c5 c10 c12 c14 c15 c16 c17 c18 c20 c25 c35 c40 c90 c100 c110 c120 c130 c140 c150 c152 c160 c170 c180 c190 c192 c200 c210 c220 c230 c240 c250 c260 c270 c280 c290 c300 c310a c310b c310c c310d c314a c314b c314c c314d c320a c320b c320c c324a c324b c324c c330 c332 c340 c350 c360 c370 c380 c390 c400 c410 c420 c430 c440 c450 c460 c490 c510a c510b c510c c510d c510e c510f c602 c604 c606 c608 c610 c612 c614 c616 c620 c640 c652 c654 c660 eof 20081201 NM 2008 12 1 K11A2008112872207 1 20070321 A 5320 STIFFENER BOEING 727 7272H3 138368N NM LT MLG WW CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 CORROSION ON BACK SIDE OF STIFFNER, (LT WHEEL WELL). 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112872208 1 20070501 A 5312 BULKHEAD BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 FWD BULKHEAD BENEATH RADOME EDGE OF STIFFNER CORRODED. 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112672214 1 20070328 A 5330 SKIN BOEING 727 7272H3 138368N NM FUSELAGE DAMAGED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 APPROX STA 328 STR 23 R SKIN DAMAGED. 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112672216 1 20070311 A 5330 LAP JOINT BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 APPROX STA 720A STR 19 R HAS CORROSION DIRECTLY BENEATH LAP SEAM. 2 L 7 3 4F RT A3WE 20081201 SO 2008 12 1 Y9PAN663P8707 1 20070807 A 2120 UNKNOWN GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU CABIN ODOR E Y9PA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 09 663P 1434 16997 CREW REPORTED SMOKE IN THE CABIN ON DESCENT INTO LGA, CREW MENTIONED THAT IT WAS EMITTING FROM THE BAGGAGE BAY AREA WITH AN ELECTRICAL SMELL. INSPECTED ACFT BAGGAGE BAY AREA BY REMOVING FLOORBOARD ACCESS PANELS, BAGGAGE BAY SIDE WALL PANEL S AT LGA WITH REPRESENTATIVE ON SITE. NO EVIDENCE OF ANY BURNING, ARCING OR ANY ELECTRICAL DEVICE HAVING FAILED IN THE B AGGAGE BAY OR ANY WHERE IN ACFT. MAINT SERVICES WHERE LIMITED IN LGA. AFTER INITIAL INSP AT LGA REVEALED NO ABNORMALITI ES, MOVED THE ACFT TO FOR FURTHER INVESTIGATION, DURING FLIGHT, THERE WAS NOT ANY SMOKE OR BURN ODOR EMITTING FROM THE ACFT. REMOVED VARIOUS BAGGAGE COMPARTMENT PANELS AND FLOOR BOARDS, PERFORMED OPS CHECKS OF ALL COMPONENTS IN BAGGAGE BA 2 L 7 2 4F 4 F RT A12EA E25NE 20081201 NM 2008 12 1 K11A2008112872205 1 20070327 A 5330 SKIN BOEING 727 7272H3 138368N NM FUSELAGE DAMAGED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 APPROX STA 1020- 1060 STR 26 R LAP SEAM HAS NUMEROUS FASTNERS W/ SKIN PILLOWING AROUND HEADS. 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112672210 1 20070321 A 5720 STIFFENER BOEING 727 7272H3 138368N NM WING CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 REAR SPAR VERTICAL STIFFNER HAS AREA OF A COOROSION. 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112672212 1 20070502 A 5330 SKIN BOEING 727 7272H3 138368N NM FUSELAGE DAMAGED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 APPROX STA 310 STR 23 R SKIN DAMAGE. 2 L 7 3 4F RT A3WE 20081201 SO 2008 12 1 Y9PAN818S83107 1 20070831 A 2611 824PT SMOKE DETECTOR GULSTM G1159 G1159A 3970109 SO RROYCE SPEY SPEY5118 54523 EU ZONE 900 MALFUNCTIONED E Y9PA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 818S 4000 2 342 1109911097 AFTER TAKEOFF, LAV SMOKE ALARM ANNUNCATOR ILLUMINATED, CREW REPORTED THAT THEY INSPECTED THE LAV AREA FOR SIGNS OF SMOKE AND FIRE, NONE OBSERVED. THE ANNUNCATOR WENT OUT AND THEN CAME BACK ON. THE CREW THEN ELECTED TO DIVERT. UPON LANDING, THE APU WOULD NOT START, ANOTHER ACFT WAS DISPATCHED TO CONTINUE TRIP WITH A WING TECH ON BOARD. THE TECH INSPECTED THE LAV AREA FOR SIGNS OF SMOKE AND/OR FIRE DAMAGE, NONE NOTICED. THE TECH THEN INSPECTED THE SMOKE DETECTOR FOR OPERATION, GROUND CHECKED NORMAL. AFTER DETERMINING THE APU PROBLEM AND DEFERRING IAW AIR CARRIER, GMM AND MEL PROCEDURES, STARTED THE ACFT WITH AN AIR START RETURN TO HOE BASE. THE TECH FOUND THAT DURING THE FLIGHT THE SMOKE DETECTOR TEST SWITCH WOU 2 L 7 2 4F 4 F A12EA E2EU 20081201 NM 2008 12 1 K11A2008112872215 1 20070425 A 5711 ATTACH ANGLE BOEING 727 7272H3 138368N NM RT WING CRACKED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 FWD SPAR ATTACH ANGLE CRACKED ( RT WING ). 2 L 7 3 4F RT A3WE 20081201 2008 12 1 K11A2008112872220 4 20070430 A 2360 STATIC WICK BOEING 727 7272H3 138368N NM RT ELEVATOR SEPARATED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 RT ELEVATOR T/E OTBD EDGE NEXT TO STATIC WICK BASE SKIN IS SEPARATING. 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112672217 1 20070322 A 5330 SKIN BOEING 727 7272H3 138368N NM FUSELAGE DAMAGED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 APPROX STA 385 25 L SKIN DAMAGE. 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112672215 1 20070426 A 5330 SKIN BOEING 727 7272H3 138368N NM FUSELAGE DAMAGED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 APPROX STA 480 STR 22 R TO 23 R HAS NUMEROUS AREAS OF SKIN DAMAGE. 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112672218 1 20070320 A 5330 SKIN BOEING 727 7272H3 138368N NM FUSELAGE DAMAGED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 APPROX STA 380 STR 17 L SKIN DAMAGE. 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112672219 1 20070310 A 5330 SKIN BOEING 727 7272H3 138368N NM FUSELAGE DAMAGED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 APPROX STA 710 STR 24 L SKIN DAMAGE. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120272201 1 20070412 A 5514 RUB STRIP BOEING 727 7272H3 138368N NM HORIZ STAB CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 RUB PADS HAVE CORROSION AROUND ADJUSTMENT SCREWS, LT HORIZONTAL STABILIZER STAB T/E 2ND AND 3RD FROM O/B ELEVATOR. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120272203 1 20070403 A 5320 STRUCTURE BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 ABOVE NR 2 ENGINE 2 INCH AREA OF CORROSION. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120272204 1 20070430 A 5514 WEB BOEING 727 7272H3 138368N NM STABILIZER CRACKED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 VERTICAL WEB HAS 4 INCH CRACK FWD OF JACKSCREW, STAB STA 32, RBL 14. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120272209 1 20070410 A 5730 SKIN BOEING 727 7272H3 138368N NM RT WING DENTED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 SEVERAL DENTS ALONG LEADING EDGE, RT WING ABOVE KRUEGER FLAPS. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120372201 1 20070501 A 5514 BEAM BOEING 727 7272H3 138368N NM HORIZ STAB CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 UPPER BEAM HAS SEVERAL AREAS OF CORROSION (RT STAB T/E). 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120372203 1 20070410 A 5730 SKIN BOEING 727 7272H3 138368N NM LT WING DENTED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 SEVERAL DENTS, LEFT WING L/E BL 70.59 - 130.59. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120372204 1 20070405 A 5330 SKIN BOEING 727 7272H3 138368N NM FUSELAGE DAMAGED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 EXTERIOR SKIN HAS AREA OF DAMAGE, 720D + 10 INCHES STRINGER 19L. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120372206 1 20070509 A 5347 SEAT TRACK BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 SEAT TRACK HAS AREAS OF CORROSION. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120372208 1 20070505 A 5347 SEAT TRACK BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 SEAT TRACK HAS AREAS OF CORROSION. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120372209 1 20070504 A 5320 TEAR STRAP BOEING 727 7272H3 138368N NM FUSELAGE DAMAGED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 TEAR STRAP DAMAGED. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120372210 1 20070605 A 5521 SPAR BOEING 727 7272H3 138368N NM ELEVATOR CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 ELEVATOR REAR SPAR CORRODED. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120372211 1 20070509 A 5751 SKIN BOEING 727 7272H3 138368N NM AILERON DAMAGED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 DAMAGED SKIN RT OUTBOARD AILERON. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120372212 1 20070520 A 5320 ANGLE BOEING 727 7272H3 138368N NM NLG WW CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 CORROSION IN THE NOSE LANDING GEAR WHEEL WELL, LT ANGLE. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120272212 1 20070508 A 5330 SKIN BOEING 727 7272H3 138368N NM FUSELAGE DENTED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 SKIN DENTED. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120272213 1 20070307 A 5330 SKIN BOEING 727 7272H3 138368N NM FUSELAGE DENTED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 SKIN DENTED. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120272214 1 20070508 A 5260 STRUCTURE BOEING 727 7272H3 138368N NM AIRSTAIRS CRACKED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 LIGHTENING HOLE CRACK, LT SIDE OF AIRSTAIRS. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120272205 1 20070430 A 5514 ANGLE BOEING 727 7272H3 138368N NM HORIZ STAB CRACKED A K11A O OTHER O OTHER UK UNKNOWN 1 GL 23 722CK 20948 ANGLE HAS 2 INCH CRACK FWD OF JACKSCREW, STAB STA 32, RBL 14. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120272206 1 20070321 A 5720 STIFFENER BOEING 727 7272H3 138368N NM RT WING CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 VERTICAL STIFFENER CORRODED WS 198. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120272207 1 20070403 A 5210 STIFFENER BOEING 727 7272H3 138368N NM L1 DOOR CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 HORIZONTAL STIFFENER CORRODED L1 DOOR 12 INCH FWD OF DOOR WINDOW. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120272208 1 20070311 A 5330 SKIN BOEING 727 7272H3 138368N NM FUSELAGE DENTED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 DENT IN SKIN, BELOW STR 19L STA 1015. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120372205 1 20070509 A 5347 SEAT TRACK BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 SEAT TRACK HAS AREAS OF CORROSION. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120372207 1 20070502 A 5347 SEAT TRACK BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 SEAT TRACK HAS AREAS OF CORROSION. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120372301 1 20070301 A 2780 SLAT BOEING 727 7272H3 138368N NM WING MALFUNCTIONED A K11A A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 23 723CK 20545 AFTER DEPARTURE AND DURING FLAP RETRACTION ^3 LED FAILED TO RETRACT AT FLAPS 2 POSITION. ATTEMPTED TO TURN OFF ENGINE H EAT AND PERFORMED ABNORMAL PROCEDURES WITH NO RESULTS. INSPECTED SLATS PER AMM 27-81-00. SLATS AND LIGHTS OP'S CHECKS OK. OK FOR SERVICE. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120272202 1 20070501 A 5320 STRUCTURE BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 BELOW AFT ENTRY DOOR SURFACE CORROSION. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120272210 1 20070410 A 5730 SKIN BOEING 727 7272H3 138368N NM LT WING DENTED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 SEVERAL DENTS ALONG LEADING EDGE, LT WING ABOVE KRUEGER FLAPS. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120272211 1 20070603 A 5330 SKIN BOEING 727 7272H3 138368N NM FUSELAGE DAMAGED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 PREVIOUSLY BLENDED AREA IN SKIN WITH QUESTIONABLE LIMITS. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120372202 1 20070410 A 5730 SKIN BOEING 727 7272H3 138368N NM RT WING DENTED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 SEVERAL DENTS, RIGHT WING L/E BL 70.59 - 130.59. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 K11A2008120272215 1 20070327 A 5330 SKIN BOEING 727 7272H3 138368N NM FUSELAGE DENTED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 FUSELAGE SKIN DAMAGED. 2 L 7 3 4F RT A3WE 2007101900226 20071019 00226 EA 2007 10 19 MASA200700665 1 20071004 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT OUT OF ADJUST A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 17337 7337 ASH 9702 OKC-PHX. FREQUENT LEFT OVERWING EMERGENCY EXIT CAUTION MESSAGE IN FLIGHT. ADJUSTED PROX SENSOR. 2 L 7 2 4F RT A21EA 20081027 NM 2008 10 27 DLM88081371 1 20070123 A 7160 INLET DOUG MD88 MD88 3023688 NM ENGINE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DL 49543 DURING SHOP VISIT EROSION AND DAMAGE FOUND TO INLET COWL OUTER COMPOSITE SKIN. REPAIRED PER ERA 095803-14. 2 L 7 2 4F RT A6WE 2007082900052 20070829 00052 NM 2007 8 29 ASAA0771960 1 20070814 A 5754 SKIN BOEING 737 737790 13844CN NM L/E SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 NR 4 SLAT LOWER SIDE T/E CHAFED. REPAIRED IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 20080808 EU 2008 8 8 M7K2008F00133 1 20070917 A 8000 975UN01B4AA5 SWITCH UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ENGINE START INTERMITTENT E M7KA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 19 807MH 2639 3912 23130 PILOT REPORTED THAT SEVERAL SELECTIONS TO THE ENGINE START POSITION WERE REQUIRED TO GET THE ENGINE TO START. UPON CLOS ER INSP IT WAS DETERMINED THAT SELECTING THE ON OR START POSITION GENTLY WITHOUT SNAPPING THE LEVER INTO THE START POSIT ION COULD CAUSE THE MALFUNCTION. NO FAULT CODE WAS GENERATED. IT THOUGHT THAT DUE TO THE NR OF CONTACTS WITHIN THE SWI TCH AND THE RATE OF FADEC INTERROGATION BEING 20 TIMES PER SECOND ANY CONTACTS WITH ARCING SURFACES MAY NOT BE PASSING C URRENT QUICKLY ENOUGH IF SELECTED SLOWLY TO THE START POSITION. REPLACED 8 SUCH SWITCHES IN 50,000 FLIGHT HOURS. MOST SWITCH PROBLEMS BUT NOT ALL HAVE GENERATED A FAULT CODE INDICATING A PROBLEM WITH THE SWITCH ON THE AC VEMD REQUIRING R 1 G 7 2 3U 3 U H9EU E00054EN 20080808 EU 2008 8 8 M7K2008F00106 1 20071105 A 6700 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE COLLECTIVE CRACKED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 824MH 51 4173 23350 AMBER GOVERNOR LIGHT ILLUMINATED IN FLIGHT AND A FAULT CODE GENERATED INDICATING FAULT WITH COLLECTIVE LEVER VALUES BEIN G PROVIDED BY THE POTENTIOMETER. NEW POTENTIOMETER INSTALLED WITH NO FURTHER DEFECT NOTED. SUGGEST DIFFERENT MFG OR DE SIGN BE CONSIDERED AS THIS IS A REPEATED DEFECT THAT AFFECTS AC DISPATCH RELIABILITY. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080808 EU 2008 8 8 M7K2008F00112 1 20070919 A 6700 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE COLLECTIVE INTERMITTENT E M7KA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 19 816MH 419 4038 23237 THIS PART IS THE POSITION INDICATOR FOR BOTH COLLECTIVE AND TAIL ROTOR FADEC CONTROL ACTIONS. IT ALMOST NEVER FAILS TOT ALLY BUT GENERATES A FAILURE CODE THAT REQUIRES THEY BE REPLACED. THESE PARTS CAN LAST THOUSANDS OF HOURS OR LESS THAN FIFTY. ONLY RECENTLY DID THE AIRCRAFT MFG MAKE THIS A TIME CHANGE ITEM AND UP TO THAT POINT THEY VERY RARELY HAD A PROB LEM. DUE TO THE WEEKLY FAILURE OF ONE OF THESE POTENTIOMETERS IN OUR FLEET WHICH WE NEVER EXPERIENCED BEFORE REPLACING THE ORIGINAL PARTS ON OUR OLDER AC AND THE FACT THAT AC DELIVERED ABOUT THE SAME TIME AS THE NEW REPLACEMENT PARTS WERE BEING INSTALLED IN OUR FLEET BEGAN HAVING RELIABILITY PROBLEMS WE ARE SURE THAT A QC ISSUE EXISTS. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080808 EU 2008 8 8 M7K2008F00114 1 20070919 A 6700 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE COLLECTIVE INTERMITTENT E M7KA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 19 804MH 705 3750 23058 THIS PART IS THE POSITION INDICATOR FOR BOTH COLLECTIVE AND TAIL ROTOR FADEC CONTROL ACTIONS. IT ALMOST NEVER FAILS TOT ALLY BUT GENERATES A FAILURE CODE THAT REQUIRES THEY BE REPLACED. THESE PARTS CAN LAST THOUSANDS OF HOURS OR LESS THAN FIFTY. ONLY RECENTLY DID THE AIRCRAFT MFG MAKE THIS A TIME CHANGE ITEM AND UP TO THAT POINT THEY VERY RARELY HAD A PROB LEM. DUE TO THE WEEKLY FAILURE OF ONE OF THESE POTENTIOMETERS IN OUR FLEET WHICH WE NEVER EXPERIENCED BEFORE REPLACING THE ORIGINAL PARTS ON OUR OLDER AC AND THE FACT THAT AC DELIVERED ABOUT THE SAME TIME AS THE NEW REPLACEMENT PARTS WERE BEING INSTALLED IN OUR FLEET BEGAN HAVING RELIABILITY PROBLEMS WE ARE SURE THAT A QC ISSUE EXISTS. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00113 1 20070919 A 6700 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE COLLECTIVE INTERMITTENT E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 813MH 54 3967 23183 THIS PART IS THE POSITION INDICATOR FOR BOTH COLLECTIVE AND TAIL ROTOR FADEC CONTROL ACTIONS. IT ALMOST NEVER FAILS TOT ALLY BUT GENERATES A FAILURE CODE THAT REQUIRES THEY BE REPLACED. THESE PARTS CAN LAST THOUSANDS OF HOURS OR LESS THAN FIFTY. ONLY RECENTLY DID THE AIRCRAFT MFG MAKE THIS A TIME CHANGE ITEM AND UP TO THAT POINT THEY VERY RARELY HAD A PROB LEM. DUE TO THE WEEKLY FAILURE OF ONE OF THESE POTENTIOMETERS IN OUR FLEET WHICH WE NEVER EXPERIENCED BEFORE REPLACING THE ORIGINAL PARTS ON OUR OLDER AC AND THE FACT THAT AC DELIVERED ABOUT THE SAME TIME AS THE NEW REPLACEMENT PARTS WERE BEING INSTALLED IN OUR FLEET BEGAN HAVING RELIABILITY PROBLEMS WE ARE SURE THAT A QC ISSUE EXISTS. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 NE 2008 8 11 M7K2008F00053 2 20070919 A 7230 70BM022010 BEARING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE IMPELLER SEIZED E M7KA E ENGINE SHUTDOWN J WARNING INDICATION HO HOVERING 1 WP 19 804MH 3750 23069 PILOT WAS IN A HOVER TAXI WHEN AN UNUSUAL HIGH FREQUENCY VIBRATION WAS FELT IN THE AC AND PARTIAL POWER LOSS BECAME APPA RENT AND AC WAS LANDED WITH A CHIP LIGHT ILLUMINATING WITHIN SECONDS OF GROUND CONTACT AND ENGINE WAS SHUTDOWN. A VERY R APID DECAY OF NG SPEED WAS NOTED. EXAMINATION OF ENGINE REVEALED THAT COMPRESSOR WAS LOCKED UP AND WHEN VIEWING INTO TH E BLEEDVALVE SCREEN THE CENTRIFUGAL IMPELLER SHROUD HAD BEEN PENETRATED BY THE IMPELLER AND SOME SMALL PIECES HAD BEEN E JECTED FROM THE BLEED VALVE PORT AND WERE ON THE ENGINE DECK. MODULE 1 AND THE ENGINE ELECTRICAL CHIP DETECTOR PLUGS HA D A GENEROUS AMOUNT OF METAL ON THEM. A PREVIOUS LIKE FAILURE HAD BEEN DETERMINED TO BE THE BEARING JUST FWD OF THE CEN 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00138 1 20071030 A 6200 350A31202304 COVER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE MAIN ROTOR CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 812MH 3956 23179 THIS PART WAS FOUND CRACKED DURING ROUTINE INSPECTION. THE CRACK ALWAYS OCCURS IN THE RADIUS OF THE LOWER IB CORNER FLA NGE ALMOST ALL OF THESE SPRING COVERS WILL REQUIRE REPLACEMENT MULTIPLE TIMES WITHIN THE FIRST FEW THOUSAND FLIGHT HOU RS OF THE AIRCRAFT. THE MFG HAS BEEN ASKED TO CHANGE THE DESIGN OR MATERIAL TO CORRECT THIS REPETITIVE CRACK PROBLEM BU T NO ACTION OTHER THAN MAKING THE PART PROCURABLE AS A SUBASSEMBLY OF THE AVA LOWER FLANGE ASSY HAD BEEN TAKEN BY THE MF G. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00057 1 20071030 A 5302 350A25040501 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAILBOOM FAILED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 808MH 3914 23072 PART FOUND CRACKED DURING ROUTINE INSPECTION IAW AD2004-01-14, REQUIREMENTS AT THE 110 HOUR INTERVAL INSPECTION. A NEW PART OF THE OLD PN WAS INSTALLED. SUGGEST MFG MAKE AVAILABLE THE NEW PN IMPROVED FITTINGS THAT DO NOT HAVE THE AD REQUIR EMENT TO AL EC 130B4 OPERATORS AS SOON AS POSSIBLE. THE PRODUCTION OF THESE PARTS TO DATE HAS ONLY MET THE NEEDS OF THE AC ASSY LINES. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00105 1 20071105 A 6700 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE COLLECTIVE DEFECTIVE E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 824MH 13 4173 23350 AMBER GOVERNOR LIGHT ILLUMINATED IN FLIGHT AND A FAULT CODE GENERATED INDICATING FAULT WITH COLLECTIVE LEVER VALUES BEIN G PROVIDED BY THE POTENTIOMETER. NEW POTENTIOMETER INSTALLED WITH NO FURTHER DEFECT NOTED. SUGGEST DIFFERENT MFG OR DE SIGN BE CONSIDERED AS THIS IS A REPEATED DEFECT THAT AFFECTS AC DISPATCH RELIABILITY. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00050 1 20070919 A 5302 350A234222220 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAILBOOM CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 803MH 4926 3735 23036 FITTING FOUND CRACKED DURING POST FLIGHT INSP. A NEW FITTING MATCH DRILLED AND INSTALLED. THIS IS A COMMON DEFECT FOR THIS PART AND OCCURS MULTIPLE TIMES ON SOME AC AND NEVER ON OTHERS FOR REASONS UNKNOWN. SOME SHIMMING IS SOMETIMES REQU IRED AND IF DONE POORLY THIS MAY AGGRAVATE THE CRACK DEVELOPMENT. SUGGEST THE PART DESIGN IS SUFFICIENT BUT A CHANGE OF MATERIAL TO A STRONGER METAL SUCH AS SS INSTEAD OF ALUMINUM ALLOY IS REQUIRED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 NE 2008 8 11 M7K2008F00118 2 20070917 A 7320 9560170620 SEAL UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE HMU LEAKING E M7KA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 19 801MH 471 ANR746B 3654 23077 SEAL FOUND LEAKING FUEL OVERBOARD WITH FUEL BOOST PUMP PRESSURE APPLIED. FOLLOWING STARTUP AND SHUTDOWN OF THE FUEL BOO ST PUMP FUEL LEAK SLOWED BUT CONTINUED AND WAS BEYOND ALLOWABLE LIMITS OF THE MM. THIS IS A VERY COMMON PROBLEM WITH AL MOST ALL CONTROLS REQUIRING SEAL REPLACEMENT TYPICALLY AROUND 500 HOURS IN SERVICE AND OFTEN EARLIER. THIS IS AGGRAVATE D BY THE FAILURE OF PILOTS TO USE THEIR CHECKLIST AND ENSURE THAT THE FUEL BOOST PUMP IS ON AND SUPPLYING LUBRICATION TO THE SEAL WHENEVER THE ENGINE IS ROTATING. IN 50,000 HOURS OF FLIGHT OPS, WE HAVE AVERAGED A SEAL EVERY 1,000 HOURS. C URRENTLY HAVE BEEN OPERATING WITH THE LATEST SEAL VERSION, TU133A, THAT TO DATE WITH 4500 HOURS SERVICE IN 8 CONTROLS, H 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00146 1 20071105 A 5610 WINDSCREEN UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE CANOPY DAMAGED E M7KA A UNSCHED LANDING C F.O.D. NR NOT REPORTED 1 WP 19 808MH 2893 3914 23072 ACFT STRUCK BIRD WITH LOSS OF PILOTS AND CENTER WINDSCREENS. ACFT LANDED AT FIRST PRACTICAL LANDING SPOT. A MAJOR REPA IR OF LT CANOPY FRAME AND LT CENTER FRAME HAS BEEN COMPLETED BY MFG SUBSIDIARY. PILOTS WINDSCREEN FOUND INADEQUATE TO P REVENT BIRDS PENETRATION. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00140 1 20071010 A 6700 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE COLLECTIVE FAILED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 805MH 428 3799 23091 A FAULT CODE WAS GENERATED AT ENGINE SHUTDOWN INDICATING A DEFECT WITH THE COLLECTIVE POTENTIOMETER. A NEW POTENTIOMETE R WAS INSTALLED. THIS HAS BECOME A VERY COMMON PROBLEM WITH THE LATEST REPLACEMENT PART THAT THEY LAST MUCH LESS THAN T HE 2000 HOUR SERVICE LIFE LIMIT. THE SAME POTENTIOMETERS ORIGINALLY INSTALLED LASTED AS LONG AS 4000 HOURS WITHOUT FAIL ING. SHORTLY AFT THE REQUIREMENT TO REPLACE THESE PART AT A 2000 HOUR INTERVAL IT SEEMS THAT THE QUALITY OF THESE PARTS DRAMATICALLY DECREASED. ENGINE ANTICIPATOR CONTROL CIRCUIT SIGNAL OF COLLECTIVE POSITION IS GENERATED BY THIS POTENTIO METER TO CONTROL DECU SIGNAL TO THE ENGINE. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00051 1 20070919 A 5302 350A234222221 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAILBOOM CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 805MH 2464 3799 23091 FITTING FOUND CRACKED DURING POST FLIGHT INSP. A NEW FITTING MATCH DRILLED AND INSTALLED. THIS IS A COMMON DEFECT FOR THIS PART AND OCCURS MULTIPLE TIMES ON SOME AC AND NEVER ON OTHERS FOR REASONS UNKNOWN. SOME SHIMMING IS SOMETIMES REQU IRED AND IF DONE POORLY THIS MAY AGGRAVATE THE CRACK DEVELOPMENT. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00056 1 20071030 A 3340 6485000 LIGHT UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ANTI COLLISION INOPERATIVE E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 808MH 3091 3914 23209 STROBE FLASH BECAME WEAKER AS THE DAYS PASSED UNTIL UNIT WOULD NO LONGER PASS STROBE INTENSITY REQUIREMENTS AND WAS REPL ACED IAW A FIELD APPROVED 337BY THE INSTALLATION OF A WHEEL FLASHING LED ANTI COLLISION LIGHT ASSEMBLY AND ADAPTER BRACK ET. THESE MONOBLOCK ANTI COLLISION LIGHT ASSY HAVE NOT HAD PREDICTABLE LIFE EXPECTANCIES AND ARE NOT REPAIRABLE. THEY A RE ALSO THREE TIMES MORE EXPENSIVE THAN THE LED REPLACEMENTS. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00134 1 20070919 A 2435 350A54112420 BRACKET UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE STARTER GEN CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 823MH 498 4158 23336 FOUND CRACKED DURING AIRFRAME 100/200/500 HOUR INSPECTION, BRACKET SUPPORTS, AIR INLET COOLING DUCT WHICH IS SUBJECT TO RAM AIR AND LIKELY VIBRATES CAUSING METAL OF BRACKET TO COLD WORK. THIS IS A COMMON PROBLEM WHICH OCCURS EVERY 200-300 HOURS FOR THIS COMPONENT. SUGGEST MFG IMPROVE STRENGTH AND INTEGRITY OF COMPONENT. USE SS INSTEAD OF ALUMINUM. (K) 1 G 7 2 3U 3 U H9EU E00054EN 2007071300176 20070713 00176 SO 2007 7 13 SWIA200718449 1 20070323 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 569SW 120344 LEFT WING NR 2 FUEL PANEL FORWARD STRINGER IS CRACKED, DISCOVERED AT C-CHECK. REPAIRED STRINGER IAW SRM 120 57-20-03, F IG 202, PG 206 TO 211. 2 L 7 2 4T RT A31SO 2008010200014 20080102 00014 EA 2008 1 2 COMA0770077 1 20071208 A 3250 STEERING SYS CNDAIR CL600 CL6002C10 1390015 EA NLG MALFUNCTIONED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 398CA 10112 FLIGHT 5250 - NOSE WHEEL STEERING INOP. PERFORMED RESET OF NWS SYSTEM. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008010200016 20080102 00016 EA 2008 1 2 COMA0770079 1 20071213 A 5320 CC670341757 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 374CA 10090 FS 280 BULKHEAD RIGHT WEB AND FLOOR SUPPORT CROSSBEAM ARE CORRODED. REPLACED THE RIGHT WEB AND CROSSBEAM IAW SRM 51-42- 21, 51-42-06 AND REO 670-53-047. 2 L 7 2 4F RT A21EA 2008010200017 20080102 00017 EA 2008 1 2 COMA0770080 1 20071213 A 5210 SH670318257 ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CORRODED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 374CA 11711 10090 PASSENGER DOOR LOWER MID CAP ANGLE EXTRUSION CORRODED BEYOND LIMITS. REPLACED THE MID CAP ANGLE IAW SRM 51-40-00 AND 51 -42-06. 2 L 7 2 4F RT A21EA 2008010200021 20080102 00021 NM 2008 1 2 ASAA0752385 1 20071212 A 5755 113A46003 SKIN BOEING 737 737890 1384527 NM SPOILER PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 558AS 35177 LEFT WING NR 6 SPOILER PUNCTURED AT LOWER SURFACE APPROX WBL 96. REPAIRED IAW B737 800 SRM 51-70-10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008010200025 20080102 00025 EA 2008 1 2 COMA0760699 1 20071208 A 3397 64641 CABLE CNDAIR CL600 CL6002B19 1900309 EA CABIN FAULTY A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 931CA 7037 CABIN EMERGENCY FLOOR LIGHTS AT ROWS 9 THROUGH 12 INOP. REMOVED AND REPLACED CABLE ASSY AT ROW 12. 2 L 7 2 4F RT A21EA 2008010200041 20080102 00041 EA 2008 1 2 COMA0760712 1 20071212 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 916CA 17421 7014 RECEIVED NOSE GEAR DISAGREE MESSAGE AFTER TAKEOFF. DECLARED EMERGENCY, RETURNED TO GSO, LANDED WITHOUT INCIDENT. REPLA CED NLG PRIORITY VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008010200047 20080102 00047 EA 2008 1 2 COMA0760718 1 20071213 A 5311 6003603024 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 779CA 7670 BAGGAGE CART STRUCK AIRCRAFT JUST AFT OF APU EXHAUST. REPLACED FRAME SECTION 718 PER SRM 51-42-06 AND SRM 51-42-20. 2 L 7 2 4F RT A21EA 2008010200066 20080102 00066 NM 2008 1 2 SWAA076338 1 20071218 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 485WN 32473 DURING SCHEDULED HC1 CHECK, MID CABIN EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008010200074 20080102 00074 NM 2008 1 2 SWAA076343 1 20071218 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008010200091 20080102 00091 NM 2008 1 2 SWAA076365 1 20071219 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1001, STR 5R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008010200092 20080102 00092 2008 1 2 SWAA076366 4 20071219 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008010200095 20080102 00095 NM 2008 1 2 SWAA076369 1 20071219 A 5512 65C27494 SKIN BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS 131. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008010200096 20080102 00096 NM 2008 1 2 SWAA076370 1 20071219 A 5755 6573735 SKIN BOEING 737 7373H4 1384600 NM NR 6 SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED BRDG CHECK, FOUND RT WING NR 6 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2008010200098 20080102 00098 NM 2008 1 2 SWAA076372 1 20071219 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2008010200112 20080102 00112 NM 2008 1 2 SWAA076399 1 20071220 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 18R CORRODED AT BS 326. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008010200113 20080102 00113 NM 2008 1 2 SWAA076403 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200120 20080102 00120 NM 2008 1 2 SWAA076404 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200126 20080102 00126 NM 2008 1 2 SWAA076427 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200128 20080102 00128 NM 2008 1 2 SWAA076428 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200138 20080102 00138 NM 2008 1 2 SWAA076415 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200140 20080102 00140 NM 2008 1 2 SWAA076417 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200141 20080102 00141 NM 2008 1 2 SWAA076418 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200160 20080102 00160 NM 2008 1 2 ASAA0772396 1 20071207 A 5315 141A550519 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 PASSENGER COMP FLOORBEAM BS 344 RBL 4 TO LBL 56 CORRODED. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008010200161 20080102 00161 NM 2008 1 2 ASAA0772398 1 20071208 A 5315 147A55048 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CABIN FLOORBEAM BS 947 LBL 53 CORRODED. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008010200165 20080102 00165 NM 2008 1 2 ASAA0772399 1 20071210 A 5320 143A52404 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 INTERCOSTAL CRACKED ABOVE CTR WING BOX AT STA 540 RBL 2 WL 208. REPLACED WITH MADE REPAIR PART PER BAC BNG DWG 143 A 52 40 & B737 700 SRM 51-40-05 & 51-40-02. 2 L 7 2 4F RT A16WE 2008010200166 20080102 00166 NM 2008 1 2 ASAA0772400 1 20071205 A 5321 453A261015 FLOORBOARD BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT FLOORBOARD BS 727+4 TO 727D CORRODED ON EDGES. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008010200190 20080102 00190 EA 2008 1 2 A6WA200740679 1 20071212 A 3246 WHEEL CNDAIR CL600 CL6002B19 1900309 EA NLG BENT A A6WA O OTHER C F.O.D. TO TAKEOFF 1 GL 31 406AW 7402 RIGHT NOSE WHEEL RIM BENT. REMOVED AND REPLACED RIGHT AND LEFT NOSE LANDING GEAR TIRE ASSEMBLIES IAW AMM 32-40. NLG WH EEL ASSY LT P/N 5010598 S/N AUG99-2288 TSN 6672 CSN 6269, AND NLG WHEEL ASSY RT P/N 5010598 S/N APR03-4829 TSN 4436 CSN 4228. (M) 2 L 7 2 4F RT A21EA 2008010200191 20080102 00191 EA 2008 1 2 A6WA200740669 1 20071129 A 5210 SUPPORT CHANNEL CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 433AW 7289 FOUND CARGO DOOR FORWARD TRACK LOWER SUPPORT CHANNEL P/N 601R35050-25 FOUND CRACK APPROX .500 LONG 1 EACH. (M) CARGO D OOR FWD TRACK, LOWER SUPPORT CHANNEL. FABRICATED IAW SRM 51-24-16, CRACKED SUPPORT CHANNEL REMOVED IAW SRM 51-42-06, FA BRICATED SUPPORT CHANNEL INSTALLED IAW SRM 51-42-06. (K) 2 L 7 2 4F RT A21EA 2008010300004 20080103 00004 NM 2008 1 3 DHLA200700082 1 20071214 A 5753 STRUCTURE BOEING 727 727224 1384076 NM RT WING FLAP DAMAGED A DHLA O OTHER O OTHER CR CRUISE 1 GL 05 746DH BN259 22252 FLT 520, RT WING INBOARD FORE FLAP DAMAGED. REMOVED AND REPLACED RT INBD FORE FLAP. OP CK GOOD. IAW AMM 27-51-01. AIRCR AFT WAS GROUNDED 2 L 7 3 4F A3WE 2008010300006 20080103 00006 2008 1 3 DXTA200702682 4 20071215 A 2210 7003897907 CONTROLLER CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE COCKPIT INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 664QS 5357 5605264 AUTOPILOT INOP AMBER TURN KNOB INDICATION ON PFD'S. TURN KNOB WAS IN THE CENTER POSITION. POSITION. REMOVED AUTOPILOT C ONTROLLER & INSTALLED SERVICEABLE AUTOPILOT CONTROLLER REMOVED FROM A/C 560XL-5176 N876QS FOR CONTINUED SERVICE ON 560-5 264 N664QS AUTO PILOT CONTROLLER CHECKS GOOD IAW CESSNA 560XL MM 22-11-03. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008010300007 20080103 00007 NM 2008 1 3 DXTA200702677 1 20071214 A 3250 2880000000 CONTROL VALVE GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE NLG STEERING BYPASSING E DXTA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 07 718QS 1399 136 AC PULLS RT WITH NEUTRAL TILLER POSITION. NWS DISENGAGES WHEN ATTEMPTING FULL RT TURN. REMOVED AND REPLACED NOSEWHEEL S TEERING CONTROL VALVE. AND ADJUSTED FEEDBACK MANIFOLD POTENTIOMETERS 1 AND 2 IAW GAC G200 AMM 32-50-00 AND 32-50-15. 2 L 7 2 4F 4 F RT A53NM E35NE 2008010300008 20080103 00008 CE 2008 1 3 DXTA200702678 1 20071214 A 3260 WARNING SYSTEM BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE MLG FALSE ACTIVATION E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 154QS RK509 RED LIGHTS IN GEAR HANDLE REMAINED ILLUMINATED AFTER GEAR RETRACTION. UPON EXTENTION THE RED LIGHTS WENT OUT AND (3) GRE ENS ILLUMINATED. JACKED AC VISUALLY INSPECTED LANDING GEAR UPLOCK AND DOWN LOCK SWITCHES. VISUALLY INSPECTED MLG DOOR S WITCHES. NO DEFECTS NOTED TO ANY OF THE SWITCHES. CYCLED GEAR 10X'S WITHOUT DEFECTS. VERIFIED THAT RED GEAR HANDLE LIGHT DOES EXTINGUISH WHEN GEAR IS UP AND LOCK AND DOWN LOCKED. PERFORMED 10 MORE GEAR CYCLES WITHOUT DEFECTS. ALL WORK IAW 4 00XP M/M 32-30-00. 2 H 7 2 4F 4 F RT A16SW E25EA 2008010300009 20080103 00009 CE 2008 1 3 DXTA200702679 1 20071214 A 5210 LATCH CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE PAX DOOR BINDING E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 603QS 5605203 CABIN DOOR WARINING LIGHT CAME ON IN FLIGHT. FOUND CABIN DOOR UPPER AFT LATCH BINDING. ADJUSTED UPPER AFT LATCH AS NEED ED TO FREE UP PIN TO CONTACT DOOR LATCH SWITCH. OPS CHECKED GOOD. ALL WORK COMPLETED I/A/W CESSNA 560XL MM 52-10-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008010300010 20080103 00010 CE 2008 1 3 DXTA200702680 1 20071214 A 5210 MS3548941 GROMMET CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE DOOR SEAL WORN E DXTA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 332QS 7566 5600523 FL410 AT CRUISE, SOUND OF SIGNIFICATE AMOUNT OF AIR PASSING THRU MAIN CABIN DOOR.CABIN PRESSURE MAINTAINED. ADJUSTED DO OR FRAME SOCKETS AS REQUIRED DUE TO DOOR SEAL CLEARANCE GAPS AND REPLACED DOOR SEAL GRUMMET WITH NEW GROMMET DUE TO WEAR IAW THE 560 MM CHAPTER 52-10-01. PERFORMED CABIN ENTRANCE DOOR SECONDARY, SEAL OPS TEST IAW 560 MM CHAPTER 21-30-00. O PS AND LEAK TEST NORMAL. 2 L 7 2 4F 4 F RT A22CE E25EA 2008010300011 20080103 00011 EU 2008 1 3 07FDEA05057 1 20071214 A 3230 224TS05Y CONTROL LEVER AIRBUS 310 A310203 3930313 EU MLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 408FE 257 GEAR LEVER WOULD NOT RETRACT PAST NEUTRAL POSITION IN SYS NR 1 OR SYS NR 2 INTERROGATED PROX BOX FOUND FAULT CODES 64 A ND 60 INSTALLED TEST BOX IN A/C. REMOVED PROX BOX AND NOSE GEAR SWITCHES FOR TEST BOX HARNESS. TESTED SYSTEM PER MM TO GEAR MODULE STILL DID NOT TEST. INSTALL NEW MODULE IN A/C STILL FAILED TEST REINSTALLED ORIGINAL GEAR MODULE. A/C TES T BOX AND HARNESS STILL INSTALL TROUBLESHOT AND CONFIRMED L/G CTL LEVER 2GA FAULTY. REMOVED AND REPLACED SAME PER A310- 200 AMM 32-31-11- 4, ALSO AS PRECAUTION REMOVED AND REPLACED LANDING GEAR POSITION SYS 1 SYS 2 SWITCH 10GA PER SWP. SYS TEM OPS CHECKED OK PER AMM 32-31-11-4. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2008010300012 20080103 00012 EU 2008 1 3 07FDEA05058 1 20071214 A 3210 C6646120 PIN AIRBUS 300 A300F4605R 3930327 EU MLG SHEARED A FDEA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SO 25 650FE 726 BOLT/PIN BROKEN ON RT MLG AT DRAG LINK/MAIN STRUT ASSY, ATTACH'S SUPPORT ASSY FOR DOWN LOCK SENSORS. REMAINDER OF SHEAR ED OFF PIN EXTRACTED FROM GEAR ASSY BY LAX MACHINE SHOP EMP'S NR 213560/519905. REPLACED BOLT FOR RT MAIN GEAR TORQUE L INK DOWN LOCK SENSOR SUPPORT BRACKET, REF MM32-11-27-4. PER ENGINEERING REMOVED TORQUE LINK ASSEMBLY AT CENTER SCISSORS ATTACHMENT POINT, FOUND NO BINDING. LUBED ALL FITTINGS ON TORQUE LINK ASSEMBLY. REINSTALLED BOLT, COMPLETED INSTALLAT ION OF TORQUE LINKS WITH AOG LOCKING WASHER AND TORQUED TO SPECS AS PER M/M 32-11-27-4. NOTE, THIS A/C DIVERTED TO LAX BECAUSE OF MULTIPLE SYSTEMS FAILURE. 2 L 7 2 4F RT A35EU 2008010400013 20080104 00013 EA 2008 1 4 TRAX200701939 1 20071215 A 3620 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA BLEED AIR SYS ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 877AS 7579 ANTI ICE DUCT WARNING MSG, C/W QRH, LT FUSELAGE SIDE, EN ROUTE TO MDT A/C DIVERTED TO GSP DUE TO MTC. EMERGENCY DECLARE D, EMERGENCY EQUIPMENT ON STANDBY, FLT 4408 CX. 2 L 7 2 4F RT A21EA 2008010400019 20080104 00019 SO 2008 1 4 C2XA07SH110 1 20071220 A 5320 14525480603 FITTING EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13118 145675 SHV - DURING C-CHECK, MAINTENANCE FOUND AT FRAME 65 SHEAR CLIP WITH CORROSION AT CARGO DOOR CUT OUT LOWER BEAM. MAINTEN ANCE REPAIRED FRAME 65 SHEAR CLIP AT CARGO DOOR CUTOUT LOWER BEAM IAW EC5330-01458. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2008010400043 20080104 00043 SO 2008 1 4 C2XA07TY082 1 20071214 A 5330 SKIN EMB 145 EMB145XR 3260214 SO FUSELAGE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11121 145683 THE REAR FUSELAGE LOWER SKINS AND ADJACENT STRUCTURE OF FRAME 66 WERE DAMAGED. MAINTENANCE INDUCED. REPLACED TWO SKIN PANELS AND SEVERAL SHEAR CLIPS AT FRAME 66 AND REPAIRED SEVERAL DENTS ON THE SKIN JUST FORWARD OF FRAME 66. REPAIRED IA W EA5330-01109. AIRCRAFT STILL IN C CHECK. 2 L 7 2 4F RT 2008010400049 20080104 00049 SO 2008 1 4 C2XA07SH104 1 20071215 A 5751 14574000405 SHROUD EMB 145 EMB145XR 3260214 SO LT AILERON DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18120 145681 SHV DURING C-CHECK, LT UPPER AILERON SHROUD HAS COMPOSITE DAMAGE. MAINTENANCE REPAIRED LT AILERON SHROUD IAW EC5750-01 315. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008010400051 20080104 00051 SO 2008 1 4 C2XA07SH103 1 20071215 A 5700 ACCESS PANEL EMB 145 EMB145XR 3260214 SO DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18120 145681 RT PNL 191FR HAS COMPOSITE DAMAGE AT SCREW HOLES. MAINTENANCE REPAIRED RT PNL 191 FR IAW EC5750-01315. THE AIRCRAFT WA S APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008010400057 20080104 00057 CE 2008 1 4 DXTA200702691 1 20071219 A 3240 BRAKE ASSY CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG MALFUNCTIONED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 634QS 5605558 CO-PILOTS RT BRAKE FADES TO STOP AND WILL NOT HOLD . TAXIED AIRCRAFT AROUND RAMP AND PERFORMED SEVERAL BRAKE CHECKS USI NG PILOT'S AND CO-PILOT'S BRAKES WITH NO DEFECTS NOTED. MADE SEVERAL TURNS USING AIRCRAFT RUDDER PEDALS ONLY WITH NO DEF ECTS BEING NOTED. INSPECTED BRAKE SYSTEM FOR LEAKS, WEAR AND DAMAGE AND FOUND NO DEFECTS AT THIS TIME, NO DEFECTS ARE NO TED WITH THE BRAKE SYSTEM. ALL WORK PERFORMED IAW CESSNA CITATION 560XLS AMM CH 32-40-01. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008010400058 20080104 00058 CE 2008 1 4 DXTA200702693 1 20071219 A 2930 99121943 CHECK VALVE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE AFT SERVICE BAY BYPASSING E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 679QS 1107 5605279 (LO HYD FLOW RT) ANNUNCIATOR ILLUMINATED ON TAKEOFF ROLL AT 40 KNOTS. NO SECONDARY INDICATIONS. ABORTED TAKEOFF. REMOVE D AND REPLACED R/H LO HYD. FLOW CHECK VALVE WITH A NEW UNIT. PERFORMED OPS TEST. CHECKED SATISFACTORY NO LEAKS NOTED. I .AW. CE-560XL M.M. CHAPTER 29-11-04. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008010400059 20080104 00059 SO 2008 1 4 C2XA07CL106 1 20071224 A 3397 CONNECTOR EMB 145 EMB145XR 3260214 SO DOOR LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 26141 145733 DURING ROUTINE MAINTENANCE, THE EMERGENCY LIGHT ON THE MAIN CABIN DOOR WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND RESECURED THE CONNECTOR ON THE MAIN CABIN DOOR EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2008010400073 20080104 00073 NM 2008 1 4 CALA0700766 1 20071218 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17619 27332 FUSELAGE FRAME IS CRACKED AT STA 867 BETWEEN STRINGERS 8R AND 9R REPAIRED PER ECRA 5310-04684. 2 L 7 2 4F RT A16WE 2008010400078 20080104 00078 NM 2008 1 4 CALA0700770 1 20071218 A 5311 6546560 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17619 27332 FUSELAGE FRAME IS CRACKED AT STA 747 BETWEEN STRINGERS 8L AND 9L. REPAIRED PER ECRA 5310-04684. 2 L 7 2 4F RT A16WE 2008010400080 20080104 00080 NM 2008 1 4 CALA0700771 1 20071218 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17619 27332 FUSELAGE FRAME IS CRACKED STATION 867 BETWEEN STRINGERS 8L AND 9L. REPAIRED PER ECRA 5310-04684. 2 L 7 2 4F RT A16WE 2008010400081 20080104 00081 NM 2008 1 4 CALA0700772 1 20071218 A 5311 6546596 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17619 27332 FUSELAGE FRAME IS CRACKED STA 727B BETWEEN STRINGERS 8R AND 9R. REPAIRED PER ECRA 5310-04684. 2 L 7 2 4F RT A16WE 2008010400088 20080104 00088 NM 2008 1 4 CALA0700750 1 20071210 A 5311 6546550 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 FUSELAGE FRAME CRACKED STA 787 B/W STR 8/9. REPAIRED PER EA5310-04498. 2 L 7 2 4F RT A16WE 2008010400091 20080104 00091 NM 2008 1 4 CALA0700753 1 20071210 A 5311 6546525 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 FUSELAGE FRAME CRACKED STA380 B/W STR 8/9 RT. REPAIRED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2008010400105 20080104 00105 SO 2008 1 4 CHQA200700096 1 20071212 A 3297 14521495403 WIRE HARNESS EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NLG DEFECTIVE A CHQA L ABORTED APPROACH J WARNING INDICATION DE DESCENT 1 GL 11 291SK 145486 CAE312631 CLE TO LGA - DURING DESCENT, THE CREW RECEIVED "LG AIR/GND FAIL" INTERMITTENTLY SEVERAL TIMES. THE CREW FOLLOWED THE QR H AND LANDED WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE CMC FOR FAULT CODES AND FOUND MESSAGES FOR A NOSE WOW FAIL. MAINTENANCE THEN REPLACED THE NOSE LANDING GEAR WOW PROX SWITCH HARNESS AND PERFORMED SEVERAL GEAR SWINGS WITH NO FURT HER DEFECTS NOTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008010400110 20080104 00110 NM 2008 1 4 DL764071626 1 20071216 A 3350 BATTERY PACK BOEING 767 767432ER 1385134 NM CABIN DEFECTIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 826MH 29697 EMERGENCY LIGHT BATTERY PACK ROW 24 LEFT IS DEFECTIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW B767-400 A MM 33-51-07. NO FAULTS NOTED ON OPS CHECK IAW B757-400 AMM 33-51-07. 2 L 7 2 4F RT A1NM 2008010400111 20080104 00111 NM 2008 1 4 DL764071627 1 20071216 A 3350 LIGHT BOEING 767 767432ER 1385134 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 826MH 29697 L2 EXTERIOR EMERG SLIDE LIGHT IS INOP. RELAMPED L2 EXTERIOR EMERGENCY SLIDE LIGHT, LIGHT OPS CHECKS GOOD IAW B767-400 M M 33-51-06. 2 L 7 2 4F RT A1NM 2008010400131 20080104 00131 NM 2008 1 4 DLM88071612 1 20071214 A 3260 658188103 LENS DOUG MD88 MD88 3023688 NM COCKPIT MISINSTALLED A DALA O OTHER W INADEQUATE Q C LD LANDING 1 SO 27 915DL 49546 ON GEAR EXTENSION FOR LANDING, RT MAIN GEAR IND LIGHT WOULD NOT ILLUM. FOUND RT MLG LIGHT LENS INSTALLED INCORRECTLY. CREW VERBAL RELAMP ATTEMPTED. REPLACED LIGHT LENS, RT GEAR IND CKS GOOD. PROX BOX CKS GOOD. NO SENSOR FAULTS, P/N 658 -1881-03. 2 L 7 2 4F RT A6WE 2008010400153 20080104 00153 2008 1 4 F3LA200700377 4 20071212 A 2565 L32A319160001 RELEASE CABLE AIRBUS A319 A319111 3930336 NM EVAC SLIDE INOPERATIVE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED LT OVERWING EMERGENCY EXIT SLIDE RELEASE CABLE WOULD NOT RETRACT. REMOVED AND R EPLACED LT OVERWING EXIT SLIDE RELEASE CABLE IAW AMM 25-62-43-000-001. COMPLETED ADJUSTMENT AND OPERATIONAL CHECK OF SL IDE RELEASE CABLE IAW AMM 25-62-43-400-001. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 2008010400182 20080104 00182 CE 2008 1 4 VUC2007F00000 1 20071126 A 2612 FIRE WARNING LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP RT NACELLE FALSE ACTIVATION E VUCA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 19 35TJ 137 DURING CLIMB, RT ENGINE FIRE WARNING LIGHT ILLUMINATED. FLT CREW RETARDED POWER PACK ON RT ENGINE (WHICH WAS AT MAX CON TINUOUS ITT INDICATION), REQUESTED CLEARANCE TO FL 390 AND DECLARED AN EMERGENCY. UPON PULLING POWER BACK THE FIRE WARN ING LIGHT EXTINGUISHED. ADVANCING POWER ON THE AFFECTED ENGINE DID NOT CAUSE THE LIGHT TO ILLUMINATE AGAIN. NO DIFFERE NCES OBSERVED BETWEEN LT AND RT ENGINE INDICATIONS. FLIGHT CREW PERFORMED FIRE WARNING CHECKLIST AND DETERMINED THAT TH ERE WAS A FALSE FIRE INDICATION. FLIGHT CREW UNDECLARED THE EMERGENCY. AC LANDED WITHOUT INCIDENT. AN EXTENSIVE VISUA L INSPECTION OF THE FIRE WARNING SYS WAS PERFORMED WITH NO DEFECTS NOTED. FIRE LOOP TEST WAS PERFORMED WITH NO DEFECTS 2 L 7 2 4F 4 F A10CE E6WE 2008010400184 20080104 00184 CE 2008 1 4 K5L2007F00001 1 20071125 A 3010 1013890067 ACTUATOR BEECH 200 A200 1152921 CE PWA PT6 PT6A41 52043 EA ICE VANE INOPERATIVE E K5LA O OTHER O OTHER DE DESCENT 1 EA 05 636B 14838 BC61 DESCENDING, PILOT SELECTED ICE VANES EXTENDED AND ONLY THE LT ONE EXTENDED. PULLED CIRCUIT BREAKER AND SLOWED AIRCRAFT AND EXTENDED RT ICE VANE WITH THE MANUAL EXTENSION HANDLE. REPLACED RT ICE VANE ACTUATOR MOTOR. (K) 1 L 7 2 4T 4 T A24CE E4EA 2008010400186 20080104 00186 WP 2008 1 4 JL92007F00000 2 20071110 A 7261 S9413117 O-RING LEAR 35 31A 5170531 CE GARRTT TFE731 TFE73123B WP OIL FILLER CAP MISSING E JL9A A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 NM 11 68ES 221 P99568 AIRCRAFT STARTED EXPERIENCING LOSS IN OIL PRESSURE INDICATED BY THE LHS ENGINE OIL PRESSURE GAUGE NEEDLE BOUNCING BETWEE N THE RED MARKINGS ON THE GAUGE, THE NEEDLE AFTER A FEW SECONDS SETTLED DOWN IN THE GREEN AND THEN SLOWLY STARTED DECREA SING, ON NOTICING THIS THE PIC DECIDED TO SHUT DOWN THE NR 1 LHS ENGINE IAW EMERGENCY PROCEDURES CHECKLIST AND FIND THE CLOSEST AIRPORT TO LAND. THEY PERFORMED AN EMERGENCY PROCEDURES LANDING AT ABOUT 6:30 PM, ON 11/10/2007 AT AIRPORT. ON INSPECTING THE AC IT WAS FOUND THAT THE OIL FILLER CAP O-RING WAS MISSING AND THAT HAD CAUSED THE OIL TO DEPART THE ENG INE. ACCESS AIR PILOTS HAVE BEEN INSTRUCTED ON INSPECTING THE OIL FILLER CAPS O-RINGS FOR DAMAGE OR LOOSENESS, ACCESS A 2 L 7 2 4F 4 F RT A10CE E6WE 2008010400187 20080104 00187 NE 2008 1 4 F3LA200700385 2 20071224 A 7200 ENGINE AIRBUS A319 A319111 3930336 NM GE CFM56 CFM56* 13802 NE NR 1 FAILED A F3LA E B J ENGINE SHUTDOWN EMER. DESCENT DUMP FUEL E VIBRATION/BUFFET CR CRUISE 1 NM 03 937FR 2400 577204 FLIGHT CREW REPORTED INFLIGHT SHUTDOWN OF NR 1 ENGINE DUE TO LOSS OF OIL QUANTITY/OIL PRESSURE. NR 1 ENGINE IS IN THE P ROCESS OF BEING REPLACED. 1/7/008 FLT CREW REPORTED NT 1 ENGINE FAILURE IN FLT. SMELLED BURNING OIL, CLASS II ECAM ENGINE NR 1 OIL FILTER CLOG, OIL PRESSURE & QTY NORMAL. WITHIN 5 MINUTES, OIL QTY DROPPED TO BELOW 5 QTS. WITHIN 1 MIN UTE, NR 1 ENGINE FAILURE. ENGINE SHUT DOWN AS PER ECAM ACTIONS. DISCHARGED AGENT 1. AFTER LANDING NO FIRE INDICATIONS WERE NOTED. R & R NR 1 ENGINE IAW TASK CARDS MP 71042-1 AND MP 71042-2 AND EA A9-72R-12347. CHECKED GOOD, NO FAULTS O R LEAKS NOTED. PERFORMED CAT 3 TEST IAW AMM 22-97-00-710-001. CAT 3B STATUS RETAINED. 2 L 7 2 4F 4 F RT A28NM E2GL 2008010400188 20080104 00188 CE 2008 1 4 E0Y2007F00000 1 20071114 A 7603 LEVER LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE7312 01518 WP LEFT OBSTRUCTED E E0YA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 15 450BK 104 DURING SCHEDULED MAINTENANCE, AN INSPECTION THROUGH THE ACCESS PANEL IN THE LT WHEEL WELL REVEALED THAT LT THRUST LEVER TELEFORCE IS FULLY IN CONTACT WITH THE LT RUDDER CABLE WHICH MIGHT CAUSE CHAFFING. FURTHER INSP SHOWED THAT THE TELEFO RCE WAS NOT ROUTED PROPERLY AND NOT IN THE TEFLON HOLDER AS WELL. TELEFORCE CABLE WAS ALSO FOUND TO BE WRAPPED AROUND T HE RUDDER CONTROL CABLE ALL ALONG. WHILE PERFORMING ELEVATOR CABLE INSPECTION, IT WAS FOUND THAT THE PRIMARY ELEVATOR C ONTROL WAS NOT POSITIONED IN ITS DEDICATED GROOVE WHERE IT WAS FOUND MOUNTED OVER THE PITCH SERVO CABLE ADJACENT TO THE ELEVATOR PRIMARY CABLE GROOVE. THE ELEVATOR PRIMARY CABLE WAS FOUND WITH 3 BROKEN STRANDS. DURING INSPECTION OF ELEVAT 2 L 7 2 4F 4 F RT T00008WI E6WE 2008010400189 20080104 00189 NM 2008 1 4 F3LA200700393 1 20071220 A 5350 NAS11020610 FASTENER AIRBUS A319 A319111 3930336 NM FAIRING CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED CORRODED FASTENERS THAT SECURE LIGHT TO RT WING-TO-BODY FAIRING 192DT. REMOVED AND REPLACED RT UPPER WING LIGHT COVER MOUNTING SCREWS ON PANEL NR 192DT. 2 L 7 2 4F RT A28NM 2008010400194 20080104 00194 NM 2008 1 4 F3LA200700396 1 20071214 A 5315 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT Y1292, FR68, CORRODED. DETERMINED CORROSION TO BE OUT OF LIMITS IA W SRM 53-00-14, PAR 4 B. REMOVED AND REPLACED FLOORBEAM Y1292 AT FR 68-69 IAW SRM 51-42-11 AND 51-44-11. 2 L 7 2 4F RT A28NM 2008010400197 20080104 00197 NM 2008 1 4 F3LA200700398 1 20071214 A 5315 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT Y765, FR68, CORRODED. DETERMINED CORROSION TO BE OUT OF LIMITS IAW 53-00-14. REMOVED AND REPLACED FLOOR BEAM AT Y768 IAW SRM 51-42-11. 2 L 7 2 4F RT A28NM 2008010400199 20080104 00199 NM 2008 1 4 F3LA200700389 1 20071216 A 5320 D5348015900400 PLATE AIRBUS A319 A319111 3930336 NM GIRT BAR LATCH CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED L2 DOOR AFT GIRT BAR LATCH FILLER CORRODED. REMOVED AND REPLACED L2 DOOR AFT GI RT BAR LATCH FILLER IAW AMM 53-42-12-PB401. 2 L 7 2 4F RT A28NM 2008010400207 20080104 00207 EU 2008 1 4 07FDEA05083 1 20071218 A 5313 STRINGER AIRBUS 300 A300B4622 3930401 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 PREVIOUS LONGERON "T" CAP REPAIR LOCATED IN BULK CARGO BETWEEN FRAMES 64 AND 65 UNDER FLOOR AT APPROX STRINGER 50 RT HAS 1 EACH REPAIR SECTION MEASURING 11" LONG AND 2 EACH REPAIR ANGLES MEASURING 10.5". PREVIOUS REPAIR FOUND NOT BE IAW A3 00-600 SRM 51-71-50 FIG 201. REMOVED AND REPLACED REPAIR WITH CORRECT REPAIR IAW A300-600 SRM 51-72-10. THIS IS A REPA IR WITH NO AIRBUS PART NUMBER. REPAIR IDENTIFIED BY AGING AIRCRAFT INSPECTION PROGRAM. 2 L 7 2 4F RT A35EU 2008010400215 20080104 00215 NM 2008 1 4 UPS07M51278 1 20071210 A 2560 BATTERY DOUG MD11 MD11F 3023600 NM EVAC SLIDE DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 251UP 48744 L1 DOOR EVACUATION SLIDE REMOTE PRESS TO TEST INOP. REMOVED AND REPLACED BATTERIES. OPS CHECKS NORMAL, REF MD11 MM 25- 61-04-4. 2 L 7 3 4F RT A22WE 2008010400216 20080104 00216 NM 2008 1 4 UPS07M51281 1 20071125 A 5753 SKIN DOUG MD11 MD11F 3023600 NM T/E FLAP CANNING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP INSPECTION TYPE:C LT I/B FLAP UPPER SURFACE FOUND OIL-CANNING AT 53 INCHES FROM I/B END AND 23" FROM T/E END AS MARKED. DAMAGED PORTION ON LT I/B FLAP UPPER SURFACE TRIM OFF PER SRM 57-10-00 FIG 34 VIR 35. HFEC INSP C/O ON TRIM OFF AREA, FOUND NO CRACK EVIDENT. REPAIR DOUBLER FAB USING 2024T3-0.040 INCH MAT'L PER SRM 57-10-00 FIG34 VIR 35. REPAIR DOUBLER FASTENER HOLES DRILLED, RE-PROTECTED AND PAINTED. NEW DOUBLER INSTALLED PER SRM 51-35-01VIIR 35 AND SRM 57-10-00 FIG 3 4 VIR 35. 2 L 7 3 4F RT A22WE 2008010400217 20080104 00217 NM 2008 1 4 MWEA070307 1 20071215 A 3350 6011779 BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 601ME 49762 LEFT AND RIGHT EMERGENCY EXTERIOR EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK. 2 L 7 2 4F RT A6WE 2008010400219 20080104 00219 NE 2008 1 4 WRNA200700062 2 20071218 A 7261 B-NUT AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE NR 1 ENGINE LOOSE A WRNA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 05 504TA 216 528358 AFTER LEVELING OFF AT 27,000' OBSERVED STEADY DECLINE IN OIL QUANTITY OF NUMBER 1 ENGINE, RETURNED TO FIELD AND MADE A S AFE LANDING, NO LOSS OF OIL PRESSURE. FOUND AND SECURED A LOOSE 'B' NUT AT AFT BEARING LINE, RE-SERVICED OIL AND ACCOMP LISHED LEAK CHECK, NO FURTHER LEAKS. AIRCRAFT RELEASED TO SERVICE. 2 L 7 2 4F 4 F RT A35EU E23EA 2008010400220 20080104 00220 EU 2008 1 4 YENA2007117 1 20071213 A 2780 5914868 CONTROL LEVER EMB ERJ190 ERJ190100IGW 3260408 EU COCKPIT FAILED A YENA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 15 190JB 3186 19000011 FLT NR 1304, IAD-JFK - SLAT FAIL EICAS MSG SLATS STUCK FULLY EXTENDED. REMOVED AND REPLACED SLAT FLAP CONTROL LEVER IAW 27-53-01. SLAT/SLATS RETRACT AND STOWED NORMALLY. 2 L 7 2 4F RT A57NM 2008010400221 20080104 00221 EA 2008 1 4 SWIA200718958 1 20071212 A 2621 PRINTED CKT BOAR CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY FAULTY A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 776SK 10241 FLT 6435 - RECEIVED A "CARGO BOTTLE LO" CAUTION MESSAGE. REPLACED PCB NR 2 IN JB2 AND PCB NR 2 IN JB3 AS WELL AS BOTH A FT AND FORWARD CARGO BOTTLES PER AMM 26-25-01, PN 446518-1, SN/OFF 12097, PN 446518-1 SN/OFF 12000, PN 473919-1, SN/OFF 0499A PN 473920-1, SN/OFF 0346N. 2 L 7 2 4F RT A21EA 2008010400224 20080104 00224 SO 2008 1 4 SWIA200718961 1 20071212 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 299SW 120329 FLT 3722 - AFT EMERGENCY LIGHT AT ROW 9 IS INOP. INSTALLED SERVICEABLE ELBP IAW AMM 33-50-02. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008010400225 20080104 00225 EA 2008 1 4 SWIA200718962 1 20071214 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 430SW 7523 FLT 3863 - RIGHT SIDE WINDOW IS CRACKED. REPLACED WINDOW IAW AM 56-12-01, PNL: NP139322-12, SON OFF: 01052H1484. 2 L 7 2 4F RT A21EA 2008010400226 20080104 00226 EA 2008 1 4 SWIA200718963 1 20071216 A 3510 OXYGEN MASK CNDAIR CL600 CL6002B19 1900309 EA COCKPIT OUT OF POSITION A SWIA G O2 MASK DEPLOYED O OTHER UK UNKNOWN 1 NM 07 412SW 7101 FA'S O2 MASKS FELL.RESECURED FA'S O2 MASK. 2 L 7 2 4F RT A21EA 2008010400227 20080104 00227 EA 2008 1 4 SWIA200718964 1 20071215 A 2150 ACM CNDAIR CL600 CL6002B19 1900309 EA A/C BAY FAILED A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 946SW 7776 FLT 6389 - AFTER TAKEOFF, SMOKE TOILET CAUTION MESSAGE APPEARED. RETURNED TO FIELD. REPLACED NR 2 ACM PER CRJ 200 21-5 1-1A. 2 L 7 2 4F RT A21EA 2008010400229 20080104 00229 2008 1 4 QXEA200701917 4 20071213 A 2300 RADIO BOMBDR DHC8 DHC8402 1390042 NM NR 2 COMM MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 416QX 4083 LAX - FLIGHT 2334 - ON TAXI NR 2 COMM RADIOS SHOW A RED FAIL MESSAGE. RETURNED TO THE GATE. MAINTENANCE CYCLED POWER T O THE AIRCRAFT. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008010400237 20080104 00237 NM 2008 1 4 QXEA200701912 1 20071216 A 3240 LINE BOMBDR DHC8 DHC8402 1390042 NM BRAKE SYSTEM CONTAMINATED A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 407QX 4049 SEA- BRAKES SOFT ON ROLLOUT USING MODERATE TO HEAVY PRESSURE. MAINTENANCE BLED BRAKE SYSTEM IAW AMM 32-42-00-870-801. FOUND AIR IN SYSTEM 1 AND 2. BLED 6 QUARTS THROUGH NR 2 SYSTEM AND 12 QUARTS THROUGH NR 1 SYSTEM AND SERVICED HYDRAULIC QUANTITIES IN SYSTEMS. PERFORMED MAINTENANCE TAXI AND OPERATIONAL CHECK OF BRAKES AND ANTI-SKID SYSTEMS. ALL CHECKS G OOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008010400240 20080104 00240 NM 2008 1 4 QXEA200701905 1 20071215 A 2133 81150C020201 OUTFLOW VALVE BOMBDR DHC8 DHC8402 1390042 NM CABIN PRESSURE MALFUNCTIONED A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 414QX 14413 4061 RNO- FLIGHT 2441 - AIRCRAFT FAILED TO PRESSURIZE AFTER TAKEOFF IN EITHER AUTO OR MANUAL MODES. MORE THEN NORMAL NOISE F ROM THE FORWARD BULKHEAD AREA. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE F ORWARD SAFETY OUTFLOW VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008010400242 20080104 00242 NM 2008 1 4 QXEA200701879 1 20071212 A 2720 83910048S019 TRIM PANEL DHAV DHC8 DHC8202 2809007 NM COCKPIT FAILED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 349PH 486 LWS - FLIGHT 2027 - WHILE BOARDING PASSENGERS WITH GROUND POWER ON, SMOKE STARTED TO COME FROM THE TRIM INDICATOR PANEL IN THE COCKPIT. POWER TURNED OFF AND BATTERIES TURNED OFF. SMOKE STOPPED. NO INDICATION OF FIRE. FOUND CIRCUIT BREA KER POPPED. MAINTENANCE REPLACED THE RUDDER TRIM PANEL. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008010400243 20080104 00243 NE 2008 1 4 QXEA200701878 2 20071212 A 7530 4120T03P04 ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE NR 2 ENGINE LEAKING A QXEA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 NM 09 617QX 11387 10130 PDX - FLIGHT 2430 - ON WALK AROUND NOTICED A FUEL LEAK FROM THE NR 2 ENGINE. MAINTENANCE REPLACED THE NR 2 SLAVE ACTUAT OR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008010700001 20080107 00001 EU 2008 1 7 YENA2007114 1 20071212 A 2780 SLAT EMB ERJ190 ERJ190100IGW 3260408 EU WING OUT OF RIG A YENA K NONE F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 15 249JB 19000045 FLT 1056 PIT-JFK, "SLAT FAIL" EICAS MSG. APPEARED WHILE CLIMBING THROUGH 10,000 FT. SLATS REMAINED FAILED AT ZERO POSIT ION. FOLLOWED QRH PROCEDURE. APPROACH & LANDING UNEVENTFUL IN ACCORDANCE WITH/QRH. FOUND SLAT PDU BRAKE ENGAGED. PER FORM RIGGING ADJUSTMENT IAW 27-81-00. COULD NOT DUPLICATE FAULT, OK TO CONTINUE SERVICE. 2 L 7 2 4F RT A57NM 2008010700002 20080107 00002 NM 2008 1 7 MWEA070303 1 20071213 A 5230 5910157109 PAN BOEING 717 717200 1383700 NM AFT CARGO DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 914ME 55177 AFT CARGO DOOR FORWARD PAN AND SEAL RETAINER AT CUTOUT BY TORQUE TUBE CRANK END IS GOUGED AND BENT. BLENDED OUT NICKS A ND FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2008010700003 20080107 00003 NM 2008 1 7 MWEA070304 1 20071211 A 5230 59101575 PAN BOEING 717 717200 1383700 NM CARGO DOOR CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 918ME 55180 FORWARD EDGE OF DOOR INNER PAN CHAFED AT TORQUE TUBE. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2008010700004 20080107 00004 NM 2008 1 7 MWEA070305 1 20071211 A 5230 59101575 PAN BOEING 717 717200 1383700 NM CARGO DOOR CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 918ME 55180 AFT EDGE OF DOOR INNER PAN CHAFED AT TORQUE TUBE. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2008010700010 20080107 00010 SO 2008 1 7 RAIA00712009 1 20071209 A 3610 O-RING EMB 145 EMB145 3260210 SO BLEED AIR SYS BLOWN A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 809HK 145187 FLT NR 7927 - ROC - NR 1 BLEED LEAK. MAINTENANCE REMOVED AND REPLACED CROSS BLEED TUBE COUPLING O-RINGS, OPS CHECK GOOD . 2 L 7 2 4F RT T00011AT 2008010700011 20080107 00011 SO 2008 1 7 RAIA00712010 1 20071211 A 3350 RPS1B BATTERY EMB 145 EMB145 3260210 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 806HK 145112 PRE FLT NR 3542 - STL - LEFTHAND AND RIGHTHAND EMERGENCY DOOR FLOOD LIGHT INOP. MAINTENANCE REMOVED AND REPLACED NR 3 B ATTERY PACK, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2008010700012 20080107 00012 SO 2008 1 7 RAIA00712011 1 20071210 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN NOT SEATED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 840HK 145341 PRE FLT NR 7954 - TYS - SERVICE DOOR FLOOD LIGHT INOP. MAINTENANCE RESEATED BULB, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2008010700013 20080107 00013 SO 2008 1 7 RAIA00712012 1 20071210 A 3610 SEAL EMB 145 EMB145 3260210 SO BLEED AIR SYS LEAKING A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 812HK 145373 FLT NR 5473 - STL - NR 1 ENGINE BLEED LEAK. MAINTENANCE REMOVED AND REPLACED BLEED SEALS, GROUND RUN, NO FURTHER MESSAG ES NOTED. 2 L 7 2 4F RT T00011AT 2008010700016 20080107 00016 SO 2008 1 7 RAIA00712013 1 20071211 A 2131 92185A010200 CONTROLLER EMB 145 EMB145 3260210 SO CABIN PRESSURE MALFUNCTIONED A RAIA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 CE 03 816HK 8021 145055 FLT NR 5523 - SDF - LOSS OF PRESSURIZATION. MAINTENANCE REMOVED AND REPLACED PRESSURIZATION CONTROLLER, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2008010700018 20080107 00018 NM 2008 1 7 BB07101 1 20071220 A 4910 7321387009 ACTUATOR BOEING 757 757225 1384959 NM APU FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 916UW 38127 1211 22192 FLIGHT 1619, PHL-FLL: AFTER TAKEOFF, THE APU SHUTDOWN. THE RIGHT GENERATOR SYSTEM WAS ALREADY ON MEL, SO THE FLIGHT RE TURNED TO PHL. MAINTENANCE REPLACED THE RIGHT IDG AND APU INLET DOOR ACTUATOR TO CLEAR BOTH FAULTS. 2 L 7 2 4F RT A2NM 2008010700020 20080107 00020 NM 2008 1 7 2007UALA05004 1 20071204 A 3250 CABLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NLG STEERING OUT OF ADJUST A UALA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 WP 29 831UA 1291 ACFT PULLING LEFT, CONFIRMED HARD PULL. REPLACED STEERING TRANSDUCER, BOTH NOSE WHEEL TIRES, BSCU, NWS SENSOR 3GC. ADJ USTED NWS FEEDBACK CABLES TO FINAL FIX THE PROBLEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010700021 20080107 00021 NM 2008 1 7 2007UALA05131 1 20071215 A 3350 BATTERY BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 203UA 24718 NR 1 RT MED EMERGENCY EXIT SIGN INOP. FOUND BATTERY FAILED. REPLACED MED EMERGENCY LIGHT BATTERY. ALL LIGHTS OPS CHEC K. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010700023 20080107 00023 NM 2008 1 7 2007UALA05133 1 20071216 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 DOOR 5L AFT SILL EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700025 20080107 00025 NM 2008 1 7 2007UALA05135 1 20071214 A 3397 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 FOUND EEL LIGHT CONNECTOR BROKEN AT SEAT 13A. REPLACED EEL CONNECTOR STRIP- OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700028 20080107 00028 NM 2008 1 7 2007UALA05138 1 20071214 A 3397 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 526UA 24994 SEATS 30-34ABC EMERGENCY LIGHTS INOP. FOUND LOOSE CONNECTOR. RECONNECTED LOOSE CONNECTOR- ALL TESTS ARE NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700030 20080107 00030 NM 2008 1 7 2007UALA05140 1 20071214 A 3350 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 526UA 24994 EXTERIOR EMERGENCY LIGHTS INOP AT RT AFT OVERWING AND BOTH LEFT OVERWING LIGHTS. FOUND BATTERY FAULTY. REPLACED BATTERY . 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700033 20080107 00033 NM 2008 1 7 2007UALA05145 1 20071218 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY LIGHT ROW 58 RT INOPERATIVE. REPLACED LIGHT ASSY. SECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700034 20080107 00034 NM 2008 1 7 2007UALA05146 1 20071218 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY LIGHT ROW 44 RT INOP. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700035 20080107 00035 NM 2008 1 7 2007UALA05147 1 20071218 A 3350 68671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY LIGHT ROW 54 LT INOP. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700038 20080107 00038 NM 2008 1 7 2007UALA05150 1 20071218 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY CEILING LIGHT ABOVE ROW 13 INOPERATIVE. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700040 20080107 00040 NM 2008 1 7 2007UALA05153 1 20071219 A 2530 OVEN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE GALLEY CONTAMINATED A UALA A UNSCHED LANDING C B F.O.D. SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 206UA 30212 FLT DIVERTED DUE TO AN ELECTRICAL ODOR IN THE AFT MAIN CABIN AREA. FOUND MELTED PLASTIC IN R51 OVEN. REMOVE PLASTIC. CHECKED ALL RECIRCULATION FANS, OPS CHECKED GOOD. CHECKED AFT GALLEY AREAS, INCLUDING CEILING AREAS, AC DUCTING, AFT C ARGO & AFT LAV. REMOVED CONTROL PANEL & CHECKED FOR BURNED ODOR ON WIRES. NONE NOTED. REMOVED & CHECKED ALL OVENS. CH ECKED POWER-WIRES FOR ODOR, NONE NOTED. RAN APU & ELECTRICALLY LOADED AC WITH A-C POWER. WITH OVENS IN OPERATION, & RE CIRCULATION FANS ON FOR 3 HRS WHILE REINSPECTING AREAS. NO ODOR OF ANY ABNORMALITIES NOTED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008010700041 20080107 00041 NM 2008 1 7 2007UALA05155 1 20071218 A 5210 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 FWD ENTRY DOOR (L1) AFT CORNER OF LOWER FRAME IS CRACKED. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010700042 20080107 00042 NM 2008 1 7 2007UALA05156 1 20071218 A 5320 SUPPORT ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 AFT CARGO DOOR CUTOUT AT BS 847 BETWEEN STR S24R & S25R FLOOR WEB SUPPORT ANGLE CORRODED. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010700043 20080107 00043 NM 2008 1 7 2007UALA05157 1 20071219 A 3350 582233 CHARGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 RIGHT WING 2 FORWARD MOST EMERGENCY EGRESS LIGHTS INOP. REPLACED BATTERY CHARGER. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700045 20080107 00045 NM 2008 1 7 2007UALA05159 1 20071219 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 SEATS 32L & 56L EEL LIGHTS ARE INOPERATIVE. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700047 20080107 00047 EU 2008 1 7 YENA2007118 1 20071219 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU CABIN ODOR A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 625JB 2535 FLT NR 382, FLL-LGA, ON CLIMB-OUT FLT ATTENDANT REPORTED BURNING ODOR FROM VICINITY OF ROW 5. SECURED TV'S AND ODOR DIS SIPATED, LEFT TV TURNED OFF. PERFORMED TASK 24-00-00810-823.COMPLIED WITH TSM 23-39-00-810-801. NO FAULTS FOUND. REMOVE D AND REPLACED XEB AT POSITIONS 5ABC AND 5DEF AND VDU'S AT 5A-F AS PRECAUTIONARY. ALL OPS NORMAL PER LTV ON 44-20-17. 2 L 7 2 4F RT A28NM 2008010700048 20080107 00048 NM 2008 1 7 UPS07M51327 1 20071226 A 2497 WIRE DOUG MD11 MD11F 3023600 NM E&E BAY BURNED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 283UP 48484 DURING TROUBLE SHOOTING OF C/B POPPING FOUND WIRE BUNDLES BURNED THROUGH, LOCATED IN E&E BAY RT SIDE. TRANSFERRED TO UPS NRC MD015501-REFER FOR DETAILS & SIGN OFF. SUMMARY INCLUDES 247 WIRES REPLACED END TO END, 3 WIRE SPLICE REPAIRED. ALL SYS AFFECTED OPS AND FUNCTIONAL CKD FOR UPS & BOEING ENG INSTRUCTIONS 2 L 7 3 4F RT A22WE 2008010700052 20080107 00052 NM 2008 1 7 2007UALA05164 1 20071218 A 5320 SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 SEAT TRACK SUPPORT AT BS 365.25 AND RBL 45 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: INSTALLED STRAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700054 20080107 00054 NM 2008 1 7 2007UALA05166 1 20071218 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 570UA 26678 EXTERIOR EMERGENCY LIGHTS AT DOOR 3L AND RIGHT FWD OVERWING ARE INOP. FOUND LAMPS WERE FAULTY. RELAMPED DOOR 3L AND RT FWD OW EXIT SIGNS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700056 20080107 00056 NM 2008 1 7 2007UALA05168 1 20071218 A 2120 2610000101 OVEN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE GALLEY CONTAMINATED A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 792UA 26934 IN CRUISE FLT ATTD'S REPORTED THAT THE BUSINESS CLASS GALLEY HAD A PLASTIC BURNING ODOR THAT APPEARED TO BE COMING FROM THE CEILING AREA. FOUND PLASTIC BURNED ON THE BOTTOM OF OVEN REMOVED PLASTIC. AC OK FOR SERVICE 2 L 7 2 4F 4 F RT T0001SE E46NE 2008010700057 20080107 00057 NM 2008 1 7 2007UALA05169 1 20071220 A 2421 GENERATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT DISCONNECTED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 546UA 25367 RTFL AFTER THE LEFT GENERATOR BECAME DISCONNECTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700058 20080107 00058 NM 2008 1 7 2007UALA05170 1 20071219 A 5320 ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 294-344 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 50327 24658 FWD GALLEY DOOR THRESHOLD Z-ANGLE IS CORRODED ON UPPER SURFACE FROM STA 294.5 TO 344 STR 17R RBL 53 TO RBL 61. SUSPECT NORMAL AC OPERATION. MAJOR REPAIR ACCOMPLISHED REPLACED THRESHOLD Z-ANGLE. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010700059 20080107 00059 NM 2008 1 7 2007UALA05171 1 20071219 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 FLOORBEAM CRACKED IN UPPER CHORD BS 325 LBL 10 AND ADJACENT FASTENER SHEARED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010700061 20080107 00061 NM 2008 1 7 2007UALA05175 1 20071219 A 2622 EXTINGUISHER BOEING 737 737322 1384676 NM FWD GALLEY LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 369UA 24538 FWD GALLEY HALON FIRE EXTINGUISHER PRESSURE APPEARS LOW. REPLACED HALON EXTINGUISHER IN FWD GALLEY. 2 L 7 2 4F RT A16WE 2008010700062 20080107 00062 NM 2008 1 7 2007UALA05176 1 20071220 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 SLIDE LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 506UA 24627 THE 1R SLIDE LIGHT BURNED OUT. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700063 20080107 00063 NM 2008 1 7 2007UALA05177 1 20071220 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EEL INOP ON SEATS 42ABC THRU 57ABC. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700065 20080107 00065 NM 2008 1 7 2007UALA05179 1 20071220 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EEL INOP LAV 111 SIDEWALL. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700068 20080107 00068 NM 2008 1 7 2007UALA05182 1 20071219 A 3350 SIGN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 DOOR 2L EMERGENCY EXIT SIGN LOOSE. REINSTALLED EXIT LENS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700070 20080107 00070 2008 1 7 2007UALA05184 4 20071219 A 2565 SLIDE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 LEFT OVERWING SLIDE AFT AREA, ARM CAM OF SLIDE HITTING STOP BLOCK FITTING. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010700071 20080107 00071 2008 1 7 2007UALA05185 4 20071219 A 2565 SLIDE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 RIGHT OVERWING SLIDE AFT AREA, ARM CAM OF SLIDE HITTING STOP BLOCK FITTING. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010700073 20080107 00073 NM 2008 1 7 2007UALA05187 1 20071219 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 647UA 25284 EMERGENCY PATH LIGHTS OUT AT ROW 24-33 AND 38A. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010700075 20080107 00075 NM 2008 1 7 2007UALA05189 1 20071219 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 227UA 30555 AFT EMERGENCY LIGHT OUT AT SEATS 2E, 2F, AND 3E. REPLACED LIGHT STRIP. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008010700077 20080107 00077 NM 2008 1 7 2007UALA05192 1 20071220 A 5512 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZ STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 RIGHT HORIZ STAB LOWER SKIN AT T/E HAS 2.25 INCH CRACK, JUST FWD OF 1ST BALANCE BAY. MAJOR REPAIR ACCOMPLISHED: FABRICA TED & INSTALLED EXTERNAL DOUBLER & FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010700079 20080107 00079 NM 2008 1 7 2007UALA05194 1 20071220 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 797 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 AFT CARGO DOOR CUTOUT, AFT FACE OF BS 797 FRAME HAS CORROSION BETWEEN STR'S 24R & 23R. SUSPECT MOISTURE CONTAMINATION. REMOVED DAMAGED FRAME AND REPLACED WITH NEW FRAME. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010700080 20080107 00080 NM 2008 1 7 2007UALA05195 1 20071220 A 5320 ATTACH ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 277-294 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 50387 24660 FWD GALLEY DOOR CUTOUT BETWEEN BS 277 AND BS 294.5 INTERCOSTAL ATTACH ANGLE CRACKED BETWEEN STRINGERS 9R & 10R. SUSPECT NORMAL AC OPERATION. MAJOR REPAIR ACCOMPLISHED BY REPLACING THE ANGLE. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010700083 20080107 00083 NM 2008 1 7 2007UALA05198 1 20071220 A 3510 OXYGEN MASK BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE COCKPIT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 667UA 29239 CAPT O2 MASK DOES NOT TEST PROPERLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010700084 20080107 00084 NM 2008 1 7 2007UALA05199 1 20071221 A 2424 GCU BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RIGHT BURNED A UALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 WP 29 213UA 30219 777112 RTFL DUE TO A RT ENGINE GENERATOR PROBLEM. AFTER TROUBLESHOOTING,FOUND RT GCU CIRCUIT BREAKER OPEN & GEN CONTROL UNIT BURNED INSIDE. REPLACED GCU AND OPS CHECKED GOOD. OPENED UP GCU MR24241-13 AND VERIFIED A UNIT INTERNAL FAILURE WITH BUR NED CIRCUIT BOARD. CONDUCTED VERIFICATION FLT & FLT CREW FOUND RT ELECTRICAL SYSTEM GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008010700085 20080107 00085 NM 2008 1 7 2007UALA05201 1 20071221 A 2751 TRANSMITTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TE FLAPS MALFUNCTIONED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 581UA 26701 LANDED UNDER AMBER ALERT DUE TO FLAP PROBLEMS. FOUND INDICATION FAILURES CAUSING FSEU TO FAULT INCORRECT FLAP POSITION . INSPECTED ALL TORQUE TUBES AND TRANSMISSIONS. ALL APPEAR NORMAL. REPLACED FLAP POSITION TRANSMITTER TS5049. SYSTE M OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700086 20080107 00086 NM 2008 1 7 2007UALA05202 1 20071221 A 2781 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE COCKPIT ACTIVATED A UALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 WP 29 672UA 30027 ON APPROACH RECEIVED L/E SLAT ASYM EICAS MESSAGE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010700087 20080107 00087 NM 2008 1 7 2007UALA05204 1 20071220 A 4920 APU BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE MALFUNCTIONED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 669UA 30025 APU FAILED TO START AFTER SEVERAL ATTEMPTS. BIT BOX, FAULT NOTED LOP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010700090 20080107 00090 NM 2008 1 7 2007UALA05209 1 20071220 A 3260 WARNING SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT MALFUNCTIONED A UALA O OTHER N FALSE WARNING CL CLIMB 1 WP 29 310UA 23671 CREW REPORTS ON GEAR RETRACTION THE NLG GREEN AND RED LIGHTS STAYED ON WITH GEAR HANDLE UP OR OFF. CYCLED GEAR AND NO H ELP. NLG APPEARS TO BE UP, NO ABNORMAL NOISE AND CREW HEARD TIRES HIT SPIN PADS. AFTER A FEW MINUTES, THE GREEN LIGHT WENT OUT BUT RED LIGHT STAYED ON. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010200186 20080102 00186 EA 2008 1 2 A6WA200740672 1 20071130 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 433AW 7289 FLOORBEAM AT FS 280 IS CRACKED AT LBL 9 AND RBL 9 CRACK AT LBL 9 IS .400 INCH CRACK AT RBL 9 IS 1.200 INCH. (M) FLOOR BEAM REPAIRED IAW REO 601R-53-11-171 REV D. (K) 2 L 7 2 4F RT A21EA 2008010200194 20080102 00194 EA 2008 1 2 A6WA200740633 1 20071116 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 427ZW 7685 CRACK ON FORWARD AND AFT PASSAGE DOOR EDGE MEMBER DAMAGED REPAIRED ON FORWARD AND AFT PASSENGER DOOR EDGE MEMBER IAW CRJ 200 REO 601R-52-11-279 REV NC. (M) 2 L 7 2 4F RT A21EA 2008010400021 20080104 00021 SO 2008 1 4 C2XA07ON0035 1 20071206 A 4910 450113A INLET EMB 145 EMB145XR 3260214 SO APU OBSTRUCTED A C2XA D RETURN TO BLOCK M OVER TEMP TX TAXI/GRND HDL 1 SW 27 11176 8630 8630 145881 FLIGHT 7735 - GEG TO LAX - FLIGHT CREW REPORTED DURING TAXI APU HIGH TEMP AND APU FIRE INDICATION ON EICAS. SPOKANE AIR WAY CONTRACT MECHANICS REMOVED ICE FROM APU INLET AND VERIFIED NORMAL OPERATION. A/C WAS RELEASE IN AIRWORTHY CONDITION S TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008010400037 20080104 00037 SO 2008 1 4 C2XA07CL105 1 20071224 A 3350 SG963 STRIP EMB 145 EMB145XR 3260214 SO CABIN LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11113 145662 CLE FLIGHT NR 2297, THE CREW REPORTED THE EMERGENCY LIGHT STRIP AT THE GALLEY WAS LOOSE. MAINTENANCE INSPECTED AND RESE CURED LIGHT STRIP AT THE GALLEY IAW FCD 3350-01003. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2008010400044 20080104 00044 SO 2008 1 4 C2XA07TY085 1 20071218 A 3350 P4010030 BATTERY EMB 135 EMB135ER 3260203 SO FLASHLIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14508 220 FA FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY IAW EMB 135 AMM 33-50-16. OPS CK GOOD AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008010400046 20080104 00046 SO 2008 1 4 C2XA07IA253 1 20071226 A 4930 UNKNOWN EMB 145 EMB145XR 3260214 SO APU ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 21130 145704 IAH - FLIGHT 2920, THE CREW REPORTED A STRONG FUEL SMELL WHEN STARTING THE APU. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE APU ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008010400048 20080104 00048 SO 2008 1 4 C2XA07TY087 1 20071221 A 2560 SG9632 GLOWSTRIP EMB 145 EMB145XR 3260214 SO CABIN MISSING A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11187 14500927 EMERGENCY PHOTO LUMINESCENT STRIP AFT OF GALLEY MISSING. REPLACED STRIP IAW EMB 145XR AMM 20-12-0,1 OPS CK GOOD. AIRCR AFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT 2008010400050 20080104 00050 SO 2008 1 4 C2XA07TY081 1 20071213 A 5751 14569009410 ATTACH BRACKET EMB 145 EMB145LR 3260212 SO RT AILERON WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12921 145354 RT AILERON PCA ATTACH BRACKET IS WORN AT BORE FOR HAT BUSHING. REMOVED AND REPLACED PCA BRACKET IAW EC 5750-01177. AIR CRAFT STILL IN C CHECK. 2 L 7 2 4T RT T00011AT 2008010400063 20080104 00063 SO 2008 1 4 C2XA07IA243 1 20071210 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO LANDING GEAR OUT OF ADJUST A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 15980 145202 IAH FLIGHT 2881, DURING CLIMB, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE AND THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE LEFT MAIN GEAR PR OX SWITCH, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008010400068 20080104 00068 SO 2008 1 4 C2XA07TY089 1 20071226 A 2560 A1140001002 FLASHLIGHT EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14508 220 NR 3 EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT LAMP IAW EMB 135 VCMM 25-60-02. OPS CK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008010400069 20080104 00069 NM 2008 1 4 DXTA200702694 1 20071219 A 3150 WARNING SYSTEM AMD FALC50 FALCON2000 2730170 NM PWC PW308 PW308C 52182 NE BRAKES MALFUNCTIONED E DXTA O OTHER N FALSE WARNING LD LANDING 1 GL 07 232QS 115 MLG HANDLE BEGAN FLASHING 2-3 MIN AFTER MLG SHOWED DOWN & LOCKED & CONTINUED FLASHING FOR APPROX 3-5 MIN. FOUND SQUAT DISAGREEMENT INDICATOR TRIPED ON FAULT DISPLAY UNIT. ACCESSED CONNECTORS PL008 & PR008 IN LT & RT WW & OHMED BOTH CONNEC TORS & RESET INDICATOR. FOUND LT & RT BRAKES TO BE AT 800 PSI PRESSURE WITH FULL DEPRESSION OF PEDALS PER MM 32-42-00, NO DEFECTS NOTED. REMOVED AUX SUPPLY LINE FROM SHUTTLE VALVE ON LT & RT BRAKES & NOTED A SMALL AMOUNT OF HYD FLUID. WITH LINES STILL REMOVED, APPLIED BRAKE PRESSURE & VERIFIED NO LEAKAGE PAST VALVE. REINSTALLED AUX HYD LINES. INSTALLED APPR OVED BRAKE BLEED FIXTURE & ACCOMPLISHED BRAKE BLEED PER MM 32-42-00 & ENGINEERING MEMO M344-07-17. NO DEFECTS WERE NOTE 2 L 7 2 4F 4 F RT A50NM E00065EN 2008010400071 20080104 00071 SO 2008 1 4 C2XA07ON044 1 20071224 A 2131 14531625411 CONTROLLER EMB 145 EMB145XR 3260214 SO CABIN PRESSURE MALFUNCTIONED A C2XA K NONE O OTHER DE DESCENT 1 SW 27 12167 9785 9785 14500834 FLT 7826 - LAX TO PDX - FLIGHT CREW REPORTED AIRCRAFT DEPRESSURIZED IN FLIGHT ON DESCENT, NO EMERGENCY WAS DECLARED. MX PERSONNEL REMOVED AND REPLACED AUTO PRESSURE CONTROLLER OPERATIONALLY CHECKED SATISFACTORY AND AIRCRAFT WAS RELEASE TO RETURN FOR SERVICE IN AIRWORTHY CONDITIONS. 2 L 7 2 4F RT 2008010400087 20080104 00087 NM 2008 1 4 CALA0700749 1 20071208 A 5311 BAC15171470 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 FUSELAGE FRAME CRACKED STA 807 B/W STA 8/9. REPAIR PER EA5310-04498. 2 L 7 2 4F RT A16WE 2008010400099 20080104 00099 NM 2008 1 4 CALA0700758 1 20071215 A 5320 434561 STRAP BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 STA 847 STR 25 R LOWER STRAP CORRODED. REMOVED, FABRICATED NEW STRAP AND INSTALLED PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008010400107 20080104 00107 NM 2008 1 4 DLM90071623 1 20071215 A 5347 5930547 SEAT TRACK DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 SEAT TRACK CORRODED OUT OF LIMITS FS 1310-1364 LBL 44. REMOVED AND REPLACED DAMAGED SEAT TRACK FS 1310 FS 1310-1364 LBL 44 PER MD-90 SRM 53-40-01 ON N/R 2700-0148 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2008010400115 20080104 00115 NM 2008 1 4 DL76S071631 1 20071218 A 5330 146T324112 SKIN BOEING 767 767332 1382001 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 125DL 24075 SKIN BLENDS FS 1444 AND S-39R, AND FS 1448 AND S-38L. REPAIRED PER ER/A 459236-14 REV A. 2 L 7 2 4F RT A1NM 2008010400125 20080104 00125 NM 2008 1 4 DL75A071642 1 20071219 A 3220 141N29232 LINK BOEING 757 757212 1384951 NM NLG WW GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 750AT 23126 NLG LOCK LINK GOUGED ON THE LT SIDE SURFACE. LOCALLY BLENDED SURFACE TO REMOVE GOUGE. 2 L 7 2 4F RT A2NM 2008010400133 20080104 00133 NM 2008 1 4 DL75E071614 1 20071213 A 2421 241080105 IDG BOEING 757 7572Q8 1384972 NM LEFT MALFUNCTIONED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SO 27 709TW 268168 LEFT ENGINE GEN DRIVE LIGHT ILLUM AFTER T/O DISCONNECTED AND RETURNED TO LAS. REMOVED AND REPLACED NR 1 ENGINE IDG ASSY SERVICED W/OIL AWAITING ENGINE RUN SAURIN 256438. PERF OPERATIONAL TEST/AND BITE TEST OPS LK CK OK. 2 L 7 2 4F RT A2NM 2008010400138 20080104 00138 NM 2008 1 4 DL76S071621 1 20071203 A 5330 146T32213 SKIN BOEING 767 767332 1382001 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 125DL 24075 FUSELAGE SKIN BLENDS, FS 1285, AND STR 36R. REPAIRED PER ER/A 459263-14 REV A. 2 L 7 2 4F RT A1NM 2008010400141 20080104 00141 NM 2008 1 4 DHL2007746002 1 20071220 A 5752 652172630 TAB BOEING 727 727224 1384076 NM RT AILERON DEBONDED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 UPON WALK AROUND INSPECTION, FOUND RIGHT OUTBOARD AILERON TAB OUTBOARD DISBONDED ON UPPER SKIN APPROX 20 INCHES LONG. P ART REPLACED. 2 L 7 3 4F A3WE 2008010400145 20080104 00145 NM 2008 1 4 DHL2007783002 1 20071218 A 5753 6521795336A FAIRING BOEING 727 727227 1384078 NM T/E FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 RT WING I/B FLAP HAS SMALL 1 1/2 CRACK ON FLAP TRACK FAIRING I/B FAIRING ON FLAP. 2 L 7 3 4F A3WE 2008010400156 20080104 00156 NM 2008 1 4 AMTA200700631 1 20071105 A 2120 UNKNOWN BOEING 737 73783N 13844HI NM COCKPIT SMOKE A AMTA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 11 304TZ 30675 ON APPROACH SMOKE AND FUMES ENTER THE CABIN AND FLT DECK. T/S IAW FIM 21-00-00-810-802, NO FALULTS FOUND, OK FOR SERVICE . (K) 2 L 7 2 4F RT A16WE 2008010400159 20080104 00159 NE 2008 1 4 AMTA200700632 2 20071104 A 7261 ENGINE BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE LEFT OVERSERVICED A AMTA D RETURN TO BLOCK W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 11 304TZ 30675 AFTER ENGINE START AND PUSHBACK, SMOKE FILLED THE CABIN FROM THE A/C SYS. FOUND LT ENGINE OVERSERVICED, DRAIN TO FULL. PERFORMED AIR COND/PNEU SYS DECONTAMINATION IAW MM 21-00-01. RAN ENGINE AND APU, NO ODOR OR SMOKE NOTED. (K) 2 L 7 2 4F 4 F RT A16WE E2GL 2008010400170 20080104 00170 NM 2008 1 4 F3LA200700402 1 20071215 A 5320 BLANKING PLATE AIRBUS A319 A319111 3930336 NM GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED F1 DOOR AFT GIRT BAR STOP LEVER FITTING BLANKING PLATE CORRODED ON BOTTOM SIDE. REMOVED AND REPLACED R1 DOOR AFT GIRT BAR STOP LEVER FITTING BLANKING PLATE IAW AMM 53-12-12-PB401. 2 L 7 2 4F RT A28NM 2008010400171 20080104 00171 NM 2008 1 4 QPR2007F00000 1 20071108 A 2120 DUCT BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE RADIO RACK CONTAMINATED I QPRB O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 614PA 20738 PRIOR TO DEPARTURE, SMELLED SOMETHING LIKE PAPER BURNING. CHECKED THE E/E COMPARTMENT AND OBSERVED COOLING FAN WAS SHU TOFF. COULD NOT LOCATE SOURCE OF SMOKE AND ALL SYSTEMS OPERATED NORMALLY. TEST FLEW AIRCRAFT, OK. LATER, FOUND A BIRD NEST IN THE RADIO RACK COOLING FAN EXIT DUCT AND REMOVED SAME. REPLACED RADIO RACK COOLING FAN PRECAUTIONARY. (K) 2 L 7 3 4F 4 F A3WE E2EA 2008010400172 20080104 00172 CE 2008 1 4 VQ82007F00000 1 20071113 A 2612 FIRE WARNING LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP NR 2 NACELLE FALSE INDICATION E VQ8A A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 19 136WE 201 P74599 AT 200 FT ON NOV 13, 2007, AC DEPARTED, DURING FLIGHT, A FIRE WARNING INDICATION LIGHT FROM THE NR 2 ENGINE CAME ON. TH E AC RETURNED TO DEPARTURE AND IS CURRENTLY IN MAINTENANCE. MAINTENANCE PERSONNEL INFORMS THAT THERE IS NO INDICATION T HAT A FIRE OCCURRED AND A FAULTY FIRE DETECTION LOOP IS SUSPECTED. (K) 2 L 7 2 4F 4 F A10CE E6WE 2008010400173 20080104 00173 NM 2008 1 4 F3LA200700403 1 20071216 A 5320 228484065 PLATE AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT AFT BULKHEAD CROSSOVER BEAM HAD FASTENERS PULLING THROUGH THE CENTER PLATE. REMOVED AND REPLACED AFT CARGO COMPARTMENT AFT BULKHEAD CROSSOVER BEAM CENTER PLATE IAW SRM 51-42-11. 2 L 7 2 4F RT A28NM 2008010400175 20080104 00175 NM 2008 1 4 Z6WR200700001 1 20071127 A 7830 315W170241 ACOUSTIC PANEL BOEING 777GE9094B BOEING 777 777 UTILUSE NM THRUST REVERSER CRACKED B KRDF K NONE O OTHER IN INSP/MAINT 1 CE 07 PHBQB 20497 000197 THE 315W1702-41 INNER WALL HAS AN 8.25 INCH LONG CRACK THROUGH THE ENTIRE PANEL 12.8 INCHES FROM THE AFT END EXTENDING F ORWARD AND CENTERED 5.2 INCHES FROM THE UPPER END OF THE WALL. THIS REPAIR IS BEING PERFORMED FOR THE MFG, WHO DISCOVER ED THE DEFECT WITH THEIR AOG TEAM. WE WERE UNABLE TO DETERMINE THAT THEY HAD REPORTED THE DEFECT UNDER THEIR 145 CERTIFI CATE. THIS REPORT IS BEING SUBMITTED IN CASE THEY HAD OMITTED TO DO SO. 2 L 7 2 4F RT T00001SE 2008010400176 20080104 00176 NM 2008 1 4 AMTA200700638 1 20071127 A 5320 FLOOR SUPPORT BOEING 757 757* NM RROYCE RB211 RB211535* NE BS 1260-1440 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 522TZ 32586 AFT CARGO COMPARTMENT DOOR LOWER SILL FLOOR SUPPORT HAS CORROSION ON UPPER SURFACE AROUND FASTENER HOLES FROM STA 1360 T O 1440, BL 25R. REMOVED CORROSION IAW SRM 51-10-02, ORIG THICK .063 MTL REMOVED .016 OUT OF LIMITS IAW 53-00-53-1A. RE PLACED LOWER SILL FLOOR SUPPORT IAW 51-40-02. TREATED AND PRIMED IAW SRM 51-20-01. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010400178 20080104 00178 NM 2008 1 4 AMTA200700653 1 20071128 A 5315 FLOORBEAM BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535* NE BS 335 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 552TZ 32586 CORROSION STA 335, LBL 22 AROUND FLOOR FITTING EXTENDING UNDER, BETWEEN FITTING AND INTERCOSTAL. FLOOR BOX BEAM AND LAV FITTING STS 334-345, BL 20L. REPLACED ON CARD 69924 BAR CODE 7817660001. (K) REF: SDR AMTA200700608 FOR ALL WORK ACCO MPLISHED. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010400180 20080104 00180 NM 2008 1 4 F3LA200700399 1 20071214 A 5320 D534711242000 SHEAR PLATE AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED SHEAR PLATE AT Y1292, BETWEEN FR69 AND FR70, CORRODED. REMOVED AND REPLACED SHE AR PLATE AND FLOORBEAM IAW SRM 51-42-11 AND EA A9-53R-12329. 2 L 7 2 4F RT A28NM 2008010400193 20080104 00193 NM 2008 1 4 F3LA200700395 1 20071214 A 5320 D53480043206 SILL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED L2 DOOR SILL CORRODED AT VARIOUS LOCATIONS BETWEEN FR 66 AND FR 68. REMOVED AND REPLACED L2 DOOR SILL PLATE IAW SRM 51-42-11, 51-44-11, DRAWING D53480505 AND EA A9-53R-12330. 2 L 7 2 4F RT A28NM 2008010400205 20080104 00205 NM 2008 1 4 F3LA200700383 1 20071214 A 2540 NAS130422 ATTACH BOLT AIRBUS A319 A319111 3930336 NM LAVATORY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED LWR ATTACHMENT BOLT ON INBD AFT CORNER OF LAV "A" SEVERELY CORRODED. REMOVED AN D REPLACED BOLT IAW AMM 25-41-41-PB401. 2 L 7 2 4F RT A28NM 2008010400228 20080104 00228 CE 2008 1 4 2G 1 20071129 A 3246 BEARING RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP NLG WHEEL LACK OF LUBE B ODAR A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 21 2G 258354 PILOT REPORTED NOSE WHEEL VIBRATION AFTER TAKEOFF ROTATION DURING CLIMBOUT. AIRCRAFT DIVERTED TO HOME BASE. NO REPORTED VIBRATION DURING TAKEOFF OR LANDING ROLL OUT. REMOVED LT AND RT NOSE WHEEL ASSEMBLIES. BALANCED LT AND RT NOSE WHEELS, I NSPECTED AND REPACKED NOSE WHEEL BEARINGS. 2 L 7 2 4F 4 F RT A3EU E6WE 2008010400230 20080104 00230 CE 2008 1 4 V6N2007F00000 1 20071118 A 2810 FUEL LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP CONTAMINATED E V6NA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 19 556HJ 028 DURING CRUISE AFTER DEPARTMENT, CREW NOTICED A REDUCTION IN FUEL FLOW TO BOTH ENGINES. UNEVENTFUL LANDING MADE. UPON D EPARTURE, NEITHER ENGINE WAS ABLE TO MAKE TARGET N1. FUEL WAS SUMPED AND CHECKED FOR CONTAMINATION, NO SIGNIFICATE RESU LTS NOTED. POWER ASSURANCE PERFORMED AND TARGENT N1 WAS MET FOR BOTH ENGINES. AFTER DEPARTURE DURING CLIMB OUT REDUCT ION IN FUEL FLOW FOR BOTH ENGINE WAS NOTED AND AC RETURNED WITH UNEVENTFUL LANDING. SUBSEQUENT MAINTENANCE PERFORMED : COMPLETELY DRAIN FUEL SYSTEM AND SUMPS, INSPECTED AND REPLACED BOTH ENGINE HIGH PRESSURE FILTERS, INSPECTED (NO MAJOR CO NTAMINATION NOTED), CLEANED AND REINSTALLED BOTH LOW PRESSURE ENGINE FUEL FILTERS (NO MAJOR CONTAMINATION NOTED). DRAIN 2 L 7 2 4F 4 F A10CE E6WE 2008010400231 20080104 00231 SO 2008 1 4 XGN2007F00029 2 20071121 A 8530 TISN712ACA CYLINDER HEAD BEECH 36 36BEECH 1151602 CE CONT O520 IO520BA 17032 SO ENGINE CRACKED E XGNA K NONE O OTHER IN INSP/MAINT 1 SW 05 1194A 901 E159 807201 CYLINDER HEAD CRACKED BEHIND INJECTOR BETWEEN FIN NR1 AND NR 3. 1 L 7 1 3O 3 O 3A15 E5CE 2008010400232 20080104 00232 SO 2008 1 4 XGN2007F00030 2 20071121 A 8530 TISN712ACA CYLINDER HEAD BEECH 36 36BEECH 1151602 CE CONT O520 IO520BA 17032 SO ENGINE CRACKED E XGNA K NONE O OTHER IN INSP/MAINT 1 SW 05 1194A 785 E159 807201 CYLINDER HEAD CRACKED BEHIND INJECTOR BETWEEN 1ST AND 3RD FING. SAME AS ALL THE OTHERS! THE (NEW E-SERIES) CYLINDER HEA D IS DEFECTIVE AND MFG KNOWS IT AND THEY KEEP SELLING THEM. (K) 1 L 7 1 3O 3 O 3A15 E5CE 2008010400233 20080104 00233 SO 2008 1 4 UG8A07GM12041 1 20071205 A 3150 WARNING SYSTEM GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE FALSE ACTIVATION E UG8A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 23 5101 550 CREW RECEIVED A CAS (AIRCRAFT CONFIG) MESSAGE DURING THE TAKEOFF ROLL. THE LOADING AND WEIGHT OF THE AIRCRAFT REQUIRED THE PITCH TRIM TO BE SET, IAW THE AFM AT THE 8 DEGREE LIMIT. IF SET AT THIS LIMIT NORMAL SYSTEM COULD CAUSE THE CONFIG WARNING TO ANNUNCIATE. THE CREW RETURNED TO THE RAMP AND RESET THE TRIM IAW AFM PROCEDURES AND CONDUCTED A NORMAL TAKE OFF WITH NO FURTHER PROBLEMS NOTED. 2 L 7 2 4F 4 F RT A12EA E00057EN 2008010400234 20080104 00234 CE 2008 1 4 GUUA12040701 1 20071204 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 218YV UE218 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT OB ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED RT OB ELEVATOR HINGE BRACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 2008010400235 20080104 00235 NM 2008 1 4 ANCF200700030 1 20071204 A 3150 WARNING SYSTEM DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE FALSE ACTIVATION W ANCF C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 23 632CT 49632 DURING ROLL T/O FLAPS CONFIGURATION ALARM SOUNDS WITH THE FLAPS T/O SELECTOR IN TO POSITION AT 60 KTS. IAW AMM 27-53-01 PAG 201. FLAPS WARNING SWITCH CHECK AND TEST WERE EFECTUATED. FAULT NOT DUPLICATED. 2 L 7 2 4F 4 F RT E9NE 2008010400238 20080104 00238 NE 2008 1 4 HAEA200700203 2 20071207 A 7200 CF7002D2 ENGINE AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D2 30010 NE RIGHT FOD E HAEA A UNSCHED LANDING C R J F.O.D. PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 05 977TW 12969 904 13 304319B DEPARTED BIS CLIMBING THROUGH 3000 FT, RT ENGINE LOST POWER. CREW REQUESTED VECTOR TO RETURN TO BLOCKS. ON DECENT RT ENG INE POWER WAS AVAILABLE. AIRCRAFT LANDED WITH OUT INCIDENT. RT ENGINE FOD'D DUE TO ICE INGESTION AND REQUIRES ENGINE CHA NGE. [CLOSED] 2 L 7 2 4F 4 F A7EU E7EA 2008010700006 20080107 00006 NM 2008 1 7 MWEA070306 1 20071107 A 5260 59137961 STRUCTURE DOUG MD88 MD88 3023688 NM AIRSTAIR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 601ME 49762 FOUND DAMAGE ON THE UPPER FORWARD OF THE FORWARD AIRSTAIR. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 2008010700022 20080107 00022 NM 2008 1 7 2007UALA05132 1 20071215 A 3350 767 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 308UA 23669 RIGHT OVERWING EMERGENCY LIGHT INOP. FOUND LAMP BURNED OUT. LAMP REPLACED. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010700027 20080107 00027 NM 2008 1 7 2007UALA05137 1 20071214 A 3350 POWER SUPPLY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 526UA 24994 SEATS 9ABC THRU 21ABC EMERGENCY LIGHTS INOP. FOUND POWER SUPPLY FAULTY. REPLACED POWER SUPPLY M107, OPS CHECKED NORMA LLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700029 20080107 00029 NM 2008 1 7 2007UALA05139 1 20071214 A 3350 SIGN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT OVERWING SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 526UA 24994 L4 LEFT OVERWING AND R4 EXTERNAL EMERGENCY LIGHTS INOP. FOUND SIGN AT L4 LEFT O/W DOOR SHORTED INTERNALLY. REPLACED SIGN AT LEFT O/W DOOR, OPS TESTED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700046 20080107 00046 NM 2008 1 7 2007UALA05160 1 20071218 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 SEAT 4E EEL LIGHT INOPERATIVE. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700049 20080107 00049 NM 2008 1 7 2007UALA05161 1 20071219 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN MISSING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 513UA 24810 EMERGENCY FLOOR LIGHTING AT ROWS 28-30 LOOSE & INTERNAL LIGHTING STRIP MISSING. APPROX 80 INCHES OF LIGHT STRIP IS MISS ING. APPEARS TO BE RIPPED OUT. REPAIRED EEL STRIP, OPS TEST GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700055 20080107 00055 NM 2008 1 7 2007UALA05167 1 20071218 A 5210 285W0955102 BATTERY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE R2 DOOR MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 779UA 26941 2R PAX DOOR EPAS BATTERY INSTALLED UPSIDE DOWN. REPOSITIONED EPAS BATTERY. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008010700060 20080107 00060 NM 2008 1 7 2007UALA05172 1 20071219 A 5320 STIFFENER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NLG WW CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 LEFT VERTICAL STIFFENER IN NOSE WHEEL WELL, BS 287, HAS ONE HALF INCH CRACK IN THE RADIUS. CRACK BEGINS 11.375 INCHES F ROM NWW UPPER CEILING WEB. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010700069 20080107 00069 2008 1 7 2007UALA05183 4 20071219 A 2565 CYLINDER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE DEFECTIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 RIGHT OVERWING ESCAPE SLIDE CYLINDER DEPLOYMENT CABLE BALL IS BELOW SPRING FORCE RETAINER. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010700076 20080107 00076 NM 2008 1 7 2007UALA05191 1 20071221 A 5330 65C32355 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 941UA 42602 26676 EXTERNAL FUSELAGE SKIN HAS SUB-SURFACE CRACK INDICATION AT STR 10L BETWEEN STA 433-434. MAJOR REPAIR ACCOMPLISH PER AMM 53-31-96 FIG 602. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010700089 20080107 00089 NM 2008 1 7 2007UALA05206 1 20071220 A 2421 IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LACK OF LUBE A UALA O OTHER W INADEQUATE Q C AP APPROACH 1 WP 29 543UA 25698 IDG DISCONNECTED DURING APPROACH. FOUND IDG SHUTDOWN DUE TO LOW OIL QTY. UNKNOWN AS TO REASON OF OIL LOW QTY. SERVICE D IDG TO FULL. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700092 20080107 00092 NM 2008 1 7 USAA920071358 1 20071114 A 5310 DOOR FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, AFT CARGO COMPARTMENT DOOR CUTOUT AFT FRAME CRACKED, BS 847, S20R. REPLACED AFT CARGO C OMPARTMENT DOOR CUTOUT AFT FRAME, BS 847, S20R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008010700093 20080107 00093 NM 2008 1 7 USAA920071359 1 20071104 A 5310 654797321 CREASE BEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CRACKED LEFT CREASE BEAM WEB, BS 616 - BS 639. REPLACED LEFT CREASE BEAM WEB, BS 616 - BS 639 IAW USAIRWAYS EA 10058. 2 L 7 2 4F RT A16WE 2008010700095 20080107 00095 NM 2008 1 7 USAA920071361 1 20071104 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT BEAM, BS 727D, LBL 10. REPAIRED AFT CA RGO COMPARTMENT FLOOR SUPPORT BEAM, BS 727D, LBL 10 IAW USAIRWAYS EA 100061. 2 L 7 2 4F RT A16WE 2008010700097 20080107 00097 NM 2008 1 7 USAA920071363 1 20071104 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT BEAM, BS 727D, LBL 2. REPAIRED AFT CAR GO COMPARTMENT FLOOR SUPPORT BEAM, BS 727D, LBL 2 IAW USAIRWAYS EA 100061. 2 L 7 2 4F RT A16WE 2008010700103 20080107 00103 NM 2008 1 7 USAA920071364 1 20071104 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT BEAM, BS 727D, RBL 2. REPAIRED AFT CAR GO COMPARTMENT FLOOR SUPPORT BEAM, BS 727D, RBL 2 IAW USAIRWAYS EA 100061. 2 L 7 2 4F RT A16WE 2008010700105 20080107 00105 NM 2008 1 7 USAA920071365 1 20071104 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT BEAM, BS 727D, RBL 7. REPAIRED AFT CAR GO COMPARTMENT FLOOR SUPPORT BEAM, BS 727D, RBL 7 IAW USAIRWAYS EA 100061. 2 L 7 2 4F RT A16WE 2008010700108 20080107 00108 NM 2008 1 7 USAA920071366 1 20071115 A 2560 ACREM1A MEGAPHONE BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 155AW 23777 CLT - EMERGENCY EVACUATION EQUIPMENT - C18, AFT MEGAPHONE INOPERATIVE. REPLACED AFT MEGAPHONE. 2 L 7 2 4F RT A16WE 2008010700114 20080107 00114 SO 2008 1 7 RAIA00712018 1 20071212 A 3020 WARNING SYSTEM EMB 145 EMB145 3260210 SO COCKPIT ACTIVATED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 821HK 145068 FLT NR 5477 - IND - DURING TAKEOFF ENGINE REFERENCE ANTI-ICE DISAGREE MESSAGE APPEARED. MAINTENANCE DEFERRED PER MEL. 2 L 7 2 4F RT T00011AT 2008010700116 20080107 00116 SO 2008 1 7 RAIA00712019 1 20071212 A 3610 SEAL EMB 145 EMB145 3260210 SO BLEED AIR SYS WORN A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 812HK 145373 FLT NR 5564 - OKC - ENGINE BLEED 1&2 LEAK IN ICING CONDITIONS. MAINTENANCE FOUND SEALS AND CLAMP WORN. REMOVED AND REP LACED CLAMP AND SEALS. 2 L 7 2 4F RT T00011AT 2008010700118 20080107 00118 SO 2008 1 7 RAIA00712015 1 20071212 A 5230 DOOR SEAL EMB 145 EMB145 3260210 SO CARGO DOOR LEAKING A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 816HK 145055 FLT NR 5535 - STL - CABIN ALTITUDE EXCEEDED 8000 FT. AS AIRCRAFT PASSED THRU 15000 FT (MAN MODE PRESS INOP). MAINTENAN CE REMOVED AND REPLACED CARGO DOOR RUBBER TRIM PERFORMED PRESSURIZATION CHECK, SYSTEM TEST GOOD. 2 L 7 2 4F RT T00011AT 2008010700119 20080107 00119 SO 2008 1 7 RAIA00712017 1 20071212 A 3610 DUCT EMB 145 EMB145 3260210 SO BLEEED AIR SYS LOOSE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 812HK 145373 FLT NR 5564 - OKC - BLEED 1 & 2 LEAK. MAINTENANCE RESECURED DUCT CHECK GOOD. 2 L 7 2 4F RT T00011AT 2008010700121 20080107 00121 SO 2008 1 7 RAIA00712016 1 20071212 A 3350 RPS1B BATTERY PACK EMB 145 EMB145 3260210 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 834HK 145269 PRE FLT NR 7882 - STL - SERVICE DOOR FLOOD LIGHT, SERVICE DOOR EXIT IDENTIFIER, AISLE FLOOD LIGHTS INOP. MAINTENANCE RE MOVED AND REPLACED NR 2 EMERGENCY BATTERY PACK, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2008010700123 20080107 00123 SO 2008 1 7 RAIA00712020 1 20071212 A 3350 RPS1B BATTERY EMB 145 EMB145 3260210 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 847HK 14500857 REP FLT NR 8065 - ORD - FORWARD OVERHEAD FLOOD LIGHT INOP. MAINTENANCE REMOVED AND REPLACED NR 1 EMERGENCY BATTERY SUPP LY, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2008010700125 20080107 00125 SO 2008 1 7 RAIA00712022 1 20071215 A 3350 3025103 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 847HK 14500857 PRE FLT NR 8010 - STL - EMERGENCY LIGHT AISLE FLOOD LIGHT INOP. MAINTENANCE REMOVED AND REPLACED LEFTHAND LIGHT ASSY. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2008010700126 20080107 00126 2008 1 7 UPS07851311 4 20071210 A 2565 SLIDE DOUG DC8 DC871F 302199D WP PAX DOOR DISLODGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 ENTRY DOOR OPENED FROM OUTSIDE A/C BY LOAD SUP. SLIDE FELL OUT OF PACK, DID NOT INFLATE. REINSTALLED SLIDE AS REQUIRED IAW MM 25-60-01-2 2 L 7 4 4F RT 4A25 2008010700127 20080107 00127 NM 2008 1 7 UPS07M51314 1 20071116 A 3350 BATTERY DOUG MD11 MD11F 3023600 NM EMERGENCY LIGHTS NO TEST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 279UP 48573 INSPECTION EMERGENCY LIGHTS BAT (1) LOW LIGHT ILLUMINATES DURING EMERGENCY LIGHTS TEST. RE-TEST EMERGENCY LIGHTS AFTER 30 MINUTES. SATIS PER AMM 33-50-00-5. 2 L 7 3 4F RT A22WE 2008010700128 20080107 00128 EU 2008 1 7 07FDEA05079 1 20071218 A 5320 TRACK AIRBUS 300 A300B4622 3930401 EU MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 718FD 365 PREVIOUS ANGLE REPAIR LOCATED AT AFT CARGO ROLLER TRACK NR 1 LEFT Y140 BETWEEN FRAMES 57.3 AND 58 HAS 2 EA. REPAIR AN GLES MEASURING 7.4 IN LONG 1 EA. REPAIR SECTION MEASURING 8.2 IN LONG AND 1 EA. REPAIR DOUBLER ON BOTTOM SURFACE MEASU RING 8.3 BY 6.3 IN. PREVIOUS REPAIR FOUND NOT TO BE IAW A300-600 SRM 53-10-15 PARA 5 PAGES 207-212 FIG 203. REMOVED AN D REPLACED REPAIR WITH CORRECT REPAIR IAW A300-600 SRM 53-10-15 PARA 5 PAGES 207-212 FIG 203. THIS IS A REPAIR WITH NO AIRBUS ISSUED PART NUMBER , REPAIR IDENTIFIED BY THE AGING A/C INSP . 2 L 7 2 4F RT A35EU 2008010700129 20080107 00129 EU 2008 1 7 07FDEA05080 1 20071218 A 5320 TRACK AIRBUS 300 A300B4622 3930401 EU MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 718FD 365 PREVIOUS ANGLE REPAIR LOCATED ON AFT CARGO ROLLER TRACK NR 3 LT Y 1470 BETWEEN FRAMES 55 AND 56 HAS 2 EA. REPAIR ANGLES MEASURING 7.1 IN LONG , 1 EA. REPAIR SECTION MEASURING 7 IN LONG AND 1 EA. REPAIR DOUBLER ON BOTTOM SURFACE MEASURING 6.8 BY 6.3 IN. PREVIOUS REPAIR FOUND NOT TO BE IAW A300-600 SRM 53-10-15 PARA 5 PAGES 207-212 FIG 203. REMOVED AND REP LACED REPAIR WITH CORRECT REPAIR IAW A300-600 SRM 53-10-15 PARA 5 PAGES 207- 212 FIG 203. THIS IS A REPAIR WITH NO AIR BUS ISSUED PT NO. REPAIR IDENTIFIED BY THE AGING AIRCRAFT PROGRAM. 2 L 7 2 4F RT A35EU 2008010700130 20080107 00130 SO 2008 1 7 RAIA00712023 1 20071216 A 3350 66901 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 834HK 145269 PRE FLT NR 7916 - STL - EMERGENCY LIGHT FLOOR PROXIMITY LIGHT INOP. MAINTENANCE INSTALLED NEW FLOOR LIGHT STRIP, CHECK GOOD. 2 L 7 2 4F RT T00011AT 2008010700131 20080107 00131 EU 2008 1 7 07FDEA05081 1 20071218 A 5320 TRACK AIRBUS 300 A300B4622 3930401 EU MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 718FD 365 PREVIOUS ANGLE REPAIR LOCATED ON AFT CARGO ROLLER TRACK NR 2 LT Y805 BETWEEN FRAMES 55 AND 56 HAS 2 EACH REPAIR ANGLES MEASURING 5.5 IN LONG, 1 EA. REPAIR SECTION MEASURING 9.7 IN LONG AND 1 EA DOUBLER ON BOTTOM SURFACE MEASURING 8.5 BY 6 .3 IN. PREVIOUS REPAIR FOUND NOT TO BE IAW A300-600 SRM 53-10-15 FIG 203. REMOVED AND REPLACED REPAIR WITH CORRECT REP AIR IAW A300-600 SRM 53-10-15 FIG 202. THIS IS A REPAIR WITH NO AIRBUS PT NUMBER, REPAIR IDENTIFIED BY THE AGING AIRCRA FT INSPECTION PROGRAM. 2 L 7 2 4F RT A35EU 2008010700132 20080107 00132 EU 2008 1 7 07FDEA05082 1 20071218 A 5320 TRACK AIRBUS 300 A300B4622 3930401 EU MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 718FD 365 PREVIOUS ANGLE REPAIR LOCATED ON AFT CARGO ROLLER TRACK NR 3 RIGHT Y1470 BETWEEN FRAMES 56 AND 57 HAS 2 EACH REPAIR AN GLES MEASURING 7.1" LONG, 1 EACH. REPAIR SECTION MEASURING 13" LONG AND 1 EACH REPAIR DOUBLER ON BOTTOM SURFACE MEASURI NG 7" BY 6.3". PREVIOUS REPAIR FOUND NOT TO BE IAW A300-600 SRM 53-10-15 FIG 203. REMOVED AND REPLACED REPAIR WITH COR RECT REPAIR IAW A300-600 SRM 53-10-15 FIG. 202. THIS IS A REPAIR WITH NO AIRBUS ISSUED PART NUMBER. REPAIR IDENTIFIED BY THE AGING AIRCRAFT INSPECTION PROGRAM. 2 L 7 2 4F RT A35EU 2008010700133 20080107 00133 EU 2008 1 7 07FDEA05084 1 20071218 A 5320 TRACK AIRBUS 300 A300B4622 3930401 EU MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 718FD 365 PREVIOUS ANGLE REPAIR LOCATED ON AFT CARGO ROLLER TRACK NR 3 RIGHT Y1470 BETWEEN FRAMES 57.3 ABD 58 HAS 2 EACH REPAIR ANGLES MEASURING 7.1" LONG, 1 EACH. REPAIR SECTION MEASURING 8.8" LONG AND 1 EACH REPAIR DOUBLER ON BOTTOM SURFACE MEAS URING 7.3" BY 6.3". PREVIOUS REPAIR FOUND NOT TO BE IAW A300-600 SRM 53-10-15 PARA 5 PAGES 207 THRU 212 FIG 203. REMOV ED AND REPLACED REPAIR WITH CORRECT REPAIR IAW A300-600 SRM 53-10-15 PARA 5 PAGES 207 THRU 212 FIG 203. THIS IS A REPAI R WITH NO AIRBUS PART NUMBER. REPAIR IDENTIFIED BY THE AGING AIRCRAFT INSPECTION PROGRAM. 2 L 7 2 4F RT A35EU 2008010700134 20080107 00134 EU 2008 1 7 07FDEA05085 1 20071218 A 5320 TRACK AIRBUS 300 A300B4622 3930401 EU MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 718FD 365 PREVIOUS ANGLE REPAIR LOCATED ON AFT CARGO ROLLER TRACK NR 3 RIGHT Y1470 BETWEEN FRAMES 55 AND 56 HAS 2 EACH ANGLES ME ASURING 7.1" LONG, 1 EACH REPAIR SECTION MEASURING 7" LONG AND 1 EACH REPAIR DOUBLER ON BOTTOM SURFACE MEASURING 7.5" BY 6.3". PREVIOUS REPAIR FOUND NOT TO BE IAW A300-600 SRM 53-10-15 FIG 203. REMOVED AND REPLACED REPAIR WITH CORRECT REP AIR IAW A300-600 SRM 53-10-15 PARA 5 PAGES 207 THRU 212 FIG 203. THIS IS A REPAIR WITH NO AIRBUS ISSUED PART NUMBER. R EPAIR INDENTIFIED BY THE AGING AIRCRAFT INSPECTION PROGRAM. 2 L 7 2 4F RT A35EU 2008010700135 20080107 00135 NM 2008 1 7 07FDEA05086 1 20071219 A 5340 652617328 ATTACH ANGLE BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 FWD LAV, I/B WALL, ATTACH ANGLE FROM WALL TO FLOOR STRUCTURE IS CRACKED, BS 315, RBL 15. REMOVED CRACKED ANGLE AND FABR ICATED NEW SUPPORT ANGLE REF DWG 65-26173 AND SRM 51-30-2 PG 3. TREATED AND PRIMED AND APPLIED TOP COAT TO NEW ANGLE R EF SRM 51-10-2 PG 1. INSTALLED SUPPORT ANGLE AT BS 315M RBL 15, REF SRM30-2 PG , THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008010700136 20080107 00136 NM 2008 1 7 07FDEA05087 1 20071219 A 5320 6517593 PAN BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 CORROSION AROUND ATTACH FWD AND UNDER EDGES OF LAV SINK CABINET FLOOR PAN, BS 304 TO BS 315, RBL 13 TO RBL 41, WL 208. REMOVED CORRODED FLOOR PAN AND FABRICATED NEW PAN REF SRM 51-30-2 PG 3, AND SRM 53-20-1 PG 5 AND 12. TREATED AND PRIMED AND APPLIED TOP COAT TO PAN REF SRM 51-10-2 PG 1. INSTALLED NEW FLOOR PAN, BS 304, RBL 13- RBL 41 REF SRM 51-30-02 PG 2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008010700137 20080107 00137 NM 2008 1 7 GTIA200700034 1 20071203 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 520NK 2784 FLOORBEAM Y-512.2 AT APPROX FRAME 69 CORRODED. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2008010700138 20080107 00138 NM 2008 1 7 GTIA200700035 1 20071216 A 3350 77233800 EPSU AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 502NK 549 2433 L2 AND R2 EMERGENCY EXIT LIGHTS INOP ON GROUND. REMOVED AND REPLACED AFT (13WL) EPSU. 2 L 7 2 4F RT A28NM 2008010700139 20080107 00139 NM 2008 1 7 HNAA0700297 1 20071219 A 6123 AUTOFEATHER SYS DHAV DHC8 DHC8102 2809003 NM MALFUNCTIONED A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 911HA 034 AUTO FX DID NOT ARM ON TAKEOFF ROLL, REJECTED TAKEOFF. C/W AUTO FEATHER OPS CK IAW RUN UP MANUAL, OPS NORMAL. CLEANED AND INSPECTED SWITCHES 6121-57, 59, 513, 56, 512, 58, NO DEFECTS NOTED. 2 H 7 2 4T RT A13NM 2008010700140 20080107 00140 NM 2008 1 7 NWAA074156307 1 20071109 A 5330 SKIN BOEING 747 747451 1384940 NM BS 1480 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 667US 24222 DURING "M" CHECK WHILE ACCOMPLISHING SB 747-53A2390, FOUND CRACK IN LEFT SKIN PANEL LAYER AT BS 1480 HOLE NR 11. REPAIR ED PER EA 63-211311. 2 L 7 4 4F RT A20WE 2008010700141 20080107 00141 NM 2008 1 7 NWAA074166307 1 20071204 A 5320 SILL BOEING 747 747451 1384940 NM BS 1990 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 667US 24222 DURING "M" CHECK, FOUND CORROSION THE UNDERSIDE OF OUTBOARD FLANGE OF BULK CARGO LOWER MAIN SILL CHORD AT BS 1990. REPA IRED PER EA 63-211345. 2 L 7 4 4F RT A20WE 2008010700142 20080107 00142 SO 2008 1 7 RAIA00712024 1 20071217 A 3397 WIRE EMB 145 EMB145 3260210 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 841HK 145382 PRE FLT NR 8058 - ORD - EMERGENCY LIGHT AFT SIDE AFT CEILING EXIT LOCATOR INOP. MAINTENANCE SECURED LOOSE WIRES, OPS CH ECK GOOD. 2 L 7 2 4F RT T00011AT 2008010700144 20080107 00144 EA 2008 1 7 TRAX200701919 1 20071212 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 903EV 7621 CLIP CRACKED O/B OF RBL 27, RESOLVED ON W/O: 77977 TASKCARD: N/R-00281. REMOVED CRACKED FS 484 RBL 27O/B CLIP. FABRICA TED SERVICEABLE CLIP FROM S6144-3 ANGLE IAW CRJ SRM 53-41-43. OK TO ALODINE, PRIME, AND TOPCOAT. INSTALLED SERVICEABLE CLIP IAW CRJ SRM 51-42-21 JM 14031. OK TO TOPCOAT FASTENERS. APPLIED TOPCOAT TO FASTENERS IAW CRJ 200 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2008010700145 20080107 00145 EA 2008 1 7 TRAX200701943 1 20071216 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 916EV 7757 EMERGENCY EXIT LIGHT AT THE SERVICE DOOR DOES NOT WORK. 2 L 7 2 4F RT A21EA 2008010700146 20080107 00146 EA 2008 1 7 TRAX200701944 1 20071216 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 916EV 7757 EMERGENCY EXIT FLOOR LIGHTS AT THE AFT CABIN SECTION DOES NOT WORK. 2 L 7 2 4F RT A21EA 2008010700147 20080107 00147 EA 2008 1 7 TRAX200701945 1 20071216 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 EMERGENCY EXIT LIGHT ON WARDROBE HAS 1 BULB INOP. 2 L 7 2 4F RT A21EA 2008010700148 20080107 00148 EA 2008 1 7 TRAX200701946 1 20071216 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 CABIN EMERGENCY EXITS LIGHTS HAS 1 BULB INOP. 2 L 7 2 4F RT A21EA 2008010700149 20080107 00149 EA 2008 1 7 TRAX200701947 1 20071216 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 903EV 7621 FS 280 FWD UPPER ANGLE HAS CORROSION. 2 L 7 2 4F RT A21EA 2008010700150 20080107 00150 EA 2008 1 7 TRAX200701948 1 20071216 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 907EV 7648 REAR PRESSURE BULKHEAD CRACK UNDER LINEAR FITTING OF CARGO DOOR SURROUNDING STRUCTURE, REO 601R-53-61-1230 TO BE C/OUT. 2 L 7 2 4F RT A21EA 2008010700151 20080107 00151 EA 2008 1 7 TRAX200701949 1 20071216 A 3210 PIN CNDAIR CL600 CL6002B19 1900309 EA LT MLG CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 907EV 7648 LT GEAR SIDE STAY PIN CORRODED. 2 L 7 2 4F RT A21EA 2008010700152 20080107 00152 NM 2008 1 7 NOCA17207 1 20071219 A 2750 7321870018 SHUTOFF VALVE BOEING 767 76739H 1385311 NM T/E FLAP MALFUNCTIONED A NOCA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 760NA 26257 AFTER BOTH ENGINES STARTED FLAP HANDLE MOVED TO 5 STATUS MESSAGE FLAP/SLAT ELEC. REPLACED FLAP/SLAT SHUT OFF VALVE AS P ER MM 27-51-48, OPS CHECK OK. 2 L 7 2 4F RT A1NM 2008010700153 20080107 00153 EA 2008 1 7 TRAX200701950 1 20071216 A 7830 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER ILLUMINATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 933EV 8022 FLT 4501 DEL 133 MINS, R THRUST REVERSER UNLOCKED CAUTION MSG INFLIGHT, A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLAR ED. 2 L 7 2 4F RT A21EA 2008010700154 20080107 00154 EA 2008 1 7 TRAX200701951 1 20071216 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 978EV 7723 EMERGENCY LIGHT ON AFT CIELING INOP. 2 L 7 2 4F RT A21EA 2008010700155 20080107 00155 WP 2008 1 7 07FDEA05107 1 20071220 A 5330 NGA6313503 SKIN DOUG DC10 DC1030 3023501 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 EXT FUSELAGE LWR SKIN FOUND 2 EA DEEP DENT: 6 INCH BY 2" THE WIDTH OF THE DENT IS APPROX .09", 7" BY 2" THE WIDTH OF THE DENT IS APPROX 09". 2 L 7 3 4F A22WE 2008010700156 20080107 00156 NM 2008 1 7 07FDEA05108 1 20071220 A 5320 65261733 CHANNEL BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 FORWARD LAV SUPPORT STRUCTURE STA 303 TO 306, RBL 15, HAT CHANNEL CORRODED ON LOWER SURFACE REMOVED CORRODED HAT CHANNEL , FABRICATED NEW CHANNEL, TREATED AND PRIMED AND INSTALLED. REF SRM 51-30-2 AND BAC DWG 65-26173. THIS IS CLASSIFIED A S A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008010700157 20080107 00157 EA 2008 1 7 SWIA200718965 1 20071217 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FALSE INDICATION A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 983SW 7961 FLT 6730 - "SMOKE TOILET" INDICATION AFTER DEPARTURE. INSPECTED SMOKE DETECTOR AND GARBAGE CANS WITH NO SIGNS OF SMOKE. NO FAULT FOUND. 2 L 7 2 4F RT A21EA 2008010700158 20080107 00158 EA 2008 1 7 SWIA200718966 1 20071217 A 3240 BRAKE ASSY CNDAIR CL600 CL6002D24 1390016 EA NR 4 WORN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 817SK 15107 FLT 4017 - BRAKES ARE DIFFICULT TO MODULATE. REPLACED NR 4 BRAKE ASSEMBLY IAW MM 32-43-26, PN 90001201, SN OFF SEP06- 0539. 2 L 7 2 4F RT A21EA 2008010700159 20080107 00159 SO 2008 1 7 SWIA200718967 1 20071214 A 5753 BRACKET EMB 120 EMB120ER 3260203 SO LT TE FLAP CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 308SW 120326 FLT 5490 - LEFT OUTBOARD FLAP, INBOARD ROLLER BRACKET IS CRACKED. REPLACED LEFT OUTBOARD FLAP, INBOARD ROLLER ASSEMBLY AS NEEDED IAW 51-40-02. 2 L 7 2 4T RT A31SO 2008010700160 20080107 00160 NM 2008 1 7 SB07110 1 20071222 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 453UW 24980 CLT - MAINTENANCE REPORTED THE AFT LEFT EMERGENCY LIGHT BATTERY PACK INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2008010700161 20080107 00161 EA 2008 1 7 SWIA200718968 1 20071217 A 3310 LIGHT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT SHORTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 709SK 10159 FLT 5832 - FIRST OFFICERS MAP LIGHT IS SHORTED. RESET CIRCUIT BREAKER AND INSPECTED CHART HOLDER. NO DISCREPENCIES NOT ED. 2 L 7 2 4F RT A21EA 2008010700162 20080107 00162 SO 2008 1 7 SWIA200718969 1 20071212 A 2133 2091G010800 OUTFLOW VALVE EMB 120 EMB120ER 3260203 SO CABIN PRESSURE MALFUNCTIONED A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 582SW 15140 15140 120350 FLT 5712 - DURING CLIMB, OXYGEN MASKS DROPPED. REPLACED ELECTROPNEUMATIC OUTFLOW VALVE IAW MM 21-30-03. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2008010700163 20080107 00163 EA 2008 1 7 SWIA200718970 1 20071218 A 2910 LINE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 416SW 7089 FLT 3826 - ON TAXI OUT, HYDRAULIC PAGE SHOWED 0 PERCENT QUANTITY ON NR 2 SYSTEM. REPLACED PRESSURE LINE IN RIGHT PYLON. LEAK AND OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008010700164 20080107 00164 EA 2008 1 7 SWIA200718971 1 20071218 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER AP APPROACH 1 NM 07 913EV 7731 FLT 3775 - RIGHT SIDE WINDOW CRACKED ON APPROACH. REPLACED SIDE WINDOW PER AMM 56-12-00, P/N: 601R139322-12, S/N OFF: 2252H5478. 2 L 7 2 4F RT A21EA 2008010700165 20080107 00165 EA 2008 1 7 SWIA200718972 1 20070901 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 980SW 7955 FOUND AT C-CHECK, STA 484 RBL 27 HAS A CRACK AT INBOARD CLIP. REPAIRED PER CRJ200 REO 601R-53-41-059 REV A. 2 L 7 2 4F RT A21EA 2008010700166 20080107 00166 EA 2008 1 7 SWIA200718973 1 20070901 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 980SW 7955 FOUND AT C-CHECK, STA 621 LOWER FLOOR ANGLE IS CRACKED AT CORNER. REPAIRED PER REO 601R 53-61-117. 2 L 7 2 4F RT A21EA 2008010700167 20080107 00167 EA 2008 1 7 SWIA200718974 1 20070901 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 980SW 7955 LEFT SIDE STA 621 LOWER FLOOR ANGLE IS CRACKED AT CORNER, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO 601R 53-61-1 17 REV C. 2 L 7 2 4F RT A21EA 2008010700168 20080107 00168 NM 2008 1 7 USAA920071367 1 20071212 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 451UW 24934 PIT - MAJOR REPAIR - FWD PRESSURE BULKHEAD INSP, FOUND A CRACK EXTENDING FROM FASTENER ON FWD PRESSURE BULKHEAD AT BS 1 78, WL 234, LBL 8. REMOVED CRACK AREA AND INSTALLED DOUBLER IAW B737-300 SRM 53-10-08 FIG 201, REPAIR 9 AND US AIRWAYS EO 5300V153. 2 L 7 2 4F RT A16WE 2008010700169 20080107 00169 NM 2008 1 7 USAA920071368 1 20071215 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 451UW 24934 PIT - MAJOR REPAIR - FWD PRESSURE BULKHEAD INSP, A CRACK FOUND ON FWD PRESSURE BULKHEAD AT BS 178, WL 234, AND LBL 8.2. REMOVED DAMAGE AND INSTALLED DOUBLER IAW B737-300 SRM 53-10-08, FIG 201, REPAIR 9. 2 L 7 2 4F RT A16WE 2008010700171 20080107 00171 EA 2008 1 7 SWIA200718975 1 20070901 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 980SW 7955 STA 625 RIGHT CLIP IN AFT EQUIPMENT COMPARTMENT IS CRACKED, FOUND AT C-CHECK. INSTALLED PER CRJ200 SRM 51-42-21, 51-25- 16, 51-40-11 AND REO'S 601R-53-61-100 AND 601R-53-61-422. 2 L 7 2 4F RT A21EA 2008010700172 20080107 00172 EA 2008 1 7 SWIA200718976 1 20070901 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 980SW 7955 LEFT SIDE LOWER FLOORBEAM AT STA 280 HAS CRACKS, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 REO 601R-53-11-171 , REV 'D'. 2 L 7 2 4F RT A21EA 2008010700173 20080107 00173 EA 2008 1 7 SWIA200718977 1 20070901 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 980SW 7955 RIGHT SIDE LOWER FLOORBEAM AT FS 280 HAS A CRACK, FOUND AT C-CHECK. INSTALLED REPAIRS AT FS 280 RBL9 PER CRJ200 REO 601 R-53-11-171 REV D. 2 L 7 2 4F RT A21EA 2008010700175 20080107 00175 NM 2008 1 7 NWAA074173138 1 20071219 A 5320 SILL AIRBUS A319 A319114 3930350 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 338NB 1693 DURING "H" CHECK, FOUND CORROSION ON FORWARD END OF RT AFT PASSENGER DOOR SILL. REPAIRED PER EA 31-211439. 2 L 7 2 4F RT A28NM 2008010700177 20080107 00177 NM 2008 1 7 UIEA200700481 1 20071130 A 5755 65B023101 SKIN BOEING 747 747228F 1384895 NM NR 7 SPOILER DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 RIGHT WING SPOILER NR 7 HAS DELAMINATION. DISBONDED UPPER AND LOWER SURFACE 35" BY 25". REMOVED AND REPLACED THE NR 7 SPOILER IAW AMM 27-62-01 OPS CHECKED TRANS TO RUN UP AND LEAK CHECK SHEET 01-AA-74A ITEM NR 3. 2 L 7 4 4F RT A20WE 2008010700178 20080107 00178 NM 2008 1 7 USAA920071372 1 20071223 A 5330 6547955 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 443US 24842 CLT - MAJOR REPAIR - DROP-IN - CORROSION FOUND ON FUSELAGE SKIN AT BS 827, S25R. REMOVED CORRODED AREA AND INSTALLED DO UBLER IAW US AIRWAYS EA 100117. 2 L 7 2 4F RT A16WE 2008010700179 20080107 00179 NM 2008 1 7 UIEA200700498 1 20071208 A 3251 STEERING SYS BOEING 747 747243B 1384830 NM NLG INOPERATIVE A UIEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 540MC 22508 TAKEOFF REJECTED DUE TO T/O WARNING HORN BECAUSE RIGHT BODY GEAR UNLOCKED LIGHT ILLUMINATED ON T/O ROLL. SYSTEM SELECTE D TO PRIMARY MODE. PERFORMED OPS CK OF BODY GEAR STEERING SYSTEM. FOUND RIGHT ALT BODY GEAR ACTUATOR SWITCH INOP. REM OVED AND REPLACED AS PER MM 32-53-16 AND PERFORMED OPS CK AS PER MM 32-53-00 FOUND SATISFACTORY. 2 L 7 4 4F RT A20WE 2008010700181 20080107 00181 NM 2008 1 7 UIEA200700499 1 20071208 A 2740 UNKNOWN BOEING 747 74747UF 1384812 NM STAB TRIM MALFUNCTIONED A UIEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 418MC 32840 UNSCHEDULED STAB TRIM EICAS MESSAGE. RAN CHECKLIST AND REACTIVATED LEFT SIDE AND RIGHT SIDE STAYED OFF. PERFORMED STAB TRIM CONT SYSTEM TEST AS PER AMM TASK 27-41-00-715-007 SYSTEM TEST PASSED. PERFORMED STAB TRIM SYSTEM TRIM TEST TASK 2 2-22-00-745-001 STAB TRIM PASSED. FCC RIGHT BITE TEST PASSED AS PER AMM 22-11-00. VISUAL INSPECTION OF STAB JACK SCREW C/W OPS CHECK GOOD. EICAS MESSAGE CLEARED. AIRCRAFT RELEASED FOR FLIGHT. 2 L 7 4 4F RT A20WE 2008010700182 20080107 00182 NM 2008 1 7 2007UALA04903 1 20071130 A 2197 V350122263011 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN TEMP MISSING A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 584UA 26706 FLIGHT DIVERTED DUE TO CABIN TEMPERATURE PROBLEMS. INDICATION PROBLEMS - FOUND SEGMENT OF AFT CABIN TEMP INDICATION WIR ING MISSING. REPLACED MISSING SEGMENT. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700183 20080107 00183 NM 2008 1 7 UIEA200700504 1 20071217 A 2410 IDG BOEING 747 74747UF 1384812 NM NR 3 CHAFED A UIEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 15 412MC 30559 EICAS MESSAGE "ELEC GEN OFF 3" GCB RESET PER QRH, OPERATION NORMAL MOMENTARILY THEN REOCCURRENCE. DIVERTED TO NRT. FOU ND CHAFF ON NR 3 IDG T2 HARNESS. PERFORMED REPAIR AS PER SWPM 20-10-13 PAGE 41 PART 2T. THIS ITEM MUST BE REPAIRED WIT HIN 500 FLIGHT HOURS. 2 L 7 4 4F RT A20WE 2008010700184 20080107 00184 NM 2008 1 7 2007UALA04911 1 20071202 A 2600 SQUIB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 514UA 24839 THE R ENG SQUIB TEST 1 FAILED. SWAPPED SQUIBS, RESET C/B OPS CHECKED NORMALLY, NO KNOWN CAUSE. NO REPEATS SINCE ORIGIN AL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700185 20080107 00185 NM 2008 1 7 UIEA200700482 1 20071203 A 5610 60B1002812 WINDSHIELD BOEING 747 74747UF 1384812 NM COCKPIT CRACKED A UIEA O OTHER O OTHER CR CRUISE 1 EA 15 498 24659 29259 R1 OUTER WINDOW PANE CRACKED DURING CRUISE. NO OTHER DIFFICULITIES EXPERIENCED, LANDING NORMAL. REPLACED WINDOW ASSY 6 0B100028-12 AFTER LANDING AT DXB IAW MM 56-11-01. RECORDED ON LOG PAGE 249587. 2 L 7 4 4F RT A20WE 2008010700186 20080107 00186 NM 2008 1 7 UIEA200700495 1 20071212 A 5730 PANEL BOEING 747 7472D7B 1384803 NM ZONE 500 DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 LEFT WING UPPER SURFACE PANEL NR 521 HAS EVIDENCE OF DELAMINATION ABOUT 3 INCHES LONG 6 INCHES FORWARD OF THE TRAILING E DGE AND 18 INCHES INBOARD OF THE OUTBOARD EDGE. ALSO AN AREA 3 INCHES LONG 21 INCHES AWAY FROM THE OUTBOARD EDGE AND 5 INCHES AFT OF THE LEADING EDGE. REPAIRED PANEL IAW SRM 51-40-12 AND XEO 57-121207. PERMANENT REPAIR TO BE ACCOMPLISHED AT NEXT C-CHECK. 2 L 7 4 4F RT A20WE 2008010700187 20080107 00187 NM 2008 1 7 UIEA200700489 1 20071212 A 5280 65B1166947 STRUCTURE BOEING 747 747341 13848AM NM MLG DOOR CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 LT WING GEAR INBOARD STRUT DOOR HAS FORWARD EDGE COMPOSITE CRACK. PERMANENT REPAIR ACCOMPLISHED AS PER B747-300 SRM 51- 40-09, FIG 12, SHEETS 1, 2 AND 3. 2 L 7 4 4F RT A20WE 2008010700188 20080107 00188 NM 2008 1 7 UIEA200700494 1 20071212 A 5730 PANEL BOEING 747 7472D7B 1384803 NM ZONE 500 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 LT WING UPPER SURFACE LEADING EDGE TO FRONT SPAR PANEL (BEHIND NR 9 LEADING EDGE FLAP WS 862) HAS 2 INCH CRACK. PANEL R EPAIRED IAW SRM 51-40-9 AND 51-40-12. 2 L 7 4 4F RT A20WE 2008010700189 20080107 00189 NM 2008 1 7 UIEA200700496 1 20071212 A 5730 PANEL BOEING 747 7472D7B 1384803 NM ZONE 500 GOUGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 LEFT WING UPPER SURFACE PANEL NR 521 HAS A CIRCULAR SHAPED GOUGE ABOUT 12 INCHES OUTBOARD OF THE INBOARD EDGE ( 7.5 INCH ES LONG BY 5.5 WIDE). INTERIM REPAIR ACCOMPLISHED IAW SRM 51-40-15 AND XEO 57-121207. 2 L 7 4 4F RT A20WE 2008010700190 20080107 00190 NM 2008 1 7 UIEA200700497 1 20071212 A 5730 PANEL BOEING 747 7472D7B 1384803 NM ZONE 500 DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 LEFT HAND WING UPPER SURFACE PANEL NR 521 HAS EVIDENCE OF DELAMINATION 3 INCHES LONG, 2INCHES AWAY FROM OUTBOARD EDGE AN D 5 INCHES FROM THE LEADING EDGE. REPAIRED PANEL IAW SRM 51-40-12 AT 250 DEGREES AND 26" HG VACUUM AND XEO 57-121207. 2 L 7 4 4F RT A20WE 2008010700192 20080107 00192 NM 2008 1 7 UIEA200700501 1 20071213 A 5311 FRAME BOEING 747 747341 13848AM NM BS 1140 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 FRAME AT STATION 1140 LT HAS A CRACK AT STRINGER 10 AND 10A LOCATION. CRACK AT STR 10A 0.875 INCH LONG AND STR 10 IS 0. 760 INCH LONG. PERMANENT REPAIR ACCOMPLISHED AS PER B747-300 SRM 53-10-04 FIG 123 AND BOEING MESSAGE NUMBER 1-711332103 -6 AND FAA FORM 8100-9. ALSO, REFERENCE ATLAS AIR XEO NR 53-121307. 2 L 7 4 4F RT A20WE 2008010700193 20080107 00193 NM 2008 1 7 UIEA200700502 1 20071213 A 5311 FRAME BOEING 747 747341 13848AM NM BS 1140 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 FRAME AT STATION 1140 RT HAS A CRACK AT STRINGER 10 AND 10A LOCATION. CRACK AT STR 10A 0.500 INCH LONG AND STR 10 IS 0. 750 IN LONG. PERMANENT REPAIR ACCOMPLISHED AS PER B747-300 SRM 53-10-04 FIG 123 AND BOEING MESSAGE NUMBER 1-711332103-6 AND FAA FORM 8100-9. ALSO, REFERENCE ATLAS AIR XEO NR 53-121307. 2 L 7 4 4F RT A20WE 2008010700194 20080107 00194 NM 2008 1 7 2007UALA05210 1 20071222 A 2910 LINE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HYD SYSTEM LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 335UA 24230 RTFL WITH A HYDRAULIC PROBLEM. FOUND GEAR UPLOCK ACTUATOR LINE LEAKING. REPLACED GEAR UPLOCK ACTUATOR LINE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010700195 20080107 00195 NM 2008 1 7 UIEA200700500 1 20071213 A 5310 65B09631614 TENSION TIE BOEING 747 747341 13848AM NM BS 1220 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 TENSION TIE LOCATED AT FUSELAGE STATION 1220 LT SIDE AT STRINGER 9 LOCATION HAS A CRACK. INTERIM REPAIR ACCOMPLISHED AS PER B747-300 SRM 53-10-11, FIG 1 AND BOEING MESSAGE NUMBER 1-711332103-6 AND FORM 8100-9. ALSO, REFERENCE ATLAS AIR XE O NO. 53-121307. 2 L 7 4 4F RT A20WE 2008010700196 20080107 00196 NM 2008 1 7 UIEA200700492 1 20071212 A 5730 PANEL BOEING 747 7472D7B 1384803 NM LT WING DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 LT WING UPPER SURFACE LEADING EDGE TO FRONT SPAR PANEL (BEHIND NR 6 LEADING EDGE FLAP WS 1028) HAS EVIDENCE OF DELAMINAT ION. PANEL REPAIRED IAW SRM 51-40-9 AND 51-40-12. 2 L 7 4 4F RT A20WE 2008010700197 20080107 00197 NM 2008 1 7 2007UALA05211 1 20071222 A 3810 O-RING BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE WATER SYSTEM FAILED A UALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 WP 29 792UA 26934 FLT DIVERTED DUE TO A FAILED WATER SYSTEM. CREW CONCERNED WATER LEAKING INTO CARGO COMPARTMENT WOULD FREEZE. REPLACED WATER LINE O-RING, DRAINED WATER FROM BELLY AND REACTIVATED WATER SYSTEM. WATER SYSTEM REMAINS FULL. OPS CHECK NORMAL LY. REF AMM 38-00-00. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008010700198 20080107 00198 NM 2008 1 7 UIEA200700485 1 20071207 A 5753 65B08548603 ARM BOEING 747 74747UF 1384812 NM LT WING TE FLAP DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 498MC 29259 LEFT WING OUTBOARD AFT FLAP OUTBOARD SWING ARM FORWARD FITTING FOUND DAMAGED. LEFT OUTBOARD AFT FLAP OUTBOARD SWING ARM FWD FITTING AND PIN REPLACED IAW AMM 27-51-06, FLAPS OPS CHECKED OKAY. 2 L 7 4 4F RT A20WE 2008010400218 20080104 00218 NM 2008 1 4 NWAA074106307 1 20071205 A 5330 SKIN BOEING 747 747451 1384940 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 667US 24222 DURING "M" CHECK, FOUND CRACK IN SKIN FASTENER HOLES AND SHORT EDGE MARGIN ON FRAME AT BS 460 BETWEEN S14 AND S16. REPA IRED PER EA 63-211348. 2 L 7 4 4F RT A20WE 2008010400241 20080104 00241 NM 2008 1 4 QXEA200701903 1 20071216 A 5230 502212 DOOR SEAL BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR FAILED A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 415QX 4081 MSO - FLIGHT 2349 - AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF IN MANUAL OR AUTO MODES. RETURNED TO THE FIELD AND ACCO MPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE AFT CARGO DOOR SEAL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 H 7 2 4T RT A13NM 2008010700008 20080107 00008 SO 2008 1 7 RAIA00712008 1 20071209 A 3350 LIGHT EMB 145 EMB145 3260210 SO EXTERIOR UNSECURE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 808HK 145157 PRE FLT NR 3508 - PIT - EMERGENCY LIGHT & COURTESY LIGHT OUTSIDE COCKPIT INOP. MAINTENANCE RESECURED EMERGENCY LIGHT AN D OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2008010700031 20080107 00031 NM 2008 1 7 2007UALA05142 1 20071216 A 2611 S283W6001 SMOKE DETECTOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LAVATORY FAULTY A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 206UA 30212 SMOKE DETECTOR GOING OFF IN LAV AT DOOR 3. SUSPECT INSTALLATION SHORT ADJUSTED SMOKE DETECTOR FOR SENSITIVITY TEST OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008010700036 20080107 00036 NM 2008 1 7 2007UALA05148 1 20071218 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY LIGHT ROW 52 RT INOP. RESECURED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700064 20080107 00064 NM 2008 1 7 2007UALA05178 1 20071220 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 DOOR 5L SLIDE LIGHT INOPERATIVE. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700067 20080107 00067 NM 2008 1 7 2007UALA05181 1 20071219 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 569UA 26677 EEL LIGHT OUT ADJACENT TO FWD GALLEY. REATTACHED ELL LIGHT ASSY- OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700074 20080107 00074 NM 2008 1 7 2007UALA05188 1 20071219 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 227UA 30555 EMERGENCY LIGHT OUT AT SEAT 18C. RELAMPED, CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008010700081 20080107 00081 NM 2008 1 7 2007UALA05196 1 20071220 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 ALL EXTERNAL EMERGENCY EXIT LIGHTS ON RIGHT SIDE OF ACFT INOPERATIVE. REPLACED BATTERY AND CHARGER. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700082 20080107 00082 NM 2008 1 7 2007UALA05197 1 20071220 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 641UA 25091 FLOOR EEL STRIP AT SEATS 13 AND 14 AB INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010700170 20080107 00170 NM 2008 1 7 USAA920071369 1 20071214 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 451UW 24934 PIT - MAJOR REPAIR - FWD PRESSURE BULKHEAD INSP, A CRACK FOUND ON FWD PRESSURE BULKHEAD AT BS 178, WL 218, AND RBL 12. REPAIRED DAMAGE AREA AND INSTALLED DOUBLER IAW B737-300 SRM 53-10-08, FIG 201, REPAIR 9. 2 L 7 2 4F RT A16WE 2008010700180 20080107 00180 NM 2008 1 7 USAA920071373 1 20071104 A 5310 CREASE BEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C-18 CHECK- A CRACK FOUND ON INNER CHORD OF LEFT CREASE BEAM AT ATTACHMENT TO BS 616, LBL 4. REMOV ED DAMAGE AND INSTALLED FABRICATED REPAIR ANGLE IAW US AIRWAYS EA 100058. 2 L 7 2 4F RT A16WE 2008010700200 20080107 00200 NM 2008 1 7 2007UALA05214 1 20071224 A 4900 APU BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE APU BAY CONTAMINATED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 221UA 30552 RTFL DUE TO SMOKE ODOR ON FLIGHT DECK. AFTER LENGTHY TROUBLESHOOTING, DETERMINED ODOR DUE TO OIL SPLASHED IN APU INLET . APU ASSY REPLACED PER AMM49-11-01 PG401. PERFORMED PACK BURNOUT, NO FURTHER REPORT OF ODOR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008010700201 20080107 00201 NM 2008 1 7 UIEA200700483 1 20071210 A 5730 PANEL BOEING 747 7472D7B 1384803 NM RT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 DURING ROUTINE INSPECTION FOUND RT WING L/E FIXED FIBERGLASS PANEL UPPER SURFACE CRACKED LATERAL 4" AT WS 1322. PERMANE NT REPAIRS ACCOMPLISHED IAW SRM 51-40-09 AND 51-40-12. DOCUMENTED ON EO 4757A407. 2 L 7 4 4F RT A20WE 2008010700203 20080107 00203 NM 2008 1 7 UIEA200700484 1 20071210 A 5730 PANEL BOEING 747 7472D7B 1384803 NM LT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 DURING ROUTINE INSPECTION FOUND LT WING L/E FIXED FIBERGLASS PANEL UPPER SURFACE AT WS 577/586 CRACKED LONGITUDINAL AND AT WS 752 PREVIOUS REPAIR DELAMINATED. PERMANENT REPAIRS ACCOMPLISHED IAW 51-40-09 AND 51-40-12, DOCUMENTED ON EO 4757A 406. 2 L 7 4 4F RT A20WE 2008010700204 20080107 00204 NM 2008 1 7 UIEA200700486 1 20071207 A 5753 65B390346 FITTING BOEING 747 74747UF 1384812 NM NR 5 TE FLAP CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 498MC 29259 RIGHT WING NR 5 CANOE FAIRING DRIVE ROD MID FLAP AFT FITTING CRACKED. FITTING REPLACED PER AMM 20-51-01 AND OPS CHECKED OK. 2 L 7 4 4F RT A20WE 2008010700205 20080107 00205 GL 2008 1 7 UIEA200700487 2 20071207 A 7300 CLAMP BOEING 747 74747UF 1384812 NM GE CF6 CF680C2* GL ZONE 600 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 498MC 29259 704864 NR 3 ENGINE FUEL SPRAY NOZZLE MANIFOLD SUPPORT LOOP "P" CLAMPS FOUND DAMAGED AT 1 AND 9 O'CLOCK POSITIONS. REPLACED DAM AGED P CLAMPS AND BOTH LEFT AND RIGHT FUEL SUPPLY MANIFOLDS. 2 L 7 4 4F 4 F RT A20WE E23EA 2008010700207 20080107 00207 NM 2008 1 7 UIEA200700503 1 20071212 A 2740 RVDT BOEING 747 74747UF 1384812 NM STAB TRIM MALFUNCTIONED A UIEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 15 418MC 32840 IN CRUISE STAB TRIM UNSCHEDULED EICAS MSG. RAN QRH 45 MINUTES LATER 2ND EICAS MSG. RAN QRH DISC AUTO PILOT AND DIVERTE D TO SYD. FOUND RIGHT RVDT IN STAB BUZZING AND CRACKING ELECTRICALLY. REPLACED UNIT, OPS CHECK OK. ALSO REPLACED RIGH T FCU AND FCC AS PRECAUTION. 2 L 7 4 4F RT A20WE 2008010700208 20080107 00208 NM 2008 1 7 2007UALA05218 1 20071221 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 AFT PIT "T" CAP CORRODED STA 1197, LBL 34 TO LBL 41. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010700209 20080107 00209 EU 2008 1 7 YENA2007119 1 20071219 A 2612 RAI2800M0706 CONTROL UNIT AIRBUS 320 A320232 3930326 EU FIRE SUPPRESSION FALSE INDICATION A YENA O OTHER J WARNING INDICATION CR CRUISE 1 EA 15 565JB 7933 2031 FLT NR 247, OAK-LGB, SMOKE DISCH AGENT 2, -AGENT2-DISCH, ECAM MESSAGE 30 MINUTES INTO FLIGHT. FWD AGENT SWITCH WAS MOVE D TO AGENT 2. REMOVED AND REPLACED FIRE EXTINGUISHER BOTTLE (4010WX). REMOVED AND REPLACED SDCU (10WQ) PER MM 26-23-41 (4010WX) AND MM 2617-36 (10WQ). ACCOMPLISHED FUNCTIONAL TEST OF THE FIRING CIRCUIT PER MM 26-23-00-05 WITH NO DEFECTS NOTED. CARGO SMOKE DETECTION SYSTEM, OPS CHECK NORMAL PER MM 26-16-00. 2 L 7 2 4F RT A28NM 2008010700211 20080107 00211 EA 2008 1 7 TRAX200701952 1 20071213 A 5510 HINGE PIN CNDAIR CL600 CL6002C10 1390015 EA HORIZONTAL STAB CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 758EV 10210 HORIZ STAB INNER AND BOTH OUTER HINGE PINS SHOW SIGNS OF CORROSION. 2 L 7 2 4F RT A21EA 2008010700212 20080107 00212 2008 1 7 2007UALA05221 4 20071221 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 462UA 1272 NR 1 LT DOOR SLIDE BROKEN. REPLACED SLIDE ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010700213 20080107 00213 EA 2008 1 7 TRAX200701953 1 20071217 A 2560 GLOWSTRIP CNDAIR CL600 CL6002C10 1390015 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 724EV 10138 MOST FORWARD STRIP OF PHOTO ILLUMINICENT EMERGENCY LIGHT ON FLOOR DOES NOT ILLUMINATE (MISSING). 2 L 7 2 4F RT A21EA 2008010700214 20080107 00214 EA 2008 1 7 TRAX200701954 1 20071218 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 903EV 7621 PILOT'S BULKHEAD AT FS 280 AND RBL 9.0 IS CRACKED. 2 L 7 2 4F RT A21EA 2008010700215 20080107 00215 EU 2008 1 7 2007UALA05224 1 20071221 A 3510 OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 427UA 512 F/O'S O2 MASK YELLOW CAT EYE REMAINS DISPLAYED AFTER TEST. FOUND WORN COVERPLATE AND DETERIORIZATION OF RUBBER ON MASK BANDS, HOSES. MASK WAS REPLACED WITH NEW OUT STOCK. CREW O2 SERVICED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010700216 20080107 00216 EA 2008 1 7 TRAX200701956 1 20071218 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FLT 4916 DEL 315 MINS, EMERGENCY LIGHTS WILL NOT COME ON. 2 L 7 2 4F RT A21EA 2008010700218 20080107 00218 EA 2008 1 7 TRAX200701957 1 20071219 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 820AS 7188 EMERGENCY FLOOR LIGHTING STRIPS ROW 11 MISSING EGRESS ARROWS. 2 L 7 2 4F RT A21EA 2008010700219 20080107 00219 NM 2008 1 7 2007UALA05226 1 20071222 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 532UA 25072 MAIN CABIN FLOORBEAM STA 324 UPPER SURFACE HAS CORROSION. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700220 20080107 00220 NM 2008 1 7 2007UALA05230 1 20071222 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 THE 'ENERG LIGHT CHARGING FWD' CIRCUIT BREAKER POPS AFTER 10 MINUTE. OVERHEAD PANEL GRID G14. FOUND EEL LIGHT FOLDED I N HALF AT 34H JUST FORWARD OF DOOR 3 RT. REPLACED LIGHT ASSY. EEL LIGHTS CHECK OK AND C-B STAYED SET. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700221 20080107 00221 EU 2008 1 7 TRAX200701958 1 20071219 A 3060 HEATER AEROSP ATR72 ATR72212 8680945 EU NR 1 PROP FAILED A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 632AS 338 FLT 4718 DEL 180 MINS, NR 1 PROP HEAT FAILED ON AND OFF 19 TIMES IN FLIGHT. A/C RETURNED TO ATL AFTER T/O, EMERGENCY DE CLARED. 2 H 7 2 4T RT A53EU 2008010700222 20080107 00222 EA 2008 1 7 TRAX200701959 1 20071220 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 1 EMERGENCY LIGHT STRIP ON FLOOR MISSING. 2 L 7 2 4F RT A21EA 2008010700223 20080107 00223 EA 2008 1 7 TRAX200701960 1 20071220 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR STICKS A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 FLT 4859 - PAX DOOR HANDLE STICKS. DIFFICULT TO OPEN FROM BOTH INSIDE AND OUTSIDE THE AIRCRAFT. WHEN CLOSING PAX DOOR OUTER HANDLE COMES ON FOR 20 SECONDS. 2 L 7 2 4F RT A21EA 2008010700224 20080107 00224 NM 2008 1 7 2007UALA05231 1 20071223 A 5210 CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR ASSIST OUT OF RIG A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 504UA 24625 AFTER DOOR 4R SLIDE INSTALLATION, DOOR ASSIST BOTTLE BLEW UPON REMOVAL OF SAFETY PINS. FOUND RIG OUT ON DOOR ASSIST BO TTLE CABLE. REPLACED DOOR ASSIST BOTTLE AND ADJUSTED RIG OF SYSTEM. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700226 20080107 00226 NM 2008 1 7 2007UALA05233 1 20071222 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L3 DOOR OBSTRUCTED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 581UA 26701 THE 3L WON'T ARM. FOUND ACCUMULATION OF DIRT AND OLD GREASE ON FITTINGS. REMOVED COVER AND CLEANED OLD GREASE AND D IRT FROM GIRT BAR FITTINGS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700227 20080107 00227 NM 2008 1 7 2007UALA05234 1 20071223 A 2910 AS4568J0460SS LINE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE HYDRAULIC SYSTEM PUNCTURED A UALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 29 787UA 46521 26939 EMERGENCY DECLARED DUE TO CENTER HYDRAULIC SYSTEM FAILURE. HYDRAULIC LINE FOR NOSE GEAR STEERING PUNCTURED, REPLACED HY DRAULIC LINE. SERVICED HYDRAULIC CENTER SYSTEM. AC OK FOR SERVICE 2 L 7 2 4F 4 F RT T0001SE E46NE 2008010700228 20080107 00228 NM 2008 1 7 2007UALA05235 1 20071223 A 5241 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 50961 24640 FWD GALLEY DOOR LOWER AFT CORNER OF THE FRAME IS CRACKED WHERE STOP FITTING ATTACHES. SUSPECT NORMAL AC OPERATION. MA JOR REPAIR ACCOMPLISHED, REMOVED AND REPLACED AFT DOOR FRAME. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010700229 20080107 00229 NM 2008 1 7 2007UALA05236 1 20071223 A 5241 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 50961 24640 FWD GALLEY DOOR LWR FWD CORNER OF FRAME IS CRACKED OUT OF 2 EACH FASTENER HOLES AT STOP FITTING ATTACH. SUSPECT NORMAL AC OPERATION. MAJOR REPAIR ACCOMPLISHED REMOVED AND INSTALLED NEW LOWER DOOR FRAME SPLICE. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010700230 20080107 00230 NM 2008 1 7 2007UALA05237 1 20071223 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 1016 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 FLOORBEAM IS CORRODED AT STA 1016 LBL 6 - LBL 9. SUSPECT MOISTURE CONTAMINATION. MAJOR REPAIR ACCOMPLISHED REMOVED DAM AGE AND INSTALLED UPPER TEE CAP FRAME REPAIR. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010700231 20080107 00231 NM 2008 1 7 2007UALA05241 1 20071221 A 2170 COALESCER BAG BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU A/C BAY ODOR A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 376UA 24641 RIGHT PACK OVERHEAT FOLLOWED BY SMOKE IN CABIN. SUSPECT FAULTY COLESCER BAG. REPLACED COALESCER BAG, RAN PACK CHECKS G OOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010700233 20080107 00233 NM 2008 1 7 2007UALA05245 1 20071222 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 DOOR 3 RIGHT LOWER WALL EMERGENCY LIGHT IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700235 20080107 00235 WP 2008 1 7 IXXA070066O 1 20071220 A 3260 WIRE DOUG DC8 DC871F 302199D WP MLG DOOR OUT OF POSITION A IXXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 11 829BX 92625 2953 45994 DURING CLIMB FROM KTOL GEAR DOOR WARNING LIGHT CAME ON WOULD NOT GO OUT. THE CREW RETURNED TO KTOL, AND LANDED WITHOUT I NCIDENT. MAINTENANCE INSPECTED GEAR DOOR AND REPOSITONED WIRING AT DOOR WARNING LIGHT SOCKET OPERATIONAL CHECK WAS GOOD IAW DC8 MAINTENANCE MANUAL 32-10-0. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2008010700236 20080107 00236 NM 2008 1 7 NWAA074185808 1 20071219 A 3350 BATTERY PACK BOEING 757 757351 1384991 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 588NW 32988 DURING OVERNIGHT CHECK, FOUND EMERGENCY LIGHTS IN SEC 694 INOP. MAINTENANCE REMOVED AND REPLACED RIGHT BATTERY PACK AT STA 694. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2008010700245 20080107 00245 NM 2008 1 7 PIDA07059 1 20071221 A 5542 SKIN BOEING 737 737228 13844AG NM RUDDER DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 251TR 23792 DURING MAINTENANCE CHECK, DAMAGE NOTED ON THE TRAILING OF THE RUDDER APPROXIMATELY 10 INCHES BELOW THE TOP. REPAIRED DA MAGE PER SRM 51-40-14. 2 L 7 2 4F RT A16WE 2008010700246 20080107 00246 NM 2008 1 7 PIDA07060 1 20071220 A 5542 SKIN BOEING 737 737228 13844AG NM RUDDER DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 251TR 23792 DURING MAINTENANCE CHECK, DAMAGE NOTED ON THE LOWER FORWARD LEFT CORNER OF THE RUDDER. REPAIRED PER BOEING TELEX MESSAG E NOS 1-724910440-9 AND -10 WITH FAA DOA APPROVED 8100-9 DATED DEC 20, 2007. 2 L 7 2 4F RT A16WE 2008010700247 20080107 00247 NM 2008 1 7 PIDA07061 1 20071220 A 7830 DOOR BOEING 737 737228 13844AG NM THRUST REVERSER DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 251TR 23792 DURING MAINTENANCE CHECK, DAMAGE NOTED ON THE LEFT ENGINE THRUST REVERSER LOWER DOOR FORWARD EDGE AT APPROXIMATELY 5 O'C LOCK POSITION. REPAIRED PER PACE AIRLINES REPAIR PROCEDURE REPORT EA NR 78-348 DATED 12/14/07 WITH FAA DER APPROVED 811 0-3 DATED 12/14/2007. 2 L 7 2 4F RT A16WE 2008010700248 20080107 00248 WP 2008 1 7 MWEA070308 1 20071223 A 5754 5922532502 SPRING DOUG DC9 DC981 3022081 WP C SLAT STICKING A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 813ME 48007 SLAT DISAGREE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF. FOUND LEFT C SLAT SENSOR TARGET SPRING MECHANISM STICKY, CLEANE D AND LUBED. 2 L 7 2 4F A6WE 2008010700249 20080107 00249 NM 2008 1 7 NWAA074206307 1 20071105 A 5330 SKIN BOEING 747 747451 1384940 NM BS 1816 S26R CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 667US 24222 DURING "M" CHECK, FOUND CRACK IN FUSELAGE SKIN AND FASTENER HOLE LOCATIONS WITH SHORT EDGE MARGIN AT UPPER FORWARD CORNE R OF AFT CARGO DOOR CUTOUT AT BS 1816 S26R. REPAIRED PER EA 63-211303. 2 L 7 4 4F RT A20WE 2008010700250 20080107 00250 NM 2008 1 7 NWAA074196307 1 20071107 A 5311 FRAME BOEING 747 747451 1384940 NM BS 1140 S10R CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 667US 24222 DURING "M" CHECK, FOUND 3 HOLES WITH CRACK INDICATIONS ON FRAME AND CRACKED FRAME WEB DOUBLER AT BS 1140 S10R TENSION TI E AREA. REPAIRED PER EA 63-211005. 2 L 7 4 4F RT A20WE 2008010700251 20080107 00251 EU 2008 1 7 UPS07151323 1 20071224 A 3230 LANDING GEAR AIRBUS A300 A300F4622R 3930360 EU MAINS MALFUNCTIONED A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 120UP 0805 LANDING GEAR WOULD NOT RETRACT AFTER T/O, LDG WT 301K#. ONLY SYS 1 UTILIZED. PERFORMED PDCU BITE TEST PER AMM 32-00-00 -05. NO FAULTS FOUND. PERFORMED TEST OF 2GA USING SIMULATED TEST BOX PER AMM 32-31-11-04 ON BOTH SYS 1 AND 2. OPS CK GOOD. LDG GEAR POSITION NR 1 DEFERRED PER MEL 32-61-04. 2 L 7 2 4F RT A35EU 2008010700252 20080107 00252 WP 2008 1 7 UPS07851324 1 20071222 A 3240 CONTROL VALVE DOUG DC8 DC873F 302199F WP BRAKE ASSY INOPERATIVE A IPXA O OTHER O OTHER LD LANDING 1 SO 01 852UP 46052 A/C CAME TO A STOP WHEN CLEARING THE ACTIVE RUNWAY AND WAS UNABLE TO MOVE WITH BRAKES OFF. THE ANTI-SKID LIGHT CAME ON WITH THE SWITCH ON WHEN CLEARING THE RUNWAY. FOUND CABLE AT BRAKE CONTROL VALVE COMING OFF OF FWD QUADRANT AND GUIDE PI N DAMAGED. REPLACED GUIDE PIN, REPOSITIONED CABLE, INSPECTED QUADRANT AND CABLE. NO DEFECTS NOTED. NO ADJUSTMENT REQU IRED OR MODE, TESTED BRAKE VALVE SYSTEM IN REF TO MM CH 32-42-02-02. OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2008010700253 20080107 00253 WP 2008 1 7 UPS07851330 1 20071226 A 3350 6012235 BATTERY DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 ON PRE-FLIGHT, FOUND EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND RELAY UNIT ASSY IAW A MM 33-50-01-2. 2 L 7 4 4F RT 4A25 2008010700254 20080107 00254 NM 2008 1 7 UPS07M51309 1 20071217 A 2597 WIRE DOUG MD11 MD11F 3023600 NM INDICATOR LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 RT SIDE PRESSURE LIGHT DOES NOT TEST ON POST FLIGHT. ITEM DEFERRED PER MEL 25-61-2. PLUG IN CONNECTOR BAD. REINSPECT DAILY PRESS CK GOOD. DMP C/W. FOUND WIRE LOOSE. RESECURED WIRE. SYSTEM CHECKS NORMAL PER WDM 25-60-01. THIS CLEARS M364913, PLACARD REMOVED. 2 L 7 3 4F RT A22WE 2008010700255 20080107 00255 WP 2008 1 7 NWAA074219871 1 20071222 A 3350 FUSE DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS BLOWN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 780NC 48102 DURING LINE CHECK FOUND EMERGENCY LIGHTS INOPERATIVE ON 1ST CLASS SEATS ROW 1 THRU 4 AND FWD EXIT DOOR EXIT SIGN INOP. REPAIRED IN ACCORDANCE WITH MM 33-53-00 BY REPLACING FUSE. AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008010700256 20080107 00256 NM 2008 1 7 761002 1 20071222 A 7500 65B94544 DUCT BOEING 747 7472F6B 1384807 NM GE CF6 CF650E2 30018 NE BLEED AIR FAILED A Q2SA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 63 761SA 21832 517269 ENGINE FIRE WARNING NR 3 ENGINE. "A" LOOP SHOWED 8.0 AND "B" LOOP SHOWED 8.5. INDICATION WENT DOWN AWAY AFTER THRUST R EDUCED TO IDLE. DUMPED 70,000 LBS OF FUEL AND RETURNED TO PANC. INSPECTED ENGINE AND FOUND TRANSITION DUCT ABOVE HIGH STAGE BLEED VALVE SPLIT AT THE CLAMP. REPLACED TRANSITION DUCT IN ACCORDANCE WITH AMM 36-11-01. LEAK CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E23EA 2008010700257 20080107 00257 EA 2008 1 7 QXEA200702026 1 20071225 A 3297 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA TEMP SENSOR BROKEN A QXEA O OTHER O OTHER AP APPROACH 1 NM 09 606QX 10023 SEA- FLIGHT 2631 - BRAKE OVERHEAT WARNING ON APPROACH BEFORE GEAR DOWN SELECTION. BTMS IN RED READS 00 UNITS. NO AURAL MESSAGE. PER THE CHECKLIST PRESSES THE RESET AND THE WARNING WENT NORMAL GREEN. MAINTENANCE FOUND THE TEMP SENSOR CON NECTOR BROKE INTERNALLY FOR THE RIGHT OUTBOARD SENSOR. PERFORMED REO 670-32-46-001. CAPPED AND STOWED THE CONNECTOR AN D PLACED ON MEL 32-46-1. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008010700258 20080107 00258 NM 2008 1 7 2007UALA05249 1 20071221 A 2120 UNKNOWN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN ODOR A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 793UA 26946 FAINT SMELL OF HOT PLASTIC OR ELEC INSULATION NEAR DOOR 4R AT AFT CAPC. SUSPECT COFFEE WARMER HAD EXCESSIVE COFFEE RESI DUE. CLEANED WARMER. ALSO OPEN ACCESS PANELS IN AFT LAV AND GALLEY TO THE RESPECTIVE LIGHTS BALLAST AND INSPECTED FOR AN Y DEFECTS, INSPECTED CSAP AT DOOR 4 LT ALL COMPONENTS SATISFACTORY. NO ABNORMAL SCENTS OR ODOR. AC OK FOR SERVICE 2 L 7 2 4F 4 F RT T0001SE E46NE 2008010700259 20080107 00259 NM 2008 1 7 2007UALA05253 1 20071222 A 5210 69242503 SPRING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR IMPROPER PART A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 375UA 24640 DOOR 1L ASSIST SPRING HAS INCORRECT PART INSTALLED. REPLACED WITH CORRECT PART. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010700260 20080107 00260 NM 2008 1 7 2007UALA05254 1 20071224 A 3397 58781 FEEDER CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 326UA 23958 EEL LIGHTS INOP AFT OF ROW 15. CLEANED AND REPLACED CABLE. RELAMPED 2 L 7 2 4F 4 F RT A16WE E21EU 2008010700269 20080107 00269 NM 2008 1 7 2007UALA05263 1 20071223 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY LIGHT AT ROW 34 SEAT HJK INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700270 20080107 00270 NM 2008 1 7 2007UALA05264 1 20071223 A 3350 78961 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 173UA 24380 THE 58C SEAT MOUNTED EEL LIGHT BROKEN OFF WITH CONNECTOR TORN OFF SEAT HARNESS ALSO. REPLACED LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700271 20080107 00271 NM 2008 1 7 2007UALA05265 1 20071223 A 3350 COVER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS MISSING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 177UA 24384 SEAT 47C EMERGENCY LIGHT COVER MISSING. REPLACED COVER. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700275 20080107 00275 NM 2008 1 7 2007UALA05269 1 20071222 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 SEAT 2J AFT EMERGENCY LIGHT IS INOPERATIVE. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700276 20080107 00276 NM 2008 1 7 2007UALA05270 1 20071224 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN UNSECURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 594UA 28145 EXIT PATH LIGHTING STRIP COMING UP AT SEAT 13C. SECURED EEL STRIP. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700278 20080107 00278 NM 2008 1 7 2007UALA05273 1 20071223 A 3510 OXYGEN BOTTLE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CREW O2 LOW PRESSURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 797UA 26924 CREW OXYGEN PRESSURE READING 1450 PSI. SUSPECT LOW DUE TO CREW CHECKS DOING PRE FLIGHT CHECK LIST. REPLACED CREW O2 BOT TLE AND LEAK CHECKED OK. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008010700279 20080107 00279 EA 2008 1 7 QXEA200702027 1 20071224 A 5100 NONE CNDAIR CL600 CL6002C10 1390015 EA NONE A QXEA O OTHER O OTHER DE DESCENT 1 NM 09 290RB 10029 PDX- ON START OF FLIGHT IDLE DESCENT FROM 33,000, RECEIVED A GENERATOR 1 CAUTION LIGHT. COMPLIED WITH CHECKLIST, NORMAL GENERATOR OPERATION FOR THE REST OF THE FLIGHT. MAINTENANCE FOUND NO MDC FAULTS LISTED. LIGHT NOT ILLUMINATED. OPERA TIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. COULD NOT DUPLICATE PROBLEM. 2 L 7 2 4F RT A21EA 2008010700280 20080107 00280 EA 2008 1 7 QXEA200702021 1 20071225 A 3150 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA ILLUMINATED A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 615QX 10065 BOI - FLIGHT 2590 - RECEIVED A XFLOW PUMP CAUTION MESSAGE. RETURNED TO THE GATE. PLACED THE SYSTEM ON MEL 28-13-10. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008010700281 20080107 00281 NM 2008 1 7 QXEA200702022 1 20071224 A 5751 BUSHING DHAV DHC8 DHC8202 2809007 NM LT AILERON DAMAGED A QXEA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 09 357PH 504 PSC- FLIGHT 2109 - LEFT AILERON CONTROL STILL. PROBLEM INCREASES WITH AIRSPEED. AIRCRAFT FERRIED TO PDX FOR REPAIRS. FOUND BUSHING ON LEFT AILERON PUSH ROD FORK INSTALLED INCORRECTLY. REINSTALLED. CHECKS GOOD. AIRCRAFT RETURNED TO SERVIC E. 2 H 7 2 4T RT A13NM 2008010700282 20080107 00282 EA 2008 1 7 QXEA200702023 1 20071225 A 3150 NONE CNDAIR CL600 CL6002C10 1390015 EA NONE A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 607QX 10024 SEA - STALL FAIL CAUTION MESSAGE ILLUMINATED. TURNED OFF THE RIGHT STALL SWITCH PER THE CHECKLIST. MAINTENANCE COMPLIE D WITH FIM 27-35-00-810-803-A01. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2008010700283 20080107 00283 EA 2008 1 7 QXEA200702024 1 20071224 A 3150 NONE CNDAIR CL600 CL6002C10 1390015 EA NONE A QXEA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 290RB 10029 ONT- FLIGHT 2570 - UPON POWER UP RECEIVED A AFT CARGO FIRE DETECTOR CAUTION MESSAGE. MAINTENANCE CYCLED POWER TO THE AI RCRAFT AND INDICATIONS WENT AWAY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2008010700284 20080107 00284 NM 2008 1 7 QXEA200702025 1 20071225 A 3610 8209076 SWITCH BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 432QX 4166 SEA - FLIGHT 2322 - NR 2 BLEED CAUTION ILLUMINATED ON TAXI. TURNED OFF THE BLEED PER THE CHECKLIST AND THE LIGHT STAYED ON. RETURNED TO THE GATE. MAINTENANCE REPLACED THE PRE COOLER OUTLET DUCT (PN 820908-3) AND THE OVERTEMP SWITCH. OPE RATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008010700285 20080107 00285 NE 2008 1 7 07FDEA05109 2 20071220 A 7532 9788422 BLEED VALVE AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D* NE NR 1 ENGINE CRACKED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 448FE 3576 3576 260 715419 DURING CLIMB TO CRUISE ALTITUDE, ECAM PRESENTED AN ADVISORY PAGE FOR NR 1 ENG NAC TEMP AT 200. SELECTED NR 1 BLEED VAL VE OFF AND REDUCED POWER ON NR 1 WITH NO CHANGE IN NR 1 NAC TEMP. AFTER THROTTLE WAS REDUCED TO ALMOST IDLE SETTING, N R 1 NAC TEMP FELL TO 190 DEGREES. THROTTLE REMAINED AT IDLE UNTIL SHORT FINAL APPROACH. DURING DESCENT WITH NR 1 AT I DLE, ADVISORY INDICATION WENT AWAY AFTER 10-15 MINUTES. FOUND A SMALL CRACK ON FAN AIR VALVE, FOUND A COUPLE OF SENSE L INES TO BE BAD. REMOVED AND REPLACED FAN AIR VALVE, REMOVED AND REPLACED SENSE LINES AND NACELLE TEMP SENSOR. 2 L 7 2 4F 4 F RT A35EU E20EA 2008010700286 20080107 00286 EU 2008 1 7 07FDEA05110 1 20071220 A 5610 NP1752014 WINDSHIELD AIRBUS 300 A300F4605R 3930327 EU COCKPIT CRACKED A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 663FE 766 F/O`S R1 WINDOW SHATTERED AT CRUISE FL 300. QRH COMPLIED WITH. REMOVED AND REPLACE R1 WINDSHIELD PER AMM 56-11-11-4. REMOVED AND REPLACED WINDSHIELD TEMP REGULATOR IAW MM 30-42-11-4 AND WINDOW HEAT PROTECTION CONTROLLER IAW MM 30-42-51-4 . PERFORMED WINDSHIELD ANTI-ICING AND DEFOGGING OPERATIONAL TEST IAW MM 30-42-00, OPS CHECKS GOOD. 2 L 7 2 4F RT A35EU 2008010700287 20080107 00287 EU 2008 1 7 07FDEA05111 1 20071220 A 5610 NP1752014 WINDOW AIRBUS 300 A300F4605R 3930327 EU COCKPIT CRACKED A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 663FE 766 F/O`S R1 WINDOW SHATTERED AT CRUISE FL 300. QRH COMPLIED WITH. ACCOMPLISHED COMPLETION OF F/O'S WINDOW INSTALLATION IA W MM 56-11-11-4. REMOVED AND REPLACED WINDSHIELD TEMP REGULATOR IAW MM 30-42-11-4 AND WINDOW HEAT PROTECTION CONTROLLER IAW MM 30-42-51-4. OPS CHECKS GOOD. PREMATURE REMOVAL/INSTALLATION. 2 L 7 2 4F RT A35EU 2008010700288 20080107 00288 WP 2008 1 7 07FDEA05113 1 20071220 A 3620 6271004 SWITCH DOUG DC10 DC1030F 3023504 WP FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 304FE 46992 PDIS: LEVEL AT FL330, 45 MINUTES INTO FLIGHT, GOT NR 3 MANF LIGHT, FOLLOWED BY A LEVEL 3 "MANIFOLD NR 3 FAIL" ALERT. CO MPLIED WITH RED TABS AND LANDED AT NEAREST SUITABLE AIRFIELD (KLAS). MAN LIGHT EXTINGUISHED SOMEWHERE BETWEEN 8000' AND 5000' IN THE DESCENT. FOUND RT WING SWITCH FAULT BALL FAULTED AT PNEU MAN IND BOX IN CENTER ACC COMP. PERFORMED NR 3 PNEUMATIC SYS DECAY CHECK PER MD-10 MM 36-00-02-5 WITH NO DEFECTS NOTED. SUSPECT MAN FAILURE DET PRESSURE SWITCH ON RIG HT SIDE. SWITCH REMOVED AND REPLACED MANIFOLD FAILURE DETECTION CONTROLLER PER REF MM 36-23-86B870. 2 L 7 3 4F RT A22WE 2008010700289 20080107 00289 NM 2008 1 7 07FDEA05117 1 20071221 A 3220 H1010153 SWITCH BOEING 727 727233 138408A NM NLG INOPERATIVE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 266FE 21672 AFTER RAISING LANDING GEAR, RED NOSE GEAR LIGHT REMAINED ILLUMINATED WITHOUT A CORRESPONDING DOORS LIGHT, OR GREEN GEAR LIGHT. CYCLED GEAR PER QRH PROCEDURES WITH NO POSITIVE RESULTS. LIGHT REMAINED ILLUMINATED ENTIRE FLIGHT. AIRCRAFT IN CURRED A MAINTENANCE FLIGHT DIVERSION INTO EWR, DURING A SCHEDULED FLIGHT INTO BOS. FOUND POSITION SWITCH S-93 FAULTY. REMOVED AND REPLACED POSITION SWITCH PER M/M32-61-071-4 AND M/M32-61-071-5. OP CHECKS GOOD. 2 L 7 3 4F RT A3WE 2008010700290 20080107 00290 NM 2008 1 7 07FDEA05118 1 20071221 A 5315 652083817 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 CORROSION AROUND NUT PLATE HOLES ON TOP OF FLOORBEAM AT SEVERAL LOCATIONS, FS 1130, LBL 64 TO RBL 64, WL 208. BLENDED D AMAGE AREA STA 1130, RBL 64, FOUND TO BE OUT OF LIMITS, REF SRM 53-10-8 TOOL NR IN17-0023 CAL DATE DUE 2-13-08. REMOVED DAMAGE AREA, REF SRM 53-10-8. FABRICATED REPAIR PARTS REF SRM 53-10-8. TREATED AND PRIMED REF SRM 51-10-2. INSTALLED REPAIR PARTS. REF SRM 51-30-2 THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008010700291 20080107 00291 NM 2008 1 7 07FDEA05119 1 20071221 A 5320 65C1703818 ANGLE BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 FORWARD LOWER PIT FLOOR STRUCTURE LEFT SIDE STA 570 TO STA 650, Z- ANGLE CORRODED ON LOWER SURFACE REMOVED CORROSION FOU ND TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER. TREATED AND PRIMED AND INSTALLED. REF SRM 51-40-2 AND SRM 53-10-1. 2 L 7 3 4F RT A3WE 2008010700292 20080107 00292 NM 2008 1 7 07FDEA05120 1 20071221 A 5347 658624534 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 CORROSION ON I/B SIDE OF SEAT TRACK CROWN AND UNDER DOUBLER PLATE, BS 1137 TO BS 1125M RBL 45, WL 208. REMOVED DAMAGED SECTION OF SEAT TRACK STA 1100 - 1135, RBL 45. FABRICATED AND INSTALLED SEAT TRACK AND REPAIR ANGLES REF SRM 53-10-5 F IG 1 SRM 51-30-2 PG 2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008010700293 20080107 00293 EU 2008 1 7 07FDEA05121 1 20071221 A 5280 A5281005220100 HINGE AIRBUS 310 A310203 3930313 EU ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 RT AFT NLG DOOR FWD HINGE FITTING CRACKED REMOVED AND REPLACED FWD HINGE FITTING ASSY. ON RT AFT NLG DOOR REF A310-200, CMM 52-82-12 AND AIRBUS INDUSTRY PMS 01-05-58. 2 L 7 2 4F RT A35EU 2008010700294 20080107 00294 NM 2008 1 7 07FDEA05122 1 20071222 A 5315 652083817 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 CORROSION AROUND NUT PLATE ON TOP OF FLOORBEAM AT FS 1130, LBL 51, WL 208. REMOVED CORROSION AROUND NUT PLATE ON TOP OF FLOORBEAM STA 1130, LBL 51, FOUND TO BE OUT OF LIMITS REF SRM 53-10-8. SAME LOCATION SEAT TRACK FOUND TO BE OUT OF LIM ITS. FABRICATED AND INSTALLED FLOORBEAM REPAIR REF 53-10-8. FABRICATED AND INSTALLED NEW SEAT TRACK REF BAC DWG 65-862 45. 2 L 7 3 4F RT A3WE 2008010700295 20080107 00295 EU 2008 1 7 07FDEA05123 1 20071222 A 5314 A53610586201 KEELBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 NOSE GEAR WELL, RT BULKHEAD STRAP CRACKED BETWEEN FR 13A AND FR 14 UNDER E/E COMPT FLOOR PANEL NR 122NF. REMOVED & REI NSTALLED HARDWARE FOR NOSE GEAR UPLOCK SUPPORT REF SRM 51-40-21. REMOVED AND REINSTALLED RT NLG GROUND CONTROL TORQUE TU BE REF AMM 32-31-00-2 & SRM 51-40-21. PERFORMED NLG DOOR GROUND OPEN & CLOSE, OPS CHECK REF AMM 32-31-00-5. OPS CHECK GOOD COMPLIED WITH EA 6-5310-109234. 2 L 7 2 4F RT A35EU 2008010700296 20080107 00296 NM 2008 1 7 2007UALA05277 1 20071224 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 FUSELAGE FRAME CRACKED, BS 277 STR 16L. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED FRAME DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010700298 20080107 00298 2008 1 7 2007UALA05279 4 20071224 A 2565 D31354437 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L2 DOOR DETACHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 306UA 23667 UPON CLOSING OF DOOR 2L SLIDE DETACHED FROM DOOR. SUSPECT SLIDE IMPROPERLY INSTALLED. REPLACED LEFT REAR DOOR SLIDE. A C OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010700303 20080107 00303 NM 2008 1 7 2007UALA05285 1 20071226 A 3350 78961 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY EXIT EEL LIGHT INOPERATIVE AT SEATS 1J (AFT), 4F (FWD) & 55 (LEFT). REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700307 20080107 00307 NM 2008 1 7 2007UALA05289 1 20071225 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EMERGENCY LIGHT INOPERATIVE AT ROWS 2J FWD, 46 ABC & 48 HJK ARE INOPERATIVE. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700308 20080107 00308 NM 2008 1 7 2007UALA05290 1 20071225 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EMERGENCY LIGHT ROW 4F INOPERATIVE. RESECURED LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700309 20080107 00309 NM 2008 1 7 2007UALA05291 1 20071225 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INTERMITTENT A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 197UA 26901 FC CABIN EMERGENCY LIGHT BY DOOR 1R & BY SEATS ARE FLASHING INTERMITTENTLY. RESECURED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700313 20080107 00313 EU 2008 1 7 USAA920071376 1 20071212 A 5320 D53112786201 ANGLE AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 649AW 803 SAL - MAJOR REPAIR - C-7 CHECK - CORROSION ON CABIN RIGHT SIDE ANGLE AT BS 808/FR20, -Y1583. REPLACED CABIN RIGHT SIDE ANGLE AT BS 808/FR20, -Y1583 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008010700315 20080107 00315 EU 2008 1 7 USAA920071378 1 20071217 A 5321 D5367302900000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU CABIN PERFORATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 649AW 803 SAL - MAJOR REPAIR - C-7 CHECK- PERFORATION DAMAGE ON AFT CABIN FLOOR PANEL 152MF AT BS 2616/FR 56 - BS 2723/ FR 58, +Y7 65 - + Y97.08. REPLACED FLOOR PANEL 152MF AT BS 2616/FR 56 - BS 2723/ FR 58, +Y765 - + Y97.08 IAW A320 SRM 53-02-00 PAR 8H SND IRM 9701 REV F. 2 L 7 2 4F RT A28NM 2008010700316 20080107 00316 EU 2008 1 7 USAA920071379 1 20071209 A 5321 D5367200800000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU CABIN PERFORATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 649AW 803 SAL - MAJOR REPAIR - C-7 CHECK- PERFORATION DAMAGE ON FWD CABIN FLOOR PANEL 131JF AT BS 1270/ FR 30 - BS 1483/ FR 34, +Y 765 - +Y970.8. REPLACED FLOOR PANEL 131JF AT BS 1270/ FR 30 - BS 1483/ FR 34, +Y765 - +Y970.8 IAW A320 SRM 53-02-00, IR M 9701 REV F. 2 L 7 2 4F RT A28NM 2008010700318 20080107 00318 NM 2008 1 7 BB07102 1 20071219 A 2910 VALVE BOEING 767 7672B7 1385107 NM HYDRAULIC SYSTEM LEAKING A USAA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 EA 19 251AY 24764 FLIGHT 798, PHL-AMS: DURING FLIGHT, CREW REPORTED LOSS OF THE CENTER HYDRAULIC SYSTEM QUANTITY. FLIGHT DIVERTED TO YQX . MAINTENANCE ACTION PENDING. UPDATED 12/28/07: MAINTENANCE FOUND WETTING IN RT MAIN WHEEL WELL. CLEANED WHEEL WELL AND OPERATED FLAPS/SLATS, SPOILERS, RUDDER, AILERONS, HYD GENERATOR. PINNED GEAR AND CYCLED. NO LEAKS FOUND. RESET ST EERING AND BRAKE ISOLATION VALVE. NO LEAKS FOUND. 2 L 7 2 4F RT A1NM 2008010700319 20080107 00319 NM 2008 1 7 BB07103 1 20071227 A 3397 WIRE BOEING 757 7572B7 1384964 NM CABIN SHORTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 936UW 27244 MAINTENANCE FOUND R1 EXTERIOR EMERGENCY LIGHT INOPERATIVE. FOUND POWER WIRE AT LIGHT SHORTED TO GROUND. REPOSITIONED W IRE, NO FURTHER FAULTS. 2 L 7 2 4F RT A2NM 2008010700320 20080107 00320 NM 2008 1 7 SWAA076431 1 20071221 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 253WN 32511 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2008010700322 20080107 00322 NM 2008 1 7 SWAA076433 1 20071222 A 5714 BAC1506 SUPPORT BEAM BOEING 737 7373H4 1384600 NM CENTER WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED 22Y CHECK, FOUND WING CENTER SECTION SUPPORT BEAM WEB CRACKED AT BS 616, BL 40.8. REPAIRED WEB PER AAR EA. 2 L 7 2 4F RT A16WE 2008010700323 20080107 00323 NM 2008 1 7 SWAA076434 1 20071222 A 3350 6042221 LIGHT BOEING 737 7373H4 1384600 NM L1 DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2008010700324 20080107 00324 NM 2008 1 7 SWAA076435 1 20071220 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 20L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008010700325 20080107 00325 NM 2008 1 7 SWAA076436 1 20071223 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 460, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008010700329 20080107 00329 NM 2008 1 7 SWAA076440 1 20071222 A 5330 6545775 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B, STR 14L. REPAIRED SKIN PER SWA EA & SRM. 2 L 7 2 4F RT A16WE 2008010700331 20080107 00331 NM 2008 1 7 SWAA076442 1 20071220 A 5330 6545776 SKIN BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 24R. MX FERRY TO DAL FOR REPAIRS. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008010700332 20080107 00332 NM 2008 1 7 SWAA076443 1 20071221 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 754, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008010700333 20080107 00333 NM 2008 1 7 SWAA076444 1 20071221 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010700334 20080107 00334 NM 2008 1 7 SWAA076445 1 20071222 A 3350 D1701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 400WN 27891 DURING SCHEDULED HC1 CHECK, FWD LEFT CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY P ACK PER MM. 2 L 7 2 4F RT A16WE 2008010700335 20080107 00335 NM 2008 1 7 SWAA076448 1 20071222 A 3350 D1701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 400WN 27891 DURING SCHEDULED HC1 CHECK, MID CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK P ER MM. 2 L 7 2 4F RT A16WE 2008010700337 20080107 00337 NM 2008 1 7 SWAA076446 1 20071222 A 3350 D1701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 400WN 27891 DURING SCHEDULED HC1 CHECK, FWD RIGHT CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008010700338 20080107 00338 NM 2008 1 7 SWAA076447 1 20071222 A 3350 D1701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 400WN 27891 DURING SCHEDULED HC1 CHECK, AFT LEFT CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY P ACK PER MM. 2 L 7 2 4F RT A16WE 2008010700339 20080107 00339 2008 1 7 SWAA076450 4 20071221 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 440LV 29835 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF DOOR WHEN OPENED. SLIDE DID NOT DEPLOY. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008010700340 20080107 00340 NM 2008 1 7 SWAA076451 1 20071223 A 3350 9250071 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 452WN 29846 EEPLS INOP AT ROW 1. REMOVED AND REPLACED BULB PER MM. 2 L 7 2 4F RT A16WE 2008010700341 20080107 00341 NM 2008 1 7 SWAA076452 1 20071225 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 459WN 32497 EEPLS COVER LOOSE AT MID CABIN. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2008010800001 20080108 00001 CE 2008 1 8 BSYA200700012 1 20071223 A 2460 CM358920 CIRCUIT BREAKER CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE FAULTY E BSYA A UNSCHED LANDING G B MULTIPLE FAILURE SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 9448B 208B0121 EN ROUTE FROM SDF TO MDW PILOT HAD TO DIVERT TO DPA BECAUSE OF HIGH WINDS. UPON ARRIVING INTO DPA LOST ALL AVIONICS, TH EN STARTED TO SMELL SOMETHING BURNING. AFTER LANDING NEITHER AVIONICS BUSS NR 1 OR BUSS NR 2 WOULD RESET, AND THE ELECT RICAL SMELL WAS COMING FROM P10 PIN (L). REMOVED AND REPLACED CIRCUIT BREAKER AND BURNT PIN IN THE CONNECTOR EVERYTHING OPS CHECKS GOOD. 1 H 7 1 3T 3 T A37CE E4EA 2008010800002 20080108 00002 NM 2008 1 8 2007UALA05298 1 20071225 A 5270 WARNING SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT ACTIVATED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 546UA 25367 ABORTED TAKEOFF AT 100 KNOTS DUE TO LEFT AFT ENTRY DOOR EICAS. ABORTED T-O MAX SPEED 100 KNOTS FOR LEFT AFT ENT DOOR EI CAS. WENT AWAY AFTER ABORT-NO HISTORY AND EVENT NEVER REOCCURRED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010800004 20080108 00004 NM 2008 1 8 ASAA0772407 1 20071205 A 5320 143A948535 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 FWD CARGO PIT FLOOR SUPPORT ANGLE (RAIL ASSY) AT 500D LBL 25 TO RBL 25 CORRODED. REPLACED WITH NEW PART. 2 L 7 2 4F RT A16WE 2008010800007 20080108 00007 NM 2008 1 8 ASAA0772410 1 20071205 A 5320 146A75021 CHANNEL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO LEFT ZEE CHANNEL BS 727+4 TO BS 847 LBL 21 CORRODED. REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 53-00-53 & 51-40-02. 2 L 7 2 4F RT A16WE 2008010800010 20080108 00010 NM 2008 1 8 ASAA0772413 1 20071205 A 5320 146A34267 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT INTERCOSTAL BS 727+8 LBL 5 TO RBL 8 CORRODED. REPLACED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008010800011 20080108 00011 NM 2008 1 8 ASAA0772414 1 20071205 A 5347 146A750125 CARGO TRACK BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT RIGHT TIE DOWN TRACK BS 727D RBL 13.84 CORRODED. TIE DOWN TRACK REPLACED ON TC 5113801. 2 L 7 2 4F RT A16WE 2008010800012 20080108 00012 NM 2008 1 8 ASAA0772415 1 20071205 A 5347 146A750125 CARGO TRACK BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT RIGHT TIE DOWN TRACK BS 747 RBL 13.84 CORRODED. TIE DOWN TRACK REPLACED ON TC 5113801. 2 L 7 2 4F RT A16WE 2008010800013 20080108 00013 NM 2008 1 8 ASAA0772416 1 20071205 A 5320 146A75036 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO FLOOR SUPPORT RAIL BS 767+5 RBL 8 CORRODED. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008010800015 20080108 00015 NM 2008 1 8 ASAA0772418 1 20071206 A 5320 146A81271 SHIELD BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT BS 767 TO BS 792 RBL 21 SHIELD CORRODED. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008010800016 20080108 00016 NM 2008 1 8 ASAA0772419 1 20071206 A 5320 146A81236 SILL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT DOOR SILL BS 792 TO BS 847 CORRODED. AFT CARGO PIT DOOR SILL BS 792 TO B847 CORROSION BLEND AND FOUND BEY OND LIMITS IAW B737 700 SRM 53-60-15. NEW PART INSTALLED IAW B737 700 SRM 51-40-02 AND B DRWG 143A 8330. 2 L 7 2 4F RT A16WE 2008010800017 20080108 00017 NM 2008 1 8 ASAA0772420 1 20071206 A 5347 146A750125 CARGO TRACK BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT TIE DOWN TRACK RBL 13.84 BS 792 TO BS 847 CORRODED. TRACK REPLACED. 2 L 7 2 4F RT A16WE 2008010800019 20080108 00019 NM 2008 1 8 2007UALA04900 1 20071201 A 2750 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE VIBRATION A UALA O OTHER E VIBRATION/BUFFET CR CRUISE 1 WP 29 203UA 24718 CREW DEBRIEFED, REPORTED ENTIRE AC VIBRATES AT FLAPS 2. OK BEFORE AND AFTER FLAPS 2. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010800020 20080108 00020 NM 2008 1 8 CALA0700775 1 20071218 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17619 27332 FUSELAGE FRAME CRACKED AT STA 787 BETWEEN STRINGER 8L AND 9L. REPAIRED PER ECRA 5310-04684. 2 L 7 2 4F RT A16WE 2008010800024 20080108 00024 NM 2008 1 8 CALA0700779 1 20071221 A 5313 617777 STRINGER SPLICE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 CABIN FWD ENTRY, NR 15 INTERCOSTAL AFT OF L-1 DOOR CUTOUT STRINGER CRACKED STA 360. REMOVED AND REPLACED STRINGER SPLIC E 15L STA 360 PER ECRA 5311-01382. 2 L 7 2 4F RT A16WE 2008010800025 20080108 00025 NM 2008 1 8 CALA0700781 1 20071217 A 5534 65737865 FITTING BOEING 737 7373T0 1384582 NM VERTICAL STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 VERTICAL STAB, LEFT AFT O/B FITTING FOUND CORROSION ON BOTH FACES. AFTER REMOVED BUSHINGS REPAIRED AS PER ECRA 5530-014 94. 2 L 7 2 4F RT A16WE 2008010800027 20080108 00027 NM 2008 1 8 CALA0700783 1 20071220 A 5230 65C36183 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 C1 DOOR OUTER SKIN CRACKED JUST ABOVE DOOR HANDLE TOP CORNER. REPAIRED PER SRM 52-00-01 FIG 201 PAGE 203. 2 L 7 2 4F RT A16WE 2008010800028 20080108 00028 NM 2008 1 8 CALA0700784 1 20071221 A 5320 50794679 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 CABIN FWD ENTRY, L-1 DOOR UPPER HINGE AT STRINGER 10L, O/B CLIP FOR WEB IS CRACKED AT AFT END STA 303. L-1 DOOR SURROUN D S-10L UPPER HINGE INTERIM REPAIRED PER ECRA 5311-01381. 2 L 7 2 4F RT A16WE 2008010800029 20080108 00029 NM 2008 1 8 CALA0700785 1 20071221 A 5320 6561777505 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 FWD CABIN NR 14L INTERCOSTAL AFT OF L-1 DOOR CUTOUT STRINGER CRACKED AT STA 360. REMOVED AND REPLACED PER ECRA 5311-013 82. 2 L 7 2 4F RT A16WE 2008010800030 20080108 00030 NM 2008 1 8 CALA0700786 1 20071209 A 5320 ACR15CE6D STRAP BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 47332 23570 PAN STRAP CORRODED AT STA 967 BETWEEN S-27L AND S-27R. REPAIRED PER ECRA 5330-03760. 2 L 7 2 4F RT A16WE 2008010800031 20080108 00031 EU 2008 1 8 07FDEA05128 1 20071224 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS CROSSBEAM REPAIR LOCATED IN BULK CARGO UNDER FLOOR AT FRAME 65 BETWEEN RT Y210 TO LT Y1470, HAS 1 EACH REPAIR S ECTION MEASURING 53.4" LONG AND 2 EACH REPAIR ANGLES MEASURING 8.8" LONG ON THE LT SIDE AND 9.5" LONG ON THE RT SIDE PRE VIOUSLY INSTALLED REPAIR LOCATED IN BULK CARGO AT FR 65 WAS DETERMINED NOT TO BE IAW A310 SRM 53-10-15 FIG 207, DUE TO I NCORRECT THICKNESS BASED ON VISUAL EVALUATION WITH THE REPAIR INSTALLED. REMOVED EXISTING REPAIR AND REPAIRED IAW A310 SRM 53-10-15 FIG 207. THIS IS A REPAIR WITH NO AIRBUS ISSUED PART NUMBER, REPAIR IDENTIFIED BY THE AGING AIRCRAFT INSPE CTION PROGRAM. 2 L 7 2 4F RT A35EU 2008010800033 20080108 00033 EU 2008 1 8 07FDEA05129 1 20071224 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS CROSSBEAM REPAIR LOCATED IN BULK CARGO UNDER FLOOR AT FRAME 64 RIGHT SIDE BETWEEN Y140 AND Y805, HAS 1 EACH REP AIR SECTION MEASURING 25.2" LONG AND 2 EACH REPAIR ANGLES MEASURING 9.2" LONG ON THE FWD AND AFT SIDES PREVIOUSLY INSTAL LED REPAIR LOCATED AT BULK CARGO FR 64 WAS DETERMINED NOT TO BE IAW A310 SRM 53-10-15 FIG 207 DUE TO INCORRECT THICKNESS BASED ON VISUAL EVALUATION WITH THE REPAIR INSTALLED. REMOVED EXISTING REPAIR AND REPAIRED IAW A310 SRM 53-10-15 FIG 2 07. THIS IS A REPAIR WITH NO AIRBUS ISSUED PART NUMBER, REPAIR IDENTIFIED BY THE AGING AIRCRAFT INSPECTION PROGRAM. 2 L 7 2 4F RT A35EU 2008010800034 20080108 00034 EU 2008 1 8 07FDEA05130 1 20071224 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS REPAIR LOCATED ON MAIN CABIN SEAT TRACK NR 4 LT Y1456 BETWEEN FRAMES 50 TO 52, HAS 4 EACH REPAIR SPLICES MEASU RING 7.4" LONG BY 3" TALL AND 1 EACH REPAIR SECTION 17" LONG. PREVIOUSLY INSTALLED REPAIR LOCATED AT MAIN CABIN SEAT TR ACK NR 4 LT Y1456 BETWEEN FRAMES 50 TO 52 WAS DETERMINED NOT TO BE IAW A310 SRM 53-10-16 FIG 205, DUE TO INCORRECT REPAI R INSTALLED, BASED ON A VISUAL EVALUATION WITH THE REPAIR INSTALLED. REMOVED EXISTING REPAIR AND REPAIRED SEAT TRACK PE R A310 SRM 53-10-16 FIG 205. THIS IS A REPAIR WITH NO AIRBUS ISSUED PART NUMBER, REPAIR IDENTIFIED BY THE AGING AIRCRAF T INSPECTION PROGRAM. 2 L 7 2 4F RT A35EU 2008010800035 20080108 00035 EU 2008 1 8 07FDEA05131 1 20071224 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS REPAIR LOCATED ON MAIN CABIN SEAT TRACK NR 4 LT Y1456 BETWEEN FRAMES 50 TO 52, HAS 4 EACH REPAIR SPLICES MEASUR ING 7.4" LONG BY 3" TALL AND 1 EACH REPAIR SECTION 17" LONG. PREVIOUSLY INSTALLED REPAIR LOCATED AT MAIN CABIN SEAT TRA CK NR 4 LT Y1456 BETWEEN FRAMES 50 TO 52 WAS DETERMINED NOT TO BE IAW A310 SRM 53-10-16 FIG 205, DUE TO INCORRECT REPAIR INSTALLED, BASED ON A VISUAL EVALUATION WITH THE REPAIR INSTALLED. REMOVED EXISTING REPAIR AND REPAIRED SEAT TRACK PER A310 SRM 53-10-16 FIG 205. THIS IS A REPAIR WITH NO AIRBUS ISSUED PART NUMBER, REPAIR IDENTIFIED BY THE AGING AIRCRAFT INSPECTION PROGRAM. 2 L 7 2 4F RT A35EU 2008010800037 20080108 00037 EU 2008 1 8 07FDEA05133 1 20071224 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS STRINGER REPAIR LOCATED IN BULK CARGO ON STRINGER 51 LT BETWEEN FRAMES 65 TO 66, HAS 1 EACH REPAIR SECTION ME ASURING 7.8" LONG AND 1 EACH REPAIR SPLICE MEASURING 7.5" LONG. PREVIOUSLY INSTALLED REPAIR LOCATED AT BULK CARGO ON ST RINGER 51 LT BETWEEN FRAMES 65 TO 66 WAS DETERMINED NOT TO BE IAW A310 SRM 53-10-14 FIG 201, DUE TO INCORRECT REPAIR SPL ICE MATERIAL INSTALLED, BASED ON A VISUAL EVALUATION WITH THE REPAIR INSTALLED. REMOVED EXISTING REPAIR SPLICE AND REPA IRED PER A310 SRM 53-10-14 FIG 201. THIS IS A REPAIR WITH NO AIRBUS ISSUED PART NUMBER, REPAIR IDENTIFIED BY THE AGING AIRCRAFT INSPECTION PROGRAM. 2 L 7 2 4F RT A35EU 2008010400222 20080104 00222 SO 2008 1 4 SWIA200718959 1 20071215 A 3520 OXYGEN MASK EMB 120 EMB120ER 3260203 SO CABIN UNWANTED DEPLOY A SWIA G O2 MASK DEPLOYED O OTHER CR CRUISE 1 NM 07 581SW 120349 FLT 3684 - INADVERTENT DEPLOYMENT OF PAX 02 MASKS. RESTOWED ALL MASKS. INSPECTED PRESSURIZATION SYSTEM WITH NO DEFECTS NOTED. 2 L 7 2 4T RT A31SO 2008010400223 20080104 00223 EA 2008 1 4 SWIA200718960 1 20071209 A 2916 73031 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYSTEM MALFUNCTIONED A SWIA O OTHER O OTHER AP APPROACH 1 NM 07 439SW 16716 16716 7578 FLT 3896 - WHEN SELECTING GEAR DOWN ON FINAL, NOSE GEAR DIDN'T COME DOWN. CYCLED GEAR TWICE AND RECEIVED THREE GREEN IN DICATIONS. REPLACED NR 3 HYDRAULIC RESERVOIR IAW AMM 29-12-30, AND PERFORMED EXTENSION/RETRACTION FUNCTIONAL TEST IAW A MM 32-30-00 OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2008010700005 20080107 00005 2008 1 7 YENA2007115 4 20071212 A 2330 ENTERTAIN SYS AIRBUS 320 A320232 3930326 EU CABIN MALFUNCTIONED A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 565JB 2031 FLT 706, SJU-JFK, APRX 04:00Z-06:00Z, LIVE TV-FLIGHT ATTENDANT REPORTED BURNING RUBBER SMELL FROM UNDER SEAT 23B. AFTER TURNING OFF SYSTEM SMELL DISAPPEARED. INSPECTED ROW 23ABC SEB & VDU'S. INSPECTED ROWS 21ABC THROUGH 25ABC. NO ABNORM ALITIES FOUND. REMOVED AND REPLACED SEB & VDU'S AS PRECAUTIONARY PER TSM 23-39-00-810-804. ALL OPS CHECK NORMAL IAW 23 -39-00. 2 L 7 2 4F RT A28NM 2008010700007 20080107 00007 NM 2008 1 7 WRLA2007135 1 20071217 A 5250 AR47261 SOLENOID DOUG MD11 MD11F 3023600 NM PWA 4460 PW4460 NE COCKPIT DOOR MALFUNCTIONED A WRLA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 279WA 48756 GEC 8282 EGNX/KJFK 12/15/2007 - INTENSE ODOR TOP OF CLIMB. DISCOVERED ODOR COMING FROM COCKPIT DOOR ELECTRIC LATCHING M ECHANISM. BREAKER PULLED ODOR CEASED. REMOVED AND REPLACED DOOR ELECTRIC STRIKER ASSY PER MM 52-51-04. 2 L 7 3 4F 4 F RT A22WE E24NE 2008010700009 20080107 00009 SO 2008 1 7 RAIA00712007 1 20071207 A 3610 40303925SD O-RING EMB 145 EMB145 3260210 SO BLEED AIR SYS BLOWN A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 812HK 145373 FLT NR 5543 - STL - BLEED NR 1 LEAK AFTER ENTERING ICE CONDITIONS. MAINTENANCE REMOVED AND REPLACED ALL BLEED LINE O-RI NGS, NO LEAKS NOTED AT THIS TIME. 2 L 7 2 4F RT T00011AT 2008010700014 20080107 00014 SO 2008 1 7 RAIA00712014 1 20071211 A 3610 SEAL EMB 145 EMB145 3260210 SO BLEED AIR SYS LEAKING A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 809HK 145187 FLT NR 8092 - ROC - BLEED LEAK 1 MESSAGE AFTER TAKEOFF. MAINTENANCE REPLACED BLEED AIR SEAL AT AFT FUSELAGE LOWER FAIRI NG, PERFORMED ENGINE GROUND RUN, NO LEAKS NOTED, NO LEAK MESSAGE NOTED. 2 L 7 2 4F RT T00011AT 2008010700015 20080107 00015 2008 1 7 YENA2007122 4 20071222 A 2370 Z010H000521A COMPUTER AIRBUS 320 A320232 3930326 EU NR 1 CIDS FAILED A YENA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 524JB 21370 68 1528 FLT NR 271, FLL-OAK, CIDS FAILED COMPLETELY IN-FLIGHT. EVACUATION HORN CAME ON AND COULD NOT BE CANCELED. ALL INTERCOM , PA FUNCTIONS LOST. CABIN LIGHTS ON AND OFF INTERMITTENTLY. OVERWEIGHT LANDING ACCOMPLISHED IN FLL. LANDING WEIGHT 1 52K LBS. SPEED 139K. VERTICAL SPEED LESS THAN 200 FT PER MIN. FOUND NR 1 CIDS DIRECTOR CYCLING & WILL NOT TEST. REMOVE D AND REPLACED NR 1 CIDS DIRECTOR IAW 23-73-34. CHECKS NORMAL. 2 L 7 2 4F RT A28NM 2008010700017 20080107 00017 NM 2008 1 7 07FDEA05124 1 20071223 A 5730 652811535 PLATE BOEING 727 727232 1384082 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 499FE 21018 CRACKED ANGULAR PLATE INBD OF LT WING INBD TE FLAP O/B TRACK ALONG AFT SUPPORT FRAME REMOVED AND REPLACED CRACKED ANGULA R PLATE IAW SRM 51-40-3 PAINTED AREA IAW SRM 51-20-151-7. 2 L 7 3 4F A3WE 2008010700019 20080107 00019 2008 1 7 SA07084 4 20071220 A 2565 CABLE AIRBUS A319 A319112 3930323 EU SLIDE CYLINDER BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 713UW 1040 DCA - THE LEFT HAND, OVERWING SLIDE CYLINDER ASSEMBLY HAS A BROKEN CABLE END. MAINTENANCE REPLACED THE LEFT HAND, OVERW ING SLIDE CYLINDER ASSEMBLY. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2008010700026 20080107 00026 NM 2008 1 7 2007UALA05136 1 20071215 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN UNSECURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 513UA 24810 EMERGENCY EXIT LIGHTS COMING UP NEAR ROW 28. SECURED TRACK COVER. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700032 20080107 00032 EU 2008 1 7 2007UALA05144 1 20071217 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 485UA 1617 CORROSION ON R2 DOOR SILL AT FWD AND AFT FASTENER HOLES. MAJOR REPAIR ACCOMPLISHED AT LCQ. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010700039 20080107 00039 NM 2008 1 7 2007UALA05151 1 20071218 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY LIGHT ROW 43 LT INOP. RELAMPED 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700050 20080107 00050 NM 2008 1 7 2007UALA05162 1 20071218 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 THE R-4 DOOR UPPER GATE CRACKED AT SECOND LT HINGE MOUNT HOLES. REPLACED LOWER GATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700053 20080107 00053 NM 2008 1 7 2007UALA05165 1 20071218 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 BS 1500 FRAME BETWEEN STR 28R - 29R HAS DAMAGE. FRAME REPAIR BETWEEN STR 28R-29R HA S BEEN DEEMED INTERIM WITH REPEAT I NSPECTIONS EVERY 12000 CYCLES. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700066 20080107 00066 NM 2008 1 7 2007UALA05180 1 20071220 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EEL LIGHTS INOP AT SEATS 5A AFT, 50L & 56L. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700078 20080107 00078 NM 2008 1 7 2007UALA05193 1 20071220 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 847 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 50961 24640 AFT PIT STA 847 RBL 20 FRAME UPPER CHORD UPPER SURFACE HAS MISDRILLED FASTENER. SUSPECT MAINTENANCE MISTAKE. REMOVED DA MAGED FRAME AND REPLACED WITH NEW FRAME. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010700094 20080107 00094 NM 2008 1 7 USAA920071360 1 20071219 A 5230 6547952524A DOOR FRAME BOEING 737 7373G7 1384595 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CRACKED AFT CARGO COMPARTMENT DOOR FRAME. REPLACED AFT CARGO DOOR IAW B737 AMM 52-31-00 -4. 2 L 7 2 4F RT A16WE 2008010700096 20080107 00096 NM 2008 1 7 USAA920071362 1 20071104 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT BEAM, BS 727D, LBL 6. REPAIRED AFT CAR GO COMPARTMENT FLOOR SUPPORT BEAM, BS 727D, LBL 6 IAW USAIRWAYS EA 100061. 2 L 7 2 4F RT A16WE 2008010700098 20080107 00098 EU 2008 1 7 YEAN2007116 1 20071216 A 3234 HANDLE EMB ERJ190 ERJ190100IGW 3260408 EU MLG MALFUNCTIONED A YENA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 EA 15 216JB 19000026 FLT NR 141, JFK TO RSW, RETURNED TO JFK, LANDING GEAR HANDLE WOULD NOT RAISE AFTER TAKEOFF. FOLLOW QRH PROCEDURES INCLU DING WOW SWITCH FAILURE. NORMAL LANDING, ALL OTHER WOW AFFECTED SYSTEMS, OPERATED NORMALLY. TROUBLESHOT AS PER FIM REF 32-33-00-810-802-A. NO LDG WOW SENSOR TGT DISAGREE MESSAGES NOTED ON CMC. ACCOMPLISHED OPS TEST OF LDG CONTROL LEVER AMM REF 32-33-00-710-801-A. CHECKS GOOD. ACCOMPLISHED SEVERAL EXTENSION AND RETRACTIONS OF THE LDG GEAR HANDLES OPERAT ED NORMAL AND NO FAULTS NOTED. CHECKED NLG AND MLG SHOCK STRUT H DIMENSIONS. ALL WITHIN LIMITS AS PER AMM REF'S 12-12- 07 AND 12-12-09. FAULT CONSIDERED TRANSITORY CONDITION OF THE LDG CONTROL LEVER. 2 L 7 2 4F RT A57NM 2008010700099 20080107 00099 EU 2008 1 7 YENA2007116 1 20071216 A 3234 HANDLE EMB ERJ190 ERJ190100IGW 3260408 EU MLG MALFUNCTIONED A YENA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 EA 15 216JB 19000026 FLT NR 141, JFK TO RSW, RETURNED TO JFK, LANDING GEAR HANDLE WOULD NOT RAISE AFTER TAKEOFF. FOLLOW QRH PROCEDURES INCLU DING WOW SWITCH FAILURE. NORMAL LANDING, ALL OTHER WOW AFFECTED SYSTEMS, OPERATED NORMALLY. TROUBLESHOT AS PER FIM REF 32-33-00-810-802-A. NO LDG WOW SENSOR TGT DISAGREE MESSAGES NOTED ON CMC. ACCOMPLISHED OPS TEST OF LDG CONTROL LEVER AMM REF 32-33-00-710-801-A. CHECKS GOOD. ACCOMPLISHED SEVERAL EXTENSION AND RETRACTIONS OF THE LDG GEAR HANDLES OPERAT ED NORMAL AND NO FAULTS NOTED. CHECKED NLG AND MLG SHOCK STRUT H DIMENSIONS. ALL WITHIN LIMITS AS PER AMM REF'S 12-12- 07 AND 12-12-09. FAULT CONSIDERED TRANSITORY CONDITION OF THE LDG CONTROL LEVER. 2 L 7 2 4F RT A57NM 2008010700100 20080107 00100 WP 2008 1 7 IXXA07SMN258S 1 20071115 A 5512 SKIN DOUG DC8 DC873F 302199F WP HORIZONTAL STAB MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE HAS A IMPROPER REPAIR AT STATION XFS 1 78.750. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION NOTED. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA, REPAIR PART. IN STALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 51-1-11, 51-1-20D, 51-3-1, FAA FORM 8110-3 NUMBER 07569 DATED 11-27-07, S EMAN DRAWING NUMBER ED-4653 DATED 11-09-07, DC8 SRM 51-1-21, SRM 51-3-0, DC8 NDT SPM PART 08-00-02 TO 07, FORM SEMAN 242 -4, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008010700101 20080107 00101 WP 2008 1 7 IXXA07SMN259S 1 20071115 A 5512 SKIN DOUG DC8 DC873F 302199F WP HORIZONTAL STAB DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE WITH DENT AT STATION XFS 242.000. REM OVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIME D AREA, REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 52-2-1 FIGURE 4, DC8 SRM 51-1-21, 51-1-21A, DC8 SRM 55-2-1, FIGURE 4, SRM 55-3-1 FIGURE 1 SHEET 1 AND 2 ITEM "A", AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008010700102 20080107 00102 NM 2008 1 7 QXEA200701913 1 20071217 A 3610 8209076 SWITCH BOMBDR DHC8 DHC8402 1390042 NM BLEED OVERTEMP MALFUNCTIONED A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 409QX 4051 SEA - FLIGHT 2322 - NR 2 BLEED HOT CAUTION LIGHT ILLUMINATED. DUCT TEMP WAS 30 DEGREES C. RAN CHECKLIST, CAUTION WENT OUT. TURNED BLEED BACK ON, DUCT WAS AT 20 DEGREES AND CAUTION CAME BACK ON. NO HEAT IN FLIGHT COMPARTMENT. LEFT BLEED OFF. MAINTENANCE REPLACED THE BLEED OVERTEMP SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008010700104 20080107 00104 NM 2008 1 7 QXEA200701907 1 20071217 A 2430 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM NR 1 DC GEN ILLUMINATED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 403QX 4037 MSO - FLIGHT 2397 - NR 1 DC GENERATOR CAUTION LIGHT ILLUMINATED. RESET GENERATOR PER THE CHECKLIST, BUT THE LIGHT REMAI NED LIT. MAINTENANCE PLACED SYSTEM ON MEL 24-30-6. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008010700106 20080107 00106 EU 2008 1 7 1218341121907 1 20070925 A 5210 24T3 SKIN AEROSP AEROSP ATR42 ATR42320 8680930 EU PUNCTURED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 14834 193 PASSENGER DOOR EXTERNAL SKIN PUNCTURED. EXTERNAL SKIN REPAIRED PER SRM 52-00-00. 2 H 7 2 4T RT A53EU 2008010700107 20080107 00107 NM 2008 1 7 MZZA0700765 1 20071216 A 5330 SKIN BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 14249 28809 FOUND IG CORROSION ON R2 DOOR STRAP, AFT CUTOUT, INNER SKIN AREA. REPAIRED PER ECRA 5330-03761. 2 L 7 2 4F RT A16WE 2008010700109 20080107 00109 NM 2008 1 7 MWEA070302 1 20071213 A 5230 PAN BOEING 717 717200 1383700 NM CARGO DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 914ME 55177 SHARP GOUGE ON INNER PAN OF AFT CARGO DOOR AT FORWARD TORQUE TUBE. BLENDED OUT NICK FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2008010700111 20080107 00111 NM 2008 1 7 SCNA07016 1 20071214 A 3350 BATTERY PACK BOEING 737 737800* NM EMERGENCY LIGHTS WEAK A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 PHHZG 28379 FLIGHT CREW REPORTED L-1 DOOR EMERGENCY LIGHT BATTERY WEAK, FAILED CAPTAIN CHECK. MAINTENANCE REMOVED AND REPLACED L1 D OOR EMERGENCY LIGHT BATTERY PACK. 2 L 7 2 4F RT A16WE 2008010700112 20080107 00112 NM 2008 1 7 NWAA074126307 1 20071106 A 5311 FRAME BOEING 747 747451 1384940 NM BS 1160 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 667US 24222 DURING "M" CHECK, FOUND 5 HOLES WITH CRACKS AT BS 1160 FRAME TENSION TIE AREA. REPAIRED PER EA 63-211309. 2 L 7 4 4F RT A20WE 2008010700113 20080107 00113 NM 2008 1 7 NWAA074136307 1 20071204 A 5311 FRAME BOEING 747 747451 1384940 NM BS 1180 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 667US 24222 DURING "M" CHECK, FOUND 3 HOLES WITH CRACKS AT BS 1180 FRAME TENSION TIE AREA. REPAIRED PER EA 63-211310. 2 L 7 4 4F RT A20WE 2008010700115 20080107 00115 NM 2008 1 7 NWAA074116307 1 20071105 A 5315 FLOORBEAM BOEING 747 747451 1384940 NM BS 940 WORN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 667US 24222 DURING "M" CHECK, FOUND UPPER DECK FLOORBEAM WEB EDGE WORN AT BS 940 RBL 30. REPAIRED PER EA 63-211312. 2 L 7 4 4F RT A20WE 2008010700117 20080107 00117 NM 2008 1 7 NWAA074146307 1 20071205 A 5340 FITTING BOEING 747 747451 1384940 NM BS 2040-2060 MISINSTALLED A NWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 01 667US 24222 DURING "M" CHECK, DURING ACCOMPLISHMENT OF DOOR 5 CREW REST MODIFICATION PER SB 747-53-2481 FOUND NEW FITTING AT BS 2040 -2060 S11R-S12R WITH INSUFFICIENT EDGE MARGIN. REPAIRED PER EA 63-211300. 2 L 7 4 4F RT A20WE 2008010700120 20080107 00120 NM 2008 1 7 SCNA07017 1 20071219 A 3397 CONNECTOR BOEING 737 737800* NM EMERGENCY LIGHTS UNSECURE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 PHHZG 28379 CREW REPORTED ROWS 13&14 CEILING AREA HAS FLAPPING NOISE DURING TAXI. MAINTENANCE FOUND EMERGENCY EXIT SIGN ELECTRICAL CONNECTOR AND WIRING HANGING DOWN FROM WIRE BUNDLE. RESECURED WIRING TO OVERHEAD WIRE BUNDLE. 2 L 7 2 4F RT A16WE 2008010700122 20080107 00122 NM 2008 1 7 PIDA07058 1 20071217 A 5542 SKIN BOEING 737 737228 13844AG NM RUDDER CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 251TR 23792 DURING MAINTENANCE CHECK, NOTED A CRACK IN THE LEADING EDGE OF THE RUDDER AT RUDDER STATION 58.6. REPAIRED PER BOEING T ELEX 1-720703898-1 AND -3 WITH FAA DOA APPROVED 8100-9 DATED DEC 15, 2007. SUSPECT DAMAGE OCCURRED DURING RUDDER REMOVA L FROM VERTICAL FIN. 2 L 7 2 4F RT A16WE 2008010700124 20080107 00124 WP 2008 1 7 UPS07851308 1 20071214 A 3350 6012233 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-50-01-2 AND TESTED. 2 L 7 4 4F RT 4A25 2008010700143 20080107 00143 CE 2008 1 7 BSAASDR0727 1 20071211 A 3620 PRESSURE SWITCH BEECH 1900 1900D 1154162 CE BLEED AIR SYS DIRTY A BSAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 05 173YV UE173 RIGHT BLEED AIR FAIL LIGHT ILLUMINATD. THE RIGHT BLEED AIR PRESSURE SWITCH WAS CLEANED AND EVA TUBING INSPECTED FOR LEA KS. AIRCRAFT RAN ON GROUND AT HIGH POWER SETTINGS. NO OTHER DEFECTS WERE NOTED. 2 L 7 2 4T RT A24CE 2008010700174 20080107 00174 EU 2008 1 7 USAA920071370 1 20071216 A 5320 D534800422006 FITTING AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 624AW 55 SAL - MAJOR REPAIR - C-6 CHECK - CORROSION ON AFT CORNER FITTING OF LEFT AFT PASSENGER CREW DOOR AT BS 3257/ FR 68. REP LACED AFT CORNER FITTING OF LEFT AFT PASSENGER CREW DOOR AT BS 3257/ FR 68 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008010700176 20080107 00176 EU 2008 1 7 USAA920071371 1 20071217 A 5320 D53480042204 FITTING AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 624AW 55 SAL - MAJOR REPAIR - C-6 CHECK - CORROSION ON FWD CORNER FITTING OF LEFT AFT PASSENGER CREW DOOR AT BS 3158+3"/ FR 66 + 3", S23L. REPLACED FWD CORNER FITTING OF LEFT AFT PASSENGER CREW DOOR AT BS 3158+3"/ FR 66 + 3", S23L IAW A320 SRM 51-7 2-11. 2 L 7 2 4F RT A28NM 2008010700202 20080107 00202 NM 2008 1 7 2007UALA05215 1 20071222 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 117UA 28810 FUSELAGE EXTERNAL SKIN DENTED & SMALL CRACK, BS 2190 STR 26R. MAJOR REPAIR ACCOMPLISHED: INSTALLED EXTERNAL DOUBLER. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700217 20080107 00217 NM 2008 1 7 2007UALA05225 1 20071221 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 526UA 24994 EMERGENCY LIGHT SIGN AT DOOR 3R IS ILLUMINATED AS WELL AS SEVERAL FLOOR PATH LIGHTS IN SEVERAL AREAS WITH EMERGENCY LIGH TS IN OFF AS WELL AS ARMED. BATTERY PACK FAILURE. REPLACED BATTERY PACKS M10817 AND M10818. EMER LIGHTS OPERATE NORMA LLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700232 20080107 00232 NM 2008 1 7 2007UALA05244 1 20071222 A 2611 SMOKE DETECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CARGO BAY FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 314UA 23675 CARGO TEST FAILED A-B FWD AND AFT. SUSPECT CIRCUIT BREAKER LEFT OPEN DURING MAINTENANCE. RESET CIRCUIT BREAKER OPS CHEC K GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010700237 20080107 00237 SW 2008 1 7 WGEA200700026 1 20071220 A 5210 521032171005 DOOR ECLIPS EA500 ECLIPSEEA500 3350000 SW ZONE 800 OUT OF ADJUST E WGEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 132DJ 180 000034 PASSING THROUGH 18,000 FT, DOOR CAS MESSAGE CAME ON, DESCENDING THROUGH 9000 FT DOOR LIGHT WENT OUT. PRESSURIZATION NOR MAL. PERFORMED CABIN PRESSURIZATION TEST IAW EA500 AMM 21-30-03. FOUND PAX DOOR TO BE OUT OF ADJUSTMENT. ADJUSTED PAX DOOR IAW EA500 AMM 52-00-00. PERFORMED CABIN PRESSURIZATION TEST, NO UNSAFE DOOR CAS MESSAGE, NO OTHER DEFECTS NOTED I AW EA500 AMM 21-30-03. 1 L 7 2 4J RT A00002AC 2008010700238 20080107 00238 2008 1 7 UPS07M51316 4 20071219 A 3414 4059060901 INDICATOR DOUG MD11 MD11F 3023600 NM AIRSPEED ERRATIC A IPXA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 285UP 48457 ATB - PASSING THRU 10000 FT (FL100) NOTED ALT COMPARATORS ON BOTH PFD, THEN A/S COMPARATOR ALTIMETERS WERE IN ERROR OF U P TO 150-180 FT. FCP PANEL FUNCTIONS WENT TO DASHES. PERFORMED AIRSPEED, LOST, SUSPECT ERRATIC. REMOVED AND REPLACED ADC NR 2 IAW AMM 34-16-01-4. SEE P/N S/N OFF BELOW. REMOVED AND REPLACED FO'S PITOT TUBE IAW AMM 34-11-01-2, P/N OFF: 851DK, S/N OFF: 246454. REMOVED AND REPLACED RT AOA SENSOR IAW AMM 27-35-02-4, P/N OFF: 2568A13, S/N OFF: 038-2A. 2 L 7 3 4F RT A22WE 2008010700239 20080107 00239 NM 2008 1 7 P5CA0701541 1 20071215 A 4900 APU BOEING 747 74746NF 13848BT NM AUTO SHUTDOWN A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 451PA 30809 RECEIVED "APU" AND "APU DOOR" STATUS MESSAGES AND APU AUTO SHUTDOWN FOLLOWING ENGINE START. RETURN TO BLOCKS AND APPLIE D MEL 49-11-1 AND 49-15-1A. MAINTENANCE ACTION WAS ACCOMPLISHED AS PER THE DDG. 2 L 7 4 4F RT A20WE 2008010700240 20080107 00240 2008 1 7 WRNA200700063 4 20071220 A 3418 2566A30A SENSOR BOEING 747 747212B 1384886 NM AOA NO TEST A WRNA C ABORTED TAKEOFF L NO TEST TO TAKEOFF 1 SO 05 526UP 21937 DURING TAKEOFF, AT 80 KNOTS, CREW RECEIVED A STALL WARNING, TAKEOFF WAS ABORTED. AOA FAILED TEST IAW B747 MM 27-32-00 P G 507. REPLACED AOA SENSOR IAW 747 MM 27-32-01 PG 102. SYSTEM TEST GOOD IAW 747 MM 27-32-00 PG 507. AIRCRAFT RELEASE D FOR SERVICE. 2 L 7 4 4F RT A20WE 2008010700241 20080107 00241 EU 2008 1 7 YEAN2007120 1 20071218 A 2911 SEAL EMB ERJ190 ERJ190100IGW 3260408 EU ATTENUATOR LEAKING A YENA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 15 179JB 5293 0202 19000006 FLT NR 1218, BUF-BOS, LOSS OF HYDRAULIC SYSTEM 2, FOUND NR 2 ENG EDP PRESS ATTENUATOR LEAKING, REMOVED AND REPLACED ATTE NUATOR FOR NR 2 EDP PER AMM 29-11-27. PERFORMED ENGINE DRIVEN PUMP INSPECTION/CHECK PER AMM 05-50-23. PERFORMED NR 2 H YD SYS PRESSURE/RETURN/CASE DRAIN FILTER INSP/REPLACEMENT PER AMM 29-11-05, NO CONTAMINATION OR DEBRIS FOUND. LEAK CHEC KS OK, PERFORMED EDP OPS TEST PER AMM 29-10-00, LEAK AND PRESS CHECK OK. PERFORMED LANDING GEAR FREE FALL CONDITION INS P/CHECK PER AMM 05-50-14 DUE TO LOSS SYS 2 HYD PRESS, ALTERNATE LANDING GEAR EXTENSION SYSTEM WAS UTILIZED. 2 L 7 2 4F RT A57NM 2008010700242 20080107 00242 2008 1 7 UPS07151322 4 20071223 A 2565 D31023101 SLIDE AIRBUS A300 A300F4622R 3930360 EU PAX DOOR DISLODGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 133UP 0816 MAIN CABIN DOOR SLIDE CAME OUT OF CONTAINER. ESCAPE SLIDE INSTALLED IAW AMM 25-61-21-4. 2 L 7 2 4F RT A35EU 2008010700243 20080107 00243 2008 1 7 UPS07851319 2 20071221 A 7261 D51P5410133 LINE DOUG DC8 DC873F 302199F WP NR 4 ENG OIL LEAKING A IPXA E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION DE DESCENT 1 SO 01 840UP 46140 NR 4 ENG LOW OIL PRESSURE AND QTY ON DESCENT INTO SDF. REMOVED AND REPLACED LINE SUPPLY OIL TO OIL PRESSURE TRANSMITTER IAW MM 20-12-00-2. LEAK AND OPS CHECK GOOD IAW MM 71-00-00. 2 L 7 4 4F RT 4A25 2008010700244 20080107 00244 NM 2008 1 7 UPS07M51321 1 20071222 A 3350 LIGHT DOUG MD11 MD11F 3023600 NM R1 DOOR INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 272UP 48571 R1 DOOR LOWER EMERGENCY LIGHTS ARE INOP. PERFORMED FUNCTIONAL TEST PER TC 112. OPS CHECK NORMAL. 2 L 7 3 4F RT A22WE 2008010700262 20080107 00262 NM 2008 1 7 2007UALA05256 1 20071222 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EMERGENCY EXIT LIGHT INOP AT LAV 112. REPLACED LAMP AND FUSE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700265 20080107 00265 NM 2008 1 7 2007UALA05259 1 20071222 A 3350 794640 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EEL INOP, "B" ZONE LT FWD & "E" ZONE RT AFT LIGHT. REPLACED CABLE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700274 20080107 00274 NM 2008 1 7 2007UALA05268 1 20071222 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 DOOR 4 LEFT EMERGENCY CROSS AISLE LIGHT IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700299 20080107 00299 NM 2008 1 7 2007UALA05280 1 20071224 A 2621 309903889U1 SQUIB BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FIRE EXTINGUISH FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 CARGO FIRE EXT SYS TEST FAILED. REPLACED SQUIB, BOTTLE B FWD SQUIB. PER MM26-23-02.SQUIB TEST NORMAL. AC OK FOR SERVICE . 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700300 20080107 00300 NM 2008 1 7 2007UALA05281 1 20071225 A 2612 FIRE LOOP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT NACELLE INTERMITTENT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 558UA 26654 RIGHT ENGINE LOOP 2 FIRE DETECTION INOPERATIVE. PROBLEM WAS INTERMITTENT FROM DAY ONE..HARD TO DIAGNOSE. AFTER SEVERAL WEEKS ON THE WATCH LIST, THE ISSUE NEVER RETURNED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700301 20080107 00301 NM 2008 1 7 2007UALA05282 1 20071224 A 5320 FITTING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 532UA 25072 AFT PRESSURE BULKHEAD BS 1720 AND STR 17R, FITTING IS CORRODED THROUGH. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700305 20080107 00305 NM 2008 1 7 2007UALA05287 1 20071226 A 3040 6240663 CONTROLLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WINDSHIELD HEAT FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 551UA 25399 RETURNED TO FIELD DUE TO A CRACKED WINDSHIELD. FOUND HEAT CONTROLLER FAILED CAUSING OVERHEATING OF WINDSHIELD, CRACKIN G. REPLACED WINDOW HEAT CONTROLLER AND FO'S WINDSHIELD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700310 20080107 00310 2008 1 7 2007UALA05293 4 20071225 A 2565 COVER BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU R1 DOOR OUT OF POSITION A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 922UA 26642 CREW REPORT: DOOR 1R UNABLE TO SEE SLIDE SIGHT PRESSURE GAUGE. SLIDE IMPROPERLY INSTALLED. REPLACED SLIDE PER MM 25-6 1-35 P201. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010700314 20080107 00314 EU 2008 1 7 USAA920071377 1 20071209 A 5321 D5367204400000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU CABIN PERFORATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 649AW 803 SAL - MAJOR REPAIR - C-7 CHECK- PERFORATION DAMAGE ON FLOOR PANEL 151QF IN AFT CABIN AT BS 2723/FR 58 - BS 2776/FR 59, - Y765 - Y970.8. REPLACED FLOOR PANEL 151QF IN AFT CABIN AT BS 2723/FR 58 - BS 2776/FR 59, -Y765 -Y970.8 IAW A320 SRM 53 -20-00. 2 L 7 2 4F RT A28NM 2008010700317 20080107 00317 NM 2008 1 7 200712271 1 20071224 A 3240 52615500 PRESSURE SWITCH EMB ERJ170 ERJ170100SE 3260406 NM BRAKE SYSTEM DEFECTIVE A UHLA O OTHER J WARNING INDICATION DE DESCENT 1 GL 11 651RW 17000072 FLIGHT 7643 ORD TO CMH DURING DESCENT EMER/PARKING BRAKE LIGHT ILLUMINATED AND REMAINED ON. THE CREW DECLARED AN EMERGE NCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 BRAKE PRESSURE SWITCH. 2 L 7 2 4F RT A56NM 2008010700327 20080107 00327 NM 2008 1 7 SWAA076439 1 20071222 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727C, STR 14R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008010800005 20080108 00005 NM 2008 1 8 ASAA0772408 1 20071205 A 5320 146A75031 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO FLOOR SUPPORT RAIL BS 727+9 LBL 3 CORRODED. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008010800006 20080108 00006 NM 2008 1 8 ASAA0772409 1 20071205 A 5320 453A261125 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO FLOOR SUPPORT ANGLE BS 727+4 LBL 21 TO RBL 21 CORRODED. SUPPORT ANGLE REPLACED REF TC 5087341 FOR INSTALL. 2 L 7 2 4F RT A16WE 2008010800008 20080108 00008 NM 2008 1 8 ASAA0772411 1 20071205 A 5347 146A750125 CARGO TRACK BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT RIGHT TIE DOWN TRACK BS 727+10 RBL 14 CORRODED. TIE DOWN TRACK REPLACED ON TC 5113801. 2 L 7 2 4F RT A16WE 2008010800021 20080108 00021 NM 2008 1 8 CALA0700776 1 20071220 A 5330 65C3578529 SKIN BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17619 27332 TOOLING MARKS AND SURFACE CORROSION AT UPPER ATC ANTENNA MOUNT SURFACE. SHEET METAL REPAIR COMPLETED AS PER ECRA 5331-0 1375 AND AMM 34-53-11. 2 L 7 2 4F RT A16WE 2008010800023 20080108 00023 NM 2008 1 8 CALA0700778 1 20071221 A 5320 66142101 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 CABIN FWD ENTRY, STRINGER 11L FWD SIDE OF L-1 DOOR CUTOUT WEB FWD UPPER SUPPORT CLIP CRACKED. REMOVED AND REPLACED INTE RCOSTAL WEB AND SHEAR TIE REF ECRA 5311-01382. 2 L 7 2 4F RT A16WE 2008010800032 20080108 00032 NM 2008 1 8 CALA0700787 1 20071209 A 5322 63353503 SHEAR TIE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 47332 23570 SHEAR TIE CORRODED BEHIND AFT PIT AFT BULKHEAD 1 FRAME AFT OF POT WATER PANEL IN CENTER OF AC BELLY SKIN. PERFORMED REP AIR STA 967 STRINGER 27L AND 27R PER ECRA 5310-04681 AND SRM 53-00-07. 2 L 7 2 4F RT A16WE 2008010800040 20080108 00040 EU 2008 1 8 07FDEA05136 1 20071224 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS CROSSBEAM REPAIR LOCATED IN AFT CARGO UNDER FLOOR AT FRAME 63 BETWEEN ROLLER TRACKS NR 3 LT Y1470 TO PRODUCTI ON SPLICE INBOARD OF NR 3 RT Y1470, HAS 3 EACH REPAIR SECTIONS PREVIOUSLY INSTALLED REPAIR LOCATED AT AFT CARGO UNDER FL OOR AT FRAME 63 BETWEEN ROLLER TRACKS NR 3 LT Y1470 TO PRODUCTION SPLICE INBOARD OF NR 3 RT Y1470 WAS DETERMINED NOT TO BE IAW A310 SRM 53-10-15 FIG 207, DUE TO INCORRECT REPAIRS INSTALLED, BASED ON A VISUAL EVALUATION WITH THE REPAIR INSTA LLED. REMOVED CROSSBEAM AND REPLACED FROM PRODUCTION SPLICE TO EXISTING REPAIR ON LEFT SIDE I/B OF NR 3 LT Y1470 ROLLER TRACK PER A310 SRM 53-10-15 FIG 207 51-72-10. NO AIRBUS PART NUMBER, IDENTIFIED BY AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008010800044 20080108 00044 EA 2008 1 8 TRAX200701962 1 20071221 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA BS 302 INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 871AS 7537 EXTERIOR EMERGENCY LIGHT FORWARD OF THE PASSENGER DOOR AT FS 302.40L IS INOP. 2 L 7 2 4F RT A21EA 2008010800045 20080108 00045 EU 2008 1 8 TRAX200701963 1 20071222 A 3350 3011210 LIGHT AEROSP ATR72 ATR72212 8680945 EU PAX DOOR INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 635AS 372 PAX DOOR LOWER STEP BOARDING LIGHT INOP. 2 H 7 2 4T RT A53EU 2008010800046 20080108 00046 EA 2008 1 8 TRAX200701964 1 20071222 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 974EV 7594 ASD AFT DRAG ANGLE CRACKED. 2 L 7 2 4F RT A21EA 2008010800048 20080108 00048 NM 2008 1 8 QXEA200702028 1 20071226 A 5230 HANDLE BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR UNSECURE A QXEA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 NM 09 408QX 4050 MFR - FLIGHT 2460 - AT ROTATION RECEIVED A FUSELAGE DOORS WARNING LIGHT. AIRCRAFT WOULD NOT PRESSURIZE. RETURNED TO TH E FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE FOUND THE CARGO DOOR HANDLE NOT SECURE (AFT). COMPLIED WITH OPERATIONAL CHECK OF THE DOOR WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008010800049 20080108 00049 EU 2008 1 8 YENA2007120 1 20071218 A 2910 SEAL EMB ERJ190 ERJ190100IGW 3260408 EU ATTENUATOR LEAKING A YENA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 15 179JB 5293 0202 19000006 FLT NR 1218, BUF-BOS, LOSS OF HYDRAULIC SYSTEM 2, FOUND NR 2 ENG EDP PRESS ATTENUATOR LEAKING. REMOVED AND REPLACED ATT ENUATOR FOR NR 2 EDP PER AMM 29-11-27. PERFORMED ENGINE DRIVEN PUMP INSPECTION/CHECK PER AMM 05-50-23. PERFORMED NR 2 HYD SYS PRESSURE/RETURN/CASE DRAIN FILTER INSP/REPLACEMENT PER AMM 29-11-05, NO CONTAMINATION OR DEBRIS FOUND. LEAK CHE CKS OK. PERFORMED EDP OPS TEST PER AMM 29-10-00, LEAK AND PRESS CHECK OK. PERFORMED LANDING GEAR FREE FALL CONDITION I NSP/CHECK PER AMM 05-50-14 DUE TO LOSS SYS 2 HYD PRESS, ALTERNATE LANDING GEAR EXTENSION SYSTEM WAS UTILIZED. 2 L 7 2 4F RT A57NM 2008010800053 20080108 00053 NM 2008 1 8 ASAA0772439 1 20071212 A 5210 141465522 SKIN BOEING 737 737790 13844CN NM R1 DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 SEVERAL ABRASION DAMAGES FOUND ON R1 DOOR AROUND UPPER INTERNAL ACCESS CUTOUT OF UPPER HINGE ARM. DAMAGED INNER SKIN RE PLACED WITH MADE REPAIR PART IAW BAC ENG DWG 141A6552 & 141A6516 AND B737 700 SRM 52-10-01, 51-40-05 & 51-40-02. 2 L 7 2 4F RT A16WE 2008010800057 20080108 00057 NE 2008 1 8 HALA0700552 2 20071224 A 7297 CONNECTOR BOEING 767 7673G5 1385126 NM PWA 4060 PW4060 52119 NE DIRTY A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM, RT PIMU MSG T5 CROSS CHECK FAIL A AND B CHANNEL FAULTED LEGS 1-4-16. CLEANED T5 CONNECTER PIM U BITE CHK OK PER FIM PIMU MSG INDEX PG 620. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010800058 20080108 00058 NM 2008 1 8 ASAA0772421 1 20071206 A 5320 146A81275 SHIELD BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT BS 847 TO BS 867 CORRODED. SHIELD RBL 21 REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 53-60-15 FIT 5 5 1-30-01, 51-40-02 & 51-40-05. 2 L 7 2 4F RT A16WE 2008010800059 20080108 00059 NM 2008 1 8 HALA0700553 1 20071225 A 2841 WARNING MESSAGE BOEING 767 76733A 1385209 NM FUEL INDICATOR FALSE INDICATION A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 587HA 33421 FUEL IND CTR TANK WENT BLANK FUEL IND STATUS MSG DISPLAYED. PERFORMED BITE TEST FUEL QUANTITY PROCESSOR PER FIM 28-41-0 0, NO FAULTS DISPLAY. FUEL IND CTR TANK NORMAL AT THIS TIME AND NO STATUS MSG DISPLAY. 2 L 7 2 4F RT A1NM 2008010800060 20080108 00060 NM 2008 1 8 HALA0700554 1 20071225 A 3600 UNKNOWN BOEING 767 76733A 1385209 NM PNEUMATIC SYS UNKNOWN A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM, APU PNEUMATIC AIR INOP. BITE CHECK ECU PER AMM 49-11-00. NO FAULTS NOTED. APU STARTED ON FI RST ATTEMPT. OK FOR SERVICE. APU AIR OPS CK GOOD. 2 L 7 2 4F RT A1NM 2008010800061 20080108 00061 NM 2008 1 8 QXEA200702029 1 20071222 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 PDX - THERE IS A 2" CRACK IN THE FUSELAGE SKIN AT THE TOP OF THE AIRCRAFT STRUCTURE AT STRINGER 1 STATION X-32.400. MAI NTENANCE MAPPED DAMAGE FOR ENGINEERING. HFEC INSPECTED CRACKED AREA TO VERIFY ENDS OF CRACK. CUT OUT DAMAGED AREA OF 4 .5" BY 3.2" PER RD 8/4-53/2196. HFEC AROUND CUT-OUT, NO CRACKES NOTED. CUT EXTERNAL STRAP AND FABRICATED PACKER IAW Q4 00 RD 8/4-53-2196. INSTALLED AND SEALED DOUBLER IAW RD 8/4-53-2196 AND PAINTED PER SRM 51-25-05. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008010800062 20080108 00062 NM 2008 1 8 ASAA0772422 1 20071206 A 5320 146A940139 STRAP BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT BS 887 LBL 8 TO RBL 21 FLOOR SUPPORT TEE STRAP CORRODED. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008010800065 20080108 00065 EA 2008 1 8 TRAX200701970 1 20071220 A 5320 LINK CNDAIR CL600 CL6002B19 1900309 EA BS 513 TWISTED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 LT AFT FUSELAGE TO WING LINK AT FS 513.00 IS TWISTED. ZERO LOADED A/C AND REPOSITIONED LT AFT LINK IAW ASA AMM SUPPLEM ENT ASA 07-11-01 REV. B. PERFORMED HIGH FREQ. EDDY CURRENT INSPECTION OF LT AFT WING/FUSELAGE FITTING IAW ASA AMM SUPPL EMENT ASA 07-11-01 REV. B. AND NDTM 51-20-06. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2008010800068 20080108 00068 EA 2008 1 8 TRAX200701973 1 20071221 A 5514 PIN CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 HORIZONTAL STABILIZER LT OUTER PIN WORN. 2 L 7 2 4F RT A21EA 2008010800069 20080108 00069 EA 2008 1 8 TRAX200701975 1 20071222 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 INTERCOSTAL CRACKED IN CORNER OF END FLANGE FS 484 LBL10 (MARKED). 2 L 7 2 4F RT A21EA 2008010800070 20080108 00070 EA 2008 1 8 TRAX200701976 1 20071222 A 5340 FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 461 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 BATHTUB FITTING CRACKED AT FS 461 RBL10. REMOVED CRACKED BATHTUB FITTING IAW CRJ SRM 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21. LOCATED SERVICEABLE FITTING P/N 600-31068-19 IAW CRJ 200 SRM 51-40-11. INSTALLED SERVICEABLE FITTING IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21. 2 L 7 2 4F RT A21EA 2008010800071 20080108 00071 EA 2008 1 8 TRAX200701977 1 20071222 A 5522 GROUND STUD CNDAIR CL600 CL6002B19 1900309 EA LT ELEVATOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 LT ELEV HORIZ CENTER HINGE HAS GROUND STUD WITH SURFACE CORROSION. 2 L 7 2 4F RT A21EA 2008010800074 20080108 00074 NM 2008 1 8 ASAA0772425 1 20071206 A 5320 146A75026 CHANNEL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT BS 927+13 TO BS 947 RBL 21 ZEE CHANNEL CORRODED. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008010800076 20080108 00076 NM 2008 1 8 ASAA0772427 1 20071206 A 5320 146A94014 SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT FLOOR PANEL BUTT SPLICE TEE SUPPORT BS 767+6 CORRODED. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008010800078 20080108 00078 NM 2008 1 8 ASAA0772430 1 20071207 A 5320 147A566021 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CABIN INTERCOSTAL BS 947 TO BS 967 LBL 50 CORRODED. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008010800079 20080108 00079 NM 2008 1 8 ASAA0772431 1 20071207 A 5312 143A948530 SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 CORROSION FOUND FWD CARGO PIT AFT LEFT BULKHEAD SUPPORT RAIL. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008010800081 20080108 00081 NM 2008 1 8 ASAA0772433 1 20071208 A 5320 111A11413 WEB BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 LEFT AIR CONDITION BAY AFT WALL BS 663 WEB CRACKED. REPAIRED IAW B737 700 SRM 57-10-10 REPAIR 2 FIG 203. 2 L 7 2 4F RT A16WE 2008010800084 20080108 00084 NM 2008 1 8 ASAA0772440 1 20071205 A 5320 143A750180 CHANNEL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 FWD CARGO PIT LEFT ZEE CHANNEL AT BS 492 TO 500 2 LBL 22 CORRODED. REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 53-0 0-53 REPAIR 5. 2 L 7 2 4F RT A16WE 2008010800085 20080108 00085 NM 2008 1 8 ASAA0772434 1 20071209 A 5312 111A11414 BULKHEAD BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 CENTER WING BULKHEAD BS 663 RBL 14 WL 150 CRACKED. REPAIRED IAW B737 700 SRM 57-10-10 REPAIR 2 FIG 203. 2 L 7 2 4F RT A16WE 2008010800086 20080108 00086 NM 2008 1 8 ASAA0772435 1 20071211 A 5755 113A46001 SKIN BOEING 737 737790 13844CN NM NR 6 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 LEFT WING NR 6 SPOILER HAS DENT AT UPPER SURFACE WS 228.0. REPAIRED DENT ON LEFT WING NR 6 SPOILER AT WS 228.0 IAW B737 700 SRM 51-70-10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008010800087 20080108 00087 EA 2008 1 8 TRAX200701979 1 20071222 A 5514 BONDING JUMPER CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 FOUND HARDWARE AND BONDING JUMPER ON HORIZONTAL STAB RT CENTER HINGE FITTING CORRODED. 2 L 7 2 4F RT A21EA 2008010800091 20080108 00091 NE 2008 1 8 QXEA200702031 2 20071225 A 7240 DRAIN MAST DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 1 ENGINE FROZEN A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 355PH 500 RDM - FLIGHT 2191 - ON SHUTDOWN AT THE GATE, RAMP NOTICED SMOKE FROM THE TOP OF NR 1 ENGINE. MAINTENANCE CHECKED NACELL E AND ENGINE AREA AND FOUND NO SOURCE FOR THE SMOKE. FOUND SOME ICE IN THE COWL DRAIN MAST AND THAWED OUT. PERFORMED E NGINE RUNS AT TEMPERATURE AND SHUT DOWN WITH NO SMOKE NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 2008010800093 20080108 00093 2008 1 8 QXEA200702032 4 20071226 A 2210 TRIM SYSTEM DHAV DHC8 DHC8202 2809007 NM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 367PH 511 PDX - FLIGHT 2188 - RECEIVED A MISTRIM NOSE UP AND TRIM NOSE DOWN MESSAGE WHEN LEVELING OFF FROM CLIMB AND DESCENT. RAN CHECKLIST AND DE SELECTED AUTOPILOT. TRIM FORCE WAS OPPOSITE OF MESSAGE, AND MESSAGE WENT AWAY. MAINTENANCE PLACED TH E SYSTEM ON MEL 22-1. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008010800098 20080108 00098 NM 2008 1 8 QXEA200702030 1 20071226 A 3610 8209074 SWITCH BOMBDR DHC8 DHC8402 1390042 NM BLEED OVERTEMP MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 413QX 4060 SEA - FLIGHT 2239 - NR 1 BLEED HOT CAUTION LIGHT CAME ON DURING TAXI. COMPLIED WITH CHECKLIST AND TAXIED BACK TO THE GA TE. MAINTENANCE REPLACED THE BLEED OVERTEMP SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008010800099 20080108 00099 NM 2008 1 8 BB07104 1 20071227 A 3397 TERMINAL BOEING 757 7572G7 1384963 NM CABIN LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 910AW 24523 MAINTENANCE FOUND ROW 12L EMERGENCY LIGHT INOPERATIVE IN OVERHEAD BIN COVE. TIGHTENED LOOSE TERMINAL. NO FURTHER FAULT S. 2 L 7 2 4F RT A2NM 2008010800100 20080108 00100 NM 2008 1 8 QXEA200701799 1 20071125 A 5410 DIAPHRAGM BOMBDR DHC8 DHC8402 1390042 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - RIGHT NACELLE OUTBOARD DIAPHRAM CRACKED. FABRICATED NEW SUPPORT ANGLES AND INSTALLED NEW SUPPORT ANGLE . PRIMED AND PAINTED AREA. 2 H 7 2 4T RT A13NM 2008010800101 20080108 00101 WP 2008 1 8 ABXA070428 1 20071204 A 5330 591140675 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 972AX 47631 FUSELAGE SKIN CRACKED AT AFT UPPER DOOR STOP AT PASSENGER ENTRANCE. CRACK WAS LESS THAN .5 INCH LONG. REPAIRED AREA IA W EA 53100126-001 AND DC9 SRM 53-05, FIGURE 114. 2 L 7 2 4F A6WE 2008010800102 20080108 00102 NM 2008 1 8 QXEA200701800 1 20071125 A 7120 COLLAR BOMBDR DHC8 DHC8402 1390042 NM ENGINE MOUNT CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - FORWARD ENGINE MOUNT COLLAR HAS CHAFE DAMAGE ALONG THE INBOARD AND OUTBOARD COWL DOOR CONTACT SURFACE. BLENDED AREA. HFEC C/W NO CRACKS. 2 H 7 2 4T RT A13NM 2008010800103 20080108 00103 WP 2008 1 8 ABXA070429 1 20071204 A 5311 991185859 FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 972AX 47631 FRAME CRACKED AT FASTENER FS 1150 CANTED AT LONGERON 4 LEFT. REMOVED FRAME, REPAIRED AND REINSTALLED IAW DC9 SRM 53-03, FIGURE 30, 51-30-02, AND 51-30-05. 2 L 7 2 4F A6WE 2008010800104 20080108 00104 NM 2008 1 8 QXEA200701803 1 20071125 A 5315 FLOORBEAM BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - FLOORBEAM AT X32 IS CORRODED ON TOP SURFACE BETWEEN FLOORBOARD AND SUPPORT. REMOVED SURFACE CORROSION FROM AREA. MATERIAL REMOVED .002, WITHIN LIMITS. ALODINE PRIMED AND PAINTED. 2 H 7 2 4T RT A13NM 2008010800106 20080108 00106 NM 2008 1 8 QXEA200701804 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK, SEAT TRACK 7 IS CORRODED ON TOP 19" FROM END. REMOVED CORROSION AND BLENDED AREA. HFEC AREA AND NO CRA CKS FOUND. ALODINE AREA. 2 H 7 2 4T RT A13NM 2008010800107 20080108 00107 NE 2008 1 8 ABXA070427 2 20071224 A 7397 CONNECTOR BOEING 767 767200 1385120 NM GE CF6 CF680A 30025 NE LT ENGINE LOOSE A ABXA O OTHER Y ENGINE STOPPAGE CR CRUISE 1 GL 23 799AX 23432 58022 LOST THE LEFT ENGINE AT CRUISE. DID ENGINE SECURE CHECKLIST, NO OTHER ABNORMALITIES. CREW ACCOMPLISHED ENGINE INFLIGHT START. THE ENGINE STARTED FINE, LANDED AT MSP. INSPECTED ENGINE INLET AND EXHAUST, NO DEFECTS. SUMPED MAIN FUEL FILT ER, NO DEBRIS NOTED. CHECKED ENGINE CONDITION CONTROL ACTUATOR ELECTRICAL CONNECTOR, FOUND IT LOOSE AND OILY. CLEANED AND RESEATED CONNECTOR. CHECKED CDP TUBE, FOUND LOOSE BULKHEAD CONNECTOR, TIGHTENED CONNECTOR. CHECKED VSV CABLES, OKA Y. ENGINE RAN GOOD. ALL WORK ACCOMPLISHED IAW B767 MM. 2 L 7 2 4F 4 F RT A1NM E13NE 2008010800109 20080108 00109 NM 2008 1 8 SWAA076453 1 20071223 A 5610 141A4B108 WINDOW BOEING 737 7377H4 1384404 NM COCKPIT ARCED A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 463WN 32467 R2 COCKPIT WINDOW ARCING. REMOVED AND REPLACED R2 COCKPIT WINDOW PER MM. 2 L 7 2 4F RT A16WE 2008010800111 20080108 00111 2008 1 8 SWAA076454 4 20071225 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 492WN 33866 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008010800113 20080108 00113 NM 2008 1 8 QXEA200701797 1 20071125 A 5311 GUSSET BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE FRAME GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 INSPECTION, AFT CARGO COMPARTMENT RIGHT FRAME X 819.102 GUSSET IS GOUGED AT Z113. BLENDED DAMAGED AREA AND FOU ND TO BE WITHIN LIMITS IAW DHC-8-400 SRM 51-14-00. MATERIAL REMOVED .077. HFEC AREA NO CRACKS. ETCHED AND ALODINE ARE A AND PAINTED. 2 H 7 2 4T RT A13NM 2008010800114 20080108 00114 NM 2008 1 8 SWAA076461 1 20071224 A 5311 6546595 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800115 20080108 00115 NM 2008 1 8 QXEA200701805 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK, SEAT TRACK 7 IS CORRODED ON TOP AT X373. REMOVED CORROSION AND BLENDED AREA, WITHIN LIMITS. HFEC AREA, NO CRACKS. APPLIED ALODINE. 2 H 7 2 4T RT A13NM 2008010800117 20080108 00117 NM 2008 1 8 SWAA076457 1 20071224 A 5311 65C33509 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800118 20080108 00118 NM 2008 1 8 SWAA076458 1 20071224 A 5311 65C33509 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800119 20080108 00119 NM 2008 1 8 DHL2007782003 1 20071223 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1103-1118 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 782DH 21998 A/C SKIN DAMAGE LT SIDE STATION BS 1110 APP STR 24-23L "C" CONTAINER. STOP DRILLED ENDS OF CRACK IN A/C SKIN PER SRM 51 -40, DAMAGE REMAINS IN AIRCRAFT. REFERENCE LOG NR 146871, N/R 138164, AND N/R 138165: CUT OUT DAMAGED AREA, 7" BY 6.62 5". FABRICATED DOUBLER, 2024T3 .080" BY 15.125" BY 13.125" AND FILLER, 2024T3 .071" BY 6" BY 1", AND INSTALLED PER B727 SRM 53-30-3 FIG 3 AND 53-30-2 FIG 2. CUT OUT DAMAGED FRAME SHEAR TIE, 5" BY 1.25" AND FABRICATED SHEAR TIE FROM 7075-T 6 6.375 BY 3.5" BY 1" AND FILLER FROM 7075T6 5.5" BY 3.375", AND INSTALLED PER B727 SRM 53-10-4 FIG 13. 2 L 7 3 4F A3WE 2008010800124 20080108 00124 EU 2008 1 8 DHLA200700095 1 20071227 A 3350 POWER SUPPLY AIRBUS 300 A300B4203 3930306 EU EMERGENCY LIGHTS NO TEST A DHLA K NONE L NO TEST IN INSP/MAINT 1 GL 05 367DH 265 EMERGENCY EXIT LIGHT OVER THE R1 WILL NOT TEST. REPLACED R1 EMERGENCY LIGHT POWER SUPPLY AS PER MM 33-51-14. OPS NORM. 2 L 7 2 4F RT A35EU 2008010800125 20080108 00125 NM 2008 1 8 SWAA076464 1 20071224 A 5311 6546555 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800128 20080108 00128 EU 2008 1 8 YENA2007123 1 20071222 A 5610 NP1653116 WINDSHIELD AIRBUS 320 A320232 3930326 EU COCKPIT CRACKED A YENA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 15 504JB 32045 1156 FLT NR 759, BOS-SJU, DIVERTED RDU, FIRST OFFICER FORWARD WINDSHIELD CRACK. REMOVED AND REPLACED FIRST OFFICER WINDSHIELD IAW AMM 56-11-11-04. 2 L 7 2 4F RT A28NM 2008010800130 20080108 00130 EA 2008 1 8 SWIA200718980 1 20071016 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 935SW 7725 FLT 6608 - FO WINDSHIELD IS CRACKED. REPLACED FO'S WINDSHIELD IAW CRJ MM 56-11-01, P/N OFF: 601R33033-14, S/N OFF: 022 40H4671. 2 L 7 2 4F RT A21EA 2008010800132 20080108 00132 EA 2008 1 8 SWIA200718982 1 20071218 A 2120 DUCT CNDAIR CL600 CL6002B19 1900309 EA CABIN AIR CONTAMINATED A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 946SW 7776 FLT 5870 - "SMOKE TOILET" MESSAGE ILLUMINATED AFTER TAKEOFF. INSPECTED AIR CONDITIONING AND LAV SMOKE DETECTION SYSTEM AND REMOVED RESIDUAL CONTAMINATION IN DUCTING. NO FURTHER DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2008010800136 20080108 00136 SO 2008 1 8 SWIA200718984 1 20071220 A 5610 WINDSHIELD EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 560SW 120334 FLT 3785 - CAPTAINS WINDSHIELD IS CRACKED. REPLACED CAPTAIN'S WINDSHIELD IAW MM 56-10-01, P/N: NP-151311-1, S/N OFF: 06 138H8653. 2 L 7 2 4T RT A31SO 2008010800137 20080108 00137 SO 2008 1 8 SWIA200718985 1 20071220 A 5610 WINDOW EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 560SW 120334 FLT 3735 - CAPTAINS DV SIDE WINDOW IS CRACKED. REPLACED CAPTAINS DV WINDOW IAW EMB MM 56-11-01. LEAK CHECK GOOD. 2 L 7 2 4T RT A31SO 2008010800138 20080108 00138 2008 1 8 SWIA200718986 2 20071224 A 7497 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA BURNED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 606SK 10250 FLT 4042 - "L IGN A FAULT" MESSAGE APPEARED. REPLACED PINS ON PLUG J551 IAW CRJ 700 WDM 20-16-00. 2 L 7 2 4F RT A21EA 2008010800139 20080108 00139 EA 2008 1 8 SWIA200718987 1 20071216 A 5711 SPAR CNDAIR CL600 CL6002B19 1900309 EA RWS 339 DAMAGED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 918SW 7645 FORWARD OUTBOARD WING SPAR ON RIGHT WING HAS DAMAGE AT WS 339. REPAIRED WING SPAR DAMAGE AT WS 335-353 IAW CRJ 200 REO 601R-57-21-898. 2 L 7 2 4F RT A21EA 2008010800142 20080108 00142 EA 2008 1 8 SWIA200718990 1 20071221 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 866AS 7517 FLT 3904 - GEAR DISAGREE WARNING ON APPROACH AND NOSE GEAR WAS NOT DOWN. REPLACED NOSE GEAR SELECTOR VALVE IAW AMM 32- 33-10. REPLACED PRIORITY VALVE IAW AMM 32-33-15. 2 L 7 2 4F RT A21EA 2008010800143 20080108 00143 EA 2008 1 8 SWIA200718991 1 20071220 A 3397 CIRCUIT CARD CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 603SK 10248 FLT 4038 - EMERGENCY LIGHTS ARE ON IN THE CABIN WITH SWITCH IN ARMED POSITION. REPLACED CIRCUIT CARD NR 5 IN JB11 IAW M M 24-06-11, P/N E520005-705A. 2 L 7 2 4F RT A21EA 2008010800144 20080108 00144 EA 2008 1 8 SWIA200718992 1 20071218 A 2120 DUCT CNDAIR CL600 CL6002B19 1900309 EA CABIN AIR CONTAMINATED A SWIA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 07 983SW 7961 FLT 5910 - SMOKE TOILET INDICATION ON CLIMB-OUT WITH HAZE IN THE CABIN. INSPECTED LAV SMOKE DETECTION SYSTEM, AFT EQUIP MENT BAY AND LEFT AND RIGHT PACKS. CLEARED RESIDUAL CONTAMINATION FROM THE SYSTEM. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008010800145 20080108 00145 EA 2008 1 8 SWIA200718993 1 20071219 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA RIGHT SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 983SW 7961 FLT 5808 - RIGHT PACK IS CAUSING SMOKE IN THE CABIN. REPLACED OIL COALESCER BAG IAW CRJ 200 MM 21-51-13. RAN RIGHT PAC K WITH NO DISCREPENCIES NOTED. 2 L 7 2 4F RT A21EA 2008010800146 20080108 00146 SO 2008 1 8 SWIA200718994 1 20071220 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 218SW 120287 EMERGENCY EXIT SIGN AT ROW 9 IS INOP. REPAIRED EXIT SIGN WIRING. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008010800151 20080108 00151 NM 2008 1 8 SWAA076467 1 20071224 A 5711 7075T73 SUPPORT FITTING BOEING 737 7375H4 138449D NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRIDGE CHECK, FOUND LT WING AFT SPAR SUPPORT FITTING NR 1 MAIN FLAP TRACK CORRODED AT OUTBOARD FLAP TRA CK MOUNT HOLE. REMOVED AND REPLACED AFT SPAR SUPPORT FITTING PER MM. 2 L 7 2 4F RT A16WE 2008010800152 20080108 00152 SO 2008 1 8 SWIA200718999 1 20071226 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 250YV 120250 FLT 5787 - EMERGENCY EXIT LIGHT AT SEAT 6C IS CRACKED. REPLACED SIGN ASSEMBLY PER MM 33-61-02. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008010800155 20080108 00155 NM 2008 1 8 UPS07451337 1 20071222 A 5730 PANEL BOEING 747 747123F NIR NM RT WING DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 RT WING UPPER INBD FIXED TRAILING EDGE PANEL DELAMINATED. REMOVED DISBONDED, DAMAGED SKIN FROM LEADING EDGE ACROSS PAN EL TO LWR EDGE IAW 51-40-20. FABRICATED SKIN FILLER. REPLACED PANEL WITH SERVICEABLE PANEL. 2 L 7 4 4F RT A20WE 2008010800156 20080108 00156 NM 2008 1 8 SWAA076469 1 20071224 A 5330 6545769 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 394, RBL 2 AT RADIO ALTIMETER CUTOUT. REPAIRED SKIN PE R SWA EA. 2 L 7 2 4F RT A16WE 2008010800157 20080108 00157 WP 2008 1 8 UPS07851332 1 20071226 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 EMERGENCY EXIT LIGHTS DIM. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK IAW MM 33-50-01-2, SN OFF 356 SN ON UP12384 . 2 L 7 4 4F RT 4A25 2008010800158 20080108 00158 NM 2008 1 8 SWAA076470 1 20071224 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SR M. 2 L 7 2 4F RT A16WE 2008010800160 20080108 00160 NM 2008 1 8 SWAA076476 1 20071221 A 5311 6546548 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800161 20080108 00161 NM 2008 1 8 SWAA076477 1 20071221 A 5311 6545805 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008010700110 20080107 00110 NM 2008 1 7 USAA920071353 1 20071218 A 3350 20121 BATTERY PACK BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 311AW 24712 PHX - FLT 091 - EEL - EMERGENCY LIGHT AT ROW 4 RT UPPER BULLNOSE INOP. MX REPLACED THE BATTERY CHARGER AND BATTERY. O PERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2008010700191 20080107 00191 EU 2008 1 7 2007UALA05098 1 20071213 A 2560 GIRT BAR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EVAC SLIDE DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 483UA 1586 DOORS 2L & 2R FAILED ARMING SLIDE FORCE TESTS. DIRTY/UNLUBED GIRT FITTING INTERFERENCE. CLEANED AND LUBED GIRT BAR FIT TING AND BAR. OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010700234 20080107 00234 2008 1 7 2007UALA05246 4 20071221 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR LOW PRESSURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 564UA 26666 DOOR 4L SLIDE PRESSURE IS ON LOW END OF GREEN BAND. REPLACED SLIDE ASSY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700263 20080107 00263 NM 2008 1 7 2007UALA05257 1 20071222 A 3350 276005 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP, 3RD & 4TH FROM FWD. REPLACED FUSE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700268 20080107 00268 NM 2008 1 7 2007UALA05262 1 20071222 A 3520 9F40427507 OXYGEN BOTTLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOW PRESSURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 118UA 28811 PAX O2 LOW PRESS DOOR 4R. SUSPECT FAULTY RELEASE VALVE SEAL. REPLACED OXYGEN BOTTLE. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700297 20080107 00297 NM 2008 1 7 2007UALA05278 1 20071224 A 2560 GIRT BAR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L2 DOOR SEPARATED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 306UA 23667 THE 2L GIRT BAR PARTIALLY SEPARATED FROM ASSEMBLY. SUSPECT IMPROPER INSTALLATION. SECURED GIRT BAR. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010700306 20080107 00306 NM 2008 1 7 2007UALA05288 1 20071225 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EMERGENCY CEILING LIGHT ABOVE ROW 12 INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700311 20080107 00311 NM 2008 1 7 2007UALA05294 1 20071225 A 3510 MC1019101 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 557UA 26653 OBSERVER`S O2 MASK WILL NOT SHUT OFF. FOUND 1ST OBS O2 MASK LEAKING AT HARNESS. REPLACED FIRST OBS O2 MASK, OPS CHECKE D NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700321 20080107 00321 NM 2008 1 7 SWAA076432 1 20071221 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 400 STR 14L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010700326 20080107 00326 NM 2008 1 7 SWAA076438 1 20071222 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 17L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008010700328 20080107 00328 NM 2008 1 7 SWAA076437 1 20071222 A 5330 6545890 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 317, STR 18R. REPAIRED SKIN PER SWA EA AND SRM. 2 L 7 2 4F RT A16WE 2008010700336 20080107 00336 NM 2008 1 7 SWAA076449 1 20071222 A 5512 65C25727 SKIN BOEING 737 7377H4 1384404 NM RT HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 400WN 27891 DURING SCHEDULED HC1 CHECK, FOUND RT LOWER HORIZONTAL STABILIZER SKIN CRACKED AT STAB STA 129.50, 17.5 " AFT OF LEADING EDGE SKIN. REPAIRED PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800003 20080108 00003 NM 2008 1 8 ASAA0772406 1 20071205 A 5330 143A32335 DOUBLER BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 FWD CARGO PIT RADIO ANTENNA INTERNAL DBLR BS 500A TO 500B BL 0 CORRODED AT DOME NUTS. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008010800009 20080108 00009 NM 2008 1 8 ASAA0772412 1 20071205 A 5347 146A750125 CARGO TRACK BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT RIGHT TIE DOWN TRACK BS 727A+4 TO 927A+11 RBL 14 CORRODED. AFT CARGO RIGHT TIE DOWN TRACK BS 727A+4 TO BS 727A TILL RBL 13 84 CORRODED AROUND ANCHOR NUTS. BLENDED OUT AND FOUND BEYOND LIMITS IAW B737 700 SRM 53 00 53. REF T ASK CARD 5113801 FOR THE REPLACEMENT OF THE TIE DOWN TRACK. 2 L 7 2 4F RT A16WE 2008010800014 20080108 00014 NM 2008 1 8 ASAA0772417 1 20071205 A 5347 146A750125 CARGO TRACK BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT RIGHT TIE DOWN TRACK BS 767+5 RBL 13.84 CORRODED. TIE DOWN TRACK REPLACED ON TC 5113801. 2 L 7 2 4F RT A16WE 2008010800018 20080108 00018 NM 2008 1 8 2007UALA00693 1 20070307 A 2611 SMOKE DETECTOR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FWD CARGO BAY FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 913UA 25291 FWD CARGO LOOP "B" & AFT CARGO LOOP "A" FAULT LIGHTS ON. POTENTIAL FAULTY SMOKE DETECTORS. REPLACED 1B AND 3A SMOKE DE TECTORS. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010800043 20080108 00043 NM 2008 1 8 CALA0700788 1 20071226 A 5230 6547952524B SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 C-2 DOOR INNER SKIN CENTER AFT LIGHTENING HOLE CRACKED. REPAIRED PER ECRA 5232-01097. 2 L 7 2 4F RT A16WE 2008010800056 20080108 00056 NM 2008 1 8 HALA0700551 1 20071226 A 3350 LIGHT BOEING 767 76733A 1385209 NM CABIN MALFUNCTIONED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 583HA 25531 EMERGENCY FLOOR LTS ILLUMINATED DURING FLT, WITH NO LOSS OF ELEC POWER. CHECKED OPERATION OF EMERGENCY LIGHT PER FIM 33 -51-00. EMERGENCY LIGHTS CHECKED NORMAL. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2008010800075 20080108 00075 NM 2008 1 8 ASAA0772426 1 20071206 A 5320 146A812210 SILL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 FWD CARGO PIT LWR SILL WEB FOUND CORRODED BS 440 TO BS 492 RBL 26. INSTALLED MADE REPAIR LWR SILL WEB AT FWD CARGO PIT AT BS 440 TO BS 492 RBL 26 IAW B737 700 SRM 51-40-02 AND BOEING DRWG 143A 8330 ID 0015. 2 L 7 2 4F RT A16WE 2008010800094 20080108 00094 SO 2008 1 8 RAIA00712027 1 20071224 A 5210 ROLLER EMB 145 EMB145 3260210 SO PAX DOOR LACK OF LUBE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 850HK 145003 POST FLT NR 8018 - IAD - PAX DOOR HARD TO CLOSE /OPEN. MAINTENANCE LUBE AND SLIGHT ADJUSTMENT ON FORWARD UPPER ROLLER S UPPORT, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2008010800097 20080108 00097 SO 2008 1 8 RAIA00712028 1 20071224 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 810HK 145231 POST FLT NR 8019 - STL - FLOOR PROXIMITY LIGHT LOOSE. MAINTENANCE INSPECTED AND FOUND SAID STRIP CAME LOOSE, RESECURED LIGHT STRIP, CHECKS GOOD. 2 L 7 2 4F RT T00011AT 2008010800110 20080108 00110 NM 2008 1 8 QXEA200701802 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK, SEAT TRACK NR 5 HAS CORROSION AROUND RIVET HOLE, 39" AFT OF FRONT END. REMOVED RIVET AND BLENDED CORROS ION. ALODINE AND PRIMED AND PAINTED. REAPPLIED RIVET. 2 H 7 2 4T RT A13NM 2008010800123 20080108 00123 NM 2008 1 8 DHLA200700093 1 20071227 A 2613 OVERHEAT LOOP BOEING 727 7272M7 138407S NM PWA JT8 JT8D15A 52051 NE NR 1 NACELLE MISROUTED A DHLA E ENGINE SHUTDOWN W N INADEQUATE Q C FALSE WARNING CR CRUISE 1 GL 05 750DH 21951 700372 NR 1 STRUT OVERHEAT LIGHT AFTER T/O PERFORMED NORMAL SHUTDOWN NR 1 ENGINE PER PROCEDURE. FOUND 4 DUCT CONNECTIONS LEAKI NG ON DUCT FROM PRECOOLER TO THE ENG. REMOVED AND REINSTALLED DUCTS PER 727 M/M 36-00-01 (DUCTS WERE MIS-ALIGNED) ALSO FOUND NR 1 PYLON OVERHEAT LOOP MIS-ROUTED-REROUTED PER 727 M/M 26-14-01. SYS GRND CKS GOOD AFTER 10 MIN AT TAKEOFF PWR PER M/M 36-00-00 AND M/M 26-14-00. OK FOR CONTINUED SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2008010800129 20080108 00129 EA 2008 1 8 SWIA200718979 1 20071225 A 2913 6619005 PUMP CNDAIR CL600 CL6002C10 1390015 EA HYD SYSTEM LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 NM 07 726SK 16 16 10190 FLT 6547 - "HYD EDP 2A" CAUTION MESSAGE, WITH QUANTITY READING 0 PERCENT. REPLACED HYDRAULIC EDP WITH SERVICEABLE UNIT IAW RJ 700 MM 29-11-01. 2 L 7 2 4F RT A21EA 2008010800131 20080108 00131 2008 1 8 SWIA200718981 4 20071219 A 2397 WIRE EMB 120 EMB120ER 3260203 SO ELECTRICAL SHORTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 290SW 120317 FLT 5772 - CVR CIRCUIT BREAKER DOES NOT STAY SET. REPAIRED WIRES W201-2514-22 AND W201-2239-22. OPS CHECKS GOOD IAW 23 -71-00 AND IAW 31-30-00. 2 L 7 2 4T RT A31SO 2008010800133 20080108 00133 NM 2008 1 8 SWAA076465 1 20071224 A 5311 65C27021 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800134 20080108 00134 SO 2008 1 8 SWIA200718983 1 20071218 A 3320 LIGHT EMB 120 EMB120ER 3260203 SO CABIN BURNED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 578SW 120346 CAPTAIN REPORTS BURNING ODOR AND SMOKE IN CABIN. REPLACED CABIN LIGHT FIXTURE WITH A SERVICEABLE UNIT. OPS CHECKS GOOD . 2 L 7 2 4T RT A31SO 2008010800140 20080108 00140 EA 2008 1 8 SWIA200718988 1 20071216 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA RWS 389 DAMAGED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 918SW 7645 RIGHT WING RIB AT WS389 IS DAMAGED. REPLACED RIGHT WING RIB AT WS 389 IAW REO 601R-57-21-899. 2 L 7 2 4F RT A21EA 2008010800149 20080108 00149 EA 2008 1 8 SWIA200718997 1 20071222 A 2913 887055 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 918SW 7812 7812 7645 FLT 6670 - SYSTEM 2 HYDRAULIC QUANTITY DROPPED TO 0 PERCENT IN FLIGHT. REPLACED NR 2 ENGINE DRIVEN HYDRAULIC PUMP IAW A MM 29-11-01. OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2008010800150 20080108 00150 SO 2008 1 8 SWIA200718998 1 20071222 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 295SW 120322 FLT 5727 - FORWARD LEFT BULKHEAD "EXIT" SIGN IS BROKEN. REPLACED "EXIT" SIGN ASSEMBLY PER MM 33-51-02. 2 L 7 2 4T RT A31SO 2008010800162 20080108 00162 NM 2008 1 8 SWAA076475 1 20071221 A 5311 6546550 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800163 20080108 00163 NM 2008 1 8 SWAA076473 1 20071221 A 5311 6546596 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800164 20080108 00164 WP 2008 1 8 UPS07851335 1 20071221 A 7931 OIL SYSTEM DOUG DC8 DC873F 302199F WP NR 4 ENGINE LOW PRESSURE A IPXA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 SO 01 840UP 46140 NR 4 ENGINE LOST PRESSURE, SHUT DOWN WITH 20 PSI N1 16 PERCENT, N2 9.4 PERCENT 5 QUARTS INDICATED 6000 FT/200 KTS. REMO VED AND REPLACED LINE SUPPLY OIL TO OIL PRESSURE TRANSMITTER IAW M/M 20-12-00-2. LEAK AND OPS CHECK GOOD IAW M/M 71-00- 00. 2 L 7 4 4F RT 4A25 2008010800167 20080108 00167 NM 2008 1 8 SWAA076471 1 20071221 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 479, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008010800168 20080108 00168 NM 2008 1 8 UPS07B51334 1 20071226 A 5220 LOCK BOEING 747 74744AF 13848B2 NM EMERGENCY EXIT STRIPPED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 571UP 35668 AT ROTATION DOOR F/O OVHD ADVISORY MSG ILLUMINATED MOMENTARILY. CHECKED RIG OF OVERHEAD LATCH PER MM 52-71-01-4, OK FOU ND HATCH HANDLE NOT ALIGNED WITH LOCK STRIPED. 2 L 7 4 4F RT A20WE 2008010800169 20080108 00169 NM 2008 1 8 SWAA076474 1 20071221 A 5311 6546548 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800170 20080108 00170 2008 1 8 SWAA076479 4 20071223 A 2565 61621469 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF POSITION A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 635SW 27708 L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008010800172 20080108 00172 EU 2008 1 8 NWAA074233235 1 20071205 A 5330 SKIN AIRBUS 320 A320212 3930322 EU FUSELAGE GOUGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 335NW 340 DURING GROUND OPERATIONS FUSELAGE SKIN WAS DENTED AND GOUGED BETWEEN STRINGER 34 TO 38 FRAMES 19 TO 24. REPAIRED PER EA 32-211270. 2 L 7 2 4F RT A28NM 2008010800173 20080108 00173 NM 2008 1 8 SWAA076482 1 20071225 A 5330 6545774 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008010800174 20080108 00174 WP 2008 1 8 NWAA074299947 1 20071221 A 5210 SKIN DOUG DC9 DC931 3022065 WP PAX DOOR DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8938E 47161 DURING GROUND OPERATIONS PASSENGER ENTRY DOOR L1 JAMB INNER SKIN AND INTERCOSTAL AT FORWARD STOP NR 5 DAMAGED. REPAIRE D PER EA 99-211510. 2 L 7 2 4F A6WE 2008010800175 20080108 00175 NM 2008 1 8 SWAA076481 1 20071225 A 5330 6545765 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 16L. REPAIRED SKIN PER SWA EA & SRM. 2 L 7 2 4F RT A16WE 2008010800176 20080108 00176 NM 2008 1 8 SWAA076483 1 20071224 A 5330 6518420 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800177 20080108 00177 NM 2008 1 8 NWAA074266731 1 20071221 A 5712 RIB BOEING 747 747251B 1384892 NM LT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 631NW 23111 DURING TURBULENCE INSPECTION FOUND LEFT WING LEADING EDGE RIB WEB CRACKED AT ILES 964.55 BETWEEN ENGINE NR 1 AND ENGINE NR 2. REPAIRED PER EA 67-21145. 2 L 7 4 4F RT A20WE 2008010800179 20080108 00179 NM 2008 1 8 NWAA074276730 1 20071223 A 5347 CARGO TRACK BOEING 747 747219B 1384852 NM BS 700 SEVERED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 630US 21668 DURING LINE CHECK, FOUND CARGO TRACK SEVERED AT BS 700 LBL 25. REPAIRED PER EA 67-210479. 2 L 7 4 4F RT A20WE 2008010800180 20080108 00180 NM 2008 1 8 SWAA076485 1 20071223 A 5314 656212518 KEELBEAM BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 696SW 23064 DURING SCHEDULED C2 CHECK, FOUND RT FUSELAGE KEEL BEAM CORRODED FROM BS 500C TO BS 540. REMOVED AND REPLACED KEEL BEAM SECTION PER SRM. 2 L 7 2 4F RT A16WE 2008010800181 20080108 00181 NM 2008 1 8 NWAA074285527 1 20071218 A 5512 PANEL BOEING 757 757251 1384970 NM HORIZONTAL STAB DEBONDED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 527US 23842 DURING "L" CHECK FOUND RT HORIZONTAL STABILIZER UPPER INBOARD PANEL DISBONDED BETWEEN FSS 83-204. REPAIRED PER EA 55-21 0445 SECTION I. REPEAT INSPECTIONS REQUIRED PER SECTION II AT INTERVALS NOT MORE THAN 6 MONTHS FOR PERIOD UP TO 24 MONT HS. SECTION III PERMANENT REPAIR REQUIRES REPLACEMENT OF PANEL. 2 L 7 2 4F RT A2NM 2008010800183 20080108 00183 WP 2008 1 8 NWAA074309856 1 20071226 A 5320 SUPPORT ANGLE DOUG DC9 DC951 3022051 WP BS 851 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 765NC 47718 DURING "L" CHECK, FOUND CRACK IN THE FORWARD FLANGE OF BULKHEAD SUPPORT ANGLE AT BS 851. REPAIRED PER EA 98-211053. 2 L 7 2 4F RT A6WE 2008010800184 20080108 00184 EU 2008 1 8 NWAA074243235 1 20071205 A 5330 SKIN AIRBUS 320 A320212 3930322 EU FUSELAGE GOUGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 335NW 340 DURING GROUND OPERATIONS FUSELAGE SKIN WAS GOUGED ON FORWARD SIDE OF CARGO DOOR OPENING AT STA C24-C24A BETWEEN STRINGER S 36R-37R. REPAIRED PER EA 32-211163. 2 L 7 2 4F RT A28NM 2008010800189 20080108 00189 EU 2008 1 8 07FDEA05116 1 20071220 A 5610 NP1752014 WINDSHIELD AIRBUS 300 A300F4605R 3930327 EU COCKPIT CRACKED A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 663FE 766 F/O`S R1 WINDOW SHATTERED AT CRUISE FL 300, QRH COMPLIED WITH. ACCOMPLISHED COMPLETION OF F/O'S WINDOW INSTALLATION IAW MM 56-11-11-4. REMOVED AND REPLACED WINDSHIELD TEMP REGULATOR IAW MM 30-42-11-4 AND WINDOW HEAT PROTECTION CONTROLLER IAW MM 30-42-51-4. PERFORMED WINDSHIELD ANTI-ICING AND DEFOGGING OPERATIONAL TEST IAW MM 30-42-00, OPS CHECKS GOOD. 2 L 7 2 4F RT A35EU 2008010800191 20080108 00191 NM 2008 1 8 07FDEA05142 1 20071227 A 5753 65246854 SKIN BOEING 727 727233 138408A NM RT WING TE FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 RIGHT WING INBOARD MID FLAP UPPER SURFACE CHAFED AT INBOARD SIDE BLENDED DAMAGE AREA, NDT VERIFIED NO DEFECTS, TREATED, PRIMED, AND TEFLON PAINTED REF SRM 57-50-1, SRM 51-10-2, MM 51-20-017-7, AND EA 7-5750-113963. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008010800193 20080108 00193 WP 2008 1 8 07FDEA05144 1 20071227 A 5420 777119105 BOLT DOUG MD10 MD1010F 3022112 WP NR 3 PYLON SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 NR 3 PYLON, TOMBSTONE LOWER SPHERICAL BEARING ATTACH BOLT SHEARED AT 6 O'CLOCK POSITION, DOT NR 1. REMOVED AND REPLACED 6 BOLTS, P/N 77711-9-105, PLATE -P/N AUB7125-1, RETAINER P/N AUB7126-501 AND PLI WASHERS REF AMM 54-00-01-4. 2 L 7 3 4F RT A22WE 2008010800194 20080108 00194 NM 2008 1 8 SWAA076490 1 20071223 A 3350 D1701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 746SW 29798 DURING SCHEDULED HC1 CHECK, AFT RIGHT CABIN EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BA TTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008010800195 20080108 00195 EU 2008 1 8 07FDEA05145 1 20071227 A 5313 A53679041201 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 ULTRASONIC INSPECTION INDICATED A CRACK IN THE LOWER FILLET RADIUS OF THE LATERAL PANEL STRINGER 36 JUST FORWARD OF FR AME 54 BETWEEN THE 4TH AND 5TH FASTENER HOLES, CRACK LENGTH ESTIMATED AT 1 INCH. REPAIRED AREA AT FRAME 54 STRINGER 36R IAW EA NR 6-5330-112997 "FUSELAGE -AD 98-26-01 SKIN PANEL AT FRAME 54 AND STRINGER 36R REPAIR". 2 L 7 2 4F RT A35EU 2008010800197 20080108 00197 NM 2008 1 8 SWAA076491 1 20071224 A 2560 65C16820 HOOK BOEING 737 7377H4 1384404 NM GIRT BAR LOOSE A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 778SW 27883 R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2008010800199 20080108 00199 NM 2008 1 8 SWAA076492 1 20071223 A 3350 BR2013 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 793SA 27888 EEPLS COVER LOOSE AT ROW 11. REMOVED AND REPLACED EEPLS SECTION PER MM. 2 L 7 2 4F RT A16WE 2008010800201 20080108 00201 NM 2008 1 8 CALA0700789 1 20071227 A 5313 6545800 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 STRINGER 27L HAS CORROSION STA 380 TO 400. REPAIRED PER SRM 53-00-03 FIG 201 SHEET 7 OF 7 PAGE 207. 2 L 7 2 4F RT A16WE 2008010800202 20080108 00202 NM 2008 1 8 CALA0700790 1 20071228 A 5330 654577572 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 FUSELAGE SKIN CRACKED ABOVE STR 22R 3 INCHES FWD OF STA 727E AND ABOVE PREVIOUS REPAIR. INSTALLED REPAIR PER EC/RA 5331 -01378. 2 L 7 2 4F RT A16WE 2008010800204 20080108 00204 NM 2008 1 8 USAA920071380 1 20071218 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 443US 24842 CLT - MAJOR REPAIR - DROP IN - CRACKED FRAME, BS 492, 24R. REPAIRED FRAME, BS 492, 24R IAW USAIRWAYS EA 100113. 2 L 7 2 4F RT A16WE 2008010800207 20080108 00207 NM 2008 1 8 USAA920071383 1 20071223 A 5330 6545774 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - C3 CHECK, CRACKED FUSELAGE SKIN, BS 727D, S23L. REPAIRED FUSELAGE SKIN, BS 727D, S23L IAW USAIRWAY S TYPICAL REPAIR 53-60-03A. 2 L 7 2 4F RT A16WE 2008010800208 20080108 00208 NM 2008 1 8 USAA920071384 1 20071223 A 5330 6545774 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - C3 CHECK, CRACKED FUSELAGE SKIN, BS 727F, S23L. REPAIRED FUSELAGE SKIN, BS 727F, S23L IAW B737 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2008010800211 20080108 00211 EU 2008 1 8 USAA920071387 1 20071210 A 5315 D53472189202 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 649AW 803 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3207 / FR 67, -Y1292. REPLACED CABIN FLOORBEAM, BS 320 7 / FR 67, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008010800212 20080108 00212 EU 2008 1 8 USAA920071388 1 20071210 A 5320 D53471124201 SHEAR PLATE AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 649AW 803 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN SHEAR PLATE, BS 3310 /FR 69 - BS 3366 / FR 70, -Y1798. REPLACED CABI N SHEAR PLATE, BS 3310 /FR 69 - BS 3366 / FR 70, -Y1798 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008010800213 20080108 00213 EU 2008 1 8 USAA920071389 1 20071210 A 5315 D53472090005 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 649AW 803 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3101 /FR 65, -Y1292. REPLACED CABIN FLOORBEAM, BS 3101 /FR 65, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008010800214 20080108 00214 NM 2008 1 8 SWAA076493 1 20071227 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 255WN 32513 EEPLS LENS MISSING AT ROW 5 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008010800216 20080108 00216 EU 2008 1 8 07FDEA05149 1 20071227 A 2131 82010B040901 CONTROLLER AIRBUS 310 A310203 3930313 EU ZONE 100 MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 427FE 362 EXCESSIVE CABIN ALT ECAM ALERT ON DEPARTURE. SYS 2 VALVES SEEMED TO BE STUCK OPEN. ON INITIAL TROUBLESHOOTING, BOTH CA B PRESS REGULATORS SHOWED ACTIVE (GREEN TRIANGLE ON SWITCH). NR 2 REGULATOR WOULD ACTIVATE AND DEACTIVATE, BUT AS LONG AS NR 1 REG WAS ON IT SHOWED ACTIVE. NR 1 CPC BITE CHECKED GOOD, EXCEPT FOR THE MAN DEPRESS VALVE OPEN CKT AND THE NR 2 CPC WOULD NOT TEST. REMOVED AND REPLACED SYSTEM NR 1 CABIN PRESSURE CONTROLLER REF A310 MM 21-31-11-4. 2 L 7 2 4F RT A35EU 2008010800220 20080108 00220 EU 2008 1 8 07FDEA05152 1 20071228 A 5315 A5327535120000 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 659FE 757 AFT CARGO COMP'T, CROSSBEAM CRACKED AT FRAME 66 BETWEEN TRACKS Y -953 AND Y- 1456. CROSSBEAM REPAIRED AT FRAME 66 BETWE EN TRACKS Y -953 AND Y -1456 IAW SRM 53-10-15, FIGURE 211 (SHEET 1 AND 2). 2 L 7 2 4F RT A35EU 2008010800222 20080108 00222 EA 2008 1 8 TRAX200701981 1 20071225 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA RT OVERWING INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 RT AFT OVERWING EMERGENCY LIGHT IS INOP. 2 L 7 2 4F RT A21EA 2008010800223 20080108 00223 EA 2008 1 8 TRAX200701982 1 20071225 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 PAX DOOR OUTER HANDLE VERY HARD TO STOW FROM INSIDE. 2 L 7 2 4F RT A21EA 2008010800225 20080108 00225 EA 2008 1 8 TRAX200701983 1 20071226 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 933EV 8022 RT 2ND FROM FRONT EXTERNAL EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2008010800226 20080108 00226 NM 2008 1 8 SWAA076498 1 20071227 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 23R CORRODED AT BS 500C. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008010800229 20080108 00229 EA 2008 1 8 TRAX200701985 1 20071226 A 5260 STEP CNDAIR CL600 CL6002C10 1390015 EA AIR STAIR DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 751EV 10163 ASD LOWER STEP DAMAGED. 2 L 7 2 4F RT A21EA 2008010800239 20080108 00239 NM 2008 1 8 HALA0700556 1 20071227 A 2150 WARNING LIGHT BOEING 767 76733A 1385209 NM LT A/C PACK FALSE ACTIVATION A HALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, AFTER ENG SHUT DOWN APU ON LEFT PACK IN AUTO "INOP" LIGHT CAME ON. SELECTED STBY INOP LIGHT W ENT OUT. BIT AIR PACK CONTROLLER PER MM 21-53-00 FIG 103. NO FAULTS. OK TO CONTINUE. 2 L 7 2 4F RT A1NM 2008010800242 20080108 00242 NM 2008 1 8 SWAA076505 1 20071227 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT ASSY CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008010800245 20080108 00245 NM 2008 1 8 SWAA076513 1 20071227 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED MV2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008010800252 20080108 00252 NM 2008 1 8 SWAA076517 1 20071225 A 5610 141A481014 WINDOW BOEING 737 7377H4 1384404 NM COCKPIT CRACKED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 417WN 29822 FLIGHT DECK L2 WINDOW ARCED AND CRACKED. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2008010800253 20080108 00253 NM 2008 1 8 SWAA076508 1 20071227 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 431WN 29845 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008010800258 20080108 00258 EU 2008 1 8 MALA070199 1 20071221 A 5350 SKIN SAAB SF340 340B 7860101 EU TAIL CONE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 418XJ 340B418 DENT LOCATED IN RT UPPER TAILCONE SKIN AT FS827 WITH DEFORMED FRAME. INSTALLED FRAME REINFORCEMENT IAW MAL EO NR S53509 . 2 L 7 2 4T RT A52EU 2008010800259 20080108 00259 EU 2008 1 8 MALA070200 1 20071221 A 5753 SKIN SAAB SF340 340B 7860101 EU TE FLAP CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 418XJ 340B418 45 SMALL SPOTS OF CORROSION LOCATED ON LT FLAP PANEL 541AT BETWEEN WS99 AND WS113. INSTALLED DOUBLER IAW MAL EO NR S571 69. 2 L 7 2 4T RT A52EU 2008010800262 20080108 00262 GL 2008 1 8 SIMA200736203 2 20071224 A 7200 CAE3007A1 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 ODOR A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 618AE 6611 145097 CAE312772 ON FLIGHT 4501 - CLIMBING THRU 700 FEET, AFL MODERATE INTENSITY HAZE FILLED COCKPIT VERIFIED IN CABIN AS WELL, FOLLOWING EMERGENCY PROCEDURES CHECK LIST HAZE BEGAN TO DISSIPATE WHEN RECIRC FAN SELECTED OFF. RETURNED TO ORD EMERGENCY VEHICL ES MET AIRCRAFT. INSPECTED A/C UPON RETURN AND THEY FOUND NO EXTERNAL OR INTERNAL ABNORMALITIES. APU WAS SELECTED OFF FOR THIS ENTIRE EVENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER ONE ENGINE IAW 71-00-00. PERFORMED OPERATIONAL CHECK OPERATION CHECK GOOD. PERFORMED FUNCTIONAL CHECK FLIGHT AND FOUND SATISFACTORY. NO ODOR OR HAZE NOTE D AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008010800263 20080108 00263 SO 2008 1 8 SIMA200736202 1 20071226 A 3411 PITOT HEAD EMB 145 EMB145LR 3260212 SO CONTAMINATED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 694AE 14500869 ON FLIGHT 3378, AFTER TAKEOFF STANDBY ATTITUDE INDICATED (OUT OF ORDER). CAPT DECIDED TO RETURN TO GPT. AIRCRAFT REMOV ED FROM SERVICE. FOUND FLUID IN PITOT STATIC PORT DRAINED FLUID FROM PITOT STATIC LINES IAW AMM 34-13-00 AND COMPLETED OPS CHECK IAW AMM 34-24-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008010800267 20080108 00267 SO 2008 1 8 CHQA200700100 1 20071228 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL BAGGAGE COMPT FALSE INDICATION A CHQA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 11 283SK 17707 145424 CAE312071 CLE TO MSY - AFTER LEVELING OUT AT FL360, THE CREW RECEIVED AN EICAS WARNING FOR "BAGG SMOKE". THE CREW COMPLETED THE A PPROPRIATE QRH CHECKLISTS AND PRESSED THE EXTINGUISHER BUTTON, THEN RECEIVED THE "BAGG EXTNGBTL INOP" MESSAGE. ON DESCE NT TO CMH, THE BAGGAGE SMOKE INDICATION EXTINGUISHED. THE FLIGHT ATTENDANT CONFIRMED THERE WAS NO SMOKE IN THE BAGGAGE COMPARTMENT AND THE FLIGHT LANDED WITHOUT INCIDENT. THE BAGGAGE COMPARTMENT WAS INSPECTED AND NO SIGNS OF FIRE OR SMOKE WERE PRESENT AND BOTH EXTINGUISHER BOTTLES WERE DISCHARGED. MAINTENANCE REPLACED BOTH EXTINGUISHER BOTTLES AND BOTH BA GGAGE COMPARTMENT SMOKE DETECTORS AND THE SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008010800268 20080108 00268 SO 2008 1 8 CHQA200700099 1 20071212 A 3297 8005701 WIRE HARNESS EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NLG DAMAGED A CHQA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 GL 11 275SK 145345 CAE312704 CLE TO DCA. ON APPROACH TO DCA, CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE. THE CREW DECIDED TO DIVERT TO IA D DUE TO ITS LONGER RUNWAYS. THE AIRCRAFT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE UNEVENTFULLY. MAINTENANCE DOW NLOADED THE CMC AND INSPECTED THE NOSE LANDING GEAR PROX SWITCHES AND HARNESSES AND FOUND A NOSE LANDING GEAR PROX SWITC H WITH A BROKEN PIN LODGED IN THE HARNESS. THE PROX SWITCH AND HARNESS WERE BOTH REPLACED AND THE LANDING GEAR SYSTEM F UNCTIONED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008010800269 20080108 00269 NM 2008 1 8 MWEA070311 1 20071228 A 3350 1001191 LIGHT DOUG MD88 MD88 3023688 NM PAX DOOR INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 701ME 49760 EMERGENCY LIGHT FORWARD PASSENGER DOOR DOES NOT LIGHT. REMOVED AND REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F RT A6WE 2008010800271 20080108 00271 NM 2008 1 8 07FDEA05153 1 20071229 A 5313 141N337011 STRINGER BOEING 757 7572B7 1384964 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 STRINGER 18L AT BS 440 HAS A CRACK IN IT'S UPPER RADIUS. REMOVED DAMAGED STRINGER FROM BS 403 TO 440 IAW SRM 51-40-02. FABRICATED NEW STRINGER IAW SRM 51-10-1. LOCATED AND DRILLED NEW STRINGER IAW SRM 51-40-05. INSTALLED NEW STRINGER IAW SRM 51-40-02 AND 53-00-03. USE OF SRM REPAIR ACCEPTABLE PER EAR 67597370130. 2 L 7 2 4F RT A2NM 2008010800272 20080108 00272 NM 2008 1 8 07FDEA05154 1 20071229 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM NLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 592FE 48550 NOSE LANDING GEAR LEFT TRUNNION FITTING FORWARD LOWER CORNER FOUND CRACKED. REPAIRED AS PER SRM 53-40-00 FIGURE 23 V OLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPETITIVELY INSPECT FOR CRACK GROWTH AT NOT TO EXCEED 1,500 LAND ING INTERVALS. 2 L 7 3 4F RT A22WE 2008010800273 20080108 00273 NM 2008 1 8 07FDEA05155 1 20071229 A 5720 ARC4009 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM LT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 592FE 48550 LEFT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER AMM 27-50-30-4. OUTBOA RD FLAP ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-00-5. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008010800276 20080108 00276 NM 2008 1 8 07FDEA05158 1 20071229 A 5753 SUPPORT DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 592FE 48550 RT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING SUPPORT OUTBOARD AFT HOLE FOUND CORROSION. REPAIRED AS PER FEDEX E.A. 1-5750-116536. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008010800285 20080108 00285 NM 2008 1 8 SWAA076520 1 20071227 A 5311 65C33511 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800286 20080108 00286 EU 2008 1 8 07FDEA05165 1 20071231 A 5315 A53612213210 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 659FE 757 FLOORBEAM AT Y 1959 AND BETWEEN FR 12A AND 13A WITH CORROSION. FLOORBEAM REPLACED PER SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008010800287 20080108 00287 EU 2008 1 8 07FDEA05166 1 20071231 A 5320 A5361221420001 FLOOR SUPPORT AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 659FE 757 PAX CABIN, BEAM Y 735 BETWEEN FR 12A TO FR 13A WITH CORROSION. SUPPORT REPLACED IAW WITH SRM 51-72-16 AND PAINTED. 2 L 7 2 4F RT A35EU 2008010800289 20080108 00289 EU 2008 1 8 07FDEA05168 1 20071231 A 5347 A5361252420002 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 659FE 757 TRACK AT Y-953 AND BETWEEN FR 15 AND 19 WITH CORROSION. TRACK REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008010800292 20080108 00292 EU 2008 1 8 07FDEA05171 1 20071231 A 5340 A5378193720100 ADAPTER AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 659FE 757 AT FR 28 AND BETWEEN TRACKS Y-450 AND Y-953 FOUND CRACKED. ADAPTER REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008010800295 20080108 00295 EU 2008 1 8 07FDEA05172 1 20071231 A 5330 A53777380200 SKIN AIRBUS 300 A300F4605R 3930327 EU ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 659FE 757 LWR AFT FUSELAGE GAUGE BETWEEN FR 38.2 AND 39 AND BETWEEN STR 40 AND 41 LT. REPAIRED IAW SRM 53-10-12, FIG 207, SHEET 5 . 2 L 7 2 4F RT A35EU 2008010800297 20080108 00297 EU 2008 1 8 07FDEA05173 1 20071231 A 5347 A5383221120400 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 659FE 757 SEAT TRACK AT Y-953 WITH CORROSION OUT OF LIMITS BETWEEN FR45 AND FR49. TRACK REPLACED BETWEEN FR45 AND FR54 AT Y-953 I AW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008010800299 20080108 00299 NM 2008 1 8 SWAA076526 1 20071227 A 5311 6546596 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800301 20080108 00301 NM 2008 1 8 SWAA076511 1 20071227 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 618WN 28034 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008010800302 20080108 00302 EU 2008 1 8 07FDEA05175 1 20071231 A 5347 A5383202020400 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 659FE 757 SEAT TRACK WITH CORROSION OUT OF LIMITS AT FR41, Y-450. SEAT TRACK REPLACED BETWEEN FR 40 AND FR 45 AT Y-450 IAW SRM 51 -72-10. 2 L 7 2 4F RT A35EU 2008010800303 20080108 00303 EU 2008 1 8 07FDEA05176 1 20071231 A 5522 A55276761008 SKIN PANEL AIRBUS 300 A300F4605R 3930327 EU LT ELEVATOR DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 659FE 757 LT ELEVATOR, DISBOND AT INNER LOWER SKIN AT T/E AREA INBD. DISBOND AT INNER LOWER SKIN WAS REPAIRED IAW SRM 55-21-12, F IG 201. 2 L 7 2 4F RT A35EU 2008010800304 20080108 00304 NM 2008 1 8 KCSA07101 1 20071222 A 2612 FIRE WARNING BOEING 747 7472B4B 138481B NM COCKPIT MALFUNCTIONED A KCSA K NONE N FALSE WARNING CR CRUISE 1 GL 23 713CK 21099 FIRE DETECTION LIGHT ON P5 PANEL AND FAULT LIGHT ON F/E PANEL FLICKERS INTERMITTENTLY AND THEN CAME ON STEADY. NO NAC T EMP INDICATED. ISOLATED FAULT TO NR 1 "A" LOOP. PLACED NR 1 SWITCH TO "B" AND LIGHT EXTINGUISHED. T/S PER AMM 26-11-0 0. UNABLE TO DUPLICATE. SYSTEM OPS CKS OK. 2 L 7 4 4F RT A20WE 2008010800305 20080108 00305 NE 2008 1 8 NWAA074319860 2 20071228 A 7200 ENGINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 2 FAILED A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 769NC 47757 688206 DURING TAKEOFF ROLL FLIGHT CREW HEARD A LOUD "POP" AND NOTICED N1 ROLLBACK. FLIGHT CREW ABORTED THE TAKEOFF AT 110 KNOT S. MAINTENANCE FOUND METAL IN THE TAILPIPE AND REPLACED ENGINE NR 2. 2 L 7 2 4F 4 F RT A6WE E2EA 2008010800307 20080108 00307 EU 2008 1 8 07FDEA05169 1 20071231 A 5340 A5378193720100 ADAPTER AIRBUS 300 A300F4605R 3930327 EU CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 659FE 757 CRACK AT FR 30 AND BETWEEN TRACKS Y-450 AND Y-953. ADAPTER REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008010800313 20080108 00313 NM 2008 1 8 HALA0700564 1 20071229 A 2710 AILERON BOEING 767 76733A 1385209 NM MALFUNCTIONED A HALA O OTHER S AFFECT SYSTEMS CR CRUISE 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, AILERON LOCKOUT 11000 FT 270 ORH NO ACTION. FOLLOWED FIM 27-11-00 FAULT CLEARED ON LSAM. OPS CK OF AILERON GOOD. NO DEFECTS NOTED. 2 L 7 2 4F RT A1NM 2008010800319 20080108 00319 NE 2008 1 8 HALA0700562 2 20071230 A 7320 FUEL SYS BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE MALFUNCTIONED A HALA O OTHER O OTHER DE DESCENT 1 WP 13 581HA 28139 ETOPS SIGNIFICANT SYSTEM, ON DESCENT AND APPROACH RIGHT ENGINE N1 AND N2 AND FUEL FLOW WERE HIGHER THAN LEFT ENGINE, (10 PERCENT OR MORE) EPR'S MATCHED. T/S PER FIM 73-21-00 AND PERFORMED PIMU CHECK IAW FIM 71-00-00. NO PROBLEMS FOUND DUR ING RAN ENG. ALL PARAMETERS NORMAL. OK FOR CONT SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010800321 20080108 00321 NM 2008 1 8 HALA0700561 1 20071230 A 2710 285T0015116 CONTROL UNIT BOEING 767 76733A 1385209 NM MALFUNCTIONED A HALA O OTHER O OTHER DE DESCENT 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, EICAS MSG "AILERON LOCKOUT" ILLUMINATED AT 9000 FT ON DESCENT, DECREASING AIRSPEED THRU 240 KT S DISAPPEARED AT 220 KTS AS A/S DECREASED THRU 6000 ALT DID NOT REAPPEAR THRU LANDING. REPLACED SAM PER AMM 27-09-00. PERFORMED TEST AMM 27-11-00. OK PERFORMED MCDP TEST 65 OK. GND CHECK NR 1 AND 2 ADC OK. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2008010800323 20080108 00323 NM 2008 1 8 DHLA200800001 1 20071229 A 5270 SWITCH BOEING 727 7272Q9 138448M NM PAX DOOR UNSECURE A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 05 741DH 21931 UNKNOWN FLT NR. AFTER LANDING FWD ENTRY LIGHT ON S/O ANNUNCIATOR PANEL ILLUMINATED. CLEANED, RESECURED SWITCH FWD ENTRY DOOR TEST OK IAW B-MM 52-11-01. AIRCRAFT WAS GROUNDED. 2 L 7 3 4F RT A3WE 2008010800327 20080108 00327 WP 2008 1 8 NWAA074339872 1 20071229 A 2710 DRAIN LINE DOUG DC9 DC951 3022051 WP LT SLANT PANEL OBSTRUCTED A NWAA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 01 781NC 48121 WHILE AT CRUISE ALTITUDE FL 250 WITH AUTOPILOT ENGAGED, AIRCRAFT WOULD NOT RESPOND TO AUTOPILOT ROLL COMMAND IN EITHER H EADING, SELECT MODE OR TURN KNOB. DISENGAGED AUTOPILOT AND CONTINUED ROLL CONTROL WAS SEVERELY RESTRICTED WITH MANUAL I NPUT TO CAPTAIN AND FIRST OFFICER CONTROL WHEEL. COM PROCEDURES WERE COMPLIED WITH AND AIRCRAFT DESCENDED TO A LOWER (W ARMER) ALTITUDE OF APPROXIMATELY 12,000 FEET. CONTACTED DISPATCH AND MC AND DECLARED EMERGENCY. ROLL CONTROL WITH COMM ANDED AUTOPILOT AND MANUAL INPUTS STARTED TO RETURN USING LESS FORCE. LANDED UNEVENTFULLY IN DTW. MAINTENANCE INSPECTI ON REVEALED LT WHEEL SLANT PANEL DRAIN CLOGGED. REMOVED DRAIN HOSE AND DRAIN SPOUT. CLEANED LARGE AMOUNT OF DEBRIS FRO 2 L 7 2 4F RT A6WE 2008010800328 20080108 00328 EU 2008 1 8 NWAA074343319 1 20071229 A 2910 LINE AIRBUS 330 A330323 3930335 EU HYD SYSTEM LEAKING A NWAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 819NW 0858 AT CRUISE 5 HOURS AFTER TAKE OFF RECEIVED MESSAGE "HYD G SYS LEAK" AND HYDRAULIC QUANTITY WAS SLIGHTLY BELOW AMBER HASH MARKS, FOLLOWED COM AND TURNED OFF GREEN HYDRAULIC SYSTEM. ON APPROACH TURNED PUMPS ON, DROPPED THE GEAR AND THE REMAIN ING HYDRAULIC FLUID WAS LOST, THE LANDING WAS UNEVENTFUL. FOUND NR 2 HYDRAULIC PUMP PRESSURE HYDRAULIC LINE LEAKING. L INE AND BOTH ENGINE DRIVE HYDRAULIC PUMPS WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A46NM 2008010800330 20080108 00330 NM 2008 1 8 UPS07651333 1 20071227 A 2150 CONTROL VALVE BOEING 767 76734AF 1385212 NM LT FLOW MALFUNCTIONED A IPXA B A EMER. DESCENT UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CR CRUISE 1 SO 01 307UP 27760 CREW RCVD A RIGHT PACK OFF EICAS MSG. UPON COMPLETION OF THE CHECKLIST THEY HAD A FORWARD EQUIP OVERHEAT LIGHT. WHEN C ABIN PRESSURE REACHED 10000 FT AN EMERGENCY WAS DECLARED. DEFERRED UNDER 365842. REMOVED AND REPLACED RT PACK CONTROLL ER PERFORMED BITE TEST, CKS OK. PERFORMED FIM 21- 58-00 FIG 107, NO DEFECTS NOTED, PERF FIM 21-51-00-FIG 103. FOUND LT FLOW CONTROL VALVE FAULTED. PER MEL 21-51-1-0-1. PERFORMED OPS AND LK CHECK OF LLV (LOW LIMITER VALVE) IAW MM 21-51-11 -2. OPS CHECK OK. THIS CLEARS M365842. PLACARD REMOVED. 2 L 7 2 4F RT A1NM 2008010800332 20080108 00332 NM 2008 1 8 UPS07M51338 1 20071029 A 5730 SKIN DOUG MD11 MD11 3023602 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C LT WING L/E LOWER ACCESS, IN BETWEEN REFUELING RECEPTACLES FOUND CORRUGATED SKIN CRACKED AT 04 EA PLAC ES AS MARKED. LT WING REFUELING RECEPTACLE O/B SIDE REMOVED. LT WING L/E CAVITY BEADED SKIN FASTENERS AT DAMAGED AREA AND ATTACH PARTS REMOVED. DAMAGED AREA ON BEADED DOUBLER TRIMMED OFF PER SRM 57-10-00 FIG27 R40VI. HFEC C/O ON TRIM E DGE, FOUND NO CRACK EVIDT. REPAIR DOUBLER AND ANGLES FAB. REPAIR PARTS REPROTECTED, PAINTED AND INSTALLED. RECEPTACLE RE-INSTALL. LEAK CK C/O SATIS. 2 L 7 3 4F RT A22WE 2008010800334 20080108 00334 NM 2008 1 8 UPS07M51339 1 20071107 A 5322 SHEAR TIE DOUG MD11 MD11 3023602 NM BS 1954 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C AFT CARGO/AT STATION 1954 IN BETWEEN LONGERON 49 LT TO 49 RT FRAME SHEAR CLIP FOUND WITH SURFACE CORRO SION. AFT CARGO STA 1954 - 1964 L52 (01EA) AND L51 (01EA) EXISTING INTERCOSTAL ALSO REMOVED. EXISTING BRACKETS 05EA RE MOVED AT STA 1954 L49 LT - L49 RT. CORRODED SHEAR CLIP REMOVED PER SRM 51-31-01VIIR35. NEW SHEAR CLIP FAB AND HEAT-TRE ATED. NEW SHEAR CLIP INSTALLED. 05 EA BRACKETS RE-INSTALLED. TWO INTERCOSTALS RE-INSTALLED TO THEIR RESPECTIVE POSITIO NS. 2 L 7 3 4F RT A22WE 2008010800341 20080108 00341 NM 2008 1 8 F3LA200700410 1 20071212 A 3350 321431 BATTERY PACK AIRBUS A319 A319111 3930336 NM EMERGENCY LIGHTS NO TEST A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 912FR 1803 DURING C4/S1 CHECK, INSPECTION REPORTED AFT EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED AND INSTALLED SERVIC EABLE AFT EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-38-000-002. PERFORMED BITE TEST OF AFT EMERGENCY LIGHT EPSU/BATTER Y PACK IAW AMM 33-51-38-400-002 AND CHECKED GOOD. 2 L 7 2 4F RT A28NM 2008010800345 20080108 00345 EA 2008 1 8 SWIA200719002 1 20071227 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 453SW 7743 FLT 3789 - ON TAKEOFF RECEIVED A GEAR DISAGREE MESSAGE AND THE NOSE WOULD NOT RETRACT. ADJUSTED PROX SENSORS PS13GA, PS 14GA AND PS4GA. OPS CHECK GOOD IAW 32-61-05. 2 L 7 2 4F RT A21EA 2008010800352 20080108 00352 CE 2008 1 8 AMWA88960BC 1 20071206 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MAIN DISCHARGED A AMWA K NONE J WARNING INDICATION CR CRUISE 1 CE 07 142ZV 2417 55 UE142 BATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED BATTERY AND CLEARED DISCREPANCY. 2 L 7 2 4T 3 T RT A24CE E2NE 2008010800353 20080108 00353 CE 2008 1 8 AMWA18345BC 1 20071207 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MAIN DISCHARGED A AMWA K NONE J WARNING INDICATION CR CRUISE 1 CE 07 162ZV 2082 122 UE162 BATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED BATTERY AND CLEARED DISCREPANCY. 2 L 7 2 4T 3 T RT A24CE E2NE 2008010800354 20080108 00354 CE 2008 1 8 AMWA071001017 1 20071206 A 5730 11811001542 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RT WING CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 244YV 23091 UE244 FRICTION CHAFING DURING ENGINE OPERATION CREATED WORN SEGMENTS ON THE RT ENGINE NACELLE. CHAFING WAS ALONG THE ENTIRE LE NGTH AND SHAPE OF THE NACELLE. OBTAINED APPROVED DATA AND REPAIRED WING SKIN. 2 L 7 2 4T 3 T RT A24CE E2NE 2008010800357 20080108 00357 CE 2008 1 8 GUUA12040702 1 20071204 A 5524 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A6 52043 EA RT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 218YV UE218 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT OB ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED RT OB ELEVATOR HINGE BRACKET. 2 L 7 2 4T 3 T RT A24CE E4EA 2008010800364 20080108 00364 CE 2008 1 8 GLBA20061040 1 20071211 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA FUSELAGE DAMAGED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 254GL UE254 DAMAGE TO SKIN AT FS 163.975 AND STRINGER 2L AND 3L. MAINTENANCE REPAIRED SKIN AT FS 163.975 AND STRINGER 2L AND 3L IAW SRM 51-70. REPAIR DIMENSIONS APPROXIMATELY 13.5 BY 13.2500. RII INSPECTION COMPLIED IAW GLA TASKCARD 8.2.1. 2 L 7 2 4T 3 T RT A24CE E2NE 2008010800373 20080108 00373 EA 2008 1 8 SWIA200719007 1 20071008 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 743SK 10199 FOUND AT C-CHECK, FS 280 BEAM IS CRACKED AT LBL9 AND RBL9. REPLACED FS 280 CROSSBEAM PER CRJ700 SRM 51-23-00 PG 9-10 / 51-42-06 PG 7-8 AND REO 670-53-11-242. 2 L 7 2 4F RT A21EA 2008010800374 20080108 00374 EA 2008 1 8 SWIA200719008 1 20071008 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 743SK 10199 FOUND AT C-CHECK, COCKPIT FLOOR SUPPORT IS CRACKED AT RBL 9 AND LBL AT FS 280. REPLACED COCKPIT FLOOR SUPPORT PER CRJ70 0/900 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008010800376 20080108 00376 NM 2008 1 8 AMTA200700675 1 20071202 A 2913 887673 PUMP BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE NR 1 ENGINE DEFECTIVE A AMTA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 11 514AT 27971 HYD QTY DECREASE TO LESS THAT .5. RSVR LIGHT (EICAS) ILLUMINATED. QTY .26 ON LANDING. REMOVED AND REPLACED NR 1 ENG E DP IAW MM 29-11-05-4, PSI CHECK GOOD, LEAK CHECK GOOD, OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010800377 20080108 00377 2008 1 8 AMTA200700699 4 20071207 A 2310 9640453011 COUPLER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE NR 2 UNSERVICEABLE A AMTA K NONE L NO TEST CR CRUISE 1 GL 11 522AT 29330 RT HF WILL NOT CHANNELIZE. REMOVED AND REPLACED RT HF COUPLER IAW MM 23-11-01-4, CHANNELIZED AND OPS NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010800378 20080108 00378 2008 1 8 AMTA200700700 4 20071208 A 2310 9640453011 COUPLER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE NR 1 UNSERVICEABLE A AMTA K NONE L NO TEST CR CRUISE 1 GL 11 522AT 29330 LT HF RECEPTION WEAK AT ALL CREW STATION. REMOVED AND REPLACED LT HF COUPLER IAW MM 23-11-01-4, LT HF OPS CHECK NORMAL, CALLED SFO ON 5574, TRANSMITT AND RECIEVE 5 X 5. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010800379 20080108 00379 2008 1 8 AMTA200700701 4 20071209 A 2310 9640453011 COUPLER BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE NR 1 UNSERVICEABLE A AMTA K NONE L NO TEST CR CRUISE 1 GL 11 560TZ 33525 LT HF RECEPTION WEAK AT ALL CREW STATIONS. REMOVED AND REPLACED NEW LT HF COUPLER IAW MM 23-11-01-4, OPS CHECK NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010700206 20080107 00206 NM 2008 1 7 2007UALA05217 1 20071221 A 5320 FLOOR SUPPORT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 MAIN CABIN GALLEY FLOOR SUPPORT CORRODED AT STA 790 TO 800 BL 9R TO 10R. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010700210 20080107 00210 NM 2008 1 7 2007UALA05219 1 20071221 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 AFT CARGO BAY, STA 1131, RBL 36, TEE CAP CORRODED UNDER NUT PLATES. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010700225 20080107 00225 NM 2008 1 7 2007UALA05232 1 20071222 A 2621 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FIRE BOTTLE INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 539UA 25223 NR 2 CARGO FIRE BOTTLE DISCHARGE LIGHT IS BURNED OUT. REPLACED NR 2 CARGO FIRE SWITCH ASSY. OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700261 20080107 00261 NM 2008 1 7 2007UALA05255 1 20071222 A 2611 2156656 SMOKE DETECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FWD CARGO BAY FALSE ACTIVATION A UALA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 29 104UA 26902 STATUS MESSAGE CARGO FWD-2 LOOP-A MESSAGE. STATUS MESSAGE CARGO FWD-2 LOOP-A MESSAGE. NO ACTIVE MESSAGE ON AIRCRAFT AR RIVAL. NO PRESENT LEG FAULTS. NUMEROUS FIRE TESTS CARRIED OUT BOTH FROM OVERHEAD SWITCH AND CMC GROUND TEST. ALL TESTS P ASS. DEFERRAL CLEARED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700266 20080107 00266 NM 2008 1 7 2007UALA05260 1 20071222 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 117UA 28810 DOOR 4R EMERGENCY EXIT LIGHT DIM. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700272 20080107 00272 NM 2008 1 7 2007UALA05266 1 20071223 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY CEILING LIGHT AT ROW 23 ABC INOPERATIVE. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700273 20080107 00273 NM 2008 1 7 2007UALA05267 1 20071222 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY LIGHT NEAR ROW 17 RIGHT IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700312 20080107 00312 NM 2008 1 7 2007UALA05295 1 20071225 A 2421 767146A IDG BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RT ENGINE DISCONNECTED A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 225UA 30554 CAPTAIN STATED VIA PHONE DISPATCH, THAT RT GENERATOR DISCONNECTED AND APU WAS STARTED PER FLT MANUAL. SUSPECT INTEGRATED DRIVE GENERATOR FREQUENCY IS LOW. REPLACED RT IDG AND CHECKED OK. ACFT OK FOR SERVICE 2 L 7 2 4F 4 F RT T0001SE E46NE 2008010700330 20080107 00330 NM 2008 1 7 SWAA076441 1 20071222 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 971, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008010700342 20080107 00342 EU 2008 1 7 07FDEA05125 1 20071224 A 5315 LN9497420 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 404FE 233 FWD CARGO COMPARTMENT AT FR 36 CROSSMEMBER HAS EXFOLIATION CORROSION AT CENTER AND RT ROLLER TRAY MATING SURFACE REMOVED CORROSION IAW A310 SRM 51-74-10 FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-10-15. FABRICATED CROSSMEMBER AND SPLICE ANG LES IAW A310 SRM 53-14-15. INSTALLED CROSSMEMBER AND SPLICE ANGLES IAW A310 SRM 53-10-15. 2 L 7 2 4F RT A35EU 2008010700343 20080107 00343 EU 2008 1 7 07FDEA05126 1 20071224 A 5315 LN9497420 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 404FE 233 FWD CARGO COMPARTMENT CROSSMEMBER AT FRAME 34 HAS EXFOLIATION CORROSION AT CENTER AND RT ROLLER TRAY MATING SURFACE REMO VED CORROSION IAW A310 SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW A310 SRM 53- 10-15. FABRICATED CROSSMEMBER AND SPL ICE ANGLES IAW A310 SRM 53-14-15. INSTALLED CROSSMEMBER AND SPLICE ANGLES IAW A310 SRM 53-10-15. 2 L 7 2 4F RT A35EU 2008010700344 20080107 00344 EU 2008 1 7 07FDEA05127 1 20071224 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS STRINGER REPAIR LOCATED IN AFT CABIN UNDER FLOOR BEHIND BULK CARGO ON STRINGER 44 RT BETWEEN FRAMES 74 TO 75, H AS 1 EACH REPAIR SPLICE MEASURING 9.6" LONG WITH A 2.1" CUTOUT ON STRINGER. PREVIOUSLY INSTALLED REPAIR LOCATED IN AFT CARGO UNDER FLOOR ON STRINGER 44 RT BETWEEN FR 74 TO 75 WAS DETERMINED NOT TO BE IAW A310 SRM 53-10-14 FIG 201 DUE TO IN CORRECT THICKNESS. REMOVED EXISTING REPAIR AND REPAIRED IAW A310 SRM 53-10-14 FIG 201. THIS IS A REPAIR WITH NO AIRBUS ISSUED PART NUMBER, REPAIR IDENTIFIED BY THE AGING AIRCRAFT INSPECTION PROGRAM. 2 L 7 2 4F RT A35EU 2008010800022 20080108 00022 NM 2008 1 8 CALA0700777 1 20071221 A 5420 A1355126 SPLICE PLATE BOEING 737 7373T0 1384582 NM NR 2 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 NR 2 PYLON LT SPLICE PLATE IS CRACKED AT NAC STA 345.28 AND NAC WL 118.95. REMOVED AND REPAIRED CRACKED SECTION ON NR 2 PYLON I/B SPLICE PLATE REF ECRA 5421-01016. 2 L 7 2 4F RT A16WE 2008010800026 20080108 00026 NM 2008 1 8 CALA0700782 1 20071218 A 5330 65C33756 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 TWO INCH CRACKED IN FUSELAGE SKIN, AT THE AFT LOWER CORNER OF R-1 DOOR CUTOUT. REPAIRED PER ECRA 5331-01367. 2 L 7 2 4F RT A16WE 2008010800036 20080108 00036 EU 2008 1 8 07FDEA05132 1 20071224 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS STRINGER REPAIR LOCATED IN BULK CARGO ON STRINGER 55 LT BETWEEN FRAMES 65 T0 68, HAS 1 EACH REPAIR SECTION ME ASURING 36.8" LONG AND 2 EACH REPAIR SPLICES MEASURING 7.8" LONG ON THE FORWARD SPLICE AND 8.1" LONG ON THE AFT SPLICE. PREVIOUSLY INSTALLED REPAIR LOCATED AT BULK CARGO ON STRINGER 55 LT BETWEEN FRAMES 65 TO 68 WAS DETERMINED NOT TO BE IA W A310 SRM 53-10-14 FIG 201, DUE TO INCORRECT REPAIR MATERIAL INSTALLED, BASED ON A VISUAL INSPECTION WITH THE REPAIR IN STALLED. REMOVED EXISTING REPAIR AND REPAIRED STRINGER PER A310 SRM 53-10-14 FIG 201. THIS IS A REPAIR WITH NO AIRBUS ISSUED PART NUMBER, REPAIR IDENTIFIED BY THE AGING AIRCRAFT INSPECTION PROGRAM. 2 L 7 2 4F RT A35EU 2008010800038 20080108 00038 EU 2008 1 8 07FDEA05134 1 20071224 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS STRINGER REPAIR LOCATED IN BULK CARGO ON STRINGER 52 LT BETWEEN FRAMES 63 TO 65, HAS 1 EACH REPAIR SECTION ME ASURING 28.9" LONG AND 1 EACH REPAIR SPLICE MEASURING 7.2" LONG. PREVIOUSLY INSTALLED REPAIR LOCATED AT BULK CARGO ON S TRINGER 52 LT BETWEEN FRAMES 63 TO 65 WAS DETERMINED NOT TO BE IAW A310 SRM 53-10-14 FIG 201, DUE TO INCORRECT REPAIR SP LICE MATERIAL INSTALLED, BASED ON A VISUAL INSPECTION WITH THE REPAIR INSTALLED. REMOVED EXISTING REPAIR SPLICE AND REP AIRED PER SRM 53-10-14 FIG 201. THIS IS A REPAIR WITH NO AIRBUS ISSUED PART NUMBER, REPAIR IDENTIFIED BY THE AGING AIRC RAFT INSPECTION PROGRAM. 2 L 7 2 4F RT A35EU 2008010800042 20080108 00042 NM 2008 1 8 07FDEA05138 1 20071224 A 3020 10605083 EJECTOR VALVE BOEING 727 727233 138408A NM NR 2 ENGINE FAILED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 25 264FE 21626 ENG ANTI ICE VALVES WERE ON FOR T/O. IMMEDIATELY AFTER T/O, THE NR 2 ENGINE ANTI ICE DUCT TEMP WENT FULL SCALE HOT AND THE OVERHEAT LIGHT ILLUMINATED. WITHIN 30 SECS, LT PACK TRIPPED AND ENG FAIL LIGHT ILLUMINATED. STANDARD BLEED/PACK CO NFIGURATION FOR T/O. EMERGENCY WAS DECLARED AND IMMEDIATE RETURN TO SWF. REMOVED AND REPLACED NR 2 ENGINE EJECTOR VALV E AND ACTUATOR ASSY PER AMM 30-21-011-4, NR 2 THERMAL ANTI-ICE DUCT TEMPERATURE SENSOR PER AMM 30-21-061-4, NR 2 COWL AN TI-ICE THERMAL SWITCH PER AMM 30-21-051-4 AND THE NR 2 INLET COWL ANTI-ICE CHECK VALVE PER AMM 30-21-041-4, FUNCTIONALLY TEST COWL TAI SYSTEM PER AMM 31-21-001-5. 2 L 7 3 4F RT A3WE 2008010800047 20080108 00047 EA 2008 1 8 TRAX200701965 1 20071222 A 2560 GLOWSTRIP CNDAIR CL600 CL6002C10 1390015 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 755EV 10185 PHOTO LUMINESCENT TAPE MISSING NEAR GALLEY CART STORAGE AREA. 2 L 7 2 4F RT A21EA 2008010800051 20080108 00051 2008 1 8 ASAA0752437 4 20071226 A 3460 1762000101 FMC BOEING 737 737890 1384527 NM E&E BAY MALFUNCTIONED A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 577AS 35186 FMC MESSAGE POPS UP AS FOLLOWS: "VERIFY THE FOLLOWING DATA LOADER IS POWERED * NO DISC IN DATA LOADER * SELECT SOURCE F MC ON DATA LOAD SELECT PANEL" SOURCE FMC SELECTED VIA THE FMC SOURCE SEL SWITCH. CYCLED SHIPS POWER AND MESSAGE CLEARED & DID NOT COME BACK. FMC NR 1 #2 NORMAL OPS. 2 L 7 2 4F RT A16WE 2008010800055 20080108 00055 NM 2008 1 8 ASAA0772429 1 20071207 A 5315 147A55068 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CABIN FLOORBEAM BS 986 LBL 52 TO RBL 52 CORRODED. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008010800066 20080108 00066 EA 2008 1 8 TRAX200701971 1 20071221 A 7830 BUSHING CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER MIGRATED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 RT ENGINE T/R NR 5 BLOCKER DOOR TO LINK UPPER BUSHING MIGRATED. 2 L 7 2 4F RT A21EA 2008010800067 20080108 00067 EA 2008 1 8 TRAX200701972 1 20071221 A 5514 PIN CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 HORIZONTAL STABILIZER RT OUTER PIN WORN. 2 L 7 2 4F RT A21EA 2008010800072 20080108 00072 EA 2008 1 8 TRAX200701978 1 20071222 A 5514 BONDING JUMPER CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 FOUND HARDWARE AND BONDING JUMPER ON HORIZONTAL STAB LT CENTER HINGE FITTING CORRODED. 2 L 7 2 4F RT A21EA 2008010800083 20080108 00083 NM 2008 1 8 ASAA0772438 1 20071205 A 5347 453A26112 PLATE BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT RIGHT TIE DOWN PLATE AT STA 8 & 9 CORRODED. REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 51-40-05 & 53 -60-53. 2 L 7 2 4F RT A16WE 2008010800090 20080108 00090 SO 2008 1 8 RAIA00712025 1 20071219 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO CABIN MALFUNCTIONED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 821HK 145068 PRE FLT 5587 - STL - GALLEY EMERGENCY LIGHT INOP. MAINTENANCE RECYCLED CONNECTOR TO LIGHT, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2008010800092 20080108 00092 SO 2008 1 8 RAIA00712026 1 20071221 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 809HK 145187 POST FLT NR 3501 - PIT - MAIN DOOR EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED LIGHT, OPS CHECK GOO D AT THIS TIME. 2 L 7 2 4F RT T00011AT 2008010800105 20080108 00105 NM 2008 1 8 QXEA200701798 1 20071125 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX C-4 INSPECTION, GOUGES AT FORWARD AND AFT APERTURE OF THE FORWARD LAV SERVICE DOOR. BLENDED AREA AND FOUND WITHIN L IMITS. ETCHED AND ALODINED AREA AND PAINTED. 2 H 7 2 4T RT A13NM 2008010800108 20080108 00108 NM 2008 1 8 QXEA200701801 1 20071125 A 5321 FLOORBOARD BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK, OUTBOARD WARDROBE FLOORBOARD ABOVE STRINGER 30L HAS CORROSION AROUND 2 NUTPLATE HOLES. REMOVED CORROSIO N AND BLENDED AREA. AREA REMOVED .003, WITHIN LIMITS. HFEC INSPECTED WITH NO CRACKS. ALODINE PRIMED AND PAINTED. 2 H 7 2 4T RT A13NM 2008010800116 20080108 00116 NM 2008 1 8 SWAA076456 1 20071224 A 5311 6545805 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16R. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008010800121 20080108 00121 NM 2008 1 8 SWAA076462 1 20071224 A 5311 6546596 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800141 20080108 00141 SO 2008 1 8 SWIA200718989 1 20071220 A 5753 HINGE EMB 120 EMB120ER 3260203 SO NACELLE FLAP CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 215SW 120281 FLT 3677 - RIGHT NACELLE FLAP INBOARD HINGE IS CRACKED. REPLACED RIGHT NACELLE FLAP IAW 27-50-03.PN 120-34383-002. 2 L 7 2 4T RT A31SO 2008010800148 20080108 00148 SO 2008 1 8 SWIA200718996 1 20071108 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 582SW 120350 RIGHT WING NR 2 FUEL PANEL STRINGER IS CRACKED ALONG AFT SIDE, FOUND AT C-CHECK. REPAIRED STRINGER IAW SRM 120 57-20-03 PG 206-211 FIG 202. 2 L 7 2 4T RT A31SO 2008010800153 20080108 00153 NM 2008 1 8 SWAA076468 1 20071224 A 5711 7075T73 FITTING BOEING 737 7375H4 138449D NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRIDGE CHECK, FOUND RT WING AFT SPAR SUPPORT FITTING NR 7 MAIN FLAP TRACK CORRODED AT OUTBOARD FLAP TRA CK MOUNT HOLE. REMOVED AND REPLACED AFT SPAR SUPPORT FITTING PER MM. 2 L 7 2 4F RT A16WE 2008010800154 20080108 00154 NE 2008 1 8 REXA200700066 2 20071227 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RIGHT FLAMED OUT A REXA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 25 8416B 7416 872571 WHEN THE CREW REDUCED POWER TO DESCEND FROM FL300, THE RIGHT ENGINE FLAMED OUT. THE ENGINE OUT PROCEDURES OF THE QRH WE RE PERFORMED AND THE ENGINE RESTARTED ON THE FIRST ATTEMPT. AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WERE MADE. MA INTENANCE TROUBLESHOT THE ENGINE CONTROL SYSTEM AND FOUND IT TO BE PROPERLY RIGGED. GROUND RUNS WERE PERFORMED INCLUDIN G ACCEL/DECEL CHECKS AND ALL CHECK NORMALLY. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008010800182 20080108 00182 NM 2008 1 8 SWAA076486 1 20071223 A 3350 BR2013 COVER BOEING 737 7373T5 1384608 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 696SW 23064 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER BROKEN FROM ROW 6 TO ROW 7. REMOVED AND REPLACED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2008010800187 20080108 00187 NM 2008 1 8 SWAA076489 1 20071223 A 3350 D1701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 746SW 29798 DURING SCHEDULED HC1 CHECK, AFT LEFT CABIN EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BAT TERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008010800188 20080108 00188 EU 2008 1 8 07FDEA05028 1 20071211 A 5330 A53772527200 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 403FE 230 FUSELAGE EXTERNAL REPAIR DOUBLER AT FR 18-19 STRINGERS 38/39 RT FWD OF FWD CARGO DOOR REQUIRES EVALUATION FOR MAJOR/MINO R DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. VISUALLY INSPECTED EXISTING REPAIR DOUBLER AT F RAME 18/19 RT BETWEEN STRINGERS 38-39 AND FOUND THAT REPAIR DID NOT CONFORM TO APPROVED REQUIREMENTS. REMOVED AND REPLA CED EXTERNAL REPAIR DOUBLER IAW A310-200 SRM 53-10-12 FIG 225. 2 L 7 2 4F RT A35EU 2008010800196 20080108 00196 EU 2008 1 8 07FDEA05146 1 20071129 A 5315 A5327534520000 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 659FE 757 AFT CARGO COMPT, CROSSBEAM CRACKED AT FRAME 60 BETWEEN TRACKS Y-1456 AND Y-1959. CROSSBEAM REPAIRED AT FRAME 60 BETWEEN Y-1456 AND Y-1959 IN ACCORDANCE WITH SRM 53-10-15 FIG 211 (SHEET 1 AND 2). 2 L 7 2 4F RT A35EU 2008010800200 20080108 00200 WP 2008 1 8 07FDEA05148 1 20071227 A 5347 6045087075T65 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 568FE 47827 UPPER CARGO SEAT TRACK 28L, FS 1884L TO 1661L HAS WORN LOBES (5 EACH) FS 1871, 1730, 1690, 1681, AND 1664. BLENDED (5 EACH) AREAS STA 1871, 1730, 1690, 1681 AND 1664 SEAT TRACK FOUND TO BE WITHIN LIMITS IAW SRM 53-70-00 FIG 5 EXCEPT STA 1730 FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG 5. FABRICATED NEW SEAT TRACK ON MAE TRAVELER NR T7/717467 AND 2 EAC H HAT SPLICES ON MAE TRAVELER T7/717468 IAW SRM. INSTALLED NEW SEAT TRACK AT UPPER CARGO SEAT TRACK 28L STA 1711 TO STA 1750 IAW SRM 53-70-00 FIG 5. 2 L 7 3 4F RT A22WE 2008010800203 20080108 00203 NM 2008 1 8 CALA0700791 1 20071227 A 2530 72067752 OVEN BOEING 757 757224 1384958 NM AFT GALLEY OVERHEATED A CALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 27 13138 49869 5022 30351 LAV SMOKE INDICATION ON EICAS. THE LEFT AFT LAV SMOKE DETECTOR WAS ACTIVATED. NO FLAME WAS NOTICED, BUT THE A/C DID HA VE A SMOKE (ELECTRICAL) SMELL. DIVERTED TO LAS. PER F/A WORKING AFT GALLEY, WHEN DOOR TO NR 1 OVEN OPENED SMOKE CAME O UT AND AFT LAV SMOKE DETECTION WENT OFF IMMEDIATELY. REMOVED NR 1 OVEN, INSPECTED WIRING, NO FAULTS FOUND. PULLED AND COLLARD NR 1 OVEN C/B AND PLACARD INOP. INSPECTED LAV PRECAUTIONARY NO FAULTS NOTED. OVEN HAS BEEN REMOVED AND REPLACE D. 2 L 7 2 4F RT A2NM 2008010800206 20080108 00206 NM 2008 1 8 USAA920071382 1 20071223 A 5330 6545775 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - C3 CHECK, CRACKED FUSELAGE SKIN, BS 727E - BS 727F, S23R. REPAIRED FUSELAGE SKIN, BS 727E - BS 727 F, S23R IAW B737 SRM 53-00-01. 2 L 7 2 4F RT A16WE 2008010800217 20080108 00217 NM 2008 1 8 07FDEA05150 1 20071227 A 3260 INDICATOR DOUG MD11 MD11F 3023600 NM MLG MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 624FE 48443 WITH LDG GEAR LEVER IN THE UP AND LOCKED POSITION, RT MAIN GEAR INDICATED RED ON BOTH PRIMARY AND SECONDARY INDICATIONS. COMPLIED WITH QRH. DISCOVERED RT MLG HYD HOSE GUIDE BROKEN. REMOVED AND REPLACED SAME. REF IPC SUP 32-43-10-01 SHEE T 4 ITEM 430. INSPECTED MLG UPLOCK ASSY. NO DAMAGE NOTED. GEAR REQUIRES RETRACTION CHECK. 2 L 7 3 4F RT A22WE 2008010800221 20080108 00221 NM 2008 1 8 SWAA076496 1 20071227 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 6 O'CLOCK POSITION. REPAIRED WEB PER E R. 2 L 7 2 4F RT A16WE 2008010800227 20080108 00227 EA 2008 1 8 TRAX200701984 1 20071226 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 979EV 7737 PAX DOOR WILL NOT CLOSE. 2 L 7 2 4F RT A21EA 2008010800228 20080108 00228 NM 2008 1 8 SWAA076499 1 20071227 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 26R CORRODED AT BS 356. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008010800232 20080108 00232 2008 1 8 SWAA076503 4 20071227 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM EVAC SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM. 2 L 7 2 4F RT A16WE 2008010800235 20080108 00235 NM 2008 1 8 SWAA076500 1 20071227 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM. 2 L 7 2 4F RT A16WE 2008010800241 20080108 00241 NM 2008 1 8 SWAA076507 1 20071227 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT AIR CONDITIONING BAY CUTOUT BETWEEN RT BS 590 AND RT BS 616. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2008010800246 20080108 00246 NM 2008 1 8 QXEA200702036 1 20071227 A 6120 CSD BOMBDR DHC8 DHC8402 1390042 NM FAULTED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 407QX 4049 PDX - FLIGHT 2462, DURING TAXI AND OVERSPEED GOVERNOR TEST, A WHITE MESSAGE AND YELLOW "ABORT" LETTERS APPEARED ON THE D ISPLAY FOR NR 1 ENGINE. THIS WAS FOLLOWED BY A POWERPLANT MESSAGE. RETURNED TO THE GATE. MAINTENANCE CHECKED THE CDS SYSTEM AND FOUND A CODE 496. COMPLIED WITH THE OVERSPEED GOVERNOR TEST IAW TAKE 61-20-00-701-03. POWERPLANT MESSAGE WE NT AWAY AND NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008010800270 20080108 00270 NM 2008 1 8 MWEA070312 1 20071228 A 3350 6011779 BATTERY PACK BOEING 717 717200 1383700 NM EMERGENCY LIGHTS INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 905ME 55169 BOTH LEFT AND RIGHT AFT EXTERNAL EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F TR A6WE 2008010800293 20080108 00293 NM 2008 1 8 SWAA076522 1 20071227 A 5311 65C34356 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800298 20080108 00298 NM 2008 1 8 SWAA076525 1 20071227 A 5311 6546552 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800300 20080108 00300 EU 2008 1 8 07FDEA05174 1 20071231 A 5347 A5383202020400 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 659FE 757 SEAT TRACK WITH CORROSION OUT OF LIMITS AT FR42, Y0. SEAT TRACK REPLACED BETWEEN FR 40 AND FR 45 AT Y0 IAW SRM 51-72-10 . 2 L 7 2 4F RT A35EU 2008010800312 20080108 00312 EU 2008 1 8 2007UALA05143 1 20071217 A 2611 CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SMOKE DETECTION FAILED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 408UA 457 SMOKE LAV + CARGO DETECTOR FAULT DISPLAYED ON ECAM WHEN RECALL CRG SMOKE TEST FAILS. SDCU FAILURE. REPLACED SDCU AND F WD PIT DETECTOR AS PRECAUTIONARY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010800315 20080108 00315 NM 2008 1 8 2007UALA05152 1 20071212 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW OXYGEN LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 846UA 1600 CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. SERVICED CREW O2 TO 1850 PSI. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010800318 20080108 00318 NM 2008 1 8 2007UALA05173 1 20071220 A 3350 GE1810 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 829UA 1211 EPSU EXT LOAD EMER R - FAULT FOUND ON 3 SVC EMERGENCY LIGHT TEST. OVERWING EMERGENCY WING LIGHTS INOP. REPLACED OVERWI NG EMERGENCY FLOOD LIGHTS. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010800329 20080108 00329 EU 2008 1 8 UPS07151350 1 20071229 A 2560 80230014 PBE AIRBUS A300 A300F4622R 3930360 EU CABIN DAMAGED A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 147UP 0830 PS1 PBE NO LONGER VACUUM SEALED. REPLACED PBE WITH SERVICEABLE UNIT. 2 L 7 2 4F RT A35EU 2008010800335 20080108 00335 NM 2008 1 8 UPS07M51340 1 20071029 A 5730 SKIN DOUG MD11 MD11 3023602 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C LT WING L/E LOWER ACCESS, 12" O/B OF SLAT TRACK NR 11, FOUND CORRUGATED SKIN CRACKED AT 05 EA PLACES A S MARKED. LHW L/E CAVITY BEADED SKIN FASTENERS AT DAMAGED AREA AND ATTACHED PARTS REMOVED. DAMAGED AREA ON BEADED DOUB LER TRIM OFF PER SRM 57-10-00 FIG 27R40 VI. HFEC INSP C/O ON TRIM OFF AREA AND FOUND NO CRACK EVIDENT. REPAIR DOUBLER, FILLER AND ANGLES FAB. REPAIR PARTS RE-PROTECTED AND PAINTED. REPAIR PARTS INSTALLED PER SRM 57-10-00 FIG 27 VIR40. 2 L 7 3 4F RT A22WE 2008010800338 20080108 00338 NM 2008 1 8 UPS07M51347 1 20071113 A 5713 STRINGER DOUG MD11 MD11 3023602 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C RT WING UPPER FUEL TANK STRINGER NR 12 END SUSPECT CRACKED. HFEC INSP C/O AT STR NR 12 END FOUND CRAC K OF APPROX 8" LONG. STR NR 12 SPLICE END AND LOCK FASTENERS AT REPAIR AREA REMOVED. CRACK AT STR NR 12 SLOT OUT PER S RM 57-20-00 FIG 10 VIR35. HFEC INSP C/O ON SLOT OUT AREA AND FOUND NO CRACK EVIDENT. REPAIR ANGLES FAB, HEAT-TREATED, REPROTECTED AND PRIMED. REPAIR ANGLES AND STR NR 12 SPLICE END INSTALLED. SEALANT APPLIED, LEAK CK SATIS. 2 L 7 3 4F RT A22WE 2008010800344 20080108 00344 SO 2008 1 8 SWIA200719001 1 20071229 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 224SW 120294 FLT 5672 - EXIT SIGN BELOW WINDOW IN 6A IS BROKEN. REPLACED EMERGENCY EXIT SIGN AT 6A. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008010800346 20080108 00346 EA 2008 1 8 SWIA200719003 1 20071223 A 3260 SENSOR CNDAIR CL600 CL6002B19 1900309 EA NLG CENTERING MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 405SW 7029 FLT 3756 - NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. INSPECTED NOSE GEAR AND ADJUSTED CENTERING SENSOR GAP IAW MM 32-6 1-05. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2008010800355 20080108 00355 SO 2008 1 8 GLBA20061036 1 20071209 A 2150 1945463 HEAT EXCHANGER EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE LEFT DETERIORATED A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 71GL 120071 SMOKE/SMELL, ENROUTE, PILOTS REPORTED THAT SMOKE FILLED THE COCKPIT AND CABIN OUT OF THE HEATER VENTS. MX RE-INSTALLED A HOSE THAT WAS ASSOCIATED WITH THE LT PACK. CHECKS ON GROUND WERE GOOD. SUBSEQUENT OPERATIONAL CHECK FLIGHT WAS UNSATISF ACTORY. MAINTENANCE REMOVED AND REPLACED THE LT HEAT EXCHANGER IAW MM 21-50. OPERATIONAL CHECKS WERE OK. 2 L 7 2 4T 4 T RT A31SO E20NE 2008010800365 20080108 00365 EA 2008 1 8 2007F00069 1 20071213 A 5610 603303025 WINDSHIELD CNDAIR CL600 CL6001A11 1900308 EA COCKPIT CRACKED E B EMER. DESCENT O OTHER CR CRUISE 1 SW 09 900LG 1233 1036 EN ROUTE AT FL330, THE CAPTAIN NOTICED A CRACK IN THE EXTERIOR PANEL OF THE LT FWD WINDSHIELD. THE APPROPRIATE CHECKLIST WAS COMPLETED AND A SPEED REDUCTION AND DECENT REQUESTED. WHILE DESCENDING A LOUD (POP) AND SUBSEQUENT WHISTLING WAS HE ARD. A FURTHER SPEED REDUCTION AND DECENT WAS INITIATED AND UPON LANDING, IT WAS DISCOVERED THAT A PORTION OF THE OUTER WINDSHIELD HAD SEPARATED THE AIRCRAFT. IT IS UNKNOWN WHEN THE FIRST CRACK OCCURRED AS THE FLIGHT WAS AT NIGHT AND THE CR ACK WAS NOT GLARINGLY NOTICED. THE PILOT'S WINDSHIELD WAS REPLACED BY MAINTENANCE AND A OPERATIONAL CHECK FLIGHT WAS PER FORMED WITH NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2008010800366 20080108 00366 CE 2008 1 8 LW29212112007 1 20071211 A 2120 UNKNOWN BEECH 90 E90 1152914 CE PWA PT6 PT6A28 EA CABIN ODOR E QMLA I A CABIN DEPRESSURIZATION UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 92DV LW292 DEPARTED, UPON REACHING 7500 FEET SMELLED BURNING OIL FUMES IN CABIN. CLOSED BLEED AIR'S, TURNED OFF ENVIRONMENTAL SYSTE MS AND DUMPED CABIN. SAFELY RETURNED TO DEPARTURE. MAINTENANCE CHECKED AIRCRAFT AND ENGINE PNEUMATIC LINES, INSPECTED T HE PRESSURIZATION SYSTEM, AND CHECKED COMPRESSOR. SUSPECTED SLIGHT OIL LEAK IN COMPRESSOR. ON MAINTENANCE OPERATIONAL CHECK FLIGHT, DUPLICATED IT MOMENTARILY, THEN DISAPPEARED. 1 L 7 2 3T 4 T 3A20 E4EA 2008010800380 20080108 00380 2008 1 8 AMTA200700671 4 20071202 A 3140 6227999003 INDICATOR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT MALFUNCTIONED A AMTA K NONE N FALSE WARNING CR CRUISE 1 GL 11 518AT 22659 22659 27974 LOWER EICAS GOES BLANK INTERMITTENTLY. FAULT REMAINS ON ALTERNATE COMPUTER. REMOVED AND REPLACED LOWER EICAS IAW MM 31 -41-01-4. OPS CHECK NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010800382 20080108 00382 2008 1 8 AMTA200700673 4 20071204 A 2310 9640453011 ANTENNA BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE HF COMM DEFECTIVE A AMTA K NONE L NO TEST CR CRUISE 1 GL 11 560TZ 33525 RT HF RADIO WILL NOT TRANSMIT CORRECTLY. AUTO TUNE ON EVERY TRANSMISSION. PERFORMED HF COM SYS BITE PROCEDURE IAW FIN 23-11-00 ER. REMOVED AND REPLACED HF COM ANTENNA IAW AMM 23-11-01-4 SYS OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010800383 20080108 00383 2008 1 8 AMTA200700674 4 20071204 A 2310 9640453011 COUPLER BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE HF COMM UNSERVICEABLE A AMTA K NONE L NO TEST CR CRUISE 1 GL 11 560TZ 33525 LT HF RADIO WILL NOT AUTO-TUNE UNLESS MIC IS CONTINUOUSLY HELD IN. PERFORMED HF COMMUNICATION SYS BITE PROCEDURE IAW FI M 23-11-00. FOUND COUPLER FAIL LIGHT. REMOVED AND REPLACED LT HF COUPLER IAW AMM 23-11-01-4. OPS CHECK OK. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010800384 20080108 00384 SO 2008 1 8 FFS2007F00001 1 20071204 A 2140 94E563 MOTOR JANITROL PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA FWD HEATER FAILED A FFSA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 AL 01 4501B 942 AO6120022 318052168 THE (HEATER FAIL) ANNUNCIATOR ILLUMINATED FOLLOWED BY AN OVERHEAT OR BURNING SMELL IN THE COCKPIT WHILE IN FLIGHT. RETU RNED TO DEPARTURE FOR AN UNSCHEDULED LANDING. MAINTENANCE FOUND THE INSULATION ON THE WIRES ON THE HEATER MOTOR HAD OVE RHEATED AND WERE HARD AND CRUMBLY. THERE WAS NO EVIDENCE OF THE WIRES SHORTING TO GROUND, HOWEVER SUSPECT FAILURE OF TH E NOISE FILTER OR MOTOR ITSELF. POWER AND GROUND WIRES FOR THE MOTOR OVERHEATED. (K) 1 L 7 2 3O 3 O A20SO E14EA 2008010800390 20080108 00390 CE 2008 1 8 DJFA2007142 1 20071213 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZ STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 741TA 481 375 RK201 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER IB RIB AND BRACKET ASSEMBLIES, THE RT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE O UTLINED IN COMMUNIQUE' NR 70. MAINT REPLACED THE RIB ASSEMBLY. 2 H 7 2 4F 4 F RT A16SW E25EA 2008010800392 20080108 00392 CE 2008 1 8 DJFA2007144 1 20071213 A 2150 22054903 ACM RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP A/C BAY SEIZED E DJFA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 23 830LX 7683 258483 ON TAXI AFTER LANDING APU GENERATED SMOKE IN THE CABIN; SWITCHING BLEED AIR OFF REDUCED THE SMOKE. MAINTENANCE DISCOVER ED THE ACM FROZEN AND A DUCT OVERHEATED TO THE POINT OF DISTORTION AND MELTING. MAINTENANCE REPLACED THE ACM. 2 L 7 2 4F 4 F RT A3EU E6WE 2008010900001 20080109 00001 EU 2008 1 9 2007UALA05174 1 20071219 A 5320 DRAIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DEFECTIVE A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 463UA 1282 FLIGHT DIVERTED DUE TO LOUD SQUEAL IN COCKPIT. PRESSURIZED A/C TO 5.7 PSI NO LEAKS, NO SQUEAL DUPLICATED. REPLACED THE FWD LOWER DRAIN. NO REPEATS SINCE ORIGINAL WRITE UP. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010900003 20080109 00003 EU 2008 1 9 2007UALA05200 1 20071221 A 2133 VFT210 VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN PRESSURE INTERMITTENT A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 415UA 475 RTFL DUE TO A VENT SCAN VALVE FAULT. TECHS WERE NOT ABLE TO DUPLICATE SKIN FAULT ONCE AIRCRAFT LANDED. CAUSE UNKNOWN. ACCOMPLISHED TEST OF AEVC SYSTEM - ALL NORMAL. REPLACED AEVC VALVE AS PRECAUTIONARY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010900005 20080109 00005 EA 2008 1 9 SWIA200719009 1 20071008 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 743SK 10199 FOUND AT C-CHECK, RIGHT WEB AT STA 280 IS CORRODED. REPLACED CORRODED WEB AT STA 280 IAW CRJ700 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008010900007 20080109 00007 EA 2008 1 9 SWIA200719011 1 20071227 A 3350 BULB CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 802SK 15061 FLT 1991 - OVERHEAD EMERGENCY LIGHT IS INOP. REPLACED BULB WITH A SERVICEABLE UNIT IAW MM 33-51-00. 2 L 7 2 4F RT A21EA 2008010900012 20080109 00012 NM 2008 1 9 2007UALA05208 1 20071221 A 5330 STRUCTURE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 837UA 1474 DENT FOUND RUNNING IN A VERTICAL DIRECTION APPROX 3 FT FWD OF DOOR 2L. MAJOR REPAIR ACCOMPLISHED AT DEN. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010900014 20080109 00014 EA 2008 1 9 HNAA0800002 1 20071230 A 3097 WIRE DHAV DHC8 DHC8311 1386006 EA WINDSCREEN BROKEN A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 EA 07 326EX 25964 7038 234 BURNING ODOR ON FINAL APPROACH IN COCKPIT, SELECTED WINDSHIELD HEAT TO WARM AND ODOR DISSIPATED, NO OTHER ABNORMAL INDIC ATIONS. REPAIRED BROKEN WIRE "A" AT CAPTAINS WINDSCREEN AND REPLACED CAPTAINS WINDSHIELD HEAT CONTROLLER, OPERATIONAL C HECK GOOD. 2 H 7 2 4T RT A13NM 2008010900015 20080109 00015 EU 2008 1 9 MALA070203 1 20071228 A 2613 OVERHEAT SENSOR SAAB SF340 340B 7860101 EU RT ENGINE MALFUNCTIONED A MALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 15 436XJ 340B436 CREW INITIATED A LOW ENERGY ABORT AFTER BOTH LEFT AND RIGHT TAIL PIPE HOT LIGHTS ILLUMINATED ON TAKEOFF. RESEALED LT AN D RT TAIL PIPE HOT SENSORS AND HARNESS, OPS CHECK PER SAAB JC 2610-302. 2 L 7 2 4T RT A52EU 2008010900018 20080109 00018 2008 1 9 2007UALA05220 4 20071222 A 2565 65C318434 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 402UA 439 PER EMER LIGHT CK ON 3SVC, LEFT AFT DOOR SLIDE FAILED TEST. ELECTRICAL FAULT IN SLIDE 2L. REPLACED SLIDE 2L- OPS CHECK ED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010900020 20080109 00020 EU 2008 1 9 2007UALA05223 1 20071223 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 427UA 512 CREW OXYGEN SYSTEM - LOW. RECORD PRESSURE PRIOR TO SERVICING. SERVICED CREW O2 SYSTEM TO PROPER OPERATING PRESSURE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010900030 20080109 00030 NM 2008 1 9 2007UALA05283 1 20071224 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 532UA 25072 L4 DOOR HANDLE BOX CRACKED. REMOVED & REPLACED DOOR 4L HANDLE BOX. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010900031 20080109 00031 2008 1 9 2007UALA05300 4 20071226 A 2565 D31591478U1 SLIDE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 934UA 26662 SLIDE PACK DOOR 1L HAS FALLEN OUT OF POUCH. SUSPECT SLIDE IMPROPERLY INSTALLED. REPLACED SLIDE 1L PER MM25-61-35. AC O K FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010900033 20080109 00033 NM 2008 1 9 2007UALA05304 1 20071226 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L3 DOOR DIRTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 576UA 26690 CREW REPORT: DOOR 3L WILL NOT DISARM. FOUND DIRT ACCUMULATION UNDER GIRT BAR. CLEANED AREA UNDER GIRT BAR, OPS NORMA LLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010900034 20080109 00034 NM 2008 1 9 2007UALA05305 1 20071226 A 5720 WEB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 LEFT WING FIXED LEADING EDGE FORWARD WEB CRACK LOWER AREA AT STA 654. MAJOR REPAIR ACCOMPLISHED: STOP DRILLED CRACK. FABRICATED & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010900039 20080109 00039 NM 2008 1 9 2007UALA05308 1 20071227 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 SEAT 2J FWD EEL INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010900061 20080109 00061 WP 2008 1 9 AALA20072465 1 20071217 A 3222 STRUT DOUG DC9 DC983 3022083 WP NLG DISCHARGED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 9407R 49400 SJC INFLIGHT T1174/17DEC - NOSE LANDING GEAR UNSAFE INDICATION. ABNORMAL LOUD NOISE IN COCKPIT. NOSE GEAR DID NOT RET RACT. RETURNED TO SJC AND LANDED WITHOUT INCIDENT. FOUND NOSE LANDING GEAR STRUT SHOCK CYLINDER FLAT. REPACKED NOSE L ANDING GEAR STRUT AND SERVICED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008010900062 20080109 00062 NM 2008 1 9 AALA20072468 1 20071218 A 3350 D71702030 CHARGER BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 955AN 29540 ATL - EMERGENCY LIGHTS IN FIRST CLASS AND FORWARD GALLEY INOPERATIVE. REPLACED CHARGER FOR EMERGENCY LIGHTS IN FIRST CL ASS AND FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008010900063 20080109 00063 WP 2008 1 9 AALA20072463 1 20071217 A 3222 SEAL DOUG DC9 DC982 3022082 WP NLG STRUT INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 423AA 49335 ORD INFLIGHT T876/17DEC - NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO ORD AND LANDED WITHOUT INCIDEN T. REPLACED NOSE GEAR SHOCK STRUT SEAL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008010900065 20080109 00065 WP 2008 1 9 AALA20072470 1 20071218 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 455AA 49560 LGA - EMERGENCY FLASHLIGHT AT AFT RIGHT FLIGHT ATTENDANT SEAT HAS BROKEN STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT RIGHT FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008010900067 20080109 00067 WP 2008 1 9 AALA20072475 1 20071218 A 2612 ELECTRONIC UNIT DOUG DC9 DC983 3022083 WP CARGO FIRE SHORTED A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 9618A 53565 LAX INFLIGHT T1943/18DEC - RECEIVED AFT CARGO FIRE INDICATION. DISCHARGED FIRE BOTTLE AND AIR INTERRUPTED TO BFL. LAND ED WITHOUT INCIDENT. NO SIGN OF FIRE IN CARGO AREA. FOUND CARGO ELECTRONIC UNIT WET AND DRIPPING WATER AND SHORTING. CHECKED FOR WATER LEAK AND REPLACED CARGO ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008010900068 20080109 00068 WP 2008 1 9 AALA20072479 1 20071219 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 486AA 49679 LGA - EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS CABI N. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008010900069 20080109 00069 WP 2008 1 9 AALA20072480 1 20071219 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7533A 49987 SFO - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 12 TO 16 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHE AD SEAT ROWS 12 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008010900071 20080109 00071 WP 2008 1 9 AALA20072477 1 20071219 A 2913 PUMP DOUG DC9 DC982 3022082 WP RT HYD SYSTEM INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 412AA 49323 SAN INFLIGHT T1429/19DEC - LOST RIGHT HYDRAULIC SYSTEM FLUID. INDICATION SHOWED FLUID LOSS BUT NO PRESSURE LOSS. LOWER ED LANDING GEAR MANUALLY. LANDED SAN WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE DRIVEN PUMP AND FILTERS AND REPLACED ELECTRONIC DRIVEN AUXILIARY PUMP AND RIGHT SYSTEM RETURN LINE FILTERS. SERVICED HYDRAULIC QUANTITY TO FULL. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008010900074 20080109 00074 NM 2008 1 9 AALA20072478 1 20071219 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 640A 24598 DFW - EMERGENCY BULL NOSE LIGHT AT FORWARD LEFT INOPERATIVE. REPLACED LAMPS FOR EMERGENCY BULL NOSE LIGHT AT FORWARD LE FT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008010900077 20080109 00077 WP 2008 1 9 AALA20072467 1 20071218 A 3397 WIRE HARNESS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 575AM 53152 JFK - EMERGENCY LIGHTS AT SEAT ROWS 3DEF TO 20DEF INOPERATIVE. REPAIRED HARNESS AT SEAT ROWS 19DEF AND 20DEF. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008010900079 20080109 00079 NE 2008 1 9 QXEA200702041 2 20071230 A 7320 4120T00P37 FADEC CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE RT ENGINE MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 611QX 3850 10041 SEA - FLIGHT 2583 - RIGHT ENGINE DEGRADE CAUTION MESSAGE WHEN TAKING THE RUNWAY. RETURNED TO THE GATE. MAINTENANCE REP LACED THE NR 2 FADEC. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008010900080 20080109 00080 2008 1 9 QXEA200702043 2 20071230 A 7200 3038400 ENGINE DHAV DHC8 DHC8202 2809007 NM NR 2 MALFUNCTIONED A QXEA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 09 349PH 486 MFR - FLIGHT 2150 - SHORTLY AFTER TAKEOFF, THE LAV SMOKE DETECTOR WENT OFF. THE FLIGHT ATTENDANT CHECKED AND SAW NO SMO KE, BUT DID SMELL A HOT DUSTY SMELL. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. AIRCRAFT FERRIED TO PDX FOR REPAIRS. IN PDX, MAINTENANCE REPLACED THE NR 2 ENGINE AFTER FINDING OIL ON THE HP IMPELLER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008010900083 20080109 00083 NM 2008 1 9 QXEA200702039 1 20071230 A 2750 C1486742003 CONTROL UNIT BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 409QX 13063 9074 4051 GEG - FLAP POWER CAUTION LIGHT ILLUMINATED AFTER FLAPS SELECTED UP AFTER TAKEOFF. AFTER DOING CHECKLIST, CAUTION LIGHT STAYED ON. DIVERTED TO GEG AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE FLAP CONTROL UNIT. OPERATI ONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008010900085 20080109 00085 2008 1 9 MALA070204 4 20071228 A 3432 1951 ANTENNA SAAB SF340 340B 7860101 EU GLIDE SLOPE MALFUNCTIONED A MALA L ABORTED APPROACH O OTHER AP APPROACH 1 GL 15 415XJ 340B415 ON ILS APPROACH TO DTW, APPROACH MODE ARMED AT 4000 FT, SHOWING HIGH ON SLOPE. AUTO PILOT ON. UNCOMMANDED DESCENT TO 4 000 FPM NOTED. AP OFF. AP REMAINED OFF FOR REMAINDER OF FLIGHT. UPON UNCOMMANDED DESCENT, AVIONICS LIGHT NOTED. YELL OW GS NOTED EADI. SLOPE INDICATIONS ERRATIC. AP DISCONNECTED. REMAINED OFF. OPEN CIRCUIT IN GS ANTENNA. REMOVED AND REPLACED GLIDESLOPE ANTENNA IAW SF340 MM CH. 34-30-10. VOR LOCALIZER AND GLIDESLOPE CHECKS GOOD IAW SF340 MM CH 34-30- 00, 34-51-00. 2 L 7 2 4T RT A52EU 2008010900086 20080109 00086 EA 2008 1 9 SWIA200719012 1 20070919 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 607SK 10251 FOUND AT C-CHECK, PAX DOOR INTERNAL HANDLE IS CRACKED. REPLACED INNER PAX DOOR HANDLE PER CRJ700 AMM 52-11-02-400-809-A 04. 2 L 7 2 4F RT A21EA 2008010900089 20080109 00089 EA 2008 1 9 SWIA200719015 1 20071229 A 3222 STRUT CNDAIR CL600 CL6002C10 1390015 EA NLG LOW A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 716SK 10180 FLT 6383 - GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF. SERVICED NOSE STRUT IAW CRJ MM 700-12-12-32. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008010900092 20080109 00092 EA 2008 1 9 SWIA200719018 1 20071231 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS UNSECURE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 935SW 7725 FLT 5914 - LEFT OVERWING FLOOR EMERGENCY LIGHT IS INOP. SECURED WIRE TERMINAL. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008010900094 20080109 00094 SO 2008 1 9 SWIA200719020 1 20071230 A 2720 ACTUATOR EMB 120 EMB120ER 3260203 SO RUDDER MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 289YV 120289 FLT 5436 - UNABLE TO DEPRESS RIGHT RUDDER PEDAL ON TAKEOFF. REPLACED BLUE ACTUATOR WITH A SERVICEABLE UNIT. OPS CHECKS GOOD. NO LEAKS NOTED, PN: 308190-1003, SN OFF: 0614. 2 L 7 2 4T RT A31SO 2008010900097 20080109 00097 EA 2008 1 9 SWIA200719023 1 20071231 A 3310 SOCKET CNDAIR CL600 CL6002C10 1390015 EA COCKPIT LIGHT SHORTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 752SK 10209 FLT 6778 - FIRST OFFICERS YOKE MAP LIGHT IS INOP. SECURED CHART HOLDER HARDWARE. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008010900100 20080109 00100 EA 2008 1 9 MASA200700763 1 20071031 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75992 7401 ASH RON DSM - NR 1 CEILING EMERGENCY FLOODLIGHT INOPERATIVE. MX RELAMPED AND OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2008010900103 20080109 00103 EA 2008 1 9 MASA200700728 1 20071023 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37178 7178 ASH FLT 2818 DSM - NR 7 EXTERIOR EMERGENCY EXIT LIGHT INOP. CONTRACT MX RELAMPED, OPS NORMAL. 2 L 7 2 4F RT A21EA 2008010900104 20080109 00104 EA 2008 1 9 MASA200700751 1 20071028 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 75984 7489 ENGINE SUPPORT BEAM RT LWR WEB CRACKED AT FWD INBD CORNER OF ACCESS PNL CUTOUT. PERFORMED PERM REPAIR. 2 L 7 2 4F RT A21EA 2008010900105 20080109 00105 EA 2008 1 9 MASA200700780 1 20071107 A 5210 LANYARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF POSITION A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 571ML 7209 ASH FLT 7197 - PAX DOOR WILL NOT OPEN ALL THE WAY. MX REPOSITIONED PAX DOOR HANDRAIL LANYARD. 2 L 7 2 4F RT A21EA 2008010900106 20080109 00106 EA 2008 1 9 MASA200700903 1 20071219 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM INOPERATIVE A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 571ML 16317 7209 ASH FLT 7000 - AFTER TAKEOFF, THE GEAR FAILED TO RETRACT. THE CREW WAS ABLE TO GET THE GEAR DOWN CONVENTIONALLY, BUT D ECLARED AN EMERGENCY. REMOVED AND REPLACED 3A HYDRAULIC PUMP. 2 L 7 2 4F RT A21EA 2008010900107 20080109 00107 EA 2008 1 9 MASA200700925 1 20071229 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77331 6936 7331 ASH 7300 GSP - IAD - EMERGENCY PATH LIGHTING INOP AT ROWS 2-5. MX REPLACED THE NR 2 BATTERY AND CHARGER. 2 L 7 2 4F RT A21EA 2008010900108 20080109 00108 NM 2008 1 9 2007UALA05311 1 20071227 A 3020 8105037 ANTI-ICE VALVE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LT ENGINE INOPERATIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 794UA 26953 LEFT ENGINE ANTI ICE INOP IN THE CLOSED POSITION. INDICATION-LEFT ENGINE ANTI ICE INOP. VALVE STUCK IN THE CLOSED POSIT ION. REPLACED CONTROLLER ASSY. OPS GOOD. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008010800041 20080108 00041 EU 2008 1 8 07FDEA05137 1 20071224 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS STRINGER REPAIR LOCATED IN BULK CARGO ON STRINGER 53 LT BETWEEN FRAMES 68 TO 70, HAS 1 EACH REPAIR SECTION ME ASURING 13.2" LONG AND 2 EACH REPAIR SPLICES MEASURING 8" LONG. PREVIOUSLY INSTALLED REPAIR LOCATED AT BULK CARGO ON ST RINGER 53 LT BETWEEN FRAMES 68 TO 70 WAS DETERMINED NOT TO BE IAW A310 SRM 53-10-14 FIG 201, DUE TO INCORRECT MATERIAL T HICKNESS OF REPAIR SPLICES INSTALLED, BASED ON A VISUAL EVALUATION WITH THE REPAIR INSTALLED. REMOVED 2 EACH REPAIR SPL ICES AND REPAIRED PER A310 SRM 53-10-14 FIG 201. THIS IS A REPAIR WITH NO AIRBUS ISSUED PART NUMBER, REPAIR IDENTIFIED BY THE AGING AIRCRAFT INSPECTION PROGRAM. 2 L 7 2 4F RT A35EU 2008010800050 20080108 00050 EU 2008 1 8 YENA2007102 1 20071119 A 2121 EVT3454H FAN AIRBUS 320 A320232 3930326 EU CABIN BURNED OUT A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 556JB 22238 13563 1904 FLT NR 411, BOS-SAN, APPROX BETWEEN 12:00Z-15:00Z, LOUD NOISE AND STRANGE/ELECTRICAL ODOR FOLLOWED BY BLOWER FAN FAULT, RAN ECAM SET BLOWER TO OVRD-SOUND AND ODOR CEASED. REMOVED AND REPLACED BLOWER FAN, NO MESSAGES REMAINED, OPS CHECK OK. 2 L 7 2 4F RT A28NM 2008010800052 20080108 00052 2008 1 8 07FDEA05106 2 20071220 A 7510 32138684 ANTI-ICE VALVE AIRBUS 310 A310222 3930315 EU NR 1 ENGINE MALFUNCTIONED A FDEA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 25 448FE 260 AFTER TAKEOFF RECEIVED NR 1 ENGINE ADVISORY NAC TEMP AT 200 DEGREES, AT CRUISE NR 1 ENG BLEED OFF, NO CHANGE. TEMP LOW ERED TO 180 DEGREES IN CRUISE WHEN THROTTLES WERE REDUCED. REMAINED AT 180 DEGREES FOR THE DURATION OF THE FLIGHT. ALL OTHER ENGINE INDICATIONS WERE NORMAL. REPAIRED PRESSURE SENSOR TUBE PER MM 20-23-11-0. REMOVED AND REPLACED NACELLE A NTI ICE VALVE PER MM 30-21-11-4. OPS CHK NORMAL. 2 L 7 2 4F RT A35EU 2008010800054 20080108 00054 EU 2008 1 8 YENA2007121 1 20071220 A 7714 2043M31P01 SENSOR EMB ERJ190 ERJ190100IGW 3260408 EU GE CF34 CF3410E6 30023 NE NR 1 ENGINE ERRATIC A YENA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 15 279JB 1331 19000090 994310 FLT NR 439, BOS-MCO DIVERTED TO RDU DUE ENGINE 1 CONTROL FAULT, ENGINE THRUST NOT CONTROLLABLE, ENGINE SHUT DOWN. ACCOMP LISHED GE ENG EM TASK 72-00-00-810-325 FOR COMP STALL. VISUAL INSP OF ENG INTAKE AND EXHAUST. ACCOMPLISHED GE EM TASK 72 -00-00-810-315 FOR ENG N1 EXCEEDANCE FOUND OUT OF LIMITS. REMOVED AND REPLACED NR 1 ENG T 1.2 SENSOR IAW AMM 77-00-00, OPS CK NORMAL. SHORT TERM DISPATCH MSG NO LONGER PRESENT, ACCOMPLISHED LOW OIL PRESS INSP OF NR 1 ENG, NO DISCREPANCIES FOUND. REMOVED AND REPLACED NR 1 ENG OIL FILTER AND FADEC PRECAUTIONARY IAW 79-00-800-813 AND IAW 7321-01-400-801, OPE RATIONAL CHECK OF NR 1 ENG CHECK OK. 2 L 7 2 4F 4 F RT A57NM E00070EN 2008010800063 20080108 00063 EA 2008 1 8 TRAX200701968 1 20071220 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA BS 676 DENTED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 FS 676 HAS A DENT IN TOP SKIN BETWEEN STR 1 AND 2R (MARKED). 2 L 7 2 4F RT A21EA 2008010800064 20080108 00064 NM 2008 1 8 ASAA0772423 1 20071206 A 5320 149A811829 SUPPORT ANGLE BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT BS 947 LBL 8 TO RBL 21 BULKHEAD TO FLOOR SUPPORT ANGLE CORRODED. REPAIRED WITH NEW PART. 2 L 7 2 4F RT A16WE 2008010800073 20080108 00073 NM 2008 1 8 ASAA0772424 1 20071206 A 5347 146A750125 CARGO TRACK BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT BS 927+16 RBL 13.84 TIE DOWN TRACK CORRODED. TRACK REPLACED. 2 L 7 2 4F RT A16WE 2008010800077 20080108 00077 NM 2008 1 8 ASAA0772428 1 20071206 A 5320 146A94018 SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT FLOOR PANEL BUTT SPLICE TEE SUPPORT BS 727D+6 CORRODED. REPAIRED WITH NEW PART. 2 L 7 2 4F RT A16WE 2008010800080 20080108 00080 NM 2008 1 8 ASAA0772432 1 20071208 A 5320 149A810921 ATTACH ANGLE BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT VACUUM WASTE COMPARTMENT ATTACH ANGLE BS 867 LBL 10 CRACKED. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008010800082 20080108 00082 NM 2008 1 8 ASAA0772436 1 20071205 A 5320 143A75014 CHANNEL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 FWD CARGO PIT CORROSION AT RIGHT ZEE CHANNEL AT BS 500A TO 500D RBL 22. REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 53 30 53 FIG 2 53-00-53 & 51-40-05. 2 L 7 2 4F RT A16WE 2008010800088 20080108 00088 EA 2008 1 8 TRAX200701980 1 20071223 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 ASD BOTTOM STEP ASSY IS DAMAGED. 2 L 7 2 4F RT A21EA 2008010800089 20080108 00089 NM 2008 1 8 KCSA07100 1 20071222 A 2612 WARNING SYSTEM BOEING 747 7472B4B 138481B NM FIRE DETECTION MALFUNCTIONED A KCSA K NONE N FALSE WARNING CR CRUISE 1 GL 23 713CK 21099 ENGINE FIRE DETECTION NACELLE FAULT LIGHT ON F/E PANEL ILLUMINATES INTERMITTENTLY AS WELL AS FIRE DETECTION LIGHTS ON TH E P5 PANEL WITH NO FULL SCALE DETECTIONS. TESTED FIRE DETECTION SYSTEM IAW B747 MM 26-11-00. OPS CHECKS GOOD. 2 L 7 4 4F RT A20WE 2008010800095 20080108 00095 NM 2008 1 8 QXEA200702035 1 20071226 A 3010 7G773 TRANSDUCER DHAV DHC8 DHC8202 2809007 NM DE-ICE PRESSURE MALFUNCTIONED A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 350PH 488 PDX - FLIGHT 2094 - LEFT DE-ICE PRESSURE GAUGE SHOWS GREATER THEN 30 PSI. RETURNED TO THE GATE. MAINTENANCE PLACED THE SYSTEM ON MEL 30-8B. AIRCRAFT RETURNED TO SERVICE. REPLACED THE LT PRESSURE TRANSDUCER. OPERATIONAL CHECKS GOOD. AIRC RAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008010800096 20080108 00096 NM 2008 1 8 QXEA200702034 1 20071226 A 3010 4100S011 REGULATOR VALVE BOMBDR DHC8 DHC8402 1390042 NM DE-ICE SYSTEM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 407QX 16522 4049 BOI - FLIGHT 2300 - DE-ICE CAUTION LIGHT ILLUMINATED MOMENTARILY. INDICATED 30 PSI, THEN NORMAL. ALL BOOTS ON THE RIGH T SIDE STAYED INFLATED. RETURNED TO THE GATE. MAINTENANCE REPLACED THE PRESSURE REGULATOR VALVE. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008010800120 20080108 00120 NM 2008 1 8 SWAA076459 1 20071224 A 5311 65C34355 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800122 20080108 00122 NM 2008 1 8 SWAA076463 1 20071224 A 5311 6546548 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800126 20080108 00126 NM 2008 1 8 MWEA070309 1 20071227 A 5310 59107845 DOOR FRAME BOEING 717 717200 1383700 NM LT MLG WW CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 907ME 55171 LEFT WHEEL WELL DOOR OPENING FORWARD FRAME CRACKED NEAR OUTBOARD END. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2008010800127 20080108 00127 WP 2008 1 8 MWEA070310 1 20071226 A 2611 CGAB140001 SMOKE DETECTOR DOUG DC9 DC982 3022082 WP AFT LAV FALSE INDICATION A MWEA O OTHER N FALSE WARNING CR CRUISE 1 GL 13 810ME 48072 WHILE EN ROUTE, LEFT AFT LAVATORY SMOKE ALARM ACTIVATED. FLIGHT ATTENDANT REPORTED, NO SIGN OF SMOKE, NO SMELL OF SMOKE AND NO SIGNS OF TAMPERING. REMOVED AND REPLACED SMOKE DETECTOR. 2 L 7 2 4F A6WE 2008010800135 20080108 00135 NM 2008 1 8 SWAA076466 1 20071224 A 5315 65C33948 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE FLOORBEAM CRACKED AT BS 947.5, LT LOWER SIDE AT CORNER FASTENER HOLE. REP AIRED FLOORBEAM PER SWA EA & SRM. 2 L 7 2 4F RT A16WE 2008010800147 20080108 00147 EA 2008 1 8 SWIA200718995 1 20071224 A 3310 LIGHT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT SHORTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 709SK 10159 FLT 6659 - FO'S CHART HOLDER LIGHT IS INTERMITTENT. SECURED HARDWARE UNDER LIGHT ASSEMBLY. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008010800159 20080108 00159 NM 2008 1 8 SWAA076460 1 20071224 A 5311 6546534 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800178 20080108 00178 NM 2008 1 8 SWAA076484 1 20071221 A 5322 6546529 SHEAR TIE BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500D, STR 28R. REMOVED AND REPLACED SHEAR TIE PE R SRM. 2 L 7 2 4F RT A16WE 2008010800185 20080108 00185 NM 2008 1 8 SWAA076487 1 20071221 A 2121 215201 GASPER FAN BOEING 737 7377H4 1384404 NM E&E BAY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 29 727SW 27859 ELECTRICAL SMELL IN CABIN, NO SMOKE PRESENT. GASPER FAN CIRCUIT BREAKER POPPED. REMOVED AND REPLACED GASPER FAN PER MM . 2 L 7 2 4F RT A16WE 2008010800186 20080108 00186 NM 2008 1 8 SWAA076488 1 20071223 A 3350 D1701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 746SW 29798 DURING SCHEDULED HC1 CHECK, FWD LEFT CABIN EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BAT TERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008010800190 20080108 00190 EU 2008 1 8 07FDEA05141 1 20071227 A 2840 SIC50774 COMPUTER AIRBUS 300 A300B4622 3930401 EU UNKNOWN A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 719FD 388 AT FL/340 GOT ECAM FUEL ADVISORY FOR 8000 LBS IMBALANCE. LEFT INNER TANK DECREASING SLOWLY THROUGH 2000 LBS IAW QRH, PULLED AND RESET FQI CHAN 1 AND 2 C/B, NO HELP. ALL COCKPIT INDICATIONS: QTY, FUEL USED, MANUAL FUEL CALCULATIONS INDIC ATED LOSS OF 8-10,000 LBS OF FUEL. DIVERTED TO KMCI. PERFORMED A VISUAL CHK FOR EVIDENCE OF FUEL LEAK AND NONE FOUND. ALL FUEL INDICATIONS AND STICK READINGS AGREE. FQIS BITE SHOW NO HARD CODE. FUELED LT INNER TANK TO A KNOWN QTY USING STICK READING OF 67, OR 10.600 LBS. APPLIED MEL 28-42-01-04. 2 L 7 2 4F RT A35EU 2008010800192 20080108 00192 NM 2008 1 8 07FDEA05143 1 20071227 A 5753 SKIN BOEING 727 727233 138408A NM ZONE 600 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 RIGHT WING INBOARD MID FLAP UPPER SURFACE, SKIN GOUGED AT OUTBOARD SIDE. BLENDED DAMAGED AREA, NDT VERIFIED NO DEFECTS. TREATED, PRIMED AND TEFLON PAINTED, REF SRM 57-50-1, SRM 51-10-2, MM 51-20-017-7 AND EA NR 7-5750-113963 THIS IS CLASS IFIED AS A MINOR. 2 L 7 3 4F RT A3WE 2008010800205 20080108 00205 NM 2008 1 8 USAA920071381 1 20071226 A 5753 6546431279 SKIN BOEING 737 7374B7 1384702 NM T/E FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - C3 CHECK - LEFT WING OUTBOARD FORE FLAP LOWER SURFACE HAS AREA OF DELAMINATION. REPLACED LEFT WING OUTBOARD FORE FLAP IAW B737 AMM 27-51-37. 2 L 7 2 4F RT A16WE 2008010800209 20080108 00209 EU 2008 1 8 USAA920071385 1 20071210 A 5320 D53480043203 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 649AW 803 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON THE R2 DOOR CUTOUT LOWER SILL, BS 3101 / FR 65, -Y1730. REPAIRED THE R2 DO OR CUTOUT LOWER SILL, BS 3101 / FR 65, -Y1730 IAW A320 SRM 53-41-14. 2 L 7 2 4F RT A28NM 2008010800210 20080108 00210 EU 2008 1 8 USAA920071386 1 20071213 A 5554 D5537131800200 HINGE FITTING AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 649AW 803 SAL - MAJOR REPAIR - C7 CHECK - NR 3 RUDDER HINGE FITTING IS LOOSE, VERTICAL STABILIZER STATION 2279 / RIB 5. REPLACED NR 3 RUDDER HINGE FITTING, VERTICAL STABILIZER STATION 2279 / RIB 5 IAW A320 AMM 55-36-41. 2 L 7 2 4F RT A28NM 2008010800215 20080108 00215 NM 2008 1 8 SWAA076494 1 20071227 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 24L CORRODED BETWEEN BS 851 AND BS 867. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008010800230 20080108 00230 NM 2008 1 8 SWAA076501 1 20071227 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800231 20080108 00231 EU 2008 1 8 MALA070197 1 20071226 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 749-765 DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 411XJ 340B411 AT SCE AIRCRAFT SUSTAINED LT FUSELAGE DAMAGE STA 749-765.85 AND UP 14" FROM THE SKIN PANEL EDGE AT SL 1520. FRAME STA 7 58.15 WAS SEVERELY DAMAGED AND FRAME STA 765.85 HAD MINOR DAMAGE. ACCOMPLISHED A TEMPORARY REPAIR IAW EOS53514 IN ORDER TO FERRY A/C TO WORTHINGTON AT MSP. PERMANENT REPAIR WAS ACCOMPLISHED IAW EOS53515 AND SAAB REPAIR STATEMENT 340SDS013 790 REV A DATED 12-19-2007. 2 L 7 2 4T RT A52EU 2008010800233 20080108 00233 2008 1 8 SWAA076502 4 20071227 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM EVAC SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM. 2 L 7 2 4F RT A16WE 2008010800234 20080108 00234 NM 2008 1 8 HALA0700560 1 20071227 A 3350 LAMP BOEING 767 767332 1382001 NM EMERGENCY LIGHTS INOPERATIVE A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 RT AFT OVERWING EMERGENCY LIGHT INOP. RELAMPED RT AFT OVERWING EXTERIOR EMERGENCY LIGHT. CHECKS OK. 2 L 7 2 4F RT A1NM 2008010800236 20080108 00236 NM 2008 1 8 SWAA076504 1 20071227 A 5512 65C25727 SKIN BOEING 737 7373H4 1384600 NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED 22Y CHECK, FOUND LT HORIZONTAL STABILIZER UPPER SKIN OUTBOARD SURFACE CORRODED. REPAIRED STABILIZER PE R SRM. 2 L 7 2 4F RT A16WE 2008010800240 20080108 00240 NM 2008 1 8 HALA0700558 1 20071227 A 2697 CONNECTOR BOEING 767 7673G5 1385126 NM SMOKE DETECTOR LOOSE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 586HA 24259 LAV H SMOKE DETECTOR APPEARS INOP. SECURED LOOSE CONNECTOR AND OPS CKD OK PER AMM 26-13-00-735-034. 2 L 7 2 4F RT A1NM 2008010800254 20080108 00254 NM 2008 1 8 SWAA076510 1 20071227 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 437WN 29832 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 7 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008010800255 20080108 00255 EA 2008 1 8 QXEA200702033 1 20071227 A 3297 4910313 WIRE HARNESS CNDAIR CL600 CL6002C10 1390015 EA WOW MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 606QX 9333 10023 PDX - FLIGHT 2612, RECEIVED A BRAKE OVERTEMP WARNING AFTER TAKEOFF. RETURNED TO THE FIELD. CFR CALLED AND ACCOMPLISHED A UNEVENTFUL LANDING. AIRCRAFT CURRENTLY OUT OF SERVICE FOR REPAIRS. MAINTENANCE REPLACED THE RIGHT MAIN GEAR OUTBOAR D WOW HARNESS. OPERATIONAL CHECKS GOOD AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008010800256 20080108 00256 NM 2008 1 8 SWAA076509 1 20071227 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 437WN 29832 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 3 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008010800264 20080108 00264 EU 2008 1 8 SIMA200736201 1 20071226 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT MALFUNCTIONED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 324AE 340B324 ON FLIGHT 3264, EMERGENCY EXIT SIGN ABOVE MAIN PAX DOOR AND EMERGENCY EXIT SIGN ABOVE FLIGHT ATTENDANT JUMP SEAT WILL NO T STAY ILLUMINATED AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY PACK AT LOC 20N1 IAW AMM 33-50-10 OPS C HECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2008010800266 20080108 00266 SO 2008 1 8 CHQA200700102 1 20071230 A 3297 CONNECTOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL PROX SWITCH LOOSE A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 266SK 145241 CAE311208 DFW TO IAH - ON TAKEOFF, THE CREW RECEIVED A "LG AIR/GND FAIL" MESSAGE AND THE LANDING GEAR WOULD NOT RETRACT. THE AIRC RAFT LANDED BACK AT DFW WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE CMC AND FOUND A MESSAGE FOR A PROX SWITCH FAIL. AFTER INSPECTING THE PROX SWITCHES, A CONNECTOR WAS FOUND LOOSE. AFTER TIGHTENING THE LOOSE CONNECTOR AND RESETTING TH E AIRCRAFT'S POWER, THE AIR/GROUND MESSAGE DISAPPEARED AND DID NOT RETURN. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008010800274 20080108 00274 NM 2008 1 8 07FDEA05156 1 20071229 A 5753 HINGE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 592FE 48550 RIGHT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING SUPPORT FITTING HOLE FOUND WITH CORROSION. REMOVED AND REPLACED AS PER AMM 27-50-30-4. OUTBOARD FLAP ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-00-5. REPAIR CLASSIFIED AS MINOR PE R GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008010800277 20080108 00277 NM 2008 1 8 07FDEA05159 1 20071229 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 592FE 48550 RIGHT WING, LEADING EDGE STRINGER FOUND CRACK AT XOS 1015. REPAIRED AS PER FEDEX E.A. 1- 5720-117239, REPAIR CLASSIFIE D AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008010800279 20080108 00279 NM 2008 1 8 07FDEA05161 1 20071231 A 5753 SUPPORT DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 592FE 48550 RIGHT WING, OUTBOARD FLAP OUTBOARD HINGE AFT FAIRING SUPPORT OUTBOARD AFT FASTENER HOLE FOUND CORRODED. CORROSION REPAI RED AS PER FEDEX E.A. 1-5750-117237, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008010800281 20080108 00281 EU 2008 1 8 07FDEA05163 1 20071231 A 5315 A5327534920000 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 659FE 757 AFT CARGO COMP'T, CROSSBEAM CRACKED AT FRAME 64 BETWEEN TRACKS Y-953 AND Y- 1456. CROSSBEAM REPAIRED AT FRAME 64 BETWEE N TRACKS Y-953 AND Y-1456 IAW SRM 53-10-15, FIG 211, (SHEETS 1 AND 2). 2 L 7 2 4F RT A35EU 2008010800282 20080108 00282 2008 1 8 SWAA076519 4 20071225 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 492WN 33866 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008010800283 20080108 00283 NM 2008 1 8 SWAA076527 1 20071227 A 5311 6546550 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800284 20080108 00284 EU 2008 1 8 07FDEA05164 1 20071231 A 5347 R5307008820400 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 659FE 757 TRACK WITH CORROSION AT Y-953 AND BETWEEN FR 30 AND 31. TRACK REPAIRED IAW SRM 53-10-16 FIG 201. 2 L 7 2 4F RT A35EU 2008010800290 20080108 00290 EU 2008 1 8 07FDEA05170 1 20071231 A 5340 A5378193720100 ADAPTER AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 659FE 757 AT FR 29 AND BETWEEN TRACKS Y-450 AND Y-953 WITH CRACK. ADAPTER REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008010800294 20080108 00294 NM 2008 1 8 SWAA076523 1 20071227 A 5311 6546534 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800306 20080108 00306 NM 2008 1 8 NWAA074325808 1 20071223 A 3350 BATTERY PACK BOEING 757 757351 1384991 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 588NW 32988 PILOT REPORTED CABIN EMERGENCY LIGHTS WOULD COME ON AND GO OFF CONTINUOUSLY. MAINTENANCE REMOVED AND REPLACED 2 BATTERY PACKS AND POWER SUPPLIES. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2008010800308 20080108 00308 EU 2008 1 8 08FDEA00001 1 20071128 A 5311 A53831908203 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 659FE 757 LT MLG, L/G MAIN DOOR LEANING WITH WEB FWD CRACKED WEB OF FRAME 48. REPAIRED IAW FEDEX EA NR 6-5320-115304. 2 L 7 2 4F RT A35EU 2008010800309 20080108 00309 EU 2008 1 8 08FDEA00002 1 20071213 A 5315 A53275351200 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 659FE 757 CROSSBEAM AT FR 66 WITH DEFORMITY BETWEEN Y953 AND Y1456. CROSSBEAM AT FS 36 REPAIRED BETWEEN Y953 AND Y1456 IAW SRM 53 -10-15, FIG 205, SHEET 2. 2 L 7 2 4F RT A35EU 2008010800314 20080108 00314 2008 1 8 HALA0700566 4 20071230 A 2310 6225272001 TRANSCEIVER BOEING 767 767332 1382001 NM HF SYSTEM INOPERATIVE A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 598HA 23278 ETOPS SIGNIFICANT SYSTEM, NR 2 HF TRANSMISSIONS INOP ON ALL STATIONS. REPLACED NR 2 HF XCVR. GND CHECK OK PER MM 23-11 -03. 2 L 7 2 4F RT A1NM 2008010800331 20080108 00331 WP 2008 1 8 UPS07851353 1 20071226 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FS 921 L24L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 CRACK ON BOTTOM OF L24L STA 921. STOP DRILLED CRACK AT STA 921 L24L IAW SRM 53-02-02. AREA HAS EXIS TING REPAIR PER SRM 53-02-02-0, NO FURTHER ACTION REQUIRED. 2 L 7 4 4F RT 4A25 2008010800339 20080108 00339 EU 2008 1 8 YENA2007124 1 20071226 A 2700 3945128102 COMPUTER AIRBUS 320 A320232 3930326 EU NR 1 ELAC MALFUNCTIONED A YENA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 15 587JB 11672 2900 2177 FLT NR 802, FLL-JFK, DIVERTED TO MCO, AIRCRAFT EXPERIENCED VERY HEAVY VIBRATION 17000-28000 FEET AT VARIOUS SPEEDS 270KT S-330KTS, UNABLE ISOLATE TO VIA VIBRATION CHECK LIST. PERFORMED INSPECTION AND OPERATION CHECK OF NOSE LANDING GEAR AND DOORS. NO DISCREPANCIES NOTED. PERFORMED BACK LASH AND FREE PLAY CHECK OF ALL ELEVATORS SERVO’S. ALL WITHIN AMM LIMI TS. REPLACED ELAC NR 1 AS PRECAUTIONARY IAW 27-93-34, NO ABNORMALITIES NOTED. OPS CHECK OK. NO VIBRATIONS NOTED ON NE XT FLIGHT. 2 L 7 2 4F RT A28NM 2008010800349 20080108 00349 CE 2008 1 8 GLBA20061037 1 20071209 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE COCKPIT ODOR A GLBA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 03 219GL UE219 SMOKE/SMELL - DURING GROUND RUNS AFTER MX CHECK AND PRIOR TO ENPLANEMENT OF PASSENGERS SMOKE/SMELL WAS REPORTED IN THE C OCKPIT. SUBSEQUENT MAINTENANCE CHECKS OF SYSTEMS AND ENGINE RUNS DID NOT PRODUCE ANY RESULTS. MAINTENANCE COULD NOT DUPL ICATE REPORT. 2 L 7 2 4T 4 T RT A24CE E26NE 2008010800363 20080108 00363 CE 2008 1 8 GLBA20061031 1 20071203 A 5311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FUSELAGE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 254GL UE254 FRAME CRACKED AT F.S. 164.4 AND STRINGER 9R. CRACK APPROXIMATELY .750 INCH IN LENGTH. MAINTENANCE REPAIRED FRAME CRACK A T F.S. 164.4 AND STRINGER 9R IAW SRM 51-70. REPAIR APPROXIMATELY 5.5 BY 2.5 INCHES. 2024-T3 .O71 INCHES RII INSPECTION COMPLIED IAW GLA TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2008010900004 20080109 00004 EU 2008 1 9 2007UALA05203 1 20071220 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 463UA 1282 OXYGEN HIGH PRESSURE INDICATION AMBER ON DOOR-OXY SYSTEM ECAM. SERVICED CREW O2 SYSTEM, NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010900008 20080109 00008 WP 2008 1 9 ARWA20071206 1 20071229 A 2910 O-RING DOUG DC10 DC1030F 3023504 WP HYD SYSTEM LEAKING A ARWA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 450ML 47831 LOST HYDRAULIC QUANTITY BELOW 6 GALLONS SYSTEM 3; HYDRAULIC SYSTEM 3 ELEVATOR OFF LIGHT "ON". REMOVED AND REPLACED "O" RING AT LOWER FITTING OF REVERSIBLE MOTOR PUMP SHUTOFF VALVE NR 1-3 IN ACCORDANCE WITH M/M 29-22-01; OPERATIONAL CHECK A ND LEAK CHECKED IN ACCORDANCE WITH M/M 29-22-01 AND FOUND NORMAL, NO LEAKS NOTED. SERVICED NR 3 HYDRAULIC SYSTEM AS NEE DED IN ACCORDANCE WITH M/M 12-13-02. 2 L 7 3 4F RT A22WE 2008010900013 20080109 00013 NM 2008 1 9 HNAA0800001 1 20071221 A 2530 180140 HOT WATER POT DHAV DHC8 DHC8102 2809003 NM GALLEY BURNED A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 825EX 32674 32674 388 BURNING ODOR COMING FROM F/A HANDSET. AFTER INSPECTION, IT WAS DETERMINED THE ODOR TO BE COMING FROM NR 1 HOT WATER BOT TLE RECEPTACLE. REMOVED AND REPLACED RECEPTACLE AND WIRING RING TERMINALS. WIRING FOUND TO BE IN GOOD CONDITION. 2 H 7 2 4T RT A13NM 2008010900025 20080109 00025 SO 2008 1 9 SIMA200800301 1 20071231 A 3350 11004920101A POWER SUPPLY EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHTS INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 816AE 145552 MAINTENANCE FOUND BOTH EMERGENCY EXIT OVERWING LIGHTS ARE INOP. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED PO WER SUPPLY AND BATTERY IAW AMM 33-50-04. OPERATIONAL CHECK GOOD IAW AMM 33-50-00 AFTER BATTERIES CHARGED. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008010900026 20080109 00026 EU 2008 1 9 2007UALA05240 1 20071224 A 3260 ABS012110 PROXIMITY SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LANDING GEAR FAULTY A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 456UA 1128 FLIGHT DIVERTED DUE TO MULTIPLE ECAM MESSAGES. INDICATION FAILURE. REPLACED PROX SENSOR 23GA, ALL SYSTEMS FUNCTION NOR MALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010900032 20080109 00032 2008 1 9 2007UALA05302 4 20071226 A 2565 O-RING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L1 DOOR SLIDE LEAKING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 DOOR 1L SLIDE BOTTLE PRESSURE READS LOW. FOUND FAULTY O-RING AT GAUGE ELBOW. REPLACED SLIDE ASSEMBLY IAW 25-65-01. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010900035 20080109 00035 NM 2008 1 9 2007UALA05306 1 20071226 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 670UA 29240 EXIT ROW LIGHT AT 21B IS LOOSE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010900038 20080109 00038 NM 2008 1 9 2007UALA05307 1 20071226 A 2520 SWITCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SEAT BURNED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 661UA 27158 FOUND LUMBAR SWITCH AT SEAT 8E BURNED AND MELTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010900043 20080109 00043 NM 2008 1 9 2007UALA05309 1 20071227 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EEL'S INOP AT CEILING AREAS, GALLEY G1 LH & DOOR 2L. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010900066 20080109 00066 NM 2008 1 9 AALA20072466 1 20071217 A 2913 PUMP BOEING 767 767323 1385205 NM HYD SYSTEM INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 366AA 25193 LHR INFLIGHT T83/17DEC FRA TO ORD - LEFT HYDRAULIC QUANTITY INDICATION AND LOSS OF LEFT HYDRAULIC PUMP DURING CRUISE. D IVERTED TO LHR AND LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE PRIMARY HYDRAULIC PUMP. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008010900070 20080109 00070 NM 2008 1 9 AALA20072476 1 20071219 A 3397 WIRE BOEING 767 767223 1385123 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 325AA 22326 JFK - EMERGENCY LIGHT AT FIRST CLASS CLOSET HAS LOOSE WIRING. REPOSITIONED WIRING FOR EMERGENCY LIGHT AT FIRST CLASS CL OSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008010900078 20080109 00078 WP 2008 1 9 AALA20072464 1 20071217 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG DAMAGED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 479AA 49654 DFW INFLIGHT T689/17DEC - NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO DFW AND LANDED WITHOUT INCIDEN T. FOUND NOSE GEAR PISTON FLAT DUE TO DAMAGE TO STRUT CYLINDER. REPLACED UPPER AND LOWER NOSE LANDING GEAR STRUTS AND SERVICED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008010900087 20080109 00087 EA 2008 1 9 SWIA200719013 1 20071231 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 613SK 10038 FLT 4003 - CEILING EMERGENCY LIGHT IS INOP. RELAMPED CEILING EMERGENCY LIGHT. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2008010900096 20080109 00096 EA 2008 1 9 SWIA200719022 1 20071228 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT LIGHTS SHORTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 954SW 7815 FIRST OFFICERS CHART HOLDER SHORTED OUT. ADJUSTED WIRING AND REPLACED ALL CHART HOLDER BULBS. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2008010900102 20080109 00102 EA 2008 1 9 MASA200700816 1 20071121 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27172 7172 ASH FLT 7307 ORD - MAIN PASSENGER DOOR OUTER HANDLE WILL NOT SECURE. ADJUSTED OUTER HANDLE. 2 L 7 2 4F RT A21EA 2008010900112 20080109 00112 EA 2008 1 9 MASA200700898 1 20071217 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27173 7173 ASH FLT 7179 IAD - LT FUSELAGE EXTERIOR EMERGENCY EXIT LIGHT INOP. MX RELAMPED, OPS CK GOOD. 2 L 7 2 4F RT A21EA 2008010900113 20080109 00113 EA 2008 1 9 MASA200700742 1 20070926 A 5753 FITTING CNDAIR CL600 CL6002B19 1900309 EA TE FLAP UNKNOWN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 693BR 7761 REPAIR TO O/B FLAP LUG FITTING WS 178 AND 264. 2 L 7 2 4F RT A21EA 2008010900117 20080109 00117 NM 2008 1 9 2007UALA05315 1 20070924 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 AFT CARGO PIT STRINGER CLIPS CRACKED AT BS 747 AT STRINGER 23L. REMOVED AND REPLACED STRINGER CLIPS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010900118 20080109 00118 EA 2008 1 9 MASA200700921 1 20071227 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A MASA O OTHER J WARNING INDICATION DE DESCENT 1 SW 07 75998 7336 ASH 7385 CLE - IAD - DURING EXTENTION ON ARRIVAL GEAR DISAGREE, NOSE GEAR DOOR OPEN CAUTION. MX REMOVED AND REPLACED SE LECTOR VALVE, OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2008010900119 20080109 00119 EA 2008 1 9 MASA200700704 1 20071016 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 UNKNOWN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 646BR 7392 REPAIR TO FLOORBEAM AT FS 280 AND RBL 12 LOWER FLANGE. 2 L 7 2 4F RT A21EA 2008010900120 20080109 00120 EA 2008 1 9 MASA200700870 1 20071211 A 3230 25301 RELIEF VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 571ML 6059 7209 ASH 7493 IAD - GEAR DISAGREE/NOSE GEAR DOOR DID NOT CLOSE. REMOVED AND REPLACED PRESSURE RELIEF VALVE. 2 L 7 2 4F RT A21EA 2008010900121 20080109 00121 EA 2008 1 9 MASA200700858 1 20071205 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17337 7337 ASH FLT 2818 PHX - DSM - NR 6 EXTERNAL EMERGENCY EXIT LIGHT INOP. MX RELAMPED, OPS NORMAL. 2 L 7 2 4F RT A21EA 2008010900126 20080109 00126 EA 2008 1 9 MASA200700721 1 20071021 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27172 7172 ASH FLT 7126 IAD PAX DOOR WILL NOT LOCK. MX COULD NOT DUPLICATE 2 L 7 2 4F RT A21EA 2008010900133 20080109 00133 NM 2008 1 9 2007UALA05326 1 20071227 A 2560 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE INOPERATIVE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 SLIDE BOTTLE LIGHT AT DOOR 2R WON'T ILLUMINATE. REMOVED LIGHT LENS CAP AND REINSTALLED FOUND LIGHTS OPERATING NORMALLY 2 L 7 2 4F 4 F RT A2NM E17NE 2008010900134 20080109 00134 NM 2008 1 9 2007UALA05330 1 20071228 A 3350 78961 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY LIGHTS AT 3A AFT & 3J AFT ARE INOPERATIVE. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010900137 20080109 00137 NM 2008 1 9 2007UALA05331 1 20071228 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 CEILING EMERGENCY LIGHT INOP AT ROW 13. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010900139 20080109 00139 NM 2008 1 9 2007UALA05332 1 20071228 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY LIGHT ABOVE DOOR 1R INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010900141 20080109 00141 NM 2008 1 9 2007UALA05334 1 20071228 A 3320 SOCKET BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE AFT GALLEY MELTED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 187UA 26877 AFT CABIN GALLEY 422 OVERHEAD PANEL ODOR OF BURN INSULATION. FOUND BURNING SMELL FROM GALLEY LIGHT DUE TO MELT SOCKET. REPLACED LIGHT ASSEMBLY OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010900142 20080109 00142 EA 2008 1 9 MASA200700811 1 20071120 A 3350 BATTERY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75993 7372 FLT 7238, ORD - ALL EMERGENCY LIGHTS INOP, SWITCH LEFT ON. MX CHARGED EMERGENCY BATTERIES, OPS GOOD. 2 L 7 2 4F RT A21EA 2008010900143 20080109 00143 EA 2008 1 9 MASA200700797 1 20071112 A 3350 505802 COVER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75994 7367 ASH FLT 7275 IAD-CAE - PAX DOOR LOWER EMERGENCY EXIT SIGN COVER MISSING. MX INSTALLED A NEW COVER. 2 L 7 2 4F RT A21EA 2008010900144 20080109 00144 EA 2008 1 9 MASA200700807 1 20071116 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A MASA O OTHER O OTHER AP APPROACH 1 SW 07 27191 7191 ASH FLT 2794 SBP - FLAPS FAIL ON APPROACH AT 30 DEGREE'S. MX COMPLIED WITH PART A. 2 L 7 2 4F RT A21EA 2008010900145 20080109 00145 NM 2008 1 9 2007UALA05339 1 20071227 A 3350 1319 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 375UA 24640 FWD ENTRY DOOR EMERGENCY EXIT LIGHT BULB FOUND BROKEN. RELAMPED. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010900147 20080109 00147 EA 2008 1 9 MASA200700813 1 20071124 A 3230 601R751451 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A MASA O OTHER O OTHER CR CRUISE 1 SW 07 27318 19113 7218 ASH FLIGHT 2802 PHX - NLG DISAGREE WARNING MESSAGE IN FLIGHT. CREW DECLARED AN EMERGENCY, NLG EXTENDED MLG DID NOT. CR EW EXTENDED THE MLG THROUGH ALTERNATE EXTENSION. REMOVED AND REPLACED MLG SELECTOR VALVE, OPS GOOD. 2 L 7 2 4F RT A21EA 2008010900151 20080109 00151 EA 2008 1 9 MASA200700727 1 20071022 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 718 CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 75984 7489 FS 718.00 RT FRAME IS CRACKED BETWEEN STRINGERS 10 AND 12. PERMANENT REPAIR WAS ACCOMPLISHED BY AAR HOT SPRINGS. 2 L 7 2 4F RT A21EA 2008010900153 20080109 00153 EA 2008 1 9 MASA200700784 1 20071108 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH 2750 IN PHX - FLOOR PATH LIGHTING INOP. MX WAS UNABLE TO DUPLICATE THE PROBLEM. 2 L 7 2 4F RT A21EA 2008010900154 20080109 00154 EA 2008 1 9 MASA200700820 1 20071123 A 5210 CABLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DISLODGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 154SF 7154 ASH 7371 LGA - REPORTED THE PAX DOOR WILL NOT OPEN FULLY. MX REINSTALLED THE DOOR CABLES ON THE PULLEYS. 2 L 7 2 4F RT A21EA 2008010900155 20080109 00155 EA 2008 1 9 MASA200700821 1 20071123 A 5420 22850081141 ACCESS PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NACELLE DEPARTED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37342 4286 7342 ASH 7160 - BHM-ORD, REPORTED AN UPPER FAN COWL ACCESS PANEL MISSING/DEPARTED ON THE RUNWAY. MX REPLACED THE COWL AND D ID NOT FIND ANY SUBSEQUENT AIRCRAFT DAMAGE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008010900156 20080109 00156 EA 2008 1 9 MASA200700809 1 20071118 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 154SF 7154 ASH FLT 7347 DSM - FIRST 4 EMERGENCY EXIT FLOOR LIGHT INOP. MX FOUND NO POWER TO THE LIGHT STRIPS. CYCLED SWITCH ON FA PANEL, OPS NORMAL. 2 L 7 2 4F RT A21EA 2008010900157 20080109 00157 NM 2008 1 9 LYNX00004 1 20071219 A 3230 301450301 PSEU BOMBDR DHC8 DHC8402 1390042 NM LANDING GEAR FAULTY A 3LYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 21 503LX 4170 DURING CLIMBOUT, CREW RETRACTED GEAR AND THE LT MLG DOORS DIDN`T CLOSE, RAN THE QRH AND EXTENDED GEAR. INDICATED 3 GREE N LIGHTS RETRACTED GEAR AGAIN AND THIS TIME INDICATION WAS A RED "LEFT" AND AN AMBER "L DOOR" GEAR DOOR OPEN AND THE GEA R SELECT HANDLE WAS AMBER (GEAR AND HANDLE DISAGREEMENT) AFTER ABOUT 5 MINS THE LT GEAR IN TRANSIT LIGHT WENT OUT AND TH E LT GEAR DOORS SHUT AND THE AMBER LIGHT WENT OUT ON THE SELECT SWITCH UNCOMMANDED BY THE CREW AT THE TIME ALTHOUGH THE SELECT SWITCH WAS IN THE RETRACT POSITION AT THE TIME. THE PSEU SHOWED FLAT LINE INDICATING NO SIGNAL FOR THE LT UPLOCK PROX SWITCH, WHILE TAPPING ON THE PSEU THE LT UPLOCK READING WOULD GO FROM -- TO OPEN. REMOVED AND REPLACED THE PSEU. 2 H 7 2 4T RT A13NM 2008010900158 20080109 00158 SO 2008 1 9 C2XA07SH11 1 20071229 A 5320 14522178005 SILL EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11119 145677 SHV - DURING C-CHECK CORROSION ON SERVICE DOOR THRESH HOLD SILL. MX REMOVED AND REPLACED SVC DOOR CENTER SILL IAW EMB 1 45 SRM 51-40-02, INSTALLED NUT PLATES IAW EMB EC 5320-0437. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008010900159 20080109 00159 SO 2008 1 9 C2XA07SH111 1 20071229 A 5320 14522178005 SILL EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11119 145677 SHV - DURING C-CHECK CORROSION ON SERVICE DOOR THRESH HOLD SILL. MX REMOVED AND REPLACED SVC DOOR CENTER SILL IAW EMB 1 45 SRM 51-40-02, INSTALLED NUT PLATES IAW EMB EC 5320-0437. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008010900160 20080109 00160 SO 2008 1 9 C2XA07SH112 1 20071229 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11119 145677 SHV - DURING C-CHECK CORROSION ON LEFT HAND OMEGA BEAM LOWER FLANGE AT FR 20. MX REPAIRED LT OMEGA BEAM LOWER FLANGE AT FR 20 IAW EMB 145 SRM 51-30-01, 51-40-04, 51-40-06, 51-40-02 AND IAW EMB 145 CPM 51-21-04, 51-21-05, 51-21-06. THE AIR CRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008010900161 20080109 00161 SO 2008 1 9 C2XA07SH113 1 20071229 A 5751 C510 PLATE EMB 145 EMB145XR 3260214 SO AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13118 145675 SHV - DURING C-CHECK PANEL 197CL HAS BAD BONDING PLATE. MX REPAIRED 197CL PANEL IAW EC 5750-01315. THE AIRCRAFT WAS AP PROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008010900162 20080109 00162 SO 2008 1 9 C2XAO7SH114 1 20071229 A 5751 C510 PLATE EMB 145 EMB145XR 3260214 SO AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13118 145675 SHV - DURING C-CHECK PANEL 197DR HAS BAD BONDING PLATES. MX REPAIRED PANEL 197 DR BONDING PLATES IAW EC 5750-01315. TH E AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008010900163 20080109 00163 SO 2008 1 9 C2XA07SH115 1 20071229 A 5751 C510 PLATE EMB 145 EMB145XR 3260214 SO AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13118 145675 SHV - DURING C-CHECK PANEL 197BB HAS CORRODED BONDING PLATES. MAINTENANCE REPAIRED PANEL 197BB IAW EC 5750-01315. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008010900164 20080109 00164 SO 2008 1 9 C2XA07SH116 1 20071229 A 5751 C510 PLATE EMB 145 EMB145XR 3260214 SO AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13118 145675 SHV - DURING C-CHECK PANEL 197AB HAS CORRODED BONDING PLATES. MX REPAIRED PANEL 197AB BONDING PLATES IAW EC 5750-01315. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008010900165 20080109 00165 SO 2008 1 9 C2XA07SH118 1 20071229 A 5751 C510 PLATE EMB 145 EMB145XR 3260214 SO LT AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13118 145675 SHV - DURING C-CHECK LT AILERON LOWER SHROUD HAS CORROSION ON BONDING PLATE. MX REPAIRED LT AILERON LOWER SHROUD BONDIN G PLATES IAW EC 5750-01315. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008010900166 20080109 00166 EA 2008 1 9 MASA200700775 1 20071105 A 2600 SWITCH CNDAIR CL600 CL6002B19 1900309 EA FIRE BOTTLE TEST OUT OF ADJUST A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 87353 7353 ASH FLT 7198 RDU - NORMAL FIRE BOTTLE WILL NOT TEST. MX ADJUSTED PUSH SWITCH, OPS GOOD. 2 L 7 2 4F RT A21EA 2008010900167 20080109 00167 EA 2008 1 9 MASA200700804 1 20071118 A 4900 8414A ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A MASA O OTHER O OTHER CR CRUISE 1 SW 07 37342 25607 7342 ASH FLT 7307 BMI - APU OVERTEMP FOLLOWED BY APU FIRE THEN APU FAULT. MX TROUBLESHOT AND FOUND NO EVIDENCE OF FIRE. REM OVED AND REPLACED THE DOOR POT AND THE LINEAR ACTUATOR, OPS NORMAL. 2 L 7 2 4F RT A21EA 2008010900168 20080109 00168 EA 2008 1 9 MASA200700806 1 20071115 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75998 7336 ASH FLT 7180 PHL - FLAPS FAIL AT 12 DEGREES. C/W PART A. 2 L 7 2 4F RT A21EA 2008010900171 20080109 00171 EA 2008 1 9 MASA200700729 1 20071023 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75995 7361 ASH 7348 IAD - RT SIDE OVERWING EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. MX RELAMPED, OPS GOOD. 2 L 7 2 4F RT A21EA 2008010900172 20080109 00172 EA 2008 1 9 MASA200700792 1 20071111 A 2510 TRACK CNDAIR CL600 CL6002B19 1900309 EA JUMP SEAT DIRTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 651ML 7139 ASH FLT 7364 ORD - FA FWD JUMPSEAT WILL NOT AUTO STOW. MX REMOVED GRIM TRACKS AND DEBRIS FROM AREA, SEAT STOWED NORMALL Y. 2 L 7 2 4F RT A21EA 2008010900173 20080109 00173 EA 2008 1 9 MASA200700793 1 20071111 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27172 7172 ASH FLT 7166, IAD - CREW REPORTED THAT THE MAIN CABIN DOOR EXTERIOR HANDLE WOULD NOT STOW. MX LUBED HANDLE, OPS GOOD. 2 L 7 2 4F RT A21EA 2008010900174 20080109 00174 EA 2008 1 9 MASA200700817 1 20071121 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX OUT OF RIG A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17337 733 ASH FLT 2737, PHX - CREW REPORTED THAT THE PAX DOOR WILL NOT CLOSE FROM INSIDE. MX RIGGED DOOR. 2 L 7 2 4F RT A21EA 2008010900175 20080109 00175 SO 2008 1 9 C2XA07SH117 1 20071229 A 5751 C510 PLATE EMB 145 EMB145XR 3260214 SO LT AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13118 145675 SHV - DURING C-CHECK LT AILERON UPPER SHROUD HAS CORROSION ON BONDING PLATES. MX REPAIRS LT AILERON UPPER SHROUD BONDIN G PLATES IAW EMB EC 5750-0315. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008010900177 20080109 00177 SO 2008 1 9 C2XA07SH119 1 20071229 A 5751 C510 PLATE EMB 145 EMB145XR 3260214 SO RT AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13118 145675 SHV - DURING C-CHECK RT UPPER AILERON SHROUDS HAS CORRODED BONDING PLATES. MX REPAIRED RT UPPER AILERON SHROUDS BONDING PLATES IAW EC5750-01315. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008010900178 20080109 00178 SO 2008 1 9 C2XA07SH120 1 20071229 A 5751 C510 PLATE EMB 145 EMB145XR 3260214 SO RT AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13118 145675 SHV - DURING C-CHECK RT LOWER AILERON SHROUDS HAS CORRODED BONDING PLATE. MX REMOVED AND REPLACED RT LOWER AILERON BOND ING PLATE IAW EC5750-01315. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008010900179 20080109 00179 EA 2008 1 9 MASA200700913 1 20071222 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 651ML 7139 ASH FLT 7289 IAD-DTW - FA MID CABIN AFT EMERGENCY CALL LIGHT WAS INOP. MX RELAMPED, OPS GOOD. 2 L 7 2 4F RT A21EA 2008010900180 20080109 00180 2008 1 9 MASA200700684 4 20071012 A 2561 P0640101 LIFE VEST CNDAIR CL600 CL6002B19 1900309 EA TORN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 654BR 123 7454 ASH FLT 1023 HNL-KOA - 2 INFANT LIFE VEST WERE TORN. MX REPLACED THE LIFE VESTS. 2 L 7 2 4F RT A21EA 2008010900181 20080109 00181 EA 2008 1 9 MASA200700685 1 20071012 A 5320 DOOR CNDAIR CL600 CL6002B19 1900309 EA OXYGEN MASK BOX DETACHED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75993 6833 7372 ASH FLT 7174 MSN-ORD - CAPTAIN'S O2 MASK BOX DOOR WAS BROKEN OFF. REMOVED AND REPLACED O2 BOX. 2 L 7 2 4F RT A21EA 2008010900182 20080109 00182 SO 2008 1 9 C2XA07SH121 1 20071229 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27200 14500956 SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION ON FR 20. MX REPAIRED LT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 53-20-10. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008010900183 20080109 00183 EA 2008 1 9 MASA200700686 1 20071012 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF ADJUST A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17337 7337 ASH FLT 2894, PHX - OUTER DOOR HANDLE WILL NOT CLOSE. MX ADJUSTED INNER DOOR STOW HANDLE. 2 L 7 2 4F RT A21EA 2008010900184 20080109 00184 SO 2008 1 9 C2XA07ON046 1 20071227 A 2611 473597 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO CARGO BAY INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17185 6533 6533 14500922 FLT MX - TYS - WHILE PERFORMING PLANNED MX INSPECTION THE NR 2 BAGGAGE SMOKE DETECTOR WILL NOT TEST. MX PERSONNEL REMOV ED AND REPLACED NR 2 BAGGAGE SMOKE DETECTOR OPERATIONALLY CHECKED SATISFACTORY AND A/C WAS RELEASED TO RETURN FOR SERVIC E IN AIRWORTHY CONDITIONS. 2 L 7 2 4F RT 2008010900186 20080109 00186 EA 2008 1 9 MASA200700748 1 20071028 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH FLT 2818 DSM - LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 2008010900187 20080109 00187 SO 2008 1 9 C2XA07ON047 1 20071224 A 3350 2013BR BATTERY EMB 145 EMB145XR 3260214 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12167 5374 1582 14500834 FLT MX - LAX - WHILE PERFORMING SERVICE AND ROUTINE CHECKS, MX PERSONNEL FOUND OVERWING EMERGENCY LIGHTS OUT. MX PERSON NEL REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY OPERATIONALLY CHECKED SATISFACTORY AND A/C WAS RELEASED TO RETURN FOR SERVICE IN AIRWORTHY CONDITIONS. 2 L 7 2 4F RT 2008010900188 20080109 00188 2008 1 9 MASA200700827 4 20071129 A 2561 P01074201 LIFE VEST CNDAIR CL600 CL6002B19 1900309 EA OPEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 693BR 7761 ASH FLT 1017 HNL-OGG, INFANT LIFE VEST OPENED. MX REPLACED THE LIFE VEST. 2 L 7 2 4F RT A21EA 2008010900189 20080109 00189 NM 2008 1 9 BB07106 1 20071230 A 3350 LIGHT BOEING 757 757225 1384959 NM CABIN BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 913AW 22207 MAINTENANCE FOUND FLOOR LEVEL LIGHT AT ROW 8L BROKEN. REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F RT A2NM 2008010900191 20080109 00191 EA 2008 1 9 MASA200700829 1 20071129 A 2610 SWITCH CNDAIR CL600 CL6002B19 1900309 EA FIRE BOTTLE DIRTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 87353 7353 FLT 7400, HSV - CARGO BOTTLE 1 PUSH TO DISCHARGE WILL NOT ILLUM. MX CLEANED SWITCH. 2 L 7 2 4F RT A21EA 2008010900192 20080109 00192 EA 2008 1 9 MASA200700733 1 20071024 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75995 7361 ASH FLT 7334 CHS - EMERGENCY FLOOR LIGHTS AT ROWS 6, 7, 8 INOP. CONTRACT MX RESECURED LOOSE CONNECTION. OPS NORMAL. 2 L 7 2 4F RT A21EA 2008010800165 20080108 00165 NM 2008 1 8 SWAA076478 1 20071221 A 5315 6546809 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 946, RBL 5. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2008010800166 20080108 00166 NM 2008 1 8 SWAA076472 1 20071221 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727B, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010800171 20080108 00171 2008 1 8 SWAA076480 4 20071222 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 646SW 28331 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008010800198 20080108 00198 NM 2008 1 8 07FDEA05147 1 20071227 A 5320 69476732 FITTING BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 NR 2 LOWER CARGO DOOR THRESHOLD TIEDOWN FITTING 23" FROM AFT EDGE OF CUT OUT CORRODED ON UPPER SURFACE. REMOVED AND REP LACED TIEDOWN FITTING REF DWG 69-47673 REF SRM 51-30-2, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008010800218 20080108 00218 EU 2008 1 8 07FDEA05151 1 20071228 A 5347 A53781932202 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 659FE 757 TRACK AT NR Y 2462 AND BETWEEN FR 18 AND 21 FOUND DAMAGED. SEAT TRACK WAS REPAIRED IAW SRM 53-10-16 FIGURE 203. 2 L 7 2 4F RT A35EU 2008010800219 20080108 00219 NM 2008 1 8 SWAA076495 1 20071227 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 711, STR 10L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2008010800224 20080108 00224 NM 2008 1 8 SWAA076497 1 20071227 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 22R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008010800237 20080108 00237 NM 2008 1 8 HALA0700555 1 20071227 A 4900 UNKNOWN BOEING 767 76733A 1385209 NM APU UNKNOWN A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 581HA 28141 ETOPS SIGNIFICANT SYSTEM, "APU FAULT" APU WILL NOT START. T/S PER FIM 49-11-00/101 FIG 103, ECU BITE SHOWED "START ABOR TED" AND LRU FAULT "AC START CIRCUIT" APU STARTED NORMALLY SEVERAL TIMES AND ALL TESTS CHECK GOOD PER FIM 49-11-00, "APU FAULT" CLEARED AND NO OTHER FAULTS NOTED. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2008010800243 20080108 00243 NM 2008 1 8 SWAA076506 1 20071227 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 270, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010800244 20080108 00244 NM 2008 1 8 SWAA076512 1 20071227 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733, STR 20L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800247 20080108 00247 NM 2008 1 8 SWAA076516 1 20071227 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800248 20080108 00248 NM 2008 1 8 SWAA076514 1 20071227 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800249 20080108 00249 EA 2008 1 8 QXEA200702037 1 20071227 A 2612 FIRE LOOP CNDAIR CL600 CL6002C10 1390015 EA APU BAY SHORTED A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 601QX 10009 SEA - FLIGHT 9851, FIRE SYSTEM FAULT MESSAGE RECEIVED, APU LOOP "A" SHORTED. MAINTENANCE PLACED THE SYSTEM ON MEL 26-00 -1. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008010800250 20080108 00250 NM 2008 1 8 SWAA076515 1 20071227 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800251 20080108 00251 NM 2008 1 8 QXEA200702038 1 20071127 A 3040 4100S02001 CONTROLLER BOMBDR DHC8 DHC8402 1390042 NM ANTI ICE SYS MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 404QX 5363 4046 SEA - FLIGHT 2372 - UPON SELECTION OF WINDSHIELD HEAT THE CONTROL LIGHT ILLUMINATED. RETURNED TO THE GATE. MAINTENANCE REPLACED THE ANTI-ICE CONTROLLER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008010800257 20080108 00257 NM 2008 1 8 SWAA076518 1 20071227 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 456WN 32463 EEPLS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008010800260 20080108 00260 EU 2008 1 8 MALA070201 1 20071221 A 5410 STIFFENER SAAB SF340 340B 7860101 EU LT NACELLE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 418XJ 340B418 LT NACELLE FIREWALL CHAFED NEAR BEADED STIFFENER PER SRM 54-10-30 PARA 5 AND 6. INSTALLED DOUBLER IAW MAL EO NR S54187. 2 L 7 2 4T RT A52EU 2008010800261 20080108 00261 EU 2008 1 8 MALA070202 1 20071221 A 5230 SKIN SAAB SF340 340B 7860101 EU CARGO DOOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 418XJ 340B418 DENT IN CARGO DOOR EXTERIOR SKIN, UPPER AFT AREA. REPAIRED IAW MAL EO NR S52028. 2 L 7 2 4T RT A52EU 2008010800265 20080108 00265 SO 2008 1 8 CHQA200700101 1 20071228 A 3340 A42027 BRACKET EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL TAXI LIGHT BROKEN A CHQA L ABORTED APPROACH O OTHER AP APPROACH 1 GL 11 263SK 145199 CAE311771 YUL TO CLE - ON FINAL APPROACH WITH LANDING GEAR DOWN, FLAPS SELECTED TO 45, AND LANDING CHECK-LIST COMPLETED, THE FLIGH T CREW HEARD A BANGING NOISE ORIGINATING FROM THE NOSE GEAR AREA. THE FLIGHT CREW ABORTED THE APPROACH TO CONVERSE WITH MX CONTROL ABOUT POSSIBLE CAUSES, AND IT WAS DECIDED THAT IT WAS MOST LIKELY THE NOSE LANDING GEAR TAXI LIGHT. THE AIR CRAFT THEN LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NOSE LANDING GEAR AND FOUND THE UPPER TAXI LIGHT BROKEN F ROM ITS MOUNT AND HANGING BY THE WIRES. THE LANDING LIGHT WAS REMOVED AND PLACED ON CDL FOR REPLACEMENT. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008010800275 20080108 00275 NM 2008 1 8 07FDEA05157 1 20071229 A 5313 ACA37961 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 592FE 48550 01 EACH FASTENER HOLE FOUND CRACK AT 9 O'CLOCK POSITION APPROXIMATELY 0.350" IN LENGTH, AT LEFT SIDE TRUNNION FITTING LO WER LONGERON DURING TRUNNION FITTING CRACK AREA TRIMMED OUT INSPECTION. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUM E II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008010800278 20080108 00278 NM 2008 1 8 07FDEA05160 1 20071231 A 5753 SUPPORT DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 592FE 48550 RT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING SUPPORT OUTBOARD AFT HOLE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1 -5750-116536. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008010800280 20080108 00280 EU 2008 1 8 07FDEA05162 1 20071231 A 5315 A5327534420000 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 659FE 757 AFT CARGO COMP'T, CROSSBEAM CRACKED AT FRAME 59 BETWEEN TRACKS Y-953 AND Y- 1456. CROSSBEAM REPAIRED AT FRAME 59 BETWEE N TRACKS Y-953 AND Y-1456 IAW SRM 53-10-15, FIG 211 (SHEET 1 AND 2). 2 L 7 2 4F RT A35EU 2008010800288 20080108 00288 EU 2008 1 8 07FDEA05167 1 20071231 A 5315 A5378196620000 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 659FE 757 CROSSBEAM CRACKED AT FR 30 AND BETWEEN TRACKS Y 450 AND Y 953. REPAIRED IAW SRM 53-10-15, FIG 212. 2 L 7 2 4F RT A35EU 2008010800291 20080108 00291 NM 2008 1 8 SWAA076521 1 20071227 A 5311 65C34355 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800296 20080108 00296 NM 2008 1 8 SWAA076524 1 20071227 A 5311 6546538 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010800310 20080108 00310 EU 2008 1 8 08FDEA00003 1 20071213 A 5315 A53275350200 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 659FE 757 CROSSBEAM AT FR 65 WITH DEFORMITY BETWEEN Y953 AND Y1456. CROSSBEAM AT FR 65 REPAIRED BETWEEN Y953 AND Y1456 IAW SRM 53 -17-15, FIG 203, SHEET 1 AND 2. 2 L 7 2 4F RT A35EU 2008010800317 20080108 00317 2008 1 8 HALA0700565 2 20071229 A 7532 BLEED VALVE BOEING 767 76733A 1385209 NM ENGINE MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM, R ENG BLEED VALVE CLOSES WHEN LEFT START SELECTOR POSITIONED TO GRND DURING XBLEED START PER A MM 71-00-00-712-021. STARTED BOTH ENGINES. OPS CK OK, COULD NOT DUPLICATE WRITE-UP. 2 L 7 2 4F RT A1NM 2008010800322 20080108 00322 NM 2008 1 8 HALA0700563 1 20071230 A 2710 AILERON BOEING 767 76733A 1385209 NM MALFUNCTIONED A HALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, AILERON LOCKOUT AT 260 KTS. T/S PER FIM 27-11-00 FIG 104 TO BLOCK 15. NO FAULTS ON LT OR RT SAMS. NO MSGS. SYS TESTS GOOD. 2 L 7 2 4F RT A1NM 2008010800324 20080108 00324 CE 2008 1 8 DJFA2007139 1 20071205 A 2120 UNKNOWN BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE CABIN ODOR E DJFA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 23 709TA RK180 ON APPROACH CREW REPORTED BURNING SMELL FROM THE RT REAR FLOOR AREA. MAINTENANCE RAN THE AIRCRAFT BUT WAS UNABLE TO DET ECT ANY SMELL IN ALL CABIN TEMPERATURE MODES (AUTO/MANUAL, HOT AND COLD). AIRCRAFT WAS RELEASED. 2 H 7 2 4F 4 F RT A16SW E25EA 2008010800336 20080108 00336 NM 2008 1 8 UPS07M51345 1 20071113 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C LT WING UPPER FUEL TANK STRINGER NR 11 END SUSPECT CRACKED. HFEC INSP C/O AT STR NR 11, FOUND CRACK O F APPROX 5" LENGTH. STR NR 11 SPLICE END AND LOCK FASTENER AT REPAIR AREA REMOVED. CRACK AT LT WING STR NR 11 SLOT OUT PER SRM 57-20-00 FIG 10VIR35. HFEC INSP C/O ON SLOT OUT AREA AND FOUND NO CRACK EVIDENT. REPAIR ANGLES FAB, HEAT TREA TED, PAINTED AND REPROTECTED. REPAIR ANGLES INSTALLED AND CAP SEALING C/O ON REPAIR AREA. LEAK CK SATIS. 2 L 7 3 4F RT A22WE 2008010800337 20080108 00337 NM 2008 1 8 UPS07M51346 1 20071113 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C LT WING UPPER FUEL TANK STRINGER NR 10 END SUSPECT CRACKED. HFEC INSP C/O AT STR NR 10 FOUND CRACK AP PROX 10" LENGTH. STR NR 10 SPLICE END AND LOCK FASTENER AT REPAIR AREA REMOVED. CRACK AT STR NR 10 SLOT OUT PER SRM 57 -20-00 FIG 10 VIR35. HFEC INSP C/O ON SLOT OUT AREA AND FOUND NO CRACK EVIDENT. REPAIR ANGLES FAB, HEAT-TREATED, REPRO TECTED AND PAINTED. REPAIR ANGLES INSTALLED. CAP SEALING C/O ON STR NR 10 REPAIR AREA. LEAK CHECKED SATIS. 2 L 7 3 4F RT A22WE 2008010800340 20080108 00340 NE 2008 1 8 YENA2007125 2 20071228 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 MALFUNCTIONED A YENA O OTHER J WARNING INDICATION DE DESCENT 1 EA 15 510JB 1280 V10934 FLT NR 917, JFK-ORD, AT FL 380, UPON COMMENCING INITIAL DESCENT ENGINE NR 1 EXPERIENCED A VERY NOTICEABLE COMPRESSOR STA LL. "ENG 1 STALL" ECAM APPEARED. QRH/ECAM PROCEDURE APPLIED. ENGINE RECOVERED SUCCESSFULLY. NO ABNORMAL PARAMETERS. NO FURTHER PROBLEMS NOTED. ACCOMPLISHED A320 TSM 71-00-00-810-808 TO INCLUDE ENGINE POWER ASSURANCE TEST AS PER A320 A MM 71-00-00-710-813 ON ENGINE NR 1. NO DEFECTS NOTED. ALL ENGINE PARAMETERS NORMAL. ENGINE OK FOR SERVICE. ACCOMPLIS HED BORESCOPE INSPECTION OF NR 1 ENG HPC AS PER A320 AMM 72-00-00-200-016. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010800343 20080108 00343 EA 2008 1 8 SWIA200719000 1 20071226 A 3230 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 403SW 7028 FLT 3822 - RECEIVED A TRIPLE CHIME AND "NOSE DOOR OPEN" WARNING MESSAGE CLIMBING THRU 9,000'. REPLACED MLG SELECTOR VAL VE IAW 32-32-10 AS WELL AS MANUAL BYPASS AND RUNAROUND VALVE IAW 32-32-2. OPS CHECK GOOD, PN: 750004000-003, SN OFF: 05 8, PN: 750005000, SN OFF: 0740. 2 L 7 2 4F RT A21EA 2008010800348 20080108 00348 EA 2008 1 8 SWIA200719004 1 20071228 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 405SW 8103 310 7029 FLT 3835 - AFTER TAKEOFF RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN MESSAGE. REPLACED NOSE SELECTOR VALVE IAW MM 32-33-1 0. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2008010800359 20080108 00359 EA 2008 1 8 SWIA200719005 1 20071229 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 455SW 7760 FLT 3994 - FLOOR EMERGENCY LIGHT IS INOP. REPLACED NR 3 ELBP INVERTER IAW MM 33-51-07. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008010800360 20080108 00360 EA 2008 1 8 SWIA200719006 1 20071230 A 5610 601R3303314 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 941SW 6 6 7750 FLT 6615 - RIGHT WINDSHIELD SHATTERED AT FL340. REPLACED SIDE WINDSHIELD IAW CRJ MM 56-11-01. 2 L 7 2 4F RT A21EA 2008010800370 20080108 00370 NM 2008 1 8 ASMF200712001 1 20071209 A 5610 589357 WINDOW BOEING 737 737* NM CFMINT CFM567 CFM567B22 13802 NE COCKPIT CRACKED W ASMF K NONE O OTHER DE DESCENT 1 SW 23 851AM 12272 12272 29363 CAPTAIN REPORTED THAT LT WINDOW NR 4, CRACKED DURING DESCENT. MAINTENANCE PERSONNEL REPLACED THE WINDOW IAW MM 56-11-31, TESTED CORRECT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2008010800386 20080108 00386 NE 2008 1 8 HCM2007F00003 2 20071106 A 7321 FCU SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE ENGINE DEFECTIVE E HCMA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 13 992BH 2989 9531 SHORTLY AFTER TAKEOFF OF A TOUR FLIGHT, AT APPROX 9:40 AM, THE PILOT NOTICED THE ENGINE NG SPEED HUNTING AND THE TORQUE FLUCTUATING (LESS THAN 20 PERCENT), THE AC ALSO EXHIBITED SLIGHT YAWING IN CONJUNCTION WITH THE FLUCTUATING NG AND TORQU E. THE PILOT PERFORMED A LOW POWER PRECAUTIONARY LANDING AT AIRPORT. INSPECTION BY MAINTENANCE REVEALED NO DEFECTS WIT H THE FCU RIGGING OR WITH THE FUEL FILTERING AND FUEL DELIVERY SYSTEM. A CHECK OF THE FCU WAS FOUND TO BE DEFECTIVE (TH E FCU CHARACTERISTICS CHECKS FAILED). THE DEFECTIVE FCU WAS REMOVED AND SERVICEABLE UNIT INSTALLED. NO FURTHER DEFECTS HAVE OCCURRED. (K) 1 G 7 1 3U 3 U H9EU E19EU 2008010900006 20080109 00006 EA 2008 1 9 SWIA200719010 1 20071008 A 5210 CONTROL ROD CNDAIR CL600 CL6002C10 1390015 EA DOOR LOCK MECH CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 743SK 10199 FOUND C-CHECK, PAX DOOR LOWER LOCK MECHANISM CONTROL ROD IS CORRODED. REMOVED CORROSION FROM LOWER LOCK MECHANISM IN CO NTROL ROD PER CRJ700 SRM 51-21-11-001-001-A01. 2 L 7 2 4F RT A21EA 2008010900017 20080109 00017 NM 2008 1 9 2007UALA05213 1 20071224 A 2497 CONNECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 TR DISCONNECTED A UALA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 WP 29 831UA 1291 RTFL DUE TO A ELECTRICAL BUSS FAULT. FOUND CONNECTOR 1PU2A COMPLETELY DISCONNECTED FROM TR2 UNIT. INSPECTED TR2 LOCKS FOR CONNECTOR 1PU2A AND CONNECTOR 1PU2A. NO DISCREPANCIES. RESECURED CONNECTOR TO TR2 AND PERFORMED DC MAIN GENERATION (TR) ADJ AND TEST- RAN ENGINES AND TRANSFERRED POWER BETWEEN APU AND ENGINES. NO PROBLEMS NOTED AFTER TEST. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010900019 20080109 00019 NM 2008 1 9 2007UALA05222 1 20071224 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW O2 LOW PRESSURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 831UA 1291 CREW OXYGEN SYSTEM - LOW. RECORD PRESSURE PRIOR TO SERVICING. SERVICED CREW O2 TO PROPER SERVICE LEVEL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010900064 20080109 00064 NM 2008 1 9 AALA20072469 1 20071218 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 681AA 25338 MIA - EMERGENCY SEAT MOUNTED LIGHT AT SEAT 19D INOPERATIVE. REPAIRED CONNECTOR FOR EMERGENCY SEAT MOUNTED LIGHT AT SEAT 19D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008010900073 20080109 00073 WP 2008 1 9 AALA20072472 1 20071218 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 480AA 49655 DFW - EMERGENCY SEAT MOUNTED LIGHT AT SEAT 19D HAD BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 19D. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008010900076 20080109 00076 WP 2008 1 9 AALA20072474 1 20071218 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 480AA 49655 DFW - EMERGENCY LIGHT AT OVERHEAD RIGHT SEAT ROW 11 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD RIGHT S EAT ROW 11. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008010900081 20080109 00081 NM 2008 1 9 QXEA200702040 1 20071230 A 7500 8209076 SWITCH BOMBDR DHC8 DHC8402 1390042 NM BLEED OVERTEMP MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 407QX 120 4049 SEA - NR 2 BLEED HOT CAUTION LIGHT CAME ON DURING CRUISE FLIGHT. WHEN OFF AFTER DOING CHECKLIST. MAINTENANCE REPLACED THE BLEED OVERTEMP SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008010900084 20080109 00084 NM 2008 1 9 QXEA200702042 1 20071228 A 7312 ELEMENT DHAV DHC8 DHC8202 2809007 NM FUEL HEATER MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 348PH 484 PDX - IN CRUISE FLIGHT, NR 1 ENGINE FUEL TEMP BELOW THE GREEN ARC. FOLLOWED CHECKLIST, WITH NR 1 AUX PUMP ON THE FUEL T EMP WAS DECREASING BY 2 DEGREES WITH POWER REDUCTION. ALL OTHER PARAMETERS NORMAL. MAINTENANCE REPLACED THE FUEL HEATE R THERMAL ELEMENT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008010900088 20080109 00088 SO 2008 1 9 SWIA200719014 1 20071208 A 5610 NP1513112 WINDSHIELD EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 07 586SW 3164 3164 120354 FLT 5554 - RIGHT WINDSHIELD SHATTERED WHILE TAXIING. REPLACED WINDSHIELD ASSEMBLY IAW EMB120 MM 56-10-01. 2 L 7 2 4T RT A31SO 2008010900101 20080109 00101 EA 2008 1 9 MASA200700815 1 20071121 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 FLT 2796, PHX - EMERGENCY TRACK LIGHTS ON RT SIDE, LAST 2 ROWS NOT SECURED. MX RESECURED TRACK LIGHTING. 2 L 7 2 4F RT A21EA 2008010900111 20080109 00111 EA 2008 1 9 MASA200700897 1 20071217 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A MASA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 571ML 16223 7209 ASH FLT 7029 JAX-IAD - GEAR DISAGREE ON TAKEOFF. MX REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2008010900116 20080109 00116 NE 2008 1 9 MASA200700836 2 20071203 A 7230 6078T57G05 FAN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE ENGINE DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 77331 12517 7331 872218 FOUND INDICATION OF ARC OUT AT THE 12 O'CLOCK POSITION IN AREA 8. REMOVED AND REPLACED FAN DISK, ALL OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2008010900135 20080109 00135 EA 2008 1 9 MASA200700747 1 20071026 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 87353 7353 ASH FLT 7240 DSM - LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 2008010900136 20080109 00136 EA 2008 1 9 MASA200700691 1 20071013 A 3510 BUTTON CNDAIR CL600 CL6002B19 1900309 EA OXYGEN MASK STICKING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 47202 7202 ASH FLT 7364- ORD-GSP - CAPTAIN'S O2 MASK PRESS TO TEST BUTTON WAS STICKING. MX CLEANED THE O2 MASK AND BUTTON. 2 L 7 2 4F RT A21EA 2008010900140 20080109 00140 EA 2008 1 9 MASA200700860 1 20071206 A 2510 SEAT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT WORN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 592ML 7410 ASH FLT 7230 CAE-OVERNIGHT - CREW REPORTED FA SEAT COVER WORN AND WOULD NOT RETRACT. RECOVERED AND LUBED TRACKS. 2 L 7 2 4F RT A21EA 2008010900152 20080109 00152 EA 2008 1 9 MASA200700783 1 20071108 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77286 7286 ASH FLT 2818 PHX-DSM - NR 3 EMERGENCY EXIT FLOOD LT INOP. MX RELAMPED, OPS GOOD. 2 L 7 2 4F RT A21EA 2008010900185 20080109 00185 EA 2008 1 9 MASA200700726 1 20071022 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 202 CRACKED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75984 7489 PRESSURE BULKHEAD FS 202.75, BL 23.71 FOUND CRACKED DURING C-CHECK, REPAIRED. 2 L 7 2 4F RT A21EA 2008010900190 20080109 00190 EA 2008 1 9 MASA200700828 1 20071129 A 3350 BATTERY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 47202 7202 FLT 7484, PHL - EMERGENCY LIGHTS INOP, SWITCH LEFT ON. CHARGED EMERGENCY BATTERIES, OPS GOOD. 2 L 7 2 4F RT A21EA 2008010900193 20080109 00193 NM 2008 1 9 NOCA17307 1 20071229 A 2611 2156204A SMOKE DETECTOR BOEING 767 76739H 1385311 NM CARGO BAY MALFUNCTIONED A NOCA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 15 760NA 26257 AFT CARGO DET 1 ON STATUS. REPLACED NR 1 & 2 AFT CARGO SMOKE DETECTORS PER MM 26-16-01. 2 L 7 2 4F RT A1NM 2008010900194 20080109 00194 EA 2008 1 9 MASA200700887 1 20071216 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCONNECTED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7264V 7264 ASH FLT 2728 AUS-PHX - FWD FLOOR EMERGENCY LIGHTS INOP. MX RECONNECTED LIGHTS. 2 L 7 2 4F RT A21EA 2008010900195 20080109 00195 EA 2008 1 9 MASA200700790 1 20071111 A 3350 LS6006182 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH FLT 2802, PHX - ROW 12 EMERGENCY FLOOR LIGHTS INOP. MX CHANGED OUT FLOOR STRIP LIGHT ASSY. 2 L 7 2 4F RT A21EA 2008010900196 20080109 00196 NM 2008 1 9 BB07105 1 20071227 A 2131 1305026 CONTROLLER BOEING 757 757225 1384959 NM CABIN PRESSURE FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 918UW 36623 1690 22196 FLIGHT 815, CLT-CUN: DURING CLIMB, CREW REPORTED FAILURE OF LEFT PACK WHILE THE RIGHT PACK WAS ALREADY ON MEL. INITIAT ED EMERGENCY DESCENT TO 10,000 FEET AND RETURNED TO CLT. MAINTENANCE ACTION PENDING. 12/31/07 UPDATE: MAINENANCE REPLA CED THE CABIN PRESSURE CONTROLLER. NO FURTHER FAULTS. 2 L 7 2 4F RT A2NM 2008010900197 20080109 00197 EA 2008 1 9 32007 1 20071226 A 3260 17051101 TARGET CNDAIR CL600 CL6002B16 1900305 EA RT MLG LOOSE E V6NA O OTHER N FALSE WARNING CL CLIMB 1 SO 19 604HJ 8898 5382 AFTER DEPARTURE FROM KPBI EN ROUTE TO KFXE, CREW NOTED RED DISAGREE MESSAGE FOR RT MLG. CREW EXECUTED EMERGENCY MLG BLO W-DOWN. MLG INDICATED DOWN AND LOCKED FOR ALL THREE GEAR. UNEVENTFUL LANDING EXECUTED AT KFXE. SUBSEQUENT INVESTIGATI ON FOUND LOOSE TARGET FOR PROXIMITY SENSOR. TARGET RETIGHTENED AND OPERATIONAL CHECKS FOUND TO BE NORMAL. 2 L 7 2 4F RT A21EA 2008010900198 20080109 00198 EA 2008 1 9 MASA200700823 1 20071128 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A MASA O OTHER O OTHER CR CRUISE 1 SW 07 77195 7195 FLT 7245, IAD - GEAR DISAGREE WARNING, GEAR WOULD NOT RETRACT. MX PERFORMED 10 GEAR SWINGS AND ALL WERE NORMAL, NO PSEU CODES. 2 L 7 2 4F RT A21EA 2008010900203 20080109 00203 EA 2008 1 9 MASA200700714 1 20071019 A 5320 LATCH CNDAIR CL600 CL6002B19 1900309 EA OXYGEN MASK BOX DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17337 7337 ASH FLT 9420 PHX - OVERNIGHT, LAV O2 MASK BOX WOULD NOT CLOSE. MX REPLACED THE STOW LATCH. 2 L 7 2 4F RT A21EA 2008010900217 20080109 00217 SO 2008 1 9 C2XA07IA257 1 20071227 A 5730 14537011003 SKIN EMB 145 EMB145EP 3260221 SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE LEFT WING SKIN TO BE CRACKED AT THE SPOILER HINGE POINT. THE CR ACK WAS INSPECTED AND PLACED ON DMI, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS SDR FILED OPEN PENDING F INAL CORRECTIVE ACTION. 2 L 7 2 4F RT T00011AT 2008010900218 20080109 00218 EA 2008 1 9 TRAX200701986 1 20071222 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 AAR - FS 484 RBL 36 CLIP CRACKED AT INTERCOSTAL (MARKED). 2 L 7 2 4F RT A21EA 2008010900219 20080109 00219 SO 2008 1 9 C2XA07IA259 1 20071230 A 5610 WINDOW EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16987 145261 IAH - FLIGHT 2653, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE CAPTAINS DV WINDOW WOULD NOT LOCK. MAINTENANC E INSPECTED THE WINDOW, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . 2 L 7 2 4T RT T00011AT 2008010900220 20080109 00220 EA 2008 1 9 MASA200700837 1 20071203 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CHAFED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 75995 7361 PAX DOOR SURROUND EXTERIOR SKIN CHAFED BETWEEN STR 9L AND STR 10L. CHAFING IS 3.3" LONG, 0.050" WIDE, AND 0.020" DEEP. LOCALLY BLEND OUT DAMAGE TO BREAK SHARP EDGES. BLEND OUT AREA SHALL HAVE A 32RHR OR BETTER FINISH. NDI BLEND OUT AREA FOR CRACK INDICATIONS, NO INDICATIONS ALLOWED. APPLIED CORROSION PROTECTION. 2 L 7 2 4F RT A21EA 2008010900221 20080109 00221 EA 2008 1 9 MASA200700916 1 20071223 A 5270 SENSOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DIRTY A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 27173 7173 FLT 7172, ORD - PAX DOOR LATCH CAUTION MESSAGE IN FLIGHT. MX CLEANED DOOR SENSOR, OP GOOD. 2 L 7 2 4F RT A21EA 2008010900222 20080109 00222 EA 2008 1 9 MASA200700917 1 20071224 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37178 7178 ASH FLT 2818 DSM- OVERNIGHT, LT AFT EXTERIOR EMERGENCY LIGHT INOP. MX REPLACED THE LAMP, OP CHECKED GOOD. 2 L 7 2 4F RT A21EA 2008010900223 20080109 00223 EA 2008 1 9 MASA200700918 1 20071225 A 2720 SWITCH CNDAIR CL600 CL6002B19 1900309 EA RUDDER TRIM OUT OF POSITION A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17275 7275 ASH FLT 2925 ICT- OVERNIGHT, RT RUDDER TRIM WAS INTERMITTENT. MX FOUND THE TRIM SWITCH OFF CENTER AND REPOSITIONED IT A ND THE SYSTEM OP CHECKED GOOD. 2 L 7 2 4F RT A21EA 2008010900224 20080109 00224 SO 2008 1 9 C2XA07IA258 1 20071230 A 5610 12037394501 TRACK EMB 145 EMB145LR 3260212 SO COCKPIT DIRTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16987 145261 IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE CAPTAINS DV WINDOW WOULD NOT CLOSE. MAINTENANCE INSPECTED THE WINDOW, CLEANED THE TRACK AND LUBRICATED THE MECHANISM, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAF T WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008010900225 20080109 00225 EA 2008 1 9 MASA200700788 1 20071110 A 2750 860D10018ABCD FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37178 9455 7178 ASH FLT 2779 PHX - FLAPS FAIL IN TRANSIT 0 TO 8 DEGREES. REMOVED AND REPLACED FECU, RIG FLAPS, C/W PART A AND B. 2 L 7 2 4F RT A21EA 2008010900226 20080109 00226 EA 2008 1 9 TRAX200701987 1 20071222 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 AAR - BATHTUB FITTING CRACKED AT FS 461 RBL10 (MARKED). 2 L 7 2 4F RT A21EA 2008010900227 20080109 00227 EA 2008 1 9 TRAX200701988 1 20071222 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 AAR - CABIN FLOOR SUPPORT STRUCTURE CORRODED BLIND FASTENER HEAD RBL 35 & FS 349.00. 2 L 7 2 4F RT A21EA 2008010900228 20080109 00228 EA 2008 1 9 TRAX200701989 1 20071222 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 AAR - PAX DOOR AFT DRAG ANGLE IS CRACKED. 2 L 7 2 4F RT A21EA 2008010900233 20080109 00233 NM 2008 1 9 ASAA0752442 1 20071229 A 2421 761574B IDG BOEING 737 737890 1384527 NM NR 2 ENGINE MALFUNCTIONED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 577AS 35186 NR 2 DRIVE LIGHT DOES NOT ILLUMINATE WHEN ENGINE SHUT DOWN. FOUND IDG OVERSERVICED. DRAINED 1.5QTS OUT OF IDG. RESET AND RAN ENGINES, NO HELP. REPLACED NR 2 IDG. OFF IDG FILTERS SHOW NO CONTAMINATION. NO HELP FOR LIGHT. RESET NR 2 GC U CB BITE CHECK GOOD. LEAK OPS & DRIVE LIGHT CHECKS GOOD. 2 L 7 2 4F RT A16WE 2008010900244 20080109 00244 EA 2008 1 9 MASA200700762 1 20071031 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77181 7181 ASH FLT 7156 GSP - ROW 1-6 EMERGENCY PATH LIGHTING INOP. RESECURED CONNECTOR. 2 L 7 2 4F RT A21EA 2008010900248 20080109 00248 EA 2008 1 9 MASA200700688 1 20071012 A 5200 HANDLE CNDAIR CL600 CL6002B19 1900309 EA DOOR LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77302 7302 ASH FLT 7355, IAD - OUTER HANDLE WILL NOT CLOSE FROM INSIDE. CLEANED AND LUBED DOOR MECHANISM. 2 L 7 2 4F RT A21EA 2008010900281 20080109 00281 SO 2008 1 9 RAIA00712038 1 20071231 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 815HK 145048 PRE FLT 5452 - STL - EMERGENCY LIGHT INOP. MAINTENANCE RESECURED WIRING TO THE AFFECTED EMERGENCY LIGHT, OPS CHECKED GO OD. 2 L 7 2 4T RT T00011AT 2008010900282 20080109 00282 EA 2008 1 9 MASA200700730 1 20071023 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LOCKED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27172 7172 ASH 7264 - ORD - HAVING TROUBLE CLOSING THE PAX DOOR OUTER HANDLE. MX CLEARED THE HYDRO LOCK AND THE DOOR OPERATED NORM ALLY. 2 L 7 2 4F RT A21EA 2008010900283 20080109 00283 EA 2008 1 9 MASA200700846 1 20071203 A 3350 LS6006182 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH FLT 2720 PHX - SBA - FLOOR EMERGENCY LIGHTS INOP AT ROWS 9 THRU 11. REPLACED FLOOR LIGHT STRIP. 2 L 7 2 4F RT A21EA 2008010900284 20080109 00284 EA 2008 1 9 MASA200700930 1 20071231 A 5240 600332171001 CONTROL ARM CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17231 7231 ASH FLT 2985 PHX - SLC, SERVICE DOOR IS HARD TO OPEN. REMOVED AND REPLACED UPPER CONTROL ARM, OPS GOOD. 2 L 7 2 4F RT A21EA 2008010900285 20080109 00285 2008 1 9 MASA200700716 4 20071020 A 2561 P01074201 LIFE VEST CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 655BR 2772 7457 ASH FLT 1043 HNL - OVERNIGHT, LIFE VEST MISSING FROM SEAT 2F. MX INSTALLED A NEW LIFE VEST. 2 L 7 2 4F RT A21EA 2008010900286 20080109 00286 EA 2008 1 9 MASA200700718 1 20071021 A 2622 BA232171 EXTINGUISHER CNDAIR CL600 CL6002B19 1900309 EA LAVATORY DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 570ML 18410 7206 ASH FLT 7400 HSV-IAD, LAV FIRE EXTINGUISHER HAD NO CHARGE. REMOVED AND REPLACED FIRE EXTINGUISHER. 2 L 7 2 4F RT A21EA 2008010900287 20080109 00287 EA 2008 1 9 MASA200700719 1 20071021 A 2560 SMOKE GOGGLES CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27173 7173 ASH FLT 7184 ORD-ATW. CAPTAIN'S, FO'S AND OBSERVER'S SMOKE GOGGLES MISSING INSPECTION STICKERS. MX INSPECTED THE SMOKE GOGGLES AND INSTALLED NEW STICKERS. 2 L 7 2 4F RT A21EA 2008010900288 20080109 00288 EA 2008 1 9 MASA200700720 1 20071021 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A MASA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 75998 7336 ASH 7322 - ROC-ORD, WHILE ON APPROACH TO LAND THE CREW INITIATED A GO AROUND, AND GOT A FLAPS FAIL. MX COMPLIED WITH P ART "A". 2 L 7 2 4F RT A21EA 2008010900289 20080109 00289 EA 2008 1 9 MASA200700764 1 20071101 A 5240 LOCK CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR OUT OF ADJUST A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 592ML 7410 ASH 7263 ORD - REPORTED SERVICE DOOR WILL NOT LOCK IN THE OPEN POSITION. MX ADJUSTED THE LOCK ASSY. 2 L 7 2 4F RT A21EA 2008010900290 20080109 00290 EA 2008 1 9 MASA200700902 1 20071218 A 5420 22850080802 ACCESS PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NR 2 NACELLE DEPARTED A MASA O OTHER O OTHER LD LANDING 1 SW 07 75993 14300 7372 ASH FLT 7307 ORD - THE NR 2 ENG LOWER COWL DEPARTED THE AIRCRAFT AFTER LANDING. MX REMOVED AND REPLACED BLOCKER DOORS A ND SUPPORT HINGES, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2008010900296 20080109 00296 EA 2008 1 9 MASA200700872 1 20071213 A 5520 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA RT ELEVATOR DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 75994 7367 FWD L/E OF RT ELEVATOR IS BENT UP BY EACH HINGE POINT. PERFORMED PERM REPAIR. 2 L 7 2 4F RT A21EA 2008010900297 20080109 00297 EU 2008 1 9 U2RA743LP3476 1 20071221 A 3260 DN1050ZMK2 INDICATION SYS BAG JETSTM JETSTM3101 1500215 EU MLG INOPERATIVE A U2RA A UNSCHED LANDING P NO WARNING INDICATION AP APPROACH 1 GL 23 743PE 755 LANDING GEAR, NO GREEN LIGHTS ON EXTENSION, COMPLETED MANUAL EXTENSION PROCEDURES. NOSE GEAR, NO GREEN LIGHT, MAIN INDI CATION OK. 2 L 7 2 4T RT A21EU 2008010900298 20080109 00298 EA 2008 1 9 MASA200700507 1 20070817 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 47202 7202 ASH 7188 ORD - EMERGENCY LIGHT AT ROW 2 INOP. MX RELAMPED AND OP CHECKED GOOD. 2 L 7 2 4F RT A21EA 2008010900300 20080109 00300 EA 2008 1 9 MASA200700692 1 20071013 A 3350 BM10006002 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17231 7231 ASH FLT 2818 DSM - OVERNIGHT, LT NR 5 EXTERNAL EMERGENCY LIGHT INOP. MX REPLACED THE LAMP AND IT OP CHECKED GOOD. 2 L 7 2 4F RT A21EA 2008010900301 20080109 00301 EA 2008 1 9 MASA200700693 1 20071013 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27318 7318 ASH FLT 2783 - PHX - CREW REPORTED THAT THE FLOOR EMERGENCY LIGHTS AT ROWS 1-5 ARE INOP. MX FOUND BAD CONNECTOR ON LIGH T STRIP. REMOVED AND REPLACED CONNECTOR AND INVERTER. 2 L 7 2 4F RT A21EA 2008010900302 20080109 00302 EA 2008 1 9 MASA200700699 1 20071015 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 593ML 7465 ASH FLT 7369 IAD - EMERGENCY EXIT FLOOR LIGHTS INOP AT ROW 2, 3, 4 AND 5. MX RECONNECTED LOOSE WIRE AT ROW 2 CONNECTIO N, OPS NORMAL. 2 L 7 2 4F RT A21EA 2008010900303 20080109 00303 EA 2008 1 9 MASA200700703 1 20071016 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17358 7358 ASH 2751 SBP - ONE OVERWING EXIT LIGHT INOP, RELAMPED. 2 L 7 2 4F RT A21EA 2008010900307 20080109 00307 SO 2008 1 9 C2XA08IA002 1 20071225 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 14105 145649 IAH - FLIGHT 2901 THE CREW REPORTED SMOKE SMELL FROM THE RECIRC FANS. THE AIRCRAFT LANDED AT IAH UNEVENTFULLY WHERE MAI NTENANCE INSPECTED THE AIRCRAFT, OPS CHECKED THE RECIRC FANS ALL WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. 2 L 7 2 4F RT 2008010900311 20080109 00311 EA 2008 1 9 MASA200700717 1 20071020 A 3350 BR9279013 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27191 7191 ASH FLT 2818 DSM- OVERNIGHT, EMERGENCY EXIT SIGNS AT THE PAX DOOR AND SERVICE DOOR INOP. REPLACED FWD FLOOR PATH LIGHTI NG STRIP. 2 L 7 2 4F RT A21EA 2008010900313 20080109 00313 EA 2008 1 9 MASA200700524 1 20070827 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER CR CRUISE 1 SW 07 17358 7358 ASH 2741 - PHX-PSP - REPORTED A CABIN CEILING LIGHT INOP. MX RELAMPED THE LIGHT. 2 L 7 2 4F RT A21EA 2008010900314 20080109 00314 EA 2008 1 9 MASA200700526 1 20070828 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75984 7489 ASH 7345 IAD - CREW REPORTED THE EXTERIOR PAX DOOR EMERGENCY LIGHT INOP. MX RELAMPED LIGHT. 2 L 7 2 4F RT A21EA 2008010900316 20080109 00316 EA 2008 1 9 MASA200700536 1 20070830 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7264V 7264 LEFT OVERWING EXTERIOR EMERGENCY LIGHT NR 3 INOP, MX RELAMPED. 2 L 7 2 4F RT A21EA 2008010900317 20080109 00317 GL 2008 1 9 C2XA08CL001 2 20071229 A 7530 23054148 TUBE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 ENGINE BROKEN A C2XA O OTHER O OTHER CL CLIMB 1 SW 27 15574 145639 CAE311713 CLE FLIGHT 4931 THE CREW REPORTED ON CLIMBOUT THE NR 1 ENGINE FUEL BURN WAS APPROX 300 LBS MORE THAN THE NR 2 ENGINE. T HE NR 1 ITT INDICATION WAS ALSO 100 DEGREES HIGHER. THE ITT WAS CONTINUING TO CLIMB WITH ALTITUDE UNTIL THE CREW ASKED ATC TO DESCEND. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE RIGHT COMPRESSOR DISCHARGE AIR TUBE. OPERATIONAL CH ECKS GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008010900319 20080109 00319 EA 2008 1 9 MASA200700554 1 20070905 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77331 7331 ASH FLT RON 7240 DSM - NR 7 EXTERIOR EMERGENCY LIGHT INOP. MX RELAMPED THE EMERGENCY LIGHT, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008010900321 20080109 00321 EA 2008 1 9 MASA200700555 1 20070905 A 3350 587387221 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75987 7405 ASH FLT 7265 ROA - EMERGENCY PATH LIGHTING INOP. MX REPLACED LIGHT STRIP, OPS GOOD. 2 L 7 2 4F RT A21EA 2008010900325 20080109 00325 EA 2008 1 9 MASA200700563 1 20070908 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77302 7302 ASH FLT 7355, IAD - RT FORWARD FUSELAGE EMERGENCY LIGHT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2008010900328 20080109 00328 EA 2008 1 9 MASA200700570 1 20070912 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77286 7286 ASH FLT 2766 PHX - SERVICE DOOR FLOOR EMERGENCY EXIT SIGN LIGHTS BURNED OUT. MX RELAMPED LIGHTS. 2 L 7 2 4F RT A21EA 2008010900329 20080109 00329 EA 2008 1 9 MASA200700572 1 20070912 A 3350 LENS CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75984 7489 ASH FLT 7163 - CLE-IAD - PAX DOOR EMERGENCY EXIT LIGHT LENS MISSING. CONTRACT MX WAS ABLE TO FIND LENS AND RESECURED IT . 2 L 7 2 4F RT A21EA 2008010900331 20080109 00331 EA 2008 1 9 MASA200700578 1 20070913 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75993 7372 ASH FLT 7341 IAD - EMERGENCY FLOOR PATH LIGHTING FWD STRIP IS OFF THE TRACK. MX RESECURED THE STRIP AND OPS CHECKED. 2 L 7 2 4F RT A21EA 20081210 WP 2008 12 10 K11A2008120391501 1 20070322 A 2133 10256852 OUTFLOW VALVE DOUG DC9 DC915F 3022037 WP CABIN PRESSURE MALFUNCTIONED A KCSA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 23 915CK 47086 CABIN WILL NOT PRESSURIZE. 2 L 7 2 4F A6WE 20081211 NM 2008 12 11 K11A2008121072012 1 20070721 A 5330 SKIN BOEING 727 7272B6 138407J NM FUSELAGE DENTED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 FUSELAGE SKIN DENTED. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008121072018 1 20070718 A 5320 FLOOR SUPPORT BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 CORROSION ON MAIN DECK FLOOR SUPPORT. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008120972001 1 20070719 A 5320 FLOOR SUPPORT BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 FLOOR SUPPORT HAS AREA OF CORROSION AROUND NUT PLATES. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008120972003 1 20070719 A 5320 FLOOR SUPPORT BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 FLOOR SUPPORT HAS AREA OF CORROSION AROUND NUT PLATES. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008120972005 1 20070719 A 5320 FLOOR SUPPORT BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21A98 FLOOR SUPPORT L-ANGLE HAS AREA OF CORROSION AROUND NUT PLATES. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008121072015 1 20070718 A 5312 STIFFENER BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 AFT PRESSURE BULKHEAD STIFFENER HAS CORROSION. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008121072016 1 20070718 A 5322 SHEAR TIE BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 SHEAR TIE HAS CORROSION ON AFT SIDE. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008121072017 1 20070718 A 5322 SHEAR TIE BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 SHEAR TIE HAS CORROSION ON AFT SIDE. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008120972007 1 20070724 A 5322 SHEAR TIE BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 SHEAR TIE HAS AREA OF CORROSION. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008120972008 1 20070724 A 5322 SHEAR TIE BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 SHEAR TIE HAS AREA OF CORROSION. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008120972010 1 20070719 A 5320 STRAP BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 FLOOR SUPPORT STABILIZATION STRAP HAS AREA OF CORROSSION UNDER NUT PLATES. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008120972011 1 20070719 A 5320 STRAP BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 FLOOR SUPPORT HORIZONTAL STABILIZATION STRAP HAS AREA OF CORROSION UNDER NUT PLATES. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008121072001 1 20070719 A 5322 SHEAR TIE BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 SHEAR TIE HAS AREA OF CORROSION ON FWD SIDE. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008121072013 1 20070719 A 5320 STIFFENER BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 CORROSION ON BACK SIDE OF VERTICAL STIFENER. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008120972002 1 20070719 A 5320 FLOOR SUPPORT BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 FLOOR SUPPORT HAS AREA OF CORROSION AROUND NUT PLATES. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008120972006 1 20070719 A 5320 FLOOR SUPPORT BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 FLOOR SUPPORT HAS AREA OF CORROSION AROUND NUT PLATES. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008121072014 1 20070717 A 5320 WEB BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 MAIN DECK FLOOR WEB, LOWER SIDE HAS AREA OF CORROSION. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008120972009 1 20070719 A 5320 FLOOR SUPPORT BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 FLOOR SUPPORT HAS AREA OF CORROSION UNDER NUT PLATES. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008121072002 1 20070718 A 5322 SHEAR TIE BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 SHEAR TIE HAS AREA OF CORROSION ON AFT SIDE. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008121072004 1 20070718 A 5311 FRAME BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 FORWARD BILGE FUSELAGE FRAME HAS CORROSION. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008121072006 1 20070722 A 5322 SHEAR TIE BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 FWD PIT CORROSION ON SHEAR TIE. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008121072008 1 20070718 A 5313 STRINGER BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 FWD BILGE CORROSION ON STRINGER AT UPPER FLANGE. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008121072009 1 20070717 A 5310 DOOR FRAME BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 OVERWING ESCAPE HATCH LOWER EDGE FRAME HAS CORROSION (RT AFT OVERWING HATCH). 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008121072010 1 20070721 A 5330 SKIN BOEING 727 7272B6 138407J NM FUSELAGE DENTED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 EXTERNAL FUSELAGE SKIN HAS A DENT. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008121072011 1 20070719 A 5511 SPAR BOEING 727 7272B6 138407J NM HORIZ STAB CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 RT HORIZONTAL STAB AFT REAR LOWER SPAR CHORD CORRODED (STAB STA 68.92 TO 78.13). 2 L 7 3 4F A3WE 20081231 NM 2008 12 31 K11A2008123072308 1 20070102 A 5315 FLOORBEAM BOEING 727 7272H3 138368N NM FUSELAGE CRACKED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 723CK 20545 FLOORBEAM HAS CRACK. 2 L 7 3 4F RT A3WE 20081231 NM 2008 12 31 K11A2008122972307 1 20070109 A 5330 SKIN BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 723CK 20545 CORROSION ON SKIN, AFT PIT. 2 L 7 3 4F RT A3WE 20090106 NM 2009 1 6 K11A2008123172311 1 20071009 A 3211 BEAM BOEING 727 7272H3 138368N NM LT MLG CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 723CK 20545 LT MLG BEAM LOWER SURFACE CORROSION HAS CORROSION IN AND AROUND FASTENER HOLES. 2 L 7 3 4F RT A3WE 2007073100001 20070731 00001 NM 2007 7 31 ASMF200707016 1 20070727 A 3240 284702 CONTROL VALVE DOUG MD80 MD83 3023681 NM BRAKES OUT OF ADJUST W ASMF D RETURN TO BLOCK E M J VIBRATION/BUFFET OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 838AM 23171 23171 49397 AIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXI RIGHT BREAKES JAMED WITH VIBRATION AND HIGH TEMPERATURE. SYSTEM WAS VER IFIED BY MAINTENANCE PERSONNEL AND THERE WERE DETECTED THE LEFT BREAK CONTROL VALVE DESAJUSTED; THE VALVE WAS ADJUSTED I AW MM 32-42-00, TESTED CORRECT. 2 L 7 2 4F RT 2007061900010 20070619 00010 NM 2007 6 19 SWAA072927 1 20070611 A 5322 69353656 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007061800213 20070618 00213 NE 2007 6 18 3732060207 2 20070602 A 7321 02929858360 HYDROMECH UNIT UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B 60037 NE ENGINE UNCONTROLLABLE E QMLA R A AUTOROTATION UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 NM 03 151AC 1609 3732 23065 ON A LOCAL TRANSPORT FLT , THE AIRCRAFT LAUNCHED AT 0930 P.M. & FLT TO PICK UP THE PATIENT WAS UNEVENTFUL. THE HOSPITAL IS A 15 MIN. FLT. WITH THE PATIENT ON BOARD, (5 PAX TOTAL), AT 2000 FT. MSL IN CRUISE FLT AT 110 KTS & 3 OR 4 MINUTES IN TO THE FLT, A LOUD JOLT WITH A YAW OF THE A/C WAS FELT. THE PILOT DETERMINED THERE WAS NOTHING DROPPED BY MED CREW. THE PILOT REQUESTED TO DIVERT TO THE AIRPORT. APC ASKED IF THERE WAS A PROBLEM & THE PILOT ADVISED THERE WAS A POSSIBLE PROB LEM. THE APT WAS ONLY 4-5 MILES TO THE S.W. THE PILOT DID NOT HAVE WARNING LIGHTS OR AURAL ALARMS. THE FLT PROCEEDED TO THE APT & PLANNED TO MAKE A SHALLOW LONG DESCENT TO THE APT. THE TWR ADVISED THAT HE COULD LAND IN THE RUN-UP AREA OF RW 1 G 7 2 3U 3 U H9EU E00054EN 2007022000349 20070220 00349 NM 2007 2 20 07FDEA00354 1 20070206 A 5311 FRAME BOEING 727 727233 138408A NM ZONE 100 DAMAGED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 284FE 22621 AFT PIT FRAME AT STA 1148, LOWER CHORD HAS MISDRILLED HOLE JUST BELOW STR 23L REMOVED DAMAGE NDT. NO DEFECTS NOTED, FAB BED AND INSTALLED SHEAR TIE ANGLE REPAIR REF SRM 51-30-2 PG 1-12, SRM 51-40-3 PG 2 FIG 1, SRM 53-10-4 PG 46-49 AND BOEIN G DWG 65-16348. CLASSIFIED AS MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007022000351 20070220 00351 NM 2007 2 20 AALA20070175 1 20070123 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR CEILING INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT NUMBER ONE CEILIN G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007022000352 20070220 00352 NM 2007 2 20 AALA20070176 1 20070123 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 786AN 30250 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR FLOOR MOUNTED INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT LEFT NUMB ER ONE FLOOR MOUNTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007022000353 20070220 00353 NM 2007 2 20 AALA20070170 1 20070123 A 3350 1317 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 182AN 29592 SFO - EMERGENCY LIGHT AT OVERHEAD SEAT 3B INOPERATIVE. RELAMPED EMERGENCY LIGHT AT OVERHEAD SEAT 3B. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007022000354 20070220 00354 NM 2007 2 20 AALA20070171 1 20070122 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 921AN 29522 TUL - BATTERY PACK FOR EMERGENCY LIGHTS IN COACH FAILED FUNCTIONAL TEST. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007022000357 20070220 00357 NM 2007 2 20 ZZDA070123123 1 20070123 A 5350 RADOME BOEING 717 717200 1383700 NM FUSELAGE DENTED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. RADOME ASSEMBLY DENTED. REPLACED RADOME ASSEMBLY PER 717 AMM CHAPTER 53 -51-01 REV 27 DATED 01/01/07. 2 L 7 2 4F TR A6WE 2007022000358 20070220 00358 NM 2007 2 20 ZZDA070123124 1 20070123 A 5280 SUPPORT BOEING 717 717200 1383700 NM NLG DOOR CRACKED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. AFT SUPPORT OF THE FWD LEFT NLG DOOR CRACKED. REPLACED AFT SUPPORT OF T HE FWD LEFT NLG DOOR PER MDC DRAWING 9957851 REV S DATED 01/26/00 AND DRAWING 9957852 REV Y DATED 01/26/00. 2 L 7 2 4F TR A6WE 2007022000359 20070220 00359 NM 2007 2 20 ZZDA070123125 1 20070123 A 3250 SUPPORT FITTING BOEING 717 717200 1383700 NM NLG STEERING CRACKED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. NLG STEERING VALVE SUPPORT FITTING CRACKED. REPLACED NLG STEERING VALVE SUPPORT FITTING AT STA 83.5 PER MDC DRAWING 5910098 REV R DATED 01-24-06. 2 L 7 2 4F TR A6WE 2007022000368 20070220 00368 NM 2007 2 20 ZZDA070123131 1 20070123 A 3070 8921536G3 DRAIN MAST BOEING 717 717200 1383700 NM FWD DAMAGED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. DRAIN MAST DAMAGED. REPLACED DRAIN MAST PER 717 AMM CHAPTER 30-72-02 RE V 27 DATED 01/01/07. 2 L 7 2 4F TR A6WE 2007022000373 20070220 00373 NM 2007 2 20 2007UALA00348 1 20070207 A 5512 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZ STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 RIGHT STAB LOWER SKIN CRACKED AT LOWER SKIN AT REAR SPAR FASTENER FWD OF ACCESS PANEL 9028 APPROX STAB STA 153 AND BETWE EN ELEV STA 94.07 AND 121.59. MAJOR REPAIR. REMOVED DAMAGE. ACCOMPLISHED A DOUBLER AND FILLER REPAIR PER SRM 55-10-01 REPAIR 6 PAGE 201 TO 205. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022000376 20070220 00376 NM 2007 2 20 2007UALA00351 1 20070207 A 5314 KEELBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 FWD PIT AC DISTRIBUTION BAY LEFT KEEL BEAM STA 500D APPROX 3 INCHES AFT. MAJOR REPAIR. REMOVED DAMAGE. ACCOMPLISHED N ESTED ANGLE REPAIR PER SRM 53-30-12 REPAIR 2. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022000387 20070220 00387 NM 2007 2 20 QXEA200700205 1 20070203 A 5310 STRUCTURE BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 415QX 4081 C2 PDX - LAVATORY EXTERIOR SERVICE PANEL MOUNTING FLANGE HAS EXFOLIATION CORROSION ALONG BOTTOM EDGE AT FS X-5.0 AND STR INGER 27S. REPAIRED IAW RD8/4-53-347. 2 H 7 2 4T RT A13NM 2007022000396 20070220 00396 NM 2007 2 20 QXEA200700168 1 20070210 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - GOUGE ON THE INNER SKIN OF THE BAGGAGE DOOR 46 1/2" FROM THE TOP AND 2 1/2" FROM THE AFT SIDE. REPAIRED IAW SR M 51-20-11, 51-20-16, AND 51-20-36. 2 H 7 2 4T RT A13NM 2007022000410 20070220 00410 NM 2007 2 20 QXEA200700187 1 20070213 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 541 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - RIGHT OUTBOARD SEAT TRACK NR 12 HAS CORROSION ON EDGE OF CLAW AT STATION X541. REPAIRED IAW RD8-53-3644. 2 H 7 2 4T RT A13NM 2007022100036 20070221 00036 2007 2 21 2007UALA00371 4 20070208 A 2565 LINKAGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 GIRT BAR OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 87UA 26713 DOOR 2R FAILS ARM-DISARM CHECK. ADJUSTED LINKAGE BETWEEN SELECTOR LEVER AND GIRT BAR MECH. ADJUSTED PUSH ROD AND GIRT B AR CARRIER, NO COMPONENTS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100047 20070221 00047 NM 2007 2 21 QXEA200700207 1 20070214 A 3040 SYLZ50970 CONTROLLER DHAV DHC8 DHC8202 2809007 NM WINDSHIELD HEAT MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 365PH 299 59 526 PDX FLIGHT NR 2190, LEFT WINDSHIELD HOT CAUTION ILLUMINATED ON TAXI OUT WITH HEAT SELECTOR SET TO NORM. AS PER MTX CONT ROL RESET THE SWITCH AND THE CAUTION LIGHT CAME ON AGAIN AFTER 30 SECONDS. LIGHT EXTINGUISHES IMMEDIATELY WHEN SELECTED TO WARM UP. MAINTENANCE REPLACED 3041-K6 AND 3041-K9 RELAYS. REPLACED CAPTAINS WINDSHIELD HEAT CONTROLLER. OPERATION AL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007022100059 20070221 00059 EU 2007 2 21 AALA20070273 1 20070203 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70073 516 MIA - FOUND EMERGENCY LIGHT AT SEAT 36C INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 36C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007022100060 20070221 00060 NE 2007 2 21 AALA20070281 2 20070204 A 7200 ENGINE BOEING 757 757223 1384957 NM RROYCE RB211 RB211535C37 54555 NE RIGHT FAILED A AALA A UNSCHED LANDING Y M J ENGINE STOPPAGE OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 601AN 27052 31153 MIA - INFLIGHT T922/04FEB - AFTER TAKEOFF RIGHT ENGINE COMPRESSOR STALLED WITH UNCOMMANDED ENGINE SHUTDOWN FOLLOWED BY E NGINE GAS TEMPERATURE OVER TEMPERATURE INDICATION. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2007022100061 20070221 00061 WP 2007 2 21 AALA20070178 1 20070124 A 5280 HINGE DOUG DC9 DC982 3022082 WP GEAR DOOR LOOSE A AALA O OTHER O OTHER CL CLIMB 1 SW 21 233AA 49180 DFW INFLIGHT T841/24JAN - LEFT MAIN LANDING GEAR LIGHT UNSAFE REMAINED ILLUMINATED AFTER GEAR RETRACTION. SOUNDED LIKE DOOR WAS PARTIALLY OPEN. GEAR WAS CYCLED AND UNSAFE LIGHT WAS EXTINGUISHED. FOUND FORWARD HINGE ON LEFT MAIN GEAR DOOR LOOSE AND MISSING FASTENERS. REMOVED AND REPLACED LEFT MAIN GEAR DOOR HINGE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007022100075 20070221 00075 NM 2007 2 21 AALA20070289 1 20070205 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 632AA 24590 DFW - AFT SEAT MOUNTED EMERGENCY LIGHT AT SEAT 6E INOPERATIVE. REPLACED AFT SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY FOR S EAT 6E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007022100084 20070221 00084 WP 2007 2 21 AALA20070287 1 20070205 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 467AA 49597 LGA - EMERGENCY LIGHTS AT SEAT ROWS 18 TO 29 INOPERATIVE. REPLACED BATTERY PACK AT B5106 FOR EMERGENCY LIGHTS AT SEAT R OWS 18 TO 29 SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007022100085 20070221 00085 NM 2007 2 21 AALA20070268 1 20070203 A 3397 WIRE HARNESS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 904AN 29506 MIA - FOUND EMERGENCY LIGHT AT SEAT 3E INOPERATIVE. REPAIRED SEAT HARNESS FOR INOPERATIVE EMERGENCY LIGHT AT SEAT 3E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007022100106 20070221 00106 NM 2007 2 21 AWXA200700183 1 20070120 A 5320 65C3267712 CHANNEL BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 MCN - MAIN CABIN FLOOR STRUCTURE WEB STIFFENER CRACKED, BS 986 - BS 1006, LBL 40.5. REPLACED MAIN CABIN FLOOR STRUCTURE WEB STIFFENER, BS 986 - BS 1006, LBL 40.5 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007022100107 20070221 00107 WP 2007 2 21 AALA20070168 1 20070123 A 3350 L201919 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 248AA 49259 LGA - EMERGENCY LIGHT AT AFT SERVICE DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT AFT SERVICE DOOR. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007022100108 20070221 00108 NM 2007 2 21 AALA20070169 1 20070123 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 182AN 29592 SFO - FOUND EMERGENCY LIGHT AT SEAT 28D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A2NM 2007022100109 20070221 00109 NM 2007 2 21 AALA20070173 1 20070109 A 5330 SKIN BOEING 767 767223 1385123 NM BS 1582 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 328AA 22328 AFW - FUSELAGE SKIN AT STATION 1582 AT BUTT SPLICE BETWEEN SECTION 46 AND 48 HAD CORROSION. CUT OUT CORROSION AT STATIO N 1582 AT BUTT SPLICE BETWEEN SECTION 46 AND 48 AND INSTALLED REPAIR DOUBLER PER DRAWING 146T3340. 2 L 7 2 4F RT A1NM 2007022100128 20070221 00128 NM 2007 2 21 UIEA200700012 1 20070122 A 5730 PANEL BOEING 747 7472D7B 1384803 NM RT WING DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 527MC 22471 RT WING INBOARD LEADING EDGE PANEL AT WBL 158.0 HAS A 2.0 INCH LONG BY 1.5 INCH WIDE BY .073 INCH DEEP DENT. ACCOMPLISH ED PERMANENT REPAIR AS PER B747-200 SRM 51-40-09 FIG 18 SHEET 1 THRU 5. ALSO, REFERENCE ATLAS AIR EO NO. 4757A314. 2 L 7 4 4F RT A20WE 2007022100129 20070221 00129 NM 2007 2 21 UIEA200700013 1 20070122 A 2510 10751 SEAT BOEING 747 7472D7B 1384803 NM COCKPIT CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 CRACK AND GOUGES WERE FOUND ON 2ND OBSERVER SEAT. REPAIR ACCOMPLISHED AS PER EO NR 4725A223 AND FAA FORM 8110-3 DATED 1 7 JAN 2007. 2 L 7 4 4F RT A20WE 2007022100138 20070221 00138 NM 2007 2 21 2007UALA00428 1 20070213 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT EEL LIGHTS INOPERATIVE AT SEATS 33 RT & 39 RT. REPLACED LAMP ASSY AT BOTH SEATS. ALL EEL LIGHTS OP. CHEC K NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022100139 20070221 00139 NM 2007 2 21 2007UALA00429 1 20070213 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EEL LIGHT INOPERATIVE AT DOOR 4 GALLEY RIGHT AFT AISLE. FOUND LOOSE CONNECTOR. SECURED CONNECTOR. OPS. CKS. NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022100151 20070221 00151 NM 2007 2 21 2007UALA00441 1 20070213 A 2421 LINE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LT IDG LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 783UA 26950 FLIGHT DIVERTED DUE TO LEFT GENERATOR PROBLEM. FOUND INTEGRATED DRIVE GENERATOR (L) OIL LEVEL IS LOW. FOUND IDG OIL SE RVICE LINE LEAKING. REPLACED LINE. RAN ENGINE AFTER IDG SVCE LINE INSTALLED. IDG OPS NORMALLY. A/C RETURNED TO SERVICE . 2 L 7 2 4F 4 F RT T0001SE E46NE 2007022100158 20070221 00158 NM 2007 2 21 2007UALA00448 1 20070213 A 3350 POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 668UA 30024 EMERGENCY EXIT LIGHTS FROM ROW 20 - 25 FLASHING ON AND OFF ON LEFT SIDE OF AIRCRAFT. REPLACED POWER SUPPLY M1559 PER MM 33-51-07. EMERGENCY LIGHTS TEST OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022100173 20070221 00173 NM 2007 2 21 2007UALA00259 1 20070130 A 2910 HOSE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE GREEN HYD SYS LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 849UA 1649 RTFL DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. LT MLG DOOR ACTUATOR AFT HOSE LEAKING. REPLACED HOSE. SERVICED GREEN HYD RAULIC SYSTEM AFTER GEAR DOOR HOSE REPLACED AND CYCLE ALL COMPONENTS TO BLEED AIR FROM SYSTEM, PUMP DID NOT RUN DRY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100174 20070221 00174 NM 2007 2 21 2007UALA00260 1 20070130 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 783UA 26950 AFT EEL LIGHT MISSING AT SEAT 1E. REPLACED THE MISSING LIGHT ASSY. OPS CHECKED OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007022100179 20070221 00179 NE 2007 2 21 2007UALA00265 2 20070131 A 7230 BLADES AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 1 ENGINE DAMAGED A UALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 WP 29 840UA 1522 V10981 ENGINE NR 1 STALL DISPLAYED ON UPPER ECAM SCREEN DURING STEADY STATE CLIMB OR CRUISE. ENGINE NOT SHUTDOWN. BORESCOPE I NSPECTION OF THE HPC REVEALED DAMAGE TO R6 BLADES BEYOND SERVICEABLE LIMITS. ENGINE WAS CHANGED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100212 20070221 00212 NM 2007 2 21 SWAA070614 1 20070205 A 5310 141A1120 DOOR FRAME BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 743SW 29279 DURING SCHEDULED 8Y CHECK, FOUND R1 DOOR CUTOUT FWD LOWER FRAME CRACKED AT BS 295, RBL 54. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007022100213 20070221 00213 WP 2007 2 21 ABXA079945 1 20070206 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 958AX 47760 EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00. 2 L 7 2 4F A6WE 2007022100214 20070221 00214 NM 2007 2 21 ABXA070047 1 20070208 A 3397 WIRE BOEING 767 767232 1385132 NM CABIN DAMAGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 740AX 22213 L1 EXTERIOR EMERGENCY LIGHTING AT STA 305, 315, & 317 IN SUPERNUMERARY AREA INOPERATIVE. REPAIRED WIRING AT PIN 9 OF CO NNECTOR J0984. TEST GOOD IAW B767 MM 33-51-00-5. 2 L 7 2 4F RT A1NM 2007022100215 20070221 00215 WP 2007 2 21 ABXA070046 1 20070207 A 3222 SEAL DOUG DC9 DC941 302207N WP NLG STRUT LEAKING A ABXA K NONE O OTHER CL CLIMB 1 GL 23 967AX 47509 LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. COMPLIED WITH ABNORMALS. FOUND NLG STRUT SERVICING 50 PSI LOW. STRUT DI D NOT EXTEND SMOOTHLY. REPLACED NLG STRUT SEALS IAW DC9 MM 32-21-02-8-0001. 2 L 7 2 4F A6WE 2007022100217 20070221 00217 WP 2007 2 21 ABXA070044 1 20070202 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 954AX 47612 EMERGENCY LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00. 2 L 7 2 4F A6WE 2007022100218 20070221 00218 WP 2007 2 21 ABXA070045 1 20070206 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 958AX 47760 EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00. 2 L 7 2 4F A6WE 2007022100220 20070221 00220 NM 2007 2 21 ASAA0741446 1 20070213 A 5210 6951337460 GUIDE ARM BOEING 737 7374Q8 138447Q NM L1 DOOR OUT OF ADJUST A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 773AS 25106 FLIGHT ATTENDANT UNABLE TO CLOSE THE L1 DOOR. ADJUSTED L1 GUIDE ARM AND HORIZONTAL PUSHROD PER AMM 52-11-00 PG 501, 518 . 2 L 7 2 4F RT A16WE 2007022100224 20070221 00224 NM 2007 2 21 ASAA0771462 1 20070213 A 5321 147A581020 FLOOR PANEL BOEING 737 737790 13844CN NM CABIN DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 FLOOR PANEL 242TF MISSING INSERT AND DELAMINATED. REPAIRED IAW SRM 53-00-50. 2 L 7 2 4F RT A16WE 2007022100226 20070221 00226 NM 2007 2 21 ASAA0771464 1 20070213 A 5321 147A5810175 FLOOR PANEL BOEING 737 737790 13844CN NM CABIN DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 FLOOR PANEL 221FG DELAMINATED. REPAIRED IAW SRM 53-00-50. 2 L 7 2 4F RT A16WE 2007022100227 20070221 00227 NM 2007 2 21 ASAA0771465 1 20070213 A 5321 147A5810237 FLOOR PANEL BOEING 737 737790 13844CN NM CABIN DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 FLOOR PANEL 222CF DELAMINATED. REPAIRED IAW SRM 53-00-50. 2 L 7 2 4F RT A16WE 2007022100228 20070221 00228 NM 2007 2 21 QXEA200700161 1 20070212 A 3040 UNKNOWN DHAV DHC8 DHC8202 2809007 NM WINDSHIELD HEAT UNKNOWN A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 365PH 526 SEA FLIGHT NR 2255 - LEFT WINDSHIELD HOT CAUTION ILLUMINATED WHEN NORM SELECTED. FOLLOWING PROCEDURES AND WARM UP SELEC TED CAUTION EXTINGUISHED. MAINTENANCE COMPLIED WITH OPERATIONAL CHECK OF THE CAPTAINS AND FIRST OFFICER WINDSHIELD HEAT ING SYSTEM IAW DHC-8-200 AMM TASK 30-41-00-710-801. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO S ERVICE. 2 H 7 2 4T RT A13NM 2007022100229 20070221 00229 NM 2007 2 21 ASAA0771466 1 20070213 A 5755 113A46173 SKIN BOEING 737 737790 13844CN NM NR 6 SPOILER PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 NR 6 SPOILER HAS TWO PUNCTURES. REPAIRED IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007022100231 20070221 00231 NM 2007 2 21 ASAA0741467 1 20070215 A 5242 6545830120 SKIN BOEING 737 7374Q8 138447Q NM E&E BAY DOOR CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 E&E BAY DOOR SKIN IS CHAFED ALONG FWD EDGE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 52-00 -01 REPAIR 3 FIGURE 201. 2 L 7 2 4F RT A16WE 2007022100233 20070221 00233 NM 2007 2 21 ASAA0741468 1 20070215 A 5320 6552878102 SILL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 L2 DOOR MOPSILL (INNER CHORD) IS CORRODED. REMOVED CORRODED CHORD, INSTALLED NEW CHORD IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007022100234 20070221 00234 NM 2007 2 21 ASAA0741469 1 20070215 A 5322 654659320 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 CORROSION ON SHEAR TIE. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW SRM 53-00-07 RE PAIR 3 FIG 201. 2 L 7 2 4F RT A16WE 2007022100235 20070221 00235 NM 2007 2 21 ASAA0741450 1 20070213 A 5753 6546430190 SKIN BOEING 737 7374Q8 138447Q NM RT FOREFLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 RIGHT I/B FORE FLAP O/B TRAILING EDGE CHAFED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-70-10 REPAIR 4. 2 L 7 2 4F RT A16WE 2007022100236 20070221 00236 NM 2007 2 21 ASAA0741451 1 20070213 A 5313 69770772 STRINGER SPLICE BOEING 737 7374Q8 138447Q NM FUSELAGE TOOL DAMAGE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 STRINGER SPLICE AT FUSELAGE HAS TOOL DAMAGE. REMOVED DAMAGED SPLICE, INSTALLED NEW STRINGER SPLICE IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007022100238 20070221 00238 NM 2007 2 21 ASAA0741471 1 20070218 A 5753 6546434369 SKIN BOEING 737 7374Q8 138447Q NM T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 LEFT I/B AFT FLAP DENTED ON LWR SURFACE. REMOVED DAMAGED AREA FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-70 -10. 2 L 7 2 4F RT A16WE 2007022100239 20070221 00239 NM 2007 2 21 DU4R2007045 1 20070124 A 5320 143N852215 INTERCOSTAL BOEING 757 757232 1384965 NM BS 1444 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 FOUND CORROSION AFT CARGO COMPARTMENT UPPER ATTACH ANGLE OF INTERCOSTAL AROUND NUTPLATES UNDERSIDE OF SIDE PANEL RT BETW EEN S-27R AND S-28R BS 1444. REMOVED WEB. FABRICATED AND INSTALLED INTERCOSTAL REPAIR 19.5" BY 6.0" FROM 7075-T6 .050" IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007022100242 20070221 00242 NM 2007 2 21 ASAA0741472 1 20070218 A 5753 6546434369 SKIN BOEING 737 7374Q8 138447Q NM T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 LEFT I/B AFT FLAP DENTED ON UPPER SURFACE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51 -70-10. 2 L 7 2 4F RT A16WE 2007022100245 20070221 00245 NM 2007 2 21 ASAA0741473 1 20070218 A 5322 65465648 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 SHEAR TIE AT STA 986 BETWEEN STR 26R 26L IS CORRODED. REMOVED CORRODED SHEAR TIE, INSTALLED NEW SHEAR TIE IAW SRM 51-40 -02. 2 L 7 2 4F RT A16WE 2007022100247 20070221 00247 NM 2007 2 21 ASAA0741474 1 20070218 A 5320 6517688175 SILL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 CORROSION ON L1 DOOR SILL INNER CHORD. REMOVED CORRODED CHORD, INSTALLED NEW CHORD IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007022100249 20070221 00249 NM 2007 2 21 ASAA0741475 1 20070218 A 5320 65558853 SHEAR WEB BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 SHEAR WEB CORRODED. REMOVED CORRODED SHEAR WEB, INSTALLED NEW SHEAR WEB IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007022100257 20070221 00257 NM 2007 2 21 ASAA0771453 1 20070213 A 5320 141A541016 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 FWD CABIN FLOOR INTERCOSTAL CRACKED AT BS 335. REPAIRED IAW SRM 51-70-11. 2 L 7 2 4F RT A16WE 2007022100259 20070221 00259 NM 2007 2 21 ASAA0771454 1 20070213 A 5320 141A541012 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 FWD CABIN FLOOR INTERCOSTAL IS CRACKED AT FS 322. REPAIRED IAW SRM 51-70-11. 2 L 7 2 4F RT A16WE 2007022100260 20070221 00260 SO 2007 2 21 CHQA200700005 1 20070201 A 2120 UNKNOWN EMB 135 EMB135KL 3260302 SO COCKPIT ODOR A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 381SK 145619 FLIGHT 5371 - CMH-STL - UPON REACHING CRUISE FLIGHT AT 26,000 FEET, THRUST MODE WAS CRUISE, WINDSHIELD HEAT ON, ANTI-ICE AUTO, NOTICED AND ODOR THAT SMELLED LIKE HOT ELECTRICAL WIRING. THE ODOR WAS INCREASING AND THE FO CONFIRMED SMELLING THE SAME THING. FLIGHT ATTENDANT ALSO CONFIRMED SMELL. COMPLETED QRH FOR SMOKE/FIRE AND DETERMINED TO LAND IMMEDIATELY . NO EMERGENCY DECLARED. LANDED UNEVENTFULLY. MAINTENANCE INSPECTED AND WAS UNABLE TO DUPLICATE FAULT. 2 L 7 2 4F RT T00011AT 2007022100262 20070221 00262 EA 2007 2 21 A6WA200740046 1 20070124 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 447AW 7812 RT WING LOWER PLANK FUEL TANK ACCESS DOOR CUT OUT HOLE NR 2 (610AB) HAS MINOR PITTING AT IB END IN AN AREA APPROX 1.5 IN CH LONG BY .005 INCH DEEP IN NON-CRITICAL AREA. (M) MAINTENANCE REPAIRED WING PLANK HOLE NR 2 (610 AB) IAW REO 601R-57 -21-030 REV F AND EO E06/021/457, REV A. (K) 2 L 7 2 4F RT A21EA 2007022100263 20070221 00263 NM 2007 2 21 ASAA0771455 1 20070213 A 5320 141A541012 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 FWD CABIN FLOOR INTERCOSTAL IS CRACKED AT FS 320. REPAIRED IAW SRM 51-70-11. 2 L 7 2 4F RT A16WE 2007022100264 20070221 00264 EA 2007 2 21 A6WA200740047 1 20070124 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 447AW 7812 RT WING LOWER PLANK FUEL TANK ACCESS DOOR CUT OUT HOLE NR 8 (PNL 640FB) HAS MINOR CORROSION AT IB AND OB ENDS APPROX 3 I NCH LONG BY .003 INCH DEEP AT IB END AND 1.25 INCH LONG BY .002 INCH DEEP AT OB END. BOTH IN NON-CRITICAL AREA. (M)MAI NTENANCE REPAIRED WING PLANK HOLE NR 8 (640FB) IAW REO 601R-57-21-030 REV F AND E06/021/457 REV A. (K) 2 L 7 2 4F RT A21EA 2007022100266 20070221 00266 NM 2007 2 21 ASAA0771456 1 20070213 A 5315 147A55068 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 CABIN FLOORBEAM CORRODED AT FS 986.5. REPAIRED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 2007022100268 20070221 00268 EU 2007 2 21 MALA070023 1 20070204 A 3260 UPLOCK SWITCH SAAB SF340 340B 7860101 EU MLG DIRTY A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 425XJ 340B425 AFTER GEAR RETRACTION, THE GEAR HANDLE INTRANSIT LIGHT REMAINED ILLUMINATED UNTIL OVERRIDE WAS SELECTED. CLEANED AND LU BED UPLOCK SWITCHES AND SERVICED HYDRAULIC QUANTITY IAW AMM CH 12-10-29. PERFORMED FUNCTIONAL CHECK OF GEAR IAW AMM CH 32-30-00. SWUNG GEAR SEVERAL TIMES, NO DEFECTS NOTED. 2 L 7 2 4T RT A52EU 2007022100269 20070221 00269 NM 2007 2 21 ASAA0771458 1 20070213 A 5321 147A581018 FLOOR PANEL BOEING 737 737790 13844CN NM CABIN CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 CABIN FLOOR PANEL 241XF IS CRACKED. REPAIRED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 2007022100270 20070221 00270 NM 2007 2 21 02072007 1 20070204 A 3260 106180349 LIGHT BOEING 737 7372L9 1384497 NM PWA JT8 JT8D9A 52048 NE MLG INDICATOR FAILED A KNNA B EMER. DESCENT P NO WARNING INDICATION LD LANDING 1 WP 25 465AT 21279 WHILE LANDING AT KLAX, DID NOT GET A GREEN LIGHT AFTER EXTENDING THE GEAR. THE MARKS ON THE LEFT MAIN GEAR. THE MARKS SEEN THROUGH THE VIEW PORT DUE TO THE MIRROR BEING DIRTY. CREW HAD TO BURN SOME FUEL AND REQUESTED EMERGENCY EQUIPMENT TO STANDBY. NORMAL LANDING WAS MADE. 2 L 7 2 4F 4 F RT A16WE E2EA 2007022100271 20070221 00271 NM 2007 2 21 ASAA0771459 1 20070213 A 5321 147A581016 FLOOR PANEL BOEING 737 737790 13844CN NM CABIN DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 FLOOR PANEL 242SF DELAMINATED. REPAIRED IAW SRM 53-00-50. 2 L 7 2 4F RT A16WE 2007022100274 20070221 00274 NM 2007 2 21 ASAA0771461 1 20070213 A 5321 147A591023 FLOOR PANEL BOEING 737 737790 13844CN NM CABIN DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 FLOOR PANEL 241AAF INSERT HOLE BROKEN OUT. REPAIRED IAW SRM 53-00-50. 2 L 7 2 4F RT A16WE 2007022100275 20070221 00275 NM 2007 2 21 UIEA200700030 1 20070122 A 5347 63B10047372 SEAT TRACK BOEING 747 74747UF 1384949 NM BS 1860-1880 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 409MC 30558 AFT CARGO COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT STA 1860 TO STA 1880 LBL 45. SEAT TRACK REPAIRED PER SRM 53-00-5 2 REPAIR NR 10, AND EO 4453A102. 2 L 7 4 4F RT 1384945 2007022100276 20070221 00276 EA 2007 2 21 TRAX200700236 1 20070215 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 882AS 7503 ANGLE CRACKED AT LOWER AFT LOCKPIN FITTING ON PAX DOOR FRAME. (FLAGGED) REPAIRED SEAL STRIKER IAW SRM SUPPLEMENT 53-21 -23 REV A. USING 2024 T-3 0.050 PO 8398-1 AND MS204705-5 PO 9506-1 EA934NA PO 9775-1 DT1097 2-20-07 REF TO WORK CARD 289 FOR LPI TEST. RA339. [SUPPLEMENTAL--SDR CLOSED 2/22/07] 2 L 7 2 4F RT A21EA 2007022100278 20070221 00278 NM 2007 2 21 UIEA200700035 1 20070129 A 5312 65B079341061 BULKHEAD BOEING 747 7472D7B 1384803 NM BS 260 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 FUSELAGE STA 260 BULKHEAD LT LBL60 CANTED BULKHEAD WEB FOUND CRACKED. BULKHEAD STA 260 WEB REPAIRED AS PER SRM 53-10-04 FIG 47. 2 L 7 4 4F RT A20WE 2007022100280 20070221 00280 NM 2007 2 21 UIEA200700027 1 20070127 A 5730 PANEL BOEING 747 7472D7B 1384803 NM LT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 LT WING UPPER FIXED PANEL, 12 INCHES FROM FORWARD EDGE OF NR 5 SPOILER, WBL 421.00 HAS A 6.0 INCH CRACK. ACCOMPLISHED P ERMANENT REPAIR AS PER 747 SRM 51-40-09 FIG 2 SHEET 5 AND SRM 51-40-12 AND ATLAS AIR EO 4757A342. 2 L 7 4 4F RT A20WE 2007022100281 20070221 00281 EA 2007 2 21 TRAX200700238 1 20070216 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 981EV 7768 RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. 2 L 7 2 4F RT A21EA 2007022100283 20070221 00283 EA 2007 2 21 TRAX200700240 1 20070217 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 355CA 10067 EMERGENCY FLOODLIGHT NEAR FLOOR BY SERVICE DOOR HAS BURNED OUT BULB. REMOVED AND REPLACED LIGHT BULBS IN EMERGENCY FLO ODLIGHT NEAR FLOOR BY SERVICE DOOR IAW CRJAMM 33-50-00.OP'S CHECK GOOD. 2 L 7 2 4F RT A21EA 2007022100284 20070221 00284 EA 2007 2 21 TRAX200700241 1 20070217 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 826AS 7210 LEFT SIDE EMERGENCY LIGHT AND RT SIDE WING INSPECTION LIGHT OUT. 2 L 7 2 4F RT A21EA 2007022100288 20070221 00288 EA 2007 2 21 TRAX200700242 1 20070217 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 722EV 10127 PASSENGER ENTRY DOOR -EXIT- PLACARD MISSING. 2 L 7 2 4F RT A21EA 2007022100289 20070221 00289 EA 2007 2 21 TRAX200700243 1 20070218 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 ASD BOTTOM STEP IS CRACKED AT ATTACHMENT ARM. REMOVED AND REPLACED BOTTOM FOLDING STEP I/A/W 200 AMM 52-11-04. 2 L 7 2 4F RT A21EA 2007022100294 20070221 00294 EA 2007 2 21 TRAX200700245 1 20070218 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 909EV 7658 FLAPS FAIL WHEN SELECTING FLAPS 20 DEGREES ON APPROACH. LEFT AT 8 DEGREES, RIGHT AT 10 DEGREES. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007022100297 20070221 00297 EA 2007 2 21 TRAX200700246 1 20070218 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 903EV 7621 FIRST OFFICER`S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007022100298 20070221 00298 NM 2007 2 21 QXEA200700201 1 20070211 A 3297 471515 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM MLG UNKNOWN A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 412QX 2946 4059 SEA FLIGHT NR 2402: AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED WOW2 CENTERING HARNESS. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007022100299 20070221 00299 EA 2007 2 21 TRAX200700233 1 20070215 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 PAX DOOR OUTER HANDLE APPEARS TO BE CRACKED AT INNER AFT RADIUS (MARKED) REF: 52-830-102 PG 7, FIG 52-11-02 ATTACHED. PERFORMED LPI ON PANEL DOOR OUTER HANDLE INNER RADIUS VERIFIED CRACK IS PRESENT. IAW CRJ 700 NDT MANUAL 51-20-00-08. REP AIRED PER APPLICABLE MATERIALS. PERFORMED OPS CHECK IAW CRJ 700 AMM 52-11-03. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007022100301 20070221 00301 EA 2007 2 21 TRAX200700234 1 20070215 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 882AS 7503 CLIP CRACKED AT UPPER HI-LITE I/B OF LBL 9 AT FS 280. 2 L 7 2 4F RT A21EA 2007022100302 20070221 00302 NM 2007 2 21 UIEA200700052 1 20070131 A 5315 65B1093025 FLOORBEAM BOEING 747 7472D7B 1384803 NM BS 400 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 BS 400 RT UPPER DECK FLOORBEAM UPPER CHORD FOUND HOLES AND CRACKED. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-2712 27292 AND FAA FORM 8100-9. 2 L 7 4 4F RT A20WE 2007022100303 20070221 00303 EA 2007 2 21 TRAX200700235 1 20070215 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 882AS 7503 FS 280 FWD FLOOR SUPPORT STRUCTURE CRACKED. 2 L 7 2 4F RT A21EA 2007022100304 20070221 00304 NM 2007 2 21 UIEA200700051 1 20070131 A 5330 65B070178 SKIN BOEING 747 7472D7B 1384803 NM BS 2300 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 FUSELAGE BS 2300 S-23 EXISTING DOUBLER FOUND DAMAGED. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-274437619. 2 L 7 4 4F RT A20WE 2007022100305 20070221 00305 NM 2007 2 21 UIEA200700054 1 20070131 A 5313 65B070241 STRINGER BOEING 747 7472D7B 1384803 NM BS 1700 S46L CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 AFT CARGO BS 1700 STRINGER S-46L FOUND CORRODED. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-272065605 AND FAA FORM 8100-9. 2 L 7 4 4F RT A20WE 2007022100306 20070221 00306 NM 2007 2 21 UIEA200700050 1 20070131 A 5315 65B079341063 FLOORBEAM BOEING 747 7472D7B 1384803 NM BS 260 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 M/DECK STA 260 RBL90 FLOORBEAM UPPER CHORD FOUND CRACKED. REPAIRED ACCOMPLISHEED AS PER BOEING SR ID NR 1-273725179 AND FAA FORM 8100-9. 2 L 7 4 4F RT A20WE 2007022100307 20070221 00307 NM 2007 2 21 UIEA200700022 1 20070126 A 7830 9059M49P039A ANGLE BOEING 747 7472D7B 1384803 NM THRUST REVERSER DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 NR 2, NR 3 AND NR 4 LT FAN T/REV ACCESS DOOR CLOSEOUT ASSY ANGLE FOUND DAMAGED. REPAIR ACCOMPLISHED AS PER EO NR 4778A0 91 AND FAA FORM 8110-3. 2 L 7 4 4F RT A20WE 2007022100308 20070221 00308 NM 2007 2 21 UIEA200700025 1 20070127 A 5610 65B270432 WINDOW BOEING 747 74747UF 1384949 NM COCKPIT CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 409MC 28499 30558 DURING C CHECK INSPECTION, FOUND FLIGHT DECK WINDOW NR 3R EXHIBITING WIDE SPREAD BORDER DELAMINATION AROUND ENTIRE WINDO W. OTHER DIFFICULTIES UNDETERMINABLE DUE TO EXTENT OF DELAMINATION AND RESTRICTED VISUAL IMPAIRMENTS IN BORDER AREA. W INDOW CHANGED PRECAUTIONARY. 2 L 7 4 4F RT 1384945 2007022100310 20070221 00310 NM 2007 2 21 UIEA200700040 1 20070130 A 5315 65B1092918 FLOORBEAM BOEING 747 7472D7B 1384803 NM BS 380 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 UPPER DECK FLOOR BEAM UPPER CHORD LT STA 380 FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-271217089 AN D FAA FORM 8110-9. 2 L 7 4 4F RT A20WE 2007022100311 20070221 00311 NM 2007 2 21 UIEA200700042 1 20070130 A 5753 BEARING BOEING 747 7472D7B 1384803 NM FLAP TRACK MIGRATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 RT WING NR 6 FLAP TRACK FWD ATTACH FITTING BEARING FOUND MIGRATED. REPAIRED ACCOMPLISHED AS PER SB747-57-2325. 2 L 7 4 4F RT A20WE 2007022100312 20070221 00312 NM 2007 2 21 UIEA200700043 1 20070130 A 5320 65B212645 SHEAR WEB BOEING 747 7472D7B 1384803 NM BS 840 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 M/DECK STA 840 LT TENSION TIE ATT SLOPING WEB FWD CORNER FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER SRM 51-30-02. 2 L 7 4 4F RT A20WE 2007022100313 20070221 00313 NM 2007 2 21 UIEA200700041 1 20070130 A 5753 BEARING BOEING 747 7472D7B 1384803 NM FLAP TRACK MIGRATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 LT WING NR 3 FLAP TRACK FWD ATTACH FITTING BEARING FOUND MIGRATION. REPAIRED ACCOMPLISHED AS PER SB747-57-2325. 2 L 7 4 4F RT A20WE 2007022100315 20070221 00315 EA 2007 2 21 TRAX200700224 1 20070213 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 856AS 7404 AFT EMERGENCY FLOOR LIGHT INOP. 2 L 7 2 4F RT A21EA 2007022100317 20070221 00317 EA 2007 2 21 TRAX200700225 1 20070213 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 871AS 7537 EMERGENCY LIGHTING AT FLOOR LEVEL INOP FROM ROW 9 AFT. 2 L 7 2 4F RT A21EA 2007022100318 20070221 00318 NM 2007 2 21 UIEA20070039 1 20070127 A 3610 65B4114840 DUCT BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE CRACKED A UIEA O OTHER O OTHER CR CRUISE 1 EA 15 516MC 22507 517607 NR 3 PYLON AIR VALVE INDICATES 10-PSI IN CRUISE WITH 95 PERCENT N1 SET IS NOT REGULATING CORRECTLY WITH ISOLATION VALVE OPEN. THE LEFT AND RIGHT MANIFOLD PRESSURE ONLY INDICATE 26-PSI. LEAK CHECK FOUND NO FAULT ON ENGINE AREA. SUSPECT CR ACKED DUCT ON THE WING CAUSED PRESSURE LOW. AFTER REMOVED AND REPLACED DUCT ENGINE RAN CHECK NORMAL AS PER MM 36-11-01 AND 71-00-00. 2 L 7 4 4F 4 F A20WE E23EA 2007022100319 20070221 00319 EA 2007 2 21 TRAX200700226 1 20070214 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 882AS 7503 OUTBOARD OF RBL 27 ANGLE CRACKED AT FS 484. 2 L 7 2 4F RT A21EA 2007022100320 20070221 00320 EA 2007 2 21 TRAX200700227 1 20070214 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 882AS 7503 CRACKED ANGLE O/B OF LBL 27 AT FS 484.00. 2 L 7 2 4F RT A21EA 2007022100327 20070221 00327 NM 2007 2 21 07FDEA00449 1 20070212 A 5313 AFA7772501 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 CENTER CARGO COMPARTMENT, BILGE AREA LONGERON 50L AT FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5310-105620, REPAIR CLASS IFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022100329 20070221 00329 EA 2007 2 21 TRAX200700232 1 20070215 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 858AS 7417 PAX DOOR HARD TO OPEN. 2 L 7 2 4F RT A21EA 2007022100333 20070221 00333 EA 2007 2 21 TRAX200700218 1 20070212 A 5620 WINDOW CNDAIR CL600 CL6002B19 1900309 EA CABIN CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 882AS 7503 PASSENGER WINDOW LEFT SIDE FS 409 CRACKED. (MARKED) REMOVED LT SIDEWALL PANEL 251 ALW IAW CRJ AMM 25-26-01. REMOVED CR ACKED SHIELD FROM SIDEWALL PANEL 251 ALW AND REPLACED WITH SERVICEABLE SHIELD P/N 3864045-1. ALL WORK DONE IAW CRJ AMM 2 5-26-01. OK TO INSTALL SIDEWALL PANEL 251 ALW. INSTALLED SIDEWALL PANEL 251 ALW IAW CRJ AMM 25-26-01. COMPLIED WITH EC/T C REO 601R-26-25-004. DAMAGE WAS TO PASSENGER SIDEWALL PANEL GLARESHIELD. PASSENGER WINDOW FOUND TO BE IN A SERVICEABLE CONDITION. NO FUTHER ACTION REQUIRED. 2 L 7 2 4F RT A21EA 2007022100338 20070221 00338 NM 2007 2 21 SWAA071005 1 20070219 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN DETERIORATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED HC1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS DETERIORATED. REMOVED AND REPLACED LIGHT LENS P ER MM. 2 L 7 2 4F RT A16WE 2007022100339 20070221 00339 NM 2007 2 21 SWAA071008 1 20070219 A 3350 20131 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007022100340 20070221 00340 NM 2007 2 21 SWAA070999 1 20070218 A 5610 6531914 HANDLE BOEING 737 7373H4 1384600 NM COCKPIT OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED 14Y CHECK, FOUND FLIGHT COMPT R2 WINDOW EMERGENCY RELEASE HANDLE INOP. ADJUSTED R2 WINDOW RELEASE HAND LE PER MM. 2 L 7 2 4F RT A16WE 2007022100344 20070221 00344 NM 2007 2 21 SWAA071003 1 20070219 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 386, STR 17L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007022100346 20070221 00346 NM 2007 2 21 SWAA071011 1 20070219 A 5752 654645518 TAB BOEING 737 737317 138447P NM AILERON WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED C2 CHECK, FOUND RT WING AILERON TAB ATTACH POINTS WORN. REMOVED AND REPLACED AILERON TAB PER MM. 2 L 7 2 4F RT A16WE 2007022100347 20070221 00347 NM 2007 2 21 SWAA070916 1 20070216 A 3350 100031 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007022100348 20070221 00348 NM 2007 2 21 SWAA070926 1 20070217 A 3350 101078101 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 FWD CABIN EMERGENCY EXIT SIGN COVER MISSING. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007022100349 20070221 00349 NM 2007 2 21 SWAA070996 1 20070217 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 725SW 27857 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM UPPER CAP CORRODED AT BS 986.5, LBL 52 TO RBL 52. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007022100351 20070221 00351 NM 2007 2 21 SWAA070928 1 20070217 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 464WN 32468 EEPLS INOP AT ROW 3 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007022100352 20070221 00352 NM 2007 2 21 QXEA200700194 1 20070213 A 5230 DOOR BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR FROZEN A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 419QX 4145 BOI FLIGHT NR 2391: THE RAMP WAS UNABLE TO OPEN THE CARGO DOOR. MAINTENANCE FOUND WATER FROZEN AROUND THE DOOR. CLEANE D AND LUBED ROLLERS AROUND THE DOOR. CYCLED DOOR SEVERAL TIMES. NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAF T RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007022100363 20070221 00363 EA 2007 2 21 SWIA200717774 1 20070128 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 455SW 7760 CABIN EMERGENCY LIGHT INOP. RELAMPED OVERHEAD EMERGENCY LIGHT AT ROW 1. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007022100366 20070221 00366 NM 2007 2 21 SWAA070930 1 20070217 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CORRODED AT GROUND AIR HOOK UP DOOR CUTOUT BS 528, LBL 3 TO RBL 3. REPA IRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007022100367 20070221 00367 EA 2007 2 21 SWIA200717776 1 20070202 A 3350 20131A BATTERY CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 712SK 10172 FOUND EMERGENCY LIGHTS INOP. REPLACED NR 2 EMERGENCY LIGHT CHARGER AND BATTERY IAW AMM 33-51-17. OPERATIONAL CHECKS GO OD, S/N OFF - 35157. 2 L 7 2 4F RT A21EA 2007022100368 20070221 00368 SO 2007 2 21 SWIA200717777 1 20070127 A 5330 SKIN EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 216SW 120285 FUSELAGE SKIN CRACKED AT MID FUSELAGE STATION BETWEEN FRAMES 21 LEFT AND 21 RIGHT, DISCOVERED DURING C-CHECK INSPECTION. FABRICATED AND INSTALLED DOUBLER FILLER PER EMBRAER AUTHORIZED REPAIR 1C 2007-120/00663 DATED 1/28/07 AND RII 53-800-1 000. 2 L 7 2 4T RT A31SO 2007022100375 20070221 00375 2007 2 21 SWAA070915 4 20070216 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007022100376 20070221 00376 2007 2 21 SWIA200717781 4 20070203 A 3417 ADC CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 932SW 7714 COPILOT'S PFD LOST INFORMATION FOR AIRSPEED, VERTICLE SPEED, ALTIMETER, AND HEADING INFORMATION. REPLACED NR 2 ADC AND STANDBY SA/IAS AND AIR DATA COMPUTER PN 822-0572-445, SN/OFF 45LK. OPERATIONAL CHECKS GOOD REF CRJ AMM 34-12-01. 2 L 7 2 4F RT A21EA 2007022100377 20070221 00377 EA 2007 2 21 SWIA200717782 1 20070128 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN SMOKE A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 449SW 7699 DURING TAKEOFF FROM SLC, SMELLED ELECTRICAL BURNING ODOR AND THE AIRPLANE FILLED WITH SMOKE. RETURNED TO FIELD. RAN BO TH PACKS IN AUTO AND MANUAL, WITH APU BLEED AIR AND ENGINE BLEED AIR. COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHE CKS GOOD. 2 L 7 2 4F RT A21EA 2007022000339 20070220 00339 NE 2007 2 20 QXEA200700115 2 20070129 A 7321 324485318 FUEL CONTROL DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 1 ENGINE MALFUNCTIONED A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 347PH 6306 480 SEA FLIGHT NR 2026 CLIMBING OUT OF AROUND 6000" HEARD ENGINE SURGE-LOOKED AT TORQUE GAUGE AND SWA 130 PERCENT. FIRST OF FICER NOTICED AND BROUGHT POWER LEVERS AND TORQUE BACK WITHIN 1 SECOND. PROPS WERE AT 1050. NO MECHANICAL INPUT FROM P ILOTS TO CAUSE SURGE. ON DESCENT NOTED A SIGNIFICANT 93.4 - 1 KNOB WIDTH POWER LEVER SPLIT AT TORQUE SETTINGS ABOVE 30 PERCENT ENGINE NR 1. MAINTENANCE REPLACED THE NR 1 ENGINE MFC, NR 1 PROP ASSEMBLY AND NR 1 NH PROBE. ALL OPERATIONAL C HECK GOOD. NO SURGE NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007022000341 20070220 00341 2007 2 20 QXEA200700127 4 20070203 A 3418 TRANSDUCER DHAV DHC8 DHC8202 2809007 NM STALL WARNING MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 355PH 500 PDX FLIGHT NR 2200, IMMEDIATELY AFTER TAKEOFF, NR 1 STALL WARNING CAUTION LIGHT ILLUMINATED STALL WARNING INOP. MAINTEN ANCE REPLACED THE NR 1 STALL WARNING TRANSDUCER. COMPLIED WITH FUNCTION TEST OF STALL WARNING SYSTEM IAW AMM 27-330-00- 720-801. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007022000345 20070220 00345 NM 2007 2 20 ZZDA070123120 1 20070123 A 3233 FITTING BOEING 717 717200 1383700 NM NLG DAMAGED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. NLG RETRACT ACTUATOR FITTING AND DETAILS COMMON TO STA 110.0 BULKHEAD DA MAGED. REPLACED NLG RETRACT ACTUATOR FITTING AND DETAILS COMMON TO STA 110.0 BULKHEAD PER MDC DRAWING 5911509 REV CC DA TED 5/16/01. 2 L 7 2 4F TR A6WE 2007022000346 20070220 00346 EU 2007 2 20 MALA070022 1 20070202 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 356 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 429XJ 340B429 FLOOR PANEL FLANGE, ON SEAT TRACK AT LBL 18.3, IS CORRODED OUT OF LIMITS AT FS 356. THE DAMAGE HAS BEEN REPAIRED IAW ME SABA EO NR S53342. REF: EAMS WORK ORDER 215462 TASK 1512. 2 L 7 2 4T RT A52EU 2007022000367 20070220 00367 2007 2 20 ZZDA070123130 4 20070123 A 3451 56553667L ANTENNA BOEING 717 717200 1383700 NM DME DAMAGED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. DME ANTENNAS DAMAGED. REPLACED DME ANTENNAS PER 717 AMM CHAPTER 34-52-0 2 REV 27 DATED 01/01/07. 2 L 7 2 4F TR A6WE 2007022000377 20070220 00377 EU 2007 2 20 2007UALA00352 1 20070207 A 5270 PROXIMITY SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE DOOR FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 402UA 439 DOOR 1 ARMS, BUT WILL NOT INDICATE ARMED ON COCKPIT. [SUP 05-08-07] FAULT TRACED TO OUT OF ADJUSTMENT PROXIMITY SWITCH . MORE SPECIFICALLY, A LOOSE LOCK WASHER ON THE PROXIMITY TARGET. REPLACED LOCK WASHER AND READJUSTED PROXIMITY SWITCH T O PROPER CLEARANCE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022000379 20070220 00379 2007 2 20 2007UALA00356 4 20070207 A 2565 COVER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE L2 DOOR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 806UA 788 SLIDE COVER AT DOOR 2L FELL OFF DOOR. [SUP 05-08-07] REPLACED SLIDE COVER. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022000390 20070220 00390 NM 2007 2 20 AWXA200700214 1 20070218 A 5330 6545775 SKIN BOEING 737 7373G7 1384595 NM BS 767 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 PHX - FOUND CRACKED FUSELAGE SKIN, BS 767, S22R. REPAIRED FUSELAGE SKIN, BS 767, S22R IAW B737-300 SRM 53-00-01-2R. 2 L 7 2 4F RT A16WE 2007022000411 20070220 00411 NM 2007 2 20 QXEA200700183 1 20070213 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 425-489 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - LEFT CENTER SEAT TRACK NR 5 HAS SCRATCHES, NICKS AT STATION 425, 439 TO 450, 473 TO 489. REPAIRED IAW RD8-53-1 339. 2 H 7 2 4T RT A13NM 2007022100002 20070221 00002 EA 2007 2 21 SWIA200717805 1 20070210 A 2913 6619003 PUMP CNDAIR CL600 CL6002C10 1390015 EA NR 2 HYD SYSTEM FAILED A SWIA O OTHER K FLUID LOSS DE DESCENT 1 NM 07 730SK 5062 5062 10193 ON DESCENT, LOST ALL HYDRAULIC FLUID IN NR 2 SYSTEM. REPLACED NR 2 EDP AND NR 2 ACMP IAW 29-11-01 AND 29-11-03. OPERAT IONAL CHECKS GOOD, ACMP PN 66195-01 SN OFF K0638. 2 L 7 2 4F RT A21EA 2007022100013 20070221 00013 EA 2007 2 21 SWIA200717810 1 20070211 A 2910 LINE CNDAIR CL600 CL6002B19 1900309 EA NR 1 HYD SYSTEM LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 909SW 7558 HYD 1 LOW PRESSURE AT FL 190, NO QUANTITY OR PRESSURE. REPAIRED LEAK IN NR 1 PRESSURE LINE. OPERATIONAL AND LEAKS CHEC KS GOOD. 2 L 7 2 4F RT A21EA 2007022100017 20070221 00017 EA 2007 2 21 SWIA200717813 1 20070217 A 5610 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 07 754SK 10215 CO-PILOTS WINDSHIELD CRACKED. REPLACED CO-PILOTS WINDSHIELD IAW MM 56-11-01 AND RII 56-220-1000. LEAK AND OPERATIONAL CHECKS GOOD, PN: NP139321-14 SN OFF: 04235H2888. 2 L 7 2 4F RT A21EA 2007022100029 20070221 00029 NM 2007 2 21 2007UALA00368 1 20070208 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR FROZEN A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 DOOR 1R UNABLE TO DISARM. FOUND ICE CHIPS ON SILL AFTER OPENING DOOR AND ICE FILM AROUND GIRT BAR FLOOR FITTING. CLEA NED WITH ICE RELEASE AND LUBE W ITH DC33 GREASE. STATIC LINE CLEAR. DOOR GIRT BAR ARM-DISARM OPERATES NORMAL AFTER ICE REMOVAL. NO COMPONENTS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100037 20070221 00037 NM 2007 2 21 QXEA200700181 1 20070211 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 545 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - LEFT SEAT TRACK NR 3 HAS CORROSION AT STATION 545. REPAIRED IAW RD8-53-9467 AND RD8-53-3644. 2 H 7 2 4T RT A13NM 2007022100038 20070221 00038 NM 2007 2 21 QXEA200700173 1 20070210 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - GOUGE ON INNER SKIN OF BAGGAGE DOOR 28" FROM THE TOP AND 2 1/2" FROM FORWARD SIDE. REPAIRED IAW SRM 51-20-11, 51-20-16, AND 51-20-36. 2 H 7 2 4T RT A13NM 2007022100039 20070221 00039 NM 2007 2 21 QXEA200700174 1 20070210 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - GOUGE ON INNER SKIN OF BAGGAGE DOOR 19 1/2" FROM THE TOP AND 2 1/2" FROM THE FORWARD SIDE. REPAIRED IAW SRM 51 -20-11, 51-20-16, AND 51-20-36. 2 H 7 2 4T RT A13NM 2007022100040 20070221 00040 2007 2 21 2007UALA00372 4 20070208 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 87UA 26713 NR 1 LEFT MED DOOR SLIDE INFLATION CYLINDER NEEDLE IS JUST OUT OF GREEN BAND ON THE LOW SIDE. LAST OVERHAUL DATE IS APR 05. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100046 20070221 00046 NM 2007 2 21 QXEA200700206 1 20070215 A 2430 UNKNOWN DHAV DHC8 DHC8202 2809007 NM NR 1 DC GEN UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 353PH 496 PUW FLIGHT NR 2197, NR 1 DC GENERATOR CAUTION LIGHT BECAME ILLUMINATED DURING TAXI OUT TO RUNWAY. FOLLOWED EMERGENCY CH ECKLIST, CAUTION LIGHT STAYED ILLUMINATED NR 1 ENGINE STARTED NORMALLY (DC GENERATOR INOP). MAINTENANCE PLACED ON MEL. 2 H 7 2 4T RT A13NM 2007022100064 20070221 00064 NM 2007 2 21 AALA20070182 1 20070124 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AM 24579 DFW - EMERGENCY LIGHT IDENTIFIER AT AFT LEFT NUMBER TWO DOOR BROKEN. REPLACED EMERGENCY LIGHT IDENTIFIER ASSEMBLY AT AF T LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007022100066 20070221 00066 NM 2007 2 21 AALA20070166 1 20070123 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 699AN 27051 MIA - EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A2NM 2007022100068 20070221 00068 EA 2007 2 21 QXEA200700147 1 20070126 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 611QX 10041 C3 OKC - FOUND CORROSION IN NUMEROUS PLACES DOWN ENTIRE LENGTH OF BOTH CABIN LEFT AND RIGHT FLOOR SEAT TRACKS. REPAIRED IAW SRM 51-21-06 AND 53-21-49. 2 L 7 2 4F RT A21EA 2007022100071 20070221 00071 EA 2007 2 21 QXEA200700144 1 20070202 A 5242 SKIN CNDAIR CL600 CL6002C10 1390015 EA E/E BAY DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 611QX 10041 C3 OKC - FOUND INNER FUSELAGE SKIN AT E AND E BAY DOOR HAS MINOR SURFACE HAS CORROSION. REPAIRED IAW SRM 53-00-01, 51-2 1-06, AND 51-21-11. 2 L 7 2 4F RT A21EA 2007022100078 20070221 00078 WP 2007 2 21 AALA20070284 1 20070204 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 593AA 53256 SFO - EMERGENCY EXIT LIGHTS ON LEFT AND RIGHT SIDE UPPER SIDEWALL AT ROW 20 FORWARD OVERWING INOPERATIVE. REPLACED BATT ERY PACK FOR FORWARD OVERWING EMERGENCY EXIT LIGHTS AT ROW 20 LEFT AND RIGHT UPPER SIDEWALL. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT A6WE 2007022100089 20070221 00089 2007 2 21 UIEA200700065 4 20070203 A 3416 A4289910016 ALTIMETER BOEING 747 7472D7B 1384803 NM COCKPIT STICKING A UIEA O OTHER J WARNING INDICATION CR CRUISE 1 EA 15 528MC 22472 DURING CLIMB CAPT'S ALTIMETER NEEDLE WOULD STICK IN POSITION CAUSING PULL-UP TERRAIN WARNING, DON'T SINK WARNING AUDIBLE S. CAPT'S ALTIMETER REMOVED AND REPLACED, INDICATION AND LEAK CHECK CARRIED OUT, OK IAW MM 34-13-04. 2 L 7 4 4F RT A20WE 2007022100091 20070221 00091 EU 2007 2 21 2007UALA00376 1 20070209 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT SMOKE A UALA G O2 MASK DEPLOYED B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 WP 29 405UA 452 CREW REPORTED SMOKE/SMELL IN CABIN & COCKPIT FOLLOWED BY A EXTRACT FAN FAULT. [SUP 05-08-07] VERIFIED THAT AVIONICS AI R EXTRACT FAN WAS FAULTY AND WAS REPLACED. SMOKE/ELECTRICAL SMELL DUE TO BEARING FAILURE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100093 20070221 00093 2007 2 21 2007UALA00377 4 20070209 A 2213 FCU AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE AUTOPILOT SYSTEM MALFUNCTIONED A UALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 WP 29 444UA 824 V10289 AUTO FLT -FCU 1 FAULT- DISPLAYED ON UPPER ECAM SCREEN. CREW COMMENTS, WITH SMOKE FROM FCU. [SUP 05-08-07] REPLACED FCU AFTER VERIFYING THAT FCU WAS FAULTY AND WAS SOURCE OF SMOKE. FURTHER FAULT TRACING DETERMINED THAT THE PSU WAS DEFE CTIVE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100112 20070221 00112 NM 2007 2 21 2007UALA00419 1 20070211 A 2612 CONTROL MODULE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FIRE WARNING INOPERATIVE A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 313UA 23674 PER CREW FAULT LIGHT ON ENGINE AND APU FIRE CONTROL MODULE INOPERATIVE. FOUND FAULTY APU/ENGINE FIRE CONTROL MODULE. R EPLACED THE FIRE CONTROL MODULE. SHOP FOUND THE MODULE TO HAVE A TEST SWITCH FAULT. REPLACED THE FAULT/TEST SWITCH. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022100121 20070221 00121 NM 2007 2 21 UIEA200700007 1 20070117 A 5315 FLOORBEAM BOEING 747 74747UF 1384949 NM BS 1780 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 416MC 31838 AFT CARGO COMPARTMENT AFT FLANGE OF FLOORBEAM UPPER CHORD DAMAGED AT STA 1780 RBL 25.75. AFT CARGO COMPARTMENT AFT FLAN GE OF FLOORBEAM REPAIRED AS PER SRM 51-70-12 REPAIR 1 AND EO 4453A100. 2 L 7 4 4F RT 1384945 2007022100124 20070221 00124 NM 2007 2 21 UIEA200700010 1 20070121 A 5311 65B0184926 FRAME BOEING 747 7472D7B 1384803 NM ZONE 200 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 CABIN BS 2231 RT FRAME INNER CHORD S-25R FOUND CRACK ON FASTENER HOLE AT STRAP. REPAIR ACCOMPLISHED AS PER SRM 53-10-04 FIG 115. 2 L 7 4 4F RT A20WE 2007022100127 20070221 00127 EU 2007 2 21 2007UALA00421 1 20070212 A 5313 FASTENER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FWD CARGO BAY CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 430UA 568 FWD PIT STRINGER ATTACH FASTENERS ARE CORRODED FROM FRAME 24A TO 29 BETWEEN STR 38R & 38L. REPLACED 1029 CORRODED RIVET S. 2 L 7 2 4F 4 F RT A28NM E40NE 2007030100125 20070301 00125 NM 2007 3 1 UIEA200700085 1 20070225 A 7830 ACCESS DOOR BOEING 747 7472D3B 1384805 NM GE CF6 CF680 30025 NE THRUST REVERSER DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 NR 3 ENGINE RT FAN T/REV ACCESS DOOR ASSY SKIN DAMAGED. REPAIRED ACCOMPLISHED AS PER EO NR 4778A095 AND FAA FORM 8110-3 . 2 L 7 4 4F 4 F RT A20WE E13NE 2007022100137 20070221 00137 NM 2007 2 21 2007UALA00426 1 20070212 A 3397 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU BAY CHAFED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 505UA 24626 APU COMPARTMENT - COMPARTMENT LIGHT SWITCH WIRE AT FIREWALL SIGNS OF ARCING, JUST ABOVE SWITCH. INSPECTED WIRES AND FO UND INSULATION CHAFED BUT WIRES SHOWED NO DAMAGE. REPAIRED WIRES FOR APU COMPARTMENT LIGHT AT SWITCH. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100154 20070221 00154 NM 2007 2 21 2007UALA00444 1 20070213 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 346UA 24250 EEL LIGHT STRIPS INOP ROWS 1-2 AND EEL STRIP IN FRONT OF FWD GALLEY CART STOWAGE COMPARTMENT. REPLACED EEL STRIPS (560- 0806 AND 560-0808) 2 L 7 2 4F 4 F RT A16WE E21EU 2007022100160 20070221 00160 2007 2 21 2007UALA00246 4 20070127 A 2565 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 535UA 25130 DOOR 2R SLIDE GIRT BAR ENGAGEMENT LIGHT INOP. CLEANED SOCKET, ARMED AND DISARMED DOOR 2R SEVERAL TIMES AND LIGHT FUNCT IONED NORMALLY. THE DISCREPANCY IS ATTRIBUTED TO SHORTING OF CONNECTION DUE TO ACCUMULATION OF DIRT. THERE WAS NO NEE D TO CHANGE ANY PART OR COMPONENT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100163 20070221 00163 NE 2007 2 21 2007UALA00249 2 20070129 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 VIBRATION A UALA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 466UA 1343 V10836 LANDED UNDER AMBER ALERT DUE TO NR 1 ENGINE VIBRATION. HPC STAGES 3 AND 6 WERE BORESCOPED AND DAMAGE WAS FOUND "BEYOND ALL LIMITS". LATER RECEIVED VERBAL CONFIRMATION THAT THE DAMAGE WAS AT STAGE 3. REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100171 20070221 00171 NM 2007 2 21 2007UALA00257 1 20070130 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 220UA 30223 SEAT 2E EMERGENCY LIGHT SEGMENT ON THE ARMREST IS BROKEN, INOP. REPLACED THE EMERGENCY LIGHT SEGMENT. OPS CHKD OK. SUSP ECT DAMAGE BY PASSENGER. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007022100177 20070221 00177 NM 2007 2 21 2007UALA00263 1 20070131 A 3350 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 510UA 24780 EXT EMERGENCY LIGHT AT DOOR L-4 INOPERATIVE. FOUND BULB INOPERATIVE.REPLACED BULB AND OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100181 20070221 00181 NM 2007 2 21 2007UALA00267 1 20070201 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY LIGHT INOP CEILING ROW 16. RELAMPED. OPS CHECKS. NORMAL 2 L 7 4 4F 4 F RT A20WE E24NE 2007022100190 20070221 00190 NM 2007 2 21 2007UALA00277 1 20070131 A 3350 FUSE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN BLOWN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 326UA 23958 LEFT AFT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BLOWN FUSE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022100191 20070221 00191 NM 2007 2 21 2007UALA00278 1 20070202 A 5280 DOOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT MLG MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 LEFT MLG SHOCK STRUT DOOR FOUND MISSING. A/C FERRIED TO GSO FOR DOOR REPLACEMENT. ACCOMPLISHED DOOR INSTALL AND RIG CH ECK. INSPECTED DOOR INSTALLATION PER MM32-12- 00. CORRECTLY INSTALLED. A/C RETURNED TO SERVICE. DOOR EXPERIENCES AIR LOADS DURING LANDING & TAKEOFF. SUSPECT VIBRATION CAUSED FAILURE OF DOOR MOUNTING. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022100196 20070221 00196 NM 2007 2 21 2007UALA00283 1 20070201 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 FUSELAGE SKIN AT STA 1700, STR 17L IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. FUSELAGE SKIN REPAIR AT STA 1700, S17L APPLI ED WITH BLIND FASTENER. REPLACED DOUBLER & ADDED EXTRA ROW OF FASTENERS ON BOTTOM END. ALL FASTENERS INSTALLED ARE SOLI D. HFEC PER NDT, NO CRACKS NOTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100200 20070221 00200 NM 2007 2 21 2007UALA00286 1 20070201 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 581UA 26701 EMERGENCY LIGHT AFT OF LEFT WING FAIRING INOPERATIVE. EMERGENCY LIGHT AFT OF LEFT WING FAIRING INOP. RELAMPED WITH 767 LAMP 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100232 20070221 00232 NM 2007 2 21 DU4R2007044 1 20070124 A 5320 143N852215 SILL BOEING 757 757232 1384965 NM BS 560-620 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION C-1 DOOR CUTOUT LOWER SILL RETAINER ATTACH POINT HOLES BS 560 TO BS 620. REMOVED AND REPLACED LOWER SILL T CH ORD C-1 DOOR P/N NR 143N8522-15 IAW B757 SRM 51-40-02 AND 53-60-15 DETAIL V PAGE 102. 2 L 7 2 4F RT A2NM 2007022100253 20070221 00253 NM 2007 2 21 ASAA0741476 1 20070220 A 5753 6590737565 FITTING BOEING 737 7374Q8 138447Q NM T/E FLAP GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 RIGHT I/B MID FLAP MISSING RUB STRIP ON O/B FITTING OF CENTER FORE FLAP TRACK. REMOVED RUBSTRIP, FOUND FITTING GOUGED, REMOVED AND REPLACED FITTING IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007022100261 20070221 00261 NM 2007 2 21 07FDEA00483 1 20070215 A 5315 FLOORBEAM BOEING 727 7272S2F 1384O81 NM BS 1166 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 208FE 22930 FOUND MAIN DECK FLOORBEAM AT STA 1166 RBL 30 - 45.5 UPPER CHORD HAS CORROSION. REPAIRED FLOORBEAM STA 1166 RBL 30 - 45. 5 IAW SR 27-53-033. 2 L 7 3 4F A3WE 2007022100309 20070221 00309 NM 2007 2 21 UIEA200700026 1 20070127 A 5730 PANEL BOEING 747 7472D7B 1384803 NM LT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 LT WING PYLON GAP PANEL AT ILES 640.47 HAS A 3.0 INCH CRACK. ACCOMPLISHED PERMANENT REPAIR AS PER 747 SRM 51-40-09 FIG 18 SHEET 5 AND SRM 51-40-12, ALSO REFERENCE ATLAS AIR EO 4757A342. 2 L 7 4 4F RT A20WE 2007022100314 20070221 00314 NM 2007 2 21 UIEA200700044 1 20070130 A 5320 65B212646 SHEAR WEB BOEING 747 7472D7B 1384803 NM BS 840 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 M/DECK STA 840 RT TENSION TIE ATT SLOPING WEB AT FWD CORNER FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER SRM 51-30-02. 2 L 7 4 4F RT A20WE 2007022100325 20070221 00325 NM 2007 2 21 07FDEA00447 1 20070212 A 5313 AJC7246507 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 WASTE TANK COMPARTMENT, LONGERON 43R END FITTING AT STA 2007 FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-31-01 V OLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022100326 20070221 00326 EA 2007 2 21 TRAX200700231 1 20070215 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 978EV 7723 CAPTAIN'S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007022100330 20070221 00330 WP 2007 2 21 07FDEA00453 1 20070212 A 5311 FRAME DOUG MD10 MD1010F 3022112 WP BS 1841 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 372FE 46610 COMPLY WITH EA8-5310-102019, FUSELAGE FRAME CRACK AT STA1841 BETWEEN L9 AND L10 COMPLIED WITH EA8-5310-102019. 2 L 7 3 4F RT A22WE 2007022100334 20070221 00334 EU 2007 2 21 TRAX200700219 1 20070212 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 642AS 395 EMERGENCY FLOOR LIGHTING FLASHING ON AND OFF. 2 H 7 2 4T RT 2007022100335 20070221 00335 NM 2007 2 21 SWAA071007 1 20070219 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED HC1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007022100336 20070221 00336 NM 2007 2 21 SWAA071006 1 20070219 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED HC1 CHECK, FOUND FWD CABIN EMERGENCY EXIT SIGN LENS LOOSE. SECURED SIGN LENS PER MM. 2 L 7 2 4F RT A16WE 2007022100337 20070221 00337 NM 2007 2 21 SWAA071015 1 20070219 A 3350 101114 LIGHT BOEING 737 7373T5 1384608 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 696SW 23064 DURING SCHEDULED SPV CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007022100343 20070221 00343 NM 2007 2 21 SWAA071004 1 20070219 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 517D, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007022100345 20070221 00345 NM 2007 2 21 SWAA071013 1 20070219 A 5315 6545808 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 294, BL 0 TO RBL 12. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007022100365 20070221 00365 EA 2007 2 21 SWIA200717775 1 20070130 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 439SW 7578 AFT CEILING EMERGENCY EXIT LIGHT INOP. RELAMPED AFT CEILING EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007022100370 20070221 00370 NM 2007 2 21 SWAA070929 1 20070217 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 375, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007022100373 20070221 00373 EA 2007 2 21 SWIA200717780 1 20070202 A 5610 NP13932211 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 963SW 7865 CAPTAIN'S SIDE WINDOW SHATTERED AFTER LANDING. REPLACED THE CAPTAIN'S SIDE WINDOW IAW MM 56-12-01 AND RII 56-220-1000, SN OFF: 03196H666. 2 L 7 2 4F RT A21EA 2007022100379 20070221 00379 NM 2007 2 21 SWAA070921 1 20070216 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED CV CHECK, FOUND LEFT FWD CABIN EEPLS PHOTOLUMINESCENT STRIP WORN. REMOVED AND REPLACED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 2007022100383 20070221 00383 NM 2007 2 21 UIEA200700023 1 20070127 A 5610 65B270431 WINDOW BOEING 747 74747UF 1384949 NM COCKPIT CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 409MC 28499 30558 DURING C-CHECK INSPECTION, PROCESS FOUND FLIGHT DECK WINDOW NR 3L EXHIBITING SIGNS OF FAIL/SAFE INTERLAYER CRACKING IN R ADIUS AREAS. GENERAL IN-SERVICE USE AND LOCALIZED DELAMINATION OF WINDOW ASSEMBLY MADE IT IMPOSSIBLE TO POSITIVELY DETE RMINE EXISTENCE AND EXTENT OF CRACKING. WINDOW CHANGED PRECAUTIONARY. 2 L 7 4 4F RT 1384945 2007022100384 20070221 00384 NM 2007 2 21 07FDEA00465 1 20070213 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 RIGHT WING, OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), CLEVIS ASSEMBLY BORE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1 -5750-107788, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022100389 20070221 00389 NE 2007 2 21 AWXA200700140 2 20070131 A 7261 O-RING AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE NR 1 ENGINE LEAKING A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 827AW 1547 1021 PHX - DURING INITIAL CLIMB, LOST ALL OIL QUANTITY IN NR 1 ENGINE. OIL PRESS AND ALL OTHER PARAMETERS REMAINED IN THE GR EEN. RETURNED TO FIELD AT IDLE THRUST. INSTALLED TEMP THERMOCOUPLE IN NR 1 ENG ACOC WITH NEW O-RING IAW MM 79-32-15 PB 401. RAN ENG, LEAK CHECK GOOD. INSPECTED MASTER CHIP DETECTOR, NO DISCREPANCIES NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100406 20070221 00406 EA 2007 2 21 SWIA200717785 1 20070202 A 5610 NP13932211 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 464SW 2604 2604 7827 CAPTAIN'S SIDE WINDOW OUTER LAYER IS SHATTERED. REPLACED CAPTAIN'S SIDE WINDOW IAW MM 56-12-01 AND RII 56-220-1000. 2 L 7 2 4F RT A21EA 2007022100413 20070221 00413 2007 2 21 SWAA071000 4 20070218 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007022100414 20070221 00414 NM 2007 2 21 SWAA071002 1 20070219 A 3350 MS155721 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 760SW 27874 LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007022100415 20070221 00415 NM 2007 2 21 SWAA071012 1 20070219 A 3350 MS155721 LIGHT BOEING 737 7373A4 1384585 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007022100416 20070221 00416 NM 2007 2 21 SWAA071016 1 20070219 A 2560 PH22300L GLOWSTRIP BOEING 737 7375H4 138449D NM CABIN DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 18Y CHECK, FOUND FWD RT CABIN EEPLS PHOTOLUMINESCENT STRIP DISBONDED. REMOVED AND REPLACED PHOTOLUMINE SCENT STRIP PER MM. 2 L 7 2 4F RT A16WE 2007022100418 20070221 00418 NM 2007 2 21 SWAA070868 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200001 20070222 00001 NM 2007 2 22 SWAA070913 1 20070215 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 410WN 27897 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 2 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007022200003 20070222 00003 EA 2007 2 22 TRAX200700221 1 20070212 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 710EV 10071 NUMEROUS LIGHTS ARE BURNED OUT ON BOTH THE LT AND RT LOWER OVERWING EMERGENCY EXIT SIGNS. 2 L 7 2 4F RT A21EA 2007022200006 20070222 00006 SO 2007 2 22 C2XA07IA042 1 20070219 A 3260 8005701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO LANDING GEAR INTERMITTENT A C2XA O OTHER N FALSE WARNING UK UNKNOWN 1 SW 27 13949 145057 GRK - FLIGHT 2963, THE CREW REPORTED A LANDING GEAR AIR GROUND FAILURE. THE CREW RESET THE SYSTEM SUCCESSFULLY AND THE AIRCRAFT LANDED AT GRK WITHOUT INCIDENT. ON FLIGHT 2114 THE DISCREPANCY RETURNED, AND THE AIRCRAFT LANDED AT IAH WITHOU T INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE RIGHT HAND WEIGHT ON WHEELS PROXIMITY SWITC H, OPERATIONALLY CHECKED WITH NO EFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007022200010 20070222 00010 EA 2007 2 22 TRAX200700198 1 20070202 A 5320 SILL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 CORROSION ON ASD SILL ANGLE AROUND NUT PLATES WHERE MARKED. REMOVED AND REPLACED ASD SILL ANGLE IAW CRJ 700 SRM 53-21-23 . 2 L 7 2 4F RT A21EA 2007022200014 20070222 00014 SO 2007 2 22 C2XA07BT018 1 20070213 A 3350 3025103 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16999 145307 BTV FLT 2874 DURING ROUTINE INSPECTION FOUND LT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LT OVERWING EMERGEN CY LIGHT IAW EMB145 AMM 33-50-10. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007022200015 20070222 00015 SO 2007 2 22 C2XA07IA037 1 20070207 A 2611 SMOKE WARNING EMB 145 EMB145EP 3260221 SO LAVATORY MALFUNCTIONED A C2XA O OTHER N FALSE WARNING UK UNKNOWN 1 SW 27 12934 145019 IAH - FLIGHT 2036, THE CREW REPORTED AN INTERMITTENT LAV SMOKE WARNING ON THE EICAS ONE TIME DURING FLIGHT. THE AIRCRAF T LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE LAV SMOKE DETECTOR WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007022200018 20070222 00018 NM 2007 2 22 CALA0700074 1 20070219 A 5330 65C35794 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND A 0.61 INCH CRACK IN FUSELAGE SKIN AT L-2 DOOR FORWARD LOWER CORNER ON DOOR TORQUE TUBE ACCESS, STA 947 .5-967, S14L. REPAIRED IAW ECRA 5331-01288. 2 L 7 2 4F RT A16WE 2007022200019 20070222 00019 NM 2007 2 22 CALA0700075 1 20070220 A 5311 6546555 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 INSPECTION FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT CENTER FLOOR AREA, STA 867, S28L TO S28R. THE CORRODED SECTION OF FRAME WAS TRIMMED OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-07, FIGURE 201. 2 L 7 2 4F RT A16WE 2007022200020 20070222 00020 NM 2007 2 22 CALA0700076 1 20070209 A 5330 141N38411 SKIN BOEING 757 757224 1384958 NM FUSELAGE LIGHTNING STRIKE A CALA K NONE O OTHER UK UNKNOWN 1 SW 27 12125 28967 THE AIRCRAFT SUSTAINED LIGHTNING STRIKE DAMAGE TO THE FUSELAGE SKIN AT STA 199 LT ABOVE THE LAP SPLICE S20L. AN INTERIM REPAIR WAS INSTALLED IAW PART 1A OF ECRA 5330-03537, REV A. A DIP WAS ISSUED TO REINSPECT THE AREA IAW PART 2 PRIOR TO THE ACCOMPLISHMENT OF 37,000 FLIGHT CYCLES AND THEREAFTER AT INTERVALS NOT TO EXCEED 12,000 FLIGHT CYCLES. 2 L 7 2 4F RT A2NM 2007022200021 20070222 00021 NM 2007 2 22 CALA0700069 1 20070217 A 5315 BAC1518338 FLOORBEAM BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17126 27566 INSPECTION FOUND FLOORBEAM CORRODED AT STA 365.25, RBL 19. THE CORRODED AREA OF FLOORBEAM WAS CUT OUT AND THE AREA WAS REPAIRED IAW ECRA 5321-01447. 2 L 7 2 4F RT A2NM 2007022200022 20070222 00022 NM 2007 2 22 CALA0700070 1 20070217 A 5230 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND A 1 INCH CRACK IN C-1 DOOR HANDLE CUTOUT IN FORWARD UPPER CORNER OF SKIN. FILLER AND DOUBLER WERE INST ALLED IAW SRM 52-00-01. 2 L 7 2 4F RT A16WE 2007022200023 20070222 00023 NM 2007 2 22 CALA0700071 1 20070217 A 5314 65C385021 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND LEFT KEEL BEAM CORRODED AT STA 500D-520, S28L. THE CORRODED SEGMENT OF KEEL BEAM WAS REMOVED AND REPLA CED IAW SRM 53-60-12. 2 L 7 2 4F RT A16WE 2007022200024 20070222 00024 EA 2007 2 22 COMA0760186 1 20070212 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP STICKING A COMA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 804CA 10953 7352 FLIGHT 9493 - DURING CVG APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WIT HOUT INCIDENT. REPLACED THE RIGHT INBOARD FLAP INBOARD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2007022200025 20070222 00025 EA 2007 2 22 COMA0760187 1 20070212 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP STICKING A COMA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 804CA 10953 7352 FLIGHT 9493 - DURING CVG APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WIT HOUT INCIDENT. REPLACED THE LEFT INBOARD FLAP OUTBOARD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2007022200027 20070222 00027 EA 2007 2 22 COMA0760189 1 20070214 A 2613 6243843 OVERHEAT SENSOR CNDAIR CL600 CL6002B19 1900309 EA LT WING FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 938CA 27782 7046 FLIGHT 9463 - DURING CLIMBOUT OF CLT RECEIVED AN ANTI-ICE CAUTION MESSAGE, FLIGHT RETURNED TO THE FIELD. REPLACED THE L EFT WING LEADING EDGE HEAT SENSOR. 2 L 7 2 4F RT A21EA 2007022200028 20070222 00028 EA 2007 2 22 COMA0760190 1 20070214 A 2613 6243843 OVERHEAT SENSOR CNDAIR CL600 CL6002B19 1900309 EA LT WING FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 938CA 10708 7046 FLIGHT 9463 - DURING CLIMBOUT OF CLT RECEIVED AN ANTI-ICE CAUTION MESSAGE, FLIGHT RETURNED TO THE FIELD. REPLACED THE L EFT WING LEADING EDGE HEAT SENSOR. 2 L 7 2 4F RT A21EA 2007022200030 20070222 00030 EA 2007 2 22 COMA0760192 1 20070214 A 2913 887055 PUMP CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE FAILED A COMA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 01 816CA 15284 7398 FLIGHT 5116 - EN ROUTE CVG-SAT LOST PRESSURE ON HYDRAULIC SYSTEM NR 2, FLIGHT RETURNED TO CVG. REPLACED THE RIGHT ENGIN E DRIVEN HYDRAULIC PUMP. 2 L 7 2 4F RT A21EA 2007022200032 20070222 00032 EA 2007 2 22 COMA0760194 1 20070215 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 443CA 7539 FLIGHT 5137 - DURING YYZ APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAG E -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTIO N MESSAGES. 2 L 7 2 4F RT A21EA 2007022200033 20070222 00033 EA 2007 2 22 COMA0760195 1 20070217 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 785CA 19061 7326 FLIGHT 5284 - F/O WINDSHIELD CRACKED. REMOVED AND REPLACED RIGHT WINDSHIELD. 2 L 7 2 4F RT A21EA 2007022200036 20070222 00036 EA 2007 2 22 COMA0760196 1 20070216 A 3230 46193 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG WHEEL WELL FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 915CA 10331 7013 FLIGHT 5179 - ON APPROACH SELECTED GEAR DOWN AND RECEIVED GEAR DISAGREE WARNING, AFTER 10 SECONDS THE NLG CAME DOWN AND LOCKED. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED MLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2007022200037 20070222 00037 EA 2007 2 22 COMA0760197 1 20070219 A 7830 744952201 CABLE CNDAIR CL600 CL6002B19 1900309 EA RT PYLON BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 597SW 7293 WHILE PERFORMING TASK CARD CRJ-2-448001, RIGHT NACELLE INSP, FOUND THE ATR CABLE TO BE BROKEN AT THE TURNBUCKLE END IN T HE PYLON, MAKING THE ATR SYSTEM INOP. REPLACED CABLE IAW AMM 78-35-01. 2 L 7 2 4F RT A21EA 2007022200039 20070222 00039 EA 2007 2 22 COMA0760199 1 20070219 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SO 01 941CA 7050 FLIGHT 5138 - FLAPS FAIL CAUTION MESSAGE, FLAPS FAILED AT 0 DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE - FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION ME SSAGES. 2 L 7 2 4F RT A21EA 2007022200040 20070222 00040 NM 2007 2 22 HNAA0700011 1 20070210 A 5311 85310908 FRAME DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 933HA 46711 46711 134 FRAME ON DOUBLER IS CRACKED AT X129.00 AND X136.800. REPAIRED PER ED8-53-3541. 2 H 7 2 4T RT A13NM 2007022200043 20070222 00043 NM 2007 2 22 HNAA0700040 1 20070215 A 4950 BLEED AIR SYS DHAV DHC8 DHC8102 2809003 NM APU ODOR A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 937HA 148 STRONG OIL SMELL IN FLIGHT DECK WITH APU BLEED ON. RAN APU OPERATED BLEEDS FOR SEVERAL MINUTES, NO SMELL DETECTED. 2 H 7 2 4T RT A13NM 2007022200044 20070222 00044 NM 2007 2 22 HNAA0700033 1 20070214 A 2120 UNKNOWN DHAV DHC8 DHC8102 2809003 NM COCKPIT SMOKE A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 827EX 390 SMOKE IN COCKPIT WHEN SELECTED APU BLEED AND INVERTERS IN. GROUND RAN APU AND NR 2 ENGINE SMOKE DISSIPATED NO OTHER DEF ECTS NOTED. INSPECTED FLIGHT DECK, NO DEFECT NOTED. 2 H 7 2 4T RT A13NM 2007022200046 20070222 00046 NM 2007 2 22 HNAA0700036 1 20070211 A 3350 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM CABIN FAULTY A HNAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 07 804EX 227 EMERGENCY LIGHTS CYCLE ON AND OFF DURING TAXI. REMOVED AND REPLACED EMERGENCY LIGHT CONTROL BOX. 2 H 7 2 4T RT A13NM 2007022200049 20070222 00049 NM 2007 2 22 UPS07449134 1 20070104 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LT BS 980 STR 38L AT DRAG SPLICE FITTING AREA FOUND 1EA FASTENER HOLE CRACKED AT SKIN APPROX .0625" RU NNING DOWNWARD. SKIN REPAIRED AS PER SRM 53-30-03 FIG 60. JUST BETWEEN BS 950 & 987 STR 37L TO 39L / OVERLAPPED SKIN R EPAIRED AS PER SRM 53-30-03 FIG 12, BETWEEN BS 968.5 & 984 STR 39L AREA. 2 L 7 4 4F A20WE 2007022200050 20070222 00050 NM 2007 2 22 UPS07549199 1 20070214 A 2120 UNKNOWN BOEING 757 75724APF 1384969 NM COCKPIT ODOR A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 01 433UP 25464 INSPECTION TYPE:N/A ON FINAL APPROACH AT GEAR DOWN, FLAPS 20 CALL. THERE WAS A FAST OCCURRENCE OF ODOR IN COCKPIT. NO SMOKE & NO ABNORMAL INSTRUMENT INDICATIONS. THE ODOR WAS DISTINCTIVELY BURNING RUBBER. IT DISSIPATED UPON TAXI IN. RA N BOTH PACKS & BOTH ENGINES, NO UNUSUAL ODORS NOTED. 2 L 7 2 4F RT A2NM 2007022200051 20070222 00051 NM 2007 2 22 UPS07549202 1 20070130 A 5330 SKIN BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 438UP 25469 INSPECTION TYPE:C3 EXTERIOR FUSELAGE SKIN HAS A DENT AT STR 7R, BS 751. REPAIRED DENT IN EXTERIOR FUSE SKIN BS 751, STR 7R, IAW SRM 53-00-01-2 -2R. 2 L 7 2 4F RT A2NM 2007022200052 20070222 00052 NM 2007 2 22 UPS07549203 1 20070209 A 5311 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 438UP 25469 INSPECTION TYPE:C3 FWD CARGO BAY FRAME DENTED AT STA 700 STR 24R. REMOVED DAMAGE ON FRAME AND REPAIRED PER SRM 51-70-11 . 2 L 7 2 4F RT A2NM 2007022200053 20070222 00053 NM 2007 2 22 UPS07549204 1 20070209 A 5311 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 438UP 25469 INSPECTION TYPE:C3 FWD CARGO BAY FRAME DENTED AT STA 680 STR 23R. REMOVED DAMAGE ON FRAME AND REPAIRED PER SRM 51-70-11 . 2 L 7 2 4F RT A2NM 2007022200060 20070222 00060 NM 2007 2 22 UPS07M49216 1 20070218 A 5270 STRIKER DOUG MD11 MD11F 3023600 NM PAX DOOR OUT OF ADJUST A IPXA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 275UP 48774 INSPECTION TYPE:N/A LEFT FWD ENTRY DOOR WARNING LIGHT ILLUMINATED ON A/C ROLL OUT REMAINED ON ALL THE WAY TO THE GATE. ADJUSTED LEFT FORWARD ENTRY DOOR AFT GIRT BAR SWITCH STRIKER PER MM 52-11-02-5. DOOR OPS CHECKS GOOD PER MM 52-70-00-5. 2 L 7 3 4F RT A22WE 2007022200061 20070222 00061 EU 2007 2 22 UPS07149191 1 20070210 A 2597 CONNECTOR AIRBUS A300 A300F4622R 3930360 EU UNKNOWN A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 149UP 0832 INSPECTION TYPE:N/A ESCAPE SLIDE TEST LIGHT DOES NOT ILLUMINATE. BUZZER SOUNDS NORMAL. RESET CONNECTOR 70WN-A ON THE A SPSU. TESTED W/REF TO AMM 52-73-00-05. SYSTEM TESTS OK. THIS CLEARS M343934. 2 L 7 2 4F RT A35EU 2007022200064 20070222 00064 NM 2007 2 22 DHL2007781002 1 20070215 A 5210 SKIN BOEING 727 727227 1384078 NM PAX DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 781DH 207 21996 FWD ENTRY DOOR UPPER AFT CORNER OF EXTERIOR SKIN, WORKING RIVETS, BS 314. REMOVED FASTENERS ON L1 DOOR, AFT UPPER CORNE R PER B727 SRM 51-30-2, CRACK FOUND ON EXISTING DOUBLER. FABRICATED DOUBLER FROM 2024-T3, .050" X 4.5" X 3.5", PO 90040 42, TREATED, PRIMED, AND INSTALLED DOUBLER, ALL PER B727 SRM 52-10-2, 51-20-1, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 2007022200066 20070222 00066 WP 2007 2 22 UPS07849210 1 20070213 A 5720 DOUBLER DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C3 LEFT WING CENTER L/E UPPER INNER DOUBLER CRACKED AT STA XOLDI 6.2246. REMOVED CRACKED DOUBLER AT LEF T WING CENTER L/E STA XOLDI 6.2246 IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT DOUBLER AT LEFT WING CENTER UP PER L/E STA XOLDI 6.2246 IAW SRM 57-03-01, 51-1-8, AND SRM 51-2-20D. 2 L 7 4 4F RT 4A25 2007022200067 20070222 00067 WP 2007 2 22 UPS07849211 1 20070212 A 5312 BULKHEAD DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD CRACKED AT STA 1766 LBL 24 L10L AREA. CUT OUT DAMAGED AREA AT AFT PRESSURE BUL KHEAD STA 1766 LBL 24 L10L IAW SRM 53-2-5 FIG 14A. FABRICATED AND INSTALLED FINGER DOUBLER, FILLER AND REPAIR DOUBLER AT AFT PRESSURE BULKHEAD STA 1766 LBL 24 L10L IAW SRM 53-2-5 FIG 14A, AND SRM TR 53-194. 2 L 7 4 4F RT 4A25 2007022200068 20070222 00068 CE 2007 2 22 DXTA200701934 1 20070213 A 2720 UNKNOWN CESSNA 750 750 2076810 CE RUDDER UNKNOWN E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 912QS 7500012 DURING STRAIGHT CRUISE FLIGHT RUDDER TRIM INDICATOR DISPLAYS TRIM INDICIES COMPLETELY LEFT OF AND OUTSIDE OF TAKEOFF RAN GE MARKINGS. INSTALLED RUDDER CONTOUR BOARD, CHECKED LT AND RT RUDDER TRIM DEGREES OF DEFLECTION. VERIFIED BOTH READING S WITHIN LIMITS. REF CESSNA CE-750 MM 27-26-00 & 27-20-00. OK FOR SERVICE. 2 L 7 2 4J RT T00007WI 2007022200069 20070222 00069 WP 2007 2 22 UPS07849223 1 20070210 A 5542 SKIN DOUG DC8 DC871F 302199D WP RUDDER DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C3 RUDDER RT SIDE LEADING EDGE STA ZR 140 SKIN HAS DENT. FOUND DENT OUT OF LIMITS AT RUDDER STA ZR 140 IAW SRM 55-02-00-0 FIG 001. REMOVED AND REPLACED SKIN AT RUDDER BAY NR 2 STA ZR 140 IAW SRM 51-3-0, 51-1-21, AND SRM 55 -06-01-0. NO WEIGHT AND BALANCE REQUIRED ONE FOR ONE SKIN CHANGE IAW SRM 55-06-01-0. 2 L 7 4 4F RT 4A25 2007022200070 20070222 00070 CE 2007 2 22 DXTA200701949 1 20070215 A 2750 FLAP SYSTEM CESSNA 750 750 2076810 CE TE FLAPS MALFUNCTIONED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 905QS 7500105 AFTER TAKEOFF WE GOT A FLAPS FAIL AMBER CAS MESSAGE & INDICATIONS WHEN WE RETRACTED THE FLAPS THEY WERE FULLY UP. RESET DIDN'T WORK, UPON APPROACH TO LANDING SLATS ONLY CAME OUT. UPON INSPECTION FOUND FAULT "2" DISPLAYED ON FLAP CONTROLLER IN TAILCONE. PUSHED THE FLAP RESET BUTTON IN COCKPIT AND CYCLED FLAPS NUMEROUS TIMES. NO DEFECTS NOTED. PLACED AIRCRAF T OUTSIDE TO COLD SOAK FOR SEVERAL HOURS. CYCLED FLAPS NUMEROUS TIMES. NO DEFECTS NOTED. NO FURTHER FAULT INDICATION IAW 750 MM 27-50-00 OPS CK GOOD. F/T CK GOOD 2 L 7 2 4J RT T00007WI 2007022200071 20070222 00071 CE 2007 2 22 DXTA200701939 1 20070211 A 2820 905 VALVE CESSNA 560 560XL 2076702 CE FUEL CELL INTERMITTENT E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 642QS 1642 5605561 AFTER CROSSFEEDING FROM LEFT OT RIGHT TANK , WHEN CROSSFEED SWITCH IS TURNED OFF ( CENTER ) THE RIGHT LO FUEL PRESS ANNU NCIATOR ILLUMINATES MOMENTARILY, FOLLOWED BY A STEADY R FUEL BOOST ON ANNUNCIATOR. SWITCHING THE RT BOOST PUMP SWITCH T O ON AND BACK TO NORM WILL NOT TURN OFF THE ANNUNCIATOR. APU WAS OFF. REMOVED INTERMITTENT RH MOTIVE FLOW VALVE, P/N 905 , S/N 905. INSTALLED AN OVERHAULED UNIT, P/N 4151 SN 644, OVERHAULED BY PNEU DRAULICS, CRS# PD6R469J, UNDER WO# 37694*1. WORK PERFORMED IAW CE-560XL M/M, CHAPTER 28-21-06. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A22CE 2007022200072 20070222 00072 2007 2 22 DXTA200701940 2 20070211 A 7200 ENGINE CESSNA 560 560XL 2076702 CE LEFT MALFUNCTIONED E DXTA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 GL 07 601QS 5605301 DURING ENGINE START, LT ENGINE OIL PRESSURE WOULD NOT COME OUT OF THE RED . AFTER APPROX 15 SEC ITT CLIMBED TO 680 DEG C AND THEN SHOT UP TO 800 DEG C FOR 2-3 SECS . AS SOON AS ITT WENT PAST 720 DEG START WAS ABORTED . ITT WAS NOT AT 800 DEG C FOR MORE THAN 3 SECS. MOTORED ENGINE FOR 30 SEC AFTER ABORT. ITT DROPPED BELOW 720 DEG C AS SOON AS START WAS AB ORTED AND CONTINUED TO DROP WILE LT ENGINE WAS MOTORED . INSPECTED LT ENGINE AND OIL LEVEL WAS NORMAL. COMPLIED WITH DC U DOWNLOAD OF LT ENGINE, SENT DOWNLOAD INFO TO PWC FOR INTERPROLATION, PWC REPORT NO EXCEEDANCES AT THIS TIME. P&WC RECO MMENDS STARTING & GROUND RUNNING ENGINE TO CHECK OPERATION. COMPLIED WITH THESE RECOMMENDATIONS ENGINE OPS CKS GOOD PER 2 L 7 2 4F RT A22CE 2007022200073 20070222 00073 WP 2007 2 22 UPS07849224 1 20070212 A 5313 DC853B00939 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C3 CORROSION UNDER SPLICE FITTING AND LONGERON 33L IN AFT ACCESSORY COMPT AT STA 1550. REMOVED SPLICE F ITTING AND CUT OUT CORRODED SECTION OF L33L FROM STA 1530-1550 IAW SRM 51-1-21. LOCATED, DRILLED UP, AND INSTALLED NEW SPLICE FITTING AND LONGERON 33L SECTION FROM STA 1530-1550 IAW SRM 53-04-01-0, AND SRM 53-02-02-0 FIG 11. 2 L 7 4 4F RT 4A25 2007022200075 20070222 00075 NM 2007 2 22 UPS07549051 1 20070104 A 5311 146N102890 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 417UP 23904 INSPECTION TYPE:C AFT PIT LEFT SIDE STA 1420, STR 25-26, FRAME DENTED. DIMENSION OF DENT .020 THE CENTER OF DENT FROM FLOOR TRANS PANEL 3.7 INCHES FROM PRODUCTION SPLICE TO DENT 9.2 INCHES LENGTH OF DENT WIDTH OF DENT .96; ACCOMPLISHED PE R FINAL EA 757-5362-A1596 AND UPS EO B757-5310- 26021; PARTIALLY REMOVED TRANSITION PANEL AT STA 1420-1440 L/F ACCESS PE R/SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007022200077 20070222 00077 WP 2007 2 22 UPS07849193 1 20070105 A 5320 5751966503 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 FITTING HEAVY CORROSION AT STA 940 L21R. REMOVED, FABRICATED AND INSTALLED FITTING IAW SAA EA 008-53 20-01- A0594, UPS RAA DC8-53-20607, SRM 51-11-8 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2007022200079 20070222 00079 NM 2007 2 22 UPS07M49200 1 20070215 A 5730 PAINT DOUG MD11 MD11F 3023600 NM LT WING MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 281UP 48538 INSPECTION TYPE:N/A LEFT WING UPPER TRAILING EDGE SKIN HAS SEVERAL AREAS OF PAINT MISSING JUST INBD OF WINGLET. LEFT WI NG INBD SIDE OF WINGLET SKIN HAS SEVERAL AREAS OF PAINT MISSING COMPOSITE PANELS & T/E IS DELAMINATED. ITEM DEFERRED D3 44293. *S/D* REMOVED PAINT, INSPECTED PANEL. THE DELAMINATION APPEARANCE WAS FROM A PREVIOUS REPAIR. THE GRITTINESS OF PANEL IS OK PER DRAWING ARB7793. UPPER PANEL ASSY, T/E WING EXT OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2007022200080 20070222 00080 NM 2007 2 22 SWAA070914 1 20070215 A 3350 471A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 434WN 32454 DURING SCHEDULED MV3 CHECK, FOUND EEPLS COVER CRACKED AT ROW 16 ABC. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2007022200082 20070222 00082 NM 2007 2 22 SWAA070877 1 20070215 A 5322 654659 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 968, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007022200083 20070222 00083 NM 2007 2 22 SWAA070912 1 20070215 A 5315 6546812 FLOORBEAM BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, LBL 35 TO RBL 5. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007022200084 20070222 00084 NM 2007 2 22 SWAA070879 1 20070215 A 5315 6546812 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 53. REMOVED AND REPLACED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2007022100058 20070221 00058 WP 2007 2 21 AALA20070271 1 20070203 A 2560 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 443AA 49469 MIA - EMERGENCY FLASHLIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT AT RIGHT NUMBER FOUR DO OR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007022100062 20070221 00062 NM 2007 2 21 AALA20070179 1 20070124 A 3350 LIGHT BOEING 757 757231 1384950 NM CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 718TW 28486 LAS - EMERGENCY LIGHT EXIT STRIP AT SEAT 13D LOOSE. SECURED EMERGENCY LIGHT EXIT STRIP AT SEAT 13D. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007022100067 20070221 00067 NM 2007 2 21 AALA20070167 1 20070123 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 699AN 27051 MIA - EMERGENCY LIGHT AT SEAT 28D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A2NM 2007022100069 20070221 00069 EA 2007 2 21 QXEA200700148 1 20070125 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 611QX 10041 C3 OKC - FOUND CABIN LEFT AND RIGHT WALL SEAT TRACKS HAVE CORROSION IN NUMEROUS AREAS DOWN FULL LENGTH OF TRACK. REPAIR ED IAW SRM 53-21-49, 51-21-06. 2 L 7 2 4F RT A21EA 2007022100070 20070221 00070 EA 2007 2 21 QXEA200700149 1 20070119 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 611QX 10041 C3 OKC - FUSELAGE SKIN SHOWS SIGNS OF SURFACE CORROSION AT ADF ANTENNA MOUNT. REPAIRED IAW SRM 53-00-01, 51-21-06. 2 L 7 2 4F RT A21EA 2007022100073 20070221 00073 EA 2007 2 21 QXEA200700146 1 20070122 A 5754 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA NR 1 SLAT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 611QX 10041 C3 OKC - FOUND RIGHT NR 1 SLAT HAS PITTING ON EXTERIOR SURFACE FROM SS 57.50 TO SS 199.66. REPAIRED IAW SRM 51-14-06, 5 1-21-11. 2 L 7 2 4F RT A21EA 2007022100079 20070221 00079 NM 2007 2 21 AALA20070286 1 20070205 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 346AN 33085 MIA - EMERGENCY LIGHTS AT SEAT ROWS 23H TO 31H INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 23H TO 31H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007022100087 20070221 00087 NM 2007 2 21 UIEA200700017 1 20070124 A 5551 65B035618 FITTING BOEING 747 7472D7B 1384803 NM HORIZONTAL STAB CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 CRACKS FOUND ON RT HORIZ STAB AT HOLE 15 IN THE SPLICE PLATE AND HOLE 28 IN THE HINGE FITTING. REPAIRED ACCOMPLISHED AS PER BOEING SRM ID NR 1-273714301 AND FAA FORM 8110-9. 2 L 7 4 4F RT A20WE 2007022100092 20070221 00092 NM 2007 2 21 UIEA200700064 1 20070202 A 5753 65B119522 FLAP TRACK BOEING 747 747341 13848AM NM NR 5 FLAP GOUGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 NR 5 FLAP TRACK FORWARD FITTING OUTBOARD SURFACE FOUND WITH GOUGE. REPAIRED GOUGED AREA, BLENDED AND SMOOTHED PER SRM 51 -10-00. DETAIL VISUAL AND HFEC INSPECTED. FOUND NO DEFECTS. AREA PROTECTED AND PAINTED. FOUND WITHIN SERVICEABLE LIM ITS. 2 L 7 4 4F RT A20WE 2007022100094 20070221 00094 NM 2007 2 21 UIEA20070063 1 20070124 A 5414 65B940521 SKIN BOEING 747 747341 13848AM NM NR 3 NACELLE WORN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 NR 3 PYLON ACCESS PANEL CUT-OUT SKIN FOUND WORN AT PANEL 472AR. REPAIR: THE EFFECTED INNER DOUBLER WAS TRIMMED. THE TRI MMED EDGE WAS NDT INSPECTED. REPAIR SKIN WAS INSTALLED WITH HILOCK FASTENERS TO RESTORE THE TRIMMED OUT AREA. A MODIFI ED STEEL WEAR PLATE WAS INSTALLED ON THE SKIN ASSEMBLY SURFACE TO PROVIDE FOR ACCESS DOOR LATCH ENGAGEMENT. 2 L 7 4 4F RT A20WE 2007022100120 20070221 00120 NM 2007 2 21 UIEA200700006 1 20070117 A 5347 SEAT TRACK BOEING 747 74747UF 1384949 NM BS 1780-1781 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 416MC 32838 AFT CARGO COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT STA 1780 RBL 25. AFT CARGO SEAT TRACK REPAIRED IAW SRM 53-00-52 REPAIR NR 10 AND EO NR 4453A100. 2 L 7 4 4F RT 1384945 2007022100123 20070221 00123 NM 2007 2 21 UIEA200700008 1 20070118 A 5311 65B0184925 FRAME BOEING 747 7472D7B 1384803 NM BS 2231 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 CABIN BS 2231 LT FRAME UPPER STRAP AND INNER CHORD FOUND CRACKED. CABIN BS 2231 LT FRAME UPPER STRAP AND INNER CHORD RE PAIRED AS PER SRM 53-10-04 FIG 115. 2 L 7 4 4F RT A20WE 2007022100142 20070221 00142 NE 2007 2 21 2007UALA00432 2 20070212 A 7230 BLADE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COMPRESSOR FAILED A UALA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 29 654UA 25392 727948 NR 1 ENGINE STALLED INFLIGHT. [SUP 4-20-07] SURGE OCCURRED AT TOD; ENGINE REPLACED AT ORD. TEARDOWN REVEALED THAT 1 HP COMPRESSOR STAGE-7 BLADE FAILED IN THE AIRFOIL NEAR THE TIP. THE AMOUNT OF MISSING AIRFOIL WAS APPROXIMATELY 1-SQ.I N. FAILURE BEGAN AS A FATIGUE CRACK AT THE AIRFOIL TRAILING EDGE, AND PROGRESSED FORWARD IN FATIGUE. THIS FRACTURE MODE EVENTUALLY TRANSITIONED TO A DUCTILE OVERLOAD THAT LED TO SEPARATION AT THE MID-CHORD LOCATION. DOWNSTREAM AIRFOIL DAM AGE WAS NOTED ON STAGES 8, 9, AND 10. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022100146 20070221 00146 EU 2007 2 21 2007UALA00436 1 20070213 A 5520 ELEVATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT AND RT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 430UA 568 LEFT AND RIGHT ELEVATORS WERE FOUND TO HAVE SUSPECTED AREAS OF WATER INGRESSION. [SUP 05-16-07] A THERMOGRAPHIC INSPEC TION FOUND 3 AREAS ON UPPER SURFACE AND 1 AREA ON LOWER SURFACE OF LEFT ELEVATOR WITH SUSPECTED WATER INGRESSION. SIMILA R INSPECTION OF RIGHT ELEVATOR FOUND 8 SUSPECTED AREAS ON UPPER SURFACE. ONE AREA ON EACH ELEVATOR WAS CUT OUT, BUT NO W ATER WAS FOUND. AIRBUS WAS ADVISED OF RESULTS AND APPROVED OTHER AREAS OF SUSPECTED DAMAGE AS INTERIM FLIGHT WORTHY WITH FOLLOW-UP INSPECTIONS AND/OR REPAIRS IN THE FUTURE. AREAS THAT WERE ALREADY CUTOUT WERE REPAIRED IN ACCORDANCE WITH SRM . 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100149 20070221 00149 NM 2007 2 21 2007UALA00439 1 20070213 A 5210 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR UNKNOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 R-2 DOOR FWD FRAME HINGE POINT REQUIRES PREVENTATIVE FRAME REPAIR. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLE D REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100156 20070221 00156 NM 2007 2 21 2007UALA00446 1 20070214 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMEGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 566UA 26670 EMERGENCY SLIDE LIGHT INOP AT DOORS 1R & 4R. RELAMPED NR 767 LAMP 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100157 20070221 00157 NM 2007 2 21 2007UALA00447 1 20070213 A 5210 SILL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 589UA 28707 DOOR 1R DIFFICULT TO DISARM. LEVER DOESN'T ALWAYS MOVE COMPLETELY TO DISARM POSITION. CLEANED DOOR SILL AND THE LEVE R MOVEMENT WAS RESTORED. NO COMPONENT NEEDED TO BE REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100161 20070221 00161 NM 2007 2 21 2007UALA00247 1 20070127 A 2120 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN SMOKE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 29 661UA 27158 CAPTAIN REPORTED SMOKE IN THE CABIN AFTER ENGINE GATE START. TROUBLE SHOOTING CONFIRMED SMOKE IN THE CABIN WITH APU RUN NING. REPLACED APU ENGINE PER AMM 49-11-01. OPS CHECKED AND LEAK CHECKED GOOD. AC PACKS NEED OIL BURN OUT TO BE ACCOM PLISHED. ITEM ROLLED FORWARD. ACCOMPLISHED PACK BURN OUT. A/C RETURNED TO SERVICE. SUSPECT CRACKED OIL LINE DUE TO VI BRATION. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022100172 20070221 00172 2007 2 21 2007UALA00258 4 20070129 A 2565 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR UNWANTED DEPLOY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 DOOR 1L SLIDE MAY BE PARTIALLY DEPLOYED. REINSTALLED SLIDE PACK IN CONTAINER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022100183 20070221 00183 NM 2007 2 21 2007UALA00269 1 20070131 A 2560 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FLASHLIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 570UA 26678 AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT BATTERY AND SEAL. OPS OK 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100184 20070221 00184 EU 2007 2 21 2007UALA00270 1 20070201 A 2560 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR INTERMITTENT A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 481UA 1559 SLIDE LIGHT INTERMITTENTLY COMING ON AND GOING OFF. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100185 20070221 00185 NM 2007 2 21 2007UALA00271 1 20070130 A 2697 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LAV SMOKE DETECT DAMAGED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 596UA 28749 LAV SMOKE DETECTOR LEFT CIRCUIT BREAKER WILL NOT RESET. FOUND WIRE CONNECTING LEFT LAV SMOKE DETECTOR SHORTED AROUND MET AL GASPER DUCT BETWEEN CIRCUIT BREAKER AND DISC. REPAIRED WIRING TO FIX CIRCUIT BREAKER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100193 20070221 00193 NM 2007 2 21 2007UALA00280 1 20070201 A 5241 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 FORWARD GALLEY DOOR SN1113, FORWARD FRAME IS CRACKED AT MOST LOWER END STOP FITTING FROM OUTBOARD FASTENER HOLE, BOTH HO LES ARE MARKED. MAJOR REPAIR: REMOVED DAMAGE. ACCOMPLISHED NEW SPLICE KIT REPAIR DOUBLER AND FILLER PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022100198 20070221 00198 2007 2 21 2007UALA00284 4 20070201 A 2565 SEAL BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SLIDE ASPIRATOR LEAKING A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 668UA PF0077 30024 LEAKING ASPIRATOR IN RIGHT OVER-WING ESCAPE SLIDE. SLIDE REPLACED. A/C OK FOR SERVICE. LEAKING ASPIRATOR ATTRIBUTED T O SEAL LEAK AT THE BASE OF METAL BELLOWS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022100199 20070221 00199 2007 2 21 2007UALA00285 4 20070201 A 2565 5A29011 ASPIRATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE LEAKING A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 660UA PF0088 27115 ASPIRATOR LEAKING. SLIDE REPLACED. A/C OK FOR SERVICE. LEAKING ASPIRATOR ATTRIBUTED TO CUTTING OF METAL BELLOWS BY AC CIDENTAL IMPACT OR CRUSH WHILE PACKING. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022100222 20070221 00222 NM 2007 2 21 ASAA0741448 1 20070213 A 5322 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 CORROSION ON SHEAR TIE AT FUSELAGE. REMOVED DAMAGED SECTION OF FRAME, FABRICATED AND INSTALLED FILLER AND SHEAR TIE IAW SRM 53-00-07 REPAIR 3. 2 L 7 2 4F RT A16WE 2007022100230 20070221 00230 NM 2007 2 21 QXEA200700162 1 20070212 A 5610 WINDSHIELD DHAV DHC8 DHC8202 2809007 NM COCKPIT LEAKING A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 347PH 480 PDX FLIGHT NR 2163 - WATER DRIPPING ON GLARESHIELD. MAINTENANCE REPLACED CORRODED NUPLATES ON UPPER EDGE OF FIRST OFFIC ERS WINDHSHIELD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007022100265 20070221 00265 EA 2007 2 21 A6WA200740048 1 20070120 A 5720 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 447AW 7812 FOUND LEFT SIDE FS 621 TO FS 625.30 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. (M) 2 L 7 2 4F RT A21EA 2007022100267 20070221 00267 NM 2007 2 21 ASAA0771457 1 20070213 A 5321 147A581028 FLOOR PANEL BOEING 737 737790 13844CN NM CABIN PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 AFT CABIN FLOOR PANEL AT FS 986 PUNCTURED. REPAIRED IAW SRM 53-00-50. 2 L 7 2 4F RT A16WE 2007022100273 20070221 00273 NM 2007 2 21 ASAA0771460 1 20070213 A 5321 147A581023 FLOOR PANEL BOEING 737 737790 13844CN NM CABIN PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 FLOOR PANEL 241 AAF PUNCTURED. REPAIRED IAW SRM 53-00-50. 2 L 7 2 4F RT A16WE 2007022100277 20070221 00277 NM 2007 2 21 UIEA200700031 1 20070129 A 5313 65B0416117 STRINGER BOEING 747 7472D7B 1384803 NM BS 2200-2220 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 BULK CARGO STA 2200-2220 STR 49L FOUND CORRODED. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-271194583 AND FAA FORM 8110-9. 2 L 7 4 4F RT A20WE 2007022100285 20070221 00285 NM 2007 2 21 UIEA200700018 1 20070117 A 5414 311U2040129 PANEL BOEING 747 74747UF 1384949 NM NR 1 NACELLE MISSING A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 416MC 32838 ON WALK AROUND, FOUND PANEL MISSING ON NR 1 PYLON RIGHT HAND SIDE, PANEL 452 CR. INSTALLED NEW PANEL IAW MM 54-62-00. 2 L 7 4 4F RT 1384945 2007022100286 20070221 00286 NM 2007 2 21 UIEA200700036 1 20070129 A 5322 65B0432546 SHEAR TIE BOEING 747 7472D7B 1384803 NM BS 1760 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 AFT CARGO STA 1760 FRAME SHEARTIE S-50L TO S-51L FOUND CORRODED. AFT CARGO STA 1760 FRAME SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3A. 2 L 7 4 4F RT A20WE 2007022100292 20070221 00292 EU 2007 2 21 07FDEA00485 1 20070215 A 5730 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 740FD 559 FOUND OLD CORROSION REPAIR ON UPPER WING SKIN LT, CLOSED TO RIB 5. REPAIR WAS VERIEFIED IAW RAS/BAE/0937/2004 ISSUE B A ND CAL EO AB6-57-00-0057R1. THE REPAIR DIDN'T CORRESPOND WITH THE DOCUMENTS. THE REPAIR WAS ACCOMPLISHED IN THE FOLLOW DR 456. 2 L 7 2 4F RT A35EU 2007022100293 20070221 00293 EU 2007 2 21 07FDEA00486 1 20070215 A 5754 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 OLD REPAIR ON LT SLAT NR 3 LEADING EDGE, BY AN EXTERNAL PATCH, FASTENERS WERE CORRODED AND SOME HOLE DIAMETERS ARE OVERS IZE. REPAIR WAS PERFORMED IAW TD FOK/308/2006 ISSUE A BY EA 6-5744-106357. 2 L 7 2 4F RT A35EU 2007022100295 20070221 00295 EU 2007 2 21 07FDEA00489 1 20070214 A 5210 DOOR AIRBUS 300 A300F4605R 3930327 EU L1 UNLATCHED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 655FE 742 CLIMBIMG THRU FL 220, ECAM WARN LEFT CABIN DOOR UNLATCHED. VISUAL INSPECTION SHOWED BOTH LATCH INDICATIONS FULL RED, RE TURNED TO MEMPHIS. RELEASED FOR SERVICE PER MEL/CDL: 52-71-01. CATEGORY: C EXPIRATION: 24FEB07 "MEL 52-71-01: (IDENTIF Y) L1 DOOR CLOSED AND LOCKED INDICATION ON ECAM DOOR PAGE, INOP. 2 L 7 2 4F RT A35EU 2007022100296 20070221 00296 EA 2007 2 21 A6WA200740049 1 20070120 A 5320 6013501252 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FS621,STR 14R CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 447AW 7812 FOUND RT SIDE FS 621 TO FS 625.30 INTERCOSTAL AT STRINGER 14R IS CRACKED NEAR RADIUS APPROX .50 INCH LONG NEAR RADIUS. MAINTENANCE REPLACED CRACKED INTERCOSTAL WITH NEW INTERCOSTAL PN 601-35012-52 IAW SRM 51-42-06. (K) 2 L 7 2 4F RT A21EA 2007022100300 20070221 00300 EU 2007 2 21 07FDEA00438 1 20070209 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 MDC - FOUND SEAT TRACK NR 2 L BETWEEN FR 68.0 TO 69.5 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW A310 SRM 51-40 -21 AND 53-10-16. 2 L 7 2 4F RT A35EU 2007022100316 20070221 00316 NM 2007 2 21 UIEA200700019 1 20070125 A 2820 65B922228 TRANSFER TUBE BOEING 747 7472D7B 1384803 NM RT WING WORN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 RT WING NR 3 RESERVE TANK AT WS 1454 TRANSFER TUBE ASSY 2 COTTER PINS HOLES FOUND WORN. REPAIRED ACCOMPLISHED AS PER BO EING SR ID NR 1-276113094 AND EO NR 4728A027. 2 L 7 4 4F RT A20WE 2007022100322 20070221 00322 NM 2007 2 21 07FDEA00439 1 20070209 A 5230 HINGE PIN BOEING 727 727233 138408A NM CARGO DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 MAIN CARGO DOOR HINGE PIN HAS A .2 INCH GAP BETWEEN THE RETENTION NUT AND WASHER ON THE AFT END OF THE HINGE (PIN CRAC KED/BROKEN). INSTALLED NEW HINGE PIN UPON DOOR INSTALL REF MM 52-34-009-4-1 PAGE 1, MM 52-34-009- 5 PAGE 1, NASI SUP FX V-727-MM14 CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007022100342 20070221 00342 NM 2007 2 21 SWAA071009 1 20070219 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518, STR 12R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007022100362 20070221 00362 EA 2007 2 21 SWIA200717773 1 20070131 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 925SW 7682 FORWARD OVERHEAD EMERGENCY LIGHT INOP, RELAMPED CABIN FORWARD OVERHEAD EMERGENCY LIGHT IAW MM 33-51-00. OPERATIONAL CHE CKS GOOD. 2 L 7 2 4F RT A21EA 2007022100374 20070221 00374 2007 2 21 SWAA070919 4 20070216 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM EVAC SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2007022100380 20070221 00380 NM 2007 2 21 SWAA071014 1 20070219 A 5511 6547505 RIB BOEING 737 7373Q8 1384670 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STAB L/E RIB CRACKED AT STA 101. REMOVED AND REPLACED L/E RIB PER SRM. 2 L 7 2 4F RT A16WE 2007022100407 20070221 00407 EA 2007 2 21 SWIA200717786 1 20070201 A 3397 FEEDER CABLE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT FAILED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 464SW 7827 EMERGENCY LIGHTS STRIP ON FLOOR MID CABIN DO NOT ILLUMINATE. REPLACED ELECTRICAL CABLE FOR EMERGENCY LIGHT FOR FLOOR MI D CABIN. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007022100411 20070221 00411 NM 2007 2 21 SWAA070998 1 20070218 A 5523 65C35943 CONTROL ROD BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED A1 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR CONTROL ROD ENDS PER M M. 2 L 7 2 4F RT A16WE 2007022100417 20070221 00417 NM 2007 2 21 SWAA070869 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200002 20070222 00002 EA 2007 2 22 TRAX200700220 1 20070212 A 3250 STEERING SYS CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 828AS 7213 ON TAKEOFF FROM ATL, AFTER GEAR RETRACTION RECEIVED STEERING INOP CAUTION MESSAGE RAN QRH PROCEDURE AND RETURNED ATL WIT H NOSEWHEEL STEERING OFF. LANDED NORMALLY TAXIED TO GATE. AIRCRAFT RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. FL T 4711 DEL 261 MINS. 2 L 7 2 4F RT A21EA 2007022200005 20070222 00005 EA 2007 2 22 TRAX200700223 1 20070212 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 876AS 7576 RIGHT EXTERIOR OVERWING AFT EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007022200007 20070222 00007 SO 2007 2 22 C2XA07IA041 1 20070215 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO CABIN ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 10156 145786 IAH - A BURNING SMELL WAS NOTED IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT, AND COULD NOT DUPLICATE THE ODOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007022200038 20070222 00038 EA 2007 2 22 COMA0760198 1 20070219 A 3250 STEERING SYS CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 920CA 7022 FLIGHT 5222 - STEERING INOP CAUTION MESSAGE ON TAKEOFF ROLL, ABORTED TAKEOFF AT 70 KTS. PERFORMED OPS CHECK OF NWS, NO FAULTS. PERFORMED BITE CHECK OF NWS ECU ON FAULTS LOGGED. 2 L 7 2 4F RT A21EA 2007022200041 20070222 00041 NM 2007 2 22 HNAA0700012 1 20070215 A 5320 85320686101 THRESHOLD DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 933HA 46711 46711 134 CORROSION FOUND ON PAX DOOR THRESHOLD AROUND ANCHOR NUT. REPLACED PAX DOOR THRESHOLD. 2 H 7 2 4T RT A13NM 2007022200047 20070222 00047 NM 2007 2 22 HNAA0700039 1 20070212 A 5320 85320460111 INTERCOSTAL DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 933HA 46711 46711 134 CORROSION FOUND AT INTERCOSTAL AT PAX DOOR ENTRANCE. REPLACED INTERCOSTAL. 2 H 7 2 4T RT A13NM 2007022200048 20070222 00048 NM 2007 2 22 HNAA0700037 1 20070105 A 5320 85321072 BRACKET DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 933HA 46711 46711 134 SURFACE CORROSION FOUND IN PAX DOOR AFT GOOSENECK DRAIN PAN. REPLACED BRACKET. 2 H 7 2 4T RT A13NM 2007022200054 20070222 00054 NM 2007 2 22 UPS07549206 1 20070215 A 3350 LIGHT BOEING 757 75724APF 1384969 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 428UP 25459 INSPECTION TYPE:N/A EMERGENCY LIGHT ASSY HAS TWENTY INOP LAMPS. RELAMPED EMERGENCY LIGHT ASSY, OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2007022200057 20070222 00057 NM 2007 2 22 UPS07M49197 1 20070129 A 5330 SKIN DOUG MD11 MD11F 3023600 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP 48774 INSPECTION TYPE:2C CENTER CARGO DOOR CUTOUT SKIN LOWER LEFT AFT CORNER CHIPPED, DENTED, & GOUGED. CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR IAW MD-11 SRM 53-50-00. 2 L 7 3 4F RT A22WE 2007022200058 20070222 00058 NM 2007 2 22 UPS07M49198 1 20070214 A 2421 IDG DOUG MD11 MD11F 3023600 NM NR 3 OVERSERVICED A IPXA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SO 01 286UP 48453 INSPECTION TYPE:N/A WHILE EN ROUTE TO CRK, THE CREW ADVISED DISPATCHER OF THE LOSS OF THE NR 3 GENERATOR. THE FLIGHT WA S APPROX 45 MINUTES OUT OF CRK DUE TO A PREV DEF OF THE NR 1 GENERATOR, & THE APU. ONLY THE NR 2 GENERATOR REMAINED AS A POWER SOURCE. EPCU FOUND IDG 3/GN/INTEC NSA. FOUND OIL OVER SERVICED BY 2 QTS. DRAINED & FLUSHED IDG OIL PER FIM 24 -20-33 FIG 129 AND CHECKED THE FILTER. FOUND NIL CONTAMINATION. PERFORMED WIRING CHECK IAW FIM 24-20-34. FOUND OK. E NGINE RUN COMPLIED WITH, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007022200074 20070222 00074 NM 2007 2 22 UPS07449183 1 20070108 A 5320 65B1635112 PANEL BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 1010-1090 CTR SHEAR PANEL EDGE FOUND CORRODED. CORROSION BLEND OUT 0.035 X .5 X 20 INCHES EXCE ED SRM LIMIT. SHEAR PANEL REPLACED AS PER MM 20-51-01 AND PILOT HOLES REPAIRED AS PER RS R53-41-35733 AND UPS ENGINNERI NG FILE 747-53-20388. 2 L 7 4 4F A20WE 2007022200081 20070222 00081 NM 2007 2 22 SWAA070881 1 20070215 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED HC1 CHECK, FOUND KEEL BEAM SKIN CRACKED AT BS 716, STR 27R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007022200085 20070222 00085 NM 2007 2 22 SWAA070908 1 20070215 A 5310 6546818 CREASE BEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT 935, RBL 70. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007022200089 20070222 00089 NM 2007 2 22 SWAA071039 1 20070220 A 5311 6546550 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED BS 787, STR 9L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007022200094 20070222 00094 NM 2007 2 22 SWAA071044 1 20070220 A 5313 6551698 STRINGER SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 663, STR 2L. REMOVED AND REPLACED STRINGER SPLICE PER S RM. 2 L 7 2 4F RT A16WE 2007022200095 20070222 00095 NM 2007 2 22 SWAA071046 1 20070220 A 5313 6551698 STRINGER SPLICE BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, STR 25L. REMOVED AND REPLACED STRINGER SPLICE PER ER. 2 L 7 2 4F RT A16WE 2007022200096 20070222 00096 2007 2 22 DXTA200701950 2 20070216 A 7320 FADEC CESSNA 750 750 2076810 CE LT ENGINE MALFUNCTIONED E DXTA E ENGINE SHUTDOWN J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 941QS 7500141 LT ENGINE START WAS NORMAL, BUT AT IDLE, AMBER CAS MSG (FADEC FAULT L A-B) ILLUMINATED, AND THE ENGINE SHUTDOWN. FADEC RESET HAD NOT AFFECT ON FADEC OPERATION. DOWNLOADED FAULTS NO FAULTS DETECTED. RAN AIRCRAFT OPS CHECK GOOD. WORK D ONE IAW CESSNA 750 MM CH 71-00-04. 2 L 7 2 4J RT T00007WI 2007022200097 20070222 00097 NM 2007 2 22 SWAA071029 1 20070220 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER MM. 2 L 7 2 4F RT A16WE 2007022200098 20070222 00098 NM 2007 2 22 SWAA071036 1 20070220 A 5311 65C22909 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED BS 500C, STR 9L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007022200099 20070222 00099 NM 2007 2 22 SWAA071038 1 20070220 A 5311 65C25228 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED BS 727E, STR 9L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007022200100 20070222 00100 NM 2007 2 22 SWAA071042 1 20070220 A 5523 65C2638416M ATTACH FITTING BOEING 737 7373G7 1384595 NM ELEVATOR TAB BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED C4 CHECK, FOUND RIGHT ELEVATOR TAB CONTROL ATTACH POINT BROKEN. REMOVED AND REPLACED ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2007022200101 20070222 00101 NM 2007 2 22 SWAA071021 1 20070220 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 L1 DOOR EMERGENCY EXIT LIGHT ASSY LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007022200103 20070222 00103 NM 2007 2 22 SWAA071025 1 20070220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200104 20070222 00104 NM 2007 2 22 SWAA070911 1 20070215 A 5311 65C22908 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500B, STR 26L TO 27R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007022200105 20070222 00105 NM 2007 2 22 SWAA070910 1 20070215 A 5311 65C25229 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727D, LBL 8. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007022200108 20070222 00108 NM 2007 2 22 SWAA070870 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200109 20070222 00109 NM 2007 2 22 SWAA070874 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200110 20070222 00110 NM 2007 2 22 SWAA070878 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200111 20070222 00111 NM 2007 2 22 SWAA070876 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200112 20070222 00112 NM 2007 2 22 SWAA070875 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200113 20070222 00113 NM 2007 2 22 SWAA070882 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200114 20070222 00114 NM 2007 2 22 SWAA070873 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200117 20070222 00117 NM 2007 2 22 SWAA070889 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200118 20070222 00118 NM 2007 2 22 SWAA070801 1 20070213 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 723SW 27855 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 41 TO RBL 5. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007022200121 20070222 00121 NM 2007 2 22 SWAA070798 1 20070213 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 474WN 33861 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER MISSING AT ROW 7 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007022200123 20070222 00123 NM 2007 2 22 SWAA070751 1 20070213 A 5220 507978 DOOR BOEING 737 7373H4 1384600 NM EMERGENCY EXIT OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 LEFT OVERWING EMERGENCY EXIT DOOR OUT OF ADJUST. ADJUSTED DOOR PER MM. 2 L 7 2 4F RT A16WE 2007022200125 20070222 00125 NM 2007 2 22 SWAA070771 1 20070213 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 450, STR 17R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007022200126 20070222 00126 NM 2007 2 22 SWAA070791 1 20070213 A 5330 6545768 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 305, STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007022200127 20070222 00127 NM 2007 2 22 SWAA070794 1 20070213 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 765, STR 23L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007022200131 20070222 00131 NM 2007 2 22 SWAA070802 1 20070213 A 5311 6545807 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 291.5, STR 15R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007022200132 20070222 00132 CE 2007 2 22 DXTA200701942 1 20070211 A 3240 BRAKE ASSY BEECH MU300 400A 1155402 CE MLG UNKNOWN E DXTA O OTHER O OTHER LD LANDING 1 GL 07 161QS RK435 BOTH SIDES BRAKES HAVE A LOT OF TRAVEL WITH NO BRAKING THEN IT BRAKES HARD TURNING TO ONE SIDE. AFTER BLEEDING THE BRAKE S WITH THE HYDRAULIC MULE AND CHECKING THE MASTER CYLINDER RESERVOIR, TAXI CHECKED AND FOUND THE BRAKES TO BE OPERATING NORMALLY IAW HAWKER 400XP AMM 32-40-00. 2 H 7 2 4F RT A16SW 2007022200133 20070222 00133 NM 2007 2 22 SWAA070792 1 20070213 A 5322 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007022200134 20070222 00134 NM 2007 2 22 SWAA070867 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200135 20070222 00135 NM 2007 2 22 SWAA070866 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200136 20070222 00136 NM 2007 2 22 SWAA070865 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200140 20070222 00140 NM 2007 2 22 SWAA070897 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200141 20070222 00141 CE 2007 2 22 DXTA200701941 1 20070211 A 2930 1304111 ANNUNCIATOR CESSNA 560 560XL 2076702 CE COCKPIT FAULTY E DXTA O OTHER S J AFFECT SYSTEMS WARNING INDICATION LD LANDING 1 GL 07 694QS 4023 5605194 WITH GEAR SELECTED DOWN AND LOCKED (3 GREEN, NO RED) SELECTED FLAP SWITCH TO 15 AND 'HYD' PRESSURE LIGHT CAME ON FLASING WITH MASTER CAUTION FLASHING INSTANTLY WITH NO DELAY.TROUBLESHOT TO FAULTY ANNUNCIATOR PANEL. REPLACED WITH SERVICEABLE UNIT. OPERATIONAL CHECK NORMAL IAW CESSNA 560XL MM 31-50-01. 2 L 7 2 4F RT A22CE 2007022200142 20070222 00142 CE 2007 2 22 DXTA200701936 1 20070213 A 3260 S33682 BULB CESSNA 500 560CESSNA 2076750 CE MLG INDICATOR BURNED OUT E DXTA O OTHER P NO WARNING INDICATION LD LANDING 1 GL 07 314QS 8341 5600441 LEFT GEAR LIGHT DID NOT ILLUMINATE WITH THE GEAR DOWN CONFIRMED LIGHT INOP WITH ROTARY TEST. CYCLED GEAR 3 TIMES WITH NO CHANGE. VISUALLY CONFIRMED GEAR EXTENDED. FOLLOWED EMERGENCY GER EXTENTION CHECKLIST WITH NO CHANGE. AFTER LANDING C ONFIRMED GEAR LOCKED BEFORE TAXI IN TO FBO. JACKED AIRCRAFT AND CYCLED GEAR IAW CESSNA 560 MM 32-01-00. INSTALLED NEW B ULB P/N S3368-2 IN LH DOWNLOCK LIGHT. DURING GEAR CYCLES, ALL INDICATIONS NORMAL. DOWNJACKED AIRCRAFT, SERVICED EMERG. G EAR BOTTLE AND HYD. RESERVOIR AS REQUIRED. SAFETIED EMERG. GEAR ARM. 2 L 7 2 4F RT A22CE 2007022200146 20070222 00146 NM 2007 2 22 SWAA070904 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200147 20070222 00147 2007 2 22 DXTA200701937 2 20070213 A 7200 960111901 SEAL BEECH MU300 400A 1155402 CE ENGINE BINDING E DXTA O OTHER O OTHER DE DESCENT 1 GL 07 142QS 910 RK432 AFTER CRUISING AT FL360 FOR APPROX. 90 MINUTES, UPON BEING CLEARED FOR DESCENT LEFT THROTTLE STUCK @ 97.0 N1, THROTTLE W OULD NOT BUDGE. FINALLY OUT OF FL240 IT CAME FREE & OPERATED NORMALLY. TEMP WAS -10 RAT. REMOVED OLD SEALS REPLACED WTH NEW. LUBED TELESCOPING ROD, RESECURED OPS CHECK GOOD. I/A/W RAYTHEON COMMUNIQUE NR 45 2 H 7 2 4F RT A16SW 2007022200148 20070222 00148 CE 2007 2 22 DXTA200701938 1 20070211 A 3260 603731 DOWNLOCK SWITCH CESSNA 680 680CE 2076811 CE MLG INOPERATIVE E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 362QS 1181 6800051 DURING APPROACH GEAR UNLOCK LIGHT LIGHT ILLUMINATED AND RIGHT GEAR WAS NOT INDICATING GREEN. LEFT MAIN AND NOSE INDICATE D GREEN. AFTER MANUEVRING AND LEAVING THE PATTERN FOR 5 MINS, UNLOCK LIGHT EXTINGUISHED AND THREE GREEN WERE PRESENT FOR A SAFE LANDING. NO BOTTLE WAS BLOWN. FOUND RT MAIN LANDING GEAR ACTUATOR DOWNLOCK SWITCH GOES INOPERATIVE WHEN FROZEN. REMOVED & REPLACED RT MAIN LANDING GEAR DOWN LOCK SWITCH. IAW CE680 MM 32-30-40 & 32-60-00 2 L 7 2 4F RC T00012WI 2007022200149 20070222 00149 NM 2007 2 22 SWAA070775 1 20070213 A 5311 6546539 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RIGHT WL 201 TO WL 208. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007022200150 20070222 00150 NM 2007 2 22 SWAA070772 1 20070213 A 5311 6546540 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 3R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007022200151 20070222 00151 NM 2007 2 22 SWAA070793 1 20070213 A 5322 6546569 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CORRODED AT BS 987, STR 23L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007022200156 20070222 00156 CE 2007 2 22 DXTA200701948 1 20070215 A 3260 MS243311 UPLOCK SWITCH BEECH MU300 400A 1155402 CE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 123QS RK486 RED LIGHT ON GEAR HANDLE REMAINS ON WHEN GEAR IS RETRACTED. GEAR WAS CYCLED ONE TIME AND RED LIGHT STILL DID NOT GO OUT . GEAR IS O.K. WHEN GEAR IS SELECTED DOWN.FOUND LEFT MAIN GEAR UPLOCK SWITCH READING HIGH RESISTANCE. REMOVED AND REPLAC ED SWITCH READING HIGH RESISTANCE. REMOVED AND REPLACED SWITCH WITH NEW SWITCH. PERFORMED SWITCH ADJUSTMENTS. GEAR SWING S AND OPERATIONAL CHECKS GOOD. ALL WORK PERFORMED I/A/W BEECH JET 400A M/M CH: 32-10-00-201 AND WIRING MANUAL CH: 32-61- 01-02 2 H 7 2 4F RT A16SW 2007022200158 20070222 00158 NM 2007 2 22 SWAA070763 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200159 20070222 00159 NM 2007 2 22 SWAA070762 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200160 20070222 00160 CE 2007 2 22 DXTA200701952 1 20070216 A 2750 FLAP SYSTEM CESSNA 750 750 2076810 CE TE FLAPS UNKNOWN E DXTA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 07 960QS 7500160 FLAPS FAIL DURING APPROACH AND DID NOT RESET. FLAPS FAILED AT 0* INDICATION (UP). PERFORMED VISUAL INSPECTION OF FLAP S YSTEM. CHECKED BITE CODES, CLEARED BITE CODES. CYCLED FLAPS AND RECHECKED BITE CODES - NO DEFECTS AT THIS TIME. OPS C HECKS - GOOD - ALL INDICATIONS AND SETTINGS NORMAL AT THIS TIME - MAINTENANCE I.A.W. CE-750 M.M. CHAPTER 27-50-00 2 L 7 2 4J RT T00007WI 2007022200161 20070222 00161 NM 2007 2 22 SWAA070766 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007022200163 20070222 00163 NM 2007 2 22 SWAA070760 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200164 20070222 00164 NM 2007 2 22 SWAA070903 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200165 20070222 00165 2007 2 22 DXTA200701945 4 20070214 A 3417 8220374419 ADC AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE FWD E/E BAY MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 218QS 256 256 118 IN FLIGHT (AUTO SLATS) LIGHT ILLUMINATED ACCOMANIED BY LOSS OF NR 2 AIRSPEED INDICATOR. MANUALLY PULLED (ADC 2) CIRCUT B REAKER IAW CHECKLIST. DUPLICATED, FOUND NR 2 ADC TO BE DEFECTIVE. REMOVED NR 2 ADC INSTALLED CUSTOMER SUPPLIED OVERHAUL ED ADC IN NR 2 ADC POSITION. C/W FUNCT. TEST & RECONNECT CHECK WITH NO DEFECTS NOTED. ALL WORK PERFORMED IAW FALCON 2000 MM 34-101. ALSO C/W FLAPS/SLATS NORMAL AND AUTO MODE FUNCT. TEST. NO DEFECTS NOTED. ALL PERFORMED IAW FALCON 2000 MM. 27 -803. C/W PITOT/STATIC SYS LEAK CHECK PERFORMED IAW FAR 91.411 ON 2/15/07 AND TRANSPONDER. 2 K 7 2 4F 4 F RT A50NM E44NE 2007022200167 20070222 00167 NM 2007 2 22 SWAA070758 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200168 20070222 00168 CE 2007 2 22 DXTA200701946 1 20070214 A 2750 FLAP SYSTEM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 998QS 7500198 ON FINAL APPROACH AMBER CAS MESSAGE FLAP FAIL WHEN FLAPS/SLATS SELECTED TO 5'. ABNORMAL PROCEDURES COMPLETED AND FLAPS FAILED TO EXTEND BEYOND ABOUT 2' WITH SLATS EXTENDED. OPERATED FLAP SYSTEM THROUGH NUMEROUS CYCLES PERFORMED CONTINUITY CHECKS & GROUND CHECKS & CHECKED ALL RESOLVER VOLTAGES WITH FLAP BREAKOUT BOX ALL CHECKS & VOLTAGES FOUND TO BE GOOD & WITHIN LIMITS NO OTHER DEFECTS OR FAULTS FOUND SYSTEM OPS CHECKED GOOD IAW CE750 MM 27-55-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007022200169 20070222 00169 CE 2007 2 22 DXTA200701944 1 20070209 A 3260 MS243311 DOWNLOCK SWITCH BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE RT MLG INOPERATIVE E DXTA O OTHER N FALSE WARNING DE DESCENT 1 GL 07 145QS 869 RK421 RT MLG DOWN AND LOCKED LIGHT DID NOT ILLUMINATE WHEN GEAR SELECTED DOWN. RAN THE CHECKLIST, ALTERNATE GEAR EXTENSION PRO CEDURE WAS NOT NECESSARY. LANDED WITHOUT INCIDENT AND THE LIGHT CAME BACK ON STEADY AFTER TOUCH DOWN. REPLACED RH MAIN G EAR DOWN LOCK SWITCH WITH NEW CUSTOMER SUPPLIED SWITCH. ADJUSTED DOWN LOCK SWITCH AND CYCLED GEAR NUMEROUS TIMES, OPS TE ST GOOD. ALL WORK IAW 400XP MM 32-10-00 AND WIRING 32-61-00 2 H 7 2 4F 4 F RT A16SW E25EA 2007022200170 20070222 00170 CE 2007 2 22 DXTA200701943 1 20070211 A 3040 85611 CONTROL MODULE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE WINDSCREEN HEAT INOPERATIVE E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 651QS 4911 5605251 RT WINDSCREEN FAULT ANNUNCIATOR ILLUMINATED, WHILE COMPLETING CHECKLIST, THE RIGHT WINDSHIELD SHATTERED. REMOVED CRACKED RT WINDSHIELD INSTALLED NEW WINDSHIELD. INSTALLED REPAIRED WINDSHIELD CONTROL RT PN ON 856-1-1 SN ON 205080073 RT WIN DSHIELD TEMP CONTROL REMOVED PN 856-1-1 SN OFF 0150026. PERFORMED SATISFACTORY LEAK AND OPS CHECK REF CE560XL MM REF 56 -12-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007022200171 20070222 00171 NM 2007 2 22 SWAA070757 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200172 20070222 00172 NM 2007 2 22 SWAA070756 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200176 20070222 00176 NM 2007 2 22 SWAA070780 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200177 20070222 00177 CE 2007 2 22 DXTA200701935 1 20070213 A 3241 ANTI-SKID SYS CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE RT MLG MALFUNCTIONED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 810QS 5600625 ON LANDING ROLL RT BRAKE ANTI-SKID ACTIVATES AS SOON AS PRESSURE IS APPLIED CAUSING A/C TO YAW & VEER LEFT ON RNWY. THE RT BRAKE WORKS FINE AT OR BELOW 50 KNOTS. VISUALLY INSPECTED LT AND RT BRAKE ASSY, CHECKED TRANSDUCERS AND WIRING OF A NTI-SKID SYSTEM. PERFORMED ANTI-SKID WIRING CHECK PER NETJETS 560 ANTI-SKID WIRING CHECK LIST 11/07/05. TAXIED AIRCRAFT OPS CHECK GOOD IAW CITAITON 560 MM CHPT 32-12-00 2 L 7 2 4F 4 F RT A22CE E00053EN 2007022200180 20070222 00180 NM 2007 2 22 SWAA070786 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200183 20070222 00183 NM 2007 2 22 SWAA070783 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200184 20070222 00184 NM 2007 2 22 SWAA070902 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200185 20070222 00185 NM 2007 2 22 SWAA070901 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200186 20070222 00186 NM 2007 2 22 SWAA070900 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200187 20070222 00187 NM 2007 2 22 SWAA070887 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200189 20070222 00189 NM 2007 2 22 SWAA070885 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200190 20070222 00190 NM 2007 2 22 SWAA070896 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200191 20070222 00191 NM 2007 2 22 SWAA070895 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200192 20070222 00192 NM 2007 2 22 SWAA070894 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200193 20070222 00193 NM 2007 2 22 SWAA070893 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022100216 20070221 00216 WP 2007 2 21 ABXA070043 1 20070202 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 900AX 47380 EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00. 2 L 7 2 4F A6WE 2007022100219 20070221 00219 NE 2007 2 21 ABXA070048 2 20070215 A 7321 8063505 CONTROL UNIT BOEING 767 767200 1385120 NM GE CF6 CF680A 30025 NE RT ENGINE MALFUNCTIONED A ABXA E ENGINE SHUTDOWN Y ENGINE STOPPAGE AP APPROACH 1 GL 23 752AX 3736 23434 580268 AS CREW WAS ON FINAL AT ILN, GOING THROUGH 27K, NR 2 ENGINE HAD AN UNCOMMANDED SHUTDOWN. CREW RESTARTED ENGINE WITHOUT ANY FURTHER ISSUES. NO EMERGENCY DECLARED. NO EN ROUTE DELAY. REMOVED AND REPLACED NR 2 ENGINE MAIN ENGINE CONTROL IA W B767 AMM 73-21-01-4, REF WORK PACK 600266182 FOR WORK ACCOMPLISHED. 2 L 7 2 4F 4 F RT A1NM E13NE 2007022100221 20070221 00221 NM 2007 2 21 ASAA0741447 1 20070213 A 5322 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 CORROSION ON SHEAR TIE. REMOVED DAMAGED SECTION OF FRAME, FABRICATED AND INSTALLED FILLER AND SHEAR TIE IAW SRM 53-00-0 7, REPAIR 3. 2 L 7 2 4F RT A16WE 2007022100223 20070221 00223 NM 2007 2 21 ASAA0741449 1 20070213 A 5322 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 CORROSION ON SHEAR TIE. REMOVED DAMAGED SECTION OF FRAME, FABRICATED AND INSTALLED FILLER AND SHEAR TIE IAW SRM 53-00-0 7 REPAIR 3. 2 L 7 2 4F RT A16WE 2007022100225 20070221 00225 NM 2007 2 21 ASAA0771463 1 20070213 A 5321 147A5810121 FLOOR PANEL BOEING 737 737790 13844CN NM CABIN DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 FLOOR PANEL 22DF DELAMINATED. REPAIRED IAW SRM 53-00-50. 2 L 7 2 4F RT A16WE 2007022100237 20070221 00237 NM 2007 2 21 ASAA0741470 1 20070218 A 5754 65C26603352 SKIN BOEING 737 7374Q8 138447Q NM L/E SLAT DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 NR 4 SLAT I/B TRAILING EDGE DELAMINATED. PREPPED DAMAGED AREA FABRICATED AND BONDED REPAIR CORE AND DOUBLER IAW SRM 51- 70-10 REPAIR 4. 2 L 7 2 4F RT A16WE 2007022100272 20070221 00272 NE 2007 2 21 UIEA200700029 2 20070126 A 7320 665038062899 MEC BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE NR 3 ENGINE UNSERVICEABLE A UIEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 523MC 21782 517675 NR 3 ENGINE ROLLED BACK IN CLIMB TO 42.6 PERCENT N1, 663KGS/HR FUEL FLOW WOULD NOT RESPOND TO THROTTLE MOVEMENT TO ADD P OWER. LOW THRUST CONFIRMED BY HIGH STAGE LIGHT ON, BLEED VALVE CLOSED LIGHT ON. REPLACED NR 3 MEC ,FUEL PUMP,AND CIT S ENSOR. ACCOMPLISHED TEST 5 MPA RUN PER AMM. 2 L 7 4 4F 4 F RT A20WE E23EA 2007022100279 20070221 00279 EA 2007 2 21 TRAX200700237 1 20070216 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 916EV 7757 SUSPECT CRACK ON UPPER CENTER SECTION OF ENG SUPPORT BEAM. FLTS 4725, 4146, 4510 CX. COMPLIED WITH RII REQUIREMENT FOR MAJOR REPAIR/ ALTERATION IAW SP607. ALL WORK ACCOMPLISHED IAW REO 601R-53-61-345. 2 L 7 2 4F RT A21EA 2007022100282 20070221 00282 EA 2007 2 21 TRAX200700239 1 20070216 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 923EV 7826 FLIGHT ATTENDANT FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007022100287 20070221 00287 NM 2007 2 21 UIEA200700037 1 20070129 A 5322 65B0432781 SHEAR TIE BOEING 747 7472D7B 1384803 NM BS 1800 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 AFT CARGO STA 1800 FRAME SHEAR TIE S-50R TO S-51L FOUND CORRODED. AFT CARGO STA 1800 FRAME SHEAR TIE REPAIRED AS PER SR M 53-10-04 FIG 3A. 2 L 7 4 4F RT A20WE 2007022100290 20070221 00290 EU 2007 2 21 07FDEA00437 1 20070209 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 407FE 254 PREVIOUS REPAIR ON STR 55 RT WITH 2 REPAIR SPLICES DO NOT MEET THE INTENT OS A310 SRM 53-10-14 FIG 201. REMOVED INCORRE CTED REPAIR AND REPAIRED AREA IAW A310 SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007022100291 20070221 00291 EA 2007 2 21 TRAX200700244 1 20070218 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 829AS 7232 EXIT FLOOR SIGN OUT. 2 L 7 2 4F RT A21EA 2007022100321 20070221 00321 EA 2007 2 21 TRAX200700228 1 20070214 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 748EV 10158 EXTERIOR EMERGENCY LIGHT AT ASD INOP. 2 L 7 2 4F RT A21EA 2007022100323 20070221 00323 EU 2007 2 21 07FDEA00446 1 20070211 A 2611 352000023 SMOKE DETECTOR AIRBUS 300 A300B4622R 3930312 EU CARGO BAY MALFUNCTIONED A FDEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 25 725FD 863 863 572 AFTER PUSHBACK AND ENGINE START RECEIVED ECAM FOR AFT CARGO CPT SMOKE. COMPLIED WITH ECAM AND QRH. PREPPED FOR REMOVAL OF NR 1 LWR CARGO COMP FIRE BOTTLE. REF:A300 M.M.CHAPT:26-23-11-4-02. OPENED FWD LWR CARGO DOOR. PULLED AND TAGGED C IRCUIT BREAKERS, REMOVED RT SIDEWALL PANEL (HARDWARE AND PANEL IN WORK AREA). ORDERED NEW FIRE BOTTLE (MPN-35200002-1) NIS OAK. NEW DISCHARGE CARTRIDGE (MPN-30900000M) IN STOCK OAK. REMOVED AND REPLACED AFT CARGO PIT FWD SMOKE DETECTOR P ER AMM 26-16-11-4 AND 26-16-00-5-01. OPS CHECK NML. DUE TO CREW QRH PROCEDURES OF DISCHARGING THE NR 1 LOWER CARGO BO TTLE REMOVED AND REPLACED THE NR 1 LOWER CARGO BOTTLE PER AMM 26-23-11-4-02 CLOSED AND SECURED THE SIDEWALL PANEL. 2 L 7 2 4F RT A35EU 2007022100324 20070221 00324 EA 2007 2 21 TRAX200700230 1 20070215 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 686BR 7715 CAPTAIN`S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007022100328 20070221 00328 WP 2007 2 21 07FDEA00452 1 20070212 A 5711 SPAR DOUG MD10 MD1010F 3022112 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 372FE 46610 C/W EA 8-5710-102021 WING LT WING REAR SPAR WEB CRACK AT XORS 217 COMPLIED WITH EA 8-5710-102021 IAW SRM 57-10-00 FIG 52 . 2 L 7 3 4F RT A22WE 2007022100331 20070221 00331 EU 2007 2 21 MALA070024 1 20070203 A 3260 UPLOCK SWITCH SAAB SF340 340B 7860101 EU MLG MALFUNCTIONED A MALA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 15 456XJ 340B456 AFTER GEAR RETRACTION ON TAKEOFF, LANDING GEAR DOWNLOCK LIGHTS WENT OUT, AND GEAR UNSAFE OR INTRANSIT LIGHT REMAINED ON. PUMP KEPT RUNNING. CYCLED LANDING GEAR PER QRH AND CONDITION REMAINED; EVEN WITH THE LANDING GEAR DOWN AND 3 GREEN IN DICATIONS THEY HYDRAULIC PUMP RAN CONTINUOUSLY. THE FLIGHT RETURNED TO INL AND LANDED WITHOUT INCIDENT. FROM L/P #1611 531: CLEANED UPLOCK SWITCHES ON ALL THREE LANDING GEAR. PERFORMED FUNCTIONAL TEST OF THE EXTENSION AND RETRACTION OF LA NDING GEARS. NO DISCREPANCIES NOTED. FUNCTION TEST DONE IAW SAAB 340 AMM. 2 L 7 2 4T RT A52EU 2007022100341 20070221 00341 NM 2007 2 21 SWAA071010 1 20070219 A 5330 6545765 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 794, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007022100350 20070221 00350 NM 2007 2 21 SWAA070917 1 20070216 A 3040 2315 CONTROLLER BOEING 737 7377H4 1384404 NM COCKPIT SHORTED A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 755SA 27871 R1 WINDOW HEAT TURNED ON, WINDOW HEAT CONNECTOR SHORTED, AND WINDOW CRACKED. REMOVED AND REPLACED WINDOW HEAT CONTROLLE R AND AND WINDOW PER MM. 2 L 7 2 4F RT A16WE 2007022100364 20070221 00364 NM 2007 2 21 SWAA070927 1 20070217 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 431WN 29845 EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007022100369 20070221 00369 NM 2007 2 21 SWAA070963 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022100371 20070221 00371 NM 2007 2 21 SWAA070920 1 20070216 A 2750 6946649 TORQUE TUBE BOEING 737 7373H4 1384600 NM T/E FLAP WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING AFT FLAP OUTBOARD TORQUE TUBE FAILED CHECK. REMOVED AND REPLACED TORQUE T UBE PER MM. 2 L 7 2 4F RT A16WE 2007022100372 20070221 00372 EA 2007 2 21 SWIA200717779 1 20070202 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS OUT OF RIG A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 939SW 7742 "FLAPS FAIL" CAUTION MESSAGE WHEN SELECTING FLAPS FROM 0 TO 8. PERFORMED FLAP BPSU RIGGING IAW RJ 200 MM 27-51-10. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007022100378 20070221 00378 EA 2007 2 21 SWIA200717783 1 20070201 A 4930 388273010 FUEL CONTROL CNDAIR CL600 CL6002B19 1900309 EA APU LEAKING A SWIA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 955SW 3361 3361 7817 UPON LANDING, SMELLED A FUEL SMELL AFTER STARTED THE APU. APU AUTO SHUT DOWN. REPLACED APU FUEL CONTROL UNIT IAW 49-31 -01. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007022100381 20070221 00381 NM 2007 2 21 SWAA071001 1 20070218 A 2560 6557463 FITTING BOEING 737 7375H4 138449D NM R2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED GIRT BAR FITTING PE R SRM. 2 L 7 2 4F RT A16WE 2007022100382 20070221 00382 SO 2007 2 21 SWIA200717784 1 20070130 A 2530 COFFEEMAKER EMB 120 EMB120ER 3260203 SO GALLEY ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 215SW 120281 FLIGHT ATTENDANT REPORTED OVERHEATED ODOR COMING OUT OF HOT JUGS. SWITCH WAS TURNED OFF AND ODOR DISAPPEARED. REPLACED HOT JUG WITH SERVICEABLE UNIT IAW 25-60-00. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007022100387 20070221 00387 NM 2007 2 21 UIEA200700033 1 20070129 A 5410 65B9405315 ACCESS PANEL BOEING 747 7472D7B 1384803 NM NR 2 PYLON WORN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 NR 2 PYLON RT ACCESS PANEL 463AR CUTOUT FOUND WORN AT TWO POSITIONS. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-272 049267 AND FAA FORM 8110-9. 2 L 7 4 4F RT A20WE 2007022100390 20070221 00390 NM 2007 2 21 NWAA070573162 1 20070209 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319114 3930350 NM EMERGENCY LIGHTS FAULTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 362NB 10407 10407 1982 CIDS IS FAULTING EPSU L. CORRECTED BY REPLACING LEFT EPSU. CHECKS OK. 2 L 7 2 4F RT A28NM 2007022100391 20070221 00391 EA 2007 2 21 QXEA200700067 1 20070115 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 309 S22R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD RIGHT SIDE OF FORWARD FUSELAGE AT FS 309 AND STRINGER 22R. REPAIRED IAW SRM 53-00-01, 53-21-01, AND 51-21-11. 2 L 7 2 4F RT A21EA 2007022100408 20070221 00408 WP 2007 2 21 DHL2007802519 1 20070129 A 5754 5652396 RIB DOUG DC8 DC873 302199C WP LT LE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 LT INBD FLAP RIB HAS FOUR CRACKS OF 1" AND 1.500" STA XW 125.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 2 PG 6 (SHEET 4). REMOVED CRACKED RIV IAW SRM 57-1-0 PG.1, SRM 51-1-21, SRM 51-1-20D. FABRICATED RIB (AL2024"0" 0. 050") IAW SRM 57-7-1 FIG 2 PG 6 SHEET 4. HEAT TREATED FROM 2024"0" TO 2024T4 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREAT ED AND PRIMED AREA AND RIB IAW SRM 51-1-8B. INSTALLED RIB IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007022100410 20070221 00410 NM 2007 2 21 SWAA071018 1 20070219 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 725SW 27857 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 771, RBL 3. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007022100412 20070221 00412 NM 2007 2 21 SWAA070997 1 20070218 A 2910 AE2464162EO163 HYDRAULIC LINE BOEING 737 7373H4 1384600 NM RT MLG LEAKING A SWAA K NONE K FLUID LOSS DE DESCENT 1 SW 29 302SW 22942 ON SHORT FINAL -A- SYSTEM HYDRAULIC FLUID LOSS AND SYSTEM FAILURE. FOUND HYDRAULIC LINE LEAKING AT RT MLG RETRACT ACTUA TOR. REMOVED AND REPLACED HYDRAULIC LINE PER MM. 2 L 7 2 4F RT A16WE 2007022200011 20070222 00011 SO 2007 2 22 C2XA07IA039 1 20070218 A 4930 FUEL SYS EMB 145 EMB145XR 3260214 SO APU LEAKING A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 11127 5664 5664 SPE0214500 145697 IAH - FLIGHT 2097, DURING PREFLIGHT INSPECTION THE CREW REPORTED A FUEL SMELL IN THE COCKPIT WITH THE APU ON. MAINTENAN CE INSPECTED THE AIRCRAFT AND PLACED THE APU ON MEL 49-00-00 -C- 116102. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. THE AIRCRAFT RETURNED TO IAH ON 02/19/07 WHERE MAINTENANCE REMOVED AND REPLACED THE APU, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007022200016 20070222 00016 NM 2007 2 22 CALA0700072 1 20070219 A 2742 6355B000103 TRIM MOTOR BOEING 737 737824 13844BZ NM HORIZ STAB FAILED A CALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 27 77258 10926 30802 THE ELECTRIC STAB TRIM FAILED WHILE ON APPROACH TO CLE. THE QRH WAS CONSULTED, AN EMERGENCY WAS DECLARED, AND MANUAL AD JUSTMENT OF TRIM WAS USED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE ELECTRIC STAB TR IM MOTOR IAW MM 27-41-71 AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2007022200017 20070222 00017 NM 2007 2 22 CALA0700073 1 20070219 A 5330 654576987 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND SKIN UNDER NR 1 DME ANTENNA CORRODED AT STA 460-480, S26L TO S26R. THE SKIN WAS REPAIRED IAW ECRA 5331 -01289. 2 L 7 2 4F RT A16WE 2007022200029 20070222 00029 EA 2007 2 22 COMA0760191 1 20070214 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA NLG OUT OF ADJUST A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 784CA 7319 FLIGHT 5317 - DURING CLIMBOUT OF CVG RECEIVED A STEERING INOPERATIVE CAUTION MESSAGE, FLIGHT RETURNED TO THE FIELD. ADJ USTED THE NLG PROXIMITY SENSOR S03 AND RETRACTED LANDING GEAR MULTIPLE TIMES WITH NO DISCREPANCIES NOTED. 2 L 7 2 4F RT A21EA 2007022200031 20070222 00031 EA 2007 2 22 COMA0760193 1 20070215 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING OBSTRUCTED A COMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 01 2750 7027 FLIGHT 5363 - DURING CLIMBOUT OF CVG RECEIVED A FLAP FAIL CAUTION MESSAGE. REMOVED ICE AND SAND FROM FLAP AREA THAT INT ERFERED WITH PROPER OPERATION OF THE FLAP SYSTEM. 2 L 7 2 4F RT A21EA 2007022200034 20070222 00034 NE 2007 2 22 COMA0760200 2 20070219 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE NR 2 POWER LOSS A COMA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 01 784CA 7319 807481 FLIGHT 5103 - DURING ADDITION OF POWER FOR TAKEOFF NR 2 ENGINE WILL NOT SPOOL ABOVE 30 PERCENT. ABORTED TAKEOFF AT 15 K TS. INSPECTED ENGINE, NO DEFECTS NOTED. PERFORMED LOW AND HIGH POWER RUNS, NO DEFECTS NOTED (CND). 2 L 7 2 4F 4 F RT A21EA E15NE 2007022200035 20070222 00035 EA 2007 2 22 COMA0770016 1 20070216 A 2720 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA RUDDER SYS MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 669CA 10176 FLIGHT 4998 - TAKEOFF ABORTED DUE TO CONFIG RUDDER WARNING MESSAGE. AIRCRAFT SPEED WAS APPROX 10 KTS. PERFORMED OPS CH ECK OF RUDDER TRIM SYSTEM AND CHECKED RUDDER POSITION TRANSMITTER RIGGING, ALL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007022200042 20070222 00042 EA 2007 2 22 HNAA0700041 1 20070215 A 2422 DH103024600C INVERTER DHAV DHC8 DHC8311 1386006 EA ELECTRICAL SYS FAILED A HNAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 327EN 46080 11466 261 CREW NOTICED SMOKE COMING OUT OF LEFT DC C/B PANEL. TURNED OFF INVERTER AND SMOKE DISSIPATED. REPLACED PRIMARY INVERTE R. 2 H 7 2 4T RT A13NM 2007022200059 20070222 00059 WP 2007 2 22 UPS07849215 1 20070218 A 3350 SWITCH DOUG DC8 DC873F 302199F WP COCKPIT STIFF A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT SWITCH HARD TO MOVE TO DISARM CHECK POSITION. REPLACED EMERGENCY EXIT LIGHT SW ITCH PER IPC 33-50-00-003. OPS CHECK OK PER AMM 33-50-00-0. 2 L 7 4 4F RT 4A25 2007022200063 20070222 00063 NM 2007 2 22 UPS07549222 1 20070203 A 5311 146N103072 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 413UP 23853 INSPECTION TYPE:C DENTS IN AFT CARGO FUSELAGE FRAME STA 1540, S26L(2EA). FRAME REPAIR STA 1540, S26L HAS (2EA) DENTS, R EPAIR HAS BEEN ACCOMPLISHED PER EA 757-5362-27-A1604 WITH NO DEVIATIONS AND PER UPS EO B757-5310-26177-A. 2 L 7 2 4F RT A2NM 2007022200087 20070222 00087 NM 2007 2 22 SWAA071043 1 20070220 A 5315 6936656 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM WEB CORRODED AT BS 1006, LBL 41. REMOVED AND REPLACED FLOORBEAM WEB PER SRM . 2 L 7 2 4F RT A16WE 2007022200090 20070222 00090 NM 2007 2 22 SWAA071037 1 20070220 A 5311 6546558 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED BS 907, STR 9L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007022200091 20070222 00091 NM 2007 2 22 SWAA071026 1 20070220 A 5311 6546560 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 947, STR 24R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007022200102 20070222 00102 NM 2007 2 22 SWAA071050 1 20070220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007022200107 20070222 00107 NM 2007 2 22 SWAA070883 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200115 20070222 00115 NM 2007 2 22 SWAA070884 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200119 20070222 00119 NM 2007 2 22 SWAA070790 1 20070213 A 3350 20131A BATTERY PACK BOEING 737 7373Y0 1384671 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED A2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007022200120 20070222 00120 NM 2007 2 22 SWAA070799 1 20070213 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 474WN 33861 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER MISSING AT ROW 22 DEF. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007022200143 20070222 00143 NM 2007 2 22 SWAA070906 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200152 20070222 00152 NM 2007 2 22 SWAA070770 1 20070213 A 5322 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 927, STR 24L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007022200174 20070222 00174 NM 2007 2 22 SWAA070754 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200181 20070222 00181 NM 2007 2 22 SWAA070785 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200194 20070222 00194 NM 2007 2 22 SWAA070892 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200197 20070222 00197 NM 2007 2 22 SWAA070888 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200198 20070222 00198 NM 2007 2 22 SWAA070886 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200201 20070222 00201 2007 2 22 SWAA070862 4 20070215 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007022200203 20070222 00203 NM 2007 2 22 SWAA070781 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200204 20070222 00204 NM 2007 2 22 SWAA070768 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 951, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200205 20070222 00205 NM 2007 2 22 SWAA070779 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200207 20070222 00207 NM 2007 2 22 SWAA070778 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200210 20070222 00210 NM 2007 2 22 SWAA070782 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200214 20070222 00214 NM 2007 2 22 07FDEA00467 1 20070213 A 2400 ELECTRICAL SYS BOEING 727 727227 1384078 NM CONTAMINATED A FDEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 25 490FE 21493 DURING MAIN DECK LOADING EXCESSIVE WATER RAN INTO E/E COMPARTMENT POPPING CABIN AIR FLOW C/B, CABIN SMOKE C/B, CARGO DOO R CONTROL C/B, AND 3 C/B'S ON THE P-18 PANEL MAIN LIGHTS C/B'S. LOWER E/E HAS WATER DRIPPING ON THE WIRE BUNDLE OVERHEA D TOP AND TO LEFT OF E/E DOOR. WATER FOUND LEAKING AROUND RIGID BARRIER BOTH SIDES INTO E/E COMPARTMENT AND FROM L1 DO OR SILL INBBD TO THE COCKPIT DOOR AND R1 DOOR HAS A WATER LEAK ON THE SIDEWALL INTO THE E/E COMPT. SEALANT BMS 5-30B DID NOT CROSS TRYING TO CONTACT LAX FOR HOT WAX GUN. VACUUMED STANDING WATER FROM BOTTOM OF BELLY OF A/C IN FRONT OF GEN C ONTROL BULKHEAD. 2 L 7 3 4F A3WE 2007022200215 20070222 00215 NE 2007 2 22 GLBA20060894 2 20070212 A 7261 LABYRINTH SEAL EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE NR 1 ENGINE DETERIORATED A GLBA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NM 03 108UX 120108 PILOT REPORT OF SMOKE IN CABIN AND COCKPIT ON FINAL DESCENT INTO DENVER. SMOKE WAS NOTICED COMING FROM NR 1 ENGINE. MA INTENANCE REMOVED AND REPLACED THE NR 1 ENGINE.PER T.C. 120-7100-00. SUBSEQUENT ENGINE RUNS SUCCESFUL. OPERATIONAL CHECK S GOOD. AIRCRAFT RELEASED FOR SERVICE 2 L 7 2 4T 4 T RT A31SO E20NE 2007022200218 20070222 00218 NM 2007 2 22 SWAA071034 1 20070220 A 3350 20131A BATTERY PACK BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007022200219 20070222 00219 NM 2007 2 22 SWAA071023 1 20070220 A 3350 411A3220 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 490WN 32476 FWD CABIN EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007022200220 20070222 00220 NM 2007 2 22 SWAA071019 1 20070216 A 3320 415A8900139 LIGHT BOEING 737 7377H4 1384404 NM FWD GALLEY SHORTED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 468WN 33858 SPARKS FROM FWD GALLEY POWER PANEL. FOUND GALLEY POWER LIGHT ASSY SHORTED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007022200221 20070222 00221 NM 2007 2 22 SWAA071022 1 20070220 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 237WN 34632 EEPLS COVER MISSING AT LT OVERWING EXIT. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007022200222 20070222 00222 NM 2007 2 22 SWAA071027 1 20070220 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 660, BL 0. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2007022200224 20070222 00224 NM 2007 2 22 SWAA071047 1 20070220 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 777, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007022300001 20070223 00001 SO 2007 2 23 C2XA07TY005 1 20070221 A 5320 14522460007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14952 145067 TYS DURING A CURRENT 1C INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM TOPCAP AT FR 20. MAINTENANCE REMOVED A ND REPLACED THE OMEGA BEAM IAW EMB 145 SRM 51-40-02. DRILL, COUNTERSUNK, ALLODINED, PRIMED AND PAINTED NEW PART IAW EMB 145 51-21-03 AND CPM 51-21-07. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE C-CHECK INSPECTIO N. 2 L 7 2 4T RT T00011AT 2007022300003 20070223 00003 SO 2007 2 23 C2XA07BT019 1 20070219 A 3350 2013BR BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST NR NOT REPORTED 1 SW 27 19554 5998 24 145587 EWR LOG SQUAWK FLT 2665 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY IAW EMB145 AMM 37-50-04. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007022300005 20070223 00005 SO 2007 2 23 C2XA07IA043 1 20070220 A 3350 LIGHT EMB 145 EMB145XR 3260214 SO CABIN MALFUNCTIONED A C2XA O OTHER O OTHER UK UNKNOWN 1 SW 27 12172 14500864 IAH - FLIGHT 2152, THE CREW REPORTED THAT THE EMERGENCY LIGHTS CAME ON DURING FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOU T INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE EMERGENCY LIGHT SYSTEM WITH NO DEFECTS NO TED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007022300006 20070223 00006 GL 2007 2 23 C2XA07TY007 2 20070220 A 7200 AE3007A1P ENGINE EMB 145 EMB145EP 3260221 SO ALLSN AE300 AE3007A GL NR 1 DAMAGED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 14942 145037 TYS A/C HAD SMOKE ON CLIMBOUT AND THEN CLEARED. THEN ANOTHER TIME ON LEVELING OFF, AGAIN LEFT. A/C WAS CHECKED OUT AND FERRIED TO TYS. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW RR TASKCARD 627100. OPS AND LEAK CHECKS WERE GOO D, RELEASED BACK TO SERVICE. [07-24-07] THE CAUSE OF THE SMOKE WAS A LEAKING NR 4 CARBON SEAL. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007022300007 20070223 00007 SO 2007 2 23 C2XA07CL023 1 20070218 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11536 145520 DURING ROUTINE MAINTENANCE THE OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENC Y LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007022300008 20070223 00008 SO 2007 2 23 C2XA07CL024 1 20070219 A 5240 14531554001 ROLLER EMB 145 EMB145EP 3260221 SO FUSELAGE FROZEN A C2XA C ABORTED TAKEOFF J WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 14940 145033 CLE FLIGHT 2795 THE CREW REPORTED A SERVICE DOOR WARNING INDICATION. TAKEOFF WAS ABORTED. MAINTENANCE INSPECTED, CLEAN ED AND LUBED THE SERVICE DOOR ROLLERS. OPERATIONAL CHECK OF DOOR WAS GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2007022300009 20070223 00009 NM 2007 2 23 CALA0700077 1 20070219 A 3350 D71701100 BATTERY PACK BOEING 737 737724 13844BY NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 54711 28782 THE AISLE PATH EMERGENCY LIGHTING AT ROWS 15-21 ABC WERE FOUND INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED I AW MM 33-51-06-960-805. 2 L 7 2 4F RT A16WE 2007022300011 20070223 00011 NM 2007 2 23 CALA0700079 1 20070220 A 5320 6545819U116 STIFFENER BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND A 1 INCH CRACK THROUGH SECOND FASTENER HOLE IN NOSE WHEEL WELL TOP CENTER ACTUATOR BEAM STIFFENER, STA 229.8. A NEW STIFFENER WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007022300012 20070223 00012 NM 2007 2 23 CALA0700080 1 20070220 A 5320 654581951 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND A 6 INCH CRACK APPROXIMATELY 6 INCHES AFT OF FORWARD BULKHEAD IN NOSE WHEEL WELL TOP CENTER ACTUATOR SU PPORT BEAM WEB AT STA 233.8. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007022300013 20070223 00013 NM 2007 2 23 CALA0700081 1 20070220 A 5330 6545778 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 INSPECTION FOUND A 0.75 INCH CRACK IN FUSELAGE SKIN AT R-2 DOOR FORWARD LOWER RADIUS, STA 947.5, S14R. A DOUBLER WAS IN STALLED IAW SRM 53-60-01, FIGURE 201. 2 L 7 2 4F RT A16WE 2007022300016 20070223 00016 2007 2 23 COMA0760204 4 20070221 A 3425 6229336400 AHRS CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 455CA 15975 7592 FLIGHT 5500 - FMS AND HSI FAILED EN ROUTE. LANDED UNSC AT CVG WITHOUT INCIDENT. COULD NOT DUPLICATE. REPLACED NR 1 AH RS. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007022300017 20070223 00017 EA 2007 2 23 COMA0760203 1 20070221 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 708CA 7235 FLIGHT 5689 - FLAP FAIL MESSAGE ON APPROACH. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. COMPLIED WITH AD 27-046 A D INCLUDING FLAP FLEX SHAFT REJUVE TASK. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007022300018 20070223 00018 EA 2007 2 23 COMA0760201 1 20070220 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYS FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 914CA 10065 7012 FLIGHT 5672 - GEAR DISAGREE MESSAGE RECEIVED ON APPROACH. MESSAGE CLEARED AFTER 30 SECONDS. LANDED WITHOUT INCIDENT. FOUND 3A PUMP TO BE PROVIDING INADEQUATE PRESSURE ON SINGLE PUMP OPERATION. REPLACED PUMP. 2 L 7 2 4F RT A21EA 2007022300019 20070223 00019 WP 2007 2 23 UPS07849225 1 20070220 A 3350 LIGHT DOUG DC8 DC873F 302199F WP COCKPIT FAULTY A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:N/A EMERGENCY LIGHTS WILL NOT DISARM. RELAMPED DISARM INDICATION LIGHT. OPS CHECK OK. 2 L 7 4 4F RT 4A25 2007022300029 20070223 00029 EU 2007 2 23 MAC020702 1 20070214 A 2910 JAM-NUT AEROSP ATR42 ATR42320 8680930 EU HYDRAULIC SYS LOOSE A MTNA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 33 904FX 259 ON DEPARTURE FROM MEM THE GREEN SYSTEM HYD LOW LEVEL LIGHT ILLUMINATED. THE PIC DECLARED AN EMERGENCY AND RETURNED TO M EM. A JAM NUT FOR THE O-RING ON A TEE FITTING COMING OUT OF THE MAIN HYD SYSTEM ACCUMULATOR WAS TIGHTENED AND LEAK CHEC KED WITH NO LEAKS FOUND AND THE A/C RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 2007022300030 20070223 00030 NM 2007 2 23 MWEA070032 1 20070214 A 2560 100502119 COVER DOUG MD88 MD88 3023688 NM EVAC SLIDE OUT OF POSITION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 701ME 49760 THE EMERGENCY SLIDE COVER ON AFT GALLEY DOOR FELL OFF. RE-INSTALLED GALLEY SLIDE COVER. 2 L 7 2 4F RT A6WE 2007022300034 20070223 00034 WP 2007 2 23 MWEA070034 1 20070213 A 5330 NAS1097AD6 DOUBLER DOUG DC9 DC981 3022081 WP FUSELAGE MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 813ME 48007 MISDRILLED HOLE AT STATION 180 JUST BELOW 2ND FASTENER FROM BOTTOM OF DOOR CUTOUT. PLUGGED WITH RIVET. 2 L 7 2 4F A6WE 2007022300035 20070223 00035 NM 2007 2 23 PIDA07009 1 20070212 A 5320 141N86312 PAN BOEING 757 757236 1384971 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 757BJ 22176 FORWARD LAVATORY SERVICE DOOR PAN AND SURROUNDING STRUCTURE CORRODED. REPLACED PAN AND SURROUNDING STRUCTURE PER DRAWIN G 141N8631 AND SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007022300036 20070223 00036 WP 2007 2 23 DHL2007802520 1 20070203 A 5710 VANE DOUG DC8 DC873 302199C WP LT OUTBOARD MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 802DH 86868 46076 LT OTBD VANE SLOT HAS A NON STANDARD REPAIR, STA XOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-31-07, DWG NR AC62-57-107 REV JR DATED 01-23-07. REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51 -1-20D. CUT OUT DAMAGED SECTION IAW DWG NR AC62-57-107. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. NO CRAC K OR CORROSION FOUND AFTER CUT OUT. ENCLOSED SMN FORM 242-2. FABRICATED EXT REPAIR DOUBLER (AL7075T6 0.071") INTERNAL DOUBLER (AL7075T6 0.050") AND FILLER (AL7075T6 0.063") IAW DWG NR AC62-57-107. CLEANED, TREATED AND PRIMED AREA, FILLER , INTERNAL DOUBLER AND INNER FACE OF EXT REPAIR DOUBLER IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51- 2 L 7 4 4F RT 4A25 2007022300037 20070223 00037 WP 2007 2 23 DHL2007802522 1 20070202 A 5210 SKIN DOUG DC8 DC873 302199C WP PAX DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 L1 DOOR CUT OUT WITH 0.600" CRACK APPROX AT STA 25.000 L-15L TO L-16L (FUS SKIN) MAJOR REPAIR. CORR.: PERFORMED MAJOR RE PAIR IAW FAA FORM 8110-3 DATED 01-31-07, DWG# AC62-53-101 REV. IR DATED 01-15-07. REMOVED EXISTING INTERIM REPAIR IAW SR M 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTION IAW DWG# AC62-53-101. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10 -01-001. NO CRACK OR CORROSION FOUND AFTER CUT OUT. ENCLOSED SMN FORM 242-2. FABRICATED REPAIR DOUBLER (AL7075T6 0.071") , 2EA INTERNAL FINGER DOUBLERS (AL7075T6 0.032") AND 2EA FILLERS (AL7075T6 0.050") IA DWG #AC62-53-101. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR 2 L 7 4 4F RT 4A25 2007022300039 20070223 00039 WP 2007 2 23 DHL2007802523 1 20070102 A 2100 HEAT EXCHANGER DOUG DC8 DC873 302199C WP PRIMARY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 RT PRIMARY HEAT EXCHANGER FWD LWR CORNER REPAIR DOUBLER 0.250" CRACKED, STA -32.000 L-27R (MAJOR REPAIR). PERFORMED MAJ OR REPAIR IAW FAA FORM 8110-3 DATED 01-30-07, DWG NR AC62-53-103 REV IR DATED 01-17-07. REMOVED FASTENERS IAW SRM 51-1- 21. CUT OUT DAMAGED SECTION IAW DWG NR AC62-53-103. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. NO CR ACK OR CORROSION FOUND AFTER CUT OUT. ENCLOSED SMN FORM 242-2. FABRICATED REPAIR DOUBLER (AL2024T3 0.050") REPAIR TRIP LER (AL2024T3 0.063") AND FILLER (AL2024T3 0.100") IAW DWG NR AC62-53-103. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW DWG NR AC62-53-1 2 L 7 4 4F RT 4A25 2007022300040 20070223 00040 NM 2007 2 23 SWAA071040 1 20070220 A 5311 6546526 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED BS 400, STR 9R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007022300041 20070223 00041 NM 2007 2 23 SWAA071035 1 20070220 A 5311 6546529 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED BS 440, STR 9L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007022300042 20070223 00042 NM 2007 2 23 SWAA071045 1 20070220 A 5311 6546541 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 1. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007022300043 20070223 00043 WP 2007 2 23 DHL2007802524 1 20070130 A 5755 SKIN DOUG DC8 DC873 302199C WP SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 NR 5 LT SPOILER PANEL DELAMINATED. REMOVED AND REPLACED NR 5 LT SPOILER PANEL IAW MM 27-61-1 PG 201-206. REFER TO NR 0 71624 FOR OPS CHECK. 2 L 7 4 4F RT 4A25 2007022300046 20070223 00046 NM 2007 2 23 SWAA070539 1 20070201 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED C3 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 19 DEF. REMOVED AND REPLACED LIGHT LE NS PER MM. 2 L 7 2 4F RT A16WE 2007022300049 20070223 00049 NM 2007 2 23 SWAA070550 1 20070201 A 5312 6516300 BULKHEAD BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 9 TO RBL 13. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 2007022300050 20070223 00050 WP 2007 2 23 DHL2007802527 1 20070203 A 5710 SPLICE DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 LT WING CTR L/E INTERNAL SPLICE DOUBLER STA XFS 341.500 CRACKED 1" (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-31-07, DWG NR AC62-57-109 REV IR DATED 01-23-07. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED I NTERNAL DOUBLER SEGMENT IAW DWG NR AC62-57-109. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK O R CORROSION FOUND AFTER CUT OUT. ENCLOSED SMN FORM 242-2. FABRICATED NEW INTERNAL DOUBLER SEGMENT (AL7075T6 0.080") (2 EA) INTERNAL STRAPS(AL7075T6 0.063") AND EXTERNAL DOUBLER (AL7075T6 0.071") IAW DWG NR AC62-57-109. CLEANED, TREATED AN D PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR P 2 L 7 4 4F RT 4A25 2007022300051 20070223 00051 NM 2007 2 23 SWAA070543 1 20070201 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 540, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007022300056 20070223 00056 NM 2007 2 23 SWAA070527 1 20070131 A 5311 6545805 FRAME BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007022300057 20070223 00057 EA 2007 2 23 SIMA200705303 1 20070219 A 5315 CC670341757 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 500AE 11503 3977 10025 DYE PENTRANT INSPECTION REVEALED THREE CRACKS ON FORWARD SIDE OF STATION 280 FLOORBEAM. SPLICED IN REPAIR PIECE IAW AME RICAN EAGLE ENGINEERING ORDER CR-53MR-107. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007022300058 20070223 00058 NM 2007 2 23 SWAA070549 1 20070201 A 5315 6545815 FLOORBEAM BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 26 TO LBL 54. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007022300061 20070223 00061 EA 2007 2 23 SIMA200705301 1 20070221 A 2130 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA CABIN PRESSURE UNKNOWN A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 509AE 10078 FOUND FAILED TO PRESSURIZE ON CLIMB-OUT, RETURNED TO ORD. PERFORMED FIM TASK 21-30-00-810-A01, AMM TASKS 45-45-00-970-8 01-A01 AND 21-31-00-910-801-A01 WITH NO DEFECTS. AIRCRAFT PRESSURIZED AND DEPRESSURIZED NORMALLY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007022300064 20070223 00064 NM 2007 2 23 SWAA070538 1 20070201 A 5755 654645262 CASTING BOEING 737 7373H4 1384600 NM NR 4 SPOILER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED C3 CHECK, FOUND LEFT WING NR 4 GROUND SPOILER OUTBOARD HINGE CASTING BROKEN. REMOVED AND REPLACED NR 4 SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007022300065 20070223 00065 NM 2007 2 23 SWAA070521 1 20070131 A 5322 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007022300068 20070223 00068 NM 2007 2 23 SWAA070605 1 20070205 A 2530 41600019 COFFEEMAKER BOEING 737 7377H4 1384404 NM CABIN FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 411WN 29821 AFT COFFEEMAKER HAD BURNING SMELL DURING FLIGHT, OPENED C/B SMELL DISSIPATED. REMOVED AND REPLACED COFFEEMAKER PER MM. 2 L 7 2 4F RT A16WE 2007022300069 20070223 00069 NM 2007 2 23 07FDEA00539 1 20070222 A 5730 SKIN DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 DURING HFEC OPEN, HOLE INSPECTION, QTY: 03 FASTENER HOLES REVEALED CRACK INDICATION FACING FORWARD OF RIGHT WING LOWER SKIN AT ACCESS DOOR AREA (APPROX XORS 696). CARRIED OUT REPAIR AS PER FEDEX E.A. 1-5710-107789, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022300070 20070223 00070 NM 2007 2 23 SWAA070615 1 20070205 A 3397 417A5700 WIRE BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 793SA 27888 DURING SCHEDULED 6Y CHECK, FOUND EEPLS AT FWD CABIN INOP. REPAIRED BROKEN WIRE AT FWD CABIN PER MM. 2 L 7 2 4F RT A16WE 2007022300071 20070223 00071 NM 2007 2 23 SWAA070616 1 20070205 A 3397 417A5700 WIRE BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 793SA 27888 DURING SCHEDULED 6Y CHECK, FOUND EEPLS AT MID CABIN INOP. REPAIRED BROKEN WIRE AT FWD CABIN PER MM. 2 L 7 2 4F RT A16WE 2007022300074 20070223 00074 2007 2 23 SWAA070604 4 20070205 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 226WN 32494 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007022300076 20070223 00076 WP 2007 2 23 N921R54815 1 20070108 A 5753 SKIN DOUG DC8 DC863F 302198F WP TE FLAP DENTED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 921R 46145 LT WING XW 68 INBOARD FLAP TRAILING EDGE LOWER SURFACE WITH DENT ( L=3 1/8, A=2 1/2, Y=.0935). CUTOUT DAMAGED AREA AND FABRICATED FILLER, SPLICE AND SKIN IAW DC8 SRM 57-2-5 AND DC8 SRM 57-7-1. TREATED AND PRIMED REPAIR AREA AND PARTS IAW DC8 SRM 51-1-8. INSTALLED PARTS IAW DC8 SRM 57-2-5. CPCP126L 0552 2 L 7 4 4F 4A25 2007022300077 20070223 00077 NM 2007 2 23 SWAA070599 1 20070204 A 5330 6516352 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505, STR 23R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007022300078 20070223 00078 NM 2007 2 23 SWAA070592 1 20070204 A 5312 6517583 STIFFENER BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD VERTICAL STIFFENER CRACKED AT BS 178, LBL 5.7, WL 184. REPAIRED STIFFENER PE R SRM. 2 L 7 2 4F RT A16WE 2007022300079 20070223 00079 NM 2007 2 23 SWAA070610 1 20070205 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007022300082 20070223 00082 NM 2007 2 23 SWAA070603 1 20070205 A 3350 OL307IBPEGL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 349SW 24408 BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 15 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007022300083 20070223 00083 NM 2007 2 23 SWAA070597 1 20070204 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED 12Y CHECK, FOUND FWD CABIN EEPPLS PHOTOLUMINESCENT STRIP WORN. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007022300085 20070223 00085 NM 2007 2 23 SWAA070606 1 20070205 A 5523 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED 12Y CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB BEARING PER MM. 2 L 7 2 4F RT A16WE 2007022300086 20070223 00086 NM 2007 2 23 SWAA070600 1 20070204 A 5344 65C346701 HINGE FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR UPPER HINGE FITTING CRACKED LOWER SIDE. REMOVED AND REPLACED UPPER HINGE FITT ING PER SWA EA. 2 L 7 2 4F RT A16WE 2007022300088 20070223 00088 NM 2007 2 23 SWAA070611 1 20070205 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 218WN 32489 DURING SCHEDULED MV2 CHECK, FOUND RIGHT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BUL B PER MM. 2 L 7 2 4F RT A16WE 2007022300091 20070223 00091 NM 2007 2 23 SWAA070596 1 20070204 A 3350 MS155721 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 710SW 27844 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007022300093 20070223 00093 NM 2007 2 23 2007UALA00404 1 20070210 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EEL AT AFT GALLEY X AISLE INOPERATIVE. REPLACED EMERGENCY LIGHT. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022300095 20070223 00095 NM 2007 2 23 2007UALA00406 1 20070210 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY LIGHT AT DOOR 4R CEILING INOP. RELAMPED EMERGENCY LIGHT. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022300096 20070223 00096 2007 2 23 AALA20070347 4 20070216 A 2565 SLIDE BOEING 737 737823 13844BZ NM L1 DOOR NO TEST A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 902AN 29504 SKB - LEFT NUMBER ONE DOOR SLIDE UNSUCCESSFULLY DEPLOYED. REPACKED SLIDE AND REINSTALLED SLIDE TO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007022300098 20070223 00098 NM 2007 2 23 2007UALA00407 1 20070210 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY LIGHTS AT UPPER DECK GALLEY, ROW 15 CEILING, AFT OF ROW 8 RT CEILING & AT ROW 24 CEILING ARE INOPERATIVE. REL AMPED EEL LIGHTS IN EACH POSITION. ALL CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022300100 20070223 00100 WP 2007 2 23 AALA20070340 1 20070215 A 2170 COALESCER BAG DOUG DC9 DC983 3022083 WP AIR CONDITIONING DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 592AA 53255 ORD INFLIGHT T1184/15FEB - CREW REPORTED SMOKE IN CABIN AND COCKPIT. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. ACCO MPLISHED BURN OUT OF HIGH PRESSURE PNEUMATIC DUCTING AND CHANGED COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION . 2 L 7 2 4F RT A6WE 2007022300101 20070223 00101 NM 2007 2 23 2007UALA00408 1 20070212 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 LEFT OVERWING EMERGENCY EXIT LIGHT INOP, 2ND FROM FWD END. RELAMPED, OP CHECKED OK 2 L 7 4 4F 4 F RT A20WE E24NE 2007022300103 20070223 00103 NM 2007 2 23 AALA20070333 1 20070214 A 3040 6240664 CONTROLLER BOEING 767 767323 1385205 NM WINDOW HEAT SMOKE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 360AA 24041 MAN INFLIGHT T55/14FEB - AT LEVEL OFF RIGHT FORWARD WINDOW HEAT WIRING STARTED SMOKING. REMOVED POWER AND SMOKE DISSAPA TED. RETURNED TO MAN AND LANDED WITHOUT INCIDENT. REPLACED RIGHT FORWARD WINDSHIELD AND HEAT CONTROLLER POWER CABLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007022100386 20070221 00386 NM 2007 2 21 UIEA200700021 1 20070125 A 7830 537L681G27 RING BOEING 747 7472D7B 1384803 NM THRUST REVERSER DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 NR 3 ENGINE RT T/REV OUTER SUPPORT RING AFT I/B EDGE DAMAGED. REPAIRED ACCOMPLISHED AS PER EO NR 4778A090 AND FAA FORM 8110-3. 2 L 7 4 4F RT A20WE 2007022100388 20070221 00388 NM 2007 2 21 UIEA200700032 1 20070129 A 5311 65B050021414 FRAME BOEING 747 7472D7B 1384803 NM BS 800 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 RT NR 2 MED FWD CUTOUT MIDDLE AREA FOUND CRACKED AT TWO LOCATIONS. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-27247 9981 AND FAA FORM 8110-9. 2 L 7 4 4F RT A20WE 2007022100409 20070221 00409 NM 2007 2 21 SWAA071017 1 20070219 A 5754 65C26601 SKIN BOEING 737 7373H4 1384600 NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND RT WING NR 6 L/E SLAT SKIN LOWER SURFACE CRACKED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007022200004 20070222 00004 EU 2007 2 22 TRAX200700222 1 20070212 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 EMERGENCY FLOOR LIGHTS WILL NOT EXTINGUISH. 2 H 7 2 4T RT 2007022200009 20070222 00009 SO 2007 2 22 C2XA07IA038 1 20070215 A 4930 M4951830 FUEL NOZZLE EMB 145 EMB145XR 3260214 SO APU UNKNOWN A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 11127 15 15 145697 IAH - FLIGHT 2041, THE CREW REPORTED A FUEL SMELL IN THE CABIN ON START. MAINTENANCE PLACED THE APU ON MEL 49-00-00, AN D THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO IAH ON FLIGHT 2891 WHERE MAINTENANCE REMOVE D AND REPLACED THE APU FUEL NOZZLES, OPERATIONALLY CHECKED WITH NO DEFECTS. THE MEL WAS REMOVED, AND THE AIRCRAFT APPRO VED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007022200012 20070222 00012 SO 2007 2 22 C2XA07IA040 1 20070218 A 3350 1317 LIGHT EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14168 14500840 IAH - FLT 2213, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE EMERGENCY EXIT LIGHT ABOVE THE CABIN DOOR TO BE INOP ERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT LIGHT BULB, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND T HE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007022200013 20070222 00013 SO 2007 2 22 C2XA07BT017 1 20070212 A 3350 110049 POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13553 145585 EWR FLT 1206 DURING ROUTINE INSPECTION FOUND LT WING FUSELAGE FRONT FAIRING AND AISLE EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY NR 1 POWER SUPPLY IAW EMB145 AMM 33-50-04. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007022200026 20070222 00026 EA 2007 2 22 COMA0760188 1 20070212 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP STICKING A COMA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 804CA 10953 7352 FLIGHT 9493 - DURING CVG APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WIT HOUT INCIDENT. REPLACED THE LEFT INBOARD FLAP INBOARD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2007022200065 20070222 00065 WP 2007 2 22 UPS07849209 1 20070213 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C3 LT WING CENTER LEADING EDGE UPPER RIB CRACKED AT XFS 366. STOP DRILLED CRACK AT LEFT WING L/E AT STA XFS 366 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR DOUBLER ON LEFT CENTER L/E AT STA XFS 366 IAW SRM 57-0 2-00 AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 2007022200076 20070222 00076 WP 2007 2 22 UPS07849192 1 20070211 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:N/A ON EMERGENCY EXIT LIGHTS TEST, NO LIGHTS WOULD OPERATE. STANDBY INSTRUMENTS OK. REMOVED AND REPLAC ED EMERGENCY LIGHT BATTERY POWER PACK ASSY & SYS. OPS CHECKED NORMAL IAW MM 33-50-01-2. 2 L 7 4 4F RT 4A25 2007022200086 20070222 00086 NM 2007 2 22 SWAA071024 1 20070220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200088 20070222 00088 NM 2007 2 22 SWAA071049 1 20070220 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 447WN 33720 DURING SCHEDULED HC1 CHECK, FWD LT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007022200092 20070222 00092 NM 2007 2 22 SWAA071028 1 20070220 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 3R. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 2007022200093 20070222 00093 NM 2007 2 22 SWAA071030 1 20070220 A 5315 6546809 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 947, LBL 53. REMOVED AND REPLACED UPPER CHORD PER ER. 2 L 7 2 4F RT A16WE 2007022200122 20070222 00122 NM 2007 2 22 SWAA070797 1 20070213 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 474WN 33861 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 15 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007022200128 20070222 00128 NM 2007 2 22 SWAA070789 1 20070213 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 763, STR 23R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007022200130 20070222 00130 NM 2007 2 22 SWAA070796 1 20070213 A 5330 6545776 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 982, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007022200139 20070222 00139 NM 2007 2 22 SWAA070872 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200145 20070222 00145 NM 2007 2 22 SWAA070905 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200153 20070222 00153 NM 2007 2 22 SWAA070800 1 20070213 A 5311 6554892 FRAME BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 723SW 27855 DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 350, STR 6R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007022200154 20070222 00154 NM 2007 2 22 SWAA070752 1 20070213 A 2560 6557463 FITTING BOEING 737 7377H4 1384404 NM R1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 231WN 32499 R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED GIRT BAR FITTING PER MM. 2 L 7 2 4F RT A16WE 2007022200157 20070222 00157 NM 2007 2 22 SWAA070764 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007022200162 20070222 00162 NM 2007 2 22 SWAA070761 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200166 20070222 00166 NM 2007 2 22 SWAA070759 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200173 20070222 00173 NM 2007 2 22 SWAA070767 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200175 20070222 00175 NM 2007 2 22 SWAA070755 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200178 20070222 00178 NM 2007 2 22 SWAA070788 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200188 20070222 00188 NM 2007 2 22 SWAA070898 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200209 20070222 00209 NM 2007 2 22 SWAA070769 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200211 20070222 00211 NM 2007 2 22 SWAA070774 1 20070213 A 3397 D10744 CONNECTOR BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED SPV CHECK, FOUND RIGHT AFT CABIN EMERGENCY EXIT LIGHTS INOP. FOUND LOOSE CONNECTOR, RECONNECTED CONNEC TOR D10744 PER MM. 2 L 7 2 4F RT A16WE 2007022300010 20070223 00010 NM 2007 2 23 CALA0700078 1 20070220 A 5311 6545801512 FRAME BOEING 737 7373T0 1384582 NM BS 227 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND BULKHEAD FORWARD SIDE LOWER FRAME CORRODED AT STA 227, LBL 5. A REPAIR WAS INSTALLED IAW ECRA 5311-012 94. 2 L 7 2 4F RT A16WE 2007022300022 20070223 00022 NM 2007 2 23 UPS07549213 1 20070203 A 5311 146N103078 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 413UP 23853 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1500. FRAME REPAIR AT STA 1500, S26R HAS BEEN ACCOMPLISHED PER E A 757-5362-27-A1603 WITH NO DEVIATIONS AND PER UPS EO B757-5310-26 9176-A. 2 L 7 2 4F RT A2NM 2007022300023 20070223 00023 NM 2007 2 23 UPS07549214 1 20070203 A 5311 146N103074 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 413UP 23853 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1580 S25R TO S26R. FRAME REPAIR AT STA 1580, S25R TO S26R HAS BE EN ACCOMPLISHED PER EA 757-5362-27-A1601, WITH NO DEVIATIONS AND PER UPS EO B757-5310- 26153-A. 2 L 7 2 4F RT A2NM 2007022300025 20070223 00025 NM 2007 2 23 UPS07549218 1 20070207 A 5311 143N102790 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 413UP 23853 INSPECTION TYPE:C DENT IN FORWARD CARGO FUSELAGE FRAME STA 760, S24R. FRAME REPAIR AT STA 760, S24R HAS BEEN ACCOMPLISH ED PER EA 757-5332-27-A1604, WITH NO DEVIATIONS AND PER UPS EO B757-5310-26181-A. 2 L 7 2 4F RT A2NM 2007022300032 20070223 00032 2007 2 23 MWEA070035 4 20070216 A 3421 142830001 GYRO DOUG DC9 DC982 3022082 WP COCKPIT FAILED A MWEA A UNSCHED LANDING I FLT. ATTITUDE INST. TO TAKEOFF 1 GL 13 808ME 48070 CAPTAIN'S ATTITUDE INDICATOR FAILED. REMOVED AND REPLACED CAPTAINS FOG GYRO. 2 L 7 2 4F A6WE 2007022300038 20070223 00038 NM 2007 2 23 PIDA07008 1 20070208 A 5230 146N6616 DOOR FRAME BOEING 757 757236 1384971 NM CARGO DOOR DENTED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 757BJ 22176 NUMBER 2 (AFT CARGO) DOOR HAS A DENT ON THE LOWER DOOR FRAME. REPLACED LOWER BEAM PER SRM 51-40-02 AND 51-10-02. 2 L 7 2 4F RT A2NM 2007022300045 20070223 00045 NM 2007 2 23 SWAA070540 1 20070201 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED C3 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007022300054 20070223 00054 WP 2007 2 23 DHL2007802529 1 20070203 A 5414 SKIN DOUG DC8 DC873 302199C WP GE CFM56 CFM56* 13802 NE NR 3 NACELLE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 RT NR 3 ENGINE NACELLE INLET COWL SHOWS CRACK 0.500" ON SKIN STA YN 138.000 AT 3 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-30-07, DWG NR AC62-54-105 REV IR DATED 01-19-07. REMOVED FASTENERS IAW SRM 51 -1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW DWG NR AC62-54-105. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-1 0-01-001. NO CRACK OR CORROSION FOUND AFTER CUT OUT. ENCLOSED SMN FORM 242-2. FABRICATED REPAIR DOUBLER 9AL2024T3 0.08 0") AND FILLER (AL2024T3 0.071") IAW DWG NR AC62-54-105. HEAT TREATED DOUBLER AND FILLER FROM 2024T3 TO 2024T4 IAW SR 5 1-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER (INNER FACE) AND FILLER IAW SRM 51-1-8B. APPLIED 2 L 7 4 4F 4 F RT 4A25 E2GL 2007022300099 20070223 00099 NM 2007 2 23 AALA20070339 1 20070215 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 384AA 26996 DFW - FOUND EMERGENCY LIGHT AT SEAT 33B INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 33B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007022300105 20070223 00105 NM 2007 2 23 AALA20070328 1 20070212 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 976AN 30099 MIA - FOUND EMERGENCY LIGHT AT SEAT 8A MISSING LENS BEZEL. REPLACED LENS BEZEL FOR EMERGENCY LIGHT AT SEAT 8A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007022300107 20070223 00107 WP 2007 2 23 AALA20070342 1 20070214 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 418AA 49329 SFO - EMERGENCY LIGHT AT LOWER FORWARD CORNER OF RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LOWER FORWARD CORNER OF RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007022300108 20070223 00108 NM 2007 2 23 AALA20070319 1 20070210 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - FOUND EMERGENCY LIGHTS AT SEAT 26C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT T00001SE 2007022300110 20070223 00110 NM 2007 2 23 AALA20070320 1 20070210 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 DFW - FOUND EMERGENCY LIGHTS AT SEAT 25C INOPERATIVE. REPLACE EMERGENCY LIGHT ASSEMBLY AT SEAT 25C. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007022300112 20070223 00112 NM 2007 2 23 AWXA200700219 1 20070202 A 5315 654583469 STRAP BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND FLOORBEAM SUPPORT STRAP CRACKED, BS 312, RBL 34L, WL 200. REPAIRED FLOORBEAM SUPPORT STRAP CRACKED, BS 312, RBL 34L, WL 200 IAW B737-300 SRM 53-10-51. 2 L 7 2 4F RT A16WE 2007022300117 20070223 00117 NM 2007 2 23 AWXA200700224 1 20070126 A 2560 ACREM1A MEGAPHONE BOEING 737 7373S3 1384711 NM ZONE 200 INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MEGAPHONE WILL NOT FUNCTION IN SPEECH OR EMERGENCY SIGNAL. REPLACED MEGAPHONE. 2 L 7 2 4F RT A16WE 2007022300118 20070223 00118 NM 2007 2 23 2007UALA00410 1 20070211 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY EXIT LIGHT INOP AT DOOR 4 LEFT BUSTLE & AT SEAT 4F FWD ASSY. REPLACED LIGHT ASSY IN BOTH POSITIONS. BOTH OP C HECKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022300119 20070223 00119 NM 2007 2 23 AWXA200700225 1 20070127 A 5330 655298873 SKIN BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND FUSELAGE SKIN CRACKED, BS 967, S17R. REPAIRED FUSELAGE SKIN, BS 967, S17R IAW B737-300 SRM 53-60-01-2R3. 2 L 7 2 4F RT A16WE 2007022300120 20070223 00120 NM 2007 2 23 AWXA200700226 1 20070131 A 5713 654576727 STRINGER BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND STRINGER 16L IS CRACKED, BS 500D, S16L. REPLACED STRINGER, BS 500D, S16L IAW AWA ER 03-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2007022300124 20070223 00124 WP 2007 2 23 AALA20070312 1 20070210 A 3230 PISTON DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 3515 49892 ORD INFLIGHT T1462/10FEB - ON RETRACTION, NOSE GEAR UNSAFE LIGHT ILLUMINATED. RETURNED TO ORD AND LANDED WITHOUT INCIDE NT. REPACKED NOSE GEAR LOWER PISTON. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007022300128 20070223 00128 NM 2007 2 23 2007UALA00413 1 20070212 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 EMERGENCY CEILING LIGHT ROW 17 INOPERATIVE. RELAMPED. OP CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022300129 20070223 00129 NM 2007 2 23 AALA20070334 1 20070215 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 690AA 25696 DFW - FOUND EMERGENCY LIGHT AT R4 DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007022300130 20070223 00130 NM 2007 2 23 AALA20070314 1 20070210 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 765AN 32879 MIA - FOUND EMERGENCY LIGHTS AT LEFT SIDE FORWARD GALLEY COAT CLOSET INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY L IGHTS AT LEFT SIDE FORWARD GALLEY COAT CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007022300134 20070223 00134 NM 2007 2 23 AALA20070301 1 20070208 A 3350 LENS BOEING 757 757231 1384950 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 705TE 28479 DFW - FOUND EMERGENCY LIGHT IN CABIN HAS BROKEN LENS COVER. REPLACED LENS FOR EMERGENCY LIGHT IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007022300137 20070223 00137 NM 2007 2 23 AALA20070337 1 20070215 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 782AN 30003 DFW - FOUND EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR CEILING INOPERATIVE. RELAMPED EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007022300138 20070223 00138 NM 2007 2 23 AALA20070303 1 20070208 A 2910 LINE BOEING 757 757223 1384957 NM HYD SYSTEM LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 660AM 25294 CUN INFLIGHT T1688 - LEFT HYDRAULIC QUANTITY MESSAGE APPEARED FOLLOWED BY LEFT HYDRAULIC PRESSURE MESSAGE INDICATIONS. VERIFIED LOSS OF LEFT HYDRAULIC FLUID AND PRESSURE. USED ALTERNATE GEAR AND FLAP EXTENSION. RETURNED TO CUN AND LANDED WITHOUT INCIDENT. FOUND ONE HYDRAULIC LINE AT RIGHT WHEEL WELL LEAKING. REPLACED HYDRAULIC LINE AND HYDRAULIC PRESSUR E FILTER. SERVICED LEFT HYDRAULIC SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007022300139 20070223 00139 EU 2007 2 23 2007UALA00469 1 20070215 A 5322 SHEAR TIE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 430UA 568 FWD CARGO PIT CORROSION AT FRAME 32 SHEAR TIES BETWEEN STR 43 & 44 LT, 41 & 42 LT, 40 & 41 LT, 42 & 43 RT, 41 & 42 RT, 4 0 & 41 RT AND 39 & 40 RT. REPAIR ACCOMPLISHED: REPLACED SHEAR TIES. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022300140 20070223 00140 WP 2007 2 23 AALA20070305 1 20070209 A 3220 PISTON DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 482AA 49675 ORD INFLIGHT T1718 - COULD NOT RETRACT THE LANDING GEAR AFTER TAKEOFF. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. RE PLACED NOSE GEAR STRUT LOWER PISTON AND SERVICED STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007022300142 20070223 00142 EU 2007 2 23 AALA20070307 1 20070209 A 3260 SWITCH AIRBUS 300 A300B4605R 3930308 EU NLG FAULTY A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7062A 474 MIA INFLIGHT T783 - DURING GEAR RETRACTION ALL THREE GEAR UNSAFE LIGHTS ILLUMINATED AND GREEN HYDRAULIC SYSTEM QUANTITY FLUCTUATED RAPIDLY. PRESSURE ALSO FLUCTUATED. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. FOUND 406B SWITCH ON NOSE GEAR TELESCOPIC DRAG STRUT FAULTY. REPLACED 406B MICROSWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007022300144 20070223 00144 WP 2007 2 23 AALA20070308 1 20070209 A 5270 TARGET DOUG DC9 DC982 3022082 WP MLG DOOR BROKEN A AALA O OTHER N FALSE WARNING LD LANDING 1 SW 21 429AA 49341 ORD INFLIGHT T363 - GEAR DOOR OPEN LIGHT ILLUMINATED WITH GEAR UP. NO OTHER GEAR LIGHTS ON. USED ALTERNATE GEAR EXTENS ION. LANDED ORD WITHOUT INCIDENT. FOUND RIGHT GER DOOR TARGET AND BRACKET BROKEN. REPLACED GEAR DOOR TARGET AND BRACK ET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007022300145 20070223 00145 NM 2007 2 23 2007UALA00472 1 20070215 A 5330 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 906UA 25006 FUSELAGE SKIN IS SCRATCHED AND DENTED APPROX 29 INCHES BELOW AFT END OF DOOR 1R OPENING. MAJOR REPAIR ACCOMPLISHED. IN STALLED DOUBLER REPAIR AND ACCMP CORROSION TREATMENT TO SHEETMETAL REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022300146 20070223 00146 2007 2 23 AALA20070311 4 20070210 A 2565 100505201 SLIDE DOUG DC9 DC982 3022082 WP SERVICE DOOR INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 559AA 53089 LAS - RAMP SERVICE FOUND SLIDE PACK AT LEFT SERVICE DOOR BROKEN AND ON GROUND. CATERING DROPPED SLIDE WHEN SERVICING AI RCRAFT. SLIDE DID NOT DEPLOY. REPLACED SLIDE FOR LEFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007022300147 20070223 00147 NM 2007 2 23 AALA20070306 1 20070209 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 349AN 33088 DFW - FOUND EMERGENCY SEAT MOUNTED LIGHT AT SEAT ROWS 24HJ TO 31HJ INOPERATIVE. FOUND CONNECTORS UNPLUGGED AT SEAT ROW 31HJ. RECONNECTED CONNECTORS FOR EMERGENCY LIGHTS AT SEAT ROWS 24HJ TO 31HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007022300148 20070223 00148 NM 2007 2 23 AALA20070321 1 20070210 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 783AN 30004 DFW - FOUND EMERGENCY LIGHTS AT SEAT 25C HAS LENS COVER MISSING. REPLACED LENS COVER FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007022300150 20070223 00150 WP 2007 2 23 AALA20070310 1 20070209 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 576AA 53153 LGA - FOUND EMERGENCY LIGHT AT SEAT 5E HAS BULBS MISSING. REPLACED BULBS FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007022300151 20070223 00151 NM 2007 2 23 2007UALA00473 1 20070215 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 STA 500D+18, STR 12R SKIN IS CRACKED AT LOWER EDGE OF BONDED DOUBLER. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SKIN RE PAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022300152 20070223 00152 NM 2007 2 23 AALA20070304 1 20070208 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 643AA 24601 DFW - FOUND EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR SLIDE INOPERATIVE. RELAMPED EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007022300154 20070223 00154 WP 2007 2 23 AALA20070300 1 20070208 A 4900 5940405503 APU DOUG DC9 DC982 3022082 WP SMOKE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 7535A 49989 ORD INFLIGHT T2455 - FOUND SMOKE AND FUMES IN CABIN AFTER TAKEOFF. REPLACED APU AND PERFORMED PACK BURN OUT. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007022300156 20070223 00156 NM 2007 2 23 2007UALA00475 1 20070215 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 LOWER AFT SIDE OF AFT CARGO DOOR CUTOUT IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER, TRIPLER AND FILLER R EPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022300157 20070223 00157 NM 2007 2 23 AALA20070292 1 20070205 A 4990 351N110126 APU BOEING 757 757223 1384957 NM LEAKING A AALA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 SW 21 642AA 24600 ORD INFLIGHT T313 - FLIGHT ATTENDANTS REPORTED ELECTRICAL SMELL MIXED WITH SMELL OF BURNED PLASTIC. DECK NEAR AFT FLIGH T ATTENDANT JUMPSEAT SLIGHTLY WARM. BOTH AFT LAVATORY SMOKE ALARMS SOUNDED. AIRCRAFT RETURNED TO ORD AND LANDED WITHOU T INCIDENT. REPLACED AUXILLIARY POWER UNIT DUE TO LOW OIL QUANTITY INDICATIONS AND OIL LEAK AND RAN AIR CONDITIONING PA CK BURN OUT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007022300158 20070223 00158 EU 2007 2 23 AALA20070297 1 20070206 A 2560 STRAP AIRBUS 300 A300B4605R 3930308 EU FLASHLIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 90070 513 MIA - FOUND EMERGENCY FLASHLIGHT AT LEFT NUMBER ONE DOOR MISSING STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007022300161 20070223 00161 NM 2007 2 23 AALA20070302 1 20070208 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 771AN 29579 EZE - FOUND EMERGENCY AISLE SEAT LIGHTS FROM DOOR 3 TO DOOR 4 INOPERATIVE. FOUND LAMPS BROKEN MAKING ELECTRICAL SHORT AT SEAT 31G. REPLACED LAMPS AT SEAT 31G AND REPLACED FUSES ON BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007022300163 20070223 00163 WP 2007 2 23 AALA20070299 1 20070208 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9401W 53137 LGA - EMERGENCY LIGHT IN FIRST CLASS FORWARD GALLEY CEILING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN F IRST CLASS FORWARD GALLEY CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007022300170 20070223 00170 NM 2007 2 23 F3LA200700035 1 20070218 A 2910 AE7074192 HOSE AIRBUS A319 A319111 3930336 NM HYD SYSTEM DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 929FR 4725 2240 DURING C-2 CHECK, INSPECTION REPORTED LT ENG HYDRAULIC PRESSURE HOSE ASSY HAD A DEEP RUB MARK FROM CLAMP AT CENTER ATTAC HMENT BRACKET (APPROX. 7:00 O'CLOCK POSITION). REPLACED HYDRAULIC PRESSURE HOSE/TUBE ASSY IAW MM 29-11-49-400-002. 2 L 7 2 4F RT A28NM 2007022300171 20070223 00171 NM 2007 2 23 AWXA200700227 1 20070122 A 5540 6549837502 SUPPORT FITTING BOEING 737 73733A 1384673 NM ZONE 300 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED RUDDER SUPPORT FITTING, RS 23.27. REPAIRED RUDDER SUPPORT FITTING, RS 23.27 IAW AWA ER 03-5530-0704 7-ES1. 2 L 7 2 4F RT A16WE 2007022300173 20070223 00173 NM 2007 2 23 NOCA03807 1 20070210 A 5315 FLOORBEAM BOEING 757 75728A 1384976 NM BS 362 CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 752NA 28174 FOUND CORROSION ON HAT CHANNEL ON TOP OF FLOORBEAM STA365 RBL12-RBL50. REMOVED AND REPLACED BOTH HAT CHANNELS ON TOP FL OOR BOARD SUPPORT AT STA 365 RBL12-RBL 50 PER SRM 51-10-02. 2 L 7 2 4F RT A2NM 2007022300174 20070223 00174 NM 2007 2 23 NOCA04207 1 20070210 A 4910 FLANGE BOEING 757 75728A 1384976 NM INLET DUCT CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 752NA 28174 APU INLET DUCT MATING FLANGE HAS HEAVY CORROSION. REPLACED FLANGE AS PER MM 49-15-01. 2 L 7 2 4F RT A2NM 2007022300175 20070223 00175 NM 2007 2 23 NOCA04007 1 20070210 A 5315 FLOORBEAM BOEING 757 75728A 1384976 NM BS 356 CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 752NA 28174 FOUND FLOORBEAM CORRODED STA 365 RBL58. REPAIRED PER NAA EO NR 757-53-048. 2 L 7 2 4F RT A2NM 2007022300176 20070223 00176 NM 2007 2 23 NOCA03907 1 20070210 A 5320 BRACKET BOEING 757 75728A 1384976 NM FUSELAGE CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 752NA 28174 THE L ANGLE BRACKET NEXT TO THE R4 DOOR DRAIN IS CORRODED ON THE BOTTOM. REPLACED L ANGLE PER SRM 51-21-03. 2 L 7 2 4F RT A2NM 2007022300177 20070223 00177 NM 2007 2 23 NOCA04307 1 20070214 A 3350 3071PBE LIGHT BOEING 757 75728A 1384976 NM SEAT 28 BC INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 754NA 29381 FOUND ONE E-PATH LIGHT INOP AT SEAT 28BC. REPLACED LIGHT AS PER MM 33-51-05. 2 L 7 2 4F RT A2NM 2007022300178 20070223 00178 EU 2007 2 23 AWXA200700228 1 20070214 A 5321 D5361060500100 FLOORBOARD AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 652AW 953 SAL - FOUND CORROSION ON MAIN CABIN FLOORBOARD 222 FF, FR 16 - FR 20, -Y1292 TO -Y1732. REPLACED MAIN CABIN FLOORBOARD 222 FF, FR 16 - FR 20, -Y1292 TO -Y1732 IAW AWA TASK CARD C1C53303. 2 L 7 2 4F RT A28NM 2007022300180 20070223 00180 NM 2007 2 23 2007UALA00478 1 20070215 A 5313 STRINGER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 FWD CABIN STA 294.5 STR 10L HAS A CRACK ON THE UPPER FLANGE, ALSO UPPER HINGE BOX WEB ANGLE CRACKED AT BS 294 ABOVE STR 10L. FWD CABIN STA 294.5 STR 16L INTERCOSTAL HAS LARGE CRACK ON FWD WEB. MAJOR REPAIR: REMOVED DAMAGE. ACCOMPLISHED REPAIR PER AAR EA I070085, EA I07010 AND I070092 REV IR AND UA-EVA-70072A. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022300182 20070223 00182 NM 2007 2 23 2007UALA00479 1 20070215 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 FWD CARGO DOORWAY AFT FRAME IS CRACKED IN UPPER RADIUS ABOVE 5TH STOP PAD FROM TOP I/B UPPER ATTACH BOLT. MAJOR REPAIR. REMOVED DAMAGE, ACCOMPLISHED REPAIR PER AAR EAI070071 REV IR AND UA-EVA-70082. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022300183 20070223 00183 NM 2007 2 23 AWXA200700231 1 20070119 A 5751 SKIN BOEING 737 73733A 1384673 NM AILERON DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW HDH303 23625 MCN - LEFT WING AILERON LEADING EDGE PANEL 8106L CUT OUT DELAMINATED, WS 484. REPAIRED LEFT WING AILERON LEADING EDGE P ANEL 8106L CUT OUT, WS 484 IAW AWA ER 03-5761-07047-ES4. 2 L 7 2 4F RT A16WE 2007022300184 20070223 00184 NM 2007 2 23 2007UALA00480 1 20070215 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 BS 1120 LEFT SIDE, INBOARD OF CREASE BEAM, WEB IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND MACHINED 1 EA FIT TING AND REINSTALLED WEB FITTING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022300186 20070223 00186 NM 2007 2 23 2007UALA00481 1 20070215 A 4920 APU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU BAY MALFUNCTIONED A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 505UA 24626 APU WENT TO 52 PERCENT N1 AND GOT AN APU FAULT DESCENDING THROUGH 25,000 FT. FOUND APU GENERATOR HOUSING CRACKED 4-6 " LONG CAUSING OIL LOSS AND SUBSEQUENT APU SHUTDOWN FOR LOW OIL QUANITY. REPLACED APU GENERATOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022300187 20070223 00187 NM 2007 2 23 AWXA200700233 1 20070202 A 5320 65298171 REVEAL BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND FORWARD AIRSTAIR CUT OUT FORWARD CORNER REVEAL CRACKED. REPLACED FORWARD AIRSTAIR CUT OUT FORWARD CORNER RE VEAL IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007022300189 20070223 00189 NM 2007 2 23 AWXA200700234 1 20070203 A 5320 69564081 INTERCOSTAL BOEING 737 7373S3 1384711 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED INTERCOSTAL, BS 351.5, S29L. REPLACED INTERCOSTAL, BS 351.5, S29L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007022300190 20070223 00190 NM 2007 2 23 AWXA200700235 1 20070131 A 5210 6545855101 STRUCTURE BOEING 737 7373S3 1384711 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CORROSION ON R2 DOOR CUT OUT LOWER THRESHOLD INNER CHORD, BS 958 - BS 987, RBL 60, WL 208. REPLACED R2 DOOR CUT OUT LOWER THRESHOLD INNER CHORD, BS 958 - BS 987, RBL 60, WL 208 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007022300191 20070223 00191 NM 2007 2 23 NWAA070595523 1 20070207 A 5414 SKIN BOEING 757 757251 1384970 NM NR 2 NACELLE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 523US 23617 DURING SCHEDULED ENGINE CHANGE INSPECTION REVEALED CRACK IN NR 2 PYLON RIGHT SIDE SKIN. REPAIRED PER EA 55-208923 SECTI ON I, SECTION II REPAIR TO BE ACCOMPLISHED WITHIN 24 MONTHS. 2 L 7 2 4F RT A2NM 2007022300192 20070223 00192 2007 2 23 2007UALA00483 4 20070214 A 2565 BOTTLE AIRCRUISERS AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EVAC SLIDE LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 840UA A9377 1522 LOW BOTTLE PRESSURE. LEAKING AROUND THREADS ON GAUGE, TEFLON TAPE PULLED AWAY FROM THREADS ON GAUGE. RESEALED W/TEFLON TAPE AROUND GAUGE THREADS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022300194 20070223 00194 EA 2007 2 23 SWIA200717821 1 20070217 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 447SW 7677 AFT CEILING LEVEL EMERGENCY FLOODLIGHT INOP. RELAMPED EMERGENCY LIGHTS IAW MM 33-51-1A. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007022300195 20070223 00195 EA 2007 2 23 SWIA200717822 1 20070217 A 5610 601R330331 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 410SW 7066 CAPTAIN'S WINDSHIELD CRACKED CLIMBING THROUGH FL 260. CAPTAIN’S WINDSHIELD INSTALLED IAW RII 56-220-1000 AND AMM 56-11- 01. OPERATIONAL AND LEAK CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007022300197 20070223 00197 EU 2007 2 23 07FDEA00440 1 20070209 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 MDC - FOUND SEAT TRACK 2R AT FS 61 HAS CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. CHECKED LIMITS PER A310 SRM 53-10-16, AREA IS OUT OF LIMITS. REMOVED SEAT TRACK SECTION PER A310 SRM 53-10-16. FABRICATED NEW SEAT TRACK SECTION AND REPAIR PARTS PER A310 SRM 53-10-16. INSTALLED REPAIR PER A310 SRM 53-10-16. REPROTECTED AREA PER A310 SRM 51-75-10 , MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2 L 7 2 4F RT A35EU 2007022300198 20070223 00198 EU 2007 2 23 07FDEA00441 1 20070209 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 MDC SEAT TRACK 1 AT FR73 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW AIRBUS DWG NR 18A532-79237. REPLACED 1 STR AP P/N A5378103620095, MAJOR REPAIR IAW FEDEX GMM 6-2-100. SEE JPF N00791. 2 L 7 2 4F RT A35EU 2007022300202 20070223 00202 EU 2007 2 23 07FDEA00445 1 20070209 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 MDC SEAT TRACK NR 3R AT FR 78 HAS EXFOLIATION CORROSION. REPAIRED SEAT TRACK IAW A310 SRM 53-10-16. MAJOR REPAIR IAW F EDEX GMM 6-2-100. SEE JPF N00818. 2 L 7 2 4F RT A35EU 2007022300203 20070223 00203 EU 2007 2 23 2007UALA00486 2 20070215 A 7200 ENGINE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU NR 2 FOD A UALA A UNSCHED LANDING C B F.O.D. SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 933UA 26659 FLIGHT DIVERTED UNDER AMBER ALERT DUE TO BURNING ODOR IN CABIN. ENGINE NR 2 INGESTED PLASTIC BAG. REMOVED PLASTIC BAG REMNANTS. ACCOMPLISHED BOROSCOPE. NO DISCREPANCIES FOUND. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022300205 20070223 00205 NM 2007 2 23 2007UALA00487 1 20070213 A 5230 HINGE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE AFT CARGO DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 178UA 24385 AFT CARGO DOOR UPPER PIANO HINGE HAS PEELING PAINT AND SURFACE CORROSION (RUST) ON SEVERAL OF THE HINGE SEGMENTS. CLEANE D UP SURFACE CORROSION (RUST) ON AFT CARGO DOOR UPPER PIANO HINGE. APPLIED CIC. A/C RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022300206 20070223 00206 SO 2007 2 23 SIMA200704701 1 20070214 A 3350 82321 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 630AE 17337 145132 FOUND MID-CEILING FOWARD EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EXIT SIGN IAW EMB AMM 33-50-15. OPERATIONAL CHECK ED GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007022300208 20070223 00208 NM 2007 2 23 2007UALA00148 1 20070119 A 2822 6075504 PUMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUEL SYSTEM WEAK A UALA O OTHER O OTHER CR CRUISE 1 WP 29 546UA 25367 FUEL IMBALANCE 1600 LBS, 4 HOUR FLT. PROGRESS PG SHOWS RT SIDE BURNED 200 LBS MORE THAN LEFT. AT ARRIVAL NOTED DRIPSTI CK READINGS AND QTY SHOWS LEFT WING = 20.8 INCH AT 4420 LBS. RIGHT WING =16.0 INCH AT 2509 LBS. FUEL QTY ACCURATE. FU EL CONFIG LEFT ILLUMINATED AT TOUCHDOWN. FUEL IMBALANCE 1300 LBS AFTER 6 HRS FLT. PRESSURIZED SYSTEM AND FOUND NO INTE RNAL LEAKS. SUSPECT BOOST PUMP NOT GENERATING ENOUGH PRESSURE. OPENED UP TANK TO REPLACE BOOST PUMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022300210 20070223 00210 NM 2007 2 23 2007UALA00379 1 20070209 A 5230 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 FWD CARGO DOOR S/N 1655 FRAME CRACKED ON INSIDE OF DOOR BY LOWER AFT STOP. MAJOR REPAIR. REMOVED AND REPLACED CRACKED FRAME PER SRM 51-40-92. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022300212 20070223 00212 NM 2007 2 23 2007UALA00381 1 20070210 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 FWD CABIN AREA SHEAR TIE IS CRACKED AT BS 360 BELOW STR 13L. MAJOR REPAIR. REMOVED AND REPLACED SHEAR TIE PER SRM 51-4 0-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022300213 20070223 00213 NM 2007 2 23 2007UALA00382 1 20070209 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 MAIN CABIN FLOORBEAM UPPER TEE CAP CORRODED STA 324.0 AND RBL 50 WL 208. MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM TEE CAP FROM LBL 50 TO LBL 55. INSTALLED TEE CAP SPLICE AND STRAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022300216 20070223 00216 EU 2007 2 23 2007UALA00385 1 20070209 A 3350 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 418UA 485 EPSU BATTERY FWD L FAULT ON CABIN EMERGENCY LIGHT TEST. REPLACED FWD LT EPSU BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022300218 20070223 00218 NM 2007 2 23 2007UALA00387 1 20070210 A 5240 STOP FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT SERVICE DOOR OUT OF ADJUST A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 378UA 24653 AFT SERVICE DOOR LIGHT ILLUMINATED ON TAKEOFF ROLL. CREW ABORTED AT 110 KIAS AND MAX BRAKING WAS APPLIED. PROBABLY CAU SE WAS DOOR STOPS OUT OF POSITION. ADJUSTED DOOR STOPS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022300219 20070223 00219 NM 2007 2 23 HALA0700046 1 20070204 A 3222 PIN BOEING 767 76733AER 1385230 NM NLG GROUND DAMAGE A HALA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 WP 13 591HA 33423 ON PUSHBACK TO RELOCATE A/C, HEARD 2 LOUD BANGS FROM NOSE GEAR. FOUND TOW BAR EXTENDED BEYOND LIMITS AND SHEAR PIN BROK EN AND DAMAGE TO LOWER GEAR. REPLACED NOSE GEAR TOW FITTING PER AMM 32-21-12/401. INSPECTED NOSE WHEEL SYSTEM PER AMM 32-51-00-735-072. NO OTHER DISCREPANCIES FOUND WITH GREASE PLATES USED. ALSO, PERFORMED NOSE LANDING GEAR EXCEEDENCE P ER 05-51-29/201. NO DISCREPANCIES. 2 L 7 2 4F RT A1NM 2007022300225 20070223 00225 NM 2007 2 23 2007UALA00392 1 20070211 A 2560 SWITCH BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE R4 DOOR FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 229UA 30557 WHILE PERFORMING EVAC TEST AT DOOR 4R WITH EVAC TEST SWITCH, THE EVAC LIGHT AND HORN FAILED TO RETURN TO NORMAL MODE. REPLACE EMERGENCY EVAC ALARM SWITCH, RETEST PER MM 25-63-02, P201. TEST OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007022300227 20070223 00227 NM 2007 2 23 QXEA200700212 1 20070220 A 5210 HANDLE BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR UNSECURE A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 419QX 4145 SEA FLIGHT NR 2379: FUSELAGE DOOR CAUTION LIGHT ILLUMINATED DURING CLIMB. REAR PAX DOOR WAS SHOWING OPEN/UNSECURE. AIR CRAFT RETURNED TO SEA. MAINTENANCE INSPECTED AND FOUND AFT PAX DOOR HANDLE NOT FULLY IN THE LOCKED POSITION. COMPLIED WITH OPERATIONAL TEST OF AFT PAX DOOR PER AMM 52-12-00-710-802. OPS TEST GOOD. PRESSURIZED AIRCRAFT. NO CAUTIONS. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007022300228 20070223 00228 NM 2007 2 23 2007UALA00394 1 20070209 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 WING LEFT SLIDE GROUND L646 AND AFT DOOR LEFT SIDE DOOR GROUND (L397) EXTERIOR EMERGENCY LIGHTS INOP. RELAMPED L397 AFT LT DOOR SLIDE LIGHT PER MM 33-51-06. OPS CHECKS NORMALLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022300232 20070223 00232 NM 2007 2 23 07FDEA00497 1 20070215 A 5730 SKIN DOUG MD11 MD11 3023602 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT WING ANTI-ICING TELESCOPING DUCT DOOR CUTOUT FOUND CRACKED. LT WING ANTI-ICING TELESCOPIC DUCT CUTOUT CRACK REPAIR ED AS PER SRM 57-10-00 FIG. 42 VOL.I. (TR) REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022300233 20070223 00233 NM 2007 2 23 2007UALA00396 1 20070209 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 LEFT C-ZONE EEL INOPERATIVE. REPLACED BATTERY PACK AT SEAT 18 A-B. OPS CHECKS NORMALLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022300234 20070223 00234 NM 2007 2 23 07FDEA00498 1 20070215 A 5713 STRINGER DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 DURING HFEC INSPECTION, CRACK FOUND AT STRINGER 12 (XORS 642) IN RIGHT TANK. CARRIED OUT REPAIR AT RT WING STRINGER NR 12 (XORS 642) AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022300235 20070223 00235 NM 2007 2 23 2007UALA00397 1 20070209 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 87UA 26713 EMERGENCY EEL LIGHT AT ROW 21 ABC WILL NOT COME ON. RELAMPED, OP CKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022300236 20070223 00236 NM 2007 2 23 07FDEA00499 1 20070215 A 5713 STRINGER DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 DURING HFEC INSPECTION, CRACK FOUND AT STRINGER 13 (XORS 577) IN RIGHT TANK. CARRIED OUT REPAIR AT RT WING STRINGER NR 13 (XORS 577) AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022300239 20070223 00239 NM 2007 2 23 07FDEA00502 1 20070216 A 5713 STRINGER DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 DURING HFEC INSPECTION, CRACK FOUND AT STRINGER 13 (XORS 577) IN LEFT TANK. CARRIED OUT REPAIR AT LT WING STRINGER 13 A S PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022300240 20070223 00240 NM 2007 2 23 07FDEA00503 1 20070216 A 5713 STRINGER DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 DURING HFEC INSPECTION, CRACK FOUND AT STRINGER 12 (XORS 642) IN LEFT TANK. REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022300243 20070223 00243 NM 2007 2 23 07FDEA00506 1 20070216 A 5713 STRINGER DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 DURING HFEC INSPECTION, CRACK FOUND AT STRINGER 09 (XORS 819) IN LEFT TANK. REPAIR CARRIED OUT PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022300247 20070223 00247 NM 2007 2 23 2007UALA00400 1 20070210 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW REST INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY LIGHT AT AFT CREW REST OVERSTAIR INOPERATIVE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022300248 20070223 00248 NM 2007 2 23 DLM88070131 1 20070215 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 256 GROUND DAMAGE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 937DL 49810 DURING THE VISIT, THE EXISTING REPAIR INSTALLED PER 265774-14 WAS REMOVED DUE TO ADDITIONAL DAMAGE AND A LARGER REPAIR I NSTALLED PER MD88 SRM 53-04 FIGURE 12C. 2 L 7 2 4F RT A6WE 2007022300249 20070223 00249 NM 2007 2 23 DLM8K070132 1 20070215 A 5512 5922578515 SKIN DOUG MD88 MD88 3023688 NM HORIZONTAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DE 53418 DURING LETTER CHECK, THE RHS HORIZONTAL STABILIZER UPPER AFT SKIN PANEL WAS FOUND CRACKED AT THE INBOARD AFT END. THE P ART WAS REPLACED PER BOEING RECOMMENDATION AS NO FEASIBLE REPAIR CURRENTLY EXISTS. DOCUMENTED ON ER/A 460015-14. 2 L 7 2 4F RT A6WE 2007022300250 20070223 00250 NM 2007 2 23 2007UALA00401 1 20070210 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EEL AT 57 HJK INOPERATIVE. RESECURED EEL CONNECTOR. OPS CHECK NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022300251 20070223 00251 NM 2007 2 23 DLM88070133 1 20070215 A 5512 5922578515 SKIN DOUG MD88 MD88 3023688 NM HORIZONTAL STABS CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 DURING LETTER CHECK, THE HORIZONTAL STABILZIER UPPER AFT SKIN PANEL WAS FOUND WITH A FOUR INCH CRACK AT THE INBOARD AFT EDGE (RHS). THE UPPER SKIN PANEL WAS REPLACED, REF 460111-14. 2 L 7 2 4F RT A6WE 2007022300252 20070223 00252 NM 2007 2 23 2007UALA00402 1 20070210 A 3350 CHARGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY EXIT SIGN AT DOOR 4R UNDER MONITOR & ON GALLEY WALL INOPERATIVE. REPLACED BATTERY CHARGER. OPS CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022300253 20070223 00253 NM 2007 2 23 2007UALA00403 1 20070210 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY LIGHT AT DOOR 4R FWD & AFT SILL LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022300254 20070223 00254 NM 2007 2 23 2007UALA00449 1 20070215 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 RIGHT AFT FUSELAGE BS 852 HAS A 4 INCH LONG VERTICAL GOUGE ACROSS STR S16R. MAJOR REPAIR ACCOMPLISHED. FABRICATED & IN STALLED DOUBLER, TRIPLER & STRUCTURAL FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022300255 20070223 00255 NM 2007 2 23 2007UALA00450 1 20070215 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 UPPER FUSELAGE EXTERIOR SKIN HAS WEAR IN AREA OF DORSAL FIN SEAL CONTACT APPROX AT BS 908 TO BS 960 LT SIDE. MAJOR REPA IR ACCOMPLISHED. FABRICATED & INSTALLED DOUBLER, TRIPLER AND TEAR STRAP REPAIR. INSTALLED WEAR STRIPS FROM BS 908 TO B S 1000. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022300258 20070223 00258 EU 2007 2 23 2007UALA00453 1 20070214 A 5322 SHEAR TIE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 430UA 568 FWD CARGO PIT CORROSION AT FRAME 28 SHEAR TIES BETWEEN STR 43 & 44 LT, 42 & 43 LT, 41 & 42 RT, 42 & 43 RT AND 43 & 44 RT . MAJOR REPAIR ACCOMPLISHED: REPLACED SHEAR TIES. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022300259 20070223 00259 EU 2007 2 23 2007UALA00454 1 20070214 A 5322 SHEAR TIE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 430UA 568 FWD CARGO PIT CORROSION AT FRAME 31 SHEAR TIES BETWEEN STR 43 & 44 LT, 41 & 42 LT, 40 & 41 LT, 42 & 43 RT, 41 & 42 RT, 4 0 & 41 RT, 39 & 40 RT. REPAIR ACCOMPLISHED: REPLACED SHEAR TIES. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022300260 20070223 00260 EU 2007 2 23 2007UALA00455 1 20070214 A 5322 SHEAR TIE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 430UA 568 FWD CARGO PIT CORROSION AT FRAME 33 SHEAR TIES BETWEEN STR 43 & 44 LT, 41 & 42 LT, 40 & 41 LT, 41 & 42 RT AND 40 & 41 RT . MAJOR REPAIR ACCOMPLISHED: REPLACED SHEAR TIES. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022300261 20070223 00261 EU 2007 2 23 2007UALA00456 1 20070214 A 5314 ATTACH ANGLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 430UA 568 KEEL BEAM LWR LEFT WEB UPPER ATTACH ANGLE IS CRACKED JUST FWD OF FR 47. MAJOR REPAIR ACCOMPLISHED: REPLACED ANGLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022300267 20070223 00267 2007 2 23 2007UALA00462 4 20070214 A 2565 O-RING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT SLIDE BOTTLE FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 LEFT OFF-WING SLIDE CYLINDER HAS LOW BOTTLE PRESSURE AND WHITE INDICATOR IS NOT IN THE ARM INDICATOR WINDOW. REPLACED CYLINDER PER MM 25-65-02. A/C READY FOR SERVICE. SUSPECT O'RINGS LEAKING DUE TO HARDENING. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022200106 20070222 00106 NM 2007 2 22 SWAA070880 1 20070215 A 5330 65C26493 SKIN PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED HC1 CHECK, FOUND KEEL BEAM SKIN PANEL CRACKED AT BS 699, STR 27L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007022200116 20070222 00116 NM 2007 2 22 SWAA070871 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200124 20070222 00124 2007 2 22 SWAA070753 4 20070213 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 231WN 32499 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007022200129 20070222 00129 NM 2007 2 22 SWAA070795 1 20070213 A 5330 6545776 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 907, STR 25L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007022200137 20070222 00137 NM 2007 2 22 SWAA070864 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200138 20070222 00138 NM 2007 2 22 SWAA070863 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200144 20070222 00144 NM 2007 2 22 SWAA070907 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 390, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200155 20070222 00155 NM 2007 2 22 SWAA070765 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007022200179 20070222 00179 NM 2007 2 22 SWAA070787 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200182 20070222 00182 NM 2007 2 22 SWAA070784 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200200 20070222 00200 NM 2007 2 22 SWAA070909 1 20070215 A 5312 BAC1514 STIFFENER BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND BULKHEAD STIFFENER CRACKED AT BS 1016, RBL 17, WL 209. REPAIRED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2007022200206 20070222 00206 NE 2007 2 22 F3LA200700026 2 20070218 A 7220 D5453011820000 GUIDE VANE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE ENGINE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 929FR 4725 2240 575826 DURING C-2 CHECK, INSPECTION REPORTED NR 1 ENG OUTLET GUIDE VANE AT 8 O'CLOCK POSITION HAD CRACK AT T/E. REPLACED OUTLE T GUIDE VANE IAW AMM 72-23-00-400-008 AND 72-23-00-400-026. 2 L 7 2 4F 4 F RT A28NM E37NE 2007022200208 20070222 00208 NM 2007 2 22 SWAA070777 1 20070213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200213 20070222 00213 NM 2007 2 22 SWAA070773 1 20070213 A 5523 REP4M6 BEARING BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED 12Y CHECK, RIGHT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR CONTROL ROD BUSHING, B EARING AND SLEEVE PER MM. 2 L 7 2 4F RT A16WE 2007022200225 20070222 00225 NM 2007 2 22 SWAA071031 1 20070220 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 743D, STR 23L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007022200226 20070222 00226 NM 2007 2 22 SWAA071032 1 20070220 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 742D, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007022300002 20070223 00002 SO 2007 2 23 C2XA07TY006 1 20070221 A 5610 163500115 WINDSHIELD EMB 145 EMB145LR 3260212 SO COCKPIT CRACKED A C2XA K NONE O OTHER DE DESCENT 1 SW 27 10575 145640 FLIGHT 2362 DESENDING INTO ATL, THE NUMBER ONE WINDSHIELD SHATTERED. A/C LANDED SAFELY AND MAINTENANCE REMOVED AND REPL ACED THE NUMBER ONE WINDSHIELD IAW EMB 145 AMM TWO 56-10-01. PRESSURIZATION CHECKS AND LEAK CHECKS GOOD. RETURNED TO S ERVICE. 2 L 7 2 4T RT T00011AT 2007022300014 20070223 00014 NM 2007 2 23 CALA0700082 1 20070221 A 5313 65C35767 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 INSPECTION FOUND LIGHT SURFACE CORROSION DOWN CENTER OF STRINGER 26L IN FORWARD BAGGAGE BIN AT STA 500D-520. THE STRING ER WAS REPAIRED IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 2007022300015 20070223 00015 EA 2007 2 23 COMA0760202 1 20070221 A 5610 601R3303313 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 916CA 4771 7014 FLIGHT 5194 - CAPTAIN'S WINDSHIELD CRACKED AT GATE. REPLACED CAPTAIN'S WINDSHIELD. 2 L 7 2 4F RT A21EA 2007022300020 20070223 00020 WP 2007 2 23 UPS07849226 1 20070221 A 3230 O-RING DOUG DC8 DC871F 302199D WP LT MLG LEAKING A IPXA K NONE K FLUID LOSS DE DESCENT 1 SO 01 703UP 45939 INSPECTION TYPE:N/A EMERGENCY DECLARED - AT TOP OF DESCENT FLUID DROPPED TO AUX POSITION PERFORMED LOSS OF FLUID ON PRES SURE CHECKLIST. AS PER QRH LANDING & TAXI IN NORMAL. FLUID INDICATION NEVER DROPPED BELOW AUX POSITION. FOUND LEFT ML G BOGIE SWIVEL UNLOCK CYLINDER PLUG O-RING LEAKING. INSTALLED NEW O-RING ON PLUG & TORQUED PLUG REF MM 20-60-00-2 USING ENGINE DRIVEN AND AUX HYDRAULIC SYSTEMS. NO LEAKS AT THIS TIME. 2 L 7 4 4F RT 4A25 2007022300028 20070223 00028 NE 2007 2 23 KPVA20072 2 20070214 A 7320 78634114 HMU DHAV DHC8 DHC8103 1386005 NM PWA PW121 PW121 52124 NE NR 1 ENGINE MALFUNCTIONED A KPVA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 13 979HA 696 373 PCE121346 NR 1 ENGINE FAILED TO PRODUCE SUFFICIENT POWER ON THE TAKEOFF ROLL. REMOVE AND REPLACED NR 1 ENGINE HMU IAW PRATT & WHI TNEY MM CHAPTER 72, 72-01-40 PAR 5. OPERATIONAL AND LEAK CHECK GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2007022300031 20070223 00031 NM 2007 2 23 MWEA070033 1 20070214 A 3350 LIGHT BOEING 717 717200 1383700 NM TAILCONE INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 928ME 55194 AFT ACCESSORY TAIL CONE RELEASE HANDLE EMERGENCY LIGHTS INOPERATIVE. RELAMPED EMERGENCY LIGHTS. 2 L 7 2 4F TR A6WE 2007022300033 20070223 00033 WP 2007 2 23 MWEA070031 1 20070211 A 5330 5911401179 DOUBLER DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 813ME 48007 CRACK IN AFT LOWER AIRSTAIRS OPENING / FORWARD AIRSTAIR. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2007022300044 20070223 00044 NM 2007 2 23 SWAA071041 1 20070220 A 5311 6546549 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED BS 767, STR 9R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007022300048 20070223 00048 NM 2007 2 23 SWAA070534 1 20070201 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 215WN 32487 EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007022300052 20070223 00052 NM 2007 2 23 SWAA070533 1 20070201 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 FUSELAGE SKIN CRACKED AT BS 540, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007022300053 20070223 00053 NM 2007 2 23 SWAA070551 1 20070201 A 5330 6545767 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 492, STR 27R. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007022300059 20070223 00059 2007 2 23 SIMA200705302 2 20070221 A 7200 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA RT ENGINE UNKNOWN A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 513AE 10114 RECEIVED RIGHT ENGINE OIL PRESSURE WARNING MESSAGE ON BOTH ENGINES DURING CLIMB-OUT, ENGINES OPERATING INDICATIONS NORMA L. RECEIVED NUMEROUS ADDITIONAL EICAS MESSAGES IN FLIGHT AND UPON LANDING. RETURNED TO CLE. INSPECTED DIGITAL CONTROL UNITS FOR MOISTURE AND CONNECTOR PIN DEFECTS WITH NO FINDINGS. PERFORMED CRJ FIM AND SERVICE NEWSLETTER 31-005. OPERA TIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007022300060 20070223 00060 NM 2007 2 23 SWAA070548 1 20070201 A 5310 6545834 CREASE BEAM BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 277 TO BS 294, RBL 55, WL 208. REMOVED AND REPLACED CR EASE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2007022300062 20070223 00062 NM 2007 2 23 SWAA070541 1 20070201 A 5753 6546435277 FLAP BOEING 737 7373G7 1384595 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED C4 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD T/E END. REMOVED AND REPLACED A FT FLAP PER MM. 2 L 7 2 4F RT A16WE 2007022300066 20070223 00066 NM 2007 2 23 SWAA070612 1 20070205 A 5320 141A57503 FITTING BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 743SW 29279 DURING SCHEDULED 8Y CHECK, FOUND INTERCOSTAL FITTING CORRODED AT BS 288 TO BS 294, RBL 19. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2007022300067 20070223 00067 NM 2007 2 23 SWAA070613 1 20070205 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 743SW 29279 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 39. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007022300075 20070223 00075 NM 2007 2 23 07FDEA00541 1 20070222 A 5230 UNKNOWN BOEING 727 727277 138408S NM MCD NONE A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 240FE 20978 DOORS, MAIN CARGO LWR AFT CORNER EXTERNAL SKIN PERMANENT REPAIR P/N 52FX1435-2. COMPLIED WITH EA 7-5230-102022 DOORS M AIN CARGO, LWR AFT CORNER EXTERNAL SKIN PERMANENT REPAIR P/N 52FX14 35-2. 2 L 7 3 4F RT A3WE 2007022300080 20070223 00080 NM 2007 2 23 SWAA070587 1 20070204 A 5311 6545805 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007022300081 20070223 00081 NM 2007 2 23 SWAA070589 1 20070204 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007022300087 20070223 00087 NM 2007 2 23 SWAA070602 1 20070204 A 2560 6949956 CABLE BOEING 737 7373Q8 1384670 NM EVAC SLIDE MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 672SW 23406 L2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2007022300089 20070223 00089 NM 2007 2 23 SWAA070595 1 20070204 A 3350 F18T5WWRS LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 249WN 34951 DURING SCHEDULED MV2 CHECK, FOUND RIGHT FWD CABIN EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT BULB P ER MM. 2 L 7 2 4F RT A16WE 2007022300090 20070223 00090 WP 2007 2 23 N921R28116 1 20070104 A 5313 STRINGER SPLICE DOUG DC8 DC863F 302198F WP BS 440-460 L31L CRACKED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 921R 46145 FWD CARGO COMPARTMENT BTW STA 440 AND 460, L31L SPLICE FITTING WITH 3/4" CRACK. REMOVED AND REPLACED SPLICE FITTING OF FWD CARGO COMPARTMENT BTW STA 440 AND STA 460, L31L IAW DC8 SRM 51-1-20 AND SRM 53-4-1 CPCP 557L 0551. 2 L 7 4 4F 4A25 2007022300092 20070223 00092 WP 2007 2 23 AALA20070345 1 20070216 A 3213 SEAL DOUG DC9 DC982 3022082 WP NLG STRUT DIRTY A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 468AA 49598 ORD INFLIGHT T1349/16FEB - CREW UNABLE TO RETRACT LANDING GEAR. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. CLEANED AND REPLACED SEALS, BEARING PLATE, AND SCHRADER VALVE. SERVICED STRUT WITH NEW FLUID. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F A6WE 2007022300097 20070223 00097 NM 2007 2 23 AALA20070348 1 20070217 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 962AN 30858 MIA - FOUND EMERGENCY LIGHT AT SEAT 9D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007022300104 20070223 00104 EU 2007 2 23 AALA20070326 1 20070211 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80084 675 MIA - FOUND EMERGENCY LIGHTS AT SEAT 33G INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 33G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007022300111 20070223 00111 EU 2007 2 23 AALA20070315 1 20070211 A 3213 ROCKER AIRBUS 300 A300B4605R 3930308 EU NLG STRUT INOPERATIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 59081 639 JFK INFLIGHT T1196/11FEB - NOSE GEAR UNSAFE LIGHT ILLUMINATED WHEN GEAR EXTENDED. CYCLED GEAR THREE TIMES WITH NO HELP . LANDED JFK WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR TELESCOPIC DRAG STRUT ROCKER ARM ASSEMBLY. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007022300113 20070223 00113 NM 2007 2 23 AWXA200700220 1 20070202 A 5320 65314431 REVEAL BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND FORWARD AIRSTAIR CUT OUT UPPER AFT CORNER REVEAL CRACKED, BS 305.9, S18L. REPLACED FORWARD AIRSTAIR CUT OUT UPPER AFT CORNER REVEAL, BS 305.9, S18 IAW B737-300 SRM 51-40-05. 2 L 7 2 4F RT A16WE 2007022300114 20070223 00114 NM 2007 2 23 AWXA200700221 1 20070125 A 5330 6552988 SKIN BOEING 737 7373S3 1384711 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND FUSELAGE SKIN CRACKED B/S 727E + 18" JUST ABOVE S24L. REPAIRED FUSELAGE SKIN BS 727E + 18" JUST ABOVE S24L IAW B737-300 SRM 53-00-01-2R. 2 L 7 2 4F RT A16WE 2007022300115 20070223 00115 NM 2007 2 23 AWXA200700222 1 20070125 A 5330 6552988 SKIN BOEING 737 7373S3 1384711 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND FUSELAGE SKIN CRACKED B/S 727D + 18" JUST ABOVE S24L. REPAIRED FUSELAGE SKIN B/S 727D + 18" JUST ABOVE S24L IAW B737-300 SRM 53-00-01-2R. 2 L 7 2 4F RT A16WE 2007022300121 20070223 00121 NM 2007 2 23 AALA20070322 1 20070210 A 3397 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHTS AT RIGHT NUMBER FOUR DOOR INOPERATIVE. RESEATED BATTERY PACK CONNECTOR FOR EMERGENCY LIGHT AT RI GHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007022300122 20070223 00122 WP 2007 2 23 AALA20070324 1 20070212 A 3350 P4010051111 MODULE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9625W 53595 LGA - FOUND EMERGENCY EGRESS LIGHTS FROM SEAT ROWS 1 TO 19 INOPERATIVE. REPLACED EMERGENCY LIGHT MODULE AT SEAT ROW 19 OVERHEAD BIN FOR SEAT ROWS 1 TO 19. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007022300123 20070223 00123 NM 2007 2 23 2007UALA00411 1 20070211 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY EXIT CEILING LIGHT INOP AT ROW 37 RIGHT. RELAMPED. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022300125 20070223 00125 WP 2007 2 23 AALA20070327 1 20070212 A 3213 SEAL DOUG DC9 DC982 3022082 WP NLG STRUT INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7530 49922 IND INFLIGHT T1077 - NOSE GEAR WOULD NOT RETRACT. RED UNSAFE INDICATION REMAINED ILLUMINATED ALONG WITH VIBRATION. RET URNED IND AND LANDED WITHOUT INCIDENT. REPLACED NOSE STRUT SEALS AND SERVICED NOSE STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007022300126 20070223 00126 NM 2007 2 23 AALA20070331 1 20070214 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 786AN 30250 MIA - EMERGENCY LIGHT AT SEAT ROW 14 MISSING LENS COVER. REPLACED LENS COVER FOR EMERGENCY LIGHT AT SEAT ROW 14. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007022300133 20070223 00133 NM 2007 2 23 AALA20070330 1 20070213 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 689AA 25731 MIA - FOUND EMERGENCY LIGHTS FROM SEAT ROWS 24D TO 36D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEA T ROWS 24D TO 36D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007022300135 20070223 00135 NM 2007 2 23 AALA20070335 1 20070215 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 782AN 30003 DFW - FOUND EMERGENCY LIGHT AT SEAT 3G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 3G. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007022300143 20070223 00143 EU 2007 2 23 2007UALA00471 1 20070215 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 430UA 568 FWD PIT STRINGER 39 LT HAS CORROSION 3 INCHES FWD OF FR 33. MAJOR REPAIR ACCOMPLISHED: INSTALLED SPLICE REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022300149 20070223 00149 WP 2007 2 23 AALA20070323 1 20070211 A 3213 STRUT DOUG DC9 DC983 3022083 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 569AA 49351 SFO INFLIGHT T860 - NOSE LANDING HEAR BOTTOMED OUT ON TAKEOFF ROLL AND COLLAPSED AFTER HITTING A BUMP RISE ON RUNWAY. A FTER GEAR RETRACTION NOSE LANDING GEAR DOORS REMAINED OPEN. GEAR UP RED LIGHT ILLUMINATED. CYCLED GEAR WITH SAME INDIC ATION. NOSE LANDING GEAR DOORS CONFIRMED OPEN. INSPECTED NOSE STRUT PISTON AND REPLACED NOSE STRUT SCHRADER VALVE O-RI NG. REPACKED NOSE STRUT. INSPECTED NOSE GEAR DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007022300153 20070223 00153 NM 2007 2 23 2007UALA00474 1 20070215 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 E&E COMPARTMENT STA 312 STR 28R CLIP HAS WEAR SPOT. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022300160 20070223 00160 NM 2007 2 23 2007UALA00476 1 20070215 A 5313 STRINGER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 FWD PIT AT STA 406 STR 25L OUTBOARD FREE FLANGE IS DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022300162 20070223 00162 WP 2007 2 23 AALA20070294 1 20070206 A 3233 59370365507 ACTUATOR DOUG DC9 DC983 3022083 WP RT MLG INOPERATIVE A AALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SW 21 966TW 53616 MCI - INFLIGHT T1926 - TUS TO ORD - RED GEAR DOOR LIGHT REMAINED ON WITH GEAR HANDLE UP. CYCLED GEAR AND RED GEAR DOOR LIGHT REMAINED ON. LANDED MCI WITHOUT INCIDENT. REPLACED RIGHT GEAR ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007022300166 20070223 00166 EU 2007 2 23 AWXA200700210 1 20070211 A 5313 D53480047204 STRINGER AIRBUS 320 A320231 3930325 EU ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 632AW 81 PHX - FOUND CORROSION ON STRINGER, FR 65, S31R, BELOW OUTFLOW VALVE CUT OUT. REPAIRED STRINGER, FR 64 - FR 67, S31R, BE LOW OUTFLOW VALVE CUT OUT IAW AWA ER 26-5341-07044-TH1. 2 L 7 2 4F RT A28NM 2007022300167 20070223 00167 NM 2007 2 23 AWXA200700211 1 20070124 A 5752 654645521SP TAB BOEING 737 7373S3 1384711 NM ZONE 500 DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR - LEFT WING AILERON TAB OUTBOARD TRAILING EDGE IS DELAMINATED, WBL 479.50 - 480.00. REPAIRED LEFT WI NG AILERON TAB OUTBOARD TRAILING EDGE, WBL 479.50 - 480.00 IAW B737-300 SRM 51-70-06 REPAIR 2. 2 L 7 2 4F RT A16WE 2007022300168 20070223 00168 NM 2007 2 23 AWXA200700212 1 20070202 A 5420 D54630462201 SUPPORT ANGLE AIRBUS A319 A319132 3930340 NM NR 2 NACELLE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 831AW 1576 SAL - NR 2 PYLON SUPPORT ANGLE (OUTBOARD EXTRUSION) CRACKED, RIB 8. REPLACED NR 2 PYLON SUPPORT ANGLE (OUTBOARD EXTRUSI ON), RIB 8 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007022300181 20070223 00181 NM 2007 2 23 AWXA200700230 1 20070119 A 5754 SKIN BOEING 737 73733A 1384673 NM NR 6 SLAT DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 174 23625 MCN - RIGHT WING NR 6 SLAT WEDGE UPPER AND LOWER SURFACES DEBONDED, SS 257. REPAIRED RIGHT WING NR 6 SLAT WEDGE UPPER A ND LOWER SURFACES, SS 254.53 - SS 277.28 IAW B737-300 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 2007022300185 20070223 00185 NM 2007 2 23 AWXA200700232 1 20070119 A 5751 SKIN BOEING 737 73733A 1384673 NM AILERON DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW HDH0059 23625 MCN - RIGHT WING AILERON LEADING EDGE PANEL 8806R CUT OUT CRACKED AND DELAMINATED, AILERON STATION 536.5. REPAIRED RIGH T WING AILERON LEADING EDGE PANEL 8806R CUT OUT CRACKED AND DELAMINATED, AILERON STATION 536.5 IAW AWA ER 03-5760-07047- ES2. 2 L 7 2 4F RT A16WE 2007022300188 20070223 00188 NM 2007 2 23 2007UALA00482 1 20070215 A 5230 STRUCTURE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CARGO DOOR DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 676UA 30028 MANUAL PIT CARGO DOOR HAS HOLE NEAR AFT EDGE OF DOOR. REPAIRED DOOR DAMAGE PER SRM 52-30-01 REPAIR 6. PAINTED TO MATCH. SUSPECT DAMAGE DUE TO GROUND EQUIPMENT CONTACT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022300193 20070223 00193 SO 2007 2 23 SWIA200717820 1 20070216 A 5610 WINDSHIELD EMB 120 EMB120ER 3260203 SO COCKPIT FAILED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 271YV 120271 CO PILOT'S WINDSHIELD SHATTERED AFTER THE LANDING ROLL. REPLACED FIRST OFFICER'S WINDSHIELD IAW EMB 120 AMM REF 56-10-0 1, P/N NP-151311-2, S/N OFF 03119H2956. 2 L 7 2 4T RT A31SO 2007022300199 20070223 00199 EU 2007 2 23 07FDEA00443 1 20070209 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 MDC SEAT TRACK NR 5R AT FR 77.5 HAS CORROSION. BLEND CORROSION, OUT OF LIMITS. REPLACED DAMAGED SEAT TRACK SECTION WIT H NEW AND SPLICES IAW A310-200 SRM 51-74-10, 53-10-16. ALSO, INSTALLED FLOORBOARDS 262VF AND 262UF IAW A310 AMM 53-10-2 3. MAJOR REPAIR IAW FEDEX GMM 6-2-100. SEE JPF N00820. 2 L 7 2 4F RT A35EU 2007022300207 20070223 00207 NE 2007 2 23 740005 2 20070213 A 7320 580278005 CABLE BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE NR 4 ENGINE FROZEN A Q2SA J A DUMP FUEL UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 NE 03 740SA 21380 528408 NR 4 ENGINE PARAMETERS INDICATED LOSS OF POWER AT CRUISE ALTITUDE OF 25,000 FEET. EGT HIGH, N1 AND N2 LOW, FUEL FLOW HI GH AND ENGINE SURGES +/- 3 PERCENT. DUMPED 96,000 LBS OF FUEL AND DIVERTED TO RKSI. FOUND FROZEN VSV FEEDBACK CABLE. REMOVED AND REPLACED NR 4 VSV FEEDBACK CABLE IN ACCORDANCE WITH AMM 75-31-03. ACCOMPLISHED MAXIMUM ASSURANCE RUN IN ACC ORDANCE WITH SAI JOB CARD RNR 4771002. OPERATIONAL CHECK GOOD ON GROUND. 2 L 7 4 4F 4 F A20WE E23EA 2007022300226 20070223 00226 2007 2 23 2007UALA00393 4 20070210 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 THE 4R DOOR SLIDE PRESSURE READS LOW. REPLACED DOOR SLIDE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022300237 20070223 00237 NM 2007 2 23 07FDEA00500 1 20070215 A 5713 STRINGER DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 DURING HFEC INSPECTION, CRACK FOUND AT STRINGER 14 (XORS 521) IN RIGHT TANK. CARRIED OUT REPAIR AT RT WING STRINGER 14R (XORS 521) AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022300238 20070223 00238 NM 2007 2 23 07FDEA00501 1 20070215 A 5713 STRINGER DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 DURING HFEC INSPECTION, CRACK FOUND AT STRINGER 09 (XORS 819) IN RIGHT TANK. REPAIR CARRIED OUT PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022300263 20070223 00263 NM 2007 2 23 2007UALA00458 1 20070213 A 2920 RAM AIR TURB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE UNWANTED EXTEND A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 508UA 24744 DURING WALK AROUND NOTICED RAT IN THE FULLY EXTENDED POSITION. STILL WIRED SHUT IN COCKPIT. REPLACED RAM AIR TURBINE AIRSPEED SWITCH, SYSTEM 1 AIR GRND RELAY, AND RAT TIME DELAY MODULE, TRANSFERRED APU TO EXTERNAL PWR, COULD NOT DUPLICA TE FAULT, VERIFIED NO VOLTAGE AT RAT CNTRL VALVE WITH MANUAL SWITCH OFF, CYCLED SWITCH AND POWER CHECKS OK. ACCOMPISHED INPECTION AND STOWING OF RAM AIR TURBINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022300264 20070223 00264 2007 2 23 2007UALA00459 4 20070215 A 2565 PIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EVAC SLIDE BINDS A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 436UA 638 FWD RIGHT MED EMERGENCY EVACUATION SLIDE INFLATION BOTTLE SAFETY PIN INSERTION WAS EXTREMELY HARD. [SUP 05-16-07] FWD RT EMERGENCY SLIDE WAS REPLACED. IT WAS LATER DETERMINED THAT THE INFLATION BOTTLE REGULATOR VALVE WAS OUT OF POSITION, WHICH WAS CAUSING THE SAFETY PIN HOLES TO NOT LINE UP CORRECTLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022300268 20070223 00268 NM 2007 2 23 2007UALA00463 1 20070214 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 786UA 26938 AFT EMERGENCY LIGHT INOPERATIVE AT SEAT 1E. REPLACED LIGHT ASSY, OPS CHECKS OK . 2 L 7 2 4F 4 F RT T0001SE E46NE 2007022300271 20070223 00271 NM 2007 2 23 2007UALA00466 1 20070215 A 5330 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 906UA 25006 FUSELAGE SKIN IS SCRATCHED AND DENTED APPROX 29 INCHES BELOW AFT END OF DOOR 1R OPENING. MAJOR REPAIR ACCOMPLISHED. MA NUFACTURED DOUBLER, TRIPLER, FILLER AND INTERNAL TEAR STRAP DOUBLERS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022300275 20070223 00275 NM 2007 2 23 USAA070107 1 20070215 A 5754 114T410338A SKIN BOEING 737 737201 1384454 NM L/E SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246US 22753 THREE AREAS, 7 INCHES DIA DELAMINATED, NR 10 SLAT, UPPER SURFACE, 0SS 798.74-815.74. CUT OUT DELAMINATION, BONDED REPAI R DOUBLER PER SRM 51-20-10, 57-43-02, DEFECT SIZE: 7 INCHES DIA. 2 L 7 2 4F A16WE 2007022300277 20070223 00277 NM 2007 2 23 USAA070111 1 20070220 A 5310 DOOR FRAME BOEING 737 7374B7 1384702 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 24781 RADIATING FROM LOWER O/B STOP BOLT HOLE, STA 492.4, S24R, FWD CARGO DOOR DAMAGE. INSTALLED DOUBLER PER EA 98497, DEFECT SIZE: .375 INCH. 2 L 7 2 4F RT A16WE 2007022300280 20070223 00280 NM 2007 2 23 USAA070108 1 20070220 A 5310 DOOR FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 24781 FWD CARGO DOOR, AFT FUSELAGE FRAME, O/B OF UPPER I/B STOP BOLT HOLE CRACKED. REMOVED DAMAGE & INSTALLED REPAIR PARTS PE R EA 98497, DEFECT SIZE: .075 INCH. 2 L 7 2 4F RT A16WE 2007022300281 20070223 00281 NE 2007 2 23 SA07012 2 20070213 A 7321 2042M14P05 ECU AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4P NE LT ENGINE FAILED A USAA K NONE R PARTIAL RPM/PWR LOSS DE DESCENT 1 EA 19 123UW 17217 14815 1310 779775 CLT FLT 1576 EN ROUTE FLL TO CLT. THE LEFT ENGINE WENT TO IDLE THRUST IN FLIGHT. THE FLIGHT LANDED WITHOUT FURTHER INC IDENT. MAINTENANCE PERFORMED AN ELECTICAL CHECK ON THE J4 HARNESS AND WIRING. NO FAULTS WERE FOUND. MAINTENANCE REPLA CED THE LEFT ENGINE J4 HARNESS AND LEFT ENGINE ECU AS A PRECAUTION. 2 L 7 2 4F 4 F RT A28NM E38NE 2007022300282 20070223 00282 NM 2007 2 23 DL738070139 1 20070217 A 2120 UNKNOWN BOEING 737 737832 13844CF NM COCKPIT ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 3760C 30816 ON ENGINE SHUT DOWN, SMELLED LIKE ACRID ELEC SMOKE ROSE FROM BEHIND F/O SEAT FROM THE VICINITY OF THE C/B PANEL A/C WAS POWERED BY THE APU GRD POWER WAS AVAILABLE. OPENED AND INSP C/B PANELS NTF INSP FOR OPEN C/B NONE FOUND RAN ENGS TRANS POWER FORM APU TO ENG AND BACK CHECKED WINDOW HEAT ALL NORMAL OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2007022300283 20070223 00283 NE 2007 2 23 DL757070142 2 20070218 A 7320 FUEL CONTROL BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 670DN 64138 25331 716401 THE CREW ADVISED AT 1000 AGL, STARTING A TURN AND HAND FLYING THE A/C, THE NR 2 ENG SLOWLY ROLLED BACK WITH RUMBLING NOT ICED. THEY WERE ABLE TO REGAIN ENGINE CONTROL AND ALL PARAMETERS WERE NORMAL. ON EICA,S NO EPCS MSGS INSPECTED INTAKE AND EXHAUST NO DAMAGE FOUND. PERFORMED ENGINE BORSCOPE LOW PRESSURE COMPRESSOR SECTION FOUND ALL NORMAL PER M/M. REMOV ED AND REPLACED FUEL PUMP. REMOVED AND REPLACED FUEL CONTROL UNIT PER M/M. REQUIRES ENGINE RUN UP AND LEAK CHK. PERFO RMED ENGINE RUN AND LEAK CHK, CHKS GOOD PER M/M. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022300284 20070223 00284 NM 2007 2 23 WRLA2007039 1 20070208 A 5751 PANEL DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE RT AILERON WORN A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 62911 48407 DURING 3C + 12A CHECK, EGAT MECHANIC FOUND WORN AT RIGHT WING INBOARD AILERON OUTBOARD FIXED PNL FWD ROW FASTENER HOLES STA XORS + 433 TO 480, REAR SPAR. PERFORM RIGHT WING INBOARD AILERON OUTBOARD FIXED PANEL REPAIRED PER ENGINEERING INST RUCTION W2007A57B-093 REV 01. CONDITION CHECK NORMAL & JOB COMPLETED. 2 L 7 3 4F 4 F RT A22WE E24NE 2007022300285 20070223 00285 NM 2007 2 23 WRLA2007038 1 20070208 A 2820 AHL74281 BRACKET DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE FUEL SYSTEM CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 62911 48407 DURING 3C+12A CHECK, EGAT MECHANIC FOUND TAIL SECTION STA 2033-2122 TAIL FUEL SYSTEM HAVE BRACKET CRACK AND CLAMP CRACK. REPLACED TAIL FUEL SYSTEM BRACKET AND CLAMP PER AMM 20-05-02 900-801 REV 57. 2 L 7 3 4F 4 F RT A22WE E24NE 2007022300290 20070223 00290 EU 2007 2 23 R61A20070005 1 20070211 A 2781 1702286A SENSOR EMB ERJ170 ERJ170100 EU L/E SLAT MALFUNCTIONED A R61A O OTHER N FALSE WARNING DE DESCENT 1 GL 11 812MD 3465 17000030 CREW REPORTED A SLAT FAIL MESSAGE ON DESCENT. CREW DIVERTED TO IAD FOLLOWED QRH AND LANDED WITH OUT INCIDENT. MAINTENA NCE WAS DISPATCHED TO THE AIRCRAFT, TROUBLESHOT AND REPLACED NR 3 AND 4 SLAT SKEW SENSORS, SYSTEM OPERATIONAL CHECK GOOD . AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A56NM 2007022300291 20070223 00291 EU 2007 2 23 R61A20070006 1 20070218 A 2782 1702885B ACTUATOR EMB ERJ170 ERJ170100 EU L/E SLAT BROKEN A R61A K NONE J WARNING INDICATION DE DESCENT 1 GL 11 801MD 7589 7589 1700012 RECEIVED SLAT FAIL MESSAGE. DECLARED EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. 2 L 7 2 4F RT A56NM 2007022300294 20070223 00294 NM 2007 2 23 SB07012 1 20070211 A 2910 HYDRAULIC LINE BOEING 737 7374B7 1384702 NM MLG WW LEAKING A USAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 444US 24862 CLT FLT1786 EN ROUTE FROM JAX TO CLT, DURING CRUISE, CREW REPORTED LOSS OF B-HYDRAULIC SYSTEM AS HYDRAULIC QUANTITY RAPI DLY WENT DOWN TO 1/4. THE FIRST INDICATION WAS NR 2 ENGINE BELOW PRESSURE LIGHT, FOLLOWED BY LOSS OF B-HYDRAULIC FLUID AND THEN B-SYSTEM LOW PRESSURE LIGHT ILLUMINATED. OVERHEAT LIGHT DID NOT ILLUMINATE AT ANYTIME. CREW DECLARED AN EMERG ENCY AND LANDED AT CLT WITHOUT FURTHER INCIDENT. AIRCRAFT TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE REMOVED AND REPLACED B-HYDRAULIC SYSTEM PRESSURE LINE PER MM 20-10-52. LEAK CHECK SATISFACTORY. 2 L 7 2 4F RT A16WE 2007022300295 20070223 00295 NM 2007 2 23 USAA070106 1 20070214 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 24811 BS 492, S-24R, WL 160 CRACKED. REPLACED FRAME PER DWG 65-20723, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007022300296 20070223 00296 NM 2007 2 23 USAA070105 1 20070214 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 24811 BS 440 S-24R WL 160 CRACKED. TRIMMED OUT CRACK, HEAT TREATED, INSTALLED REPAIR DOUBLERS PER EA 98453, DEFECT SIZE: 1 I NCH. 2 L 7 2 4F RT A16WE 2007022300297 20070223 00297 EU 2007 2 23 USAA070104 1 20070214 A 5320 D5311282600101 TRACK AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 169UW 1455 AT 21 INCHES LEFT OF CENTER FROM COCKPIT DOOR TO FLOORBEAM C16, FR 12-16 HAS CORROSION. REMOVED & REPLACED PER AIRBUS S RM 51-72-11; CORR TASK JA-220-25503; LEVEL 1, DEFECT SIZE: 1 X 21 INCHES. 2 L 7 2 4F RT A28NM 2007022300298 20070223 00298 EU 2007 2 23 USAA070103 1 20070214 A 5322 D5347112420000 SHEAR TIE AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 169UW 1455 FROM 69 TO 70 AT Y1162.5 HAS CORROSION. REPLACED SHEAR TIE WITH IDENT PART PER SRM 51-72-11; CORR LEVEL 1; TASK JA-260- 53500, DEFECT SIZE: 4 SQ INCHES. 2 L 7 2 4F RT A28NM 2007022300299 20070223 00299 EU 2007 2 23 USAA070102 1 20070214 A 5315 D5311281520200 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 169UW 1455 TOP OF BEAM, FWD END OF SEAT TRACK I/B LEFT BEAM HAS CORROSION. REMOVED & REPLACED BEAM PER SRM 51-72-11; CORR LEVEL 1; TASK JA-220-25503, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A28NM 2007022300300 20070223 00300 EU 2007 2 23 USAA070101 1 20070214 A 5320 D53112830202 FLOOR SUPPORT AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 169UW 1455 AFT END OF FLOOR SUPPORT AT C16 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11; CORR TASK JA-220-25503; LEVEL 1, DEFECT SIZE: 1 X 1 INCH. 2 L 7 2 4F RT A28NM 2007022300301 20070223 00301 EU 2007 2 23 USAA070100 1 20070214 A 5315 D5347218920400 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 169UW 1455 FLOORBEAM -Y1292 BETWEEN FRAMES 66 & 68, SEVERAL SPOTS CORRODED. DEFECTIVE PART REPLACED WITH IDENTICAL PART; CORR LEVE L 1; TASK JA-260-53500, DEFECT SIZE: .5 X .5 INCH. 2 L 7 2 4F RT A28NM 2007022300302 20070223 00302 EU 2007 2 23 USAA07099 1 20070214 A 5315 D5311281820401 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 169UW 1455 TWO AREAS, 13 INCHES LEFT OF CENTER FLOORBEAM C16 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53 -14-14; CORR LEVEL 1; CORR TASK: JA-220-25503, DEFECT SIZE: 1 X 1 INCH. 2 L 7 2 4F RT A28NM 2007022300304 20070223 00304 NM 2007 2 23 SB07014 1 20070221 A 3350 20131ASMI BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 504AU 23379 DCA - MAINTENANCE REPORTED THE EMERGENCY EXIT SIGNS AT THE FORWARD ENTRY DOOR AND FORWARD SERVICE DOOR INOPERATIVE. MAI NTENANCE REMOVED AND REPLACED THE FORWARD LEFT AND FORWARD RIGHT BATTERY PACKS. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007022300305 20070223 00305 NM 2007 2 23 SB07015 1 20070221 A 3350 03600570010 FUSE BOEING 737 737401 1384701 NM BATTERY PACK BLOWN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 424US 23991 ORD - MAINTENANCE FOUND THE LAST TWO ROWS OF FLOOR PROXIMITY EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE SUSPECTS A BRO KEN WIRE BUT WAS UNABLE TO LOCATE IT. AIRCRAFT WAS MAINTENANCE FERRIED TO PIT FOR REPAIRS. MAINTENANCE FOUND THE FUSE IN THE AFT EMERGENCY LIGHT BATTERY PACK BLOWN. REMOVED AND REPLACED FUSE. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007022300307 20070223 00307 NM 2007 2 23 USAA070125 1 20070222 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 BS 294.5 STR 7L CRACKED. FAB'D NEW PART & INSTALLED PER DRAWING 65-17684, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007022300308 20070223 00308 NM 2007 2 23 USAA070124 1 20070222 A 5320 STIFFENER BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 277 S2L AND S3L CRACKED. REMOVED OLD PART & FAB'D NEW, DRILLED, TREATED & PRIMED PER SRM 51-10-02, BOEING DWG 65-49 806, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007022300311 20070223 00311 NM 2007 2 23 USAA070121 1 20070222 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 867-947 AT S26R, UPPER & LOWER SURFACE OF TRANSITION ANGLE HAS CORROSION. FOUND CRACK & REPAIRED PER T/P, TREATED, PRIMED & REINSTALLED TRANSITION ANGLE PER SRM 51-60-53, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007022300312 20070223 00312 NM 2007 2 23 USAA070120 1 20070222 A 5320 STRAP BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 839-853 2 S26R BENEATH UPPER FLANGE OF WEB HAS CORROSION. FABRICATED NEW PART PER DWG 69-43456; CORR TASK C53-208-0 1; LEVEL 2, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007022300313 20070223 00313 NM 2007 2 23 USAA070119 1 20070222 A 5320 PAN BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 AFT WET AREA FLOOR PAN A BASE OF PRESS BULKHEAD HAS CORROSION. REMOVED DAMAGED AREA & FABRICATED DOUBLER & INSTALLED PE R SRM 51-70-13, DEFECT SIZE: 10 INCHES. 2 L 7 2 4F RT A16WE 2007022300314 20070223 00314 NM 2007 2 23 USAA070118 1 20070222 A 5754 65C26602258A WEDGE BOEING 737 737401 1384701 NM L/E SLAT DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 NR 5 SLAT ON O/B END OF WEDGE DISBONDED. REPAIRED DISBOND AREA & INSTALLED EXTERNAL DOUBLER PER SRM 51-70-10, DEFECT SI ZE: .5 X .75 INCH. 2 L 7 2 4F RT A16WE 2007022300316 20070223 00316 EU 2007 2 23 USAA070116 1 20070222 A 5315 D53111460202 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 163US 1417 FLOORBEAM Y-254 FR 17-19 HAS CORROSION. REMOVED AND REPLACED BEAM PER SRM 53-00-14; CORR TASK JA-220-53500; LEVEL 1, DE FECT SIZE: .5 X 4 INCHES. 2 L 7 2 4F RT A28NM 2007022300317 20070223 00317 EU 2007 2 23 USAA070115 1 20070222 A 5315 D53111460202 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 163US 1417 Y254 AT FRAME 16 HAS CORROSION. REMOVED AND REPLACED BEAM PER SRM 53-00-14; CORR TASK JA-220-53500; LEVEL 1, DEFECT SIZ E: 5 X 5 INCHES. 2 L 7 2 4F RT A28NM 2007022300318 20070223 00318 EU 2007 2 23 USAA070114 1 20070222 A 5315 D5347208900400 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 163US 1417 RIGHT FLOORBEAM TOP FLANGE FROM FR 64-69, -Y1160-1292 HAS CORROSION. REMOVED AND REPLACED 3 FLOORBEAMS PER SRM 51-72-11 ; CORR TASK JA-260-53500, LEVEL 1, DEFECT SIZE: 4 SQ INCHES. 2 L 7 2 4F RT A28NM 2007022300320 20070223 00320 EU 2007 2 23 USAA070112 1 20070222 A 5315 D5347218820400 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 163US 1417 LEFT FLOORBEAM ON TOP FLANGE FROM FR 65-69 AT Y1160 - 1292 HAS CORROSION. REMOVED AND REPLACED 3 FLOORBEAMS PER DWG D53 472815, SRM 51-74-12; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 8 INCHES SQ. 2 L 7 2 4F RT A28NM 2007022300321 20070223 00321 NM 2007 2 23 WRNA200700005 1 20070104 A 5412 STRUCTURE BOEING 747 747212B 1384886 NM NR 4 PYLON WORN A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING B-CHECK, FOUND NR 4 PYLON BULKHEAD STA 221.9 WORN FROM CONTACT WITH HYDRAULIC LINE AT INSIDE TOP AFT PIGEON HOLE. REPAIRED IAW BOEING 747 SRM 54-14-03 FIG 16. 2 L 7 4 4F A20WE 2007022300322 20070223 00322 NM 2007 2 23 WRNA200700006 1 20070103 A 5411 FRAME BOEING 747 747212B 1384886 NM NR 1 PYLON CRACKED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING B-CHECK, FOUND NR 1 PYLON FRAME STA 250 CRACKED AT INSIDE BOTTOM AFT PIGEON HOLE. REPAIRED IAW BOEING 747 SRM 54 -14-03 FIG 1. 2 L 7 4 4F A20WE 2007022300323 20070223 00323 NM 2007 2 23 WRNA200700011 1 20070212 A 5320 ATTACH ANGLE BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, FOUND FLOOR ATTACH ANGLE FOR L-1 DOOR FRAME CRACKED, STA 441. REPLACED ANGLE PER 747 SRM 51-30-02 2 L 7 4 4F A20WE 2007022300324 20070223 00324 EU 2007 2 23 WRNA200600042 1 20070112 A 2730 A2737460520000 ROD END GENELC AIRBUS 300 A300B4203 3930306 EU RT ELEVATOR BROKEN A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 506TA 207 DURING HEAVY MAINTENANCE WHILE PERFORMING SB A300-27-189, ROD END ON RIGHT ELEVATOR BLUE SYSTEM SERVO SPRING ROD ASSEMBL Y, WAS FOUND BROKEN. 2 L 7 2 4F RT A35EU 2007022300326 20070223 00326 NM 2007 2 23 WRNA200700003 1 20070113 A 5340 STRINGER CLIP BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT STA 1540, STR 23R. 2 L 7 4 4F A20WE 2007022300327 20070223 00327 NM 2007 2 23 DL76S070143 1 20070220 A 5753 FLAP TRACK BOEING 767 767332 1382001 NM WING DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 129DL 24079 DAMAGE FOUND ON ATTACH HOLES FOR RT I/B FLAP O/B TRACK. REPAIRED DAMAGE PER ERA 089397-14MA. C/W STEP 13 TO SUBMIT MRR PER SAME ERA. 2 L 7 2 4F RT A1NM 2007022300328 20070223 00328 NM 2007 2 23 DLM88070144 1 20070219 A 5512 5922578515 SKIN DOUG MD88 MD88 3023688 NM HORIZONTAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 HORIZONTAL STAB RT UPPER AFT SKIN, INBD AFT EDGE HAS CRACK REPAIR. THE UPPER AFT SKIN OF THE RT HORIZONTAL STAB WAS FOU ND WITH A 1.25" CRACK AT THE INBD, AFT EDGE OF THE PANEL. THE CRACK WAS HFEC INSPECTED AND STOP DRILLED ON A TIME-LIMIT ED BASIS. THE PERMANENT REPAIR IS A REPLACEMENT OF THE SKIN PANEL. THE REPAIR WAS ACCOMPLISHED PER ER/A 460229-14. 2 L 7 2 4F RT A6WE 2007022300329 20070223 00329 NM 2007 2 23 07FDEA00507 1 20070216 A 5713 STRINGER DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 DURING HFEC INSPECTION, CRACK FOUND AT STRINGER 10 (XORS 760) IN LEFT TANK. REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022600001 20070226 00001 WP 2007 2 26 DHL2007802521 1 20070203 A 5753 VANE DOUG DC8 DC873 302199C WP TE FLAP MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 802DH 86868 46076 LT OTBD SLOT VANE HAS A NON STANDARD REPAIR, STA XS 512.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-31-07, DWG AC62-57-108 REV IR DATED 01-23-07. REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-3-0 . CUT OUT DAMAGED SECTION IAW DWG AC62-57-108 REV IR DATED 01-23-07. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01- 001. NO CRACK OR CORROSION FOUND. ENCLOSED SMN FORM 242-2. FABRICATED EXT REPAIR DOUBLER INTERNAL DOUBLER AND FILLER IAW DWG NR AC62-57-108. CLEANED, TREATED AND PRIMED AREA, FILLER, INTERNAL DOUBLER AND INNER FACE OF EXT REPAIR DOUBLER IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW DWG NR AC62-57-108, S 2 L 7 4 4F RT 4A25 2007022600002 20070226 00002 WP 2007 2 26 DHL2007802526 1 20070202 A 5753 VANE DOUG DC8 DC873 302199C WP TE FLAP MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 802DH 86868 46076 RT OTBD SLOT VANE HAS A NON STANDARD REPAIR, STA XS 512.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-31-07, DWG NR AC62-57-104 REV A DATED 01-31-07. REMOVED NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-3-0, SRM 5 1-1-20D. CUT OUT DAMAGED SECTION IAW DWG AC62-57-104 AND PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. N O CRACK OR CORROSION FOUND. ENCLOSED SMN FORM 242-2. FABRICATED (1EA) SPLICE DOUBLER (AL7075T6 0.071") INTERNAL DOUBLE R (AL7075T6 0.050") AND 1 EA PLATING SEGMENT (AL7075T6 0.063") IAW DWG NR AC62-57-104. CLEANED, TREATED AND PRIMED AREA , SPLICE DOUBLER, INTERNAL DOUBLER AND PLATING SEGMENT INNER FACE IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW 2 L 7 4 4F RT 4A25 2007022600003 20070226 00003 WP 2007 2 26 DHL2007802528 1 20070203 A 5753 VANE DOUG DC8 DC873 302199C WP TE FLAP MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 802DH 86868 46076 RT OTBD SLOT VANE HAS A NON STANDARD REPAIR STA XOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-30-07, DWG NR AC62-57-106 REV IR DATED 01-22-07. REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51- 3-0. CUT OUT DAMAGED SECTION IAW DWG NR AC62-57-106. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. NO C RACK OR CORROSION FOUND. ENCLOSED SMN FORM 242-2. FABRICATED EXT REPAIR DOUBLER (AL7075T6 0.071") INTERNAL DOUBLER (AL 7075T6 0.050") AND FILLER (AL7075T6 0.063") IAW DWG# AC62-57-106. CLEANED, TREATED AND PRIMED AREA, FILLER, INTERNAL DO UBLER AND INNER FACE OF EXT REPAIR DOUBLER IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-11. INSTALL 2 L 7 4 4F RT 4A25 2007022600005 20070226 00005 EA 2007 2 26 A6WA200740050 1 20070201 A 2120 350023000 CHECK VALVE CNDAIR CL600 CL6002B19 1900309 EA RAM AIR MALFUNCTIONED A A6WA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 31 419AW 7633 AFTER TAKEOFF, HAD RIGHT PACK OVERTEMP MESSAGE AND SMOKE FROM AIR CONDITIONING VENTS. TURNED RIGHT PACK OFF AND SMOKE C LEARED. REMOVED AND REPLACED RAM AIR CHECK VALVE. INSPECTED RIGHT PACK, FOUND BLOWN GASKET ON PLATE ABOVE OIL SIGHT GA UGE, REF 148439/4. (M) 2 L 7 2 4F RT A21EA 2007022600006 20070226 00006 SO 2007 2 26 GLBA2006901 1 20070214 A 2497 TERMINAL EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE RCCB LOOSE A GLBA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 03 96ZK 120096 UNSCHEDULED LANDING, FLIGHT 5045, SECOND FLIGHT, PILOTS REPORTED SMOKE IN THE COCKPIT. MAINTENCE INSPECTED RELAY PANELS ON THE RT AND LT SIDES. MAINTENANCE FOUND LOOSE TERMINAL ON REMOTE CONTROL CIRCUIT BREAKER 0265. MAINTENANCE SECURED RC CB TERMINAL IAW MM 24-52-05 AND SECURED APU TEST PROBE POINT AT RT APU RELAY BOX. REFERENCE GMM VOL 6 9.1.0. SUBSEQUENT OPERATIONAL CHECK FLIGHT SATISFACTORY. NO ODOR/SMOKE NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 2007022600009 20070226 00009 CE 2007 2 26 GLBA20060907 1 20070219 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 352 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 202UX UE202 UPON ROUTINE INSPECTION- MAINTENANCE FOUND A CRACK APPROXIMATELY 7.750 INCHES LONG AT APPROXIMATELY FS 352, APPROXIMATEL Y 27.5 INCHES LT OF THE BELLY CENTERLINE. MAINTENANCE REPAIRED THE AFFECTED AREA IAW SRM 51-70 FROM FS 298 TO 305.75. PA TCH DIMENSION 14 INCH BY 6 INCH. 2 L 7 2 4T 4 T RT A24CE E26NE 2007022600010 20070226 00010 CE 2007 2 26 GLBA20060902 1 20070214 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CABIN ODOR A GLBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 211GL UE211 UNSCHEDULED LANDING DURING TRAINING, GLA FLIGHT 41. PILOTS REPORTED THAT THE AIRCRAFT HAD JUST BEEN FUELED AND AFTER TAK EOFF A STRONG FUEL ODOR WAS PRESENT. MAINTENANCE INSPECTED THE WINGS AND FUSELAGE FOR LEAKS, AIRED OUT CABIN AND PERFORM ED ENVIRONMENTAL CHECKS. NO LEAKS NOTED PER BMM 28-10. MAINTENANCE CLEANED BOTH EPA CAN CHECK VALVES AND FILTERS FOR PRE CAUTIONARY REASONS PER BMM 71-70. ENGINE RUNS WERE PERFORMED WITH NO LEAKS NOTED AND ODORS WERE NOT PRESENT. 2 L 7 2 4T 4 T RT A24CE E26NE 2007022600011 20070226 00011 CE 2007 2 26 021407N605CS1 1 20070214 A 3230 LANDING GEAR CESSNA 680 680CE 2076811 CE RT MAIN MALFUNCTIONED E Z5FA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NE 03 605CS 6800001 UPON APPROACH, AFTER SELECTING GEAR EXTEND, THE RT MAIN GEAR DOWN INDICATION FAILED TO ILLUMINATE AND THE GEAR UNLOCK LI GHT REMAINED ILLUMINATED. CREW EXECUTED A GO AROUND AND FOLLOWED AFM GEAR EXTEND EMERGENCY PROCEDURES. THE MANUAL MAIN G EAR RELEASE WAS PULLED AND GEAR WAS BLOWN DOWN WITH EMERGENCY GEAR BOTTLE. THE GEAR UNLOCK AND RT MAIN GREEN LIGHT WERE NOT AFFECTED BY THIS ACTION. AFTER A SHORT TIME, THE RT MAIN GEAR GREEN DOWN LIGHT DID ILLUMINATE AND THE UNLOCK LIGHT E XTINGUISHED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT IS IN MAINTENANCE AT THIS TIME. 2 L 7 2 4F RC T00012WI 2007022600015 20070226 00015 SO 2007 2 26 ECI10516 1 20070216 A 2752 1159SC21216 ACTUATOR GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6108 NE TE FLAPS ERRATIC E E0XA O OTHER O OTHER NR NOT REPORTED 1 SO 35 919CT 1051 FLAPS WILL NOT EXTEND BEYOND 0 DEGREES. REMOVED AND REPLACED IB FLAP ACTUATORS. 2 L 7 2 4F 4 F RT A12EA E25NE 2007022600016 20070226 00016 2007 2 26 UG8A2007GM02O 4 20070212 A 3120 50118600102 DISPLAY GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU INSTRUMENT PANEL INOPERATIVE E UG8A G O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 23 5113 790 4013 ON APPROACH, EADI SCREEN FAILED AND THEN EMITTED A SLIGHT AMOUNT OF SMOKE. DONNED O2 MASKS AS PRECAUTION. AIRCRAFT LAN DED WITHOUT INCIDENT. REMOVED AND REPLACED STANDBY FLIGHT DISPLAY. PERFORMED ALL OPS AND LEAK CHECKS IAW AMM 34-13-00 AND CMP CODES 342710 AND 342005. STOWED O2 MASKS IAW AMM 35-11-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A12EA E25NE 2007022600018 20070226 00018 CE 2007 2 26 GUUA02170702 1 20070217 A 3230 571302 MOTOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG FAILED A GUUA O OTHER J WARNING INDICATION CL CLIMB 1 SO 29 81546 UE187 AFTER TAKEOFF LANDING GEAR CIRCUIT BREAKER POPPED GEAR UNSAFE LIGHT ILLUMINATED NOSE GEAR RETRACTED BUT BOTH MAIN GEARS STAYED DOWN. CONTINUED, MANUALLY EXTENDED NOSE GEAR LANDED WITHOUT INCIDENT. REPLACED THE LANDING GEAR DC MOTOR OPERATI ONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007022600019 20070226 00019 SO 2007 2 26 GUUA02170703 1 20070217 A 3350 D36604011 POWERPACK EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE EMERGENCY LIGHTS DISCHARGED A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 29 268AS 120202 EMERGENCY LIGHTS WILL NOT STAY ON PAST ONE MINUTE. REPLACED FORWARD EMERGENCY LIGHT POWER PACK OPERATIONAL CHECK NORMAL . 2 L 7 2 4T 4 T RT A31SO E20NE 2007022600021 20070226 00021 NM 2007 2 26 SWAA071067 1 20070221 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 360 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022600022 20070226 00022 NM 2007 2 26 SWAA071068 1 20070221 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 360 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022600024 20070226 00024 NM 2007 2 26 SWAA071052 1 20070221 A 2612 7C14 CLAMP BOEING 737 7377H4 1384404 NM WW FIRE LOOP LOOSE A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 29 240WN 32503 DIVERSION, WHEEL WELL OVERHEAT LIGHT ILLUMINATED AND ALARM BELL SOUNDED AT FL 380. LOWERED LANDING GEAR PER QRH. INSPE CTED WHEEL WELL NO EVIDENCE OF FIRE, INSPECTED W/W FIRE LOOP, FOUND THREE CLAMPS LOOSE. SECURED CLAMPS PER MM. 2 L 7 2 4F RT A16WE 2007022600026 20070226 00026 2007 2 26 SWAA071061 4 20070221 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007022600027 20070226 00027 NM 2007 2 26 SWAA071069 1 20070221 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 754SW 29849 DURING SCHEDULED HC2 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007022600029 20070226 00029 NM 2007 2 26 AWXA200700245 1 20070221 A 5610 141T480149 WINDSHIELD BOEING 757 7572G7 1384963 NM COCKPIT ARCED A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 909AW 5870 5838 24522 FLIGHT 432: PHX - OGG - ATB - PRIOR TO REACHING THE COAST, THE CREW NOTICED AN ELECTRICAL SMELL IN THE FLIGHT STATION. THE CREW SHUT DOWN THE LEFT PACK AND THE SMELL WENT AWAY. BASED ON THE REQUIREMENTS TO HAVE BOTH PACKS OPERATING FOR ET OPS OPERATION, THE CREW RETURNED TO PHX. NO EMERGENCY DECLARED. THE LANDING WAS UNEVENTFUL. MX NOTICED THE CAPTAINS W INDSHIELD SHOWED SIGNS OF ARCHING, MX REMOVED AND REPLACED THE CAPTAINS WINDSHIELD, OPS/LEAK CHECK WAS GOOD. THE A/C W AS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007022600149 20070226 00149 NM 2007 2 26 NOCA01907 1 20070121 A 2612 FIRE DETECTOR BOEING 767 767324 1385203 NM NR 1 NACELLE DIRTY A NOCA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 15 767NA 27569 LEFT ENG FIRE LOOP NR 1 ON STATUS. CLEANED LOWER FWD FIRE DET TS683, OPS CHECK FIRE WARNING PER MM 26-11-00. OPS CHECK OK. 2 L 7 2 4F RT A1NM 2007022600032 20070226 00032 EA 2007 2 26 A6WA200740040 1 20070131 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG UNKNOWN A A6WA O OTHER J WARNING INDICATION CL CLIMB 1 GL 31 423AW 8836 7636 NOSE GEAR DISAGREE ILLUMINATED ON GEAR RETRACTION. FOLLOWED QRH, PUT GEAR DOWN, MESSAGE CLEARED. REMOVED AND REPLACED NOSE LANDING GEAR SELECTOR VALVE PER AMM 32-22-02, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007030100127 20070301 00127 NM 2007 3 1 UIEA200700089 1 20070225 A 5320 WEB BOEING 747 7472D3B 1384805 NM BS 1350 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 FOUND LT WLG BS 1350 HORIZONTAL WEB UPPER SURFACE FOUND CORROSION. CORROSION REMOVED AND AREA PROTECTED AS PER SRM 51-1 0-01 AND 51-10-02. 2 L 7 4 4F RT A20WE 2007030100136 20070301 00136 NM 2007 3 1 UIEA200700079 1 20070216 A 5280 65B1091685 DOOR BOEING 747 74747UF 1384949 NM MLG DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 418MC 32840 ON WAC, FOUND BOTH LEFT HAND AND RIGHT BODY GEAR SHOCK STRUT DOORS WITH IMPACT DAMAGE. LEFT AND RIGHT SHOCK STRUT DOORS REMOVED IAW TASK 32-14-05-004-001, DOORS LOADED IN A/C HOLD. A/C CLEARED FOR FERRY FLIGHT FROM AKL-SYD PER SPECIAL FLI GHT PERMIT AND CDL 32-14-1, RESTRICTED GEAR DISPATCH SWITCH SELECTED TO GEAR DOWN DISPATCH, DMI M07-015. SERVICEABLE BO DY GEAR SHOCK STRUT DOORS INSTALLED AS PER AMM 32-14-05. 2 L 7 4 4F RT 1384945 2007030100137 20070301 00137 NM 2007 3 1 UIEA200700074 1 20070220 A 5730 65B1448623 SKIN BOEING 747 7472D3B 1384805 NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 LEFT WING LEADING EDGE BULLNOSE FOUND CORROSION OUTBOARD OF LANDING LIGHT. PERMANENT REPAIRED ACCOMPLISHED AS PER BOEIN G MESSAGE 1-286780848-2 DATED 13 FEB,2007 AND EO NR 4757A281. 2 L 7 4 4F RT A20WE 2007030100150 20070301 00150 2007 3 1 070041 4 20070216 A 2220 DISPLAY DOUG DC9 DC982 3022082 WP COCKPIT UNKNOWN A WX0A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 19 887GA 49932 FLIGHT 715 SFB/LAN - THE FLIGHT CREW REPORTED; DURING TAKEOFF ROLL "F/S FAIL" INTERMITTENTLY APPEARED ON BOTH PRIMARY FL IGHT DISPLAYS. REJECTED TAKEOFF AT 100 KTS. UPON CLEARING THE RUNWAY THE SYSTEM INDICATION RETURNED TO NORMAL. SFB MA INTENANCE REPORT THAT DFGC NR 2 FAILED A RETURN-TO-SERVICE TEST. THEY PERFORMED A LOGIC RESET ON DFGC NR 2 AND THE SYST EM PASSED THE RETURN-TO-SERVICE TEST. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007030100152 20070301 00152 NM 2007 3 1 AWXA200700283 1 20070223 A 5711 654532421 SPAR BOEING 737 73733A 1384673 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND LEFT WING SPAR CHORD CRACKED, WBL 157, UNDER AFT OUTBOARD GEAR BEAM SUPPORT FITTING. REPAIRED LEFT WING SPA R CHORD, WBL 157, UNDER AFT OUTBOARD GEAR BEAM SUPPORT FITTING IAW AWA ER 03-5700-07052-SS4. 2 L 7 2 4F RT A16WE 2007030100154 20070301 00154 NM 2007 3 1 AWXA200700285 1 20070222 A 5743 65494913 FITTING BOEING 737 73733A 1384673 NM ZONE 600 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND RIGHT WING OUTBOARD RIGHT MAIN LANDING GEAR SUPPORT BEAM FITTING CRACKED, WBL 157. REPAIRED RIGHT WING OUTB OARD RIGHT MAIN LANDING GEAR SUPPORT BEAM FITTING CRACKED, WBL 157 IAW AWA ER 03-5700-07052-SS4. 2 L 7 2 4F RT A16WE 2007030100161 20070301 00161 NM 2007 3 1 AWXA200700292 1 20070124 A 5311 6546541 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED FRAME WEB, BS 663.75, S2R. REPAIRED FRAME WEB, BS 663.75, S2R IAW AWA ER 03-5362-07052-SS6. 2 L 7 2 4F RT A16WE 2007030100163 20070301 00163 NM 2007 3 1 AWXA200700294 1 20070129 A 5311 65479602 FRAME BOEING 737 73733A 1384673 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CORROSION ON AFT CARGO COMPARTMENT FRAME, BS 847, S25R - S26R. REPAIRED AFT CARGO COMPARTMENT FRAME, BS 847 , S25R - S26R IAW AWA ER 03-5300-07054-HF6. 2 L 7 2 4F RT A16WE 2007030100175 20070301 00175 NM 2007 3 1 USAA070134 1 20070226 A 5414 SKIN BOEING 737 737401 1384701 NM RT PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 AT PANEL (5827) OPENING FLANGE ON TOP OF RT PYLON INBOARD SIDE, STA 212.84 HAS CRACK. STOP DRILL CRACK, FAB'D SKIN DOUB LER & INSTALLED PER TYP REPAIR 54-30-07, DEFECT SIZE: .025 INCH. 2 L 7 2 4F RT A16WE 2007030100182 20070301 00182 NM 2007 3 1 USAA070127 1 20070226 A 5754 1145410532 SKIN BOEING 737 737201 1384454 NM L/E SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246AY 23898 NR 8 SLAT, WEDGE UPPER SURFACE OSS 319.71-324.71 DELAMINATED. CUT OUT DELAMINATED SKIN, BONDED REPAIR DOUBLER PER SRM 5 1-70-10, PARA 20, DEFECT SIZE: 1 INCH DIA. 2 L 7 2 4F A16WE 2007030100183 20070301 00183 NM 2007 3 1 WRNA200700004 1 20070209 A 5755 ATTACH FITTING BOEING 747 747212B 1384886 NM NR 5 SPOILER BROKEN A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, FOUND NR 5 SPOILER CENTER ATTACH FITTING BROKEN AFT OF WS 680 IN FLAP WELL. 2 L 7 4 4F A20WE 2007030100189 20070301 00189 NM 2007 3 1 WRNA200700009 1 20070212 A 5320 65B0966113 SHEAR WEB BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, FOUND A 1 INCH CRACK IN SHEAR WEB BETWEEN S-10A AND S10 LEFT SIDE BS 820, WL 330, LBL 80. REPLACED SHEA R WEB IAW B747 SRM 51-30-02 AND DRAWING 65B9661. 2 L 7 4 4F A20WE 2007030100214 20070301 00214 SO 2007 3 1 SIMA200705701 1 20070221 A 5542 12020808509 SKIN EMB EMB 135 EMB135LR 3260305 SO ZONE 300 CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 709GB 15825 4800 145211 RUDDER 1 LEADING EDGE FOUND TO BE CHAFED ON LOWER LEFT SIDE. CUT OUT DAMAGE. FABRICATED REPAIR FILLER AND DOUBLER. IN STALLED REPAIR PIECES AND RESTORED SURFACE FINISH IAW EMB IC2007-145/00812. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007030100221 20070301 00221 SO 2007 3 1 SIMA200705710 1 20070223 A 3350 20131A BATTERY PACK EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS FAILED A SIMA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SW 21 610AE 12256 9496 145073 FOUND EMERGENCY LIGHTS AT ROW 3BC, ROW 12 CEILING AND ROWS 12 THROUGH 18 FLOOR LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK ABOVE ROW 15 IAW EMB AMM 33-50-30. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007030100239 20070301 00239 NM 2007 3 1 QXEA200700254 1 20070223 A 5210 85217008101 SEAL BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR TORN A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 410QX 4053 PDX FLIGHT NR 2352: FLIGHT WAS DIVERTED TO PDX. AIRCRAFT WOULD NOT PRESSURIZE IN AUTO OR MANUAL MODE. FA REPORTS LOUD NOISE COMING FROM MCD. MAINTENANCE FOUND MCD SEAL TORN. REPLACED MCD SEAL PER Q400 AMM 52-11-31-000-801 AND 52-11-31-4 00-801 AND GREEN SHEET QX44. PRESSURIZED AIRCRAFT PER 21-00-00-863-801. TESTS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030100244 20070301 00244 WP 2007 3 1 07FDEA00574 1 20070226 A 5712 RIB DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 RT WING L/E INT SIDE FOUND 1 CRACK ON RIB AT STA XORS 562. REPAIRED RIB IAW SRM 57-20-00 PAG 3 FIG 1 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER I035577-3/N00577-3. REPAIR ANGLE IAW SRM 57-20-00 FIG 1 VOL 1. 2 L 7 3 4F A22WE 2007030100245 20070301 00245 WP 2007 3 1 07FDEA00575 1 20070226 A 5730 SKIN DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 RT WING L/E EXT FOUND 1 CRACK 1.50" LONG ON SKIN AT STA XORS 506. REMOVED REFUELING DOOR IAW MM 20-50-02-2 AND DWG ARB1 067. REMOVED PLATE SP10240168 IAW SRM 51-31-01 VOL 2 PAR 6. REMOVED EXISTING DOUBLER AND INSTALLED A NEW ONE IAW SRM 5 7-10-00 VOL 1 FIG 68. REINSTALLED PLATE IAW SRM 51-31-01 VOL 2 PAR 6. REINSTALLED REFUELING DOOR IAW MM 20-50-02-2 AND DWG ARB1067. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N00580 AND IAW SRM 57-10-00 FIG 68 VOL 1. 2 L 7 3 4F A22WE 2007030100248 20070301 00248 EU 2007 3 1 MALA070031 1 20070221 A 3350 HOUSING SAAB SF340 340B 7860101 EU EMERGENCY LIGHT CRACKED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 439XJ 340B439 EMERGENCY LIGHT ABOVE SEAT 10A INOP, UPON BULB REPLACEMENT FOUND BULB HOUSING CRACKED MAKING IT IMPOSSIBLE TO REPLACE TH E BULB. REMOVED AND REPLACED AFT OVERHEAD EMERGENCY LIGHT HOUSING, P/N 2LA005115-20 IAW SAAB AMM 33-50-55-990-801-1. 2 L 7 2 4T RT A52EU 2007030100253 20070301 00253 EA 2007 3 1 QXEA200700249 1 20070214 A 5610 601R3303311 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A QXEA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 09 290RB 3209 10029 EUG - FLIGHT 2558 (BUR-EUG) - DURING CRUISE AT 36,000 FEET CAPTAIN'S SIDE WINDOW STARTED TO CRACK. COMPLETED EMERGENCY CHECKLIST AND DIVERTED TO EUGENE AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE SIDE WINDOW. OPERATIO NAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007030200003 20070302 00003 NM 2007 3 2 SWAA071109 1 20070226 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 467WN 33830 FWD CABIN EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007030200010 20070302 00010 NM 2007 3 2 EIA2007003 1 20070109 A 3350 RPS1B SIGN BOEING 747 747212B 1384886 NM EMERGENCY LIGHTS INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482EV 20713 FOUND DOOR 5R AND 5L EXIT IDENTIFIER SIGNS INOP. REMOVED AND REPLACED POWER SUPPLY IAW MM 33-51-00 PG 9, OPS CHECKED GO OD. 2 L 7 4 4F A20WE 2007030200025 20070302 00025 NM 2007 3 2 EIA2007016 1 20070215 A 5310 65B04699601 BEAM BOEING 747 747273C 1384896 NM DOOR FRAME CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 FOUND FORWARD CARGO DOOR INTERNAL LOWER, CLOSE OUT BEAM, CORROSION AT SCREW HOLES FROM STA 567 TO STA 662. CORRODED BEA M WEB REPLACED AND INSTALLED FASTENERS WITH EDGE MARGINS WERE REPAIRED AS PER BOEING MSG 1-273529392-12 AND FAA 8100-9 D ATED 13 FEB 07. 2 L 7 4 4F A20WE 2007030500004 20070305 00004 2007 3 5 NOCA02407 4 20070126 A 2215 163000108 SERVO BOEING 757 75728A 1384976 NM AUTOPILOT SYS LEAKING A NOCA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 15 750NA 26277 HYD LEAK COMING FROM LATERAL A/P SERVO CENTER POSITION IN LEFT W/W AREA. REMOVED AND REPLACED CENTER A/P LATERAL SERVO AS PER MM 22-13-03-4. OPS CHECK AND LEAK CHECKS OK. 2 L 7 2 4F RT A2NM 2007030500007 20070305 00007 NM 2007 3 5 NOCA02707 1 20070130 A 2611 G1382AS10 LAMP BOEING 767 76739H 1385311 NM SMOKE DETECTOR INOPERATIVE A NOCA K NONE N FALSE WARNING UK UNKNOWN 1 EA 15 760NA 26257 AFT CARGO DET 1 EICAS STATUS MSG. RELAMPED DET 1, AFT CARGO BIN PER AMM 26-16-01. OPS CHKS NORMAL. 2 L 7 2 4F RT A1NM 2007030500015 20070305 00015 NM 2007 3 5 NOCA03607 1 20070207 A 3350 767 CONTACT BOEING 767 767300 1385204 NM EXTERIOR LIGHT DIRTY A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 768NA 29898 FOUND EXTERIOR EMERGENY LIGHT AT L3 DOOR INOP. CLEANED CONTACTS AND RELAMPED PER AMM 33-51-00. OPS CHECKS OK. 2 L 7 2 4F RT A1NM 2007030500053 20070305 00053 EA 2007 3 5 TRAX200700261 1 20070220 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 FOUND RT CABIN FLOOR SEAT TRACK CORRODED AT FS 544. 2 L 7 2 4F RT A21EA 2007030500058 20070305 00058 EA 2007 3 5 TRAX200700266 1 20070220 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 FOUND 349 FRAME CORRODED AT LBL45. 2 L 7 2 4F RT A21EA 2007030500063 20070305 00063 EU 2007 3 5 TRAX200700271 1 20070220 A 2750 WARNING SYSTEM AEROSP ATR72 ATR72212 8680945 EU COCKPIT ACTIVATED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 634AS 370 DURING APPROACH AT APPROX 400 W/FLAPS 30 DEG, RECEIVED "FLAP UNLOCK". EXECUTED MISSED APPROACH. RAN QRH. EXECUTED NO F LAP LANDING, EMERGENCY DECLARED. 2 H 7 2 4T RT A53EU 2007030500069 20070305 00069 EA 2007 3 5 TRAX200700253 1 20070220 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 FOUND CORROSION ON FRAME 280 LT SIDE PRESSURE BULKHEAD. REPAIRED IAW REO 601R-53-11-926. 2 L 7 2 4F RT A21EA 2007030500079 20070305 00079 NM 2007 3 5 AWXA200700303 1 20070201 A 5320 69482042 ATTACH ANGLE BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED FRAME VERTICAL ATTACH ANGLE, BS 360, S14L - S15L. REPLACED FRAME VERTICAL ATTACH ANGLE, BS 360, S14 L - S15L IAW AWA ER 03-5312-07054-HF4. 2 L 7 2 4F RT A16WE 2007030500085 20070305 00085 NM 2007 3 5 AWXA200700271 1 20070216 A 5340 6935352 STRINGER CLIP BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND CRACKED STRINGER CLIP, BS 639, S4L. REPLACED STRINGER CLIP, BS 639, S4L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007030500088 20070305 00088 NM 2007 3 5 AWXA200700274 1 20070202 A 5320 65C2782165 ATTACH ANGLE BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED ATTACH ANGLE, BS 663, S8L - S9L. REPLACED ATTACH ANGLE, BS 663, S8L - S9L IAW B737-300 SRM -51-40-0 2. 2 L 7 2 4F RT A16WE 2007030500093 20070305 00093 EU 2007 3 5 AWXA200700237 1 20070215 A 5320 D5347218920400 BEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 652AW 953 SAL- MAJOR REPAIR - FOUND CORROSION ON MAIN CABIN LONGITUDINAL BEAM AT -Y1292, FR 68 - FR 69. REPLACED MAIN CABIN LONGI TUDINAL BEAM AT -Y1292, FR 68 - FR 69, IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007030500100 20070305 00100 NM 2007 3 5 AWXA200700308 1 20070131 A 5313 6561777503 STRINGER SPLICE BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED STRINGER SPLICE CHANNEL, BS 359, S14L. REPLACED STRINGER SPLICE CHANNEL, BS 359, S14L IAW AWA ER 03 -5312-07054-HF4. 2 L 7 2 4F RT A16WE 2007030500104 20070305 00104 NM 2007 3 5 AWXA200700312 1 20070131 A 5320 69489854 FITTING BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED INTERCOSTAL CLIP, BS 360, S10L. REPLACED INTERCOSTAL CLIP, BS 360, S10L IAW AWA ER 03-5312-0754-HF4 . 2 L 7 2 4F RT A16WE 2007030500106 20070305 00106 EU 2007 3 5 AWXA200700244 1 20070218 A 5311 D5347112320300 FRAME AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 652AW 953 SAL - FOUND CORROSION ON SUPPORT FRAME, FR 69 - FR 70, S-23R. REPLACED SUPPORT FRAME LOCATED ON , FR 69 - FR 70, S-23R, IAW A320 SRM 51-72-11, PAGE 1, 2 AND 51-42-11. 2 L 7 2 4F RT A28NM 2007030500112 20070305 00112 NM 2007 3 5 CALA0700105 1 20070227 A 3350 LIGHT BOEING 737 737824 13844BZ NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 36272 31590 EMERGENCY PATH LIGHTING INOP AT SEAT 8C. REPAIRED IAW AMM 33-51-01. 2 L 7 2 4F RT A16WE 2007030500132 20070305 00132 NM 2007 3 5 DHL2007781011 1 20070227 A 3230 651767321 FITTING BOEING 727 727227 1384078 NM NLG CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 781DH 21996 FOUND NLG DRAG BRACE FITTING HAS CORROSION ON BOTH DRAG BRACE ATTACH LUGS, IN LUG BORE'S AND ON LUG FACES. REMOVED CORR OSION IN LUG BORES; MATERIAL REMOVED FOUND OUT OF LIMITS PER B727 SRM 53-40-1 FIG 1. REMOVED AND REPLACED NLG DRAG BRA CE FITTING PER B727 SRM 51-30-5 AND 51-30-2. 2 L 7 3 4F A3WE 2007030500133 20070305 00133 NM 2007 3 5 DHL2007781013 1 20070227 A 5330 SKIN BOEING 727 727227 1384078 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 781DH 21996 FOUND SKIN AT BS 481, STR 28R, HAS CORROSION. FOUND CORROSION ON SKIN OUT OF LIMITS. CUT OUT DAMAGED SECTION OF SKIN, 9.75" BY 3". FABRICATED DOUBLER FROM 2024-T3, .100" BY 15.875" BY 10.375", PO NR 9003970; AND FILLER FROM 2024-T3, .090 " BY 9.75" BY 3.125", PO NR 9004085; PER B727 SRM 53-30-3 FIG 3A. TREATED, PRIMED, AND INSTALLED REPAIR PARTS PER B727 SRM 51-10-2 AND 53-30-3 FIG 3A. 2 L 7 3 4F A3WE 2007030500136 20070305 00136 WP 2007 3 5 DHL2007802530 1 20070206 A 5730 56110121 PANEL DOUG DC8 DC873 302199C WP LT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 LT WING T/E LWR PANEL DELAMINATED (STA XW 97.000 - XRS 162.000). REMOVED AND REPLACED LT WING T/E LWR PANEL IAW SRM 51- 3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007030500138 20070305 00138 WP 2007 3 5 DHL2007802532 1 20070205 A 5350 5653923505 FILLET DOUG DC8 DC873 302199C WP FUSELAGE DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 FOUND FUSELAGE LWR FILLET PANEL NR 732 DELAMINATED (STA 990.000 - 1050.000). REMOVED AND REPLACED LWR FILLET PANEL NR 7 32 IAW SRM 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007030500144 20070305 00144 WP 2007 3 5 DHL2007802538 1 20070206 A 5313 LONGERON DOUG DC8 DC873 302199C WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 AFT ACCY COMPT SHOWS CORROSION AT STA 1660.000 L-24L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-2 FIG 4A. REM OVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICATED NEW LONGERON SEGMENT (EXTRUSION P/N S2610338) IAW SRM 53-2-2 FIG 4A, SRM 53-4-1 FIG 44 SHEET 2 ITEM "C", SRM 51-2-0 FIG 50 SHEET 51 AND SPLICE (EXTRUSION P/N S2641454) IAW SRM 53-2-2 FIG 10 SHEET 4, T R NR 53-193 DATED 06-15-04, SRM 51-2-0 FIG 50 SHEET 62, SRM 53-2-2 FIG 10 SHEET 1, 3, TR NR 53-153 DATED 12-10-02. PERF ORMED NDT INSPECTION IAW DC8 SRM 53-2-2 FIG 10 SHEET 4 NOTE 22. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW S 2 L 7 4 4F RT 4A25 2007030500145 20070305 00145 WP 2007 3 5 DHL2007802539 1 20070213 A 5312 BULKHEAD DOUG DC8 DC873 302199C WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 FWD ACCY COMPT FWD PRESSURE BULKHEAD CAP SHOWS CORROSION AT STA 8.000 L-29R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-30-07, DWG NR ACG2-53-110 REV IR DATED 01-26-07. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-2 0D. CUT OUT DAMAGED SECTION IAW DWG NR ACG2-53-110. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK OR CORROSION FOUND AFTER CUT OUT. FABRICATED (2EA) REPAIR ANGLES (EXTRUSION 7075T6511 0.250"/0.125") AND NEW CAP SEGMENT (EXTRUSION S2616279 0.200"/0.188") AND STRAP (AL7075T6 0.125") IAW DWG NR ACF2-53-110. HEAT TREATED ANGLES FROM 7075T65 11 IAW SRM 51-1-1 PG 1, 13, 17. PERFORMED NDT INSP IAW DC8 NDT SPM PART 08-00-02 TO 07. NO CRACK OR CORROSION FOUND. 2 L 7 4 4F RT 4A25 2007030500153 20070305 00153 WP 2007 3 5 DHL2007802513 1 20070124 A 5753 ANGLE DOUG DC8 DC873 302199C WP T/E FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 LT OTBD FLAP "T" ANGLE CRACKED 1" STA XF 165.000. REMOVED CRACKED T ANGLE IAW SRM 51-1-21. FABRICATED NEW T-ANGLE (EXT RUSION P/N 1243286) IAW SRM 57-7-0 FIG 3, SRM 51-2-0 FIG 50. CLEANED, TREATED AND PRIMED AREA AND T-ANGLE IAW SRM 51-1- 8B. INSTALLED T-ANGLE IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007030500162 20070305 00162 NM 2007 3 5 EIA2007023 1 20070222 A 5753 SEAL BOEING 747 747273C 1384896 NM T/E FLAP ERODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 MANY FLAP MOLDING SEALS WERE FOUND ERODED AT DIFFERENT LOCATIONS. ERODED MOLDING SEAL WAS REPLACED, REPAIRED PER N471EV -07-0001. 2 L 7 4 4F A20WE 2007030500176 20070305 00176 NM 2007 3 5 QXEA200700276 1 20070213 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND RIGHT CARGO COMPARTMENT SEAT TRACK NR 9 HAS CORROSION ON THE TOP SURFACE OF THE FOOT LATCH SECTION AT STA TION X596. REPAIRED IAW RD8-53-4936, RD8-53-4472, AND SRM 51-40-00, 51-20-36. 2 H 7 2 4T RT A13NM 2007030500180 20070305 00180 NM 2007 3 5 QXEA200700275 1 20070208 A 5347 RIVET DHAV DHC8 DHC8202 2809007 NM SEAT TRACK CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND RIGHT FUSELAGE INTERIOR, AFT FRAME 355.95 OUTBOARD SEAT TRACK NR 10, SEVERAL RIVETS APPEAR TO HAVE CORROS ION. REPAIRED IAW SRM 51-20-11, 51-40-00, AND 51-20-16, 51-20-16. 2 H 7 2 4T RT A13NM 2007030500190 20070305 00190 NM 2007 3 5 QXEA200700283 1 20070213 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND RIGHT OUTBOARD SEAT TRACK NR 11 HAS CORROSION ON EDGES OF CLAWS AT STATION X455. REPAIRED IAW RD8-53-134 2. 2 H 7 2 4T RT A13NM 2007030500209 20070305 00209 NM 2007 3 5 CALA0700093 1 20070224 A 5314 65621257 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 AFT CARGO COMPARTMENT CORRODED AT KEEL BEAM STA 727, LBL 6. REPAIRED IAW ECRA 5311-01293 AND 5311-01296. 2 L 7 2 4F RT A16WE 2007030500210 20070305 00210 NM 2007 3 5 CALA0700094 1 20070224 A 5314 65621258 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 LOWER FUSE SKIN BULGED BETWEEN RIVETS ALONG STRINGER 28R STA 500C TO 500D. REPAIRED KEEL BEAM IAW SRM 53-60-12. 2 L 7 2 4F RT A16WE 2007030500211 20070305 00211 NM 2007 3 5 CALA0700095 1 20070224 A 5320 147A8540U7 STRUCTURE BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27239 28951 L1 CHORD CORRODED. REPAIRED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007030600003 20070306 00003 NM 2007 3 6 2007UALA00592 1 20070224 A 3397 WIRE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 811UA 847 EMERGENCY ESCAPE PATH LIGHTING INOP AT SEAT ROW LOCATIONS 6 & 7, 10, 13 & 14, 17 & 18 AND 21 & 22. [5-1-07] REPLACED W IRE TERMINATION OF WIRE HARNESS 350WL4 IN REF WITH ASM 33-51-00 PG103. ESCAPE PATH LIGHTING OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007030600007 20070306 00007 NM 2007 3 6 2007UALA00596 1 20070224 A 4970 WARNING SYSTEM BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE APU ACTIVATED A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 795UA 26927 STATUS MSG -APU-, BUT APU NEVER SHUT DOWN. REBOOTED ACFT, BUT NO HELP. AFTER TROUBLESHOOTING, DETERMINED THAT APU FIRE -OVERHEAT DETECTOR CARD WAS FAULTY. REPLACED CARD & APU OPERATED OK FOR SERVICE. SUSPECT DISTURBED CIRCUIT PATH ON CAR D. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007030600019 20070306 00019 2007 3 6 2007UALA00608 4 20070227 A 2565 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT ENTRY DOOR FRAYED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 AFT ENTRY DOOR EVACUATION SLIDE GIRT IS FRAYED & TORN. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007030600023 20070306 00023 NM 2007 3 6 2007UALA00612 1 20070227 A 5310 UNKNOWN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE VIBRATION A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 905UA 25005 WHILE DEPARTING FELT VIBRATION FOR APPROX FOUR MINUTES. F/A'S HEARD LOUD NOISE AROUND WING. DEBRIEFED CREW FLIGHT ATTE NDANTS FELT VIBRATION IN FLOOR MID AREA OVER WINGS MOSTLY ON LEFT SIDE THROUGHOUT FLIGHT. NOISE DECREASED WHILE DESCEND ING. 21 MARCH 07, SUPPLEMENTAL DATA UPDATE CAUSE: FOUND RIGHT GEAR STRUT DOOR NOT FAIRED. ADJUSTED DOOR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007030600024 20070306 00024 NM 2007 3 6 2007UALA00613 1 20070227 A 2612 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FIRE TEST PANEL INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 517UA 24861 FIRE-OVERHEAT TEST PANEL SYSTEM FAIL LIGHT NEEDS TO BE RELAMPED. [SUP 05-18-07] REPLACED KOREY LIGHT SWITCH FIRST WIT H INCANDESCENT LIGHT SWITCH, DETERMINED THAT BASE ASSEMBLY NEEDS TO BE REPLACED. REPLACED SW MODULE AND TESTS OK. LA TER INSTALLED WITH LED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030600030 20070306 00030 NM 2007 3 6 SWAA071144 1 20070227 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007030600042 20070306 00042 NM 2007 3 6 SWAA071136 1 20070227 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007030600044 20070306 00044 NM 2007 3 6 SWAA071135 1 20070227 A 5753 6546431279 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD FORE FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007030600047 20070306 00047 NM 2007 3 6 SWAA071123 1 20070226 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030600048 20070306 00048 NM 2007 3 6 SWAA071124 1 20070226 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030600049 20070306 00049 NM 2007 3 6 SWAA071115 1 20070226 A 3350 65C34691 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED SERVICE CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 20 DEF. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007030600051 20070306 00051 NM 2007 3 6 SWAA071169 1 20070301 A 5551 6551524 FITTING BOEING 737 7373H4 1384600 NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND LT AND RT HORIZONTAL STAB FITTING CLEVIS LUG FACES CORRODED. REPAIRED STAB FITTING PE R SRM. 2 L 7 2 4F RT A16WE 2007030600052 20070306 00052 NM 2007 3 6 SWAA071172 1 20070301 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 17L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030600053 20070306 00053 NM 2007 3 6 SWAA071151 1 20070228 A 5512 65C25727 SKIN BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STAB SKIN CRACKED AT LOWER SURFACE STA 120. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007030600057 20070306 00057 2007 3 6 SWAA071168 4 20070301 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007030600058 20070306 00058 2007 3 6 SWAA071150 4 20070228 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007030600059 20070306 00059 2007 3 6 SWAA071166 4 20070301 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 606SW 27926 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007030600060 20070306 00060 2007 3 6 SWAA071157 4 20070301 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007030600061 20070306 00061 NM 2007 3 6 SWAA071155 1 20070228 A 5523 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BEARING PER MM. 2 L 7 2 4F RT A16WE 2007030600064 20070306 00064 NM 2007 3 6 AMTA200700069 1 20070214 A 5320 STRIP BOEING 737 73783N 13844HI NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 323TZ 30033 CORROSION LT FLOOR STRIP AT STA 747 IN AFT PIT LBL 22. REMOVED CORROSION ON LT FLOOR STRIP IAW SRM, ORIG MAT THK IS .05 0 MAT REMOVED IS .003. FOUND TO BE WITHIN LIMITS IAW SRM. (K) 2 L 7 2 4F RT A16WE 2007030600065 20070306 00065 NM 2007 3 6 AMTA200700087 1 20070217 A 5551 PIN BOEING 737 73783N 13844HI NM HORIZ STAB CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 323TZ 30033 RT AFT LOWER STAB PIN CORRODED. REPLACED PIN 180A16124 IAW EO 737-55AD-2935, REV B. (K) 2 L 7 2 4F RT A16WE 2007030600066 20070306 00066 NM 2007 3 6 AMTA200700092 1 20070217 A 5551 BOLT BOEING 737 73783N 13844HI NM HORIZ STAB CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 323TZ 30033 LT FWD UPPER STAB PIN ATTACH BOLT SEVERAL NICKS AND CORROSION. REPLACED BOLT PN 180A1611-3 IAW EO 73755AD-2935, REV B. (K) 2 L 7 2 4F RT A16WE 2007030600069 20070306 00069 NM 2007 3 6 AMTA200700061 1 20070207 A 4920 APU BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE APU BAY SHUTDOWN A AMTA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 561TZ 33526 APU HAD AUTO SHUTDOWN, FAULT LIGHT ILLUM, AND EICAS MSG, APU FAULT DISPLAYED. INTEROGATED APU (-19) AND CLEARED FAULTS. NO FAULTS DISPLAYED. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007030600070 20070306 00070 2007 3 6 AMTA200700079 4 20070213 A 2330 ELECTRICAL BOX BOEING 737 73783N 13844HI NM CABIN MALFUNCTIONED A AMTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 310TZ 28243 INFLIGHT AT CRUISE ALT FUMES SMELLED AT ROWS 1, 2 AND 3 ON LT SIDE. APPEAR TO BE ELECTRICAL SMELL. REMOVED AND REPLACE D SEB AT ROW 2 ABC IAW MM. OPERATIONAL CHECK NORMAL. (K) 2 L 7 2 4F RT A16WE 2007030600072 20070306 00072 NM 2007 3 6 AMTA200700093 1 20070217 A 5511 ATTACH BOLT BOEING 737 73783N 13844HI NM HORIZ STAB GALLED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 323TZ 30033 LT STAB FWD SPAR ATTACH BOLT GALLED. INSTALLED NEW BOLT 180A1611-3, EO 737-55AD-2935, REV B. (K) 2 L 7 2 4F RT A16WE 2007030600075 20070306 00075 NM 2007 3 6 AMTA200700078 1 20070211 A 2120 WARNING LIGHT BOEING 737 73783N 13844HI NM COCKPIT ILLUMINATED A AMTA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 308TZ 28244 RT PACK LIGHT ILLUMINATED DURING RECALL RESET WITH MASTER CAUTION RESET. (K) 2 L 7 2 4F RT A16WE 2007030600076 20070306 00076 WP 2007 3 6 AMTA200700099 1 20070201 A 7932 8TJ99GAV6 INDICATOR LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE OIL SYSTEM UNSERVICEABLE A AMTA K NONE K FLUID LOSS CR CRUISE 1 GL 11 161AT 1219 14784 NR 3 ENG OIL QTY INDICATOR DECREASED TO 10 QTS DURING FLIGHT RETURNED TO 17 QTS ON DESCENT. REMOVED AND REPLACED ENGINE OIL QUANITY INDICATOR IAW MM 79-37-01. LEAK AND OPS CHECK GOOD. (K) 2 L 7 3 4F 4 F A23WE E12EU 2007030600079 20070306 00079 NM 2007 3 6 AMTA200700088 1 20070217 A 5551 BOLT BOEING 737 73783N 13844HI NM HORIZ STAB CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 323TZ 30033 RT FWD LOWER BOLT HAS CORROSION. REMOVED AND REPLACED BOLT WITH NEW BOLT PN 180A1611-3 IAW EO 737-55AD-2935 REV B. (K) 2 L 7 2 4F RT A16WE 2007030600080 20070306 00080 WP 2007 3 6 AMTA200700095 1 20070218 A 3397 POWER CABLE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE CABIN DEFECTIVE A AMTA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 11 161AT 1219 EGRESS STRIP BY B-1 LAV INOPERATIVE. REMOVED AND REPLACED POWER CABLE AT B-1 LAV. EGRESS STRIP. OPS CHECK NORMAL. (K ) 2 L 7 3 4F 4 F A23WE E12EU 2007030600081 20070306 00081 WP 2007 3 6 AMTA200700100 1 20070213 A 2780 BRAKE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE L/E SLAT MALFUNCTIONED A AMTA K NONE F FLT CONT AFFECTED DE DESCENT 1 GL 11 164AT 1238 LEADING EDGE SLATS DID NOT EXTEND. LANDED WITH PARTIAL FLAPS. FLAP/SLAT LOCK ILLUMINATED. RESET BOTH SLAT ASSEMETRY B RAKES IAW MM 27-81-37. FLAPS/SLATS OPS CHECK NORMAL. (K) 2 L 7 3 4F 4 F A23WE E12EU 2007030600084 20070306 00084 2007 3 6 2007UALA00614 4 20070227 A 2565 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 516UA 24860 DOOR 2R SLIDE ARMED LIGHT INOPERATIVE. [SUP 05-18-07] REPLACED LAMPS. THIS WAS A CASE OF A FUSED LAMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030600085 20070306 00085 2007 3 6 2007UALA00615 4 20070226 A 2565 B14056914 O-RING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EVAC SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 1881 24536 LOW BOTTLE PRESSURE. CAUSED BY GAUGE ADAPTER FITTING O-RING LEAKING. REPLACED O-RING. 2 L 7 2 4F 4 F RT A16WE E21EU 2007030600086 20070306 00086 EU 2007 3 6 2007UALA00616 2 20070228 A 7261 INDICATION SYS BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT ACTIVATED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 351UA 24319 725193 FLIGHT DIVERTED DUE TO NR 1 ENG LOW OIL QUANTITY INDICATION. FOUND LEAK AT ACCESSORY GEARBOX CARBON SEAL DURING TROUBLE SHOOTING. REPLACED STARTER DRIVE PAD CARBON SEAL ASSEMBLY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007030600097 20070306 00097 NM 2007 3 6 2007UALA00627 1 20070228 A 3213 CYLINDER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT MLG CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 87UA 26713 RT OUTER CYLINDER HAS CORROSION. [SUP 05-18-07] RT OUTER CYLINDER CORROSION HAS BEEN REMOVED. SHOP CONTINUES TO BLEND FURTHER CRACK INDICATIONS. INSTALLED RT MLG SHOCK STRUT INNER CYLINDER AND RT MLG SHOCK STRUT. FOUND RUSTY WATER AND S LUDGE ABOVE SCRAPER. SCRAPER WAS FOUND UPSIDE DOWN. ALSO FOUND EXCESSIVE AMOUNT OF CORROSION ABOVE GLAND NUT THREAD ON OUTR CYLINDER. REPLACED GLAND NUT WITH NEW PART. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030600098 20070306 00098 SO 2007 3 6 SIMA200706401 1 20070302 A 2133 2097K011100 OUTFLOW VALVE EMB 135 EMB135KL 3260302 SO CABIN PRESSURE FAILED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 806AE 12995 10013 145503 LOST PRESSURIZATION ON CLIMB-OUT. REMOVED AND REPLACED ELECTRONEUMATIC OUTFLOW VALVE IAW EMB AMM 21-31-03. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007030600099 20070306 00099 NM 2007 3 6 AWXA200700321 1 20070128 A 5310 6520723506 DOOR FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND FORWARD CARGO DOOR CUT OUT AFT FRAME WEB CRACKED, BS 493, S24R. REPAIRED FORWARD CARGO DOOR CUT OUT AFT FRA ME WEB IAW AWA ER 03-5331-07058-SS1. 2 L 7 2 4F RT A16WE 2007030600105 20070306 00105 GL 2007 3 6 DL764070167 2 20070227 A 7240 COMBUSTION LINER BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 1 ENGINE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 840MH 29717 706232 ENGINE FAILED BORO OPN 5003 COMBUSTION LINER DAMAGED. REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F RT A1NM E23EA 2007030600111 20070306 00111 NM 2007 3 6 DHL2007751501 1 20070226 A 5311 FRAME BOEING 727 727264 138408M NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 751DH 22982 WHILE IN "C" CHECK, AFT CARGO COMPT FRAME AT STA1050 IS DENTED BETWEEN STR 26L AND 27L IN THE UPPER FLANGE. CUTOUT DEN TED AREA (DIM 7" BY 2 1/2" BY 1 1/2") IAW B727 SRM 51-40-3 FIG 1. FABRICATED FRAME REPAIR ANGLE FROM 7075-0 0.063 (D.7" X 2 1/2") PO NR 9004384 IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1. HEAT TREATED NEW ANGLE TO T6 IAW FAS ENGINEERING REPORT NR 2-37153-801 REVIR. TREATED AND PRIMED PART IAW B727 SRM 51-10-2. INSTALLED FRAME REPAIR AT BS 1050 STR 26L-2 7L IN THE UPPER FLANGE IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007030600112 20070306 00112 NM 2007 3 6 DHL2007751502 1 20070226 A 5311 FRAME BOEING 727 727264 138408M NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 751DH 22982 WHILE IN "C" CHECK, FWD CARGO COMPT FRAME STA 500 IS DENTED IN TWO PLACES AT UPPER FLANGE BETWEEN STR 23R-24R. CUTOUT D AMAGED AREA AT FWD CARGO COMPT BS 500 BETWEEN STR 23R AND 24R APPROX DIM 1 1/2" BY 1" IAW B727 SRM 51-40-3 FIG 1. FAB R EPAIR ANGLE FROM 7075-0 .050 PO NR 9004219 APPROX DIM 11 1/4" BY 3 3/4" IAW B727 SRM 51-40-3 FIG 1 AND SRM 53-10-2 FIG 3 . HEAT TREATED MAT TO T6 CONDITION IAW FAS0115 REV 10. INSTALLED REPAIR ANGLE AT FWD CARGO COMPT BS 500 IAW B727 SRM 5 1-40-3 FIG 1. 2 L 7 3 4F A3WE 2007030600113 20070306 00113 NM 2007 3 6 DHL2007781017 1 20070130 A 5753 STRUCTURE BOEING 727 727227 1384078 NM T/E FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 781DH 21996 FOUND LT IB MID FLAP WBL 71-134 HAS 4 CRACKS ON 3 CUTOUTS ON THE AFT LOWER CHORD. REMOVED DAMAGED SECTION OF AFT LOWER CHORD APPROX 70 3/8. LOCATED AND DRILLED NEW CHORD P/N BAC1503-100046 PO NR 652296 DIM 70 3/8 IAW B727 SRM 57-50-2 FIG 5, 51-40-4 FIG 1 AND 51-30-5. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 51-40 -4 FIG 1. OPS CHECK GOOD IAW B727 MM 27-51-00. 2 L 7 3 4F A3WE 2007030600114 20070306 00114 NM 2007 3 6 DHL2007751503 1 20070228 A 5754 SKIN BOEING 727 727264 138408M NM L/E SLAT DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 751DH 22982 A/C IN "C" CHECK, NR 7 SLAT UPPER SKIN IS DENTED AT RIVET WS 601. REMOVED FASTENERS IN AFFECTED AREA IAW B727 SRM 51-30 -2. CUTOUT DAMAGED AREA (DIM.1" BY 1") IAW B727 SRM 57-50-3 FIG 1. FAB REPAIR DOUBLER FROM 2024T3 0.080 PO NR 9004617 (DIM.5 1/4" BY 4 1/4") IAW B727 SRM 57-50-3 FIG 1. TREATED AND PRIMED DOUBLER IAW B727 SRM 51-10-2. INSTALLED REPAIR D OUBLER AT NR 7 SLAT UPPER SKIN IAW B727 SRM 57-50-3 FIG 1 AND 51-30-2. 2 L 7 3 4F A3WE 2007030600115 20070306 00115 NM 2007 3 6 DHL2007751504 1 20070302 A 5320 ANGLE BOEING 727 727264 138408M NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 751DH 22982 IN "C" CHECK, NOSE WW INSIDE LT UPPER PRESSURE PANEL ACCESS "L" ANGLE IS CRACKED AT STA 258 LBL 6. REMOVED CRACKED ANGL E IAW B727 SRM 51-30-2. FAB NEW ANGLE FROM 2024T3 0.040 PO NR 9004539 DIM 10 1/4" BY 1"BY 1" IAW B727 SRM 53-10-2 FIG 1 AND 51-20-1. TREATED AND PRIMED NEW ANGLE IAW B727 SRM 51-10-2 AND INSTALLED NEW ANGLE AT NOSE WW INSIDE LT UPPER PRES SURE ACCESS PANEL AT STA 258 LBL 6 IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007030600116 20070306 00116 NM 2007 3 6 DHL2007751505 1 20070302 A 5320 ANGLE BOEING 727 727264 138408M NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 751DH 22982 IN "C" CHECK, NOSE WW INSIDE LT UPPER PRESSURE PANEL ACCESS, "L" ANGLE IS CRACKED AT STA.259 LBL 12. REMOVED CRACKED AN GLE IAW B727 SRM 51-30-2. FAB NEW ANGLE FROM 2024T3 0.040 PO NR 9004539 DIM 6 1/2" BY 1"BY 1" IAW B727 SRM 53-10-2 FIG 1 AND 51-20-1. TREATED AND PRIMED NEW ANGLE IAW B727 SRM 51-10-2. INSTALLED NEW ANGLE AT NOSE WW INSIDE LT UPPER PRESS URE PANEL AT STA 259 LBL 12 IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007032800027 20070328 00027 GL 2007 3 28 C2XA07IA069 2 20070326 A 7200 AE3007A1P ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LEFT LEAKING A C2XA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 27 14950 11831 11831 145061 IAH - FLIGHT 2978, THE CREW REPORTED THAT ON TOUCHDOWN HAD HEAVY SMOKE IN THE COCKPIT AND CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007032800029 20070328 00029 NM 2007 3 28 KCSA071077 1 20070323 A 5347 SEAT TRACK BOEING 747 747236B 1384804 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STA 1903 RBL 25 SEAT TRACK HAS FLANGE PORTION BLENDED OUT WL 118. 2 L 7 4 4F A20WE 2007030600117 20070306 00117 NM 2007 3 6 DHL2007751506 1 20070226 A 5311 FRAME BOEING 727 727264 138408M NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 751DH 22982 IN "C" CHECK, FWD CARGO COMPT FRAME STA 520 IS DENTED AT UPPER FLANGE ABOVE STR 24R. CUT OUT DAMAGED AREA APPROX DIM 1" BY 3/4" IAW B727 SRM 51-40-3 FIG 1. FAB REPAIR ANGLE FROM 7075-0 .050 PO NR 9004219 APPROX DIM 10 1/4" BY 3 1/4" IAW B 727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3. HEAT TREATED MAT T0 T6 CONDITION IAW FAS FORM NR FAS0115 REV 10. INSTALLED RE PAIR ANGLE AT FWD CARGO COMPT FRAME BS520 STR 24R IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2007032800030 20070328 00030 NM 2007 3 28 KCSA071078 1 20070323 A 5414 STRUCTURE BOEING 747 747236B 1384804 NM NR 3 PYLON WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 NR 3 PYLON O/B SIDE STA 180 LOWER SKIRT CORNER WORN AWAY. 2 L 7 4 4F A20WE 2007030600118 20070306 00118 NM 2007 3 6 EIA2007027 1 20070222 A 5521 SPAR BOEING 747 747273C 1384896 NM RT ELEVATOR DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 DAMAGE FOUND COMMON TO FRONT SPAR, LOWER CHORD OF RT O/B ELEVATOR STA 227.65. TRIM OUT DAMAGED PORTION OF LOWER CHORD, CARRY OUT HFEC ON TRIM EDGES. FABRICATE FILLER AND REPAIR ANGLES. APPLY ALODINE COATING TO ALL REPAIR PARTS AND BASE M ETAL EDGES. INSTALL REPAIR PARTS TO FAYING SURFACE WITH BMS 3-95. 2 L 7 4 4F A20WE 2007030600120 20070306 00120 NM 2007 3 6 EIA2007030 1 20070222 A 5753 SKIN BOEING 747 747273C 1384896 NM FLAP FAIRING DEBONDED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 DIS-BOND OF INNER PANEL SKIN AT TITANIUM AREA ON NR 5 MOVABLE FLAP-TRACK FAIRING. X-RAY INTERSECTION OF ADJACENT AREA A ND SUB-STRUCTURE, CONFIRM ALL DAMAGE. REMOVE DAMAGE SECTION OF TITANIUM SCRAP WITH 10 PLIES 9-8 INCLUDED 2 EXTRA FIBERG LASS PLIES COMPLETELY COVERING GRAPHITE PLIES WITH 0.5 INCH OVERLAP. INSTALLED FASTENERS WITH BMS 5-95 AND ASSEMBLE BRA CKETS WITH BMS 5-95, REPLACE DAMAGED INSERTS. 2 L 7 4 4F A20WE 2007030600121 20070306 00121 NM 2007 3 6 EIA2007032 1 20070222 A 5521 SPAR BOEING 747 747273C 1384896 NM RT ELEVATOR DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 RIGHT OUTBOARD FRONT SPAR LOWER CHORD FOUND DAMAGED. TRIMMED OUT DAMAGED PORTION OF LOWER CHORD PERFORMED HFEC ON TRIM EDGES AND FABRICATE FILLER AND REPAIR ANGLES. APPLIED ALODINE AND PRIMER ON PARTS AND INSTALL FASTENERS AND NUT PLATES WITH RIVETS AT NUT PLATE LOCATIONS. INSTALL REPAIR PARTS WITH BMS 5-95. 2 L 7 4 4F A20WE 2007030600122 20070306 00122 NM 2007 3 6 EIA2007033 1 20070222 A 5753 FLAP TRACK BOEING 747 747273C 1384896 NM T/E FLAP CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 FOUND NR 6 FLAP TRACK WITH CORROSION ON SURFACE BETWEEN FITTING AND WING SKIN AT REAR SPAR WBL 553. OVERSIZE HOLE IN BA THTUB FITTING AND LOWER WING SKIN, PERFORM HFEC TO CONFIRM NIL DEFECTS. FABRICATE NEW REPAIR BUSHING, INSTALL NEW REPAI R BUSHING AND FASTENERS. 2 L 7 4 4F A20WE 2007030600123 20070306 00123 NM 2007 3 6 EIA2007034 1 20070222 A 5330 SKIN BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 FOUND CORROSION FOUND ON SKIN AT STA 680 AND 750 BETWEEN STR 40R AND STR 43R. PARTS FORMED, INSTALLED WITH BMS-5-95 AND INSTALL FASTENERS. 2 L 7 4 4F A20WE 2007030600124 20070306 00124 NM 2007 3 6 EIA2007036 1 20070222 A 5753 SEAL BOEING 747 747273C 1384896 NM T/E FLAP ERODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 FLAP MOLDING SEAL FOUND ERODED AT SEVERAL LOCATIONS. REPLACED WITH BACR15BB8DD RIVETS COMMON TO OUTBOARD SPOILER FITTIN G, THE REAR SPAR WEB AND WS 1028 RIB POST WITH BACB30NX*K*Y HILOCKS AND BACC30AC8 COLLARS IN 0.2772-0.2792 IN DIA HOMES. 2 L 7 4 4F A20WE 2007030600129 20070306 00129 NM 2007 3 6 EIAA2007040 1 20070222 A 5534 65B033371 STRUCTURE BOEING 747 747273C 1384896 NM VERTICAL STAB CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 STAB COMPARTMENT VERTICAL FIN INSPECTION FOUND TOP BOX CORRODED (EXFOLIATION) LEFT SIDE CHORD AT STA 395. CORROSION BLE NDED OUT HFEC INSPECTED, ALODINE AND PRIMED, FASTENERS INSTALLED. 2 L 7 4 4F A20WE 2007030600130 20070306 00130 NM 2007 3 6 07FDEA00616 1 20070301 A 5310 DOOR FRAME DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 MAIN DECK CARGO DOOR JAMB UNDER CENTERING GUIDE AREA FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5310-106596. REPAIR CLA SSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007030600131 20070306 00131 NM 2007 3 6 07FDEA00617 1 20070301 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM T/E FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LT WING I/B FLAP L/E AT O/B HINGE AREA FOUND CHAFED. REPAIR CARRIED OUT AS PER SRM 57-00-01 FIG. 7 VOL.I. REPAIR CLA SSIFIED AS MINOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007030600132 20070306 00132 NM 2007 3 6 07FDEA00618 1 20070301 A 2810 SKIN DOUG MD11 MD11 3023602 NM FUEL TANK CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 MAIN DECK CARGO CENTER FUEL TANK UPPER SURFACE FOUND CORROSION AT STA 1218, X=75.25. COMPLIED WITH FEDEX EA 1-5710-1056 29. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007030600133 20070306 00133 EU 2007 3 6 07FDEA00619 1 20070301 A 7830 UNKNOWN AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER UNSECURE A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 681FE 799 ON T/O ROLL BELOW 80K, NR 1 T/R PRESSURIZED AS NOTED ON LEFT ECAM AND NR 1 REV UNLOCK LT ILLUMINATED. FOUND C/P FOR DPV NOT SECURED CAUSING LT, REF MEL 78-30-01-A. 2 L 7 2 4F RT A35EU 2007030600136 20070306 00136 EU 2007 3 6 07FDEA00629 1 20070302 A 5320 A53813311 FITTING AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CORRODED A FDEA K NONE O OTHER UK UNKNOWN 1 SO 25 748FD 633 FOUND CORROSION AT C54, TRACK 5, LT AND RT REPAIR WAS PERFORMED IAW EA 6-5315-106393 AND RAS/049222/.008/2006 ISS A, LT INSTALL FITTING P/N A538-13311, RT INSTALL COUNTRSINK BUSH. 2 L 7 2 4F RT A35EU 2007030600137 20070306 00137 NM 2007 3 6 07FDEA00608 1 20070227 A 5753 65825166 BUSHING BOEING 727 727225 1384077 NM T/E FLAP MIGRATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 NR 6 FLAP TRACK FWD ATTACH FITTING HAS MIGRATING BUSHING AND INBD FACE HAS CORROSION (BORE ALSO CORRODED) WBL 203. REMO VE BUSHING, REAMED BORE, MPI BORE, FABRICATE BUSHING, CAD PLATE BUSHING, ROTOPEEN BORE AND FACES, CAD PLATE LUG AND INST ALLED BUSHING REF FED EX DWG SR 27-57-020 REV A., NOTES 1-9. 2 L 7 3 4F A3WE 2007030600138 20070306 00138 EU 2007 3 6 07FDEA00609 1 20070227 A 5610 SEAL AIRBUS 310 A310222 3930315 EU COCKPIT DIRTY A FDEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 25 417FE 333 REJECTED TAKEOFF AT 115 KTS DUE TO INCREASING COCKPIT NOISE AS IF CAPT'S WINDOW SEAL RUPTURED. INSPECTED CAPT'S SLIDING WINDOW SEAL, FOUND DEBRIS. CLEANED DEBRIS AND RESEATED WINDOW SEAL. PRESSURIZATION CHECK PER MM21-31-00-5. NO LEAK F OUND. A/C OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2007030600139 20070306 00139 NM 2007 3 6 07FDEA00610 1 20070227 A 3242 BRAKE DOUG MD11 MD11 3023602 NM NR 1 SEPARATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 DURING TIRE CHANGE, FOUND THAT NR 1 BRAKE COMING APART REMOVED AND REPLACE NR 1 BRAKE PER AMM 32-43-01-4. OPS AND LEAK CHECK GOOD. 2 L 7 3 4F RT A22WE 2007030700001 20070307 00001 EU 2007 3 7 SIMA200706402 1 20070302 A 2430 51539007B GCU SAAB SF340 340B 7860101 EU LT ENGINE FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 390AE 11833 3065 340B390 LEFT GENERATOR ANNUNCIATOR ILLUMINATED. RESET UNSUCCESSFUL, PLACED SWITCH IN OFF POSITION. DECLARED EMERGENCY. REMOVE D AND REPLACED GENERATOR CONTROL UNIT IAW SAAB 24-31-10. OPERATIONAL TEST GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007030700002 20070307 00002 SO 2007 3 7 SIMA200706404 1 20070301 A 3610 ACTUATOR EMB 135 EMB135LR 3260305 SO RAM AIR SYS WORN A SIMA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SW 21 731BE * 145356 VIBRATION FELT IN BOTH IN CABIN AROUND ROW 6 AND FLIGHT DECK, NO VIBRATION IN FELT IN CONTROLS. REMOVED AND REPLACED NR 1 RAM AIR VALVE ACTUATOR ASSEMBLY, LEFT EMERGENCY VENT VALVE ASSEMBLY AND RIGHT EMERGENCY VENT VALVE ASSEMBLY IAW EMB A MM. OPERATIONAL CHECK GOOD. PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007030700003 20070307 00003 EU 2007 3 7 SIMA200706403 1 20070302 A 2697 AMP321893 TERMINAL SAAB SF340 340B 7860101 EU RT ENGINE BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 238AE 25473 340B238 FOUND RIGHT TAIL PIPE HOT NO TEST. REPLACED TWO BROKEN TERMINALS ON LOWER HEAT SENSOR ON TAIL PIPE IAW WIRING STANDARD PRACTICES. OPERATIONAL CHECK GOOD IAW SAAB AMM 26-11-00. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007030700005 20070307 00005 WP 2007 3 7 NWAA070689885 1 20070129 A 5753 STRINGER DOUG DC9 DC951 3022051 WP TE FLAP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 401EA 17234 47682 DURING "H" CHECK, FOUND CRACK IN LT WING TRAILING EDGE FLAP FORWARD SPAR UPPER STRINGER. REPAIRED PER EA 99-208451. 2 L 7 2 4F RT A6WE 2007030700007 20070307 00007 2007 3 7 SWAA071158 4 20070301 A 2565 63550 SLIDE BOEING 737 737* NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 270WN 29089 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. (A/C MODEL 737-705) 2 L 7 2 4F RT A16WE 2007030700008 20070307 00008 NM 2007 3 7 ASAA0741485 1 20070223 A 5754 65C26603191 WEDGE BOEING 737 7374Q8 138447Q NM L/E SLAT DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 NR 3 SLAT DENTED ON T/E WEDGE ASSY LOCATED 28 INCHES I/B OF O B E.D. NR 3 SLAT REPAIRED IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007030700009 20070307 00009 2007 3 7 AMTA200700105 4 20070220 A 3460 UNKNOWN BOEING 737 73783N 13844HI NM COCKPIT MALFUNCTIONED A AMTA K NONE O OTHER TX TAXI/GRND HDL 1 GL 11 317TZ 28246 UNABLE TO COMPLETE IRS MONITOR CHECK, BOTH FMCS LT AND RT DISPLAY BLANK WHERE NM/HR NORMALLY APPEAR. FMCS BITE FIM 34-61 -00-810-80. NO FAULT FOUND. AC OK FOR SERVICE. (K) 2 L 7 2 4F RT A16WE 2007030700010 20070307 00010 NM 2007 3 7 AMTA200700062 1 20070209 A 4910 7321387012 ACTUATOR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE APU UNSERVICEABLE A AMTA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 522AT 29330 UPON ARRIVAL, APU WOULD NOT START UP AFTER 3 ATTEMPTS. NO OTHER FAULTS, FLAGS OR STATUS MSGS ANNUNCIATED. REMOVED AND REPLACED APU INLET DOOR ACTUATOR IAW MM, APU OPS CHECKS GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007030700011 20070307 00011 2007 3 7 AMTA200700097 2 20070218 A 7310 FUEL BOEING 737 73783N 13844HI NM LEAKING A AMTA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 GL 11 305TZ 30706 ON PREFLIGHT FOUND FUEL PUDDLE UNDER ENGINE NR 2. RAN ENG AND INSPECT FOR FUEL LEAK NON FOUND, OK FOR SVC IAW AMM. (K) 2 L 7 2 4F RT A16WE 2007030700012 20070307 00012 2007 3 7 AMTA200700080 4 20070213 A 3460 4052506955 COMPUTER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LEFT MALFUNCTIONED A AMTA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 522AT 29330 EICAS MSG LT FMC FAIL DISPLAYED OTHER CDU DISPLAYS SINGLE FMC OPERATION MESSAGE. REMOVED AND REPLACED LT FMC IAW MM. C ROSS LOAGED. OPS CHECK OK. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007030700016 20070307 00016 2007 3 7 AMTA200700084 4 20070215 A 3416 4039892904 ALTIMETER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT INOPERATIVE A AMTA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 522AT 29330 FO`S ALTIMITER INOPERATIVE. REMOVED AND REPLACED ALTIMITER IAW AMM. OPS CHECKS NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007030700017 20070307 00017 NM 2007 3 7 AMTA200700096 1 20070218 A 4997 CONNECTOR BOEING 737 73783N 13844HI NM APU DIRTY A AMTA K NONE N FALSE WARNING DE DESCENT 1 GL 11 304TZ 30675 APU FAULT CODE ON AFTER A MANUAL SHUTDOWN 1 HOUR PRIOR TO LANDING. LIGHT EXTINGUISHED AFTER 5 MIN. APU MASTER CAUTION LIGHT DID NOT STAY ILLUMINATED AFTER FAULT LIGHT WENT OUT. PERFORMED FIM, STEP F (1) B (4) VALVE OPERATION NORMAL. NO MX MESSAGE. (CLEAN AND RESEATED CONNECTOR PLUG) OPS CHECK GOOD. OK FOR SERVICE. (K) 2 L 7 2 4F RT A16WE 2007030700021 20070307 00021 NM 2007 3 7 ASAA0741498 1 20070227 A 5315 65C335332 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 FLOORBEAM UPPER CHORD IS CORRODED. REMOVED UPPER CHORD, INSTALLED NEW CHORD IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007030700023 20070307 00023 NM 2007 3 7 ASAA0741500 1 20070227 A 5754 SKIN BOEING 737 7374Q8 138447Q NM L/E SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 NR 4 SLAT CHAFED AT O/B TRAILING EDGE BOTTOM SURFACE. PREPPED CHAFED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-70-10 REPAIR 4. 2 L 7 2 4F RT A16WE 2007030700024 20070307 00024 NM 2007 3 7 ASAA0741501 1 20070227 A 5753 6590737563 FITTING BOEING 737 7374Q8 138447Q NM T/E FLAP DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 RIGHT I/B MIDFLAP CENTER FORE FLAP TRACK I/B ROLLER SUPPORT BOSS ACCOMPLISH BORE REPAIR PER BOEING MSG 1 222431189 2. R EMOVED DAMAGED RIB, INSTALLED NEW RIB FITTING PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007030700025 20070307 00025 NM 2007 3 7 ASAA0741486 1 20070223 A 5753 6546435339 SKIN BOEING 737 7374Q8 138447Q NM T/E FLAP DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 LEFT O/B AFT FLAP END CAP DISBONDED. LEFT O/B AFT FLAP REPAIRED IAW CASCADE ERO 6540 AND ASA EA 57 50 02331. 2 L 7 2 4F RT A16WE 2007030700026 20070307 00026 NM 2007 3 7 ASAA0741487 1 20070223 A 5320 6517688U1 SILL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER NR NOT REPORTED 1 NM 02 756AS 25097 L1 DOOR SILL CHORD CORRODED. REPLACED L1 DOOR SILL CHORD IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007030700028 20070307 00028 NM 2007 3 7 ASAA0741489 1 20070223 A 5320 6545875520 STRAP BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 R1 DOORWAY LOWER SILL CHORD REINFORCEMENT STRAP EXFOILATED. REINFORCEMENT STRAPS REPLACED WITH NEW PART IAW SRM 51-40-0 5. 2 L 7 2 4F RT A16WE 2007030700030 20070307 00030 NM 2007 3 7 ASAA0741491 1 20070223 A 5320 654587547 WEB BOEING 737 7374Q8 138447Q NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 R1 DOORWAY LOWER SILL WEB SCRATCHED. FLOOR WEB REPLACED WITH FABRICATED REPAIR PART IAW SRM 51-40-02 AND 51-40-05. 2 L 7 2 4F RT A16WE 2007030700031 20070307 00031 NM 2007 3 7 ASAA0741492 1 20070223 A 5320 6545875U70 SILL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 R1 DOORWAY LOWER SILL CHORD CORRODED. REPLACED SILL WITH NEW PART IAW SRM 51-40-05 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007030700034 20070307 00034 EA 2007 3 7 TRAX200700280 1 20070221 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 699BR 7801 RIGHT FORWARD EMERGENCY LIGHT OUT BY GALLEY DOOR INOP. FLT 4690 DEL 44 MINS. 2 L 7 2 4F RT A21EA 2007030700036 20070307 00036 EA 2007 3 7 TRAX200700282 1 20070222 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 LEFT FWD SEAT TRACK IN PAX COMPARTMENT CORRODED. 2 L 7 2 4F RT A21EA 2007030700037 20070307 00037 EA 2007 3 7 TRAX200700283 1 20070222 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 RIGHT FWD SEAT TRACK IN PAX COMPARTMENT CORRODED. 2 L 7 2 4F RT A21EA 2007030900257 20070309 00257 NM 2007 3 9 SWAA071246 1 20070306 A 5311 6546538 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030900261 20070309 00261 NM 2007 3 9 SWAA071256 1 20070307 A 2120 32194211 VALVE BOEING 737 7377H4 1384404 NM A/C PACK FAULTY A SWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 246LV 32507 DECLARED EMERGENCY/AIR TURNBACK. CREW REPORTED STRONG ELECTRICAL/OZONE SMELL IN COCKPIT AND CABIN. REMOVED AND REPLACE D LEFT A/C PACK 35 DEGREE VALVE PER MM. 2 L 7 2 4F RT A16WE 2007030900268 20070309 00268 NM 2007 3 9 SWAA071265 1 20070307 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030900287 20070309 00287 NM 2007 3 9 SWAA071250 1 20070306 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030900291 20070309 00291 NM 2007 3 9 SWAA071237 1 20070306 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 228WN 32496 DURING SCHEDULED MV1 CHECK, FOUND LEFT FWD FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007030900302 20070309 00302 NM 2007 3 9 BB07018 1 20070219 A 3213 161N15013 TORQUE LINK BOEING 757 757225 1384959 NM RT MLG BROKEN A USAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 19 925UW 44543 665 22205 FLIGHT 1827, PHL-FLL: DURING TAXI, RIGHT LOWER MLG TORQUE LINK BROKE, ALLOWING RIGHT TRUCK TO TWIST OFF CENTER. A/C WAS TOWED BACK TO GATE. MAINTENANCE REPLACED THE TORQUE LINK ASSEMBLY. 2 L 7 2 4F RT A2NM 2007031200001 20070312 00001 SO 2007 3 12 RAIA00702048 1 20070227 A 3297 WIRE HARNESS EMB 145 EMB145LR 3260212 SO NLG DAMAGED A RAIA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 CE 03 837HK 145255 FLT NR 7997 - IAD - LG AIR-GROUND FAIL. MAINTENANCE REPAIRED WIRING TO NLG WOW PROX SWITCH, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007031200002 20070312 00002 SO 2007 3 12 RAIA00702035 1 20070223 A 3350 78241 INVERTER EMB 145 EMB145 3260210 SO CABIN UNKNOWN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 820HK 145064 PRE FLT NR 5496 - STL - EMERGENCY LIGHT FWD SIDE OF AFT CEILING EXIT LOCATOR IS OUT. MAINTENANCE REMOVED AND REPLACED E MERGENCY LIGHT INVERTER NR 6. 2 L 7 2 4F RT T00011AT 2007031200005 20070312 00005 SO 2007 3 12 RAIA00702037 1 20070223 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 830HK 145313 PRE FLT NR 5498 - STL - EMERGENCY LIGHT AT AISLE 1A AND LOWER EXIT ON SERVICE DOOR INOP. MAINTENANCE RESEATED CONNECTOR TO LIGHT FLOOR PROXIMITY LIGHT. 2 L 7 2 4T RT T00011AT 2007031200006 20070312 00006 SO 2007 3 12 RAIA00702045 1 20070228 A 2750 FLAP EMB 145 EMB145LR 3260212 SO WING MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 816HK 145055 FLT NR 5518 - AUS - FLAPS STUCK AT 9 DEGREES AFTER TAKEOFF. MAINTENANCE RESET FLAP SYSTEM. OPS CHECKS GOOD AT THIS TIM E. 2 L 7 2 4T RT T00011AT 2007031200007 20070312 00007 NE 2007 3 12 DXTA200701998 2 20070304 A 7200 ENGINE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE LEFT SURGES E DXTA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 07 149QS RK473 AFTER LEVEL OFF FOLLOWING AN UNRESTRICTED CLIMB TO FL 380, LT ENGINE BEGAN TO SURGE +- 2 PERCENT N1 (APPROX). ENGINE SYN C-ON. EGT, N2 AND FUEL FLOW WERE ALSO FLUXUATING WITH FUEL FLOW =- 50 TO 75 PSI. ENGINE SYNC TURNED OFF WITH NO CHANGE ( STILL FLUXUATING). BOTH ENGINE ANTI-ICE SYSTEMS WERE TURNED (ON) AND ABOUT 3 SEC TO 1 MINUTE LATER ALL ENG PARAMETERS RE TURNED TO NORMAL (ENG. TREND LOG TAKEN AND FAXED SEPERALY) SHORTLY BEFORE DECENT ENG. A/I TURNED OFF (STILL AT FL 380) E NGINE AGAIN BEGAN TO SURGE. ENG A/I TURNED BACK (ON) ALL PARAMETER RETURNED TO NORMAL (FUEL WAS SUMPED PRIOR TO FLT CLE AN). DURING CLIMBOUT AND AT LOWER ALTITUDES (OAT >10 DEGREES C) ALL ENG PARAMETERS NORMAL 2 H 7 2 4F 4 F RT A16SW E25EA 2007031200009 20070312 00009 SO 2007 3 12 RAIA00703006 1 20070302 A 3350 SG9632 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MISSING A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 846HK 14500855 PRE FLT NR 7961 - IAD - RIGHT SIDE MOST FORWARD EMERGENCY FLOOR LIGHTING MISSING. MAINTENANCE REPLACED FLOOR LIGHT STRI P. 2 L 7 2 4T RT T00011AT 2007031200011 20070312 00011 CE 2007 3 12 DXTA200701992 1 20070303 A 3260 UPLOCK SWITCH BEECH MU300 400A 1155402 CE CFMINT CFM567 CFM567B22 13802 NE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 122QS RK467 RED LIGHT ON GEAR HANDLE REMAINS ON AFTER GEAR RETRACTION. JACKED AIRCRAFT PERFORMED GEAR RETRACT TEST MAIN GEAR INBD D OORS DID NOT CLOSE. TROUBLSHOT SYSTEM & FOUND RIGHT GEAR UPLOCK SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH & PERFORMED NUMEROUS GEAR SWINGS WITH NO FURTHER FAULTS.SERVICED HYDRAULIC RESERVOIR WITH M1/5606.REMOVED AIRCRAFT FROM JACKS.ALL WO RK PERFORMED IAW BEECH 400A MM CHAPTER 32 2 H 7 2 4F 4 F RT A16SW E00055EN 2007031200013 20070312 00013 2007 3 12 RAIA00703001 4 20070301 A 3418 0861DT5 SENSOR EMB 145 EMB145LR 3260212 SO STALL WARNING MALFUNCTIONED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 814HK 18796 145046 FLT NR 5551 - STL - SPS 1 FAIL/INOP WARNING TAKEOFF ABORTED AT 50 KNOTS. MAINTENANCE REMOVED AND REPLACED AOA SENSOR, S YS CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2007031200033 20070312 00033 SO 2007 3 12 RAIA00702053 1 20070228 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 810HK 145231 PRE FLT NR 8059 - RIC - EMERGENCY LIGHT INOP, LEFT EMERGENCY DOOR FLOOD LIGHT. MAINTENANCE REMOVED AND REPLACED BULB, O PS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007031200037 20070312 00037 CE 2007 3 12 ACE020507 1 20070205 A 2822 1333890311 PUMP BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65* EA RT RUPTURED E YADA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AL 03 112AX 190 UC45 RT FUEL PRESSURE ILLUMINATED WHEN RT STANDBY PUMP NOT ON, REPLACED FAILED LOW PSI PUMP DUE FUEL LEAKING FROM DIAPHRAGM. 2 L 7 2 4T 4 T RT A24CE E4EA 2007031200038 20070312 00038 SO 2007 3 12 DJFA2007020 1 20070213 A 4930 211171 PRESSURE SWITCH EMB 135 EMB135BJ 3260306 SO ALLSN AE300 AE3007A GL APU LEAKING E DJFA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 23 908LX 3078 E145528 TRIP NR 1133786, CREW REPORTED SMELL OF BURNING RUBBER OR OIL IN THE CABIN WITH THE APU RUNNING. SMELL WENT AWAY 2.5 HR S INTO THE FLIGHT AND CAME BACK WHEN THE APU WAS STARTED. THE SMELL INCREASED WHEN THE PACKS WERE TRANSITIONED FROM THE ENGINES TO THE APU. MAINTENANCE FOUND THE APU LOW PRESSURE SWITCH LEAKING. THE PRESSURE SWITCH WAS REPLACED. 2 L 7 2 4F 4 F RT TE6CH 2007031200045 20070312 00045 CE 2007 3 12 GLBA20060906 1 20070219 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 351-354 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 240GL UE240 UPON ROUTINE INSPECTION, MAINTENANCE DISCOVERED A 3.25 INCH LONG CRACK 27.5 INCHES LT OF BELLY CENTERLINE AT APPROXIMATE LY STA. F.S. 352. MAINTENANCE REPAIRED THE CRACK IN THE FUSELAGE IAW SRM 51-70 FROM F.S. 351 TO F.S. 354.25. REPAIR DIME NSIONS 7.25 INCHES BY 4 INCHES. 2 L 7 2 4T 4 T RT A24CE E26NE 2007031200047 20070312 00047 SO 2007 3 12 RAIA00702051 1 20070228 A 2750 FLAP EMB 145 EMB145LR 3260212 SO WING MALFUNCTIONED A RAIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CE 03 816HK 145055 FLT NR 5464 - STL - FLAPS WOULD NOT RETRACT AFTER T/O. MAINTENANCE RESET POWER TO SYSTEM. OPS CHECK GOOD OF FLAP EXTEN SION AND RETRACTION, NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2007031200049 20070312 00049 SO 2007 3 12 RAIA00703012 1 20070304 A 2720 15793101 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO RUDDER MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 836HK 7713 145695 FLT NR 7916 - DEN - RUDDER SYSTEM 1-2 INOP ON CLIMBOUT 10 MIN AFTER TAKEOFF, BOTH SYSTEMS CAME BACK AFTER FOLLOWING THE CHECKLIST. MAINTENANCE REMOVED AND REPLACED THE NR 2 RUDDER PRESSURE SWITCH. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007031200060 20070312 00060 EU 2007 3 12 AIUA200704115 1 20070215 A 2140 350A72072001 DUCT SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE RUPTURED E A1UA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 03 123LN 34 4115 AT 1920, THERE WAS A NOISE, WHICH SOUNDED LIKE A (POP) AND A SLIGHT ODOR OF SOMETHING GETTING HOT. IT SHOULD BE NOTED H ERE THAT THE CABIN HEAT WAS ON HIGH, AND HAVE SMELLED SMELLS LIKE THAT BEFORE. IN OTHER WORDS, THE ODOR WAS NOT ENTIREL Y UNCOMMON. LOOKED OVER LT SHOULDER OUT THE LT SLIDING DOOR WINDOW. SAW LIGHTS ON THE HORIZON, BUT IT APPEARED AS IF SEEING THEM THROUGH SMOKE. THIS, OF COURSE, GOT IMMEDIATE ATTENTION AND WAS THE REASON FOR THE PRECAUTIONARY LANDING. AT THAT POINT, THOUGHT THERE WAS A FIRE IN THE ENGINE OR TRANSMISSION, ALTHOUGH THERE WERE NO OTHER INDICATIONS OF FIRE. 1 G 7 1 3U 3 U H9EU E19EU 2007031200064 20070312 00064 CE 2007 3 12 GLBA20060903 1 20070216 A 5610 10138402524 WINDOW BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE COCKPIT CRACKED A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 03 245GL UE245 ABORTED TAKEOFF, AIRCRAFT FLIGHT 5133, UPON ADVANCEMENT OF THROTTLE LEVERS A NEW CRACK APPEARED ON THE FIRST OFFICERS WI NDOW. APPROXIMATELY 12 INCHES IN LENGTH. OUTER PANE ONLY. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDOW IAW MM 56-10. OPERATIONAL CHECK OF WINDOW SYSTEM GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2007031200066 20070312 00066 CE 2007 3 12 GLBA20060884 1 20070112 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 289 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 122UX UE122 LT FUSELAGE LOWER SKIN, FORWARD SPAR FLANGE HAS (2) PULLED RIVETS WITH 1.2500 INCH CRACK AT F.S. 289.0 AND W.S. 29.06. REPAIRED CRACK AND RIVETS IAW SRM 53-90-18. 2 L 7 2 4T 4 T RT A24CE E26NE 2007031200069 20070312 00069 NM 2007 3 12 SWAA071290 1 20070308 A 2560 6557463 FITTING BOEING 737 737301 1384611 NM R1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FIT TING PER SRM. 2 L 7 2 4F RT A16WE 2007031200070 20070312 00070 NM 2007 3 12 SWAA071282 1 20070308 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031200071 20070312 00071 NM 2007 3 12 SWAA071272 1 20070308 A 3350 65C27093 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 765SW 29805 R2 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007031200073 20070312 00073 NM 2007 3 12 SWAA071280 1 20070308 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007031200075 20070312 00075 NM 2007 3 12 SWAA071278 1 20070308 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007031200079 20070312 00079 WP 2007 3 12 MWEA070039 1 20070301 A 5330 5924802509 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 808ME 48070 GOUGE/DENT IN FUSELAGE SKIN AT FRAME STATION 237 LEFT BETWEEN LONGERON 18 LEFT & LONGERON 17 LEFT. FABRICATED AND INSTA LLED FILLER. 2 L 7 2 4F A6WE 2007031200082 20070312 00082 NE 2007 3 12 ANCF200600045 2 20070202 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LEFT MALFUNCTIONED W ANCF E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 23 160BS 53463 P725956D ON TAKEOFF LT ENGINE PARAMETER DROOPED & EGT RAISED UP TO 610. POWER REDUCED AND EPR 1.61 N1 57 PERCENT N2 62 PERCENT A DVANCING LT THROTTLE THERE WAS NO REACTION AND ENGINE WAS SHUTDOWN. 2 MINUTES BEFORE LANDING, OIL PRESSURE NORMAL, OIL TEMP NORMAL. IAW AMM 77-11-01 CONF 1 PAG 202 WERE CHECKED BY LEAK AND WAS FOUND LEAK BY TUBE PT2 IAW AMM 77-11-03 PAG 201 CHANGE TUBE, ALSO WERE CHANGE FILTER MAIN IAW AMM 79-20-00 PAG 201. BOROSCOPIA IAW AMM 72-00-00 PAG 518 TABLE 504 ZONE C TEST RUNNING IAW AMM 71-00-00 PAG 501 TEST OK. PT2 TUBE PART 7938007-505. FILTER 815345. BY REQUIREMENT OF MAIN TENANCE REMOVE VOICE RECORDER: IAW AMM 23-70-01 PAG WAS REMOVE AND INSTALLED COCKPIT VOICE RECORDER AND WAS ACCOMPLISHE 2 L 7 2 4F 4 F RT A6WE E9NE 2007031200083 20070312 00083 CE 2007 3 12 GLBA20060917 1 20070226 A 5313 STRINGER BEECH 1900 1900D 1154162 CE BS 163 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 195GL UE195 UPON ROUTINE INSPECTIONS MAINTENANCE FOUND A STRINGER RELIEF HOLE CRACKED AT FS 163.9 RT STRINGER 9AL. MAINTENANCE REPA IRED THE AFFECTED AREA AT FS 163.9 RT STRINGER 9AL RELIEF HOLE IAW SRM 51-70 AND TC 8.2.1. 2 L 7 2 4T RT A24CE 2007031200086 20070312 00086 NM 2007 3 12 DHL2007751516 1 20070309 A 5311 FRAME BOEING 727 727264 138408M NM BS 950C CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 751DH 22982 AFT CARGO COMPT FRAME AT STA 950C IS CORRODED AT BOTTOM BETWEEN STR 29L AND 30L. CORROSION DMG EXCEEDS LIMITS PER B727 SRM 53-10-2 FIG 5. CUT OUT DAMAGE, FABRICATED SHEAR TIE REPAIR FROM 7075-T0, .080" BY 4.5" BY 1.5" BY 1", PO NR 9002619 PER B727 SRM 53-10-4 FIG 15 AND 51-20-1 FIG 7. HEAT TREATED REPAIR TO T6 IAW FASI EO REPORT 2-37153-801 REV IR. TREAT ED, PRIMED, AND INSTALLED REPAIR PARTS PER B727 SRM 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 2007031200088 20070312 00088 EU 2007 3 12 AWXA200700337 1 20070306 A 3350 321431 BATTERY PACK AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 655AW 1075 LAS - FOUND EMERGENCY LIGHTS FAILS L OVERWING. MX REPLACED POWER SUPPLY REF MM 33-51-38 P401 AND BATTERY PACK REF TASK CARD A1C33302, OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 2007031200089 20070312 00089 EU 2007 3 12 AWXA200700338 1 20070306 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 642AW 47606 4707 584 ORD - FOUND RT OVERWING EMERGENCY POWER SUPPLY UNIT INOP. MX REMOVED AND REPLACED RT EMER PSU 12WL IAW MM 33-51-38. OP S CHECK GOOD. 2 L 7 2 4F RT A28NM 2007031200092 20070312 00092 NM 2007 3 12 AWXA200700330 1 20070213 A 5310 6545871515 DOOR FRAME BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND R1 DOOR AFT FRAME CRACKED, BS 329 AT THE 3RD AND 4TH STOP PIN FITTING FROM THE TOP. REPAIRED R1 DOOR AFT FR AME, BS 329 AT THE 3RD AND 4TH STOP PIN FITTING FROM THE TOP IAW AWA ER 03-5240-07059-ES1 2 L 7 2 4F RT A16WE 2007031200093 20070312 00093 NM 2007 3 12 AWXA200700323 1 20070303 A 5753 6546431 SKIN BOEING 737 7373B7 1384580 NM FORE FLAP DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 23384 PHX - RIGHT WING OUTBOARD FOREFLAP IS DISBONDED ON UPPER AND LOWER SKIN TRAILING EDGE, WBL 202.69 - WBL 413.61, APPROX 7 INCHES LONG. REPAIRED RIGHT WING OUTBOARD FOREFLAP UPPER AND LOWER SKIN TRAILING EDGE, WBL 202.69 - WBL 413.61 IAW B73 7-300 SRM 51-70-10-2R. 2 L 7 2 4F RT A16WE 2007031200095 20070312 00095 EA 2007 3 12 TRAX200700305 1 20070228 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 821AS 7194 LEFT FS 484 INTERCOSTAL CRACKED ON I/B SIDE. REMOVED DAMAGED CLIP FROM L/H FS 484 INTERCOSTAL I/B SIDE. FABRICATED SERVI CEABLE CLIP USING 2024-T3, .063", PO# 8743-1. ALODINED, PRIMED, AND PAINTED IAW CRJ SRM 51-25-16. INSTALLED CLIP IAW REO -601R-53-41-059. 2 L 7 2 4F RT A21EA 2007031200098 20070312 00098 NM 2007 3 12 AWXA200700326 1 20070221 A 5320 D53112198201 FITTING AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 803AW 931 SAL - FOUND CORROSION ON R1 DOOR SILL CENTER FITTING, FR16 + 6". REPLACED R1 DOOR SILL CENTER FITTING, FR16 - FR 20 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007031200106 20070312 00106 EA 2007 3 12 TRAX200700307 1 20070228 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 821AS 7194 RIGHT FS 484 INTERCOSTAL CRACKED ON I/B SIDE. 2 L 7 2 4F RT A21EA 2007031200107 20070312 00107 NM 2007 3 12 AWXA200700342 1 20070213 A 5210 SKIN BOEING 737 7373S3 1384711 NM ZONE 800 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 1388 24060 MCN - FOUND CRACKED L2 DOOR SKIN AT THE UPPER HINGE CUT OUT, BETWEEN BEAM 2 AND BEAM 4. REPAIRED L2 DOOR SKIN AT THE UP PER HINGE CUT OUT, BETWEEN BEAM 2 AND BEAM 4 IAW ER 03-5200-07066-ES1. 2 L 7 2 4F RT A16WE 2007031200111 20070312 00111 NM 2007 3 12 HALA0700086 1 20070305 A 2613 89873202 CIRCUIT CARD BOEING 767 767300 1385204 NM OVERHEAT UNKNOWN A HALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 13 585HA 24257 BTB - ETOPS SIGNIFICANT SYSTEM, L ENG OH LP 1 AFTER START. REPLACED NR 1 ENG OVERHEAT DETECT CARD M687 PER AMM 26-10-01 . OPS CHK OK ON GROUND RUN CHECKED GOOD, NO DEFECTS NOTED. 2 L 7 2 4F RT A1NM 2007031200112 20070312 00112 EA 2007 3 12 TRAX200700310 1 20070302 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 920EV 7810 CABIN EMERGENCY TRACK LIGHTS, CENTER SECTION INOP. 2 L 7 2 4F RT A21EA 2007031200126 20070312 00126 NM 2007 3 12 DL76L070195 1 20070308 A 2410 IDG BOEING 767 767332 1382001 NM LEFT FAILED A DALA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 SO 27 198DN 28455 P2119 ON ENGINE START LT ENG GEN DRIVE LIGHT ILLUMINATED. BPCU FAULTS IDG PRESS SW WIRING/UNDER FREQ TRIP. SWAPPED GCU NO HE LP. REMOVED AND REPLACED LT IDG PER AMM. LEAK AND OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2007031200129 20070312 00129 EU 2007 3 12 07FDEA00423 1 20070209 A 5753 SKIN AIRBUS 310 A310203 3930313 EU TE FLAP MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 409FE 273 PREVIOUS REPAIR FOUND LOCATED ON THE RT INBOARD FLAP VANE, UPPER SURFACE OUTBOARD END. REPAIR REQUIRES EVALUATION FOR M AJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUN D NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED WITH FEDEX EA 6-5720-105666. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS 'MAJOR'. 2 L 7 2 4F RT A35EU 2007031200135 20070312 00135 EA 2007 3 12 TRAX200700313 1 20070302 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 681BR 7680 FLIGHT ATTENDANT'S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007031200140 20070312 00140 WP 2007 3 12 07FDEA00657 1 20070305 A 5230 FITTING DOUG MD10 MD1010F 3022112 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 566FE 46989 FOUND MAIN CARGO DOOR NR 6 SPOOL FITTING HAS CRACK INDICATION. 2 L 7 3 4F RT A22WE 2007031200144 20070312 00144 WP 2007 3 12 ARWA20070301 1 20070308 A 5610 WINDOW DOUG DC10 DC1010 3022110 WP COCKPIT DISLODGED A ARWA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 19 68041 46900 ON TAKEOFF ROLL ,F/O SLIDING WINDOW CAME OFF TRACK CAUSING LOW SPEED ABORT. PREFLIGHT INSPECTION OVER CENTER LOCKED AND NORMAL. LUBRICATED INSPECTED AND ADJ. SLIDING WINDOW CHECKED OPERATION SEVERAL TIMES AND FOUND NORMAL IAW DC-10 MM 56- 12-00. 2 L 7 3 4F A22WE 2007031200146 20070312 00146 EA 2007 3 12 TRAX200700315 1 20070227 A 5242 HOUSING CNDAIR CL600 CL6002C10 1390015 EA E&E DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 709EV 10068 AVIONIC DOOR OUTER HANDLE HOUSING CRACKED AROUND BOSS. REMOVED AND REPLACED AVIONICS DOOR HANDLE PER CRJ700 SRM 51-42-06 AND SRM 51-21-16. PRESSURIZATION LK CK GOOD IAW CRJ 700 MM 21-30 2 L 7 2 4F RT A21EA 2007031200152 20070312 00152 CE 2007 3 12 DJFA2007022 1 20070222 A 5522 45A220046 SKIN RAYTHN BEECH MU300 400A 1155402 CE RT ELEVATOR CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 417LX 6610 RK230 DURING A SCHEDULED MAINTENANCE EVENT, MAINTENANCE DISCOVERED A CRACK ON THE RH ELEVATOR LOWER SKIN APPROX. 9.5 INCHES FR OM THE INBD END. THE CRACK TRANSECTS A RIVET HOLE FROM LEFT TO RIGHT AND IS APPROX .75" IN LENGTH. THE ELEVATOR WAS RE PLACED. 2 H 7 2 4F RT A16SW 2007031200164 20070312 00164 EA 2007 3 12 TRAX200700323 1 20070305 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 970EV 7527 EMERGENCY FLOOR TRACK LIGHTING FROM 8CD TO 12CD INOP. 2 L 7 2 4F RT A21EA 2007031200165 20070312 00165 EA 2007 3 12 TRAX200700324 1 20070305 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 874AS 7551 FLAPS FAIL AT 0 ON APPROACH. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007031200168 20070312 00168 2007 3 12 MWEA070038 4 20070225 A 2565 D29985107 SLIDE DOUG DC9 DC982 3022082 WP GALLEY DOOR UNSERVICEABLE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 809ME 48071 AFT GALLEY SERVICE DOOR EMERGENCY SLIDE GAUGE SHOWS -NO GO-. REMOVED AND REPLACED AFT GALLEY SERVICE DOOR EMERGENCY SLI DE. 2 L 7 2 4F A6WE 2007031200172 20070312 00172 NM 2007 3 12 HNAA0700042 1 20070227 A 5343 STRUCTURE DHAV DHC8 DHC8102 2809003 NM NLG WW CRACKED A HNAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 07 815EX 321 RED NOSE GEAR ADVISORY LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION. CREW DECLARED AND EMERGENCY, CYCLED GEAR BUT IN DICATION REMAINED UNSAFE, PERFORMED SEVERAL TOWER FLYBY'S AND GEAR APPEARED TO BE DOWN. FLIGHT LANDED SAFELY. FOUND SE VERAL LARGE CRACKS IN THE NOSE GEAR DECK. REPAIRED DECK AND SURROUNDING STRUCTURE IN ACCORDANCE WITH ENGINEERING ORDER EO8-53-07-3059. 2 H 7 2 4T RT A13NM 2007031200173 20070312 00173 NM 2007 3 12 HNAA0700043 1 20070227 A 3350 0L3071BPEGPL LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 934HA 47479 70 134 CABIN AISLE ESCAPE PATH LIGHTING LIGHT NR 21 IS INOP. RELAMPED LIGHT. 2 H 7 2 4T RT A13NM 2007031200174 20070312 00174 NM 2007 3 12 HNAA0700044 1 20070227 A 3350 OL3071BPEGPL LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 934HA 47479 70 134 CABIN AISLE ESCAPE PATH LIGHTING IS INOP. RELAMPED LIGHTING. 2 H 7 2 4T RT A13NM 2007031200178 20070312 00178 WP 2007 3 12 ABXA070062 1 20070216 A 5210 9915565159 FITTING DOUG DC9 DC941 302207N WP ENTRY DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 AFT ENTRY DOOR CENTER BEAM RIGHT END FITTING WAS CRACKED. REMOVED AND REPLACED ANGLES IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 2007031200179 20070312 00179 WP 2007 3 12 ABXA070063 1 20070219 A 5412 99122433 WEB DOUG DC9 DC941 302207N WP LT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 LEFT AFT PYLON BULKHEAD WEB AT STA 1117 CRACKED AROUND LIGHTNING HOLE AT LONGERON 12 LEFT. STOP DRILLED CRACK AND REPAI RED IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 2007031200180 20070312 00180 WP 2007 3 12 ABXA070065 1 20070222 A 5347 S2914913M24000 SEAT TRACK DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 SEAT TRACK AT RIGHT BUTT LINE 44, APPROXIMATELY STA 330 - CORRODED. REMOVED AND REPLACED TRACK RIGHT BUTT LINE 44, STA 200 - 285 IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 2007031200183 20070312 00183 NM 2007 3 12 ABXA070056 1 20070212 A 5230 140T26033 BEAM BOEING 767 767281 1385109 NM CARGO DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 FORWARD LOWER CARGO DOOR BEAM BELOW VENT DOORS WAS CORRODED AT NUT PLATE HOLES. REPLACED DOOR BEAM AS REQUIRED IAW B767 SRM. 2 L 7 2 4F RT A1NM 2007031200188 20070312 00188 2007 3 12 HNAA0700046 4 20070225 A 3418 COMPUTER DHAV DHC8 DHC8102 2809003 NM STALL WARNING FAULTY A HNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 07 937HA 46942 46942 148 STALL WARNING STICK SHAKER ACTIVATED IN FLIGHT, ALSO NOTED F/O'S FAST/SLOW INDICATOR READING SLOW. REMOVED AND REPLACED RIGHT LIFT TRANSDUCER. EVENT REOCCURRED FOLLOWING DAY, CREW DECLARED AND EMERGENCY LANDING TO GET A VISUAL APPROACH VI A ATC. STALL WARN ACTIVATED IN FLIGHT F/O SPEED BUG SHOWING SLOW ON ADI. REMOVED AND REPLACED NR 2 STALL WARNING COMPU TER. 2 H 7 2 4T RT A13NM 2007031200189 20070312 00189 2007 3 12 SWAA071271 4 20070308 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 434WN 32454 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007031200196 20070312 00196 EA 2007 3 12 TRAX200700325 1 20070305 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 355CA 10067 PAX DOOR W/N CLOSE, HAND RAIL PIN DIFFICULT TO REMOVE. FLT 4519 DEL 67 MINS. 2 L 7 2 4F RT A21EA 2007031200220 20070312 00220 WP 2007 3 12 ABXA070068 1 20070305 A 3350 60030451 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 939AX 1155 47201 COCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY SUPPLY POWER PACK IAW DC9 MM 33-53-00 . 2 L 7 2 4F A6WE 2007031200221 20070312 00221 SO 2007 3 12 RAIA00702040 1 20070225 A 3010 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO ANTI-ICE SYS MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 CE 03 811HK 145256 FLT NR 5496 - STL - WING ANTI-ICE FAIL IN FLIGHT. MAINTENANCE PERFORMED OPS CHECK OF ICE AND RAIN PROTECTION SYSTEM. C HECKS GOOD. 2 L 7 2 4T RT T00011AT 2007031200223 20070312 00223 NM 2007 3 12 FDKA200702075 1 20070220 A 3350 1013073 LIGHT DHAV DHC8 DHC8101 2809002 NM CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 809LR 083 FDM 6206 JFK-PVD (1142 PHX LCL). ROW 2 AND 5 EMERGENCY FLOOD LIGHTS INOP. MX RELAMPED. 2 H 7 2 4T RT A13NM 2007031200224 20070312 00224 NM 2007 3 12 ABXA070053 1 20070227 A 3397 WIRE BOEING 767 767232 1385132 NM CONNECTOR OUT OF POSITION A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 740AX 22213 DOOR 1 LEFT EMERGENCY EXIT SIGN INOPERATIVE. FOUND WIRE M748-033-14, MIS-PINNED IN PIN 13 OF CONNECTOR D1084, REPOSITIO NED TO PIN 9 OF CONNECTOR D1084. OPS CHECKED GOOD IAW B767 MM 33-51-00-715-801. 2 L 7 2 4F RT A1NM 2007031200231 20070312 00231 EA 2007 3 12 TRAX200700301 1 20070228 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 880AS 7606 FLAP FAIL AT 0 DEGREE ON APPROACH. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007031200240 20070312 00240 EA 2007 3 12 TRAX200700291 1 20070224 A 5320 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 BONDED DOUBLER CRACK AFT 640 LT SIDE. INSTALLED UPPER AND LOWER BOX BEAM ANGLES PER REO 601R-53-61-506. JP 21771 JOB C OMPLETE. SUPPLEMENTAL - SDR CLOSED 03/02/07. 2 L 7 2 4F RT A21EA 2007031200251 20070312 00251 NM 2007 3 12 NOCA05207 1 20070305 A 3350 3071PBE LIGHT BOEING 767 76739H 1385311 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 760NA 26257 EMERGENCY EXIT LAMP INOP AT 18AB. RELAMPED EXIT LAMP AT 18AB, OPS OK. 2 L 7 2 4F RT A1NM 2007031200258 20070312 00258 WP 2007 3 12 FXG2007F00000 1 20070131 A 5753 BRACKET DOUG DOUG DC6 DC6B 3021712 WP PWA R2000 R2000* 52023 NE T/E FLAP BROKEN A FXGA O OTHER O OTHER NR NOT REPORTED 1 AL 01 151 504632 45496 AFTER FLIGHT MAINTENANCE FOUND THE OB ATTACH BRACKET AT THE OB END OF FLAP ASSY 5363998-501 BROKEN. THIS ALLOWED THE VA NE ASSY 5371802-1 TO COME LOOSE AND DAMAGE THE FLAP. REPLACE THE FLAP AND VANE ASSY. RETURNED AC TO SERVICE. (K) 2 L 7 4 4R 4 R 6A4 5E5 2007031200271 20070312 00271 EA 2007 3 12 SWIA200717964 1 20070208 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 863AS PAX DOOR - THE FWD WEB IS CRACKED UNDER THE HANDRAIL STOW BRACKET AND IN THE RADIUS BETWEEN THE 3RD & 4TH FIXED STEPS. (DISCOVERED DURING C-CHECK INSPECTION) INSTALLED EXTERNAL DOUBLER, REPAIR ANGLES & HANDRAIL STOW BRACKET ON THE FWD PAX DOOR SIDE PNL IAW CRJ200 REO 601R-52-11-702, REV A REPAIR ZONE 2. 2 L 7 2 4F RT A21EA 2007031300001 20070313 00001 EU 2007 3 13 07FDEA00661 1 20070306 A 2920 RAM AIR TURB AIRBUS 300 A300F4605R 3930327 EU UNWANTED DEPLOY A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 664FE 768 DURING WALKAROUND, FOUND RAT DEPLOYED, NOT SURE OF WHEN (INFLIGHT OR TAXI IN) RAT DEPLOYED. FLT CREW UNAWARE, CONTROLS WERE STILL SAFETIED IN C/P. VISUALLY INSP RAT FOR DEFECTS PER AMM 29-25-00-6. NO DEFECTS NOTED AT THIS TIME. STOWED R AT PER AMM SUP 29-25-00-3. CYCLED RAT, OPS NORMAL, RESTOWED PER AMM SUP 29-25-00-3. 2 L 7 2 4F RT A35EU 2007031300002 20070313 00002 WP 2007 3 13 07FDEA00662 1 20070306 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 FOUND MAIN CARGO COMPARTMENT SEAT TRACK AT LBL10 AT STA 1521 IS GOUGED. REMOVED AND REPLACED SEAT TRACK SECTION IAW DC/ MD10 SRM 51-31-01 VOL II,53-70-00 VOL I FIG 1 AND 5. MAJOR REPAIR MECH 110847, QC423. 2 L 7 3 4F A22WE 2007031300006 20070313 00006 NM 2007 3 13 07FDEA00666 1 20070306 A 5711 SPAR CAP DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RIGHT WING REAR SPAR UPPER CAP FOUND CORROSION AT XORS 1043. SUPPLEMENTAL 21 MARCH 07; CORROSION REMOVED ON RIGHT HAND WING REAR SPAR UPPER CAP XORS 1043 AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS = 0.119", MATERIAL REMOVED = 0.039" , REMAINED THICKNESS = 0.080" AND FOUND EXCEEDED LIMIT AS PER SRM 57-20-00 FIGURE 16 VOLUME I. REWORKED AREA REPAIRED AS PER FEDEX EA 1-5710-107801, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007031300009 20070313 00009 NM 2007 3 13 07FDEA00669 1 20070306 A 5343 FITTING DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 NOSE LANDING GEAR RIGHT FITTING FOUND CRACKED. CRACK ON NOSE LANDING GEAR RIGHT HAND FITTING TRIMMED OUT AS PER FEDEX E A 1-5310-107811, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. PER SRM 53-40-00 FIGURE 22 SHEET 4 VOLUME I, OPTION 2 : REPETITIVELY INSPECT FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS. 2 L 7 3 4F RT A22WE 2007031300012 20070313 00012 EU 2007 3 13 07FDEA00672 1 20070307 A 5313 LONGERON AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 FOUND CORROSION ON FLOOR SUPPORT STRUCTURE IN SEC 12. THE AFFECTED PARTS ARE SHOWN IN SRM 53-12-15 FIG.19, SHEET 3: ITE M 190,200 AND 275. REPAIR WAS PERFORMED IAW SRM 53-12-15, FIG 207 (ITEM 190 / 200) AND BY REPLACE A NEW PART IAW SRM 51 -72-10 (ITEM 275). 2 L 7 2 4F RT A35EU 2007031300019 20070313 00019 EU 2007 3 13 07FDEA00400 1 20070209 A 5210 SKIN AIRBUS 310 A310203 3930313 EU R2 DOOR MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 409FE 273 PREVIOUS REPAIR FOUND LOCATED ON LOWER SECTION OF NR 2 RT DOOR. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATIO N AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 52-30-00 FIG 203. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJO R". 2 L 7 2 4F RT A35EU 2007031300020 20070313 00020 NM 2007 3 13 UPS07649362 1 20070308 A 2560 INERTIA REEL BOEING 767 76734AF 1385212 NM COCKPIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 304UP 27242 4TH INERTIAL REEL FROM FWD INOP. REMOVED AND REPLACED INERTIAL REEL IAW MM 25-61-03-2. GROUND OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2007031300021 20070313 00021 WP 2007 3 13 070059 1 20070306 A 5730 SKIN DOUG DC9 DC983 3022083 WP WING CRACKED A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 883GA 49710 DURING A ROUTINE MAINTENANCE INSPECTION MAINTENANCE REPORTED AN APPARENT CRACK IN AN UPPER WING SURFACE PANEL AT APPROXI MATELY WING STATION 48.00. FURTHER INSPECTION REVEALED A CRACK OF APPROXIMATELY 13-INCHES LENGTH IN THE COMPOSITE PANEL AT WING STATION 47.95. A TEMPORARY REPAIR WAS ACCOMPLISHED ON THE CRACKED PANEL PER ENGINEERING REPAIR ORDER 5704-001. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007031300022 20070313 00022 NE 2007 3 13 YENA2007011 2 20070302 A 7532 8085745 FILTER EMB ERJ190 ERJ190100IGW 3260408 EU GE CF34 CF3410E6 30015 NE BLEED VALVE CLOGGED A YENA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 EA 15 198JB 2762 19000021 CLIMBING THROUGH 2500 FT RCVD BLEED ONE OVER PRESSURE EICAS MSG. PERFORMED QRH PROCEDURE WITH NO CHANGE IN THE FAULT. RETURN TO JFK. PERFORMED FIM TASK 36-14-00-810-838A. BLEED TROUBLESHOOT GUIDE. FOUND CLOGGED HIGH STAGE BLEED FILTER. REMOVED AND REPLACED HIGH STAGE VALVE FILTER AS PER MM 36-11-01/401. 2 L 7 2 4F 4 F RT A57NM E00070EN 2007031300023 20070313 00023 NM 2007 3 13 QXEA200700358 1 20070307 A 2730 3985001007 CONTROL UNIT BOMBDR DHC8 DHC8402 1390042 NM ELEVATORS MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 420QX 136 4147 SEA-BTM FLIGHT NR 2328: ELEVATOR ASSY CAUTION LIGHT ILLUMINATED. C/W CHECKLIST. DISENGAGED THE AUTO PILOT AND REDUCED AIRSPEED TO 200 KIAS. ALL FLIGHT CONTROLS WERE NORMAL. UPON THE LANDING ROLL-OUT, BELOW 40 KTS, THE ELEVATOR ASSY CAU TION LIGHT WENT OUT. THE FLIGHT WAS DIVERTED TO GEG. MAINTENANCE PERFORMED FIM TASK 24-30-00-810-801. ELEVATOR ASYMME TRY CAUTION LIGHT DID NOT COME ON DURING OPS TEST. CDS CURRENT FAULTS WERE 'ADC FAILURE' (X2) AND 'ELEV ASSY' FAILURE. ALL FAULTS CLEARED AND DID NOT REOCCUR AFTER OPS TEST. AS A PRECAUTIONARY MEASURE, PERFORMED GVI OF LT AND RT ELEVATOR PCU INSTALLATION. NO DEFECTS NOTED. CHECKED CDS ELE RIT STATUS. ASYMMETRY WITHIN LIMITS. REPLACED FCECU IAW AMM 27- 2 H 7 2 4T RT A13NM 2007031300024 20070313 00024 EU 2007 3 13 YENA200713 1 20070306 A 2131 2160903AD CONTROLLER EMB ERJ190 ERJ190100IGW 3260408 EU CABIN PRESSURE UNKNOWN A YENA B A EMER. DESCENT UNSCHED LANDING O OTHER DE DESCENT 1 EA 15 231JB 1915 19000033 WHILE DESCENDING FROM FL370 TO FL350 A/T DISCONNECT OCCURRED. THIS WAS FOLLOWED IMMEDIATELY BY A RAPIDLY RISING CABIN A LTITUDE. MAX CABIN ALT REACHED 9400-9500 FT. INITIATED EMERGENCY DESCENT. PRESSURIZATION RETURNED TO NORMAL AT 10,000 FT LEVEL OFF. ACCOMPLISHED VISUAL CHECK OF PACK DUCTS & LEAK CHECK INCLUDING CHECK OF BELLOWS. PRESSURIZED A/C MANUAL LY IAW CABIN PRESSURIZATION. FUNCTIONAL TEST AMM 21-31-720-802 STEP F1-G2. NO LEAKS NOTED. PERFORMED ENG 1 & ENG 2 EN GINE BLEED OPERATIONAL TEST IAW AMM 36-11-00-710-801-A ENG 1 & ENG 2 BLEED SYSTEMS OPS CHECK OK. AUTO THROTTLE SYSTEMS HZ, OPS CHECK OK IAW AMM 22-31-00-710. REMOVED AND REPLACED CPCS CONTROLLER PRECAUTIONARY PER AMM 21-31-01. FUNCTIONAL 2 L 7 2 4F RT A57NM 2007031300025 20070313 00025 EU 2007 3 13 YENA2007013 1 20070306 A 2130 2160903AD CONTROLLER EMB ERJ190 ERJ190100IGW 3260408 EU CABIN PRESSURE UNKNOWN A YENA B A EMER. DESCENT UNSCHED LANDING O OTHER DE DESCENT 1 EA 15 231JB 1915 19000033 WHILE DESCENDING FROM FL370 TO FL350 A/T DISCONNECT OCCURRED. THIS WAS FOLLOWED IMMEDIATELY BY A RAPIDLY RISING CABIN A LTITUDE. MAX CABIN ALT REACHED 9400-9500 FT. INITIATED EMERGENCY DESCENT. PRESSURIZATION RETURNED TO NORMAL AT 10,000 FT LEVEL OFF. ACCOMPLISHED VISUAL CHECK OF PACK DUCTS & LEAK CHECK INCLUDING CHECK OF BELLOWS. PRESSURIZED A/C MANUAL LY IAW CABIN PRESSURIZATION. FUNCTIONAL TEST AMM 21-31-720-802 STEP F1-G2. NO LEAKS NOTED. PERFORMED ENG 1 & ENG 2 EN GINE BLEED OPERATIONAL TEST IAW AMM 36-11-00-710-801-A ENG 1 & ENG 2 BLEED SYSTEMS OPS CHECK OK. AUTO THROTTLE SYSTEMS HZ, OPS CHECK OK IAW AMM 22-31-00-710. REMOVED AND REPLACED CPCS CONTROLLER PRECAUTIONARY PER AMM 21-31-01. FUNCTIONAL 2 L 7 2 4F RT A57NM 2007031300026 20070313 00026 NM 2007 3 13 07FDEA00681 1 20070307 A 5340 654531313 STRINGER CLIP BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FOUND MAIN DECK BODY FRAME STRINGER CLIP IS CRACKED AT BS 950D, STR 9L. REMOVED DAMAGED CLIP REF SRM 51-30-2. INSTALLE D NEW CLIP REF SRM 51-30-2. 2 L 7 3 4F A3WE 2007031300027 20070313 00027 EA 2007 3 13 QXEA200700364 1 20070310 A 2150 GG43620041 SENSOR CNDAIR CL600 CL6002C10 1390015 EA LT A/C PACK MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 615QX 10065 PDX - FLIGHT 2518 - LEFT AIR CONDITIONING PACK CYCLES OFF AND ON SEVERAL TIMES IN FLIGHT. LEFT PACK SELECTED OFF PER TH E CHECKLIST PROCEDURE. LEFT PACK READINGS OBSERVED TO BE ERRATIC AND VARIABLE WITH PACK ON OR OFF. MAINTENANCE PLACED ON MEL 21-51-1A. 3/11. MAINTENANCE REPLACED THE LEFT PACK INLET TEMP SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F RT A21EA 2007031300028 20070313 00028 EA 2007 3 13 QXEA200700365 1 20070310 A 2720 530113 CONTROL MODULE CNDAIR CL600 CL6002C10 1390015 EA RUDDER PEDALS MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 613QX 13672 10045 PDX - FLIGHT 2533, PRESSING THE RIGHT RUDDER PEDAL CAUSES THE AIRCRAFT TO TURN TO THE LEFT. PRESSING THE LEFT RUDDER PE DAL CAUSES THE AIRCRAFT TO TURN RIGHT. THE STEERING TILLER WORKS NORMALLY. RETURNED TO THE GATE. MAINTENANCE REPLACED THE RUDDER PEDAL INPUT COMMAND MODULE (RVDT). OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007031300029 20070313 00029 NM 2007 3 13 QXEA200700362 1 20070311 A 3060 RELAY DHAV DHC8 DHC8202 2809007 NM PROP DEICE SYS MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 348PH 484 SEA FLIGHT NR 203, NR 1 PROP SHOWED NR 2 LIGHT WAS STUCK ON DURING FLIGHT WITH NR 2 PROP TIMER AT -10 BELOW. LT VAR AC B PHASE INDICATED .28 LOAD WHILE LIGHT WAS STUCK ON. LIGHT WENT OUT AND B PHASE RETURNED TO NORMAL. MAINTENANCE REPLAC ED PROP DEICE RELAY 3061-K1 AND K3. PERFORMED FUNCTIONAL TEST OF PROP DEICE IAW Q200 AMM 30-60-00-720-801. FUNCTION TE ST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007031300030 20070313 00030 NM 2007 3 13 QXEA200700361 1 20070311 A 2430 GENERATOR DHAV DHC8 DHC8202 2809007 NM NR 2 DC OVERHEATED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 354PH 498 SEA FLIGHT NR 2116 - DURING TAXI, NR 2 DC GEN HOT CAUTION ILLUMINATED. AFTER TURNING OFF NR 2 DC GENERATOR (AS PER CHEC KLIST) CAUTION EXTINGUISHED AFTER APPROXIMATELY 2 MINUTES. MAINTENANCE REPLACED NR 2 DC GENERATOR IAW MTC 9801001. PER FORMED FUNCTIONAL TEST OF THE DC GENERATORS IAW AMM TASK 24-31-00-720-801. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED T O SERVICE. 2 H 7 2 4T RT A13NM 2007031300040 20070313 00040 2007 3 13 070058 4 20070305 A 2312 UNKNOWN DOUG DC9 DC983 3022083 WP VHF RADIOS UNKNOWN A WX0A A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 WP 19 864GA 49912 FLIGHT 833 PIE/SBN - DURING CLIMB-OUT, FLT CREW REPORTED THAT BOTH THE CAPTAIN'S & FIRST OFFICER'S VHF RADIOS WERE INTER MITTENT USING EITHER HEADSET OR HAND MIC. THE ISSUE WAS TRANSMISSION RATHER THAN RECEPTION. RETURNED TO POINT OF DEPAR TURE & LANDED WITHOUT INCIDENT. MX REPORT THAT VHF TRANSCEIVERS NR 1 & 2 WERE REMOVED, CONNECTORS CLEANED/INSPECTED, AN D RE-INSTALLED IN ORIGINAL POSITIONS. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 23-20-00. THE AIRPLANE WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007031300041 20070313 00041 WP 2007 3 13 070054 1 20070224 A 5520 STRUCTURE DOUG DC9 DC982 3022082 WP LT ELEVATOR GROUND DAMAGE A WX0A D RETURN TO BLOCK W INADEQUATE Q C TX TAXI/GRND HDL 1 WP 19 881GA 49708 FLIGHT 475 FSD/LAS - DURING THE DE-ICING OPERATION THE EQUIPMENT OPERATOR STRUCK THE AIRPLANE ON THE LEFT ELEVATOR AT TH E AFT OUTBOARD CORNER. AMERICAN AIRLINES PERSONNEL REPORT THAT THEY REMOVED AND REPLACED THE LEFT ELEVATOR TRAILING EDG E. REF SRM 55-01-00. PERFORMED MEGGER CHECK FOR REMOVE/REPLACE OF STATIC WICK PER AMM 23-60-00-5. ELEVATOR BALANCE CH ECKED AND WEIGHT REMOVED AT NOSE CAP STATION 41.5. VALANCE TAG UPDATED PER SRM 55-20-01, PARAGRAPH 18.A.(9)(C) AND AMER ICAN AIRLINES ERO 5520-01. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007031300042 20070313 00042 NM 2007 3 13 UPS07449296 1 20070214 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 1960 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C BULK CARGO LT STA 1960 LBL 56" FLOOR SUPPORT CORRODED AS MARKED. CORROSION BLEND OUT 0.025" X .5" X 1 " EXCEED SRM 53-10-01 FIG 1 LIMITS, BULK CARGO COMPT FLOOR SUPPORT REPLACED WITH EXISTING SPLICE FROM BS 1920-1970 LBL 5 5 - 57" PER SRM 51-10-01 PG 9 & INSTALLED PER SRM 51-30-02 REF NRC NO AFQ516607 FOR DETAIL. 2 L 7 4 4F A20WE 2007031300043 20070313 00043 NM 2007 3 13 UPS07449313 1 20070220 A 5320 65B089309 WEB BOEING 747 747121 1384871 NM BS 1500-1520 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C AFT CARGO COMPT LT VERTICAL WEB FOUND CRACKED AT STA 1500 TO STA 1520 STR 34L AFT EDGE AREA. CRACK LE NGTH .75 INCH. VERTICAL WEB REPLACED PER SRM 51-10-01 PG 9. 2 L 7 4 4F A20WE 2007031300044 20070313 00044 NM 2007 3 13 UPS07449345 1 20070215 A 5740 69B024453 ATTACH FITTING BOEING 747 747121 1384871 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT WING L/E RIB TO FRONT SPAR UPPER CHORD ATT FITTING AT ISLES 270 FOUND CRACKED. CRACK LENGTH: .25 INCH. UPPER CHORD ATT CLIP REPLACED PER SRM 51-10-01 PG 9 & INSTALLED PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007031300045 20070313 00045 NM 2007 3 13 UPS07449346 1 20070213 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 860 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 860 LBL 47 TO 49 FLOORBEAM WEB FOUND CRACKED. CRACK LENGTH: .75 INCH. M/D FLOORBEAM WEB REPA IRED AS PER SRM 53-10-07 FTG 11 JUST AT BS 860 BETWEEN LBL 39 & LBL 49. 2 L 7 4 4F A20WE 2007031300046 20070313 00046 NM 2007 3 13 UPS07449347 1 20070216 A 5320 SILL BOEING 747 747121 1384871 NM BS 400 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C U/D RIGHT DOOR SILL BS 400 RBL TO FLOOR SUPPORT CHORD FOUND CRACKED. CRACK LENGTH: .75 INCH. FLOOR SUPPORT CHORD REPAIRED AS PER SRM 51-40-04 FIG 1. 2 L 7 4 4F A20WE 2007031300047 20070313 00047 NM 2007 3 13 UPS07449348 1 20070214 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1820 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C AFT CARGO LEFT STA 1820 FRAME LBL 90 FOUND CORRODED UNDER ANCHOR NUT AREA AS MARKED. CORROSION BLEND OUT 0.020" X .5" X .5" EXCEED SRM LIMIT. AFT CARGO LEFT BS 1820 FRAME LBL 90" AREA REPAIRED AS PER SRM 51-40-03 FIG 2. 2 L 7 4 4F A20WE 2007031300048 20070313 00048 NM 2007 3 13 UPS07449349 1 20070214 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 1940 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 1940 RBL 89 TO 92 FLOORBEAM UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.082" X 1" X 1" EXCEED SRM LIMIT. M/D BS 1940 RBL 70" TO 92" RIGHT O/B FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 3. 2 L 7 4 4F A20WE 2007031300049 20070313 00049 NM 2007 3 13 UPS07449350 1 20070213 A 5730 SKIN BOEING 747 747121 1384871 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT WING UPPER SURFACE I/B LEADING EDGE SKIN FOUND CRACKED AT WS 450 AFT NR 12 K/FLAP. LEFT WING UPP ER SURFACE LEADING EDGE SKIN REPAIRED AS PER SRM 57-30-04 FIG 2. 2 L 7 4 4F A20WE 2007031300050 20070313 00050 NM 2007 3 13 UPS07449352 1 20070215 A 5420 WEB BOEING 747 747121 1384871 NM NR 1 NACLLE MISREPAIRED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C NR 1 PYLON LWR WEB CRACK PREVIOUS REPAIR DOES NOT APPEAR TO COVER ENTIRE CONDITION. CRACK LENGTH .75 INCH. WEB REPAIRED PER SRM 54-10-03 FIG 2. 2 L 7 4 4F A20WE 2007031300051 20070313 00051 NM 2007 3 13 UPS07449353 1 20070214 A 5310 FRAME BOEING 747 747121 1384871 NM BS 1840 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C AFT CARGO LEFT STA 1840 FRAME LBL 90 FOUND CORRODED UNDER ANCHOR NUT AREA AS MARKED. CORROSION BLEND OUT 0.024" X .875" X 1" EXCEED SRM LIMIT. AFT CARGO BS 1840 LBL 90" FRAME REPAIRED AS PER SRM 51-40-03 FIG 2. 2 L 7 4 4F A20WE 2007031300052 20070313 00052 NM 2007 3 13 UPS07449357 1 20070215 A 5210 FRAME BOEING 747 747121 1384871 NM R4 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D R4 DOOR UPPER FWD FRAME FOUND CRACKED. CRACK LENGTH 1.25 INCH. FWD FRAME REPAIRED AS PER SRM 52- 10-02 FIG 10. 2 L 7 4 4F A20WE 2007031300053 20070313 00053 SO 2007 3 13 LR7A07014 1 20070226 A 5320 3431947 STRUT LKHEED 382 382G 526414U SO FS 858 FRACTURED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 862 4698 DURING SCHEDULED A CHECK PER JOB CARD HA1200, FOUND TUBE STRUT FRACTURED AT FS858 RH. REPLACED TUBE STUT IAW SMP583 51- 10 PG3, LOG PAGE 23378 ITEM M1. 2 H 7 4 4T A1SO 2007031300054 20070313 00054 EU 2007 3 13 07FDEA00677 1 20070307 A 5540 HINGE FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 300 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 FOUND CORROSION INSIDE OF FORK ON RUDDER HINGE FITTING NR 5, NR 6 AND NR 7. REPAIR WAS PERFORMED IAW EA 6-5546-106387 I NCLUDES REPAIR REF.: TD/K4/S1/21625/2006/A AND IS APPROVED BY RAS/DAHAM/4021625/2008 ISS B. 2 L 7 2 4F RT A35EU 2007031300055 20070313 00055 NM 2007 3 13 07FDEA00678 1 20070307 A 5311 FRAME BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FRAME 277 IS CRACKED IN THE RADIUS OF CUT OUT FOR STRINGER 16R DISPLACED WIRING FOR ACCESS. VERIFIED CRACK, REMOVED FAS TENERS AND DAMAGE, VERIFIED DAMAGE REMOVED AND MATERIAL LOSS. FABRICATED, TREATED AND INSTALLED DOUBLER, FILLER AND C LIP REF SRM 51-40-2 FIG 1 AND SRM 51-30-2. RESECURED DISPLACED WIRING FOR ACCESS. 2 L 7 3 4F A3WE 2007031300056 20070313 00056 EU 2007 3 13 07FDEA00679 1 20070307 A 5730 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 FOUND CORROSION AROUND TWO FASTENERS BETWEEN RIB 7-8 AT STRINGER 19 ON RT WING BOTTOM SKIN. REPAIR WAS PERFORMED IAW EA 6-5721-106402, APPROVED BY RAS/BAE/1004132/2007. 2 L 7 2 4F RT A35EU 2007031300057 20070313 00057 NM 2007 3 13 07FDEA00680 1 20070307 A 5347 BAC1520792 SEAT TRACK BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FOUND MAIN DECK FS 500 AND FS 525, LBL 26 SEAT TRACK CORRODED, DUE TO BEING PREVIOUSLY BLENDED AND NO PROTECTIVE FINISH APPLIED. REMOVED SEAT TRACK. FABRICATED NEW SEAT TRACK FROM BAC 1520-792, 7178T6511. INSTALLED NEW SEAT TRACK FROM BS 480-680 10 AT LBL 26, REF SRM 51-30-2, 53-30-2, 51-30-5 AND FX GMM 7-0-1001. FASTENER HOLES FOR INTERCOSTAL WEB AT BS 560-580 TO BE DRILLED ON WEB INSTALLATION ON SNRM NR N01084. 2 L 7 3 4F A3WE 2007031300058 20070313 00058 NM 2007 3 13 QXEA200700357 1 20070308 A 2110 SWITCH DHAV DHC8 DHC8202 2809007 NM UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 352PH 494 SEA FLIGHT NR 2194, AFTER TAKING PROPS OUT OF FEATHER INTERMITTENT DEICE PRESSURE CAUTION LIGHT. DEICE PRESSURE INDICAT ES 12-14 PSI WITH POWER LEVERS AT DISC AND FLIGHT IDLE. MAINTENANCE REPLACED NR 1 ENG AND NR 2 ENGINE 55PSI AND 65PSI S WITCHES IAW Q200 AMM 21-11-21-000-801 AND 21-11-21-400-801. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007031300059 20070313 00059 WP 2007 3 13 UPS07849331 1 20070221 A 5712 RIB DOUG DC8 DC873F 302199F WP LWS 765 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C3 CRACKED UPPER RIB INSIDE PANEL 518A ON LEFT WING OUTBOARD LEADING EDGE. STOP DRILLED CRACK ON UPPER RIB INSIDE PANEL 518A LEFT WING OUTBOARD LEADING EDGE IAW SRM 57-02-00 FIG 002. FABRICATED AND INSTALLED ANGLE DOUBLER ON RIB INSIDE PANEL 518A ON LEFT WING OUTBOARD LEADING EDGE IAW SRM 57-02-00 FIG 002, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007031300060 20070313 00060 WP 2007 3 13 070060 1 20070307 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A WX0A O OTHER O OTHER CR CRUISE 1 WP 19 878GA 53487 FLIGHT 716 LAN/SFB - CABIN CREW REPORTED THAT THE FORWARD CABIN EXIT SIGNS FLICKERED ON AND OFF THROUGHOUT THE FLT. SAN FORD MAINTENANCE REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK (POSITION AND PART NUMBER NOT REPORTED). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007031300061 20070313 00061 WP 2007 3 13 070061 1 20070309 A 3350 1315 LAMP DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT NO TEST A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 868GA 49554 DURING A ROUTINE OVERNIGHT SERVICE CHECK MAINTENANCE INSPECTION RENO MAINTENANCE REPORTED THAT 2 CEILING MOUNTED EMERGEN CY LIGHTS DID NOT TEST. RENO MAINTENANCE ALSO REPORT THAT THEY RELAMPED THE FIXTURES. A SATISFACTORY OPERATIONAL TEST WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007031300062 20070313 00062 WP 2007 3 13 070062 1 20070309 A 3350 60030431 POWER SUPPLY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A WX0A O OTHER O OTHER CR CRUISE 1 WP 19 878GA 53487 FLIGHT 708 DSM/SFB, THE CABIN CREW REPORT THAT THE EMERGENCY EXIT LIGHT AT THE R2 DOOR FLICKERS IN FLIGHT. SANFORD MAIN TENANCE REPORT THE REMOVAL AND REPLACEMENT OF THE ASSOCIATED POWER SUPPLY UNIT. A SATISFACTORY OPERATIONAL TEST WAS ACC OMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007031300063 20070313 00063 WP 2007 3 13 070065 1 20070311 A 3350 AD4002P BATTERY PACK DOUG DC9 DC987 3022087 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 945MA 49725 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION ST. PETERSBURG MAINTENANCE REPORTED THAT THE EMERGENCY LIGHTS AT SEA T ROWS 21 AND 22 WOULD NOT TEST. ST. PETERSBURG MAINTENANCE FURTHER REPORT THE REMOVAL AND REPLACEMENT OF THE APPROPRIA TE EMERGENCY LIGHT POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007031300064 20070313 00064 WP 2007 3 13 070057 1 20070302 A 3350 57761 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 869GA 53294 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION LAS VEGAS MAINTENANCE REPORTED THAT THE EMERGENCY EGRESS PATH LIGHTI NG FROM SEAT ROW 30 TO SEAT ROW 35 WOULD NOT TEST. FURTHER, THEY REPORT THE REMOVAL AND REPLACEMENT OF AN EMERGENCY LIG HT POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RET URNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007031300065 20070313 00065 WP 2007 3 13 IXXA07SMN039S 1 20070119 A 5330 564932975N1 SKIN DOUG DC8 DC871F 302199D WP ZONE 100 MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2944 46065 DURING ROUTINE C CHECK INSPECTION, FOUND AN IMPROPER REPAIR AT STATION FS1710, LONGERON 34 LEFT. REMOVED DAMAGED SKIN P ANEL. CLEANED TREATED AND PRIMED AREA AND NEW SKIN PANEL. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN PANE L FROM STATION 1696 TO STATION 1890 FROM LONGERON 28 RIGHT TO LONGERON 28 LEFT IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, DC8 SRM 53-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 53-5-1 FIGURE 1 ITEM "E", DC8 SRM 51-1-8B, DC8 SRM 51-1-11, BOEING MESSAGE NUMBER 1-271850875-2 DATED 01-10-07. 2 L 7 4 4F RT 4A25 2007031300066 20070313 00066 WP 2007 3 13 IXXA07SMN040S 1 20070119 A 5754 5751185506 SUPPORT FITTING DOUG DC8 DC871F 302199D WP ZONE 600 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND A CRACKED OUTBOARD FLAP HINGE SUPPORT FITTING ON THE RIGHT WING AT STATION XF21 3.000. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8, SRM 51-3-1, DC8 SRM 5 1-1-21,DC8 SRM 51-3-0 AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007031300070 20070313 00070 WP 2007 3 13 IXXA07SMN043S 1 20070119 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 DAMAGED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HAND WING OUTBOARD SLOT VANE HOLES ELONGATED AT STATION XOLDI6.225. REMO VED EXISTING INTERNAL DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAM AGE REMOVED. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SU RFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 NDT SPM PART 06-10.01.001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SEMAN DRAWING NUMBER ED-4425 DATED 01-17-07 AND COMPLETED FAA FORM 8110- 3 NUMBER 07019 DATED 01-18-07. 2 L 7 4 4F RT 4A25 2007031300071 20070313 00071 WP 2007 3 13 IXXA07SMN047S 1 20070119 A 5751 FITTING DOUG DC8 DC871F 302199D WP ZONE 600 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD AILERON FITTING CRACKED BETWEEN STATION XA494.000 AND XA504. 000. REPLACED AILERON HINGE FITTING IAW DC8 SRM 51-1-21, 51-1-20D AND 51-3-0, 51-3-1. 2 L 7 4 4F RT 4A25 2007031300072 20070313 00072 WP 2007 3 13 UPS07849332 1 20070221 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FS 1400 L23R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C1 HFEC INSPECTED DETECTED A CRACK ON THE D-PIT UPPER FWD CORNER APPROX .156" ON LWR SIDE OF FASTENER AN D .156" UPPER SIDE OF FASTENERS. CUT OUT DAMAGED AREA AT STA 1400 L23R IAW SRM 53-2-0 FIG 21. FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER, AND TRIPLER AT STA 1400 L23R D-PIT UPPER FWD DOOR CORNER IAW SRM 53-2-0 FIG 21 AND SRM TR 53-18 8. 2 L 7 4 4F RT 4A25 2007031300073 20070313 00073 NM 2007 3 13 SWAA071303 1 20070311 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHT LENS CRACKED ABOVE AFT F/A'S SEAT. REMOVED AND REPLACED LIGHT LEN S. 2 L 7 2 4F RT A16WE 2007031300074 20070313 00074 NM 2007 3 13 SWAA071297 1 20070307 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 500C S19R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007031300075 20070313 00075 NM 2007 3 13 SWAA071298 1 20070307 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 500C S19L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007031300076 20070313 00076 NM 2007 3 13 SWAA071299 1 20070311 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 791 S17L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 791, STR 17L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007031300114 20070313 00114 EA 2007 3 13 COMA0760235 1 20070306 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA LT WING FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 479CA 9705 7675 FLIGHT 5436 - RECEIVED A FLAP FAIL CAUTION MESSAGE DURING CLIMBOUT OF BGR, CREW DECLARED EMERGENCY AND RETURNED TO THE F IELD. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT BRAKE POSITION SENSING UNIT. 2 L 7 2 4F RT A21EA 2007031300115 20070313 00115 NM 2007 3 13 CALA0700117 1 20070303 A 5311 6520722U98 FRAME BOEING 737 737524 1384721 NM BS 400 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69603 27316 INSPECTION FOUND A 1 INCH CRACK IN FORWARD BAGGAGE BIN FORWARD FRAME AT LOWER STOP PAD FITTING AT STA 400. THE FRAME WA S REPLACED IAW SRM 51-40-02 AND BOEING DRAWING 65C33514. 2 L 7 2 4F RT A16WE 2007031300116 20070313 00116 NM 2007 3 13 CALA0700118 1 20070226 A 5320 147A57101 ANGLE BOEING 737 737824 13844BZ NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17244 28954 INSPECTION FOUND LIGHT SURFACE CORROSION AT LEFT SIDE Z-ANGLE AFT OF STA 986.5, LBL 32. THE Z-ANGLE WAS REMOVED AND REP LACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007031300117 20070313 00117 NM 2007 3 13 CALA0700119 1 20070226 A 5315 BAC15181211 FLOORBEAM BOEING 737 737824 13844BZ NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17244 28954 INSPECTION FOUND LEFT SIDE UPPER SURFACE OF FLOORBEAM CORRODED AT STA 986.5, RBL 6 TO LBL 43. THE FLOORBEAM WAS REPAIRE D IAW ECRA 5321-01451. 2 L 7 2 4F RT A16WE 2007031300118 20070313 00118 NM 2007 3 13 CALA0700120 1 20070304 A 5320 147A85401 STRUCTURE BOEING 737 737824 13844BZ NM BS 967-1006 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17244 28954 INSPECTION FOUND CHORD CORRODED AT STA 967-1006, LBL 53. A NEW CHORD WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007031300119 20070313 00119 NM 2007 3 13 CALA0700121 1 20070226 A 5320 147A567103 CHANNEL BOEING 737 737824 13844BZ NM BS 992-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17244 28954 INSPECTION FOUND Z-CHANNEL CORRODED ON FORWARD EDGE AT STA 992-1016, LBL 29. THE Z-CHANNEL WAS REPLACED IAW SRM 51-40-0 2. 2 L 7 2 4F RT A16WE 2007031300120 20070313 00120 WP 2007 3 13 IXXA07SMN056S 1 20070131 A 5340 3757665IN FITTING DOUG DC8 DC871F 302199D WP ZONE 100 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND A CORRODED FITTING AT STATION FS450.000, LONGERON 26 LEFT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51 -1-8 PAGE 17-18, DC8 SRM 53-2-0 PAGE 2P, DC8 SRM 51-1-8B, DC8 SRM 51-1-20D AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007031300121 20070313 00121 EA 2007 3 13 COMA0760236 1 20070307 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS UNKNOWN A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 917CA 7017 FLIGHT 5156 - RECEIVED FLAP CAUTION MESSAGE. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. PERFORMED EO 27-046AD. N O FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007031300122 20070313 00122 WP 2007 3 13 IXXA07SMN053S 1 20070131 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER LEADING EDGE CORRODED, BETWEEN STATIONS XFS341.500 AND XFS304. 000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. F ABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALL ED REPAIR PARTS IAW DC8 SRM 51-1-21, DC8 51-1-20D, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 57-2-1 FIGURE 2G, DC8 SRM 57-2-1, FIGURE 44 DC8 SRM 57-3-1 PAGE 8 FIGURE 4 ITEM "A", DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-3-0 AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007092000117 20070920 00117 NM 2007 9 20 F3LA200700230 1 20070912 A 5347 A258224522400 BUSHING AIRBUS A319 A319111 3930336 NM SEAT MOUNT CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 921FR 5402 2010 DURING C-3 CHECK, INSPECTION REPORTED AFT LT FLT ATTENDANT SEAT (HOLD DOWN INSERTS) CORRODED IN MOUNTING HOLE AND EXTEND ING INTO THE FLOORBEAM. REPLACED AFT LT FLT ATTENDANT SEAT FLOOR MOUNT BUSHINGS IAW AMM 25-22-42-400-001. 2 L 7 2 4F RT A28NM 2007092000122 20070920 00122 EU 2007 9 20 07FDEA03548 1 20070911 A 5311 A53810787 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 FOUND CRACK (17 MM) IN FRAME 44 RT. REPAIR MOD PERFORMED IAW FEDEX WIC 6-5310-7-5015 FROM FRAME 41-46. 2 L 7 2 4F RT A35EU 2007092000133 20070920 00133 NM 2007 9 20 07FDEA03553 1 20070911 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM FUSLEAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 588FE 48490 RIGHT NOSE LANDING GEAR TRUNNION FITTING SUSPECT WITH CRACK. 09-28-07 REPAIR CARRIED OUT AT RT NLG TRUNNION FITTING AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007092000137 20070920 00137 NM 2007 9 20 2007UALA03597 1 20070905 A 2432 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MAIN FAULTY A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 574UA 26686 MAIN BATTERY CHARGER DISPLAYED ON STATUS PAGE. UNABLE TO CLEAR. FOUND BATTERY HOT TO THE TOUCH. REPLACED MAIN SHIPS BATTERY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092000146 20070920 00146 NM 2007 9 20 DLM88071176 1 20070905 A 5753 99359426 SKIN DOUG MD88 MD88 3023688 NM RT WING TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 954DL 49885 A TIME-LIMITED REPAIR WAS REMOVED FROM THE RT WING INBD MAIN FLAP LOWER SKIN. PERMANENT REPAIR WAS MADE BY A SPLICE TO THE LOWER SKIN AT XIFO=90. 2 L 7 2 4F RT A6WE 2007092000157 20070920 00157 NE 2007 9 20 2007UALA03605 2 20070906 A 7230 COMPRESSOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 1 ENGINE STALLED A UALA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 29 825UA 980 V10189 NR 1 ENGINE COMPRESSOR STALL CAUSED BY CLEAR AIR TURBULENCE - MOUNTAIN WAVE. ACCOMPLISHED BOROSCOPE OF COMPRESSOR SEC TION OF ENGINE-RESULTS NORMAL, ACCOMPLISHED TEST OF 7TH AND 10TH STAGE SOLENOID AND POTS AND FOUND 10TH STAGE POT FAILIN G-REPLACED 10TH STAGE POT. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092000176 20070920 00176 NM 2007 9 20 2007UALA03620 1 20070909 A 5320 STRUCTURE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUSELAGE DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 221UA 30552 EXTERNAL FUSELAGE FWD OF NR 2 MAIN ENTRY DOOR IS DAMAGED. 10-11-07 MAJOR REPAIR DOUBLER INSTALLED FWD OF NR 2 MAIN E NTRY DOOR REF SRM 53-00-01. SUSPECT DAMAGE DUE TO IMPACT WITH GROUND EQUIPMENT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007092000194 20070920 00194 NM 2007 9 20 QXEA200701386 1 20070905 A 2120 UNKNOWN DHAV DHC8 DHC8202 2809007 NM CABIN ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 348PH 484 EAT - SMOKE OBSERVED IN COCKPIT AFTER NR 2 ENGINE START AND NR 2 BLEED SELECTED ON. INSPECTED ENGINES. OPERATIONAL CHE CK OF BLEED SYSTEM. ALL CHECKS GOOD. NO SMOKE ODOR IN BLEEDS. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007092000196 20070920 00196 NM 2007 9 20 QXEA200701410 1 20070910 A 3010 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007 NM BLEED SYS MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 354PH 498 PDX FLIGHT NR 2107, 18 PSI BLEED AIR INDICATES 10 PSI WITH POWER LEVERS AT FLIGHT IDLE. INSTALLED NEW 55 AND 65 PSI SWI TCHES IN BOTH RIGHT AND LEFT NACELLES IAW AMM 30-10-00-720-001. GROUND RAN BOTH ENGINES. OPERATIONAL CHECK GOOD. AIRC RAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007092000198 20070920 00198 NM 2007 9 20 2007UALA03637 1 20070908 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 526UA 24994 ONE SEGMENT OF EEL LAMP AT ROW 3 IS CUT OFF. ALSO THE LAST SEGMENT OF EEL LAMP AT ROW 32 IS INOP. REPLACED WITH LAMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092000217 20070920 00217 NM 2007 9 20 DHL2007746524 1 20070821 A 5230 STIFFENER BOEING 727 727224 1384076 NM CARGO DOOR CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 C-1 DOOR LOWER STIFFENERS AND FRAMES CORRODED ABOVE LOWER FRAME BODY STATION 560-620. REMOVED LOWER STIFFENERS AND FRAM E AT C1 DOOR IAW B727 SRM 51-30-2. FABRICATED TWO TEE SUPPORT DIMENSION 9 3/4 EACH MATERIAL USED BAC1505-29222 7075T6 P O NR 9004174 AND FABRICATED 4 ANGLE MATERIAL USED 7075T6 0.050 PO NR 9004940 DIMENSION 8 3/4" BY 5 1/4" EACH IAW B727 SR M 52-30-1 FIG 4 AND SRM 51-30-5. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED TWO TEE SUPPORT AND 4 NEW ANGLES I AW B727 SRM 51-30-2, LEAK CHECK IAW B727 MM 52-31-00 GOOD. 2 L 7 3 4F A3WE 2007092000233 20070920 00233 EU 2007 9 20 AALA2071553 1 20070815 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 JFK - EMERGENCY LIGHT AT SEAT MOUNTED RIGHT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT MO UNTED RIGHT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007092000240 20070920 00240 EU 2007 9 20 07FDEA03596 1 20070912 A 5712 A57240457203 RIB AIRBUS 300 A300B4605R 3930308 EU ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 FOUND CHAFING MARK ON LT WING INTERMEDIATE RIB AT WIAX 21.9. REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5 751-112495 AND RAS/BAE/1005322/2007 ISS A. 2 L 7 2 4F RT A35EU 2007092000242 20070920 00242 NM 2007 9 20 091707001 1 20070913 A 2611 SMOKE DETECTOR BOEING 767 76723B 1385112 NM LAVATORY MALFUNCTIONED A L43A O OTHER N FALSE WARNING CR CRUISE 1 EA 27 253MY 23974 LAV SMOKE DETETECTORS IN MID AND AFT LAV ALARMED 5 HRS INTO FLIGHT. DETECTORS WERE RESET AFTER NO INDICATION OF SMOKE. THE SMOKE DETECTORS WERE OPS CHECKED ON THE GROUND WITH NO FAULTS NOTED AND RETURNED TO SERVICE. 2 L 7 2 4F RT A1NM 2007092000245 20070920 00245 NM 2007 9 20 2007UALA03651 1 20070909 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 651UA 25389 FWD GALLEY EEL LIGHT INOPERATIVE. 10-11-07 REPLACED LIGHT AND REPAIRED WIRING. EEL OP CHECKED OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092000261 20070920 00261 NE 2007 9 20 HALA0700373 2 20070910 A 7261 CARBON SEAL BOEING 767 7673G5 1385126 NM PWA 4060 PW4060 52119 NE ENGINE LEAKING A HALA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEMS, TSI FOR NR 1 ENG HIGH OIL CONSUMPTION. FOUND OIL DRIPPING FROM PMA GEARBOX DRAIN AT SHUTDOWN AT 1 DROP PER SECOND. REMOVED AND REPLACED EEC/PMA CARBON SEAL AND SEAT AT DRIVE SHAFT PER PWEM 72-61-09. REINSTALLED PMA PER AMM 73-21-05-404-038/404-030-N00. PERFORMED ENG RUN LEAK CK AND TEST NO NR 6.71-00-00-745-006-N00. NO FAULTS FOUND, PIMU CHECK NORMAL. NO LEAKS NOTED. NO LEAKS FROM DRAIN, OIL QTY NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092000265 20070920 00265 SW 2007 9 20 WGEA200700006 1 20070908 A 5532 551204881002 SKIN PANEL ECLIPS EA500 ECLIPSEEA500 3350000 SW VERTICAL STAB DAMAGED E WGEA K NONE O OTHER UK UNKNOWN 1 EA 27 109DJ 250 000006 VERTICAL STABILIZER LEADING EDGE PANEL HAS NUMEROUS DINGS THROUGH PAINT AND INTO COMPOSITE. REPAIRED VERTICAL STABILIZE R LEADING EDGE IAW EA500 AMM 20-09-00 AND SRM 51-70-01. REFERENCE ECLIPSE AVIATION TECHNICAL SERVICE REGUEST FSR CASE 5 3-090507. 1 L 7 2 4J RT A00002AC 2007092000268 20070920 00268 NM 2007 9 20 KCSA071356 1 20070911 A 5310 DOOR FRAME BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 L-5 DOOR LOWER HINGE CUTOUT LOWER WEB CRACKED .25 INCH AT STA-2242 WL-230. 2 L 7 4 4F RT A20WE 2007092000270 20070920 00270 NM 2007 9 20 KCSA071358 1 20070911 A 5330 SKIN BOEING 747 7472B4B 138481B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-690 BETWEEN STR-41R AND STR-42R SKIN DAMAGED. 2 L 7 4 4F RT A20WE 2007092000277 20070920 00277 EA 2007 9 20 VNAA0708022 1 20070829 A 5242 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE GROUND POWER OPEN A VNAA A UNSCHED LANDING O OTHER TO TAKEOFF 1 GL 05 702PS 10135 CREW REPORTED A GROUND POWER DOOR LEFT OPEN AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND EXTERNAL POWER DOOR OPEN. MAINTENANCE SECURED DOOR CLOSED. NO DEFECTS OR DAMAGE NOTED AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007092000294 20070920 00294 EA 2007 9 20 TRAX200701316 1 20070905 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 834AS 7254 AAR - RIGHT O/B INTERCOSTAL AT FS 484 CRACKED. CUT AWAY DAMAGED (CRACKED) ATTACHMENT FLANGE AT FS 484.00 O/B SIDE RIGHT INTERCOSTAL IAW REO 601R-53-41-059. (FABRICATED) ANGLE CLIP FROM 2024 T-3 .063" (PO 950261). COMPLIED WITH LPI OF CUT LINE AND FABRICATED ANGLE IAW REO 601R-53-41-059. NO DEFECTS NOTED ANGLE CLIP REQUIRES DRILLED AND CONFORMED. LOCATED HOLES AND CONFORMED ANGLE IAW REO 601R-53-41-059 OK TO ALODINE AND PRIME. ALODINED AND PRIMED IAW CRJ 200 SRM 51-25-06 . OK TO INSTALL. INSTALLED SERVICEABLE INTERCOSTAL AT RIGHT O/B FS 484 IAW REO 601R-53-41-059. OK TO TOP COAT. TOP C OATED IAW CRJ 200 SRM 51-25-16. SUPPLEMENTAL - SDR CLOSED 09/12/07. 2 L 7 2 4F RT A21EA 2007092000303 20070920 00303 WP 2007 9 20 ABXA070283 1 20070911 A 5230 59101575 PAN DOUG DC9 DC941 302207N WP AFT CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 WHILE COMPLYING WITH NEA 52300001-001, FOUND INNER DOOR PAN CRACKED. REPAIRED PAN IAW DC9 SRM 52-05, FIGURE 26A. 2 L 7 2 4F A6WE 2007092000304 20070920 00304 NM 2007 9 20 ABXA070276 1 20070824 A 3397 PIN BOEING 767 767232 1385132 NM CONNECTOR OUT OF POSITION A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 739AX 22216 LT EMERGENCY "EXIT" PANEL LIGHT WOULD NOT TEST. TROUBLESHOT PER WD 33-51-13. RELOCATED PIN 13 IN CONNECTOR J9084 TO PO SITION 9 PER REA B633-56326. EMERGENCY LIGHTS TEST GOOD IAW B767 MM 33-51-01. 2 L 7 2 4F RT A1NM 2007092000310 20070920 00310 EU 2007 9 20 MALA070117 1 20070915 A 3297 WIRE SAAB SF340 340B 7860101 EU MLG CHAFED A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 454XJ 340B454 ON APPROACH TO LANDING, THE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. THE CREW FOLLOWED THE QRH, BLEW THE BOLTS TO EXTEND THE LANDING GEAR. CREW DID NOT DECLARE AN EMERGENCY, BUT CFR WAS CALLED FOR ASSISTANCE. THE FLIGHT LANDED WITHOUT FUR THER INCIDENT. PMI: ON DECENT CHECK LANDING GEAR WILL NOT MOVED DOWN, FOLLOW THE GEAR DOWN UNSAFE OHM, USED THE EMERGEN CY LDF HANDLE. GEAR CAME DOWN WITH THREE GREEN OHM WAS COMPLETED. LANDING WAS SAFE CB F7 IS OUT TRANSFERRED TO 409 #27 9020. INSPECTED AND FOUND CHAFED WIRE IAW SRM 91-10-00. REMOVED AND REPLACED SEPARATION BOLTS IAW 32-34-15-02. PERFOR MED GEAR SWINGS, OK FOR SERVICE. 2 L 7 2 4T RT A52EU 2007092000312 20070920 00312 NM 2007 9 20 QXEA200701420 1 20070915 A 3040 M390166105L RELAY DHAV DHC8 DHC8202 2809007 NM WINDSHIELD HEAT MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 347PH 480 MFR - RIGHT WINDSHIELD HOT CAUTION LIGHT ILLUMINATED WITH WINDSHIELD HEAT IN NORM POSITION, RAN CHECKLIST LIGHT EXTINGUI SHED WITH SELECTOR BACK IN WARM-UP. MAINTENANCE REPLACED 3041K7 RELAY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO S ERVICE. 2 H 7 2 4T RT A13NM 2007092000319 20070920 00319 WP 2007 9 20 ABXA070286 1 20070810 A 5320 991555047 INTERCOSTAL DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 907AX 47203 AFT LOWER CARGO INTERCOSTAL WAS CORRODED AT THE NUT PLATES AND ON THE UPPER SURFACE BETWEEN STA 980 AND 996 AT LONGERON 28 LEFT. REMOVED AND REPLACED INTERCOSTAL IAW DC9 SRM. 2 L 7 2 4F A6WE 2007092000342 20070920 00342 NM 2007 9 20 AWXA200701105 1 20070817 A 5754 114N407513 SKIN BOEING 757 7572S7 1384962 NM ZONE 600 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 MCN - MAJOR REPAIR - C-11 CHECK - NR 5988280, RIGHT WING NR 10 SLAT COVE SKIN CRACKED, OSS 797.46 - OSS 809.46. REPLACE D RIGHT WING NR 10 SLAT COVE SKIN, OSS 797.46 - OSS 809.46 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007092000344 20070920 00344 NM 2007 9 20 AWXA200701107 1 20070830 A 5542 SKIN BOEING 757 7572S7 1384962 NM RUDDER DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 MCN - MAJOR REPAIR - C-11 CHECK - NR 5988823 AND 5988924, RUDDER TRAILING EDGE HAS AREA OF DELAMINATION, RUDDER STATION 228.850, RUDDER STATION 233.852. REPAIRED RUDDER TRAILING EDGE, RUDDER STATION 228.850 - RUDDER STATION 233.852 IAW USA IRWAYS EA 120229. 2 L 7 2 4F RT A2NM 2007092000349 20070920 00349 EU 2007 9 20 CPCP20070095 1 20070827 A 5312 BULKHEAD AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 414WF 414 CORROSION FOUND FWD PRESSURE BULKHEAD LT LOWER BONDING POINT. FWD PRESSURE BULKHEAD LT LOWER BONDING POINT REPAIRED AS PER SRD 53-00-00 FIG 438. 2 H 7 2 4T RT A53EU 2007092000350 20070920 00350 EU 2007 9 20 CPCP20070096 1 20070827 A 5320 THRESHOLD AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 414WF 414 RT THRESHOLD ANGLES (3) AT FRAME 36,37 AND 39 ARE CORRODED. RT THRESHOLD ANGLE FRAME 36, 37, 39. REPLACED IAW SRM 51-2 5-01. 2 H 7 2 4T RT A53EU 2007092000359 20070920 00359 NM 2007 9 20 KCSA071368 1 20070912 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 CO-PILOT AFT I/B SEAT TRACK HAS A 1.5 INCH CRACK IN FWD END. 2 L 7 4 4F RT A20WE 2007092000373 20070920 00373 EA 2007 9 20 TRAX200701326 1 20070905 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 834AS 7254 AAR - FLOOR SUPPORT ANGLE AFT OF FS 280, O/B OF LBL 9 IS CRACKED. REFERENCE ROUTINE 50186/2000/0022 FOR CORRECTIVE ACTI ON 14211 9-11-07. SUPPLEMENTAL - SDR CLOSED 09/14/07. 2 L 7 2 4F RT A21EA 2007092000380 20070920 00380 WP 2007 9 20 ABXA070290 1 20070811 A 5330 591140214 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 FUSELAGE SKIN CRACKED AT SERVICE DOOR HOLD OPEN CUP. REPAIRED AREA IAW DC9 SRM 53-04, FIGURE 24. 2 L 7 2 4F A6WE 2007092000383 20070920 00383 WP 2007 9 20 ABXA070294 1 20070820 A 5310 591228611 PAN DOUG DC9 DC941 302207N WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 WINDOW PAN RING CRACKED AT FORWARD TOP AND AFT LOWER TABS AT STA 677. REPAIRED AREA IAW DC9 SSRM K07226. 2 L 7 2 4F A6WE 2007092000386 20070920 00386 EA 2007 9 20 TRAX200701338 1 20070910 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 875AS 7559 PAX DOOR FWD ANCHOR FITTING IS CRACKED. REPAIRED IAW AMM 52-11-17, SRM 51-40-11, MM 52-11-17, AND MM 52-11-17. NO DE FECTS NOTED. 2 L 7 2 4F RT A21EA 2007092000388 20070920 00388 EA 2007 9 20 TRAX200701340 1 20070911 A 5320 BEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 720EV 10115 THE 280 TRANSVERSE BEAM HAS MINOR CORROSION ON TOP SIDE BETWEEN LBL 9 AND RBL 9. 2 L 7 2 4F RT A21EA 2007092000392 20070920 00392 NM 2007 9 20 SWAA074524 1 20070911 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092000394 20070920 00394 NM 2007 9 20 SWAA074541 1 20070911 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 LEFT OVERWING EMERGENCY EXIT LIGHT ASSY LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007092000396 20070920 00396 NM 2007 9 20 SWAA074534 1 20070911 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092000399 20070920 00399 NM 2007 9 20 SWAA074527 1 20070911 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092000401 20070920 00401 NM 2007 9 20 SWAA074530 1 20070911 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092100003 20070921 00003 NM 2007 9 21 AALA20071692 1 20070905 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 606AA 27057 SJU - EMERGENCY LIGHTS FROM SEAT ROWS 16D TO 25D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT ROWS 16D TO 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092100012 20070921 00012 NM 2007 9 21 AALA20071688 1 20070904 A 3350 SHROUD BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 958AN 30091 MIA - EMERGENCY LIGHT AT SEAT 9D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092100013 20070921 00013 NM 2007 9 21 AALA20071689 1 20070904 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 958AN 30091 MIA - EMERGENCY LIGHT AT SEAT 9D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092100018 20070921 00018 EU 2007 9 21 07FDEA03881 1 20070918 A 5320 A53981009200 COUPLING AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 804FD 549 FOUND OLD MISDRILLED HOLES IN COUPLING AT FRAME 73, BETWEEN STRG 33-36 LT. REPLACEMENT OF COUPLING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100021 20070921 00021 NM 2007 9 21 07FDEA03884 1 20070918 A 5710 STRUCTURE DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 RIGHT WING NR 3 SLAT TELESCOPIC DUCT CUTOUT FOUND CRACKED. 10-04-07 REPAIRED AS PER SRM 57-10-00 FIGURE 43 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007092100036 20070921 00036 EU 2007 9 21 07FDEA03805 1 20070917 A 5320 A53988624209 STRUT AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 CORRODED CROSS STRUTS FWD OF FRAME 86 RT, STRG 15. REPLACEMENT OF CROSS STRUT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100043 20070921 00043 EU 2007 9 21 07FDEA03812 1 20070917 A 5320 A53773213224 PLATE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 CORRODED SHEAR PLATE AT FWD CARGO COMPARTMENT BETWEEN FRAME 21-22, STRG 43-44 LT. REPLACEMENT OF SHEAR PLATE IAW SRM 51 -72-10. 2 L 7 2 4F RT A35EU 2007092100055 20070921 00055 WP 2007 9 21 AALA20071660 1 20070831 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 461AA 49566 LGA - EMERGENCY LIGHT AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007092100056 20070921 00056 EU 2007 9 21 AALA20071658 1 20070830 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 91050 423 JFK - EMERGENCY LIGHT AT SEAT MOUNTED RIGHT MID CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT MO UNTED RIGHT MID CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007092100057 20070921 00057 NM 2007 9 21 AALA20071659 1 20070831 A 3350 70LA837 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 ORD - EMERGENCY LIGHT AT SEAT 25C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007092100070 20070921 00070 EU 2007 9 21 07FDEA03777 1 20070914 A 5320 A53612519202 SUPPORT AIRBUS 310 A310324 3930206 EU ZONE 200 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 OLD ANGLE REPAIR ON LONGERON (SUPPORT) BETWEEN FRAME 13B-16A, Y-953, FLOOR STRUCTURE, NOT CONFORM TO SRM 53-12-15 / FIG 207. REPAIR OF SUPPORT LONGERON PERFORMED IAW SRM 53-12-15/FIG 207. 2 L 7 2 4F RT A35EU 2007092100091 20070921 00091 EU 2007 9 21 07FDEA03860 1 20070917 A 5320 A53973174236 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 HEAVY CORROSION ON CLIP AT FRAME 61, BETWEEN STRG 55-56 LT. REPLACEMENT OF CLIP IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100094 20070921 00094 EU 2007 9 21 07FDEA03863 1 20070917 A 5313 A53974267 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 HEAVY CORROSION ON STRINGER 56 LT AND RT BETWEEN FRAME 55/58-65. STRINGER SPLICE REPAIRS PERFORMED IAW SRM 53-10-14 / F IG 201A. 2 L 7 2 4F RT A35EU 2007092100099 20070921 00099 NM 2007 9 21 07FDEA03870 1 20070917 A 5320 655617923 CHANNEL BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 LWR AFT CARGO PIT NR 3 CUTOUT THRESHOLD SUPPORT CHANNEL, STA 1130 STR 26R IS CORRODED. SUPPORT CHANNEL FOR NR 3 DOOR CU TOUT THRESHOLD IS REMOVED AND REPLACE ON WO NR 37678/N00602 ITEM 17 AND 18 ON JPF. THIS IS CLASSIFIED AS A MAJOR REPAIR . 2 L 7 3 4F RT A3WE 2007092100110 20070921 00110 NM 2007 9 21 AALA20071669 1 20070901 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 618AA 24526 MIA - EMERGENCY LIGHT AT SEAT 2E INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 2E. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT A2NM 2007092100129 20070921 00129 NM 2007 9 21 AALA20071711 1 20070909 A 3231 ROD END BOEING 777 777223 1385213 NM STRUT DOOR DISCONNECTED A AALA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 784AN 29588 JFK INFLIGHT T104/09SEP - CREW REPORTED LOUD VIBRATION NOISE. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. FOUND LEFT NOSE GEAR STRUT DOOR ROD END OFF OF ROD. RECONNECTED ROD END AND SECURED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007092100130 20070921 00130 EU 2007 9 21 AALA20071712 1 20070909 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80052 460 MIA - EMERGENCY LIGHT AT SEAT 29G INOPERATIVE. SECURED WIRE AT CONNECTOR FOR EMERGENCY LIGHT AT SEAT 29G. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007092100141 20070921 00141 WP 2007 9 21 AALA20071656 1 20070830 A 3350 0201804001 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 408AA 49319 TPA - EMERGENCY LIGHT AT SEAT 8D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 8D. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F A6WE 2007092100142 20070921 00142 EU 2007 9 21 AALA20071657 1 20070830 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 91050 423 JFK - EMERGENCY LIGHT AT SEAT MOUNTED RIGHT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT MOUNTED RIGHT FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007092100143 20070921 00143 WP 2007 9 21 AALA20071653 1 20070830 A 3350 OL1098BPEGPL BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 408AA 49319 TPA - EMERGENCY LIGHT AT SEAT 8D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 8D. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F A6WE 2007092100144 20070921 00144 WP 2007 9 21 AALA20071654 1 20070830 A 3350 OL1098BPEGPL BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 408AA 49319 TPA - EMERGENCY LIGHT AT SEAT 9D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F A6WE 2007092100145 20070921 00145 WP 2007 9 21 AALA20071655 1 20070830 A 3350 0201804001 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 408AA 49319 TPA - EMERGENCY LIGHT AT SEAT 9D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F A6WE 2007092100146 20070921 00146 NM 2007 9 21 AALA20071643 1 20070829 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 603AA 27054 MIA - EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092100147 20070921 00147 NM 2007 9 21 AALA20071641 1 20070829 A 3397 WIRE BOEING 757 757223 1384957 NM EMERGENCY LIGHTS CUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 611AM 24487 MIA - EMERGENCY LIGHT EXIT ARROW SIGN AT RIGHT SIDE LOWER AFT GALLEY INOPERATIVE. FOUND CUT WIRES BEHIND LAVATORY. REP AIRED PER E58 9376176. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092100148 20070921 00148 EU 2007 9 21 AALA20071640 1 20070829 A 2730 4909505 COMPUTER AIRBUS 300 A300B4605R 3930308 EU PITCH FEEL FAULTED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 25071 514 MIA INFLIGHT T2110/29AUG - AFTER TAKEOFF LOST SECOND PITCH FEEL SYSTEM. FIRST SYSTEM WAS ALREADY ON PLACARD. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED SLAT FLAP CONTROL COMPUTERS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007092100149 20070921 00149 NM 2007 9 21 AALA20071704 1 20070907 A 5320 SILL BOEING 767 767323 1385205 NM CARGO DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 351AA 24032 AFW FORWARD CARGO DOOR CUTOUT LOWER MAIN SILL, OUTER CHORD HAS CORROSION REMOVAL ON INBOARD SURFACE OF VERTICAL LEG. AR EA IS 1 INCH BY 2.2 INCHES WITH A DEPTH OF 0.098 AND 0.100 INCH. BLEND CORROSION OVERSIZE FASTENER HOLES. PERFORM 10 T IMES VISUAL AND HIGH FREQUENCY EDDY CURRENT INSPECTIONS. SPOTFACE BOLT HOLES AND BLEND AREAS, ALODINE, PRIME, AND INSTA LL SPOTFACE WASHER AND ALUMINUM FASTENER. 2 L 7 2 4F RT A1NM 2007092100150 20070921 00150 2007 9 21 AALA20071707 4 20070908 A 2565 BOTTLE BOEING 757 757223 1384957 NM SLIDE INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 655AA 24613 LAS LEFT NUMBER ONE SLIDE WAS NOT DISARMED AND DOOR WAS OPEN FROM INSIDE. SLIDE DID NOT DEPLOY. FELL ON AIR STAIRS. D OOR ASSIST BOTTLE EXPENDED. REINSTALLED SLIDE WITH NEW DOOR ASSIST BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092100151 20070921 00151 WP 2007 9 21 AALA20071708 1 20070908 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7509 49803 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 16 MISSING SHROUD. REPLACED SHROUD FOR SEAT MOUNTED EMERGENCY LIGHT AT S EAT ROW 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007092100152 20070921 00152 WP 2007 9 21 AALA20071709 1 20070908 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7509 49803 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 17 HAS BROKEN SHROUD. REPLACED SHROUD FOR SEAT MOUNTED EMERGENCY LIGHT A T SEAT ROW 17. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007092100153 20070921 00153 EU 2007 9 21 AALA20071710 1 20070909 A 3350 BR964814 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70074 517 JFK - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 10G BROKEN. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 10G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007092100154 20070921 00154 NE 2007 9 21 AALA20071721 2 20070910 A 7261 PUMP BOEING 777 777223 1385213 NM RROYCE RB211 RB211TRENT89 NE LT ENGINE INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 773AN 29583 51165 LAX INFLIGHT T136/10SEP NUMBER ONE ENGINE OIL PRESSURE LIGHT ILLUMINATED DURING CLIMB AT 1000 FEET. RETARDED THROTTLE W ITH NO HELP. SHUT DOWN NUMBER ONE ENGINE. LANDED LAX WITHOUT INCIDENT. SINGLE ENGINE TIME 15 MINUTES. REPLACED NUMBE R ONE ENGINE OIL PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT T00001SE E00050EN 2007092100155 20070921 00155 NM 2007 9 21 AALA20071716 1 20070910 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 361AA 24042 CDG - EMERGENCY DOOR EXIT SIGN LIGHT AT LEFT NUMBER ONE DOOR UNSECURED. SECURED LOOSE DOOR EXIT SIGN FOR EMERGENCY LIGH T AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007092100156 20070921 00156 2007 9 21 AALA20071715 4 20070910 A 2565 SLIDE BOEING 777 777223 1385213 NM L1 DOOR FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 768AA 33540 ORD - LEFT NUMBER ONE DOOR WAS OPENED WITH DOOR SLIDE ARMED. SLIDE FELL ON TO JETBRIDGE AND PINS PULLED OUT. DID NOT D EPLOY. REPLACED LEFT NUMBER ONE DOOR SLIDE. 2 L 7 2 4F RT T00001SE 2007092100157 20070921 00157 NM 2007 9 21 AALA20071719 1 20070910 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 JFK - EMERGENCY LIGHT IN COACH CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN COACH CABIN. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007092100158 20070921 00158 NM 2007 9 21 AALA20071702 1 20070907 A 3350 CM1317 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AA 25201 JFK - EMERGENCY LIGHT AT CEILING RIGHT SIDE NEXT TO FLIGHT ATTENDANT READING LIGHT INOPERATIVE. REPLACED LAMP FOR EMERG ENCY LIGHT AT CEILING RIGHT SIDE NEXT TO FLIGHT ATTENDANT READING LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007092100159 20070921 00159 EU 2007 9 21 AALA20071703 1 20070907 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 90070 513 JFK - EMERGENCY LIGHTS AT SEAT ROWS 19 TO 29 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 19 TO 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007092100160 20070921 00160 NM 2007 9 21 AALA20071714 1 20070909 A 3397 CONNECTOR BOEING 767 767223 1385123 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 335AA 22333 LAX - EMERGENCY LIGHT AT SEAT 30B INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 30B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007092100161 20070921 00161 EU 2007 9 21 CPCP20070102 1 20070824 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 414WF 414 FLOORBEAM AT FRAME 39 IS CORRODED. NEW FLOORBEAM IS INSTALLED IAW SRM 51-25-0 AND 51-25-04. 2 H 7 2 4T RT A53EU 2007092400002 20070924 00002 2007 9 24 BJNA070601 4 20070627 A 2565 D31591478 SLIDE BOEING 737 737400 138449A NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR FAILED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 42XA 25729 DURING TRAINING DEPLOYMENT OF L-1 DOOR EMERGENCY EXIT SLIDE, THE SLIDE FAILED TO COMPLETELY UNFOLD, THE BOTTOM 2 LANYARD S FAILED TO PULL THROUGH STRAP EYELETS WHICH PREVENTED APPROXIMATELY THE LAST 1.5 - 2.0 FT TO UNFOLD AND INFLATE. AN EN GINEERING EVALUATION WAS PERFORMED, ALL COMPONENTS INCLUDING THE FRANGIBLE LINKS WHICH DID NOT BREAK WERE TESTED AND FOU ND TO CONFORM TO SYSTEM REQUIREMENTS. POSSIBLE CAUSES, BASED ON THE EVIDENCE PRESENTED, CYLINDER WAS NOT COMPLETELY CHA RGED OR THE ASPIRATOR AIRFLOW WAS PARTIALLY BLOCKED DURING THE INITIAL STAGES OF DEPLOYMENT. THE BLOCKAGE COULD HAVE OC CURRED IF THE SLIDE FOLDING WAS NOT IN COMPLETE IAW THE FOLDING PROCEDURE. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2007092400007 20070924 00007 CE 2007 9 24 DXTA200702438 1 20070831 A 2750 99145101 RESOLVER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS FAILED E DXTA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 GL 07 933QS 6651 7500133 DURING DESCENT THROUGH 15,000 AT 340 KIAS, THE FLAP FAIL CAS, AMBER FLAP SYNOPTIC AND FLAPS RESET LIGHT CAME ON. AFM PR OCDURES WERE FOLLOWED. SLATS EXTENDED, BUT FLAPS DID NOT. VERIFIED FLAPS INOP ON INITIAL OPS CHECK. CONNECTED FLAP SYST EM BREAKOUT BOX. FOUND RH RESOLVER BAD. SYSTEM OPS CHECKED GOOD USING ONLY THE LT RESOLVER. REPLACED RH RESOLVER IAW 750 M/M 27-52-00. FOUND LT FLAPS OUT OF MECHANICAL RIG. MECHANICALLY AND ELECTRICALLY RIGGED FLAPS IAW 750 M/M 27-50-00. PE RFORMED FLAP SYSTEM OPERATIONAL TEST AND FLAP CONTROLLER FUNCTIONAL TEST IAW 750 M/M 27-50-00. OPS CHECK GOOD IAW 750 M/ M 27-50-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007092400008 20070924 00008 CE 2007 9 24 DXTA200702439 1 20070831 A 3240 215672 BRAKE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RIGHT LEAKING E DXTA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 945QS 296 296 7500029 ON TAXI IN, RT BRAKE WAS SMOKING. AFTER PARKING, FLUID SEEN DRIPPING FROM RT BRAKE OF RT WHEEL. REMOVED NR 4 BRAKE AS SY AND INSTALLED OVERHAULED UNIT OPSAND LEAK CHECK GOOD AT THIS TIME. IAW CE750 M/M 32-42-01 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007092400009 20070924 00009 SO 2007 9 24 C2XA07ON022 1 20070905 A 2820 FUEL SYS EMB 145 EMB145XR 3260214 SO MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 27200 145956 FLT 419 - LAS TO COS - DURING CRUISE FLIGHT CREW REPORTED AND DECLARED EMERGENCY AND DIVERTED THE FLIGHT BACK TO LAS WHE RE IT LANDED SATISFACTORY WITHOUT INCIDENT DUE TO NR 1 FUEL QTY IND 0, FUEL INBALANCE, FUEL 1 LOW LEVEL EICAS MSGS. MX CONTROL AUTHORIZED FLIGHT CREW TO RELEASE THE AIRCRAFT IAW MEL 28-40-00/2. 10-12-07 ON 09/06/2007 THE AIRCRAFT WAS F LOWN TO ONT FOR FURTHER INSPECTION. MX PERSONNEL PERFORMED NR 1 FUEL LOW LEVEL OPERATIONAL CHECKS AND SATISFACTORY CHECK GOOD AND AIRCRAFT WAS RELEASE TO RETURN FOR SERVICE IN AIRWORTHY CONDITIONS. 2 L 7 2 4F RT 2007092400010 20070924 00010 CE 2007 9 24 GLBA20060994 1 20070911 A 5314 1181200363603 KEEL BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT WHEEL WELL CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 251GL UE251 LT WHEEL WELL KEEL CRACKED APPROXIMATELY .5 INCH FORWARD OF LT MAIN LANDING GEAR MOUNT. MAINTENANCE REPAIRED FLANGE CRA CK ON L/H INBOARD KEEL RIB I.A.W. E.O. 07-UE251-01. REPAIR DIMENSION 4 3/4" BY 3 1/2". 7075-T7351. RII INSPECTION COMPL IED WITH PER TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007092400011 20070924 00011 EU 2007 9 24 07FDEA03584 1 20070911 A 5313 A53974216242 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION ON CLIP AT C 71, P57-56RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092400012 20070924 00012 EU 2007 9 24 07FDEA03775 1 20070914 A 7830 32143306 SHUTOFF VALVE AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER MALFUNCTIONED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 685FE 803 ON TAKEOFF, GOT ENG NR 2 REVERSER PRESSURIZED-REJECT SAME ON SECOND TRY. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C "MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) NR 2 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FOR WARD THRUST POSITION." R&R NR 2 ENG T/R PRSOV PER A-300 AMM 78-31-05-4-05 AND PERFORMED T/R FUNCTIONAL TEST PER JRH CHAP 7. ALL OPS TESTS NORMAL WITH NO ALERTS. 2 L 7 2 4F RT A35EU 2007092400013 20070924 00013 EU 2007 9 24 07FDEA03795 1 20070825 A 5230 A52374235204 SKIN AIRBUS 310 A310222 3930315 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 419FE 345 PREVIOUS REPAIR FOUND LOCATED ON FWD CARGO DOOR SKIN, FR 25-25A BETWEEN BEAM 3 AND BEAM 4. REPAIR REQUIRES EVALUATION F OR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. THE REPAIR WAS EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. A NEW REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FEDEX ENGINEERING AUTHORIZATION 6- 5230-113174. 2 L 7 2 4F RT A35EU 2007092400014 20070924 00014 EU 2007 9 24 07FDEA03874 1 20070918 A 7830 SHUTOFF VALVE AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER MALFUNCTIONED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 685FE 803 ON TAKEOFF, NR 2 THRUST REVERSER PRESSURIZED-REJECT AT 50 KNOTS. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATE GORY: C EXPIRATION: 24SEP07 "MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) 2 THRUST REVERSER INOP. THRUST REVERSER IS DEAC TIVATED IN FORWARD THRUST POSITION." R&R NR 2 ENGINE T/R PRSOV PER A-300 AMM 78-31-05-4-05 AND PERFORMED T/R FUNCTIONA L TEST PER JRH CHAP 7. ALL OPS TESTS NORMAL WITH NO ALERTS. 2 L 7 2 4F RT A35EU 2007092400048 20070924 00048 EU 2007 9 24 07FDEA03927 1 20070918 A 5310 A53778685206 PLATE AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT MANHOLE INTEGRAL PLATE C 38.1-39, P 49RH-54 LT AND OLD POCKET REPAIRS, NOT CONFORM TO SRM 53-14-12. REPAIR PERFORMED BY REPLACEMENT OF PART IAW DRAWING R537-06164-000 AND SRM 51-72-10 AND INSTALLING OF ALTERNATE FASTENER , APPROVED BY EA 6-5314-81070 AND RAS/DABRE/004470/2004 ISS A. 2 L 7 2 4F RT A35EU 2007092400049 20070924 00049 EU 2007 9 24 07FDEA03928 1 20070918 A 5312 BULKHEAD AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 CORROSION FOUND BEHIND AFT PRESSURE BULKHEAD C80 AT CIRCUMFERENTIAL STRAP AND FLANGE REPAIR PERFORMED IAW SRM 53-19-17 F IG 201 AND DRAWING R539-707100. 2 L 7 2 4F RT A35EU 2007092400050 20070924 00050 EU 2007 9 24 07FDEA03929 1 20070918 A 5320 A53984700256 ANGLE AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 CORROSION FOUND BEHIND AFT PRSSURE BULKHEAD C80 AT INNER RIM ANGLE. REPAIR PERFORMED BY RELACEMENT OF PART IAW SRM 51- 72-10. 2 L 7 2 4F RT A35EU 2007092400051 20070924 00051 EU 2007 9 24 07FDEA03930 1 20070918 A 5312 A53984667208 STRAP AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 CORROSION FOUND BEHIND AFT PRESSURE BULKHEAD C80 AT INNER STRAP. REPAIR PERFORMED BY RELACEMENT OF PART IAW SRM 51-72-1 0. 2 L 7 2 4F RT A35EU 2007092400052 20070924 00052 EU 2007 9 24 07FDEA03931 1 20070918 A 5210 F52181310201 BEAM AIRBUS 310 A310324 3930206 EU PAX DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 FOUND CORROSION ON LONGITUDINAL WEB OF BEAM 3 OF PAX DOOR NR 1 RT, BETWEEN XP=590 AND XP=715MM. REMAINING THICKNESS IS 0,5MM, AS THE NOMINAL THICKNESS IS 2,0MM. AFFECTED AREA IS ABOUT 1600MM X MM. REPAIR PERFORMED BY CUTTING CORRODED AR EA. INSTALLING A MACHINED ANGLE DOUBLER ON THE WEB OF BEAM 3 AND A REINFORCING STRIP ON THE INTERNAL FLANGE IAW EA 6-52 11-81114 AND RAS/AS/0005/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007092400053 20070924 00053 EU 2007 9 24 07FDEA03932 1 20070918 A 5330 A53778669210 PLATE AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT MANHOLE INTEGRAL PLATE C 23-24, P 49RH-54 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW DRAWING R537 -06163 AND INSTALLING ALTERNATE FASTENER HL111VF8, APPROVED BY EA 6-5313-8106 AND RAS/DABRE/7004239/2004 ISS B. 2 L 7 2 4F RT A35EU 2007092400054 20070924 00054 EU 2007 9 24 07FDEA03933 1 20070918 A 5330 A53978152200 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 434FE 355 FOUND EXTERNAL DOUBLER REPAIR AT C65-66, P 39-42 RT NOT CONFORM TO SRM. REPAIR RENEWED IAW SRM 53-10-12 FIG 203. 2 L 7 2 4F RT A35EU 2007092400055 20070924 00055 EU 2007 9 24 07FDEA03934 1 20070918 A 5330 A53610567236 DOUBLER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT INTERNAL DOUBLER C 17-18, P 42-44 LT. REPAIR PERFORMED BY BLEND OUT CORROSION AND NTD INSPECTION OF CRACK FREE IAW EA 6-5312-81047 AND RAS/AS/246/2004 ISS A. 2 L 7 2 4F RT A35EU 2007092400056 20070924 00056 EU 2007 9 24 07FDEA03935 1 20070918 A 5313 A53778088 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION ON STRINGER P 32RT 35-37 STRINGER REPAIR PERFORMED IAW EA 6-5314-81040 AND RAS/DATLS/0002032/2004 ISS. A 9 CUT OUT THE CORRODED PART AND SPLICE REPAIR. 2 L 7 2 4F RT A35EU 2007092400057 20070924 00057 EU 2007 9 24 07FDEA03936 1 20070918 A 5313 A53974203220 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION ON STRINGER P 52LT, C 65-66 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007092400058 20070924 00058 EU 2007 9 24 07FDEA03937 1 20070918 A 5313 A53974202 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION ON STRINGER P 53 LT, C 63-65. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007092400059 20070924 00059 EU 2007 9 24 07FDEA03938 1 20070918 A 5313 A53773636202 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION ON STRINGER P 43LH, C 22-23. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007092400060 20070924 00060 EU 2007 9 24 07FDEA03939 1 20070918 A 5313 A53980670 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION ON STRINGER P 40LH AND P 42, C 79-80. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007092400061 20070924 00061 EU 2007 9 24 07FDEA03940 1 20070827 A 5230 BEAM AIRBUS 310 A310222 3930315 EU ZONE 800 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 PREVIOUS REPAIR FOUND LOCATED ON FWD CARGO DOOR, LOWER CORNER OF FR 20A BTW BEAM 4 AND BEAM 5. REPAIR REQUIRES EVALUATI ON FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. SECTION EDGE WAS REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092400062 20070924 00062 EU 2007 9 24 07FDEA03941 1 20070918 A 5313 A53980670 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION ON STRINGER P 44LT AND P 45LT, C 79-80. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007092400063 20070924 00063 EU 2007 9 24 07FDEA03942 1 20070827 A 5230 A5237204320200 SKIN AIRBUS 310 A310222 3930315 EU ZONE 800 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 419FE 345 PREVIOUS REPAIR FOUND LOCATED ON FWD CARGO DOOR, ON INNER SKIN BETWEEN BEAM 4 AND 5, AT FR 20A-21. REPAIR REQUIRES EVAL UATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS EVALUATED AND F OUND NOT TO CONFORM TO AN SRM REPAIR. SKIN PANEL WAS REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092400064 20070924 00064 EU 2007 9 24 07FDEA03943 1 20070827 A 5347 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 CABIN DUMMY TRACK NR 5 LT AT Y1959 BETWEEN FR 54 AND FR 54.2 WITH WEAR OF 1.7MM AT AFT HOLE ATTACHMENT AND WITH CRACKS A T LOCKS. THE AFFECTED PART WAS REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092400065 20070924 00065 EU 2007 9 24 07FDEA03944 1 20070827 A 5347 A5381312720008 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 CABIN, DUMMY TRACK NR 3 RT (Y-953) CRACKED BETWEEN FR 54 AND FR 54.2. THE PART WAS REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092400066 20070924 00066 EU 2007 9 24 07FDEA03945 1 20070910 A 5310 A53275336200 CROSSBEAM AIRBUS 310 A310222 3930315 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 CROSS-BEAM CRACKED AT FRAME 54.3 BETWEEN Y-1450 AND Y-1950. THE CROSS-BEAM WAS REPAIRED IAW FEDEX EA 6-5310-113718. 2 L 7 2 4F RT A35EU 2007092400067 20070924 00067 EU 2007 9 24 07FDEA03946 1 20070827 A 5347 A5381312720008 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 DUMMY TRACK NR 1 AT Y0 BETWEEN FR 54 AND FR 54.2 WITH CRACK AT LOCKS. THE PART WAS REPLACED PER SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092400068 20070924 00068 EU 2007 9 24 07FDEA03948 1 20070903 A 5510 ANGLE AIRBUS 310 A310222 3930315 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 RT THS, SPOT OF CORROSION AT UPPER ANGLE AT AREA OF RIB 14/15. IT WAS REPAIRED IAW SRM 55-11-21 FIG 215. 2 L 7 2 4F RT A35EU 2007092400069 20070924 00069 EU 2007 9 24 07FDEA03949 1 20070903 A 5510 ANGLE AIRBUS 310 A310222 3930315 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 RT THS, SPOT OF CORROSION AT UPPER ANGLE AT AREA OF RIB 18/19. IT WAS REPAIRED IAW SRM 55-11-21 FIG 221. 2 L 7 2 4F RT A35EU 2007092400070 20070924 00070 NM 2007 9 24 07FDEA03950 1 20070918 A 5754 SKIN BOEING 757 7572B7 1384964 NM SLAT MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 901FD A10605 27122 FLUSH REPAIR ON L/E OF NR 5 SLAT DOES NOT COMPLY WITH SRM. REMOVED AND REPLACED REPAIR ON NR 5 L/E SLAT IAW SRM 57-43-0 1, FIG 201. FABRICATED REPAIR FILLER, HEAT TREATED TO T6 ON MAE TRAVELER T7/696092. FABRICATED DOUBLER AND SPLICES, HEAT TREATED ON MAE TRAVELERS T7/696091, T7/696093 AND T7/696094. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-02. TH IS IS A MAJOR REPAIR BASED ON GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2007092400071 20070924 00071 NM 2007 9 24 DL76G071226 1 20070917 A 2913 271T00424 MODULE BOEING 767 7673P6 1385105 NM HYD PUMP CRACKED A DALA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SO 27 154DL 25241 C-2 PUMP FILTER MODULE LEAKING. FOUND C2 PUMP FILTER MODULE CRACKED. REPLACED PART. 2 L 7 2 4F RT A1NM 2007092400072 20070924 00072 NM 2007 9 24 DL764071228 1 20070917 A 3350 BATTERY PACK BOEING 767 767432ER 1385134 NM EMERGENCY LIGHTS FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831MH 29702 BATTERY PACK (EMERG) M1208 FAILED DEEP CYCLE/REMOVED BAD BATTERY AND REPLACED WITH SERVICABLE EMERG MIZOT, OPS CHECK GOO D IAW B767 MM 33-51-07. 2 L 7 2 4F RT A1NM 2007092400073 20070924 00073 NM 2007 9 24 DL764071229 1 20070916 A 3350 BATTERY PACK BOEING 767 767432ER 1385134 NM EMERGENCY LIGHT FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831MH 29702 EMERGENCY LIGHT BATTERY PACK MG757 FAILED DEEP CYCLE. REMOVED AND REPLACED (MG757) EMERG BATTERY PACK. OPS CHECK GOOD IAW B767 MM 33-51-07. 2 L 7 2 4F RT A1NM 2007092400074 20070924 00074 NM 2007 9 24 AALA20071756 1 20070916 A 2910 VALVE BOEING 767 767323 1385205 NM HYD SYSTEM INOPERATIVE A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 21 382AN 25451 AUA INFLIGHT T929/16SEP MIA TO GRU - CENTER HYDRAULIC SYSTEM QUANTITY DECREASING. DIVERTED TO AUA AND LANDED WITHOUT IN CIDENT. REPLACED VALVE FOR CENTER HYDRAULIC SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007092400075 20070924 00075 NM 2007 9 24 AALA20071743 1 20070914 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 627AA 24585 LAX - EMERGENCY LIGHTS AT AFT THREE SEATS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT THREE SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092400076 20070924 00076 WP 2007 9 24 AALA20071760 1 20070917 A 3241 TRANSDUCER DOUG DC9 DC983 3022083 WP NR 3 WHEEL INOPERATIVE A AALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 9404V 53140 STL INFLIGHT T1603/17SEP - AT 120 KNOTS DURING TAKEOFF WHEEL NOT TURNING INDICATION ILLUMINATED. ABORTED TAKEOFF. REPL ACED NUMBER THREE WHEEL TRANSDUCER ADAPTER AND TRANSDUCER. REPLACED NUMBER THREE AND FOUR TIRES. SYSTEM GROUND CHECK N ORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007092400077 20070924 00077 EU 2007 9 24 AALA20071742 1 20070914 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 34078 615 SJU - EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT IN CABIN. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007092400078 20070924 00078 NM 2007 9 24 AALA20071734 1 20070912 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 961AN 30092 DFW - EMERGENCY LIGHTS AT FORWARD CABIN RIGHT SIDE INOPERATIVE. REPLACED BATTERY PACK M1674 FOR EMERGENCY LIGHTS AT FOR WARD CABIN RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092400079 20070924 00079 NM 2007 9 24 AALA20071735 1 20070912 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 961AN 30092 DFW - EMERGENCY EXIT SIGN LIGHT AT RIGHT AFT OVERWING BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT SIGN LIGHT AT RIGHT AFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092400080 20070924 00080 NM 2007 9 24 AALA20071733 1 20070912 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 961AN 30092 DFW - EMERGENCY LIGHT AFT OF THE LEFT AFT PASSENGER DOOR BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AFT OF THE LEFT AFT PASSENGER DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092400081 20070924 00081 NM 2007 9 24 AALA20071736 1 20070912 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 961AN 30092 DFW - EMERGENCY EXIT SIGN LIGHT AT RIGHT FORWARD OVERWING BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT SIGN LIGHT AT RIGHT FORWARD OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092400082 20070924 00082 NM 2007 9 24 AALA20071728 1 20070912 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39365 24046 MIA - SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROWS 2HJ TO 6HJ INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT ROWS 2HJ TO 6HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007092400083 20070924 00083 NM 2007 9 24 AALA20071749 1 20070915 A 2910 B-NUT BOEING 757 757223 1384957 NM HYD LINE LOOSE A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 658AA 24616 MSY INFLIGHT T9404/15SEP DFW TO FLL - LEFT HYDRAULIC QUANTITY LOSS IN FLIGHT. DIVERTED TO MSY AND LANDED WITHOUT INCIDE NT. TIGHTENED LOOSE B NUT ON PYLON HYDRAULIC LINE. SERVICED LEFT HYDRAULIC SYSTEM. ACCOMPLISHED OVERWEIGHT LANDING IN SPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092400084 20070924 00084 2007 9 24 AALA20071738 4 20070913 A 2330 CONTROL UNIT BOEING 777 777223 1385213 NM VIDEO DISPLAY FAULTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 779AN 29955 DEN INFLIGHT T134/13SEP SMOKE WAS REPORTED IN CABIN AROUND VIDEO SCREENS. FLIGHT DIVERTED TO DEN AND LANDED WITHOUT INC IDENT. FOUND FAULTY CONTROL UNIT UNDER SEAT 35F. REPLACED FAULTY CONTROL UNIT UNDER SEAT 35F. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007092400085 20070924 00085 NM 2007 9 24 AALA20071731 1 20070912 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 615AM 24491 LAS - EMERGENCY LIGHTS AT MID COACH CLASS CABIN INOPERATIVE. FOUND LEFT NUMBER ONE DOOR FLIGHT ATTENDANT EMERGENCY LIGH T CONSOLE SWITCH LEFT ON. REPLACED BATTERY PACK AT AFT SEAT ROW 19 FOR EMERGENCY LIGHTS AT MID COACH CLASS CABIN. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092400086 20070924 00086 NM 2007 9 24 07FDEA03867 1 20070917 A 5311 65561322 FRAME BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 AFT LWR CARGO PIT FUSE. CUTOUT FOR NR 3 DOOR, STA 1130 PLUS 13" AFT SIDE FRAME HAS CORROSION DOWN LOW WHERE SCUFF PLATE MOUNTS AT STR 26R. REMOVED FRAME AT STA 1130 PLUS 13, FROM STRINGER 18R-28. REPLACED WITH NEW FRAME STA 1130 PLUS 13, FROM STRINGER 18R - 28R, IN REF TO SRM 51-30-2 PG 1-17, BAC DWG 65-56132. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007092400087 20070924 00087 NM 2007 9 24 AALA20071744 1 20070914 A 3350 OL3071BPEGPL BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 761AJ 31478 JFK - EMERGENCY LIGHT AT SEAT 2D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 2D. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT T00001SE 2007092400088 20070924 00088 EU 2007 9 24 07FDEA03678 1 20070913 A 5310 A53610688424 PROFILE AIRBUS 310 A310324 3930206 EU ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 FOUND AN OLD REPAIR (CUT OUT) FLANGE WITH CHAFING MARKS AT FRAME 16 LT, OUT OF LIMIT. REPLACEMENT OF FLANGE IAW SRM 51- 72-10. 2 L 7 2 4F RT A35EU 2007092400089 20070924 00089 NM 2007 9 24 AALA20071745 1 20070914 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 761AJ 31478 JFK - EMERGENCY LIGHT AT SEAT 2D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 2D. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT T00001SE 2007092400090 20070924 00090 NM 2007 9 24 AALA20071723 1 20070911 A 3610 CLAMP BOEING 757 757223 1384957 NM RT ENGINE LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 194AA 32388 DFW INFLIGHT T979/11SEP - ON CLIMB-OUT RECEIVED NUMBER TWO ENGINE FIRE WARNING WITH NUMBER TWO TURBINE OVERHEAT DETECTO R LOOP PLACARDED INOPERATIVE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND NUMBER TWO ENGINE CLAMPS ON FAN AIR V ALVE LOOSE. TIGHTENED CLAMPS AND REPLACED NUMBER ONE TURBINE OVERHEAT DETECTOR SWITCH FOR RIGHT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092400091 20070924 00091 NM 2007 9 24 AALA20071729 1 20070912 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 615AM 24491 LAS - EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. FOUND LEFT NUMBER ONE DOOR FLIGHT ATTENDANT EMERGENCY LIGHT CO NSOLE SWITCH LEFT ON. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OP ERATION. 2 L 7 2 4F RT A2NM 2007092400092 20070924 00092 2007 9 24 AALA20071724 4 20070911 A 2565 SLIDE BOEING 757 757223 1384957 NM NR 1 DOOR MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 687AA 25695 DFW INFLIGHT T1034/11SEP - DURING CLIMB RECEIVED LEFT NUMBER ONE DOOR EICAS MESSAGE. DURING DESCENT RETURNING TO DFW CR EW IN CABIN REPORTED THUMPING SOUND COMING FROM FLOOR LEVEL. LANDED DFW WITHOUT INCIDENT. FOUND LEFT OVERWING SLIDE IN FLIGHT DEPLOYMENT WITH ASSOCIATED DAMAGE. REPLACED SLIDE. TEMPORARY REPAIRS ACCOMPLISHED AND AIRCRAFT WAS FERRIED TO TUL AND REPAIRS TO FUSELAGE AND FLAP ACCOMPLISHED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092400093 20070924 00093 WP 2007 9 24 AALA20071739 1 20070913 A 2822 3980001 PUMP DOUG DC9 DC982 3022082 WP FUEL BOOST FAILED A AALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 SW 21 248AA 49259 ORD INFLIGHT T1493/13SEP - AFT CENTER TANK BOOST PUMP CIRCUIT BREAKER POPPED. RETURNED TO ORD AND LANDED WITHOUT INCIDE NT. REPLACED AFT CENTER TANK BOOST PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007092400094 20070924 00094 NM 2007 9 24 AALA20071730 1 20070912 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 615AM 24491 LAS EMERGENCY LIGHTS AT FORWARD COACH CLASS CABIN INOPERATIVE. FOUND LEFT NUMBER ONE DOOR FLIGHT ATTENDANT EMERGENCY L IGHT CONSOLE SWITCH LEFT ON. REPLACED BATTERY PACK AT FORWARD SEAT ROW 9 FOR EMERGENCY LIGHTS AT FORWARD COACH CLASS CA BIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092000224 20070920 00224 NM 2007 9 20 NWAA073196307 1 20070915 A 3350 CONNECTOR BOEING 747 747451 1384940 NM EMERGENCY LIGHTS LOOSE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 667US 24222 DURING OVERNIGHT CHECK, FLOOR PROXIMITY EMERGENCY LIGHTS WILL NOT TURN ON. MAINTENANCE SECURED CONNECTORS. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007092000227 20070920 00227 EU 2007 9 20 DHLA200700043 1 20070912 A 2560 INERTIA REEL AIRBUS 300 A300B4203 3930306 EU SEAT BELT LOOSE A DHLA O OTHER O OTHER TO TAKEOFF 1 GL 05 365DH 149 INERTIAL REEL CAME LOOSE DURING TAKEOFF ROLL. INSPECTED INERTIAL REEL. FOUND OK. REINSTALLED IN POSITION AS PER MM 25- 61-13. 2 L 7 2 4F RT A35EU 2007092000237 20070920 00237 EU 2007 9 20 07FDEA03593 1 20070912 A 5420 A54611160500 FITTING AIRBUS 300 A300B4605R 3930308 EU ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 DEEP CHAFING MARK FOUND ON PYLON NR 1SPIGOT FITTING FWD PYLON TO ENGINE MOUNT REPAIR PERFORMED BY BLEND OUT TO ELIMINATE SHARP EDGES IAW EA 6-5451-112496 AND RAS 053455/005/2007 ISS A. 2 L 7 2 4F RT A35EU 2007092000262 20070920 00262 NM 2007 9 20 HALA0700372 1 20070907 A 2912 FILTER BOEING 767 767332 1382001 NM HYD SYSTEM LEAKING A HALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 13 598HA 23278 ATB - HYD QTY R SYSTEM DECREASED TO .42. FOUND PACKING ON RT HYD DPI ON RETURN FILTER MODULE LEAKING. REPLACED PACKING S OPS LK OK. RESERVICED RT HYD SYS AND CLEANED AREA. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007092000275 20070920 00275 EA 2007 9 20 VNAA0709004 1 20070902 A 4990 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE APU OVERSERVICED A VNAA B EMER. DESCENT J WARNING INDICATION AP APPROACH 1 GL 05 241PS 7909 WITH THE APU SUPPLYING AIR TO THE PACK, AN OIL SMELL WAS NOTED ALONG AN ANTI-ICE DUCT WING WARNING MESSAGE. MAINTENANCE INSPECTED AND PERFORMED AN OPERATIONAL TEST OF THE RIGHT HAND FUSELAGE LOOPS AND THE APU. MAINTENANCE REMOVED REPLACED THE LOOP A18WK. MAINTENANCE ALSO FOUND THE APU OIL OVER SERVICED AND PROPERLY REDUCED THE OIL LEVEL. OPERATIONAL CHEC KS WERE GOOD AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007092000283 20070920 00283 EA 2007 9 20 TRAX200701272 1 20070829 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 CRACK FOUND ON ANGLE AT FS 280 RBL 9 OUTBOARD. REF: REO 601R-53-00-027. NEW ANGLE AT FS 280 RBL 9 OUTBOARD INSTALL IAW SRM 51-42-20. SUPPLEMENTAL - SDR CLOSED 09/12/07. 2 L 7 2 4F RT A21EA 2007092000286 20070920 00286 EU 2007 9 20 TRAX200701291 1 20070827 A 5711 SPAR AEROSP ATR72 ATR72 EU WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 CRACK DETECT - REAR SPAR LOWER SURFACE FLANGE AT RIB 4. COMPLIED WITH UNDER EXELTECH W/O YUL000780 NONROUTINE 280. REF ER TO THIS NONROUTINE FOR MTC ACTION. SUPPLEMENTAL - SDR CLOSED 09/12/07. 2 H 7 2 4T RT 2007092000296 20070920 00296 NM 2007 9 20 CALA0700511 1 20070910 A 5330 65C35768 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17326 23456 INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE R-2 DOOR LOWER HINGE CUTOUT AT STA 947.5-967, S14R TO S15R. THE CRACKED A REA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-60-01, REPAIR 7. 2 L 7 2 4F RT A16WE 2007092000306 20070920 00306 EA 2007 9 20 TRAX200701330 1 20070908 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT BINDS A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 820AS 7188 EXCESSIVE FORCE REQUIRED TO OPEN EMERGENCY DOOR. 2 L 7 2 4F RT A21EA 2007092000308 20070920 00308 NM 2007 9 20 QXEA200701413 1 20070912 A 2133 88060B010003 OUTFLOW VALVE BOMBDR DHC8 DHC8402 1390042 NM CABIN PRESSURE MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 429QX 673 673 4161 SEA FLIGHT NR 2232: AFTER TAKEOFF, THE A/C DID NOT PRESSURIZE AND CNT FAULT LIGHT ILLUMINATED. AFTER A FEW SECONDS, FAU LT LIGHT EXTINGUISHED AND A/C DID PRESSURIZE. AIRCRAFT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED FWD SAFETY VALVE, AFT OUTFLOW VALVE AND PRESSURE CONTROLLER. C/W FUNCTIONAL TEST OF THE PRESSURIZATION CONTROL IAW Q400 AMM 21-31- 00, TR 21-061, TASK 21-30-00-720-801. OPS CHECKED GOOD IN MANUAL AND AUTO MODE. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007092000309 20070920 00309 NM 2007 9 20 KCSA071361 1 20070912 A 5312 BULKHEAD BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 CRACK IN BULKHEAD AT BS 1440, LBL-118, WL-194. 2 L 7 4 4F RT A20WE 2007092000320 20070920 00320 NM 2007 9 20 QXEA200701428 1 20070914 A 2620 SQUIB BOMBDR DHC8 DHC8402 1390042 NM EXTINGUISHER BLOWN A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 424QX 4006 SMF FLIGHT NR 2359: 45 MINUTES INTO FLIGHT FROM PDX, MASTER WARNING AND CHECK FIRE DETECT LIGHT ILLUMINATED. ALSO BAGGA GE AFT AND FWD FIRE BOTTLE CAUTION LIGHT ILLUMINATED. MAINTENANCE PER Q400 FIM TASK 26-10-00-810-815, ITEM 4A(1). REMO VED AND REPLACED LOW RATE FIRE EXTINGUISHER BOTTLE AND FOUND SQUIB BLOWN. REMOVED AND REPLACED LOW RATE FIRE EXTINGUISH ER BOTTLE IAW MTC 6262205. REMOVED AND REPLACED DISCHARGED SQUIB IAW MTC 6262206. REMOVED SERVICEABLE SQUIB AND INSTAL LED ON NEW SERVICEABLE LOW RATE FIRE EXTINGUISHER BOTTLE. OPS CHECK GOOD PER AMM TASK 26-12-06-710-801 AND 26-20-00-710 -802. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007092000333 20070920 00333 NM 2007 9 20 AALA20071577 1 20070818 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 916AN 29517 DFW - EMERGENCY LIGHT AT SEAT ROW 14D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092000337 20070920 00337 NM 2007 9 20 AALA20071572 1 20070816 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 771AN 29579 MIA - EMERGENCY LIGHT AT SEAT 33C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 33C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007092000338 20070920 00338 NM 2007 9 20 QXEA200701412 1 20070911 A 5100 NONE BOMBDR DHC8 DHC8402 1390042 NM NONE NONE A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 424QX 4006 PDX FLIGHT NR 2244: AFTER ENGINE START AT PUSHBACK, NOTED NR 2 RUD HYD CAUTION LIGHT STAYED ILLUMINATED. AIRCRAFT RETUR NED TO BLOCK. MAINTENANCE REFERENCED SERVICE LETTER DH8-400-SL-007B AND DETERMINED TO BE A NUISANCE FAULT. POWERED A/C DOWN AND UP. GROUND RAN NR 2 ENGINE PER SAME SERVICE LETTER. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007092000356 20070920 00356 NM 2007 9 20 KCSA071365 1 20070912 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 CO-PILOT FWD I/B SEAT TRACK HAS A 3 INCH CRACK IN FWD CORNER. 2 L 7 4 4F RT A20WE 2007092000379 20070920 00379 WP 2007 9 20 ABXA070289 1 20070828 A 5320 991557713 INTERCOSTAL DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 INTERCOSTAL CRACKED AT STA 370, LONGERON 30 AND 2 GUSSETS GOUGED. REMOVED AND REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2007092000389 20070920 00389 NM 2007 9 20 SWAA074522 1 20070911 A 5311 6546533 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092000402 20070920 00402 NM 2007 9 20 SWAA074531 1 20070911 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092100004 20070921 00004 EU 2007 9 21 AALA20071672 1 20070901 A 3210 A5341130500201 BRACKET AIRBUS 300 A300B4605R 3930308 EU MLG UPLOCK BROKEN A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 40064 507 SJU INFLIGHT T1480/01SEP - NOSE GEAR WOULD NOT RETRACT. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. FOUND UPLOCK AFT SUPPORT BRACKET BROKEN. REPLACED UPLOCK ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007092100010 20070921 00010 WP 2007 9 21 AALA20071671 1 20070901 A 3222 STRUT DOUG DC9 DC983 3022083 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 948TW 49575 ORD INFLIGHT T1426 - AFTER GEAR RETRACTION RED NOSE GEAR DOOR LIGHTS REMAINED ILLUMINATED. RECYCLED GEAR WITH NO HELP. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPACKED NOSE LANDING HEAR STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION . 2 L 7 2 4F RT A6WE 2007092100014 20070921 00014 NM 2007 9 21 AALA20071674 1 20070901 A 2611 INDICATION SYS BOEING 777 777223 1385213 NM SMOKE DETECTION MALFUNCTIONED A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 21 759AN 32638 LHR INFLIGHT T100/01SEP - DURING APPROACH RECEIVED EICAS MESSAGE FOR SMOKE IN LAVATORY. LANDED WITHOUT INCIDENT. FOUND NO DAMAGE TO LAVATORIES AND NO EICAS MESSAGE PRESENT AND LAVATORY SMOKE DETECTORS PASSED TESTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007092100016 20070921 00016 EU 2007 9 21 07FDEA03878 1 20070918 A 5315 A53978267208 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 HEAVY CORROSION ON CROSSBEAM AT FRAME 67 RT, AFT CARGO COMPARTMENT FLOOR STRUCTURE, CARGO DOOR AREA. REPLACEMENT OF CRO SSBEAM IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100028 20070921 00028 EU 2007 9 21 07FDEA03796 1 20070825 A 5330 A53777054200 SKIN AIRBUS 310 A310222 3930315 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 PREVIOUS REPAIR FOUND LOCATED ON RT FUSELAGE, STA 1764/1817, BETWEEN STRG 31- 33RT. REPAIR REQUIRES EVALUATION FOR MAJO R/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAIR WAS ACCOMPLISHED IAW SRM 53-10-12 FIG 225 SHEET 1 AND FIG 217. 2 L 7 2 4F RT A35EU 2007092100032 20070921 00032 NM 2007 9 21 07FDEA03801 1 20070916 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 588FE 48490 CENTER LANDING GEAR LEFT MOUNTING. TRUNNION FITTING FORWARD AND AFT HOLE FOUND WITH CORROSION. 10-01-07 COMPLIED WI TH FEDEX E.A. 1-5310-115189. CLASSIFIED AS A MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007092100037 20070921 00037 EU 2007 9 21 07FDEA03806 1 20070917 A 5320 A53986750214 WEB AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND DAMAGED WEB PLATES BETWEEN FRAME 85-86, STRG 33 RT. REPLACMENT OF WEB PLATE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100045 20070921 00045 EU 2007 9 21 07FDEA03814 1 20070917 A 5320 A53778338248 PLATE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 CORRODED SHEAR PLATE AT FWD CARGO COMPARTMENT BETWEEN FRAME 38.1-38.2, STRG 43-44 LT. REPLACEMENT OF SHEAR PLATE IAW SR M 51-72-10. 2 L 7 2 4F RT A35EU 2007092100078 20070921 00078 EU 2007 9 21 07FDEA03785 1 20070914 A 5320 A53974265200 PROFILE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 CORRODED CORNER PROFILE (FITTING) BETWEEN FRAME 63-64 LT, CARGO COMPARTMENT FLOOR STRUCTURE. REPAIR PERFORMED BY REPLAC EMENT OF CORNER PROFILE (FITTING) IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100080 20070921 00080 EU 2007 9 21 07FDEA03787 1 20070914 A 5315 A53974222202 FLOORBEAM AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 CORROSION ON CROSSBEAM AT FRAME 66 RT, CARGO COMPARTMENT FLOOR STRUCTURE. CROSSBEAM SPLICE REPAIR PERFORMED IAW SRM 53- 10-15/FIG 207. 2 L 7 2 4F RT A35EU 2007092100082 20070921 00082 NM 2007 9 21 07FDEA03789 1 20070914 A 5311 66118088 FRAME BOEING 727 727233 138408A NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FWD PIT FRAME, STA 660 UPPER FLANGE HAS A DENT BETWEEN STR 23R-24R FOUND 3 DENTS ON UPPER FLANGE OF STA 660, BETWEEN S-2 2R -S-25R AND FOUND OUT OF LIMITS, CUTOUT DAMAGE, FORMED NEW FRAME SPLICE DOUBLER OUT OF 7075 O .050, HEAT TREATED MAT ERIAL 7075-T6 THEN DRILLED UP, TREATED AND PRIMED AND INSTALLED. REF SRM53-10-1 FIG IV, 51-30-3 FIG 1-6 AND EA NR 7-53 10-113085 2 L 7 3 4F RT A3WE 2007092100085 20070921 00085 NM 2007 9 21 07FDEA03792 1 20070914 A 5740 112N7011 FITTING BOEING 757 7572B7 1384964 NM ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 RIGHT WING DIAGONAL BRACE ATTACH FITTING (WING SIDE) HAS MIGRATING BUSHING. REMOVED, FABRICATED AND REPLACED MIGRATED B USHINGS IN ACCORDANCE WITH FEDEX EA NR F-5720-110765, DATED 7/30/2007 AND MAE TRAVELER NR T7/695654. CLASSIFIED AS A " MAJOR REPAIR" WITH NO FOLLOW UP ACTIONS REQUIRED. 2 L 7 2 4F RT A2NM 2007092100087 20070921 00087 EU 2007 9 21 AALA20071682 1 20070903 A 2750 COMPUTER AIRBUS 300 A300B4605R 3930308 EU SLAT FLAP FAULTED A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 40064 507 BOG INFLIGHT T915/03SEP - SLATS DID NOT EXTEND FOR LANDING. SLAT SYSTEM ONE AND TWO FAULT LIGHT ILLUMINATED. LANDED BO G WITHOUT INCIDENT. FOUND JAM FAULT ON BOTH SLAT FLAP CONTROL COMPUTERS (SFCC) AND FLAP COMMAND SENSOR UNIT ON SFCC NUM BER TWO. RESET BOTH SFCC AND FAULTS ERASED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007092100093 20070921 00093 EU 2007 9 21 07FDEA03862 1 20070917 A 5320 A53974216240 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 HEAVY CORROSION ON CLIP AT FRAME 71, BETWEEN STRG 55-56 LT. REPLACEMENT OF CLIP IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100098 20070921 00098 EU 2007 9 21 07FDEA03868 1 20070917 A 5320 A53974355200 FLANGE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 HEAVY CORROSION ON FLANGE BETWEEN FRAME 61-62, STRG 56 LT TO 56 RT. REPLACEMENT OF FLANGE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100103 20070921 00103 NM 2007 9 21 07FDEA03669 1 20070913 A 5753 6524691 SKIN BOEING 727 727233 138408A NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 LEFT WING INBD MID FLAP, LOWER SURFACE, VERY AFT ANGLE STRUCTURE IS CRACKED AT NUTPLATE, 55" FROM INBD EDGE INSTALLED AN GLE IAW 51-40-4 THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007092100106 20070921 00106 NM 2007 9 21 AALA20071665 1 20070901 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 681AA 25338 MIA - EMERGENCY LIGHTS FROM SEAT ROW 26 TO AFT OF CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SE AT ROW 26 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092100123 20070921 00123 NM 2007 9 21 AALA20071678 1 20070902 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 383AN 26995 DFW - EMERGENCY LIGHT AT SEAT 34H HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 34H. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007092100124 20070921 00124 NM 2007 9 21 AALA20071687 1 20070904 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 958AN 30091 MIA - EMERGENCY LIGHT AT SEAT 9D HAS MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092100125 20070921 00125 NM 2007 9 21 AALA20071701 1 20070907 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 795AN 30257 NRT - EMERGENCY LIGHT AT LOWER EDGE OF FORWARD COAT CLOSET IS BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LO WER EDGE OF FORWARD COAT CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007092100126 20070921 00126 NM 2007 9 21 AALA20071720 1 20070910 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 775AN 29584 MIA - EMERGENCY LIGHT AT SEAT 3D AFT MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 3D AFT. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007092100127 20070921 00127 EU 2007 9 21 AALA20071722 1 20070910 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80057 465 JFK - EMERGENCY LIGHT AT AFT CABIN RIGHT SIDE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT CABIN RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007092100128 20070921 00128 EU 2007 9 21 AALA2071706 1 20070908 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 40064 507 MIA - EMERGENCY LIGHT AT SEAT 28C BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 28C. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007092400005 20070924 00005 CE 2007 9 24 DXTA200702440 1 20070901 A 3240 BRAKE ASSY CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG NONE E DXTA K NONE O OTHER IN INSP/MAINT 1 GL 07 908QS 7500108 RT BRAKE REQUIRES EXCESSIVE FORCE FOR NORMAL BRAKING. SAME FOR LT AND RT SEAT PEDALS. PERFORMED HIGH SPEED TAXI CHECK AND APPLIED BRAKES NUMEROUS TIMES. NO EXCESSIVE FORCE WAS NEEDED TO APPLY RT BRAKE. INSPECTED NR 3 & 4 BRAKE ASSY. NO D EFECTS FOUND. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007092400006 20070924 00006 CE 2007 9 24 DXTA200702436 1 20070830 A 3240 387072 MOTOR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE BRAKE SYSTEM INTERMITTENT E DXTA K NONE O OTHER TX TAXI/GRND HDL 1 GL 07 394QS 9664 5600394 DURING TAXI, HEAVY PRESSURE HAS TO BE APPLIED TO BRAKES AND THEN THEY GRAB HARD. ALSO ON LANDING IT FEELS LIKE ANTISKID IS ACTIVATING FOR APPLIED PRESSURE. C/W 560 ANTI-SKID WIRING CHECK NO DEFECTS NOTED C/W VISUAL INSPECTION OF WIRING HARNESS CHECK GOOD. REMOVED AND REPLACED POWER BRAKE VALVE. BLED BRAKES TAXIED A/C BRAKES CHECK GOOD IAW CE560 MM 32 -42-05. 2 L 7 2 4F 4 F RT A22CE E25EA 2007092400095 20070924 00095 EU 2007 9 24 AALA20071737 1 20070912 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70054 461 MIA - EMERGENCY LIGHT AT SEAT 28G INOPERATIVE. REPAIRED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 28G. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007092400096 20070924 00096 NM 2007 9 24 AALA20071746 1 20070914 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 761AJ 31478 JFK - EMERGENCY LIGHT AT SEAT 4G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 4G. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT T00001SE 2007092400097 20070924 00097 NE 2007 9 24 AALA20071740 2 20070913 A 7230 COMPRESSOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RT ENGINE STALLED A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 234AA 49181 728077 STL INFLIGHT T1914/13SEP - FLIGHT EXPERIENCED COMPRESSOR STALL AT 800 FEET AND SEVERAL STALLS AT 16000 FEET. ENGINE INS TRUMENT INDICATIONS NORMAL. REDUCED NUMBER TWO ENGINE TO IDLE. RETURNED TO STL AND LANDED WITHOUT INCIDENT. REPLACED N UMBER TWO ENGINE ON 15 SEP 2007 AT STL DUE TO COMPRESSOR STALLS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007092400098 20070924 00098 WP 2007 9 24 AALA20071741 1 20070913 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 402A 49313 TPA - EMERGENCY LIGHT AT SEAT ROW 21E MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 21E. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007092400099 20070924 00099 NM 2007 9 24 AALA20071725 1 20070911 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 661AA 25295 SFO - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 22 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROW 22. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092400100 20070924 00100 EU 2007 9 24 AALA20071726 1 20070911 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 8067A 510 MIA - EMERGENCY LIGHTS AT LEFT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007092400101 20070924 00101 NM 2007 9 24 AALA20071747 1 20070915 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 928AN 29528 MIA - EMERGENCY LIGHT AT SEAT 20C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092400102 20070924 00102 NM 2007 9 24 DL764071194 1 20070911 A 2560 P20700140 FLASHLIGHT BOEING 767 767432ER 1385134 NM AFT CABIN WORN A DALA O OTHER O OTHER CR CRUISE 1 SO 27 838MH 29711 AFT LT F/A STATION EMERGENCY FLASHLIGHT USED. 2 L 7 2 4F RT A1NM 2007092400103 20070924 00103 NM 2007 9 24 DLM88071195 1 20070908 A 5310 DOOR FRAME DOUG MD88 MD88 3023688 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 951DL 49882 CORROSION ON AFT CARGO BIN DOOR JAMB WEB. BEAM OF LOWER DOOR JAMB WAS REPLACED IAW DOUGLAS REF INST DWG 5930483 REV AL. 2 L 7 2 4F RT A6WE 2007092400104 20070924 00104 NM 2007 9 24 DLM88071196 1 20070908 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 951DL 49882 FOUND CRACKED LT CUSP WEB AT STA Y=240. REPAIRED PER ERA 398191-14MA REV A. 2 L 7 2 4F RT A6WE 2007092400105 20070924 00105 NM 2007 9 24 DLM88071197 1 20070908 A 5320 BRACKET DOUG MD88 MD88 3023688 NM BS 660 BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 951DL 49882 BROKEN BRACKET AT STA 660 LT CUSP WEB. FABRICATED PER DOUGLAS DRW 5913698. INSTALLED PER DOUGLAS DWG 9930538. 2 L 7 2 4F RT A6WE 2007092400106 20070924 00106 NM 2007 9 24 DLM88071198 1 20070908 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 951DL 49882 FOUND CORROSION ON RIGHT CUSP WEB AT STA 322. REPAIRED PER ERA 398191-14MA REV A. 2 L 7 2 4F RT A6WE 2007092400107 20070924 00107 NM 2007 9 24 DLM88071199 1 20070908 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 664 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 951DL 49882 FOUND CORROSION ON RT CUSP WEB STA 664. REPAIRED PER SRM 51-70-4 FIG.2 2 L 7 2 4F RT A6WE 2007092400108 20070924 00108 NM 2007 9 24 DLM88071200 1 20070908 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 736 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 951DL 49882 FOUND CORROSION ON RT CUSP WEB AT STA 736. REPAIRED PER ERA 398191-14MA REV A. 2 L 7 2 4F RT A6WE 2007092400111 20070924 00111 WP 2007 9 24 AALA20071727 1 20070911 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 214AA 49162 DFW - EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD CABIN. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007092400112 20070924 00112 NM 2007 9 24 AALA20071732 1 20070912 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 615AM 24491 LAS - EMERGENCY LIGHTS AT AFT COACH CABIN INOPERATIVE. FOUND LEFT NUMBER ONE DOOR FLIGHT ATTENDANT EMERGENCY LIGHT CONS OLE SWITCH LEFT ON. REPLACED BATTERY PACK AT AFT SEAT ROW 32 FOR EMERGENCY LIGHTS AT AFT COACH CABIN. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092400113 20070924 00113 NM 2007 9 24 AALA20071761 1 20070917 A 3350 P4010049 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 329AA 22329 LAX - EMERGENCY LIGHTS AT SEAT 17AB AND LEFT FORWARD OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS A T SEAT 17AB AND LEFT FORWARD OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007092400114 20070924 00114 NM 2007 9 24 AALA20071762 1 20070918 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 697AN 26977 BOS - SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 25DEF MISSING. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092400115 20070924 00115 EU 2007 9 24 AALA20071751 1 20070915 A 2780 JACKSCREW AIRBUS 300 A300B4605R 3930308 EU SLATS INOPERATIVE A AALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 21 40064 507 JFK INFLIGHT T1582/15SEP - LEADING EDGE SLATS WOULD NOT EXTEND ON LANDING. AIRCRAFT DECLARED AN ALERT NUMBER 8. LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE LEADING EDGE SLAT JACKSCREW TRANSMISSION ON RIGHT WING, NUMBER ONE, TWO, THREE, AND FIVE LEADING EDGE SLAT JACKSCREW LEFT WING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007092400116 20070924 00116 WP 2007 9 24 AALA20071753 1 20070916 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 405A 49316 ORD - EMERGENCY LIGHT AT OVERHEAD FIRST CLASS GALLEY MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007092500001 20070925 00001 EU 2007 9 25 07FDEA03989 1 20070919 A 5310 A53610607206 FITTING AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION ON RUN OUT FITTING AT STRINGER P 44, C 16A-17. REPAIR PERFORMED BY REPLACEMENT OF PART IAW DRAWING R536 -10440 2 L 7 2 4F RT A35EU 2007092500002 20070925 00002 NM 2007 9 25 UPS07450630 1 20070910 A 3240 ACCUMULATOR BOEING 747 747123 1384873 NM BRAKE SYSTEM LEAKING A IPXA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 676UP 20101 INSPECTION TYPE:N/A PILOT REPORT - BRAKES SLOW TO RESPOND, FOUND BRAKE ACCUMULATOR LOW DURING ATTEMPTED SERVICE. FOUND LARGE AMOUNT OF HYD FLUID ON NITROGEN SIDE OF ACCUMULATOR. REMOVED AND REPLACED BRAKE ACCUMULATOR PER MM 32-41-09. SER VICED, OPS CHECK GOOD. 2 L 7 4 4F A20WE 2007092500005 20070925 00005 SO 2007 9 25 SIMA200726302 1 20070919 A 3210 LANDING GEAR EMB 135 EMB135KL 3260302 SO INOPERATIVE A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 807AE 145506 SOC REPORTED THE AIRCRAFT WAS RETURNING TO FIELD WITH GEAR THAT WOULD NOT RETRACT. 2 L 7 2 4F RT T00011AT 2007092500006 20070925 00006 SO 2007 9 25 SIMA200726202 1 20070917 A 2120 4611028900 FAN EMB 145 EMB145LR 3260212 SO RECIRCULATION FAILED A SIMA D RETURN TO BLOCK M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 630AE 145132 DURING TAXI OUT FLIGHT ATTENDANT ADVISED CREW OF ODOR OF SMOKE IN CABIN. PAX COMPLAINED OF THERE FEET FELT HOT ON THE FLOOR. A/C RETURN TO GATE. OTHER PAX CONFIRMED ODOR OF SMOKE. INSPECTED BLEED AIR SYSTEM NO DEFECT NOTED. REMOVE FLO OR PANEL TO INSPECT THE RECIRCULATION FAN. FAN WAS INOP. MEL RECIRCULATION FAN. REMOVED AND REPLACED RECIRCULATION FA N. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007092500007 20070925 00007 2007 9 25 SIMA200726201 4 20070918 A 3442 7021450601 ANTENNA EMB 145 EMB145LR 3260212 SO WX RADAR SYS FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 693AE 14500868 DIVERTED TO DFW WEATHER RADAR FAILED EN ROUTE TO MCI WHEN RADAR TESTED IT DISPLAYED RADAR FAIL CODE J TILT UNCALIBRATED POC O EL POSITION. REMOVED AND REPLACED WEATHER RADAR ANTENNA ASSEMBLY. OPS CK GOOD IAW AMM 34-42-00. AIRCRAFT RETURN ED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007092500008 20070925 00008 NM 2007 9 25 QXEA200701436 1 20070914 A 5321 FLOORBOARD DHAV DHC8 DHC8202 2809007 NM BS 599 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - FLOORBOARD FLANGE AT STATION 599.00 RIGHT END UPPER SURFACE HAS CORROSION. REPAIRED IAW SRM 51-20-11, 51-40-11 , AND 51-20-16. 2 H 7 2 4T RT A13NM 2007092500009 20070925 00009 NM 2007 9 25 QXEA200701439 1 20070915 A 5210 SKIN DHAV DHC8 DHC8202 2809007 NM PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - MAIN CABIN DOOR SHELL HAS CORROSION BY FORWARD NR 1 STOP/STEP ASSEMBLY ATTACH POINT. REPAIRED IAW SRM 51-20-11 , 51-20-16, 51-20-26. 2 H 7 2 4T RT A13NM 2007092500011 20070925 00011 NM 2007 9 25 QXEA200701430 1 20070914 A 5310 FRAME DHAV DHC8 DHC8202 2809007 NM BS 201 S31L CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - FORWARD CENTER UNDERFLOOR VERTICAL FRAME STRUCTURE AT STATION 201, STRINGER 31L. SUSPECT CORROSION UP FRONT SK IN ON AFT INBOARD CORNER OF FLOOR RISER FRAME. REPAIRED IAW SRM 51-20-36, 51-20-11, 51-20-26, AND 51-2016. 2 H 7 2 4T RT A13NM 2007092500012 20070925 00012 NM 2007 9 25 QXEA200701431 1 20070913 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM RT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX -TOP SURFACE OF BOTTOM PANEL OF RIGHT WING IS SCRATCHED IN MULTIPLE PLACES BETWEEN YW 171 AND YW 139 AFT OF FRONT SPAR. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-20-41. 2 H 7 2 4T RT A13NM 2007092500014 20070925 00014 2007 9 25 UPS07850631 4 20070905 A 2565 SLIDE DOUG DC8 DC871F 302199D WP COCKPIT LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:N/A ESCAPE SLIDE IS LOOSE. REINSTALLED ESCAPE SLIDE. 2 L 7 4 4F RT 4A25 2007092500015 20070925 00015 NM 2007 9 25 QXEA200701432 1 20070915 A 5320 BRACKET DHAV DHC8 DHC8202 2809007 NM BS 201 S31R CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - SUSPECT CORROSION TO HORIZONTAL STRINGER/RISER BRACKET AT STRINGER 31R STATION 201. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007092500016 20070925 00016 WP 2007 9 25 UPS07850633 1 20070816 A 5320 5615530183SAAU ATTACH ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 ATTACH ANGLE CORRODED AT RIGHT END OF CENTER J-BEAM ON STA 8 BULKHEAD IN A/C COMPARTMENT. REMOVED, F ABRICATED AND INSTALLED A/C COMPARTMENT RIGHT CENTER J-BEAM ATTACH ANGLE ON STA 8 BULKHEAD IAW SRM 51-01-21, SRM 51-1-8, SRM 53-2-0 FIG 1F AND DWG 5615530. 2 L 7 4 4F RT 4A25 2007092500017 20070925 00017 NM 2007 9 25 QXEA200701433 1 20070913 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM LT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - TOP SURFACE OF BOTTOM PANEL OF LEFT WING IS SCRATCHED IN MULTIPLE PLACES BETWEEN YW 155 AND YW 139 FORWARD REAR SPAR. REPAIRED IAW SRM 51-20-11, 51-20-16, AND 51-20-41. 2 H 7 2 4T RT A13NM 2007092500022 20070925 00022 WP 2007 9 25 UPS07850636 1 20070910 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK PER MM 33-50-01- 2. OPS CHECKS NORMAL. 2 L 7 4 4F RT 4A25 2007092500023 20070925 00023 EU 2007 9 25 07FDEA03947 1 20070827 A 5347 A5381312920000 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 DUMMY TRACK NR 5 RT AT Y-1959 BETWEEN FR 54 AND FR 54.2 CRACKED AT LOCKS. THE DUMMY TRACK WAS REPLACED IAW SRM 51-72-10 . 2 L 7 2 4F RT A35EU 2007092500024 20070925 00024 WP 2007 9 25 UPS07850639 1 20070911 A 2560 DOOR DOUG DC8 DC873F 302199F WP COCKPIT LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:N/A CAPT ESCAPE ROPE DOOR LOOSE, ROPE FELL OUT. ROLLED, INSTALLED ESCAPE ROPE. RESECURED ESCAPE ROPE D OOR, OK TO CONTINUE. 2 L 7 4 4F RT 4A25 2007092500027 20070925 00027 WP 2007 9 25 MWEA070212 1 20070910 A 5752 5910047502 TAB DOUG DC9 DC981 3022081 WP RT AILERON CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 RIGHT WING AILERON CONTROL TAB HAS CORROSION UNDER SKIN, OUTBOARD TRAILING EDGE. REMOVED CORROSION AND FABRICATED AND I NSTALLED CONTROL TAB. 2 L 7 2 4F A6WE 2007092500031 20070925 00031 NM 2007 9 25 QXEA200701441 1 20070916 A 2435 400SG163Q STARTER GEN BOMBDR DHC8 DHC8402 1390042 NM NR 2 WARNING LIGHT A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 431QX 6157 134 4164 SEA FLIGHT NR 2241: NR 2 DC GEN CAUTION. AIRCRAFT RETURNS TO BLOCK. MAINTENANCE REMOVED AND REPLACED NR 2 DC STARTER/G ENERATOR IAW TC 6243101 (1-4). GROUND RAN. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007092500034 20070925 00034 NM 2007 9 25 AALA20071759 1 20070917 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 767AJ 33539 NRT - EMERGENCY LIGHT AT FIRST CLASS GALLEY WALL MISSING. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FIRST CLASS GA LLEY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007092500035 20070925 00035 2007 9 25 ZZDA2007269 4 20070910 A 2565 5A33075 SLIDE BOEING 737 7377BD 1384511 NM R1 DOOR UNWANTED DEPLOY A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 296AT 34861 R-1 DOOR SLIDE ACCIDENTALLY DEPLOYED WHEN DOOR WAS OPENED. GIRT BAR WAS NOT IN FLOOR RECEPTACLE, IT HAD BEEN DISARMED. SLIDE FULLY DETACHED FROM A/C. REMOVED & REPLACED R-1 DOOR SLIDE, OPS CHECK GOOD IAW AMM 25-66-01. A/C OK FOR SERVICE . 2 L 7 2 4F RT A16WE 2007092500036 20070925 00036 NM 2007 9 25 AALA20071752 1 20070915 A 3350 CM767 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 183AN 29593 SFO - EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092500038 20070925 00038 NM 2007 9 25 ZZDA2007270 1 20070905 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 932AT 55073 MAJOR REPAIR TO FUS STA 237 LONG 16 AND 17 LT SIDE DENTED. FABRICATED DOUBLER REPAIR PER B717 SRM 53-00-01 REPAIR 6. 2 L 7 2 4F TR A6WE 2007092500039 20070925 00039 2007 9 25 AALA20071750 2 20070915 A 7261 PUMP DOUG DC9 DC983 3022083 WP RT ENGINE INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 980TW 53630 DFW INFLIGHT T2320/15SEP - DURING CLIMB NUMBER TWO ENGINE OIL PRESSURE BEGAN TO DROP. DROPPED RAPIDLY THEN CAME BACK TO NORMAL WHEN THROTTLES BROUGHT BACK TO IDLE. OIL TEMPERATURE INDICATED HIGH. RETURNED TO DFW AND LANDED WITHOUT INCIDE NT. REPLACED NUMBER TWO ENGINE OIL PUMP AND CHECKED OIL FILTERS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007092500040 20070925 00040 NM 2007 9 25 SWAA074518 1 20070911 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 408WN 27895 DURING SCHEDULED HC2 CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007092500041 20070925 00041 NM 2007 9 25 AALA20071754 1 20070916 A 3350 LIGHT BOEING 757 7572Q8 1384972 NM CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 713TW 28173 DFW - EMERGENCY LIGHT STRIP IN FIRST CLASS LOOSE. SECURED EMERGENCY LIGHT STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092500043 20070925 00043 NM 2007 9 25 AALA20071755 1 20070916 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 359AA 24040 MIA - EMERGENCY LIGHT AT SEAT 11B INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 11B. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007092500045 20070925 00045 NM 2007 9 25 SWAA074517 1 20070911 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 219WN 32490 DURING SCHEDULED MV1 CHECK, FOUND EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007092500047 20070925 00047 2007 9 25 SWAA074540 4 20070911 A 2565 63550 SLIDE BOEING 737 7373Q8 1384670 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007092500049 20070925 00049 NM 2007 9 25 SWAA074521 1 20070911 A 5311 6546527 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092500050 20070925 00050 NM 2007 9 25 SWAA074550 1 20070911 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092500051 20070925 00051 NM 2007 9 25 SWAA074523 1 20070911 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092500052 20070925 00052 NM 2007 9 25 SWAA074536 1 20070911 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092500053 20070925 00053 NM 2007 9 25 SWAA074537 1 20070911 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092500054 20070925 00054 NM 2007 9 25 2007UALA03344 1 20070823 A 3230 EXTENSION SYS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RT MLG OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA 25158 DRNG TEST FLT RT WING GEAR DOOR NOT OPEN IN ALTERNATE GEAR MODE. LT WING DID OPEN SATISFACTORIALLY. ADJUSTED RT MLG A LT EXT SYS IAW MM32 36 00 PB 501. DURING OP TEST, GEAR DOOR OPS OK IN ALTERNATE EXTEND MODE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092500055 20070925 00055 NM 2007 9 25 SWAA074538 1 20070911 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092500059 20070925 00059 NM 2007 9 25 SWAA074547 1 20070911 A 5313 65C27314 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER 16L CRACKED AT BS 500B. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007092500061 20070925 00061 NM 2007 9 25 SWAA074544 1 20070911 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER 4R CRACKED AT BS 313. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007092500062 20070925 00062 NM 2007 9 25 USAA920070823 1 20070910 A 5330 6545774 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 531AU 24478 CLT - MAJOR REPAIR - RON -NR 7639822, CRACKED FUSELAGE SKIN, BS 727E, S23L. REPAIRED FUSELAGE SKIN, BS 727E, S23L IAW B 737-300 SRM 53-00-01 REPAIR 31 AND USAIRWAYS TYPICAL REPAIR 53-60-03A. 2 L 7 2 4F RT A16WE 2007092500064 20070925 00064 NM 2007 9 25 USAA920070825 1 20070908 A 5754 65C267751 ATTACH FITTING BOEING 737 7374B7 1384702 NM KRUEGER FLAP CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 459UW 25023 CLT - MAJOR REPAIR, CRACKED WING NR 2 KRUEGER FLAP ATTACH FITTING, LEADING EDGE STATION 106.5 - LEADING EDGE STATION 118 .47. REPLACED WING NR 2 KRUEGER FLAP ATTACH FITTING, LEADING EDGE STATION 106.5 - LEADING EDGE STATION 118.47 IAW USAIR WAYS EA 98873. 2 L 7 2 4F RT A16WE 2007092500066 20070925 00066 NE 2007 9 25 HEEA116985 1 20070822 A 7100 70BMA01080 ECU SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL2S1 60057 NE INOPERATIVE E HEEA O OTHER O OTHER LD LANDING 1 SW 03 734P 760600 ON LANDING, NR 1 DECU CIRCUIT BREAKER POPPED. ON TURNING ON THE BATTERY, CIRCUIT BREAKER POPPED AGAIN. MAINTENANCE REP LACED THE ELECTRONIC CONTROL UNIT. 1 G 7 2 3U 4 U NC H1NE E00054EN 2007092500067 20070925 00067 CE 2007 9 25 DXTA200702444 1 20070903 A 2612 FIRE WARNING RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP CARGO BAY FALSE ACTIVATION E DXTA O OTHER N FALSE WARNING CL CLIMB 1 GL 07 821QS 258709 BAG FIRE LIGHT ILLUMINATED INTERMITTENTLY AFTER TAKEOFF. REPLACED SMOKE DETECTOR SYSTEM CONTROL AMPLIFIER I/A/W 800XP M M ADDENDA 26-11-00. OPS CHECK GOOD WITH TEST SWITCHES. 2 L 7 2 4F 4 F RT A3EU E6WE 2007092500070 20070925 00070 NE 2007 9 25 DXTA200702451 2 20070906 A 7200 ENGINE BEECH MU300 400A 1155402 CE PWA 545 PW545A NE POWER LOSS E DXTA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 07 147QS RK436 TARGET TAKEOFF POWER COMPUTED AS 99.0 PERCENT N1. CONDITIONS SEA LEVEL 22 DEG C. POWER AT 0 KNOTS 97.5 PERCENT N1. POWER AT 80 KNOTS 98.0 PERCENT N1 TAKEOFF ABORTED. PERFORMED ENGINES GROUND CHECKS I.A.W HAWKER 400XP MAINT MANUAL 71-00-00 , FIG 206. FOUND THAT N1 FOR THE DAY WAS ACHIEVED WELL WITHIN LIMITS. PERFORMED CHECK 3 TIMES ALL CHECKED OK. 2 H 7 2 4F 4 F RT A16SW E00059EN 2007092500073 20070925 00073 CE 2007 9 25 DXTA200702446 1 20070903 A 3240 BRAKE ASSY RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MALFUNCTIONED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 885QS 258743 WHEN APPLYING BRAKES, LT BRAKE PRESSURE INDICATES 400 TO 500 PSI HIGHER THAN THE RT BRAKE PRESSURE INDICATION. RT BRAKE FEELS SPONGY AND MORE RT BRAKE TRAVEL IS REQUIRED WHEN BRAKING BOTH PEDALS. AT 80 KNOTS ON LANDING ROLL OUT LT BRAKE IND ICATED 1000 PSI AND RT BRAKE INDICATED 500 PSI. ALSO, AT SLOW TAXI SPEEDS LT BRAKE INDICATES HIGHER PRESSURE THAN RT BRA KE. ACCOMPLISHED RT BRAKE BLEEDING IAW 800XP AMM 32-40-00. OPERATED BRAKES SEVERAL TIMES BOTH WITH RUDDER PEDALS AND P ARKING BRAKE HANDLE. BRAKE FEEL AND PRESS INDICATION MATCH SIDE TO SIDE. 2 L 7 2 4F 4 F RT A3EU E6WE 2007092500074 20070925 00074 CE 2007 9 25 DXTA200702454 1 20070907 A 3260 SWITCH CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE NLG OUT OF RIG E DXTA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 07 387QS 6800119 WHEN RETRACTING THE LANDING GEAR, A LOUD RATTLING SOUND AND VIBRATION OCCURED AND THE LANDING GEAR WOULD NOT RETRACT. I T APPEARED TO COME FROM THE NOSE GEAR. ALL GREEN LIGHTS WENT OUT AND THE RED UNLOCK LIGHT REMAINED. ADDITIONALLY, THE AMBER WOW MISCOMPARE EICAS MSG ILLUMINATED. WHEN THE GEAR HANDLE WAS LOWERED TO THE EXTEND POSITION, ALL INDICATIONS WE RE NORMAL AND ALL SYSTEMS WORKED NORMALLY ON LANDING. FOUND NOSE WOW SWITCH OUT OF RIG. ADJUSTED NOSE WOW SWITCH IAW CE SSNA 680 MM 32-60-00. VERIFIED NO WOW MISCOMPARE EICAS MESSAGE. INTERROGATED CMC WOW PCB BOARDS WITH NO DISCREPANCIES NO TED. 2 L 7 2 4F 4 F RC T00012WI E35NE 2007092500075 20070925 00075 NM 2007 9 25 USAA920070826 1 20070912 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 452UW 24979 CLT - MAJOR REPAIR - FPBH, CRACKED BULKHEAD WEB, BS 178, RBL 9.6, WL 234. REPAIRED BULKHEAD WEB, BS 178, RBL 9.6, WL 23 4 IAW B737-400 SRM 53-10-08. 2 L 7 2 4F RT A16WE 2007092500076 20070925 00076 CE 2007 9 25 DXTA200702455 1 20070907 A 3240 CABLE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG BRAKE ASSY STICKING E DXTA O OTHER O OTHER LD LANDING 1 GL 07 908QS 7500108 BRAKES REQUIRE EXCESSIVE FORCE FOR LANDING AND TAXIING. AFTER LANDING, BRAKES SEEMED AT TIMES AS IF THEY WERE DRAGGING A ND HAD TO APPLY 50+ N2 TO TAXI. VERIFIED SQUAWK. RT BRAKES LOCK UP WHEN HYDRAULIC POWER IS ON. TROUBLESHOT STICKY CABL E, C/P SEAT. LUBED CABLE COMPLIED WITH TAXI CHECK. OPS CHECKED GOOD IAW 750 M/M CH 32-42-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007092500078 20070925 00078 CE 2007 9 25 DXTA200702456 1 20070909 A 2910 LINE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL HYD SYSTEM RUPTURED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 923QS 7500023 ON TAKEOFF AT GEAR RETRACTION, A POP WAS HEARD FOLLOWED BY (L) HYD, LOW CAS( L), HYD PUMP FAIL, PTU FAIL, AND RT HYD OVE RTEMP. CHECKLIST FOLLOWED. GEAR BLOWN DOWN AND LANDED UNEVENTFULLY. ALL CAS OCCURED WITHIN 3 MINS. FOUND NOSE RETRACT LINE RUPTURED. REPLACED BOTH PRESSURE LINES BOTH ENGINE DRIVEN HYD PUMPS, PTU, SYS A & B PRESSURE & RETURN FILTERS. SY STEMS FLUSHED. LEAK & OPS CHKS OK. IAW MM 29-10-00, 29-10-08, 29-20-04, 29-10-02, 32-30-00, & 32-00-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007092500079 20070925 00079 CE 2007 9 25 DXTA200702458 1 20070909 A 3241 ANTI-SKID SYS BEECH MU300 400A 1155402 CE MLG INOPERATIVE E DXTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 114QS RK469 ANTI SKID INOP ON LANDING IN SDF (HARD PEDALS AND WHEEL BRAKES LOCKING). RAN & TAXIED AIRCRAFT TO PERFORM OPERATIONAL CHECK AND TO VERIFY SQUAWK. COULD NOT DUPLICATE SQUAWK AFTER SEVERAL ATTEMPTS W/ SWITCH IN EACH POSITION. SYSTEM OPERATE S NORMALLY. PERFORMED WORK IAW THE HAWKER 400XP MM CH 32-40. 2 H 7 2 4F RT A16SW 2007092500082 20070925 00082 NM 2007 9 25 USAA920070815 1 20070906 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518UW 23704 CTL - MAJOR REPAIR - C-5 CHECK, LEVEL 2 CORROSION ON FRAME, BS 1006, BL 0. REPAIRED FRAME, BS 1006, BL 0 IAW B737-300 S RM 53-00-07 REPAIR 6. 2 L 7 2 4F RT A16WE 2007092500083 20070925 00083 NM 2007 9 25 224297 1 20070905 A 2910 144327 HOUSING WHITTAKER DOUG MD80 MD83 3023681 NM VALVE CRACKED B K NONE O OTHER IN INSP/MAINT 1 NM 01 5654 BODY IS CRACKED BELOW THREADS. 2 L 7 2 4F RT 2007092500086 20070925 00086 SO 2007 9 25 C2XA07TY051 1 20070913 A 5320 14521725001 SILL EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16525 145403 LT SILL CORROSION AROUND FASTENERS AT FRM 22. REMOVED AND REPLACED SILL IAW SRM 51-40-22, AIRCRAFT STILL IN C CHECK. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007092500087 20070925 00087 SO 2007 9 25 UG8A2007GM05S 1 20070829 A 5730 1159WM54575 SKIN GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE LT WING CHAFED E UG8A K NONE O OTHER IN INSP/MAINT 1 GL 23 5101 5623 550 DURING COMPLIANCE WITH POST FLIGHT INSPECTION IT WAS NOTED THAT THE LT AND RT WING A FLAP TRACK ISLAND HAT PANELS WERE C HAFING THROUGH THE WING TRAILING EDGE FIXED COVE PANEL. MFG ENGINEERING DISPOSITION NR CS117877 RELEASED OUTLINING REPA IR FOR CONDITION. REPAIRED IAW ENGINEERING DISPOSITION AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A12EA E00057EN 2007092500090 20070925 00090 CE 2007 9 25 DXTA200702441 1 20070902 A 7830 WARNING LIGHT CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE THRUST REVERSER ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 362QS 6800051 AFTER TAKEOFF (ABOUT 500 FT) THE LT RED EMERGENCY STOW LIGHT ILLUMINATED. A FEW SECONDS LATER THE AMBER CAS MSG (T/R UNL OCK LIGHT) CAME ON. COULD NOT DUPLICATE, ALL CHECKS ON GROUND GOOD. REACTIVATED T/R'S WORK DONE IAW 78-30-00 AND 45-40- 00 OF THE CE680 M/M AND 78-30-01 OF THE CE680 WIRING DIAGRAM MANUAL 2 L 7 2 4F 4 F RC T00012WI E35NE 2007092500091 20070925 00091 CE 2007 9 25 DXTA200702442 1 20070902 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE WEAK E DXTA K NONE O OTHER TX TAXI/GRND HDL 1 GL 07 398QS 5600522 COPILOTS RT BRAKE PEDAL IS SOFT. 2 L 7 2 4F 4 F RT A22CE E25EA 2007092500098 20070925 00098 NM 2007 9 25 KPVA200715 1 20070912 A 2611 SMOKE WARNING DHAV DHC8 DHC8103 1386005 NM PWA 120 PW120 NE CARGO BAY INTERMITTENT A KPVA O OTHER N FALSE WARNING DE DESCENT 1 WP 13 808WP 026 INTERMITTENT SMOKE WARNING LIGHT ILLUMINATED DURING FLIGHT. (MX) INSPECTED SMOKE WARNING SYSTEM AND FOUND CELL PHONE RIN GING IN BAGGAGE COMPARTMENT. PERFORMED SMOKE WARNING SYSTEM TEST IAW MM 26-12-00 PG. 201, NO DEFECTS NOTED. 2 H 7 2 4T 4 T RT A13NM E20NE 2007092500099 20070925 00099 CE 2007 9 25 GLBA20061005 1 20070921 A 5311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A6 52043 EA FUSELAGE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 210GL UE210 FRAME CRACKED AT FS 164 AT STRINGER 9AL. CRACK LENGTH APPROXIMATELY 4 INCHES. 09-26-07 REPAIRED FRAME CRACK AT STRING ER RELIEF HOLE FS 164 AT STRINGER 9AR IAW BEECH 1900D SRM 51-70. REAPIR APPROXIMATELY 2.5" BY 4.1" .080 2024 T-3. 2 L 7 2 4T 3 T RT A24CE E4EA 2007092500101 20070925 00101 WP 2007 9 25 MWEA070214 1 20070912 A 5534 9911839 SUPPORT ANGLE DOUG DC9 DC981 3022081 WP VERTICAL STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 VERTICAL STABILIZER TO FUSELAGE INTERSECTION LINE, AFT SPAR LEFT SUPPORT ANGLE IS CRACKED. FABRICATED AND INSTALLED ANG LE. 2 L 7 2 4F A6WE 2007092500102 20070925 00102 CE 2007 9 25 DXTA200702466 1 20070910 A 2435 STARTER GEN CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE LEFT TRIPPED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 338QS 6800011 DURING TAKEOFF POWER APPLICATION THE LT GENERATOR HAS TRIPPED OFF LINE. ALL PRE-FLIGHT TESTS AND STARTS SHOW NORMAL OPER ATION. REPLACED LT ENGINE STARTER/GEN WITH OVH STARTER/GEN. PERFORMED GROUND OPS TEST OF BOTH GENERATORS, TEST GOOD. R AN LT ENG TO POWER WITH NO FAILURES. ALL WORK IAW 560 M/M 80-11-01 2 L 7 2 4F 4 F RC T00012WI E35NE 2007092500103 20070925 00103 CE 2007 9 25 DXTA200702465 1 20070910 A 2710 SERVO CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE AILERONS OUT OF ADJUST E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 338QS 6800011 AIRCRAFT WILL NOT FLY STRAIGHT WITH A/P AT FL360. AILERON TRIM FULL R. RUDDER TRIM .1250 L, SLIGHT LT TURN, FUEL BALAN CED, .79M / FL240 A TRIM FULL R - RUD TRIM .1250 L, NO TURNS, FUEL BALANCED, 290 KTS / 10,000 FT A TRIM .5 R - RUD T RIM .1250 L, NO TURNS FUEL BALANCED, 250KTS & VMO. 09-27-07 ADJUSTED RT AILERON SERVO TAB FROM TRAILING EDGE UP 4.8* TO TRAILING EDGE UP 3.0*. I.A.W. CE680 MM 27-00-00. VERIFIED RUDDER RIG CHECK REFERENCE CE680 MM 27-20-00. FOUND TO BE WITHIN SPEC. 2 L 7 2 4F 4 F RC T00012WI E35NE 2007092500104 20070925 00104 WP 2007 9 25 MWEA070215 1 20070913 A 5321 993663915 FLOOR PANEL DOUG DC9 DC981 3022081 WP CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 CENTER CABIN FLOOR PANEL FRAME STATION 826-886 HAS SIDE FLANGE CRACKED AT RIVETS. FABRICATED AND INSTALLED FLANGE. 2 L 7 2 4F A6WE 2007092500105 20070925 00105 CE 2007 9 25 DXTA200702463 1 20070910 A 2897 CIRCUIT BOARD CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE CROSSFEED SYS MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 673QS 5605651 AIRCRAFT WILL NOT CROSSFEED IN FLIGHT. HAD NORMAL INDICATIONS OF CROSSFEED BUT NO FUEL TRANSFER FROM LT TO RT. TRANSFER FROM T TO LT HAD BOTH LOW FUEL PRESSURE LIGHTS AND LT BOOST PUMP ILLUMINATED. NO CROSSFEED LIGHT INDICATION. ON THE GRO UND STILL NO FLOW INDICATION WHEN CROSSFEEDING LT TO RT. ATTEMPTING TO CROSSFEED RT TO LT ONLY CROSSFEED LIGHT INDICATI ON. RT BOOST PUMP ON, NO INDICATION OR NOISE. 09-27-07 T/S TO INTEMITTENT RT FUEL BOOST "CB" & RT FUEL PC BOARD REMO VED & REPLACED RT FUEL "CB" & RT FUEL PC BOARD. RAN FOR OPS CHECKS. SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME. ALL WO RK DONE IAW CE560XL MM 24-00-00 & 28-20-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007092500106 20070925 00106 CE 2007 9 25 DXTA200702462 1 20070910 A 3240 BRAKE ASSY CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG DRAGGING E DXTA O OTHER M B J OVER TEMP SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 936QS 7500036 DURING HIGH SPEED TAXI CHECK AT 80 KTS, APPLIED LIBERAL BRAKING AND TAXIED TO FBO USING MINIMAL BRAKING. AFTER EXITING A IRCRAFT WE NOTICED LT WHEEL WAS SMOKING HEAVILY. BRAKES CONTINUED TO SMOKE FOR 15 - 20 MINUTES. NR 1 MAIN TIRE WAS EXT REMELY HOT TO THE TOUCH. SUSPECT NR 1 AND NR 2 BRAKES WERE DRAGGING ON LT MAIN GEAR. NO FLUIDS WERE FOUND IN OR AROUND W HEEL ASSEMBLY. AXIAL MOVEMENT NR 1 BRAKE ROTOR LESS THAN THE OTHERS STATIC. REMOVED DEFECTIVE NR 1 AND 2 BRAKE ASSY'S. INSTALLED BRAKE ASSY'S OVERHAULED IAW CE750 MM 32-42-01. BLED BRAKES. BRAKES LEAK AND OP'S CHECK OK IN HGR AND ON TAX I CHECK. RESERVIOR SERVICED TO 77% (A) WITH HYD FLUID 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007092500108 20070925 00108 EU 2007 9 25 TRAX200701288 1 20070827 A 5711 SPAR AEROSP ATR72 ATR72 EU WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 SDI - CRACK DET - REAR SPAR LOWER SURFACE FLANGE BETWEEN RIB 12 & RIB 13. COMPLIED WITH UNDER EXELTECH W/O YUL000780 NO N-ROUTINE 284. REFER TO THIS NONROUTINE FOR MTC ACTION. SUPPLEMENTAL - SDR CLOSED 09/13/07. 2 H 7 2 4T RT 2007092500109 20070925 00109 CE 2007 9 25 S2YA07005 1 20070908 A 5347 114430074141 SEAT TRACK BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 290 CRACKED A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 91SK UE91 DURING STRUCTURAL INSPECTION OF THE AIRCRAFT, A CRACK WAS FOUND IN A SEAT TRACK EXTRUSION. THE SEAT TRACK IS LOCATED AT FS 290.85 EXTENDING APPROXIMATELY 5 INCHES. THE DAMAGE CONSISTED OF A HALF-INCH CRACK IN THE LOWER VERTICAL FLANGE WHERE THE UPPER PORTION OF THE TRACK IS CUT AWAY FOR ATTACHMENT TO THE MAIN SPAR. THE TRACK WAS REPAIRED IAW ENGINEERING REPO RT 6739-1 REVISION A. THE REPAIR CONSISTED OF STOP DRILLING THE CRACK AND BONDING AND RIVETING A DOUBLER OVER THE CRACKE D FLANGE. THE REPAIR WAS RECORDED AND SUBMITTED ON A 337. THE TIME OF THIS PART IS UNKNOWN, MOST LIKELY ORIGINAL EQUIPME NT. 2 L 7 2 4T 4 T RT A24CE E26NE 2007092500111 20070925 00111 EU 2007 9 25 09152007TB 1 20070915 A 5300 NONE BOLKMS 105 BO105LSA3 5626020 EU STRUCTURE NONE D JBZA A UNSCHED LANDING E VIBRATION/BUFFET NR NOT REPORTED 1 WP 27 31RX 2015 THE EMS FLIGHT WAS ENROUTE WITH PATIENT ON BOARD, CREW HEARD LOUD BAND SOUND OUTSIDE OF AIRCRAFT, NO INSTRUMENTATION WAR NINGS, PILOT ELECTED PRECAUTIONARY LANDING A CLOSEST AIRPORT. EMS FLIGHT CONTINUED WITH ANOTHER AIRCRAFT, BASE MECHANIC RESPONDED, FOUND EVIDENCE OF SMALL BIRD STRIKE NEAR MAIN ROTOR HEAD ASSEMBLY AND UPPER COWL. MECHANIC PERFORMED INSPECTI ON AND OPERATIONAL CHECKS OF SYSTEM, AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 2 3U H3AU 2007092500112 20070925 00112 EU 2007 9 25 TRAX200701293 1 20070827 A 5711 SPAR AEROSP ATR72 ATR72 EU WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 SDI - CRACK DETECT - REAR SPAR LOWER SURFACE FLANGE AT RIB 8. COMPLIED WITH UNDER EXELTECH W/O YUL000780 NON-ROUTINE 21 4. REFER TO THIS NON-ROUTINE FOR MTC ACTION. SUPPLEMENTAL - SDR CLOSED 09/13/07. 2 H 7 2 4T RT 2007080200051 20070802 00051 EA 2007 8 2 SWIA200718524 1 20070531 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 973SW 7949 FS280 FLOOR SUPPORT BEAM IS CRACKED AT LOWER RBL9, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLES, CLIPS, AND FILLER IA W CRJ200 REO 601R-53-11-171, REV D. 2 L 7 2 4F RT A21EA 2007092000381 20070920 00381 WP 2007 9 20 ABXA070291 1 20070811 A 5330 99234345 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 LEFT SIDE KIDNEY PANEL OPENING, SKIN APPEARED BULGED AND RIVETS CUPPED AT FORWARD LOWER CORNER. REPAIRED AREA IAW DC9 S RM 53-04. 2 L 7 2 4F A6WE 2007092000387 20070920 00387 EU 2007 9 20 TRAX200701339 1 20070910 A 5720 ANGLE AEROSP ATR72 ATR72 EU RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 RIGHT WING BOX AREA, ANGLE CRACKED AT FR 25 (FABRICATION REQ'D). 2 H 7 2 4T RT 2007092000390 20070920 00390 NM 2007 9 20 SWAA074543 1 20070911 A 5315 6546546 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 713, BL 0. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007092000391 20070920 00391 NM 2007 9 20 SWAA074525 1 20070911 A 5311 6546557 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092100007 20070921 00007 NM 2007 9 21 AALA20071695 1 20070906 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 192AN 32386 BOS - EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RIG HT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092100009 20070921 00009 NE 2007 9 21 AALA20071686 2 20070904 A 7310 PRESSURE SWITCH BOEING 737 737823 13844BZ NM GE CFM56 CFM567B24 NE RT ENGINE INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 977AN 29550 888785 DFW INFLIGHT T2484/04SEP - NUMBER TWO ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED THE FUEL FILTER DIFFERENTIAL PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007092100011 20070921 00011 WP 2007 9 21 AALA20071693 1 20070905 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 248AA 49259 LGA - EMERGENCY LIGHT ON ANNUNCIATOR PANEL INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT ON ANNUNCIATOR PANEL. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007092100019 20070921 00019 EU 2007 9 21 07FDEA03882 1 20070918 A 5310 A53973100200 BEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 HEAVY CORROSION ON BEAM 10 BETWEEN FRAME 67-69, STRG 45-47 RT, BULK CARGO COMPARTMENT DOOR. REPLACEMENT OF BEAM IAW S RM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100020 20070921 00020 NM 2007 9 21 07FDEA03883 1 20070918 A 5713 ARB29324 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 RIGHT WING LEADING EDGE CAVITY STRINGER AT XOS 667 FOUND CRACKED. 10-04-07 STRINGER REPAIRED AS PER FEDEX E.A. 1-5710- 113193. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007092100025 20070921 00025 NM 2007 9 21 07FDEA03888 1 20070918 A 5320 STRUT DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 RIGHT MAIN LANDING GEAR WHEEL WELL FOUND STRUT ATTACHING FLIPPER DOOR CRACKED. 10-04-07 CARRIED OUT REPAIR AS PER SR M 52-10-00 FIGURE 18 VOLUME I. OPERATIONS CHECK OF RIGHT HAND MAIN LANDING GEAR FLIPPER DOOR CARRIED OUT AS PER AMM 32-3 1-00-700-803 FOUND 'SATIS'. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007092100027 20070921 00027 NM 2007 9 21 07FDEA03794 1 20070914 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 588FE 48490 FASTENER HOLE FOUND CRACK AT 9 AND 3 O'CLOCK POSITION ON LONGERON AT RIGHT SIDE NOSE LANDING GEAR TRUNNION. 09-28-07 REPAIR CARRIED OUT AT FASTENER HOLE, 9 AND 3 O'CLOCK POSITION ON LONGERON AT RT NLG TRUNNION AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007092100031 20070921 00031 NM 2007 9 21 07FDEA03800 1 20070916 A 2170 COALESCER BAG BOEING 727 727227 1384078 NM CABIN AIR DIRTY A FDEA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 25 483FE 21465 ON DESCENT PASSING THROUGH 17,000 FT, STRONG ODOR SIMILAR TO ELECTRICAL SMOKE DETECTED IN COCKPIT. ODOR SUBSIDED BUT R ETURNED ON SHORT FINAL. INSPECTION OF A/C IN PROGRESS. INSPECTED A/C'S CB'S NONE WERE FOUND POPPED. NO LINGERING ODOR OF SMOKE ANYWHERE ON A/C WHEN IT ARRIVED AT THE GATE. INSPECTED E/E AND RADAR R/T COMPT, NO DEFECTS NOTED. RAN BOTH R T AND LT PACKS WITH ENG'S AND APU. SLIGHT ODOR USING RT PACK. FOUND COALESCER BAGS DIRTY. REMOVED AND REPLACED BOTH L T AND RT PER MM 21-55-051. A/C OK FOR SERVICE. 2 L 7 3 4F A3WE 2007092100035 20070921 00035 EU 2007 9 21 07FDEA03804 1 20070917 A 5320 A53988424206 STRUT AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 CORRODED CROSS STRUTS FWD OF FRAME 84 LT, STRG 15. REPLACEMENT OF CROSS STRUT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100038 20070921 00038 EU 2007 9 21 07FDEA03807 1 20070917 A 5320 A53986743210 WEB AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 DAMAGED WEB PLATES BETWEEN FRAME 86-87, STRG 36 RT. REPLACMENT OF WEB PLATE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100044 20070921 00044 EU 2007 9 21 07FDEA03813 1 20070917 A 5320 A53778329208 PLATE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 CORRODED SHEAR PLATE AT FWD CARGO COMPARTMENT BETWEEN FRAME 22-23, STRG 43-44 LT. REPLACEMENT OF SHEAR PLATE IAW SRM 51 -72-10. 2 L 7 2 4F RT A35EU 2007092100052 20070921 00052 WP 2007 9 21 07FDEA03822 1 20070917 A 5730 ARB1067 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 600 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 RT WING L/E SKIN EXISTING DOUBLER. REPLACED DOUBLER IAW SRM 51-30-00 VOL II. 2 L 7 3 4F A22WE 2007092100054 20070921 00054 EU 2007 9 21 07FDEA03824 1 20070917 A 5320 A53974341200 PROFILE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 HEAVY CORROSION ON LONGITUDINAL PROFILE AT BULK CARGO COMP FLOOR STRUCTURE BETWEEN FRAME 63-64, Y-805, RT. REPLACEMENT OF LONGITUDINAL PROFILE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100058 20070921 00058 NE 2007 9 21 AALA20071642 2 20070829 A 7230 BLADES DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RT ENGINE DAMAGED A AALA A UNSCHED LANDING C B F.O.D. SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 236AA 49251 717884 SJC INFLIGHT T2426/29AUG - BIRD STRIKE ON NUMBER TWO ENGINE DURING CLIMB. CREW REPORTED ODOR AFTER BIRD STRIKE. RETURN ED TO SJC AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE. FOUND TWO FAN BLADES WITH MINOR DAMAGE. BLENDE D BLADES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007092100059 20070921 00059 NM 2007 9 21 AALA20071644 1 20070829 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 603AA 27054 MIA - EMERGENCY LIGHT AT SEAT 2E INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 2E. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092100060 20070921 00060 NM 2007 9 21 AALA20071645 1 20070829 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 603AA 27054 MIA - EMERGENCY LIGHT AT SEAT 19D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 19D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092100061 20070921 00061 NM 2007 9 21 AALA20071651 1 20070830 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 387AM 27184 DFW - EXTERIOR EMERGENCY LIGHT AT LEFT WING AFT OF TRAILING EDGE INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGH T AT LEFT WING AFT OF TRAINING EDGE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007092100062 20070921 00062 2007 9 21 AALA20071649 4 20070830 A 2320 4630404 PRINTER BOEING 757 757223 1384957 NM COCKPIT SMOKE A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 623AA 24581 ORD INFLIGHT T844/30AUG - ACARS PRINTER STARTED SMOKING. PULLED PRINTER CIRCUIT BREAKERS ON OVERHEAD PANEL. OPENED PRI NTER AND PAPER ROLL NOT BURNED. LANDED ORD WITHOUT INCIDENT. REPLACED ACARS PRINTER AND INSPECTED AREA. NO DAMAGE. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092100063 20070921 00063 NM 2007 9 21 AALA20071650 1 20070830 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 387AM 27184 DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007092100064 20070921 00064 WP 2007 9 21 AALA20071661 1 20070831 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 461AA 49566 LGA - EMERGENCY LIGHTS AT SEAT ROW 25DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROW 25DEF. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007092100069 20070921 00069 EU 2007 9 21 07FDEA03776 1 20070914 A 5230 A52175004 SKIN AIRBUS 310 A310324 3930206 EU ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 804FD 549 FOUND OLD REPAIR DOUBLER ON AFT PAX DOOR RT OUTER SKIN LOWER EDGE, NOT CONFORM TO SRM 52-10-00/FIG 204. REPAIR RENEWE D AS PER SRM 52-10-00/FIG 204. 2 L 7 2 4F RT A35EU 2007092100076 20070921 00076 EU 2007 9 21 07FDEA03783 1 20070914 A 5510 7075T6 STRAP AIRBUS 310 A310222 3930315 EU HORIZONTAL STAB MISINSTALLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 446FE 224 LEFT HORIZ STAB ON UPPER REAR SPAR BETWEEN RIBS 5 AND 8 REPAIR STRAP REQUIRES REMOVAL FOR MATERIAL TYPE VERIFICATION REM OVED DOUBLER STRAP DUE INCORRECT MATL IN REF A310 SRM 55-11-21 PG 202. REPLACED STRAP DOUBLER IAW A310 SRM 55-11-21 FI G 214. 2 L 7 2 4F RT A35EU 2007092100079 20070921 00079 EU 2007 9 21 07FDEA03786 1 20070914 A 5311 A53870037201 FRAME AIRBUS 310 A310222 3930315 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 446FE 224 FRAME CRACKED IN FASTENER HOLE AT FRAME 42A LOWER HOLE COMMON TO CRICIFORM FITTING SEE JOB CARD 41 BY 5271ALI. RT SIDE FROM CABIN SIDE THE FIRST LAYER RUNNING IN THE 6 O`CLOCK AND 9 O`CLOCK DIRECTIONS APPROX .100 DEEP TO THE 2ND LAYER 100 PERCENT + AMPLITUDE ON SCREEN REMOVED AND REPLACED FRAME FITTING P/N A538-70037-201 IAW A310 SRM 51-40-2. 2 L 7 2 4F RT A35EU 2007092100083 20070921 00083 EU 2007 9 21 07FDEA03790 1 20070914 A 5311 A53970003200 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOR REPLACEMENT OF STRINGER 50 LT AND RT FROM THE COUPLING FWD OF FRAME 55 (NON ROUTINE DR106) IT IS NECESSARY TO CUT FR AME 54.2 BETWEEN STRG 50-51, LT AND RT FRAME SPLICE REPAIR PERFORMED ON BOTH SIDES LT AND RT AS PER A300-600 FREIGHTER S RM 53-10-13/ FIG 203, WITH 1-2 MM GAP AFTER STRINGER INSTALLATION, APPROVED BY EA 6-5316-81081 AND RAS/DAHAM/4018801/200 4 ISSUE A. 2 L 7 2 4F RT A35EU 2007092100088 20070921 00088 EU 2007 9 21 07FDEA03857 1 20070917 A 5320 A53974225212 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 HEAVY CORROSION ON CLIP AT FRAME 69, BETWEEN STRG 56-57 LT. REPLACEMENT OF CLIP IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100097 20070921 00097 EU 2007 9 21 07FDEA03866 1 20070917 A 5313 A53974203 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 HEAVY CORROSION ON STRINGER 54 BETWEEN FRAME 65-58 LT. STRINGER SPLICE REPAIRS PERFORMED IAW SRM 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007092100105 20070921 00105 EU 2007 9 21 07FDEA03687 1 20070913 A 5320 A53973054200 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 CRACKED CORNER FITTING AT AFT CARGO DOOR CUT OUT (SILLBEAM) BETWEEN FRAME 63-63A. REPLACEMENT OF CORNER FITTING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100108 20070921 00108 WP 2007 9 21 AALA20071667 1 20070901 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 409AA 49320 LGA - EMERGENCY LIGHT AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007092400001 20070924 00001 CE 2007 9 24 DXTA200702372 1 20070801 A 3260 UPLOCK SWITCH CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE NLG OUT OF ADJUST E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 808QS 5600619 UPON GEAR RETRACTION THE 3 GREEN LIGHTS WENT OUT, THE HYDRAULIC PUMP LIGHT WENT OUT, AND THE RED GEAR UNLOCK LIGHT REMAI NED ON. JACKED A/C, PERFORMED LANDING GEAR HYD SYSTEM ADJ TEST. SWUNG GEAR 10 TIMES, NO DISCREPANCY'S. INSPECTED GEAR UPLOCK SWITCHES FOR PROPER ADJUSTMENT. ADJUSTED NOSE GEAR UPLOCK SWITCH, SWUNG GEAR 10 MORE TIMES, OPS CHECKED GOOD. RE SET AND SERVICED ONGOING GEAR BLOW DOWN BOTTLE. REF MM 32-01-00, 32-31-05/32-30-00. 2 L 7 2 4F 4 F RT A22CE E00053EN 2007092400003 20070924 00003 CE 2007 9 24 DXTA200702429 1 20070824 A 3250 66426438 BUNGEE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE NLG STEERING INOPERATIVE E DXTA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 07 616QS 4274 5605345 ON TAKEOFF ROLL A/C EXPERIENCED EXTREME LT YAW. APPLIED FULL RT RUDDER WITH NO RESULT. T/O ABORTED. RUDDER BIAS TEST W AS SATISFACTORY. AIRSPEED WAS UNDER 20 KNOTS. REMOVED AND REPLACED STEERING BUNGEE CHECKED ADJUSTMENT/TEST IAW MM 32-50 -00. TAXI A/C IAW MM 9-30-00, NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007092500013 20070925 00013 NM 2007 9 25 UPS07550632 1 20070910 A 5610 WINDOW BOEING 757 75724APF 1384969 NM L2 CRACKED A IPXA K NONE O OTHER NR NOT REPORTED 1 SO 01 460UP 25481 INSPECTION TYPE:N/A L2 WINDOW HAS DELAMINATION IN LOWER FORWARD CORNER. MULTIPLE SMALL CRACK LINES VISIBLE IN AREA OF D ELAMINATION. REMOVED AND REPLACED L2 WINDOW PER MM 56-11-024 AND 56-11-00-6. 2 L 7 2 4F RT A2NM 2007092500037 20070925 00037 NE 2007 9 25 AALA20071748 2 20070915 A 7200 SHAFT BOEING 757 757223 1384957 NM RROYCE RB211 RB211535* NE LT ENGINE DAMAGED A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 609AA 27447 31181 IAH INFLIGHT T931/15SEP LAX TO MIA - NUMBER ONE ENGINE OIL LOSS. CREW PERFORMED IN FLIGHT SHUT DOWN OF NUMBER ONE ENGIN E. SINGLE ENGINE TIME 18 MINUTES. LANDED IAH WITHOUT INCIDENT. FOUND NUMBER ONE ENGINE TOWER SHAFT AND HOUSING DAMAGE D. REPLACED NUMBER ONE ENGINE ON 16 SEP 2007 AT IAH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2007092500063 20070925 00063 NM 2007 9 25 USAA920070824 1 20070910 A 5754 65C267751 ATTACH FITTING BOEING 737 7374B7 1384702 NM KRUEGER FLAP CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 459UW 25023 CLT - MAJOR REPAIR - NR 6007656, CRACKED LEFT WING NR 2 KRUEGER FLAP ATTACH FITTING, LEADING EDGE STATION 106.5 - LEADIN G EDGE STATION 118.47. REPLACED LEFT WING NR 2 KRUEGER FLAP ATTACH FITTING, LEADING EDGE STATION 106.5 - LEADING EDGE S TATION 118.47 IAW USAIRWAYS EA 98873A. 2 L 7 2 4F RT A16WE 2007092500069 20070925 00069 SO 2007 9 25 S8A2007F00000 1 20070726 A 5610 1159CE2003437 WINDOW GULSTM G1159 G1159A 3970109 SO RROYCE SPEY SPEY511* 54523 EU COCKPIT CRACKED E S8AA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 39 457JC 457 AC DEPARTED AT APPROX 1930 ON 7/26/2007 AT APPROX 150 MILES OUT AND FL 350 A LOUD POP WAS HEARD IN THE CABIN. FLIGHT CR EW INVESTIGATED AND NOTED THE NR 3 RT CABIN WINDOW OUTER PANE CRACKED. AT THAT TIME FLIGHT CREW DECLARED AN EMERGENCY, RETURNED AND MADE AN UNEVENTFUL LANDING. INSPECTION OF WINDOW BY MFG FIELD TECH REP DETERMINED THAT WINDOW WAS SCRATCHE D FROM THE OUTSIDE AND INDUCED A WEAK AREA IN THE OUTER PANE OF THE WINDOW FURTHER INSP OF ALL CABIN WINDOWS INSTALLED ON AIRCRAFT FOUND 2 OTHER WINDOWS, NR 4 RT AND NR 5 LT HAD SCRATCHES OUT OF LIMIT AND WERE REPLACED. AT THIS TIME UNABL E TO DETERMINE WHAT CAUSED SCRATCHES IN WINDOWS. SERVICEABLE WINDOWS INSTALLED IN AC, INSPECTED AND AIRCRAFT RETURNED T 2 L 7 2 4F 4 F A12EA E2EU 2007092500071 20070925 00071 CE 2007 9 25 DXTA200702452 1 20070609 A 2750 FLAP SYSTEM CESSNA 750 750 2076810 CE TE FLAPS MALFUNCTIONED E DXTA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 07 903QS 7500162 AMBER CAS (FLAPS FAIL) IN FLIGHT SLAT EXTENDED AND FLAPS FAILED APPROX 15 DEGREES WITH FLAPS SELECTED TO 35 DEGREES. T ROUBLESHOT DISCREPANCY TO INTERNAL FAILURE OF THE FLAP SOFT START MODULE. REMOVED MODULE AND INSTALLED REPAIRED SOFT STA RT MODULE. OPERATIONAL CHECK GOOD. WORK PERFORMED I.A.W CHATPER 27-50-00 OF THE CITATION 750 M.M 2 L 7 2 4J RT T00007WI 2007092500094 20070925 00094 SW 2007 9 25 HEER117188 1 20070520 A 5313 407030014101S LONGERON BELL 407 407 1182206 SW ALLSN AE3007 AE3007C GL FUSELAGE CRACKED B HEER O OTHER O OTHER NR NOT REPORTED 1 SW 03 415PH 5911 53390 LT LOWER LONGERON IS CRACKED AT TAILBOOM ATTACH FITTING. REMOVED LONGERON AND REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U 4 F O H2SW TE6CH 2007092500113 20070925 00113 EU 2007 9 25 TRAX200701296 1 20070827 A 5711 SPAR AEROSP ATR72 ATR72 EU WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 SDI - CRACK DET-4 LOWER SPAR FASTENERS BETWEEN RIB 13 & 14. COMPLIED WITH UNDER EXELTECH W/O YUL000780 NON-ROUTINE 312. REFER TO THIS NON-ROUTINE FOR MTC ACTION. SUPPLEMENTAL - SDR CLOSED 09/13/07. 2 H 7 2 4T RT 2007092500115 20070925 00115 EU 2007 9 25 TRAX200701331 1 20070904 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 CORROSION FOUND ON RIGHT SEAT TRACK BETWEEN FR 39-40 OUT OF LIMIT, NEED TO FABRICATE NEW SEAT TRACK. 2 H 7 2 4T RT 2007092500116 20070925 00116 EU 2007 9 25 TRAX200701332 1 20070904 A 5720 ANGLE AEROSP ATR72 ATR72 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 WING BOX AREA ANGLE CRACKED AT FR 25 LEFT SIDE. 2 H 7 2 4T RT 2007092500117 20070925 00117 SW 2007 9 25 YTRR117247 1 20070908 A 6410 BALANCE WEIGHT BELL 407 407 1182206 SW ALLSN 250C 250C47B GL T/R BLADE MISSING B YTRR O OTHER E VIBRATION/BUFFET CR CRUISE 1 SW 03 167RL 3974 53167 IN CRUISE FLIGHT THE PILOT EXPERINCED A SEVERE VIBRATION IN THE TAIL ROTOR. UPON RETURN TO BASE, IT WAS DISCOVERED THAT THE TAIL ROTOR BLADE HAD A TIP WEIGHT MISSING. THE TAIL ROTOR BLADE HAD BEEN REPAIRED IN JUNE 2007 AND HAD ACCUMULATED APPROXIMATELY 205.8 HRS SINCE REPAIR. 1 G 7 1 3U 3 U O H2SW E1GL 2007092500118 20070925 00118 EA 2007 9 25 TRAX200701333 1 20070907 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 875AS 7559 AAR - CRACKS ON FLOOR SILL AT FS 589 AND 605 UNDER FLOORBOARD 281 LLF IN CARGO BAY. 2 L 7 2 4F RT A21EA 2007092500120 20070925 00120 CE 2007 9 25 DXTA200702480 1 20070915 A 3210 LANDING GEAR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 960QS 7500160 UNABLE TO RETRACT LANDING GEAR INITIALLY ON TAKE-OFF FROM HPN. GEAR FINALLY RETRACTED AND FLIGHT CONTINUED UNEVENTLY. GE AR EXTENDED NORMALLY. 09-28-07 JACKED AIRCRAFT & PERFORMED GEAR SWING. UNABLE TO DUPLICATE SQUAWK INSPECTED NLG & M LG IAW 750 MM CHP. 32-10-00 & 32-20-00. OPS CHECK OK AT THIS TIME, NO DISCREPANCIES NOTED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007092500121 20070925 00121 CE 2007 9 25 DXTA200702477 1 20070915 A 2120 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CABIN FUMES E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 998QS 7500198 ENVIRONMENTAL FUMES IN AIRCRAFT, WORSE WHEN APU BLEED AIR IS ON. APU OIL LEVEL LOW AGAIN AFTER SERVICE (4) DAYS AGO. REMOVED AND REPLACED WITH REPAIRED APU DUE TO LEAKING OIL. OPS CHECKED GOOD. LEAK CHECKED GOOD. WORK DONE IAW 750 MM CHA PTER 49-10-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007092500122 20070925 00122 CE 2007 9 25 DXTA200702479 1 20070915 A 3234 HANDLE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 GL 07 154QS RK509 RT MLG LIGHT OUT & RED GEAR HANDLE ILLUMINATED DURING APPROACH. STAYS ON WHILE ON GROUND. CHECKED RT MLG UPLOCK SWITCH, RT MLG DOWNLOCK SWITCH & RT MLG DOOR CLOSE SWITCH, NO DISCREPANCIES NOTED. VISUALLY NOTED RT MLG NOT LOCKED. JACKED R T WING. PUSHED LOCK IN PLACE & FOUND IT TO BE STIFF. DISCONNECTED RT MLG UNLOCK ACTUATOR & FOUND LOCK MECHANISM BINDIN G. REMOVED RT DOWNLOCK SWITCH FROM BRACKET. REMOVED SWITCH BRACKET & FOUND PAINT IN HOLE LOCK PIVOT PIN PASSES THRU. REMOVED PAINT & REINSTALLED ACT. VERIFIED EMERGENCY MLG DOWN HANDLE & EMERGENCY MLG DOOR UP HANDLES PUSHED IN. RESAFT IED HANDLES. SERVICED EMERGENCY PNEUMATIC GEAR BLOW BOTTLE. JACKED ACFT & CYCLED MLG 15 TIMES, NO DISCREPANCIES NOTED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007092500124 20070925 00124 CE 2007 9 25 DXTA200702478 1 20070915 A 3243 MASTER CYLINDER CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE BRAKE ASSY FAILED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 671QS 5605071 PILOTS SIDE RT PEDAL WENT TO THE FLOOR ON LANDING. REMOVED AND INSTALLED OVERHAULED MASTER CYCLINDER ON PILOTS SIDE. R T PEDAL. ALL WORK DONE IAW CESSNA 560 M/M 32-42-02. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007092500125 20070925 00125 NM 2007 9 25 DXTA200702475 1 20070914 A 2120 UNKNOWN AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE COCKPIT ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 280QS 181 BURNING RUBBER ODOR ENTERS COCKPIT DURING CLIMB 17000 TO 19000 FT AND LASTS FOR 30-40 SECONDS THEN DISAPPEARS. NO SMOKE VISIBLE, SEEMS TO ORIGINATE FROM LT SIDE OF COCKPIT IN THE AUDIO PANEL AREA. 09-28-07 VISUALLY INSPECTED DV WINDOW E LECTRICAL CONTACTS, COCKPIT TEMP SENSOR, LT SIDE CONSOLE FOR WATER INTRUSION. NO DEFECTS NOTED. ALSO INSPECTED BEHIND LT & RT COCKPIT SIDE CONSOLES BEHIND PEDESTAL CONSOLE, BEHIND LT & RT INSTRUMENT PANELS. NO DEFECTS NOTED. POWERED ALL AV IONICS FOR 3 HOURS, NO EVIDENCE OF BURNING ODOR. MX PERF IAW FA-2000 MM CHP 31-00-00. 2 K 7 2 4F 4 F RT A50NM E44NE 2007092500126 20070925 00126 EA 2007 9 25 TRAX200701335 1 20070909 A 2530 COFFEEMAKER CNDAIR CL600 CL6002B19 1900309 EA GALLEY MALFUNCTIONED A ASOA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 978EV 7723 IN FLIGHT, F/A REPORTING A BURNED ODOR SMELL COMING FROM COFFEEMAKER AND ADJACENT WALL IS VERY HOT. PULLED GALLEY COFFE EMAKER C/B AND ODOR AND HEAT WENT AWAY. 2 L 7 2 4F RT A21EA 2007092500128 20070925 00128 CE 2007 9 25 DXTA200702476 1 20070914 A 4900 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL APU MALFUNCTIONED E DXTA O OTHER R Y PARTIAL RPM/PWR LOSS ENGINE STOPPAGE TX TAXI/GRND HDL 1 GL 07 908QS 7500108 THE APU WAS RUNNING NORMAL WHEN IT SHUTDOWN BY ITSELF FOR NO REASON. TRIED TO RESTART THE APU BUT IT WOULD NOT GO PAST 2 3 PERCENT. DID A COMPLETE RESET OF THE AIRPLANE AND SYSTEMS. TRIED TO START THE APU AGAIN AND WOULD NOT PASS 23 PERCENT. THE APU WILL NOT START. 09-28-07 CHECKED THE INTAKE AND EXHAUST CONNECTORS ON APU, AND APU OIL LEVEL. ALL FOUND NOR MAL. PERFORMED HONEYWELL ECU BIT DISPLAY FOUND NO FAULTS. MADE 2 STARTS WITH ELECTRIC AND PNEUMATIC LOADS. SYSTEM RUNS N ORMAL- IAW WITH HONEYWELL M/M 49-20-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007092500129 20070925 00129 NM 2007 9 25 USAA920070827 1 20070910 A 5230 6546921225 SKIN BOEING 737 7374B7 1384702 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 455UW 24997 CLT - MAJOR REPAIR - C6 CHECK, FORWARD CARGO DOOR EXTERIOR SKIN CRACKED AT DOOR HANDLE OPENING, BS 442.55 - BS 489.90. REPAIRED FORWARD CARGO DOOR EXTERIOR SKIN AT DOOR HANDLE OPENING, BS 442.55 - BS 489.90 IAW USAIRWAYS EA 98877. 2 L 7 2 4F RT A16WE 2007092500133 20070925 00133 SW 2007 9 25 475332837 1 20070814 A 5302 STRUCTURE BELL 222 222U 1182140 SW LYC LTS101 LTS101650C2 41560 NE TAILBOOM CRACKED E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 222HX 47533 TAILBOOM HAS CRACK APPROXIMATELY 1.26 INCHES LONG, 8 INCHES FORWARD OF THE VERTICAL STABILIZER. BOOM STATION 229.2 WL 82.19 1 G 7 2 3U 3 U H9SW E5NE 2007092500134 20070925 00134 SO 2007 9 25 C2XA07RI076 1 20070910 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13964 145123 RIC - DURING ROUTINE MAINTENANCE, MX FOUND NR 3 EMERGENCY FLOOR PROXIMITY LIGHT STRIP HAD THE CONNECTOR BROKEN. MX REMO VED AND REPLACED CONNECTOR PIN IAW EMB 145 AMM 20-13-12 AND WM 33-50-50. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007092500135 20070925 00135 NE 2007 9 25 DXTA200702486 2 20070919 A 7200 ENGINE CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE RIGHT FAILED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 673QS 5605651 (RT LO OIL PRESS) LIGHT CAME ON DURING T/O, WHICH WAS ABORTED. 09-28-07 REMOVED AND REPLACED NR 2 ENGINE WITH SERVI CEABLE UNIT USING NEW SEALS. ALL ACCESSORIES AND WIRE HARNESS SWAPPED TO INSTALLED ENGINE WORK PERFORMED PER CESSNA 560X L M/M 71-00-03 AND PRATT& WHITNEY 545B M/M 71-00-00. OPS AND LEAK CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007092500138 20070925 00138 CE 2007 9 25 DXTA200702467 1 20070911 A 5610 WINDSHIELD CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE COCKPIT FAILED E DXTA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 681QS 5605181 PIC SIDE WINDSHIELD SHATTERED AT FL430. REMOVED AND INSTALLED A NEW WINDSHIELD IN THE PILOTS POSITION. INSTALLED WITH NEW HARDWARE- TORQUED PER M/M. INSTALLED WITH NEW STICK N STRIP SEAL. PRESSURIZED AIRCRAFT. LEAK RATE WITHIN LIMITS. RA N A/C TO OPS CHECK PILOT'S HEATED WINDSHIELD- OPS CHECKED GOOD- PERFORMED IAW CE560XL M/M CH 56-11-00/30-41-00/71-00-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007092500141 20070925 00141 CE 2007 9 25 GLBA20060999 1 20070911 A 5330 12943004521 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FUSELAGE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 251GL UE251 ROW 6A, CABIN WINDOW INNER SKIN CRACKED AT THE LOWER FORWARD CORNER. MAINTENANCE REMOVED AND REPLACED SKIN ON EMERGENCY EXIT WINDOW 6A IAW. SRM 51-40. P/N NR 129-430045-21. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007092500143 20070925 00143 NM 2007 9 25 AMTA200700403 1 20070827 A 5321 FLOOR PANEL BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE FUSLEAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 CORROSION ON LT AFT PIT CATWALK STA 1310-1400, AROUND SCREW HOLES LBL 20. FOUND PANEL TO BE OUT OF LIMITS IAW 53-00-53. REMOVED AND REPLACED IAW SRM 51-40-02 TREATED AND PRIMED AND TOP COAT SRM 51-21-10-1 FROM FS 1200 TO 1640. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007092500148 20070925 00148 CE 2007 9 25 DXTA200702485 1 20070918 A 3222 STRUT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG DISCHARGED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 950QS 7500050 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. 09-28-07 FOUND NOSE STRUT FLAT AND WOULD NOT EXTEND TO MAKE SQUAT SWIT CH. REPACKED NOSE STRUT AND SERVICED. CYCLED GEAR. OPS CHECK GOOD IAW C750 MM 32-20-02. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007092500149 20070925 00149 CE 2007 9 25 DXTA200702450 1 20070906 A 3150 WARNING MESSAGE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 929QS 7500129 DURING TO ROLL (FGC A FAIL), (MACH TRIM OFF), AND (PRI STAB TRIM FAIL) CAS MESSAGES ILLUMINATED. 09-27-07 T/S AND RE MOVED AND REPLACED NR 1 IAC AND LOADED SN, AC DATABASE, CUSTOM DATABASE AND ALL OPS CHECKS WERE GOOD IAW CESSNA 750 M/M 34-25-01 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007092500150 20070925 00150 CE 2007 9 25 GUUA05100702 1 20070510 A 5220 1295140671 COUPLING BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE EMERGENCY EXIT DIRTY A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87557 UE246 EMERGENCY EXIT 6A INOPERATIVE, UNABLE TO OPEN. CLEANED AND LUBRICATED COUPLING ATTACHED TO EXTERIOR HANDLE. 2 L 7 2 4T 4 T RT A24CE E26NE 2007092500152 20070925 00152 CE 2007 9 25 DXTA200702449 1 20070905 A 3240 BRAKE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RIGHT NOISY E DXTA O OTHER E VIBRATION/BUFFET LD LANDING 1 GL 07 908QS 7500108 AFTER LANDING THE RT BRAKE MADE A LOUD GRINDING NOISE. WE REQUIRED 50 PERCENT N1 TO TAXI THE AIRCRAFT. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007092500154 20070925 00154 CE 2007 9 25 DXTA200702495 1 20070923 A 3150 WARNING LIGHT CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE CABIN PRESSURE ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 844QS 5600629 EMER PRESS CAME ON DURING TAKEOFF AND WAS WITHOUT AN ANNUNCIATOR. COULD HEAR THE "RUSHING AIR" SOUND WHEN THE THROTTLES WERE POWERED UP. RAN A/C FOR 30 MINUTES AT VARIOUS POWER SETTINGS WITH PRESSURIZATION SELECTED NORMAL - SELECTED EMERG ENCY SEVERAL TIMES. ALL SYSTEMS WORKED PROPERLY - NO DEFECTS NOTED. ALL WORK I/A/W CESSNA 560 M.M. 2 L 7 2 4F 4 F RT A22CE E00053EN 2007092500155 20070925 00155 NM 2007 9 25 SB07077 1 20070912 A 7797 TC17401 HARNESS BOEING 737 7374B7 1384702 NM NR 2 ENGINE FAULTY A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 442US 24841 PHL - FLT 1157 ON CLIMBOUT FROM PHL, EN ROUTE TO RSW, THE NR 2 ENGINE EXPERIENCED AN OVERTEMP WITH EGT INDICATING 1083 DEGREES C. ALL OTHER ENGINE PARAMETERS WERE NORMAL. CREW DECLARED AN EMERGENCY, PULLED THE NR 2 ENGINE BACK TO IDLE AN D RETURNED TO FIELD AT PHL. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. MAINTENANCE ACCOMPLISHED BO ROSCOPE INSPECTION OF HPT AND LPT BLADES PER MM. NO DAMAGE FOUND. INSPECTED RECEPTACLES D3304 AND D1208 AND TORQUED TO 60 IN/LBS. NO DEFECTS NOTED. REMOVED AND REPLACED THE NR 2 ENGINE UPPER LEFT-HAND EGT HARNESS AND THE NR 2 ENGINE EGT INDICATOR, AS PRECAUTIONARY. ACCOMPLISHED POWER ASSURANCE CHECK, TEST NR 5, AND ACCEL/DECEL TEST. ALL CHECKS GOOD. 2 L 7 2 4F RT A16WE 2007092500157 20070925 00157 2007 9 25 SA07058 4 20070910 A 2565 62292110 SLIDE AIRBUS A321 A321211 3930370 EU R2 DOOR FAULTY A USAA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 19 169UW 22429 1317 1455 CLT - RECEIVED A RIGHT EMERGENCY EXIT SLIDE ECAM MESSAGE DOOR 2R. MAINTENANCE ACCOMPLISHED A CHECK OF THE DOOR SLIDE AR MING/DISARMING SYSTEM, AND CHECKED WIRING AND LINKAGE. NO FAULTS FOUND. REPLACED THE RIGHT SIDE, POSITION 2, EMERGENCY DOOR ESCAPE SLIDE AND BOTTLE. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2007092500158 20070925 00158 CE 2007 9 25 DXTA200702494 1 20070922 A 2750 DRIVE UNIT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS FAILED E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 919QS 7500224 FLAPS FAILED AT 5 DEGREES. REMOVED & REPLACED POWER DRIVE UNIT, OPERATIONALY CHECKS GOOD. IAW: CE750 M/M 27-50-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007092500159 20070925 00159 CE 2007 9 25 DXTA200702491 1 20070921 A 3260 SENSOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG OUT OF LIMITS E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 938QS 7500183 ON TAKEOFF, THE ACFT BEGAN TO SHIMMY AT 30 KNOTS AND BEGAN TO BECOME VIOLENT THROUGH 60 KNOTS. ABORTED T/O AT 75 KNOTS . AT 70 KNOTS THROUGH STOPPING, ACFT SHOOK VIOLENTLY. IT APPEARS TO BE A NOSE WHEEL SHIMMY. TAXI IN WAS NORMAL. 09-2 8-07 FOUND UPPER SENSOR LINK ATTACH HARDWARE BELOW TORQUE LIMITS. RETORQUED PER 750 MM CH 32-20-00. REMOVED AND REPLA CED BOTH NOSE WHEEL AND TIRE ASSYS PER 750 MM CH 32-24-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007092500160 20070925 00160 SO 2007 9 25 C2XA07CL076 1 20070912 A 2697 W101181324 WIRE EMB 145 EMB145XR 3260214 SO FIRE DETECTION CHAFED A C2XA K NONE N FALSE WARNING DE DESCENT 1 SW 27 23139 145731 CLE FLIGHT 2578 THE CREW REPORTED THE NR 1 ENGINE FIRE DETECT CAUTION MESSAGE CAME ON FOR A BRIEF MOMENT ON DESCENT. MA INTENANCE INSPECTED AND REPAIRED A CHAFED WIRE W101-1813-24 BETWEEN PO873 AND PO962. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2007092500161 20070925 00161 CE 2007 9 25 AMWA87546 1 20070919 A 2432 121013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA CORRODED A AMWA K NONE O OTHER CR CRUISE 1 CE 07 244YV UE244 AFTER ARRIVING, THE CREW CALLED MAINT CONTROL TO WRITEUP THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLT. THIS BATTER Y CHARGE ANNUNCIATOR WRITEUP IS A NUISANCE ALARM AND IS DISTRACTING TO THE FLIGHTCREW. MAINTENANCE CLEANED THE BATTERY SHUNT, OPS NORMAL. 2 L 7 2 4T 3 T RT A24CE E2NE 2007092500164 20070925 00164 SW 2007 9 25 HEER117209 1 20070706 A 5302 206032409001 FITTING BELL 206 206L4 1182110 SW ALLSN 250C 250C30P 03013 GL TAILBOOM CRACKED B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 266P 4850 52271 52271 UPPER LT TAILBOOM ATTACH FITTING CRACKED. REPLACED FITTING. 1 G 7 1 3U 3 U NC H2SW E1GL 2007092500165 20070925 00165 SO 2007 9 25 C2XA07CL077 1 20070913 A 3213 23092005005 SHOCK ABSORBER EMB 135 EMB135ER 3260203 SO RT MLG BINDING A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16502 16366 888 145166 CLE FLIGHT 2514 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED AND LANDED WI THOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT GEAR SHOCK ABSORBER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2007092500166 20070925 00166 SW 2007 9 25 HEER117233 1 20070611 A 6510 206040339103 BEARING BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL T/R DRIVE SEPARATED B HEER O OTHER O OTHER NR NOT REPORTED 1 SW 03 2249Z 5715 BT150 45753 DURING A DAILY INSPECTION TECHNICIAN FOUND BEARING CAGE SEPARATED AT THE RIVETS. ALSO FOUND SEALS OUT OF THEIR RESPECTI VE RETENTION GROOVES. REQUEST THAT SHAFT ASSY BE SENT TO MFG FOR EVALUATION TO FILAB. REPLACED SHAFT ASSY WITH NEW. 1 G 7 1 3U 3 U H2SW E1GL 2007092500177 20070925 00177 NM 2007 9 25 UPS07550651 1 20070823 A 5311 70750071C FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 432UP 25463 INSPECTION TYPE:C DENT IN AFT CARGO COMPARTMENT, FUSELAGE FRAME STA 1540, BETWEEN S25L AND S26L. REPAIR AT STA 1540, S2 5L AND S26L WERE ACCOMPLISHED IAW SRM 53-00-07 DETAIL I, FIG 201 (SHT 4 OF 15). THIS IS A CATEGORY -B- REPAIR AND REQUI RES REINSPECTION IAW SRM 53-00-07, FIG 201 (SHT 10 OF 15) TABLE II AND FIG 201, (SHT 12 OF 15) DETAIL V ZONE 1. 2 L 7 2 4F RT A2NM 2007092500179 20070925 00179 CE 2007 9 25 GLBA20060992 1 20070827 A 5310 1144300027180 ANGLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 288 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 245GL UE245 RT HEAVY ANGLE CRACKED APPROXIMATELY 1.5 INCHES AT FS 288.0. MAINTENANCE INSTALLED DOUBLER ON RT HEAVY ANGLE IAW. SRM 53-90-23. REPAIR APPROXIMATELY 13.8 INCHES IN LENGTH FROM NEW HEAVY ANGLE. 2 L 7 2 4T 4 T RT A24CE E26NE 2007092500180 20070925 00180 NM 2007 9 25 UPS07550652 1 20070823 A 5311 70750071C FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 432UP 25463 INSPECTION TYPE:C DENT IN AFT CARGO COMPARTMENT, FUSELAGE FRAME STA 1500, S25L. REPAIRED IAW SRM 53-00-07 THIS REPAIR I S A CATEGORY -B- REPAIR PER DETAIL V FIG 201 (SHT 12 OF 15) PG 212. INSPECTION REQUIREMENTS AS SHOWN IN TABLE II FIG 20 1 (SHT 10 OF 15) PG 210 REPAIR ACCOMPLISHED PER DETAIL I, FIG 201 (SHT 4 OF 15) ZONE 1, FIG 201. 2 L 7 2 4F RT A2NM 2007092500183 20070925 00183 WP 2007 9 25 UPS07850637 1 20070820 A 5320 3649114U ATTACH FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 SUBFLOOR ATTACH FITTING HEAVY CORROSION AROUND BOLT AREA AT STA 920 RBL 65. REMOVED AND REPLACED SUB FLOOR ATTACH FITTING AT STA 920 AND RBL 65 IAW SRM 51-03-02-0, SRM 51-3-0, SRM 51-1-20D, AND SRM 51-1-8. 2 L 7 4 4F RT 4A25 2007092500185 20070925 00185 2007 9 25 UPS07M50643 4 20070912 A 2565 26B175191 INDICATOR DOUG MD11 MD11F 3023600 NM EVAC SLIDE FAULTY A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 256UP 48405 INSPECTION TYPE:N/A R1 EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST INDICATING SYSTEM INOP. RELAMPED, NO HELP. ITEM DEFERRED IAW MD11 MEL 25-01-2. DMI M358567. T/S PERFORMED FOUND EVAC SLIDE PRESSURE VESSEL INDICATOR AT FAULT. REMOVE D AND REPLACED EVAC SLIDE PRESS VESSEL IND IAW AMM 25-61-04-4. OPS CHECK NOW SATISFACTORY. 2 L 7 3 4F RT A22WE 2007092500186 20070925 00186 CE 2007 9 25 GLBA20060995 1 20070911 A 5311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 177 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 251GL UE251 FUSELAGE FRAME CRACKED AT F.S. 177.3 AT STRINGER 9AR APPROXIMATELY 1.1 INCH IN LENGTH. MAINTENANCE REPAIRED FUSELAGE FRA ME CRACK AT STRINGER RELIEF HOLE AT FS 177.3 STRINGER 9R IAW SRM 51-70. REPAIR DIMENSIONS APPROX 5 INCH BY 2.5 INCH, 202 4 T-3 .080. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007092500187 20070925 00187 CE 2007 9 25 GLBA20060997 1 20070911 A 5210 DOOR FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 150 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 251GL UE251 AIRSTAIR DOOR FRAME ANGLE CRACKED AT FS 150.6.AND APPROXIMATELY 3 INCHES ABOVE STRINGER 10L. CRACK APPROXIMATELY 1.3 IN CHES. MAINTENANCE INSTALLED REPAIR INSERT AND REINFORCED ANGLE IAW SRM 53-90-28. ANGLE PART NR 129-420034-3. INSERT 2 INCHES, ANGLE 10 INCH COVER PATCH 9 INCH BY 8 INCH. 2024 T-3 .071. RII COMPLIED IAW TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007092500188 20070925 00188 CE 2007 9 25 AMWA87499 1 20070917 A 3240 1148100559 BRAKE ASSY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG WEAK A AMWA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 07 143YV UE143 AFTER LANDING, THE NIGHT CREW CALLED MAINT CONTROL TO REPORT CAPT'S BRAKES FELT SPONGY. MAINTENANCE BLED BRAKES AS NEED ED. 2 L 7 2 4T 4 T RT A24CE E26NE 2007092500191 20070925 00191 NM 2007 9 25 KCSA071373 1 20070913 A 5320 ANGLE BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA 380 ANGLE IS CRACKED .5 INCH BETWEEN STR 1R AND STR 2R. 2 L 7 4 4F RT A20WE 2007092500193 20070925 00193 CE 2007 9 25 GUUA05080703 1 20070508 A 5220 1295140841 LATCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE EMERGENCY DOOR DIRTY A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 81536 UE152 AT SCHEDULED FLEET CAMPAIGN INSPECTION: EMERGENCY DOOR AT SEAT 6A UNABLE TO OPEN FROM INSIDE AIRCRAFT. CLEANED AND LUBE D DOOR LATCH ASSEMBLY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007092500196 20070925 00196 CE 2007 9 25 GLBA20060996 1 20070911 A 5311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 163 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 251GL UE251 FUSELAGE FRAME CRACKED AT FS 163.9 AT STRINGER 9AR APPROXIMATELY 1.2 INCHES IN LENGTH. MAINTENANCE REPAIRED FUSELAGE F RAME AT STRINGER RELIEF HOLE AT FS 163.9 AT STRINGER 9R IAW SRM 51-70. REPAIR APPROXIMATELY 6.5 INCHES BY 2.5 INCHES. 20 24 T-3. .080. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007092500198 20070925 00198 CE 2007 9 25 DXTA200702469 1 20070911 A 3243 MASTER CYLINDER CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG MALFUNCTIONED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 671QS 5605071 PILOT'S SIDE (LT) LEFT FOOT BRAKE PEDAL GOES TO FLOOR. 09-27-07 REMOVED AND REPLACED PILOTS LT AND RT BRAKE PEDAL MA STER CYLINDER IAW C-560XL MAINT. MANUAL 32-42-02. OPS AND LEAK CHECKED GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007092500199 20070925 00199 EU 2007 9 25 M7K2007F00002 1 20070726 A 5302 CASTING UROCOP UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAILBOOM CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 806MH 2903 7096 3833 23072 DURING ROUTINE 500 HOUR INSPECTION IT WAS DISCOVERED THAT THE CASTING AT THE AFT MOST POSITION OF THE TAILBOOM, WHICH IS THE ATTACHMENT POINT FOR THE FENESTRON (DUCTED FAN TAIL ROTOR) HAD SEVERAL CRACKS EXCEEDING 1.5 INCHES RADIATING FROM O NE POINT AT THE 3:00 POSITION WITH TAILBOOM VIEWED FROM THE REAR. THIS CRACKING COULD ONLY BE VIEWED EASILY WITH THE HO RIZONTAL STABILIZER REMOVED. THIS WAS DETERMINED BY THE OEM TO BE A NON FIELD REPAIRABLE DEFECT AND SERVICEABLE TAILBOO M ASSEMBLY HAS BEEN ORDERED AND WE WILL REPLACE THE DEFECTIVE TAILBOOM WHEN IT ARRIVES IAW THE MANUFACTURERS INSTRUCTION S AND TECHNICAL REPRESENTATIVE’S SUPERVISION. IT DID NOT APPEAR THAT A CATASTROPHIC FAILURE WAS IMMINENT. (K) 1 G 7 2 3U 3 U H9EU E00054EN 2007092500203 20070925 00203 NE 2007 9 25 HEEA117030 1 20070808 A 6320 SB3317201 BEARING SKRSKY S76 S76A 8143006 NE TMECA ARRIEL ARRIEL2S2 60036 NE M/R GEARBOX FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 764P 2507 A08100335 760276 MGB CHIP PLUGS INDICATED A METAL IN OIL CONDITION. THE MGB WAS REMOVED AND SENT TO COMPONENT OVERHAUL SHOP TO DETERMINE CAUSE OF METAL. OHS COMPLETELY DISASSEMBLED THE MGB AND DETERMINED THE BEARING CUP IN THE LEFT HAND BEVEL SPUR GEAR AS SY WAS THE PRIMARY CAUSE OF METAL. THE BEARING CONE SB3317-101 WAS ALSO SCRAPPED DUE ROLLOVER DAMAGE CAUSED BY THE BEA RING CUP FAILURE. THE LT INPUT PINION 76351-09132-102 AND BEVEL GEAR 76351-09011-106 WERE SCRAPPED DUE TO UNUSUAL PATTE RN ON THE TEETH. 1 G 7 2 3U 4 U H1NE E00054EN 2007092500204 20070925 00204 CE 2007 9 25 S2YA07007 1 20070908 A 5320 114430002180 ANGLE BEECH 1900 1900D 1154162 CE FUSELAGE CRACKED A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 91SK 14599 UE91 DURING STRUCTURAL INSPECTION OF THE AIRCRAFT, A CRACK WAS FOUND IN THE RIGHT HAND FUSELAGE TO WING ANGLE P/N 114-43002-1 80 AND THE DOUBLER INSTALLED IN AUGUST OF 2000. THE ANGLE HAD BEEN PREVIOUSLY REPAIRED, RECORDED AND SUBMITTED ON A 337 DATED 08/15/00. THE DAMAGE INCLUDED SEVERAL SEARED RIVETS AND AN 1 INCH CRACK IN THE DOUBLER NEAR FS 288. THE DAMAGE WAS REPAIRED BY REMOVING THE OLD DOUBLER AND ANGLE AND INSTALLING A NEW ANGLE IAW 1900 AIRLINES SERIES SRM. THE TIME BE TWEEN THE TWO MAJOR REPAIRS WAS 14599.6. 2 L 7 2 4T RT A24CE 2007092500205 20070925 00205 EA 2007 9 25 COMA0770047 1 20070910 A 5311 CC670341757 FRAME CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 669CA 7574 10176 FS 280 FRAME CORRODED BEYOND LIMITS. REPAIRED THE FS 280 FRAME IAW BOMBARDIER REO 670-53-11-047. 2 L 7 2 4F RT A21EA 2007092500206 20070925 00206 SW 2007 9 25 HEEA117034 1 20070823 A 2844 41800014 TRANSMITTER BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE FUEL PRESSURE MALFUNCTIONED E HEEA O OTHER N FALSE WARNING CR CRUISE 1 SW 03 142PH 33150 DURING CRUISE FLIGHT, NR 2 FUEL PRESSURE INDICATOR MAXED OUT AT 50 PSI INDICATED. MAINTENANCE REPLACED FUEL PRESSURE T RANSMITTER. 1 G 7 2 4U 4 U H4SW E22EA 2007092500208 20070925 00208 NM 2007 9 25 UPS07M50648 1 20070629 A 3221 TRUNNION DOUG MD11 MD11F 3023600 NM NLG CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C NLG WHEEL WELL, NLG LEFT TRUNNION FITTING FOUND CRACK WITH STOP DRILL. NLG W/W LEFT TRUNNION FITTING CRACK WITH STOP DRILL AREA TRIM OUT PER SRM 53-40-00 FIG 23 VI R40. HFEC INSPECT C/O DAC NDTSPM R13 PART06-10-01-0 1 ON TRIM OUT AREA FOUND NO CRACK EVIDENT. REPAIR DOUBLER, STRAP & FILLER FAB PER SRM 53-40-00 FIG 23 VI R40 & REPROTECTED PER SRM 51-21-01 VII R40 DOUBLER, STRAP & FILLER INSTALLED PER SRM 53-40-00 FIG 23 VI R40. 2 L 7 3 4F RT A22WE 2007092500210 20070925 00210 WP 2007 9 25 MWEA070216 1 20070911 A 5320 5930584121 SUPPORT CHANNEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 PREVIOUS REPAIR CRACKED AT LWW DOOR CUTOUT FORWARD INBOARD CORNER SUPPORT CHANNEL STATION 933. REMOVED DAMAGED PREVIOUS REPAIR, FABRICATED AND INSTALLED CHANNEL. 2 L 7 2 4F A6WE 2007092500211 20070925 00211 CE 2007 9 25 DXTA200702432 1 20070827 A 3222 PACKING CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG STRUT UNKNOWN E DXTA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 07 987QS 7500087 AFTER TAKEOFF, UPON GEAR RETRACTION, THE 3 GREEN GEAR LIGHTS EXTINGUSHED AND HAD RED UNLOCK LIGHT ILLUMINATED ,TWENTY SE CONDS LATER ,GREEN NOSE GEAR LIGHT ILLUMINATED , AIR SOUNDS DURING RETRACTION INDICATED NOSE GEAR NEVER RETRACTED. TROU BLESHOT TO NLG STRUT NOT EXTENDING FULLY. DISASSEMBLED, CLEANED, INSPECTED, AND REPACKED NOSE STRUT IAW MM 32-20-02. GEA R RETRACT AND OPERATIONAL CHECKS GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007092500214 20070925 00214 NE 2007 9 25 DXTA200702431 2 20070827 A 7261 30B627501 SIGHT GLASS ISRAEL GALAXY GALAXY 4500307 EU PWC PW306 PW306A 52165 NE LEFT ENGINE CRACKED E DXTA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 07 700QS 4020 052 LT ENG OIL PRESS LOW EICAS MSG ON CLIMB OUT. (OIL PRESS 5 PSI INDICATED ON LT ENG) COMPLIED WITH QRH AND SECURED/SHUTDOW N ENG. REMOVED LT ENGINE UPPER AND LOWER COWLS. FOUND OIL FILLER NECK SIGHT GLASS LEAKING. REMOVED OIL FILLER NECK SIGHT P/N 30B6275-01 NSN AND INSTALLED NEW OIL FILLER NECK P/N 30B6275-01 NSN. REFERENCE MM 79-20-04 AS IAW MM 05-50-00. REMO VED OIL FILTER P/N 30B6070-1 NSN AND INSPECTED FOR DEBRIS, NO DEBRIS FOUND AT THIS TIME. REINSTALLED NEW FILTER P/N 30B6 070-1 NSN. REFERENCE MM 79-20-01. 2 L 7 2 4F 4 F RT A53NM E35NE 2007092500216 20070925 00216 CE 2007 9 25 DXTA200702471 1 20070912 A 3240 BRAKE ASSY CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG MALFUNCTIONED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 990QS 7500190 MAIN GEAR ON LT SIDE APPEARS TO SENSE A LOCKED CONDITION DURING NORMAL BRAKING. BRAKES ON LT SIDE RELEASE MOMENTARILY DU RING LANDING ROLL DURING SPEEDS OF AROUND 90 KTS. 09-27-07 PERFORM POWER BRAKE AND ANTI-SKID FUNCTIONAL CHECK OPS C HECK GOOD. PERFORMED A COMPLETE BRAKE BLEED. INSPECTED ALL BRAKES FOR WEAR. WEAR CHECKS GOOD. WORK DONE IAW CHAPTER 32-4 2-00 OF THE CITATION 750 M.M. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007092500220 20070925 00220 CE 2007 9 25 DXTA200702490 1 20070920 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE RIGHT WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 398QS 5600522 CO-PILOTS RT BRAKE GOES SOFT. CAN BE PUMPED UP BUT GOES SOFT AGAIN. 09-28-07 BLED RT BRAKE. OPS CHECKS GOOD. WORK DONE IAW CITATION 560 M/M 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007092500223 20070925 00223 NE 2007 9 25 DXTA200702473 2 20070913 A 7200 ENGINE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LT NONE E DXTA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 GL 07 625QS 5605319 JUST PRIOR TO V1 CALLOUT; SEAGULL STRIKE TO OB EDGE OF LT ENGINE NACELLE LIP. ABORTED TAKEOFF. OBVIOUS SIGNS OF (DEBRIS) INSIDE AND OUTSIDE INTAKE TO ENGINE. INSPECTED AIRCRAFT FOUND BIRD DEBRIS LT ENGINE COWL. CLEANED AREA BORESCOPED LT ENGINE NO DAMAGE NOTED. NO FURTHER DAMAGE TO AIRCRAFT NOTED INSPECTED RT ENGINE NO DAMAGE NOTED IAW CESSNA 560XL M/M 5 -50-00 PAGE 2. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007092500225 20070925 00225 EA 2007 9 25 TRAX200701344 1 20070913 A 3350 STRIP CNDAIR CL600 CL6002B19 1900309 EA CABIN CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 827AS 7212 EMERGENCY LIGHT STRIP AT ROW 5 CRACKED. 2 L 7 2 4F RT A21EA 2007092500226 20070925 00226 EU 2007 9 25 TRAX200701345 1 20070913 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 THE "TWO MINUTE" LIGHTS WILL NOT EXTINGUISH. 2 H 7 2 4T RT 2007092500227 20070925 00227 CE 2007 9 25 DXTA200702474 1 20070913 A 2120 UNKNOWN CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE CABIN ODOR E DXTA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 07 663QS 5605263 IMMEDIATELY AFTER T/O ACM O'HEAT LIGHT CAME ON FOLLOWED BY LT BLEED AIR OVERHEAT. EMER PRESS LIGHT DID NOT COME ON. ST ARTED TO SMELL FUMES. RETURNED TO BASE. REMOVED & REPLACED LT BI-LEVEL FLOW VALVE IAW 560XL M/M CH 21-11-00 LEAK & OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007092500228 20070925 00228 CE 2007 9 25 GLBA20061000 1 20070917 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 290 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 169GL UE169 BELLY SKIN CRACKED AT WING SPAR FS 290.5 AT BL 29.06 CRACK LENGTH APPROXIMATELY 1.250 INCHES. MAINTENANCE REPAIRED SKIN CRACK AT LT WING SPAR AREA FS 290 AND BL 29.06 IAW SRM 53-90. REPAIR DIMENSION 7 INCH BY 5.8 INCHES. 2024 T3, .040 IN CH. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007092500231 20070925 00231 SW 2007 9 25 2007F00053 1 20070921 A 5330 3P5340A01131 PANEL AGUSTA AB139 AB139 0260110 SW FUSELAGE DELAMINATED B UGAW K NONE O OTHER IN INSP/MAINT 1 SW 03 139EH 1491 31027 AFT UPPER DECK BETWEEN STATIONS 7920MM AND 7720MM IS DEBONDED.THE AREA IS APPROXIMATELY 800MM WIDE AND 200MM LONG. WATER WAS FOUND INSIDE THE HONEYCOMB CORE. 2 G 7 2 4U R00002RD 2007092500232 20070925 00232 CE 2007 9 25 GLBA20061004 1 20070921 A 5310 ANGLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A6 52043 EA BS 288 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 210GL UE210 LT HEAVY ANGLE CRACKED AT FS STA 288.0 FORWARD END IN BEND RADIUS. 09-26-07 CRACK APPROXIMATELY 1.75" IN LENGTH. MAI NTENANCE INSTALLED REPAIR ANGLE I.A.W. BEECH SRM 53-90-23. REPAIR LENGTH 13.8 INCHES. .080 2024-0. 2 L 7 2 4T 3 T RT A24CE E4EA 2007092500235 20070925 00235 GL 2007 9 25 AC2A117358 2 20070912 A 7321 23078035 HMU BELL 430 430 1182150 SW ALLSN 250C 250C30 03013 GL ENGINE MALFUNCTIONED E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 31 430CV 49072 ENGINE STARTING HOT. 1 G 7 2 3U 3 U RT H9SW E1GL 2007092500236 20070925 00236 SO 2007 9 25 C2XA07IA201 1 20070911 A 3350 BATTERY EMB 135 EMB135LR 3260305 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14522 145383 IAH - FLIGHT 2800, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS WERE INOP ON PREFLIGHT INSPECTION. MAINTENANCE CHAR GED EMERGENCY LIGHTS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007092500237 20070925 00237 NM 2007 9 25 KCSA071372 1 20070913 A 5311 FRAME BOEING 747 7472B4B 138481B NM PWA JT9 JT9D7F 52054 NE BS 520 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 B S 520 FUSELAGE FRAME CRACKED AT STR-11L CUTOUT. 2 L 7 4 4F 4 F RT A20WE E20EA 2007092500239 20070925 00239 SO 2007 9 25 C2XA07IA202 1 20070913 A 3397 16405080 CONNECTOR EMB 145 EMB145EP 3260221 SO CABIN BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 14945 145049 IAH FLT 2302, MX WORKING MEL 33-20-001/C PLASTIC BURNT SMELL IN AIRCRAFT. MAINTENANCE REMOVED AND REPLACED CONNECTOR TO OVERHEAD LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007092500240 20070925 00240 SO 2007 9 25 N93A12092007 1 20070912 A 3250 50503 STEERING SYS GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU NLG FAILED E N93A O OTHER O OTHER TX TAXI/GRND HDL 1 SO 13 416QS 9438 1316 AFTER LANDING AIRCRAFT, STEERING MADE AN UNCOMMANDED TURN TO THE RIGHT. 2 L 7 2 4F 4 F RT A12EA E25NE 2007092500241 20070925 00241 NM 2007 9 25 CO1Y200700005 1 20070913 A 5230 ADG70323 BEAM DOUG MD11 MD11 3023602 NM FWD CARGO DOOR CORRODED B CO1Y K NONE O OTHER IN INSP/MAINT 1 EA 33 702BC 48504 FOUND CORROSION ON BEAM P/N ADG7032-3. 2 L 7 3 4F RT A22WE 2007092500242 20070925 00242 CE 2007 9 25 DXTA200702472 1 20070810 A 3240 FITTING CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE BRAKE ASSY LEAKING E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 331QS 5600331 FIRST OFFICER RT BRAKE SLOW TO DEVELOP PRESSURE. INSPECTED CO-PILOTS MASTER CYLINDERS & FOUND TOP FITTING LEAKING & LO OSE, TIGHTENED & CLEANED, BLED BRAKES SEVERAL TIMES FROM PILOTS & CO-PILOTS SEATS & ALL LEAK & OPERATIONAL CHECKS WERE G OOD IAW CESSNA 560 M/M 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007092500243 20070925 00243 CE 2007 9 25 GUUA09080701 1 20070908 A 3210 1148100231 BOLT BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67 52043 NE LT MLG BROKEN A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 190YV UE190 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT MLG UPPER ATTACH BOLT BROKEN. REPLACED LT MAIN LANDING GEAR UPPER DR AG LEG ATTACH BOLT, AIRFRAME FITTING AND DRAG BRACE ASSEMBLY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007092500244 20070925 00244 CE 2007 9 25 GUUA09110701 1 20070911 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT MLG MALFUNCTIONED A GUUA O OTHER J WARNING INDICATION CR CRUISE 1 SO 29 81546 UE187 DURING FLIGHT LANDING GEAR INTRANSIT LIGHT ILLUMINATED. REPLACED LT MLG ACTUATOR. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007092500245 20070925 00245 CE 2007 9 25 GUUA09110702 1 20070911 A 3260 MS24171D1 RELAY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG FAILED A GUUA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 29 69549 UE194 AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. REPLACED MLG RELAY, COULD NOT DUPLICATE OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007092500246 20070925 00246 SO 2007 9 25 GUUA08300701 1 20070830 A 3397 WIRE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE EMERGENCY LIGHTS LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 282AS 120226 DURING ROUTINE SCHEDULED MAINTENANCE FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE. SECURED LOOSE WIRES AND SPLICES OPERATIO NAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 2007092500248 20070925 00248 CE 2007 9 25 DXTA200702460 1 20070909 A 2435 STARTER GEN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LEFT TRIPPED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 326QS 5600526 DURING TAKEOFF POWER APPLICATION, LT GENERATOR TRIPPED OFF LINE (LOW SPEED ABORT). VISUALLY INSPECTED LH GENERATOR WIR ING. ALL CONNECTIONS TIGHT. RAN BOTH ENGINES WITH GENERATOR SELECTED ON. CYCLED RT GEN OFF AND VERIFIED LT TOOK LOAD ON AMP METER. GENERATOR SYSTEM OPS CHECK GOOD I.A.W. 560 M/M 24-31-01. 2 L 7 2 4F 4 F RT A22CE E25EA 2007092500251 20070925 00251 SO 2007 9 25 C2XA07SH070 1 20070914 A 5320 14521713005 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17524 145399 SHV - DURING C-CHECK MAINTENANCE FOUND CENTER OMEGA BEAM WITH CORROSION AT FRAME 20. MAINTENANCE REPAIRED CENTER OMEGA BEAM AT FRAME 20 IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007092500252 20070925 00252 EU 2007 9 25 07FDEA03991 1 20070919 A 5313 A53980165202 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT STRINGER P 27 LT, C 75-76 REPAIR PERFORMED IAW A300-600 FREIGHTER SRM 53-10-14 FIG 201, APPROVED BY E A 6-5310-81054 AND RAS/DATLS/0002051/2004 ISS A . 2 L 7 2 4F RT A35EU 2007092500253 20070925 00253 EU 2007 9 25 07FDEA03992 1 20070919 A 5313 A53974203 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION ON STRINGER P57 , C69-71 AND P56 RT, C 70-72 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007092500255 20070925 00255 EU 2007 9 25 07FDEA03994 1 20070919 A 5310 A53974219220 CROSSBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT CROSS BEAM C 63 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10 2 L 7 2 4F RT A35EU 2007092500256 20070925 00256 EU 2007 9 25 07FDEA03995 1 20070919 A 5730 A53750143 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 CRACK IN TRAILING EDGE OF BOTTOM SKIN PANEL NR 2, ON RT ZONE 675CB ONE HOLE WITH CRACK IN SKIN. FOR LOCATION SEE EA 6- 5710-81091/PG 4 (CRACK LENGTH IN HOLE ABOUT 3MM). DOUBLER PLATE INSTALLED, REPAIR PERFORMED IAW DRW R573-49237 AND EA 6 -5710-81091. 2 L 7 2 4F RT A35EU 2007092500257 20070925 00257 SO 2007 9 25 C2XA07IA200 1 20070911 A 3222 7329MTE1604750 SEAL EMB 145 EMB145LR 3260212 SO NLG LEAKING A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 11548 00708 145565 IAH - FLIGHT 2593, AFTER LIFTOFF THE CREW REPORTED A LANDING GEAR AIR/GROUND FAILURE. THE AIRCRAFT RETURNED TO IAH WHER E IT LANDED WITHOUT INCIDENT. MAINTENANCE REPACKED & SERVICED THE NOSE LANDING GEAR, OPERATIONALLY CHECKED WITH NO DEFE CTS NOTED. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007092500258 20070925 00258 EU 2007 9 25 07FDEA03996 1 20070919 A 5315 A53973599204 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT CROSS BEAM C 60, REPAIR PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 2007092500261 20070925 00261 NM 2007 9 25 USAA920070828 1 20070911 A 5310 DOOR FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 23700 CLT - MAJOR REPAIR - NR 6007658, CRACKED WEB, BS 294.5, S15L, FORWARD ENTRY DOOR CUTOUT FORWARD FRAME. REPAIRED WEB, BS 294.5, S15L, FORWARD ENTRY DOOR CUTOUT FORWARD FRAME IAW B737-300 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007092500263 20070925 00263 EU 2007 9 25 07FDEA04000 1 20070919 A 5313 A53973344 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 FOUND SEVERAL MISDRILLED HOLES ON T-STRINGER 26 RT, AT FRAME 71. REPAIR PERFORMED BY INSTALLING NEW PARTIAL STRINGER PR OFILE FABRICATED WITH COUPLINGS IAW ENG-STATEMENT: REA 0492-009. 2 L 7 2 4F RT A35EU 2007092500264 20070925 00264 NM 2007 9 25 USAA920070829 1 20070911 A 5310 6517684638 DOOR FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 23700 CLT - MAJOR REPAIR - NR 6007659, CRACKED WEB, BS 294.5, S12L, FORWARD ENTRY DOOR CUTOUT FORWARD FRAME. REPAIRED WEB, BS 294.5, S12L, FORWARD ENTRY DOOR CUTOUT FORWARD FRAME IAW B737-300 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007092500265 20070925 00265 EU 2007 9 25 07FDEA04001 1 20070919 A 5311 A53978284200 FRAME AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 FOUND OLD ENLARGED HOLE (DIA 6MM) AT CONNECTING SEGMENT FRAME 55/58, STRG 25 LT. REPLACEMENT OF CONNECTING SEGMENT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092500267 20070925 00267 NM 2007 9 25 USAA920070830 1 20070911 A 5320 692655 FITTING BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 23700 CLT - MAJOR REPAIR - NR 6007479, CRACKED UPPER AND LOWER FRAME CHANNEL CLIPS, BS 348 - BS 351, S16L. REPLACED UPPER AND LOWER FRAME CHANNEL CLIPS, BS 348 - BS 351, S16L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007092500270 20070925 00270 WP 2007 9 25 07FDEA04004 1 20070919 A 5313 ACA3353 LONGERON DOUG DC10 DC1010F 3022111 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 AIR CONDITIONING COMPT LT SIDE FOUND SEVERE EXFOLIATION CORROSION. REPAIRED AREA IAW SRM 53-10-00 VOL I. 2 L 7 3 4F A22WE 2007092500271 20070925 00271 WP 2007 9 25 07FDEA04005 1 20070919 A 5347 ADA7656509 SEAT TRACK DOUG DC10 DC1010F 3022111 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 SEAT TRACK SEVERE CORROSION WITH EXFOLIATION ON SEAT TRACK. REPAIRED SEAT TRACK IAW SRM 53-60-01 FIG 1 VOL I. 2 L 7 3 4F A22WE 2007092500272 20070925 00272 EU 2007 9 25 07FDEA04006 1 20070919 A 5340 A53978048 STRINGER CLIP AIRBUS 310 A310324 3930206 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 FOUND FRAME-STRINGER-CONNECTING ANGLES WITH LESS EDGE MARGIN AT STRINGER 26 RT BETWEEN FRAME 67-68, 69-70 AND 71-72 AND ON STRG 26 LT BETWEEN FRAME 70-71 AND 71-72. REPLACEMENT WITH FABRICATED ENLARGED REPAIR ANGLES IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092500273 20070925 00273 WP 2007 9 25 07FDEA04007 1 20070919 A 5347 ACA7400515 SEAT TRACK DOUG DC10 DC1010F 3022111 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 SEAT TRACK BALLMAT AREA CRACKS ON SEAT TRACK. REPAIRED AREA IAW SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F A22WE 2007092500274 20070925 00274 NM 2007 9 25 07FDEA04009 1 20070919 A 5320 69226705 BRACKET BOEING 727 727227 1384078 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 CROSS BRACKET INSIDE GROUND POWER PLUG ACCESS DOOR HAS CRACKED ATTACH BRACKET AT TOP AFT ATTACH POINT REMOVED CRACKED BRACKET IN REF TO SRM 51-30-2. FABRICATED NEW BRACKET IN REF TO DWG 69-22670-5. INSTALLED NEW BRACKET IN REF TO SRM 51 -30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2007092700287 20070927 00287 EA 2007 9 27 COMA0770048 1 20070910 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 669CA 10176 LEFT AND RIGHT SEAT TRACKS ARE CORRODED FROM FS 500.00 TO FS 785. REMOVED THE CORROSION BY BLENDING IAW REO 670-53-00-0 13. 2 L 7 2 4F RT A21EA 2007092700296 20070927 00296 NM 2007 9 27 SWAA074654 1 20070918 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 216WR 32488 DURING SCHEDULED MV1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007092700309 20070927 00309 NM 2007 9 27 QXEA200701452 1 20070924 A 3233 ACTUATOR BOMBDR DHC8 DHC8402 1390042 NM LT MLG OUT OF ADJUST A QXEA O OTHER O OTHER CL CLIMB 1 NM 09 416QX 4083 BOI FLIGHT NR 2388: LEFT MAIN GEAR WAS SLOW TO RETRACT ON TAKEOFF. TOOK APPROXIMATELY 15 SECONDS LONGER TO RETRACT THAN THE RIGHT MAIN GEAR. MAINTENANCE ADJUSTED OF THE LT MLG RETRACTION ACTUATOR. SWUNG GEAR. FUNCTIONAL TEST GOOD. NO P ARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007092700312 20070927 00312 NM 2007 9 27 QXEA200701455 1 20070923 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - LEFT INBOARD SEAT TRACK HAS WEAR DAMAGE, BOTTOM OF TRACK FRAME AT STATION X507 - X516/Y9.2. REPAIRED IAW RD8-5 3-1339. 2 H 7 2 4T RT A13NM 2007092700313 20070927 00313 NM 2007 9 27 SWAA074662 1 20070918 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092700318 20070927 00318 NM 2007 9 27 SWAA074663 1 20070918 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092700319 20070927 00319 NM 2007 9 27 QXEA200701461 1 20070917 A 5551 MOUNT DHAV DHC8 DHC8202 2809007 NM HORIZONTAL STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - HORIZONTAL STAB FORWARD MOUNT POSTS ARE SCRATCHED ON OUTBOARD SURFACE. REPAIRED IAW RD8-55-847 AND SRM 51-20-5 1, 51-20-16. 2 H 7 2 4T RT A13NM 2007092700327 20070927 00327 NM 2007 9 27 SWAA074667 1 20070918 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092700345 20070927 00345 NM 2007 9 27 QXEA200701468 1 20070921 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 110 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - SKIN CORROSION AT NR 1 DME ANTENNA MOUNT LOCATED JUST AFT OF NOSE GEAR AT STATION 110 LT SIDE OF CENTER. REPAI RED IAW RD8-53-5384 AND RD8-53-9800, AND SRM 51-20-16. 2 H 7 2 4T RT A13NM 2007092700350 20070927 00350 NM 2007 9 27 QXEA200701466 1 20070920 A 5340 STRINGER CLIP DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - STRINGER 23L CLEAT IS CORRODED FORWARD SIDE OF FRAME 424.124 AT STATION X419-X422. REPAIRED IAW SRM 51-20-11, 51-40-11. 2 H 7 2 4T RT A13NM 2007092700351 20070927 00351 NM 2007 9 27 QXEA200701467 1 20070919 A 5340 STRINGER CLIP DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - STRINGER 24L CLEAT IS CORRODED AFT SIDE OF FRAME 387.350 AT STATION X389-X392. REPAIRED IAW SRM 51-20-11, 51-4 0-11. 2 H 7 2 4T RT A13NM 2007092700365 20070927 00365 NM 2007 9 27 AALA20071795 1 20070828 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 903AN 29505 TUL - EMERGENCY LIGHTS AT RIGHT MID COACH CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT MID CO ACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092700372 20070927 00372 EU 2007 9 27 07FDEA04103 1 20070907 A 5310 A53973898200 DOOR FRAME AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 AFT CARGO COMPARTMENT DOOR FRAME, CORROSION AT FRAME 59A BETWEEN STRG29-30 RT. REPAIRED IAW SRM 53-17-13 FIG 210A. 2 L 7 2 4F RT A35EU 2007092700385 20070927 00385 EU 2007 9 27 07FDEA04134 1 20070920 A 5320 A53970875 SHIM AIRBUS 300 A300B4622 3930401 EU ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND SCRUB MARKS AT TORSION BOX LT/RT CROSS SHIM C 56-57, P 15A-16 REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5316-70333 AND RAS/DATLS/0001412/2003 ISS A. 2 L 7 2 4F RT A35EU 2007092700386 20070927 00386 EU 2007 9 27 07FDEA04135 1 20070920 A 5330 A53812189201 SKIN PANEL AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND CORROSION AT SKIN PANEL C39-40, P28-32 RT OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW DRAWING R538- 10533, APPROVED BY EA 6-5315-70344 AND RAS/AS/0273/2003 ISS A. 2 L 7 2 4F RT A35EU 2007092800009 20070928 00009 NM 2007 9 28 SWAA074795 1 20070925 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 220WN 32491 EEPLS LENS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007092800016 20070928 00016 NM 2007 9 28 SWAA074810 1 20070925 A 5754 65C26602 SKIN BOEING 737 7373H4 1384600 NM NR 2 SLAT DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 14Y CHECK, FOUND LEFT WING NR 2 L/E SLAT OUTBOARD UPPER SURFACE DISBONDED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007092800024 20070928 00024 NM 2007 9 28 SWAA074774 1 20070924 A 3350 3071BPEGPL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AT ROW 6 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007092800047 20070928 00047 NE 2007 9 28 2007UALA03742 2 20070916 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LEFT SHUTDOWN A UALA O OTHER E Y VIBRATION/BUFFET ENGINE STOPPAGE NR NOT REPORTED 1 WP 29 768UA 26919 777009 CREW REPORTED LEFT ENGINE AUTO SHUTDOWN, HIGH VIBRATION AND HIGH EGT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007092800048 20070928 00048 EU 2007 9 28 2007UALA03743 1 20070914 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 451UA 865 CREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092800055 20070928 00055 2007 9 28 2007UALA03753 4 20070917 A 3460 FMC BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RIGHT FAILED A UALA O OTHER F FLT CONT AFFECTED DE DESCENT 1 WP 29 545UA 25323 RIGHT FMC ON TOP OF DESCENT WOULDN'T HOLD VNAV=GLIDE PATH HSI WOULD VARY+-1200-MIN PROG 2-2. 10-19-07 THE PROBLEM IS ATTRIBUTED TO A FAILED FLIGHT MANAGEMENT COMPUTER. REPLACED RT FMC. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092800070 20070928 00070 2007 9 28 SWAA074759 4 20070923 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 760SW 27874 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPL ACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007092800075 20070928 00075 NM 2007 9 28 SWAA074761 1 20070923 A 5312 6545819 PRESSURE PANEL BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT RBL 7.5. REPAIRED PANEL PER ACO. 2 L 7 2 4F RT A16WE 2007092800076 20070928 00076 NM 2007 9 28 UPS07M50692 1 20070719 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORZ STAB CONSTANT SECTION BARREL NUT BORE RT NR 18 FOUND WITH CORROSION. CORROSION REMOVED PER SRM 5 1-21-01 VII R38. BOTTOM BORED THRU & BORE REAMED TO 1.067 INCH DIA. REMN BLEND OUT 0.065 INCH DEEP FOUND EXCEED LIMITS PER EO MD11-55 10-19409-L. 10X MAGNIFICATION C/O, NO CORROSION FOUND. REPAIR BUCKET BUSHING FAB & PROTECTED. SEALANT APPLIED AT BLEND OUT VOID & BUSHING INSTALLED. REPAIR C/O AT BARREL NUT BORE RIGHT NR 18 ACCEPTABLE PER EN1457-07. 2 L 7 3 4F RT A22WE 2007092800081 20070928 00081 NM 2007 9 28 F3LA200700247 1 20070916 A 5730 SKIN AIRBUS A319 A319111 3930336 NM LT WING DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 INSPECTION REPORTED LIGHTNING DAMAGE TO LEFT WING UPPER SURFACE RIB 17, APPROX 12 INCHES AFT OF MIDSPAR AT FASTENER LOCA TION. REMOVED FASTENER, BLENDED DAMAGE TO COUNTERSINK IAW SRM 51-11-13. REPLACED FASTENER IAW EA A9-574-12145. 2 L 7 2 4F RT A28NM 2007092800094 20070928 00094 2007 9 28 2007UALA03766 4 20070918 A 3460 COMPUTER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FLT MANAGE MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 116UA 26908 FLIGHT DIVERTED DUE TO MULTIPLE FAULT INDICATIONS. 10-16-07 AFTER TROUBLESHOOTING, REPLACED R-FLIGHT MANAGEMENT CO MPUTER PER MM 34-61-01. GRD TESTED FMC AND SERVO PASSED, NO DEFECT FOUND. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092800095 20070928 00095 EU 2007 9 28 2007UALA03767 1 20070919 A 3150 WARNING MESSAGE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ILLUMINATED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 439UA 683 LANDED UNDER AMBER ALERT DUE TO GREEN HYDRAULIC OVERHEAT ECAM MESSAGE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092800099 20070928 00099 NM 2007 9 28 2007UALA03771 1 20070919 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BS 1990 S43R DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 198UA 28716 EXTERNAL FUSELAGE SKIN DENTED BELOW BULK CARGO DOOR CUTOUT, APPROX BS 1990 STR 43R. MAJOR REPAIR ACCOMPLISHED: INSTALL ED SKIN DOUBLER REPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092800105 20070928 00105 NM 2007 9 28 SWAA074699 1 20070919 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 986 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 735SA 27867 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 986, RBL 45. REPAIRED FLOORBEAM WEB PER MM. 2 L 7 2 4F RT A16WE 2007092800107 20070928 00107 NM 2007 9 28 SWAA074703 1 20070919 A 3350 1619 LAMP BOEING 737 7373Q8 1384670 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007092800108 20070928 00108 NM 2007 9 28 SWAA074701 1 20070919 A 3350 20131A BATTERY BOEING 737 7373Q8 1384670 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007092800110 20070928 00110 NM 2007 9 28 KCSA071387 1 20070923 A 5340 FITTING BOEING 747 7472B4B 138481B NM BS 1910 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 AFT PIT, AFT PALLET STOP BATHTUB FITTING CRACKED AT BS 1910, RBL 45. 2 L 7 4 4F RT A20WE 2007092800124 20070928 00124 NM 2007 9 28 KCSA071392 1 20070924 A 5330 SKIN BOEING 747 7472B4B 138481B NM BS 690 S35-36R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA 690 BETWEEN STR 35R AND STR 36R SKIN DAMAGED. 2 L 7 4 4F RT A20WE 2007092800129 20070928 00129 NM 2007 9 28 SWAA074695 1 20070919 A 3350 3017BPEGPL LAMP BOEING 737 737317 138447P NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND FWD RIGHT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007092800139 20070928 00139 NM 2007 9 28 SWAA074687 1 20070919 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM BS 910 S27L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 910, STR 27L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007092800142 20070928 00142 NM 2007 9 28 UPS07M50719 1 20070629 A 5330 SKIN DOUG MD11 MD11F 3023600 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C FUSELAGE SKIN AROUND FORWARD CARGO DOOR OPENING AT LOWER AFT CORNER HAS DAMAGE (MATERIAL MISSING). DA MAGED AREA TRIMMED OFF PER EN 1486-07. HFEC INSP C/O AS PER DAC NDTSPM R13 06-10-01.001 ON TRIMMED OFF AREA & FOUND NO CRACK. REPAIR INNER & OUTER DOUBLERS FAB PER EN 1486-07. SKIN REPAIRED PER EN1486-0 7 & SRM 51-31-01 VII R38. SKIN DO UBLERS REINSTALLED PER SRM 51-31-01 VII R38. 2 L 7 3 4F RT A22WE 2007092800147 20070928 00147 NM 2007 9 28 SWAA074692 1 20070919 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 827 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092800152 20070928 00152 NM 2007 9 28 SWAA074715 1 20070919 A 2560 P4010021 BATTERY BOEING 737 7375H4 138449D NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND FWD CABIN EMERGENCY EXIT FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2007092800157 20070928 00157 NM 2007 9 28 2007UALA03776 1 20070919 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EXIT LIGHT INOP AT DOOR 1L AFT SILL LIGHT. 10-16-07 REPLACED LAMP. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092800162 20070928 00162 NM 2007 9 28 2007UALA03781 1 20070918 A 3520 OXYGEN MASK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE SEAT 2AB UNWANTED DEPLOY A UALA O OTHER O OTHER TO TAKEOFF 1 WP 29 851UA 1664 OXYGEN MASKS AT 2AB DEPLOYED ON TAKEOFF. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092800172 20070928 00172 NM 2007 9 28 SWAA074702 1 20070919 A 3350 W998491020 WIRE BOEING 737 7373Q8 1384670 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. FOUND UN-TERMINATED WIRE, RE-TERMINATED WIRE PER MM. 2 L 7 2 4F RT A16WE 2007092800176 20070928 00176 EU 2007 9 28 2007UALA03786 1 20070918 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW READS LOW A UALA O OTHER O OTHER CR CRUISE 1 WP 29 480UA 1555 CREW REPORT: CREW O2 DROPPED FROM 1680 PSI TO 1420 PSI INFLIGHT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092800184 20070928 00184 NM 2007 9 28 2007UALA03794 1 20070919 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 500D S27R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 FORWARD CARGO PIT FRAME CRACKED AT STA 500D AFT SIDE STRINGER 27R AND RBL 14. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED FORMED INTERNAL DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092800185 20070928 00185 EU 2007 9 28 MAC090702 1 20070917 A 5710 STRUCTURE AEROSP ATR42 ATR42300 8680920 EU CENTER WING CORRODED A MTNA K NONE O OTHER IN INSP/MAINT 1 SO 33 923FX 135 DURING INSPECTION, FRETTING CORROSION WAS FOUND ON THE CENTER WING CUTOUT OF THE FUEL PANEL HOUSING AT 522CT. REFERENCE ATR42 SRM 57-14-12 PAGE 302 FIG 301 SHEET 1. AFTER DAMAGE REMOVAL THE REMAINING THICKNESS IS 0.425 AROUND THE ENTIRE C IRCUMFERENCE OF THE DOOR HOUSING. THE REPAIR IS IAW ATR 42 STRUCTURAL REPAIR INSTRUCTION DO/TS-3988/079267 REF: ANA/E/4 237/2007/E-001. APPLICABILITY: ATR 42 MSN 135 DATED 09/21/2007. 2 H 7 2 4T RT A53EU 2007092800186 20070928 00186 WP 2007 9 28 ABXA070311 1 20070904 A 5753 59110041503 VANE DOUG DC9 DC933F 302207A WP LT WING TE FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 LEFT FLAP INBOARD FIXED VANE UPPER AND LOWER SURFACES CORRODED. REMOVED AND REPLACED LEFT FLAP INBOARD FIXED VANE IAW D C9 MM 27-51-03-2-0002. 2 L 7 2 4F A6WE 2007092800198 20070928 00198 EA 2007 9 28 TRAX200701360 1 20070916 A 1100 SIGN CNDAIR CL600 CL6002C10 1390015 EA CABIN TORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 717EV 10088 ASD EXIT SIGN TORN. 2 L 7 2 4F RT A21EA 2007092800199 20070928 00199 EA 2007 9 28 TRAX200701361 1 20070916 A 3350 CHARGER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 NR 2 EMERGENCY LIGHTS BATTERY CHARGER NEEDS TO BE REPLACED. 2 L 7 2 4F RT A21EA 2007092800200 20070928 00200 EA 2007 9 28 TRAX200701362 1 20070916 A 3350 CHARGER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 NR 3 EMERGENCY LIGHTS BATTERY CHARGER NEEDS TO BE REPLACED. 2 L 7 2 4F RT A21EA 2007092800212 20070928 00212 NM 2007 9 28 UPS07M50720 1 20070729 A 5320 ADA00331 SUPPORT DOUG MD11 MD11F 3023600 NM BS 1039 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C FWD CARGO COMPT AT STATION 1039 X-16.5 FOUND SUPPORT STRUT DEFORMED/DAMAGED. FWD CARGO COMPT STA 1039 X-16.5 RT DEFORMED DMG SUPPORT STRUT REMOVED. NEW SUPPORT STRUT ADA0033-1 HOLES P/UP. NEW SUPPORT STRUT ADA0033-1 INS TALLED AT FWD CARGO COMPT STA 1039 X-16.5 RT. PAINT TOUCHED UP ON REWORK AREA. 2 L 7 3 4F RT A22WE 2007092800214 20070928 00214 NM 2007 9 28 UPS07M50728 1 20070725 A 5730 SKIN DOUG MD11 MD11F 3023600 NM LT WING TE FLAP DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C LEFT WING INBOARD FLAP UPPER SURFACE SKIN DENT. LEFT WING I/B FLAP UPPER SURFACE SKIN DENT AREA TRIMM ED OUT. HFEC INSP C/OUT ON TRIMMED OUT FOUND NO CRACK. REPAIR DOUBLER FABRICATED USING MAT'L 2024T3-0.040" & HOLES PIC KED UP. REPAIR PARTS REPROTECTED & PAINTED. REPAIR PARTS INSTALLED AS PER SRM 57-10-00 VOL I REV 38 FIG 34. 2 L 7 3 4F RT A22WE 2007092800218 20070928 00218 NM 2007 9 28 UPS07M50732 1 20070810 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZ STAB CONSTANT SECTION BARREL NUT BORE RT NR 31 FOUND WITH CORROSION. CORR AT BARREL NUT BORE RM VD PER SRM 51-21-01VII R38. BOTTOM SURFACE BORED THRU BORE REAMED TO 1.178" DIA, REMN BLEND OUT 0.030" DEEP, EXCEEDED L IMITS. BARREL NUT BORE & BLEND OUT VOID RADIUS SMOOTHENED & PROTECTED PER SRM 51-21-01 VII R38. BUCKET BUSHING FAB, PR OTECTED & INSTALLED. REPAIR C/O AT BARREL NUT BORE NR 31 RT IS ACCEPTABLE AS PER EN 1517-07. 2 L 7 3 4F RT A22WE 2007092800219 20070928 00219 NM 2007 9 28 UPS07M50733 1 20070810 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZ STAB CONSTANT SECTION BARREL NUT BORE RT NR 34 FOUND WITH CORROSION. CORR AT BARREL NUT BORE RM VD PER SRM 51-21-01 VII R38. BOTTOM SURFACE BORE THRU. BORE REAMED TO 1.178" DIA, REMN BLEND OUT 0.065" DEEP. EXCEEDE D LIMITS. BARREL NUT BORE & BLEND OUT VOID RADIUS SMOOTHEN & PROTECTED PER SRM 51-21-01 VII R38. BUCKET BUSHING FAB, P ROTECTED & INSTALLED. REPAIR C/O AT BARREL NUT BORE NR 34 RT IS ACCEPTABLE PER EN 1518-07. 2 L 7 3 4F RT A22WE 2007092800220 20070928 00220 NM 2007 9 28 UPS07M50734 1 20070810 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZ STAB CONSTANT SECTION BARREL NUT BORE LT NR 28 FOUND WITH CORROSION. CORR AT BARREL NUT BORE RM VD PER SRM 51-21-01 VII R38. BOTTOM BORE THRU BORE REAM TO 1.178" DIA. RMN BLEND OUT 0.025" DEEP, EXCEEDED LIMITS. B ARREL NUT BORE, BLEND OUT VOID SMOOTHEN & PROTECTED. BUCKET BUSHING FAB, PROTECTED & INSTALLED. REPAIR C/O AT BARREL N UT BORE NR 28 LT IS ACCEPTABLE AS PER EN 1519-07. 2 L 7 3 4F RT A22WE 2007092800221 20070928 00221 NM 2007 9 28 UPS07M50735 1 20070813 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZ STAB CONSTANT SECTION BARREL NUT RT NR 33 FOUND WITH CORROSION. CORR AT BARREL NUT BORE RMVD PE R SRM 51-21-01 VII R38. BOTTOM BORED THRU & BORE REAM TO 1.178" DIA. RMN BLEND OUT 0.050" DEEP. EXCEEDED LIMITS. BOR E REWK FURTHER TO 1.203" DIA PER EN 1522-07. BUCKET BUSHING FAB, PROTECTED PER SRM 51-21-01 VII R38. BUCKET BUSHING IN STALLED. REPAIR C/O AT BARREL NUT BORE NR 33 RT IS ACCEPTABLE PER EN 1522-07. 2 L 7 3 4F RT A22WE 2007092800224 20070928 00224 NM 2007 9 28 07FDEA04188 1 20070921 A 3230 SELECTOR VALVE DOUG MD11 MD11F 3023600 NM RT MLG MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 521FE 48478 RIGHT MAIN LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. RED INDICATION IN BOTH MAIN LG DISPLAY AND CONFIG PAGE. REFERED TO QRH, RECYCLED GEAR, GOOD INDICATIONS (ALL UP) FOLLOWED. VISUALLY INSPECTED RT MAIN LDG GEAR AND AROUND OF SELECTOR VALVE, FOUND NORMAL. LDG GEAR POSITION INDICATION SYS NORMAL PER MM 32-61-00-5. A/C OK FOR SVC. 2 L 7 3 4F RT A22WE 2007100100011 20071001 00011 SO 2007 10 1 C2XA07TY054 1 20070921 A 3350 1317 BULB EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14930 145011 EMERGENCY LIGHT IN SERVICE DOOR AND AT SEAT 12 BC AT TOP INOP. REMOVED AND REPLACED BULBS IAW EMB 145 AMM 33-50-00, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007100100016 20071001 00016 NM 2007 10 1 KCSA071412 1 20070926 A 5313 STRINGER BOEING 747 7472B4B 138481B NM BS 2360 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STR 19R END FITTING CORRODED FWD OF BS 2360. 2 L 7 4 4F RT A20WE 2007100100020 20071001 00020 NM 2007 10 1 KCSA071397 1 20070925 A 5310 PANEL BOEING 747 747122 1384872 NM TORQUE BOX PUNCTURED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 AFT PIT BILGE TORQUE BOX UPPER PANEL PUNCTURED AT BS 1843, LBL 28 AND BS 1850, LBL 43. 2 L 7 4 4F A20WE 2007100100022 20071001 00022 NM 2007 10 1 USAA920070852 1 20070924 A 5320 FLOOR SUPPORT BOEING 757 757225 1384959 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916UW 22192 PIT - MAJOR REPAIR - C-4 CHECK, CORROSION ON FLOOR SUPPORT ANGLE, BS 800 - BS 880, S17. REPAIRED FLOOR SUPPORT ANGLE, B S 800 - BS 880, S17 IAW B757-200 SRM 51-70-12. 2 L 7 2 4F RT A2NM 2007100100027 20071001 00027 NM 2007 10 1 KCSA071406 1 20070926 A 5312 STRAP BOEING 747 7472B4B 138481B NM BULKHEAD CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 LEFT AND RIGHT BS 1241 BULKHEAD SPICE STRAPS CORRODED AT AFT BOLT HOLES BS 1241, STR 27L AND STR 27R. 2 L 7 4 4F RT A20WE 2007100100028 20071001 00028 NM 2007 10 1 KCSA071408 1 20070926 A 5410 STIFFENER BOEING 747 7472B4B 138481B NM NR 2 NACELLE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 NR 2 PYLON NAC STA 219 LOWER SPAR STIFFENER DENTED AND GOUGED. 2 L 7 4 4F RT A20WE 2007100100029 20071001 00029 NM 2007 10 1 KCSA071409 1 20070926 A 5313 STRINGER BOEING 747 7472B4B 138481B NM BS 2360 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STR 49L END FITTING CORRODED FWD OF BS 2360. 2 L 7 4 4F RT A20WE 2007100100030 20071001 00030 NM 2007 10 1 KCSA071410 1 20070926 A 5313 STRINGER BOEING 747 7472B4B 138481B NM BS 2360 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STR 40R END FITTING CORRODED FWD OF BS 2360. 2 L 7 4 4F RT A20WE 2007100100031 20071001 00031 NM 2007 10 1 KCSA071411 1 20070926 A 5313 STRINGER BOEING 747 7472B4B 138481B NM BS 2360 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STR 36R END FITTING CORRODED FWD OF BS 2360. 2 L 7 4 4F RT A20WE 2007100100032 20071001 00032 NM 2007 10 1 KCSA071413 1 20070926 A 5313 STRINGER BOEING 747 7472B4B 138481B NM BS 2360 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STR 36L END FITTING CORRODED FWD OF BS 2360. 2 L 7 4 4F RT A20WE 2007100100033 20071001 00033 NM 2007 10 1 KCSA071414 1 20070926 A 5313 STRINGER BOEING 747 7472B4B 138481B NM BS 2360 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STR 50L END FITTING CORRODED FWD OF BS 2360. 2 L 7 4 4F RT A20WE 2007100100034 20071001 00034 NM 2007 10 1 KCSA071415 1 20070926 A 5313 STRINGER BOEING 747 7472B4B 138481B NM BS 2360 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STR 44L END FITTING CORRODED FWD OF BS 2360. 2 L 7 4 4F RT A20WE 2007100100042 20071001 00042 NM 2007 10 1 USAA920070834 1 20070915 A 5320 141N5160 FLOOR SUPPORT BOEING 757 757225 1384959 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916UW 22192 PIT - MAJOR REPAIR - C-4 CHECK, CORROSION ON FLOOR SUPPORT, BS 324 - BS 345, RBL 63. REPLACED FLOOR SUPPORT, BS 324 - BS 345, RBL 63 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007100100043 20071001 00043 NM 2007 10 1 USAA920070835 1 20070914 A 5320 141N5160079 FLOOR SUPPORT BOEING 757 757225 1384959 NM BS 324-345 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916UW 22192 PIT - MAJOR REPAIR - C-4 CHECK, CORROSION ON FLOOR SUPPORT, BS 324 - BS 345, RBL 60. REPLACED FLOOR SUPPORT, BS 324 - B S 345, RBL 60 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007100100044 20071001 00044 NM 2007 10 1 USAA920070836 1 20070914 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916UW 22192 PIT - MAJOR REPAIR - C-4 CHECK, CORROSION ON FLOORBEAM, BS 1640. REPLACED FLOORBEAM, BS 1640 IAW USAIRWAYS TYPICAL REPA IR 53-15-01. 2 L 7 2 4F RT A2NM 2007100100045 20071001 00045 NM 2007 10 1 USAA920070837 1 20070915 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916UW 22192 PIT - MAJOR REPAIR - C-4 CHECK, CORROSION ON FLOORBEAM, BS 1640, LBL 20 - RBL 60. REPLACED FLOORBEAM, BS 1640, LBL 20 - RBL 60 IAW USAIRWAYS TYPICAL REPAIR 53-15-01. 2 L 7 2 4F RT A2NM 2007100100048 20071001 00048 NM 2007 10 1 USAA920070840 1 20070915 A 5347 146N51261 SEAT TRACK BOEING 757 757225 1384959 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916UW 22192 PIT - MAJOR REPAIR - C-4 CHECK, CORROSION ON SEAT TRACK, BS 1620 - BS 1640, RBL 25. REPLACED SEAT TRACK, BS 1620 - BS 1 640, RBL 25 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007100100059 20071001 00059 EA 2007 10 1 TRAX200701365 1 20070917 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA BS 640 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 681BR 7680 LEFT FS 640.00 BONDED SKIN DOUBLER IS CRACKED. 10-18-07 REPAIRED CRACKED LT BONDED SKIN DOUBLER IAW EC/TC REO 601R -53-61-506. 2 L 7 2 4F RT A21EA 2007100100070 20071001 00070 EU 2007 10 1 07FDEA04324 1 20070927 A 5311 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 724FD 530 LESS EDGE MARGIN FOR INSTALLATION OF FASTENER HL DAN 5-6 DURING PTOF CONVERSION ON ATTACH ANGLE AT FRAME 66, STGR 35 RT. REPLACEMENT OF ATTACH ANGLE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100071 20071001 00071 EU 2007 10 1 07FDEA04325 1 20070927 A 5315 A53612248202 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 HEAVY CORROSION ON CROSSBEAM BETWEEN FLOORBEAM 12A-14. REPLACEMENT OF CROSSBEAM IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100079 20071001 00079 EU 2007 10 1 07FDEA04281 1 20070925 A 5754 A53510287201 SKIN AIRBUS 300 A300B4622R 3930312 EU KRUEGER FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 FOUND DENT ON NOSE SKIN OF RT KRUEGER FLAP (70MMX50MM, DEEPNESS 2.7MM). REPAIR PERFORMED BY DRESSING OUT THE PANEL, HFEC -ROTOTEST INSPECTION AND OVERSIZING RIVETS IN DENTED AREA IAW EA 6-5745-92141 AND RAS/AS/0160/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100100082 20071001 00082 NM 2007 10 1 07FDEA04284 1 20070925 A 5311 65255818 FRAME BOEING 727 727227 1384078 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 RIGHT LOWER FUSELAGE PANEL NR 3438, INBOARD FORMER RIB AT CENTER OF ACCESS PANEL CUT-OUT CRACKED AT OUTBOARD ATTACH POIN T ON INNER SIDE. REPLACED Z ANGLE IAW BOEING DWG 65-25581, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2007100100084 20071001 00084 NM 2007 10 1 07FDEA04286 1 20070925 A 5340 6611809 STRINGER CLIP BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 AFT PIT STA 1030 LBL 23" WL 147, STRINGER CLIP HAS LIGHT CORROSION. REMOVED DAMAGED STRINGER CLIP, FABRICATED NEW CLIP TREATED, PRIMED AND INSTALLED REF 51-30-2, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007100100086 20071001 00086 NM 2007 10 1 07FDEA04288 1 20070925 A 5754 652167228 ANGLE BOEING 727 727227 1384078 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 LEFT WING LE NR 2 SLAT, ACTUATOR LWR FAIRING SUPPORT ANGLE CRACKED ON INBD SIDE FWD FASTENER LOCATION. REMOVED CRACKED ANGLE ON L/E NR 2 SLAT ACTUATOR FAIRING SUPPORT IAW SRM 51-30-02 PG 1. LOCATED DRILLED, TREATED, PRIMED AND PAINTED IAW SRM'S 51-10-1 PG 10, 51-10-2 PG 1. INSTALLED ANGLE IAW SRM 51-30-2 PG 14. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2007100100093 20071001 00093 EU 2007 10 1 07FDEA04194 1 20070924 A 5311 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 HEAVY CORROSION ON CROSS STRUT FRAME 87 LT, AFT SIDE. REPLACEMENT OF CROSS STRUT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100095 20071001 00095 EU 2007 10 1 07FDEA04196 1 20070924 A 5320 A53810966200 DIAPHRAGM AIRBUS 300 A300B4605R 3930308 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 FOUND DENTS AND NICKS IN DIAPHRAGM C 53-54, TR1-2RT. REPAIR PERFORMED BY CUT OUT DAMAGED AREA AND INSTALLING A DOUBLER IAW EA 6-5315-112500 AND RAS 053448/012/2007 ISS A . 2 L 7 2 4F RT A35EU 2007100100096 20071001 00096 EU 2007 10 1 07FDEA04197 1 20070924 A 5320 A53973310206 ANGLE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 HEAVY CORROSION ON CONNECTING ANGLE FRAME 64, STRG 36 RT. REPLACEMENT OF ANGLE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100097 20071001 00097 EU 2007 10 1 07FDEA04198 1 20070924 A 5330 A53773487 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 TWO CORROSION SPOTS OUT OF SRM LIMITS ON INTERNAL SKIN BETWEEN FRAME 19-20, STRG 51-52 LHS. REPAIR PERFORMED BY CORROSI ON REMOVAL, FLAP PEENING, NDT INSPECTION FOR CRACK FREE CONDITION AND INSTALLATION OF ENLARGED FILLER AND FINGER STRAP I AW EA 6-5313-82909 AND RAS/DABRE/7005417/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007100100109 20071001 00109 EU 2007 10 1 07FDEA04208 1 20070924 A 5310 A53973085 BEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FOUND CORROSION ON AFT CARGO DOOR SILL BEAM BETWEEN FRAME 59-60. AREA IS UNDER FRAME 59A. REPAIR PERFORMED BY CUT OUT SILL BEAM WEB AND INSTALLING REPAIR ANGLE AND FILLER IAW EA 6-5317-82915 AND RAS/DAHAM/4019686/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100100111 20071001 00111 EU 2007 10 1 07FDEA04210 1 20070924 A 5313 A53980165202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 HEAVY CORROSION ON STRG 27 RT, BETWEEN FRAME 74-75 AND FRAME 75-75A. PARTIAL REPLACEMENT OF STRINGER 27 RT, C74-76 WITH THREE COUPLINGS BETWEEN FRAME 73A-74, FRAME 74-75 AND FRAME 75A-76 IAW EA 6-5318-82912 AND RAS/DAHAM/4019688/2005 ISS UE A. 2 L 7 2 4F RT A35EU 2007100100116 20071001 00116 EU 2007 10 1 07FDEA04215 1 20070924 A 5330 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 ENLARGED HOLES IN FUSELAGE SKIN AT BEAM 10 BETWEEN FRAME 68-69 AND AT FRAME 67 BETWEEN STRINGER 43-44 RT, BULK CARGO DOO R CUT OUT. REPLACEMENT OF BEAM 10 IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100121 20071001 00121 EU 2007 10 1 07FDEA04219 1 20070924 A 5313 A53773633202 STRINGER AIRBUS 300 A300B4622 3930401 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND OLD STRINGER REPAIR C20-21, P 54 LT NOT COMPATIBLE WITH P TO F CONVERSION. STRINGER REPAIR RENEWED IAW SRM 53-10- 14 FIG 201. 2 L 7 2 4F RT A35EU 2007100100128 20071001 00128 EU 2007 10 1 07FDEA04226 1 20070924 A 5320 A53986751207 WEB AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FOUND DAMAGED WEB PLATE BETWEEN FRAME 86-87, STRG 33 RT. REPLACEMENT OF WEB IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100129 20071001 00129 EU 2007 10 1 07FDEA04227 1 20070924 A 5320 A53986750214 WEB AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 DAMAGED WEB PLATE BETWEEN FRAME 85-86, STR 33 RT. REPLACEMENT OF WEB IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100130 20071001 00130 EU 2007 10 1 07FDEA04228 1 20070924 A 5320 A53986733207 WEB AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 DAMAGED WEB PLATE BETWEEN FRAME 86-87, STRG 39 RT. REPLACEMENT OF WEB IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100132 20071001 00132 EU 2007 10 1 07FDEA04230 1 20070924 A 5313 A53974202 STRINGER AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND CORROSION AT STRINGER P 51 LT, C 59-60; P 52 LT AT C58-59 AND P 53 LT AT C58-59. STRINGER REPAIR PERFORMED IAW SR M 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007100100133 20071001 00133 NM 2007 10 1 F3LA200700250 1 20070924 A 3397 CONNECTOR AIRBUS A319 A319111 3930336 NM EMERGENCY LIGHTS LOOSE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 932FR 2258 DURING HEAVY SERVICE CHECK, MAINTENANCE REPORTED EMERGENCY FLOOR PATH LIGHTS INOPERATIVE AT ROWS 15 AND 16. RE-SECURED LOOSE CONNECTOR AT SIDE PANEL. PERFORMED OPERATIONAL CHECK IAW AMM 33-51-00-710-001 AND CHECKED GOOD. 2 L 7 2 4F RT A28NM 2007100100134 20071001 00134 EU 2007 10 1 07FDEA04233 1 20070924 A 5320 A53974202418 WEDGE AIRBUS 300 A300B4622 3930401 EU CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND CORROSION AT WEDGE C 59-60, P 52 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100136 20071001 00136 EU 2007 10 1 07FDEA04236 1 20070924 A 5320 A53974242200 FITTING AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND CORROSION AT FITTING C63. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100137 20071001 00137 EU 2007 10 1 07FDEA04237 1 20070924 A 5315 A53978254202 FLOORBEAM AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND CORROSION AT CROSS BEAM C 64 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100144 20071001 00144 EU 2007 10 1 07FDEA04244 1 20070924 A 5320 A53773644 FITTING AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND CORROSION AT CORNER FITTING C33 LT AND RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100146 20071001 00146 EU 2007 10 1 07FDEA04246 1 20070924 A 5730 A57340087 SKIN PANEL AIRBUS 300 A300B4622 3930401 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 ELONGATED HOLES OF HYDRAULIC PIPE SUPPORT BRACKET AND LOWER SKIN PANEL NR 2, BOTH WINGS. REPAIR PERFORMED BY OVERSIZING HOLES, SPOTFACING AND BUSHING USING THE PRINCIPLES OF REPAIR INSTRUCTION R571-50532 IAW EA 6-5720-82902 AND RAS/BAE/100 0997/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100100147 20071001 00147 EU 2007 10 1 07FDEA04247 1 20070924 A 5511 SPAR AIRBUS 310 A310222 3930315 EU HORIZONTAL STAB DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 446FE 224 RIGHT HORIZONTAL STAB ON UPPER REAR SPAR BETWEEN RIBS 9 AND 10 REPAIR STRAP REQUIRES REMOVAL FOR MATERIAL TYPE VERIFICAT ION REMOVED STRAP REF A310-200 SRM 51-40-21. FABRICATED STRAP IAW FED ED A310-200 SRM 55-11-21 FIG 215 AND PG 285. INS TALLED REPAIR STRAP IAW FED EX SRM A310-200 SRM 55-11-21 FIG 215 AND PAGE 285. 2 L 7 2 4F RT A35EU 2007100100148 20071001 00148 EU 2007 10 1 07FDEA04248 1 20070924 A 5511 SPAR AIRBUS 310 A310322 3930334 EU HORIZONTAL STAB FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 446FE 224 LEFT HORIZONTAL STAB ON UPPER REAR SPAR BETWEEN RIBS 4/5 REPAIR STRAP IN WRONG MATERIAL TYPE. REMOVE AND REPLACE AS R EQUIRED REMOVED STRAP IAW A310-200 FX SRM 55-11-21. FABRICATED NEW STRAP IAW FX A310-200 SRM 55-11-21 FIG 214 AND PG 28 5. INSTALLED NEW STRAP IAW FX SRM A310-200 51-40-21. 2 L 7 2 4F RT A35EU 2007100100149 20071001 00149 EU 2007 10 1 07FDEA04249 1 20070924 A 5415 A54612403 PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 WEARED HOLES IN LATERAL PANELS (INBOARD AND OUTBOARD), RIB 8 UPPER SPAR OF PYLON NR 2 RT. REPAIR PERFORMED BY INSTALLAT ION OF BUTTERFLY DOUBLERS ON BOTH PANELS IAW SRM 54-51-31/CONFIG 2/PB201. 2 L 7 2 4F RT A35EU 2007100100151 20071001 00151 EU 2007 10 1 07FDEA04251 1 20070924 A 5511 SPAR AIRBUS 310 A310322 3930334 EU HORIZONTAL STAB DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 446FE 224 LEFT HORIZONTAL STAB ON UPPER REAR SPAR BETWEEN RIBS 10 AND 11 REPAIR STRAP REQUIRES REMOVAL FOR MATERIAL TYPE VERIFICAT ION REMOVED STRAP IAW A310-200 SRM 55-11-21 PG 202. FABRICATED NEW STRAP IAW A310-200 SRM 55-11-21 FIG 214 AND PG 285. INSTALLED NEW STRAP IAW A310-200 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007100100153 20071001 00153 EU 2007 10 1 07FDEA04253 1 20070924 A 5730 A57340087225 SKIN AIRBUS 300 A300B4605R 3930308 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 FOUND ELONGATED HOLES ON RT WING BOTTOM SKIN AFT OF REAR SPAR. REPAIR PERFORMED BY OVERSIZING AND BUSH INSTALLATION IAW DRAWING R571-50532 AND SB 29-6058, APPROVED BY EA 6-2910-112501 AND RAS/BAE/1005314/2007 ISS A. 2 L 7 2 4F RT A35EU 2007100100154 20071001 00154 EU 2007 10 1 07FDEA04254 1 20070924 A 5730 A572609306201 SKIN PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORROSION FOUND UNDER RT WING TIP STATIC DISCHARGER NR 1 AND NR 2 REPAIR PERFORMED BY BLEND OUT CORROSION AND INSTALLING A PATCH IAW EA 6-5730-112504 AND RAS/FOK/179/2007 ISS A. 2 L 7 2 4F RT A35EU 2007100100155 20071001 00155 EU 2007 10 1 07FDEA04255 1 20070924 A 5730 A57260306201 SKIN PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORROSION FOUND UNDER LT WING TIP STATIC DISCHARGER NR 1. REPAIR PERFORMED BYBLEND OUT CORROSION AND INSTALLING A PATCH IAW EA 6-5730-112474 AND RAS/FOK/178/2007 ISS A. 2 L 7 2 4F RT A35EU 2007100100156 20071001 00156 NM 2007 10 1 07FDEA04146 1 20070921 A 5311 AFA00203 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 MAIN DECK CARGO COMPARTMENT: MAINFRAME STA 1701 AT LONGERON 12L FOUND WITH DENT. 10-04-07 REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG I VOL I. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9500 CYLCES TO BE CARRIE OUT AS PER SRM 53-30-00 FIG 1 VOL I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007100100157 20071001 00157 NM 2007 10 1 07FDEA04147 1 20070921 A 5311 AFA00183 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 MAIN DECK CARGO COMPARTMENT, MAIN FRAME STA 1741 AT LONGERON 12L FOUND WITH DENT. 10-04-07 REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG I VOL I. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9500 CYLCES TO BE CARRIED O UT AS PER SRM 53-30-00 FIG 1 VOL I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007100100158 20071001 00158 NM 2007 10 1 07FDEA04148 1 20070921 A 5311 AFA00283 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 MAIN DECK CARGO COMPARTMENT: MAINFRAME STA 1681 AT LONGERON 12R FOUND WITH DENT. 10-04-07 REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG I VOL I. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9500 CYLCES TO BE CARRIED OU T AS PER SRM 53-30-00 FIG 1 VOL I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007100100159 20071001 00159 NM 2007 10 1 07FDEA04149 1 20070921 A 5347 ACA7104521 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 MAIN DECK CABIN SEAT TRACK AT STA 635, X = 27.5 LT FOUND WITH CRACK. FOUND AFTER REMOVAL OF LOWER FWD CARGO CEILING PAN EL. 10-04-07 REPAIRED BY SECTION A SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG 1 VOL I. REPAIR CLASSIFIED AS MAJ OR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007100100160 20071001 00160 NE 2007 10 1 A6WA200740482 2 20070823 A 7261 2810044101 CHECK VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT ENGINE FLUCTUATES A A6WA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 31 446AW 10063 7806 AT FLIGHT LEVEL 28 NOTED OIL FLUCTUATION ON RIGHT ENGINE. RAN QRH. FLUCTUATION MAINTAINED ABOVE 28-40 PSI INDICATED. DECLARED AN EMERGENCY. LANDED WITHOUT ANY PROBLEMS. FOUND LEAK ON ENGINE SERVICING LINE TO RT ENGINE, ALONG WITH AN OP EN OIL SERVICE CHECK VALVE. REMOVED AND REPLACED OIL SERVICE LINE P/N 600-63100-15, IAW AMM 20-21-20 AND 20-22-00. REM OVED AND REPLACED OIL SERVICE CHECK VALVE ON RIGHT ENGINE IAW 79-12-13. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007100200001 20071002 00001 NM 2007 10 2 DXTA200702430 1 20070823 A 2612 FIRE WARNING AMD FALC50 FALCON2000 2730170 NM PWC PW308 PW308C 52182 NE CARGO BAY FALSE ACTIVATION E DXTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 221QS 54 BAGGAGE COMPARTMENT FIRE WARNING LIGHT AND ARUAL WARNING WITH MASTER WARNING AND CAS MESSAGE. M2B INSPECTED SENSOR AND P ERFORMED BAGGAGE BAY FIRE WARNING TEST IAW F2000 MM 26-103 NO DEFECT NOTED. 2 K 7 2 4F 4 F RT A50NM E00065EN 2007100200002 20071002 00002 CE 2007 10 2 LHO2007F00000 1 20070802 A 2910 572700229 LINE CESSNA 441 441 2076020 CE GARRTT TPE331 TPE331* 01514 WP HYD SYSTEM FAILED E LHOA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 05 716SM 4410004 THE LT FIRE WALL TO WING ROOT (RESEVOIR) HIGH PRESSURE HYDRAULIC LINE DEVELOPED A CRACK IN THE BEND RADIUS NEAR THE ATTA CH FITTING TO THE FIREWALL. A FACTORY REPLACEMENT LINE WAS INSTALLED. THIS OPERATOR FEELS THIS IS DUE TO THE AGE OF TH E FLEET ALONG WITH THE FACTORY BENDING MANDREL. (K) 1 L 7 2 3T 3 T RT A28CE E2WE 2007100200007 20071002 00007 NM 2007 10 2 AMTA200700431 1 20070910 A 5321 FLOOR PANEL BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE BS 310-350 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 CABIN FLOOR PANEL AT STA 310-350, LBL 22 HAS HEAVY CORROSION, OUT OF LIMITS. FAB NEW PANEL IAW DRWNG 141N5369. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007100200011 20071002 00011 NM 2007 10 2 AMTA200700436 1 20070911 A 5315 FLOORBEAM BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE BS 377 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 CORROSION ON BEAM FLOOR SUPPORT UPPER CAP LOWER SURFACE AT BS 377.7, LBL 61. REMOVED CORROSION, SRM 53-00-51-1A FOUND A REA OUT OF LIMITS SRM 53-00-51-2R-3 AND SRM 51-40-02. (K) REMOVED AND REPLACED FLOORBEAM UPPER CAP STATION 377.7 LBL 6 5 IAW SRM 53-00-51-2R-3 AND SRM 51-40-02. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2007100200012 20071002 00012 NM 2007 10 2 AMTA200700412 1 20070829 A 3350 D71701100 BATTERY BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHT UNSERVICEABLE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 552TZ 32586 LT OVERWING EXITS EMERGENCY LIGHTS POWER SUPPLY IN OP. REMOVED AND REPLACED LT OVERWING EXIT EMERGENCY LIGHT POWER SUPP LY IAW AMM 31-51-07-22, OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007100200013 20071002 00013 NM 2007 10 2 MWEA070220 1 20070919 A 7830 7150922505 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 905ME 55169 LEFT THRUST REVERSER, BOTTOM DEFLECTOR DOOR, ZEE FRAME IS CRAKCED IN RADIUS INBOARD END OF OUTER SKIN ATTACH POINT AT ST ATION 26. REMOVED DAMAGE, FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F TR A6WE 2007100200015 20071002 00015 2007 10 2 AMTA200700414 4 20070831 A 2310 RECEIVER BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE HF RADIO INOPERATIVE A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 552TZ 32586 LT HF INOPERATIVE. TRANSMISSION OK. RECEPTION INOPERATIVE. DATA LINK ALSO INOP. PERFORMED TROUBLESHOOTING OF LT HF SY STEM, SYSTEM TESTED OK IAW FIM 23-11-00, OK FOR SERVICE, PLACARD REMOVED. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007100200017 20071002 00017 NM 2007 10 2 AMTA200700416 1 20070902 A 4930 FUEL CONTROL BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE APU MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 323TZ 30033 DURING CREW PREFLIGHT, APU WOULD NOT START. PERFORMED FIM 49-40-00 FOR A (NO FLAME SHUTDOWN) MESSAGE SHOWN FOR APU BITE ON THE CDU. VERIFIED APU IGNITION AND STARTER OPERATION AS NORMAL. VERIFIED FUEL FLOW. REMOVED AND REPLACED FUEL CON TROL UNIT. (K) 2 L 7 2 4F 4 F RT A16WE E2GL 2007100200018 20071002 00018 2007 10 2 AMTA200700417 4 20070904 A 2565 5WD260100211 SLIDE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL L2 DOOR UNSERVICEABLE A AMTA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 11 702TZ 46912 L2 DOOR SLIDE/ AIR BOTTLE LOW PRESSURE LIGHT WILL NOT TEST. REMOVED AND REPLACED L2 DOOR SLIDE REF MM 25-61-07. SLIDE BOTTLE LOW PRESS LIGHT NOW CHECKS NORMAL. (K) 2 L 7 3 4F 4 F A22WE A23EA 2007100200020 20071002 00020 NM 2007 10 2 AMTA200700420 1 20070906 A 3150 WARNING LIGHT BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE THRUST REVERSER FALSE ACTIVATION A AMTA O OTHER N FALSE WARNING LD LANDING 1 GL 11 304TZ 30675 ON LANDING, NR 2 REVERSER LIGHT ON AND OVERHEAD REVERSE ON LIGHT ON CYCLED REV. ONCE THEN BOTH REVERSER LIGHTS STAYED O N, CYCLED 2ND TIME BOTH REV LIGHTS OUT AND NR 2 ENGINE CONTROL LIGHT CAME ON, ON SHUTDOWN ALL PERFORMED BITE CHECK OF EA U PER FIM 78-31-00-810-801. PERFORMED RESET OF EAU NO FAULTS FOUND. THEN PERFORMED EEC BITE IAW 73-21-005 NO FAULTS FO UND. RAN NR 2 ENG CHECKED FOR FAULTS NONE NOTED. (K) 2 L 7 2 4F 4 F RT A16WE E2GL 2007100200022 20071002 00022 2007 10 2 AMTA200700427 4 20070907 A 3160 DISPLAY BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT INOPERATIVE A AMTA O OTHER O OTHER CL CLIMB 1 GL 11 520AT 27976 CAPT`S CDU WENT BLANK AFTER T/O AND REMAINED BLANK. REMOVED AND REPLACED CAPT`S CDU IAW AMM 34-61-02-422-035, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2007100200023 20071002 00023 2007 10 2 AMTA200700428 4 20070908 A 3442 20414440402 DRIVE UNIT BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE RADAR UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 550TZ 32584 REMOVED AND REPLACED RADAR DRIVE UNIT IAW CHAPTER 34. OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007100200027 20071002 00027 NM 2007 10 2 ASMF200709007 1 20070922 A 3150 WARNING MESSAGE BOEING 737 737* NM CFMINT CFM567 CFM567B22 13802 NE CONFIGURATION MALFUNCTIONED W ASMF C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 23 904AM 28262 AIRCRAFT REJECTED TAKEOFF AT 90 KNOTS,TAKEOFF CONFIGURATION WARNING WAS SHOWN. AT PLATFORM, MAINTENANCE PERSONNEL PERFOR MED FMCS AND PSEU TESTS IAW MM 34-61-00 AND 32-09-10, ALL CORRECT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007100200031 20071002 00031 EU 2007 10 2 COEA0705821 1 20070821 A 5322 S53370005210 SHEAR TIE AEROSP ATR72 ATR72212 8680945 EU FUSELAGE DAMAGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FE 253 FOUND TOOLING DAMAGE ON SHEAR TIE. REPLACED. WO NR 72242 NR 200001. (K) 2 H 7 2 4T RT A53EU 2007100200033 20071002 00033 EU 2007 10 2 COEA0703821 1 20070817 A 5753 S5751211120400 GUIDE AEROSP ATR72 ATR72212 8680945 EU LT FLAP CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FE 253 FOUND LEVEL 2 CORROSION IN HEAVY CHECK. LT WING OB FLAP CAM GUIDES CORRODED. REPLACED WITH NEW GUIDES. WO NR 72244, N R 601004. (K) 2 H 7 2 4T RT A53EU 2007100200035 20071002 00035 EU 2007 10 2 COEA0701821 1 20070822 A 5751 S271120200 BRACKET AEROSP ATR72 ATR72212 8680945 EU RT OB AILERON CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FE 253 FOUND LEVEL 2 CORROSION IN HEAVY CHECK. RT WING OB AILERON PENDULUM BRACKET HAS CORROSION JUST OB OF OB FLAP HANGER. R EPLACED WITH NEW BRACKET. WO NR 72241, NR 602006. (K) 2 H 7 2 4T RT A53EU 2007100200036 20071002 00036 NM 2007 10 2 MWEA070221 1 20070919 A 7830 7150922505 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 905ME 55169 LEFT THRUST REVERSER, BOTTOM DEFLECTOR DOOR ZEE FRAME IS CRACKED ON INBOARD END AT OUTER SKIN ATTACH POINT STATION 35. REMOVED DAMAGE, FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F TR A6WE 2007100200037 20071002 00037 EU 2007 10 2 COEA0702821 1 20070823 A 5330 13S53370561200 DOUBLER AEROSP ATR72 ATR72212 8680945 EU GPS ANTENNA CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FE 253 FOUND LEVEL 2 CORROSION IN HEAVY CHECK. KLN 900 ANTENNA DOUBLER IS CORRODED AT CROWN BELOW AFT FRAME 16. REMOVED AND I NSTALLED NEW FABRICATED DOUBLER. WO NR 72242, 80014. (K) 2 H 7 2 4T RT A53EU 2007100200038 20071002 00038 NM 2007 10 2 MWEA070222 1 20070919 A 7830 7150922505 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 905ME 55169 RIGHT THRUST REVERSER, UPPER DEFLECTOR DOOR ZEE FRAME AT STATION 26 OUTBOARD SIDE IS CRACKED. REMOVED DAMAGE AND FABRIC ATED AND INSTALLED ANGLE. 2 L 7 2 4F TR A6WE 2007100200039 20071002 00039 EU 2007 10 2 COEA0701900 1 20070828 A 5311 S53372411210 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 900FX 170 CORROSION FOUND IN HEAVY CK: FLIGHT DECK FRAME 13 STRINGER 21R-14R HAS LEVEL 2 CORROSION TOP AND LOWER SIDE OF FLOORBEAM . REMOVED CORRODED FLOORBEAM FROM STR 21R TO RBL RUNOUT. INSTALLED FABRICATED FLOORBEAM AT FRAME 13 STR 21R-14R. WO N R 69312, NR 100014. (K) 2 H 7 2 4T RT A53EU 2007100200041 20071002 00041 EU 2007 10 2 COEA0702900 1 20070828 A 5310 53070205202 CREASE BEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 900FX 170 FOUND LEVEL 2 CORROSION IN HEAVY CHECK: FLIGHT DECK CREASE BEAM AT FRAME 13 LT SIDE. INSTALLED FABRICATED CREASE BEAM A NGLE AT FRAME 13. WO NR 69312, NR 100015. (K) 2 H 7 2 4T RT A53EU 2007100100127 20071001 00127 EU 2007 10 1 07FDEA04225 1 20070924 A 5510 A55171542000 SUPPORT FITTING AIRBUS 310 A310324 3930206 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FOUND CORROSION ON THS SUPPORT FITTING, STA 93, RIB3 LT. REPLACEMENT OF FITTING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100131 20071001 00131 EU 2007 10 1 07FDEA04229 1 20070924 A 5210 A52111410200 FITTING AIRBUS 310 A310324 3930206 EU ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FOUND CORROSION SPOT ON LT FWD PAX DOOR FITTING AT XP715 BETWEEN BEAMS 3 AND 5. REPAIR PERFORMED BY CUTTING-OUT THE FIT TING WEB IN ORDER TO REMOVE CORROSION AND PERFORMING HFEC INSPECTION OF THE REWORKED AREA, INSTALLING REPAIR DOUBLER WIT H MONEL RIVETS IAW EA 6-5211-92150 AND RAS/AS/0178/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100100142 20071001 00142 EU 2007 10 1 07FDEA04242 1 20070924 A 5313 A53770975200 STRINGER AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND CORROSION AT STRINGER SEGMENT P 45 LT, C 26. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100145 20071001 00145 EU 2007 10 1 07FDEA04245 1 20070924 A 5320 A53773644 FITTING AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND CORROSION AT CORNER FITTING C32 LT AND RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100150 20071001 00150 EU 2007 10 1 07FDEA04250 1 20070924 A 5414 A54612403 PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 WEARED HOLES IN LATERAL PANELS (INBOARD AND OUTBOARD), RIB 8 UPPER SPAR OF PYLON NR 1 LT. REPAIR PERFORMED BY INSTALLAT ION OF BUTTERFLY DOUBLERS ON BOTH PANELS IAW SRM 54-51-31/CONFIG 2/PB 201. 2 L 7 2 4F RT A35EU 2007100200003 20071002 00003 EU 2007 10 2 DTX2007F00000 1 20070806 A 4930 46704100 MANIFOLD BRAERO DH125 HS125700A 4230170 EU GARRTT TFE731 TFE7313R1H 29001 WP APU FUEL LEAKING E DTXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 943CE 164 257141 P84315 THE FLIGHT CREW NOTED A STRONG FUEL ODOR IN THE AFT CABIN, UPON INVESTIGATION, FUEL WAS FOUND ON THE AFT EQUIPMENT ACCES S DOOR AND UNDER THE APU. THE APU SHROUD WAS OPENED AND THE FUEL MANIFOLD WAS REMOVED AND IT WAS DISCOVERED TO HAVE A S MALL PINHOLE IN ONE OF THE MAIN FUEL LINES WHICH WAS LEAKING ONTO THE APU AND CAUSING THE FUEL ODOR. THE MANIFOLD WAS R EPLACED AND NO LEAKS WERE FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 2 4F 4 F A3EU E6WE 2007100200009 20071002 00009 NM 2007 10 2 AMTA200700433 1 20070911 A 5320 FLOOR SUPPORT BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE BS 1660-1680 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 CORROSION ON FLOOR SUPPORT AT STA 1670, RBL 57. REMOVED CORROSION SRM 53-00-51-1A, FIG 101, FOUND TO BE OUT OF LIMITS S RM 53-00-51-1A. REMOVED FLOOR SUPPORT STA 1660-1680, RBL 57, SRM 51-40-02. REPLACED FLOOR SUPPORT SRM 51-40-05 AND 51- 40-02. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007100200026 20071002 00026 NM 2007 10 2 ASMF200709006 1 20070921 A 7830 SLEEVE BOEING 737 73776Q 13845AA NM CFMINT CFM567 CFM567B22 13802 NE THRUST REVERSER DAMAGED W ASMF O OTHER O OTHER CR CRUISE 1 SW 23 997AM 30283 CAPTAIN REPORTED LIGHTNING ACTIVITY NEAR TO THE AIRCRAFT DURING FLIGHT; AT GDL PLATFORM, TECHNICAL PERSONNEL DETECTED A LIGHTNING STRIKE DAMAGE IN THE LT ENGINE THRUST REVERSER TRANSLATING SLEEVE PANEL, 10 INCHES FROM THE TRAILING EDGE OF P ANEL, WITH LOSS OF MATERIAL IN AN AREA OF 2 INCHES X 20 INCHES. DURING OVERNIGHT CHECK, THE LT ENGINE THRUST REVERSER T RANSLATING SLEEVE PANEL WAS REPAIRED IAW SRM 51-70-05 REPAIR 1 AND SRM 54-30-01, TESTED CORRECT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007100200030 20071002 00030 EA 2007 10 2 WWQ2007F00001 1 20070805 A 3297 6015778827 WIRE HARNESS CNDAIR CL600 CL6002A12 1900304 EA GE CF34 CF341A NE NLG DOWNLOCK SHORTED E WWQA O OTHER O OTHER NR NOT REPORTED 1 WP 07 39CD 3030 DURING APPROACH, THE CREW EXTENDED THE LANDING GEAR (NORMAL PROCEDURE). SEVERAL SECONDS AFTER THE GEAR EXTENSION THE NO SE LANDING GEAR DOWN AND LOCKED GREEN LIGHT EXTINGUISHED AND THE NOSE GEAR DOORS OPENED AND CLOSED. A FEW SECONDS LATER THE DOORS CYCLED AGAIN AT THAT TIME THE GREEN DOWN AND LOCKED LIGHT ILLUMINATED. THE GEAR INDICATED AND REMAINED DOWN AND LOCKED. THE AC LANDED WITH NO PROBLEMS AND THE CREW CALLED MAINTENANCE. DOM AND TECH WENT TO AC TO EVALUATE THE PR OBLEM. ONCE ON SIDE THE AC WAS JACKED FOR GEAR SWINGS AND TROUBLESHOOTING IAW THE AC MM, CHAPTER 32. FOUND THAT THE NR 2 DOWN LOCK MICRO SWITCH AND HARNESS ASSY HAD FAILED. REMOVED THE HARNESS AND SWITCH ASSY PN 601-57788-27 AND REPLACE 2 L 7 2 4F 4 F RT A21EA E15NE 2007100200034 20071002 00034 EU 2007 10 2 COEA0707900 1 20070816 A 5320 S5317400021401 STIFFENER AEROSP ATR42 ATR42320 8680930 EU BULKHEAD CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 900FX 170 LEVEL 2 CORROSION FUND IN HEAVY CK: FWD BULKHEAD STIFFENER CORRODED. REPLACED WITH NEW STIFFENER. WO NR 69313, NR 8000 09. (K) 2 H 7 2 4T RT A53EU 2007100200059 20071002 00059 EA 2007 10 2 TRAX200701372 1 20070918 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 904EV 7628 ASD EXTERIOR HANDLE CRACKED IN TWO PLACES. 2 L 7 2 4F RT A21EA 2007100200064 20071002 00064 EA 2007 10 2 TRAX200701377 1 20070920 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 681BR 7680 NR 3 AND NR 4 EMERGENCY LIGHT BATTERY PACKS INOP. 2 L 7 2 4F RT A21EA 2007100200065 20071002 00065 EA 2007 10 2 TRAX200701378 1 20070920 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 919EV 7780 FIRST THREE EMERGENCY LIGHT STRIPS ON THE FLOOR INOP. 2 L 7 2 4F RT A21EA 2007100200067 20071002 00067 EU 2007 10 2 MAC090704 1 20070901 A 5751 FITTING AEROSP AEROSP ATR42 ATR42300 8680920 EU AILERON CRACKED A MTNA K NONE O OTHER IN INSP/MAINT 1 SO 33 923FX NT1132 135 DURING INSPECTION, LEVEL 2 INTERGRANULAR CORROSION AND CRACKS WERE FOUND ON THE CENTER HINGE BEARING FITTING. THE PART NUMBERS REPLACED ARE: 576106-02 & 576106-01. REFERENCE ATR 42 CMM 5761-11 AND SRM 57-61-00. 2 H 7 2 4T RT A53EU 2007100200073 20071002 00073 NM 2007 10 2 SWAA074716 1 20070920 A 3350 147A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 220WN 32491 EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007100200077 20071002 00077 2007 10 2 SWAA074717 4 20070920 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 264LV 32521 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007100200079 20071002 00079 NM 2007 10 2 SWAA074734 1 20070920 A 2730 6545187 TORQUE TUBE BOEING 737 7373H4 1384600 NM RT ELEVATOR FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED 10Y CHECK, RIGHT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR OUTPUT TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007100200085 20071002 00085 NM 2007 10 2 SWAA074724 1 20070920 A 5315 6584176 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 707, LBL 25. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007100200092 20071002 00092 EU 2007 10 2 USA2007F00011 1 20070727 A 5300 ASNA2051DKS STRUCTURE AIRBUS A321 A321211 3930370 EU CFMINT CFM56 CFM565B32P 13008 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 177US 21354 1517 CORRODED RIVET TAILS WERE FOUND IN FUSELAGE CARGO COMPARTMENT BETWEEN FRAME 26 TO 35.8 STRINGER 38R TO 38L. APPROX 1500 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD THE PAINT FLAKING O FF THE RIVET TAILS THAT WERE CLEANED AND PRIMER AND PAINT REAPPLIED. AC WAS MFG 22, AUG, 2001. (K) 2 L 7 2 4F 4 F RT A28NM 2007100200101 20071002 00101 NM 2007 10 2 SWAA074725 1 20070920 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER 22R CRACKED AT BS 494. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007100200105 20071002 00105 NM 2007 10 2 ASAA0792061 1 20070921 A 5230 1036541 HOUSING BOEING 737 737990 NM CARGO DOOR GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 306AS 30014 AFT CARGO DOOR HOUSING GOUGED. REPAIRED IAW EA 5230 01123. 2 L 7 4 4F RT A16WE 2007100200110 20071002 00110 NM 2007 10 2 USAA920070849 1 20070921 A 5313 140N1530 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 920UW 22199 CLT - MAJOR REPAIR - C-3 CHECK, CORROSION ON STRINGER, BS 1420, S29R. REPAIRED STRINGER, BS 1420, S29R IAW B757-200 SRM 53-00-03 AND 51-40-02. 2 L 7 2 4F RT A2NM 2007100200117 20071002 00117 SO 2007 10 2 RAIA00709023 1 20070918 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 819HK 145062 PRE FLT NR 5505 - JAX - LEFTHAND OVERWING EXIT IDENTIFIER EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED EMERGENCY LIGHT. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007100200122 20071002 00122 SO 2007 10 2 RAIA00709016 1 20070914 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 817HK 145058 PRE FLT NR 5587 - STL - EMERGENCY LIGHT AT MAIN DOOR HINGE OUT. MAINTENANCE INSPECTED AND FOUND BROKEN CONNECTION. REP LACED CONNECTOR, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007100200125 20071002 00125 SO 2007 10 2 C2XA07CL083 1 20070921 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16951 145063 DURING ROUTINE MAINTENANCE THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPL ACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007100200129 20071002 00129 WP 2007 10 2 ABXA070306 1 20070807 A 5753 99575761 SKIN DOUG DC9 DC931 3022065 WP T/E FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 907AX 47203 LEFT FLAP UPPER OUTBOARD SURFACE HAD SKIN BULGING AND CUPPED RIVETS. REMOVED SEGMENT FOR REPAIR AND REINSTALLED IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 2007100200131 20071002 00131 WP 2007 10 2 ABXA070304 1 20070905 A 5313 39248101 FITTING DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 LONGERON END FITTING CRACKED ON FORWARD END LONGERON 26 RIGHT INSIDE KIDNEY AREA. REMOVED AND REPLACED LONGERON END FIT TING IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2007100200137 20071002 00137 NM 2007 10 2 CALA0700529 1 20070922 A 5330 65C38606 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70330 23460 INSPECTION FOUND A 1.5 INCH CRACK IN RIGHT FUSELAGE SKIN LAP AT STA 880, S25R. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 31. 2 L 7 2 4F RT A16WE 2007100200139 20071002 00139 NM 2007 10 2 CALA0700531 1 20070923 A 5330 6545774 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 61304 23355 INSPECTION FOUND A 2.5 INCH CRACK IN SKIN AT STA 727E, S24L. REPAIRED IAW SRM 53-00-01, REPAIR 31. 2 L 7 2 4F RT A16WE 2007100200146 20071002 00146 WP 2007 10 2 UPS07850707 1 20070904 A 5322 SHEAR TIE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 SHEAR TIE CRACKED AT STA 1080 BETWEEN L22L AND L23L. REMOVED AND REPLACED SHEAR TIE AT STA 1080 L22L AND L23L IAW SRM 51-1-20D AND DWG 3750891. 2 L 7 4 4F RT 4A25 2007100200149 20071002 00149 WP 2007 10 2 UPS07850710 1 20070822 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 WEB UNDER BAYONET FITTING IS CRACKED, L-1 DOOR. REMOVED, FABRICATED, AND INSTALLED WEB INTERCOSTAL U NDER BAYONET FITTING ON L-1 DOOR IAW DWG 5615403, AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 2007100200151 20071002 00151 WP 2007 10 2 UPS07850712 1 20070814 A 5514 FITTING DOUG DC8 DC873F 302199F WP RT HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 UPPER AFT BANANA FAIRING ATTACH FITTING CRACKED AT RIGHT HORIZ STAB. REMOVED, FABRICATED, AND INSTAL LED UPPER AFT BANANA FAIRING ATTACH FITTING ON RIGHT HORIZ STAB IAW DWG 4701959, AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 2007100200157 20071002 00157 NM 2007 10 2 USAA920070850 1 20070923 A 5313 STRINGER SPLICE BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 920UW 22199 CLT - MAJOR REPAIR - C-3 CHECK, LEVEL 2 CORROSION ON STRINGER SPLICE, BS 1460, 29R. REPLACED STRINGER SPLICE, BS 1460, S29R IAW B757-200 SRM 51-10-02. 2 L 7 2 4F RT A2NM 2007100200160 20071002 00160 NM 2007 10 2 MWEA070225 1 20070921 A 2560 P4010021 BATTERY PACK DOUG MD88 MD88 3023688 NM FLASHLIGHT DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 822ME 49759 CABIN FLIGHT ATTENDANT EMERGENCY FLASHLIGHT DOES NOT BLINK. REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F RT A6WE 2007100200161 20071002 00161 NM 2007 10 2 HNAA0700176 1 20070812 A 8097 63D4985443517 CABLE DHAV DHC8 DHC8102 2809003 NM NR 1 ENGINE DAMAGED A HNAA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 841HA 161 AFTER PUSHBACK, WITH NUMBER 2 ENGINE RUNNING, ATTEMPTED TO START NUMBER 1 ENGINE AND GOT BUSS FAULTS. TURNED OFF APU GE N. F/A THEN INDICATED A CLOUD OF SMOKE CAME OUT OF THE CEILING VENTS, LIMITED TO THE BACK OF THE AIRCRAFT, DID NOT FILL THE CABIN AND DISSIPATED VERY QUICKLY. MAINTENANCE TOWED THE AIRCRAFT BACK TO THE GATE. DID NOT NEED EMERGENCY VEHICL ES, NOT MEDICAL PERSONNEL. REMOVED AND REPLACED NEGATIVE CABLE FROM FIREWALL TO GEN, INSPECTED AND CLEANED TERMINAL AT FIREWALL, NO DAMAGE NOTED. STARTED NR 1 ENG AND RAN BLEEDS, NO DEFECTS NOTED OK FOR SERVICE. 2 H 7 2 4T RT A13NM 2007100200175 20071002 00175 WP 2007 10 2 WRLA2007095 1 20070923 A 5330 SKIN DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 303WL 46917 DURING C-5 CHECK, NR 3 AIR CONDITION COMPARTMENT DOOR WAY AFT UPPER CORNER SKIN IS CRACKED. REF NR 67328. 10-12-07 R EPAIRED REF DC10 SRM 53-50-00 FIG.3 REV.91. 2 L 7 3 4F 4 F RT A22WE E23EA 2007100200189 20071002 00189 NM 2007 10 2 MASA200700559 1 20070907 A 2611 PU90461R2 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY FAULTY A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 448YV 5173 448 LAV SMOKE DETECTOR GOES OFF RANDOMLY. MX REPLACED SMOKE DETECTOR. 2 H 7 2 4T RT A13NM 2007100200192 20071002 00192 NM 2007 10 2 KCSA07073 1 20070923 A 2120 UNKNOWN BOEING 747 747212B 1384886 NM COCKPIT ODOR A KCSA K NONE B E SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET CR CRUISE 1 GL 23 703CK 21939 SMOKE (ODOR) FROM AIR COND SYSTEM. SMOKE OBSERVED FROM FLT DECK FAN. SMOKE (ODOR) STOPPED WHEN FLT DECK FAN OFF. WHEN FLT DECK FAN ON, MADE UNUSUAL SOUND W/VIBRATION. 2 L 7 4 4F A20WE 2007100200199 20071002 00199 NM 2007 10 2 SWAA074788 1 20070924 A 2160 6938610 MIXING VALVE BOEING 737 7373Q8 1384670 NM A/C BAY FAULTY A SWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 29 663SW 23256 AIRTURN BACK/DECLARED EMERGENCY. ON DESCENT TO DHN EXPERIENCED SMOKE IN FLIGHTDECK, NO SMOKE DETECTED IN LAV OR CABIN. SMOKE DISSIPATED, SOURCE OF SMOKE NOT DETERMINED. INSPECTED AIRCRAFT, REMOVED AND REPLACED RT MIX VALVE PER MM. 2 L 7 2 4F RT A16WE 2007100200218 20071002 00218 NM 2007 10 2 KCSA071424 1 20070926 A 5340 STRINGER CLIP BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA 400 STRINGER CLIP STR 2L IS CRACKED .5 INCH. 2 L 7 4 4F RT A20WE 2007100200220 20071002 00220 EA 2007 10 2 COMA0770051 1 20070918 A 2150 GG670950091 ACM CNDAIR CL600 CL6002C10 1390015 EA A/C BAY SEIZED A COMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 642CA 10125 FLIGHT 5650 - SMOKE IN CABIN DURING TAXI. DECLARED EMERGENCY, EVACUATED PASSENGERS ON RAMP, RETURNED TO GATE. REPLACED RIGHT ACM. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007100200233 20071002 00233 EA 2007 10 2 TRAX200701385 1 20070923 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 851AS 7360 EMERGENCY LIGHT INOP RIGHT SIDE OF FUSELAGE MIDDLE LAMP ABOVE WING. 2 L 7 2 4F RT A21EA 2007100200238 20071002 00238 NM 2007 10 2 SWAA074813 1 20070926 A 3350 311500 LENS BOEING 737 7373K2 13844BA NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED SPV CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 10 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007100200241 20071002 00241 NM 2007 10 2 SWAA074812 1 20070926 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 220WN 32491 EEPLS LENS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007100200247 20071002 00247 NM 2007 10 2 SWAA074831 1 20070926 A 5553 6547450 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED 10Y CHECK, FOUND VERTICAL STABILIZER FWD ATTACH FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA. 2 L 7 2 4F RT A16WE 2007100200249 20071002 00249 NM 2007 10 2 SWAA074819 1 20070926 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007100200258 20071002 00258 NM 2007 10 2 KCSA071425 1 20070927 A 5412 BULKHEAD BOEING 747 747246F 1384850 NM NR 3 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 NR 3 PYLON STA 221.9 BULKHEAD WEB WHERE HYD LINE GOES THROUGH IS CRACKED .75 INCH. 2 L 7 4 4F RT A20WE 2007100300048 20071003 00048 CE 2007 10 3 EPUA092007A 1 20070905 A 5730 SKIN CESSNA 208 208B 2073701 CE RT WING CRACKED E EPUA K NONE O OTHER IN INSP/MAINT 1 AL 03 407GV 208B0616 DURING ROUTINE INSPECTION, DISCOVERED 4" CRACK ON UPPER RT AFT WING SKIN 18" FROM WING ROOT AT WS 53.00. DAMAGE WAS REP AIRED IAW CESNNA MM 51-75-00. AIRCRAFT WAS RETURNED TO SERVICE. 1 H 7 1 3T A37CE 2007100300050 20071003 00050 2007 10 3 AALA20071790 4 20070315 A 2565 D30654122 SLIDE BOEING 757 757223 1384957 NM L1 DOOR FAILED A AALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 21 670AA 25335 SCU - LEFT NUMBER ONE DOOR SLIDE WAS LEFT IN ARMED POSITION AND SLIDE FELL ON AIRSTAIRS WHEN DOOR OPENED. SLIDE FAILED TO DEPLOY. REPLACED LEFT NUMBER ONE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007100300051 20071003 00051 2007 10 3 AALA20071791 4 20070315 A 2565 1005042005 SLIDE DOUG DC9 DC982 3022082 WP R1 DOOR FAILED A AALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 21 7538A 49992 FLL - RIGHT NUMBER ONE DOOR SLIDE FELL TO RAMP WHEN DOOR OPENED BY CATERING. SLIDE WAS NOT ARMED. FOUND DEFECTIVE CLIP S THAT HOLD CHUTE INSIDE DOOR. SLIDE FELL OFF DOOR AND LANDED INTACT. DID NOT DEPLOY. PRESSURE INDICATOR IS DAMAGED A ND UNREADABLE. REPLACED RIGHT NUMBER ONE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007100300052 20071003 00052 EA 2007 10 3 A6WA200740500 1 20070831 A 3150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA FALSE ACTIVATION A A6WA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 31 464AW 7890 ON TAKEOFF ROLL, AIRCRAFT PULLED HARD LEFT, AT 10 KNOTS ABORTED. BRAKE TEMPS NORMAL 3, 3, 3, 3. AFTER REDUCING POWER T O IDLE RECEIVED CONFIG SPOILER MESSAGE. ENGINE POWER SETTINGS EQUAL. INSPECTED NLG TIRES AND MLG BRAKES 1 AND 2 PER AM M 32-40-00, NO FAULTS. TESTED NWS ECU PER AMM 32-50-00-240-801. NO FAULTS FOUND. FUNCTION CHECKED SPOILER CONTROL IAW AMM 27-61-00-720-801, NO FAULTS. (M) 2 L 7 2 4F RT A21EA 2007100300053 20071003 00053 EA 2007 10 3 A6WA200740491 1 20070831 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 424AW 7656 PASSENGER DOOR FORWARD SKIN IS CRACKED AT STEP 832CT. SUP - MAINTENANCCE REPAIRED IAW BSC EO 601R-52-12944. (M) 2 L 7 2 4F RT A21EA 2007100300054 20071003 00054 EA 2007 10 3 A6WA200740487 1 20070826 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 467AW 7900 FOUND AFT WEB CRACKED IN RADIUS .300 INCH LONG AT STEP 832CT ON PAX DOOR. 10-04-07 MAINTENANCE REPAIRED WEB IAW BOMB ARDIER REO 601R-52-11-702. (M) 2 L 7 2 4F RT A21EA 2007100300055 20071003 00055 EA 2007 10 3 A6WA200740486 1 20070923 A 5340 601R75262157 BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT MLG BAY CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 424AW 7656 RIGHT MLG WHEEL WELL HYDAULIC SUPPORT BRACKETS ARE CRACKED BETWEEN RBL 18 AND RBL 27. SUP - MAINTENANCE REMOVED AND REP LACED CRACKED BRACKETS AT RBL 18 TO RBL 27 IAW SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007100300056 20071003 00056 EA 2007 10 3 A6WA200740489 1 20070828 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 424AW 7656 PAX DOOR AFT STAIR SKIN CRACKED IN CORNER BETWEEN FIXED STEP AND MID STEP 832CT. SUP - MAINTENANCE REPAIRED AFT STAIR S KIN PANEL IAW REO 601R-52-11-702. (M) 2 L 7 2 4F RT A21EA 2007100300057 20071003 00057 EA 2007 10 3 A6WA200740510 1 20070907 A 5320 S61444 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FS 559 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 425AW 7663 FOUND FS 559 LBL 9 VERTICAL POST AT OUTBOARD LEG IS CRACKED AT BOTTOM RIVET. SUP - MAINTENANCE REPAIRED POST OUTBOARD L EG AT LBL 9, FS 559 IAW REO 601R-53-41-057 REV A. (M) 2 L 7 2 4F RT A21EA 2007100300058 20071003 00058 EA 2007 10 3 A6WA200740485 1 20070823 A 5340 601R75262159 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT MLG BAY CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 424AW 7656 LT MLG WHEEL WELL HYDRAULIC SUPPORT BRACKET BETWEEN LBL 18 AND LBL 27 IS CRACKED. SUP - MAINTENANCE REMOVED AND REPLACE D CRACKED BRACKET IAW CRJ 200 SRM 51-42-06 DAMAGED WAS APPROX .5 INCH LONG. (M) 2 L 7 2 4F RT A21EA 2007100300059 20071003 00059 EA 2007 10 3 A6WA200740496 1 20070904 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 202 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 425AW 7663 FS 202.75 FORWARD PRESSURE BULKHEAD IS CRACKED LT SIDE AT WL 65, APPROX LBL 28, FITTING FOR RT INBOARD BRAKE NR 3 HYD LI NE. CRACK IS APPROX 1.3 INCHES LONG. SUP - MAINTENANCE REPAIRED CRACK BY TRIMMING OUT DAMAGE AND INSTALLING FILLER AND DOUBLE IAW BSC EO 601R-53-13065. (M) 2 L 7 2 4F RT A21EA 2007100300060 20071003 00060 2007 10 3 SIMA200726801 4 20070924 A 3140 7014300901 DISPLAY EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 649PP 145234 FO DISPLAY UNIT FLICKERED OFF THEN ON THEN EMITTED STRONG ELECTRICAL ODOR WHICH WAS NOTICED BY PASSENGERS IN THE CABIN. REPLACED DISPLAY UNIT. 2 L 7 2 4T RT T00011AT 2007100300061 20071003 00061 SO 2007 10 3 SIMA200726802 1 20070924 A 2720 3603401005 ACTUATOR EMB 135 EMB135LR 3260305 SO RUDDER LEAKING A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 720AE 145279 HYDRAULIC NR 1 LOW QUANTITY LEVEL WENT FROM TOP OF YELLOW TO BOTTOM OF YELLOW IN LESS THAN 40 MINUTES. DID NOT GET A HY DRAULIC FAIL MESSAGE. REMOVED AND REPLACED NR 1 RUDDER ACTUATOR AND COMPLETED RUDDER BACKLASH CHECK. ALL LEAK AND OPER ATIONAL/FUNCTIONAL CHECKS WERE GOOD AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007100300062 20071003 00062 SO 2007 10 3 SIMA200726803 1 20070924 A 3297 CONNECTOR EMB 135 EMB135LR 3260305 SO RT MLG LOOSE A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 728AE 145328 AFTER TAKEOFF FROM RDU GEAR WOULD NOT RETRACT UNLESS OVERRIDE USED. FOUND LOOSE CONNECTOR ON RT MLG NR 2 WOW SWITCH. R ESECURED CONNECTOR AND PERFORMED EXT/RETRACTION OPS CHECKS IAW EMB AMM 32-30-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007100300063 20071003 00063 EA 2007 10 3 SIMA200726901 1 20070924 A 2150 GG670950091 ACM CNDAIR CL600 CL6002C10 1390015 EA LEFT SMOKE A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 504AE 10044 DURING CROSS BLEED START OF RIGHT ENGINE, CABIN AND COCKPIT FILLED WITH SMOKE. SMOKE CLEARED AFTER ENGINE ABORT AND SHU T OF LEFT PACK. ISSUED MEL 21-12 LT PACK. REMOVED AND REPLACED LEFT AIR CYCLE MACHINE IAW CRJ700/900 AMM 21-51-08. OP ERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007100400003 20071004 00003 EA 2007 10 4 SIMA200726904 1 20070912 A 5315 CC670341757 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 508AE 11463 10072 DURING 2C CHECK INSPECTION REVEALED STA 280 FLOORBEAM CORRODED ALONG TOP FLANGE. SPLICED IN FRAME 280, SUPPORT AND EXTE NSION MOUNTS IAW AEA EO CR-53MR AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007100400005 20071004 00005 EA 2007 10 4 A6WA200740501 1 20070831 A 2621 365000183 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY LOW A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 410AW 7992 7490 CARGO BOTTLE LOW MESSAGE. COMPLIED WITH QRH, MESSAGE CLEARED DESCENT. FIRE DEPARTMENT INSPECTION FOUND NO EVIDENCE OF HEAT. PLACED ON MEL. REMOVED AND REPLACED LT FIRE BOTTLE, OPS CHECK GOOD IAW 26-20-00 REMOVED OFF MEL. 2 L 7 2 4F RT A21EA 2007100400012 20071004 00012 NM 2007 10 4 AALA20071825 1 20070928 A 2751 SENSOR BOEING 737 737823 13844BZ NM TE FLAP INOPERATIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 921AN 29522 YYZ INFLIGHT T1562/28SEP - DURING APPROACH RECEIVED FLAP ASYMMETRY INDICATION ON TRAINING EDGE FLAP SYSTEM. LANDED WITH FLAPS UP. LANDED YYZ WITHOUT INCIDENT. REPLACED LEFT INBOARD TRAINING EDGE INPUT ASSEMBLY, FLAP SKEW DETECTION SENSOR AND FLAP SKEW DETECTION SENSOR ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007100400013 20071004 00013 WP 2007 10 4 AALA20071826 1 20070928 A 3260 833605A PROXIMITY SWITCH DOUG DC9 DC982 3022082 WP INOPERATIVE A AALA O OTHER N FALSE WARNING CR CRUISE 1 SW 21 290AA 49302 ORD INFLIGHT T1101/28SEP - DURING CLIMB CREW RECEIVED STALL THEN SLAT OVERSPEED INDICATION. ON APPROACH ANTI-SKID CIRCU IT BREAKER POPPED. LANDED ORD WITHOUT INCIDENT. REPLACED GROUND PROXIMITY BOX. SYSTEM GROUND CHECKED NORMAL OPERATION . 2 L 7 2 4F A6WE 2007100400014 20071004 00014 NM 2007 10 4 HALA0700419 1 20070927 A 5340 BRACKET BOEING 767 76733A 1385209 NM BS 246 CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 CRACK AT STATION 246 RBL 19, ON VERTICAL O/B PULLEY BRACKET, ELEVATOR PULLEY, CABLE RUN E2A AND E2B. REPLACED CRACKED E LEVATOR PULLEY BRACKET PER BOEING DRAWING 255T1241 AND 255T4410. 2 L 7 2 4F RT A1NM 2007100400015 20071004 00015 NM 2007 10 4 QXEA200701487 1 20070927 A 3620 8209074 SWITCH BOMBDR DHC8 DHC8402 1390042 NM NR 1 BLEED INOPERATIVE A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 409QX 4051 BOI - ON FLIGHT 2326, NR 1 BLEED HOT CAUTION LIGHT, RAN CHECKLIST AND REMAINS ON. MAINTENANCE REMOVED AND REPLACED NR 1 LEFT BLEED OVERTEMP SWITCH. GROUND RAN, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007100400016 20071004 00016 SO 2007 10 4 CHQA200700046 1 20070926 A 3610 14538590401 DUCT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 ENGINE CRACKED A CHQA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 294SK 145497 CAE311697 LGA TO IAD - DEPARTED LGA AT TAKEOFF POWER, AT APPROXIMATELY 300 FT AGL ENGINE NR 1 HAD AN ITT OF 950 DEGREES. WHEN ENG INE POWER WAS REDUCED, ITT LOWERED, BUT WAS STILL AROUND 900 DEGREES. AT 1,000 FT AGL, RECEIVED FIRE WARNING INDICATION FOR ENGINE NR 1. ENGINE NR 1 WAS SHUTDOWN AND THE FIRE INDICATION QUICKLY EXTINGUISHED. RETURNED TO FIELD WITH UNEVEN TFUL LANDING. MAINTENANCE INSPECTED AND RAN ENGINE AND FOUND A CRACKED BLEED DUCT NEAR THE HIGH PRESSURE SWITCH. MAINT ENANCE REPLACED THE CRACKED BLEED DUCT, PERFORMED HIGH POWER ENGINE RUNS AND OPS CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007100400019 20071004 00019 NM 2007 10 4 DLM90071253 1 20070919 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 1364 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 LT CUSP WEB CRACKED AT LIGHTENING HOLE STA 1364. REPAIRED CUSP WEB IAW MD90 SRM 51-11-01 FIG 2. 2 L 7 2 4F RT A6WE 2007100400020 20071004 00020 NM 2007 10 4 DLM90071254 1 20070918 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 924 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 FOUND LT CUSP WEB CORRODED AT STA 924. REPAIRED LEFT CUSP WEB IAW MD90 SRM 53-06-05 FIG 827D. 2 L 7 2 4F RT A6WE 2007100400024 20071004 00024 NM 2007 10 4 DLM90071258 1 20070924 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 503-522 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 RT CUSP WEB CORRODED STA 503 - 522. CUSP WEB REPLACED ON W/O 102897 2400 0227, DL 63329. 2 L 7 2 4F RT A6WE 2007100400025 20071004 00025 EA 2007 10 4 SWIA200718701 1 20070919 A 3350 AD20131A POWER SUPPLY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCHARGED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 492SW 2479 2479 7168 FLOOR EMERGENCY LIGHTING IS PARTIALLY INOP. REPLACED NR 3 ELBP WITH A SERVICEABLE UNIT IAW 33-51-17. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007100400028 20071004 00028 EA 2007 10 4 SWIA200718704 1 20070918 A 3350 POWER SUPPLY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCHARGED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 955SW 7817 FLT 5958 - EMERGENCY ROW LIGHTS INOP. REPLACED NR 2 CHARGER AND BATTERY PACK. OPS CHECK GOOD IAW 33-50-00, PN: 2013-1A SN OFF: 64829. 2 L 7 2 4F RT A21EA 2007100400029 20071004 00029 SO 2007 10 4 SWIA200718705 1 20070922 A 3350 RELAY EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS FAULTY A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 227SW 120304 FLT 5580 - EMERGENCY LIGHTS CAME ON WHEN SWITCH IS PLACED IN THE OFF POSITION. REPLACED THE EMERGENCY ARM RELAY K0201. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007100400030 20071004 00030 SO 2007 10 4 SWIA200718706 1 20070921 A 2121 BLOWER EMB 120 EMB120ER 3260203 SO RT A/C PACK SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 290SW 120317 FLT 5609 - RIGHT PACK PRODUCED SMOKE IN CABIN. REPLACED GROUND COOLING FAN RCCB W/SERVICEABLE UNIT. OPS CHECK GOOD, PN : EVAC2322C23, SN OFF: 94. 2 L 7 2 4T RT A31SO 2007100400031 20071004 00031 EA 2007 10 4 SWIA200718707 1 20070921 A 3220 TORQUE LINK CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING DISCONNECTED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 927SW 7693 AFTER TAKEOFF, RECEIVED A GEAR DISAGREE, NOSE WHEEL STEERING INOP, AND WOW INPUT. DIVERTED TO SFO, FLIGHT NR 6507. CON NECTED NOSE GEAR TORQUE LINKS AND PERFORMED A VISUAL INSPECTION. REPLACED BOTH NOSE TIRES AND SWUNG GEAR SEVERAL TIMES. ALL OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007100400035 20071004 00035 SO 2007 10 4 SWIA200718711 1 20070905 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS BROKEN A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 284YV 120284 FLT 5415 - EMERGENCY LIGHTS ON FLOOR LIGHTING STRIP ARE INOP. REPAIRED BROKEN WIRE ON FLOOR LIGHTING STRIP. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007100400038 20071004 00038 NE 2007 10 4 AALA20071824 2 20070928 A 7320 LINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 1 ENG FUEL BROKEN A AALA E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING K A J FLUID LOSS FLAME/FIRE WARNING INDICATION CL CLIMB 1 SW 21 454AA 49559 725872 STL INFLIGHT T1400/28SEP - NR 1 ENGINE FIRE IN FLIGHT. LOST BOTH SYS HYDRAULICS. RETURNED TO STL AND LANDED WITHOUT IN JURIES. FIRE TEAM MET FLT UPON LANDING AND FOAMED BOTH ENGINES. PASSENGERS DEPLANED VIA FORWARD LEFT DOOR USING STAIRS . SINGLE ENGINE TIME 20 MINUTES. 10-16-07 AIRCRAFT OUT OF SERVICE FOR EVALUATION. AIRCRAFT UNDER CONTROL OF NTSB. I NITIAL FINDING IS MAIN FUEL LINE FLEX HOSE BROKE. BOTH ENGINES HAVE BEEN REMOVED. SIGNIFICANT PYLON DAMAGE. UNABLE TO DETERMINE COURSE OF ACTION FOR AIRCRAFT AT THIS TIME. (SUPP CLOSED) 2 L 7 2 4F 4 F A6WE E9NE 2007100400041 20071004 00041 EA 2007 10 4 A6WA200740498 1 20070904 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 202 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 425AW 7663 FS 202.75 FORWARD PRESSURE BULKHEAD IS CRACKED LT SIDE AT WL 65, APPROX LBL 28, FITTING FOR RT INBOARD BRAKE NR 3 HYD LI NE. CRACK IS APPROX 1.3 INCH LONG. (M) 2 L 7 2 4F RT A21EA 2007100400042 20071004 00042 EA 2007 10 4 A6WA200740508 1 20070907 A 5340 601R3111357 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 425AW 7663 FOUND FS 280 LBL 9 OUTBOARD CLIP CRACKED. SUP - MAINTENANCE REPLACED CLIP IAW SRM 51-42-13, 51-42-21 AND BSC SRM 601R-5 7-0057A. (M) 2 L 7 2 4F RT A21EA 2007100400043 20071004 00043 EA 2007 10 4 QXEA200701497 1 20070929 A 2150 GG670950033 CONTROL VALVE CNDAIR CL600 CL6002C10 1390015 EA LT A/C PACK MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 604QX * 2884 10019 BOI - FLIGHT 2573, LEFT PACK CAUTION MESSAGE ON TAXI. RETURNED TO THE GATE. MAINTENANCE PLACED THE SYSTEM ON MEL 21-51 -1A. MAINTENANCE REPLACED THE FLOW CONTROL VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007100400044 20071004 00044 EA 2007 10 4 QXEA200701498 1 20070930 A 5242 H34455 HANDLE CNDAIR CL600 CL6002C10 1390015 EA E/E BAY DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 PDX - AVIONICS BAY DOOR HANDLE CRACKED. MAINTENANCE REPLACED THE HANDLE ASSEMBLY. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007100400049 20071004 00049 NM 2007 10 4 DL76G071262 1 20070925 A 5315 AND101331202 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 654+88 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 156DL 25354 0 FLOORBEAM CORRODED. REMOVED AND REPLACED FLOORBEAM UPPER CHORD PER SRM 53-0051D. 2 L 7 2 4F RT A1NM 2007100400050 20071004 00050 NM 2007 10 4 DL76G071263 1 20070925 A 5315 BAC1505100547 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 654 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 156DL 25354 FLOORBEAM CORRODED. REMOVED AND REPLACED FLOORBEAM UPPER CHORD PER SRM 53-00-51D. 2 L 7 2 4F RT A1NM 2007100400052 20071004 00052 NM 2007 10 4 DLM90071265 1 20070925 A 5330 5936007 SKIN DOUG MD90 MD9030 3023690 NM BS 1310-1330 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 RT FUSELAGE SKIN 4 FEET AFT OF C-3 DOOR HAS SCRATCH THAT IS OUT OF LIMITS. REPAIRED SKIN WITH EXTERNAL DOUBLER IAW MD90 SRM 53-04D FIG 12B AT FS 1310 TO 1330 AND L-21R TO L23R. 2 L 7 2 4F RT A6WE 2007100400053 20071004 00053 NM 2007 10 4 DLM90071266 1 20070925 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 655 - 674 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 SEAT TRACK AT RBL 54 CORRODED OUT OF LIMITS, STA 655 - 674. REPAIRED SEAT TRACK IAW MD90 SRM53-40-01 VOL 1 FIG 6. 2 L 7 2 4F RT A6WE 2007100400054 20071004 00054 NM 2007 10 4 DLM90071267 1 20070924 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 826-845 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 SEAT TRACK AT RBL 54 STA 826-845 CORRODED OUT OF LIMITS. REPAIRED SEAT TRACK IAW MD90 SRM 53-40-1 VOL 1 FIG 9. 2 L 7 2 4F RT A6WE 2007100400055 20071004 00055 NM 2007 10 4 DLM90071268 1 20070924 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 1328 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 SEAT TRACK AT LBL54 STA 1328 IS CORRODED OUT OF LIMITS. REPAIRED SEAT TRACK IAW MD90 SRM 53-40-01 VOL1 FIG 6. 2 L 7 2 4F RT A6WE 2007100400057 20071004 00057 NM 2007 10 4 QXEA200701485 1 20070925 A 4970 APU BOMBDR DHC8 DHC8402 1390042 NM INOPERATIVE A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 411QX 4055 SEA - ON FLIGHT 2475, RETURNED TO GATE, WITH APU OFF ELECTRIC PAGE ON MFD SHOWS INTERM LOAD OF UP TO 13. PLACED ON MEL. 10-18-07 MAINTENANCE REMOVED AND REPLACED APU DC STARTER/GENERATOR PER Q400 AMM TASK 24-33-01-000-801 AND 24-33-0 1-400-801. OPS CHECK GOOD. NO LEAKS. NOTED APU LOAD SHOWS NO LOAD WITH APU OFF. THIS CLEARS MEL. AIRCRAFT RETURNED TO SE RVICE. 2 H 7 2 4T RT A13NM 2007100400058 20071004 00058 NM 2007 10 4 QXEA200701502 1 20070928 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM DE ICE SYS FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 427QX 4156 SEA - ON FLIGHT 2268, DEICE PRESSURE CAUTION LIGHT ILLUMINATED. RAN CHECKLIST AND NOTED DECREASE IN PRESSURE AND THE NR 2 INTAKE BOOT LIGHT DID NOT ILLUMINATE DURING CYCLE. MAINTENANCE VISUALLY INSPECTED AIRFRAME BOOTS AND INTAKE BOOTS FO R DEFECTS. NONE FOUND. RAN ENGINES AND OPERATED DEICE SYSTEM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007100400059 20071004 00059 NM 2007 10 4 QXEA200701503 1 20070911 A 3231 DOOR BOMBDR DHC8 DHC8402 1390042 NM MLG MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 NM 09 425QX 4039 PDX - MAIN LANDING GEAR DOOR REMAINED OPEN AFTER GEAR RETRACTION AND ON APPROACH TO PDX. MAIN LANDING GEAR DID NOT EXTE ND ON RETRACTION. PERFORMED ALT EXT AND ALL GEAR INDICATED GREEN PRIMARY AND ALT INDICATION. THIS SDR IS LEFT OPEN DUE TO NO PAPERWORK AS OF 9/11/07. 2 H 7 2 4T RT A13NM 2007100400060 20071004 00060 NM 2007 10 4 QXEA200701500 1 20070928 A 3010 4100S01806 TMU BOMBDR DHC8 DHC8402 1390042 NM INOPERATIVE A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 424QX 1211 1211 4006 SEA - ON FLIGHT 2394, ON DESCENT, IN ICING CONDITIONS. THE DEICE PRESSURE CAUTION LIGHT ILLUMINATED. CAUTION LIGHT REM AINED ILLUMINATED AFTER THE CHECKLIST WAS RUN. MAINTENANCE DUPLICATED FAULT. INTERROGATED CDS FOR FAULTS. TMU FAIL ME SSAGE. REMOVED AND REPLACED TMU. FUNCTIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007100400061 20071004 00061 EA 2007 10 4 A6WA200740499 1 20070904 A 5320 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 425AW 7663 EXTERNAL POWER RECEPTACLE SUPPORT BRACKET, P/N 600-33283-33, IS CRACKED AT RECEPTACLE FORWARD OUTBOARD ATTACH MEDT BOLT HOLE. CRACK IS APPROX .6 INCHES LONG. (M) 2 L 7 2 4F RT A21EA 2007100400062 20071004 00062 EA 2007 10 4 A6WA200740504 1 20070905 A 5340 601R3111358 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 422AW 7341 RIGHT OUTBOARD 280 CLIP IS CRACKED APPROX .25 INCH LONG. SUP - MAINTENANCE REMOVED CRACKED CLIP AND INSTALLED A NEW CLI P, P/N 601R31113-58 IAW BSC STANDARD REPAIR 601R-53-0057A AND CRJ SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007100400063 20071004 00063 EA 2007 10 4 A6WA200740507 1 20070907 A 5340 601R3111357 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 425AW 7663 FOUND FS 280 RBL 9 INBOARD CLIP CRACKED. SUP - MAINTENANCE REPLACED CLIP IAW SRM 51-42-06 AND 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007100400064 20071004 00064 EA 2007 10 4 A6WA200740538 1 20070911 A 5753 SKIN CNDAIR CL600 CL6002B19 1900309 EA TE FLAP DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 422AW 7341 LT INBOARD FLAP HAS DENT MEASURING 2 INCHES LONG BY 2 INCHES WIDE AND .050 INCHES DEEP LOCATED 24 INCHES FROM INBOARD ED GE OF FLAP AND .500 INCH FROM TRAILING EDGE, LOWER SKIN. MAINTENANCE CUT AWAY DAMAGED SECTION OF SKIN AND INSTALLED NON -FLUSH REPAIR DOUBLER IAW CRJ SRM 57-52-00, REPAIR NR 3. (M) 2 L 7 2 4F RT A21EA 2007100400068 20071004 00068 NM 2007 10 4 DL76G071272 1 20070927 A 3210 SPRING BOEING 767 767332 1382001 NM RT MLG MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 16065 30199 R MLG JURY BRACE SPRING MISSING. REPLACED RT MLG JURY BRACE SPRING PER MM. 2 L 7 2 4F RT A1NM 2007100400069 20071004 00069 NM 2007 10 4 AALA20071805 1 20070925 A 3350 LIGHT BOEING 757 7572Q8 1384972 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 712TW 27624 DFW - EMERGENCY LIGHT AT SEAT ROW 11 BULLNOSE INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 11 B ULLNOSE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007100400072 20071004 00072 NM 2007 10 4 AALA20071808 1 20070925 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 794AN 30256 JFK - EMERGENCY LIGHT AT SEAT ROW 35G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 35G. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007100400076 20071004 00076 WP 2007 10 4 AALA20071814 1 20070926 A 3350 OL1098BPEGPL BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 465A 49595 LAX - EMERGENCY LIGHT AT SEAT 10D MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F A6WE 2007100400079 20071004 00079 NM 2007 10 4 AALA20071811 1 20070926 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 772AN 29580 NRT - EMERGENCY LIGHT AT FORWARD RIGHT G3 GALLEY INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FORWARD RI GHT G3 GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007100400080 20071004 00080 EA 2007 10 4 A6WA200740495 1 20070804 A 5312 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA BULKHEAD CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 422AW 7341 THE STIFFENER POST AT RBL 9 ON THE AFT FACE OF THE BULKHEAD AT FS 559 IS CRACKED ON THE INBOARD AND OUTBOARD SIDES APPRO X .5 INCH LONG AT THE LOWER RIVETS. SUP - MAINTENANCE PERFORMED MAJOR REPAIR TO STIFFENER POST AT BULKHEAD FS 559 AT RB L 9 IAW CRJ 200 SRM 51-42-06 AND BOMBARDIER REO 601R-53-41-057. (M) 2 L 7 2 4F RT A21EA 2007100400083 20071004 00083 EA 2007 10 4 A6WA200740493 1 20070831 A 5230 601R35050109 ANGLE CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 424AW 7656 FOUND CARGO DOOR SUPPORT BEAM LOWER ANGLE TO REAR PRESSURE BULKHEAD CRACKED. SUP - REPLACED ANGLE IAW SRM 51-40-11 AND 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007100400085 20071004 00085 EU 2007 10 4 MALA070122 1 20070930 A 3397 TERMINAL SAAB SF340 340B 7860101 EU EMERGENCY LIGHT BROKEN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 407XJ 340B407 FLOOR PROX EMERGENCY LIGHT STRIP 42LN COMING LOOSE AND WIRE TERMINALS BROKEN OFF. REPLACED LIGHT STRIP WITH NEW UNIT PN 6636-2 IAW SAAB AMM 33-50-02. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2007100400086 20071004 00086 EA 2007 10 4 A6WA200740534 1 20070901 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 424AW 7656 REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS AN INDICATION NOTED APPROX .3 INCHES IN LENG TH FAILED NDT. MAINTENANCE REWORKED LINTEL INSTALLED BY CUTTING AWAY DAMAGED SECTION OF WEB AND INSTALLED REPAIR DOUBLE R AND ANGLE IAW BOMBARDIER REO 601R-53-61-1230 REV D. (M) 2 L 7 2 4F RT A21EA 2007100400094 20071004 00094 EU 2007 10 4 07FDEA04154 1 20070921 A 5330 A53611171 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 EXISTING FLUSH REPAIR ON SKIN BETWEEN FRAME 2-3 AD, CAUSED BY A FLIGHT TEST INSTALLATION CONFORM TO DRW A536-11822, GO T IN CONFLICTS WITH PTOF CONVERSION. REPAIR MODIFIED WITH A THIRD FASTENER ROW THROUGH ALL LAYERS CONFORM TO REPAIR DRW A536-11822 IAW. EA 6-5311-82922 AND RAS/DABRE/7005422/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100400096 20071004 00096 EU 2007 10 4 07FDEA04156 1 20070921 A 5320 A53778329 PLATE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORRODED SHEAR PLATE BETWEEN FRAME 36-37 LT, STRG 44. REPLACEMENT OF SHEAR PLATE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100400098 20071004 00098 EU 2007 10 4 07FDEA04160 1 20070921 A 5330 A53778160 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 DAMAGES ON SKIN PANEL AT FRAME 33 BETWEEN STRG 38-39 RT. REPAIR PERFORMED BY REWORK DAMAGES TO A SMOOTH CONTOUR. MINIM UM THICKNESS FOLLOWING REWORK IS 1.37MM, NDT INSPECTION FOR CRACK FREE CONDITION AND ENLARGE THE INNER STRAP TO ACT AS A REPAIR DOUBLER IAW DD-0378007 ISSUE A, APPROVED BY EA 6-5314-92144 AND RAS/DABRE/7005386/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100400099 20071004 00099 WP 2007 10 4 07FDEA04161 1 20070921 A 5730 ARC19534 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 600 LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 RT WING UPPER SURFACE OUTBD FLAP FOUND 180 EA LOOSE RIVETS ON SKIN. REPAIRED EFFECTED AREAS IAW SRM 57-20-00 VOL I FIG 11 AND WORK IN CONJUNCTION OF NRC N00468. 2 L 7 3 4F A22WE 2007100400100 20071004 00100 EU 2007 10 4 07FDEA04256 1 20070924 A 5310 A53612180000 WINDOW FRAME AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 FOUND CORROSION AT LT SLIDING WINDOW IN 2 AREAS REPAIR PERFORMED BY BLEND OUT THE CORROSION AND NDT FOR CRACK FREE IAW E A 6-5612-112518 AND RAS 054295/005/2007. 2 L 7 2 4F RT A35EU 2007100400104 20071004 00104 EU 2007 10 4 07FDEA04260 1 20070924 A 5320 A53611111220 WEB AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 CRACKED WEB BETWEEN FRAME 16A-18, Y 2462, FLOOR STRUCTURE SECTION 12. REPLACEMENT OF WEB IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100400105 20071004 00105 NM 2007 10 4 07FDEA04261 1 20070924 A 5420 691447614 ANGLE BOEING 727 727227 1384078 NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 NR 2 ENG INLET DUCT HOUSING FRAME-TO-VERTICAL STAB LEADING EDGE ATTACH CLIP IS CRACKED. LOCATED ON LT SIDE STA 1233. R EMOVED CRACKED ATTACHED BRACKET, FABRICATED NEW ATTACH CLIP AND INSTALLED. REF BOEING DOCUMENT NR 69-14476 AND SRM 51-3 0-02. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007100400106 20071004 00106 NM 2007 10 4 AALA20071812 1 20070926 A 3350 3020421 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 601AN 27052 MIA - EMERGENCY LIGHT AT LEFT AFT OVERWING EXIT DOOR INOPERATIVE. REPLACED LAMP FORE EMERGENCY LIGHT AT LEFT AFT OVERWI NG EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007100400107 20071004 00107 EU 2007 10 4 07FDEA04163 1 20070921 A 5310 A52271017201 BEAM AIRBUS 310 A310324 3930206 EU ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 HEAVY CORROSION ON BEAM NR 5 AT EMERGENCY EXIT DOOR RT, ZONE 844. REPLACEMENT OF BEAM NR 5 IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100400108 20071004 00108 EU 2007 10 4 07FDEA04164 1 20070921 A 5311 A52271025203 FRAME AIRBUS 310 A310324 3930206 EU ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 HEAVY CORROSION ON FRAME SEGMENT AT EMERGENCY EXIT DOOT RT, BETWEEN BEAM 4-5. REPLACEMENT OF FRAME SEGMENT IAW SRM 51-7 2-10. 2 L 7 2 4F RT A35EU 2007100400110 20071004 00110 EU 2007 10 4 07FDEA04166 1 20070824 A 5753 SKIN AIRBUS 310 A310222 3930315 EU ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 RT WING INBD FLAP T/E SKIN W/DEBONDS (UPPER SKIN RIB 14-15) REPAIRED IAW SRM 57-52-12. 2 L 7 2 4F RT A35EU 2007100400111 20071004 00111 WP 2007 10 4 07FDEA04167 1 20070921 A 5320 ABA720323 WEB DOUG DC10 DC1010F 3022111 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 PERFORMED INSPECTION AFTER REMOVAL FLOOR PANEL IN COCKPIT WITH OAN J/C SP10530208-2JR, FOUND SEVERE CORROSION WITH EXF OLIATION ON MEMBRANE AND CRACK 2" LONG. REPAIRED WEB IAW SRM 53-00-01 VOL I FIG 10. 2 L 7 3 4F A22WE 2007100400113 20071004 00113 WP 2007 10 4 07FDEA04169 1 20070921 A 5730 ARC1210 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 LT WING INBD AILERON CORROSION BOTTOM UPPER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 86 VOL I. 2 L 7 3 4F A22WE 2007100400115 20071004 00115 EU 2007 10 4 07FDEA04133 1 20070920 A 5740 A57112205 FITTING AIRBUS 300 A300B4622 3930401 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 CRACKS FOUND AT FRAME 47 INTERNAL FITTING LT HOLE NR E (1MM) IN REAR SPAR, HOLE NR G (2MM) IN CORNER FITTING, HOLE NR I (2MM) IN FWD FITTING, HOLE NR N (2MM) IN FWD FITTING, REPAIR PERFORMED BY OVERSIZING THE HOLES (E,G,N) UNTIL CRACK REMOV AL AND CUT OUT THE EXTERNAL FITTING PER SB 57-6049 ON HOLE NR I AND INSTALL A CONICAL WASHER IAW EA 6-5710-73899 AND RAS /AS/310/2003 ISS A. 2 L 7 2 4F RT A35EU 2007100400119 20071004 00119 EU 2007 10 4 07FDEA04173 1 20070921 A 5320 A53981113200 PLATE AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 HEAVY CORROSION ON SHEAR PLATE BETWEEN FRAME 79-80, STRG 26 RT. REPLACEMENT OF CONN SEGMENT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100400120 20071004 00120 EU 2007 10 4 07FDEA04174 1 20070921 A 5313 A53778392 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORROSION ON STRINGER 51 LT, BETWEEN FRAME 37-38.1. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007100400121 20071004 00121 EU 2007 10 4 07FDEA04175 1 20070921 A 5313 A53778392 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORROSION ON STRINGER 52 LT, BETWEEN FRAME 35-38.1. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007100400123 20071004 00123 EU 2007 10 4 07FDEA04177 1 20070921 A 5311 A53989155 FLANGE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORROSION ON OUTER FLANGE AT FRAME 91, BETWEEN STRG 45 LT-AD. REPLACEMENT OF OUTER FLANGE BETWEEN STRG 37 RT-37 LT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100400127 20071004 00127 EU 2007 10 4 07FDEA04182 1 20070921 A 5310 A53988624205 CROSSBEAM AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORROSION ON CROSS STRUT AT FRAME 86, STRG 15 RT FRONT SIDE. REPLACEMENT OF CROSS STRUT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100400129 20071004 00129 CE 2007 10 4 RU3A0709 1 20070925 A 3610 MANIFOLD LEAR 60 60LEAR 5170707 CE RT BLEED AIR LEAKING E RU3A H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 15 58 057 IFR EN ROUTE, FL190, NOTICED "HOT AIR" TYPE OF ODOR. NO SMOKE OBSERVED. SHORTLY AFTER ODOR "BLEED AIR R" ANNUNCIATOR L IGHT ILLUMINATED. INITIATED EMERGENCY PROCEDURE (EP) "BLEED AIR LIGHT". AFTER COMPLETION OF "BLEED AIR LIGHT" CHECKLIS T, INCLUDING RIGHT BLEED SHUT-OFF AND RIGHT ENGINE THRUST REDUCTION, BLEED AIR LIGHT EXTINGUISHED. REQUESTED IMMEDIATE RETURN TO KACY, BASED ON CONTINUED ODOR AND CONCERN THAT LEAK MAY NOT BE CONTAINED. LANDING WAS UNEVENTFUL WITH LOW TOU CHDOWN G'S AND MINIMAL BRAKE USAGE. GROUND CREW FOUND RT BLEED AIR MANIFOLD LOCATED AT LOWER AFT END OF ENGINE LEAKING. 2 L 7 2 4F RT A10CE 2007100400133 20071004 00133 EU 2007 10 4 07FDEA04292 1 20070926 A 5320 A53970875201 PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 FOUND GOUGE AS CAUSED BY INCORRECT EQUIPMENT FASTENER INSTALLATION AT TORSION BOX CROSS SHEET (PANEL) BETWEEN FRAME 56-5 6A, STGR 14-16 RT, EMERGENCY EXIT DOOR SURROUND PANEL. REPAIR PERFORMED BY SMOOTH BLEND OUT, HFEC INSPECTION FOR CRACK FREE CONDITION AND FLAP PEENING IAW EA 6-5316-82928 AND RAS/DATLS/0002657/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100400135 20071004 00135 EU 2007 10 4 07FDEA04294 1 20070926 A 5310 A53610633226 FAILSAFE AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 FOUND EXFOLIATION CORROSION AT LT FWD PAX DOOR FAIL/SAFE RING (FWD LOWER CORNER) BETWEEN FRAME 13-14, STRINGER 25-28 L T. REPAIR PERFORMED BY BLEND OUT CORROSION AND NDT INSPECTION FOR ANY REMAINING CORROSION IAW EA 6-5312-82930 AND RAS/A S/182/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100400136 20071004 00136 EU 2007 10 4 07FDEA04295 1 20070926 A 5310 A53611658201 FAILSAFE AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 FOUND CORROSION AT RT FWD PAX DOOR FAIL/SAFE RING (AFT LOWER CORNER) BETWEEN FRAME 14C-17, STGR 26-27 RT. REPAIR PERFOR MED BY BLEND OUT CORROSION AND NDT INSPECTION FOR ANY REMAINING CORROSION IAW EA 6-5312-82932 AND RAS/AS/185/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007030100012 20070301 00012 NM 2007 3 1 CALA0700083 1 20070222 A 5311 6546554 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 INSPECTION FOUND AFT CARGO COMPARTMENT FLOOR FRAME CORRODED AT STA 847 BETWEEN STRINGERS 27L AND 27R, LBL 8 TO RBL 8. T HE CORRODED SECTION OF FLOOR FRAME WAS REMOVED AT FLOOR FRAME ATTACH AND A SHEAR TIE REPAIR WAS INSTALLED IAW SRM 53-00- 07. 2 L 7 2 4F RT A16WE 2007030100017 20070301 00017 EA 2007 3 1 COMA0760209 1 20070223 A 2740 3094334 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A COMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 958CA 7111 FLIGHT 5106 - DURING CLIMBOUT OF RDU PITCH TRIM ACTIVATED UNCOMMANDED INTERMITTENTLY, FLIGHT RETURNED TO RDU. REPLACED THE CAPTAIN'S PITCH TRIM SWITCH. 2 L 7 2 4F RT A21EA 2007100900170 20071009 00170 NM 2007 10 9 SWAA074903 1 20071002 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 400 S14L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007100900177 20071009 00177 EA 2007 10 9 TRAX200701397 1 20070924 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 751EV 10163 FWD EMERGENCY LIGHT ABOVE ROW TWO IS INOP, CABIN EMERGENCY LIGHTS - CEILING LEVEL FLOODLIGHTS. 2 L 7 2 4F RT A21EA 2007100900197 20071009 00197 EA 2007 10 9 TRAX200701411 1 20070926 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 880AS 7606 TWO SECTIONS IN THE PASSENGER CABIN OF THE EMERGENCY LIGHT IS BURNED OUT. 2 L 7 2 4F RT A21EA 2007100900206 20071009 00206 NM 2007 10 9 USAA920070867 1 20070925 A 5340 65516989 STRINGER SPLICE BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NON-ROUTINE 6504931, CRACKED STRINGER SPLICE, BS 907, S4L. REPLACED STRINGER SPLICE C HANNEL, BS 907, S4L IAW BOEING 737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007100900207 20071009 00207 NM 2007 10 9 USAA920070868 1 20070928 A 5313 65596644 STRINGER SPLICE BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6504930, CRACKED STRINGER SPLICE, BS 360, S4L. REPLACED STRINGER SPLICE CHANNEL, B S 360, S4L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007100900209 20071009 00209 NM 2007 10 9 USAA920070871 1 20070928 A 5320 143N515726 INTERCOSTAL BOEING 757 7572S7 1384962 NM ZONE 200 - FUSEL CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 903AW 23323 MCN - MAJOR REPAIR - C-12 CHECK - NR 5976769, CRACKED INTERCOSTAL CLIP, BS 859 - BS 879, BL 0, WL 208. REPLACED INTERCO STAL CLIP, BS 859 - BS 879, BL 0, WL 208 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007100900211 20071009 00211 EU 2007 10 9 USAA920070873 1 20070928 A 5320 D5348004820200 SILL AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 631AW 077 MCN - MAJOR REPAIR - C-06 CHECK - NR 5966749, CORROSION ON THE L2 DOOR CUTOUT LOWER SILL SHAPE SILL FITTING, BS 3158 - B S 3257, S23L. REPLACED THE L2 DOOR CUTOUT LOWER SILL SHAPE SILL FITTING, BS 3158 - BS 3257, S23L IAW A320 SRM 51-42-11. 2 L 7 2 4F RT A28NM 2007101000001 20071010 00001 SO 2007 10 10 RAIA007100002 1 20071003 A 2720 CONTROL SYSTEM EMB 145 EMB145LR 3260212 SO RUDDER MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 811HK 145256 FLT NR 5553 - STL - RUDDER SYSTEM 2 INOP. MAINTENANCE OPS CHECK RUDDER SYSTEM, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007101000002 20071010 00002 NM 2007 10 10 USAA920070905 1 20071005 A 5330 6545776 SKIN BOEING 737 7373B7 1384580 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 23381 CLT - MAJOR REPAIR - C-4 CHECK, CRACKED FUSELAGE SKIN, BS 727E - BS 747, S25R. REPAIRED FUSELAGE SKIN, BS 727E - BS 747 , S25R IAW B737-300 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2007101000003 20071010 00003 EU 2007 10 10 USAA920070906 1 20070920 A 5522 D55281242000 SKIN AIRBUS 320 A320231 3930325 EU ZONE 300 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 644AW 317 SAL - MAJOR REPAIR - C-04 CHECK - NR 5975503, LEFT ELEVATOR LEADING EDGE CRACKED, ELEVATOR RIB STATION 2 - ELEVATOR RIB STATION 3. REPAIRED LEFT ELEVATOR LEADING EDGE ELEVATOR RIB STATION 2 - ELEVATOR RIB STATION 3 IAW A320 SRM 55-21-11. 2 L 7 2 4F RT A28NM 2007101000006 20071010 00006 NM 2007 10 10 HNAA0700183 1 20071003 A 5755 85710559001 BRACKET DHAV DHC8 DHC8102 2809003 NM SPOILER ACTUATOR CRACKED A HNAA K NONE Z SIGNIFICANT FAILURE REPORT IN INSP/MAINT 1 EA 07 805EX 228 DURING HEAVY MAINTENANCE THE MOUNTING BRACKET FOR THE RIGHT OUTBOARD FLIGHT SPOILER ACTUATOR CRACKED AROUND BOTTOM CIRCU MFERENCE. REMOVED AND REPLACED BRACKET (P/N 85710559-001). 2 H 7 2 4T RT A13NM 2007101000007 20071010 00007 NM 2007 10 10 KCSA071438 1 20071004 A 5312 ANGLE BOEING 747 7472B4B 138481B NM BS 1700 BULKHEAD CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 AFT BILGE BULKHEAD SUPPORT ANGLE IS CRACKED .5 INCH AT STA 1700, BELOW FLOOR LINE, RBL 18. 2 L 7 4 4F RT A20WE 2007101000008 20071010 00008 EA 2007 10 10 TRAX200701458 1 20071001 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 FLIGHT ATTENDANT REPORTS, PAX DOOR DIFFICULT OPEN FROM INSIDE. 2 L 7 2 4F RT A21EA 2007101000009 20071010 00009 EA 2007 10 10 TRAX200701459 1 20071002 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 908EV 7654 SECOND FROM FRONT LEFT EXTERNAL EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007101000012 20071010 00012 EA 2007 10 10 TRAX200701417 1 20070927 A 3350 CHARGER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 923EV 7826 NR 2 EMERGENCY LIGHT BATTERY CHARGER INOP. 2 L 7 2 4F RT A21EA 2007101000016 20071010 00016 EU 2007 10 10 YENA2007088 1 20071002 A 2133 VTF300B00 OUTFLOW VALVE AIRBUS 320 A320232 3930326 EU CABIN PRESSURE FAILED A YENA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 546JB 21581 1827 ECAM VENT SKIN VALVE FAULT SHORTLY AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE. CYCLED TO BURN FUEL AND AIRCRAFT LANDE D AT 141,000 LBS. PERFORMED BITE TEST OF AEVC. PFR & BITE SHOWED SKIN AIR OUTLET VALVE FAULT. REMOVED AND REPLACED SK IN AIR VALVE (OUTLET) PER AMM 21-26-53-04, NO FURTHER FAULTS, OPS CHECK NORMAL. 2 L 7 2 4F RT A28NM 2007101000017 20071010 00017 NM 2007 10 10 KCSA071439 1 20071004 A 5320 REVEAL BOEING 747 7472B4B 138481B NM BS 441 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 MAIN DECK R1 DOOR FORWARD REVEAL IS CRACKED 4 INCHES AT STA, 441, RBL 107 WL 265. 2 L 7 4 4F RT A20WE 2007101000018 20071010 00018 EU 2007 10 10 YENA2007087 1 20071001 A 3350 340022 BATTERY PACK EMB ERJ190 ERJ190100IGW 3260408 EU EMERGENCY LIGHTS FAILED A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 197JB 4300 19000020 LEFT FWD OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK NR 4, OPS CHECK OF EMERGENCY LIGHTS GOOD REF AMM 33-50-01-04. 2 L 7 2 4F RT A57NM 2007101000021 20071010 00021 NM 2007 10 10 USAA920070882 1 20071002 A 5320 6517684 INTERCOSTAL BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT - MAJOR REPAIR - FPBH INSPECTION - INTERCOSTAL WEB ANGLE .25 CRACKED AT BS 294, S16L. REPLACED INTERCOSTAL WEB ANGL E BS 294, S16L IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007101000025 20071010 00025 NM 2007 10 10 ZZDA2007274 1 20070927 A 2497 5314A2103 FEEDER CABLE BOEING 737 73776N 13844CH NM NR 1 GENERATOR ARCED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 273AT 32662 ON ROUTINE INSPECTION FOUND NR 1 GENERATOR FEEDER CABLE ARCED, FAN COWL CENTER FITTING HAS BURN MARKS FROM ARCING. REMO VED AND REPLACED FAN COWL O/B. 2 L 7 2 4F RT A16WE 2007101000026 20071010 00026 NM 2007 10 10 HNAA0700186 1 20071003 A 2520 8SC0182 STRUT DHAV DHC8 DHC8102 2809003 NM OVERHEAD BIN LEAKING A HNAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 EA 07 933HA 134 HYD/OIL LEAKING FROM PSU AREA ROW 4/5 RIGHT SIDE. CAPT RETURNED TO FIELD WITHOUT CONTACTING MX OR DISPATCH. HISTORY FR OM PREVIOUS DAY, SAME DISCREPANCY OVERHEAD BIN WAS MEL'D DUE TO STRUT LEAKING. FLUID FOUND LEAKING FROM ROW 5 OVERHEAD BIN FWD GAS STRUT. OVERHEAD BIN PREVIOUSLY MEL'D. CLEANED AREA PLACARD BIN NOT TO BE USED. SBY MAINTENANCE REMOVED SI DEWALL PANEL AND EXAMINED HYDRAULIC LINES FROM OVERHEAD TO WAIST LVL. NO LEAKS NOTED. REMOVED AND REPLACED BOTH SNUBBE RS FOR OVERHEAD BIN 5F. 2 H 7 2 4T RT A13NM 2007101000043 20071010 00043 SO 2007 10 10 RAIA00709029 1 20070922 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 822HK 145069 PRE FLT NR 5488 - IAD - EMERGENCY LIGHT IN CEILING BY ROW 12 OUT. MAINTENANCE RELAMPED BULB, OPS OK. 2 L 7 2 4T RT T00011AT 2007101000051 20071010 00051 NM 2007 10 10 USAA920070859 1 20070923 A 5340 69414372 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6505198, CRACKED STRINGER CLIP, BS 663.75, S10R. REPLACED STRINGER CLIP, BS 663.75 , S10R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007101000055 20071010 00055 SO 2007 10 10 RAIA00710001 1 20071002 A 3350 BULB EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS BURNED OUT A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 807HK 145119 POST FLT NR 3568 - PIT - EMERGENCY EXIT LIGHT ON OVERHEAD NEAR EMERGENCY EXIT DOOR INOP. MAINTENANCE RELAMPED OVERHEAD LIGHT. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2007101000056 20071010 00056 NM 2007 10 10 SWAA074889 1 20071001 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 932 S23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 23L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007101000059 20071010 00059 SO 2007 10 10 RAIA00709033 1 20070926 A 2720 3603001001 PCU EMB 145 EMB145LR 3260212 SO RUDDER INOPERATIVE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 811HK 12976 12976 145256 FLT NR 5539 - STL - RUDDER SYSTEM 2 INOP AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED RUDDER PCU. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007101000063 20071010 00063 NM 2007 10 10 CALA0700556 1 20071002 A 5320 651768465 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 294.5-303.9 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR CUTOUT FORWARD SIDE STA 294.5 TO 303.9 AT STRINGER 10L O/B SUPPORT ANGLE F OR WEB. WEB INTERCOSTALS WERE INSTALLED IAW ECRA 5311-01361. 2 L 7 2 4F RT A16WE 2007101000074 20071010 00074 NM 2007 10 10 SWAA074890 1 20071001 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED HC1 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLA P PER MM. 2 L 7 2 4F RT A16WE 2007101000075 20071010 00075 NM 2007 10 10 SWAA074869 1 20070930 A 5753 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 14Y CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER BOEING SB. 2 L 7 2 4F RT A16WE 2007101000076 20071010 00076 NM 2007 10 10 SWAA074861 1 20070930 A 5311 6546525 FRAME BOEING 737 7375H4 138449D NM BS 380 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 18L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007101000078 20071010 00078 NM 2007 10 10 SWAA074880 1 20071001 A 5311 6546550 FRAME BOEING 737 7375H4 138449D NM BS 787 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007101000079 20071010 00079 NM 2007 10 10 USAA920070874 1 20070919 A 5340 96249113 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6505181, CRACKED STRINGER CLIP, BS 294.5, S9L. REPLACED STRINGER CLIP, BS 294.5, S 9L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007101000082 20071010 00082 NM 2007 10 10 USAA920070877 1 20071002 A 5320 141N51603 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 903AW 23323 MCN - MAJOR REPAIR - C-12 CHECK - NR 5976960, CORROSION ON CABIN FLOOR CHANNEL, BS 359, RBL 35.5, WL 208.1. REPLACED CA BIN FLOOR CHANNEL, BS 345 - BS 365.25, RBL 35.5, WL 208.1 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007101000083 20071010 00083 EU 2007 10 10 USAA920070878 1 20070929 A 5552 D5598141100000 HINGE FITTING AIRBUS 320 A320231 3930325 EU ZONE 300 WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 636AW 098 SAL - MAJOR REPAIR - C-05 CHECK - NR 5989775, RIGHT ELEVATOR HINGE ARM FITTING NR 2 WORN, HORIZONTAL STABILIZLER STATION 227 / RIB 6. REPLACED RIGHT ELEVATOR HINGE ARM FITTING NR 2, HORIZONTAL STABILIZLER STATION 227 / RIB 6 IAW A320 SRM 5 1-72-11. 2 L 7 2 4F RT A28NM 2007101000084 20071010 00084 EU 2007 10 10 USAA920070879 1 20070921 A 5347 D57130147202 SEAT TRACK AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 636AW 098 SAL - MAJOR REPAIR - C-05 CHECK - NR 5989136, CORROSION ON SEAT TRACK, BS 1430 - BS 1560, +Y1292. REPLACED SEAT TRACK, BS 1430 - BS 1560, +Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007101000085 20071010 00085 NM 2007 10 10 USAA920070880 1 20070925 A 5320 6517684 WEB BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438U 24560 CLT - MAJOR REPAIR - FPBH INSPECTION, CRACKED WEB, BS 296, S7L. REPLACED WEB, BS 296, S7L IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007101000097 20071010 00097 2007 10 10 HEER117364 4 20070917 A 2564 ASI50001 LIFE RAFT SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL2S2 60036 NE LEFT UNBONDED B HEER K NONE O OTHER IN INSP/MAINT 1 SW 03 45138 760675 OB ATTACHMENT EDGE OF LT LIFE RAFT POD FOUND TO BE DISBONDED FROM CENTER FILLET. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U 4 U NC H1NE E00054EN 2007101000105 20071010 00105 CE 2007 10 10 GUUA09120701 1 20070912 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87552 UE216 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT OB ELEVATOR HINGE BRACKET HAS CORROSION. REPLACED LT OB ELEVATOR HIN GE BRACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101000107 20071010 00107 SO 2007 10 10 GUUA09220702 1 20070922 A 3220 LANDING GEAR EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE NOSE SLOW A GUUA O OTHER O OTHER AP APPROACH 1 SO 29 285AS 120265 DURING APPROACH WHEN LANDING GEAR EXTENDED NOSE GEAR DELAYED WELL OVER 30 SECONDS TO EXTEND. PERFORMED LANDING EXTENSIO N SEVERAL TIMES NO DEFECTS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 2007101000115 20071010 00115 EA 2007 10 10 QXEA200701418 1 20070914 A 5242 H34455 HOUSING CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE E/E BAY DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 AVIONICS DOOR HANDLE HOUSING CRACKED AROUND THE SHAFT. REPLACED THE HANDLE HOUSING. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007101000117 20071010 00117 CE 2007 10 10 DXTA200702496 1 20070925 A 2730 TRIM SYSTEM CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE ELEVATOR OUT OF ADJUST E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 676QS 5605176 ELEVATOR TRIM INDICATOR IS INCORRECT ELEVATOR SET TO FORWARD END OF TAKE OFF RANGE THE AIRCRAFT REQUIRED ADDITIONAL NOSE DOWN TRIM IMMEDIATELY AFTER TAKEOFF. ADJUSTED TRIM TAB POINTER IAW THE MM 27-32-01. ADJUSTED ELEVATOR TRIM SYSTEM IAW THE MM 27-31-00. OPERATIONAL CHECK SATISFACTORY. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007101000121 20071010 00121 CE 2007 10 10 DXTA200702500 1 20070926 A 3110 BEPBA07RBL LAMP CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL INST PANEL LIGHT BURNED OUT E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 913QS 7637 7500113 LT PANEL LIGHTING C/B POPPED WITH BURNING INSULATION ODOR UPON ACTIVATION OF DAY/ NIGHT DIM SWITCH PRIOR TO ENGINE START . KPHL CHECKED AND LT PANEL LTS AND CB OPERATED NORMALLY. PERFORMED PIN OUT FOR POWER, GND AND CONTINUITY. AH PANEL CB JC028 AND LIGHTING INVERTER PLUG PC035. FOUND 40 OHMS TO VARY TO 160 OHMS ON PC035 PIN F. TRACED TO DEFECTIVE RT ICE DETECTOR BULB (PARTIALLY MELTED). REPLACED BULB WITH A NEW BULB. INSP AND CLOSED AREA. PAND AND ANTI ICE LIGHTS OPS O K 2 HRS. REF MM 33-40-08. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007101000128 20071010 00128 NM 2007 10 10 UPS07M50739 1 20070729 A 5320 AFA00436 SUPPORT DOUG MD11 MD11F 3023600 NM BS 1059 DEFORMED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C FWD CARGO COMPT AT STATION 1059 X=16.5 FOUND SUPPORT STRUT DEFORMED DAMAGED. FWD CARGO COMPT STA 1059 X=16.5 LT DEFORMED DAMAGED SUPPORT STRUT REMOVED AS PER SRM 51-33-01 VOL II REV 38. NEW SUPPORT STRUT AFA0043-6 HOLES P/UP PER SRM 51-33-01 VOL II REV 38. NEW SUPPORT STRUT AFA0043-6 INSTALLED AT FWD CARGO COMPT STA 1059 X=16.5 LT PER SR M 51-33-01 VOL II REV 38. PAINT TOUCHED UP ON REWORK AREA PER SRM 51-21-01 VOL II REV 38. 2 L 7 3 4F RT A22WE 2007101000129 20071010 00129 NM 2007 10 10 UPS07M50740 1 20070729 A 5320 ADA00332 SUPPORT DOUG MD11 MD11F 3023600 NM BS 1039 DEFORMED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C FWD CARGO COMPT AT STATION 1039 X=16.5 FOUND SUPPORT STRUT DEFORMED DAMAGED. FWD CARGO COMPT STA 1039 X=16.5 LT DEFORMED DAMAGED SUPPORT STRUT REMOVED PER SRM 51-33-01 VOL II REV 38. NEW SUPPORT STRUT ADA0033-2 HOLES P/U P PER SRM 51-33-01 VOL II REV 38. NEW SUPPORT STRUT ADA0033-2 INSTALLED AT FWD CARGO COMPT STA1039 X=16.5 LT PER SRM 51 -33-01 VOL II REV 38. PAINT TOUCHED UP ON REWORK AREA PER SRM 51-21-01 VOL II REV 38. 2 L 7 3 4F RT A22WE 2007101000137 20071010 00137 SO 2007 10 10 C2XA07SH075 1 20070921 A 5751 14574000405 SHROUD EMB 145 EMB145EP 3260221 SO LT AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14947 145054 SHV - DURING C-CHECK MAINTENANCE FOUND LT AILERON UPPER SHROUD WITH CORRODED BONDING PLATES. MAINTENANCE REPAIRED LT AIL ERON SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007101000140 20071010 00140 SO 2007 10 10 C2XA07SH078 1 20070921 A 5320 14532636401 FLOOR SUPPORT EMB 145 EMB145EP 3260221 SO FUSLEAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14947 145054 SHV - DURING C-CHECK MAINTENANCE FOUND LT OMEGA BEAM WITH CORROSION BETWEEN FRAMES 20 & 23. MAINTENANCE REPAIRED LT OME GA BEAM AT FRAME 20 & 23 IAW IC 2007-145-06463. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007101000145 20071010 00145 CE 2007 10 10 DELA200720007 1 20070927 A 3297 CONNECTOR LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP NLG DOWNLOCK DIRTY E DELA O OTHER J WARNING INDICATION DE DESCENT 1 CE 03 431AS 431 NOSE GEAR UNSAFE LIGHT ILLUMINATED ON APPROACH. FLY BY TOWER INDICATED GEAR WAS DOWN. LANDED UNEVENTFULLY. TROUBLESHO T WIRING TO NLG DOWNLOCK SWITCH, FOUND CONTACTS AT CONNECTOR PLUG NEEDED CLEANING. CLEANED AND REATTACHED. CONDUCTED G EAR SWING, OPS CHECK GOOD. 2 L 7 2 4F 4 F A10CE E6WE 2007101000146 20071010 00146 NM 2007 10 10 KCSA071429 1 20070928 A 5412 BULKHEAD BOEING 747 7472B4B 138481B NM NR 3 NACELLE WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 NR 3 PYLON FWD ENG MOUNT BULKHEAD STA 128.95 HAS DEEP WEAR AT I/B LOWER AREA. 2 L 7 4 4F RT A20WE 2007101000154 20071010 00154 CE 2007 10 10 DXTA200702502 1 20070927 A 2700 WARNING LIGHT CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE HORIZONTAL STAB FALSE ACTIVATION E DXTA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 07 600QS 5605664 DURING APPROACH, THE FLAPS WERE SELECTED TO 15. THE STAB MISCOMPARE LIGHT ILLUMINATED. EMER CHECKLIST ACCOMPLISHED. ONCE FLAP HANDLE WAS SELECTED TO 35 DEGREES THE STAB MISCOMPARE LIGHT WENT OUT AFTER 5 SECONDS. PERFORMED THE TWO POSITION HORIZONTAL STABILIZER OPERATIONAL CHECK IAW THE CITATION 560XL M/M CHAPTER 27-40-00. DISCREPANCY COULD NOT BE DUPLICATE D. OPERATIONAL CHECKS NORMAL. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007101000155 20071010 00155 CE 2007 10 10 DXTA200702503 1 20070927 A 3620 1103P0912 PRESSURE SWITCH CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL AFT SERVICE BAY FAILED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 949QS 2044 7500049 ON TAKEOFF, GOT AN AMBER HP DUCT OVER PRESS R CAS MESSAGE, ABORTED TAKEOFF AND RAN CHECKLIST, CAS MESSAGE REMAINED ON AF TER SHUTDOWN. TROUBLESHOT "RT HP. DUCT OVER PRESSURE" EICAS MSG, FOUND RT DUCT OVER PRESSURE. PRESSURE SWITCH FAILED. REMOVED & REPLACED WITH A NEW UNIT PER CE-750 M/M. CH. 36-11-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007101000156 20071010 00156 CE 2007 10 10 DXTA200702505 1 20070927 A 3260 MS25237327 BULB CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LT MLG INDICATOR BURNED OUT E DXTA O OTHER P NO WARNING INDICATION LD LANDING 1 GL 07 352QS 10572 5600352 NO GREEN LIGHT ON LT MAIN GEAR DURING GEAR EXTENTION, RAN THE EMERGENCY EXTENTION CHECKLIST. BLOWED GEAR DOWN FOR POSITI VE DOWN AND LOCKED. CREW VERIFIED GREEN VISUAL INDICATOR IS SHOWING ON THE MLG ACTUATOR. AT THIS TIME WITH ROTARY TEST, THE LT MAIN GEAR INDICATOR LIGHTS DO NOT LIGHT. RELAMPED INDICATOR, JACKED A/C. RESET EMERG. BLOWDOWN BOTTLE SYSTEM, SERVICED BOTTLE, CYCLED GEAR MULTIPLE TIMES, SERVICED RESERVOIR. ALL IAW REFS: 560 AMM 32-60-00, 12-13-01. LAMP SUPP LIED FROM N352QS FLYAWAY KIT. SYSTEM OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2007101000157 20071010 00157 WP 2007 10 10 UPS07850758 1 20070927 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1746 L28L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:N/A PULLED RIVETS AND SKIN CORROSION AFT OF PRESSURE BULKHEAD. A/C FERRIED TO SAA 9047. REPAIRED EXTE RNAL SKIN CRACKS AT STA 1746 L28L IAW SRO 8530032. 2 L 7 4 4F RT 4A25 2007101000158 20071010 00158 EA 2007 10 10 TRAX200701388 1 20070924 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 838AS 7276 AAR - RIGHT HAND 621 OBLIQUE ANGLE CRACKED (INTERCOSTAL). REMOVED CRACKED OBLIQUE ANGLE AND LOCATED AND INSTALLED S ERVICEABLE RT OBLIQUE ANGLE (P/N 601-35012-52) IAW CRJ 200 SRM 51-42-21. 1367. 10-1-07. 2 L 7 2 4F RT A21EA 2007101000159 20071010 00159 EA 2007 10 10 TRAX200701392 1 20070924 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 855AS 7395 ETNRC - PAX DOOR HANDLE BETA LIGHT INOP. BETA LIGHT PAX DOOR REPLACED IAW AMM 33-51-09-000-801 FUNCTIONAL TEST OF THE DOOR EXIT SIGN BETA LIGHT IAW AMM 33-51-09-720-801. 2 L 7 2 4F RT A21EA 2007101000160 20071010 00160 EA 2007 10 10 TRAX200701393 1 20070924 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 838AS 7276 AAR - PAX DOOR PANEL 832BT HAS DAMAGED -EXIT- PLACARD. REMOVED ADN APPLIED NEW SERVICEABLE EXIT PLACARD PN S1574-18 T O PAX DOOR PANEL 832BT IAW CRJ 200 AMM 11-30-00. 2 L 7 2 4F RT A21EA 2007101000161 20071010 00161 EA 2007 10 10 TRAX200701394 1 20070924 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 838AS 7276 INTERCOSTAL CLIP CRACKED AT FS 484, LBL 27 O/B. REMOVED CRACKED INTERCOSTAL CLIP AT FS 484 LBL 27 O/B IAW CRJ 200 SRM 51-42-21. DUPLICATED ANGLE, LOCATED, DEBURRED, ALODINED, PRIMED, AND PAINTED IAW CRJ 200 SRM 53-41-43. INSTALLED SERVI CEABLE ANGLE IAW CRJ 200 SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007101000169 20071010 00169 EU 2007 10 10 2007UALA03616 1 20070903 A 2710 341085200 ROD END AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT AILERON WORN A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 432UA 587 LOW HUM WITH ASSOCIATED LOW VIBRATION ON C-P FLOOR IN CLIMB AND CRUISE. WORN SERVO ROD OF AILERON CONTROL SYSTEM. REPL ACED L OUTBOARD AILERON SERVO ROD END. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101000170 20071010 00170 NM 2007 10 10 2007UALA03802 1 20070919 A 5754 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RT WING LE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 197UA 26901 CRACK FOUND IN RIGHT WING LEADING EDGE SKIN PANEL OUTBOARD OF LANDING LIGHT LENS RUNNING THROUGH 4 RIVETS TO EDGE OF SKI N. 10-19-07 ACCOMPLISH EDDY CURRENT INSPECTION OF CUTOUT REPAIR AND SURROUNDING STRUCTURE OUTBOARD OF RH OUTBOARD LANDING LIGHT PER SRM. MANUFACTURED DOUBLERS AND HEAT TREAT TO REQ'D VALUE. INSTALLED DOUBLERS. INSPECTED AFTER COMPL ETION & AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007101000171 20071010 00171 NM 2007 10 10 2007UALA03803 1 20070919 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 543UA 25698 ELECTRICAL ODOR UPON CLIMB OUT BY FLT CREW. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101000172 20071010 00172 EU 2007 10 10 2007UALA03804 1 20070920 A 2910 HYDRAULIC SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 406UA 454 EVIDENCE OF HYD LEAK AFT FUSELAGE GREEN SYSTEM. LOST 1 US GAL IN 1.5 HRS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101000173 20071010 00173 EU 2007 10 10 2007UALA03805 1 20070920 A 7830 STRUCTURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE THRUST REVERSER DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 408UA 457 NR 1 ENG THRUST REVERSER INNER WALL AT 11 O'CLOCK POSITION HAS DAMAGE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101000174 20071010 00174 EU 2007 10 10 2007UALA03806 1 20070920 A 2560 FLASHLIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 432UA 587 FLASHLIGHT AT AFT JUMPSEAT INOP. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101000176 20071010 00176 2007 10 10 2007UALA03808 4 20070920 A 2565 INDICATOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU R1 DOOR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 THE 1R DOOR SLIDE GAUGE OUT OF POSITION AND ALMOST IMPOSSIBLE TO READ. REPACKED SLIDE ASSEMBLY. GAUGE READABLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007101000177 20071010 00177 NM 2007 10 10 2007UALA03809 1 20070920 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 175UA 24382 STAIR CASE TO UPPER DECK EEL LIGHT IS COMING OFF. 10-16-07 SECURED LIGHT. EEL SYSTEM READY FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007101000178 20071010 00178 NM 2007 10 10 2007UALA03810 1 20070920 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR SLIDE INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 EMERGENCY SLIDE LIGHT INOP AT DOOR 4L. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101000179 20071010 00179 NM 2007 10 10 2007UALA03811 1 20070920 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 529UA 25019 EEL LAMPS INOP ROW 31 TO AFT GALLEY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101000180 20071010 00180 NM 2007 10 10 2007UALA03812 1 20070920 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 AISLE EMERGENCY LIGHTS INOP ROWS 27, 31 & 34. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101000181 20071010 00181 2007 10 10 2007UALA03813 4 20070920 A 2565 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 EMERGENCY SLIDE LIGHT INOP AT DOOR 4R. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101000182 20071010 00182 NM 2007 10 10 2007UALA03814 1 20070920 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GALLEY INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 EEL LIGHT INOP AT FWD GALLEY CART STOWAGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101000184 20071010 00184 NM 2007 10 10 2007UALA03817 1 20070920 A 3260 WARNING LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MLG ILLUMINATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 543UA 25698 ON GEAR EXT GOT GEAR DISAGREE EICAS & YELLOW GEAR LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101000185 20071010 00185 NE 2007 10 10 2007UALA03818 2 20070920 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 MAKING METAL A UALA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION DE DESCENT 1 WP 29 588UA 26717 CREW REPORTED NR 2 ENGINE SHUTDOWN DUE TO HIGH OIL TEMPERATURE 178-179 DEGREES AND ENG OIL BYPASS MESSAGE. OIL QTY AND PRESSURE NORMAL. ENGINE WAS SHUT DOWN FOR ABOUT 20 MINUTES PRIOR TO LANDING. INSPECTED CHIP DETECTORS AND ALL DETECTOR S ARE FULL WITH METAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101000186 20071010 00186 NM 2007 10 10 2007UALA03819 1 20070920 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 675UA 29243 MID GALLEY X AISLE EEL LIGHT INOP. 10-16-07 REPLACED EEL STRIP, OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101000187 20071010 00187 NM 2007 10 10 2007UALA03820 1 20070921 A 3397 CONNECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 806UA 788 CABIN EMERGENCY LIGHT TEST FAIL. MSG - EPSU INT LOAD EMER L. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101000188 20071010 00188 NM 2007 10 10 2007UALA03821 1 20070922 A 3350 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 816UA 871 FWD EMERGENCY LIGHT POWER SUPPLY FAIL TEST PER 3 SVC. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101000189 20071010 00189 NM 2007 10 10 2007UALA03822 1 20070921 A 3510 OXYGEN MASK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE 1ST OFFICER'S LEAKING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 824UA 965 F/O'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). 2 L 7 2 4F 4 F RT A28NM E40NE 2007101000190 20071010 00190 NM 2007 10 10 2007UALA03823 1 20070921 A 3500 OXYGEN MASK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE 2ND OBSERVER'S INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 824UA 965 SECOND OBS QUICK DONNING MASK INOP. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101000191 20071010 00191 NM 2007 10 10 2007UALA03824 1 20070921 A 5347 SEAT TRACK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 848UA 1647 LEFT INBOARD SEAT TRACK FROM FRAME 42 THROUGH 47-51 IS GOUGED BEYOND LIMITS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101000192 20071010 00192 EU 2007 10 10 2007UALA03825 1 20070923 A 3397 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 443UA 820 CABIN EMERGENCY LIGHT TEST FAILS (EPSU EXT LOAD FWD L). 2 L 7 2 4F 4 F RT A28NM E40NE 2007101000193 20071010 00193 NM 2007 10 10 2007UALA03826 1 20070924 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY LIGHTS INOP AT SEATS 4J AFT & 50 ABC. 10-19-07 REPLACED EMERGENCY LAMP BOTH SEAT POSITIONS. OP CHECKS N ORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007101000194 20071010 00194 NM 2007 10 10 KCSA071432 1 20070929 A 5312 PRESSURE PANEL BOEING 747 747132 1384882 NM NLG WW CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 709CK 20247 NOSE WHEEL WELL LEFT SIDE WALL PANEL WEB IS CRACKED .75 INCH AT STA 310, WL 170 BONDED STRAP. 2 L 7 4 4F A20WE 2007101000195 20071010 00195 NM 2007 10 10 KCSA071433 1 20070929 A 5312 PRESSURE PANEL BOEING 747 747132 1384882 NM BS 290 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 709CK 20247 NOSE WHEEL WELL LEFT SIDE WALL PANEL WEB IS CRACKED .75 INCH AT STA 290, WL 170 BONDED STRAP. 2 L 7 4 4F A20WE 2007101000196 20071010 00196 NM 2007 10 10 KCSA071434 1 20070929 A 5312 PRESSURE PANEL BOEING 747 747132 1384882 NM BS 268 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 709CK 20247 NOSE WHEEL WELL LEFT SIDE WALL PANEL WEB IS CRACKED .75 INCH AT STA 268, WL 170 BONDED STRAP. 2 L 7 4 4F A20WE 2007101000197 20071010 00197 NM 2007 10 10 SB07085 1 20070930 A 2133 0321309001 OUTFLOW VALVE BOEING 737 7373B7 1384580 NM CABIN PRESSURE MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 589US 23934 FLT 1253 CLT - ORF ON DEPARTURE AIRCRAFT DID NOT PRESSURIZE. RETURN TO CLT. RESET PRESSURIZATION SYSTEM. NO FURTHER F AULTS. 2 L 7 2 4F RT A16WE 2007101000217 20071010 00217 NM 2007 10 10 HALA0700421 1 20071001 A 3150 WARNING LIGHT BOEING 717 717200 1383700 NM FALSE ACTIVATION A HALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 13 481HA 55126 PODS ANTI ICE FAULT LIGHT ON. PERFORMED BITE TEST. NO FAULTS, PERFORMED RTS, TEST PASSED. OK FOR SERVICE. 2 L 7 2 4F TR A6WE 2007101000222 20071010 00222 EU 2007 10 10 07FDEA04463 1 20071002 A 5320 A53773644 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION AT CORNER FITTING C 33 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007101000223 20071010 00223 EU 2007 10 10 07FDEA04464 1 20071002 A 5311 A53776575207 FRAME AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND ENLARGED HOLES AT C 26/32 BETWEEN P 13-22 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007101000224 20071010 00224 EU 2007 10 10 07FDEA04465 1 20071002 A 5320 A53974243202 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION AT CORNER FITTING P 44 LT, C64 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007101000225 20071010 00225 EU 2007 10 10 07FDEA04466 1 20071002 A 5313 A53974484204 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION AT STRINGER P 48 LT, C 69-70 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007101100004 20071011 00004 NM 2007 10 11 AMTA200700458 1 20070922 A 2150 3964801 VALVE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE FLOW CONTROL UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 520AT 27976 EICAS MSG L PACK OFF DISPLAYED. PACK OFF LIGHT ILLUMINATED. LIGHTS FAILED TO EXTINGUISH WHEN PACK RESET SW PUSHED. PA CK OPPERATES NORMAL. REPLACED LT FLOW CONTROL VALVE, OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007101100005 20071011 00005 NM 2007 10 11 AMTA200700459 1 20070924 A 3350 20131A BATTERY BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHT UNSERVICEABLE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 514AT 27971 FWD L/L EMERGENCY LT INOPERATIVE. REPLACED BATTERY PACK CHECKS NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007101100011 20071011 00011 NM 2007 10 11 DLM90071283 1 20070930 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 1136-1155 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 RT CUSP WEB CORRODED STA 1136-1155. REMOVED AND REPLACED CUSP WEB AT STA 1136-1155 IAW MD-90 SRM 51-30-02, 51-30-05, 51 -10-05, 51-30-01 ON N/R 2000-0110 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007101100012 20071011 00012 NM 2007 10 11 DLM90071284 1 20070803 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 1080 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 RT CUSP WEB CORRODED OUT OF LIMITS FS 1080. TRIMMED OFF DAMAGED CUSP WEB SECTION, FABRICATED NEW, AND INSTALLED IAW EA 398191-14MA, MD-90 SRM 51-30-02, 51-30-01, 51-30-05 AND 51-10-03 ON NR 2700-0172 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007101100014 20071011 00014 NM 2007 10 11 DLM90071289 1 20071001 A 5730 SKIN DOUG MD90 MD9030 3023690 NM LT WING PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 LT FIXED WING L/E SKIN STA XRS 105.000 HAS A PUNCTURE. REPAIRED L/E SKIN IAW MD-90 SRM 57-20-01 FIG 11 VOL 1 ON N/R 520 0-0043 ON HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007101100016 20071011 00016 EU 2007 10 11 AALA20071837 1 20071001 A 2910 VALVE AIRBUS 300 A300B4605R 3930308 EU HYD SYSTEM LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 80052 460 BOG INFLIGHT T915/01OCT - BLUE HYDRAULIC SYSTEM AMBER LOW QUANTITY INDICATION AND CHIME. LANDED BOG WITHOUT INCIDENT. FOUND PRESSURE LINE IN WHEEL WELL LEAKING. TIGHTENED LINE AT C PORT OF RELIEF VALVE 2063. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007101100018 20071011 00018 NM 2007 10 11 AALA20071836 1 20071001 A 7700 N14FF104 TRANSDUCER BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE INOPERATIVE A AALA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SW 21 647AM 24605 31010 PHX INFLIGHT T2289/01OCT - CAPTAIN REPORTED HEARING LOUD BANG FROM THE NUMBER TWO ENGINE AT FLIGHT LEVEL 400. ENGINE GA S TEMPERATURE AND OTHER ENGINE INDICATIONS DECREASED. CAPTAIN SHUTDOWN NR 2 ENGINE & LANDED WITHOUT INCIDENT. SINGLE E NGINE TIME 22 MINUTES. ACCOMPLISHED BOROSCOPE OF NR 2 ENGINE COMPRESSOR. REPLACED NR 2 ENGINE POWER LEVEL ANGLE TRANSD UCER AND RT ENGINE DRIVEN HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2007101100019 20071011 00019 NM 2007 10 11 AALA20071829 1 20070929 A 3350 COVER BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS DETACHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 916AN 29517 MEX - CABIN SEAT TRIM COVER THAT HOLDS EMERGENCY LIGHTS DETACHED. REINSTALLED CABIN SEAT TRIM COVER WITH EMERGENCY LIGH TS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007101100028 20071011 00028 NM 2007 10 11 AALA20071830 1 20070929 A 2910 HOSE BOEING 757 757223 1384957 NM HYD SYSTEM LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SW 21 636AM 24594 MIA INFLIGHT T1913/29SEP - LANDED WITH A BRAKE HYDRAULIC FAILURE (LEFT HYDRAULIC SYSTEM). AIRCRAFT LANDED WITHOUT INCID ENT AND MOVED OFF RUNWAY. AIRCRAFT WAS TOWED TO GATE. REPLACED LEFT DOWN LOCK ACTUATOR HYDRAULIC LINES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007101100034 20071011 00034 NM 2007 10 11 07FDEA04480 1 20071003 A 5720 CHANNEL BOEING 727 7272S2F 1384O81 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 205FE 22927 THE RT AFT WING TIP SECTION HAS A BROKEN NUT PLATE CHANNEL IN THE LOWER AFT END. THIS DISCREPANCY WAS FOUND DURING A "B " CHECK. REPAIRED NUTPLATE CHANNEL PER EA NR 7-5730-115028 2 L 7 3 4F A3WE 2007101100035 20071011 00035 WP 2007 10 11 070161 1 20070926 A 3350 408822101 BATTERY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 878GA 53487 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007101100043 20071011 00043 2007 10 11 DHLA200700051 2 20071004 A 7200 ENGINE BOEING 727 7272B7 138407L NM MALFUNCTIONED A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 770AT 21953 REJECTED T/O ELP DUE TO NR 1 ENG PARAMETERS OUT OF NORMAL RANGE VS NR 2 AND NR 3 ENGS GW=147.9, SPEED EST .50 KNOTS, TEM P 29 DEGREES C PA 3950 REVERSE THRUST USED RAN NR 1 AND NR 3 ENG'S AND VERIFIED N1 AND N2 MATCHED. DEFERRED NR 1 ENG EP R GAUGE PER MEL 77-1-1 CAT A CONTROL NR 30271 0254Z KPS RTO INSP NOT REQUIRED PER M/M 5-51-121. 2 L 7 3 4F A3WE 2007101100047 20071011 00047 EU 2007 10 11 07FDEA04483 1 20071004 A 5313 A53974482 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION AT STRINGER SEGMENT P48, C 68-69 AND C 70-71. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007101100051 20071011 00051 NM 2007 10 11 AALA20071845 1 20071003 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 347AN 33086 MIA - EXTERIOR EMERGENCY LIGHT AT LEFT AFT INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY EXIT LIGHT AT LEFT AFT. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007101100054 20071011 00054 EA 2007 10 11 QXEA200701506 1 20071001 A 2820 M259882230 O-RING CNDAIR CL600 CL6002C10 1390015 EA VALVE CUT A QXEA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 NM 09 611QX 10041 SEA - FLIGHT 2531 - FUEL LEAKING FROM THE CENTER SECTION DURING SINGLE POINT REFUELING. MAINTENANCE REPLACED THE CUT O- RING ON THE INLET SIDE OF THE REFUEL/DEFUEL VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007101100057 20071011 00057 EA 2007 10 11 SWIA200718728 1 20070929 A 5410 ROD CNDAIR CL600 CL6002B19 1900309 EA NACELLE UNSECURE A SWIA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 NM 07 448SW 7678 FLT 3923 - LEFT THRUST LEVER WOULD NOT PULL BACK. SECURED UPPER CORE COWL SUPPORT ROD INTO STOWED POSITION. PERFORMED ENGINE RUNS WITH NO BINDING NOTED. 2 L 7 2 4F RT A21EA 2007101100058 20071011 00058 EA 2007 10 11 SWIA200718729 1 20070918 A 2913 887055 PUMP CNDAIR CL600 CL6002B19 1900309 EA NR 2 LEAKING A SWIA O OTHER K FLUID LOSS NR NOT REPORTED 1 NM 07 935SW 12007 12007 7725 FLT 6635 - FOUND FLUID LEAKING FROM NR 2 EDP. INSTALLED NR 2 EDP IAW AMM 29-11-01. 2 L 7 2 4F RT A21EA 2007101100061 20071011 00061 EA 2007 10 11 SWIA200718732 1 20070930 A 3350 SIGN CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT MISSING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 703SK 10139 FLT 6570 - EMERGENCY EXIT SIGN IS MISSING AT ROW 3. FOUND EMERGENCY EXIT SIGN COVER AND REINSTALLED IT. 2 L 7 2 4F RT A21EA 2007101100063 20071011 00063 EA 2007 10 11 SWIA200718734 1 20070927 A 3350 SIGN CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT MISSING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 713SK 10174 FLT 5915 - FOUND LOWER GALLEY EMERGENCY EXIT SIGN IS MISSING. REPLACED EMERGENCY LIGHT COVER IAW CRJ 700 AMM 33-51-11. 2 L 7 2 4F RT A21EA 2007101100064 20071011 00064 EA 2007 10 11 SWIA200718735 1 20070928 A 5297 WIRE HARNESS CNDAIR CL600 CL6002C10 1390015 EA DOOR SENSOR SHORTED A SWIA O OTHER N FALSE WARNING CL CLIMB 1 NM 07 713SK 10174 FLT 5821 - PROX SYSTEM FAULT 2 STATUS MESSAGE CAME ON IN FLIGHT. RETURNED TO FIELD. REPLACED AFT BAGGAGE BAY DOOR SENS OR HARNESS PER MM 52-70-02. 2 L 7 2 4F RT A21EA 2007101100070 20071011 00070 EA 2007 10 11 SWIA200718741 1 20071002 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 955SW 7418 7418 7817 FOUND LEFT EMERGENCY LIGHT INOP. REPLACED NR 2 EMERGENCY BATTERY PACK PER MM 33-51-04. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007101100073 20071011 00073 NM 2007 10 11 HALA0700424 1 20071001 A 4900 APU BOEING 767 76733A 1385209 NM MALFUNCTIONED A HALA O OTHER O OTHER DE DESCENT 1 WP 13 580HA 28140 ETOPS SIGNIFICANT SYSTEM, APU WILL NOT START GETS TO 15 PERCENT THEN NO ACCELERATION. BITE CHECK APU ECU PER FIM 49-11- 00 FIG 103, NO DEFECTS NOTED, STARTED APU 3X OPS CHECK OK, OK FOR SVC. 2 L 7 2 4F RT A1NM 2007101100075 20071011 00075 2007 10 11 HALA0700426 4 20071001 A 3417 2587400542 ADC BOEING 767 76733A 1385209 NM MALFUNCTIONED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 581HA 37619 37619 28141 ETOPS SIGNIFICANT SYSTEM, FIRST OFFICERS AIRSPEED IND INSTRUMENT AND EFIS A/S MACH INDICATOR WENT OVERSPEED AT CRUZ ALT 35000 ALSO F/O'S ALTIMETER CLIMBED 600'. SWITCHED F/O'S AIR DATA SOURCE SELECTOR TO ALTERNATE POSITION. T/S PER FIM 34 -12-00 FIG 109. TEST OF RIGHT ADC NORMAL. NO FAULTS TEST OF LEFT ADC NORMAL. NO FAULTS. INSPECTED F/O PITOT PROBES A ND LINES. NO FAULTS. NO EXT SENSOR FAULTS ON EITHER ADC PERFMD MCDP LAST FLT AND NR 30 TEST NO FLTS. REMOVED AND REPL ACED F/O'S ADC PER AMM 34-12-01-006, TEST 30, NO FLTS. 2 L 7 2 4F RT A1NM 2007101100076 20071011 00076 EA 2007 10 11 QXEA200701512 1 20071002 A 2840 COMPUTER CNDAIR CL600 CL6002C10 1390015 EA FUEL QTY MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 611QX 10041 PDX - FLIGHT 2514 - DURING PUSHBACK AUTO TRANSFER FUEL SYSTEM FAILED. RETURNED TO THE GATE. MAINTENANCE CYCLED POWER T O THE FQGC. PERFORMED FUEL AUTO TRANSFER, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007101100079 20071011 00079 EU 2007 10 11 1212 1 20071003 A 3300 3011180 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU EMERGENCY LIGHTS DAMAGED A HYIA K NONE L NO TEST IN INSP/MAINT 1 NE 01 14834 193 EMERGENCY LIGHTING BATTERY PACK UNIT FOUND DAMAGED DURING CAP CHECK. BATTERY AND TRAY NEED TO BE REPLACED. BATTERY PACK (P/N 301-1180) AND TRAY (301-1066) WERE REMOVED AND REPLACED IN ACCORDANCE WITH CMM 33-51-21. 2 H 7 2 4T RT A53EU 2007101100080 20071011 00080 EU 2007 10 11 1214 1 20071003 A 3350 3011180 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU EMERGENCY LIGHTS DAMAGED A HYIA K NONE L NO TEST IN INSP/MAINT 1 NE 01 14834 193 EMERGENCY LIGHTING BATTERY PACK UNIT FOUND DAMAGED DURING CAP CHECK. BATTERY PACK AND TRAY NEED TO BE REPLACED. BATTER Y PACK (P/N 30-1180) AND TRAY (301-1066) WERE REMOVED AND REPLACED IN ACCORDANCE WITH CMM 33-51-21. 2 H 7 2 4T RT A53EU 2007101100083 20071011 00083 EU 2007 10 11 HYIA1213 1 20071003 A 3350 3011180 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU EMERGENCY LIGHTS DEFECTIVE A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 EMERGENCY LIGHTING BATTERY PACK UNIT FOUND DEFFECTIVE DURING CAP CHECK. BATTERY PACK UNIT REMOVED AND REPLACED PER CMM 33-51-21. 2 H 7 2 4T RT A53EU 2007101100084 20071011 00084 WP 2007 10 11 NWAA073349759 1 20070825 A 5330 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 759NW 47287 DURING "M" CHECK, FOUND CRACK IN FUSELAGE EXTERIOR SKIN AT UPPER FORWARD CORNER OF L1 PASSENGER DOOR. REPAIRED PER EA 9 7-210178. 2 L 7 2 4F A6WE 2007101100085 20071011 00085 WP 2007 10 11 IXXA070050O 1 20071003 A 2612 92274473 RELAY DOUG DC8 DC871F 302199D WP ZONE 600 FAILED A IXXA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 11 828BX 86929 445 45993 THIRTY MINUTES AFTER TAKEOFF FROM KTOL NR 4 FIRE WARNING LIGHT CAME ON, THE CREW DISCHARGED BOTH NR 4 ENGINE FIRE BOTTLE S INTO ENGINE, THE FIRE WARNING LIGHT WENT OUT AFTER THE SECOND BOTTLE WAS DISCHARGED. 5 MINUTES LATER FIRE WARNING WAS INTERMITTENT, NR 4 GENERATOR WAS DISCONNECTED. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INS PECTED AND REPLACED UNIVERSAL RELAY, MAINTENANCE RECONNECTED THE GEN RAN ENGINE FOR 30 MINUTES AT 70 PERCENT POWER OPERA TIONAL CHECK WAS GOOD BEFORE, DURING, AND AFTER RUN IAW DACO MAINTENANCE MANUAL 26-0, AND ATI DC8 ERH 70-01. AIRCRAFT W AS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2007101100089 20071011 00089 EU 2007 10 11 07FDEA04494 1 20071005 A 5730 A57241967 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION AT LT WING BOTTOM SKIN BETWEEN 18-19 FWD OF FRONT SPAR REPAIR PERFORMED BY BLEND OUT CORROSION AND REPRO TECTING IAW EA 6-5720-112535 AND RAS/BAE/1005212/2007. 2 L 7 2 4F RT A35EU 2007101100099 20071011 00099 NM 2007 10 11 NWAA073365504 1 20071003 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMEGENCY LGIHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 504US 23193 DURING OVERNIGHT LINE CHECK, FOUND EMERGENCY LIGHT ON OUTSIDE OF A/C AT DOOR 2 RIGHT INOP. MAINTENANCE REMOVED AND REPL ACED BATTERY PACK. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007101100108 20071011 00108 NM 2007 10 11 F3LA200700255 1 20070925 A 5315 D5347217220390 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM -Y1292 ON UPPER SURFACE AT NUTPLATE HOLE, APPROX 8 INCHES A FT OF FR 67. REMOVED AND REPLACED FLOORBEAM IAW SRM'S 51-42-11, 51-72-11 AND 51-44-11. 2 L 7 2 4F RT A28NM 2007101100110 20071011 00110 NM 2007 10 11 F3LA200700256 1 20070922 A 5315 D5347218820200 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT Y1162, FR 68. REMOVED AND REPLACED FLOORBEAM IAW SRM 51 -42-11, PARA 7, AND AIRBUS DRAWING D53472780. 2 L 7 2 4F RT A28NM 2007101100112 20071011 00112 NM 2007 10 11 F3LA200700257 1 20070923 A 5320 D5391635520000 PLATE AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED RT FWD CARGO COMPARTMENT UNDER FLOOR TRANSITION PANEL SUPPORT HAD CORRODED FASTENE R HOLE FROM FR 28 TO FR 31. REMOVED AND REPLACED SUPPORT PLATE IAW SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007101100118 20071011 00118 WP 2007 10 11 070165 1 20070829 A 5510 STRUCTURE DOUG DC9 DC982 3022082 WP HORIZONTAL STAB CRACKED A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 894GA 49660 HORIZONTAL STABILIZER LEFT SIDE CRACKED AT REAR UPPER INBOARD SIDE BETWEEN UPPER AND LOWER BOLTS AT STATION XH8.50. HOR IZONTAL STABILIZER SENT TO VENDOR FOR REPAIR. REPAIRED IAW ESO 80559 AND BOEING DRAWING 5R09550027. HORIZONTAL STABILI ZER OK FOR CONTINUED SERVICE. 2 L 7 2 4F A6WE 2007101100120 20071011 00120 NM 2007 10 11 F3LA200700259 1 20070927 A 5755 LUG AIRBUS A319 A319111 3930336 NM NR 3 SPOILER GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED GOUGES IN RT WING NR 3 SPOILER ANTI-ROTATION LUG SURFACE. MACHINED ANTI-ROTATION FLAT, PERFORMED HFEC, AND BONDED REINFORCEMENT PLATE IAW EA NR A9-57R-12169. 2 L 7 2 4F RT A28NM 2007101100127 20071011 00127 SO 2007 10 11 SIMA200728107 1 20071007 A 3350 602024 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 918AE 14500902 EMERGENCY EXIT SIGN INOP LOCATED BELOW COCKPIT DOOR. REMOVED AND REPLACED FORWARD LOWER EXIT SIGN IAW EMB145 AMM 33-50- 13. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007101100128 20071011 00128 SO 2007 10 11 SIMA200728108 1 20070928 A 5311 14523123417 FRAME EMB 135 EMB135KL 3260302 SO FUSELAGE CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 817AE 145554 DURING A MBV INSPECTION, FUSELAGE FRAME BETWEEN STRINGERS 15 AND 16 RIGHT WAS FOUND TO HAVE A CRACKED FLANGE. REPAIRED THE FLANGE IAW EMB IC 2007-145/06705 DATED 27 SEPT 07. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007101100133 20071011 00133 SO 2007 10 11 SIMA200728109 1 20070928 A 5320 14521700007 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 817AE 12829 145554 DURING A MBV INSPECTION A PREVIOUSLY REPAIR ANGLE ON THE LT OMEGA BEAM WAS FOUND CORRODED BETWEEN 24 AND 25. REPAIRED O MEGA BEAM IAW EMB 145 SRM CHAPTER 53-00-10 AND 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007101100135 20071011 00135 NM 2007 10 11 F3LA200700263 1 20070923 A 5320 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED CORRODED FASTENER HOLES UNDER FLOOR SUPPORT IN FWD CARGO COMPARTMENT FROM FR 24 TO FR 28. REMOVED CORROSION IAW SRM 51-74-00. PERFORMED HFEC ON BLENDOUTS OF CORROSION IAW NTM 51-10-08, PART 6. NO CRA CKS NOTED. PERFORMED ULTRASOUND IAW NTM 51-10-04, PART 4. ONE LOCATION FWD OF FR C27 OUT OF LIMITS. AREA BLENDED WITH ADJACENT NUTPLATE REMOVED IAW EA #A9-53R-12159. PERFORMED ROTO PROBE INSPECTION OF FASTENER HOLE IAW NTM 51-10-01, PA RT 6. NO DEFECTS NOTED. 2 L 7 2 4F RT A28NM 2007101100136 20071011 00136 NM 2007 10 11 F3LA200700264 1 20070923 A 5320 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED CORRODED FASTENER HOLES UNDER FLOOR SUPPORT AT FR 28 IN FWD CARGO COMPARTMENT AND EXISTING REPAIR FROM STR 38L TO 38R. REMOVED AND REPLACED FLOOR SUPPORT PLATE AT FR 28 FROM STR 38L TO STR 38R IAW SRM 51-42-11, 51-44-11, 51-46-11, AND 51-72-11. 2 L 7 2 4F RT A28NM 2007101100138 20071011 00138 NM 2007 10 11 F3LA200700266 1 20070923 A 5320 D5361019720040 COVER AIRBUS A319 A319111 3930336 NM L1 DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON LOWER SURFACE OF L1 DOOR THRESHOLD STRIP. REMOVED AND REPLACED THRES HOLD STRIP IAW AMM 53-12-12-400-001. 2 L 7 2 4F RT A28NM 2007101100142 20071011 00142 EA 2007 10 11 QXEA200701515 1 20071005 A 2150 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA RT A/C PACK ILLUMINATED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 608QX 10026 FAT - ON FLIGHT 2544, DURING TAXI, RECEIVED R PACK FAULT STATUS MESSAGE. RETURNED TO GATE. MAINTENANCE CYCLED AIRCRAFT POWER AND FOUND NO CURRENT FAULTS IN MDC. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007101100145 20071011 00145 EU 2007 10 11 AALA20071855 1 20071004 A 3510 MSE101157 OXYGEN SYSTEM AIRBUS 300 A300B4605R 3930308 EU COCKPIT LEAKING A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 7083A 645 PTY INFLIGHT T2110/04OCT LIM TO MIA - CREW OXYGEN LOW. LANDED PTY WITHOUT INCIDENT. FOUND LEAK AT SECOND OBSERVER OXYG EN MASK COMPARTMENT. REPLACED CREW OXYGEN BOTTLE AND BOX. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007101100147 20071011 00147 NM 2007 10 11 AALA20071862 1 20070921 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 AFW - EMERGENCY LIGHT BATTERY PACK AT LEFT NUMBER TWO DOOR M33099 INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK AT LEFT NUMBER TWO DOOR M33099. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007101100149 20071011 00149 WP 2007 10 11 AALA20071858 1 20071004 A 2450 GCU DOUG DC9 DC983 3022083 WP LEFT INOPERATIVE A AALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SW 21 980TW 53630 PDX INFLIGHT T9663/04OCT SEA TO SFO - LEFT GENERATOR FAILED AND RIGHT GENERATOR ON MEL. ONLY AUXILIARY POWER UNIT GENERA TOR OPERATING. LANDED PDX WITHOUT INCIDENT. REPLACED LEFT GENERATOR CONTROL UNIT BUS CONTROL UNIT AND LEFT BUS POWER R ELAY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007122700151 20071227 00151 NM 2007 12 27 SWAA076316 1 20071217 A 5314 656212518 KEELBEAM BOEING 737 7375H4 138449D NM BS 487B CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BDRG CHECK, FOUND RT KEEL BEAM CORRODED AT BS 487B. REPAIRED KEEL BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700152 20071227 00152 NM 2007 12 27 SWAA076297 1 20071217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 360 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007122700153 20071227 00153 NM 2007 12 27 SWAA076284 1 20071217 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700161 20071227 00161 NM 2007 12 27 SWAA076313 1 20071217 A 5553 6547450 FITTING BOEING 737 7373G7 1384595 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND RT VERTICAL STABILIZER LUG FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700162 20071227 00162 NM 2007 12 27 SWAA076315 1 20071217 A 5340 6545819 ATTACH FITTING BOEING 737 7373G7 1384595 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND NLG W/W LT SNUBBER ATTACHMENT CRACKED AT LBL 7.75. REPAIRED ATTACHMENT PER ACO. 2 L 7 2 4F RT A16WE 2007122700168 20071227 00168 NM 2007 12 27 SWAA076287 1 20071217 A 5311 6546595 FRAME BOEING 737 7373TO 138447G NM BS 727A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700180 20071227 00180 SO 2007 12 27 C2XA07ON040 1 20071218 A 2120 UNKNOWN EMB 145 EMB145 3260210 SO CABIN ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16559 145603 FLIGHT 615 - RDU TO JAX - FLIGHT CREW REPORTED BURNING PLASTIC ODOR IN COCKPIT FROM PACK 1 & AUTO PRESSURE FAIL. CONTRA CT MX TAC-AIR PERFORMED OPERATIONAL CHECK OF PACK 1 AND COULD NOT DUPLICATE ODOR AND MEL AUTO PRESSURE CONTROL. OPEN 2 L 7 2 4F RT T00011AT 2007122700181 20071227 00181 NM 2007 12 27 BB07099 1 20071218 A 3397 WIRE BOEING 767 7672B7 1385107 NM EMERGENCY LIGHTS BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 255AY 25257 MAINTENANCE FOUND FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE FOR THREE SECTIONS ON A/C RIGHT SIDE. REPAIRED WIRING. NO F URTHER FAULTS. 2 L 7 2 4F RT A1NM 2007122700190 20071227 00190 NM 2007 12 27 USAA920071346 1 20071206 A 5311 651630219 FRAME BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C-16 CHECK - A CRACK FOUND ON FUSELAGE FRAME BS 188, LBL 31, WL 207. REMOVED DAMAGE AND INSTALLED FILLER IAW B737-300 SRM 53-00-07-2R11. 2 L 7 2 4F RT A16WE 2007122700200 20071227 00200 NM 2007 12 27 USAA920071355 1 20071218 A 5754 SKIN BOEING 757 7572B7 1384964 NM NR 8 SLAT DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU A2762 27810 MCN - MAJOR REPAIR - C-4 CHECK - DENT ON UPPER OUTBOARD SKIN OF NR 8 SLAT TRAILING EDGE AT NR 8 SLAT STA 569. REPAIRED NR 8 SLAT IAW B757-200 SRM 51-70-10 REPAIR 2 FIG 203. 2 L 7 2 4F RT A2NM 2007122700201 20071227 00201 NM 2007 12 27 USAA920071356 1 20071219 A 5753 SKIN BOEING 737 7374B7 1384702 NM TE FLAP WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 442US BN1272 24841 CLT - MAJOR REPAIR - C-6 CHECK - WORN ON UPPER SKIN, AFT ROLLER ARM OF RIGHT INBOARD AFT FLAP. REMOVED AND INSTALLED RI GHT INBOARD AFT FLAP ASSEMBLY IAW B737-300 AMM 27-51-11. 2 L 7 2 4F RT A16WE 2007122700202 20071227 00202 EU 2007 12 27 USAA920071357 1 20071207 A 5321 D5367003400000 FLOOR PANEL AIRBUS 320 A320231 3930325 EU ZONE 200 DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 624AW 55 SAL - MAJOR REPAIR - C-6 CHECK - DELAMINATION ON CABIN FLOOR PANEL 241JF , BS 1869/FR42 - BS 2136/FR47, -Y254 - Y254. R EPLACED CABIN FLOOR PANEL 241JF, BS 1869/FR42 - BS 2136/FR47, -Y254 - Y254 IAW A320 SRM 53-02-00 TABLE 103 AND IRM 9701 REV F. 2 L 7 2 4F RT A28NM 2007122700203 20071227 00203 SO 2007 12 27 C2XA07TY086 1 20071220 A 3350 110049 BATTERY EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11107 145654 OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT NR 4 BATTERY POWER SUPPLY IAW EMB 145XR AMM 33-50- 04. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT 2007122800004 20071228 00004 2007 12 28 HALA0700543 4 20071225 A 2310 TRANSCEIVER BOEING 767 76733A 1385209 NM NR 2 HF SYS INOPERATIVE A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 ETOPS SIGNIFICANT SYSTEM, NR 2 HF RADIO WILL NOT TRANSMIT ON ANY FREQUENCIES ALSO DATA LINK IS INOP. NO SIDE TONE OR TU NING. T/S PER FIM 23-11-00 FIG 103 SYSTEM OPS TEST NORMAL ON GROUND PDX, SFO CONTACTED ON 5547 RESPONSE LOUD AND CLEAR. NO FAULTS ON BITE, CONTROL PANEL CHECKS OK. PER FAULT ISOLATION TIP REMOVED AND REPLACED F/O MIC. OPS CHECK NORMAL P RECAUTIONARY CHANGE. ACARS STATUS PAGE HF NR 2, NO FAULTS ON GROUND VOICE AND DATA MODE. 2 L 7 2 4F RT A1NM 2007122800009 20071228 00009 NM 2007 12 28 07FDEA05094 1 20071219 A 3150 WARNING LIGHT BOEING 727 727227 1384078 NM ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 492FE 21530 AFTER T/O AMBER AFT AIRSTAIR LIGHT ILLUMINATED. RAN QRH. AFTER LANDING LIGHT WENT OUT. REPLACED THE AFT AIRSTAIR SWI TCH ACTUATOR PER 727-200 MM 52-62-001-5, 52-70-001-5,OPS C. REPLACED ACTUATOR. COMPLIED WITH MTSI 52-62-9902. 2 L 7 3 4F A3WE 2007122800041 20071228 00041 NM 2007 12 28 HALA0700535 1 20071220 A 2910 LINE BOEING 767 767332 1382001 NM HYD SYSTEM CHAFED A HALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 13 598HA 23278 SUP - ATB - L PYLON HYDRAULIC LEAK DURING FLIGHT. IN LEFT ENGINE PYLON FOUND HYDRAULIC LINE TO HEAT EXCHANGER CHAFED TH ROUGH. REMOVED STRUT TRAILING EDGE FAIRING. REMOVED DAMAGED LINE. INSTALLED REPAIRED LINE. LEAK CHECK OK. INSTALLED LT STRUT TRAILING EDGE FAIRING. HYDRAULIC LINES REMOVED AND INSTALLED PER AMM 20-10-09. 2 L 7 2 4F RT A1NM 2007122800046 20071228 00046 NM 2007 12 28 AALA20072456 1 20071216 A 2750 18173812 TRANSMITTER BOEING 737 737823 13844BZ NM TE FLAPS INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 935AN 30081 IAD INFLIGHT T2187/16DEC DCA TO MIA - FLAPS STUCK AT FIVE DEGREES. LANDED IAD WITHOUT INCIDENT. REPLACED RIGHT FLAP LE VER POSITION TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007122800051 20071228 00051 NM 2007 12 28 07FDEA05088 1 20071219 A 5320 6517593 FLOOR SUPPORT BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 FWD LAV FLOOR STRUCTURE STA 312 RBL 41 SUPPORT ANGLE CORRODED ON LWR SURFACE. BLENDED CORROSION ON ANGLE. OUT OF LIMIT S. REMOVED, FABRICATED NEW ANGLE AND INSTALLED REF BOEING DWG 65-17593, SRM 51-10-2, SRM 53-10-2 AND SRM 51-30-02. THI S IS AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007122800056 20071228 00056 EU 2007 12 28 07FDEA05115 1 20071220 A 7540 9788422 VALVE AIRBUS 310 A310222 3930315 EU FAN AIR CRACKED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 448FE 9494 9494 260 DURING CLIMB TO CRUISE ALTITUDE, ECAM PRESENTED AN ADVISORY PAGE FOR NR 1 ENG NAC TEMP AT 200. SELECTED NR 1 BLEED VALV E OFF AND REDUCED POWER ON NR 1 WITH NO CHANGE IN NR 1 NAC TEMP. AFTER THROTTLE WAS REDUCED TO ALMOST IDLE SETTING, NR 1 NAC TEMP FELL TO 190 DEGREES. THROTTLE REMAINED AT IDLE UNTIL SHORT FINAL APPROACH. DURING DESCENT WITH NR 1 AT ID LE, ADVISORY INDICATION WENT AWAY AFTER 10-15 MINUTES OPEN ENGINE AND INSPECTED DUCTS, VALVES, CLAMPS ETC. FOUND A SMAL L CRACK ON FAN AIR VALVE, FOUND A COUPLE OF SENSE LINES TO BE BAD. REMOVED AND REPLACED FAN AIR VALVE, REMOVED AND REPL ACED SENSE LINES AND NACELLE TEMP SENSOR. OPS CHECK NORMAL A/C OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2007122800058 20071228 00058 EU 2007 12 28 07FDEA05104 1 20071219 A 5230 A52378014202 SKIN AIRBUS 310 A310203 3930313 EU CARGO DOOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 BULKPIT DOOR SKIN HAS TWO DENTS ON TOP OF DOOR CENTER. DENT OUT OF LIMITS. FABRICATED REPAIR PARTS IAW A310 SRM 52-30- 00. ALODINED, PRIMED, INSTALLED AND PAINTED REPAIR IAW A310 SRM 51-21-00, 51-23-10, 51-40-21 AND 51-23-20. 2 L 7 2 4F RT A35EU 2007122800059 20071228 00059 WP 2007 12 28 AALA20072458 1 20071216 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 456AA 49561 ORD INFLIGHT T1659/16DEC - NOSE LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. RETURNED TO ORD AND LANDED WITHOUT INCIDENT . FOUND STRUT FLAT. REPACKED NOSE LANDING GEAR STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007122800069 20071228 00069 EU 2007 12 28 07FDEA05061 1 20071215 A 5270 ABS030901 SWITCH AIRBUS 310 A310203 3930313 EU ZONE 800 MISALIGNED A FDEA O OTHER N FALSE WARNING CR CRUISE 1 SO 25 402FE 201 FWD CARGO DOOR UNLOCK WARNING AND ECAM MESSAGE AT 18,000' AND PSID 7.0, SPEED 340 KTS. PREECEDING THE CARGO DOOR UNLOCK WARNING BY LESS THAN 1" WAS A LOUD "THINK" FROM UNDERSIDE OF AIRCRAFT. SLOWED TO 240 KTS, NO CHANGE. DEPRESSURIZED AN D DESCENDED AND PSID 4.0 THE WARNING DISAPPEARED. ADJUSTED FWD CARGO DOOR SWITCH 14WS IAW FEDEX A310-200 AMM 52-71-11, AND ACCOMPLISHED AN INSPECTION OF FWD CARGO DOOR SILL AND FRAME AREA. NO DISCREPANCIES NOTED IAW FEDEX A310-200 AMM 52-3 1-11. 2 L 7 2 4F RT A35EU 2007122800086 20071228 00086 WP 2007 12 28 UPS07851292 1 20071212 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 NO EMERGENCY LIGHTS ON PREFLIGHT CHECK, COCKPIT INSTRUMENT FLOODS AND COCKPIT DOME. REMOVED AND REPLACED EMERGENCY BATT ERY PACK. OPS CHECK NORMAL. REF DC8 MM 26-00. 2 L 7 4 4F RT 4A25 2007122800093 20071228 00093 NM 2007 12 28 2007UALA04995 1 20071205 A 3251 STEERING SYS BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NLG LACK OF LUBE A UALA D RETURN TO BLOCK W INADEQUATE Q C TX TAXI/GRND HDL 1 WP 29 376UA 24641 NOSE WHEEL STEERING BINDING WITH LEFT AND RIGHT TURNS. IT STUCK IN THE FULL RIGHT TURN. FOUND LUBRICATION NOT SUFFICIE NT. LUBED STEERING MECH AND COLLAR, SYSTEM OPERATED NORMALLY AFTER LUBE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122800095 20071228 00095 WP 2007 12 28 07FDEA05064 1 20071215 A 5610 WINDSHIELD DOUG MD10 MD1010F 3022112 WP COCKPIT FAILED A FDEA O OTHER C F.O.D. AP APPROACH 1 SO 25 385FE 46619 ON ARRIVAL IN KAFW, TOOK BIRDSTRIKE IN RT WINDSHIELD, SHATTERED OUTER PANEL. DECLARED EMERGENCY, LANDED UNEVENTFUL AF W FOUND RIGHT WINDSHIELD OUTER PANEL SHATTERED. NEEDS CHANGED OUT. REMOVED AND REPLACED RIGHT WINDSHIELD PER MM 56-11 -00-2. SEE OIL 56-10/9049 FOR MISC SEALANT APPLICATION, P/N NBA6045-502. 2 L 7 3 4F RT A22WE 2007122800100 20071228 00100 NM 2007 12 28 2007UALA05012 1 20071207 A 5753 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE TE FLAP GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 RT OTBD MID FLAP ASSY SN 1099 AT EXHAUST GATE MECHANISM FWD SPAR WEB HAS VERY DEEP GOUGES AROUND THE FORE FLAP ACTUATING LINK ASSY. MAJOR REPAIR ACCOMPLISHED: REMOVED INBD FWD SPAR AND REPLACED WITH NEW SPAR PN 65-50759 PER BACO RECOMMENDA TIONS. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122800102 20071228 00102 NM 2007 12 28 2007UALA05031 1 20071207 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR CUTOUT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 FOUND DOOR R2 UPPER HINGE CUTOUT HAS DAMAGE. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007122800103 20071228 00103 NE 2007 12 28 2007UALA05109 2 20071215 A 7261 CARBON SEAL BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE ENGINE LEAKING A UALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 WP 29 220UA CCWKAM4242 30223 222055 LANDED UNDER EMERGENCY CONDITIONS DUE TO REPORTED SMOKE IN THE CABIN. SLIDE RAFTS DEPLOYED AND AIRCRAFT EVACUATED ONCE CLEAR OF ACTIVE. NR 2 ENGINE REPLACED AT ORD DUE TO HEAVY METAL DEPOSITS ON MAGNETIC CHIP DETECTORS. TEARDOWN REVEALED A FAILURE OF NR 2 BEARING. BEARING FAILURE CAUSED LARGE CHIPS OF CARBON TO BE LIBERATED FROM NR 2 FRONT CARBON SEAL, A LLOWING OIL TO LEAK INTO THE HP COMPRESSOR. THIS WAS THE SOURCE OF THE CABIN SMOKE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007122800114 20071228 00114 NM 2007 12 28 2007UALA05117 1 20071215 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 727A BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 AFT PIT SHEAR TIE BROKEN STA 727A STR 20L TO 21L. MAJOR REPAIR ACCOMPLISHED: REPLACED WITH NEW SHEAR TIE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122800115 20071228 00115 NM 2007 12 28 2007UALA05120 1 20071215 A 3510 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE 1ST OBSERVERS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 FIRST OBSERVERS O2 MASK INOPERATIVE. REPLACED FO O2 MASK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007122800122 20071228 00122 EU 2007 12 28 2007UALA05128 1 20071214 A 2560 GIRT BAR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE DOOR 1R OBSTRUCTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 419UA 487 FOUND DOOR 1R WILL NOT DISARM. SPRAYED ICE RELEASE ON GIRT BAR ARMS. MECHANISM IS WORKING NOW. SHOULD PREVENT FURTHER FREEZE UP AS WELL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007122800123 20071228 00123 EU 2007 12 28 2007UALA05129 1 20071214 A 3350 BULB AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 421UA 500 EMERGENCY LIGHT TEST FAILED, SHOWING EXTERNAL FAULT LEFT. FOUND BULB BURNED OUT. RELAMPED AND TEST PASSES. 2 L 7 2 4F 4 F RT A28NM E40NE 2007122800129 20071228 00129 EU 2007 12 28 TRAX200701902 1 20071210 A 5320 ANGLE AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 ANGLE CRACK ON LT O/B FUSELAGE FR 23D, BRACKET FIXED ON FUSELAGE SKIN. 2 H 7 2 4T RT A53EU 2007122800134 20071228 00134 NM 2007 12 28 TSAA0729066 1 20071216 A 2917 3141602 REGULATOR BOEING 737 737236 1384476 NM HYD SYSTEM MALFUNCTIONED A TSAA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 WP 13 828AL 23168 FLIGHT 208 HNL-OGG - UPON RETRACTION OF THE LANDING GEAR AND FLAPS, THE CREW NOTED A LOUD FLUTTERING NOISE AND BUFFET. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC RESERVOIR AIR PRESSURE RE GULATOR PER AMM 29-09-341 AND THE HYDRAULIC RESERVOIR PRESSURE RELIEF VALVE PER AMM 29-09-351. ALL OPERATIONAL AND LEAK CHECKS FOUND SATISFACTORY. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2008010200001 20080102 00001 EA 2008 1 2 COMA0760686 1 20071203 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 588SW 7069 FLIGHT 5391 - AFTER TAKEOFF RECEIVED GEAR DISAGREE AND NOSE DOORS OPEN MESSAGES. DECLARED EMERGENCY AND LANDED CHS WITH OUT INCIDENT. REPLACED NOSE GEAR PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2008010200003 20080102 00003 NE 2008 1 2 COMA0760688 2 20071204 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30068 NE LEFT FLAMED OUT A COMA D RETURN TO BLOCK X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 SO 01 931CA 7037 FLIGHT 5672 - LEFT ENGINE FLAMED OUT DURING START. FOUND THAT THE PREVIOUS ENGINE START HAD A TAILWIND OF APPROXIMATELY 40 KTS. DRY MOTORED ENGINE AND PERFORMED 2 ENGINE STARTS WITH NO FAULTS. 2 L 7 2 4F 4 F RT A21EA E15NE 2008010200009 20080102 00009 EA 2008 1 2 COMA0760692 1 20071205 A 2170 PA096 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA A/C BAY DIRTY A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 917CA 7017 FLIGHT 5603 - IMMEDIATELY AFTER TAKEOFF, SMOKE TOILET CAUTION MESSAGE DISPLAYED. FOLLOWED QRH PROCEDURE. AFT PAX REPOR TED SMOKE SMELL. AIRCRAFT RETURNED TO JFK AND LANDED SAFELY. REMOVED AND REPLACED COALESCER BAG. 2 L 7 2 4F RT A21EA 2008010200011 20080102 00011 EA 2008 1 2 COMA0760694 1 20071205 A 2760 4916405 SECU CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 785CA 13387 4916405 FLIGHT 5151 - ON TAKEOFF ROLL RECEIVED CONFIG SPOILERS MESSAGE WITH FLIGHT SPOILER MESSAGE. ABORTED TAKEOFF AND RETURNE D TO GATE SAFELY. REMOVED AND REPLACED NR 2 SECU. 2 L 7 2 4F RT A21EA 2008010200012 20080102 00012 EA 2008 1 2 COMA0760695 1 20071205 A 2752 1104SD100401 FLEX DRIVE CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP WORN A COMA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 01 806CA 7359 FLIGHT 5675 - FLAPS FAIL CAUTION MESSAGE. FLAPS FAILED AT 0 DEGREES ON APPROACH INTO DCA. AIRCRAFT DIVERTED TO IAD AND LANDED SAFELY. REMOVED AND REPLACED RIGHT FLAP SYSTEM NR 4 FLEX SHAFT. 2 L 7 2 4F RT A21EA 2008010200013 20080102 00013 EA 2008 1 2 COMA0760696 1 20071206 A 5230 DOOR SEAL CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR DEBONDED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 926CA 7027 FLIGHT 5208 - AIRCRAFT FAILED TO PRESSURIZE. NO EICAS INDICATIONS. RETURNED TO CVG, LANDED WITHOUT INCIDENT. RESEALED DEBONDED CARGO DOOR, SEALED DEBONDED CARGO DOOR SEAL. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008010200018 20080102 00018 EA 2008 1 2 COMA0770081 1 20071213 A 5414 CN6220201007 DOOR CNDAIR CL600 CL6002C10 1390015 EA LT ENGINE DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 374CA 11711 10090 LEFT ENGINE LOWER FAN COWL DOOR DENTED BEYOND LIMITS. REPAIRED LEFT ENGINE LOWER FAN COWL DOOR IAW REO 670-54-14-019. 2 L 7 2 4F RT A21EA 2008010200019 20080102 00019 NM 2008 1 2 ASAA0752382 1 20071214 A 2421 332A260012 IDG BOEING 737 737890 1384527 NM NR 1 ENGINE OVERSERVICED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 02 558AS 35177 NR 1 ENGINE IDG IS OVERSERVICED WITH OIL. RESERVICED NR 1 ENGINE IDG IAW AMM12 13 21. REMOVED 0.75QT. 2 L 7 2 4F RT A16WE 2008010200020 20080102 00020 NM 2008 1 2 ASAA0752383 1 20071214 A 2421 332A260012 IDG BOEING 737 737890 1384527 NM NR 2 ENGINE OVERSERVICED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 02 558AS 35177 NR 2 ENGINE IDG IS OVER SERVICED WITH OIL. RESERVICED NR 2 IDG IAW AMM12 13 21. REMOVED 0.50QT. 2 L 7 2 4F RT A16WE 2008010200024 20080102 00024 EA 2008 1 2 COMA0760698 1 20071207 A 3020 5399001 ANTI-ICE VALVE CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 812CA 213 7381 FLIGHT 5137 - ON CLIMBOUT FROM CVG TO YYZ RECEIVED LEFT COWL ANTI-ICE INOP MESSAGE. CREW DECLARED EMERGENCY AND RETURNE D BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED LEFT ENGINE COWL ANTI-ICE VALVE. 2 L 7 2 4F RT A21EA 2008010200027 20080102 00027 EA 2008 1 2 COMA0760701 1 20071208 A 2170 P1096 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA A/C BAY DIRTY A COMA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 971CA 7145 FLIGHT 5188 - SMOKE AND OIL SMELL IN CABIN. REMOVED AND REPLACED RIGHT PACK COALESCER BAG. 2 L 7 2 4F RT A21EA 2008010200028 20080102 00028 EA 2008 1 2 COMA0760702 1 20071209 A 3010 32144424 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYSTEM FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 917CA 15903 7017 FLIGHT 5964 - DURING CLIMBOUT FROM CVG RECEIVED ANTI-ICE DUCT WARNING. LEFT FUSELAGE RED ON ANTI-ICE PAGE. RAN QRH AND MESSAGE WENT OUT. A/C RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED LEFT MODULATION/SHUTOFF VALVE. 2 L 7 2 4F RT A21EA 2008010200032 20080102 00032 NM 2008 1 2 ASAA0752388 1 20071217 A 2421 332A260012 IDG BOEING 737 737890 1384527 NM NR 1 & 2 OVERSERVICED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 02 557AS 35176 NR 1 & NR 2 ENGINE IDG'S OVER SERVICED. DRAINED NR 1 & NR 2 ENGINE IDG'S TO TOP OF FULL BAND. REF: MM12 13 21. 2 L 7 2 4F RT A16WE 2008010200034 20080102 00034 NE 2008 1 2 ASAA0782386 2 20071213 A 7250 JT8D217C TURBINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217C 52053 NE RIGHT FAILED A ASAA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 NM 02 961AS 9406 53075 P726845D EN ROUTE SEA TO DEN RIGHTHAND ENGINE STARTED TO EXPERIENCE WHAT APPEARED TO BE COMPRESSOR STALLS. ENGINE WAS PURPOSELY SHUTDOWN AND THE FLIGHT WAS DIVERTED TO SLC. INSPECTION REVEALED TURBINE FAILURE. ENGINE WAS REPLACED. CAUSE OF FAILU RE TO BE DETERMINED AT TEARDOWN. 2 L 7 2 4F 4 F RT A6WE E9NE 2008010200035 20080102 00035 EA 2008 1 2 COMA0760706 1 20071211 A 3397 487191 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN FAULTY A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 962CA 7123 ROW 8 FLOOR EMERGENCY LIGHTING INOP. REPLACED ROW 5 EMERGENCY LIGHT JUMPER. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008010200036 20080102 00036 EA 2008 1 2 COMA0760707 1 20071211 A 3397 59465 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN CHAFED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 962CA 7123 ROW 8 FLOOR EMERGENCY LIGHTING INOP. REPAIRED CHAFED WIRE AT ROW 5 JUMPER. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008010200037 20080102 00037 EA 2008 1 2 COMA0760708 1 20071211 A 3397 487190 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN FAULTY A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 962CA 7123 ROW 8 FLOOR EMERGENCY LIGHTING INOP. REPLACED ROW 5 EMERGENCY LIGHT JUMPER. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008010200038 20080102 00038 EA 2008 1 2 COMA0760709 1 20071211 A 3320 BC10059003 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GALLEY BURNED A COMA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 01 967CA 7134 FLIGHT 5377 - NOTICED ELECTRICAL SMELL AND LIGHT SMOKE IN COCKPIT. REPLACED GALLEY LIGHT ASSEMBLY. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008010200040 20080102 00040 EA 2008 1 2 COMA0760711 1 20071211 A 5315 601R3111357 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 712CA 23431 7244 LONGITUDINAL FLOORBEAM ATTACH CLIP CRACKED AND HAS LOOSE FASTENERS, INBOARD SIDE OF BEAM FS 280, LBL 9. REMOVED AND REP LACED CLIP IAW CRJ SRM 51-42-21. 2 L 7 2 4F RT A21EA 2008010200042 20080102 00042 EA 2008 1 2 COMA0760713 1 20071212 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DAMAGED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 729CA 7265 FLOOR EMERGENCY LIGHTING INOP AT ROWS 2-6. ALSO ROW 8 FLUSH EMERGENCY EXIT SIGN INOP. REPAIRED BROKEN PIN ON POWER CON NECTOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008010200043 20080102 00043 EA 2008 1 2 COMA0760714 1 20071212 A 3350 59257 INVERTER CNDAIR CL600 CL6002B19 1900309 EA CABIN FAULTY A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 729CA 7265 FLOOR EMERGENCY LIGHTING INOP AT ROWS 2-6. ALSO, ROW 8 FLUSH EMERGENCY EXIT SIGN INOP. REPLACED INOP INVERTER. NO FUR THER DEFECTS. 2 L 7 2 4F RT A21EA 2008010200044 20080102 00044 EA 2008 1 2 COMA0760715 1 20071213 A 3010 355844255 SENSING ELEMENT CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYSTEM FAILED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 938CA 7046 FLIGHT 5485 - ON CLIMBOUT FROM CVG TO STL ANTI-ICE DUCT MESSAGE CAME ON WITH ANTI-ICE SELECTED ON. AIRCRAFT RETURNED BA CK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED RIGHT FUSELAGE FWD OVERWING HEAT SENSING ELEMENT. 2 L 7 2 4F RT A21EA 2008010200045 20080102 00045 EA 2008 1 2 COMA0760716 1 20071213 A 3097 3530358 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYSTEM WORN A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 590SW 7077 FLIGHT 5449 - ON CLIMBOUT FROM CVG TO DTW ANTI-ICE DUCT WARNING MESSAGE CAME ON WITH BOTH, WING AND COWLING ANTI-ICE SEL ECTED ON IN ICING CONDITIONS. AIRCRAFT RETURNED TO CVG AND LANDED SAFELY. REMOVED AND REPLACED FENWAL LOOP CONNECTOR A T FS 628 RIGHT SIDE. 2 L 7 2 4F RT A21EA 2008010200046 20080102 00046 EA 2008 1 2 COMA0760717 1 20071213 A 5330 601R35004441 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 779CA 7670 BAGGAGE CART STRUCK AIRCRAFT JUST AFT OF APU EXHAUST. CUT OUT DAMAGED SKIN FROM STA 694 TO STA 755 BETWEEN STRINGER 12 AND 13 TO STRINGER 20 AND REPLACED SKIN PER REO 601R-53-61-2444. 2 L 7 2 4F RT A21EA 2008010200050 20080102 00050 EA 2008 1 2 COMA0760721 1 20071213 A 5313 601R3500485 STRINGER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 779CA 7670 BAGGAGE CART STRUCK AIRCRAFT JUST AFT OF APU EXHAUST. REPLACED STRINGER 13 FROM STA 682 TO STA 755 PER SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008010200051 20080102 00051 EA 2008 1 2 COMA0760722 1 20071213 A 5313 601R3500473 STRINGER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 779CA 7670 BAGGAGE CART STRUCK AIRCRAFT JUST AFT OF APU EXHAUST. REPLACED STRINGER 14 FROM STA 682 TO STA 736 PER SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008010200052 20080102 00052 EA 2008 1 2 COMA0760723 1 20071213 A 5311 60036031112 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 779CA 7670 BAGGAGE CART STRUCK AIRCRAFT JUST AFT OF APU EXHAUST. REPLACED FRAME SECTION STA 736 PER SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008010200053 20080102 00053 EA 2008 1 2 COMA0760724 1 20071213 A 5311 6003602923 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 779CA 7670 BAGGAGE CART STRUCK AIRCRAFT JUST AFT OF APU EXHAUST. REPLACED FRAME SECTION STA 700 PER SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008010200054 20080102 00054 NM 2008 1 2 SWAA076346 1 20071218 A 5322 65353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 380, STR 25L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008010200055 20080102 00055 NM 2008 1 2 SWAA076347 1 20071218 A 5311 6546529 BELTFRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED BRDG CHECK, FOUND BELTFRAME CRACKED AT BS 500B, STR 20L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010200056 20080102 00056 NM 2008 1 2 SWAA076330 1 20071218 A 2750 65503245 TRANSMISSION BOEING 737 7373H4 1384600 NM T/E FLAP LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED C2 CHECK, FOUND LT WING NR 4 FLAP TRANSMISSION JACK SCREW LOOSE AT TRANSMISSION. REMOVED AND REPLACED TRANSMISSION AND JACK SCREW PER MM. 2 L 7 2 4F RT A16WE 2008010200057 20080102 00057 NM 2008 1 2 SWAA076331 1 20071218 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010200061 20080102 00061 NM 2008 1 2 SWAA076334 1 20071218 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1006, STR 5R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008010200065 20080102 00065 NM 2008 1 2 SWAA076339 1 20071218 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 485WN 32473 DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008010200069 20080102 00069 NM 2008 1 2 SWAA076349 1 20071218 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008010200070 20080102 00070 NM 2008 1 2 SWAA076351 1 20071218 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008010200071 20080102 00071 NM 2008 1 2 SWAA076352 1 20071218 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200072 20080102 00072 NM 2008 1 2 SWAA076348 1 20071218 A 5322 69353656 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008010200073 20080102 00073 NM 2008 1 2 SWAA076342 1 20071218 A 2560 6949956 CABLE BOEING 737 7373H4 1384600 NM L1 DOOR FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM. 2 L 7 2 4F RT A16WE 2008010200076 20080102 00076 NM 2008 1 2 SWAA076357 1 20071218 A 5312 6546568 STIFFENER BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CORRODED AT BS 1016, LBL 0.5. REPAIRED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2008010200078 20080102 00078 NM 2008 1 2 SWAA076354 1 20071218 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008010200079 20080102 00079 NM 2008 1 2 SWAA076355 1 20071218 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 14R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008010200081 20080102 00081 2008 1 2 SWAA076345 4 20071218 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 703SW 27837 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008010200084 20080102 00084 NM 2008 1 2 SWAA076383 1 20071219 A 5314 6562125 KEELBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED BRDG CHECK, FOUND LT KEEL BEAM CORRODED AT BS 523. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2008010200085 20080102 00085 NM 2008 1 2 SWAA076358 1 20071215 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 480, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008010200086 20080102 00086 NM 2008 1 2 SWAA076360 1 20071219 A 2560 6949956 CABLE BOEING 737 7373H4 1384600 NM EVAC SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM. 2 L 7 2 4F RT A16WE 2008010200087 20080102 00087 NM 2008 1 2 SWAA076361 1 20071219 A 2560 6949956 CABLE BOEING 737 7373H4 1384600 NM EVAC SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM. 2 L 7 2 4F RT A16WE 2008010200088 20080102 00088 NM 2008 1 2 SWAA076362 1 20071219 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010200090 20080102 00090 NM 2008 1 2 SWAA076364 1 20071219 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010200093 20080102 00093 NM 2008 1 2 SWAA076367 1 20071219 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 408WN 27895 EEPLS END CAP LOOSE AT ROW 1 ABC. SECURED END CAP PER MM. 2 L 7 2 4F RT A16WE 2008010200094 20080102 00094 NM 2008 1 2 SWAA076368 1 20071219 A 3350 65C27093 LIGHT BOEING 737 73776Q 13845AA NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 550WN 30279 R1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008010200097 20080102 00097 NM 2008 1 2 SWAA076371 1 20071219 A 5754 65C26602311A SLAT BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED AT OUTBOARD CORNER. REMOVED AND REPLACED SLAT PER M M. 2 L 7 2 4F RT A16WE 2008010200099 20080102 00099 2008 1 2 SWAA076373 4 20071219 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008010200101 20080102 00101 NM 2008 1 2 SWAA076381 1 20071219 A 5530 6546872 FITTING BOEING 737 7373G7 1384595 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND LT VERTICAL STABILIZER AFT INBOARD FAIL SAFE FITTING CORRODED. REMOVED AND REPLACED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008010200103 20080102 00103 2008 1 2 SWAA076380 4 20071217 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 708SW 27842 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008010200104 20080102 00104 2008 1 2 SWAA076375 4 20071219 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 756SA 27872 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008010200105 20080102 00105 NM 2008 1 2 SWAA076376 1 20071219 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 783SW 29809 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008010200106 20080102 00106 NM 2008 1 2 SWAA076377 1 20071219 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 797MX 27890 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008010200107 20080102 00107 NM 2008 1 2 SWAA076378 1 20071219 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 797MX 27890 DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK P ER MM. 2 L 7 2 4F RT A16WE 2008010200108 20080102 00108 NM 2008 1 2 SWAA076379 1 20071219 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 797MX 27890 DURING SCHEDULED HC1 CHECK, RT OVERWING EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008010200109 20080102 00109 NM 2008 1 2 SWAA076384 1 20071220 A 3350 3071BPEGPL LIGHT BOEING 737 737705 13844SC NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 271LV 29090 DURING SCHEDULED HC2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008010200114 20080102 00114 NM 2008 1 2 SWAA076411 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200115 20080102 00115 NM 2008 1 2 SWAA076410 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200118 20080102 00118 NM 2008 1 2 SWAA076407 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200121 20080102 00121 NM 2008 1 2 SWAA076408 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200122 20080102 00122 NM 2008 1 2 SWAA076402 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200123 20080102 00123 NM 2008 1 2 SWAA076401 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200124 20080102 00124 NM 2008 1 2 SWAA076400 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200129 20080102 00129 NM 2008 1 2 SWAA076413 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200131 20080102 00131 NM 2008 1 2 SWAA076425 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200132 20080102 00132 NM 2008 1 2 SWAA076424 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200133 20080102 00133 NM 2008 1 2 SWAA076423 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200134 20080102 00134 NM 2008 1 2 SWAA076422 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200137 20080102 00137 NM 2008 1 2 SWAA076421 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200142 20080102 00142 NM 2008 1 2 SWAA076419 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200144 20080102 00144 NM 2008 1 2 SWAA076385 1 20071220 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 325SW 23689 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008010200145 20080102 00145 2008 1 2 SWAA076386 4 20071220 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008010200146 20080102 00146 NM 2008 1 2 SWAA076387 1 20071218 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505D, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008010200147 20080102 00147 NM 2008 1 2 SWAA076388 1 20071220 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 425LV 29829 EEPLS ASSY LOOSE AT ROW 1 ABC. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008010200148 20080102 00148 NM 2008 1 2 SWAA076389 1 20071220 A 2560 65C16820 HOOK BOEING 737 7377H4 1384404 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 425LV 29829 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2008010200149 20080102 00149 NM 2008 1 2 SWAA076390 1 20071220 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 451WN 32495 DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS CRACKED AT ROW 4 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008010200150 20080102 00150 NM 2008 1 2 SWAA076391 1 20071220 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 452WN 29846 EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008010200151 20080102 00151 NM 2008 1 2 SWAA076394 1 20071220 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 486WN 33852 DURING SCHEDULED HC1 CHECK, RT OVERWING EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PAC KS PER MM. 2 L 7 2 4F RT A16WE 2008010200153 20080102 00153 NM 2008 1 2 SWAA076393 1 20071220 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 486WN 33852 DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008010200154 20080102 00154 NM 2008 1 2 SWAA076395 1 20071220 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER 4L CRACKED AT BS 867. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008010200156 20080102 00156 NE 2008 1 2 ASAA0752391 2 20071221 A 7261 CFM567B27 OIL SYSTEM BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE NR 1 & 2 ENGINE LOW A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 587AS 35684 PILOT REPORTED OIL LEVELS LOW BOTH ENGINES. NR 1 ENGINE ADDED 4.5QTS NR 2 ENGINE ADDED 5.5 QTS. APU FULL ADDED 0. 2 L 7 2 4F 4 F RT A16WE E00055EN 2008010200157 20080102 00157 WP 2008 1 2 ASAA0782392 1 20071218 A 5330 591007127 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 982AS 53473 FUSELAGE SKIN DENTED BY JETWAY. REPLACED DAMAGED SECTION OF SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-04-12B. 2 L 7 2 4F RT A6WE 2008010200158 20080102 00158 2008 1 2 ASAA0752390 4 20071219 A 3460 1762000101 FMC BOEING 737 737890 1384527 NM E&E BAY FAILED A ASAA K NONE J WARNING INDICATION CR CRUISE 1 NM 02 587AS 564 35684 AT TOP OF DESCENT "VTK" FLAG APPEARED ON LEFT EFIS DISPLAY. BOTH FMC DISPLAYS DEFAULTED TO THE "MENU" PAGE. THREW FMC SWITCH TO "BOTH ON RIGHT" MESSAGE NOTE OF "SINGLE FMC OPS" FOLLOWED BY "DUAL FMC OPS RESTORED". RETURNED FMC SWITCH TO "NORMAL". OPS NORMAL. BOTH LT & RT FMC COMPUTERS LOGGED "L FMC FAILED". DEFERRED MAINTENANCE. LT FMC ON MEL PENDING ENGINEERING EVALUATION. REMOVED AND REPLACED LEFT FMC PER AMM REF 34 61 02 2 L 7 2 4F RT A16WE 2008010200159 20080102 00159 2008 1 2 ASAA0752393 4 20071219 A 3460 1762000101 FMC BOEING 737 737890 1384527 NM E&E BAY FAILED A ASAA K NONE J WARNING INDICATION CR CRUISE 1 NM 02 587AS 35684 RIGHT AT TOP OF DESCENT "VTK" FLAG APPEARED ON LEFT EFIS DISPLAY. BOTH FMC'S DEFAULTED TO THE "MENU" PAGE. THREW FMC S WITCH TO "BOTH ON RIGHT". MESSAGE NOTE OF "SINGLE FMC OPS" FOLLOWED BY "DUAL FMC OPS RESTORED". RETURNED FMC SWITCH TO "NML" AND ALL FMC EFIS HAD NORMAL DISPLAYS. REPLACED LEFT FMC PER 34-61-02. OP CHECKS GOOD. REFERENCE PREVIOUSLY SUB MITTED SDR ASAA0752390. 2 L 7 2 4F RT A16WE 2008010200162 20080102 00162 NM 2008 1 2 ASAA0772394 1 20071206 A 5320 146A75031 FLOOR SUPPORT BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT BS 767+5 TO BS 767+14 FLOOR SUPPORT RAIL LBL 3 CORRODED. REPAIR WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008010200163 20080102 00163 NM 2008 1 2 ASAA0772395 1 20071206 A 5320 146A75035 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT BS 767+5 LBL 8 SUPPORT RAIL CORRODED. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008010200168 20080102 00168 NM 2008 1 2 ASAA0772402 1 20071205 A 5321 453A261017 FLOOR PANEL BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT FLOOR PANEL BS 767+6 TO 887 CORRODED ALONG EDGES. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008010200169 20080102 00169 NM 2008 1 2 ASAA0772403 1 20071205 A 5320 141A851228 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 E & E COMPT DOOR INTERCOSTAL WEB BS 330 RBL 15.47 GOUGED. E & E COMP DOOR SURROUND RT INTERCOSTAL WEB AT BS 330 RBL 15. 47 REPLACED IAW B737 700 SRM 51-40-02 & SRM 53 10 15 01 03. 2 L 7 2 4F RT A16WE 2008010200170 20080102 00170 NM 2008 1 2 ASAA0772404 1 20071205 A 5320 143A812619 INTERCOSTAL BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 FWD CARGO PIT FLOOR SUPPORT INTERCOSTAL BS 492 TO BS 500A RBL 25 CORRODED. REPAIR WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008010200175 20080102 00175 WP 2008 1 2 AMTA200700619 1 20071115 A 5210 BOTTLE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL L1 DOOR BLOWN A AMTA K NONE O OTHER TX TAXI/GRND HDL 1 GL 11 705TZ 46915 DOOR 1L BLEW THE BOTTLE. RESERVICED L1, DOOR RESERVOIR IAW MM 52-10-01, CYLINDER, PSI NOW GOOD. (K) 2 L 7 3 4F 4 F A22WE A23EA 2008010200176 20080102 00176 EA 2008 1 2 TRAX200701849 1 20071201 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 AAR-2069 - LEFT O/B 484 I/B CLIP CRACKED, RESOLVED ON W/O: 75508 TASKCARD: N/R-00107. REMOVED DAMAGED CLIP AT 484 LEFT O/B - I/B CLIP AND FABRICATED NEW PART FROM 2024T3.063 IAW REO 601R-53-41-059. (13225) 12-4-07. AAR-338. CLIP REQUIRES NOT PERFORMED LPI ON FABRICATED CLIP FOR LT O/B 484 I/B SIDE IAW REO 601R-53-41-059 AND NDTM 51-20-08. NO DEFECTS NOTED (13311) 12-4-07. AAR-338. INSTALLED CLIP IAW REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2008010200178 20080102 00178 EA 2008 1 2 TRAX200701890 1 20071208 A 3350 BATTERY CNDAIR CL600 CL6002C10 1390015 EA CABIN READS LOW A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 722EV 10127 EMERGENCY BATTERY NR 3 AND NR 4 READING LOW VOLTAGE. 2 L 7 2 4F RT A21EA 2008010200179 20080102 00179 NE 2008 1 2 DL777071603 2 20071209 A 7200 TRENT89517 ENGINE BOEING 777 777232 1385232 NM RROYCE RB211 RB211TRENT89 NE NR 1 MAKING METAL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 866DA 26114 29738 051156 NR 1 ENGINE, FOUND SMALL QUANTITY OF FINDS ON THE MASTER CHIP DETECTOR. RAN ENGINE PER PFHB. FOUND METAL ON NR 1 ENG C HIP DETECTOR AND EGB AND SAGB CHIP DETECTORS 984543. DUE NR 1 ENGINE CHANGE. REPLACED NR 1 ENGINE PER TRANS 11T003. 2 L 7 2 4F 4 F RT T00001SE E00050EN 2008010200180 20080102 00180 EU 2008 1 2 DHLA200700081 1 20071212 A 3242 AUTOBRAKE SYS AIRBUS 300 A300B4203 3930306 EU MALFUNCTIONED A DHLA K NONE O OTHER LD LANDING 1 GL 05 367DH 265 DURING ROLL OUT WITH AUTOBRAKES ENGAGE (MIN) AFTER PRESSING BRAKES AUTO BRAKES CONTINUED TO BRAKE THE AIRCRAFT EVEN WITH THE AUTO BRAKE OFF LIGHT ILLUMINATED AND NO PRESSURE ON BRAKE PEDALS. PERFORMED OPERATIONAL CK OF AUTOBRAKE AND LIFT D UMPING CKS NORMAL IAW M/M 32-45-54. 2 L 7 2 4F RT A35EU 2008010200181 20080102 00181 EU 2008 1 2 TRAX200701826 1 20071128 A 5260 STEP AEROSP ATR72 ATR72212 8680945 EU PAX DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 CORROSION ON STEP OF STAIRSCASE, PAX DOOR RESOLVED ON W/O: 75891TASKCARD: N/R-00406. CORROSION ON STEPS OF STAIR CASE, PAX DOOR REMOVED IAW SRM 51-21-42. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APP ENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42 MATERIAL THICKNESS: 0.040 MATERIAL REMOVED: 0.003 WITHIN L IMITS AS PER SRM: 51-10-10. 2 H 7 2 4T RT A53EU 2008010200182 20080102 00182 EU 2008 1 2 TRAX200701827 1 20071128 A 5260 SUPPORT ANGLE AEROSP ATR72 ATR72212 8680945 EU STAIRCASE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 CORROSION ON AFT STAIR CASE SUPPORT ANGLE FLANGE, RESOLVED ON W/O: 75891 TASKCARD: N/R-00409. CORROSION ON AFT STAIR CA SE SUPPORT ANGLE FLANGE REMOVED IAW SRM 51-21-42. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 66 3 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42 MATERIAL THICKNESS: 0.050 MATERIAL REMOVE D: 0.002 WITHIN LIMITS AS PER SRM: 51-10-10. 2 H 7 2 4T RT A53EU 2008010200183 20080102 00183 EU 2008 1 2 TRAX200701833 1 20071129 A 5315 DOUBLER AEROSP ATR72 ATR72212 8680945 EU FLOORBEAM CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 DOUBLER FOUND CORRODED OUT OF LIMITS ON W/C 100-43 NEEDS TO BE FABRICATED (RESOLVED ON W/O: 75891 TASKCARD: N/R-00648 ) DOUBLER ON FLOORBEAM 40 AT LBL 10. FABRICATED IAW SRM 51-24-01, INSTALLATION COVER ON W/C 100-43. 2 H 7 2 4T RT A53EU 2007122800081 20071228 00081 SO 2007 12 28 SIMA200735101 1 20071215 A 3350 14521325405 CONTROL PANEL EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHTS MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 853AE 145742 ON CLIMB-OUT THREW FL240 ON EICAS MESSAGE "EMER LT NOT ARMED" AND "ELEC EMER ABNORMAL". RAN CHECK LIST PER AOM VOL 1. CREW ELECTED TO RETURN TO LAX. DECLARED AN EMERGENCY. AIRCRAFT LANDED AND RETURNED TO THE GATE WITHOUT FURTHER INCIDEN T. FOLLOWED ETN EM-24-023 REMOVED AND REPLACED ELECTRICAL CONTROL PANEL IAW EMB EM 24-00-01. ALL REQUIRED CHECKS CHECK ED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007122800109 20071228 00109 NM 2007 12 28 2007UALA05115 1 20071215 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 1016 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 AFT LT LAV FLOOR STRUCTURE STA 1016 FLOORBEAM LBL5 WL 208 IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABR ICATED AND INSTALLED REPAIR ANGLE AND STRAP REPAIR. INSTALLED NEW INTERCOSTALS AT RBL 3" AND LBL 3". 2 L 7 2 4F 4 F RT A16WE E2GL 2007122800116 20071228 00116 NM 2007 12 28 2007UALA05121 1 20071216 A 5754 WEDGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 6 SLAT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 NR 6 L/E SLAT T/E WEDGE MISSING OTBD 8-12 INCHES. ALSO DAMAGE TO WING L/E UNDER SLAT. REPAIRED WING LE AND REPLACED NR 6 SLAT WITH A NEW ONE. AFTER RIGGING, OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007122800120 20071228 00120 NM 2007 12 28 2007UALA05126 1 20071216 A 3810 VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WATER SYS OPEN A UALA A UNSCHED LANDING W E INADEQUATE Q C VIBRATION/BUFFET CR CRUISE 1 WP 29 87UA 26713 FLIGHT DIVERTED DUE TO LOSS OF WATER PRESSURE AND VIBRATION ISSUES. WATER FILL VALVE WAS LEFT IN OPEN POSITION CAUSING BOTH WATER LOSS AND AFT AIRFRAME VIBRATION. SERVICED WATER SYSTEM AND CLOSED VALVE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007122800124 20071228 00124 WP 2007 12 28 IXXA07SMN265S 1 20071115 A 5542 SKIN DOUG DC8 DC873F 302199F WP ZONE 300 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT RUDDER RIGHT SKIN AT STATION ZR 150.000 TO STATION ZR 178.00 0. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKINS AND INTERNAL AND EXTER NAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. PERFORMED BALANCE TO RUDDER FOUND MOMENT WITHIN TOLERANCE MOMENT 2455 INCH/LB. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 55-6 -1 FIGURE 1, DC8 SRM 55-1-0 PAGE 1 AND SRM 51-1-21, DC8 SRM 55-6-1 FIGURE 1 ITEM "A", DC8 SRM 51-1-9 T/R 51-142 DATED 04 -05-06 AND DC8 SRM 51-1-9A T/R 51-141 DATED 04-03-06, DC8 SRM 51-1-8B, DC8 SRM 51-4-6 PAGES 1-6. DC8 SRM 51-1-11, AND 51 2 L 7 4 4F RT 4A25 2007122800126 20071228 00126 EU 2007 12 28 TRAX200701899 1 20071210 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 FOUND FLOORBEAM 41 CORRODED. 2 H 7 2 4T RT A53EU 2007122800133 20071228 00133 EU 2007 12 28 TRBA2007110 1 20071210 A 2612 FIRE WARNING AEROSP ATR72 ATR72212 8680945 EU FALSE INDICATION A TRBA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 29 308AE 309 APPROXIMATELY 3 TO 5 MINS AFTER STARTING ENG NR 1, AN ENG NR 1 FIRE INDICATION ON CAP, CONDITION LEVER NR 1 AND FIRE HAN DLE NR 1 ENGINE FIRE EMERGENCY PROCEDURES WERE PERFORMED. SPECIAL DVI AFTER ENGINE FIRE WAS PERFORMED IAW JIC NR 70-00- 00 SDI 10000. RE-CHECKED WIRES AND TESTED LT ENGINE LP VALVE SEVERAL TIMES WITH NR 1 FIRE HANDLE IAW JIC NR 28-24-00 AN D FOUND WORKING PROPERLY. GROUND RUN-UP PERFORMED IAW JIC NR 72-00-00 AND FOUND SATISFACTORY. ANALYZED AS A FALSE FIRE INDICATION. POSSIBLE HEAVY TAIL WIND WHILE TAXIING. 2 H 7 2 4T RT A53EU 2008010200185 20080102 00185 EA 2008 1 2 A6WA200740668 1 20071130 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 433AW 7289 LT AND RT ANGLES CRACKED ON REAR PRESSURE BULKHEAD AFT SURFACE. (M) LT AND RT ANGLES ON AFT PRESSURE BULKHEAD (AFT FAC E) AT FS 622, WL 73 TO 75, BTW STR 16 AND 17 INSTALLED AS IAW SRM 51-42-20. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008010200189 20080102 00189 EA 2008 1 2 A6WA200740640 1 20071115 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 427ZW 7685 LT MLG WHEEL WELL HYD SUPPORT BRACKET CRACKED. LT MLG WHEEL WELL HYD SUPPORT BRACKET REPLACED. 2 L 7 2 4F RT A21EA 2008010200193 20080102 00193 EA 2008 1 2 A6WA200740690 1 20071210 A 5280 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT MLG DOOR DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 432AW 7257 ON LT MLG DOOR INNER SKIN, FOUND ABRASION ON FORWARD SIDE OF DOOR, LOWER AND UPPER. (M) REPAIRED IAW REO 601R-52-82-0 16 AND REO 601R-52-82-102. (K) 2 L 7 2 4F RT A21EA 2008010200195 20080102 00195 NM 2008 1 2 ANCF200700032 1 20071215 A 3620 SENSE LINE BOEING 767 7673Y0 NM BLEED AIR SYS OUT OF ADJUST W ANCF C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 23 948AV 24948 PILOT REPORT:R ENG HPRSOV DISPLAYED THE CAUTION AND CHIME COME ON. IN ACCORDANCE WITH FIM 36-10-00 FIG 111, SENSE LINE AT RT HPRSOV CONTROLLER WAS ADJUSTED AND THEIR BLEED AIR CONTROL WAS CHECKED. 2 L 7 2 4F RT A1NM 2008010200197 20080102 00197 SO 2008 1 2 C2XA07CL107 1 20071225 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 48901 145501 DURING ROUTINE MAINTENANCE, THE OVERWING EXIT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008010300001 20080103 00001 EA 2008 1 3 TRAX200701911 1 20071211 A 5340 FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 472 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 903EV 7621 BATHTUB FITTING CRACKED AT FS 472 O/B OF RBL 9.00. REMOVED CRACKED BATHTUB FITTING, LOCATED NEW SERVICEABLE FITTING P/ N 600-31068-19 AND INSTALLED IAW CRJ 200 SRM 51-42-21. OK TO TOPCOAT FASTENERS. APPLIED TOPCOAT TO FASTENERS IAE CRJ SRM 51-21-16. 2 L 7 2 4F RT A21EA 2008010300002 20080103 00002 EA 2008 1 3 TRAX200701915 1 20071211 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA CABIN WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 758EV 10210 ASD "EXIT" PLACARD WORN. REMOVED AND REPLACED ASD "EXIT" PLACARD IAW CRJ 700 AMM 11-30-00. 2 L 7 2 4F RT A21EA 2008010300003 20080103 00003 EA 2008 1 3 TRAX200701925 1 20071213 A 5320 ANGLE CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 758EV 10210 RT VERTICAL STAB TO FUSELAGE ANGLE T/E CRACKED. NEEDS PAINT REMOVED FOR FURTHER EVALUATION. CRACK CONFIRMED IN RADIUS . CRACK LENGTH MARKED. 2 L 7 2 4F RT A21EA 2008010300014 20080103 00014 WP 2008 1 3 07FDEA05062 1 20071215 A 3610 8986264 VALVE DOUG DC10 DC1030F 3023504 WP PNEUMATIC SYS FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 301FE 46800 NEAR TOP OF CLIMB, NR 3 AIR SYS OFF LIGHT ILLUMINATED. NR 3 DUCT DISPLAYED RED MOMENTARILY UNTIL AUTO SHUTDOWN. DIVER TED DUE TO INABILITY TO USE WING ANTI-ICE VALVE - INOP CLOSED. DO NOT USE NR 3 PNEUMATIC SUPPLY SYSTEM." DECAY CHECK C/W PER M/M 36-00-01-5 PASS PER LIMITS CHECKED FAULT ISOLATION PANEL NO BALLS TRIP, ONLY FAULT WAS PRV. RELEASED FOR S ERVICE PER MEL/CDL: 36-12-01-A CATEGORY: C EXPIRATION: 25DEC07 "MEL 36-12-01-A: NR 3 PNEUMATIC PRESS REGULATOR VALVE. 2 L 7 3 4F RT A22WE 2008010300015 20080103 00015 EU 2008 1 3 07FDEA05063 1 20071214 A 7930 TRANSMITTER AIRBUS 300 A300F4605R 3930327 EU OIL PRESSURE FAILED A FDEA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 25 684FE 5794 2189 802 ON CLIMB-OUT, ECAM ADVISORY INDICATED NR 1 ENGINE ZERO OIL PRESSURE CONFIRMED WITH GUAGE WHICH INDICATED ZERO AS WELL. COMPLIED WITH QRH. SHUT NR 1 ENGINE DOWN. LANDED IND. REMOVED AND REPLACED NR 1 ENG. OIL PRESSURE TRANSMITTER IAW AM M 79-33-11-4-05. PERFORMED ENG POS-WINDMILLING INSP PER AMM 72-00-00-6-05. RAN ENG. APROX 3 TO 5 MINS AND ENG OIL PRE SSURE CHK'S GOOD AND NO LEAKS NOTED AT THIS TIME. 2 L 7 2 4F RT A35EU 2008010300016 20080103 00016 NE 2008 1 3 07FDEA05065 2 20071216 A 7320 UNKNOWN DOUG MD11 MD11F 3023600 NM GE CF6 CF680 30025 NE NR 2 ENGINE MALFUNCTIONED A FDEA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SO 25 587FE 48489 702853 NR 2 ENG RPM LO ON CLIMB-OUT (FLAMEOUT). CREW REPORTED DURING CLIMB-OUT NR 2 ENG N1 WENT TO 11 PERCENT WITH N2 ALMOST 0 PERCENT, LOW EGT, AND FF APPROX 600 PPM. INSP NR 2 ENG INLET AND EXH FOR METAL PARTICLES AND FOD. NO DEFECTS NOTED. CHKD NR 2 ECU, NO FAULTS FOUND IN BOTH CHNLS A AND B. PERFORMED RTS ON NR 2 ECU CHNLS A AND B. ALL TESTS PASSED. PE RFORMED NR 2 ENG RUN, NRML ENG START. PERFORMED HIGH PWR RUN AT 70 PERCENT N1 ON ALL 3 ENG. RECEIVED SAME READINGS ON ALL 3 ENGS WENT DOWN TO IDLE AND RAN NR 2 ENG AT 85 PERCENT N1 BACK TO IDLE AND WENT UP TO 100 PERCENT N1. NR 2 ENG IN D NML AND STEADY WHOLE TIME. WENT BACK TO IDLE AND RETURNED TO GATE. ENG RUNS PERFORMED BY FLT CREW. R & R NR 2 ENG E 2 L 7 3 4F 4 F RT A22WE E13NE 2008010300017 20080103 00017 NM 2008 1 3 07FDEA05066 1 20071217 A 5320 ADJ70982 CHANNEL DOUG MD11 MD11F 3023600 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 524FE 48480 FORWARD CARGO COMPARTMENT: STA 959 TO STA 979 X = -40 CHANNEL DOLLY ASSEMBLY RETRACTOR, MOUNTING HOLE FOUND DAMAGED. CO MPLIED WITH FEDEX EA. 1-5340-117082. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008010300018 20080103 00018 NM 2008 1 3 07FDEA05067 1 20071217 A 5320 A6J700812 CHANNEL DOUG MD11 MD11F 3023600 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 524FE 48480 FORWARD CARGO COMPARTMENT: STA 6-70 X = -40 CHANNEL DOLLY ASSEMBLY END STOP MOUNTING AREA FOUND DAMAGED. DAMAGED. COMPL IED WITH FEDEX E.A.1-5340-117081. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008010300019 20080103 00019 NM 2008 1 3 07FDEA05068 1 20071217 A 5320 A6J700812 CHANNEL DOUG MD11 MD11F 3023600 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 524FE 48480 FORWARD CARGO COMPARTMENT: STA 6-70 X = 40 CHANNEL DOLLY ASSEMBLY END STOP MOUNTING AREA FOUND HOLE ELONGATED. COMPLIED WITH FEDEX E.A.1-5340-117081. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008010400002 20080104 00002 EA 2008 1 4 TRAX200701930 1 20071212 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 903EV 7621 WEB CRACKED OB OF LBL 9 UNDER PARKING BRAKE PULLEY HOUSING. 2 L 7 2 4F RT A21EA 2008010400003 20080104 00003 EA 2008 1 4 TRAX200701931 1 20071214 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 844AS 7317 NR 3 EPSU BATTERY PACK IS DEAD. 2 L 7 2 4F RT A21EA 2008010400004 20080104 00004 EA 2008 1 4 TRAX200701932 1 20071214 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 844AS 7317 NR 4 EPSU BATTERY PACK IS DEAD. 2 L 7 2 4F RT A21EA 2008010400006 20080104 00006 EA 2008 1 4 TRAX200701856 1 20071201 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 FS 280 RBL 9 INBOARD AND OUTBOARD ANGLES ARE CRACKED. REMOVED INBOARD/OUTBOARD CLIPS AT FS 280.00 RBL 9.00 DISCARDED DU PLICATED NEW CLIPS. INSTALLED IAW REO 601R-53-11-171 9, REQUIRES FILLET SEAL/TOPCOAT. FILLET SEALED IAW 51-23-00 AND T OPCOATED IAW 51-25-16. FOUND TWO CLIP NUTS MISSING AND INSTALLED TWO SERVICEABLE CLIP NUTS, COMPLIED WITH ASA EO 600-53 -90 RII 5000528. 2 L 7 2 4F RT A21EA 2008010400008 20080104 00008 EU 2008 1 4 TRAX200701934 1 20071214 A 3350 COVER AEROSP ATR72 ATR72212 8680945 EU EXIT SIGN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 FLT 4268 - LEFT FWD LOWER EXIT SIGN IS MISSING COVER. 2 H 7 2 4T RT A53EU 2008010400011 20080104 00011 EA 2008 1 4 TRAX200701937 1 20071215 A 7931 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INTERMITTENT A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 921EV 7819 ON DEPARTURE OUT OF ATL, RECEIVED A "RENG MOIL PRESS" INTERMITTENTLY. COMPLIED WITH QRH AND EVENTUALLY SHUT DOWN THE R IGHT ENG, A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. EMERGENCY EQUIPMENT ON STANDBY. 2 L 7 2 4F RT A21EA 2008010400014 20080104 00014 EU 2008 1 4 TRAX200701940 1 20071215 A 3350 LIGHT AEROSP ATR72 ATR72212 8680945 EU CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 TWO MINUTE LIGHT WILL NOT EXTINGUISH. 2 H 7 2 4T RT A53EU 2008010400015 20080104 00015 EA 2008 1 4 TRAX200701912 1 20071211 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 903EV 7621 CLIP CRACKED O/B OF LBL 27, RESOLVED ON W/O: 77977 TASKCARD: N/R-00247. REMOVED CRACKED FS 487 LBL 27 O/B CLIP. FABRIC ATED SERVICEABLE CLIP FROM S6144-3 ANGLE IAW CRJ 200 SRM 53-41-43. OK TO ALODINE, PRIME, AND TOPCOAT. INSTALLED SERVIC EABLE CLIP IAW CRJ SRM 51-42-21 JM 14031. OK TO TOPCOAT FASTENERS. APPLIED TOPCOAT TO FASTENERS IAW CRJ 200 SRM 51-21- 16 JM 14031 12/15/07. 2 L 7 2 4F RT A21EA 2008010400016 20080104 00016 EA 2008 1 4 TRAX200701913 1 20071211 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 903EV 7621 CLIP CRACKED INBOARD OF LBL 36, RESOLVED ON W/O: 77977 TASKCARD: N/R-00248. REMOVED CRACKED FS 484 CLIP INBOARD OF LBL 36. FABRICATED SERVICEABLE CLIP FROM 2024T-3 .063 IAW CRJ SRM 51-24-16. OK TO ALODINE, PRIME, ABD TOPCOAT. APPLIED FIN ISH TO CLIP IAW CRJ 200 SRM 51-16-21. INSTALLED SERVICEABLE CLIP IAW CRJ SRM 51-42-21. OK TO TOPCOAT FASTENERS. APPLI ED TOPCOAT TO FASTENERS IAW CRJ 200 SRM 51-16-21 JM 14031 12/15/07. 2 L 7 2 4F RT A21EA 2008010400018 20080104 00018 SO 2008 1 4 C2XA07ON043 1 20071220 A 2130 PRESSURE SYSTEM EMB 145 EMB145XR 3260214 SO CABIN MALFUNCTIONED A C2XA K NONE O OTHER CR CRUISE 1 SW 27 14180 14500900 FLT 7657 - ZLO TO LAX - DURING CRUISE FLIGHT CREW REPORTED AIRCRAFT LOST PRESSURIZATION IN AUTO MODE AT FL 350. MX REMO VED AN REPLACED AUTO PRESSURIZATION CONTROLLER OPERATIONALLY CHECKED SATISFACTORY. A/C WAS RELEASED TO RETURN FOR SERVIC E 2 L 7 2 4F RT 2008010400022 20080104 00022 SO 2008 1 4 C2XA07ON035 1 20071206 A 4910 450113A INLET EMB 145 EMB145XR 3260214 SO APU OBSTRUCTED A C2XA D RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 11176 8630 8630 145881 FLIGHT 7735 - GEG TO LAX - FLIGHT CREW REPORTED DURING TAXI APU HIGH TEMP AND APU FIRE INDICATION ON EICAS. SPOKANE AIR WAY CONTRACT MECHANICS REMOVED ICE FROM APU INLET AND VERIFIED NORMAL OPERATION. A/C WAS RELEASE IN AIRWORTHY CONDITION S TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008010400027 20080104 00027 SO 2008 1 4 C2XA07IA252 1 20071220 A 3230 LANDING GEAR EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A C2XA K NONE O OTHER CL CLIMB 1 SW 27 12924 145311 FLIGHT 2412 - DGO - IAH, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO DGO AND LAN DED WITHOUT INCIDENT. THE AIRCRAFT WAS REPOSITIONED TO IAH WHERE LANDING GEAR EXTENSION AND RETRACTION TESTS WERE PERFO RMED. THE GEAR RETRACTED AND EXTENDED NORMALLY DURING THE SYSTEM TESTS AND THE DISCREPANCY WAS CLEARED. 2 L 7 2 4T RT T00011AT 2008010400028 20080104 00028 SO 2008 1 4 C2XA07IA248 1 20071216 A 5730 14567011003 SKIN EMB 145 EMB145EP 3260221 SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15932 145015 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED A CRACK IN THE UPPER RT WING SKIN. THE CRACK WAS INSPECTED AND PLA CED ON A 500 FLIGHT CYCLE DEFERRAL IN ACCORDANCE WITH EMBRAER IC2007-145/08976, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008010400029 20080104 00029 SO 2008 1 4 C2XA07IA247 1 20071214 A 3260 852701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO NLG INOPERATIVE A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 15980 145202 IAH - FLIGHT 2173, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL ON TAKEOFF. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS PROXIMITY SENSOR, OPER ATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008010400030 20080104 00030 SO 2008 1 4 C2XA07IA249 1 20071216 A 5730 14537011003 SKIN EMB 145 EMB145EP 3260221 SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE UPPER LT WING SKIN. THE CRACK WAS INSPECTED AND PLAC ED ON A 500 FLIGHT CYCLE DEFERRAL IN ACCORDANCE WITH EMBRAER IC2007-145/08980, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008010400033 20080104 00033 SO 2008 1 4 C2XA07RI106 1 20071214 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT ODOR A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 18102 145643 FLT 3136 - RDU TO EWR - CREW REPORTED STRONG ELECTRICAL STRONG SMELL IN THE COCKPIT. CREW DIVERTED FLIGHT TO IAD AND LA NDED UNEVENTFULLY. IAD-MX PERFORMED OPERATIONAL TEST OF ELECTRICAL AND AIR SYSTEMS AND COULD NOT DUPLICATE THE PROBLEM. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2008010400036 20080104 00036 SO 2008 1 4 C2XA07SH108 1 20071220 A 5751 1457400416 SHROUD EMB 145 EMB145XR 3260214 SO RT AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13118 145675 SHV - DURING C-CHECK, MAINTENANCE FOUND RT AILERON UPPER SHROUD BONDING STRIP WITH CORROSION. MAINTENANCE REPAIRED RT A ILERON UPPER SHROUD IAW EC 5750-01315 REV E. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2008010400038 20080104 00038 SO 2008 1 4 C2XA07SH109 1 20071220 A 5751 14573900400 SHROUD EMB 145 EMB145XR 3260214 SO RT AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13118 145675 SHV - DURING C-CHECK, MAINTENANCE FOUND RT AILERON LOWER SHROUD WITH CORRODED BONDING PLATES. MAINTENANCE REPAIRED RT L OWER AILERON SHROUD IAW EC 5750-01315 REV. E. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008010400039 20080104 00039 2008 1 4 ARWA20071203 4 20071215 A 3414 HG280D80 CADC DOUG DC10 DC1010 3022110 WP MALFUNCTIONED A ARWA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 SO 19 68041 46900 ABORTED AT 85 KTS DUE TO NO AIRSPEED INDICATION ON CAP SIDE. REMOVED AND REPLACED CADC IN ACCORDANCE WITH M/M 34-16-01. OPERATIONAL CHECK GOOD IN ACCORDANCE WITH M/M 34-16-00 AND M/M 34-11-00. 2 L 7 3 4F A22WE 2008010400040 20080104 00040 CE 2008 1 4 DXTA200702688 1 20071218 A 2701 SWITCH BEECH MU300 400A 1155402 CE PWA JT15 JT15D4 52112 NE YOKE INOPERATIVE E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 101QS RK484 AFTER TAKEOFF PITCHTRIM FAILED AT 2000 FT AGL, PITCH TRIM WOULD NOT LEAVE GREEN ARC. FOUND PILOTS PITCH TRIM SWITCH INO P. REMOVED PILOTS YOKE ASSY. PN 128284060-13 SN 0039 AND INSTALLED NEW PILOTS YOKE ASSY. PN 128384060-13, SN 0076. IAW C MM 27-10-15 OPERATIONAL CHECKS OF SWITCHES ON YOKE SATISFACTORY. 2 H 7 2 4F 4 F RT A16SW E1NE 2008010400041 20080104 00041 CE 2008 1 4 DXTA200702689 1 20071218 A 3260 387 BULB CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG INDICATOR BURNED OUT E DXTA A UNSCHED LANDING P NO WARNING INDICATION LD LANDING 1 GL 07 982QS 6050 7500182 GREEN NOSE GEAR DOWN AND LOCKED LIGHT IS INOP, LANDING GEAR BLOW DOWN BOTTLE AND NOSE GEAR UPLOCK MANUAL RELEASE (D-RING ) WAS USED. INSTALLED NEW BULBS IN NOSE DOWNLOCK LIGHT IAW MM 31-10-00. OPS CHECKED GOOD. RESECURED D-RING AND EMERGENCY KNOB AND RESET BUTTON IAW MM 32-00-01. PERFORMED ALTERNATE HYD SYS BLEED TO VERIFY FLIGHT CONTROLS ON T/RS IAW MM 12-10 -15. OPS CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008010400042 20080104 00042 CE 2008 1 4 DXTA200702690 1 20071218 A 3411 PITOT TUBE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LEFT CONTAMINATED E DXTA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 GL 07 637QS 5605137 ABORTED TAKEOFF DUE TO NO AIRSPEED INDICATION ON PILOTS SIDE. DRAINED MOISTURE FROM LT PITOT TUBE. PERFORMED PURGE TO PILOTS SYSTEM. TESTED LT PITOT SYSTEM. OPERATIONAL CHECK SATISFACTORY IAW MANUAL 34-11-08. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008010400045 20080104 00045 SO 2008 1 4 C2XA07IA241 1 20071210 A 2611 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO LAVATORY MALFUNCTIONED A C2XA O OTHER N FALSE WARNING UK UNKNOWN 1 SW 27 11192 14500936 SAT - FLIGHT 216, THE CREW REPORTED A LAV SMOKE EICAS MASTER WARNING IN FLIGHT AFTER THE AIRCRAFT HAD JUST BEEN DEICED I N OKC. THE MESSAGE CLEARED BY ITSELF, AND THE FO VERIFIED NO SMOKE IN THE LAV. THE AIRCRAFT CONTINUED TO SAT WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE LAV SMOKE DETECTOR WITH NO DEFEC TS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008010400047 20080104 00047 SO 2008 1 4 C2XA07IA254 1 20071224 A 5210 14532349401 HANDLE EMB 145 EMB145XR 3260214 SO CABIN DOOR LOOSE A C2XA K NONE O OTHER NR NOT REPORTED 1 SW 27 21129 145703 IAH - FLIGHT 2785, THE CREW REPORTED THAT THE MAIN CABIN DOOR COULD NOT BE OPENED FROM THE INSIDE. MAINTENANCE TIGHTENE D THE INTERNAL HANDLE ON THE MAIN DOOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008010400052 20080104 00052 SO 2008 1 4 C2XA07CL104 1 20071218 A 3350 SIGN EMB 145 EMB145XR 3260214 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17108 145655 DURING ROUTINE MAINTENANCE, THE SMALL EMERGENCY EXIT SIGN ON THE RIGHT OVERWING EXIT WOULD NOT TEST. MAINTENANCE PERFOR MED A ELECTRICAL RESET AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2008010400053 20080104 00053 SO 2008 1 4 C2XA07TY088 1 20071224 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15985 145248 NR 4 EMERGENCY LIGHT INVERTER INOP. REMOVED AND REPLACED INVERTER IAW EMB 145MM 33-50-10 OPS CK GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008010400054 20080104 00054 SO 2008 1 4 C2XA07ON039 1 20071217 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO LAVATORY MALFUNCTIONED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 33182 7826 7826 145909 FLT 7738 - LAX TO SAN - CREW REPORTED LAV SMOKE INDICATION. MX RESET SYSTEM AND OPERATIONALLY CHECKED GOOD AND AIRCRAFT WAS RELEASE IN AIRWORTHY CONDITIONS TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008010400060 20080104 00060 SO 2008 1 4 C2XA07ON041 1 20071219 A 2611 M83726316002P RELAY EMB 145 EMB145XR 3260214 SO CARGO BAY BURNED A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 11192 145936 FLT 16 - SAT TO ONT - FLIGHT CREW REPORTED BAGGAGE FIRE TEST LIGHT WILL NOT COME ON DURING TEST. MX PERSONNEL AT ONT RE MOVED AND REPLACED RELAY K0629 IAW EMB145XR WM 20-13-02 AND 26-10-00, OPERATIONALLY CHECKED SYSTEM AND AIRCRAFT WAS RELE ASED TO RETURN FOR SERVICE IN AIRWORTHY CONDITION. 2 L 7 2 4F RT 2008010400064 20080104 00064 SO 2008 1 4 C2XA07IA245 1 20071211 A 4930 4504727 FUEL LINE EMB 145 EMB145XR 3260214 SO APU LOOSE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 16151 SPE0214324 145758 IAH - FLIGHT 2533, THE CREW REPORTED THAT THE APU CAUSES FUEL SMELL IN THE CABIN AND COCKPIT. MAINTENANCE PLACED THE AP U ON MEL 49-00-00 CAT-C CTL NR 134748, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. IN BNA, MAINTENANCE TIGHTEN ED LOOSE FUEL LINE AT APU FUEL CONTROL IAW VCMM HAM SUN 49-32-01 MM. OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT 2008010400065 20080104 00065 SO 2008 1 4 C2XA07ON042 1 20071211 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO LAVATORY MALFUNCTIONED A C2XA K NONE N FALSE WARNING UK UNKNOWN 1 SW 27 11192 6259 6259 14500936 FLT 0017 - ONT TO SAT - CREW REPORTED LAV SMOKE EICAS MASTER WARNING IN FLIGHT. A/C HAD JUST BEEN DEICED MESSAGE CLEARE D FO CKD LAV AND THERE WAS NO SIGN OF SMOKE. MX PERSONNEL PERFORMED OPERATIONAL CHECK AND NO FAULTS WERE NOTED AT THAT TIME. A/C WAS RELEASED IN AIRWORTHY CONDITIONS. 2 L 7 2 4F RT 2008010400066 20080104 00066 SO 2008 1 4 C2XA07RI110 1 20071225 A 5220 DOOR SEAL EMB 145 EMB145XR 3260214 SO EMERGENCY EXIT DIRTY A C2XA K NONE O OTHER CL CLIMB 1 SW 27 24103 145645 FLIGHT 2146 DAB TO EWR. CREW REPORTED,: EMERGENCY EXIT LEFT SIDE BY SEAT 12A HAD WHISTLE ON CLIMB TO ALTITUDE. REPAIR EW R MX "CLEANED AND LUBED EMERGENCY EXIT 12A DOOR SEAL IAW EMB 145 AMM 52-21-01." A/C APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008010400067 20080104 00067 GL 2008 1 4 C2XA07TY090 2 20071223 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 MALFUNCTIONED A C2XA E ENGINE SHUTDOWN K FLUID LOSS UK UNKNOWN 1 SW 27 29906 145472 311419 NR 2 ENG OIL QUANTITY DROPPED TO 3 QUARTS AND OIL PRESSURE DROPPED TO 25 PSI. PERFORMED ENG SHUT DOWN. REMOVED AND REP LACED NR 2 ENG IAW AMP T/C 6271001. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008010400070 20080104 00070 GL 2008 1 4 C2XA07RI107 2 20071223 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 SMOKE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 16951 145063 FLIGHT 2291 MEM TO EWR:CREW NOTED "SMOKE FROM NR 2 ENGINE WAS REPORTED FROM START OF TAKEOFF ROLL TO APPROX THREE MILES FROM DEPARTURE END OF RUNWAY. OIL PRESSURE RANGED 117-111 PSI DURING TAKEOFF ROLL WITH 12 QTS OF OIL IN THE ENGINE". M X INSPECTED NR 2 ENGINE FOR OIL LEAKS WITH NO LEAKS NOTED. RAN NR 2 ENGINE ON GROUND IAW EMB 145 AMM 71-00-01. NO SMOK E NOTED. A/C WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008010400072 20080104 00072 SO 2008 1 4 C2XA07ON045 1 20071225 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT & CABIN SMOKE A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 33182 14500909 FLT 7664 - SLC TO OKC - FLIGHT CREW REPORTED SMOKE IN COCKPIT AND CABIN DURING CLIMB/OVERWEIGHT LANDING. MX PERSONNEL R AN APU AND ENGINES NO SMOKE NOTED, POSSIBLE DEICE FLUID INGESTION/OVERWEIGHT OVERWEIGHT LANDING WITHIN LIMITS. A/C WAS RELEASED TO RETURN FOR SERVICE IN AIRWORTHY CONDITIONS. 2 L 7 2 4F RT 2008010400074 20080104 00074 NM 2008 1 4 CALA0700767 1 20071218 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17619 27332 FUSELAGE FRAME IS CRACKED AT STA 787 BETWEEN STRINGER 8R AND 9R. REPAIRED PER ECRA 5310-04684. 2 L 7 2 4F RT A16WE 2008010400077 20080104 00077 NM 2008 1 4 CALA0700764 1 20071217 A 5311 65C25228 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 FUSELAGE FRAME STA 727C MIS-DRILLED. REPAIR PER ECRA 5310-04683. 2 L 7 2 4F RT A16WE 2008010400079 20080104 00079 NM 2008 1 4 CALA0700763 1 20071217 A 5311 65C25228 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 FRAME CRACKED AT STA 727C B/W STR 8RT 9RT. INSTALLED REPAIRED PER ECRA 5310-04683. 2 L 7 2 4F RT A16WE 2008010400082 20080104 00082 NM 2008 1 4 CALA0700773 1 20071218 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17619 27332 FUSELAGE FRAME IS CRACKED STA 907 BETWEEN STRINGERS 8L AND 9L. REPAIRED PER ECRA 5310-04684. 2 L 7 2 4F RT A16WE 2008010400083 20080104 00083 NM 2008 1 4 CALA0700774 1 20071218 A 5311 6546225 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17619 27332 FUSELAGE FRAME IS CRACKED STATION 827 BETWEEN STRINGERS 8L AND 9L. REPAIRED PER ECRA 5310-04684. 2 L 7 2 4F RT A16WE 2008010400085 20080104 00085 NM 2008 1 4 CALA0700747 1 20071208 A 5311 6546526 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 FRAME CRACKED B/W STA400 STR 8 AND 9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2008010400086 20080104 00086 NM 2008 1 4 CALA0700748 1 20071208 A 5311 6546529 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 FUSELAGE FRAME CRACKED STA440 B/W STR 8/9 LT. REPAIRED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2008010400089 20080104 00089 NM 2008 1 4 CALA0700751 1 20071208 A 5311 BAC15171470 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 FRAME CRACKED AT STA 907 B/W STR 8/9. REPAIRED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2008010400090 20080104 00090 NM 2008 1 4 CALA0700752 1 20071210 A 5311 6546526 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 FUSELAGE FRAME CRACKED STA 400 B/W STR 8/9. REPAIRED PER EA 5310-85405. 2 L 7 2 4F RT A16WE 2008010400093 20080104 00093 CE 2008 1 4 Z5FA121807001 1 20071218 A 2150 92722322 SWITCH CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE ACM OVERTEMP DEFECTIVE E Z5FA G H A O2 MASK DEPLOYED DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 EA 63 629CS 136 6800165 ENROUTE, CREW NOTICED "EMERGENCY PRESSURE ON" ANNUNCIATION. 1ST OFFICER DONNED O2 MASK AND CREW REQUESTED DECENT TO 10, 000 FT. SHORTLY AFTER GOING THROUGH AFM CHECK-LIST, NOTED STRONG ODOR OF BURNING, NO SMOKE OR FLAMES NOTICED. DECLARED E MERGENCY LANDING FOR IAD. TURNED OFF PRESSURIZATION AND BLEED-AIR SOURCES. SHORTLY AFTER, NOTED ODOR STOPPED. ACFT LAND ED WITHOUT INCIDENT. ACFT SHUTDOWN ON TAXI WAY AND CHECKED FOR ANY ANOMALIES. NONE NOTED, AIRCRAFT TAXIED TO FBO. FOUN D DEFECTIVE ACM OVERTEMP SWITCH. SWITCH REPLACED, OPS CHECK WAS GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RC T00012WI E35NE 2008010400094 20080104 00094 CE 2008 1 4 DXTA200702621DXTA 1 20071120 A 3297 CONNECTOR CESSNA 500 560CESSNA 2076750 CE DOWNLOCK SWITCH DIRTY E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 809QS 5600698 LEFT MAIN MOUNT DID NOT LOCK DOWN WITH OTHER GEAR. GREEN LIGHT STAYED OFF ADN RED UNSAFE INDICATOR LIGHT ILLUMINATED FOR 15+ SECONDS. JACKED A/C PERFORMED GEAR SWING I/A/W CE560E M/M 32-01-00. LANDING GEAR HYD SYSTEM ADJ/TEST. GEAR SWING OP S CHECKED GOOD. SUSPECTED MOISTURE IN GEAR DOWN LOCK SWITCH. CLEANED DOWNLOCK SWITCH CONNECTOR. GEAR TRAVEL TIMES WITHIN LIMITS. 5 SECONDS AND 4 SECONDS EXTEND. OPS CHECKED GOOD. 2 L 7 2 4F RT A22CE 2008010400096 20080104 00096 NM 2008 1 4 CALA0700755 1 20071210 A 5311 6546549 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 FUSELAGE FRAME CRACKED STA 767 B/W STR 8/9 RT. REPAIRED PER EA5310-04498. 2 L 7 2 4F RT A16WE 2008010400097 20080104 00097 NM 2008 1 4 CALA0700756 1 20071214 A 5320 6562276 ATTACH FITTING BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17619 27332 PAX CABIN STR 11 L HAS CRACKED ATTACHMENT CLIP AT STA 360. REMOVED AND REPLACED PER EA5311-01383. 2 L 7 2 4F RT A16WE 2008010400102 20080104 00102 NM 2008 1 4 CALA0700761 1 20071215 A 5310 65C352436 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 AFT CARGO AFT DOOR FRAME CRACKED AT LOWER STOP PAD REMOVED AND REPLACED AFT CARGO DOOR AFT FRAME PER SRM 51-40-02 REF DW G 65-47960 2 L 7 2 4F RT A16WE 2008010400103 20080104 00103 NM 2008 1 4 CALA0700762 1 20071217 A 5313 65C80736426 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 ABB HEAVY IGC CORROSION STR 26 R STA 790. REPAIRED PER SRM 53-00-03. 2 L 7 2 4F RT A16WE 2008010400104 20080104 00104 GL 2008 1 4 CHQA200700095 2 20071211 A 7200 AE3007A1P ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 MALFUNCTIONED A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 284SK 16152 7324 145427 CAE311281 STL TO IAH - AFTER TAKEOFF FROM STL FLIGHT CREW RECEIVED A LAV SMOKE EICAS MESSAGE. AT THE SAME TIME THE FLIGHT ATTENDA NT CALLED THE COCKPIT TO REPORT SMOKE IN THE CABIN COMING FROM THE LAV TO ABOUT MID CABIN. THE FLIGHT CREW ALSO DETECTE D A FAINT ELECTRICAL BURNING SMELL IN THE COCKPIT. THE FLIGHT CREW FOLLOWED THE QRH AND MADE AN IMMEDIATE RETURN TO FIE LD. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RAN ENGINES AND TRACED THE SOURCE OF THE SMOKE TO THE NR 2 ENGINE. THE NR 2 ENGINE WAS REPLACED AND THE SMOKE DID NOT RETURN. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008010400108 20080104 00108 NM 2008 1 4 DL764071624 1 20071215 A 3350 CHARGER BOEING 767 767432ER 1385134 NM CABIN DEFECTIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 826MH 29697 EMERGENCY LIGHT BATTERY CHARGER ROW 6 LEFT IS DEFECTIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY IAW B767-400 AMM 33-51-07. NO FAULTS NOTED ON OPS CHECK IAW B767-400 AMM 33-51-07. 2 L 7 2 4F RT A1NM 2008010400109 20080104 00109 NM 2008 1 4 DL764071625 1 20071215 A 3350 BATTERY PACK BOEING 767 767432ER 1385134 NM CABIN DEFECTIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 826MH 29697 EMERGENCY LIGHT BATTERY PACK ROW 32 RIGHT IS DEFECTIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AND POWER SUP PLY IAW B767-400 AMM 33-51-07. NO FAULTS NOTED ON OPS CHECK IAW B757-400 AMM 33-51-07. 2 L 7 2 4F RT A1NM 2008010400112 20080104 00112 NM 2008 1 4 DL764071628 1 20071215 A 3350 LIGHT BOEING 767 767432ER 1385134 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 826MH 29697 R4 EXTERIOR EMERG SLIDE LIGHT IS INOP. RELAMPED R4 EXTERIOR EMERGENCY SLIDE LIGHT, LIGHT OPS CHECKS GOOD IAW B767-400 M M 33-51-06. 2 L 7 2 4F RT A1NM 2008010400114 20080104 00114 NM 2008 1 4 DL764071630 1 20071215 A 3350 POWER SUPPLY BOEING 767 767432ER 1385134 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 826MH 29697 LT EMERGENCY LIGHTS IN C ZONE ARE INOP. T/S SUPPLY POWER NO OUT RT REPLACED POWER SUPPLY OPS CHECK GOOD PER B767 MM 33- 51-08. 2 L 7 2 4F RT A1NM 2008010400116 20080104 00116 NM 2008 1 4 DLM90071633 1 20071217 A 5321 FLOOR PANEL DOUG MD90 MD9030 3023690 NM CABIN CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 CABIN CUSP FLOOR PANEL 221AG CORRODED. REMOVED CORROSION IAW MD-90 SRM 53-00-01 PG 5. FILLER FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01 PG 9 FIG 3 VOL 1. FAB NEW REPAIR PANEL IAW MD-90 SRM 51-10-05 VOL 2. REMOVED AND REPLACED FITTINGS I AW MD-90 SRM 51-30-01 VOL 2 ON N/R 2400-0174 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2008010400118 20080104 00118 NM 2008 1 4 DLM90071635 1 20071215 A 5320 5930961 FLOOR SUPPORT DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 AFT PAX CABIN FLOOR SUPPORT BEAM AT STA 1307 CENTER AISLE HAS CORROSION ON LT SIDE. FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW MD-90 SRM 51-30-05 ON N/R 2000-0200 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2008010400121 20080104 00121 NM 2008 1 4 DLM88071638 1 20071220 A 5310 THRESHOLD DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 917DE 49958 A MAJOR REPAIR TO PRIMARY STRUCTURE WAS ACCOMPLISHED TO THE FWD CARGO DOOR JAMB PER SRM 53-05D FIG 804D DUE TO CORROSION . 2 L 7 2 4F RT A6WE 2008010400122 20080104 00122 NM 2008 1 4 DL76S071639 1 20071218 A 5330 146T3340 SKIN BOEING 767 767332 1382001 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 125DL 24075 MINOR SKIN BLENDS AT FS 1438 TO 1540, ALONG S-19L TO S-26L. REPAIRED PER ER/A 459229-14ADREVA. 2 L 7 2 4F RT A1NM 2008010400123 20080104 00123 NM 2008 1 4 DL764071640 1 20071218 A 5330 146T35313 SKIN BOEING 767 767432ER 1385134 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 826MH 29697 DURING HMV AT TIMCO GSO, THE FUSELAGE SKIN WAS FOUND DENTED OUT OF LIMITS AT STA 1373 BETWEEN S-28R AND S-29R. THE DAMA GE WAS CUT OUT AND REPAIRED PER ER/A 465100-14. 2 L 7 2 4F RT A1NM 2008010400124 20080104 00124 NM 2008 1 4 DL76S071641 1 20071220 A 5330 146T3520 SKIN BOEING 767 767332 1382001 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 125DL 24075 MINOR SKIN BLENDS AT FS 1219-1270 ALONG S-21R TO S-26R. 2 L 7 2 4F RT A1NM 2008010400127 20080104 00127 CE 2008 1 4 DXTA200702696 1 20071220 A 2731 MOUNT CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE TRIM WHEEL LOOSE E DXTA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 07 669QS 5605689 ON TAKEOFF, F/O HAD TO USE FULL FORWARD PRESSURE TO KEEP NOSE DOWN. FOUND ELEVATOR TRIM WHEEL MOUNTING SCREWS LOOSE CAU SING THE POINTER TO SKIP ITS TRACK. REINDEX POINTER TO TRIM WHEEL AND TAKEOFF MARKER INDEX. RESECURED TRIM WHEEL SCREWS AS ORIGINAL REF CESSNA 560XLS MM 27-32-01 CHECKED ELEVATOR TRIM TRAVELS FOUND TO BE WITHIN LIMITS PER CESSNA MM 560XLS 27-32-01. OPS CHECKED GOOD NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008010400128 20080104 00128 NM 2008 1 4 DLM88071607 1 20071212 A 2910 JT8D219 HYDRAULIC LINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE LOOSE A DALA O OTHER K FLUID LOSS CR CRUISE 1 SO 27 933DL 39340 49720 726047 LEFT HYD PRESSURE SYSTEM FAIL IN FLT PRESSURE DROPPED TO ZERO AND QTY DROPPED TO 2 QTS. FOUND PRESSURE LINE AT NR 1 ENG DISCONNECT LEAKING. TIGHTENED LINE AND RAN ENG, THRUST REVERSER AND ELEC PUMPS. NO LKS FOUND. 2 L 7 2 4F 4 F RT A6WE E9NE 2008010400130 20080104 00130 NM 2008 1 4 DLM90071611 1 20071201 A 5347 6022044 SEAT TRACK DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 CABIN SEAT TRACK CORRODED OUT OF LIMITS FS 1231-1364 LBL 22. REMOVED AND REPLACED DAMAGED SEAT TRACK FS 1231-1364 LBL 2 2 PER MD-90 SRM 53-40-01 VOL 1 FIG 6 AND 53-10-5 AND 53-10-03 ON N/R 2700-0150 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2008010400132 20080104 00132 NM 2008 1 4 DL757071613 1 20071216 A 2120 UNKNOWN BOEING 757 75726D 1384907 NM CABIN ODOR A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 900PC 28446 STRONG RUBBER SMELL FROM A/C PACKS. INSPECTED A/C BAY READING AND O/H LIGHTS RAN PACKS USING ENG BL AIR NO TROUBLE FOUN D 2 L 7 2 4F RT A2NM 2008010400134 20080104 00134 NM 2008 1 4 DLM90071615 1 20071214 A 5310 DOOR FRAME DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 AFT CARGO BAY DOOR JAMB LOWER WEB CORROSION FROM FWD TO AFT END. REMOVED AND FAB NEW REPAIR STRAP AND INSTALLED IAW MD- 80 SRM 53-05D FIF 63 ON N/R 1600-0108 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2008010400136 20080104 00136 NM 2008 1 4 DLM90071618 1 20071214 A 5320 993061217 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 LT CUSP WEB CORRODED OUT OF LIMITS FS 984-1003. REPAIRED CUSP WEB IAW ERA 398191-14MA REV ORG DATED 9-18-02 ON N/R 2400 -0165 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2008010400137 20080104 00137 NM 2008 1 4 DLM90071616 1 20071214 A 5320 993053882 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 RT CUSP WEB CRACKED BETWEEN 525-533. REPAIRED CRACKED LIGHTNING HOLE IAW MD-80 SRM 53-05D FIG 827D ON N/R 2700-0160 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2008010400139 20080104 00139 NM 2008 1 4 DLM90071619 1 20071216 A 5320 9930538 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 LT CABIN CUSP WEB OUT OF LIMITS FS 456-461. REPAIRED LT CABIN CUSP WEB FS 456-461 IAW MD-80 SRM 53-05D FIG 827D ON N/R 2400-0162 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2008010400140 20080104 00140 NM 2008 1 4 DL757071620 1 20071214 A 5330 143N35214 SKIN BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 603DL 22810 FUSELAGE/SKIN/FS 880/STRG 28L-28R :CORROSION REPAIR. THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION AT FS 880 BE TWEEN STRINGERS 28L AND 28R. THE CORROSION WAS ADJACENT TO AN AIR CONDITIONING DUCT CUTOUT. THE DAMAGE WAS REMOVED WIT H A CUTOUT TO THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 465214-14. 2 L 7 2 4F RT A2NM 2008010400143 20080104 00143 NE 2008 1 4 DHLA200700092 2 20071224 A 7314 6411194 PUMP DOUG DC8 DC873 302199C WP CFMINT CFM56 CFM565C3G 13034 NE NR 2 ENGINE MALFUNCTIONED A DHLA O OTHER X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 GL 05 805DH 46125 693431 AFTER LDG NR 2 ENG FLAMED OUT WHILE TAXIING IN. REMOVED AND REPLACED NR 2 ENG DRIVEN FUEL BOOST PUMP IAW MM 37-10-1. O PS AND LEAK CHECK GOOD. 2 L 7 4 4F 4 F RT 4A25 2008010400144 20080104 00144 NM 2008 1 4 DHLA200700091 1 20071221 A 3610 CLAMP BOEING 727 727227 1384078 NM PWA JT8 JT8D17 52049 NE BLEED AIR SYS LOOSE A DHLA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 05 782DH 21998 654760 NR 1 ENG STRUT OVERHEAT DURING CRUISE. PERFORMED ABNORMALS PROCEDURE RESULTED IN IN-FLIGHT ENG SHUTDOWN ALL CHECK LISTS , PROCEDURES DONE. T/S FOUND CLAMP ON PRESSURE MODULATING VALVE LEAKING ON PRECOOLER SIDE TIGHTENED CLAMP IAW MM 36-00- 1 MM 36-12-42, RAN ENG PER JRH 6.5 AND FOUND ALL PARAMETERS NORMAL. NO LEAKS NOTED 2 L 7 3 4F 4 F A3WE E2EA 2008010400146 20080104 00146 NM 2008 1 4 DHL2007783 1 20071214 A 5730 6521795336A SKIN PANEL BOEING 727 727227 1384078 NM LT WING DEBONDED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 UPON VISUAL INSPECTION OF THE LEFT WING UPPER SURFACE FOUND THE PANEL JUST OUTBOARD OF THE NR 1 SPOILER WITH SKIN DISBON DING. W/S629-656.5 IS PANEL LOCATION. DISBONDING AREA IS APPROX 56 SQ IN. PANEL TO BE REPLACED. 2 L 7 3 4F A3WE 2008010400147 20080104 00147 NM 2008 1 4 DHLA200700094 1 20071223 A 5330 SKIN BOEING 727 727227 1384078 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 782DH 21998 A/C SKIN DAMAGE LT SIDE STATION BS 1110 APP. STR. 24-23L "C" CONTAINER. STOP DRILLED ENDS OF CRACK IN A/C SKIN PER SRM 51-40, DAMAGE REMAINS IN AIRCRAFT. 2 L 7 3 4F A3WE 2008010400148 20080104 00148 NM 2008 1 4 F3LA200700380 1 20071214 A 5315 D5347218920400 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT BS -Y1292 HAD CORROSION AT NUT PLATE HOLES BETWEEN FR 68 AND FR 69. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG. 102. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11. 2 L 7 2 4F RT A28NM 2008010400149 20080104 00149 2008 1 4 F3LA200700406 4 20071212 A 2565 L32A319160001 RELEASE CABLE AIRBUS A319 A319111 3930336 NM EVAC SLIDE INOPERATIVE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED RT OVERWING EXIT SLIDE RELEASE CABLE WOULD NOT RETRACT. REMOVED AND REPLACED RT OVERWING SLIDE RELEASE CABLE IAW AMM 25-62-43-PB401. 2 L 7 2 4F RT A28NM 2008010400150 20080104 00150 NM 2008 1 4 F3LA200700407 1 20071212 A 3350 321431 BATTERY PACK AIRBUS A319 A319111 3930336 NM CABIN FAILED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 1803 DURING C4/S1 CHECK, INSPECTION REPORTED FWD EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED AND INSTALLED SERVIC EABLE BATTERY IN FWD EPSU (10WL) IAW AMM 33-51-38-400-002. PERFORMED A BITE TEST OF THE FWD EMERGENCY LIGHT EPSU/BATTER Y PACK IAW AMM 33-51-38-400-002. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 2008010400154 20080104 00154 NM 2008 1 4 F3LA200700405 1 20071213 A 2540 NAS130431 MOUNT BOLT AIRBUS A319 A319111 3930336 NM LAVATORY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED LAV E LOWER FLOOR MOUNT BOLTS CORRODED. REMOVED AND REPLACED CORRODED FLOOR MOU NT BOLTS IN LAV E IAW AMM 25-43-42-PB401. 2 L 7 2 4F RT A28NM 2008010400155 20080104 00155 NM 2008 1 4 F3LA200700409 1 20071212 A 3350 321431 BATTERY PACK AIRBUS A319 A319111 3930336 NM CABIN FAILED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 1803 DURING C4/S1 CHECK, INSPECTION REPORTED LT OVERWING EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED AND INSTALLE D SERVICEABLE BATTERY IN LT OVERWING EPSU IAW AMM 33-51-38-420-052. PERFORMED BITE TEST IAW AMM 33-51-38-400-002 AND TE STED GOOD. 2 L 7 2 4F RT A28NM 2008010400157 20080104 00157 NM 2008 1 4 F3LA200700408 1 20071212 A 3350 321431 BATTERY PACK AIRBUS A319 A319111 3930336 NM CABIN FAILED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 1803 DURING C4/S1 CHECK, INSPECTION REPORTED RT OVERWING EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED AND INSTALLE D SERVICEABLE BATTERY PACK IN RT OVERWING EPSU IAW AMM 33-51-38-400-002. PERFORMED BITE TEST OF RT OVERWING EMERGENCY L IGHT EPSU/BATTERY PACK IAW 33-51-38-400-002 AND CHECKED GOOD. 2 L 7 2 4F RT A28NM 2008010400158 20080104 00158 NM 2008 1 4 F3LA200700386 1 20071215 A 5320 D531128720200 DUMMY RAIL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED DUMMY RAIL AT Y503.2, FR 12 TO FR 16, CORRODED ON TOP. CORROSION FOUND TO BE OU T OF LIMITS IAW SRM 53-11-14. REMOVED AND REPLACED DUMMY RAIL IAW SRM 51-42-11 AND 51-44-11. 2 L 7 2 4F RT A28NM 2008010400160 20080104 00160 NM 2008 1 4 F3LA200700388 1 20071215 A 5321 D5361060500000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 221FF (L1 DOOR) CORRODED ON BOTTOM SIDE. REMOVED AND REPLACED FLOOR PANEL 221FF IAW AMM 53-12-12-PB401. 2 L 7 2 4F RT A28NM 2008010400161 20080104 00161 NM 2008 1 4 F3LA200700392 1 20071220 A 5350 FASTENER AIRBUS A319 A319111 3930336 NM FAIRING CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED RT WING-TO-BODY FAIRING 192DT HAD CORRODED FASTENERS AT LOWER SEAL. REMOVED AND REPLACED RT WING UPPER WING-TOO-BODY FAIRING PANEL NR 192DT LOWER SEAL MOUNTING SCREWS IAW 51-42-11. 2 L 7 2 4F RT A28NM 2008010400162 20080104 00162 NM 2008 1 4 F3LA200700400 1 20071214 A 2560 LOCK FASTENER AIRBUS A319 A319111 3930336 NM GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED L2 DOOR SILL AFT GIRT BAR FITTING CORRODED AT LOCK FASTENER. REMOVED AND REPLAC ED FASTENER IAW SRM 51-42-11. 2 L 7 2 4F RT A28NM 2008010400164 20080104 00164 NM 2008 1 4 F3LA200700401 1 20071214 A 5320 SUPPORT BEAM AIRBUS A319 A319111 3930336 NM FUSELAGE BENT A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED AFT CARGO FWD BULKHEAD PANEL SUPPORT BEAM AT APPROX STR 42L, FR47 TO FR51, BENT. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SUPPORT BEAM IAW SRM 51-42-11, SRM 51-44-11, 51-75-12 AND DRAWING D53974 679. 2 L 7 2 4F RT A28NM 2008010400165 20080104 00165 2008 1 4 AMTA200700634 4 20071123 A 2310 9640453011 COUPLER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE NR 2 HF XMITTER UNSERVICEABLE A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 522AT 29330 RT HF TRANSMITTER INOPERATIVE AT ALL CREW STATIONS. REMOVED AND REPLACED RT HF COUPLER IAW MM 23-11-01-4. OPS NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010400167 20080104 00167 2008 1 4 AMTA200700636 4 20071125 A 2310 TRANSCEIVER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE HF SYSTEM INOPERATIVE A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 522AT 29330 RT HF WILL NOT TRANSMIT EACH TIME MIKE IS KEYED, RT HF CONTINUOUSLY RE-TUNES. PERFORM BITE ON RT HF TRANSCEIVER RESET. OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010400168 20080104 00168 WP 2008 1 4 AMTA200700637 1 20071122 A 3397 CONNECTOR LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE EMERGENCY LIGHTS DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 163AT 1229 FWD GALLEY FLOOR TRACK EMERGENCY LIGHT EGRESS STRIP INOPERATIVE. REINSTALLED ORIGINAL PART T/S AND FOUND DISCONNECTED C ONNECTOR. RECONNECTED CONNECTOR, OPS CHECK GOOD. OK TO SERVICE. (K) 2 L 7 3 4F 4 F A23WE E12EU 2008010400169 20080104 00169 NM 2008 1 4 GAIA07018OP 1 20071030 A 4920 340428101 APU BOEING 737 7373Y0 1384671 NM CFMINT CFM56 CFM563B2 13802 EU APU BAY FLAMED OUT A GAIA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SW 07 108KH 24902 DURING CLIMBOUT, THE APU FLAMMED OUT AT FL 320. AND EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DEPARTURE. AN UNEVENTFUL LANDING WAS MADE. NOTE: NR 1 GENERATOR ON DMI. PERFORMED APU INSPECTION, NO DEFECTS NOTED. OPS CHECKED GOO D. AIRCRAFT RETURNED TO SERVICE. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2008010400174 20080104 00174 NM 2008 1 4 F3LA200700404 1 20071223 A 5321 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 262FF CORRODED ON LOWER SURFACE. REMOVED AND REPLACED FLOOR PANEL 2 62FF IAW EO A0-53T-11996. 2 L 7 2 4F RT A28NM 2008010400179 20080104 00179 NM 2008 1 4 F3LA200700391 1 20071216 A 5320 D5348015900600 PLATE AIRBUS A319 A319111 3930336 NM GIRT BAR LATCH CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED L2 DOOR FWD GIRT BAR LATCH FLOOR FILLER HAD A SMALL SPOT OF CORROSION. REMOVED AND REPLACED L2 DOOR FWD GIRT BAR LATCH FILLER PANEL IAW AMM 53-42-12-PB401. 2 L 7 2 4F RT A28NM 2008010400181 20080104 00181 NM 2008 1 4 F3LA200700378 1 20071214 A 5320 HL11VF6 RIVET AIRBUS A319 A319111 3930336 NM FUSELAGE SHEARED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED SHEARED RIVETS ON WEB AT STA. -Y1292 BETWEEN FR68 AND FR69. REMOVED AND REPLACE D RIVETS IAW A319 SRM 51-44-11, 51-46-11 AND EA A9-53R-12329. 2 L 7 2 4F RT A28NM 2008010400183 20080104 00183 NM 2008 1 4 F3LA200700384 1 20071215 A 5315 D5311281520200 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT Y1292 AND FR16, AT ATTACH POINT. REMOVED AND REPLACED FLOORBEAM AT Y1292 IAW SRM 51-42-11. 2 L 7 2 4F RT A28NM 2008010400190 20080104 00190 NM 2008 1 4 IU6R229069 1 20071206 A 2913 654467447 HOUSING BOEING BOEING 737 737 UTILSYS NM INTERNAL PORT CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 2390 HOUSING CRACKED IN PORT. 2 L 7 2 4F RT A16WE 2008010400192 20080104 00192 EU 2008 1 4 SSHA118378 1 20071203 A 3300 55670 LIGHT AEROSP AS355 AS355* EU TMECA ARRIEL ARRIEL1 60030 NE SMOKE E SSHA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 13 141MK 2424 POWERED UP AND BOX STARTED TO SMOKE. 1 G 7 2 3U 3 U H11EU E19EU 2008010400196 20080104 00196 NE 2008 1 4 HEEA118383 1 20071126 A 2913 7665009808102 PUMP SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL2S1 60057 NE NR 1 FAILED D HEEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 766P 760594 ENROUTE , TLP NR 1 HYD PRESS WENT TO ZERO AND NR 1 SERVO LIGHT ILLUMINATED. FOLLOWED RFM PROCEDURE AND LANDED ON THE BE ACH. MAINTENANCE REPLACED NR 1 HYD PUMP. 1 G 7 2 3U 4 U NC H1NE E00054EN 2008010400198 20080104 00198 NM 2008 1 4 F3LA200700387 1 20071215 A 5321 D5361060500100 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CABIN CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 222FF (R1 DOOR) CORRODED ON BOTTOM SIDE. REMOVED AND REPLACED FLOOR PANEL 222FF IAW AMM 53-12-12-PB401. 2 L 7 2 4F RT A28NM 2008010400200 20080104 00200 NM 2008 1 4 JJWA118400 1 20071205 A 6310 A1902 BELT ROBSIN R22 R22BETA 7640110 NM LYC O320 O320* 41508 EA ENG-TRANSMISSION DISINTEGRATED E JJWA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 19 413RM 504 1412 §135.415(A)(16) EMERGENCY ACTIONS EXC ENGINE SHUTDOWN THIS IS NOT A CHARTER AIRCRAFT. IN LEVEL FLIGHT DURING VFR CONDIT IONS, DURING CROSS COUNTRY FLIGHT TRAINING WHILE IN LEVEL FLIGHT, A SUDDEN VIRATION AND NOISE WAS HEARD FROM ENGINE AREA . INSTRUCTOR AND STUDENT MADE PRECAUTIONARY POWERED LANDING TO SUITABLE SITE. FOUND AFT MAIN ENGINE TO TRANSMISSION DRI VE SYSTEM BELT HAD DISINTEGRATED, CAUSING FORWARD BELT TO SKIP A GROOVE FORWARD SO ONLY ONE OF FOUR DRIVE BELT SECTIONS WAS POWERING ROTOR DRIVE SYSTEM. DISSASEMBLY, INSPECTION OF SYSTEMS IN AREA, AND NEW PART REPLACEMENT TO BE PERFORMED. 1 G 7 1 3O 3 O H10WE E274 2008010400201 20080104 00201 EU 2008 1 4 F3LA200700379 1 20071224 A 3350 321430 BATTERY PACK AIRBUS A318 A318111 3940019 EU CABIN INOPERATIVE A F3LA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 03 801FR 1939 FLIGHT CREW REPORTED EPSU "13WL" AFT LEFT MESSAGE. REPLACED EPSU BATTERY AT 13WL LOCATION IAW AMM 33-51-38-400-002. OP S CHECK GOOD. 2 L 7 2 4F RT 2008010400202 20080104 00202 NM 2008 1 4 JJWA118401 1 20071205 A 6310 A1902 BELT ROBSIN R22 R22BETA 7640110 NM LYC O320 O320* 41508 EA DEFECTIVE B JJWA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 19 413RM 503 1412 INSTRUCTOR MADE UNSCHEDULED LANDING IN SAFE AREA AFTER EXCESSIVE NOISE AND VIBRATION FROM ENGINE AREA. FOUND AFT MAIN DR IVE BELT HAD FAILED COMPLETELY AND HAD PUSHED THE FORWARD BELT FORWARD WHERE ONLY ONE SECTION WAS STILL POWERING ROTOR D RIVE SYSTEM. ADDITIONAL DAMAGE TO ENGINE COOLING FAN SHROUD BY ENGINE OIL COOLER. ALL BELTS AND FAN SHROUD TO BE REPLAC ED. ONE ANTENNA CONNECTOR TO BE RELACED. THIS IS NOT A CHARTER AIRCRAFT. 1 G 7 1 3O 3 O H10WE E274 2008010400203 20080104 00203 NM 2008 1 4 AMTA200700661 1 20071129 A 3150 WARNING LIGHT BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE WXR FALSE ACTIVATION A AMTA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 519AT 27975 ON TAXI OUT STATUS MESSAGE (WXR SYS) DISPLAYED CHECKED MEL; CALLED DISPATCH INSTRUCTED RTG. PERFORMED BITE CHECK AND TE STED SYS. WXR SYS TEST GOOD IAW FIM 34-43-00. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010400204 20080104 00204 NM 2008 1 4 AMTA200700664 1 20071201 A 2410 727792M GENERATOR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LEFT UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 514AT 26406 5983 27971 LT GEN CONTROL EICAS MESSAGE. REMOVED AND REPLACED LT IDG IAW MM 24-11-01-4. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010400206 20080104 00206 NM 2008 1 4 AMTA200700665 1 20071130 A 2160 3987505 CONTROL VALVE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT PACK TEMP INOPERATIVE A AMTA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 GL 11 517AT 27973 RT PACK INOPERATIVE LITE ILLUMINATED. RT PACK BITE MSS ON EICAS. REMOVED AND REPLACED PACK TEMP CONTROL VALVE IAW MM 2 1-51-12-4. OPS CHECK GOOD, OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010400208 20080104 00208 2008 1 4 AMTA200700667 4 20071202 A 2310 RADIO BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT HF RADIO INOPERATIVE A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 522AT 29330 RT HF RADIO W/N CHANNELIZE PROPERLY. WILL NOT TRANSMITT. REOCCURRING PROBLEM. TRANSMITT AND RECEIVE 5X5. OPS CHECKS NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010400209 20080104 00209 NM 2008 1 4 AMTA200700668 1 20071130 A 3010 VALVE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE LT WING LOCKED A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 550TZ 32584 WITH WING ANTI-ICE SWT SELECTED ON EICAS MSG DISPLAYED REPECTIVE VALVE LIGHTS ILLUM. FOUND BOTH RT AND LT WING TAI VALV ES IN MANUAL LOCKED POSITION, REOPENED BOTH VALVES, PERFORMED ADJ AND TEST IAW 30-11-00-5. OPS NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010400210 20080104 00210 NM 2008 1 4 AMTA200700669 1 20071130 A 2497 WIRE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE GENERATOR BROKEN A AMTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 11 552TZ 32586 ON ENGINE START, NR 2 GENERATOR WOULD NOT COME ON THE LINE. TROUBLESHOT RT GEN STS. FOUND WIRE W4502-0012-20 BROKEN OU T OF CONNECTOR D40492P. RETERMINATED AND REPLACED CONTACT IAW SWPM 20-60-02, OPS CHECK GOOD, IAW MM 24-11-00. REF SAA WO NR 11771, NR 78177730001. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010400211 20080104 00211 NM 2008 1 4 AMTA200700670 1 20071204 A 3260 SENSOR BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE RT MLG MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 301TZ 28239 PSEU LIGHT ILLUMINATED AFTER LANDING. REMOVED AND REPLACED RT MLG AIR/GROUND SENSOR S1011, IAW FIM 32-09-810-803. IAW MM 32-09-01-4. NO FAULTS NOTED. OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A16WE E2GL 2008010400212 20080104 00212 WP 2008 1 4 UPS07851279 1 20071211 A 2150 A/C PACK DOUG DC8 DC873F 302199F WP A/C BAY ODOR A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 801UP 46101 WHEN PACKS TURNED ON AFTER T/O, CHEMICAL SMELL OBSERVED. ODOR DECREASED AS FLIGHT CONTINUED. A/C LAYOVER IN PHL FOR W/ E WITH FREEZING RAIN SUSPECT FLUID IN PACKS. 2 L 7 4 4F RT 4A25 2008010400213 20080104 00213 2008 1 4 702DK 4 20071113 A 3452 6226523008 CONTROL HEAD BEECH 90 C90A 1152911 CE PWA PT6 PT6A60A 52043 NE TRANSPONDER FAULTY E ODAR A UNSCHED LANDING O OTHER CR CRUISE 1 EA 21 702DK LJ1259 BOTH NR 1 AND NR 2 TRANSPONDER DISPLAYS WENT OUT DURING FLIGHT ATC REPORTED TRANSPONDER FAULTS. AIRCRAFT RETURNED TO POI NT OF DEPARTURE WITHOUT INCIDENT. FAILURES TROUBLESHOT TO FAULTY TRANSPONDER CONTROL HEAD. 1 L 7 2 3T 4 T RT 3A20 E4EA 2008010400214 20080104 00214 WP 2008 1 4 UPS07851280 1 20071208 A 2510 INERTIA REEL DOUG DC8 DC873F 302199F WP COCKPIT STICKS A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 CAPTAIN'S LEFT SHOULDER HARNESS INERTIAL REEL IS STICKY. REMOVED AND REPLACED CAPTAIN'S INERTIA REEL. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2008022700216 20080227 00216 NM 2008 2 27 UPS08M51658 1 20071207 A 5320 A5A7116505 SPLICE DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C CENTER CARGO/AT STATION 1537 LONGERON 46RT FOUND SUSPECTED CRACK ON SPLICE DOUBLER. HFEC INSP C/O PER DAC NDT SPM R13, 06-10-01.001 & CRACK FOUND AS MARKED APPROX 2" IN LENGTH. CRACKED SPLICE REMOVED PER SRM 51-33-01 VII R35. NEW SPLICE P/N:A5A7116-505 FAB PER DWG A5A7116. FPI C/O ON NEW SPLICE FOUND NO CRACK EVIDENT. NEW SPLICE INSTAL LED AS PER SRM 51-31-01 VOL II REV 35. 2 L 7 3 4F RT A22WE 2008022800171 20080228 00171 NM 2008 2 28 DHL2007742053 1 20071119 A 5311 FRAME BOEING 727 727225 1384077 NM BS 1050 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 DENT AFT PIT AT FRAME BS 1050 ABOVE STRINGER 26R. REMOVED FASTENERS AS REQUIRED FOR ACCESS IAW SRM 51-30-2. CUT OUT DA MAGED AREA DIMENSION 1" BY 1.5: AND FABRICATED REPAIR ANGLE IAW SRM 51-40-3 AND M/I 53-10-2 FIGURE 9. HEAT TREATED MAT ERIAL TO T6 0.071 CONDITION IAW FAS REPORT NR 2-37153-801 REV A. TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED A NGLE REPAIR ON FRAME BS 1050 ABOVE STRINGER 26R IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008022800281 20080228 00281 NM 2008 2 28 DHL2007748013 1 20071002 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 1030 - 1100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 SEAT TRACK BS 1050-1130 LBL 45 CORRODED. REMOVED SEAT TRACK SECTION AT MAIN CABIN STATION 1070 TO 1090 LBL 45 IAW B-727 SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION MATERIAL USED BAC 1520-792-7178-T616 PO NR 9005692 DIMENSION 69" LONG, 2 EACH ANGLE MATERIAL USED P/N BAC 1503-100126 7178-T6311 DIMENSION (14" BY 2.5") AND 1 EACH FILLER STRAP MATERIAL USED 7075-T6 0.250" PO NR 9003467 DIMENSION (7" BY 2") IAW B-727 SRM 53-10-5 FIGURE 1. TREATED AND PRIMED PARTS AND AREA IAW B-727 SRM 51-10-2. INSTALLED NEW PARTS IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008022800283 20080228 00283 NM 2008 2 28 DHL2007748024 1 20071018 A 5314 KEELBEAM BOEING 727 727225 1384077 NM BS 870 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 RAM KEEL BEAM LOWER CHORD CRACKED BS 870. TRIMMED CRACKED AREA OF KEEL BEAM. FABRICATED AND INSTALLED REPAIR DOUBLER I AW SB 727-53-0208 REV 1 MATERIAL USED 0.071" 15-5PH STEEL. HEAT TREATED TO 170-190 KSI PER BRADDOCK METAL SPECS PO NR 7 307279 8.75" BY 4" CADMIUM PLATED DOUBLER IAW BOEING SOPM 20-42-01 AND FASI FORM FAS0036 REV 4 PO NR FOR DOUBLER 6522231 . TREATED AND PRIMED PARTS AND AREA IAW B-727 SRM 51-10-2. 2 L 7 3 4F A3WE 2008022800284 20080228 00284 NM 2008 2 28 UPS08M51680 1 20071230 A 5320 STIFFENER DOUG MD11 MD11 3023602 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C RIGHT WING FIXED L/E COMPT AT STA XORS 690 APPROX FOUND STIFFENER CRACK AS MARKED. CRACKED STIFFENER AT RT WING FIXED L/E COMPT AT STA XORS 690 AREA REMOVED PER SRM 51-31-01 V.II R35. NEW STIFFENER FAB PER DWG ARB2923-4. HOLES TRANSFERRED ONTO NEW STIFFENERS PER SRM 51-31-01 V.II R35. NEW FAB STIFFENER REPROTECTED PER SRM 51-21-01 V.II R35. NEW FAB STIFFENER INSTALLED AT RT WING FIXED L/E COMPT PER SRM 51-35-01 V.II R35 & 51-33-01 V.II REV 35. 2 L 7 3 4F RT A22WE 2008022800279 20080228 00279 NM 2008 2 28 DHL2007748002 1 20071018 A 5320 ANGLE BOEING 727 727225 1384077 NM BS 870 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 RIGHT WHEEL WELL STATION 870 RBL 8, VERTICAL ANGLE IS CRACKED. REMOVED AND REPLACED VERTICAL ANGLE IN RIGHT WHEEL WELL STATION 870 RBL 8 IAW B-727 SRM 51-30-5 AND 51-30-2. 2 L 7 3 4F A3WE 2008022800282 20080228 00282 NM 2008 2 28 DHL2007748017 1 20071011 A 5311 FRAME BOEING 727 727225 1384077 NM BS 990 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 FRAME DENTED AT BS 990 JUST ABOVE STRINGER 27L. CUT DAMAGE AREA AT BS 990 ABOVE STRINGER 27L DIMENSION 1" BY .75" IAW B -727 SRM 51-40-3 FIGURE 1. FABRICATED FRAME REPAIR FROM 7075-O PO NR 9004690 DIMENSION 9" BY 4" IAW B-727 SRM 51-40-3 F IGURE 1. HEAT TREATED PART FROM 7075-0 TO 7075-T6 IAW FAS REPORT NR 2-37153-801 REV A FORM NR FAS0115 REV 11. PART AND AREA TREATED AND PRIMED IAW B-727 SRM 51-10-2. FRAME REPAIR INSTALLED AT BS 990 ABOVE STRINGER 27L IAW B-727 SRM 51-40 -3 FIGURE 1 AND 53-10-2 FIGURE 5. 2 L 7 3 4F A3WE 2008022800285 20080228 00285 NM 2008 2 28 DHL2007748025 1 20071025 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 940 S18A L CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 LEFT WHEEL WELL STRINGER 18A CRACKED AT BS 940. CUT OUT DAMAGED SECTION OF STRINGER 18A LEFT AFT OF STATION 940 NDT ARE A IAW B-727 NDTM PT 6 51-00-00 FIGURE 23. NO CRACK BEYOND CUT OUT. FABRICATED AND INSTALLED REPAIR PARTS IAW BOEING SV C REQUEST AND REPAIR SKETCH NR 1-635344962. MATERIAL USED: ANGLES 2 EACH 0.100" 4130 STEEL AND 1 STRAP 0.100" 4130 STEE L PO NR 627737, RADIUS FILLERS 2 EACH 0.040" 4130 STEEL PO NR 314613 ALL STEEL PARTS HEAT TREATED TO 160-180 KSI IAW BRA DDOCK METAL SPECS PO NR 7307388 STRINGER REPAIR FILLER 21.5" LONG P/N 65-58488-47 PO NR 7307281. ALL PARTS AND AREA TRE ATED AND PRIMED IAW B-727 SRM 51-10-2. 2 L 7 3 4F A3WE 2008022800121 20080228 00121 NM 2008 2 28 DHL2007742027 1 20071203 A 5322 SHEAR TIE BOEING 727 727225 1384077 NM BS 720F S26-27L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 BS 720F BETWEEN STRINGER 26L AND 27L FRAME SHEAR TIE HAS CORROSION. CUT OUT DAMAGED AREA APPROXIMATE DIMENSION 5.5" BY 2.125" IAW B-727 SRM 53-10-3 FIGURE 11. FABRICATED REPAIR DOUBLER FROM 7075-T6 0.071 PO NR 9005482 APPROXIMATE DIMENSIO N 4.25" BY 5.375" IAW B-727 SRM 53-10-2 FIGURE 11 AND SRM 53-10-2 FIGURE 3. TREATED AND PRIMED REPAIR DOUBLER IAW B-727 SRM 51-10-2. INSTALLED FRAME SHEAR TIE REPAIR AT BS 720F BETWEEN STRINGER 26L AND 27L IAW B-727 SRM 53-10-3 FIGURE 11. 2 L 7 3 4F A3WE 2008022800123 20080228 00123 NM 2008 2 28 DHL2007742031 1 20071211 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 930 S18A R CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 STRINGER 18A RIGHT CRACKED AT BS 930. CUT OUT DAMAGED SECTION AT STRINGER 18A RIGHT FROM BS 940 AFT APPROXIMATE DIMENSI ON 21.375" IAW EVA:B253-00027. FABRICATED 2 EACH STEEL ANNEALED REPAIR ANGLES APPROXIMATE DIMENSION 21.5" BY 1" BY 1" F ROM 4130 NORMALIZED STEEL 0.100" PO NR 627737. FABRICATED REPAIR STRAP FROM 4130 NORMALIZED STEEL 0.100" PO NR 627737 A PPROXIMATE DIMENSION 21.5" BY 3". FABRICATED 2 EACH RADIUS FILLERS FROM 4130 NORMALIZED STEEL 0.090" APPROXIMATE DIMENS ION 21.5" BY 1" IAW ASTAR EVA B253-00027. HEAT TREATED REPAIR PARTS TO 160-180 KSI IAW ASTAR EVA B253-00027, CADMIUM PL ATED REPAIR PARTS IAW FAS FORM NR FAS0036 REV 4. LOCATED AND DRILLED AND TRIMMED STRINGER 18A REPLACEMENT APPROXIMATE D 2 L 7 3 4F A3WE 2008022800321 20080228 00321 NM 2008 2 28 DHL2007793028 1 20071206 A 5322 SHEAR TIE BOEING 727 727247 138408F NM BS 1130 S29-30R CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 CORROSION ON SHEAR TIE AT STATION 1130 BETWEEN STRINGER 29R AND 30. REMOVED SHEAR TIE AT AFT CARGO COMPARTMENT STATION 1130 STRINGER 29R TO 30 AS REQUIRED IAW B-727 SRM 53-10-4 FIGURE 15. FABRICATED NEW SHEAR TIE ANGLE MATERIAL USED 7075- T6 0.063" PO NR 9006022 DIMENSION 4.75" BY 2" IAW B-727 SRM 53-10-4 FIGURE 15. TREATED AND PRIMED SHEAR TIE AND AREA IA W B-727 SRM 51-10-2. INSTALLED SHEAR TIE IAW B-727 SRM 53-10-4 FIGURE 15. 2 L 7 3 4F A3WE 2008022800276 20080228 00276 NM 2008 2 28 DHL2007742055 1 20071118 A 5311 FRAME BOEING 727 727225 1384077 NM BS 950F DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 MULTIPLE DENTS AFT PIT FRAME BS 950F BETWEEN STRINGER 26L AND 25L. CUT OUT DAMAGED AREAS (2 EACH DIMENSION 1" BY 1"). FABRICATED REPAIR ANGLE FROM 7075-0 0.080" PO NR 9005665 (DIMENSION 17" BY 5.5") IAW B-727 SRM 53-10-2 FIGURE 5 AND 51-4 0-3 FIGURE 1. HEAT TREATED ANGLE TO T6 IAW FAS ENGINEERING REPORT NR 2-37153-801 REVA. TREATED AND PRIMED NEW ANGLE IA W B-727 SRM 51-10-2 AND INSTALLED REPAIR ANGLE AT AFT PIT FRAME BS 950F BETWEEN STRINGER 25L AND 26L IAW B-727 SRM 51-30 -2 AND 51-40-3 FIGURE 1. 2 L 7 3 4F A3WE 2008022800278 20080228 00278 NM 2008 2 28 DHL2007742060 1 20071209 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 660 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 FLOORBEAM SPLICE PLATE AT LBL 65 BS 660 HAS CRACK FROM SLOT RADIUS. REMOVED CRACK FLOORBEAM SPLICE PLATE IAW B727 SRM 5 1-30-2 AND AEI DRAWING NR AE727-3-A004. FABRICATED NEW SPLICE PLATE FROM 2024-T3 0.125" PO NR 9005802 APPROXIMATE DIMEN SION 10.9375" BY 6.75" BY 6.125" BY 4.8125" IAW AEI DRAWING NR AE727-1-042 REV E AND JC EC00670-001. INSTALLED NEW PLAT E AT FLOOR BEAM BS 660 LBL65 IAW AEI DRAWING NR AE727-1-042 REV E AND B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008022800320 20080228 00320 NM 2008 2 28 DHL2007793018 1 20071130 A 5522 SKIN BOEING 727 727247 138408F NM ELEVATOR CANNING A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 DENT, PLUS OIL CANNING ON TOP OF ELEVATOR SKIN, ELEVATOR STATION 99.79 LEFT SIDE. CUT OUT DAMAGE AREA AT ELEVATOR SKIN STATION 99.75 LEFT SIDE DIMENSION CUT OUT 2.5" BY 1.625"IAW B-727 SRM 55-20-3 FIGURE 5. FABRICATED DOUBLER REPAIR MATER IAL USED 2024-T3 0.032" PO NR 9006027 DIMENSION 6.25" BY 4.625" IAW B-727 SRM 53-20-3 FIGURE 5. TREATED AND PRIMED PART IAW B-727 SRM 51-10-2. INSTALLED DOUBLER IAW B-727 SRM 55-20-3 FIGURE 3. CALCULATED REPAIR MOMENT "M" AT 132 (.009 RE MOVED .144 ADDED) BY 18"(Y) = 2.376. ORIGINAL MOMENT 117.813 + 2.376 = NEW MOMENT 120.189 FOUND WITHIN LIMITS 120 +/- 5 . NO FURTHER ACTION REQUIRED IAW B-727 51-80-2. 2 L 7 3 4F A3WE 2008030400012 20080304 00012 NM 2008 3 4 DHL2007748032 1 20071024 A 5753 SKIN BOEING 727 727225 1384077 NM WBL 124 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 LEFT INBOARD MID FLAP UPPER SURFACE WBL124 AT MID SPAR SKIN IS CRACKED AT LOCK FASTENER. REMOVED FASTENERS ON LEFT INBO ARD MID FLAP UPPER SURFACE COMMON TO MID FLAP SPAR STA 124.2 IAW SRM 51-30-2. C/W HFEC IAW NDT PT 6 51-00-00 FIGURE 23, ALUMINUM PART SURFACE INSPECTION AND PT 6 51-00-00 FIGURE 16 ALUMINUM PART FASTENER HOLE INSPECTION (ROTARY SCANNER). NO RELEVANT INDICATIONS WERE NOTED IN FASTENER HOLES. C/W HFEC IAW NDTM PT 6 51-00-00 FIGURE 23 ALUMINUM PART SURFACE I NSPECTION OF UPPER SKIN CRACK MARKED END OF CRACK ABOVE LOCK FASTENERS COUNTERSINK. CUT DAMAGE AREA DIMENSION 1" BY 1" IAW DRAWING NR ES87100018-001-B REV 1R. FABRICATED REPAIR FILLER IAW DRAWING NR ES87100018-001-B REV IR. PARTS AND ARE 2 L 7 3 4F A3WE 2008030400013 20080304 00013 NM 2008 3 4 DHL2007793002 1 20071201 A 5753 STRUCTURE BOEING 727 727247 138408F NM TE FLAPS CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 LT WING MID FLAP, CRACKS IN TRAILING EDGE CUT OUT FOR INBOARD AFT FLAP ACTUATION ROD. CUT OUT DAMAGED SECTION OF LT WIN G INBOARD MID FLAP 47" LONG AT INBOARD ACTUATOR ROD IAW SRM 51-40-4. FABRICATED AND INSTALLED NEW SECTION AND SPLICE DO UBLER IAW SRM 51-40-4 AND 57-50-2 FIGURE 5. DOUBLER IS 7.5" LONG, SECTION IS 47" LONG. TREATED AND PRIMED PART AND ARE A IAW SRM 51-10-2. 2 L 7 3 4F A3WE 2008030400016 20080304 00016 NM 2008 3 4 DHL2007793001 1 20071120 A 5313 STRINGER BOEING 727 727247 138408F NM BS 740 S27R CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 FORWARD CARGO COMPARTMENT, STRINGER 27R IS CORRODED AT STATION 740. REMOVED CORRODED PORTION OF STRINGER 27R, FABRICATE D AND INSTALLED REPAIR PARTS, STRINGER PORTION 5" BAC 1498-147 PO NR 7332238 AND SPLICE SECTION BAC 1498-131 PO NR 73322 31 11" IAW SRM 53-10-3, 51-30-2 AND 51-10-2. 2 L 7 3 4F A3WE 2008030400019 20080304 00019 NM 2008 3 4 DHL2007793016 1 20071207 A 5347 SEAT TRACK BOEING 727 727247 138408F NM BS 740-830 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 CABIN SEAT TRACK HAS CORROSION AT BS 740 TO 830 RBL 24. REMOVED SECTION AS REQUIRED IAW SRM 51-30-2. FABRICATED NEW SE CTION IAW SRM 51-20-1 AND 53-10-2 FIGURE 7. TREATED AND PRIMED NEW SECTION IAW SRM 51-10-2. INSTALLED NEW SECTION IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008030400021 20080304 00021 NM 2008 3 4 DHL2007793017 1 20071207 A 5347 SEAT TRACK BOEING 727 727247 138408F NM BS 500-680 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 CABIN SEAT TRACK HAS CORROSION AT BS 500 TO 680 LBL45. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED 2 EACH SECTION SE AT TRACKS , 2 ANGLE REPAIRS, AND 1 STRAP IAW SRM 53-10-5 FIGURE 1. TREATED AND PRIMED PART IAW SRM 51-10-2. INSTALLED 2 SECTION SEAT TRACKS AND SPLICES IAW SRM 53-10-5 FIGURE 1. 2 L 7 3 4F A3WE 2008030400022 20080304 00022 NM 2008 3 4 DHL2007793019 1 20071202 A 5522 SKIN BOEING 727 727247 138408F NM ELEVATOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 DENT, UNDERNEATH ELEVATOR SKIN PANEL AT ELEVATOR STATION 50.50 LT. CUT OUT DAMAGE AREA AT LT ELEVATOR LOWER SKIN IAW SR M 55-20-3 FIGURE 4. FABRICATED REPAIR DOUBLER IAW SRM 55-20-3 FIGURE 4 AND 55-20-3 FIGURE 1. PART AND AREA TREATED AND PRIMED IAW SRM 51-10-2 FIGURE 1. REPAIR DOUBLER INSTALLED AT LT ELEVATOR LOWER SKIN IAW SRM 55-20-3 FIGURE 4. CALCULA TED REPAIR MOMENT "M" 0.066 TIMES 10.5" = 0.0693. ORIGINAL MOMENT WAS 120.189 + 0.0693 = NEW MOMENT OF 120.882, FOUND TO BE WITHIN LIMITS. NO FURTHER ACTION REQUIRED IAW SRM 51-80-7 PARA 2 FIGURE 1. 2 L 7 3 4F A3WE 2008030400026 20080304 00026 NM 2008 3 4 DHL2007793025 1 20071201 A 5311 FRAME BOEING 727 727247 138408F NM BS 1110 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 AFT CARGO COMPARTMENT FRAME AT FS 1110 UPPER FLANGE IS DENTED BETWEEN STRINGER 27L AND 26L. CUT OUT DAMAGED IAW SRM 51- 40-3 FIGURE 1. FABRICATED REPAIR FRAME IAW SRM 51-40-3 FIGURE 1 AND 53-10-2 FIGURE 5. HEAT TREATED PART IAW NR FAS0115 REV 11. TREATED AND PRIMED PART IAW SRM 51-10-2. INSTALLED FRAME REPAIR IAW SRM 51-30-2 AND 53-10-2 FIGURE 5. 2 L 7 3 4F A3WE 2008030400027 20080304 00027 NM 2008 3 4 DHL2007793027 1 20071212 A 5322 SHEAR TIE BOEING 727 727247 138408F NM BS 700 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 INTERGRANULAR CORROSION NOTED ON BS 700 FRAME LOWER LIP BETWEEN STRINGERS 27R AND 28R FORWARD PIT. CUT OUT DAMAGE. FAB RICATED AND INSTALLED A DOUBLER REPAIR IAW SRM 53-10-4 FIGURE 13 AND 53-10-2 FIGURE 2. HEAT TREATED TO T6 CONDITION IAW FAS0115 REV 11 AND ER 2-37153-801 REV A. 2 L 7 3 4F A3WE 2008030400028 20080304 00028 NM 2008 3 4 DHL2007793030 1 20071202 A 5347 SEAT TRACK BOEING 727 727247 138408F NM BS 850 - 950C CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 CABIN SEAT TRACK CORRODED AT BS 870 TO 959 LBL45. FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-5 FIGURE 1. TREATED AND PRIMED PART IAW SRM 51-10-2. INSTALLED NEW SECTION IAW SRM 53-10-5 FIGURE 1. 2 L 7 3 4F A3WE 2008030400030 20080304 00030 NM 2008 3 4 DHL2007793005 1 20071204 A 5330 SKIN BOEING 727 727247 138408F NM BS 1220 S19R CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 DENT RT FUSELAGE SKIN BS 1220 ABOVE STRINGER 19R. EVALUATED DENT AND FOUND IT TO BE WITHIN LIMITS IAW SRM 53-30-1 FIGU RE 1. HFEC SHOW CRACK AT DENT AREA IAW NDT PT 6 51-00-00 FIGURE 23. CUT OUT DAMAGE AREA IAW SRM 53-30-3 FIGURE 1. FA BRICATED DOUBLER REPAIR IAW SRM 53-30-3 FIGURE 1 AND 53-30-2 FIGURE 3. TREATED AND PRIMED PART AND AREA IAW SRM 51-30- 2. INSTALLED REPAIR IAW SRM 51-30-2 AND 53-30-3 FIGURE 1. 2 L 7 3 4F A3WE 2008030400031 20080304 00031 NM 2008 3 4 DHL2007793023 1 20071201 A 5410 DUCT BOEING 727 727247 138408F NM CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 CRACK AT "S" INSIDE DUCT INLET 7 O'CLOCK POSITION BS 1130. REMOVED PREVIOUS REPAIR AND FILLER ON "S" DUCT AT 7 O'CLOCK POSITION BS 1130 IAW SRM 51-30-2 FIGURE 1. REMOVED FRAME IAW SRM 51-30-2 FIGURE 1. FABRICATED NEW FILLER FRAME. FABRI CATED REPAIR DOUBLER IAW SRM 54-10-2 FIGURE 5 AND 54-10-3 FIGURE 10. PARTS AND AREA TREATED AND PRIMED IAW SRM 51-10-2 FIGURE 1. REPAIR AND FRAME INSTALLED IAW SRM 54-10-3 FIGURE 10. 2 L 7 3 4F A3WE 2008030400032 20080304 00032 NM 2008 3 4 DHL2007793032 1 20071211 A 5410 NOSE COWL BOEING 727 727247 138408F NM NR 1 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 NR 1 ENGINE NOSE COWL EXTERIOR SKIN SURFACE AT 12 O'CLOCK POSITION JUST OUTBOARD OF INSPECTION PANEL HAS A 2" LONG CRACK RUNNING FROM RIVET HEAD. CUT OUT DAMAGED SECTION. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 54-30-3 FIGURE 3 AN D 3A. 2 L 7 3 4F A3WE 2008041000169 20080410 00169 CE 2008 4 10 VQMA051807001 1 20070518 A 3411 CM29337 STATIC PORT CESSNA 500 560CESSNA 2076750 CE LEAKING E VQMA K NONE O OTHER IN INSP/MAINT 1 NM 03 225CV 7414 400 0225 DURING AVIONICS MAINTENANCE FOUND PILOT'S STATIC PORT LEAKING. 2 L 7 2 4F RT A22CE 2008041000176 20080410 00176 CE 2008 4 10 VQMA081907001 1 20070809 A 3230 99140993 BOTTLE CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP MLG LEAKING E VQMA K NONE O OTHER IN INSP/MAINT 1 NM 03 650Z 11697 11697 6500108 GEAR PNEUMATIC BLOWDOWN BOTTLE IS LEAKING. 2 L 7 2 4F 4 F A9NM E6WE 2008041000177 20080410 00177 CE 2008 4 10 VQMA121807001 1 20071218 A 3230 99140993 BOTTLE CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP MLG LEAKING E VQMA K NONE O OTHER IN INSP/MAINT 1 NM 03 650Z 147 147 6500108 EMERGENCY GEAR PNEUMATIC BOTTLE HAS TO BE SERVICED REPEATEDLY. 2 L 7 2 4F 4 F A9NM E6WE 2008041100120 20080411 00120 EA 2008 4 11 SWIA200719453 1 20071223 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 454SW 7749 FOUND AT C-CHECK, STA 280 AT LBL 9 UPPER FLOORBEAM IS CRACKED. COMPLIED WITH REPAIRS IAW CRJ200 REO 601R-53-11-138. 2 L 7 2 4F RT A21EA 2008041100121 20080411 00121 EA 2008 4 11 SWIA200719454 1 20071223 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 454SW 7749 STA 280 AT RBL 9 LOWER FLOORBEAM IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH FLOORBEAM REPAIR PER 601R -53-11-1305/601R 53-11-171. 2 L 7 2 4F RT A21EA 2008041100122 20080411 00122 EA 2008 4 11 SWIA200719455 1 20071223 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 454SW 7749 EMERGENCY LIGHT FLOOR TRACK IS INOP, FOUND AT C-CHECK. REPAIRED WIRING FOR EMERGENCY LIGHTS PER CRJ200 ECSPM 20-17-80 P G 2-5. 2 L 7 2 4F RT A21EA 2008041100126 20080411 00126 EA 2008 4 11 SWIA200719456 1 20071223 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY NO TEST A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 454SW 7749 NUMBER 2 CARGO FIRE TEST IS INOP, FOUND AT C-CHECK. REPLACED NR 2 SMOKE DETECTOR PER CRJ200 AMM 26-15-00-440-801. 2 L 7 2 4F RT A21EA 2007022200195 20070222 00195 NM 2007 2 22 SWAA070891 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200196 20070222 00196 NM 2007 2 22 SWAA070890 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200199 20070222 00199 NM 2007 2 22 SWAA070899 1 20070215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200202 20070222 00202 NM 2007 2 22 SWAA070776 1 20070213 A 5344 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022200212 20070222 00212 2007 2 22 SWAA070750 4 20070213 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007022200216 20070222 00216 GL 2007 2 22 15HA0758001 2 20070110 A 7321 4002604 AMPLIFIER CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13 03004 GL ZONE 400 DAMAGED A I5HA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 23 584E 24 ON TAKEOFF ROLL THE RT ENGINE FAILED TO MAKE TAKEOFF POWER. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO BLOCKS. M AINTENANCE FOUND THAT THE TEMPERATURE DATUM (TD) FUEL CONTROL SYSTEM HAD DRIVEN TO THE FULL (TAKE) POSITION RESULTING IN LOW POWER DURING THE TAKEOFF ROLL. MAINTENANCE FOUND A PIN PUSHED BACK IN THE CONNECTOR FOR THE TD AMPLIFIER. THE AIR CRAFT WAS RUN WITH THE TD SYSTEM IN (NULL) AND OPERATION WAS NORMAL. THE TD SYSTEM WAS DEFERRED PENDING FURTHER TROUBLE SHOOTING. ON JANUARY 14, 2007, THE CONNECTOR WAS REPAIRED AND THE DEFERRAL CLEARED. LOG PAGE 75597 TAT 60357.9. 2 L 7 2 4R 4 T 6A6 E282 2007022200217 20070222 00217 GL 2007 2 22 SWAA071020 2 20070220 A 7297 D404 CONNECTOR BOEING 737 7373H4 1384600 NM CFMINT CFM56 CFM563B1US GL NR 2 ENGINE FAULTY A SWAA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 SW 29 379SW 26586 720563 INFLIGHT SHUTDOWN/AIRTURN BACK/DECLARED EMERGENCY. NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. REMAINED ON WITH THRUST LEVER CLOSED. ENGINE SHUTDOWN PER QRH. FOUND D404 CONNECTOR FAULTY. REMOVED AND REPLACED CONNECTOR PE R MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2007022200223 20070222 00223 NM 2007 2 22 SWAA071048 1 20070220 A 5330 6545765 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007022200227 20070222 00227 NM 2007 2 22 SWAA071033 1 20070220 A 5210 6545871 DOOR FRAME BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR FRAME CRACKED AT LOWER AFT CORNER. REMOVED AND REPLACED R1 DOOR PER MM. 2 L 7 2 4F RT A16WE 2007022300004 20070223 00004 SO 2007 2 23 C2XA07CL022 1 20070215 A 4950 4952375 BLEED VALVE EMB 145 EMB145LR 3260212 SO APU FAULTY A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 14977 5688 145175 CLE FLIGHT 2212 THE CREW REPORTED AFTER STARTING THE APU THERE WAS A STRONG FUEL SMELL. MAINTENANCE INSPECTED AND REPLA CED THE APU BLEED VALVE. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007022300021 20070223 00021 NM 2007 2 23 UPS07549212 1 20070203 A 5311 146N100527 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 413UP 23853 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1280, S26L. FRAME REPAIR AT STA 1280, S26L HAS BEEN ACCOMPLISHED PER EA 757-536 2-27-A1602 WITH NO DEVIATIONS AND PER UPS EO B757-5310-26175-A. 2 L 7 2 4F RT A2NM 2007022300024 20070223 00024 NM 2007 2 23 UPS07549217 1 20070207 A 5311 143N1024115 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 413UP 23853 INSPECTION TYPE:C DENTS IN FORWARD CARGO FUSELAGE FRAME STA 680, APPROX S23L TO S24L (2EA). FRAME REPAIR AT STA 680, S2 3L TO S24L (2EA) DENTS HAS BEEN ACCOMPLISHED PER EA 757-5332-27-A1605 AND UPS EO B757-5310-26179A WITH NO DEVIATIONS. 2 L 7 2 4F RT A2NM 2007022300026 20070223 00026 NM 2007 2 23 UPS07549219 1 20070207 A 5311 143N1018 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 413UP 23853 INSPECTION TYPE:C DENT IN FORWARD CARGO FUSELAGE FRAME STA 780, S23L TO S24L. FRAME REPAIR AT STA 780, S23L TO S24L HAS BEEN ACCOMPLISHED PER EA 757-5310-27-A1607, WITH NO DEVIATIONS AND PER UPS EO B757-5310-2 6180-A. 2 L 7 2 4F RT A2NM 2007022300027 20070223 00027 NM 2007 2 23 UPS07549221 1 20070203 A 5311 146N1019 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 413UP 23853 INSPECTION TYPE:C DENTS IN AFT CARGO FUSELAGE FRAME STA 1560 BETWEEN S25R TO S27R (2EA). FRAME REPAIR AT STA 1560, S25 R TO S27R HAS BEEN ACCOMPLISHED PER EA 757-5310-27-A1600 WITH NO DEVIATIONS AND PER UPS EO B757-5310-26178-A. 2 L 7 2 4F RT A2NM 2007022300047 20070223 00047 WP 2007 2 23 DHL2007802525 1 20070130 A 5755 SKIN DOUG DC8 DC873 302199C WP SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 NR 2 LT SPOILER PANEL DELAMINATED. REMOVED AND REPLACED NR 2 LT SPOILER PANEL IAW MM 27-61-1 PG 201-206. REFER TO NR 0 71624 FOR OPS CHECK. 2 L 7 4 4F RT 4A25 2007022300055 20070223 00055 NM 2007 2 23 SWAA070536 1 20070201 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 390, BL 0, RADIO ALTIMETER ANTENNA CUTOUT. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007022300072 20070223 00072 NM 2007 2 23 07FDEA00540 1 20070222 A 5410 NONE BOEING 727 727227 1384078 NM NACELLE NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 240FE 20978 NACELLES AND PYLONS MINOR DEVIATION TO SRM S DUCT HOUSING SKIN REPAIR. COMPLIED WITH EA 7-5410-102026 THIS ITEM CLEARED BY REPAIR PER SRM 54-10-3 FIG 4 WITH MINOR DEVIATION DOCUMENTED BY THIS EA. 2 L 7 3 4F A3WE 2007022300073 20070223 00073 NM 2007 2 23 SWAA070594 1 20070204 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 222WN 34290 DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER MISSING AT ROW 2 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007022300084 20070223 00084 NM 2007 2 23 SWAA070607 1 20070205 A 5523 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED 12Y CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB BEARING PER MM. 2 L 7 2 4F RT A16WE 2007022300102 20070223 00102 NM 2007 2 23 AALA20070341 1 20070216 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 919AN 29520 TPA - FOUND EMERGENCY SEAT MOUNTED LIGHT AT SEAT 18D INOPERATIVE. RECONNECTED CONNECTOR WIRE FORE EMERGENCY SEAT MOUNTE D LIGHT AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007022300106 20070223 00106 NM 2007 2 23 2007UALA00409 1 20070211 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY EXIT EEL LIGHT INOP, JUST FWD OF LAV 111 LEFT AISLE. REPAIRED FEEDER CABLE. OPS CKS. NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022300109 20070223 00109 WP 2007 2 23 AALA20070332 1 20070214 A 3213 SEAL DOUG DC9 DC982 3022082 WP NLG STRUT DAMAGED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7508 49802 ORD INFLIGHT T644/14FEB - COULD NOT RETRACT LANDING GEAR. RED UNSAFE INDICATION. RETURNED TO ORD AND LANDED WITHOUT IN CIDENT. REPACKED NOSE LANDING GEAR STRUT SEALS AND REPLACED LOWER TURNING TUBE BEARING. SERVICED STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007022300127 20070223 00127 NM 2007 2 23 2007UALA00412 1 20070212 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 DOOR 1R EMERGENCY CEILING LIGHT INOP. REPINNED CONNECTOR. CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022300132 20070223 00132 NE 2007 2 23 AALA20070329 2 20070213 A 7230 BLADE BOEING 777 777223 1385213 NM RROYCE RB211 RB211TRENT89 NE COMPRESSOR FAILED A AALA A UNSCHED LANDING J R WARNING INDICATION PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 21 770AN 29578 51165 ORD INFLIGHT T289 - LEFT ENGINE COMPRESSOR STALL JUST AFTER LIFT OFF. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REP LACED NUMBER ONE ENGINE ON 17 FEB AT ORD DUE TO FAILURE OF NUMBER SIX HIGH PRESSURE COMPRESSOR BLADE. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT T00001SE E00050EN 2007022300155 20070223 00155 NM 2007 2 23 AALA20070317 1 20070210 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 778AN 29587 DFW - FOUND EMERGENCY LIGHTS AT SEAT 21C HAS LENS MISSING. RELAMPED AND REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007022300164 20070223 00164 WP 2007 2 23 AALA20070309 1 20070209 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 576AA 53153 LGA - FOUND EMERGENCY LIGHT AT SEAT 5E HAS LENS BROKEN. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007022300165 20070223 00165 NM 2007 2 23 2007UALA00477 1 20070215 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE MISDRILLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 AFT CABIN CREASE BEAM WEB HAS MISDRILLED HOLE 6 INCHES AFT OF BS 947 RBL 55. MAJOR REPAIR ACCOMPLISHED. DAMAGED AREA O F WEB MADE WHOLE WITH A SINGLE LAYER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022300172 20070223 00172 NM 2007 2 23 NOCA04107 1 20070210 A 5320 INTERCOSTAL BOEING 757 75728A 1384976 NM BS 1660-1680 CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 752NA 28174 FOUND R4 AFT DRAIN SUPPORT INTERCOSTAL HAS CORROSION AT NUT PLATES. REPLACED R4 DRAIN SUPPORT PER SRM 51-21-03. 2 L 7 2 4F RT A2NM 2007022300179 20070223 00179 NM 2007 2 23 AWXA200700229 1 20070119 A 5754 WEDGE BOEING 737 73733A 1384673 NM ZONE 500 DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 174 23625 MCN - MAJOR REPAIR - LEFT WING NR 4 SLAT WEDGE UPPER AND LOWER SURFACES DEBONDED, SS 19. REPAIRED LEFT WING NR 4 SLAT W EDGE UPPER AND LOWER SURFACES, SS 12.25 - SS 24.25 IAW B737-300 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 2007022300200 20070223 00200 EU 2007 2 23 07FDEA00444 1 20070209 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 MDC SEAT TRACK 0 AT FR 77.5 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW DWG 18A532-79237. MAJOR REPAIR IAW FEDE X GMM 6-2-100. SEE JPF N00789. 2 L 7 2 4F RT A35EU 2007022300211 20070223 00211 NM 2007 2 23 2007UALA00380 1 20070210 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 UPPER FUSELAGE EXTERNAL SKIN HAS WEAR IN AREA OF DORSAL FIN CONTACT APPROX STA 860 TO 908 LT SIDE AND 860 TO 880 RT SIDE . MAJOR REPAIR. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND INTERNAL STRAP DOUBLER REPAIR PER SRM 5 3-60-01 REPAIR 9. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022300222 20070223 00222 NM 2007 2 23 2007UALA00389 1 20070210 A 3397 58781 POWER STRIP BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 902UA 25002 EMERGENCY EEL LIGHTING INOP FROM ROW 12 AFT. REPLACED POWER STRIP. REPLACED POWER STRIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022300231 20070223 00231 NM 2007 2 23 2007UALA00395 1 20070209 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 EXTERNAL FUSELAGE AFT RIGHT EMERGENCY LIGHT L392 INOP. REPLACED LIGHT. OP CHECKS OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022300244 20070223 00244 EU 2007 2 23 2007UALA00398 1 20070212 A 3350 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 418UA 485 EMERGENCY LIGHT TEST FAULTED AFT LEFT BATTERY. REPLACED AFT LEFT BATTERY. EMERGENCY LIGHT TESTS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022300246 20070223 00246 NM 2007 2 23 07FDEA00495 1 20070213 A 5340 B27530711 STRAP BOEING 727 727227 1384078 NM ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 490FE 21493 DURING WIRING REPAIR WORK, FOUND STABILIZER STRAP AT RBL 24.75 APPROX STA 312 BROKEN, DISOVERED DURING OTHER WORK. REPA IRED FLOOR STRAP PER SRM 53-10-8,FIG 6 P/N B27-53-071-1 STRAP, REPAIR DOUBLER P/N 65-17594-4. 2 L 7 3 4F A3WE 2007022300257 20070223 00257 EU 2007 2 23 2007UALA00452 1 20070214 A 5322 SHEAR TIE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 430UA 568 FWD CARGO PIT CORROSION AT FRAME 29 SHEAR TIES AT STR 43 & 44 LT, 41 & 42 LT, 40 & 41 LT AND 41 & 42 RT. MAJOR REPAIR A CCOMPLISHED: REPLACED SHEAR TIES. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022300262 20070223 00262 2007 2 23 2007UALA00457 4 20070214 A 2565 O-RING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L4 SLIDE BOTTLE FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 198UA 28716 FLIGHT ATTENDANT REPORTS DOOR 4L SLIDE PRESSURE LOWER THAN 2000 PSI. SLIDE ASSY PRESSURE CHECKS NORMAL RANGE. SLIDE P ROBLEM ROOT CAUSE: LEAKING O'RINGS HARDENED BY TIME IN POSITION & COLD. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022300273 20070223 00273 NM 2007 2 23 DLM88070134 1 20070215 A 4990 LINE DOUG MD88 MD88 3023688 NM APU OIL SYSTEM LEAKING A DALA C ABORTED TAKEOFF K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 904DE 53409 ON TAKEOFF AND ENGINE START ODOR FROM A/C SYSTEM CAUSED SMOKE DETECTORS IN REAR TO GO OFF. ODOR DISSIPATED AFTER 15 MIN UTES BUT STILL LINGERS A BIT IN CLIMB. FOUND APU OIL LINE B NUT LOOSE. TIGHTENED SAME LEAK CKS GOOD CLEANED INLET. PE RFORMED PHEN SYS DUCT BURNOUT OP 5089. OK FOR SVC. 2 L 7 2 4F RT A6WE 2007022300286 20070223 00286 NM 2007 2 23 WRLA2007037 1 20070215 A 5320 ANB720314 STIFFENER DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE RT MLG WW CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 62911 48407 DURING 3C + 12A CHECK, EGAT MECHANIC FOUND RIGHT WHEEL WELL DOOR OUTBOARD JAMB ASSY STIFFENER CRACK L =.06" AT STA Y = 1 474. REF DRAWING ANS7203. REMOVED THE CRACKED STIFFENER AND INSTALLED NEW PARTS PER MD-11 SRM 51-35-01 VOL II REV 38. CONDITION CHECK NORMAL AND JOB COMPLETED. 2 L 7 3 4F 4 F RT A22WE E24NE 2007022300287 20070223 00287 NE 2007 2 23 WRLA2007036 2 20070215 A 7230 BLADES DOUG MD11 MD11F 3023600 NM PWA 4460 PW4460 NE NR 2 ENGINE DAMAGED A WRLA J A DUMP FUEL UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 11 279 48756 P733823 JFK/BRU AIR TURNBACK DUE TO ENGINE VIBRATION HIGH ALERT ON NR 2 ENGINE AT 700 FT ON TAKEOFF NR 2 ENGINE COMPRESSOR READS 5.8 VIBRATION AND SOUND PRESENT. WHEN THROTTLE RETARDED VIBRATION CEASED. DUMPED FUEL AND RETURNED BACK FOR LANDING A T JFK. NR 2 ENGINE BOROSCOPED AT AP-2 & AP-3, NO DAMAGE OBSERVED. ALL FAN BLADES REPLACED DUE TO 17 BLADES DAMAGED. E NGINE VIBRATION SURVEY ACCOMPLISHED PER MD-11 MM 71-02-08. 2 L 7 3 4F 4 F RT A22WE E24NE 2007022300292 20070223 00292 NM 2007 2 23 SB07016 1 20070221 A 2750 654643489MC FLAP BOEING 737 7374B7 1384702 NM LT WING OUT OF RIG A USAA O OTHER F FLT CONT AFFECTED DE DESCENT 1 EA 19 459UW 20293 20293 25023 CLT FLT750 ON DESCENT INTO CLT FROM GCM, WHEN FLAPS WERE SELECTED TO 30 UNITS, THE AIRCRAFT ROLLS TO THE LEFT. WINGS CA N BE KEPT LEVEL WITH 3 DEGREES OF RIGHT AILERON. FUEL WAS BALANCED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENAN CE FOUND THE CABLE DRUM CLUTCH SLIPPED IN THE LEFT INBOARD MIDFLAP DUE TO THE AFT FLAP BINDING. RESET CLUTCH. FOUND DE ADWEIGHT ROLLERS ON AFT FLAP NOT RIGGED CORRECTLY. ADJUSTED AFT FLAP PER MM 27-51-11-404. FLAPS TEST GOOD. 2 L 7 2 4F RT A16WE 2007022300306 20070223 00306 NM 2007 2 23 USAA070126 1 20070222 A 5313 STRINGER SPLICE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 BS 360 FRAME & STR 15L, STRINGER SPLICE CHANNEL CRACKED. INSTALLED NEW STRINGER PER SRM 51-10-02, DEFECT SIZE: .5 INCH . 2 L 7 2 4F RT A16WE 2007022300309 20070223 00309 NM 2007 2 23 USAA070123 1 20070222 A 5320 STIFFENER BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 BS 328 RBL 33 ON VERT STIFFENER CRACKED. DEFETIVE PART REPLACED WITH IDENT PART, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007022600020 20070226 00020 EA 2007 2 26 A6WA200740039 1 20070131 A 5753 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA LT WING JAMMED A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 449AW 7818 ON APPROACH INTO YOW, FLAPS FAIL CAS MESSAGE FAILED AT 0 DEGREES, COMPLIED WITH QRH. LANDED AT APPROXIMATELY 40,600 LBS , CREW DID NOT CALL IN DISCREPANCY. NO HES/RTO INSPECTION REQUIRED. INTERROGATED FECU, FECU SHOWS FLAP FAIL WAS DUE TO JAM ON LEFT WING. REMOVED AND REPLACED LT BPSU, OPS CHECK GOOD. INSPECTED FLAPS, NO EVIDENCE OF TWISTING OR SKEWING I AW AWAC SUPPLEMENT 98-018A. RESET FLAP CIRCUIT BREAKERS ONCE, MESSAGE CLEARED. FLAPS OPERATE NORMALLY. PLACED ON 72 H OUR FLAP WATCH. REF 164559/4 FOR DIL FECU INTERROGATION. BRAKE AND POS SENS UNIT P/N 855D100-11, S/N 2262. (M) 2 L 7 2 4F RT A21EA 2007022600037 20070226 00037 WP 2007 2 26 DXTA200701957 2 20070219 A 7200 ENGINE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP RIGHT STALLED E DXTA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 07 862QS 258362 WHILE TRANSFER OF FUEL, A LOSS OF FUEL PRESSURE ON RT ENG FOLLOWED BY A COMPRESSOR STALL, PRESSURE RETURNS WITH FUEL PUM P ON. HAPPENED TWICE. FUEL PRESS DROPS WITH PUMP OFF, WITH A LOUD BANG & KICK. PRESSURE RETURNED WITH PUMP ON. COULD NO T DUPLICATE. TRANSFER LEVER STIFF TO OPERATE. INSPECTED CROSSFEED QUADRANT, NO DEFECTS NOTED. CLEANED & LUBED TRANSFER Q UADRANT. RAN ACFT AT IDLE & TAKE-OFF POWER. CYCLED FUEL PUMPS, NO CHANGE IN READINGS. CYCLED FUEL PUMPS WHILE TRANSFERIN G & CROSSFEEDING FUEL. NO CHANGE. VISUAL INSPECTION OF 1ST STAGE FAN. NO DEFECTS. FUEL TANKS SUMPED & NO WATER OR DEBRIS FOUND. INSPECTED P2/T2 SENSOR. NO DEFECTS NOTED. ALL WORK PERFORMED IAW 800XP MM 72-00-00 & LMM TFE731-5BR 75-40-01. 2 L 7 2 4F 4 F RT A3EU E6WE 2007022600038 20070226 00038 CE 2007 2 26 DXTA200701956 1 20070219 A 3230 LANDING GEAR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MALFUNCTIONED E DXTA O OTHER S J AFFECT SYSTEMS WARNING INDICATION DE DESCENT 1 GL 07 966QS 7500166 GEAR RED UNSAFE LIGHT CAME ON WITH EXTENSION OF THE LANDING GEAR ALONG WITH 3 GREEN GEAR LIGHTS. ACCOMPLISHED CHECKLIST ITEMS. RED UNSAFE LIGHT WENT OUT. BLEW GEAR DOWN AND PULLED UP LOCK HANDLES. NORMAL LANDING AND TAXI IN WAS ACCOMPLISHE D. RESET MLG AND MLG MANUAL UPLOCK RELEASE RESET PNEUMATIC OVERRIDE VALVE. RESET VALVE ON GEAR N2 BOTTLE. PERFORMED 15 FAULT FREE CYCLES, ALL INDICATIONS OPERATED NORMAL. NO DEFECTS NOTED. SERVICED GEAR BOTTLE WITH N2. WORK PERFORMED IAW C E-750 MM 32-00-01. REF FAS WO 07-437 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007022600039 20070226 00039 EA 2007 2 26 A6WA200740037 1 20070128 A 3220 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA NOSE ICED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 444ZW 7788 AFTER TAKEOFF SELECTED GEAR UP, MAINS CAME UP AND STOWED FULLY. NLG REMAINED DOWN AND LOCKED. COMPLIED WITH QRH, NO HE LP. INSPECTED NOSE GEAR, FOUND EXCESSIVE ICE ACCUMULATION, REMOVED ICE AS REQUIRED. PERFORMED SEVERAL GEAR SWINGS REF AMM 07-11-01. CLEANED PROXIMITY SWITCHES AS REQUIRED. NO DEFECTS NOTED. (M) 2 L 7 2 4F RT A21EA 2007022600040 20070226 00040 2007 2 26 AMW082646 4 20070214 A 2220 6229682002 DPU BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE WILL NOT ARM A AMWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 161YV 19708 UE161 AFTER T/O, THE FOS FEES COMPARE (PUSH TO RESET) BUTTON ILLUMINATED AND WOULD NOT RESET. AC RETURNED TO FIELD WITH NO O THER INCIDENT. REMOVED AND REPLACED NR1 DPU, INSPECTED WIRING, OPS NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007022600041 20070226 00041 CE 2007 2 26 AMW070219056 1 20070219 A 5511 10162000061 SPAR BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA HORIZONTAL STAB CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 146ZV UE146 HORIZONTAL STAB MAIN SPAR CENTER WEB (4 EA) 0.5 INCH LONG CRACKS EXTENDED OUT FROM DEICE TUBE HOLE. FABRICATED/INSTALLE D WEB PATCH. 2 L 7 2 4T 3 T RT A24CE E2NE 2007022600042 20070226 00042 EA 2007 2 26 QXEA200700244 2 20070222 A 7200 ENGINE BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA NR 2 UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 421QX 4149 LAX FLIGHT NR 2343: AS THE AIRCRAFT TAXIED ONTO THE RUNWAY, THE POWER PLANT MESSAGE APPEARED ON THE ED. AIRCRAFT RETURN ED TO GATE. MAINTENANCE UPON INTERROGATION OF CDS FOR ENGINE FAULTS, FOUND NR 2 ENGINE LANE B FAULT 130. C/W FIM TASK 61-20-03-810-815. AFTER FAULT CODE WAS CLEARED, RAN NR 2 ENGINE TWICE IN BETA RANGE. FAULT DID NOT RETURN. NO PARTS R EPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2007022600043 20070226 00043 NM 2007 2 26 SWAA071073 1 20070222 A 3233 273A21012 ACTUATOR BOEING 737 7377H4 1384404 NM MLG FAULTY A SWAA O OTHER J WARNING INDICATION AP APPROACH 1 SW 29 739GB 29275 ON APPROACH WHEN LANDING GEAR SELECTED LEFT MLG INDICATION REMAIN RED AND NO GREEN INDICATION ON OVERHEAD PANEL. RECYCL ED GEAR WITH NORMAL INDICATION. REMOVED AND REPLACED LEFT MLG RETRACT ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2007022600044 20070226 00044 NM 2007 2 26 SWAA071072 1 20070222 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 464WN 32468 EEPLS COVER LOOSE AT ROW 3 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007022600045 20070226 00045 2007 2 26 SWAA071071 4 20070222 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 449WN 32469 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007022600046 20070226 00046 NM 2007 2 26 SWAA071081 1 20070222 A 5330 6545766 SKIN BOEING 737 7373A4 1384585 NM BS 505C S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505C, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007022600047 20070226 00047 NM 2007 2 26 SWAA071079 1 20070222 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 450 S1 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 450, STR 1. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2007022600048 20070226 00048 NM 2007 2 26 SWAA071078 1 20070222 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 430 S1 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 430, STR 1. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2007022600049 20070226 00049 NM 2007 2 26 SWAA071074 1 20070222 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 986 S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 986, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007022600060 20070226 00060 NM 2007 2 26 QXEA200700245 1 20070221 A 2910 CIRCUIT BREAKER BOMBDR DHC8 DHC8402 1390042 NM MAINT ERROR A QXEA D RETURN TO BLOCK W N INADEQUATE Q C FALSE WARNING TX TAXI/GRND HDL 1 NM 09 425QX 4039 SEA FLIGHT NR 2328: DURING TAXI, ELEVATOR PRESSURE CAUTION ILLUMINATED. AIRCRAFT RETURNED TO GATE. STANDBY HYD PUMP WA S RUNNING WHEN NOT SELECTED. MAINTENANCE FOUND HYD SYS CONT CB H7 PULLED AND COLLARED. REMOVED COLLAR AND RESET CB. P ERFORMED OPS TEST OF THE STANDBY POWER UNIT IAW Q400 AMM TASK 29-11-36-710-801. OPS TEST IS GOOD WITH NO DISCREPANCIES NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007022600061 20070226 00061 NM 2007 2 26 SWAA071075 1 20070222 A 5754 65C26603202A SKIN BOEING 737 7373H4 1384600 NM NR 4 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 4 L/E SLAT T/E WEDGE UPPER SURFACE DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 2007022600063 20070226 00063 EA 2007 2 26 N6WA00702001 1 20070216 A 3350 RPS1B BATTERY CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE EMERGENCY LIGHTS INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 159GJ 10238 CABIN EMERGENCY LIGHTS CEILING LEVEL LIGHT SIGN INOP. REPLACED NR 3 BATTERY PACK. 2 L 7 2 4F 4 F RT A21EA E15NE 2007022600064 20070226 00064 EA 2007 2 26 VNAA0702003 1 20070204 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS UNKNOWN A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 250PS 7929 CREW REPORTED A FLAPS FAIL MESSAGE AFTER TAKEOFF. CREW ELECTED TO RETURN TO CVG AND LANDED WITHOUT INCIDENT. MAINTENAN CE INSPECTED AND CYCLED CIRCUIT BREAKERS IAW THE SERVICE LETTER. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007022600065 20070226 00065 NM 2007 2 26 HALA0700053 1 20070222 A 5100 NONE BOEING 767 76733A 1385209 NM NONE NONE A HALA O OTHER O OTHER CL CLIMB 1 WP 13 593HA 33424 LIGHTNING STRIKE ON CLIMB-OUT. ACCOMPLISHED HAL M251-767 "INSP OF AIRCRAFT AND OPERATIONAL CHECK OF RADIO AND NAVIGATIO N SYSTEMS AFTER LIGHTNING STRIKE". CHECKED GOOD, OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007022600066 20070226 00066 EA 2007 2 26 QXEA200700224 1 20070211 A 5754 SKIN CNDAIR CL600 CL6002C10 1390015 EA LT WING SLAT CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - FOUND LEFT WING MID SLAT OUTBOARD HAS CHAFING. REPAIRED IAW SRM 51-12-00, 57-42-01. 2 L 7 2 4F RT A21EA 2007022600067 20070226 00067 EA 2007 2 26 QXEA200700226 1 20070213 A 5754 SKIN CNDAIR CL600 CL6002C10 1390015 EA WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - FOUND PANEL 522CB LEADING EDGE IS CHAFED. REPAIRED IAW SRM 57-00-01, 51-12-00. 2 L 7 2 4F RT A21EA 2007022600068 20070226 00068 EA 2007 2 26 QXEA200700227 1 20070210 A 5754 SKIN CNDAIR CL600 CL6002C10 1390015 EA WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - FOUND PANEL 584AB LEADING EDGE IS CHAFED. REPAIRED IAW SRM 51-12-00, 57-52-01. 2 L 7 2 4F RT A21EA 2007022600069 20070226 00069 EA 2007 2 26 QXEA200700228 1 20070211 A 5754 SKIN CNDAIR CL600 CL6002C10 1390015 EA WING LE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - FOUND PANEL 584GB LEADING EDGE IS CHAFED. REPAIRED IAW SRM 51-12-00, 57-52-01. 2 L 7 2 4F RT A21EA 2007022600070 20070226 00070 EA 2007 2 26 QXEA200700229 1 20070208 A 5754 SKIN CNDAIR CL600 CL6002C10 1390015 EA WING LE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - FOUND PANEL 584EB LEADING EDGE IS CHAFED. REPAIRED IAW SRM 51-12-00, 57-61-01. 2 L 7 2 4F RT A21EA 2007022600071 20070226 00071 EA 2007 2 26 QXEA200700225 1 20070211 A 5753 SKIN CNDAIR CL600 CL6002C10 1390015 EA TE FLAP[ CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - FOUND FLAP PANEL 584LB HAS MINOR CHAFING. REPAIRED IAW SRM 57-52-01, 51-21-16. 2 L 7 2 4F RT A21EA 2007022600072 20070226 00072 EA 2007 2 26 QXEA200700218 1 20070210 A 5753 SKIN CNDAIR CL600 CL6002C10 1390015 EA TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - FOUND FLAP PANEL 684JB HAS MINOR CHAFING. REPAIRED IAW SRM 57-52-01, 51-12-00. 2 L 7 2 4F RT A21EA 2007022600073 20070226 00073 EA 2007 2 26 QXEA200700219 1 20070210 A 5753 SKIN CNDAIR CL600 CL6002C10 1390015 EA TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - FOUND FLAP PANEL 684EB HAS MINOR CHAFING. REPAIRED IAW SRM 51-12-00, 57-52-01. 2 L 7 2 4F RT A21EA 2007022600074 20070226 00074 EA 2007 2 26 QXEA200700215 1 20070208 A 5753 SKIN CNDAIR CL600 CL6002C10 1390015 EA TE FLAPS CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - FOUND FLAP PANEL 584JB HAS MINOR CHAFING AFT OF CUTOUT. REPAIRED IAW SRM 51-12-00, 57-61-01. 2 L 7 2 4F RT A21EA 2007022600075 20070226 00075 EA 2007 2 26 QXEA200700216 1 20070210 A 5753 SKIN CNDAIR CL600 CL6002C10 1390015 EA TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - FOUND FLAP LEADING EDGE PANEL 684DB IS CHAFED ON INBOARD SIDE. REPAIRED IAW SRM57-52-01, 51-12-00. 2 L 7 2 4F RT A21EA 2007022600077 20070226 00077 EA 2007 2 26 QXEA200700217 1 20070212 A 5754 SKIN CNDAIR CL600 CL6002C10 1390015 EA LE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - FLAP LEADING EDGE PANEL 684LB IS CHAFED ON LEADING EDGE. REPAIRED IAW SRM 57-52-01, 51-21-11. 2 L 7 2 4F RT A21EA 2007022600078 20070226 00078 EA 2007 2 26 SWIA200717823 1 20070216 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 614SK 10051 FOUND OVERHEAD EMERGENCY LIGHT OUT SECOND FROM AFT. REPLACED LAMP. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007022600079 20070226 00079 SO 2007 2 26 SWIA200717824 1 20070219 A 2720 3081401003 ACTUATOR EMB 120 EMB120ER 3260203 SO RT RUDDER JAMMED A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 223SW 14364 13812 120291 RIGHT RUDDER JAMMED AFTER TAKEOFF. REPLACED BLUE SYSTEM RUDDER ACTUATOR IAW MM 27-22-02. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007022600080 20070226 00080 2007 2 26 SWIA200717825 4 20070218 A 3417 8220372445 ADC CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 915EV 7754 IN FLIGHT, LEFT ALTIMETER AND VERTICAL SPEED BECAME INOP ALONG WITH "MACH TRIM". REPLACED ADC NR 1 IAW ST34-220-1016 AN D MM 34-13-01. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007022600081 20070226 00081 SO 2007 2 26 SWIA200717826 1 20070217 A 3230 12038594501 CONTROL MODULE EMB 120 EMB120ER 3260203 SO MLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION DE DESCENT 1 NM 07 213SW 13471 13471 120277 AT ABOUT 2000' PUT GEAR DOWN, ALL RED IN ADDITION TO A RATTLING OUTSIDE AIRCRAFT. RETRACTED GEAR AND THEN EXTENDED AGAI N. REPLACED LANDING GEAR RELAY BOX IAW 32-31-02 AND MLG CONTROL MODULE ASSY IAW 32-31-03. OPERATIONAL CHECKS GOOD, P/N 1 - (RELAY BOX) - 120-43270-501 S/N OFF - 120101. 2 L 7 2 4T RT A31SO 2007022600082 20070226 00082 EU 2007 2 26 MALA070030 1 20070222 A 3230 CONTROL UNIT SAAB SF340 340B 7860101 EU MLG MALFUNCTIONED A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 422XJ 340B422 AFTER TAKEOFF FROM GLH, THE LANDING GEAR TRANSIT LIGHT DID NOT ILLUMINATE WHEN THE GEAR WERE RETRACTED. RAN THE QRH AND THE TRANSIT LIGHT DID WORK WHEN THE GEAR WERE EXTENDED AND GOT THREE GREEN. THE LIGHT DID NOT WORK WHEN THE GEAR WERE RETRACTED AGAIN. LAMPS TEST IS GOOD AND HYDRAULIC PRESSURE WAS NORMAL. REPLACED LANDING GEAR CONTROL UNIT; PN ON AND O FF: D494-12-001; SN ON: 672/05-98; SN OFF: 604/04-96. REF. AMM 32-31-05-02. 2 L 7 2 4T RT A52EU 2007022600083 20070226 00083 NM 2007 2 26 DLM88070145 1 20070220 A 5512 5922578516 SKIN DOUG MD88 MD88 3023688 NM HORIZONTAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DE 53415 FOUND FATIGUE CRACK IN UPPER AFT SKIN ON LT HORIZONTAL STABILIZER. ACCOMPLISHED BAC APPROVED STOP DRILL REPAIR. 2 L 7 2 4F RT A6WE 2007022600084 20070226 00084 NM 2007 2 26 DL764070146 1 20070215 A 4920 491040000 TURBINE BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL APU MAKING METAL A DALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 27 831MH 16977 29702 P1002C APU AUTO SHUT DOWN 2 TIMES WHEN APPLYING APU ELECT. APU FAULTED MSG 49-27250 LUBE MODULE FILTER SHOWS CLOGGED. PULLED CHIP DETECTORS AND FILTER FOUND METAL AND OIL SMELLS BURNED. FWD TO MCO AND PLAC 49-00-01A. REPLACED APU PER MM. 2 L 7 2 4F 4 F RT A1NM E23EA 2007022600085 20070226 00085 2007 2 26 ZZDA070215137 4 20070215 A 2565 5A33075 SLIDE BOEING 737 73776N 13844CH NM R1 DOOR UNWANTED DEPLOY A ZZDA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 15 168AT 32653 A/C CLEANERS DEPLOYED R1 SLIDE BY OPENING DOOR. REMOVED AND REPLACED R1 DOOR SLIDE IAW AMM 25-66-01 SHELF LIFE EXP 4-30 -09, HYDRO STATIC TEST DATE 07-05. 2 L 7 2 4F RT A16WE 2007022600098 20070226 00098 NM 2007 2 26 SWAA071063 1 20070221 A 5311 65C22909 FRAME BOEING 737 7373Y0 1384671 NM BS 500C S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 9R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007022600099 20070226 00099 NM 2007 2 26 SWAA071066 1 20070221 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 360 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022600100 20070226 00100 EA 2007 2 26 QXEA200700223 1 20070211 A 5751 SKIN CNDAIR CL600 CL6002C10 1390015 EA RT AILERON CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - RIGHT AILERON PANEL 699CB HAS MINOR CHAFING. REPAIRED IAW SRM 57-52-01, 51-61-01. 2 L 7 2 4F RT A21EA 2007022600101 20070226 00101 EA 2007 2 26 QXEA200700220 1 20070210 A 5753 SKIN CNDAIR CL600 CL6002C10 1390015 EA TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - FOUND FLAP PANEL684AB HAS MINOR CHAFING. REPAIRED IAW SRM 51-12-00, 57-52-01. 2 L 7 2 4F RT A21EA 2007022600102 20070226 00102 EA 2007 2 26 QXEA200700221 1 20070211 A 5753 SKIN CNDAIR CL600 CL6002C10 1390015 EA TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - FOUND FLAP PANEL 684GB HAS MINOR CHAFING. REPAIRED IAW SRM 57-52-01, 51-12-00. 2 L 7 2 4F RT A21EA 2007022600103 20070226 00103 EA 2007 2 26 QXEA200700222 1 20070210 A 5753 SKIN CNDAIR CL600 CL6002C10 1390015 EA TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - FOUND FLAP PANEL 684BB HAS MINOR CHAFING. REPAIRED IAW SRM 57-52-01, 51-12-00. 2 L 7 2 4F RT A21EA 2007022600105 20070226 00105 EA 2007 2 26 QXEA200700236 1 20070212 A 5320 SILL CNDAIR CL600 CL6002C10 1390015 EA CARGO DOORWAY GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - FOUND CARGO DOOR LOWER SILL IS GOUGED. REPAIRED IAW SRM 53-61-01, 51-12-00. 2 L 7 2 4F RT A21EA 2007022600106 20070226 00106 EA 2007 2 26 QXEA200700237 1 20070212 A 5320 SILL CNDAIR CL600 CL6002C10 1390015 EA CARGO DOORWAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - FOUND CARGO DOOR LOWER SILL HAS CORROSION. REPAIRED IAW 51-21-06, 51-25-16, AND 51-25-06. 2 L 7 2 4F RT A21EA 2007022600107 20070226 00107 EA 2007 2 26 QXEA200700239 1 20070210 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - FOUND FORWARD PASSENGER DOOR CRACKED IN FORWARD WEB RADIUS BETWEEN 1ST AND 2ND STEP. REPAIRED IAW REO670-52-11 -104. 2 L 7 2 4F RT A21EA 2007022600108 20070226 00108 EA 2007 2 26 QXEA200700233 1 20070209 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - FOUND RIGHT WALL SEAT TRACK NR 6 HAS POSSIBLE SURFACE CORROSION. REPAIRED IAW SRM 51-21-06, 53-41-49. 2 L 7 2 4F RT A21EA 2007022600109 20070226 00109 EA 2007 2 26 QXEA200700232 1 20070207 A 5310 ANGLE CNDAIR CL600 CL6002C10 1390015 EA DOOR SEAL CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - FOUND MAIN AVIONICS BAY DOOR CUTOUT SEAL LANDING HAS LIGHT CORROSION AROUND PERIMETER. REPAIRED IAW SRM 53-21- 01, 51-21-11. 2 L 7 2 4F RT A21EA 2007022600110 20070226 00110 EA 2007 2 26 QXEA200700238 1 20070213 A 5210 VENT CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - FOUND PASSENGER DOOR VENT FLAP DOOR CHAFED ON INSIDE BY THE ICE BRAKE CABLE. REPAIRED IAW SRM 51-12-00, 52-35- 06, 51-25-06. 2 L 7 2 4F RT A21EA 2007022600111 20070226 00111 EA 2007 2 26 QXEA200700234 1 20070212 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - FOUND RIGHT WALL SEAT TRACK NR 3 HAS SURFACE CORROSION. REPAIRED IAW SRM 51-26-06, 53-21-49. 2 L 7 2 4F RT A21EA 2007022600112 20070226 00112 EA 2007 2 26 QXEA200700230 1 20070208 A 5753 SKIN CNDAIR CL600 CL6002C10 1390015 EA TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 C2 OKC - FOUND FLAP PANEL 584BB CHAFED ON LEADING EDGE. REPAIRED IAW SRM 57-00-01, 51-12-00. 2 L 7 2 4F RT A21EA 2007022600113 20070226 00113 SO 2007 2 26 RAIA00702034 1 20070222 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BROKEN A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 819HK 145062 PRE FLT NR 5471 - STL - EMERGENCY LIGHT IS OUT AT ROW 12 FLOOR PROXIMITY LIGHTS. MAINTENANCE REPAIRED BROKEN WIRE TO FL OOR STRIP. 2 L 7 2 4T RT T00011AT 2007022600114 20070226 00114 SO 2007 2 26 RAIA00702033 1 20070222 A 7830 UNKNOWN EMB 145 EMB145LR 3260212 SO THUST REVERSER UNKNOWN A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 850HK 145003 FLT NR 8018 - STL - NR 2 THRUST REVERSER DISAGREE. MAINTENANCE DEFERRED NR 2 THRUST REVERSER PER MEL. 2 L 7 2 4T RT T00011AT 2007022600115 20070226 00115 SO 2007 2 26 RAIA00702031 1 20070222 A 3260 8005701 PROXIMITY SENSOR EMB 145 EMB145 3260210 SO MLG UNKNOWN A RAIA O OTHER J WARNING INDICATION DE DESCENT 1 CE 03 820HK 145064 FLT NR 5526 - STL - ON APPROACH BROUGHT GEAR DOWN, LEFT MAIN FAILED TO SHOW DOWN AND LOCK. CYCLED GEAR ON SECOND ATTEMP T, GEAR SHOWED DOWN AND LOCK. MAINTENANCE REMOVED AND REPLACED THE NR 1 MLG DOWNLOCK PROX SWITCHES. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007022600116 20070226 00116 SO 2007 2 26 RAIA00702029 1 20070221 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 811HK 145256 PRE FLT NR 5502 - STL - EMERGENCY LIGHT FLOOR STRIP 17D IS INOP. MAINTENANCE ATTACHED LOOSE WIRE CONNECTION ON THE BOTT OM OF EMERGENCY FLOOR STRIP LIGHT. 2 L 7 2 4T RT T00011AT 2007022600117 20070226 00117 SO 2007 2 26 RAIA00702028 1 20070221 A 7830 UNKNOWN EMB 145 EMB145LR 3260212 SO NR 2 ENGINE UNKNOWN A RAIA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 811HK 145256 FLT NR 5588 - SAT - ENGINE 2 T/R DISAGREE. MAINTENANCE DEFERRED THE THRUST REVERSER SYSTEM PER THE MEL. 2 L 7 2 4T RT T00011AT 2007022600118 20070226 00118 SO 2007 2 26 RAIA00702025 1 20070221 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 802HK 145066 PRE FLT NR 3554 - RIC - EMERGENCY LIGHT AT GALLEY WALL EXIT IS INOP. MAINTENANCE RECONNECTED WIRES TO EMERGENCY LIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007022600119 20070226 00119 SO 2007 2 26 RAIA00702027 1 20070221 A 3297 JD3899926KA98SN CONNECTOR EMB 145 EMB145LR 3260212 SO PRESSURE SWITCH LOOSE A RAIA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 818HK 145059 FLT NR 5587-STL - NO T/O CONFIG WARNING ONCE TLA ADVANCED. MAINTENANCE REPLACED PARKING BRAKE PRESSURE SWITCH CONNECTOR . OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007022600120 20070226 00120 SO 2007 2 26 RAIA00702024 1 20070220 A 3350 LIGHT EMB 145 EMB145 3260210 SO COCKPIT INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 821HK 145068 POST FLT NR 5490 - STL - EMERGENCY LIGHT COCKPIT STEP EXIT INOP. MAINTENANCE RESET EMERGENCY LIGHT SYSTEM. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2007022600121 20070226 00121 2007 2 26 RAIA00702023 2 20070220 A 7297 CONNECTOR EMB 145 EMB145LR 3260212 SO NR 1 ENGINE LOOSE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 810HK 145231 FLT NR 5587 - STL - NO FUEL FLOW ON NR 1 ENGINE DURING START. MAINTENANCE RESEATED CONNECTOR TO FADEC 1A & 1B. OPS CHE CK GOOD. 2 L 7 2 4T RT T00011AT 2007022600122 20070226 00122 SO 2007 2 26 RAIA000702030 1 20070221 A 3010 UNKNOWN EMB 145 EMB145LR 3260212 SO UNKNOWN A RAIA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 CE 03 823HK 145475 FLT NR 7968 - MKE - WING & STAB VALVE OPEN INSCRIPTIONS DID NOT ILLUMINATE DURING ICE TEST WITH SWITCH IN THE NR 2 POSIT ION. MAINTENANCE DEFERRED WING A-ICE SYS PER MEL. 2 L 7 2 4T RT T00011AT 2007022600123 20070226 00123 EU 2007 2 26 07FDEA00509 1 20070216 A 5730 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 FOUND CORROSION ON BOTTOM SKIN, MLG REINFORCING PLATE RT WING. NDT DETECTED A CRACK IN HOLE NR 552. REPAIR WAS PERFORM ED IAW RAS/BAE/1003853/2006 ISS.: A AND EA 6-5720-103395. 2 L 7 2 4F RT A35EU 2007022600124 20070226 00124 CE 2007 2 26 DXTA200701932 1 20070213 A 2822 UNKNOWN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE BOOST PUMP UNKNOWN E DXTA O OTHER O OTHER DE DESCENT 1 GL 07 303QS 5600343 LT FUEL BOOST PUMP CB POPED DURING LT FUEL X FEED OPERATION. REMOVED UNSERVICEABLE FUEL BOOST PUMP P/N 1C7-12 S/N BB18 AND INSTALLED OVERHAULED PUMP P/N 1C7-12-OH, S/N 10AD110 I/A/W 560 MM 28-21-01. OPS CHECKED LEAK CHECKED. NO DEFECTS WER E NOTED. 2 L 7 2 4F 4 F RT A22CE E25EA 2007022600125 20070226 00125 CE 2007 2 26 DXTA200701933 1 20070213 A 2697 WIRE CESSNA 650 650 2076802 CE GARRTT TFE731 TFE7314R 01518 WP FIRE DETECTION BROKEN E DXTA K NONE J WARNING INDICATION IN INSP/MAINT 1 GL 07 791QS 6507091 RT ENGINE FIRE DETECT ANUNCIATOR ILLUMINATED AFTER COCKPIT PREP WAS COMPLETED. T/S TO BROKEN RT FIRE LOOP ON ENG. REMOV ED & REPLACED FIRE LOOP. BLEED T/R'S, SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME. ALL WORK DONE IAW CE 650 M/M 26-10- 01 2 L 7 2 4F 4 F A9NM E6WE 2007022600127 20070226 00127 SO 2007 2 26 RAIA00702018 1 20070218 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 845HK 14500842 PRE FLT NR 5573 - STL - EMERGENCY LIGHT STRIP FWD GALLEY AREA CAME LOOSE. MAINTENANCE RESECURED EMERGENCY LIGHT STRIP. 2 L 7 2 4T RT T00011AT 2007022600128 20070226 00128 SO 2007 2 26 RAIA00702019 1 20070218 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 830HK 145313 PRE FLT NR 5539 - STL - EMERGENCY FLOOR ESCAPE PATH LIGHTING INOPERATIVE IN FORWARD HALF OF CABIN. MAINTENANCE RECONNEC TED LOOSE WIRING ON FLOOR STRIP BY ROW 1A. 2 L 7 2 4T RT T00011AT 2007022600129 20070226 00129 SO 2007 2 26 RAIA00702017 1 20070218 A 3297 CONNECTOR EMB 145 EMB145 3260210 SO NLG STEERING LOOSE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 806HK 145112 FLT NR 3574 - STL - NOSE WHEEL STEERING C/B POPPED. MAINTENANCE REPAIRED WIRES TO CONNECTOR AT P4672. 2 L 7 2 4F RT T00011AT 2007022600130 20070226 00130 SO 2007 2 26 RAIA00702020 1 20070215 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 810HK 145231 PRE FLT NR 7877 - STL - EMERGENCY LIGHT WIRE LOOSE ON HANDRAIL. MAINTENANCE RESECURED PAX DOOR EMERGENCY LIGHT. 2 L 7 2 4T RT T00011AT 2007022600131 20070226 00131 SO 2007 2 26 RAIA00702021 1 20070215 A 7830 UNKNOWN EMB 145 EMB145LR 3260212 SO THRUST REVERSER UNKNOWN A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 850HK 145003 FLT NR 8020 - STL - E1 T/R DISAGREE. MAINTENANCE DEFERRED NR 1 THRUST REVERSER. 2 L 7 2 4T RT T00011AT 2007022600132 20070226 00132 SO 2007 2 26 RAIA00702016 1 20070214 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 821HK 145068 PRE FLT NR 5512 - STL - EMERGENCY EXIT SIGN AT CABIN ENTRY WAY ON FWD BULKHEAD INOP. MAINTENANCE RESEATED CONNECTOR TO THE EMERGENCY EXIT SIGN AT CABIN ENTRY WAY. 2 L 7 2 4F RT T00011AT 2007022600133 20070226 00133 SO 2007 2 26 RAIA00702022 1 20070214 A 8012 32153582 START VALVE EMB 145 EMB145LR 3260212 SO NR 1 ENGINE UNKNOWN A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 812HK 15388 145373 FLT NR 5501 - STL - EXPERIENCED DIFFICULTY STARTING ENGINE NR 1. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE START CON TROL VALVE. 2 L 7 2 4T RT T00011AT 2007022600134 20070226 00134 EU 2007 2 26 F3LA200700036 1 20070216 A 5610 WINDSHIELD AIRBUS A319 A319112 3930323 EU COCKPIT CRACKED A F3LA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 03 909FR 16916 1761 UPON ARRIVAL AT GATE, CAPTAIN'S WINDSHIELD CRACKED. REPLACED NR 1 WINDSHIELD IAW AMM 56-11-11, PB 401, P/N STA320-2-7-1 A, S/N 5910 (MFG SULLY). ON PUSHBACK, FIRST OFFICER'S WINDSHIELD CRACKED. REPLACED NR 2 WINDSHIELD IAW AMM 56-11-11, P B 401, P/N STA320-2-7-1A, S/N 56109 (PPG). 2 L 7 2 4F RT A28NM 2007022600135 20070226 00135 NM 2007 2 26 F3LA200700038 1 20070217 A 5610 NP1653115 WINDSHIELD AIRBUS A319 A319111 3930336 NM COCKPIT CRACKED A F3LA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 923FR 11777 2019 AIR TURN BACK, CAPTAIN'S WINDSHIELD CRACKED. REPLACED NR 1 WINDSHIELD IAW AMM 56-11-11. 2 L 7 2 4F RT A28NM 2007022600136 20070226 00136 NM 2007 2 26 F3LA200700037 1 20070216 A 5610 NP1653116 WINDSHIELD AIRBUS A319 A319111 3930336 NM COCKPIT CRACKED A F3LA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 03 923FR 11777 2019 FIRST OFFICERS WINDSHIELD CRACKED ALL THE WAY ACROSS. REPLACED NR 2 WINDSHIELD IAW MM 56-11-11 PB401. 2 L 7 2 4F RT A28NM 2007022600137 20070226 00137 NM 2007 2 26 07FDEA00529 1 20070220 A 5710 ANGLE DOUG MD11 MD11 3023602 NM CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 FOUND CENTER UNDERWING TANK LT SIDE APPROX STA 1305 TO 1321 SUSPECT CRACK ON CORNER ANGLE SPLICE. COMPLIED WITH FEDEX EA 1-5310-106592. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022600138 20070226 00138 NM 2007 2 26 07FDEA00531 1 20070220 A 5710 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT WING L/E TELESCOPING DUCT PASSAGE CUTOUT FOUND TOP I/B CORNER EDGE CRACKED. REPAIRED AS PER SRM 57-10-00 FIG. 42 VOL.I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022600139 20070226 00139 NM 2007 2 26 07FDEA00532 1 20070221 A 5711 SPAR CAP DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RT WING, REAR SPAR CAP FOUND TOP SURFACE AT XORS=1048 CORRODED. COMPLIED WITH FEDEX EA 1-5720-106595. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022600140 20070226 00140 NM 2007 2 26 07FDEA00533 1 20070221 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 MAIN DECK CARGO, FLOOR SEAT TRACK FOUND CORROSION AT STA 1495 - 1510, X=-75.25. SEAT TRACK REPAIR CARRIED OUT AS PER SR M 53-70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022600141 20070226 00141 NM 2007 2 26 07FDEA00534 1 20070221 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 MAIN DECK CARGO, FLOOR SEAT TRACK FOUND CORROSION AT STA 1521, X=8.5. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022600142 20070226 00142 NM 2007 2 26 07FDEA00535 1 20070221 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 MAIN DECK CARGO, FLOOR SEAT TRACK FOUND CORROSION AT STA 1505, X= 75.25. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70 -00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022600143 20070226 00143 NM 2007 2 26 07FDEA00536 1 20070221 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 MAIN DECK CARGO, FLOOR SEAT TRACK FOUND CORROSION AT STA 1328, X=75.25. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70- 00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022600144 20070226 00144 NE 2007 2 26 07FDEA00537 2 20070221 A 7261 OIL SYSTEM BOEING 727 727227 1384078 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE UNKNOWN A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 493FE 52347 1326 21531 687394 NR 1 ENG OIL QUANTITY BEGAN TO DECREASE SHORTLY AFTER T/O WITH ASSOCIATED NOTICEABLE DECREASE IN OIL TEMP, (OUT OF LIMIT S) PRECAUTIONARY ENGINE SHUTDOWN. OIL QTY DECREASED TO BELOW 1 GAL. AFTER SHUTDOWN OIL QTY ROSE AGAIN TO 4 GALS. DUE TO THE FACT THAT THE AIRCREW SHUT DOWN THE ENG INFLIGHT AND WINDMILLED. THE FLIGHT CREW WAS UNABLE TO ID HOW MUCH OIL P RESSURE THEY HAD DURING WIND-MILLING PER AMM MIN OIL PRESSURE 10 PSI. 2 L 7 3 4F 4 F A3WE E2EA 2007022600145 20070226 00145 WP 2007 2 26 ASMF200702005 1 20070213 A 3260 833605 PROXIMITY SWITCH DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE MLG FAILED W ASMF O OTHER J WARNING INDICATION CL CLIMB 1 SW 23 754RA 53804 9026 49641 CAPTAIN REPORTED THAT 3 RED LANDING GEARS LIGHTS TURNED ON DURING CLIMB AND CRUISE. PROXIMITY SWITCH COMPUTER WAS TESTED , CIRCUIT BREAKER WAS RESEATED, LANDING UP SENSORS AND CONNECTORS WERE CHECKED, ALL CORRECT. DURING TRANSIT CHECK AT GDL , THE PROXIMITY SWITCH COMPUTER WAS REPLACED IAW MM 32-60-04, TESTED CORRECT. DURING OVERNIGHT CHECK, THE FAILURE CONTIN UED, THEREFORE THE RT THROTTLE SWITCH UNIT WAS REPLACED IAW MM 76-10-03 AND LANDING GEAR TEST WAS PERFORMED IAW MM 32-60 -00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007022600146 20070226 00146 NM 2007 2 26 NOCA01607 1 20070118 A 2611 32V92 PRESSURE SWITCH BOEING 767 767306 1385148 NM SMOKE DETECTOR UNKNOWN A NOCA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 15 768NA 29898 STATUS MSG FWD DET FAN DISPLAYED ON EICAS CORRECTIVE ACTION T/S FWD DET FAN MSG PER FIM 26-16-00. REPLACED FWD CARGO SM OKE DETECTOR PRESS SWITCH PER MM 26-16-03. 2 L 7 2 4F RT A1NM 2007022600147 20070226 00147 NM 2007 2 26 NOCA01807 1 20070120 A 3350 BPS73 BATTERY PACK BOEING 767 767306 1385148 NM EMERGENCY LIGHTS INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 768NA 29898 FOUND RIGHT SIDE EXTERIOR LIGHTS INOP. REPLACED EMERGENCY BATTERY POWER SUPPLY, OPS NML AS PER MM 33-51-07. 2 L 7 2 4F RT A1NM 2007022600148 20070226 00148 NM 2007 2 26 NOCA01707 1 20070102 A 2613 285N002836 CIRCUIT CARD BOEING 757 75728A 1384976 NM OVERHEAT LOOP MALFUNCTIONED A NOCA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 15 750NA 26277 FOUND RIGHT ENGINE OVERHEAT LOOP 1 STATUS MESSAGE. REMOVED AND REPLACED AFOLTS NR 2 CARD AS PER MM 26-10-01, OPS CHECK NORMAL. 2 L 7 2 4F RT A2NM 2007022300116 20070223 00116 NM 2007 2 23 AWXA200700223 1 20070125 A 5753 SKIN BOEING 737 7373S3 1384711 NM FORE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW BN1066 23713 MCN - FOUND RIGHT WING INBOARD FOREFLAP UPPER SKIN DELAMINATED, WBL 181. REPAIRED RIGHT WING INBOARD FOREFLAP UPPER SKI N, WBL 181 IAW B737-300 SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007022300136 20070223 00136 NM 2007 2 23 AALA20070336 1 20070215 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 782AN 30003 DFW - FOUND EMERGENCY LIGHT AT SEAT 3G MISSING LAMPS. RELAMPED EMERGENCY LIGHT AT SEAT 3G. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT T00001SE 2007022300159 20070223 00159 NM 2007 2 23 AALA20070298 1 20070206 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 692AA 26972 DFW - FOUND EMERGENCY LIGHT AT RIGHT NUMBER ONE SLIDE INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT NUMBER ONE SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007022300169 20070223 00169 NM 2007 2 23 F3LA200700027 1 20070218 A 5414 D5453011820000 PIN AIRBUS A319 A319111 3930336 NM RYLON PANEL CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 929FR 4725 2240 DURING C-2 CHECK, INSPECTION REPORTED RT PYLON PANEL 483BL ONE ALIGNMENT PIN CORRODED. REPLACED PIN IAW AMM 51-42-11. 2 L 7 2 4F RT A28NM 2007022300201 20070223 00201 2007 2 23 2007UALA00485 4 20070215 A 2565 O-RING AIRCRUISERS BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SLIDE BOTTLE DETERIORATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 225UA 0042 30554 LOW BOTTLE PRESSURE. REPLACED SLIDE. A/C RETURNED TO SERVICE. SLIDE PROBLEM ROOT CAUSE: FOUND FILLER VALVE LEAKING C AUSING LOW BOTTLE PRESSURE. SUSPECT O-RING DETERIORATION LEAD TO LEAKAGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007022300204 20070223 00204 NM 2007 2 23 753001 1 20070219 A 7500 1990M90G01 CLAMP BOEING 747 747228F 1384895 NM GE CF6 CF650E2 30018 NE BLEED AIR DUCT BROKEN A Q2SA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 03 753SA 21787 517737 DURING THE CLIMB-OUT OF PANC, NR 4 ENGINE FIRE WARNING AND HIGH NACELLE TEMPERATURE. ENGINE SHUTDOWN, DUMPED 61,000 LBS FUEL. NO FIRE EXTINGUISHER ACTIVATED. RETURNED TO PANC. FOUND BROKEN CLAMP AT 14TH STAGE BLEED AIR DUCT AND HIGH STA GE VALVE. 2 L 7 4 4F 4 F A20WE E23EA 2007022300209 20070223 00209 NM 2007 2 23 2007UALA00378 1 20070209 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE SCRATCHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 327UA 24147 UPPER FUSELAGE OUTER SKIN SCRATCHED AT STA 288 S23L. MAJOR REPAIR. REMOVED DAMAGE, FABRICATED AND INSTALLED DOULBER, F ILLER AND STRUCTURAL FILLER PER SRM 53-00-01 REPAIR 31 DETAIL XIX. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022300214 20070223 00214 NM 2007 2 23 2007UALA00383 1 20070209 A 5347 SEAT TRACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 662UA 27159 MAIN CABIN SEAT TRACK AT RBL 88.50, APPROX STA 753 TO 819 IS CRACKED OUT, 2 PLACES AT UPPER SCALLOPS WHERE GALLEY MOUNTS . REPLACED SEAT TRACK SECTION RBL 88.5, STA 753 TO 819, A/C READY FOR SERVICE. SUSPECT DAMAGE IS DUE TO SERVICE CARTS & IMPACT BY PAX CARRY-ON ITEMS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022300215 20070223 00215 NM 2007 2 23 2007UALA00384 1 20070209 A 2120 UNKNOWN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 843UA 1573 ELECTRICAL ODOR IN FLIGHT DECK WITH NO ECAM MESSAGE AT FL350. TURNED CABIN FANS OFF. ODOR WENT AWAY. [SUP 05-08-07] DETERMINED THAT LEFT RECIRC FAN WAS SOURCE OF ELECTRICAL ODOR AND WAS REPLACED. FURTHER DIAGNOSTICS FOUND THAT THE STATO R WAS DAMAGED DUE TO WORN BEARINGS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022300217 20070223 00217 EU 2007 2 23 2007UALA00386 1 20070211 A 3260 WARNING SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT ACTIVATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 411UA 464 RTFL DUE TO A MAIN LANDING GEAR INDICATION. [SUP 05-16-07] ALL DOOR INDICATORS WERE AMBER. ALL INDICATORS GREEN AFTER SECOND ATTEMPT. CREW STATED THAT IT SEEMED THAT ALL GEAR RETRACTED BUT DOORS REMAINED OPEN SUPPLEMENTAL DATA UPDATE FAUL T TRACED TO OUT OF ADJUSTMENT NOSE LANDING GEAR PROXIMITY SENSOR. MAIN LANDING GEAR PROXIMITY SENSORS WERE CHECKED AS A PRECAUTION WITH NO FAULTS FOUND. ADJUSTED NOSE GEAR PROXIMITY SENSOR TO PROPER CLEARANCES. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022300220 20070223 00220 NM 2007 2 23 HALA0700047 1 20070213 A 3260 893602 PROXIMITY SENSOR BOEING 717 717200 1383700 NM MLG MALFUNCTIONED A HALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 13 475HA 55121 FOUND LEFT LANDING GEAR RED IN TRANSIT LIGHT ON. QRH PROCEDURE FOLLOWED. RED LIGHT STILL ON INFLIGHT. NO VIBRATION OR NO NOISE. BITE CHECKED PROX BOX, NO FAULTS NOTED. CHECKED UPLOCK SENSOR PER 32-61-00. NO FAULTS NOTED, GEAR SWING AC COMPLISHED. READINGS ON MCDU FOR SENSORS WITHIN LIMITS. REPLACED UPLOCK PROXIMITY SENSOR FOR LEFT GEAR PER 32-61-00 AD J PENDING PER AMM 32-61-00. OPS CHECK GOOD. GEAR SWING CHECK GOOD. OK FOR SERVICE. 2 L 7 2 4F TR A6WE 2007022300221 20070223 00221 2007 2 23 DHL2007364007 4 20070215 A 2565 MECHANISM AIRBUS 300 A300B4203 3930306 EU LT DOOR SLIDE CONTAMINATED A DHLA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 364DH 141 LEFT MAIN DOOR SLIDE WARNING LIGHT FLASHING IN FLIGHT WITH SLIDE ARMED AND NO DOORS LIGHT ILLUMINATED. REMOVED ICE DEBR IS FROM LT DOOR SLIDE ARMING MECHANISIM. OPS CK GOOD IAW AMM 52-10-30. 2 L 7 2 4F RT A35EU 2007022300223 20070223 00223 NM 2007 2 23 2007UALA00390 1 20070211 A 3810 WATER SYSTEM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE ENTIRE AIRCRAFT LOW PRESSURE A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 213UA 30219 FLT DIVERTED DUE TO NO WATER PRESSURE IN ENTIRE ACFT. PERFORMED OPS CHECK OF WATER SYS ALSO OPS CHECK PRESELECT WATER VALVE ABOVE CEILING PANEL IN FIRST CLASS, ALSO CHK DRAIN VALVE, PRESURE CHECK WITH AND WITHOUT APU BLEED, ALSO REFILLED WATER TO FULL. UNABLE TO DUPLICATE PROBLEM. SYS CHECKS OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007022300229 20070223 00229 EU 2007 2 23 07FDEA00442 1 20070209 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 FWD CARGO COMPARTMENT, MDC FLOORBEAM FRAME 21 CRACKED RT SIDE. LENGTH OF CRACK .380 INCH. REPAIRED PER ENG DISPO AND A 310-200 SRM SUPP 53-10-15 FIG 201 SHEET 2. MAJOR REPAIR IAW FEDEX GMM 6-2-100. SEE JPF N00344. 2 L 7 2 4F RT A35EU 2007022300230 20070223 00230 EU 2007 2 23 07FDEA00496 1 20070215 A 5753 SKIN AIRBUS 310 A310203 3930313 EU ZONE 500 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 LT WING OUTBOARD FLAP LWR SURFACE HAS EVIDENCE OF DELAMINATION. REPAIRED DELAMINATED AREA IAW A310-200 SRM 57-53-12 FI G 207. 2 L 7 2 4F RT A35EU 2007022300241 20070223 00241 NM 2007 2 23 07FDEA00504 1 20070216 A 5713 STRINGER DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 DURING HFEC INSPECTION, CRACK FOUND AT STRINGER 44 (XORS 523) IN LEFT TANK. COMPLIED WITH FEDEX EA 1-5720-106593. REPA IR CLASSIFIED AS MINOR ALTERATION AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022300242 20070223 00242 NM 2007 2 23 07FDEA00505 1 20070216 A 5713 STRINGER DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 DURING HFEC INSPECTION, CRACK FOUND AT STRINGER 40 (XORS 747) IN LEFT TANK. REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022300245 20070223 00245 EU 2007 2 23 2007UALA00399 1 20070211 A 3350 CHARGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 411UA 464 EMERGENCY LIGHTS CHARGER UNIT AT DOOR 1L HAS FAILED. REPLACED CHARGER. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022300256 20070223 00256 EU 2007 2 23 2007UALA00451 1 20070214 A 5322 SHEAR TIE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 430UA 568 FWD CARGO PIT CORROSION AT FRAME 27 SHEAR TIES BETWEEN STR 43 & 44 LT, 42 & 43 RT, 41 & 42 RT AND FRAME 24 SHEAR TIE BET WEEN STR 42 & 43 RT. MAJOR REPAIR ACCOMPLISHED: REPLACED SHEAR TIES. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022300265 20070223 00265 NM 2007 2 23 2007UALA00460 1 20070214 A 3350 20131 BATTERY PACK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 374UA 24639 EEL LIGHTS INOP AT STA 540 TO 663 LT SIDE AND OVER ESCAPE HATCH. REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022300270 20070223 00270 2007 2 23 2007UALA00465 4 20070214 A 2565 HOSE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EVAC SLIDE KINKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 436UA 638 RIGHT OVERWING SLIDE INFLATION HOSE KINKED NEAR REGULATOR END. [SUP 05-16-07] REPLACED OVERWING SLIDE INFLATION BOTTLE . INSTALLATION ERROR FROM PREVIOUS REPLACEMENT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022300278 20070223 00278 NM 2007 2 23 USAA070110 1 20070220 A 5310 DOOR FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 24781 RADIATING FROM UPPER I/B STOP BOLT HOLE, STA 492.4, S-24R, FWD CARGO DOOR CRACKED. INSTALLED DOUBLER PER EA 98497, DEFE CT SIZE: .5 INCHES. 2 L 7 2 4F RT A16WE 2007022300279 20070223 00279 NM 2007 2 23 USAA070109 1 20070220 A 5310 DOOR FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 24781 STA 440 S-21R CARGO DOOR FUSELAGE FRAME, UPPER I/B STOP BOLT HOLE CRACKED. REMOVED DAMAGE & INSTALLED PARTS PER EA 9849 6, DEFECT SIZE: .5 INCHES. 2 L 7 2 4F RT A16WE 2007022300293 20070223 00293 NM 2007 2 23 SB07013 1 20070215 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 530AU 24412 CLT MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 5, 6, 7 AND 22 INOPERATIVE. MAINTENANCE RELAMPED ROW S 5, 7 AND 22. AT ROW 6 REPAIRED WIRING. OPERATIONAL CHECK OF LIGHTS GOOD. 2 L 7 2 4F RT A16WE 2007022300303 20070223 00303 NM 2007 2 23 SB07017 1 20070222 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 451UW 24934 DCA - MAINTENANCE REPORTED THE EMERGENCY EXIT SIGN AT THE FORWARD ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE BATTERY PACK PER MM 33-51-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007022300325 20070223 00325 NM 2007 2 23 WRNA200700001 1 20070210 A 5347 8121688 SEAT TRACK BOEING 747 747212B 1384886 NM COCKPIT CRACKED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, FIRST OFFICERS AFT INBOARD SEAT TRACK WAS FOUND CRACKED, VERIFIED WITH HFEC. REPLACED SEAT TRACK IAW B7 47 MM 20-51-1 2 L 7 4 4F A20WE 2007022600007 20070226 00007 SO 2007 2 26 GLBA20060900 1 20070214 A 2121 FAN EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN SMOKE A GLBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 96ZK 120096 UNSHEDULED LANDING, FLIGHT 5045, AFTER TAKEOFF AT APPROXIMATELY 8000FT. PILOTS REPORTED SMOKE THAT APPEARED TO BE COMIN G FROM THE RT SIDE PANEL. MAINTENANCE PERFORMED HIGH POWER ENGINE RUNS AND PERFORMED OPERATIONAL CHECKS OF THE ENVIRONME TAL SYSTEM. MAINTENANCE FOUND THE LT RECIRCULATION FAN INOPERATIVE AND PLACED THE AFFECTED ITEM ON MEL 21-25-1 CATEGORY C. MAINTENANCE REMOVED AND REPLACED THE RECIRCUALTION FAN PER EMB-120 MM 21-25-02. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 2007022600023 20070226 00023 NM 2007 2 26 SWAA071054 1 20070221 A 5322 6946569 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 908 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 908, STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007022600028 20070226 00028 NM 2007 2 26 SWAA071059 1 20070221 A 5523 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM LT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED OTS CHECK, FOUND LEFT ELEVATOR TAB BEARING WORN AT CONTROL ROD ATTACH POINT. REMOVED AND REPLACED BEAR ING PER MM. 2 L 7 2 4F RT A16WE 2007022600035 20070226 00035 EA 2007 2 26 A6WA200740051 1 20070201 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 419AW 11445 7633 GEAR DISAGREE AFTER TAKEOFF. NOSE GEAR DID NOT COME OUT OF DOWN AND LOCKED. AIRSPEED MAINTAINED LESS THAN 190 KNOTS CO MPLIED WITH QRH ALL GEAR WENT DOWN AND LOCKED AS NORMAL. REMOVED AND REPLACED NLG PRIORITY VALVE P/N 4622 IAW CRJ AMM 3 2-33-51. (M) 2 L 7 2 4F RT A21EA 2007022600036 20070226 00036 EU 2007 2 26 07FDEA00545 1 20070223 A 2910 COUPLING AIRBUS 310 A310222 3930315 EU HYD SYSTEM LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 456FE 318 YELLOW SYSTEM HYD FLUID LOST DURING CRUISE. FOUND HYDRAULIC FLUID LEAKING FROM PRIORITY VALVE UNION IN STABILIZER COMPT AND PACKING WAS DAMAGED. REPLACED PACKING AND RESECURED UNION PER SMP REF IPC 27-44-04-10 ITEM 40. PERFORMED ENGINE R UN AND C/OUT, LEAK CHK FOUND SATISFACTORY. 2 L 7 2 4F RT A35EU 2007022600059 20070226 00059 NM 2007 2 26 QXEA200700243 1 20070222 A 3411 PITOT SYSTEM BOMBDR DHC8 DHC8402 1390042 NM NR 1 & 2 MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 418QX 4143 PDX FLIGHT NR 2362: PITOT NR 1 AND PITOT NR 2 CB OUT. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE RESET PITOT 1 AND 2 CB I AW GMM 5-18-0. GROUND RAN NR 2 ENGINE. SELECTED PITOT HEAT ON WITH NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RET URNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007022600150 20070226 00150 NM 2007 2 26 HALA070048 1 20070216 A 2520 7002299001 MONITOR BOEING 767 76733A 1385209 NM CABIN OVERHEATED A HALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 13 587HA 33421 FORWARD FLIGHT ATTENDANT REPORTED SMOKE IN CABIN FROM FORWARD BULKHEAD MONITOR. CONFIRMED THAT THE SMOKE WAS FROM THE F ORWARD VIDEO MONITOR. DEFERRED VIDEO SYSTEM, LATER REPLACED MONITOR AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A1NM 2007022600151 20070226 00151 WP 2007 2 26 ASMF200702006 1 20070215 A 2420 UNKNOWN DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE GENERATOR UNKNOWN W ASMF F K ACTIVATE FIRE EXT. NONE M J OVER TEMP WARNING INDICATION IN INSP/MAINT 1 SW 23 803ML 1159 49726 CAPTAIN REPORTED THAT A GEN LOW AND TAIL COMP TEMP HIGH LIGHTS TURNED ON. DURING MAINTENANCE CHECK, THE TAIL CONE COMPAR TMENT WAS DETECTED WITH HIGH TEMPERATURE AND THE FIRE EXTINGUISHER CONTAINER ACTIVATED. AIRCRAFT WAS SENT TO THE HANGAR AND RT FIRE EXTINGUISHER CONTAINER WAS REPLACED IAW MM 26-20-01 AND AIR CONDITIONING, PNEUMATIC AND ANTI-ICE SYSTEMS WER E CHECKED BY LEAKS IAW MM 21-10-00, 30-10-00 AND 35-10-00, DETECTING A LEAK IN THE APU CONTROL VALVE DUE TO CLAMPS WERE DAMAGED. CLAMPS WERE REPLACED AND SYSTEM TESTED BY LEAKS IAW MM 21-10-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007022600152 20070226 00152 EU 2007 2 26 YENA2007010 1 20070210 A 5100 NONE AIRBUS 320 A320232 3930326 EU NONE NONE A YENA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 648JB 2970 A/C RETURNED TO GATE DUE TO SMOKE IN THE CABIN. MAINTENANCE FOUND FIRE AND SMOKE DAMAGE TO OVERHEAD BIN AT ROW 18/19 LE FT CAUSED BY CAMERA EQUIPMENT BATTERY SHORTED IN PAX CARRY ON BAG. DAMAGED AREA WAS INSPECTED AND FOUND NO DAMGE TO STR UCTURE. AREA WAS CLEANED AND DAMAGED OVERHEAD BIN AT ROW 18/19 REPLACED. SEVERAL USED OXYGEN AND FIRE BOTTLES WERE REP LACED AND ALL ASSOCIATED SYSTEMS WERE CHECKED AND FOUND SATISFACTORY. AIRCRAFT RELEASED FOR OPERATION. 2 L 7 2 4F RT A28NM 2007022600153 20070226 00153 2007 2 26 YENA2007009 4 20070208 A 2330 17722201 VIDEO MONITOR AIRBUS 320 A320232 3930326 EU PAX SEAT 17C UNKNOWN A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 552JB 1861 TV MONITOR FOR PAX SEAT 17C APPEARS TO HAVE BURN IN SCREEN. PASSENGER AND FLIGHT ATTENDANT COMPLAINED OF ELECTRIC SMELL . TURNED OFF TV SYSTEM MASTER AND SMELL WENT AWAY. PERFORMED TSM 24-00-00-810-823 AND 23-39-00-810-801 AND IDENTIFIED LIVE TV MONITOR 17C CAUSING PROBLEM. ITEM WAS DEFERRED PER MEL 25-22-03. ON 02/09/07 THE VDU WAS REPLACED AND SYSTEM I S ACTIVATED. REPLACED VDU P/N 177222-01 IS AN EXPENDABLE PART AND NOT TRACKED. 2 L 7 2 4F RT A28NM 2007022600155 20070226 00155 NM 2007 2 26 MZZA0700003 1 20070219 A 3350 D71701100 BATTERY BOEING 737 737824 13844BZ NM ROW 19 ABC INOPERATIVE A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 25201 28958 THE EMERGENCY LIGHT BATTERY PACK AT ROW 19ABC FAILED CAPACITY CHECK. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 3 3-51-06. 2 L 7 2 4F RT A16WE 2007022600156 20070226 00156 WP 2007 2 26 07FDEA00524 1 20070220 A 5710 STRUCTURE DOUG DC10 DC1010 3022110 WP WING CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 397FE 46631 MD10-10 ACF MODIFICATION DURING BOLT REMOVAL, FOR EO.8-5710-7-3314 PART 8 STEP 7 FOUND SEVERE CORROSION ON BOLT AND LIGH T CORROSION IN HOLE. REMOVED CORROSION FOR SRM 51 VOL II CHECKED DIA HOLE IS IN LIMIT, PROTECT AREA INSTALL SERVICEABLE BOLT FOR EO 8-5710-7-3314. 2 L 7 3 4F A22WE 2007022600157 20070226 00157 WP 2007 2 26 07FDEA00526 1 20070220 A 5710 STRUCTURE DOUG DC10 DC1010 3022110 WP WING CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 397FE 46631 MD10-10 ACF MODIFICATION DURING BOLT REMOVAL E. FOR EO.8-5710-7-3314 PART 8 STEP 7 FOUND SEVERE CORROSION ON BOLT AND LI GHT CORROSION IN HOLE. REMOVED CORROSION FOR SRM 51 VOL.II CHECKED DIA HOLE IS IN LIMIT, PROTECT AREA. INSTALL SERVICE ABLE BOLT FOR EO 8-5710-7-3314. 2 L 7 3 4F A22WE 2007022600158 20070226 00158 EA 2007 2 26 VNAA0702009 1 20070212 A 5100 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE UNKNOWN UNKNOWN A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 05 248PS 7925 CREW REPORTED A LOUD NOISE COMING FROM THE F/O'S SIDE AFTER TAKEOFF. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE RIGHT HAND FORWARD FUSELAGE AREA. SUSPECT COMM DOOR LEFT OPEN BUT WAS NOT OPEN UPON ARRIVAL TO AIRCRAFT. NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. NOTE: WHEN MAINTENANCE ARRIVED AT THE AIRCRAFT, DOO R WAS CLOSED. 2 L 7 2 4F 4 F RT A21EA E15NE 2007022600162 20070226 00162 2007 2 26 VNAA0702007 4 20070208 A 3418 501177003 ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE STICK PUSHER FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 725PS 5448 10186 CREW REPORTED A STALL FAIL CAS MESSAGE AFTER TAKEOFF. CREW RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE REMOVED AND R EPLACED THE STICK PUSHER ACTUATOR IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE . 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007022600167 20070226 00167 NM 2007 2 26 ASAA0791482 1 20070220 A 5230 143A61121 SKIN BOEING 737 737990 NM CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 323AS 30021 FWD CARGO DOOR WAS FOUND TO HAVE THREE DENTS WITH GOUGES. REPAIRED IAW SRM 52-00-01 REPAIR NR 2. 2 L 7 4 4F RT A16WE 2007022600168 20070226 00168 EA 2007 2 26 VNAA0702012 1 20070216 A 5200 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE GROUND POWER OPEN A VNAA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 GL 05 725PS 10186 CREW REPORTED A LOUD NOISE COMING FROM THE RT SIDE ON CLIMBOUT. CREW RETURNED TO GSO AND LANDED WITHOUT INCIDENT. MAIN TENANCE INSPECTED AND FOUND THE GROUND POWER SERVICE DOOR OPEN. MAINTENANCE CLOSED AND SECURED DOOR. NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007022600169 20070226 00169 SO 2007 2 26 CHQA200700006 1 20070224 A 3411 DRAIN EMB 135 EMB135LR 3260305 SO STATIC SYS CONTAMINATED A CHQA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 11 831RP 145663 FLIGHT 6302 - CVG-XNA - AT CRUISE FLIGHT, FL310, WINDSHIELD ANTI-ICE FAIL WITH NO ASSOCIATED MESSAGES. SOON AFTER, CAPT AIN SIDE AIRSPEED AND ATTITUDE FAILED, AUTOPILOT FAIL, IC WOW INOP. NO ANTI-ICE, SPS ADV MESSAGE ON EICAS. DECLARED EM ERGENCY. MAINTENANCE FOUND STATIC DRAIN TRAPS FULL OF WATER. PERFORMED OPS CHECK OF AUTOPILOT, IC 600, PITOT HEAT, ADC , AND WINDSHIELD, ALL OPS CHECK NORMAL. 2 L 7 2 4F RT T00011AT 2007022600174 20070226 00174 NM 2007 2 26 AWXA200700247 1 20070202 A 5315 654583469 STRAP BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED FLOORBEAM STABILIZER STRAP, BS 312, RBL 4. REPAIRED FLOORBEAM STABILIZER STRAP, BS 312, RBL 4 IAW B 737-300 SRM 53-10-51-2R4. 2 L 7 2 4F RT A16WE 2007022600175 20070226 00175 NM 2007 2 26 AWXA200700248 1 20070202 A 5315 654583469 STRAP BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED FLOORBEAM STABILIZER STRAP, BS 312, LBL 8. REPAIRED FLOORBEAM STABILIZER STRAP, BS 312, LBL 8 IAW B 737-300 SRM 53-10-51-2R4. 2 L 7 2 4F RT A16WE 2007022600176 20070226 00176 NM 2007 2 26 AWXA200700249 1 20070126 A 5230 6547952133 FRAME BOEING 737 73733A 1384673 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND AFT CARGO DOOR UPPER FORWARD FRAME CRACKED, BS 795, S18R. REPAIRED AFT CARGO DOOR UPPER FORWARD FRAME, BS 7 95, S18R IAW B737-300 SRM 51-70-13. 2 L 7 2 4F RT A16WE 2007022600178 20070226 00178 NM 2007 2 26 AWXA200700251 1 20070125 A 5313 65617772 STRINGER SPLICE BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND STRINGER SPLICE CHANNEL CRACKED, BS 351.2, S8L. REPLACED STRINGER SPLICE CHANNEL CRACKED, BS 351.2, S8L IA W AWA ER ER 03-5312-07051-SS1. 2 L 7 2 4F RT A16WE 2007022600179 20070226 00179 NM 2007 2 26 AWXA200700252 1 20070125 A 5320 69265533 INTERCOSTAL BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND INTERCOSTAL WEB CRACKED, BS 348.2 S16L. REPLACED INTERCOSTAL WEB, BS 348.2 S16L IAW AWA ER 03-5312-07051-S S1. 2 L 7 2 4F RT A16WE 2007022600180 20070226 00180 NM 2007 2 26 AWXA200700253 1 20070125 A 5340 69265552 ATTACH ANGLE BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND UPPER INTERCOSTAL CLIP CRACKED, BS 348.2 TO 351.2, S16L. REPLACED UPPER INTERCOSTAL CLIP, BS 348.2 TO 351.2 , S16L IAW AWA ER 03-5312-07051-SS1. 2 L 7 2 4F RT A16WE 2007022600181 20070226 00181 NM 2007 2 26 AWXA200700254 1 20070125 A 5320 69165096 ATTACH ANGLE BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND LOWER INTERCOSTAL CLIP CRACKED, BS 348.2 TO 351.2, S16L. REPLACED LOWER INTERCOSTAL CLIP, BS 348.2 TO 351. 2, S16L IAW AWA ER 03-5312-07051-SS1 . 2 L 7 2 4F RT A16WE 2007022600182 20070226 00182 NM 2007 2 26 AWXA200700255 1 20070125 A 5320 6517684634 INTERCOSTAL BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND INTERCOSTAL WEB CRACKED BETWEEN BS 294.5 AND 303.9, S16L. REPLACED INTERCOSTAL WEB BETWEEN BS 294.5 AND 303 .9, S16L IAW AWA ER 03-5312-07051-SS1. 2 L 7 2 4F RT A16WE 2007022600184 20070226 00184 NM 2007 2 26 AWXA200700257 1 20070125 A 5340 66142101 ATTACH ANGLE BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND INTERCOSTAL CLIP CRACKED, BS 294.5, S11L. REPLACED INTERCOSTAL CLIP, BS 294.5, S11L IAW AWA ER 03-5312-0705 1-SS1. 2 L 7 2 4F RT A16WE 2007022600189 20070226 00189 NM 2007 2 26 ASAA0741477 1 20070221 A 5315 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 FLOORBEAM STA 321 UPPER CHORD IS CORRODED AT FASTENER REPAIRS. REMOVED DAMAGED SECTION OF UPPER CHORD (T-CAP) FABRICATE D AND INSTALLED REPAIR CHORD ANGLES AND FILLERS IAW SRM 53-10-51 REPAIR 5. 2 L 7 2 4F RT A16WE 2007022600191 20070226 00191 NM 2007 2 26 ASAA0741479 1 20070221 A 5315 FLOORBEAM BOEING 737 7374Q8 138447Q NM BS 947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 FLOORBEAM UPPER CHORD CORRODED. REMOVED UPPER FLANGE FABRICATED AND INSTALLED REPAIR CHORD ANGLES STRAPS AND FILLERS IA W ASA EA 5310 02699. 2 L 7 2 4F RT A16WE 2007022600192 20070226 00192 NM 2007 2 26 ASAA0741480 1 20070221 A 5315 FLOORBEAM BOEING 737 7374Q8 138447Q NM BS 360 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 FLOORBEAM UPPER FLANGE IS CORRODED. REMOVED COMPLETE UPPER CHORD INCLUDING PREVIOUS REPAIR AT RBL 35-45, FABRICATED AND INSTALLED REPLACEMENT UPPER T-CHORD SPLICE ANGLES SPLICE STRAPS AND FILLERS IAW ASA EA 53 10 02700. 2 L 7 2 4F RT A16WE 2007022600193 20070226 00193 NM 2007 2 26 AWXA200700258 1 20070122 A 5340 69489852 ATTACH FITTING BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND ATTACH CLIP FOR FRAME/WEB CRACKED BS 360, S8L. REPLACED ATTACH CLIP FOR FRAME/WEB, BS 360, S8L IAW AWA ER 0 3-5312-07051-SS1. 2 L 7 2 4F RT A16WE 2007022700004 20070227 00004 NM 2007 2 27 NOCA04507 1 20070225 A 3350 363674 LIGHT BOEING 767 767300 1385204 NM CABIN INOPERATIVE A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 769NA 28039 E-PATH LIGHTS AT SEAT 26CD PARTIALLY LIGHT. REMOVED AND REPLACED E-PATH STRIP AT SEAT 26CD. OPS CHECKS OKAY. BOEING 76 7-304ER 2 L 7 2 4F RT A1NM 2007022700005 20070227 00005 NM 2007 2 27 NOCA04607 1 20070225 A 3240 427571 CONTROL UNIT BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE AUTOBRAKES INOPERATIVE A NOCA O OTHER O OTHER NR NOT REPORTED 1 EA 15 754NA 29381 AUTOBRAKE SYSTEM INOP. REMOVED AND REPLACED ANTISKID/AUTOBRAKE CONTROL UNIT IAW MM 32-42-00 OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E12EU 2007022700006 20070227 00006 NM 2007 2 27 DHL2007781006 1 20070226 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM BS 500-600 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 781DH 21996 RT CABIN, SEVERAL AREAS OF CORROSION ON SEAT TRACK AT BS 500-600, RBL 48. REMOVED DAMAGED SEAT TRACK SECTION. FABRICAT ED NEW SECTION FROM BAC1520-792, PO NR 9003797, 111.5" LONG, PER B727 SRM 53-10-5 FIG 1. FABRICATED REPAIR SPLICE FROM BAC1503-10122, PO NR 9004539, 2 EA AT 13.5" LONG, AND STRAP FROM 7075-T6, .250" X 8" X 2", PO NR 9001189, PER B727 SRM 5 3-10-5 FIG 1. TREATED, PRIMED, AND INSTALLED REPAIR PARTS/SEAT TRACK PER B727 SRM 51-10-2 AND 53-10-5 FIG 1. 2 L 7 3 4F A3WE 2007022700008 20070227 00008 NM 2007 2 27 UPS07249235 1 20070221 A 2910 LINE BOEING 727 72731C 1384011 NM "A" HYD SYSTEM LEAKING A IPXA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 01 922UP 19231 INSPECTION TYPE:N/A A-SYSTEM HYDRAULIC QUANTITY LOSS DURING FINAL APPROACH. NO EMERGENCY DECLARED. MX IS I/W REPLACING A LEAKING RETURN LINE. FOUND UNION LEAKING AT A SYSTEM PRESS LINE, REMOVED AND REPLACED UNION, LOCATED AND MARKED ON A AFT RIGHT STAIRWELL. REQUIRES LEAK CHECK. LEAK CHECK ON ENG RUN. NO LEAKS NOTED. OK FOR SERVICE. 2 L 7 3 4F A3WE 2007022700009 20070227 00009 NM 2007 2 27 UPS07449228 1 20070215 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 460 S15R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C 1EA FASTENER HOLE FOUND CRACKED AT BS 460 S15R CRACKS WERE LOCATED AT UPWARD AND DOWNWARD DIRECTION. STRINGER REPLACED AS PER SRM 51-10-01 PG 9. 2 L 7 4 4F A20WE 2007022700012 20070227 00012 WP 2007 2 27 FX7A200700003 1 20070129 A 7711 LINE DOUG DC9 DC983 3022083 WP PT2 CLOGGED A FX7A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 19 836NK 53045 DURING TAKEOFF ROLL, AFTER 1.4 EPR CHECK & AUTOTHROTTLE ENGAGEMENT ENGINE NR 2 EPR INDICATION WENT TO 1.75 AND REMAINED FIXED. AUTOTHROTTLE DISENGAGED AND WOULD NOT RE-ENGAGED. ABORTED T/O AT 65 KIAS & RETURNED TO GATE. FOUND PT2 LINE CL OGGED. CLEANED PT2 LINE AND REPLACED ENGINE FUEL FILTERS. SYSTEM TESTED NORMAL DURING TEST FLIGHT. 2 L 7 2 4F RT A6WE 2007022700014 20070227 00014 NM 2007 2 27 KCSA071063 1 20070222 A 5412 BULKHEAD BOEING 747 747146 1384905 NM NR 2 NACELLE CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 NR 2 PYLON AFT OF NAC STA 221.9 PRESSURE SUPPLY LINE JAM NUT CHAFING BULKHEAD. 2 L 7 4 4F RT A20WE 2007022700015 20070227 00015 WP 2007 2 27 IXXA07SMN070S 1 20070131 A 5313 NP1616757 LONGERON DOUG DC8 DC871F 302199D WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND LONGERON 17 LEFT CRACKED AT STATION 1776.000. REMOVED DAMAGED LONGERON. CLEAN ED TREATED AND PRIMED AREA AND NEW LONGERON. INSTALLED NEW LONGERON IAW DC8 SRM 53-5-1 FIGURE 7, SHEET 1, PAGE 22, DC8 SRM 53-1-0 PAGE 1 DC8 SRM 51-1-8B, DC8 SRM 51-2-0, FIGURE 50, DC8 SRM 51-1-21, DC8 SRM 51-1-20D AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007022700018 20070227 00018 NM 2007 2 27 UPS07449236 1 20070223 A 3350 BATTERY PACK BOEING 747 747123 1384873 NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:N/A AFT EMERGENCY LIGHT IN MAIN ENTRY DOOR INOP. RELAMP, NO HELP. REMOVED AND REPLACED BATTERY PACK PE R CHAPTER 33. OPS CHECKS OK. 2 L 7 4 4F A20WE 2007022700020 20070227 00020 WP 2007 2 27 UPS07849232 1 20070214 A 5320 FLOOR SUPPORT DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C3 CABIN SUBFLOOR STA 25-48 RBL 10 FLOOR SUPPORT ANGLE IS BROKEN. REMOVED FLOOR SUPPORT ANGLE AT CABIN SUBFLOOR AT STA 25-48 RBL 10, REPAIRED FLOOR SUPPORT ANGLE AT STA 25-48 RBL10 IAW SRM 51-01-19, AND SRM 51-3-2. 2 L 7 4 4F RT 4A25 2007022700021 20070227 00021 WP 2007 2 27 UPS07849233 1 20070213 A 5740 BRACKET DOUG DC8 DC871F 302199D WP FUEL DUMP CHUTE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C3 LEFT WING FLAP WELL FUEL DUMP CHUTE HORSE SHOE BRACKET CRACKED. REMOVED CRACKED HORSE SHOE BRACKET F ROM LEFT WING DUMP CHUTE IAW SRM 51-1-20D. FABRICATED AND INSTALLED HORSE SHOE BRACKET AT LEFT WING FUEL DUMP CHUTE IAW DWG 5649654, AND SRM 51-1-4, 51-3-2, AND SRM 51-1-21A. 2 L 7 4 4F RT 4A25 2007022700022 20070227 00022 NM 2007 2 27 USAA200702001 1 20070223 A 5712 RIB BOEING 737 7374B7 1384702 NM CRACKED CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 24893 24893 CRACK FOUND AT RIB 135.5 SKIN CLIP CRACKED BETWEEN STR 2 & 3. REPAIRED PER EA 84116. 2 L 7 2 4F RT A16WE 2007022700023 20070227 00023 SO 2007 2 27 C2XA07RI005 1 20070219 A 3350 3025101 POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13958 145085 RIC - MX DURING ROUTINE MAINTENANCE, MX FOUND LT & RT OVERWING EMERGENCY LIGHTS INOP. MX TROUBLESHOT THE PROBLEM AND FO UND EMERGENCY POWER SUPPLY NR 4 INOP. MX REMOVED AND REPLACED POWER SUPPLY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY . ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007022700029 20070227 00029 NM 2007 2 27 HALA0700049 1 20070131 A 5420 CHANNEL BOEING 767 767300 1385204 NM NR 2 NACELLE CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 584HA 24258 NR 2 ENGINE PYLON AFT FAIRING LT UPPER SUPPORT CHANNEL IS CRACKED AT FWD END. REMOVED DAMAGED LT SUPPORT CHANNEL ON THE NR 2 ENGINE AFT FAIRING AND INSTALLED A NEW SUPPORT CHANNEL PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007022700030 20070227 00030 NM 2007 2 27 HALA0700050 1 20070131 A 5420 CHANNEL BOEING 767 767300 1385204 NM NR 2 NACELLE CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 584HA 24258 NR 2 ENGINE PYLON AFT FAIRING RT UPPER SUPPORT CHANNEL IS CRACKED AT FWD END. REMOVED DAMAGED RT UPPER SUPPORT CHANNEL O NR 2 ENGINE AFT FAIRING AND INSTALLED A NEW SUPPORT CHANNEL PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007022700032 20070227 00032 NM 2007 2 27 HALA0700052 1 20070103 A 5753 FLAP BOEING 767 767332 1382001 NM TE FLAPS GROUND DAMAGE A HALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 13 598HA 23277 RT O/B FLAP LWR T/E WAS DAMAGED BELOW THE NR 12 SPOILER WHILE POSITIONING SCISSOR LIFT. THE CORNER OF THE RAIL CONTACTE D THE FLAP. REPAIRED DAMAGE ON THE RIGHT O/B FLAP LWR T/E BELOW THE NR 12 SPOILER IAW SRM 51-70-0G. 2 L 7 2 4F RT A1NM 2007022700033 20070227 00033 NM 2007 2 27 HALA0700054 1 20070222 A 4900 UNKNOWN BOEING 767 76733A 1385209 NM APU UNKNOWN A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 587HA 33421 ETOPS SIGNIFICANT SYSTEM - BTB - APU SHUTDOWN ON PUSHBACK, PRIOR TO ENG START. ECU SELF TEST PER FIM 49-11-00. TEST OK NO FAULTS OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007022700036 20070227 00036 EU 2007 2 27 AWXA200700236 1 20070217 A 3350 RELAY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS UNKNOWN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 604AW 1196 PHX - EEL - FOUND EMERGENCY EXIT LIGHTS FLASHING ON AND OFF DURING TAXI. MX REPLACED RELAY 8WL PER TSM 33-51-00-810-819 . EMERGENCY LIGHTS OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007022700037 20070227 00037 NM 2007 2 27 AWXA200700259 1 20070122 A 5340 69482042 ATTACH FITTING BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND ATTACH CLIP CRACKED, BS 360, S14 - S15L. REPLACED ATTACH CLIP, BS 360, S14 - S15L IAW AWA ER 03-5312-07051- SS1. 2 L 7 2 4F RT A16WE 2007022700039 20070227 00039 NM 2007 2 27 AWXA200700261 1 20070125 A 5311 65582803 FRAME BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CORROSION ON FRAME, BS 358, S28L - S28R. REPAIRED FRAME, BS 358, S28L - S28R IAW B737-300 SRM 53-00-07-2R7. 2 L 7 2 4F RT A16WE 2007022700041 20070227 00041 NM 2007 2 27 AWXA200700263 1 20070122 A 5330 654577882 SKIN PANEL BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED FUSELAGE SKIN, R2 DOOR CUT OUT, BS 965, S17R. REPAIRED FUSELAGE SKIN, R2 DOOR CUT OUT, BS 965, S17R IAW B737-300 SRM 53-00-01 REPAIR 32. 2 L 7 2 4F RT A16WE 2007022700042 20070227 00042 NM 2007 2 27 AWXA200700264 1 20070127 A 2560 P4010021 POWER SUPPLY BOEING 737 73733A 1384673 NM ZONE 200 INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - EEL - FOUND OUTBOARD AFT FLIGHT ATTENDANTS EMERGENCY FLASH LIGHT INOPERATIVE. REPLACED OUTBOARD AFT FLIGHT ATTEND ANTS EMERGENCY FLASH LIGHT POWER SUPPLY. 2 L 7 2 4F RT A16WE 2007022700043 20070227 00043 NM 2007 2 27 AWXA200700265 1 20070126 A 5754 65C26601179 SKIN BOEING 737 7373S3 1384711 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND LEFT WING NR 1 SLAT LOWER SURFACE HAS 6 CRACKS, SS 291.75 - SS 300.5. REPAIRED LEFT WING NR 1 SLAT LOWER SU RFACE, SS 284.4 - SS 333.4 IAW B737-300 SRM 57-43-01. 2 L 7 2 4F RT A16WE 2007022700045 20070227 00045 NM 2007 2 27 AWXA200700267 1 20070203 A 5330 6545770 SKIN BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED FUSELAGE SKIN, BS 586, S4L. REPAIRED FUSELAGE SKIN, BS 586, S4L IAW B737-300 SRM 53-00-01-2R. 2 L 7 2 4F RT A16WE 2007022700050 20070227 00050 WP 2007 2 27 IXXA07SMN044S 1 20070119 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING-UPPER LEADING EDGE CORRODED AT STATION 472.099. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INTER NAL SURFACE. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN IAW DC8 SRM 57-3-1 FIGURE 5 PAGE 10, DC8 SRM 51-1- 8 PAGES 17-18, DC8 SRM 57-2-0 PAGE 16, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-8B, DC8 SR M 57-1-0 PAGE 1, DC8 SRM 51-1-11, DC8 SRM 51-3-0 AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007022700053 20070227 00053 NM 2007 2 27 DHL2007781005 1 20070226 A 5415 ATTACH ANGLE BOEING 727 727227 1384078 NM NR 3 NACELLE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 781DH 21996 FOUND UPPER OTBD NR 3 PYLON ATTACH ANGLE CRACKED AT HOLE "P" AT ENG BL 28, REF B727 SB 54A0010. REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE FROM P/N 4130 ANNEALED, .100" X 20.5" X 3", PO NR 7114153, PER B727 SRM 54-10-2 FIG 3, 51-30-2, AND 51-30-5. HEAT TREATED ANGLE TO 180-200 KSI IAW MIL-SPEC MIL-H-6875. INSTALLED NEW ANGLE PER B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007022700055 20070227 00055 NM 2007 2 27 SB07018 1 20070223 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM EMERGENCY LIGHTS DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 24893 PIT MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT FOR THE LEFT FORWARD OVERWING EMERGENCY ESCAPE DOOR, BETWEEN SEAT ROWS 10 AND 11, WAS INOPERATIVE. MAINTENANCE CHARGED THE EMERGENCY EXIT LIGHTS. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007022700057 20070227 00057 NM 2007 2 27 ASAA0771484 1 20070223 A 5320 143A52409 FLOOR SUPPORT BOEING 737 737790 13844CN NM BS 540 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 CABIN FLOOR SUPPORT ANGLE CRACKED AT FS 540. REPAIRED IAW EA 5320 01790. 2 L 7 2 4F RT A16WE 2007022700058 20070227 00058 WP 2007 2 27 IXXA07SMN029S 1 20070113 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 500 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING-EXTERNAL UPPER SKIN CRACKED AT STATION XRS74.000 STRINGER 11. REMOVE D FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATED REPAIR DOUBLER AND FILLERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPL IED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW DC8 SRM 57-2-1 FIGURE 10 SHEET 3, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 57-3-1 FIGURE 10 PAGE 17 ITEM "A", DC8 SRM 51-10-0, FIGURE 1 SHEET 6, DC8 SRM 51-1-8B, DC8 SRM 51-1-12 AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007022700062 20070227 00062 EU 2007 2 27 07FDEA00527 1 20070220 A 5330 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 300 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 FOUND CORROSION ON SKIN PANEL BETWEEN C77-87, P3-6 RT AND C78-86, P3-6 LT. REPAIR PERFORMED BY REMOVE CORROSION IAW SRM 51-74-10, SRM 53-19-12/FIG 1. 2 L 7 2 4F RT A35EU 2007022700064 20070227 00064 NM 2007 2 27 07FDEA00547 1 20070224 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 MAIN DECK CARGO, FLOOR SEAT TRACK FOUND CORROSION AT STA 5-0 TO 5-53, X=-75.25. SEAT TRACK REPAIR CARRIED OUT AS PER SR M 53-70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022700065 20070227 00065 NM 2007 2 27 07FDEA00548 1 20070225 A 5711 SPAR CAP DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LT WING REAR SPAR LWR CAP XORS=1050 FOUND UPPER SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5720-106594. CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022700067 20070227 00067 NM 2007 2 27 07FDEA00550 1 20070225 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 MAIN DECK CARGO, FLOOR SEAT TRACK FOUND CORROSION AT STA 1508, X=-8.5. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-0 0 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022700068 20070227 00068 WP 2007 2 27 07FDEA00553 1 20070226 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 615 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 FWD CARGO COMPT FOUND 1 CRACK 0.25" LONG ON FRAME AT STA 615 BTWN LONG NR 39 AND LONG NR 40 LT FRAME FLANGE REPAIR CARRI ED OUT IAW SRM 53-30-00 FIG 4A VOL 1 AND SRM 53-12-01 FIG 2 VOL 3 "SATIS" AREA REPROTECTED IAW SRM 51-21-01 VOL 2. FRAM E REPAIRED IAW SRM 53-30-00 FIG 5 VOL 2. SHEAR CLIP REPAIRED STA 615 LT LONG NR 41-42 IAW SRM 53-30-00 FIG 10 VOL 1. S TRUT INSTALLATION AT STA 615 LT. INSTALLED IAW TRANSAMERICA MOD DWG 10-5301440. 2 L 7 3 4F A22WE 2007022700069 20070227 00069 NM 2007 2 27 07FDEA00554 1 20070226 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 MAIN DECK CARGO FLOOR SEAT TRACK FOUND CORRODED AT STA 5-0 TO 5-10, X=-8.5. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53 -70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022700070 20070227 00070 NM 2007 2 27 07FDEA00555 1 20070226 A 5311 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 MAIN DECK CARGO FRAME FOUND DENT AT STA 1641. REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG. 1 VOL.I. REPETITIVE INSPE CTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES TO BE CARRIED OUT AND THEREAFTER 9500 CYCLES AS PER SRM 53-30-00 F IG.1. VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM CHAPTER 6-2-100. ITEM TRANSFERRED TO OPEN ITEMS LIST CONT ROL NO. 309719. 2 L 7 3 4F RT A22WE 2007022700072 20070227 00072 CE 2007 2 27 DXTA200701947 1 20070214 A 5610 WINDSHIELD CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL COCKPIT FAILED E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 930QS 7500130 RT WINDSHEILD SHATTERED AFTER TAKEOFF. REPLACED RT WINDSHIELD PRE CESSNA 750 MM CH 56-11-00 CHECKS OK. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007022700073 20070227 00073 EU 2007 2 27 BAQA20070008 1 20070212 A 7100 9550177590 THERMOCOUPLE AGUSTA A109 A109E 0260119 EU TMECA ARRIUS ARRIUS2K1 NE NR 2 ENGINE ERODED E BAQA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 EA 03 109DK 2635 11504 33008 DURING NR 2 ENGINE START-UP. NR 2 ECU MAINTENANCE AND TOT CAUTION LIGHT ILLUMINATED AND THE NR 2 ENGINE SHUTDOWN. DOWN L OADED NR 2 ECU AND FOUND FAULT CODE FOR T-4 SIGNAL LOSS. DURING START THE ECU MONITORS T-4 TEMPERATURE. IF SIGNAL IS LOS S THE ECU SHUT THE ENGINE DOWN TO PREVENT OVER TEMP OF THE ENGINE (ONLY DURING START). FOUND PYROMETRIC HARNESS PROBE E RRODED. THE NR 2 ENGINE PYROMETRIC HARNESS WAS REPLACED AND OPS CHECKS PERFORMED WITH NO DEFECTS NOTED AT THIS TIME. POW ER CHECKS WITHIN MANUFACTURERS SPECIFICATIONS. 1 G 7 2 3U 3 U RT H7EU E34NE 2007022700074 20070227 00074 WP 2007 2 27 07FDEA00556 1 20070226 A 5347 SEAT TRACK DOUG DC10 DC1030F 3023504 WP BS 1079-1099 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 FOUND MAIN CABIN CRACK 12" LONG ON TRACK X=27 BTWN STA 1079 AND 1099. REMOVED FLOOR PANEL IAW MM 53-21-01-2. REMOVED S EAT TRACK SPLICE AT STA 1129 IAW SRM 51-33-01 VOL 2. CUT AND REPLACED SEAT TRACK SECTION AT STA 1069 IAW SRM 53-70-00 F IG 1 SHEET 1-2. REINSTALLED ORIGINAL SPLICE IAW SRM 51-33-01 VOL 2. FABRICATED PART IAW DETAIL PARTS TRAVELER N/R N008 23 AND SRM 53-70-00 FIG 1 SHEET 2 VOL 1. REINSTALLED FLOOR PANEL IAW MM 53-21-01-2. 2 L 7 3 4F RT A22WE 2007022700075 20070227 00075 WP 2007 2 27 07FDEA00557 1 20070226 A 5310 DOOR FRAME DOUG DC10 DC1030 3023501 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 FOUND MAIN CABIN CRACK 1" LONG ON WEB FWD JAMB DOOR NR 3 LT STA 1251 LONG NR 27. PERFORMED NDI CHECK FOR CRACKS POSITIO N. REMOVED JAMB DOOR COVER FOR ACCESS IAW MM 20-50-02. MAKE 2 STOP DRILL CRACK .250" DIA HOLE, INSTALLED REPAIR DOUBLE R P/N I030889-3A IAW SRM 53-50-00 FIG 19 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER N/R N00889 AND SRM 53-50-00 FI G 19 VOL 1 DETAIL -3. REINSTALLED JAMB DOOR COVER IAW MM 20-50-02. RESEALED AREA IAW SRM 51-42-01 VOL 2. 2 L 7 3 4F A22WE 2007022700076 20070227 00076 WP 2007 2 27 07FDEA00558 1 20070226 A 2810 FUEL TANK DOUG DC10 DC1030 3023501 WP LT CENTER CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 MAIN CABIN SEVERE CORROSION WITH EXFOLIATION ON LT CENTER TANK SKIN TUNNEL AREA, STA 1370 X= 101 (NEAR SLANT PANEL ). L T SLANT PANEL REMOVED, REMOVED BOLTS, ACCESSED AUX UPPER ANGLE REAR SPARE ANGLE. REMOVED CORROSION. FOUND TO BE WITHI N LIMITS. ALL REMOVED PARTS. REINSTALLED PROTECTIVE COATING APPLIED. WORK PERFORMED IAW SRM 51-31-01 PAGE 34/47, SR M 57-20-00 FIG 18 VOL 2 STEPS 4A-4C DWG APB7242, DWG APB7132 SRM 51-42-03. 2 L 7 3 4F A22WE 2007022700078 20070227 00078 WP 2007 2 27 07FDEA00565 1 20070226 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 FOUND UPPER FUSELAGE EXTERNAL SKIN DENT 1, 5" BY 1" DEPTH 0.040" FROM LONG NR 17 TO LONG NR 18 RT SIDE AT STA 1621. ACC OMPLISHED FUSELAGE PLATTING REPAIR AT FUS STA 1621 LONG NR 17-18 RT IAW SRM 53- 20-00 FIG 6 SHT 3-4 VOL 1. FABRICATED P ARTS IAW DETAIL PARTS TRAVELER I025032/N00032 AND IAW SRM 53-20-00 FIG 6 SHT 3-4 VOL 1. 2 L 7 3 4F A22WE 2007022700081 20070227 00081 WP 2007 2 27 07FDEA00567 1 20070226 A 5311 FRAME DOUG DC10 DC1010 3022110 WP FUSLEAGE CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 MAIN CABIN UPPER LOBE, FOUND CRACK 5" LONG ON FRAME AT STA 1741 LONG NR 13 RT. REMOVED EXISTING SPLICE (L13) AND SHEAR CLIP FROM LONG NR 13 TO NR 9 IAW SRM 51-35-01 AND 51-33-01 VOL 2. CUT FRAME BTWN LONG NR 10 AND NR 9 AND PERFORMED SPLI CE REPAIR PER SRM 53-30-00 FIG 5 VOL 1 (ONE PIECE FRAME) DWG AFA0018 REF. INSTALLED EXISTING SPLICE (L13) AND SHEAR CLI P REMOVED PER SRM 51-35-01 AND SRM 51-33-01 VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I025429/N00429 AND IAW SR M 53-30-00 FIG 5 VOL 1 AND DWG AFA0018. 2 L 7 3 4F A22WE 2007022700082 20070227 00082 CE 2007 2 27 20060892 1 20070211 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 298-304 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 245GL UE245 DURING ROUTINE MAINTENANCE 6 INCH CRACK FOUND IN BELLY SKIN 27.5 INCH RT OF BELLY CENTER LINE AT STATION 298 TO STATION 304. MX REPAIRED CRACK ON BELLY SKIN IAW SRM 51-70. REPAIR DIMENSIONS OF 15.75 INCHES X 6 INCHES. INSERT 12 INCHES X 4 .5 INCHES. RII COMPLIED WITH. 2 L 7 2 4T 4 T RT A24CE E26NE 2007022700083 20070227 00083 CE 2007 2 27 20060893 1 20070211 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 545 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 122UX UE122 DURING ROUTINE MAINTENANCE, A CRACK WAS FOUND ON THE RT SIDE OF THE FUSELAGE AT FUSELAGE STATION 545.5 AND RIVETS PROTRU DING DOWN THE 3 INCH CRACK AT WATERLINE 112. MX REMOVED DAMAGED AREA APPROXIAMTELY 6.25 INCHES LONG BY 5.25 INCHES WIDE AT FUSELAGE STATION 545.5 AND WATERLINE 112. MX REPAIRED THE AFFECTED AREA USING 2024-T3 .O32 INCH FOR FILLER AND .040 FOR DOUBLERS IAW SRM 51-70-08. 2 L 7 2 4T 4 T RT A24CE E26NE 2007022700085 20070227 00085 CE 2007 2 27 GLBA20060892 1 20070211 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 298-304 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 245GL UE245 DURING ROUTINE MAINTENANCE 6 INCH CRACK FOUND IN BELLY SKIN 27.5 INCH, RT OF BELLY CENTER LINE AT STATION 298 TO STATION 304. MX REPAIRED CRACK ON BELLY SKIN IAW SRM 51-70. REPAIR DIMENSIONS OF 15.75 INCH X 6 INCH. INSERT 12 INCH X 4.5 IN CH. RII COMPLIED WITH. 2 L 7 2 4T 4 T RT A24CE E26NE 2007022700086 20070227 00086 CE 2007 2 27 GLBA20060893 1 20070211 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 545 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 122UX UE122 DURING ROUTINE MAINTENANCE, A CRACK WAS FOUND ON THE RT SIDE OF THE FUSELAGE AT FUSELAGE STATION 545.5 AND RIVETS PROTRU DING DOWN THE 3 INCH CRACK AT WATERLINE 112. MX REMOVED DAMAGED AREA APPROXIAMTELY 6.25 INCH LONG BY 5.25 INCHES WIDE A T FUSELAGE STATION 545.5 AND WATERLINE 112. MX REPAIRED THE AFFECTED AREA USING 2024-T3 .O32 INCH FOR FILLER AND .040 FO R DOUBLERS SRM 51-70-08. 2 L 7 2 4T 4 T RT A24CE E26NE 2007022700088 20070227 00088 SO 2007 2 27 GUUA02170701 1 20070217 A 3260 922AA2YA6PZ722A PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE LT MLG OUT OF ADJUST A GUUA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 29 283AS 120236 AFTER TAKEOFF LT LANDING GEAR (A) AND (B) DISAGREEMENT LIGHTS WOULD NOT EXTINGUISH UPON RETRACTION, A GRINDING SOUND COU LD BE HEARD IN THE FLIGHT DECK. RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. ADJUSTED THE LT MAIN LANDING GEAR UP LOCK PROXIMITY SENSORS OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 2007022700089 20070227 00089 NE 2007 2 27 C8GA20070003 2 20070216 A 7230 BLADES BOEING 727 727225 1384077 NM PWA JT8 JT8D17 52049 NE NR 2 COMPRESSOR DAMAGED A C8GA E ENGINE SHUTDOWN E VIBRATION/BUFFET CL CLIMB 1 SO 29 815EA 22552 688114 FLT 1723 FROM BOS TO TOL, DURING CLIMB-OUT, NR 2 ENGINE BEGAN TO VIBRATE AND WAS CONFIRMED WITH THE THROTTLE. ENGINE BE GAN TO COMPRESSOR STALL, ENGINE WAS SHUTDOWN AND AIRCRAFT LANDED WITHOUT INCIDENT IN TOL. POST FLIGHT INSPECTION REVEAL ED FOD DAMAGE TO THE C1 AND C2 FAN BLADES. NR 2 ENGINE WAS REMOVED AND REPLACED. NO OTHER DEFECTS WERE NOTED, AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2007022700098 20070227 00098 NM 2007 2 27 07FDEA00528 1 20070220 A 2422 BUSS DOUG MD11 MD11 3023602 NM MALFUNCTIONED A FDEA A J UNSCHED LANDING DUMP FUEL H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 25 593FE 48551 WHILE EXPERIENCING DU4,5 &6 INTERMITTENT BLANKING RECIEVED 'BUS R EMER AC OFF' LVL 1 ALERT,THEN 'IRU 2 ON BAT' LVL 1,F INALLY 'IRU2 FAIL' LVL 2 ALERT.LATER RECEIVED 'SELECT FADEC ALTN' LVL 2 ALERT ON ALL ENGINES,'ATC XPNR 1 & 2 'FAIL A LERTS,ETC. DIVERTED CDG PRIOR TO OCEANIC AIRSPACE. PRECAUTIONARY FOR LOSS OF POWER OF RIGHT EMERGENCY AC BUSS, R & R RC CB B1-138, B1-139, R2-18, R2-5157, DU'S 4-5-6, DEU-2, CK S1-281 & ADJUST, B1-139 CHECK GROUNDS AT PINS 5A & 3 PIN 3 VIA CB'S B1-139. INSPECTED BUNDLES AND WIRING. RAN ENGINES 5 MINUETS. ALL TEST OK. TEST FLIGHT WAS PERFORMED FOR ADG FUN CTIONAL TEST. ALL SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F RT A22WE 2007022700099 20070227 00099 2007 2 27 C2XA07RI006 2 20070220 A 7200 ENGINE EMB 145 EMB145EP 3260221 SO NR 1 CONTAMINATED A C2XA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 14942 145037 FLT 4930 - IAD CREW REJECTED TAKE OFF DUE TO SMOKE IN COCKPIT. SMOKE OCCURRED WHEN THRUST WAS ADVANCED TO DETENT. SMOKE CLEARED WHEN THRUST WAS REDUCED AND AFTER ENGINES WERE SHUT DOWN. SMOKE WAS A BLUE/GRAY COLOR. IAD MX RAN NR 1 & 2 ENGIN ES WITH PAKS TO PURGE THE SYSTEM OF RESIDUAL DE-ICING FLUID. NO MORE SMOKE FOUND AT THIS TIME. ACFT WAS APPROVED TO RETU RN TO SERVICE. 02-26-2007. 2 L 7 2 4F RT T00011AT 2007022700105 20070227 00105 NM 2007 2 27 WRNA200700002 1 20070210 A 5347 8121687 SEAT TRACK BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING 'C' CHECK, CAPTAINS AFT INBD SEAT TRACK WAS FOUND CRACKED, CRACKED VERIFIED WITH HFEC. REPLACED CAPTAINS AFT INBD SEAT TRACK IAW 747 MM 20-51-1. 2 L 7 4 4F A20WE 2007022700115 20070227 00115 NM 2007 2 27 DL757070159 1 20070226 A 2121 731376 FAN BOEING 757 757232 1384965 NM FWD CARGO BIN SEIZED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 655DL 24395 EN ROUTE ATL-SNA, CREW NOTICED BURNING/SMOKE ODOR IN FLIGHT DECK AND CABIN. NO VISIBLE SMOKE REPORTED. CREW COULD NOT ISOLATE SOURCE SO THEY ELECTED TO DIVERT TO DFW. UPON ARRIVAL DFW CONTRACT MECH FOUND NR 1 FWD EQUIP COOLING SUPPLY FAN EXTREMELY HOT AND SEIZED. MECH REPLACED FAN PER MM AND AIRCRAFT DISPATCHED ON TO SNA. 2 L 7 2 4F RT A2NM 2007022700116 20070227 00116 NM 2007 2 27 DL76L070160 1 20070226 A 3350 20121 CHARGER BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 188DN 27583 FOUND CEILING EMERGENCY LIGHTS AT ROW 16 AND 31 INOP. REPLACED EMERGENCY LIGHT BATTERY CHARGER AT SEAT 23L AND INSTALLE D BATTERY PER AMM CKS GOOD. 2 L 7 2 4F RT A1NM 2007022700117 20070227 00117 EA 2007 2 27 SIMA200705806 1 20070112 A 5315 CC67034157 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 515AE 8208 4042 10121 FOUND STATION 280 FLOORBEAM CORRODED AND CRACKED. SPLICED IN FRAME 280 AND EXTENSION MOUNTS IAW AMERICAN EAGLE ENGINEER ING ORDER CR-53MR-101. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007022800003 20070228 00003 EA 2007 2 28 SIMA200705801 1 20070226 A 2913 6619003 PUMP CNDAIR CL600 CL6002C10 1390015 EA HYD SYSTEM FAILED A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 517AE 8396 10124 HYDRAULIC SYSTEM 2 FAILURE, DECLARED EMERGENCY AND RETURNED TO ORD. REMOVED AND REPLACED NUMBER 2 HYDRAULIC ENGINE DRIV EN PUMP IAW CRJ AMM 29-11-01 AND AMERICAN EAGLE WORK CARD 02-05-900-016 WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SER VICE. 2 L 7 2 4F RT A21EA 2007022800004 20070228 00004 NM 2007 2 28 DHL2007781008 1 20070226 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM BS 480-610 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 781DH 21996 LT CABIN, SEVERAL AREAS OF CORROSION ON SEAT TRACK AT BS 500-600, LBL24. REMOVED DAMAGED SEAT TRACK SECTIONS, BS 480-61 0. FABRICATED NEW SEAT TRACK SECTION FROM BAC1520-792, PO NR 9003797, 130" LONG, PER B727 SRM 53-10-5 FIG 1. FABRICATED REPAIR ANGLES FROM BAC1503-10122, PO NR 9004539, 2 AT 13" LONG, AND STRAP FROM 7075-T6, .250" BY 7.5" BY 2", PO NR 9001 189, PER B727 SRM 53-10-5 FIG 1. TREATED, PRIMED, AND INSTALLED REPAIR PARTS/SEAT TRACK PER B727 SRM 51-10-2 AND 53-10- 5 FIG 1. 2 L 7 3 4F A3WE 2007022800005 20070228 00005 NM 2007 2 28 CALA0700085 1 20070223 A 3260 252005 FUSE BOEING 757 757224 1384958 NM MLG INDICATOR FAILED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 29129 28969 THE RIGHT MLG RED UNSAFE LIGHT ILLUMINATED 15-20 SECONDS AFTER GEAR HANDLE WAS PLACED TO OFF DEPARTING IAH. APPROXIMATE LY 15 MINUTES LATER THE GEAR FELL DOWN ON ITS OWN. THE GEAR HANDLE WAS LOWERED, ALL GEAR WERE EXTENDED AND INDICATIONS WERE GREEN. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE RETRACTED THE GEAR AND PLACED T HE HANDLE TO OFF. APPROXIMATELY 20 MINUTES ELAPSED WITH NO PROBLEM. THE FAILURE COULD NOT BE DUPLICATED. THE RIGHT ML G UPLOCK ACTUATOR WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE IAW MM 32-32-41. THE GEAR WAS SWUNG AND ALL OPERA TION CHECKED GOOD. 2 L 7 2 4F RT A2NM 2007022800006 20070228 00006 EU 2007 2 28 SA07014 1 20070226 A 3350 321431 BATTERY PACK AIRBUS A321 A321211 3930370 EU EMERGENCY LIGHT FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 191UW 1447 TPA - A BATTERY FAULT LIGHT CAME ON FOR THE EMERGENCY LIGHTS SYSTEM. MAINTENANCE REPLACED THE BATTERY PACK IN THE FORWA RD LEFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007030100002 20070301 00002 WP 2007 3 1 ABXA070051 1 20070221 A 2752 5751152503 DRIVE LINK DOUG DC8 DC863F 302198F WP T/E FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LEFT INBOARD FLAP DRIVE LINK AT STA XW 98.00 FOUND CRACKED WHILE COMPLYING WITH JC 8020401 AND ASB 27-269, AD 088-10-7. REMOVED AND REPLACED LINK, DETAILS IN WORK PACK 600264601. 2 L 7 4 4F 4A25 2007030100003 20070301 00003 WP 2007 3 1 ABXA070052 1 20070213 A 5310 3917624511 STOP FITTING DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 VENTRAL DOOR JAMB LOWER RIGHT STOP PAD HAD FITTING CRACKED .5 INCH AND BROKEN FASTENERS. REMOVED AND REPLACED BROKEN FI TTINGS IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 2007030100007 20070301 00007 EA 2007 3 1 TRAX200700248 1 20070219 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 AT 349 FRAME BL 45R IS CORRODED. EO 600-53-0350 COMPLIED WITH FOR FABRICATED CLIP, AND EC/TC REO 601R-53-21-742 COMPLIED WITH FOR REPAIR. THIS REPAIR IS ACCEPTABLE WITH NO FURTHER ACTION REQUIRED REF EC/TC REO 601R-53-21-742 ITEM 13. 2 L 7 2 4F RT A21EA 2007030100011 20070301 00011 CE 2007 3 1 BSYA200700006 1 20070224 A 3040 353801327 SWITCH BEECH 58 58 1152740 CE WINDSHIELD HEAT SHORTED E BSYA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 07 140S TH1155 AIRCRAFT WAS ON APPROACH INTO BDL WHEN PILOT NOTICED SMOKE IN THE COCKPIT. DECLARED AN EMERGENCY AND LANDED AT BDL WITH NO PROBLEMS. MAINTENANCE FOUND WINDSHIELD HEAT SWITCH SHORTED. REMOVED AND REPLACED DEFECTIVE SWITCH, OPS CHECKS GOOD . 1 L 7 2 3O 3A16 2007022300272 20070223 00272 NM 2007 2 23 2007UALA00467 1 20070215 A 2620 HOSE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FIRE EXTINGUISH KINKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 903UA 25003 FIREX HOSE GOING FROM BOTTLE TO NR 2 ENG DISCHARGE TUBE HAS A KINK THAT IS APPROX 20 PERCENT OF THE DIAMETER OF THE HOSE . -SD04-17-07- REPLACED HOSE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022300274 20070223 00274 EU 2007 2 23 2007UALA00468 1 20070214 A 2611 SMOKE WARNING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT ACTIVATED A UALA F ACTIVATE FIRE EXT. J WARNING INDICATION NR NOT REPORTED 1 WP 29 423UA 504 V10281 WHILE STARTING NR 1 ENGINE GOT SMOKE AFT CARGO SMOKE ECAM. DISCHARGED FWD AND AFT BOTTLES. MOMENTARILY GOT AN AFT SQUI B FAULT AND AFT BOTTLE DISCHARGE LIGHT NEVER ILLUMINATED. INSPECTED CARGO COMPARTMENTS AND DID NOT FIND ANY DEFECTS WI TH SMOKE DETECTION SYSTEM OR EVIDENCE OF FIRE. REPLACED BOTH FWD AND AFT BOTTLES. SUSPECT THAT MOMENTARY SQUIB FAULT AND DISCHARGE LIGHT NOT ILLUMINATING WAS DUE TO A DELAY IN THE SQUIB FIRING. NO SPECIFIC PART/COMPONENT IS RESPONSIBLE FOR THIS PARTICULAR EVENT SINCE THE CAUSE OF THE INITIAL SMOKE INDICATION IS STILL UNKNOWN. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022300276 20070223 00276 NE 2007 2 23 DL76L070135 2 20070214 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 OIL CONSUMPTION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1200K 43652 11316 28457 727621 NR 2 ENGINE OIL CONSUMPTION BEYOND AMM LIMITS, PER FIM 71-08-00 PAGE 132 OPENED AND INSPECTED NR 4 BEARING COMPT 614338. NO LEAKAGE AT BEARING COVER. RETORQUED NR 4 BEARING SCAVENGE LINES. PERFORMED ENGINE RUN TEST 13. NO GOOD OIL PUDD LING FWD OF LPT LAST STAGE. REPLACED NR 2 ENGINE PER 1T149AD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022300289 20070223 00289 WP 2007 2 23 CNMA20070003 1 20070126 A 3350 EMBS1392 POWER SUPPLY DOUG DC10 DC1030 3023501 WP CABIN DISCHARGED A CNMA K NONE L NO TEST IN INSP/MAINT 1 SW 07 810AX 8563 48265 EMERGENCY LIGHTS WILL NOT TEST FROM COCKPIT. REPLACED FWD POWER SUPPLY AT DOOR 1L IAW MM 33-51, SYSTEM OPS CHECK GOOD. 2 L 7 3 4F A22WE 2007022300310 20070223 00310 NM 2007 2 23 USAA070122 1 20070222 A 5414 SKIN BOEING 737 737401 1384701 NM RT PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 RT PYLON TOP OUTBOARD SIDE, PANEL 5828 OPENING, PYLON STA 220.84 FLANGE CRACKED. STOP DRILL CRACK, FAB'D DOUBLER & INST ALLED PER TYP REP 54-30-07, DEFECT SIZE: .75 INCH. 2 L 7 2 4F RT A16WE 2007022300315 20070223 00315 NM 2007 2 23 USAA070117 1 20070222 A 5313 STRINGER BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STR 4I AT STA 907, CRACK EXTENDING FROM FASTENER HOLE. INSTALLED STRINGER SPLICE, REPAIR PARTS PER SRM 51-10-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007022300319 20070223 00319 EU 2007 2 23 USAA070113 1 20070222 A 5315 D53472190200200 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 163US 1417 FLOORBEAM AT Y765 AT LAV D AFT MOUNT NEAR FRAME 66 HAS CORROSION. REMOVED & REPLACED WITH IDENTICAL PART PER SRM 53-00- 14 FIG 102, DEFECT SIZE: 2 SQ INCHES. 2 L 7 2 4F RT A28NM 2007022600008 20070226 00008 CE 2007 2 26 GLBA20060908 1 20070219 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 288 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 210UX UE210 UPON ROUTINE INSPECTION MAINT FOUND A CRACK AT A RIVET .2500 INCH LONG ON THE RT LOWER BELLY AREA AT FS 288. MAINTENANC E REPAIRED THE AFFECTED AREA AT FS288 IAW SRM 53-90 AND TC 8.2.1. REPAIR DIMENSIONS 7 INCHES BY 6 INCHES. 2 L 7 2 4T 4 T RT A24CE E26NE 2007022600012 20070226 00012 CE 2007 2 26 GLBA20060912 1 20070219 A 5260 ANGLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE AIRSTAIR CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 195GL UE195 UPON ROUTINE INSPECTION MAINTENANCE FOUND AN AIRSTAIR DOOR ENTRANCE ANGLE CRACKED AT FS 150.6 AND RT STRINGER 9AL. MAIN TENANCE AIRSTAIR DOOR ENTRANCE ANGLE IAW BEECH 1900D SRM 53-90. RII INSPECTION COMPLIED WITH PER TC 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007022600014 20070226 00014 EA 2007 2 26 A6WA200740041 1 20070131 A 2751 SENSOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA O OTHER J WARNING INDICATION CR CRUISE 1 GL 31 428AW 7695 FLAP FAIL CAUTION MESSAGE INFLIGHT, FAILED AT ZERO. PERFORMED EXTERNAL VISUAL INSPECTION OF EACH OUTBOARD FLAP, NO EVID ENCE OF TWISTING, SQUEEZING OR ABNORMAL DEFORMATIONS, RESET. UPON INSPECTION OF THE FECU FOUND LEFT BPSU SENSOR FAULT E RROR CODES. REMOVED AND REPLACED LT BPSU. BRAKE AND POS SENSOR UNIT P/N 855D10011, S/N 1878. (M) 2 L 7 2 4F RT A21EA 2007022600017 20070226 00017 SO 2007 2 26 GUUA02200701 1 20070220 A 3350 1317 BULB EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE EMERGENCY LIGHTS INOPERATIVE A GUUA K NONE L NO TEST IN INSP/MAINT 1 SO 29 268AS 120202 AT SCHEDULED ROUTINE MAINTENANCE RT AND LT EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED LT AND RT AFT EMERGENCY EXIT LIG HT BULBS. 2 L 7 2 4T 4 T RT A31SO E20NE 2007022600086 20070226 00086 2007 2 26 758001 4 20070214 A 2200 2591415904 TRIM SYSTEM BOEING 747 747200 1384847 NM AUTOPILOT FAILED A Q2SA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 NE 03 758SA 23138 ASTU WAS ON DEFERRAL. REMOVED AND REPLACED ASTU PRIOR TO DEPARTURE OUT OF PANC IAW AMM 22-14-01. AFFECTED BOTH AUTOPILO T A AND B SYSTEMS AND COULD NOT ENGAGE BOTH AUTOPILOT IN FLIGHT. RETURNED TO PANC. ASTU OPERATIONAL CHECK ACCOMPLISHED ON GROUND AND FAILED IAW AMM 22-14-01. REPLACED WITH PREVIOUSLY REMOVED ASTU. DEFERRAL REMAINS OPEN. RERACKED AUTOPI LOT MONITOR AND LOGIC UNIT. OPERATIONAL CHECK NORMAL ON GROUND IAW AMM 22-11-07. 2 L 7 4 4F RT A20WE 2007022600087 20070226 00087 NM 2007 2 26 AMTA200700064 1 20070221 A 4920 1589352 BYPASS VALVE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211524B4 54555 NE APU UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 561TZ 33526 APU CONTINUALLY SHUTS DOWN. AFTER REMOVAL AND REPLACEMENT OF COOLER BYPASS VALVE, INSPECTED ALL CHIP DETECTORS AND FILTE R BYPASS PINS. ALL CKD GOOD. RAN APU UNLOADED FOR 20 MIN. NO FAULTS. RAN APU 45 MIN UNDER ELEC AND PNEUMATIC LOAD. OPS CK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007022600088 20070226 00088 NM 2007 2 26 SWAA071051 1 20070221 A 3350 101331 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 214WN 32486 LEFT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007022600089 20070226 00089 NM 2007 2 26 SWAA071056 1 20070221 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED SPV CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, LBL 5.7, WL 207. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007022600090 20070226 00090 NM 2007 2 26 SWAA071057 1 20070221 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED SPV CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, LBL 12, WL 218. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007022600091 20070226 00091 NM 2007 2 26 SWAA071065 1 20070221 A 5315 6545812 FLOORBEAM BOEING 737 7373Q8 1384670 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 328, LBL 28 TO RBL 57. REMOVED AND REPLACED FLOO RBEAM CHORD PER SRM. 2 L 7 2 4F RT A16WE 2007022600092 20070226 00092 NM 2007 2 26 SWAA071060 1 20070221 A 5753 6546435277 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED C1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP UPPER INBOARD SURFACE DELAMINATED. REMOVED AND REPLACE D FLAP PER MM. 2 L 7 2 4F RT A16WE 2007022600093 20070226 00093 NM 2007 2 26 SWAA071064 1 20070221 A 5311 6546526 FRAME BOEING 737 7373Y0 1384671 NM BS 400 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 9L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007022600094 20070226 00094 NM 2007 2 26 SWAA071062 1 20070221 A 5311 6546529 FRAME BOEING 737 7373Y0 1384671 NM BS 440 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 9R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007022600095 20070226 00095 NM 2007 2 26 SWAA071055 1 20070221 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 294 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CRACKED AT BS AT BS 294, STR 10L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007022600096 20070226 00096 NM 2007 2 26 SWAA071070 1 20070221 A 5314 6562125 KEELBEAM BOEING 737 7373H4 1384600 NM BS 520 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND KEEL BEAM CHORD CORRODED AT BS 520, LBL 6.5. REPAIRED KEEL BEAM CHORD PER SRM. 2 L 7 2 4F RT A16WE 2007022600097 20070226 00097 2007 2 26 SWAA071058 4 20070221 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM L1 GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2007022600159 20070226 00159 EA 2007 2 26 VNAA0702010 1 20070211 A 2150 GG670950093 ACM CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE LEFT SEIZED A VNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 05 703PS 6820 10137 CREW REPORTED AN OILY SMOKE SMELL IN COCKPIT AND CABIN AFTER NR 2 ENGINE STARTED ON PUSHBACK. CREW RETURNED TO GATE IN CLT. MAINTENANCE REMOVED AND REPLACED THE AIR CYCLE MACHINE IN ACCORDANCE WITH THE AIRCRAFT MAINTNENANCE MANUAL. AIRCR AFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007022600161 20070226 00161 EA 2007 2 26 VNAA0702011 1 20070214 A 3411 B0818022001 STATIC WICK CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE DAMAGED A VNAA O OTHER O OTHER CR CRUISE 1 GL 05 710PS 10167 CREW REPORTED A LIGHTNING STRIKE EN ROUTE TO CLT. MAINTENANCE PERFORMED AN EN ROUTE LIGHTNING STRIKE INSPECTION AND A D ETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE REPAIRED ALL DAMAGE AND REPLACED A STATIC DISCHARGER IN ACCORDANCE WIT H THE AIRCRAFT MAINTNENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007022600172 20070226 00172 NM 2007 2 26 AWXA200700240 1 20070122 A 5340 69489856 ATTACH FITTING BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND L1 DOOR CUT OUT SURROUND STRUCTURE FRAME ATTACH CLIP CRACKED, BS 360, S11L. REPLACED L1 DOOR CUT OUT SURRO UND STRUCTURE FRAME ATTACH CLIP, BS 360, S11L IAW AWA ER 03-5312-07051-SS1. 2 L 7 2 4F RT A16WE 2007022600173 20070226 00173 NM 2007 2 26 AWXA200700246 1 20070202 A 5320 6545834552 INTERCOSTAL BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED INTERCOSTAL, BS 312 - BS 328, RBL 30. REPLACED INTERCOSTAL, BS 312 - BS 328, RBL 30 IAW B737-300 SR M 51-40-02. 2 L 7 2 4F RT A16WE 2007022600186 20070226 00186 WP 2007 2 26 IXXA070008O 1 20070215 A 3231 LIMIT SWITCH DOUG DC8 DC871F 302199D WP ZONE 700 DAMAGED A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 829BX 81557 1885 45994 DURING CLIMB-OUT OF KTOL, AFTER SATISFACTORY UPLATCH CHECK, THE MAIN LANDING DOOR LIGHT REMAINED ILLUMINATED. THE CREW COMPLIED WITH THE ABNORMAL PROCEDURES AND CONTINUED THE FLIGHT TO KSJC AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECT ED WIRING OF THE RIGHT AND LEFT LANDING GEAR DOOR LIMIT SWITCHES. NO PROBLEMS NOTED. DOOR WARNING SYSTEMS OPS CHECK NO RMAL. DUE TO HISTORY MAINTENANCE REPLACED RIGHT LANDING GEAR DOOR LIMIT SWITCH. PERFORMED MAIN LANDING GEAR DOOR LIMIT SWITCH TEST PER DACO MM 32-60-0. SYSTEM OPS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2007022700001 20070227 00001 NM 2007 2 27 XXUA200701037 1 20070221 A 2530 4333100006600 OVEN BOEING 757 7572Q8 1384972 NM PWA 2037 PW2040 NE NR 2 AFT GALLEY INOPERATIVE A XXUA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 401JS 26332 OVEN NR 2 AFT INOPERATIVE (CB PULLED AND COLLARED AFTER SEVERE SMOKE) SPILLAGE NOTED. REPLACED OVEN IAW MM 25-31-00, OP S CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022700016 20070227 00016 NM 2007 2 27 KCSA071064 1 20070223 A 5412 BULKHEAD BOEING 747 747146 1384905 NM NR 3 NACELLE CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 NR 3 PYLON NAC STA 221.9 BULKHEAD PRESSURE SUPPLY LINE FITTING IS CHAFING. 2 L 7 4 4F RT A20WE 2007022700025 20070227 00025 NM 2007 2 27 FDKA200701029 1 20070128 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 801LR 047 FDM 6023 BTV-JFK (1615 PHX LCL), 1 BULB OUT IN ESCAPE PATH LIGHTS. MX REPLACED THE LIGHT. 2 H 7 2 4T RT A13NM 2007022700026 20070227 00026 SO 2007 2 27 FDKA200702042 1 20070203 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCONNECTED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6068 ATL-HSV (0638 PHX LCL), SERVICE DOOR EMERGENCY EXIT SIGN INOP. MX RECONNECTED THE CONNECTOR ON THE SIGN AND OP S CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007022700031 20070227 00031 NM 2007 2 27 HALA0700051 1 20070131 A 5420 ANGLE BOEING 767 767300 1385204 NM NR 2 NACELLE CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 584HA 24258 NR 2 ENGINE PYLON AFT FAIRING AFT SKIN OB STIFFENER FWD ANGLE IS CRACKED. REMOVED NR 2 PYLON FAIRING AFT SKIN O/B STIFF ENER, FWD ANGLE (P/N 313T3080-69) AND FABRICATED REPLACEMENT ANGLE FROM .063 2034T3 IAW SRM 54-53-71-1A-1 AND SRM 51-70- 11-0G-0. INSTALLED NEW ANGLE IAW SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007022700040 20070227 00040 NM 2007 2 27 AWXA200700262 1 20070122 A 5330 655298873 SKIN PANEL BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED FUSELAGE SKIN, L2 DOOR CUT OUT, BS 959, S17L. REPAIRED FUSELAGE SKIN, L2 DOOR CUT OUT, BS 959, S17L IAW B737-300 SRM 53-00-01 REPAIR 32. 2 L 7 2 4F RT A16WE 2007022700046 20070227 00046 NM 2007 2 27 AWXA200700268 1 20070202 A 5311 654580761 FRAME BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED R1 DOOR CUT OUT FORWARD STUB FRAME, BS 294, S16R - S16R. REPLACED R1 DOOR CUT OUT FORWARD STUB FRAM E, BS 294, S16R - S16R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007022700066 20070227 00066 NM 2007 2 27 07FDEA00549 1 20070225 A 5711 SPAR CAP DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LT WING REAR SPAR TOP CAP TAPER FILLER AT XORS=480 FOUND UPPER SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5720-106599 . REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022700079 20070227 00079 WP 2007 2 27 07FDEA00566 1 20070226 A 5311 FRAME DOUG DC10 DC1010 3022110 WP FUSELAG4E CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 MAIN CABIN RT SIDEWALL, FOUND NR 1 CRACK 7" LONG ON FRAME AT STA 1781 LONG NR 13. REMOVED EXISTING SPLICE (L13) AND SHE AR CLIP FROM LONG NR 13 TO NR 9 IAW SRM 51-35-01 AND 51-33-01 VOL 2. CUT FRAME BTWN LONG NR 10 AND NR 9 AND PERFORMED S PLICE REPAIR PER SRM 53-30-00 FIG 5 VOL 1 (ONE PIECE FRAME) DWG AFA0030 REF. INSTALLED EXISTING SPLICE (L13) AND SHEARC LIP REMOVED PER SRM 51-35-01 AND SRM 51-33-01 VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I026541/N01541 AND IAW SRM 53-30-00 FIG 5 VOL 17 DWG AFA0030. 2 L 7 3 4F A22WE 2007022700084 20070227 00084 NE 2007 2 27 20060894 2 20070212 A 7261 LABYRINTH SEAL EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE ENGINE DETERIORATED A GLBA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NM 03 108UX 120108 PILOT REPORT OF SMOKE IN CABIN AND COCKPIT ON FINAL DESCENT. SMOKE WAS NOTICED COMING FROM NR 1 ENGINE. **SUPPLEMENTAL I NFORMATION WILL BE PROVIDED UPON ENGINE REMOVAL AND REPLACEMENT**. 2 L 7 2 4T 4 T RT A31SO E20NE 2007022700090 20070227 00090 EU 2007 2 27 AWXA200700176 1 20070214 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 679AW 4719 4719 2613 LAS - EEL - MX REPORTED EMERGENCY LIGHTS FAILED TEST. MX REPLACED MID LEFT POWER SUPPLY AND BATTERY PER MM 33-51-38 P40 1 AND TASK CARD A1C33302, OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007022700091 20070227 00091 NM 2007 2 27 WRLA2007027 1 20070207 A 5712 ARB2850506 RIB DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE ZONE 600 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 62911 48407 DURING 3C & 12A CHECK, EGAT MECHANIC FOUND CRACK AT RT WING FIXED LE SLAT INTERNAL NO. 16 RIB APPROX 05". REMOVED RT WIN G NR 16 RIB, REPAIRED AREA, WIRE, CLAMP, PULLEY, TRACK AND CABLE PER T/C. REPLACED WITH NEW RIB AT RT WING NR 16 RIB PER MD-11 SRM 51-33-01 VOL II. REV:38. INSTALLED RT WING NR 16 RIB REPAIRED AREA, WIRE CLAMP, PULLEY,TRACK AND CABLE. RIG RT NR 8 SLAT DRIVE CALE & OPERATION TEST SATIS PER AMM 57-80-830~804,REV: 57. 2 L 7 3 4F 4 F RT A22WE E24NE 2007022700104 20070227 00104 NM 2007 2 27 07FDEA00544 1 20070222 A 5710 ARC4125502 RIB DOUG MD11 MD11 3023602 NM ZONE 600 MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 DURING REPLACEMENT OF RIB (P/N ARC4125-502) AT RIGHT HAND WING OUTBOARD FLAP FOUND FASTENER HOLE ON NEW FITTING FLANGE R ADIUS UNABLE TO INSTALL FASTENER. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II ANDFEDEX E.A. 1-5750-88919 PT4, R EPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022700106 20070227 00106 2007 2 27 NWAA070663308 4 20070221 A 2565 7A1539046 SLIDE AIRBUS 330 A330323 3930335 EU R2 DOOR FAULTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 808NW 6597 427 591 DURING TEST OF THE EMERGENCY LIGHT SYSTEM THE ESCAPE SLIDE LIGHT DOOR NR 4 RIGHT FAULTED. TROUBLE SHOT DOWN TO THE ESCA PE SLIDE. REMOVED AND REPLACED ESCAPE SLIDE AND TESTED OK. 2 L 7 2 4F RT A46NM 2007022700107 20070227 00107 NE 2007 2 27 DL76L070147 2 20070222 A 7210 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 MAKING METAL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 191DN 43012 28448 727707 FOUND METAL IN GEARBOX IN NR 2 ENGINE. REPLACING NR 2 ENGINE. T/S PER FIM FOUND PMA BAD ON FURTHER INVESTIGATION FOUND BEARING FAILED REMOVED PM9 DRIVE HOUSING FOUND METAL PARTIC FALLING FROM CASE INTO GEAR BOX ENG SHOP CALLED OUT TO REVI PROBLEM. INSPECTED METAL AND ENG, CHG WILL BE REQUIRED DUE T METAL IN GEARBOX. REMOVED AND REPLACED NR 2 ENG ON R/C 1 -3 1T149. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022700108 20070227 00108 NM 2007 2 27 DL764070149 1 20070223 A 4910 B-NUT BOEING 767 767432ER 1385134 NM GE CF6 CF680 30025 NE PNEUMATIC LINE LOOSE A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 830MH 14876 29701 P1027C APU BLEED UNAVAILABLE AFTER PUSHBACK RTB. FOUND B-NUT ON PNEUMATIC SENSE LINE AT TOP OF APU COMPLETELY BACKED OFF OF TH READS. RETORQUED, MOTORED ENGS 30.1 N2. 40P DURING ROTATION. APU AIR CKS GOOD. 2 L 7 2 4F 4 F RT A1NM E13NE 2007022700109 20070227 00109 NM 2007 2 27 DL76G070151 1 20070224 A 3245 EM91794 VALVE BOEING 767 767332 1382001 NM PARKING BRAKE UNSERVICEABLE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 178DZ 30596 ON PUSHBACK NO PARKING BRAKE LIGHT OR EICAS MESSAGE. ACCUMULATOR PRESSURE DROPS IMMEDIATELY WHEN HYD TURNED OFF. FOUND PARKING BRAKE SHUTOFF VALVE PARTIALLY OPEN. CYCLED MANUALLY AND IT OPS NORMAL. CYCLED PARKING BRAKE GOT ALL MSGS AND LIGHTS. NO HYD LOSS ON BRAKE PRESS. 2 L 7 2 4F RT A1NM 2007022700110 20070227 00110 NM 2007 2 27 DL764070153 1 20070225 A 3350 D71701100 BATTERY BOEING 767 767432ER 1385134 NM EMERGENCY LIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 834MH 29707 FOUND EMERGENCY LIGHTS INOP AFT OF SEAT 41F. REMOVED AND REPLACCED BATTERY PACK AT WL 1790. 2 L 7 2 4F RT A1NM 2007022700111 20070227 00111 NM 2007 2 27 DLM88070154 1 20070225 A 5512 5922578515 SKIN DOUG MD88 MD88 3023688 NM HORIZONTAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 900DE 53372 FOUND HORIZ STAB RT UPPER AFT SKIN PANEL, CRACK REPAIR. THE UPPER AFT SKIN PANEL OF THE RT HORIZONTAL STABILIZER WAS FO UND WITH A 1.5" CRACK AT THE INBD AFT CORNER OF THE PANEL. THE CRACK WAS STOP DRILLED ON A TIME LIMITED BASIS PER ER/A 460327-14. THE DAMAGE WILL BE PERMANENTLY. REPAIRED THROUGH PART REPLACEMENT. 2 L 7 2 4F RT A6WE 2007022700112 20070227 00112 NM 2007 2 27 DLM88070155 1 20070225 A 5512 5922578515 SKIN DOUG MD88 MD88 3023688 NM HORIZONTAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 939DL 49812 HORIZONTAL STABILIZER, RT UPPER AFT SKIN PANEL, CRACK REPAIR. THE UPPER AFT SKIN PANEL ON THE RT HORIZONTAL STABILIZER WAS FOUND WITH A .75" CRACK NEAR THE AFT INBD CORNER OF THE PANEL. THE CRACK WAS HFEC INSPECTED AND STOP DRILLED ON TIM E LIMITED BASIS. THE PERMANENT REPAIR REQUIRES REPLACEMENT OF THE SKIN PANEL. THE REPAIR WAS DOCUMENTED PER ER/A 460308-14, REV A. 2 L 7 2 4F RT A6WE 2007022700113 20070227 00113 NM 2007 2 27 DLM8K070156 1 20070226 A 5512 5922578515 SKIN DOUG MD88 MD88 3023688 NM HORIZONTAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DE 49956 FATIGUE CRACK FOUND IN RT HORIZONTAL STABILIZER UPPER INBOARD SKIN PANEL. SKIN PANEL REPLACED. 2 L 7 2 4F RT A6WE 2007022700114 20070227 00114 2007 2 27 DL76G070157 4 20070226 A 2565 SLIDE BOEING 767 767332 1382001 NM L1 DOOR DISLODGED A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 174DZ 29693 FOUND L1 DOOR MSG WITH DOOR CLOSED. OPERATED DOOR OPEN SLIDE FELL OUT. REINSTALLED SLIDE PER M/M, OPS NML. 2 L 7 2 4F RT A1NM 2007022700119 20070227 00119 SO 2007 2 27 SIMA200705802 1 20070226 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN FAILED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 624AE 11457 38 145111 FOUND EMERGENCY PATH LIGHTS AT ROW 8 THROUGH 12 INOPERATIVE, ALL 4 EMERGENCY OVERWING EXIT SIGNS INOPERATIVE. REMOVED A ND REPLACED NUMBER 3 EMERGENCY LIGHT BATTERY PACK IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SE RVICE. 2 L 7 2 4T RT T00011AT 2007022800002 20070228 00002 EA 2007 2 28 SIMA200705805 1 20070112 A 5320 67053110521 WEB CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 515AE 8208 4042 10121 FOUND WEB AT STATION 280 CORRODED. SPLICED IN NEW WEB AT STATION 280 IAW AMERICAN EAGLE ENGINEERING ORDER CR-53MR-103. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007022800007 20070228 00007 EU 2007 2 28 2007UALA00488 1 20070216 A 2910 HYDRAULIC SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN SYSTEM LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 442UA 780 RTFL UNDER AMBER ALERT DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. A/C WAS TOWED TO GATE. FLUID LOSS DUE TO FAULTY RH MLG D OOR BYPASS VALVE. REPLACED THE DOOR BYPASS VALVE AND NR 1 ENGINE DRIVEN HYDRAULIC PUMP AS A PRECAUTIONARY MEASURE. CHECK ED HYDRAULIC SYSTEM FILTERS AND DID NOT FIND ANY METAL FRAGMENTS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022800008 20070228 00008 NE 2007 2 28 2007UALA00489 2 20070217 A 7200 2607MK2 ACTUATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE MALFUNCTIONED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING A FLAME/FIRE CL CLIMB 1 WP 29 457UA 17768 31 1146 V10007 RTFL DUE TO NR 2 ENGINE SURGE AT TAKEOFF. ENGINE WAS SHUTDOWN. [SUP 05-08-07] VSVA SETTING TRACK CHECK FAULTS ON BOT H CHANNELS SUGGESTING OPERATIONAL PROBLEMS. UNIT HAS BEEN SENT TO OSV FOR INVESTIGATION. UNIT HAS 31 HOURS SINCE SHOP V ISIT AND REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022800009 20070228 00009 NM 2007 2 28 2007UALA00490 1 20070217 A 2130 106120921 RELIEF VALVE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN PRESSURE MALFUNCTIONED A UALA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 330UA 24191 FLIGHT DIVERTED UNDER AMBER ALERT DUE TO CABIN PRESSURE PROBLEM. FOUND INBOARD AND OUTBOARD PRESSURE SAFETY RELIEF VALV ES FAILED. REPLACED PRESSURE SAFETY RELIEF VALVES. [SUP 4-24-07] FOUND OUTBOARD SAFETY VALVE OUT OF LIMITS. REPAIRED AND CALIBRATED. NO FAULT FOUND ON INBOARD SAFETY VALVE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022800010 20070228 00010 EU 2007 2 28 2007UALA00491 1 20070217 A 3260 PROXIMITY SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG OUT OF ADJUST A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 426UA 510 ON TAKEOFF, GEAR DID NOT RETRACT. RED AND GREEN LIGHTS STAYED ON. RECYCLED GEAR & GEAR CAME UP. FAULT TRACED TO OUT OF ADJUSTMENT NOSE LANDING GEAR PROXIMITY SENSOR. PROXIMITY SENSOR BRACKETS, TARGETS AND SPACERS WERE REMOVED FOR INSPEC TION AND THEN REINSTALLED AND ADJUSTED TO PROPER CLEARANCES. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022800011 20070228 00011 NM 2007 2 28 2007UALA00492 1 20070218 A 2710 CONTROL CABLE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU AILERONS MISROUTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 904UA 25004 LT WING AFT AILERON BUS CABLE CONTACTING MLG BEAM APPROX RSS 268 ON OUTBD SIDE OF GEAR BEAM. AILERON CABLES MIS-ROUTED. IMPROPER ROUTING OF CABLES. REROUTED CABLES CORRECLTY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022800012 20070228 00012 2007 2 28 2007UALA00493 4 20070216 A 2565 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU R2 DOOR UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 FOUND DOOR 2R: SLIDE PACK FALLING OUT. REPACKED SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022800013 20070228 00013 2007 2 28 2007UALA00494 4 20070218 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 1L DETACHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 FOUND DOOR 1L SLIDE HAS BECOME DETACHED FROM DOOR. REPLACED SLIDE ASSY 2 L 7 2 4F 4 F RT A2NM E17NE 2007022800014 20070228 00014 2007 2 28 2007UALA00495 4 20070216 A 2565 CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE DOOR 1R & 2R SLI DISCONNECTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 FOUND DOORS 1R AND 2R SLIDE AFT CABLES DISCONNECTED FROM PACK BOARD. DOOR 1R & DOOR 2R SLIDES, AFT CABLES DISCONNECTED FROM PACK BOARD. BY-093796. REINSTALLED CABLES ON BOTH. OK FOR SERVICE. SLIDE PROBLEM ROOT CAUSE: SUSPECT IMPROPERLY C ONNECTED DURING REFURBISHMENT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022800015 20070228 00015 NM 2007 2 28 2007UALA00496 1 20070215 A 3397 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 505UA 24626 FOUND EMERGENCY EXIT SIDE ROW LIGHTS ROW 21 INOPERATIVE. TROUBLESHOT AND FOUND LIGHT ASSY CONNECTOR DISCONNECTED UNDER SEAT. SECURED CONNECTOR. NO COMPONENT REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022800017 20070228 00017 2007 2 28 2007UALA00498 4 20070218 A 2565 GAUGE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU SLIDE OBSTRUCTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 904UA 25004 FOUND MAIN DECK AFT ENTRY DOOR SLIDE PRESS VIEW WINDOW FOGGY, GLAZED. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022800018 20070228 00018 NM 2007 2 28 2007UALA00499 1 20070218 A 5310 DOOR FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 904UA 25004 FOUND FORWARD CARGO DOOR AFT FRAME IS CRACKED AT TWO PLACES AT LOWER STOP FITTING. THE CRACK LOCATIONS ARE AS FOLLOWS: IN RADIUS OF FRAME AT INBOARD CORNER OF STOP FITTING AND ON FORWARD SIDE OF FRAME NEAR UPPER INBOARD CORNER OF STOP FITT ING. FABRICATED AND INSTALLED TWO EXTERNAL NESTED REPAIR ANGLES. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022800019 20070228 00019 NM 2007 2 28 2007UALA00500 1 20070218 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 36 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 FOUND EEL INOP, ROW 36 LT, DOOR 5 LT SLIDE ILLUM AND DOOR 5 RT CROSS AISLE AFT SIDE. REPLACED LIGHT ASSY ALL THREE POSI TIONS. EACH EEL LIGHT OPS. CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022800020 20070228 00020 NM 2007 2 28 2007UALA00501 1 20070218 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 FOUND EMERGENCY LIGHT INOP, UPPER DECK CEILING ROWS 16 AND 17 AND AT CEILING ROW 61 RT. REPLACED LAMPS IN EACH POSITIO N. ALL EEL LIGHTS OPS CHECKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022800021 20070228 00021 NM 2007 2 28 2007UALA00502 1 20070218 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 FOUND EEL INOP RT ROW 35 THRU 44. TROUBLE SHOOTING IDENTIFIED A SHORT TO GROUND IN CABLE. REPAIRED CABLE AND CORRECTED SHORT. EEL LIGHTS CHECKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022800022 20070228 00022 NM 2007 2 28 2007UALA00503 1 20070217 A 3397 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 656UA 25394 FOUND EMERGENCY EEL LIGHTS INOP FROM SEATS 15AB TO 27AB. REPLACED SEVERAL EEL STRIPS & CONNECTION CABLE. OPS CK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022800023 20070228 00023 2007 2 28 2007UALA00504 4 20070217 A 2565 SLIDE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RH OVERWING EXIT UNRELIABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 RT OVERWING EXIT SLIDE, FOUND TO BE UNLACED DURING THE FIRST OPENING OF OVERWING SLIDE DOOR FOR INTEGRATOR TEST. REPLA CED SLIDE. READY FOR SERVICE. SLIDE PROBLEM ROOT CAUSE: SUSPECT IMPROPER CINCHING DURING SLIDE REFURBISHING & REINSTA LLATION AGGRAVATED BY VIBRATION. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022800024 20070228 00024 2007 2 28 2007UALA00505 4 20070217 A 2565 SLIDE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT OVERWING UNRELIABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 FOUND PRESSURE LINE FOR LT OVERWING SLIDE AT BS 1153 IS KINKED AT BEND. REPLACED SLIDE. OK FOR SERVICE. SLIDE PROBLEM ROOT CAUSE: SUSPECT PRESSURE LINE MISROUTED DURING REFURBISHMENT & INSTALLATION RESULTING IN DOWNWARD LOAD ON LINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022800025 20070228 00025 NM 2007 2 28 2007UALA00506 1 20070217 A 3397 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 659UA 27114 FOUND LT 1ST CLASS EEL LIGHTS INOPERATIVE. REPAIRED BROKEN EEL CABLE. OPS CHECKS NORMALLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007030100008 20070301 00008 EA 2007 3 1 TRAX200700249 1 20070219 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 823AS 7196 FLIGHT ATTENDANT FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007030100010 20070301 00010 EA 2007 3 1 TRAX200700251 1 20070219 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 919EV 7780 CAPTAIN'S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007030100013 20070301 00013 NM 2007 3 1 CALA0700084 1 20070223 A 3350 20121 CHARGER BOEING 737 737524 1384721 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17614 27327 THE EMERGENCY EXIT LIGHTS AT SEATS 20-25 WERE FOUND INOPERATIVE. THE CHARGER AND BATTERY PACK WAS REMOVED AND REPLACED, OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2007030100015 20070301 00015 2007 3 1 2007UALA00508 4 20070217 A 2565 PIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE OVERWING SLIDE SHEARED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 659UA 27114 RT OVERWING SLIDE PACK GUIDE PIN FOUND SHEARED WHEN SLIDE WAS REMOVED, AND REQUIRES A NEW INSERT. SUPPLEMENTAL DATA UPD ATE, INSTALLED INSERT IN SLIDE PACK DOOR USING RMS5-28TY7, REF BOAC DRWG 416T2024. INSTALLED GUIDE PIN. AC RETURNED TO SERVICE STATUS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007030100018 20070301 00018 EA 2007 3 1 COMA0760210 1 20070224 A 3250 166550101 CONTROL MODULE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A COMA K NONE J WARNING INDICATION CL CLIMB 1 SO 01 518CA 9605 7816 FLIGHT 5614 - EN ROUTE GSO-ATL RECEIVED A STEERING INOPERATIVE MESSAGE, CREW DECLARED AN EMERGENCY AND LANDED WITHOUT IN CIDENT. REPLACED THE STEERING HAND CONTROL MODULE. 2 L 7 2 4F RT A21EA 2007030100019 20070301 00019 EA 2007 3 1 COMA0760206 1 20070222 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE F FLT CONT AFFECTED CL CLIMB 1 SO 01 739CA 7273 FLIGHT 5446 - FLAPS FAIL AT 0 DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTIO N, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007030100020 20070301 00020 EA 2007 3 1 COMA0760207 1 20070223 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 931CA 7037 FLIGHT 5294 - DURING PIT APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAG E -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007030100025 20070301 00025 NE 2007 3 1 2007UALA00513 2 20070217 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 INOPERATIVE A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 460UA 1248 V10435 NR 1 ENGINE FAILED TO START. VALVE INDICATES OPEN. REPLACED STARTER DUE TO FAILURE. UPON FURTHER TEARDOWN, FOUND THAT THE TURBINE WHEEL BEARING HAD FAILED CAUSING DAMAGE TO THE INLET HOUSING, CAGE, TURBINE WHEEL AND CLUSTER GEARS. THE ST ART VALVE WAS ALSO REPLACED AS A PRECAUTIONARY MEASURE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007030100029 20070301 00029 EA 2007 3 1 COMA0760211 1 20070225 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING OBSTRUCTED A COMA K NONE J WARNING INDICATION CL CLIMB 1 SO 01 719CA 7253 FLIGHT 5174 - EN ROUTE CID-CVG RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOU T INCIDENT. REMOVED ICE BETWEEN THE LEFT AND RIGHT INBOARD FLAP LEADING EDGE AND THE MOVEABLE VANE. 2 L 7 2 4F RT A21EA 2007030100030 20070301 00030 2007 3 1 2007UALA00516 4 20070216 A 2565 B14056916 O-RING BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU ESCAPE SLIDE UNSERVICEABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 925UA 1815 26646 FOUND BOTTLE - LOW PSI. FOUND BAD O-RING. REPLACED BOTTLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007030100031 20070301 00031 2007 3 1 2007UALA00517 4 20070216 A 2565 B14108601B14 O-RING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE BOTTLE UNSERVICEABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 87UA 5687 26713 FOUND LOW BOTTLE. DAMAGED O-RING. REPLACED O-RING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030100035 20070301 00035 NM 2007 3 1 2007UALA00520 1 20070219 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 122UA 29168 FOUND EMERGENCY LIGHT ROW 56 RT INOPERATIVE. RELAMPED ROW 56RH EMERGENCY LIGHT. OP CK NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030100036 20070301 00036 NM 2007 3 1 2007UALA00521 1 20070219 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 122UA 29168 FOUND EMERGENCY LIGHT ROW 26 LT INOPERATIVE. SECURED CONNECTOR. SYSTEM CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030100038 20070301 00038 NM 2007 3 1 2007UALA00523 1 20070217 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SEAT 2E MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 226UA 30226 FOUND SEAT 2E, AISLE EMERGENCY EVACUATION LIGHT (AFT) IS MISSING. REPLACED LIGHT SEGMENT. EEL OP CHECKED OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007030100041 20070301 00041 WP 2007 3 1 UPS07849241 1 20070208 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C3 LEFT FUSELAGE STA 1580 BETWEEN L24L & L25L EXT SKIN HAS DENT WITH GOUGE 6 INCHES LONG 1.5 INCH WIDE A ND APPROX. .100 INCH DEEP. CUT OUT DAMAGED AREA AT STA 1580 BETWEEN L24L & L25L EXTERIOR SKIN IAW SRM 53-2-1 FIG 7. FA BRICATED AND INSTALLED REPAIR DOUBLER AND FILLER, AND FINGER DOUBLER AT STA 1580 BETWEEN L24L & L25L IAW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 2007030100044 20070301 00044 NM 2007 3 1 2007UALA00528 1 20070219 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 127UA 28813 FOUND OVERWING EMERGENCY EXIT LIGHTS INOP, 1ST AND 2ND FROM FWD END. RELAMPED & REPLACED FUSES, OP CHECKED OK 2 L 7 4 4F 4 F RT A20WE E24NE 2007030100046 20070301 00046 NM 2007 3 1 2007UALA00530 1 20070219 A 5753 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT TE FLAP CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 FOUND LT WING INBOARD FLAP UPPER SKIN, OUTBD UPPER CORNER IS CHAFED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALL ED A SINGLE REPAIR DOUBLER AND BONDED DOUBLER. PERFORMED RIG CHECK FLAP TO SPOILER NR 6 CLEARANCE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030100047 20070301 00047 WP 2007 3 1 UPS07849242 1 20070210 A 5313 DC853B00939 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C3 HEAVILY CORRODED LONGERON IN AFT ACC COMPT STA 1570 L34L. REMOVED CORRODED LONGERON SECTION L34L STA 1560-1570 IAW SRM 51-01- 20D, AND SRM 51-01-21-0. FABRICATED AND INSTALLED LONGERON SPLICE SECTION AND NEW END FITTING AT STA 1560-1570 L34L IAW SRM 53-04-01-0, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007030100048 20070301 00048 NM 2007 3 1 2007UALA00531 1 20070219 A 5753 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT TE FLAP DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 FOUND RT WING TRAILING EDGE INBD FLAP, UPPER SURFACE EVEN WITH AFT FLAP, OUTBD END FOUND CHAFED AND GOUGED. MAJOR REPA IR ACCOMPLISHED. REPAIRED FLAP AND BOND INSTALLED DOUBLER. PERFORMED FLAP TO SPOILER CLEARANCE RIG CHECK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030100050 20070301 00050 NM 2007 3 1 2007UALA00533 1 20070219 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1400 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 FOUND AFT PIT STA 1400 AT STR 26L, FRAME UPPER FLANGE DENTED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED A N ESTED J-ANGE L REPAIR THIS REPAIR IS TIME LIMITED FOR 12 MONTHS FROM 13FEB07. THIS REPAIR BECOMES UNAIRWORTHY UNLESS A N EW FAA 8100-9 IS ISSUED PRIOR TO THAT TIME. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030100053 20070301 00053 WP 2007 3 1 UPS07849245 1 20070214 A 5320 BEAM DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C3 CRACK IN RADIUS OF NR 3 J-BEAM, 60 COMPT RBL 2. STOP DRILLED CRACK IN RADIUS OF NR 3 J-BEAM IN THE 6 0 COMPT IAW SRM 53-02-05. FABRICATED AND INSTALLED REPAIR DOUBLER, AND ANGLE IN RADIUS OF THE NR 3 J-BEAM IN THE 60 COM PT IAW SRM 53-02-05-0 AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 2007030100056 20070301 00056 NM 2007 3 1 2007UALA00536 1 20070219 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 500 S0-1R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 FOUND UPPER CROWN AT STA 560, APPROX BETWEEN STR 0 AND 1R, SKIN HAS STATIC DISCHARGE AT FASTENER AND BLENDED OUT OF LIMI TS. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED A REPAIR DOUBLER. THIS REPAIR IS TIME LIMITED FOR 12 MONTHS F ROM 18FEB07. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030100059 20070301 00059 2007 3 1 2007UALA00538 4 20070219 A 3416 ALTIMETER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 557UA 26653 FOUND CAPT'S ALTIMETER INOPERATIVE PER CREW. CYCLED CB AND ALT AIR DATA AND NO HELP. REPLACED NR 1 ALTIMETER 2 L 7 2 4F 4 F RT A2NM E17NE 2007030100061 20070301 00061 NM 2007 3 1 UPS07M49239 1 20070112 A 5730 DOUBLER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C LEFT WING FIXED L/E COMPT CRACKED FOUND ON UPPER DOUBLER PANEL AS MARKED (REFUEL ACCESS 519CB COMPT AR EA). LEFT WING FIXED L/E COMPT UPPER DOUBLER FASTENER REMOVED PER SRM 51-31-01 VOL 2 R.38. REPAIR DOUBLER FILLERS & AN GLES FABRICATED & HOLES DRILLED PER SRM 57-10-00 FIG 258 TEMP R.57-5. VISUAL INSP CARRIED OUT 'OK' TO INSTALL PARTS. R EPAIR PARTS INSTALLED AT LEFT WING FIXED L/E COMPT PER SRM 57-10-00 FIG 258 TEMP R.57-5. FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007030100062 20070301 00062 NM 2007 3 1 UPS07M49251 1 20070225 A 3020 ANTI-ICE VALVE DOUG MD11 MD11F 3023600 NM NR 2 ENGINE INOPERATIVE A IPXA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 250UP 48745 INSPECTION TYPE:N/A ATB - ENG 2 ANTI-ICE OFF - LVL 1 ALERT WITH ANTI-ICE ON. DEFERRED PER MEL M345008. LOCKED NR 2 ENG ANTI-ICE VALVE IN THE OPEN POSITION. REF DMP 30-22-1. ACCOMPLISHED DMP 30-22-1 AND SATISFIED MEL 30-22-1. 2 L 7 3 4F RT A22WE 2007030100064 20070301 00064 NM 2007 3 1 MWEA070036 1 20070223 A 3350 033500110 LIGHT BOEING 717 717200 1383700 NM EXTERIOR INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 916ME 55178 RIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHT. 2 L 7 2 4F TR A6WE 2007030100065 20070301 00065 NM 2007 3 1 2007UALA00539 1 20070219 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 507UA 24743 FOUND ROW 13 OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK AND OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030100066 20070301 00066 NM 2007 3 1 2007UALA00540 1 20070219 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 507UA 24743 FOUND EEL FLOOR LIGHTS INOP AT ROWS 22-16 AND ROW 13 FWD. REMOVED AND REPLACED BATTERY PACK AND CHARGER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030100067 20070301 00067 NM 2007 3 1 2007UALA00541 1 20070219 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ROW 31DEF INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 FOUND ROW 31 DEF BULLNOSE EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT AND OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030100068 20070301 00068 NM 2007 3 1 2007UALA00542 1 20070219 A 3520 DOOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LAV OXYGEN MASK UNRELIABLE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 507UA 24743 FOUND S-LAV OXYGEN MASK DOOR DID NOT OPEN WHEN MASKS WERE DEPLOYED. REPACKED S-LAV O2 MASK. ACCOMPLISHED DROP CHECK T O ASSURE PROPER FUNCTIONALITY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030100070 20070301 00070 NM 2007 3 1 2007UALA00544 1 20070219 A 2150 3F18871509 FILTER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RT PACK DIRTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 341UA 24245 CREW REPORTS MAIN CABIN FLIGHT ATTENDANTS AND PASSENGERS HAVING DIFFICULTY BREATHING AND SNEEZING. SUPPLEMENTAL DATA UP DATE CAUSE: HEPA FILTER. REPLACED RIGHT PACK RECIRCULATION FAN HEPA FILTER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007030100071 20070301 00071 NM 2007 3 1 NOCA04407 1 20070220 A 3350 1317 LIGHT BOEING 767 767* NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 769NA 28039 E-PATH LIGHTING AT SEAT 6AB CEILING LIGHT INOP. REPLACED LIGHT AS PER MM 33-51-00. 2 L 7 2 4F RT A1NM 2007030100074 20070301 00074 NM 2007 3 1 SWAA071103 1 20070224 A 5330 6545766 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 696SW 23064 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED BS 516D, STR 12R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007030100076 20070301 00076 NM 2007 3 1 2007UALA00546 1 20070221 A 5330 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 NR 2 LT MED FWD FRAME CRACKED AT UPPER HINGE CUTOUT. ALSO, EXTERNAL HANDLE DOES NOT STOW AND LATCH IN PAN AUTOMATICALLY . [SUP 4-17-07] MAJOR REPAIR ACCOMPLISHED. REPAIRED DOOR 2L PER A BOEING APPROVED REPAIR SCHEME. BOEING AND UA ENGI NEERING STILL EVALUATING THE CAUSE OF FAILURE. INCORPORATED A PLAN OF INSTALLING A PREVENTIVE STEEL DOUBLER AT UPPER HI NGE CUTOUT AT NEXT HEAVY MAINTENANCE VISITS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030100077 20070301 00077 NM 2007 3 1 SWAA071102 1 20070224 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 762, STR 25R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007030100079 20070301 00079 NM 2007 3 1 SWAA071096 1 20070223 A 5311 6546525 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 9R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030100080 20070301 00080 NM 2007 3 1 2007UALA00548 1 20070220 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE SEAT 20 DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 807UA 798 FOUND EEL PATH LIGHTING DAMAGED AT SEAT 20. REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007030100081 20070301 00081 NM 2007 3 1 SWAA071097 1 20070223 A 5311 6546534 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 9R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030100084 20070301 00084 NM 2007 3 1 2007UALA00551 1 20070221 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN MISSING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 FOUND CABIN EMERGENCY LIGHT NOT ON AT (54H) AND LIGHTS MISSING AT (32A & 1J). REPLACED WITH NEW EMERGENCY LIGHTS IN ALL THREE POSITIONS. ALL POSITIONS OP CHKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030100087 20070301 00087 NM 2007 3 1 SWAA071093 1 20070223 A 5311 6546552 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 9R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030100088 20070301 00088 NM 2007 3 1 2007UALA00553 1 20070221 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 FOUND EMERGENCY CEILING LIGHT INOP UPPER DECK ABOVE STAIRS. RELAMPED CEILING EEL. OP CHECKED GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030100091 20070301 00091 NM 2007 3 1 2007UALA00554 1 20070221 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 FOUND EEL INOPERATIVE AT DOOR 4L GALLEY SIDEWALL. REPAIRED SHORTED CONNECTOR TO RESTORE EEL AT 53 ABC. OP CHECKED OK FO R SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030100092 20070301 00092 NM 2007 3 1 2007UALA00555 1 20070221 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROWS 46-54 LT SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 FOUND EEL INOPERATIVE, CONNECTOR SHORTED ROWS 46-54 LT. REPAIRED SHORTED CONNECTOR AT EEL ROW 53. SYSTEM OP CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030100093 20070301 00093 NM 2007 3 1 2007UALA00556 1 20070221 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 FOUND EEL INOPERATIVE AT DOOR 5L XAISLE. REPLACED FEEDER TO LT CROSS AISLE EEL AT DOOR 5L. OP CHECKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030100094 20070301 00094 NM 2007 3 1 2007UALA00557 1 20070221 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 FOUND EMERGENCY LIGHT INOPERATIVE AT DOOR 4R AFT SILL. RELAMPED EEL AT DOOR 4R. OP CHECKED GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030100095 20070301 00095 NM 2007 3 1 2007UALA00558 1 20070221 A 3397 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 576UA 26690 FOUND EEL LIGHTS INOP IN FWD CABIN FROM ROW 1-6. REPLACED EEL CABLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030100096 20070301 00096 2007 3 1 2007UALA00559 4 20070220 A 2565 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L3 DOOR OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 FOUND DOOR 3L HARD TO DISARM. SECURED LOWER LINER AND ADJUSTED SLIDE GIRT. OPS CHECKS OK. ACCOMPLISHED INSPECTION, D OOR ARMS AND DISARMS NORMALLY. SECURED LOWER LINER AND ADJUSTED SLIDE GIRT BAR. NO COMPONENTS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030100097 20070301 00097 NM 2007 3 1 SWAA071101 1 20070224 A 5743 6552235 FITTING BOEING 737 7373H4 1384600 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND LT MLG SUPPORT BEAM FWD STABILIZER FITTING CORRODED. REMOVED AND REPLACED STABILIZER FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007030100098 20070301 00098 NM 2007 3 1 SWAA071104 1 20070225 A 2560 6557463 FITTING BOEING 737 7377H4 1384404 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 776WN 30591 L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED GIRT BAR FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007030100100 20070301 00100 NM 2007 3 1 SWAA071099 1 20070224 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030100102 20070301 00102 NM 2007 3 1 SWAA071092 1 20070223 A 5311 65C34356 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 9R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030100104 20070301 00104 NM 2007 3 1 2007UALA00560 1 20070220 A 3397 CONNECTOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 226UA 30226 FOUND SEAT 3F AISLE EEL LIGHT INOPERATIVE, CONNECTOR DISCONNECTED. RECONNECTED CONNECTOR UNDER THE SEAT AND OP CHECKE D OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007030100105 20070301 00105 NM 2007 3 1 SWAA071106 1 20070225 A 3350 810022607 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 413WN 29819 DURING SCHEDULED MV2 CHECK, FOUND LT AFT CABIN EEPLS INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007030100106 20070301 00106 NE 2007 3 1 2007UALA00561 2 20070222 A 7200 ENGINE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 FAULTED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 823UA 952 V11298 RTFL DUE TO MULTIPLE NR 2 ENGINE FAULTS. [SUP 05-16-07] COMPOUNDING FAULTS DUE TO A FAULTY ENGINE INTERFACE UNIT. NR 2 ENGINE EIU WAS REPLACED. UPON FURTHER TEARDOWN AND INSPECTION, EIU MOTHERBOARD WAS FOUND TO BE FAULTY. PRESSURIZATION S YSTEM, PACKS AND AUTO THROTTLES CHECKED OK AND NO REVERSER INDICATIONS WERE NOTED DURING ENGINE TEST RUN. 2 L 7 2 4F 4 F RT A28NM E40NE 2007030100107 20070301 00107 NM 2007 3 1 2007UALA00562 1 20070221 A 5414 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 NACELLE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 NR 2 NACELLE STRUT SIDE SKIN OUTBOARD FORWARD ACCESS DOOR CUT-OUT HAS A CRACK INDICATION, INSIDE OF CUT-OUT, CRACK ENDS MARKED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED & INSTALLED 3 EACH DOUBLERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030100109 20070301 00109 NM 2007 3 1 2007UALA00563 1 20070222 A 3350 LIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 942UA 26679 FOUND EEL STRIP INOP AT FWD GALLEY CART STOWAGE. REPAIRED POWER CABLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007030100112 20070301 00112 NM 2007 3 1 SWAA071086 1 20070222 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 261WN 32517 LEFT FWD CABIN EMERGENCY BATTERY INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007030100114 20070301 00114 2007 3 1 2007UALA00567 4 20070221 A 2565 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE DOOR 1L UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 127UA 28813 FOUND DOOR 1L EMERGENCY EXIT SLIDE COMING UNPACKED. REPLACED SLIDE. OK FOR SERVICE. SLIDE PROBLEM ROOT CAUSE; SUSPE CT INADEQUATE BINDING OF SLIDE CAUSED BY IMPROPER REFURBISHMENT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030100116 20070301 00116 NM 2007 3 1 SWAA071089 1 20070223 A 3350 MS155721 LIGHT BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED A1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007030100117 20070301 00117 2007 3 1 UIEA200700068 4 20070205 A 3416 A4289910016 ALTIMETER BOEING 747 7472D7B 1384803 NM COCKPIT FAULTY A UIEA O OTHER O OTHER CR CRUISE 1 EA 15 528MC 22472 CAPT ALT UNRESPONSIVE TO ALL CHANGE BOTH CADC/STBY MODES, PERFORMED CHECK DIFFERENCE BETWEEN ALT INDICATORS (3,34,7), CH ANGE ALT LAGS IN DESCENT BY OVER 300' AND DIFFERS BY OVER 180' AT EL 290-310-MACH .84. T/S AND FOUND PIN NR 22 AT PLUG DN 101. CAPT ALT INDICATOR WIRE BROKEN, REPAIRED WIRING PER WDM 34-12-12. ALSO, R/R WITH NEW CAP ALT INDICATOR AS PREC AUTIONARY AS PER MM 34-13-04. PERFORMED PRIMARY ALT TEST AS PER AMM 34-13-04, ALL OPS CHECK NORMAL. 2 L 7 4 4F RT A20WE 2007030100119 20070301 00119 NM 2007 3 1 UIEA200700092 1 20070226 A 2150 3206257 RELIEF VALVE BOEING 747 7472D7B 1384803 NM A/C PACK FAILED A UIEA O OTHER J WARNING INDICATION CL CLIMB 1 EA 15 523MC 21782 DURING PASSING 3000' WHEN PACKS WERE TURNED ON DUCT PRESS LOW LIGHT ILLUMINATED. DUCT PRESS 9 PSI. ENGINE BLEED VALVES 2, 3 AND 4 OPEN. REMOVED AND REPLACED NR 4 PRESS RELIEF VALVE. LEAK CHECKED COMPLIED WITH, NO DEFECTS AT THIS TIME RE F AMM 71-00-00. 2 L 7 4 4F RT A20WE 2007022600034 20070226 00034 WP 2007 2 26 DXTA200701954 2 20070218 A 7200 ENGINE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP RIGHT UNKNOWN E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 895QS 258606 ABORTED TAKEOFF AT APPROXIMATLEY 40 KTS, DUE TO RED FLASHING INDICATOR WITH 105 PERCENT N1 ON RT ENGINE MAX KIAS INDIC ATED 60 KNTS DURING ABORT TAKEOFF TAXIED TO FBO. DOWNLOADED DEEC'S & FORWARDED TO HONEYWELL, RECORDED LIVE ENGINE DATA & FWD TO HONEYWELL, NO DEFECTS NOTED. OHMED OUT N1 MONOPOLE, NO DEFECTS NOTED. NO DEFECTS NOTED IAW HAWKER 800XP MM 31-4 1-05. 2 L 7 2 4F 4 F RT A3EU E6WE 2007022600160 20070226 00160 EA 2007 2 26 VNAA0702006 1 20070207 A 3213 STRUT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NLG DISCHARGED A VNAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 05 202PS 7858 CREW REPORTED A GEAR DISAGREE MESSAGE AFTER TAKEOFF. CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT IN DAY. MAINTEN ANCE INSPECTED AND SERVICED THE NOSE LANDING GEAR SHOCK STRUT OIL AND NITROGEN IAW THE AIRCRAFT MAINTENANCE MANUAL. MAI NTENANCE ALSO PERFORMED OPERATIONAL TESTS. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007022600050 20070226 00050 NM 2007 2 26 SWAA071077 1 20070222 A 5753 65464301903 SKIN BOEING 737 7373H4 1384600 NM RT WING FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING INBOARD FORE FLAP UPPER OUTBOARD SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007022600051 20070226 00051 NM 2007 2 26 SWAA071080 1 20070222 A 5753 6546435335 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED C2 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT LOWER INBOARD END. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007022600052 20070226 00052 NM 2007 2 26 SWAA071082 1 20070222 A 5322 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM BS 500A S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500A, STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007022600053 20070226 00053 NM 2007 2 26 SWAA071083 1 20070222 A 5311 6546532 FRAME BOEING 737 7375H4 138449D NM BS 480 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 9L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007022600054 20070226 00054 NM 2007 2 26 SWAA071084 1 20070222 A 5311 6546536 FRAME BOEING 737 7375H4 138449D NM BS 559 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 9L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007022600055 20070226 00055 NM 2007 2 26 SWAA071085 1 20070222 A 5311 6546552 FRAME BOEING 737 7375H4 138449D NM BS 827 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 9L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007022600056 20070226 00056 NM 2007 2 26 SWAA071076 1 20070222 A 5754 65C26602312A SKIN BOEING 737 7373H4 1384600 NM NR 5 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT T/E WEDGE UPPER SURFACE DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 2007022600057 20070226 00057 CE 2007 2 26 RU3A0701 1 20070215 A 3260 444EN496 SQUAT SWITCH BEECH 300 300BEECH 1152930 CE RT MLG DEFECTIVE E RU3A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 15 74 FF9 LANDING GEAR HANDLE CANNOT BE RAISED INFLIGHT WITHOUT USING DOWNLOCK RELEASE. REPLACED SWITCH ON RT MAIN SCISSORS. 2 L 7 2 4T A24CE 2007022600058 20070226 00058 NM 2007 2 26 QXEA200700242 1 20070221 A 5270 DOOR BOMBDR DHC8 DHC8402 1390042 NM MAIN PAX UNKNOWN A QXEA O OTHER N FALSE WARNING DE DESCENT 1 NM 09 418QX 4143 BOI FLIGHT NR 2320: UPON DESCENT, RECEIVED FUSELAGE DOOR WARNING ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTE NANCE PERFORMED GVI OF AFT PAX DOOR HANDLE LOCKS AND DOOR CLOSE SWITCH WITH NO DEFECTS NOTED. INTEROGATED PSEU FOR DOO R LOCK AND HANDLE FAULTS. NO FAULTS WERE NOTED. OPEN AND CLOSED DOOR MULITIPLE TIMES AND COULD NOT DUPLICATE DOOR WARN ING LIGHT. LUBED DOOR CLOSED SWITCH. CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007022600177 20070226 00177 NM 2007 2 26 AWXA200700250 1 20070126 A 5310 654580761 DOOR FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND R1 DOOR CUT OUT LOWER FORWARD STUB FRAME CRACKED, BS 312, RBL 65, WL 208.5. REPLACED R1 DOOR CUT OUT LOWER FORWARD STUB FRAME CRACKED, BS 312, RBL 65, WL 208.5 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007022600183 20070226 00183 NM 2007 2 26 AWXA200700256 1 20070125 A 5320 66142081 INTERCOSTAL BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND INTERCOSTAL CRACKED, BS 294.5, S11L. REPLACED INTERCOSTAL BS 294.5, S11L IAW AWA ER 03-5312-07051-SS1. 2 L 7 2 4F RT A16WE 2007022700002 20070227 00002 WP 2007 2 27 IXXA07SMN082S 1 20070131 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER FORWARD SKIN CORRODED AT STATION XFS410.250. REMOVED FASTENER S AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND DAMAGE OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAI R DOUBLER AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLE D REPAIR PARTS AND NEW FASTENERS IAW DC8 SRM 57-2-1 FIGURES 16 AND 38 PAGE 2 TR NUMBER57-85 DATED 11-22-2000, DC8 SRM 51 -1-8 PAGES 17 AND 18, DC8 SRM 57-2-1 FIGURE 2G, DC8 SRM 57-2-1 FIGURE 38, DC8 SRM 57-3-1 FIG 4 ITEM "A", DC8 SRM 51-1-8B , DC8 SRM 51-1-11, DC8 SRM 57-2-1 FIG 38 DC8 SRM 51-1-21, DC8 SRM 51-1-20D AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007022700003 20070227 00003 NM 2007 2 27 DHL2007781007 1 20070226 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM BS 480-690 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 781DH 21996 FOUND RT CABIN, SEVERAL AREAS OF CORROSION ON SEAT TRACK AT BS 500-600, RBL 24. REMOVED DAMAGED SEAT TRACK SECTIONS, BS 480-690. FABRICATED 2 NEW SEAT TRACK SECTIONS, 1 AT BS 480-610, AND 2 AT 610-690, FROM BAC1520-792, PO NR 9003797, 128 .5" AND 80" LONG, PER B727 SRM 53-10-5 FIG 1. FABRICATED REPAIR ANGLES FROM BAC1503-10122, PO NR 9004539, 4 AT 15" LON G, AND 2 STRAPS FROM 7075-T6, .250" BY 8" BY 2", PO NR 9003467, PER B727 SRM 53-10-5 FIG 1. TREATED, PRIMED, AND INSTAL LED REPAIR PARTS/SEAT TRACK PER B727 SRM 51-10-2 AND 53-10-5 FIG 1. 2 L 7 3 4F A3WE 2007022700019 20070227 00019 WP 2007 2 27 UPS07849227 1 20070104 A 5330 561537271N1 SKIN DOUG DC8 DC871F 302199D WP FS 1350-1490 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 HFEC & VISUAL INSP DETECTED A .225 INCH CRACK ON THE C-4 (D-PIT) LOWER FORWARD JAMB CORNER AS MARKED ON PART. REMOVED AND REPLACED FUSELAGE SKIN IAW SRM 51-1-20D, 51-1-21, 51-1-22, FS 1350 - 1490 L31R - L31L. 2 L 7 4 4F RT 4A25 2007022700024 20070227 00024 NM 2007 2 27 SCNA07003 1 20070223 A 3350 LIGHT BOEING 737 737800* NM CABIN BROKEN A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 PHHZG 28379 CREW REPORTED 11-C EMERGENCY LIGHTING STRIP BROKEN. MAINTENANCE RESECURED LIGHT STRIP. OPS CHECKS OK. 2 L 7 2 4F RT A16WE 2007022700027 20070227 00027 SO 2007 2 27 FDKA200702078 1 20070221 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN UNKNOWN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 838MJ 145384 FDM 6096 MCO-RDU (1619 PHX LCL), EMERGENCY LIGHT INOPERATIVE ABOVE ROW 12. MX OPS CHECKED THE LIGHT AND FOUND NO DEFECT S. 2 L 7 2 4T RT T00011AT 2007022700038 20070227 00038 NM 2007 2 27 AWXA200700260 1 20070216 A 5315 654583471 STRAP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND FLOORBEAM STABILIZER STRAP CRACKED, BS 328, LBL 45.5, WL 208. REPAIRED FLOORBEAM STABILIZER STRAP, BS 328, LBL 45.5, WL 208 IAW B737-300 SRM 53-10-51-2R4. 2 L 7 2 4F RT A16WE 2007022700056 20070227 00056 NM 2007 2 27 ASAA0771483 1 20070223 A 5320 143A524010 SUPPORT ANGLE BOEING 737 737790 13844CN NM BS 540 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 CABIN FLOOR SUPPORT ANGLE IS CRACKED AT FS 540. REPAIRED IAW ASA EA 5320 01790. 2 L 7 2 4F RT A16WE 2007022700061 20070227 00061 NM 2007 2 27 SB07019 1 20070226 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM EMERGENCY LIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 24811 PHL MAINTENANCE REPORTED THE FORWARD SERVICE DOOR LOWER EMERGENCY EXIT SIGN ALONG WITH THE ONE ABOVE THE DOOR WERE INOPE RATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007022700063 20070227 00063 NM 2007 2 27 07FDEA00546 1 20070224 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1521-1528 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 MAIN DECK CARGO, FLOOR SEAT TRACK FOUND CORROSION AT STA 1521-1528, X=8.5. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53- 70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022700092 20070227 00092 NM 2007 2 27 WRLA2007028 1 20070207 A 5712 ARB2850505 RIB DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 62911 48407 DURING 3C &12A CHECK, EGAT MECHANIC FOUND CRACK AT L/H WING FIXED L/E SLAT INTERNAL NO. 16 RIB APPROX 05". REMOVED LT W ING NR 16 RIB & REPAIRED AREA, WIRE, CLAMP, PULLEY, TRACK AND CABLE PER NR 0028049, ITEM 1&2. REPLACED WITH NEW RIB AT L T WING NR 16 RIB PER MD-11 SRM 51-33-01 VOL II. REV:38. 3. INSTALLED LT WING NR 16 RIB REPAIRED AREA, WIRE CLAMP, PULLEY ,TRACK AND CABLE PER NR 0028049 ITEM 3&4. RIG LT NR 8 SLAT DRIVE CALE & OPERATION TEST SATIS PER AMM 57-80-830~804,REV:5 7. 2 L 7 3 4F 4 F RT A22WE E24NE 2007022700093 20070227 00093 NM 2007 2 27 WRLA2007029 1 20070208 A 5245 STRUCTURE DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE A/C DOOR CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 62911 48407 DURING 3C & 12A CHECK, EGAT MECHANIC FOUND CRACK AT NR 3 AIR CONDITION COMPARTMENT DOOR UPPER SIDE CRACK 3". PERFORM NR 3 AIR CONDITION DOOR SKIN CRACK AREA REPAIR PER MD-11 SRM VOL 1 52-10-00 FIG.1 REV:38. CONDITION CHECK NORMAL AND JOB COMPLETED. 2 L 7 3 4F 4 F RT A22WE E24NE 2007022700094 20070227 00094 WP 2007 2 27 IXXA07SMN064S 1 20070131 A 5753 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION FOUND RIGHT HAND UPPER OUTBOARD FLAP HAS A NON STANDARD REPAIR AT STATION XF210.000. R EMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN AS NEE DED. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN. IAW DC8 SRM 57-7-1 FIGURE 4 TR NUMBER 57-94 DATED 10-01-02, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-7-1 FIGURE 4 ITEM "C", DC8 SRM 51-1-8B, DC8 SRM 51-1-11 AND DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007022700095 20070227 00095 SO 2007 2 27 SIMA200705004 1 20070218 A 2770 SYLC53058 GUST LOCK EMB 135 EMB135LR 3260305 SO RUDDER FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 21 725AE 14716 145312 GUST LOCK LIGHT ILLUMINATED AT ROTATION - NOTICED CIRCUIT BREAKER 24 POPPED - RESET WITH NO EFFECT TO SYSTEM - DIVERTED TO IAD - EMERGENCY DECLARED. C/A - REMOVED AND REPLACED GUST LOCK ACTUATOR IAW EMB AMM 27-71-01 AND READJUSTED SPRING CA RTRIDGE IAW EMB AMM 27-71-14. PERFORMED OPERATIONAL CHECK IAW EMB ACC 27-70-700-802-A. RETURNED AIRCRAFT TO SERVICE 2 L 7 2 4F RT T00011AT 2007022700096 20070227 00096 CE 2007 2 27 DJFA2007021 1 20070219 A 7160 INTAKE BEECH MU300 400A 1155402 CE ENGINE CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 465LX RK454 DURING A SCHEDULED MAINTENANCE EVENT MAINTENANCE FOUND A CRACK ON THE ENGINE INLET RING AT THE 12 OCLOCK POSITION. THE CRACK WAS APPROX .67 INCH LONG AND TRANSECTED THE SCREW HOLE FROM THE AFT EDGE OF THE RING. MAINTENANCE IS REPLACING TH E INLET RING. THE SDR WILL BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION. 2 H 7 2 4F RT A16SW 2007022700097 20070227 00097 2007 2 27 WRLA2007040 4 20070222 A 2565 AWD9830507 SLIDE DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE CABIN UNWANTED DEPLOY A WRLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 11 275 48631 R1 SLIDE WAS INADVERTANTLY DEPLOYED, THE DEPLOYMENT WAS UNSUCCESSFUL. REMOVED DEPLOYED SLIDE, REARMED DOOR, REARMED EMER GENCY BOTTLE, REFILLED EMERGENCY DOOR BOTTLE TO NORMAL WORKING PRESSURE OPS CHECK ALL NORMAL. DEFERRED R1 DOOR SLIDE PER MEL 52-10-03 TO DMI M52FE2307-97 CAT "C". 02/24/07 REPLACED R1 DOOR SLIDE ASSEMBLY PER MM 25-61-15 AND ACCOMPLISHED RII , ALL OPS CHECK NORMAL. 2 L 7 3 4F 4 F RT A22WE E24NE 2007022700100 20070227 00100 NE 2007 2 27 RYNA200700002 2 20070215 A 7261 CFM563C1 ENGINE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 OIL CONSUMPTION A RYNA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 07 672RY 42954 5093 24672 724640 DURING CRUISE OIL QUANITY NR 1 ENGINE FELL TO 8, OIL PRESSURE FELL TO 30 PISG OIL TEMP STAYED AT 95. REMOVED AND REPLAC ED ENGINE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007022700101 20070227 00101 EU 2007 2 27 MALA070029 1 20070220 A 3260 CONTROL UNIT SAAB SF340 340B 7860101 EU MLG MALFUNCTIONED A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 449XJ 340B449 WHEN THE LANDING GEAR IS SELECTED UP, THE INTRANSIT LIGHT DOES NOT ILLUMINATE. TESTED TRANSIT LIGHT WHILE GEAR WAS UP AN D LIGHT BULB WORKS. REPLACED LANDING GEAR CONTROL UNIT WITH SERVICEABLE UNIT, P/N OFF AND ON: D494-12-001, S/N OFF: 614/ 091-96, S/N ON: 645/09-97. OPS CKS GOOD. DONE PER SAAB AMM 32-31-05-02 & 32-30-00-05. 2 L 7 2 4T RT A52EU 2007022700102 20070227 00102 NM 2007 2 27 07FDEA00542 1 20070222 A 5710 ARC050312 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK ATTACHMENT BARREL NUT BORE FOUND CORRODED. REPAIRE D AS PER FEDEX E.A. 1-5750-107782, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022700103 20070227 00103 NM 2007 2 27 07FDEA00543 1 20070222 A 5710 ARC050312 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. REPAIRED AS PE R FEDEX E.A. 1-5750-107782, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007030100001 20070301 00001 NM 2007 3 1 ABXA070050 1 20070222 A 3260 LIGHT BOEING 767 767205 1385121 NM COCKPIT SHORTED A ABXA O OTHER N FALSE WARNING LD LANDING 1 GL 23 713AX 23058 AFTER LANDING, WHEN TURNING OFF 22R ONTO A3 TAXIWAY, STA ILN, THE WHEEL WELL FIRE WARNING LIGHT CAME ON ALONG WITH MASTE R WARNING LIGHT. EMERGENCY DECLARED. SHUT DOWN AIRCRAFT ON A3 AND EVACUATED AIRCRAFT. DEPLOYED SLIDE FOR EVACUATION. VERIFIED PROBLEM. FOUND RIGHT GEAR DOWNLOCK GREEN LIGHT ASSEMBLY SHORTED IN IT'S SOCKET, CAUSING A SHORT TO GROUND AND ILLUMINATING MASTER WARNING WHEEL WELL FIRE AND OTHER LIGHTS. REPLACED RIGHT GEAR DOWNLOCK LIGHT ASSEMBLY IAW B767 AMM CH 33. OPS CHECKED GOOD. REPLACED/INSTALLED SLIDE ASSEMBLY IAW B767 AMM 25-66-01. SLIDE REMOVED - P/N: 101623-303, S /N: PB0422. 2 L 7 2 4F RT A1NM 2007030100004 20070301 00004 NM 2007 3 1 ABXA070049 1 20070219 A 2750 285T004953 FSEU BOEING 767 767281 1385109 NM T/E FLAP DEFECTIVE A ABXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 784AX 3091 23017 A 27 51 12 00 STATUS MSG; FLAP/SLAT ELEC FLAP INDICATOR INDICATES 1 WITH FLAP LEVER IN UP POSITION. REPLACED FSEU IAW B 767 MM 27-51-01. 2 L 7 2 4F RT A1NM 2007030100005 20070301 00005 NM 2007 3 1 ASAA0741481 1 20070220 A 2150 2205170 A/C PACK BOEING 737 7374Q8 138447Q NM A/C BAY LEAKING A ASAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 NM 02 779AS 45532 1796 25111 SMOKE IN CABIN ON TAKEOFF OUT OF ADQ. REMOVED AND REPLACED LEFT PACK ACM PER AMM 21-51-11. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A16WE 2007030100023 20070301 00023 NM 2007 3 1 2007UALA00511 1 20070218 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE 2E AFT SEAT SIDE MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 225UA 30554 FOUND 2E AFT SEAT SIDE MOUNT EMERGENCY PATH MARKING LIGHT MISSING. REPLACED LIGHT, OP CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007030100024 20070301 00024 NM 2007 3 1 2007UALA00512 1 20070216 A 3350 SWITCH AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 854UA 1731 FOUND EMERGENCY EEL LIGHTS (NO SMOKING) FLASH ON AND OFF. [5-1-07] CYCLED NO SMOKING SWITCH EEL LIGHTS OPS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007030100028 20070301 00028 2007 3 1 2007UALA00515 4 20070218 A 2565 BOTTLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE DOOR 1L SLIDE UNDERSERVICED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 830UA 1243 FOUND DOOR 1L SLIDE BOTTLE PRESSURE LOW. REPLACED DOOR 1L SLIDE PACK. SHOP EVALUATION FOUND NOTHING WRONG WITH PACK AND ATTRIBUTED LOW PRESSURE READING TO UNIT AGE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007030100040 20070301 00040 NM 2007 3 1 2007UALA00525 1 20070218 A 3350 LAMP AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 839UA 1507 FOUND SEAT 6C AISLE EMERGENCY LIGHT INOPERATIVE. [5-1-07] RELAMPED, GROUND CHECKS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007030100043 20070301 00043 NM 2007 3 1 2007UALA00527 1 20070219 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 127UA 28813 FOUND EEL INOP AT AFT OF DOOR 1L AT CLOSET. RELAMPED, OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030100049 20070301 00049 NM 2007 3 1 2007UALA00532 1 20070219 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1440 S25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 FOUND AFT PIT STA 1440 BELOW STR 25L, FRAME DENTED. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME WITH A PRODUCTION SPLICE REPAIR ANGLE. THIS REPAIR IS TIME LIMITED FOR 12 MONTHS FROM 13FEB07. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030100054 20070301 00054 WP 2007 3 1 UPS07849249 1 20070214 A 5320 WEB DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C3 CABIN STA 3.0 RBL 45 SUBFLOOR WEB IS CRACKED. STOP DRILLED CRACK ON WEB AT STA 3.0 RBL 45 IAW SRM 53 -2-00 FIG 001B. FABRICATED AND INSTALLED REPAIR DOUBLER AT SUBFLOOR STA 3.0 RBL 45 IAW SRM 53-02-00-0 FIG 001D, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007030100075 20070301 00075 NM 2007 3 1 2007UALA00545 1 20070220 A 5344 HINGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE PAX DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 NR 2 RT MED UPPER HINGE CUTOUT IS CRACKED ON DOOR FRAME. [SUP 4-17-07] REPAIRED DOOR 2R PER A BOEING APPROVED REPAIR S CHEME. BOEING AND UA ENGINEERING STILL EVALUATING THE CAUSE OF FAILURE. INCORPORATED A PLAN OF INSTALLING A PREVENTIVE STEEL DOUBLER AT UPPER HINGE CUTOUT AT NEXT HEAVY MAINTENANCE VISITS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030100083 20070301 00083 NM 2007 3 1 2007UALA00550 1 20070221 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 FOUND EEL 2A FWD, EEL 1J AFT AND EEL 4J FWD ARE INOPERATIVE. REPLACED LIGHT ASSY IN EACH POSITION. OP CHECKED OK FOR S ERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030100085 20070301 00085 NM 2007 3 1 SWAA071094 1 20070223 A 5311 6546548 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030100099 20070301 00099 NM 2007 3 1 SWAA071090 1 20070223 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM L1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIR T BAR FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007030100101 20070301 00101 NM 2007 3 1 SWAA071091 1 20070223 A 5311 65C34355 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 9R AND STR 9L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030100110 20070301 00110 NM 2007 3 1 2007UALA00564 1 20070222 A 3397 FEEDER CABLE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 942UA 26679 FOUND EEL STRIP INOP AT AFT GALLEY CART STOWAGE. REPAIRED POWER FEEDER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007030100124 20070301 00124 NM 2007 3 1 UIEA200700087 1 20070225 A 5330 65B041072 SKIN BOEING 747 7472D3B 1384805 NM BS 570 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 FUSELAGE SKIN BS 570 EQUIPMENT COOLING OUTLET FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER SB747-53-2386 FIG 5 AND 10. 2 L 7 4 4F RT A20WE 2007030100126 20070301 00126 EU 2007 3 1 200702221 1 20070216 A 2913 5116403 PUMP EMB ERJ170 ERJ170100SE 3260406 EU HYDRAULIC SYS LEAKING A UHLA O OTHER K FLUID LOSS AP APPROACH 1 GL 17 644RW 17000061 FLIGHT 7707 IAD TO IAH ON DESCENT A -HYD 1 LO QTY- MESSAGE WAS ANNUNCIATED ON THE EICAS. CREW NOTED THE FLUID IN THE NR 1 SYSTEM WAS AT 16 PERCENT, AND DECREASING BY 2 PERCENT EVERY 3-4 MINUTES. CREW RAN QRH PROCEDURE. LANDING AND TAXI T O THE GATE WERE UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED NR 1 EDP. 2 L 7 2 4F RT A56NM 2007030100128 20070301 00128 NM 2007 3 1 UIEA200700076 1 20070221 A 5330 SKIN BOEING 747 7472D3B 1384805 NM BS 2310 S38-40L SCRATCHED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 FOUND FUSELAGE SKIN SCRATCH FOUND AT BS 2310, S38L-S40L. SCRATCH SLIGHTLY SMOOTHED AND PROTECTED AS PER SRM 51-10-02. 2 L 7 4 4F RT A20WE 2007030100130 20070301 00130 NM 2007 3 1 UIEA200700078 1 20070221 A 5410 BLOWOUT DOOR BOEING 747 7472D3B 1384805 NM GE CF6 CF680 30025 NE NR 1 NACELLE CHAFED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 ENGINE NR 1 AND NR 2, RT C-DUCT BLOW OUT DOOR ASSEMBLY HAS MISSING MATERIAL AND CHAFE MARKED. REPAIRED ACCOMPLISHED AS PER EO NR 4778A093 AND FAA FORM 8110-3. 2 L 7 4 4F 4 F RT A20WE E13NE 2007030100131 20070301 00131 NM 2007 3 1 UIEA200700086 1 20070225 A 7120 MOUNT BOEING 747 7472D3B 1384805 NM NR 4 ENGINE DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 NR 4 PYLON FWD ENGINE MOUNT FITTING BOTH I/B AND O/B LUG BORE HOLES FOUND OVERSIZED. REPAIRED ACCOMPLISHED AS PER BOEIN G SR ID NR 1-290193672-1 THRU -3 AND FAA FORM 8100-9. 2 L 7 4 4F RT A20WE 2007030100133 20070301 00133 NM 2007 3 1 AWXA200700279 1 20070225 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHT FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 820AW 22975 2762 1397 ATL - EEL - FOUND EMERGENCY POWER SUPPLY UNIT FWD LEFT INOP. MX REMOVED AND REPLACED EPSU AND BATTERY IAW REF AMM 33-51 -38-000-001, 33-51-38-400-001 AND 33-51-38-400-2, OPERATIONAL CHECK WAS NORMAL. 2 L 7 2 4F RT A28NM 2007030100134 20070301 00134 NM 2007 3 1 AWXA200700280 1 20070223 A 3350 321431 BATTERY AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 808AW 1088 PHX - EEL - FOUND EMERGENCY EXIT" PUSH BUTTON" TEST FAULTING "EPSU UNIT EMER R ". MX REMOVED AND REPLACED THE BATTERY I AW 33-51-38. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007030100135 20070301 00135 2007 3 1 NWAA070643224 4 20070224 A 2210 B397CAM0101 COMPUTER AIRBUS 320 A320211 3930320 EU NR 1 FAC MALFUNCTIONED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 324US 36047 37 273 AT CRUISE, FLIGHT LEVEL 340, FAC 1 FAIL LIGHT ECAM MESSAGE ANNUNCIATED. COMPLIED WITH COM PROCEDURE, BURNED INSULATION ODOR NOTED ON FLIGHT DECK, 1ST CLASS. ODOR DISSIPATED WITH FAC TURNED OFF, CIRCUIT BREAKER PULLED. FLIGHT DIVERTED TO MIA. AIRCRAFT LANDED AND TAXIED TO GATE UNEVENTFULLY. CORRECTED BY REPLACING NR 1 FAC COMPUTER. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 2007030100138 20070301 00138 NM 2007 3 1 UIEA200700080 1 20070222 A 5730 SKIN BOEING 747 7472D3B 1384805 NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 FOUND LEFT WING UPPER WING SKIN AT WS 1280 FOUND CORROSION. CORROSION REMOVED AND PROTECTED AS PER SRM 51-10-01 AND 51- 10-02. 2 L 7 4 4F RT A20WE 2007030100139 20070301 00139 NM 2007 3 1 UIEA200700081 1 20070222 A 5730 SKIN BOEING 747 7472D3B 1384805 NM RT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 FOUND RIGHT WING UPPER SURFACE RWS642 AT MID SPAR FOUND CORROSION. CORROSION REMOVED AND PROTECTED AS PER SRM51-10-01 A ND 51-10-02. 2 L 7 4 4F RT A20WE 2007030100140 20070301 00140 NM 2007 3 1 UIEA200700072 1 20070218 A 5320 65B126461 INTERCOSTAL BOEING 747 7472D3B 1384805 NM BS 395 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 FOUND UPPER DECK FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 395 RBL 6. U/DECK FLOOR SUPPORT INTERCOSTAL REPLACED AS PER SR M 51-10-01. 2 L 7 4 4F RT A20WE 2007030100141 20070301 00141 NM 2007 3 1 UIEA200700073 1 20070220 A 7500 1756M94G03 DUCT BOEING 747 7472D7B 1384803 NM NR 1 ENGINE DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 17007 1983 22337 NUMBER ONE POSITION ENGINE SERIAL NUMBER 517598 WAS FOUND WITH A 4 INCH BLOWN HOLE ON 8TH STAGE "Y" DUCT. DUCT WAS REMO VED AND REPLACED AS PER 747 MM 75-25-00. 2 L 7 4 4F RT A20WE 2007030100144 20070301 00144 NM 2007 3 1 UIEA200700084 1 20070222 A 5730 SKIN BOEING 747 7472D3B 1384805 NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 LEFT WING UPPER WING SKIN AT WS320, STR 14L-14L FOUND CORROSION. CORROSION REMOVED AND PROTECTED AS PER SRM 51-10-01 AN D 51-10-02. 2 L 7 4 4F RT A20WE 2007030100147 20070301 00147 NM 2007 3 1 UIEA200700071 1 20070218 A 5320 65B113573 STIFFENER BOEING 747 7472D3B 1384805 NM BS 400 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 FOUND UPPER DECK FLOORBEAM ONE STIFFENER CRACKED AT BS 400 LBL15. UPPER DECK FLOORBEAM STIFFENER REPLACED AS PER SRM 51 -10-01. 2 L 7 4 4F RT A20WE 2007030100148 20070301 00148 NE 2007 3 1 QXEA200700246 3 20070225 A 6110 UNKNOWN DHAV DHC8 DHC8202 2809007 NM HAMSTD 14SF 14SF* NE BETA LOCKOUT UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 359PH 514 BOI FLIGHT NR 2202 - DURING NR 1 BETA LOCK-OUT TEST PROP GROUND RANGE LIGHT ILLUMINATES IMMEDIATELY WHEN BRINGING POWER LEVER TO DISC BEFORE PUSHING TEST BUTTON ON PROP RPM GAUGE. MAINTENANCE RESET BETA LOCK-OUT. NO PART REPLACED. OPERAT IONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 6 C P7NE 2007030100149 20070301 00149 NM 2007 3 1 QXEA200700247 1 20070226 A 2435 23088008 STARTER GEN DHAV DHC8 DHC8202 2809007 NM LT ENGINE MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 356PH 15565 660 502 BOI FLIGHT NR 2192, DURING AFTER START FLOW WITH LEFT ENGINE FEATHERED WHEN TURNING MAIN BUSS TIE TO OFF AUX INVERTER CA UTION ILLUMINATED ALONG WITH SEVERAL ASSOCIATED ITEMS. MAINTENANCE REPLACED NR 1 STARTER/GENERATOR IAW AMM 80-10-11 TAS K CARD 9801001. GROUND RAN BOTH ENGINES. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030100151 20070301 00151 NM 2007 3 1 AWXA200700282 1 20070224 A 5743 65C365451 FITTING BOEING 737 73733A 1384673 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND LEFT WING OUTBOARD LEFT MAIN LANDING GEAR SUPPORT BEAM FITTING CRACKED, WBL 157. REPLACED LEFT WING OUTBOAR D LEFT MAIN LANDING GEAR SUPPORT BEAM FITTING CRACKED, WBL 157 IAW AWA ER 03-5700-07052-SS1 2 L 7 2 4F RT A16WE 2007030100155 20070301 00155 NM 2007 3 1 AWXA200700286 1 20070221 A 5320 69169707 INTERCOSTAL BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND LOWER INTERCOSTAL CLIP CRACKED, BS 348.2, S15L. REPLACED LOWER INTERCOSTAL CLIP, BS 348.2, S15L IAW AWA ER 03-5312-07051-SS1. 2 L 7 2 4F RT A16WE 2007030100156 20070301 00156 NM 2007 3 1 AWXA200700287 1 20070221 A 5340 650163312 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED STRINGER CLIP, BS 294.5, S13L. REPLACED STRINGER CLIP, BS 294.5, S13L IAW AWA ER 03-5312-07051-SS1. 2 L 7 2 4F RT A16WE 2007030100157 20070301 00157 NM 2007 3 1 AWXA200700288 1 20070220 A 5320 65176856 SUPPORT BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED INTERCOSTAL SUPPORT STRAP, BS 348.2, S16L. REPLACED INTERCOSTAL SUPPORT STRAP, BS 348.2, S16L IAW AWA ER 03-5312-07051-SS1. 2 L 7 2 4F RT A16WE 2007030100158 20070301 00158 NM 2007 3 1 AWXA200700289 1 20070217 A 5311 652072354 FRAME BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED FRAME, BS 492, S24R AT FORWARD CARGO DOOR CUT OUT LOWER DOOR STOP FITTING. REPAIRED FRAME, BS 492, S24R AT FORWARD CARGO DOOR CUT OUT LOWER DOOR STOP FITTING IAW AWA ER 03-5332-07047-ES3. 2 L 7 2 4F RT A16WE 2007030100159 20070301 00159 NM 2007 3 1 AWXA200700290 1 20070118 A 5330 6545775594 SKIN PANEL BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED FUSELAGE SKIN, BS 727D+18", S23R. REPAIRED FUSELAGE SKIN, BS 727D+18", S23R - S25R IAW AWA ER 03- 5300-07054-HF3. 2 L 7 2 4F RT A16WE 2007030100164 20070301 00164 NM 2007 3 1 AWXA200700295 1 20070211 A 5347 6546815138 SEAT TRACK BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED MAIN CABIN SEAT TRACK, BS 727B, RBL 45. REPLACED MAIN CABIN SEAT TRACK, BS 727B, RBL 45 IAW B737-30 0 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007030100165 20070301 00165 NM 2007 3 1 BB07017 1 20070226 A 2120 GTCP331200ER APU BOEING 757 7572B7 1384964 NM APU BAY FAILED A USAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 19 206UW 54049 27808 FLIGHT 1026, TPA-CLT: ON TAXI OUT, CABIN BEGAN TO FILL WITH SMOKE AND THE LAV SMOKE DETECTORS BEGAN TO SOUND. FLIGHT R ETURNED TO GATE. MAINTENANCE FOUND THE APU HAD CONTAMINATED THE A/C SYSTEM WITH OIL. ACCOMPLISHED DE-CONTAMINATION OF AIR DISTRIBUTION SYSTEM. NO FURTHER FAULTS. 2 L 7 2 4F RT A2NM 2007030100167 20070301 00167 NM 2007 3 1 USAA070141 1 20070226 A 5313 STRINGER BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 AREA ON STRINGER STA 847, STR 24R HAS CORROSION. U-CHANNEL INSTALLED INSIDE OF STRINGER PER SRM 53-00-03; CORR LEVEL 2; TSK C53-208-01, DEFECT SIZE: 3 X 4 INCHES. 2 L 7 2 4F RT A16WE 2007030100170 20070301 00170 NM 2007 3 1 USAA070138 1 20070226 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 1016 STR 5L AT LAV ATTACH MOUNT ELONGATED. INSTALLED DOUBLER & TRIPLER PER EA 98446, DEFECT SIZE: .5 INCH AREA. 2 L 7 2 4F RT A16WE 2007030100172 20070301 00172 NM 2007 3 1 USAA070137 1 20070226 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 AT 492.4 STR 24R FWD CARGO AFT FRAME HAS CRACK. REMOVED DAMAGE & INSTALLED FABRICATED REPAIR PARTS PER SRM 51-40-02 & 5 1-10-02, DEFECT SIZE: 3 INCHES. 2 L 7 2 4F RT A16WE 2007030100173 20070301 00173 NM 2007 3 1 USAA070136 1 20070226 A 5320 TIE CLIP BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 BS 360 S-9L HAS CRACK. FABRICATED & INSTALLED REPLACEMENT TIE CLIP PER BOEING DWG 69-46882 & SRM 51-10-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007030100174 20070301 00174 NM 2007 3 1 USAA070135 1 20070226 A 5411 FRAME BOEING 737 737401 1384701 NM NR 1 PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 THE U-SHAPE FRAME IN NR 1 PYLON BELOW AFT SPAR CRACKED. REPLACED U-SHAPE FRAME PER EA 98483, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007030100176 20070301 00176 NM 2007 3 1 USAA070133 1 20070226 A 5320 TIE CLIP BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 360 STR 11L HAS CRACK. REMOVED DAMAGE & INSTALLED FAB'D REPAIR PARTS PER SRM 51-10-02, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007030100177 20070301 00177 NM 2007 3 1 USAA070132 1 20070226 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 SKIN AT STA 727D + 12 INCHES STR 23R HAS CRACK. REMOVED DAMAGE & INSTALLED REPAIR DOUBLER & TRIPLER PER EA 98457, DEFEC T SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007030100178 20070301 00178 NM 2007 3 1 USAA070131 1 20070226 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 FWD END OF INTERCOSTAL WEB AT STR 12L AND BS 294.5 HAS CRACK. REMOVED CRACKED INTERCOSTAL & REPLACED WITH FAB'D PART PE R BOEING DWG 55-17684, DEFECT SIZE: .125 INCH. 2 L 7 2 4F RT A16WE 2007030100179 20070301 00179 NM 2007 3 1 USAA070130 1 20070226 A 5313 STRINGER BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STRINGER SPLICE CHANNEL, BS 360 FRAME AND STRINGER 15L HAS CRACK. INSTALLED NEW STRINGER PER SRM 51-10-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007030100180 20070301 00180 NM 2007 3 1 USAA070129 1 20070226 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 747 AND S23L HAS CRACK. INSTALLED DOUBLER PER SRM 53-00-01, DEFECT SIZE: 4 INCHES. 2 L 7 2 4F RT A16WE 2007030100181 20070301 00181 NM 2007 3 1 USAA070128 1 20070226 A 5754 1147410426 SKIN BOEING 737 737201 1384454 NM L/E SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246AY 23898 NR 9 SLAT, WEDGE UPPER SURFACE OSS 643.74-648.74 DELAMINATED. CUT OUT DELAMINATED SKIN, BONDED REPAIR DOUBLER PER SRM 5 1-70-10, PAR 20, DEFECT SIZE: 2.5L X 1.5W INCHES. 2 L 7 2 4F A16WE 2007030100185 20070301 00185 2007 3 1 HALA0700058 4 20070223 A 3417 UNKNOWN BOEING 767 76733A 1385209 NM FMC UNKNOWN A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 581HA 28141 ETOPS SIGNIFICANT SYSTEM, FMC SINGLE OPERATION LEFT WITH FMC FAIL LIGHT ON. CYCLED LEFT FMC CBS TEST OF LEFT FMC GOOD P ER FIM 34-61-00, SYSTEM NORMAL. 2 L 7 2 4F RT A1NM 2007030100186 20070301 00186 NM 2007 3 1 WRNA200700007 1 20070214 A 7120 MOUNT BOEING 747 747212B 1384886 NM NR 4 ENGINE CRACKED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, WHILE ACCOMPLISHING ULTRASONIC INSPECTION OF NR 4 STRUT REAR ENGINE MOUNT THRUST LINKIAW 747 MM 71-21-03 , THE FORWARD BORE HAD A CRACK INDICATION AT O/B LUG BORE EDGE. 2 L 7 4 4F A20WE 2007030100187 20070301 00187 NM 2007 3 1 HALA0700059 1 20070223 A 4900 233T3233212 CONTROL PANEL BOEING 767 767300 1385204 NM APU MALFUNCTIONED A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 584HA 16469 16469 24258 ETOPS SIGNIFICANT SYSTEM, APU START SWITCH SPRING DEFECTIVE. WILL NOT SPRING BACK TO "ON" FROM "START" OTHERWISE OPERAT ES NORMAL. REPLACED APU CONTROL PANEL PER AMM 49-41-81-004-001. INSTALLED APU CONTROL AMM49-41-81-404-007. OPS CHECK GOOD SECURITY CONDITION GOOD. 2 L 7 2 4F RT A1NM 2007030100191 20070301 00191 EU 2007 3 1 WRNA200700013 1 20070222 A 3260 221TS02Y02 SWITCH AIRBUS 300 A300B4203 3930306 EU LANDING GEAR MALFUNCTIONED A WRNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 501TR 53 AFTER TAKEOFF FROM GSO, GOT NOSE LANDING GEAR DOOR UNSAFE INDICATION, WHEN GEAR HANDLE WAS PLACED IN NEUTRAL POSITION AL L GEARS EXTENDED. RETURNED TO GSO AND MADE A SAFE LANDING. PERFORMED NORMAL SYSTEM LANDING GEAR RETRACTION IAW A300 MM 32-30-00 PAGE 501, 5 TIMES, NO FAULTS NOTED. AS PRECAUTION, THE LANDING GEAR CONTROL MICRO SWITCH UNIT WAS REPLACED AS MOST PROBABLE CAUSE. COMPLETED NORMAL SYSTEM LANDING GEAR RETRACTION TEST IAM 32-30-00 PAGE 501, NO DEFECTS NOTED. AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A35EU 2007030100193 20070301 00193 NM 2007 3 1 HALA0700060 1 20070224 A 4900 UNKNOWN BOEING 767 767300 1385204 NM APU UNKNOWN A HALA K NONE O OTHER CR CRUISE 1 WP 13 584HA 24258 ETOPS SIGNIFICANT SYSTEM, APU WILL NOT START. BITE CHECKED ECU, NORMAL SHUTDOWN NOTED. NO DATA PREVIOUS STARTS. CLEAR ED AND STARTED APU. OPS CHECK GOOD. VERIFIED START SWITCH OPERATES NORMALLY W/NO DEFECT NOTED. 2 L 7 2 4F RT A1NM 2007030100194 20070301 00194 NM 2007 3 1 HALA0700061 1 20070225 A 4940 ECU BOEING 767 767300 1385204 NM APU FAILED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 584HA 24258 ETOPS SIGNIFICANT SYSTEM, APU FAILED TO START 3 TIMES. BITE CHECK ECU FOUND GEN FILTER PRESS SW FAULT REMOVED AND REPLA CED PR SW PER AMM 49-27-15 COND SAME 6821. REMOVED AND REPLACED ECU PER AMM 49-61-05 COND SAME 5979 REPL K617 AND K197 RELAY PER 767 WDM49-41-11. OPS CKS OK PER 767 AMM 49-11-00. 2 L 7 2 4F RT A1NM 2007030100197 20070301 00197 NM 2007 3 1 HALA0700064 1 20070226 A 2410 745329F IDG BOEING 767 76733A 1385209 NM LT GENERATOR CONTAMINATED A HALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 WP 13 589HA 16508 16508 33466 ETOPS SIGNIFICANT SYSTEM, L GEN DRIVE LIGHT ON WITH ASSOC EICAS MESSAGE. FOLLOWED QRH AND DISCONNECTED L GEN AT 0254Z, APU STARTED. ECS MSG (IDG OIL LEVEL, ELX HYD PAGE MSG L GEN DRIVE, IDG OUT TEMP 103, RISE 27 ON AUTO EVENT PAGE T/S PER FIM 24-20-00/101 FIG 101, PERFORMED BPCU BITE. LEFT GEN SYS HAD IDG RISE TEMP, IDG LOW OIL PRESS AND DISC TRIP, PER FI M 24-20-00. TABLE 102 LOW OIL PRESS MSG WITH DPI POPPED, NEEDS IDG. REMOVED IDG FILTER PER AMM 24-11-02. FOUND FRESH BRIGHT SHINY METAL IN FILTER, NO EVIDENCE OF CONTAMINATION IN IDG OIL OR FUEL, WATER, SKYDROL. NO FLUSH REQUIRED PER AM M TASK 24-11-01-286-075 H(1) SCAVENGE FILTER AND OIL CONDITION CHECK TABLE. REMOVED IDG PER AMM 24-11-01-004-002-004. 2 L 7 2 4F RT A1NM 2007030100207 20070301 00207 NM 2007 3 1 AWXA200700297 1 20070121 A 5310 65C2518022 DOOR FRAME BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND AFT CARGO DOOR LOWER FORWARD FRAME CRACKED, BS 800, S22R - S25R. REPLACED AFT CARGO DOOR LOWER FORWARD FRAM E, BS 800, S22R - S25R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007030100208 20070301 00208 NM 2007 3 1 AWXA200700298 1 20070117 A 5753 6546486130 WEDGE BOEING 737 73733A 1384673 NM ZONE 600 DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND RIGHT WING INBOARD MIDFLAP TRAILING EDGE WEDGE PANEL LOWER SURFACE DELAMINATED, WS 161.5 - WS 168. REPAIRED RIGHT WING INBOARD MIDFLAP TRAILING EDGE WEDGE PANEL LOWER SUFACE, WS 161.5 - WS 168 IAW B737-300 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 2007030100211 20070301 00211 NM 2007 3 1 AWXA200700300 1 20070121 A 5320 69434961 INTERCOSTAL BOEING 737 73733A 1384673 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CORROSION ON INTERCOSTAL CHANNEL, BS 847 - BS 867, S25R. REPLACED INTERCOSTAL CHANNEL, BS 847 - BS 867, S25 R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007030100212 20070301 00212 SO 2007 3 1 SIMA200705707 1 20070216 A 5315 14530645411 FLOORBEAM EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 712AE 15662 4800 145247 PREVIOUS REPAIR ON LEFT OMEGA BEAM AT FRAME 20 CORRODED. FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS. CLEANED , TREATED AND RESTORED PROTECTIVE FINISH IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007030100215 20070301 00215 SO 2007 3 1 SIMA200705712 1 20070223 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO ZONE 700 FAILED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 639AE 16705 145182 LOUD THUMP HEARD FROM NOSE WHEEL WELL AREA DURING CLIMB AND CRUISE, THUMPS FELT IN FIRST OFFICER'S LEFT RUDDER PEDAL, SO UNDS LIKE NOSE WHEEL STEERING IS ACTIVATED. REMOVED AND REPLACED NOSE GEAR PROXIMITY SWITCH IAW EMB AMM 32-61-01. OPER ATIONAL CHECK GOOD, FUNCTIONAL CHECK FLIGHT PERFORMED WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007030100223 20070301 00223 SO 2007 3 1 SIMA200705704 1 20070222 A 5315 14530645411 FLOORBEAM EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 804AE 13150 4800 145487 FOUND LEFT OMEGA BEAM FOUND CORRODED AT FRAME 20. FABRICATED AND INSTALLED FILLER AND DOUBLER. CLEANED, TREATED AND RE STORED PROTECTIVE FINISH IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007030100224 20070301 00224 SO 2007 3 1 SIMA200705705 1 20070220 A 5315 14530645411 FLOORBEAM EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 709GB 15825 4800 145211 PREVIOUS REPAIR ON LEFT OMEGA BEAM FOUND CORRODED AT FRAME 20. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED REPAI R DOUBLERS AND FILLERS. CLEANED, TREATED AND RESTORED PROTECTIVE FINISH IAW EMB SRM 51-40-02 AND 53-00-10. RETURNED AI RCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007030100225 20070301 00225 SO 2007 3 1 SIMA200705706 1 20070213 A 5330 12022656054 SKIN EMB 135 EMB135LR 3260305 SO ZONE 200 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 712AE 15662 4800 145247 FOUND RIGHT NOSE SKIN DENTED BETWEEN STRINGER 13 RIGHT AND 16 RIGHT AND FRAMES 7 AND 8. PERFORMED RECONTOUR OF DENT, PE RFORMED NDT. FABRICATED AND INSTALLED REPAIR DOUBLER. RESTORED PROTECTIVE FINISH IAW EMB IC2007-145/01083. 2 L 7 2 4F RT T00011AT 2007030100228 20070301 00228 SO 2007 3 1 SIMA200705702 1 20070221 A 5320 14525480603 SILL EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 709GB 15825 4800 145211 BAGGAGE DOOR FRAME LOWER SILL FOUND CORRODED. REMOVED AND REPLACED SILL. CLEANED, TREATED AND RESTORED PROTECTIVE FINI SH IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007030100229 20070301 00229 NM 2007 3 1 DHL2007781009 1 20070226 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM BS 480-610 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 781DH 21996 FOUND LT CABIN, SEVERAL AREAS OF CORROSION ON SEAT TRACK AT BS 500-600, LBL48. REMOVED DAMAGED SEAT TRACK SECTIONS, BS 480-610. FABRICATED NEW SEAT TRACK SECTION FROM BAC1520-792, PO NR 9003797, 130" LONG, PER B727 SRM 53-10-5 FIG 1. FAB RICATED REPAIR ANGLES FROM BAC1503-10122, PONR 9004539, 2 AT 13" LONG, AND STRAP FROM 7075-T6, .250" BY 8.5" BY 2", PO NR 9001189, PER B727 SRM 53-10-5 FIG 1. TREATED, PRIMED, AND INSTALLED REPAIR PARTS/SEAT TRACK PER B727 SRM 51-10-2 AND 53-10-5 FIG 1. 2 L 7 3 4F A3WE 2007030100230 20070301 00230 NM 2007 3 1 DHL2007781016 1 20070227 A 5311 INTERCOSTAL BOEING 727 727227 1384078 NM BS 925 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 781DH 21996 AFT CARGO COMPT AT BS 925, INTERCOSTAL WEB ATTACH TO STR 20L IS CRACKED. STOP DRILLED CRACK PER B727 SRM 51-10-1. CRAC K CONTAINMENT VERIFIED BY HFEC METHOD. FABRICATED REPAIR ANGLE FROM 7075-T6, .080" BY 9" BY 2.25", PO NR 9003958, PER B 727 SRM 53-10-2 FIG 5. TREATED, PRIMED, AND INSTALLED REPAIR ANGLE PER B727 SRM 51-10-2 AND 53-10-2 FIG 5. 2 L 7 3 4F A3WE 2007030100231 20070301 00231 NM 2007 3 1 USAA070094 1 20070213 A 5414 SKIN BOEING 737 7374B7 1384702 NM LT NACELLE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 24811 LT ENG PYLON PANEL OPENING 5727L AT O/B AFT CORNER OF OPENING. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER TYP REP 54-30-07, DEFECT SIZE: .5". 2 L 7 2 4F RT A16WE 2007030100232 20070301 00232 CE 2007 3 1 815AC701 1 20070129 A 3230 UNKNOWN CESSNA 310 310R 2074245 CE CONT O520 IO520* 17032 SO LANDING GEAR MALFUNCTIONED D FSEA O OTHER O OTHER AP APPROACH 1 EA 65 815AC 310R0597 APPROACH TO LANDING, WOULD NOT EXTEND, ELECTRICALLY. MANUAL EXTENSIONS PROCEDURES WERE FOLLOWED AND OPERATED NORMALLY. PILOT EXTENDED LANDING GEAR USING MANUAL EXTENSION PROCEDURES, 3 GREEN DOWN AND LOCKED INDICATIONS, AN UNEVENTFUL LANDI NG WAS COMPLETED. AC RETURNED ON A FERRY FLIGHT. TROUBLESHOOTING IS ON GOING, PROBLEM COULD NOT BE DUPLICATED. (K) 1 L 7 2 3O 3 O 3A10 E5CE 2007030100233 20070301 00233 NM 2007 3 1 QXEA200700252 1 20070225 A 2440 RECEPTACLE BOMBDR DHC8 DHC8402 1390042 NM GROUND POWER DAMAGED A QXEA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 NM 09 415QX 4081 SMF FLIGHT NR 2415: DURING DE-PLANING, GROUND POWER CORD CAUGHT FIRE. AT RECEPTICAL PART OF PLUG, CORD APPEARS TO BE FU SED TO RECEPTICAL. MAINTENANCE CLEANED SOOT AND PERFORMED DETAILED INSPECTION OF GPU AREA. NO DISCOLORATION OF PAINT. NO DAMAGE TO CONNECTOR. CONTACT PLUG NOT FUSED TO RECEPTICAL. REMOVED WITH FINGER PRESSURE ONLY. PERFORMED DC EXTERN AL POWER SYSTEM TEST PER Q400 AMM 24-42-00-710-801. TESTS GOOD. NO DEFECTS. FIRE DAMAGE INVESTIGATION COMPLETED PER Q 400 SRM 51-12-00-200-002. NO DEFECTS. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030100234 20070301 00234 NM 2007 3 1 QXEA200700253 1 20070226 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM ICED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 410QX 4053 GEG FLIGHT NR 2351: FA REPORTS MCD HARD TO OPEN FROM THE INSIDE. MAINTENANCE INSPECTION FOUND ICE ACCUMULATION AROUND D OOR SEAL AND AT BASE OF MCD. THAWED AND REMOVED MOISTURE AS REQUIRED. MCD OPS CHECK GOOD INSIDE AND OUTSIDE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030100235 20070301 00235 2007 3 1 QXEA200700240 4 20070222 A 3410 CONTROL PANEL DHAV DHC8 DHC8202 2809007 NM COCKPIT ODOR A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 374PH 528 PDX FLIGHT NR 2276 - EXTERNAL POWER CART DROPPED OFF-LINE. ELECTRICAL SMOKE SMELL IN COCKPIT. REMOVED AND REPLACED ALE RT AURAL PANEL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030100238 20070301 00238 NM 2007 3 1 DHL2007781015 1 20070227 A 7160 NOSE COWL BOEING 727 727227 1384078 NM NR 3 ENGINE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 781DH 21996 NR 3 ENG NOSE COWL LOWER SIDE DENTED BETWEEN NAC STA 70 AND 85. CUT OUT DAMAGED AREA OF COWL, 17.5" BY 9.5" APPROX, PER B727 SRM 54-30-3 FIG 3.FABRICATED; FILLER FROM 2024-T3, .040" BY 9" BY 18", PO NR 9004042; AND DOUBLER FROM 2024-T3, .0 50" BY 20.5" BY 6.5" (INTERNAL), PO NR 9003958, PER B727 SRM 54-30-2 FIG 1 AND 54-30-3 FIG 3. TREATED, PRIMED, AND INST ALLED REPAIR PARTS PER B727 SRM 51-10-2 AND 54-30-3 FIG 3. 2 L 7 3 4F A3WE 2007030100240 20070301 00240 WP 2007 3 1 07FDEA00569 1 20070226 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP BS 594 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 FOUND LT AIR CONDITIONING COMPT, CRACK ON STIFFENER AND ANGLE REPAIR OF UPPER BULKHEAD AT STA 594, X= 57. REPAIRED ANG LE IAW SRM 53-00-01 VOL 1 FIG 2 SHT 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N00884 AND IAW SRM 53-00-01 FIG 2 SH T 2 VOL 1. 2 L 7 3 4F A22WE 2007030100242 20070301 00242 WP 2007 3 1 07FDEA00572 1 20070226 A 5712 RIB DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 FOUND RT WING L/E INT SIDE FOUND 1 CRACK ON RIB AT STA XORS 923. REPAIRED RIB IAW SRM 57-20-00 PAG 3 FIG 1 VOL 1. FABR ICATED PART IAW DETAIL PART TRAVELER I035571-3/N00571-3. REPAIR ANGLE IAW SRM 57-20-00 FIG 20 SHT 2 VOL 1. 2 L 7 3 4F A22WE 2007030100243 20070301 00243 WP 2007 3 1 07FDEA00573 1 20070226 A 5712 RIB DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 RT WING L/E INT SIDE FOUND 1 CRACK ON HORIZONTAL RIB AT STA XORS 548. REPAIRED RIB IAW SRM 57-00-01 VOL 1 FIG 10. FABR ICATED PART IAW DETAIL PART TRAVELER I035578-3/N00578-3 REPAIR ANGLE IAW SRM 57-00-01 FIG 10 VOL 1. 2 L 7 3 4F A22WE 2007030100246 20070301 00246 WP 2007 3 1 07FDEA00576 1 20070226 A 5754 ANGLE DOUG DC10 DC1010 3022110 WP SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 LT WING L/E DURING INSPECTION FOUND 1 CRACK 2" LONG ON ANGLE OF SLAT NR 2 AT STA XORS 264. REPAIRED ANGLE IAW SRM 57-00 -01 FIG 3 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER I035530-3/N00530-3 AND IAW SRM 57-00-01 FIG 3 VOL 1. 2 L 7 3 4F A22WE 2007030100247 20070301 00247 WP 2007 3 1 07FDEA00577 1 20070226 A 5712 RIB DOUG DC10 DC1010 3022110 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 LT WING L/E INT SIDE FOUND 1 CRACK 1" LONG ON HORIZONTAL RIB AT STA XORS 570. REPAIRED RIB IAW SRM 57-00-01 FIG 10 SHT 1 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER I035526/N00526 AND SRM 57-00-01 VOL 1. 2 L 7 3 4F A22WE 2007030100249 20070301 00249 NM 2007 3 1 07FDEA00578 1 20070225 A 2611 710121 ELEMENT DOUG MD11 MD11 3023602 NM APU COMPARTMENT FAILED A FDEA F ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 SO 25 585FE 48481 APU FIRE ALARM AND LIGHT CAME ON WITH APU FIRE LEVEL 3 ALERT AT 12000 FEET DESCENT ONTO FINAL APPROACH PULLED APU FIRE H ANDLE AND DISCHARGED FIRE BOTTLE LIGHT WENT OUT AFTER 30 SECONDS BLEED AIR NR 2 AND NR 2 PACK AUTO SHUT DOWN. APU COMPA RTMENT INSPECTION REVEALED NO SIGNS OF FIRE OR HOT AIR LEAK. APU WAS NOT RUNNING DURING OCCURRENCE. MAINTENANCE REPLAC ED NR 2 FIRE EXTINGUISHER BOTTLE AND APU FIRE DETECT ELEMENT LOOP B. 2 L 7 3 4F RT A22WE 2007030100250 20070301 00250 EA 2007 3 1 QXEA200700250 1 20070226 A 7830 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA THRUST REVERSER UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 611QX 10041 DEN - FLIGHT 4165 - RECEIVED A RIGHT THRUST REVERSER FAULT STATUS MESSAGE. RETURNED TO THE GATE. MAINTENANCE PLACED TH E SYSTEM ON MEL 78-30-1. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007030100252 20070301 00252 NM 2007 3 1 QXEA200700255 1 20070225 A 3060 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM PROP HEAT UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 406QX 4048 MSO FLIGHT NR 2340: NR 2 PROP HEAT INOP ON TAXI. AIRCRAFT RETURNED TO GATE. MAINTENANCE INTERROGATED CDS AND FOUND NO FAULTS. GROUND RAN BOTH ENGINES WITH ALL POWER ONLINE AND PERFORMED FUNCTIONAL TEST OF PROP DEICE SYSTEM IAW AMM 30-60- 00. OPS CHECK GOOD. BOTH PROP LIGHTS ILLUMINATE AND LOADS SHOWN ON ELECTRICAL PAGE. NO PARTS REPLACED. AIRCRAFT RETU RNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030100255 20070301 00255 NM 2007 3 1 AMTA200700059 1 20070206 A 2560 BATTERY BOEING 737 73783N 13844HI NM FLASHLIGHT DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 301TZ 28239 EMERGENCY FLASH LIGHT AT AFT LT/LT F/A SEAT NEEDS TO REPLACED DURING L/S NO RED BLINK. REMOVED AND REPLACED F/A FLASH L IGHT BATTERY, OPS AND SECURED OK. (K) 2 L 7 2 4F RT A16WE 2007030100256 20070301 00256 NM 2007 3 1 AMTA200700086 1 20070217 A 5551 PIN BOEING 737 73783N 13844HI NM HORIZ STAB CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 323TZ 30033 RT AFT UPPER STAB PIN CORRODED. REMOVED AND REPLACED PIN 180A1612-3 IAW EO 735-55AD-2935 REV B. (K) 2 L 7 2 4F RT A16WE 2007030200001 20070302 00001 NM 2007 3 2 SWAA071116 1 20070226 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 410WN 27897 DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007030200002 20070302 00002 NM 2007 3 2 SWAA071108 1 20070226 A 3350 101073 LENS BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 EMERGENCY EXIT LIGHT LENS MISSING AT ROW 16 DEF. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007030200005 20070302 00005 NM 2007 3 2 SWAA071110 1 20070226 A 2910 272A4451 HYDRAULIC LINE BOEING 737 7377H4 1384404 NM MLG W/W CHAFED A SWAA D RETURN TO BLOCK K FLUID LOSS CR CRUISE 1 SW 29 705SW 27839 AIR TURNBACK, AT FL 350 MASTER CAUTION AND HYDRAULIC LIGHTS ILLUMINATED, HYDRAULIC B-SYSTEM QUANTITY AT -0-. FOUND B-HY DRAULIC SYSTEM SPOILER PRESSURE LINE CHAFED. REMOVED AND REPLACED SPOILER PRESSURE LINE PER MM. 2 L 7 2 4F RT A16WE 2007030200006 20070302 00006 2007 3 2 SWAA071117 4 20070226 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 445WN 29841 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FELL OUT. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007030200012 20070302 00012 NM 2007 3 2 SWAA071126 1 20070226 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CRACKED AT BS 665, LBL 24. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007030200014 20070302 00014 NM 2007 3 2 SWAA071112 1 20070226 A 5320 6545819 GUSSET BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED MV2 CHECK, FOUND NLG W/W GUSSETT CRACKED. REMOVED AND REPLACED GUSSETT PER SRM. 2 L 7 2 4F RT A16WE 2007030200015 20070302 00015 NM 2007 3 2 SWAA071113 1 20070226 A 5753 6546435282 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP UPPER SURFACE DELAMINATED AT INBOARD END. REMOVED AND RE PLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2007030200016 20070302 00016 NM 2007 3 2 SWAA071125 1 20070226 A 5311 6546540 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030200018 20070302 00018 NM 2007 3 2 SWAA071119 1 20070226 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022600163 20070226 00163 EA 2007 2 26 VNAA0702008 1 20070210 A 3000 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE UNKNOWN A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 05 223JS 7892 CREW REPORTED PITOT BASE HEAT/ L AOA HEAT/ L STATIC HEAT/ L PITOT HEAT CAS MESSAGES AFTER TAKEOFF. CREW DIVERTED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED CIRCUIT BREAKER RESETS PER BBD SERVICE LETTER. MAINT ENANCE ALSO PERFORMED OPERATIONAL CHECKS IAW THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007022600166 20070226 00166 NM 2007 2 26 SPAA0700090 1 20070216 A 3350 900542 BATTERY PACK BOEING 737 7372Y5 1384554 NM EMERGENCY LIGHTS INOPERATIVE A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 28 712S 23038 MID CABIN OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT POWER SUPPLY (BATTERY PACK) PER AM M 33-51-111, OPS CHECK SATISFACTORY. 2 L 7 2 4U RT A16WE 2007022600190 20070226 00190 NM 2007 2 26 ASAA0741478 1 20070221 A 5315 FLOORBEAM BOEING 737 7374Q8 138447Q NM BS 986 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 FLOORBEAM UPPER CHORD CORRODED ON TOP AND BOTTOM SURFACES. REMOVED CORRODED UPPER CHORD FABRICATED AND INSTALLED REPLAC EMENT UPPER T-CHORD SPLICE ANGLES SPLICE STRAPS AND FILLERS IAW ASA EA 5310 02698. 2 L 7 2 4F RT A16WE 2007022700007 20070227 00007 2007 2 27 UPS07149234 4 20070220 A 2565 WARNING LIGHT AIRBUS A300 A300F4622R 3930360 EU ESCAPE SLIDE INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 121UP 0806 INSPECTION TYPE:N/A FWD ENTRY DOOR ESCAPE SLIDE ARM WARNING LIGHT IS INOP. CLEANED AND RESEATED THE CONNECTOR ON THE AU TONOMOUS STANDBY POWER SUPPLY UNIT 70WN AS REQUIRED. WARNING LIGHT OPS CHECKS GOOD. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2007022700010 20070227 00010 NM 2007 2 27 UPS07449229 1 20070215 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 460 S15L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C 1EA FASTENER HOLE FOUND CRACKED AT BS 460 S15L CRACKS WERE LOCATED AT UPWARD AND DOWNWARD DIRECTION. STRINGER REPLACED AS PER SRM 51-10-01 PG 9. 2 L 7 4 4F A20WE 2007022700011 20070227 00011 NM 2007 2 27 UPS07449230 1 20070215 A 5310 STRUCTURE BOEING 747 747121 1384871 NM BS 460 S15L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C 1EA FASTENER HOLE FOUND CRACKED AT BS 460 S15L BONDED STRAP, CRACK LOCATED AT DOWNWARD DIRECTION. BS 460 S15L CRACKED BONDED STRAP REPAIRED AS PER RS R53-11-35753A AND UPS EO B747-5310-26158. 2 L 7 4 4F A20WE 2007022700013 20070227 00013 2007 2 27 FX7A200700002 4 20070119 A 3400 COMPUTER DOUG DC9 DC983 3022083 WP OUT OF ADJUST A FX7A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 19 836NK 53045 ABORTED TAKEOFF DUE TAKEOFF WARNING. FOUND TAKEOFF CONDITION COMPUTER SETTING NOT SET CORRECTLY. 2 L 7 2 4F RT A6WE 2007022700017 20070227 00017 NM 2007 2 27 UPS07449231 1 20070219 A 5330 SKIN BOEING 747 747121 1384871 NM BS 460 S15R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C BS 460 STR 15R FOUND ONE EA FASTENER HOLE CRACKED AT SKIN BOND DOUBLER & STRAP. FX BS 460 STR 15R SKI N BOND DOUBLER & STRAP REPAIRED AS PER HX RS R53-11-35754 & UPS EO B747-5310-26195. 2 L 7 4 4F A20WE 2007022700044 20070227 00044 NM 2007 2 27 AWXA200700266 1 20070204 A 5330 6545770 SKIN BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED FUSELAGE SKIN, BS 606, S4L. REPAIRED FUSELAGE SKIN, BS 606, S4L IAW B737-300 SRM 53-00-01-2R. 2 L 7 2 4F RT A16WE 2007022700049 20070227 00049 WP 2007 2 27 IXXA07SMN063S 1 20070131 A 5753 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT UPPER OUTBOARD FLAP CRACKED AT STATION XF442.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND REPAIR PARTS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA, NEW SKIN A ND REPAIR PARTS AS NEEDED. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN AND REPAIR PARTS IAW DC8 SRM 57-7-1 FIGURE 4 TR NUMBER 57-94 DATED 10-01-02, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-7-1 FIGURE 4 ITEMS "U" AND "Q", DC8 SRM 51-1- 9, DC8 SRM 51-1-8B, DC8 SRM 51-1-11 AND DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007022700059 20070227 00059 WP 2007 2 27 IXXA07SMN073S 1 20070131 A 5753 SKIN DOUG DC8 DC871F 302199D WP ZONE 500 MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING FLAP UPPER SKIN HAS A NON STANDARD REPAIR BETWEEN STATIONS XF415.000 AND XF420.000. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INTERNAL SURFACE. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN IAW DC8 SRM 57-7-1 FIGURE 4 TR N UMBER 57-94 DATED 10-01-02, DC8 SRM 57-1-0.PAGE 1, DC8 SRM 57-7-1 FIG 4 ITEM "P", DC8 SRM 51-1-8B, DC8 SRM 51-1-11 AND D C8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007022700077 20070227 00077 WP 2007 2 27 07FDEA00560 1 20070226 A 5753 FITTING DOUG DC10 DC1010 3022110 WP TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 RT INBD FLAP, FOUND FITTING ITEM 665 WITH NR 4 ROLLERS BOLTS HOLES WITH CORROSION REF IPC 27-51-10-01 VIEW F. REMOVED SUPPORT IAW SRM 51-31-01 VOL 2 PAR 6-10. REMOVED CORROSION AND CORROSION LOCAL BLEND IAW SRM 51-21-01 VOL 2 PAR 34D AND IAW SRM 57-20-00 FIG 19 VOL1. REWORKED HOLES ON COUNTERSINK AREAS MAX DIA ON TOP IS 1.279/1.338. FABRICATED AND INSTA LLED REPAIR BUSHING IAW EA NR 8-5750-103683 AND SRM 57-20-00 FIG 19 VOL 1. INSTALLED SUPPORT IAW SRM 51-31-01 VOL 2 P AR 6-10. 2 L 7 3 4F A22WE 2007030100006 20070301 00006 EA 2007 3 1 TRAX200700247 1 20070219 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 902EV 7620 CEILING EMERGENCY LIGHT 1EA INOP. 2 L 7 2 4F RT A21EA 2007030100009 20070301 00009 EA 2007 3 1 TRAX200700250 1 20070219 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 744EV 10157 FWD FLIGHT ATTENDANT FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007030100026 20070301 00026 EA 2007 3 1 COMA0760208 1 20070223 A 3222 STRUT CNDAIR CL600 CL6002B19 1900309 EA NLG LOW A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 936CA 7043 FLIGHT 9452 - AFTER TAKEOFF FROM RFD RECEIVED A NLG DISAGREE WARNING, CREW DECLARED AN EMERGENCY AND RETURNED TO RFD. P ERFORMED COMPLETE SERVICING OF THE NLG STRUT. 2 L 7 2 4F RT A21EA 2007030100032 20070301 00032 NM 2007 3 1 2007UALA00518 1 20070219 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 34R BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 127UA 28813 FOUND EEL STRIP BROKEN, LIGHT INOP AFT OF ROW 34R. REPLACED EEL STRIP, OP CHECKED OK 2 L 7 4 4F 4 F RT A20WE E24NE 2007030100034 20070301 00034 WP 2007 3 1 UPS07849240 1 20070215 A 5320 SUPPORT CHANNEL DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C3 SUPPORT CHANNEL CRACKED AT STA 1730 RBL 20. REMOVED SUPPORT CHANNEL AT STA 1730 RBL 20 IAW SRM 51-01 -21. FABRICATED AND INSTALLED SUPPORT CHANNEL AT STA 1730 RBL 20 IAW SRM 51-3-0, AND DWG 5755032. 2 L 7 4 4F RT 4A25 2007030100037 20070301 00037 NM 2007 3 1 2007UALA00522 1 20070218 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SEAT 3E AFT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 225UA 30554 FOUND SEAT 3E, AFT EMERGENCY PATH LIGHT BROKEN AND INOP. REPLACED LIGHT, OP CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007030100042 20070301 00042 NM 2007 3 1 2007UALA00526 1 20070219 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 122UA 29168 FOUND EMERGENCY CEILING LIGHT ABOVE ROW 17 INOPERATIVE. RELAMPED. OP CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030100051 20070301 00051 WP 2007 3 1 UPS07849243 1 20070220 A 5720 WEB DOUG DC8 DC871F 302199D WP NR 2 MAIN TANK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C3 NR 2 MAIN TANK THRU PNL 506C WEB IS CRACKED FWD OF CTR/SPAR XRS -6. STOP DRILLED CRACK AT NR 2 MAIN TANK WEB AT STA XRS -6 IAW SRM 57-02-00 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER AT NR 2 MAIN TANK WEB AT STA X RS -6 IAW SRM 57-02-00 FIG 002A, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007030100058 20070301 00058 NM 2007 3 1 UPS07M49237 1 20070123 A 5730 DOUBLER DOUG MD11 MD11 3023602 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C LEFT WING L/E LWR COMPT STA XORS 558 FOUND UPPER DOUBLER PANEL CRACKED AS MARKED. LEFT WING L/E LWR C OMPT STA XORS 558 UPPER DOUBLER REMOVED PER SRM 51-31-01, V2R 2, R38. REPAIR DOUBLER FILLER ANGLES FAB & HOLES DRILLED PER SRM 57-10-00 -00, FIG 258, TEMP R.57-5. BEAM DOUBLER DAMAGED PORTIONED TRIMMED & RE-INSTALLATION PER SRM 57-10-00 F IG 258 TEMP R.57.5L, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007030100089 20070301 00089 NM 2007 3 1 SWAA071095 1 20070223 A 5311 6546555 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030100090 20070301 00090 NM 2007 3 1 SWAA071098 1 20070223 A 5311 6546596 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 9R AND STR 9L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030100115 20070301 00115 NM 2007 3 1 DHL2007781014 1 20070227 A 5512 SKIN BOEING 727 727227 1384078 NM HORIZONTAL STAB GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 781DH 21996 RT NR 5 BALANCE BAY (HORIZ STAB) UPPER SKIN GOUGED. REMOVED GOUGED PREVIOUS REPAIR DOUBLER. FABRICATED NEW DOUBLER FRO M 7075-T0, .032" BY 6" BY 5", PO NR 44953 PER B727 SRM 55-20-3 FIG 3. HEAT TREATED REPAIR TO T6 CONDITION IAW FASI FORM FAS 0115. TREATED, PRIMED, AND INSTALLED REPAIR DOUBLER PER B727 SRM 51-10-2 AND 55-20-3 FIG 3. 2 L 7 3 4F A3WE 2007030100121 20070301 00121 NM 2007 3 1 UIEA200700090 1 20070226 A 5330 65B076581005 SKIN BOEING 747 7472D3B 1384805 NM BS 240 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 FUSELAGE SKIN EXTERNAL DOUBLER FOUND CRACKED AT NLG LT FWD CORNER. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-29019 3820-1 THRU -5 AND FAA FORM 8100-9. 2 L 7 4 4F RT A20WE 2007030100123 20070301 00123 NM 2007 3 1 UIEA200700088 1 20070225 A 7830 FAIRING BOEING 747 7472D3B 1384805 NM GE CF6 CF680 30025 NE THRUST REVERSER CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 ENGINE NR 2 RT T/REV AFT UPPER BEAVER TAIL FAIRING ASSY INNER SKIN FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER EO NR 47 78A094 AND FAA FORM 8110-3. 2 L 7 4 4F 4 F RT A20WE E13NE 2007030100129 20070301 00129 NM 2007 3 1 UIEA200700077 1 20070221 A 5330 SKIN BOEING 747 7472D3B 1384805 NM BS 1020 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 FOUND CENTER TANK LOWER SKIN LOWER SURFACE FOUND CORROSION JUST ABOVE NR 1 ACM. CORROSION BLEND OUT AND HFEC INSPECTION PERFORMED AS PER BOEING SR ID NR 1-290707077-1 THRU -3 AND FAA FORM 8100-9. 2 L 7 4 4F RT A20WE 2007030100142 20070301 00142 NM 2007 3 1 UIEA200700075 1 20070221 A 5320 65B21264401 SHEAR WEB BOEING 747 7472D3B 1384805 NM BS 840-860 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 TENSION TIE BS 840-BS 860, LT SLOPING SHEAR WEB FOUND CRACKED AT FWD I/B LOWER CORNER. LEFT SLOPING SHEAR WEB REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F RT A20WE 2007030100143 20070301 00143 NM 2007 3 1 UIEA200700082 1 20070222 A 5330 SKIN BOEING 747 7472D3B 1384805 NM BS 1810 DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 FUSELAGE SKIN DENT FOUND AT BS 1810, S51L-S51R. DENT AREA REWORKED AND PROTECTED AS PER SRM 51-40-01 AND 51-10-02. 2 L 7 4 4F RT A20WE 2007030100146 20070301 00146 NM 2007 3 1 UIEA200700070 1 20070210 A 3233 1011986 ACTUATOR BOEING 747 7472D3B 1384805 NM GE CF6 CF650E2 30018 NE NLG DOOR BROKEN A UIEA O OTHER K FLUID LOSS CR CRUISE 1 EA 15 506MC 21252 517579 LOSS OF HYD SYSTEM NR 1, PERFORMED EMERGENCY/ABNORMAL CHECKLIST 3.29 FHB EDP, PUMP PLACED TO SUPPLY OFF AT TIME 2133Z, F LUID QTY TO 0. REMOVED AND REPLACED NOSE DOOR ACTUATOR AS PER AMM 32-34-14. 2 L 7 4 4F 4 F RT A20WE E23EA 2007030100153 20070301 00153 NM 2007 3 1 AWXA200700284 1 20070223 A 5711 65C530105354 SPAR BOEING 737 73733A 1384673 NM ZONE 600 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND RIGHT WING SPAR CHORD CRACKED, WBL 157, UNDER AFT OUTBOARD GEAR BEAM SUPPORT FITTING. REPAIRED RIGHT WING S PAR CHORD, WBL 157, UNDER AFT OUTBOARD GEAR BEAM SUPPORT FITTING IAW AWA ER 03-5700-07052-SS4. 2 L 7 2 4F RT A16WE 2007030100160 20070301 00160 NM 2007 3 1 AWXA200700291 1 20070117 A 5330 655298874 SKIN PANEL BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED FUSELAGE SKIN, BS 943.5, S24L. REPAIRED FUSELAGE SKIN, BS 943.5, S24L IAW AWA ER 03-5361-07054-HF5. 2 L 7 2 4F RT A16WE 2007030100162 20070301 00162 NM 2007 3 1 AWXA200700293 1 20070117 A 5330 6552988110 SKIN BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED FUSELAGE SKIN, BS 961, S21L - S22L. REPAIRED FUSELAGE SKIN, BS 961, S21L - S22L IAW B737-300 SRM 53 -00-01-2R31. 2 L 7 2 4F RT A16WE 2007030100169 20070301 00169 NM 2007 3 1 USAA070139 1 20070226 A 5320 FLOOR SUPPORT BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 860 RBL 23 - LBL 33 HAS CORROSION. REMOVED DAMAGE & INSTALLED REPAIR ANGLE PER TR 53-10-06B; CORR LEVEL 2; TASK C53 -208-01, DEFECT SIZE: 12 INCHES. 2 L 7 2 4F RT A16WE 2007030100188 20070301 00188 NM 2007 3 1 WRNA200700008 1 20070212 A 5320 65B0966114 SHEAR WEB BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, FOUND A 1 INCH CRACK IN SHEAR WEB, BETWEEN S-10A AND S-10 RIGHT SIDE BS 820, WL 332, RBL 80. REPLACED S HEAR WEB IAW B747 SRM 51-30-02 AND DRAWING 65B09661. 2 L 7 4 4F A20WE 2007030100190 20070301 00190 NM 2007 3 1 WRNA200700010 1 20070215 A 5510 BALL SCREW BOEING 747 747212B 1384886 NM HORIZ STAB FAILED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, HORIZONTAL STABILIZER BALL SCREW AND BALL NUT FAILED FREE PLAY CHECK. REMOVED STABILIZER DRIVE MECHANISM , CHECKED WEAR OF PINS AND FITTINGS, FOUND IN TOLERANCE IAW 747 MM 27-41-06. REINSTALLED DRIVE MECHANISM PER 747 MM 27-4 1-06 AND PERFORMED BALL NUT TO BALL SCREW FEE PLAY TEST IAW SB 747 27A2396, FOUND FREE PLAY LESS THAN 0.012, WITH-IN LIM ITS, ACCOMPLISHED LUBRICATION OF BALL NUT AND JACKSCREW IAW 747 MM 12-21-19 AND S/B 747-272396 2 L 7 4 4F A20WE 2007030100192 20070301 00192 EU 2007 3 1 WRNA200700012 1 20070221 A 3230 LANDING GEAR AIRBUS 300 A300B4203 3930306 EU NLG MALFUNCTIONED A WRNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 501TR 53 AFTER TAKEOFF FROM IND, NOSE LANDING GEAR FAILED TO RETRACT, PERFORMED ABNORMAL CHECK LIST AND DIVERTED TO GSO AND MADE A SAFE LANDING. PERFORMED NORMAL EXTENSION AND RETRACTION OF SYSTEM 1 AND 2, NO DEFECTS NOTED, AIRCRAFT RELEASED TO SER VICE. 2 L 7 2 4F RT A35EU 2007030100195 20070301 00195 NM 2007 3 1 HALA0700062 1 20070222 A 2612 UNKNOWN BOEING 767 767300 1385204 NM FIRE DETECTION UNKNOWN A HALA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM, STATUS MESSAGE AFTER ENG SHUTDOWN L ENG FIRE LP 2. PERFORMED FIRE DET BITE CHECK, ERASED MESS AGE. NO DEFECTS NOTED. REF FIM 26-11-00-101 FIG 105. 2 L 7 2 4F RT A1NM 2007030100199 20070301 00199 NM 2007 3 1 QXEA200700256 1 20070219 A 3080 4100S01906 PROBE BOMBDR DHC8 DHC8402 1390042 NM ICE DETECTOR FAILED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 416QX 4083 LAX FLIGHT NR 2304: ICE DETECT ON ED. CDS INDICATES R PROBE FAIL. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED RT ICE DETECTOR PROBE IAW Q400 AMM TASK 30-80-01-400-801. OPS CHECK GOOD. RESET CIRCUIT BREAKER. AIRCRAFT RE TURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030100200 20070301 00200 NM 2007 3 1 AWXA200700296 1 20070204 A 5330 65C357901 SKIN PANEL BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED FUSELAGE SKIN, S4L AT BODY STATIONS: 679.5, 692, 693, 694, 700, 701, 703, 705, 715.5. REPAIRED FUS ELAGE SKIN, BS 665 - BS 720, S4L IAW B737-300 SRM 53-00-01-2R30. 2 L 7 2 4F RT A16WE 2007030100226 20070301 00226 SO 2007 3 1 SIMA200705703 1 20070220 A 5320 14522178005 SILL EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 709GB 15825 4800 145211 FOUND SERVICE DOOR FRAME LOWER CENTER SILL FOUND CORRODED. FABRICATED AND INSTALLED REPAIR DOUBLERS. CLEAN, TREATED AN D RESTORED PROTECTIVE FINISH IAW EMB SRM 53-21-02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007030100227 20070301 00227 SO 2007 3 1 SIMA200705708 1 20070225 A 5315 14000235003 FLOORBEAM EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 804AE 13150 4800 145487 FOUND CENTER OMEGA BEAM CORRODED BETWEEN FRAME 23 AND FRAME 25. CLEANED, TREATED AND RESTORED PROTECTIVE FINISH. FABRI CATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007030100254 20070301 00254 WP 2007 3 1 070048 1 20070222 A 3350 1864 LAMP DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 877GA 53467 DURING A ROUTINE OVERNIGHT SERVICE CHECK SANFORD MAINTENANCE REPORTED THAT THE TAILCONE EMERGENCY LIGHTS WOULD NOT TEST. THEY FURTHER REPORT THEY RELAMPED THE TAILCONE EMERGENCY LIGHT ASSEMBLIES. A SATISFACTORY OPERATIONAL TEST WAS ACCOMP LISHED PER AMM 33-53-00.THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007030100257 20070301 00257 NM 2007 3 1 AMTA200700090 1 20070217 A 5551 PIN BOEING 737 73783N 13844HI NM HORIZ STAB CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 323TZ 30033 LT STAB AFT FAIL SAFE PIN CENTER CORRODED. REPLACED PIN 190A1612-4 IAW EO 737-55AD-2935 REV B. (K) 2 L 7 2 4F RT A16WE 2007030200007 20070302 00007 CE 2007 3 2 4516502162007 1 20070226 A 5320 4532301180005 SUPPORT LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE7312 01518 WP UPLOCK ROLLER SHEARED E J7SA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SW 05 429FX 165 ON GEAR RETRACTION, ALL GEARS RETRACTED, BUT THE NOSE GEAR DOWN AND LOCKED INDICATION STAYED ILLUMINATED AND THE LT /RT MAIN GEAR INDICATORS EXTINGUISHED. THE PILOT SELECTED THE GEAR DOWN AND ALL (3) GEARS EXTENDED AND INDICATED GREEN DOWN AND LOCKED. AFTER LANDING AND TAXI TO MAINTENANCE, CREW DISCOVERED THE NOSE GEAR UPLOCK ROLLER IS SHEARED AND THE LT NO SE DOOR EXTEND ROD IS BENT. 2 L 7 2 4F 4 F RT T00008WI E6WE 2007030200008 20070302 00008 CE 2007 3 2 4512002282007 1 20070228 A 3220 UNKNOWN LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE731* 01518 WP NLG UNKNOWN E J7SA A UNSCHED LANDING S J AFFECT SYSTEMS WARNING INDICATION CL CLIMB 1 SW 05 418FX 120 NOSE GEAR FAILS TO RETRACT AFTER TAKEOFF. MECHANIC JACKED AIRCRAFT AND PERFORMED 25 GEAR SWINGS. UNABLE TO DUPLICATE A LL COCKPIT INDICATION INDICATE NORMAL. HELD NOSE GEAR WHILE SELECTING GEAR UP TO CHECK GEAR ACTUATOR FOR POSSIBLE HYDRA ULIC BYPASS, TECH UNABLE TO HOLD GEAR NO HYDRAULIC BYPASS INDICATION NOTED. DISCONNECTED NOSE GEAR DOORS PERFORMED GEAR SWINGS MONITORED NOSE GEAR UP LOCK MECHANISM NO ABNORMALITIES NOTED . REGULATED HYD MULE PRESSURES TO AS LOW AS 2200 P SI STILL NO DEFECTS NOTED. FSR RECOMMENDED REPLACEMENT OF NOSE GEAR UPLOCK. 2 L 7 2 4F 4 F RT T00008WI E6WE 2007030200019 20070302 00019 NM 2007 3 2 SWAA071121 1 20070226 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030200020 20070302 00020 NM 2007 3 2 EIA2007007 1 20070128 A 2611 LAMP BOEING 747 747212B 1384886 NM SMOKE DETECTORS INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486EV 20888 FOUND 5B SMOKE DETECTOR WILL NOT TEST. RELAMPED BEACON BULB IAW MM 26-14-00. RELAMPED BEACON BULB CHECKS GOOD. 2 L 7 4 4F A20WE 2007030200021 20070302 00021 NM 2007 3 2 EIA2007009 1 20070205 A 2611 LAMP BOEING 747 747273C 1384896 NM SMOKE DETECTOR INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 470EV 200653 NR 6 SMOKE DETECTOR OF AFT CARGO COMPARTMENT WILL NOT TEST. RELAMPED PER MM 26-14-00, SYS TESTS OK. 2 L 7 4 4F A20WE 2007030200023 20070302 00023 NM 2007 3 2 EIA2007013 1 20070124 A 2611 LAMP BOEING 747 747212B 1384886 NM SMOKE DETECTOR INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482EV 20713 NR 4 AFT SMOKE DETECTOR INOP, LP 259652. RELAMPED NR 4 AFT SMOKE DETECTOR PER MM 26-16-02. 2 L 7 4 4F A20WE 2007030200024 20070302 00024 NM 2007 3 2 EIA2007014 1 20070216 A 2611 LAMP BOEING 747 747212B 1384886 NM SMOKE DETECTOR INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482EV 20713 NR 4 LOWER AFT SMOKE DETECTOR WILL NOT TEST. RELAMPED PER 12-16-02, OPS CHK GOOD. 2 L 7 4 4F A20WE 2007030200028 20070302 00028 NM 2007 3 2 QXEA200700293 1 20070227 A 5230 HANDLE BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR UNSECURE A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 420QX 4147 RNO FLIGHT NR 2495: DURING TAKEOFF ROLL, FUSELAGE DOOR WARNING ILLUMINATED AT APPROX 85 KNOTS. AFTER RETURN TO GATE, AF T CARGO DOOR HANDLE WAS POPPED OUT. MAINTENANCE, ON INITIAL INSPECTION FOUND CARGO DOOR HANDLE NOT STOWED. PERFORMED G VI OF DOOR HANDLE LATCH/LOCK ASSY WITH NO DEFECTS NOTED. C/W TASK FIM 51-70-00-810-801 PARA 1-3A AND PARA 5. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030200030 20070302 00030 WP 2007 3 2 IXXA07SMN076S 1 20070131 A 5522 SKIN DOUG DC8 DC871F 302199D WP ZONE 300 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR.-LOWER SKIN HAS A NON STANDARD REPAIR FROM STATION XE55.062 TO ST ATION XE65.156. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN AND REPAIR PARTS. BONDED REPAIR P ARTS WITH HYSOL AS NEEDED. CLEANED, TREATED AND PRIMED AREA, NEW SKIN AND REPAIR PARTS AS NEEDED. APPLIED SEALANT TO F AYING SURFACES. INSTALLED NEW SKIN FROM STATION XAR0.00 TO XE132.000. BALANCED LEFT ELEVATOR. MOMENT 1454.8 INCH POUN DS, FOUND WITHIN TOLERANCE IAW DC8 SRM 55-4-1 FIGURE 1 SHEET 1 AND 2, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 55-4-1 FIGURE 1 SHE ET 1 AND 2. ITEM "E" AND "F", DC8 SRM 51-1-9, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-21 AND DC8 SRM 51-4-4 PAGES 2 L 7 4 4F RT 4A25 2007030200031 20070302 00031 WP 2007 3 2 IXXA07SMN027S 1 20070113 A 5740 SUPPORT FITTING DOUG DC8 DC871F 302199D WP RT WING CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 46065 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING TRAPEZOIDAL FITTING CRACKED AT STATION 902.000. REMOVED DAMAGED TRA PEZOIDAL SUPPORT FITTING. INSTALLED NEW TRAPEZOIDAL SUPPORT FITTING IAW DOUGLAS DRAWINGS, NUMBER 5750127 AND NUMBER 575 0092, DC8 SRM 53-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-1-20D AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007030200036 20070302 00036 NM 2007 3 2 DU4R2007061 1 20070227 A 5300 SKIN DOUG MD80 MD83 3023681 NM BS 326-355 CORRODED B BWIA K NONE O OTHER IN INSP/MAINT 1 SO 15 789BV 49789 FOUND PREV REPAIRED AREA AT FS 332 TO FS 355 BETWEEN L-23L AND L-26L. REPAIRED BY REMOVING SECTION OF SKIN AND 2 EXISTI NG REPAIRS IAW DC-9/MD-80 SRM 53-04 FIG 12C. FABRICATED AND INSTALLED SKIN REPAIR 31.75 BY 25.5 FROM 2024-T3 .050, 3 SK IN REPAIRS 17.75 BY 5.5, 36.25 BY 9.5 AND 17.2 BY 5.25 FROM 2024-T3 .025 AND 6 SKIN REPAIRS 7 BY 5.5 BY, .7 BY 9.5, 4 B Y 5, 3.5 BY 5, 5.0 BY 5.5 AND 34.75 AND 5.5 IAW DC-9/MD-80 SRM 53-04. 2 L 7 2 4F RT 2007030200037 20070302 00037 NM 2007 3 2 DU4R2007063 1 20070227 A 5320 CUSP WEB DOUG MD80 MD83 3023681 NM BS 1135-1175 CORRODED B BWIA K NONE O OTHER IN INSP/MAINT 1 SO 15 789BV 49789 FOUND EXFOLIATED CORROSION AT LT O/B CUSP WEB FROM FS 1135 TO FS 1175. REPAIRED BY FABRICATING AND INSTALLING CUSP WEB REPAIR SECTION 4.5 BY 20.2 FROM 7075-T6 .063 IAW DC-9/MD-80 SRM 51-10-2, 51-10-3, 51-10-4 AND 53-14-3 FIG 12. 2 L 7 2 4F RT 2007030200038 20070302 00038 NM 2007 3 2 DU4R2007064 1 20070227 A 5320 CUSP WEB DOUG MD80 MD83 3023681 NM BS 1174-1193 CORRODED B BWIA K NONE O OTHER IN INSP/MAINT 1 SO 15 789BV 49789 FOUND CORRODED CUSP WEB AT LT O/B FS 1175. REPAIRED BY CUTTING OUT CORRODED SECTION FROM FS 1174 TO FS 1193. FABRICATE D AND INSTALLED REPAIR CUSP WEB 21 BY 15 FROM 7075-T6 .025 IAW MD-80 SRM 51-70-4. 2 L 7 2 4F RT 2007030500001 20070305 00001 WP 2007 3 5 IXXA070006S 1 20070213 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92358 2468 45813 LOWER D PIT DOOR HAS NON-STANDARD REPAIR PER AD2005-18-07 AND SB DC8-53-078. REMOVED EXISTING SKIN PANEL. LOCATED, DRIL LED, TRIMMED, TREATED AND PRIMED NEW SKIN PANEL, APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN PANEL AT LOWER D PIT DOOR FROM STATION 1350 TO STATION 1490 AND FROM LONGERON 31 LEFT TO LONGERON 31 RIGHT IAW DACO DC8 SRM 51-1-20, 51 -1-21, 51-1-5, 51-1-8, 51-1-11, 51-1-14, 51-1-15, 53-1-0 AND 53-4-0, OPS CHECK WITH PRESSURIZATION IAW DACO DC8 MM 21-22 -0. NO LEAKS NOTED. 2 L 7 4 4F RT 4A25 2007030500002 20070305 00002 NM 2007 3 5 NOCA02107 1 20070117 A 2612 710107 FIRE LOOP BOEING 767 767306 1385148 NM NR 2 ENGINE FAULTY A NOCA K NONE N FALSE WARNING UK UNKNOWN 1 EA 15 765NA 28098 RIGHT ENGINE FIRE LOOP STATUS MSG. REMOVED AND REPLACED LOWER FWD FIRE WARN ELEMENT ON NR 2 ENG PER MM 26-11-01. OPS C HECKS OK, CI CLEARED. 2 L 7 2 4F RT A1NM 2007030500003 20070305 00003 NM 2007 3 5 NOCA02207 1 20070112 A 7830 07482933M CDU BOEING 767 76739H 1385311 NM THRUST REVERSER CRACKED A NOCA K NONE J WARNING INDICATION LD LANDING 1 EA 15 760NA 26257 LEFT REV ISLN VALVE EICAS CAME ON, ON LANDING WITH LEFT ENG REV MESSAGE IN YELLOW STAYED ON. STATUS MESSAGE L REV ISLN VAL AND L REV INTERLOCK WAS ALSO DISPLAYED. VISUAL INSPECTION SHOW IB REV SHELL FULLY OPEN, FOUND CENTER DRIVE UNIT AND FOUND BACK HOUSING CRACKED. REMOVED AND REPLACED CENTER DRIVE IAW MM 78-31-21, OPS CHECKS GOOD. 2 L 7 2 4F RT A1NM 2007030500005 20070305 00005 NM 2007 3 5 NOCA02507 1 20070127 A 2611 033638 BLOWER BOEING 757 75728A 1384976 NM CARGO BAY FAILED A NOCA K NONE J WARNING INDICATION UK UNKNOWN 1 EA 15 750NA 26277 "AFT DET FAN" MAINTENANCE MESSAGE. REMOVED AND REPLACED THE AFT CARGO DET BLOWER ASSY PER AMM 21-16-01. OPS CHECKS OK. 2 L 7 2 4F RT A2NM 2007030500006 20070305 00006 NM 2007 3 5 NOCA02607 1 20070126 A 2720 3800022107 ACTUATOR BOEING 757 75728A 1384976 NM RUDDER MALFUNCTIONED A NOCA K NONE J WARNING INDICATION CR CRUISE 1 EA 15 752NA 28174 WHILE IN LEVEL CRUISE AT FL360 DURING LIGHT TO MODERATE TURBULENCE RUDDER RATION CAUTION LIGHT AND EICAS MSG APPEARED. PERFORMED FIM TASK 27-09-00 FIG 106B, FOUND LEFT AND RIGHT MODULES WITH PCA FAULTBALL. REMOVED AND REPLACED RUDDER RATI O CHARGER ACTUATOR PER AMM 27-71-13. OPS CHECKS OK. 2 L 7 2 4F RT A2NM 2007030500008 20070305 00008 NM 2007 3 5 NOCA02807 1 20070130 A 2760 285T0012201 CONTROL MODULE BOEING 757 75728A 1384976 NM SPOILER MALFUNCTIONED A NOCA K NONE J WARNING INDICATION UK UNKNOWN 1 EA 15 756NA 32448 SPOILER EICAS MESSAGE. FOUND SCM MS30 AT FAULT. REMOVED AND REPLACED SPOILER CONTROL MODULE PER MM 27-09-00. OPS CHEC KS OK, NO FAULTS NOTED. 2 L 7 2 4F RT A2NM 2007030500009 20070305 00009 NM 2007 3 5 NOCA02907 1 20070131 A 3610 7998014 SHUTOFF VALVE BOEING 767 767306 1385148 NM BLEED AIR SYS MALFUNCTIONED A NOCA K NONE J WARNING INDICATION UK UNKNOWN 1 EA 15 765NA 28098 LEFT REVERSER INTERLOCK STATUS MSG. REMOVED AND REPLACED NR 1 ENG PRSOV IAW MM 36-11-09. SYSTEM OPS CHECK OK. 2 L 7 2 4F RT A1NM 2007030500010 20070305 00010 NM 2007 3 5 NOCA03007 1 20070207 A 3350 S417T51013 LIGHT BOEING 767 767300 1385204 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 768NA 29898 MID GALLEY LT SIDE E-PATH LIGHT STRIP ONLY HALF IS ILLUMINATED. REMOVED AND REPLACED E-PATH LIGHT STRIP AS PER AMM 33-5 1-00. OPS CHECKS OK. 2 L 7 2 4F RT A1NM 2007030500012 20070305 00012 NM 2007 3 5 NOCA03207 1 20070203 A 3350 276005 FUSE BOEING 757 75728A 1384976 NM POWER SUPPLY BLOWN A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 756NA 32448 FOUND EMERGENCY EXIT FLOOR LIGHTING IS INOP FROM ROW 28ABC TO ROW 32ABC. REMOVED AND REPLACED THE POWER SUPPLY FUSE PER TASK 33-51-07-962-071. OPS CHECKS GOOD. 2 L 7 2 4F RT A2NM 2007030500013 20070305 00013 NM 2007 3 5 NOCA03407 1 20070207 A 3260 BAC27TEX1255 SENSOR BOEING 767 767300 1385204 NM NLG MALFUNCTIONED A NOCA K NONE N FALSE WARNING IN INSP/MAINT 1 EA 15 768NA 29898 LANDING GEAR MONITOR EICAS MESSAGE. REMOVED AND REPLACED NOSE GEAR DOOR SENSORS S234,S235 ADJUSTED NOSE GEAR DOOR AS PE R AMM 32-22-02. ACCOMPLISHED GEAR SWING NO EICAS MSG, FAULTS BITE CHECK PROX DET UNIT SHOWS NO FAULTS. 2 L 7 2 4F RT A1NM 2007030500014 20070305 00014 NM 2007 3 5 NOCA03507 1 20070208 A 3350 PBE3071 LIGHT BOEING 737 737300 1384610 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 768NA 29898 E-PATH LIGHT INOP AT SEAT 8A AND R2 DOOR CEILING INOP. REMOVED AND REPLACED EMERGENCY LIGHTS AT SEAT 8A AND R2 DOOR CEI LING PER AMM 33-51-00. OPS CHECKS OK. 2 L 7 2 4F RT A16WE 2007030500016 20070305 00016 NM 2007 3 5 NOCA03707 1 20070212 A 2421 729825H IDG BOEING 767 767300 1385204 NM NR 2 MALFUNCTIONED A NOCA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 768NA 29898 DURING PUSHBACK AND AFTER RT ENGINE START, RECEIVED R GEN OFF AND R GEN DRIVE LIGHT ON UPPER EICAS AND OVHD. REMOVED AN D REPLACED NR 2 IDG PER MM 24-11-01. OPS CHECKS OK. 2 L 7 2 4F RT A1NM 2007030500017 20070305 00017 2007 3 5 NOCA02307 4 20070126 A 2215 163200100 SERVO BOEING 757 75728A 1384976 NM AUTOPILOT MALFUNCTIONED A NOCA K NONE O OTHER UK UNKNOWN 1 EA 15 750NA 26277 LT AUTOPIOLOT DOES NOT ENGAGE. REMOVED AND REPLACED LEFT A/P SERVO, NO LEAKS NOTED. ACCOMPLISHED MCDP TEST AND CHECK G OOD. 2 L 7 2 4F RT A2NM 2007030500018 20070305 00018 EU 2007 3 5 07FDEA00491 1 20070215 A 5720 REPAIR AIRBUS 300 A300B4622R 3930312 EU WING UNKNOWN A FDEA O OTHER O OTHER UK UNKNOWN 1 SO 25 740FD 559 FOUND OLD REPAIR BY INSTALLATION OVERSIZE FASTENERS, HOLE 2 LT, 187 RT AND 165 RT. REPAIR VERIFICATION OF OVERSIZED FAS TENERS IAW RAS 033237/017/2004 ISSUE: A AND EA 6-5710-106363. 2 L 7 2 4F RT A35EU 2007030500019 20070305 00019 EU 2007 3 5 07FDEA00493 1 20070215 A 5720 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU WING DAMAGED A FDEA K NONE O OTHER UK UNKNOWN 1 SO 25 740FD 559 DAMAGED HOLES FOUND DURING ACCOMPLISHMENT OF EO 6-5710-7-3305, HOLES L/U/I/K ON LT AND K ON RT. REPAIR WAS PERFORMED IA W. RAS 033237/026/2004 ISSUE: A AND EA 6-5710-106351. 2 L 7 2 4F RT A35EU 2007030500020 20070305 00020 EU 2007 3 5 07FDEA00494 1 20070215 A 5720 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU WING DAMAGED A FDEA K NONE O OTHER UK UNKNOWN 1 SO 25 740FD 559 DAMAGED HOLES FOUND DURING ACCOMPLISHMENT OF EO 6-5710-7-3305. HOLES H/I ON LT AND L/K ON RT. REPAIR WAS PERFORMED IAW RAS 033237/026/2004 ISSUE: A AND EA 6-5710-106351. 2 L 7 2 4F RT A35EU 2007030500023 20070305 00023 NM 2007 3 5 DHL2007781003 1 20070215 A 5313 STRINGER BOEING 727 727227 1384078 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 781DH 21996 FWD CARGO COMPT, BS 555, AND BS 562, STR 28R, HAS EXFOLIATED CORROSION. CORROSION OUT OF LIMITS PER B727 SRM 53-10-1 FI G 1. GAINED ACCESS AS REQ TO FOM. CUT OUT DAMAGED MATERIAL APPROX 9", FABRICATED REPAIR SPLICE FROM BAC1498-131, 22" I N LENGTH, PO NR 9005866, PER B727 SRM 53-10-2 FIG 9 AND 51-10-3 FIG 1. TREATED AND PRIMED REPAIR PARTS/AREA, AND INSTAL LED STR REPAIR SPLICE PER B727 SRM 51-10-2, 53-10-3, AND 51-30-2. RETURNED AREA TO NORMAL. 2 L 7 3 4F A3WE 2007030500024 20070305 00024 NE 2007 3 5 07FDEA00492 2 20070215 A 7200 ENGINE AIRBUS 310 A310324 3930206 EU PWA 4152 PW4152 NE NR 2 UNKNOWN A FDEA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 25 806FD 458 717799 NR 2 ENG DOES NOT RESPOND TO THROTTLE MOVEMENT, ATS LEVER OFF. REPLACED NR 2 EEC PER MM 73-21-01-4-06 AND WAS NO HELP. CHECKED FADEC FAULTS AND HAD NONE. RAN ENGINE WITH NO EPR MODE FAULTS OR COMMAND POINT, ER FAULTS, ALL ENGINE INDICAT IONS GOOD. INSTALLED NEW TCC NO HELP REINSTALLED ORIGINAL. CHECKED PB SENSE LINE FOUND OK. FOUND TR SLEEVE POSITION A T 16. 1 PERCENT CHA AND 16.2 PERCENT CH B. ADDED MPN 3M3-212A. REINSTALLED ORIGINAL EEC ADJUSTED LT RVDT PER A310-300 MM 78-31-40-4 ENGINE RUN C/W PER JRH THROTTLE RESPONSE NORMAL. 2 L 7 2 4F RT A35EU E24NE 2007030500026 20070305 00026 NM 2007 3 5 TSAA0726012 1 20070211 A 2613 355992255 OVERHEAT LOOP BOEING 737 73776N 13844CH NM RT WING DEFECTIVE A TSAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 740AL 28640 FLT 484, OGG-SNA; RIGHT WING-TO-BODY OVERHEAT LIGHT CAME ON AT 8,000 FEET. FOLLOWED QRH PROCEDURES AND RETURNED TO OGG. UNEVENTFUL LANDING. REPLACED THE RIGHT WING LEADING EDGE OVERHEAT DETECTION LOOP M269. SYSTEM CHECK GOOD PER TASK 26 -18-00-810-801. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007030500027 20070305 00027 SO 2007 3 5 SIMA200705001 1 20070215 A 5320 14000492403 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 848AE 9680 4800 145710 FOUND FLOOR SUPPORT ON RIGHT SIDE CORRODED BETWEEN FRAME 22 AND FRAME 23. REMOVED AND REPLACED PANEL SUPPORT IAW EMB SR M 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007030500029 20070305 00029 SO 2007 3 5 SIMA200705003 1 20070215 A 5320 14522178005 SILL EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 848AE 9680 4800 145710 FOUND SERVICE DOOR SILL CORRODED. REMOVED AND REPLACED SERVICE DOOR SILL IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4F RT T00011AT 2007030500030 20070305 00030 EU 2007 3 5 07FDEA00510 1 20070216 A 5315 FLOORBEAM AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 FOUND CORROSION IN AND AROUND FASTENER HOLE FR55/58 LT SIDE AFT CARGO COMPARTMENT MDCC FLOORBEAM. REMOVED CORROSION IAW A310-200 SRM 51-74-10 AREA WENT OUT OF LIMITS IAW A310-200 SRM 53-10-15. INSTALLED FABBED REPAIR ANGLE PARTS IAW A310- 200 SRM 53-10-15. ALODINED, PRIMED AND TOP COATED PARTS IAW A310-200 SRM 51-75-10. 2 L 7 2 4F RT A35EU 2007030500032 20070305 00032 EU 2007 3 5 07FDEA00512 1 20070216 A 5315 FLOORBEAM AIRBUS 310 A310222 3930315 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 FOUND FWD CARGO COMPT, FR36 FLOORBEAM LBL 66 (1) EA CRACK IN RADIUS 0.380 INCH LENGTH. REPAIRED FLOORBEAM FR36 LBL66 IA W A310-200 SRM 53-10-15 PB 201 FIG 201. 2 L 7 2 4F RT A35EU 2007030500033 20070305 00033 EU 2007 3 5 07FDEA00513 1 20070216 A 5315 FLOORBEAM AIRBUS 310 A310222 3930315 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 FOUND FWD CARGO COMPT, FS 38, FLOORBEAM, LBL66, (1) EA CRACK IN RADIUS 0.380 INCH LENGTH. REPAIRED FLOORBEAM PER A310-2 00 SRM 53-10-15. 2 L 7 2 4F RT A35EU 2007030500034 20070305 00034 EU 2007 3 5 07FDEA00514 1 20070216 A 5347 SEAT TRACK AIRBUS 310 A310222 3930315 EU FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 MDCC SEAT TRACK HAS 1 AREA GOUGED, 1 PREVIOUS REPAIR AND 6 SPOTS OF CORROSION BETWEEN FR 58-72. REMOVED SEAT TRACK IAW A310 SRM 51-72-10. FABBED REPLACEMENT SEAT TRACK IAW A310 SRM 53-10-16 AND AIRBUS DWG A53278820. INSTALLED REPLACEMENT SEAT TRACK IAW A310 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007030500037 20070305 00037 EU 2007 3 5 07FDEA00517 1 20070216 A 5540 MS1410316 BEARING AIRBUS 310 A310222 3930315 EU RUDDER EXCESS PLAY A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 NR 3 RUDDER HINGE ARM HAS 1 BEARING WITH PLAY (ZONE 320) REMOVED BEARING AND BUSHING ARM AS PER AIRBUS A310 SERVICE BUL LETIN A310-55-2025. INSTALLED BEARING AND BUSHING IAW AIRBUS PMS 01-05-58 AND EA 6-5530-107658. 2 L 7 2 4F RT A35EU 2007030500038 20070305 00038 NM 2007 3 5 AALA20070318 1 20070210 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHTS AT SEAT 23C HAS LENS MISSING. RELAMPED AND REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23C. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007030500039 20070305 00039 EU 2007 3 5 AALA20070325 1 20070211 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80084 675 MIA - EMERGENCY LIGHTS AT SEAT 18G INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 18G. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007030500040 20070305 00040 NM 2007 3 5 AALA20070338 1 20070215 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 782AN 30003 DFW - FOUND EMERGENGY LIGHT AT CENTER GALLEY CEILING INOPERATIVE. RELAMPED EMERGENCY LIGHT AT CENTER GALLEY CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007030500041 20070305 00041 WP 2007 3 5 AALA20070343 1 20070216 A 3222 SEAL DOUG DC9 DC982 3022082 WP NLG STRUT INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 466AA 49596 ORD INFLIGHT - NOSE GEAR WOULD NOT RETRACT. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED NOSE STRUT SEAL AND S ERVICED NOSE STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007030500043 20070305 00043 NM 2007 3 5 AALA20070295 1 20070204 A 3350 3168593 LENS BOEING 767 767323 1385205 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 379AA 25448 MIA - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR SLIDE HAS LENS COVER MISSING. REPLACED LENS FOR EMERGENCY LIGHT AT LEFT N UMBER ONE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007030500044 20070305 00044 EU 2007 3 5 AALA20070296 1 20070206 A 3350 BR964814 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14068 511 MIA - FOUND EMERGENCY LIGHT AT SEAT 22C IS BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007030500045 20070305 00045 NE 2007 3 5 AALA20070316 2 20070211 A 7310 FUEL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE CENTER TANK CONTAMINATED A AALA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 SW 21 110HM 49787 DFW INFLIGHT SAT-ORD, AFT CENTER FUEL BOOST PUMP CIRCUIT BREAKER POPPED. UNABLE TO TRANSFER FUEL FROM CENTER TANK. LAN DED DFW WITHOUT INCIDENT. SUMPED THREE GALLONS OF WATER OUT OF CENTER TANK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A6WE E9NE 2007030500046 20070305 00046 NM 2007 3 5 AALA20070313 1 20070210 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 389AA 27449 MIA - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007030500047 20070305 00047 NM 2007 3 5 AALA20070351 1 20070217 A 3350 OL1098BPEGPL LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 335AA 22333 JFK - EMERGENCY LIGHT AT SEAT 2B INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 2B. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F RT A1NM 2007030500048 20070305 00048 EU 2007 3 5 AALA20070344 1 20070216 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 90070 513 MIA - EMERGENCY LIGHTS FROM SEAT ROWS 7C TO 18C INOPERATIVE. RECHARGED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT ROWS 7C TO 18C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007030500050 20070305 00050 WP 2007 3 5 AALA20070350 1 20070216 A 2560 BATTERY DOUG DC9 DC982 3022082 WP FLASHLIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 253AA 49286 SFO - EMERGENCY FLASHLIGHT AT FORWARD LEFT DOOR INOPERATIVE. REPLACED BATTERY IN EMERGENCY FLASHLIGHT AT FORWARD LEFT D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007030500052 20070305 00052 EA 2007 3 5 TRAX200700279 1 20070221 A 3250 STEERING SYS CNDAIR CL600 CL6002C10 1390015 EA NLG INOPERATIVE A ASOA K NONE J WARNING INDICATION CL CLIMB 1 SO 27 744EV 10157 FOUND NOSE WHEEL STEERING INOP MSG AFTER TAKEOFF, EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007030500054 20070305 00054 EA 2007 3 5 TRAX200700262 1 20070220 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 FOUND LT AND RT CABIN FLOOR SEAT TRACKS CORRODED AT FS 559+112. 2 L 7 2 4F RT A21EA 2007030500055 20070305 00055 EA 2007 3 5 TRAX200700263 1 20070220 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 FOUND LT AND RT CABIN FLOOR SEAT TRACKS CORRODED AT FS 559+80. 2 L 7 2 4F RT A21EA 2007030500061 20070305 00061 EU 2007 3 5 TRAX200700269 1 20070220 A 3350 LIGHT AEROSP ATR72 ATR72212 8680945 EU CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 ON TAXI OUT, FIRST HALF OF EMERGENCY FLOOR TRACK LIGHTING WILL NOT EXTINGUISH, GATE RETURN. FLT 4582 DEL 180 MINS. 2 H 7 2 4T RT A53EU 2007030500065 20070305 00065 EA 2007 3 5 TRAX200700273 1 20070221 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 FOUND CLIP CRACKED AT FS 484 AT LBL36. 2 L 7 2 4F RT A21EA 2007030500066 20070305 00066 EA 2007 3 5 TRAX200700274 1 20070221 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 FOUND CLIP CRACKED AT FS 484 AT RBL 36. 2 L 7 2 4F RT A21EA 2007030500067 20070305 00067 EA 2007 3 5 TRAX200700278 1 20070221 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 FOUND CARGO DOOR TRACK UPPER BEAM AFT CLIP CRACKED AT FS 621. 2 L 7 2 4F RT A21EA 2007030500068 20070305 00068 EA 2007 3 5 TRAX200700252 1 20070220 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 FOUND CORROSION ON FRAME 280 FWD ANGLE. REMOVED 280 FWD FLOOR SUPPORT ANGLE. BLENDED CORROSION ON FWD SIDE OF 280. BLEND ED AREA IS OUT OF LIMITS MORE THAN 10% OF MATERIAL WAS REMOVED. PER CRJ200 SRM 53-00-31. CM20420. 2 L 7 2 4F RT A21EA 2007030500070 20070305 00070 EA 2007 3 5 TRAX200700254 1 20070220 A 5311 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 FOUND POSSIBLE CRACK ON RT 640 FRAME DOUBLER NEEDS NDT. 2 L 7 2 4F RT A21EA 2007030500071 20070305 00071 EA 2007 3 5 TRAX200700255 1 20070220 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 FOUND RT WHEEL WELL BATT RIB CRACKED. REPAIRED IAW ALL FAA STANDARDS. 2 L 7 2 4F RT A21EA 2007030500072 20070305 00072 EA 2007 3 5 TRAX200700256 1 20070220 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 FOUND LT WHEEL WELL BATTERY RIB CRACKED. REPAIRED IAW REO 601R-57-51-046. 2 L 7 2 4F RT A21EA 2007030500073 20070305 00073 EA 2007 3 5 TRAX200700257 1 20070220 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 FOUND RT CABIN FLOOR SEAT RAIL CORRODED FROM FS 364 TO FS 394. 2 L 7 2 4F RT A21EA 2007030500075 20070305 00075 EA 2007 3 5 TRAX200700259 1 20070220 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 FOUND RT CABIN FLOOR SEAT TRACK CORRODED AT FS 409+64. 2 L 7 2 4F RT A21EA 2007030500077 20070305 00077 NM 2007 3 5 AWXA200700301 1 20070224 A 5320 69169707 ATTACH FITTING BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED INTERCOSTAL ATTACH CLIP,BS 348.2, S15L. REPLACED INTERCOSTAL ATTACH CLIP, BS 348.2, S15L IAW AWA ER 03-5312-07054-HF4. 2 L 7 2 4F RT A16WE 2007030500080 20070305 00080 NM 2007 3 5 AWXA200700304 1 20070125 A 5330 6545775594 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND FUSELAGE SKIN CRACKED, BS 727D +3", S23R. REPAIRED FUSELAGE SKIN, BS 727D +3", S23R IAW AWA ER 03-5361-0705 3-HF2. 2 L 7 2 4F RT A16WE 2007030500081 20070305 00081 NM 2007 3 5 AWXA200700305 1 20070131 A 5320 69265552 FITTING BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED INTERCOSTAL UPPER CLIP, BS 348.2, S16L. REPLACED INTERCOSTAL UPPER CLIP, BS 348.2, S16L IAW AWA ER 03-5312-07054-HF4. 2 L 7 2 4F RT A16WE 2007030500082 20070305 00082 NM 2007 3 5 AWXA200700306 1 20070131 A 5320 65176856 STRAP BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED INTERCOSTAL STRAP, BS 348.2, S16L. REPLACED INTERCOSTAL STRAP, BS 348.2, S16L IAW AWA ER 03-5312-07 054-HF4. 2 L 7 2 4F RT A16WE 2007030500083 20070305 00083 NM 2007 3 5 AWXA200700269 1 20070216 A 5320 654797321 WEB BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND CRACKED WEB, BS 639, LBL 65, WL 208. REPLACED WEB, BS 639, LBL 65, WL 208 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007030500087 20070305 00087 NM 2007 3 5 AWXA200700273 1 20070217 A 5322 69353663 ATTACH ANGLE BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND SEAT TRACK ATTACH ANGLE CRACKED, BS 520, RBL 24.75. REPLACED SEAT TRACK ATTACH ANGLE, BS 520, RBL 24.75 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007030500089 20070305 00089 NM 2007 3 5 AWXA200700275 1 20070119 A 5310 65458076 DOOR FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND R1 DOOR CUT OUT FORWARD UPPER FRAME CRACKED, BS 294, S8L - S10L. REPLACED R1 DOOR CUT OUT FORWARD UPPER FRA ME, BS 294, S8L - S10L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007030500090 20070305 00090 NM 2007 3 5 AWXA200700276 1 20070212 A 5330 65C3579021 DOUBLER BOEING 737 7373S3 1384711 NM FUSELAGE DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND DEBONDED FUSELAGE SKIN INTERNAL BONDED DOUBLER, BS 675, S1R - S2R. REPAIRED FUSELAGE SKIN INTERNAL BONDED D OUBLER, BS 675, S1R - S2R IAW B737-300 SRM 53-00-01-2R-25. 2 L 7 2 4F RT A16WE 2007030500092 20070305 00092 NM 2007 3 5 AWXA200700281 1 20070131 A 5340 69353521 STRINGER CLIP BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CORROSION CRACK ON STRINGER TIE CLIP, BS 847, S25R. REPLACED STRINGER TIE CLIP, BS 847, S25R IAW B737-300 S RM 51-40-02. 2 L 7 2 4F RT A16WE 2007030500094 20070305 00094 EU 2007 3 5 AWXA200700238 1 20070216 A 5320 D53472172204 BEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 652AW 953 SAL- MAJOR REPAIR - FOUND CORROSION ON MAIN CABIN LONGITUDINAL BEAM, +Y1292, FR 66 +5" - FR 67 + 15". REPLACED MAIN CAB IN LONGITUDINAL BEAM, +Y1292, FR 66 +5" - FR 67 + 15" IAW A320 SRM 51-72-11 PAGE 1 AND 2. 2 L 7 2 4F RT A28NM 2007030500095 20070305 00095 EU 2007 3 5 AWXA200700239 1 20070218 A 5340 D53112198200 FITTING AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 652AW 953 SAL- MAJOR REPAIR - BC-6 CHECK - FOUND CORROSION ON L1 DOOR CUT OUT FLOOR LEVEL CENTRAL FITTING, FR 16 - FR 20, S-23L. REPLACED L1 DOOR CUT OUT FLOOR LEVEL CENTRAL FITTING, FR 16- FR 20, S-23L, IAW A320 SDR 51-42-11 AND 51-72-11. 2 L 7 2 4F RT A28NM 2007030500096 20070305 00096 EU 2007 3 5 AWXA200700241 1 20070218 A 5320 D53471124201 SHEAR PLATE AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 652AW 953 SAL- MAJOR REPAIR- BC-6 CHECK- FOUND CORROSION ON RIGHT CABIN FLOOR SHEAR PLATE, FR 69 - FR 70, S-23R. REPLACED RIGHT C ABIN FLOOR SHEAR PLATE, FR 69 - FR 70, S-23R IAW A320 SRM 51-71-11, PAGE 1-2 AND 51-42-11 PAGE 23, FIG 8. 2 L 7 2 4F RT A28NM 2007030500098 20070305 00098 EU 2007 3 5 AWXA200700243 1 20070215 A 5321 D5361060500000 FLOORBOARD AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 652AW 953 SAL- MAJOR REPAIR - FOUND CORROSION ON MAIN CABIN FLOORBOARD 221FF, FR 16 - FR 20, +Y1292 TO +Y1732. REPLACED MAIN CABI N FLOORBOARD 221FF, FR 16 - FR 20, +Y1292 TO +Y1732, IAW A320 ARM 51-72-11 AND AWA TASK CARD CIC53302. 2 L 7 2 4F RT A28NM 2007030500101 20070305 00101 NM 2007 3 5 AWXA200700309 1 20070201 A 5320 6517684642 INTERCOSTAL BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED INTERCOSTAL, BS 294.5, S7L. REPLACED INTERCOSTAL, BS 294.5, S7L IAW AWA ER 03-5312-07054-HF4. 2 L 7 2 4F RT A16WE 2007030500103 20070305 00103 NM 2007 3 5 AWXA200700311 1 20070131 A 5320 69165096 FITTING BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED INTERCOSTAL CLIP, BS 348.2, S16L. REPLACED INTERCOSTAL CLIP, BS 348.2, S16L IAW AWA ER 03-5312-0754 -HF4. 2 L 7 2 4F RT A16WE 2007030500105 20070305 00105 NM 2007 3 5 AWXA200700313 1 20070131 A 5320 69489856 FITTING BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED INTERCOSTAL CLIP, BS 360, S11L. REPLACED INTERCOSTAL CLIP, BS 360, S11L IAW AWA ER 03-5312-0754-HF4 . 2 L 7 2 4F RT A16WE 2007030500108 20070305 00108 NM 2007 3 5 CALA0700101 1 20070228 A 5330 654577678 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 A 3 INCH CRACK LOWER AFT FUSELAGE STA 727D AND 727E. REPAIRED IAW ECRA5331-01292. 2 L 7 2 4F RT A16WE 2007030500110 20070305 00110 NM 2007 3 5 CALA0700103 1 20070301 A 5210 507945178 BEAM BOEING 737 7373T0 1384582 NM L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 CRACKED L1 DOOR AFT SIDE OF THE THIRD FROM BOTTOM DOOR STOP CUTOUT. REPAIRED IAW ECRA 5210-01919. 2 L 7 2 4F RT A16WE 2007030500113 20070305 00113 NM 2007 3 5 CALA0700106 1 20070228 A 5220 SPRING BOEING 767 767424ER 1385270 NM EMERGENCY EXIT DEFECTIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69063 29458 L3 EMERGENCY DOOR INTERIOR HANDLE CANNOT MOVE BACK AGAINST THE DOOR LININIG. REPLACED DOOR ASSIST SPRING IAW AMM 52-22- 01. 2 L 7 2 4F RT A1NM 2007030500114 20070305 00114 2007 3 5 CALA0700107 4 20070228 A 2565 60176103 LOCK PIN BOEING 767 767424ER 1385270 NM EVAC SLIDE DETACHED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69063 29458 L3 EMERGENCY DOOR SLIDE BATTERY RED COUR LOCK PIN DETACHED. REPLACE SLIDE IAW AMM 36-66-10 2 L 7 2 4F RT A1NM 2007030100014 20070301 00014 NM 2007 3 1 2007UALA00507 1 20070217 A 3397 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 659UA 27114 FOUND RT SEATS 29FG-35FG EEL LIGHTS INOP. FOUND FEEDER CABLE CONNECTING TO EEL TRACK LOOSE. RECONNECTED CABLE. OPS CH ECKS NORMALLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007030100016 20070301 00016 EA 2007 3 1 COMA0760205 1 20070222 A 3250 STEERING SYS CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 920CA 7022 FLIGHT 5111 - STEERING INOP CAUTION MESSAGE DURING TAKEOFF, ABORTED TAKEOFF AT 70 KTS. PERFORMED OPS CHECK AND RESET OF NWS, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007030100022 20070301 00022 NM 2007 3 1 2007UALA00510 1 20070217 A 3350 SIGN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 FOUND DOORS 4R 4L EMERGENCY EXIT SIGNS ARE DAMAGED. DOOR 4R EXIT LIGHT COVER MISSING AT POSITIONS FORE & AFT OF DOOR A T KNEE LEVEL. REPLACED BOTH EEL LIGHT LENS. COVERS ALSO MISSING FROM DR-4L LOWER AFT SIGN. LENS REPLACED ON LEFT SIDE AS WELL. A/C RETURNED TO NORMAL SERVICE. SUSPECT IMPACTS W/ GND EQUIP. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007030100033 20070301 00033 NM 2007 3 1 2007UALA00519 1 20070219 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 122UA 29168 FOUND EMERGENCY CEILING LIGHT ROWS 39 AND 58 RT INOPERATIVE. RELAMPED CEILING LIGHTS, BOTH POSITIONS. OP CHECKED N ORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030100039 20070301 00039 NM 2007 3 1 2007UALA00524 1 20070217 A 3350 LAMP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 226UA 30226 FOUND SEAT 2F (AFT) AND SEAT 3F AISLE EMERGENCY EVACUATION LIGHTS ARE NOT WORKING. REPLACED LAMP. OP CHECKED OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007030100045 20070301 00045 NM 2007 3 1 2007UALA00529 1 20070219 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 34 LT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 127UA 28813 FOUND EEL STRIP BROKEN, LIGHT INOP AFT OF SEAT ROW 34 LT. REPLACED EEL STRIP, OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030100052 20070301 00052 NM 2007 3 1 2007UALA00534 1 20070219 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1420 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 FOUND AFT PIT STA 1420 AND STR 26L, FRAME UPPER FLANGE IS DENTED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED A NEW PRODUCTION SPLICE ANGLE REPAIR. THIS REPAIR IS TIME LIMITED FOR 12 MONTHS FROM 13FEB07. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030100055 20070301 00055 NM 2007 3 1 2007UALA00535 1 20070219 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1681 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 FOUND CABIN FRAME INBOARD CHORD CORRODED AT BS 1681.8 AND RBL 57. MAJOR REPAIR ACCOMPLISHED. FABRICATED REPAIR DOUBLE R, FILLER AND STRAP. THIS REPAIR IS TIME LIMITED FOR 12 MONTHS FROM 16FEB07. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030100057 20070301 00057 NM 2007 3 1 2007UALA00537 1 20070219 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 646 S0-1R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 FOUND UPPER CROWN, BS 646 BETWEEN STR 0 AND 1R HAS STATIC DISCHARGE AROUND FASTENER AND BLEND OUT EXCEEDS LIMITS. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED A REPAIR DOUBLER. THIS REPAIR IS TIME LIMITED FOR 12 MONTHS FROM 18FEB0 7. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030100060 20070301 00060 NM 2007 3 1 UPS07M49238 1 20070117 A 5730 DOUBLER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C LEFT L/E COMPT UPPER DOUBLER PANEL CRACKED AS MARKED APPROX STA XORS 562. LEFT L/E COMPT UPPER DOUBLE R PNL FASTENERS REMOVED PER SRM 51-31-01 VOL II R.38. REPAIR DOUBLER FABRICATED & HOLES DRILLED PER SRM 57-10-00 FIG 25 8 TEMP R.57-5. VISUAL INSP CARRIED OUT 'OK' TO INSTALL PARTS. REPAIR PARTS INSTALLED AT LEFT L/E COMPT APPROX STA XORS 562 PER SRM 57-10-00 FIG 258 TEMP R.57-5. FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007030100072 20070301 00072 NM 2007 3 1 SWAA071088 1 20070223 A 3350 10107451 SIGN BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 701GS 27836 FWD CABIN EMERGENCY EXIT SIGN MISSING. INSTALLED EMERGENCY EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007030100073 20070301 00073 NM 2007 3 1 SWAA071100 1 20070224 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 241WN 32504 DURING SCHEDULED MV1 CHECK, FOUND EEPLS COVER MISSING AT ROW 7 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007030100078 20070301 00078 NM 2007 3 1 2007UALA00547 1 20070222 A 2910 BLADE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE RAT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 814UA 862 FOUND RAM AIR TURBINE BLADE HAS DAMAGE AND BLADE MATERIAL PEELED BACK. [SUP 05-16-07] RAT WAS DEPLOYED FOR MAINTENANCE 3 SEGMENTS PRIOR IN LAX AND DID NOT HAVE ANY DAMAGE NOTED AT THAT TIME. DAMAGE TO TURBINE BLADE WAS DISCOVERED PRIOR TO AN AD RELATED INSPECTION IN BOS AND RAT WAS REPLACED. SUSPECT DAMAGE TO TURBINE BLADE WAS INCURRED DURING STOWAGE POST LAX MAINTENANCE ACTIVITY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007030100082 20070301 00082 NM 2007 3 1 2007UALA00549 1 20070220 A 3350 BATTERY PACK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 812UA 850 FOUND EEL LIGHTS DIM IN FWD PART OF CABIN, TESTED AT FWD FLT ATTN PANEL MSG. EPSU BATTERY EMER R. REPLACED BATTERY PACK AT RT OVERWING FLOOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007030100103 20070301 00103 NM 2007 3 1 SWAA071105 1 20070225 A 5330 65C381921 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007030100108 20070301 00108 2007 3 1 SWAA071087 4 20070223 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007030100111 20070301 00111 NM 2007 3 1 2007UALA00565 1 20070221 A 3350 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 334UA 24229 FOUND RIGHT OVERWING EMERGENCY LIGHT AND ICE DETECTION LIGHT ASSEMBLIES ARE INOP. CLEANED AND ADJUSTED CONTACTS. RELAMPE D. 2 L 7 2 4F 4 F RT A16WE E21EU 2007030100118 20070301 00118 NM 2007 3 1 UIEA20070067 1 20070205 A 5730 SKIN BOEING 747 747341 13848AM NM RT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 RIGHT WING LOWER SKIN FOUND WITH CORROSION JUST INBOARD OF OUTBOARD MIDSPAR FUSE PIN FITTING OF NR 4 PYLON. CORROSION O N SAID WING LOWER SKIN REMOVED PER SRM 51-10-00. HFEC ACCOMPLISHED, NO DEFECTS. SKIN SHOT PEENED AND REPROTECTED. 2 L 7 4 4F RT A20WE 2007030100120 20070301 00120 NM 2007 3 1 UIEA200700091 1 20070226 A 2420 705117 CSD BOEING 747 7472D7B 1384803 NM NR 3 ENGINE LEAKING A UIEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 15 523MC 21782 DIVERSION TO JFK WHILE AIRCRAFT WAS EN ROUTE TO PIK FROM CHS. AT LEVEL OFF AT FL 33.0 #3 ENGINE OIL QTY DROPPED TO 2 GA LLONS. 15 MIN LATER DROPPED TO 0.5 GALLONS. ENGINE POWER REDUCED TO IDLE. REINSTALLED PREVIOUSLY DEFERRED GENERATOR AN D REPLACED THE CSD. 2 L 7 4 4F RT A20WE 2007030100132 20070301 00132 NM 2007 3 1 AWXA200700278 1 20070225 A 2560 P2070001214 FLASHLIGHT BOEING 737 7373G7 1384595 NM FWD CABIN FAILED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 DFW - FOUND FORWARD LEFT ENTRY EMERGENCY FLASHLIGHT, NO LED INDICATION. MX REPLACED THE FORWARD LEFT ENTRY EMERGENCY FL ASHLIGHT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2007030100166 20070301 00166 NM 2007 3 1 HALA0700055 1 20070225 A 2612 CIRCUIT CARD BOEING 767 767300 1385204 NM LT ENG FIRE LOOP MALFUNCTIONED A HALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 13 586HA 24259 L ENG FIRE LOOP 2 EICAS MESSAGE. CHECKED ALL ENGINE CONNECTORS FOR SECURITY AND FOUND TO BE NORMAL AND TROUBLESHOT PER FIM 26-11-00. RESEATED CARD M683. NO FURTHER DISCREPANCIES NOTED ALL NORMAL PER FIM 26-11-00. 2 L 7 2 4F RT A1NM 2007030100168 20070301 00168 NM 2007 3 1 USAA070140 1 20070226 A 5320 WEB BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 847 & 867 BETWEEN STR 26R & 25R HAS CORROSION. REMOVED DAMAGE & INSTALLED FAB'D REPAIR PARTS PER SRM 53-60-53, 51-1 0-02, CORR LEVEL 2; TASK C53-202, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007030100196 20070301 00196 NM 2007 3 1 HALA0700063 1 20070224 A 3397 WIRE BOEING 767 767300 1385204 NM EMERGENCY LIGHTS EXPLODED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 586HA 24259 FOUND MID GALLEY FLOOR LIGHTS HAS WIRE EXPOSED. REPLACED MID GALLEY EMERGENCY LIGHT TRACK COVER. OPS CHECK OK. 2 L 7 2 4F RT A1NM 2007030100198 20070301 00198 NE 2007 3 1 HALA0700065 2 20070223 A 7200 285T045812 CIRCUIT CARD BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE MALFUNCTIONED A HALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 594HA 23275 UNABLE TO START NR 2 (RIGHT) ENGINE. START SWITCH WILL NOT ENGAGE INTO GNG POSITION. REPLACED RT N2 SPEED CARD PER AMM 73-21-54, OPS CHK GOOD ON GROUND RUN. 2 L 7 2 4F 4 F RT A1NM E24NE 2007030100204 20070301 00204 SO 2007 3 1 O2G2007F00000 1 20070117 A 5230 2677TR4TT2 CHECK VALVE GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU CARGO DOOR FAILED E O2GA B EMER. DESCENT O OTHER CR CRUISE 1 EA 63 917W 1158 AT 43,000 FT THE AIRCRAFT WOULD NOT MAINTAIN PRESSURIZATION, CREW TOOK AIRCRAFT DOWN TO 22,000 FT AND MAINTAIN AT 8.6. REMOVED AND REPLACED BAGGAGE DOOR SEAL CHECK VALVE. (K) 2 L 7 2 4F 4 F RT A12EA E25NE 2007030100210 20070301 00210 NM 2007 3 1 AWXA200700299 1 20070120 A 5311 6545801512 FRAME BOEING 737 73733A 1384673 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CORROSION ON FUSELAGE SKIN FRAME, BS 225 - BS 227, S27R - S28R. REPAIRED FUSELAGE SKIN CHORD, BS 225 - BS 2 27, S27R - S28R IAW B737-300 SRM 51-70-12. 2 L 7 2 4F RT A16WE 2007030100219 20070301 00219 SO 2007 3 1 SIMA200705711 1 20070223 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A SIMA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 660CL 145764 AFTER NUMBER 2 ENGINE START RECEIVED ELECTRICAL ABNORMAL MESSAGE FOLLOWED WITH A STRONG ELECTRICAL SMELL. CLEARED APU F AULTS AND TESTED ALL AIRCRAFT ELECTRICAL SYSTEMS IAW EMB AMM 24-31-00 WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVI CE. 2 L 7 2 4T RT T00011AT 2007030100220 20070301 00220 SO 2007 3 1 SIMA200705709 1 20070224 A 5320 14525480603 SILL EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 804AE 13150 4800 145487 FOUND CARGO DOOR FRAME LOWER SILL CORRODED. REMOVED AND REPLACED SILL. CLEANED, TREATED AND RESTORED PROTECTIVE FINISH IAW EMB SRM 51-20-03, 51-40-03 AND 51-40-06. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007030100237 20070301 00237 2007 3 1 QXEA200700241 4 20070222 A 3420 IRS DHAV DHC8 DHC8202 2809007 NM COCKPIT OUT OF ALIGNMENT A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 352PH 494 PDX FLIGHT NR 2149 - ATTITUDE AND HEADING FAIL MESSAGES IN HDG. MAINTENANCE REALIGNED IRS BYU POWERING DOWN AIRCRAFT, P OWER UP CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030200004 20070302 00004 NM 2007 3 2 SWAA071114 1 20070226 A 3350 101114 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED SPV CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007030200009 20070302 00009 WP 2007 3 2 IXXA07SMN083S 1 20070131 A 5710 VANE DOUG DC8 DC871F 302199D WP ZONE 500 MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LEADING EDGE SLOT VANE HAS A NON STANDARD REPAIR FROM STATION XFS521. 000 TO STATION XFS527.000. REMOVED EXISTING NON STANDARD REPAIRS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND, AFTER DAMAGE REMOVAL. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-1-20D, DC8 SRM 51-3-1 AND SEMAN DRAWING NUMBER ED-4437 DAT ED 01-17-07. COMPLETED FAA FORM 8110-3 NUMBER 07019 DATED 01-18-07. 2 L 7 4 4F RT 4A25 2007030200011 20070302 00011 NM 2007 3 2 SWAA071111 1 20070226 A 5311 6517684 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR CUTOUT FWD FRAME CRACKED AT BS 303, STR 16L. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007030200013 20070302 00013 NM 2007 3 2 SWAA071107 1 20070226 A 5330 6545768 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 376, STR 14L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007030200017 20070302 00017 NM 2007 3 2 SWAA071120 1 20070226 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030200032 20070302 00032 NM 2007 3 2 P5CA0701510 1 20070213 A 5720 65B2285814 SUPPORT TUBE BOEING 747 74746NF 13848BT NM FUEL ACCESS DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 451PA 30809 LT WING FIXED L/E PANEL DAMAGED AT REFUEL ACCESS PANEL DOOR. REPLACED FIXED L/E SUPPORT RODS FORWARD OF REFUEL PANEL DO OR. ACCOMPLISHED TIME LIMITED, INTERIM REPAIR TO SKIN AND RIB IAW MA A4 57-41-01:01. 2 L 7 4 4F RT A20WE 2007030200039 20070302 00039 NM 2007 3 2 DU4R2007065 1 20070227 A 5340 ANGLE DOUG MD80 MD83 3023681 NM BS 1155-1175 MISINSTALLED B BWIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 15 789BV 49789 FOUND INTERCOSTAL 22 IMPROPERLY FITTED FS 1155 TO FS 1175 LT. REPAIRED BY REMOVING ANGLE, TRIMMED REPAIR ANGLE 13-1/4 B Y 3/4 BY 2-3/4 FROM 7075-T6 .071 AND INSTALLED IAW MD-80 SRM 51-30-2, 51-70-5 FIG 1. 2 L 7 2 4F RT 2007030500036 20070305 00036 EU 2007 3 5 07FDEA00516 1 20070216 A 5347 SEAT TRACK AIRBUS 310 A310222 3930315 EU FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 GOUGE FOUND ON SEAT TRACK NR 5 ZONE 231 LT SIDE BETWEEN FRAME 18 AND 20. REPAIRED SEAT TRACK PER A310 SRM 53-10-16. 2 L 7 2 4F RT A35EU 2007030500057 20070305 00057 EA 2007 3 5 TRAX200700265 1 20070220 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 FOUND LT CABIN SIDEWALL SEAT TRACKS HAVE MINOR CORROSION IN SEVERAL LOCATIONS AS MARKED. 2 L 7 2 4F RT A21EA 2007030500059 20070305 00059 EA 2007 3 5 TRAX200700267 1 20070220 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 FOUND FRAME AT FS 349.00 FRONT AND BACK CORRODED BETWEEN STR 26L-26R. 2 L 7 2 4F RT A21EA 2007030500060 20070305 00060 EA 2007 3 5 TRAX200700268 1 20070220 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 885AS 7521 FOUND LT AFT EXT O/W EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007030500076 20070305 00076 EA 2007 3 5 TRAX200700260 1 20070220 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 FOUND RT CABIN FLOOR SEAT TRACK CORRODED AT FS 439. 2 L 7 2 4F RT A21EA 2007030500084 20070305 00084 NM 2007 3 5 AWXA200700270 1 20070213 A 5311 6546561509 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND R-2 DOOR CUTOUT UPPER FORWARD STUB FRAME CRACKED, BS 927 - BS 947.5, S8R - S10R, WL 265. REPLACED R-2 DOOR CUTOUT UPPER FORWARD STUB FRAME, BS 927 - BS 947.5, S8R - S10R, WL 265 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007030500091 20070305 00091 NM 2007 3 5 AWXA200700277 1 20070127 A 5414 311A102311 SKIN BOEING 737 7373S3 1384711 NM LT PYLON CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND LEFT PYLON ACCESS PANEL NR 5727L, CUT OUT LAND CRACKED, NAC STATION 254. REPAIRED LEFT PYLON ACCESS PANEL N R 5727L, CUT OUT LAND, NAC STATION 254 IAW AWA ER 03-5433-00340-DL1 AND SB 737-54-1035. 2 L 7 2 4F RT A16WE 2007030500097 20070305 00097 EU 2007 3 5 AWXA200700242 1 20070219 A 5340 D53112198201 FITTING AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 652AW 953 SAL-MAJOR REPAIR- BC-6 CHECK- FOUND CORROSION ON CENTRAL FITTING AROUND R1 DOOR CUT OUT FLOOR LEVEL, FR 16 - FR 20, S23R . REPLACED CENTRAL FITTING ON R1 DOOR CUT OUT FLOOR LEVEL, FR16 - FR20, S23R IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007030500099 20070305 00099 NM 2007 3 5 AWXA200700307 1 20070201 A 5320 6517684638 INTERCOSTAL BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED INTERCOSTAL, BS 294.5, S12L. REPLACED INTERCOSTAL, BS 294.5, S12L IAW AWA ER 03-5312-07054-HF4. 2 L 7 2 4F RT A16WE 2007030500107 20070305 00107 NM 2007 3 5 CALA0700100 1 20070227 A 5311 BAC1518393 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 AFT CARGO COMPARTMENT CRACKED ON FWD BULKHEAD FRAME. INSTALLED STIFFENER IAW SRM 51-10-02, 51-30-01, AND 51-40-02. 2 L 7 2 4F RT A16WE 2007030500109 20070305 00109 NM 2007 3 5 CALA0700102 1 20070228 A 5330 6560552 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 A 2 INCH CRACK IN R1 DOOR AT THE LOWER BOTTOM CORNER. REPAIRED IAW ECRA 5331-01291. 2 L 7 2 4F RT A16WE 2007030500111 20070305 00111 NM 2007 3 5 CALA0700104 1 20070226 A 3350 6104781 BATTERY BOEING 737 737524 1384721 NM CABIN DISCHARGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11641 28902 EMERGENCY LIGHTS FOUND ON. REPLACED BATTERIES IAW 33-51-51. 2 L 7 2 4F RT A16WE 2007030500115 20070305 00115 2007 3 5 CALA0700108 4 20070228 A 2565 60176104 SLIDE RAFT BOEING 767 767424ER 1385270 NM EMERGENCY EXIT DEFECTIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69063 29458 RIGHT EMERGENCY EXIT SLIDE RAFT SAFETY PIN CANNOT BE INSERTED. REPLACED SLIDE IAW AMM 25-66-00. 2 L 7 2 4F RT A1NM 2007030500118 20070305 00118 2007 3 5 SWAA071159 4 20070301 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 757LV 29850 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007030500119 20070305 00119 NM 2007 3 5 SWAA071160 1 20070301 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 414, LBL 2. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007030500120 20070305 00120 NM 2007 3 5 SWAA071152 1 20070228 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED BRDG CHECK, FOUND UPPER FUSELAGE SKIN CHAFED AT DORSAL FIN SECTION BS 857 TO BS 870. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2007030500124 20070305 00124 NM 2007 3 5 SWAA071154 1 20070228 A 5753 6546434 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED C4 CHECK, FOUND LEFT WING OUTBOARD T/E FLAP DELAMINATED AT UPPER T/E SURFACE. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2007030500125 20070305 00125 NM 2007 3 5 SWAA071167 1 20070301 A 5753 6546486129 WEDGE BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 606SW 27926 DURING SCHEDULED C4 CHECK, FOUND LEFT WING INBOARD MID FLAP WEDGE DELAMINATED AT INBOARD T/E. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007030500126 20070305 00126 WP 2007 3 5 DU4R2007066 1 20070227 A 5512 REPAIR DOUG DC9 DC983 3022083 WP HORIZ STAB DAMAGED B BWIA K NONE O OTHER IN INSP/MAINT 1 SO 15 789BV 49789 FOUND CORROSION BLEND OUTS AND EXISTING EXTERNAL REPAIRS ON LT HORIZONTAL STABILIZER INBD LEADING EDGE. REPAIRED BY FAB RICATING AND INSTALLED REPAIRS 5 BY 4 FROM 6AL-4V040 AND 6 BY 5 FROM 6AL-4V032 AS DIRECTED TIMCO RFTS 60030 AND REO-L00 677 REV A DATED 10-30-03 APPROVED BY FAA FORM 8110-3. 2 L 7 2 4F RT A6WE 2007030500127 20070305 00127 WP 2007 3 5 DU4R2007067 1 20070227 A 5512 REPAIR DOUG DC9 DC983 3022083 WP HORIZ STAB DAMAGED B BWIA K NONE O OTHER IN INSP/MAINT 1 SO 15 789BV 49789 FOUND CORROSION BLEND OUTS AND EXISTING EXTERNAL REPAIRS ON LT HORIZONTAL STABILIZER INBD LEADING EDGE. REPAIRED BY FAB RICATING AND INSTALLED REPAIRS 17-1/4 BY 5-1/2, 15 BY 4-1/2 AND 5-1/2 BY 5-1/2 FROM 6AL-4V032 AND 6.0 BY 6.0, 15-1/2 BY 5-1/4 AND 5-1/4 BY 5-1/4 FROM 6AL-4V040 AS DIRECTED BY TIMCO RFTS 60031 AND REO-L00676 REV A DATED 10-30-03 APPROVED BY FAA FORM 8110-3. 2 L 7 2 4F RT A6WE 2007030500129 20070305 00129 NM 2007 3 5 DHL2007781010 1 20070226 A 5343 TRUNNION BOEING 727 727227 1384078 NM NLG CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 781DH 21996 FOUND LT UPPER NLG TRUNNION BORE HAS PITTING CORROSION. REMOVED CORROSION ON TRUNNION BORE PER B727 SRM 53-40-1 FIG 2; ORIGINAL DIA 2.640", FINAL BORE DIA 2.7", MAX ALLOWABLE DIM 2.75", IS WITHIN LIMITS PER B727 SRM 53-40-1 FIG 2. TREATED AND PRIMED TRUNNION BORE PER B727 SRM 51-10-2. 2 L 7 3 4F A3WE 2007030500130 20070305 00130 NM 2007 3 5 DHL2007781004 1 20070226 A 5313 STRINGER BOEING 727 727227 1384078 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 781DH 21996 FOUND FWD CARGO BS 495, STR 28R HAS EXFOLIATING CORROSION. CUT OUT DAMAGED SECTION OF STR FROM BS 483 TO 515, FABRICATE D REPAIR SPLICE FROM BAC1498-132, PO NR 6452106, APPROX LENGTH 12", AND FILLER FROM BAC1498-138, PO NR 7114324, APPROX L ENGTH 34", PER B727 SRM 53-10-3 FIG 1 AND 53-10-2 FIG 3. TREATED, PRIMED, AND INSTALLED REPAIR PARTS PER B727 SRM 51-10 -2 AND 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2007030500134 20070305 00134 WP 2007 3 5 DHL2007802504 1 20070125 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 MAIN CARGO COMPT NR 4 TRACK LUG WORN (STA 1670.000 - 1705.000). CUT OUT NR 4 TRACK DAMAGED SEGMENT AND FABRICATED (3EA) SPLICES (AL7075T6 0.100"/0.125"/0.160") IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA AND SPLICES IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT (P/N SE08530006-3) AND SPLICES IAW SRM 53-2-3 PG 49-50, SRM 51-3-0, SRM 51-3-1 PG 2A. 2 L 7 4 4F RT 4A25 2007030500135 20070305 00135 WP 2007 3 5 DHL2007802505 1 20070118 A 5320 ANGLE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 AFT CARGO COMPT CRACKED ANGLE AT STA 1420.000 BL 0". REMOVED CRACKED ANGLE IAW SRM 51-1-21. CLEANED, TREATED AND PRIME D AREA IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007030500139 20070305 00139 WP 2007 3 5 DHL2007802533 1 20070202 A 5315 FLOORBEAM DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 AFT ACCY COMPT FLOORBEAM SHOWS CRACK 5" AT STA 1700.000 BL 0 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-30-07, DWG NR AC62-53-102, REV IR DATE 01-15-07. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMA GED SECTION IAW DWG AC62-53-102. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK OR CORROSION FOU ND AFTER CUT OUT. ENCLOSED SMN FORM 242-2. FABRICATED REPAIR ANGLE (AL7075T6 51 0.080") FILLER (AL7075T6 0.071") AND S HIM (AL7075T6 0.154") IAW DWG AC62-53-102. TAPERED SHIM ENDS FROM 0.154" TO 0.071" IAW DWG AC62-53-102. CLEANED, TREATE D AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED PART 2 L 7 4 4F RT 4A25 2007030500140 20070305 00140 WP 2007 3 5 DHL2007802534 1 20070202 A 5751 HINGE FITTING DOUG DC8 DC873 302199C WP LT AILERON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 LT NR 4 AILERON HINGE FITTING IS CRACKED. REMOVED AND REPLACED NR 4 LT AIL HINGE SUPPORT FITTING IAW MM 20-16-0 PG 201- 207. REFER TO NR 069055 FOR LT INBD AIL REMOVAL/REINSTALLATION AND NR 071624 FOR OPS CK. 2 L 7 4 4F RT 4A25 2007030500141 20070305 00141 WP 2007 3 5 DHL2007802535 1 20070208 A 5313 LONGERON DOUG DC8 DC873 302199C WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 AFT ACCY COMPT L-30L CORRODED, STA 1746.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-2 FIG 4A. REMOVED CORR OSION IAW SRM 51-1-18 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICATED NEW LONGERON SEGMENT (EXTRUSION P/N S1415997) IAW SRM 53-2-2 FIG 4A, SRM 53-5-3 FIG 5 PG 16 ITEM "A", SRM 51-2-0 FIG 50 SHEET 27 AND SPLICE (EXTRUSION P/N S2645716) IAW SRM 53-2-2 FIG 10 SHEET 4 TR NR 53-193 D ATED 03-15-04, SRM 51-2-0 FIG 50 SHEET 65, SRM 53-2-2 FIG 10 SHEET 1, 3, TR NR 53-153 DATED 12-10-02. PERFORMED NDT INS P IAW SRM 53-2-2 FIG 16 SHEET 4 NOTE 22. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SE 2 L 7 4 4F RT 4A25 2007030500142 20070305 00142 WP 2007 3 5 DHL2007802536 1 20070211 A 5730 56488912 ACCESS DOOR DOUG DC8 DC873 302199C WP RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 RT WING T/E UPPER ACCESS DOOR NR 510 DELAMINATED (XA 475.000 - 507.000). REMOVED AND REPLACED DELAMINATED ACCESS DOOR N R 510 RT WING T/E IAW SRM 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007030500143 20070305 00143 WP 2007 3 5 DHL2007802537 1 20070208 A 5712 97532973 RIB DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 NR 1 LT STUB WING UPPER INTERNAL RIB CRACKED STA XS 530.168 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EA NR 06783 IAW DOUGLAS DWG NR 9753297. REMOVED CRACKED RIB IAW SRM 51-1-21, SRM 51-1-20D. INSTALLED NEW RIB IAW DOUGLAS DWG NR 975329 7, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 PG 2A (TORQUE) REFER TO JC EA57100032-001-D (WO 600017917) FOR RIB FABRICATION. 2 L 7 4 4F RT 4A25 2007030500146 20070305 00146 WP 2007 3 5 DHL2007802506 1 20070120 A 5310 DOOR FRAME DOUG DC8 DC873 302199C WP FUSELAGE UNKNOWN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 PERFORM REPAIR/MODIFICATION OF FWD PAX DOOR LWR FWD JAMB CORNER IAW AD2000-20-08, DWG SR08530021 (MAJOR REPAIR). PERFOR MED MAJOR REPAIR IAW AD2000-20-08, S/B DC8 53-075, DOUGLAS DWG NR SR08530021, 5750776. REMOVED FASTENERS IAW SRM 51-1-2 1, SRM 51-1-20D. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK OR CORROSION FOUND. ENCLOSED SM N FORM 242-2. FABRICATED REPAIR DOUBLER (AL7075T6 0.063") AND REPAIR TRIPLER (AL7075T6 0.080") IAW DOUGLAS DWG SR085300 21. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1 -11. INSTALLED REPAIR PARTS IAW DOUGLAS DWG SR08530021, SRM 51-1-21, SRM 51-1-20B, SRM 51-1-20D, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007030500147 20070305 00147 WP 2007 3 5 DHL2007802507 1 20070120 A 5310 DOOR FRAME DOUG DC8 DC873 302199C WP FUSELAGE UNKNOWN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 PERFORM REPAIR/MODIFICATION OF FWD PAX DOOR UPPER AFT JAMB CORNER IAW AD2000-20-08, DWG SR08530021 (MAJOR REPAIR). PERF ORMED MAJOR REPAIR IAW AD2000-20-08, S/B DC8 53-075, DOUGLAS DWG SR08530021, 5750776. REMOVED FASTENERS IAW SRM 51-1-21 , SRM 51-1-20D. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK OR CORROSION FOUND. ENCLOSED SMN FORM 242-2. FABRICATED REPAIR DOUBLER (AL7075T6 0.063") AND REPAIR TRIPLER (AL7075T6 0.080") IAW DOUGLAS DWG NR SR08530021. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW DOUGLAS DWG SR08530021, SRM 51-1-21, SRM 51-1-20B, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007030500148 20070305 00148 WP 2007 3 5 DHL2007802508 1 20070124 A 5753 RIB DOUG DC8 DC873 302199C WP T/E FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 RT INBD FLAP RIB 1" CRACK STA XW 125.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED R IB IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 57-7-1 FIG 2 SHEET 4, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007030500149 20070305 00149 WP 2007 3 5 DHL2007802509 1 20070124 A 5730 SKIN DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 RT WING UPPER SKIN 0.750" CRACKED STA XRS 74.000 S-14R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 10 SHE ET 1. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW SRM 57-2-1 FIG 10 SHEET 1. PERFORMED NDT INSP I AW DC8 NDT SPM PART 06-10-01-001. NO CRACK OR CORROSION FOUND AFTER CUT OUT. ENCLOSED SMN FORM 242-2. FABRICATED DOUB LER (AL7075T6 0.125") AND FILLER PLUG (AL7075T6 0.200") IAW SRM 57-2-1 FIG 10 SHEET 1. TAPERED DOUBLER FROM 0.125" TO 0 .080" IAW SRM 57-2-1. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SUR FACES IAW SRM 51-1-12. INSTALLED REPAIR PARTS IAW SRM 57-2-1 FIG 10 SHEET 1 SRM 51-1-20D, SRM 51-3-1 (TORQUE). FOR FUE 2 L 7 4 4F RT 4A25 2007030500150 20070305 00150 WP 2007 3 5 DHL2007802510 1 20070120 A 5730 SKIN DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 LT WING UPPER SKIN CRACKED 1" S-9 AT STA XRS 74.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR ON LT WING UPPER SKIN STA XR S 74.000 S-9 IAW SRM 57-2-1 FIG 17 PG 87-88. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW SRM 57-2- 1 FIG 17 PG 87-88. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK OR CORROSION FOUND AFTER CUT O UT, ENCLOSED SMN FORM 242-2. FABRICATED REPAIR DOUBLER (AL7075T6 0.160") AND FILLER PLUG (AL7075T6 0.190") IAW SRM 57-2 -1 FIG 17 PG 87-88. TAPERED DOUBLER FROM 0.160" TO 0.080" IAW SRM 51-10-0 FIG 1 SHEET 20. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-12. INSTALLED REPAIR PARTS IAW 2 L 7 4 4F RT 4A25 2007030500151 20070305 00151 WP 2007 3 5 DHL2007802511 1 20070125 A 5720 SPLICE DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 RT WING CTR LE UPPER INTERNAL SPLICE 2" CRACK STA XOLD 6.2246. REMOVED CRACKED SPLICE IAW SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. FABRICATED SPLICE (AL7075T6 0.080") IAW BOEING MSG NR 1-275396206-21 DATED JAN 23,2007. CLEANED, TREATED AND PRIMED AREA AND SPLICE IAW SRM 51-1-8B. INSTALLED SPLICE IAW SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D, SRM 51-3-1 PG 2A. 2 L 7 4 4F RT 4A25 2007030500152 20070305 00152 WP 2007 3 5 DHL2007802512 1 20070124 A 5753 ANGLE DOUG DC8 DC873 302199C WP T/E FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 RT OUTBD FLAP SHOWS "T" ANGLE WITH CRACK 1" AT STA XT 165.000. REMOVED CRACKED T-ANGLE IAW SRM 51-1-21. FABRICATED NEW T-ANGLE (EXTRUSION P/N 1213286) IAW SRM 57-7-0 FIG 3, SRM 51-2-0 FIG 50. CLEANED, TREATED AND PRIMED AREA AND T-ANGLE IAW SRM 51-1-8B. INSTALLED T-ANGLE IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007030500154 20070305 00154 WP 2007 3 5 DHL2007802514 1 20070126 A 5730 SKIN DOUG DC8 DC873 302199C WP RT WING MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 802DH 86868 46076 NR 4 RT STUB WING LWR SURFACE HAS A NON STANDARD REPAIR AT STA XFS 562.500. PERFORMED MAJOR REPAIR IAW SRM 57-2-1A FIG 1 PG 3. REMOVED NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED EXT REPAIR DOUBLER (AL7075T6 0.080") AND INTERNAL DOUBLER (AL7075"0" 0.063") IAW SRM 57-2-1A FIG 1 PG 3. HEAT TREATED INTERNAL DOUBLER FROM 7075"0" TO 7075T6 I AW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW SRM 57-2-1A FIG 1 PG 3, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007030500157 20070305 00157 WP 2007 3 5 DHL2007802517 1 20070128 A 5753 FRAME DOUG DC8 DC873 302199C WP T/E FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 FOUND LT OTBD FLAP FORMER 1.500" CRACKED STA XF 165.000. REMOVED CRACKED FORMER IAW SRM 51-1-21. FABRICATED NEW FORMER (AL7075"0" 0.050") IAW SRM 57-2-0 PG 1. HEAT TREATED FORMER FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 13-17. CLEANED, TREATED AND PRIMED FORMER AND AREA IAW SRM 51-1-8B. INSTALLED FORMER IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007030500158 20070305 00158 WP 2007 3 5 DHL2007802518 1 20070126 A 5210 DOOR DOUG DC8 DC873 302199C WP R2 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 R2 DOOR AFT UPPER CORNER CRACKED 1.250" LENGTH. PERFORMED MAJOR REPAIR IAW AD200-20-08 S/B DC8 53-075, DOUGLAS DWG SR08 530021 AND 5750776. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION IAW DOUGLAS DWG SR08530021. PERFORMED NDT INSPECTION IAW NDT SPM PART 06-10-01-001. NO CRACK OR CORROSION FOUND AFTER CUT OUT. ENCLOSED SMN FORM 242-2. FAB RICATED REPAIR DOUBLER (AL7075T6 0.090") AND REPAIR TRIPLER (AL7075T6 0.125") AND FILLER (AL7075T6 0.032") IAW DOUGLAS D WG SR08530021. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES I AW SRM 51-1-11. INSTALLED REPAIR PARTS IAW DOUGLAS DWG SR08530021, SRM 51-1-21, SRM 51-1-20B, SRM 51-1-20D, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007030500161 20070305 00161 NM 2007 3 5 EIA2007022 1 20070222 A 5330 SKIN BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 FORWARD CARGO CEC CUTOUT, BILGE, SKIN UNDER DOUBLER FOUND CORRODED AND FORWARD RIGHT DOUBLER FOUND CRACKED OFF. ACCOMPL ISHED SKIN REPAIR PER BOEING RESPONSE 1-280156778. 2 L 7 4 4F A20WE 2007030500163 20070305 00163 NM 2007 3 5 EIA2007024 1 20070124 A 5753 FITTING BOEING 747 747273C 1384896 NM T/E FLAP CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 FOUND NR 6 FLAP TRACK AFT ALIGNMENT FITTING WITH CORROSION ON SURFACE BETWEEN FITTING AND WING SKIN. HOLES WERE OVERSIZ ED AND SPOT FACED. REPAIR BUSHINGS INSTALLED PER BOEING MESSAGE 1-277661910-9. 2 L 7 4 4F A20WE 2007030500164 20070305 00164 NM 2007 3 5 EIA2007025 1 20070222 A 5330 SKIN BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 PROPAGATING CORROSION WAS FOUND AROUND CEC DOOR CUT OUT AREA BETWEEN STA 780 TO 850. FUSELAGE SKIN AND CUTOUT DOUBLER R EPLACED. 2 L 7 4 4F A20WE 2007030500165 20070305 00165 NM 2007 3 5 F3LA200700028 1 20070218 A 5415 D545100790000 BEARING AIRBUS A319 A319111 3930336 NM RT PYLON CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 929FR 4725 2240 DURING C-2 CHECK, INSPECTION REPORTED RT PYLON PANEL 483BL, BOTH SPHERICAL BEARINGS HAD CORROSION. REPLACED BEARINGS IA W AMM 20-21-11-991-003. 2 L 7 2 4F RT A28NM 2007030500167 20070305 00167 2007 3 5 F3LA200700033 4 20070220 A 2565 WARNING LIGHT AIRBUS A319 A319111 3930336 NM EVAC SLIDE MALFUNCTIONED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 929FR 2240 DURING C-2 CHECK, INSPECTION REPORTED RT WING OVERWING EXIT SLIDE ARMED LIGHT INOP. UNABLE TO REPRODUCE FAULT PER OPS T EST IAW AMM 52-73-00-710-002. 2 L 7 2 4F RT A28NM 2007030500168 20070305 00168 NM 2007 3 5 F3LA200700034 1 20070219 A 3397 PIN AIRBUS A319 A319111 3930336 NM WIRING HARNESS BACKED OUT A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 929FR 4725 2240 DURING C-2 CHECK, INSPECTION REPORTED EMERGENCY EXIT LIGHT AT ROW 3 INOP. FOUND PIN PUSHED BACK ON WIRE HARNESS 350WL2 AT SEAT ROW 2. REPLACED WIRE HARNESS IAW 33-51-06, PG 003, SHEET 2. PERFORMED OPS CHECK IAW AMM 33-51-00-710-009. CHE CKED GOOD. 2 L 7 2 4F RT A28NM 2007030500172 20070305 00172 NM 2007 3 5 QXEA200700294 1 20070227 A 5297 CONNECTOR BOMBDR DHC8 DHC8402 1390042 NM DOOR WARNING LOOSE A QXEA O OTHER N FALSE WARNING AP APPROACH 1 NM 09 420QX 4147 BOI FLIGHT: ON FINAL APPROACH, THE FUSELAGE DOOR WARNING ILLUMINATED. THE MCD WAS INDICATING OPEN ON THE DOORS SYSTEM PA GE. THE INDICATION WENT OUT DURING TAXI TO THE GATE. MAINTENANCE RESECURED LOOSE CONNECTOR BACK SHELL AND LUBED FWD PA SSENGER DOOR CLOSED SENSOR. FWD PAX DOOR OPS CHECK GOOD IAW AMM 52-11-00 PGS 503-506. PADRCL PROXIMITY SENSOR READING NORMAL AT PSEU IN CLOSED AND LOCKED POSITION. ALL DOOR INDICATIONS NORMAL. REF AMM TR 32-200-32-61-11 PGS 1-7. NO PART S REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030500173 20070305 00173 NM 2007 3 5 QXEA200700280 1 20070214 A 5320 COVER DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND RIGHT INBOARD SEAT TRACK INNER DRIP TRAY COVER IS CRACKED BY RIVET HOLES STATION X240 FORWARD TO X182. R EPAIRED IAW SRM 51-40-00. 2 H 7 2 4T RT A13NM 2007030500179 20070305 00179 NM 2007 3 5 QXEA200700274 1 20070214 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - NR 7 SEAT TRACK HAS CORROSION ON INBOARD FLANGE AT STATION X202.750, NEXT TO CAMLOCK FASTENER HOLE. REPAIRED I AW RD8-53-4698, RD8-53-1102, RD8-53-4473, SRM 51-40-00 AND 51-40-11. 2 H 7 2 4T RT A13NM 2007030500181 20070305 00181 NM 2007 3 5 QXEA200700277 1 20070213 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 19479 C4 PDX - FOUND LEFT CARGO COMPARTMENT SEAT TRACK NR 6 HAS CORROSION IN AND AROUND THE FOOT LATCH SECTION AT STATION X59 6. REPAIRED IAW RD8-53-4936, SRM 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 2007030500183 20070305 00183 NM 2007 3 5 QXEA200700301 1 20070226 A 3250 4063000502 CONTROL UNIT BOMBDR DHC8 DHC8402 1390042 NM NLG STEERING MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 416QX 9046 4083 SEA FLIGHT NR 2361: NOSE STEERING CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLAC ED SCU AND NWS MANIFOLD ASSY. REPAIRED BENT PIN BY REPLACING RVDT NR 2. PERFORMED FUNCTIONAL TEST OF THE NWS AND TAXI CHECK. NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030500184 20070305 00184 NM 2007 3 5 QXEA200700286 1 20070207 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND RIGHT INBOARD SEAT TRACK NR 7 HAS CORROSION ON EDGE OF CLAW AT STATION X405. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2007030500185 20070305 00185 NM 2007 3 5 QXEA200700287 1 20070214 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND CORROSION ON LEFT CENTER SEAT TRACK NR 4 AROUND RIVETS ON OUTBOARD FLANGE FROM STATION 201 TO 262. REPAI RED IAW RD8-53-4698, SRM 51-40-11, RD8-53-1102, AND RD8-53-4473. 2 H 7 2 4T RT A13NM 2007030500186 20070305 00186 NM 2007 3 5 QXEA200700289 1 20070216 A 5711 SPAR CAP DHAV DHC8 DHC8202 2809007 NM RT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND RIGHT WING FRONT SPAR CAPS BOTH UPPER AND LOWER FROM STATION YW 171 TO YW 200 HAVE SCRATCHES IN AND NEAR THE BEND RADIUS. REPAIRED IAW RD8-57-1119, AND SRM 51-20-16, 51-20-36. 2 H 7 2 4T RT A13NM 2007030500187 20070305 00187 NM 2007 3 5 QXEA200700284 1 20070214 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND RIGHT OUTBOARD SEAT TRACK NR 10 HAS CORROSION ON TOP EDGE AND IN CENTER OF TRACK AT STATION X280. REPAIR ED IAW RD8-53-3644, AND RD8-53-1342. 2 H 7 2 4T RT A13NM 2007030500188 20070305 00188 NM 2007 3 5 QXEA200700288 1 20070207 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND RIGHT INBOARD SEAT TRACK NR 7 HAS A CHAFE IN THE FLANGE AT STATION X242. REPAIRED IAW RD8-53-4698. 2 H 7 2 4T RT A13NM 2007030500189 20070305 00189 NM 2007 3 5 QXEA200700291 1 20070217 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND LEFT INBOARD FLAP TRACK NR 2 HAS A DIVOT ON LOWER RAMP AT AFT OF FORWARD EDGE. REPAIRED IAW RD8-57-986. 2 H 7 2 4T RT A13NM 2007030500191 20070305 00191 NM 2007 3 5 QXEA200700285 1 20070213 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND RIGHT OUTBOARD SEAT TRACK NR 10 HAS CORROSION ON EDGE OF CLAWS AT STATION X262 TO X264. REPAIRED IAW RD8 -53-1342. 2 H 7 2 4T RT A13NM 2007030500192 20070305 00192 NM 2007 3 5 QXEA200700290 1 20070218 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND TOP OF BOTTOM RAIL ON LEFT WING NR 2 FLAP TRACK IS PITTED ON ITS ENTIRE LENGH. REPAIRED IAW RD8-57-986. 2 H 7 2 4T RT A13NM 2007030500193 20070305 00193 NM 2007 3 5 AWXA200700314 1 20070218 A 5310 65140796 STOP FITTING BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - L1 DOOR CUT OUT AFT LOWER STOP FITTING, UPPER FASTENER HOLE CRACKED, BS 348.2, S16L. REPLACED L1 DOOR CUT OUT AFT LOWER STOP FITTING, BS 348.2, S16L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007030500194 20070305 00194 NM 2007 3 5 AWXA200700315 1 20070201 A 5315 693877710 STIFFENER BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED CABIN FLOORBEAM VERTICLE STIFFENER ANGLE, BS 1006, LBL 39, WL 208. REPLACED CABIN FLOORBEAM VERTICL E STIFFENER ANGLE, BS 1006, LBL 39, WL 208 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007030500197 20070305 00197 NM 2007 3 5 AWXA200700318 1 20070126 A 5754 65C267943 SKIN BOEING 737 7373S3 1384711 NM L/E SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND RIGHT WING NR 5 SLAT TRAILING EDGE SKIN CRACKED, SS 219. RIGHT WING NR 5 SLAT TRAILING EDGE SKIN, SS 219 I AW B737-300 SRM 57-43-01-02R6. 2 L 7 2 4F RT A16WE 2007030500198 20070305 00198 NM 2007 3 5 AWXA200700319 1 20070220 A 5347 D53371112005 SEAT TRACK AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 803AW 931 SAL - FOUND CORROSION ON MAIN CABIN SEAT TRACK, FR 41 - FR 47, -Y1292. REPLACED MAIN CABIN SEAT TRACK, FR 41 - FR 47, - Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007030500199 20070305 00199 NM 2007 3 5 AWXA200700320 1 20070301 A 3350 20131A POWER SUPPLY BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 305AW 24012 PHX - EEL - MOST AFT LT AND RT BULLNOSE EMERGENCY LIGHTS INOP. MX REPLACED POWER SUPPLY AND BATTERY IN AFT GALLEY OVER HEAD, RT SIDE PER 33-51-51-201. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2007030500201 20070305 00201 NM 2007 3 5 SWAA071163 1 20070301 A 5312 6546578 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6R. REPAIRED BULKHEAD WEB PER ER. 2 L 7 2 4F RT A16WE 2007030500202 20070305 00202 NM 2007 3 5 CALA0700086 1 20070223 A 3350 ADD71701100 BATTERY PACK BOEING 737 737724 13844BY NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14704 28765 BATTERY PACK DEAD ON RT EMERGENCY EXIT DOOR. INSTALLED SERVICEABLE BATTERY PER MM 33-51-06. 2 L 7 2 4F RT A16WE 2007030500203 20070305 00203 NM 2007 3 5 CALA0700087 1 20070225 A 3397 D5967 CONNECTOR BOEING 767 767424ER 1385270 NM CABIN DISCONNECTED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 69059 29454 LIGHT ASSY CONNECTOR DISCONNECTED. EMERGENCY LIGHT INOP AT 18D. RECONNECTED AND PER MM 33-51-10. 2 L 7 2 4F RT A1NM 2007030500204 20070305 00204 NM 2007 3 5 CALA0700088 1 20070223 A 5320 6562125 STRUCTURE BOEING 737 7373T0 1384582 NM FUSELAGE BULGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 FWD BAG BIN BULGED ALONG S28L FROM STA 500D 6 INCHES. REPAIRED IAW SRM 53-30-12. 2 L 7 2 4F RT A16WE 2007030500205 20070305 00205 NM 2007 3 5 CALA0700089 1 20070223 A 5312 6546568524 BULKHEAD BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 FWD APB LOWER CENTER SECTION WEB CORRODED. REPAIRED IAW ECRA 5311-01298. 2 L 7 2 4F RT A16WE 2007030500212 20070305 00212 NM 2007 3 5 CALA0700096 1 20070225 A 5311 6546548 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 AFT CARGO FLOOR FRAME AT STA 747 IS CORRODED FROM STR 26L TO 26R. REPAIRED IAW SRM 53-00-07 DETAIL 2, 51-40-02 & 51-10- 02. 2 L 7 2 4F RT A16WE 2007030500213 20070305 00213 NM 2007 3 5 CALA0700097 1 20070221 A 5320 147A8540U8 STRUCTURE BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27239 28951 R2 CHORD CORRODED. REPAIRED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007030500215 20070305 00215 NM 2007 3 5 SWAA071161 1 20070301 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND RIGHT CREASE BEAM CRACKED AT BS 639, RBL 70. REPAIRED CREASE BEAM PER ER. 2 L 7 2 4F RT A16WE 2007030600001 20070306 00001 EU 2007 3 6 2007UALA00125 1 20070118 A 2742 47145137 ACTUATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HORIZ STAB FAULTY A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 476UA 1508 RTFL DUE TO LOSS OF LEFT ELAC. REPLACED TRIM ABLE HORIZONTAL STABILIZER ACTUATOR. SYSTEM OPS CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007030600004 20070306 00004 EU 2007 3 6 2007UALA00593 1 20070225 A 3350 BULB AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 409UA 462 MIDSHIP OVERHEAD EXIT SIGN FWD SIDE HAS 1 BULB, AFT FACE HAS 3 BULBS & AFT BULKHEAD OVERHEAD EXIT SIGN HAS 1 BULB INOPER ATIVE. [5-1-07] REPLACED LAMPS OPS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007030600009 20070306 00009 NM 2007 3 6 2007UALA00598 1 20070226 A 5320 INTERCOSTAL BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 910UA 25254 BS 294, STR-7L, FWD SIDE OF FWD ENTRY DOOR, INTERCOSTAL CRACK AT FWD INBOARD RADIUS. 21 MARCH 07, SUPPLEMENTAL DATA UPDATE MAJOR REPAIR: REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007030600010 20070306 00010 NM 2007 3 6 2007UALA00599 1 20070226 A 5320 ATTACH ANGLE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 910UA 25254 BS 348 STR 15L AFT OF FWD ENTRY FUSELAGE FRAME, FRAME TO INTERCOSTAL ATTACH ANGLE CRACK, ACCESS THRU LIGHTENING HOLE BEL OW STR 15L. 21 MARCH 07, SUPPLEMENTAL DATA UPDATE MAJOR REPAIR: REPLACED ATTACH ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007030600013 20070306 00013 NM 2007 3 6 2007UALA00602 1 20070227 A 3397 WIRE HARNESS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY LIGHT ROW 2J INOPERATIVE. REPLACED EEL SEAT HARNESS AT ROW 2J, OP CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030600014 20070306 00014 NM 2007 3 6 2007UALA00603 1 20070227 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 OVERWING LT EMERGENCY LIGHT 2 BOTTOM INOPERATIVE. REPLACED ASSY. CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030600015 20070306 00015 NM 2007 3 6 2007UALA00604 1 20070226 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 541UA 25253 EEL LIGHT STRIP BROKEN AT ROW 13. [SUP 4-17-07] SPLICED POWER STRIP AND RESECURED, LIGHT OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030600017 20070306 00017 NM 2007 3 6 2007UALA00606 1 20070226 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 557UA 26653 L-2 DOOR LOWER GATE CORRODED ON OUTER LOWER FLANGE SURFACES. [SUP 05-08-07] REMOVED CORROSION AND FOUND TO BE WITHIN SRM LIMITS. ORIGINAL MATERIAL THICKNESS OF 0.140" IS NOW DOWN TO 0.136" AFTER CORROSION REMOVAL. NO COMPONENTS NEEDED TO BE REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030600018 20070306 00018 NM 2007 3 6 2007UALA00607 1 20070227 A 5320 ANGLE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 910UA 25254 BS 302 FWD SIDE OF FWD ENTRY FUSELAGE FRAME JUST ABOVE STR 10L INTERCOSTAL ANGLE CRACKED AT OUTBOARD AFT END. 21 MARCH 0 7,SUPPLEMENTAL DATA UPDATE MAJOR REPAIR: REPLACED AUX INTERCOSTAL ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007030600021 20070306 00021 NM 2007 3 6 2007UALA00610 1 20070227 A 2930 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RAT SWITCH INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 588UA 26717 AMBER UNLOCK LIGHT ON RAT SWITCH INOPERATIVE. [SUP 05-18-07] RELAMPED SWITCH AND OPS CHECK GOOD. THIS DISCREPANCY IS ATTRIBUTED TO A FUSED LAMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030600025 20070306 00025 NM 2007 3 6 AMTA200700108 1 20070222 A 3260 PSEU BOEING 737 73783N 13844HI NM MALFUNCTIONED A AMTA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 308TZ 28244 PSEU LIGHT ILLUMINATED ON RECALL DURING TAXI IN. PERFORMED PSEU BITE IAW FIM 32-09-00-810-801 FAULT CODES 27-62004 AND 32-62006, AND FIM 32-61-00-810-806 AND 823. FOR R/RADIO ALTIMETER, CLEARED FAULTS AND PERFORMED BITE ON PSEU AND RAD-AL T NO FAULTS NOTED. (K) 2 L 7 2 4F RT A16WE 2007030600026 20070306 00026 NM 2007 3 6 SWAA071145 1 20070227 A 5312 6582671 PRESSURE PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 665, RBL 38. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007030600027 20070306 00027 NM 2007 3 6 SWAA071146 1 20070227 A 5754 65C26602 SKIN BOEING 737 7373H4 1384600 NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND RT WING NR 5 L/E SLAT SKIN CRACKED INBOARD OF ACTUATOR. REPAIRED SLAT SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007030600028 20070306 00028 NM 2007 3 6 SWAA071142 1 20070227 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030600029 20070306 00029 NM 2007 3 6 SWAA071143 1 20070227 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030600032 20070306 00032 2007 3 6 SWAA071127 4 20070227 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007030600034 20070306 00034 NM 2007 3 6 SWAA071128 1 20070227 A 2560 10107451 SIGN BOEING 737 7373T5 1384608 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 MID CABIN EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007030600035 20070306 00035 NM 2007 3 6 SWAA071147 1 20070227 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 726SW 27858 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 5 TO RBL 49. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007030600036 20070306 00036 NM 2007 3 6 SWAA071140 1 20070227 A 3350 20131A BATTERY PACK BOEING 737 7373T5 1384608 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007030600038 20070306 00038 2007 3 6 SWAA071129 4 20070227 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 454WN 29851 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007030600039 20070306 00039 2007 3 6 SWAA071131 4 20070227 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 757LV 29850 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007030600040 20070306 00040 NM 2007 3 6 SWAA071132 1 20070227 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515, STR 21R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007010300361 20070103 00361 NM 2007 1 3 HALA0700001 1 20070101 A 4990 OIL SYSTEM BOEING 767 767332 1382001 NM APU LOW A HALA K NONE O OTHER NR NOT REPORTED 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, APU AUTO SHUTDOWN. PERFORMED FIM 49-11-00 FOUND OIL PRESS ON ECU, ADDED 6 PINTS OF OIL CLEARE D ECU FAULT RAN APU FOR 20 MIN SHUT DOWN APU PERFORMED BITE WITH NO FAULTS FOUND PERFORMED LEAK CHECK WITH NO LEAKS. 2 L 7 2 4F RT A1NM 2007010400005 20070104 00005 EU 2007 1 4 MALA070001 1 20070101 A 3010 BOOT SAAB SF340 340B 7860101 EU LT WING RUPTURED A MALA A UNSCHED LANDING O OTHER UK UNKNOWN 1 GL 15 446XJ 340B446 THE CREW RETURNED TO DTW WHEN THEY EXPERIENCED AN OPERATIONAL FAULT WITH THE DE-ICE BOOT. THE LEFT WING OUTBOARD BOOT R UPTURED. THE FLIGHT RETURNED TO DTW WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED LHOB LEADING EDGE, P/N OFF/ON 72572 11-513, S/N OFF 2395509, S/N ON 0204666. OPS CHECKS GOOD IAW SF340 AMM 30-10-00-05. 2 L 7 2 4T RT A52EU 20081128 WP 2008 11 28 K11A 200811219150 1 20070212 A 5310 CROSSBEAM DOUG DC9 DC915F 3022037 WP CARGO DOORWAY CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 915CK 470869 AFT PIT DOOR FWD STOP FITTING CROSSBEAM CRACKED UNDER RADIOUS FILLER ON OUT FASTENER FOR STOP FITTING VERIFIED USING HFE C. 2 L 7 2 4F A6WE 20081128 WP 2008 11 28 K11A2008112191503 1 20070202 A 5311 FRAME DOUG DC9 DC915F 3022037 WP FUSELAGE BENT A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 915CK 40086 STA 58 FRAME INNER FLANGE BENT LBL 27 10 INCHES UP FROM NOSE GEAR DOOR OPENING. 2 L 7 2 4F A6WE 20081128 WP 2008 11 28 K11A2008112191505 1 20070221 A 5321 FLOOR PANEL DOUG DC9 DC915F 3022037 WP MAIN DECK DAMAGED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 915CK 47086 MAIN DECK FLOOR PANEL EDGE LIFTING BETWEEN BS 503 AND 566 AT LBL 21. 2 L 7 2 4F A6WE 20081128 WP 2008 11 28 K11A2008112191507 1 20070213 A 5320 SUPPORT FITTING DOUG DC9 DC915F 3022037 WP BS 623 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 915CK 47086 WHEEL WELL CEILING HAS EVIDENCE OF CORROSION AROUND SIDE BRACE SUPPORT FITTING APPROX STA 623 LBL 56. 2 L 7 2 4F A6WE 20081128 WP 2008 11 28 K11A2008112091508 1 20070227 A 5320 WEB DOUG DC9 DC915F 3022037 WP BS 646 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 915CK 47086 BS 646 APPROX RBL 55 WEB UNDER FLOOR BOARD CORRODED. 2 L 7 2 4F A6WE 20081128 WP 2008 11 28 K11A2008112091509 1 20070212 A 5320 VERTICAL BEAM DOUG DC9 DC915F 3022037 WP CARGO BAY CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 915CK 47086 FORWARD PIT DOOR UPPER CENTER AFT STOP FITTING VERTICAL BEAM WEB CRACKED AT TOOLING HOLE AT UPPER AREA VERIFIED USING HI GH FREQ EDDY CURRENT. 2 L 7 2 4F A6WE 20081128 WP 2008 11 28 K11A2008112091501 1 20070214 A 5315 FLOORBEAM DOUG DC9 DC915F 3022037 WP BS 200 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 915CK 47086 FLOOR SUPPORT CORRODED AT STA 200 LBL 55. 2 L 7 2 4F A6WE 20081128 NM 2008 11 28 K11A2008112572401 1 20070323 A 5320 WEB BOEING 727 727225 1384077 NM BS 1223 CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 724CK 20383 VERTICAL WEB CRACKED AT LIGHTING HOLE. 2 L 7 3 4F A3WE 20081128 NM 2008 11 28 K11A2008112572402 1 20070323 A 5320 WEB BOEING 727 727225 1384077 NM BS 1223 CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 724CK 20383 VERTICAL WEB CRACKED AT LIGHTNING HOLE. 2 L 7 3 4F A3WE 20081128 NM 2008 11 28 K11A2008112572403 1 20070323 A 5310 BEAM BOEING 727 727225 1384077 NM DAMAGED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 724CK 20383 TRANSVERSE LOWER CHORD BEAM DAMAGED. 2 L 7 3 4F A3WE 20081128 NM 2008 11 28 K11A2008112572404 1 20070321 A 5210 WEB BOEING 727 727225 1384077 NM DOOR CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 724CK 20383 VERTICAL WEB FWD OF AIRSTAIRS HAS 6 INCH CRACK IN WEB. 2 L 7 3 4F A3WE 20081128 WP 2008 11 28 K11A2008112191506 1 20070220 A 5310 DOOR FRAME DOUG DC9 DC915F 3022037 WP BS 180 S13R CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 915CK 47086 GALLEY SERVICE DOOR INTERIOR HORIZONTAL FRAME CRACKED BEYOND STOP DRILL IN OUTBOARD RADIUS AT FORWARD SIDE OF DOOR APPRO X BS 180 STRINGER 13R 1 INCH CRACK. 2 L 7 2 4F A6WE 20081128 WP 2008 11 28 K11A2008112191502 1 20070212 A 5310 CROSSBEAM DOUG DC9 DC915F 3022037 WP CARGO DOORWAY CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 915CK 47086 AFT PIT DOOR 2ND FROM THE BOTTOM STOP FITTING CROSSBEAM CRACKED IN 2 PLACES UNDER RADIUS FILLER ON INNER FASTENER FOR ST OP FITTING VERIFIED USING HFEC. 2 L 7 2 4F A6WE 20081128 NM 2008 11 28 K11A2008112672201 1 20070122 A 5340 ATTACH ANGLE BOEING 727 7272H3 138368N NM CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 722CK 20948 FORWARD SPAR VERTICAL ATTACH ANGLE HAS EVIDENCE OF A CRACK 2 L 7 3 4F RT A3WE 20081128 NM 2008 11 28 K11A2008112672202 1 20070122 A 5320 ATTACH ANGLE BOEING 727 7272H3 138368N NM CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 722CK 20948 FORWARD SPAR VERTICAL ATTACH ANGLE HAS EVIDENCE OF A CRACK. 2 L 7 3 4F RT A3WE 20081128 NM 2008 11 28 K11A2008112672203 1 20070122 A 5720 ATTACH ANGLE BOEING 727 7272H3 138368N NM CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 722CK 20948 FORWARD SPAR VERTICAL ATTACH ANGLE HAS EVIDENCE OF A CRACK. 2 L 7 3 4F RT A3WE 20081128 NM 2008 11 28 K11A2008112672204 1 20070122 A 5720 ATTACH ANGLE BOEING 727 7272H3 138368N NM CRACKED A K11A O OTHER O OTHER NR NOT REPORTED 1 GL 23 722CK 20948 FWD SPAR VERTICAL ATTACH ANGLE HAS EVIDENCE OF A CRACK. 2 L 7 3 4F RT A3WE 20081128 NM 2008 11 28 K11A2008112672205 1 20070122 A 5720 ATTACH ANGLE BOEING 727 7272H3 138368N NM CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 722CK 20948 FWD SPAR VERTICAL ATTACH ANGLE HAS EVIDENCE OF A CRACK. 2 L 7 3 4F RT A3WE 20081126 WP 2008 11 26 K11A2008112091505 1 20070208 A 5321 FLOOR PANEL DOUG DC9 DC915F 3022037 WP BS 370-446 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 915CK 47086 CORROSION ON TOP OF MAIN DECK FLOOR PANELS BETWEEN BS 370 AND 446, RBL 52. 2 L 7 2 4F A6WE 20081128 WP 2008 11 28 K11A2008112191508 1 20070213 A 5310 STRUCTURE DOUG DC9 DC915F 3022037 WP BS 620 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 915CK 47086 W/W CEILING AT STA 620 RBL 40 HAS SIGNS OF CORROSION. 2 L 7 2 4F A6WE 20081128 WP 2008 11 28 K11A2008112091510 1 20070212 A 5230 BEAM DOUG DC9 DC915F 3022037 WP CARGO DOOR CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 915CK 47086 FORWARD CARGO DOOR UPPER CENTER FORWARD STOP FITTING VERTICAL BEAM WEB CRACKED AT TOOLING HOLE AT UPPER AREA VERIFIED BY HFEC. 2 L 7 2 4F A6WE 20081128 NM 2008 11 28 K11A2008112572405 1 20070321 A 5320 WEB BOEING 727 727225 1384077 NM FUSELAGE PUNCTURED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 724CK 20383 VERTICAL WEB JUST FORWARD OF AIRSTAIRS HAS 1 INCH PUNCTURE. 2 L 7 3 4F A3WE 20081128 NM 2008 11 28 K11A2008112572406 1 20070920 A 5511 SPAR BOEING 727 727225 1384077 NM HORIZONTAL STAB CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 724CK 20383 HORIZONTAL STABILIZER CORROSION ON LOWER CHORD RT HORIZONTAL REAR SPAR. 2 L 7 3 4F A3WE 20081128 WP 2008 11 28 K11A2008112091502 1 20070223 A 5310 DOOR FRAME DOUG DC9 DC9* WP BS 180 BROKEN A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 915CK 47086 GALLEY SERVICE DOOR FRAME BROKE APPROX STA 180 21 INCHES FROM BOTTOM OF DOOR STR 15 RT. 2 L 7 2 4F A6WE 20081201 NM 2008 12 1 K11A2008112872201 1 20070124 A 5330 SKIN BOEING 727 7272H3 138368N NM FUSELAGE DAMAGED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 APPROX STA 1230 STR 23 L SKIN DAMAGED. 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112872202 1 20070325 A 5330 SKIN BOEING 727 7272H3 138368N NM FUSELAGE DAMAGED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 APPROX STA 1263 STR 26 R SKIN DAMAGE. 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112872203 1 20070605 A 5230 SKIN BOEING 727 7272H3 138368N NM CARGO DOOR DAMAGED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 C-3 BULKPIT DOOR EXTERIOR SURFACE WIDE ARRAY OF DAMAGE, INCLUDING CORROSION, DING/DENTS AND EDGE DAMAGE. 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112872204 1 20070426 A 5310 DOOR FRAME BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 STA 1090, STR 22 R VICINITY CORROSION ALONG FWD EDGE OF C-3 DOOR CUT OUT. 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112672207 1 20070502 A 5720 ATTACH ANGLE BOEING 727 7272H3 138368N NM WING CRACKED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 FWD SPAR VERTICAL ATTACH ANGLE HAS EVIDENCE OF A CRACK 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112672208 1 20070409 A 5720 STIFFENER BOEING 727 7272H3 138368N NM WING CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 VERTICAL STIFFNER HAS AREA OF CORROSION. 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112672209 1 20070321 A 5720 STIFFENER BOEING 727 7272H3 138368N NM LT WING CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 REAR SPAR VERTICAL STIFFNER HAS AREA OF CORROSION. 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112672211 1 20070327 A 5330 SKIN BOEING 727 7272H3 138368N NM FUSELAGE DAMAGED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 APPROX STA 200 STR 23 R SKIN DAMAGE. 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112872206 1 20070321 A 5320 STIFFENER BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 CORROSION ON BACK SIDE OF STIFFNERS. 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112872209 1 20070430 A 5522 SKIN BOEING 727 7272H3 138368N NM ELEVATOR CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 CORROSION ON LT ELEVATOR UPPER SURFACE, FWD OF T/E. ( ELEVATOR STA 199 3.5 INCHES) 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112872210 1 20070411 A 5711 ATTACH ANGLE BOEING 727 7272H3 138368N NM RT WING CRACKED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 FWD SPAR ATTACH ANGLE CRACKED. ( RT WING ) 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112872211 1 20070411 A 5711 ATTACH ANGLE BOEING 727 7272H3 138368N NM RT WING CRACKED A K11A O OTHER O OTHER UK UNKNOWN 1 GL 23 722CK 20948 FWD SPAR ATTACH ANGLE CRACKED. ( RT WING ) 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112872212 1 20070411 A 5711 ATTACH ANGLE BOEING 727 7272H3 138368N NM RT WING CRACKED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 FWD SPAR ATTACH ANGLE CRACKED. ( RT WING ) 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112872213 1 20070425 A 5711 ATTACH ANGLE BOEING 727 7272H3 138368N NM RT WING CRACKED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 FWD SPAR ATTACH ANGLE CRACKED ( RT WING ). 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112872214 1 20070425 A 5711 ATTACH ANGLE BOEING 727 7272H3 138368N NM RT WING CRACKED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 FWD SPAR ATTACH ANGLE CRACKED ( RT WING). 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112872216 1 20070505 A 5330 LAP JOINT BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 CORROSION BENEATH LAP SEAM. 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112872217 1 20070504 A 5330 LAP JOINT BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 CORROSION BENEATH LAP SEAM. 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112872218 1 20070504 A 5330 LAP JOINT BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 CORROSION BENEATH LAP SEAM. 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112872219 1 20070510 A 5512 SKIN BOEING 727 7272H3 138368N NM HORIZ STAB CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 RT STAB TOP SKIN HAS SURFACE CORROSION AT THE 3 OTBD ELEVATOR HINGE POINT. ( RT STAB STA 168 ) 2 L 7 3 4F RT A3WE 20081128 WP 2008 11 28 K11A2008112191504 1 20070208 A 5321 FLOOR PANEL DOUG DC9 DC915F 3022037 WP MAIN DECK DAMAGED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 915CK 47086 MAIN DECK FLOOR PANEL EDGE LIFTING BETWEEN BS 503 AND 566 AT RBL 21. 2 L 7 2 4F A6WE 20081201 NM 2008 12 1 K11A2008112672206 1 20070502 A 5711 ATTACH ANGLE BOEING 727 7272H3 138368N NM LT WING CRACKED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 FEW SPAR VERTICAL ATTACH ANGLE HAS EVIDENCE OF A CRACK. 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112672213 1 20070531 A 5330 SKIN BOEING 727 7272H3 138368N NM FUSELAGE DAMAGED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 APPROX STA 300 STR 18R SKIN DAMAGE AT LAV SERVICE CUTOUT FWD UPPER CORNER. 2 L 7 3 4F RT A3WE 20081201 NM 2008 12 1 K11A2008112672220 1 20070311 A 5330 SKIN BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 APPROX STA 740 STR 19 L CORROSION ON SKIN JUST BENEATH LAP SEAM. 2 L 7 3 4F RT A3WE 2007010300305 20070103 00305 NM 2007 1 3 AWXA200702131 1 20070101 A 5330 6545774 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 PHX - FOUND FUSELAGE EXTERIOR SKIN CRACKED AT BS 7 27E, S22L. REPAIRED FUSELAGE EXTERIOR SKIN CRACKED AT BS7 27E, S22L IAW B737 SRM 53-00-01-2R, REPAIR 31. 2 L 7 2 4F RT A16WE 2007010400247 20070104 00247 NM 2007 1 4 AWXA200700004 1 20070102 A 5330 6552988 SKIN BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 PHX - AFT FUSELAGE EXTERIOR SKIN CRACKED, BS 920 S23L, FWD OF A PREVIOUS REPAIR. REPAIRED AFT FUSELAGE EXTERIOR SKIN, B S 920 S23L IAW AWA ER 03-5361-07002-SS1. 2 L 7 2 4F RT A16WE 2007010400273 20070104 00273 NM 2007 1 4 ASAA0741351 1 20070102 A 5755 SKIN BOEING 737 7374Q8 138447Q NM LT SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 775AS 25108 THE LEFT SPOILER NR 3 HAS UPPER SURFACE IRREGULARITY (DENT) NR 3 LT WING SPOILER REPAIRED IAW SRM 57-70-01. 2 L 7 2 4F RT A16WE 2007010400301 20070104 00301 SO 2007 1 4 C2XA07IA007 1 20070101 A 3350 3104404 FUSE EMB 145 EMB145XR 3260214 SO BATTERY PACK BLOWN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12166 14500831 IAH - FLIGHT 2644, DURING PRE-FLIGHT INSPECTION THE EMERGENCY LIGHT AT THE EXIT ROW WAS FOUND TO BE INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE EXIT ROW BATTERY PACK FUSE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS A PPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007010400290 20070104 00290 CE 2007 1 4 BSAASDR0701 1 20070103 A 3260 404EN16 DOWNLOCK SWITCH BEECH 1900 1900D 1154162 CE RT MLG FAILED A BSAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 NM 05 140ZV 1000 UE140 WHEN CREW EXTENDED GEAR FOR LANDING THE RIGHT GEAR INDICATOR DIDN'T COME ON. THE BULBS WERE CHECKED WITH THE PRESS TO T EST AND FOUND TO BE GOOD. CREW REQUESTED A MISSED APPROACH TO RUN GEAR LIGHT CHECKLIST PROCEDURES. BOTH MAIN GEAR WERE VISUALLY VERIFIED TO BE DOWN AND COMPARED TO MAKE SURE BOTH AT THE SAME CONFIGURATION. THE EMERGENCY GEAR SYSTEM WAS U SED TO VERIFY GEAR WAS DOWN WITH POSITIVE PRESSURE. THE CREW LANDED WITH NO FURTHER INCIDENT. IT WAS DETERMINED THE DO WNLOCK SWITCH HAD FAILED. 2 L 7 2 4T RT A24CE 2007010400327 20070104 00327 SO 2007 1 4 C2XA07SH001 1 20070104 A 5312 14526850401 FIREWALL EMB 135 EMB135LR 3260305 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV - DURING C-CHECK THE APU FIREWALL WAS FOUND CRACKED AT FIVE RIVETS NEAR STRINGER 12R. MAINTENANCE REPAIRED THE CRAC KED APU FIREWALL IAW IC2006-145/10117. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007010400329 20070104 00329 SO 2007 1 4 C2XA07SH002 1 20070104 A 5320 13500436003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV - DURING C-CHECK LEFT OMEGA BEAM LOWER FLANGE WAS FOUND WITH CORROSION BETWEEN FRAMES 32 AND 36. MAINTENANCE REPAIR ED LT OMEGA BEAM AT FRAME 33 IAW EMB 135 SRM 53-00-10 FIG 202, CPM 51-21-07 AND EMB 135 SRM 51-40-02. AIRCRAFT WAS APPR OVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007010400330 20070104 00330 SO 2007 1 4 C2XA07SH003 1 20070104 A 5320 13500436001 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV - DURING C-CHECK LEFT OMEGA BEAM LOWER FLANGE WAS FOUND WITH CORROSION BETWEEN FRAME 23 AND 32. MAINTENANCE REPAIRE D LT OMEGA BEAM AT LOWER FLANGE IAW EMB 145 SRM 53-00-10 & CPM 51-21-07. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007010500011 20070105 00011 EA 2007 1 5 COMA0760001 1 20070101 A 3010 14463109 TUBE CNDAIR CL600 CL6002B19 1900309 EA LT WING FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 936CA 30880 7043 FLIGHT 5223 - EN ROUTE BOS - BNA RECEIVED AN ANIT-ICE DUCT WARNING MESSAGE, FLIGHT DIVERTED TO GSO. REPLACED THE LEFT W ING OUTBOARD PICCOLO TUBE. 2 L 7 2 4F RT A21EA 2007010500016 20070105 00016 EA 2007 1 5 COMA0760002 1 20070101 A 7830 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 975CA 7150 FLIGHT 5418 - EN ROUTE JAX-LGA RECEIVED A RIGHT THRUST REVERSER UNLOCK MESSAGE, FLIGHT DIVERTED TO CHS. DEFERRED THE RI GHT THRUST REVERSER PER MEL 78-30-01. 2 L 7 2 4F RT A21EA 2007010500019 20070105 00019 EA 2007 1 5 COMA0770001 1 20070102 A 5242 SERVICE DOOR CNDAIR CL600 CL6002C10 1390015 EA GPU DOOR OPEN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 642CA 10125 FLIGHT 5258 - DURING CLIMBOUT OF CVG THE GPU DOOR OPENED, FLIGHT RETURNED TO THE FIELD. INSPECTED CONDITION OF DOOR AND LATCHES, NO DISCREPANCIES NOTED, CLOSED DOOR. 2 L 7 2 4F RT A21EA 2007010500077 20070105 00077 NM 2007 1 5 UPS07M48815 1 20070101 A 5730 SKIN DOUG MD11 MD11F 3023600 NM WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 LEADING EDGE CRACK AFT OF NR 7 SLAT. FIXED L/E SKIN AFT OF NR 7 LT SLAT I/B SIDE AT STA X0S 906 REF 57-10-00 PG 104. DM G REMOVED. ROLLED DBLR & PICK UP HOLES FAB FROM 7075-76-063. DRILLED,TRIMMED, BEVELED & PRIMED SURFACE PER SRM 57-10-00 . INSTALL DBLR. INSTALL FASTENERS & REPAIR I/B SUPPORT. FABBED REPAIR DOUBLER FOR L/E STRINGER DOUBLER AT STA X02 906 PE R SRM 57-10-00. INSTALL COMPLETE 2 L 7 3 4F RT A22WE 2007010500079 20070105 00079 NM 2007 1 5 KCSA071000 1 20070102 A 3350 LIGHT BOEING 747 747249F 1384849 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 706CK 21827 LEFT UPPER DECK EMERGENCY LIGHT INOP. 2 L 7 4 4F A20WE 2007010500080 20070105 00080 NM 2007 1 5 KCSA071002 1 20070102 A 5314 STIFFENER BOEING 747 747246F 1384850 NM FUSELGAE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 LEFT BODY GEAR WHEEL WELL KEEL BEAM EXTERNAL STIFFENER CORRODED AT BOTTOM AT BS 1466.5, WL 97. 2 L 7 4 4F RT A20WE 2007010500085 20070105 00085 NM 2007 1 5 KCSA071001 1 20070102 A 5412 BULKHEAD BOEING 747 747122 1384872 NM NR 2 NACELLE CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 NR 2 PYLON HYD PRESSURE SUPPLY LINE JAM NUT CHAFING INTO AFT SIDE OF NAC STA 221 BULKHEAD WEB. 2 L 7 4 4F A20WE 2007010500087 20070105 00087 NM 2007 1 5 KCSA071003 1 20070102 A 5315 FLOORBEAM BOEING 747 747122 1384872 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 AFT PIT FLOORBEAM DAMAGED AT BS 1800, LBL 50. 2 L 7 4 4F A20WE 2007010500108 20070105 00108 NM 2007 1 5 07FDEA00021 1 20070104 A 5711 ARB74131 SPAR CAP DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LT WING, TRAILING EDGE REAR SPAR UPPER CAP LOWER SURFACE AT XORS= 1047 WAS FOUND WITH CORROSION. COMPLIED WITH FEDEX E. A. 1-5710-105595, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007010500109 20070105 00109 NM 2007 1 5 07FDEA00022 1 20070104 A 5314 KEELBEAM DOUG MD11 MD11F 3023600 NM ZONE 700 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 CENTER LANDING GEAR, RT SIDE KEEL BEAM WEB AT DRAG BRACE FOUND BEAM CORRODED. CORROSION REMOVED ON BOOTSTRAP AT CENTER LANDING GEAR RIGHT HAND SIDE KEEL BEAM WEB AS PER SRM 53-00-01 VOLUME I FIGURE 1A AND MACHINED NEW BOOTSTRAP AS PER DWG AEA7131. NEW BOOTSTRAP INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 2 L 7 3 4F RT A22WE 2007010500110 20070105 00110 2007 1 5 NOCA00107 4 20070102 A 2211 6224591512 COMPUTER BOEING 757 75728A 1384976 NM AUTOPILOT SYS MALFUNCTIONED A NOCA K NONE O OTHER CL CLIMB 1 EA 15 750NA 26277 CENTER AUTOPILOT FLUCTUATES DURING CLIMBOUT AND CRUISE. LEFT AND RIGHT AUTOPILOT OPERATES NORMAL. REMOVED AND REPLACED CENTER FCC COMPUTER PER MM 22-11-01. 2 L 7 2 4F RT A2NM 2007010500111 20070105 00111 NM 2007 1 5 07FDEA00023 1 20070104 A 5320 SILL BOEING 727 727233 138408A NM BS 575-596 CRACKED A FDEA K O NONE OTHER O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 FOUND MAIN DECK CARGO DOOR UPPER SILL UPPER FLANGE CRACKED AT RIVET BUCKTAILS AT STATIONS 575.5, 584, 590 & 596. REMOV ED CRACKED SILL REF SRM 51-30-2. FABRICATED SILL REF FED EX DWG 53FX1467. DRILLED UP AND INSTALLED INSTALLED SILL AN D STRUCTURE REF SRM 51-30-2 & DWG 53FX1467. ALSO WORKED ON SNRM N00492. 2 L 7 3 4F RT A3WE 2007010500112 20070105 00112 NE 2007 1 5 AWXA200700020 2 20070101 A 7320 8249722016 EEC AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE NR 1 ENGINE OUT OF TOLERANCE A AWXA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 WP 28 815AW 19031 19031 1323 FLIGHT 237: DTW - PHX - THE A/C HAD JUST REACHED CRUISE ALTITUDE WHEN THE CREW NOTICED THE NR 1 ENGINE HAD RETARDED TO F LIGHT IDLE FOLLOWED BY AN ENGINE FLAMEOUT/SHUT DOWN. THE CREW ATTEMPTED AN IN-FLIGHT RESTART, THE IN-FLIGHT RESTART WAS NOT SUCCESSFUL. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO ORD. THE LANDING WAS UNEVENTFUL AND THE A/C TAXIED TO THE GATE. MX REPLACED THE EEC AND THE FMU. OPS/LEAK CHECK WAS GOOD. THE A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007010500113 20070105 00113 EU 2007 1 5 AWXA200700032 1 20070101 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 619AW 527 LAS - EEL - MX DISCOVERED EMERGENCY EXIT LIGHTS INOP LEFT OVERWING WALL AND CEILING. MX REPLACED THE EMERGENCY LIGHT PO WER SUPPLY. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007010500086 20070105 00086 NM 2007 1 5 KCSA071004 1 20070102 A 5230 SKIN BOEING 747 747122 1384872 NM CARGO DOOR DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 AFT CARGO DOOR FWD LOWER CORNER HAS APPROX .750 INCH X 1.5 INCH AREA OF EDGE SKIN DAMAGED. 2 L 7 4 4F A20WE 2007010400297 20070104 00297 SO 2007 1 4 C2XA07IA002 1 20070101 A 2121 011768500 FAN EMB 145 EMB145XR 3260214 SO CARGO BAY MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION DE DESCENT 1 SW 27 23139 145731 IAH - FLT 2239, ON DESCENT THE CREW REPORTED A BAGGAGE SMOKE INDICATION. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BAGGAGE VENT FAN, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007010400331 20070104 00331 SO 2007 1 4 C2XA07BT001 1 20070101 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO FUSELAGE INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14902 145496 BTV DURING 3A CHECK FOUND EMERGENCY LIGHT ON CEILING ROW 17 INOP. REPLACED BULB IAW AMM 33-50-08. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007010500261 20070105 00261 NM 2007 1 5 SWAA070028 1 20070103 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 4R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007010500262 20070105 00262 NM 2007 1 5 SWAA070029 1 20070103 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 365, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007010500263 20070105 00263 NM 2007 1 5 SWAA070030 1 20070103 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 7 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007010500264 20070105 00264 NM 2007 1 5 SWAA070031 1 20070103 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007010500265 20070105 00265 NM 2007 1 5 SWAA070032 1 20070103 A 5753 65522461 CARRIAGE BOEING 737 7373H4 1384600 NM T/E FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD MID FLAP INBOARD CARRIAGE CORRODED AT TORQUE TUBE ATTACHMENT BORE. RE MOVED AND REPLACED INBOARD CARRIAGE PER MM. 2 L 7 2 4F RT A16WE 2007010500267 20070105 00267 NM 2007 1 5 SWAA070034 1 20070103 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007010500268 20070105 00268 NM 2007 1 5 SWAA070035 1 20070103 A 5330 6546882 SKIN BOEING 737 7373H4 1384600 NM TAIL CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SKIN CHAFED AT BS 1148, BELOW RT HORIZONTAL STAB REAR LUGS. REPAIRED SKIN PE R BOEING DRAWING AND SRM. 2 L 7 2 4F RT A16WE 2007010500271 20070105 00271 NM 2007 1 5 SWAA070006 1 20070102 A 2560 6557463 FITTING BOEING 737 7377H4 1384404 NM GIRT BAR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 466WN 30677 R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING BROKEN. REMOVED AND REPLACED AFT GIRT BAR FITTING PER MM. 2 L 7 2 4F RT A16WE 2007010500279 20070105 00279 NM 2007 1 5 SWAA070014 1 20070102 A 2750 65522111 TORQUE TUBE BOEING 737 7373H4 1384600 NM T/E FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD MID FLAP, INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE T UBE PER MM. 2 L 7 2 4F RT A16WE 2007010500280 20070105 00280 NM 2007 1 5 SWAA070015 1 20070102 A 2750 65522112 TORQUE TUBE BOEING 737 7373H4 1384600 NM T/E FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD MID FLAP, OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007010500282 20070105 00282 NM 2007 1 5 SWAA070001 1 20070101 A 5610 5717623121 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT CRACKED A SWAA K NONE O OTHER NR NOT REPORTED 1 SW 29 331SW 23695 FLIGHT DECK L2 WINDOW ARCHED AND CRACKED IN FLIGHT. REMOVED AND REPLACED L2 WINDOW PER MM. 2 L 7 2 4F RT A16WE 2007010500283 20070105 00283 2007 1 5 SWAA070002 4 20070101 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007010500284 20070105 00284 NM 2007 1 5 SWAA070003 1 20070102 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 EEPLS PHOTO LUMINESCENT STRIP WORN AT ROW 6 ABC TO ROW 8 ABC. REMOVED AND REPLACED PHOTO LUMINESCENT STRIP PER MM. 2 L 7 2 4F RT A16WE 2007010500286 20070105 00286 NM 2007 1 5 SWAA070017 1 20070102 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME SECTION CRACKED AT BS 440, STR 8L. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007010500288 20070105 00288 NM 2007 1 5 SWAA070018 1 20070102 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME SECTION CRACKED AT BS 787, STR 8L. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007010500289 20070105 00289 NM 2007 1 5 SWAA070019 1 20070102 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME SECTION CRACKED AT BS 867, STR 8L. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007010500290 20070105 00290 NM 2007 1 5 SWAA070020 1 20070102 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME SECTION CRACKED AT BS 480, STR 8L AND STR 8R. REPAIRED FRAME PER SWA E A. 2 L 7 2 4F RT A16WE 2007010500292 20070105 00292 NM 2007 1 5 SWAA070022 1 20070102 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 792, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007010500293 20070105 00293 NM 2007 1 5 SWAA070023 1 20070102 A 3350 101073 LENS BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED SERVICE CHECK, FOUND FWD RT EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007010500294 20070105 00294 NM 2007 1 5 SWAA070024 1 20070102 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 713SW 27847 DURING SCHEDULED HC1 CHECK, LT AFT CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PAC K PER MM. 2 L 7 2 4F RT A16WE 2007010800009 20070108 00009 NM 2007 1 8 SWAA070037 1 20070103 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007010800013 20070108 00013 NM 2007 1 8 SWAA070041 1 20070103 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 487WN 33854 DURING SCHEDULED MV1 CHECK, FOUND EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007010800014 20070108 00014 NM 2007 1 8 SWAA070042 1 20070103 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM R2 GIRT BAR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING BROKEN. REMOVED AND REPLACED GIRT B AR FITTING PER MM. 2 L 7 2 4F RT A16WE 2007010800015 20070108 00015 NM 2007 1 8 SWAA070025 1 20070103 A 3350 101331108 LENS BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 LEFT OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007010800016 20070108 00016 NM 2007 1 8 SWAA070026 1 20070103 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 203WN 32483 EEPLS LIGHT COVER AT LEFT AFT CABIN LOOSE. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007010800039 20070108 00039 2007 1 8 HALA0700005 4 20070103 A 2310 7126140001 COUPLER BOEING 767 767332 1382001 NM HF SYSTEM INOPERATIVE A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 596HA 59467 59467 23276 ETOPS SIGNIFICANT SYSTEM, TRANSMISSION ON RT HF INOP. REPLACED NR 2 HF COMM ANT COUPLER PER AMM 23-11-01, OPS CHECK OK. 2 L 7 2 4F RT A1NM 2007010800040 20070108 00040 NM 2007 1 8 HALA0700006 1 20070103 A 2697 WIRE BOEING 767 767300 1385204 NM FIRE LOOP BROKEN A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 DURING NR 1 ENG HARDWARE INSP, FOUND WIRE TERMINAL END BROKEN FOR UPPER AFT FIRE DETECTION LOOP. REMOVED AND REPLACED F IRE LOOP WIRE TERMINAL END PER AMM 26-11-00. OPS CHECK OF ENG FIRE WARNING SYSTEM CHECKS GOOD. 2 L 7 2 4F RT A1NM 2007010800084 20070108 00084 NM 2007 1 8 07FDEA00003 1 20070101 A 5711 SPAR CAP DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RT WING REAR SPAR LOWER CAP UPPER SURFACE FOUND CORROSION AT XORS 1075 TO 1082. COMPLIED WITH FEDEX E.A. 1-5710-105596, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2- 100. 2 L 7 3 4F RT A22WE 2007010800085 20070108 00085 NM 2007 1 8 07FDEA00004 1 20070101 A 5711 SPAR CAP DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RT WING REAR SPAR LOWER CAP UPPER SURFACE FOUND CORROSION AT XORS 1062 TO 1072. COMPLIED WITH FEDEX E.A. 1-5710-105596, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007010800087 20070108 00087 NM 2007 1 8 07FDEA00006 1 20070101 A 5512 ALC84305 SKIN DOUG MD11 MD11 3023602 NM ZONE 300 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 529FE 48624 LT HORIZONTAL STAB LEADING EDGE O/B SECTION NR 331FT FOUND WITH DENT ON O/B EDGE. FOUND OUT OF LIMIT AS PER SRM 55-00-0 1 VOL. I. DEPTH= 0.080", WIDTH= 2". REPAIR CARRIED OUT AS PER SRM 55-20-00 FIG. 5 VOL. I. REPAIR CLASSIFIED MAJOR AS P ER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007010500018 20070105 00018 EA 2007 1 5 COMA0760003 1 20070102 A 3020 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYSTEM MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 969CA 7141 FLIGHT 5358 - DURING TAKEOFF ROLL RECEIVED AN ANTI-ICE CAUTION MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFO RMED AN OPERATIONAL CHECK OF THE LEFT AND RIGHT ANTI-ICE SYSTEM, NO DISCREPANCIES NOTED. 2 L 7 2 4F RT A21EA 2007010500075 20070105 00075 NM 2007 1 5 UPS07248814 1 20070101 A 2560 LATCH BOEING 727 727108C 1384039 NM PAX DOOR BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE:N/A MAIN CABIN DOOR ENTRY EMERGENCY DOOR SLIDE LATCH ASSY BROKEN. INSTALLED NEW LATCH ON EMERGENCY SLID E ASSY AS OUTLINED IN AMM 25-60-15-2 (IPC 25-60-00 ITEM 015). 2 L 7 3 4F A3WE 2007010500078 20070105 00078 WP 2007 1 5 UPS07848816 1 20070102 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:N/A ON COCKPIT PREFLIGHT EMERGENCY EXIT LIGHTS WHEN ARMED WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS GOOD. 2 L 7 4 4F RT 4A25 2007010500269 20070105 00269 NM 2007 1 5 SWAA070036 1 20070103 A 5753 6546430 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SKIN DISBONDED AT OUTBOARD TRAILING EDGE. REPAIRED SK IN SRM. 2 L 7 2 4F RT A16WE 2007010500270 20070105 00270 2007 1 5 SWAA070005 4 20070102 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 431WN 29845 R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007010500276 20070105 00276 NM 2007 1 5 SWAA070011 1 20070102 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007010500277 20070105 00277 NM 2007 1 5 SWAA070012 1 20070102 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007010500278 20070105 00278 NM 2007 1 5 SWAA070013 1 20070102 A 5753 6546435274 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP LOWER SKIN DISBONDED AT OUTBOARD T/E. REMOVED AND REPLA CED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2007010500285 20070105 00285 NM 2007 1 5 SWAA070004 1 20070102 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 402WN 29814 EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2007010800120 20070108 00120 2007 1 8 TSAA0723001 4 20070101 A 2310 9640452011 TRANSMITTER BOEING 737 73776N 13844CH NM HF RADIO FAILED A TSAA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 740AL 28640 FLIGHT 483 SNA-OGG. DURING CRUISE FLIGHT, THE CREW NOTED THE NR 2 HF RADIO WOULD NOT CHANNELIZE, BUT RECEPTION AND SELC AL OPERATED NORMAL. CREW CONTINUED TO OGG WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE NR 2 HF ON MEL FOR THE AIRC RAFT TO FLY TO HNL. MAINTENANCE REMOVED AND REPLACED THE NR 2 HF RECEIVER TRANSMITTER PER AMM 23-11-00-5. THE NR 2 HF RADIO PASSED A GROUND OPERATIONAL CHECK AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE NR 2 HF RADIO SUCCESSFULLY PASSED A FLIGHT VERIFICATION CHECK ON THE NEXT FLIGHT LEG. 2 L 7 2 4F RT A16WE 2007010800127 20070108 00127 CE 2007 1 8 AMWA81813 1 20070103 A 3230 LANDING GEAR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RIGHT MALFUNCTIONED A AMWA O OTHER J WARNING INDICATION AP APPROACH 1 CE 07 155ZV UE155 WHEN GEAR WAS EXTENDED FOR LANDING, THE RT MAIN GEAR DID NOT SHOW DOWN AND LOCKED. THE CREW DECLAIRED AN EMERGENCY AND F OLLOWED EMERGENCY PROCEDURES, BY PUMPING THE GEAR DOWN. THE AIRCRAFT THEN LANDED SAFELY WITH NO FURTHER INCIDENT. 2 L 7 2 4T 4 T RT A24CE E26NE 2007011900043 20070119 00043 WP 2007 1 19 07FDEA00071 1 20070110 A 2913 PUMP DOUG DC10 DC1030F 3023504 WP NR 1 INOPERATIVE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 303FE 46802 ON CLIMB-OUT PASSING 16,000', GOT HYD LEVEL 1 ALERT WITH HYD NR 1, NR 2, NR 3 PUMPS OFF. FOUND C/B POPPED. RESET AND I T POPPED AGAIN. RETURNED TO BASE(SJU) MEL 10JAN07. ACN RELEASED FOR SERVICE PER MEL/CDL: 29-11-01 CATEGORY: C EXPIRAT ION: 20JAN07 "MEL 29-11-01: ENG NR 1 HYD PUMP - INOP. PUMP REMOVED." 2 L 7 3 4F RT A22WE 2007010500266 20070105 00266 NM 2007 1 5 SWAA070033 1 20070103 A 5753 65C263431 CARRIAGE BOEING 737 7373H4 1384600 NM T/E FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD MID FLAP OUTBOARD CARRIAGE CORRODED AT TORQUE TUBE ATTACHMENT BORE. R EMOVED AND REPLACED OUTBOARD CARRIAGE PER MM. 2 L 7 2 4F RT A16WE 2007010500272 20070105 00272 NM 2007 1 5 SWAA070007 1 20070102 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 13R. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007010500273 20070105 00273 NM 2007 1 5 SWAA070008 1 20070102 A 5311 6546595 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 13R. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007010500281 20070105 00281 NM 2007 1 5 SWAA070016 1 20070102 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME SECTION CRACKED AT BS 400, STR 8L. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007010800011 20070108 00011 NM 2007 1 8 SWAA070039 1 20070103 A 5340 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007010800012 20070108 00012 NM 2007 1 8 SWAA070040 1 20070103 A 5311 65C22910 FRAME BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 26L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007010800067 20070108 00067 2007 1 8 HALA0700004 4 20070102 A 3460 COMPUTER BOEING 767 767332 1382001 NM FLT MANAGE FAILED A HALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 13 596HA 23276 ETOPS SIGNIFICANT SYSTEM, F/O HIS DISPLAYED MAP FAILED SELETING ALT FMC CORRECTS FAULT. REMOVED AND REINSTALLED RIGHT F MC, OPS CK OK PER AMM 34-61-01. 2 L 7 2 4F RT A1NM 2007010800238 20070108 00238 NM 2007 1 8 USAA070014 1 20070105 A 5511 SPAR BOEING 737 737301 1384611 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 501UW 23231 LEFT HORIZ STAB REAR SPAR ALONG TOP CAP CORRODED. REMOVED CORROSION AND REPLACED REPAIR PARTS IAW EA 98333 DEFECT SIZE : 100 INCH SPAN. 2 L 7 2 4F RT A16WE 2007010800251 20070108 00251 NM 2007 1 8 USAA070013 1 20070103 A 5511 SPAR CAP BOEING 737 737301 1384611 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 501UW 23231 HORIZ STAB REAR SPAR TOPCAP HAS CORROSION STA 166. MAJOR REPAIR IAW EA 98333 LEVEL 1, C55-709-20, DEFECT SIZE: 1 X 3 IN CH. 2 L 7 2 4F RT A16WE 2007010800254 20070108 00254 NM 2007 1 8 USAA070010 1 20070103 A 5340 ATTACH ANGLE BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 501UW 23231 STA 847 BL 0 FRAME TO BELLY SKIN ATTACH ANGLE HAS CORROSION. REMOVED DAMAGE, AND INSTALLED FABRICATED REPAIR PARTS IAW SRM 53-00-07 LEVEL 2 C53-208-01, DEFECT SIZE: 1 X .50 INCH. 2 L 7 2 4F RT A16WE 2007010800255 20070108 00255 NM 2007 1 8 USAA07009 1 20070103 A 5420 SKATE ANGLE BOEING 737 737301 1384611 NM NR 1 PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 501UW 23231 NR 1 PYLON O/B SIDE LOWER SKATE ANGLE AT FWD END CRACKED. REPAIRED ANGLES AND INSTALLED SKATE ANGLES IAW EA 98354, DEFE CT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007010800256 20070108 00256 NM 2007 1 8 USAA07008 1 20070103 A 5754 65C26603100 WEDGE BOEING 737 737301 1384611 NM L/E SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 501UW 23231 INBOARD END OF TRAILING EDGE WEDGE ON NR 4 SLAT DELAMINATED. FABRICATED AND INSTALLED CORE AND DOUBLER IAW SRM 51-70-10 , DEFECT SIZE: 2 X .750 X .500 INCH. 2 L 7 2 4F RT A16WE 2007010800258 20070108 00258 NM 2007 1 8 USAA07006 1 20070103 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 501UW 23231 WEB OF BS 639 FRAME S-17R CRACKED. FABRICATED AND INSTALLED DOUBLER IAW EA 98343, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007010800259 20070108 00259 NM 2007 1 8 USAA07005 1 20070103 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 501UW 23231 AT FRAME 500D LBL 10 HAS CORROSION. REMOVED DAMAGED FRAME, ATTACH ANGLES IAW SRM 51-70-11 LEVEL 1 C53-208-01, DEFECT SI ZE: 1 X 1 INCH. 2 L 7 2 4F RT A16WE 2007010800260 20070108 00260 NM 2007 1 8 USAA07004 1 20070103 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 RIGHT FWD CORNER OF THE EXTERNAL GROUND A/C CUTOUT CRACKED. INSTALLED DOUBLER PER EA 98372, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007010800267 20070108 00267 NM 2007 1 8 2007UALA00019 1 20070103 A 3350 9F19948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 107UA 26900 DOOR 1L AND 5L EMERGENCY SLIDE LT DIM. REPLACED LT ASSY. OP CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007010800271 20070108 00271 NM 2007 1 8 2007UALA00022 1 20070103 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY LIGHTS INOP AT CREW REST OVERSTAIRS, DOOR 4R CEILING ENTRY, DOOR 4R FWD & AFT EMERGENCY SILL, COCKPIT EMERGENC Y LIGHT, ROW 16 & 17 CEILING, UPPER DECK OVERSTAIRS, AND FWD GALLEY RT CEILING. REPLACED LIGHT ASSEMBLIES, CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007010800273 20070108 00273 SW 2007 1 8 AC2A113419 1 20070103 A 7714 23054164 SENSOR BELL 430 430 1182150 SW ALLSN 250C 250C40B 03032 NE NR 1 ENGINE MALFUNCTIONED E AC2A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 07 430CM 49090 844077 NR 1 ENGINE NP2 RPM PICKUP MALFUNCTIONED/FAILED. INSTALLED SERVICABLE PART. 1 G 7 2 3U 3 U RT H9SW E1GL 2007010800274 20070108 00274 NE 2007 1 8 AC2A113446 1 20070104 A 6220 7610208001045 SPINDLE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL MAIN ROTOR CRACKED E AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 7266K 2933 760283 THE SPINDLE ASSEMBLY WAS REMOVED TO REPLACE A DEFECTIVE ELASTOMERIC BEARING. WHILE CLEANING THE SPINDLE BEFORE INSTALLI NG THE NEW BEARING, THE SHOP TECHNICIAN DISCOVERED THE CRACKED SPINDLE. 1 G 7 2 3U 3 U H1NE E1GL 2007010800284 20070108 00284 2007 1 8 2007UALA00023 4 20070102 A 2565 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 566UA 26670 DOOR 2L SLIDE ARMED LIGHT WILL NOT ILLUMINATE. REPLACED LAMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007010800289 20070108 00289 2007 1 8 2007UALA00025 4 20070103 A 2565 O-RING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE BOTTLE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 557UA 0456 26653 LOW BOTTLE PRESSURE. FOUND A LEAKING FUSIBLE PLUG O-RING. REPLACED O-RING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007010800290 20070108 00290 NM 2007 1 8 2007UALA00026 1 20070103 A 5210 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD ENTRY DOOR BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FORWARD ENTRY DOOR UPPER AFT CORNER BENT INTO AIRSTREAM. MAJOR REPAIR: COLD WORKED REF SRM 51-70-01. FOUND CRACK FROM F ASTENER HOLD. FABRICATED AND INSTALLED EXTERNAL DOUBLER PER SRM 52-00-01 PAGE 201 ITEM 11. 2 L 7 2 4F 4 F RT A16WE E21EU 2007010800291 20070108 00291 NM 2007 1 8 2007UALA00027 1 20070103 A 3211 PIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LT MLG CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 LEFT MLG AFT MAIN BEAM O/B ATTACH PIN CORRODED. MAJOR REPAIR: REPLACED ATTACH PIN. 2 L 7 2 4F 4 F RT A16WE E21EU 2007010800293 20070108 00293 NE 2007 1 8 DJFA2007001 2 20070103 A 7220 45A030051 INLET BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE ENGINE CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 478LX 1866 RK387 PCEJA0559 DURING A SCHEDULED MAINTENANCE INSPECTION, MAINTENANCE FOUND THE INLET CRACKED. THE CRACK WAS LOCATED AT THE INNER SECT ION WHERE THE INLET MOUNTS TO THE ENGINE AND WAS ABOUT .25 INCH LONG FROM THE FASTENER HOLE TO THE INLET EDGE. THE INLE T WAS REPAIRED IAW SRM SECTION 51-00 AND REINSTALLED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007010800295 20070108 00295 NM 2007 1 8 2007UALA00028 1 20070103 A 5314 KEELBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 FWD PIT KEEL BEAM EXFOLIATED AT BS 500D TO 500D +5\ RBL 7 TO RBL 8 AT WL 145. MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED NESTED ANGLE REPAIR PER SRM 53-30-12 REPAIR NR 2. 2 L 7 2 4F 4 F RT A16WE E21EU 2007010800301 20070108 00301 NM 2007 1 8 2007UALA00031 1 20070103 A 4990 OIL COOLER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE APU CLOGGED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 848UA 1647 FLIGHT DIVERTED DUE TO FAILED APU. FOUND APU OIL COOLER AIR T INLET CLOGGED. REPLACED OIL COOLER. LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007010800303 20070108 00303 NM 2007 1 8 2007UALA00032 1 20070103 A 3150 PROXIMITY SWITCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE PSEU FAILED A UALA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 656UA 25394 TAKEOFF CONFIGURATION WARNING WITH EICAS -FLAPS- & -NOSE A-G DISAGREE- DISPLAYED. REPLACED PROXIMITY SWITCH ELECTRONICS UNIT. OP CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007010800313 20070108 00313 2007 1 8 ASAA0741352 4 20070104 A 2565 61620468 SLIDE BOEING 737 7374Q8 138447Q NM R1 DOOR TWISTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 756AS 25097 DURING R1 DOOR SLIDE DEPLOY TEST THE SLIDE TWISTED UPON DEPLOYMENT. REPLACED R1 DOOR EVAC SLIDE. 2 L 7 2 4F RT A16WE 2007010800351 20070108 00351 NM 2007 1 8 BB07002 1 20070103 A 3350 FUSE BOEING 757 7572B7 1384964 NM CABIN BLOWN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 939UW 27303 R4 DOOR EXTERIOR EMERGENCY LIGHT FOUND INOPERATIVE. MAINTENANCE REPLACED THE FUSE AND RELAMPED. 2 L 7 2 4F RT A2NM 2007010800353 20070108 00353 2007 1 8 SA07001 4 20070104 A 2565 60592101 BOTTLE AIRBUS 320 A320214 3930316 EU EVAC SLIDE READS LOW A USAA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 19 117UW 15317 3243 1224 PHX - A CIDS WARNING WAS GENERATED ON THE FORWARD FLIGHT ATTENDANT'S PANEL FOR THE LEFT OVERWING SLIDE INFLATION BOTTLE. MAINTENANCE REPLACED THE LEFT OVERWING SLIDE INFLATION BOTTLE. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2007010800355 20070108 00355 NM 2007 1 8 CALA0700006 1 20070104 A 5314 65C385021 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12327 23457 INSPECTION FOUND FUSELAGE SKIN BULGING AT S28L BETWEEN STA 500C AND 500D, 6 INCHES LEFT OF AIRCRAFT CENTERLINE. REPLACE D FORWARD SECTION OF LT KEEL BEAM IAW SRM 53-60-12. 2 L 7 2 4F RT A16WE 2007010800357 20070108 00357 NM 2007 1 8 CALA0700008 1 20070104 A 2560 284N4152 LEVER BOEING 757 757224 1384958 NM EMERGENCY EXIT BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 58101 27291 THE RIGHT OFF WING ESCAPE SYSTEM DISABLE LEVER AT RIGHT EMERGENCY EXIT HATCHES WOULD NOT MOVE FROM THE DISABLED POSITION TO THE ARMED POSITION. THE DISABLE LEVER ASSEMBLY WAS FOUND BROKEN. A NEW DISABLE LEVER WAS INSTALLED IAW MM 25-60-11 . OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A2NM 2007010800359 20070108 00359 NM 2007 1 8 CALA0700002 1 20070103 A 5240 655487154 ANGLE BOEING 737 7373T0 1384582 NM R1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12327 23457 INSPECTION FOUND A 1 INCH CRACK IN ANGLE AT R-1 DOOR TORQUE BOX UPPER FORWARD ATTACH HOLES, NEAREST TORQUE TUBE. THE AN GLE WAS REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007010800360 20070108 00360 NM 2007 1 8 CALA0700003 1 20070104 A 5310 6520722U98 DOOR FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69602 27315 INSPECTION FOUND FORWARD CARGO DOOR CUTOUT FORWARD FRAME WEB CRACKED AT DOOR STOP FITTING FWD/LWR AREA, STA 400, S24R, W L 160. THE FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007010800361 20070108 00361 NM 2007 1 8 CALA0700004 1 20070104 A 5315 65C33950 FLOORBEAM BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69602 27315 INSPECTION FOUND FLOORBEAM UPPER FLANGE CORRODED AROUND SCREW HOLES AT STA 986.5, RBL 19 TO RBL 46. THE CORRODED SECTIO N OF FLOORBEAM WAS CUT OUT AND A TEE REPAIR ANGLE AND STRAP WERE INSTALLED IAW ECRA 5310-04494, REPAIR OPTION B. 2 L 7 2 4F RT A16WE 2007010800362 20070108 00362 NM 2007 1 8 CALA0700005 1 20070103 A 3350 FUSE BOEING 757 757224 1384958 NM CABIN BLOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 34131 28971 SEVERAL FORWARD CABIN EMERGENCY AISLE PATH LIGHTS WERE FOUND INOPERATIVE DURING A SERVICE CHECK AT EWR. THE NR 3 FUSE O N M731 WAS FOUND BLOWN. THE FUSE WAS REPLACED AND OPERATIONAL CHECK OF THE LIGHTS WAS GOOD. 2 L 7 2 4F RT A2NM 2007010800363 20070108 00363 EA 2007 1 8 TRAX200700016 1 20070101 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING STUCK A ASOA K NONE F P FLT CONT AFFECTED NO WARNING INDICATION AP APPROACH 1 SO 27 846AS 7328 FLAPS STUCK AT 43 DEG DURING APPROACH (LEFT SIDE 43 RIGHT SIDE 45) NO FLAP FAIL MESSAGE WAS RECEIVED. EMERGENCY DECLARE D. 2 L 7 2 4F RT A21EA 2007010900004 20070109 00004 SO 2007 1 9 C2XA07CL002 1 20070104 A 2120 UNKNOWN EMB 135 EMB135ER 3260203 SO CABIN ODOR A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 19503 145176 CLE FLIGHT 3029 THE CREW REPORTED A BURNING SMELL NOTICED IN THE CABIN AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLEVELAN D AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RAN ENGINES AND APU AT POWER WITH NO SMELL NOTICED. THE AIRCR AFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2007010900014 20070109 00014 SO 2007 1 9 C2XA07IA008 1 20070103 A 3040 3801D2MODA CONTROLLER EMB 145 EMB145XR 3260214 SO WINDOW HEAT MALFUNCTIONED A C2XA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 27 11155 8497 8497 145782 IAH FLIGHT 2196, THE CREW REPORTED A WINDSHIELD 2 HEAT FAIL MESSAGE FOLLOWED BY A SMOKE SMELL IN THE COCKPIT. THE CREW DEACTIVATED THE F/O'S WINDSHIELD HEAT, AND THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE R EMOVED AND REPLACED THE F/O'S WINDSHIELD HEAT CONTROLLER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS AP PROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007010900017 20070109 00017 NM 2007 1 9 UPS07548821 1 20070103 A 3211 TRUNNION BOEING 757 75724APF 1384969 NM NLG BENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 460UP 25481 NLG OPERATING SEQUENCE SLIDE ROD & TRUNNION ASSY BENT. A/C FERRIED TO MAE FOR REPAIR. REPLACED ROD ASSY & R&R TRUNNION ASSY IAW MM 32-34-06.NR930536 REPLACED SUPPORT ASSY IAW MM 32-34-06. PERFORM NLG EXTEMSION/RETRACTION TEST IAW MM 32-34 -00 TEST GOOD. REPLACED CRANK ASSY. REWORK DAMAGED BRACKET TO CORRECT ALIGNMENT. HFEC REWORK AREA IAW NDTM 51-00-00 NO C RACK FOUND. TEST PROXIMITY SENSOR FOR NLG. TEST SATISFACTORY IAW MM 32-61-03-2 2 L 7 2 4F RT A2NM 2007010900019 20070109 00019 EA 2007 1 9 COMA0760004 1 20070103 A 2421 755469E IDG CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE FAILED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 629BR 18300 7251 FLIGHT 5620 - DURING TAKEOFF ROLL RECEIVED A NR 1 IDG CAUTION MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLAC ED THE NR 1 IDG. 2 L 7 2 4F RT A21EA 2007010500260 20070105 00260 NM 2007 1 5 SWAA070027 1 20070103 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 464, STR 26L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007010500274 20070105 00274 NM 2007 1 5 SWAA070009 1 20070102 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPV CHECK, FOUND STRINGER 24L CRACKED AT BS 987. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007010500275 20070105 00275 NM 2007 1 5 SWAA070010 1 20070102 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPV CHECK, FOUND STRINGER 22L CRACKED AT BS 1010. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007010500291 20070105 00291 NM 2007 1 5 SWAA070021 1 20070102 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007010800010 20070108 00010 NM 2007 1 8 SWAA070038 1 20070103 A 5330 6545767 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED RADIO ALTIMETER ANTENNA CUTOUT BS 406, RBL 1.5. REPAIRED SKIN P ER ER. 2 L 7 2 4F RT A16WE 2007010800083 20070108 00083 NM 2007 1 8 07FDEA00002 1 20070101 A 5711 SPAR DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LT WING, TRAILING EDGE REAR SPAR LOWER CHORD AT XORS 1042 TO 1070 FOUND WITH CORROSION. COMPLIED WITH FEDEX E.A. 1-5710 -105594, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007010800086 20070108 00086 NM 2007 1 8 07FDEA00005 1 20070101 A 5711 SPAR CAP DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RT WING REAR SPAR LOWER CAP UPPER SURFACE FOUND CORROSION AT XORS 1050 TO 1059. REPAIRED AS PER FEDEX E.A. 1-5710-10559 6, REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007010800253 20070108 00253 NM 2007 1 8 USAA070011 1 20070103 A 5511 SPAR BOEING 737 737301 1384611 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 501UW 23231 LEFT HORIZONTAL STAB REAR SPAR ALONG TOPCAP HAS CORROSION. REMOVED CORROSION AND INSTALLED REPAIR PARTS IAW EA 98333 LE VEL 2 C55-709-20, DEFECT SIZE: 100 INCHES. 2 L 7 2 4F RT A16WE 2007010800257 20070108 00257 NM 2007 1 8 USAA07007 1 20070103 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 501UW 23231 STA 827 RBL 15-20 WORN. INSTALLED REPAIR ANGLES IAW SRM 51-70-12, DEFECT SIZE: .5 X .5 INCH. 2 L 7 2 4F RT A16WE 2007010800261 20070108 00261 NM 2007 1 8 USAA07003 1 20070103 A 5310 DOOR FRAME BOEING 737 7374B7 1384702 NM FUSELAGE GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 AFT CARGO DOOR FWD FRAME BS 797 GOUGED. REPAIRED IAW EA 98374, DEFECT SIZE: .010 INCH. 2 L 7 2 4F RT A16WE 2007010800272 20070108 00272 CE 2007 1 8 DJFA2007004 1 20070101 A 2170 21BC112 COALESCER BAG BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE CABIN AIR ODOR E DJFA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 23 462LX RK423 TRIP NR 1124081 CREW REPORTED UNCONTROLLABLE COCKPIT HEAT AND THE ODOR OF SOMETHING BURNING. AIRCRAFT RETURNED TO FIEL D. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THE COALESCER SOCK EXTREMELY DIRTY. SUBSEQUENT OPERATIONAL CHECKS PROV ED SATISFACTORY. 2 H 7 2 4F 4 F RT A16SW E25EA 2007010800297 20070108 00297 NM 2007 1 8 2007UALA00029 1 20070103 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 INTERIOR CABIN OVERWING EXIT FRAME BS 616 LT FWD INBOARD SIDE FRAME STUB INNER CHORD BOTTOM FASTENER HOLE JUST ABOVE PRE SSURE DECK IS CRACKED. MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED NESTED ANGLE AND FILLER REPAIR PER MM 53- 11-89. 2 L 7 2 4F 4 F RT A16WE E21EU 2007010800310 20070108 00310 NM 2007 1 8 SB07003 1 20070103 A 2497 6130200502 FEEDER CABLE BOEING 737 737301 1384611 NM NR 2 ENGINE CHAFED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 502UW 23232 PHL FLT1776 - EN ROUTE FROM ORF TO PHL, CREW REPORTED A BURNING SMELL IN THE FLIGHT DECK AND FUMES IN THE CABIN. MULTIP LE SYSTEM LIGHTS ON OVERHEAD PANEL WERE ILLUMINATED AND THE CIRCUIT BREAKER FOR THE NR 2 TRANSFORMER RECTIFIER TRIPS. F LIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 TRANSFORMER RECTIFIER AND FOUND THE T2 AND T3 FEEDER CABLES ON NR 2 ENGINE CHAFED ON BRACKET FOR FEEDER CABLE CLAMP. REPAIRED CABLE INSULATION PER SWPM 20-10 -13 AND REPOSITIONED CABLES FOR CLEARANCE. OPERATIONAL CHECK OF NR 2 ENGINE AC AND DC SYSTEMS NORMAL. 2 L 7 2 4F RT A16WE 2007010800320 20070108 00320 WP 2007 1 8 ASAA0781354 1 20070104 A 5330 5930543 DOUBLER DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 DAMAGE FOUND AFT OF L1 DOOR AT STA 238 TO 240. DENT AND GOUGE ON EXISTING REPAIR DOUBLER. INSTALLED NEW EXTERNAL REPAI R DOUBLER PER SRM 53-04 FIG 12B. 2 L 7 2 4F RT A6WE 2007010900015 20070109 00015 SO 2007 1 9 C2XA07IA009 1 20070104 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 16918 145397 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED A SMOKE SMELL IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT, AND COULD NOT FIND ANY EVIDENCE OF SMOKE SMELL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007010900018 20070109 00018 NM 2007 1 9 UPS07548823 1 20070104 A 2424 GCU BOEING 757 75724APF 1384969 NM RT ENGINE FAILED A IPXA K NONE O OTHER CL CLIMB 1 SO 01 458UP 25479 INSPECTION TYPE:N/A A/C DIVERTED TO MCO DUE TO RIGHT AC BUS FAILURE IN FLT. REMOVED AND REPLACED RIGHT ENG IDG PER MM 2 4-11-01-4. REMOVED AND REPLACED RIGHT ENG GEN CONTROL UNIT PER MM 24-22-02-4. REMOVED AND REPLACED BPCU PER MM 24-41-0 3-4. SYS OPS CHECKED NORMALLY. LEAK CHECK GOOD. 2 L 7 2 4F RT A2NM 2007010900024 20070109 00024 WP 2007 1 9 UPS07848822 1 20070104 A 3350 MODULE DOUG DC8 DC873F 302199F WP CABIN MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:N/A EMERGENCY LIGHTS BATTERY CHARGING (K5) CB POPPED, TRIED TO RESET & WILL NOT STAY IN. REMOVED AND RE PLACED EMERGENCY LIGHT BATTERY & RELAY MODULE IAW MM 33-50-01-2. OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2007010900064 20070109 00064 NM 2007 1 9 07FDEA00025 1 20070104 A 5340 65453139 STRINGER CLIP BOEING 727 727233 138408A NM BS 440 S7L DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 STRINGER CLIP HAS GROUND AT RADIUS CUT OUT BS440 STRINGER L7 REMOVED DAMAGED STRINGER CLIP, DRILLED HOLES IN NEW CLIP AN D INSTALLED REF SRM 51-30-02 PG 2-5. 2 L 7 3 4F RT A3WE 2007010900065 20070109 00065 NM 2007 1 9 07FDEA00026 1 20070104 A 5754 SLAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING FIXED LEADING EDGE SLAT TRACK 12 CUT-OUT FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REP AIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007010900066 20070109 00066 NM 2007 1 9 07FDEA00027 1 20070105 A 5754 SLAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING FIXED LEADING EDGE SLAT TRACK 14 CUT-OUT FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REP AIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007010900072 20070109 00072 NM 2007 1 9 UIEA200700002 1 20070108 A 5347 BAC15201890 SEAT TRACK BOEING 747 747228F 1384895 NM BS 1960 BROKEN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 MAIN CARGO COMPARTMENT SEAT TRACK AT STATION 1960 RT, RBL 11 HAS 1 EACH BROKEN CROWN LUG. REMOVED AND REPLACED SECTION OF SEAT TRACK FROM STATION 1946 TO 1969 RT AS PER 747 SRM 53-10-05 FIG 14. 2 L 7 4 4F A20WE 2007010900074 20070109 00074 NM 2007 1 9 07FDEA00028 1 20070105 A 5754 ARB28931 DOUBLER DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 FOUND LEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS= 665 CRACKED. REPAIRED AS PER SRM 57-10- 00 VOLUME I, FIGU RE 25. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007010900077 20070109 00077 NM 2007 1 9 07FDEA00031 1 20070105 A 5311 AFA00203 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 MAIN DECK CARGO COMPARTMENT MAIN FRAME STA 1701 LONGERON 12L FOUND DENTED. REPAIR CARRIED OUT AS PER SRM 53-30-00 VOLUM E I FIGURE 1. INITIAL INSPECTION REQUIRED AT 14,500 CYCLES AND REPETITIVE INSPECTION REQUIRED EVERY 9,500 CYCLES THER EAFTER AS PER SRM 53-30-00 VOLUME I FIGURE 1. REPAIR CLASSSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007010900079 20070109 00079 NM 2007 1 9 07FDEA00033 1 20070105 A 5753 NRC67021 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LEFT WING, INBOARD FLAP VANE LOWER OUTBOARD SURFACE FOUND DELAMINATED. REPAIRED AS PER FEDEX E.A. 1-5750-105602, REPA IR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007010900080 20070109 00080 NM 2007 1 9 07FDEA00034 1 20070105 A 5753 NRC67622 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING, INBOARD FLAP VANE LOWER INBOARD SURFACE FOUND DELAMINATED. REPAIRED AS PER FEDEX E.A. 1-5750-105603, REPAI R CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007010900081 20070109 00081 NM 2007 1 9 07FDEA00035 1 20070105 A 5753 NRC67021 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LEFT WING, INBOARD FLAP VANE LOWER OUTBOARD SURFACE FOUND DELAMINATED. REPAIRED AS PER FEDEX E.A. 1-5750-105602, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007010900083 20070109 00083 NM 2007 1 9 07FDEA00037 1 20070105 A 5340 STRINGER CLIP BOEING 727 727233 138408A NM BS 660 S6L DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 STRINGER CLIP HAS BEEN GROUND/DAMAGED AT RADIUS CUT OUT AT BS 660 STR 6L WO NR 35039 SNRM NR N00736. REMOVED AND REPLAC ED WITH NEW STRINGER CLIP AT STA BS 660 STR 4L CLASSIFIED AS A MAJOR REPAIR REF SRM 51-30-3 PG 1. 2 L 7 3 4F RT A3WE 2007010900084 20070109 00084 NM 2007 1 9 07FDEA00038 1 20070105 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM BS 660 S4L DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 STRINGER CLIP HAS BEEN GROUND/DAMAGED IN RADIUS CUT OUT AT BS 660 STR 4L WO NR 35039 SNRM NR N00734. REMOVED AND REPLAC ED STR CLIP AT BS 660 STR 4L CLASSIFIED AS A MAJOR REPAIR REF SRM 51-30-2 PG 1. 2 L 7 3 4F RT A3WE 2007010900085 20070109 00085 NM 2007 1 9 07FDEA00039 1 20070105 A 5340 STRINGER CLIP BOEING 727 727233 138408A NM BS 660 S3R CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 STRINGER CLIP IS CRACKED AT RADIUS CUT OUT AT BS 660 STR 3R. REMOVED AND REPLACED STR CLIP WITH NEW AT BS 660 STR 3R REF 51-30-2 PG 1. 2 L 7 3 4F RT A3WE 2007010900086 20070109 00086 NM 2007 1 9 07FDEA00040 1 20070105 A 5340 STRINGER CLIP BOEING 727 727233 138408A NM BS 660 S1R DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 STRINGER CLIP HAS BEEN GROUND/DAMAGED AT RADIUS CUT OUT AT BS 660 STR 1R. REMOVED AND REPLACED STRINGER CLIP AT BS 660 STR1R ERF SRM 51-30-2 PG 1. 2 L 7 3 4F RT A3WE 2007010900087 20070109 00087 WP 2007 1 9 IXXA070001O 1 20070105 A 2910 CONTROL VALVE DOUG DC8 DC873F 302199F WP HYD SYSTEM LEAKING A IXXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 11 602AL 98559 1446 45991 DURING CLIMB-OUT FROM KBNA, AFTER THE FLAPS WERE RAISED, THE CREW NOTICED THE HYDRAULIC QUANTITY DECREASING. THE CREW P ERFORMED LOSS OF HYDRAULIC CHECKLIST AND RETURNED TO KBNA AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRA FT AND FOUND THE RIGHT WHEEL WELL SOAKED IN HYDRAULIC FLUID. FURTHER INSPECTION FOUND THE WING SLOT CONTROL VALVE LEAK ING FROM DETERIORATED PACKINGS AT THE CENTER MOUNT BOLT. MAINTENANCE REMOVED AND REPLACED THE DEFECTIVE PACKINGS AND RE INSTALLED THE WING SLOT CONTROL VALVE. MAINTENANCE RESERVICED AUXILIARY HYDRAULIC. SYSTEM AND RAN ENGINES AS REQUIRED TO REFILL THE HYDRAULIC SYSTEM. NO LEAKS NOTED AND THE OPERATIONAL CHECK WAS GOOD IAW ATI DC-8 ERH 70.01 AND DC-8 M/M 2 2 L 7 4 4F RT 4A25 2007010900091 20070109 00091 SO 2007 1 9 SIMA200700802 1 20070103 A 3297 14521495403 WIRE HARNESS EMB 145 EMB145LR 3260212 SO LANDING GEAR SHORTED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 637AE 16522 145170 LANDING GEAR AIR GROUND FAIL AND THRUST REVERSER DISAGREE MESSAGE, RETURNED TO DFW. REMOVED AND REPLACED NOSE LANDING G EAR HARNESS IAW EMB 32-63-05. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007010900093 20070109 00093 SO 2007 1 9 SIMA200700807 1 20070104 A 5315 14530645411 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 707EB 15844 4600 145195 FOUND PREVIOUS LEFT OMEGA BEAM REPAIR CORRODED AT FRAME 20. REMOVED EXISTING REPAIR. CLEANED AND TREATED AREA. FABRIC ATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007010900094 20070109 00094 SO 2007 1 9 SIMA200700801 1 20070105 A 3350 20131A BATTERY PACK EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 703MR 10354 2294 145173 EMERGENCY LIGHTS AFT OF ROW 9 INOPERATIVE. REMOVED AND REPLACED NUMBER 4 EMERGENCY BATTERY PACK IAW EMB 33-50-04. OPER ATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007010900095 20070109 00095 SO 2007 1 9 SIMA200700804 1 20070103 A 2520 7277220501 CIRCUIT CARD EMB 145 EMB145LR 3260212 SO PSU BURNED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 694AE 5411 14500869 BURNING ELECTRICAL ODOR AT ROW 4 ON TAXI. REMOVED AND REPLACED PSU CIRCUIT CARD AT ROW 7 IAW EMB AMM 25-28-23. OPERATI ONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007010900105 20070109 00105 NE 2007 1 9 NACA20070001 2 20070105 A 7414 10884501 DISTRIBUTOR PWA CB3 DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE ENGINE SHORTED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 43872 1732 345 P33324 533294 P33324 NR 2 ENGINE BACK FIRING, SUSPECT NR 11 CYLINDER REARS. ENGINE WAS UNABLE TO TAKE LEANING. FOUND PART OF A BROKEN BRUSH WEDGED BETWEEN INNER AND OUTER SEGMENT PLATES OF LEFT DISTRIBUTOR. REPLACED FAULTY DISTRIBUTOR WITH SERVICEABLE UNIT. REF: DAC DC-6 LMM SEC II CH 6-10-2, GROUND RUN CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2007010900106 20070109 00106 NM 2007 1 9 DHL2007747001 1 20070105 A 5753 SKIN BOEING 727 727224 1384076 NM RT FORE FLAP GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 RT INBD FORE FLAP O/B LEADING EDGE HAS GOUGE ON REPAIR DOUBLER. REMOVED AND REPLACED DAMAGED REPAIR FROM RT INBD FORE F LAP O/B LEADING EDGE IAW B727 SRM 57-50-4. 2 L 7 3 4F A3WE 2007010900122 20070109 00122 2007 1 9 QXEA200700009 4 20070105 A 2210 46502004000401 IRS CNDAIR CL600 CL6002C10 1390015 EA NR 2 FAILED A QXEA A UNSCHED LANDING G MULTIPLE FAILURE NR NOT REPORTED 1 NM 09 608QX 8789 773 10026 DEN - FLIGHT 4340, RECEIVED A YAW DAMPER INOP STATUS MESSAGE, PITCH FEEL FAULT STATUS MESSAGE, AUTOPILOT FAILURE, AND PF D AND MFD FAILURES (RED X) ON FO SIDE. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLAC ED THE NR 2 INERITAL REFERENCE SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007010900125 20070109 00125 EA 2007 1 9 QXEA200700010 1 20070104 A 2410 IDG CNDAIR CL600 CL6002C10 1390015 EA NR 2 MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 604QX 10019 DEN - ON TAXI FOR FLIGHT 4321, RECEIVED A GENERATOR NR 2 MESSAGE. RETURNED TO THE GATE. MAINTENANCE PLACED THE NR 2 ID G ON MEL 24-11-1B. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007010900136 20070109 00136 WP 2007 1 9 AALA20070001 1 20070101 A 2432 100105901 CHARGER DOUG DC9 DC982 3022082 WP MASTER BATTERY INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 7509 49803 STL - BATTERY CHARGER LIGHT ILLUMINATED IN FLIGHT. BATTERY CHARGER CIRCUIT BREAKER POPPED. LANDED STL WITHOUT INCIDENT . REPLACED BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007010800118 20070108 00118 EU 2007 1 8 AWXA200700026 1 20070103 A 5320 D53112067200 WEB AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 642AW 584 SAL - CORROSION ON MAIN CABIN WEB, FS 20+2", - Y1670. REPAIRED MAIN CABIN WEB, FS 20 + 2", -Y1670 IAW AWA ER 26-5311-06 362-ES3. 2 L 7 2 4F RT A28NM 2007010800119 20070108 00119 NM 2007 1 8 TSAA0725002 1 20070102 A 2530 72067002 OVEN BOEING 737 73776N 13844CH NM GALLEY SMOKE A TSAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 13 741AL 28641 FLIGHT 476 OGG-SAN, DURING CRUISE FLIGHT, A FLIGHT ATTENDANT NOTICED SMOKE FROM THE RIGHT OUTBOARD OVEN IN THE AFT GALLE Y. THE FLIGHT ATTENDANTS TURNED OFF THE OVEN AND THE SMOKE DISSIPATED. THE FLIGHT CONTINUED TO SAN WITHOUT FURTHER INC IDENT. MAINTENANCE FOUND AND REMOVED BURNT FOOD FROM THE OVEN. THE OVEN THEN OPERATED NORMALLY WITH NO SMOKE. AIRCRAF T WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007010800232 20070108 00232 NM 2007 1 8 SB07001 1 20070101 A 5610 5893543129 WINDSHIELD BOEING 737 7373B7 1384580 NM COCKPIT CRACKED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 530AU 10436 10436 24412 PHL - FLT1612 ON CLIMBOUT FROM PHL, EN ROUTE TO BOS, THE TOP OF THE CAPTAIN'S L1 WINDSHIELD STARTED TO ARC, THEN CRACK. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S L1 WINDSHIELD PER JOB CARD J356-11-01. ALSO, REMOVED AND REPLACED THE WINDOW HEAT CONTROL UNIT PER MM 30-41-11, AS PRECAU TIONARY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007010800237 20070108 00237 NM 2007 1 8 SB07002 1 20070101 A 2420 2299 TRANSFORMER BOEING 737 737301 1384611 NM E&E BAY FAULTY A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 502UW 23232 RDU - FLT849 EN ROUTE FROM CLT TO RDU, CREW REPORTED AN ELECTRICAL BURNING SMELL THROUGHOUT THE CABIN. SMELL APPEARED S TRONGEST AROUND ROW 14. MAINTENANCE FOUND THE CEILING LIGHTS AT ROWS 11/12, RIGHT-HAND SIDE, HAD FAILED. SUSPECT BALLA ST HAD FAILED. AIRCRAFT RELEASED PER MEL 33-2A. ON THE NEXT FLIGHT (FLT1674), EN ROUTE FROM RDU TO CLT, CREW AGAIN REP ORTED AN ODOR IN THE CABIN OF SULPHUR AND/OR PLASTIC BURNING IN THE VICINITY OF ROWS 10 THRU 13. ODOR SEEMED TO IMPROVE WHEN RIGHT PACK AND RECIRCULATION FAN WAS TURNED OFF. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENAN CE FOUND THE SMOKE/SMELL NOT ASSSOCIATED WITH THE CEILING LIGHTS. FOUND THE ODOR COMING FROM THE NR 2 TRANSFORMER RECTI 2 L 7 2 4F RT A16WE 2007010800266 20070108 00266 2007 1 8 2007UALA00018 4 20070102 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R1 DOOR FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 428UA 523 EMERGENCY LIGHT TEST PER 3SV HAS FAULT, EXT LOADS FWD L FAULT. REPLACED DOOR 1R SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007010800328 20070108 00328 EA 2007 1 8 TRAX200700015 1 20070101 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 976EV 7601 EMERGENCY CEILING LIGHT 1 EACH INOP. 2 L 7 2 4F RT A21EA 2007010800349 20070108 00349 EU 2007 1 8 YENA2007001 1 20070101 A 2432 2726CH1 BATTERY EMB ERJ190 ERJ190100IGW 3260408 EU NR 2 OVERTEMP A YENA D RETURN TO BLOCK M OVER TEMP TX TAXI/GRND HDL 1 EA 15 197JB 972 150 19000020 BATTERY 2 OVERTEMP MESSAGE APPEARED ON TAXI. TROUBLESHOT PER E190 FIM TASK 24-36-00-810-804-A. REMOVED AND REPLACED BA TTERY NR 2 PER AMM PART II 24-36-01. OPS CHECKED NORMAL. 2 L 7 2 4F RT A57NM 2007010800354 20070108 00354 NM 2007 1 8 BB07001 1 20070102 A 3230 273N20071 ACTUATOR BOEING 757 757225 1384959 NM RT MLG MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 924UW 68961 22204 FLIGHT 1065, CLT-SXM: AFTER TAKEOFF AND GEAR UP SELECTION, CREW RECEIVED GEAR DISAGREE MESSAGE AND GEAR DOOR LIGHTS. F LIGHT RETURNED TO CLT. MAINTENANCE REPLACED THE RIGHT GEAR UPLOCK ACTUATOR, UPLOCK, AND UPLOCK OPERATED SEQUENCE VALVE. 2 L 7 2 4F RT A2NM 2007010800356 20070108 00356 NM 2007 1 8 CALA0700007 1 20070104 A 5313 BAC1498161 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12327 23457 INSPECTION FOUND STRINGER 27L CORRODED IN FORWARD BAGGAGE BIN AT STA 500A+10 TO 500C. THE CORRODED STRINGER SECTION WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 2007010900082 20070109 00082 NM 2007 1 9 07FDEA00036 1 20070105 A 5340 654531313 STRINGER CLIP BOEING 727 727233 138408A NM BS 660 S9L DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 STRINGER CLIP HAS BEEN GROUND/DAMAGED AT RADIUS CUT OUT BS 660 STR 9L WO NR 35039 SNRM NR N00739. REMOVED AND REPLACED WITH NEW SRT CLIP AT BS 660 STR 9L. THIS CLASSIFIED AS A MAJOR REPAIR REF SRM 51-30-2 PG 1. 2 L 7 3 4F RT A3WE 2007010900150 20070109 00150 NM 2007 1 9 AWXA200700035 1 20070104 A 2560 P4010021 FLASHLIGHT BOEING 737 73733A 1384673 NM ZONE 200 INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 175AW 23634 MCN - EEL - C-21 - FORWARD FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT IS INOPERATIVE. REPLACED FORWARD FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT POWER SUPPLY, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A16WE 2007010900156 20070109 00156 EA 2007 1 9 QXEA200700003 1 20070103 A 2840 73811812 COMPUTER CNDAIR CL600 CL6002C10 1390015 EA FUEL QTY MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 602QX 3231 10010 ELP - TAXI FOR FLIGHT 4017, RECEIVED A "X FLOW" PUMP CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENANCE REPLACED THE F UEL QUANTITY GAUGING COMPUTER AND THE PUMP CARTRIDGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007010900167 20070109 00167 NM 2007 1 9 QXEA200700005 1 20070104 A 6123 POTENTIOMETER DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS OUT OF ADJUST A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 353PH 496 PSC FLIGHT NR 2094, AUTO FEATHER FAILED TO ARM ON TAKEOFF ROLL, AUTO FEATHER SYSTEM INOP. MAINTENANCE ADJUSTED THE POTE NTIOMETER. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007010900168 20070109 00168 EU 2007 1 9 MALA070002 1 20070104 A 3020 NH2466808108 INTAKE DUCT SAAB SF340 340B 7860101 EU RIGHT FAILED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 457XJ 340B457 NOTICED SLIGHT ODOR. FO THEN NOTICED RIGHT ENGINE INTAKE SPARKING, TURNED OFF RIGHT INTAKE, SMOKE ODOR WENT AWAY. THE RIGHT INTAKE LIGHT DID NOT COME ON. REMOVED AND REPLACED RIGHT INTAKE DUCT P/N NH24668-081-08 IAW SF340 AMM 71-60-05. SECURITY CHECK GOOD, SN ON L155395 ALSO REMOVED AND REPLACED RIGHT DE-ICE MODULE IAW SF340 AMM 30-20-15, ALL OPS CHECK G OOD, PN 44730-501 SN ON L248376. 2 L 7 2 4T RT A52EU 2007010900169 20070109 00169 NM 2007 1 9 AWXA200700037 1 20070104 A 5753 6546430129 SKIN BOEING 737 73733A 1384673 NM ZONE 500 DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 PHX - LEFT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED IN SEVERAL PLACES, WBL 73 - WBL 184.275. REPLACED LEFT WIN G INBOARD FORE FLAP IAW AWA TASK CARD R3M27008. 2 L 7 2 4F RT A16WE 2007010900174 20070109 00174 NM 2007 1 9 AWXA200700043 1 20070106 A 5753 6546435343A SKIN BOEING 737 7373G7 1384595 NM ZONE 500 DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 PHX - LEFT WING OUTBOARD TRAILING EDGE FLAP HAS A SMALL AREA DISBOND AT INBOARD LOWER END, WBL 230.68. REPLACED LEFT W ING OUTBOARD TRAILING EDGE FLAP IAW AWA TASK CARD R3M27034. 2 L 7 2 4F RT A16WE 2007010900175 20070109 00175 NM 2007 1 9 AWXA200700044 1 20070105 A 5753 6546431255 SKIN BOEING 737 73733A 1384673 NM ZONE 500 DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 PHX - LEFT WING OUTBOARD FOREFLAP, UPPER SURFACE INBOARD END DELAMINATED, WBL 202.69 - WBL 413.61. REPLACED LEFT WING OUTBOARD FOREFLAP IAW AWA TASK CARD R3M27022. 2 L 7 2 4F RT A16WE 2007010900179 20070109 00179 NM 2007 1 9 QXEA200700007 1 20070104 A 3411 DRAIN BOMBDR DHC8 DHC8402 1390042 NM PITOT STATIC SYS CLOGGED A QXEA C ABORTED TAKEOFF C J F.O.D. WARNING INDICATION TO TAKEOFF 1 NM 09 404QX 4046 SLC FLIGHT NR 2452: ABORTED TAKEOFF DUE TO IAS MISMATCH AT 70 TO 80 KTS, FO AIRSPEED WAS LAGGING UP TO 30 TO 40 KTS. MA INENANCE INSPECTED RT PRIMARY PITOT/STATIC PROBE IAW Q400 AMM TASK 34-11-06-280-801. FOUND THE DRAIN HOLE TO BE PLUGGED . CLEANED DRAIN HOLE AND THEN COMPLIED WITH TASK 34-11-06-680-801 FOR WATER ACCUMULATION PURGE. RAN UP BOTH NR 1 AND N R 2 AIRSPEED FROM 30-250 KTS. NO DEFECTS NOTED. C/W HORZION MTC 6341102 FOR NR 2 PITOT AND NR 2 STATIC. ALL CHECKS GO OD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007010900181 20070109 00181 NM 2007 1 9 07FDEA00045 1 20070105 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 STRINGER CLIP CRACKED AT RADIUS CUT OUT BS 660 STR 2R WO NR 35039 SNRM NR N00731. REMOVED STRINGER CLIP, DRILLED UP NEW CLIP AND INSTALLED NEW CLIP REF SRM 51-30-2. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007010900184 20070109 00184 WP 2007 1 9 AALA20070008 1 20070101 A 3350 BULB DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9627R 53597 DFW - EMERGENCY FLOOD LIGHT IN COCKPIT INOPERATIVE. RELAMPED EMERGENCY FLOOD LIGHT IN COCKPIT. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007010900185 20070109 00185 NM 2007 1 9 AALA20070003 1 20070101 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 348AN 33087 MIA - EMERGENCY LIGHT AT RIGHT AFT OVERWING INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT AFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007010900186 20070109 00186 WP 2007 1 9 AALA20070010 1 20070101 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9627R 53597 DFW - EMERGENCY LIGHT AT OVERWING EXIT SIGN INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT OVERWING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007010900187 20070109 00187 NM 2007 1 9 AALA20070025 1 20070105 A 3350 PBS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 SFO - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007010900189 20070109 00189 EU 2007 1 9 AALA20070006 1 20070101 A 3350 BR964814 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14061 471 MIA - EMERGENCY LIGHT AT SEAT 12C BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY FORE SEAT 12C. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A35EU 2007010900190 20070109 00190 WP 2007 1 9 AALA20070009 1 20070101 A 3350 LENS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9627R 53597 MIA - EMERGENCY LIGHTS AT SEAT ROW 3 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHTS AT SEAT ROW 3. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007010900191 20070109 00191 WP 2007 1 9 AALA20070011 1 20070101 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9627R 53597 DFW - AFT EMERGENCY FLOOD LIGHT AT STAIR WELL INOPERATIVE. CLEANED CONNECTOR FOR AFT EMERGENCY FLOOD LIGHT AT STAIR WEL L. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007010900192 20070109 00192 NM 2007 1 9 AALA20070012 1 20070102 A 2781 ACTUATOR BOEING 757 757223 1384957 NM SLATS INOPERATIVE A AALA O OTHER J WARNING INDICATION DE DESCENT 1 SW 21 620AA 24578 MIA - DURING DESCENT, LEADING EDGE SLAT DISAGREE OCCURRED DURING FLAP EXTENSION FROM ONE DEGREE TO FIVE DEGREES. FOUND N UMBER NINE AND TEN LEADING EDGE ROTARY ACTUATORS TRIPPED. REPLACED NUMBER NINE AND TEN LEADING EDGE ROTARY ACTUATORS. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007010900193 20070109 00193 NM 2007 1 9 AALA20070004 1 20070101 A 2720 ES4101538 RELAY BOEING 737 737823 13844BZ NM RUDDER INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 935AN 30081 MIA - AFTER TAKEOFF, THE STANDBY RUDDER LIGHT ILLUMINATED AND STAYED ON UNTIL THE FLAPS WERE PULLED UP. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED RELAY IN FLIGHT CONTROLS MODULE 053. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007010900194 20070109 00194 WP 2007 1 9 AALA20070013 1 20070102 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 246AA 49258 LGA - EMERGENCY LIGHT AT SEAT 5E INOPERATIVE. FOUND WIRES PULLED FROM CONNECTOR. REPAIRED WIRING FOR EMERGENCY LIGHT A T SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007010900209 20070109 00209 NM 2007 1 9 07FDEA00009 1 20070103 A 5313 A6A71231 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 CAC: LEFT COMPARTMENT AT APPROX LONGERON 38L FOUND LONGERON SPLICE CRACKED. COMPLIED WITH FEDEX E.A. 1-5310-106576, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007010900210 20070109 00210 NM 2007 1 9 07FDEA00010 1 20070103 A 5330 ADA31391 SKIN DOUG MD11 MD11F 3023600 NM ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 FWD CARGO DOOR CUT-OUT, FWD DOOR JAMB FUSELAGE SKIN FOUND WITH SCRATCHES AT LONGERON 41R. REPAIRED AS PER SRM 53-50-00 VOLUME I FIGURE 16. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007011000051 20070110 00051 EA 2007 1 10 SWIA200717633 1 20070102 A 3310 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 740SK 10196 SMOKE FROM FOS SIDE FLOOD LIGHTS. REPLACED RHEOSTAT AND LIGHT ASSEMBLY ABOVE LIGHTING PANEL. OPERATIONAL CHECKS GOOD I AW AMM 33-24-01. 2 L 7 2 4F RT A21EA 2007011000054 20070110 00054 EA 2007 1 10 SWIA200717641 1 20070104 A 3350 INVERTER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 929SW 7703 FORWARD SECTION OF FLOOR EMERGENCY LIGHTS ARE NOT WORKING. REPLACED EMERGENCY LIGHT POWER INVERTER. OPERATIONAL CHECKS GOOD IAW MM 33-51-07. 2 L 7 2 4F RT A21EA 2007011000056 20070110 00056 NM 2007 1 10 07FDEA00013 1 20070103 A 5347 AFA7795507 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 MAIN DECK CARGO COMPARTMENT: SEAT TRACK STA Y = 1185, X = -8.5 FOUND CORRODED. REPLACEMENT FROM STA 1811 TO STA 1885, X = -8.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007011000058 20070110 00058 EU 2007 1 10 07FDEA00015 1 20070103 A 2510 SPRING AIRBUS 300 A300F4605R 3930327 EU RELEASE HANDLE DETACHED A FDEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 25 685FE 803 CAPT SEAT SLIPPED BACK AT 80 KTS REJECTED TAKEOFF, SEAT CHECKED AND LOCKED INTO POSITION. INSPECTED SEAT LOCK MECHANISM , FOUND LEVER SPRING OFF, LEVER-REATTACHED SAME PER SMP-SEAT LOCKS NORMAL. OK FOR SERVICE. INSPECTED SEAT IAW MM 25-11 -11-06-1. FOUND RELEASE HANDLE SPRING OFF, REATTACHED SPRING. CAPT SEAT LOCK CKS GOOD PER MM 25-11-11-05-1. OK FOR SE RVICE. 2 L 7 2 4F RT A35EU 2007011000059 20070110 00059 NM 2007 1 10 07FDEA00016 1 20070103 A 5347 AEA7325 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 MAIN DECK CARGO COMPARTMENT: SEAT TRACK STA Y = 1356, X = -27.5 FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007011000062 20070110 00062 EU 2007 1 10 AALA20070016 1 20070104 A 3350 BR964814 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 90070 513 JFK - EMERGENCY LIGHT AT SEAT 17G INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 17G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A35EU 2007011000063 20070110 00063 NM 2007 1 10 0700016312 1 20070106 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 672US 30267 DURING OVERNIGHT CHECK, CABIN EMERGENCY FLOOR LIGHTS INOP LT SIDE ROWS 51-66. MAINTENANCE REMOVED AND REPLACED EMERGENC Y LIGHTS. OPERATIONAL CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007011000066 20070110 00066 WP 2007 1 10 AALA20070021 1 20070105 A 2150 CONTROL VALVE DOUG DC9 DC983 3022083 WP RT A/C PACK DISCONNECTED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 9302B 49528 LAX - DURING CLIMB UNABLE TO PRESSURIZE AIRCRAFT. RIGHT PACK ON MEL. LEFT RAM AIR SENSE LINE DISCONNECTED. RECONNECTE D LEFT RAM AIR SENSE LINE AND DISCONNECTED RIGHT RAM AIR SENSE LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007011000067 20070110 00067 WP 2007 1 10 AALA20070022 1 20070105 A 4920 5940405503 APU DOUG DC9 DC982 3022082 WP APU BAY CONTAMINATED A AALA A UNSCHED LANDING C B F.O.D. SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 409AA 49320 ATL - RIGHT PACK FILLED CABIN WITH SMOKE AFTER TAKEOFF. SMOKE DISSIPATED WITH NO PACKS RUNNING. LANDED ATL WITHOUT INCI DENT. REPLACED COALESCER BAGS AND ACCOMPLISHED BURN OUT OF HIGH PRESSURE PNEUMATIC DUCTING. PLACARDED APU INOPERATIVE DU E TO HYDRAULIC FLUID INGESTED BY APU. REPLACED APU ON 08JAN2007 AT LGA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007010800240 20070108 00240 EU 2007 1 8 2007UALA00001 1 20070101 A 5210 DOOR FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 488UA 1680 R2 DOOR SILL HAS CORROSION OF AFT FRAME AT FR 68. [SUP 05-04-07] INITIAL BLEND OUT OF CORROSION RESULTED IN THE FRA ME BECOMING OUT OF COMPLIANCE WITH THE ALLOWABLE DAMAGE LIMITS. THE DAMAGED AREA WAS CUT OUT AND REPAIRED IN ACCORDANCE WITH SRM 53-41-14-201. 2 L 7 2 4F 4 F RT A28NM E40NE 2007010800252 20070108 00252 NM 2007 1 8 USAA070012 1 20070103 A 5340 ATTACH ANGLE BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 501UW 23231 STA 767 BL 0 FRAME TO BELLY SKIN ATTACH ANGLE CORRODED. INSTALLED DOUBLER IAW SRM 53-00-07 LEVEL 1 C53-208-01 DEFECT SI ZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007010800262 20070108 00262 NM 2007 1 8 USAA07002 1 20070103 A 5320 FITTING BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 STA 303.5 LBL 11 LBL 44 HAS CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-10-02 LEVEL 1 C53-107-02, DEFECT SIZE: . 5 X 1 INCH. 2 L 7 2 4F RT A16WE 2007010800265 20070108 00265 NM 2007 1 8 2007UALA00017 1 20070103 A 5330 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 226UA 30226 A DENT WAS DISCOVERED APPROXIMATELY 30 INCHES FWD OF DOOR 4L AND 6 INCHES BELOW THE FLOOR. MEASURED DENT AND FOUND IT BEYOND DETAILED LIMITS. BLENDED AREA , APPLIED ALODINE AND PRIMED AREA. DENT IS 3.75" X 4.75" X .132" DEEP. OK TO CARRY FORWARD FOR 16000 FLIGHT CYCLES. REPAIRED :CUT AND REMOVED DAMAGE, ACCOMPLISHED HEFC INSP ON DAMAGE REMOVAL, MADE REP AIR DOUBLER AND INSTALLED. OK FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007010800268 20070108 00268 NM 2007 1 8 2007UALA00020 1 20070103 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 AFT GALLEY RIGHT EEL SIDEWALL INOP. REPLACED POWER CONNECTOR. OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007010800316 20070108 00316 NM 2007 1 8 ASAA0741353 1 20070103 A 5314 65C385021 KEELBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 THE LEFT KEEL BEAM LWR CHORD IS CORRODED CLOSE TO THE BS 540 BUTT JOINT. KEEL BEAM REPAIRED WITH REPAIR PART IAW EA 531 0 02688. 2 L 7 2 4F RT A16WE 2007010800358 20070108 00358 NM 2007 1 8 CALA0700001 1 20070103 A 5315 BAC1518399 FLOORBEAM BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69602 27315 INSPECTION FOUND FLOORBEAM CORRODED AROUND HOLE AT STA 967, RBL 30. THE CORRODED SECTION OF FLOORBEAM WAS CUT OUT AND A REPAIR SECTION WAS INSTALLED IAW SRM 53-00-51, FIGURE 201. 2 L 7 2 4F RT A16WE 2007010900063 20070109 00063 NM 2007 1 9 07FDEA00024 1 20070104 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM BS 440 S6L DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 STRINGER CLIP HAS BEEN GROUND/DAMAGED AT RADIUS CUT OUT BS 440 STRINGER 6L WO NR 35039 SNRM NR N00724. REMOVED DAMAGED STRINGER CLIP DRILLED HOLES AND INSTALLED NEW STRINGER CLIP REF SRM 51-30-02 CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007010900146 20070109 00146 EU 2007 1 9 AALA20070002 1 20070101 A 3260 PROXIMITY SENSOR AIRBUS 300 A300B4605R 3930308 EU LANDING GEAR INOPERATIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 14068 511 JFK INFLIGHT - LANDING GEAR WOULD NOT RETRACT. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED PROXIMITY BOX. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007010900171 20070109 00171 NM 2007 1 9 AWXA200700040 1 20070105 A 5311 654868720 FRAME BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 MCN - RIGHT WHEEL WELL CUT-OUT, FORWARD FRAME CRACKED, BS 663, RBL 63, WL 178. REPLACED RIGHT WHEEL WELL CUT-OUT, FORWA RD FRAME CRACKED, BS 663, RBL 63, WL 178 IAW B737-300 SRM 51-40-05 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007010900172 20070109 00172 NM 2007 1 9 AWXA200700041 1 20070105 A 5311 654868719 FRAME BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 MCN - LEFT WHEEL WELL CUT-OUT, FORWARD CHORD CRACKED, BS 663, LBL 63, WL 178. REPLACED LEFT WHEEL WELL CUT-OUT, FORWARD CHORD CRACKED, BS 663, LBL 63, WL 178 IAW B737-300 SRM 51-40-05 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007010900176 20070109 00176 EU 2007 1 9 AWXA200700045 1 20070107 A 5753 D57571601272 SKIN AIRBUS 320 A320232 3930326 EU ZONE 500 DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 650AW 856 PHX - LEFT WING OUTBOARD FLAP LOWER SURFACE DELAMINATED, WS 8268 - WS 9235. REPAIRED LEFT WING OUTBOARD FLAP LOWER SURF ACE, WS 8268 - WS 9235 IAW A320 SRM 57-30-00. 2 L 7 2 4F RT A28NM 2007010900211 20070109 00211 NM 2007 1 9 07FDEA00011 1 20070103 A 5347 AEA732523 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 MAIN DECK CARGO COMPARTMENT, SEAT TRACK STA Y = 1149, X = -8.5 FOUND CORRODED. REPAIRED AS PER SRM 53-70-00 FIGURE 1 VO LUME 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007011000055 20070110 00055 NM 2007 1 10 07FDEA00012 1 20070103 A 5347 AEA732523 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 MAIN DECK CARGO COMPARTMENT: SEAT TRACK STA Y = 1189, X = -8.5 FOUND CORRODED. REPLACEMENT CARRIED OUT FROM STA 1129 T O STA 1229, X= 8.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007011000057 20070110 00057 NM 2007 1 10 07FDEA00014 1 20070103 A 5347 AEA732523 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 MAIN DECK CARGO COMPARTMENT: SEAT TRACK STA Y = 1356, X = -8.5 FOUND CORRODED. REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007011000064 20070110 00064 WP 2007 1 10 AALA20070018 1 20070104 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 449AA 49475 LGA - EMERGENCY LIGHT AT FIRST CLASS FORWARD ATTENDANT SEAT INOPERATION. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT F IRST CLASS FORWARD ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007011000065 20070110 00065 NM 2007 1 10 AALA20070019 1 20070105 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39367 25194 MIA - EMERGENCY LIGHT AT SEAT 32H INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 32H. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A1NM 2007011000075 20070110 00075 NM 2007 1 10 HALA0700007 1 20070104 A 4990 GTCP331200ER APU BOEING 767 767300 1385204 NM APU BAY INOPERATIVE A HALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 13 585HA 16153 16153 24257 ETOPS SIGNIFICANT SYSTEM, APU FAIL EICAS AND NO APU START ON TAXI IN. APU FAULT. APU OIL SHOWS ADD THEN .25 ON BLOCK I N. REMOVED AND REPLACED APU PER HAL M266-767, OPS CHECK NORMAL REMOVED PLACARD. 2 L 7 2 4F RT A1NM 2007011000077 20070110 00077 NM 2007 1 10 HALA0700009 1 20070106 A 8011 774860A4 STARTER BOEING 767 767300 1385204 NM NR 1 ENGINE FAILED A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 586HA 2851 2851 24259 BTB - ENG NR 1, N2 FAILED TO ROTATE WITH START SELECTOR IN GRD. START VLV LIGHT EXTINGUISHED AND DUCT PRESS NORM. FOUN D NR 1 STARTER ASSY FAILED REPLACED NR 1 STARTER ASSY PER AMM 80-11-01. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A1NM 2007011000081 20070110 00081 2007 1 10 SIMA200700317 4 20070102 A 3420 DISPLAY EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 637AE 145170 FIRST OFFICERS MULTIPLE FUNCTIONAL DISPLAY FLICKERED AND FOLLOWED BY ELECTRICAL SMELL. 2 L 7 2 4T RT T00011AT 2007011000083 20070110 00083 2007 1 10 SIMA200700316 4 20070102 A 3420 7014300901 DISPLAY EMB 135 EMB135KL 3260302 SO COCKPIT FAILED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 811AE 12482 145529 "SUP" CAPTAINS MULTIPLE FUNCTIONAL DISPLAY WENT BLANK FOLLOWED BY A BURNING ODOR. REMOVED AND REPLACED MULTIPLE FUNCTIO NAL DISPLAY. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007011000096 20070110 00096 EA 2007 1 10 TRAX200700031 1 20070105 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 171 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 ETNRC 2000-16 LOWER FRAME AND SUPPORT CLIPS AT FS 171.00 BETWEEN LBL 12.00 AND RBL 12.00 ARE BENT, CRACKED. LOWER FRAME AND SUPPORT CLIPS AT FS 171.00 BTW LBL12.00 AND RBL 12.00 REMOVED AND REPLACED IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007011000099 20070110 00099 NM 2007 1 10 SWAA070043 1 20070104 A 3350 20121 CHARGER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007011000101 20070110 00101 NM 2007 1 10 SWAA070045 1 20070104 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 775SW 30590 EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT ROW 6 ABC. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007011000102 20070110 00102 NM 2007 1 10 SWAA070046 1 20070104 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 504 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPV CHECK, FOUND STRINGER 14L CRACKED AT BS 504. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007011000103 20070110 00103 NM 2007 1 10 SWAA070047 1 20070104 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM BS 378 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 378.5, LBL 2.8 E&E EXHAUST PORT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007011000105 20070110 00105 NM 2007 1 10 SWAA070049 1 20070104 A 5551 6551524 ATTACH FITTING BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND RT AND LT HORIZONTAL STAB FITTING CLEVIS LUG FACES CORRODED. REPAIRED HORIZONTAL STAB PER SRM. 2 L 7 2 4F RT A16WE 2007011000108 20070110 00108 SO 2007 1 10 RAIA00701002 1 20070102 A 2760 14533022409 CONTROL UNIT EMB 145 EMB145LR 3260212 SO SPOILERS UNKNOWN A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 815HK 12745 145048 FLT NR 5577 - STL - DURING TAXI INTERMITTENT SPOILER FAIL CAPTION APPEARED ON THE EICAS. MAINTENANCE REMOVED AND REPLAC ED THE SPOILER CONTROL UNIT. 2 L 7 2 4T RT T00011AT 2007011000109 20070110 00109 SO 2007 1 10 RAIA00701003 1 20070104 A 3246 31551 WHEEL EMB 145 EMB145LR 3260212 SO MLG OUT OF BALANCE A RAIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 03 817HK 145058 FLT NR 5454 - STL - JUST AFTER TAKEOFF, CREW EXPERIENCED VERY STRONG VIBRATION COMING FROM THE COCKPIT. MAINTENANCE INS PECTED THE AIRCRAFT AND PERFORMED SEVERAL GEAR OPERATIONAL CHECKS. FOUND THE NOSE WHEEL ASSEMBLIES TO BE OUT OF BALANCE . REMOVED AND REPLACED THE NOSE WHEEL ASSEMBLIES. 2 L 7 2 4T RT T00011AT 2007011000110 20070110 00110 SO 2007 1 10 RAIA00701005 1 20070104 A 3350 1317 BULB EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHTS BURNED OUT A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 827HK 145021 PRE FLT NR 5511 - STL - EMERGENCY LIGHT AT SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BULB. 2 L 7 2 4F RT T00011AT 2007011000111 20070110 00111 SO 2007 1 10 RAIA00701006 1 20070101 A 8000 241244013002 CONTROL BOX EMB 145 EMB145LR 3260212 SO NR 2 ENGINE UNKNOWN A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 815HK 14897 14897 145048 FLT NR 5485 - STL - AFTER NR 2 ENGINE STARTED ENGINE NR 1 VIBRATION METER WAS AT THE TOP OF THE AMBER RANGE AND NR 2 ENG INE HP WAS AT THE TOP OF THE RANGE. MAINTENANCE REMOVED AND REPLACED THE ENGINE VIBRATION MONITOR CONTROL BOX. 2 L 7 2 4T RT T00011AT 2007011000113 20070110 00113 NM 2007 1 10 NOCA00607 1 20070106 A 2560 SG9422 GLOWSTRIP BOEING 757 75728A 1384976 NM CAIBN FAILED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 755NA 30043 PHOTO LUMINESCENT STRIP LEFT-HAND AND RIGHT-HAND FWD GALLEY TO SEATS 1 ABC AND 1 DEF WILL NOT ILLUMINATE. REPLACED LUMI NESCENT STRIP AT 1 ABC AND 1 DEF. 2 L 7 2 4F RT A2NM 2007011000114 20070110 00114 NM 2007 1 10 NOCA00707 1 20070106 A 2560 SG9601 GLOWSTRIP BOEING 757 75728A 1384976 NM CABIN FAILED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 755NA 30043 PHOTO LUMINESCENT E-PATH STRIP AT SEATS 34 DEF TO 37 DEF WILL NOT ILLUMINATE. REPLACED E-PATH LUMINESCENT STRIP AT 34 D EF AND 37 DEF. 2 L 7 2 4F RT A2NM 2007011000120 20070110 00120 EA 2007 1 10 TRAX200700020 1 20070103 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 ASD LOWER STEP CRACKED AT ATTACH POINT. 2 L 7 2 4F RT A21EA 2007011000121 20070110 00121 EA 2007 1 10 TRAX200700022 1 20070103 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 843AS 7310 FUSELAGE STATION 621 AFT PRESSURE BULKHEAD IS CRACKED BY UPPER CARGO DOOR CUTOUT STIFFENER ATTACH POINT. CRACK APPROX 0 .025 IN LENGTH MARKED. 2 L 7 2 4F RT A21EA 2007011000122 20070110 00122 NE 2007 1 10 PCSA10420071 2 20070104 A 7230 JT8D17 COMPRESSOR BOEING 727 727212 138407G NM PWA JT8 JT8D* NE NR 3 ENGINE DAMAGED A PCSA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SO 29 598AJ 54904 2660 21947 687350 FLIGHT 743 DURING THE TAKEOFF ROLL FROM MIA THE CREW EXPERIENCED A VIBRATION ON THE NUMBER 3 ENGINE, THE TAKEOFF WAS ABO RTED AND THE AIRCRAFT RETURNED BACK TO THE GATE WITHOUT ANY FURTHER INCIDENT. MAINTENANCE INSPECTED THE NR 3 ENGINE AND FOUND THE C-2 COMPRESSOR BLADES SHOWED EVIDENCE OF FOD DAMAGE, THE NR 3 ENGINE WAS REMOVED AND ANOTHER SERVICEABLE NR 3 ENGINE IS IN PROCESS OF INSTALLATION. A SUPPLEMENT TO THIS SDR WILL FOLLOW. 2 L 7 3 4F 4 F A3WE E2EA 2007011000127 20070110 00127 NM 2007 1 10 SWAA070054 1 20070104 A 3350 GE1317 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 254WN 32512 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 15 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007011000128 20070110 00128 NM 2007 1 10 SWAA070055 1 20070104 A 3350 307IBPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 408WN 27895 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 7 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007011000129 20070110 00129 NM 2007 1 10 SWAA070056 1 20070104 A 3350 307IBPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 408WN 27895 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 19 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007011000132 20070110 00132 NM 2007 1 10 SWAA070079 1 20070108 A 3350 311500 LENS BOEING 737 7373Y0 1384671 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 15 DEF. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007011000133 20070110 00133 NM 2007 1 10 SWAA070080 1 20070108 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 970 S22L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 22L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007011000135 20070110 00135 NM 2007 1 10 SWAA070082 1 20070108 A 3350 656633 SIGN BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 LEFT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2007011000136 20070110 00136 2007 1 10 SWAA070083 4 20070108 A 2565 D31354433 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007011000138 20070110 00138 2007 1 10 SWAA070085 4 20070108 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007011000145 20070110 00145 NM 2007 1 10 SWAA070092 1 20070108 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 417WN 29822 DURING SCHEDULED HC2 CHECK, FWD CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007011000147 20070110 00147 EA 2007 1 10 TRAX200700024 1 20070104 A 5730 PANEL CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 841AS 7300 RIGHT WING PLANK CRACKED AT WS 148.19 APPROX (REF AD2002-03-14REP). REPAIRED IAW ALL SRMS. 2 L 7 2 4F RT A21EA 2007011000152 20070110 00152 NM 2007 1 10 SWAA070065 1 20070106 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727B S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007011000153 20070110 00153 NM 2007 1 10 SWAA070066 1 20070106 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM BS 908 S22L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 22L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007011000156 20070110 00156 NM 2007 1 10 SWAA070069 1 20070106 A 5753 65C26343 CARRIAGE BOEING 737 7373H4 1384600 NM RT WING TE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND RIGHT WING INBOARD MID FLAP OUTBOARD CARRIAGE CORRODED. REMOVED AND REPLACED FLAP CAR RIAGE PER MM. 2 L 7 2 4F RT A16WE 2007011000158 20070110 00158 NM 2007 1 10 SWAA070071 1 20070106 A 5311 6545815 FRAME BOEING 737 7373H4 1384600 NM BS 344 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 344, STR 16L. REMOVED AND REPLACED FRAME SECTION PER SRM . 2 L 7 2 4F RT A16WE 2007011000159 20070110 00159 2007 1 10 SWAA070072 4 20070106 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007011000161 20070110 00161 NM 2007 1 10 SWAA070057 1 20070105 A 3350 65C27093 HOUSING BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED A2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT HOUSING BROKEN. REMOVED AND REPLACED HOUSING ASSY PER MM. 2 L 7 2 4F RT A16WE 2007011000162 20070110 00162 NM 2007 1 10 SWAA070058 1 20070105 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 933 S23R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 933, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007011000165 20070110 00165 NM 2007 1 10 SWAA070061 1 20070105 A 5330 6545765 SKIN BOEING 737 7375H4 138449D NM BS 872 S25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 872, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007011000166 20070110 00166 NM 2007 1 10 SWAA070074 1 20070106 A 5310 6547952358 DOOR FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR FWD FRAME CRACKED AT BETWEEN NR 2 AND NR 3 STOP FITTINGS. REMOVED AND R EPLACED CARGO DOOR PER MM. 2 L 7 2 4F RT A16WE 2007011000167 20070110 00167 2007 1 10 SWAA070075 4 20070107 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 R1 DOOR EMERGENCY EVAC SLIDE OUT ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007011000169 20070110 00169 2007 1 10 SWAA070077 4 20070107 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 771SA 27879 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007011000170 20070110 00170 NM 2007 1 10 SWAA070078 1 20070107 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 724SW 27856 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 26 TO RBL 42. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007011000173 20070110 00173 WP 2007 1 10 UPS07848831 1 20070105 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 COURIER EMERGENCY LIGHTING INOP. REPLACED BATTERY PACK. OPS CHECKS GOOD 33-31-01-2. 2 L 7 4 4F RT 4A25 2007011000174 20070110 00174 NM 2007 1 10 WRLA2007002 1 20070108 A 2120 UNKNOWN DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE COCKPIT SMOKE A WRLA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 277WA 34816 48743 TO+15 MIN SMOKE & FUMES IN COCKPIT, UNKNOWN SOURCE. COCKPIT DOOR POWER & RECIRC FANS TURNED OFF. SMOKE DISSIPATED SOME . RETURN TO ORIGIN. CHECKED RECIRC FANS, ALL CHECKED GOOD, CHECKED MUX SYSTEM OPS CHECK GOOD. CHECKED WIRING IN OVERH EAD, FOUND NO PROBLEMS. CHECKED WIRING IN CAC ALL CHECKED GOOD. CHECK AVIONIC BAY NO SMELL OR SMOKE NOTED. NO APPAREN T BURNT WIRING. RAN ALL 3 ENG OPERATED PACKS NO SMELLS NOTED. PERFORMED VISUAL WALKAROUND OF OUTSIDE OF ACFT NO DEFECT S NOTED. NO POPPED C/B'S OR WARNINGS DETECTED, ACFT OK FOR FURTHER FLIGHT. 2 L 7 3 4F 4 F RT A22WE E24NE 2007011000180 20070110 00180 NM 2007 1 10 2007UALA00040 1 20070105 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE GALLEY INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 194UA 26892 WALL EEL INOP AT LT SIDE MID GALLEY. REPAIRED CONNECTION . OP CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007011000181 20070110 00181 NM 2007 1 10 2007UALA00041 1 20070105 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 194UA 26892 ALL RIGHT OUTBOARD FIRST CLASS EEL INOP. *S/D* REPLACED BATTERY, OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007011000182 20070110 00182 NM 2007 1 10 2007UALA00042 1 20070105 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 194UA 26892 EMERGENCY LIGHT INOP AT CEILING ROW 6 LT AND RT OVERWING AFT MOST ASSY AFT BULB. RELAMPED EMERGENCY LIGHT, OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007011000189 20070110 00189 NM 2007 1 10 SWAA070097 1 20070108 A 3350 GE1317 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 754SW 29849 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 6 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007011000190 20070110 00190 NM 2007 1 10 SWAA070098 1 20070108 A 3350 GE1317 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 754SW 29849 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 11 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007011000191 20070110 00191 NM 2007 1 10 SWAA070099 1 20070108 A 3350 GE1317 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 754SW 29849 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 16 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007011000192 20070110 00192 NM 2007 1 10 07FDEA00055 1 20070109 A 5730 DOUBLER DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RT WING UPPER SURFACE DOUBLER AT XORS 264 FOUND CORROSION. REPAIRED AS PER FEDEX E.A. 1-5710-105593, REPAIR CLASSIFIE D AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007011000194 20070110 00194 NM 2007 1 10 07FDEA00058 1 20070109 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 CABIN STA 755 X = -8.5 SEAT TRACK LOWER FLANGE FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007011100001 20070111 00001 EU 2007 1 11 0700043239 1 20070106 A 3350 LIGHT AIRBUS 320 A320212 3930322 EU ESCAPE SLIDE FAILED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 339NW 367 TEST OF EMERGENCY LIGHT SYSTEM FAILED. DOOR 2 RIGHT EVACUATION SLIDE LIGHTS LOAD FAULTED. REPLACED DOOR 2 RIGHT SLIDE ASSEMBLY. CHECKS OK. 2 L 7 2 4F RT A28NM 2007011100009 20070111 00009 NM 2007 1 11 07FDEA00048 1 20070106 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM BS 680 S5L CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 CABIN, STRINGER CLIP AT BS 680 STR 5L IS CRACKED IN RADIUS OF CUTOUT. REMOVED AND REPLACED STRINGER CLIP AT BS 680 STR 5L REF SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007011100011 20070111 00011 NM 2007 1 11 07FDEA00051 1 20070108 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 DURING HFEC INSPECTION AT THE RIGHT WING TANK, CRACK WAS FOUND AT THE END OF STRINGER 14 (XORS 521) WITH APPROX 11" IN LENGTH. TRIMMED OUT AND REPAIRED WITH SPLICE AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GM M 6- 2-100. 2 L 7 3 4F RT A22WE 2007011100013 20070111 00013 NM 2007 1 11 07FDEA00053 1 20070108 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 DURING HFEC INSPECTION ON THE LEFT WING TANK, CRACK WAS FOUND AT THE END OF STRINGER 14 (XORS 521) WITH APPROX 13" IN LENGTH. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007011100015 20070111 00015 EA 2007 1 11 SWIA200717642 1 20070102 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 920SW 7660 EMERGENCY LIGHT OVERHEAD ROW 5 INOP. REPLACED LAMP. OPERATIONAL TEST GOOD, REF MM CH 33-51-00. 2 L 7 2 4F RT A21EA 2007010900076 20070109 00076 NM 2007 1 9 07FDEA00030 1 20070105 A 5311 AFA00273 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 MAIN DECK CARGO COMPARTMENT: MAIN FRAME STA 1781 LONGERON 12R FOUND DENTED. REPAIR CARRIED OUT AS PER SRM 53-30-00 VOLU ME I FIGURE 1. INITIAL INSPECTION REQUIRED AT 14,500 CYCLES AND REPETITIVE INSPECTION REQUIRED EVERY 9,500 CYCLES THERE AFTER AS PER SRM 53-30-00 VOLUME I FIGURE 1. REPAIR CLASSSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007010900090 20070109 00090 EU 2007 1 9 SIMA200700803 1 20070104 A 5410 COWLING SAAB SF340 340B 7860101 EU LT NACELLE DEPARTED A SIMA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SW 21 904AE 340B314 LEFT INBOARD ENGINE COWLING DEPARTED AIRCRAFT ON TAKEOFF, POST INSPECT FOUND NUMBER 1 STARTER/GENERATOR, LEFT ELEVATOR A ND LEFT HORIZONTAL STABILIZER DAMAGED. 2 L 7 2 4T RT A52EU 2007010900180 20070109 00180 NM 2007 1 9 07FDEA00043 1 20070105 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM BS 440 S2R DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 STRINGER CLIP HAD UPPER RADIUS GROUND/DAMAGED AT BS 440 STR 2R. REMOVED AND REPLACED STRINGER CLIP AT STA 440 STR 2R, R EF SRM51-30-02 PG 2. 2 L 7 3 4F RT A3WE 2007010900182 20070109 00182 NM 2007 1 9 07FDEA00046 1 20070105 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM BS 560 S3R GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 STRINGER CLIP AT BS 560 STR 3R IS GOUGED/DAMAGED WO NR 35039 SNRM NR N00947. REMOVED AND REPLACED STRINGER CLIP REF SR M 51-30-2 PG 2 CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007010900188 20070109 00188 WP 2007 1 9 AALA20070017 1 20070104 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 449AA 49475 LGA - CEILING EMERGENCY LIGHTS AT SEAT ROW 9 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT SEAT RO W 9. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007010900195 20070109 00195 NM 2007 1 9 AALA20070014 1 20070102 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 674AN 29424 MIA - EMERGENCY LIGHT AT SEAT 36D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 36D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007011000052 20070110 00052 EA 2007 1 10 SWIA200717634 1 20070101 A 3310 HOLDER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT SPARKS A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 956SW 7825 FOS CHART HOLDER SHOT OUT SPARKS AND CHART HOLDER CB 246 POPPED OUT. SECURED SCREW ON FOS CHART HOLDER. OPERATIONAL CH ECKS GOOD. 2 L 7 2 4F RT A21EA 2007011000069 20070110 00069 NM 2007 1 10 AALA20070023 1 20070105 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 349AN 33088 DFW - CEILING EMERGENCY LIGHT AT LEFT SIDE FORWARD LEFT NUMBER FOUR DOOR INOPERATIVE. RELAMPED CEILING EMERGENCY LIGHT AT LEFT SIDE FORWARD OF LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007011000094 20070110 00094 EA 2007 1 10 TRAX200700029 1 20070105 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA BS 169 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 ETNRC 2000-13 LOWER SKIN AT FS 169.00 BETWEEN LBL 12.00 AND RBL 12.00 IS CRACKED. LOWER SKIN AT FS 169.00 BTW LBL 12.00 AND RBL 12.00 REMOVED AND REPLACED IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007011000106 20070110 00106 SO 2007 1 10 RAIA00701007 1 20070104 A 3350 BULB EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS BURNED OUT A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 807HK 145119 PRE FLIGHT NR 3542 - STL - AFT EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BULB. 2 L 7 2 4F RT T00011AT 2007011000115 20070110 00115 NM 2007 1 10 NOCA00807 1 20070107 A 3350 LENS BOEING 757 75728A 1384976 NM EMERGENCY LIGHTS MISSING A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 752NA 28174 L4 DOOR EMERGENCY EXIT SIGN ASSY MISSING LENS. REMOVED AND REPLACED LIGHT ASSY. 2 L 7 2 4F RT A2NM 2007011000123 20070110 00123 NM 2007 1 10 SWAA070050 1 20070104 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007011000143 20070110 00143 2007 1 10 SWAA070090 4 20070108 A 2565 6557463 GIRT BAR BOEING 737 7373H4 1384600 NM R1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FWD GIRT BAR FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007011000148 20070110 00148 EA 2007 1 10 TRAX200700025 1 20070104 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BULKHEAD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 841AS 7300 RIGHT FS 625 CLIP SUSPECTED CRACKED ON AFT SIDE OF AFT PRESSURE BULKHEAD 3:00. REMOVED, FABRICATED, AND INSTALLED RT FS 625 CLIP ON AFT SIDE OF AFT PRESSURE BULKHEAD 3:00 IAW CRJ 200 SRM 51-24-16, 51-25-01, AND 51-42-06 .050" 2024 T3 PO 10079142. 2 L 7 2 4F RT A21EA 2007011000155 20070110 00155 NM 2007 1 10 SWAA070068 1 20070106 A 5753 65522112 TORQUE TUBE BOEING 737 7373H4 1384600 NM RT WING TE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND RIGHT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQU E TUBE PER MM. 2 L 7 2 4F RT A16WE 2007011000157 20070110 00157 NM 2007 1 10 SWAA070070 1 20070106 A 3350 1619 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED A2 CHECK, FOUND FWD RIGHT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007011000163 20070110 00163 2007 1 10 SWAA070059 4 20070105 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007011000168 20070110 00168 NM 2007 1 10 SWAA070076 1 20070107 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 483WN 32472 EEPLS COVER BROKEN AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007011000179 20070110 00179 NM 2007 1 10 2007UALA00039 1 20070104 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 POWER INTERRUPTION, EMERGENCY EXIT LIGHTS CAME ON, FLOOR STRIP INOP AT ROWS 15-21. REPLACED INTERTER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007011000185 20070110 00185 NM 2007 1 10 SWAA070093 1 20070108 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 417WN 29822 DURING SCHEDULED HC2 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007011000186 20070110 00186 NM 2007 1 10 SWAA070094 1 20070108 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 417WN 29822 DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007011000187 20070110 00187 NM 2007 1 10 SWAA070095 1 20070108 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 462WN 32466 DURING SCHEDULED HC2 CHECK, FOUND FWD LEFT CABIN EEPLS COVER LOOSE. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007011000188 20070110 00188 NM 2007 1 10 SWAA070096 1 20070108 A 3350 307IBPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 462WN 32466 DURING SCHEDULED HC2 CHECK, FOUND FWD LEFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007011000193 20070110 00193 NM 2007 1 10 07FDEA00057 1 20070109 A 5710 DUCT DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LEFT WING TELESCOPIC DUCT OUTBOARD CUTOUT FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 42 VOLUME I AND FEDEX E.A. #1-5710-107766, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007011100014 20070111 00014 NM 2007 1 11 07FDEA00054 1 20070109 A 5730 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RT WING UPPER SURFACE TRAILING EDGE MOST INBD FOUND CORROSION. REPAIRED AS PER FEDEX E.A. 1-5710-107764, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007011100017 20070111 00017 NM 2007 1 11 07FDEA00017 1 20070103 A 5730 ARB73952 SKIN DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING UPPER SURFACE CORROSION AT XORS 1011. COMPLIED WITH FEDEX E.A.# 1-5710-105601, REPAIR CLASSIFIED AS MINOR PE R GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007011100021 20070111 00021 NM 2007 1 11 07FDEA00020 1 20070104 A 5730 ARB73952 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RT WING UPPER SKIN LOWER SURFACE FOUND CORROSION AT XORS= 720 TO XORS= 726. COMPLIED WITH FEDEX E.A 1-5720-106578, REP AIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007011100022 20070111 00022 EU 2007 1 11 MALA070003 1 20070108 A 3297 CONNECTOR SAAB SF340 340B 7860101 EU LT MLG DISCONNECTED A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 438XJ 340B438 LT MAIN GEAR INDICATION DID NOT SHOW DOWN AND LOCKED. INTRANSIT LIGHT WENT OUT WITH NOSE AND RT MAIN GEAR DOWN. FOLLOW ED QRH. FOUND LT GEAR DOWNLOCK CONNECTOR TO BE DISCONNECTED. RECONNECTED CONNECTOR, COMPLETED OPS CHECKS. 2 L 7 2 4T RT A52EU 2007011100023 20070111 00023 2007 1 11 HALA0700011 4 20070106 A 3410 6225048104 CONTROL PANEL BOEING 767 767300 1385204 NM HSI FAILED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 584HA 13647 13647 24258 ETOPS SIGNIFICANT SYSTEM, HSI RANGE SELECTOR WHEN 10 MI RANGE IS SELECTED, HSI DISPLAYS 20 MI, ON F/O SIDE. REPLACE F/O EFIS CONTROL PANEL OPS CK OK PER MM 34-22-02 PERFORMED MCDP TEST 30 PASS, A/C TO MAINTAIN LMP LAND 3 STATUS. 2 L 7 2 4F RT A1NM 2007011100034 20070111 00034 NM 2007 1 11 ASAA0741373 1 20070110 A 5751 SKIN BOEING 737 7374Q8 138447Q NM AILERON PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 0867 25107 RIGHT AILERON HAS PUNCTURE ON LOWER SURFACE AT O/B END. PREPPED DAMAGED AREA, FABRICATED AND BONDED REPAIR PIECES IAW S RM 51-70-03 REPAIR 2. 2 L 7 2 4F RT A16WE 2007011100035 20070111 00035 NM 2007 1 11 ASAA0741374 1 20070110 A 5330 655298865 SKIN BOEING 737 7374Q8 138447Q NM BS 1004-1016 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 FUSELAGE SKIN DENTED AT 2 PLACES BSTA 1011 ONE ABOVE AND ONE BELOW STR 14R LAP. REMOVED DAMAGED AREAS OF SKIN, FABRICAT ED AND INSTALLED FILLERS DOUBLERS AND TRIPLERS IAW SRM 53-00-01 FIG 201. 2 L 7 2 4F RT A16WE 2007011100039 20070111 00039 NM 2007 1 11 SWAA070103 1 20070109 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED SPV CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 1, WL 186. REMOVED AND REPLACED WEB SECTION PER S RM. 2 L 7 2 4F RT A16WE 2007011100041 20070111 00041 NM 2007 1 11 ASAA0741357 1 20070107 A 2530 860902000 OVEN BOEING 737 7374Q8 138447Q NM NR 1 GALLEY ODOR A ASAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 02 764AS 25101 FWD GALLEY OVEN CAUSES STRONG ELEC ODOR AND TRIPS GALLEY PWR. DEFERRED OVENS INOP COLLARDED CB'S PER MEL. 2 L 7 2 4F RT A16WE 2007011100043 20070111 00043 NM 2007 1 11 ASAA0741359 1 20070108 A 5753 65C2632018 SKIN BOEING 737 7374Q8 138447Q NM RT TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 775AS 25108 RIGHT OUTBOARD MID FLAP INBOARD SIDE LWR SURFACE OF LEADING EDGE HAS CHAFING DAMAGE. REPAIRED OUTBOARD MID FLAP LEADING EDGE IAW SRM 57-53-01 FIG 201. 2 L 7 2 4F RT A16WE 2007011100044 20070111 00044 NM 2007 1 11 ASAA0741360 1 20070108 A 5754 65C26602311 SKIN BOEING 737 7374Q8 138447Q NM NR 2 SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 775AS 25108 SLAT NR 2 OUTBOARD UPPER TRAILING EDGE PREVIOUS REPAIR IS DAMAGED. NR 2 SLAT REPAIRED CORE AND DOUBLER IAW SRM 51-70-10 . 2 L 7 2 4F RT A16WE 2007011100045 20070111 00045 NM 2007 1 11 ASAA0741361 1 20070108 A 5311 654795978 FRAME BOEING 737 7374Q8 138447Q NM BS 794 S19-27R CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 775AS 25108 AFT CARGO DOORWAY FWD FRAME WEB CORRODED 3 INCHES ABOVE STR 25R BS 794.3. REPAIRED WITH FABRICATED REPAIR PART IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007011100047 20070111 00047 NM 2007 1 11 ASAA0741363 1 20070108 A 5553 6547401510 ATTACH ANGLE BOEING 737 7374Q8 138447Q NM VERTICAL STAB CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 775AS 25108 VERTICAL STABLIZER AT REAR SPAR AREA PANEL ATTACH ANGLE CRACKED AT APPROX FIN STA 140. VERTICAL STABLIZER REAR SPAR TO SKIN PANEL ATTACH ANGLE AT FIN STATION 140 REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007011100048 20070111 00048 NM 2007 1 11 ASAA0741364 1 20070108 A 5751 65C2591129 SPAR BOEING 737 7374Q8 138447Q NM LT AILERON DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 775AS 25108 THE LEFT WING AILERON REAR SPAR IS DELAMINATED AT THE INBOARD END. LEFT WING AILERON REAR SPAR DELAMINATION REPAIRED IA W SRM 51-70-04 AND ERO 6448 AND EA 2710 01106. 2 L 7 2 4F RT A16WE 2007011100049 20070111 00049 NM 2007 1 11 ASAA0741366 1 20070108 A 5320 65C333671 INTERCOSTAL BOEING 737 7374Q8 138447Q NM BS 947-967 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 PASSENGER CABIN FLOOR INTERCOSTAL CORRODED OUT OF LIMITS AT FS 947.5 967 LBL 44. REMOVED THE DAMAGED INTERCOSTAL LOCATE D DRILLED AND INSTALLED A REPLACEMENT INTERCOSTAL IAW SRM 51-40-05 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007011100050 20070111 00050 NM 2007 1 11 ASAA0741367 1 20070108 A 5320 65C333672 INTERCOSTAL BOEING 737 7374Q8 138447Q NM BS 947-967 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 PASSENGER CABIN FLOOR INTERCOSTAL CORRODED OUT OF LIMITS AT FS 947.5 967 RBL 44. REMOVED THE DAMAGED INTERCOSTAL, LOCAT ED, DRILLED AND INSTALLED A REPLACEMENT INTERCOSTAL IAW SRM 51-40-05 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007011100051 20070111 00051 NM 2007 1 11 ASAA0741368 1 20070108 A 5320 6552878102 SILL BOEING 737 7374Q8 138447Q NM BS 920-1004 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 THE L2 DOOR CUTOUT LOWER MAIN SILL INNER CHORD IS CORRODED OUT OF LIMITS AT FS 920 986.5 WL 208. REMOVED THE DAMAGED CH ORD, LOCATED, DRILLED AND INSTALLED A REPLACEMENT CHORD IAW SRM 51-40-2 AND 51-40-5. 2 L 7 2 4F RT A16WE 2007011100054 20070111 00054 NM 2007 1 11 ASAA0741371 1 20070108 A 5512 657378345 SKIN BOEING 737 7374Q8 138447Q NM HORIZONTAL STAB DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 THE LEFT HORIZONTAL STABLIZER L/E SKIN IS DENTED OUT OF LIMITS AT L/E STA 98. CUT OUT THE DAMAGED AREA OF SKIN, FABRICA TED AND INSTALLED A SKIN FILLER AND INTERNAL REPAIR DOUBLER IAW SRM 55-10-01 FIG 201. 2 L 7 2 4F RT A16WE 2007011100055 20070111 00055 NE 2007 1 11 HNAA0600218 2 20070103 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE NR 2 ODOR A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 07 936HA 145 120637 DURING DESCENT WITH POWER LEVERS AT FLIGHT IDLE THE FLIGHT ATTENDANT NOTICED SMOKE IN FORWARD SECTION OF CABIN, SHUT DOW N RIGHT HAND BLEED WITHOUT IMPROVEMENT, SHUT DOWN BOTH BLEEDS AND SMOKE DISSIPATED. REMOVED AND REPLACED NR 1 ENGINE. MAINTENANCE EVALUATION FLIGHT REQUIRED. EVALUATION FLIGHT UNSATISFACTORY. OIL ODOR IN CABIN AND FLIGHT DECK WITH NR 2 BLEED SELECTED ON, WHEN POWER IS REDUCED TO 20-30 PERCENT TORQUE. REMOVED AND REPLACED NR 2 ENGINE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007011100062 20070111 00062 NM 2007 1 11 DL757070002 1 20070101 A 2700 340565 ISOLATION VALVE BOEING 757 757232 1384965 NM LT HYD SYSTEM LEAKING A DALA O OTHER K FLUID LOSS DE DESCENT 1 SO 27 621DL 22911 LEFT HYD SYS PRESS LIGHT .17 HYD FLUID IN RESEVIOR. FOUND LT SYSTEM EMPANAGE ISOLATION VALVE LEAKING. REPLACED VALVE P ER AMM SERVICED LT HYD SYS CLEANED AFFECTED AREA OF HYD FLUID VALVE LEAK AND OPS CKS NORM. 2 L 7 2 4F RT A2NM 2007011100064 20070111 00064 NM 2007 1 11 DL764070006 1 20070102 A 2131 CONTROLLER BOEING 767 767432ER 1385134 NM CABIN PRESSURE MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 828MH 29699 AT FL 330, CAB ALTITUDE WARNING AND LOSS OF CABIN PRESSURIZATION. CABIN ALT AUTO 2 AND AUTO 1 ON STATUS PAGE. NR 1 PRE SSURE CONTROLLER FAULTS LOW INFLOW. NO PRSOV FAULTS ON ASCTU. REPLACED NR 1 CONTROLLER PER AMM. BITE CHK NR 2 CONTROL LER BITE CHECKS OK. ASCTU BITE CHKS OK. ALSO FOUND ALT SELECT KNOB ON PRESS PANEL STUCK AT 3500. REPLACED PANEL PER A MM. CHECKS OK. 2 L 7 2 4F RT A1NM 2007011100065 20070111 00065 NM 2007 1 11 DL76L070008 1 20070104 A 5751 SEAL BOEING 767 767332 1382001 NM AILERON LOOSE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 192DN 28449 RTB - AILERON SEAL LOOSE. REPLACED SEAL. 2 L 7 2 4F RT A1NM 2007011100067 20070111 00067 NM 2007 1 11 DL764070011 1 20070105 A 2597 WIRE BOEING 767 767432ER 1385134 NM SEAT CHAFED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 828MH 29699 PAX SITTING 35G CLAIMS TO HAVE SEEN A SPARK BETWEEN 34G AND SIDEWALL. ANOTHER PAX VERIFIED THAT. NO CREW MEMBER OBSERVE D ANYTHING AND THERE WAS NO EVIDENCE OF A PROBLEM TO THE CREW. INSPECTED ALL WIRING AND SEAT UNITS. NO PROBLEMS FOUND. AS PRECAUTION FWD EMPOWER SYSTEM TO MCO/PLAC PER MEL 25-20-01I. ALL CBS PULLED/COLLARED. FOUND CHAFFED WIRING AT 34G AT SEAT TRACK. REPAIRED WIRING PER BOEING WIRING STANDARD PRACTICE MANUAL. 2 L 7 2 4F RT A1NM 2007011100078 20070111 00078 WP 2007 1 11 AALA20070035 1 20070108 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 443AA 49469 MIA - EMERGENCY LIGHT AT SEAT 28D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F A6WE 2007011100079 20070111 00079 EU 2007 1 11 AALA20070036 1 20070108 A 3350 BR964814 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 77080 626 MIA - EMERGENCY LIGHT AT SEAT 19C INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 19C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A35EU 2007011100082 20070111 00082 NM 2007 1 11 AALA20070040 1 20070109 A 3350 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 777AN 29585 DFW - EMERGENCY LIGHT AT SEAT 3D FORWARD POSITION INOPERATIVE. RECONNECTED EMERGENCY LIGHT AT SEAT 3D FORWARD POSITION. 2 L 7 2 4F RT T00001SE 2007011100084 20070111 00084 NM 2007 1 11 AALA20070044 1 20070109 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 936AN 29532 MIA - EMERGENCY LIGHT AT SEAT 27D INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 27D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A16WE 2007011100086 20070111 00086 NM 2007 1 11 AALA20070037 1 20070108 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 632AA 24590 MIA - EMERGENCY EXIT LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007011100087 20070111 00087 NM 2007 1 11 AALA20070041 1 20070109 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 797AN 30012 DFW - EMERGENCY LIGHT AT FORWARD GALLEY LEFT EXIT MARKER MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT FORWARD GAL LEY LEFT EXIT MARKER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007011100088 20070111 00088 NM 2007 1 11 AALA20070042 1 20070109 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 797AN 30012 DFW - EMERGENCY LIGHT AT FORWARD GALLEY RIGHT EXIT MARKER MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT FORWARD GA LLEY RIGHT EXIT MARKER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007011100089 20070111 00089 EU 2007 1 11 AALA20070029 1 20070106 A 2720 8168 ACTUATOR AIRBUS 300 A300B4605R 3930308 EU ZONE 100 INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 70072 515 MIA INFLIGHT T1845/06JAN - AFTER TAKEOFF AT FLAP RETRACTION BOTH RUDDER TRAVEL SYSTEMS ONE AND TWO FAULTED. RESET AND F AULTED AGAIN. LANDED MIA WITHOUT INCIDENT. REPLACED THE VARIABLE STOP TRANSDUCER UNIT AND THE VARIABLE STOP ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007011100090 20070111 00090 NE 2007 1 11 AALA20070028 2 20070105 A 7320 VALVE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE FUEL HEAT INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7506 49800 718483 IAD INFLIGHT T1507/05JAN DEC TO DFW - DURING CLIMB, THE LEFT FUEL TEMPERATURE ROSE AT 120 DEGREES THE OIL TEMPERATURE RO SE TO 150 DEGREES AND WAS IN THE YELLOW BAND FOR APPROXIMATELY 10 MINUTES. PULLED LEFT FUEL HEAT TIMER K29. OIL TEMPER ATURE WENT BELOW THE YELLOW ARC AND FUEL TEMPERATURE DROPPED SLIGHTLY DURING DESCENT. LANDED IAD WITHOUT INCIDENT. REP LACED LEFT ENGINE FUEL HEAT VALVE AND INSPECTED TEMPERATURE TABS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007011100092 20070111 00092 NM 2007 1 11 AALA20070031 1 20070106 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 752AN 30260 DFW - EMERGENCY LIGHT AT OVERHEAD LEFT NUMBER THREE DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT OVERHEAD LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007011100093 20070111 00093 WP 2007 1 11 AALA20070030 1 20070106 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 562AA 49344 LGA - EMERGENCY LIGHT AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD GALLEY. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007011100094 20070111 00094 NM 2007 1 11 AALA20070032 1 20070106 A 2530 COFFEEMAKER BOEING 777 777223 1385213 NM GALLEY SPARKS A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 762AN 31479 LHR INFLIGHT T116/06JAN - DURING CLIMB FROM JFK FLIGHT ATTENDANT REPORTED SPARKING UNDER NUMBER 17 COFFEEMAKER IN AFT G ALLEY WHEN TURNED ON. PULLED CIRCUIT BREAKER AS PRECAUTION. NO FAULTS FOUND ON AIRCRAFT WIRING TO COFFEEMAKER NUMBER 1 7 IN AFT GALLEY. REPLACED COFFEEMAKER NUMBER 17 IN AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007011100095 20070111 00095 NM 2007 1 11 AALA20070033 1 20070107 A 3350 CONTROL CIRCUIT BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 917AN 29518 MIA - EMERGENCY EXIT LIGHT AT LEFT AFT DOOR AND AFT GALLEY CEILING INOPERATIVE. RESET SYSTEM FOR INOPERATIVE EMERGENCY EXIT LIGHT AT LEFT AFT DOOR AND AFT GALLEY CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007011100103 20070111 00103 NM 2007 1 11 SWAA070109 1 20070109 A 5523 65C2638416M TAB BOEING 737 7375H4 138449D NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED C3 CHECK, RIGHT ELEVATOR TAB FAILED T/E FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB ASSY PER MM . 2 L 7 2 4F RT A16WE 2007011100105 20070111 00105 NM 2007 1 11 SWAA070111 1 20070109 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM BS 745 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 745, STR 4R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007011100106 20070111 00106 NM 2007 1 11 SWAA070112 1 20070109 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM BS 735B S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 735B, STR 4R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007011100107 20070111 00107 NM 2007 1 11 SWAA070113 1 20070109 A 5330 6545768 SKIN BOEING 737 7375H4 138449D NM BS 370 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 370, STR 4L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007011100108 20070111 00108 NM 2007 1 11 SWAA070100 1 20070109 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM EMERGENCY EXIT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 LEFT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2007011100111 20070111 00111 2007 1 11 SWAA070114 4 20070109 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 428WN 29844 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007011100114 20070111 00114 NM 2007 1 11 SWAA070117 1 20070109 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 773SA 27881 DURING SCHEDULED HC1 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007011100118 20070111 00118 NM 2007 1 11 USAA070016 1 20070108 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 847 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 AFT CARGO FLOORBEAM AT STATION 847 + 12 RBL 13 HAS CORROSION. REPAIRED IAW TR 53-10-06B, DEFECT SIZE: 4 INCHES. 2 L 7 2 4F RT A16WE 2007011100119 20070111 00119 NM 2007 1 11 USAA070015 1 20070108 A 5311 FRAME BOEING 737 737401 1384701 NM BS 277 S3R SEVERED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 BS 277 INBOARD OF S3R ABOVE COCKPIT BULKHEAD SEVERED FRAME. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 53-10-08, DEFECT SIZE: 4 INCHES. 2 L 7 2 4F RT A16WE 2007011100120 20070111 00120 NM 2007 1 11 USAA070022 1 20070109 A 5510 STIFFENER BOEING 737 737401 1384701 NM HORIZONTAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 STATION 175.5 RT HORIZONTAL STAB CRACKED. REPLACED STIFFENER IAW DRAWING NUMBER 65-47513, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007011100123 20070111 00123 NM 2007 1 11 USAA070019 1 20070109 A 5311 FRAME BOEING 737 737401 1384701 NM BS 360 S14-15L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 BS 360 BETWEEN S14L AND 15L CRACKED. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-10-02 AND DRAWING 69-48204, DEFEC T SIZE: 3 INCHES. 2 L 7 2 4F RT A16WE 2007011100124 20070111 00124 NM 2007 1 11 DL738070013 1 20070106 A 3350 767 BULB BOEING 737 737832 13844CF NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 383DN 30346 EMERGENCY LIGHT INOP OUTSIDE AFT OF 2 RT DOOR ON FUSELAGE, RELAMPED. 2 L 7 2 4F RT A16WE 2007011100125 20070111 00125 NM 2007 1 11 DL738070014 1 20070106 A 3350 767 BULB BOEING 737 737832 13844CF NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 383DN 30346 EMERGENCY LIGHT INOP FOR OVERWING AFT HATCH LEFT SIDE, RELAMPED. 2 L 7 2 4F RT A16WE 2007011100127 20070111 00127 NM 2007 1 11 DL76G070016 1 20070107 A 3610 ISOLATION VALVE BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6F 30025 NE LEFT STUCK A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 1501P 24983 704865 L ISOLATION BLD VALVE EICAS MSG WITH OVERHEAD PANEL LIGHT ON. VALVE APPEARS TO BE OPEN. REPLACED L ISOLATION VALVE. V ALVE WAS FROZEN IN MID POSITION RAN VLV, OPS NORMAL. 2 L 7 2 4F 4 F RT A1NM E13NE 2007011100132 20070111 00132 SO 2007 1 11 LR7A07002 1 20070107 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FS 792 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 75 4676 DURING SCHEDULED A CHECK IN WSSS PER JOB CARD HA1200, FOUND BULKHEAD CRACKED AT FS792, WL170, RBL71. REPAIRED BULKHEAD IAW SMP583 53-50-14. LOG PAGE 23307, ITEM M2. 2 H 7 4 4T A1SO 2007011100133 20070111 00133 WP 2007 1 11 IXXA070002O 1 20070109 A 5280 DOOR SEAL DOUG DC8 DC873F 302199F WP NLG DAMAGED A IXXA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 11 606AL 95481 1366 46044 AFTER TAKEOFF OUT OF KIAH, THE CREW FELT A SEVERE VIBRATION AND LOUD NOISE COMING FROM THE NOSE GEAR AREA, WITH THE GEAR UP OR DOWN. THE CREW RETURNED TO KIAH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LANDING GEAR AND FOUND T HE LEFT FORWARD NOSE GEAR DOOR SEAL AFT HALF MISSING. MAINTENANCE REMOVED REMAINING GEAR DOOR SEAL. THE AIRCRAFT WAS R ETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2007011600001 20070116 00001 NE 2007 1 16 SWAA070119 2 20070108 A 7230 COMPRESSOR BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B22 13802 NE LT ENGINE STALLED A SWAA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 29 731SA 27863 874167 INFLIGHT SHUTDOWN/AIR TURNBACK, ON LEVEL OFF AT 10,000 NR 1 ENGINE STARTED TO COMPRESSOR STALL. SECURED NR 1 ENGINE PER QRH. REMOVED AND REPLACED NR 1 ENGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007011600002 20070116 00002 2007 1 16 SWAA070120 4 20070110 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM L1 DOOR SLIDE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2007011600003 20070116 00003 NM 2007 1 16 SWAA070121 1 20070110 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 493WN 32477 EEPLS COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007011600004 20070116 00004 NM 2007 1 16 SWAA070122 1 20070110 A 5310 6545815 DOOR FRAME BOEING 737 7373H4 1384600 NM BS 348 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR CUTOUT AFT LOWER FRAME CRACKED AT BS 348, WL 209. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007011600005 20070116 00005 NM 2007 1 16 SWAA070123 1 20070110 A 5311 6936642 FRAME BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND BULKHEAD FRAME CRACKED AT RIGHT BS 178, WL 208. REMOVED AND REPLACED CHORD SECTION PE R ACO. 2 L 7 2 4F RT A16WE 2007010900147 20070109 00147 NM 2007 1 9 QXEA200700008 1 20070104 A 3297 471515 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM MLG UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 410QX 623 4053 SEA FLIGHT NR 2398: DURING AIRCRAFT LOADING, WEIGHT ON WHEELS CAUTION LIGHT CAME ON. IAS FAIL WENT AWAY WHEN BOARDING C OMPLETED. PUSHED BACK. JUST PRIOR TO TAXI, CAUTION LIGHT ILLUMINATED AGAIN WITH IAS FAIL. UPON RETURNING TO GATE, SAM E THING HAPPENED 3 MORE TIMES. MAINTENANCE REMOVED AND REPLACED NGWOFW2 HARNESS. PERFORMED RIGGING ADJUSTMENT OF NGWOF W2 SENSORS. OPS CHECK GOOD. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007010900208 20070109 00208 NM 2007 1 9 07FDEA00008 1 20070102 A 5330 AFA83461 SKIN DOUG MD11 MD11F 3023600 NM ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 CENTER CARGO DOOR CUTOUT, AFT DOOR JAMB FUSELAGE SKIN FOUND WITH SCRATCHES AT LONGERON 40R. REPAIRED AS PER SRM 53-50-0 0 VOLUME 1 FIGURE 16. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007011000068 20070110 00068 EU 2007 1 10 AALA20070007 1 20070101 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14061 471 MIA - EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007011000070 20070110 00070 NM 2007 1 10 AALA20070024 1 20070105 A 3350 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 SFO - EMERGENCY LIGHT AT SEAT 22B INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 22B. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007011000071 20070110 00071 EU 2007 1 10 AALA20070020 1 20070105 A 3350 0L3229BPE BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 40064 507 JFK - EMERGENCY EXIT LIGHT AT RIGHT AND LEFT NUMBER TWO DOOR INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT RIGHT AND LE FT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007011000076 20070110 00076 NM 2007 1 10 HALA0700008 1 20070106 A 4910 49200101350 APU BOEING 717 717200 1383700 NM APU BAY EXPLODED A HALA O OTHER Z B SIGNIFICANT FAILURE REPORT SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 13 480HA 55125 ON PARKING AT KOA PILOTS SMELLED FAINT SMOKE THEN NOTICED VISIBLE SMOKE COMING OUT OF A/C VENTS. SECURED BOTH PACKS, EX PEDITED DEPLANING OF PAX THEN APU BLEW UP. NO FIRE INDICATION ON PANEL, DISCHARGED BOTH BOTTLES. REMOVED AND REPLACED NR 2 FIRE BOTTLE PER AMM 26-21-01 FUNC/ADJ PER AMM26-21-01-720-801OK REM NR 1 FIRE BOTTLE ASSY PER MM REINSTL ORIG NR 1 BOTTLE DISCHARGE. FERRIED A/C TO HNL. INSTALLED NR 1 FIRE BOTTLE AND SQUIBS. 2 L 7 2 4F TR A6WE 2007011000078 20070110 00078 NM 2007 1 10 HALA0700010 1 20070107 A 2420 76888B IDG BOEING 767 767300 1385204 NM NR 1 MALFUNCTIONED A HALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 13 592HA 10795 10795 33468 ETOPS SIGNIFICANT SYSTEM, LEFT GENERATOR CONTROL OFF LIGHT OVERHEAD PANEL AND EICAS MESSAGE CAME ON WHILE TAXING INTO GA TE. REMOVED AND REPLACED NR 1 IDG PER MM 24-11-01 AND INSTALLED PER AMM 24 11, ALSO CW HAL W/C 767-3-405001 BPCU FAULTS CONT TO SCROLL FROM OVERVOLTAGE TRIP AND GEN WIRING CKD ALL WIRING GOOD PER FIM 24 20 TABLE 102. RERACKED BPCU AND GCU PER 24-41-03 AND 24-22-42. IDG CHECKED GOOD ON ENG RUN PER MM 24-11-01 AND HAL 767-3-405001 VERIFIED ALL COMPONENTS SE CURED ENG CLOSED AND SECURED. 2 L 7 2 4F RT A1NM 2007011000104 20070110 00104 NM 2007 1 10 SWAA070048 1 20070104 A 3350 20121 CHARGER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED SERVICE CHECK, FOUND MID CABIN EMERGENCY EXIT BATTERY CHARGER INOP. REMOVED AND REPLACED BATTERY CHARG ER PER MM. 2 L 7 2 4F RT A16WE 2007011000112 20070110 00112 NM 2007 1 10 USAASB07004 1 20070108 A 4960 655280131 CONTROL UNIT BOEING 737 7373B7 1384580 NM E3-3 RACK FAULTY A USAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 530AU 54304 54304 24412 IND FLT1831 EN ROUTE FROM ORD TO CLT, THE NR 2 ENGINE CSD LOW OIL PRESSURE LIGHT ILLUMINATED. CREW DISCONNECTED THE NR 2 ENGINE CSD. CREW THEN STARTED THE APU BUT THE APU OVERSPEED LIGHT ILLUMINATED AND THE APU AUTOSHUTDOWN. FLIGHT DIVE RTED TO IND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED APU CONTROL UNIT (M280 MODULE). OPER ATIONAL CHECK GOOD. ALSO, REMOVED AND REPLACED THE NR 2 ENGINE CSD PER MM 24-11-11. OPERATIONAL CHECK AND LEAK CHECK G OOD. 2 L 7 2 4F RT A16WE 2007011000125 20070110 00125 NM 2007 1 10 SWAA070052 1 20070104 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM BS 380 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007011000126 20070110 00126 NM 2007 1 10 SWAA070053 1 20070104 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007011000139 20070110 00139 NM 2007 1 10 SWAA070086 1 20070108 A 5210 6545971523 FRAME BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR LOWER FRAME CRACKED BELOW LOWER CAM. REMOVED AND REPLACED R1 DOOR PER MM. 2 L 7 2 4F RT A16WE 2007011000141 20070110 00141 NM 2007 1 10 SWAA070088 1 20070108 A 5230 6547952358 FRAME BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR AFT FRAME CRACKED AT NR 5 STOP FITTING. REMOVED AND REPLACED AFT CARGO DOOR PER SWA EA. 2 L 7 2 4F RT A16WE 2007011000142 20070110 00142 2007 1 10 SWAA070089 4 20070108 A 2565 6557463 GIRT BAR BOEING 737 7373H4 1384600 NM R1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED AFT GIRT BAR FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007011000144 20070110 00144 NM 2007 1 10 SWAA070091 1 20070108 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM BS 930 S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007011000176 20070110 00176 NM 2007 1 10 USAABB07003 1 20070109 A 3350 CHARGER BOEING 757 7572B7 1384964 NM EMERGENCY LIGHTS INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 937UW 27245 MAINTENANCE FOUND AFT GALLEY EMERGENCY LIGHT ABOVE R4 DOOR INOPERATIVE. REPLACED BATTERY CHARGER. NO FURTHER FAULTS. 2 L 7 2 4F RT A2NM 2007011000177 20070110 00177 NM 2007 1 10 2007UALA00036 1 20070104 A 2497 BUSS AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 FAILED A UALA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 WP 29 832UA 1321 RTFL DUE TO LOST GENERATOR BUSS 2 & FAC 2 ON CLIMBOUT. REPLACED GENERATOR CONTROL UNIT-2. RAN ENGINE AND CYCLED POWER, ALL CHECKS GOOD 2 L 7 2 4F 4 F RT A28NM E40NE 2007011000183 20070110 00183 NM 2007 1 10 2007UALA00043 1 20070105 A 3350 20131A BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 194UA 26892 EMERGENCY LIGHT INOP AT AFT CREW REST STAIR ILLUM AND DOOR 2R SLIDE ILLUM. REPLACED BATTERY, OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007011100006 20070111 00006 NM 2007 1 11 0700026312 1 20070106 A 2910 LINE BOEING 747 747451 1384940 NM HYD SYSTEM LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 672US 30267 DURING CRUISE, HYDRAULIC QUANTITY WENT TO ZERO. FOLLOWED COM PROCEDURE FOR LOSS OF HYDRAULIC SYSTEM. FLIGHT CONTINUED ON TO DTW. YELLOW EMERGENCY WAS DECLARED UPON ARRIVAL IN DTW. AIRCRAFT LANDING WAS UNEVENTFUL. MAINTENANCE REMOVED AN D REPLACED RETURN TUBE WITH A TEMPORARY FLEX LINE, SERVICED NR 1 HYDRAULIC SYSTEM, AND SYSTEM LEAK CHECKS GOOD. OPERATI ONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007011100007 20070111 00007 EU 2007 1 11 07FDEA00042 1 20070105 A 2133 OUTFLOW VALVE AIRBUS 310 A310203 3930313 EU CABIN PRESSURE MALFUNCTIONED A FDEA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 25 401FE 191 A/C WOULD NOT PRESSURIZE IN FLIGHT ECAM INDICATES MANUAL PRESS VALVE FULL OPEN. AGREES WITH VALVE POSITION INDICATOR ON PRESSURIZATION PANEL. DIVERTED TO CLT. TROUBLE SHOT DOWN TO MANUAL PRESS VALVE 93HM. VALVE 93HM SEEMS TO BE LOCKED IN THE OPEN POSITION. REMOVED AND INSTALLED DEPRESSURIZATION VALVE 93HM AND FUNCTIONAL TEST PER MM 21-31-15-4, 21-31-00 -5. MOCC REQUEST PERFORM AIRCRAFT PRESSURIZATION CHECK AFTER PERFORMED AIRCRAFT PRESSURIZATION CHECK OFF MFG 88005A0101 . 2 L 7 2 4F RT A35EU 2007011100008 20070111 00008 NM 2007 1 11 07FDEA00047 1 20070105 A 5330 SKIN BOEING 727 727233 138408A NM BS 1140 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 AIRCRAFT FUSELAGE HAS AIR LEAK AT LOWER EXT SKIN WITH CORROSION PRESENT BS 1140 RBL 2 WO NR 35039 SNRM NR N01014, ALSO W ORKED WITH SNRM NR N00249. REMOVED DAMAGE, FABRICATED DOUBLER, INSTALLED DOUBLER, WEB INTERCOSTAL, FILLER, STIFFENER, W EB SUPPORT, 2 EACH STIFFENERS REF SRM 53-30-3 DETAIL II PG 8 FIGURE 3 CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007011100018 20070111 00018 NM 2007 1 11 07FDEA00018 1 20070103 A 5711 ARB74132 SPAR CAP DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING REAR SPAR CAP UPPER SURFACE FOUND CORROSION AT XORS=1046. COMPLIED WITH FEDEX E.A. 1-5710-105597, REPAIR CL ASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007011100056 20070111 00056 NE 2007 1 11 HNAA0600217 2 20070102 A 7261 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 OVERSERVICED A HNAA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 07 936HA 145 STRONG BURNING ODOR IN FLIGHT DECK AND CABIN AFTER REDUCING POWER ON APPROACH. SELECTED BLEEDS OFF AND ODOR WENT AWAY. SELECTED BLEEDS BACK ON, ON GROUND NO BURNING ODOR NOTICED. INSPECTED AND FOUND NR 2 ENGINE OIL LEVEL ONE QUART OVER S ERVICED. SERVICED TO CORRECT LEVEL, RAN NR 1 AND NR 2 ENGINES AND APU FOR ONE HOUR, NO BURNING ODOR EVIDENT AT THIS TIM E, CHECKED HP BLEED VALVE FOR CONTAMINATION, NONE FOUND. 2 H 7 2 4T 4 T RT A13NM E20NE 2007011100063 20070111 00063 NM 2007 1 11 DL76G070003 1 20070101 A 2121 211002542 FAN BOEING 767 767332 1382001 NM FWD FROZEN A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1603 29695 CREW REPORTED BURNED ELECTRICAL ODOR IN FLT DECK. ALSO REPORTED AROUND ROW 2AB. UTIL BUSSES WERE SECURED AND ODOR DISS IPATED. ODOR RETURNED A FEW HRS LATER AND QUICKLY DISSIPATED ALSO GOT FWD EQ EXH FAN MSG. REPLACED FWD EXHAUST FAN WOU ND NOT RESET REPLACED FILE CARD AND RELAY K345 PER FIM EXH FAN NOW CKS OK MCOPLAC REMOVED. 2 L 7 2 4F RT A1NM 2007011100066 20070111 00066 NM 2007 1 11 DLM88070010 1 20070105 A 5330 5936434129 SKIN DOUG MD88 MD88 3023688 NM FS 260 L29-30L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 941DL 49814 DURING THE CURRENT HMV, ADDITIONAL DAMAGE WAS FOUND IN THE AREA OF REPAIR DOUBLER INSTALLED PER ERA 383116-14. THE EXIS TING REPAIR WAS REMOVED, AND A BOEING APPROVED REPAIR, WHICH INCREASED THE SIZE OF THE EXISTING REPAIR, INSTALLED. LOCA TED AT FS 237 TO 256, L-29L TO L-30. 2 L 7 2 4F RT A6WE 2007011100099 20070111 00099 NM 2007 1 11 SWAA070105 1 20070109 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM BS 754 S19L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 754, STR 19L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007011100101 20070111 00101 NM 2007 1 11 SWAA070107 1 20070109 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM BS 739D S22R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739D, STR 22R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007011100102 20070111 00102 NM 2007 1 11 SWAA070108 1 20070109 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM BS 733E S25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733E, STR 25R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007011100110 20070111 00110 2007 1 11 SWAA070102 4 20070109 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 487WN 33854 R1 DOOR EMERGENCY EVAC OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007011100115 20070111 00115 NM 2007 1 11 SWAA070118 1 20070109 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 773SA 27881 DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007011100128 20070111 00128 NM 2007 1 11 DL76L070017 1 20070108 A 2997 291100440 CIRCUIT CARD BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE OVERSPEED UNKNOWN A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 198DN 28455 704865 AIR DRIVEN HYD PUMP INOP. C SYS DEMAND PUMP EICAS MSG. RTB FOR MTC. MTC IN PROGRESS. O/SPEED CONTROL CARD M1057 P/N 2117844-5 REPLACED IAW AMM 29-11-69-024 AND 29-11-69-424-005. ALL INDICATIONS NORMAL FL SLATS CYCLED USING APU POW ER AND ELECT HYD PUMPS AND ADP A INDICATIONS SATIS. 2 L 7 2 4F 4 F RT A1NM E13NE 2007011100129 20070111 00129 2007 1 11 DL76L070018 4 20070108 A 3416 341080108 ALTIMETER BOEING 767 767332 1382001 NM COCKPIT FAILED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 181DN 25986 CAPT ALTIMETER FAILED AT 35780 FT. REMOVED AND REPLACED CAPT ALTIMETER PER AMM. TESTS OK. NO FLAGS. 2 L 7 2 4F RT A1NM 2007011100131 20070111 00131 SO 2007 1 11 LR7A07001 1 20070107 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FS 770 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 75 4676 DURING SCHEDULED A CHECK IN WSSS PER JOB CARD HA1200, FOUND BULKHEAD CRACKED AT FS 770, WL160, RBL68. REPAIRED BULKHEAD IAW SMP583 53-50-14. LOG PAGE 23307, ITEM M1. 2 H 7 4 4T A1SO 2007011600008 20070116 00008 NM 2007 1 16 SWAA070126 1 20070110 A 5753 6550756 RIB BOEING 737 7373H4 1384600 NM RT FORE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND RIGHT WING INBOARD FORE FLAP INBOARD RIB CORRODED. REMOVED AND REPLACED FORE FLAP RIB PER SRM. 2 L 7 2 4F RT A16WE 2007011600036 20070116 00036 NE 2007 1 16 2007UALA00038 2 20070103 A 7200 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE UNKNOWN A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 455UA 1105 V10545 STALL DISPLAYED ON UPPER ECAM SCREEN DURING STEADY STATE CLIMB OR CRUISE. ENGINE NOT SHUTDOWN, ENG 2. [5-1-07] HPC WAS BORO'D AND PASSED. ONE 7TH STAGE BLEED VALVE FOUND BAD. IT WAS REPLACED AND PWR RUN WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007011600046 20070116 00046 CE 2007 1 16 A8J2007F00000 1 20070102 A 3246 95439914 WHEEL LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP MLG DAMAGED E A8JA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 135FA 067 ON 1/2/2007, AC DEPARTED, DURING THE TAKEOFF ROLL. GROUND PERSONNEL REPORTED SMOKE FROM THE LT SIDE OF THE AC AROUND TH E GEAR AREA. THE CREW WAS NOTIFIED. AC LOWERED ITS GEAR AND PERFORMED A FLIGHT BY THE TOWER. THE TOWER CONFIRMED THAT THE LT SIDE TIRES WERE GONE. THE AIRCRAFT DIVERTED, AC PERFORMED A FLY BY THE TOWER AND CONFIRMED THAT WHEEL AND BRAKE S WERE STILL ATTACHED BUT TIRES ON THE NR 1 AND NR 2 POSITION WERE GONE. THEY LANDED AND DEPLOYED THE DRAG CHUTE AND TH EN DEPLOYED THRUST REVERSER. THERE WERE A MINIMUM AMOUNT OF SPARKS AND THE AC CAME TO A HALT WITHIN THE RUNWAY AND WITH OUT ANY INJURIES. UPON VISUAL INSPECTION PART OF THE INNER SECTION OF THE TIRE WAS STILL ATTACHED TO THE RIMS AND THE I 2 L 7 2 4F 4 F A10CE E6WE 2007011600055 20070116 00055 NM 2007 1 16 SWAA070128 1 20070110 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM BS 727D CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, S8R. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007011600058 20070116 00058 NM 2007 1 16 SWAA070129 1 20070110 A 5330 6545767 SKIN BOEING 737 7373Q8 1384670 NM BS 475 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 475, STR 10R. REPAIRED SKIN PER ACO. 2 L 7 2 4F RT A16WE 2007011700006 20070117 00006 EA 2007 1 17 SWIA200717665 1 20070112 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 449SW 7699 FORWARD LEFT FUSELAGE EMERGENCY LIGHT BURNED OUT. RELAMPED LEFT FUSELAGE FORWARD EMERGENCY LIGHT. OPERATIONAL CHECKS G OOD. 2 L 7 2 4F RT A21EA 2007011700011 20070117 00011 EA 2007 1 17 SWIA200717645 1 20070104 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 910EV 7727 RIGHT WINDSHIELD CRACKED. REPLACED RIGHT WINDSHIELD IAW CRJ MM 56-11-01 AND RII 56-220-1000. OPS CHECKS GOOD. P/N OFF : NP139321-003 S/N OFF: 02248H5152. 2 L 7 2 4F RT A21EA 2007011700017 20070117 00017 EA 2007 1 17 SWIA200717651 1 20070107 A 2700 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A SWIA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 NM 07 916SW 7634 ON FINAL APPROACH INTO BURBANK, SPOILERONS CAUTION MESSAGE APPEARED. DIVERTED TO LAX. RESET CBS 1N8, 2N8, 4A2, 4A3. O PERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007011700019 20070117 00019 NM 2007 1 17 QXEA200700017 1 20070106 A 3297 471509 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM NLG DAMAGED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 410QX 1692 4053 BOI FLIGHT NR 2411: DU BAD CONFIG MESSAGE ON ED. CYCLED DISPLAYS PER PROCEDURE IN EA CHECKLIST SEVERAL TIMES. DU BAD C ONFIG MESSAGE REMAINED DISPLAYED. MAINTENANCE REMOVED NLG WOW1 HARNESS PER Q400 AMM TASK 32-21-11-000-801. INSTALLED S ERVICEABLE NLG WOW1 HARNESS PER Q400 AMM TASK 32-21-11-400-801. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007011700022 20070117 00022 NM 2007 1 17 07FDEA00076 1 20070111 A 5320 ANGLE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING ROOT, CENTER TANK LOWER TEE ANGLE FOUND CRACKED AT STA 1298. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-105590. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007011700023 20070117 00023 NM 2007 1 17 07FDEA00077 1 20070111 A 5753 SUPPORT FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING O/B FLAP ARC4012 OUTBOARD SUPPORT FITTING FOUND CRACK. LEFT HAND OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRIED OUT FOUND SATIS AS PER AMM 27-50-00-5. 2 L 7 3 4F RT A22WE 2007011700024 20070117 00024 WP 2007 1 17 07FDEA00078 1 20070111 A 5313 LONGERON SPLICE DOUG MD10 MD1010F 3022112 WP BS 1139 S17R CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 381FE 46615 RT FUSELAGE AT STA 1139 LONGERON SPLICE 17R CRACKED. REMOVED CRACKED LONGERON SPLICE. FABRICATED LONGERON SPLICE PER DAC DRAWING ADA0179. LOCATED NEW STRINGER SPLICE AT STA 1139 I-17R. OK TO INSTALL. PENETRANT INSPECTION REQUIRERD PER DAC DRAWING ADA 0179. OK TO INSTALL. INSTALLED SPLICE PER SRM53-10-00 ADA 0179. 2 L 7 3 4F RT A22WE 2007011700025 20070117 00025 WP 2007 1 17 07FDEA00079 1 20070111 A 5313 LONGERON SPLICE DOUG MD10 MD1010F 3022112 WP BS 1139 S16R CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 381FE 46615 RT FUSELAGE AT BS 1139 LONGERON SPLICE 16R CRACKED. REMOVED CRACKED LONGERON SPLICE. FABRICATED LONGERON SPLICE PER DAC DRAWING ADA0179. LOCATED NEW STRINGER SPLICE AT BS 1139 L16R. INSTALLED SPLICE PER SRM 53-10-00 AND DAC DRAWINF ADA017 9 2 L 7 3 4F RT A22WE 2007011700030 20070117 00030 NM 2007 1 17 QXEA200700020 1 20070109 A 3080 4100S01906 PROBE BOMBDR DHC8 DHC8402 1390042 NM ICE DETECTOR MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 417QX 7526 4086 SEA FLIGHT NR 2378: ICE DETECT FAIL CAUTION ILLUMINATED (FAILED TO EXTINGUISH AFTER PROPS OUT OF FEATHER). AIRCRAFT RET URNED TO GATE. MAINTENANCE REMOVED AND REPLACED LT ICE DETECTOR PROBE IAW Q400 AMM TASKS 30-80-01-000-801 AND 30-80-01- 400-801. LT ICE DETECTOR PROBE, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007011700031 20070117 00031 NM 2007 1 17 07FDEA00073 1 20070110 A 5753 ARC4009 FITTING DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LT WING OUTBOARD TRAILING EDGE FLAP FITTING ARC4009 FASTENER HOLES CORROSION BEYOND LIMIT. LT WING OUTBOARD FLAP REMOVE D AND REPLACED AS PER AMM 27-50-30. P/N ON: NRC6753-503, S/N ON: 098 REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007011700032 20070117 00032 NM 2007 1 17 DLM88070024 1 20070111 A 5230 STRUCTURE DOUG MD88 MD88 3023688 NM FWD CARGO DOOR WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 918DE DL5 49959 MAJOR REPAIR TO MD88 CARGO DOOR AFT EDGE IAW SRM 52-05D, FIG 50 REF NRC 18168 AND SON W33364. DOOR REMOVED FROM 9018, STOCKED AS SPARE, REPLACED DOOR ASSY. 2 L 7 2 4F RT A6WE 2007011700033 20070117 00033 NM 2007 1 17 DLM88070025 1 20070111 A 4990 1945189004 OIL CAP DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE APU LEAKING A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 917DL 16595 49573 P80168 DURING T/O, STRONG ODOR AND HAZE IN AFT CABIN. FOUND APU OIL CAP LEAKING AND APU INGESTED OIL. FOUND OIL LEAKING PAST OIL FILLER CAP SEAL. REPLACED CAP AND SEAL SERVICED TO FULL. CLEANED AREA LEAK CKS GOOD. REMOVED AND REPLACED COALES CER BAGS AND PERFORMED FULL DUCT BURN OUT PER OPN 5089. 2 L 7 2 4F 4 F RT A6WE E9NE 2007011700036 20070117 00036 NM 2007 1 17 DL777070029 1 20070113 A 3020 388040002 VALVE BOEING 777 777232 1385232 NM ANTI ICE SYSTEM FAILED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 863DA 29735 ANTI-ICE ENG L EICAS MSG ON ENG SHUTDOWN. MTC MSG 30-10101 VLV FAILED IN CLOSED POSITION. NO ICE NOT AVIAL TRIED TO ME L PER 30-21-01B. MTC UNABLE TO C/W MEL ENG RUN. DEFERRED TO CREW PROCEDURE WHICH FAILED AFTER PUSH BACK. MTC REPLACED L ENG ANTI ICE VALVE AND REMOVED MCO. 2 L 7 2 4F RT T00001SE 2007011700038 20070117 00038 NM 2007 1 17 DL757070031 1 20070113 A 3260 841602 PSEU BOEING 757 757232 1384965 NM E/E BAY FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 6701 30187 GEAR DOORS LIGHT ON AFTER GEAR RETRACTION RETURNED FOR MTC. PERFORMED PSEU BIT. NO FAULTS FOUND, CYCLED GEAR DOORS SEV ERAL TIMES ALL IND CKD GOOD. DURING VERIFY ON PSEU FOUND CARD 6. FAULTED TRIED NEW CARD 6, NO HELP. REPLACED PSEU PER MM, OPS CK GOOD. 2 L 7 2 4F RT A2NM 2007011700039 20070117 00039 NE 2007 1 17 DL777070032 2 20070114 A 7320 738040007 EEC BOEING 777 777232 1385232 NM RROYCE RB211 RB21122* 54555 NE NR 1 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 867DA 29743 051149 AFTER T/O LT ENG RELATED MESSAGES, HIGH OIL PRESS EPR/N1/EGT/N3 EXCEEDANCES. AUTOTHROTTLES KICKED OFF. ENGINE RESPONDE D NORMALLY. ENG CTLL/EEC C1L/ REPLACED L ENG EEC. UPDATED SOFTWARE. RAN ENG NO FAULTS NO MESSAGES. 2 L 7 2 4F 4 F RT T00001SE A12EU 2007011700046 20070117 00046 SO 2007 1 17 SIMA200701103 1 20070110 A 2750 3631001005 CONTROL UNIT EMB 135 EMB135KL 3260302 SO SPOILERS FAILED A SIMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SW 21 802AE 15256 3249 145471 FLAP FAIL MESSAGE, EMERGENCY DECLARED. REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT, NUMBER 1 AND 2 FLAP TRANSMISS ION BRAKES. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007011700047 20070117 00047 SO 2007 1 17 SIMA200701104 1 20070109 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 653AE 13302 4800 145433 SERVICE DOOR FRAME CENTER SILL CORRODED. CLEANED AND TREATED AREA, REMOVED AND REPLACED CENTER SILL IAW EMB SRM 51-20-0 3, 51-40-02 AND 51-40-06. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007011000093 20070110 00093 EA 2007 1 10 TRAX200700027 1 20070105 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY HATCH MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 841AS 7300 EMERGENCY CREW HATCH MISSING ALL OUTER PLACARDS. 2 L 7 2 4F RT A21EA 2007011000095 20070110 00095 EA 2007 1 10 TRAX200700030 1 20070105 A 5322 SHEAR TIE CNDAIR CL600 CL6002B19 1900309 EA BS 169 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 ETNRC 2000-15 LOWER LLEFT SKIN ANGLE AT FS 169.00 LBL 12.00 IS CRACKED. LOWER LT SKIN ANGLE AT FS 169.00 LBL12.00 REMOV ED AND REPLACED IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007011000097 20070110 00097 NM 2007 1 10 HNAA0600212 1 20070104 A 5312 85310055 PRESSURE PANEL DHAV DHC8 DHC8102 2809003 NM NLG WW CRACKED A HNAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 07 808EX 37336 37336 299 ON EXTENSION GEAR UNSAFE LIGHT ILLUMINATED ACCOMPANIED BY NOISE. CYCLED GEAR A SECOND TIME AND ALL INDICATIONS NORMAL. FOUND NOSE GEAR UPPER DECK (WEB) FAILED. 2 H 7 2 4T RT A13NM 2007011000098 20070110 00098 EU 2007 1 10 USAASA07002 1 20070107 A 2910 238D0660507 LINE AIRBUS A319 A319112 3930323 EU HYDRAULIC SYS LEAKING A USAA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 EA 19 752US 1319 CLT FLT 1667, EN ROUTE DCA - CLT. DURING DESCENT THROUGH FL 200, THE AIRCRAFT LOST THE GREEN SYSTEM HYDRAULIC PRESSURE. THE CREW FOLLOWED ECAM PROCEDURES AND COMPLIED WITH THE GRAVITY EXTENSION OF THE LANDING GEAR. THE FLIGHT LANDED WITH OUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE HYDRAULIC PUMP CASE DRAIN LINE DUE TO A HOLE. SERVICED THE GREEN HYDRAULIC SYSTEM, AND RESET THE GRAVITY GEAR EXTENSION HANDLE, SYSTEM OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2007011000100 20070110 00100 2007 1 10 SWAA070044 4 20070104 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 734SA 27866 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007011000107 20070110 00107 SO 2007 1 10 RAIA00701001 1 20070102 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BURNED OUT A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 841HK 145382 PRE FLIGHT NR 8006 - RIC - EMERGENCY LIGHT OVER SEAT 12BC INOP. MAINTENANCE REMOVED AND REPLACED THE BULB. 2 L 7 2 4T RT T00011AT 2007011000124 20070110 00124 NM 2007 1 10 SWAA070051 1 20070104 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007011000131 20070110 00131 NM 2007 1 10 SWAA070062 1 20070105 A 3350 8200048501 BALLAST BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 739GB 29275 DURING SCHEDULED HC2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM. 2 L 7 2 4F RT A16WE 2007011000134 20070110 00134 NM 2007 1 10 SWAA070081 1 20070108 A 2121 6454051 FAN BOEING 737 7373H4 1384600 NM E/E BAY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 29 355SW 25250 FLIGHT ATTENDANT REPORTED BURNT RUBBER ODOR, TURNED OFF RECIRC FAN, ODOR DISSIPATED. REMOVED AND REPLACED RECIRC FAN PE R MM. 2 L 7 2 4F RT A16WE 2007011000137 20070110 00137 NM 2007 1 10 SWAA070084 1 20070108 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 514D S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514D, STR 15L. REPAIRED SKIN SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007011000140 20070110 00140 NM 2007 1 10 SWAA070087 1 20070108 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED C2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 1 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007011000146 20070110 00146 EU 2007 1 10 TRAX200700023 1 20070103 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 EMERGENCY LIGHTS CAME ON WHEN IN THE ARMED POSITION WITH GENERATOR RUNNING, WILL NOT RESET. 2 H 7 2 4T RT 2007011000150 20070110 00150 NM 2007 1 10 SWAA070063 1 20070105 A 5753 113A370020 SKIN BOEING 737 7377H4 1384404 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 739GB 29275 DURING SCHEDULED HC2 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER CORNER. REMOVED AND REP LACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2007011000151 20070110 00151 NM 2007 1 10 SWAA070064 1 20070106 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727C S3R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007011000154 20070110 00154 NM 2007 1 10 SWAA070067 1 20070106 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 616 S5L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007011000160 20070110 00160 NM 2007 1 10 SWAA070073 1 20070106 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM BS 847 S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 847, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007011000164 20070110 00164 2007 1 10 SWAA070060 4 20070105 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007011000178 20070110 00178 NM 2007 1 10 2007UALA00037 1 20070105 A 5230 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CARGO DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 226UA 30226 AFT BULK CARGO DOOR HAS A V-SHAPED DENT OR GOUGE IN SKIN. REMOVED DAMAGED AREA AND FASTENERS. MANUFACTURED DOUBLER & I NSTALLED. INTERIM REPAIR MADE WITH BLIND FASTENERS. CATEGORY C INSPECTION REQUIREMENTS APPL Y. INSPECTION INTERVAL EVERY 1000 CYCLES WITH A MAX. ACCOMPLISHED PERMANENT MAJOR REPAIR AT PEK HMV. REPLACED ALL BLIND FASTNERS. OK FOR RETURN T O SERVICE. SUSPECT DAMAGED CAUSED BY CONTACT WITH GROUND SERVICE EQUIPMENT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007011000184 20070110 00184 SO 2007 1 10 PNSA070101 1 20070103 A 2434 ALY6421 ALTERNATOR PIPER PA32 PA32301 7103207 SO ENGINE FAILED E PNSA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 AL 03 8327S 635 328106039 EN ROUTE TO AKN FROM PDB AIRCRAFT HAD AN ALTERNATOR FAILURE AND LOSS RADIOS. PILOT TRIED TO GET LIGHT SIGNAL FROM AKN T OWER WITH NO SUCCESS AND DIVERTED TO 5NK AND CONTACTED AKN MAINTENACE. MAINTENANCE CHANGED OUT THE FAILED ALTERNATOR AN D BATTERY. FLIGHT CONTINUED TO AKN. 1 L 7 1 3O A3SO 2007011100010 20070111 00010 NM 2007 1 11 07FDEA00049 1 20070106 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 STRINGER CLIP HAS HAD RADIUS CUT OUT GROUND AT BS 440 STRINGER 5L REPLACED STRINGER CLIP REF SRM 51-30-2 PG 5/6. 2 L 7 3 4F RT A3WE 2007011100012 20070111 00012 NM 2007 1 11 07FDEA00052 1 20070108 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 DURING HFEC INSPECTION ON THE LEFT WING TANK, CRACK WAS FOUND AT THE END OF STRINGER 13 (XORS 577) WITH APPROX 8" IN L ENGTH. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007011100033 20070111 00033 NM 2007 1 11 07FDEA00019 1 20070103 A 5711 ARB74132 SPAR CAP DOUG MD11 MD11F 3023600 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RT WING REAR SPAR UPPER CAP LOWER SURFACE FOUND CORROSION AT X0RS= 1047 TO X0RS= 1053. COMPLIED WITH FEDEX E.A.# 1-5710 -105597, REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007011100038 20070111 00038 NM 2007 1 11 ASAA0741378 1 20070109 A 5512 657378345 SKIN BOEING 737 7374Q8 138447Q NM HORIZONTAL STAB DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 THE LEFT HORIZONTAL STAB L/E SKIN IS DENTED OUT OF LIMITS AT L/E STA 92. CUT OUT THE DAMAGED AREA OF SKIN, FABRICATED A ND INSTALLED A SKIN FILLER AND INTERNAL REPAIR DOUBLER IAW SRM 55-10-01 FIG 201. 2 L 7 2 4F RT A16WE 2007011100046 20070111 00046 NM 2007 1 11 ASAA0741362 1 20070108 A 5320 65479599 INTERCOSTAL BOEING 737 7374Q8 138447Q NM BS 787-794 S25R CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 775AS 25108 AFT CARGO COMPARTMENT INTERCOSTAL CORRODED. INTERCOSTAL REPAIRED IAW SRM 51-40-05 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007011100077 20070111 00077 WP 2007 1 11 AALA20070034 1 20070107 A 2420 97652528 GENERATOR DOUG DC9 DC983 3022083 WP LEFT ENGINE INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 9617R 53564 PHX INFLIGHT T1782/07JAN SAN - DFW AT FLIGHT LEVEL 310, LEFT GENERATOR TRIPPED ON AND OFF SEVERAL TIMES. CONSTANT SPEE D DRIVE OIL TEMPERATURE OVER RED LINE. UNABLE TO START APU. TURNED LEFT GENERATOR SWITCH OFF. CONSTANT SPEED DRIVE OI L TEMPERATURE COOLED BELOW RED LINE. LANDED PHX WITHOUT INCIDENT. REPLACED LEFT CONSTANT SPEED DRIVE AND GENERATOR. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007011100081 20070111 00081 EU 2007 1 11 AALA20070039 1 20070109 A 3211 DAMPER AIRBUS 300 A300B4605R 3930308 EU LANDING GEAR INOPERATIVE A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 90070 513 JFK INFLIGHT T1375/09JAN BDL TO SJU - LANDING GEAR WOULD NOT RETRACTION SYSTEM ONE AND TWO. CREW CONFIRMED GEAR WAS DOW N AND LOCKED. LANDED JFK WITHOUT INCIDENT. REPLACED LEFT MAIN LANDING GEAR PITCH DAMPER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007011100083 20070111 00083 NM 2007 1 11 AALA20070043 1 20070107 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 910AN 29512 MIA - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT NUNBER FOUR DOOR. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007011100091 20070111 00091 NM 2007 1 11 AALA20070027 1 20070106 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 638AA 24596 MIA - LEFT EMERGENCY LIGHT AFT OF OVERWING INOPERATIVE. RELAMPED LEFT EMERGENCY LIGHT AFT OF OVERWING. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007011100098 20070111 00098 NM 2007 1 11 SWAA070104 1 20070109 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 807 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807 LBL 10. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007011100100 20070111 00100 NM 2007 1 11 SWAA070106 1 20070109 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM BS 731 S23R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 731, STR 23R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007011100104 20070111 00104 NM 2007 1 11 SWAA070110 1 20070109 A 5330 6545765 SKIN BOEING 737 7375H4 138449D NM BS 927 S23R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 23R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007011100112 20070111 00112 2007 1 11 SWAA070115 4 20070109 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 428WN 29844 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007011100113 20070111 00113 NM 2007 1 11 SWAA070116 1 20070109 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 773SA 27881 DURING SCHEDULED HC1 CHECK, FWD CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007011100117 20070111 00117 NM 2007 1 11 USAA070017 1 20070108 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 847 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 AFT CARGO FLOOR TRACK/BEAM AT STATION 847 + 12 LBL 8 HAS CORROSION. REPAIRED IAW TR 53-10-06B, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007011100121 20070111 00121 NM 2007 1 11 USAA070021 1 20070109 A 5311 FRAME BOEING 737 737401 1384701 NM CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 FWD CARGO AFT FRAME AT STRINGER 24R CRACKED. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW EA 98384, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007011100122 20070111 00122 2007 1 11 USAA070020 4 20070109 A 2565 MOUNT BOEING 737 737401 1384701 NM GIRT BAR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 STATION 312 & 344 LBL 58 HAS CORROSION. REPLACED MOUNTS IAW SRM 51-20-02, DEFECT SIZE: 1 X 1 INCH. 2 L 7 2 4F RT A16WE 2007011600009 20070116 00009 NM 2007 1 16 SWAA070127 1 20070110 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007011600059 20070116 00059 NM 2007 1 16 SWAA070130 1 20070110 A 5315 6545815 FLOORBEAM BOEING 737 7373T5 1384608 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, RBL 5, WL 208. REMOVED AND REPLACED FLOORBEAM SECTION P ER SRM. 2 L 7 2 4F RT A16WE 2007011700007 20070117 00007 SO 2007 1 17 SWIA200717666 1 20070113 A 5415 BEAM EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 215SW 120281 RIGHT NACELLE INBOARD BEAM AT HYDRAULIC BAY IS CRACKED, DISCOVERED DURING A-CHECK INSPECTION. REPLACED RIGHT NACELLE IN BOARD BEAM AT HYD BAY PER SRM 51-40-02 AND SEE RII 54-900-1000. 2 L 7 2 4T RT A31SO 2007011700027 20070117 00027 NM 2007 1 17 TSAA0626006 1 20070109 A 2612 894093 FIRE LOOP BOEING 737 737210C 1384459 NM NR 1 NACELLE FAILED A TSAA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 WP 13 834AL 20917 DURING CRUISE FLIGHT, CREW NOTED THE NR 1 ENGINE OVERHEAT INDICATION ILLUMINATED. CREW SHUT DOWN THE NR 1 ENGINE AND PU LLED THE FIRE HANDLE UP. THE OVERHEAT INDICATION THEN EXTINGUISHED. CREW LANDED IN HNL WITHOUT FURTHER INCIDENT. MAI NTENANCE FOUND THE NR 1 ENGINE LOWER FIRE LOOP PINCHED BY THE GENERATOR AIR DUCT AND REPLACED THE LOOP PER AMM 26-11-11. THE SYSTEM OPERATION CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A16WE 2007011700034 20070117 00034 NM 2007 1 17 DL757070026 1 20070109 A 5210 INTERCOSTAL BOEING 757 757232 1384965 NM R-2 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 608DA 22815 INTERCOSTAL FOUND CRACKED DURING AD INSPECTION, LOCATED ON R2 PASSENGER DOOR. REPAIRED PER DELTA ERA 459424-14 REV A. 2 L 7 2 4F RT A2NM 2007011700037 20070117 00037 NM 2007 1 17 DL757070030 1 20070110 A 5312 BULKHEAD BOEING 757 757232 1384965 NM BS 1720 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 604DL 22811 DURING WALK AROUND, THE FLIGHT CREW FOUND DAMAGE TO THE TAIL AREA STA 1720 BY THE P-DOME FERRY A/C TO ATL. REPAIRED P-D OME LOWER WEB. 2 L 7 2 4F RT A2NM 2007011700048 20070117 00048 SO 2007 1 17 SIMA200701101 1 20070110 A 2750 363100 CONTROL UNIT EMB 135 EMB135LR 3260305 SO TE FLAPS FAILED A SIMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 21 733KR 10862 1131 145368 SPS ADVANCED, FLAP FAIL MESSAGE, FLAPS DID NOT EXTEND TO 9 DEGREES, EMERGENCY DECLARED. REMOVED AND REPLACED FLAP CONTR OL UNIT IAW EMB AMM 27-51-12. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. OPEN 2 L 7 2 4F RT T00011AT 2007011700049 20070117 00049 NE 2007 1 17 AWXA200700060 2 20070111 A 7320 ENGINE BOEING 757 7572G7 1384963 NM RROYCE RB211 RB211535E4 54555 NE NR 1 SHUTDOWN A AWXA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 WP 28 908AW 24233 908 - IFSD - KOA - PHX - DURING CLIMB, THE CREW NOTICED THE NR 1 ENGINE HAD SHUTDOWN IN-FLIGHT. THE CREW DECLARED AN EM ERGENCY AND RETURNED TO KOA. MX FOUND PINS 2 AND 5 SHORTED IN CON. D2142, FOUND DAMAGED WIRING IN SHIELD TERMINATION FO R WIRE W3306/R/Y/B-20 NEAR D2142. MX REMOVED OLD CABLE, ROUTED NEW CABLE, TERMINATED PER ESWP 20-10-15, REF. 76-11-11 FO R CONNECTOR D40902P. TERMINATED NEW WIRE INTO D2142, REF WDM 28-22-21 AND ESPM 20-10-15. PERFORMED OPS CHECK OF SPAR VAL VE. OPS CHECK WAS GOOD PER MM 28-22-00-5. RAN NR 1 ENGINE FOR 25 MIN, NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A2NM E12EU 2007011700051 20070117 00051 NM 2007 1 17 UIEA200700003 1 20070110 A 5740 65B156949 ATTACH FITTING BOEING 747 74747UF 1384812 NM FLAP TRACK DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 492 29253 UPON ARRIVAL, FOUND NR 2 CANOE DAMAGED, PUNCTURED HOLE OUTBOARD SIDE, IN ADDITION FOUND FLAP TRACK ATTACH FITTING DAMAGE D. TRANSFERRED TO DMI NR M07-003 CDL 27-51-02. 2 L 7 4 4F RT A20WE 2007011700052 20070117 00052 NM 2007 1 17 UIEA200700004 1 20070110 A 5310 65B01838135 DOOR FRAME BOEING 747 7472D7B 1384803 NM L1 DOORWAY CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 96210 96210 21783 AT XMN UNDER C-1 CHECK, DURING PERFORMING EO NR 4753A531 AS PER AD 2005-22-06.AS PER NR NR 215, CRACK FOUND DURING HFEC AT BS488 ME DOOR 1L CUT OUT FRAME WEB AT STOP 9. RECTIFICATION, BS 488 MED 1L DOOR FRAME WEB REPAIRED AS PER SRM 53-10- 04 FIG 121. 2 L 7 4 4F RT A20WE 2007011700058 20070117 00058 NE 2007 1 17 Q2SA509001 2 20070110 A 7200 9057M74G01 SENSE LINE BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE NR 4 ENGINE CLOGGED A Q2SA J A DUMP FUEL UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 NE 03 509MC 21221 530255 NR 4 ENGINE ROLL BACK TO 93.5 PERCENT N1 AT FLIGHT LEVEL 310. EGT AT 641 DEGREES, N2 AT 94.5 PERCENT AND FUEL FLOW AT 5 648. AFTER LANDING NO RESPONSE FROM THROTTLE LEVER. DUMPED 140,000 LBS FUEL. AIRCRAFT EN ROUTE ZSPD TO PANC, DIVERTED TO RKSI. NR 4 ENGINE WAS NOT SHUTDOWN. CLEANED CDP LINE IN ACCORDANCE WITH AMM 71-00-42. ACCOMPLISHED HIGH POWER RUN IN ACCORDANCE WITH 71-00-00, TEST NR 4. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F 4 F A20WE E23EA 2007011700059 20070117 00059 EU 2007 1 17 AALA20070048 1 20070110 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70079 619 MIA - EMERGENCY LIGHT AT SEAT 19G INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 19G. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007011700060 20070117 00060 EU 2007 1 17 AALA20070049 1 20070110 A 3397 WIRE HARNESS AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70079 619 MIA - EMERGENCY LIGHT AT SEAT 32G INOPERATIVE. REPLACED HARNESS FOR EMERGENCY LIGHT AT SEAT 32G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007011700062 20070117 00062 NM 2007 1 17 AALA20070057 1 20070108 A 3350 D71701100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 953AN 29539 TUL - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED OPERATIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007011700065 20070117 00065 NM 2007 1 17 AALA20070046 1 20070108 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 936AN 29632 MIA - EMERGENCY LIGHT AT AFT LEFT OVERWING INOPERATIVE. REPLACED BATTERY PACK M1670 FOR EMERGENCY LIGHT AT AFT LEFT OVE RWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007011700066 20070117 00066 NM 2007 1 17 AALA20070052 1 20070102 A 3350 D71701001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 919AN 29520 TUL - EMERGENCY LIGHT BATTERY PACK FOR SEAT ROWS 7 TO 11 AT STATION 500 FAILED OPERATIONAL TEST. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 7 TO 11. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007011700067 20070117 00067 WP 2007 1 17 AALA20070061 1 20070111 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 510AM 49804 DFW - EMERGENCY EXIT LIGHT AT LEFT FIRST CLASS GALLEY IS LOOSE. REPLACED LOWER EMERGENCY EXIT LIGHT ASSEMBLY AT LEFT FI RST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007011700071 20070117 00071 NM 2007 1 17 AALA20070056 1 20070108 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 920AN 29521 TUL- EMERGENCY LIGHT BATTERY PACK AT STATION 1016 RIGHT AFT OVERHEAD FAILED OPERATIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK AT STATION 1016 RIGHT AFT OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007011700072 20070117 00072 NE 2007 1 17 MALA070004 2 20070110 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT MALFUNCTIONED A MALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 15 449XJ 340B449 DURING FLIGHT AT CRUISE, LT ENGINE OIL PRESSURE WARNING LIGHT CWP ILLUMINATED WITH OIL PRESSURE VERIFIED LOW (ENG OIL GA UGE PSI BELOW 30 PSI (REDLINE) ON INDICATION. CREW FOLLOWED QRH AND SECURED ENGINE. EN ROUTE BETWEEN CWA AND MSP, EAST OF EAU, ENGINE NR 1, OIL PRESSURE WARNING ILLUMINATED AND WAS VERIFIED WITH THE ENGINE OIL PRESSURE GAUGE. THE CREW SH UT DOWN THE ENGINE AND DIVERTED TO EAU. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. UPON ARRIVAL, DURING POST FLIGHT WALK AROUND OBSERVED OIL ALONG RIGHT SIDE OF LEFT ENGINE COWLING AND UPPER OF WING EXHAUST APPEARED DRY UPON INSPECTION. REMOVED AND REPLACED LEFT ENGINE IAW JOB CARD 7100-301 P/N ENGINE CT7-9B S/N ON GE-E78569 2 L 7 2 4T 4 T RT A52EU E8NE 2007011700075 20070117 00075 NM 2007 1 17 DU4R2007006 1 20070101 A 5320 SPLICE BOEING 757 757232 1384965 NM BS 1470 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 FOUND CORRODED SPLICE IN AFT CARGO AT BS 1470. REPAIRED CORRODED SPLICE BY FABRICATING AND INSTALLING NEW SPLICE 1-3/4 BY 40 FROM BAC1505-100766 7075-T6 IAW B757 SRM 51-20-1, 51-40-02 AND DWG 453N1611. 2 L 7 2 4F RT A2NM 2007011700087 20070117 00087 NM 2007 1 17 AALA20070054 1 20070103 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 919AN 29520 TUL - EMERGENCY LIGHT BATTERY PACK AT AFT CABIN OVERHEAD FAILED OPERATIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK AT AFT CABIN OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007011700089 20070117 00089 NM 2007 1 17 AALA20070047 1 20070110 A 3397 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 788AN 30011 JFK - EMERGENCY SIDE MARKER LIGHT FORWARD OF LEFT NUMBER THREE DOOR INOPERATIVE. FOUND PIN 15 PUSHED BACK. RESEATED PI N 15 FOR EMERGENCY SIDE MARKER LIGHT FORWARD OF LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007011700090 20070117 00090 NM 2007 1 17 F3LA200600166 1 20070107 A 5321 D5367180500500 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 917FR 5893 1890 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON LOWER SURFACE OF FLOOR PANEL 262FF. REPLACED FLOOR PANEL PER WORK CA RD C534103-2. 2 L 7 2 4F RT A28NM 2007011700094 20070117 00094 NM 2007 1 17 NWAA700076623 1 20070109 A 2131 CONTROLLER BOEING 747 747251B 1384892 NM CABIN PRESSURE MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 01 623US 21705 DURING CRUISE, THERE WAS A RAPID DEPRESSURIZATION AT FL 390. EMERGENCY DESCENT COMMENCED UNTIL CONTROL OF CABIN ALTITUD E ATTAINED AT FL 300 WITH MANUAL CONTROL. CABIN ALTITUDE DID NOT EXCEED 12,000, AND PASSENGER O2 MASKS DID NOT DEPLOY. AT FL 300 IT WAS OBSERVED THAT THE GROUND SAFETY LIGHT WAS ILLUMINATED. COM PROCEDURE COMPLIED WITH. FLIGHT CONTINUED ON TO GUM, AND LANDING WAS UNEVENTFUL. MAINTENANCE ACCOMPLISHED CABIN DEPRESSURIZATION CONDITION INSPECTION AND GROUND SAFETY RELAY TEST. REMOVED AND REPLACED AUTO PRESSURE CONTROLLER, PRIMARY TILT CARD AND 3 RELAYS. OPERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F A20WE 2007011700104 20070117 00104 NM 2007 1 17 F3LA200700003 1 20070105 A 5315 D5347218920200 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 917FR 5893 1890 DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND FASTENER HOLE AT FR68, RT SIDE, APPROX ONE FOOT INBD OF DOOR SKIN . BLENDED CORROSION AROUND HOLE AND FOUND INTERGRANULAR CORROSION INSIDE FASTENER HOLE THAT WAS FOUND TO BE OUT OF LIMI TS IAW SRM 51-74-00. REPLACED FLOORBEAM IAW SRMS 51-42-11 AND 51-44-11. 2 L 7 2 4F RT A28NM 2007011700105 20070117 00105 NM 2007 1 17 QXEA200700026 1 20070111 A 3097 697070642 BUSS BAR BOMBDR DHC8 DHC8402 1390042 NM PROP DEICE BROKEN A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 404QX 4046 BOI FLIGHT NR 2419: PROP DEICE CAUTION LIGHT ILLUMINATED WHEN PROP NR 1 CYCLES ON. LOAD SHOWN NORMAL ON ELECTRICAL PAGE . FLIGHT DIVERTED TO BOI. MAINTENANCE REPLACED BROKEN BUSS BAR STRAP ON NR 1 PROP NR 4 BLADE WITH SERVICEABLE UNIT. C/W FUNCTIONAL TEST IAW AMM TASK 30-61-00-720-801. SYSTEM OPS NORMAL. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007011700106 20070117 00106 WP 2007 1 17 IXXA070003O 1 20070110 A 2910 LINE DOUG DC8 DC862F 3021972 WP HYDRAULIC SYS LEAKING A IXXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 11 41CX 81058 825 46129 DURING CLIMB FROM FHAW, THE CREW NOTICED THE HYDRAULIC QUANTITY BEGAN DECREASING. THE CREW RAN THE HYDRAULIC LOSS OF QU ANTITY CHECK LIST AND RETURNED TO FHAW AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NU MBER THREE ENGINE HYDRAULIC HIGH PRESSURE LINE LEAKING. MAINTENANCE REPLACED THE LINE, SERVICED THE HYDRAULIC RESERVOIR . THE OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE IAW DACO DC8 MM 29-10-12. 2 L 7 4 4F 4A25 2007011700108 20070117 00108 NM 2007 1 17 07FDEA00081 1 20070112 A 5330 SKIN BOEING 727 727233 138408A NM BS 680-700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 EXT FUSELAGE LOWER HALF BETWEEN STA 680-700 AND BETWEEN 28L - 30. SKIN SURFACE CRACKED AND HOLE NOTED DURING PRESSURIZA TION CHECK. REPAIRED AREA AT STA 680 STR 28L IAW SRM 53-30-3 FIG 3A. 2 L 7 3 4F RT A3WE 2007011700113 20070117 00113 NM 2007 1 17 F3LA200700002 1 20070109 A 5210 LEVER AIRBUS A319 A319111 3930336 NM R1 DOOR BINDING A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 917FR 5893 1890 DURING C-3 CHECK, INSPECTION REPORTED THE R-1 DOOR ARMED LEVER WOULD NOT MOVE TO ARMED POSITION. REMOVED EXCESS LUBRICA NT AND RETORQUED NUTS IAW AMM 52-11-22-820-001, STEP 4E(E). DOOR OPERATION NORMAL. 2 L 7 2 4F RT A28NM 2007011700114 20070117 00114 2007 1 17 F3LA200700004 4 20070105 A 2565 GIRT BAR AIRBUS A319 A319111 3930336 NM L2 DOOR SLIDE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 917FR 5893 1890 DURING C-3 CHECK, INSPECTION REPORTED CORROSION IN FWD GIRT BAR FITTING FASTENER HOLES ON L2 DOOR FRAME SILL. REMOVED C ORROSION IAW SRM 53-41-14, FIG 101. FABRICATED REPAIR DOUBLER PER EA A9-54R-11722, STEP 5. 2 L 7 2 4F RT A28NM 2007011700116 20070117 00116 NM 2007 1 17 F3LA200700005 1 20070105 A 5320 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 917FR 5893 1890 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM BETWEEN FR 66 AND FR 69, ABOUT 1 FT INBD OF THE MOLD LINE O N LT SIDE NEAR L2 DOOR - CORROSION AROUND SEVERAL HOLES AND AN AREA OF CORROSION THROUGH THE FLOORBEAM. REMOVED AND REP LACED FLOORBEAM PER SRM'S 51-42-11 AND 51-44-11, AND AIRBUS DRAWINGS D53472780 AND D53472816. 2 L 7 2 4F RT A28NM 2007011700117 20070117 00117 NM 2007 1 17 QXEA200700024 1 20070110 A 3097 697071268 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM PROP DEICE DAMAGED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 414QX 4061 PDX FLIGHT NR 2416: PROP DEICE CAUTION LIGHT ILLUMINATES WHENEVER PROP NR 2 CYCLES ON. SHOWS GOOD LOAD ON THE ELECTRICA L. AIRCRAFT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED DEICE HARNESS ON NR 2 PROP, NR 2 BLADE IAW Q400 AMM TA SK 61-10-06-000-805/61-10-06-400-805. FUNCTIONAL AND CALIBRATION TEST OF PROP DEICE SYSTEM TESTS GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 H 7 2 4T RT A13NM 2007011700118 20070117 00118 NM 2007 1 17 QXEA200700025 1 20070111 A 3040 MS24166D1 RELAY BOMBDR DHC8 DHC8402 1390042 NM WINDSHIELD HEAT FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 411QX 4055 GEG FLIGHT NR 2340: EN ROUTE TO MSO, CAPTAIN'S WINDSHIELD HEAT FAILED WITH NO ASSOCIATED CAUTION LIGHT. ON DESCENT INTO GEG, WINDSHIELD HEAT RETURNED AND CAPTAIN'S WINDOW CLEARED. FLIGHT DIVERTED TO GEG. MAINTENANCE REMOVED AND REPLACED K1, K2 AND K7 (P/N JC-DYN103) PER AMM 30-41-01 PAGES 407-413. CAPTAIN'S WINDSHIELD OPS CHECK NORMALLY. AIRCRAFT RETURN ED TO SERVICE. 2 H 7 2 4T RT A13NM 2007011700120 20070117 00120 EU 2007 1 17 SIMA200701502 1 20070112 A 2613 1734362450 OVERHEAT SENSOR SAAB SF340 340B 7860101 EU RT TAILPIPE FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 384AE 340B384 RIGHT TAIL PIPE HOT LIGHT CAME ON CLIMB-OUT, LIGHT WENT OUT WITHOUT ANY CREW ACTION. MGM EGT 874 DEGREES, OAT 8 DEGREES WITH ANTI-ICE ON. REMOVED AND REPLACED THREE TEMPERATURE SENSORS IN THE RIGHT ENGINE NACELLE IAW SAAB AMM 26-12-05. O PERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007011700121 20070117 00121 SO 2007 1 17 SIMA200701503 1 20070111 A 2752 3633001023 ACTUATOR EMB 135 EMB135KL 3260302 SO TE FLAPS FAILED A SIMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 21 834AE 10989 145631 RECEIVED FLAPS FAIL AND SPS ADVANCE MESSAGE WHEN FLAPS SELECTED TO 45 DEGREE POSITION. REMOVED AND REPLACED LEFT OUTBOA RD FLAP ACTUATOR IAW EMB AMM 27-51-10. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007011700126 20070117 00126 NM 2007 1 17 QXEA200700028 1 20070110 A 3230 301450301 SWITCH BOMBDR DHC8 DHC8402 1390042 NM MLG FAILED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 415QX 4081 PDX FLIGHT: NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED WITH GEAR RETRACTION. RAN CHECKLIST. CYCLED GEAR LIGHT WENT OUT. MAINTENANCE REMOVED AND REPLACED NGDRCC S19 PROX SWITCH IAW AMM TASK 32-61-06-000-802 AND 32-61-06-400-802. REMOVED A ND REPLACED NLG DOOR MECHANISM IAW AMM TASK 32-31-61-000-801 AND 32-31-61-400-801. OPS CHECK GOOD. NO OTHER DEFECTS NO TED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007011700127 20070117 00127 NE 2007 1 17 NACA20070002 2 20070112 A 8530 356993 CYLINDER DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 4 CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 6174C 499 35 44075 P33192 NR 2 ENGINE SHUT DOWN DUE TO LOW COMPRESSION INDICATION ON NR 4 CYLINDER. REPLACED NR 4 CYLINDER DUE TO A CRACKED HEAD PER NAC DC-6MM SECT V PG 16 AND 16A. OP AND LEAK CHECKED GOOD. 2 L 7 4 4R 4 R 6A3 5E8 2007011700128 20070117 00128 NM 2007 1 17 HALA0700017 1 20070110 A 3350 LAMP BOEING 767 76733A 1385209 NM EMERGENCY LIGHTS INOPERATIVE A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 R3 EXTERIOR EMERGENCY AREA LIGHT INOP. RELAMPED OPS CK GOOD. 2 L 7 2 4F RT A1NM 2007011700129 20070117 00129 NE 2007 1 17 HALA0700015 2 20070109 A 7420 IGNITER BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE RT ENGINE INOPERATIVE A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 479HA 55124 13235 BTB - RT ENGINE NO IGNITE, 2ND ATTEMPT START ABORTED. REMOVED AND REPLACED R ENG B IGNITER PER AM 74-20-04 OPS CK OK. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007011700131 20070117 00131 NM 2007 1 17 HALA0700016 1 20070109 A 5310 DOOR FRAME BOEING 767 767300 1385204 NM FUSELAGE DAMAGED A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 580HA 28140 3.5 INCH SCRATCH IN FUSELAGE AT TOP RIGHT CORNER OF C 2 DOOR FRAME. SCRATCH WITHIN SRM 53 00 01 LIMITS CLEANED SCRATCHE S PER FIGURE 101. NO FLIGHT RESTRICTIONS OK FOR SERVICE ALLOWABLE DAMAGE PER FIG 101. 2 L 7 2 4F RT A1NM 2007011700132 20070117 00132 EU 2007 1 17 MALA070006 1 20070113 A 3260 DOWNLOCK SWITCH SAAB SF340 340B 7860101 EU MLG CONTAMINATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 425XJ 340B425 ON DEPARTURE FROM DTW, THE CREW FOUND THAT THE GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH. THE CREW FOLLOWED THE QRH AND RETURNED TO DTW WITHOUT INCIDENT. INSPECTED UPLOCK SWITCHES AND FOUND NLG SWITCH COVERED WITH SAND AND ICE. CLEANED S WITCHES. DID EXTENSION AND RETRACTION IAW 32-30. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2007011700136 20070117 00136 EU 2007 1 17 SIMA200701510 1 20070112 A 5330 7253811001 SKIN SAAB SF340 340B 7860101 EU BS 702-710 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 902AE 24619 2000 340B269 SKIN PUNCTURED BETWEEN FUSELAGE STATION 702 TO 710. PERFORMED CUTOUT OF DAMAGE AND REMOVED FRAMES 702 AND 710. REMOVED AND REPLACED FRAMES 702 AND 710. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SAAB SRM 51-20-40, 51-40-21 AND 53-80-10. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007011700139 20070117 00139 NM 2007 1 17 USAABB07004 1 20070109 A 3233 273N10052 ACTUATOR BOEING 757 7572B7 1384964 NM MLG FAILED A USAA O OTHER O OTHER AP APPROACH 1 EA 19 933UW 27199 FLIGHT 1827, PHL-FLL: NOSE GEAR GREEN LIGHT FAILED TO ILLUMINATE WITH GEAR HANDLE DOWN. EICAS MESSAGE GEAR DISAGREE AN D GEAR DOORS DISPLAYED. DOORS AND GEAR AMBER LIGHTS ILLUMINATED. INDICATIONS WERE NORMAL AFTER ALTERNATE GEAR EXTENSIO N. FLIGHT LANDED WITH NO FURTHER DIFFICULTIES. MAINTENANCE REPLACED THE NLG LOCK ACTUATOR. ACCOMPLISHED GEAR SWING AN D RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007011700140 20070117 00140 2007 1 17 SWAA070211 4 20070115 A 2565 6557463 GIRT BAR BOEING 737 7373H4 1384600 NM L1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2007011700141 20070117 00141 2007 1 17 SWAA070212 4 20070115 A 2565 6557463 GIRT BAR BOEING 737 7373H4 1384600 NM L1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2007011700142 20070117 00142 NM 2007 1 17 SWAA070214 1 20070115 A 5753 65C26343 CARRIAGE BOEING 737 7373T5 1384608 NM TE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND LT WING INBOARD MID FLAP OUTBOARD CARRIAGE CORRODED. REMOVED AND REPLACED MID FLAP CA RRIAGE PER MM. 2 L 7 2 4F RT A16WE 2007011800003 20070118 00003 NM 2007 1 18 SWAA070221 1 20070116 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 408WN 27895 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007011800008 20070118 00008 NM 2007 1 18 USAA070033 1 20070111 A 5330 SKIN BOEING 737 737301 1384611 NM BS 747 S24R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 501UW 23231 AT 747 + 3 INCHES STRINGER 24R CRACKED. INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 REPAIR 31, DEFECT SIZE: 4 INCHES. 2 L 7 2 4F RT A16WE 2007011800009 20070118 00009 NM 2007 1 18 USAA070032 1 20070111 A 5311 FRAME BOEING 737 737401 1384701 NM BS 350 S9R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 STATION 350 ABOVE STRINGER 9R CRACKED. INSTALLED REPAIR DOUBLER IAW TR 53-10-20D, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007011800010 20070118 00010 NM 2007 1 18 USAA070031 1 20070111 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM BS 312-328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 STATION 312-328 RBL 11.5 HAS CORROSION. REPLACED INTERCOSTAL IAW SRM 51-10-02, DEFECT SIZE: .75 INCH. 2 L 7 2 4F RT A16WE 2007011800011 20070118 00011 NM 2007 1 18 USAA070030 1 20070111 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 STATION 312 LBL 7 TO LBL 8 HAS CORROSION. ACCOMPLISHED T-CAP REPAIR IAW SRM 53-10-51, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007011800013 20070118 00013 NM 2007 1 18 USAA070027 1 20070111 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 312-360 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 STATION 312-360 RBL 56 HAS CORROSION. REPLACED ANGLE IAW 51-10-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007011800014 20070118 00014 NM 2007 1 18 USAA070026 1 20070111 A 5320 SUPPORT ANGLE BOEING 737 737401 1384701 NM BS 294-328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 STATION 294.5-328 RBL 58 HAS CORROSION. REPLACED SUPPORT IAW SRM 51-10-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007011800015 20070118 00015 NM 2007 1 18 USAA070025 1 20070111 A 5320 FLOOR SUPPORT BOEING 737 737401 1384701 NM 335 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 STATION 335 RBL 52 HAS CORROSION. REPLACED SUPPORT IAW SRM 51-40-00, 51-40-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007011800016 20070118 00016 NM 2007 1 18 USAABB07006 1 20070112 A 3350 FUSE BOEING 767 767201 1385125 NM EMERGENCY LIGHTS FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 245AY 23897 MAINTENANCE FOUND FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE ROWS 1 AND 5 LEFT. REPLACED FUSE IN BATTERY CHARGER. NO FUR THER DIFFICULTIES. 2 L 7 2 4F RT A1NM 2007011800017 20070118 00017 NM 2007 1 18 USAABB07007 1 20070114 A 3230 2670296 VALVE BOEING 757 7572B7 1384964 NM MLG FAILED A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 933UW 48725 27199 FLIGHT 704, LAS-CLT: WHEN GEAR WAS EXTENDED ON APPROACH, NOSE GEAR GREENLIGHT DID NOT ILLUMINATE AND AMBER -DOORS- AND -GEAR- LIGHTS REMAINED ON. ABORTED APPROACH, RECYCLED GEAR, RECEIVED THREE GREEN LIGHTS. LANDED WITH NO FURTHER DIFFIC ULTIES. MAINTENANCE REPLACED THE NOSE LANDING GEAR, GEAR-OPERATED SEQUENCE VALVE. 2 L 7 2 4F RT A2NM 2007011800020 20070118 00020 NM 2007 1 18 SWAA070131 1 20070111 A 3040 BCREF129514 WIRE BOEING 737 7377H4 1384404 NM COCKPIT WINDOW SPARKS A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 420WN 29825 FLIGHT DECK L2 WINDOW ELECTRICAL CHORD SPARKED AND SMOKED. REMOVED AND REPLACED ELECTRICAL CHORD PER MM. 2 L 7 2 4F RT A16WE 2007011800024 20070118 00024 NM 2007 1 18 SWAA070135 1 20070111 A 5754 65C26602 SKIN BOEING 737 7373H4 1384600 NM NR 6 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED C1 CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT LOWER L/E. REPAIRED L/E SLAT PER SWA EA. 2 L 7 2 4F RT A16WE 2007011800025 20070118 00025 NM 2007 1 18 SWAA070136 1 20070111 A 5753 6546435304 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED C1 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD T/E. REMOVED AND REPLACED AFT FLA P PER MM. 2 L 7 2 4F RT A16WE 2007011100016 20070111 00016 EA 2007 1 11 SWIA200717644 1 20070106 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 866AS 7517 FORWARD OVERHEAD EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007011100036 20070111 00036 NM 2007 1 11 ASAA0741375 1 20070110 A 5754 65C2668654 WEDGE BOEING 737 7374Q8 138447Q NM NR 5 SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 THE RIGHT WING NR 5 SLAT IS CHAFED ON THE T/E LOWER SURFACE AT SS 144 152 AND 189 199. PREPAIRED THE DAMAGED SURFACES F OR BONDING, FABRICATED AND INSTALLED TWO REPAIR DOUBLERS IAW SRM 51-70-10 REPAIR 2. 2 L 7 2 4F RT A16WE 2007011100037 20070111 00037 NM 2007 1 11 ASAA0741377 1 20070109 A 5340 69489856 ATTACH ANGLE BOEING 737 7374Q8 138447Q NM BS 360 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 STRINGER 11L ATTACH CLIP CRACKED AT FS 360. REMOVED THE DAMAGED CLIP AND INSTALLED A REPLACEMENT CLIP IAW EA 5310 02689 AND AAR EA 11818. 2 L 7 2 4F RT A16WE 2007011100042 20070111 00042 NM 2007 1 11 ASAA0711358 1 20070105 A 5210 65299945 GUIDE ARM BOEING 737 7372Q8 138448K NM L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 741AS 21959 FWD ENTRY DOOR HANDLE IS RELUCTANT TO STAY COMPLETELY CLOSED. ADJUSTED L1 DOOR GUIDE ARM. 2 L 7 2 4F RT A16WE 2007011100052 20070111 00052 NM 2007 1 11 ASAA0741369 1 20070108 A 5755 654645263 SKIN BOEING 737 7374Q8 138447Q NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 THE LEFT WING NR 4 SPOILER LOWER SURFACE HAS NUMEROUS DENTS AND DINGS AT WBL 87.75. PREPAIRED THE DAMAGED SURFACE FOR B ONDING, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 51-70-10 PG 211, 213, 221, 238, 244 AND 249. 2 L 7 2 4F RT A16WE 2007011100053 20070111 00053 NM 2007 1 11 ASAA0741370 1 20070108 A 5755 654645163 SKIN BOEING 737 7374Q8 138447Q NM NR 3 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 THE LEFT WING NR 3 SPOILER UPPER SURFACE IS DENTED AT WS 334. PREPAIRED THE DAMAGED SURFACE FOR BONDING, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 51-70-10 REPAIR 2. 2 L 7 2 4F RT A16WE 2007011100068 20070111 00068 NM 2007 1 11 DL738070012 1 20070106 A 3350 LIGHT BOEING 737 737832 13844CF NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 383DN 30346 EMERGENCY LIGHTING LAMP INOP AT SEAT 31D. REPLACED EMERGENCY LIGHT ASSY AT SEAT 31D. 2 L 7 2 4F RT A16WE 2007011100080 20070111 00080 NM 2007 1 11 AALA20070038 1 20070108 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 632AA 24590 MIA - EMERGENCY LIGHT AT LEFT OVERWING EXIT INOPERATIVE. RELAMPED AFT LAMP FOR EMERGENCY LIGHT AT LEFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007011100085 20070111 00085 NM 2007 1 11 AALA20070045 1 20070109 A 3350 CONNECTOR BOEING 737 737823 13844BZ NM EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 936AN 29532 MIA - EMERGENCY LIGHT AT SEAT 12D INOPERATIVE. REPINNED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007011100109 20070111 00109 NM 2007 1 11 SWAA070101 1 20070109 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 402WN 29814 EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007011100116 20070111 00116 NM 2007 1 11 USAA070018 1 20070108 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 321-344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 STATION 321 TO 344 LBL 60-62 HAS CORROSION. REPLACED ANGLE IAW SRM 51-10-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007011100130 20070111 00130 NE 2007 1 11 DL757070019 2 20070109 A 7261 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 LEAKING A DALA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 651DL 24391 728775 AFTER START OF NR 2 ENGINE OIL QTY WENT TO 4 ON T/O ROLL QTY FELL TO 1. FOUND NR 2 ENGINE LEAKING OIL FROM DE-OILER MAS T. REMOVED AND REPLACED DE-OILER CARBON SEAL PER AMM. NO LEAKS NOTED. OIL CKS NORMAL. MCO AND PLACARD REMOVED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007011600007 20070116 00007 NM 2007 1 16 SWAA070125 1 20070110 A 5753 6550756 RIB BOEING 737 7373H4 1384600 NM RT FORE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND RIGHT WING INBOARD FORE FLAP OUTBOARD RIB CORRODED. REMOVED AND REPLACED FORE FLAP RI B PER SRM. 2 L 7 2 4F RT A16WE 2007071000111 20070710 00111 SO 2007 7 10 FDKA200705236 1 20070509 A 7160 ACOUSTIC PANEL EMB 145 EMB145LR 3260212 SO NR 2 ENGINE DENTED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 850MJ 145568 NR 2 INLET, INNER SKIN, IS DAMAGED IN TWO AREAS. THE DAMAGE HAS BEEN REPAIRED. 2 L 7 2 4T RT T00011AT 2007011700005 20070117 00005 NM 2007 1 17 QXEA200700016 1 20070107 A 3150 304723701 SENSOR BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 416QX 6479 4083 29257 MFR FLIGHT NR 2460, FOLLOWING ENGINE START, DURING TAXI, POWER PLANT MESSAGE ON ED DISPLAYED ALONG WITH NR 2 ENGINE FADE C CAUTION LIGHT. AIRCRAFT RETURNED TO GATE. MAINTENANCE FOUND CDS SQUAWKED 32 INLT TEMP SENSOR. REPLACED T1.8 SENSOR PER Q400 AMM TASK 77-21-02-00-801 AND 77-21-02-400-801. TESTS GOOD. AIRCRAFT RETURNED TO SERVICE 2 H 7 2 4T 4 T RT A13NM E00062EN 2007011700020 20070117 00020 NM 2007 1 17 QXEA200700019 1 20070108 A 3297 471525 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM NLG UNKNOWN A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 401QX 14325 4031 MSO FLIGHT NR 2347: GEAR (ALL 3) FAILED TO RETRACT. LEFT MAIN LANDING GEAR DOOR LIGHT (AMBER) WOULD FLASH MOMENTARILY ( EVERY 5 SECONDS OR SO) WHEN THE GEAR HANDLE WAS IN THE UP POSITION. RAN THE GEAR FAILURE CHECKLIST AND IT DID NOT SOLVE THE PROBLEM. AIRCRAFT RETURNED TO FIELD AND GATE. MAINTENANCE REMOVED AND REPLACED THE NLG ELECTRICAL HARNESS. CHECK S GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007011700035 20070117 00035 NM 2007 1 17 DLM88070027 1 20070112 A 2120 DUCT DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE AFT CONTAMINATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 917DL 16595 49573 P80168 AIRBORNE RETURN FOR SMOKE/FUMES IN CABIN. FIRST OFFICERS AFT LAV SMOKE DETECTOR ACTIVATED. MTC IN WORK DOING DUCT BURN OUT AND WASHING APU INLET. REMOVED AND REPLACED COALESCER BAGS CLEANED RESIDUAL OIL FROM APU INLET PERFORM FULL DUCT BU RNOUT PER OPN 5089. NO SMOKE OR ODORS. REMOVED AND REPLACED COALESCER BAGS. 2 L 7 2 4F 4 F RT A6WE E9NE 2007011700040 20070117 00040 NM 2007 1 17 DL76L070034 1 20070114 A 3350 276005 FUSE BOEING 767 767332 1382001 NM EMERGENCY LIGHT BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 194DN 28451 1ST EMER LIGHT AFT OF LEFT WING MOUNTED ON FUSELAGE INOP. REPLACED FUSE AT M9008. OPS NORMAL. EXT EMERGENCY LIGHT AT 1L INOP. REPLACED FUSE AT M0736. OPS NORMAL. 2 L 7 2 4F RT A1NM 2007011700057 20070117 00057 NM 2007 1 17 DL76G070023 1 20070106 A 4920 380029817 TURBINE BOEING 767 767332 1382001 NM GE CF6 CF680 30025 NE APU MAKING METAL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1602 12044 29694 P2550 APU AUTO SHUTDOWN AT GATE. FOUND METAL ON CHIP DETECTOR. REPLACED APU. 2 L 7 2 4F 4 F RT A1NM E13NE 2007011700061 20070117 00061 NM 2007 1 17 AALA20070050 1 20070111 A 3350 BPS73 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 325AA 22326 LAX - EMERGENCY LIGHTS AT SEAT ROWS 10AB, 11AB, 17AB AND 19AB COME ON WHEN POWER AND BATTERY ARE TURNED OFF. REPLACED B ATTERY PACK FOR INOPERATIVE EMERGENCY LIGHTS AT SEAT ROWS 10AB, 11AB AND 19AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007011700063 20070117 00063 NM 2007 1 17 AALA20070058 1 20070108 A 3350 D71701100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 953AN 29539 TUL - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED OPERATIONAL TEST. PLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007011700069 20070117 00069 NM 2007 1 17 AALA20070053 1 20070102 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 919AN 29520 TUL - EMERGENCY LIGHT BATTERY PACK AT STATION 380 TO 400 FOR FIRST CLASS SEATS FAILED OPERATIONAL TEST. REPLACED EMERGE NCY LIGHT BATTERY PACK AT STATION 380 TO 400 FOR FIRST CLASS SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007011700086 20070117 00086 NM 2007 1 17 AALA20070060 1 20070109 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 920AN 29521 TUL- EMERGENCY LIGHT BATTERY PACK AT STATION 590 LEFT FORWARD EMERGENCY EXIT FAILED OPERATIONAL TEST. REPLACED EMERGENC Y LIGHT BATTERY PACK AT STATION 590 LEFT FORWARD EMERGENCY EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007011700091 20070117 00091 NM 2007 1 17 F3LA200700006 1 20070106 A 5320 D53471124200201 SHEAR PLATE AIRBUS A319 A319111 3930336 NM RIGHT CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 917FR 5893 1890 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON AFT CORNER OF RT LATERAL SHEAR PLATE. DETERMINED SHEAR PLATE AND SUP PORT FRAME TO BE OUT OF LIMITS. REMOVED SHEAR PLATE SUPPORT FRAME ASSY PER SRM 53-41-14, FIG 2 AND 51-42-11. REPLACED SHEAR PLATE AND SUPPORT FRAME AFT GALLEY, RT SIDE, PER SRM 51-42-11. 2 L 7 2 4F RT A28NM 2007011700092 20070117 00092 2007 1 17 F3LA200700007 4 20070106 A 2565 D5348015900400 GIRT BAR AIRBUS A319 A319111 3930336 NM L2 DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 917FR 5893 1890 DURING C-3 CHECK, INSPECTION REPORTED GIRT BAR PLATES ON FWD AND AFT L2 DOOR CORRODED. REPLACED FWD AND AFT L2 DOOR GIR T BAR PLATES PER AMM 52-13-31. RIGGED AND SEALED GIRT BAR LATCHES PER AMM 52-13-00-820-001. 2 L 7 2 4F RT A28NM 2007011700109 20070117 00109 NM 2007 1 17 07FDEA00083 1 20070112 A 5340 65453133 STRINGER CLIP BOEING 727 727233 138408A NM BS 680 S1 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 REWORK OF N/R N00848, STRINGER CLIP AT STA 680 STR 1 CLIP REPAIRED WITH INCORRECT REF. REMOVED OLD STRINGER CLIP, DRILL ED NEW STRING CLIP, INSTALLED NEW STRINGER CLIP REF SRM 51-30-2 PG 1-12. 2 L 7 3 4F RT A3WE 2007011700122 20070117 00122 EA 2007 1 17 SIMA200701506 1 20070112 A 3250 TARGET CNDAIR CL600 CL6002C10 1390015 EA NLG STEERING MISSING A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 512AE 10110 GEAR WOULD NOT RETRACT, EMERGENCY DECLARED. FOUND NOSE LANDING GEAR STEERING TARGET MISSING ON POST INSPECTION. REPLAC ED NOSE LANDING GEAR COLLAR AND STEERING TARGET IAW CRJ AMM 32-61-05. OPERATIONAL CHECK GOOD - RETURNED AIRCRAFT TO SERV ICE 2 L 7 2 4F RT A21EA 2007011700135 20070117 00135 EU 2007 1 17 SIMA200701509 1 20070113 A 5512 7255150523 SKIN SAAB SF340 340B 7860101 EU HORIZONTAL STAB PUNCTURED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 904AE 22528 340B314 LEFT HORIZONTAL STABILIZER LOWER SKIN PUNCTURED. REMOVED AND REPLACED SKIN IAW SAAB SDS 011469, DATED 7 JANUARY 2007. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007011700137 20070117 00137 NM 2007 1 17 USAA070023 1 20070110 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 727 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 FLOORBEAM AT STATION 727 + 7 RBL 3. ACCOMPLISHED DOUBLER REPAIR IAW SRM 51-10-02, 53-60-53, TR 53-10-06B DEFECT SIZ E: .5" 2 L 7 2 4F RT A16WE 2007011700143 20070117 00143 NM 2007 1 17 SWAA070213 1 20070115 A 5512 SKIN BOEING 737 7373T5 1384608 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED SPV CHECK, FOUND LT HORIZONTAL STAB UPPER SKIN CORRODED AT REAR SPAR STA 198. REMOVED AND REPLACED HOR IZONTAL STAB PER MM. 2 L 7 2 4F RT A16WE 2007011800002 20070118 00002 NM 2007 1 18 SWAA070220 1 20070116 A 5340 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM BS 767 S21R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007011800042 20070118 00042 NM 2007 1 18 SWAA070139 1 20070111 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 578 S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007011800043 20070118 00043 NM 2007 1 18 SWAA070140 1 20070111 A 5311 6546533 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007011800044 20070118 00044 NM 2007 1 18 SWAA070141 1 20070111 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM BS 380 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007011800045 20070118 00045 NM 2007 1 18 SWAA070142 1 20070111 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM BS 520 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007011800046 20070118 00046 NM 2007 1 18 SWAA070143 1 20070111 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 400 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007011800047 20070118 00047 2007 1 18 SWAA070144 4 20070111 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007011800048 20070118 00048 2007 1 18 SWAA070145 4 20070111 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007011800049 20070118 00049 NM 2007 1 18 SWAA070146 1 20070111 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 750 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED C4 CHECK, FOUND FUSELGAE SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007011800051 20070118 00051 NM 2007 1 18 SWAA070148 1 20070111 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM BS 616 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, STR 15R. REPAIRED FRAME PER BOEING SB. 2 L 7 2 4F RT A16WE 2007011800052 20070118 00052 NM 2007 1 18 SWAA070149 1 20070111 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 360 S11L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007011800054 20070118 00054 NM 2007 1 18 SWAA070151 1 20070111 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007011800055 20070118 00055 NM 2007 1 18 SWAA070152 1 20070111 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8R-8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007011800059 20070118 00059 NM 2007 1 18 SWAA070153 1 20070111 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM BS 867 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007011800060 20070118 00060 NM 2007 1 18 SWAA070154 1 20070111 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007011800061 20070118 00061 NM 2007 1 18 SWAA070155 1 20070111 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007011800062 20070118 00062 NM 2007 1 18 SWAA070156 1 20070111 A 5311 6546535 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007011800063 20070118 00063 NM 2007 1 18 SWAA070157 1 20070111 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 793SA 27888 DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007011800064 20070118 00064 NM 2007 1 18 SWAA070158 1 20070111 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 793SA 27888 DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2007011800065 20070118 00065 NM 2007 1 18 SWAA070159 1 20070111 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 793SA 27888 DURING SCHEDULED HC2 CHECK, LT OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007011800079 20070118 00079 NM 2007 1 18 SWAA070162 1 20070112 A 2121 215201 FAN BOEING 737 7377H4 1384404 NM GASPER ODOR A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 29 779SW 27884 WITH GASPER FAN OPERATING, SMELL/ODOR IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2007011800080 20070118 00080 NM 2007 1 18 SWAA070163 1 20070112 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727D CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007011800082 20070118 00082 NM 2007 1 18 SWAA070165 1 20070112 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 360-440 S20R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPV CHECK, FOUND STR 20R CORRODED AT BS 360 TO BS 440. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007011800083 20070118 00083 NM 2007 1 18 SWAA070166 1 20070112 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 420 S21R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 420, STR 21R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007011800084 20070118 00084 NM 2007 1 18 SWAA070167 1 20070112 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 21 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007011800085 20070118 00085 NM 2007 1 18 SWAA070168 1 20070112 A 5310 6547962 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME SECTION PER ER. 2 L 7 2 4F RT A16WE 2007011800086 20070118 00086 NM 2007 1 18 SWAA070169 1 20070112 A 3350 20121 CHARGER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED MV1 CHECK, FOUND LT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007011800088 20070118 00088 NM 2007 1 18 SWAA070171 1 20070112 A 5320 BAC1509100146 FLOOR SUPPORT BOEING 737 7373H4 1384600 NM BS 727C-727D CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPT FLOORBEAM CORRODED AT BS 727C TO BS 727D, STR 28R. REMOVED AND REPLAC ED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007011800090 20070118 00090 NM 2007 1 18 SWAA070173 1 20070112 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM BS 378 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 378.5, LBL 2.8 EQUIPMENT COOLING EXHAUST CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007011800096 20070118 00096 NM 2007 1 18 SWAA070161 1 20070112 A 3350 100031 SIGN BOEING 737 7375H4 138449D NM EMERGENCY LIGHTS DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 RIGHT OVERWING EMERGENCY EXIT SIGN FELL OFF. INSTALLED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007011800098 20070118 00098 NM 2007 1 18 SWAA070174 1 20070112 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, LBL 3, AC GROUND RECEPTACLE FWD RADIUS. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007011800099 20070118 00099 NM 2007 1 18 SWAA070175 1 20070112 A 5330 6552880 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR CUTOUT, UPPER AFT CORNER. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 2007011800100 20070118 00100 NM 2007 1 18 SWAA070176 1 20070112 A 5315 6545812 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 27 TO RBL 48. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007011800101 20070118 00101 NM 2007 1 18 SWAA070177 1 20070112 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 706 S11L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007011800102 20070118 00102 NM 2007 1 18 SWAA070178 1 20070112 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 706 S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007011800103 20070118 00103 2007 1 18 SWAA070179 4 20070112 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007011800105 20070118 00105 NM 2007 1 18 SWAA070181 1 20070112 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 465WN 33829 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 3 ABC TO ROW 5 ABC. REMOVED AND REPLACED EEPLS COVER PER M M. 2 L 7 2 4F RT A16WE 2007011800108 20070118 00108 NM 2007 1 18 SWAA070184 1 20070113 A 2910 65C26839 LINE BOEING 737 7377H4 1384404 NM A-HYD SYSTEM LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 29 211WN 34163 DECLARED EMERGENCY/DIVERSION. EN ROUTE BETWEEN LAS AND PHL -A- HYDRAULIC SYSTEM LOST PRESSURE AND QUANTITY, COMPLIED WI TH QRH, LANDED AT BWI. REMOVED AND REPLACED HYDRAULIC LINE AT PRESSURE MODULE PER MM. 2 L 7 2 4F RT A16WE 2007011800109 20070118 00109 NM 2007 1 18 SWAA070185 1 20070113 A 3350 65C3330486 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM . 2 L 7 2 4F RT A16WE 2007011800110 20070118 00110 NM 2007 1 18 SWAA070186 1 20070113 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007011800113 20070118 00113 NM 2007 1 18 SWAA070189 1 20070113 A 3397 65C27093 WIRE BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 602SW 27953 DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. FOUND BROKEN WIRE AT LIGHT ASSY. REPAIRED BRO KEN WIRE PER MM. 2 L 7 2 4F RT A16WE 2007011800115 20070118 00115 NM 2007 1 18 SWAA070191 1 20070114 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 460 S25L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 460, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007011800116 20070118 00116 NM 2007 1 18 SWAA070192 1 20070114 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 440 S25L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 440, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007011800117 20070118 00117 NM 2007 1 18 SWAA070193 1 20070114 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 727E S18R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007011800118 20070118 00118 NM 2007 1 18 SWAA070194 1 20070114 A 5320 146A5530 FLOOR SUPPORT BOEING 737 7377H4 1384404 NM BS 755-779 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 794SW 30605 DURING SCHEDULED 8Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 755 TO BS 779, RBL 13. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007011800135 20070118 00135 NE 2007 1 18 BB07008 2 20070116 A 7310 AC9227F1740 FILTER BOEING 767 767201 1385125 NM GE CF6 CF680 30025 NE FUEL CLOGGED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 248AY 23900 690197 FLIGHT 1565, MXP-PHL: AFTER TAKEOFF, CREW RECEIVED A LEFT ENGINE FUEL FILTER MESSAGE. RETURNED TO MXP. MAINTENANCE RE PLACED THE LEFT ENGINE FUEL FILTER. NO FURTHER DIFFICULTIES. 2 L 7 2 4F 4 F RT A1NM E13NE 2007011800139 20070118 00139 NM 2007 1 18 2007UALA00045 1 20070105 A 2133 OUTFLOW VALVE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN PRESSURE INOPERATIVE A UALA B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 331UA 24192 ACFT EXPERIENCED RAPID DEPRESSURIZATION. EMERGENCY DESCENT, O2 MASKS DID NOT DEPLOY. AC MOTOR FAILED ON OUTFLOW VALVE. REPLACED OUTFLOW VALVE ON A/C. REPLACED THE AC MOTOR ON THE REMOVED OUTFLOW VALVE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007011800141 20070118 00141 NM 2007 1 18 2007UALA00047 1 20070105 A 3350 78941 LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 777UA 26916 SEAT 3F AFT EEL LIGHT IS MISSING. *S/D* REPLACED AFT EEL LIGHT ASSY AT SEAT 3F. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007011900001 20070119 00001 NM 2007 1 19 RYNA200700001 1 20070108 A 3610 32145525 SHUTOFF VALVE BOEING 737 737800* NM BLEED SYSTEM LEAKING A RYNA O OTHER J WARNING INDICATION CL CLIMB 1 GL 31 EIDKD 28617 AIR TURNBACK, AFTER DEPARTURE CLIMBING THROUGH FL370 LEFT BLEED TRIP LIGHT ILLUMINATED WHILE TRYING TO RESET, THE RIGHT BLEED TRIPPED. ALSO MANAGED TO RESET BOTH, BUT BOTH TRIPPED AGAIN. FINALY MADE AN AIR TURNBACK TO DTW. COMPLIED WITH FIM AND FOUND LEFT ENGINE PRESSURE REGULATING SHUT OFF VALVE (PRSOV) LEAKING. REMOVED AND REPLACED PRSOV IAW AMM 36-11- 04, OPS AND LEAK CHECKED GOOD. 2 L 7 2 4F RT A16WE 2007011900012 20070119 00012 CE 2007 1 19 DXTA200701841 1 20070108 A 3240 AHA1897 BRAKE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP NR 1 WORN E DXTA O OTHER S AFFECT SYSTEMS LD LANDING 1 GL 07 805QS 3127 3127 258505 BRAKES FEEL MUSHY AFTER LANDING AND DURING TAXI. REPLACED NR 1 AND 2 BRAKE ASSEMBLIES. BLED SYSTEM. OPS CHECKED OK IAW H AWKER 800XP M.M. 32-40-00 2 L 7 2 4F 4 F RT A3EU E6WE 2007011900013 20070119 00013 CE 2007 1 19 DXTA200701843 1 20070109 A 3240 BRAKE ASSY BEECH MU300 400A 1155402 CE MLG MALFUNCTIONED E DXTA D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 GL 07 149QS RK473 RT BRAKE ON LT SEAT PILOT INOPERATIVE. THE BRAKE WORKS INTERMITTENTLY. BRAKE ON RT PANEL GOES TO THE FLOOR THEN WILL ST ART TO WORK AGAIN FOR A SHORT TIME. RT SEAT HAD GOOD BRAKES AT ALL TIMES. RETURNED TO DEPARTURE. PERFORM "POWER BRAKE BLEEDING" OF THE BRAKE SYSTEM PER RAS TECH SUPPORT (BILL) IN ACCORDANCE WITH HAWKER 400XP M.M. CHAPTER 32-40-00 A THRU K . PERFORM OPERATIONAL CHECK OF THE BRAKE SYSTEM DURING TAXI CHECK, FOUND NO DISCREPANCY AT THIS TIME. 2 H 7 2 4F RT A16SW 2007011900014 20070119 00014 CE 2007 1 19 DXTA200701844 1 20070109 A 2910 AE1011889G0171 LINE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL HYDRAULIC SYS FAILED E DXTA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 07 923QS 8781 7500023 AFTER TAKE-OFF LOST SYSTEM (A) FLUID AND (A) PRESSURE AND IAW EJA ABNORMAL PROCEDURED UNLOADED (A) PUMP, RETURNED TO BFI FOR NORMAL LANDING, WENT THROUGH LOSS OF A HYDRAULICS CHECK LIST AND AFTER LANDING WE WERE TOWED TO FBO. REMOVED NOSE WHEEL CENTERING HYDRAULIC LINE AND INSTALLED CUSTOMER SUPPLIED NEW HYDRAULIC LINE IAW CESSNA 750 MM 32-50-00. BLED SYST EM AND LEAK CHECKED HOSE ASSY. LEAK CHECK GOOD. FUNCTIONAL TEST IN REFERENCE TASK 32-50-00-720 CHECK GOOD. SERVICED A-HY D. SYSTEM IAW CESSNA 750 MM 12-00-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007011900015 20070119 00015 CE 2007 1 19 DXTA200701845 1 20070109 A 3230 HANDLE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG STUCK E DXTA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 GL 07 934QS 7500034 LANDING GEAR HANDLE WOULD NOT MOVE FROM THE DOWN POSITION WHEN ATTEMPTING TO RETRACT THE LANDING GEAR AFTER TAKEOFF. JAC KED AIRCRAFT CHECKED SYSTEM FOR PROPER OPERATION COULD NOT DUPLICATE. REMOVED AND REPLACED LANDING GEAR CONTROL UNIT. OP S CHECKED GOOD IAW 750 M/M CH 32-30-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007011900022 20070119 00022 EU 2007 1 19 USAA070037 1 20070111 A 3213 STRUT AIRBUS A321 A321211 3930370 EU NLG CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 65 US 1431 NOSE LANDING GEAR UPPER STRUT TORQUE LINK LUGS HAS CORROSION. INSTALLED OVERSIZED BUSHINGS, REAMED HOLES & REMOVED CORR OSION PER TYP REPAIR 32-20-01, DEFECT SIZE: .125 INCH. 2 L 7 2 4F RT A28NM 2007011900023 20070119 00023 EU 2007 1 19 USAA070036 1 20070111 A 5320 THRESHOLD AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 65 US 1431 RIGHT AFT PAX DOOR THRESHOLD FWD CORNER HAS CORROSION. CORRODED AREA WAS CUT OUT & REPAIRED PER SRM 53-41-14, FIG 201; CORR TASK JA-260-25500; LEVEL 1. 2 L 7 2 4F RT A28NM 2007011900024 20070119 00024 EU 2007 1 19 USAA070035 1 20070111 A 5320 THRESHOLD AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 65 US 1431 LEFT AFT PAX DOOR THRESHOLD FRAME 67 HAS CORROSION. INSTALLED DOUBLER REPAIR AND FILLER PER SRM 53-41-14; CORR TASK JA- 260-25500; LEVEL 1, DEFECT SIZE: .75 INCH DIA. 2 L 7 2 4F RT A28NM 2007011900027 20070119 00027 2007 1 19 DJFA2007002 4 20070102 A 3418 SLZ7715EX COMPUTER CESSNA 650 650 2076802 CE STALL WARNING ODOR E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 364CW 9279 6500164 KLUK-KTUL TRIP 1124319 THE CREW REPORTED A STRONG ELECTRICAL BURNING ODOR IN THE COCKPIT AREA WITH NO SMOKE PRESENT. T HEY WERE UNABLE TO ISOLATE IN FLIGHT. MAINTENANCE TROUBLESHOT THE ELECTRICAL SMELL AND ISOLATED IT TO THE STALL WARNING COMPUTER. THE STALL WARNING ANNUNCIATOR ALSO ILLUMINATED DURING FLIGHT. MAINTENANC FOUND THE STALL WARNING COMPUTER BUR NED AND OVERHEATED. THE UNIT WAS REPLACED AND OPERATIONALLY CHECKED. ALL CHECKS WERE SATISFACTORY. 2 L 7 2 4F A9NM 2007011600006 20070116 00006 NM 2007 1 16 SWAA070124 1 20070110 A 5311 6936642 FRAME BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND BULKHEAD FRAME CRACKED AT LEFT BS 178, WL 208. REMOVED AND REPLACED CHORD SECTION PER ACO. 2 L 7 2 4F RT A16WE 2007011700026 20070117 00026 WP 2007 1 17 07FDEA00080 1 20070112 A 5347 AGA3855509 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 AFT CARGO COMPARTMENT, SEAT TRACK AT STA 1846, X= 20 CORRODED. REPAIRED AS PER SRM 53-70- 00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007011700045 20070117 00045 SO 2007 1 17 SIMA200701102 1 20070108 A 2760 14533022405 CONTROL UNIT EMB 135 EMB135LR 3260305 SO SPOILERS FAILED A SIMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SW 21 704PG 14440 145174 RECEIVED SPOILER OPEN AND FAIL MESSAGE IN CRUISE, EMERGENCY DECLARED. REMOVED AND REPLACED SPOILER CONTROL UNIT IAW EMB AMM 27-63-02. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007011700064 20070117 00064 NM 2007 1 17 AALA20070059 1 20070108 A 3350 D71701100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 953AN 29539 TUL - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED OPERATIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007011700076 20070117 00076 NM 2007 1 17 DU4R2007007 1 20070101 A 5321 SPLICE BOEING 757 757232 1384965 NM BS 1330 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 FOUND CORROSION AFT CARGO FLOOR PANEL SPLICE AT BS 1330. REPAIRED CORRODED SPLICE BY FABRICATING AND INSTALLING NEW SPL ICE 1-3/4 BY 40 FROM BAC1505-100766 7075-T6 IAW B757 SRM 51-20-1, 51-40-02 AND DWG 453N1611. 2 L 7 2 4F RT A2NM 2007011700077 20070117 00077 NM 2007 1 17 DU4R2007008 1 20070101 A 5321 SPLICE BOEING 757 757232 1384965 NM BS 1510 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 FOUND CORROSION AFT CARGO FLOOR PANEL SPLICE AT BS 1510. REPAIRED CORRODED SPLICE BY FABRICATING AND INSTALLING NEW SPL ICE 1-3/4 BY 40 FROM BAC1505-100766 7075-T6 IAW B757 SRM 51-20-1, 51-40-02 AND DWG 453N1611. 2 L 7 2 4F RT A2NM 2007011700110 20070117 00110 NM 2007 1 17 07FDEA00084 1 20070112 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 REWORK OF N/R N00849, STRINGER CLIP AT BS 680 STR 2L REPAIRED WITH INCORRECT REF. REMOVED OLD STRINGER CLIP, BACK DRILL ED STRINGER CLIP, INSTALLED NEW STRINGER CLIP REF SRM 51-30-2 PG 1-12. 2 L 7 3 4F RT A3WE 2007011700112 20070117 00112 NM 2007 1 17 07FDEA00086 1 20070112 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 FOUND STRINGER CLIP CRACKED IN RADIUS CUTOUT BS 680 STR S-4L. REMOVED STRINGER CLIP, DRILLED STRINGER CLIP, INSTALLED S TRINGER CLIP REF SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007011700115 20070117 00115 NM 2007 1 17 F3LA200700001 1 20070107 A 5321 D5367180500500 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 917FR 5893 1890 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON LOWER SURFACE OF FLOOR PANEL 262FF. REPLACED FLOOR PANEL PER WORK CA RD C534103-2. 2 L 7 2 4F RT A28NM 2007011700130 20070117 00130 NM 2007 1 17 HALA0700021 1 20070109 A 3270 SAFETY WIRE BOEING 767 76733A 1385209 NM TAIL SKID BROKEN A HALA O OTHER O OTHER LD LANDING 1 WP 13 591HA 33423 CREW REPORTED THAT F/A IN AFT GALLEY REPORTS LOUD NOISE ON LANDING. UPON EXAMINATION OF TAIL SKID FOUND SAFETY WIRE BRO KEN ONLY. REPLACED BROKEN SAFETY WIRE AND PERFORMED TAIL DRAG CONDITION INSP PER HAL M291-767, NO DAMAGE NOTED. 2 L 7 2 4F RT A1NM 2007011700133 20070117 00133 WP 2007 1 17 NWAA70089611 1 20070112 A 2131 OUTFLOW VALVE DOUG DC9 DC932 3022066 WP CABIN PRESSURE MALFUNCTIONED A NWAA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 GL 01 611NA 47435 DURING CLIMB AT FL 200 WITH WING ANTI-ICE ON SELECTED CABIN BEGAN TO CLIMB AND DESCEND RAPIDLY. FLIGHT DESCENDED TO FL 100. NO MENTION OF OXYGEN MASKS BEING DEPLOYED. FLIGHT DIVERTED TO PHL AND LANDED WITHOUT INCIDENT. MAINT REPLACED CA BIN PRESS CONTROLLER AND OUTFLOW VALVE. ALSO, REPLACED ICE PROTECT THERMOSTAT AND ANTICIPATOR. OPERATION CHECKS GOOD. 2 L 7 2 4F A6WE 2007011700134 20070117 00134 EU 2007 1 17 SIMA200701513 1 20070113 A 5514 AL2024T3 SPAR CAP SAAB SF340 340B 7860101 EU HORIZONTAL STAB BENT A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 904AE 22528 340B314 LEFT HORIZONTAL STABILIZER REAR LOWER SPAR CAP BENT. PERFORMED CUT OUT OF DAMAGE, FABRICATED REPAIR DOUBLERS. INSTALLE D REPAIR DOUBLERS AND RESTORED PROTECTIVE FINISH IAW SAAB SDS 011469, DATED 8 JANUARY 2007. RETURNED AIRCRAFT TO SERVIC E. 2 L 7 2 4T RT A52EU 2007011700138 20070117 00138 NM 2007 1 17 USAA070024 1 20070110 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 727 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 FLOORBEAM AT STATION 727 + 7 RBL8. ACCOMPLISHED DOUBLER REPAIR IAW SRM 51-10-02, 53-60-53, TR 53-10-06B DEFECT SIZE: .5" 2 L 7 2 4F RT A16WE 2007011800006 20070118 00006 NM 2007 1 18 SWAA070224 1 20070116 A 5315 147A5500 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 987 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 742SW 29278 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, LBL 43 TO RBL 40. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007011800012 20070118 00012 NM 2007 1 18 USAA070028 1 20070111 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM BS 294-312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 STATION 294.5 - 312 RBL 11.5 HAS CORROSION. REPLACED INTERCOSTAL IAW SRM 51-10-02, DEFECT SIZE: 18 INCHES. 2 L 7 2 4F RT A16WE 2007011800023 20070118 00023 NM 2007 1 18 SWAA070134 1 20070111 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 460WN 32464 EEPLS COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007011800026 20070118 00026 NM 2007 1 18 SWAA070137 1 20070111 A 5523 65C26384 STRUCTURE BOEING 737 7373H4 1384600 NM RT ELEVATOR TAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED C1 CHECK, FOUND RIGHT ELEVATOR TAB MAST FITTING CRACKED AT INBOARD CONTROL ROD ATTACHMENT. REMOVED AND REPLACED ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2007011800035 20070118 00035 NM 2007 1 18 SWAA070138 1 20070111 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 559 S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007011800050 20070118 00050 NM 2007 1 18 SWAA070147 1 20070111 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 510D S11L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510D, STR 11L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007011800057 20070118 00057 NM 2007 1 18 USAASB07005 1 20070107 A 5610 5893543129 WINDSHIELD BOEING 737 737401 1384701 NM COCKPIT CRACKED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 424US 16362 16362 23991 ORD FLT 1919 EN ROUTE FROM CLT TO ORD, CREW REPORTED THE CAPTAIN'S L1 WINDSHIELD BEGAN TO ARC AND THEN CRACK. FLIGHT L ANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S L1 WINDSHIELD PER JOB CARD J356-11-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007011800089 20070118 00089 NM 2007 1 18 SWAA070172 1 20070112 A 5320 BAC1509100146 FLOOR SUPPORT BOEING 737 7373H4 1384600 NM BS 767-787 S27L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPT FLOORBEAM CORRODED AT BS 767 TO BS 787, STR 27L. REMOVED AND REPLACED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007011800104 20070118 00104 2007 1 18 SWAA070180 4 20070112 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007011800119 20070118 00119 NM 2007 1 18 SWAA070195 1 20070114 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 772 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 794SW 30605 DURING SCHEDULED 8Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 772, LBL 3. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007011900025 20070119 00025 EU 2007 1 19 USAA070029 1 20070111 A 5347 D5311278220201 SEAT TRACK AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 65 US 1431 Y765 FR 23 SEAT TRACK FWD GALLEY HAS CORROSION. REMOVED AND REPLACED SEAT TRACK PER SRM 51-42-11; CORR TASK JA-220-5350 0; CORR LEVEL 2, DEFECT SIZE: 4 X 2 INCHES. 2 L 7 2 4F RT A28NM 2007011900026 20070119 00026 CE 2007 1 19 DXTA200701847 1 20070110 A 3220 315381 WHEEL CESSNA 750 750 2076810 CE NLG OUT OF BALANCE E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 950QS 193 193 7500050 WHILE ACCELERATING THROUGH 50 KTS DURING TAKEOFF ROLL, EXPERIENCED AN EXTREME NOSE WHEEL SHIMMY, WHICH CAUSED THE AIRCRA FT TO SHAKE AND VIBRATE HARSALLY, TAKEOFF WAS ABORTED.REMOVED LT NOSE WHEEL P/N 3-1538-1; S/N 0513/0513 AND INSTALLED OV H P/N 3-1538-1; S/N 0428/0428 ON LT AXLE. REMOVED RT NOSE WHEEL P/N 3-1538-1, S/N 1028/1028 AND INSTALLED OVH P/N 3-1538 -1 S/N 0514/0514 ON RT AXLE. INFLATED NOSE TIRES TO 140 PSI. WORK DONE IAW CESSNA CITATION 750AMM SECTION 32-41-01. LEAK CHECK SATISFACTORY. 2 L 7 2 4J RT T00007WI 2007011900028 20070119 00028 NM 2007 1 19 DXTA200701850 1 20070111 A 2612 7101771050730 FIRE LOOP GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE RT ENGINE FAILED E DXTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 724QS 1992 100 RT ENG FIRE DETECT CAS MSG ILLUMINATED RT AFTER ENGINE START. REPLACED RIGHT ENGINE ZONE 2 DETECTOR & FIRE LOOP CMP 261 102 W/O REF FL008823 2 L 7 2 4F 4 F RT A53NM E35NE 2007011900029 20070119 00029 CE 2007 1 19 DXTA200701851 1 20070111 A 3240 AC65216 MAXARET RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7314R 01518 WP LT MLG INOPERATIVE E DXTA O OTHER E VIBRATION/BUFFET LD LANDING 1 GL 07 805QS 968 968 258505 WHEN BRAKING, NOTHING HAPPENS UNTIL PRESSURE GAUGE READS 200PSI THEN BRAKES GRAB HARD. THIRD WRITEUP. RECEIVED OH MAXAR ET P/N AC65216 S/N 58268 & NEW MAXARET P/N AC65218 THROUGH NJA SUPPLY. REMOVED AND REPLACED EXISTING MAXARET NR 1 P/N AC 65218 S/N 022CJ, NR 2 AC65216 P/N S/N GX189. INSTALLED MAXARET S/N 58268 ON NR 1 AND S/N 58268 ON NR 2. PERFORMED OP CHE CK OF BRAKE SYSTEM. OPS CHECK WAS GOOD. ALL WORK ACCOMPLISHED IAW H-800XP MM CH 32-40-101 2 L 7 2 4F 4 F RT A3EU E6WE 2007011900030 20070119 00030 CE 2007 1 19 DXTA200701852 1 20070112 A 2910 67177706 LINE CESSNA 750 750 2076810 CE HYD SYSTEM LEAKING E DXTA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 07 936QS 8375 7500036 DURING CRUISE FLIGHT AMBER CAS MESSAGE HYD A VOL LOW APPEARED.QUANTITY WAS 16% AND FALLING CREW ACCOMPLISHED CHECKLIST A ND LANDED. FOUND LEFT T/R PRESSURE LINE IN AFT EQUIPMENT BY LEAKING. REMOVED AND REPLACED LINE WITH A NEW LINE ASSEMBLY. PERFORMED LEAK CHECKS OF HYD LINE & SERVICED HYD SYSTEM AND CYCLES LEFT T/R SEVERAL TIMES, NO DEFECTS NOTED. ALL WORK W AS DONE IAW CESSNA CITATION 750 M/M 20-10-01 AND 29-00-00. 2 L 7 2 4J RT T00007WI 2007011900037 20070119 00037 NM 2007 1 19 07FDEA00088 1 20070112 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 SEAT TRACK AT MAIN DECK CARGO AT STA 495-515 X=27.5 RT FOUND EDGE BROKEN OFF. REPAIR CARIED OUT AT MAIN DECK CARGO SEAT TRACK (STA 495-515 X=27.5 RT) AS PER SRM 53-70- 00 FIGURE 4 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007011900038 20070119 00038 NM 2007 1 19 07FDEA00089 1 20070114 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 COMPLIED WITH EA 7-5310-102014 FUSELAGE-BASIC-BS 870 FLOORBEAM UPPER CAP CORROSION, RBL 51-57. 2 L 7 3 4F RT A3WE 2007011900039 20070119 00039 2007 1 19 07FDEA00090 4 20070112 A 3442 TRANSCEIVER BOEING 727 727233 138408A NM WX RADAR SYSTEM FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 25 271FE 22036 WEATHER RADAR INDICATOR DISPLAYS "FAIL" WITH "T/R". DISPLAYED IN GREEN-YELLOW-RED UNDER THE WORD "TEST". REMOVED AND R EPLACED WEATHER RADAR R/T REF B727-200 AMM 34-41-041-4. WEATHER RADAR SYSTEM TESTS OK NOW REF B727-200 AMM 34-41-000-5. PREMATURE REMOVAL/INSTALLATION OFF MFG 622-5132-101 SRL 2112 ON MFG 622-5132-109, SRL 9841. 2 L 7 3 4F RT A3WE 2007011900040 20070119 00040 NM 2007 1 19 07FDEA00091 1 20070115 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 740 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 AT FS 740 RBL 70, TEE CAP AND FITTING AT LIGHTENING HOLE HAS BEEN GROUND ON, NOT TREATED OR PRIMED, AREA HAS CORROSION O N BOTH PARTS. REMOVED CORROSION REF SRM 51-10-1 PAGES 14-16, ROTO PEENED REF SOPM 20-10-03 PG 19. ALODINED AND PRIMED AREA REF EA IO 70053 PG 2. APPLIED ONE COAT LPS REF EA IO 70053 REV IR. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007011900041 20070119 00041 NM 2007 1 19 07FDEA00092 1 20070113 A 2100 UNKNOWN BOEING 727 727225 1384077 NM UNKNOWN A FDEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 25 463FE 22551 AFTER APPLICATION OF STANDARD TAKEOFF POWER AT APPROXIMATELY 60KTS A LOUD HIGH PITCH WHINE ACCOMPANIED WITH SOUND OF RUS HING AIR WAS HEARD. TAKEOFF WAS REJECTED AT 80KTS. CHECKED CARGO AND ENTRY DOOR SEALS FOR DAMAGE, NONE FOUND. PRESSUR IZED AC IAW JRH CHAP 8. NO ABNORMAL LOUD NOISE HEARD. RAN NR 1 ENG IAW JRH, FOUND BLEED SYSTEM TO FUNCTION NORMALLY. AIRCRAFT OK FOR SERVICE. 2 L 7 3 4F A3WE 2007011900042 20070119 00042 EA 2007 1 19 VNAA0701002 1 20070110 A 3297 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF343B1 NE MLG LOOSE A VNAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 05 256PS 7937 CREW REPORTED A GEAR DISAGREE WARNING MESSAGE ON APPROACH. CREW ABORTED THE APPROACH, FOLLOWED THE QRH AND LANDED WITHOU T INCIDENT. MAINTENANCE INSPECTED AND FOUND A LOOSE CONNECTOR TO THE MAIN LANDING GEAR SELECTOR VALVE. MAINTENANCE REINS TALLED THE CONNECTOR. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007011900046 20070119 00046 SO 2007 1 19 C2XA07BT004 1 20070112 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13949 145057 BTV DURING ROUTINE/SERVICE CHECK FOUND EMERGENCY EXIT LIGHT ON CEILING AT 1A INOP. ALSO EMERGENCY EXIT LIGHT ON COCKPIT STEP INOP. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007011900047 20070119 00047 SO 2007 1 19 C2XA07IA014 1 20070108 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14180 14500900 IAH - FLIGHT 2667, DURING PREFLIGHT INSPECTION THE PAX CABIN OVERHEAD CENTER FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO B E INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DE FECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007011900048 20070119 00048 EA 2007 1 19 COMA0760016 1 20070109 A 3020 5399001 VALVE CNDAIR CL600 CL6002B19 1900309 EA LT NACELLE FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 588SW 2088 7069 FLIGHT 5199 - LEFT COWL ANTI-ICE CAUTION MESSAGE CAME ON EN ROUTE TO CVG. LANDED JFK WITHOUT INCIDENT. REMOVED AND REP LACED LEFT COWL ANTI-ICE VALVE AND COWL ANTI-ICE PRESSURE SWITCH. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007011900049 20070119 00049 EA 2007 1 19 COMA0770003 1 20070104 A 5347 SH670RPA0045 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 354CA 10064 NUMEROUS FLOOR AND SIDE SEAT TRACKS ARE CORRODED. BLENDED WITHIN LIMIT SEAT TRACKS IAW REO 670-53-00-013, AND REPLACED 2 EA OUT OF LIMIT TRACKS IAW SRM 53-41-51. 2 L 7 2 4F RT A21EA 2007011900050 20070119 00050 NM 2007 1 19 WRLA2007004 1 20070108 A 5712 RIB DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE LT WING CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 41081 48632 DURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND LEFT WING L/E RIB CRACKED AT FRONT SPAR APPROXIMATELY AT XORS840. REPAIRE DTHE DAMAGED AREA PER MD-11F SRM VOL1 57-00-01 FIG 10 REV 38. CONDITION CHECK NORMAL. EGAT NRC NO U05067. 2 L 7 3 4F 4 F RT A22WE E24NE 2007011900052 20070119 00052 EA 2007 1 19 COMA0760019 1 20070110 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 915CA 7013 FLIGHT 5411 - EN ROUTE BGR-BOS RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREE FLAP SETTING. CREW DECLARED AN EMERG ENCY AND FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACT ION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007011900053 20070119 00053 NM 2007 1 19 NOCA01107 1 20070112 A 7830 07482933M88P08 DRIVE ASSY BOEING 767 76739H 1385311 NM THRUST REVERSER CRACKED A NOCA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 760NA 26257 LEFT REV ISOLATION VALVE EICAS CAME ON AT LANDING WITH LEFT ENGINE REVERSER YELLOW STAYING ON. STATUS MESSAGE LT REVERS ER ISOLATION VALVE & LT REVERSER INTERLOCK WAS ALSO DISPLAYED. VISUAL INSP SHOWS INBOARD REVERSER SHELL FULLY OPEN, FOU ND CENTER DRIVE & FWD BACK HOUSING CRACKED. REMOVED AND REPLACED CENTER DRIVE IAW MM 78-31-21. 2 L 7 2 4F RT A1NM 2007011900054 20070119 00054 2007 1 19 NOCA00907 4 20070108 A 3431 8221152002 RECEIVER BOEING 757 75728A 1384976 NM MALFUNCTIONED A NOCA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 755NA 30043 GLIDESLOPE AND LOC WARNING FLAGS ON CAPTS EADI, GROUND PROXIMITY EICAS ILLUMINATED ON TAXI IN AFTER LANDING. REMOVED AN D REPLACED MMR PER MM 34-31-01, OPS CHECK OK. 2 L 7 2 4F RT A2NM 2007011900055 20070119 00055 NM 2007 1 19 NOCA01007 1 20070114 A 2560 S417N5091 LIGHT BOEING 757 75728A 1384976 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 754NA 29381 EMERGENCY PATH LIGHTING ON FLOOR BY DOOR 3L IS INOP. REMOVED AND REPLACED LIGHT ASSY PER MM 25-60. 2 L 7 2 4F RT A2NM 2007011900056 20070119 00056 2007 1 19 NOCA01207 4 20070115 A 3420 INDICATOR BOEING 757 75728A 1384976 NM ATTITUDE MALFUNCTIONED A NOCA O OTHER I FLT. ATTITUDE INST. CR CRUISE 1 EA 15 750NA 26277 STANDBY ATTITUDE INDICATOR HELD 5 DEG TURN AFTER A/C WAS ROLLED. OPS CHECK STANDBY ATTITUDE INDICATOR PER MM 34-24-00, NO FAULTS FOUND. 2 L 7 2 4F RT A2NM 2007011900057 20070119 00057 NM 2007 1 19 NOCA01307 1 20070117 A 3350 20131A BATTERY BOEING 767 767324 1385203 NM EMERGENCY LIGHT INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 767NA 27569 EMERGENCY E-PATH LIGHTS INOP 1GH 10GH. REMOVED AND REPLACED CHARGER ASSY AND BATTERY OPS CHECK NORMAL PER MM 33-51-07, BATTERY CHARGER P/N 2012-1, S/N 13433. 2 L 7 2 4F RT A1NM 2007011900058 20070119 00058 NM 2007 1 19 NOCA01407 1 20070116 A 2612 710107 FIRE LOOP BOEING 767 767306 1385148 NM RT NACELLE DAMAGED A NOCA K NONE N FALSE WARNING IN INSP/MAINT 1 EA 15 765NA 28098 RIGHT ENG FIRE LOOP STATUS MSG. REMOVED AND REPLACED LOWER FWD FIRE WARNING ELEMENT PEM MM 26-11-01, OPS CHECK OK. 2 L 7 2 4F RT A1NM 2007011900059 20070119 00059 NM 2007 1 19 NOCA00507 1 20070105 A 2760 3312148014 ACTUATOR BOEING 757 75728A 1384976 NM GROUND SPOILERS MALFUNCTIONED A NOCA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 15 754NA 29381 GROUND SPOILER INOP. REMOVED AND REPLACED NR 7 PCA IAW MM 27-61-02, OPS CHECK NORMAL. 2 L 7 2 4F RT A2NM 2007011900060 20070119 00060 NM 2007 1 19 HNAA0600221 1 20070112 A 3320 40481 CARRIER ASSY DHAV DHC8 DHC8102 2809003 NM LIGHT SOCKET BURNED A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 815EX 37105 37105 321 ELECTICAL BURNING ODOR AT ROW 9 LEFT SIDE, CREW FOUND SIDEWALL LIGHT SOCKET BURNED. REPLACED LAMP CARRIER. 2 H 7 2 4T RT A13NM 2007011900061 20070119 00061 NM 2007 1 19 HNAA0700227 1 20070105 A 5347 85320490135 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 182-229 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 982HA 32746 32746 380 CORROSION ON RIGHT INBOARD SEAT TRACK AT X201.00. REPLACED SEAT RAIL. 2 H 7 2 4T RT A13NM 2007011900063 20070119 00063 NM 2007 1 19 HNAA0600219 1 20070112 A 2120 UNKNOWN DHAV DHC8 DHC8102 2809003 NM CABIN ODOR A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 912HA 040 ELECTRICAL BURNING ODOR LT CABIN BETWEEN ROWS 1 AND 2. AFTER SELECTING OVERHEAD LIGHTS OFF ODOR DISSIPATED, ISSUED MEL. MORE TO FOLLOW. 2 H 7 2 4T RT A13NM 2007011900064 20070119 00064 NM 2007 1 19 ASAA0741393 1 20070116 A 5753 6546430517 SKIN BOEING 737 7374Q8 138447Q NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 THE LEFT WING TRAILING EDGE I/B FORE FLAP LWR SURFACE HAS AN EXISTING REPAIR WITH MULTIPLE DENTS AND DINGS AT WBL 119. REMOVED THE EXISTING REPAIR DOUBLER AND DAMAGED AREA OF LWR SKIN FABRICATED AND INSTALLED A SKIN FILLER AND A REPAIR DOU BLER IAW SRM 51-70-10 PARA 7, 8, 11, 15, 18 AND 20. 2 L 7 2 4F RT A16WE 2007011900065 20070119 00065 NM 2007 1 19 ASAA0741394 1 20070116 A 5315 65C339503 FLOORBEAM BOEING 737 7374Q8 138447Q NM BS 986 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 PASSENGER CABIN FLOORBEAM CORRODED OUT OF LIMITS. REMOVED THE DAMAGED AREA OF THE BEAM UPPER HORIZONTAL FLANGE, FABRICA TED AND INSTALLED A REPAIR T-CHORD SECTION 2 SPLICE ANGLES 2 SPLICE STRAPS AND FILLERS IAW ASA EA 5310 02690 AND AAR EA 11805. 2 L 7 2 4F RT A16WE 2007011900066 20070119 00066 NM 2007 1 19 ASAA0741395 1 20070116 A 5753 6546430518 SKIN BOEING 737 7374Q8 138447Q NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 THE RIGHT WING TRAILING EDGE I/B FORE FLAP LWR SURFACE HAS MULTIPLE DENTS AND DINGS FROM WBL 101.5 - 121.5. REMOVED THE DAMAGED AREA OF LOWER SKIN, FABRICATED AND INSTALLED A SKIN FILLER AND REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 11, 1 5, 18 AND 20. 2 L 7 2 4F RT A16WE 2007011900067 20070119 00067 NM 2007 1 19 ASAA0741396 1 20070116 A 5753 6546430517 SKIN BOEING 737 7374Q8 138447Q NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 THE LEFT WING TRAILING EDGE I/B FORE FLAP LWR SURFACE IS DINGED AT WBL 126. REMOVED THE DAMAGED AREA OF LWR SKIN, FABRI CATED AND INSTALLED A SKIN FILLER AND A REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 11, 15, 18 AND 20. 2 L 7 2 4F RT A16WE 2007012200001 20070122 00001 NM 2007 1 22 USAA070043 1 20070117 A 5311 FRAME BOEING 737 737401 1384701 NM BS 492 S21R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 BS 492 S-21R, FWD CARGO DOOR CUTOUT, AFT FRAME AT INNER STOP HOLE. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-0 0-02, EO 5305V113, DEFECT SIZE: .250 INCH. 2 L 7 2 4F RT A16WE 2007012200003 20070122 00003 EU 2007 1 22 USAA070041 1 20070117 A 5320 BEAM AIRBUS A321 A321211 3930370 EU DOOR SEAL CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 168US 1447 DOOR SEAL BEAM Y1290 & 5 INCHES FWD OF FR 68 CORRODED. CUT OUT DAMAGED AREA, INSTALLED FILLER & DOUBLER PER SRM 53-41-1 4; CORR TASK JA-260-53500, LEVEL 1, DEFECT SIZE: .5 X .625 INCH. 2 L 7 2 4F RT A28NM 2007012200004 20070122 00004 NM 2007 1 22 USAA070040 1 20070117 A 5522 65C25746131A SKIN BOEING 737 737301 1384611 NM LT ELEVATOR PEELING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 23742 PEELING FABRIC LEFT ELEV AT MOUNT FLANGE OF LEADING EDGE ACCESS PANEL 9143L. REMOVED DAMAGE, INSTALLED FILLER PLIES PER SRM 51-70-17 & EA 98399, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007012200006 20070122 00006 NM 2007 1 22 USAA070044 1 20070117 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM BS 328-344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 AT SCREW HOLES, STA 328-344, RBL 11.5 HAS CORROSION. FAB'D NEW PART & INSTALLED; CORR TASK C53-107-02; LEVEL 2, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007012200008 20070122 00008 NM 2007 1 22 HNAA0700229 1 20070105 A 5340 UNKNOWN BRACKET DHAV DHC8 DHC8102 2809003 NM ZONE 100 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 982HA 32746 32746 380 CORROSION FOUND ON BRACKET AND CARGO FLOOR AT X598 ZONE 144 NEAR ENTRANCE AFT. CORROSION ON CARGO FLOOR REMOVED AND BRA CKET REPLACED. 2 H 7 2 4T RT A13NM 2007012200009 20070122 00009 NM 2007 1 22 ASAA0741401 1 20070117 A 5347 655548425 CARGO TRACK BOEING 737 737490 1384715 NM BS 480 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 713AS 30161 FWD CARGO PIT TIE DOWN TRACK CORRODED. REPAIRED WITH REPAIR PART PER SRM 53-00-53. 2 L 7 2 4F RT A16WE 2007012200012 20070122 00012 NM 2007 1 22 HNAA0600220 1 20070112 A 2120 UNKNOWN DHAV DHC8 DHC8102 2809003 NM CABIN ODOR A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 815EX 321 F/A REPORTS BURNING ODOR FROM GALLEY OVERHEAD GASPER VENT. INSPECTED ASSOCIATED AREA NO HIDDEN DAMAGE NOTED, RAN APU WI TH BLEEDS ON AND ALL LIGHTS ON, NO DEFECTS NOTED AT THIS TIME. 2 H 7 2 4T RT A13NM 2007012200013 20070122 00013 EA 2007 1 22 COMA0760023 1 20070112 A 5210 601R386493 PUSHROD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 783CA 7315 FLIGHT 4979 - CABIN WOULD NOT PRESSURIZE DURING CLIMB. STOPPED CLIMB AT 10,000 FT RECEIVED EXHAUST STATUS MESSAGE AND D ISPLAY COOL CAUTION MESSAGE. FOLLOWED QRH, DIVERTED TO BUF AND LANDED WITHOUT INCIDENT. FERRIED TO JFK, REPLACED PAX D OOR FLAPPER DOOR ROD. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007012200014 20070122 00014 EA 2007 1 22 COMA0760024 1 20070112 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 7013 FUSELAGE SKIN CHAFED BY PYLON SEAL RIGHT SIDE. REPAIRED IAW REO 601R-53-61-268. 2 L 7 2 4F RT A21EA 2007012200015 20070122 00015 NM 2007 1 22 SWAA070227 1 20070117 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 431WN 29845 EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007012200016 20070122 00016 NM 2007 1 22 SWAA070240 1 20070117 A 3350 D31354 SLIDE BOEING 737 7373A4 1384585 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007012200017 20070122 00017 NM 2007 1 22 SWAA070241 1 20070117 A 3350 D31354 SLIDE BOEING 737 7373A4 1384585 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007012200019 20070122 00019 NM 2007 1 22 SWAA070243 1 20070117 A 5753 65522112 TORQUE TUBE BOEING 737 7373T5 1384608 NM LT WING TE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND LT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE T UBE PER MM. 2 L 7 2 4F RT A16WE 2007012200022 20070122 00022 NM 2007 1 22 SWAA070246 1 20070117 A 3350 810022607 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP LOOSE AT ROW 6 DEF. SECURED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 2007012200023 20070122 00023 NM 2007 1 22 SWAA070225 1 20070117 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2007012200024 20070122 00024 2007 1 22 SWAA070226 4 20070117 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 430WN 33659 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007012200027 20070122 00027 EA 2007 1 22 COMA0760011 1 20070107 A 3231 TORQUE LINK CNDAIR CL600 CL6002B19 1900309 EA NLG DOOR DISCONNECTED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 926CA 7027 FLIGHT 5086 - ON T/O FROM CLT UPON GEAR RETRACTION RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGE. A/C RETUR NED BACK TO CLT AND LANDED SAFELY. INSPECTED A/C AND FOUND NOSE TORQUE LINK DISCONNECTED, RECONNECTED TORQUE LINK. NO FURTHER DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007012200028 20070122 00028 EA 2007 1 22 COMA0760014 1 20070108 A 3020 22856480109 RELIEF VALVE CNDAIR CL600 CL6002B19 1900309 EA LEFT ENGINE FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 496CA 7791 FLIGHT 5478 - LEFT ENGINE COWL ANTI-ICE CAUTION MESSAGE IN FLIGHT. AIRCRAFT DIVERTED TO YYZ AND LANDED SAFELY. REMOVED AND REPLACED LEFT ENGINE COWL ANTI-ICE RELIEF VALVE. 2 L 7 2 4F RT A21EA 2007012200030 20070122 00030 EA 2007 1 22 COMA0760007 1 20070104 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 487CA 7729 FLIGHT 5604 - FLAPS FAILED AT 20 DEGREES AT GATE. COMPLIED WITH AD 2006-12-21, FLAP CAUTION MESSAGE FIRST EVENT MAINTEN ANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2007012200032 20070122 00032 EA 2007 1 22 COMA0760009 1 20070105 A 3231 SPRING CNDAIR CL600 CL6002B19 1900309 EA NLG DOOR LACK OF LUBE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 973CA 7146 FLIGHT 5576 - DURING CLIMBOUT OF CVG RECEIVED A NOSE GEAR DOOR WARNING, FLIGHT RETURNED TO THE FIELD. LUBRICATED THE NL G DOOR SPRING BUNGEE ASSEMBLY AND RE-RIGGED THE NOSE DOOR ACTUATOR. 2 L 7 2 4F RT A21EA 2007012200033 20070122 00033 EA 2007 1 22 COMA0760010 1 20070106 A 7830 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER FALSE ACTIVATION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 941CA 7050 FLIGHT 5662 - DURING CLIMB THRU APPROX FL 180 LEFT REV UNLOCK MESSAGE CAME ON. FOLLOWED QRH AND RETURNED BACK TO PHF AN D LANDED SAFELY. INSPECTED LEFT T/R AND STOW, DEPLOY AND THROTTLE LOCKOUT SWITCHES. ALL CHECKED GOOD. OPS CHECKED T/R , OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007012200034 20070122 00034 EA 2007 1 22 COMA0760015 1 20070108 A 3040 601R515185 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA WINDSHILD WIPERS FAULTY A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 510CA 7802 FLIGHT 4952 - DURING CLIMBOUT OF RIC THE CAPTAIN'S WINDSHIELD WIPER ACTIVATED UNCOMMANDED, FLIGHT RETURNED TO THE FIELD. REPLACED THE WIPER/STALL CONTROL PANEL. 2 L 7 2 4F RT A21EA 2007012200035 20070122 00035 EA 2007 1 22 COMA0760018 1 20070110 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 931CA 7037 FLIGHT 5072 - FLAP FAIL AT 4000 FT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION P ARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007012200038 20070122 00038 EA 2007 1 22 VNAA0701005 1 20070114 A 2420 O-RING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 IDG CRACKED A VNAA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 GL 05 257PS 7939 CREW REPORTED THE NR 2 GENERATOR FAILED ON TAKEOFF ROLL. CREW ABORTED TAKEFOFF AND RETURNED TO GATE. MAINTENANCE INSPE CTED THE NR 2 IDG AND FOUND CRACKED O-RINGS AND OIL LEAKING FROM THE STANDPIPE OVERFILL. MAINTENANCE REPLACED DAMAGED O -RINGS AND SERVICED THE OIL LEVEL IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE . 2 L 7 2 4F 4 F RT A21EA E15NE 2007012200039 20070122 00039 EA 2007 1 22 COMA0760013 1 20070108 A 2620 365000183 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIP BAY FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 819CA 22572 7415 FLIGHT 5025 - DURING CRUISE AT FL 290, CARGO BOTTLE LOW CAUTION MESSAGE. REMOVED AND REPLACED CARGO BOTTLE. 2 L 7 2 4F RT A21EA 2007012200040 20070122 00040 SO 2007 1 22 C2XA07CL006 1 20070115 A 5210 14531589401 SUPPORT EMB 145 EMB145XR 3260214 SO PAX DOOR OUT OF ADJUST A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 27190 14500934 CLE FLIGHT 2327 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO CLOSE WITH LARGE GAP AT THE TOP OF THE DOOR. MAI NTENANCE INSPECTED AND ADJUSTED THE UPPER AFT MAIN CABIN DOOR ROLLER SUPPORT. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2007012200042 20070122 00042 EA 2007 1 22 COMA076027 1 20070114 A 3097 WIRE CNDAIR CL600 CL6002B19 1900309 EA THERMIAL SWITCH FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 965CA 7131 FLIGHT 5342 - RECEIVED ANTI-ICE DUCT WARNING MESSAGE IN FLIGHT. FOLLOWED QRH AND DIVERTED TO GSO. FLIGHT LANDED WITHOU T INCIDENT. REPLACED THERMAL SWITCH WIRE AT LEFT WING STATION 250. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007012200043 20070122 00043 EA 2007 1 22 COMA0760028 1 20070115 A 5610 NP1393211 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 969CA 26421 7141 FLIGHT 9467 - LEFT WINDSHIELD SHATTERED FOLLOWED BY LEFT WINDSHIELD HEAT MESSAGE. REPLACED LEFT WINDSHIELD. 2 L 7 2 4F RT A21EA 2007012200044 20070122 00044 SO 2007 1 22 C2XA07CL005 1 20070112 A 5210 14525311403 SEAL EMB 145 EMB145XR 3260214 SO MAIN DOOR FAULTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 21129 145703 CLE FLIGHT 2451 THE CREW REPORTED UPON ARRIVAL IN MKE THE F/A WAS UNABLE TO OPEN THE MAIN CABIN DOOR. MAINTENANCE INSPE CTED AND REPLACED THE MAIN CABIN DOOR SEAL. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT 2007012200046 20070122 00046 EA 2007 1 22 COMA0760017 1 20070109 A 3097 WIRE CNDAIR CL600 CL6002B19 1900309 EA CONTROL SENSOR BROKEN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 455CA 7562 FLIGHT 5217 - INTERMITTENT ANTI-ICE WARNING MESSAGE DURING CLIMB WITH WINGS AND COWLS ON, RIGHT WING RED ON SYNOPTIC PAG E. DIVERTED BACK TO CVG, LANDED WITHOUT INCIDENT. REPAIRED BROKEN WIRE FOUND AT RIGHT WING CONTROL SENSOR (1RT1HA). N O FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007012200050 20070122 00050 NM 2007 1 22 HNAA0700225 1 20070105 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 982HA 380 CORROSION ON FORWARD LEFT SEAT RAIL. REMOVED CORROSION AND RETREATED RAIL. 2 H 7 2 4T RT A13NM 2007012200054 20070122 00054 NM 2007 1 22 KCSA071026 1 20070116 A 5411 SPAR BOEING 747 747209F 1384800 NM NR 1 NACELLE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 NR 1 PYLON MID SPAR WEB CRACKED BY REAR ENGINE MOUNT, NAC STA 221.9, WL 138.5. 2 L 7 4 4F RT A20WE 2007012200056 20070122 00056 NM 2007 1 22 KCSA071029 1 20070116 A 5320 SUPPORT BOEING 747 747209F 1384800 NM BS 2775 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 APU AFT MOUNT HORIZONTAL SUPPORT HAS CRACKED AND ELONGATED HOLE AT MOUNT FORWARD BOLT HOLES, BS 2775, LBL 3. 2 L 7 4 4F RT A20WE 2007012200057 20070122 00057 NM 2007 1 22 KCSA071030 1 20070116 A 5311 FRAME BOEING 747 747209F 1384800 NM BS 2360 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 CORROSION ON BS 2360 BULKHEAD LOWER FORWARD FRAME AT STR 38L. 2 L 7 4 4F RT A20WE 2007012200058 20070122 00058 NM 2007 1 22 KCSA071031 1 20070116 A 5311 FRAME BOEING 747 747209F 1384800 NM BS 2360 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 CORROSION ON BS 2360 BULKHEAD FORWARD LOWER FRAME AT STR 36R. 2 L 7 4 4F RT A20WE 2007012200059 20070122 00059 NM 2007 1 22 KCSA071032 1 20070116 A 5311 FRAME BOEING 747 747209F 1384800 NM BS 2360 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 CORROSION ON BS 2360 BULKHEAD FORWARD LOWER FRAME AT STR 48R. 2 L 7 4 4F RT A20WE 2007012200060 20070122 00060 NM 2007 1 22 WRLA2007010 1 20070111 A 2810 RIVET DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUEL TANK CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 41081 48632 DURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND MAIN DECK CGO CENTER WING TANK UPPER STRUCTURE SEVERAL RIVETS HAVE CORROSI ON AT STA Y=1366, X=30 TO X=75. BLEND OUT CORRODED AREA AND MEASURE REMAIN SKIN THICKNESS STILL WITHIN ALLOWABLE DAMAGE LIMITATION PER MD-11F SRM VOL.1 57-20-00 FIG.12 REV.38. CONDITION CHECK NORMAL. 2 L 7 3 4F 4 F RT A22WE E24NE 2007012200071 20070122 00071 NM 2007 1 22 WRLA2007003 1 20070108 A 2530 831620405 OVEN DOUG MD11 MD11 3023602 NM PWA 4060 PW4060 52119 NE GALLEY SMOKE A WRLA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 801DE 59858 48472 MID GALLEY OVEN NR 2 STOPPED WORKING, C/B PULLED. ELECTRICAL SMOKE WAS SENSED ON LEFT SIDE OF VENT, NO SMOKE WAS EVIDEN T ALTHOUGH SMELL WAS NOTICEABLE. OPS CHECKED MID OVENS, NO SIGN OF ELECTRICAL SMOKE OR ODOR. COOKED WITH MID GALLEY OV ENS FOR MEAL SERVICE, OPS CHECK GOOD. 2 L 7 3 4F 4 F RT A22WE E24NE 2007012200072 20070122 00072 NM 2007 1 22 WRLA2007012 1 20070108 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE BS 630-670 CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 41081 48632 DURING 2C+12A+150M CHECK, EGAT MAINT FOUND CORROSION AT STA 630 - STA 670 LONGERON L51. CUT & FABRICATE REPAIR THE DAMA GED AREA PER MD-11F SRM 53-10-00 REV.38 FIG.1 & FIG.2. CONDITION CHECK NORMAL. 2 L 7 3 4F 4 F RT A22WE E24NE 2007012200074 20070122 00074 NM 2007 1 22 HNAA0700226 1 20070105 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM BS 201 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 982HA 380 CORROSION FOUND ON FRAME UNDERFLOOR AT X201.1560 BETWEEN STR 32S AND 30S. REPAIRED FRAME IAW ENGINEERING ORDER. 2 H 7 2 4T RT A13NM 2007012200081 20070122 00081 SO 2007 1 22 C2XA07TY001 1 20070115 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 15986 145254 BNA - STRONG ODOR IN COCKPIT AT CRUISE. FOUND FORWARD ELECTRICAL COMPARTMENT FAN INOP IAW MEL 21-26-00, CATAGORY C, CON TROL 113884. VERIFIED NORMAL OPERATION OF ELECTRONIC COMPARTMENT VENTALATION SYSTEM. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007012200082 20070122 00082 SO 2007 1 22 C2XA07BT003 1 20070108 A 2697 WIRE EMB 145 EMB145XR 3260214 SO SMOKE DETECTION DAMAGED A C2XA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 17159 145792 EWR LOG SQUAWK LAV SMOKE WARNING INTERMITTENT ON SHORT FINAL AND TAXI. REPAIRED WIRE W102-8012-22 IAW EMB145 MM 20-21-0 0. OPS CHECK GOOD IAW EMB145 MM 26-14-00 AND MM 26-14-50. 2 L 7 2 4F RT 2007012200083 20070122 00083 SO 2007 1 22 C2XA07IA013 1 20070112 A 3230 355022002MOD CONTROL UNIT EMB 145 EMB145LR 3260212 SO MLG DEFECTIVE A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 12564 329 329 145618 IAH - FLIGHT 2197, THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL WITH A LOCKED SELECTOR LEVER AFTER TAKEOFF FROM MCI. THE MESSAGE CLEARED ITSELF, AND THE CREW WAS ABLE TO RETRACT THE LANDING GEAR AND CONTINUE TO IAH WHERE THE AIRCRAFT LAN DED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LGEU (LANDING GEAR ELECTRONICS UNIT), OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007012200084 20070122 00084 SO 2007 1 22 C2XA07IA012 1 20070111 A 3260 INDICATION SYS EMB 135 EMB135LR 3260305 SO MLG MALFUNCTIONED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 15527 145413 IAH - FLIGHT 3109, THE CREW REPORTED AFTER T/O THE GEAR STARTED TO RETRACT, GOT AMBER THEN RED INDICATIONS WITH LANDING GEAR LEVER DISAGREE MESSAGE. THE GEAR STOWED AT 1300 FT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT . MAINTENANCE INSPECTED THE AIRCRAFT OPERATIONALLY CHECKED THE EXTENSION & RETRACTION SYSTEMS WITH NO DEFECTS NOTED, AN D THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007012200086 20070122 00086 SO 2007 1 22 C2XA07RI003 1 20070116 A 2121 FAN EMB 145 EMB145XR 3260214 SO CONTAMINATED A C2XA O OTHER C B F.O.D. SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14105 145649 FLT 2279 - ORF - DURING CRUISE, CREW DETECTED SMOKE IN COCKPIT WHEN RECIRC FAN WAS ON. MX FOUND PIECE OF INSULATION ON FWD AVIONICS FAN. MX REMOVED INSULATION AND PERFORMED OPERATIONAL CHECK SUCCESFULLY. ACFT WAS APPROVED TO RETURN TO FL IGHT. 2 L 7 2 4F RT 2007012200087 20070122 00087 NM 2007 1 22 WRLA2007014 1 20070111 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 41081 48632 DURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND M/D CARGO FLOOR SEAT TRACK CORROSION AT Y=470, X=30. CLEANED UP CORROSION AREA PER MD-11F SRM VOL.II 51-21-01 REF 38. MEASURE REWORK DEPTH=0.009" STILL WITHIN ALLOWABLE LIMIT PER MD-11F SRM V OL.1 53-70-00 FIG.3. APPLY PROTECTIVE COATING, CONDITION CHK NORMAL AND JOB COMPLETED. 2 L 7 3 4F 4 F RT A22WE E24NE 2007012200088 20070122 00088 SO 2007 1 22 C2XA07SD001 1 20070111 A 3350 7287580509 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14991 145278 SDF - DISCREPANCY - EMERGENCY EXIT LIGHT INOP AT 12A. OPS CHECKED EMERGENCY LIGHTS FOUND EMERGENCY EXIT LIGHT AT 12A TO BE WORKING CORRECTLY IAW 33-50-00. 2 L 7 2 4T RT T00011AT 2007012200089 20070122 00089 SO 2007 1 22 C2XA07CL007 1 20070113 A 3411 ST3002PTH STATIC PORT EMB 145 EMB145LR 3260212 SO FUSELAGE INOPERATIVE A C2XA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 27 26549 145571 CLE FLIGHT 2061 THE CREW REPORTED A PITOT NR 2 INOPERATIVE MESSAGE ON THE ECIAS WITH A BURNING SMELL IN THE COCKPIT. TH E AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 STATIC PORT ASSEMB LY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007012200091 20070122 00091 NM 2007 1 22 SWAA070228 1 20070117 A 3350 417A5703 WIRE BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 793SA 27888 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP BETWEEN ROW 11 ABC AND ROW 16 ABC. FOUND LIGHT ASSY WIRE BROKEN AT ROW 15 ABC. REPAIRED WIRE PER MM. 2 L 7 2 4F RT A16WE 2007012200092 20070122 00092 NM 2007 1 22 SWAA070229 1 20070117 A 5340 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 767 S27L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007011700073 20070117 00073 NM 2007 1 17 F3LA200600167 1 20070109 A 5210 LEVER AIRBUS A319 A319111 3930336 NM R1 DOOR BINDING A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 917FR 5893 1890 DURING C-3 CHECK, INSPECTION REPORTED THE R-1 DOOR ARMED LEVER WOULD NOT MOVE TO ARMED POSITION. REMOVED EXCESS LUBRICA NT AND RETORQUED NUTS IAW AMM 52-11-22-820-001, STEP 4E(E). DOOR OPERATION NORMAL. 2 L 7 2 4F RT A28NM 2007011700088 20070117 00088 NM 2007 1 17 AALA20070055 1 20070103 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 919AN 29520 TUL - EMERGENCY LIGHT BATTERY PACK AT SEAT 13F FAILED OPERATIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK AT SEAT 1 3F. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007011700093 20070117 00093 NM 2007 1 17 QXEA200700023 1 20070106 A 5210 85217002003 DOOR BOMBDR DHC8 DHC8402 1390042 NM MAIN PAX STIFF A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX FLIGHT NR 2453: FLIGHT ATTENDANT REPORTS REAR PAX DOOR HARD TO OPEN AND CLOSE. MAINTENANCE REMOVED AND REPLACED AFT PAX DOOR IAW HORIZON EO 6-52-298. ALL TESTS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007011700111 20070117 00111 NM 2007 1 17 07FDEA00085 1 20070112 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 REWORK OF N/R N00850, REPAIR ACP'D WITH INCORRECT SRM REF. STR CLIP CRACKED IN RADIUS BS 680 STR 3L. REMOVED OLD STRIN GER CLIP, BACK DRILLED NEW STRINGER CLIP REF SRM 51-30-02. INSTALLED NEW STRINGER CLIP REF SRM 51-30-2 PG1-12. 2 L 7 3 4F RT A3WE 2007011700119 20070117 00119 SO 2007 1 17 SIMA200701504 1 20070111 A 2752 3633001023 ACTUATOR EMB 135 EMB135KL 3260302 SO TE FLAPS FAILED A SIMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 21 802AE 12640 145471 FALP FAIL MESSAGE WHEN FLAPS SELECTED TO 9 DEGREE POSITION, FLAPS REMAINED AT ZERO. REMOVED AND REPLACED NUMBER 1, 2, 3 AND 4 FLAP SCREW ACTUATORS 2 L 7 2 4F RT T00011AT 2007011700123 20070117 00123 NM 2007 1 17 NWAA70065513 1 20070106 A 5414 SKIN BOEING 757 757251 1384970 NM NR 2 NACELLE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 513US 23201 DURING "M" CHECK, FOUND CRACK IN NR 2 PYLON OUTBOARD SKIN AT NAC STA 144. REPAIRED PER EA 55-208680. 2 L 7 2 4F RT A2NM 2007011800001 20070118 00001 NM 2007 1 18 USAABB07005 1 20070112 A 3350 LIGHT BOEING 767 767201 1385125 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 245AY 23897 MAINTENANCE FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE IN ENVOY CLASS CABIN AREA. REPLACED FUSE IN BATTERY CHARGER. 2 L 7 2 4F RT A1NM 2007011800004 20070118 00004 NM 2007 1 18 SWAA070222 1 20070116 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 470WN 33860 DURING SCHEDULED HC2 CHECK, LT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007011800005 20070118 00005 NM 2007 1 18 SWAA070223 1 20070116 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 470WN 33860 DURING SCHEDULED HC2 CHECK, LEFT AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK P ER MM. 2 L 7 2 4F RT A16WE 2007011800007 20070118 00007 EU 2007 1 18 USAA070038 1 20070111 A 5315 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 168US 1447 TOPSIDE OF FLOORBEAM Y1732 AT FR 66 HAS CORROSION. ACCOMPLISHED REPAIR PER SRM 53-41-14; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 2 X 2 INCHES. 2 L 7 2 4F RT A28NM 2007011800021 20070118 00021 2007 1 18 SWAA070132 4 20070111 A 2565 D31354 SLIDE BOEING 737 7373T0 1384582 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED RON CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007011800022 20070118 00022 NM 2007 1 18 SWAA070133 1 20070111 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 416WN 32453 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007011800027 20070118 00027 2007 1 18 USAASA07004 4 20070111 A 2330 RDAV300702 VIDEO UNIT AIRBUS A319 A319112 3930323 EU CABIN SMOKE A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 746UW 19592 2724 1297 CLT FLT 1822, MIA TO CLT - DURING CRUISE, THE CABIN CREW NOTICED AN ELECTRICAL ODOR. THE PASSENGER ENTERTAINMENT AND VI DEO EQUIPMENT WERE SHUT DOWN, AS WELL AS POWER TO THE SEATS. THE ODOR WENT AWAY, BUT WAS NOTICED AGAIN DURING THE APPRO ACH TO CLT. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE VIDEO SYSTEM CONTROL UNIT. OK FOR SE RVICE. 2 L 7 2 4F RT A28NM 2007011800071 20070118 00071 NM 2007 1 18 USAASB07006 1 20070111 A 3350 20131ASMI BATTERY PACK BOEING 737 737401 1384701 NM EMERGENCY LIGHTS DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 23876 MCO - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT ROW 11 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PAC K. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007011800081 20070118 00081 NM 2007 1 18 SWAA070164 1 20070112 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 500D S19R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPV CHECK, FOUND STRINGER 19R CRACKED AT BS 500D. REPAIRED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007011800091 20070118 00091 2007 1 18 SWAA070160 4 20070112 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007011800112 20070118 00112 NM 2007 1 18 SWAA070188 1 20070113 A 5312 6936642 VERTICAL BEAM BOEING 737 7373H4 1384600 NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED SPV CHECK, FOUND BULKHEAD VERTICAL BEAM CHORD CRACKED AT BS 178, LBL 5.7, WL 184. REMOVED AND REPLACED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2007011800142 20070118 00142 NM 2007 1 18 2007UALA00048 1 20070106 A 3397 FEEDER CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 EEL LIGHTS INOP FROM ROW 15 TO GALLEY. REPLACED CABLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007011900002 20070119 00002 CE 2007 1 19 DXTA200701849 1 20070111 A 2910 AE1011889G0166 LINE CESSNA 750 750 2076810 CE HYDRAULIC SYS RUPTURED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 971QS 7141 7500071 AFTER GEAR RETRACTION RECIEVED A NOSE GEAR GREEN LIGHT AND GEAR UNSAFE LIGHT. THE FOLLOWING CAS MESSAGE WERE PRESENT, HYDRAULIC VOLUME LOW "A" HYDRAULIC PUMP FAIL "A" & HYDRAULIC PTU FAIL. "A" SIDE QUANTITY ZERO AND FLUID VISIBLE ON BOT H SIDES OF FUSELAGE. NOSE WHEEL STEERING HOSE REMOVED AND REPLACED IAW CESSNA CITATION 750 MAINTENANCE MANUAL CHAP 12-10 -15. BRAKE SYSTEM BLED IAW 750 MM CHAP 32-42-00 & HYDRALIC SYSTEM BLED IAW 750 MM 29-10-00. OPERATIONAL & LEAK CHECKS GO OD. 2 L 7 2 4J RT T00007WI 2007011900004 20070119 00004 CE 2007 1 19 DXTA200701848 1 20070110 A 2170 7464513 COALESCER BAG CESSNA 500 560CESSNA 2076750 CE AFT SERVICE BAY DIRTY E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 325QS 8263 5600425 SHARP IRRITATING ODOR/SMELL MAINLY IN COCKPIT, STRONGER RIGHT AFTER TAKE OFF REMAINED THROUGH WHOLE FLIGHT INCREASED AGA IN DURING DESCENT. RAN ENGINES FOR 30 MINUTES AT 70% FOUND NO ODOR. CHECK OIL LEVELS GOOD. NO SIGN OF EXTERNAL OIL LEAKS . CHECK ACM OIL LEVEL FULL. NO FLUID IN ACM EPA CAN EXAMINED ACM FOR OIL LEAKS NONE FOUND. CHECKED BLEED AIR LINE GOING TO ACM NO SIGNS OF OIL FOUND. REPLACED COLISER SOCK WITH NEW. RAN ENGINES AT 80% FOR 15 MINUTES NO ODOR NOTICED. ENGINE OIL LEVELS STAYED CONSTENT IAW CE560 MM 21-70-00, 71-00-00, 21-21-06 2 L 7 2 4F RT A22CE 2007011900005 20070119 00005 EU 2007 1 19 07FDEA00070 1 20070110 A 2910 TRANSMITTER AIRBUS 310 A310 EU HYD SYSTEM LEAKING A FDEA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 25 434FE 355 AT TOGA FOR TAKEOFF, LOST BLUE HYD SYSTEM. QTY WENT TO ZERO. REJECTED TAKEOFF,CLEARED RWY WORKED QRH. FOUND LEAK COMMING FROM BLUE SYSTEM PRESSURE TRANSMITTER AREA ON BLUE SYSTEM MODULE. LEAK IS OBVIOUS. R & R BLUE SYSTEM PRIORITY VALVE REF. A310-200 MM 29-12-12-4 AND SERVICE & OPS CHECKED REF. MM29-00-00-3. LEAK CHECKED GOOD AND OPS CHECKED NOR MAL. MOTORED NR 1 ENGINE REF. JRH AND OPS CHECKED FLIGHT CONTROLS. ALL CHECKED GOOD. 2 L 7 2 4F RT A35EU 2007011900006 20070119 00006 EU 2007 1 19 07FDEA00072 1 20070110 A 3260 UPLOCK AIRBUS 300 A300F4605R 3930327 EU NLG DOOR DAMAGED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 664FE 768 ON GEAR RETRACTION ECAM INDICATED GEAR DOOR FAULT WITH NOSE GEAR DOOR. REMOVED AND REPLACED RT NOSE GEAR DOOR UPLOCK ASSY PER A300 AMM 32-31-14-4. COMPLETED STEPS UP TO PAGE 407. COMPLETED RIGHT HAND NOSE DOOR UPLOCK INSTALLATION, AN D REINSTALLED NOSE DOORS PER MM 32-31-14-4,32-22-11-4 JACKED AIRCRAFT PER MOCC REQUEST, PER M/M 07-11-00-0 OPS CHECKS NORMAL 2 L 7 2 4F RT A35EU 2007011900007 20070119 00007 EA 2007 1 19 TRAX200700065 1 20070111 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 PAX DOOR 'EXIT' PLACARD WORN REMOVED AND REPLACED "EXIT" PLACARD IAW CRJ 700 AMM 11-20. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2007011900008 20070119 00008 EA 2007 1 19 TRAX200700066 1 20070111 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 PAX DOOR 'OPEN' PLACARD WORN. REMOVED AND REPLACED "OPEN " PLACARD IAW CRJ AMM 11-20. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2007011900009 20070119 00009 EA 2007 1 19 TRAX200700067 1 20070111 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 PAX DOOR ARROW PLACARD WORN. REMOVED AND REPLACED ARROW PLACARD IAW CRJ 700 AMM 11-20. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2007011900010 20070119 00010 EU 2007 1 19 USAA070034 1 20070111 A 5347 D5311278220201 GALLEY TRACK AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 165US 1431 FWD GALLEY SEAT TRACK Y-1292 FR 23 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK PER SRM 51-42-11; CORR TASK JA-220-53 500; CORR LEVEL 2, DEFECT SIZE: 6 X 2 INCHES. 2 L 7 2 4F RT A28NM 2007012200002 20070122 00002 NM 2007 1 22 USAA070042 1 20070117 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 BS 328 RBL 28.5 FLOORBEAM UPPER TEE HAS CORROSION. CORROSION REMOVED, BLENDED; FAB'D STRAP & INSTALLED PER SRM 53-00-51 ; CORROSION LEVEL 2; TASK C53-107-02, DEFECT SIZE: 1 X 1 X .020 INCH. 2 L 7 2 4F RT A16WE 2007012200010 20070122 00010 NM 2007 1 22 ASAA0741402 1 20070117 A 5315 654681189 FLOORBEAM BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 713AS 30161 FLOORBEAM CAP CORRODED AROUND NUT HOLES. FLOORBEAM REPAIRED PER SRM 53-60-51 FIG 201 REPAIR 3. 2 L 7 2 4F RT A16WE 2007012200025 20070122 00025 EA 2007 1 22 COMA0760025 1 20070113 A 2613 6243843 SENSOR CNDAIR CL600 CL6002B19 1900309 EA LT WING OVERHEAT FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 589CA 7072 FLIGHT 5207 - RECEIVED WING OVERHEAT MESSAGE. LEFT WING LEADING EDGE IS RED ON SYNOPTIC PAGE. DIVERTED TO ACY AND LAND ED WITHOUT INCIDENT. FERRIED TO CVG. REPLACED LEFT WING OVERHEAT/SUFFICIENT HEAT SENSOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007012200026 20070122 00026 EA 2007 1 22 COMA0760012 1 20070107 A 5610 NP13932211 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 729CA 2037 7265 FLIGHT 5238 - DURING CLIMBOUT AT FL1200 FT. LEFT SIDE WINDOW OUTER PLY CRACKED. A/C RETURNED BACK TO ROC AND LANDED SA FELY. REMOVED AND REPLACED LEFT SIDE WINDOW. 2 L 7 2 4F RT A21EA 2007012200029 20070122 00029 EA 2007 1 22 COMA0760006 1 20070104 A 5270 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA E/E BAY DOOR MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 685BR 7712 FLIGHT 5123 - DURING TAKEOFF ROLL BELOW 10 KTS AVIONICS BAY DOOR INDICATION. ABORTED TAKEOFF AND RETURNED TO GATE. VER IFIED DOOR CLOSED, LOCKED AND LATCHED, TRANSFERRED TO DMI LIST PER 52-70-02. 2 L 7 2 4F RT A21EA 2007012200051 20070122 00051 NM 2007 1 22 KCSA071023 1 20070115 A 5313 STRINGER BOEING 747 747209F 1384800 NM BS 2360 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 CORROSION IN BOLT HOLES OF STR-1L END FITTING FORWARD OF BS 2360 BULKHEAD. 2 L 7 4 4F RT A20WE 2007012200055 20070122 00055 NM 2007 1 22 KCSA071028 1 20070116 A 5313 STRINGER BOEING 747 747209F 1384800 NM BS 840 GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 STR 16R UPPER FLANGE HAS A DEEP GOUGE AT BS 840. 2 L 7 4 4F RT A20WE 2007012200061 20070122 00061 NM 2007 1 22 AMTA200700012 1 20070109 A 4930 211734219 ECU BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE APU FAILED A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 550TZ 32584 APU AUTO SHUTDOWN, SHOW REV FLOW LAST 3 SHUTDOWNS AND CODES 36 AND 43. REMOVED AND REPLACED APU ECU REF MM. OPS AND BI TE CHECK GOOD. APU RUN NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007012200063 20070122 00063 NM 2007 1 22 WRLA2007008 1 20070111 A 5330 SKIN DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE BS 1165 CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 41081 48632 DURING 2C+12A+150M CHECK, MECHANIC FOUND CENTER ACCESSORY COMPARTMENT LWR SKIN SPLICE SURFACE CORRODED AT STA Y=1165, LO NGERON 51L LEFT SIDE. BLEND OUT CORRODED AREA PER MD-11F SRM VOL.II 51-21-01 REV.38. MEASURE REWORK AREA STILL WITHIN A LLOWABLE DAMAGE LIMITATION PER MD-11F SRM VOL.1 53-00-01 FIG 4 REV.38. APPLY PROTECTIVE COATING, CONDITION CHECK NORMAL. (EGAT NRC NO. U5065). 2 L 7 3 4F 4 F RT A22WE E24NE 2007012200073 20070122 00073 EA 2007 1 22 COMA0760026 1 20070113 A 3097 M817142DE1 TERMINAL BLOCK CNDAIR CL600 CL6002B19 1900309 EA LEFT WING FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 589CA 7072 FLIGHT 5207 - RECEIVED WING OVERHEAT MESSAGE. LEFT WING LEADING EDGE IS RED ON SYNOPTIC PAGE. DIVERTED TO ACY AND LAND ED WITHOUT INCIDENT. FERRIED TO CVG. REPLACED LEFT WING ANTI-ICE SENSOR TERMINAL BLOCK. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007012200076 20070122 00076 NM 2007 1 22 CALA0700011 1 20070109 A 5320 141T5190U124 FLOOR SUPPORT BOEING 767 767424ER 1385270 NM BS 303-325 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 68061 29456 INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 303-325, LBL 30. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007012200093 20070122 00093 NM 2007 1 22 SWAA070230 1 20070117 A 5311 6547959 FRAME BOEING 737 7373H4 1384600 NM BS 847 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME CRACKED BS 847, LOWER CORNER. REMOVED AND REPLACED FR AME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007012200094 20070122 00094 NM 2007 1 22 SWAA070231 1 20070117 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 500 S18R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007012200096 20070122 00096 NM 2007 1 22 SWAA070233 1 20070117 A 5315 6546812 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 54, WL 207. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2007012200100 20070122 00100 2007 1 22 SWAA070237 4 20070117 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007012200101 20070122 00101 NM 2007 1 22 SWAA070238 1 20070117 A 3350 MS155721 LAMP BOEING 737 7373A4 1384585 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007012200102 20070122 00102 NM 2007 1 22 SWAA070239 1 20070117 A 3350 MS155721 LAMP BOEING 737 7373A4 1384585 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007012200104 20070122 00104 NM 2007 1 22 CALA0700013 1 20070112 A 5315 147A5502 FLOORBEAM BOEING 737 737724 13844BY NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27734 28949 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 43 TO RBL 43. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01435. 2 L 7 2 4F RT A16WE 2007012200105 20070122 00105 NM 2007 1 22 CALA0700014 1 20070114 A 5320 65C34356 SHEAR WEB BOEING 737 737524 1384721 NM BS 482 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14601 27314 INSPECTION FOUND C-1 COMPARTMENT BELTFRAME LOWER SHEAR CLIP CORRODED AT STA 482, S27R TO S27L. THE CORROSION WAS REMOVE D AND A REPAIR SHEAR TIE WAS INSTALLED IAW SRM 53-00-07, REPAIR 3. 2 L 7 2 4F RT A16WE 2007012200110 20070122 00110 SO 2007 1 22 C2XA07IA010 1 20070109 A 3350 BA50933901 POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16951 145063 MCI - DURING MAINTENANCE INSPECTION, BOTH LEFT AND RIGHT HAND AFT EXTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE . MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY POWER SUPPLY, OPERATIONALLY CHECKED WITH NO D EFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007012200111 20070122 00111 SO 2007 1 22 C2XA07IA011 1 20070109 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16951 145063 MCI - DURING MAINTENANCE INSPECTION, THE AFT OVERWING EMERGENCY EXIT LOCATOR SIGN WAS FOUND TO BE INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRA FT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007012200112 20070122 00112 SO 2007 1 22 C2XA07BT002 1 20070106 A 3350 1317 BULB EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17196 14500945 BTV DURING SERVICE CHECK FOUND MAIN DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB IAW EMB145XR AMM 33-50-06. OP S CHECK GOOD. 2 L 7 2 4F RT 2007012200113 20070122 00113 NM 2007 1 22 KCSA071027 1 20070116 A 5315 FLOORBEAM BOEING 747 747209F 1384800 NM BS 1580 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 CORROSION ON MAIN DECK FLOORBEAM LOWER SPLICE AT BS 1580, LBL 90 TO LBL 100. 2 L 7 4 4F RT A20WE 2007012200114 20070122 00114 NM 2007 1 22 ASAA0741391 1 20070116 A 5315 65C3394422 FLOORBEAM BOEING 737 7374Q8 138447Q NM BS 360 CORRODED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 782AS 25113 PASSENGER CABIN FLOORBEAM IS CORRODED OUT OF LIMITS. REMOVED EXISTING REPAIR IN THE DAMAGE AREA REMOVED THE DAMAGED ARE A OF UPPER CHORD HORIZONTAL FLANGE, FABRICATED AND INSTALLED A REPLACEMENT UPPER T-CHORD SEGMENT 2 SPLICE ANGLES AND TWO SPLICE STRAPS PER ASA EA 53 10 02691 AND AAR EA 11808. 2 L 7 2 4F RT A16WE 2007012200115 20070122 00115 NM 2007 1 22 ASAA0741392 1 20070116 A 5730 6546430517 SKIN BOEING 737 7374Q8 138447Q NM LT WING DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 THE LEFT WING TRAILING EDGE I/B FORE FLAP LWR SURFACE HAS AN EXISTING REPAIR WITH MULTIPLE DENTS AND DINGS AT WBL 90. R EMOVED THE EXISTING REPAIR DOUBLER AND DAMAGED AREA OF LOWER SKIN FABRICATED AND INSTALLED A SKIN FILLER AND REPAIR DOUB LER IAW SRM 51-70-10 PARA 7, 8, 11, 15, 18 AND 20. 2 L 7 2 4F RT A16WE 2007012200117 20070122 00117 EU 2007 1 22 YENA2007003 1 20070113 A 2797 19017235401 WIRE HARNESS EMB ERJ190 ERJ190100IGW 3260408 EU LT WING SLAT INTERMITTENT A YENA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 15 178JB 2523 19000004 SLAT FAIL EICAS MESSAGE ON FLAP RETRACTION (LT HARNESS INTERMITTENT). REMOVED AND REPLACED LT WING SLAT HARNESS AS PER E-190 AMM 27-83-07 AS PER FIM 27-83-00-814-A. PERFORMED AMM OPS CHECK OF THE SLATS AS PER AMM 27-88-00-710-801-A OPS CH ECK OK. NO FAULTS FOR SLAT FAIL MSG ON EICAS. 2 L 7 2 4F RT A57NM 2007012200120 20070122 00120 NM 2007 1 22 ASAA0711380 1 20070111 A 5210 65299946 ARM BOEING 737 7372Q8 138448K NM L1 DOOR OUT OF ADJUST A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 02 741AS 21959 L1 DOOR HARD TO CLOSE. ADJUSTED STOPS AND GUIDE ARM, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2007012200122 20070122 00122 NM 2007 1 22 ASAA0741383 1 20070111 A 5330 6552988107 SKIN BOEING 737 7374Q8 138447Q NM BS 949-963 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 FUSELAGE SKIN GOUGED AT BSTA 950 STR 18L. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS DOUBLERS AND TRIPLERS IAW SRM 53-00-01 FIG 201. 2 L 7 2 4F RT A16WE 2007012200123 20070122 00123 NM 2007 1 22 ASAA0741384 1 20070111 A 5330 654577870 SKIN BOEING 737 7374Q8 138447Q NM BS 986-1016 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 FUSELAGE DENTED AT STA 1007 5 INCHES ABOVE STR 14L. REMOVED SKIN SECTION, INSTALLED NEW SKIN IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 2007012200124 20070122 00124 NM 2007 1 22 ASAA0741385 1 20070111 A 5330 6546881115 SKIN BOEING 737 7374Q8 138447Q NM BS 1052-1062 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 FUSELAGE SKIN DENTED AT BSTA 1050 BELOW STR 16L. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW ASA EA 5330 02172. 2 L 7 2 4F RT A16WE 2007012200126 20070122 00126 2007 1 22 HNAA0700230 2 20070117 A 7310 DSC1975 LINE DHAV DHC8 DHC8102 2809003 NM ZONE 400 LEAKING A HNAA D RETURN TO BLOCK K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 827EX 29982 29982 390 AFTER STARTING NR 2 ENGINE WITH BLEEDS SELECTED ON, THERE WAS A STRONG FUEL SMELL IN CABIN. FOUND WASTE FUEL DRAIN LINE LEAKING IN NR 2 COMBUSTOR SECTION. INSTALLED TEMPORARY FLEX LINE IN ACCORDANCE WITH MP&P 20.1. 2 H 7 2 4T RT A13NM 2007012200128 20070122 00128 EU 2007 1 22 YENA2007002 1 20070113 A 2797 19017140401 WIRE HARNESS EMB ERJ190 ERJ190100IGW 3260408 EU SLATS INTERMITTENT A YENA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 EA 15 178JB 2523 19000004 SLAT FAIL EICAS MESSAGE ON FLAP RETRACTION (RT HARNESS INTERMITTENT). REMOVED AND REPLACED RT WING SLAT HARNESS AS PER E-190 AMM 27-83-07 AS PER FIM 27-83-00-810-814-A. PERFORMED AMM OPS CHECK OF THE SLATS AS PER AMM 27-88-00-710-801-A, O PS CHECK OK, NO FAULTS FOR SLAT FAIL MSGS ON EICAS. 2 L 7 2 4F RT A57NM 2007012200129 20070122 00129 NM 2007 1 22 CALA0700010 1 20070109 A 5315 141T5107 FLOORBEAM BOEING 767 767424ER 1385270 NM BS 303 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 68061 29456 INSPECTION FOUND FLOORBEAM CORRODED AT BS 303, LBL 28 TO 50. THE CORROSION WAS REMOVED AND THE FLOORBEAM WAS REPAIRED I AW SRM 53-00-51, REPAIR 1, FIGURE 201. 2 L 7 2 4F RT A1NM 2007012200131 20070122 00131 EA 2007 1 22 VNAA0701001 1 20070110 A 2750 1104SD100501 SHAFT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 5 FLAP BROKEN A VNAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 05 258PS 6040 7941 CREW REPORTED A FLAPS FAIL CAUTION MESSAGE ON APPROACH. CREW ABORTED APPROACH, WENT AROUND AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE FLEXIBLE DRIVE SHAFT BROKEN. MAINTENANCE REPLACED THE FLEXIBLE DRIVE SHAFT PER AM M 27-53-10. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007012200135 20070122 00135 SO 2007 1 22 C2XA07CL003 1 20070110 A 3246 118145 HUB CAP EMB 145 EMB145LR 3260212 SO RT MLG WHEEL UNSECURE A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 16911 145446 CLE FLIGHT 2098 AFTER TAKEOFF THE RIGHT MAIN GEAR DID NOT INDICATE LOCKED AND THE LANDING GEAR LEVER DISAGREE MESSAGE AP PEARED ON THE EICAS. CYCLED GEAR 3 TIMES WITH SAME RESULTS. MAINTENANCE INSPECTED AND FOUND THE NR 3 MAIN WHEEL ASSEMB LY HUBCAP UNSECURED. THE HUBCAP WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007012200137 20070122 00137 NM 2007 1 22 2007UALA00050 1 20070105 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 194UA 26892 EEL INOP AT 4F AND 5F BOTH SECTIONS. REPLACED BATTERY, OP CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012200139 20070122 00139 NM 2007 1 22 2007UALA00052 1 20070107 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY EEL LIGHT INOP AT SEAT 35 LEFT. *S/D* REPLACED LAMP, OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012200140 20070122 00140 NM 2007 1 22 2007UALA00053 1 20070107 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY EEL LIGHT VERY DIM AT UPPER DECK SEAT 17 LEFT, UPPER DECK AISLE LEADING TO STAIRS, AND FWD STAIRS. *S/D* REP LACED BATTERY ASSYS. OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012200142 20070122 00142 NM 2007 1 22 2007UALA00055 1 20070108 A 3350 20131A BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY LIGHT INOP AT DR1R SILL, OVERHEAD DR1R, ENTRY CEILING AT DR1R. *S/D* REPLACED BATTERY PACKS, OPS CHECK NORMA L. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012200147 20070122 00147 NM 2007 1 22 2007UALA00059 1 20070108 A 3397 794640 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 177UA 24384 EEL INOP AT 4F AND 5F, BOTH SECTS. REPLACED FEEDER CABLE BOTH LOCATIONS. OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012200148 20070122 00148 NM 2007 1 22 2007UALA00060 1 20070108 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 177UA 24384 EEL INOP AT ROW 50 LEFT AND ROW 17 LEFT. REPLACED EMERGENCY LAMP, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012200152 20070122 00152 NM 2007 1 22 2007UALA00066 1 20070109 A 5240 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 924UA 26645 FWD GALLEY DOOR OUTER SKIN LOWER AFT CORNER HAS TWO INCH CRACK. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012200153 20070122 00153 NM 2007 1 22 2007UALA00067 1 20070109 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 171UA 24322 EEL LIGHT INOP AT EXIT SIGN AT AFT SIDE DR2L AND LEFT SIDE B-ZONE. *S/D* REPLACED EEL BATTERY. OP CHECKS OK FOR SERVI CE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012200155 20070122 00155 NM 2007 1 22 2007UALA00069 1 20070109 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY LEFT INOP AT CEILING ROW 61 LEFT. REPLACED LAMP, OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012200156 20070122 00156 NM 2007 1 22 2007UALA00070 1 20070109 A 3350 9F19948501 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY LIGHT INOP AT DR4L SLIDE ILLUM. REPLACED EEL ASSY. OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012200159 20070122 00159 NM 2007 1 22 2007UALA00073 1 20070109 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 FWD ENTRY DOOR AFT FRAME CRACKED AT 4TH STOP FROM BOTTOM. REMOVED DAMAGE. FABRICATED AND INSTALLED EXTERNAL DOUBLER RE PAIR PER SRM 51-70-11 PAGE 1-6. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012200162 20070122 00162 NM 2007 1 22 2007UALA00076 1 20070112 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 175UA 24382 EMERGENCY LIGHT AT 26R CEILING INOP. RELAMPED EEL, CHECKS OKAY FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012200163 20070122 00163 NM 2007 1 22 2007UALA00077 1 20070112 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 175UA 24382 EEL INOP AT 46HJK, 34ABC, 4E AFT, AND 4F AFT. RELAMPED EACH EEL, OP CHECKS OKAY FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012200164 20070122 00164 NM 2007 1 22 2007UALA00078 1 20070108 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 301UA 23642 DOOR 2R CUTOUT LOWER FWD CORNER 2.75 INCH CRACK. MAJOR REPAIR: REMOVED DAMAGE. STOP DRILLED AND PLUGGED BEAR STRAP. FA BRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012200165 20070122 00165 2007 1 22 AMTA200700004 4 20070102 A 2565 PROXIMITY SWITCH BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE ESCAPE SLIDE UNKNOWN A AMTA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 552TZ 32586 SLIDE LIGHT OFF WITH BAR ENGAGED. REPLACED NR 4 LT DOOR AFT GIRT BAR PROX SWITCH IAW AMM 25-66-11-2. SLIDE LIGHT OPS C HECK NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007012200167 20070122 00167 NM 2007 1 22 SWAA070216 1 20070116 A 2710 655228611 BEARING BOEING 737 7373H4 1384600 NM AILERONS BINDING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 AILERONS BIND BEYOND 10 TO 15 DEGREES OF TRAVEL IN BOTH DIRECTIONS. ELEVATOR TRAVEL NORMAL. REMOVED AND REPLACED FEEL CENTERING SPRING CAM ROLLER BEARING PER MM. 2 L 7 2 4F RT A16WE 2007012200169 20070122 00169 NM 2007 1 22 SWAA070218 1 20070116 A 5311 6520722 FRAME BOEING 737 7373H4 1384600 NM BS 440 S17R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 440, STR 17R. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007012200170 20070122 00170 NM 2007 1 22 SWAA070219 1 20070116 A 5340 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM BS 767 S20R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 20R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012200171 20070122 00171 NM 2007 1 22 SWAA070197 1 20070115 A 2731 69482181 SPRING BOEING 737 7377H4 1384404 NM ELEVATOR FEEL WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 703SW 27837 PITCH FELT -MUSHY- LIGHTER THAN NORMAL DURING CONTROL CHECK. FEEL DIFF LIGHT ILLUMINATED WHILE CYCLING CONTROLS. REMOV ED AND REPLACED ELEVATOR FEEL CENTERING SPRING PER MM. 2 L 7 2 4F RT A16WE 2007012200175 20070122 00175 NM 2007 1 22 SWAA070201 1 20070115 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007012200176 20070122 00176 NM 2007 1 22 SWAA070202 1 20070115 A 3350 6556633 SIGN BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2007012200177 20070122 00177 2007 1 22 SWAA070203 4 20070115 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 454WN 29851 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007012200178 20070122 00178 2007 1 22 SWAA070204 4 20070115 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 494WN 33868 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007012200179 20070122 00179 NM 2007 1 22 SWAA070205 1 20070115 A 3350 PH22300L LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 751SW 29803 EEPLS PHOTOLUMINESCENT STRIP LOOSE BETWEEN ROW 1 ABC AND ROW 4 ABC. REMOVED AND REPLACED EEPLS PHOTOLUMINESCENT STRIP P ER MM. 2 L 7 2 4F RT A16WE 2007012200180 20070122 00180 NM 2007 1 22 SWAA070206 1 20070115 A 5512 65C25727 SKIN BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED C4 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED AT REAR SPAR STA 125. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007012200183 20070122 00183 NM 2007 1 22 SWAA070209 1 20070115 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 463WN 32467 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 2 ABC. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2007012200185 20070122 00185 NM 2007 1 22 AMTA200700005 1 20070104 A 4990 41321591 HOUSING BOEING 737 73783N 13844HI NM APU UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 315TZ 28245 APU LOW OIL PRESSURE LIGHT BLINKED THEN CAME ON STEADY. APU SHOT DOWN. TROUBLESHOOT IAW FIM REF 49-90-00-810-803. REM OVED AND REPLACED OIL FILTER HOUSING AND DIFF. PRESSURE INDICATOR IAW AMM 49-91-13-4 RAN APU, NO LEAKS OR FAULTS DETECT ED. OK FOR SERVICE. (K) 2 L 7 2 4F RT A16WE 2007012200187 20070122 00187 EU 2007 1 22 07FDEA00138 1 20070119 A 5230 SKIN AIRBUS 310 A310203 3930313 EU CARGO DOOR MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 433FE 335 PREVIOUS REPAIR FWD CARGO DOOR EXTERIOR AFT SKIN, BETWEEN FR 25 AND 25A ABOVE BEAM 4 HAS EXTERNAL. REPAIR DOUBLER MEASU RING 5.6IN * 8.4 IN DUE TO PREVIOUSLY INSTALLED REPAIR LOCATED AT FWD CARGO DOOR EXTERIOR AFT SKIN BETWEEN FS 25 AND 25A ABOVE BEAM 4 WAS DETERMINED NOT TO BE IAW A310 SRM 52-30-00 FIG 203 DUE TO INCORRECT THICKNESS USED. REMOVED AND REPLA CED REPAIR DOUBLER IAW A310 SRM 52-30-00 FIG 203. 2 L 7 2 4F RT A35EU 2007012200188 20070122 00188 NM 2007 1 22 AWXA200700091 1 20070109 A 5315 D5347218920400 FLOORBEAM AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 829AW 1563 SAL - CORROSION ON MAIN CABIN FLOORBEAM, FR 68, -Y1162. REPLACED MAIN CABIN FLOORBEAM, FR 68 - FR 69, -Y1162 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007012200191 20070122 00191 NM 2007 1 22 KCSA071036 1 20070121 A 5347 SEAT TRACK BOEING 747 747209F 1384800 NM BS 482 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 FOUND MAIN DECK SEAT TRACK CRACKED AT BS 482, RBL-90. 2 L 7 4 4F RT A20WE 2007012200192 20070122 00192 NM 2007 1 22 KCSA071037 1 20070121 A 5413 STRINGER BOEING 747 747209F 1384800 NM BS 157 S14L CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 FOUND NOSE CARGO DOOR STR-14L CHAFED AT BS 157. 2 L 7 4 4F RT A20WE 2007012200193 20070122 00193 NM 2007 1 22 KCSA071038 1 20070121 A 5315 SEAT TRACK BOEING 747 747209F 1384800 NM BS 440 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 FOUND CORROSION ON MAIN DECK SEAT TRACK UPPER CHORD AT BS 440, LBL-33. 2 L 7 4 4F RT A20WE 2007012200195 20070122 00195 EU 2007 1 22 MALA070011 1 20070115 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 702 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 408XJ 340B408 AIRCRAFT SUSTAINED DAMAGE TO LEFT SIDE AFT FUSELAGE SECTION BY CONTACT WITH A BAGGAGE CART. THE FUSELAGE SKIN WAS DENTE D IN 4 PLACES BETWEEN STA 698 AND 720 CENTERED ON A LINE 7.5 INCHES BELOW STRINGER SL1514. THE DENT AT STA 702 CAUSED D EFORMATION OF FRAME STA 702 OUTBOARD FLANGE AND WEB. A DOUBLER/TRIPLER SKIN PATCH WAS INSTALLED TO THE DAMAGED AREA AND THE STA 702 FRAME WAS REPAIRED. ALL WORK WAS ACCOMPLISHED IN ACCORDANCE WITH MESABA ENGINEERING ORDER EOS53397, SAAB R EPAIR STATEMENT SDS011534 AND THE SAAB SRM. 2 L 7 2 4T RT A52EU 2007012200196 20070122 00196 NM 2007 1 22 P5CA0701508 1 20070114 A 2910 O-RING BOEING 747 74746NF 13848BT NM HYD SYSTEM FAILED A P5CA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 EA 15 452PA 30810 AT PUSHBACK, FOUND BODY GEAR (LT) TRUCK POSITION ACTUATOR HYDRAULIC FUSE LEAKING. REPLACED PACKING SET OF HYDRAULIC FUS E PER MM 32-13-24. NO LEAK NOTED. 2 L 7 4 4F RT A20WE 2007012200198 20070122 00198 NM 2007 1 22 07FDEA00139 1 20070119 A 5320 FLOOR SUPPORT BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 MAIN DECK FLOOR SUPPORT OB FLG LWR SURFACE IS CORRODED AT NUT CLIPS BS 330-340, RBL 41, WL 208. REMOVED SUPPORT BRACKET REF SRM 51-30-2 PG 2. DRILLED UP NEW FLOOR SUPPORT AND INSTALLED REF SRM 51-30-2 PG 5. 2 L 7 3 4F RT A3WE 2007012200200 20070122 00200 NM 2007 1 22 BB07010 1 20070119 A 3350 20121 POWER SUPPLY BOEING 757 7572B7 1384964 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 935UW 27201 BDL - MAINTENANCE REPORTED THE AFT SECTION OF EMERGENCY LIGHTS ARE DIM. MAINTENANCE REMOVED AND REPLACED THE POWER SUPP LY AND BATTERY PACK AT POSITION M736. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 2007012200202 20070122 00202 SO 2007 1 22 GUUA01060701 1 20070106 A 3260 DOWNLOCK SWITCH EMB 120 EMB120ER 3260203 SO LT MLG OUT OF ADJUST A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 29 283AS 120236 FLIGHT: 9131 TPA/MIA - DURING FLIGHT, THE LEFT MAIN LANDING GEAR "B" LOOP RED ANNUNCIATOR ILLUMINATES INTERMITTENTLY. C ONTINUED TO MIA LANDED WITHOUT INCIDENT. ADJUSTED THE LEFT "B" SYSTEM DOWNLOCK PROXIMITY SENSOR. 2 L 7 2 4T RT A31SO 2007012300001 20070123 00001 2007 1 23 FX7A200700001 4 20070120 A 2565 100505105 SLIDE DOUG DC9 DC982 3022082 WP L2 DOOR UNWANTED DEPLOY A FX7A O OTHER O OTHER CR CRUISE 1 SO 19 905TA 722 96 49905 AFT SERVICE DOOR EVACUATION SLIDE RAFT DEPLOYED IN-FLIGHT. 2 L 7 2 4F A6WE 2007012300002 20070123 00002 NM 2007 1 23 DL757070036 1 20070115 A 3350 333780101 CHARGER BOEING 757 757232 1384965 NM EMERGENCY LIGHTS INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 640DL 23994 FOUND EMERGENCY LIGHT INOP OVERHEAD SEAT 23D BY 2R DOOR. REMOVED AND REPLACED EMERGENCY BATTERY PACK ASSY. OPS OK. 2 L 7 2 4F RT A2NM 2007012300003 20070123 00003 NM 2007 1 23 DL76L070037 1 20070116 A 3030 0856LU6 PITOT HEAD BOEING 767 767332 1382001 NM RT UNSERVICEABLE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 176DN 25061 AFTER START, F/O'S PITOT HEAT LIGHT FAILED TO EXTINGUISH. REPLACED F/O'S AUX PITOT PROBE PER M/M. LEAK CHECKED PER M/M SYSTEM CHECKS NORMALLY. 2 L 7 2 4F RT A1NM 2007012300004 20070123 00004 NM 2007 1 23 DL76G070038 1 20070116 A 3097 WIRE BOEING 767 767324 1385203 NM CONTROL PANEL OPEN A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 394DL 27394 TAT LIGHT NOT ON WHILE ON GROUND FWD TO MCO AND PLACARD AS PER MEL 30-31-02, T/S PER WDM. FOUND BAD WIRE AT PIN D-3 OF K644 L PROBE HT N2 P33 PANEL. RETERMINATED WIRE NOW ALL CHECKS GOOD. MCO AND P REMOVED. 2 L 7 2 4F RT A1NM 2007012300007 20070123 00007 2007 1 23 DL764070041 4 20070118 A 3440 ANTENNA BOEING 767 767432ER 1385134 NM FAILED A DALA D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 27 841MH 29714 TCAS FAIL LIGHT AFTER ENGINES STARTED. PERFORM BITE CHECK FAULTING LOWER ANT. REMOVED AND REPLACED LOWER ANT. OP CKD NORMAL. 2 L 7 2 4F RT A1NM 2007012300008 20070123 00008 NM 2007 1 23 DL738070043 1 20070117 A 2750 256A35152 GEARBOX BOEING 737 737832 13844CF NM TE FLAPS LEAKING A DALA L ABORTED APPROACH K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 27 3732J 30380 FLAPS WOULD NOT EXTEND PAST 5 DEGREES DURING LANDING WITH FLAP HANDLE. FOUND FLAP PDU DRY TRIED TO SERVICE, BUT PDU WOU LD NOT HOLD FLUID . CHANGED PDU, CKED OK. 2 L 7 2 4F RT A16WE 2007012300010 20070123 00010 NM 2007 1 23 DLM88070045 1 20070117 A 3213 59353487 CYLINDER DOUG MD88 MD88 3023688 NM RT MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 990DL 53342 RT MLG OUTER CYLINDER WAS FOUND WITH CORROSION. LOCALLY BLENDED TO REMOVE CORROSION PITTING AND REFINISHED. 2 L 7 2 4F RT A6WE 2007012300011 20070123 00011 NM 2007 1 23 DL757070046 1 20070110 A 5315 146N51114 FLOORBEAM BOEING 757 757232 1384965 NM BS 1681 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 605DL 22812 THE STA 1681.8 FLOORBEAM WAS FOUND CORRODED BEYOND SRM LIMITS AT SEVERAL LOCATIONS ON THE UPPER CAP. CUT OFF THE DAMAGE D UPPER CAP AND REPLACED IT WITH A NEW TEECAP SECTION. 2 L 7 2 4F RT A2NM 2007012300012 20070123 00012 EA 2007 1 23 TRAX200700104 1 20070115 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA CONTAMINATED A ASOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 870AS 7530 STRONG ACRID ODOR THROUGHOUT AIRCRAFT WHEN PACK TEMP IS INCREASED, SUSPECT PACKS ARE CONTAMINATED. AIRCRAFT RETURNED TO ATL AFTER T/O. 2 L 7 2 4F RT A21EA 2007011800053 20070118 00053 NM 2007 1 18 SWAA070150 1 20070111 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM BS 747 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007011800087 20070118 00087 NM 2007 1 18 SWAA070170 1 20070112 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 887-947 S28R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 12Y CHECK, FOUND STRINGER 28R CORRODED AT BS 887 TO BS 947.5. REMOVED AND REPLACED STRINGER SECTION PE R SRM. 2 L 7 2 4F RT A16WE 2007011800106 20070118 00106 NM 2007 1 18 SWAA070182 1 20070112 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 465WN 33829 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 20 ABC TO ROW 22 ABC. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2007011800107 20070118 00107 NM 2007 1 18 SWAA070183 1 20070112 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 465WN 33829 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 3 ABC. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2007011800111 20070118 00111 NM 2007 1 18 SWAA070187 1 20070113 A 5330 6552880 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR CUTOUT LOWER FWD CORNER. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 2007011800114 20070118 00114 2007 1 18 SWAA070190 4 20070114 A 2565 BACR12BU9B RIVET BOEING 737 7377H4 1384404 NM R1 DOOR GIRT BAR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 472WN 33831 R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR BRACKET HAS MISSING RIVET. INSTALLED RIVET PER MM. 2 L 7 2 4F RT A16WE 2007011800120 20070118 00120 NM 2007 1 18 SWAA070196 1 20070114 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 708SW 27842 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 40 TO RBL 44. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 2007011900051 20070119 00051 EA 2007 1 19 COMA0760005 1 20070104 A 2410 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 2 LOW A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 708CA 7235 FLIGHT 5143 - IDG CAUTION CAME ON DURING TAKEOFF, ABORTED TAKEOFF AT 60 KTS. SERVICED NR 2 IDG, NO LEAKS NOTED, NO FURT HER DEFECTS, ABORTED TAKEOFF INSPECTION NOT REQUIRED 90 KTS. 2 L 7 2 4F RT A21EA 2007011900068 20070119 00068 NM 2007 1 19 ASAA0741404 1 20070117 A 5320 6552878125 SILL BOEING 737 737490 1384715 NM BS 947-986 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 713AS 30161 L2 DOOR SILL CHORD CORRODED. SILL CHORD REPLACED WITH NEW PART IAW SRM 51-40-02 AND 51-40-05. 2 L 7 2 4F RT A16WE 2007011900069 20070119 00069 NM 2007 1 19 ASAA0741405 1 20070117 A 5347 6546813122 SEAT TRACK BOEING 737 737490 1384715 NM BS 520-500G WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 713AS 30161 SEAT TRACK WORN. SEAT TRACK REPAIRED PER SRM 53-00-50 FIG 201. 2 L 7 2 4F RT A16WE 2007011900070 20070119 00070 NM 2007 1 19 ASAA0741397 1 20070116 A 5753 6546430517 SKIN BOEING 737 7374Q8 138447Q NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 THE LEFT WING TRAILING EDGE I/B FORE FLAP HAS A DING AT WBL 96.5. CUT OUT THE DAMAGED AREA ON THE LWR SKIN, FABRICATED AND INSTALLED A SKIN FILLER AND A REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 11, 15, 18 AND 20. 2 L 7 2 4F RT A16WE 2007011900071 20070119 00071 NM 2007 1 19 ASAA0741398 1 20070116 A 5755 654645245 SKIN BOEING 737 7374Q8 138447Q NM NR 5 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 THE RIGHT WING NR 5 SPOILER LWR SURFACE HAS A DING AT WBL 112.75. REMOVED THE DAMAGED AREA OF LOWER SKIN FABRICATED AND INSTALLED A SKIN FILLER AND REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 11, 15, 18 AND 20. 2 L 7 2 4F RT A16WE 2007011900072 20070119 00072 NM 2007 1 19 ASAA0741399 1 20070116 A 5755 654645263 PANEL BOEING 737 7374Q8 138447Q NM NR 4 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 LEFT WING NR 4 SPOILER LWR SURFACE HAS DENTS AND DINGS AT WBL 122. REMOVED THE DAMAGED AREA OF THE LWR SURFACE, FABRICA TED AND INSTALLED A SKIN FILLER AND A REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 11, 15, 18 AND 20. 2 L 7 2 4F RT A16WE 2007011900073 20070119 00073 NM 2007 1 19 ASAA0741400 1 20070117 A 5347 655384425 CARGO TRACK BOEING 737 737490 1384715 NM BS 847 WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 713AS 30161 AFT CARGO PIT TIE DOWN TRACK WORN. REPAIRED WITH REPAIR PART PER SRM 53-00-53 REPAIR 2. 2 L 7 2 4F RT A16WE 2007012200011 20070122 00011 NM 2007 1 22 ASAA0741403 1 20070117 A 5347 6546813123 SEAT TRACK BOEING 737 737490 1384715 NM BS 520 WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 713AS 30161 SEAT TRACK WORN. REPAIRED WITH REPAIR PART PER SRM 53-00-02 FIG 201. 2 L 7 2 4F RT A16WE 2007012200021 20070122 00021 NM 2007 1 22 SWAA070245 1 20070117 A 5753 65522111 TORQUE TUBE BOEING 737 7373T5 1384608 NM RT WING TE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND RT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TU BE PER MM. 2 L 7 2 4F RT A16WE 2007012200045 20070122 00045 SO 2007 1 22 C2XA07CL004 1 20070111 A 3350 FUSE EMB 145 EMB145LR 3260212 SO CHARGER BLOWN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14972 13379 145151 CLE FLIGHT 2664 THE CREW REPORTED THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 2 EM ERGENCY LIGHT BATTERY AND CHARGER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007012200062 20070122 00062 EA 2007 1 22 COMA0760022 1 20070111 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 967CA 7134 FLIGHT 9486 - INBOUND TO JFK RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREE FLAP POSITION, CREW DECLARED AN EMERGEN CY AND FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTIO N, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007012200068 20070122 00068 NM 2007 1 22 WRLA2007001 1 20070104 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM PWA 4460 PW4460 NE BS 630-670 CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 41081 48632 DURING 2C+12A+150M CHECK, EGAT MAINT FOUND CORROSION AT STA 630 - STA 670 LONGERON R51. CUT AND FABRICATE REPAIR THE DAM AGED AREA PER MD-11F SRM 53-10-00 REV 38 FIG 1 & 2. CONDITION CHECK NORMAL. 2 L 7 3 4F 4 F RT A22WE E24NE 2007012200069 20070122 00069 NM 2007 1 22 WRLA2007005 1 20070111 A 5730 SKIN DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE LT WING CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 41081 48632 DURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND CORROSION UNDER LEFT WING T/E FIXED PANEL UPPER SURFACE NEAR NR 5 SPOILER OUTBOARD SIDE. REPAIR THE DAMGED AREA PER EGAT E1 NR W2007A57B-066 REV.OO & APPROVED DOCUMENT BOEING MESSAGE NR 1-2776 55111-2. 2.CONDITION CHECK NORMAL. REF EGAT NRC NO.UO5072 2 L 7 3 4F 4 F RT A22WE E24NE 2007012200075 20070122 00075 SO 2007 1 22 C2XA07RI001 1 20070113 A 3350 110049 POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14558 145598 RIC MX - DURING ROUTINE MAINTENANCE, MX FOUND FWD NR 1 EMERGENCY LIGHT INOP. AFTER TROUBLESHOOTING THE SYSTEM, IT WAS F OUND EMERGENCY LIGHT BATTERY POWER SUPPLY INOP. MX REMOVED AND REPLACED POWER SUPPLY NR 1. OPERATIONAL CHECK WAS PERFO RMED SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007012200077 20070122 00077 NM 2007 1 22 CALA0700012 1 20070109 A 5315 141T5108 FLOORBEAM BOEING 767 767424ER 1385270 NM BS 325 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 68061 29456 INSPECTION FOUND FLOORBEAM CORRODED AT BS 325, LBL 30 TO LBL 55. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, REPAIR 1, FIGURE 201. 2 L 7 2 4F RT A1NM 2007012200078 20070122 00078 SO 2007 1 22 C2XA07RI002 1 20070113 A 5210 SEAL EMB 135 EMB135ER 3260203 SO PAX DOOR LEAKING A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 16502 145166 FLT 3031 - RIC - DURING FLIGHT, RIGHT OVERWING EMERGENCY EXIT DOOR AIR LEAK. RIC MX REMOVED THE DOOR, LUBRICATED DOOR S EAL, AND REINSTALLED IT. OPERATIONAL CHECK WAS PERFORMED SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007012200079 20070122 00079 NM 2007 1 22 CALA0700009 1 20070109 A 5754 65C26799 SKIN BOEING 737 737524 1384721 NM NR 6 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13665 28926 A 1 INCH CRACK WAS FOUND IN THE RIGHT WING NR 6 SLAT AT FASTENER BELOW O/B MAIN TRACK AND 34 INCHES I/B OF O/B END OF SL AT. THE CRACKED AREA OF SKIN WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 57-43-01. 2 L 7 2 4F RT A16WE 2007012200095 20070122 00095 2007 1 22 SWAA070232 4 20070117 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007012200103 20070122 00103 EA 2007 1 22 COMA0770002 1 20070104 A 5410 CN6220101009 COWL DOOR CNDAIR CL600 CL6002C10 1390015 EA LEFT NACELLE CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 354CA 10064 LEFT UPPER FAN COWL DOOR IS GOUGED AND RIB IS CHAFED FROM THE THRUST REVERSER FLEX DRIVE CABLE. REPAIRED DAMAGE IAW COM AIR EA 70-5414-01485. 2 L 7 2 4F RT A21EA 2007012200145 20070122 00145 NM 2007 1 22 2007UALA00057 1 20070108 A 3397 7956185 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 177UA 24384 EEL EXIT SIGN INOP AFT OF DR1L. *S/D* REPLACED FEEDER WIRE. EEL SYSTEM CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012200158 20070122 00158 EU 2007 1 22 2007UALA00071 2 20070108 A 7230 COMPRESSOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 ENGINE STALLED A UALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 WP 29 366UA 24535 725833 NR 1 COMPRESSOR STALL IN DESCENT. [SUP 4-17-07] CAUSE WAS CIT SENSOR NOT RESPONDING TO TEMPERATURE CHANGE. REPLACED C IT SENSOR AND MAIN ENGINE CONTROL UNIT. MEC BENCH TEST FOUND NO FAULTS. CIT SENSOR DID NOT RESPOND TO TEMPERATURE CHAN GE. BOTH UNITS MADE SERVICEABLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012200172 20070122 00172 NM 2007 1 22 SWAA070198 1 20070115 A 3350 1010427 COVER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 BULLNOSE EMERGENCY EXIT LIGHT COVER MISSING AT ROW 1 DEF. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007012200173 20070122 00173 NM 2007 1 22 SWAA070199 1 20070115 A 3350 1010427 COVER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 BULLNOSE EMERGENCY EXIT LIGHT COVER MISSING AT ROW 16 DEF. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007012200184 20070122 00184 NM 2007 1 22 SWAA070210 1 20070115 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 463WN 32467 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 12 ABC. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2007012200189 20070122 00189 NM 2007 1 22 KCSA071034 1 20070121 A 5320 WEB BOEING 747 747209F 1384800 NM BS 1660-1680 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 AFT CARGO COMP FLOOR TORQUE BOX TOP WEB CRACKED BETWEEN BS 1660 AND BS 1680, LBL-39. 2 L 7 4 4F RT A20WE 2007012200190 20070122 00190 NM 2007 1 22 KCSA071035 1 20070121 A 5347 SEAT TRACK BOEING 747 747209F 1384800 NM BS 525 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 FOUND MAIN DECK SEAT TRACK CRACKED AT BS 525, RBL-98. 2 L 7 4 4F RT A20WE 2007012200197 20070122 00197 EA 2007 1 22 QXEA200700014 1 20070108 A 2841 73811812 COMPUTER CNDAIR CL600 CL6002C10 1390015 EA FUEL QTY MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 609QX 6670 10031 LAS- FLIGHT 4299 (FAT-DEN), RECEIVED A FUEL CHANNEL 1 FAIL STATUS MESSAGE DURING CRUISE FLIGHT. DIVERTED TO LAS VEGAS A ND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE FUEL QUANTITY GAUGING COMPUTER. OPERATIONAL CHECKS GOOD . AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007012200199 20070122 00199 EU 2007 1 22 07FDEA00140 1 20070119 A 2550 TRACK AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 433FE 335 AFTER REMOVAL OF FLOORBOARDS FOR MOD E6-5320-7-5001 PT2, FWD PIT ROLLER TRACK 2R INBD SIDE OF TRACK (FLANGE) HAS 7 AREAS OF CORROSION AS MARKED BETWEEN FR 34 AND FR 38.2. REMOVED CORROSION IAW A310 SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-10-15. REMOVED AND REPLACED ROLLER TRACK IAW A310 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007012200204 20070122 00204 EA 2007 1 22 QXEA200700013 1 20070106 A 2410 766277B IDG CNDAIR CL600 CL6002C10 1390015 EA NR 2 FAILED A QXEA D RETURN TO BLOCK J WARNING INDICATION NR NOT REPORTED 1 NM 09 604QX 2217 68 10019 DEN - FLIGHT 4430 - NR 2 GENERATOR FAIL MESSAGE (CONSTANT SPEEDDRIVE INOP). RETURNED TO THE GATE. MAINTENANCE PLACED T HE SYSTEM ON MEL. AIRCRAFT RETURNED TO SERVICE. NR 2 IDG REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERV ICE. 2 L 7 2 4F RT A21EA 2007012300005 20070123 00005 NM 2007 1 23 DLM88070039 1 20070115 A 3260 833703 SENSOR DOUG MD88 MD88 3023688 NM RT MLG DOOR FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 907DL 49538 AFTER T/O, GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR RAISED GEAR INDICATED UP AND LOCKED COMPLIED W/QRH LOWER ED GEAR AND LIGHT REMAINED ILLUM GEAR INDICATED DOWN AND LOCKED C/W QRH PROCEDURES. FOUND SENSOR D1-29 BAD AND LATCH LI NK LOOSE. 2 L 7 2 4F RT A6WE 2007012300015 20070123 00015 NM 2007 1 23 CALA0700023 1 20070120 A 5315 147A5506 FLOORBEAM BOEING 737 737724 13844BY NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14735 28950 INSPECTION FOUND CABIN FLOORBEAM UPPER TEE CORRODED AT FASTENER HOLE, STA 986.5, LBL 27. REPAIRED IAW ECRA 5321-01437. 2 L 7 2 4F RT A16WE 2007012300016 20070123 00016 NM 2007 1 23 CALA0700024 1 20070121 A 5320 65516396 SUPPORT ANGLE BOEING 737 7373T0 1384582 NM BLADE SEAL CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 47332 23570 INSPECTION FOUND RT WHEEL WELL BLADE SEAL RING SUPPORT ANGLE CORRODED AT AFT AREA. THE BLADE SEAL RING SUPPORT ANGLE WA S REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007012300021 20070123 00021 NM 2007 1 23 HALA0700027 1 20070118 A 3350 LIGHT BOEING 767 767300 1385204 NM CABIN INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 588HA 33466 FIRST CLASS A/C RIGHT EMERGENCY FLOOR LIGHT INOP. REPLACED LIGHT STRIP FIRST CLASS CABIN A/C RIGHT OK FOR SVC, OPS CHEC K GOOD AMM 33-51-05. 2 L 7 2 4F RT A1NM 2007012300023 20070123 00023 SO 2007 1 23 C2XA07SH0004 1 20070121 A 4910 14526850401 FIREWALL EMB 145 EMB145EP 3260221 SO APU BAY CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15926 145005 SHV - DURING C-CHECK, APU FIREWALL HAS CHAFE DAMAGE BETWEEN 4/8 O`CLOCK POSITION. MAINTENANCE REPAIRED APU FIREWALL AT FR 81 IAW EMB 145 EC5310-01359. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE 2 L 7 2 4F RT T00011AT 2007012300025 20070123 00025 NM 2007 1 23 07FDEA00093 1 20070115 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT WING OUTBOARD FLAP INBOARD AFT HINGE OUTBOARD CENTER BOLT HOLE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5750- 107761, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007012300027 20070123 00027 NM 2007 1 23 07FDEA00094 1 20070115 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT WING OUTBOARD FLAP INBOARD AFT HINGE OUTBOARD AFT BOLT HOLE FOUND CORRODED. REMOVED AND REPLACED AS PER CMM 57-52 - 04. FLAP ADJUSTMENT REFER TO FEDEX EO 1-5720-7-5001 PT2, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007012300033 20070123 00033 NM 2007 1 23 07FDEA00100 1 20070115 A 3212 TRUNNION DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 CENTER LANDING GEAR RT TRUNNION AFT HOLE FOUND CORROSION. REPAIR CARRIED OUT AT CENTER LANDING GEAR RH TRUNNION AFT HOL E AS PER FEDEX EA 1-5340-105661, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007012300036 20070123 00036 NM 2007 1 23 07FDEA00103 1 20070116 A 3150 UNKNOWN BOEING 727 727233 138408A NM MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 222FE 20933 UPON RAISING GEAR HANDLE THE FOLLOWING LIGHTS ILLUMINATED, CAPT AND FO DECISION HEIGHT, SPEED BRAKE DO NOT ARM, SPEED B RAKE ARMED, ALL REVERSER OPERATING, RED AND GREEN GEAR AND DOOR LIGHTS, TAIL SKID, GREEN AND AMBER LE FLAPS, FO ALT. 2 L 7 3 4F RT A3WE 2007012300038 20070123 00038 NM 2007 1 23 DHL2007743500 1 20070105 A 5753 SKIN BOEING 727 727225 1384077 NM RT FOREFLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 RT WING O/B FOREFLAP HAS DELAMINATION DAMAGE. REMOVED DELAMINATED AREA APPROX 4.8" BY 2". CLEANED AND PREPPED REPAIR A REA TO BOND IAW B727 SRM 51-40-20 PAR 7 FIG 3. FABRICATED LOWER FILLER AND DOUBLER FROM .016" 2024T3 PO NR 9003189, REP AIR CORE FROM HRP-3/16-40-.5 PO NR 6348114 AND UPPER DOUBLER FROM .016 7075T6 PO 9003989 ANODIZED AND PRIMED REPAIR PART S AND AREA TO BE REPAIRED IAW B727 SRM 51-40-20 PAR 8, 9, 14, 15 AND 51-40-24 FIG 2. INSTALLED ADHESIVE FILM AND CORE S PLICE ADHESIVE. INSTALLED REPAIR PARTS AND CURED REPAIR (IN TWO STAGE CURE) IAW B727 SRM 51-40-20 PAR 18, 19, 20 AND 51 -40-24 FIG 2. FINISHED REPAIR AREA IAW B727 SRM 51-40-20 PAR 22 AND AMM 51-20-00. DIM OF REPAIR IS FILLER 2" BY 4.8" D 2 L 7 3 4F A3WE 2007012300039 20070123 00039 WP 2007 1 23 DHL2007802500 1 20070111 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP BS 340 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 MAIN CARGO COMPT NR 1 TRACK PLUG LUG WORN STA 340.000. REMOVED WORN TRACK PLUG IAW SRM 51-3-0. CLEANED, TREATED AND PR IMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG IAW SRM 51-3-0, SRM 51-3-1 PG 3. 2 L 7 4 4F RT 4A25 2007012300040 20070123 00040 WP 2007 1 23 DHL2007802501 1 20070111 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP BS 786 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 MAIN CARGO COMPT NR 7 TRACK LUG WORN STA 786.000. CUT OUT NR 7 TRACK DAMAGED SECTION IAW SRM 53-2-3 PG 17 FIG 6D. CLEA NED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG AND CHANNEL IAW SRM 53-2-3 PG 17 FIG 6D, SRM 51- 3-0, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007012300042 20070123 00042 WP 2007 1 23 07FDEA00105 1 20070116 A 5730 SKIN DOUG DC10 DC1030 3023501 WP LT WING MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 304FE 46992 LT WING L/E UPPER SIDE AT STA XIS240 EXISTING SKIN REPAIR. PERFORMED INSPECTION OF REPAIR AND NOT FOUND INCOMPLIANCE WI TH CRITERIA REQ BY EO NR 8-5100-7-5001 BECAUSE FOUND WEAR ON SURFACE OF DOUBLER. REMOVED AND REPLACED REPAIR IAW SRM 57-10-00 FIG 15A SHT1 VOL 1. 2 L 7 3 4F A22WE 2007012300044 20070123 00044 WP 2007 1 23 07FDEA00107 1 20070116 A 5512 SKIN DOUG DC10 DC1030 3023501 WP HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 FOR CUSTOMER REQUEST, HORIZONTAL STAB UPPER INTERIOR SKIN PANELS, FOUND CRACKED PANELS P/N7228-1, POSITION 6 AND 7 AND P ANEL P/N7229-1 POSITION 2, SEE ATTACHING MAP FOR DETAIL. REMOVED AND REPLACED PANELS ALC7228-1 AND ALC7229-1 IAW SB55-1 6 GROUP 2 FOLLOWING INSTRUCTIONS FROM FIG 2 AND 3. REPAIR RIB WITH REPAIR ANGLE IAW SRM 55-00-01 VOL 1 PAGE 2B AND FIG 2 SHT 2. 2 L 7 3 4F A22WE 2007012300046 20070123 00046 WP 2007 1 23 07FDEA00112 1 20070116 A 5730 SKIN DOUG DC10 DC1010 3022110 WP RT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 RT WING TIP WING LOWER SKIN TWO DOUBLERS REPAIR O/B OF ACCESS DOOR XFS 1191. REMOVED AND REPLACED STIFFENER IAW DWG ARB 2204 ARB1044. INSTALLED DOUBLER REPAIR IAW SRM 57-00-01 FIG 4 SHEET 2 VOL 1. FABRICATED PART IAW DETAIL PARTS TRAVELER N01124 AND SRM 57-00-01 FIG 4 SHT 2 VOL 1. 2 L 7 3 4F A22WE 2007012300047 20070123 00047 WP 2007 1 23 07FDEA00113 1 20070116 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1801-1810 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 LOWER EXT FUSELAGE FOUND DENT 5" BY 4" DEPTH .030" FROM STA 1801 TO STA 1810 L50-51 RT. DENT DIMENSIONS MEASURED PER SR M 53-20-00 VOL 1 FIG 1 B SHEET 2 STEP 1 AND FOUND TO BE OUT OF LIMITS, PROVISION 1A NOT MET DENTS ARE 1" A PART, MINIMUM REQUIREMENT IS 3". REFER TO JPF FOR REPAIR. REMOVED EXISTING DOUBLER, INSTALLED REPAIR PARTS IAW SRM 53-20-00 VOL1 FI G 6 SHT 3.4. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N00232 AND SRM 53-20-00 VOL1 FIG 6 SHT 3.4. 2 L 7 3 4F A22WE 2007012300048 20070123 00048 WP 2007 1 23 07FDEA00115 1 20070116 A 5710 BULKHEAD DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 XORS 346 LWR BULKHEAD CAP IS CRACKED HORIZONTALLY THRU THE LUG AT STR 44. CUT LOWER VERTICAL LEG FLUSH TO HORIZONTAL LE G TO COMPLETLY REMOVE CRACK AND INSTALLED "T" REPAIR IAW SRM 57-20-00 VOL1 FIG 27 SHT 2. 2 L 7 3 4F A22WE 2007012300052 20070123 00052 WP 2007 1 23 07FDEA00119 1 20070116 A 5522 SKIN DOUG DC10 DC1010 3022110 WP ELEVATOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 RT INBOARD ELEVATOR FOUND DEEP DENT 2" BY 2" MAX DEEP .080" ON UPPER SKIN FROM STA XH 153 TO XH 158. REPAIRED SKIN IAW SRM 57-00-01 VOL 1 FIG4 SHT 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I025079/N00079 AND IAW SRM 57-00-01 VOL1 FIG 14 SHT 2. 2 L 7 3 4F A22WE 2007012300053 20070123 00053 WP 2007 1 23 07FDEA00120 1 20070116 A 5753 FITTING DOUG DC10 DC1010 3022110 WP TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 LT INB FLAP FOUND FITTING ITEM 665 WITH NR 3EA HOLES WITH CORROSION REF IPC 27-51-10-01 VIEW F. REMOVED SUPPORT IAW SRM 51-31-01 VOL 2 PAG 6-10. REMOVED CORROSION AND CORROSION LOCAL BLEND IAW SRM 51-21-01 VOL 2 PAR 34A AND IAW SRM 57-20- 00 VOL 1 FIG 19. REWORKED HOLE ON COUNTER SINK AREA MAX DIA ON TOP IS 1,279. FABRICATED AND INSTALLED A REPAIR BUSHING IAW EA NR 8-5750-103681. INSTALLED SUPPORT IAW SRM 51-31-01 VOL 2 PART 6-10. 2 L 7 3 4F A22WE 2007012300054 20070123 00054 NM 2007 1 23 07FDEA00122 1 20070116 A 5340 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 STRINGER CLIP HAS BEEN GROUND AT RADIUS CUT OUT BS 660 STRINGER 7L. REPLACED STRINGER CLIP REFERENCE SRM 51-30-2 PAGES 2, 3 AND 32. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007012300055 20070123 00055 NM 2007 1 23 07FDEA00123 1 20070116 A 5753 SKIN BOEING 727 727233 138408A NM ZONE 500 DELAMINATED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 284FE 22621 EXISTING REPAIR FOUND AT LT IN FOREFLAP UPPER SURFACE 91" FROM INBD END FOUND DELAMINATED. REMOVED OLD REPAIR AND REPAI RED AREA REF SRM 51-40-20 PGS 1-62 AND APPLIED EXTERIER PROTECTIVE FINISH REF MM 51-21-151-7 PGS 1-4. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007012300057 20070123 00057 NM 2007 1 23 07FDEA00125 1 20070116 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 STRINGER CLIP HAS BEEN GROUND AT RADIUS CUT OUT BS 660 STRINGER 3L. REMOVED CLIP, DRILLED UP NEW CLIP. INSTALLED NEW C LIP REF SRM 51-30-2. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007012300062 20070123 00062 WP 2007 1 23 UPS07848842 1 20070109 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 EMERGENCY LIGHT BATTERY PACK INOP. CLEANED AND TIGHTENED CONNECTOR ON EXISTING BATTERY PACK. OPS CKS OK, REF MM 33-50- 01-2. 2 L 7 4 4F RT 4A25 2007012300063 20070123 00063 WP 2007 1 23 UPS07848843 1 20070109 A 2120 UNKNOWN DOUG DC8 DC873F 302199F WP COCKPIT ODOR A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 852UP 46052 MUSTY SMELL COMING FROM A/C SYSTEMS. RAN SUPPLEMENTAL HEAT, NO MUSTY SMELL AT THIS TIME. HAS AIR TO GROUND CLEAN TOILE T AND COCKPIT. 2 L 7 4 4F RT 4A25 2007012300064 20070123 00064 NM 2007 1 23 UPS07M48833 1 20070108 A 3350 BATTERY DOUG MD11 MD11F 3023600 NM EMERGENCY LIGHT DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 285UP 48457 EMERGENCY LIGHT "BAT 1 LOW LVL 1" WARNING ILLUMINATED. DEFERRAL NR M341506. PER WDM 33-51-01 WIRE CONTINUITY CK FOR EM ER LT CONTROL SYSTEM CONDITION NML. REPLACED EMERG LT BATTERY POWER SUPPLY RELAYS PER AMM 33-51-01-4. REPLACE EMERG LT POWER SUPPLY AND RECHARGEABLE BATTERY PER AMM 33-51-01-5. EMERGENCY LT TEST PASS. 2 L 7 3 4F RT A22WE 2007012300065 20070123 00065 NM 2007 1 23 UPS07M48835 1 20070109 A 2170 20D103 COALESCER BAG DOUG MD11 MD11F 3023600 NM DIRTY A IPXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 275UP 48774 FUMES IN COCKPIT. INSPECTED COCKPIT OVERHEAD AND MAIN C/B PNLS FOR BURNED WIRES, NO FAULTS NOTED. INSPECTED PACK INLE TS, NO DEBRIS NOTED. RAN ENG, FOUND SLIGHT FUMES FROM PACKS. CLEANED COALESCER BAGS PER MM 21-54-05-2. RAN ENG PERFOR MED OPS TEST PER 21-53-00-7 FOR 30 MIN. NO FUMES NOTED. 2 L 7 3 4F RT A22WE 2007012300068 20070123 00068 NE 2007 1 23 DL76L070047 2 20070119 A 7297 WIRE BOEING 767 767332 1382001 NM PWA 4460 PW4460 NE NR 2 ENGINE CHAFED A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 173DN 24800 724165 DURING BRAKE RELEASE WHILE PUSHING THROTTLES FORWARD AT APPROX 1.3 EPR, THE RIGHT ENG OIL PRESSURE LIGHT ILLUMINATED AND PRESSURE GAUGE READ AT APPROX 213PSI. IMMEDIATE ABORT PERFORMED. AT IDLE RIGHT ENG OIL PRESS IS NORMAL APPROX 106 PSI . R ENG OIL PRESS EICAS MSG ALSO. FOUND CHAFFED WIRE W354-017-18 ON R ENGINE. MADE TEMP REPAIR PER AMM 71-51-00 BLOCK 801. COMPLETED ENG RUN ALL CHECKS GOOD. TIME LIMITED REPAIR 500 FLT HRS PER SWPM 20-10-13 PARA 2. 2 L 7 2 4F 4 F RT A1NM E24NE 2007012300071 20070123 00071 NM 2007 1 23 DL757070049 1 20070119 A 5330 SKIN BOEING 757 757232 1384965 NM BS 508 S28L WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 624DL 22914 THE FUSELAGE SKIN WAS BURNISHED OUT OF SRM LIMITS AT STA 508 APPROX 3.5" INBOARD OF STR 28L. THE DAMAGED SKIN WAS CUT O UT AND A REPAIR DOUBLER WAS INSTALLED. 2 L 7 2 4F RT A2NM 2007012300072 20070123 00072 NM 2007 1 23 DL76L070050 1 20070121 A 2822 233T323521 CONTROL PANEL BOEING 767 767332 1382001 NM BOOST PUMP MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 187DN 27582 RIGHT FWD BOOST PUMP PRESS LIGHT ILLUMINATED. REMOVED AND REPLACED FUEL BOOST PUMP PANEL PER M/M. OPS CK GOOD. 2 L 7 2 4F RT A1NM 2007012300075 20070123 00075 SO 2007 1 23 RAIA00701029 1 20070120 A 3397 WIRE EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHTS BROKEN A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 826HK 145016 PRE FLT NR 5555 - STL - EMERGENCY LIGHTS ON FLOOR INOPERATIVE FROM ROW 13 BACK. MAINTENANCE REPAIRED A FAULTY CONNECTIO N AT ROW 16 LIGHT STRIP. 2 L 7 2 4F RT T00011AT 2007012300076 20070123 00076 SO 2007 1 23 RAIA00701028 1 20070118 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BLOWN A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 839HK 14500829 PRE FLT NR 8011 - RIC - EMERGENCY LIGHT OUT AT CENTER AISLE. MAINTENANCE REMOVED AND REPLACE THE BULB. 2 L 7 2 4T RT T00011AT 2007012300078 20070123 00078 NM 2007 1 23 QXEA200700033 1 20070116 A 2420 11522184 GENERATOR BOMBDR DHC8 DHC8402 1390042 NM NR 2 WARNING LIGHT A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 416QX 8709 4083 SJC FLIGHT NR 2404: ABORTED TAKEOFF, NR 2 AC GEN CAUTION LIGHT ILLUMINATED ON TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED NR 2 AC GEN IAW HORIZON TASK CARD 6242101. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERV ICE. 2 H 7 2 4T RT A13NM 2007012300080 20070123 00080 WP 2007 1 23 ABXA070013 1 20070119 A 2611 100064901 SMOKE DETECTOR DOUG DC9 DC941 302207N WP CARGO BAY DEFECTIVE A ABXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 23 957AX 2314 47759 AT FL320, LOWER CARGO FIRE LIGHT ILLUMINATED. LANDED AIRCRAFT. REPLACED SDU PER DC9 MM 26-15-00. 2 L 7 2 4F A6WE 2007012300081 20070123 00081 EA 2007 1 23 QXEA200700045 1 20070120 A 2612 FIRE LOOP CNDAIR CL600 CL6002C10 1390015 EA RT NACELLE MALFUNCTIONED A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 600QX 10005 SEA - FIRE SYSTEM FAULT STATUS MESSAGE APPEARED INTERMITTENTLY. MAINTENANCE FOUND A RIGHT ENGINE FIRE LOOP A MESSAGE IN THE MDC. PLACED ON MEL 26-00-1, RSI 268959. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007012300083 20070123 00083 WP 2007 1 23 0700119870 1 20070113 A 2161 60714621 CONTROLLER DOUG DC9 DC951 3022051 WP AUTO TEMP FAILED A NWAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 01 779NC 52473 6607 48101 DURING TAXI OUT CABIN AIR HOT. PACK CONTROL SWITCHED TO MANUAL AND FULL COLD. AT ROTATION CREW REPORTED SMOKE AND HEAT IN CABIN. FLIGHT RETURNED TO ATL FOR AN UNEVENTFUL LANDING. MAINTENANCE FOUND AUTO TEMP CONTROLLER BAD. MANUAL CONTR OL WORKS OK. REPLACED TEMP CONTROL. OPERATION CHECKS GOOD. 2 L 7 2 4F RT A6WE 2007012300084 20070123 00084 NM 2007 1 23 0700125502 1 20070116 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHTS DISCHARGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 502US 23191 EMERGENCY LIGHT AT DOOR 2L AND EMERGENCY PROXIMITY LIGHTS AT PASSENGER SEATS 20-23 INOPERATIVE. REPLACED EMERGENCY BATT ERY PACK AND BATTERY AT DOOR 2L CEILING. FLOOR TRACK EMERGENCY LIGHTS CHECK NORMAL. 2 L 7 2 4F RT A2NM 2007012300085 20070123 00085 WP 2007 1 23 UPS07848873 1 20070104 A 5312 BULKHEAD DOUG DC8 DC871F 302199D WP FS 1766 LBL 25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD CRACKED AT STA 1766 LBL25. CUT OUT DAMAGE, FABRICATED AND INSTALLED 1 FILLER A ND 2 DOUBLERS IAW SRM 53-2-5 FIG 14A. 2 L 7 4 4F RT 4A25 2007012300090 20070123 00090 EA 2007 1 23 TRAX200700034 1 20070106 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 841AS 7300 FOUND FS 484 LT SIDE INTERCOSTAL CRACKED OTBD SIDE AT LBL 36. 2 L 7 2 4F RT A21EA 2007012300091 20070123 00091 EA 2007 1 23 TRAX200700035 1 20070106 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 841AS 7300 FOUND FS 484 RT SIDE INTERCOSTAL INBD ATTACH CLIP CRACKED AT RBL 27. 2 L 7 2 4F RT A21EA 2007012300092 20070123 00092 EA 2007 1 23 TRAX200700036 1 20070106 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 310-349 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 841AS 7300 FOUND FLOOR SUPPORT ANGLE CORRODED, STA 310-349 AT LOWER SERVICE DOOR SILL (MARKED). REMOVED AND REPLACED FLOOR SUPPO RT ANGLE FROM AIRCRAFT. 2 L 7 2 4F RT A21EA 2007012300094 20070123 00094 EA 2007 1 23 QXEA200700042 1 20070118 A 3030 C16258AA TRANSDUCER CNDAIR CL600 CL6002C10 1390015 EA AOA SENSOR INOPERATIVE A QXEA D RETURN TO BLOCK J WARNING INDICATION NR NOT REPORTED 1 NM 09 614QX 12829 10049 BUR - FLIGHT 2552 - AFTER ACTIVATION OF THE PROBE HEAT SWITCHES, THE LEFT AOA HEAT CAUTION MESSAGE APPEARED AND CIRCUIT BREAKER POPPED. RESETTING THE CIRCUIT BREAKER HAD THE SAME EFFECT. RETURNED TO THE GATE. MAINTENANCE REPLACED THE AOA TRANSDUCER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007012300095 20070123 00095 EA 2007 1 23 TRAX200700071 1 20070113 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND FS 280 LT WEB CORRODED. REPAIRED IAW REO 670-53-11-052. ITEM: 9 RII SATISFACTORY PER ASA SP 607 AND EO700- 53-0062. 2 L 7 2 4F RT A21EA 2007012300096 20070123 00096 EA 2007 1 23 TRAX200700072 1 20070113 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND FS 280 HAS CORROSION ON RT WEB. REPAIRED IAW REO 670-53-11-052. SM 17032ITEM: 9 AND ALL SRMS. RII SATISFACTORY PER ASA SP 607 AND EO700-53-0062 01 2 L 7 2 4F RT A21EA 2007012300098 20070123 00098 EA 2007 1 23 TRAX200700074 1 20070113 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 858AS 7417 FOUND FWD EMERGENCY EXTERIOR OVERWING EXITING LIGHTS INOP. BOTH SIDES. 2 L 7 2 4F RT A21EA 2007012300100 20070123 00100 GL 2007 1 23 TAMF20070001O 2 20070114 A 7210 GEARBOX BOEING 767 767200 1385120 NM GE CF6 CF680C GL LT ENGINE LEAKING W TAMF A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 23 768QT 23803 690164 DURING CLIMB ON FLIGHT # 861 (MDE-SCL) LT ENGINE OIL QTY DECREASED TO ZERO AND OIL PRESS DECREASED FROM 64 TO 15 PSI. EN GINE WAS REDUCED TO IDLE AND OIL PRESS REMAINED IN 15 PSI. AIRCRAFT WAS RETURNED TO MDE AND LANDED IN NORMAL CONDITION. DURING MAINTENANCE INSPECTION IAW FIM 710500 FIG 119 WAS DISCOVERED ENGINE INTERNAL LEAK BY TRANSFER GEARBOX. LT ENGINE WAS REMOVED & REPLACED IAW BOEING TASK CARD 71-R05 "POWER PLANT REPLACE". OVERWEIGHT LANDING INSPECTION WAS PERFORMED I AW EWO 767-32-010 & AMM 05-51-35 PHASE I, OPTION A AND NONE STRUCTURAL DAMAGE WAS FOUND. MAIN WHEELS NR 1, 2, 5 & 6 WERE REPLACED IAW AMM 32-45-01 PAGE 401-405 DUE TO THERMAL FUSE PLUGS WERE FOUND MELTED & BRAKE TEMP LIGHT INSPECTION WAS PE 2 L 7 2 4F 4 F RT A1NM E23EA 2007012300101 20070123 00101 EA 2007 1 23 TRAX200700048 1 20070107 A 4910 HEAT SHIELD CNDAIR CL600 CL6002C10 1390015 EA APU BAY CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 841AS 7300 BARE METAL AND CORROSION AFT OF APU HEAT SHEILD. NO CORROSION FOUND PAINTED IAW SRM 51-25-01. 2 L 7 2 4F RT A21EA 2007012300103 20070123 00103 EA 2007 1 23 TRAX200700043 1 20070107 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 333 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 841AS 7300 CORROSION FOUND AT FUSELAGE FRAME STA 333 IN BELLY OF AIRCRAFT. STARTED BLENDING CORROSION FOUND AT FUSELAGE FRAME ST A 333 IN BELLY OF AIRCRAFT IAW CRJ 200 SRM 51-21-06. COMPLIED WITH UT THICKNESS CHECK OF BLENDED AREAS IAW CRJ NDTM 51 -20-04 FOUND MINIMUM THICKNESS TO BE .038. BEGAN REMOVAL OF 333 FRAME ALL WORK DONE IAW CRJ 200 SRM 51-42-06. FINISHED REMOVING 333 FRAME. DRILLED NEW 333 FRAME ALL WORK DONE IAW CRJ 200 CRM 51-42-06. REAMED ENLONGATED HOLE TO MAX DIA. (.164) TO A ROUND CONDTION AND INSALLED RIVETS IAW CRJ 200 SRM 51-42-06. STARTED INSTALLING FRAME AT FS 333 IAW CRJ 2 00 SRM 51-42-06. FINISTHED INSTALLING STA. 333 FRAME, INSTALLED BONDING POINTS, AND INSTALLED FLOORBOARD SUPPORT ANGLE, 2 L 7 2 4F RT A21EA 2007012300105 20070123 00105 EU 2007 1 23 0700143218 1 20070114 A 2910 HYDRAULIC SYSTEM AIRBUS 320 A320211 3930320 EU OVERSERVICED A NWAA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 01 318US 206 PASSENGER AND FLIGHT ATTENDANTS COMPLAINED OF BURNING OIL SMELL ON APPROACH INTO CANCUN. NOTED AS NOT DEICE FLUID AND A LL HYDRAULIC SYSTEMS OVER FULL ESPECIALLY GREEN SYSTEM. CORRECTED BY MAINTENANCE DRAINING 1.5 GALLONS OF EXCESS FLUID F ROM GREEN RESERVOIR. 2 L 7 2 4F RT A28NM 2007012300106 20070123 00106 NM 2007 1 23 0700176638 1 20070120 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 638US 23549 DURING OVERNIGHT CHECK, ZONE D FLOOR EMERGENCY LIGHTS WERE INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. OPERAT IONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F A20WE 2007012300107 20070123 00107 NM 2007 1 23 0700166638 1 20070120 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 638US 23549 DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT SIGN AT DOOR 4L INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. OPER ATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F A20WE 2007012300109 20070123 00109 NM 2007 1 23 DU4R2007012 1 20070101 A 5321 FLOOR PANEL BOEING 757 757232 1384965 NM BS 700 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION FWD CARGO FLOOR SPLICE BS 700. FABRICATED AND INSTALLED NEW FLOOR PANEL 1-3/4" BY 39-3/4" FROM BAC 1505-10076 6 7075-T6 IAW B757 DWG 435N1611AND SRM 51-40-2. 2 L 7 2 4F RT A2NM 2007012300112 20070123 00112 EU 2007 1 23 07FDEA00141 1 20070119 A 5414 PANEL AIRBUS 310 A310203 3930313 EU NR 1 NACELLE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 433FE 335 A DENT EXIST AT NR 1 ENG PYLON UPPER FWD FIXED L/E PNL MEASURING 6 INCH BY 4 INCH BY 0.350 INCH REMOVED AND REINSTALLED FIXED PANEL IAW A310 SRM 51-40-21. REWORKED DENT IAW A310 SRM 54-50-00 FIG 201 AND EA 6-5480-106313 PT1. 2 L 7 2 4F RT A35EU 2007012300113 20070123 00113 EU 2007 1 23 200701101 1 20070105 A 2913 PUMP EMB ERJ170 ERJ170100SE 3260406 EU HYD SYSTEM LEAKING A UHLA O OTHER J WARNING INDICATION LD LANDING 1 GL 17 863RW 17000100 FLIGHT 6482 SRQ TO ATL, CREW HAD AN ABNORMAL LANDING ROLE OUT AND TAXI. ON APPROACH A HYDRAULIC 2 LOW QTY MESSAGE APPEA RED ON THE EICAS. ON SHORT FINAL IN THE LANDING FLARE, A HYDRAULIC 2 LOW PRESSURE MESSAGE APPEARED ON THE EICAS, NOSE WH EEL STEERING WAS LOST ON LANDING. COULD NOT TAXI THE AIRCRAFT ANY FURTHER, OPERATIONS TOWED THE AIRPLANE TO THE GATE. MAINTENANCE REMOVED AND REPLACED ENG 2 ED HYDRAULIC PUMP, HOSES AND FITTINGS. WAITING ON REPLACEMENT PART INFORMATION. 2 L 7 2 4F RT A56NM 2007012300114 20070123 00114 2007 1 23 F3LA200700008 4 20070116 A 2565 D31516313 SLIDE AIRBUS A319 A319111 3930336 NM R1 DOOR NO TEST A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 927FR 5757 2209 DURING C-2 CHECK, INSPECTION REPORTED R1 DOOR SLIDE FAILED BITE TEST. REPLACED R1 DOOR SLIDE PER AMM 25-62-44-560-050 A ND TASK CARD C528001-8. 2 L 7 2 4F RT A28NM 2007012300115 20070123 00115 NM 2007 1 23 F3LA200700009 1 20070113 A 4940 27045062 STARTER AIRBUS A319 A319111 3930336 NM APU BURNED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 927FR 5757 2209 DURING C-2 CHECK, INSPECTION REPORTED THE APU STARTER TERMINAL BLOCK AND RUBBER FOOT BURNED AND MELTED. WIRES GOING TO APU STARTER MOTOR BURNED AT TERMINAL LUGS. REPLACED APU STARTER PER SMM 49-42-51-000-004 AND 49-42-51-400-004. RE-TERM INATED POSITIVE WIRE WITH NEW TERMINAL PER AMM 20-48-11. TERMINATED SENSE WIRE TO APU STARTER PER AMM 49-42-01, PAGE 00 1, SHEET 1. CONNECTED WIRES AND INSTALLED NEW BOOT PER AMM 49-42-51-991-006, STEPS 4A (9)(10). PERFORMED FUNCTION CHEC K OF THE STARTER MOTOR CLUTCH PER AMM 49-42-51-400-004, STEP 4B. PERFORMED OPS CHECK OF APU STARTER PER AMM 49-00-00-86 0-008. 2 L 7 2 4F RT A28NM 2007012300116 20070123 00116 NM 2007 1 23 07FDEA00146 1 20070120 A 3212 TRUNNION DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 FOUND CENTER LANDING GEAR LT TRUNNION FWD HOLE FOUND CORROSION. 2 L 7 3 4F RT A22WE 2007012300117 20070123 00117 NM 2007 1 23 07FDEA00147 1 20070120 A 3212 TRUNNION DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 CENTER LANDING GEAR LT TRUNNION FOUND CORROSION. CTR LANDING GEAR LT TRUNNION FITTING REMOVED & REPLACED AS PER DWG AEA 7035 AND SRM 51-31- 01 VOL.II. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007012300118 20070123 00118 EU 2007 1 23 07FDEA00148 1 20070122 A 5330 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 433FE 335 PREVIOUS REPAIR, LWR RT SIDE FUSELAGE SKIN JUST BELOW AFT LAV ACCESS DOOR BETWEEN FR 78 AND FR 79, STR 49 RT TO STR 50 R T HAS EXTERNAL REPAIR DOUBLER MEASURING 13.4 IN BY 6.8 IN BELOW CUTOUT AND ABOVE THE LAP SEAM PREVIOUSLY INSTALLED REPAI R WAS DETERMINED NOT TO BE IAW A310 SRM 53-10-16 FIG 216 SHEETS 1 AND 2 AND FIG 217 SHEET 3, DUE TO REPAIR ENDING ON TOP OF LAP SEAM STRINGER 50 RT AND CRACK STOPPER, BASED ON VISUAL EVALUATION WITH THE REPAIR INSTALLED. REMOVED EXISTING R EPAIR AND REPAIRED SKIN IAW A310 SRM 53-10-12 FIG 216 SHEETS 1 AND 2 AND FIG 217 SHEET 3. 2 L 7 2 4F RT A35EU 2007012300119 20070123 00119 NM 2007 1 23 07FDEA00149 1 20070122 A 5320 WEB BOEING 727 727233 138408A NM ZONE 200 MISINSTALLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 284FE 22621 INBD STUB WEB AT STA 608 FOR MAIN CARGO DOOR HAS NO EDGE DISTANCE FOR FASTENER HOLE. STUB WEB LOCATED AT STR 2L AND DOO R SILL CHANNEL AT CARGO DOOR CUTOUT. FABRICATED NEW STUB WEB REF 53FX656 (REV B) PART IS TO BE INSTALLED ON SNRM N00492 . CLASSIFIED AS A MAJOR REPAIR. REF HAYES INTERNATIONAL CORP DRAWING NUMBER 53FX656 (REV B). 2 L 7 3 4F RT A3WE 2007012300120 20070123 00120 NM 2007 1 23 07FDEA00150 1 20070122 A 5320 WEB BOEING 727 727233 138408A NM ZONE 200 MISINSTALLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 284FE 22621 OTBD STUB WEB LOCATED AT STA 608, STR 2L AND DOOR SILL CHANNEL FOR MAIN CARGO DOOR, HAS FASTENER HOLE WITH NO EDGE DISTA NCE. FABRICATED NEW STUB WEB REF DRAWING 53FX656 (REV B). THE PART IS TO BE INSTALLED ON SNRM N00492. CLASSIFIED AS A MAJOR REPAIR. REF HAYES INTERNATIONAL CORP DRAWING 53FX656 REV B. 2 L 7 3 4F RT A3WE 2007012300121 20070123 00121 2007 1 23 07FDEA00151 4 20070122 A 2565 D30546201 SLIDE AIRBUS 310 A310304 3930339 EU ZONE 800 LOW A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 817FD 3501 552 R1 DOOR ESCAPE SLIDE PRESSURE INDICATOR NOT IN GREEN BAND REMOVED AND REPLACED R1 DOOR ESCAPE SLIDE IAW A310-300 AMM 25- 61-22-4-01 AND A310 - 300 AMM 52-10-00-3. 2 L 7 2 4F RT A35EU 2007012300127 20070123 00127 EA 2007 1 23 TRAX200700083 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS581-687 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND RT FLOOR SEAT TRACK CORROSION, FS 581 TO 687 - SEC 3. 2 L 7 2 4F RT A21EA 2007012300128 20070123 00128 EA 2007 1 23 TRAX200700084 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 687-836 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND RT FLOOR SEAT TRACK HAS CORROSION, FS 687 TO 836 - SEC 4. 2 L 7 2 4F RT A21EA 2007012300129 20070123 00129 EA 2007 1 23 TRAX200700085 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 836-985 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND RT FLOOR SEAT TRACK CORRODED, FS 836 TO 985 SEC 5. 2 L 7 2 4F RT A21EA 2007012300130 20070123 00130 EA 2007 1 23 TRAX200700086 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 365-495 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND LT FLOOR SEAT TRACK CORROSION, FS 365 TO 495 - SEC 1. 2 L 7 2 4F RT A21EA 2007012300132 20070123 00132 EA 2007 1 23 TRAX200700087 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 495-581 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND LT FLOOR SEAT TRACK CORROSION, FS 495 TO 581, SEC 2. 2 L 7 2 4F RT A21EA 2007012300133 20070123 00133 EA 2007 1 23 TRAX200700088 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 581-687 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND LT FLOOR SEAT TRACK CORROSION, FS 581 TO 687, SEC 3. 2 L 7 2 4F RT A21EA 2007012300134 20070123 00134 EA 2007 1 23 TRAX200700089 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 687- 836 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND LT FLOOR SEAT TRACK CORROSION, FS 687 TO 836, SEC 4. 2 L 7 2 4F RT A21EA 2007012300135 20070123 00135 EA 2007 1 23 TRAX200700090 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 836-985 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND LT FLOOR SEAT TRACK CORROSION, FS 836 TO 985, SEC 5. 2 L 7 2 4F RT A21EA 2007012300136 20070123 00136 EA 2007 1 23 TRAX200700091 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 350-485 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND LT SIDEWALL SEAT TRACK CORROSION, FS 350 TO 485, SEC 1. 2 L 7 2 4F RT A21EA 2007012300137 20070123 00137 EA 2007 1 23 TRAX200700092 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 485-576 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND LT SIDEWALL SEAT TRACK CORROSION, FS 485 TO 576, SEC 2. 2 L 7 2 4F RT A21EA 2007012300138 20070123 00138 EA 2007 1 23 TRAX200700093 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 576-680 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND LT SIDEWALL SEAT TRACK CORRODED, FS 576-TO 680, SEC 4. 2 L 7 2 4F RT A21EA 2007012300139 20070123 00139 EA 2007 1 23 TRAX200700094 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 581-687 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND LT SIDEWALL SEAT TRACK CORRODED, FS 581 TO 687, SEC 3. 2 L 7 2 4F RT A21EA 2007012300140 20070123 00140 EA 2007 1 23 TRAX200700095 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 836-985 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND LT SIDEWALL SEAT TRACK CORRODED, FS 836 TO 985, SEC 5. 2 L 7 2 4F RT A21EA 2007012300141 20070123 00141 EA 2007 1 23 TRAX200700096 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 785-863 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND LT SIDEWALL SEAT TRACK CORRODED, FS 785 TO 863, SEC 6. 2 L 7 2 4F RT A21EA 2007012300142 20070123 00142 EA 2007 1 23 TRAX200700097 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 863-985 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND LT SIDEWALL SEAT TRACK CORRODED, FS 863 TO 985. 2 L 7 2 4F RT A21EA 2007012300143 20070123 00143 EU 2007 1 23 TRAX200700098 1 20070109 A 5740 BRACKET AEROSP ATR72 ATR72212 8680945 EU LT WING BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 635AS 372 LT WING AT RIB 8 FWD OUTBOARD OMEGA BRACKET ID BROKEN. 2 H 7 2 4T RT A53EU 2007012300146 20070123 00146 NM 2007 1 23 HALA0700028 1 20070121 A 3600 58494241 FILTER BOEING 717 717200 1383700 NM RT ENGINE UNKNOWN A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 487HA 55132 AIR SYS FAULT PRIOR TO T/O. REMOVED AND REPLACED RT ENG INLINE FILTER PER AMM 36-11-08 OPS AND LK CK OKAY. 2 L 7 2 4F TR A6WE 2007011900044 20070119 00044 EA 2007 1 19 VNAA0701003 1 20070114 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE MAIN PAX UNKNOWN A VNAA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 05 237PS 7906 CREW REPORTED A LOUD SQUEAL FROM PASSENGER DOOR ON INITIAL CLIMBOUT. CREW ELECTED TO RETURN TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND SEAL WAS NOT INFLATING. MAINTENANCE CLEANED SEAL AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007011900045 20070119 00045 EA 2007 1 19 VNAA0701004 1 20070114 A 3000 5399001 VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ANTI ICE FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 05 256PS 5849 7937 CREW REPORTED A LEFT HAND COWL ANTI-ICE MESSAGE IN FLIGHT. CREW PERFORMED AN UNSCHEDULED LANDING IN TRI WITHOUT INCIDEN T. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND COWL ANTI ICE VALVE. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007012200005 20070122 00005 NM 2007 1 22 USAA070039 1 20070117 A 5312 BULKHEAD BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 23742 LOCK FASTENER O/B GLIDE SLOPE ANTENNA SUPPORT AT LBL 5.7 & WL 234, STA 178 BULKHEAD WEB CRACKED. CUT OUT CRACK, FAB'D D OUBLER & FILLER PER EA 98402, SRM 53-10-08 REP 9, DEFECT SIZE: 0.125 INCH. 2 L 7 2 4F RT A16WE 2007012200007 20070122 00007 NM 2007 1 22 HNAA0700228 1 20070105 A 5347 85330217013 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 547-625 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 982HA 32746 32746 380 SURFACE CORROSION ON LEFT INBOARD SEAT TRACK IN CARGO AREA. REPLACED LEFT INBOARD SEAT TRACK AFT CARGO BAY. 2 H 7 2 4T RT A13NM 2007012200018 20070122 00018 NM 2007 1 22 SWAA070242 1 20070117 A 5753 65522111 TORQUE TUBE BOEING 737 7373T5 1384608 NM LT WING TE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND LT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TU BE PER MM. 2 L 7 2 4F RT A16WE 2007012200020 20070122 00020 NM 2007 1 22 SWAA070244 1 20070117 A 5753 65522112 TORQUE TUBE BOEING 737 7373T5 1384608 NM RT WING TE FLAP9 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND RT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE T UBE PER MM. 2 L 7 2 4F RT A16WE 2007012200031 20070122 00031 EA 2007 1 22 COMA0760008 1 20070105 A 2120 601R952081 DUCT CNDAIR CL600 CL6002B19 1900309 EA CABIN AIR FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 964CA 7129 FLIGHT 4935 - AT CRUISE RECEIVED CABIN ALT WARNING MESSAGE. AIRCRAFT DIVERTED TO IND AND LANDED SAFELY. FOUND LEFT PAC K ACM COMPRESSOR OUTLET DUCT DISCONNECTED, REPLACED DUCT. 2 L 7 2 4F RT A21EA 2007012200036 20070122 00036 EA 2007 1 22 COMA0760020 1 20070110 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 931CA 7037 FLIGHT 5072 - EN ROUTE YUL-JFK RECEIVED A FLAP FAIL CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHO UT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 ( A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007012200037 20070122 00037 EA 2007 1 22 COMA0760021 1 20070110 A 7830 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER FALSE INDICATION A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 589SW 7072 FLIGHT 5274 - DURING TAKEOFF ROLL RECEIVED A RIGHT THRUST REVERSER UNLOCK MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE G ATE. DEFERRED THE RIGHT THRUST REVERSER PER MEL 78-30-01. 2 L 7 2 4F RT A21EA 2007012200049 20070122 00049 NM 2007 1 22 HNAA0700224 1 20070118 A 5320 85300686101 THRESHOLD DHAV DHC8 DHC8102 2809003 NM BS 222-252 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 982HA 32746 32746 380 AIR STAIR DOOR MAIN ENTRANCE THRESHOLD MEMBER CORRODED. REPLACED THRESHOLD. 2 H 7 2 4T RT A13NM 2007012200052 20070122 00052 NM 2007 1 22 KCSA071024 1 20070115 A 5313 STRINGER BOEING 747 747209F 1384800 NM BS 2360 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 CORROSION IN STR 36R END FITTING BOLT HOLES FWD OF BS 2360. 2 L 7 4 4F RT A20WE 2007012200053 20070122 00053 NM 2007 1 22 KCSA071025 1 20070116 A 5313 STRINGER BOEING 747 747209F 1384800 NM BS 2360 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 CORROSION ON STR 49R END FITTING FORWARD OF BS 2360. 2 L 7 4 4F RT A20WE 2007012200065 20070122 00065 NM 2007 1 22 WRLA2007006 1 20070111 A 5280 STRUCTURE DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE LT MLG DOOR WORN A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 41081 48632 DURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND LEFT MAIN LANDING GEAR DOOR AFT SIDE CORNER HAS WEAR AT STA Y=1461 AREA. REMOVE THE WORN CORNER PER MD-11F SRM VOL.II 51-35-01 REV.38. REPLACED DOOR CORNER PER MD-11F SRM VOL.II 51-35-01 REV. 38. 3. CONDITION DOOR OPERATION CHECK NORMAL. 2 L 7 3 4F 4 F RT A22WE E24NE 2007012200066 20070122 00066 NM 2007 1 22 WRLA2007009 1 20070111 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 41081 48632 DURING 2C+12A+120M CHECK, EGAT MECHANIC FOUND MAIN DECK CARGO SEAT TRACK FLANGE CORROSION AT STA Y=1321 TO Y=1381, X=27. CUT,FABRICATE REPAIR THE CORRODED SEAT TRACK SECTION & SPLICE HAT PER MD-11F SRM VOL.1 53-70-00 FIG.1 REV.38. 2.CONDIT ION CHECK NORMAL. 2 L 7 3 4F 4 F RT A22WE E24NE 2007012200070 20070122 00070 NM 2007 1 22 WRLA2007007 1 20070111 A 2810 FUEL TANK DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE CENTER WING CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 41081 48632 DURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND CENTER WING TANK UPPER SKIN CORRODED AT STA Y=1227, X=75 TO X=79 AREA. MEC HANIC FOUND CENTER WING TANK UPPER SKIN UPPER SURFACE SEVERAL CORROSION EXIST. REPAIRED CORRODED AREA PER EGAT E1 W2007A 57B-047 REV.01 WITH APPROVED LETTER FAA FORM 8100-9 DATED JAN/17/2007.(MAJOR REPAIR) PERFORMED FUEL LEAK CHECK, NO LEAK FOUND. ALL CONDITION CHECKED NORMAL. 2 L 7 3 4F 4 F RT A22WE E24NE 2007012200097 20070122 00097 NM 2007 1 22 SWAA070234 1 20070117 A 5310 6517684 HINGE FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR CUTOUT FWD FRAME LOWER HINGE FITTING UPPER HALF CRACKED. REMOVED AND REPLACED HINGE FITTING PER SWA EA AND SB. 2 L 7 2 4F RT A16WE 2007012200136 20070122 00136 NM 2007 1 22 2007UALA00049 1 20070106 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 EEL LIGHT IN FWD RIGHT STOW BIN BULL NOSE IS INOP. REPLACED LIGHT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012200143 20070122 00143 NM 2007 1 22 2007UALA00056 1 20070108 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 177UA 24384 EEL INOP AT ACROSS LAV 102, FWD OF LAV 102, RT OB\B\ZONE, RT FWD GALLEY FWD AND AFT, AND BELOW ENT SYSTEM CLOSET. REPLA CED BATTERIES. OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012200150 20070122 00150 2007 1 22 2007UALA00062 4 20070105 A 2565 680146904 O-RING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ESCAPE SLIDE UNSERVICEABLE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 178UA G467 24385 LOW BOTTLE, LEAKING AROUND GAUGE O-RING. REPLACED O-RING. REPLACED SLIDE. A/C RETURNED TO SERVICE. ROOT CAUSE SUSPECT ED TO BE GAUGE OVER TORQUED DURING INSTALLATION WITH RESULTING DAMAGE TO O-RING. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012200174 20070122 00174 NM 2007 1 22 SWAA070200 1 20070115 A 3350 MS155721 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 EMERGENCY EXIT LIGHT INOP AT ROW 10 ABC. FOUND LOOSE LIGHT BULB, SECURED BULB PER MM. 2 L 7 2 4F RT A16WE 2007012200181 20070122 00181 2007 1 22 SWAA070207 4 20070115 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007012200182 20070122 00182 NM 2007 1 22 SWAA070208 1 20070115 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 463WN 32467 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2007012300009 20070123 00009 NM 2007 1 23 DL76L070044 1 20070116 A 3350 20121 CHARGER BOEING 767 767332 1382001 NM EMERGENCY LIGHTS CORRODED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 181DN 25986 ALL 4 OVERWING EMERGENCY EXIT SIGNS WOULD ONLY ILLUMINATE FOR 15-30 SECONDS BEFORE TURNING OFF WHEN THE COCKPIT EMERGENC Y LIGHT SWITCH WAS PLACED TO ON. REPLACED THE BATTERY PACK, NO HELP. REPLACED THE POWER SUPPLY/CHARGER AND THE SYSTEM OPERATED NORMAL, MFG P/N OF CHARGER WAS 2012-1, DPN 333780101, S/N OFF28335. 2 L 7 2 4F RT A1NM 2007012300014 20070123 00014 NM 2007 1 23 CALA0700022 1 20070120 A 5315 147A5506 FLOORBEAM BOEING 737 737724 13844BY NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14735 28950 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT FASTENER HOLE, STA 986.5, LBL 4. REPAIRED IAW ECRA 5321-01437. 2 L 7 2 4F RT A16WE 2007012300026 20070123 00026 NM 2007 1 23 DHL2007788001 1 20070118 A 5753 SKIN BOEING 727 727214 138407R NM TE FLAPS DEBONDED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 LT WING OUTBOARD AFT FLAP SHOW DISBONDED SPOT TEMPORARY REPAIR FROM TE OUTBOARD END. REMOVED DELAMINATED AREA APPROX 9 .75" BY 3.8" (UPPER SKIN) AND 3" BY 8.6" (LOWER SKIN), CLEANED AND PREPPED REPAIR AREA TO BOND. FABRICATED UPPER FILLER (9.75" BY 3.9") UPPER DOUBLER (12.75" BY 5.4") FROM .016 7075T6 PO NR 9003989 AND LOWER FILLER (3" BY 8.6") AND DOUBLER (4.5" BY 11.6") ANODIZED, PRIMED, AND APPLIED ADHESIVE FILM IAW B727 SRM 51-40-20 PARA'S 7, 8, 14, 15, AND 18 FIG 3 AND 57-40-2 FIG 3. INSTALLED FILLERS AND DOUBLERS AND CURED REPAIR AREA (2 STAGE CURES) IAW B727 SRM 51-40-20 PARA 20 FIG 12 AND 51-40-24 FIG 2. FINISHED REPAIR AREAS IAW B727 SRM 51-40-20 PARA'S 21, 22 AND 51-40-24 FIG 2 AND MM 51-20-00. 2 L 7 3 4F A3WE 2007012300028 20070123 00028 NM 2007 1 23 07FDEA00095 1 20070115 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT WING OUTBOARD FLAP INBOARD HINGE INBOARD FORWARD HOLE FOUND CORRODED. REPAIRED AS PER FEDEX EA 1-5750-107761, RE PAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007012300030 20070123 00030 NM 2007 1 23 07FDEA00097 1 20070115 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT WING OUTBOARD FLAP INBOARD HINGE OUTBOARD AFT HOLE FOUND CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-10 7761, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007012300043 20070123 00043 WP 2007 1 23 07FDEA00106 1 20070116 A 5512 SKIN DOUG DC10 DC1030 3023501 WP HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 DURING U/S INSP OF HORIZ STAB COSTANT AND OUTER SECTION SKIN PANEL, FOUND CRACKED PANEL: P/N7228-1, POSITION 6&7, P/N722 9-1 POSITION 2 AND P/N7226-1 POSITION 18, SEE ATTACHED SHEET FOR DETAIL, POSITION 6, 7 AND 2 CRACKS ARE HANDLED BY NRC N 00628. POSITION 18 CRACK NEEDED TO BE HANDLE BY THIS NRC. REMOVED AND REPLACED PANEL ALC7226-1 IAW SB55-16 GROUP 2 (DC 10-30 SERIES). FOLLOWING INSTRUCTIONS OF PARA "SINGLE PANEL REPLACEMENT OF CONSTANT SECTION SKIN PANELS" AND FIGURE 6. 2 L 7 3 4F A22WE 2007012300059 20070123 00059 2007 1 23 UPS07548841 2 20070104 A 7532 BLEED VALVE BOEING 757 75724APF 1384969 NM RT ENGINE ODOR A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 430UP 25461 BURNING SMELL DETECTED DURING FLIGHT AFTER R ENG BLEED VAL DISPLAYED, FOLLOWED FIM 36-10-00 FIG 110. REPLACED RT ENG HP SOV PER MM 36-11-07. OK TO CONTINUE. 2 L 7 2 4F RT A2NM 2007012300077 20070123 00077 SO 2007 1 23 RAIA00701030 1 20070121 A 2700 GUST LOCK EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 837HK 145255 FLT NR 7885 - SYR - GUST LOCK WILL NOT DISENGAGE. MAINTENANCE DEFERRED THE ELECTROMECHANICAL GUSTLOCK PER THE MEL. 2 L 7 2 4T RT T00011AT 2007012300089 20070123 00089 EA 2007 1 23 TRAX200700033 1 20070106 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 841AS 7300 FS 484 LT SIDE INTERCOSTAL INBD ATTACH CLIP CRACKED AT LBL 27. 2 L 7 2 4F RT A21EA 2007012300097 20070123 00097 EA 2007 1 23 TRAX200700073 1 20070113 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND FS 280 HAS CORROSION ON CROSS BEAM. WORK COMPLETED IN ACCORDANCE WITH: CRJ700 REO 670-53-11-046, REO 670-53-11-0 47, IS 67053110002, AND ASA SP 607 AND EO700-53-0061. 2 L 7 2 4F RT A21EA 2007012300102 20070123 00102 EA 2007 1 23 TRAX200700064 1 20070111 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 PAX DOOR OUTER HANDLE CRACKED (MARKED) REMOVED RODS AND LOCKING DIVCE. REMOVED PAX DOOR OUTER HANDLE. DRILLED UP NEW PAX DOOR OUTER HANDLE AND INSTALLED IAW CRJ 700 AMM 52-11-03 PAGES 401-403. REINSTALLED LOCKING DIVICE , RODS, AND UPPE R STEP IAW CRJ 700 AMM 52-11-03 JOB COMPLETE. 2 L 7 2 4F RT A21EA 2007012300147 20070123 00147 NM 2007 1 23 HALA0700029 1 20070120 A 2410 UNKNOWN BOEING 717 717200 1383700 NM UNKNOWN A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 476HA 55118 GROUND SERVICE BUSS LOCKED OUT. ACCOMPLISHED FIM TASK 24-20-807 AND TASK 24-20-808. GROUND RUN UP BOTH ENGINES OPERATI ON CHECK OKAY. 2 L 7 2 4F TR A6WE 2007012300148 20070123 00148 NM 2007 1 23 HALA0700030 1 20070120 A 3600 UNKNOWN BOEING 767 76733A 1385209 NM UNKNOWN A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 580HA 28140 BTB: ON LEFT ENG START BLEED LIGHT CAME ON. DISCONNECTED START, BLEED LIGHT WENT OUT. ACCOMP SUCCESSFUL LEFT ENG GRD R UN PER AMM 71-00-00 BLEED LIGHT REMAINED EXTINGUISHED. NO EICAS MSGS. ALL PNEUMATIC FUNCTIONS NORMAL. ACCOMP BLEED AI R SUPPLY MODULE BITE PER AMM 36-23-01. NO FAULTS NOTED. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007012300149 20070123 00149 NM 2007 1 23 HALA0700031 1 20070119 A 2797 WIRE BOEING 717 717200 1383700 NM STICK SHAKER DAMAGED A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 480HA 55125 FLT CREW REPORTS, STALL WARNING FAULT LEVEL ONE ALERT ANNUNCIATED, NO TAKEOFF. FOUND WIRES TO FO STICK SHAKER N/G. REP AIRED WIRES PER SWPM 20-10-03. RTS FOR STALL WARNING SYSTEM CHECK OK. 2 L 7 2 4F TR A6WE 2007012300150 20070123 00150 NM 2007 1 23 HALA0700032 1 20070119 A 3350 BATTERY PACK BOEING 767 767332 1382001 NM EMERGENCY LIGHTS INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 596HA 23276 RT AFT HALF OF EXTERIOR EMERGENCY LIGHTS STAY ON IN OFF POSITION AND LEFT AFT HALF OF EXTERIOR EMERGENCY LIGHT DON’T TES T. REPLACED M733 BATTERY PACK AND CONTROLLER. REPLACED M738 BATTERY PACK, OPS CK AND TEST OK. 2 L 7 2 4F RT A1NM 2007012300151 20070123 00151 EU 2007 1 23 MALA070013 1 20070120 A 3310 LIGHT SAAB SF340 340B 7860101 EU COCKPIT SHORTED A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 422XJ 340B422 FO'S CHART HOLDER/YOKE CLIP LIGHT SHORTED OUT AND SMOKED. REMOVED AND REPLACED FO'S CHART HOLDER. 2 L 7 2 4T RT A52EU 2007012300152 20070123 00152 SO 2007 1 23 SIMA200702201 1 20070118 A 5610 NP15131112 WINDSHIELD EMB 135 EMB135LR 3260305 SO COCKPIT CRACKED A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 726AE 13891 145314 FIRST OFFICER WINDSHIELD CRACKED. REMOVED AND REPLACED WINDSHIELD IAW EMB AMM. PRESSURIZATION AND LEAKED CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007012500227 20070125 00227 SO 2007 1 25 136001042007 1 20070104 A 2530 3115C HEATER GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU GALLEY ODOR E N93A O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 13 460QS 1360 SMOKE AND ODOR EMTTED FROM GALLEY HOT CUP. 2 L 7 2 4F 4 F RT A12EA E25NE 2007012300153 20070123 00153 NM 2007 1 23 2007UALA00106 1 20070116 A 5512 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZONAL STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 RT HORIZ STAB LOWER SKIN IS CRACKED AFT SPAR, APPROX 72" FROM INBD EDGE IS CRACKED. MAJOR REPAIR: FABRICATED AND INS TALLED EXTERNAL SKIN DOUBLER REPAIR PER MM 55-10-94 AND TWO ACCESS HOLE DOUBLER REPAIR PER SRM 55-10-01 REPAIR 6. 2 L 7 2 4F 4 F RT A16WE E2GL 2007012300154 20070123 00154 NM 2007 1 23 2007UALA00107 1 20070116 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 304UA 23665 AFT SECTION OF EEL STRIP FROM APPROX 15 AFT INTO AFT GALLEY INOP. REPLACED EEL STRIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2007012300155 20070123 00155 NM 2007 1 23 2007UALA00108 1 20070116 A 3350 CONTACTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXT SLIDE LIGHT CORRODED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 562UA 26664 EMERGENCY EXIT LIGHT INOP, EXTERIOR SLIDE LIGHT ON AFT CARGO DOOR INOP. CLEANED CORRODED AREAS AT CONTACT POINTS FOR BU LB. 2 L 7 2 4F 4 F RT A2NM E17NE 2007012300156 20070123 00156 NM 2007 1 23 2007UALA00109 1 20070116 A 3397 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 562UA 26664 EMERGENCY EXIT LIGHT INOP, FLOOR LIGHT INBOARD OF 'S' LAV INOP. PLUGGED IN LOOSE CONNECTOR TO POWER FEEDER STRIP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007012300157 20070123 00157 2007 1 23 2007UALA00110 4 20070117 A 2565 SLIDE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE DOOR 1L UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 DOOR 1L SLIDE FELL OUT OF SLIDE CONTAINER. SECURED DOOR SLIDE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007012300158 20070123 00158 NM 2007 1 23 2007UALA00111 1 20070117 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 AFT PIT DOOR CUTOUT BEAR STRAP DAMAGED AT STOP FITTING LOCATIONS STR'S 21R, 22R, 23R. INSTALLED LOWER DOOR CUTOUT WRAP AROUND EXTERNAL SKIN DOUBLER-TRIPLER AND INTERNAL FILLER PER SRM 53-00-01 REPAIR 31 AND 32. 2 L 7 2 4F 4 F RT A16WE E2GL 2007012300160 20070123 00160 NM 2007 1 23 2007UALA00113 1 20070117 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 847 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 AFT CARGO DOOR CUTOUT, FWD FRAME BS 847 CORRODED ON AFT SIDE BTWN STR'S 24R AND 25R. INSTALLED NEW FRAME SECTION REPAI R PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2007012300161 20070123 00161 NM 2007 1 23 2007UALA00114 1 20070117 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 492 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 FWD CARGO DOOR CUTOUT, AFT DOORWAY FRAME BS 492 IS CRACKED IN TWO PLACES JUST ABOVE LOWER STOP FITTING. MAJOR REPAIR : INSTALLED NESTED DOUBLER FRAME REPAIR PER AAR EA I060559 AND UA EVA 70030 ON AAR NR11660-1400-0001. 2 L 7 2 4F 4 F RT A16WE E2GL 2007012300162 20070123 00162 NM 2007 1 23 2007UALA00115 1 20070117 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 EXTERNAL FUSELAGE SKIN WORN UNDER DORSAL FIN LANDING. MAJOR REPAIR: INSTALLED EXTERNAL SKIN DOUBLER-TRIPLER REPAIR PER SRM 53-60-01 REPAIR 9. 2 L 7 2 4F 4 F RT A16WE E2GL 2007012300163 20070123 00163 NM 2007 1 23 2007UALA00116 1 20070117 A 5551 ATTACH FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT HORIZONTAL CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 LT HORIZ STAB FWD UPPER LUG CORRODED, AFT FACE. MAJOR REPAIR: BLENDED AND REWORKED LUG PER AAR EA I060563 AND SRM 55-10 -10 DAMAGE 3. 2 L 7 2 4F 4 F RT A16WE E2GL 2007012300164 20070123 00164 EA 2007 1 23 HNAA0700231 1 20070118 A 3097 TERMINAL DHAV DHC8 DHC8311 1386006 EA WINDSHEILD HEAT BURNED A HNAA A UNSCHED LANDING A FLAME/FIRE CR CRUISE 1 EA 07 336EN 11448 11448 336 SMOKE AND FLAMES COMING FROM F/O'S WINDSCREEN. SECONDS LATER IND SCREEN SHOWED SEVERAL CRACKS. FOUND TERMINAL END L2 B URNED, REMOVED AND REPLACED TERMINAL END AND F/O'S WINDSHIELD. 2 H 7 2 4T RT A13NM 2007012300165 20070123 00165 EA 2007 1 23 TRAX200700041 1 20070107 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 FOUND LOWER EMERGENCY EXIT SIGN AT SEAT 14CD HAS SEVERAL BULBS BURNED OUT. 2 L 7 2 4F RT A21EA 2007012300166 20070123 00166 EA 2007 1 23 TRAX200700042 1 20070107 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 730EV 10141 FOUND RT SIDE I/B ( FLOOR) SEAT TRACK FWD END CORRODED. 2 L 7 2 4F RT A21EA 2007012300167 20070123 00167 NM 2007 1 23 2007UALA00117 1 20070118 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY EXIT CEILING LIGHT INOPERATIVE AT ROW 5 LEFT. RELAMPED, OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012300168 20070123 00168 EA 2007 1 23 TRAX200700044 1 20070107 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA BS 559 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 841AS 7300 RT FLOOR SEAT TRACK HAS CORROSION IN AREA BY LAV FUS STA 559+48 TO 559+80 APROX. 2 L 7 2 4F RT A21EA 2007012300169 20070123 00169 EA 2007 1 23 TRAX200700045 1 20070107 A 5347 CARGO TRACK CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 841AS 7300 FOUND RT CARGO FLOOR TRACK HAS CORROSION (MARKED). 2 L 7 2 4F RT A21EA 2007012300170 20070123 00170 EA 2007 1 23 TRAX200700046 1 20070107 A 5340 FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 310 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 841AS 7300 FOUND STA 310 FLOOR FTG AT RBL 45 BADLY CORRODED. 2 L 7 2 4F RT A21EA 2007012300171 20070123 00171 EA 2007 1 23 TRAX200700047 1 20070107 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 349 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 841AS 7300 FOUND FLOORBEAM AT FS STA 349 LBL 45 HAS CORROSION. 2 L 7 2 4F RT A21EA 2007012300172 20070123 00172 EA 2007 1 23 TRAX200700049 1 20070107 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA RT OVERWING INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 684BR 7708 RT EMERG EXTERIOR OVERWING FWD LIGHT IS INOP. 2 L 7 2 4F RT A21EA 2007012300173 20070123 00173 EA 2007 1 23 TRAX200700050 1 20070107 A 2760 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA SPOILERS UNKNOWN A ASOA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 27 718EV 10095 I/B SPOILERON AND O/B FLT SPOILER FAULT CAUTION MSG DURING APPROACH. EN ROUTE TO EYW A/C DIVERTED TO MIA AFTER T/O. EM ERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007012300174 20070123 00174 NM 2007 1 23 2007UALA00118 1 20070118 A 3397 80603 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY EEL LIGHT INOP AT FWD GALLEY LEFT AISLE. REPLACED FEEDER CABLE. OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012300175 20070123 00175 NM 2007 1 23 2007UALA00119 1 20070118 A 3350 582240 CHARGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP. TWO AFT ASSEMBLIES. REPLACED CHARGER ASSY. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012300178 20070123 00178 2007 1 23 2007UALA00122 4 20070117 A 2565 PROXIMITY SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 1L GIRT BAR DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 588UA 26717 DOOR 1L ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT DID NOT COME ON WHEN DOOR 1L WAS ARMED. CLEANED DEBRIS FROM PROX SENSO R, 2 L 7 2 4F 4 F RT A2NM E17NE 2007012300179 20070123 00179 2007 1 23 2007UALA00123 4 20070109 A 2565 WIRE HARNESS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SLIDE 2L MISROUTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 453UA 1001 FOUND DOOR SLIDE AT 2L HARNESS ROUTED INCORRECTLY. ROUTED HARNESS CORRECTLY. COMPLETE INSPECTION OF HARNESS, VERIFIED ROUTING. 2 L 7 2 4F 4 F RT A28NM E40NE 2007012300184 20070123 00184 EA 2007 1 23 TRAX200700100 1 20070114 A 3220 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA NLG UNKNOWN A ASOA O OTHER C F.O.D. CL CLIMB 1 SO 27 925EV 7831 FOUND BIRDSTRIKE ON NOSE GEAR, EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007012300185 20070123 00185 EA 2007 1 23 TRAX200700101 1 20070115 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN WEAK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 720EV 10115 AFT EMERGENCY LIGHT DIM. 2 L 7 2 4F RT A21EA 2007012300186 20070123 00186 EA 2007 1 23 TRAX200700102 1 20070115 A 5553 ATTACH ANGLE CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 RT VERTICAL STAB TO FUSELAGE ATTACH ANGLE IS CRACKED AT AFT END. REPAIR OF RT VERTICAL STAB TO FUSELAGE ANGLE IAW REO 6 70-55-31-017. 2 L 7 2 4F RT A21EA 2007012400001 20070124 00001 SO 2007 1 24 C2XA07BT006 1 20070116 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO CARGO BAY FALSE INDICATION A C2XA O OTHER N FALSE WARNING DE DESCENT 1 SW 27 36915 145421 CARGO BAY SMOKE INDICATION AT 19000 FT IN DESCENT. NO EICAS MESSAGE. LOOKED AND SAW NO SMOKE IN CARGO BAY. REMOVED AN D REPLACED NR 1 BAGGAGE SMOKE DETECTOR IAW EMB145 MM 26-15-01. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007012400005 20070124 00005 SO 2007 1 24 C2XA07CL008 1 20070117 A 3350 78241 INVERTER EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12946 145052 DURING ROUTINE MAINTENANCE, THE LEFT EMERGENCY EXIT MARKER SIGN WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLAC ED THE NR 4 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2007012400011 20070124 00011 EA 2007 1 24 A6WA200740008 1 20070109 A 2710 AILERON CNDAIR CL600 CL6002B19 1900309 EA RATCHETING A A6WA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 31 414ZW 7586 NOTICEABLE HANGUP/LATCH IN AILERON ROLL CONTROL ON BOTH YOKES NEAR NEUTRAL POSITION, NOTICED IN FLIGHT, 6000-7000 FT WHI LE HAND FLYING. (M) 2 L 7 2 4F RT A21EA 2007012400015 20070124 00015 WP 2007 1 24 ASAA0781416 1 20070119 A 5311 991150391 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 NLG WHEELWELL LEFT FRAME JUST FORWARD OF LEFT INNER BULKHEAD WAS DENTED. REPLACE FRAME PER SRM 51 30 02. 2 L 7 2 4F RT A6WE 2007012400016 20070124 00016 NM 2007 1 24 ASAA0741417 1 20070123 A 5753 654643099 STRUCTURE BOEING 737 737490 1384715 NM FORE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 LT IB FORE FLAP HAS SEVERAL DENTS ON THE LOWER SURFACE. PREPPED DENTED AREAS FABRICATED AND INSTALLED A REPAIR DOUBLER I AW SRM 51 70 10. 2 L 7 2 4F RT A16WE 2007012400017 20070124 00017 NM 2007 1 24 QXEA200700038 1 20070119 A 2720 7G773 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007 NM RUDDER FALSE ACTIVATION A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 368PH 512 SEA FLIGHT NR 2194 - ON PUSHBACK RUDDER PRESSURE CAUTION LIGHT ILLUMINATED. MAINTENANCE REPLACED BOTH RUDDER PRESSURE S WITCHES IAW D8200 MM 27-20-38. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007012400019 20070124 00019 SO 2007 1 24 C2XA07CL010 1 20070122 A 3040 3801D2MODA CONTROLLER EMB 145 EMB145EP 3260221 SO TEMP BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 27 17928 145007 CLE FLIGHT NR 2676, THE CREW REPORTED A BURNING ODOR IN THE COCKPIT AND CABIN DURING ICE CONDITIONS THROUGHOUT DESCENT. MAINTENANCE INSPECTED AND FOUND THE TERMINAL BURNED ON THE CAPTAINS WINDSHIELD TEMP CONTROLLER. THE TEMP CONTROLLER WA S REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2007012400020 20070124 00020 SO 2007 1 24 C2XA07CL009 1 20070119 A 5210 14531554001 ROLLER EMB 145 EMB145LR 3260212 SO CABIN DOOR SEIZED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13988 145265 CLE FLIGHT NR 2816, THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. MAINTENANCE INSPECTED AND REPLACED THE AFT UPPER ROLLER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007012400023 20070124 00023 NM 2007 1 24 CALA0700027 1 20070123 A 5315 147A5506 FLOORBEAM BOEING 737 737824 13844BZ NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12238 28808 INSPECTION FOUND FLOORBEAM FORWARD FLANGE CORRODED AT NUTPLATE HOLE, STA 986.5, LBL 43. REPAIRED IAW ECRA 5321-01439. 2 L 7 2 4F RT A16WE 2007012400025 20070124 00025 NM 2007 1 24 0700185517 1 20070122 A 3350 LAMP BOEING 757 757251 1384970 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 517US 23205 EMERGENCY LIGHTS INOPERATIVE AT DOORS 2 RIGHT AND LEFT. RE-LAMPED, NO HELP. FOUND BROKEN WIRE AT PIN E OF D40488J. RE PINNED WIRE PER WDM 33-51-11. EMERGENCY LIGHTS AT DOOR 2L AND DOOR 2R OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2007012400026 20070124 00026 NM 2007 1 24 QXEA200700044 1 20070119 A 3260 860TS09Y00 PSEU DHAV DHC8 DHC8202 2809007 NM MLG MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 365PH 3018 526 SEA FLIGHT NR 2115, AFTER TAKEOFF AND GEAR RETRACTION WEIGHT ON WHEELS CAUTION LIGHT ILLUMINATED FOR APPROXIMATELY 5-7 M INUTES. LIGHT EXTINGUISHED ON ITS OWN AFTER THAT. COMPLIED WITH EMERGENCY CHECKLIST. MAINTENANCE FOUND MULTIPLE FAULT S IN PSEU MEMORY ALONG WITH CARD FAULT. REMOVED AND REPLACED PROXIMITY SWITCH ELECTRONIC UNIT IAW -8 200 AMM 32-61-00 P AGES 401-405 AND PERFORMED THE BITE DIAGNOSTIC TEST OF THE PSEU SYSTEM IAW 32-61-00-740-801 WITH NO DEFECTS NOTED. 2 H 7 2 4T RT A13NM 2007012400027 20070124 00027 NM 2007 1 24 QXEA200700043 1 20070120 A 6120 30005000056 TSCU DHAV DHC8 DHC8202 2809007 NM PROPELLER MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 353PH 1305 496 SEA FLIGHT NR 2257, NR 1 WOULD NOT FEATHER WHEN TESTED DURING DAILY CHECKS. MAINTENANCE REPLACED NR 1 TSCU. PERFORMED G ROUND RUNS IAW MTC 9720019. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007012400043 20070124 00043 EU 2007 1 24 AWXA200700093 1 20070115 A 2460 CIRCUIT BREAKER AIRBUS 320 A320232 3930326 EU TRIPPED A AWXA O OTHER G MULTIPLE FAILURE CR CRUISE 1 WP 28 672AW 2193 LAS - AT FL 350, SEC 2 FAULTED, THEN SEC 3, C/B BD POPPED CAUSING NUMEROUS FAULTS. THE CREW DECLARED AN EMERGENCY AND D IVERTED TO DEN. THE LANDING WAS UNEVENTFUL AND THE A/C TAXIED TO THE GATE. MX FOUND C/B BD ON THE 124VU TRIPPED, MX RE SET AND RAN ENG NR 2, LOADED ENG NR 2 GEN FOR SEVERAL MINUTES. NO FAULTS NOTED. MX INSPECTED C/B BD 6PP, DC SERVICE FO UND IN GOOD CONDITION. NO FAULTS, T/S PER ASM 24-61-00 AND AWM 24-61-02. THE A/C WAS RETURNED TO SERVICE. AS A PRECAU TIONARY MEASURE, MX GENERATED A FUP TO REPLACE C/B'S 7PN AND 3PN2. 2 L 7 2 4F RT A28NM 2007012400044 20070124 00044 EU 2007 1 24 AWXA200700094 1 20070115 A 3350 321431 BATTERY PACK AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHT FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 640AW 448 LAS - EEL - LEFT OVERWING EXIT LIGHT POWER SUPPLY FAULTS BATTERY PACK. REMOVED AND REPLACED BATTERY PACK PER T/C AIC333 02. OP'S CHECK GOOD. 2 L 7 2 4F RT A28NM 2007012400045 20070124 00045 NM 2007 1 24 AWXA200700095 1 20070113 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHT FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 660AW 19370 8560 1234 PHX - EEL - EMERGENCY LIGHTS ILLUMINATE WHILE EMER LT CB AT HA6 ON PNL 49VU (OVERHEAD) IS PULLED WHILE THE EMERG EXIT LT SWITCH IS OFF. MX REMOVED AND REPLACED ESPU PLUS BATTERY PACK AT RIGHT MID CABIN (12WL). EMERGENCY LIGHTS OPS CK GOOD . 2 L 7 2 4F RT A28NM 2007012400046 20070124 00046 NM 2007 1 24 AWXA200700096 1 20070113 A 3350 321431 BATTERY PACK AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHT FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 802AW 924 PHX - EEL - AFT EMERGENCY LIGHTS FAIL TEST. REMOVED AND REPLACED BATTERY FOR EMERGENCY LIGHT POWER SUPPLY 13WL. OPS C HECK GOOD IAW AMM 33-51-38. 2 L 7 2 4F RT A28NM 2007012400047 20070124 00047 EU 2007 1 24 AWXA200700098 1 20070115 A 3350 321431 BATTERY PACK AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHT FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 640AW 448 LAS - EEL - RT MID EMERGENCY LIGHT BATTERY NEEDS REPLACEMENT. MX REPLACED BATTERY PER TASK CARD A1C33302. 2 L 7 2 4F RT A28NM 2007012400049 20070124 00049 EU 2007 1 24 AWXA200700103 1 20070116 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHT FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 636AW 098 LAS - EEL - POWER SUPPLY ROW 23 A/C LEFT INOP. REMOVED AND REPLACED POWER SUPPLY ROW 23 A/C LEFT REF AMM 23-73-38. OPS CHECK NORMAL. 2 L 7 2 4F RT A28NM 2007012400050 20070124 00050 EU 2007 1 24 AWXA200700104 1 20070116 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHT FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 634AW 19370 8560 091 LAS - EEL - EMERGENCY EXIT LIGHTS TEST FAILS FOR AFT LEFT EXT LOAD FAULT, STEP 6 OF T/C I8M05334. REMOVED AND REPLACED POWER SUPPLY UNIT AND BATTERY PACK PER AMM 33-51-38 + T/C A1C33302. POWER SUPPLY OPS CK GOOD. 2 L 7 2 4F RT A28NM 2007012400052 20070124 00052 NM 2007 1 24 AWXA200700099 1 20070115 A 3610 CLAMP BOEING 757 7572G7 1384963 NM NR 2 ENG PNEU SY DISLODGED A AWXA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 WP 28 908AW 24233 FLIGHT 320: PHX - LAS - AT FL 240 NR 2 ENGINE (RT OVHT) ILLUM, EICA AND LOWER PANEL MSG. THE CREW COMPLIED W/QRH, SHUTD OWN NR 2 ENG, (CAPT STATED LIGHT EXTINGUISHED AFTER THROTTLE REDUCTION, AND ILLUMINATED AFTER POWERED BACK UP, THAT'S WH EN INITIATED AN IN-FLIGHT SHUT DOWN OF THE NR 2 ENGINE. MX FOUND NR 2 ENG CLAMP OFF PNEUMATIC DUCT GOING TO ENGINE ANTI -ICE IN PYLON. REPLACED CLAMP AND SEAL ON DUCT PER MM 36-11-01-4. RAN AT TAKEOFF POWER NO FAULTS MESSAGES, LEAK CHECK WAS GOOD. MX INSPECTED HP2 "Y" DUCT CLAMPS ON THE NR 1 ENGINE PER BOEING MM 36-11-01-4 SUB TASK 424-296. NO DEFECTS NOT ED. 2 L 7 2 4F RT A2NM 2007012400055 20070124 00055 2007 1 24 UPS07248886 4 20070119 A 2565 SLIDE BOEING 727 72730C 1384009 NM PAX DOOR DISLODGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 FWD ENTRY ESCAPE SLIDE IS OUT OF CONTAINER. INSTALLED FORWARD ENTRY DOOR EVACUATION SLIDE IAW 25-60-14-2. OPS CHECK GO OD. 2 L 7 3 4F A3WE 2007012400056 20070124 00056 NM 2007 1 24 UPS07448875 1 20070105 A 5310 141U11074 VERTICAL BEAM BOEING 747 747123F NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C NWW TUNNEL RT BS 320 VERTICAL BEAM WEB WL 190 STAND OFF HOLE FOUND CRACKED. NWW RT TUNNEL BS 320 VERT ICAL BEAM WEB REPLACED AS PER SRM 51-10-01 P9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007012400057 20070124 00057 NM 2007 1 24 UPS07548878 1 20070117 A 2150 A/C PACK BOEING 757 75724APF 1384969 NM RIGHT MALFUNCTIONED A IPXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 404UP 23726 CABIN ALT LIGHT AND EICAS MESSAGE APPEARED. CABIN ALT CONFIRMED AT 10000' CABIN RATE WAS CLIMBING. OUTFLOW VALVE WAS C LOSED. SWITCHED TO AUTO 2-NO EFFECT. MANUAL INITIALLY DID NOT CLOSE OUTFLOW VALVE. T/S BOTH NR 1 AND NR 2 CABIN PRESS URE CONTROLLERS PER FIM 21-30-00. NO FAULTS NOTED. PRESSURIZED A/C WITH RT PACK ONLY PER MM 05-51-24-2. COULD ONLY GE T 1.5 PSID. PRESSURIZED WITH LT PACK OK. DEFERRED RT PACK PER MEL 21-51-1. NO DMP. INSTALLED PLACARD. ASSIGNED DEFE RRAL M-342219. 2 L 7 2 4F RT A2NM 2007012400058 20070124 00058 WP 2007 1 24 UPS07848879 1 20070105 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 CRACKED RIB IN RT CTR LE AT XFS 443. FABRICATED AND INSTALLED 2 REPAIR ANGLES IAW SRM 57-02-00 FIG 0 02 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 2007012400061 20070124 00061 WP 2007 1 24 UPS07848885 1 20070118 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY LIGHTING BATTERY UNIT PER DC8 MM 33-50-01-2. OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 2007012400063 20070124 00063 2007 1 24 UPS07M48877 4 20070118 A 2210 COMPUTER DOUG MD11 MD11F 3023600 NM NR 1 FCC INOPERATIVE A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 250UP 48745 ATB - DURING T/O "AP OFF" AND "ATS OFF" AND WILL NOT ENGAGE. DURING CLIMB, CRUISE AND DESCENT ALL ENGINE AND FMS UNAVIL ABLE. REMOVED AND REPLACED FCC-1 IAW MM 22-01-03-4. 2 L 7 3 4F RT A22WE 2007012400070 20070124 00070 EU 2007 1 24 07FDEA00135 1 20070119 A 5330 SKIN AIRBUS 310 A310203 3930313 EU FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 433FE 335 SKIN GOUGE AT FS 76 - 77 LT SIDE JUST AFT OF L2 DOOR APPROX 10 INCHES L BY .10W BY .085D BETWEEN STRINGERS 25 TO 28 LT R EF N00426. REPAIRED SKIN IAW A310 SRM 53-10-12 FIG 228 SHEET 3. REPROTECTED SURFACE IAW A310-200 SRM 51-75-10. 2 L 7 2 4F RT A35EU 2007012400071 20070124 00071 EU 2007 1 24 07FDEA00136 1 20070119 A 2550 ROLLER TRAY AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 433FE 335 AFTER REMOVAL OF FLOORBOARDS FOR MOD E6-5320-7-5001 PT2 - FWD PIT ROLLER TRACK 1R OTBD SIDE OF TRACK (FLANGE) HAS 9 EA A REAS OF CORROSION AS MARKED BETWEEN FS 34 AND 6" AFT OF FS 38.2. REMOVED CORROSION 11 PLACES FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED ROLLER TRACK IAW A310-200 AMM25-52-24-4, 25-52-57-4, 25-52-34-4 SRM 51-74-10, 53-10-15, 51-21-10, 51-75-10. 2 L 7 2 4F RT A35EU 2007012400072 20070124 00072 EU 2007 1 24 07FDEA00137 1 20070119 A 5100 SKIN AIRBUS 310 A310203 3930313 EU ZONE 200 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 433FE 335 PREVIOUS REPAIR, LEFT OF AFT PAX DOOR EXTERIOR SKIN LWR AFT CORNER HAS EXTERNAL REPAIR DOUBLE MEASURING 9.2IN BY 7.3IN. PREVIOUSLY INSTALLED REPAIR LOCATED AT AFT PAX DOOR EXTERIOR SKIN LOWER AFT CORNER WAS DETERMINED NOT TO BE IAW A310 SR M 52-10-00 FIG 203, DUE TO THE OUTER ROW OF FASTENERS WERE MISSING 7 RIVETS BASED ON A VISUAL EVALUATION WITH THE REPAIR INVOLVED. DRILLED AND COUNTERSUNK 7 NEW HOLES AND INSTALLED 7 NEW RIVETS PER A310 SRM 52-10-00 FIG 203. 2 L 7 2 4F RT A35EU 2007012400073 20070124 00073 NM 2007 1 24 PIDA07001 1 20070110 A 2910 B-NUT BOEING 737 7373Y0 1384671 NM HYD LINE LOOSE A PIDA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 05 373PA 23749 DURING LANDING ROLL-OUT, CONTROLLER OBSERVED SMOKE FROM LEFT WHEEL AREA. FOUND BRAKE HYDRAULIC LINE "B" NUT LOOSE AND L EAKING HYDRAULIC FLUID ONTO BRAKE. TIGHTENED NUT AND LEAK AND OPS CHECKED BRAKE. NO FURTHER INCIDENTS. 2 L 7 2 4F RT A16WE 2007012400074 20070124 00074 EA 2007 1 24 SWIA200717670 1 20070115 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 979SW 7954 RIGHT FORWARD EMERGENCY OVERWING LIGHT INOP. REPLACED BULB. OPERATIONAL CHECK GOOD. REF PMM 33-51-00. 2 L 7 2 4F RT A21EA 2007012400079 20070124 00079 EA 2007 1 24 SWIA200717675 1 20070116 A 2701 CONTROL COLUMN CNDAIR CL600 CL6002C10 1390015 EA COCKPIT OBSTRUCTED A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 703EV 10038 AILERONS SEEM TO BIND MOMENTARILY WHEN ROLLING. MOST NOTICEABLE WHEN TURNING LEFT. RE-POSITIONED CONTROL COLUMN WIRE B UNDLE. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007012400080 20070124 00080 EA 2007 1 24 SWIA200717676 1 20070116 A 4930 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA APU FUEL SYS ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 417SW 7400 STRONG ODOR OF FUEL WHEN APU IS RUNNING ON GROUND. REPLACED METERED FUEL OUTLET TUBE AND FUEL SHUT OFF VALVE IAW 49-31- 01. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007012400081 20070124 00081 EA 2007 1 24 SWIA200717677 1 20070116 A 3231 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA NLG DOOR MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 982SW 7956 AFTER TAKEOFF, RETRACTED GEAR AND RECEIVED NOSE DOOR WARNING MESSAGE. RETURNED TO FIELD. VISUALLY INSPECTED NOSE LANDI NG GEAR DOOR PROXIMITY SWITCHES AND NOSE LANDING GEAR DOOR WARNING SYSTEM. PERFORMED SYSTEM TEST OF PSEU REF CRJ FIM 32 -60-05. COULD NOT DUPLICATE DISCREPANCY. 2 L 7 2 4F RT A21EA 2007012400084 20070124 00084 EU 2007 1 24 UPS07148857 1 20070102 A 5210 HANDLE AIRBUS A300 A300F4622R 3930360 EU PAX DOOR JAMMED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 120UP 0805 CABIN MAIN ENTRY DOOR DIS-ARM HANDLE IS JAMMING WHEN DIS-ARMING SLIDE. MAIN ENTRY DOOR SLIDE RAIL LOCKS CLEANED, DRIED, AND LUBRICATED. TESTED SEVERAL TIMES SATISFACTORY. 2 L 7 2 4F RT A35EU 2007012400085 20070124 00085 2007 1 24 UPS07148858 4 20070102 A 2565 ARMING LEVER AIRBUS A300 A300F4622R 3930360 EU PAX DOOR SLIDE JAMMED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 120UP 0805 CABIN DOOR SLIDE ARMING HANDLE JAMMING WHEN DISARMING. CHECKED DOOR SLIDE ARMING SYSTEM IAW MM 25-61-04. FOUND NO ABNO RMALS. 2 L 7 2 4F RT A35EU 2007012400087 20070124 00087 WP 2007 1 24 UPS07848838 1 20070103 A 5313 3750257U503 LONGERON SPLICE DOUG DC8 DC871F 302199D WP FS 1040 L31L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C2 C-PIT STA 1040 L31L, LONGERON SPLICE FITTING CRACKED. REMOVED AND REPLACED LONGERON SPLICE FITTING A T STA 1040 L31L IAW SRM 51-01-20D, 51-03-02. 2 L 7 4 4F RT 4A25 2007012400089 20070124 00089 WP 2007 1 24 UPS07848840 1 20070105 A 5720 STIFFENER DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C2 RADIOGRAPHIC INSP DETECTED A CRACK ON THE LT WING AT STA XRS437.00 VERTICAL STIFFENER IN THE LEADING EDGE. REMOVED REPAIR FROM VERTICAL STIFFENER IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR DOUBLER, AND REPAIR ANGL E AT LT WING STA XRS 437.00 VERTICAL STIFFENER IAW DWG 5770170-5, AND SRM'S 57-02-00 FIG 2, 51-1-4, AND 51-1-20D. 2 L 7 4 4F RT 4A25 2007012400096 20070124 00096 WP 2007 1 24 UPS07848853 1 20070111 A 3350 6012235 LIGHT DOUG DC8 DC873F 302199F WP COCKPIT NO TEST A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 806UP 46006 EMERGENCY LIGHTS WOULD NOT TEST. INSTALLED SERVICEABLE EMERGENCY LIGHT BATTERY AND RELAY UNIT ASSY PER AMM 33-50-01. O PS CK NORMAL. 2 L 7 4 4F RT 4A25 2007012400099 20070124 00099 EU 2007 1 24 200701122 1 20070109 A 2752 ACTUATOR EMB ERJ170 ERJ170100SE 3260406 EU TE FLAPS TRIPPED A UHLA O OTHER J WARNING INDICATION AP APPROACH 1 GL 17 650RW 17000071 FLIGHT 7701 IND TO DEN, ON APPROACH THE CREW ATTEMPTED TO EXTEND FLAPS 1 AT 210KTS AND OBTAINED A FLAP FAIL MESSAGE ON T HE EICAS. CYCLED THE FLAPS THREE TIMES PER THE QRH AND DISCOVERED THE SLATS WOULD MOVE, BUT THERE WAS NO FLAP MOVEMENT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE WARMED AIRCRAFT IN HANGAR, DROPPED FLAPS AND FOUND LT OB ACTUATOR TRIPP ED, RESET AND OPS CHECKED GOOD. 2 L 7 2 4F RT A56NM 2007012400102 20070124 00102 2007 1 24 MWEA070004 4 20070115 A 3100 4056510903 DISPLAY DOUG DC9 DC982 3022082 WP COCKPIT INOPERATIVE A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 13 809ME 48071 BURNING SMELL IN THE COCKPIT. REMOVED AND REPLACED PRIMARY FLIGHT DISPLAY. 2 L 7 2 4F A6WE 2007012400103 20070124 00103 EU 2007 1 24 MALA070009 1 20070118 A 3350 BATTERY PACK SAAB SF340 340B 7860101 EU NO TEST A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 421XJ 340B421 FAILED CAP CHECK PER L3 COMMUNICATIONS AVIONICS SYSTEMS, GOODRICH AVIONICS SYSTEMS, INC. REPLACED BATTERY PACK. 2 L 7 2 4T RT A52EU 2007012400104 20070124 00104 2007 1 24 COMA0760031 2 20070116 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA NR 1 VIBRATION A COMA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 01 995CA 7229 FLIGHT 5350 - NR 1 ENGINE VIB GAUGE PEGGED OFF CHART, REDUCED THRUST TO IDLE AND VIBS STOP. A/C DIVERTED TO LGA AND LAN DED SAFELY. PERFORMED ENGINE RUNS WITH CREW WITH NO DEFECTS NOTED. SUSPECT SEVERE ICING. 2 L 7 2 4F RT A21EA 2007012400105 20070124 00105 EU 2007 1 24 AWXA200700101 1 20070115 A 5320 D53112198201 FITTING AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 602AW 565 SAL - MAJOR REPAIR - CORROSION ON THE R1 DOOR CUT OUT LOWER SILL CENTER FITTING, FR 16+6", S23R. REPLACED THE R1 DOOR C UT OUT LOWER SILL CENTER FITTING, FR 16+6", S23R IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007012400106 20070124 00106 NM 2007 1 24 ABXA070007 1 20070112 A 2421 739515C IDG BOEING 767 767281 1385109 NM LEFT DEFECTIVE A ABXA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 23 793AX 2403 23143 EICAS MESSAGE LEFT GENERATOR OFF DISPLAYED, OIL LIGHT ILLUMINATED. GENERATOR SWITCH RESET DID NOT CORRECT CONDITION. A PU SHUT DOWN AT TOP OF DESCENT, FOLLOWED PROCEDURES WOULD NOT RESET. RESTARTED ON VECTORS FOR THE APPROACH INTO IND, EM ERGENCY AIR DIVERSION. REMOVED AND REPLACED LEFT IDG IAW B767 AMM 24-11-01-4. PERFORMED APU BITE PROCEDURE IAW B767 AM M 49-11-00-12, FIGURE 103. SYSTEM CHECKED GOOD. 2 L 7 2 4F RT A1NM 2007012400111 20070124 00111 SO 2007 1 24 RAIA00701026 1 20070116 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT UNSECURE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 850HK 145003 PRE FLT NR 7983 - IAD - SERVICE DOOR EMERGENCY LIGHT INOP. MAINTENANCE SECURED THE CONNECTOR TO THE LIGHT ASSEMBLY. 2 L 7 2 4T RT T00011AT 2007012400113 20070124 00113 SO 2007 1 24 RAIA00701022 1 20070115 A 7830 WARNING MESSAGE EMB 145 EMB145LR 3260212 SO THRUST REVERSER ACTIVATED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 811HK 145256 FLT NR 5463 - MSN - ENGINE NR 2 THRUST REVERSER EICAS MESSAGE PRESENT. MAINTENANCE DEFERRED THE NR 2 THRUST REVERSER PE R THE MEL. 2 L 7 2 4T RT T00011AT 2007012200098 20070122 00098 NM 2007 1 22 SWAA070235 1 20070117 A 5310 6516352 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007012200099 20070122 00099 2007 1 22 SWAA070236 4 20070117 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007012200106 20070122 00106 NM 2007 1 22 CALA0700015 1 20070114 A 5320 65C34356 SHEAR WEB BOEING 737 737524 1384721 NM BS 482 S26-27L CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14601 27314 INSPECTION FOUND C-1 COMPARTMENT BELTFRAME LOWER SHEAR CLIP CORRODED AT STA 482, S26L TO S27L. THE CORROSION WAS REMOVE D AND A REPAIR WAS INSTALLED IAW SRM 53-00-07, REPAIR 10. 2 L 7 2 4F RT A16WE 2007012200121 20070122 00121 NM 2007 1 22 ASAA0741382 1 20070111 A 5755 SKIN BOEING 737 7374Q8 138447Q NM GROUND SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 LEFT I/B GROUND SPOILER HAS NUMERIOUS DENTS ON LWR SURFACES. PREPPED DENTED AREA, FABRICATED AND INSTALLED REPAIR PIECE S IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007012200138 20070122 00138 NM 2007 1 22 2007UALA00051 1 20070105 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 194UA 26892 EEL INOP AT ROW 25 RIGHT. RELAMPED, OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012200141 20070122 00141 NM 2007 1 22 2007UALA00054 1 20070107 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY EXIT FWD STAIRS ILLUMINATION LIGHT LAMP INOP AND DOOR 3 LEFT FWD EMERGENCY EXIT SILL LIGHT INOP. *S/D* RELAM PED, OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012200146 20070122 00146 NM 2007 1 22 2007UALA00058 1 20070108 A 3397 80603 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 177UA 24384 WALL EEL INOP AT LEFT SIDE FWD GALLEY. REPAIRED FEEDER. OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012200149 20070122 00149 NM 2007 1 22 2007UALA00061 1 20070108 A 3350 9F19948501 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY LIGHT INOP AT DR1R SLIDE AND DR5R SLIDE ILLUM. REPLACED SLIDE EMERGENCY LIGHT. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012200151 20070122 00151 NM 2007 1 22 2007UALA00065 1 20070106 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 583UA 26705 FLOOR MOUNTED EEL LIGHTS INOP FROM ROW 22 TO ROW 29. REPLACED POWER STRIP IN FLOOR TRACK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007012200160 20070122 00160 EU 2007 1 22 2007UALA00074 1 20070109 A 5270 TARGET AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY EXIT OUT OF ADJUST A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 459UA 1192 LT FWD EMERGENCY EXIT ECAM DURING CLIMB PRESSURE NORMAL. [SUP 05-04-07] TARGET FOR PROXIMITY SWITCH FOUND TO BE OUT OF POSITION. READJUSTED PROXIMITY TARGET TO PROPER CLEARANCE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007012200166 20070122 00166 NM 2007 1 22 SWAA070215 1 20070116 A 3350 6556633 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 LEFT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007012200168 20070122 00168 2007 1 22 SWAA070217 4 20070116 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM R2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED AFT GIRT BAR HOOK PER MM . 2 L 7 2 4F RT A16WE 2007012200194 20070122 00194 EU 2007 1 22 MALA070010 1 20070113 A 3350 66363 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 404XJ 340B404 FOUND FLOOR EMERGENCY LIGHT AT SEAT 7A INOP. REMOVED AND REPLACED FLOOR PROXIMITY ESCAPE PATH LIGHT P/N 6636-3 IAW SF3 AMM 33-50-20. 2 L 7 2 4T RT A52EU 2007012200201 20070122 00201 SO 2007 1 22 GUUA01140701 1 20070114 A 3260 12038594001 CONTROL BOX EMB 120 EMB120ER 3260203 SO MLG MALFUNCTIONED A GUUA O OTHER J WARNING INDICATION CR CRUISE 1 SO 29 283AS 120236 FLIGHT: 9180 TCB/FLL DURING FLIGHT LEFT MAIN LANDING GEAR "B" LOOP RED ANNUNCIATOR ILLUMINATED INTERMITTENTLY. CONTINUE D TO FLL LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR CONTROL BOX OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A31SO 2007012200203 20070122 00203 SO 2007 1 22 GUUA01100701 1 20070110 A 3297 120411261 WIRE HARNESS EMB 120 EMB120ER 3260203 SO UPLOCK DAMAGED A GUUA O OTHER J WARNING INDICATION CR CRUISE 1 SO 29 283AS 120236 FLIGHT:9258 FPO/FLL DURING FLIGHT, THE LEFT MAIN LANDING GEAR "B" LOOP RED ANNUNCIATOR ILLUMINATES INTERMITTENTLY. CONT INUED TO FLL LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN LANDING GEAR "B" LOOP UPLOCK PROXIMITY SENSOR AND HARNESS. 2 L 7 2 4T RT A31SO 2007012300013 20070123 00013 NM 2007 1 23 CALA0700021 1 20070119 A 5330 6562125U26 SKIN BOEING 737 7373T0 1384582 NM BS 500D S28R BUCKLED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 47332 23570 INSPECTION FOUND FUSELAGE SKIN BUCKLED WITH STRESSED RIVETS AT BS 500D + 10, S28R, RBL 10. A REPAIR WAS INSTALLED IAW S RM 53-30-12. 2 L 7 2 4F RT A16WE 2007012300022 20070123 00022 NM 2007 1 23 QXEA200700031 1 20070115 A 2910 PRESSURE SWITCH BOMBDR DHC8 DHC8402 1390042 NM HYD SYSTEM UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 412QX 1178 4059 BOI FLIGHT NR 2385: UPON PUSHBACK, FLAP POWER CAUTION LIGHT ILLUMINATED. FLAP HANDLE MOVED TO 15 DEG BUT NO FLAP MOVEME NT INDICATED ON FLAP GAUGE. RAN CHECKLIST, CAUTION LIGHT EXTINGUISHED. THEN RE-ILLUMINATED AGAIN AFTER SELECTING FLAP HANDLE. MAINTENANCE INTEROGATED CDS. FOUND HYD PRESS LOSS FAULT. REMOVED AND REPLACED FPU PRESSURE SWITCH IAW DH8-400 TASK 27-52-01-400-802. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007012300024 20070123 00024 SO 2007 1 23 C2XA07SH005 1 20070121 A 5315 14521700007 FLOORBEAM EMB 145 EMB145EP 3260221 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 SHV - DURING C-CHECK, FS 23 LT OMEGA BEAM I/B L-FLANGE HAS AREA WITH CORROSION. MAINTENANCE REPAIRED LT OMEGA BEAM I/B L-FLANGE FR 23 IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007012300029 20070123 00029 NM 2007 1 23 07FDEA00096 1 20070115 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT WING OUTBOARD FLAP INBOARD HINGE INBOARD AFT HOLE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5750-107761, REPA IR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007012300031 20070123 00031 NM 2007 1 23 07FDEA00098 1 20070115 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT WING OUTBOARD FLAP OUTBOARD HINGE OUTBOARD AFT HOLE FOUND CORRODED. REPAIRED AS PER FEDEX EA 1-5750-107762, REPA IR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007012300032 20070123 00032 NM 2007 1 23 07FDEA00099 1 20070115 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT WING OUTBOARD FLAP OUTBOARD HINGE OUTBOARD CENTER HOLE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5750-107762, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007012300034 20070123 00034 NM 2007 1 23 07FDEA00101 1 20070115 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 M/D CARGO SEAT TRACK (STA 5/0, LT, X=8.5) FOUND FLANGE UNDER FLOOR PANEL CORRODED. REPAIR CARRIED OUT AT M/D CARGO SEA T TRACK (STA 5/0, LH, X=8.5) AS PER SRM 53-70-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007012300037 20070123 00037 EU 2007 1 23 07FDEA00104 1 20070116 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 413FE 397 DURING ACCESS OPENING ON MAIN CARGO DECK CROSS TRACK FS 45,Y1456/Y1956, P/N R53DD1048-200-00, WAS FOUND CRACKED AND NEED TO BE REPLACED TRACK REPLACED PER SRM 51-40-00. 2 L 7 2 4F RT A35EU 2007012300041 20070123 00041 NM 2007 1 23 DHL200776201 1 20070116 A 5754 SKIN BOEING 727 7272M7 138407S NM NT 6 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 762DH 22162 WHILE COMPLYING WITH VISUAL INSPECTION NOTICED NR 6 LE SLAT SKIN AT THE OUTBOARD TRACK ATTACH AREA WITH TWO CRACKS IN CO RNERS. 2 L 7 3 4F A3WE 2007012300056 20070123 00056 NM 2007 1 23 07FDEA00124 1 20070116 A 5330 SKIN BOEING 727 727233 138408A NM BS 288 BULGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 RT EXT FUSELAGE STA 288 BELOW STR 21 HAS A SKIN BULGE. REMOVED DAMAGE AND REPAIRED IAW SRM 53-30-2 FIG 3. 2 L 7 3 4F RT A3WE 2007012300058 20070123 00058 2007 1 23 UPS07148834 4 20070104 A 2565 LEVER AIRBUS A300 A300F4622R 3930360 EU SLIDE ARM BINDING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 120UP 0805 MAIN ENTRANCE DOOR (CREW DOOR) SLIDE ARMING LEVER BINDS WHEN UNLOCKING, SEVERAL ATTEMPTS TO UNLOCK WERE NEEDED TO DISARM THE SLIDE. PERFORMED LUBRICATION ON THE SLIDE ARM/DISARM MECHANISM. 2 L 7 2 4F RT A35EU 2007012300060 20070123 00060 NM 2007 1 23 UPS07648824 1 20070104 A 2131 CONTROLLER BOEING 767 76734AF 1385212 NM CABIN PRESSURE MALFUNCTIONED A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 309UP 27740 UNABLE TO PRESSURIZE AIRCRAFT. FOUND NO POWER ON BOTH CONTROLLERS. RE-ESTABLISH AIRFLOW IN E/E CABIN PRESS CONTROLLERS . FOUND "AC POWER LOSS" AND "NO AIR FLOW" BITE FAULTS ON BOTH CONTROLLERS. C/O VERIFICATION AGAIN AND FOUND BOTH NO FA ULTS. RESET BOTH CONTROLLERS. SYSTEM OK, REF FIM 21-31-00 FIG 103. 2 L 7 2 4F RT A1NM 2007012300070 20070123 00070 NM 2007 1 23 DLM90070048 1 20070119 A 2612 FIRE LOOP DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE LEFT MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 915DN 28367 53395 020031 LEFT ENGINE FIRE DETECT FAULT ILLUMIINATED ON OAP. REPLACED LT ENG DET. PERFORMED HIGH VOLTAGE MEG OHM CHECK ON ALL LT ENG A LOOP WIRES NO FAULTS FOUND FROM CONDUCTOR TO GROUND. REPLACED FAN FIRE DET LOOP A D1-910. REPLACED LOOP D1-911D 1-912D1-914D1-915 NEEDS CHECKOUT 889313 LT ENG A A B FIRE SYS TEST NORMAL AND ENG RUN CKS NORMAL. 2 L 7 2 4F 4 F RT A6WE E40NE 2007012300079 20070123 00079 EU 2007 1 23 AWXA200700100 1 20070114 A 5320 D53480048202 SILL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 602AW 565 SAL - MAJOR REPAIR - CORROSION ON L2 DOOR CUT OUT CENTER FITTING (SHAPE SILL), FR 68 -14", S23L. REPLACED L2 DOOR CUT O UT CENTER FITTING (SHAPE SILL), FS 68 -14", S23L IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007012300144 20070123 00144 NE 2007 1 23 PCSA10520071 2 20070105 A 7314 384300 PUMP BOEING 727 7272K5 138004P NM PWA JT8 JT8D17 52049 NE ENGINE FUEL FAILED A PCSA E ENGINE SHUTDOWN E VIBRATION/BUFFET CL CLIMB 1 SO 17 909PG 649 649 21852 DURING CLIMB FELT VIBRATION, NR 1 ENGINE EPR AND FUEL FLOW DROPPED TO ZERO. NR 1 ENGINE WAS SHUT DOWN AS A PRECAUTIONAR Y MEASURE. SHUTDOWN WAS LESS THAN 30 MINUTES. 2 L 7 3 4F 4 F RT A3WE E2EA 2007012300145 20070123 00145 EU 2007 1 23 TRAX200700099 1 20070109 A 5740 BRACKET AEROSP ATR72 ATR72212 8680945 EU LT WING BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 635AS 372 LT WING AT RIB 8 FWD UPPER INBOARD OMEGA IS BROKEN . 2 H 7 2 4T RT A53EU 2007012300176 20070123 00176 2007 1 23 2007UALA00120 4 20070117 A 2565 SQUIB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT SLIDE NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 549UA 25397 SQUIB TEST 2 EMERG ESCAPE RIGHT NOT TESTING. SERVICED RIGHT OVERWING SLIDE BOTTLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007012400002 20070124 00002 SO 2007 1 24 C2XA07BT005 1 20070116 A 3350 2013BR BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13949 7802 1120 145057 DURING SERVICE/ROUTINE CHECK, FOUND EMERGENCY LIGHT FWD AISLE STRIP INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY NR 2 IAW EMB-145 AMM 33-50-04. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007012400008 20070124 00008 EA 2007 1 24 A6WA200740024 1 20070113 A 3260 TARGET CNDAIR CL600 CL6002B19 1900309 EA MLG OUT OF ADJUST A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 458AW 7861 GEAR DISAGREE WARNING MESSAGE AFTER DEPARTING PHL. COMPLIED WITH QRH. GEAR DOWN 3 GREEN. (M) ADJUSTED RT MLG UPLOCK T ARGET REF CMM 32-30-15, OPS CHECK GOOD. (K) 2 L 7 2 4F RT A21EA 2007012400009 20070124 00009 EA 2007 1 24 A6WA200740025 1 20070114 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 443AW 7781 WHILE IN FLIGHT, FLAPS FAILED AT ZERO WHILE ATTEMPTING TO EXTEND. LANDED FLAPS AT ZERO. NORMAL BRAKING ACTION. BRAKE TEMPS READ 5, 5, 5, 6. RESET PER AMM SUPPLEMENT 98-018A. PLACED ON 72 FLAP WATCH. (M) COMPLIED WITH AMM SUPPLEMENT 9 8-018A, NO FURTHER INCIDENT. (K) 2 L 7 2 4F RT A21EA 2007012400053 20070124 00053 NM 2007 1 24 QXEA200700048 1 20070120 A 5270 SENSOR BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR OUT OF ADJUST A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 414QX 4061 LAX FLIGHT NR 2385: FUSELAGE DOOR MASTER WARNING ILLUMINATED IN CRUISE FLIGHT. CHECKLIST COMPLETED. MAIN CABIN DOOR SH OWING OPEN. PRESSURIZATION APPEARED NORMAL. MAINTENANCE INTERROGATED PSEU AND FOUND PADRKL UNREASONABLY FAR. ADJUSTED PAX DOOR LOCKED SENSOR IAW Q400 AMM TASK 71-01-830-803. PSEU REPORTS PADRKL OD AND INDUCTANCE VALUES IN MIDDLE RANGE A S REQUIRED PER TASK. NO OTHER DEFECTS NOTED. PRESSURIZED AND DEPRESSURIZED AC IAW Q400 AMM TASKS 21-00-00-863-801 AND 21-00-00-863-802. NO LEAKS NOTED. OPS CHECKS GOOD. NO PARTS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007012400059 20070124 00059 WP 2007 1 24 UPS07848880 1 20070105 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 CRACKED RIB IN RT CTR LE AT XFS 410. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2. REPAIR ANGLES IAW SRM 57-02-00 FIG 002, 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2007012400066 20070124 00066 NM 2007 1 24 07FDEA00131 1 20070118 A 5310 WINDOW FRAME BOEING 727 727233 138408A NM BS 950E MAINT ERROR A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 284FE 22621 L - ANGLE ATTACHED TO FS 950E FRAME JUST BELOW WINDOW ON AFT SIDE OF FRAME HAS 1 EACH MISSDRILLED HOLE REMOVED DAMAGE. FABRICATED REPAIR ANGLES, TREATED, PRIMED AND INSTALLED REPAIR PIECES REF SRM 51-30-02 PG 32 AND SRM 51-10-02 PG. 1. CL ASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007012400069 20070124 00069 EU 2007 1 24 07FDEA00134 1 20070117 A 3260 PROXIMITY SENSOR AIRBUS 300 A300F4605R 3930327 EU MLG FAILED A FDEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 663FE 766 APPROACH TO GEG LOWERED LANDING GEAR, ECAM AND LANDING GEAR LIGHTS INDICATED UNSAFE NOSE GEAR. SAME INDICATION ON OVERH EAD PANEL. FOLLOWED QRH, MANUALLY LOWERED GEAR. C/W TSM A300-600-32-30-00 FIGURE 117 STEP 1 PREFORMED FREE FALL EXTEN SION DOORS DID NOT FULLY OPEN ORDERED SEQUENCE VALVE AND UPLOCK ASSEMBLY. REMOVED AND REPLACED PROX DETECTION UNIT. RE MOVED AND REPLACED LEFT AND RIGHT NOSE GEAR SEQUENCE VALVES. REMOVED AND REPLACED NOSE GEAR UPLOCK ASSEMBLY. CYCLED NO SE GEAR 2O TIMES, NO DEFECTS NOTED. TIRES CLEAR OF NOSE GEAR DOORS IAW A300-600 MM 32-31-00-5. 2 L 7 2 4F RT A35EU 2007012400077 20070124 00077 EA 2007 1 24 SWIA200717673 1 20070116 A 3350 BATTERY CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT DISCHARGED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 754SK 10215 AFT - FACING CABIN EMERGENCY LIGHTS CEILING EXIT SIGN AT ROW 12 INOP AND LOWER EMERGENCY LIGHT EXIT SIGN ON LEFT OVERWIN G EXIT INOP. EMERGENCY LIGHT BATTERIES CHARGED. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007012400090 20070124 00090 WP 2007 1 24 UPS07848845 1 20070104 A 5512 SKIN DOUG DC8 DC871F 302199D WP HORIZONTAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C2 LT HORIZ STAB L/E UPPER SKIN CRACKED AT STA XFS 60. CUT OUT DAMAGED AREA ON HORIZ STAB LT L/E UPPER SKIN AT STA XFS 60 IAW SRM 55-02-01-0 FIG 4. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER ON LT HORIZ STAB L/E UP PER SKIN STA XFS 60 IAW SRM 55-02-01-0 FIG 4. 2 L 7 4 4F RT 4A25 2007012400095 20070124 00095 WP 2007 1 24 UPS07848852 1 20070102 A 3350 BATTERY DOUG DC8 DC873F 302199F WP EMERGENCY EXIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND TESTED OK PER MM 33-50-01-2. 2 L 7 4 4F RT 4A25 2007012400100 20070124 00100 NE 2007 1 24 200701121 2 20070108 A 7200 ENGINE EMB ERJ170 ERJ170100SE 3260406 EU GE CF34 CF348E5 30015 NE NR 2 VIBRATION A UHLA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 17 634RW 17000055 GEE193232 FLIGHT 7717 MSP TO IAD ON CLIMB CREW NOTICED HIGH LP VIBRATIONS IN ENGINE TWO. RAN THE QRH AND REDUCED POWER TO THE EN GINE. THE VIBRATIONS REMAINED WITHIN LIMITS AT THE REDUCED POWER. COULD NOT RETURN TO NORMAL POWER WITHOUT THE VIBRATI ONS GOING OUT OF LIMITS. CREW FELT AND HEARD THE VIBRATIONS FROM THE ENGINE. ON DECENT VIBRATIONS REDUCED. ON FINAL D URING POWER CHANGES, CREW NOTICED ERRATIC LP VIBRATIONS IN THE ENGINE. CREW LANDED SAFELY WITH NO OTHER PROBLEMS. ENG D ID NOT EXCEED 4.0 IN TEST RUNS, NO EXCEEDANCE WAS RECORDED, VG SYS CHECKED OUT GOOD, ISSUED DMI FOR 25 FLIGHT CYCLES TO ACCOMPLISH FAN LUBE AS RECOMMENDED BY GE. 2 L 7 2 4F 4 F RT A56NM E00063EN 2007012400114 20070124 00114 SO 2007 1 24 RAIA00701023 1 20070115 A 7830 WARNING MESSAGE EMB 145 EMB145LR 3260212 SO THRUST REVERSER ACTIVATED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 815HK 145048 FLT NR 5481 - STL - NR 1 ENGINE THRUST REVERSER DISAGREE MESSAGE ON THE EICAS. MAINTENANCE DEFERRED THE NR 1 THRUST REV ERSER IAW MEL. 2 L 7 2 4T RT T00011AT 2007012400116 20070124 00116 SO 2007 1 24 RAIA00701025 1 20070116 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO EMERGENCY LIGHT LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 821HK 145068 PRE FLT NR 5502 - STL - EMERGENCY LIGHT AT SERVICE DOOR INOP. MAINTENANCE RESECURED THE CONNECTION TO THE LIGHT ASSEMBL Y. 2 L 7 2 4F RT T00011AT 2007012400117 20070124 00117 EU 2007 1 24 0700053274 1 20070109 A 3610 342D030000 THERMOSTAT AIRBUS 320 A320212 3930322 EU CUSTOMER AIR UNKNOWN A NWAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 01 374NW 26087 2104 1646 AIR ENGINE NR 1 AND NR 2 BLEEDS FAULTED AT FLIGHT LEVEL 390. STARTED LOSING CABIN PRESSURIZATION, ATC CLEARED AND EXECU TED RAPID DESCENT, DURING WHICH CABIN ALTITUDE WENT TO 12500 FEET. BLEEDS RECOVERED AT 10,000 FEET. MASKS WERE NOT DRO PPED, AND AIRCRAFT LANDED UNEVENTFULLY AT DESTINATION. NR 2 BLEED, FAN AIR VALVE AND PNEUMATIC TEMP CONTROL THERMOSTAT (TCT) REPLACED. NR 1 BLEED, BLEED MONITOR COMPUTER (BMC) REPLACED. CHECKS NORMAL. 2 L 7 2 4F RT A28NM 2007012400119 20070124 00119 NM 2007 1 24 0700155528 1 20070118 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 528US 23843 INOPERATIVE EMERGENCY LIGHTS: FLOOR PROXIMITY MIDDLE AND AFT ZONES, AND DOOR 3 RIGHT AND LEFT. REPLACED BATTERY PACK M9 004 PER MM 33-51-00. OPS CHECKS GOOD. 2 L 7 2 4F RT A2NM 2007012400121 20070124 00121 NM 2007 1 24 AWXA200700106 1 20070118 A 5754 65C26602218 WEDGE BOEING 737 7373S3 1384711 NM ZONE 600 DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 PHX - MAJOR REPAIR - RIGHT WING NR 5 SLAT OUTBOARD END LOWER SURFACE WEDGE DELAMINATED, SS 254.27. REPLACED RIGHT WING NR 5 SLAT, SS 124.53 - SS 254.27 IAW B737-300 SRM 27-81-21. 2 L 7 2 4F RT A16WE 2007012400122 20070124 00122 NM 2007 1 24 AWXA200700107 1 20070109 A 5321 D5361060500100 FLOOR PANEL AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 829AW 1563 SAL - MAJOR REPAIR - CORROSION ON MAIN CABIN FLOOR PANEL 222FF, FR 16 - FR 20, -Y1292 TO -Y1732. REPLACED MAIN CABIN FL OOR PANEL 222FF, FR 16 - FR 20, -Y1292 TO -Y1732 IAW AWA TASK CARD C1C53302. 2 L 7 2 4F RT A28NM 2007012400123 20070124 00123 NM 2007 1 24 AWXA200700108 1 20070121 A 5753 D5757114000100 ACCESS PANEL AIRBUS A319 A319132 3930340 NM ZONE 600 DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 829AW 1563 SAL - MAJOR REPAIR - BC-4 CHECK - RIGHT WING OUTBOARD FLAP LEADING EDGE ACCESS PANEL DELAMINATED, BETWEEN RIB 5 AND RIB 6. REPAIRED RIGHT WING OUTBOARD FLAP LEADING EDGE ACCESS PANEL BETWEEN RIB 5 AND RIB 6 IAW AWA ER 25-5753-07021-SS1. 2 L 7 2 4F RT A28NM 2007012400124 20070124 00124 EA 2007 1 24 TRAX200700105 1 20070116 A 5720 ANGLE CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 832AS 7243 RT WING MIDDLE LEADING EDGE, I/B ATTACH ANGLE CRACK. 2 L 7 2 4F RT A21EA 2007012400125 20070124 00125 EA 2007 1 24 TRAX200700106 1 20070116 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 EMERGENCY LIGHTS OFF ANNUNICATOR LIGHT HAS LIGHT BULBS INOP. 2 L 7 2 4F RT A21EA 2007012400131 20070124 00131 EA 2007 1 24 COMA0760032 1 20070117 A 2750 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 720SW 7297 FLIGHT 5438 - FLAPS FAIL CAUTION MESSAGE AT ZERO DEGREES ON TAXI OUT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (G) 1,2,3, (A,B,C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSA GES. 2 L 7 2 4F RT A21EA 2007012400132 20070124 00132 WP 2007 1 24 0700099995 1 20070116 A 5711 SPAR DOUG DC9 DC931 3022065 WP LT WING DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8978E 47327 DURING SPECIAL VISIT AIRCRAFT SUSTAINED DAMAGED FROM LT WING JACK. THE LT WING FRONT SPAR LOWER CHORD, LEADING EDGE LOW ER DOUBLER AND LEADING EDGE RIB WERE DAMAGED. REPAIR WAS ACCOMPLISHED PER EA 99-208716 SECT I, SECTION II TO CALLS FOR A DETAILED FATIGUE ANALYSIS OF REPAIR NO LATER THAN JAN 12, 2009. 2 L 7 2 4F A6WE 2007012400135 20070124 00135 WP 2007 1 24 ABXA070008 1 20070112 A 2170 1808491 COALESCER BAG DOUG DC9 DC932 3022066 WP A/C PACKS DEFECTIVE A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 900AX 47380 PILOT REPORTED OIL ODOR FROM AIR CONDITIONING SYSTEM. REPLACED LEFT AND RIGHT WATER SEPARATOR BAGS IAW DC9 MM 21-20-02. 2 L 7 2 4F A6WE 2007012400136 20070124 00136 NM 2007 1 24 0700136310 1 20070117 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670US 24225 DURING LINE CHECK, FOUND UPPER DECK RT EMERGENCY LIGHT BATTERY PACK INOP. MAINTENANCE REMOVED AND REPLACED BATTERY BACK . OPERATIONAL CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007012400138 20070124 00138 EA 2007 1 24 TRAX200700059 1 20070110 A 5320 SILL CNDAIR CL600 CL6002C10 1390015 EA BS 409-559 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 841AS 7300 LT FUSELAGE PRESSURE DOOR SILL HAS CORROSION FROM FS409+128 TO 559 MULTIPLE LOCATIONS COMPLIED WITH EC/TC REO 601R-53- 41-479, NO FURTHER ACTION REQUIRED REF EC/TC REO 601R-53-41-479 ITEM 7. 2 L 7 2 4F RT A21EA 2007012400139 20070124 00139 EA 2007 1 24 TRAX200700060 1 20070110 A 5320 SILL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 841AS 7300 RT FUSELAGE PRESSURE DOOR SILL HAS CORROSION FROM FS409+128 TO 559 MULTIPLE LOCATIONS COMPLIED WITH EC/TC REO 601R-53-4 1-479, NO FURTHER ACTION REQUIRED REF EC/TC REO 601R-53-41-479 ITEM 7. 2 L 7 2 4F RT A21EA 2007012400140 20070124 00140 EU 2007 1 24 TRAX200700061 1 20070110 A 5712 RIB AEROSP ATR72 ATR72 EU RT WING CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 635AS 372 RT WING, OUTB FLAP, FLAP BEAM AT RIB 14 AFT PICK UP, CORROSION FOUND. REFER TO EXELTECH WORK PACKAGE YUL000164 NRTC 6 00-23 FOR ALL WORK ACCOMPLISHED. RT WING OUTBD FLAP, FLAP BEAM ATRIB 14 AFT PICK UP. CORROSION REMOVED AS PER SRM 51 2 1 42. AND FOUND WITH IN LIMIT S PER SRM 57 53 10 FIG 310 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SP 663 AND FAR 43 APPENDIX A REPAIR ACCOMPLISHED IAW 57 55 10. MATERIA THICKNESS .475" MATERAIL REMOVED .001" WITHIN LIMITS AS PER S RM 57 55 10 FIG 310. 2 H 7 2 4T RT 2007012400141 20070124 00141 EU 2007 1 24 TRAX200700062 1 20070110 A 5720 WEB AEROSP ATR72 ATR72 EU WING CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 635AS 372 CORROSION FOUND ON THE LOWER WEB OF LE 612. REFER TO EXELTECH WORK PACKAGE YUL000164 NRTC 600-28 FOR ALL WORK ACCOMPLI SHED. CORROSION REMOVED AS PER SRM 51-21-42 ON THE LOWER WEB OF L/E 612 AND FOUND WITHIN LIMIT AS PER SRM 51 10 10 REPA IR DETERMINED NOT TO BE A MAJOR REPAIR IAW SP 663 AND FAR 43 APPENDIX A REPAIR ACCOMPLISHED IAW 57 53 10. MATERIA THI CKNESS .080" MATERIAL REMOVED .001" WITHIN LIMITS AS PE SRM 51 10 10...SUPPLEMENTAL - SDR CLOSED 01/23/07... 2 H 7 2 4T RT 2007012400151 20070124 00151 EA 2007 1 24 REXA200700005 1 20070123 A 2611 PU90421R3 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FALSE INDICATION A REXA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 8942A 7942 ON APPROACH TO DTW, RECEIVED LAVATORY SMOKE MESSAGE. QRH FOLLOWED, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. SMO KE MESSAGE DETERMINED TO BE FALSE. LAVATORY SMOKE DETECTOR REPLACED IAW BOMBARDIER AMM 26-16-01. OPERATIONALLY CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007012400154 20070124 00154 EA 2007 1 24 REXA200700008 1 20070122 A 2150 ACM CNDAIR CL600 CL6002B19 1900309 EA CONTAMINATED A REXA A UNSCHED LANDING C B J F.O.D. SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 25 8970D 7970 AIR RETURN TO SWF, AFTER RECEIVING SMOKE TOILET MESSAGE ON TAKEOFF. GROUND RUNS AND OPERATIONAL CHECKS OF ACM SYSTEM PE RFORMED NO DEFECTS. DETERMINED TO BE RESIDUAL DE-ICE FLUID INTO ACM SYSTEM. 2 L 7 2 4F RT A21EA 2007012400155 20070124 00155 2007 1 24 QXEA200700049 4 20070122 A 2310 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM ARCDU UNKNOWN A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 415QX 4081 BOI FLIGHT NR 2300, NR 1 ARCDU FAIL MESSAGE APPEARED ON NR 1 ARCDU. RAN CHECKLIST AND SYSTEM RETURNED TO NORMAL. REPOR TED BY CREW THAT THE NR 1 ARCDU IS OPERATING NORMALLY. NO FURTHER ACTION REQUIRED. AIRCRAFT OK FOR CONTINUED SERVICE. 2 H 7 2 4T RT A13NM 2007012400156 20070124 00156 NM 2007 1 24 AWXA200700109 1 20070115 A 5730 SKIN BOEING 737 7373S3 1384711 NM ZONE 600 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 MCN - MAJOR REPAIR - C-19 CHECK, CRACKS FOUND ON NR 6 SLAT BOTTOM SKIN AT SLAT STA 300 - 351. REPAIRED CRACKS ON NR 6 S LAT BOTTOM SKIN AT SLAT STA 300 - 351 IAW B737-300 SRM 57-43-01-2R6, FIG 201. INSTALLED COVE PANEL IAW B737 AMM 20-50-1 1-2, FIG 202. INSTALLED SEAL AND SEAL RETAINER IAW B737 AMM 20-50-11-2, FIG 202. 2 L 7 2 4F RT A16WE 2007012400157 20070124 00157 NE 2007 1 24 0700219953 2 20070121 A 7230 COMPRESSOR DOUG DC9 DC931 3022065 WP PWA JT8 JT8D15 52051 NE NR 1 ENGINE STALLED A NWAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 01 918RW 47158 695303 DURING TAKEOFF ROLL, AT APPROXIMATELY 100KTS, NR 1 ENGINE COMPRESSOR STALLED. TAKEOFF WAS ABORTED AND THE AIRCRAFT SKID DED OFF THE RUNWAY. THE AIRCRAFT IS BEING REPAIRED AND THE NR 1 ENGINE IS BEING REPLACED. 2 L 7 2 4F 4 F A6WE E2EA 2007012400158 20070124 00158 EA 2007 1 24 REXA200700006 1 20070122 A 2150 ACM CNDAIR CL600 CL6002B19 1900309 EA CONTAMINATED A REXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 839AY 8039 PERFORMED RETURN TO YOW AFTER RECEIVING SMOKE TOILET MESSAGE AFTER TAKEOFF. INVESTIGATED AIRCRAFT FOUND TO BE RESIDUAL DE-ICE FLUID HAD ENTERED ACM PACKS. PERFORMED GROUND OPERATIONAL CHECKS WITH NO DEFECTS. 2 L 7 2 4F RT A21EA 2007012400159 20070124 00159 NM 2007 1 24 HALA0700033 1 20070122 A 2410 755359C IDG BOEING 767 76733A 1385209 NM LEFT UNKNOWN A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 591HA 33423 BTB - LEFT GEN CONTROL LIGHT ON TRIED TO RESET, NO RESET. "LEFT FGEN TRIPPED DIODE" FAULT ON BCU. REMOVED IDG PER AMM 24-11-01. INSTALLED NEW IDG LEFT ENG PER MM 24-11-01. GRD RUN OPS/LEAK CHK OK. BITE CHK BPCU, NO DEFECTS NOTED. 2 L 7 2 4F RT A1NM 2007012400163 20070124 00163 EA 2007 1 24 SWIA200717681 1 20070116 A 3350 20131A POWER SUPPLY CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 802SK 15061 FORWARD MOUNTED CEILING EXIT SIGN, FLOOR LEVEL EXIT SIGNS AT OVERWING EMERGENCY EXITS AND EXIT SIGNS ON CLOSET ON ROW 4 BOTH FWD AND AFT FACING ARE ALL INOP. REPLACED NR 3 EMERGENCY BATTERY PACK IAW MM 33-51-17. OPERATIONAL CHECKS GOOD, S N OFF 43882. 2 L 7 2 4F RT A21EA 2007012400164 20070124 00164 SO 2007 1 24 SWIA200717682 1 20070117 A 3350 BULB EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 288SW 120316 EMERGENCY FLOOR LIGHT AT ROW 11A IS NOT WORKING. REPLACE LIGHT BULB ON FLOOR EMERGENCY LIGHT AT SEAT 11A. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007012400165 20070124 00165 EA 2007 1 24 SWIA200717683 1 20070119 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 754SK 10215 OVERWING EMERGENCY LIGHTS INOP. REPLACED OVERWING EMERGENCY BATTERY PACK. OPERATIONAL CHECKS GOOD, SN OFF 40211. 2 L 7 2 4F RT A21EA 2007012400166 20070124 00166 EA 2007 1 24 SWIA200717684 1 20070121 A 5210 601R945563 MOTOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 913EV 7731 MAIN CABIN DOOR WOULDN'T OPEN ALL THE WAY. REPLACED PASSENGER DOOR MOTOR ASSIST IAW MM 52-11-08. OPERATIONAL CHECKS GO OD, SN OFF 0436. 2 L 7 2 4F RT A21EA 2007012400167 20070124 00167 SO 2007 1 24 SWIA200717685 1 20070119 A 6120 78249046 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PROPELLER FLUCTUATES A SWIA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 07 218SW 32559 11135 7731 RIGHT PROPELLER (NP) FLUCTUATING (ANALOG AND DIGITAL) ERRATICALLY AFTER TAKEOFF. REPLACED RIGHT PROP CONTROL UNIT IAW E MB-120 MM 61-21-00 AND C/W RII 61-900-1003. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007012400168 20070124 00168 SO 2007 1 24 SWIA200717686 1 20070115 A 3320 BULB EMB 120 EMB120ER 3260203 SO CABIN LIGHTS OVERHEATED A SWIA O OTHER M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 226SW 120296 ELECTRICAL SMELL AT ROW 7 IN CABIN. REPLACED CABIN OVERHEAD BULBS AT ROW 7. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007012400169 20070124 00169 SO 2007 1 24 SWIA200717687 1 20070118 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 308SW 120326 NR 10 STRINGER CRACKED BETWEEN RIBS NR 8 AND NR 9 AT RIGHT INBOARD WING, DISCOVERED DURING C-CHECK INSPECTION. REPAIRED NR 10 STRINGER BETWEEN RIBS NR 8, NR 9 INSIDE RIGHT WING IAW SRM 57-20-03 AND RII CARD 57-900-1000. 2 L 7 2 4T RT A31SO 2007012400170 20070124 00170 SO 2007 1 24 SWIA200717688 1 20070118 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 308SW 120326 LEFT FLOORBEAM AT FRAME 13 CRACKED BOTH SIDES, DISCOVERED DURING C-CHECK INSPECTION. SPLICED IN REPLACEMENT SECTION PER EMB 120 SRM 53-10-10. SEE RII 53-800-1000. 2 L 7 2 4T RT A31SO 2007012400171 20070124 00171 SO 2007 1 24 SWIA200717689 1 20070118 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 308SW 120326 RIGHT FLOORBEAM AT FRAME 13 ANGLE, INBOARD SIDE, CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED SUPPORT ANGLE AT FRAME 13A FLOOR PROP, INBOARD SIDE OF RIGHT FLOOR PROP PER EMB 120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2007012400172 20070124 00172 NM 2007 1 24 QXEA200700050 1 20070120 A 2750 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 412QX 4059 GEG FLIGHT NR 2393, FLAP POWER CAUTION LIGHT ILLUMINATED DURING ENGINE START WHILE PUSHING BACK FROM THE GATE WITHOUT FL AP LEVER INPUT. MAINTENANCE PERFORMED FIM TASK 27-50-00-810-802. CONTINUOUS BIT, CONTINUSOUS BIT FLAP DRIVE SYSTEM-SYS TEM CAL: L TRANSDUCER 2, R TRANSDUCER 1, FLAP LEVER TRANSDUCER 100. CLEARED NVM, FLAPS CYCLED THROUGH THE OPS TEST 3 TI MES WITH NO DEFECTS NOTED. FLAP POWER CAUTION DID NOT RETURN. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007012400173 20070124 00173 NM 2007 1 24 QXEA200700051 1 20070121 A 3260 401020101 SENSOR BOMBDR DHC8 DHC8402 1390042 NM MLG FAILED A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 410QX 4053 BOI FLIGHT NR 2403: NOSE AND MLG FAILED TO RETRACT AFTER LANDING GEAR HANDLE SELECTED UP. NO INTRANSIT LIGHT, 3 GREEN L IGHTS AND 3 RED LIGHTS. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INTERROGATED PSEU AND FOUND NWSCENT UNREASONABLY FAR I N FAULT HISTORY. CHECKED GAP OF NWCENT PROX SENSOR AND COMPARED IT TO THE INDUCTANCE LIMITS. FOUND THE INDUCTANCE OUT OF LIMITS AT 8.047 WITH TARGET AT NEAR CONDITION. INSTALLED NEW NWCENT PROX SENSOR IAW WM STANDARD PRACTICES 20-17-10. RIGGED NWCENT PROX SENSOR IAW 32-61-06-830-801. NEW INDUCTANCE VALUE IS 8.527. CHECKED CLEARANCE OF NLG HARNESS PER R IL84-32-42. CLEARANCE CHECKED GOOD. INSTALLED CLAMP FOR NWCENT/WOW2 HARNESS CONNECTOR 32-61 P32 IAW Q400 AMM. LANDING 2 H 7 2 4T RT A13NM 2007012400174 20070124 00174 EU 2007 1 24 AWXA200700110 1 20070119 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHTS FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 624AW 055 PHX - EEL - EMERGENCY EXIT LIGHTS TEST FAILS-INT. LOADS EMERG. L, AND COMM EMERG L. MX REMOVED AND REPLACED THE LEFT MID EMERGENCY POWER SUPPLY UNIT IAW MM 33-51-38PB401. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007012400175 20070124 00175 2007 1 24 AWXA200700111 4 20070122 A 2565 D30665109 SLIDE AIRBUS 320 A320231 3930325 EU RT CABIN DOOR NO TEST A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 634AW 33305 1267 091 LAS - EE - EMERGENCY EXIT LIGHT TEST FAILED FOR LEFT AFT EXT LOAD FAULT (STEP 6 OF T/C I8M05334). MX REMOVED AND REPLAC ED AFT RT CABIN DOOR SLIDE ASSY PER T/C R1C25305. MX PERFORMED EMERG EXIT LIGHT TEST PER STEP 6 OF T/C I8M05334. OPS C HECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007012400176 20070124 00176 NM 2007 1 24 AWXA200700112 1 20070122 A 3350 321431 BATTERY PACK BOEING 737 7373G7 1384595 NM EMERGENCY LIGHTS FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 157AW 23779 PHX - EEL - EMERGENCY EXIT LIGHT ROW 2 LT INOP (ESCAPE PATH). MX REMOVED AND REPLACED SEAT MOUNTED LIGHT ASSY, BATTERY PACK, AND CHARGER M 01133, OPS CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2007012500001 20070125 00001 WP 2007 1 25 ASMF200701002 1 20070108 A 2797 P1041 CONNECTOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE STAB TRIM INTERMITTENT W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 838AM 49397 DURING TRANSIT CHECK, THE ALT LONG TRIM STABILIZER WAS OUT OF SERVICE. CIRCUIT BREAKER WAS RESEATED BUT FAILURE CONTINUE D. AIRCRAFT WAS SENT TO THE HANGAR AND DURING WIRING CHECK WAS DETECTED THE CONNECTOR P10-41 PIN A WITH INTERMITTENT CON TACT. PIN A WAS REPLACED IAW WDM 27-42-01 AND THE STABILIZER WAS ADJUSTED AND TESTED IAW MM 27-40-09 AND MM 22-01-01, RE SPECTIVELY, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007012500006 20070125 00006 CE 2007 1 25 DXTA200701839 1 20070105 A 3411 PITOT TUBE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CONTAMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 924QS 7500124 (YD OFF LOWER) AND MACH TRIM OFF OCCURED DURING TAKEOFF, ABORTED TAKEOFF AND COMPLIED WITH CHECKLIST. SECOND ATTEMPT, ID ENTIICAL MESSAGES APPEARED. FOUND WATER IN BOTH PITOT TUBES. PURGED SYSTEM AND PERFORMED PITOT LEAK CHECK IAW MM 34-11-0 8 AND FAR 91-411- SYSTEM. OPS CHECKS SERVICEABLE. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007012500008 20070125 00008 NM 2007 1 25 AWXA200700046 1 20070107 A 5754 WEDGE BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE ZONE 500 DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 292 23634 MAJOR REPAIR - C-21 CHECK - NR 5916465, LT WING NR 3 SLAT WEDGE UPPER AND LOWER SURFACE DEBONDED, SS 50 -SS 80. REPLACE D LT WING NR 3 SLAT IAW AMM 27-81-00-5. 2 L 7 2 4F 4 F RT A16WE E2GL 2007012500013 20070125 00013 NM 2007 1 25 KCSA071021 1 20070116 A 5340 FITTING BOEING 747 747209F 1384800 NM PWA JT9 JT9D7R4G2 52054 NE BS 2360 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 B.S. 2360 PRESSURE BULKHEAD STR 38L END FITTING IS CORRODED ON FORWARD SIDE. 2 L 7 4 4F 4 F RT A20WE E3NE 2007012500014 20070125 00014 NE 2007 1 25 COMA0770005 2 20070123 A 7320 4120T02P03 ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE RT ENGINE MALFUNCTIONED A COMA K NONE R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 SO 01 369CA 3819 10079 FLIGHT 4950 - RIGHT ENGINE REVERTED TO IDLE WITH RIGHT FADEC MESSAGE AND HIGH TEMP OF 790. DECLARED EMERGENCY AND LANDE D WITHOUT INCIDENT. REPLACED RIGHT ENGINE MASTER VG ACTUATOR. NO FURTHER DEFECTS. 2 L 7 2 4F 4 F RT A21EA E00063EN 2007012500015 20070125 00015 NE 2007 1 25 BAQA200700002 2 20070111 A 7200 TURBINE WHEEL AEROSP AS365 AS365N2 8680815 EU TMECA ARRIEL ARRIEL2B NE NR 1 ENGINE DAMAGED E BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 520CF 6537 24003 DURING MAINTENANCE GROUND RUNS, STARTED NR 1 ENGINE AND NR 2 ENGINES TO PERFORM REQUIRED MAINTENANCE CHECKS AFTER INSPEC TION OF AIRCRAFT AND ENGINES. SHUTDOWN ENGINES TO MAKE TAILROTOR BLADE WEIGHT CHANGE. ATTEMPTED TO START NR 1 ENGINE AND IT WOULD NOT TURN. ATTEMPTED TO MANUALLY ROTATE COMPRESSOR AND COULD NOT. REMOVED STARTER/GENERATOR AND ATTEMPTED TO TURN COMPRESSOR. STILL WOULD NOT TURN. AFTER ENGINE COOLED DOWN, WAS ABLE TO TURN COMPRESSOR BY HAND AND HEARD TURBINE RUB. HP TURBINE DISK IS RUBBING. CHANGING MODULE 2 AND 3 OF EFFECTED ENGINE. PILOT REPORTED NO ABNOMALIES DURING FIRS T RUN OF NR 1 ENGINE. 1 G 7 2 3U 3 U RT H10EU E00054EN 2007012500016 20070125 00016 2007 1 25 DXTA200701842 4 20070108 A 2210 SQUAT SWITCH BEECH MU300 400A 1155402 CE AUTOPILOT SYS DISCONNECTED E DXTA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 GL 07 139QS RK483 AUTOPILOT WILL NOT FOLLOW HEADING BUG COMMAND. FOUND BOTH SQUAT SWITCHES DISCONNECTED. RECONNECTED BOTH SQUAT SWITCHES IAW MM 32-60. PERFORMED OPERATIONAL CHECK OF AUTOPILOT. OP CHECKS GOOD. 2 H 7 2 4F RT A16SW 2007012500017 20070125 00017 NE 2007 1 25 COMA0770006 2 20070123 A 7320 4123T31G01 SENSE LINE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE RT ENGINE FAULTY A COMA K NONE R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 SO 01 369CA 10079 FLIGHT 4950 - RIGHT ENGINE REVERTED TO IDLE WITH RIGHT FADEC MESSAGE AND HIGH TEMP OF 790. DECLARED EMERGENCY AND LANDE D WITHOUT INCIDENT. REPLACED RIGHT ENGINE P3 LINE. NO FURTHER DEFECTS. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007012500019 20070125 00019 WP 2007 1 25 ABXA070010 1 20070102 A 5312 5910130 BULKHEAD DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 AFT PRESSURE BULKHEAD LEFT LOWER CORNER WAS CRACKED. REPAIRED AREA IAW DC9 REA D953-55282MR. 2 L 7 2 4F A6WE 2007012500024 20070125 00024 EU 2007 1 25 SA07006 1 20070122 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 712US 23456 1038 DCA - THE AFT EMERGENCY POWER SUPPLY UNIT FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE AFT EMERGENCY POWE R SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007012500025 20070125 00025 NM 2007 1 25 KCSA071019 1 20070116 A 5340 FITTING BOEING 747 747209F 1384800 NM PWA JT9 JT9D7R4G2 52054 NE BULKHEAD CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 B.S. 2360 PRESSURE BULKHEAD STR 48R END FITTINGS ARE CORRODED ON FORWARD AND AFT SIDES. 2 L 7 4 4F 4 F RT A20WE E3NE 2007012500026 20070125 00026 EU 2007 1 25 SA07005 1 20070112 A 2120 87292325V06 COMPUTER AIRBUS A319 A319112 3930323 EU E&E BAY FAILED A USAA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 EA 19 767UW 706 1382 PHL FLT 1190 EN ROUTE PHX TO PHL. CREW RECEIVED AN AVIONICS SMOKE WARNING ON ECAM. THE CREW SELECTED THE VENT BLOWER TO OVER-RIDE. THE WARNING CANCELLED AND THE STATUS PAGE INDICATED VENT BLOWER INOPERATIVE. THE AVIONICS SMOKE WARNING RETURNED AGAIN PRIOR TO ARRIVAL IN PHL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED A BITE CHECK OF THE AEVC COMPUTER. NO FAULTS WERE NOTED. OK FOR SERVICE. SUBSEQUENT INFO: MAINTENANCE REPLACED THE AVIONICS EQUIPME NT VENTILATION COMPUTER ON 1/19/07. 2 L 7 2 4F RT A28NM 2007012500027 20070125 00027 EA 2007 1 25 COMA0760034 1 20070120 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 SO 01 812CA 17632 7381 FLIGHT 5168 - FLAPS FAIL MESSAGE WHEN SELECTING 30 DEGREES. FAILED AT 20 DEGREES. REMOVED AND REPLACED RIGHT BPSU. 2 L 7 2 4F RT A21EA 2007012500029 20070125 00029 EA 2007 1 25 COMA0760036 1 20070119 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE F FLT CONT AFFECTED LD LANDING 1 SO 01 477CA 7670 FLIGHT 5397 - FLAPS FAILED AT 27 DEGREES DURING FLAP RETRACTION ON THE GROUND. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007012500036 20070125 00036 SO 2007 1 25 RAIA00701010 1 20070108 A 3350 RPSB1 BATTERY EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT DISCHARGED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 802HK 145066 PRE FLT NR 3574-STL-OVERHEAD EMERGENCY EXIT CEILING LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGH T BATTERY. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007012500037 20070125 00037 NM 2007 1 25 USAA200701004 1 20070119 A 5320 TIE CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 526AU 23861 A 1 INCH CRACK FOUND AT STA 294.5, STR 11, CLIP. REMOVED & REPLACED CRACKED TIE CLIP PER EO 5305V203 (DROP-IN A/C). 2 L 7 2 4F RT A16WE 2007012500041 20070125 00041 CE 2007 1 25 DJFA2007009 1 20070115 A 5511 45A11965 SUPPORT BRACKET BEECH BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE LT HORZ STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 482LX 1321 RK413 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE LT IB HORIZONTAL STA BILIZER RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. SD R WILL BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION. MAINTENANCE REPLACED THE RIB ASSEMBLY. 2 H 7 2 4F 4 F RT A16SW E25EA 2007012500043 20070125 00043 NM 2007 1 25 USAA070054 1 20070122 A 5522 65C25746131A SKIN BOEING 737 737301 1384611 NM LT ELEVATOR PEELING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 23742 PEELING FABRIC LT ELEV AT MOUNT FLANGE OF LEADING EDGE ACCESS PANEL 9143L. REMOVED DAMAGE & INSTALLED FILLER PLIES PER SRM 51-70-17 & EA 98399, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007012500044 20070125 00044 NM 2007 1 25 USAA070045 1 20070122 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 589US 23934 BS 727E AND S-21R CRACKED. INSTALLED REPAIR DOUBLER 12' X 10" PER SRM 53-00-01 FIG 201, DEFECT SIZE: 4 INCHES. 2 L 7 2 4F RT A16WE 2007012500046 20070125 00046 NM 2007 1 25 USAA070047 1 20070122 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 23742 STA 785 - 847 RBL 14 HAS CORROSION. REMOVED DAMAGE & INSTALLED FAB'D PARTS PER SRM 53-00-53, FIG 201; CORR LEVEL 2; TAS K C53-100-01, DEFECT SIZE: 65 INCHES. 2 L 7 2 4F RT A16WE 2007012500047 20070125 00047 NM 2007 1 25 USAA070048 1 20070122 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 23742 FRAME AT STA 947.5 UNDER AFT EDGE OF WATER TANK, STR 27 HAS CORROSION. ACCOMPLISHED DOUBLER REPAIR PER EA 98405. DEFEC T SIZE: 4-5 INCHES LONG X 3-4 INCHES HIGH. 2 L 7 2 4F RT A16WE 2007012500049 20070125 00049 NM 2007 1 25 SWAA070282 1 20070120 A 3350 65C34691 LIGHT BOEING 737 7373A4 1384585 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 BULL NOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 19 DEF. SECURED LIGHT ASSY AND REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007012500050 20070125 00050 NM 2007 1 25 SWAA070283 1 20070120 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 409WN 27896 DURING SCHEDULED RON CHECK, FOUND EEPLS LIGHT COVER MISSING AT ROW 11 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007012500051 20070125 00051 NM 2007 1 25 SWAA070284 1 20070120 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 380, STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007012500052 20070125 00052 NM 2007 1 25 SWAA070285 1 20070120 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 24L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007012500054 20070125 00054 NM 2007 1 25 SWAA070287 1 20070120 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 14R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007012500055 20070125 00055 NM 2007 1 25 SWAA070288 1 20070120 A 5330 6550570 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007012500058 20070125 00058 NM 2007 1 25 SWAA070291 1 20070120 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER SRM. 2 L 7 2 4F RT A16WE 2007012500060 20070125 00060 NM 2007 1 25 SWAA070293 1 20070120 A 5330 6545766 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 290, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007012500061 20070125 00061 NM 2007 1 25 SWAA070294 1 20070120 A 5313 BAC1498 STRINGER BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND STRINGER 24R CORRODED AT BS 848. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007012500062 20070125 00062 NM 2007 1 25 SWAA070295 1 20070120 A 5313 BAC1498 STRINGER BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND STRINGER 23R CORRODED AT BS 848. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007012500065 20070125 00065 NM 2007 1 25 SWAA070268 1 20070119 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 909, STR 3L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007012300017 20070123 00017 WP 2007 1 23 ABXA070011 1 20070103 A 5347 S2914913M24000 SEAT TRACK DOUG DC9 DC941 302207N WP BS 224-232 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 FLOOR TRACK CORRODED AT STA 224 - 232, RIGHT BUTT LINE 54. REMOVED AND REPLACED TRACK IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 2007012300035 20070123 00035 NM 2007 1 23 07FDEA00102 1 20070116 A 3230 LANDING GEAR BOEING 727 727277 138408S NM FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 244FE 21647 LANDING GEAR FAILED TO RETRACT NORMALLY. FOLLOWED QRH PROCEDURE TEST 1: INTERMITTENT HORN SOUNDED WHEN RETRACTING FLAPS FROM 5' TO 2'. UNABLE TO TEST WING ANTI-ICE DUE TO SYSTEM OPERATING ALREADY. NOSEWHEEL STEERING ALIGNMENT APPEARED NO RMAL. QRH STATES STRUTS NOT EXTENDED. RETURNED FOR NORMAL LANDING. 2 L 7 3 4F RT A3WE 2007012300045 20070123 00045 WP 2007 1 23 07FDEA00109 1 20070116 A 5347 SEAT TRACK DOUG DC10 DC1030 3023501 WP BS 745-949 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 MAIN CABIN FROM STA 745 TO STA 949 X= -47 RT 6 EA EXISTING SEAT TRACK SPLICE. REMOVED SEAT TRACK SPLICE IAW SRM 51-30-0 0 VOL 2. REMOVED CORROSION (LIGHT) IAW SRM 51-21-01 PAGE 28 ORIGINAL THK IS .50" IAW SRM 53-70-00 FIG 1 SHEET 2 AND DWG S4932154, RESIDUAL THK IS .492" 1,6% MAT REMOVED. REPAIR IS WITHIN LIMITS IAW SRM 51-21-01 PAGE 28. TREATED REWORKED AREA IAW SRM 51-21-01 WITH ALODINE AND PRIMER. REINSTALLED SPLICE IAW SRM 51-30-00 VOL 2. 2 L 7 3 4F A22WE 2007012300049 20070123 00049 WP 2007 1 23 07FDEA00116 1 20070116 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1099-1521 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 LOWER FUS EXT SKIN MODERATE PITTING CORROSION FROM STA 1099 TO STA 1521 FROM L 48 LT TO L 48 RT. REPAIRED AREA STA 1268 AND STA1329 IAW SRM 53-40-00 FIG 20 SHT 1&4 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01728/I026728 IAW SRM 5 3-40-00 FIG 20 SHT 4 VOL 1. 2 L 7 3 4F A22WE 2007012300051 20070123 00051 WP 2007 1 23 07FDEA00118 1 20070116 A 5310 BEAM DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 AFT CARGO COMPT AREA FOUND CORROSION WITH EXFOLIATION ON BEAM AT STA 1902 BTWN X=0 CTR & X= 20 LT. REPAIRED BEAM IAW SR M 53-00-01 VOL 1 FIG 8. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I025371/N00371 IAW SRM 53-30-00 VOL1 FIG 5 AND SRM 5 3-00-01 VOL 1 FIG 8. 2 L 7 3 4F A22WE 2007012300074 20070123 00074 SO 2007 1 23 RAIA00701027 1 20070118 A 5270 UNKNOWN EMB 145 EMB145 3260210 SO PAX DOOR WARNING LIGHT A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 806HK 145112 FLT NR 3521 - RIC - MAIN DOOR WARNING DURING TAKEOFF ROLL. MAINTENANCE DEFERRED THE DOOR INDICATING SYSTEM AS PER THE M EL. 2 L 7 2 4F RT T00011AT 2007012300088 20070123 00088 NM 2007 1 23 TSAA0727007 1 20070115 A 2751 90004212 SENSOR BOEING 737 73773A 1384606 NM TE FLAPS FAILED A TSAA O OTHER N FALSE WARNING DE DESCENT 1 WP 13 739AL 28500 ETOPS FLIGHT 476 OGG-SAN - WHEN CREW MOVED THE FLAP LEVER, THE FLAPS WOULD NOT DEPLOY DUE TO ASYMMETRY INDICATION. CREW DECLARED AN EMERGENCY AND DETERMINED 2 DEGREES OF FLAPS WAS REQUIRED FOR LANDING. CREW USED ALTERNATE FLAP SETTING TO DEPLOY FLAPS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE FLAP SKEW SENSOR FAILED AND REMOVED AND REPLACE D THE SENSOR PER AMM 27-59-00-730-801. FLAP SYSTEM PASSED ALL OPERATIONAL CHECKS PER AMM 27-59-00-730-801 AND THE AIRCR AFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007012300093 20070123 00093 EA 2007 1 23 TRAX200700037 1 20070106 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 349 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 841AS 7300 FOUND STA 349 TRANSVERSE BEAM CORRODED RT SIDE AT RBL 45 (MARKED). REMOVED CORROSION AND FOUND WITHIN LIMITS IAW CRJ SR M 53-21-15 AND REPLACED AFT ANGLE IAW CRJ SRM 51-42-13. 2 L 7 2 4F RT A21EA 2007012400004 20070124 00004 NM 2007 1 24 0700125642 1 20070116 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHT DISCHARGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 542US 26489 EMERGENCY LIGHT AT DOOR 2L AND EMERGENCY PROXIMITY LIGHTS AT PASSENGER SEATS 20-23 INOPERATIVE. REPLACED EMERGENCY BATT ERY PACK AND BATTERY AT DOOR 2L CEILING. FLOOR TRACK EMERGENCY LIGHTS CHECK NORMAL. 2 L 7 2 4F RT A2NM 2007012400007 20070124 00007 EA 2007 1 24 A6WA200740010 1 20070110 A 4930 O-RING CNDAIR CL600 CL6002B19 1900309 EA FCU LINE LEAKING A A6WA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 31 444ZW 7788 WITH BLEEDS SUPPLIED BY APU, STRONG FUEL ODOR NOTED. WITH BLEED SON ENGINE, NO ODOR NOTED. FOUND FUEL LEAKING FROM FCU ELBOW/NUT FITTING. REMOVED AND REPLACED O-RING. LEAK CHECK GOOD. NO FUEL SMELL NOTED. RED AMM 49-30-01. (M) 2 L 7 2 4F RT A21EA 2007012400010 20070124 00010 EA 2007 1 24 A6WA200740009 1 20070109 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS UNKNOWN A A6WA O OTHER J WARNING INDICATION AP APPROACH 1 GL 31 443AW 7781 FLAPS FAIL YELLOW CAUTION MESSAGE IN FLIGHT. LANDED AT FLAPS ZERO. (M) 2 L 7 2 4F RT A21EA 2007012400022 20070124 00022 NM 2007 1 24 CALA0700026 1 20070117 A 5347 151W6294 SEAT TRACK BOEING 777 777224 1385225 NM BS 1520-1546 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 78005 27581 INSPECTION FOUND SEAT TRACK FLANGE CORRODED AT STA 1520-1546, RBL 74. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52, REP AIR 3. 2 L 7 2 4F RT T00001SE 2007012400041 20070124 00041 EA 2007 1 24 TRAX200700103 1 20070115 A 7830 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER ILLUMINATED A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 981EV 7768 RT REV UNLOCK MSG IN FLT. EN ROUTE TO ATL, A/C DIVERTED TO TYS DUE TO MTC. EMERGENCY DECLARED. REPLACED RT ENG T/R PD U. OPS CHECK GOOD. DML CLEARED PLACARD REMOVED. 3 MAN HRS. 2 L 7 2 4F RT A21EA 2007012400042 20070124 00042 EU 2007 1 24 AWXA200700059 1 20070110 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHT FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 637AW 15660 3264 099 LAS - EEL - EMERGENCY EXIT LIGHT TEST FAILS LT SIDE. MX REMOVED AND REPLACED LT EMERGENCY LIGHT POWER SUPPLY PER AMM 33 -51-38 PG 401. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007012400051 20070124 00051 NM 2007 1 24 AWXA200700097 1 20070114 A 2750 UNKNOWN BOEING 737 7373G7 1384595 NM TE FLAPS UNKNOWN A AWXA O OTHER J WARNING INDICATION AP APPROACH 1 WP 28 157AW 23779 FLIGHT 391: SEA - LAS - WHEN SELECTING FLAPS 25, AIRCRAFT ROLLED MODERATELY TO THE LEFT, FLAP INDICATOR INDICATED 15 (LE FT) AND 23 (RIGHT). FLAP INDICATION THEN RETURNED TO NORMAL (BOTH INDICATING 25). FLAPS 40 WERE THEN SELECTED. THE C REW DECLARED AN EMERGENCY. THE LANDING WAS UNEVENTFUL. MX REMOVED LT O/B FLAP FWD FAIRINGS AND VISUALLY INSPECTED FLAP TRACKS AND ATTACH POINTS NO DEFECT WAS NOTED OPERATED FLAP SEVERAL TIMES. OPS CHECK WAS GOOD. MX REINSTALLED FAIRINGS AND SECURED. MX REMOVED LT INBD T/E FLAP FAIRING, INSPECTED BOOM CABLE FOR BREAKAGE, NO DEFECTS NOTED. MX REINSTALLED FAIRING. AS A PRECAUTION, MX REPLACED THE FLAP POSITION INDICATOR. 2 L 7 2 4F RT A16WE 2007012400054 20070124 00054 2007 1 24 UPS07148887 4 20070118 A 2565 HANDLE AIRBUS 300 A300B4622R 3930312 EU PAX DOOR SLIDE STIFF A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 120UP 0805 CABIN DOOR EVA SLIDE DISARM HANDLE VERY HARD TO MOVE. DEFERRED MAIN CABIN DOOR SLIDE IAW MEL 52-11-01-3. ACCOMPLISHED DMP 52-11-01-3. SLIDE NEEDS NOT BE REMOVED. DMI OPENED. 2 L 7 2 4F RT A35EU 2007012400078 20070124 00078 EA 2007 1 24 SWIA200717674 1 20070115 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 453SW 7743 FORWARD CEILING EMERGENCY LIGHT POD INOP. RELAMPED FORWARD CEILING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007012400083 20070124 00083 2007 1 24 UPS07148847 4 20070110 A 2565 A521106010100 ARMING LEVER AIRBUS A300 A300F4622R 3930360 EU ESCAPE SLIDE BINDING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 120UP 0805 EMERGENCY SLIDE ARMING LEVER BINDS AND DOES NOT MOVE WHEN DISARMING. AFTER NUMEROUS ATTEMPTS TO UNLOCK LEVER FINALLY DI SARMED. DEFERRED #M341771. CHECKED ESCAPE SLIDE RELEASE MECHANISM IAW MM 52-10-30-06. NO DAMAGE OR ADJUSTMENT OUT OF LIMITS FOUND. OPS CHECKED ARM/DISARM HANDLE W/O SLIDE INSTALLED. FOUND SATIS. REMOVED AND REPLACED SLIDE GIRT BAR ASS Y IAW MM 25-61-21-04. OPS CHECKED ARM/DISARM HANDLE. FOUND SATIS. THIS CLOSES DMI 341771. 2 L 7 2 4F RT A35EU 2007012400086 20070124 00086 NM 2007 1 24 UPS07248848 1 20070110 A 3350 BATTERY BOEING 727 727185C 138406N NM EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 CONTROL CABIN EMERGENCY LIGHTS FOUND TO BE INOP. REPLACED EMERGENCY LIGHT BATTERY IAW MM 33-50-01-2 AND 33-50-01-5. OP S CHECKED NORMAL. 2 L 7 3 4F A3WE 2007012400092 20070124 00092 WP 2007 1 24 UPS07848849 1 20070110 A 3350 LAMP DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 EMERGENCY LIGHTS DISARMED LAMP INOP. RELAMPED, OPS GOOD. 2 L 7 4 4F RT 4A25 2007012400094 20070124 00094 WP 2007 1 24 MWEA070002 1 20070112 A 5312 995188851 CHANNEL DOUG DC9 DC982 3022082 WP BS 218 BULKHEAD PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 808ME 48070 STATION 218 BULKHEAD WALL ZEE CHANNEL STATION 0.007" ABOVE FLOOR IS PUNCTURED. INSTALLED ZEE CHANNEL. 2 L 7 2 4F A6WE 2007012400097 20070124 00097 NM 2007 1 24 UPS07M48854 1 20070112 A 2910 418575 FLANGE DOUG MD11 MD11F 3023600 NM TRIM MOTOR LEAKING A IPXA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 01 275UP 48774 NR 3 HYDRAULIC QUANTITY LOSS. FOUND HYD LEAK FROM RT STAB TRIM MOTOR FLANGE. REMOVED AND REPLACED RT STAB TRIM MOTOR P ER AMM 27-43-30-4. CHECKED OPERATION OF STAB TRIM PER AMM 27-40-00-710-801. OPS CK OK. NO HYD LEAKS. SERVICED NR 3 H YD SYSTEM TO CORRECT LEVEL. 2 L 7 3 4F RT A22WE 2007012400098 20070124 00098 EU 2007 1 24 200701123 1 20070111 A 3000 UNKNOWN EMB ERJ170 ERJ170100SE 3260406 EU WING MALFUNCTIONED A UHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 17 865RW 17000122 FLIGHT 6471 SLC TO IAH WING FAIL ON TAKEOFF ROLL, RAN QRH. CLEARED THEN CAME ON AGAIN ONTAXI/SPEED 90KTS. OCM DID FIM TASK AND FAULT CLEARED AND WAS OPS CK NORMAL. 2 L 7 2 4F RT A56NM 2007012400101 20070124 00101 NM 2007 1 24 MWEA070003 1 20070113 A 2731 ELEVATOR BOEING 717 717200 1383700 NM WING FROZEN A MWEA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 GL 13 922ME 55184 ELEVATOR IS SLOW TO MOVE FROM FULL NOSE DOWN POSITION AFTER HYD ASSISTS. DISCREPANCY NOTED AFTER A/C DE-ICED, FLUSHED T AIL WITH TYPE I GLYCOL LUBED CONTROL TABS (LT AND RT) HINGES REF MM 12-24-00, PERFORMED ELEVATOR TRAVEL AND POSITION IND ICATION CK PER MM 27-30-00, PG 604, CHECKED GOOD. 2 L 7 2 4F TR A6WE 2007012400107 20070124 00107 EA 2007 1 24 TRAX200700051 1 20070108 A 2910 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 928EV 8006 CLIMBING OUT OF BTR RECEIVED HYD 2 LOW PRESS MSG WITH ZERO QTY AND ZERO PSI. EN ROUTE TO ATL A/C DIVERTED TO GPT. EMER GENCY DECLARED. 2 L 7 2 4F RT A21EA 2007012400109 20070124 00109 NM 2007 1 24 CALA0700017 1 20070118 A 3350 BR964411 LIGHT BOEING 757 757224 1384958 NM SEAT 11 ABC INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 21108 27298 THE EMERGENCY PATH LIGHT AT SEAT ROW 11 ABC WAS FOUND INOPERATIVE. MAINTENANCE FOUND THE LIGHT SOCKET AT FAULT. THE LI GHT ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-51-11. 2 L 7 2 4F RT A2NM 2007012400112 20070124 00112 SO 2007 1 24 RAIA00701021 1 20070115 A 7830 WARNING LIGHT EMB 145 EMB145LR 3260212 SO THRUST REVERSER ACTIVATED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 811HK 145256 FLT NR 5462 - STL - ENGINE NR 1 REVERSER DISAGREE EICAS MESSAGE ON EICAS ON TAKEOFF ROLL. MAINTENANCE DEFERRED THE NR 1 THRUST REVERSER PER MEL. 2 L 7 2 4T RT T00011AT 2007012400118 20070124 00118 EA 2007 1 24 SIMA200701508 1 20070114 A 5220 SEAL CNDAIR CL600 CL6002C10 1390015 EA ESCAPE HATCH LEAKING A SIMA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 510AE 10105 MULTIPLE WARNING AND STATUS MESSAGE WITH STAB TRIM RUNAWAY. POST INSPECTION FOUND EMERGENCY ESCAPE HATCH LEAKING. RESE ALED ESCAPE HATCH PER AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE CR-52-018 WITH NO LEAKS NOTED. PERFORMED MULTIPLE SYS TEM OPERATIONAL CHECKS IAW CRJ AMM 28-23-02, 31-41-04, 27-50-00, 71-00-00 AND 27-61-05 WITH NO DEFECTS. AIRCRAFT PERFOR MED FUNCTIONAL CHECK FLIGHT WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007012400128 20070124 00128 EA 2007 1 24 TRAX200700110 1 20070118 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 723EV 10132 FOUND EMERGENCY CEILING LIGHT ABOVE ROW 10 INOP. 2 L 7 2 4F RT A21EA 2007012400181 20070124 00181 2007 1 24 DXTA200701837 4 20070104 A 2200 UNKNOWN CESSNA 650 650 2076802 CE GARRTT TFE731 TFE7314R 01518 WP UNKNOWN E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 715QS 6507105 AIRCRAFT EXPERIENCED UNCOMMANDED HARD LT YAW CAUSED BY YAW DAMPER. OPERATION CHECK OF A AND B YAW DAMPER SYSTEMS GOOD, S PZ-8000 DIAG. TEST GOOD. RUDDER SERVO OPERATION CHECK GOOD, FLIGHT GUIDANCE, FGC'S, AND AHRS SYSTEMS CHECK GOOD IAW MFG SPZ-8000 AFCD MM SECTION 4. 2 L 7 2 4F 4 F A9NM E6WE 2007012400182 20070124 00182 CE 2007 1 24 DXTA200701838 1 20070105 A 3260 UNKNOWN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE UNKNOWN E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 367QS 5600367 UPON GEAR RETRACTION GEAR UNLOCKED LIGHT REMAINED ON AND HYD PRESS ON LIGHT REMAINED ON. GEAR EXTENDED NORMALLY. JACKED AND SWUNG THE GEAR OVER 12 TIMES OPS CHECKED GOOD. CLEANED UPLOCK SWITCHES AND CONNECTOR PLUGS SYSTEM OPS CHECKS GOOD A T THIS TIME ALL WORK DONE IAW MM CHAPTER 32-30-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007012500004 20070125 00004 2007 1 25 ASMF200701003 4 20070113 A 3414 2594466905 INDICATOR DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE LT AIRSPEED FAILED W ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 158PL 14451 14441 49761 CAPTAIN REPORTED THAT LT AIRSPEED INDICATOR SHOWED MACH 0.50, SO AIRSPEED INDICATOR WAS REPLACED IAW MM 34-13-01, TESTED CORRECT. AIRCRAFT WAS DISPATCHED BUT REJECTED TAKEOFF AT 80 KNOTS DUE TO LT AIRSPEED INDICATOR FAILED. CADC NR 1 AND 2 WERE TESTED IAW MM 34-16-00 BUT CADC NR 1 AIRSPEED INDICATION WAS ZERO. LT AIRSPEED INDICATOR WAS REPLACED AGAIN IAW MM 34-13-01, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007012500005 20070125 00005 CE 2007 1 25 DXTA200701836 1 20070104 A 2930 45AS655735 TRANSDUCER BEECH MU300 400A 1155402 CE HYD SYSTEM INOPERATIVE E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 153QS 18 RK490 HYDRAULIC PRESSURE GAUGE INDICATED 0 PSI IN FLIGHT. VARIED BETWEEN 0 AND 1000 PSI THEN WENT TO 0 PSI FOR THE REMAINDER O F THE FLIGHT. REMOVED AND REPLACED HYDRAULIC PRESSURE TRANSDUCER. AND CONNECTOR PLUG FOR PRESSURE TRANSDUCER (P339) IAW MM 29-30-00. OPS CHECKED GOOD. LEAK CHECKED GOOD. 2 H 7 2 4F RT A16SW 2007012500022 20070125 00022 EA 2007 1 25 N6WA00701002 1 20070115 A 3350 8GH00508606 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 163GJ 10255 EMERGENCY LIGHT AT ROW 7 OUT. REPLACED BULB, OPS OK. 2 L 7 2 4F RT A21EA 2007012500030 20070125 00030 EA 2007 1 25 COMA0760037 1 20070120 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE F FLT CONT AFFECTED AP APPROACH 1 SO 01 720SW 7279 FLIGHT 5228 - FLAPS FAILED AT 8 DEGREES ON APPROACH. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAI NTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007012500031 20070125 00031 EA 2007 1 25 COMA0760038 1 20070121 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 SO 01 973CA 7146 FLIGHT 5162 - DURING DESCENT RECEIVED A PAX DOOR STOW CAUTION MESSAGE. AIRCRAFT DIVERTED TO ACY AND LANDED SAFELY. INS PECTED AND OPERATED PAX DOOR NUMEROUS TIMES WITH NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007012500032 20070125 00032 SO 2007 1 25 ECI10512 1 20070111 A 2750 1159SCC2121 SWITCH GULSTM G1159 GIV 3980115 SO RROYCE TAY TAYMK6108 NE TE FLAPS MISALIGNED E E0XA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 35 919CT 1051 FLAPS WOULD NOT RETRACT DURING GROUND OPERATION. FLAP ASYMMETRY SWITCHES FOUND TO BE OUT OF ADJUSTMENT. 2 L 7 2 4F 4 F RT A12EA E25NE 2007012500033 20070125 00033 SO 2007 1 25 RAIA00701004 1 20070104 A 7500 14536587402 TUBE EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL ZONE 100 CRACKED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 808HK 145157 FLT NR 5485-STL-EICAS MESSAGE (BLD 2 LEAK) CAME ON SHORTLY AFTER TAKEOFF, THEN WITHIN A MINUTE (BLD 1 LEAK) CAME ON. MA INTENANCE REMOVED AND REPLACED A BLEED TUBE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007012500039 20070125 00039 EA 2007 1 25 HNAA0600222 1 20070115 A 6123 BETA LOCKOUT DHAV DHC8 DHC8311 1386006 EA NR 2 MALFUNCTIONED A HNAA D RETURN TO BLOCK O OTHER CL CLIMB 1 EA 07 337EN 284 CLIMBING AT 500 FT, NR 2 ENGINE TORQUE FLUXED 20 TO 90 PERCENT, SUSPECT BETA LOCKOUT. RESET BETA LOCKOUT CIRCUIT BREAKE R GROUND RAN ENGINE, NO DEFECTS NOTED. 2 H 7 2 4T RT A13NM 2007012500056 20070125 00056 NM 2007 1 25 SWAA070289 1 20070120 A 5753 6546486 WEDGE BOEING 737 7373H4 1384600 NM T/E FLAP DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING INBOARD MID FLAP T/E WEDGE DISBONDED AT OUTBOARD END. REMOVED AND REPLACED MID FLAP WEDGE PER MM. 2 L 7 2 4F RT A16WE 2007012500057 20070125 00057 NM 2007 1 25 SWAA070290 1 20070120 A 5344 69784383 HINGE FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR CUTOUT FWD FRAME UPPER HINGE FITTING UPPER HALF CRACKED. REMOVED AND REPLACED HINGE FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2007012500059 20070125 00059 NM 2007 1 25 SWAA070292 1 20070120 A 5330 6545800219 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007012500070 20070125 00070 SO 2007 1 25 RAIA00701011 1 20070108 A 3350 37591 LIGHT EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 802HK 145066 PRE FLT NR 3574-STL-EMERGENCY EXIT LIGHT INOP AT OVERWING EMERGENCY EXIT. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASS EMBLY. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007012500073 20070125 00073 NM 2007 1 25 SWAA070270 1 20070119 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 851, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007012500076 20070125 00076 NM 2007 1 25 SWAA070272 1 20070119 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007012500077 20070125 00077 NM 2007 1 25 SWAA070273 1 20070119 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK CRACKED. REMOVED AND REPLACED FWD GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2007012500079 20070125 00079 NM 2007 1 25 SWAA070275 1 20070119 A 5551 6551524 FITTING BOEING 737 7373H4 1384600 NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND LT AND RT HORIZONTAL STAB FITTING CLEVIS LUG FACES CORRODED. REPAIRED STAB FITTING PE R SRM. 2 L 7 2 4F RT A16WE 2007012500080 20070125 00080 NM 2007 1 25 SWAA070276 1 20070119 A 5322 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007012500082 20070125 00082 NM 2007 1 25 SWAA070278 1 20070119 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM R1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED FWD GIRT BAR HOOK PER S RM. 2 L 7 2 4F RT A16WE 2007012500085 20070125 00085 NM 2007 1 25 SWAA070280 1 20070119 A 5753 65C30462 WEDGE BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD FORE FLAP T/E WEDGE DELAMINATED AT OUTBOARD L/E. REPAIRED FORE FLAP P ER SRM. 2 L 7 2 4F RT A16WE 2007012500087 20070125 00087 NM 2007 1 25 USAA070050 1 20070122 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 23742 SEVERAL AREAS ON FLOORBEAM, STA 986.5, RBL 24, RBL 28, BL 0, RBL 7, LBL 7 HAVE CORROSION. REMOVED CORROSION & INSTALLED ANGLE DOUBLERS & SHIMS PER EA 98409, DEFECT SIZE: .250 INCH EACH, SEVERAL AREAS. 2 L 7 2 4F RT A16WE 2007012500090 20070125 00090 NM 2007 1 25 USAA070053 1 20070122 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 23742 AFT OF PREVIOUS REPAIR, STA 727E + 6 INCHES, AT S-24R CRACKED. REMOVED EXISTING REPAIR & DAMAGED AREA, FABRICATED & INS TALLED DOUBLER & TRIPLER PER T/R 53-50-03A, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007012500092 20070125 00092 NM 2007 1 25 USAA070055 1 20070122 A 5347 BAC1520792 SEAT TRACK BOEING 757 7572B7 1384964 NM FUSELAGE WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 27122 SEAT TRACK BS 850 - 879 RBL 45.5 WORN. REMOVED DAMAGE SECTION OF SEAT TRACK & REPLACED PER SRM 53-00-52, DEFECT SIZE: .5 X .5 INCH. 2 L 7 2 4F RT A2NM 2007012500093 20070125 00093 NM 2007 1 25 USAA070056 1 20070122 A 5340 BAC1520792 SEAT TRACK BOEING 757 7572B7 1384964 NM FUSELAGE WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 27122 BS 850 - 879 RBL 24.75 WORN. REMOVED DAMAGED SECTION OF SEAT TRACK, REPLACED PER SRM 53-00-52, DEFECT SIZE: 1 X 5 INCH ES. 2 L 7 2 4F RT A2NM 2007012500094 20070125 00094 NM 2007 1 25 USAA070057 1 20070122 A 5347 BAC1520792 SEAT TRACK BOEING 757 7572B7 1384964 NM FUSELAGE WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 27122 BS 850-879 LBL 45.5 WORN. REMOVED DAMAGED SECTION OF SEAT TRACK & REPLACED PER SRM 53-00-52, DEFECT SIZE: 1 X 1 INCH. 2 L 7 2 4F RT A2NM 2007012500095 20070125 00095 CE 2007 1 25 DJFA2007005 1 20070108 A 2900 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE300 AE3007A GL HYD SYSTEM UNKNOWN E DJFA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 23 705LX 7500082 TRIP NR 1127054, CREW REPORTED (HYDRAULIC VOLUME LOW-B) EICAS MESSAGE 5 MINUTES AFTER TAKEOFF. CREW VERIFIED (0) QTY ON HYDRAULICS PAGE IN EICAS FOR B SYSTEM. CREW PERFORMED CHECKLIST FOR FAILED B HYD SYS AND DIVERTED. NO UNUSUAL FLIGHT CONTROL PROBLEMS WERE NOTED. ON LANDING CREW REPORTED NO ABNORMAL SITUATIONS. MAINTENANCE IS EVALUATING THE DISCREPANC Y. OPEN 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007012500096 20070125 00096 NM 2007 1 25 USAA070058 1 20070122 A 5347 BAC1520792 SEAT TRACK BOEING 757 7572B7 1384964 NM FUSELAGE WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 27122 BS 850-879 LBL 24.75 WORN. REMOVED DAMAGED SECTION OF SEAT TRACK & REPLACED PER SRM 53-00-52, DEFECT SIZE: 1 X 1 INCH. 2 L 7 2 4F RT A2NM 2007012500097 20070125 00097 NM 2007 1 25 USAA070052 1 20070122 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 23742 BS 847 S-19R & S-20R FRAME CRACKED. REMOVED DAMAGE, FABRICATED & INSTALLED REPAIR ANGLES PER EA 98398, DEFECT SIZE: .2 50 (1 EA) AND .0312 INCH (2 EA). 2 L 7 2 4F RT A16WE 2007012500099 20070125 00099 NM 2007 1 25 SWAA070281 1 20070119 A 3350 MS155721 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 747SA 29799 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007012500103 20070125 00103 NM 2007 1 25 ASAA0741407 1 20070122 A 5755 SKIN BOEING 737 737490 1384715 NM NR 4 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 NR 4 GROUND SPOILER HAS SEVERAL DENTS ON LWR SURFACE. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED FILLERS AND DOUBLE RS IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007012500104 20070125 00104 NM 2007 1 25 ASAA0741408 1 20070122 A 5754 WEDGE BOEING 737 737490 1384715 NM L/E SLAT DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 NR 2 SLAT INBOARD END TRAILING EDGE WEDGE IS DELAMINATED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOU BLER IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007012500105 20070125 00105 NM 2007 1 25 ASAA0741409 1 20070119 A 5315 654681189 FLOORBEAM BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 713AS 30161 FLOORBEAM CAP HAS CORROSION AROUND A NUT HOLES. FLOORBEAM REPAIRED IAW SRM 53-60-51 FIG 201 REPAIR 3. 2 L 7 2 4F RT A16WE 2007012500106 20070125 00106 NM 2007 1 25 ASAA0741410 1 20070119 A 5320 6545855122 SILL BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 713AS 30161 R2 DOOR SILL CHORD CORRODED. SILL CHORD REPLACED WITH NEW PART IAW SRM 51-40-02 AND 51-40-05. 2 L 7 2 4F RT A16WE 2007012500111 20070125 00111 NM 2007 1 25 ASAA0741413 1 20070119 A 5754 65C26602312A SKIN BOEING 737 737490 1384715 NM L/E SLAT DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 713AS 30161 RIGHT NR 5 SLAT DELAMINATION AT THE O/B CORNER. RIGHT NR 5 SLAT DELAMINATION AT THE O/B CORNER REPAIRED IAW SRM 51-70-1 0 REPAIR 4. 2 L 7 2 4F RT A16WE 2007012500116 20070125 00116 NM 2007 1 25 ASAA071411 1 20070117 A 5210 141A61506 DOOR FRAME BOEING 737 737800* NM L1 DOOR BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 564AS 35103 AFT INNER FRAME UPPER CORNER OF THE L1 DOOR IS BENT AND CRACKED DUE TO CONTACT WITH JETWAY. ACCOMPLISHED EA5210 01220 R EPAIR ANGLE. 2 L 7 2 4F RT A16WE 2007012500120 20070125 00120 NM 2007 1 25 SWAA070261 1 20070119 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 847, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007012500122 20070125 00122 NM 2007 1 25 SWAA070262 1 20070119 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 827, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007012500123 20070125 00123 NM 2007 1 25 SWAA070263 1 20070119 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007012500126 20070125 00126 NM 2007 1 25 SWAA070265 1 20070119 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 494, STR 17L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007012500137 20070125 00137 EA 2007 1 25 COMA0760039 1 20070121 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 781CA 7312 FLIGHT 5460 - PAX DOOR LATCH CAUTION MESSAGE RECEIVED AT 6000 FT. RAN QRH PRESS NORMAL. CONTINUED PER QRH RECEIVED PAX DOOR WARNING AT 10,500 FT. AIRCRAFT RETURNED BACK TO DSM AND LANDED SAFELY. INSPECTED AND PERFORMED OPS CHECK OF PAX DOOR AND WARNING SYSTEM, NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007012500146 20070125 00146 CE 2007 1 25 DJFA2007007 1 20070113 A 2120 UNKNOWN BEECH MU300 400A 1155402 CE CABIN ODOR E DJFA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 23 465LX RK454 TRIP NR 1129042 CREW NOTED A SMOKE ODOR IN THE CABIN DURING PRE-LANDING ENVIRONMENTAL SYSTEM CHECK. ODOR WENT AWAY AFTE R HEAT WAS TURNED DOWN. MAINTENANCE PERFORMED SEVERAL GROUND RUNS AND WAS UNABLE TO DUPLICATE THE DISCREPANCY. AIRCRAF T WAS RELEASED AND HAS NOT DISPLAYED THIS ISSUE IN SUBSEQUENT FLIGHTS. 2 H 7 2 4F RT A16SW 2007012500159 20070125 00159 2007 1 25 DXTA200701854 2 20070112 A 7200 ENGINE BEECH MU300 400A 1155402 CE NR 1 POWER LOSS E DXTA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 07 153QS RK490 NR 1 ENGINE WOULD NOT MAKE TAKEOFF THRUST AT FIREWALL. 2 H 7 2 4F RT A16SW 2007012500160 20070125 00160 NM 2007 1 25 KCSA071007 1 20070110 A 5340 ATTACH BRACKET BOEING 747 747209F 1384800 NM PWA JT9 JT9D7R4G2 52054 NE BS 900 BROKEN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 FUSELAGE LT TENSION TIE ATTACH BRACKET IS BROKEN AT STA. 900, LBL 38.5. 2 L 7 4 4F 4 F RT A20WE E3NE 2007012500161 20070125 00161 NM 2007 1 25 KCSA071009 1 20070110 A 5340 STRINGER CLIP BOEING 747 747209F 1384800 NM PWA JT9 JT9D7R4G2 52054 NE BS 820 S10AR GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 FUSELAGE STRINGER CLIP IS GOUGED AT STA. 820, RT SIDE STR 10A. 2 L 7 4 4F 4 F RT A20WE E3NE 2007012500165 20070125 00165 EA 2007 1 25 COMA0760041 1 20070118 A 3097 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYS DIRTY A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 938CA 7046 FLIGHT 5531 - ANTI-ICE DUCT WARNING RECEIVED IN FLIGHT. A/I PAGE SHOWED LEFT WING LEADING EDGE RED. DECLARED EMERGENCY AND LANDED AVP WITHOUT INCIDENT. CLEANED AND INSPECTED ELECTRICAL CONNECTORS ON BALCU'S TEMP CONTROL. PERFORMED OPS C HECK. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007012500170 20070125 00170 EA 2007 1 25 COMA0760048 1 20070123 A 2752 1104SD100501 FLEX DRIVE CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP TWISTED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 721CA 7259 FLIGHT 5156 - FLAPS FAIL MESSAGE APPEARED WHEN FLAPS WERE SELECTED TO 8 DEGREES. LANDED WITHOUT INCIDENT. REPLACED LEF T WING NR 5 FLAP FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2007012500176 20070125 00176 NM 2007 1 25 KCSA071005 1 20070110 A 5310 SHEAR WEB BOEING 747 747209F 1384800 NM BS 820 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 FUSELAGE RT SLOPING SHEAR WEB IS CRACKED (1 INCH) AT STA. 820, RBL 77, STR. 9R. 2 L 7 4 4F RT A20WE 2007012500177 20070125 00177 NM 2007 1 25 KCSA071010 1 20070110 A 5310 TENSION TIE BOEING 747 747209F 1384800 NM PWA JT9 JT9D7R4G2 52054 NE BS 920 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 FUSELAGE TENSION TIE FORWARD CHANNEL IS CRACKED (1 INCH) AT UPPER FLANGE STA. 920, LBL 15. 2 L 7 4 4F 4 F RT A20WE E3NE 2007012500180 20070125 00180 NM 2007 1 25 KCSA071006 1 20070110 A 5310 SHEAR WEB BOEING 747 747209F 1384800 NM PWA JT9 JT9D7R4G2 52054 NE BS 820 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 FUSELAGE LT SLOPING SHEAR WEB IS CRACKED (1 INCH) AT STA. 820, LBL 77, STR. 9L. 2 L 7 4 4F 4 F RT A20WE E3NE 2007012500181 20070125 00181 NE 2007 1 25 COMA0770007 2 20070123 A 7320 4120T01P02 FMU CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE RT ENGINE MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 369CA 10354 10079 FLIGHT 4950 - RIGHT ENGINE REVERTED TO IDLE WITH RIGHT FADEC MESSAGE AND HIGH TEMP OF 790. DECLARED EMERGENCY AND LANDE D WITHOUT INCIDENT. REPLACED RIGHT ENGINE FMU, NO FURTHER DEFECTS. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007012500187 20070125 00187 NM 2007 1 25 SWAA070299 1 20070120 A 5753 6546486 WEDGE BOEING 737 7373T5 1384608 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND RT WING INBOARD MID FLAP WEDGE LOWER SKIN DELAMINATED AT OUTBOARD END. REPAIRED MID F LAP WEDGE PER SRM. 2 L 7 2 4F RT A16WE 2007012500190 20070125 00190 NM 2007 1 25 SWAA070302 1 20070121 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED A1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 1 DEF. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2007012500191 20070125 00191 2007 1 25 SWAA070303 4 20070122 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007012500194 20070125 00194 NM 2007 1 25 SWAA070306 1 20070122 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 409WN 27896 EEPLS COVER LOOSE AT ROW 11 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007012500202 20070125 00202 EA 2007 1 25 COMA0760047 1 20070123 A 2752 1104SD100301 FLEX DRIVE CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP TWISTED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 721CA 7259 FLIGHT 5156 - FLAPS FAIL MESSAGE APPEARED WHEN FLAPS WERE SELECTED TO 8 DEGREES. LANDED WITHOUT INCIDENT. REPLACED LEF T WING NR 3 FLAP FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2007012500207 20070125 00207 NM 2007 1 25 2007UALA00083 1 20070113 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 AFT GALLEY DOOR TRESHOLD SEAL AREA HAS NUMEROUS SPOTS OF CORROSION, CREASE BEAM INNER CHORD CORRODED STA 947.5 - STA 994 . 5 STR 17R RBL 44 TO RBL 52. MAJOR REPAIR: REMOVED AND REPLACED CREASE BEAM PER SRM 51-40-02 AND SRM 51-20-01. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012500208 20070125 00208 NM 2007 1 25 2007UALA00084 1 20070113 A 5320 ATTACH FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 AFT CARGO PIT LEFT STA 787 STR 22L ATTACH CLIP DAMAGED. MAJOR REPAIR: REMOVED AND REPLACED CLIP PER SRM 51-40-02 PAGE 2. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012500213 20070125 00213 NM 2007 1 25 2007UALA00087 1 20070113 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 FLOORBEAM CORRODED AT STA 947 LBL 16 - RBL 16. MAJOR REPAIR: REMOVED DAMAGE. REPAIRED THE T-CAP AT STA 947 PER MM 53- 10-95. REPLACED ENTIRE UPPOER FLOOR BEAM CAP, SPLICE LOCATED AT 947 RBL6. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012500217 20070125 00217 EU 2007 1 25 2007UALA00089 1 20070113 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 489UA 1702 DOOR 2R SILL PLATE HAS CORROSION JUST AFT OF FRAME 65 AT FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE & I NSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007012500222 20070125 00222 NM 2007 1 25 2007UALA00090 1 20070112 A 3397 45160 CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 541UA 25253 EEL ROW 9-16 ABC LEFT INOPERATIVE. REPAIRED EEL CABLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007012500226 20070125 00226 NM 2007 1 25 2007UALA00092 1 20070113 A 3350 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 810UA 843 EMERGENCY LIGHT TEST ON PTP PANEL, SHOWS EPSU R UNIT. REPLACED EPSU AT RIGHT OVERWING. 2 L 7 2 4F 4 F RT A28NM E40NE 2007012300177 20070123 00177 NM 2007 1 23 2007UALA00121 1 20070117 A 8011 STARTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 548UA 25396 726583 ON STARTING R ENG N2, SPUN UP TO 19 PERCENT THEN DOWN TO 0 PUSH, CREW SAW SPARKS FRM CWL. REPLACED STARTER AND START VA LVE ON NUMBER TWO ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007012400003 20070124 00003 SO 2007 1 24 CHQA200700002 1 20070122 A 2797 CONNECTOR EMB 135 EMB135LR 3260305 SO FLAP CONTROL DIRTY A CHQA B EMER. DESCENT J WARNING INDICATION AP APPROACH 1 GL 11 831RP 145663 FLIGHT 6420 - TRI-CVG - ON APPROACH, WHEN PLACING FLAPS FROM "9" TO "22" RECEIVED "FLAP FAIL" ON EICAS WITH "9" INDICATE D. BROKE OFF APPROACH AND RAN QRH. DECLARED EMERGENCY AND LANDED SUCCESSFULLY. MAINTENANCE CLEANED AND RESET FECU CON NECTOR AND OPS CHECK OF FLAPS THROUGH 5 COMPLETE CYCLES AFTER FLAP RESET IAW MM 27-51-00. OPS CHECK OF FLAPS GOOD AT TH IS TIME. 2 L 7 2 4F RT T00011AT 2007012400006 20070124 00006 EA 2007 1 24 A6WA200740023 1 20070109 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALADJUSTMENT A A6WA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 31 460AW 7867 FLAP FAIL YELLOW CAUTION ILLUMINATED INFLIGHT WITH FLAP A ZERO. INSPECTED FLAPS, NO EVIDENCE OF TWISTING OR SKEWING PER AWAC AMM SUPPLEMENT 98-018A, RESET CIRCUIT BREAKERS, FLAPS OPERATE NORMALLY PER AMM 27-50. PLACED ON 72 HOUR FLAP WATC H. REMOVED AND REPLACED RT BPSU. 2 L 7 2 4F RT A21EA 2007012400021 20070124 00021 NM 2007 1 24 CALA0700025 1 20070117 A 5347 151W6240 SEAT TRACK BOEING 777 777224 1385225 NM BS 1525-1546 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 78005 27581 INSPECTION FOUND SEAT TRACK CORRODED AT STA 1525-1546, LBL 108. THE SEAT TRACK WAS REPAIRED AND FASTENERS WERE INSTALLE D IAW SRM 53-00-52, REPAIR 4. 2 L 7 2 4F RT T00001SE 2007012400060 20070124 00060 WP 2007 1 24 UPS07848881 1 20070106 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 CRACKED RIB BEHIND INTERCOSTAL IN RT OB L/E AT XFS 650 PANEL 519B. STOP DRILLED CRACK, FABRICATED AN D INSTALLED REPAIR ANGLE IAW SRM 57-02-00 FIG 002 , 57-03-01 FIG 1, AND 51-1-21. 2 L 7 4 4F RT 4A25 2007012400068 20070124 00068 NM 2007 1 24 07FDEA00133 1 20070118 A 5330 SKIN BOEING 727 727233 138408A NM BS 720 S19L CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 LT EXTERNAL FUSE SKIN IS FRETTED AT FILLET FAIRING PANEL INTERFACE AT BS 720D 10", STRINGER 19L. REMOVED LEADING EDGE FOR ACCESS TO REPAIR, INSTALLED EXTERNAL REPAIR AT LAP SPLICE. REF. SRM 53-30-3 PG.20. REINSTALLED LEADING EDGE AND L EAKED CHECKED HYD. LINES REF. MM 27-81-000-2 (HYD LEAK CK) AND T.A.I DUCT LEAK CHECK ACCOMPLISHED. 2 L 7 3 4F RT A3WE 2007012400093 20070124 00093 WP 2007 1 24 MWEA070001 1 20070112 A 5312 BULKHEAD DOUG DC9 DC982 3022082 WP BS 218 PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 808ME 48070 FOUND STATION 218 BULKHEAD WEB AT STATION 0.007" ABOVE FLOOR HAS PUNCTURE APPROXIMATELY 1/2" DIAGRAM. FABRICATED AND IN STALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2007012400108 20070124 00108 NM 2007 1 24 CALA0700016 1 20070118 A 5347 65C80736155 CARGO TRACK BOEING 737 737524 1384721 NM BS 794-827 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14601 27314 INSPECTION FOUND AFT CARGO COMPARTMENT RT FLOOR TIEDOWN TRACK CORRODED AT STA 794-827, RBL 13.8. INSTALLED NEW TIEDOWN TRACK IAW SRM 53-60-53. 2 L 7 2 4F RT A16WE 2007012400110 20070124 00110 NM 2007 1 24 QXEA200700040 1 20070118 A 3220 PROXIMITY SENSOR BOMBDR DHC8 DHC8402 1390042 NM WHEEL CENTERING OUT OF RIG A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 410QX 4053 ACV FLIGHT NR 2310: AIRCRAFT RETURNED TO FIELD WHEN GEAR FAILED TO RETRACT. MAINTENANCE FOUND THE NWCENT FAULT IN PSEU PRESENT FAULTS (NEAR GAP TO LARGE). CHECKED NWCENT PROX SENSOR GAP AND FOUND IT OUT OF RANGE. RIGGED NLG WHEEL CENTERI NG PROX SENSOR IAW Q400 AMM TASK 32-61-06-830-801. NO PRESENT FAULTS NOTED IN PSEU. NO PARTS REPLACED. AIRCRAFT RETUR NED TO SERVICE. 2 H 7 2 4T RT A13NM 2007012400126 20070124 00126 EA 2007 1 24 TRAX200700108 1 20070117 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 FLOOR LEVEL LIGHTS BETWEEN 6CD BROKEN. 2 L 7 2 4F RT A21EA 2007012400142 20070124 00142 NM 2007 1 24 USAABB07009 1 20070116 A 3230 27N10952 BYPASS VALVE BOEING 757 7572B7 1384964 NM MLG MALFUNCTIONED A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 933UW 45425 27199 CLT FLT 722 EN ROUTE CLT TO BWI. ON APPROACH, THE NOSE LANDING GEAR WAS SLOW TO EXTEND. FLIGHT ABORTED APPROACH AND M ADE A GO-AROUND. CREW LOWERED THE GEAR BY USING THE ALTERNATE GEAR EXTENSION. FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS MAINTENANCE FERRIED TO PHL. MAINTENANCE REPLACED THE NLG SEQUENCE VALVE BYPASS VALVE. 2 L 7 2 4F RT A2NM 2007012400144 20070124 00144 CE 2007 1 24 DJFA2007006 1 20070113 A 5542 SKIN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE RUDDER CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 525CW 5600225 DURING A SCHEDULED MAINTENANCE, DISCOVERED A CRACK ON THE RUDDER LEADING EDGE SKIN AND ONE RIB AT A FASTENER HOLE. UPON FURTHER INVESTIGATION MAINTENANCE FOUND THAT SEVERAL OF THE FASTENER HOLES ON (3) RIBS WERE ELONGATED. THE CRACKS ON T HE RIB ORIGINATED IN A STAR PATTERN FROM THE FASTENER HOLE (WHICH WAS DIMPLED FOR COUNTERSUNK FASTENERS) AND WERE LESS T HAN .125 LONG. THE CRACK IN THE SKIN WAS SIMILAR AND ALSO ABOUT .125 IN LENGTH. MAINTENANCE IS REPLACING THE 3 RIBS WI TH ELONGATED HOLES AND THE CRACKED RIB AND SKIN. THE SDR WILL BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION. 2 L 7 2 4F 4 F RT A22CE E25EA 2007012400145 20070124 00145 2007 1 24 2007UALA00102 4 20070112 A 2565 BRACKET BOEING 737 737322 1384676 NM PAX DOOR SLIDE MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 347UA 24251 AFT ENTRY DOOR EVAC SLIDE COVER FWD GIRT BAR STORAGE BRACKET IS LOOSE. INCORRECT FASTENERS INSTALLED. INSTALLED CORR ECT FASTENERS. 2 L 7 2 4F RT A16WE 2007012400147 20070124 00147 NM 2007 1 24 2007UALA00104 1 20070116 A 2612 2156656 FIRE LOOP BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CARGO BAY FALSE INDICATION A UALA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 105UA 26473 FLIGHT DIVERTED DUE TO FWD CARGO FIRE WARNING. SUPPLEMENTAL DATA UPDATE FWD CARGO RED FIRE WARNING ILLUM DURING CRUISE. ARMED & DISCHARGED FIRE BOTTLES. ACFT DIVERTED TO APW WESTERN SAMOA. NO EVIDENCE OF FIRE DISCOVERED. IDENTIFIED FAULT S IN BOTH A & B LOOPS. REPLACED BOTH SMOKE DETECTORS. OP CHECKED OK. RETURNED TO SERVICE. SUSPECT MOISTURE CONDENSED IN SENSING TUBES LEADING TO FALSE SMOKE READINGS. CARGO INCLUDED BEES & DRY-ICE COOLED CARGO. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012400148 20070124 00148 NM 2007 1 24 0700196740 1 20070116 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 860 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 640US 23888 DURING "M" CHECK, FOUND CRACK IN FRAME WEB AT BS 860 RT. REPAIRED PER EA 67-207927. 2 L 7 4 4F A20WE 2007012400149 20070124 00149 NM 2007 1 24 0700206740 1 20070116 A 5320 TENSION TIE BOEING 747 747251F 1384898 NM BS 940 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 640US 23888 DURING "M" CHECK, FOUND CRACK IN FRAME TENSION TIE AT BS 940 LT. REPAIRED PER EA 67-207925. 2 L 7 4 4F A20WE 2007012400152 20070124 00152 2007 1 24 SIMA200702302 2 20070121 A 7261 UNKNOWN EMB 135 EMB135LR 3260305 SO NR 2 ENGINE LEAKING A SIMA E A ENGINE SHUTDOWN UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 21 732DH 145358 NR 2 SHUTDOWN DUE TO A LOUD POP FOLLOWED BY ENGINE OIL QUANTITY DROPPING TO 3 QUARTS, ITT IN AMBER RANGE EXCEEDING 930 D EGREES, AIRSPEED 280 KNOTS, FLIGHT LEVEL 350. MULTIPLE EICAS MESSAGES, PUNGENT WHITE SMOKE ENTERED CABIN, DISSIPATED AF TER SHUTDOWN OF NR 2 PACK AND BLEEDS. REMOVED AND REPLACED NUMBER 2 ENGINE IAW AMERICAN EAGLE WORK CARD - OPERATIONAL C HECK GOOD - RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007012400153 20070124 00153 EA 2007 1 24 SIMA200702301 1 20070119 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT FAILED A SIMA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SW 21 509AE 8760 806 10078 FOUND EMERGENCY LIGHT SWITCH ON FLIGHT ATTENDANT PANEL IN THE ON POSITION. REMOVED AND REPLACED NUMBER 1, 2, 3 AND 4 EM ERGENCY LIGHT BATTERIES IAW CRJ AMM 33-51-17. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007012500003 20070125 00003 NM 2007 1 25 DHL2007743501 1 20070117 A 5311 FRAME BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE BS 1166 S29L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 REF ASTAR N/R'S 079970 AND 080116. AFT CARGO COMPT; CORROSION ON FLANGE ON FUSELAGE FRAME AT BS 1166 AND STR 29L. CORR OSION OUT OF LIMITS. CUT OUT DAMAGE TO FRAME, 3.125 INCHES X 2.375 INCHES SRM 53-10-4 FIG 11. FABRICATED REPAIR PARTS: FILLER FROM 7075-T6, .063 INCH X 3.125INCHES X 2.375 INCHES, PO NR 9002695, AND DOUBLER FROM 7075-T0, .071INCH X 8 INC H X 4.625 INCH, PO NR 9004150, SRM 53-10-4 FIG 11 AND SRM 53-10-2 FIG 5. HEAT TREATED DOUBLER TO T6 CONDITION FASI FORM FAS0115. TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW SRM 51-10-2 AND 53-10-4 FIG 11. 2 L 7 3 4F 4 F A3WE E2EA 2007012500021 20070125 00021 CE 2007 1 25 01082007650Z 1 20070108 A 2741 UNKNOWN CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP TRIM SYSTEM UNKNOWN E VQMA O OTHER J WARNING INDICATION CR CRUISE 1 NM 03 650Z 1221 6500108 DISCREPANCY (PRIMARY TRIM INDICATOR DOES NOT MOVE FULL RANGE.) DURING FLIGHT, FLIGHT CREW OBSERVED INTERMITTENT FAILURE OF THE HORIZONTAL STABILIZER PRIMARY TRIM (CLACKER). UPON ARRIVAL, FLIGHT CREW PERFORMED ALL PRE AND POST TAKEOFF OPERAT IONAL CHECKS AND OBSERVED A HORIZONTAL STABILIZER TIME FAILURE ANNUNCIATION AND MASTER CAUTION WARNING. ADDITIONALLY, TH E FLIGHT CREW FOUND THAT THEY WERE UNABLE TO OPERATE THE TRIM WITH THE PRIMARY SYSTEM BEYOND THE -10.5 POSITION. THE AIR CRAFT WAS FLOWN USING A SPECIAL FLIGHT PERMIT FOR FURTHER TROUBLESHOOTING AND REPAIR. 2 L 7 2 4F 4 F A9NM E6WE 2007012500023 20070125 00023 NM 2007 1 25 ABXA070014 1 20070112 A 2421 739515C IDG BOEING 767 767281 1385109 NM LT ENGINE FAILED A ABXA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 23 793AX 2405 23143 EICAS LEFT GENERATOR OFF DISPLAYED, OFF LIGHT ILLUMINATED. GENERATOR SWITCH RESET, DID NOT CORRECT CONDITION. APU SHUT DOWN AT TOP OF DESCENT, FOLLOWED PROCEDURES, WOULD NOT RESET. RESTARTED ON VECTORS FOR APPROACH INTO IND. EMERGENCY A IR DIVERSION INTO IND DUE TO GEN/APU ISSUES. REPLACED IDG IAW B767 MM 24-11-005. LEAK CHECKED GOOD. PERFORMED APU BIT E PROCEDURE IAW B767 MM 49-11-00-12. SYSTEM CHECKED NORMAL. 2 L 7 2 4F RT A1NM 2007012500040 20070125 00040 CE 2007 1 25 DJFA2007008 1 20070115 A 2120 UNKNOWN BEECH MU300 400A 1155402 CE LAVATORY ODOR E DJFA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 23 469LX RK463 TRIP NR 1129156 CREW NOTED BURNING ODOR FROM LAV AREA DURING CLIMB ENROUTE. AIRCRAFT DIVERTED. MAINTENANCE PERFORMED N UMEROUS GROUND RUNS WITH CREW ON BOARD AND WAS UNABLE TO DUPLICATE THE DISCREPANCY. 2 H 7 2 4F RT A16SW 2007012500048 20070125 00048 NM 2007 1 25 USAA070049 1 20070122 A 5310 DOOR FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 23742 BS 492 S-24R DOOR FRAME CRACKED. REPAIRED PER EA 98396, DEFECT SIZE: .625 INCH. 2 L 7 2 4F RT A16WE 2007012500083 20070125 00083 NM 2007 1 25 SWAA070279 1 20070119 A 5753 65C30462 WEDGE BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD FORE FLAP T/E WEDGE DELAMINATED AT INBOARD L/E. REPAIRED FORE FLAP PE R SRM. 2 L 7 2 4F RT A16WE 2007012500102 20070125 00102 CE 2007 1 25 2007F00005 1 20070116 A 5410 016A133223 LATCH MTSBSI MU2 MU2B60 5780460 CE GARRTT TPE331 TPE33110 01514 WP LT NACELLE BROKEN E BKAA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 13 610CA 788SA LT IB COWL LATCH FOR THE NR 2 ENGINE TOP COWL BROKE. VISUAL INSP REVEALED THE LATCH LINK ASSY BROKE INTO 2 PIECES. 1 H 7 2 3T 4 T RT A10SW E4WE 2007012500109 20070125 00109 NM 2007 1 25 ASAA0741412 1 20070119 A 5311 654655089 FRAME BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 713AS 30161 AFT CARGO PIT BODY FRAME FAIL SAFE ANGLE CORRODED. AFT CARGO BODY FRAME FAILSAFE REINFORCEMENT ANGLE REPLACED WITH NEW PART IAW SRM 51-40-02 AND 51-40-05. 2 L 7 2 4F RT A16WE 2007012500167 20070125 00167 EA 2007 1 25 COMA0760042 1 20070119 A 2910 6017523839 DRAIN LINE CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYS FAILED A COMA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 01 712CA 7244 FLIGHT 5385- HYD SYS NR 2 LOW PRESS (SYS QTY SHOWED 5 PERCENT) A/C DIVERTED TO RIC AND LANDED SAFELY. REMOVED AND REPLA CED HYD SYS NR 2 CASE DRAIN TUBE ASSY. 2 L 7 2 4F RT A21EA 2007012500183 20070125 00183 NM 2007 1 25 KCSA071008 1 20070110 A 5340 ATTACH BRACKET BOEING 747 747209F 1384800 NM PWA JT9 JT9D7R4G2 52054 NE BS 900 BROKEN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 FUSELAGE RT TENSION TIE ATTACH BRACKET IS BROKEN AT STA. 900, RBL 38.5. 2 L 7 4 4F 4 F RT A20WE E3NE 2007012500189 20070125 00189 2007 1 25 SWAA070301 4 20070121 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007012500195 20070125 00195 2007 1 25 SWAA070307 4 20070122 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 436WN 32456 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007012500201 20070125 00201 CE 2007 1 25 A8J2007F00001 1 20070110 A 2710 62184014 CIRCUIT BOARD CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP AILERON SYS FAULTY C A8JA O OTHER O OTHER NR NOT REPORTED 1 SW 09 777XS 6500008 ON 1/10-07 AT 1900, AIRCRAFT EXPERIENCED AN AILERON BOOST FAILURE. PILOT DECLEARED AN EMERGENCY AND LANDED AT ITS SCHED ULE DETINATION WITHOUT ANY COMPLICATIONS. AILERON BOOST CIRCUIT BOARD WAS REPLACED AND THE SYSTEM CHECKED GOOD. (K) 2 L 7 2 4F 4 F A9NM E6WE 2007012500216 20070125 00216 NM 2007 1 25 2007UALA00088 1 20070113 A 5320 WEB BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 AFT CARGO COMPARTMENT THRESHOLD SILL WEB STA 780-787 RBL 20-21 HAS CORROSION. MAJOR REPAIR: REMOVED AND REPALCED THRESH OLD WEB PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012500224 20070125 00224 NM 2007 1 25 2007UALA00091 1 20070112 A 5210 MECHANISM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR MISRIGGED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 504UA 24625 DOOR 1R BOTTLE MECHANISM ASSEMBLED IMPROPERLY AND WILL NOT ACCEPT SAFETY PIN. FOUND LOWER CLAMP UP WASHER DISLODGED AND NOT CAPTURED BY LINK ATTACH BOLT, BLOCKING SAFETY PIN HOLE. DISASSEMBLED LINK ATTACH POINT AND REASSEMBLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007012500229 20070125 00229 2007 1 25 COMA0760044 4 20070122 A 2340 508812 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 798CA 24557 7348 FLIGHT 5132 - SMOKE WAS BEING EMITTED FROM CALL LIGHT ON P/A PANEL IN COCKPIT. AIRCRAFT DIVERTED TO GSP AND LANDED SAFE LY. REMOVED AND REPLACED INTERPHONE CONTROL PANEL. 2 L 7 2 4F RT A21EA 2007012500232 20070125 00232 NM 2007 1 25 2007UALA00093 1 20070114 A 2597 WIRE HARNESS AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE L1 DOOR MISROUTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 851UA 1664 DOOR SLIDE 1L HAS INCORRECT ROUTING OF ELECTRICAL HARNESS. ROUTED ELECTRICAL HARNESS IN CORRECT DIRECTION. 2 L 7 2 4F 4 F RT A28NM E40NE 2007012500234 20070125 00234 NM 2007 1 25 2007UALA00094 1 20070114 A 2597 WIRE HARNESS AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R1 DOOR MISROUTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 851UA 1664 DOOR SLIDE 1R HAS INCORRECT ROUTING OF ELECTRICAL HARNESS. HARNESS RUNS AFT, AWAY FROM DOOR SUPPORTS. ROUTED ELECTR ICAL HARNESS IN CORRECT DIRECTION. 2 L 7 2 4F 4 F RT A28NM E40NE 2007012500238 20070125 00238 NM 2007 1 25 2007UALA00096 1 20070113 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 669UA 30025 SEAT 24A EMERGENCY LIGHT INOPERATIVE. REPLACED EEL STRIP. OP CHECKS OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007012500252 20070125 00252 SO 2007 1 25 RAIA00701012 1 20070110 A 3350 BULB EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT BLOWN A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 821HK 145068 PRE FLT NR 5596-STL-EMERGENCY LIGHT AT REAR CEILING INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007012500256 20070125 00256 NM 2007 1 25 2007UALA00097 1 20070113 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 669UA 30025 DOOR 2R EXTERIOR EMERGENCY LIGHT. LEFT HAND MIDDLE OVERWING EXTERIOR EMERGENCY AFT EMERGENCY LIGHT INOP. RELAMPED. OP CHECKED OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007012500259 20070125 00259 NM 2007 1 25 2007UALA00100 1 20070114 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EEL INOP ROW SEAT 32L. REPLACED BATTERY, OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012500264 20070125 00264 NM 2007 1 25 SCNA07001 1 20070119 A 3350 BATTERY BOEING 737 737800* NM CABIN FAILED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 PHHZX 28248 DURING A FUNCTIONAL CHECK MAINTENANCE FOUND THAT BATTERY M1676 FOR THE EMERGENCY LIGHTING FAILED IT'S CAPACITY CHECK. M AINTENANCE REPLACED THE BATTERY PACK. 2 L 7 2 4F RT A16WE 2007012500268 20070125 00268 EA 2007 1 25 COMA0760045 1 20070124 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 915CA 7013 FLIGHT 5057- FLAP FAIL CAUTION MESSAGE AT 28 DEGREES DURING TAXI. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIR ST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2007012500269 20070125 00269 EA 2007 1 25 COMA0760046 1 20070123 A 2752 1104SD100201 FLEX DRIVE CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP TWISTED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 721CA 7259 FLIGHT 5156 - FLAPS FAIL MESSAGE APPEARED WHEN FLAPS WERE SELECTED TO 8 DEGREES. LANDED WITHOUT INCIDENT. REPLACED LEF T WING NR 2 FLAP FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2007012500270 20070125 00270 NM 2007 1 25 2007UALA00127 1 20070118 A 2130 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN PRESSURE MALFUNCTIONED A UALA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 WP 29 339UA 24243 LANDED UNDER AMBER ALERT DUE TO LOSS OF CABIN PRESSURE. FOUND DAMAGED DUCT AND MISSING CLAMP IN ELEVATOR ACCESS COMPAR TMENT, WHERE APU DUCT ENTERS AT AFT PRESSURIZED BULKHEAD. REPLACED DUCT AND CLAMP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012500271 20070125 00271 EU 2007 1 25 2007UALA00128 1 20070118 A 2560 GIRT BAR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 423UA 504 DOOR 2R HARD TO ARM-DISARM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007012500272 20070125 00272 NM 2007 1 25 2007UALA00129 1 20070119 A 5320 TORQUE BOX BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 177UA 24384 TORQUE BOX PLATE AT STA 870 IS DAMAGED. DISCOVERED DAMAGE TO ROLLER TRAYS. ALSO FWD PIT TORQUE BOX DAMAG 3 LOCATIONS. WORKED WITH LINE ENGINEERING, ORDLE, TO REPAIR ROLLER TRAYS PER SRM. ALSO FABRICATED TORQUE BOX "L" ANGLE LOCALLY & IN STALLED PER SRM. REPAIRS COMPLETED. AIRCRAFT RETURNED TO SERVICE. SUSPECT TRAYS & TORQUE BOX DAMAGED BY PRY BAR LOADING TO MOVE CONTAINERS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012500273 20070125 00273 NM 2007 1 25 2007UALA00130 1 20070118 A 5320 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 DAMAGE FOUND AT STA 410, STA 430, AND STA 450 AT BL 0. MAJOR REPAIR: INSTALLED REPAIR DOUBLER AND SPACER AT STA 410, 4 30, AND 450. REFERENCE MM 53-30-99 AND SB 737-53-1230 FIG 6, FIG21 AND FIG 22. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012500276 20070125 00276 NM 2007 1 25 2007UALA00133 1 20070118 A 5743 FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RT MLG TOOL DAMAGE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 RIGHT MLG FITTING HAS TWO EACH TOOLING MARKS. MAJOR REPAIR: BLENDED TOOLING MARKS PER AAR EA I060568 REV IR AND FAA F ORM 8100-9. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012500278 20070125 00278 EU 2007 1 25 2007UALA00136 1 20070118 A 2597 CABLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EVAC SLIDE MISROUTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 435UA 613 AFT RIGHT SLIDE ELECTRICAL CABLE WAS ROUTED THROUGH THE AFT END OF THE GIRT. ELECTRICAL CABLE INSTALLED CORRECTLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007012500282 20070125 00282 NM 2007 1 25 2007UALA00139 1 20070118 A 3040 6240665 CONTROLLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT ERRATIC A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 579UA 26697 1ST OFFICER'S SIDE WINDOW HEAT INOP LIGHT IS COMING ON AND GOING OFF. *S/D* RANG OUT ALL WIRES, ALL RESISTANCES WERE W ITHIN RANGE. REPLACED WINDOW HEAT CONTROLLER AS PRECAUTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007012500283 20070125 00283 NM 2007 1 25 2007UALA00140 1 20070118 A 2560 LATCH BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EVAC SLIDE DOOR FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 674UA 29242 RIGHT OVERWING SLIDE COMPARTMENT DOOR LATCHES FAILED TORQUE CHECK. REPLACED 4 EACH LATCHES AT RT OVERWING SLIDE COMPART MENT DOOR. OPS TEST GOOD. RETURNED TO SERVICE. SUSPECT OVER TORQUING FAILED THE LATCHES. 2 L 7 2 4F 4 F RT A1NM E24NE 2007012500286 20070125 00286 NM 2007 1 25 SWAA070309 1 20070122 A 3350 8200037709 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 488WN 33853 EMERGENCY EXIT LIGHT LENS AT L1 DOOR BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007012500287 20070125 00287 NM 2007 1 25 SWAA070310 1 20070122 A 3350 8200037702 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 779SW 27884 EMERGENCY EXIT LOWER LIGHT LENS AT L2 DOOR BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007012500290 20070125 00290 NM 2007 1 25 SWAA070313 1 20070122 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SKIN CREASED AT BS 747, STR 27R. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007012500291 20070125 00291 NM 2007 1 25 SWAA070314 1 20070122 A 5312 6545409 PRESSURE PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663.75, LBL 32. REPAIRED PRESSURE WEB PER SRM. 2 L 7 2 4F RT A16WE 2007012500302 20070125 00302 SO 2007 1 25 RAIA00701017 1 20070112 A 3350 BULB EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT BLOWN A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 821HK 145068 PRE FLT NR 5485-STL-OVERHEAD EMERGENCY LIGHT OUT OVER ROW 16. MAINTENANCE RESEATED THE OVERHEAD EMERGENCY LIGHT BULB AT ROW 16. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007012500303 20070125 00303 SO 2007 1 25 RAIA00701018 1 20070113 A 3610 14521182403 DUCT EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL BLEED AIR CRACKED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 820HK 145064 FLT NR 5542-DSM-NR 1 BLEED LEAK INDICATION IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE BLEED DUCT SEALS AND REMOVED AND REPLACED THE T-DUCT. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007012500304 20070125 00304 SO 2007 1 25 RAIA00701013 1 20070110 A 5260 BOLT EMB 145 EMB145EP 3260221 SO ALLSN AE300 AE3007A GL AIRSTAIR BENT A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 827HK 145021 POST FLT NR 5566-STL-AIRSTAIRS DO NOT DEPLOY WHEN DOOR IS OPENED. MAINTENANCE REMOVED AND REPLACED A BENT BOLT ON THE PA SSENGER DOOR PIVOT ARM. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007012500306 20070125 00306 SO 2007 1 25 RAIA00701014 1 20070111 A 3350 LIGHT EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL CABIN LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 821HK 145068 PRE FLT NR 5525-STL-OVERHEAD AFT EMERGENCY LIGHT AT ROW 16 INOP. MAINTENANCE RESECURED EMERGENCY LIGHT. OPS CHECKED GOO D. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007012500308 20070125 00308 NE 2007 1 25 01172007N220C 2 20070117 A 7200 CF7002D2 ENGINE AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D2 30010 NE RIGHT MALFUNCTIONED E CEDA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 220CA 14000 2685 220 245U166B AFTER TAKEOFF AND CLIMBOUT TO FL210 FROM KDAY, THE CREW NOTICED THE OIL PRESSURE INDICATION WAS ERRATIC. CREW NOTIFIED ATC OF SHUT DOWN RIGHT HAND ENGINE AS A PRECAUTIONARY MEASURE. CREW PROCEEDED TO CHANGE DESTINATION TO KTOL. LANDED WI THOUT FURTHER INCIDENT. MAINTENANCE HAS YET TO EXAMINE ENGINE FOR THE SPECIFIC CAUSE. 2 L 7 2 4F 4 F A7EU E7EA 2007012500310 20070125 00310 2007 1 25 RAIA00701015 4 20070111 A 2330 246318 HANDSET EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL ODOR A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 841HK 145382 FLT NR 7918-IAD-ELECTRICAL BURNING ODOR THROUGHOUT CABIN AND COCKPIT. MAINTENANCE REMOVED AND REPLACE THE FORWARD FLIGHT ATTENDANT HANDSET. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007012500312 20070125 00312 SO 2007 1 25 RAIA00701016 1 20070112 A 3350 78241 INVERTER EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHTS INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 826HK 145016 PRE FLT NR 5511-STL-EMERGENCY LIGHTS INOP ON FLOOR SRTIPS. MAINTENANCE REMOVED AND REPLACED THE NR 6 INVERTER AND FLOOR STRIP. ALSO RECONNECTED THE PLUG TO THE AISLE FLOOD LIGHT. 2 L 7 2 4F RT T00011AT 2007012500315 20070125 00315 NM 2007 1 25 CALA0700028 1 20070117 A 5347 151W1294 SEAT TRACK BOEING 777 777224 1385225 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 78005 27581 INSPECTION FOUND SEAT TRACK FLANGE CORRODED AT STA 415-422, RBL 68. THE SEAT TRACK WAS REPLACED IAW SRM 51-10-02 AND SR M 51-40-02. 2 L 7 2 4F RT T00001SE 2007012500317 20070125 00317 NM 2007 1 25 CALA0700029 1 20070117 A 5347 151W6294 SEAT TRACK BOEING 777 777224 1385225 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 78005 27581 INSPECTION FOUND SEAT TRACK CORRODED AT STA 1546, LBL 74. THE SEAT TRACK WAS REPAIRED AND FASTENER INSTALLED IAW SRM 53 -00-52, REPAIR 3. 2 L 7 2 4F RT T00001SE 2007012500318 20070125 00318 SO 2007 1 25 RAIA00701020 1 20070114 A 7830 UNKNOWN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL THRUST REVERSER MALFUNCTIONED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 811HK 145256 FLT NR 5536-DEN-NR 1 ENGINE THRUST REVERSER DISAGREE MESSAGE ON EICAS. MAINTENANCE DEFERRED THE AFFECTED T/R. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007012500320 20070125 00320 CE 2007 1 25 6018701012007 1 20070101 A 3234 HANDLE LEAR 60 60LEAR 5170707 CE MLG STUCK E J7SA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 05 247FX 187 LANDING GEAR HANDLE IS STUCK IN THE DOWN POSITION AND CANNOT BE MOVED. GEAR COULD NOT BE RETRACTED AFTER TAKE-OFF. MX C LEANED AND LUBRICATED THE GEAR HANDLE SHAFT. PERFORMED SEVERAL SATISFACTORY GEAR EXTENSIONS/RETRACTIONS. NO FURTHER DE FECTS NOTED. 2 L 7 2 4F RT A10CE 2007012500325 20070125 00325 NM 2007 1 25 ANCF200600044 1 20070123 A 3830 TOILET BOEING 767 7673Y0 NM LAVATORY MALFUNCTIONED W ANCF A UNSCHED LANDING O OTHER CR CRUISE 1 SO 23 948AV 24948 PILOT REPORT: ALL TOILETS FAILED TO FLUSH, AIRPLANE WAS 16,000 FT OR ABOVE. PERFORMED INSPECTION AND CHECK, TOILET SER VICE ACCOMPLISHED. WASTE TANK WAS DRAINED AND CLEANED IAW AMM 38-32-00. OPERATIONAL CHECK WAS PERFORMED ON GROUND, IT SHOWED NORMAL CONDITION. 2 L 7 2 4F RT A1NM 2007012500332 20070125 00332 NE 2007 1 25 MAC010701 3 20070123 A 6197 WIRE AEROSP ATR42 ATR42320 8680930 EU HAMSTD 14SF 14SF5 NE FEATHER SOLENOID OUT OF POSITION A MTNA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 SO 33 904FX 259 DURING DESCENT INTO DHN THE NR 2 ENGINE BEGAN SURGEING (PROP CHANGEING PITCH). WIRE NR 101 WAS FOUND NEARLY SEPARATED F ROM IT'S PIN IN THE CONNECTOR TO THE RIGHT FEATHER SOLENOID. 2 H 7 2 4T RT A53EU 6 C P7NE 2007012500333 20070125 00333 SO 2007 1 25 C2XA07CL011 1 20070123 A 5610 163500112 WINDSHIELD EMB 145 EMB145LR 3260212 SO COCKPIT SHORTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 27 16559 145603 CLE FLIGHT 2201 THE CREW REPORTED A BURNING ELECTRICAL SMELL IN THE COCKPIT WHILE OPERATING BELOW 10,000 FT. MAINTENANC E INSPECTED AND FOUND THE TERMINAL BLOCK BURNED ON THE NR 2 WINDSHIELD. THE NR 2 WINDSHIELD WAS REPLACED. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007012500337 20070125 00337 2007 1 25 MWEA070006 4 20070122 A 2565 100502119 SLIDE DOUG DC9 DC981 3022081 WP AFT GALLEY DOOR UNSECURE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 AFT GALLEY DOOR SLIDE PACK CAME UNFASTENED. REINSTALLED AFT GALLEY DOOR SLIDE. 2 L 7 2 4F A6WE 2007012500342 20070125 00342 NM 2007 1 25 KCSA071017 1 20070116 A 5220 LATCH BOEING 747 747209F 1384800 NM PWA JT9 JT9D7R4G2 52054 NE EMERGENCY DOOR BROKEN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 UPPER DECK EMERGENCY DOOR FORWARD LOWER GUIDE RAIL LATCH/SPRING ASSY. IS BROKEN ON BOTTOM OF DOOR. 2 L 7 4 4F 4 F RT A20WE E3NE 2007012500345 20070125 00345 CE 2007 1 25 DXTA200701835 1 20070103 A 3260 65430087 UPLOCK SWITCH CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE NLG INOPERATIVE E DXTA O OTHER O OTHER CL CLIMB 1 GL 07 646QS 4762 5605246 AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT. REMOVED AND REPLACED FAULTY NOSE LANDING GEAR UPLOCK SWITCH. OPS CHECK GOOD I AW WDM CHPT 32-60-01. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007012500349 20070125 00349 NM 2007 1 25 SWAA070316 1 20070122 A 5340 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012500351 20070125 00351 NM 2007 1 25 SWAA070318 1 20070122 A 5330 6545768 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 390, BL 0. REPAIRED SKIN P ER ER. 2 L 7 2 4F RT A16WE 2007012500354 20070125 00354 NM 2007 1 25 SWAA070321 1 20070122 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 771SA 27879 DURING SCHEDULED HC1 CHECK, LT OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007012500355 20070125 00355 NM 2007 1 25 SWAA070322 1 20070122 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 771SA 27879 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2007012500356 20070125 00356 NM 2007 1 25 SWAA070323 1 20070122 A 5315 149A5510 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 708SW 27842 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 38 TO LBL 48. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007012500357 20070125 00357 NM 2007 1 25 SWAA070324 1 20070122 A 5315 149A5510 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 708SW 27842 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 19 TO RBL 57. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007012500358 20070125 00358 NM 2007 1 25 SWAA070325 1 20070123 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 LEFT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007012500359 20070125 00359 2007 1 25 SWAA070326 4 20070123 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007012500361 20070125 00361 NM 2007 1 25 SWAA070327 1 20070123 A 5310 6547956 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME CRACKED AT BS 847, STR 18R. REMOVED AND REPLACED FRAM E SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007012400115 20070124 00115 SO 2007 1 24 RAIA00701024 1 20070115 A 7830 WARNING MESSAGE EMB 145 EMB145LR 3260212 SO THRUST REVERSER ACTIVATED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 850HK 145003 FLT NR 7892 - OMA - ENGINE NR 2 THRUST REVERSER DISAGREE EICAS MESSAGE. MAINTENANCE DEFERRED THE NR 2 THRUST REVERSER P ER THE MEL. 2 L 7 2 4T RT T00011AT 2007012400127 20070124 00127 EU 2007 1 24 TRAX200700109 1 20070117 A 2120 UNKNOWN AEROSP ATR72 ATR72212 8680945 EU CABIN ODOR A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 631AS 362 BURNING ELECT ODOR IN FLT, ODOR GREW STRONGER AS FLT PROGRESSED. DID NOT SEE ANY SMOKE FLT 4120 P DEL 150 MINS. FLTS 4 416,4642 CX. 2 H 7 2 4T RT A53EU 2007012400130 20070124 00130 SO 2007 1 24 SIMA200701507 1 20070113 A 3297 WIRE HARNESS EMB 135 EMB135KL 3260302 SO NLG UPLOCK DAMAGED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 840AE 145656 FELT BUMPING AND CLANKING AFTER GEAR RETRACTED, EMERGENCY DECLARED. REMOVED AND REPLACED BOTH NOSE GEAR UPLOCK SWITCH H ARNESS, THREE UPLOCK PROXIMITY SWITCH, LANDING GEAR ELECTRONIC UNIT AND NOSE LANDING GEAR SOLENOID VALVE. AIRCRAFT PERF ORMED FUNCTIONAL CHECK FLIGHT WITH NO DISCREPANCIES. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007012400133 20070124 00133 NM 2007 1 24 QXEA200700032 1 20070113 A 2750 C1486742003 FCU BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 412QX 213 4059 GEG FLIGHT NR 2357: FLAP POWER CAUTION LIGHT ILLMINATED WHEN FLAPS WERE SELECTED DOWN AFTER START. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED THE FCU AND A SERVICEABLE UNIT WAS INSTALLED IAW Q400 AMM 27-51-01-000-801 AND 27-51-01-400- 801. TRANSDUCER WAS REMOVED AND SERVICEABLE ONE INSTALLED IAW Q400 AMM 27-53-06-000-801 AND 27-53-06-400-801. FPU REMO VED AND SERVICEABLE UNIT INSTALLED IAW Q400 AMM 27-52-01-000-801 AND 27-52-01-400-801. NO DEFECTS NOTED AFTER FUNCTIONA L CHECKS. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007012400134 20070124 00134 NM 2007 1 24 QXEA200700034 1 20070116 A 2611 47359715 SMOKE DETECTOR BOMBDR DHC8 DHC8402 1390042 NM CARGO BAY MALFUNCTIONED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 424QX 4006 PDX FLIGHT NR 2309: INTERMITTENT FWD BAGGAGE SMOKE DETECTOR WARNING WITH NO EVIDENCE OF SMOKE OF FIRE IN FWD BAGGAGE COM PARTMENT. MAINTENANCE REMOVED AND REPLACED THE SMOKE DETECTOR LOCATED IN THE FWD BAGGAGE COMPARTMENT IAW Q400 AMM TASK 26-12-06-000-801 AND 26-12-06-400-801. PERFORMED OPS TEST OF THE FWD BAGGAGE COMPARTMENT SMOKE DETECTOR IAW TASK 12-12- 06-710-801. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007012400137 20070124 00137 NM 2007 1 24 TSAA0724008 1 20070113 A 2420 761574B IDG BOEING 737 73773A 1384606 NM NR 1 ENGINE FAILED A TSAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 738AL 28499 NON-ETOPS FLIGHT 483 RNO-SNA. AFTER ENGINE START, CREW NOTED THE NR 1 ENGINE IDG DRIVE LIGHT ILLUMINATED. CREW DISCONN ECTED THE NR 1 IDG AND RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE DEFERRED THE NR 1 IDG PER MEL 24-1-2 AND RELEASED THE AIRCRAFT FOR SERVICE. FLIGHT 483 CONTINUED TO SNA WHERE MAINTENANCE REMOVED AND REPLACED THE NR 1 IDG IN A CCORDANCE WITH ALOHA MAINTENANCE TASK FORM M-727. THE IDG PASSED ALL MAINTENANCE CHECKS AND INSPECTIONS AND THE AIRCRAF T WAS RELEASED FOR SERVICE. THE IDG PASSED A FLIGHT VERIFICATION ON THE NEXT FLIGHT LEG. 2 L 7 2 4F RT A16WE 2007012500002 20070125 00002 2007 1 25 DJFA2007010 4 20070115 A 2312 CI108BCHL ANTENNA BEECH MU300 400A 1155402 CE NR2 COM BROKEN E DJFA O OTHER O OTHER CR CRUISE 1 EA 23 768TA 7373 RK168 TRIP NR 1129456 ON REPO, CREW NOTICED A LOUD NOISE COMING FROM THE REAR OF THE AIRCRAFT AT FL030 AND 250 KTS. ON LANDING , MAINTENANCE DISCOVERED A LARGE PORTION OF THE NR 2 VHF ANTENNA HAD BROKEN OFF AND DEPARTED THE AIRCRAFT, THE FLIGHT PH ONE ANTENNA WAS DAMAGED AND MISSING MUCH OF THE FIBERGLASS OUTER COATING, AND DAMAGE TO THE SKIN WAS FOUND THAT WAS PROB ABLY CAUSED BY THE DEPARTING FRAGMENTS OF FAILED ANTENNAS. MAINTENANCE HAS REPLACED BOTH ANTENNAS AND IS EVALUATING THE STRUCTURAL DAMAGE FOR A REPAIR. THE SDR WILL BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION. 2 H 7 2 4F RT A16SW 2007012500028 20070125 00028 EA 2007 1 25 COMA0760035 1 20070119 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE F FLT CONT AFFECTED AP APPROACH 1 SO 01 812CA 7381 FLIGHT 5168 - ON APPROACH FLAPS SELECTED TO 30 BUT REMAINED AT 20 DEGREES. RECEIVED FLAPS FAIL CAUTION MESSAGE. COMPLI ED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYS TEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007012500034 20070125 00034 SO 2007 1 25 RAIA00701009 1 20070106 A 3040 3801D2MODA CONTROLLER EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL WINDSHIELD TEMP ODOR A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 03 802HK 991 991 145066 FLT NR 3542-BDL-CREW REPORTED STRONG ELECTRICAL/PLASTICE BURNING ODOR IN COCKPIT. MAINTENANCE REMOVED AND REPLACED THE NR 1 WINDSHIELD TEMP CONTROLLER. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007012500045 20070125 00045 NM 2007 1 25 USAA070046 1 20070122 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 589US 23934 BS 727D S-21L, BS 727E S-22L CRACKED. REPAIR DOUBLER/TRIPLER INSTALLED 28 X 24 INCHES PER TYPICAL 53-60-03A, DEFECT SIZ E: 3 INCHES (2) EACH. 2 L 7 2 4F RT A16WE 2007012500053 20070125 00053 NM 2007 1 25 SWAA070286 1 20070120 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 420, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007012500064 20070125 00064 NM 2007 1 25 SWAA070267 1 20070119 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 765, STR 19L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007012500075 20070125 00075 NM 2007 1 25 SWAA070271 1 20070119 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 924, STR 4R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007012500078 20070125 00078 NM 2007 1 25 SWAA070274 1 20070119 A 5330 6550570 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT BS 960, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007012500081 20070125 00081 NM 2007 1 25 SWAA070277 1 20070119 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012500101 20070125 00101 NM 2007 1 25 ASAA0741406 1 20070122 A 5753 6546435339 FLAP BOEING 737 737490 1384715 NM LT WING DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 LEFT OUTBOARD T/E FLAP IS SPLIT (DELAMINATED) AT INBOARD EDGE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AN D DOUBLER IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007012500113 20070125 00113 NM 2007 1 25 ASAA0741414 1 20070119 A 5754 65C26602312A SKIN BOEING 737 737490 1384715 NM L/E SLAT DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 713AS 30161 RIGHT WING NR 5 SLAT DELAMINATED AT I/B CORNER (UPPER SKIN). RIGHT WING NR 5 SLAT DELAMINATION REPAIRED IAW SRM 51-70-1 0 REPAIR 4. 2 L 7 2 4F RT A16WE 2007012500117 20070125 00117 NM 2007 1 25 SWAA070260 1 20070119 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED SPV CHECK, FOUND STRINGER 27L CORRODED BETWEEN BS 360 AND BS 365. REMOVED AND REPLACED STRINGER SECTIO N PER SRM. 2 L 7 2 4F RT A16WE 2007012500125 20070125 00125 NM 2007 1 25 SWAA070264 1 20070119 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007012500141 20070125 00141 CE 2007 1 25 ACE010507 1 20070105 A 5610 10138402523 WINDSHIELD BEECH 1900 1900C 1154161 CE COCKPIT CRACKED E YADA A UNSCHED LANDING O OTHER CL CLIMB 1 AL 03 111AX 4053 UC81 PILOT REPORTED LT WINDSHIELD CRACKED AT 400 FT ON DEPARTURE. PILOT BURNED OFF FUEL AND RETURNED TO DEPARTURE FOR WINDSH IELD REPLACEMENT. 2 L 7 2 4T RT A24CE 2007012500174 20070125 00174 EA 2007 1 25 COMA0760050 1 20070123 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 721CA 11535 7259 FLIGHT 5156 - FLAPS FAIL MESSAGE APPEARED WHEN FLAPS WERE SELECTED TO 8 DEGREES. LANDED WITHOUT INCIDENT. REPLACED LEF T INBOARD FLAP OUTBOARD ACTUATOR. 2 L 7 2 4F RT A21EA 2007012500178 20070125 00178 CE 2007 1 25 4516401122007 1 20070112 A 3232 74691 ACTUATOR LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE731* 01518 WP MLG DOOR MALFUNCTIONED E J7SA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SW 05 428FX 5033 164 ON TAKEOFF, THE GEAR WOULD NOT RETRACT WHEN THE GEAR HANDLE WAS RAISED TO THE (UP) POSITION. THE GEAR THEN MOMENTARILY R ETRACTED, THEN EXTENDED EVEN THOUGH THE GEAR HANDLE WAS STILL IN THE (UP) POSITION. MX REPLACED THE LT IB GEAR DOOR ACT UATOR. OPS CHECK AND GEAR SWINGS PERFORMED WITH NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT T00008WI E6WE 2007012500179 20070125 00179 CE 2007 1 25 4511401112007 1 20070111 A 7697 MONOPOLE LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE731* 01518 WP RT ENGINE MALFUNCTIONED E J7SA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 05 417FX 114 P116217C ON TAKEOFF, THE RT ENGINE BEGAN SURGING. CREW ELECTED TO RETURN TO DEPARTURE AIRPORT FOR MAINTENANCE. MAINTENANCE RE-SH IMMED THE N-2 MONOPOLE SENSOR AND PERFORMED SATISFACTORY GROUND ENGINE RUNS. 2 L 7 2 4F 4 F RT T00008WI E6WE 2007012500184 20070125 00184 NM 2007 1 25 SWAA070297 1 20070120 A 5340 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012500193 20070125 00193 2007 1 25 SWAA070305 4 20070122 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007012500203 20070125 00203 EU 2007 1 25 2007UALA00079 1 20070112 A 2913 PUMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYDRAULIC SYS FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 405UA 452 RTFL WITH A HYDRAULIC SYSTEM PROBLEM. BLUE HYDDRAULIC PUMP OVER HEAT DURING FLIGHT. PUMP TURNED OFF. REPLACED PUMP. 2 L 7 2 4F 4 F RT A28NM E40NE 2007012500204 20070125 00204 EU 2007 1 25 2007UALA00080 1 20070113 A 5230 SEAL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO DOOR MISINSTALLED A UALA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 WP 29 409UA 462 FLIGHT DIVERTED DUE TO PRESSURIZATION PROBLEM. FOUND AFT CARGO DOOR SEAL INSTALLED INCORRECTLY. HOLES IN SEAL ARE NOT I N A POSITION TO LET THE AIR GET INTO THE SEAL. CORRECTLY INSTALLED AFT CARGO DOOR SEAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007012500210 20070125 00210 NM 2007 1 25 2007UALA00085 1 20070113 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 AFT CARGO PIT STA 787L STR 23L ATTACH CLIP IS DAMAGED. MAJOR REPAIR: REMOVED AND REPLACED STRINGER CLIP PER SRM 51-40- 02. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012500251 20070125 00251 CE 2007 1 25 UG8APA07001 1 20070104 A 3246 AHA1814 WHEEL RAYTHN DH125 HAWKER800XP 7150012 CE MLG CRACKED E UG8A K NONE O OTHER IN INSP/MAINT 1 GL 23 715P 688 258715 MAIN LANDING GEAR WHEEL WAS REMOVED FOR A WORN TIRE. A CRACK IN THE WHEEL WAS DISCOVERED BY VENDOR DURING TEARDOWN AND INSPECTION PROCESS TO CHANGE THE TIRE. THE WHEEL WAS DETERMINED TO BE B.E.R. MFG HAS REQUESTED RETURN OF THEIR WHEEL F OR ANALYSIS. 2 L 7 2 4F RT A3EU 2007012500279 20070125 00279 2007 1 25 2007UALA00137 4 20070118 A 2565 SLIDE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU R1 DOOR FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 904UA 25004 FWD DOOR ESCAPE SLIDE IS FAULTY. SLIDE FAILED AD COMPLIANCE VERIFICATION TEST. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012500280 20070125 00280 NM 2007 1 25 2007UALA00138 1 20070118 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY EXIT LIGHT VERY DIM, DOOR 5 LEFT BUSTLE. RELAMPED, OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012500289 20070125 00289 NM 2007 1 25 SWAA070312 1 20070122 A 5523 18A80101 BOLT BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 1 HINGE BOLT AND SPACER PER MM. 2 L 7 2 4F RT A16WE 2007012500305 20070125 00305 NE 2007 1 25 HNAA0600223 2 20070115 A 7321 7982133007 EEC DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 2 ENGINE FAILED A HNAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 07 337EN 284 CLIMBING TO 500 FEET NR 2 ENGINE TORQUE FLUXED 70 TO 90 PERCENT SUSPECT BETA LOCKOUT, MEL'D USING 61-4. AT RON MAINTENA NCE REMOVED AND REPLACED EEC, TSCU, REMOVED AND REPLACED THE BETA SWITCH 6141-S4. RIGGED SWITCH AND TRIMMED ENGINE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007012500313 20070125 00313 SO 2007 1 25 C2XA07IA017 1 20070120 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14105 145649 BFL - FLIGHT 2608, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE GALLEY AND RIGHT WING EMERGENCY EXIT SIGNS WE RE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 5 EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECK ED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007012500319 20070125 00319 2007 1 25 ASMF200701004 4 20070113 A 3421 KAD9F010 RELAY DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE AHRS FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 754RA 49641 CAPTAIN REPORTED AHRS 1, 2 AND 3 BASIC MODE LIGHTS TURNED ON. AHRS 1, 2 AND 3 BREAKERS WERE RESEATED AND AHRS 1 AND 2 WO RKED CORRECT BUT AHRS NR 3 FAILED, SO IT WAS DEFERRED IAW MEL 34-38. AIRCRAFT WAS DISPATCHED BUT RETURNED TO PLATFORM DU E TO THE SAME FAILURE. THE FLIGHT DIRECTOR BARS WERE CHECKED BEING CORRECT AND AIRCRAFT WAS DISPATCHED WITH THE 1, 2 AND 3 AHRS´S IN BASIC MODE. DURING OVERNIGHT CHECK, WIRING WAS CHECKED, BREAKER B10-407 AND RELAYS R20-92 AND R20-91 WERE R EPLACED IAW WDM 34-24-01 AND TESTED IAW MM 34-24-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007012500335 20070125 00335 NM 2007 1 25 MWEA070005 1 20070120 A 2560 D29982225 COVER BOEING 717 717200 1383700 NM DOOR DETACHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 920ME 55182 CABIN DOOR EMERGENCY SLIDE DOOR COVER DETACHED FROM DOOR. INSTALLED SLIDE COVER ASSEMBLY. 2 L 7 2 4F TR A6WE 2007012500339 20070125 00339 NM 2007 1 25 MWEA070007 1 20070115 A 3350 60030451 BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 701ME 49760 AFT ACCESSORY UPPER EMERGENCY LIGHT INOPERATIVE RIGHT SIDE. REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F RT A6WE 2007012500348 20070125 00348 NM 2007 1 25 SWAA070315 1 20070122 A 5313 BAC1498 STRINGER BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND STRINGER 25R CORRODED AT BS 908. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007012500364 20070125 00364 NM 2007 1 25 SWAA070329 1 20070123 A 3350 OL3071BPEGL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED HC1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 19 DEF. REMOVED AND REPLACED LIGHT BULB PE R MM. 2 L 7 2 4F RT A16WE 2007012500377 20070125 00377 NM 2007 1 25 SWAA070331 1 20070123 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012500378 20070125 00378 NM 2007 1 25 SWAA070332 1 20070123 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012500379 20070125 00379 NM 2007 1 25 SWAA070333 1 20070123 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012500381 20070125 00381 EA 2007 1 25 N6WA00701001 1 20070103 A 3350 6100976 BULB CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE EMERGENCY LIGHT INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 156GJ 10227 CEILING LEVEL EMERGENCY FLOOD LIGHT ROW 7 INOP. REPLACED LAMP, OPS OK. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007012600004 20070126 00004 WP 2007 1 26 AMTA200700026 1 20070124 A 5753 SKIN LKHEED 1011 10113853 5265020 WP TE FLAP CHAFED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 164AT 1238 RIGHT WING NR 1 FLAP VANE ASSY FOUND DEEP CHAFING ALONG THE UPPER SKIN FROM INBOARD TO OUTBOARD OF VAN. REPAIRED PER EE R 12978 GAMCO WORKORDER 316063. (M) 2 L 7 3 4F A23WE 2007012600005 20070126 00005 NM 2007 1 26 DU4R2007014 1 20070117 A 5321 FLOOR PANEL BOEING 757 757232 1384965 NM BS 1200-1340 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 HEAVY CORROSION ON FLOOR PANEL BS 1200 TO 1340 IN AFT CARGO. REPAIRED BY FABRICATING AND INSTALLING FLOOR PANEL 129 BY 39.5 FROM 2024-T3 .071 IAW B757 SRM 51-10-02, PARA. 10A, 51-40-08 PARA 5C AND 51-20-01. 2 L 7 2 4F RT A2NM 2007012600009 20070126 00009 NM 2007 1 26 DU4R2007017 1 20070114 A 5320 65C80678180 SUPPORT BOEING 757 757232 1384965 NM THRESHOLD CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION AFT CARGO DOOR THRESHOLD BOEING CASTING UNDER NUT PLATES BS 1438. REPAIRED BY REMOVING AND INSTALLING NEW SUP PORT P/N 65C80678-180 IAW B757 SRM 51-40-02, AND 51-40-04. 2 L 7 2 4F RT A2NM 2007012600010 20070126 00010 WP 2007 1 26 AALA20070075 1 20070113 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 464AA 49594 LGA - EMERGENCY ESCAPE PATH LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK B5107 FOR EMERGENCY ESCAPE PATH LIGH TS AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007012600013 20070126 00013 NM 2007 1 26 AALA20070067 1 20070111 A 3350 LIGHT BOEING 757 757223 1384957 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 624AA 24582 SFO - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. RELAMPED EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER F OUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007012600014 20070126 00014 WP 2007 1 26 AALA20070071 1 20070112 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 599AA 53289 LGA - EMERGENCY LIGHT AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007012600015 20070126 00015 NM 2007 1 26 AALA20070078 1 20070113 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 181AN 29591 DFW - EMERGENCY SLIDE LIGHT AT LEFT NUMBER THREE DOOR INOPERATIVE. RELAMPED EMERGENCY SLIDE LIGHT AT LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007012600018 20070126 00018 EU 2007 1 26 AALA20070081 1 20070114 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 59081 639 MIA - EMERGENCY LIGHT AT SEAT 25G INOPERATIVE. SECURED WIRE CONNECTOR UNDER SEAT FOR EMERGENCY LIGHT AT SEAT 25G. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007012600023 20070126 00023 NM 2007 1 26 AALA20070077 1 20070114 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 750AN 30259 NRT - EMERGENCY EXIT LIGHT AT FIRST CLASS COAT CLOSET HAS MISSING LENS AND DAMAGED. REPLACED EMERGENCY EXIT LIGHT ASSEM BLY AT FIRST CLASS COAT CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007012600024 20070126 00024 NM 2007 1 26 AALA20070068 1 20070111 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 629AA 24587 LAX - EMERGENCY LIGHT AT FORWARD LEFT HAND OVERWING INOPERATIVE. RELAMPED EMERGENCY LIGHT AT STATION 310 AT FORWARD LEF T HAND OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007012600026 20070126 00026 EU 2007 1 26 AALA20070085 1 20070114 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 25071 514 MIA - EMERGENCY LIGHT AT SEAT 22G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A35EU 2007012600027 20070126 00027 WP 2007 1 26 AALA20070064 1 20070111 A 3350 LENS DOUG DC9 DC982 3022082 WP CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 557AN 53087 LGA - EMERGENCY ESCAPE PATH LIGHTING AT SEAT 23D HAS MISSING LENS COVER. REPLACED LENS COVER FOR EMERGENCY ESCAPE PATH LIGHTING AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007012600028 20070126 00028 WP 2007 1 26 AALA20070072 1 20070112 A 2560 BATTERY DOUG DC9 DC982 3022082 WP FLASHLIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 237AA 49253 SFO - EMERGENCY FLASHLIGHT AT AFT FLIGHT ATTENDANT DOUBLE SEAT POSITION INOPERATIVE. REPLACED BATTERY ASSEMBLY FOR EMER GENCY FLASHLIGHT AT AFT FLIGHT ATTENDANT DOUBLE SEAT POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007012600030 20070126 00030 NM 2007 1 26 AALA20070070 1 20070112 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 929AN 30078 MIA - EMERGENCY LIGHT AT SEAT 21D INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 21D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A16WE 2007012600031 20070126 00031 NM 2007 1 26 DU4R2007020 1 20070111 A 5340 STRINGER CLIP BOEING 757 757232 1384965 NM BS 1620 S30R CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION ON STRINGER CLIP AT BS 1620 STRINGER 30 IN AFT PIT. REPAIRED BY REMOVING CLIP, FABRICATED AND INSTALLED STRIN GER CLIP 3" BY 5" AND END SPLICE 6.5" BY 3" FROM 7075-T6 .050" IAW B757 DRAWING 146N2821, 51-30-01 AND 51-40-02. 2 L 7 2 4F RT A2NM 2007012600032 20070126 00032 NM 2007 1 26 ABXA070015 1 20070118 A 5751 113T710035A SKIN BOEING 767 767232 1385132 NM LT AILERON DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 745AX 22222 LEFT OUTBOARD AILERON SKIN PEELED BACK/DELAMINATED. REPLACED LEFT OUTBOARD AILERON IAW B767 AMM 27-11-02-4. 2 L 7 2 4F RT A1NM 2007012600034 20070126 00034 WP 2007 1 26 ABXA070017 1 20070116 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 EMERGENCY EXIT LIGHTS GO OFF AFTER 5 SECONDS. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00-8-000 1. 2 L 7 2 4F A6WE 2007012600038 20070126 00038 NM 2007 1 26 DU4R2007018 1 20070116 A 5320 FLOOR SUPPORT BOEING 757 757232 1384965 NM BS 1400-1440 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION ON PNL UNDER CARGO FLOOR SUPPORT STRINGER IN AFT CARGO COMPT LOCATED AT BS 1400 TO BS 1440 RBL 16.1. REMOVED CORRODED FLOOR SUPPORT, FABRICATED AND INSTALLED REPLACEMENT PANEL 20" BY 5" FROM 7075-T6 .032" IAW 51-40-05 FIG 6, 51- 20-01, DELTA PROCESS STANDARD 900-2 NR 5 AND 51-40-07 FIG 8. 2 L 7 2 4F RT A2NM 2007012600039 20070126 00039 NE 2007 1 26 QXEA200700047 2 20070124 A 7314 5008269H PUMP DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 1 MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 366PH 499 510 SEA FLIGHT NR 2411, IN CRUISE WITH CRUISE POWER SET THE NR 1 FUEL FLOW WOULD FLUCTUATE BETWEEN 770 AND 810. THE TORQUE WOULD ALSO FLUCTUATE FROM 93 PERCENT TO 103 PERCENT. WITH THE FUEL FLOW AT LOWER POWER SETTINGS THE FUEL FLOW WOULD FLU CTUATE LESS OR NOT AT ALL. WITH POWER LEVERS NEAR 100 PERCENT TORQUE THE FLUCTUATION WOULD RETURN. MAINTENANCE REPLACE D THE MFC AND PUMP REPLACEMENT OF TRANSFER TUBE AND PACKING. REPLACEMENT ON EDP. OPERATIONAL CHECK GOOD. LEAK CHECK A ND ENGINE RUNS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007012600040 20070126 00040 NM 2007 1 26 AMTA200700016 1 20070115 A 5210 SEAL BOEING 737 73783N 13844HI NM L1 DOOR DISLODGED A AMTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 317TZ 28246 L1 DOOR DID NOT SEAL PROPERLY. A/C AIR TURN BACK DUE TO NOT PRESSURIZING, FOUND SEAL OFF TRACK AND OBSTRUCTING, CLEANED AND RE-INSERTED SEAL OK FOR CONT`D SVC. (M) 2 L 7 2 4F RT A16WE 2007012600041 20070126 00041 WP 2007 1 26 AMTA200700020 1 20070121 A 5320 SUPPORT ANGLE LKHEED 1011 10113853 5265020 WP FUSELAGE CRACKED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 162AT 1220 CENTER SECTION LOWER AREA SUPPORT ATTACHMENT ANGLE FOUND CRACKED AT FS 1212, LBL 42.5. REPAIR CARRIED OUT ON CRACKED SU PPORT ANGLE AT FS 1212, LBL 42.5 CENTER SECTION AREA IAW L1011 SRM 51-50-04. PAINT TOUCH-UP AS IAW AMM 20-51-08. (M) 2 L 7 3 4F A23WE 2007012600045 20070126 00045 EA 2007 1 26 TRAX200700111 1 20070119 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 824AS 7203 FLAP FAIL ON ARRIVAL. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007012600047 20070126 00047 WP 2007 1 26 AMTA200700025 1 20070124 A 5312 BULKHEAD LKHEED 1011 10113853 5265020 WP BS 1212 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 164AT 1238 RIGHT MLG WHEEL WELL FORWARD BULKHEAD AT FS 1212 RBL 105.07 AND WL174.315 SUSPECT CORROSION BENEATH FITTING 27, SRM 3-11 -00 PAGE 50 FIG 14 SHEET 2. REPAIRED PER EER 12903 GAMCO WORKORDER 316063. (M) 2 L 7 3 4F A23WE 2007012600049 20070126 00049 EA 2007 1 26 TRAX200700112 1 20070119 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 27 824AS 7203 ON APPROACH IN ROC, SELECTED FLAPS 8 AND FLAPS FAIL CAUTION MSG, FLAPS FAILED AT ZERO. C/W QRH AND DECLARED EMERGENCY, TOUCH DOWN SPEED AT BUF WAS 172 KNOTS, DIVERTED TO BUF. FLT 4249 CX ON 1/20/07. 2 L 7 2 4F RT A21EA 2007012600051 20070126 00051 NM 2007 1 26 KCSA071040 1 20070122 A 5315 FLOORBEAM BOEING 747 747209F 1384800 NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 STA 720 FORWARD PIT FLOORBEAM UPPER CHORD DENTED WL 119 RBL 10. 2 L 7 4 4F RT A20WE 2007012600052 20070126 00052 NM 2007 1 26 KCSA071041 1 20070123 A 5412 BULKHEAD BOEING 747 747209F 1384800 NM NR 2 PYLON GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 NR 2 PYLON 221 BULKHEAD HAS THREE GAUGES AFT SIDE ABOVE HYD LINE. 2 L 7 4 4F RT A20WE 2007012600053 20070126 00053 NM 2007 1 26 KCSA071042 1 20070123 A 5412 FIRESHIELD BOEING 747 747209F 1384800 NM NR 4 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 NR 4 PYLON LOWER SKIRT O/B SIDE FIRESHIELD FROM STA180-250 CHAFED. 2 L 7 4 4F RT A20WE 2007012600055 20070126 00055 NM 2007 1 26 KCSA071044 1 20070123 A 5315 FLOORBEAM BOEING 747 747209F 1384800 NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 STA 560 FLOORBEAM UPPER CHORD DENTED RBL 50. 2 L 7 4 4F RT A20WE 2007012600058 20070126 00058 SO 2007 1 26 RAIA00701032 1 20070123 A 3260 852701 DOWNLOCK SENSOR EMB 145 EMB145 3260210 SO LT MLG MALFUNCTIONED A RAIA O OTHER N FALSE WARNING DE DESCENT 1 CE 03 820HK 145064 FLT NR 5567 - PHL - LEFT MLG INDICATION RED ON EICAS WHEN GEAR HANDLED WAS SELECTED DOWN. MAINTENANCE REMOVED AND REPLA CED THE LEFT MLG DOWN AND LOCK SENSOR. 2 L 7 2 4F RT T00011AT 2007012600059 20070126 00059 SO 2007 1 26 RAIA00701031 1 20070122 A 3397 WIRE EMB 145 EMB145 3260210 SO CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 821HK 145068 PRE FLT NR 5541 - STL - EMERGENCY LIGHT AT THE COCKPIT STEP IDENTIFIER INOP. MAINTENANCE RESECURED A BROKEN WIRE AT THE COCKPIT STEP IDENTIFIER. 2 L 7 2 4F RT T00011AT 2007012600060 20070126 00060 SO 2007 1 26 RAIA00701033 1 20070124 A 3397 WIRE EMB 145 EMB145 3260210 SO CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 803HK 145077 PRE FLT NR 3551 - PIT - FLOOR EMERGENCY LIGHT AT ROW 10 WILL NOT ILLUMINATE. MAINTENANCE REPAIR A BROKEN WIRE TO THE FL OOR PROXIMITY LIGHT STRIP. 2 L 7 2 4F RT T00011AT 2007012600062 20070126 00062 2007 1 26 SWAA070338 4 20070124 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007012600063 20070126 00063 NM 2007 1 26 SWAA070347 1 20070124 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007012600064 20070126 00064 NM 2007 1 26 SWAA070348 1 20070124 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007012600065 20070126 00065 NM 2007 1 26 SWAA070349 1 20070124 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007012600066 20070126 00066 NE 2007 1 26 SWAA070350 2 20070123 A 7320 8283005 HMU BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B22 13802 NE NR 2 ENGINE MALFUNCTIONED A SWAA K NONE E VIBRATION/BUFFET NR NOT REPORTED 1 SW 29 748SW 29800 AIRCRAFT HAD TWO INCIDENTS OF HIGH FREQUENCY LATERAL OSCILLATIONS AT FL 390. TURNED YAW DAMPNER OFF NO EFFECT, RUDDER T RIM 1-2 UINTS EITHER SIDE, SLIGHT DAMPENING EFFECT. REMOVED AND REPLACED NR 2 ENGINE HMU, FUEL PUMP AND RUDDER PCU PER MM. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007012600067 20070126 00067 NM 2007 1 26 SWAA070351 1 20070124 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007012600069 20070126 00069 NM 2007 1 26 SWAA070353 1 20070124 A 5315 6546816 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM WEB CORRODED AT BS 1003, RBL 50. REMOVED AND REPLACED FLOORBEAM WEB PER SRM . 2 L 7 2 4F RT A16WE 2007012600070 20070126 00070 NM 2007 1 26 SWAA070354 1 20070124 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 20Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM . 2 L 7 2 4F RT A16WE 2007012600071 20070126 00071 NM 2007 1 26 SWAA070355 1 20070124 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM R1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED FWD GIRT BAR HOOK PER M M. 2 L 7 2 4F RT A16WE 2007012600072 20070126 00072 NM 2007 1 26 SWAA070356 1 20070124 A 5551 6551524 FITTING BOEING 737 7373H4 1384600 NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND LT AND RT HORIZONTAL STAB FITTING CLEVIS LUG FACES CORRODED. REPAIRED STAB FITTING PE R ACO. 2 L 7 2 4F RT A16WE 2007012600074 20070126 00074 NM 2007 1 26 SWAA070337 1 20070123 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 772SW 27880 DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP MISSING AT ROW 12 DEF. INSTALLED PHOTOLUMINESCENT STRIP PER MM. 2 L 7 2 4F RT A16WE 2007012600075 20070126 00075 NM 2007 1 26 SWAA070336 1 20070123 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012600076 20070126 00076 2007 1 26 SWAA070339 4 20070124 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 449WN 32469 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007012600078 20070126 00078 NM 2007 1 26 SWAA070341 1 20070124 A 5310 6545874 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT R1 DOOR AFT CUTOUT NR 4 DOOR STOP. REMOVED AND REPLACED FRA ME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007012600080 20070126 00080 NM 2007 1 26 SWAA070343 1 20070124 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007012600081 20070126 00081 NM 2007 1 26 SWAA070344 1 20070124 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012600082 20070126 00082 NM 2007 1 26 SWAA070345 1 20070124 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012600083 20070126 00083 NM 2007 1 26 SWAA070346 1 20070124 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012600085 20070126 00085 NE 2007 1 26 2007UALA00167 2 20070119 A 7200 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE SMOKE A UALA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 659UA 27114 724347 AFTER NR 2 ENG START GROUND REPORTED SMOKE FROM BOTTOM OF ENG COWL. ENG SHUTDOWN BY CREW. SECOND START ATTEMPT NO ROTA TION AND HAD R START VLV LT PER CREW. REPLACED STARTER & STARTER VALVE. SUSPECT BEARING DRAG. 2 L 7 2 4F 4 F RT A1NM E24NE 2007012600086 20070126 00086 EU 2007 1 26 2007UALA00168 1 20070122 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 431UA 571 AFT RIGHT DOOR SILL PLATE HAS CORROSION DAMAGE AT INBOARD EDGE MID POINT OF PLATE. MAJOR REPAIR. INSTALLED DOUBLER REPA IR PER SRM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007012600087 20070126 00087 NM 2007 1 26 2007UALA00169 1 20070123 A 5414 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT NACELLE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 RIGHT NACELLE STRUT O/B SKIN CRACKED AT STA 110 FWD UPPER QUADRANT. MAJOR REPAIR ACCOMPLISHED. REPAIRED PER ENGINEERIN G AUTHORIZATION AND MAINTENANCE SPECIFICATION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007012600088 20070126 00088 NM 2007 1 26 2007UALA00170 1 20070122 A 2560 EXTINGUISHER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE AFT CABIN LEAKING A UALA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 29 582UA 26702 AFT WATER FIRE EXTINGUISHER APPEARS TO BE LEAKING. REPLACED WATER FIRE EXTINQUISHER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007012600092 20070126 00092 NM 2007 1 26 USAA070069 1 20070124 A 5312 PRESSURE PANEL BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 BS 665, LBL 30, MLG WHEEL WELL PRESSURE FLOOR HAS CRACK. CUT OUT DAMAGED AREA, FAB'D & INSTALLED REPAIR DOUBLER, FILLER S, SHIMS, ANGLE PER TR 53-60-04, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007012600095 20070126 00095 NM 2007 1 26 USAA070067 1 20070124 A 5720 ATTACH ANGLE BOEING 737 737401 1384701 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 ATTACH ANGLE AT LT WING STA 114 INBOARD SIDE UPPER AFT END IN FUEL TANK HAS CRACK. REMOVED DAMAGE, FABRICATED ANGLE DOU BLERS & INSTALLED PER EA 98389, DEFECT SIZE: 0.1 INCH. 2 L 7 2 4F RT A16WE 2007012500066 20070125 00066 NM 2007 1 25 SWAA070269 1 20070119 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 972, STR 23L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007012500089 20070125 00089 NM 2007 1 25 USAA070051 1 20070122 A 5312 PRESSURE PANEL BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 23742 OVERHEAD PRESSURE WEB AT BS 665 AT LBL 30 CRACKED. REMOVED DAMAGE, FABRICATED & INSTALLED FILLER & DOUBLER PER T/R 53-6 0-04, DEFECT SIZE: .6 INCH. 2 L 7 2 4F RT A16WE 2007012500098 20070125 00098 CE 2007 1 25 DXTA200701855 1 20070114 A 2916 RESERVOIR BEECH MU300 400A 1155402 CE HYD SYSTEM UNDERSERVICED E DXTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 149QS RK473 ON TAXI OUT, RT BRAKE PEDAL, CAPT, PRESSED TO FLOOR. NO PRESSURE OR BRAKING ACTION. LT PEDAL HAD PRESSURE BUT ALSO NO BR AKING ACTION. APPLIED EMER BRAKE TO STOP. OPS CHECKED BRAKES, FOUND TO BE SPONGY. PERFORMED PILOT AND COPILOT BRAKE SYS TEM BLEEDING (BLEED MIXERS). PERFORMED POWER BRAKE BLEEDING AND HYDRAULIC FLUID PURGING. ALL ABOVE MENTIONED WORK WAS PERFORMED IAW CH 32-40 OF THE MM. SERVICED HYDRAULIC RESERVIOR IAW CH 12-10 OF THE MM. BRAKES OPS CHECKED GOOD. 2 H 7 2 4F RT A16SW 2007012500100 20070125 00100 EU 2007 1 25 BAQA2007004 1 20070112 A 6420 109013307101 BUSHING AGUSTA A109 A109E 0260119 EU TAIL ROTOR HUB DEBONDED E BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 109UP 11061 FOUND EXCESSIVE PLAY IN THE TAIL ROTOR HUB PITCH CHANGE ASSEMBLY. AFTER DISASSEMBLY WE FOUND BUSHING P/N 109-0133-07-10 1 DEBONDED FROM SLEEVE ASSEMBLY P/N 109-0130-70-119. WE ALSO FOUND DAMAGE TO THE TAIL ROTOR GEARBOX OUTPUT SHAFT P/N 10 9-0445-08-115.S/N 557. 1 G 7 2 3U RT H7EU 2007012500115 20070125 00115 SO 2007 1 25 GUUA01040701 1 20070104 A 3297 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE MLG DIRTY A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 29 283AS 120236 FLIGHT: 9258 FPO/FLL DURING FLIGHT LT MAIN LANDING GEAR (B) LOOP LIGHT ILLUMINATES INTERMITTENTLY. CONTINUED TO FLL LAN DED WITHOUT INCIDENT.CLEANED AND RESECURED CONNECTORS 151548 AND 151549 OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 2007012500128 20070125 00128 NM 2007 1 25 SWAA070266 1 20070119 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 804, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007012500151 20070125 00151 EA 2007 1 25 COMA0760040 1 20070118 A 2613 OVERHEAT LOOP CNDAIR CL600 CL6002B19 1900309 EA LT MLG WW DIRTY A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 938CA 7046 FLIGHT 5531 - ANTI-ICE DUCT WARNING RECEIVED IN FLIGHT. A/I PAGE SHOWED LEFT WING LEADING EDGE RED. DECLARED EMERGENCY AND LANDED AVP WITHOUT INCIDENT. CLEANED AND INSPECTED A/I LOOP IN LEFT WHEEL AREA AND AFT EQUIP BAY. PERFORMED OPS C HECK. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007012500172 20070125 00172 EA 2007 1 25 COMA0760049 1 20070123 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 721CA 11535 7259 FLIGHT 5156 - FLAPS FAIL MESSAGE APPEARED WHEN FLAPS WERE SELECTED TO 8 DEGREES. LANDED WITHOUT INCIDENT. REPLACED LEF T INBOARD FLAP INBOARD ACTUATOR. 2 L 7 2 4F RT A21EA 2007012500182 20070125 00182 NM 2007 1 25 SWAA070296 1 20070120 A 5313 BAC1498 STRINGER BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND STRINGER 22R CORRODED AT BS 848. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007012500185 20070125 00185 NM 2007 1 25 SWAA070298 1 20070120 A 5340 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 24L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012500188 20070125 00188 NM 2007 1 25 SWAA070300 1 20070120 A 5753 65C30462 SKIN BOEING 737 7373T5 1384608 NM FORE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND RIGHT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED AT OUTBOARD END. REPAIRED FORE FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007012500192 20070125 00192 2007 1 25 SWAA070304 4 20070122 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007012500205 20070125 00205 NM 2007 1 25 2007UALA00081 1 20070112 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 RIGHT LOWER EXTERIOR FUSELAGE SKIN APPROX STA 253 BETWEEN STR 25R & 24R HAS A DENT. ACCOMPLISHED MANUFACTURED AND INSTA LLED DOUBLER AND STRUCTURAL FILLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012500211 20070125 00211 NM 2007 1 25 2007UALA00086 1 20070113 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 STRINGER CLIP CRACKED AT BS 277 STR 15R. MAJOR REPAIR: REMOVED AND REPLACED STRINGER CLIP PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012500277 20070125 00277 NM 2007 1 25 2007UALA00135 1 20070118 A 5720 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU WING MISDRILLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 FWD INBOARD HOLE OF UPPER WING WAS MISDRILLED. MAJOR REPAIR: INSTALLED FREEZE PLUG REPAIR TO DAMAGED HOLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012500288 20070125 00288 NM 2007 1 25 SWAA070311 1 20070122 A 5330 6545890 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 296, STR 14R. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007012500323 20070125 00323 NM 2007 1 25 CALA0700030 1 20070123 A 2897 280W00021 CONNECTOR BOEING 777 777224 1385225 NM NR 1 BOOST PUMP BURNED A CALA K NONE M OVER TEMP IN INSP/MAINT 1 SW 27 77006 29476 NR 1 MAIN FUEL TANK FORWARD BOOST PUMP FOUND INOPERATIVE. PUMP WAS PLACARD INOPERATIVE. MX FOUND PUMP TO BE EXTREMELY HOT DURING TROUBLESHOOTING. CONNECTOR COULD NOT BE REMOVED & WIRING HAD MELTED OFF PUMP. APPROX 6 INCHES OF WIRING HAR NESS WAS BURNED & CONNECTOR WAS BURNED. RELATED CIRCUIT BREAKER HAD NOT POPPED. BOOST PUMP CONNECTOR PINS BURNED. ARCI NG OF PINS HAS BEEN ADDRESSED IN BOEING SERVICE BULLETIN 777-28-0028. VENDOR TEARDOWN FOUND THAT THE PRIMARY CAUSE OF TH E PIN FAILURE TO BE CONTAMINANT INGRESS/PRESENCE. CONTAMINANT COMBINED WITH FRETTING DAMAGE TO GOLD LAYER OF PINS RESULT S IN GALVANIC CORROSION DAMAGE BETWEEN THE PINS AND AIRCRAFT FEMALE SOCKETS. 2 L 7 2 4F RT T00001SE 2007012500350 20070125 00350 NM 2007 1 25 SWAA070317 1 20070122 A 2560 6557463 FITTING BOEING 737 7373T5 1384608 NM L1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007012500352 20070125 00352 NM 2007 1 25 SWAA070319 1 20070122 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 771SA 27879 DURING SCHEDULED HC1 CHECK, FWD CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007012500363 20070125 00363 CE 2007 1 25 DXTA200701834 1 20070103 A 3240 UNKNOWN BEECH MU300 400A 1155402 CE BRAKE ASSY UNKNOWN E DXTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 153QS RK490 BRAKE PEDALS FEEL SPONGY ON LT AND RT SIDE. BRAKES DO STOP AIRCRAFT BUT TAKE EXCESSIVE AMOUNT OF TRAVEL. BLEED BRAKES REF MM 32-40-00. NO DEFECT NOTED. TAXIED AIRCRAFT AND TESTED BRAKING SYSTEM. NO DEFECT NOTED. PEDALS FUNCTION NORMAL LY AT THIS TIME. 2 H 7 2 4F RT A16SW 2007012600011 20070126 00011 NM 2007 1 26 AALA20070065 1 20070111 A 3350 LIGHT BOEING 757 757223 1384957 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 624AA 24582 SFO - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. RELAMPED EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ON E DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007012600012 20070126 00012 NM 2007 1 26 AALA20070066 1 20070111 A 3350 LIGHT BOEING 757 757223 1384957 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 624AA 24582 SFO - EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. RELAMPED EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007012600021 20070126 00021 NM 2007 1 26 AALA20070084 1 20070114 A 3350 LENS BOEING 737 737823 13844BZ NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 950AN 30087 MIA - EMERGENCY LIGHT AT SEAT 15D HAS MISSING LENS COVER. REPLACED LENS COVER FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007012600022 20070126 00022 NM 2007 1 26 AALA20070086 1 20070114 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 661AA 25295 DFW - EMERGENCY LIGHT IN CEILING AT FORWARD MID LAVATORY INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT AT CEILI NG FORWARD MID LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007012600048 20070126 00048 WP 2007 1 26 AMTA200700032 1 20070124 A 5753 ATTACH FITTING LKHEED 1011 10113853 5265020 WP NR 2 FLAP CHAFED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 164AT 1238 LEFT NR 2 FLAP OUTBOARD ATTACH FITTING WITH CHAFING. REPAIRED PER EER 12926 GAMCO WORKORDER 316063. (M) 2 L 7 3 4F A23WE 2007012600061 20070126 00061 SO 2007 1 26 RAIA00701034 1 20070124 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 817HK 145058 PRE FLT NR 5517 - STL - EMERGENCY LIGHT IN GALLEY INOP. MAINTENANCE RESECURED THE CONNECTOR TO THE LIGHT ASSEMBLY. 2 L 7 2 4T RT T00011AT 2007012600068 20070126 00068 NM 2007 1 26 SWAA070352 1 20070124 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 64, WL 200. REPAIRED FRAME SECTION PER ER. 2 L 7 2 4F RT A16WE 2007012600079 20070126 00079 NM 2007 1 26 SWAA070342 1 20070124 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007012600090 20070126 00090 2007 1 26 2007UALA00172 4 20070123 A 2565 5A29011 ASPIRATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ESCAPE SLIDE UNSERVICEABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA PK0075 27115 BOTH ASPIRATORS LEAKING. SLIDE REPLACED. A/C RETURNED TO SERVICE. DAMAGE TO ONE ASPIRATOR CAUSED DURING PACKING. OTHE R ASPIRATOR SHOWED IMPROPER ASSEMBLY OF ASPIRATOR'S JET PLATE DURING INITIAL FABRICATION. 2 L 7 2 4F 4 F RT A1NM E24NE 2007012600093 20070126 00093 NM 2007 1 26 USAA070068 1 20070124 A 5754 SKIN BOEING 737 737401 1384701 NM L/E SLAT WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 LOWER I/B CORNER T/E WEDGE NR 4 SLAT, WORN AREA/CHAFED. INSTALLED DOUBLER PER SRM 57-41-01-1A, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007012600097 20070126 00097 NM 2007 1 26 USAA070066 1 20070124 A 5313 STRINGER BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 RADIUS LT STRINGER 5A STA 1138 AT FUSELAGE CUTOUT FOR HORIZ STAB AFT LUG HAS CRACK. INSTALLED DOUBLER, REPAIR ANGLES PE R SRM 53-00-01 FIG 201, REP 21, DEFECT SIZE: 3 INCHES. 2 L 7 2 4F RT A16WE 2007012600098 20070126 00098 NM 2007 1 26 AMTA200700019 1 20070118 A 3020 7646B000 ANTI-ICE VALVE BOEING 757 75733N 1384931 NM LT ENGINE MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 11 561TZ 33526 EICAS MSG L ENG ANTI-ICE DISPLAYED AND ENG ANTI-ICE VALVE LIGHT REMAINED ILLUMINATED WITH SWITCH ON. REMOVED AND REPLAC ED LEFT ENGINE INLET TAI VALVE PER MM 30-21-03-4, OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A2NM 2007012600099 20070126 00099 WP 2007 1 26 AMTA200700029 1 20070124 A 5753 ATTACH FITTING LKHEED 1011 10113853 5265020 WP NR 1 FLAP CHAFED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 164AT 1238 RIGHT WING NR 1 FLAP INBOARD ATTACH FITTING WITH CHAFING MARK. REPAIRED PER EER 12929 GAMCO WORK ORDER 316063. (M) 2 L 7 3 4F A23WE 2007012600105 20070126 00105 WP 2007 1 26 AMTA200700028 1 20070124 A 5753 ATTACH FITTING LKHEED 1011 10113853 5265020 WP NR 3 FLAP GOUGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 164AT 1238 RIGHT WING NR 3 FLAP INBOARD ATTACH FITTING UPPER SURFACE WITH GOUGE. REPAIRED PER EER 12928 GAMCO WORKORDER 316063. ( M) 2 L 7 3 4F A23WE 2007012600112 20070126 00112 WP 2007 1 26 0700239861 1 20070114 A 5315 FLOORBEAM DOUG DC9 DC951 3022051 WP BS 148 TOOL DAMAGE A NWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 01 770NC 47758 DURING "L" CHECK, FOUND DRILL START IN THE UPPER FLANGE OF THE FLOORBEAM AT BS 148 RBL 13. REPAIRED PER EA 98-208456. 2 L 7 2 4F RT A6WE 2007012600113 20070126 00113 NM 2007 1 26 0700256732 1 20070104 A 5313 LONGERON BOEING 747 747251B 1384892 NM BS 2701-2709 DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 632US 23112 DURING "L" CHECK WHILE PERFORMING REPLACEMENT OF DAMAGED TAILCONE FOUND MISALIGNED FASTENER HOLES IN LT UPPER LONGERON B ETWEEN BS 2701 AND BS 2709. REPAIRED PER EA 67-208745. 2 L 7 4 4F A20WE 2007012600116 20070126 00116 NM 2007 1 26 USAA070061 1 20070124 A 5310 DOOR FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 442US 24841 FWD CARGO DOOR/FWD FRAME AT 1F FOOTPRINT HAS CRACK. REMOVED DAMAGE & INSTALLED FABRICATED REPAIR PARTS PER EA 98414, DE FECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007012600126 20070126 00126 NM 2007 1 26 USAA070059 1 20070124 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 442US 24841 E&E AREA EXHAUST PORT FOR EQUIPMENT COOLING HAS CRACK. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER EA 98416, DEFECT SIZ E: 1 INCH. 2 L 7 2 4F RT A16WE 2007012600140 20070126 00140 SO 2007 1 26 SWIA200717690 1 20070118 A 5712 RIB EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 308SW 120326 LEFT INBOARD WING RIB NR 8 LOWER CLIP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP ON LEFT INBOARD WING RIB NR 8 LOWER. SEE RII 28-900-1000 IAW SRM 51-40-02. 2 L 7 2 4T RT A31SO 2007012600142 20070126 00142 NM 2007 1 26 C8GA20070002 1 20070112 A 2612 CONTROL UNIT BOEING 727 727227 1384078 NM FIRE DECTECTION MALFUNCTIONED A C8GA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 29 89427 21365 FLT 711 FROM DEN TO TOL, AFTER TAKEOFF FROM DEN, AFT CARGO COMPARTMENT INDICATED A FIRE. EMERGENCY WAS DECLARED AIRCRAF T RETURNED TO DEN AND LANDED WITHOUT INCIDENT. ON POST FLIGHT, INSPECTED AFT CARGO COMPARTMENT FOR FIRE OR SMOKE, NO IN DICATIONS WERE PRESENT. ITEM WAS PLACED ON DMI AND AIRCRAFT WAS RETURNED TO SERVICE. FURTHER TROUBLESHOOTING, RESET CB 'S RAN SYSTEM TESTS OF LOWER CARGO SMOKE DETECTION SYSTEM OPS CHECKS GOOD, DMI CLEARED, PLACARDS REMOVED. AS PRECAUTION ARY REMOVED AND REPLACED CENTRAL CONTROL UNIT, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2007012600151 20070126 00151 EU 2007 1 26 2007UALA00174 1 20070123 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 410UA 463 AFTER REINSTALLING DOOR 2L SLIDE WHILE ACP EMERGENCY LIGHT TEST FAILS TEST SHOWS EPSU COM 1 LT ON CIDS PANEL. MSG WAS E PSU EXT LOADS FWD LT AND COM FWD LT. REPLACED EPSU AND BATTERY, NO HELP. REINSTALLED ORIGINAL EPSU AND BATTERY. AC COMPLISHED TEST, TEST PASSED, NO FAULTS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007012600152 20070126 00152 2007 1 26 UPS07148867 4 20070113 A 2565 LEVER AIRBUS A300 A300F4622R 3930360 EU SLIDE ARM STIFF A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 159UP 0848 WHILE DISARMING SLIDE, LEVER HANGS UP 2/3 OR THE WAY. REQUIRES FIRM MOTION TO GET PAST 2/3 POSITION. CLEANED DEBRIS FR OM GIRT BAR FITTINGS AND GREASED GIRT. MEASURED HANDLE FORCE AT 18 LBS. OK PER MM 52-10-11-05. 2 L 7 2 4F RT A35EU 2007012600154 20070126 00154 NE 2007 1 26 2007UALA00176 2 20070123 A 7200 ENGINE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 STALLED A UALA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 29 836UA 1460 V10945 NR 2 ENGINE STALL AT 39K. CREW COMMENTS: ENGINE 2 STALL ECAM AT 39000 FT-CRUISE UNACCELERATED FLT DURING MOD TURBULENCE . CLEARED WITHIN 2 SECONDS ALL INDICATIONS REPORTED NORMAL PER CREW. ACCOMPLISHED BOROSCOPE INPECTION OF NUMBER 2 ENGI NE HPC STAGES 3 AND 6. FOUND MISSING BLADE AND DAMAGE OUT OF LIMITS TO ALL BLADES OF STAGE 6 HPC. REPLACED ENGINE NUMB ER 2 2 L 7 2 4F 4 F RT A28NM E40NE 2007012600155 20070126 00155 NM 2007 1 26 2007UALA00177 1 20070124 A 5320 WEB BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 128UA 30023 WEB INBOARD CHORD HAS HOOKED SHAPE CRACK. FWD CARGO AREA, LT SIDE STA 800. REMOVED DAMAGED CAP ANGLE SECTION OF FWD CA RGO FLOOR SUPPORT, LEFT SIDE, STA 800, AND REPLACED WITH NESTED ANGLE REPAIR PER SRM. SUSPECT DAMAGED BY PRY BAR CONTACT DURING UNLOADING. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012600156 20070126 00156 2007 1 26 UPS07148869 4 20070112 A 2565 ANNUNCIATOR AIRBUS A300 A300F4622R 3930360 EU SLIDE NO TEST A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 129UP 0813 FWD ENTRY DOOR EVACUATION SLIDE WARNING SYSTEM BUZZER WON'T TEST (INOP) PROPERLY. PERFORMED ADJ/TEST PER AMM 52-73-00-0 5. SYSTEM TESTS NORMAL. THIS CLEARS M341897. 2 L 7 2 4F RT A35EU 2007012600157 20070126 00157 NM 2007 1 26 2007UALA00178 1 20070123 A 3350 POWER UNIT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 311UA 23672 EMERGENCY EXIT FLOOR LIGHTING OUT FROM SEAT 15 AFT. REPLACED POWER STRIP IN FLOOR TRACK. OP CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012600162 20070126 00162 NM 2007 1 26 2007UALA00181 1 20070123 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 DOOR 2L EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. RELAMPED AND OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007012600167 20070126 00167 NM 2007 1 26 CALA0700019 1 20070118 A 5320 147A5660Y22 INTERCOSTAL BOEING 737 737724 13844BY NM BS 949 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14735 28950 INSPECTION FOUND INTERCOSTAL CORRODED AT STA 949.5, RBL 51. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007012600170 20070126 00170 NM 2007 1 26 UPS07M48870 1 20070112 A 3350 LIGHT DOUG MD11 MD11F 3023600 NM COCKPIT MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP 48745 EMERGENCY EXIT LIGHTS ON IN ARM. PASSED EMERGENCY LIGHT TEST BUT LIGHT IS STILL ON. T/S PER FIM 33-52-01-00 BLK 1. FO UND EMERGENCY LIGHT CONTROL C/B WAS OPEN. CLOSED C/B C/O EMERGENCY LIGHT TEST PASS ON THE EAD, FOUND C/B WAS CLOSED ALL THE WAY AFTER THE TEST. C/O COUPLE OF TIMES TEST. SYSTEM GOOD. ITEM CLOSED. 2 L 7 3 4F RT A22WE 2007012600173 20070126 00173 EU 2007 1 26 TRAX200700053 1 20070109 A 5312 BULKHEAD AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 635AS 372 FR1 FWD PRESSURE BULKHEAD CORROSION FOUND AT BONDING POINTS (6X SPOTS). 2 H 7 2 4T RT A53EU 2007012600174 20070126 00174 EU 2007 1 26 TRAX200700054 1 20070109 A 5712 RIB AEROSP ATR72 ATR72212 8680945 EU LT WING BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 635AS 372 LT WING AT RIB 13 UPPER FLAP BEAM OMEGA BRACKET BROKEN. 2 H 7 2 4T RT A53EU 2007012600175 20070126 00175 EU 2007 1 26 TRAX200700055 1 20070109 A 5712 RIB AEROSP ATR72 ATR72212 8680945 EU LT WING BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 635AS 372 LT WING AT RIB FWD HINGE AFT OMEGA BRACKET BROKEN. 2 H 7 2 4T RT A53EU 2007012600178 20070126 00178 SO 2007 1 26 SIMA200701511 1 20070115 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 653AE 13302 4800 145433 FOUND CARGO DOOR FRAME CENTER SILL CORRODED. REMOVED AND REPLACED SILL, CLEANED AND TREATED AREA. RESTORED SURFACE PRO TECTIVE FINISH IAW EMB SRM 51-21-04, 51-21-05 AND 51-21-06. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007012600179 20070126 00179 SO 2007 1 26 SIMA200701512 1 20070114 A 5315 14530645411 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 653AE 13302 145433 FOUND LEFT OMEGA BEAM CORRODED AT FRAME 20. REMOVED EXISTING REPAIR. CLEAN AND TREATED AREA. FABRICATED REPAIR DOUBLE R. INSTALLED DOUBLER AND RESTORED PROTECTIVE FINISH IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007012600180 20070126 00180 EU 2007 1 26 MALA070018 1 20070123 A 3230 HP848430721 LANDING GEAR SAAB SF340 340B 7860101 EU MAINS UNKNOWN A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 451XJ 340B451 CREW REPORTED NO THREE GREEN DOWN AND LOCKED LIGHTS WHEN GEAR SELECTED AND IN TRANSIT LIGHT REMAINED ILLUMINATED. FOLLO WED QRH AND PULLED EMERGENCY GEAR HANDLE RELEASE, GEAR SHOWED 3 GREEN. AFTER PULLING THE EMERGENCY HANDLE AND PUMPING F OR ABOUT 10 SECONDS THE GEAR LOCKED DOWN. HYDRAULIC PRESSURE WAS NORMAL. REPLACED LANDING GEAR CONTROL VALVE IAW JOBCA RD 3230-301. PN ON AND OFF HP848430-721 SN ON 2080 SN OFF 2107. REPLACED LEFT EXPLOSIVE SEPARATION BOLTS AND RIGHT EXP LOSIVE SEPARATION BOLTS. 2 L 7 2 4T RT A52EU 2007012600181 20070126 00181 NM 2007 1 26 DHL2007760003 1 20070124 A 2710 LINE BOEING 727 7272B7 138407L NM HYD SYSTEM LEAKING A DHLA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 01 760AT 21954 A ENG 1/2 HYDRAULIC PUMP LOW PRESS LIGHTS ILLUMINATED IN FLT LOSS OF ALL A PRESS AND QUANTITY PERFORMED HYDRAULIC SYSTEM A FAILED ABNORMAL CHECKLIST. FOUND FLEX LINE AT ELEVATOR POWER CONTROL PACKAGE WITH HOLE IN IT REPLACED LINE WITH TEMP (17114-4CR-0240). OPS CK NORMAL IAW MM 27-30-81. 2 L 7 3 4F A3WE 2007012600189 20070126 00189 EA 2007 1 26 REXA200700002 1 20070117 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA NR 2 CONTAMINATED A REXA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 25 8409N 7409 AIR RETURN FOR SMOKE IN COCKPIT. LANDING UNEVENTFUL. REMOVED AND REPLACED NR 2 COALESCER BAG IAW BOMBARDIER AEROSPACE AMM, RAN ENGINES AND APU, NO SMELL OR SMOKE NOTED. 2 L 7 2 4F RT A21EA 2007012600190 20070126 00190 EA 2007 1 26 REXA200700003 1 20070116 A 2750 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS LACK OF LUBE A REXA O OTHER W J INADEQUATE Q C WARNING INDICATION AP APPROACH 1 SO 25 8745B 7745 FLAPS FAIL CAUTION MESSAGE WHEN SELECTING APPROACH. FLAPS FAILED AT ZERO DEGREES. PERFORMED QRH. LANDING UNEVENTFUL. C/W AD 2006-12-21 BY CLEANING, LUBRICATING, AND SEALING LT AND RT FLAP FLEX DRIVE SHAFTS IAW AMM 27-53-10. 2 L 7 2 4F RT A21EA 2007012600191 20070126 00191 EA 2007 1 26 REXA200700004 1 20070117 A 2750 SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS LACK OF LUBE A REXA O OTHER W J INADEQUATE Q C WARNING INDICATION AP APPROACH 1 SO 25 8745B 7745 FLAPS FAIL. LANDING UNEVENTFUL. CLEANED AND LUBED ALL FLEX SHAFT AND COMPLIED WITH AD 2006-12-21. 2 L 7 2 4F RT A21EA 2007012600192 20070126 00192 EA 2007 1 26 TRAX200700068 1 20070111 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA LT OVERWING INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 878AS 7590 LT OVERWING EMER LIGHT IS INOP. 2 L 7 2 4F RT A21EA 2007012600193 20070126 00193 EA 2007 1 26 SWIA200717653 1 20070109 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT FAILED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 740SK 10196 FORWARD EMERGENCY EXIT LIGHT INOP. RELAMPED BULBS AT FORWARD EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007012600194 20070126 00194 EA 2007 1 26 SWIA200717654 1 20070107 A 3230 VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 918SW 7645 AFTER SELECTING GEAR DOWN NOSE GEAR DID NOT COME DOWN. RECYCLED GEAR HANDLE THREE TIMES, NO HELP. MANUALLY EXTENDED NO SE GEAR. REPLACED NLG PRIORITY VALVE IAW RJ 200 MM 32-33-15. OPERATIONAL CHECKS GOOD, P/N; 4622. 2 L 7 2 4F RT A21EA 2007012600195 20070126 00195 EA 2007 1 26 SWIA200717655 1 20070109 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 954SW 7815 REAR EMERGENCY EXIT POD IN CEILING BULB INOP. RELAMPED EMERGENCY LIGHT IAW AMM 33-51-00. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007012600196 20070126 00196 SO 2007 1 26 SWIA200717656 1 20070115 A 5320 SUPPORT ANGLE EMB 120 EMB120ER 3260203 SO DOOR THRESHOLD CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 297SW 120327 PAX - DOOR THRESHOLD SUPPORT ANGLE IN FUSELAGE FRAME CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED PAX DOOR S UPPORT ANGLE IAW SRM 120 51-10-02 PG 3 SEC 3B. 2 L 7 2 4T RT A31SO 2007012600197 20070126 00197 SO 2007 1 26 SWIA200717657 1 20070115 A 5310 WINDOW FRAME EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 297SW 120327 FRAME BEHIND CAPT'S DV WINDOW CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED FRAME BEHIND CAPT'S DV WINDOW IAW SRM 120 51-10-02 PG 3 SEC 3A AND RII 53-800-1000. 2 L 7 2 4T RT A31SO 2007012600199 20070126 00199 SO 2007 1 26 SWIA200717659 1 20070108 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 301YV 120301 FOUND EMERGENCY LIGHTS IN ROW 6 ARE INOP. REPLACED MIDDLE EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD IAW 33-50-02, P N: D366-04-001,SN ON: 1003/05-91, SN OFF: 720-03/90. 2 L 7 2 4T RT A31SO 2007012600201 20070126 00201 SO 2007 1 26 SWIA200717661 1 20070109 A 2121 EVAC2322C2 FAN EMB 120 EMB120ER 3260203 SO LT PACK SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 586SW 13103 13103 120354 LEFT PACK FAILED ON GROUND WITH APU BLEED. COCKPIT FILLED WITH SMOKE RAPIDLY. REPLACED LEFT GROUND COOLING FAN. OPERA TIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007012600202 20070126 00202 EA 2007 1 26 SWIA200717662 1 20070110 A 3234 750006000 SELECTOR CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 918SW 11479 11479 7645 UPON GEAR EXTENSION, GOT A GEAR DISAGREE WITH THE NOSE GEAR REMAINING UP. EXTENDED GEAR MANUALLY WITH ALL GEAR EXTENDIN G NORMALLY. REPLACED NLG SELECTOR VALVE ASSY IAW CANDAIR REGIONAL SET MM 32-22-25 PG 401. 2 L 7 2 4F RT A21EA 2007012600203 20070126 00203 EA 2007 1 26 SWIA200717663 1 20070112 A 3230 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 918SW 7645 UPON GEAR EXTENSION GOT A GEAR DISAGREE AND TOWER CONFIRMED THAT THE NOSE GEAR WAS STILL UP. PERFORMED MANUAL RELEASE G EAR EXTENSION AND RECEIVED THREE GREEN INDICATIONS. REPLACED NLG SELECTOR VALVE ASSY IAW CRJ 200 MM 32-33-10. OPERATIO NAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007012600204 20070126 00204 EA 2007 1 26 SWIA200717664 1 20070110 A 4920 38004883 APU CNDAIR CL600 CL6002B19 1900309 EA ODOR A SWIA A UNSCHED LANDING B M J SMOKE/FUMES/ODORS/SPARKS OVER TEMP WARNING INDICATION CL CLIMB 1 NM 07 455SW 2840 2840 7760 ON CLIMB-OUT, BURNING SMELL IN COCKPIT AND CABIN FOLLOWED BY APU OVERTEMP MESSAGE AND SHUT DOWN. RETURNED TO FIELD. RE PLACED APU ASSY IAW RII 49-310-1004 AND AMM 49-00-00. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007012600205 20070126 00205 NM 2007 1 26 AT0700009 1 20070109 A 5311 FRAME BOEING 717 717200 1383700 NM BS 1178 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 966AT 55027 AFT FUSELAGE COMPARTMENT LT STA 1178 CANTED FRAME CRACKED JUST BELOW L-7.L. CUT OUT DAMAGED SECTION 3.0" BY 1.0" AND IN STALLED FILLER .071" 70-75-T6 PO 021267 AND REPAIR ANGLE DOUBLER .080" 7075-0 PO NR 04721. HEAT TREATED TO T-6 PER B717 SRM 51-32-01 AND INSTALLED IAW B717 SRM 51-70-11. 2 L 7 2 4F TR A6WE 2007012600206 20070126 00206 NM 2007 1 26 AT0700010 1 20070108 A 5320 STRUCTURE BOEING 717 717200 1383700 NM VENT BOX CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 966AT 55027 RT AFT FUSELAGE COMPARTMENT VENT BOX AFT CORNER CRACKED. STOP DRILLED CRACK PER B717 SRM 51-00-07. FABRICATED AND INST ALLED REPAIR PER TASK CARD 5320-2023. 2 L 7 2 4F TR A6WE 2007012600207 20070126 00207 NM 2007 1 26 DU4R2007015 1 20070112 A 5321 FLOOR PANEL BOEING 757 757232 1384965 NM BS 1330-1470 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 HEAVY CORROSION AFT CARGO FLOOR PANEL BS 1330 TO 1470. REMOVED CORRODED PANEL. FABRICATED AND INSTALLED PANEL 139.5" B Y 40.0" FROM 2024-T3 .071" IAW B757 SRM 51-40-05, 51-40-08, 51-20-01. 2 L 7 2 4F RT A2NM 2007012600208 20070126 00208 WP 2007 1 26 ABXA070006 1 20070105 A 3340 SWITCH DOUG DC9 DC941 302207N WP TAXI LIGHT LOOSE A ABXA O OTHER O OTHER CR CRUISE 1 GL 23 957AX 47759 NOSE LIGHT SWITCH SPARKED WHEN TURNED ON. RESECURED NOSE LANDING TAXI LIGHT, SWITCH NOW OPERATES NORMAL. 2 L 7 2 4F A6WE 2007012600209 20070126 00209 NM 2007 1 26 AWXA200700114 1 20070119 A 5754 114N407611 SKIN BOEING 757 7572G7 1384963 NM ZONE 600 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 909AW 24522 MCN - CRACK FOUND ON COVE SKIN OF RIGHT WING NR 9 SLAT INBOARD PANEL 624CB, WS 574.8 - 605.3. REPAIRED COVE SKIN OF RI GHT WING NR 9 SLAT INBOARD PANEL 624CB, WS 574.8 - 605.3 IAW BOEING DWG 114N4076, B757 SRM 51-40-02-06 PAR 4-7/4-9, FIG 8-12/8-16, AND B757 SRM 51-40-04-0E, FIG 1. 2 L 7 2 4F RT A2NM 2007012600210 20070126 00210 2007 1 26 COMA0770004 4 20070116 A 3418 C16258AA SENSOR CNDAIR CL600 CL6002C10 1390015 EA AOA FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 331CA 11210 10061 FLIGHT 5440 - STALL FAIL CAUTION MESSAGE IN FLIGHT, AIRCRAFT DIVERTED TO CVG AND LANDED SAFELY. REMOVED AND REPLACED NR 2 AOA SENSOR. 2 L 7 2 4F RT A21EA 2007012600213 20070126 00213 EA 2007 1 26 TRAX200700075 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 350-495 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND RT SIDEWALL SEAT TRACK CORRODED, FS 350 TO 495, SEC 1. 2 L 7 2 4F RT A21EA 2007012600214 20070126 00214 NM 2007 1 26 2007UALA00183 1 20070124 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 OVERWING EMERGENCY LIGHT LT 2 BOTTOM INOP. REPLACED LAMP IN OW LEFT HAND DOOR, BOTTOM EEL. OP CKD NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012600215 20070126 00215 NM 2007 1 26 2007UALA00184 1 20070124 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY LIGHT ROW 35 HKJ INOPERATIVE. REPLACED EMERGENCY LIGHT. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012600216 20070126 00216 NM 2007 1 26 2007UALA00185 1 20070124 A 3350 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY LIGHT ROW 58 ABC INOPERATIVE. RESECURED LIGHT CONNECTOR. OP CK NORMAL. SUSPECT IMPACT BY PASSENGER OR IN-FLT SVCE PERSONNEL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012600217 20070126 00217 NM 2007 1 26 2007UALA00186 1 20070124 A 3397 POWER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY LIGHT ROW 35 ABC TO 44 ABC INOPERATIVE. REPLACED EEL POWER LEAD. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012600218 20070126 00218 NM 2007 1 26 2007UALA00187 1 20070124 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 DOOR 3 LEFT FWD EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK. OP CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012600219 20070126 00219 NM 2007 1 26 2007UALA00188 1 20070124 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY LIGHT ROW 32, 33, 34 ABC INOPERATIVE. REPLACED BATTERY PACK. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012600220 20070126 00220 EU 2007 1 26 2007UALA00189 1 20070124 A 7710 STALL WARNING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 422UA 503 V10043 NR 1 ENG STALL DISPLAYED ON UPPER ECAM SCREEN DURING STEADY STATE CLIMB OR CRUISE. ENGINE NOT SHUTDOWN. PERFORMED FUN CTIONAL CHECK OF 7TH AND 10TH STAGE HPC VALVES. FOUND 7TH STAGE B AND C VALVES STUCK. REPLACED 7TH STAGE HPC. FADEC INTERROGATION REPORT REFLECTS VSV MECH BLD VLV LPC1 LATCHED. PERFORMED BORO INSPECTION OF HPC STG 3 AND 6 ON NR 1 ENGIN E. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007012600221 20070126 00221 NM 2007 1 26 2007UALA00191 1 20070124 A 3260 405FW504B SWITCH BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NLG MALFUNCTIONED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 350UA 24301 ON TAKEOFF NOSE GEAR GREEN AND RED LIGHTS REMAINED ON AFTER RETRACTION. EXPERIENCED REOCCURRENCE ON SUBSEQUENT FLIGHT. FAULTY NOSE UPLOCK LOGIC CARD AND INTERMITTMENT NOSE GEAR LOCK SWITCH. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012600222 20070126 00222 NM 2007 1 26 2007UALA00192 1 20070124 A 5512 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZ STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 LEFT HORIZ STAB LOWER SKIN CRACKED AT AFT SPAR APPROX 70 INCHES FROM ROOT. MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED EXTERNAL DOUBLER AND FILLER REPAIR PER MM 55-10-94 PAGE 801. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012600223 20070126 00223 NM 2007 1 26 2007UALA00193 1 20070124 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE SCRATCHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 UPPER FUSELAGE EXTERIOR SKIN SCRATCHED AT STA 287 STR 3L. MAJOR REPAIR: REMOVED DAMAGE. ACCOMPLISHED FILLER AND DOUBL ER REPAIR PER SRM 53-00-01 REPAIR 31 DETAIL IX. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012600224 20070126 00224 NM 2007 1 26 2007UALA00194 1 20070124 A 2820 CHECK VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT FUEL TANK STUCK A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 644UA 25094 FUEL CONFIG LIGHT ON AND RT MAIN TANK QTY INCREASED TO 42.6 WHEN LEFT READS 40.4. TTL READS 127.3 AND FMC CALC READS 124 .1. FUEL AT DEPT READ 126.6. [5-1-07] REPLACED RT FUEL TANK COMPENSATOR & EMITTER. ALSO, SUSPECT RT MAIN INTANK HARNE SS. REPLACED RT MAIN INTANK HARNESS & SUMMING PLUG. SEALED & RETURNED TO SERVICE. FUEL TANK IMBALANCE STILL PARTIALLY I NDICATED UNTIL 26MAR07. A/C INPUT TO GSO FOR C13 VISIT 27MAR07. PERFORMED FUEL TANK FLAME ARRESTOR MOD. NO RECURRENCE OF FUEL IMBALANCE AFTER C13 VISIT. SUSPECT TANK WORK/ MOD ACTIVITY RELIEVED A PARTIALLY STUCK FUEL CHECK VALVE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007012600225 20070126 00225 NM 2007 1 26 2007UALA00195 1 20070124 A 3510 OXYGEN SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CREW O2 LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 302UA 23643 CREW OXYGEN SYSTEM LOW. FOUND O2 PRESSURE AT 1K PSI. SERVICE OXYGEN SYSTEM TO FULL. [SUP 4-17-07] CAUSE UNKNOWN, SER VICED OXYGEN SYSTEM TO FULL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012600226 20070126 00226 NM 2007 1 26 2007UALA00196 1 20070125 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 46L & AT AFT CREW REST STAIR LIGHT. REPLACED LIGHT ASSY BOTH POSITIONS. BOTH OP CHECK NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012500236 20070125 00236 EU 2007 1 25 2007UALA00095 1 20070112 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 410UA 463 FWD L COMM MSG ON TEST EMERGENCY LIGHT SYSTEM TEST. REPLACED EPSU. EMERGENCY LIGHT TEST PASSED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007012500257 20070125 00257 NM 2007 1 25 2007UALA00098 1 20070113 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 669UA 30025 LEFT MIDDLE OVERWING EXTERIOR EMERGENCY AFT BULB EMERGENCY LIGHT INOPERATIVE. LT MIDDLE OVERWING EXTERIOR EMERGENCY AF T EMERGENCY LIGHT INOP. RELAMPED. CHECKED OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007012500274 20070125 00274 NM 2007 1 25 2007UALA00131 1 20070118 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 STA 360 INBOARD OF STR 27 LEFT SHEAR TIE HAS A DAMAGED HOLE. MAJOR REPAIR: FABRICATED AND INSTALLED NEW SHEAR TIE PER SRM 53-00-07 PAGE 201. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012500275 20070125 00275 NM 2007 1 25 2007UALA00132 1 20070118 A 5330 SKIN PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 EXTERIOR FUSELAGE SKIN BS 964 TO 970 LBL 12 SKIN WORN AT DORSAL FIN SEAL AREA. MAJOR REPAIR: FABRICATED AND INSTALLED D OUBLER TRIPLER AND STAINLESS WEAR TRIPLER PER AAR EA I060562 REV IR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012500285 20070125 00285 NM 2007 1 25 SWAA070308 1 20070122 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 474WN 33861 EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007012500309 20070125 00309 SO 2007 1 25 C2XA07RI004 1 20070119 A 3230 355022002MOD4 ELECTRONIC UNIT EMB 145 EMB145LR 3260212 SO E&E BAY MALFUNCTIONED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 14902 9267 3247 145496 FLT 2820 - EWR - DURING CLIMB LANDING GEAR WILL NOT RETRACT - AIR/GROUND FAIL. FLIGHT CREW PERFORMED AN AIR RETURN AND LANDED UNEVENTFULLY. MX PERFORMED TROUBLESHOOTING AND FOUND LGEU FAIL. MX REMOVED AND REPLACED LGEU AND PERFORMED OPER ATIONAL TESTS SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007012500311 20070125 00311 SO 2007 1 25 C2XA07IA018 1 20070120 A 2120 14522273401 DUCT EMB 145 EMB145XR 3260214 SO CABIN RUPTURED A C2XA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 27 33182 14500909 MCO - FLT 4932, ON TAKEOFF AT 1200 FT THE CREW RECEIVED A LAV SMOKE WARNING, AND THE AIRCRAFT STARTED FILLING UP WITH SM OKE. THE SMOKE COLOR WAS DARK GREY STARTED AT REAR OF A/C FILLED UP ALL THE WAY TO COCKPIT. THE AIRCRAFT RETURNED TO I AH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED A CABIN DISTRIBUTION DUCT, PERFORMED ENG RUNS, BL EED OPS AND ICE TEST WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007012500314 20070125 00314 NM 2007 1 25 WRLA2007015 1 20070121 A 3350 551981 BATTERY PACK DOUG MD11 MD11 3023602 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A WRLA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 11 801DE 48472 NR 1 EMERGENCY LIGHT PWR SUPPLY HAS A LOW ALERT. REMOVED AND REPLACED BATTERY PACK PER MM 33-51-00. OPS NORMAL. 2 L 7 3 4F 4 F RT A22WE E24NE 2007012500334 20070125 00334 NM 2007 1 25 2007F00009 1 20070111 A 5610 4AS3430000510 WINDSHIELD GULSTM 200 200 4500308 NM COCKPIT CRACKED E K NONE O OTHER UK UNKNOWN 1 SO 19 726DA 58 TAKEN FROM AIR TAXI TURBINE DAILY RECORD SHEET/MANIFEST. RT COCKPIT WINDSHIELD IS SHATTERED. REMOVED AND REPLACED RT C OCKPIT WINDSCREEN IAW G-200 M/M 56-10-05. NO LEAKS NOTED. WINDSHIELD HEATING SYSTEM OPS OK. AIRCRAFT RECORD TAKEN FRO M GENERAL DYNAMICS AVIATION SERVICE, DALLAS TEXAS. ACCOMPLISHED THE FOLLOWING MAINTENANCE AND INSPECTIONS: REMOVED CO- PILOT WINDSHIELD 4AS3430000-510 S/N 01211H4481 AND INSTALLED NEW WINDSHIELD P/N 4AS3430000-510 S/N 06352H9987. OPERATIO NAL TEST NORMAL. REFERENCE CMP CODES 561005, 561001, 304001 AND G-200 M/M 56-10-00 AND 21-30-00 FOR WORK PERFORMED. TH E MAINTENANCE LISTED ABOVE WAS PERFORMED IN ACCORDANCE WITH AIW AIR TAXI INC'S AAIP AND MANUFACTURERS MAINTENANCE MANUAL 2 L 7 2 4F RT A53NM 2007012500343 20070125 00343 NM 2007 1 25 KCSA071020 1 20070116 A 5340 FITTING BOEING 747 747209F 1384800 NM PWA JT9 JT9D7R4G2 52054 NE BS 2360 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 BS 2360 PRESSURE BULKHEAD S50R END FITTINGS ARE CORRODED ON FORWARD AND AFT SIDES. 2 L 7 4 4F 4 F RT A20WE E3NE 2007012500353 20070125 00353 NM 2007 1 25 SWAA070320 1 20070122 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 771SA 27879 DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007012500362 20070125 00362 NM 2007 1 25 SWAA070328 1 20070123 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012500406 20070125 00406 NM 2007 1 25 SWAA070334 1 20070123 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012500407 20070125 00407 NM 2007 1 25 SWAA070335 1 20070123 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012600007 20070126 00007 NM 2007 1 26 DU4R2007016 1 20070114 A 5320 65C80678180 SUPPORT BOEING 757 757232 1384965 NM THRESHOLD CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION AFT CARGO DOOR THRESHOLD BOEING CASTING BS 1400. REPAIRED BY REMOVING AND INSTALLING NEW SUPPORT P/N 65C80678 -180 IAW B757 SRM 51-40-02, AND 51-40-04. 2 L 7 2 4F RT A2NM 2007012600016 20070126 00016 NM 2007 1 26 AALA20070079 1 20070113 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 181AN 29591 DFW - EMERGENCY LIGHT AT M735 INOPERATIVE. REPLACED BATTERY PACK AT M735 FOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2007012600017 20070126 00017 EU 2007 1 26 AALA20070080 1 20070114 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 59081 639 MIA - EMERGENCY LIGHT AT SEAT 17C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 17C. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A35EU 2007012600019 20070126 00019 EU 2007 1 26 AALA20070082 1 20070114 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 59081 639 MIA - EMERGENCY LIGHT AT SEAT 33G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 33G. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F RT A35EU 2007012600029 20070126 00029 NM 2007 1 26 DU4R2007019 1 20070117 A 5320 SUPPORT BOEING 757 757232 1384965 NM BS 1470 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION AFT CARGO BS 1470 RBL 16.10 CARGO SUPPORT STRINGER CORROSION AROUND NUT PLATE HOLE. REPAIRED BY REMOVING FLOO R SUPPORT BS 1445 TO BS 1555, FABRICATED AND INSTALLED NEW FLOOR SUPPORT 60" BY 3-1/2" FROM 7075-T6 .063" IAW B757 SRM 5 3-60-53, FIG 1, AND 51,10-01 PG 3-7, 21 AND 51-40-02. 2 L 7 2 4F RT A2NM 2007012600035 20070126 00035 NM 2007 1 26 DU4R2007021 1 20070113 A 5320 SUPPORT BRACKET BOEING 757 757232 1384965 NM BS 984 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION ON SUPPORT BRACKET AT BS 984 JUST BELOW RT WING FWD EMERG ESCAPE DOOR. REPAIRED BY REMOVING BRACKET, FABRICAT ED AND INSTALLED REPAIR BRACKET 3" BY 2" FROM 7075-T6 .071" IAW B757 SRM 53-40-15, 51-40-02 AND 51-30-01. 2 L 7 2 4F RT A2NM 2007012600036 20070126 00036 WP 2007 1 26 ABXA070018 1 20070125 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 957AX 47759 EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00-8-0001. 2 L 7 2 4F A6WE 2007012600037 20070126 00037 NM 2007 1 26 DU4R2007022 1 20070122 A 5320 146N5246U5 FLOOR SUPPORT BOEING 757 757232 1384965 NM BS 1660-1680 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION AT L-4 DOOR AFT FLOORBOARD SUPPORT BETWEEN BS 1660 AND BS 1680 B/L 54L I/B OF S-17L AT NUTPLATES. REPAIRED BY REMOVING FLOOR SUPPORT. INSTALLED P/N 146N5246U5 IAW B757 SRM 51-40-05 AND 51-40-02. 2 L 7 2 4F RT A2NM 2007012600044 20070126 00044 EA 2007 1 26 TRAX200700114 1 20070120 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 923EV 7826 FUSELAGE EMERGENCY LIGHT NOT COMING ON. 2 L 7 2 4F RT A21EA 2007012600054 20070126 00054 NM 2007 1 26 KCSA071043 1 20070123 A 5315 FLOORBEAM BOEING 747 747209F 1384800 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 STA 780 RBL 22 FLOORBEAM UPPER CAP DAMAGED. 2 L 7 4 4F RT A20WE 2007012600056 20070126 00056 NM 2007 1 26 KCSA071045 1 20070124 A 5313 STRINGER BOEING 747 747209F 1384800 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 FUSELAGE STRINGER IS CRACKED AT STA 280, STR 41R. 2 L 7 4 4F RT A20WE 2007012600057 20070126 00057 NM 2007 1 26 R5KB0107002 1 20070108 A 3350 900835A BATTERY PACK BOEING 727 727191 1384063 NM CABIN DISCHARGED I R5KB K NONE L NO TEST IN INSP/MAINT 1 SO 33 502M 149 N2740 19391 RIGHT SIDE CENTER EMERGENCY ESCAPE LIGHT INOP. 2 L 7 3 4F A3WE 2007012600091 20070126 00091 NM 2007 1 26 BB07011 1 20070123 A 3350 SOCKET BOEING 767 767201 1385125 NM CABIN FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 245AY 23897 MAINTENANCE FOUND FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE AT ROWS 5 AND 6. REPLACED ONE LIGHT SOCKET. NO FURTHER DIFF ICULTIES. 2 L 7 2 4F RT A1NM 2007012600094 20070126 00094 NE 2007 1 26 AMTA200700034 2 20070119 A 7310 FILTER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE ENGINE FUEL UNKNOWN A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 402TZ 24667 724575 NR 2 ENGINE EXTREMELY SLOW TO SPOOL UP WHEN THROTTLE ADVANCED. INSPECTED REMOVED AND REPLACED NR 2 ENGINE MAIN FUEL FIL TER AS EPR 73-11-02. PERFORMED ENGINE TEST NR 8 ACCEL/DECEL CHECK AS PER 71-00-00 PAGE 577 WITHIN LIMIT. (M) 2 L 7 2 4F 4 F RT A16WE E2GL 2007012600101 20070126 00101 WP 2007 1 26 AMTA200700027 1 20070124 A 5753 ATTACH FITTING LKHEED 1011 10113853 5265020 WP NR 2 FLAP GOUGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 164AT 1238 RIGHT WING NR 2 FLAP ATTACH FITTING TOP AREA WITH GOUGE. REPAIRED PER EER 12927 GAMCO WORK ORDER 316063. (M) 2 L 7 3 4F A23WE 2007012600104 20070126 00104 NM 2007 1 26 USAA070064 1 20070124 A 5414 SKIN BOEING 737 7374B7 1384702 NM LT PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 442US 24841 PYLON SKIN, LT PYLON PANEL CUTOUT NR 5728L HAS CRACK. INSTALLED DOUBLER & REPAIR PARTS PER T/R 54-30-07, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007012600150 20070126 00150 NM 2007 1 26 2007UALA00173 1 20070124 A 5414 FAIRING BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RT NACELLE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 228UA 30556 CRACK IS FOUND ON RIGHT NACELLE AFT FAIRING, LWR LEFT CHORD, SAF STA 16.152. REMOVED AND REPLACED DAMAGED CHORD. AIRCR AFT RETURNED TO SERVICE.SUSPECT COMBINATION OF VIBRATION & FATIGUE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007012600166 20070126 00166 NM 2007 1 26 CALA0700018 1 20070118 A 5320 147A5660Y21 INTERCOSTAL BOEING 737 737724 13844BY NM BS 947 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14735 28950 INSPECTION FOUND INTERCOSTAL CORRODED AT STA 947.5, LBL 51. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007012600172 20070126 00172 EA 2007 1 26 TRAX200700052 1 20070108 A 5230 DOOR TRACK CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 841AS 7300 FOUND CARGO DOOR TRACK CROSS BEAM MEMBER AFT SIDE BOTTOM ANGLE CRACKED (MARKED). 2 L 7 2 4F RT A21EA 2007012600176 20070126 00176 EA 2007 1 26 TRAX200700058 1 20070109 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 717EV 10088 EMERGENCY LIGHTS WILL NOT COME ON FOR MORE THAN A FEW SECONDS. 2 L 7 2 4F RT A21EA 2007012600177 20070126 00177 EA 2007 1 26 TRAX200700063 1 20070110 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 PAX DOOR WILL NOT CLOSE, FLT 4836 DEL 120 MINS. 2 L 7 2 4F RT A21EA 2007012600200 20070126 00200 EA 2007 1 26 SWIA200717660 1 20070110 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 452SW 7716 CAPT LEFT SIDE WINDOW HAS TWO CRACKS. REPLACED LEFT SIDE WINDOW IAW RII 56-220-1000 AND AMM 56-12-01, PN OFF NP139322-0 01 SN OFF 02212H2635. 2 L 7 2 4F RT A21EA 2007012600243 20070126 00243 CE 2007 1 26 ACE011507 1 20070115 A 2822 DIAPHRAGM BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA FUEL PUMP RUPTURED E YADA K NONE K FLUID LOSS NR NOT REPORTED 1 AL 03 112AX 1276 B1401 UC45 PILOT REPORTED FUEL LEAKING FROM NR 1 ENGINE DRAIN LINE. REPLACED LOW PSI PUMP DUE DIAPHRAGM RUPTURE (SUSPECTED CAUSE). 2 L 7 2 4T 4 T RT A24CE E4EA 2007012600244 20070126 00244 EA 2007 1 26 TRAX200700076 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 495-581 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND RT SIDEWALL SEAT TRACK CORRODED, FS 495 TO 581, SEC 2. 2 L 7 2 4F RT A21EA 2007012600245 20070126 00245 EA 2007 1 26 TRAX200700077 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 680-712 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND RT SIDEWALL SEAT TRACK CORRODED, FS 680 TO 712. 2 L 7 2 4F RT A21EA 2007012600247 20070126 00247 CE 2007 1 26 C90A 1 20070108 A 3213 10574XYR1145 BUSHING BEECH 90 C90A 1152911 CE PWA PT6 PT6A21 52043 EA HARTZL HCE4N HCE4N3 NE RT MLG MISSING E QVFA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 04 990TF 395 395 LJ1548 PCEPEO211 HH578 FOUND VERY SLIGHT MOVEMENT IN RT MLG OB PART OF MLG STRUT. UPON FURTHER INVESTIGATION, FOUND THAT PN 10574X-YR1145 BUSHI NG WAS NOT INSTALLED IN MLG STRUT. FURTHER INVESTIGATION FOUND THAT THIS AREA HAD NOT BEEN THOROUGHLY INSPECTED SINCE DE CEMBER 2004 DURING 6 YEAR INSPECTION OF LANDING GEAR. INSPECTED MLG ATTACH AREA FOR DAMAGE, NONE FOUND, INSPECTED TRUNN ION ATTACH AREA, NO DAMAGE FOUND. INSTALLED NEW BUSHINGS, BOLTS, WASHERS AND NUTS. SUBMITTER SUGGESTS THAT THOROUGH VISU AL INSPECTION OF BUSHING INSTALLATION BE CONDUCTED BEFORE INSTALLING WASHER AND NUT ON BOLT P/N 130909B95 1 L 7 2 3T 4 T RT 3A20 E4EA 5 C P10NE 2007012600248 20070126 00248 CE 2007 1 26 QVFA001 1 20070108 A 3213 10574XYR1145 BUSHING BEECH 90 C90A 1152911 CE PWA PT6 PT6A21 52043 EA HARTZL HCE4N HCE4N3 NE RT MLG MISSING E QVFA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 04 990TF 395 395 LJ1548 PCEPEO211 HH578 FOUND VERY SLIGHT MOVEMENT IN RT MLG OB PART OF MLG STRUT. UPON FURTHER INVESTIGATION, FOUND THAT P/N 10574X-YR1145 BUSH ING WAS NOT INSTALLED IN MLG STRUT. FURTHER INVESTIGATION FOUND THAT THIS AREA HAD NOT BEEN THOROUGHLY INSPECTED SINCE D ECEMBER 2004 DURING 6 YEAR INSPECTION OF LANDING GEAR. INSPECTED MLG ATTACH AREA FOR DAMAGE, NONE FOUND, INSPECTED TRUN NION ATTACH AREA, NO DAMAGE FOUND. INSTALLED NEW BUSHINGS, BOLTS, WASHERS AND NUTS. SUBMITTER SUGGESTS THAT THOROUGH VIS UAL INSPECTION OF BUSHING INSTALLATION BE CONDUCTED BEFORE INSTALLING WASHER AND NUT ON BOLT P/N 130909B95. 1 L 7 2 3T 4 T RT 3A20 E4EA 5 C P10NE 2007012600249 20070126 00249 EA 2007 1 26 TRAX200700079 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 785-863 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND RT SIDEWALL SEAT TRACK CORRODED, 785 TO 863, SEC 6. 2 L 7 2 4F RT A21EA 2007012600250 20070126 00250 EA 2007 1 26 TRAX200700080 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 863-985 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND RT SIDEWALL SEAT TRACK CORRODED, FS 863 TO 985, SEC 7. 2 L 7 2 4F RT A21EA 2007012600253 20070126 00253 EA 2007 1 26 TRAX200700082 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 495-581 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND RT FLOOR SEAT TRACK CORRODED, FS 495 TO 581, SEC 2. 2 L 7 2 4F RT A21EA 2007012600266 20070126 00266 NM 2007 1 26 HALA0700034 1 20070123 A 4900 APU BOEING 767 767300 1385204 NM UNKNOWN A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 592HA 33468 BTB - ETOPS SIGNIFICANT SYSTEM, APU SHUT DOWN ON PUSH BACK. PERFORMED FIM 49-11-00 AND REVERSE FLOW FAULT ERASE BOX. P ERFORMED BIT TEST. NO FAULTS NOTED. START APU OK. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007012600267 20070126 00267 NM 2007 1 26 KCSA071033 1 20070118 A 5320 WEB BOEING 747 747209F 1384800 NM BS 878 DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 FOUND FORWARD CARGO COMP FLOOR TORQUE BOX TOP WEB DENTED AT BS 878, RBL 60. 2 L 7 4 4F RT A20WE 2007012600268 20070126 00268 EU 2007 1 26 200701185 1 20070115 A 2780 1702288A SENSOR EMB ERJ170 ERJ170100SE 3260406 EU SLATS DEFECTIVE A UHLA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 17 637RW 17000051 FLIGHT 7726 DEN TO MCI, ON APPROACH, IMMEDIATELY AFTER ENTERING THE ICING CONDITIONS THE CREW RECEIVED THE SLAT FAIL MES SAGE. CREW RAN THE APPROPRIATE CHECKLIST ITEMS PER THE QRH. DIVERTED TO ICT AND LANDED WITHOUT INCIDENT. ON CALL MAIN T; SYSTEM FOUND TO BE TRANSITORY OF SLAT CONTROL SYSTEM. FERRY TO ORD. ORD MAINT REMOVED AND REPLACED RIGHT OUTBOARD S LAT SKEW SENSOR. 2 L 7 2 4F RT A56NM 2007012600269 20070126 00269 EU 2007 1 26 200701181 1 20070114 A 2497 1701337C ELECTRICAL SYS EMB ERJ170 ERJ170100SE 3260406 EU BURNED A UHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 17 650RW 17000071 FLIGHT 7540 IAD TO BDL, CREW REPORTS WHILE DEPLANING PAX SMOKE FILLED THE CABIN FROM UNDER THE FLOOR MID-CABIN. CAPT HA D GPU REMOVED AND BLEW BOTH ENGINE FIRE BOTTLES. THERE WAS NO INDICATION OF ENGINE FIRE, NO FIRE WAS FOUND. OCM FOUND THE EPM IN THE LICC BURNED. 2 L 7 2 4F RT A56NM 2007012600270 20070126 00270 EU 2007 1 26 200701182 1 20070114 A 2780 UNKNOWN EMB ERJ170 ERJ170100SE 3260406 EU SLATS UNKNOWN A UHLA O OTHER J WARNING INDICATION AP APPROACH 1 GL 17 644RW 17000061 FLIGHT 7635 YUL TO ORD, ON APPROACH SELECTING FLAPS 1, CREW RECEIVED A SLAT FAIL MSG ALONG WITH A SHAKER ANTICIPATED, AN D AOA LIMIT FAIL ALONG WITH SEVERAL OTHER ASSOCIATED MESSAGES. CREW FOLLOWED THE QRH PROCEDURES, DETERMINED THEY NEEDED TO MAKE A FLAPS UP LANDING AND DECLARED AN EMERGENCY. MAINT CLEARED FAULTS ON SF ACE 1 AND SLAT ACE 2. PERFORMED BIT O N SF ACE 1 AND SLAT ACE 2 BOTH TEST PASSED, SLAT FAIL MESSAGE CLEARED. SLAT/FLAP OPS CHECK GOOD. 2 L 7 2 4F RT A56NM 2007012600271 20070126 00271 EU 2007 1 26 200701183 1 20070114 A 2780 UNKNOWN EMB ERJ170 ERJ170100SE 3260406 EU SLATS UNKNOWN A UHLA O OTHER J WARNING INDICATION LD LANDING 1 GL 17 640RW 17000058 FLIGHT 7731 YYZ TO DEN, CREW REPORTS A SLAT/FLAP FAIL ON LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. MAINT CLEARED SF A CE 1 AND 2 INHIBITS. FLAPS OPS NORMAL. 2 L 7 2 4F RT A56NM 2007012600272 20070126 00272 EU 2007 1 26 200701184 1 20070114 A 2781 5913306 SENSOR EMB ERJ170 ERJ170100SE 3260406 EU TE FLAPS DEFECTIVE A UHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 17 874RW 17000148 FLIGHT 6455 ATL TO MLI, ON DEPARTURE SELECTING FLAPS UP, CREW RECEIVED AN EICAS MESSAGE "SLAT FAIL." CREW CONFIRMED VIS UALLY THAT THE SLATS WERE NOT IN THE RETRACTED POSITION, RAN THE QRH CHECKLIST AND RETURNED TO ATL. REMOVED AND REPLACE D NR 2 AND NR 3 SLAT SKEW SENSOR RT WING. RIGGED ELECTRICALLY AND OPS CK GOOD. 2 L 7 2 4F RT A56NM 2007012600275 20070126 00275 NM 2007 1 26 KCSA071011 1 20070115 A 5313 STRINGER BOEING 747 747209F 1384800 NM PWA JT9 JT9D7R4G2 52054 NE FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 STRINGER 39L HAS .25 INCH CRACK BETWEEN STA580 AND 600. 2 L 7 4 4F 4 F RT A20WE E3NE 2007012600278 20070126 00278 SO 2007 1 26 C2XA07IA015 1 20070117 A 3350 110049 CHARGER EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17513 145292 IAH - DURING MAINTENANCE INSPECTION, THE AISLE PATH LIGHTING BEHIND THE EMERGENCY EXITS WERE FOUND TO BE INOPERATIVE. M AINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS , AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007012600279 20070126 00279 NM 2007 1 26 KCSA071013 1 20070115 A 5330 SKIN BOEING 747 747209F 1384800 NM PWA JT9 JT9D7R4G2 52054 NE FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 STA 580 BETWEEN STR 41R AND 42R SKIN DENTED 1.5 INCHES. 2 L 7 4 4F 4 F RT A20WE E3NE 2007012600280 20070126 00280 NM 2007 1 26 KCSA071014 1 20070115 A 5347 SEAT TRACK BOEING 747 747209F 1384800 NM PWA JT9 JT9D7R4G2 52054 NE FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 SEAT TRACK CORRODED AT STA 600 BL-0 WL312. 2 L 7 4 4F 4 F RT A20WE E3NE 2007012600281 20070126 00281 NM 2007 1 26 KCSA071015 1 20070115 A 5311 FRAME BOEING 747 747209F 1384800 NM PWA JT9 JT9D7R4G2 52054 NE FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 FRAME WEB CRACKED 1 INCH STA1680 STR40R WL118. 2 L 7 4 4F 4 F RT A20WE E3NE 2007012600282 20070126 00282 NM 2007 1 26 KCSA071022 1 20070116 A 5313 STRINGER BOEING 747 747209F 1384800 NM PWA JT9 JT9D7R4G2 52054 NE FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 FUSELAGE STRINGER 38R HAS A .25 CRACK BETWEEN STA. 500 AND 520. 2 L 7 4 4F 4 F RT A20WE E3NE 2007012600283 20070126 00283 NM 2007 1 26 KCSA071016 1 20070115 A 5311 FRAME BOEING 747 747209F 1384800 NM PWA JT9 JT9D7R4G2 52054 NE FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 FRAME WEB DENTED APROX .75 INCH STA 1760 4 INCH, WL114, RBL53. 2 L 7 4 4F 4 F RT A20WE E3NE 2007012600284 20070126 00284 NM 2007 1 26 KCSA071018 1 20070116 A 5313 FITTING BOEING 747 747209F 1384800 NM PWA JT9 JT9D7R4G2 52054 NE FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 BS 2360 STR 42L END FITTINGS ARE CORRODED ON FORWARD AND AFT SIDES 2 L 7 4 4F 4 F RT A20WE E3NE 2007012600285 20070126 00285 CE 2007 1 26 GUUA01140702 1 20070114 A 2697 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT FIRE BOTTLE LOOSE A GUUA K NONE N FALSE WARNING CR CRUISE 1 SO 29 69547 UE189 FLIGHT: 9147, DURING FLIGHT RT ENGINE FIRE DISCHARGE LIGHT ILLUMINATED. CONTINUED, LANDED WITHOUT INCIDENT. RESECURED L OOSE WIRE AT RT FIRE BOTTLE. 2 L 7 2 4T 4 T RT A24CE E26NE 2007012600286 20070126 00286 CE 2007 1 26 GUUA01150701 1 20070115 A 2697 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT FIRE BOTTLE LOOSE A GUUA K NONE N FALSE WARNING CR CRUISE 1 SO 29 69547 UE189 FLIGHT: 9175, DURING FLIGHT RT ENGINE FIRE DISCHARGE LIGHT ILLUMINATED. CONTINUED, LANDED WITHOUT INCIDENT. SECURED LOO SE WIRE AT RT ENGINE FIRE BOTTLE. 2 L 7 2 4T 4 T RT A24CE E26NE 2007012600287 20070126 00287 CE 2007 1 26 GUUA01160701 1 20070116 A 2697 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT FIRE BOTTLE LOOSE A GUUA K NONE N FALSE WARNING CR CRUISE 1 SO 29 69547 UE189 FLIGHT: 9176, DURING FLIGHT RT ENGINE FIRE DISCHARGE LIGHT ILLUMINATED. CONTINUED, LANDED WITHOUT INCIDENT. SECURED LOO SE WIRE CONNECTION AT THE RT FIRE BOTTLE. 2 L 7 2 4T 4 T RT A24CE E26NE 2007012600292 20070126 00292 CE 2007 1 26 DXTA200701833 1 20070102 A 2913 66166 PUMP CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LT ENGINE FAILED E DXTA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 934QS 2329 2329 7500034 LOST (A) HYD FLUID IN FLIGHT. REPLACED HYDRAULIC PUMP IAW MM 29-10-02. EXERCISED SYSTEM AND COMPLIED WITH FILTER INSPEC TION. FILTERS CHECK GOOD. NO DEBRIS PRESENT. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007012600293 20070126 00293 NE 2007 1 26 DXTA200701830 2 20070101 A 7200 ENGINE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE RIGHT SHUTDOWN E DXTA K NONE X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 GL 07 358QS 5600455 PCEJC0352 DURING THE CONTROL AND SPEED BRAKE CHECK, THE RT ENGINE SHUTDOWN AFTER BRINGING THE THROTTLE TO IDLE. RAN BOTH ENGINES AND ACCOMPLISHED RAPID DECELERATION CHECKS ON BOTH (10 TIMES) EACH. NO DISCREPANCIES NOTED. TAXIED TO RUN-UP AREA AND EXTENDED SPEED BRAKES. RAN ENGINES ABOVE 85 PERCENT N1 AND SPEED BRAKES STOWED. RAPIDLY DECELERATED BOTH ENGINES, NO FAULTS. CHECKED IDLE INDEX ON FUEL CONTROL UNIT. CHECKED GOOD. DONE IN REF TO MM. 2 L 7 2 4F 4 F RT A22CE E25EA 2007012600295 20070126 00295 NM 2007 1 26 ASMF200701001 1 20070104 A 3810 H151615 LINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE WATER SYS LEAKING W ASMF D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SW 23 161PL 49764 DURING PUSH BACK, A WATER LEAK WAS DETECTED ON ELECTRICAL/ELECTRONIC COMPARTMENT AT COMPUTERS AREA. AIRCRAFT WAS SENT T O HANGAR AND DURING MAINTENANCE CHECK, A WATER LINE WAS DETECTED LEAKING ON FORWARD CARGO COMPARTMENT. THE LINE P/N H151 -615 WAS REPLACED IAW IPC 38-10-00 FIGURE 2D AND THE LINE P/N S00267AE8E0810 WAS REPAIRED AND REINSTALLED IAW IPC 38-10- 00, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007012600316 20070126 00316 SO 2007 1 26 C2XA07IA016 1 20070118 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO CABIN/COCKPIT ODOR A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 14168 14500840 IAH - FLIGHT 2358, THE CREW REPORTED A STRONG ELECTRICAL ODOR IN THE COCKPIT AND CABIN. THE AIRCRAFT RETURNED TO IAH WH ERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE ENGINES WITH NO DEFECTS N OTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007012600319 20070126 00319 EA 2007 1 26 A6WA200740026 1 20070115 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 31 460AW 7867 FLAPS FAIL CAUTION MESSAGE, ZERO DEGREE FLAP LANDING. TOUCHDOWN SPEED 173, MAX BRAKE TEMP WAS 4, 45,000 LBS LANDING WEI GHT. DID NOT LAND OVERWEIGHT OR MAKE OR HARD LANDING. INSPECTED FLAPS, NO EVIDENCE OF TWISTING OR SKEWING IAW AWAC SUP PLEMENT 98-018A. RESET FLAP C/B`S ONCE, MESSAGE CLEARED. FLAPS OPERATE NORMALLY. PLACED ON 72-HOUR WATCH. (M) REMOVE D AND REPLACED RT BPSU. (K) 2 L 7 2 4F RT A21EA 2007012600337 20070126 00337 EU 2007 1 26 MALA070012 1 20070120 A 2611 7211121100 SMOKE DETECTOR SAAB SF340 340B 7860101 EU AVIONICS BAY MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 443XJ 340B443 JUST AFTER DEPARTURE THE CREW REPORTED THAT THE CWP AVIONICS SMOKE WARNING ACTIVATED INTERMITTENTLY. THERE WAS NO OBSER VATION OF SMOKE OR SMELL OF FUMES. FA REPORTED A BURNING SMELL. THE FLIGHT RETURNED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. REMOVED AND REPLACED AVIONICS SMOKE DETECTOR IAW AMM 26-13-05 NO BURNING SMELL NO TED. ALL CHECKS GOOD, P/N ON OFF 72-111211-00 S/N ON A5305 S/N OFF B5488. 2 L 7 2 4T RT A52EU 2007012600358 20070126 00358 NM 2007 1 26 QXEA200700029 1 20070113 A 2913 570347 PUMP DHAV DHC8 DHC8202 2809007 NM HYDRAULIC SYS MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 358PH 10966 506 SEA FLIGHT NR 2182, NR 2 ENGINE HYDRAULIC PUMP CAUTION LIGHT STAYS ILLUMINATED AFTER NR 2 ENGINE OUT OF START-FEATHER. NR 2 HYDRAULIC PRESSURE 0. MAINTENANCE REPLACED NR 2 ENGINE DRIVE HYDRAULIC PUMP. OPERATIONAL CHECK GOOD. NO LEAKS NO TED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007012500376 20070125 00376 NM 2007 1 25 SWAA070330 1 20070123 A 5754 65C26601 SKIN BOEING 737 7373H4 1384600 NM L/E SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND LT WING NR 3 L/E SLAT UPPER SURFACE DELAMINATED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007012600002 20070126 00002 2007 1 26 AMTA200700023 4 20070121 A 2200 UNKNOWN BOEING 757 75723N 1384973 NM UNKNOWN A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 522AT 29330 MACH/SPD TRIM EICAS DISPLAYED. PERFORMED RESET PROCEDURE PER FIMM 27-09-00. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A2NM 2007012600003 20070126 00003 2007 1 26 AMTA200700024 4 20070120 A 3442 ANTENNA BOEING 737 73783N 13844HI NM WX RADAR SYS INOPERATIVE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 317TZ 28246 WX RADAR INOPERATIVE. REMOVED AND REPLACED WX RADAR ANTENNA IAW MM 34-43-11-4, OPS CHECK GOOD. OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2007012600020 20070126 00020 NM 2007 1 26 AALA20070083 1 20070114 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 950AN 30087 MIA - EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A16WE 2007012600025 20070126 00025 NM 2007 1 26 AALA20070069 1 20070112 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 939AN 30883 MIA - EMERGENCY LIGHT AT SEAT 14A EXIT SIDEWALL INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 14A EXIT SIDEWALL. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007012600042 20070126 00042 EA 2007 1 26 TRAX200700113 1 20070120 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 EMERGENCY FLOOR PATH MARKING STRIPS IN CENTER AISLE ARE BROKEN IN SEVERAL PLACES. OK TO INSTALL EMERGENCY FLOOR PATH MA RKING STRIP. (RA313) REPLACED AND INSTALLED NEW SERVICEABLE EMERGENCY FLOOR PATH MARKING STRIPS COVERS IAW AMM 33-50-00. FOUND MERGENCY STRIPS SERVICEABLE. REPLACED CRACKED STRIPS COVERS P/N 505-802. 2 L 7 2 4F RT A21EA 2007012600043 20070126 00043 NM 2007 1 26 QXEA200700046 1 20070123 A 2997 WIRE DHAV DHC8 DHC8202 2809007 NM HYD INDICATOR DAMAGED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 368PH 512 PDX FLIGHT NR 2284, NR 2 STANDBY HYDRAULIC PRESSURE INOP, STANDBY HYDRAULIC PRESSURE INDICATOR INOP. MAINTENANCE REPAIR ED WIRE SHIELDING AT NR 2 STANDBY PUMP PRESSURE TRANSDUCER. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETUR NED TO SERVICE. 2 H 7 2 4T RT A13NM 2007012600046 20070126 00046 WP 2007 1 26 AMTA200700030 1 20070124 A 5753 ATTACH FITTING LKHEED 1011 10113853 5265020 WP TE FLAP GOUGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 164AT 1238 RIGHT NR 1 FLAP OUTBOARD ATTACH FITTING HAS GOUGES. REPAIRED PER EER 12925 GAMCO WORKORDER 316063. (M) 2 L 7 3 4F A23WE 2007012600050 20070126 00050 NM 2007 1 26 KCSA071039 1 20070122 A 5320 WEB BOEING 747 747209F 1384800 NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 AFT PIT STA 1540 WL 119 VERT WEB DENTED LBL 8 TO RBL 8. 2 L 7 4 4F RT A20WE 2007012600073 20070126 00073 NM 2007 1 26 SWAA070357 1 20070124 A 5310 6546817 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 294.5 TO BS 328, RBL 61. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007012600077 20070126 00077 NM 2007 1 26 SWAA070340 1 20070124 A 3320 AL5273 LIGHT BOEING 737 7377H4 1384404 NM AFT GALLEY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 29 762SW 27876 CABIN REPORTED SMOKE, ELECTRICAL SMELL ON GROUND. SECURED CABIN CEILING LIGHTS SMOKE SMELL DISSIPATED. INSPECTED CABIN LIGHTS, RT AND LT PACKS, RAN GASPER AND RECIRC FANS, NO FAULTS NOTED. REMOVED AND REPLACED AFT GALLEY WORK LIGHT BULBS PER MM. 2 L 7 2 4F RT A16WE 2007012600089 20070126 00089 NM 2007 1 26 2007UALA00171 1 20070123 A 3350 LENS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 THE -EMERGENCY EXIT- LIGHT PANEL AT 15 ABC IS LOOSE FROM SIDEWALL. LIGHT IS SECURE. LENS IS LOOSE ON ONE END, SECURE O N OTHER END. MADE INTERIM REPAIR OF EXIT SIGN OVERWING LENS WITH TAPE. VERIFIED LENSE SECURE EVEN WITHOUT TAPE. REPAI R IS TO KEEP LENS FROM BEING SNAGGED ACCIDENTLY BY PASSENGER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007012600100 20070126 00100 WP 2007 1 26 AMTA200700033 1 20070124 A 5510 PIVOT LKHEED 1011 10113853 5265020 WP RT STAB GOUGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 164AT 1238 RIGHT STABILIZER OUTBOARD PIVOT PITTING WITH DEEP GOUGE AT LOWER END. REPAIRED IAW EER12968 WORKORDER 316063. (M) 2 L 7 3 4F A23WE 2007012600106 20070126 00106 EU 2007 1 26 0700223256 1 20070123 A 3350 BATTERY AIRBUS 320 A320212 3930322 EU EMERGENCY LIGHTS NO TEST A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 356NW 818 EMERGENCY LIGHT TEST FAILED "EPSU BATTERY EMERG R" MESSAGE. CORRECTED BY REPLACING BATTERY ON RIGHT EPSU (12WL), CHECKS OK. 2 L 7 2 4F RT A28NM 2007012600108 20070126 00108 NM 2007 1 26 USAA070062 1 20070124 A 5310 DOOR FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 442US 24841 FWD CARGO/AFT DOOR FRAME AT 1A STOP FOOTPRINT HAS CRACK. REMOVED DAMAGE & INSTALLED REPAIR DOUBLER & TRIPLER PER EA 984 13, DEFECT SIZE: .100 INCH. 2 L 7 2 4F RT A16WE 2007012600109 20070126 00109 NM 2007 1 26 0700266732 1 20070104 A 5313 LONGERON BOEING 747 747251B 1384892 NM BS 2742 MISALIGNED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 632US 23112 DURING "L" CHECK, WHILE PERFORMING REPLACEMENT OF DAMAGED TAILCONE FOUND MISALIGNED FASTENER HOLES IN LT AND RT LOWER LO NGERON AFT OF BS 2742. REPAIRED PER EA 67-208748. 2 L 7 4 4F A20WE 2007012600110 20070126 00110 NM 2007 1 26 0700246732 1 20070104 A 5311 FRAME BOEING 747 747251B 1384892 NM BS 2725 DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 632US 23112 DURING "L" CHECK WHILE PERFORMING REPLACEMENT OF DAMAGED TAILCONE FOUND MISALIGNED FASTENER HOLES IN FRAME AT BS 2725. REPAIRED PER EA 67-208742. 2 L 7 4 4F A20WE 2007012600120 20070126 00120 NM 2007 1 26 USAA070060 1 20070124 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 442US 24841 BS 379 BL 0 HAS CRACK. REMOVED DAMAGE, INSTALLED REPAIR PARTS, INSTALLED DOUBLER PER EA 98415, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007012600153 20070126 00153 EU 2007 1 26 UPS07148868 1 20070113 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU EMERGENCY EXIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 134UP 0817 EMERGENCY EXIT LIGHT DISARMED LIGHT IS NOT ON WITH THE SWITCH IN THE DISARMED POSITION. THE EMERGENCY EXIT LIGHTS ARE O N IN THE COCKPIT. CYCLED SWITCH ON, THEN TO DISARM. EMERGENCY EXIT LIGHTS SHUTOFF. EMERGENCY EXIT LIGHT SWITCH OPERAT ES AS REQUIRED. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2007012600188 20070126 00188 EU 2007 1 26 MALA070008 1 20070116 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 619-686 DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 340B433 FOUND SEAT TRACK AT LBL 18.3, BETWEEN FS 619 AND FS 686 IS DAMAGED. REMOVED AND REPLACED IAW MESABA EO#S53060. REF: EAM S WORK ORDER 215326 TASK 1503. 2 L 7 2 4T RT A52EU 2007012600198 20070126 00198 SO 2007 1 26 SWIA200717658 1 20070115 A 5330 SKIN EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 297SW 120327 FUSELAGE SKIN CLEAT CRACKED ABOVE AND FORWARD OF CARGO DOOR CUT OUT DISCOVERED DURING C-CHECK INSPECTION. NEW SKIN CLEA T INSTALLED IAW SRM 120 51-40-02, ALSO IAW RII CARD 53-800-1000. 2 L 7 2 4T RT A31SO 2007012600211 20070126 00211 EA 2007 1 26 COMA0760029 1 20070116 A 3010 6229820009 DCU CNDAIR CL600 CL6002B19 1900309 EA AVIONICS BAY FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 934CA 9673 7042 FLIGHT 5567 - RIGHT ANTI-ICE DUCT WARNING MESSAGE IN FLIGHT. AIRCRAFT DIVERTED TO BTR AND LANDED SAFELY. REMOVED AND R EPLACED DCU 1. 2 L 7 2 4F RT A21EA 2007012600230 20070126 00230 NM 2007 1 26 UPS07448948 1 20070109 A 5320 65B0171836 TIE CLIP BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO BS 500 S33R CLIP FOUND CRACKED AS MARKED. FWD CARGO COMPT BS 500 STR 33R TIE CLIP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007012600231 20070126 00231 NM 2007 1 26 UPS07448950 1 20070109 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO RT BS 760-780 STRINGER S35R FOUND CRACKED AS MARKED. FWD CARGO COMPT BS 742 TO BS 830 STR 3 5R REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007012600232 20070126 00232 NM 2007 1 26 UPS07448951 1 20070110 A 5313 65B074916 STRINGER BOEING 747 747123 1384873 NM FUSELAGE DEFORMED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C BULK CARGO COMPT STRINGER WEB FOUND DEFORM AT STA 2020-2040 S39L. BULK CARGO COMPT STRINGER WEB REPLA CED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02 JUST AT STA 2020-2040 S39L AREA. 2 L 7 4 4F A20WE 2007012600246 20070126 00246 EA 2007 1 26 TRAX200700078 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 712-761 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND RT SIDEWALL SEAT TRACK CORRODED, FS 712 TO 761, SEC 5. 2 L 7 2 4F RT A21EA 2007012600277 20070126 00277 NM 2007 1 26 QXEA200700035 1 20070114 A 2160 7276045 FILTER BOMBDR DHC8 DHC8402 1390042 NM SHUTOFF VALVE UNKNOWN A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 401QX 4031 LAX FLIGHT NR 2403 TO SUN: DIVERTED TO BOI. CREW WAS UNABLE TO GET DUCT TEMP OVER 25C. MAINTENANCE REPLACED PACK FLOW CONTROL SHUTOFF VALVE FILTER IAW Q400 MM 21-52-00. OPS CHECK GOOD IAW Q400 MM 21-61-00. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007012600296 20070126 00296 NM 2007 1 26 ASMF200701005 1 20070114 A 5350 FAIRING DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE MLG DAMAGED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 158PL 49761 AIRCRAFT WAS HIT IN THE RT LOWER WING BY A BAGGAGE CONVEYOR, CAUSING A DAMAGE OF 2 X 2 INCHES WITH .3125 INCH DEPTH IN T HE MLG FAIRING. DUE, IT WAS A NON PRESSURIZED AREA, HI-SPEED TAPE WAS INSTALLED IAW MGMYPTA 10-24-1 AND AIRCRAFT WAS DI SPATCHED. DURING OVERNIGHT CHECK, FAIRING NR 2216C WAS REPAIRED IAW SRM 51-70-1 FIGURE 6 PARAGRAPH 13, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007012600356 20070126 00356 2007 1 26 QXEA200700041 4 20070118 A 3418 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM STICK PUSHER UNKNOWN A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 424QX 4006 PDX FLIGHT NR 2359: STICK PUSHER MASTER CAUTION ILLUMINATED ON TAXI OUT. MAINTENANCE CYCLED POWER OF SPM 1 AND 2. POWE R UP SELF TEST NORMAL. CAUTION LIGHT OUT. SYSTEM TESTS NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007012600365 20070126 00365 EA 2007 1 26 SWIA200717734 1 20070104 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 969SW 7876 PAX DOOR STEP 832DT AND 832CR CRACKED AT AFT WEB, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS ON AFT W EB PER REO 601R-52-11-1172. 2 L 7 2 4F RT A21EA 2007012600366 20070126 00366 EA 2007 1 26 SWIA200717735 1 20070104 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 969SW 7868 PAX DOOR STEP 832 DT AND 832 CT CRACKED AT FORWARD WEB, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS PE R REO 601R-52-11-702 REV A. 2 L 7 2 4F RT A21EA 2007012600373 20070126 00373 EA 2007 1 26 SWIA200717741 1 20070104 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 969SW 7876 FS 625 LT INTERCOSTAL AT STR 12 IS CRACKED AT RADIUS P/N 601-35012-51, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED INTERCOSTAL AT FS 625 S-12L PER CRJ200 SRM 51-42-41. 2 L 7 2 4F RT A21EA 2007012900003 20070129 00003 SO 2007 1 29 LR7A07004 1 20070117 A 5340 342603 ATTACH ANGLE LKHEED 382 382G 526414U SO FS 597 WL 230 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 652 4698 DURING SCHEDULED B 2 CHECK PER JOB CARD HB5302, FOUND INTERCOSTAL ATTACH ANGLE TO CENTER WING REAR WEB CRACKED AT FS 59 7, WL230, LBL16. REPLACED ANGLE IAW SMP583 51-70, AND DWG 342603. 2 H 7 4 4T A1SO 2007012900010 20070129 00010 SO 2007 1 29 LR7A07009 1 20070117 A 5413 LONGERON LKHEED 382 382G 526414U SO FS 485 WL 256 DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 652 4698 DURING SCHEDULED B2 CHECK PER JOB CARD HSP71189, FOUND NR 1 QEC OB UPPER LONGERON OB FWD HOLE FOR FASTENER OF SUPORT BEA M WITH OVERSIZED HOLE AT FS485, WL256. REPAIRED LONGERON IAW MEA 382-54-07-004.. 2 H 7 4 4T A1SO 2007012900012 20070129 00012 NM 2007 1 29 AWXA200700113 1 20070123 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS NO TEST A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 830AW 19988 19988 1565 PHX - EEL - EMERGENCY LIGHTS FAIL TO TEST. MX REPLACED ESPU AFT LT AND BATTERY IAW MM 33-51-38. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007012900013 20070129 00013 NM 2007 1 29 AWXA200700117 1 20070123 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 802AW 22617 8425 924 LAX - EEL - EMERG EXIT LIGHTING REMAINS ON WITH SWITCH IN ARMED POSITION. MX REMOVED AND REPLACED AFT CABIN POWER SUPPL Y PER AMM 33-51-38PB401, OPS CHECK WAS OK. 2 L 7 2 4F RT A28NM 2007012900019 20070129 00019 NM 2007 1 29 UPS07448932 1 20070109 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 2320 STR 20-21R FRAME FOUND CRACK. M/D BS 2320 STR 20-21R FRAME REPAIRED AS PER SRM 53-10-04 F IG 4. 2 L 7 4 4F A20WE 2007012900022 20070129 00022 EU 2007 1 29 DHL2007362506 1 20070107 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 47663 84 MAIN CABIN SEAT TRACK HAS WORN LUGS BETWEEN FRAMES 63 AN 64 RBL 75. BLENDED OUT WORN LUGS IAW A300 SRM 51-10-10 FOUND O UT OF LIMITS PER A300 SRM 53-10-00 FIG 612, MAT REMOVED .050" ORG MAT .145 MAT REMAINING .095, CUT OUT SECTION DAMAGE AT MAIN CABIN SEAT TRACK 6' RBL 75 FROM FR 63 TO FR 65.5 IAE A300 SRM 53-10-10 AND 51-41-00. TREATED PARTS WITH ALODINE A N WHITE PAINT IAW A300 SRM 51-40-12. INSTALLED SEAT TRACK SECTION AND PARTS REPAIR IAW A300 SRM 53-10-10 AN 51 30-30 P/ N 6022457,PO NR 031938. THIS IS A PERMANENT REPAIR. 2 L 7 2 4F RT A35EU 2007012900024 20070129 00024 NM 2007 1 29 07FDEA00059 1 20070109 A 5713 ARB754102 STRINGER DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 DURING HFEC INSPECTION, CRACK FOUND AT STRINGER END 14R (XORS 685) INSIDE RT WING TANK. REPAIR CARRIED OUT AT STRINGER END-41R (XORS 685) INSIDE RT WING TANK AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6- 2-100. 2 L 7 3 4F RT A22WE 2007012900025 20070129 00025 EA 2007 1 29 SWIA200717754 1 20070124 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 926SW 7687 RIGHT WING FORWARD EMERGENCY EXIT LIGHT INOP. RELAMPED RIGHT WING FORWARD EMERGENCY EXIT LIGHT BULB. OPERATIONAL CHECK S GOOD. 2 L 7 2 4F RT A21EA 2007012900026 20070129 00026 EA 2007 1 29 SWIA200717755 1 20070123 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER DE DESCENT 1 NM 07 918SW 7645 DESCENDING THRU 9,000 FT RIGHT WINDOW CRACKED. REPLACED RIGHT SIDE WINDOW IAW CRJ MM 53-12-01 AND RII 56-220-1000, PN O FF: NP139322-001 SN OFF: 02014H6515. 2 L 7 2 4F RT A21EA 2007012900027 20070129 00027 EA 2007 1 29 SWIA200717756 1 20070123 A 5610 601R3303313 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 453SW 7743 CAPTAIN'S WINDSHIELD SHATTERED. REPLACED LEFT WINDSHIELD IAW AMM 56-11-01 AND COMPLIED WITH RII 56-220-1000. 2 L 7 2 4F RT A21EA 2007012900029 20070129 00029 NM 2007 1 29 UPS07448934 1 20070111 A 5313 WEB BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 820-840 STR 10L STRINGER ATT WEB FWD CORNER AREA FOUND CRACK. M/D BS 820-840 STR 10L STRINGER ATT WEB FWD CORNER AREA REPAIRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2007012900031 20070129 00031 EA 2007 1 29 SWIA200717759 1 20070121 A 3213 O-RING CNDAIR CL600 CL6002B19 1900309 EA NLG STRUT DAMAGED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 454SW 7749 NOSE WHEEL WOULD NOT RETRACT, NOSE DOOR OPEN WARNING. RETURNED TO FIELD. REPLACED O-RINGS AND PACKINGS ON NLG FLOATING STRUT PISTON IAW CMM 32-20-04 AND IAW CRJ 200 MM 32-21-25 AND C/W ST12-710-1002. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007012900032 20070129 00032 EA 2007 1 29 SWIA200717760 1 20070118 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 941SW 7750 LEFT WING FORWARD EMERGENCY EXIT LIGHT INOP. RELAMPED LEFT WING FORWARD EMERGENCY EXIT LIGHT BULB. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007012900033 20070129 00033 NM 2007 1 29 UPS07448935 1 20070111 A 5313 WEB BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 820-840 STR 10R STRINGER ATT WEB FWD CORNER AREA FOUND CRACK. M/D BS 820-840 STR 10R STRINGER ATT WEB FWD CORNER AREA REPAIRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2007012900035 20070129 00035 NM 2007 1 29 UPS07448943 1 20070109 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO BS 820-840 S35R FOUND CRACKED AS MARKED. FWD CARGO COMPT BS 742 TO BS 830 STR 35R REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007012900036 20070129 00036 NM 2007 1 29 07FDEA00063 1 20070109 A 5713 ARB751402 STRINGER DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 DURING HFEC INSPECTION, CRACK FOUND AT STRINGER END-14R (XORS 521) INSIDE RT WING TANK. REPAIR CARRIED OUT AT STRINGER END-14R (XORS 521) INSIDE RT WING TANK AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6- 2-100. 2 L 7 3 4F RT A22WE 2007012900040 20070129 00040 NM 2007 1 29 07FDEA00065 1 20070110 A 5311 AFA00203 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 CABIN RIGHT STA 1701 BETWEEN LONGERON 12 TO LONGERON 14 FRAME FOUND DENT. CABIN RIGHT STA 1701 BETWEEN LONGERON 12 TO LONGERON 14 FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION RE QUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTIONS AT 9,500 CYCLES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007012900041 20070129 00041 NM 2007 1 29 07FDEA00066 1 20070110 A 5311 AFA00283 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 CABIN LEFT STA 1681 BETWEEN LONGERON 12 AND LONGERON 14 FRAME FOUND DENT. CABIN LEFT STA 1681 BETWEEN LONGERON 12 AND LONGERON 14 FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION RE QUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTIONS AT 9,500 CYCLES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007012900042 20070129 00042 NM 2007 1 29 UPS07448946 1 20070109 A 5320 65B38600292 TIE CLIP BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO LT BS 540 STRINGER S31R TIE CLIP FOUND CRACKED AS MARKED. FWD CARGO RT BS 540 STRINGER S31R TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007012900043 20070129 00043 NM 2007 1 29 07FDEA00067 1 20070110 A 5311 AFA00263 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 CABIN, LEFT STA 1641 BETWEEN LONGERON 12 AND LONGERON 14 FRAME FOUND DENT. CABIN, LEFT STA 1641 BETWEEN LONGERON 12 A ND LONGERON 14 FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTIONS AT 9,500 CYCLES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007012900044 20070129 00044 NM 2007 1 29 UPS07448947 1 20070109 A 5320 65B0171888 TIE CLIP BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO BS 500 S32R I/B CLIP FOUND CRACKED AS MARKED. FWD CARGO BS 500 S32R I/B CLIP REPLACED AS PE R SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007012900046 20070129 00046 2007 1 29 SWAA070359 4 20070125 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007012900047 20070129 00047 NM 2007 1 29 SWAA070360 1 20070125 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 360, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007012900048 20070129 00048 NM 2007 1 29 SWAA070361 1 20070125 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 360, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007012900049 20070129 00049 NM 2007 1 29 SWAA070362 1 20070125 A 5312 6545819 PRESSURE PANEL BOEING 737 7373H4 1384600 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SERVICE CHECK, FOUND LT NOSE WHEEL WELL PRESSURE WEB CRACKED AT BS 247, WL 168.6. REPAIRED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2007012900050 20070129 00050 NM 2007 1 29 SWAA070363 1 20070125 A 5312 6545819 PRESSURE PANEL BOEING 737 7373H4 1384600 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SERVICE CHECK, FOUND RT NOSE WHEEL WELL PRESSURE WEB CRACKED AT BS 259, WL 174. REPAIRED WEB PER SWA E A. 2 L 7 2 4F RT A16WE 2007012900052 20070129 00052 NM 2007 1 29 SWAA070365 1 20070125 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007012900054 20070129 00054 NM 2007 1 29 SWAA070367 1 20070125 A 2750 65522112 TORQUE TUBE BOEING 737 7373H4 1384600 NM T/E FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE T UBE PER MM. 2 L 7 2 4F RT A16WE 2007012900055 20070129 00055 NM 2007 1 29 SWAA070368 1 20070125 A 2750 65522111 TORQUE TUBE BOEING 737 7373H4 1384600 NM T/E FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TU BE PER MM. 2 L 7 2 4F RT A16WE 2007012900056 20070129 00056 NM 2007 1 29 SWAA070369 1 20070125 A 2750 6935349 TORQUE TUBE BOEING 737 7373H4 1384600 NM T/E FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD FORE FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007012900060 20070129 00060 NM 2007 1 29 SWAA070373 1 20070125 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED C1 CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT OUTBOARD T/E. REPAIRED NR 6 L/E SLAT PER SWA EA. 2 L 7 2 4F RT A16WE 2007012900061 20070129 00061 NM 2007 1 29 SWAA070374 1 20070125 A 5753 6546435333 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT T/E OUTBOARD END. REMOVED AND REPLACED AF T FLAP PER MM. 2 L 7 2 4F RT A16WE 2007012900062 20070129 00062 NM 2007 1 29 SWAA070375 1 20070125 A 5755 654645262A ATTACH FITTING BOEING 737 7373H4 1384600 NM NR 4 SPOILER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED C1 CHECK, FOUND LT WING NR 4 GROUND SPOILER OUTBOARD ACTUATOR ATTACH POINT BROKEN ON SPOILER SIDE. REM OVED AND REPLACED NR 4 SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007012900063 20070129 00063 NM 2007 1 29 SWAA070376 1 20070125 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 540, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007012900064 20070129 00064 NM 2007 1 29 SWAA070377 1 20070125 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 550, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007012900066 20070129 00066 NM 2007 1 29 SWAA070379 1 20070125 A 2560 65659725 MOUNT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FWD FLOOR MOUNT LOOSE. SECURED FLOOR MOUNT PER MM. 2 L 7 2 4F RT A16WE 2007012900070 20070129 00070 NM 2007 1 29 SWAA070383 1 20070125 A 5322 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007012900071 20070129 00071 NM 2007 1 29 SWAA070384 1 20070125 A 5313 6551698 STRINGER SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 359, STR 7L. REMOVED AND REPLACED STRINGER SPLICE PER S RM. 2 L 7 2 4F RT A16WE 2007012900074 20070129 00074 NM 2007 1 29 SWAA070387 1 20070125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012900075 20070129 00075 NM 2007 1 29 07FDEA00068 1 20070110 A 5311 AFA00273 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 CABIN LEFT STA 1661 BETWEEN LONGERON 12 AND LONGERON 14 FRAME FOUND CRACKED. CABIN LEFT STA 1661 BETWEEN LONGERON 12 AN D LONGERON 14 FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION R EQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTIONS AT 9,500 CYCLES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007012900077 20070129 00077 NM 2007 1 29 07FDEA00126 1 20070116 A 5347 AEA732523 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 M/D CARGO SEAT TRACK (STA 1520, LT, X=8.5) FOUND FLANGE UNDER FLOOR CORRODED. REPAIR CARRIED OUT AT M/D CARGO SEAT TRAC K (STA 1520, LT, X=8.5) AS PER SRM 53-70-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007012900078 20070129 00078 EU 2007 1 29 07FDEA00152 1 20070123 A 5730 PANEL AIRBUS 310 A310203 3930313 EU ZONE 500 MAINT ERROR A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 433FE 335 WHILE DRILLING HEAD FROM STRIPPED SCREW A HOLE WAS ELONGATED IN WING PLANK COMMON TO PANEL 550 JB COMPLIED WITH EA6-5700 -106331 PT1 BY PERFORMING REPAIR IAW AIB TD /J1/S1/04141/2007 ISSUE A. 2 L 7 2 4F RT A35EU 2007012900079 20070129 00079 NM 2007 1 29 07FDEA00153 1 20070123 A 3080 32902781 VALVE DOUG MD11 MD11 3023602 NM ZONE 600 FAILED A FDEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 582FE 48420 ON DEPARTURE WHEN WING ANTI-ICE SELECTED ON GOT WING ANTI-ICE DISAGREE AND MOMENTARILY MANIFOLD FAIL. PERFORMED QRH PRO CEDURE, REMAINED CLEAR OF ICING CONDITION. WING DISAGREE INDICATION REMAINED. TROUBLE SHOT CARRIED OUT PRECAUTIONARY M EASURE DELTA P SENSOR REMOVED AND REPLACED PER MD11 MM CHP30-11-02-4 AND RT WING ANTI-ICE SHUTOFF VALVE REMOVED AND REPL ACED PER MD11 MM CHP30-11-01-4. ENGINE RUN CARRIED OUT PER MD11 JRH CHP5A ALL INDICATIONS NORMAL AND ANTI-ICE TEST CARR IED OUT PER MD11 MM CHP 30-11-00-5. ALL TESTS PASSED. 2 L 7 3 4F RT A22WE 2007012900081 20070129 00081 NM 2007 1 29 07FDEA00154 1 20070123 A 5300 SILL BOEING 727 727233 138408A NM BS 620 MAINT ERROR A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 284FE 22621 MAIN CARGO DOOR CUTOUT AT BS 620 AND UPPER SILL HAS DOUBLE DRILLED HOLES AND DRILL STARTS ON LOWER SURFACES. REF DRAWIN G 53FX1286 FABRICATED 2EA. TENSION CLIPS ON WO 11701/2000/0013 AND INSTALLED REF. SRM 51-30-02 ALSO WORK ACCOMPLISHED O N WO 35039/N01449 2 L 7 3 4F RT A3WE 2007012900083 20070129 00083 NM 2007 1 29 SWAA070389 1 20070125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012900084 20070129 00084 EU 2007 1 29 07FDEA00156 1 20070124 A 5320 FLOOR SUPPORT AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 717FD 361 AFT PIT FLOOR SUPPORT STRUCTURE AT FR66 RBL 36R IS CORRODED. REMOVED AND REPLACED DAMAGED FLOORBEAM AT FR66 IAW FEDEX G MM 7-0-1001 AND FEDEX A300-6-SRM'S 51-40-21 PG 7 AND 51-40-21 PG24 AND AIRBUS DRAWING AS397432222. 2 L 7 2 4F RT A35EU 2007012900085 20070129 00085 NM 2007 1 29 SWAA070390 1 20070125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012900087 20070129 00087 WP 2007 1 29 07FDEA00158 1 20070124 A 5730 ACCESS PANEL DOUG MD10 MD1010F 3022112 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 368FE 46606 LEFT WING FUEL ACCESS PANEL 535AT PITTED ON BOTTOM SIDE. FABRICATED NEW FUEL PANEL IAW DAC DRAWING ARB0872 REV AP. INS TALLED ON CARD, 28C1701-01. MECH 4678 QC 231. 2 L 7 3 4F RT A22WE 2007012900089 20070129 00089 NM 2007 1 29 SWAA070392 1 20070125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012900090 20070129 00090 WP 2007 1 29 07FDEA00159 1 20070124 A 5730 ACCESS PANEL DOUG MD10 MD1010F 3022112 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 368FE 46606 LEFT WING FUEL ACCESS PANEL 534 CT GOUGED ON BOTTOM SIDE. FABRICATED NEW FUEL PANEL IAW DAC DRAWING 0872 REV AP. INSTA LLED ON 28C1701-01, MECH 4678 QC 231. 2 L 7 3 4F RT A22WE 2007012900091 20070129 00091 NM 2007 1 29 SWAA070393 1 20070125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012900092 20070129 00092 NM 2007 1 29 SWAA070394 1 20070125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012900093 20070129 00093 EU 2007 1 29 07FDEA00161 1 20070125 A 7830 UNKNOWN AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER UNKNOWN A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 684FE 802 ON POWER UP, NO REV UNLK LIGHTS NOTED ECAM. ENG NR 1 R REV PRESSURIZED. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 04FEB07 "MEL 78-30-01-A: ENGINE. NR 1 THRUST REVERSER, INOP. THRUST REVERSER IS DEACTIVATED I N FORWARD THRUST POSITION." REACTIVATED NR 1 T/R AND PERFORMED OPS CK REF JRH USING APU AIR. ALL INDICATIONS NORMAL. R EMOVED AND REPLACED PRSOV PRECAUTIONARY REF A300 MM 78-31-05-4. PERFORMED ENG POWER RUN, DID NOT GET "REV PRESSURIZED" INDICATION. CHECKED OPERATION OF T/R USING APU AIR AGAIN WITH ALL INDICATIONS NORMAL. RETURNED VALVE MPN 320522-5 TO TSP. 2 L 7 2 4F RT A35EU 2007012900100 20070129 00100 NM 2007 1 29 SWAA070399 1 20070125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012900103 20070129 00103 NM 2007 1 29 07FDEA00165 1 20070125 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE MAINT ERROR A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 284FE 22621 MAIN DECK FLOORBEAM UPPER CHORD AND INTERCOSTAL ATTACHMENT HAS DOUBLE DRILLED/MISREPAIRED FASTENER HOLES AT BS 380, RB L 12, WL 208 REMOVED DAMAGE AND REPAIRED ON UPPER CHORD STA 380. REMOVED AND REPLACED INTERCOSTAL AT 380-400 REF SRM 53 -10-08 FIG 3 STEP 3 PG 18, SRM 51-30-02 PG 1-2. TREATED AND PRIMED REF SRM 51-10-02 PG 1-2. CLASSIFIED AS A MAJOR REPA IR. 2 L 7 3 4F RT A3WE 2007012900104 20070129 00104 NM 2007 1 29 SWAA070401 1 20070125 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012900105 20070129 00105 NM 2007 1 29 SWAA070402 1 20070125 A 5344 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012900107 20070129 00107 NM 2007 1 29 SWAA070404 1 20070125 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 776WN 30591 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER DISCOLORED AT ROW 18 DEF. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2007012900108 20070129 00108 NM 2007 1 29 07FDEA00166 1 20070125 A 5320 FLOOR SUPPORT BOEING 727 727233 138408A NM BS 400-420 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 MAIN DECK FLOOR SUPPORT INTERCOSTAL UPPER FLANGE IS CORRODED AT BS 400-420, RBL 12, WL 208 REMOVED AND REPLACED INTERCOS TAL STA 400-420, REF BOEING DRWG 64-64950. TREATED, PRIMED REPAIR REF SRM 51-10-02 PG 1-2. CLASSIFIED AS A MAJOR REPAI R. 2 L 7 3 4F RT A3WE 2007012900109 20070129 00109 NM 2007 1 29 SWAA070405 1 20070125 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 776WN 30591 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER DISCOLORED AT ROW 8 DEF. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2007012900110 20070129 00110 NM 2007 1 29 SWAA070406 1 20070125 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 776WN 30591 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER DISCOLORED AT ROW 7 ABC. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2007012900111 20070129 00111 NM 2007 1 29 SWAA070407 1 20070125 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 438WN 29833 DURING SCHEDULED MV3 CHECK, FOUND EEPLS COVER BROKEN AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007012900114 20070129 00114 NM 2007 1 29 07FDEA00168 1 20070125 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 400 MAINT ERROR A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 284FE 22621 MAIN DECK FLOORBEAM UPPER CHORD AND INTERCOSTAL ATTACHMENT HAS DOUBLE DRILLED/MISREPAIRED FASTENER HOLES AT BS 400, RB L 12, WL 208. REMOVED DAMAGE ON UPPER CHORD, REPAIRED AREA REF SRM 53-10-08 FIG 3, TABLE I. REMOVED AND REPLACED INTER COSTAL AT 400-420, REF BOEING DRWG 65-6495. TREATED, PRIMED REF SRM 51-10-02 PG 1-2. CLASSIFIED AS MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007012900115 20070129 00115 NM 2007 1 29 AT0700013 1 20070124 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 993AT 55137 DENT AT P$237L LONG 18L AND RUNS FROM L18 UP 5 INCHES ABOVE L18 MEASURES 5 X 5 X .035. REPAIR DENT AT P$237L LONG 18C I AW B717 SRM 53-00-01 FIG 201. 2 L 7 2 4F TR A6WE 2007012900116 20070129 00116 WP 2007 1 29 07FDEA00170 1 20070126 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 1521 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 MAIN CABIN DEEP WEAR ON SEAT TRACK AT STA 1521 X= -27 REF J/C 5300E290-1J. INSTALLED SEAT TRACK SECTION WITH SPLICE AT STA 1531 IAW SRM 53-70-00 FIG 1. FABRICATED PART IAW DETAIL PART TRAVELER N01369 AND SRM 53-70-00 VOL1 FIG 1. 2 L 7 3 4F A22WE 2007012900117 20070129 00117 WP 2007 1 29 07FDEA00171 1 20070126 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 1721-1741 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 MAIN CABIN DEEP WEAR ON SEAT TRACK BETWEEN STA 1721 AND 1741 X= -27. REF J/C 5300E290-1J. INSPECTION PERFORMED AND FOUN D SEAT TRACK NOMINAL THK NOT TO BE WITHIN LIMITS IAW SRM 53-70-00 PAGE 22. SEAT TRACK REPAIR IS PERFORMED SEAT TRACK IS CUT AT STA 1711 AND 1751 IAW SRM 53-70-00 FIG 1. TRIMMED NEW FABRICATED SECTION IAW DETAIL PARTS TRAVELER I026368 AND SRM 53-70-00 FIG 1. INSTALLED NEW SEAT TRACK SECTION AND 2 SPLICES IAW SRM 53-70-00 FIG 1. 2 L 7 3 4F A22WE 2007012900118 20070129 00118 WP 2007 1 29 07FDEA00172 1 20070126 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 967-979 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 LWR EXT FUSELAGE FOUND NR 3 DEEP DENTS 15" BY 4" MAX DEPTH .090" FROM STA 979 TO STA 967 FROM L39 RT TO 42 RT. REMOVED 2 EXISTING REPAIRS BTWN STA 999 TO STA 959 FROM L#38 TO #42 RT IAW SRM 51-33-01 VOL2 P34/47. TRIM OUT DENTS AREA WITHOU T CUT INNER DOUBLER. PERFORMED INSP IAW NDT SPM06, NO CRACK FOUND. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-20 -00 VOL 1 FIG 6 AND SRM 53-50-00 VOL1 FIG 26. IN ORDER TO PERFORM REPAIR, REMOVED AND INSTALLED SCUFF PLATE IAW SRM 51- 31-01 VOL2 PAGE 36/41. CLEANED SCUFF PLATE AREA AND TREAT REPAIR AREA IAW SRM 51-21-01 VOL 2 PAR 22. SEAL SCUFF PLATE IAW SRM 51-41-01 VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N00219 AND SRM 53-20-00 VOL1 FIG 6 AND SRM 53-50-00 2 L 7 3 4F A22WE 2007012900122 20070129 00122 NM 2007 1 29 07FDEA00180 1 20070126 A 5340 ATTACH ANGLE BOEING 727 727233 138408A NM FUSELAGE MAINT ERROR A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 284FE 22621 MAIN CARGO DOOR CUTOUT STRUCTURE UPPER SEAL ANGLE ATTACH CASTING HAS 2 MISDRILLED HOLES. FABRICATED NEW UPPER SEAL ANGL E REF AAR NON-ROUTINE 11701-2000-0011 FOR FABRICATION OF UPPER SEAL ANGLE. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007012900123 20070129 00123 WP 2007 1 29 07FDEA00183 1 20070126 A 5347 CARGO TRACK DOUG DC10 DC1010 3022110 WP BS 1801-1871 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 AFT CARGO COMPT AREA FOUND SEVERE CORROSION ON TRACK BETWEEN STA 1871 AND 1801 X=20 RT. REMOVED CORROSION IAW SRM 51-21 -01 VOL 2 PAR 34. REMOVED 0.059" AT BS 1821 RT MAX ALLOWABLE IS .025" IAW SRM 53-70-00 VOL1 FIG 5, SHT 1 AND 2 NOTE 3. REMOVED .040" AT BS 1830, REMAINING MAT IS .050", MINIMUM REQUIREMENT IS .060" IAW SRM 53-70-00 VOL1 FIG 5 SHT 1 AND 2 NOTE 8. REPAIR PERFORMED IAW SRM 53-70-00 VOL 1 FIG1 SHT 3 AND 4 (NEW SEAT TRACK SECTION INSTALLED). FABRICATED PARTS IAW DETAIL PARTS TRAVELER N00372/I025372 AND SRM 53-70-00 VOL1 FIG 1 SHT 3-4. 2 L 7 3 4F A22WE 2007012900125 20070129 00125 NM 2007 1 29 AALA20070074 1 20070113 A 3610 LINE BOEING 757 757223 1384957 NM LEFT ENGINE LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 647AM 24605 MIA INFLIGHT T447/13JAN - LEFT ENGINE BLEED LIGHT ILLUMINATED ON TAKEOFF ROLL. WOULD NOT RESET. ENGINE BLEED RESET ON D ESCENT. LANDED MIA WITHOUT INCIDENT. FOUND LOOSE LINE AT HIGH STAGE VALVE. SECURED LINE AND RESEATED CONNECTORS AT HI GH STAGE VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007012900126 20070129 00126 NM 2007 1 29 AALA20070063 1 20070111 A 2530 OVEN BOEING 757 757223 1384957 NM GALLEY DIRTY A AALA A UNSCHED LANDING W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 199AN 32393 SJU INFLIGHT T1044/11JAN AUA TO BOS - FIRST CLASS GALLEY OVEN BEGAN SMOKING. SMELLED LIKE ORGANIC MATERIAL. OVEN TEMPE RATURE WAS SET AT 175 AND THE OVERHEAT LIGHT DID NOT COME ON. THE NUMBER ONE AND NUMBER TWO FIRST CLASS OVENS WERE TURN ED OFF AND THE CIRCUIT BREAKER PULLED. LANDED AT SJU WITHOUT INCIDENT. FOUND FOOD RESIDUE IN FIRST CLASS GALLEY OVEN. CLEANED OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION FOR BOTH OVENS. 2 L 7 2 4F RT A2NM 2007012900127 20070129 00127 EU 2007 1 29 AALA20070062 1 20070111 A 2910 224D4418501 HOSE AIRBUS 300 A300B4605R 3930308 EU HYD SYSTEM LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 21 70073 516 SJU INFLIGHT T1075/11JAN - ON FINAL APPROACH HAD GREEN HYDRAULIC SYSTEM FAILURE. LANDED SJU WITHOUT INCIDENT. AIRCRAF T WAS TOWED TO GATE. REPLACED NUMBER ONE ENGINE GREEN SYSTEM HYDRAULIC PUMP PRESSURE HOSE. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A35EU 2007012900128 20070129 00128 NM 2007 1 29 DL76L070051 1 20070122 A 2410 UNKNOWN BOEING 767 767332 1382001 NM LT GENERATOR UNKNOWN A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 198DN 28455 LEFT GEN DRIVE LIGHT CAME ON PRIOR TO T/O RTB. FWD TO MCO AND PLACARD PER MEL 24-00-01. REPLACED NR 1 ENG IDG RAN ENG OPS CKS GOOD. MCO AND PLAC REMOVED. 2 L 7 2 4F RT A1NM 2007012900130 20070129 00130 NE 2007 1 29 DLM88070053 2 20070124 A 7261 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 LEAKING A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 990DL 43073 53342 718225 LEFT ENG OIL QTY DROPPED TO ZERO. THE ENG WAS SHUT DOWN WHEN THE OIL PRESS WAS AT 35 PSI. THE ENG WINDMILLED FOR 10 MIN S AT ZERO OIL PRESS. REPLACED ENGINE NR 1 PER TRANSMITTAL 9T102. 2 L 7 2 4F 4 F RT A6WE E9NE 2007012900131 20070129 00131 NE 2007 1 29 DL76G070054 2 20070125 A 7320 LINE BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6 30025 NE NR 1 ENGINE CLOGGED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 156DL 58102 25354 695476 NO THROTTLE RESPONCE TO THROTTLE MOVEMENT AFTER ENG START. ALL PARAMETERS NORMAL. FOUND BURNER PRESSURE SENSE LINE CLO GGED. CLEARED LINE, OPS CK NORMAL. 2 L 7 2 4F 4 F RT A1NM E13NE 2007012900132 20070129 00132 NM 2007 1 29 DL76L070055 1 20070123 A 2450 CIRCUIT BREAKER BOEING 767 767332 1382001 NM GE CF6 CF680C2B6 30025 NE APU FAILED A DALA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 SO 27 175DN 24803 695476 DUE RT A/C BUSS FAILURE DURING TAXI. T/S PER SSM NTF. REMOVED AND REPLACED AUX POWER BREAKER C905 PER MM. NORMAL RT/L T APU BUSS ISOLATION OPS NORMAL. 2 L 7 2 4F 4 F RT A1NM E13NE 2007012600102 20070126 00102 WP 2007 1 26 AMTA200700031 1 20070124 A 5753 ATTACH FITTING LKHEED 1011 10113853 5265020 WP NR 3 FLAP GOUGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 164AT 1238 GOUGE ON NR 3 FLAP LEFT INBOARD ATTACH FITTING. REPAIRED PER EER 12910 GAMCO WORKORDER 316063. (M) 2 L 7 3 4F A23WE 2007012600103 20070126 00103 NM 2007 1 26 USAA070065 1 20070124 A 5720 ANGLE BOEING 737 737401 1384701 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 LEFT WING STA 135.50 AFT INBOARD TOP CHORD ANGLE HAS CRACK. INSTALLED REPAIR PLATES, DOUBLERS & FILLER PER EA 98385, DE FECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007012600107 20070126 00107 NM 2007 1 26 USAA070063 1 20070124 A 5310 DOOR FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 442US 24841 FWD CARGO DOOR/FWD FRAME AT 1F FOOTPRINT HAS CRACK. REMOVED DAMAGE & INSTALLED FABRICATED REPAIR PARTS FROM EA 98414, D EFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007012600141 20070126 00141 SO 2007 1 26 SWIA200717691 1 20070118 A 5312 BULKHEAD EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 308SW 120326 LEFT FORWARD BULKHEAD IN FRONT OF 1ST SEAT LOWER ATTACH TRACK CORRODED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LOWER ATTACH TRACK FOR LEFT FORWARD BULKHEAD WITH A SERVICEABLE UNIT. 2 L 7 2 4T RT A31SO 2007012600145 20070126 00145 2007 1 26 UPS07148866 4 20070113 A 2565 LEVER AIRBUS A300 A300F4622R 3930360 EU SLIDE ARM STIFF A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 127UP 0811 SLIDE ARMING LEVER ON ENTRY DOOR IS EXTREMELY HARD TO ARM/DISARM. IT WILL NOT MOVE TO ARMED UNLESS WITH A LOT OF EFFORT . ABOVE NORMAL FORCE REQUIRED. CLEANED GIRT BAR ATTACH FITTINGS. OPS CK NORMAL PER MM 25-61-20-06 PARAGRAPH 4. 2 L 7 2 4F RT A35EU 2007012600159 20070126 00159 NM 2007 1 26 UPS07448863 1 20070115 A 5270 WARNING LIGHT BOEING 747 747212B 1384886 NM L1 DOOR FALSE ACTIVATION A IPXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 522UP 21936 L1 DOOR INDICATION LIGHT CAME ON DURING CLIMB-OUT. LOUD AIR NOISE IN C CARGO AREA. INSPECTED L1 DOOR SEAL. NO DAMAGE. CYCLE L1 DOOR 5 TIMES. NO FAULT FOUND, PRESSURIZING AIRCRAFT TO 2.0, DOOR WARNING LIGHT DID NOT COME ON. OPS CHECK L 1 ENTRY DOOR. OK PER MM 52-11-01. 2 L 7 4 4F A20WE 2007012600161 20070126 00161 2007 1 26 UPS07848851 4 20070112 A 3442 463001C1800413 INU DOUG DC8 DC873F 302199F WP NR 1 FAILED A IPXA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 866UP 45966 ATB - INS ERROR ON CAPT'S SIDE. REMOVED AND REPLACED CAPT'S (1) INU AS PER DC8 MM 34-44-03-4 ADJ/TEST CKS GOOD. 2 L 7 4 4F RT 4A25 2007012600163 20070126 00163 WP 2007 1 26 UPS07848862 1 20070105 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 RIB CRACKED UNDER GUSSET IN RT CTR LE NEXT TO PANEL 523. STOP DRILLED CRACK. FABRICATED 2. REPAIR ANGLES AND INSTALLED IAW SRM 57-03-01, 57-02-00 FIG 002, 51-1-20 AND 51-1-21D. 2 L 7 4 4F RT 4A25 2007012600164 20070126 00164 WP 2007 1 26 UPS07848864 1 20070114 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK ASSY IAW MM 33-50-01-2. 2 L 7 4 4F RT 4A25 2007012600168 20070126 00168 NM 2007 1 26 CALA0700020 1 20070118 A 5320 141A541012 INTERCOSTAL BOEING 737 737724 13844BY NM BS 312-328 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14735 28950 INSPECTION FOUND A 1/2" CRACK IN INTERCOSTAL AT BS 312-328, RBL 31.6. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007012600171 20070126 00171 EU 2007 1 26 DHL2007362503 1 20070106 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 47663 84 CABIN FLOOR SEAT TRACK AND SEAT TRACK FLANGE HAS CORROSION AT LBL 17 BETWEEN FRAMES 18 THRU FRAME 38B. INSTALLED NEW SE CTION OF SEAT TRACK AT CABIN FLOOR BETWEEN FS 18 THRU FS 38B LBL 17 IAW A300 SRM 53-10-10 AND 51-10-40. 2 L 7 2 4F RT A35EU 2007012600212 20070126 00212 EA 2007 1 26 COMA0760030 1 20070116 A 3020 5399001 ANTI-ICE VALVE CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE FAULTY A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 969CA 2326 7141 FLIGHT 5111- ON TAKEOFF ROLL, RECEIVED RIGHT ENGINE COWL ANTI-ICE CAUTION MESSAGE. REMOVED AND REPLACED RIGHT COWL ANTI -ICE PRSOV. 2 L 7 2 4F RT A21EA 2007012600227 20070126 00227 NM 2007 1 26 2007UALA00197 1 20070125 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EXIT LIGHT INOP AT DOOR 4 LEFT AFT SILL, UPPER DECK EXIT DOOR AFT CEILING, UPPER DECK CEILING AT ROW 17 & SEAT 5F AFT. REPLACED LAMPS IN ALL FOUR POSITIONS. EACH OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012600228 20070126 00228 NM 2007 1 26 2007UALA00198 1 20070124 A 2560 BRACKET BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT ENTRY DOOR LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 AFT ENTRY DOOR EVACUATION SLIDE CONTAINER FWD GIRT BAR STOWAGE BRACKET IS LOOSE. SECURED BRACKET. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012600229 20070126 00229 NM 2007 1 26 2007UALA00199 1 20070125 A 5330 SKIN PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 EXTERNAL KEEL BEAM LOWER SKIN PANEL BETWEEN MLG WHEEL WELLS IS CRACKED AT BS 683 APPROX AT LBL 4. MAJOR REPAIR: FABRIC ATED AND INSTALLED EXTERNAL DOUBLER REPAIR PER SRM 53-60-12 PAGE 1. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012600233 20070126 00233 NM 2007 1 26 UPS07448952 1 20070111 A 5320 65B07498204 INTERCOSTAL BOEING 747 747123 1384873 NM FUSELAGE DEFORMED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C AFT OF BULK CARGO COMPT FX FRAME INTERCOSTAL WEB FOUND DEFORMED BETWEEN BS 2220 AND BS 2240 STR 40R AS MARKED. AFT OF BULK CARGO COMPT FX FRAME INTERCOSTAL WEB REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51 -30-02 JUST AT BS 2220 AND BS 2240 STR 40R AREA. 2 L 7 4 4F A20WE 2007012600234 20070126 00234 NM 2007 1 26 UPS07548956 1 20070123 A 5610 HANDLE BOEING 757 75724APF 1384969 NM F/O WINDOW STIFF A IPXA K NONE O OTHER NR NOT REPORTED 1 SO 01 431UP 25462 INSPECTION TYPE:N/A FIRST OFFICER'S WINDOW UNLOCK HANDLE VERY STIFF. RIGGED RT SLIDING WINDOW IAW MM 56-11-02, OPS CK G OOD, THIS CLEARS DEFERRAL D342628. PLACARD REMOVED. 2 L 7 2 4F RT A2NM 2007012600235 20070126 00235 2007 1 26 UPS07648938 4 20070122 A 3431 UNKNOWN BOEING 767 76734AF 1385212 NM ILS SYSTEM MALFUNCTIONED A IPXA A UNSCHED LANDING O OTHER UK UNKNOWN 1 SO 01 330UP 27756 INSPECTION TYPE:N/A DIVERSION - ALL 3 ILS SYSTEMS INOP. REPLACED ILS CONTROL PANEL PER AMM 34-31-02-4. OPS CHECKS GOOD. 2 L 7 2 4F RT A1NM 2007012600236 20070126 00236 WP 2007 1 26 UPS07848926 1 20070103 A 5514 37014261 ANGLE DOUG DC8 DC871F 302199D WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C2 LEFT HORIZ STAB LEADING EDGE VERY INBOARD UPPER T-ANGLE CRACKED. CUT OUT DAMAGED AREA ON INBOARD UPP ER T-ANGLE ON LT HORIZ STAB LEADING EDGE IAW SRM 51-1-21, RECEIVED, LOCATED, DRILLED UP AND INSTALLED T-ANGLE FITTING ON THE LEFT HORIZ STAB LEADING EDGE IAW SRM 51-1-21, AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 2007012600237 20070126 00237 WP 2007 1 26 UPS07848936 1 20070106 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 TWO CRACKS IN END OF RIB AT INBOARD END F/O RIGHT OUTBOARD LEADING EDGE. STOP DRILLED CRACKS, FABRIC ATED AND INSTALLED 2 REPAIR ANGLES IAW SRM 57-02-00-0 FIG 002, 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2007012600238 20070126 00238 WP 2007 1 26 UPS07848937 1 20070105 A 5754 SKIN DOUG DC8 DC871F 302199D WP L/E SLOT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 INNER SKIN WORN/CHAFED AT OUTBOARD END OF RIGHT OUTBOARD SLOT VANE. FABRICATED AND INSTALLED INNER D OUBLER IAW SRM 57-3-1 FIG 9. 2 L 7 4 4F RT 4A25 2007012600239 20070126 00239 WP 2007 1 26 UPS07848941 1 20070106 A 5320 375151402 SUPPORT FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C2 SUPPORT FITTING CRACKED AT STA 980 RBL 24 4 INCHES BELOW CABIN SEAT TRACK. REMOVED AND REPLACED SUPP ORT FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 2007012600240 20070126 00240 WP 2007 1 26 UPS07848942 1 20070105 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 LARGE DENT ON NOSE OF RT CTR L/E. CRACKED SKIN, BROKEN RIVETS XFS 392. CUT OUT DAMAGE, FABRICATED F ILLER AND DOUBLER. INSTALLED CONICAL WASHERS, FILLER AND DOUBLER IAW SRM 57-02-01-0 FIG 0024, 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2007012600241 20070126 00241 WP 2007 1 26 UPS07848954 1 20070104 A 5347 3657502U507 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 CAPTAIN`S AFT SEAT TRACK I/B WORN AND O/B HAS ELONGATED HOLES. REMOVE AND REPLACE CAPTAIN`S AFT I/B AND O/B SEAT TRACKS IAW SRM 51-1-20D, 51-03-02 AND 51-3-0. 2 L 7 4 4F RT 4A25 2007012600242 20070126 00242 WP 2007 1 26 UPS07848955 1 20070114 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C2 AFTER REMOVAL OF CORROSION, FOUND CORROSION OUT OF LIMITS ON FRAME AT STA 1973, LT & RT. REMOVED FRA ME SPLICE AT STA 1973 FWD OF TAIL NAV LIGHT IAW SRM 51-1-21. FABRICATED, AND INSTALLED REPAIR FRAME SPLICES AT STA 1973 LT & RT IAW SRM 51-1-4, 53-02-00 FIG 6, AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007012600301 20070126 00301 NM 2007 1 26 QXEA200700039 1 20070118 A 3297 471515 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM MLG MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 424QX 186 4006 PDX FLIGHT NR 2345: LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. HANDLE SELECTED UP BUT GEAR REMAINED 3-GREEN. AIRCRA FT RETURNED TO FIELD. MAINTENANCE INTERROGATED PSEU. FOUND NLG CENTERING PROX SENSOR OPEN. REMOVED WOW2 AND CENTERING HARNESS IAW Q400 TASK 32-61-06-000-802 AND REPLACED THE WOW2/CENTERING HARNESS IAW Q400 AMM TASK 32-61-06-400-802. PER FORMED OPS TEST OF EXT/RETRACTION SYSTEM IAW TASK 32-31-00-710-801. OPS TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007012600317 20070126 00317 NM 2007 1 26 KPVA20071 1 20070118 A 5753 734380B TORQUE TUBE DHAV DHC8 DHC8103 1386005 NM ZONE 600 BROKEN A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 811WP 366 FIRST FLAP DRIVE TORQUE TUBE CONNECTED TO FPU ON RIGHT SIDE IS BROKEN. REMOVED AND REPLACED RT FIRST FLAP DRIVE TORQUE TUBE IAW DHC-8 MM, CHAP 27-52-20 PG 201-209. 2 H 7 2 4T RT A13NM 2007012600361 20070126 00361 NE 2007 1 26 QXEA200700037 2 20070117 A 7320 UNKNOWN DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 366PH 510 PDX FLIGHT NR 2060 NOTICED PRE FLIGHT, NR 1 AND NR 2 ENGINE MANUAL CAUTION LIGHTS ILLUMINATED. MAINTENANCE RESET BETA L OCK OUT C/B ON DC CONTRACTOR PANEL. NR 1 AND NR 2 ECU MANUAL CAUTION LIGHTS NOT ILLUMINATED. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007012600368 20070126 00368 EA 2007 1 26 SWIA200717737 1 20070104 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 969SW 7876 STA 621 LOWER FRAME AT FLOOR LEVEL RT SIDE HAS CRACK CORNER, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PAR TS 601R-53-61-117 ANGLE, REPAIR ANGLE AND STRAP IAW CR200 SRM 51-23-00 AND REO 601R-53-61-117. 2 L 7 2 4F RT A21EA 2007012600375 20070126 00375 NM 2007 1 26 QXEA200603358 1 20070102 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 412QX 4059 PDX C3 - HEAVY CORROSION AT RIGHT OUTBOARD SEAT TRACK APPROXIMATELY X290.00. REPAIRED IAW DHC-8-400 SRM 51-42-0555 AND 51-40-10. 2 H 7 2 4T RT A13NM 2007012600376 20070126 00376 NM 2007 1 26 QXEA200603363 1 20070107 A 5312 BULKHEAD BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 412QX 4059 PDX C3 - CHAFE ON NOSE LANDING GEAR WHEELWELL AFT BULKHEAD. REPARIED IAW RD 8/4-53-1224. 2 H 7 2 4T RT A13NM 2007012600377 20070126 00377 NM 2007 1 26 DHL2007743502 1 20070118 A 5753 SKIN BOEING 727 727225 1384077 NM FOREFLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 RT IB TE FOREFLAP LOWER SKIN PRESENTS DELAMINATION APPROX AT WBL 210.0. CUT OUT DELAMINATED AREA APPROX 13" BY 15.5". FABRICATED FILLER APPROX 13" BY 15.5" AND DOUBLERS 2EA APPROX 3" BY 15.5" FROM 2024T3 .016 PO NR 9003189. CLEANED, PREP PED, BONDED, TREATED, PRIMED, AND SEALED EDGES IAW B727 SRM 57-50-2 FIG 3, 51-40-20, AND 51-40-24 FIG 3. 2 L 7 3 4F A3WE 2007012600378 20070126 00378 NM 2007 1 26 DU4R2007028 1 20070110 A 5313 STRINGER BOEING 757 757232 1384965 NM FUSELAGE CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION AFT CARGO LOCATED ON STRINGER 29R BS 1515. REMOVED CORRODED SECTION OF STRINGER. DRILLED AND INSTALLED EXTRU SION FROM BAC1498-204 7075-T62 CLAD IAW B757 SRM 53-00-03 FIG 201, 51-30-01 AND 51-40-02. 2 L 7 2 4F RT A2NM 2007012600379 20070126 00379 NM 2007 1 26 DU4R2007029 1 20070114 A 5320 CUSP WEB BOEING 757 757232 1384965 NM FUSELAGE CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION AT BS 1380 TO BS 1400 STRINGER 17 WEB RT. REMOVED CORRODED CUSP WEB. FABRICATED AND INSTALLED REPLACEMENT WE B 19.5" BY 19.5" FROM 7075-T6 .040" IAW B757 SRM 51-40-02, 51-20-01 AND DELTA PS 900-2 NR 5. 2 L 7 2 4F RT A2NM 2007012600380 20070126 00380 NM 2007 1 26 DU4R2007030 1 20070110 A 5320 FLOOR SUPPORT BOEING 757 757232 1384965 NM FUSELAGE CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION AT L-4 DOOR FWD FLOORBOARD SUPPORT BETWEEN BS 1640 AND BS 1680 B/L 54L I/B OF S-17L. REMOVED FLOOR SUPPORT, D RILLED AND INSTALLED NEW FLOOR SUPPORT P/N 146N5246U5 IAW B757 SRM 51-40-02, 51-40-05 AND 51-20-01. 2 L 7 2 4F RT A2NM 2007012600381 20070126 00381 NM 2007 1 26 DU4R2007031 1 20070113 A 5320 CUSP WEB BOEING 757 757232 1384965 NM FUSELAGE CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION AT BS 1400 AND BS 1420 RT CUSP WEB. REMOVED CUSP WEB. FABRICATED AND INSTALLED NEW WEB FROM 7075-T6 .040" 19 .5" BY 9.5" IAW B757 SRM 51-40-05 FIG 3.6, 51-20-01 AND 51-40-02 AND DELTA PS 900-2 NR 5. 2 L 7 2 4F RT A2NM 2007012600382 20070126 00382 NM 2007 1 26 DU4R2007023 1 20070115 A 5320 FLOOR SUPPORT BOEING 757 757232 1384965 NM FUSELAGE CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION ON LWR FLANGE OF FLOOR SUPPORT WEB AT BS 1620 LBL 3 IN AFT PIT. REMOVED CORRODED INTERCOSTAL WEB. FABRICATED AND INSTALLED REPAIR INTERCOSTAL WEB 20" BY 9" FROM 7075-T6 .040" IAW B757 SRM 51-30-01, 51-40-05, 51-20-01, 51-40-02. 2 L 7 2 4F RT A2NM 2007012600383 20070126 00383 NM 2007 1 26 DU4R2007024 1 20070116 A 5311 ATTACH FITTING BOEING 757 757232 1384965 NM FUSELAGE CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION ON FRAME ATTACH CLIP AT BS 1540 LBL 9 AFT PIT. REMOVED CORRODED ATTACH CLIP. FABRICATED AND INSTALLED REPAIR CLIP 4.5" BY 2.0" FROM 7075-T6 .050" IAW B757 SRM 53-00-07, 51-20-01, 51-40-02 AND DELTA PS 900-4-1. 2 L 7 2 4F RT A2NM 2007012600384 20070126 00384 NM 2007 1 26 DU4R2007025 1 20070117 A 5320 WEB BOEING 757 757232 1384965 NM FUSELAGE CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION ON UPPER SURFACE OF WEB BETWEEN FLOOR SUPPORTS AT BS 1520 TO BS 1540 RBL 7 RBL 11. REMOVED WEB. FABRICATED A ND INSTALLED REPAIR INTERCOSTAL 20.0" BY 5.0" FROM 7075-T6 .032" IAW B757 SRM 51-40-02, 51-20-01 DELTA PS 900-4-01 NR 1. 2 L 7 2 4F RT A2NM 2007012600385 20070126 00385 NM 2007 1 26 DU4R2007026 1 20070119 A 5322 SHEAR TIE BOEING 757 757232 1384965 NM FUSELAGE CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION AT BASE OF FRAME UNDER FLOOR SUPPORT STRUCTURE THE BULGE OF THE AFT CARGO PIT AT BS 1460 B/O 0 TO B/L 13L. RE MOVED SHEAR TIE. FABRICATED AND INSTALLED SHEAR TIE 7.0" BY 2.0" FROM 7075-T6 .050" IAW B757 SRM 51-30-01, 51-10-021 AN D 51-40-02. 2 L 7 2 4F RT A2NM 2007012600386 20070126 00386 NM 2007 1 26 DU4R2007027 1 20070109 A 5313 STRINGER BOEING 757 757232 1384965 NM FUSELAGE CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION FOUND AT STRINGER 28R FROM BS 1500 TO BS 1520 IN AFT CARGO COMPARTMENT. REMOVED CORRODED SECTION OF STRINGER. FABRICATED AND INSTALLED SPLICE 7075-T62 CLAD 11" "Z" CHANNEL IAW B757 SRM 53-00-03 FIG 201, AND 51-40-02. 2 L 7 2 4F RT A2NM 2007012600388 20070126 00388 NM 2007 1 26 0700363167 1 20070120 A 5220 CABLE AIRBUS A319 A319114 3930350 NM ESCAPE HATCH BROKEN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 367NB 9449 9449 2028 DURING "L" CHECK, FOUND LT OVERWING EMERGENCY ESCAPE HATCH CABLE BROKEN. REMOVED AND REPLACED LT INFLATION RESERVOIR IN ACCORDANCE WITH MM 25-65-46. OPS CHECK AND CABLE TENSION GOOD IN ACCORDANCE WITH MM 25-62-46. 2 L 7 2 4F RT A28NM 2007012900004 20070129 00004 SO 2007 1 29 LR7A07005 1 20070117 A 5340 3528962 FITTING LKHEED 382 382G 526414U SO FS 946 WL 270 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 652 4698 DURING SCHEDULED B 2 CHECK PER JOB CARD HB5302, FOUND GUSSET FITTING CRACKED AT FS 946, WL 270, RBL 61.5. REPLACED FITT ING IAW SMP 583 51-70. 2 H 7 4 4T A1SO 2007012900005 20070129 00005 NM 2007 1 29 UPS07448968 1 20070110 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C BULK CARGO COMPT FLOOR SUPPORT LWR SURFACE FOUND CORROSION AT STA 2039 TO STA 2100 CENTER LINE TO RBL 2. BULK CARGO COMPT FLOOR SUPPORT REPAIRED AS PER SRM 53-10-07 FIG 20 AT STA 2030 TO STA 2160 RBL 2. 2 L 7 4 4F A20WE 2007012900006 20070129 00006 NM 2007 1 29 UPS07M48927 1 20070121 A 2913 PUMP DOUG MD11 MD11F 3023600 NM NR 2 ENGINE FAILED A IPXA K NONE K FLUID LOSS UK UNKNOWN 1 SO 01 283UP 48484 INSPECTION TYPE:N/A SYSTEM 2 HYD QTY LOSS IN FLIGHT, 50 MINUTES INTO FLIGHT HYD PUMP 2L OFF, 10 MINUTES LATER HYD 2R OFF . QTY 8.2 FOLLOWED BY HYD 2 OFF, 15 MINUTES LATER HYD 2 FIL QTY WAS 0.0. REMOVED AND REPLACED NR 2 ENG LT HYD PUMP PER 29-11-20-4. REQUIRES OPS CHECK. REMOVED AND REPLACED NR 2 ENG R/H HYD PUMP PER 29-11-20. PUMP REQUIRES LEAK AND OPS CHECK. LEAK AND OPS CHECKED PER MM 29-11-20-4-2. 2 L 7 3 4F RT A22WE 2007012900011 20070129 00011 SO 2007 1 29 LR7A07010 1 20070125 A 5310 WINDOW FRAME LKHEED 382 382G 526414U SO FS 124 WL 251 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 669 4763 DURING SCHEDULED B 2 CHECK PER JOB CARD HB5301, FOUND RT DV WINDOW FRAME CRACKED AT FS 124, WL 251. REPAIRED FRAME IAW SMP583 53-30-25 AND LAC MEA 382-53-07-007. 2 H 7 4 4T A1SO 2007012900023 20070129 00023 NM 2007 1 29 UPS07448933 1 20070111 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C AFT OF BULK CARGO COMPT - FX STRINGER FOUND CORROSION CRACK AT BS 2177 STR 48 RT AS MARKED. AFT OF BU LK CARGO COMPT - FX STRINGER 48R REPAIRED AS PER SRM 53-10-03 FIG 1, JUST BETWEEN BS 2150 AND 2185 AREA. 2 L 7 4 4F A20WE 2007012900034 20070129 00034 EU 2007 1 29 0700373269 1 20070123 A 2530 COFFEEMAKER AIRBUS 320 A320212 3930322 EU GALLEY ODOR A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 01 369NW 1011 FLIGHT ATTENDANT REPORTED LARGE WATER MESS IN AFT GALLEY, THEN ODOR OF ELECTRICAL FUMES AND SMOKE. FLIGHT CREW REMOVED POWER FROM GALLEY, OBSERVATION REVEALED THAT ODOR STILL PERSISTED, NO SMOKE. AN EMERGENCY WAS DECLARED AND THE FLIGHT D IVERTED INTO DTW. AIRCRAFT LANDED UNEVENTFULLY. CORRECTIVE ACTION WAS TO REPLACE AFT GALLEY COFFEEMAKER. 2 L 7 2 4F RT A28NM 2007012900057 20070129 00057 NM 2007 1 29 SWAA070370 1 20070125 A 2750 6935349 TORQUE TUBE BOEING 737 7373H4 1384600 NM T/E FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD FORE FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE T UBE PER MM. 2 L 7 2 4F RT A16WE 2007012900067 20070129 00067 NM 2007 1 29 SWAA070380 1 20070125 A 5322 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007012900072 20070129 00072 NM 2007 1 29 SWAA070385 1 20070125 A 5313 6551698 STRINGER SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 359, STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007012900080 20070129 00080 NM 2007 1 29 SWAA070388 1 20070125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 23R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012900082 20070129 00082 NM 2007 1 29 07FDEA00155 1 20070124 A 5313 STRINGER BOEING 727 727233 138408A NM BS 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 FWD PIT 3" FWD OF STA 600, STR 27L EXFOLIATED REPAIRED STR 27L AT STA 600 IAW SRM 53-10-3 PG4 FIG1 SHEET 2,TABLE I. 2 L 7 3 4F RT A3WE 2007012900088 20070129 00088 NM 2007 1 29 SWAA070391 1 20070125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012900099 20070129 00099 NM 2007 1 29 SWAA070398 1 20070125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012900102 20070129 00102 NM 2007 1 29 SWAA070400 1 20070125 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012900121 20070129 00121 WP 2007 1 29 07FDEA00176 1 20070126 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 899 L50-52R DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 LOWER EXT FUSELAGE FOUND DEEP DENT 13" BY 4" MAX DEPTH .200" LOWER SKIN AT STA 899 FROM LONG NR 50 RT TO LONG NR 52 C/L. REMOVE DOUBLER AAU7010-3 AND DOOR ADA8067-1 IAW SRM 51-30-00 VOL 2. TRIMMED OUT DAMAGED AREA AND REMOVED EXISTING REP AIR AT STA 899 LONG NR 51L IAW SRM 53-20-00 FIG 6 SHT 3, 4 VOL 1. PERFORMED HFEC INSP IAW NDT SPM 06, NO CRACK FOUND. INSTALLED REPAIR PARTS P/N I025213-3 TO -19 IAW SRM 53-20-00 VOL1 FIG 6 SHT 3, 4. REINSTALLED AAU7010-3 AND AADA8067- 1 IAW SB 53-86 PAGE 12, 13 VIEW A-A. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N00213 AND SRM 53-20-00 VOL1 FIG 6 SHT 3, 4. 2 L 7 3 4F A22WE 2007012900124 20070129 00124 WP 2007 1 29 07FDEA00185 1 20070126 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1521-1541 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 CTR CARGO COMPT BILGE FOUND CORROSION WITH EXFOLIATION ON SKIN BTWN STA 1521 AND STA 1541 FROM LONG NR 45 RT TO LONG NR 42 LT. TRIMMED OUT DAMAGED SKIN AND REPAIRED IAW SRM 53-20-00 VOL 2 FIG 6 SHT 15. FABRICATED PARTS IAW ETAIL PARTS TRA VELER I026602/N01602 AND IAW SRM 53-20-00 VOL1 FIG 6 SHT 3-6. 2 L 7 3 4F A22WE 2007012900141 20070129 00141 EA 2007 1 29 QXEA200603372 1 20070102 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSLEAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 290RB 10029 OKC - CORROSION FOUND ON LOWER SECTION OF SERVICE DOOR CUTOUT. REPAIRED IAW CRJ 700 SRM 53-21-23. 2 L 7 2 4F RT A21EA 2007012900146 20070129 00146 NM 2007 1 29 QXEA200700100 1 20070124 A 3010 4100S00503 VALVE BOMBDR DHC8 DHC8402 1390042 NM ANTI ICE SYS UNKNOWN A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 413QX 4919 4060 GEG FLIGHT NR 2356: UPON DESCENT INTO GEG, ENTERED CLOUDS WITH ICE. TURNED ON AIRFRAME ANTI-ICE TO SLOW POSITION. THE DEICE PRESSURE CAUTION LIGHT ILLUMINATED IMMEDIATELY. RAN THE CHECKLIST. PROBLEM WAS FIXED FOR APPROXIMATELY 30 SECOND S AFTER RE-SELECTION OF SLOW THEN THE DEICE PRESSURE CAUTION LIGHT ILLUMINATED. PRESSURE GAGE APPEARED TO HAVE NORMAL P RESSURE. MAINTENANCE REMOVED AND REPLACED NR 2 DDV VALVE IAW Q400 AMM 30-11-16, PGS 401-408. OPS CHECK GOOD. REMOVED AND INSTALLED LEADING EDGE 613AR IAW AMM TASKS 57-23-01-000-801 AND 57-23-01-400-801. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007012900147 20070129 00147 EA 2007 1 29 SWIA200717743 1 20070105 A 5340 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 710BR 7852 RT FS 621 PRESSURIZED BULKHEAD FLOOR ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE, REPAIR ANGLE AND STRAP PER REO 601R 53-61-117 REV 'C'. 2 L 7 2 4F RT A21EA 2007012900149 20070129 00149 EA 2007 1 29 SWIA200717744 1 20070105 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 710BR 7852 RT FS 484 O/B INTERCOSTAL CRACKED AT LBL9, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLE 601R 53-41-059- 2 PER REO 601R 53-41-059. 2 L 7 2 4F RT A21EA 2007012900156 20070129 00156 EA 2007 1 29 SWIA200717746 1 20070105 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 710BR 7852 LBL9 STA 280 LOWER FRAME CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS AND CLIPS AS PER CRJ200 REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 2007012900157 20070129 00157 NM 2007 1 29 SWAA070251 1 20070118 A 5311 6546530 FRAME BOEING 737 7373H4 1384600 NM BS 460 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 460, BETWEEN STR 28L AND STR 28R. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007012900159 20070129 00159 NM 2007 1 29 SWAA070252 1 20070118 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 312 S28R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 312, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007012900160 20070129 00160 NM 2007 1 29 SWAA070253 1 20070118 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM BS 780 S19L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007012900162 20070129 00162 2007 1 29 SWAA070255 4 20070118 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007012900164 20070129 00164 NM 2007 1 29 SWAA070257 1 20070118 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 775SW 30590 DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER M M. 2 L 7 2 4F RT A16WE 2007012900165 20070129 00165 NM 2007 1 29 SWAA070258 1 20070118 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 775SW 30590 DURING SCHEDULED HC1 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER M M. 2 L 7 2 4F RT A16WE 2007012900167 20070129 00167 NM 2007 1 29 SWAA070259 1 20070118 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 775SW 30590 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2007012900170 20070129 00170 NM 2007 1 29 SWAA070248 1 20070118 A 5754 65C26602 SKIN BOEING 737 7373H4 1384600 NM NR 2 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED C3 CHECK, FOUND LT WING NR 2 L/E SLAT CRACKED AT INBOARD AFT CORNER. REPAIRED SLAT PER SWA EA. 2 L 7 2 4F RT A16WE 2007012900176 20070129 00176 EA 2007 1 29 SWIA200717748 1 20070105 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 710BR 7852 PAX DOOR AFT WEB CRACKED/LOWER CORNERS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS AS PER CRJ200 REO 601R-52-11-702. 2 L 7 2 4F RT A21EA 2007012900205 20070129 00205 EA 2007 1 29 SWIA200717752 1 20070105 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 710BR 7852 PAX DOOR FWD SIDE BENEATH TOP FOLDING STEP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS ON PAX DOOR TOP STEP AREA AS PER CRJ200 REO 601R-52-11-279. 2 L 7 2 4F RT A21EA 2007012900206 20070129 00206 EA 2007 1 29 SWIA200717753 1 20070105 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 710BR 7852 STA 625 LT INTERCOSTAL CRACKED AT RADIUS, DISCOVERED DURING C-CHECK INSPECTION. REPLACED INTERCOSTAL P/N 601-35012-51 P O 71471 AT STA 65 LHS PER CRJ200 REO 601R-53-61-422. 2 L 7 2 4F RT A21EA 2007012900208 20070129 00208 EU 2007 1 29 TRAX200700070 1 20070112 A 5320 BRACKET AEROSP ATR72 ATR72212 8680945 EU FUSELAGE BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 635AS 372 FOUND ANGLE BRACKET BROKEN ON FRAME 23D IN WING BOX. 2 H 7 2 4T RT A53EU 2007012900210 20070129 00210 WP 2007 1 29 0700389971 1 20070118 A 5210 5910081105 DOOR DOUG DC9 DC931 3022065 WP MAIN PAX OUT OF RIG A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9335 91839 5540 47337 UNABLE TO OPEN MAIN CABIN DOOR, TRIED FROM INSIDE AND OUTSIDE OF AIRCRAFT. MAINTENANCE DISCOVERED UPPER FORWARD CORNER OF MAIN CABIN DOOR BINDING AGAINST DOOR CUTOUT STRUCTURE. PRESSED IN ON UPPER FORWARD CORNER AND WAS ABLE TO OPEN MAIN CABIN DOOR. PRESSURIZED AIRCRAFT TO 3.5 PSI, DOOR JAMMED AGAIN. MAIN CABIN DOOR WAS FOUND TO BE OUT OF RIG. RIGGED DO OR PER AMM 52-11-00. ALSO, FOUND BOLT GOING THROUGH OUTER HANDLE LOOSE, REPLACED BOLT. FOUND A DEEP GOUGE IN OUTER DOO R HANDLE PAN. MAINTENANCE REPLACED DOOR PER MM 52-11-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007012900215 20070129 00215 EU 2007 1 29 MALA070016 1 20070122 A 3350 330151 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 416XJ 340B416 DURING LC2 NOTED EMERGENCY LIGHTS FROM BATTERY PACK 24LN INOP. REMOVED AND REPLACED POWER SUPPLY 24LN PN 3301-51, SN ON 2205, SN OFF 2129. 2 L 7 2 4T RT A52EU 2007012900217 20070129 00217 EU 2007 1 29 MALA070019 1 20070125 A 5753 SKIN SAAB SF340 340B 7860101 EU RT TE FLAPS DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 340B427 THE RT FLAP TRAILING EDGE, APPROXIMATELY 9.0 INCHES FROM THE INBOARD END, IS DAMAGED. THE DAMAGE HAS BEEN REPAIRED IAW MESABA EO NR S57143. REF: EAMS WORK ORDER 217373 TASK 6501. 2 L 7 2 4T RT A52EU 2007012900218 20070129 00218 NM 2007 1 29 DHL2007743504 1 20070126 A 5312 BULKHEAD BOEING 727 727225 1384077 NM CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 AFT CABIN, BS 1183 BULKHEAD SHOWS CRACK AT VERTICAL FLANGE ANGLE, APPROX BETWEEN BBL 36.8 AND WL 225. COMPLIED WITH REP AIR PROCEDURES PER B727 SB 727-53-0192, TO INCLUDE: TERMINATION OF CRACK END BY STOP DRILLING (.250" HOLE), AND INSTALLA TION OF REPAIR PARTS FROM SB REPAIR KIT P/N 65C34406-15. BARE AREA'S TREATED AND PRIMED AS REQ PER B727 SRM 51-10-2. A REA RETURNED TO NORMAL. 2 L 7 3 4F A3WE 2007012600252 20070126 00252 EA 2007 1 26 TRAX200700081 1 20070114 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 350-495 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FOUND RT FLOOR SEAT TRACK CORRODED, FS 350 TO 495, SEC 1. 2 L 7 2 4F RT A21EA 2007012600273 20070126 00273 EU 2007 1 26 MALA070007 1 20070116 A 5520 SKIN SAAB SF340 340B 7860101 EU RT ELEVATOR DELAMINATED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 340B433 RT ELEVATOR OUTBOARD LEADING EDGE SURFACE DELAMINATION PUNCTURE. REPAIRED IAW EOS51031. REF EAMS WO NR 215326 TASK 350 4. 2 L 7 2 4T RT A52EU 2007012600274 20070126 00274 EA 2007 1 26 COMA0760033 1 20070117 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA K NONE O OTHER AP APPROACH 1 SO 01 783CA 7315 FLIGHT 4940 - ON FINAL APPROACH WHEN FLAPS SELECTED FROM 30 TO 45 DEGREES FLAPS STAYED AT 30 DEGREES WITH FLAP FAIL MESS AGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (G) 1,2,3, (A,B,C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007012600362 20070126 00362 NM 2007 1 26 QXEA200700036 1 20070112 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY DAMAGED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 364PH 524 PDX FLIGHT NR 2142, INTERMITTENT SMOKE WARNING DURING FLIGHT. NO INDICATIONS OF SMOKE OR HEAT FROM CARGO AREA. AS WE G OT CLOSER TO PDX WARNINGS GOT MORE FREQUENT. MAINTENANCE INSPECTED AND FOUND NR 2 BAGGAGE SMOKE DETECTOR MISSING EMIRMI TAPE. INSTALLED TAPE IAW EO 2-26-028. PERFORMED OPS CHECK IAW 26-15-00-710-801. SMOKE DETECTORS OPERATIONAL CHECK GO OD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007012600367 20070126 00367 EA 2007 1 26 SWIA200717736 1 20070104 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 969SW 7876 PAX DOOR AFT DRAG ANGLE CRACKED AT PULL CABLE EXIT, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER RE O 601R 52-11-513 REV 'A'. 2 L 7 2 4F RT A21EA 2007012600369 20070126 00369 EA 2007 1 26 SWIA200717738 1 20070104 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 969SW 7876 LT STA621 LOWER CORNER CRACK AT FLOOR LEVEL, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS 601R-53-61-11 7 ANGLE, REPAIR ANGLE AND STRAP IAW CR200 SRM 51-23-00 AND REO 601R-53-61-117. 2 L 7 2 4F RT A21EA 2007012900007 20070129 00007 SO 2007 1 29 LR7A07006 1 20070117 A 5310 WINDOW FRAME LKHEED 382 382G 526414U SO BS 124 WL 251 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 652 4698 DURING SCHEDULED B 2 CHECK PER JOB CARD HB5301, FOUND LT DV WINDOW FRAME CRACKED AT FS 124, WL 251.5 - WL 255. REPAIRED FRAME IAW SMP583 53-30-25 AND LAC MEA 382-53-07-002. 2 H 7 4 4T A1SO 2007012900008 20070129 00008 SO 2007 1 29 LR7A07007 1 20070117 A 5420 WEB LKHEED 382 382G 526414U SO FS 497 WS 220 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 652 4698 DURING SCHEDULED B 2 CHECK PER JOB CARD HB7201, FOUND NR 3 ENGINE NACELLE OB FAIRING WEB CRACKED AT FS497, WS220. REPAI RED WEB IAW SMP 583 57-40-11 AND LAC MEA 382-54-07-003. 2 H 7 4 4T A1SO 2007012900009 20070129 00009 SO 2007 1 29 LR7A07008 1 20070117 A 5413 LONGERON LKHEED 382 382G 526414U SO FS 485 WL 256 DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 652 4698 DURING SCHEDULED B 2 CHECK PER JOB CARD HSP71189, FOUND NR 1 QEC OB UPPER LONGERON OB AFT HOLE FOR FASTENER OF SUPORT BE AM WITH OVERSIZED HOLE AT FS 485, WL 256. REPAIRED LONGERON IAW MEA 382-54-07-004. 2 H 7 4 4T A1SO 2007012900018 20070129 00018 NM 2007 1 29 UPS07448931 1 20070109 A 5320 TIE CLIP BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 2180 STR 13R FRAME ATT TIE CLIP FOUND CRACK. M/D BS 2180 STR 13R FRAME ATT TIE CLIP REPLACED A S PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007012900021 20070129 00021 EU 2007 1 29 DHL2007362504 1 20070121 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 47663 84 CABIN FLOOR SEAT TRACK AT SEAT TRACK FLANGE HAS CORROSION BETWEEN FRAME 18 THRU FRAME 37 AT LBL 76. REMOVED CORROSION F ROM FS 18 TO FS 37 LBL 76 IAW A300 SRM 51-40-11, FOUND WITHIN LIMITS TREATED AN PRIMED AN PAINTED IAW A300 SRM 51-40-12. FOUND OUT OF LIMITS FROM FR 21.5- 26.5 IAW A300 SRM 53-10-00 FIG 612. REPLACED SECTION FROM FS 21.5 TO FS 26.5 IAW A3 00 SRM 53-10-10 FIG 724 MAT USED 60-22457 PO NR 031938. FOUND TO BE WITHIN LIMITS FROM FS 26.5 TO FS 37 IAW A300 SRM 53 -10-00 FIG 612,TREATED/PRIMED/PAINTED IAW A300 SRM 57-40-12. THIS IS A PERMANENT REPAIR. 2 L 7 2 4F RT A35EU 2007012900028 20070129 00028 EA 2007 1 29 SWIA200717757 1 20070117 A 5280 DOOR CNDAIR CL600 CL6002B19 1900309 EA RT MLG MISSING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 978SW 7953 ON POST FLIGHT, DISCOVERED RIGHT MAIN GEAR DOOR MISSING. REPLACED RIGHT MLG DOOR IAW CRJ 200 MM 32-12-01. 2 L 7 2 4F RT A21EA 2007012900038 20070129 00038 NM 2007 1 29 07FDEA00064 1 20070110 A 5311 AFA00283 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 CABIN RIGHT STA 1681 BETWEEN LONGERON 12 TO LONGERON 14 FRAME FOUND DENT. CABIN, RIGHT STA 1681 BETWEEN LONGERON 12 T O LONGERON 14 FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION R EQUIRED AT 14,500 CYCLE WITH REPETITIVE INSPECTIONS AT 9,500 CYCLES. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007012900039 20070129 00039 NM 2007 1 29 UPS07448945 1 20070109 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO BS 780-800 S35R FOUND CRACKED AS MARKED. FWD CARGO COMPT BS 742 TO BS 830 STR 35R REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F RT A20WE 2007012900051 20070129 00051 NM 2007 1 29 SWAA070364 1 20070125 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 480, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007012900058 20070129 00058 NM 2007 1 29 SWAA070371 1 20070125 A 5753 6546430101 SKIN BOEING 737 7373H4 1384600 NM FORE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SKIN DELAMINATED AT OUTBOARD END. REPAIRED FORE FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007012900059 20070129 00059 2007 1 29 SWAA070372 4 20070125 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007012900065 20070129 00065 NM 2007 1 29 SWAA070378 1 20070125 A 2560 65659725 MOUNT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT FLOOR MOUNT LOOSE. SECURED FLOOR MOUNT PER MM. 2 L 7 2 4F RT A16WE 2007012900069 20070129 00069 NM 2007 1 29 SWAA070382 1 20070125 A 5322 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007012900073 20070129 00073 NM 2007 1 29 SWAA070386 1 20070125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012900076 20070129 00076 NM 2007 1 29 07FDEA00074 1 20070111 A 5730 ARB2886504 SKIN DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT WING TELESCOPIC DUCT CUTOUT FOUND CRACKED. CRACK AREA ON THE RIGHT WING TELESCOPIC DUCT CUTOUT REPAIRED AS PER SR M 57-10-00 FIGURE 42 VOLUME I AND FEDEX EA NR 1-5710-107767, TITLE: WINGS, RIGHT WING ANTI-ICING TELESCOPIC DUCT DOOR CU TOUT REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100. 2 L 7 3 4F RT A22WE 2007012900086 20070129 00086 WP 2007 1 29 07FDEA00157 1 20070124 A 5730 ACCESS PANEL DOUG MD10 MD1010F 3022112 WP ZONE 900 CORRODED A FDEA K NONE O O O OTHER OTHER OTHER IN INSP/MAINT 1 SO 25 368FE 46606 RIGHT WING FUEL ACCESS PANEL 634CT IS PITTED ON BOTTOM. FABRICATED NEW FUEL ACCESS PANEL 634CT IAW DAC DRAWING ARB0872 REVISION AP. INSTALLED ON CARD 28C1506-01. 2 L 7 3 4F RT A22WE 2007012900096 20070129 00096 NM 2007 1 29 SWAA070396 1 20070125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R AND 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012900098 20070129 00098 NM 2007 1 29 07FDEA00163 1 20070125 A 5310 DOOR FRAME BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 AFT ENTRY DOOR, DOOR RT FRAME, LWR CORNER HAS WEAR BELOW STOP FITTING INSTALLED REPAIR DOUBLER PER SRM 51-40-3, PG 3 FIG 1, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007012900112 20070129 00112 NM 2007 1 29 SWAA070408 1 20070125 A 3350 101331 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 739GB 29275 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM . 2 L 7 2 4F RT A16WE 2007012900113 20070129 00113 NM 2007 1 29 07FDEA00167 1 20070125 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 420 MAINT ERROR A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 284FE 22621 MAIN DECK FLOORBEAM UPPER CHORD AND INTERCOSTAL ATTACHMENT HAS DOUBLE DRILLED/MISREPAIRED FASTENER HOLES AT BS 420, RB L 12, WL 208 REMOVED AND REPLACED INTERCOSTAL AND REPAIR UPPER CHORD REF SRM 53-10-08 STA 420-440, REF GMM 7-0-1001 PG 1 AND 2, SRM 51-30-02 PG 1 AND 2. TREATED AND PRIMED AREA AND REPAIR REF SRM 51-10-02 PG 1-2. CLASSIFIED AS A MAJOR REP AIR. 2 L 7 3 4F RT A3WE 2007012900134 20070129 00134 NM 2007 1 29 DL76L070057 1 20070125 A 3697 CONNECTOR BOEING 767 767332 1382001 NM GE CF6 CF680C2B6 30025 NE CONTROLLER LOOSE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 171DN 24759 695476 ATB DUE TO NO DUCT PRESSURE FROM LEFT ENGINE AND LEFT PACK WOULD NOT COME ON LINE. OPERATED WITH RIGHT ENGINE AND PACK AND DUCT PRESSURE NORMAL. FOUND CONNECTOR ON PRV CONTROLLER LOOSE. TIGHTENED SAME. RAN ENGINE AND PRESSURE CAME UP. A/C RTS. 2 L 7 2 4F 4 F RT A1NM E13NE 2007012900135 20070129 00135 NM 2007 1 29 F3LA200700010 1 20070122 A 5210 BUSHING AIRBUS A319 A319111 3930336 NM R1 DOOR OUT OF ADJUST A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 945FR 2751 R1 DOOR WOULD NOT LATCH IN OPEN POSITION. RESEATED BUSHING UNDER PUSHBUTTON. PERFORMED OPS CHECK IAW AMM 52-10-00, PAG E 201. CHECKED GOOD. INSPECTED R1 DOOR GUST LOCK. OPERATED PROPERLY. 2 L 7 2 4F RT A28NM 2007012900180 20070129 00180 EA 2007 1 29 SWIA200717751 1 20070105 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 710BR 7852 PAX DOOR HANDLE APPEARS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW PAX DOOR OUTER HANDLE P/N 601R 317 634 PER CRJ200 AMM 52-11-03-400-802. 2 L 7 2 4F RT A21EA 2007012900244 20070129 00244 EU 2007 1 29 SIMA200702603 1 20070124 A 5347 7253742407 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 236AE 23655 4000 340B236 FOUND SEAT TRACK AT BUTT LINE 36L CORRODED. REMOVED AND REPLACED SEAT TRACK, RESTORED PROTECTIVE FINISH, APPLIED CORROS ION PREVENTATIVE IAW EMB SRM 51-40-21, 51-40-22, 51-40-25, 51-40-40 AND 53-70-60. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007012900247 20070129 00247 GL 2007 1 29 SIMA200702601 2 20070125 A 7200 AE3007A13 ENGINE EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL NR 1 ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 21 701MH 4266 187 145162 CAE312784 EXCESSIVE STINK COMING FROM PACKS DURING DESCENT. REMOVED AND REPLACED NUMBER 1 ENGINE IAW EMB 72-00-00. OPERATIONAL A ND LEAKS CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007012900248 20070129 00248 EU 2007 1 29 DHL2007362507 1 20070119 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 47663 84 CABIN FLOOR SEAT TRACK SUPPORT BEAM AND SEAT TRACK FLANGE HAS CORROSION AT RBL 17 BETWEEN FRAME 18 THRU FRAME 38B. CORR OSION REMOVED ON SEAT TRACK FLANGE AN SEAT TRACK SUPPORT BEAM FROM FR 18 THRU FR 38B AT RBL 17 AS PER A300 SRM 51-40-11. FOUND SECTIONS OUT OF LIMITS SEVERAL SPOTS IAW A300 SRM 53-10-00 FIG 612. REMOVED AND REPLACED SEAT TRACK SECTIONS FR OM FR 18.5 TO FR 38B AT RBL 17 IAW A300 SRM 51-40-00, 53-10-10, 51-40-12, 51-10-40, 51-30-30. THIS A PERMANENT REPAIR. 2 L 7 2 4F RT A35EU 2007012900249 20070129 00249 EU 2007 1 29 DHL2007362508 1 20070106 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 47663 84 CABIN FLOOR SEAT TRACK FLANGE BETWEEN FRAME 50 THRU FRAME 53 AT RBL 37 HAS CORROSION. CORROSION REMOVED AT CABIN FLOOR SEAT TRACK FLOOR FLANGE BETWEEN FR 50 THRU FR 53 AT RBL 37 IAW A300 SRM 51-40-11, MAT REMOVED .018" NOMINAL THICKNESS .0 78 REMAINING .060 OUT OF LIMITS IAW A300 SRM 53-10-00 FIG 612. REMOVED AN REPLACED SEAT TRACK SECTION FROM FR 44.5 TO F R 54 AT RBL 37 IAW A300 SRM 51-41-00, 51-10-40, 51-40-12, 51-30-30. THIS A PERMANENT REPAIR. 2 L 7 2 4F RT A35EU 2007012900250 20070129 00250 EU 2007 1 29 07FDEA00187 1 20070126 A 7830 UNKNOWN AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER UNKNOWN A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 665FE 769 ON TAKEOFF AT APPROX, 60 KIAS LT ECAM (W/O CHIME) ALERTED US TO "ENG 2 REVERSER PRESSURIZED" AFTER CONSULTING TO W/MX, C YCLED NR 2. REVERSER ON THEN OFF THIS TEMPORARILY SOLVES THE PROBLEM AS THE THROTTLE ADVANCE ON NR 2 ENG FOR TAXI PROB LEM RESURFACED ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 05FEB07 "MEL 78-30-01-A: ENGIN E (IDENTIFY 1 OR 2) NR 2 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION." NR 2 ENG T /R PER A300-600 AMM 78-31-00-9-05 . PERFORMED T/R SYSTEM FUNCTIONAL TEST PER A300-600 JRH CHP 7-17 OPERATED 10 TIMES A S SPECIFIED IN JRH OPS CHKS GOOD. RNRD PRSOV VALVE PER A300-600 AMM 78-31-05-04-05 T/R SYSTEM FUNCTIONAL CHECK PER JRH 7 2 L 7 2 4F RT A35EU 2007012900252 20070129 00252 NM 2007 1 29 07FDEA00189 1 20070126 A 5320 FLOOR SUPPORT BOEING 727 727233 138408A NM BS 650-710 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 FWD LWR CARGO PIT LT SIDE FLOOR SUPPORT Z-ANGLE HAS MANY AREAS OF CORROSION ON UPPER AND LWR SURFACE, BETWEEN STA 650 SP LICE AND STA 710 SPLICE LBL 24 " STR 26L. REMOVED AND REPLACED Z ANGLE FROM STA 650 TO 710 REF SRM 51-30-02 PGS 4 TO 9 . THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007012900253 20070129 00253 NM 2007 1 29 DHL2007743503 1 20070126 A 5312 BULKHEAD BOEING 727 727225 1384077 NM BS 1183 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 AFT CABIN, BS 1183 BULKHEAD SHOWS CRACK AT VERTICAL FLANGE APPROX BETWEEN RBL 36.8 AND WL 230. COMPLIED WITH REPAIR PRO CEDURES PER B727 SB 727-53-0192, TO INCLUDE: TERMINATION OF CRACK END BY STOP DRILLING (.250" HOLE), AND INSTALLATION O F REPAIR PARTS FROM SB REPAIR KIT P/N 65C34406-14. BARE AREA'S TREATED AND PRIMED AS REQ PER B727 SRM 51-10-2. AREA RE TURNED TO NORMAL. 2 L 7 3 4F A3WE 2007012900258 20070129 00258 EU 2007 1 29 DHL2007362510 1 20070106 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 47663 84 CABIN FLOOR SEAT TRACK AND SEAT TRACK FLANGE AT RBL 37 AN BETWEEN FRAME 40 THRU 50 HAS CORROSION. CORROSION REMOVED AT CABIN FLOOR SEAT TRACK FLANGE BETWEEN FR 40 THRU FR 50 RBL 37 IAW A 300 SRM 51-40-11,NOMINAL THICKNESS .078 MAT REMOVED .020,MAT REMAINING .058. FOUND OUT OF LIMITS IAW A300 SRM 53-10-00 FIG 612. REMOVED AND REPLACED SEAT TRACK SECTION FRO M FR 40 THRU FR 44.5 AT RBL 37 IAW A300 SRM 51-41-00,51-10-40, 51-40-12, 51-30-30. INSTALLED PERMANENT REPAIR. 2 L 7 2 4F RT A35EU 2007012900260 20070129 00260 EU 2007 1 29 DHL2007362512 1 20070122 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 47663 84 CABIN FLOOR SEAT TRACK AND SEAT TRACK FLANGE HAS CORROSION BETWEEN FRAME 18 THRU FRAME 38 AT RBL 37. CORROSION REMOVED FROM FR 38 TO FR 35.5 RBL 37 AY SEAT TRACK FLANGE IAW A300 SRM 51-40-11. NOMINAL THICKNESS .078 MAT REMOVED .004 MAT RE MAINING .074 WITHIN LIMITS IAW A300 SRM 53-10-10 FIG 612. AREA TREATED AN PRIMED IAW A300 SRM 51-40-12. FOUND SEVERAL SPOTS OUT OF LIMITS IAW A300 SRM 53-10-00. REMOVED AND REPLACED SEAT TRACK BETWEEN FR 18 THRU FR 35.5 AT RBL 37 IAW A30 0 SRM 51-41-00, 51-10-40, 51-40-12, 53-10-10. THIS IS A PERMANENT REPAIR. 2 L 7 2 4F RT A35EU 2007012900262 20070129 00262 NM 2007 1 29 QXEA200700107 1 20070123 A 3260 PROXIMITY SENSOR BOMBDR DHC8 DHC8402 1390042 NM MLG DOOR OUT OF ADJUST A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 403QX 4037 LAX FLIGHT NR 2443: ON DESCENT AT 15,000' AND 270 KIAS, THE LANDING GEAR INITIATED ITS OWN EXTENSION (UNCOMMANDED). IT CYCLED DOORS OPEN FOR 2 SECONDS AND THEN CLOSED. NOT KNOWN HOW FAR DOOR OPENED BUT GEAR DID NOT EXTEND. EVENT MARKER P RESSED. MAINTENANCE INTERROGATED CDS. FOUND CURRENT FAULT RGDRLL NEAR GAP TOO LARGE. ADJUSTED RIGHT GEAR DOOR CLOSED PROX SENSOR IAW Q400 MM TASK 32-61-06-830-801 TI ITS NOMINAL NEAR GAP. PERFORMED INDUCTANCE VALUE CHECK OF RIGHT GEAR D OOR CLOSED PROX SENSOR IAW Q400 MM TASK 32-61-00-280-801. INDUCTANCE VALUE CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. FAULT CODE CLEARED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007012900263 20070129 00263 EU 2007 1 29 DHL2007362505 1 20070121 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 47663 84 CABIN FLOOR SEAT TRACK AT SEAT TRACK FLANGE HAS CORROSION BETWEEN FRAME 18 THRU FRAME 37 AT LBL 76. REMOVED CORROSION F ROM FR 18 TO FR 37 LBL 76 IAW A300 SRM 51-40-11, FOUND WITHIN LIMITS TREATED AN PRIMED AN PAINTED IAW A300 SRM 51-40-12. FOUND OUT OF LIMITS FROM FR 21.5- 26.5 IAW A300 SRM 53-10-00 FIG 612. REPLACED SECTION FROM FR 21.5 TO FR 26.5 IAW A3 00 SRM 53-10-10 FIG 724 MAT USED 60-22457 PO NR 031938. FOUND TO BE WITHIN LIMITS FROM FR 26.5 TO FR 37 IAW A300 SRM 53 -10-00 FIG 612 AND TREATED, PRIMED AND PAINTED IAW A300 SRM 57-40-12. THIS IS A PERMANENT REPAIR. 2 L 7 2 4F RT A35EU 2007012900264 20070129 00264 EU 2007 1 29 DHL2007362501 1 20070106 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 47663 84 CABIN FLOOR SEAT RACK AND SEAT TRACK FLANGE HAS CORROSION AT LBL 17 BETWEEN FRAMES 18 THRU FRAME 38B. INSTALLED NEW SEC TION OF SEAT TRACK AT CABIN FLOOR BETWEEN FR 18 THRU FR 38B LBL 17 IAW A300 SRM 53-10-10 AND 51-10-40. 2 L 7 2 4F RT A35EU 2007012900265 20070129 00265 EU 2007 1 29 DHL2007362502 1 20070106 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 47663 84 CABIN FLOOR SEAT RACK AND SEAT TRACK FLANGE HAS CORROSION AT LBL 17 BETWEEN FRAMES 18 THRU FRAME 38B.CORRECTIVE ACTION-I NSTALLED NEW SECTION OF SEAT TRACK AT CABIN FLOOR BETWEEN FR 18 THRU FR 38B LBL 17 IAW A300 SRM 53-10-10 AND 51-10-40. 2 L 7 2 4F RT A35EU 2007012900266 20070129 00266 WP 2007 1 29 DHL2007802503 1 20070118 A 5754 FRAME DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 RT WING CTR L/E FORMER 0.500" CRACK STA XFS 291.500. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE AND FABRIC ATED (2) ANGLE DOUBLER (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007012900268 20070129 00268 EU 2007 1 29 DHL2007362509 1 20070106 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 47663 84 CABIN FLOOR SEAT TRACK FLANGE BETWEEN FRAME 41 THRU FRAME 46 AT LBL 37 HAD CORROSION AROUND THE SCREWS HOLES. REMOVED C ORROSION FROM FR 41 THRU FR 46 LBL 37 IAW A300 SRM 51-40-11, FOUND OUT OF LIMITS IAW A300 SRM 53-10-00 FIG 612. REPLACE D SEAT TRACK FROM FR 40 TO FR 44.5 IAW A300 SRM 51-30-30, 51-10-40, 51-41-00 AND REPLACED SEAT TRACK SECTION FROM FR 44. 5 TO 49.5 IAW A300 SRM 53-10-10 FIG 725, MAT USED IN BOTH SECTIONS 60-22457 PO NR 031938. INSTALLED PERMANENT REPAIR. 2 L 7 2 4F RT A35EU 2007012900269 20070129 00269 WP 2007 1 29 DHL2007802502 1 20070113 A 5320 FLOOR SUPPORT DOUG DC8 DC873 302199C WP BS 132-175 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 MAIN CARGO COMPT NR 5 TRACK LUGS WORN (STA 132.000 - 175.000). REMOVED DAMAGED TRACK SEGMENT AND SPLICES IAW SRM 51-3-0 . CLEANED, TREATED AND PRIMED AREA AND SPLICES IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND REINSTALLED SPLICES IA W SRM 53-2-3 PG 49-50, SRM 51-3-0, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007012900270 20070129 00270 EU 2007 1 29 AWXA200700120 1 20070116 A 5755 D5754148420000 HINGE PIN AIRBUS 320 A320232 3930326 EU ZONE 600 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 602AW 565 SAL - CORROSION ON RIGHT WING NR 2 SPOILER INBOARD HINGE PIN, WS 6132 - WS 6699. REPLACED RIGHT WING NR 2 SPOILER INBOA RD HINGE PIN, WS 6132 - WS 6699 IAW A320 AMM 27-64-42. 2 L 7 2 4F RT A28NM 2007012900271 20070129 00271 EU 2007 1 29 AWXA200700121 1 20070116 A 5755 D5754148420000 HINGE PIN AIRBUS 320 A320232 3930326 EU ZONE 600 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 602AW 565 SAL - CORROSION ON RIGHT WING NR 4 SPOILER OUTBOARD HINGE PIN,WS 9235 - WS 9704. REPLACED RIGHT WING NR 4 SPOILER OUTBO ARD HINGE PIN, WS 9235 - WS 9704 IAW A320 AMM 27-64-42. 2 L 7 2 4F RT A28NM 2007012900274 20070129 00274 SO 2007 1 29 CHQA200700003 1 20070125 A 5240 SEAL EMB 145 EMB145LR 3260212 SO SERVICE DOOR FAILED A CHQA B EMER. DESCENT E VIBRATION/BUFFET CL CLIMB 1 GL 11 571RP 14500827 FLIGHT 6431 - CMH-MCO - UPON LEVELING AT FL340, FLIGHT ATTENDANT CONTACTED FLIGHT DECK AND INFORMED THAT THERE WAS A LOU D "CRACK" FOLLOWED BY AIR RUSHING INTO THE CABIN FROM THE SERVICE DOOR. CONTACTED AIR TRAFFIC CONTROL AND ASKED TO GET A LOWER ALTITUDE TO REDUCE THE PRESSURE ON THE DOOR WHILE RUNNING THE QRH CHECKLIST. DECLARED AN EMERGENCY. AFTER SECU RING THE AIRCRAFT AT THE GATE, IT WAS DETERMINED THAT A TORN DOOR SEAL HAD GIVEN WAY IN THE UPPER LEFT CORNER OF THE SER VICE DOOR, BUT NO STRUCTURAL COMPONENTS WERE DAMAGED. AIRCRAFT WAS FERRIED TO CMH WHERE MAINTENANCE REPAIRED THE DOOR S EAL. 2 L 7 2 4T RT T00011AT 2007012900275 20070129 00275 EU 2007 1 29 AWXA200700123 1 20070125 A 3231 DOOR AIRBUS 320 A320232 3930326 EU NLG FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 619AW 527 MSP - ATB - DURING CLIMB-OUT, THE NOSE LANDING GEAR DOORS WOULD NOT CLOSE. THE CREW RETURNED TO MSP WITHOUT INCIDENTA/C IS AOS IN MSP. 2 L 7 2 4F RT A28NM 2007012900276 20070129 00276 EU 2007 1 29 AWXA200700124 1 20070125 A 3231 DOOR AIRBUS 320 A320232 3930326 EU NLG MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 619AW 527 MSP - ATB - DURING CLIMB-OUT, THE NOSE LANDING GEAR DOORS WOULD NOT CLOSE. THE CREW RETURNED TO MSP WITH OUT INCIDENT. A/C IS AOS IN MSP. 2 L 7 2 4F RT A28NM 2007012900289 20070129 00289 NM 2007 1 29 ASAA0711387 1 20070113 A 3350 873100211 BULB BOEING 737 7372Q8 138448K NM R2 DOOR MISSING A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 741AS 21959 R2 DOOR AND RT OVERWING EXIT "EXIT MARKER" LIGHTS MISSING 1 EACH LAMP. RELAMPED BOTH EMERGENCY LIGHTS AS REQUIRED. 2 L 7 2 4F RT A16WE 2007012900290 20070129 00290 NM 2007 1 29 ASAA0741388 1 20070113 A 2432 08550000 BATTERY BOEING 737 7374Q8 138447Q NM MASTER OVERHEATED A ASAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 02 778AS 25110 FLT CREW AND FLT ATTENDANTS REPORT BURNING PLASTIC SMELL IN CABIN AND COCPIT JUST BEFORE BEGINNING DESCENT. FOUND MAIN BATTERY VOLTAGE LESS THAN 20 VOLTS BATTERY VERY WARM AND SMELLING HOT REPLACED BATTERY. 2 L 7 2 4F RT A16WE 2007012900291 20070129 00291 NM 2007 1 29 ASAA0741389 1 20070116 A 5330 65C357873 SKIN BOEING 737 7374Q8 138447Q NM BS 360-365 DENTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 782AS 25113 PREVIOUS REPAIR ON FUSELAGE IS DENTED. REMOVED THE DAMAGED EXITING REPAIR DOUBLER AND TRIMMED OUT THE DAMAGED AREA OF S KIN FABRICATED AND INSTALLED A SKIN FILLER AND EXTERNAL REPAIR DOUBLER IAW ASA EA 5330 02171 AND AAR EA 11803. 2 L 7 2 4F RT A16WE 2007012900292 20070129 00292 NM 2007 1 29 ASAA0741390 1 20070116 A 5512 657378345 SKIN BOEING 737 7374Q8 138447Q NM HORIZONTAL STAB DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 THE LT HORIZ STAB LE WAS DROPPED DURING INSTALLATION RESULTING IN A SKIN DENT AT TWO EXITING REPAIRS. REMOVED THE TWO E XITING REPAIR DOUBLERS AND FILLERS CUTOUT THE DAMAGED AREA OF SKIN FABRICATED AND INSTALLED A SKIN FILLER AND REPAIR DOU BLER IAW SRM 55 10 01 FIG 201. 2 L 7 2 4F RT A16WE 2007012900295 20070129 00295 WP 2007 1 29 U2RA1535872 1 20070119 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1418 S36R CORRODED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 872SJ 46040 DURING INSPECTION FOUND CORROSION AT AFT CARGO COMPARTMENT AREA STATION 1418 STRINGER 36 RT ON EXTERNAL LOWER SKIN. FOU ND 1" CRACK FWD OF FLIGHT STATION 1418 STRINGER 36 RT EXTERNAL SKIN. COMPLETED FUSELAGE SKIN TEMPORARY EXTERNAL REPAIR AT FS 1418/LONG 36 RT PER FLIGHT VEHICLES CONSULTING, INC DRAWING NUMBER 53-07027-1 AND FAA FORM 8110-3 NR 07027 DATED J ANUARY 22, 2007. 2 L 7 4 4F RT 4A25 2007012900297 20070129 00297 WP 2007 1 29 U2RA1576872 1 20070123 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1380 S36R CRACKED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 872SJ 46040 DURING INSPECTION FOUND CRACK AT AFT CARGO COMPARTMENT STATION 1380 STRINGER 36 RT ON EXTERNAL LOWER SKIN. COMPLETED FU SELAGE SKIN TEMPORARY EXTERNAL REPAIR AT FUSELAGE STATION 1380/LONG 36R PER FLIGHT VEHICLES CONSULTING, INC DRAWING NR 5 3-07027-1 AND FAA FORM 8110-3 NR 07027 DATED JANUARY 22, 2007. 2 L 7 4 4F RT 4A25 2007012900299 20070129 00299 NM 2007 1 29 QXEA200603362 1 20070103 A 5753 FLAP BOMBDR DHC8 DHC8402 1390042 NM RT OUT OF ADJUST A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 412QX 4059 PDX C3 - RIGHT INBOARD FLAP DOES NOT MEET GAP CHECK BETWEEN FLAP AND FLAP SHROUD AT APPROXIMATELY STATION YW48.00. REPA IRED IAW RD 8/4-57-001, DHC-8-400 SRM 51-42-45, 51-42-05. 2 H 7 2 4T RT A13NM 2007012900321 20070129 00321 NM 2007 1 29 AWXA200700115 1 20070122 A 5510 183N1326 BEAM BOEING 757 757225 1384959 NM ZONE 300 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 PHX - CORROSIONS FOUND OUT OF LIMIT ON UPPER BEAM OF LEFT HORIZONTAL STAB TRAILING EDGE BEAM FROM ELEVATOR STA 70 TO ELE V STA 172 IAW B757 SRM 55-10-13-1A AND BOEING MESSAGE 1-276738147-3. CORROSIONS ARE WITHIN LIMITS FOR ACCEPTABLE FERRY FLT. REPAIRED LT STABILZER TRAILING EDGE BEAM UPPER CHORD, STABILIZER STA 70 - STABILZER STA 172 IAW AWA ER 19-5511-070 36-TH1. THIS REPAIR WAS ACCOMPLISHED ON NON-ROUTINE 3984004. 2 L 7 2 4F RT A2NM 2007012900334 20070129 00334 2007 1 29 AALA20070076 4 20070113 A 2250 PSEU BOEING 757 757223 1384957 NM E/E BAY INOPERATIVE A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 606AA 27057 BOS INFLIGHT T586/13JAN AT FLIGHT LEVEL 320, AIRCRAFT YAWED HARD TO THE LEFT. EMERGENCY DOOR MESSAGE ON FORWARD EICAS. MULTIPLE DOOR LIGHTS ON OVERHEAD PANEL. LEFT YAW DAMPER EICAS MESSAGE ILLUMINATED AND REMAINED ON. TURNED OFF LEFT Y AW DAMPER. DURING DESCENT MORE DOOR AND ELECTRONIC COMPARTMENT LIGHTS CAME ON. AUTOBRAKES DISCONNECTED ON APPROACH. A FTER INITIAL YAW AIRCRAFT FLEW NORMALLY. LANDED BOS WITHOUT INCIDENT. REPLACED PROXIMITY SENSOR ELECTRONIC UNIT. REPL ACED RIGHT YAW DAMPER ACTUATOR AND D347 CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007012900335 20070129 00335 EU 2007 1 29 MALA070005 1 20070109 A 3350 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT NO TEST A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 451XJ 340B451 FAILED CAP CHECK PER BFGOODRICH AEROSPACE CMMWO 417868. REPLACED BATTERY PACK. 2 L 7 2 4T RT A52EU 2007012900339 20070129 00339 SO 2007 1 29 SIMA200701913 1 20070116 A 5330 12020334048 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 653AE 13302 4800 145433 DENT WITH GOUGES FOUND ON LEFT REAR FUSELAGE BETWEEN FRAME 78 AND JUNCTION 7 AND STRINGERS 5L AND 7L. PERFORMED CUTOUT OF DAMAGED AREA. FABRICATED FILLER, REPAIR DOUBLER. INSTALLED REPAIR PIECES AND RESTORED PROTECTIVE FINISH IAW EMB SRM 53-32-01. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007012900349 20070129 00349 SW 2007 1 29 AC2A113661 1 20070117 A 5510 NAS660429 BOLT BELL 427 427 1182207 SW PWC PW207 PW207D NE STABILIZER SHEARED E AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 427CU 1333 56047 END OF BOLT SHEARED OFF WITH NUT. 1 G 7 1 3U 3 U R00001RC E42NE 2007012900354 20070129 00354 CE 2007 1 29 CIEA200700001 1 20070124 A 5312 PRESSURE PANEL BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA FUSELAGE CRACKED E CIEA K NONE O OTHER IN INSP/MAINT 1 NM 03 520MC 12720 BB43 DURING INSPECTION OF THE AIRCRAFT TO EVALUATE A PRESSURIZATION LEAK, THE PANEL BEHIND THE REAR SPAR WAS FOUND TO BE CRAC KED IN THE LOWER RADIUS AREA. THERE WAS A CRACK APPROXIMATELY 4 INCHES LONG NEAR THE CENTER LINE OF THE AIRCRAFT. THE AIRCRAFT SKIN WAS NOT FOUND TO BE CRACKED AT THIS TIME. THIS PANEL COVERS THE REAR PART OF THE REAR WING SPAR AS IT PAS SES THROUGH THE FUSELAGE. IT IS NOT BELIEVED THAT THE SPAR ITSELF IS CRACKED AT THIS TIME. 1 L 7 2 4T 4 T A24CE E4EA 2007012900360 20070129 00360 SO 2007 1 29 SIMA200701901 1 20070117 A 2910 3604401003 ACTUATOR EMB 135 EMB135KL 3260302 SO HYD SYSTEM FAILED A SIMA O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 21 818AE 11862 145561 TOTAL LOSS OF NUMBER ONE HYDRAULIC SYSTEM FLUID. REMOVED AND REPLACED NUMBER ONE SYSTEM AILERON MANIFOLD AND RIGHT GROU ND SPOILER ACTUATOR. PERFORMED OPERATIONAL CHECK WITH NO DEFECTS NOTED IAW EMB AMM, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007012900361 20070129 00361 SO 2007 1 29 SIMA200701905 1 20070110 A 5347 14530659005 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 705AE 15855 4800 145184 FOUND LEFT INBOARD SEAT TRACK FROM FRAME 34 TO 43 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AM ERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007012900363 20070129 00363 SO 2007 1 29 SIMA200701912 1 20070108 A 2720 13500816417 CABLE EMB 135 EMB135LR 3260305 SO RUDDER WORN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 705AE 15855 4800 145184 FOUND OUTBOARD RUDDER CABLE WORN AT FRAME 50 PRESSURE SEAL. REMOVED AND REPLACED CABLE IAW EMB AMM 27-21-01. OPERATION AL CHECK GOOD, RETURN AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007012900364 20070129 00364 SO 2007 1 29 SIMA200701910 1 20070109 A 2730 14520456405 CONTROL CABLE EMB 135 EMB135LR 3260305 SO ELEVATOR WORN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 705AE 15855 145184 FOUND RIGHT SIDE ELEVATOR CABLE WORN AT PRESSURE SEALS JUST AFT OF VERTICAL LEADING EDGE. REMOVED AND REPLACED ELEVATOR CABLE IAW EMB AMM 27-31-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007012900365 20070129 00365 SO 2007 1 29 SIMA200701911 1 20070109 A 2720 13500816415 CONTROL CABLE EMB 135 EMB135LR 3260305 SO RUDDER WORN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 705AE 15855 4800 145184 FOUND RIGHT RUDDER CABLE WORN AFT OF FRAME 50 PRESSURE SEAL. REMOVED AND REPLACED CABLE IAW EMB AMM 27-21-01. OPERATIO NAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007012900366 20070129 00366 SO 2007 1 29 SIMA200701906 1 20070110 A 5347 13500439007 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 705AE 15855 4800 145184 FOUND LEFT INBOARD SEAT TRACK AT FRAME 19 TO 25 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06 AND AMER ICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007012900368 20070129 00368 SO 2007 1 29 SIMA200701908 1 20070109 A 5320 14521725012 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 705AE 15855 4800 145184 FOUND FORWARD SERVICE DOOR SILL CORRODED AT FRAME 20. REPAIRED FORWARD SILL IAW EMB SRM 53-21-10, FIGURE 204. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007012900369 20070129 00369 SO 2007 1 29 SIMA200701904 1 20070116 A 5347 13500438001 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 705AE 15855 4800 145184 FOUND RIGHT FORWARD INBOARD SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGL E ENGINEERING TECHINCAL NOTICE EM-53-110R1. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007012900370 20070129 00370 SO 2007 1 29 SIMA200701902 1 20070118 A 3350 110049 CHARGER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 667GB 9473 690 145784 NUMBER 2 EMERGENCY LIGHT POWER SUPPLY INOPERATIVE. REMOVED AND REPLACED NUMBER 2 EMERGENCY LIGHTING POWER SUPPLY IAW AM ERICAN EAGLE WORK CARD 33-700-19. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007012900371 20070129 00371 NM 2007 1 29 AWXA200700078 1 20070107 A 5755 654645262 SKIN BOEING 737 7373G7 1384595 NM ZONE 500 DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - LEFT WING NR 4 SPOILER, BOTTOM SKIN DELAMINATED, WS 149 - WS 156.5. REPAIRED LEFT WING NR 4 SPOILE R, BOTTOM SKIN, WS 149 - WS 156.5 IAW B737-300 SRM 51-70-10-02R, FIGURE 207. 2 L 7 2 4F RT A16WE 2007012900372 20070129 00372 NM 2007 1 29 AWXA200700079 1 20070109 A 5315 654583468 FLOORBEAM BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR -E/E BAY CABIN FLOORBEAM LOWER STRAP CRACKED, BS 324, RBL 24. REPAIRED E/E BAY CABIN FLOORBEAM LOWER STRAP, BS 324, RBL 24, IAW B737-300 SRM 53-10-51-2R4, FIGURE 201, DETAIL VI. 2 L 7 2 4F RT A16WE 2007012900375 20070129 00375 EU 2007 1 29 N93A20070115 2 20070115 A 7250 TURBINE GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU NR 1 ENGINE DAMAGED E N93A A UNSCHED LANDING E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 13 440QS 4025 85051 DURING CLIMBOUT A STRONG SHUDDER WAS FELT THROUGHOUT THE AIRFRAME. MAINTENANCE DISCOVERED SPARKS COMING FROM NR 1 ENGIN E EXHAUST. FURTHER INVESTIGATION DETERMINED DAMAGE TO TURBINE SECTION. CAUSE TO BE DETERMINED AT TEARDOWN. 2 L 7 2 4F 4 F RT A12EA E25NE 2007012600371 20070126 00371 EA 2007 1 26 SWIA200717739 1 20070104 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 969SW 7876 STA 280 LBL9 UPPER FRAME HAS A CRACK, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FILLER ANGLE REPAIR SPLICE ANGLES AND TWO -57 CLIPS FS 280 UPPER FLOORBEAM LBL9 AS PER REO 601R-53-11-138 SHEET 1-3 NOTES 1-10. 2 L 7 2 4F RT A21EA 2007012600372 20070126 00372 EA 2007 1 26 SWIA200717740 1 20070104 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 969SW 7876 RBL9 LOWER FRAME CRACKED FS 280, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS TO RBL9 LWR FS 280 PER CR J200 REO 6011R-53-11-171 STEP 6, 7, 8, 12, 13. 2 L 7 2 4F RT A21EA 2007012900002 20070129 00002 SO 2007 1 29 LR7A07003 1 20070117 A 5340 342603 ATTACH ANGLE LKHEED 382 382G 526414U SO FS 597 WL 230 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 652 4698 DURING SCHEDULED B 2 CHECK PER JOB CARD HB5302, FOUND INTERCOSTAL ATTACH ANGLE TO CENTER WING REAR WEB CRACKED AT FS 597 , WL230, RBL16. REPLACED ANGLE IAW SMP583 51-70, AND DWG 342603. 2 H 7 4 4T A1SO 2007012900020 20070129 00020 NM 2007 1 29 AWXA200700119 1 20070122 A 2751 FLAP SYSTEM BOEING 737 7373G7 1384595 NM TE FLAPS MALFUNCTIONED A AWXA L A ABORTED APPROACH UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 WP 28 157AW 23779 PHX - EL - ON APPROACH TO SAN THE CREW NOTICED A SPLIT FLAP INDICATION IN THE 2 AND 5 POSITION. THE FLAPS WOULD NOT MOV E TO THE SELECTED POSITION. THE CREW DECIDED TO DIVERT TO LAX TO USE THE LONGER RUNWAYS. THE CREW DECLARED AN EMERGENC Y AND LANDED IN LAX. THE LANDING WAS UNEVENTFUL, THE PASSENGERS DID NOT BRACE. THE A/C IS AOS AT THIS TIME. 2 L 7 2 4F RT A16WE 2007012900030 20070129 00030 SO 2007 1 29 SWIA200717758 1 20070110 A 3350 FUSE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS FAILED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 224SW 120294 FORWARD CEILING EMERGENCY LIGHT INOP. REPLACED FUSE AND FORWARD CEILING EMERGENCY LIGHT HOUSING. OPERATIONAL CHECKS GO OD. 2 L 7 2 4T RT A31SO 2007012900037 20070129 00037 NM 2007 1 29 UPS07448944 1 20070109 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO BS 800-820 S35R FOUND CRACKED AS MARKED. FWD CARGO COMPT BS 742 TO BS 830 STR 35R REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007012900045 20070129 00045 NM 2007 1 29 SWAA070358 1 20070125 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING AT FWD CABIN. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007012900053 20070129 00053 NM 2007 1 29 SWAA070366 1 20070125 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007012900068 20070129 00068 NM 2007 1 29 SWAA070381 1 20070125 A 5322 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007012900094 20070129 00094 NM 2007 1 29 SWAA070395 1 20070125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012900095 20070129 00095 NM 2007 1 29 07FDEA00162 1 20070125 A 5320 65489616 WEB BOEING 727 727233 138408A NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 MAIN DECK LAV COMP FLOOR WEB IS CORRODED AS MARKED BS 304-342, RBL 41-62, WL 208 REMOVED CORROSION, MATERIAL LOSS BEYOND LIMITS .015, TRANSFERS FASTENER HOLES FOR NEW LAV PANELS. INSTALLED NEW LAV PANEL, CLASSIFIED AS A MINOR REPAIR, REF S RM 51-10-6 PG 1, 4, 5 SRM 51-30-5 PG 5 AND 51-30-02 PG 3. 2 L 7 3 4F RT A3WE 2007012900097 20070129 00097 NM 2007 1 29 SWAA070397 1 20070125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012900106 20070129 00106 NM 2007 1 29 SWAA070403 1 20070125 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007012900119 20070129 00119 WP 2007 1 29 07FDEA00173 1 20070126 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 879 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 FWD CARGO COMPT BILGE MODERATE CORROSION ON CAP FRAME AT STA 879 LONG NR 50 LT TO LONG NR 51 LT. REMOVED EXIST REPAIR S PLICE FOR ACCESS, REMOVED CORROSION, MTL REMOVED IS OUT LIMITS. INSTALLED A REPAIR CAP SECTION BTWN LONG NR 47 LT TO LO NG NR 47 RT IAW SRM 53-30-00 VOL 1 FIG 8. INSTALLED A REPAIR SPLICE BTWN LONG NR 48 RT AND LONG NR 47 RT IAW SRM 53-30- 00 VOL 1 FIG 8. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01646 AND SRM 53-30-00 VOL1 FIG 8. 2 L 7 3 4F A22WE 2007012900133 20070129 00133 NM 2007 1 29 DLM88070056 1 20070125 A 3610 CLAMP DOUG MD88 MD88 3023688 NM GE CF6 CF680C2B6 30025 NE AUG VALVE LOOSE A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 27 900DE 53372 695476 AFTER T/O OUT OF LGA. GOT A TAIL COMPARTMENT TEMP HIGH ANNUNCIATOR. RAN QRH AND LIGHT EXTINGUISHED WHEN LEFT THROTTLE RETARDED TO IDLE. DIVERTED TO JFK. REPOSITION CLAMPS ON LT AUGMENTATION VALVE, RETORQUE SAME. AS PER MM, PERFORM PROC 36-00-00201. AUG VALVE AND ANTI-ICE SYSTEM CHECK, PERFORM HIGH POWER RUN-UP PER 72-00-00-501. RUN-UP CHECK GOOD. 2 L 7 2 4F 4 F RT A6WE E13NE 2007012900161 20070129 00161 2007 1 29 SWAA070254 4 20070118 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007012900163 20070129 00163 2007 1 29 SWAA070256 4 20070118 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007012900169 20070129 00169 NM 2007 1 29 SWAA070247 1 20070118 A 2121 6454051 FAN BOEING 737 7373H4 1384600 NM E&E BAY FAULTY A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 29 631SW 27706 CREW REPORTED A SMELL ON CLIMB-OUT, GASPER FAN AND RECIRC FAN TURNED OFF, SMELL DISSIPATED. REMOVED AND REPLACED RECIRC FAN PER MM. 2 L 7 2 4F RT A16WE 2007012900171 20070129 00171 NM 2007 1 29 SWAA070249 1 20070118 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMIESCENT STRIP MISSING AT ROW 7 ABC. INSTALLED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 2007012900175 20070129 00175 EA 2007 1 29 SWIA200717747 1 20070105 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 710BR 7852 RBL9 LOWER FRAME CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS AS PER CRJ200 REO 601R-53-11-171 REV C. 2 L 7 2 4F RT A21EA 2007012900178 20070129 00178 EA 2007 1 29 SWIA200717750 1 20070105 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 710BR 7852 PAX DOOR AFT DRAG ANGLE IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FABRICATED ANGLE SECTION AND SERVIC EABLE SPLICE ANGLES PER CRJ200 REO 601R 52-11-513 REV 'A'. 2 L 7 2 4F RT A21EA 2007012900207 20070129 00207 EU 2007 1 29 TRAX200700069 1 20070109 A 5753 BRACKET AEROSP ATR72 ATR72212 8680945 EU TE FLAP BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 635AS 372 LT WING AT RIB 13 UPPER FLAP BEAM OMEGA BRACKET BROKEN AT LOWER SECTION. 2 H 7 2 4T RT A53EU 2007012900251 20070129 00251 NM 2007 1 29 07FDEA00188 1 20070126 A 5310 DOOR FRAME BOEING 727 727233 138408A NM SERVICE DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 AFT LT SERVICE DOOR OPENING CUTOUT FWD FRAME INBD FLANGE HAS 3 AREAS OF WEAR, LOCATED BETWEEN GUIDE ARM AND TOP STOP. INSTALLED NEW FRAME SECTION AND COVER PLATE REF SRM 51-30-2 PAGE 2 ITEM 4B, AND BOEING DRW 65-60316. THIS IS CLASSIFIE D AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007012900254 20070129 00254 NM 2007 1 29 HALA0700035 1 20070122 A 2120 UNKNOWN BOEING 767 767300 1385204 NM PWA 4060 PW4060 52119 NE CABIN ODOR A HALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 13 581HA 28141 MAY HAVE INJESTED A BIRD ON TAKEOFF BURNED FEATHERS ODOR, TURNED OFF LEFT PACK AND ODOR WENT AWAY. ACCOMPLISHED FIMS 71 -05-00 FIGURE 101 AND 102 EXAMINE NR 1 ENGINE PER FIM. FOUND NO DAMAGE, OK FOR SERVICE. ODOR CHECK LT PACK NO ABNORMAL ODOR NOTED. ACCOMPLISHED BIRD STRIKE INSP PER AMM05-51-18-212-001. 2 L 7 2 4F 4 F RT A1NM E24NE 2007012900293 20070129 00293 NM 2007 1 29 SWAA070250 1 20070118 A 5311 6517684 FRAME BOEING 737 7373H4 1384600 NM BS 303 S14L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 12Y CHECK, FOUND FWD ENTRY DOOR CUTOUT FRAME CRACKED AT BS 303.9, STR 14L. REMOVED AND REPLACED FRAME SECTION PER EA. 2 L 7 2 4F RT A16WE 2007012900322 20070129 00322 NM 2007 1 29 AWXA200700116 1 20070122 A 5510 182N1101 STRUCTURE BOEING 757 757225 1384959 NM ZONE 300 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 PHX - MAJOR REPAIR - CORROSIONS FOUND OUT OF LIMIT ON UPPER CHORD OF LEFT HORIZONTAL STAB TRAILING EDGE REAR SPAR FROM S TAB STA 69.0 TO STAB STA 204.0 IAW B757 SRM 55-10-10-1A AND BOEING MESSAGE 1-27638147-3, CORROSIONS ARE WITHIN LIMITS FO R ACCEPTABLE FERRY FLIGHT. REPAIRED LEFT HAND STABILZER TRAILING EDGE REAR SPAR UPPER CHORD, STABILIZER STA 69 - STABIL ZER STA 281 I/A/W AWA ER 19-5510-07034-ES2. 2 L 7 2 4F RT A2NM 2007012900323 20070129 00323 NM 2007 1 29 AWXA200700118 1 20070124 A 5330 6555074 SKIN BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 PHX - MAJOR REPAIR - A CRACK FOUND ON EXTERIOR SKIN AT RIGHT BS 219.8, UPPER OUTBOARD CORNER OF COPILOT NR 1 WINDOW. RE PAIRED EXTERIOR SKIN AT RIGHT BS 219.8, UPPER OUTBOARD CORNER OF COPILOT NR 1 WINDOW AND COMPLIED WITH HFEC INSPECTION I AW B737 SRM 53-10-01-2R. 2 L 7 2 4F RT A16WE 2007012900324 20070129 00324 EA 2007 1 29 REXA200700001 1 20070106 A 4920 38004883 APU CNDAIR CL600 CL6002B19 1900309 EA FLAMED OUT A REXA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 25 8797A 9732 155 7797 DURING APU START WHILE SITTING AT THE GATE IN YUL, THE APU OVERTEMPED AND SHUTDOWN. SMOKE ENTERED THE CABIN THROUGH THE ENVIRONMENTAL CONTROL SYSTEM. THE FLIGHT CREW CALLED FOR CFR AND DEPLANED THE PASSENGERS. CFR FOUND NO INDICATION OF FIRE. THE APU WAS DEFERRED AND THE AIRCRAFT RELEASED FOR FLIGHT. MAINTENANCE TROUBLESHOT THE APU AT MSP. THE APU WAS INSPECTED AND OPS CHECKED NORMAL. IT IS BELIEVED THAT AN INCOMPLETE APU START CAUSED THE SMOKE. 2 L 7 2 4F RT A21EA 2007012900337 20070129 00337 NM 2007 1 29 AWXA200700077 1 20070102 A 5320 65496171 WEB BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - AFT CARGO COMPARTMENT DOOR CUT OUT TORQUE BOX WEB CRACKED, BS 794, S23R. REPLACED AFT CARGO COMPAR TMENT DOOR CUT OUT TORQUE BOX WEB, BS 794, S23R IAW B737-300 SRM 51-40-02 AND BOEING DRAWING 65-49617. 2 L 7 2 4F RT A16WE 2007012900353 20070129 00353 NM 2007 1 29 ASMF200701006 1 20070123 A 4920 38003681 INLET DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE APU OBSTRUCTED W ASMF K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 23 169PL 2268 53175 CAPTAIN REPORTED SMOKE ODOR IN THE CABIN. AIR CONDITIONING SYSTEM WAS SHUTDOWN AND APU DOORS WERE CHECKED, DETECTING A P LASTIC IN THE APU INLET. PLASTIC WAS REMOVED AND WATER SEPARATORS WERE REPLACED IAW MM 21-20-2, TESTED CORRECT. DURING B OARDING, CAPTAIN REPORTED AGAIN SMOKE ODOR IN THE CABIN, SO THE AIRCRAFT WAS SENT TO THE HANGAR. APU, WATER SEPARATORS A ND PRIMARY AND SECONDARY HEAT EXCHANGERS OF BOTH SYSTEMS WERE REPLACED IAW MM 49-10-00, 21-20-2 AND 21-51-02, TESTED COR RECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007012900359 20070129 00359 SO 2007 1 29 SIMA200701903 1 20070115 A 7500 346000731 DUCT EMB 145 EMB145LR 3260212 SO BLEED AIR SYS BLOWN A SIMA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 21 614AE 17728 145086 HEARD LOUD POP FOLLOWED BY EICAS BLEED 1 LEAK MESSAGE, LAVATORY SMOKE MESSAGE, BAGGAGE SMOKE MESSAGE, DISCHARGED BAGGAGE EXTINGUISHER - CABIN/FLIGHT DECK FILLED WITH SMOKE. EMERGENCY DECLARED AND RETURNED TO ORD. POST INSPECTION FOUND BLE ED DUCT DISCONNECTED AND DAMAGE TO THE INSULATION UNDER CABIN FLOOR. REMOVED AND REPLACED DUCT, BLANKETS AND O-RINGS IA W EMB AMM. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007012900373 20070129 00373 NM 2007 1 29 AWXA200700080 1 20070114 A 5340 692655552 ATTACH ANGLE BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - S16L INTERCOSTAL OUTBOARD ATTACH ATTACH ANGLE CRACKED BS 348.2 TO BS 351.2. REPLACED S16L INTERCOSTAL OUTBOARD AT TACH ATTACH ANGLE BS 348.2 TO BS 351.2 IAW AWA ER 03-5312-07013-HF2. 2 L 7 2 4F RT A16WE 2007012900374 20070129 00374 NM 2007 1 29 AWXA200700081 1 20070114 A 5340 69165096 ATTACH ANGLE BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - S16L INTERCOSTAL INBOARD ATTACH ANGLE CRACKED BS 348.2 TO BS 351.2. REPLACED S16L INTERCOSTAL INBO ARD ATTACH ANGLE BS 348.2 TO BS 351.2 IAW AWA ER 03-5312-07013-HF2. 2 L 7 2 4F RT A16WE 2007012900379 20070129 00379 NM 2007 1 29 AWXA200700084 1 20070109 A 5340 146N51961 ATTACH ANGLE BOEING 757 7572G7 1384963 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 909AW 24522 MCN - MAIN CABIN INTERCOSTAL UPPER ATTACH ANGLE CRACKED, BS 1520 - BS 1540, BL 0. REPLACED MAIN CABIN INTERCOSTAL UPPER ATTACH ANGLE CRACKED, BS 1520 - BS 1540, BL 0 IAW B737-300SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007012900380 20070129 00380 NM 2007 1 29 AWXA200700085 1 20070109 A 5320 D53471124200 SHEAR PLATE AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 829AW 1563 SAL - MAJOR REPAIR - CORROSION ON MAIN CABIN SHEAR PLATE, FS 69 - FS 70, S23R. REPLACED MAIN CABIN SHEAR PLATE, FR 69 - FR 70, S23R IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007012900381 20070129 00381 NM 2007 1 29 AWXA200700086 1 20070109 A 5320 D53471124200201 SHEAR PLATE AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 829AW 1563 CORROSION ON SHEAR PLATE LOCATED BETWEEN FS 69 TO 70 AND STRG 23 LT. CORROSION ON MAIN CABIN SHEAR PLATE, FS 69 - FS 7 0, S23L. REPLACED MAIN CABIN SHEAR PLATE, FS 69 - FS 70, S23L IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007012900392 20070129 00392 CE 2007 1 29 DXTA200701879 1 20070125 A 3150 WARNING SYSTEM CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE COCKPIT UNKNOWN E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 825QS 5600655 DURING TAKEOFF ROLL , AMBER (IAS) COMPARATOR MESSAGE APPEARED ON PFD. TAKEOFF WAS ABORTED IAW CHECKLIST PROCEDURES. (IA S) MESSAGE EXTINGUISHED AND DID NOT REAPPEAR. NO SNOW OR ICE WAS FALLING PRIOR TO OR DURING TAKEOFF ROLL. THE PILOTS AN D COPILOTS AIRSPEED SYSTEMS OPERATIONALLY CHECKED NORMAL IN ACCORDANCE WITH CESSNA 560 MAINTENANCE MANUAL CHAPTER 34-11- 26. ALL WORK PERFORMED BY DUNCAN AVIONICS - TEB CRS XJRR155L 2 L 7 2 4F 4 F RT A22CE E00053EN 2007013000003 20070130 00003 NM 2007 1 30 KCSA071049 1 20070125 A 5412 FIRESHIELD BOEING 747 747209F 1384800 NM NR 4 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 NR 4 PYLON LOWER SKIRT INBOARD SIDE FIRESHIELD IS CHAFED AT NAC STA 180 TO 250. 2 L 7 4 4F RT A20WE 2007013000004 20070130 00004 SO 2007 1 30 C2XA07CL013 1 20070125 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY MALFUNCTIONED A C2XA B EMER. DESCENT N FALSE WARNING DE DESCENT 1 SW 27 13988 16099 145265 CLE FLIGHT 2913 THE CREW REPORTED A LAV SMOKE INDICATION INFLIGHT. NO FIRE OR SMOKE WAS PRESENT. THE AIRCRAFT LANDED W ITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007013000005 20070130 00005 NM 2007 1 30 QXEA200700110 1 20070126 A 3097 697071272 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM PROP DEICE SYS BROKEN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 413QX 4060 GEG FLIGHT NR 2439: PROP DEICE CAUTION ON TAXI OUT. MAINTENANCE FOUND TERMINAL END OF HARNESS NR 5 BLADE, NR 2 PROP AT BACK PLATE BROKEN. REPLACED HARNESS IAW AMM 61-00-06, PAGES 420-426. FUNCTIONAL TESTS GOOD. AIRCRAFT RETURNED TO SERV ICE. 2 H 7 2 4T RT A13NM 2007013000008 20070130 00008 NM 2007 1 30 ASAA0741418 1 20070125 A 5753 6546434370 SKIN BOEING 737 737490 1384715 NM T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 RIGHT I/B AFT FLAP UPPER SKIN DENTED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-70-1 0. 2 L 7 2 4F RT A16WE 2007013000012 20070130 00012 EA 2007 1 30 REXA200700012 1 20070128 A 2750 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS UNKNOWN A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8409N 7409 FLAPS FAILED AT ZERO DEGREES ON APPROACH. LANDING UNEVENTFUL. COMPLIED WITH AD2006-12-21, RESET FLAPS AND MONITORING F OR 72 HOURS. 2 L 7 2 4F RT A21EA 2007013000013 20070130 00013 NM 2007 1 30 0700396732 1 20070108 A 5350 SKIN BOEING 747 747251B 1384892 NM TAIL CONE DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 632US 23112 DURING "L" CHECK WHILE REPLACING DAMAGED TAIL CONE FOUND SKIN PANEL WITH ELONGATED FASTENER HOLES AT BS 2701-2742 SECTIO N 48. REPAIRED PER EA 67-208732. 2 L 7 4 4F A20WE 2007013000014 20070130 00014 NM 2007 1 30 0700276740 1 20070116 A 5310 TENSION TIE BOEING 747 747251F 1384898 NM BS 800 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 640US 23888 DURING "M" CHECK, FOUND CRACKS IN FRAME TENSION TIE AT LT FORWARD AND RT AFT CHANNELS AT BS 800. REPAIRED PER EA 67-207 924. 2 L 7 4 4F A20WE 2007013000016 20070130 00016 NM 2007 1 30 0700296740 1 20070116 A 5310 TENSION TIE BOEING 747 747251F 1384898 NM BS 820 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 640US 23888 DURING "M" CHECK, FOUND CRACKS IN TENSION TIE RT FRAME DOUBLER AND LT FRAME AT BS 820. REPAIRED PER EA 67-207929. 2 L 7 4 4F A20WE 2007013000017 20070130 00017 NM 2007 1 30 0700306740 1 20070116 A 5310 TENSION TIE BOEING 747 747251F 1384898 NM BS 780 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 640US 23888 DURING "M" CHECK, FOUND CRACK IN TENSION TIE LT FORWARD CHANNEL AT BS 780. REPAIRED PER EA 67-208610. 2 L 7 4 4F A20WE 2007013000018 20070130 00018 NM 2007 1 30 0700316740 1 20070117 A 5315 FLOORBEAM BOEING 747 747251F 1384898 NM BS 380 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 640US 23888 DURING "M" CHECK, FOUND FASTENER HOLES WITH CRACK AND SHORT EDGE MARGIN ON UPPER DECK FLOORBEAM AT BS 380. REPAIRED PER EA 67-208611. 2 L 7 4 4F A20WE 2007013000020 20070130 00020 NM 2007 1 30 0700346740 1 20070116 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 480 S11L CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 640US 23888 DURING "M" CHECK, FOUND CRACK IN FRAME WEB AT BS 480 STRINGER 11L. REPAIRED PER EA 67-208614. 2 L 7 4 4F A20WE 2007013000021 20070130 00021 NM 2007 1 30 0700326740 1 20070115 A 5310 TENSION TIE BOEING 747 747251F 1384898 NM BS 840 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 640US 23888 DURING "M" CHECK, FOUND CRACK IN LT TENSION TIE FORWARD CHANNEL AT BS 840. REPAIRED PER EA 67-208612. 2 L 7 4 4F A20WE 2007013000022 20070130 00022 NM 2007 1 30 0700356740 1 20070111 A 5412 FRAME BOEING 747 747251F 1384898 NM NR 1 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 640US 23888 DURING "M" CHECK, FOUND CRACK IN NR 1 PYLON REAR ENGINE MOUNT BULKHEAD FRAME WEB. REPAIRED PER EA 67-208618. 2 L 7 4 4F A20WE 2007013000023 20070130 00023 GL 2007 1 30 C2XA07CL015 2 20070126 A 7200 ENGINE EMB 145 EMB145EP 3260221 SO ALLSN AE300 AE3007A GL CONTAMINATED A C2XA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14942 145037 CLE FLIGHT 2965 THE CREW REPORTED CLIMBING THRU 7500 FT. THE F/A REPORTED SMOKE FILLING THE CABIN. THE AIRCRAFT RETURN ED TO CLEVELAND AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RAN ENGINES AND PACKS UNTIL SMOKE DISSIPATED. F OUND CAUSE TO BE DEICE FLUID IN ENGINES. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007013000024 20070130 00024 NM 2007 1 30 07FDEA00191 1 20070127 A 5320 FLOOR SUPPORT BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 54431 21102 AFT PIT ALONG LEFT SIDE OF S-29L FROM STA 950F-970 HAS SURFACE CORROSION REMOVED FLOOR SUPPORT FOR ACCESS IAW SRM 51-30- 2. REMOVED CORROSION IAW SRM 51-10-6. AREA FOUND WITHIN LIMITS FOR STRAP REPAIR IAW SRM 27-53-023. FABBED STRAP IAW S R 27-53-023, MATERIAL USED TO MAKE STRAP IS 7075-T6-.071, BATCH NR 1119665. LOCATED AND DRILLED IAW SRM 51-30-5. TREAT ED AND PRIMED AREA IAW SRM 51-10-2. INSTALLED STRAP IAW SR 27-53-023. 2 L 7 3 4F RT A3WE 2007013000027 20070130 00027 NM 2007 1 30 CALA0700034 1 20070127 A 5320 147A5660Y22 INTERCOSTAL BOEING 737 737724 13844BY NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27733 28800 INSPECTION FOUND INTERCOSTAL CORRODED AT STA 947.5-967, RBL 30-45. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51- 40-02 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007013000029 20070130 00029 NM 2007 1 30 UPS07448969 1 20070102 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FX STA 1171 FAIRING SUPPORT FRAME FOUND CORRODED AT RBL 12 AS MARKED. FX BS 1171 FAIRING SUPPORT FRAM E UPPER CHORD REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007013000030 20070130 00030 NM 2007 1 30 UPS07448970 1 20070108 A 5313 65B046561 STRINGER SPLICE BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 1732-1738 STR 2L STRINGER END SPLICE FOUND CORROSION. M/D BS 1732-1748 STR 2L STRINGER SPLICE REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007013000031 20070130 00031 NM 2007 1 30 UPS07448971 1 20070109 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT STRINGER FOUND CRACK AT STA 945 S35R. FWD CARGO COMPT BS 930 TO BS 950 STR 35R STRING ER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007013000033 20070130 00033 NM 2007 1 30 UPS07448973 1 20070111 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C AFT CARGO COMPT STRINGER FOUND CORRODED AT STA1640 S40R. AFT CARGO COMPT BS 1632 TO BS 1648 STR 40R S TRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007013000034 20070130 00034 NM 2007 1 30 UPS07448974 1 20070105 A 5320 141U11076 BEAM BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C NWW RT TUNNEL BS 300 VERTICAL BEAM WEB WL 190 STAND OFF HOLE FOUND CRACKED. NWW RT TUNNEL BS 300 VERT ICAL BEAM WEB REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007013000036 20070130 00036 NM 2007 1 30 UPS07448986 1 20070111 A 5320 69B0280015 TIE CLIP BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 1960 STR 3L FRAME ATT TIE CLIP FOUND CRACK. M/D BS 1960 STR 3L FRAME ATT TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007013000037 20070130 00037 NM 2007 1 30 UPS07448987 1 20070110 A 5320 69B142679 SUPPORT FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 1000 RBL 33 SEAT TRACK SUPPORT FOUND CRACKED. M/D BS 1000 RBL 33 SEAT TRACK SUPPORT FITTING RE PLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007013000039 20070130 00039 NM 2007 1 30 UPS07448989 1 20070106 A 5313 65B1180513 STRINGER SPLICE BOEING 747 747123 1384873 NM FUSELAGE SCRATCHED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FX - MEC LT TUNNEL STA 300 S28AL STRINGER SPLICE FOUND SCRATCH MARK. FX - MEC LT TUNNEL BS 300 STR 28 AL STRINGER SPLICE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007013000040 20070130 00040 SO 2007 1 30 C2XA07BT007 1 20070122 A 2120 M1075066242 THERMAL SWITCH EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 16559 145603 EWR LOG SQUAWK DURING FLIGHT IN ICING CONDITIONS A BURNING SMELL IS PRESENT IN COCKPIT WHEN THE ANTI ICE SYSTEM TURNS ON . REMOVED AND REPLACED SWITCHES S0285 AND S0200 IAW EMB145 AMM 21-26-04. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007013000043 20070130 00043 NM 2007 1 30 UPS07448992 1 20070109 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D - BS 2320 STR 18-19L FRAME FOUND CRACK. M/D BS 2320 STR 18-19L FRAME REPAIRED AS PER SRM 53-10-04 FIG 4. 2 L 7 4 4F A20WE 2007013000044 20070130 00044 WP 2007 1 30 UPS07848975 1 20070103 A 5313 4610355 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C2 CORROSION OUT OF LIMITS ON END FITTING AT STA 70 L35R. REMOVED AND REPLACED LONGERON END FITTING AT STA 70 L35R IAW SRM 51-1-21, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007013000047 20070130 00047 WP 2007 1 30 UPS07848978 1 20070104 A 5320 577384444 ATTACH ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD TO LONGERON INTERCOSTAL ATTACH ANGLE CRACKED AT STA 1766 L6L. REMOVED, FABRICA TED AND INSTALLED ATTACH ANGLE IAW SRM 51-1-21, 51-3-2, 51-1-20D AND DWG 5773844. 2 L 7 4 4F RT 4A25 2007013000049 20070130 00049 WP 2007 1 30 UPS07848981 1 20070111 A 5713 3704840502 FITTING DOUG DC8 DC871F 302199D WP WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 NR 2 MAIN FUEL TANK HAS STRINGER END FITTING CRACKED AT STRINGER 55 JUST INBOARD XRS74. REMOVED AND REPLACED STRINGER END FITTING IAW SRM 51-1-20D, 51-3-0 AND 51-01-15. 2 L 7 4 4F RT 4A25 2007013000051 20070130 00051 NM 2007 1 30 KCSA071052 1 20070127 A 5315 FLOORBEAM BOEING 747 747209F 1384800 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 UPPER DECK FLOORBEAM UPPER CHORD HAS CORROSION AT STA 520, BL 0. 2 L 7 4 4F RT A20WE 2007013000053 20070130 00053 NM 2007 1 30 KCSA071054 1 20070128 A 5312 BULKHEAD BOEING 747 747209F 1384800 NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 BS 2360 PRESSURE BULKHEAD WEB DENTED AT LBL 32, WL 320. 2 L 7 4 4F RT A20WE 2007013000054 20070130 00054 NM 2007 1 30 KCSA071055 1 20070128 A 5312 BULKHEAD BOEING 747 747209F 1384800 NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 BS 2360 PRESSURE BULKHEAD WEB DENTED AT RBL 72, WL 225. 2 L 7 4 4F RT A20WE 2007013000056 20070130 00056 EU 2007 1 30 07FDEA00193 1 20070127 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 CRACK IN FLOORBEAM UNDER CLS ADAPTER AT FRAME 34 BETWEEN TRACK 3L AND 4L (SEEN FROM FWD PIT). REMOVED AND REINSTALLED F LOORPANEL FOR FOM IAW A310-200 AMM SUPP 53-10-25-4. REMOVED AND REINSTALLED CLS ADAPTER IAW A310-200 SRM 51-40-21. REM OVED CRACK IAW A310 SRM SUPP 53-10-15 FIG 201 SHT 2. FABRICATED, LOCATED, AND DRILLED REPAIR ANGLES IAW A310-SRM SUPP 5 3-10-15. INSTALLED REPAIR IAW A310 SRM 51-40-21. REPROTECTED AREA IAW A310 SRM 51-75-10. 2 L 7 2 4F RT A35EU 2007013000057 20070130 00057 CE 2007 1 30 DXTA200701868 1 20070119 A 5540 991455811 ACTUATOR CESSNA 750 750 2076810 CE VERTICAL STAB FAILED E DXTA O OTHER O OTHER DE DESCENT 1 GL 07 979QS 6733 7500079 ON DESCENT TO THE AIRPORT WE GOT A RUD LIMITER B FAIL CAS MESSAGE SHOWING AT 30%. T/S TO BAD ACTUATOR. REMOVED 7 REPLACE D RUDDER LIMIT "B" ACTUATOR. SYSTEM OPS CHECKS SATISFACTORY AT THIS TIME. PERFORMED RIG CHECKS. ALL WORK DONE IAW CE750 M/M 27-20-00 2 L 7 2 4J RT T00007WI 2007013000058 20070130 00058 SO 2007 1 30 C2XA07IA019 1 20070123 A 2150 8152403 ACM EMB 145 EMB145LR 3260212 SO A/C BAY MALFUNCTIONED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14923 15325 15325 145318 IAH - FLIGHT 2980, THE CREW REPORTED A BURNED RUBBER ODOR EMINATING FROM PACK 2 IN THE COCKPIT AND CABIN WITH NO SMOKE V ISIBLE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ACM, OPERATIO NALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007013000059 20070130 00059 CE 2007 1 30 DXTA200701867 1 20070119 A 3230 7093011 CONTROL MODULE CESSNA 650 650 2076802 CE MLG INOPERATIVE E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 715QS 46 6507105 LANDING GEAR WOULD NOT RETRACT, AFTER T.O. OUT OF SFO. FINALLY 2-3 SECONDS LATER THE GEAR CAME UP. REMOVED AND REPLACED THE LANDING GEAR CONTROL PERFORMED 10 GEAR SWINGS OSP CHECKS GOOD ALL WORK DONE IAW CE-650 M.M. 32-30-01 2 L 7 2 4F A9NM 2007013000061 20070130 00061 EU 2007 1 30 TRAX200700057 1 20070109 A 5220 DOOR AEROSP ATR72 ATR72 EU EMERGENCY EXIT STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 635AS 372 ETNRTC 800-11 ON RT EMERGENCY DOOR, FORCE TO OPEN DOOR. TS 700 HIGH. REFER TO EXELTECH WORK PACKAGE YUL000-164 NRTC 2000 -89 FOR ALL WORK ACCOMPLISHED. CABIN WINDOW NR 6 LT REPLACED IAW JIC 56 21 00 RAI 10000 001. 2 H 7 2 4T RT 2007013000064 20070130 00064 CE 2007 1 30 DXTA200701869 1 20070119 A 2741 444303657 ACTUATOR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE AFT SERVICE BAY INOPERATIVE E DXTA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 07 353QS 4445 4445 5600530 DURING CRUISE AT 17,00 AND 280 KIAS THE AIRCRAFT WOULD CLIMB +500'/MIN WITH FULL NOSE DOWN TRIM. REMOVED AND REPLACED E LEVATOR TRIM ACTUATOR. OPS CHECKS GOOD IAW CESSNA MM 27-31-07. 2 L 7 2 4F 4 F RT A22CE E25EA 2007013000068 20070130 00068 NM 2007 1 30 KCSA071051 1 20070125 A 5412 FIRESHIELD BOEING 747 747209F 1384800 NM NR 1 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 NR 1 PYLON LOWER SKIRT OUTBOARD SIDE SKIN & FIRESHIELD IS CHAFED AT NAC STA 180. 2 L 7 4 4F RT A20WE 2007013000071 20070130 00071 SO 2007 1 30 C2XA07CL012 1 20070124 A 3260 355022002 CONTROL UNIT EMB 145 EMB145XR 3260214 SO COCKPIT FAULTY A C2XA K NONE N FALSE WARNING LD LANDING 1 SW 27 13124 145689 CLE FLIGHT 2451 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE ECIAS AFTER LANDING. MAINTENANCE INSPEC TED AND REPLACED THE LGEU AND RELAY'S KO453 AND KO353. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2007013000073 20070130 00073 EU 2007 1 30 UPS07148979 1 20070123 A 2560 WARNING LIGHT AIRBUS A300 A300F4622R 3930360 EU EVAC SLIDE INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 128UP 0812 INSPECTION TYPE:N/A EVAC SLIDE WARNING LIGHT INOP. RESET (ASPSU), OPS CHECK OK PER MM 52-73-00-05. 2 L 7 2 4F RT A35EU 2007013000074 20070130 00074 CE 2007 1 30 DXTA200701865 1 20070119 A 3150 S2899L50 CIRCUIT BREAKER CESSNA 560 560XL 2076702 CE ALLSN AE3007 AE3007C GL OPEN E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 662QS 4792 5605262 DURING TAKEOFF PRIOR TO V1, LT SIDE MASTER WARNING LIGHT CAME ON STEADY. RT SIDE MASTER WARNING DID NOT COME ON AT ALL. (WILL NOT RESET) ALL OTHER INDICATIONS NORMAL. 2 L 7 2 4F 4 F RT A22CE TE6CH 2007013000075 20070130 00075 NM 2007 1 30 UPS07448958 1 20070111 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 1850 LBL 33 SEAT TRACK I/B FLANGE FOUND CORRODED. M/D BS 1830-1870 LBL 33 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2007013000076 20070130 00076 NM 2007 1 30 UPS07448959 1 20070111 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 980 RBL 11 SEAT TRACK O/B FLANGE FOUND CORROSION. M/D BS 950-1000 RBL 11 SEAT TRACK REPAIRED A S PER SRM 53-10-05 FIG 14. 2 L 7 4 4F A20WE 2007013000077 20070130 00077 NM 2007 1 30 UPS07448960 1 20070108 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 1954-1958 STR 1R STRINGER END FOUND CRACK. M/D BS 1920-1958 STR 1R STRINGER REPAIRED AS PER SR M 53-10-03 FIG 4. REPEAT INSPECTION IS REQUIRED AS PER SRM 53-10-03 FIG 4 TABLE 3. 2 L 7 4 4F A20WE 2007013000079 20070130 00079 NM 2007 1 30 UPS07448962 1 20070110 A 5320 65B38600212 TIE CLIP BOEING 747 747132 1384882 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 2180 S25R FRAME ATT TIE CLIP FOUND CRACKED. M/D BS 2180 S25R FRAME ATT TIE CLIP REPLACED AS PE R SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007013000081 20070130 00081 NM 2007 1 30 UPS07448964 1 20070110 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 2240 LBL 33 SEAT TRACK CROWN FOUND CRACKED APPROX 3 INCHES LONG. M/D BS 2240 LBL 33 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A JUST BETWEEN BS 2230 AND BS 2280. 2 L 7 4 4F A20WE 2007013000082 20070130 00082 NM 2007 1 30 UPS07448965 1 20070109 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 1920 STR 12-13R FRAME I/B CHORD FOUND CRACK. M/D BS 1920 STR 12-13R FRAME I/B CHORD REPAIRED A S PER SRM 53-10-04 FIG 87. 2 L 7 4 4F A20WE 2007013000083 20070130 00083 NM 2007 1 30 UPS07448966 1 20070110 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 2040 LBL 85 FLOORBEAM FOUND CORRODED. M/D BS 2040 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51 -40-04 FIG 1 JUST BETWEEN LBL 43 AND LBL 118 LT MOST O/B. 2 L 7 4 4F A20WE 2007013000084 20070130 00084 NM 2007 1 30 UPS07448967 1 20070111 A 5322 SHEAR TIE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C AFT CARGO COMPT - BELOW FLOOR BILGE AREA SUPPORT FRAME SHEAR TIE FOUND CRACKED AT STA 1740 STR 44L TO STR 47L (3EA). AFT CARGO COMPT BS 1740 BETWEEN STR -43L TO STR 47L AREA SHEAR TIE REPAIRED AND TIE CLIPS 5EA REPLACED A S PER SRM 53-10-04 FIG 42. 2 L 7 4 4F A20WE 2007013000085 20070130 00085 SO 2007 1 30 C2XA07CL014 1 20070125 A 5240 14533417405 CABLE EMB 145 EMB145EP 3260221 SO SERVICE DOOR OUT OF ADJUST A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 14940 145033 CLE FLIGHT 2879 THE CREW REPORTED THE SERVICE DOOR WAS HARD TO CLOSE. MAINTENANCE INSPECTED AND ADJUSTED THE SERVICE DO OR CABLES. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2007013000087 20070130 00087 NM 2007 1 30 SB07007 1 20070125 A 5610 5893543130 WINDSHIELD BOEING 737 7374B7 1384702 NM COCKPIT CRACKED A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 449US 18128 18128 24893 DCA FLT 1781 EN ROUTE FROM MHT TO DCA, THE FIRST OFFICER'S WINDSHIELD ARCED, THEN CRACKED. APPEARS TO BE THE OUTER PANE THAT CRACKED. FLIGHT LANDED WITHOUT FURTHER INCIDENT AT DCA. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICER'S WIN DSHIELD PER MM 56-11-11-404-001. ALSO, REMOVED AND REPLACED WINDOW HEAT CONTROL UNIT FOR FIRST OFFICER'S WINDSHIELD PER MM. OPERATIONAL CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT A16WE 2007013000089 20070130 00089 NM 2007 1 30 SB07008 1 20070127 A 3350 20131ASMI BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 501UW 23231 LGA - MAINTENANCE REPORTED THE FORWARD SECTION OF LOW LEVEL EMERGENCY LIGHTS WERE WEAK. MAINTENANCE REMOVED AND REPLACE D THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007013000090 20070130 00090 NM 2007 1 30 PIDA07002 1 20070124 A 5330 SKIN BOEING 757 757236 1384971 NM FUSELAGE DENTED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 757BJ 22176 DENT IN FUSELAGE SKIN AT BS 760 JUST AFT OF THE L2 DOOR. REPAIRED PER SRM 53-00-01 REPAIR 3. 2 L 7 2 4F RT A2NM 2007013000091 20070130 00091 NM 2007 1 30 MWEA070008 1 20070124 A 2730 CONTROL CABLE BOEING 717 717200 1383700 NM ELEVATOR LOOSE A MWEA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 GL 13 925ME 55191 ELEVATOR CONTROLS ARE CATCHING. FOUND LOW CABLE TENSION, PERFROMED ADJUSTMENT OF ELEVATOR CABLE STAND-BY SYSTEM. 2 L 7 2 4F TR A6WE 2007013000107 20070130 00107 CE 2007 1 30 DXTA200701862 1 20070117 A 3240 UNKNOWN CESSNA 500 560CESSNA 2076750 CE BRAKE SYSTEM UNKNOWN E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 304QS 5600408 WHILE APPLYING BRAKE PRESSURE ON LANDING ROLLOUT THE BRAKE SYSTEM SURGES GIVING YOU THE SENSATION OF SLIPPING ON RUNWAY SURFACE.REMOVED ANTI-SKID TRANSDUCERS & INSPECTED FOR ANY UNUSUAL MOISTURE. FOUND NONE. TAXI (HIGH SPREAD) AIR CRAFT & APPLIED HEAVY BRAKING AIRCRAFT STOPPED STRAIGHT & ANTI SKID COVER BE FELT WORKING. OPS CHECKED GOOD. A SLIPPING SENSATIO N NEVER FELT WORK DONE IAW CE-560 AFM & CE-560 AMM CHAPTER 32-42-00. 2 L 7 2 4F RT A22CE 2007013000108 20070130 00108 2007 1 30 DXTA200701859 4 20070117 A 2200 99146003 ACTUATOR CESSNA 750 750 2076810 CE VERTICAL STAB INOPERATIVE E DXTA O OTHER O OTHER CR CRUISE 1 GL 07 966QS 2566 7500166 CHANNEL B ON UPPER RUDDER OSCILLATES THE AIRCRAFT BACK AND FORTH OPERATES NORMALLY ON CHANNEL A. REMOVED AND REPLACED UP PER RUDDER ACTUATOR I/A/W CE-750 M/M 27-24-01. OPS CHECKED GOOD 2 L 7 2 4J RT T00007WI 2007013000109 20070130 00109 CE 2007 1 30 DXTA200701860 1 20070117 A 7603 LINKAGE CESSNA 500 560CESSNA 2076750 CE LT THROTTLE OBSTRUCTED E DXTA C ABORTED TAKEOFF C R J F.O.D. PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 07 328QS 5600428 ON TAKEOFF, LEFT ENGINE WOULD NOT GO ABOVE 90% N1 TAKEOFF ABORTED.TROUBLESHOOTING DETERMINED THE THROTTLE LINKAGE WAS ST RIKING THE INBOARD IGNITER LEAD. REPOSITIONED IGNITER LEAD TO CLEAR LINKAGE. RAN AIRCRAFT, OPERATIONAL CHECK GOOD. I/ A/W P&W M.M. 71-00-00 2 L 7 2 4F RT A22CE 2007013000110 20070130 00110 CE 2007 1 30 DXTA200701861 1 20070117 A 3230 UPLOCK SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE NLG OUT OF ADJUST E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 838QS 258338 ON FINAL APPROACH AT ABOUT 1000 FT NOSE GEAR LIGHT WENT OUT. DESCENDING DOWN FOR A FLY BY WE GOT THE AUDIBLE WARNING "PU LL UP NO GEAR". ON GO AROUND THE LIGHT CAME BACK ON. THE PIN WAS UP THE ENTIRE TIME. ADJUSTED NOSE GEAR LEGLOCK SWITCH. OPERATIONAL CHECKED NORMAL I.A.W. HAWKER 800XP M/M CH. 32-60-00. REF RAS VNY W.O. 21-04-450 SQK 1.3 2 L 7 2 4F RT A3EU 2007013000111 20070130 00111 2007 1 30 UPS07149031 4 20070123 A 2565 SLIDE AIRBUS A300 A300F4622R 3930360 EU COCKPIT INOPERATIVE A IPXA K NONE O OTHER UK UNKNOWN 1 SO 01 122UP 0807 INSPECTION TYPE:N/A ESCAPE SLIDE INOP. M342678 D/D 1/26/07. INSTALLED SERVICEABLE ESCAPE SLIDE WITH REF TO MM 25-61-21 -04. THIS CLEARS M342678. 2 L 7 2 4F RT A35EU 2007013000112 20070130 00112 EU 2007 1 30 UPS07149032 1 20070126 A 2560 LATCH AIRBUS A300 A300F4622R 3930360 EU LIFE RAFT BIN LACK OF LUBE A IPXA K NONE O OTHER UK UNKNOWN 1 SO 01 122UP 0807 INSPECTION TYPE:N/A UNABLE TO UNLATCH OR OPEN LIFE RAFT BIN. LUBED LATCH, OPS CHECKS GOOD. 2 L 7 2 4F RT A35EU 2007013000113 20070130 00113 NM 2007 1 30 UPS07448983 1 20070111 A 5347 65B3825317 SPLICE BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D RBL 11 SEAT TACK I-BEAM BS 1740-1760 LWR SPLICE CORRODED. M/D BS 1740-1760 RBL 11 SEAT TRACK I-BE AM LWR SPLICE REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007013000115 20070130 00115 NM 2007 1 30 UPS07448991 1 20070110 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C BULK CARGO COMPT FLOOR SUPPORT FOUND CORRODED AT STA 2100 AND STA 2140 LBL 55. BULK CARGO COMPT FLOOR SUPPORT REPAIRED AT BS 2090-2160 LBL 55 AS PER SRM 51-40-04 FIG 2. 2 L 7 4 4F A20WE 2007013000116 20070130 00116 NM 2007 1 30 UPS07449001 1 20070110 A 5340 STRINGER CLIP BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C BULK CARGO COMPT STRINGER CLIP FOUND CORRODED AT STA 2060 S28L. CORROSION BLEND OUT 0.030 X .5 X .5 I NCH EXCEED SRM LIMIT. BULK CARGO COMPT STRINGER CLIP REPLACED AT STA 2060 S28L AS PER SRM 51-10-01 PG 9 AND INSTALLED A S PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007013000117 20070130 00117 NM 2007 1 30 UPS07449002 1 20070104 A 5314 65B140571 SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FX - KEEL BEAM PANEL SUPPORT LOWER SURFACE FOUND SURFACE CORROSION AT STA 1427 LBL 16 TO RBL 16. CORR OSION BLEND OUT 0.025 X .5 X 10 INCHES EXCEED SRM LIMIT. FX - KEEL BEAM PANEL SUPPORT REPLACED AT STA 1427 LBL 16 TO RB L 16 AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007013000119 20070130 00119 NM 2007 1 30 UPS07449004 1 20070111 A 5320 65B091912 SUPPORT FITTING BOEING 747 747123 1384873 NM FWD CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT AFT FIXED STOP SUPPORT FITTING LOWER SURFACE FOUND CRACK AT STA 980 RBL 25. CRACK LEN GTH 2 INCHES. FWD CARGO COMPT AT BS 980 RBL 25 AFT FIXED STOP SUPPORT FITTING REPLACED AS PER SRM 51-10-01 PG 9 AND INS TALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007013000123 20070130 00123 NM 2007 1 30 UPS07449008 1 20070111 A 5210 BEAM BOEING 747 747123 1384873 NM DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LT MED NR 4 FWD VERTICAL BEAM INTERIOR LOWER CORNER FOUND CRACKED. LT MED NR 4 FWD VERTICAL BEAM LOWE R CORNER AREA REPAIRED AS PER SRM 52-10-02 FIG 10. 2 L 7 4 4F A20WE 2007012900150 20070129 00150 EA 2007 1 29 SWIA200717745 1 20070105 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 710BR 7852 LBL9 STA 280 HAS CRACK UPPER FRAME, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS AT STN 280, LBL9.0 UPP ER IAW CRJ200 REO 601R-53-11-138 REVNC. 2 L 7 2 4F RT A21EA 2007012900177 20070129 00177 EA 2007 1 29 SWIA200717749 1 20070105 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 710BR 7852 PAX DOOR FWD WEB CRACK AT HANDRAIL STOWAGE CASTING AND STEP JUST BELOW AT CORNER, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS ON FWD WEB OF PAX DOOR PER CRJ200 REO 52-11-702 REV 'A'. 2 L 7 2 4F RT A21EA 2007012900216 20070129 00216 EU 2007 1 29 MALA070017 1 20070116 A 2430 501171202 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS NO TEST A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 412XJ 340B412 FAILED CAP CHECK PER BF GOODRICH CMM WO 418119 PN501-1712-02. REPLACED BATTERY PACK. 2 L 7 2 4T RT A52EU 2007012900240 20070129 00240 2007 1 29 QXEA200700106 4 20070126 A 3160 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 401QX 4031 BOI FLIGHT NR 2360: DU BAD CONF MESSAGE ON ED. UNABLE TO CLEAR USING CHECKLIST. MAINTENANCE CYCLED SHIPS POWER. MESSA GE WENT AWAY. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007012900241 20070129 00241 WP 2007 1 29 07FDEA00186 1 20070126 A 5730 SKIN DOUG DC10 DC1010 3022110 WP LT WING DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 LT WING INBD FLAP: DENTS ON LOWER SKIN AFT PANEL AT STA XIFH 171, XIFH 177 AND XIFH 201 WITH DEFORMATION OF BACK-UP STRU CTURE. PERFORMED REPAIR SKIN IAW SRM 57-10-00 FIG 3 VOL 1 IAW SRM 51-41-01 FIG 1 VOL 2. REPLACED TEE IAW SRM 51-35-01 PAG 1/13 VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I027615/N02615 AND SRM 57-10-00 VOL1 FIG 3, DWG ARC2481 (-5) AND ATM P0208753. 2 L 7 3 4F A22WE 2007012900243 20070129 00243 EU 2007 1 29 SIMA200702602 1 20070124 A 5347 7253742409 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 236AE 23655 4000 340B236 SEAT TRACK FOUND CORRODED AT BUTT LINE 36R. REMOVED AND REPLACED SEAT TRACK, RESTORED PROTECTIVE FINISH, APPLIED CORROS ION PREVENTATIVE IAW SRM 51-40-21, 51-40-22, 51-40-25, 51-40-40 AND 53-70-60. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007012900256 20070129 00256 NM 2007 1 29 HALA0700036 1 20070105 A 5330 SKIN BOEING 767 767332 1382001 NM BS 494 DENTED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 598HA 23278 FOUND DENT IN SKIN AT BS 494, 1.5 INCHES ABOVE STRINGER 34L, BS 494L, 1.5" ABOVE STRINGER 34L, INVESTIGATED DENT, FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE. HFEC AREA TO ENSURE CRACK FREE CONDITION. FABRICATED, ALODINED, PRIMED AND INSTA LLED REPAIR PER SRM 53-00-01-2R-1. PRIMED AND PAINTED AREA PER SRM 51-20-01. 2 L 7 2 4F RT A1NM 2007012900273 20070129 00273 EU 2007 1 29 AWXA200700122 1 20070118 A 5755 D5754148400000 HINGE PIN AIRBUS 320 A320232 3930326 EU ZONE 600 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 602AW 565 SAL - CORROSION ON RIGHT WING NR 5 SPOILER INBOARD HINGE PIN, WS 10729. REPLACED RIGHT WING NR 5 SPOILER INBOARD HINGE PIN, WS 10729 IAW A320 AMM 27-64-42. 2 L 7 2 4F RT A28NM 2007012900277 20070129 00277 EA 2007 1 29 MALA070015 1 20070119 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT STUCK A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 602XJ 8045 DURING PILOT TRAINING ON A/C 602, THE PILOT CLASS COULD NOT OPEN THE LT OVERWING EMERGENCY EXIT DOOR. MAINTENANCE INSP ECTED DOOR AND NOTED EXIT PREVIOUSLY INSTALLED INCORRECTLY CAUSING DOOR TO JAM. THE 2 HOOK FITTINGS ON THE BOTTOM OF DO OR WERE INCORRECTLY ALIGNED WITH THE AIRFRAME HINGE FITTINGS, BUT THE DOOR INDICATION IN THE FLT DECK SHOWED CLOSED. MA INTENANCE REMOVED DOOR. INSPECTED AND FOUND NO DAMAGE AND REINSTALLED EXIT. 2 L 7 2 4F RT A21EA 2007012900288 20070129 00288 WP 2007 1 29 ASAA0781386 1 20070111 A 5210 SKIN DOUG DC9 DC983 3022083 WP L1 DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 L1 DOOR SKIN AT UPPER CORNER PEELED BACK. REMOVED DAMAGED SECTION OF SKIN. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 52 05. PERFORMED CLASS III REPAIR PER SRM 53 04. 2 L 7 2 4F RT A6WE 2007012900338 20070129 00338 EA 2007 1 29 QXEA200700099 2 20070124 A 7320 8193007008 FADEC BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 407QX 1618 4049 SEA FLIGHT NR 2328: SHORTLY AFTER TAKEOFF, NR 2 ENGINE FADEC CAUTION LIGHT ILLUMINATED. THERE WAS NO LOSS OF NR 2 ENGIN E POWER. MAINTENANCE FOUND CHANNEL A CODES NR 700, 701, 702, 709, 710, 715, 721, 724, 725, 759, 760, 779, 788, 789, 791 , 793, 799, 806. CHANNEL B FAULT CODE NR 779. REMOVED AND REPLACED THE NR 2 ENGINE FADEC IAW AMM 73-21-01-000-801 AND 73-21-01-400-801. ALL FAULT CODES CLEARED. PERFORMED TWO ENGINE STARTS WITH NO DEFECTS NOTED. CODES DID NOT RETURN. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2007013000010 20070130 00010 EA 2007 1 30 REXA200700010 1 20070127 A 2750 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS UNKNOWN A REXA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 8672A 7672 FLAPS FAIL ON TAXI OUT. COMPLIED WITH AD2006-12-21, RESET FLAPS, AND MONITORING FOR 72 HRS. 2 L 7 2 4F RT A21EA 2007013000026 20070130 00026 NM 2007 1 30 CALA0700033 1 20070127 A 5240 6545871503 SKIN BOEING 737 737524 1384721 NM R-1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14667 28927 INSPECTION FOUND A 2 INCH CRACK AT LIGHTENING HOLE OF LOWER ROW 2ND FROM AFT IN R-1 DOOR SKIN. THE DOOR SKIN WAS REPAIR ED IAW ECRA 5241-01017. 2 L 7 2 4F RT A16WE 2007013000041 20070130 00041 SO 2007 1 30 C2XA07BT008 1 20070123 A 4950 4952304 BLEED VALVE EMB 145 EMB145XR 3260214 SO APU FAULTY A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 11127 5565 145697 EWR LOG SQUAWK STRONG FUEL ODOR IN COCKPIT DURING TAKEOFF. FOUND WINDSHIELD HEAT NR 2 CONTROLLER POWER TERMINALS MELTED . REMOVED AND REPLACED WINDSHIELD HEAT CONTROLLER NR 2 IAW EMB145 AMM 30-42-01 AND REPAIRED WIRE TERMINAL TO CONTROLLER IAW EMB145 AMM 20-21-00. OPS CHECK GOOD. *S/D* IAH FLIGHT 2940 THE CREW REPORTED FUEL SMELL ON TAKEOFF GOES AWAY WHE N ENGINE BLEEDS ARE SELECTED AND APU BLEED CLOSED. CLE MAINTENANCE REPLACED THE APU BLEED VALVE. OPERATIONAL CHECKS WE RE GOOD. 2 L 7 2 4F RT 2007013000118 20070130 00118 NM 2007 1 30 UPS07449003 1 20070104 A 5314 65B140581 SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FX - KEEL BEAM PANEL SUPPORT LOWER SURFACE FOUND SURFACE CORROSION AT STA 1460 LBL 16 TO RBL 16. CORR OSION BLEND OUT 0.029 X 1 X 10 INCHES EXCEED SRM LIMIT. FX KEEL BEAM PANEL SUPPORT REPLACED AT STA 1460 LBL 16 TO RBL 1 6 AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007013000120 20070130 00120 NM 2007 1 30 UPS07449005 1 20070109 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT STRINGER FOUND CRACK AT STA 745 S39L. FWD CARGO COMPT BS 740-770 STR 39L STRINGER REP AIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007013000124 20070130 00124 NM 2007 1 30 UPS07449009 1 20070108 A 5347 69B1459210 SPLICE BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 1000 RBL 11 SEAT TRACK LOWER SPLICE FOUND CORROSION. CORROSION BLEND OUT 0.030 X .5 X 1 INCH E XCEED SRM LIMIT. M/D BS 1000 RBL 11 SEAT TRACK LOWER SPLICE FITTING REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007013000126 20070130 00126 NM 2007 1 30 UPS07449011 1 20070108 A 5313 65B0677818 FITTING BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 1961-1964 STR 1R STRINGER END STRINGER SPLICE FITTING FOUND CORROSION. CORROSION BLEND OUT 0.0 80 X .375 X 2 INCHES EXCEED SRM LIMIT. M/D BS 1954-1966 STR 1R STRINGER SPLICE FITTING REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007013000132 20070130 00132 NM 2007 1 30 UPS07449018 1 20070109 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO BS 800-820 S34R FOUND CRACKED AS MARKED. FWD CARGO COMPT BS 742 TO BS 820 STR 34R REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007013000133 20070130 00133 NM 2007 1 30 UPS07449019 1 20070109 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO RIGHT BS 760-780 S34R FOUND CORROSION. CORROSION BLEND OUT 0.043 X .5 X 4 INCHES EXCEED SRM LIMIT. FWD CARGO COMPT BS 742 TO BS 830 STR 34R REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007013000134 20070130 00134 NM 2007 1 30 UPS07449020 1 20070109 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO BS 780-800 S34R FOUND CRACKED AS MARKED. FWD CARGO COMPT BS 742 TO BS 830 STR 34R REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007013000137 20070130 00137 NM 2007 1 30 UPS07449023 1 20070109 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT STRINGER FOUND CRACK AT STA 800 S35L. CRACK LENGTH .375 INCH. FWD CARGO COMPT BS 740 TO BS 890 STR 35L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007013000138 20070130 00138 NM 2007 1 30 UPS07449024 1 20070109 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT STRINGER FOUND CRACK AT STA 845 S35L. CRACK LENGTH .5 INCH. FWD CARGO COMPT BS 740 T O BS 890 STR 35L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007013000140 20070130 00140 NM 2007 1 30 UPS07449026 1 20070109 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT STRINGER FOUND CRACK AT STA 790 S35L. CRACK LENGTH .375 INCH. FWD CARGO COMPT BS 740 TO BS 890 STR 35L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007013000142 20070130 00142 NM 2007 1 30 UPS07449028 1 20070109 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT STRINGER FOUND CORROSION AT STA 780 S35L. CORROSION BLEND OUT 0.041 X .75 X 2 INCHES EXCEED SRM LIMIT. FWD CARGO COMPT BS 740 TO BS 890 STR 35L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007013000144 20070130 00144 WP 2007 1 30 UPS07848993 1 20070104 A 5313 DC853B0093 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 LONGERON CRACKED AT STA 1766 L14L. REMOVED DAMAGED LONGERON, FABRICATED AND INSTALLED REPLACEMENT LO NGERON AND 2 EA SPLICES IAW SRM 51-1-21, 53-02-02-0 FIG 011, AND 51-1-20D. 2 L 7 4 4F RT 4A25 2007013000146 20070130 00146 WP 2007 1 30 UPS07848994 1 20070109 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 STA 1700 LBL 26 UNDERSIDE OF FLOORBEAM HAS CORROSION. REMOVED CORROSION, FABRICATED AND INSTALLED ST RAP AND 2 EA REPAIR ANGLES IAW SRM 51-1-21 AND 53-2-0. 2 L 7 4 4F RT 4A25 2007013000149 20070130 00149 SO 2007 1 30 SIMA200703007 1 20070127 A 5315 14000235003 FLOORBEAM EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 805AE 13051 4800 145489 FOUND CENTER FLOORBEAM CORRODED AT FRAME 24. PERFORMED CUTOUT OF DAMAGE, FABRICATED REPAIR PIECES. INSTALLED REPAIR PI ECES IAW EMB SRM 53-00-10. RESTORED PROTECTIVE FINISH AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007013000150 20070130 00150 SO 2007 1 30 SIMA200703011 1 20070126 A 5315 14530645411 FLOORBEAM EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 850AE 9246 4800 145722 FOUND PREVIOUS REPAIR AT FRAME 20 CORRODED. REMOVED EXISTING REPAIR. CLEANED AND TREATED AREA, FABRICATED AND INSTALLE D NEW REPAIR PIECES IAW EMB SRM 53-00-10. RESTORED PROTECTIVE FINISH, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007013000151 20070130 00151 SO 2007 1 30 SIMA200703001 1 20070129 A 3320 BR900022 BALLAST EMB 135 EMB135LR 3260305 SO CABIN LIGHTS FAILED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 713AE 15157 145249 ELECTRICAL SMELL IN CABIN AFTER OVERHEAD LIGHTS SELECTED OFF. REMOVED AND REPLACED BALLAST AT LEFT GALLEY AND ROW ONE I AW EMB AMM 33-21-03. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007013000152 20070130 00152 SO 2007 1 30 SIMA200703009 1 20070128 A 5340 14525369003 STRINGER CLIP EMB 135 EMB135KL 3260302 SO CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 805AE 13051 4800 145489 FOUND SHEAR CLIP AT FRAME 68 CORRODED. PERFORMED CUTOUT OF DAMAGED AREA. FABRICATED REPAIR PIECES, INSTALLED REPAIR PI ECES IAW EMB IC2007-145/00513A. RESTORED PROTECTIVE FINISH, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007013000153 20070130 00153 SO 2007 1 30 SIMA200703012 1 20070126 A 5320 14525480603 SILL EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 850AE 9246 4800 145722 FOUND CARGO DOOR FRAME LOWER SILL TO BE CORRODED. REMOVED AND REPLACED LOWER SILL IAW EMB SRM 51-40-02. RESTORED PROTE CTIVE FINISH, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007013000154 20070130 00154 WP 2007 1 30 UPS07848998 1 20070106 A 5711 SAA36440462 SPAR CAP DOUG DC8 DC871F 302199D WP WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C3 POSSIBLE CRACK AT NR 4 ALT BETWEEN LWR FRT SPAR CAP FLANGE AND STRINGER 64 JUST OUTBOARD XRS428. REM OVED, FABRICATED AND INSTALLED SPAR CAP FLANGE IAW SRM 51-1-20D & DWG 3644046. 2 L 7 4 4F RT 4A25 2007013000155 20070130 00155 WP 2007 1 30 UPS07848999 1 20070102 A 5320 SAA5613064104 SUPPORT DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C3 A-PIT FWD BULKHEAD STA 70 RBL 24 SUPPORT FRAME CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMEN T FRAME SUPPORT IAW SRM 51-1-21, 51-1-20D AND DWG 5613064. 2 L 7 4 4F RT 4A25 2007013000156 20070130 00156 NM 2007 1 30 UIEA200700038 1 20070127 A 8011 3978921 START VALVE BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE NR 3 ENGINE FAULTY A UIEA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 EA 15 527MC 5204 2450 22471 530276 NR 3 ENGINE START VALVE OPEN LIGHT CAME ON DURING CRUISE, FOLLOWED FHB PROCEDURES AND SHUT DOWN THE ENGINE. TRANSFERRED TO DEFERRED ITEM M07-010, MEL 80-1-1. AS PER MCC REQUEST REMOVED AND REPLACED START VALVE. REMOVED AND REPLACED START VALVE AS REQUIRED. 2 L 7 4 4F 4 F RT A20WE E23EA 2007013000157 20070130 00157 NM 2007 1 30 DHL2007743505 1 20070130 A 5321 FLOOR PANEL BOEING 727 727225 1384077 NM BS 1178 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 BS 1178, RBL 18.0, AREA UNDER FLOOR PANEL (WEB), SHOWS CORROSION. CUT OUT DAMAGE, 5.5" BY 6", FABRICATED DOUBLER OUT OF 2024-T3, .050" BY 9.5" BY 10", PO NR 9004384; AND FILLER OUT OF 2024-T3, .040" BY 7.125" BY 8.75", PO NR 9004150, TREAT ED, PRIMED, AND INSTALLED REPAIR PARTS, ALL PER B727 SRM 53-10-2 FIG 3, 51-40-2 FIG 1, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 2007013000159 20070130 00159 2007 1 30 QXEA200700108 4 20070126 A 3160 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 401QX 4031 BOI FLIGHT NR 2360: DU BAD CONF MESSAGE ON ED UNABLE TO CLEAR USING CHECKLIST. MAINTENANCE CYCLED SHIPS POWER. MESSAGE CLEARED. NO OTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007013000161 20070130 00161 NM 2007 1 30 07FDEA00194 1 20070129 A 5340 69191222 SUPPORT FITTING BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 NLG DOWNLOCK ACTUATOR SUPPORT FITTING IS CRACKED AT UPPER FASTENER INSTALLED NLG DOWNLOCK ACTUATOR SUPPORT FITTING WITH SERVICEABLE CHANNEL FITTING 69-19122-2 (TAG NR AD0511) AND FASTENERS (TAG NR A78094). WORK ACCOMPLISHED IAW 51-30-2 PG 5. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007013000162 20070130 00162 NM 2007 1 30 ASAA0741421 1 20070129 A 5753 SKIN BOEING 737 737490 1384715 NM FORE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 RIGHT O/B FORE FLAP L EADING EDGE CHAFED. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-5 3-01 FIG 201 REPAIR 1. 2 L 7 2 4F RT A16WE 2007013000163 20070130 00163 NE 2007 1 30 ABXA070019 2 20070124 A 7230 BLADE BOEING 767 767231 1385131 NM PWA JT9 JT9D7R4D 52054 NE LT ENGINE DAMAGED A ABXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 23 708AX 3021 22571 709643 ON TAKEOFF FROM ILN, DURING LANDING GEAR RETRACTION, GOT SUBSTANTIAL IMPACT SOUND FROM LEFT ENGINE AREA, AND BURNING SME LL AFTER SOUND. NO ENGINE ABNORMALITIES OR EXCEEDANCES. LANDED UNDER WEIGHT. C/W BIRD STRIKE INSPECTION BORESCOPE & B LADE REPLACEMENT ON LT ENGINE REF W/P 600264766 FOR DOCUMENTATION. MAINTENANCE PULLED THE THREE DAMAGED BEYOND LIMIT BL ADES AND ADDITIONAL 180 BLADE FOR A TOTAL OF FOUR BLADES THAT NEED CHANGED. AIRCRAFT TOOK SOME BIRDS AS WELL, BUT NO DE NTS ON AIRFRAME FOUND. 2 L 7 2 4F 4 F RT A1NM E3NE 2007013000166 20070130 00166 WP 2007 1 30 ABXA070020 1 20070112 A 5711 5911301501 SPAR CAP DOUG DC9 DC941 302207N WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 LEFT WING LOWER OUTBOARD SPAR CAP CORRODED, RIVETS POPPED, CUPPED AND SKIN BULGING AT XRS 509. REPAIRED LEFT WING LOWER OUTBOARD SPAR CAP IAW REA D957-55323MR. 2 L 7 2 4F A6WE 2007013000168 20070130 00168 WP 2007 1 30 ABXA070022 1 20070112 A 5342 591214159 RIVET DOUG DC9 DC941 302207N WP VERTICAL STAB SHEARED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 LEFT VERTICAL STAB ATTACH ANGLE CHECKED AND HAD 2 SHEARED RIVETS. REPAIRED LEFT VERTICAL STAB ATTACH ANGLE IAW DC9 SRM 53-05, FIG 23. 2 L 7 2 4F A6WE 2007013000169 20070130 00169 WP 2007 1 30 ABXA070023 1 20070115 A 5320 591014211 THRESHOLD DOUG DC9 DC941 302207N WP CARGO BAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 FORWARD LOWER CARGO DOOR THRESHOLD WEB HAD IMPROPERLY INSTALLED RIVET THAT HAD CRACKED THE WEB BETWEEN STA 389 - 408. R EMOVED AND INSTALLED NEW INTERCOSTAL AND REPAIRED AREA IAW REA D953-55-335MR. 2 L 7 2 4F A6WE 2007013000170 20070130 00170 EU 2007 1 30 AWXA200700125 1 20070125 A 5751 D57640024200 CHANNEL AIRBUS 320 A320232 3930326 EU ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 602AW 565 SAL - CRACK ON LEFT WING AILERON LOWER SURFACE TRAILING EDGE PLATE, 16" FROM OUTBOARD END, WS 1166, RIB 22. REPLACED LE FT WING AILERON LOWER SURFACE TRAILING EDGE PLATE, 16" FROM OUTBOARD END, WS 1166, RIB 22 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007013000171 20070130 00171 EU 2007 1 30 AWXA200700126 1 20070118 A 5755 D5754148420000 HINGE PIN AIRBUS 320 A320232 3930326 EU SPOILER CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 602AW 565 SAL - CORROSION ON RIGHT WING NR 2 SPOILER OUTBOARD HINGE PIN, WS 6699, RIB 12. REPLACED RIGHT WING NR 2 SPOILER OUTBOA RD HINGE PIN, WS 6699, RIB 12 IAW A320 AMM 27-64-43. 2 L 7 2 4F RT A28NM 2007013000172 20070130 00172 WP 2007 1 30 ABXA070024 1 20070117 A 5347 S2914913M24000 SEAT TRACK DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 RIGHT BUTT LINE 54, STA 225, SEAT TRACK HAD EXFOLIATION CORROSION. REMOVED & REPLACED SEAT TRACK SECTION IAW DC9 SRM 51 -10-4 AND 51-30-1. 2 L 7 2 4F A6WE 2007013000173 20070130 00173 EU 2007 1 30 AWXA200700127 1 20070118 A 5755 D5754148420000 HINGE PIN AIRBUS 320 A320232 3930326 EU SPOILER CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 602AW 565 SAL - MAJOR REPAIR - CORROSION ON RIGHT WING NR 3 SPOILER OUTBOARD HINGE PIN, WS 7792, RIB 14. REPLACED RIGHT WING NR 3 SPOILER OUTBOARD HINGE PIN, WS 7792, RIB 14 IAW A320 AMM 27-64-43. 2 L 7 2 4F RT A28NM 2007013000174 20070130 00174 EU 2007 1 30 AWXA200700128 1 20070126 A 5755 D574148420000 HINGE PIN AIRBUS 320 A320232 3930326 EU ZONE 500 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 602AW 565 SAL - CORROSION ON LEFT WING NR 2 SPOILER OUTBOARD HINGE PIN, WS 4067, RIB 8 - WS 4862, RIB 9. REPLACED LEFT WING NR 2 SPOILER OUTBOARD HINGE PIN, WS 4067, RIB 8 - WS 4862, RIB 9 IAW AWA TASKCARD C3L57322. 2 L 7 2 4F RT A28NM 2007013000175 20070130 00175 EU 2007 1 30 AWXA200700129 1 20070123 A 5755 D5754148420000 HINGE PIN AIRBUS 320 A320232 3930326 EU NR 2 SPOILER CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 602AW 565 SAL - CORROSION ON LEFT WING NR 2 SPOILER INBOARD HINGE PIN, WS 4067, RIB 8 - WS 4862, RIB 9. REPLACED LEFT WING NR 2 SPOILER INBOARD HINGE PIN, WS 4067, RIB 8 - WS 4862, RIB 9 IAW AWA TASKCARD C3L57322. 2 L 7 2 4F RT A28NM 2007013000180 20070130 00180 NM 2007 1 30 07FDEA00196 1 20070129 A 5330 SKIN BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 LT EXT FUSE SKIN IS FRETTED AT FILLET FRG PANEL INTERFACE BS 720D 10 TO 720D 15, STR 19L REMOVED LEADING EDGE FOR ACCESS TO REPAIR, INSTALLED EXTERNAL REPAIR AT LAP SPLICE REF SRM 53-30-3 PG 20. REINSTALLED LEADING EDGE AND LEAKED CHECKED HYD LINES REF MM 27-81-000-2 (HYD LEAK CK) AND TAI DUCT LEAK CHECK ACCOMPLISHED ON WO NR 35039/WC NR 70C53-00. 2 L 7 3 4F RT A3WE 2007013000181 20070130 00181 NM 2007 1 30 07FDEA00197 1 20070130 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 STRINGER CLIP CRACKED IN CUT OUT RADIUS AT BS 680 STR 8L REMOVED DAMAGED CLIP TRANSFERED FASTENER HOLES FOR NEW CLIP, IN STALLED NEW CLIP REF SRM 51-30-2 PG 2 AND 5, SRM 51-30-5 PG 1. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007013000183 20070130 00183 NM 2007 1 30 AALA20070112 1 20070118 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 193AN 32387 DFW - EMERGENCY LIGHT AT SEAT 6E HAS BROKEN SHROUD. REPLACED THE SHROUD FOR THE EMERGENCY LIGHT AT SEAT 6E. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007013000184 20070130 00184 NM 2007 1 30 AALA20070113 1 20070118 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 193AN 32387 DFW - EMERGENCY LIGHT AT SEAT 11D HAS BROKEN SHROUD. REPLACED THE SHROUD FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007013000185 20070130 00185 NM 2007 1 30 AALA20070114 1 20070118 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 193AN 32387 DFW - EMERGENCY LIGHT AT SEAT 14D HAS BROKEN SHROUD. REPLACED THE SHROUD FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007013000186 20070130 00186 NM 2007 1 30 AALA20070115 1 20070118 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 907AN 29509 LAX - EMERGENCY LIGHTS FROM SEAT ROWS 22 TO 28 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT ROWS 2 2 TO 28. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007013000187 20070130 00187 NM 2007 1 30 AALA20070097 1 20070115 A 3350 BULB BOEING 757 7572Q8 1384972 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 712TW 27624 DFW - EMERGENCY FLOOD LIGHT AT RIGHT NUMBER THREE DOOR INOPERATIVE. RELAMPED EMERGENCY FLOOD LIGHT AT RIGHT NUMBER THRE E DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007013000189 20070130 00189 NM 2007 1 30 AALA20070101 1 20070116 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 610AA 24486 MIA - EMERGENCY EXTERIOR LIGHT AT LEFT NUMBER THREE DOOR INOPERATIVE. FOUND LIGHT BULB LOOSE. ADJUSTED LIGHT BULB FOR EMERGENCY EXTERIOR LIGHT AT LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007013000190 20070130 00190 WP 2007 1 30 AALA20070090 1 20070115 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 467AA 49597 PHX - EMERGENCY LIGHTS ABOVE SEAT ROW 25DEF INOPERATIVE. CHARGED EMERGENCY LIGHT SYSTEM FOR EMERGENCY LIGHTS ABOVE SEAT ROW 25DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007013000191 20070130 00191 WP 2007 1 30 AALA20070091 1 20070115 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 467AA 49597 PHX - EMERGENCY LIGHTS AT AFT TAIL COMPARTMENT AT STATION 1322 INOPERATIVE. CHARGED EMERGENCY LIGHT SYSTEM FOR EMERGENC Y LIGHTS AT AFT TAIL COMPARTMENT AT STATION 1322. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007013000192 20070130 00192 WP 2007 1 30 AALA20070104 1 20070116 A 2150 ACM DOUG DC9 DC982 3022082 WP LEAKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 456AA 49561 ORD INFLIGHT T1392/16JAN - DURING CLIMB SMOKE AND FUMES IN CABIN COMING FROM AIR CONDITIONING SYSTEM. TURNED OFF PACKS AND RECIRCULATION SWITCH AND BREAKERS. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. FOUND LEFT PACK AIR CYCLE MACHINE LEAKING OIL. REPLACED AIR CYCLE MACHINE FOR LEFT PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007013000193 20070130 00193 WP 2007 1 30 AALA20070093 1 20070115 A 3231 LINK DOUG DC9 DC982 3022082 WP NLG DOOR INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 253AA 49286 ORD INFLIGHT - DURING GEAR RETRACTION AFTER TAKEOFF HEARD LOUD AIR NOISE AND FELT VIBRATION FROM NOSE GEAR AREA. CYCLED GEAR WITH NO CHANGE. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. FOUND NOSE GEAR DOOR IN OPEN POSITION. ADJUSTED LE FT FORWARD DOOR LINK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007013000194 20070130 00194 WP 2007 1 30 AALA20070095 1 20070115 A 2611 2026TP DUCT DOUG DC9 DC982 3022082 WP RT ENGINE BLOWN A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 297AA 49309 TPA INFLIGHT - DURING CLIMB RIGHT ENGINE FIRE WARNING ILLUMINATED. WARNING WENT OUT AND ILLUMINATED AGAIN TWO TIMES THE N WENT OFF. ALL GAUGES WERE NORMAL ON BOTH ENGINE. FIRE BOTTLES WERE NOT DISCHARGED. RETURNED TO TPA AND LANDED WITHO UT INCIDENT. FOUND BLOWN DUCT ON RIGHT ENGINE INBOARD ANTI ICE VALVE AT AFT SIDE OF VALVE. REPLACED ANTI ICE VALVE DUC T AT AFT SIDE OF VALVE ON NUMBER TWO ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007013000196 20070130 00196 NM 2007 1 30 AALA20070096 1 20070115 A 3350 BPS73 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 320AA 22321 LAX - EMERGENCY LIGHTS AT RIGHT FORWARD DOOR AND OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK M731 FOR EMERGENCY LI GHTS AT RIGHT FORWARD DOOR AND OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007013000197 20070130 00197 NM 2007 1 30 AALA20070098 1 20070115 A 3350 SOCKET BOEING 757 7572Q8 1384972 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 712TW 27624 DFW - EMERGENCY SLIDE LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED THE SOCKET ASSEMBLY FOR THE L60 EMERGENCY S LIDE LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007013000198 20070130 00198 NM 2007 1 30 AMTA200700039 1 20070126 A 3350 BATTERY PACK BOEING 737 73783N 13844HI NM CABIN MALFUNCTIONED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 301TZ 28239 L2 EMERGENCY LIGHT INOPERATIVE. RESET BATTERY PACK TEST, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2007013000199 20070130 00199 WP 2007 1 30 AALA20070099 1 20070115 A 3244 HUB DOUG DC9 DC982 3022082 WP MLG WHEEL FAILED A AALA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 279AA 49295 DFW - NUMBER ONE BRAKE REPORTED LOCKED DURING TAXI OUT FOUND NUMBER ONE WHEEL AND BEARING FAILURE AND SUBSEQUENT DAMAGE TO SHEEL AXLE. REPLACED NUMBER ONE TIRE TO ENABLE TAXI TO HANGAR. REPLACED NUMBER ONE MAIN LANDING GEAR AND BRAKE DUE TO NUMBER ONE TIRE HUB FAILURE AND BRAKE DAMAGE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007013000200 20070130 00200 NM 2007 1 30 AALA20070103 1 20070116 A 3350 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39365 24046 DFW - EMERGENCY LIGHTS AT SEAT 3H INOPERATIVE. REPLACED WALL TO SEAT HARNESS CONNECTOR FOR EMERGENCY LIGHTS AT SEAT 3H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007013000201 20070130 00201 2007 1 30 AMTA200700038 4 20070127 A 2310 COUPLER BOEING 757 75733N 1384931 NM NR 1 HF COMM DEFECTIVE A AMTA K NONE O OTHER CR CRUISE 1 GL 11 560TZ 33525 L HF INOPERATIVE, AT ALL CREW STATIONS. DOES NOT TUNE PROPERLY WHEN TRANSMIT BUTTON IS PUSHED, RADIO TRIES TO TUNE FOR ABOUT 20 SECONDS EACH TIME BUTTON IS PUSHED. REPLACED HF NR 1 SYSTEM COUPLER IAW AMM 23-11-01-4 PERFORMED SATISFACTORY INSTALLATION TEST. (M) 2 L 7 2 4F RT A2NM 2007013000203 20070130 00203 NM 2007 1 30 ASAA0741422 1 20070129 A 5512 655482133 SKIN BOEING 737 737490 1384715 NM HORIZ STAB DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 LEFT STABLIZER I/B LEADING EDGE PANEL IS CREASED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED PLATE AND FILLER IAW S RM 55-10-01 FIGURE 201 REPAIR 2. 2 L 7 2 4F RT A16WE 2007013000207 20070130 00207 EA 2007 1 30 TRAX200700119 1 20070122 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 854AS 7382 PAX DOOR -EXIT- PLACARD ON STEP 832 BT WORN. 2 L 7 2 4F RT A21EA 2007013000208 20070130 00208 EA 2007 1 30 TRAX200700120 1 20070122 A 3250 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING MALFUNCTIONED A ASOA K NONE N FALSE WARNING CL CLIMB 1 SO 27 906EV 7642 NOSE WHEEL STEERING INOP MSG. AFTER TAKEOFF FROM KMLU. FOLLOWED QRH AND MSG CLEARED. RESET NOSE WHEEL STEERING SYS PE R MTC REQUEST ON THE GROUND IN KATL. NWS WAS WORKING PROPERLY ALL THE WAY TO THE GATE. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007013000210 20070130 00210 EU 2007 1 30 TRAX200700122 1 20070123 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 643AS 413 ASD EMERGENCY LIGHT INOP. 2 H 7 2 4T RT 2007013000212 20070130 00212 EA 2007 1 30 TRAX200700115 1 20070121 A 5320 SILL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 CORROSION ON LOWER LEG OF PAX DOOR SILL FS 330. REMOVED AND TREATED CORROSION AS REQUIRED. APPLIED AO23 FINISH AS REQU IRED. ALL WORK PERFORMED IAW CRJ 700 SRM 51-25-01. SM17032 SUPPLEMENTAL - SDR CLOSED 01/26/07. 2 L 7 2 4F RT A21EA 2007013000213 20070130 00213 EA 2007 1 30 TRAX200700116 1 20070121 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A ASOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 970EV 7527 AFTER TAKEOFF SWITCHED BLEEDS TO ENGINES AND GOT RT PACK HI PRESS WITH BURNT SMELL IN A/C. FOLLOWED QRH TO RESET BUT DI D NOT, ALREADY SINGLE PACK. FINALLY GOT TO RESET AFTER STARTING APU AND SWITCHING BLEEDS. AIRCRAFT RETURNED TO ATL AFT ER T/O. FLTS 4856, 4866 CX. 2 L 7 2 4F RT A21EA 2007013000214 20070130 00214 EA 2007 1 30 TRAX200700117 1 20070120 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 EVALUATE AREAS OF SURFACE CORROSION ON 280 FRAME. ALL WORK ACCOMPLISHED USING REO 670-53-11-052, REO 670-53-11-047, CRJ 700 SRM 51-42-06 SOLID FASTENERS, 51-42-13 BLIND RIVETS AND 51-42-21 LOCK FASTENERS, 51-25-06 ALODINE AND PRIME, AND 51 -25-16. 2 L 7 2 4F RT A21EA 2007013100001 20070131 00001 NM 2007 1 31 QXEA200700117 1 20070129 A 5230 HANDLE BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR STIFF A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 417QX 4086 SEA FLIGHT NR 2378: GROUND CREW REPORTS AFT BAGGAGE DOOR HANDLE VERY DIFFICULT TO OPEN. MAINTENANCE INSPECTED, CLEANED AND APPLIED LUBRICANT. CYCLED MANY TIMES WITH NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT CONTINUED SERVICE. 2 H 7 2 4T RT A13NM 2007013100003 20070131 00003 SO 2007 1 31 SIMA200730308 1 20070128 A 5340 14525175001 STRINGER CLIP EMB 135 EMB135KL 3260302 SO FUSLEAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 805AE 13051 4800 145489 FOUND STRINGER CLIP AT FRAME 65 TO BE CORRODED. PERFORMED CUTOUT OF DAMAGED SHEAR CLIP, FABRICATED REPAIR PIECES. INST ALLED REPAIR PIECES IAW EMB IC2007-145/00513A. RESTORED PROTECTIVE FINISH, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007013100004 20070131 00004 SO 2007 1 31 SIMA200703013 1 20070129 A 5320 14525480603 SILL EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 805AE 13051 4800 145489 FOUND CARGO DOOR FRAME LOWER SILL CORRODED. REMOVED AND REPLACED LOWER SILL IAW EMB SRM 51-40-02. RESTORED PROTECTIVE FINISH, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007013100005 20070131 00005 SO 2007 1 31 SIMA200703002 1 20070129 A 2910 AE71379016 LINE EMB 135 EMB135LR 3260305 SO HYDRAULIC SYS BROKEN A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 735TS 13360 145386 NUMBER ONE HYDRAULIC SYSTEM FAIL, EMERGENCY DECLARED. REMOVED AND REPLACED BROKEN HYDRAULIC LINE AND HYDRAULIC PUMP DUE TO FUILD STARVATION. ALL WOORK DONE IAW EMB AMM 29-10-30 AND 29-10-03. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO S ERVICE. 2 L 7 2 4F RT T00011AT 2007013100006 20070131 00006 SO 2007 1 31 SIMA200703004 1 20070124 A 5315 14530645411 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 702AE 15957 4800 145164 FOUND OMEGA BEAM CORRODED AT FRAME 38. PERFORMED CUTOUT OF DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PIECES IAW EMB SRM 53-00-10. RESTORED PROTECTIVE COATING, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007013100011 20070131 00011 EA 2007 1 31 COMA0760056 1 20070124 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 915CA 7013 FLIGHT 5689 - AT 2210Z 3000 FT RECEIVED FLAPS FAIL CAUTION MESSAGE WHEN FLAPS WERE SELECTED. COMPLIED WITH AD 2006-12-2 1 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C) FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2007013100018 20070131 00018 EA 2007 1 31 COMA0760055 1 20070122 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION LD LANDING 1 SO 01 720SW 11450 7297 FLIGHT 5117 - FLAP FAIL CAUTION DESCENDING THROUGH FL 19, OAT -10. REPLACED RIGHT WING BPSU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007013100020 20070131 00020 EA 2007 1 31 COMA0770008 1 20070125 A 3213 CC670851002 STRUT CNDAIR CL600 CL6002C10 1390015 EA RT MLG CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 367CA 10987 10069 RIGHT MLG I/B UPPER TORQUE LINK ATTACH LUG HAS INTERNAL PITTING CORROSION. REPAIRED IAW BF GOODRICH CONSESSION SCR0073- 06 REV A. 2 L 7 2 4F RT A21EA 2007013100028 20070131 00028 EA 2007 1 31 COMA0760053 1 20070122 A 2750 860D10018ABCD CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAULTY A COMA K NONE J WARNING INDICATION LD LANDING 1 SO 01 720SW 19232 7297 FLIGHT 5117 - FLAP FAIL CAUTION DESCENDING THROUGH FL 10, OAT -10. REPLACED FECU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007013100029 20070131 00029 NM 2007 1 31 QXEA200700109 1 20070126 A 5297 WIRE BOMBDR DHC8 DHC8402 1390042 NM DOOR WARNING BROKEN A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 408QX 4050 PDX FLIGHT NR 2423: FUSELAGE DOOR WARNING LIGHT ILLUMINATED PASSING 17,500 MSL AT 5.0 PSID. SERVICE DOOR RIGHT REAR WAS PROBLEM. DOOR WARNING LIGHT REMAINED ON UNTIL LEVEL 10,000 MSL AT 3.5 PSID. LIGHT REMAINED ON AND STEADY UNTIL LANDIN G. MAINTENANCE REPAIRED BROKEN WIRE AT AFT SERVICE DOOR HINGE. OPS CHECK NORMAL IAW AMM 31-62-00-710-801 AND SUBTASK 3 1-62-00-701-801(A) ITEM 4 AND (B). NO OTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007013100030 20070131 00030 NM 2007 1 31 AALA20070117 1 20070118 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 198AA 32392 TPA - EMERGENCY LIGHTS AT SEAT ROWS 26 TO 36 AND EXIT SIGN IN AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGEN CY LIGHTS AT SEAT ROWS 26 TO 36 AND EXIT SIGN IN AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007013100034 20070131 00034 EU 2007 1 31 AALA20070105 1 20070116 A 3397 087022260 WIRE HARNESS AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70079 619 JFK - EMERGENCY LIGHT AT SEAT 32G INOPERATIVE. REPLACED HARNESS FOR EMERGENCY LIGHT AT SEAT 32G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007013100035 20070131 00035 NM 2007 1 31 AALA20070106 1 20070116 A 3397 WIRE BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 698AN 26980 DFW - EMERGENCY LIGHTS ON LEFT SIDE EXTERNAL OVERWING INOPERATIVE. REPAIRED LOOSE WIRE FOR EMERGENCY LIGHTS ON LEFT SID E EXTERNAL OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007013100036 20070131 00036 NM 2007 1 31 AALA20070108 1 20070117 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 782AN 30003 MIA - EMERGENCY LIGHTS AT SEAT 3D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 3D. SYSTEM GROUND CHECKED NORMAL OPERA TION. 2 L 7 2 4F RT T00001SE 2007013100037 20070131 00037 NM 2007 1 31 AALA20070109 1 20070117 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 782AN 30003 MIA - EMERGENCY LIGHT AT SEAT 3D HAS MISSING LENS CAP. REPLACED LENS CAP FOR EMERGENCY LIGHT AT SEAT 3D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007013100038 20070131 00038 NM 2007 1 31 AALA20070116 1 20070117 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 767AJ 33539 DFW - EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR ABOVE FLIGHT ATTENDANT SEAT INOPERATIVE. RELAMPED EMERGENCY LIGHT AT LE FT NUMBER THREE DOOR ABOVE FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007013100040 20070131 00040 WP 2007 1 31 AALA20070094 1 20070115 A 4990 5940405503 APU DOUG DC9 DC982 3022082 WP LEAKING A AALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 484AA 49677 DFW INFLIGHT T1200/15JAN AFTER TAKE OFF BLUE HAZE WAS REPORTED IN CABIN. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. SMOKE DISSIPATED PRIOR TO LANDING. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. FOUND APU LEAKING OIL. CHANGED APU AND ACCOMPLISHED PACK BURN AND CHANGED COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007013100041 20070131 00041 EU 2007 1 31 IJ02007F00000 1 20070115 A 3222 STRUT BRAERO DH125 BAE125800A 1500285 EU GARRTT TFE731 TFE731* 01518 WP NLG COLLAPSED E IJ0A A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 WP 15 150SB 258197 (REF CNTRL NR: 1-15-07) DURING THE TAKEOFF ROLL (APPROXIMATELY 100 KTS), THE CREW EXPERIENCED BOUNCING OF THE AIRCRAFT N OSE WITH INCREASING SEVERITY. THE CREW CONTINUED THE TAKE-OFF SEQUENCE, AND NOTED A RED NOSE GEAR (UNSAFE) INDICATION L IGHT AFTER THE LANDING GEAR WAS SELECTED TO THE RETRACT POSITION. THE NOISE LEVEL IN THE COCKPIT ALSO INDICATED AN EXTE NDED NOSE GEAR. CREW SELECTED THE LANIND GEAR TO THE EXTENDED POSITION WHICH RESULTED IN ALL 3 GREEN LANDING GEAR (SAFE ) INDICATION LIGHTS AND ADVISED THAT THEY WOULD BE RETURNING BACK DUE TO THE CONDITION AC LANDED WITHOUT INCIDENT. UPO N AIRCRAFT SHUTDOWN, AN EXAMINATION OF THE NOSE GEAR REVEALED THE NOSE STRUT WAS COMPLETELY COLLAPSED WITH HYDRAULIC FLU 2 L 7 2 4F 4 F RT A3EU E6WE 2007013100044 20070131 00044 NM 2007 1 31 AALA20070121 1 20070118 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 399AN 29606 DFW - EMERGENCY EXIT LIGHT AT OVERHEAD ABOVE SEAT 5H INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT OVERHEAD ABOVE SEAT 5H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007013100046 20070131 00046 NM 2007 1 31 DL76L070058 1 20070126 A 2121 732591C COOLING FAN BOEING 767 767332 1382001 NM EQUIPMENT BAY ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 186DN 27962 UNUSUAL ELECRICAL ODOR IN COCKPIT. ALL C/BS WERE CHECKED IN BUT FOUND FWD EQUIPMENT EXHAUST FAN STATUS MESSAGE. AFT EQ EXHAUST FAN WAS ALREADY ON MCO. ACC SMOKE AND FUMES REMOVAL CHECK LIST. AFTER SELECTING EQUIPMENT COOLING OVRD BOTH OD OR AND STATUS MSG DISSAPPEARED FOUND FWD EQUIPMENT COOLING FAN C/B P6-4 H20 TRIPPED WITH FAINT ODOR. REMOVED AND REPLAC ED FWD EXH EQUIPMENT COOLING FAN. 2 L 7 2 4F RT A1NM 2007013100050 20070131 00050 NM 2007 1 31 DL76L070062 1 20070125 A 3610 SHUTOFF VALVE BOEING 767 767332 1382001 NM BLEED SYSTEM UNKNOWN A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 171DN 24759 WITH LEFT HPSOV ON MCO. AFTER TAKEOFF LEFT ENGINE BLEED OFF STAYED ILLUMINATED. 2 L 7 2 4F RT A1NM 2007013100051 20070131 00051 CE 2007 1 31 JEM2007F00000 1 20070102 A 3210 RIVET BEECH 200 200BEECH 1152920 CE PWA PT6 PT6* 52043 EA RT MLG LOOSE E JEMA K NONE O OTHER IN INSP/MAINT 1 CE 01 376RC 10071 BB376 FOUND LOOSE AND BROKEN RIVETS IN THE RT MLG DRAG LEG SUPPORT AND CHANNEL. RIVETS ON BOTH THE IB AND OB SIDES OF THE SUP PORT WERE EITHER MISSING THE MACHINE HEADS AND WORKING THEIR WAY OUT OR WERE FOUND TO BE BROKEN IN HALF, BUT STILL IN TH EIR RESPECTIVE PLACES. THE GEAR WAS OPERATING NORMALLY AND NO OTHER DAMAGE WAS DISCOVERED. THE SITUATION WAS MOST LIKE LY CAUSED BY AIRCRAFT AGE, RIVET FATIGUE AND GEAR BEING EXTENDED OR RETRACTED AT TOO HIGH OF AN AIRSPEED. (K) 1 L 7 2 4T 3 T A24CE E2NE 2007013100053 20070131 00053 NM 2007 1 31 SWAA070410 1 20070126 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 RIGHT OVERWING EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007013100054 20070131 00054 WP 2007 1 31 AALA20070087 1 20070115 A 3213 STRUT DOUG DC9 DC982 3022082 WP LANDING GEAR INOPERATIVE A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 70425 49337 TUL INFLIGHT - NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO TUL AND LANDED WITHOUT INCIDENT. AIRCRAF T TAKEN OUT OF SERVICE FOR EVALUATION. SERVICED NOSE LANDING GEAR STRUT PER MAINTENANCE MANUAL 32 21 02 3. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007013100055 20070131 00055 WP 2007 1 31 AALA20070088 1 20070115 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 467AA 49597 PHX - EMERGENCY LIGHTS AT DROP DOWN PANEL OUTSIDE FORWARD LAVATORY INOPERATIVE. REPLACED BATTERY PACK AT STATION 211 FO R EMERGENCY LIGHTS AT DROP DOWN PANEL OUTSIDE FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007013100058 20070131 00058 WP 2007 1 31 AALA20070092 1 20070115 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 467AA 49597 PHX - EMERGENCY LIGHTS AT AFT FLIGHT ATTENDANT STATION AND TAIL COMPARTMENT AT STATION 1330 INOPERATIVE. CHARGED EMERGE NCY LIGHT SYSTEM FOR EMERGENCY LIGHTS AT AFT FLIGHT ATTENDANT STATION AND TAIL COMPARTMENT AT STATION 1330. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007013100059 20070131 00059 NM 2007 1 31 AALA20070100 1 20070115 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 383AN 26995 LAX - EMERGENCY LIGHTS AT OVERHEAD SEAT 26A INOPERATIVE. REPLACED BATTERY PACK AT SEAT 23A FOR EMERGENCY LIGHTS AT OVER HEAD SEAT 26A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007013100060 20070131 00060 NM 2007 1 31 AALA20070123 1 20070118 A 7830 218900015 ACTUATOR BOEING 757 757223 1384957 NM RIGHT REVERSER LEAKING A AALA O OTHER K FLUID LOSS LD LANDING 1 SW 21 629AA 24587 JFK INFLIGHT - LOSS OF RIGHT HYDRAULIC DURING LANDING. LANDED JFK WITHOUT INCIDENT. AIRCRAFT TAXIED TO GATE NORMALLY. REPLACED ACTUATOR FOR RIGHT REVERSER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007013100068 20070131 00068 2007 1 31 QXEA200700114 2 20070127 A 7397 CONNECTOR BOMBDR DHC8 DHC8402 1390042 NM FUEL TEMP IND LOOSE A QXEA O OTHER O OTHER DE DESCENT 1 NM 09 414QX 4061 BOI FLIGHT NR 2418: DURING DESCENT, NR 1 FUEL TEMP FLUCTUATED FROM +50 TO +99C. MAINTENANCE CLEANED AND RESEATED NR 1 F UEL TEMP CONNECTOR. GROUND RAN NR 1 ENGINE. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007013100069 20070131 00069 WP 2007 1 31 8012007001 1 20070129 A 5347 MS21064L489 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1690-1696 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 DURING A "B" CHECK IN FT LAUDERDALE FL, THE FOLLOWING DISCREPANCIES WERE NOTED; A .500 CRACK WAS FOUND ON THE RT O/B SEA T TRACK AT FUSE STA 1690. PER DOUGLAS AIRCRAFT SRM, 53-2-3 THE FOLLOWING REPAIR WAS PERFORMED, REMOVED SEAT TRACK FROM STA 1690 TO 1696. INSTALLED NEW SECTION OF SEAT TRACK P/N 7452952-7 BATCH NR 228475 ALODINE AND PRIMED IAW, DMM 51-10-4 . INSTALLED REPAIR PARTS IAW DOUGLAS SRM 53-2-3, NO OTHER INSPECTIONS REQUIRED. 2 L 7 4 4F RT 4A25 2007013100074 20070131 00074 NM 2007 1 31 AWXA200700090 1 20070108 A 5313 140N1530 STRINGER BOEING 757 757225 1384959 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 PHX - MAJOR REPAIR - EXTERIOR FUSELAGE SKIN BULGE, 1380, S28R CAUSED BY CORROSION ON STRINGER. REPAIRED S28R, BS 1380 IAW ER 19-5361-07012-HF1. 2 L 7 2 4F RT A2NM 2007013100077 20070131 00077 NM 2007 1 31 HALA0700024 1 20070113 A 2797 CABLE BOEING 717 717200 1383700 NM FLAP BUSS DAMAGED A HALA O OTHER O OTHER AP APPROACH 1 WP 13 484HA 55129 ON APPROACH WHEN FLAPS WERE SEL TO 13 GOT A SLIGHT ROLL TO LEFT. AFTER LDG WHEN FLAPS WERE SEL TO 18 GOT FLAP DISAG ALE ART AND CONFIG PG SHOWED L FLAP AT 13 AND R FLAP AT 19. FOUND FLAP BUS CABLE 3XA BROKEN AND BUSS 33B CRUSHED. REMOVED AND REPLACED FLAP BUSS CABLES 34A AND 33B PER AMM 27-50-00. OPS CHECK GOOD. 2 L 7 2 4F TR A6WE 2007012900259 20070129 00259 EU 2007 1 29 DHL2007362511 1 20070106 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 47663 84 CORROSION ON SEAT TRACK FLANGE BETWEEN FR 73 AN 74 LBL 56. REMOVED CORROSION FROM SEAT TRACK FLANGE FR 73-FR 74 LBL 56 PER A300 SRM 51-40-11 ORG MAT. .078, MAT REMOVED .007 MAT REMAINING .071 FOUND WITHIN LIMITS PER A300 SRM 53-10-00 EXCEP T O/B SCREW HOLE 11 INCHS AFT OF FR 73 REMAINING MAT MEASURED .060 OUT OF LIMITS PER A300 SRM 53-10 10 FIG 612. CUT OUT DAMAGED AREA AT O/B FLANGE SEAT TRACK LBL 56 BETWEEN FR 73-FR 74 (3") PER A300 SRM 53-10-10 FIG 721A. TREATED AREA AN PARTS WITH ALODINE, PRIMER AN GRAY PAINT IAW A300 SRM 51-40-12. INSTALLED REPAIR IAW A300 SRM 53-10-10 FIG 721A MAT USE D 7075T6 .130, 10"BY 2' BY 1 1/2" PO NR004127. INSTALLED PERMANENT REPAIR. 2 L 7 2 4F RT A35EU 2007012900362 20070129 00362 SO 2007 1 29 SIMA200701909 1 20070109 A 5347 14530658005 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 705AE 15855 4800 145184 FOUND SEAT TRACK BETWEEN FRAME 36 TO 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007012900367 20070129 00367 SO 2007 1 29 SIMA200701907 1 20070110 A 5320 14522178005 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 705AE 15855 4800 145184 FOUND CENTER SERVICE DOOR SILL CORRODED. REMOVED AND REPLACED SERVICE DOOR SILL IAW EMB SRM 51-40-02. RETURNED AIRCRAF T TO SERVICE. 2 L 7 2 4F RT T00011AT 2007013000006 20070130 00006 NM 2007 1 30 QXEA200700111 1 20070127 A 2900 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 404QX 4046 BIL FLIGHT NR 2411: NR 3 HYD PUMP CAUTION LIGHT ILLUMINATED. MAINTENANCE RESEATED RELAY RL4. NR 3 HYD PUMP CAUTION CLE ARED. NR 3 HYD PUMP OPERATES NORMALLY PER AMM TASK 29-00-00-863-803. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007013000015 20070130 00015 NM 2007 1 30 0700286740 1 20070116 A 5310 TENSION TIE BOEING 747 747251F 1384898 NM BS 880 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 640US 23888 DURING "M" CHECK, FOUND CRACK IN TENSION TIE FORWARD CHANNEL AT BS 880. REPAIRED PER EA 67-207926. 2 L 7 4 4F A20WE 2007013000019 20070130 00019 NM 2007 1 30 0700336740 1 20070118 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 420 S15R CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 640US 23888 DURING "M" CHECK, FOUND CRACKS IN FRAME WEB AND DOUBLER AT BS 420 S15R. REPAIRED PER EA 67-208613. 2 L 7 4 4F A20WE 2007013000032 20070130 00032 NM 2007 1 30 UPS07448972 1 20070109 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO BS 840-845 S37R FOUND CRACKED AS MARKED. FWD CARGO COMPT BS 830 TO BS 850 STR 37R AREA REPA IRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007013000038 20070130 00038 NM 2007 1 30 UPS07448988 1 20070111 A 5411 65B904084 FRAME BOEING 747 747123 1384873 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C NR 2 PYLON UPPER WING CAVITY O/B FRAME AT NAC STA 237 TOP CORNER AREA CRACKED AS RED MARKED. NR 2 PYL ON AT NAC STA 237 O/B FRAME REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND SRM 51-30-02. 2 L 7 4 4F A20WE 2007013000042 20070130 00042 NM 2007 1 30 UPS07448990 1 20070110 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C AFT COMPT - RIGHT STA 1580 FRAME AFT FACE UPPER EDGE AT S39 TO S40 CRACKED. AFT CARGO COMPT BS 1580 A T STR 39R STRINGER STR 39R-40R AREA FRAME REPAIRED AS PER SRM 53-10-04 FIG 69. 2 L 7 4 4F A20WE 2007013000046 20070130 00046 WP 2007 1 30 UPS07848977 1 20070102 A 3230 BOSS DOUG DC8 DC871F 302199D WP RT MLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C2 RIGHT MAIN LANDING GEAR RETRACT PIN BOSS ID CORRODED. RIGHT MLG RETRACT PIN BORE BOSS CORROSION IS O UT OF LIMITS IAW EO DC8-3230-0450-O. RIGHT MLG TO BE REMOVED AND REPLACED ON NRC 949517 AND TC 9132-3. 2 L 7 4 4F RT 4A25 2007013000050 20070130 00050 WP 2007 1 30 UPS07848982 1 20070124 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:N/A DURING PDC, EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC8 AMM 33-50-01-2. CH ECK SERVICEABLE. 2 L 7 4 4F RT 4A25 2007013000060 20070130 00060 SO 2007 1 30 C2XA07IA020 1 20070122 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13958 145085 IAH - DURING MAINTENANCE INSPECTION, THE NUMBER 4 AND 5 AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENAN CE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007013000063 20070130 00063 NM 2007 1 30 KCSA071047 1 20070125 A 5411 FRAME BOEING 747 747209F 1384800 NM NR 2 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 NR 2 PYLON REAR ENGINE MOUNT BULKHEAD FRAME IS CRACKED 1 INCH FORWARD SIDE, INBOARD & OUTBOARD OF PYLON UPPER SPAR CHORD AT NAC STA 221.9. 2 L 7 4 4F RT A20WE 2007013000067 20070130 00067 SO 2007 1 30 C2XA07SH006 1 20070128 A 3350 276005 FUSE EMB 145 EMB145LR 3260212 SO BATTERY PACK BLOWN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 19966 145131 RIGHT OUTBOARD FWD EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED BLOWN FUSE ON NR 2 EMERGENCY LIGHT BATTERY PACK IAW RA DIANT POWER CORP CMM 25-60-03, OPS CHECK GOOD. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007013000078 20070130 00078 NM 2007 1 30 UPS07448961 1 20070105 A 5350 65B06755601 SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FX REAR BODY FAIRING SUPPORT LWR SURFACE FOUND CORROSION AT STA 1520 TO STA 1525 CENTER SUPPORT. BODY FAIRING SUPPORT REPLACED AS PER SRM 51-10-01 PG 9. 2 L 7 4 4F A20WE 2007013000080 20070130 00080 NM 2007 1 30 UPS07448963 1 20070110 A 5347 69B044803 SPLICE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D RBL 11 SEAT TRACK BS 1760 - 1780 LT SPLICE CRACKED. M/D RBL 11 SEAT TRACK LT SPLICE ANGLE REPLACE D AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02 JUST BETWEEN BS 1760 AND BS 1780 AREA. 2 L 7 4 4F A20WE 2007013000121 20070130 00121 NM 2007 1 30 UPS07449006 1 20070111 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C AFT CARGO COMPT FLOOR SUPPORT FOUND CRACKED AT STA 1775 RBL 40. AFT CARGO COMPT FLOOR SUPPORT REPAIRE D AS PER SRM 51-40-03 FIG 1, JUST AT STA 1775 RBL 40 AREA. 2 L 7 4 4F A20WE 2007013000125 20070130 00125 NM 2007 1 30 UPS07449010 1 20070111 A 5347 CARGO TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 2040-2060 RBL12 TIE DOWN TRACK FLANGE AREA LWR FACE FOUND CORROSION AS MARKED. M/D BS 2030-213 0 RBL 11-33 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 14. 2 L 7 4 4F A20WE 2007013000128 20070130 00128 NM 2007 1 30 UPS07449013 1 20070123 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FWD CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT SEAT TRACK FOUND CORROSION AT STA 980 LBL 25. FWD CARGO COMPT BS 930 TO BS 980 LBL 25 AREA TRACK REPAIRED AS PER SRM 53-10-05 FIG 5. 2 L 7 4 4F A20WE 2007013000129 20070130 00129 NM 2007 1 30 UPS07449015 1 20070110 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 2040-2140 RBL 98 SEAT TRACK CROWN ATT BOLTS AREA FOUND CORRODED. CORROSION BLEND OUT 0.070 X . 75 X 3 INCHES EXCEED SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A, JUST AT RBL 98 BETWEEN BS 2090 AND 2150 . 2 L 7 4 4F A20WE 2007013000141 20070130 00141 NM 2007 1 30 UPS07449027 1 20070109 A 5340 65B386001223 STRINGER CLIP BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT FRAME STRINGER CLIP FOUND CORROSION AT STA 980 S37L. CORROSION BLEND OUT 0.037 X .5 X .5 INCH EXCEED SRM LIMIT. FWD CARGO COMPT STA 980 S37L STRINGER CLIP REPLACED AS PER SRM 51-10-01 P9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007013000164 20070130 00164 WP 2007 1 30 ABXA070026 1 20070129 A 5330 59114013 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 951AX 47616 DURING INSPECTION OF FUSELAGE SKIN AT LONGERON 22, FOUND SKIN CRACKED AT LOWER AFT CORNER OF AIR STAIR DOOR, STA 200. R EPAIRED CRACK IAW ABX EA 5300001-003-2. 2 L 7 2 4F A6WE 2007013000165 20070130 00165 WP 2007 1 30 ABXA070025 1 20070125 A 2133 OUTFLOW VALVE DOUG DC9 DC931 3022065 WP CABIN PRESSURE FROZEN A ABXA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 23 906AX 47072 DURING CLIMB, CABIN WOULD NOT PRESSURIZE, DID ABNORMAL. COULD NOT PRESSURIZE MANUALLY EITHER. CABIN PRESSURE CONTROL W HEEL JAMMED. DUE TO COLD WEATHER, SUSPECT OUTFLOW VALVE FROZEN. HEATED AND LUBRICATED VALVE. PRESSURIZED AIRCRAFT ON GROUND, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2007013000188 20070130 00188 NM 2007 1 30 AMTA200700041 1 20070128 A 5240 HANDLE BOEING 737 73783N 13844HI NM SERVICE DOOR NOT SEATED A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 323TZ 30033 RETURNED TO GATE UNABLE TO EXTINGUISH FORWARD SERVICE DOOR LIGHT. FOUND INTERIOR HANDLE HALF ENGAGED, CLOSED DOOR HANDL E PROPERLY, OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2007013100012 20070131 00012 EA 2007 1 31 COMA0770009 1 20070125 A 3222 520009 STRUT CNDAIR CL600 CL6002C10 1390015 EA NLG CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 367CA 10987 10069 NLG AXLE/PISTON ASSEMBLY, CORROSION IN BOTH TORQUE LINK ATTACH BORES. REPLACED NLG ASSEMBLY IAW AMM 32-21-01. 2 L 7 2 4F RT A21EA 2007013100013 20070131 00013 EA 2007 1 31 COMA0760059 1 20070124 A 2697 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA BLEED AIR SYS DIRTY A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 451CA 7562 FLIGHT 5222 - ANTI-ICE DUCT WARNING IN CLIMB. LEFT FUSELAGE DUCT ON EICAS WAS RED. CLEANED CONNECTORS FOR 14TH STAGE B LEED AIR LOOP IN LEFT WHEEL WELL. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007013100016 20070131 00016 EA 2007 1 31 COMA0760054 1 20070122 A 2750 7805013 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A COMA K NONE J WARNING INDICATION LD LANDING 1 SO 01 720SW 19232 7297 FLIGHT 5117 - FLAP FAIL CAUTION DESCENDING THROUGH FL 19, OAT -10. REPLACED FLAP LEVER ASSEMBLY. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007013100019 20070131 00019 EA 2007 1 31 COMA0760052 1 20070122 A 3010 124112450 SWITCH CNDAIR CL600 CL6002B19 1900309 EA LT WING FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 983CA 7169 FLIGHT 5389 - ANTI-ICE DUCT WARNING MESSAGE AT 8000 FT. PERFORMED OPS CHECK OF ANTI-ICE SYSTEM, VISUAL CHECK OF FUSELAG E LOOPS AND OHMED WING SENSORS. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007013100021 20070131 00021 EA 2007 1 31 COMA0760060 1 20070125 A 3020 5399001 ANTI-ICE VALVE CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 959CA 4857 7116 FLIGHT 4963 - EN ROUTE CVG-MDT RECEIVED A LEFT COWL ANTI-ICE CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND DIVERTED TO CMH. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT ENGINE COWL ANTI-ICE VALVE. 2 L 7 2 4F RT A21EA 2007013100024 20070131 00024 EA 2007 1 31 CHQA200700004 1 20070128 A 5101 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA VIBRATION A CHQA B EMER. DESCENT E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 11 650BR 7418 FLIGHT 3257 - IAH-MSP - WHILE CLIMBING THROUGH 3,000 FEET, RECEIVED MULTIPLE "STALL FAIL" MESSAGE ON THE EICAS. THROUGH 3,500 FEET, HEARD A NOISE IN THE FRONT OF THE AIRCRAFT. THE NOISE BECAME LOUDER. LEVELED OFF AT 4,000 FEET AND NOTIFI ED ATC AND BEGAN TO RUN CHECKLISTS. SOUNDED LIKE THE RAT WAS DEPLOYED, ALSO VIBRATION ON THE COCKPIT FLOOR WHICH MATCHE D NOISE OF RAT DEPLOYING. RAN QRH AND CHECKLISTS THAT CALLED TO DISENGAGE THE STALL PTC SYSTEM. TROUBLESHOT THROUGH TH E AC/DC SYNOPTIC PAGE AND NOTICED THE ADG WAS NOT DEPLOYED ACCORDING TO THE ELECTRICAL PAGE ALTHOUGH THE SOUND WAS GETTI NG LOUDER. FINISHED THE QRH AND ALL CHECKLISTS. LANDED UNEVENTFULLY. MAINTENANCE PERFORMED OPS CHECK OF STALL PROTECT 2 L 7 2 4F RT A21EA 2007013100025 20070131 00025 EA 2007 1 31 COMA0760058 1 20070124 A 3010 6243843 SENSOR CNDAIR CL600 CL6002B19 1900309 EA LT WING FAILED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 409CA 982 7441 FLIGHT 5276 - LEFT WING ANTI-ICE CAUTION MESSAGE DURING TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AN D REPLACED A LEFT WING TEMP SENSOR. 2 L 7 2 4F RT A21EA 2007013100026 20070131 00026 EA 2007 1 31 COMA0760051 1 20070122 A 3010 124112450 THERMAL SWITCH CNDAIR CL600 CL6002B19 1900309 EA LT WING FAULTY A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 983CA 7169 FLIGHT 5141 - TAKEOFF WITH WING AND COWL ANTI-ICE ON, ANTI-ICE DUCT WARNING AT 100 KTS. MESSAGE EXTINGUISHED AS THRUST REDUCED. ABORTED TAKEOFF. REPLACED THERMAL SWITCH AT LEFT WS 250. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007013100039 20070131 00039 NM 2007 1 31 AALA20070110 1 20070117 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 196AA 32390 SJU - EMERGENCY LIGHTS FROM SEAT ROWS 9D TO 15D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT ROWS 9D TO 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007013100052 20070131 00052 NM 2007 1 31 SWAA070409 1 20070126 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 LT OVERWING EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007013100057 20070131 00057 WP 2007 1 31 AALA20070089 1 20070115 A 3350 CHARGER DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 467AA 49597 PHX - EMERGENCY LIGHTS AT STATION 909 RIGHT AT AFT OVERWING EXIT SIGNS ABOVE SEAT 21DEF INOPERATIVE. REPLACED CHARGER F OR EMERGENCY LIGHTS AT STATION 909 RIGHT AT AFT OVERWING EXIT SIGNS ABOVE SEAT 21DEF. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F A6WE 2007013100084 20070131 00084 NM 2007 1 31 HALA0700041 1 20070129 A 3350 LIGHT BOEING 767 76733A 1385209 NM CABIN INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 580HA 28140 ON OVERNIGHT CHK, FOUND EMERGENCY LTS ON FWD FLT ATTN STATION INOP. REMOVED AND REPLACED 40 INCH PHOTOLUMINESCENT EMERG ENCY ESCAPE PATH STRIP OPS CHK NML. 2 L 7 2 4F RT A1NM 2007013100086 20070131 00086 EA 2007 1 31 QXEA200700119 1 20070129 A 3241 6007047 TRANSDUCER CNDAIR CL600 CL6002C10 1390015 EA ANTI-SKID SYS FAULTED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 605QX 10022 SFO- FLIGHT 4166 (DEN-SJC) DURING CRUISE FLIGHT RECEIVED A ANTI-SKID FAULT STATUS MESSAGE. DUE TO THE RUNWAY LENGTH AT SJC, DIVERTED TO SFO AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE NR 2 WHEEL SPEED TRANSDUCER. OPER ATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007013100087 20070131 00087 EA 2007 1 31 QXEA200700120 1 20070129 A 4900 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA APU UNKNOWN A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 600QX 10005 PSP - FLIGHT 2580, AT PUSHBACK RECEIVED A APU LOAD CONTROL VALVE OPEN CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENAN CE RESET ALL CIRCUIT BREAKERS. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007013100088 20070131 00088 EA 2007 1 31 QXEA200700121 1 20070129 A 5230 DOOR CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY OPEN A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 605QX 10022 LIT- FLIGHT 4324, AFTER ROTATION CARGO DOOR OPENED. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINT ENANCE INSPECTED THE DOOR AND FOUND NO DEFECTS. COMPLIED WITH TEST OF DOOR AND PRESSURIZATION WITH NO DEFECTS. AIRCRAF T RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007013100089 20070131 00089 EA 2007 1 31 QXEA200700105 1 20070126 A 2730 8221310002 CONCENTRATOR CNDAIR CL600 CL6002C10 1390015 EA MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 09 602QX 9782 10010 TUL- FLIGHT 4202 RECEIVED A ELEVATOR SPLIT CAUTION MESSAGE. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING . THE AIRCRAFT WAS FERRIED TO DENVER WHERE THE NR 1 DATA CONCENTRATOR WAS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007013100090 20070131 00090 EA 2007 1 31 QXEA200700104 1 20070124 A 5297 WIRE HARNESS CNDAIR CL600 CL6002C10 1390015 EA DOOR WARNING DAMAGED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 610QX 10033 PDX - RECEIVED A PROXI SYSTEM FAULT 2 STATUS MESSAGE (SERVICE DOOR). RETURNED TO THE GATE. MAINTENANCE REPAIRED THE SE RVICE DOOR WIRE HARNESS TO SENSOR PX-45. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007013100092 20070131 00092 SO 2007 1 31 SWIA200717761 1 20070122 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 224SW 120294 FORWARD FLOOR RED EMERGENCY LIGHTS INOP. REPAIRED RED EMERGENCY FLOOR LIGHT BY MCD. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007013100093 20070131 00093 EA 2007 1 31 SWIA200717762 1 20070125 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 965SW 7871 AFT TWO CABIN OVERHEAD EMERGENCY LIGHTS INOP. RELAMPED OVERHEAD EMERGENCY LIGHTS IAW AMM 33-61-01. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007013100095 20070131 00095 EA 2007 1 31 SWIA200717764 1 20070125 A 3350 CHARGER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 730SK 10193 EMERGENCY "EXIT" SIGNS OVERHEAD BY MCD AND SERVICE DOOR ARE BURNED OUT. REPLACED FORWARD BATTERY CHARGER PER AMM 33-51- 15. OPERATIONAL CHECKS GOOD, P/N: OFF: 11-0049, S/N OFF: 20705. 2 L 7 2 4F RT A21EA 2007030500116 20070305 00116 NM 2007 3 5 SWAA071173 1 20070301 A 5322 141A1130 SHEAR TIE BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 726SW 27858 DURING SCHEDULED 8Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, STR 24L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007030500117 20070305 00117 NM 2007 3 5 SWAA071149 1 20070228 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007013100111 20070131 00111 WP 2007 1 31 07FDEA00202 1 20070130 A 5347 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 368FE 46606 CABIN SEAT TRACK STA 1249, LBL 75 TOPSCALLOPED AREA WORN AND GOUGED, APPROX 3 INCHES. REMOVED AND REPLACED SEAT TRACK S TA 1229 TO 1411 IAW DC/MD 10 SRM 53-70-00 PAGE 5, FIG 1 VOL I, MECH 110217, QC002. 2 L 7 3 4F RT A22WE 2007013100112 20070131 00112 WP 2007 1 31 07FDEA00203 1 20070130 A 5415 ATTACH ANGLE DOUG MD10 MD1010F 3022112 WP ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 368FE 46606 NR 1 PYLON ATTACHED ANGLE FOR PANEL 488GL CHAFED. REMOVED, FABRICATED AND INSTALLED NEW DOUBLER IAW DAC DRAWING AUB7108 REV AN, AND DC10/MD 10 SRM 51-35-01 VOL II, MECH 2891, QC227. 2 L 7 3 4F RT A22WE 2007013100114 20070131 00114 CE 2007 1 31 AMWA82619BC 1 20070122 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA DISCHARGED A AMWA K NONE J WARNING INDICATION CR CRUISE 1 CE 07 176YV 15065 148 UE176 BATTERY CHARGE LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED BATTERY TO CLEAR DISCREPANCY. THIS BATTERY CHARGE LIG HT ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS. 2 L 7 2 4T 3 T RT A24CE E2NE 2007013100116 20070131 00116 SO 2007 1 31 07006 1 20070125 A 7713 HOSE PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA RT ENGINE BROKEN E DGCA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 27316 317752142 L237468A PILOT NOTICED A DECREASE IN MANIFOLD PRESSURE ON THE RT ENGINE. LANDED AIRCRAFT, AND CALLED DOM FOR INSTRUCTIONS. MAINT ENANCE FOUND UPPER DECK PRESSURE HOSE BROKEN. NEW HOSE WAS INSTALLED. RAN AND OPS, CHECKED GOOD. 1 L 7 2 3O 3 O A20SO E14EA 2007013100118 20070131 00118 SO 2007 1 31 DGCA0707006 1 20070125 A 7713 HOSE PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA RT ENGINE BROKEN E DGCA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 27316 317752142 L237468A PILOT NOTICED A DECREASE IN MANIFOLD PRESSURE ON THE RT ENGINE. LANDED AIRCRAFT, AND CALLED DOM FOR INSTRUCTIONS. MAINT ENANCE FOUND UPPER DECK PRESSURE HOSE BROKEN. NEW HOSE WAS INSTALLED. RAN AND OPS, CHECKED GOOD. 1 L 7 2 3O 3 O A20SO E14EA 2007013100122 20070131 00122 NM 2007 1 31 AWXA200700131 1 20070121 A 5311 69429862 FRAME BOEING 737 7373S3 1384711 NM BS 810 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 MCN - AFT CARGO COMPARTMENT FRAME CRACKED, BS 810, S26R. REPLACED AFT CARGO COMPARTMENT FRAME CRACKED, BS 810, S26R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007013100124 20070131 00124 CE 2007 1 31 DXTA200701856 1 20070115 A 3260 15500004 DOWNLOCK SWITCH CESSNA 560 560XL 2076702 CE RT MLG INTERMITTENT E DXTA K NONE N FALSE WARNING TO TAKEOFF 1 GL 07 654QS 935 5605611 DURING APPROACH INTO ASE RT LANDING GEAR WAS SLOW TO EXTEND BUT DID LOCK NORMALLY , DURING DEPARTURE RT GEAR WOULD NOT I NDICATE RETRACTED. GREEN RT STAYED ILLUMINATED. EXTENDED THE GEAR NORMALLY AND LANDED. (M2B) INSTALLED AND ADJUSTED NEW RT MAIN ACTUATOR DOWNLOCK SWITCH ON REPAIRED RT MAIN LANDING GEAR ACTUATOR IAW COMPONENT MM CH 32-32-14. OPS CHECKED G OOD IAW MM CH 32-00-50. 2 L 7 2 4F RT A22CE 2007013100128 20070131 00128 NM 2007 1 31 2007UALA00202 1 20070126 A 5230 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CARGO DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 181UA 25278 AFT MANUAL PIT DOOR, TWO DEEP DENTS APPROX 8" AFT OF FWD EDGE AT MID POINT IN DOOR. INSTALLED EXTERNAL DOUBLER REF SRM. CREATED MF5469 TO MONITOR & CALL-OUT VISUAL RECHECK EVERY 250 CYCLES, EDDY CURRENT RECHECK EVERY 1500 CYCLES. & REPAIR NEXT SCHEDULED MAJOR MAINT CHECK. SUSPECT IMPACT WITH GROUND EQUIPMENT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007013100129 20070131 00129 NM 2007 1 31 2007UALA00203 1 20070125 A 3397 FEEDER CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 331UA 24192 AFT SECTION EEL LIGHTS ARE FAULTY. REPLACED CABLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007013100130 20070131 00130 CE 2007 1 31 DXTA200701858 1 20070116 A 3260 65430087 UPLOCK SWITCH CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE NLG MALFUNCTIONED E DXTA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 GL 07 699QS 4887 5605199 AFTER RAISING LANDING GEAR ON TAKEOFF GEAR UNLOCK LIGHT REMAINED ON. ((3) OTHER GEAR INDICATORS BLANK). HYD PRESS ANNUN ILLUMINATED. UPON RAISING FLAPS TO 0 DEG, STAP MIS COMP CAME ON AND STAYED ON, WITH HYD PRESS ANNUNCIATOR. LOWERED GEAR: 3 GREEN, NO RED .LOWERED FLAPS : STAB MISCOMPARE WENT OUT, ALL ANNUNCIATORS EXTINGUISHED.ACCOMPLISHED A NORMAL LANDING.T ROUBLESHOT TO NOSE GEAR UPLOCK SWITCH P/N 65-430087 S/N N/A. INSTALLED NEW SWITCH P/N 65-430087 S/N N/A. OPS CHECK GOOD. WORK DONE IAW CESSNA 560XL MM CH 32-30-05 2 L 7 2 4F 4 F RT A22CE E00059EN 2007013100131 20070131 00131 EU 2007 1 31 2007UALA00204 1 20070126 A 3350 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 403UA 442 DURING EMERGENCY LIGHT TEST FOUND MESSAGE UNIT EMER L. REPLACED BATTERY PACK AT DOOR 1L. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007013100138 20070131 00138 NM 2007 1 31 2007UALA00211 1 20070125 A 5797 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WS 300 CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 595UA 28748 LEFT WING AFT SPAR BAY, WS 300, WIRING BUNDLE CHAFING HARD AGAINST HYD B-NUT, OUTER SHIELD ON BUNDLE IS TORN. REROUTE D WIRE BUNDLE TO ENSURE ADEQUATE SEPARATION AND REPLACED OUTER SHIELD FOR BETTER PROTECTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007013100141 20070131 00141 NE 2007 1 31 2007UALA00213 2 20070122 A 7261 OIL SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 659UA 27114 717655 DURING CLIMB TO FL 350 QTY DECREASED TO 0 CURRENTLY LEVEL AT FL350 SHOWING 0 OIL QTY L ENG. 2 L 7 2 4F 4 F RT A1NM E24NE 2007013100143 20070131 00143 2007 1 31 2007UALA00215 4 20070126 A 2565 D31591478U1 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU UNSERVICEABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 FOUND SLIDE TUBE BLOWN. CAUSE UNKNOWN. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007013100144 20070131 00144 CE 2007 1 31 DXTA200701881 1 20070126 A 3260 WARNING SYSTEM RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP COCKPIT ACTIVATED E DXTA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 07 838QS 258338 AT 300FT ON FINAL, GOT GPWS WARNING (TOO LOW GEAR, PULL UP). NOSE GEAR INDICATOR WENT BLANK. DID EMERG PROCEDURES INCL UDING PULLING GPWS AND HORN C/BS. DID LOW FLY BY TOWER TO CONFIRM GEAR DOWN. ON WAVEOFF DID AGRESSIVE PULLUP. NOSEGEAR I NDICATOR WENT BLANK TO GREEN. ALL SECONDARY INDICATORS (PIN AND AUX MAIN INDICATORS) INDICATED DOWN THROUGHOUT. TROUBLE SHOT SYSTEM. SUSPECT MOISTURE IN THE LEG LOCK MICROSWITCH OR CHANGEOVER SWITCH. REPLACED BOTH SWITCHES I.A.W. HS 125-800 XP MM RIGGED SWITCHES & SAFETIED GEAR OPS CK SATISFACTORYREF CH 32-60-00 PG 502 PG 504. 2 L 7 2 4F 4 F RT A3EU E6WE 2007013100146 20070131 00146 WP 2007 1 31 DXTA200701871 2 20070121 A 7230 BEARING CESSNA 750 750 2076810 CE GARRTT TFE731 TFE7315BR WP ENGINE DAMAGED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 936QS 7500036 STRONG FUMES IN THE COCKPIT, NO VISIBLE SMOKE. FUMES STRONGEST WITH ENGINE POWER HIGH. FUMES ARE LOCALIZED IN COCKPIT AREA NOT NOTICEABLE IN CABIN AREA. NO DIVERT. INSTALLED LT ENGINE NEW FAN SHAFT, BEARING AND SEAL IAW ROLLS ROYCE MM 7 2-21-20. RAN AIRCRAFT AT POWER. NO FUMES NOTED SYSTEM OPS CHECK GOOD. CLEANED WATER SEPERATORS AND SOCKS. KRBW TO KA PF. 2 L 7 2 4J 4 F RT T00007WI E6WE 2007013100152 20070131 00152 NE 2007 1 31 DXTA200701832 2 20070102 A 7320 CONNECTOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE DIRTY E DXTA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 07 695QS 5605293 DURING TAKEOFF THERE WAS A LARGE THROTTLE SPLIT AND TOOL, A LOT OF RT RUDDER TO MAINTAIN DIRECTIONAL CONTROL. RESET FAU LT, DISCONNECTED, CLEANED AND INSPECTED, RECONNECTED WIRING HARNESS IAW MM 73-20-02. PERFORMED ENGINE GROUND RUN. NO DE FECTS NOTED. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007013100156 20070131 00156 SO 2007 1 31 GUUA01240701 1 20070124 A 3397 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN LOOSE A GUUA K NONE L NO TEST IN INSP/MAINT 1 SO 29 261AS 120141 AT SCHEDULED ROUTINE MAINTENANCE FOUND LT AND RT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. SECURED LOOSE CONNECTION AT THE LT ACM AREA OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 2007013100157 20070131 00157 SO 2007 1 31 GUUA01260701 1 20070126 A 3230 20700 SPRING EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE NLG DOWNLOCK STICKING A GUUA O OTHER J WARNING INDICATION DE DESCENT 1 SO 29 266AS 120188 9210 FLL/NAS DURING APPROACH NOSE LANDING GEAR (A) AND (B) LIGHTS INDICATE GEAR UNSAFE. RETURNED, LANDED WITHOUT INCIDE NT. REPLACED NOSE LANDING GEAR DOWNLOCK SPRING CARTRIDGE OPERATIONAL CHECK NORMAL TEST FLIGHT SATISFACTORY. 2 L 7 2 4T 4 T RT A31SO E20NE 2007013100158 20070131 00158 CE 2007 1 31 GUUA01160702 1 20070116 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FUSELAGE CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 17541 UE203 AT SCHEDULED INSPECTION DISCOVERED 2 CRACKS AT NR 2 COMM ANTENNA (FS400) 1 CRACK 5.5 INCHES RUNNING LONGITUDINALLY FORWA RD FROM FS 403 THE OTHER CRACK 1.5 INCHES LONG RUNNING LONGITUDINALLY FORWARD FROM FS 397. STOP DRILLED CRACKS AND INST ALLED EXTERNAL REINFORCEMENT DOUBLER IAW STRUCTURAL REPAIR MANUAL 51-70-06. 2 L 7 2 4T 4 T RT A24CE E26NE 2007013100161 20070131 00161 EA 2007 1 31 COMA0760064 1 20070125 A 2420 IDG CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE UNKNOWN A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 477CA 7670 FLIGHT 5690 - LEFT ENGINE IDG CAUTION MESSAGE ILLUMINATED ON TAKEOFF ROLL AT 40 KTS. TAKEOFF ABORTED AND RETURNED TO GA TE. TRANSFERRED TO DMI LIST (24-11-01-1). 2 L 7 2 4F RT A21EA 2007091800125 20070918 00125 NM 2007 9 18 AALA20071639 1 20070829 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 772AN 29580 NRT - EMERGENCY LIGHT AT PILOTS BUNK INOPERATIVE. REPAIRED EMERGENCY LIGHT AT PILOTS BUNK. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT T00001SE 2007013100164 20070131 00164 NM 2007 1 31 2007UALA00105 1 20070110 A 3150 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU UNKNOWN UNKNOWN A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 329UA 24149 MASTER CAUTION ANNUNCIATOR BAT C-B POPS. LOCATED AT P6-3 PANEL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007013100172 20070131 00172 NM 2007 1 31 2007UALA00146 1 20070121 A 4920 ENGINE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU APU CONTAMINATED A UALA O OTHER C F.O.D. CR CRUISE 1 WP 29 332UA 24193 CREW REPORTS STILL HAVE SMELL OF BURNING PLASTIC NOTICED IN-FLIGHT USING BOTH ENG BLEEDS ON LEFT PACK. FOUND PLASTIC BA G STUCK TO APU COMPRESSOR INLET SCREEN. REMOVED BAG. 2 L 7 2 4F 4 F RT A16WE E21EU 2007013100173 20070131 00173 EU 2007 1 31 2007UALA00147 1 20070121 A 3350 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 410UA 463 FOUND EMERGENCY LIGHT TEST FAILED AT 3SV. REPLACED LEFT OVERWING EMERGENCY EXIT EPSU BATTERY. EMERGENCY LIGHT TEST PAS SED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007013100174 20070131 00174 NM 2007 1 31 2007UALA00149 1 20070119 A 3350 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 825UA 980 EMERGENCY LIGHTS BATTERY CAPACITY TEST REQUIRED. REPLACED EPSU BATTERIES AS ALTERNATE PROCEDURE TO CAPACITY TEST. 2 L 7 2 4F 4 F RT A28NM E40NE 2007013100175 20070131 00175 2007 1 31 2007UALA00150 4 20070121 A 2565 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ESCAPE SLIDE NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 428UA 523 EMERGENCY LIGHT TEST FAILED LEFT FWD DOOR SLIDE. FAULT READS EXT LOAD FWD LEFT. REPLACED DOOR 1L SLIDE PACK. EMERGENC Y LIGHT TEST OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007013100176 20070131 00176 EU 2007 1 31 2007UALA00151 1 20070121 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 484UA 1609 FAILED CABIN EMERGENCY LIGHTS TEST. EMERGENCY LIGHTS OPERATION CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007013100178 20070131 00178 2007 1 31 2007UALA00152 4 20070120 A 2565 COVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE 2L DOOR SLIDE DISLODGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 444UA 824 DOOR 2L SLIDE FELL OFF. SLIDE DID NOT FALL OFF. COVER WAS LOOSE AND WAS SECURED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007013100179 20070131 00179 NM 2007 1 31 2007UALA00154 1 20070119 A 3350 POWER SUPPLY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 521UA 24891 EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY POWER SUPPLY AND CHARGER ASSEMBLY, AND BATTERY PACK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007013100180 20070131 00180 2007 1 31 2007UALA00155 4 20070121 A 2565 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 L-2 CABIN DOOR, ARM HANDLE HARD TO ENGAGE. ADJUSTED GIRT BAR MECHANISM WHICH FIXED THE DISCREPANCY. NO COMPONENTS NEEDED TO BE REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007013100184 20070131 00184 NM 2007 1 31 2007UALA00159 1 20070120 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 674UA 29242 EEL LIGHTS FROM SEAT ROW 37HJ AND BACK ARE INOP. REPLACED BATTERY PACK AND EEL OPS CHECKS NORMALLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007013100188 20070131 00188 NM 2007 1 31 2007UALA00162 1 20070120 A 3350 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 FOUND WALL EEL INOP, LT SIDE LAV 111 AND BTWN MID LAVS. WALL EEL INOP ON LT SIDE LAV 111. ALSO IN OP BETWEEN MID LAVS. FOUND DISCONNECTED CONNECTER, RESECURED, CHKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007013100190 20070131 00190 NM 2007 1 31 2007UALA00163 1 20070120 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 FOUND EEL INOP, SEAT 5J AFT SECTION, ROW 25 RT AND CEILING ROW 37 RT. REPLACED LAMPS AT SEAT 5J AFT, ROW 25 RIGHT HAND SIDE & CEILING ROW 37 RIGHT HAND SIDE. ALL EEL LIGHTS OP CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007013100191 20070131 00191 NM 2007 1 31 2007UALA00164 1 20070120 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 FOUND WALL EEL INOP, LT SIDE MID GALLEY. FOUND LOOSE CONNECTOR ON WALL EEL, LH SIDE MID GALLEY. RESECURED, CHKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007013100192 20070131 00192 NM 2007 1 31 2007UALA00165 1 20070115 A 3350 LENS BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 225UA 30554 EMERGENCY LIGHT ON SEAT 2E MOVEABLE ARMREST IS DAMAGED. LENSE HAS BROKEN OFF. REPLACED LENS & LAMP ASSY. OP CHECKED O K. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007013100194 20070131 00194 NM 2007 1 31 2007UALA00166 1 20070122 A 3320 RELAY BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 310UA 23671 AFT GALLEY LTS, WINDOW AND SIDEWALL LIGHTING WHEEL WELL LIGHTS, WING ILLUMINATION LIGHTS AND EMERGENCY EXIT LIGHTS ARE I NOPERATIVE ON APU GENERATOR AND ENGINE GENERATOR POWER. ALSO, THE NORMAL EQUIPMENT COOLING FAN IS INOP. EXCEPT WHEN EX TERNAL POWER IS CONNECTED. FOUND BROKEN LUG ON R6 RELAY . 2 L 7 2 4F 4 F RT A16WE E21EU 2007013100195 20070131 00195 CE 2007 1 31 012107N338CS1 1 20070121 A 3297 MS27467T9F35S CONNECTOR CESSNA 500 550 2076604 CE PWA 530 PW530A NE LANDING GEAR FAULTY E Z5FA L B ABORTED APPROACH EMER. DESCENT O OTHER AP APPROACH 1 NE 03 338CS 2481 5501084 ON APPROACH, CREW NOTICED LT MLG DOWN/LOCK LIGHT OUT. ABORTED APPROACH, CONFIRMED LT MLG WAS PHYSICALLY DOWN. DIVERTED, DECLARED EMERGENCY, FOLLOWED AFM EMERGENCY PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE STAFF FOUND LT DOWN AND LOCK CONNECTOR TO BE WET WITH WATER. DISCONNECTED ALL AFFECTED CONNECTORS AND CLEANED, RECONNECTED AND OPERATIONAL CHEC KS PERFORMED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 4F 4 F A22CE E00053EN 2007013100196 20070131 00196 2007 1 31 SWAA070411 4 20070126 A 2565 63551101 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 255WN 32513 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATED OUT OF LIMITS. REMOVED AND REPLACED E VAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007013100197 20070131 00197 NM 2007 1 31 SWAA070412 1 20070126 A 3350 417A5600 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 428WN 29844 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED EEPLS ASSY PER MM. 2 L 7 2 4F RT A16WE 2007013100198 20070131 00198 NM 2007 1 31 SWAA070426 1 20070126 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN BETWEEN ROW 3 DEF AND 5 DEF. REMOVED AND REPLACED ST RIP PER MM. 2 L 7 2 4F RT A16WE 2007013100199 20070131 00199 NM 2007 1 31 SWAA070427 1 20070126 A 5315 6546811 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 47 TO LBL 5. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007013100200 20070131 00200 NM 2007 1 31 SWAA070428 1 20070126 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2007013100201 20070131 00201 NM 2007 1 31 SWAA070429 1 20070126 A 5311 6546558 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007013100202 20070131 00202 NM 2007 1 31 SWAA070430 1 20070126 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007013100203 20070131 00203 NM 2007 1 31 SWAA070431 1 20070123 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 250WN 34972 DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER MISSING AT ROW 15 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007013100204 20070131 00204 NM 2007 1 31 SWAA070432 1 20070126 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 270WN 29089 DURING SCHEDULED MV1 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007013100205 20070131 00205 NM 2007 1 31 SWAA070433 1 20070126 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 704SW 27838 DURING SCHEDULED MV2 CHECK, FOUND LEFT AFT CABIN EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007013100206 20070131 00206 NM 2007 1 31 SWAA070434 1 20070127 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 603SW 27954 R1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007013100207 20070131 00207 2007 1 31 SWAA070435 4 20070127 A 2565 1061323468 SLIDE BOEING 737 737301 1384611 NM L1 DOOR INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 L1 DOOR EMERGENCY EVAC SLIDE INOP. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007013100208 20070131 00208 NM 2007 1 31 SWAA070436 1 20070127 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 431WN 29845 EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007013100209 20070131 00209 NM 2007 1 31 SWAA070437 1 20070127 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007013100210 20070131 00210 NM 2007 1 31 SWAA070438 1 20070127 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007013100211 20070131 00211 NM 2007 1 31 SWAA070439 1 20070127 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, STR 25R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007013100212 20070131 00212 NM 2007 1 31 SWAA070440 1 20070127 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007013100213 20070131 00213 NM 2007 1 31 SWAA070441 1 20070127 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, BL 0. REPAIRED SKIN P ER SB AND EA. 2 L 7 2 4F RT A16WE 2007013100214 20070131 00214 NM 2007 1 31 SWAA070442 1 20070127 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 748, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007013100215 20070131 00215 NM 2007 1 31 SWAA070443 1 20070127 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 738E, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007013100216 20070131 00216 NM 2007 1 31 SWAA070444 1 20070127 A 5551 6551524 FITTING BOEING 737 7373H4 1384600 NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND RT AND LT HORIZONTAL STAB FITTING CLEVIS LUG FACES CORRODED. REPAIRED STAB FITTING PE R ACO. 2 L 7 2 4F RT A16WE 2007013100217 20070131 00217 NM 2007 1 31 SWAA070445 1 20070127 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 286WN 02471 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 2 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007013100218 20070131 00218 NM 2007 1 31 SWAA070446 1 20070127 A 3350 8200048401 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 437WN 29832 DURING SCHEDULED MV3 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT L1 DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007013100219 20070131 00219 NM 2007 1 31 SWAA070447 1 20070127 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007013100220 20070131 00220 NM 2007 1 31 SWAA070448 1 20070127 A 5311 6546526 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007013100221 20070131 00221 NM 2007 1 31 SWAA070449 1 20070127 A 5311 6546550 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007013100222 20070131 00222 NM 2007 1 31 SWAA070450 1 20070127 A 5311 6546555 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007013100223 20070131 00223 NM 2007 1 31 SWAA070451 1 20070128 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007013100224 20070131 00224 NM 2007 1 31 SWAA070452 1 20070128 A 5311 6546533 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007013100225 20070131 00225 NM 2007 1 31 SWAA070413 1 20070126 A 3350 307IBPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 485WN 32473 DURING SCHEDULED MV3 CHECK, FOUND EEPLS INOP AT ROW 6 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007013100226 20070131 00226 NM 2007 1 31 SWAA070414 1 20070126 A 3350 GE1317 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 716SW 27850 DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 6 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007013100227 20070131 00227 NE 2007 1 31 SWAA070415 2 20070126 A 7200 CFM567B ENGINE BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B22 13802 NE RIGHT VIBRATION A SWAA K NONE E VIBRATION/BUFFET CR CRUISE 1 SW 29 748SW 29800 875814 FELT STRONG VIBRATION CLIMBING THROUGH FL 235 AND FL 270 FOR 5 SECONDS EACH, THEN AT CRUISE FL 380. VIBRATION 2 TO 3 M INUTES. DURING FERRY FLIGHT TO DAL, CONFIRMED VIBRATION COMING FROM NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007013100228 20070131 00228 NM 2007 1 31 SWAA070416 1 20070126 A 3350 GE1317 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 780SW 27885 DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 23 ABC. REMOVED AND REPLACED LIGHT BULB PE R MM. 2 L 7 2 4F RT A16WE 2007013000001 20070130 00001 SO 2007 1 30 C2XA07CL016 1 20070128 A 3350 78241 INVERTER EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14940 145033 DURING ROUTINE MAINTENANCE THE NR 2 AND NR 3 AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND RE PLACED THE NR 2 INVERTER AND THE NR 2 AISLE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2007013000002 20070130 00002 NM 2007 1 30 KCSA071048 1 20070125 A 5411 FRAME BOEING 747 747209F 1384800 NM NR 4 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 NR 4 PYLON ENGINE MOUNT BULKHEAD FRAME IS CRACKED 1 INCH FORWARD SIDE, INBOARD OF PYLON UPPER SPAR CHORD AT NAC STA 221. 9 2 L 7 4 4F RT A20WE 2007013000007 20070130 00007 EA 2007 1 30 REXA200700007 1 20070126 A 2750 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS UNKNOWN A REXA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 25 8974C 7974 FLAPS FAIL AT ZERO DEGREES. RESET FLAPS AND MONITOR FOR 72 HRS PER AD2006-12-21. 2 L 7 2 4F RT A21EA 2007013000009 20070130 00009 EA 2007 1 30 REXA200700000 1 20070126 A 2750 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FALSE ACTIVATION A REXA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 25 8458A 7458 FLAPS FAIL MESSAGE ON TAXI OUT. COMPLIED WITH AD2006-12-21, NO DISCREPANCIES NOTED. MONITORING FLAPS FOR 72 HOURS. 2 L 7 2 4F RT A21EA 2007013000011 20070130 00011 EA 2007 1 30 REXA200700011 1 20070128 A 2750 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS UNKNOWN A REXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 8672A 7672 FLAPS FAILED AT ZERO DEGREES. COMPLIED WITH AD2006-12-21. RESET FLAPS AND MONITORING FOR 72 HOURS. 2 L 7 2 4F RT A21EA 2007013000025 20070130 00025 EU 2007 1 30 07FDEA00192 1 20070127 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 CRACK IN FLOORBEAM UNDER CLS ADAPTER AT FRAME 36 BETWEEN TRACK 3L AND 4L (SEEN FROM FWD CARGO PIT). REMOVED AND REINSTA LLED FLOOR PANEL TO FOM IAW A310-200 AMM SUPP 53-10-25-4. REMOVED AND REINSTALLED CLS ADAPTER IAW A310-200 SRM 51-40-21 . REMOVED CRACK IAW SRM SUPP 53-10-15 FIG 201 SHT 2. FABRICATED, LOCATED, AND DRILLED REPAIR ANGLES IAW A310 SRM SUPP 53-10-15. INSTALLED REPAIR IAW A310-200 SRM 51-40-21. REPROTECTED AREA IAW A310 SRM 51-75-10. 2 L 7 2 4F RT A35EU 2007013000035 20070130 00035 NM 2007 1 30 UPS07448984 1 20070105 A 5320 65B0794114 STIFFENER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C NWW TOP PANEL AREA FOUND 1EA STIFFENER CRACKED AT BS 290 RBL 20 AS MARKED. NWW TOP PANEL AREA 1EA STI FFENER REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007013000045 20070130 00045 WP 2007 1 30 UPS07848976 1 20070103 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C2 CORROSION OUT OF LIMITS ON LONGERON L35R STA 50-70. REMOVED LONGERON L35R AT STA 50-70 IAW SRM 51-1- 21. FABRICATED AND INSTALLED LONGERON L35R AT STA 50-70 IAW DWG 3702969, AND SRM 51-1-21, AND 51-1-20D. 2 L 7 4 4F RT 4A25 2007013000048 20070130 00048 WP 2007 1 30 UPS07848980 1 20070104 A 5320 577384443 ATTACH ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD TO LONGERON INTERCOSTAL ATTACH ANGLE CRACKED AT STA 1766 L6R. REMOVED, FABRICA TED AND INSTALLED ATTACH ANGLE IAW SRM 51-1-21, 51-3-2, 51-20D AND DWG 5773844. 2 L 7 4 4F RT 4A25 2007013000052 20070130 00052 NM 2007 1 30 KCSA071053 1 20070128 A 5315 FLOORBEAM BOEING 747 747209F 1384800 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 MAIN DECK BS 480 FLOORBEAM UPPER CHORD CORRODED AT LBL 59. 2 L 7 4 4F RT A20WE 2007013000055 20070130 00055 SO 2007 1 30 C2XA07SH007 1 20070128 A 3350 276005 FUSE EMB 145 EMB145LR 3260212 SO BATTERY PACK BLOWN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 19966 145131 RIGHT OUTBOARD FWD EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED BLOWN FUSE ON NR 2 EMERGENCY LIGHT BATTERY PACK IAW RA DIANT POWER CORP CMM 25-60-03, OPS CHECK GOOD. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007013000062 20070130 00062 NM 2007 1 30 KCSA071046 1 20070125 A 5411 FRAME BOEING 747 747209F 1384800 NM NR 1 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 NR 1 PYLON REAR ENGINE MOUNT BULKHEAD FRAME IS CRACKED 1 INCH, FORWARD SIDE, INBOARD & OUTBOARD OF PYLON UPPER SPAR CHOR D AT NAC STA 221.9. 2 L 7 4 4F RT A20WE 2007013000069 20070130 00069 NM 2007 1 30 CALA0700031 1 20070124 A 3350 FUSE BOEING 757 757224 1384958 NM BATTERY CHARGER BLOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 19130 28970 THE EMERGENCY AISLE PATH LIGHTING WAS FOUND INOPERATIVE FROM ROW 7 TO ROW 14. THE BATTERY CHARGER FUSE ABOVE 9DEF WAS R EPLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A2NM 2007013000072 20070130 00072 NM 2007 1 30 KCSA071050 1 20070125 A 5411 FRAME BOEING 747 747209F 1384800 NM NR 1 PYLON GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 NR 1 PYLON INTERNAL FRAME IS GOUGED AT NAC STA 194, WL 150, ABOVE MID SPAR AREA. 2 L 7 4 4F RT A20WE 2007013000086 20070130 00086 NM 2007 1 30 SB07009 1 20070127 A 3350 1012721 LIGHT BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 512AU 23595 CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHT ON SEAT ROW 15, LEFT-HAND SIDE WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007013000088 20070130 00088 NM 2007 1 30 USAA200701005 1 20070123 A 5414 SKIN BOEING 737 7374B7 1384702 NM RT PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 A .5 INCH CRACK FOUND ON PYLON SKIN AT RIGHT ENGINE PYLON OPENING FOR PANEL 5827R. 2 L 7 2 4F RT A16WE 2007013000114 20070130 00114 NM 2007 1 30 UPS07448985 1 20070102 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FX STA 1171 FAIRING SUPPORT FRAME FOUND CORRODED AT LBL 49. FX BS 1171 LBL 49 FAIRING SUPPORT REPAIRE D AS PER SRM 53-50-04 FIG 2. 2 L 7 4 4F A20WE 2007013000122 20070130 00122 NM 2007 1 30 UPS07449007 1 20070110 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D RBL 97 SEAT TRACK BS 1500-1584 CORRODED. CORROSION BLEND OUT 0.040 X .75 X 3 INCHES EXCEED SRM LI MIT. M/D SEAT TRACK REPAIRED AT BS 1480-1590 RBL 97 AS PER SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2007013000127 20070130 00127 NM 2007 1 30 UPS07449012 1 20070122 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C AFT OF BULK CARGO COMPT STR 32R BETWEEN BS 2200 TO BS 2220 FOUND 1EA HOLE CRACK AS MARKED (AFTER SKIN TRIMMED OFF) CRACK LENGTH .125 INCH. AFT OF BULK CARGO COMPT BETWEEN BS 2181 TO BS 2220 STR 32R REPAIRED AS PER SRM 53- 10-03 FIG 1. 2 L 7 4 4F A20WE 2007013000131 20070130 00131 NM 2007 1 30 UPS07449017 1 20070109 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO BS 820-840 S34R FOUND CRACKED AS MARKED. FWD CARGO COMPT BS 742 TO BS 830 STR 34R REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007013000135 20070130 00135 NM 2007 1 30 UPS07449021 1 20070105 A 5320 65B1406111 SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FX - KEEL BEAM FAIRING SUPPORT LOWER SURFACE FOUND CORROSION AT STA 1405 TO STA 1416 LBL 16. CORROSIO N BLEND OUT 0.017 X .5 X 10 INCHES EXCEED SRM LIMIT. SUPPORT REPLACED AS PER SRM 51-10-01 PG 9. 2 L 7 4 4F A20WE 2007013000143 20070130 00143 NM 2007 1 30 UPS07449029 1 20070110 A 5320 69B621001 PLATE BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D - BS 1760 FLOOR SUPPORT PLATE RBL 50-55 CORRODED. CORROSION BLEND OUT 0.045 X .5 X 1 INCH EXCEED SRM LIMIT. SUPPORT PLATE REPLACED AS PER SRM 53-40-00. 2 L 7 4 4F A20WE 2007013000147 20070130 00147 WP 2007 1 30 UPS07848996 1 20070104 A 5313 DC8553B0093 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 LONGERON CRACKED AT STA 1766 L14R. REMOVED CRACKED LONGERON, FABRICATED & INSTALLED REPLACEMENT LONG ERON AND 2 EA REPAIR SPLICES IAW SRM 53-05-0, 51-02-00, 53-02-02, 51-3-0, 51-1-20D. 2 L 7 4 4F RT 4A25 2007013000167 20070130 00167 WP 2007 1 30 ABXA070021 1 20070112 A 5730 5911300502 SKIN DOUG DC9 DC941 302207N WP RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 RIGHT WING UPPER SKIN BULGED AT REMOVEABLE TRAILING EDGE AND PANEL NR 1252. REPAIRED RIGHT WING UPPER SKIN BULGE ON TRA ILING EDGE PANEL IAW DC9 SRM 51-10-4. 2 L 7 2 4F A6WE 2007013000177 20070130 00177 NM 2007 1 30 07FDEA00056 1 20070109 A 3210 ARC28271 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LANDING GEAR: LT LDG AT FLIPPER DOOR FWD SIDE FOUND CRACKED. LANDING GEAR, LT LDG AT FLIPPER DOOR FWD SIDE REPAIRED AS PER SRM 52-10-00 VOLUME I, FIGURE 18. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007013000178 20070130 00178 NM 2007 1 30 07FDEA00195 1 20070129 A 5330 SKIN BOEING 727 727233 138408A NM BS 720D-720E CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 RT EXT FUSE SKIN AT FILLET FRG PANEL INTERFACE IS FRETTED BS 720D 10 TO 720E, STR 19R TO 4" ABOVE STR 18R REMOVED LEADIN G EDGE FOR ACCESS TO REPAIR. INSTALLED EXTERNAL REPAIR AT LAP SPLICE REF SRM 53-30-3 PG 20. REINSTALLED LEADING EDGE A ND LEAKED CHECKED HYD LINES. REF 27-81-000-2 AND LEAK CHECKED TAI DUCT REF WO NR 35039/WC NR 70C53-00. 2 L 7 3 4F RT A3WE 2007013000195 20070130 00195 2007 1 30 AMTA200700040 4 20070127 A 3460 COMPUTER BOEING 737 73783N 13844HI NM COCKPIT MALFUNCTIONED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 318TZ 28247 L FMC FAILED AFTER ETP. INSPECTED AND OPS CHECK PER AMM 34-61-00. NO FAULT NOTED. (M) 2 L 7 2 4F RT A16WE 2007013000202 20070130 00202 NM 2007 1 30 HALA0700039 1 20070128 A 5730 PANEL BOEING 767 767332 1382001 NM RT WING DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23276 FOUND RT WING PANEL 611CB LEADING EDGE AND RIGHT WING SLAT LOWER INBOARD CLOSEOUT PANELS DAMAGED. REMOVED AND REPLACED RT WING PANEL 611CB AND RT WING SLAT LWR CLOSEOUT PANEL SECURITY CHECK OKAY. 2 L 7 2 4F RT A1NM 2007013000204 20070130 00204 2007 1 30 HALA0700038 4 20070128 A 3460 COMPUTER BOEING 767 76733A 1385209 NM COCKPIT FAILED A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 589HA 33422 BTB - ETOPS SIGNIFICANT SYSTEM ICAS MESSAGE (R) FMC FAIL. FMC FAILED AFTER ENGINE START, RETURNED TO GATE. SWAPPED POS ITION OF LT AND RT FMC COMPUTERS. MSG CLEARED. OPS CK NOW OK. FMC'S LEFT IN SWAPPED POSITIONS. 2 L 7 2 4F RT A1NM 2007013100002 20070131 00002 SO 2007 1 31 SIMA200703010 1 20070126 A 5313 145641319001 STRINGER EMB 135 EMB135KL 3260302 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 850AE 9246 4800 145722 FOUND STRINGER 19L CHAFED BETWEEN FRAMES 52 AND 53. REMOVED DAMAGE BY BLENDING, PERFORMED NDT OF AREA. FABRICATED DOUB LER AND SHIMS, INSTALLED REPAIR PIECES IAW EMB SRM 53-24-02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007013100014 20070131 00014 SO 2007 1 31 SIMA200703003 1 20070128 A 3350 744436 LIGHT EMB 145 EMB145LR 3260212 SO RT OVERWING FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 679AE 6737 14500814 RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT IAW EMB 33-50-00. OPERATIONAL CH ECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007013100017 20070131 00017 SO 2007 1 31 SIMA200703006 1 20070127 A 5315 14530645411 FLOORBEAM EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 805AE 13051 4800 145489 FOUND LEFT OMEGA BEAM CORRODED AT FRAME 25. PERFORMED CUTOUT OF DAMAGE, FABRICATED REPAIR PIECES. INSTALLED REPAIR PIE CES IAW EMB SRM 53-00-10. RESTORED PROTECTIVE FINISH. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007013100042 20070131 00042 EU 2007 1 31 AALA20070111 1 20070117 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7062A 474 MIA - EMERGENCY LIGHT AT SEAT 2D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 2D. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F RT A35EU 2007013100043 20070131 00043 WP 2007 1 31 AALA20070120 1 20070118 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 406A 49317 MSP - EMERGENCY LIGHT EXIT SIGNS ABOVE OVERWING FORWARD LEFT AND RIGHT DOORS INOPERATIVE. REPLACED BATTERY PACK FOR EME RGENCY LIGHT EXIT SIGNS ABOVE OVERWING FORWARD LEFT AND RIGHT DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007013100045 20070131 00045 NM 2007 1 31 AALA20070122 1 20070118 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 399AN 29606 DFW - EMERGENCY LIGHT ASSEMBLY LOOSE AT SEAT 25H. RESECURED EMERGENCY LIGHT ASSEMBLY AT SEAT 25H. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007013100047 20070131 00047 NM 2007 1 31 DL757070059 1 20070126 A 3340 3015269 LIGHT BOEING 757 757232 1384965 NM ANTICOLLISION BROKEN A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 602DL 22809 ON ARRIVAL TO GATE, FOUND LOWER ANTI COLLISION BEACON LIGHT LENS BROKEN. REPLACED LIGHT ASSY. 2 L 7 2 4F RT A2NM 2007013100049 20070131 00049 CE 2007 1 31 JEM2007F00001 1 20070102 A 3210 RIVET BEECH 200 200BEECH 1152920 CE PWA PT6 PT6* 52043 EA RT MLG BROKEN E JEMA K NONE O OTHER IN INSP/MAINT 1 CE 01 376RC 10071 BB376 FOUND LOOSE AND BROKEN RIVETS IN THE RT MLG DRAG LEG SUPPORT AND CHANNEL. RIVETS ON BOTH THE IB AND OB SIDES OF THE SUP PORT WERE EITHER MISSING THE MACHINE HEADS AND WORKING THEIR WAY OUT OR WERE FOUND TO BE BROKEN IN HALF, BUT STILL IN TH EIR RESPECTIVE PLACES. THE GEAR WAS OPERATING NORMALLY AND NO OTHER DAMAGE WAS DISCOVERED. THE SITUATION WAS MOST LIKE LY CAUSED BY AIRCRAFT AGE, RIVET FATIGUE AND GEAR BEING EXTENDED OR RETRACTED AT TOO HIGH OF AN AIRSPEED. (K) 1 L 7 2 4T 3 T A24CE E2NE 2007013100056 20070131 00056 NM 2007 1 31 AALA20070102 1 20070116 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39365 24046 DFW - EMERGENCY LIGHT AT OVERHEAD ROW 39 RIGHT SIDE INOPERATIVE. RELAMPED OVERHEAD EMERGENCY LIGHT AT ROW 39 RIGHT SID E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007013100096 20070131 00096 EA 2007 1 31 SWIA200717765 1 20070128 A 5610 NP1393221 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA O OTHER O OTHER DE DESCENT 1 NM 07 611SK 10035 THE INTERIOR PANE OF THE CAPTAIN'S SIDE WINDOW CRACKED WHILE DESCENDING INTO DFW. REPLACED LEFT SIDE WINDOW IAW RII 56- 220-1000, S/N OFF: 01131H7735. 2 L 7 2 4F RT A21EA 2007013100097 20070131 00097 EU 2007 1 31 DHL2007362514 1 20070106 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 CABIN SEAT TRACK FLANGE BETWEEN FR 40 THRU FR 45 AT LBL 56 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK SECTION FROM FR 40 TO FR 45.5 AT LBL 56 IAW A300 SRM 51-41-00, 51-40-12, 51-30-30. 2 L 7 2 4F RT A35EU 2007013100098 20070131 00098 NM 2007 1 31 QXEA200700118 1 20070130 A 3010 4100S01806 CONTROL UNIT BOMBDR DHC8 DHC8402 1390042 NM DEICE SYS MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 408QX 2079 4050 BTM FLIGHT NR 2381: DEICE TIMER CAUTION LIGHT ILLUMINATED ON TAXI OUT. RETURNED TO GATE. MAINTENANCE REMOVED AND REPLA CED TMCU IAW AMM Q400 TASK 30-11-01-000-801 AND INSTALLED IAW TASK 31-11-01-400-801. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007013100109 20070131 00109 NM 2007 1 31 07FDEA00200 1 20070130 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 420 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 FLOORBEAM HAS OPEN HOLES AT BS 420 ACCOMPLISHED EA NR 7-5330-106980 PART 1, TO COMPLETE WO NR 35039/N01471. INSTALLED R IVETS IN ALL OPEN HOLES, PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007013100123 20070131 00123 EA 2007 1 31 COMA0760067 1 20070126 A 2750 1104SD100501 SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAP DAMAGED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 931CA 7037 FLAP FAIL MESSAGE RECEIVED ON APPROACH AT ZERO DEGREES. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REMOVED AND RE PLACED NR 5 LEFT WING FLEX SHAFT. 2 L 7 2 4F RT A21EA 2007013100127 20070131 00127 EU 2007 1 31 2007UALA00201 1 20070125 A 5101 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE AIRFRAME VIBRATION A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 435UA 613 A/C VIBRATION FELT ON CLIMB-OUT 3 TIMES. CHECKED ELEVATOR FOR FREE PLAY, RIGHT SIDE HAD ENOUGH PLAY TO WARRANT REPLACEM ENT OF YELLOW SERVO CONTROL. AFTER REPLACEMENT OF SERVO CONTROL PLAY WAS WITHIN STANDARDS. OPS CHECKED GOOD. ACCOMPLI SHED INSTALLATION INSPECTION OF REPLACED SERVO, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007013100133 20070131 00133 NM 2007 1 31 2007UALA00206 1 20070126 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L1 DOOR SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 FOUND EMERGENCY LIGHTS AT DOOR 1L SLIDE ILLUM, ROW 34 ABC AND ROW 46 HJK ARE INOPERATIVE. REPLACED LT ASSY AT EACH POSI TION. ALL OP CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007013100134 20070131 00134 NM 2007 1 31 2007UALA00207 1 20070126 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EEL AT 2A AFT AND 55 HJK ARE INOPERATIVE. CONNECTOR LOOSE AT ASSY JUNCTION. RETIGHTENED. OP CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007013100135 20070131 00135 NM 2007 1 31 2007UALA00208 1 20070126 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L2 DOOR SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 FOUND EMERGENCY LIGHT AT DR 2L SLIDE ILLUMINATED INOPERATIVE. EMERGENCY LT AT DR 2L SLIDE ILLUM INOP. BATTERY PACK LOST CHARGE. AFTER CHARGING EEL CKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007013100136 20070131 00136 NM 2007 1 31 2007UALA00209 1 20070126 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. RELAMPED BOTH SIDES; OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007013100145 20070131 00145 NM 2007 1 31 DXTA200701876 1 20070125 A 3620 WARNING SYSTEM GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE BLEED AIR SYS ACTIVATED E DXTA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 07 712QS 073 L BLEED AIR MESSAGE ILLUMINATED IN FLIGHT AS DIRECTED BY THE CHECKLIST THE LT ENGINE WAS SHUTDOWN BY CREW BECAUSE THE ME SSAGE REMAINED ON AFTER X-LIST ITEMS WERE COMPLETED SIDE NOTE ENGINE EVENT BUTTONS WERE PRESSED ABOUT 45 SECONDS AFTER M ESSAGE ILLUMINATED. T/S GAINED ACCESS TO LEFT BLEED AIR DUCTING. NO DEFECTS NOTED. RANG OUT FIRELOOP & CONTROL BOXES. N O DEFECTS NOTED. PER GAC TECH REP SWAPPED CONTROL BOXES. RAN ACFT AT T/O POWER. NO DEFECTS NOTED PER TECH OPS. REMOVED A ND REPLACED THE LEFT BLEED LEAK DETECT LOOP AND THE CONTROL BOX WITH A NEW LOOP AND NEW BOX. RAN ACFT. OPS CHECK GOOD I/ A/W G-200 M/M 21-61-00. REINSTALLED ACCESS ITEMS. 2 L 7 2 4F 4 F RT A53NM E35NE 2007013100162 20070131 00162 EA 2007 1 31 COMA0760065 1 20070126 A 5753 1104SD100301 SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS BENT A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 924CA 7026 FLIGHT 5564 - RECEIVED FLAP FAIL MESSAGE AT ZERO DEGREES ON APPROACH. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED RIGHT SIDE FLEX SHAFTS NR 3. 2 L 7 2 4F RT A21EA 2007013100163 20070131 00163 NM 2007 1 31 2007UALA00064 1 20070107 A 7920 5007436C PUMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OIL TANK FAILED A UALA D RETURN TO BLOCK M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 WP 29 511UA 24799 RED OIL TEMP ON NR 2 ENGINE EICAS INDICATION. ACFT RETURNED TO BLOCKS. INSPECTED OIL TANK, FOUND OIL IN TANK BELOW LI P, DRAINED APPROX 2 GALLONS FROM GEARBOX. REPLACED LUBE AND SCAVENGE OIL PUMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007013100167 20070131 00167 NM 2007 1 31 2007UALA00143 1 20070119 A 2150 SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT PACK TEMP INOPERATIVE A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 570UA 26678 RTFL DUE TO A FLIGHT DECK TEMPERATURE CONTROL PROBLEM. LEFT PACK WAS FOUND INOP. CREW TOOK SNAPSHOT FOR MAINTENANCE T RIED USING LEFT BLEED TO RIGHT PACK TO ISOLATE IF BLEED TEMP WAS CAUSE. REPLACED RT PACK TEMP SENSOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007013100177 20070131 00177 EA 2007 1 31 COMA0760062 1 20070125 A 7830 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER UNKNOWN A COMA C ABORTED TAKEOFF J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 807CA 7364 FLIGHT 5457- DURING TAKEOFF ROLL RECEIVED A LEFT THRUST REVERSER UNLOCK MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GAT E. DEFERRED THE LEFT THRUST REVERSER PER MEL 78-30-01. 2 L 7 2 4F RT A21EA 2007013100229 20070131 00229 NM 2007 1 31 SWAA070417 1 20070126 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER 28L CORRODED AT BS 497. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007013100230 20070131 00230 NM 2007 1 31 SWAA070418 1 20070126 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 492, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007013100231 20070131 00231 NM 2007 1 31 SWAA070419 1 20070126 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 497, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007013100232 20070131 00232 NM 2007 1 31 SWAA070420 1 20070126 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007013100233 20070131 00233 NM 2007 1 31 SWAA070421 1 20070126 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007013100234 20070131 00234 NM 2007 1 31 SWAA070422 1 20070126 A 5340 65C2714 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 348, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007013100235 20070131 00235 NM 2007 1 31 SWAA070423 1 20070126 A 5753 6546486 WEDGE BOEING 737 7373H4 1384600 NM T/E FLAP DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND LEFT WING INBOARD MID FLAP T/E WEDGE LOWER T/E OUTBOARD END DISBONDED. REPAIRED MID F LAP PER SRM. 2 L 7 2 4F RT A16WE 2007013100237 20070131 00237 NM 2007 1 31 SWAA070424 1 20070126 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED C2 CHECK, FOUND RIGHT WING NR 6 L/E SLAT CRACKED AT LOWER INBOARD T/E END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007013100238 20070131 00238 NM 2007 1 31 SWAA070425 1 20070126 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007013100239 20070131 00239 EA 2007 1 31 COMA0760069 1 20070126 A 5753 1104SD100401 SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS DAMAGED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 931CA 7037 FLIGHT 5164 - FLAP FAIL MESSAGE RECEIVED ON APPROACH AT ZERO DEGREES. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 4 LEFT WING FLEX SHAFT. 2 L 7 2 4F RT A21EA 2007013100243 20070131 00243 EA 2007 1 31 COMA0760078 1 20070126 A 2752 854D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 SO 01 675BR 7617 7635 FLIGHT 5425 - RECEIVED FLAP FAIL CAUTION MESSAGE. DIVERTED FROM LGA TO JFK. LANDED WITHOUT INCIDENT. REPLACED RIGHT O UTBOARD FLAP OUTBOARD ACTUATOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007013100245 20070131 00245 NM 2007 1 31 07FDEA00210 1 20070131 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 480 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 MAIN DECK FLOORBEAM UPPER FLANGE IS CORRODED AT BS 480, LBL 10, WL 208. BLENDED OUT CORRODED AREA, ROTO PEENED AREA, WI THIN ALLOWABLE LIMITS REF SRM 51-10-02. TREATED, PRIMED, REF WRI NR 53108450, EA 7-5310-106968, WRI 53108465, EA 7-5310 -106968. CLASSIFIED AS MAJOR. 2 L 7 3 4F RT A3WE 2007013100246 20070131 00246 WP 2007 1 31 07FDEA00211 1 20070131 A 5310 DOOR FRAME DOUG DC10 DC1010 3022110 WP BS 1306-1317 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 INTERNAL FUSELAGE AFT MAIN CABIN AT STA 1306 TO STA 1317 LONGS 26 LT AND 27 LT DOOR JAMB FRAME FOUND EXISTING DOUBLER RE PAIR. PERFORMED GVI ON REPAIR NOT IN COMPLIANCE WITH EO NR 8-5100-7-5001 P2 AND REPAIR FASTENERS WITH SRM 53-50-00 FIG 19 SHT 2 VOL 1. REMOVED EXISTING DOUBLER IAW SRM 51-30-00 AND INSTALLED NEW REPAIR IAW SRM 53-50-00 FIG 19 VOL 1. FABR ICATED PARTS IAW DETAIL PARTS TRAVELER I026147/N01147 AND IAW SRM 53-50-00 VOL1 FIG 19. 2 L 7 3 4F A22WE 2007013100248 20070131 00248 WP 2007 1 31 07FDEA00213 1 20070131 A 5710 BULKHEAD DOUG DC10 DC1010 3022110 WP WS 402 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 XORS 402 UPPER BULKHEAD CAP IS CRACKED BELOW STR NR 15, NR 3 TANK. ACCOMPLISHED EA NR 8-5710-99377. 2 L 7 3 4F A22WE 2007013100251 20070131 00251 WP 2007 1 31 07FDEA00216 1 20070131 A 5753 SKIN DOUG DC10 DC1010 3022110 WP TE FLAP UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 RT WING I/B FLAP LOWER SKIN FWD I/B OF HINGE AT STA XIFH 255, EXISTING DOUBLER REPAIR. NEW REPAIR INSTALLED IAW SRM 57-1 0-00 FIG 86 VOL 1. RUB STRIP INSTALLED IAW DWG ARC3007. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01106 AND SRM 57-1 0-00 VOL1 FIG 86 AND DWG ARC3007. REINSTALLED PNL IAW MM 20-50-02. 2 L 7 3 4F A22WE 2007013100253 20070131 00253 WP 2007 1 31 07FDEA00218 1 20070131 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP BS 939 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 FWD CARGO COMPT AT STA 939 X= 38 EXISTING ANGLE REPAIR IN FLOORBEAM. REMOVED CHANNEL AS REQUIRED IAW SRM 51-30-00 VOL 2 , CUTTED FLOORBEAM AT X= 22. INSTALLED REPAIR IAW SRM 53-60-01 FIG 3 VOL 1. REINSTALLED CHANNEL IAW SRM 51-30-00 VOL 2 . FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01198 AND SRM 53-60-01 VOL1 FIG 3. 2 L 7 3 4F A22WE 2007013100254 20070131 00254 NM 2007 1 31 07FDEA00219 1 20070131 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 360 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 MAIN DECK FLOORBEAM UPPER FLANGE IS CORRODED BS 360, LBL 8, WL 208. BLENDED CORROSION AT STA 360, LBL 8. ROTO PEENED, TREATED AND PRIMED AREA. REF WRI NR 53108448, EA 7-7310-106965. CLASSIFIED AS MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007013100258 20070131 00258 EA 2007 1 31 COMA0760077 1 20070126 A 2750 1104SD100101 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAP DAMAGED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 815CA 7397 FLIGHT 5620 - RECEIVED FLAP FAIL MESSAGE AT 8 DEGREES. DECLARED EMERGENCY, FOLLOWED QRH AND LANDED WITHOUT INCIDENT. R EPLACED LEFT WING NR 1 FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2007013100260 20070131 00260 NM 2007 1 31 07FDEA00207 1 20070131 A 5347 SEAT TRACK BOEING 727 727233 138408A NM BS 620 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 MAIN DECK FLOOR SEAT TRACK IS CORRODED BS 620, LBL 1, WL 208. REMOVED DAMAGED SEAT TRACK, FAB SEAT TRACK, TRANSFERRED H OLES TO NEW TRACK. INSTALLED NEW TRACK REF SRM 51-30-2. ALODINE TRACK REF SRM 51-10-2 PG 7 PRIME TRACK REF MM 51-20-15 1. CLASSIFIED AS MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007013100262 20070131 00262 EA 2007 1 31 COMA0760079 1 20070126 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 507CA 7796 FLIGHT 5080 - FLAP FAIL MESSAGE RECEIVED AT ZERO DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE "FIRST EVENT " MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A,B,C) FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2007013100264 20070131 00264 EA 2007 1 31 COMA0760081 1 20070127 A 2750 1104SD100101 SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS DAMAGED A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 797CA 7344 FLIGHT 5421 - FLAP FAIL MESSAGE AT 8 DEGREES. REPLACED NR 1 FLEX DRIVE, LEFT SIDE. 2 L 7 2 4F RT A21EA 2007013100265 20070131 00265 EA 2007 1 31 COMA0760071 1 20070126 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 986CA 7174 FLIGHT 5505 - RECEIVED FLAP FAIL CAUTION AT 42 DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (G) 1,2,3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2007013100267 20070131 00267 EA 2007 1 31 COMA0760073 1 20070126 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 785CA 20558 7326 FLIGHT 5206 - RECEIVED FLAP FAIL MESSAGE AT 8 DEGREES. LANDED WITHOUT INCIDENT. REPLACED PDU. 2 L 7 2 4F RT A21EA 2007013100268 20070131 00268 EA 2007 1 31 COMA0760074 1 20070126 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 806CA 7359 FLIGHT 5528 - RECEIVED FLAP FAIL CAUTION MESSAGE AT 20 DEGREES. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. COMPLI ED WITH AD 2006-12-21 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (G) 1,2,3, (A, B, C). FLAP SYSTE M WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2007013100269 20070131 00269 EA 2007 1 31 COMA0760075 1 20070126 A 2750 1104SD100101 SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS DAMAGED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 806CA 7359 FLIGHT 5145 - RECEIVED FLAP FAIL CAUTION MESSAGE AT 0 DEGREES. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACE D LEFT SIDE NR 1 FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2007020100003 20070201 00003 NM 2007 2 1 SWAA070468 1 20070130 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 967 S22L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 22L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007020100005 20070201 00005 NM 2007 2 1 SWAA070479 1 20070130 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007020100007 20070201 00007 NM 2007 2 1 SWAA070482 1 20070130 A 5753 65522112 TORQUE TUBE BOEING 737 7373H4 1384600 NM LT TE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE T UBE PER MM. 2 L 7 2 4F RT A16WE 2007020100008 20070201 00008 NM 2007 2 1 SWAA070471 1 20070130 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 766 S11L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 766, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007020100012 20070201 00012 EA 2007 2 1 COMA0760103 1 20070130 A 5350 FAIRING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE LOOSE A COMA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 420CA 7451 FLIGHT 7451 - AFTER TAKEOFF FROM CVG A LOUD RUMBLING NOISE WAS EMANATING FROM UNDER THE FLOOR AREA, FLIGHT RETURNED TO C VG FOR INVESTIGATION. RESEALED THE BELLY FAIRINGS. 2 L 7 2 4F RT A21EA 2007020100016 20070201 00016 EA 2007 2 1 COMA0760097 1 20070128 A 2752 853D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA LT OB FLAP FAILED A COMA O OTHER O OTHER DE DESCENT 1 SO 01 987CA 11423 7199 FLIGHT 5396 - FLAPS FAIL AT 0 DEGREES. A/C LANDED SAFELY. REMOVED AND REPLACED FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2007020100017 20070201 00017 EA 2007 2 1 COMA0760100 1 20070130 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 924CA 7026 FLIGHT 5532 - FLAPS FAIL ON APPROACH. FAILED AT 20 DEGREES. A/C LANDED SAFELY. COMPLIED WITH AD 2006-12-21 FLAP CAUTI ON MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FL AP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007020100020 20070201 00020 NM 2007 2 1 SWAA070473 1 20070130 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727A S6L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007020100022 20070201 00022 NM 2007 2 1 SWAA070475 1 20070130 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727D S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007020100023 20070201 00023 NM 2007 2 1 SWAA070476 1 20070130 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 807 S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007020100026 20070201 00026 NM 2007 2 1 SWAA070455 1 20070128 A 5743 69378771 FITTING BOEING 737 7375H4 138449D NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED MV2 CHECK, FOUND LT MLG WALKING BEAM OUTBOARD FWD STABILIZER FITTING CORRODED. REPAIRED FITTING PER SW A EA. 2 L 7 2 4F RT A16WE 2007020100027 20070201 00027 NM 2007 2 1 SWAA070454 1 20070128 A 5743 69378772 FITTING BOEING 737 7375H4 138449D NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED MV2 CHECK, FOUND RIGHT MLG WALKING BEAM OUTBOARD FWD STABILIZER FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2007020100028 20070201 00028 NM 2007 2 1 SWAA070453 1 20070128 A 5743 6959886Y2 FITTING BOEING 737 7375H4 138449D NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED MV2 CHECK, FOUND RT MLG AFT HANGER FITTING CORRODED. REMOVED AND REPLACED AFT FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007020100044 20070201 00044 NM 2007 2 1 UPS07549045 1 20070105 A 5412 311N32712 BULKHEAD BOEING 757 75724APF 1384969 NM NR 1 PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 417UP 23904 INSPECTION TYPE:C NR 1 PYLON AFT BULKHEAD INBOARD AND OUTBOARD SIDE LOWER AREA CHAFED. ACCOMPLISHED PER FINAL EA 757-54 53-27-A1592 AND UPS EO B757-5410- 26011. 2 L 7 2 4F RT A2NM 2007020100045 20070201 00045 EA 2007 2 1 COMA0760088 1 20070128 A 2760 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILERS UNKNOWN A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 816CA 7398 FLIGHT 4940 - AFTER RTO BELOW 50 KTS WHEN THRUST LEVERS WERE RETARDED, RECEIVED CONFIG SPOILER MESSAGE. RESET SPOILER S YSTEM PER FIM. RTO BELOW 80 KTS, NO INSPECTION REQUIRED. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007020100046 20070201 00046 EA 2007 2 1 COMA0760087 1 20070128 A 2420 755469B IDG CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 815CA 30368 7397 FLIGHT 5117 - RECEIVED IDG NR 1 CAUTION DURING 2 TAKEOFF ATTEMPTS AT 85 PERCENT N1. REPLACED NR 1 IDG, NO FURTHER DEFEC TS. 2 L 7 2 4F RT A21EA 2007020100047 20070201 00047 EA 2007 2 1 COMA0770010 1 20070127 A 5220 DOOR CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT UNKNOWN A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 668CA 10162 FLIGHT 5032 - ON TAKEOFF ROLL RIGHT EMERGENCY DOOR MESSAGE CAME ON. ABORTED TAKEOFF AND RETURNED TO GATE. TRANSFERRED TO DMI LIST 52-70-03. 2 L 7 2 4F RT A21EA 2007020100050 20070201 00050 EA 2007 2 1 COMA0760095 1 20070126 A 3230 617501 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG WW FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 932CA 30810 7038 FLIGHT 5608 - NOSE GEAR SLOW TO EXTEND. NOSE GEAR DOES NOT SOUND NORMAL WHEN EXTENDING AND LOCKING. GEAR DISAGREE MESS AGE RECEIVED THEN WENT 3 GREEN AFTER A MINUTE. LANDED WITHOUT INCIDENT. REPLACED MAIN LANDING GEAR SELECTOR VALVE AND GEAR CONTROL HANDLE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007020200002 20070202 00002 NM 2007 2 2 DHL2007783005 1 20070130 A 5297 WIRE BOEING 727 727227 1384078 NM DOOR WARNING BROKEN A DHLA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 SO 01 783DH 21999 FWD ENTRY DOOR ANNUNCIATOR DOES NOT ILLUMINATE WITH DOOR OPEN LIGHT TESTS OK. REPAIRED 3(EA) BROKEN WIRES AT T-7000 BUR NED BLOCK BEHIND F/E TABLE IAW B727 WAD 52-71-01 PG 31 SYS OPS CHECKED GOOD IAW B727 MM 52-70-01. 2 L 7 3 4F A3WE 2007020200005 20070202 00005 NM 2007 2 2 USAA070070 1 20070130 A 5310 65C3760727 VERTICAL BEAM BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 589US 23934 FOUND CRACK LT VERTICAL BEAM BETWEEN 5.7 LBL AND WL 184. REMOVED CRACK VERTICAL BEAM AND INSTALLED REPAIR KIT CPN 11311 56 PER EO 5300V155, DEFECT SIZE: 2". 2 L 7 2 4F RT A16WE 2007020200007 20070202 00007 CE 2007 2 2 DXTA200701898 1 20070131 A 2120 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CABIN ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 908QS 7500108 BURNING SMELL COMING FROM OUTSIDE THE LT AFT FUSELAGE. (NEAR TAILCONE AND NR 1 ENGINE). ACRID AND OILY CONSISTENCY. R AN APU & BOTH ENGINES FOR A PERIOD OF 30 MINS. INSPECTED LEFT AFT FUSELAGE, NR 1 AND 2 ENGINES FOR ANY LEAKS AND NONE WE RE NOTED. OPENED TAIL CONE DOOR, INSPECTED APU & ECU FOR LEAKS AND ALSO NO DEFECTS WERE NOTED. COULD NOT DUPLICATE DISCR EPANCY. WORK ACCOMPLISHED IAW CESSNA CE750 MM CH 21-51-00, 71-00-04 AND 49-10-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007020200008 20070202 00008 NM 2007 2 2 C1HA200793002 1 20070129 A 5313 1498147 STRINGER BOEING 727 727212 138407G NM BS 740 S27R CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 FOUND CORROSION ON STR 27R AT BS 737 FWD PIT. REPAIRED STR 27R AT BS 737 - 740 IAW B727 SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2007020200012 20070202 00012 NM 2007 2 2 C1HA200793003 1 20070130 A 5320 WEB BOEING 727 727212 138407G NM BS 351 CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 NOSE WHEEL WELL HAS WEB CORRODED BEHIND NLG LOCK ACTUATOR SUPPORT BRACKET AT BS 351.2. REPAIRED NWW WEB AT BS 351.2 IAW B727 SRM 51-40-2 FIG 1 AND 53-10-2 FIG 1. 2 L 7 3 4F A3WE 2007020200014 20070202 00014 2007 2 2 SA07007 4 20070130 A 2565 GIRT BAR AIRBUS A319 A319112 3930323 EU PAX DOOR SLIDE DETACHED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 0997 DEN - THE FORWARD LEFT MAIN ENTRY DOOR EMERGENCY ESCAPE SLIDE GIRT BAR WAS FOUND DETACHED. MAINTENANCE SECURED THE GIRT BAR. OPERATIONALLY CHECKED OK. 2 L 7 2 4F RT A28NM 2007020200016 20070202 00016 WP 2007 2 2 0700429992 1 20070123 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 560-579 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8960E 45869 DURING "H" CHECK, FOUND CRACK IN FORWARD CARGO COMPARTMENT LONGERON AT S29L BETWEEN BS 560-579. REPAIRED PER EA 99-2084 33. 2 L 7 2 4F A6WE 2007020200018 20070202 00018 NM 2007 2 2 07FDEA00220 1 20070131 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 MAIN DECK FLOORBEAM UPPER FLANGE IS CORRODED BS 400, RBL 33, WL 208. BLENDED CORRODED AREA, WITHIN LIMITS REF SRM 53-10 -1, PG 22. ROTO PEENED AREA, TREATED AND PRIMED AREA, REFERENCE WRI NR 53108449, EA NR 7-5310-106967 CLASSIFIED AS MAJO R. 2 L 7 3 4F RT A3WE 2007020200021 20070202 00021 WP 2007 2 2 07FDEA00223 1 20070131 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 1505 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 RT MLG W/W FOUND 1 CRACK 2" LONG ON FRAME AT STA 1505 X= 96. REPLACED FRAME IAW SRM 51-35-01 VOL 2 AND DWG AEA0439 WITH NEW P/N AEA0439-4. 2 L 7 3 4F A22WE 2007020200022 20070202 00022 WP 2007 2 2 07FDEA00224 1 20070131 A 5754 SKIN DOUG DC10 DC1010 3022110 WP NR 2 SLAT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 LT WING SLAT NR 2 SCRATCH ON L/E SKIN FROM STA XIS 247 TO STA XIS 258. REPAIRED CARRIED OUT IAW SRM 57-10-00 VOL 1 FIG 43 AND SRM 57-10-00 VOL 1 FIG 29. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N00269 AND SRM 57-10-00 VOL1 FIG 29. 2 L 7 3 4F A22WE 2007020200023 20070202 00023 NM 2007 2 2 ASAA0741427 1 20070131 A 5210 SKIN BOEING 737 737490 1384715 NM L1 DOOR BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 THE L 1 DOOR EXTERNAL SKIN IS BENT AT THE UPPER AFT CORNER. CUTOUT THE DAMAGED AREA OF SKIN FABRICATED AND INSTALLED A SKIN FILLER AND AN EXTERNAL REPAIR DOUBLER IAW SRM 52 00 01 FIG 201. 2 L 7 2 4F RT A16WE 2007020200029 20070202 00029 CE 2007 2 2 DXTA200701878 1 20070125 A 2750 FLAP SYSTEM RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP TE FLAPS MALFUNCTIONED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED DE DESCENT 1 GL 07 836QS 258436 WHEN FLAPS SET AT 15 DEG AIRPLANE BANKS RT AT 5000FT AT 190KTS. RAN AND OPERATED FLAPS WITH PROTRACTOR. HOOKED UP TO BOT H FLAP'S. BOTH FLAPS WITHIN .1 DEGREE DURING OPERATION. RAN SPOILERS AND LIFT DUMP SEVERAL TIMES. NO PROBLEMS NOTED. IAW M/M 27-10 AND 27-50. 2 L 7 2 4F 4 F RT A3EU E6WE 2007020200030 20070202 00030 NM 2007 2 2 UPS07549050 1 20070104 A 5311 146N102848 FRAME BOEING 757 75724APF 1384969 NM BS 1240 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 417UP 23904 INSPECTION TYPE:C - FOUND AFT PIT STA 1240, STR 2526 FRAME DENTED, RIGHT SIDE DIMENSION OF DENT .020 FROM CENTER OF DENT TO TRANS PANEL 5"4 FROM CENTER OF DENT TO PRODUCTIONS SPLICE 9.8 LENGTH OF DENT .900 W= 1.0. TRIMMED OUT DENTED A REA PER EA NR 757-5362-27-A1595 L= 1", W= 1" ACCOMPLISHED ON FINAL EA 757-5362-A1595 AND UPS EO B757-5310-26022. 2 L 7 2 4F RT A2NM 2007020200033 20070202 00033 WP 2007 2 2 UPS07849041 1 20070126 A 3397 WIRE DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 FOUND EMERGENCY LIGHTS INOP. FOUND WIRE NR L610A20 BROKEN AT TOGGLE SWITCH. REPAIRED WIRE IAW DCI WDM 33-50-01. TOGGLE SWITCH REPLACED AS PRECAUTION IAW DC8 AMM 20-50-01-4. CHECKS SERVICEABLE IAW DC8 AMM 33-50-02-2. 2 L 7 4 4F RT 4A25 2007020200036 20070202 00036 WP 2007 2 2 UPS07849049 1 20070106 A 5320 STIFFENER DOUG DC8 DC871F 302199D WP FS 1944 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 - FOUND EMPENNAGE TAIL SECTION AT STA 1944 RT SIDE, HAT CHANNEL CROSS MEMBER STIFFENER HAS CRACK AT E ND. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2. REPAIR ANGLES IAW SRM 51-1-21, 53-02-00. 2 L 7 4 4F RT 4A25 2007020200038 20070202 00038 WP 2007 2 2 UPS07849053 1 20070104 A 5210 SKIN DOUG DC8 DC871F 302199D WP L1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 - FOUND EXT FUSE SKIN HAS 1/4" CRACKED AT L1 DOOR HOLD OPEN RECPT. REMOVED EDGE DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-02-00 FIG 001R, 51-3-0 AND EO DC8-5330-19684. 2 L 7 4 4F RT 4A25 2007020200040 20070202 00040 CE 2007 2 2 DXTA200701885 1 20070128 A 3233 55275043 ACTUATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG LOCK INOPERATIVE E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 699QS 818 5605199 UPON LANDING GEAR RETRACTION, GEAR DOWN GREEN LIGHTS GO OUT BUT RED LIGHT AND HYD PRESS LIGHTS REMAIN ON. REPLACED UPLOC K ACTUATOR AND RIGGED UPLOCK SWITCH IAW MM, CH - 32-30-05, LEAK AND OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007020200042 20070202 00042 NM 2007 2 2 ABXA070027 1 20070130 A 2910 O-RING BOEING 767 767281 1385109 NM HYD SYSTEM LEAKING A ABXA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 GL 23 774AX 22789 HYDRAULIC QUANTITY DECREASED TO .46 QTY STABLE WITH EDP DEPRESSURIZED ACMP OFF. OPENED COWLINGS, SERVICED RIGHT HYDRAUL IC SYSTEM IAW B767 MM. RIGHT ENGINE FOUND FLUID LEAK AT STRUT DISCONNECTOR, REPLACED O-RING. NO LEAKS NOTED. 2 L 7 2 4F RT A1NM 2007013000130 20070130 00130 NM 2007 1 30 UPS07449016 1 20070110 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 2152 LBL100 FLOOR SUPPORT FOUND CORRODED. CORROSION BLEND OUT 0.050 X .5 X 1 INCH EXCEED SRM L IMIT. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2, JUST AT LBL 100 BETWEEN BS 2130 AND 2160. 2 L 7 4 4F A20WE 2007013000136 20070130 00136 NM 2007 1 30 UPS07449022 1 20070109 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT STA 745 STRINGER S35L FOUND CRACK. CRACK LENGTH .25 INCH. FWD CARGO COMPT STA 740 TO BS 890 STR 35L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007013000139 20070130 00139 NM 2007 1 30 UPS07449025 1 20070109 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT STRINGER FOUND CRACK AT STA 880 S35L. CRACK LENGTH .375 INCH. FWD CARGO COMPT BS 740 TO BS 890 STR 35L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007013000145 20070130 00145 CE 2007 1 30 DXTA200701863 1 20070118 A 3340 LIGHT CESSNA 560 560XL 2076702 CE FIRE E DXTA K NONE A FLAME/FIRE IN INSP/MAINT 1 GL 07 631QS 5605131 LEFT LOGO LIGHT CAUGHT FIRE, EXTINGUSHED W/ FIRE RETARDANT. (TAIL WAS DEICED PRIOR TO INCIDENT) INSPECTED AREA & FOUND N O DAMAGE. REMOVED LIGHT ASSY & FOUND NO DAMAGE. SUSPECT DE-ICE FLUID REACHED ITS FLASH POINT OF 230 DEGREES F DUE TO TEM P OF LENS. FIRE RETARDANT WAS CLEANED FROM SURFACES BY JET BLAST CLEANING CO. LIGHT ASSY OPS CHECKED GOOD NO FAULTS NOTE D AT THIS TIME. ALL WORK DONE IAW CE560XL MM 2 L 7 2 4F RT A22CE 2007013000148 20070130 00148 EU 2007 1 30 TRAX200700056 1 20070109 A 2710 CONTROL CABLE AEROSP ATR72 ATR72212 8680945 EU AILERONS FRAYED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 635AS 372 AILERON SERVO AUTO PILOT CABLE FRAYING AND SERVO ACTUATOR DRUM DAMAGED. REFER TO EXELTECH WORK PACKAGE YUL000164 NRTC A ILERON AUTO PILOT ROLL ACTUATOR AND CABLES REMOVED IAW JIC 22-13-71 RAI 10000, AILERON SERVO AUTO PILOT CABLE AND SERVO ACTUATOR REPLACED IAW JIC 22-13-71 RA110000, AILERON SERVO AUTO PILOT ACTUATOR TESTED SERVICEABLE IAW AMM JIC 22-13-71 OPT 10000. 2 H 7 2 4T RT A53EU 2007013000160 20070130 00160 NM 2007 1 30 ASAA0741420 1 20070129 A 5753 SKIN BOEING 737 737490 1384715 NM T/E FLAP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 RIGHT I/B AFT FLAP IS DELAMINATED ON O/B EDGE LOWER SURFACE. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007013000205 20070130 00205 NM 2007 1 30 ASAA0711423 1 20070129 A 3260 655241921 SQUAT SWITCH BOEING 737 7372Q8 138448K NM MLG OUT OF ADJUST A ASAA D RETURN TO BLOCK O OTHER CL CLIMB 1 NM 02 741AS 21959 DURING TAKEOFF CLIMB MLG HANDLE FAILED TO RETRACT TO DETENT WITHOUT USING OVERRIDE BUTTON. MAINTENANCE FOUND WEIGHT ON WHEELS SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2007013000206 20070130 00206 EA 2007 1 30 TRAX200700118 1 20070122 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 901EV 7616 CEILING EMERGENCY LIGHT 1EA INOP. 2 L 7 2 4F RT A21EA 2007013000209 20070130 00209 EU 2007 1 30 TRAX200700121 1 20070123 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 643AS 413 EMERGENCY LIGHT STRIP NEXT TO SEAT 8B FAILS TO OPERATE. 2 H 7 2 4T RT 2007013000211 20070130 00211 EA 2007 1 30 TRAX200700123 1 20070125 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 824AS 7203 FLAPS FAILED MSG FLAPS FAILED AT 0 WHEN FLAPS SELECT TO 8, LANDED WITH ZERO FLAPS. AS A PRECAUTION EMERGENCY EQUIP ON S TANDBY. 2 L 7 2 4F RT A21EA 2007013100009 20070131 00009 SO 2007 1 31 C2XA07IA021 1 20070116 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO CABIN SMOKE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 14125 145690 IAH - DURING POST-FLIGHT INSPECTION THE CREW REPORTED A SMOKE/BURNING SMELL NEAR ROWS 16-18. MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DISCREPANCIES NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007013100010 20070131 00010 SO 2007 1 31 C2XA07IA022 1 20070128 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13988 145265 IAH - FLIGHT 2642, DURING PREFLIGHT INSPECTION THE CREW REPORTED THE AFT EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE RESET THE AFT EMERGENCY LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007013100015 20070131 00015 SO 2007 1 31 SIMA200703005 1 20070124 A 5315 14530645411 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 702AE 15957 4800 145164 FOUND LEFT OMEGA BEAM CORRODED AT FRAME 44. PERFORMED CUTOUT OF DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES IAW EMB SRM 53-00-10. RESTORED PROTECTIVE COATING, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007013100022 20070131 00022 EA 2007 1 31 COMA0760061 1 20070125 A 2740 3094334 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 960CA 7117 FLIGHT 5078 - DURING CLIMBOUT CAPTAIN SIDE STAB TRIM WOULD NOT MOVE IN THE DOWN POSITION. AIRCRAFT RETURNED BACK TO BOS AND LANDED SAFELY. REMOVED AND REPLACED CAPTAIN SIDE PITCH TRIM SWITCH. 2 L 7 2 4F RT A21EA 2007013100023 20070131 00023 EA 2007 1 31 COMA0760057 1 20070124 A 3010 6243843 SENSOR CNDAIR CL600 CL6002B19 1900309 EA LT WING FAILED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 409CA 16186 7441 FLIGHT 5276 - LEFT WING ANTI-ICE CAUTION MESSAGE DURING TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AN D REPLACED A LEFT WING TEMP SENSOR. 2 L 7 2 4F RT A21EA 2007013100027 20070131 00027 NE 2007 1 31 HALA0700037 2 20070127 A 7421 IGNITER BOEING 717 717200 1383700 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE INOPERATIVE A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 485HA 55130 BTB - NR 1 ENG WILL NOT START. REMOVED AND REPLACED IGNITER PLUG A NR 1 ENG, OPS AND LK CK OKAY PER AMM 74-20-04. 2 L 7 2 4F 4 F TR A6WE E24NE 2007013100031 20070131 00031 WP 2007 1 31 AALA20070118 1 20070118 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 964TW 53614 LGA - EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS CABI N. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007013100032 20070131 00032 WP 2007 1 31 AALA20070119 1 20070118 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 406A 49317 MSP - EMERGENCY LIGHT AT 19D AFT HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 19D AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007013100048 20070131 00048 NM 2007 1 31 DL76L070060 1 20070126 A 4920 38002981 TURBINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE APU UNKNOWN A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 178DN 21102 25143 P1969 APU AUTO SHUT DOWN. REPLACED APU. 2 L 7 2 4F 4 F RT A1NM E24NE 2007013100061 20070131 00061 EA 2007 1 31 ZFD2007F00000 2 20070116 A 7314 481824RG34720 PUMP PIPER PA42 PA42 7104202 SO PWA PT6 PT6A41 52043 EA ENGINE MALFUNCTIONED E ZFDA O OTHER O OTHER NR NOT REPORTED 1 GL 25 94EW 428001054 PILOT STATED THAT THE LT FUEL PRESSURE WOULD GO TO ZERO IF THE ELECTRIC PUMPS WERE TURNED OFF. FOUND AIRFRAME MFG INSTA LLED ENGINE DRIVEN PUMP INOPERATIVE.. THE PUMP DRIVE WAS FOUND TO BE SLIPPING. INSPECTED THE PUMP AND NO OTHER DEFECTS WERE NOTED. THE PUMP WAS REPLACED AND NO FURTHER PROBLEMS. (K) 1 L 7 2 4T 4 T A23SO E4EA 2007013100062 20070131 00062 NM 2007 1 31 QXEA200700113 1 20070129 A 5230 SWIVEL BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR OBSTRUCTED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 416QX 4083 SEA FLIGHT NR 2363: GROUND CREW UNABLE TO OPEN AFT CARGO DOOR. MAINTENANCE OPENED AFT CARGO DOOR AND FOUND DOOR SUPPORT ROD SWIVEL JOINT TO BE HITTING METAL TRIM PIECE ON THE FWD LWR DOOR SURROUND. ADJUSTED METAL TRIM PIECE FOR CLEARANCE FROM SUPPORT ROD SWIVEL JOINT. C/W OPS CHECK OF THE AFT CARGO DOOR IAW Q400 AMM TASK 52-31-00-710-801. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007013100070 20070131 00070 NM 2007 1 31 QXEA200700112 1 20070127 A 3213 UNKNOWN DHAV DHC8 DHC8202 2809007 NM NLG STRUT UNKNOWN A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 351PH 490 PDX FLIGHT NR 2125, LOUD SCRAPING THUD HEARD WHEN DISCONNECTING FROM TUG RAMP SAID NOSE WHEEL JERKED TO THE SIDE. MAINT ENANCE COMPLIED WITH GENERAL VISUAL INSPECTION OF NOSE STRUT ASSEMBLY. NO OBVIOUS DEFECTS NOTED. NO PARTS REPLACED. A IRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007013100076 20070131 00076 NM 2007 1 31 HALA0700025 1 20070113 A 8010 7755383 CONTROL VALVE BOEING 767 767300 1385204 NM RT ENGINE STUCK A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 586HA 15630 15630 24259 BTB - RT ENG STAT VALVE WILL NOT OPEN. REPLACED NR 2 START CONTROL VALVE PER AMM 80-11-02. LEAK CHECK GOOD START TEST GOOD. 2 L 7 2 4F RT A1NM 2007013100101 20070131 00101 NM 2007 1 31 07FDEA00199 1 20070130 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 380 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 FLOORBEAM HAS OPEN HOLE AT BS 380 ACCOMPLISHED EA NR 7-5330-106980 PART 1, TO COMPLETE WO NR 35039/N01472. INSTALLED RI VETS IN ALL OPEN HOLES. 2 L 7 3 4F RT A3WE 2007013100121 20070131 00121 NM 2007 1 31 07FDEA00205 1 20070126 A 5210 DOOR BOEING 727 727232 1384082 NM MALFUNCTIONED A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 498FE 20867 CREW ENTRY DOOR SHOWED CLOSED AND LOCKED WITH HANDLE FULL DOWN AND DOOR LIGHT OUT. AIRCRAFT WOULD NOT PRESSURIZE. RTB , UPON INITAL INSP FOUND ROLLERS ON AFT SIDE OF DOOR NOT IN TRACKS ON THE UPPER AND LOWER TRACK. UNABLE TO OPEN DOOR. AFTER OFF LOAD VISUALLY INSPECTED DOOR AND FOUND AFT LOWER ROLLER OUT OF POSITION. RAISED DOOR HANDLE WITH MINIMAL PRE SSURE AND DOOR OPENED. VISUALLY INSPECTED DOOR ROLLERS AND GUIDES NO PROBLEM NOTED. OPENED AND CLOSED DOOR A NUMBER OF TIMES WITH NO NOTICEABLE PROBLEMS OR EXCESS PRESSURE REQUIRED TO CLOSE DOOR. 2 L 7 3 4F A3WE 2007013100132 20070131 00132 NM 2007 1 31 2007UALA00205 1 20070126 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY LIGHT AT ROW 4 RT IS INOPERATIVE AND EMERG EXIT SIGN AT AFT CREW REST AREA LAMP IS DIM. RELAMPED ROW 4 RT EE L & EMERGENCY EXIT SIGN IN AFT CREW REST AREA. BOTH POSITIONS OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007013100142 20070131 00142 NM 2007 1 31 2007UALA00214 1 20070124 A 3510 OXYGEN BOTTLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CREW UNDERSERVICED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 659UA 27114 FOUND CREW OXYGEN PRESSURE BELOW LIMITS. SERVICED CREW OXYGEN CYLINDER. HOLDS PRESSURE; OK FOR RETURN TO SERVICE. SUSP ECT PERIODIC CHECKING BY CREW DEPLETES SUPPLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007013100148 20070131 00148 CE 2007 1 31 DXTA200701873 1 20070121 A 2740 TRIM SYSTEM CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE COCKPIT INOPERATIVE E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 631QS 5605131 ELECTRIC PITCH TRIM IS INOP ON BOTH PILOT AND COPILOT YOKES, DIVERTED. FOUND PILOTS AUTOPILOT DISENGAGE SWITCH FAILED. REMOVED AND REPLACED PILOTS AUTOPILOT SWITCH WITH NEW PERFORMED OPERATIONAL TEST. OPERATION TESTS GOOD. WORK DONE IAW CESSNA 560XL MM CH 27-10-05. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007013100149 20070131 00149 2007 1 31 DXTA200701874 4 20070122 A 2210 TRIM SYSTEM GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE AUTOPILOT SYS FAILED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 707QS 066 AUTOPILOT PITCH TRIM FAILED AFTER TAKEOFF WE WERE UNABLE TO CONTROL TRIM W/YOKE THUMB SELECTOR AUTOPILOT WAS FUNCTIONAL AFTER WE TRIMMED AIRCRAFT IN SECONDARY DISCONNECT POSITION TRIM BECAME SEMI FUNCTIONAL UPON ARRIVAL. TROUBLESHOT SYSTEM AND DETERMINED THAT TEH NR 2 HORIZONTAL TRIM ACTUATOR UNSERVICEABLE, WOULD NOT OPERATE INDEPENDANT OF NR 1 SYS TROUBLES HOOTING DONE PER G200 AMM CH 27-40-10. ORDERED, RECEIVED AND INSTALLED REPLACEMENT ACTUATOR. REMOVAL AND INSTALLATION DO NE PER CMP 274301 (REF SC104923.1.25). PERFORMED OPS CHECK. OPERATIONAL CHECK WAS GOOD. OPS CHECK DONE PER CMP (REF SC10 4923). FOR DETAILS SEE W/O SC104923. 2 L 7 2 4F 4 F RT A53NM E35NE 2007013100151 20070131 00151 CE 2007 1 31 DXTA200701870 1 20070118 A 3240 AC67732 CONTROL VALVE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP BRAKE SYSTEM FAULTY E DXTA K NONE O OTHER TX TAXI/GRND HDL 1 GL 07 805QS 4918 258505 WHEN BRAKING NOTHING HAPPENS UNTIL BRAKE HYD PRESSURE GAUGES READ 200 PSI THEN BRAKES GRAB HARD. SEEMS THE CAPTAINS BRAK E PEDALS ARE BAD, CO-PILOT'S SIDE BRAKES SEEM NORMAL.REMOVED AND REPLACED BRAKE CONTROL VALVE. ALL WORK DONE IAW MM. 2 L 7 2 4F 4 F RT A3EU E6WE 2007013100153 20070131 00153 NM 2007 1 31 DXTA200701880 1 20070125 A 3230 CIRCUIT CARD AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE NLG & MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 07 269QS 169 GEAR FAILED TO RETRACT ON TAKEOFF. WHEN GEAR HANDLE WAS RAISED, WE GOT TWO RED MAIN GEAR LIGHTS AND RT GREEN LIGHT. 10 SECS LATER WE HAD 2 RED MAIN GEAR DOOR LIGHTS, A FLASHING GEAR HANDLE AND 2 MAIN GEAR GREEN LIGHTS. FOLLOWED CHECKLIST A ND LOWERED GEAR. THEN HAD 3 GREEN LIGHTS AND NO RED LIGHTS AND NORMAL GEAR HANDLE LIGHT. TROUBLESHOT AND FOUND PCB CARD 417JE TO BE DEFECTIVE. REPLACED P.C.B. CARD 417JE WITH INSPECTED UNIT IN ACCORDANCE WITH F2000 SP 20-500. PERFORMED F UNCTIONAL TESTS OF EXTENSION AND RETRACTION IN NORMAL MODE WITH NO DEFECTS NOTED. 2 K 7 2 4F 4 F RT A50NM E44NE 2007013100170 20070131 00170 NE 2007 1 31 2007UALA00145 2 20070120 A 7261 OIL SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE LOW A UALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 562UA 26664 717951 FLIGHT DIVERTED DUE TO LOSS OF OIL PRESSURE AND OIL QUANTITY IN NR 1 ENGINE. ENGINE WIND-MILLED FOR 15 TO 20 MINUTES, N OTED THAT N2 WAS TURNING (ABOUT 17%) DURING WIND MILL. FOUND OIL IN TAIL PIPE. REPLACED NR 1 ENG. NO FAULTS ON ENGINE RUN. 2 L 7 2 4F 4 F RT A2NM E17NE 2007013100183 20070131 00183 NM 2007 1 31 2007UALA00158 1 20070120 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 674UA 29242 EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR INSIDE COCKPIT DOES NOT COME ON. REPLACED BATTERY PACK AND OPS CHECKS NORMALLY . 2 L 7 2 4F 4 F RT A1NM E24NE 2007013100187 20070131 00187 NM 2007 1 31 2007UALA00161 1 20070120 A 3350 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 FOUND EEL INOP ROW 34L. FOUND DISCONNECTED CONNECTOR, RESECURED, CHKS OK 2 L 7 4 4F 4 F RT A20WE E24NE 2007013100189 20070131 00189 CE 2007 1 31 011607N152CS1 1 20070114 A 3233 15419005 ACTUATOR CESSNA 525 525 2076601 CE WILINT FJ44 FJ44 66000 GL NLG FAULTY E Z5FA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 NE 03 152CS 2045 5250539 AFTER TAKE-OFF FROM SAT, CREW NOTICED POWER BRAKE FAIL AND POWER BRAKE PRESS LOW ANNUNCIATORS. CREW PERFORMED AFM PROCED URE CHECKS FOR THIS INDICATION WITH NO EFFECT. CREW DECLARED AN EMERGENCY AND RETURNED TO SAT FOR INSPECTION AND REPAIR OF FAULT.MAINTENANCE FACILITY FOUND FAULT TO BE WITH NOSE LANDING GEAR ACTUATOR, AFTER REPLACEMENT ANTISKID SYSTEM WORKE D SATISFACTORY WITH GEAR SWING. 1 L 7 2 4F 4 F RT A1WI E3GL 2007013100193 20070131 00193 NE 2007 1 31 011907N515CS1 2 20070119 A 7321 8237007 FUEL CONTROL CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE RT ENGINE FAILED E Z5FA B EMER. DESCENT X J H ENGINE FLAMEOUT WARNING INDICATION ELECT. POWER LOSS-50 PC AP APPROACH 1 NE 03 515CS 2472 1795 5605335 DB0682 ON APPROACH TO PSP,WHEN POWER INCREASE SELECTED, RT ENGINE FAILED TO RESPOND AND FLAMED OUT. ATTEMPTED TO RESTART UNSUCC ESSFULLY. DECLARED AN EMERGENCY, FOLLOWED AFM PROCEDURES FOR SINGLE ENGINE OPERATION. AIRCRAFT LANDING WAS UNEVENTFUL. MAINTENANCE PERSONNEL FOUND INTERNAL FAILURE OF FUEL CONTROL. REPLACED FUEL CONTROL ENGINE GROUND RUN GOOD, POST MAINTEN ANCE FLIGHT CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. FUEL CONTROL HAS BEEN RETURNED TO VENDOR FOR INSPECTION AND REPAI R. TEARDOWN REPORT HAS BEEN REQUESTED. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007013100242 20070131 00242 EA 2007 1 31 COMA0760076 1 20070126 A 2750 1104SD100301 SHAFT CNDAIR CL600 CL6002B19 1900309 EA LEFT WING #3 DAMAGED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 815CA 7397 FLIGHT 5620 - RECEIVED FLAP FAIL MESSAGE AT 8 DEGREES. DECLARED EMERGENCY, FOLLOWED QRH AND LANDED WITHOUT INCIDENT. R EPLACED LEFT WING NR 3 FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2007013100244 20070131 00244 NM 2007 1 31 07FDEA00209 1 20070131 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 480 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 MAIN DECK FLOORBEAM UPPER FLANGE IS CORRODED BS 480, LBL 38, WL 208. BLENDED CORROSION AT STA 480, LBL 38, ROTO PEENED, TREATED AND PRIMED AREA REF WRI NR 53108450, EA NR 7-5310-106968, WRI NR 53108465, EA NR 7-5310-106968 REV A. CLASSI FIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007013100247 20070131 00247 WP 2007 1 31 07FDEA00212 1 20070131 A 5310 BEAM DOUG DC10 DC1010 3022110 WP BS 570-577 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 NLG WW NOSE GEAR BEAM SUPPORT WEB AT STA 570 TO 577 Z= -40 RT SIDE, EXISTING DOUBLER WEB REPAIR. REMOVED AND SCRAPED REPAIR DOUBLERS AND STIFFENER IAW SRM 51-30-00 VOL 2, STRIPPED PAINT IAW SRM 51-21-01 VOL2 PAG 26. PERFORMED NDI SPM 06 , FOUND 7 CRACKS. TRIMMED OUT CRACKS AND INSTALLED FILLER, DOUBLERS, NEW NCA6046-116 STIFFENER IAW DWG NCA6046 AND SRM 53-30-00 FIG 6 SHT 3. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01210/I026210 -3, -5, -11 IAW SRM 53-30-00 VOL1 FIG 6 SHT 2, 3, 10. 2 L 7 3 4F A22WE 2007013100249 20070131 00249 WP 2007 1 31 07FDEA00214 1 20070131 A 5712 RIB DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 RT WING O/B FLAP UPPER SKIN AT STA XOF 563 AND STA XOF 569 EXISTING DOUBLERS REPAIR. REMOVED NR 4 DOUBLERS IAW SRM 51-3 0-00. REMOVED T/E SECTION IAW CMM 57-52-02. AFTER REMOVED DAMAGED SKIN FOUND RIB P/N ARC1905-4 WITH CRACK 2" LONG. PE RFORMED HFEL INSP IAW NDT SPM 06 AND NO CRACK FOUND. PERFORMED REPAIR DAMAGED AREA IAW SRM 57-10-00 FIG 7 VOL 1 AND REI NSTALLED T/E PANEL IAW CMM 57-52-02, SEALED T/E PNL IAW SRM 51-41-01 VOL 2. 2 L 7 3 4F A22WE 2007020100002 20070201 00002 NM 2007 2 1 C1HA200793001 1 20070129 A 5322 SHEAR TIE BOEING 727 727212 138407G NM BS 380 CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 FOUND CORROSION AT SHEAR TIE AT BS 380 I/B OF STR 28L. REMOVED CORROSION FOUND OUT OF LIMITS FAB DOUBLER REPAIR AND INS TALLED IAW B727 SRM 53-10-4 FIG 13. 2 L 7 3 4F A3WE 2007020100009 20070201 00009 NM 2007 2 1 SWAA070472 1 20070130 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727D S6L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007020100010 20070201 00010 EA 2007 2 1 COMA0760096 1 20070128 A 2752 853D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA LT OB FLAP FAILED A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 987CA 11423 7199 FLIGHT 5396 - FLAPS FAIL AT 0 DEGREES. A/C LANDED SAFELY. REMOVED AND REPLACED FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2007020100029 20070201 00029 NM 2007 2 1 SWAA070467 1 20070130 A 3350 MS155721 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED A1 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007020100043 20070201 00043 NM 2007 2 1 UPS07549043 1 20070105 A 5412 311N32712 BULKHEAD BOEING 757 75724APF 1384969 NM NR 2 PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 417UP 23904 INSPECTION TYPE:C NR 2 PYLON LOWER O/B CORNER OF MIDSPAR BULKHEAD IS HEAVILY CHAFED. ACCOMPLISHED PER FINAL EA 757-5453 -27-A1592 AND UPS EO B757-5410-26011. 2 L 7 2 4F RT A2NM 2007020100048 20070201 00048 EA 2007 2 1 COMA0770011 1 20070129 A 5512 SKIN PANEL CNDAIR CL600 CL6002C10 1390015 EA HORIZONTAL STAB CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 355CA 10067 RIGHT HORIZONTAL STABILIZER LOWER SKIN HAS A 3 INCH CRACK EMINATING O/B FROM THE O/B LOWER DRAIN HOLE O/B OF RIB 11. RE PAIRED DAMAGE IAW GENERIC REO 670-55-11-001. 2 L 7 2 4F RT A21EA 2007020200004 20070202 00004 EU 2007 2 2 200701301 1 20070126 A 2780 SLAT SYSTEM EMB ERJ170 ERJ170100SE 3260406 EU MALFUNCTIONED A UHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 17 638RW 170000053 FLIGHT 7624 ORD TO HPN - SLATS FAILED TO FULLY RETRACT. CREW FOLLOWED QRH, DID NOT RESOLVE THE ISSUE. DIVERTED TO IND. FLAPS 2 LANDING, SLATS WERE SLIGHT PAST A ZERO. NORMAL LANDING AND TAXI TO GATE. MAINTENANCE REPLACED THE NR 4 SLAT W512 HARNESS. STILL RESEARCHING COMPONENT CHANGE INFORMATION. 2 L 7 2 4F RT A56NM 2007020200017 20070202 00017 NM 2007 2 2 0700416740 1 20070118 A 5414 SKIN BOEING 747 747251F 1384898 NM NR 3 NACELLE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 640US 23888 DURING "M" CHECK, FOUND CRACK IN NR 3 PYLON CAP SKIN AT FRONT SPAR CHORD AND REAR ENGINE MOUNT BULKHEAD UPPER FORWARD FR AME. REPAIRED PER EA 67-208615. 2 L 7 4 4F A20WE 2007020200031 20070202 00031 NM 2007 2 2 UPS07549068 1 20070130 A 3350 FUSE BOEING 757 75724APF 1384969 NM EMERGENCY LIGHTS FAILED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 457UP 25478 FOUND EMERGENCY EGRESS LIGHT INOP. REMOVED AND REPLACED POWER SUPPLY DUE TO BLOWN INTERNAL FUSE. OPS CK OK PER MM 33-5 1-07-2. 2 L 7 2 4F RT A2NM 2007020200034 20070202 00034 WP 2007 2 2 UPS07849044 1 20070106 A 5320 STIFFENER DOUG DC8 DC871F 302199D WP BS 1916 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 - FOUND EMPENNAGE TAIL SECTION AT STA 1916 INSIDE 62 ACCESS HAT CHANNEL CROSS MEMBER STIFFENER HAS CR ACK AT END RT SIDE. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 REPAIR ANGLES IAW SRM 53-02-00 FIG 001B, 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2007020200041 20070202 00041 CE 2007 2 2 DXTA200701883 1 20070128 A 3233 99125373 ACTUATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LT MLG INTERMITTENT E DXTA O OTHER S AFFECT SYSTEMS LD LANDING 1 GL 07 607QS 3644 5605340 DURING LANDING GEAR EXTENSION, LT MAIN GEAR LIGHT DID NOT ILLUMINATE AND UNLOCK LIGHT STAYED ON. DID ROTARY TEST AND DE TERMINED LT GEAR LIGHT WORKED. CYCLED GEAR UP AND DOWN TWICE AND COULD NOT GET 3 GREEN LIGHTS. UNLOCK LIGHT REMAINED I LLUMINATED. DECLARED EMERGENCY. CONDUCTED (GEAR WILL NOT EXTEND) CHECKLIST. PUT GEAR HANDLE DOWN - GOT 3 GREEN AND NO UNLOCK LIGHT. CONTINUED CHECKLIST AND ACTIVATED NITROGEN BLOW DOWN BOTTLE TO INSURE GEAR WAS DOWN - NORMAL LANDING FOLLO WED. TROUBLESHOT TO LT MAIN ACTUATOR. REMOVED ACTUATOR P/N 9912537-3 S/N 0752. INSTALLED NEW ACTUATOR P/N 9912537-3 S /N 1145. OPS AND LEAK CHECK GOOD. WORK DONE IAW MM CH 32-30-04 SERVICED GEAR N2 BOTTLE. DONE IAW MM 12-13-01. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007020200043 20070202 00043 NM 2007 2 2 CALA0700043 1 20070131 A 5730 114N2107 SKIN BOEING 757 757224 1384958 NM WS 425.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12125 28967 INSPECTION FOUND AN 8" CRACK IN LT WING FIXED LEADING EDGE SKIN PANEL UPPER SURFACE AT WS 425.5. PERFORMED OPERATION 04 OF EA 5731-01010 AND REPAIRED CRACKED AREA IAW SRM 51-70-17 AND ATTACHED LAYUP PROCEDURE WORK CARD (COMPOSITE REPAIR WI THOUT CORE REPLACEMENT). 2 L 7 2 4F RT A2NM 2007020200048 20070202 00048 CE 2007 2 2 DXTA200701882 1 20070127 A 3230 LANDING GEAR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MALFUNCTIONED E DXTA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 GL 07 694QS 5605194 AFTER TAKEOFF WITH GEAR SELECTED UP AND FLAPS SELECTED UP MASTER CAUTION ILLUMINATED. (HYD PRESS) (STAB MISCOPARE) AND G EAR (UNLOCK) LIGHTS ILLUMINATED. PLACED GEAR DOWN - ALL LIGHTS WENT OUT-GEAR INDICATED 3 GREEN. PLACED GEAR UP, UNLOCK L IGHT REMAINED ON AND (HYD PRESS) ANNUNCIATION. SWUNG GEAR MULTIPLE TIMES WITH NO FAULTS NOTED. ALL WORK DONE IAW MM CHA P 32-30-05. OPS CHECK AND LEAK CHECK GOOD AT THIS TIME. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007020200050 20070202 00050 NM 2007 2 2 TSAA0749009 1 20070126 A 4900 1319B APU BOEING 737 73773A 1384606 NM SHUTDOWN A TSAA K NONE O OTHER TX TAXI/GRND HDL 1 WP 13 738AL 28499 AIRCRAFT GROUND EVENT IN OGG, THE APU AUTO SHUTDOWN FOR LOW OIL PRESSURE INDICATION. MAINTENANCE COMPLIED WITH FIM TASK 49-90-00-810-803. INSPECTED THE LOW OIL PRESSURE SWITCH AND THE OIL DELTA P INDICATOR WITH NO DEFECTS NOTED. APU OPER ATED NORMAL WITH ALL INDICATIONS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007020200051 20070202 00051 NM 2007 2 2 TSAA0749010 1 20070127 A 4990 1605641 OIL COOLER BOEING 737 73773A 1384606 NM APU OIL SYSTEM UNKNOWN A TSAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 738AL 28499 AIRCRAFT GROUND EVENT IN SNA, THE APU AUTO SHUTDOWN FOR HIGH OIL TEMPERATURE INDICATION AND FAULT CODE 49-91005. MAINTE NANCE PERFORMED FIM TASK 49-90-00-810-801, REMOVED AND REPLACED THE APU OIL COOLER PER AMM 49-91-41-000-801. MAINTENANC E ALSO REMOVED AND REPLACED THE APU OIL TEMPERATURE CONTROL VALVE PER AMM 49-91-21-000-801. NO DEFECTS NOTED ON GROUND RUN. AIRCRAFT WAS RETURNED TO SERVICE. A FLIGHT VERIFICATION WAS COMPLETED. 2 L 7 2 4F RT A16WE 2007020200054 20070202 00054 EA 2007 2 2 COMA0760086 1 20070128 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 720SW 7297 FLIGHT 5103 - FLAP FAIL CAUTION MESSAGE AT 20 DEGREE FLAP SETTING. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FI RST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MES SAGES. 2 L 7 2 4F RT A21EA 2007020200055 20070202 00055 EA 2007 2 2 COMA0760091 1 20070129 A 2750 1104SD100301 SHAFT CNDAIR CL600 CL6002B19 1900309 EA NR 3 TE FLAP DAMAGED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 812CA 7381 FLIGHT 5170 - FLAP FAIL MESSAGE RECEIVED. ABORTED APPROACH, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND WATER I N SYSTEM, REPLACED RIGHT NR 3 FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2007020200056 20070202 00056 CE 2007 2 2 DXTA200701888 1 20070129 A 3260 INDICATION SYS CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 912QS 7500012 AFTER LANDING GEAR HANDLE HAD MOVED TO THE UP POSTION. LIGHTS SHOWED 3 GREEN AND RED UNSAFE INDICATION. GEAR HANDLE WAS RETURNED TO DOWN POSTION AND UNSAFE CONDITION WAS NO LONGER PRESENT (RED LIGHT OUT). INSPECTED LANDING GEAR HANDLE MODUL E, NO DEFECT NOTED. JACKED AIRCRAFT AND PERFORMED LANDING GEAR OPERATIONAL CHECK. CYCLED GEAR SEVERAL TIMES. OPS CHECK GOOD. DOWNJACKED A/C AND CHECK GEAR HANDLE- SOLENOID. OPS CHECK GOOD, WORK DONE IAW MM CHAPTER 32-30-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007020200058 20070202 00058 WP 2007 2 2 UPS07849056 1 20070123 A 5320 SAA577384458 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 1781 L19R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 - UPON REMOVAL OF LONGERON END FITTING FOUND ATTACHED BRACKET CRACKED AT 1781-L19R. REMOVED, FABRICA TED AND INSTALLED INTERCOSTAL IAW SRM 51-3-2, 51-1-21 AND DWG 5773844. 2 L 7 4 4F RT 4A25 2007020200059 20070202 00059 WP 2007 2 2 UPS07849069 1 20070130 A 3350 BATTERY DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 FOUND COCKPIT COURIER AREA AND ENTRY DOORS LIGHT INOP DURING PREFLIGHT BATTERY SAI EMERGENCY LIGHTS CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT PER MM 33-50-01-2. 2 L 7 4 4F RT 4A25 2007020200060 20070202 00060 WP 2007 2 2 UPS07849070 1 20070130 A 5610 WINDOW DOUG DC8 DC871F 302199D WP COCKPIT STUCK A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 F/O WINDOW WILL NOT OPEN. ADJUSTED F/O SLIDING CLEARVIEW WINDOW IAW AMM 56-10-03-5. OPS CK GOOD. 2 L 7 4 4F RT 4A25 2007020200061 20070202 00061 WP 2007 2 2 UPS07849071 1 20070102 A 5711 55978341 SPAR DOUG DC8 DC871F 302199D WP WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C2 FOUND CRACK ON LOWER CENTER SPAR CHORD AND WEB JUST I/B OF XRS 255 NR 1 MAIN TANK. REPAIRED CRACKED SPAR CHORD AND WEB AT NR 1 MAIN TANK JUST I/B OF XRS 255 IAW SAA EA# 008-5710-01-A0595, UPS EO DC8-5710-25944-A, BAC SER V MSG NR 1-270145772, AND FAA FORM 8100-9 . THIS REPAIR IS TIME LIMITED PENDING A DAMAGE TOLERANCE ANALYSIS OF 24 MONTHS IN WHICH DTA IS INCORPORATED. 2 L 7 4 4F RT 4A25 2007020200067 20070202 00067 NM 2007 2 2 BB07012 1 20070131 A 3350 20121 CHARGER BOEING 757 7572B7 1384964 NM EMERGENCY LIGHTS FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 928UW 27124 MAINTENANCE FOUND EMERGENCY LIGHT ON BULLNOSE 12/13R INOPERATIVE. REPLACED BATTERY CHARGER AT 12R. NO FURTHER DIFFICUL TIES. 2 L 7 2 4F RT A2NM 2007020200070 20070202 00070 NM 2007 2 2 SWAA070456 1 20070128 A 3397 417N5214 WIRE BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT DISCONNECTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 408WN 27895 DURING SCHEDULED MV1 CHECK, FOUND LT AFT CABIN EEPLS INOP. FOUND DISCONNECTED WIRE AT LIGHT ASSY. RECONNECTED WIRE PER MM. 2 L 7 2 4F RT A16WE 2007020200071 20070202 00071 2007 2 2 SWAA070463 4 20070129 A 2565 5A33075F SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 494WN 33868 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007020200073 20070202 00073 NM 2007 2 2 SWAA070469 1 20070130 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 731D S18R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 731D, STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007020200075 20070202 00075 CE 2007 2 2 DXTA200701889 1 20070129 A 3230 LANDING GEAR BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE UNKNOWN E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 142QS RK432 AFTER T/O THE LANDING GEAR HANDLE LIGHT REMAINED ILLUMINATED. AIRSPEED WAS KEPT BELOW 190 KTS AND SLIGHT VIBRATION FELT. UPON EXTENSION LIGHT EXTINGUISHED AMD 3 GREEN LIGHTS. JACKED ACFT., INSPECTED MLG, NO FAULTS FOUND. PERFORMED 10 GEAR CYCLES, NO FAULTS NOTED. MLG/NGEAR AND GEAR INDICATION SYSTEMS OPS CHECK GOOD AT THIS TIME. IAW 400XP M/M 32-10-00 2 H 7 2 4F 4 F RT A16SW E25EA 2007020200076 20070202 00076 CE 2007 2 2 DXTA200701890 1 20070129 A 3244 TIRE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG SMOKE E DXTA K NONE O OTHER TX TAXI/GRND HDL 1 GL 07 314QS 5600441 UPON TAXI IN THE LINE PERSONNEL ADVISED US THAT THE RT MAIN GEAR WAS SMOKING. THERE APPEARS TO BE A FILM OF OIL OR GREA SE ON THE OUTSIDE AND PORTIONS OF THE INSIDE OF THE TIRE. CLEANED RT MAIN GEAR BRACKET WHEEL ASSY VISUALLY INSP'D FOR L EAKS, EXERCISED BRAKES, SET PARKING BRAKE FOR 1 HR, INSP'D FOR LEAKS, NONE NOTED, CLEANED RH MAIN GEAR WHEEL WELL INSP'D FOR LEAKS, CK'D UPLOCK AND MAIN GEAR ACTUATOR B-NUTS FOR SECURITY, SATISFACTORY AT THIS TIME PER CE 560 M/M CH 32-42-01 & CH 29-11-00 2 L 7 2 4F 4 F RT A22CE E25EA 2007020200078 20070202 00078 NE 2007 2 2 DXTA200701894 2 20070130 A 7200 ENGINE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LEFT SHUTDOWN E DXTA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 361QS 5600361 PCEJC0247 ON THE GROUND, DURING THE SPEED BRAKE CHECK, POWER LEVER WAS RETARDED TO IDLE ON THE LT ENGINE AND ENGINE SHUTDOWN. ADJ USTED GROUND IDLE IAW CE 560 MM CH 71-01-03. GROUND CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2007020200080 20070202 00080 EU 2007 2 2 SA07008 1 20070201 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 754UW 21082 586 1328 DCA - NUMEROUS EMERGENCY LIGHTS WERE FOUND INOPERATIVE DURING AN EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE MID-CA BIN, RIGHT SIDE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007020200081 20070202 00081 NE 2007 2 2 BAQA200700006 2 20070131 A 7320 70MK01010 ECU AGUSTA A109 A109E 0260119 EU PWC PW206C PW206C NE NR 1 FAILED E BAQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 03 109DK 1985 40 11504 33011 NR 1 ECU WARNING LIGHT ILLUMINATED IN FLIGHT. ALONG WITH THE NR 1 ECU CAUTION LIGHT NR 1 ECU FAIL LIGHT ILLUMINATED. THE NR 1 ENGINE WENT INTO MANUAL MODE. NO LIMITS WERE EXCEEDED. AIRCRAFT IS CURRENTLY IN MAINTENANCE TO TROUBLESHOOT PROBL EM. THE AC LANDED. 1 G 7 2 3U 3 U RT H7EU E42NE 2007020200082 20070202 00082 EU 2007 2 2 MALA070021 1 20070131 A 3350 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 427XJ 340B427 DURING EMERGENCY LIGHT FUNCTIONAL CHECK, POWER SUPPLY 21LN FAILED, 21LN WAS REMOVED AND REPLACED TO CORRECT FAILURE. 2 L 7 2 4T RT A52EU 2007020200085 20070202 00085 EU 2007 2 2 DHL2007362515 1 20070116 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSLEAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 CABIN FLOOR SEAT TRACK AT SEAT TRACK FLANGE HAS GOUGE AND CORROSION BETWEEN FS 18 THRU FS 38B AT LBL 56. REMOVED CORROS ION FROM FR 18 TO FR 38B IAW A300 SRM 51-40-11 FOUND TO BE WITHIN LIMITS FROM FR 26.5 TO 33.5 AND FR 37 TO 38B TREATED P RIMED AND PAINTED IAW A300 SRM 51-40-12. FOUND OUT OF LIMITS FROM FR 18 TO FR 26.5 AN FR 33.5 TO FR 37 IAW A300 SRM 53- 10-00 FIG 612. REPLACED SECTIONS FROM FR 18 TO 26.5 AN FR 33.5 TO FR 38B IAW A300 SRM 53-10-10 FIG 724. 2 L 7 2 4F RT A35EU 2007020200086 20070202 00086 NM 2007 2 2 USAA070079 1 20070131 A 5320 1122173 INTERCOSTAL BOEING 737 7373B7 1384580 NM BS 295 S12L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 511AU 23594 FOUND INTERCOSTAL CRACKED, S-12L AT STA 295. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER EO 5305V203 DWG 65-17684, DEFECT SIZE: .5". 2 L 7 2 4F RT A16WE 2007020200087 20070202 00087 NM 2007 2 2 USAA070078 1 20070131 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 511AU 23594 FOUND FRAME WITH TWO CRACKS 1 INCH AND 1/4 INCH, STA 440, WL160 AND WL 162. TRIMMED OUT DAMAGE, FAB'D DOUBLERS AND SHIM S AND INSTALLED PER EA 98425, DEFECT SIZE: 1" AND 1/4". 2 L 7 2 4F RT A16WE 2007020200088 20070202 00088 NM 2007 2 2 USAA070077 1 20070131 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 492 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 511AU 23594 FOUND FRAME WITH TWO CRACKS, .250" AND .750", BS 492 S-24R, WL 160, WL 162. FABRICATED AND INSTALLED REPAIR PARTS AND M ACHINED TWO DOOR STOP FITTINGS PER EA 98426, DEFECT SIZE: .250" AND .750". 2 L 7 2 4F RT A16WE 2007020200089 20070202 00089 EU 2007 2 2 DHL2007362516 1 20070126 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 CABIN SEAT TRACK AND SEAT TRACK FLANGE HAS CORROSION AT LBL 17 BETWEEN FRAME 40 THRU FRAME 50. REMOVED CORROSION FROM S EAT TRACK AND SEAT TRACK FLANGE IAW A300 SRM 51-40-11. FOUND WITHIN LIMITS FROM FR 48 TO FR 50 FOUND OUT OF LIMITS FROM FR 40 TO FR 48 IAW A300 SRM 53-10-00 FIG 612. REPLACE SEAT TRACK SECTION FROM FR 40 TO FR 44.5 IAW A300 SRM 51-30-30,5 1-10-40, 51-10-40 AND INSTALLED NEW SECTION FROM FR 44.5 TO FR 50.5 IAW A300 SRM 53-10-10 FIG 725. THIS IS A PERMANENT REPAIR. 2 L 7 2 4F RT A35EU 2007020200090 20070202 00090 NM 2007 2 2 USAA070076 1 20070131 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM BS 295 S11L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 511AU 23594 FOUND INTERCOSTAL CRACKED, S-11L AT STA 295. INSTALLED MOD KIT PER EO 5305V203, DEFECT SIZE: .5". 2 L 7 2 4F RT A16WE 2007020200095 20070202 00095 EA 2007 2 2 COMA0760108 1 20070131 A 5101 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 983CA 7169 FLIGHT 5270 - ANTI-ICE DUCT MESSAGE ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. PERFORMED OPS CHECK OF WING ANTI -ICE SYSTEM, NO DEFECTS NOTED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007020200097 20070202 00097 EA 2007 2 2 SIMA200703202 1 20070131 A 5610 601R33030311 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SIMA O OTHER O OTHER DE DESCENT 1 SW 21 516AE 8521 10123 ON DESCENT, CAPTAIN'S SIDE WINDOW CRACKED NO PRESSURE LOSS. REMOVED AND REPLACED SIDE WINDOW IAW CRJ AMM 56-10-05. PRE SSURIZATION CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007020200098 20070202 00098 SO 2007 2 2 SIMA200703204 1 20070130 A 5315 14530645411 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 918AE 4778 14500902 FOUND LEFT OMEGA BEAM CORRODED AT FRAME 20. PERFORMED CUTOUT OF DAMAGE. FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 5 3-00-10 AND 51-40-02. RESTORED PROTECTIVE FINISH AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007020200099 20070202 00099 EU 2007 2 2 SIMA200703201 1 20070130 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A SIMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 21 323AE 25135 2614 340B323 DISCOVERED FIVE REAR FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY IAW EMB AMM 33-50-10. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007020200101 20070202 00101 CE 2007 2 2 BSAASDR0702 1 20070127 A 5610 10138402523 WINDSHIELD BEECH 1900 1900D 1154162 CE COCKPIT CRACKED A BSAA O OTHER Z SIGNIFICANT FAILURE REPORT CR CRUISE 1 NM 05 132YV UE132 NR 1 WINDSHIELD CRACKED AT FL 170, JUST PRIOR TO THE START OF DESCENT. CREW DECLARED INFLIGHT EMERGENCY, REVIEWED AND F OLLOWED ABNORMAL CHECKLIST PROCEDURES, AND LANDED WITHOUT FURTHER INCIDENT. WINDSHIELD WAS REPLACED. CAPTAIN STATED WI NDSHIELD HEAT WAS TURNED ON AT 400' AGL ON DEPARTURE, AND WASN'T CHANGED DURING THE FLIGHT. 2 L 7 2 4T RT A24CE 2007020200102 20070202 00102 SO 2007 2 2 LR7A07011 1 20070130 A 5311 FRAME LKHEED 382 382G 526414U SO FS 386 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 196 4676 DURING SCHEDULED A CHECK PER JOB CARD HA1200, FOUND RING FRAME CRACKED AT FS 386, WL160-174, RBL79. REPAIRED FRAME IAW LAC MEA 382-53-07-009. 2 H 7 4 4T A1SO 2007020200103 20070202 00103 SO 2007 2 2 LR7A07012 1 20070130 A 5342 ANGLE LKHEED 382 382G 526414U SO FS 386 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 196 4676 DURING SCHEDULED A CHECK PER JOB CARD HA1200, FOUND DORSAL FIN ATTACH ANGLE CRACKED AT FS 848, WL285, RBL10. REPAIRED FRAME IAW LAC MEA 382-53-07-010. 2 H 7 4 4T A1SO 2007020200105 20070202 00105 EU 2007 2 2 07FDEA00231 1 20070131 A 3510 FLOW VALVE AIRBUS 300 A300F4605R 3930327 EU COCKPIT OXYGEN MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 671FE 778 ACFT DIVERTED INTO LBB WITH CREW LP SUPPLY READING 0 PSI AND NO AIR FLOW TO ANY POSS ON FLT DECK. TROUBLE SHOT PROBLEM TO CREW LP FLOW VALVE. SWAPED FLOW VALVE FROM COURIER POSS TO CREW POSS. CREW LP SYSTEM NOW OPERATIONAL. NO LEAKS NOT ED AT THIS TIME. WILL MEL COURIER LP OXY SYSTEM. 2 L 7 2 4F RT A35EU 2007020200107 20070202 00107 NM 2007 2 2 07FDEA00233 1 20070201 A 5340 652448012 ATTACH FITTING BOEING 727 727233 138408A NM ZONE 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 RT MLG UPLOCK ASSY MOUNTING LUGS ON FUSELAGE BOLT HOLES CORRODED AT STA 910, WL 188 RBL 63-66. REMOVED MLG UP LOCK ASSY MOUNTING LUG, VERIFIED PART AND DRILLED PART. INSTALLED FITTING, PAINTED FITTING, REF SRM 51-30-2, 51-10-2, WO NR 1170 1-7000-0001. 2 L 7 3 4F RT A3WE 2007020200109 20070202 00109 NM 2007 2 2 07FDEA00235 1 20070201 A 5340 654531313 STRINGER CLIP BOEING 727 727233 138408A NM BS 680 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 STRINGER CLIP CRACKED IN RADIUS CUTOUT BS 680 STRINGER L9. REMOVED DAMAGED STRINGER CLIP, TRANSFERED FASTENER HOLES FOR NEW CLIP. INSTALLED NEW CLIP, REF SRM 51-30-2 PG 2 AND 5, SRM 51-30-5 PG 1. 2 L 7 3 4F RT A3WE 2007020200110 20070202 00110 NM 2007 2 2 07FDEA00236 1 20070201 A 5320 652165832 SUPPORT ANGLE BOEING 727 727233 138408A NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 LT WING LOWER T/E PANEL SUPPORT ANGLE I/B OF NR 3 SPOILER ACTUATOR, I/B ANGLE IS CRACKED IN RADIUS AND AROUND ATTACH HOL E. REMOVED CRACKED SUPPORT ANGLE AND REPLACED WITH NEW SUPPORT ANGLE REF SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007020200113 20070202 00113 EA 2007 2 2 COMA0760106 1 20070131 A 5210 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNKNOWN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 587SW 7062 FLIGHT 5378 - ON CLIMB-OUT FROM DTW AT 5000 MSL PAX DOOR HANDLE CAUTION MESSAGE CAME ON, APPROXIMATELY 30 SECONDS LATER DOOR WARNING MESSAGE AND AURAL CHIME. AIRCRAFT DIVERTED BACK TO DTW AND LANDED SAFELY. INSPECTED PAX DOOR, NO DEFECTS NOTED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007020200114 20070202 00114 NM 2007 2 2 07FDEA00239 1 20070201 A 5313 STRINGER BOEING 727 727233 138408A NM BS 999 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 AFT PIT STR 29L CORRODED STA 999 OUTBD SIDE. REMOVED CORROSION, CHECKED MATERIAL LOSS, ORIG MATERIAL = .156". REMOVED .036", ROTO PEENED, TREATED, PRIMED, PAINTED. INSTALLED FASTENERS (2EA) REF AAR EA NR I070060. 2 L 7 3 4F RT A3WE 2007020200115 20070202 00115 EA 2007 2 2 TRAX200700126 1 20070128 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 861AS 7445 FLAPS FAULT AT 8 DEGREES. EMERGENCY EQUIPMENT ON STANDBY. 2 L 7 2 4F RT A21EA 2007020200116 20070202 00116 EA 2007 2 2 REXA200700013 1 20070129 A 5100 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE UNKNOWN A REXA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 25 820AY 8020 GEE950321 AFTER ESTABLISHING CRUISE ALTITUDE OUT OF DTW, THE FLIGHT CREW WAS ALERTED TO HIGHER THAN NORMAL N1 VIBRATION ON THE LEF T ENGINE. WHEN VIBRATION LEVELS CONTINUED TO INCREASE, THE QRH CHECKLIST WAS COMPLETED AND THE ENGINE WAS SHUT DOWN. T HE FLIGHT CREW DECLARED AN EMERGENCY AND TURNED BACK TO DTW. AN OTHERWISE UNEVENTFUL SINGLE ENGINE APPROACH AND LANDING WAS MADE. MAINTENANCE PERSONNEL OBSERVED A LARGE QUANTITY OF ICE BUILT UP ON THE FAN SPINNER AND BLADES. THE ICE WAS REMOVED AND ENGINE VIBRATION RUNS WERE PERFORMED. VIBRATION LEVELS WERE NORMAL. THERE WERE NO REPORTED MALFUNCTIONS OF THE ENGINE'S ANTI-ICE SYSTEM. 2 L 7 2 4F 4 F RT A21EA E15NE 2007020200117 20070202 00117 NE 2007 2 2 MASA200700056 2 20070125 A 7200 GUIDE VANE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 1 ENGINE DEPARTED A MASA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 07 17337 7337 872749 ASH 2985 DEN - DURING CRUISE FLIGHT, THE CREW HEARD A LOUD POP FOLLOWED BY A LOUD BANG THEN RECEIVED A NR 1 ENGINE OIL P RESS WARNING. THE CREW THEN ISOLATED THE ENGINE, DECLARED AND EMERGENCY AND RETURNED TO THE FIELD. MX FOUND THE FAN SE CTION FWD OF THE BY-PASS GUIDE VANES DEPARTED THE ENGINE ALONG WITH THE T/R ASSY INLET COWL FAN COWL AND HAD DONE DAMAGE TO THE PYLON AND FUSELAGE SKIN AFT OF THE PRESSURE BULKHEAD. CVR AND FDR CB'S WERE PULLED BY MX. A/C IS CURRENTLY OUT OF SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007020200118 20070202 00118 NE 2007 2 2 200700006 2 20070201 A 7320 70MK01010 ECU AGUSTA A109 A109E 0260119 EU PWC PW206C PW206C NE NR 1 ENGINE FAILED E BAQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 03 109DK 1985 40 11504 33011 NR 1 ECU WARNING LIGHT ILLUMINATED IN FLIGHT. ALONG WITH THE NR 1 ECU CAUTION LIGHT NR 1 ECU FAIL LIGHT ILLUMINATED. TH E NR 1 ENGINE WENT INTO MANUAL MODE. NO LIMITS WERE EXCEEDED. AIRCRAFT IS CURRENTLY IN MAINTENANCE TO TROUBLESHOOT PROBL EM. 1 G 7 2 3U 3 U RT H7EU E42NE 2007020200119 20070202 00119 EA 2007 2 2 COMA0760105 1 20070131 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 587SW 7062 FLIGHT 5689 - FLAPS FAIL AT 2000FT, FAILED AT ZERO DEGREES. AIRCRAFT LANDED SAFELY. COMPLIED WITH AD 2006-12-21 FLAP C AUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (G) 1,2,3, (A,B,C). FLAP SYSTEM WAS RESET WITH NO FURTHER FL AP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007020200120 20070202 00120 EU 2007 2 2 MALA070020 1 20070130 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 340B428 THE LT FORWARD FUSELAGE, JUST AFT OF THE RADOME AND BETWEEN THE TWO RADOME LATCHES IS DENTED. THE DAMAGE HAS BEEN REPAI RED IAW MESABA EO NR S53344. REF: EAMS WORK ORDER 215422 TASK 1502. 2 L 7 2 4T RT A52EU 2007020200121 20070202 00121 NM 2007 2 2 SWAA070515 1 20070131 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 458WN 33857 DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER MISSING AT ROW 20 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007020200124 20070202 00124 NM 2007 2 2 SWAA070516 1 20070131 A 5315 6545410366 FLOORBEAM BOEING 737 7375H4 138449D NM BS 664 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED BRDG CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 664.5, BL 0. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007020200125 20070202 00125 NM 2007 2 2 SWAA070483 1 20070131 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 514D CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514D, STR 12R. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007020200127 20070202 00127 NM 2007 2 2 SWAA070500 1 20070131 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 730E CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730E, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007020200137 20070202 00137 NM 2007 2 2 SWAA070518 1 20070131 A 5311 6546558 FRAME BOEING 737 7375H4 138449D NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 21R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007020200139 20070202 00139 NM 2007 2 2 SWAA070509 1 20070131 A 5311 6546596 FRAME BOEING 737 7375H4 138449D NM BS 727B CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020200140 20070202 00140 NM 2007 2 2 0701001 1 20070117 A 3350 LAMP BOEING 737 737230C 1384472 NM EMERGENCY LIGHT LOOSE A MJYA K NONE L NO TEST IN INSP/MAINT 1 SW 07 767TW 20258 R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. 2 L 7 2 4F A16WE 2007020200143 20070202 00143 NM 2007 2 2 07FDEA00228 1 20070131 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 380 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 MAIN DECK FLOORBEAM UPPER FLANGE IS CORRODED BS 380, RBL 35, WL208. REMOVED, BLENDED CORROSION, FROM BS380, RBL 35. RO TO PEENED AREA, TREATED AND PRIMED AREA. REF EA NR 5310-106966 AND EA NR-7-5310-106966 REV A. 2 L 7 3 4F RT A3WE 2007020200145 20070202 00145 EU 2007 2 2 07FDEA00230 1 20070131 A 5230 SKIN AIRBUS 310 A310203 3930313 EU CARGO DOOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 435FE 369 AFT BULK CARGO DOOR HAS TWO DENTS EXTERNAL SKIN, FOUND UPPER DENT TO BE WITHIN LIMIT AND LOWER DENT FOUND TO BE OUT OF L IMIT. FOUND TO BE CRACKED ON LOWER DENT. REPAIRED CRACKED IAW SRM 52-30-00 FIG 207. 2 L 7 2 4F RT A35EU 2007020200152 20070202 00152 EA 2007 2 2 COMA0760090 1 20070129 A 2750 1104SD100501 SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAP CORRODED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 812CA 7381 FLIGHT 5170 - FLAP FAIL MESSAGE RECEIVED. ABORTED APPROACH, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND WATER I N SYSTEM, REPLACED LEFT NR 5 FLEX SHAFT. 2 L 7 2 4F RT A21EA 2007020200153 20070202 00153 EA 2007 2 2 COMA0760092 1 20070129 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 479CA 7675 FLIGHT 4984 - FLAP FAIL MESSAGE RECEIVED AT 0 DEGREE FLAP SETTING. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLI ED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYS TEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007020200155 20070202 00155 NM 2007 2 2 SWAA070457 1 20070129 A 3350 101073 LENS BOEING 737 7373K2 13844BA NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 L1 DOOR EMERGENCY EXIT LOWER LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007020200156 20070202 00156 NM 2007 2 2 SWAA070460 1 20070129 A 3350 101114 COVER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 RIGHT OVERWING EMERGENCY EXIT SIGN COVER LOOSE. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007020200157 20070202 00157 NM 2007 2 2 SWAA070459 1 20070129 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 LEFT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN LENS PER MM. 2 L 7 2 4F RT A16WE 2007020200158 20070202 00158 NM 2007 2 2 SWAA070458 1 20070129 A 3350 20121 CHARGER BOEING 737 7373K2 13844BA NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED OTS CHECK, FWD CABIN EMERGENCY BATTERY PACK AND BATTERY CHARGER FAILED TEST. REMOVED AND REPLACED BATT ERY PACK AND BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007020200159 20070202 00159 NM 2007 2 2 SWAA070461 1 20070129 A 2121 215201 FAN BOEING 737 7373H4 1384600 NM E&E BAY FAULTY A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 29 386SW 26601 DECLARED EMERGENCY. ON DESCENT ACRID ODOR IN COCKPIT AND IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2007013100085 20070131 00085 NM 2007 1 31 HALA0700040 1 20070129 A 4950 BLEED VALVE BOEING 717 717200 1383700 NM APU MALFUNCTIONED A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 480HA 55125 BTB - NO AIR ON APU ON START. PERFORMED APU RTS TEST FAILED BLEED CONTROL VALVE OPEN CIRCUIT FAULT. PERFORMED FIM 49-5 0-00-810-804 REF WDM 49-30-004. PERFORMED REPAIR CONFIRMATION RTS PASSED. 2 L 7 2 4F TR A6WE 2007013100091 20070131 00091 EU 2007 1 31 DHL2007362513 1 20070106 A 5320 WEB AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 CABIN FLOOR SUPPORT PAN SKIN BETWEEN RBL 17 AND RBL 56 HAS CORROSION AT SURFACE SKIN AT FRAME 30. REMOVED FASTENERS AT CABIN FLOOR SUPPORT PAN FROM RBL 50 FR 30 FOR ACCESS AT CORROSION PER A300 SRM 51-30-30. REMOVED CORROSION FROM RBL 17 TO RBL36 FR 30 PER A300 SRM 51-40-11 MAT LOSS .003,ORG. MAT .040 MAT REMAINING .037 FOUND WITHIN LIMITS PER A300 SRM 51- 41-20. REMOVED CORROSION FROM RBL 36 TO RBL 56 FR 30 PER A300 SRM 51-40-11 FOUND OUT OF LIMITS AT RBL 48 PER A300 SRM 5 1-40-20 CUT OUT DAMAGE AREA (7" X 1 3/4") FROM RBL 30 TO RBL 50 FR 30 PER A300 SRM 51-41-20 FIG 702 TREATED AREA AN PART S REPAIR PER A300 SRM 51-40-12. INSTALLED FASTENERS AN WEB REPAIR PER A300 SRM 51-30-30,51-40-20 FIG 702, PERMANENT REP 2 L 7 2 4F RT A35EU 2007013100094 20070131 00094 EA 2007 1 31 SWIA200717763 1 20070125 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 728SK 10192 CEILING EMERGENCY LIGHT POD (AFT) INOP. RELAMPED CEILING EMERGENCY LIGHT IN AFT CABIN. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007013100110 20070131 00110 NM 2007 1 31 07FDEA00201 1 20070130 A 5320 INTERCOSTAL BOEING 727 727233 138408A NM BS 303 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 UPPER FWD LT FUSELAGE AT ENTRY DOOR CUTOUT TOP HINGE FWD OF BS 303.5 FRAME AT STRINGER 6L HAS A INTERCOSTAL WITH A CRACK ED OUTER ANGLE REMOVED AND REPLACED INTERCOSTAL AND UPPER ANGLE AT ENTRY DOOR CUTOUT REF SRM 51-30-2 PG 1. 2 L 7 3 4F RT A3WE 2007013100120 20070131 00120 CE 2007 1 31 DJFA20070011 1 20070118 A 2497 WIRE HARNESS BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE COCKPIT CHAFED E DJFA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 23 715TA RK189 TRIP NR 1130219 ON TAKEOFF ROLL CREW NOTED FLUCTUATION IN ELECTRICAL SYSTEM FOLLOWED BY EMERGENCY BUS FAIL AND BATT CUTO FF CAUTION LIGHTS. TAKEOFF WAS ABORTED. MAINTENANCE DISCOVERED WIRE HARNESS ROUTED ON LT SIDE OF THE AIRCRAFT RUNS OVE R THE PILOTS PFD AND WAS CHAFING ON THE UPPER LT CORNER OF THE PFD MOUNT. THE WIRE WAS REPAIRED AND THE HARNESS PROTECT ED AND SECURED TO PREVENT FURTHER CHAFFING. 2 H 7 2 4F 4 F RT A16SW E25EA 2007013100125 20070131 00125 CE 2007 1 31 DXTA200701857 1 20070116 A 3260 1EN114N119 SQUAT SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP LT MLG FAILED E DXTA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 GL 07 870QS 967 258732 AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. SNOW AND SLUSH ALL GROUND SURFACES. RETURNED TO DEPARTURE. JACKED AC AND ACCOMPLISHED GEAR SWINGS, NO DEFECTS WERE NOTED ACCESSED GEAR SELECTOR VALVE IN NOSE WHEEL WELL AND CHECKED FOR FREEDOM OF MEASUREMENT OF LINKAGE, NO DEFECTS WERE NOTED. GAINED ACCESS TO TERMINAL BLOCK (JK) AND RANG OUT LT WEIGHT ON SWITCH (JP) AND FOUND SWITCH RINGING OUT TO AIRFRAFE GROUND. REMOVED UNSERVICEABLE LT WOW SWITCH. INSTALLED A NEW SWITCH OPERAT IONAL CHECK WAS FOUND TO BE SATISFACTORY. 2 L 7 2 4F 4 F RT A3EU E6WE 2007013100126 20070131 00126 2007 1 31 2007UALA00200 4 20070125 A 2565 LATCH BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE OVERWING SLIDE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 30024 RT OVERWING SLIDE COMPARTMENT DOOR LATCH (NR4 AFT), SLIDER IS CRACKED, SPLIT ALONG FWD, OUTBD, AND AFT EDGES. DID NOT P ASS INTEGRATOR TORQUE TEST. REMOVED AND REPLACED LATCH PER MM 25-65-09 AND OPS TEST GOOD. SUSPECT SLIDER HAD MANUFACTU RING FLAW. 2 L 7 2 4F 4 F RT A1NM E24NE 2007013100139 20070131 00139 NM 2007 1 31 2007UALA00212 1 20070125 A 2997 WIRE HARNESS BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 2 HYD BAY CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 30024 NR 2 HYD BAY WIRE HARNESS CHAFING AGAINST STRUCTURE AND HYD LINE AT FWD LT SIDE OF BAY. REROUTED AND SECURED WIRE HAR NESS PER GN-MM 2-0-10-004. NO WIRE DAMAGE BEYOND ACCEPTABLE STANDARD. SUSPECT HARNESS MIS-ROUTED DURING PREVIOUS MAINT ENANCE ACCESS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007013100147 20070131 00147 NE 2007 1 31 DXTA200701872 2 20070121 A 7321 VALVE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE RT ENGINE FAILED E DXTA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 684QS 5605084 RT ENGINE EEC FAILED TO MANUAL DURING T/O ROLL. ABORTED TAKEOFF. REPLACED RT ENGINE BOV SERVO VALVE IAW CE560XL MAINTE NANCE MANUAL CHAP 20-10-00 & P & W 535 MAINTENANCE CHAP 75-30-01. OPERATIONAL & LEAK CHECKS GOOD. CLEARED MEL. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007013100159 20070131 00159 CE 2007 1 31 GUUA01250701 1 20070125 A 2697 CONNECTOR BEECH 1900 1900D 1154162 CE PWA JT9 JT9D7R4G2 52054 NE FIRE BOTTLE LOOSE A GUUA K NONE N FALSE WARNING CR CRUISE 1 SO 29 46AR UE27 (9262) FPO/PBI DURING FLIGHT RT FIRE DISCHARGE ANNUNCIATOR ILLUMINATED. SECURED RT FIRE BOTTLE WIRE CONNECTION OPERATIO NAL CHECK NORMAL. 2 L 7 2 4T 4 F RT A24CE E3NE 2007013100160 20070131 00160 EA 2007 1 31 COMA0760063 1 20070125 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 814CA 7387 FLIGHT 5396 - RECEIVED A FLAP FAIL CAUTION MESSAGE DURING YYZ APPROACH AT ZERO DEGREE FLAP SETTING. COMPLIED WITH AD 20 06-12-21 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (G) 1,2,3, (A,B,C). FLAP SYSTEM WAS RESET WIT H NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007013100165 20070131 00165 NM 2007 1 31 2007UALA00141 1 20070121 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 756 S16L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 SKIN DENTED AT STA 756 STR 16L MEASURING 1.5 INCHES WIDE AND A DEPTH OF 0.124 INCH. MAJOR REPAIR ACCOMPLISHED. INSTALL ED DOUBLER REPAIR. PERMANENT REPAIR TO BE ACP AT OR BEFORE NEXT C CHECK NOT TO EXCEED 24 MONTHS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007013100166 20070131 00166 NM 2007 1 31 2007UALA00142 1 20070119 A 5753 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU TE FLAP DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 912UA 25290 LEFT WING OTBD FORE FLAP INBD END DELAMINATED. MAJOR REPAIR: REPAIRED FLAP PER SRM 95-57-53-04 IN SHOP. REINSTALLED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007013100181 20070131 00181 2007 1 31 2007UALA00156 4 20070120 A 2565 LATCH BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE OVERWING SLIDE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 674UA 29242 LEFT OVERWING SLIDE DOOR LATCH NR 3 AFT, VERY HARD TO OPERATE. SLIDE PROBLEM. LATCH DIFFICULT TO OPERATE. REPLACED LAT CH. OPS CHECKS NORMALLY. SUSPECT IMPROPER PRIOR INSTALLATION . 2 L 7 2 4F 4 F RT A1NM E24NE 2007013100186 20070131 00186 2007 1 31 2007UALA00160 4 20070120 A 2565 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE R2 DOOR SLIDE INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 FOUND EMERGENCY LIGHT INOP, DOOR 2R SLIDE ILLUMINATED. REPLACED EMERG LT ASSY. OP CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007013100236 20070131 00236 EA 2007 1 31 COMA0760068 1 20070126 A 5753 1104SD100101 SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAP DAMAGED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 931CA 7037 FLIGHT 5164 - FLAP FAIL MESSAGE RECEIVED ON APPROACH AT ZERO DEGREES. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. R EMOVED AND REPLACED NR 1 LEFT WING FLEX SHAFT. 2 L 7 2 4F RT A21EA 2007013100240 20070131 00240 EA 2007 1 31 COMA0760070 1 20070126 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 931CA 18749 7037 FLIGHT 5164 - FLAP FAIL MESSAGE RECEIVED ON APPROACH AT ZERO DEGREES. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED LEFT BPSU. 2 L 7 2 4F RT A21EA 2007013100241 20070131 00241 EA 2007 1 31 COMA0760094 1 20070126 A 5753 1104SD100401 SHAFT CNDAIR CL600 CL6002B19 1900309 EA NR 4 FLAP DAMAGED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 806CA 7359 FLIGHT 5145 - RECEIVED FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPL ACED LEFT SIDE NR 4 FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2007020100006 20070201 00006 NM 2007 2 1 SWAA070480 1 20070130 A 5311 6546560 FRAME BOEING 737 7373H4 1384600 NM BS 947 S3L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 947.5, STR 3L. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007020100011 20070201 00011 EA 2007 2 1 COMA0760099 1 20070128 A 2752 854D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA RT OB FLAP FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 814CA 9826 7387 FLIGHT 5086 - FLAPS FAIL AT 500 FT ON APPROACH TO CVG FAILED AT 0 DEGREES WHEN SELECTING 8 DEGREES. REMOVED AND REPLACE D FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2007020100013 20070201 00013 EA 2007 2 1 COMA0760104 1 20070131 A 5610 NP13932110 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 455CA 13006 7592 FLIGHT 5056 - EN ROUTE TO YYZ RIGHT FORWARD WINDSHIELD CRACKED. A/C RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AN D REPLACED RIGHT WINDSHIELD. 2 L 7 2 4F RT A21EA 2007020100018 20070201 00018 EA 2007 2 1 COMA0760101 1 20070130 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNKNOWN A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 962CA 7123 FLIGHT 5120 - PASSENGER DOOR OTR HANDLE CAUTION MESSAGE INFLIGHT. A/C DIVERTED TO GSO AND LANDED SAFELY. TRANSFERRED T O DMI LIST 52-70-01-1. 2 L 7 2 4F RT A21EA 2007020100021 20070201 00021 NM 2007 2 1 SWAA070474 1 20070130 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727A S5L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007020100025 20070201 00025 NM 2007 2 1 SWAA070481 1 20070130 A 5315 65C33940 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 294, RBL 27, WL 208. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007020100049 20070201 00049 EA 2007 2 1 COMA0770012 1 20070130 A 5310 CC670341747 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FS 280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 355CA 11206 10067 FS 280 FLOOR SUPPORT CROSSBEAM IS CRACKED AND CORRODED. REPAIRED IAW GENERIC REO 670-53-11-047 AND SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007020200011 20070202 00011 NM 2007 2 2 C1HA200793006 1 20070131 A 5313 14581317075T6 STRINGER BOEING 727 727212 138407G NM BS 1160 S30 CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 AFT CARGO COMPT BS 1160 STR 30 AND SPLICE REPAIR CORRODED. REPAIRED STR 30 AT BS 1160 IAW B727 SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2007020200019 20070202 00019 WP 2007 2 2 07FDEA00221 1 20070131 A 5320 CHANNEL DOUG DC10 DC1010 3022110 WP BS 879-899 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 FWD CARGO COMPT SUMP AREAS, CHANNEL WITH CRACK BTWN STA 879 AND STA 899, Z= -70, X=-5.5. TRIMMED OUT CHANNEL SECTION, B TWN STA 899-879 AND INSTALLED NEW SECTION IAW SRM 53-70-00 VOL 1 FIG 7 SHT 3. FABRICATED PARTS IAW DETAIL PARTS TRAVELE R N01660 AND SRM 53-70-00 VOL1 FIG 7 SHT 3. 2 L 7 3 4F A22WE 2007020200024 20070202 00024 NM 2007 2 2 ASAA0741428 1 20070131 A 5210 65C362311 SKIN BOEING 737 737490 1384715 NM BS 806-807 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 THE AFT CARGO DOOR EXTERIOR SKIN IS DENTED OUT OF LIMITS 13.25" FROM THE TOP EDGE 11" FROM THE FWD EDGE BETWEEN THE NR 1 AND NR 2 BEAMS. CUT OUT THE DAMAGED AREA OF SKIN FABRICATED AND INSTALLED AN EXTERNAL REPAIR DOUBLER IAW SRM 52 00 01 FIG 201. 2 L 7 2 4F RT A16WE 2007020200032 20070202 00032 2007 2 2 UPS07849040 4 20070130 A 2565 GIRT BAR DOUG DC8 DC871F 302199D WP PAX DOOR SLIDE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 GIRT BAR DIFFICULT TO ARM, NOT ENOUGH MATERIAL TO PULL BAR INTO PLACE. ADJ EVAC SLIDE IN CONTAINER. GIRT BAR OPERATION AL NORMAL, REF MM 25-60-01-2. 2 L 7 4 4F RT 4A25 2007020200044 20070202 00044 NM 2007 2 2 CALA0700044 1 20070131 A 5730 114N2107 SKIN BOEING 757 757224 1384958 NM WS 418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12125 28967 INSPECTION FOUND A 6" CRACK IN RT WING FIXED LEADING EDGE SKIN PANEL UPPER SURFACE AT WS 418. PERFORMED OPERATION 04 OF EA 5731-01010 AND REPAIRED THE CRACKED AREA IAW SRM 51-70-17 AND ATTACHED LAYUP PROCEDURE WORK CARD, COMPOSITE REPAIR W ITHOUT CORE REPLACEMENT. 2 L 7 2 4F RT A2NM 2007020200052 20070202 00052 SO 2007 2 2 C2XA07CL017 1 20070130 A 8011 35059106 STARTER EMB 145 EMB145LR 3260212 SO NR 1 ENGINE FAILED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 26545 10629 4949 145558 PVD FLIGHT NR 3001, THE CREW REPORTED NR 1 ENGINE HUNG START WITH VERY LOUD NOISE AND BURNING SMELL. MAINTENANCE INSPEC TED AND REPLACED NR 1 STARTER (ATS). OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007020200057 20070202 00057 CE 2007 2 2 HUN2007F00000 1 20070117 A 3240 BRAKE ASSY BEECH B300 B300 1159232 CE MALFUNCTIONED E HUNA O OTHER O OTHER NR NOT REPORTED 1 NM 01 92TH FL509 PILOT REPORTED A RECURRING PROBLEM WITH SPONGY BRAKES. THE LT MASTER CYLINDER HAD BEEN REPLACED AND SYSTEM HAD BEEN BLE D SEVERAL TIMES. WE CHECKED BRAKES AND FOUND AIR IN LT SYSTEM. CHECKED TORQUE ON ALL (B-NUTS) IAW KA300 SERIES MM, CHA PTER 20-06-00, SECTION 3, CHART 1, ALL CHECKED SATISFACTORY. DURING INSPECTION OF THE SYSTEM, A SHIPPING CAP WAS FOUND TO BE INSTALLED ON THE END OF THE TUBE ASSEMBLY THAT SUPPLIES CABIN PRESSURE TO BRAKE RESERVOIR, PREVENTING PROPER PRESS URIZATION OF THE RESERVOIR. WE REMOVED CAP, BLED LT BRAKE SYSTEM AND FUNCTIONALLY CHECKED PILOT`S AND COPILOT`S BRAKES. NO FURTHER DEFECTS WERE NOTED. WE BELIEVE THE CAP MAY HAVE BEEN LT IN PLACE DURING CONSTRUCTION OF THE AIRCRAFT. IT 2 L 7 2 4T RT A24CE 2007020200072 20070202 00072 NM 2007 2 2 SWAA070464 1 20070129 A 5330 6145767129 SKIN BOEING 737 7373Y0 1384671 NM BS 520 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007020200074 20070202 00074 NM 2007 2 2 SWAA070470 1 20070130 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 560 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 560, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007020200094 20070202 00094 EA 2007 2 2 COMA0760107 1 20070131 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 975CA 7150 FLIGHT 6056 - FLAPS FAILED AT ZERO DEGREES ON APPROACH, AIRCRAFT LANDED SAFELY. COMPLIED WITH AD 2006-12-21, FLAP CAUTI ON MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A,B,C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007020200106 20070202 00106 NM 2007 2 2 07FDEA00232 1 20070201 A 5347 SEAT TRACK BOEING 727 727233 138408A NM BS 360-380 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 MAIN DECK FLOOR SEAT TRACK IS CORRODED AT BS 360-380, RBL 23, WL 208 REMOVED CORROSION REF SRM 51-10-6 AND EA 7-5310-108 847. HFEC IAW EA 7-5310-108847. FLAP PEEN AREA REF SOPM 20-10-3 AND EA 7-5310-108847. TREAT AND PRIME AREA REF SRM 51 -10-2 PG 7 AND 24. REPAIR CLASSIFIED AS MAJOR. 2 L 7 3 4F RT A3WE 2007020200108 20070202 00108 NM 2007 2 2 07FDEA00234 1 20070201 A 5340 STRINGER CLIP BOEING 727 727233 138408A NM BS 680 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 STRINGER CLIP CRACKED IN RADIUS CUTOUT BS 680, STR L9. REMOVED CLIP, REMOVED DAMAGE FROM CLIP, HFEC CLIP, NO DEFECTS NO TED, ALODINED AND PRIMED, INSTALLED CLIP, REF SRM 51-30-2, 53-10-4. 2 L 7 3 4F RT A3WE 2007020200111 20070202 00111 EU 2007 2 2 07FDEA00237 1 20070201 A 5246 A2151037800300 ACCESS PANEL AIRBUS 310 A310324 3930206 EU FUSELAGE MISSING A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 811FD 457 AFTER FLIGHT ARRIVAL DURING WALK AROUND, FOUND FUELING PANEL MISSING AND WIRE EXPOSED. DOOR BROKEN OFF APPROX 2 IN BELO W HINGE POINT. REFUEL/DEFUEL PANEL DOOR MISSING. CDL PERFORMANCE LIMITING WEIGHT PENALTY IS NEGLIGIBLE. COMPLIED WITH EA 6-5350-107589 TAPED AS REQUIRED. THE EXACT CAUSE IS UNKNOWN, MISSING PANEL NOT FOUND. 2 L 7 2 4F RT A35EU 2007020200123 20070202 00123 NM 2007 2 2 SWAA070517 1 20070131 A 5310 573149 WINDOW FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED BRDG CHECK, FOUND FIRST OFFICERS WINDOW POST CRACKED AT FWD UPPER CORNER. REPAIRED POST PER SRM. 2 L 7 2 4F RT A16WE 2007020200129 20070202 00129 NM 2007 2 2 SWAA070499 1 20070131 A 5753 SKIN BOEING 737 7373H4 1384600 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED C1 CHECK, FOUND LEFT WING INBOARD AFT FLAP DELAMINATED AT INBOARD FLAP TRACK. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2007020200151 20070202 00151 EA 2007 2 2 COMA0760089 1 20070128 A 3010 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 816CA 7398 FLIGHT 4973 - WING ANTI-ICE SELECTED ON FOR TAKEOFF. NO AMBER BANDS ON N2 GAUGES OR WING ANTI-ICE ADVISORY MESSAGES. A BORTED TAKEOFF AT 55 KTS. ANTI-ICE CAME ON WHEN EXITING RUNWAY. WING ANTI-ICE TESTED NORMAL BEFORE TAKEOFF. PERFORMED WING ANTI-ICE OPS TEST, BOTH ENGINES ON. STANDBY AND NORMAL MODES TEST GOOD. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007020200160 20070202 00160 SO 2007 2 2 FAA200723001 1 20070123 A 5312 1159B2156227 ANGLE GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6108 NE BULKHEAD CRACKED W K NONE O OTHER IN INSP/MAINT 1 EA 29 254GA 11823 1032 DURING SCHEDULED 5000 LANDING FS793 BULKHEAD CAP ANGLE NDT INSPECTION, DETECTED A 1/25 INCH LONG CRACK IN RT BULKHEAD CA P ANGLE. MANUFACTURER HAS RECOMMENDED REPLACEMENT OF THE LT AND RT, FS793 BULKHEAD CAP ANGLES. 2 L 7 2 4F 4 F RT A12EA E25NE 2007020200161 20070202 00161 NM 2007 2 2 ASAA0741424 1 20070130 A 5330 65C357787 SKIN BOEING 737 737490 1384715 NM BS 986-1006 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 FOUND DENT IN FUSELAGE SKIN. REMOVED DAMAGED SECTION OF SKIN FABRICATED AND INSTALLED FILLERS AND DOUBLER IAW ASA EA 53 30 02175. 2 L 7 2 4F RT A16WE 2007020200162 20070202 00162 NM 2007 2 2 ASAA0741425 1 20070130 A 5330 SKIN BOEING 737 737490 1384715 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 FOUND DAMAGE TO EXISTING REPAIR DOUBLER. REMOVED EXISTING REPAIR PIECES TRIMMED OUT UPPER SKIN AREA WITH SHORT ED. FAB RICATED AND INSTALLED FILLERS DOUBLERS AND TRIPLER IAW ASA EA 5330 02176. 2 L 7 2 4F RT A16WE 2007020200164 20070202 00164 EU 2007 2 2 200701242 1 20070119 A 2780 FLAP SYSTEM EMB ERJ170 ERJ170100SE 3260406 EU LE FLAPS MALFUNCTIONED A UHLA O OTHER J WARNING INDICATION DE DESCENT 1 GL 17 647RW 17000067 FLIGHT 7527 IAD TO YYZ, ON DESCENT CREW WENT TO MOVE FLAPS DOWN AND RECEIVED FLAP FAIL MSG. CREW CYCLED FLAP/SLAT HANDL E THREE TIMES PER QRH. NO HELP. CREW WAS ABLE TO GET SLATS TO THREE WITH THE HANDLE AT FLAP ONE. FLIGHT TERMINATED WI THOUT INCIDENT. ON CALL MAINTENANCE CYCLED AIRCRAFT POWER, RAN FLAPS THREE TIMES, COULD NOT DUPLICATE FAULT. OPS CHECK NORMAL. 2 L 7 2 4F RT A56NM 2007020200165 20070202 00165 NM 2007 2 2 KCSA071058 1 20070201 A 5551 FITTING BOEING 747 747209F 1384800 NM DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 LT HORIZ STAB O/B HINGE FITTING UPPER TWO FASTENER HOLES DAMAGED, APPROX BS 2538. 2 L 7 4 4F RT A20WE 2007020200168 20070202 00168 EA 2007 2 2 COMA0760098 1 20070128 A 2751 852D10021 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA RT IB FLAP FAILED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 814CA 3082 7387 FLIGHT 5086 - FLAPS FAIL AT 500 FT ON APPROACH TO CVG FAILED AT 0 WHEN SELECTING 8 DEGREES. REMOVED AND REPLACED FLAP A CTUATOR. 2 L 7 2 4F RT A21EA 2007020200170 20070202 00170 NM 2007 2 2 CALA0700036 1 20070126 A 5315 BAC15181211 FLOORBEAM BOEING 737 737724 13844BY NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27733 28800 INSPECTION FOUND FLOORBEAM CORRODED AT BS 986.5 BETWEEN RBL 22.5 AND 43. THE FLOORBEAM WAS REPAIRED IAW ECRA 5320-01877 . 2 L 7 2 4F RT A16WE 2007020200173 20070202 00173 EA 2007 2 2 TRAX200700124 1 20070123 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA CABIN DELAMINATED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 PAX DOOR PLACARDS "EXIT" AND "TO OPEN LIFT AND PUSH" ARE DELAMINATED. 2 L 7 2 4F RT A21EA 2007020200177 20070202 00177 NM 2007 2 2 USAA070073 1 20070130 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 847 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 511AU 23594 FOUND FRAME CRACKED, BS 847 S-23R WL 160. REMOVED DAMAGE AND INSTALLED REPAIR ANGLES PER EA 98427 REV A, DEFECT SIZE: . 500. 2 L 7 2 4F RT A16WE 2007020200178 20070202 00178 NM 2007 2 2 USAA070072 1 20070130 A 5313 656177505 STRINGER BOEING 737 7373B7 1384580 NM BS 360 S14L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 511AU 23594 FOUND STRINGER CRACKED, FWD OF STA 360 FRAME S-14L. REPLACED PART PER SRM 510-10-02 AND BOEING DWG 65-17685, DEFECT SIZ E: .5". 2 L 7 2 4F RT A16WE 2007020200179 20070202 00179 NM 2007 2 2 USAA070071 1 20070130 A 5313 6916970501 STRINGER BOEING 737 7373B7 1384580 NM BS 348 S15L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 511AU 23594 FOUND STRINGER CRACKED, BS 348, S-15L BRACKET STRINGER ATTACH. REPLACED PART PER SRM 51-10-02, DEFECT SIZE: .5. 2 L 7 2 4F RT A16WE 2007020200180 20070202 00180 SO 2007 2 2 C2XA07BT009 1 20070126 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16559 145603 BTV FLT NR 2874 - DURING SERVICE/ROUTINE CHECK, FOUND PAX DOOR EMERGENCY LIGHT INOP. REPLACED BULB ON EMERGENCY LIGHT. OPS CHECK GOOD IAW EMB145 MM 33-50-09. 2 L 7 2 4T RT T00011AT 2007020200184 20070202 00184 SO 2007 2 2 C2XA07BT012 1 20070126 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 27 12924 145311 FLT NR 2312 - SMELLED BURNING ODOR 20 MINUTES AND 5 MINUTES BEFORE LANDING. NO SMOKE OBSERVED. FLT ATTENDANT SMELLED I T FIRST IN FWD CABIN. INSP COCKPIT AREA OVERHEAD PANELS, SIDE WALL PANELS UNDER COCKPIT FOORS RAN BOTH ENGINES AT MAX P OWER WITH ENGINE BLEEDS ON. INSP LEFT/RIGHT RELAY SUPPORTS AND LEFT/RIGHT WINDSHIELD HEAT CONTROLLERS AND LEFT/RIGHT DI STRIBUTION CONTACTERS BELOW FLIGHT ATTENDANT SEAT. NO FAULT FOUND. 2 L 7 2 4T RT T00011AT 2007020200185 20070202 00185 NM 2007 2 2 BB07013 1 20070129 A 3260 BULB BOEING 757 757225 1384959 NM MLG INDICATOR FAILED A USAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 19 925UW 22205 FLIGHT 714, CLT-PVD: ON APPROACH, CREW SELECTED GEAR DOWN AND FOUND MAIN GEAR INDICATIONS NOT WORKING PROPERLY. ABORTED APPROACH AND HAD TOWER VISUALLY CONFIRM GEAR DOWN. CREW SWAPPED BULBS AND HOUSINGS IN FLIGHT TO ASSURE GEAR DOWN. LANDE D WITH NO FURTHER DIFFICULTIES. MAINTENANCE REPLACED THE LEFT GEAR GREEN LIGHT CAPSULE AND REPLACED RIGHT GEAR AND NOSE GEAR LIGHT BULBS. 2 L 7 2 4F RT A2NM 2007020200186 20070202 00186 2007 2 2 UPS07149072 4 20070131 A 2565 PIN AIRBUS A300 A300F4622R 3930360 EU DOOR SLIDE STUCK A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 151UP 0834 UNABLE TO REINSTALL DOOR SLIDE SAFETY PIN AFTER THE SLIDE LEVER WAS MOVED TO DISARM POSITION. CYCLED SLIDE LEVER SEVERA L TIMES. INSERTED PIN IN DISARM POSITION SATISFACTORILY EACH TIME. OK TO CONTINUE. 2 L 7 2 4F RT A35EU 2007020200188 20070202 00188 NM 2007 2 2 UPS07449034 1 20070111 A 5330 SKIN BOEING 747 747123F NM BS 2200-2220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 AFT BULK CARGO COMPT FX SKIN FOUND CORRODED BTN BS 2200 TO BS 2220 STR 33R TO 34R AS MARKED. CORROSION BLEND OUT 0.035" BY 1/2" BY 4" EXCEED SRM LIMIT. FX BS 2193 TO BS 2217 BTN STR 31R TO STR 34R SKIN REPAIRED AS PER SRM 53-30-03 FIG 17. 2 L 7 4 4F A20WE 2007020200190 20070202 00190 NM 2007 2 2 UPS07449060 1 20070109 A 5322 65B38600365 SHEAR TIE BOEING 747 747123F NM BS 700 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO RT BS 700 STR 30R TIE CLIP FOUND CRACKED AS MARKED, CRACK LENGTH 1/4". FWD CARGO RT BS 700 STR 30R TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007020200192 20070202 00192 NM 2007 2 2 UPS07449062 1 20070110 A 5320 FLOOR SUPPORT BOEING 747 747123F NM BS 1525-1535 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 FOUND RBL117 FLR SUPPORT BS 1525-1535 CRACKED, CRACK LENGTH 7/8". BS 1525-1535 RBL117 FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2. 2 L 7 4 4F A20WE 2007020200194 20070202 00194 NM 2007 2 2 UPS07549042 1 20070105 A 5412 311N32712 BULKHEAD BOEING 757 75724APF 1384969 NM NR 2 NACELLE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 417UP 23904 NR 2 PYLON LOWER I/B CORNER OF MIDSPAR BULKHEAD IS HEAVILY CHAFED. ACCOMPLISHED PER FINAL EA 757-5453-27-A1592 AND UPS EO B757-5410-26011. 2 L 7 2 4F RT A2NM 2007020200197 20070202 00197 SO 2007 2 2 RAIA00701037 1 20070126 A 3411 08561UE PITOT HEAD EMB 145 EMB145 3260210 SO NR 3 UNKNOWN A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 806HK 18062 18062 145112 FLT NR 3554 - RIC - PITOT 3 INOP MESSAGE ON THE EICAS AFTER ENGINE START. MAINTENANCE REMOVED AND REPLACED THE NR 3 PIT OT PROBE. 2 L 7 2 4F RT T00011AT 2007020200199 20070202 00199 SO 2007 2 2 RAIA00701035 1 20070126 A 2197 WIRE EMB 145 EMB145LR 3260212 SO CABIN PRESSURE LOOSE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 837HK 145255 FLT NR 8010 - STL - NO CONTROL OF PRESSURIZATION IN AUTO OR MANUAL. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A LOOS E WIRE AT CB0029 "PRES CPAM" AND RESECURED IT. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007020500003 20070205 00003 2007 2 5 SWAA070494 4 20070131 A 2565 65659765 PLATE BOEING 737 7373H4 1384600 NM R1 DOOR SLIDE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FLOOR ATTACH PLATE CORRODED. REMOVED AND RE PLACED ATTACH PLATE PER SRM. 2 L 7 2 4F RT A16WE 2007020500004 20070205 00004 2007 2 5 SWAA070496 4 20070131 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM R2 DOOR SLIDE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2007020500005 20070205 00005 NM 2007 2 5 SWAA070513 1 20070131 A 5754 65C266011 SKIN BOEING 737 7373H4 1384600 NM NR 1 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED C1 CHECK, FOUND LEFT WING NR 1 L/E SLAT CRACKED AT LOWER AFT CORNER. REPAIRED SLAT PER SWA EA. 2 L 7 2 4F RT A16WE 2007020500006 20070205 00006 NM 2007 2 5 SWAA070491 1 20070131 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 663 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007020500007 20070205 00007 NM 2007 2 5 SWAA070492 1 20070131 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727D S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007020500008 20070205 00008 NM 2007 2 5 SWAA070493 1 20070131 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 766 S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 766, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007020500009 20070205 00009 NM 2007 2 5 SWAA070485 1 20070131 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 400 S14R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007020500014 20070205 00014 NE 2007 2 5 AMWA82088 2 20070117 A 7200 PT6A67DGG ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE LEFT DRAGGING A AMWA E A ENGINE SHUTDOWN UNSCHED LANDING A FLAME/FIRE CL CLIMB 1 CE 07 142YV 19431 8916 UE142 114390 HJ629 FLIGHT 450, AFTER TAKEOFF, CAPTAIN NOTICED LOUD (BANG) AND FLAMES COMING FROM LT ENGINE. PRIOR TO NOISE, ALL INDICATIONS REPORTED AS NORMAL. NO T-HANDLE (FIRE PULL) LIGHTS ILLUMINATED. CREW SHUT DOWN LT ENGINE, DISCHARGED LT FIRE BOTTLE, FI RE EXTINGUISHED AND AIRCRAFT RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. PASSENGERS WERE EVACUATED WITH ASSISTANCE O F AIRPORT EMERGENCY PERSONNEL WITH NO FURTHER INCIDENTS. SUBSEQUENT OBSERVATIONS BY COMPANY MAINTENANCE PERSONNEL SENT TO THE AIRCRAFT CONFIRMED (LT ENGINE HARD TO TURN BY HAND). NO EXTERNAL DAMAGE IN ENGINE COMPARTMENT OR EXCESSIVE OIL LE AKAGE NOTED. SUSPECT INTERNAL BRG FAILURE AS OF 1/18/07. ENGINE CURRENTLY BEING REMOVED FOR SHIPMENT AS A UNIT TO MFG F 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2007020500017 20070205 00017 CE 2007 2 5 AMW1070010901 1 20070108 A 5330 12940003197 SKIN PANEL BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA BS 213-220 CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV 24761 UE163 DISCOVERED DURING MAINTENANCE INSPECTION FOR PRESSURIZATION PROBLEM. MAINTENANCE FOUND THE FUSELAGE SKIN TO BE CRACKED ALONG THE RT SIDE OF THE NR 1 COMM ANTENNA. THE CRACK WAS 7 IN LONG, EXTENDING FROM APPROX FS 213.00 TO FS 220.750 RUNNI NG PARALLEL TO THE ANTENNA DOUBLER IN BETWEEN (STRINGERS) 1 AND 2R. REPAIRED CRACK IN FUSELAGE SKIN BETWEEN FS 213.00 A ND FS220.75. STOP DRILLED CRACK AT ALL ENDS, ONE CUT AWAY AREA APPROX. 2 INCHES BY 4 INCHES FABRICATED EXTERNAL DOUBLER (.040 INCH 2024-T3) AND FILLER (.025 INCH 2024-T3) INSTALLED DOUBLER AND FILLER WITH HYSOL EA9309.3NA IAW THE MFG INSTRU CTIONS. INSTALLED RIVETS WET WITH SEALANT. THERE IS AN EXISTING INTERNAL DOUBLER THAT IS REMOVED AND REINSTALLED. ALL A 2 L 7 2 4T 3 T RT A24CE E2NE 2007020500023 20070205 00023 NE 2007 2 5 AC2A113672 1 20070120 A 6500 7636104008101 COUPLING SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL TAIL ROTOR DRIVE CRACKED E AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 5447C 760180 COUPLING WAS FOUND CRACKED ON 110 HR, AIRFRAME INSPECTION. 1 G 7 2 3U 3 U H1NE E1GL 2007020500028 20070205 00028 SO 2007 2 5 SIMA200703309 1 20070201 A 5315 14500469401 FLOORBEAM EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL CORRODED CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 739AE 13518 4800 145402 FOUND UPPER FLOORBEAM AT FRAME 22 BETWEEN SERVICE DOOR AFT SILL AND CENTER HAT BEAM CORRODED. REMOVED AND REPLACED FLOO RBEAM IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007020500029 20070205 00029 SO 2007 2 5 SIMA200703302 1 20070201 A 3210 14571035409 CAP EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL LT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 739AE 13518 4800 145402 FOUND LT MLG BEARING CAP CORRODED. REMOVED AND REPLACED BEARING CAP IAW AMM 32-10-01. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007020500033 20070205 00033 CE 2007 2 5 DXTA200701901 1 20070201 A 3260 INDICATION SYS CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 983QS 7500083 NOSE WHEEL UNSAFE INDICATION. NOSE LIGHT NOT ILLUMINATED WITH GEAR HANDLE DOWN. COMPLETED EMERGENCY PROCEDURES AND BLEW GEAR DOWN. LIGHT STILL NOT ILLUMINATED. LIGHT ILLUMINATED APPOX 20 MIN AFTER LANDING. TIGHTENED BACKSHELL ON NOSEGEAR A CTUATOR DOWNLOCK SWITCH. RESET EMERGENCY GEAR EXTENSION BOTTLE & SYSTEM. PERFORMED SEVERAL GEAR SWINGS (15+) AND DID N OT HAVE ANY DEFECTS. LANDING GEAR SYSTEM AND GEAR INDICATION - OPS CHECKS GOOD AT THIS TIME. MAINTENANCE IAW CESSNA CE 750 MM 32-90-10 & 12-10-36 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007020500034 20070205 00034 CE 2007 2 5 DXTA200701902 1 20070201 A 2750 FLAP SYSTEM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 967QS 7500067 FLAPS FAIL CAS MSG. WOULD NOT RESET. FAILED WHEN FLAPS FULLY RETRACTED. REMOVED AND REPLACED RT RESOLVER WITH NEW. RIGG ED SYSTEM PER CESSNA 750 M/M CHAP 27-50-00. OP'S CHECKED GOOD REF WO 319330 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007020500036 20070205 00036 CE 2007 2 5 DXTA200701904 1 20070201 A 2170 WATER SEPARATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CABIN AIR ODOR E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 926QS 7500026 VERY STRONG ODOR IN CABIN, POSSIBLE PAC OIL BURNING SMELL. REMOVED AND CLEANED RT AND LT WATER SEPARATOR SOCKS IAW CESS NA AMM FOR MODEL 750 TASK # 12-10-01-160 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007020500040 20070205 00040 CE 2007 2 5 GUUA01310701 1 20070131 A 3246 13889 BEARING BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NOSE WHEEL FAILED A GUUA O OTHER O OTHER LD LANDING 1 SO 29 47542 396 2165 UE198 FLIGHT: 9179 FLL/EYW AFTER LANDING IN EYW FELT SOME VIBRATION LOST NOSE WHEEL. REPLACED NOSE GEAR ASSEMBLY AND NOSE WHE EL ASSEMBLY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007020500041 20070205 00041 CE 2007 2 5 DJFA2007013 1 20070126 A 5280 DOOR FRAME RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP NLG DOOR CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 843CW 258543 WHILE TROUBLESHOOTING A NOSE STEERING PROBLEM, MAINTENANCE FOUND THE LT NOSE GEAR DOOR FRAME CRACKED BEYOND THE LIMITS A CCEPTABLE IAW THE SRM. THE CRACK WAS APPROXIMATELY .5 INCHES IN LENGTH. MAINTENANCE PERFOMRED A REPAIR FROM ENGINEERIN G IAW EO 4731-187607 REV NC AS APPROVED ON 8110-3 DATE 29 JAN 2007. 2 L 7 2 4F 4 F RT A3EU E6WE 2007020500046 20070205 00046 SO 2007 2 5 IKJ2007F00000 2 20070118 A 8530 173116 CYLINDER CESSNA 206 TU206F 2073353 CE CONT O520 TSIO520C 17040 SO ENGINE CRACKED E IKJA O OTHER O OTHER NR NOT REPORTED 1 NM 07 8482Q 900 U20603340 CYLINDER DEVELOPED CRACK FROM INTAKE SEAT AROUND THE OUTER PORTION OF CYLINDER TO SPARK PLUG HOLE. CRACK FOLLOWED THE P ATH OF 1 OR 2 FINS AND WENT JUST AFT (CASE SIDE) OF FUEL INJECTOR PORT. THE CRACK WAS ALLOWING NOTICABLE FUEL LEAK/STAI N NEAR INJECTOR PORT AND AT THE 3 O`CLOCK POSITION FOLLOWING THE FINS TO THE RT. THE ENGINE HAD BEEN ON AIRCRAFT AS A R EBUILT EXCHANGE SINCE JULY 2004. (K) 1 H 7 1 3O 3 O A4CE E8CE 2007020500047 20070205 00047 NM 2007 2 5 07FDEA00226 1 20070131 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 380 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 MAIN DECK FLOORBEAM UPPER FLANGE IS CORRODED BS 380, LBL 28-31 WL208 BLENDED CORROSION AT STA 380 LBL 28-31. ROTO PEENE D, TREATED AND PRIMED AREA. REF EA NR 7-5310-106966, AND EA NR 7-5310-106966 REV A. 2 L 7 3 4F RT A3WE 2007020500051 20070205 00051 NM 2007 2 5 CALA0700041 1 20070126 A 5320 141A54103 INTERCOSTAL BOEING 737 737724 13844BY NM BS 280-294 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27733 28800 INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL BETWEEN STA 280 AND 294.5, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLAC ED IAW SRM 51-42-21. 2 L 7 2 4F RT A16WE 2007020500054 20070205 00054 CE 2007 2 5 DJFA2007014 1 20070128 A 2620 PIN RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP FIRE BOTTLE BENT E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 817TA 258552 DURING THE SCHEDULED REPLACEMENT OF THE SQUIBS AND FIRE BOTTLES MAINTENANCE DISCOVERED A PIN BENT OVER ON THE FORWARD FI RE BOTTLE SQUIB WHICH WOULD HAVE PREVENTED THE DISCHARGE OF THE BOTTLE DURING AN EMERGENCY. THE SDR WILL BE UPDATED UPO N COMPLETION OF THE CORRECTIVE ACTION. 2 L 7 2 4F 4 F RT A3EU E6WE 2007020500055 20070205 00055 NE 2007 2 5 KCSA07011 2 20070201 A 7200 ENGINE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 4 FLAMED OUT A KCSA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 23 716CK 19753 FLT LEVEL 34.0 NR 4 ENG FLAMED OUT, DESCENDED TO F.L 280. RESTARTED ENG - ALL PARAMETERS NORMAL. ENG RESTARTED ON FIRST ATTEMPT. CLIMBED TO FL 340 ENG OPERATES NORMAL. PERFORMED ENG FLAME OUT INSPECTION IAW MM 71-00-42 P-118. PERFORMED ENG WINDMILL INSPECTION IAW MM 72-00-00 P-682R. NO DAMAGE OR DEFECTS FOUND. NR 4 ENGINE OPS CHECKS NORMAL IAW MM 71-00-00 P-235. 2 L 7 4 4F 4 F A20WE E20EA 2007020500056 20070205 00056 CE 2007 2 5 DXTA200701892 1 20070130 A 3260 UNKNOWN CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG UNKNOWN E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 699QS 5605199 AFTER GEAR RETRACTION, ALL GREEN LIGHTS WENT OUT BUT THE RED UNLOCK STAYED ON. PULLED THE GEAR CONTROL CB AND THE RT MAI N WENT TO DOWN AND LOCKED. THE LT MAIN AND NOSE REMAINED UP WITH LIGHTS OFF. REPLACED UPLOCK ACTUATOR AND RIGGED UPLOCK SWITCH PER 560XL M/M, CH - 32-30-05, LEAK AND OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007020500057 20070205 00057 CE 2007 2 5 012807N514CS1 1 20070128 A 3233 99125373 ACTUATOR CESSNA 560 560XL 2076702 CE MLG MALFUNCTIONED E Z5FA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 63 514CS 4081 5605328 DURING FINAL APPROACH, THE GEAR WAS SELECTED DOWN. THE LT MAIN FAILED TO GIVE A DOWN AND LOCKED INDICATION AND THE RED UNLOCKED LIGHT STAYED ON. THE CREW DECLARED AN EMERGENCY AND USING THE CHECKLIST THE GEAR WAS BLOWN DOWN. THE GEAR STI LL DID NOT INDICATE DOWN AND LOCKED. THE CREW REQUESTED A TOWER FLY-BY TO SEE IF GEAR WAS DOWN. TOWER REPORTED GEAR LO OKED DOWN, DURING CLIMB OUT TO SET UP APPROACH THE INDICATOR SWITCHED AND ALL DOWN AND LOCKED INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITH NO PROBLEM. LOCAL MAINTENANCE CHANGED GEAR ACTUATOR, PERFORMED ALL REQUIRED CHECKS WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE 01/30/2007. 2 L 7 2 4F RT A22CE 2007020500059 20070205 00059 NM 2007 2 5 SWAA070489 1 20070131 A 5315 6546809 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, LBL 5 AND LBL 11. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007020500061 20070205 00061 NM 2007 2 5 SWAA070519 1 20070131 A 5315 6546810 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 967, RBL 28 TO RBL 42. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007020500062 20070205 00062 NM 2007 2 5 SWAA070495 1 20070131 A 5315 6546811 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 45 TO LBL 27. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007020500063 20070205 00063 NM 2007 2 5 SWAA070488 1 20070131 A 5315 6546811 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 43. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007020500064 20070205 00064 NM 2007 2 5 SWAA070504 1 20070131 A 5551 6547450 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND VERTICAL STAB FITTING CLEVIS LUG FACES CORRODED. REPAIRED VERTICAL STAB FITTING PER E R. 2 L 7 2 4F RT A16WE 2007020500065 20070205 00065 NM 2007 2 5 SWAA070501 1 20070131 A 5330 6550570 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT LOWER FWD CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007020500067 20070205 00067 NM 2007 2 5 SWAA070547 1 20070201 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, LBL 63, WL 202. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2007020500068 20070205 00068 NM 2007 2 5 SWAA070552 1 20070201 A 5322 6546546 SHEAR TIE BOEING 737 7373T5 1384608 NM BS 767 S26L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007020500070 20070205 00070 NM 2007 2 5 SWAA070526 1 20070131 A 5322 6546546 SHEAR TIE BOEING 737 7373T5 1384608 NM BS 727E S19R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, STR 19R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007020500072 20070205 00072 NM 2007 2 5 SWAA070546 1 20070201 A 5311 6546548 FRAME BOEING 737 7375H4 138449D NM BS 747 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020500073 20070205 00073 NM 2007 2 5 SWAA070529 1 20070131 A 5312 6546568 BULKHEAD BOEING 737 7373T5 1384608 NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 4 O'CLOCK POSITION. REPAIRED WEB PER SR M. 2 L 7 2 4F RT A16WE 2007020500074 20070205 00074 NM 2007 2 5 SWAA070528 1 20070131 A 5312 6546568 BULKHEAD BOEING 737 7373T5 1384608 NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 2 O'CLOCK POSITION. REPAIRED WEB PER SR M. 2 L 7 2 4F RT A16WE 2007020500076 20070205 00076 NM 2007 2 5 SWAA070545 1 20070201 A 5311 6546596 FRAME BOEING 737 7375H4 138449D NM BS 727B S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020500078 20070205 00078 NM 2007 2 5 SWAA070530 1 20070131 A 5753 65C26310 SKIN BOEING 737 7373T5 1384608 NM LT WING MID FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND LT WING INBOARD MID FLAP OUTBOARD T/E DELMAINATED. REPAIRED MID FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007020500084 20070205 00084 WP 2007 2 5 AALA20070160 1 20070122 A 4940 STARTER PWA DOUG DC9 DC982 3022082 WP APU LEAKING A AALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 456AA P80406 49561 ORD INFLIGHT, SMOKE AND FUMES REPORTED AFTER TAKEOFF. ENGINE ANTI ICE ON PACKS MEDIUM SETTING. SMOKE DISSIPATED WITH R EDUCTION IN POWER AND TEMPERATURE CONTROLLERS SET TO FULL COLD. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED AUXILIARY POWER UNIT DUE TO OIL LEAK AT MATING SURFACE OF STARTER. PERFORMED PACK BURN. SYSTEM GROUND CHECKED NORMAL O PERATION. 2 L 7 2 4F A6WE 2007020500085 20070205 00085 2007 2 5 AALA20070161 4 20070122 A 2565 SLIDE BOEING 757 757223 1384957 NM CABIN UNKNOWN A AALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 647AM 24605 MIA - AFTER LANDING, CREW RECEIVED A LEFT WING SLIDE EICAS MESSAGE MOMENTARILY. REPLACED LEFT OVERWING SLIDE PACK ASSEM BLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007020500086 20070205 00086 WP 2007 2 5 AALA20070162 1 20070122 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 287AA 49299 YUL - EMERGENCY LIGHT BATTERY PACKS IN CABIN INOPERATIVE. BATTERY SWITCH LEFT ON. REPLACED EMERGENCY LIGHT BATTERY PAC KS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007020600001 20070206 00001 EU 2007 2 6 U0GA113886 1 20070123 A 6321 109011226103 DAMPER AGUSTA A109 A119 0261102 EU PWA PT6 PT6* 52043 EA ROTOR BRAKE SHEARED B U0GA O OTHER E VIBRATION/BUFFET LD LANDING 1 SW 03 822MM 598 14055 PILOT FELT VIBRATION WHEN ROTOR BRAKE WAS ENGAGED AFTER LANDING AND SHUTDOWN. POSTFLIGHT INSPECTION REVEALED THE DAMPER HAD SHEARED AT THE ROD END FLUSH WITH THE OUTER THREADED PORTION OF THE DAMPER ASSEMBLY 1 G 7 2 3U 3 T H7EU E2NE 2007020600002 20070206 00002 SW 2007 2 6 AC2A113940 1 20070127 A 6320 427040006111 TRANSMISSION BELL 427 427 1182207 SW PWC PW207 PW207D NE MAIN ROTOR MAKING METAL D AC2A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 07 427CU 1346 56047 TRANSMISSION CHIP LIGHT. CALLED MECHANIC OUT TO AIRCRAFT TO CHECK AND VERIFY TRANSMISSION CHIP PLUG CONTAMINATION. MECHA NIC FOUND THIN HAIRLIKE SLIVER OF METAL APPROX. .2500 INCH LONG ACROSS CONTACTS OF PLUG. CLEANED OF CHIP DETECTOR AND RE INSTALLED. NO FURTHER MAINTENANCE IS REQUIRED FOR THIS SIZE CHIP IAW MAINTENANCE MANUAL INSTRUCTIONS. 1 G 7 1 3U 3 U R00001RC E42NE 2007020600003 20070206 00003 EA 2007 2 6 COMA0760114 1 20070131 A 2750 1104SD100401 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS WORN A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 806CA 7359 FLIGHT 5375 - DURING YHZ APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. REPLACED THE RIGHT WING NR 4 FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2007020600004 20070206 00004 NM 2007 2 6 DXTA200701910 1 20070204 A 2120 UNKNOWN AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE CABIN ODOR E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 259QS 159 DURING CLIMB OUT AROUND 7000 FT THE AIRPLANE FILLED WITH THE ODOR OF WHAT APPEARED TO BE AN ELECTRICAL FIRE. NO SMOKE WA S NOTICED BY ANYONE. THE SMELL DISSIPATED AFTER APPROXIMATELY 2 MINUTES THEN RETURNED INTERMITTENTLY. THE ODOR CAME BACK FAIRLY STRONG WHEN THE APU WAS TURNED ON AFTER LANDING. RETURNED TO DEPARTURE. NO EMER. DECLARED. RAN APU AND NR 1 A ND 2 ENGINES. OPERATED AIR CONDITIONER IN HOT & COLD. NO ODERS NOTED. REMOVED PFD & MFD (COPILOTS) INSPECTED BEHIND I NSTRUMENT PANEL WITH NO DISCREPANCIES NOTED. INSPECTED BLEAD AIR LINES FOR EVIDENCE OF OIL. NO OIL NOTED. INSPECTED C O-PILOTS DV WINDOW CONECTIONS, NO DISCREPANCIES NOTED. 2 K 7 2 4F 4 F RT A50NM E44NE 2007020600006 20070206 00006 NM 2007 2 6 BB07014 1 20070202 A 3350 1630080 BATTERY PACK BOEING 757 757225 1384959 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 924UW 22204 MID SECTION OF CABIN EMERGENCY LIGHTS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT THE 2L DOOR. 2 L 7 2 4F RT A2NM 2007020600008 20070206 00008 SO 2007 2 6 SIMA200703307 1 20070201 A 3210 14571035409 CAP EMB 135 EMB135LR 3260305 SO RT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 739AE 13518 4800 145402 FOUND RIGHT MAIN LANDING GEAR BEARING CAP CORRODED. REMOVED AND REPLACED BEARING CAP IAW EMB AMM 32-10-01. RETURNED AI RCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007020600009 20070206 00009 SO 2007 2 6 SIMA200703306 1 20070201 A 3210 14571035409 CAP EMB 135 EMB135LR 3260305 SO LT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 739AE 13518 4800 145402 FOUND LEFT MAIN LANDING GEAR BEARING CAP CORRODED. REMOVED AND REPLACED GEAR CAP IAW EMB AMM 32-10-01. RETURNED AIRCRA FT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007020600011 20070206 00011 SO 2007 2 6 SIMA200703301 1 20070201 A 5347 14530658005 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 739AE 13518 4800 145402 FOUND SEAT TRACK FROM FRAME 36 TO FRAME 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AI RCRAFT TO SERVICE 2 L 7 2 4F RT T00011AT 2007020600012 20070206 00012 SO 2007 2 6 SIMA200703308 1 20070201 A 5347 13500438001 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 739AE 13518 4800 145402 FOUND RIGHT INBOARD SEAT TRACK CORRODED BETWEEN FRAME 24 TO FRAME 36. REMOVED AND REPLACED SEAT IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007020600013 20070206 00013 SO 2007 2 6 SIMA200703304 1 20070201 A 5347 13500438001 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 739AE 13518 4800 145402 FOUND RIGHT SEAT TRACK BETWEEN FRAME 24 TO FRAME 36 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007020600014 20070206 00014 SO 2007 2 6 SIMA200703305 1 20070201 A 5347 14530658005 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 739AE 13518 4800 145402 FOUND RIGHT INBOARD SEAT TRACK FROM FRAME 36 TO FRAME 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 56-10-01 . RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007020600015 20070206 00015 NM 2007 2 6 CALA0700046 1 20070127 A 5270 MS25307272 SWITCH BOEING 757 757324 1384930 NM AFT CARGO DOOR INOPERATIVE A CALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 27 75853 32812 A NOISE WAS HEARD FROM AROUND THE R-3 DOOR AFTER LANDING AT IAH. MAINTENANCE FOUND THE AFT CARGO DOOR OPERATIONAL SWITC H WAS STICKING INTERMITTENTLY IN THE CLOSED POSITION CAUSING THE DOOR TO CONTINUE TO CLOSE AFTER THE SWITCH WAS RELEASED . THE CARGO DOOR SWITCH WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A2NM 2007020600017 20070206 00017 NM 2007 2 6 SWAA070531 1 20070131 A 5753 69378151 TORQUE TUBE BOEING 737 7373T5 1384608 NM TE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND LEFT INBOARD FORE FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007020600026 20070206 00026 NM 2007 2 6 UIEA200700061 1 20070202 A 5743 65B1090118 BEAM BOEING 747 7472D7B 1384803 NM RT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523 21782 DURING NDT INSPECTION OF THE RT WING GEAR DOOR ACTUATOR BEAM IAW NDT MANUAL D6-7170, PART 4, 32-10-01. FOUND ACTUATOR B EAM BEARING BORE HOLE CRACKED. CRACK LOCATED WITHIN THE REQUIRED INSPECTION AREA. REPLACED ACTUATOR BEAM IAW AMM 32-32 -28. 2 L 7 4 4F RT A20WE 2007020600028 20070206 00028 CE 2007 2 6 DXTA200701908 1 20070202 A 3241 ANTI-SKID SYS CESSNA 560 560XL 2076702 CE MALFUNCTIONED E DXTA O OTHER J S WARNING INDICATION AFFECT SYSTEMS LD LANDING 1 GL 07 657QS 5605636 AT FL 320 ANTI-SKID ILLUMINATED STEADY THEN FLASHED RESET TO STEADY. WHEN GEAR WAS LOWERED, LOW BRAKE PRESS ILLUMINATED , FLASHING. CONDUCTED APPRORIATE CHECKLISTS, THEN LANDED USING EMER BRAKES, TOWED TO PARKING. T/S TO PWR BRAKE C/B. R EMOVED & REPLACED PWR BRAKE C/B. BLED BRAKE SYS. RAN AIRCRAFT & TAXIED FOR OPS CHECK OPS CHECKED GOOD ALL WORK IAW C E560XL M/M 24-00-00 & 32-42-00 2 L 7 2 4F RT A22CE 2007013100261 20070131 00261 NM 2007 1 31 07FDEA00208 1 20070131 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 312 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 MAIN DECK FLOORBEAM LOWER FLANGE IS CORRODED AT BS 312, RBL 44, WL 200 AT STANDOFF. REMOVED CORROSION REF SRM 51-10-0 6, MADE REPAIR ANGLES DRILLED UP AND INSTALLED REPAIR REF SRM 53-10-8 PG 39 - 43. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007013100263 20070131 00263 EA 2007 1 31 COMA0760080 1 20070126 A 2750 SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS DAMAGED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 528CA 7841 FLIGHT 5510 - FLAP FAIL MESSAGE AT 8 DEGREES. LANDED WITHOUT INCIDENT. PERFORMED EO 27-046 AD INCLUDING FLAP SHAFT REJ UVENATION. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007013100270 20070131 00270 SO 2007 1 31 RAIA00701039 1 20070127 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 818HK 145059 PRE FLT NR 5535 - STL - EMERGENCY LIGHTS AT COCKPIT STEP AND FORWARD CEILING INOP. MAINTENANCE RESEATED THE CONNECTOR T O THE CONTROLLING INVERTER. 2 L 7 2 4T RT T00011AT 2007020100004 20070201 00004 NM 2007 2 1 SWAA070478 1 20070130 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 277 S11L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 11L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007020100019 20070201 00019 EA 2007 2 1 COMA0760102 1 20070130 A 3020 5399001 VALVE CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 779CA 5789 7306 FLIGHT 5269 - DURING CLIMBOUT OF CVG RECEIVED A LEFT ENGINE COWL ANTI-ICE CAUTION MESSAGE, FLIGHT RETURNED TO CVG. REPL ACED THE LEFT ENGINE ANTI-ICE COWL VALVE. 2 L 7 2 4F RT A21EA 2007020100024 20070201 00024 NM 2007 2 1 SWAA070477 1 20070130 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 827 S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007020100030 20070201 00030 NM 2007 2 1 SWAA070466 1 20070130 A 3350 MS155721 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007020200001 20070202 00001 NM 2007 2 2 QXEA200700122 1 20070131 A 2840 BULB DHAV DHC8 DHC8202 2809007 NM FUEL INDICATOR BURNED OUT A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 09 357PH 504 SEA FLIGHT NR 2224, "TANK 2 AUX PUMP" LIGHT BURNED OUT. MAINTENANCE RELAMPED TANK 2 AUX PUMP LIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007020200006 20070202 00006 CE 2007 2 2 DXTA200701897 1 20070131 A 2120 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 934QS 7500034 AC HAS BAD ODOR. SMELLS LIKE ACM EVAPORATOR SOCKS & PACKINGS. INSTALLED NEW COALESCER SOCKS W/PACKINGS IAW CE750 MM CHA P 21-51-00. NO FURTHER DEFECTS NOTED - OPS CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007020200009 20070202 00009 NM 2007 2 2 C1HA200793004 1 20070131 A 5313 69436951 STRINGER BOEING 727 727212 138407G NM BS 738 S27L CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 FOUND CORROSION ON STR 27L AT BS 737 FWD PIT. REPAIRED AREA AS REQUIRED IAW CHAMPION AIR EO 727-5331-18. 2 L 7 3 4F A3WE 2007020200010 20070202 00010 NM 2007 2 2 C1HA200793005 1 20070131 A 5320 SILL BOEING 727 727212 138407G NM BS 950-983 CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 C2 - DOOR SILL ON FUSELAGE FRAME HAS CORROSION. REPAIRED AREA AS REQUIRED IAW CHAMPION AIR EO 727-5314-02 2 L 7 3 4F A3WE 2007020200020 20070202 00020 WP 2007 2 2 07FDEA00222 1 20070131 A 5310 BEAM DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 CTR CARGO COMPT SUMP AREA FOUND SEVERE CORROSION ON BEAM AT STA 1721 LONG NR 45 LT. REMOVED CORROSION IAW SRM 51-21-01 VOL 2 PAR 34. MAX REMOVED IS .056", REMAINING MAT IS .035", PERCENT REMOVED IS 61 PERCENT, ORIGINAL THK .091". OUT OF LIMITS IAW SRM 53-15-01 VOL 3 FIG 6 AND SRM 53-00-01 VOL 1 FIG 1B. VERIFIED BY NDT INSPECTION SEE JPF. FAB AND INSTALL ED NEW PART IAW SRM 53-60-01 VOL 1 FIG 3. REPLACED FASTENERS IAW SRM 51-35-01 AND SRM 51-33-01 VOL 2. REPROTECTED AREA IAW SRM 51-21-01 VOL 2 PAR 31-24. 2 L 7 3 4F A22WE 2007020200035 20070202 00035 WP 2007 2 2 UPS07849046 1 20070105 A 5340 5646955503 FITTING DOUG DC8 DC871F 302199D WP FS 960 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 - FOUND LONGERON TO FLOORBEAM FITTING HEAVY CORRODED AND CRACKED AT STA 960 L21R. REMOVED AND REPLAC ED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007020200037 20070202 00037 WP 2007 2 2 UPS07849052 1 20070104 A 5720 SAA75293143 INTERCOSTAL DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 - FOUND IB UPPER RIB OF OB SLOT DOOR STRUCTURE HAS 4" CRACK,CENTER LEADING EDGE LW ABOVE PNEUMATIC DU CT. REMOVED, STOP DRILLED CRACK, FABRICATED AND INSTALLED 1 INTERCOSTAL, AND 1 REPAIR ANGLE IAW SRM 51-1-20D, 57-03-01- 0, 51-03-02. 2 L 7 4 4F RT 4A25 2007020200045 20070202 00045 NM 2007 2 2 CALA0700045 1 20070126 A 5320 141A541016 INTERCOSTAL BOEING 737 737724 13844BY NM BS 328-344 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27733 28800 INSPECTION FOUND A 1/2" CRACK IN INTERCOSTAL BETWEEN STA 328 AND 344, LBL 35. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-42-21. 2 L 7 2 4F RT A16WE 2007020200068 20070202 00068 NM 2007 2 2 SWAA070465 1 20070129 A 3350 307IBPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 442WN 32459 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 20 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007020200077 20070202 00077 CE 2007 2 2 DXTA200701893 1 20070130 A 2612 FIRE DETECTOR RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP CARGO BAY MALFUNCTIONED E DXTA O OTHER N FALSE WARNING LD LANDING 1 GL 07 875QS 258375 BAGGAGE FIRE LIGHT FLASHES INTERMITTENTLY UPON LANDING. TESTED MWS AND LIGHT WOULD NOT COME ON. COULD NOT DUPLICATE SMO KE DETECTOR FAILURE. CLEANED CONTACTOR EYES & CONNECTORS FOR EACH OF THE THREE DETECTORS. RETESTED & FOUND NO DISCREPA NCIES AT THIS TIME. WORK DONE IAW 26-11-00 OF THE HAWKER 800 XP AMM. 2 L 7 2 4F 4 F RT A3EU E6WE 2007020200079 20070202 00079 CE 2007 2 2 DXTA200701895 1 20070130 A 3260 LANDING GEAR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MALFUNCTIONED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 694QS 5605194 GEAR UNLOCKED LIGHT REMAINS ON AFTER GEAR RETRACTION. CYCLED BREAKER NO CHANGE. RETURN TO FIELD. JACKED AIRCRAFT & SW UNG GEAR SEVERAL TIMES & COULD NOT DUPLICATE SQK. REPLACED NOSE GEAR UPLOCK SWITCH WITH NEW UNIT IAW CE560XL M/M CHAP 32 -61-00. GEAR SWING & OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007020200091 20070202 00091 EU 2007 2 2 DHL2007362517 1 20070106 A 5320 PAN AIRBUS 300 A300B4203 3930306 EU CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 CABIN FLOOR SUPPORT WEB PAN BETWEEN LBL 96 AND LBL 17 AT FR 30 HAS CORROSION. REMOVED FASTENERS AT CABIN FLOOR SUPPORT WEB PAN BETWEEN LBL 17 TO LBL 96 FR 30 FOR ACCESS OF CORROSION AS PER A300 SRM 51-30-30. REMOVED CORROSION FROM LBL 17 T O LBL 36 AND LBL 56 TO LBL 96 MAT LOSS .004 ORIG MAT .040 MAT REMAINING .036 AS PER A300 SRM 51-40-11 FOUND WITHIN LIMIT S PER A300 SRM 51-41-20. REMOVED CORROSION FROM LBL 36 TO LBL 56 PER A300 SRM 51-40-11 FOUND OUT OF LIMITS AT LBL 49, CU T OUT DAMAGE AREA 7"1 3/4" FROM LBL 36 TO LBL 56 FR 30 PER A300 SRM 51-41-20 FIG 702. TREATED WITH ALODINE AND PRIMED A ND GRAY PAINT AREA AND PARTS REPAIR PER A300 SRM 51-40-12 AN INSTALLED FAST AND WEB REPAIR PER A300 SRM 51-30-30 AND 51- 2 L 7 2 4F RT A35EU 2007020200093 20070202 00093 NM 2007 2 2 AT0700012 1 20070116 A 2820 366200001 SELECTOR PANEL BOEING 717 717200 1383700 NM FUEL SYSTEM INOPERATIVE A ZZDA B EMER. DESCENT O OTHER TO TAKEOFF 1 SO 15 979AT 55038 AFTER TAKEOFF, NOTICED FUEL MIGRATION IMBALANCE OCCURING. RIGHT TANK WAS +600 LBS. DECLARED EMERGENCY. UPON LANDING F UEL TOTALIZER (X) OUT THEN CAME BACK LATER. REMOVED AND REPLACED LSDU IAW AMM 28-41-20, OPS CHECK GOOD. PN/OFF/ON-366- 200-001, SN/OFF-1137, SN/ON-1063. 2 L 7 2 4F TR A6WE 2007020200112 20070202 00112 NM 2007 2 2 07FDEA00238 1 20070201 A 5512 SKIN BOEING 727 727233 138408A NM ZONE 300 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 RT HORIZ STAB OUTBD BALANCE BAY PANEL UPPER SKIN, PANEL IS GOUGED ON INNER SURFACE OUTBD SIDE. REMOVED EXISTING DOUBLER , VERIFY NO DAMAGE NOTED. FABRICATED, TREATED AND PRIMED, AND REINSTALLED REPAIR. REF SRM 55-20-3 FIG 7 SHEET 1, PG 4. 2 L 7 3 4F RT A3WE 2007020200126 20070202 00126 NM 2007 2 2 SWAA070484 1 20070131 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM BS 304 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 304, STR 10L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007020200128 20070202 00128 NM 2007 2 2 SWAA070498 1 20070131 A 5330 6545857 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT R2 DOOR LOWER HINGE CUTOUT LOWER AFT CORNER CRACKED. REPAIRED SKIN PE R SWA EA. 2 L 7 2 4F RT A16WE 2007020200130 20070202 00130 NM 2007 2 2 SWAA070505 1 20070131 A 5311 6546525 FRAME BOEING 737 7375H4 138449D NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020200146 20070202 00146 2007 2 2 DHL2007745004 2 20070118 A 7200 ENGINE BOEING 727 727224 1384076 NM NR 2 MALFUNCTIONED A DHLA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 01 745DH 20665 NR 2 ENGINE N1 GAUGE FLUCTUATED RAPIDLY FINALLY WENT TO 0 NR 2 ENGINE OIL TEMP IN YELLOW. C/W ABNORMAL PROCEDURES INFLI GHT SHUTDOWN. COMPLETED OIL TEMP IN YELLOW ARC PRIOR TO ABOVE PROCEDURE. REMOVED AND REPLACED NR 2 ENGINE ASSY IAW B72 7 MTM 71.1. 2 L 7 3 4F A3WE 2007020200147 20070202 00147 CE 2007 2 2 BSYA200700005 1 20070131 A 3200 LANDING GEAR LEAR 35 35A 5170602 CE MALFUNCTIONED E BSYA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 64CP 264 ON ARRIVAL INTO STP SELECTED GEAR DOWN NOTHING HAPPENED, THEN BLEW GEAR DOWN AND LANDED NO PROBLEMS. MAINTENANCE COULD NOT DUPLICATE PROBLEM, CLEANED AND LUBED SWITCHES CYCLED GEAR MANY TIMES, OPS CHECKS GOOD. 2 L 7 2 4F A10CE 2007020200148 20070202 00148 EA 2007 2 2 COMA0760082 1 20070127 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NOSE HYD BAY FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 809CA 17776 7366 FLIGHT 5389 - RECEIVED GEAR DISAGREE DURING EXTENSION INDICATION NOSE GEAR MALFUNCTION. PRIOR TO QRH COMPLETION, MESSAG E DISAPPEARED. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR PRIORITY VALVE, CLEANED AND LUBRICAT ED NOSE LANDING GEAR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007020200149 20070202 00149 EA 2007 2 2 COMA0760083 1 20070127 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA LEFT MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 436CA 7482 FLIGHT 5683 - WHEN POWER LEVER IS ADVANCED AND ECS DUCT PRESSURE EXCEEDS 60 PSI, LT PACK TRIPS OFF AND LT PACK HIGH PRES SURE MESSAGE COMES ON. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. PERFORMED OPS CHECK OF AIR CONDITIONING SYSTEM. CO ULD NOT DUPLICATE PROBLEM. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007020200166 20070202 00166 NM 2007 2 2 0700405507 1 20070129 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 507US 23196 NUMEROUS FORWARD, MIDDLE EMERGENCY LIGHTS INOPERATIVE. REPLACED-2 RIGHT DOOR POWER SUPPLY AND BATTERY PACK; STOCK NR 55 -3300-4-0138 AND 55-3300-4-0007. ALL LIGHTS ILLUMINATE EXCEPT TWO LEFT BULL NOSE LIGHTS, AFT OF DOOR 2 LEFT; REQUIRES S TOCK NR 55-3300-4-0138 AND 55-3300-4-0007 PER WDM 33-51-13. POWER SUPPLY PLACED ON MEL 33-51-1. REMOVED AND REPLACED E MERGENCY LIGHT POWER SUPPLY AND BATTERY PACK OVER 2 LEFT DOOR (M733) PER AMM 30-51-07 OPS CHECK OKAY. OKAY FOR SERVICE. 2 L 7 2 4F RT A2NM 2007020200167 20070202 00167 CE 2007 2 2 E07A0709001 1 20070109 A 2121 903840311 MOTOR BEECH 90 C90A 1152911 CE BLOWER BURNED OUT I E07A G O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CE 07 395AS 674 LJ1575 ON APPROCAH THE CABIN FAN BLOWER GOT HOT AND PUT SMOKE IN THE CABIN. 1 L 7 2 3T RT 3A20 2007020200171 20070202 00171 NM 2007 2 2 CALA0700037 1 20070110 A 5542 173A01037 SKIN BOEING 737 737824 13844BZ NM RUDDER DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 37267 31586 INSPECTION FOUND THE RIGHT SIDE OF RUDDER SKIN TRAILING EDGE DAMAGED BY LIGHTNING STRIKE NEAR THE TOP BETWEEN THE TWO ST ATIC WICKS. REPAIRED RUDDER SKIN IAW ECRA 5540-01229. 2 L 7 2 4F RT A16WE 2007020200172 20070202 00172 NM 2007 2 2 CALA0700038 1 20070122 A 5720 6545402279 STIFFENER BOEING 737 7373T0 1384582 NM WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 47332 23570 INSPECTION FOUND A CRACK IN THE WING CENTER SECTION REAR SPAR VERTICAL STIFFENER AT RBL 6.15. THE STIFFENER WAS REPAIRE D IAW ECRA 5714-01019. 2 L 7 2 4F RT A16WE 2007020200183 20070202 00183 SO 2007 2 2 C2XA07BT011 1 20070126 A 3397 7287500605 WIRE HARNESS EMB 145 EMB145LR 3260212 SO CABIN LIGHTS BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 13949 145057 FLT NR 1271 ABOVE SEAT 15A PASSENGER REPORTED SEEING SMOKE AND BURNING SMELL. REMOVED AND REPLACED SIDEWALL LIGHT HARNE SS IAW EMB145 IPC 33-21-06. OPS CHECK GOOD IAW EMB145 AMM 33-21-00. 2 L 7 2 4T RT T00011AT 2007020200187 20070202 00187 NM 2007 2 2 UPS07449033 1 20070110 A 5320 69B621001 FLOOR SUPPORT BOEING 747 747123F NIR NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 FOUND BS 1760 FLOOR SUPPORT PLATE RBL65-70 CORRODED. CORROSION BLEND OUT 0.035" BY 1" BY 1" EXCEED SRM LIMIT. SUPPORT PLATE REPLACED AS PER MM 20-51-01. 2 L 7 4 4F RT A20WE 2007020200191 20070202 00191 NM 2007 2 2 UPS07449061 1 20070109 A 5340 65B018589 STRINGER CLIP BOEING 747 747123F NM BS 1980 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C BULK CARGO COMPT FLOOR SUPPORT FRAME ATT STRINGER CLIP FOUND CORROSION AT STA 1980 RBL41 STR 45R. COR ROSION BLEND OUT 0.050" BY 1" BY 1" EXCEED SRM LIMIT. BULK CARGO COMPT FLOOR SUPPORT FRAME ATTACH STRINGER CLIP REPLACE D AS PER SRM 51-10-01 P9 AND INSTALLED AS PER SRM 51-30-02 JUST AT BS1980 R13L AND S45R. 2 L 7 4 4F A20WE 2007020200196 20070202 00196 EU 2007 2 2 YENA2007004 1 20070126 A 3610 10070863 VALVE EMB ERJ190 ERJ190100IGW 3260408 EU GE CF34 CF3410E6 30015 NE NR 1 BLEED SYS FAILED A YENA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 EA 15 198JB 993 19000021 E994155 BLEED OVERPRESS AFTER T/O - BLEED NR 1 QRH PROCEDURE CLEARED MSG. A-I WING FAIL - EICAS MSG DURING CLIMBOUT. ACCOMPLIS HED QRH PROCEDURE. MSG REMAINED. MSG CAUSED BY FAILURE OF FAN AIR VALVE REPLACED NR 1 ENG FAN AIR VALVE PER AMM 36-11- 09. PERFORMED POWER RUN. RUN CHECK IS GOOD. A/C CLEARED FOR SERVICE. MSG CLEARED. 2 L 7 2 4F 4 F RT A57NM E00070EN 2007020500010 20070205 00010 NM 2007 2 5 SWAA070514 1 20070131 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 431WN 29845 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007020500020 20070205 00020 CE 2007 2 5 AMWA81913 1 20070108 A 3233 ACTUATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT MLG FAILED A AMWA O OTHER J WARNING INDICATION AP APPROACH 1 CE 07 174YV UE174 ON APPROACH, THE CREW PLACED THE GEAR HANDLE DOWN. THE LT MAIN LANDING GEAR INDICATOR FAILED TO ILLUMINATE. THE CREW PE RFORMED THE INDICATOR LIGHT TEST AND FOUND THE ANNUNCIATOR TO BE OPERATIVE. THE CREW THEN DECLARED AN EMERGENCY AND CONF IRMED THE GEAR DOWN AND LOCKED WITH THE TOWER. THE AIRCRAFT LANDED WITHOUT INCIDENT AND TAXI'ED TO THE GATE WITHOUT FURT HER INCIDENT. REMOVED AND REPLACED LT MLG ACTUATOR, OPS CK GOOD. PENDING ADL RETURN. 2 L 7 2 4T 4 T RT A24CE E26NE 2007020500032 20070205 00032 CE 2007 2 5 DXTA200701900 1 20070201 A 2120 UNKNOWN CESSNA 560 560XL 2076702 CE COCKPIT ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 685QS 5605650 LEAVING 11,000, STRONG BURNING ODOR FILLED COCKPIT AREA. APU - OFF, ANTI ICE - ON, TURNED PRESSURIZATION, ANTI-ICE, INTE RIOR MASTER OFF. ODOR PERSISTED. 15 MIN AFTER LANDING, WITH MAIN DOOR CLOSED, ENTIRE INSIDE HAD STRONG BURNING ODOR, COC KPIT WAS VERY STRONG. PERFORM WARM AIR DISTRUBUTION CHECK, CE560XLMM 21-22-00, NO DEFECTS. COMPLIED WITH COLD AIR DISTRI BUTION CHECK, CE560XLMM 21-21-00, NO DEFECTS. PERFORMED WING ENGINE ANTI-ICE CHECK CE560XL MM 30-11-00, NO DEFECTS. 2 L 7 2 4F RT A22CE 2007020500038 20070205 00038 EA 2007 2 5 SWIA200717742 1 20070104 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 969SW 7876 RT FS 625 CRACKED INTERCOSTAL STR 12, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED INTERCOSTAL AT FS 625-S12R PER CR J200 SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007020500048 20070205 00048 NM 2007 2 5 07FDEA00227 1 20070131 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 380 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 MAIN DECK FLOORBEAM UPPER FLANGE IS CORRODED, BS 380, RBL 48-55, WL208. BLENDED CORROSION AREA, ROTO PEENED, TREATED AN D PRIMED. REF EA NR 7-5310-106966, AND 7-5310-106966 REV A. 2 L 7 3 4F RT A3WE 2007020500050 20070205 00050 NM 2007 2 5 CALA0700040 1 20070126 A 5320 141A541012 INTERCOSTAL BOEING 737 737724 13844BY NM BS 312-328 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27733 28800 INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL AT STA 312-328, RBL 30. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SR M 51-42-21. 2 L 7 2 4F RT A16WE 2007020500052 20070205 00052 NM 2007 2 5 CALA0700042 1 20070126 A 5320 141A541012 INTERCOSTAL BOEING 737 737724 13844BY NM BS 312-328 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27733 28800 INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL AT STA 312-328, LBL 35. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SR M 51-42-21. 2 L 7 2 4F RT A16WE 2007020500060 20070205 00060 NM 2007 2 5 SWAA070487 1 20070131 A 5315 6546810 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 967, RBL 5. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007020500075 20070205 00075 NM 2007 2 5 SWAA070522 1 20070131 A 5312 6546568524 BULKHEAD BOEING 737 7373Q8 1384670 NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 5 O'CLOCK POSITION. REPAIRED WEB PER SR M. 2 L 7 2 4F RT A16WE 2007020500077 20070205 00077 NM 2007 2 5 SWAA070537 1 20070201 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM BS 360 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020500079 20070205 00079 NM 2007 2 5 SWAA070542 1 20070201 A 2730 65C2638416M CONTROL ROD BOEING 737 7373G7 1384595 NM ELEVATOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED C4 CHECK, FOUND RIGHT ELEVATOR TAB CONTROL ROD ATTACH POINT BROKEN. REMOVED AND REPLACED RIGHT ELEVATO R TAB PER MM. 2 L 7 2 4F RT A16WE 2007020500082 20070205 00082 WP 2007 2 5 AALA20070165 1 20070122 A 4990 5940405503 RESERVOIR DOUG DC9 DC983 3022083 WP APU OIL SYSTEM EMPTY A AALA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 591AA 53254 BUR - SMOKE IN CABIN AFTER LANDING AND THE APU AIR SWITCH WAS SELECTED ON. UPON REACHING THE GATE, THE APU WAS TURNED O FF AND SMOKE DISSIPATED RAPIDLY AFTER DOORS OPEN. REPLACED COALESCER BAGS FOR LEFT AND RIGHT AND PACKS. FOUND APU OIL RESERVOIR EMPTY AND LOWER FUSELAGE WET WITH OIL. CLEANED FUSELAGE AND SERVICED APU. SYSTEM GROUND CHECKED NORMAL OPERA TION. 2 L 7 2 4F RT A6WE 2007020500083 20070205 00083 WP 2007 2 5 AALA20070164 1 20070122 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 287AA 49299 YUL - EMERGENCY LIGHT BATTERY PACKS INOPERATIVE IN CABIN. REPLACED EMERGENCY LIGHT BATTERY PACKS IN CABIN. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007020500089 20070205 00089 CE 2007 2 5 DXTA200701911 1 20070204 A 2120 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL COCKPIT SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 960QS 7500160 SMOKE IN CABIN & COCKPIT LANDED IN APPROX 2 MIN UNABLE TO DETERMINE CAUSE. EMERGENCY DECLARED. STARTED APU & RAN EACH PACK ONE AT A TIME, STARTED RT ENG SHUTDOWN APU AIR RAN PACKS USING RT ENG. PERFORMED SAME TASK ON LT ENG. NO SMOKE OR O DORS NOTED. PERFORMED POWER RUNS TO CHECK HP & LP ON ENGS. NOTHING NOTED. ACCESSED BOTH COALESCER SOCKS. NORMAL. REINST ALLED RAN APU WITH BOTH PACKS ON & FULL ELECTRICAL LOAD ON APU. NOTHING NOTED. MOVED ACFT INTO HGR. POWERED UP EVERYTHIN G, NO DEFECTS NOTED. CHECKED ALL C/BS, ALL NORMAL. CHECK BEHIND BOTH CO-PILOTS & PILOTS CB PANEL. NOTHING NOTED. CHECKED INLET & OUTLET OF ACM'S, CHECKED ACM'S FOR ROTATION BOTH TURN FREELY. ALL WORK IAW CE-750 MM. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007020600018 20070206 00018 NM 2007 2 6 SWAA070524 1 20070131 A 5313 BAC1498 STRINGER BOEING 737 7373T5 1384608 NM BS 362 S28L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND STRINGER 28L CORRODED AT BS 362. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007020600019 20070206 00019 NM 2007 2 6 SWAA070532 1 20070201 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 AFT CABIN EMERGENCY FLASHLIGHT HAS LOW BATTERY. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2007020600020 20070206 00020 NE 2007 2 6 ASMF200701008 2 20070131 A 7200 1A9031001 BLADE BOEING 757 757200 1384950 NM PWA 2037 PW2040 NE RT ENGINE BENT W ASMF K NONE C F.O.D. IN INSP/MAINT 1 SW 23 703AM 27203 727137 DURING TRANSIT CHECK, A BLADE WAS DETECTED DAMAGED DUE TO A FOD IN RT ENGINE. 3 BENDS WERE DETECTED AT 2 INCHES FROM BL ADE LEADING EDGE TO MIDSPAN SHROUD, ONE OF 1.2500 INCH, OTHER OF 1.1250 INCH AND THE LAST ONE OF .8750 INCH. (2) BLADES SETS OF FAN STAGE WERE REPLACED IAW MM 72-31-02 AND TEST WAS PERFORMED IAW MM 71-00-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007020600021 20070206 00021 NM 2007 2 6 UIEA200700049 1 20070202 A 5414 SKIN BOEING 747 747341 13848AM NM GE CF6 CF650E2 30018 NE NR 4 NACELLE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 NR 4 PYLON PRECOOLER EXHAUST CUT-OUT CRACKED AT LOWER AFT SIDE. THE SKIN ASSEMBLY AND WINDOW STRAP WERE TRIMMED TO REMO VE CRACKS. NET FIT ALUMINUM FILLERS WERE INSTALLED AT ALL THE SUBJECT TRIMMED AREAS TO FACILITATE ALL REPAIR PARTS AND FASTENER INSTALLATION. REPAIRED AREAS WERE NDT INSPECTED. THE NR 3 STIFFENER WAS REINFORCED WITH NEW STEEL LOWER REPAI R ANGLE FROM NAC STATION 235 TO 259. THE RIB INSTALLATION AT NAC STATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW LOWER STEEL REPAIR ANGLE ON THE NR 3 STIFFENER. 2 L 7 4 4F 4 F RT A20WE E23EA 2007020600031 20070206 00031 NM 2007 2 6 HALA0700042 1 20070130 A 2497 BUSS TIE BOEING 767 767332 1382001 NM LT GENERATOR MALFUNCTIONED A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 594HA 323275 BTB - GROUND TURNBACK PRIOR TO TAKEOFF L GEN CONTROL L BUSS TIE ISOLATED AFTER RE-ESTABLISHING BUSS PER CHECKLIST FWD EZ SUPPLY FAN 1 AND T/R UNIT STATUS LIGHTS REMAIN ILLUMINATED. PERFORMED FIM 24-33-00 RESET AS NEEDED GROUND RUN CHECK GO OD. 2 L 7 2 4F RT A1NM 2007020600035 20070206 00035 2007 2 6 DXTA200701907 4 20070202 A 2210 TRIM SYSTEM CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE PITCH TRIM STUCK E DXTA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 07 626QS 5605126 AFTER TAKEOFF, COULD NOT ENGAGE AUTOPILOT. MANUAL PITCH TRIM STUCK, COULD NOT MOVE. ELECTRIC TRIM NORMAL. YAW DAMPER OPS NORMAL, PRESSED AUTOPILOT RELEASE BUTTON SEVERAL TIMES IN ORDER TO GET AUTOPILOT TO ENGAGE WITH NO SUCESS . AFTE R LANDING , MANUAL PITCH TRIM CHECKED THROUGH IT'S FULL RANGE & IT WAS FREE AND CLEAR , NO BINDING OR RESISTANCE. PREFO RMED OPERATIONAL CHECKS OF AUTOPILOT. CYCLED AUTOPILOT NUMEROUS TIMES THROUGH DIFFERENT CONFIGURATIONS. OPS CHECK MANU AL AND ELECTRIC PITCH TRIM THROUGH DIFFERENT CONFIGURATIONS. OPS CHECKED AUTOPILOT IN CONJUNCTION WITH PITCH TRIM. SYS TEM OPS CHECKED GOOD ON GROUND. ALL WORK DONE IAW CE-560XL M/M 22-11-03. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007020600036 20070206 00036 EU 2007 2 6 07FDEA00261 1 20070203 A 5730 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 OLD CORROSION REPAIR ON LT OUTER WING, BOTTOM SKIN, NEAR RIB 21 REPAIR WAS PERFORMED BY BLEND OUT THE CORROSION WITH CAL EO AB 6-57-00-0023 AND APPROVED BY RAS/BAE/0701/2003 ISS.A AND EA 6-5720-106353. 2 L 7 2 4F RT A35EU 2007020600038 20070206 00038 NM 2007 2 6 HNAA0700232 1 20070130 A 3320 1010817M PSU DHAV DHC8 DHC8102 2809003 NM BURNED A HNAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 942HA 46326 46326 163 FLIGHT ATTENDANT NOTICED SMOKE COMING FROM AROUND PSU AT 2AC. FOUND CIRCUIT CARD BURNED, REMOVED AND REPLACED PSU AT 2A C. 2 H 7 2 4T RT A13NM 2007020600039 20070206 00039 NM 2007 2 6 WRLA2007016 1 20070120 A 5313 RIB DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE MLG WW CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 48632 DURING 2C+12A+150M CHECK, MECHANIC FOUND 2 EA RIBS CRACK IN LEFT W/W OUTBOARD END AFT SIDE. REPLACED THE DAMAGED RIBS 2 EA PER MD 11F SRM VOL II 51-35-01 FIG REV 38. CONDITION CHECK NORMAL AND JOB COMPLETED. 2 L 7 3 4F 4 F RT A22WE E24NE 2007020600040 20070206 00040 EA 2007 2 6 COMA0760111 1 20070131 A 2750 1104SD100201 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS WORN A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 806CA 7359 FLIGHT 5375 - DURING YHZ APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. REPLACED THE LEFT WING NR 2 FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2007020600041 20070206 00041 NM 2007 2 6 SCNA07002 1 20070203 A 3350 FUSE BOEING 737 737800* NM EMERGENCY LIGHTS FAILED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 PHHZC 28375 MAINTENANCE FOUND EMERGENCY LIGHTS OUT AT ROW 25, 2 LOWER RIGHT SIDE, FWD LOWER LEFT SIDE. REPLACED POWER PACK FUSES FW D SIDE OF EMERGENCY EXITS RIGHT SIDE PER M/M 33-50-01, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2007020600042 20070206 00042 NM 2007 2 6 FDKA200701001 1 20070103 A 3397 WIRE DHAV DHC8 DHC8101 2809002 NM EMERGENCY LIGHTS DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 809LR 083 FDM 6175 JFK-PHL (0749 PHX LCL) FLOOR EMREGENCY LIGHT STRIP INOP. MX REPAIRED WIRING TO LIGHT STRIP. 2 H 7 2 4T RT A13NM 2007020600043 20070206 00043 SO 2007 2 6 FDKA200701002 1 20070104 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 FDM 6059 MCO-RIC (1512 PHX LCL) EMERGENCY EXIT SIGN INOP. MX SECURED WIRES TO LIGHT ASSEMBLY. 2 L 7 2 4T RT T00011AT 2007020600044 20070206 00044 SO 2007 2 6 FDKA200701005 1 20070107 A 3350 1317 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 FDM 6168 JFK-ORF (1008 PHX LCL) CREW REPORTED EMERGENCY EXIT ROW LIGHT INOP. MX RELAMPED. 2 L 7 2 4T RT T00011AT 2007020600047 20070206 00047 SO 2007 2 6 FDKA200701023 1 20070124 A 3350 110049 BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 1482 145214 FDM RON MCO (0059 PHX LCL) LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MX REPLACED THE BATTERY PACK AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2007020600051 20070206 00051 EA 2007 2 6 REXA200700015 1 20070202 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA FAILED A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8541D 8541 FLAPS FAIL AT ZERO DEGREES UPON APPROACH. LANDING UNEVENTFUL. COMPLIED WITH AD 2001-12-21 BY RESET AND MONITORING FOR 72 HOURS. 2 L 7 2 4F RT A21EA 2007020600052 20070206 00052 EA 2007 2 6 REXA200700016 1 20070202 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A REXA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 8672A 8672 FLAPS FAIL AT ZERO DEGRESS AFTER BLOCK OUT. REMOVED AND REPLACED LT BPSU. FLAPS OPERATIONALLY CHECK GOOD. 2 L 7 2 4F RT A21EA 2007020600053 20070206 00053 NM 2007 2 6 0700445655 1 20070203 A 3350 LIGHT BOEING 757 757251 1384970 NM CABIN FAILED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 555NW 33391 DURING LINE CHECK, FOUND EMERGENCY SLIDE EXTERIOR LIGHTS AT DOORS 2 LT AND RT AND DOORS 4 LT AND RT, ALSO EXTERIOR EMERG ENCY LIGHT ON AFT CARGO DOOR INOP. TROUBLESHOT PER WDM 33-51-13, REPLACED POWER SUPPLY AT 2 LT & RELAMPED; NO HELP. AL L INTERIOR EMERGENCY LIGHTS ARE OPERATION. RELAMPED EXTERIOR SLIDE LIGHT AT 2R, 2L, 4R, AND 4L PER AMM 33-51-06. OPS C HECK GOOD. RELAMPED AFT CARGO DOOR SLIDE LIGHT PER AMM 33-51-06, NO HELP. SLAVED LT SIDE POWER SUPPLY TO RIGHT SIDE AL SO NO HELP. CHECKED POWER SUPPLY FUSES, ALL CHECK GOOD. TROUBLESHOT AFT CARGO DOOR EMERGENCY LIGHT FOUND LIGHT ASSEMBL Y TO BE BAD. CLEANED SOCKET AT AFT CARGO DOOR. SYSTEM CHECKS GOOD. 2 L 7 2 4F RT A2NM 2007020600054 20070206 00054 NM 2007 2 6 0700455507 1 20070204 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 507US 23196 FIRST CLASS FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK (M9001) PER AMM 33-51-07. OPS CHECKS GOOD. 2 L 7 2 4F RT A2NM 2007020600056 20070206 00056 NM 2007 2 6 0700473122 1 20070201 A 3350 BATTERY PACK AIRBUS A319 A319114 3930350 NM EMERGENCY LIGHT NO TEST A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 322NB 1434 EPSU FAULT ON EXIT LIGHT SYSTEM TEST. CORRECTED BY REPLACING BOTH LEFT EPSU BATTERIES. CHECKS OK. 2 L 7 2 4F RT A28NM 2007020600059 20070206 00059 EU 2007 2 6 07FDEA00271 1 20070203 A 5313 A5397308020490 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 FOUND CORRODED STRINGER P46RH, C60-C60A REPAIR WAS PERFORMED IAW RAS/DATLS/0003135/2006 ISS.A, STRINGER SPLICE REPAIR WI TH DWR 17 R539 70094B), APPROVED ALSO BY EA 6-5317-106347. 2 L 7 2 4F RT A35EU 2007020600062 20070206 00062 EU 2007 2 6 07FDEA00274 1 20070203 A 5313 A5397330620000 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 STRINGER P50 LT BETWEEN C72 AND C73 CORRODED AND CONNECTION SECTION AT C72, P50 LT CORRODED STRINGER REPAIR WAS PERFORM ED IAW SRM 53-10-14 FIG 201 AND REPLACEMENT OF CORRODED CONNECTING SECTION WAS PERFORMED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007020600064 20070206 00064 EU 2007 2 6 07FDEA00276 1 20070203 A 5313 A5397420357000 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 FOUND STRINGER P50 LT AT C70 CORRODED STRINGER REPAIR WAS PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007020600065 20070206 00065 EU 2007 2 6 07FDEA00277 1 20070203 A 5340 A5377364320400 ATTACH FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 FOUND CORRODED CLIP AT C35 BETWEEN P43-44 LT AND STRINGER P 44 BETWEEN C35-C36, LT CORROSION REPAIR WAS PERFORMED BY REP LACEMENT OF CLIP IAW SRM 51-72-10 AND STRINGER REPAIR IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007020600068 20070206 00068 WP 2007 2 6 07FDEA00249 1 20070202 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 368FE 46606 ACCOMPLISH REPAIR AFT OF CENTER CARGO DENT REPAIR CARD T8-5330-106226,W/O35111. C/W EA 8-5330-102770 (FUSELAGE-GROSS WE IGHT DOUBLER DENT AT FUS STA 1850, L39R-40R. REPAIR ON CARD T8-5330-106226-W/035111. MAJOR REPAIR. MECH 1985 QC227 C/ W EA 8-5330-106226 FUSELAGE, PLATE/SKIN AFT OF CENTER CARGO DOOR, RT, FS 1850, DENT, INTERIM REPAIR. PERMANENT REPAIR A CCOMPLISHED ON EA 8-5330-102770 ON CARD T 8-5330-106226, W/O35111. 2 L 7 3 4F RT A22WE 2007020600069 20070206 00069 NM 2007 2 6 07FDEA00250 1 20070202 A 3260 INDICATION SYS BOEING 727 727233 138408A NM MLG MALFUNCTIONED A FDEA O OTHER N FALSE WARNING LD LANDING 1 SO 25 285FE 22622 AFTER LANDING LEVER PLACED DOWN, FRONT GEAR INDICATION PANEL HAD ALL 8 LIGHTS ON. PER CHECK LIST, RECYCLED LANDING GEAR , INDICATIONS NORMAL. PER CREW ACTIONS AND RESULTING NORMAL INDICATIONS, SUSPECT INDICATION ANOMALY. NO FAULTS NOTED. NO PRIOR HISTORY. VISUALLY INSPECTED LANDING GEAR, NO FAULTS NOTED. OPS CHECKED PER MM 32-09-122-5 STEP A. OPS CHEC KS NORMAL. OK TO CONTINUE. 2 L 7 3 4F RT A3WE 2007020600071 20070206 00071 EU 2007 2 6 200702051 1 20070131 A 2780 SLAT SYSTEM EMB ERJ170 ERJ170100SE 3260406 EU FAILED A UHLA O OTHER O OTHER AP APPROACH 1 GL 17 657RW 17000115 FLIGHT 7586 ORD TO YUL SLAT FAIL ON APPROACH. DECLARED EMERGENCY AND LANDED SAFELY. MAINTENANCE RESET SF-ACE PER FIM; RAN UP SEVERAL TIMES NO DEFECTS AT THIS TIME AND DATE. 2 L 7 2 4F RT A56NM 2007020600072 20070206 00072 EU 2007 2 6 UHLA200702052 1 20070131 A 2780 SLAT SYSTEM EMB ERJ170 ERJ170100SE 3260406 EU MALFUNCTIONED A UHLA O OTHER J WARNING INDICATION AP APPROACH 1 GL 17 642RW 17000063 FLIGHT 7536 MSP TO IAD - ON APPROACH FLAPS AT 1 DEGREE, CREW RECEIVED SLAT FAIL AND AN EMERGENCY WAS DECLARED. AC LANDE D WITHOUT INCIDENT. MAINTENANCE CLEARED INHIBITS ON SF-ACE'S, RELEASED BRAKES ON SLAT PDU'S, RAN SLATS SEVERAL TIMES AN D COULD NOT DUPLICATE FAULT ON GROUND. 2 L 7 2 4F RT A56NM 2007020600074 20070206 00074 NM 2007 2 6 ASAA0791429 1 20070131 A 5330 143A32541 SKIN BOEING 737 737990 NM BS 450 GROUND DAMAGE A ASAA D RETURN TO BLOCK W INADEQUATE Q C TX TAXI/GRND HDL 1 NM 02 323AS 30021 RAMP HIT AIRCRAFT WITH BELT LOADER AT FWD CARGO DOOR AFT EDGE DAMAGED AT BS 450 AND WL 155. REPAIRED IAW SRM 53-00-01 R EPAIR 25. 2 L 7 4 4F RT A16WE 2007020600078 20070206 00078 EA 2007 2 6 COMA0760115 1 20070131 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 806CA 10305 7359 FLIGHT 5375 - DURING YHZ APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. REPLACED THE RIGHT INBOARD FLAP - OUTBOARD ACTU ATOR. 2 L 7 2 4F RT A21EA 2007020600079 20070206 00079 2007 2 6 F3LA200700012 4 20070202 A 2565 D5348015900600 PLATE AIRBUS A319 A319111 3930336 NM GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 5911 1943 DURING C-3 CHECK, INSPECTION REPORTED L2 AFT GIRT BAR PLATE CORRODED. REPLACED L2 DOOR GIRT BAR PLATE PER MM 52-13-31. REPLACED L2 DOOR GIRT BAR FITTING BLANKING PLATE PER AMM 52-13-31-400-007. 2 L 7 2 4F RT A28NM 2007020600083 20070206 00083 NM 2007 2 6 UPS07449114 1 20070111 A 5340 65B0717417 STRINGER CLIP BOEING 747 747123 1384873 NM BS 1860 S43R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C AFT CARGO COMPT - STRINGER CLIP FOUND CORRODED AT STA1860 S43R INSIDE OF TORQUE BOX. CORROSION BLEND OUT 0.040 X .5 X .5 INCH EXCEED SRM LIMIT. STRINGER CLIP REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51- 30-02. 2 L 7 4 4F A20WE 2007020600086 20070206 00086 WP 2007 2 6 UPS07849108 1 20070107 A 5313 SAA3646937501 LONGERON DOUG DC8 DC871F 302199D WP FS1400-1440 L35R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 LONGERON 35R CRACKED ALONG RADIUS AT FS 1400-1440. REMOVED, FABRICATED AND INSTALLED LONGERON IAW SR M 51-1-20D, 51-1-21 & DWG 3646937. 2 L 7 4 4F RT 4A25 2007020600087 20070206 00087 WP 2007 2 6 UPS07849109 1 20070104 A 5730 7529372 SKIN DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 LEFT UPPER WING SKIN POSSIBLE CRACKED AT XCW69 AFT SPAR VERY I/B SIDE. CUT OUT DAMAGE, FABRICATED 2 EA DOUBLERS, 1 EA FILLER AND 1 EA ANGLE AND INSTALLED IAW SRM 57-02-01-0 FIG 020 AND 51-1-21. 2 L 7 4 4F RT 4A25 2007020600088 20070206 00088 WP 2007 2 6 UPS07849110 1 20070121 A 5730 57573183 SKIN DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 LT STUB WING L/E ABOVE NR 2 HAS A CRACK ON UPPER O/B SIDE. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SAA EA 008-5710-01-A0615. 2 L 7 4 4F RT 4A25 2007020600089 20070206 00089 WP 2007 2 6 UPS07849112 1 20070122 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FS 80 RBL 57 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C2 CORROSION ON FLOORBEAM LOWER T-CAP EXFOLIATED STA -80 RBL 54. REMOVED OUT OF LIMITS CORROSION AT STA -80 RBL 57 IAW SRM 51-2-1. FABRICATED AND INSTALLED REPAIR PARTS AT STA -80 RBL 57 IAW SRM 51-2-1 FIG 1, AND TR 51-130 . 2 L 7 4 4F RT 4A25 2007020600090 20070206 00090 WP 2007 2 6 UPS07849115 1 20070202 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:N/A EMERGENCY LIGHT WILL NOT TURN ON PREFLIGHT CHECK. EMERGENCY LIGHT BATTERY PACK REPLACED IAW AMM 33- 50-01-2 AND SYSTEM CHECK SERVICEABLE. 2 L 7 4 4F RT 4A25 2007020600092 20070206 00092 EA 2007 2 6 REXA200700026 1 20070203 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A REXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 8733G 7733 FLAPS FAIL. RESET PER AD 2006-12-21. 2 L 7 2 4F RT A21EA 2007020600093 20070206 00093 NE 2007 2 6 NACA20070003 2 20070131 A 8530 VALVE PWA DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 8 CYLINDER FAILED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 43872 2501 2501 561212 533294 P32304 NR 1 ENGINE BACKFIRED AND WOULD NOT HOLD A LEAN. ANALYZER PATTERN FOR NR 8 CYLINDER FRONT AND REAR ABNORMAL, SHOWS LOW COMPRESSION. ENGINE SHUT DOWN. NR 8 CYLINDER FRONT AND REAR HAD LOW COMPRESSION DUE TO VALVE FAILURE. FURTHER INSPECT ION RESULTED IN THE DISCOVERY OF A FRONT CAM FAILURE INDUCED BY THE VALVE FAILURE. ENGINE REPLACED. 2 L 7 4 4R 4 R A781 5E8 2007020600094 20070206 00094 NM 2007 2 6 AWXA200700130 1 20070129 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 660AW 10649 172 1234 PHX - EEL - MID CABIN EMERG LIGHTS INOP. MX REMOVED AND REPLACED EMERG PWR SUPPLY AND BATTERY. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007020600095 20070206 00095 NM 2007 2 6 AWXA200700136 1 20070129 A 2750 FLAP SYSTEM BOEING 737 7373G7 1384595 NM UNKNOWN A AWXA O OTHER J WARNING INDICATION AP APPROACH 1 WP 28 157AW 23779 MCI - TRAILING EDGE FLAPS INDICATED SPLIT CONDITION AT FLAPS 5. NO ADVERSE ROLL NOTED. LANDED FLAPS 5. A/C CURRENTLY AOS. 2 L 7 2 4F RT A16WE 2007020600101 20070206 00101 NM 2007 2 6 DLM88070067 1 20070201 A 4920 APU DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE ODOR A DALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 965DL 26380 49984 P80210 AFTER TAKEOFF EXPERIENCED SMOKE IN CABIN AND COCKPIT OIL SMELL, APU WAS OPERATING. REPLACED APU PER TRANS 9T103. PERFO RMED PNEUMATIC DIST CABIN SMOKE ODOR TROUBLESHOOTING PER OPN 5088. PERFORMED DUCT BU OUT PER OPN 5089. 2 L 7 2 4F 4 F RT A6WE E9NE 2007020600102 20070206 00102 NM 2007 2 6 DL76G070069 1 20070201 A 2612 WARNING HORN BOEING 767 767332 1382001 NM FIRE WARNING MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 174DZ 29693 FIRE WARNING HORN SOUNDED/AURALLY ALERTED IMMEDIATELY ON LIFT OFF. NO LIGHTS EICAS MESSAGES OR ANY INDICATIONS AT ALL W ERE APPARENT. THE HORN SOUNDED UNTIL LANDED AND TAXIED BACK. PULLED J34 AND B18 WARN ELEX CBS. HORN SILENCED WHEN B18 PULLED LANDING WEIGHT 319.9 NO OVERWEIGHT LANDING. REMOVED AND REPLACED PWR SUPPLY MODULE B AND ENG/CARGO FIRE TEST PA NEL. ALL OPS CHK NML. TEST OPS NML FIRE WARNING SHUTDOWN. 2 L 7 2 4F RT A1NM 2007020600104 20070206 00104 NM 2007 2 6 QXEA200700123 1 20070201 A 3097 697071272 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA PROP DE ICE SYS UNKNOWN A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 413QX 4060 FLIGHT NR 2416: PROP DEICE CAUTION LIGHT ILLUMINATED WHEN NR 2 PROP DEICE IS ACTIVATED. PERFORMED ABNORMAL CHECKLIST. RE SET PROP DEICE CONTROL CAUTION LIGHT REILLUMINATED. FLIGHT DIVERTED. MAINTENANCE REMOVED NR 2 SPINNER IAW AMM TASK 61-10 -11-000-801. REPLACED NR 4 BLADE HARNESS ON NR 2 PROP IAW AMM 61-10-06-000-805 AND 61-10-05-400-805. REINSTALLED NR 2 SP INNER IAW AMM TASK 61-10-11-400-801. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2007020600105 20070206 00105 EA 2007 2 6 REXA200700027 1 20070203 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A REXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 8974C 7974 FLAP FAIL, SECOND OCCURRENCE WITHIN 72 HOURS 2 L 7 2 4F RT A21EA 2007020600113 20070206 00113 NM 2007 2 6 07FDEA00247 1 20070202 A 5753 652163586 SKIN BOEING 727 727233 138408A NM ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 REPAIR FOUND ON THE RT OB AFT FLAP LOWER SURFACE SKIN 17" FROM IB END REQUIRED EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR FOUND TO BE OUT OF LIMITS. REPLACED AFT FLAP. NEW AFT FLAP INSTALLED ON SNRM NR N00418, REF MM 27-51-072-4. FINAL ADJUSTMENT ACP ON WC NR 76C017-00. 2 L 7 3 4F RT A3WE 2007020600115 20070206 00115 SO 2007 2 6 SIMA200703601 1 20070201 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 619AE 145101 EMERGENCY LIGHTS NOT ARMED AND ELECTRICAL ABNORMAL MESSAGE, AIRCRAFT RETURNED TO MQT. REMOVED AND REPLACED NUMBER 2 BA TTERY SWITCH IAW EMB AMM 24-31-00. OPERATIONAL CHECK GOOD - PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS NOTED - RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007020600117 20070206 00117 2007 2 6 SIMA200703602 2 20070203 A 7200 ENGINE CNDAIR CL600 CL6002C10 1390015 EA NR 2 VIBRATION A SIMA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 21 514AE 10119 ENGINE 2 VIBRATION INDICATION WENT TO 2.2 WHILE IN CRUISE, REDUCED THROTTLES AND VIBRATION LOWERED AND THEN RETURNED TO 2.2.INDICATION, DIVERTED TO CMH. COMPLIED WITH ENGINEERING TECHNICAL NOTICE CR-72-002R1. PERFORMED FUNCTIONAL CHECK FL IGHT. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007020600118 20070206 00118 NM 2007 2 6 AWXA200700141 1 20070203 A 5315 D5347209001000 FLOORBEAM AIRBUS A319 A319132 3930340 NM ZONE 200 - FUSEL CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 831AW 1576 SAL - CORROSION ON MAIN CABIN FLOORBEAM, +Y1292, FR65+19". REPLACED MAIN CABIN FLOORBEAM, +Y1292, FR 64 - FR 66 IAW A31 9 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007020600120 20070206 00120 NM 2007 2 6 AWXA200700143 1 20070124 A 5320 69374024 ANGLE BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - ANGLE CRACKED, BS 312, S17R. REPLACED ANGLE, BS 312, S17R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600121 20070206 00121 SO 2007 2 6 SWIA200717766 1 20070127 A 5400 NACELLE EMB 120 EMB120ER 3260203 SO LEFT CONTAMINATED A SWIA O OTHER C B F.O.D. SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 299SW 120329 UPON AIRCRAFT POWER DOWN CREW NOTICED SMOKE COMING FROM THE LEFT ENGINE NACELLE. INSPECTED ENGINE COMPARTMENT AND NOTED EXCESS GLYCOL. NO OTHER DISCREPANCIES NOTED. 2 L 7 2 4T RT A31SO 2007020600122 20070206 00122 SO 2007 2 6 SWIA200717767 1 20070129 A 5753 BEARING EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 212SW 120276 OUTBOARD FLAPS WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO FIELD. REPLACED 4 ROLLER BEARINGS IAW MM 27-50-12. OPERAT IONAL CHECKS GOOD IAW MM 27-50-00. 2 L 7 2 4T RT A31SO 2007020600123 20070206 00123 EA 2007 2 6 SWIA200717768 1 20070130 A 2120 UNKNOWN CNDAIR CL600 CL6002D24 1390016 EA CABIN ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 806SK 15070 UPON LANDING THERE WAS A FUEL SMELL IN CABIN. INSPECTED AIRCRAFT AND FOUND NO SIGNS OF FUEL LEAKING AND NO FUEL SMELL. 2 L 7 2 4F RT A21EA 2007020600124 20070206 00124 SO 2007 2 6 SWIA200717769 1 20070130 A 3350 BULB EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 295SW 120322 EMERGENCY LIGHT OVER MCD IS INOP. REPLACED BULB OVER MCD. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007020600125 20070206 00125 EA 2007 2 6 SWIA200717770 1 20070126 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 406SW 7030 RIGHT EMERGENCY EXIT LIGHT FORWARD INOP. RELAMPED RIGHT FORWARD EXTERNAL EMERGENCY LIGHT PER MM 33-52-01. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007020600128 20070206 00128 NM 2007 2 6 AWXA200700144 1 20070130 A 5340 69353521 STRINGER CLIP BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR - CRACKED STRINGER CLIP, BS 706, S10L. REPLACED STRINGER CLIP, BS 706, S10L IAW B737-300 SRM 51-40-0 2. 2 L 7 2 4F RT A16WE 2007020600130 20070206 00130 NM 2007 2 6 AWXA200700146 1 20070116 A 5320 65479576 INTERCOSTAL BOEING 737 7373S3 1384711 NM BS 790 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 MCN - CORROSION ON AFT CARGO COMPARTMENT DOOR CUT OUT TORQUE BOX INTERCOSTAL WEB, BS 790, S25R, WL 153. REPLACED AFT CA RGO COMPARTMENT DOOR CUT OUT TORQUE BOX INTERCOSTAL WEB, BS 790, S25R, WL 153 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600131 20070206 00131 NM 2007 2 6 AWXA200700147 1 20070118 A 5320 65479573 THRESHOLD BOEING 737 7373S3 1384711 NM BS 840 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 MCN - CORROSION ON AFT CARGO COMPARTMENT DOOR CUT OUT THRESHOLD WEB, BS 840 S26R. REPLACED AFT CARGO COMPARTMENT DOOR C UT OUT THRESHOLD WEB, BS 840 S26R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600133 20070206 00133 NM 2007 2 6 AWXA200700149 1 20070120 A 5320 654795711 STRAP BOEING 737 7373S3 1384711 NM BS 857-874 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 MCN - AFT CARGO COMPARTMENT DOOR CUT OUT THRESHOLD SUPPORT STRAP CRACKED, BS 857 - BS 874, S25R. REPLACED AFT CARGO COM PARTMENT DOOR CUT OUT THRESHOLD SUPPORT STRAP, BS 857 - BS 874, S25R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600135 20070206 00135 NM 2007 2 6 AWXA200700151 1 20070116 A 5310 655287846 DOOR FRAME BOEING 737 7373S3 1384711 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 MCN - FOUND CORROSION ON L2 DOOR CUT OUT INNER CHORD, BS 967 - BS 986.5, LBL 62, WL 208. REPLACED L2 DOOR CUT OUT INNER CHORD, BS 967 - BS 986.5, LBL 62, WL 208 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600136 20070206 00136 NM 2007 2 6 AWXA200700152 1 20070115 A 5310 652072354 DOOR FRAME BOEING 737 7373S3 1384711 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 MCN - FOUND FORWARD CARGO COMPARTMENT DOOR CUT OUT AFT FRAME CRACKED, BS 492.50, S24R. REPAIRED FORWARD CARGO COMPARTME NT DOOR CUT OUT AFT FRAME, BS 492.50, S24R IAW AWA ER 03-5331-07032-ES2. 2 L 7 2 4F RT A16WE 2007020600138 20070206 00138 NM 2007 2 6 AWXA200700154 1 20070130 A 5340 65353521 STRINGER CLIP BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED STRINGER CLIP, BS 663, S10L. REPLACED STRINGER CLIP, BS 663, S10L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600144 20070206 00144 NM 2007 2 6 AWXA200700160 1 20070121 A 5340 69353521 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED STRINGER CLIP, BS 727E, S14R. REPLACED STRINGER CLIP, BS 727E, S14R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600145 20070206 00145 NM 2007 2 6 AWXA200700161 1 20070121 A 5340 69353521 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED STRINGER CLIP, BS 747, S8R. REPLACED STRINGER CLIP, BS 747, S8R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600146 20070206 00146 NM 2007 2 6 AWXA200700162 1 20070121 A 5340 693535214 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED STRINGER CLIP, BS 727E, S7L. REPLACED STRINGER CLIP, BS 727E, S7L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600147 20070206 00147 NM 2007 2 6 AWXA200700163 1 20070121 A 5340 693535214 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED STRINGER CLIP, BS 767, S16R. REPLACED STRINGER CLIP, BS 7BS 767, S16R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600148 20070206 00148 NM 2007 2 6 AWXA200700164 1 20070122 A 5340 693535214 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED STRINGER CLIP, BS 616, S2L. REPLACED STRINGER CLIP, BS 616, S2L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600149 20070206 00149 NM 2007 2 6 AWXA200700165 1 20070122 A 5340 693535214 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED STRINGER CLIP, BS 616, S2R. REPLACED STRINGER CLIP, BS 616, S2R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600151 20070206 00151 NM 2007 2 6 AWXA200700167 1 20070122 A 5340 69353521 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED STRINGER CLIP, BS 380, S8L. REPLACED STRINGER CLIP, BS 380, S8L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600155 20070206 00155 NM 2007 2 6 AWXA200700133 1 20070113 A 5311 6546921116 FRAME BOEING 737 7373S3 1384711 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 MCN - FORWARD CARGO COMPARTMENT DOOR CUT OUT FORWARD FRAME CRACKED, BS 440, S25R. REPLACED FORWARD CARGO COMPARTMENT DO OR CUT OUT FORWARD FRAME CRACKED, BS 440, S25R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600156 20070206 00156 NM 2007 2 6 AWXA200700134 1 20070122 A 5320 654587545 STRUCTURE BOEING 737 73733A 1384673 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CORROSION ON MAIN CABIN INNER CHORD, BS 277 - BS 344, RBL 65, WL 208. REPLACED MAIN CABIN INNER CHORD, BS 2 77 - BS 344, RBL 65, WL 208 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600159 20070206 00159 NM 2007 2 6 AWXA200700171 1 20070120 A 5754 65C267995 SKIN BOEING 737 73733A 1384673 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND LEFT WING NR 1 SLAT LOWER SURFACE SKIN HAS CRACKS, SS 322.50 - SS 325.65. REPAIRED LEFT WING NR 1 SLAT LOWE R SURFACE SKIN, SS 322.50 - SS 325.65 IAW B737-300 SRM 57-43-01 FIGURE 201. 2 L 7 2 4F RT A16WE 2007020600160 20070206 00160 NM 2007 2 6 AWXA200700172 1 20070125 A 5321 D53610605000100 FLOOR PANEL AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 830AW 1565 SAL - FOUND CORROSION ON MAIN CABIN FLOORBOARD 222FF, FS 16 - FS 20, -Y1292 TO -Y1732. REPLACED MAIN CABIN FLOORBOARD 2 22FF, FS 16 - FS 20, -Y1292 TO -Y1732 IAW AWA TASK CARD C1D25306. 2 L 7 2 4F RT A28NM 2007020600165 20070206 00165 EA 2007 2 6 REXA200700036 1 20070204 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8665A 7665 FLAPS FAIL ON APPROACH. RESET FLAPS AND PLACED ON 72 HOUR MONITORING PER AD 2006-12-21. 2 L 7 2 4F RT A21EA 2007020600166 20070206 00166 EA 2007 2 6 REXA200700037 1 20070204 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8974C 7974 FLAPS FAIL ON APPROACH. 2 L 7 2 4F RT A21EA 2007020600174 20070206 00174 NM 2007 2 6 DL76G070075 1 20070203 A 5330 146T31321 TEAR STRAP BOEING 767 767332 1382001 NM BS 1417 S2R DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1612T 30575 WHILE ACCOMPLISHING A LAP JOINT REPAIR PER SRM AT STA 1417, S-2R, THE TEAR STRAP WAS INADVERTENTLY CUT. THE DAMAGED PAR T OF THE TEAR STRAP WAS CUT OUT AND A TRIPLER WAS INSTALLED AS PART OF THE LAP JOINT REPAIR. 2 L 7 2 4F RT A1NM 2007020200049 20070202 00049 NM 2007 2 2 TSAA0749011 1 20070127 A 4900 1319B APU BOEING 737 73773A 1384606 NM SHUTDOWN A TSAA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 13 738AL 28499 AIRCRAFT GROUND EVENT IN KOA. THE APU AUTO SHUTDOWN FOR LOW OIL PRESSURE INDICATION. MAINTENANCE VISUALLY CHECKED OIL LEVEL AND VERIFIED AT FULL. THE APU WAS RESTARTED AND RAN NORMAL WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVI CE. 2 L 7 2 4F RT A16WE 2007020200053 20070202 00053 EA 2007 2 2 COMA0760085 1 20070128 A 5210 CAM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 739CA 7273 FLIGHT 9750 - EN ROUTE PIT-CVG RECEIVED A CABIN DOOR WARNING MESSAGE, FLIGHT RETURNED TO PIT. CLEANED AND LUBRICATED TH E UPPER LATCH CAMS. 2 L 7 2 4F RT A21EA 2007020200069 20070202 00069 NM 2007 2 2 SWAA070462 1 20070129 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 431WN 29845 EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007020200083 20070202 00083 NM 2007 2 2 SWAA070497 1 20070131 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED C1 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007020200084 20070202 00084 NM 2007 2 2 SWAA070502 1 20070131 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED SPV CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007020200092 20070202 00092 NM 2007 2 2 AT0700011 1 20070115 A 2820 7971500597 LINE BOEING 717 717200 1383700 NM LEFT TANK BROKEN A ZZDA B EMER. DESCENT O OTHER CL CLIMB 1 SO 15 979AT 55038 AT ABOUT 2100 FT THE ENGINE -LT FUEL PRESS- LIGHT ILLUMINATED. OBSERVED LT TANK FUEL DECREASING AND RT TANK FUEL INCREA SING. DECLARED EMERGENCY AND LANDED AT RDU. REPLACED FUEL LINE IN LEFT MAIN TANK M/M 28-22-02. FWD BOOST PUMP VOLUTE PLUMBING. OPS CHECKS GOOD. 2 L 7 2 4F TR A6WE 2007020200100 20070202 00100 SO 2007 2 2 SIMA200703203 1 20070128 A 5315 14000235003 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 702AE 15957 4800 145164 FOUND OMEGA BEAM CORRODED AT FRAME 32. PERFORMED CUTOUT OF DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 53-00-1 0. RESTORED PROTECTIVE FINISH AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007020200104 20070202 00104 NM 2007 2 2 07FDEA00087 1 20070112 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 STRINGER CLIP CRACKED AT RADIUS CUTOUT BS660 STRINGER R3. REMOVED AND REPLACED STR CLIP WITH NEW AT BS 660 STR 3R REF 5 1-30-2 PG 1. 2 L 7 3 4F RT A3WE 2007020200131 20070202 00131 NM 2007 2 2 SWAA070486 1 20070131 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 460 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 460, STR 13R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007020200132 20070202 00132 NM 2007 2 2 SWAA070511 1 20070131 A 5311 6546532 FRAME BOEING 737 7375H4 138449D NM BS 480 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020200133 20070202 00133 NM 2007 2 2 SWAA070503 1 20070131 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 63, WL 202. REPAIRED FRAME SECTION PER ER. 2 L 7 2 4F RT A16WE 2007020200134 20070202 00134 NM 2007 2 2 SWAA070506 1 20070131 A 5311 6546549 FRAME BOEING 737 7375H4 138449D NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020200135 20070202 00135 NM 2007 2 2 SWAA070510 1 20070131 A 5311 6546551 FRAME BOEING 737 7375H4 138449D NM BS 827 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020200136 20070202 00136 NM 2007 2 2 SWAA070507 1 20070131 A 5311 6546554 FRAME BOEING 737 7375H4 138449D NM BS 867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020200138 20070202 00138 NM 2007 2 2 SWAA070508 1 20070131 A 5311 6546558 FRAME BOEING 737 7375H4 138449D NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020200144 20070202 00144 EU 2007 2 2 07FDEA00229 1 20070131 A 7830 UNKNOWN AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680 30025 NE UNKNOWN A FDEA C ABORTED TAKEOFF J WARNING INDICATION CL CLIMB 1 SO 25 665FE 769 705242 NR 2 ENG REVERSER PRESSURIZED LIGHT ON ECAM ILLUMINATED AT GEAR RETRACTION ON TAKEOFF COMPLIED WITH E-CAM AND QRH ATB. R&R DIR. PILOT VALVE, HARNESS FOR T/R, PRESS REG. S/O VALVE,DIODE UNIT 20KM,MOD BLOCK 204VT, RELAYS 6KM&16KM, AWAITING FINAL OPS CHECK & ENG RUN-UP MEL ON NR 2 T/R DUE TO TOOLING NOT AVAIL FOR DPV CHECK 2 L 7 2 4F 4 F RT A35EU E13NE 2007020200150 20070202 00150 EA 2007 2 2 COMA0760084 1 20070128 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 721CA 7259 FLIGHT 5529 - DURING CMH APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 8 DEGREE FLAP SETTING, CREW DECLARED AN EMERGE NCY AND FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTI ON, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007020200154 20070202 00154 EA 2007 2 2 COMA0760093 1 20070129 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 495CA 7774 FLIGHT 5009 - RECEIVED FLAP FAIL MESSAGE AT 45 DEGREES DURING FLAP RETRACTION ON GROUND. COMPLIED WITH AD 2006-12-21 FL AP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FU RTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007020200174 20070202 00174 EA 2007 2 2 TRAX200700125 1 20070126 A 2560 MEGAPHONE CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 FA MEGAPHONE INOP. 2 L 7 2 4F RT A21EA 2007020200176 20070202 00176 NM 2007 2 2 USAA070074 1 20070130 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 511AU 23594 FOUND FRAME CRACKED STA 440, WL 180. TRIMMED OUT DAMAGED, FAB'D DOUBLERS AND SHIMS AND INSTALLED PER EA 98425, DEFECT S IZE: 1/32". 2 L 7 2 4F RT A16WE 2007020200198 20070202 00198 SO 2007 2 2 RAIA00701038 1 20070127 A 3350 BULB EMB 145 EMB145 3260210 SO EMERGENCY LIGHT FAILED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 804HK 145082 PRE FLT NR 3550 - PIT - EMERGENCY LIGHT OUT AT MAIN DOOR. MAINTENANCE REMOVED AND REPLACED THE BULB. 2 L 7 2 4F RT T00011AT 2007020200200 20070202 00200 SO 2007 2 2 RAIA00701036 1 20070126 A 2910 CONNECTOR EMB 145 EMB145LR 3260212 SO HYD SYSTEM LOOSE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 819HK 145062 FLT NR 5504 - STL - HYDRAULIC SYSTEM NR 1 "LOW QTY" MESSAGE ON THE EICAS WITH GAUGE SHOWING AT BOTTOM OF THE AMBER BAND. MAINTENANCE INSPECTED AND FOUND A LOOSE FITTING IN NR 1 HYDRAULIC BAY. FITTING WAS SECURED AND THE SYSTEM INSPECTED F OR FURTHER DEFECTS WITH NO FINDINGS. 2 L 7 2 4T RT T00011AT 2007020500013 20070205 00013 CE 2007 2 5 AMW1061010024 1 20070110 A 5711 1181000131 SPAR CAP BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA LT WING CORRODED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 127ZV 23346 UE127 DURING STRUCTURAL INSPECTION, MAINTENANCE FOUND SOME BIO-CORROSION ON LT WING MAIN SPAR LOWER CAP BETWEEN WS 114 AND WS 124. REPAIRED IAW MFG FR-CO-01443 REV. 4 SPAR CAP PLUG INSTALLATION ACCOMPLISHED IAW MFG FR-CO-01444 REV 2 IN CONJUNCT ION WITH MFG FR-CO-01443 REV. 4. 2 L 7 2 4T 3 T RT A24CE E2NE 2007020500015 20070205 00015 CE 2007 2 5 AMWA81896 1 20070107 A 3260 BULB BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE ANNUNCIATOR INOPERATIVE A AMWA O OTHER P NO WARNING INDICATION AP APPROACH 1 CE 07 126YV UE126 WHEN GEAR WS EXTENDED FOR LANDING, THERE WAS NO DOWN AND LOCKED INDICATION ON ANNUNCIATOR. CREW DECLAIRED EMERGENCY, AND FOLLOWED PROCEDURES. A/C LANDED WITH NO FURTHER INCIDENT. REPLACED ANNUNCIATOR BULBS. PENDING ADL RETURN. 2 L 7 2 4T 4 T RT A24CE E26NE 2007020500018 20070205 00018 CE 2007 2 5 AMWA82340BC 1 20070130 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER DISCHARGED A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 166YV 14367 414 UE166 BATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED BATTERY TO CLEAR DISCREPANCY. THIS BATTERY CHAR GE LIGHT ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS. 2 L 7 2 4T 4 T RT A24CE E26NE 2007020500019 20070205 00019 CE 2007 2 5 AMW1070126025 1 20070129 A 2720 AN17517A BOLT BEECH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RUDDER CONTROL BENT A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 135YV 22990 1062 UE135 WHILE PERFORMING THE INSPECTION REQUIREMENTS OF THE RUDDER SYSTEM FOR THE NR 6 DETAIL INSPECTION, IT WAS DISCOVERED THAT THE RUDDER HAD EXCESSIVE UP AND DOWN MOVEMENT. THE FIRST ACTION IS TO CHECK THE TORQUE OF THE RUDDER CONTROL HORN PIVOT BOLT (ITEM NR 312, MFG IPC 27-20-00-11, PAGE 0E). WHILE CHECKING FOR PROPER TORQUE, IT WAS DISCOVERED THAT THE BOLT WAS BENT. THE RUDDER WAS REMOVED AND INSPECTED AND REINSTALLED. THE BOLT AND ASSOCIATED HARDWARE WAS REPLACED AND PROPERLY TORQUED. AIRCRAFT WAS TEST FLOWN WITH NO FAULTS FOUND. IT IS UNKNOWN HOW THIS BOLT WAS BENT. THIS AREA IS INSPECTED AT EACH NR 6 DETAIL INSPECTION WHICH WOULD BE 1200 OR FEWER FLIGHT HOURS. 2 L 7 2 4T 4 T RT A24CE E26NE 2007020500021 20070205 00021 NM 2007 2 5 KCSA071059 1 20070201 A 5313 STRINGER BOEING 747 747209F 1384800 NM PWA JT9 JT9D7R4G2 52054 NE BS 1480 S8L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 FUSELAGE STRINGER CRACKED AT B.S.1480, STR-8L. 2 L 7 4 4F 4 F RT A20WE E3NE 2007020500022 20070205 00022 SO 2007 2 5 JBGA200700002 1 20070130 A 5610 1159SCB31023 WINDSHIELD GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU COCKPIT CRACKED E JBGA O OTHER O OTHER CR CRUISE 1 GL 07 602PL 1402 IN ROUTE, CO-PILOTS WINDSHIELD STARTED SPARKING, CREW TURNED OFF WINDSHIELD HEAT THEN AFTER AWHILE THE OUTER LAYER OF WI NDSHIELD CRACKED. CONTINUED ON, NO PROBLEMS. REMOVED AND REPLACED WINDSHIELD. 2 L 7 2 4F 4 F RT A12EA E25NE 2007020500042 20070205 00042 EU 2007 2 5 UG8A2007GM002 2 20070129 A 7230 STATOR RROYCE 6118C GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU NR 1 ENGINE CRACKED E UG8A K NONE O OTHER IN INSP/MAINT 1 GL 23 5115 718 85053 4019 85053 DURING VOLUNTARY COMPLIANCE WITH MFG SB 72-1706 (BORESCOPE INSPECTION OF HP COMPRESSOR 7TH STAGE STATOR VANE) A CRACKED STATOR VANE WAS DISCOVERED. 2 L 7 2 4F 4 F RT A12EA E25NE 2007020500044 20070205 00044 NM 2007 2 5 KCSA071060 1 20070202 A 5315 VERTICAL SUPPORT BOEING 747 747209F 1384800 NM PWA JT9 JT9D7R4G2 52054 NE BS 1920 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 AFT BILGE FLOORBEAM VERTICAL SUPPORT IS CORRODED AT STA 1920, LBL 63. 2 L 7 4 4F 4 F RT A20WE E3NE 2007020500058 20070205 00058 NM 2007 2 5 SWAA070490 1 20070131 A 5315 6546807 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 927 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 927, LBL 5 AND LBL 11. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007020500066 20070205 00066 NM 2007 2 5 SWAA070544 1 20070201 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM BS 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R AND 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020500069 20070205 00069 NM 2007 2 5 SWAA070525 1 20070131 A 5322 6546546 SHEAR TIE BOEING 737 7373T5 1384608 NM BS 787 S26R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007020500071 20070205 00071 NM 2007 2 5 SWAA070535 1 20070201 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 827 S25L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007020500087 20070205 00087 NM 2007 2 5 KCSA071061 1 20070203 A 5412 BULKHEAD BOEING 747 747246F 1384850 NM NR 3 NACELLE WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 NR 3 PYLON AFT ENGINE MOUNT BULKHEAD NAC STA 221.9, WORN AT HYDRAULIC LINES. 2 L 7 4 4F RT A20WE 2007020500088 20070205 00088 CE 2007 2 5 DXTA200701909 1 20070204 A 3150 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL UNKNOWN E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 905QS 7500105 2 ABORTED TAKE OFFS IN WEST PALM BEACH NR 1. WE GOT 2 CHIMES BUT NO CAS MESSAGE NR 2 POWER UPSTABLIZE, BRAKES RELEASE, STARTED TO ROLL THE NO TAKEOFF CASS AND CHIMES. THE MESSAGE MM FUEL-WE HAD (3700) ON BOARD. A/C, NO PROBLEMS FOUND, PE RFORMED POWER RUNS, ALL OK. SYSTEM OPS OK IAW CE750 MM 31-52-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007020600005 20070206 00005 2007 2 6 F3LA200700011 4 20070131 A 2565 FE240004 CYLINDER DAMPER AIRBUS A319 A319112 3930323 EU L1 DOOR SLIDE FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 915FR 902 1851 WHILE PERFORMING OPS TEST OF SLIDE DEPLOYMENT PER TC 25830-1, L1 DOOR ASSIST BOTTLE DID NOT FULLY OPEN DOOR TO DEPLOY SL IDE. REPLACED L1 DOOR CYLINDER DAMPER ASSY IAW MM 52-11-14-000-001 AND 52-11-14-400-001, PARA 4 A-D AND 5 A-C. SERVICE D AND PERFORMED PRESSURE CHECK OF L1 DOOR CYLINDER DAMPER AND RE-SAFETIED ARMING PIN, IAW AMM 52-11-14, PB 401. OPS CHE CKED NORMAL. 2 L 7 2 4F RT A28NM 2007020600010 20070206 00010 SO 2007 2 6 SIMA200703310 1 20070201 A 5310 14522460009 GUSSET EMB 135 EMB135LR 3260305 SO FUSLEAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 739AE 13518 4800 145402 FOUND GUSSET OVER CENTER HAT BEAM BETWEEN FRAME 18 TO FRAME 22 CORRODED. REMOVED AND REPLACED GUSSET IAW EMB SRM 51-40- 02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007020600025 20070206 00025 NM 2007 2 6 UIEA200700047 1 20070202 A 5414 65B940512 SKIN BOEING 747 747341 13848AM NM GE CF6 CF650E2 30018 NE NR 2 NACELLE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 NR 2 PYLON PRECOOLER EXHAUST CUT-OUT CRACKED AT LOWER AFT CORNER AT NAC 248. THE SKIN ASSEMBLY CRACKS WERE REMOVED BY T RIMMING. THE NR 3 STIFFENER WAS REINFORCED WITH A SUPPLEMENTARY STEEL LOWER ANGLE FROM NAC STATION 235 TO 254. THE RIB INSTALLATION AT NAC STATION 248 WAS MODIFIED TO ACCOMMODATE THE STEEL REPAIR ANGLE INSTALLED ON THE NR 3 STIFFENER. RE PAIRED AREAS WERE NDT INSPECTED. 2 L 7 4 4F 4 F RT A20WE E23EA 2007020600027 20070206 00027 CE 2007 2 6 DXTA200701906 1 20070202 A 3246 WHEEL CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG VIBRATION E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 920QS 7500120 NOSE WHEEL SHIMMY BETWWEN 60-70 KNOTS. DURING TAKE-OFF ROLL. REMOVED AND REPLACED NR 1 AND 2 NOSE WHEEL ASSEMBLIES WITH AN OVERHAULED UNITS AND SECURED, LUBRICATED NOSE GEAR TORQUE LINKS AS NEEDED IAW CE750 MM CHAPTER 32-41-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007020600055 20070206 00055 EU 2007 2 6 0700463233 1 20070131 A 3350 BATTERY PACK AIRBUS 320 A320211 3930320 EU EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 333NW 329 FORWARD EMERGENCY LIGHT BATTERY PACK INOP. CORRECTED BY REPLACING BATTERY PACK. CHECKS OK. 2 L 7 2 4F RT A28NM 2007020600060 20070206 00060 EU 2007 2 6 07FDEA00272 1 20070203 A 5310 A5397826720800 CROSSBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 FOUND CROSSBEAM ATTACHMENT PROFILE IS CORRODED ON C67 RT REPLACEMENT OF CORRODED PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007020600061 20070206 00061 EU 2007 2 6 07FDEA00273 1 20070203 A 5100 A5397359920800 CROSSBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 OLD REPAIRS ON CROSSBEAM C60 WITHOUT ANY OLD RECORDS CROSSBEAM WAS REPLACED BY NEW PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007020600067 20070206 00067 NM 2007 2 6 07FDEA00062 1 20070109 A 5713 ARB75132 STRINGER DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 DURING HFEC INSPECTION, CRACK FOUND AT STRINGER END-13R (XORS 577) INSIDE RT WING TANK. REPAIR CARRIED OUT AT STRINGER END-13 (XORS 577) INSIDE RT WING TANK AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2 -100. 2 L 7 3 4F RT A22WE 2007020600073 20070206 00073 EA 2007 2 6 COMA0760113 1 20070131 A 2750 1104SD100401 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS WORN A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 806CA 7359 FLIGHT 5375 - DURING YHZ APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. REPLACED THE LEFT WING NR 4 FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2007020600075 20070206 00075 NM 2007 2 6 ASAA0791430 1 20070131 A 5330 143A322321 SKIN BOEING 737 737990 NM GROUND DAMAGE A ASAA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 NM 02 323AS 30021 RAMP HIT AIRCRAFT WITH BELT LOADER AT FWD CARGO DOOR AFT EDGE DAMAGED AT BS 450 AND WL 155. REPAIRED IAW SRM 53-00-01 R EPAIR 25. 2 L 7 4 4F RT A16WE 2007020600077 20070206 00077 SO 2007 2 6 C2XA07CL018 1 20070202 A 3350 110049 POWER SUPPLY EMB 135 EMB135ER 3260203 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16510 145251 DURING ROUTINE MAINTENANCE THE RIGHT FORWARD EMERGENCY LIGHT AND THE FORWARD AISLE PATH LIGHT STRIP WERE INOPERATIVE. M AINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT BATTERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2007020600085 20070206 00085 WP 2007 2 6 UPS07849107 1 20070106 A 5340 FITTING DOUG DC8 DC871F 302199D WP FS 1766 L11R GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 AFT FUSELAGE INSIDE 60 ACCESS AT STA 1766 L11R, LONGERON END FITTING HAS SEVERAL DEEP GOUGES. REMOVE D, FABRICATED AND INSTALLED END FITTING IAW SRM 53-02-00 FIG 001F, 51-1-20D AND DWG 7531590. 2 L 7 4 4F RT 4A25 2007020600099 20070206 00099 NM 2007 2 6 DL757070065 1 20070129 A 5330 SKIN BOEING 757 757232 1384965 NM BS 340 S7L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 611DL 22818 FATIGUE CRACK IN BEAR STRAP AT UPPER FORWARD CORNER OF L-1 DOOR CUTOUT, FS 340, S-7L. CUT OUT DAMAGE IN BEAR STRAP AND SKIN AND INSTALLED DOUBLER STACKUP. 2 L 7 2 4F RT A2NM 2007020600106 20070206 00106 EA 2007 2 6 REXA200700028 1 20070203 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A REXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 8674A 7674 FLAPS FAIL AT 20 DEGREES. RESET PER AD 2006-12-21. 2 L 7 2 4F RT A21EA 2007020600107 20070206 00107 EA 2007 2 6 REXA200700029 1 20070203 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A REXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 8698A 7698 FLAP FAIL, SECOND OCCURNACE WITHIN 72 HOURS. 2 L 7 2 4F RT A21EA 2007020600109 20070206 00109 EA 2007 2 6 REXA200700031 1 20070203 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A REXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 8771A 7771 FLAPS FAIL, SECOND OCCURRENCE WITHIN 72 HRS. 2 L 7 2 4F RT A21EA 2007020600127 20070206 00127 EA 2007 2 6 SWIA200717772 1 20070130 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 445SW 7651 AFT CENTER CEILING LEVEL EMERGENCY FLOOD LIGHT IS INOP. RELAMPED AFT CENTER CEILING EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2007020600134 20070206 00134 NM 2007 2 6 AWXA200700150 1 20070116 A 5330 6545775594 SKIN PANEL BOEING 737 7373S3 1384711 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 MCN - FUSELAGE SKIN CRACKED, BS 797, S24R - S25R. REPAIRED FUSELAGE SKIN CRACKED, BS 797, S24R - S25R IAW B737-300 SRM 53-00-01 FIGURE 201. 2 L 7 2 4F RT A16WE 2007020600140 20070206 00140 NM 2007 2 6 AWXA200700156 1 20070131 A 5340 69353521 STRINGER CLIP BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED STRINGER CLIP, BS 639, S4L. REPLACED STRINGER CLIP, BS 639, S4L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600141 20070206 00141 NM 2007 2 6 AWXA200700157 1 20070122 A 5340 693535214 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED STRINGER CLIP, BS 639, S2L. REPLACED STRINGER CLIP, BS 639, S2L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600143 20070206 00143 NM 2007 2 6 AWXA200700159 1 20070122 A 5340 693535214 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED STRINGER CLIP, BS 706, S9R. REPLACED STRINGER CLIP, BS 706, S9R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600150 20070206 00150 NM 2007 2 6 AWXA200700166 1 20070121 A 5340 693535214 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED STRINGER CLIP, BS 767, S6R. REPLACED STRINGER CLIP, BS 767, S6R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600153 20070206 00153 NM 2007 2 6 AWXA200700169 1 20070123 A 5320 654581211 STIFFENER BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED CHORD ANGLE, BS 328, LBL 26. REPLACED CHORD ANGLE, BS 328, LBL 26 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600164 20070206 00164 EA 2007 2 6 REXA200700035 1 20070204 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8492C 7492 FLAPS FAIL ON APPROACH. LANDING UNEVENTFUL. COMPLIED WITH AD 2006-12-21, RESET AND MONITORING FOR 72 HOURS. 2 L 7 2 4F RT A21EA 2007020600167 20070206 00167 EA 2007 2 6 REXA200700038 1 20070204 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A REXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 8432A 7432 FLAPS FAIL AT ZERO DEGREES. 2 L 7 2 4F RT A21EA 2007020600169 20070206 00169 EA 2007 2 6 REXA200700040 1 20070204 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A REXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 8674A 7674 FLAPS FAIL, SECOND OCCURRENCE WITHIN 72 HOURS. 2 L 7 2 4F RT A21EA 2007020600173 20070206 00173 NM 2007 2 6 DL757070073 1 20070203 A 2612 FIRE LOOP BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE ENGINE BAY MALFUNCTIONED A DALA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 656DL 64864 24396 716308 DURING ENG START THE CREW GOT A LT ENG FIRE WARNING. DURING SHUTDOWN AND FIRE HANDLE PULL THE FIRE WARNING CONTINUED. THE NR 1 FIRE BOTTLE WAS DISCHARGED. REMOVED/REPLACED LT ENG NR 1 FIRE BOTTLE PER M/M. T/S FIRE WARNING PER FIM. REP LACED CORE AREA LOWER LOOP TS5251 DUE T CONDITION. CHECKED ALL LINES AND CLAMPS FOR LEAKS. REPLACED AFOLTS CARD M10224 . CHKS GOOD. CARD S/N OFF D03025 S/N D09072. RAN ENG SEVERAL TIMES WITH NO PROBLEMS NOTED. SEVERAL CLAMPS TIGHTENED TCA MANIFOLD SUPPLY DUCTS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007020600175 20070206 00175 GL 2007 2 6 DL764070076 2 20070203 A 7200 CF680C2B8F ENGINE BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 1 MAKING METAL A DALA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 27 836MH 20446 29709 704897 IR/METAL FOUND ON LT ENG MASTER CHIP DETECTOR. REPLACED NR 1 ENG PER TRANS 14T103. 2 L 7 2 4F 4 F RT A1NM E23EA 2007020600177 20070206 00177 NM 2007 2 6 DL76L070081 1 20070204 A 2410 S281T00140 GCU BOEING 767 767332 1382001 NM RIGHT UNKNOWN A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 182DN 25987 ON ENG START RT GEN CONT OFF LIGHT ILLUM FWD TO MCO AS PER MEL 24-00-01. PLACARD INSTALLED. PART NEEDED GCU MFG PN S28 1T001-40. 2 L 7 2 4F RT A1NM 2007020600178 20070206 00178 NM 2007 2 6 DL757070083 1 20070202 A 5330 143N3420 SKIN BOEING 757 757232 1384965 NM BS 520 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 684DA 27104 AT CURRENT HMV, THE CRADLE SHORING INSTALLED AT FS 520 CAUSED TWO DENTS IN THE AIRCRAFT SKIN. ONE DENT IS LOCATED JUST ABOVE S-23R AND THE SECOND DENT IS JUST BELOW S-24R. THE DENTS WERE TRIMMED OUT AND WERE REPAIRED WITH A SINGLE DOUBLER PER ER/A 459969-14. 2 L 7 2 4F RT A2NM 2007020600187 20070206 00187 2007 2 6 F3LA200700014 4 20070202 A 2565 D5348015800600 GIRT BAR AIRBUS A319 A319111 3930336 NM R2 DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 5911 1943 DURING C-3 CHECK, INSPECTION REPORTED R2 FWD GIRT BAR PLATE CORRODED. REPLACED R2 DOOR FWD GIRT BAR PLATE IAW MM 52-13- 31. REPLACED R2 DOOR FWD GIRT FITTING BLANKING PLATE IAW MM 52-13-31. 2 L 7 2 4F RT A28NM 2007020600190 20070206 00190 NM 2007 2 6 AALA20070129 1 20070119 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY EXIT LIGHT AT SEAT 20C INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007020600191 20070206 00191 NM 2007 2 6 AALA20070143 1 20070120 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 391AA 27451 DFW - EMERGENCY LIGHT AT SEAT 26B IS MISSING LENS. REPLACED EMERGENCY LIGHT LENS AT SEAT 26B. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A1NM 2007020600192 20070206 00192 NM 2007 2 6 AALA20070138 1 20070120 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 936AN 29532 MIA - EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A16WE 2007020600199 20070206 00199 EU 2007 2 6 AALA20070140 1 20070119 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80084 675 MIA - EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A35EU 2007020600200 20070206 00200 EU 2007 2 6 AALA20070141 1 20070119 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80084 675 MIA - EMERGENCY LIGHT AT SEAT 22G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A35EU 2007020600201 20070206 00201 EU 2007 2 6 AALA20070142 1 20070119 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80084 675 MIA - EMERGENCY LIGHT AT SEAT 33G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 33G. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A35EU 2007020600202 20070206 00202 WP 2007 2 6 AALA20070135 1 20070119 A 2150 DUCT DOUG DC9 DC983 3022083 WP ACM DISCONNECTED A AALA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 SW 21 978TW 53628 DFW - ON CLIMB FLIGHT ATTENDANT REPORTED SMELL OF FUMES IN CABIN FOLLOWED BY LEFT ENGINE VALVE LIGHT ILLUMINATED FOLLOWE D BY PRESSURE ABNORMAL LIGHT AND AIR FRAME VIBRATIONS. CAPTAIN SECURED WING AND ENGINE ANTI-ICE AND VIBRATIONS DECREASE D. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND CABIN AIR SUPPLY DUCT FOR RIGHT AIR CYCLE MACHINE DISCONNECTED. CONNECTED DUCT TO RIGHT AIR CYCLE MACHINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007020600203 20070206 00203 NM 2007 2 6 AALA20070134 1 20070119 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 387AM 27184 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 23B MISSING LENS. REPLACED OVERHEAD EMERGENCY LIGHT LENS AT SEAT ROW 23B. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007020600205 20070206 00205 NM 2007 2 6 07FDEA00240 1 20070202 A 5713 STRINGER DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 CRACK FOUND (APPROX 3" LONG) DURING HFEC INSPECTION ON LEFT WING TANK AT THE END OF UPPER STRINGER 12 (XORS 642). CRA CK ON LEFT HAND WING TANK AT THE END OF UPPER STRINGER 12 (XORS 642) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. RE PAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020600208 20070206 00208 NM 2007 2 6 07FDEA00243 1 20070202 A 5713 STRINGER DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 CRACK FOUND (APPROX. 0.5" LONG) DURING HFEC INSPECTION ON RIGHT WING TANK AT THE END OF UPPER STRINGER 43 (XORS 565). CRACK ON RIGHT HAND WING TANK AT THE END OF UPPER STRINGER 43 (XORS 565) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020600209 20070206 00209 NM 2007 2 6 07FDEA00244 1 20070202 A 5713 STRINGER DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 CRACK FOUND (APPROX 0.5" LONG) DURING HFEC INSPECTION ON RIGHT WING TANK AT THE END OF UPPER STRINGER 44 (XORS 523). CRACK ON RIGHT HAND WING TANK AT THE END OF UPPER STRINGER 44 (XORS 523) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020600211 20070206 00211 EU 2007 2 6 07FDEA00246 1 20070202 A 5320 SILL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 CORROSION SPOTS ON TOP CAP BEAM OF SILL BEAM C59-C64 REPAIR PERFORMED IAW, RAS/ DATLS/0003479/2006 ISS A APPROVED BY EA 6-5317-103384. 2 L 7 2 4F RT A35EU 2007020600216 20070206 00216 EU 2007 2 6 AALA20070132 1 20070119 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 MIA - EMERGENCY LIGHT AT SEAT 20G INOPERATIVE. FOUND CONNECTOR LOOSE AT SEAT 20G. RECONNECTED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 20G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007020600217 20070206 00217 WP 2007 2 6 AALA20070125 1 20070119 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 258AA 49288 PHX - EMERGENCY EXIT SIGN LIGHT AT STATION 909 RIGHT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN LIGHT A T STATION 909 RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007020600219 20070206 00219 NE 2007 2 6 AALA20070127 2 20070119 A 7261 37604331 O-RING BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4B3 NE OIL CAP TORN A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 604AA 27055 31102 BOS - INFLIGHT, RIGHT ENGINE IN FLIGHT SHUT DOWN DUE TO OIL QUANTITY LOSS. RETURNED TO BOS AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME 25 MINUTES. FOUND O-RING FOR OIL CAP TORN. FOUND DEBRIS UNDER OIL TANK CHECK VALVE. REMOVED DEBR IS AND REPLACED OIL CAP O-RING. REPLACED SCAVENGE AND PRESSURE FILTERS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2007020600221 20070206 00221 NM 2007 2 6 AALA20070159 1 20070121 A 3297 273A33016 MODULE BOEING 737 737823 13844BZ NM MLG INOPERATIVE A AALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 21 922AN 29523 ATL INFLIGHT - GEAR WOULD NOT RETRACT AFTER TAKEOFF. FOLLOWED PROCEDURE AND RAISED GEAR. ALL SYSTEMS NORMAL AFTER GEAR RETRACTED. LANDED ATL WITHOUT INCIDENT. REPLACED LANDING GEAR CONTROL PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007020600222 20070206 00222 NM 2007 2 6 AALA20070156 1 20070121 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 938AN 29533 MIA - EMERGENCY LIGHT AT SEAT 13A INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 13A. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007020700001 20070207 00001 NE 2007 2 7 HEEA113938 1 20070131 A 3297 WIRE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL MLG BROKEN E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 1545X 760050 LANDING GEAR WOULD NOT GO DOWN. REPAIRED BROKEN WIRE AT DIODE CR1. 1 G 7 2 3U 3 U H1NE E1GL 2007020700003 20070207 00003 CE 2007 2 7 DXTA200701912 1 20070118 A 2910 LINE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL HYD SYSTEM RUPTURED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 975QS 7500175 (HYD VOLUME LOW A) CAS MESSAGE ILLUMINATED. FOUND NLG STEERING HYDRAULIC LINE RUPTURED. R+R'D LINE. C/W NLG FUNCTIONA LS + LEAK CHECKS GOOD. CHECKED HYD. FILTERS TWICE. NO DEFECTS FOUND. ALL WORK DONE I/A/W 750 MM 29-10-08 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007020700005 20070207 00005 NM 2007 2 7 WRLA2007025 1 20070110 A 5510 AJC789928 RIB DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE HORIZONTAL STAB BROKEN A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 41081 48632 ITEM:DURING 2C+12A+150M CHECK, MECHANIC FOUND RT HORI STAB UPPER TO BODY FAIRING PANEL SUPPORT RIB BROKEN AT INTERSECTIO N STA 2025.00. FABRICATE FAIRING PANEL SUPPORT RIB IAW EGAT E1 NO.W2007P55B-075 REV.01. AND APPROVED DOCUMENT MFG CONTR OL NR PO209380. INSTALL THE FAIRING PANEL SUPPORT RIB IAW MD-11FSRM 51-35-01 PAGE01-13 VOL.II REV.38. 3.CONDITION CHECK NORMAL.(EGAT NRC NO. U05079). 2 L 7 3 4F 4 F RT A22WE E24NE 2007020700008 20070207 00008 NM 2007 2 7 07FDEA00339 1 20070205 A 5344 HINGE DOUG MD11 MD11 3023602 NM CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 529FE 48624 FWD CARGO DOOR HINGE AT FUSELAGE AREA FOUND WITH CORROSION. CORROSION ON FUSELAGE CARGO DOOR HINGE ASSY REMOVED AND FOU ND OUT OF LIMIT AS PER SRM 52-10-00 FIG. 14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.021" REMAINING THK 0.319". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020700013 20070207 00013 NM 2007 2 7 07FDEA00344 1 20070206 A 5344 HINGE DOUG MD11 MD11 3023602 NM CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 529FE 48624 CENTER CARGO DOOR HINGE ASSY FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10- 00 FIG. 14 VOL.I . ORIGINAL THK 0.340" MATERIAL REMOVED 0.040" REMAINING THK 0.300". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020700014 20070207 00014 NM 2007 2 7 07FDEA00345 1 20070206 A 5753 SKIN DOUG MD11 MD11 3023602 NM ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 RIGHT WING INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REPAIRED AS PER FEDEX EA 1- 5750-107771, REPAIR CLASSI FIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020700018 20070207 00018 EU 2007 2 7 07FDEA00278 1 20070203 A 5754 A53510218201 BEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 DURING KRUEGER FLAP INSTALLATION, RT WING, FOUND BEAM A535-10218-201 CORRODED REPLACEMENT OF CORRODED BEAM IAW SRM 57-45 -11. 2 L 7 2 4F RT A35EU 2007020700021 20070207 00021 EU 2007 2 7 07FDEA00281 1 20070203 A 5312 A53984814204 BULKHEAD AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 TOOLING MARKS FOUND ON AFT PRESSURE BULKHEAD AT ME15, C80/82. REPAIR WAS PERFORMED IAW RAS/DAHAM/4021516/2006 ISS. A (B LEND OUT, FASTENER REPLACEMENT), APPROVED BY EA 6-5319-103386. 2 L 7 2 4F RT A35EU 2007020700022 20070207 00022 EU 2007 2 7 07FDEA00282 1 20070203 A 5313 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 FOUND CORROSION ON STRINGER P55 LT BETWEEN C69-C70. REPAIR WAS PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007020700023 20070207 00023 EU 2007 2 7 07FDEA00283 1 20070203 A 5330 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 FOUND CORROSION ON INNER SKIN BETWEEN C55/56 BETWEEN STRINGER 55/56 RT AND 55/56 LT, AND CORROSION ON STRINGER 45 RT BET WEEN C57.3-58 AND STRINGER 51 LT BETWEEN C57.3-58. REPAIR WAS PERFORMED IAW RAS/DATLS/0003480/2006 ISS.A (CORROSION REWO RK), APPROVED BY EA 6-5316-103387. 2 L 7 2 4F RT A35EU 2007020700026 20070207 00026 NM 2007 2 7 07FDEA00287 1 20070203 A 5220 65C80678107 ANGLE BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 LT FWD O/W EMERG EXIT HATCH LOWER SEAL ANGLE FLANGE IS CORRODED ALONG MATERIAL SURFACE AND 3 FASTENER HOLES HAVE NO ED. REPLACED LOWER SEAL ANGLE REF SRM 51-30-2 PG 1. 2 L 7 3 4F RT A3WE 2007020700029 20070207 00029 NM 2007 2 7 07FDEA00290 1 20070203 A 5340 6543132 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 STRINGER CLIP HAS BEEN GROUND AT RADIUS CUT OUT BS 380 STRINGER 2L REMOVED AND REPLACED STRINGER CLIP AT 380 STR 2L REF SRM 53-10-4 PG 3 CLASSIFIED AS MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007020700033 20070207 00033 NM 2007 2 7 07FDEA00294 1 20070203 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 FOUND STRINGER CLIP HAS BEEN GROUND AT RADIUS CUT OUT BS 660 STRINGER 8L. REPLACED STRINGER CLIP, REF SRM 51-30-2 PG 2. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007020700034 20070207 00034 NM 2007 2 7 07FDEA00295 1 20070203 A 5320 53FX1565 WEB BOEING 727 727233 138408A NM ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 FOUND MAIN DECK FLOOR WEB UPPER SURFACE IS GOUGED BS 617-620, LBL 57-60, SL 208. FABRICATED NEW WEB REF DWG 53FX1565 AN D SRM 51-30-2 P3 1-12. 2 L 7 3 4F RT A3WE 2007020700037 20070207 00037 NM 2007 2 7 07FDEA00298 1 20070203 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 620 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 FOUND MAIN DECK FLOORBEAM UPPER FLANGE IS CORRODED BS 620 LBL 4-20, WL 208. INSTALLED REPAIR ON MAIN DECK FLOORBEAM UPP ER CHORD AT STA 620, LBL 4 THRU 20, WL 208 REF B727 SRM 53-10-8 PG 18-23 AND DWG 53FX1547. CLASSIFIED AS A MAJOR REPAIR . 2 L 7 3 4F RT A3WE 2007020700038 20070207 00038 NM 2007 2 7 07FDEA00299 1 20070203 A 5754 651622193 SKIN BOEING 727 727233 138408A NM ZONE 500 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 LT WING NR 4 SLAT REPAIR AT O/B TRACK SKIN DOES NOT CONFORM TO FEDX DWG SR 27-57-034 REMOVED AND REPLACED LT NR 4 SLAT R EF MM 27-81-011. 2 L 7 3 4F RT A3WE 2007020700039 20070207 00039 NM 2007 2 7 07FDEA00300 1 20070205 A 5710 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 LEFT WING TELESCOPIC DUCT CUTOUT FOUND CRACKED. LEFT HAND WING CRACKED TELESCOPIC DUCT CUTOUT TRIMMED OFF AND REPAIR DO UBLER AND FILLER FABRICATED AND INSTALLED AS PER SRM 57-10-00 FIGURE 42 VOLUME I AND FEDEX E.A. 1-5710-107772, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020700041 20070207 00041 NM 2007 2 7 07FDEA00302 1 20070205 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 RIGHT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2007020700042 20070207 00042 NM 2007 2 7 07FDEA00303 1 20070205 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 LEFT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION ON LE FT HAND WING - INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE REPAIRED AS PER FEDEX E.A. 1 -5750-107781 PT1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020700043 20070207 00043 NM 2007 2 7 07FDEA00304 1 20070205 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 LEFT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION ON LEF T HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE REPAIRED AS PER FEDEX E.A. 1-575 0-107781 PT1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020700045 20070207 00045 NM 2007 2 7 07FDEA00306 1 20070205 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 LEFT WING, OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION ON LEF T HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE REPAIRED AS PER FEDEX E.A. 1-5750-107783 PT1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020700046 20070207 00046 NM 2007 2 7 07FDEA00307 1 20070205 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 LEFT WING, OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), FORWARD ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION ON LEF T HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), FORWARD ATTACHMENT INBOARD BORE REPAIRED AS PER FEDEX E.A. 1 -5750-107783 PT1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020700047 20070207 00047 NM 2007 2 7 07FDEA00308 1 20070205 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 LEFT WING, OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), FORWARD ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION ON LE FT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), FORWARD ATTACHMENT OUTBOARD BORE REPAIRED AS PER FEDEX E.A. 1-5750-107783 PT1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020700048 20070207 00048 NM 2007 2 7 07FDEA00309 1 20070205 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 LEFT WING, OUTBOARD FLAP OUTBOARD HINGE, WING SIDE, PIVOT BORE FOUND CORRODED. CORROSION ON LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), PIVOT BORE REPAIRED AS PER FEDEX E.A. 1-5750-107783 PT1, REPAIR CLASSIFIED AS MAJ OR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020700049 20070207 00049 NM 2007 2 7 07FDEA00310 1 20070205 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 RIGHT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), FORWARD ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION ON RIGH T HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), FORWARD ATTACHMENT INBOARD BORE REPAIRED AS PER FEDEX E.A. 1- 5750-107784, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020700051 20070207 00051 NM 2007 2 7 07FDEA00312 1 20070205 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 RIGHT WING, OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION ON RI GHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE REPAIRED AS PER FEDEX E.A. 1-5750-107782, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020700053 20070207 00053 NM 2007 2 7 07FDEA00314 1 20070205 A 5311 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 CABIN, LEFT STA 1661 BETWEEN LONGERON 12 TO LONGERON 14 FRAME FOUND DENT. CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTION AT 9,500 CYCLE S. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020700054 20070207 00054 NM 2007 2 7 07FDEA00315 1 20070205 A 5311 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 CABIN, LEFT STA 535 AT 9G NET FRAME FOUND DAMAGED BY SUPPORT YOKES. CABIN - LEFT HAND STA 535 AT 9G NET DAMAGED FRAME R EPAIRED AS PER FEDEX DRAWING SRZ-53-503. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020700055 20070207 00055 NM 2007 2 7 07FDEA00316 1 20070205 A 5230 PAN BOEING BOEING 727 727233 138408A NM CARGO DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 FUSELAGE LOWER LOBE NR 1 CARGO DOOR EXT HANDLE PAN LOWER SIDE IS GOUGED FROM CONTACT WITH CONTROL ROD FWD EYE BOLT AT BS 569 REF N01095. REPLACED DOOR REF MM 52-35-011-4, OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 2007020700056 20070207 00056 EU 2007 2 7 07FDEA00317 1 20070205 A 3230 DAMPER AIRBUS 300 A300B4622R 3930312 EU MLG DISCHARGED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 728FD 581 L/G WOULD NOT RETRACT USING EITHER SYS 1 OR 2. CHECKED PROX DETECT CONTROL UNIT FOR FAILURES. NOTED THAT THE FAILURE C ODE "BL" IS LOGGED. T/S AT THIS TIME PER TSM 32-30-00 PER AMM 32-10-00-6. CLEARED MEMORIZED FAULT ON PROX DETECTION U NIT WITH NO FURTHER FAULTS NOTED. ALL SENSORS SERVICEABLE PER BITE TEST OF PROX DETECTION CONTROL UNIT PER TSM SERVICE OF LT BOOGIE PITCH DAMPER WITH NITROGEN PER AMM 12-12-32-0 PARAGRAPH 10. FOUND THAT PITCH DAMPER ONLY HAD A 400 PSI PR ECHARGE. CURRENT LIMITS PER CHART FIG 11 IS 1300 PSI. RECHARGED PITCH DAMPER TO SERVICEABLE LIMITS PER AMM 12-12-32-0. PERFORMED LT BOOGIE PITCH DAMPER NITROGEN PRESSURE DECAY CHECK WITH NO PRESSURE DROP OVER A ONE HOUR. 2 L 7 2 4F RT A35EU 2007020700057 20070207 00057 EU 2007 2 7 07FDEA00318 1 20070205 A 3230 D226550003 DAMPER AIRBUS A300 A300F4622R 3930360 EU ZONE 700 DAMAGED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 728FD 1149 1149 581 GEAR WOULD NOT RETRACT IN FLIGHT. SWITCHED POSITION DETECTORS, NO AVAIL. PLZ REFERENCE MTSI 32-30 / 1119 FOR ALL WORK ACCOMPLISHED REGARDS THIS ITEM. A/C LDG GEAR RETRACT SYS NOW ON MEL. REMOVED AND REPLACED BOGIE PITCH DAMPER/FLEW AC GEAR DWN ON MEL 32-30-01 TO MEM FOR GEAR SWING/ALL FUNCTIONAL CHKS WERE GOOD. 2 L 7 2 4F RT A35EU 2007020700059 20070207 00059 NM 2007 2 7 SWAA070556 1 20070202 A 3350 20121 CHARGER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 10Y CHECK, FOUND AFT CABIN BATTERY CHARGER INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007020700063 20070207 00063 NM 2007 2 7 SWAA070579 1 20070203 A 3350 307IBPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 797MX 27890 DURING SCHEDULED MV1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 13 ABC. REMOVED AND REPLACED LIGHT BULB PE R MM. 2 L 7 2 4F RT A16WE 2007020700064 20070207 00064 NM 2007 2 7 SWAA070553 1 20070202 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 793SA 27888 EEPLS COVER LOOSE AT ROW 17 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007020700065 20070207 00065 NM 2007 2 7 SWAA070573 1 20070202 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 415WN 29836 DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007020700067 20070207 00067 NM 2007 2 7 SWAA070554 1 20070202 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 506D S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 FUSELAGE SKIN CRACKED AT BS 506D, STR 8L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007020700068 20070207 00068 NM 2007 2 7 SWAA070563 1 20070202 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 376 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 376, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007020700069 20070207 00069 NM 2007 2 7 SWAA070559 1 20070202 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 380 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007020700070 20070207 00070 NM 2007 2 7 SWAA070572 1 20070202 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM BS 970 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007020700072 20070207 00072 SO 2007 2 7 C2XA07IA025 1 20070203 A 3350 20131A BATTERY PACK EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14186 15035 2129 14500924 DURING MAINTENANCE INSPECTION ,THE FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. 2 L 7 2 4F 4 F RT TE6CH 2007020700074 20070207 00074 EA 2007 2 7 COMAO760118 1 20070131 A 2752 853D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAP FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 806CA 2966 7359 FLIGHT 5375 - DURING YHZ APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. REPLACED THE LEFT OUTBOARD FLAP INBOARD ACTUATO R. 2 L 7 2 4F RT A21EA 2007020700075 20070207 00075 EA 2007 2 7 COMA0760119 1 20070131 A 2750 860D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAP FAULTY A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 814CA 18309 7387 FLIGHT 5295 - RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED PDU AND COMPLIED WI TH EO 27-046AD. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007020700076 20070207 00076 EA 2007 2 7 COMA0760120 1 20070131 A 2750 860D10018ABCD FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 814CA 14054 7387 FLIGHT 5295 - RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED FECU AND COMPLIED W ITH EO 27-046AD. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007020700078 20070207 00078 CE 2007 2 7 DXTA200701886 1 20070128 A 3241 320892 METERING VALVE CESSNA 680 680CE 2076811 CE ANTI SKID SYS MALFUNCTIONED E DXTA O OTHER O OTHER CL CLIMB 1 GL 07 370QS 263 6800099 DURING NOSE GEAR RETRACTION STRONG BANGING AND FLASHING UNSAFE LIGHT DURING MULTIPLE ATTEMPS ON OCF. ALWAYS DOES IT IN C LIMB, NEVER IN LEVEL FLIGHT. TO RULE OUT VIBRATION ON NOSE BY OUT OF BALANCE MAIN TIRES, TURNED OFF ANTI-SKID TAPPED BRA KES BEFORE RETRACTION-STILL DOES IT. REMOVED BRAKE METERING VALVE DUE TO INTERNAL FAILURE. INSTALLED NEW VALVE IAW MM CH 32-42-00, OPS CHECKED AND LEAK CHECKED GOOD. 2 L 7 2 4F RC T00012WI 2007020700079 20070207 00079 NM 2007 2 7 SWAA070562 1 20070202 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 937 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 937, STR 4R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007020700080 20070207 00080 NM 2007 2 7 SWAA070557 1 20070202 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007020200163 20070202 00163 EU 2007 2 2 200701241 1 20070119 A 2781 1702288A SENSOR EMB ERJ170 ERJ170100SE 3260406 EU LE FLAP DEFECTIVE A UHLA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 17 644RW 17000061 FLIGHT 7629 AUS TO ORD, ON TAKEOFF BEFORE FLAP RETRACTION RECEIVED SLAT FAIL CAUTION MESSAGE. CREW RTF AND LANDED WITHO UT INCIDENT. MTX CLEARED MESSAGES, CYCLED FLAPS SEVERAL TIMES, DETERMINED SAFE FOR FLIGHT. ON SECOND TAKEOFF, CREW GO T SAME SLAT FAIL MESSAGE. 0/0 ON SLAT/FLAP POSITION INDICATOR. CREW WAS ABLE TO DETERMINE THAT SLATS WERE FULLY RETRAC TED. EN ROUTE PORTION OF FLIGHT NORMAL. LANDED WITH SLATS 0, FLAPS 2. MAINTENANCE REMOVED AND REPLACED RT OUTBOARD SK EW SENSOR. OPS CK GOOD, NO DEFECTS NOTED. 2 L 7 2 4F RT A56NM 2007020200169 20070202 00169 NM 2007 2 2 CALA0700035 1 20070124 A 5320 65C80737353 FLOOR SUPPORT BOEING 737 737524 1384721 NM BS 344-360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14667 28927 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT TOP ANGLE BETWEEN STA 344 AND 360, BL 0. THE FLOOR SUPPORT WAS REMO VED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020200175 20070202 00175 NM 2007 2 2 USAA070075 1 20070130 A 5340 ATTACH ANGLE BOEING 737 7373B7 1384580 NM BS 348-351 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 511AU 23594 FOUND CRACKS IN ATTACH ANGLES AT STA 348-351, S-16L. REMOVED DAMAGED ANGLES, FAB'D NEW PART (3) PER EO 5305V203, SRM 53 -10-04. .25 INCH DEFECT SIZE. 2 L 7 2 4F RT A16WE 2007020200181 20070202 00181 SO 2007 2 2 C2XA07BT010 1 20070126 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14974 145161 BTV FLT 2414 - DURING 5A CHECK FOUND RT OVERWING EMERGENCY LIGHT DOES NOT COME ON. REMOVED AND REPLACED RT OVERWING EME RGENCY LIGHT BULB IAW EMB145 AMM 33-50-10. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007020200182 20070202 00182 SO 2007 2 2 C2XA07TY002 1 20070123 A 5330 14554051003 SKIN EMB 145 EMB145XR 3260214 SO FUSELAGE DAMAGED A C2XA O OTHER O OTHER AP APPROACH 1 SW 27 25134 10764 10764 145714 AIRCRAFT HAD BIRDSTRIKE WHILE AIRBORNE AT 210 KNOTS AND 5000 FEET, AIRCRAFT LANDED UNEVENTFULLY. AFTER TEMPORARY REPAIR AND FERRY FLIGHT EWR TO TYS, TYS MAINTENANCE REPAIRED DAMAGE TO FRAMES 1A THROUGH FRAME 3 PART NUMBERS: 145-21705-403, 145-51202, AND 145-51203-403], STRINGER 1L, 4L, AND 6L PART NUMBERS: 145-54053-001, 145-54054-001, AND 145-54055-001 AND LT FORWARD NOSE SKIN, RT FORWARD NOSE SKIN, NOSE CENTER SKIN, SPLICED DAMAGED SKIN, PART NUMBERS: RT 145-54052-003 AND NOSE CENTER 145-30203-001, SEE LT NOSE SKIN BELOW. AIRCRAFT CURRENTLY UNDER GOING REPAIRS. 2 L 7 2 4F RT 2007020200189 20070202 00189 NM 2007 2 2 UPS07449059 1 20070111 A 5313 STRINGER BOEING 747 747123F NM BS 2177 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C AFT OF BULK CARGO COMPT, FX STRINGER FOUND CRACK AT BS 2177 S46R AS MARKED, CRACK LENGTH 2". FX BS 21 50 TO BS 2185 STR 46R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007020200193 20070202 00193 NM 2007 2 2 UPS07449063 1 20070111 A 5410 65B903162 FITTING BOEING 747 747123F NM NR 3 NACELLE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 NR 3 PYLON FWD B/H I/B HANGER FTG AREA FASTENER REMOVED UPPERR HOLE AT T/R SYNC LOCK MOD HFEC INSP FOUND WITH CRACK INDI CATION, CRACK LENGTH 0.030". NR 3 PYLON FWD BULKHEAD CHORD REPLACED AS PER SRM 51-10-01 P9. 2 L 7 4 4F A20WE 2007020200195 20070202 00195 NM 2007 2 2 KCSA071056 1 20070130 A 5315 FLOORBEAM BOEING 747 747209F 1384800 NM BS 1800 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 AFT PIT BS 1800 FLOORBEAM WEB CRACKED AT RBL-15, WL-115. 2 L 7 4 4F RT A20WE 2007020500001 20070205 00001 SW 2007 2 5 AC2A113718 1 20070116 A 6410 222016001131 TAIL ROTOR BELL 430 430 1182150 SW ALLSN 250C 250C30S 03013 GL TAIL ROTOR WILL NOT BALANCE E AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 430CT 4663 49089 THIS BLADE WAS HEAVY, COULD NOT BALANCE ON AIRCRAFT. MARVEL AND IT TOOK 52.26 GRAMS SPANWISE TO BRING IT IN. INSPECTION REVEALED OPENING AT TRAILING EDGE BY WEIGHTS AND PITCH HORN MOUNTING POINT, ALSO CORROSION ON OUTER BEARING BOSS. 1 G 7 2 3U 3 U RT H9SW E1GL 2007020500002 20070205 00002 CE 2007 2 5 BSYA200700002 1 20070109 A 2130 660020756 VALVE LEAR 35 35A 5170602 CE CABIN PRESSURE MALFUNCTIONED E BSYA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 51LC 302 AIRCRAFT DEPARTED LCK AND WAS CLIMBING THRU 16,000 FT WHEN CABIN PRESSURIZATION STARTED TO CLIMB. AIRCRAFT RETURNED TO LCK WHERE MAINTENANCE FOUND BAD SAFETY VALVE PRESSURIZATION DIFFERENTIAL VALVE. 2 L 7 2 4F A10CE 2007020500011 20070205 00011 NM 2007 2 5 SWAA070512 1 20070130 A 3350 MS155721 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007020500035 20070205 00035 CE 2007 2 5 DXTA200701903 1 20070201 A 3220 WHEEL CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG VIBRATION E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 920QS 7500120 SEVERE NOSE WHEEL SHIMMY ON TAKE-OFF ROLL UNDER 60 KTS. KICKED OFF LOWER YD. REMOVED AND REPLACED LEFT AND RIGHT NOSE W HEEL ASSEMBLYS IAW CESSBA MODEL 750 MM CHAP 32-41-01 PAGE 1-5. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007020500037 20070205 00037 CE 2007 2 5 DXTA200701905 1 20070201 A 3240 BRAKE ASSY BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 161QS RK435 BRAKES DO NOT WORK UNTIL MAXIMUM FORCE IS APPLIED (ON BOTH SIDES). HYDRAULIC PRESSURE NORMAL AND NO LIGHTS. PERFORMED V ISUAL INSPECTION OF BRAKE ASSEMBLIES, MASTER CYLINDERS, MIXING & ANTISKID VALVES AND ASSOCIATED LINES. NO DEFECTS OR LEA KAGE FOUND. VERIFIED CORRECT MLG STRUTS SERVICING. VISUALLY INSPECTED L&R SQUAT SWITCHES. PERFORMED ANTI SKID BOX CONTIN UITY CHECKS, ALL SATISFACTORY. CLEANED & RECONNECTED CONNECTOR (P304). OPS CHECK ON TAXI SATISFACTORY. ALL WORK PERFORME D IAW HAWKER 400X M/M 32-40-00. 2 H 7 2 4F 4 F RT A16SW E25EA 2007020500039 20070205 00039 CE 2007 2 5 012807N556CS1 1 20070128 A 3233 99125374 ACTUATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG MALFUNCTIONED E Z5FA O OTHER N FALSE WARNING AP APPROACH 1 EA 63 556CS 1337 5605577 ENROUTE THERE WERE GEAR DOWN INDICATIONS WHEN THE GEAR WAS UP, THIS CAUSED INTERMITTENT BRAKE PRESSURE AND ANTI-SKID WAR NINGS. THINGS APPEARED NORMAL AFTER A GEAR SWING WAS PERFORMED. ON APPROACH, THE RT MAIN GEAR WOULD NOT INDICATE DOWN AND LOCKED, EVEN AFTER CYCLING GEAR. THE EMERGENCY CHECKLIST WAS USED, BLOWING THE GEAR DOWN. THIS FAILED TO BRING ON THE DOWN AND LOCKED INDICATION. AIRCRAFT LANDED WITH NO PROBLEMS. LOCAL MAINTENANCE REPLACED GEAR ACTUATOR, PERFORMED ALL REQUIRED CHECKS AND THE AIRCRAFT WAS RETURNED TO SERVICE 01/30/2007 2 L 7 2 4F 4 F RT A22CE E00059EN 2007020500049 20070205 00049 NM 2007 2 5 CALA0700039 1 20070126 A 5315 BAC15181211 FLOORBEAM BOEING 737 737724 13844BY NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27733 28800 INSPECTION FOUND FLOORBEAM CORRODED AT BS 986.5 BETWEEN LBL 26.5 AND LBL 43. THE FLOORBEAM WAS REPAIRED IAW ECRA 5320-0 1876. 2 L 7 2 4F RT A16WE 2007020500080 20070205 00080 NM 2007 2 5 SWAA070520 1 20070131 A 5754 65C26602 SKIN BOEING 737 7373H4 1384600 NM NR 2 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND LEFT WING NR 2 L/E SLAT OUTBOARD AFT CORNER DELAMINATED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007020500081 20070205 00081 WP 2007 2 5 AALA20070163 1 20070122 A 3260 TARGET DOUG DC9 DC982 3022082 WP LANDING GEAR INOPERATIVE A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 21 7508 49802 RNO INFLIGHT - GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR EXTENSION. ALL THREE GEAR GREEN LIGHTS ON. SLIGHT BUFFETING NOTED. EMERGENCY GEAR EXTENSION HANDLE PULLED. AIRCRAFT LANDED RNO WITH GEAR DOORS OPEN. FOUND SCRAPING ON DOOR SKID PADS. REPLACED MAIN LANDING GEAR POSITION TARGET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007020600007 20070206 00007 SO 2007 2 6 SIMA200703303 1 20070201 A 3210 14571035409 CAP EMB 135 EMB135LR 3260305 SO RT MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 739AE 13518 4800 145402 FOUND RIGHT MAIN LANDING GEAR BEARING CAP CORRODED. REMOVED AND REPLACED BEARING CAP IAW EMB AMM 32-10-01. RETURNED AI RCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007020600016 20070206 00016 NM 2007 2 6 SWAA070523 1 20070131 A 5340 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM BS 747 S21R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007020600024 20070206 00024 NM 2007 2 6 UIEA200700045 1 20070203 A 5313 STRINGER BOEING 747 747341 13848AM NM GE CF6 CF650E2 30018 NE BS 500 S10L CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 STRINGER FOUND CRACKED AT STATION 500 STR 10L. STRINGER AT STATION 500 STRINGER 10L REPAIRED PER SB 747-53A2484 FIGURE 20 AND DEVIATION PER 8100-9. 2 L 7 4 4F 4 F RT A20WE E23EA 2007020600029 20070206 00029 NE 2007 2 6 ASMF200701007 2 20070129 A 7220 815331 BLADE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE RT ENGINE NICKED W ASMF K NONE C F.O.D. IN INSP/MAINT 1 SW 23 216AM 49586 725745 DURING TRANSIT CHECK, A BLADE WAS DETECTED DAMAGED DUE TO A FOD IN RT ENGINE. A NICK WAS DETECTED AT 2.5 INCHES BETWEEN PLATFORM AND MIDSPAN SHROUD OF 1 INCH LONG WITH .1250 INCH DEPTH. THE BLADE WAS REWORKED IAW MM 72-33-21 AND BOROSCOPIC INSPECTION WAS PERFORMED TO 6TH AND 7TH STAGES OF COMPRESSOR IAW MM 72-30-01, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007020600030 20070206 00030 WP 2007 2 6 IXXA070005O 1 20070130 A 5270 PROXIMITY SWITCH DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE MLG DOOR DEFECTIVE A IXXA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 11 606AL 95510 1395 46044 AFTER GEAR RETRACTION,THE LANDING GEAR DOORS NOT LATCHED LIGHT ILLUMINATED. THE CREW RECYCLED THE GEAR AND THE LIGHT REM AINED ON, UNTIL THE GEAR WAS EXTENDED. THE CREW CONTINUED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE GEAR AN D FOUND SEVERAL LOOSE HI-LOKS ALONG THE KEELBEAM TEE FITTINGS. MAINTENANCE REPLACED THE LOOSE HI-LOKS AND ALSO REPLACED THE LT PROXIMITY SWITCH. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2007020600033 20070206 00033 NM 2007 2 6 HALA0700043 1 20070131 A 3241 ANTI-SKID SYS BOEING 717 717200 1383700 NM LT MLG CHATTERING A HALA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 WP 13 477HA 55122 BTB - LEFT BRAKE CHATTERING WHEN APPLIED. ACCOMPLISHED FIM 32-40 TASK 804 FOUND INTERNAL FAULT ON BCU 32431E AND 32431D . REMOVED AND REPLACED BCU PER AMM 32-45-01 ACCOMPLISHED RTS PER ANTI-SKID CHECK OK BLED BRAKES PER AMM 32-43-01. LEAK CHECK OK SERVICED FLUID AS REQUIRED TAXIED CHECK OK. 2 L 7 2 4F TR A6WE 2007020600046 20070206 00046 SO 2007 2 6 FDKA200701007 1 20070107 A 3350 BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 829MJ 145228 FDM 5967 ATL-GSP (1915 PHX LCL) BOTH LOWER OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MX RESET THE BATTERY PACKS AND O PS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007020600058 20070206 00058 EU 2007 2 6 07FDEA00268 1 20070203 A 5320 A5361215220500 FLOOR SUPPORT AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 FLOOR STRUCTURE BETWEEN C10 AND C12A ANGLE CRACKED REPLACEMENT OF CRACKED ANGLE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007020600063 20070206 00063 EU 2007 2 6 07FDEA00275 1 20070203 A 5320 A5377264320000 SILL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 ANGLE BRACKET AT DOOR SILL C24A-25 IS DAMAGED AND CORRODED PART WAS REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007020600066 20070206 00066 NM 2007 2 6 07FDEA00060 1 20070109 A 5713 ARB75111 STRINGER DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 DURING HFEC INSPECTION, CRACK FOUND AT STRINGER END-11 (XORS 704) INSIDE LT WING TANK. REPAIR CARRIED OUT AT STRINGER E ND-11 (XORS 704) INSIDE LT WING TANK AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2- 100. 2 L 7 3 4F RT A22WE 2007020600070 20070206 00070 NE 2007 2 6 07FDEA00325 2 20070205 A 7532 32910481 BLEED VALVE AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680 30025 NE ZONE 400 LEAKING A FDEA E ENGINE SHUTDOWN J WARNING INDICATION LD LANDING 1 SO 25 664FE 768 REPORT OF NR 1 FIRE INDICATION ON LANDING ROLLOUT AT KROC. AML LOGPAGE FROM FLIGHT CREW TO FOLLOW REFER TO WRI 72-00-9 550 FOR ACTION TAKEN ON THIS ITEM. BLEED AIR TO NR 1 ENG DUCTING. FOUND BLEED VALVE VENT FITTING LEAKING EXCESSIVELY, VERIFIED THIS TO BE EXCESSIVE BY CHECKING NR 2 ENG BLEED VLV, REPLACED NR 1 ENG BLEED VLV PER M/M 36-11-14-4-01. ENG R UN AND LEAK CK GOOD. SEE WRI 36-10/9555 FOR MORE DETAILS. 2 L 7 2 4F 4 F RT A35EU E13NE 2007020600076 20070206 00076 EA 2007 2 6 COMA0760112 1 20070131 A 2750 1104SD100301 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAP WORN A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 806CA 7359 FLIGHT 5375 - DURING YHZ APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. REPLACED THE LEFT WING NR 3 FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2007020600080 20070206 00080 EA 2007 2 6 TRAX200700127 1 20070129 A 5320 STIFFENER CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 VERTICAL WEB STIFFENER CRACKED AT BOTTOM HOLE RBL 25.75 ON FRONT SIDE OF WEB. 2 L 7 2 4F RT A21EA 2007020600081 20070206 00081 EA 2007 2 6 TRAX200700128 1 20070129 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 680BR 7679 FLAPS FAIL MESSAGE IN FLIGHT FAILED AT 8 COMPLIIED WITH QRH LANDED ON 27R WITH 200 FPM MAXIUM AT TOUCHDOWN WITHOUT INCID ENT. EMERGENCY EQUIPMENT ON STANDBY. 2 L 7 2 4F RT A21EA 2007020600082 20070206 00082 EA 2007 2 6 TRAX200700129 1 20070129 A 3250 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING UNKNOWN A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 830AS 7236 NOSEWHEEL STEERING MESSAGE AFTER TAKEOFF. AIRCRAFT RETURNED TO MSN AFTER T/O. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007020600084 20070206 00084 WP 2007 2 6 UPS07849105 1 20070107 A 5313 SAA3645897503 LONGERON DOUG DC8 DC871F 302199D WP FS1350-1490 L34L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 L34L BETWEEN 1420-1440 HAS CORROSION UNDER REPAIR & ON LONGERON. REMOVED, FABRICATED AND INSTALLED L ONGERON IAW SRM 53-02-02 FIG 4A, 51-1-20D, 51-1-21 AND DWG 4613495. 2 L 7 4 4F RT 4A25 2007020600096 20070206 00096 EA 2007 2 6 COMA0760109 1 20070130 A 2750 860D10018ABCD CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 931CA 7389 7037 FLIGHT 5092 - FLAP FAIL MESSAGE RECEIVED, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED FECU. 2 L 7 2 4F RT A21EA 2007020600100 20070206 00100 NM 2007 2 6 DLM88070066 1 20070128 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 530 S26-27R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 986DL 53313 FOUND AIRCRAFT FUSELAGE DAMAGED AT APPROX STA 530 BETWEEN LONGERON 26R AND 27R. REMOVED DAMAGE. FABRICATED REPAIR PER SRM 53-04 FIG 12B CLASS I REPAIR. OK TO TREAT AND PAINT AREA AND REPAIR PIECE QC1509. TREATED AND PAINTED AREA AND REP AIR PER SRM 53-04 FIG 12B. TREAT AND PAINT OK. OK TO INSTALL REPAIR QC1509, INSTALLED REPAIR PER SRM 53-04 FIG 12B. R EPAIR INSTALLATION OKQC1418. 2 L 7 2 4F RT A6WE 2007020600112 20070206 00112 EA 2007 2 6 REXA200700034 1 20070204 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A REXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 820AY 8020 FLAPS FAIL, SECOND OCCURRENCE WITHIN 72 HOURS. 2 L 7 2 4F RT A21EA 2007020600119 20070206 00119 NM 2007 2 6 AWXA200700142 1 20070202 A 5320 D53112827202 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 831AW 1576 SAL - CORROSION ON MAIN CABIN FLOOR SUPPORT BEAM,+ Y503, F15+2". REPLACED MAIN CABIN FLOOR SUPPORT BEAM,+ Y503, FR 12 - FR 16 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007020600132 20070206 00132 NM 2007 2 6 AWXA200700148 1 20070113 A 5320 65566551 REVEAL BOEING 737 7373S3 1384711 NM BS 787 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 MCN - AFT CARGO COMPARTMENT DOOR CUT OUT FORWARD TORQUE BOX LOWER REVEAL STRIP CRACKED, BS 787, S18R - S24R. REPLACED A FT CARGO COMPARTMENT DOOR CUT OUT FORWARD TORQUE BOX LOWER REVEAL STRIP CRACKED, BS 787, S18R - S24R IAW B737-300 SRM 51 -40-02. 2 L 7 2 4F RT A16WE 2007020600142 20070206 00142 NM 2007 2 6 AWXA200700158 1 20070122 A 5340 66235744 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED STRINGER CLIP, BS 706, S10R. REPLACED STRINGER CLIP, BS 706, S10R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600157 20070206 00157 NM 2007 2 6 AWXA200700135 1 20070118 A 3397 BRZ013P7373HP2 WIRE HARNESS BOEING 737 7373S3 1384711 NM ZONE 200 DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 MCN - EEL - EMERGENCY ESCAPE PATH LEFT WIRE HARNESS HAS MISSING/DAMAGED INSULATION AND LOOSE JIFF CONNECTORS. REPAIRED AND SECURED THE EMERGENCY ESCAPE PATH LEFT WIRE HARNESS HAS MISSING/DAMAGED INSULATION AND LOOSE JIFF CONNECTORS IAW BSW PM 20-10-13, 20-90-14, 20-30-12 AND 20-42-01. 2 L 7 2 4F RT A16WE 2007020600168 20070206 00168 EA 2007 2 6 REXA200700039 1 20070204 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A REXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 8598B 7598 FLAPS FAIL. COMPLIED WITH AD 2006-12-21, PERFORMED VISUAL INSPECTION, NO DEFECTS NOTED. PLACED UNDER 72 HOUR MONITORIN G. 2 L 7 2 4F RT A21EA 2007020600171 20070206 00171 NM 2007 2 6 DL757070071 1 20070203 A 5311 148N11301 FRAME BOEING 757 757232 1384965 NM FS 1743 BUCKLED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 FRAME DAMAGED FROM IMPACT WITH GSE EQUIP. NEW FRAME SECTION FABRICATED AND SPLICED PER SRM. 2 L 7 2 4F RT A2NM 2007020600172 20070206 00172 NM 2007 2 6 DL76G070072 1 20070201 A 2612 MODULE BOEING 767 767332 1382001 NM CONTROL PANEL MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 174DZ 29693 FIRE WARNING HORN SOUNDED/AURALLY ALERTED IMMEDIATELY ON LIFT OFF. NO LIGHTS EICAS MESSAGES O ANY INDICATIONS AT ALL WE RE APPARENT. THE HORN SOUNDED UNTIL LANDED AND TAXIED BACK. PULLED J34 AND B18 WARN ELEX CBS. HORN SILENCED WHEN B18 PULLED. LANDING WEIGHT 319.9. NO OVERWEIGHT LANDING. REMOVED AND REPLACED PWR SUPPLY MODULE B AND ENG/CARGO FIRE TEST PANEL. ALL OPS CHK NML. TEST OPS NML FIRE WARNING SHUTS DOWN. 2 L 7 2 4F RT A1NM 2007020600176 20070206 00176 NM 2007 2 6 DL757070080 1 20070204 A 4990 OIL CAP BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE APU MISSING A DALA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 621DL 10224 22911 P2748 WITH THE RT ENG GEN ON MCO AND THE APU RUNNING IN FLIGHT, THE CREW GOT AN APU LOW OIL QTY MESSAGE. LATER THE APU SHUT D OWN AND THE A/C WAS DOWN TO A SINGLE ELECTRICAL SOURCE. IDG REPLACEMENT AND APU T/S IN WORK OPEN COWLING SERVICED APU. RAN APU. FOUND OIL FITTING WITH A MISSING CAP. REPLACED MISSING CAP. RAN APU. FOUND NO LEAKS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007020600179 20070206 00179 2007 2 6 F3LA200700013 4 20070202 A 2565 D5348015800700 GIRT BAR AIRBUS A319 A319111 3930336 NM L2 DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 5911 1943 DURING C-3 CHECK, INSPECTION REPORTED L2 FWD GIRT BAR PLATE CORRODED. REPLACED L2 DOOR GIRT BAR PLATE IAW AMM 52-13-31. REPLACED L2 DOOR GIRT BAR BLANKING PLATE IAW AMM 52-13-31-400-007. 2 L 7 2 4F RT A28NM 2007020600183 20070206 00183 EA 2007 2 6 REXA200700042 1 20070204 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A REXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 8836A 7836 FLAPS FAIL, SECOND OCCURRENCE WITHIN 72 HOURS. 2 L 7 2 4F RT A21EA 2007020600188 20070206 00188 2007 2 6 F3LA200700015 4 20070202 A 2565 D5348015800600 GIRT BAR AIRBUS A319 A319111 3930336 NM R2 DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 5911 1943 DURING C-3 CHECK, INSPECTION REPORTED R2 AFT GIRT BAR PLATE CORRODED. REPLACED R2 DOOR AFT GIRT BAR PLATE IAW MM 52-13- 31. REPLACED R2 DOOR AFT GIRT BAR FITTING BLANKING PLATE IAW AMM 52-13-31400-007. 2 L 7 2 4F RT A28NM 2007020600193 20070206 00193 EU 2007 2 6 AALA20070136 1 20070118 A 2910 SEAL AIRBUS 300 A300B4605R 3930308 EU HYD SYSTEM LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SW 21 14056 463 JFK INFLIGHT - DURING DESCENT GREEN PUMP LOW PRESSURE LIGHT FOR BOTH PUMPS ILLUMINATED. MANUALLY EXTENDED LANDING GEAR DURING APPROACH. FLUID CYCLED FROM ZERO TO MID RANGE. LANDED JFK WITHOUT INCIDENT AND AIRCRAFT WAS TOWED TO HANGAR. FOUND GREEN SYSTEM HYDRAULIC LEAK AT GREEN SYSTEM ACCUMULATOR FITTING AND LEAK UNDER FLOOR AT SEATS 15AB TO 16AB GREEN S YSTEM PRESSURE LINE. REPLACED SEAL FOR GREEN SYSTEM ACCUMULATOR FITTING LEAK AND ACCOMPLISHED PERMASWAGE DEUTSCH REPAIR AND REPLACED BOTH ENGINE CREW SYSTEM HYDRAULIC PUMPS AND REQUIRED FILTERS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007020600195 20070206 00195 NM 2007 2 6 AALA20070130 1 20070119 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY EXIT LIGHT AT SEAT 39C INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT SEAT 39C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007020600196 20070206 00196 NM 2007 2 6 AALA20070124 1 20070119 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 756AM 30264 LGW - EMERGENCY LIGHT COVER AT SEAT 40G IS MISSING. REPLACED EMERGENCY LIGHT COVER AT SEAT 40G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007020600197 20070206 00197 NM 2007 2 6 AALA20070131 1 20070119 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY EXIT LIGHT AT SEAT 26G INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT SEAT 26G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007020600198 20070206 00198 NM 2007 2 6 AALA20070139 1 20070120 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 936AN 29532 MIA - EMERGENCY LIGHT AT SEAT 22D HAS MISSING LENS COVER. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007020600204 20070206 00204 NM 2007 2 6 Q2SA740004 1 20070203 A 3210 65B054522 BOLT BOEING BOEING 747 747230B 1384889 NM ACTUATOR SHEARED A Q2SA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 03 740SA 377 21380 GEAR WILL NOT RETRACT AFTER TAKEOFF. BOTH RIGHT BODY GEAR TILT LIGHTS CAME ON. AIR TURN BACK TO PANC. FOUND RIGHT BOD Y GEAR TRUCK POSITION ACTUATOR FORWARD ATTACH BOLD SHEARED. INSPECTED AND NO OTHER DISCREPANCIES FOUND. REMOVED AND RE PLACED RIGHT BODY GEAR TRUCK POSITION ACTUATOR AND HARDWARE’S IN ACCORDANCE WITH AMM 32-13-15. 2 L 7 4 4F A20WE 2007020600214 20070206 00214 NM 2007 2 6 AALA20070126 1 20070119 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 790AN 30251 NRT - EMERGENCY LIGHT AT AFT GALLEY ON LEFT SIDE HAS BROKEN LENS. REPLACED EMERGENCY LIGHT LENS AT AFT GALLEY LEFT SIDE . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007020600215 20070206 00215 EU 2007 2 6 AALA20070133 1 20070119 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 MIA - EMERGENCY LIGHT AT SEAT 26G INOPERATIVE. FOUND CONNECTOR LOOSE AT SEAT 26G. RECONNECTED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 20G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007020700007 20070207 00007 NM 2007 2 7 QXEA200700129 1 20070203 A 5230 SHAFT BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR LACK OF LUBE A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 419QX 4145 BOI FLIGHT NR 2360: FUSELAGE DOOR WARNING LIGHT ILLUMINATED CLIMBING THROUGH 18000 FEET. RAN CHECKLIST. AIRCRAFT RETU RNED TO FIELD. MAINTENANCE INSPECTED AIRCRAFT FUSELAGE DOORS. FOUND FWD CARGO DOOR HANDLE PARTIALLY CLOSED. INSPECTED FWD CARGO DOOR AND LOCKING MECHANISM. NO DEFECTS NOTED. CLEANED AND LUBED FWD CARGO DOOR HANDLE SHAFT. OPS CHECK NOR MAL IAW AMM TASK 31-62-00-710-801 AND SUBTASK 31-62-00-710-001(A)(2). NO OTHER DEFECTS NOTED. NO PARTS REPLACED. AIRC RAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007020700009 20070207 00009 NM 2007 2 7 07FDEA00340 1 20070206 A 5344 HINGE DOUG MD11 MD11 3023602 NM CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 529FE 48624 FWD CARGO DOOR HINGE FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10- 00 FIG.14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.025" REMAINING THK 0.315". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02. REPA IR CLASSIFIED MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020700015 20070207 00015 NM 2007 2 7 07FDEA00346 1 20070206 A 5754 STIFFENER DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 LEFT WING LEADING EDGE STIFFENER AROUND XORS 690 FOUND CRACKED. LEFT HAND WING LEADING EDGE CRACKED STIFFENER AROUND XO RS 690 REPAIRED AS PER FEDEX E.A. 1-5710-107779, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020700016 20070207 00016 NM 2007 2 7 QXEA200700128 1 20070204 A 5270 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM DOOR WARNING UNKNOWN A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 414QX 4061 RNO FLIGHT NR 2443: FUSELAGE DOOR WARNING CLIMBING THROUGH ABOUT4-5000 AGL. DOOR PAGE INDICATED PROBLEM WAS AFT CARGO D OOR. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE VISUALLY INSPECTED AFT CARGO DOOR UPON LANDING. FOUND HANDLE NOT IN DE TENT. PERFORMED OPERATIONAL TASK OF AFT CARGO DOOR IAW Q400 TASK 52-31-00-710-801. OPS CHECK GOOD. PERFORMED PRESSURI ZATION CHECK TO VERIFY AFT CARGO DOOR HANDLE FLUSH AND NO DOOR OPEN LIGHT PER TASK 21-00-00-863-801 AND 21-00-00-863-802 . NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007020700017 20070207 00017 CE 2007 2 7 AMWA82406 1 20070202 A 3213 130909B132 BOLT BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT MLG MISSING A AMWA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 CE 07 174YV 115 115 UE174 UPON TAXI, CREW STATED AIRCRAFT WAS SHAKING AND RETURNED TO GATE. RT MAIN LANDING GEAR TORQUE KNEES FOUND TO HAVE PIVOT BOLT MISSING. CAUSE UNKNOWN. SUBSEQUENT INSPECTION OF RT MAIN GEAR SATISFACTORY. REPLACED UPPER AND LOWER TORQUE LINKS AND HARDWARE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A24CE E26NE 2007020700020 20070207 00020 EU 2007 2 7 07FDEA00280 1 20070203 A 5330 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 FOUND SEVERAL SCRUB MARKS ON SKIN PANEL BETWEEN C56-C57, P34-P35 LT AND RT. REPAIR WAS PERFORMED IAW RAS/DATLS/0003483/ 2006 ISS. A (BLEND OUT), APPROVED BY EA 6-5316-103385. 2 L 7 2 4F RT A35EU 2007020700032 20070207 00032 NM 2007 2 7 07FDEA00293 1 20070203 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 FOUND STRINGER CLIP CRACKED IN CUT OUT RADIUS AT BS 680 STR 7L. REMOVED AND REPLACED STR CLIP AT STA 680 STR 7L REF SRM 51-30-02 CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007020700035 20070207 00035 NM 2007 2 7 07FDEA00296 1 20070203 A 5320 INTERCOSTAL BOEING 727 727233 138408A NM BS 1086 S23R TOOL DAMAGE A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 284FE 22621 INTERCOSTAL AT BS 1086, JUST ABOVE STRINGER 23R HAS A HOLE DRILLED IN RADIUS. HOLE LOCATED BELOW NUT PLATE ATTACH RIVET . DAMAGED INTERCOSTAL REMOVED NEW PART FABRICATED AND INSTALLED REF BAC DWG 65-56131, SRM 51-30-2, SRM 51-10-2 PG 7. C LASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007020700044 20070207 00044 NM 2007 2 7 07FDEA00305 1 20070205 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 LEFT WING, OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION ON LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE REPAIRED AS PER FEDEX E.A. 1-5 750-107783 PT1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020700060 20070207 00060 NM 2007 2 7 SWAA070574 1 20070202 A 3350 307IBPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 429WN 33658 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 3 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007020700073 20070207 00073 SO 2007 2 7 C2XA07IA026 1 20070203 A 3350 20131A BATTERY PACK EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14186 11148 2133 14500924 DURING MAINTENANCE INSPECTION ,THE FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. 2 L 7 2 4F 4 F RT TE6CH 2007020700082 20070207 00082 NM 2007 2 7 SWAA070566 1 20070202 A 5311 6546529 FRAME BOEING 737 7373Q8 1384670 NM BS 440 S8R-8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R AND 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020700084 20070207 00084 NM 2007 2 7 SWAA070581 1 20070203 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM BS 520 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020700085 20070207 00085 NM 2007 2 7 SWAA070568 1 20070202 A 5311 6546534 FRAME BOEING 737 7373Q8 1384670 NM BS 520 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020700086 20070207 00086 NM 2007 2 7 SWAA070570 1 20070202 A 5311 6546549 FRAME BOEING 737 7373Q8 1384670 NM BS 767 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020700087 20070207 00087 NM 2007 2 7 SWAA070582 1 20070203 A 5311 6546554 FRAME BOEING 737 7373H4 1384600 NM BS 847 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020700088 20070207 00088 NM 2007 2 7 SWAA070583 1 20070203 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM BS 867 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020700089 20070207 00089 NM 2007 2 7 SWAA070571 1 20070202 A 5311 6546558 FRAME BOEING 737 7373Q8 1384670 NM BS 907 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020700091 20070207 00091 NM 2007 2 7 SWAA070567 1 20070202 A 5311 6558280 FRAME BOEING 737 7373Q8 1384670 NM BS 360 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020700093 20070207 00093 NM 2007 2 7 SWAA070580 1 20070203 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM BS 500C S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020700094 20070207 00094 NM 2007 2 7 SWAA070569 1 20070202 A 5311 65C22909 FRAME BOEING 737 7373Q8 1384670 NM BS 500C S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020700096 20070207 00096 NM 2007 2 7 SWAA070561 1 20070202 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 500 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C4 CHECK, FOUND STRINGER 16R CRACKED AT BS 500. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007020700097 20070207 00097 NM 2007 2 7 SWAA070586 1 20070203 A 3350 MS155721 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED A1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007020700100 20070207 00100 CE 2007 2 7 DXTA200701884 1 20070128 A 3230 LANDING GEAR CESSNA 680 680CE 2076811 CE RIGHT UNKNOWN E DXTA O OTHER S J AFFECT SYSTEMS WARNING INDICATION LD LANDING 1 GL 07 301QS 6800010 RT GEAR WOULD NOT INDICATE DOWN (RED UNLOCK LIGHT ON, NO RT GREEN GEAR LIGHT ). ON DOWNWIND GEAR BLEW DOWN SUCCESFULLY ( 3 GREEN LIGHT) LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RT MAIN ACTUATOR IAW CE680 M/M 32-30-40. OPS CHECKED GOOD. 2 L 7 2 4F RC T00012WI 2007020700102 20070207 00102 CE 2007 2 7 DXTA200701891 1 20070130 A 3210 LANDING GEAR CESSNA 560 560XL 2076702 CE RIGHT UNKNOWN E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 642QS 5605561 GREEN RT MLG LIGHT ILLUMINATED AFTER GEAR RETRACTION, STAYED ON FOR ABOUT 5-6 MINUTES AND THEN LIGHT WENT OUT, AIRCRAFT WAS COLD SOAKED. THE AIRCRAFT WAS COLD SOAKED THE NIGHT BEFORE. APPROACH AND LANDING RESULTED IN NO ABNORMALITES. REM OVED AND REPLACED RT MAIN LANDING GEAR ACTUATOR IAW CE560XLS MM CH 32-30-04. GROUND CHECKS GOOD. 2 L 7 2 4F RT A22CE 2007020700103 20070207 00103 SO 2007 2 7 C2XA07IA023 1 20070130 A 2750 3632001003 PDU EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL TE FLAPS INOPERATIVE A C2XA O OTHER J WARNING INDICATION DE DESCENT 1 SW 27 16520 12088 12088 145372 CVG, FLIGHT 2620, THE CREW REPORTED A FLAP FAIL MESSAGE ON EICAS DURING DESCENT. THE AIRCRAFT DIVERTED, WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP POWER DRIVE UNIT, OPERATIONALLY CHECKED WITH NO DEFECTS, AN D THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007020700104 20070207 00104 EU 2007 2 7 XN0A1360 1 20070203 A 2721 CONTROL UNIT AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE RUDDER TRIM MALFUNCTIONED A XN0A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 472AS 125 RUDDER WILL ONLY GO .5 TO .6666 OR 20 UNITS TO THE LT DURING GROUND CONTROL CHECK. FOUND ARTIFICIAL FEEL AND TRIM UNIT CATCHING ON TRIM STOP. REMOVED AND REPLACED RUDDER ARTIFICIAL FEEL AND TRIM UNIT IAW AMM CHAPTER 27-23-11, OPS CHECKS GO OD IAW AMM CHAPTER 27-22-00.(STATUS:ORIG/CLOSED) 2 L 7 2 4F 4 F RT A35EU E23EA 2007020700105 20070207 00105 CE 2007 2 7 DXTA200701913 1 20070205 A 3230 VALVE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG MALFUNCTIONED E DXTA A UNSCHED LANDING S J AFFECT SYSTEMS WARNING INDICATION CL CLIMB 1 GL 07 961QS 7500061 GEAR WOULD NOT RETRACT. AFTER T/O GEAR LIGHT INDICATED 4 GREEN / AND UNLOCK HANDLE UP. 3 GREEN ONLY HANDLE DOWN. CYCLED GEAR NO CHANGE. FOUND EMERGENCY BLOW DOWN HAS BEEN DISCHARGED. RESET PNEUMATIC BOTTLE VALVE, AND THE LANDING GEAR HYDRA ULIC CONTROL VALVE. BLED THE AIR OUT OF SYSTEM, CONNECTED MULE AND PERFORMED MULTIBLE GEAR SWING. SYSTEM OPS CHECKED GOO D PER CESSNA MAINTENANCE MANUAL CHPT 32-00-01. SERVICED HYDRAULICS SYSTEM AND EMERGENCY BLOW DOWN BOTTLE I/A/W APPICABLE SECTIONS OF CHAPTER 12 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007020700108 20070207 00108 EU 2007 2 7 YENA2007005 1 20070131 A 2780 19017235401 WIRE HARNESS EMB ERJ190 ERJ190100IGW 3260408 EU GE CF34 CF3410E6 30015 NE SLATS FAILED A YENA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 15 198JB 2567 19000021 IN FLIGHT SHORTLY AFTER T/O WING A-1 FAIL MSG. AFTER PUSHING OUT WING A/I BUTTON FOLLOWING QRH TO RESET. A-1 WING 1 LEAK CAME ON EICAS. FOLLOWED QRH ISOLATED LT WING FROM ALL BLEED SOURCES. ON SYSTEMS PAGE LT WING DIAGRAM WAS AMBER AND TEMP WAS 290 C. WHILE RT WING TEMP WAS -4 C. THE WING LEAK MSG DID NOT EXTINGUISH AT LEAST 5 MIN. THE TEMP INDICATION ALSO W ENT TO AMBER DASHES THEN CAME BACK IN 5 MIN AND SHOWED ROUGHLY -4 C. FAULTS WERE LT IB SLAT 4 TEMP SENSOR R/R TEMP SENSO R IAW 30-11-02, NO HELP. R/R LT IB SLAT 4 WIRE HARNESS IAW MM 27-83-07-000-801 INSTALLED IAW AMM 27-83-07-416-801. OPS CHECK GOOD IAW AMM 27-80-00-710-801A (W512) OK FOR SVC. 2 L 7 2 4F 4 F RT A57NM E00070EN 2007020700110 20070207 00110 EU 2007 2 7 AALA20070157 1 20070121 A 3350 LENS AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 33069 512 MIA - EMERGENCY LIGHT AT SEAT 21G HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007020700111 20070207 00111 NM 2007 2 7 AALA20070158 1 20070121 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 796AN 30796 DFW - WALL MOUNTED EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. RELAMPED WALL MOUNTED EMERGENCY LIGHT AT LEFT N UMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007020700112 20070207 00112 WP 2007 2 7 AALA20070146 1 20070121 A 2150 39613011 VALVE DOUG DC9 DC982 3022082 WP AIR CONDITIONING INOPERATIVE A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 476AA 49651 DFW INFLIGHT - LEFT AND RIGHT AIR CONDITION PACKS INOPERATIVE. UNABLE TO PRESSURIZE AIRCRAFT. RETURNED TO DFW AND LAN DED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE FOR EVALUATION. REPLACED LEFT FLOW CONTROL VALVE. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007020700114 20070207 00114 WP 2007 2 7 0700439610 1 20070129 A 2132 CLAMP DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE DUCT BROKEN A NWAA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 GL 01 610NW 47432 WHILE CLIMBING PASS FL280, THE CABIN ALTITUDE BEGAN TO CLIMB UNCONTROLLABLY AT 1000 FPM. FLIGHT CREW INITIATED AN EMERG ENCY DESCENT TO 8000 FEET AND RETURNED TO DEPARTURE. COM PROCEDURES WERE COMPLIED WITH, THE OUTFLOW VALVE WAS CONFIRMED CLOSED BUT THE CABIN ALTITUDE REACHED 14500 FEET AND THE CABIN MASKS DID DEPLOY. THE LANDING WAS UNEVENTFUL. MAINTENANC E FOUND A BROKEN CLAMP AND A BLOWN DUCT AND REPAIRED THEM. THE MASKS WERE RE-STOWED AND THE AIRCRAFT HAS RETURNED TO SER VICE. 2 L 7 2 4F 4 F A6WE E2EA 2007020700115 20070207 00115 NM 2007 2 7 AALA20070145 1 20070120 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 361AA 24042 LAX - EMERGENCY LIGHT AT RIGHT OVERWING EXIT SLIDE INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT OVERWING EXIT SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007020700116 20070207 00116 EU 2007 2 7 2007UALA00217 1 20070128 A 5101 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE VIBRATION A UALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 29 435UA 613 MODERATE TO SEVERE VIBRATIONS FELT IN AFT CABIN & FLT DECK FLOOR ON CLIMBOUT. VIBRATIONS SUBSIDED AT LEVEL OFF. CONDIT IONS REAPPEARED ON SUBSEQUENT FLIGHT. ACCOMPLISHED ELEVATOR INTEGRITY CHECKS. ALL 4 SERVOS REQUIRED ADJUSTMENT TO .5 DEGREES NOSE UP. FREEPLAY CHECKS ALL WITHIN LIMITS USING DIAL INDICATOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007020700120 20070207 00120 NM 2007 2 7 2007UALA00221 1 20070127 A 5310 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 942 S24L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 A 3.5 INCH CRACK FOUND AT STATION 942 THROUGH 945.5 JUST ABOVE STRINGER 24L, FWD AND ABOVE POTABLE WATER SERVICE. MAJOR REPAIR: REPAIRED PER EVA 70035 A REV DATE 27JAN07. 2 L 7 2 4F 4 F RT A16WE E21EU 2007020700122 20070207 00122 NM 2007 2 7 2007UALA00223 1 20070126 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 773UA 26929 SEAT 3F EEL LIGHT ASSY IS MISSING. REPLACED AFT EEL LIGHT ASSY ON SEAT 3F.OPS CHECK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007020700124 20070207 00124 NM 2007 2 7 2007UALA00225 1 20070129 A 3397 FEEDER CABLE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 906UA 25006 EEL LIGHTS INOPERATIVE AFT OF ROW 15. REPLACED CABLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007020700127 20070207 00127 SO 2007 2 7 RAIA00701040 1 20070130 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN SMOKE A RAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 814HK 145046 POST FLT NR 5560 - STL - SMOKE IN CABIN AFTER PARKING AT GATE. SMOKE SEEMED TO CLEAR OUT AFTER CLOSING NR 2 PACK AND AP U BLEED. MAINTENANCE INSPECTED THE CABIN LIGHTING AND PERFORMED AN OPS CHECK OF THE AIRCRAFT BLEED SYSTEMS WITH NO DEFE CTS NOTED. 2 L 7 2 4T RT T00011AT 2007020700128 20070207 00128 WP 2007 2 7 AALA20070147 1 20070122 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 481AA 49656 LGA - EMERGENCY LIGHTS AT FORWARD GALLEY CEILING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD GAL LEY CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007020700129 20070207 00129 NM 2007 2 7 AALA20070148 1 20070121 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 662AA 25296 MIA - EMERGENCY LIGHT AT SEAT 23D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A2NM 2007020700131 20070207 00131 NM 2007 2 7 AALA20070150 1 20070121 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 602AN 27053 MIA - EMERGENCY LIGHT AT SEAT 30D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 30D. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A2NM 2007020700132 20070207 00132 NM 2007 2 7 AALA20070152 1 20070121 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 948AN 30086 MIA - EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007020700133 20070207 00133 NM 2007 2 7 AALA20070153 1 20070121 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 948AN 30086 MIA - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LEFT NUMBER O NE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007020700134 20070207 00134 NM 2007 2 7 AALA20070154 1 20070121 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 948AN 30086 MIA - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR NEXT TO JUMPSEAT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR NEXT TO JUMPSEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007020700136 20070207 00136 NM 2007 2 7 AALA20070151 1 20070121 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 696AN 26976 MIA - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIGHT NUMBER O NE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007020700137 20070207 00137 EA 2007 2 7 COMA0760110 1 20070131 A 2750 1104SD100101 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS WORN A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 806CA 7359 FLIGHT 5375 - DURING YHZ APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. REPLACED THE LEFT WING NR 1 FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2007020700138 20070207 00138 NM 2007 2 7 AWXA200700137 1 20070114 A 5311 65458076 FRAME BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 MCN - R1 DOOR CUTOUT FRAME CRACKED, BS 312, S8R AT THE FORWARD UPPER STOP PAD FITTING AREA. REPLACED R1 DOOR CUTOUT FR AME CRACKED, BS 312, S8R AT THE FORWARD UPPER STOP PAD FITTING AREA IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020700142 20070207 00142 NM 2007 2 7 UPS07449097 1 20070109 A 5313 STRINGER BOEING 747 747123 1384873 NM BS 900-910 S28L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT STRINGER FOUND CRACK AT STA 900 AND STA 910 S28L. CRACK LENGTH .375 INCH. FWD CARGO COMPT BS 890-950 STR 28L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007020700147 20070207 00147 NM 2007 2 7 UPS07649104 1 20070201 A 5610 WINDOW BOEING 767 76734AF 1385212 NM COCKPIT STUCK A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 308UP 27761 INSPECTION TYPE:N/A FIRST OFFICER`S SLIDING WINDOW WILL NOT OPEN. INSTALLED GUIDE BEARING PER IPC AND AMM 56-11-02-4. ITEM CLEARED. 2 L 7 2 4F RT A1NM 2007020700148 20070207 00148 WP 2007 2 7 UPS07849074 1 20070102 A 5315 9750471517 FLOORBEAM DOUG DC8 DC871F 302199D WP FS 240 LBL 36 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C2 FLOORBEAM VIEWED FROM A-PIT STA 240 LBL 36 HAS A 9 INCH CRACK. REPAIRED FLOORBEAM AT STA 240 LBL 36 IAW SAA EA008-5310-01-A00586 UPS RAA DC8-53-20605-A, BAC MSG 1-271080190, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007020700150 20070207 00150 WP 2007 2 7 UPS07849091 1 20070103 A 5321 5612298343 PRESSURE PANEL DOUG DC8 DC871F 302199D WP FS 80 LBL24 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C2 COCKPIT SUBFLOOR HORIZ PRESS PANEL STA -80 LBL 24 HAS EXFOLIATION CORROSION. REPAIRED COCKPIT SUBFLO OR HORIZ PRESS PANEL AT STA -80 LBL 24 IAW SAA EA 008-5330-01-A0608, UPS EO DC8-5330-26007-A, BAC SERVICE MSG 1-27599134 7, AND FAA FORM 8100-9. THIS REPAIR MUST BE REPLACED AT 24,000 CYCLES, WITH REPEAT INSPECTIONS AT 4,000 CYCLES AFTER A/ C LEAVES HEAVY MAINT. 2 L 7 4 4F RT 4A25 2007020700152 20070207 00152 SO 2007 2 7 BQVA200721071 1 20070201 A 5730 WEDGE GULSTM G1159 G1159A 3970109 SO RROYCE SPEY SPEY511* 54523 EU LT WING DAMAGED E BQVA K NONE O OTHER IN INSP/MAINT 1 EA 01 982RK 10771 310 DURING THE SCHEDULED 72 MONTH LT WING WEDGE INSPECTION CMP 575030, ONE WING WEDGE HOLD DOWN RIVNUT WAS FOUND TO BE IN AN OVERSIZED HOLE. 2 L 7 2 4F 4 F A12EA E2EU 2007020700153 20070207 00153 WP 2007 2 7 UPS07849093 1 20070131 A 3350 RELAY DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY/RELAY UNIT. NOW OPS OK. REF 3 3-50-01-2. 2 L 7 4 4F RT 4A25 2007020700154 20070207 00154 WP 2007 2 7 UPS07849094 1 20070104 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 450-610 L31RL CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 HFEC & VISUAL INSP DETECTED A .335 INCH CRACK ON THE C-2 (B-PIT) LOWER AFT JAMB CORNER. CRACK EXTEND S FROM EDGE OF SKIN TO FASTENER HOLE AS MARKED. REMOVED AND REPLACED BELLY SKIN FROM FS 450 TO FS 610 L31R TO L31L IAW SRM 51-1-21, 51-1-20D, DWG 5779913. 2 L 7 4 4F RT 4A25 2007020700155 20070207 00155 WP 2007 2 7 UPS07849101 1 20070107 A 5313 SAA3646107 LONGERON DOUG DC8 DC871F 302199D WP FS1400-1410 L35L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 LONGERON 35L CRACKED ALONG RADIUS AT FS 1400-1410. REMOVED, FABRICATED AND INSTALLED LONGERON IAW SR M 53-2-2 FIG 4A, 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2007020700159 20070207 00159 NM 2007 2 7 UPS07249102 1 20070201 A 3350 LIGHT BOEING 727 72731C 1384011 NM EMERGENCY EXIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. PERFORMED EMERGENCY LIGHT CHECK PER MM 33-50-01-5. NO DEFECT NOTED. 2 L 7 3 4F A3WE 2007020700160 20070207 00160 NM 2007 2 7 UPS07449077 1 20070110 A 5313 65B082314 LONGERON BOEING 747 747123 1384873 NM RT MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C L/G - RIGHT WLG W/W OVERWING LONGERON WEB UPPER SURFACE AT BS 1258-1261 FOUND CORROSION AND CRACKED. CORROSION BLEND OUT 0.055 X .5 X 3 INCHES EXCEED SRM LIMIT. L/G - RIGHT WLG W/W OVERWING LONGERON WEB REPLACED AT BS 12 54-1264 AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007020700161 20070207 00161 NM 2007 2 7 UPS07449078 1 20070110 A 5320 654U61345 SUPPORT FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LEFT BLG ACTUATOR UPPER SUPPORT FITTING I/B LUG BORE FOUND CRACKED. CRACK LENGTH 0.25 INCH. LEFT BLG ACTUATOR UPPER SUPPORT FITTING REPLACED IAW UPS EO B747-5340-0994-D APP 8.4 TO 8.6. 2 L 7 4 4F A20WE 2007020700163 20070207 00163 NM 2007 2 7 UPS07449080 1 20070111 A 5340 65B15085330 ANGLE BOEING 747 747123 1384873 NM BS 1480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C AFT CARGO COMPT STA 1480 BULKHEAD LOWER ANGLE FOUND CORRODED AT RBL 25. CORROSION BLEND OUT 0.060 X . 5 X 3 INCHES EXCEED SRM LIMIT. ANGLE REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007020700165 20070207 00165 NM 2007 2 7 UPS07449082 1 20070115 A 5313 STRINGER BOEING 747 747123 1384873 NM BS 1760-1780 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D AFTER BS 1760-1780 RIGHT WINDOW FORGING REMOVED FOUND STR 22R FWD END CORRODED AS MARKED. CORROSI ON BLEND OUT 0.039 X 1 X 3 INCHES EXCEED SRM LIMIT. M/D BS 1740-1960 STR 22R STRINGER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007020700168 20070207 00168 NM 2007 2 7 UPS07449085 1 20070115 A 5313 STRINGER BOEING 747 747123 1384873 NM BS 1800-1820 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D AFTER BS 1800-1820 RIGHT WINDOW FORGING REMOVED FOUND STR 22R AFTER END CORRODED. CORROSION BLEND OUT 0.080 X .5 X 2 INCHES EXCEED SRM LIMIT. M/D BS 1740-1960 STR 22R STRINGER REPLACED AND INSTALLED AS PER SRM 51-10- 01 PG 9 AND 51-30-02 REFER NRC 51873 FOR WORKING DETAIL. 2 L 7 4 4F A20WE 2007020700169 20070207 00169 NM 2007 2 7 UPS07449086 1 20070121 A 5313 65B0765737 STRINGER BOEING 747 747123 1384873 NM BS 460 S15L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LEFT SIDE BS 460 STR 15 STRINGER FASTENER HOLE CRACK FOUND RUNNING TO UPPER EDGE AND RUNNING DOWNWARD APPROX .25 INCH, CRACK LENGTH .5 INCH. M/D LEFT BS 460 STR 15L STRINGER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007020700170 20070207 00170 NM 2007 2 7 ZZDA070123099 1 20070123 A 5340 SUPPORT BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. GLIDE SLOPE ANTENNA SUPPORT AND SHIELD DENTED AND BENT BEYOND REPAIR. R EPLACED GLIDE SLOPE ANTENNA SUPPORT AND SHIELD PER MDC DRAWING 9971488 REV (NEW) DATED 10-22-97. 2 L 7 2 4F TR A6WE 2007020700174 20070207 00174 NM 2007 2 7 ZZDA070123103 1 20070123 A 5311 FRAME BOEING 717 717200 1383700 NM BS 69 CRACKED A ZZDA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. LEFT SIDE FRAME AT STA 69.0 CRACKED AND BENT BEYOND REPAIR. REPLACED LE FT SIDE FRAME AT STA 69.0 PER MDC DRAWING 9911503 REV CT DATED 1/7/04. 2 L 7 2 4F TR A6WE 2007020700177 20070207 00177 NM 2007 2 7 ZZDA070123106 1 20070123 A 5343 SUPPORT BEAM BOEING 717 717200 1383700 NM NLG CRACKED A ZZDA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. NLG LT AND RT SUPPORT BEAMS CRACKED AND BENT BEYOND REPAIR. REPLACED NL G LT AND RT SUPPORT BEAMS PER MDC DRAWING 9910088 REV CJ DATED 01/24/06. 2 L 7 2 4F TR A6WE 2007020700178 20070207 00178 NM 2007 2 7 ZZDA070123107 1 20070123 A 5320 WEB BOEING 717 717200 1383700 NM NLG CRACKED A ZZDA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. NLG LEFT AND RIGHT SUPPORT WEB CRACKED AND BENT BEYOND REPAIR. REPLACED NLG LEFT AND RIGHT SUPPORT WEB AND DETAILS PER MDC DRAWING 9910088 REV CJ DATED 01/24/06. 2 L 7 2 4F TR A6WE 2007020700180 20070207 00180 NM 2007 2 7 ZZDA070123109 1 20070123 A 5312 BULKHEAD BOEING 717 717200 1383700 NM BS 110 CRACKED A ZZDA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. BULKHEAD AT STA 110 CRACKED AND BENT BEYOND REPAIR. REPAIRED BULKHEAD A T STA 110 PER MDC DRAWING 9911509 REV L DATED 5/13/02 AND PER BOEING ENGINEERING ROD/SKETCH NUMBER 06-12-10-003-002, 810 0-9 APPROVED ON 01-07-07. 2 L 7 2 4F TR A6WE 2007020700184 20070207 00184 NM 2007 2 7 CALA0700050 1 20070204 A 5320 143A5410 INTERCOSTAL BOEING 737 737824 13844BZ NM BS 380-400 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18243 28806 INSPECTION FOUND A .5 INCH CRACK IN FORWARD WET AREA INTERCOSTAL AT STA 380-400, LBL 24. A NEW INTERCOSTAL WAS INSTALLE D IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020700185 20070207 00185 NM 2007 2 7 CALA0700051 1 20070204 A 5347 143A531033 SEAT TRACK BOEING 737 737824 13844BZ NM BS 375 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18243 28806 INSPECTION FOUND SEAT TRACK CORRODED AT STA 375, LBL 24.75. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND REPLACED IAW ECRA 5321-01379 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020700186 20070207 00186 NM 2007 2 7 ZZDA070123110 1 20070123 A 3220 SUPPORT BOEING 717 717200 1383700 NM BS 110 CRACKED A ZZDA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. LEFT & RIGHT BUNGEE SUPPORT INSTALLATION AT STA 110.0 RIGHT CRACKED AND BENT BEYOND REPAIR. REPLACED LEFT & RIGHT BUNGEE SUPPORT INSTALLATION AT STA 110.0 RIGHT PER MDC DRAWING 9911599 REV Z DATED 02/03/99. 2 L 7 2 4F TR A6WE 2007020700187 20070207 00187 WP 2007 2 7 MWEA070025 1 20070202 A 5230 59101419 PAN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE CARGO DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 809ME 48071 MID CARGO DOOR INNER PAN GOUGED ON INNER RADIUS AT FORWARD LATCH. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F A6WE E9NE 2007020700188 20070207 00188 NM 2007 2 7 DU4R2007032 1 20070107 A 5330 SKIN BOEING 757 757232 1384965 NM BS 620-640 DENTED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 AIRCRAFT SKIN HAS DENT BETWEEN FRAME 620 TO 640, S-17-18 LT SIDE. CUT OUT DENTED AREA. HFEC CUT OUT IAW B757 SRM 51-20 -02 AND NDT MANUAL. FABRICATED AND INSTALLED DOUBLER AND FILLER 5.00" ROUND FROM 2024-T3 .040" IAW B757 SRM 53-00-01 A ND NDT MANUAL PT 6 51-00-19. 2 L 7 2 4F RT A2NM 2007020700189 20070207 00189 NM 2007 2 7 DU4R2007034 1 20070118 A 5320 PANEL BOEING 757 757232 1384965 NM BS 1386 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION AFT CARGO DOOR THRESHOLD SIDE PANEL UNDERSIDE BS 1386 RBL 20. REMOVED CORRODED PANEL INSTALLED P/N 146N5391-2 4 IAW B757 SRM. 2 L 7 2 4F RT A2NM 2007020700190 20070207 00190 NM 2007 2 7 DU4R2007035 1 20070114 A 5320 WEB BOEING 757 757232 1384965 NM BS 1420-1440 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION AT BS 1420 TO BS 1440 SIDEWALL WEB RT. FABRICATED AND INSTALLED CUSP WEB 19.5" BY 9.5" FROM 7075-T6 .040" IAW B757 SRM 51-40-02, 53-60-13 AND 51-30-01. 2 L 7 2 4F RT A2NM 2007020700191 20070207 00191 NM 2007 2 7 DU4R2007036 1 20070128 A 5340 284N16331 SUPPORT FITTING BOEING 757 757232 1384965 NM BS 1440 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION AFT PIT RT SIDE BS 1440 S-26R E6 AVIONICS RACK BOLT RUSTED. REMOVED AND REPLACED SUPPORT FITTING WITH P/H 284 N1633-1 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007020700193 20070207 00193 NM 2007 2 7 DU4R2007038 1 20070124 A 5320 146N5391U72 PANEL BOEING 757 757232 1384965 NM BS 1310-1380 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION AFT CARGO RT TRANSITION PANEL AT BS 1310 TO BS 1380. HEAVY CORROSION BS 1343.5 TO BS 1380 AROUND GILL LINER A TTACH HOLES AND FLOOR PANEL ATTACH HOLES. DRILLED UP AND INSTALLED NEW TRANSITION PANEL 69-1/2" BY 7-1/2" P/N 146N5391U 72 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007020600037 20070206 00037 EU 2007 2 6 07FDEA00262 1 20070203 A 5711 SPAR AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 OLD BLEND OUT REPAIR ON RT OUTER WING AT PANEL 3, BOTTOM SKIN, CLOSED TO RIB 28 ON REAR SPAR REPAIR WAS PERFORMED BY BLE ND OUT THE CORROSION WITH CAL EO AB 6-57-00-0001 AND APPROVED BY RAS/BAE/0573/2002 ISS. A 2 L 7 2 4F RT A35EU 2007020600048 20070206 00048 NM 2007 2 6 FDKA200701031 1 20070129 A 3350 1317 LAMP DHAV DHC8 DHC8101 2809002 NM EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 809LR 083 FDM 6181 JFK (0631 PHX LCL) FLOOR EMERGENCY LIGHT INOP AT ROW 8. MX REMOVED & REPLACED LAMP. 2 H 7 2 4T RT A13NM 2007020600049 20070206 00049 EA 2007 2 6 COMA0760116 1 20070131 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAP FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 806CA 10305 7359 FLIGHT 5375 - DURING YHZ APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. REPLACED THE RIGHT INBOARD FLAP - INBOARD ACTUA TOR. 2 L 7 2 4F RT A21EA 2007020600057 20070206 00057 EU 2007 2 6 07FDEA00265 1 20070203 A 5753 RIB AIRBUS 300 A300B4622R 3930312 EU TE FLAP CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 OLD REPAIR ON RT INNER FLAP RIB 25 CRACK FINDING (3, 5 INCHES) DURING SB A300-57-6098 EMBODIMENT REPAIR WAS PERFORMED WI TH CAL EO AB6-57-00-0063 AND APPROVED BY RAS/FOK/176/2004. 2 L 7 2 4F RT A35EU 2007020600091 20070206 00091 EA 2007 2 6 REXA200700025 1 20070203 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA FAILED A REXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 8694A 7694 FLAPS FAIL, SECOND OCCURANCE WITHIN 72 HOURS. 2 L 7 2 4F RT A21EA 2007020600097 20070206 00097 NM 2007 2 6 DL76G070063 1 20070129 A 4900 380029817 APU BOEING 767 7673P6 1385105 NM GE CF6 CF680C2* GL UNKNOWN A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 155DL 7706 P2793 25269 P2793 C HYD DEMAND DURING FLAP OPERATION, USING APU AIR, APU AIR FWD TO MCO 49-11-01C. CHECKED APU PRESS. PRESS SHOW 36PSI. RAN BOTH PACK PRESS OK. RAN ADP OPS OK. EXT RETRACT FLAPS NO MSG. MCO AND PLACARD REMOVED. 2 L 7 2 4F 4 F RT A1NM E23EA 2007020600108 20070206 00108 EA 2007 2 6 REXA200700030 1 20070203 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A REXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 8710A 7710 FLAP FAIL AT ZERO DEGREES, SECOND OCCURRENCE WITHIN 72 HOURS. 2 L 7 2 4F RT A21EA 2007020600110 20070206 00110 EA 2007 2 6 REXA200700032 1 20070203 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A REXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 8836A 7836 FLAPS FAIL. RESET PER AD 2006-12-21. 2 L 7 2 4F RT A21EA 2007020600111 20070206 00111 EA 2007 2 6 REXA200700033 1 20070203 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A REXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 8836A 7836 FLAPS FAIL, SECOND OCCURRENCE WITHIN 72 HOURS. 2 L 7 2 4F RT A21EA 2007020600114 20070206 00114 EU 2007 2 6 07FDEA00248 1 20070202 A 5210 DOOR AIRBUS 300 A300B4622R 3930312 EU UNKNOWN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 EXTERNAL DOUBLER ON FWD PAX DOOR RT SIDE LOWER EDGE REPAIR WAS PERFORMED IAW RAS 025042/011/2003. 2 L 7 2 4F RT A35EU 2007020600116 20070206 00116 EA 2007 2 6 SIMA200703603 1 20070202 A 2780 766359B PDU CNDAIR CL600 CL6002C10 1390015 EA SLAT SYS FAILED A SIMA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 511AE 9418 10107 SLAT FAIL MESSAGE ON APPROACH, EMERGENCY DECLARED. REMOVED AND REPLACED NUMBER 1 AND NUMBER 2 SLAT POWER DRIVE UNITS IA W CRJ AMM 27-81-37. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007020600126 20070206 00126 EA 2007 2 6 SWIA200717771 1 20070126 A 7120 YOKE CNDAIR CL600 CL6002C10 1390015 EA ENG MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 760SK 10223 UPPER LINK ON FWD ENG MOUNT YOKE SHOWS SIGNS OF CORROSION INCLUDING BUSHING. REMOVED AND REPLACED HARDWARE ON YOKE IAW TASK CARD RII 72-400-1000. 2 L 7 2 4F RT A21EA 2007020600129 20070206 00129 NM 2007 2 6 AWXA200700145 1 20070115 A 5320 69434562 FILLER BOEING 737 7373S3 1384711 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 MCN - CORROSION ON AFT CARGO COMPARTMENT DOOR CUT OUT REINFORCEMENT STRAP FILLER, BS 790, S25R, WL 153. REPLACED AFT CA RGO COMPARTMENT DOOR CUT OUT REINFORCEMENT STRAP FILLER, BS 790, S25R, WL 153 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600137 20070206 00137 NM 2007 2 6 AWXA200700153 1 20070130 A 5340 6935321 STRINGER CLIP BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FRAME CRACKED STRINGER CLIP, BS 597, S8L. REPLACED STRINGER CLIP, BS 597, S8L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600139 20070206 00139 NM 2007 2 6 AWXA200700155 1 20070130 A 5340 69353521 STRINGER CLIP BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED STRINGER CLIP, BS 685, S4L. REPLACED STRINGER CLIP, BS 685, S4L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600152 20070206 00152 NM 2007 2 6 AWXA200700168 1 20070121 A 5322 654654311 SHEAR TIE BOEING 737 73733A 1384673 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CORROSION ON FRAME SHEAR TIE, BS 967, S26L - S27L. REPLACED FRAME SHEAR TIE, BS 967, S26L - S27L IAW B737-3 00 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600154 20070206 00154 NM 2007 2 6 AWXA200700132 1 20070131 A 5347 D53112815202 SEAT TRACK AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 808AW 1088 PHX - CORROSION ON MAIN CABIN SEAT TRACK, FS 16, +Y765, AT THE FORWARD GALLEY ATTACH POINT. REPAIRED MAIN CABIN SEAT TR ACK, FR 16, +Y765, AT THE FORWARD GALLEY ATTACH POINT IAW A319 SRM 53-11-15 FIGURE 202. 2 L 7 2 4F RT A28NM 2007020600158 20070206 00158 NM 2007 2 6 AWXA200700170 1 20070123 A 5320 6545834551 INTERCOSTAL BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED INTERCOSTAL, BS 328, RBL 30, WL 208. REPLACED INTERCOSTAL, BS 328, RBL 30, WL 208 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020600161 20070206 00161 NM 2007 2 6 AWXA200700173 1 20070125 A 5321 D5361060500000 FLOOR PANEL AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 830AW 1565 SAL - MAJOR REPAIR - BC-4 CHECK - NR# 5896894, CORROSION ON MAIN CABIN FLOORBOARD 221FF, FS 16 - FS 20, +Y1292 TO +Y1732 . REPLACED MAIN CABIN FLOORBOARD 221FF, FR 16 - FR 20, +Y1292 TO +Y1732 IAW AWA TASK CARD C1D25306. 2 L 7 2 4F RT A28NM 2007020600162 20070206 00162 NM 2007 2 6 AWXA200700174 1 20070125 A 5321 D5367180500500 FLOOR PANEL AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 830AW 1565 SAL - FOUND CORROSION ON MAIN CABIN FLOORBOARD 262FF, FS 66 - FS 68, -Y1292 TO -Y1732. REPLACED MAIN CABIN FLOORBOARD 2 62FF, FS 66 - FS 68, -Y1292 TO -Y1732 IAW AWA TASK CARD C1D25306. 2 L 7 2 4F RT A28NM 2007020600163 20070206 00163 NM 2007 2 6 AWXA200700175 1 20070125 A 5751 65C2591117A SPAR BOEING 737 7373S3 1384711 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 MCN - LEFT WING AILERON FORWARD LOWER SPAR CRACKED, WS 446.620. REPAIRED LEFT WING AILERON FORWARD LOWER SPAR, WS 446.6 20 IAW AWA ER 03-5760-07035-TH2. 2 L 7 2 4F RT A16WE 2007020600170 20070206 00170 EA 2007 2 6 REXA200700041 1 20070204 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A REXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 8688C 7688 FLAPS FAIL AT ZERO DEGREES WHEN SELECTED TO 20 DEGREES. RESET PER AD 2006-12-21, SET TO MONITORING FOR 72 HOURS. 2 L 7 2 4F RT A21EA 2007020600181 20070206 00181 NM 2007 2 6 AT0700097 1 20070112 A 3350 8039251 BATTERY BOEING 717 717200 1383700 NM EMERGENCY LIGHTS FAILED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 926AT 55078 RIGHT ROW 1 THRU 10 EMERGENCY LIGHTS ON SEATS INOP G2 GALLERY EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTER Y PACK/POWER SUPPLY B5-118 IAW AMM 33-51-03 REF WDM 33-51-14, EMERGENCY LIGHTS OPS CHECK GOOD PER 33-51-00. 2 L 7 2 4F TR A6WE 2007020600185 20070206 00185 SO 2007 2 6 JBGA200700001 1 20070101 A 3040 1159SCB51025 WINDSHIELD GULSTM G1159 G1159 3953505 SO COCKPIT SPARKS E JBGA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 350 GOING INTO AIRPORT, PILOT NOTICED SPARKS DANCING AROUND PILOTS WINDSHIELD. ON THE GROUND MAINTENANCE FOUND WINDSHIELD DE LAMINATING, REMOVED AND REPLACED WINDSHIELD. 2 L 7 2 4F RT A12EA 2007020600194 20070206 00194 NM 2007 2 6 AALA20070137 1 20070119 A 3350 BULB BOEING 767 767223 1385123 NM EMERGENCY LIGHT SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 329AA 22329 JFK - SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 9AB TO 19AB INOPERATIVE. FOUND SEAT 19AB LIGHT BULBS SHORTED OUT CAUSING P OWER SUPPLY TO SHORT TO GROUND. RELAMPED EMERGENCY LIGHTS AT SEAT 19AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007020600207 20070206 00207 NM 2007 2 6 07FDEA00242 1 20070202 A 5713 STRINGER DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 CRACK FOUND (APPROX 3.5" LONG) DURING HFEC INSPECTION ON RIGHT WING TANK AT THE END OF UPPER STRINGER 10 (XORS 760). CRACK ON RIGHT HAND WING TANK AT THE END OF UPPER STRINGER 10 (XORS 760) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020600218 20070206 00218 NM 2007 2 6 AALA20070128 1 20070118 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY EXIT LIGHT AT LEFT FORWARD CORNER OF FORWARD COAT CLOSET DAMAGED. REPLACED EMERGENCY LIGHT ASSEMBLY AT LEFT FORWARD CORNER OF FORWARD COAT CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007020600220 20070206 00220 NE 2007 2 6 2007F00017 2 20070201 A 7250 VANE BOEING 737 737500 138449E NM CFE CFE73811B NE LP TURBINE CRACKED A K NONE O OTHER IN INSP/MAINT 1 EA 19 927UW 27123 NR 2 ENG WITH HIGH EGT, BEING INSPECTED DEFECTS WERE FOUND ON THE LPT, SEVERAL CRACKS ON 1 STAGE OF LPT. 3 BOROSCOPES WE RE PERFORMED AND NO CORRECTIVE ACTION DONE. 2 L 7 2 4F 4 F RT A16WE E44NE 2007020700006 20070207 00006 EA 2007 2 7 COMA0760121 1 20070129 A 2750 860D10018ABCD FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 721CA 8152 7259 FLIGHT 5524 - DURING ROC APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WIT HOUT INCIDENT. REPLACED THE FLAP CONTROL UNIT. 2 L 7 2 4F RT A21EA 2007020700010 20070207 00010 NM 2007 2 7 07FDEA00341 1 20070206 A 5344 HINGE DOUG MD11 MD11 3023602 NM CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 529FE 48624 AFT CARGO DOOR HINGE ASSY FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10- 00 FIG.14 VOL.I. OR IGINAL THK 0.340" MATERIAL REMOVED 0.035" REMAINING THK 0.305". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20- 50-02. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020700012 20070207 00012 NM 2007 2 7 07FDEA00343 1 20070206 A 5344 HINGE DOUG MD11 MD11 3023602 NM CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 529FE 48624 CENTER CARGO DOOR HINGE AT FUSELAGE AREA FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10-00 F IG. 14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.028" REMAINING THK 0.312". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020700019 20070207 00019 EU 2007 2 7 07FDEA00279 1 20070203 A 5320 A53973085210 SILL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 FOUND CORROSION SPOTS ON AFT CARGO DOOR SILL BEAM A539-73085-210 BETWEEN C 59-63 REPAIR WAS PERFORMED IAW RAS/DATLS/0003 479/2006 ISS.A (FLANGE REPAIR AND CORROSION REWORK), APPROVED BY EA 6-5317-103384. 2 L 7 2 4F RT A35EU 2007020700030 20070207 00030 NM 2007 2 7 07FDEA00291 1 20070203 A 5340 65453133 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 STRINGER CLIP HAS BEEN GROUND AT RADIUS CUT OUT BS 440 STR 1 BLENDED RADIUS ON STR CLIP REF SRM 53-10-4 PG 3. DAMAGE OU T OF LIMITS, REMOVED STR CLIP REF SRM 51-30-2 PG 2. VERIFY MATERIAL FOR FABRICATION OF NEW STR CLIP 7075-T6- .032 (A 02779) REF BOEING DWG 65-45313. FABRICATED NEW STR CLIP REF BOEING DWG 65- 45313 TREATED STR CLIP REF MM 51-20-21-7 PG 1-3. PRIMED STR CLIP REF MM 51-20-31-7 PGS 1-3. INSTALLED NEW STR CLIP REF SRM 51-30-02, PG 5-7 CLASSIFIED AS MAJOR R EPAIR. 2 L 7 3 4F RT A3WE 2007020700031 20070207 00031 NM 2007 2 7 07FDEA00292 1 20070203 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 STRINGER CLIP HAS BEEN GROUND AT THE RADIUS CUT OUT BS 440 STR 3L REMOVED STR CLIP STA 440 STR 3L. RECEIVED CLEARANCE A ND INSTALLED STR CLIP REF SRM 51-30-2 PG 1. CLASSIFIED AS MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007020700050 20070207 00050 NM 2007 2 7 07FDEA00311 1 20070205 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 RIGHT WING, OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION ON RIG HT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE HOLE REWORKED AND REPAIR CAR RIED OUT AS PER FEDEX E.A.1-5750-107782, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020700052 20070207 00052 NM 2007 2 7 07FDEA00313 1 20070205 A 5311 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 CABIN, LEFT STA 1641 BETWEEN LONGERON 12 TO LONGERON 14 FRAME FOUND DENT. CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTION AT 9,500 CYCLE S. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020700062 20070207 00062 NM 2007 2 7 SWAA070578 1 20070203 A 3350 307IBPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 797MX 27890 DURING SCHEDULED MV1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 11 ABC. REMOVED AND REPLACED LIGHT BULB PE R MM. 2 L 7 2 4F RT A16WE 2007020700071 20070207 00071 GL 2007 2 7 C2XA07IA024 2 20070204 A 7230 AE3001A1P FAN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL RT ENGINE FOD A C2XA O OTHER C Y J F.O.D. ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 SW 27 14905 10168 10168 145476 CAE311693 FLIGHT 2055, ON APPROACH, THE CREW REPORTED A BIRD STRIKE FOLLOWED BY AN UNCOMMANDED SHUTDOWN OF THE NR 2 ENGINE. THE AI RCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE, OPERATIONALLY CHECKED WITH NO DE FECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007020700077 20070207 00077 NM 2007 2 7 0700485802 1 20070205 A 3350 POWER SUPPLY BOEING 757 757351 1384991 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 582NW 32981 FORWARD EMERGENCY LIGHTS DO NOT ILLUMINATE, DOOR 1L SLIDE LIGHT (EXTERNAL), AND ROWS 1, 2, AND 3 SEAT LIGHTS. REMOVED AN D REPLACED POWER SUPPLY IAW AMM 33-51-07, OPS CHECKS GOOD. 2 L 7 2 4F RT A2NM 2007020700081 20070207 00081 NM 2007 2 7 SWAA070565 1 20070202 A 5311 6546525 FRAME BOEING 737 7373Q8 1384670 NM BS 380 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020700090 20070207 00090 NM 2007 2 7 SWAA070560 1 20070202 A 5210 6550570 SKIN BOEING 737 7373H4 1384600 NM L2 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER AFT RADIUS CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007020700092 20070207 00092 NM 2007 2 7 SWAA070585 1 20070203 A 5754 65C22602 SKIN BOEING 737 7373H4 1384600 NM NR 4 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING NR 4 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED L/E SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007020700098 20070207 00098 NM 2007 2 7 SWAA070575 1 20070202 A 3350 OL307IBPEGL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 789SW 29816 DURING SCHEDULED MV3 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 19 ABC. REMOVED AND REPLACED LIGHT BULB PE R MM. 2 L 7 2 4F RT A16WE 2007020700117 20070207 00117 EU 2007 2 7 2007UALA00218 2 20070128 A 7230 BLADES BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 ENGINE DAMAGED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING C F.O.D. CL CLIMB 1 WP 29 330UA 24191 723233 RTFL DUE TO A BIRD STRIKE IN THE NR 1 ENGINE. BLADES BENT AND DAMAGED. :REPLACED FAN BLADES PER MM 72-21-04. NR 1 ENGI NE WAS NOT SHUT DOWN UNTIL ON GROUND. 2 L 7 2 4F 4 F RT A16WE E21EU 2007020700121 20070207 00121 NM 2007 2 7 2007UALA00222 1 20070127 A 2432 CHARGER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 BATTERY FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 828UA 1031 BATTERY 2 FAULT ON GROUND. REPLACED NR 2 BATTERY AND BATTERY CHARGER. BATTERY OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007020700125 20070207 00125 SO 2007 2 7 RAIA00701041 1 20070131 A 3350 100865 POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 830HK 145313 PRE FLT NR 5587 - STL - EMERGENCY LIGHTS OUT AT MAIN DOOR, FORWARD CEILING AND FORWARD AISLE FLOOR PROXIMITY LIGHTS. MA INTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY. 2 L 7 2 4T RT T00011AT 2007020700126 20070207 00126 SO 2007 2 7 RAIA0070201 1 20070201 A 7830 UNKNOWN EMB 145 EMB145LR 3260212 SO UNKNOWN A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 850HK 145003 FLT NR 8003 - DAY - ENG 1 THRUST REVERSER DISAGREE MESSAGE ON TAKEOFF ROLL ON EICAS. MAINTENANCE DEFERRED THE NR 1 ENGI NE THRUST REVERSER. 2 L 7 2 4T RT T00011AT 2007020700135 20070207 00135 NM 2007 2 7 AALA20070155 1 20070121 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 938AN 29533 MIA - EMERGENCY LIGHT AT SEAT 11A INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 11A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007020700140 20070207 00140 NM 2007 2 7 AWXA200700139 1 20070117 A 5753 6546486130 WEDGE BOEING 737 73733A 1384673 NM ZONE 600 DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND RIGHT WING INBOARD MID FLAP, LOWER SURFACE TRAILING EDGE WEDGE DELAMINATED, WS 116.8 - WS 124.0. REPAIRED R IGHT WING INBOARD MID FLAP, LOWER SURFACE TRAILING EDGE WEDGE, WS 116.8 - WS 124.0 IAW B737-300 SRM 51-70-10-2R4, REPAIR NR 4, FIGURE 202. 2 L 7 2 4F RT A16WE 2007020700149 20070207 00149 WP 2007 2 7 UPS07849075 1 20070103 A 5310 575514956 WINDOW FRAME DOUG DC8 DC871F 302199D WP FS 117 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C2 RIGHT & LEFT WINDOW FRAME Z-ANGLES (CENTER WINDSHIELD) ARE CORRODED AND PITTED. REPAIRED CENTER WIND SHIELD Z-ANGLE IAW SAA EA 008-5310-01-A0570 UPS EO DC8-5310-25945-A, BAC MSG 1-269510850, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007020700151 20070207 00151 WP 2007 2 7 UPS07849092 1 20070131 A 3350 RELAY DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTT BATTERY/RELAY UNIT. NOW OPS OK. REF 33-50-01-2. 2 L 7 4 4F RT 4A25 2007020700162 20070207 00162 NM 2007 2 7 UPS07449079 1 20070111 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C AFT CARGO COMPT - LEFT FLOORBEAM LOWER SURFACE FOUND SURFACE CORROSION AT STA 1820 LBL 42 TO LBL 45 AN CHOR NUT AREA. CORROSION BLEND OUT 0.041 X 2 X 3 INCHES EXCEED SRM LIMIT. AFT CARGO COMPT - LEFT FLOORBEAM REPAIRED AT BS 1820 LBL 20 TO LEFT MOST O/B AS PER SRM 51-40-04 FIG 2. 2 L 7 4 4F RT A20WE 2007020700166 20070207 00166 NM 2007 2 7 UPS07449083 1 20070115 A 5313 STRINGER BOEING 747 747123 1384873 NM BS 1920-1940 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D AFTER BS 1920 TO BS 1940 RIGHT WINDOW FORGING REMOVED, STR 22R FOUND CORROSION AS MARKED. CORROSI ON BLEND OUT 0.040 X .5 X 3 INCHES EXCEED SRM LIMIT. M/D BS 1740-1960 STR 22R STRINGER REPLACED AND INSTALLED AS PER SR M 51-10-01 AND 51-30-02 REFER NRC51873 FOR WORKING DETAIL AFTER COR BLENDED. ORIGINAL THICKNESS 0.104 INCH. 2 L 7 4 4F A20WE 2007020700176 20070207 00176 NM 2007 2 7 ZZDA070123105 1 20070123 A 5311 FRAME BOEING 717 717200 1383700 NM BS 83 CRACKED A ZZDA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. LEFT SIDE FRAME AT STA 83.0 CRACKED AND BENT BEYOND REPAIR. REPLACED LE FT SIDE FRAME AT STA 83.0 PER MDC DRAWING 9911505 REV AN DATED 8/20/99. 2 L 7 2 4F TR A6WE 2007020700194 20070207 00194 NM 2007 2 7 DU4R2007040 1 20070127 A 5320 654N02441033 PANEL BOEING 757 757232 1384965 NM BS 1445-1530 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 FOUND CORROSION AFT CARGO BS 1445.6 TO BS 1530 LT TRANSITION SIDE PANEL CORROSION ON GILL LINER ATTACH AREA AND FLOOR PA NEL ATTACH AREA. FABRICATED AND INSTALLED SPLICE PLATE 4" BY 6" BY 12" AND TRANSITION PANEL 654N0244-1033 (SEE ROUTINE 3770) IAW B757 SRM 51-10-02 AND 51-40-05 FIG 3, AMM 53-88-01-801. 2 L 7 2 4F RT A2NM 2007020700195 20070207 00195 NM 2007 2 7 DU4R2007041 1 20070127 A 5320 654N02441033 PANEL BOEING 757 757232 1384965 NM BS 620-645 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 FWD CARGO COMPT RT TRANSITION PANEL HAS SURFACE CORROSION FROM BS 620 TO BS 645. CORROSION ON UPPER SURFACE AND AROUND FASTENER HOLES. ROUTED OUT CORROSION. FABRICATED AND INSTALLED DOUBLER 18" BY 8" FROM 7075-T6 .071" AND FILLERS FROM 2 024-T3 .063" IAW B757 AMM 53-88-01-801. 2 L 7 2 4F RT A2NM 2007020700197 20070207 00197 NM 2007 2 7 ZZDA070123111 1 20070123 A 5311 FRAME BOEING 717 717200 1383700 NM BS 120 DAMAGED A ZZDA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. LOWER FRAME AT STA 120.0 DAMAGED. REPAIRED LOWER FRAME AT STA 120.0 PER MDC DRAWING 9911510 REV M DATED 7/13/00 AND PER BOEING ENGINEERING ROD/SKETCH NUMBER 06-12-10-004, 8100-9 APPROVED ON 0 1-07-07. 2 L 7 2 4F TR A6WE 2007020700200 20070207 00200 NM 2007 2 7 ZZDA070123114 1 20070131 A 5330 SKIN BOEING 717 717200 1383700 NM BS 212 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 910AT 55086 DENT ON RIGHT SIDE OF FUSELAGE AFT OF R1 DOOR STA 212 53-00-01 REPAIR 2. INSTALLED DOUBLER REPAIR AT RIGHT SIDE OF FUSE LAGE AFT OF R1 DOOR STA 212 AS PER B717 SRM. 2 L 7 2 4F TR A6WE 2007020700201 20070207 00201 NM 2007 2 7 ZZDA070123115 1 20070131 A 5330 SKIN BOEING 717 717200 1383700 NM BS 218-246 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 910AT 55086 DENT APPROX 6 INCHES UP FROM L18 AND 8 INCHES AFT OF STA 218. INSTALLED DOUBLER REPAIR STA 218 TO STA 246 AS PER B717 S RM 53-00-01 REPAIR NR 6. 2 L 7 2 4F TR A6WE 2007020700202 20070207 00202 NM 2007 2 7 ZZDA070123116 1 20070130 A 5330 SKIN BOEING 717 717200 1383700 NM BS 237 L24R DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 910AT 55086 DENT FOUND ON LWR FUSELAGE RIGHT SIDE AFT OF FWD DRAIN MAST. INSTALLED DOUBLER REPAIR AT RIGHT SIDE AFT OF FWD DRAIN MA ST AS PER B717 SRM 53-00-01 FIG 204. 2 L 7 2 4F TR A6WE 2007020800001 20070208 00001 NM 2007 2 8 SWAA070618 1 20070206 A 3350 101331 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 459WN 32497 LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007020800003 20070208 00003 NM 2007 2 8 SWAA070632 1 20070206 A 5330 6545774 SKIN BOEING 737 737317 138447P NM BS 787 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007020800005 20070208 00005 EU 2007 2 8 0700493302 1 20070203 A 3350 EPSU AIRBUS 330 A330323 3930335 EU EMERGENCY LIGHTS FAILED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 802NW 533 EPSU (18WL) DOOR 4 FAILED EPSU BATTERY CAPACITY TEST. REMOVED AND REPLACED EPSU AND TESTED OK. 2 L 7 2 4F RT A46NM 2007020800006 20070208 00006 NM 2007 2 8 UPS07449088 1 20070111 A 5340 65B091912 FITTING BOEING 747 747123 1384873 NM BS 980 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT AFT FIXED STOP SUPPORT FITTING LOWER SURFACE FOUND CRACK AT STA 980 LBL 45. CRACK LEN GTH 4 INCHES. FWD CARGO COMPT BS 980 LBL 45 AFT FIXED STOP SUPPORT FITTING REPLACED AND INSTALLED AS PER SRM 51-10-01 P G 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007020800019 20070208 00019 EA 2007 2 8 TRAX200700159 1 20070203 A 5260 HANDLE CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 ASD OUTER HANDLE CRACKED IN RADIUS (MARKED). REMOVED DOOR HANDLE AND TRANSFERED HARDWARE (NOT SAFTIED). PER AMM 52-11-0 0PRIMED AND PAINTED NEW OUTER PAX DOOR HANDLE PER CRJ 700 SRM 51-21-16. SAFTIED HARDWARE PER CRJ 700 AMM 20-00-00 OK TO INSTALL OUTER PAX DOOR HANDLE INSTALLD NEW OUTER PAX DOOR HANDLE PER CRJ 700 AMM 52-11-00. 2 L 7 2 4F RT A21EA 2007020800020 20070208 00020 EA 2007 2 8 TRAX200700160 1 20070203 A 7830 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSERS UNKNOWN A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 924EV 7830 RIGHT REV UNLOCK MSG IN FLIGHT AT FL260. EN ROUTE TO ATL A/C DIVERTED TO MDT DUE TO MTC EMERGENCY DECLARED. (THRUST RE VERSER SYSTEMS). 2 L 7 2 4F RT A21EA 2007020900004 20070209 00004 NM 2007 2 9 SWAA070631 1 20070206 A 5753 6546435333 SKIN BOEING 737 7373H4 1384600 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED C3 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED LOWER INBOARD END. REMOVED AND REPLACED AF T FLAP PER MM. 2 L 7 2 4F RT A16WE 2007020900007 20070209 00007 NM 2007 2 9 AMTA200700049 1 20070201 A 3600 3964801 VALVE BOEING 757 75723N 1384973 NM RT BLEED SYS UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 517AT 27973 EICAS MSG R ENG BLEED OFF DISPLAYED R ENG BLEED OFF LIGHT ILLUMINATED, CUICT PRESS NO RM 2119Z. REMOVED AND REPLACED FL OW CONTROL AND SHUTOFF VALVE PER AMM 21-51-01-2. RAN ENGINE, OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A2NM 2007020900010 20070209 00010 NM 2007 2 9 SWAA070620 1 20070206 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 847 S27R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 847, STR 27R. REMOVED AND REPLACED SHEAR TIE PER ACO. 2 L 7 2 4F RT A16WE 2007020900011 20070209 00011 NM 2007 2 9 SWAA070624 1 20070206 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 807 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020900013 20070209 00013 NM 2007 2 9 SWAA070628 1 20070206 A 5310 6546956 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 400-420 S17R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 400 TO BS 420 STR 17R. REMOVED AND REPLACED CREASE BEA M WEB PER SRM. 2 L 7 2 4F RT A16WE 2007020900015 20070209 00015 NM 2007 2 9 SWAA070630 1 20070206 A 5523 65C26384 SKIN BOEING 737 7373H4 1384600 NM ELEVATOR TAB DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED 12Y CHECK, FOUND LEFT ELEVATOR TAB DELAMINATED LOWER END. REPAIRED TAB PER SRM. 2 L 7 2 4F RT A16WE 2007020900016 20070209 00016 NM 2007 2 9 SWAA070626 1 20070206 A 3350 CONNECTOR BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT ASSY CONNECTOR CORRODED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007020900017 20070209 00017 NM 2007 2 9 SWAA070621 1 20070206 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 277 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007020900018 20070209 00018 NM 2007 2 9 SWAA070619 1 20070206 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 294 S13L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007020900019 20070209 00019 NM 2007 2 9 SWAA070627 1 20070206 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 388 S2L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 2L. REMOVED AND REPLACED RT STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 2007020900020 20070209 00020 NM 2007 2 9 SWAA070633 1 20070206 A 5313 BAC1498 STRINGER BOEING 737 7373T5 1384608 NM BS 932 S24R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND STRINGER 24R CORRODED AT BS 932. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007020900021 20070209 00021 2007 2 9 SWAA070629 4 20070206 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007020900022 20070209 00022 NM 2007 2 9 SWAA070638 1 20070206 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 764SW 27878 DURING SCHEDULED MV2 CHECK, FWD CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007020900028 20070209 00028 EA 2007 2 9 COMA0760134 1 20070204 A 2752 853D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 01 479CA 11480 7675 FLIGHT 5390 - DURING JFK APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WIT HOUT INCIDENT. REPLACED THE LEFT OUTBOARD FLAP INBOARD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2007020900029 20070209 00029 EA 2007 2 9 COMA0760136 1 20070205 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 917CA 7017 FLIGHT 5244 - DURING PIT APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WIT HOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007020900030 20070209 00030 EA 2007 2 9 COMA0760137 1 20070205 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 938CA 7046 FLIGHT 5503 - DURING BOS APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAG E -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007020900031 20070209 00031 EA 2007 2 9 COMA0760138 1 20070205 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 587CA 7062 FLIGHT 5659 - DURING MDW APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WIT HOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007020900032 20070209 00032 EA 2007 2 9 COMA0760139 1 20070205 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 966CA 7132 FLIGHT 5464 - DURING JFK APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WIT HOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007020900034 20070209 00034 NM 2007 2 9 WRLA2007018 1 20070128 A 5320 ADA852010 FLOOR SUPPORT DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE ZONE 100 BROKEN A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 41081 48632 DURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND FWD CARGO COMPARTMENT FLOOR PANEL SUPPORT BRACKET AT STA Y=879, RT. FABRI CATE THE NEW PARTS IAW E1 NR W2007P53B-057 REV.00 AND APPROVED DOCUMENT MFG CONTROL NR PO209353. INSTALLED THE NEW FAB RICATED PARTS IAW MD-11F SRM VOL.II 51-35-01 REV.38. CONDITION CHECK NORMAL.(EGAT NRC NO.U05109). 2 L 7 3 4F 4 F RT A22WE E24NE 2007020900035 20070209 00035 NM 2007 2 9 WRLA2007 1 20070204 A 5315 AEA03971 FLOORBEAM DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE ZONE 100 CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 41081 48632 DURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND M/D CARGO FLOORBEAM CORRODED AT STA Y=1321,X= -8 TO -25 AREA. FABRICATED THE NEW PARTS IAW E1 NR W2007P53B-056 REV. 00 AND APPROVED DOCUMENT MFG CONTROL NR PO209366. INSTALLED THE NEW FABRICATE D PARTS IAW MD-11F SRM VOL II 51-35-01 REV.38. APPLY CHEMICAL PROTECTIVE COATINGS AND CONDITION CHECK NORMAL. EGAT NRC N R U05094. 2 L 7 3 4F 4 F RT A22WE E24NE 2007020900037 20070209 00037 EA 2007 2 9 COMA0760146 1 20070205 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 436CA 7482 FLIGHT 5516 - DURING DESCENT INTO JFK RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007020900039 20070209 00039 EA 2007 2 9 COMA0760147 1 20070206 A 3010 ANTI-ICE SYSTEM CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 914CA 7012 FLIGHT 5561 - EN ROUTE LEX-CVG RECEIVED AN ANTI-ICE DUCT WARNING MESSAGE, FLIGHT DIVERTED TO BNA DUE TO INCLEMENT WEATHE R. PERFORMED ENGINE RUNS AND OPERATIONAL CHECK OF THE WING ANTI-ICE CONTROL INDICATION SYSTEM. UNABLE TO DUPLICATE DIS CREPANCY. 2 L 7 2 4F RT A21EA 2007020900043 20070209 00043 NM 2007 2 9 AWXA200700184 1 20070122 A 5320 654797321 SHEAR WEB BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - SHEAR WEB CRACKED, BS 616 - BS 639, S17L. REPAIRED SHEAR WEB, BS 616 - BS 639, S17L IAW B737-300 SRM 51-70-13. 2 L 7 2 4F RT A16WE 2007020900050 20070209 00050 EA 2007 2 9 COMA0760141 1 20070205 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 720SW 7297 FLIGHT 5304 - DURING DCA APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WI THOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007020900051 20070209 00051 EA 2007 2 9 COMA0760142 1 20070205 A 2741 TRIM MOTOR CNDAIR CL600 CL6002B19 1900309 EA FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 798CA 7348 FLIGHT 5524 - EN ROUTE CMH-JFK RECEIVED A STAB AND MACH TRIM CAUTION MESSAGE, STAB TRIM FAILED TO RESET. CREW DECLARED AN EMERGENCY AND RETURNED TO CMH. FLIGHT LANDED WITHOUT INCIDENT. PERFORMED STAB AND MACH TRIM RESET, OPERATIONAL CHE CK SATISFACTORY. 2 L 7 2 4F RT A21EA 2007020900052 20070209 00052 EA 2007 2 9 COMA0760143 1 20070205 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 804CA 7352 FLIGHT 5580 - DURING BOS APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WI THOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007020900053 20070209 00053 EA 2007 2 9 COMA0760144 1 20070205 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 811CA 15675 7380 FLIGHT 5640 - DURING LAN APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. REPLACED THE LEFT BRAKE POSITION SETTING UNIT. 2 L 7 2 4F RT A21EA 2007020900054 20070209 00054 NM 2007 2 9 DXTA200701896 1 20070131 A 2730 UNKNOWN GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE ELEVATOR FEEL UNKNOWN E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 720QS 085 ELEVATOR FEEL FAIL LIGHT CAME ON IN CLIMBOUT. REMAINED ON, THE ENTIRE FLIGHT. UPON A/C ARRIVAL VERIFIED DISCREPANCY AN D NOTED THAT THE SPQC WAS NOT FULLY INSTALLED IN RACK, RERACKED SPQC AND MESSAGE EXTINGUISHED. PERFORMED A SPQC DOWNLOA D AND OPS CHECK WITH NO FURTHER DEFECTS NOTED. COPIED DOWNLOADED INFORMATION TO DISK. ALL WORK PERFORMED IAW WATCH SPQ C TOOL KIT USERS GUIDE D9520200 REV B. 2 L 7 2 4F 4 F RT A53NM E35NE 2007020900056 20070209 00056 SO 2007 2 9 C2XA07CL021 1 20070207 A 3231 355022002MOD2 CONTROL UNIT EMB 145 EMB145EP 3260221 SO MLG FAULTY A C2XA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 27 14933 20095 145018 CLE FLIGHT 2727 THE CREW REPORTED LOUD NOISE AND VIBRATION FROM FRONT OF AIRPLANE. THE GEAR WAS RECYCLED AND THE NOISE WENT AWAY. MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR DOORS STAYING OPEN. THE LGEU WAS REPLACED AND OPERATIONAL CHE CKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2007020900057 20070209 00057 NM 2007 2 9 07FDEA00363 1 20070207 A 5347 SEAT TRACK BOEING 727 727233 138408A NM BS 380-400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 MAIN DECK FLOOR SEAT TRACK I/B FLANGE IS CORRODED BS 380-400, LBL 44, WL208 BLENDED CORROSION, ACCOMPLISHED HFEC NO DEF ECTS NOTED. FLAP PEENED ALL BLENDED AREAS. ALODINED AND PRIMED, AS NEEDED REF EA NR 7-5310-108847 A. 2 L 7 3 4F RT A3WE 2007020900060 20070209 00060 NM 2007 2 9 EIA2007004 1 20070119 A 3350 13561337 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 FOUND UPPER DECK STAIR EMERGENCY LIGHT INOP. PART ORDERED FOR REPLACEMENT. REPLACED EMERGENCY LIGHT ASSY. OPS CHK OK PER 33-51-00. 2 L 7 4 4F A20WE 2007020900061 20070209 00061 NE 2007 2 9 EIA2007005 2 20070122 A 7261 308031 PLUG BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE ENGINE DRAIN LEAKING A EIAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 09 485EV 20712 662567 FLT 906, STATION PVG, "IN FIGHT SHUTDOWN OF NR 1 ENGINE, NO OIL QTY, OR PRESSURE." ON CLIMB-OUT THROUGH FL 310, F/E NOTE D OIL QTY DECREASING AND PRESS FLUX CONTACTED DISPATCH AND WAS DIRECTED TO RETURN TO PVG FOR MX. MX FOUND "NR 1 ENGINE GEAR BOX CHIP DETECTOR THREADED BORE THREADS DAMAGED." AIRCRAFT FERRY TO SINGAPORE FOR ENGINE CHANGE. REPLACED NR 1 EN GINE PER MM 72-00-00 AND ASSOC WORKCARDS. 2 L 7 4 4F 4 F A20WE E20EA 2007020900062 20070209 00062 2007 2 9 DXTA200701915 4 20070206 A 2200 MOTOR GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE AUTOPILOT MALFUNCTIONED E DXTA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 GL 07 706QS 131 AUTO PILOT DISENGAGES ON APPROACH IN ALL MODES AND DURING TURNS. ALSO, IN STRAIGHT FLIGHT, YOKE JERKS RT AND LT ROUTINEL Y ABOVE MACH .78. FOUND THE RUDDER SERVO MOTOR, AUTOPILOT TO BE FAULTY. REMOVED AND REPLACED THE AUTOPILOT RUDDER SERV O MOTOR WITH AN OVERHAULED SERVO IAW G200 CMP 221008. COMPLIED WITH THE AUTOPILOT FLIGHT DIRECTOR FUNCTIONAL TEST IAW G 200 CMP 224010 WITH NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A53NM E35NE 2007020900063 20070209 00063 NM 2007 2 9 DXTA200701916 1 20070206 A 3150 UNKNOWN AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE MASTER WARNING UNKNOWN E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 218QS 118 ON TAKEOFF, MASTER WARNING T/O CONFIG CAME ON ALL CONFIG ITEMS CHECKED AND RESET T/O CONFIG LIGHT STILL COMES ON. ABORT ED TAKEOFF. WITH BSCU NR 1 RESET, T/O WARNING SYSTEM OPS CHECK GOOD. BSCU BELIEVED TO BE THE CAUSE OF "T/O CONFIG" ANN . TAKE-OFF WARNING SYSTEM OFF WARNING SYSTEM OPS CHECK GOOD AT THIS TIME IAW F-2000 31-300 & 31-300. 2 K 7 2 4F 4 F RT A50NM E44NE 2007020900066 20070209 00066 2007 2 9 ASAA0741443 4 20070206 A 2565 CABLE AIRCRUISERS BOEING 737 7374Q8 138447Q NM ESCAPE SLIDE MISROUTED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 02 784AS 1409A 28199 EVAC SLIDE NEW FROM STOCK INFLATION CABLE MISROUTED AT GIRT FROM MANUFACTURES OVERAHUL. REROUTED INFLATION CABLE PRIOR TO INSTALLATION. 2 L 7 2 4F RT A16WE 2007020900067 20070209 00067 EU 2007 2 9 COEA0701914 1 20070105 A 3234 F96GA0102 CONTROL LEVER AEROSP ATR42 ATR42300 8680920 EU MLG MALFUNCTIONED E COEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 13 914FX 293 AIR TURN BACK YVR, AFTER DEPARTURE LANDING GEAR SELECTED UP AND RECEIVED THREE GREEN AND RED INDICATIONS ON BOTH PRIMARY AND SECONDARY INDICATIONS. CYCLED THE GEAR SELECTOR WITH THE SAME RESULTS. AN EMERGENCY WAS DECLARED AND AIRCRAFT RET URNED TO THE AIRFIELD. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEV ER. THE LANDING GEAR SELECTOR VALVE WAS REPLACED AS A PRECAUTION. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2007020900068 20070209 00068 NM 2007 2 9 EIA2007006 1 20070123 A 3350 900835A BATTERY PACK BOEING 747 747230B 1384889 NM EMERGENCY LIGHT INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487EV 23286 LT CREW SERVICE DOOR UPPER JAMB EMERGENCY LIGHT DOES NOT REMAIN LIGHTED WITH EMERGENCY LIGHT SW ON. REPLACED BATTERY PA CK, OPS CHECK NORMAL PER MM 33-55-00. 2 L 7 4 4F A20WE 2007020900069 20070209 00069 EA 2007 2 9 A6WA200740031 1 20070112 A 2400 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A A6WA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 GL 31 466AW 7899 AT TAKEOFF UNDER 80 KNOTS, RED WARNING IDG MESSAGE FOLLOWED BY GEN 2 CAUTION MESSAGE BRAKE TEMPS NR 1 AND 2 AT 4, NR 3 A T 6, AND NR 4 AT 4. SERVICED OIL ON IDG NR 2 IAW AMM 12-13-24. OPS CHECK GOOD. ALL PARAMETER DO NOT REQUIRE REJECTED TAKEOFF INSPECTION IAW AMM 05-51-27-601. (M) 2 L 7 2 4F RT A21EA 2007020900070 20070209 00070 CE 2007 2 9 DJFA2007016 1 20070205 A 2130 CHECK VALVE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP CABIN PRESSURE MISALIGNED E DJFA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 23 831LX 258510 TRIP NR 1128608, CREW REPORTED, WHILE CLIMBING THROUGH FL320 RECEIVED (CABIN ALTITUDE) WARNING. CABIN ALTITUDE WAS AT 1 2,000 AND CLIMBING. CREW DONNED O2 MASKS AND REQUESTED EMERGENCY DESCENT TO FL100; PAX MASK WERE DEPLOYED AUTOMATICALLY . AIRCRAFT DIVERTED. MAINTENANCE FOUND THE SILENCER DUCT, WATER SEPARATOR DUCT, AND CABIN PRESSURIZATION CHECK VALVE D UCT MISALIGNED. ALSO FOUND UPPER SILENCER DUCT DENTED AND NOT VIABLE TO CREATE A GOOD SEALING SURFACE FOR DUCT SLEEVE T O BRIDGE THE SILENCER DUCT TO THE WATER SEPARATOR. THE DENTED DUCT WAS REPLACED AND THE OTHERS REALIGNED AND REBLOCKED. SYSTEM CHECKS WERE SATISFACTORY. 2 L 7 2 4F 4 F RT A3EU E6WE 2007020900071 20070209 00071 WP 2007 2 9 07FDEA00364 1 20070207 A 5755 SKIN DOUG DC10 DC1030 3023501 WP SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 313FE 48311 LT WING NR 3 SPOILER UPPER SURFACE AREA HAS APPROX 19 INDENTATIONS/PUNCTURES, POSSIBLY LIGHTING STRIKES IN A GROUPED ARE A CENTER OF SPOILER. REPAIRED NR 3 SPOILER UPPER SURFACE AREA BY REMOVING DAMAGED SECTION OF SKIN, DOUBLER AND CORE. F ABRICATED AND BONDED NEW CORE, DOUBLERS AND SKIN IAW DC/MD 10-30 SRM 51-71-00 VOL II SEALED REPAIR IAW DC 10/MD10-30 SRM 51-71-00 VOL II. 2 L 7 3 4F A22WE 2007020900072 20070209 00072 NM 2007 2 9 EIA2007010 1 20070205 A 5330 SKIN PANEL BOEING 747 747212B 1384886 NM BS 2360 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 DURING CHECK, FOUND LIFTING FUSELAGE SKIN WITH DIMPLED SKIN AROUND FASTENERS, L/E SKIN BS 2360 BETWEEN STR 23L AND 35L. REMOVED CORROSION, REMOVED DAMAGED SKIN, NDT AREA, FABBED AND INSTALLED REPAIR PER BSRM 53-30-30 FIG 47. 2 L 7 4 4F A20WE 2007020900073 20070209 00073 SO 2007 2 9 RAIA00702005 1 20070204 A 5610 WINDOW EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 832HK 145771 FLT NR 8024 - PVD - FO DV WINDOW WOULD NOT COMPLETELY CLOSE, ABORTED T/O AT 40-50KTS. MAINTENANCE INSPECTED THE WINDOW AREA FOR POSIBLE DEBRIS. INSPECTED WINDOW AND ASSOCIATED LINK. NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2007020900074 20070209 00074 SO 2007 2 9 RAIA00702004 1 20070203 A 5210 ROLLER EMB 145 EMB145ER 3260211 SO PAX DOOR OUT OF ADJUST A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 808HK 145157 POST FLT NR 8052 - ORD - MAIN CABIN DOOR WOULD NOT OPEN. MAINTENANCE ADJUSTED INNER DOOR HANDLE ROLLER. DOOR CHECKED G OOD AFTERWARDS. 2 L 7 2 4F RT T00011AT 2007021200001 20070212 00001 NM 2007 2 12 UPS07449127 1 20070206 A 3350 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 EMERGENCY LIGHT MODULE M306 INOP. LOCATED AT UPPER DECK STA 590. ITEM DEFERRED REFERENCE M343595. REPOSITIONED CEILIN G PANEL TO CORRECT PANEL POSITION. OPS CHECKED GOOD. THIS CLEARS M343595. 2 L 7 4 4F A20WE 2007021200003 20070212 00003 WP 2007 2 12 UPS07849119 1 20070105 A 5320 97558061 CUSP WEB DOUG DC8 DC871F 302199D WP FS 1100-1140 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 MAIN CABIN CUSP HAS HEAVY CORROSION AT STA 1120 LT AROUND FITTING. REPAIRED LT CUSP/SKIN AT STA 1100 -1140 IAW RAA DC8-53-20608. 2 L 7 4 4F RT 4A25 2007021200005 20070212 00005 NE 2007 2 12 DJFA2007015 2 20070205 A 7320 HMU BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE LT ENGINE MALFUNCTIONED E DJFA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 23 755TA RK324 PCEJA0777 TRIP NR 1136187, CREW REPORTED WHILE CLIMBING THROUGH FL260 THEY NOTICED A YAW OF THE AIRCRAFT AND DISCOVERED THE LT ENG INE HAD ROLLED BACK TO 62 PERCENT N1. THEY TURNED THE ENGINE ANTI-ICE ON AND TURNED THE EEC OFF AND PUSHED THROTTLES FO RWARD WITH NO IMPROVEMENT IN PERFORMANCE. ALL OTHER ENGINE INDICATIONS WERE CONSISTENT WITH 62 PERCENT N1. AIRCRAFT DI VERTED. MAINTENANCE WAS ABLE TO DUPLICATE THE DISCREPANCY ON ENGINE RUNS THEY WERE UNABLE TO EXCEED 57 PERCENT N1. MAI NTENANCE REPLACED THE NR 1 HMU. 2 H 7 2 4F 4 F RT A16SW E25EA 2007021200006 20070212 00006 NM 2007 2 12 07FDEA00061 1 20070109 A 5713 ARB75401 STRINGER DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 DURING HFEC INSPECTION, CRACK FOUND AT STRINGER END-40 (XORS 747) INSIDE LT WING TANK. REPAIR CARRIED OUT AT STRINGER E ND-40 (XORS 747) INSIDE LT WING TANK AS PER FEDEX EA NR 1-5720-105598, TITLE: "WINGS-STRINGER 40 LEFT CRACK AT WING STAT ION XORS = 747 - REPAIR". REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007021200007 20070212 00007 NM 2007 2 12 QXEA200700141 1 20070207 A 2760 ARM BOMBDR DHC8 DHC8402 1390042 NM SPOILER ROLLER LOCKED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 412QX 4059 SEA FLIGHT NR 2476: SPOILER OUTBOARD, ROLL SPOILER INBOARD HYD AND ROLL SPOILER OUTBOARD HYD CAUTION LIGHTS ILLUMINATED. MAINTENANCE PERFORMED GVI OF ROLL SPOILER CABLE SENSOR ASSY IAW Q400 AMM TASK 27-61-00-210-801 AND FOUND THE ROLLER AR M IN THE LATCHED POSITION. UNLATCHED ROLLER ARM IAW Q400 AMM TASK 27-61-41-400-801, PAGE 405, STEP 4 A (1)NOTE. C/W OP S CHECK OF THE ROLL SPOILER CABLE SENSOR ASSY IAW Q400 AMM TASK 27-61-00-710-805. OPS CHECK GOOD. C/W OPS CHECK OF THE ROLL SPOILER SYSTEM IAW Q400 AMM TASK 27-61-00-710-801. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERV ICE. 2 H 7 2 4T RT A13NM 2007021200012 20070212 00012 EA 2007 2 12 VNAA0701007 1 20070124 A 2150 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE A/C PACK UNKNOWN A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 05 709PS 10165 CREW REPORTED THE RIGHT HAND PACK CYCLED ON/OFF MULTIPLE TIMES AFTER TAKEOFF. CREW RETURNED TO CLT AND LANDED WITHOUT I NCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE RIGHT HAND PACK IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE M ANUAL 21-51-00-710-801. NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007021200013 20070212 00013 EA 2007 2 12 VNAA0701008 1 20070124 A 2750 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS UNKNOWN A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 250PS 7929 CREW REPORTED A FLAPS FAIL AT 20 DEGREES MESSAGE AFTER TAKEOFF. CREW RETURNED TO DCA AND LANDED WITHOUT INCIDENT. MAIN TENANCE INSPECTED AND CYCLED CIRCUIT BREAKERS IN ACCORDANCE WITH THE SERVICE LETTER. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007021200014 20070212 00014 EA 2007 2 12 VNAA0701009 1 20070126 A 2400 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 IDG UNKNOWN A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 257PS 7939 CREW REPORTED A LOSS OF THE NR 2 GENERATOR ON TAKEOFF ROLL. CREW ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PROPERLY SERVICED THE NR 2 IDG IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007021200015 20070212 00015 EA 2007 2 12 VNAA0701010 1 20070127 A 2133 32156222 OUTFLOW VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN PRESSURE FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 250PS 6685 7929 CREW REPORTED A LEFT & RIGHT HAND PACK HIGH PRESSURE MESSAGE ALONG WITH AN APU OVERTEMP MESSAGE ON CLIMBOUT. CREW FOLLO WED THE QRH AND RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PRESSURE REGULATING VALVE IN ACC ORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007021200020 20070212 00020 NM 2007 2 12 AWXA200700188 1 20070202 A 5315 654581216 STIFFENER BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED FLOORBEAM STIFFENER, BS 328, LBL 51, WL 208. REPLACED FLOORBEAM STIFFENER, BS 328, LBL 51, WL 208 I AW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007021200021 20070212 00021 EU 2007 2 12 AWXA200700189 1 20070205 A 5330 D53480022213 SKIN AIRBUS 320 A320231 3930325 EU ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 PHX - FOUND CORROSION ON EXTERNAL FUSELAGE SKIN, FR 70, S31R - S32R. REPAIRED EXTERNAL FUSELAGE SKIN, FR 70, S31R - S32 R IAW A320 SRM 53-00-11 FIGURE 235. 2 L 7 2 4F RT A28NM 2007021200024 20070212 00024 NM 2007 2 12 AWXA200700192 1 20070202 A 5321 D5367180500500 FLOOR PANEL AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 831AW 1576 SAL - FOUND CORROSION ON MAIN CABIN FLOORBOARD 262 FF, FR 66 - FR 68, -Y1292. REPLACED MAIN CABIN FLOORBOARD 262 FF, FR 66 - FR 68, - Y1292 IAW A319 SRM 53-12-12. 2 L 7 2 4F RT A28NM 2007021200029 20070212 00029 NM 2007 2 12 QXEA200700140 1 20070202 A 3080 4100S01904 PROBE BOMBDR DHC8 DHC8402 1390042 NM ICE DETECTOR MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 425QX 235 4039 PDX FLIGHT NR 2416: ICE DETECT FAIL CAUTION LIGHT ILLUMINATED AFTER ENGINE START. MAINTENANCE REMOVED RT ICE DETECTOR P ROBE IAW Q400 AMM 30-80-01-000-801. INSTALLED A NEW FROM STOCK ICE DETECTOR PROBE IAW Q400 AMM TASK 30-80-01-400-801. OPS TEST GOOD. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007021200031 20070212 00031 NM 2007 2 12 DL757070084 1 20070205 A 5330 SKIN BOEING 757 757232 1384965 NM FUSELAGE MAINT ERROR A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 684DA 27104 DURING HMV AT TIMCO LCQ, THE CRADLE SHORING INSTALLED AT FS 680 CAUSED DENTING ON THE FUSELAGE SKIN. DENTING IS JUST AB OVE S-24R TO JUST BELOW S-25R. THE DENT WAS TRIMMED OUT AND A REPAIR DOUBLER WAS INSTALLED, WITH TIME-LIMITED RESTRICTI ONS PER ER/A 459984-14. 2 L 7 2 4F RT A2NM 2007021200033 20070212 00033 NE 2007 2 12 DL76S070088 2 20070206 A 7200 ENGINE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 FAILED A DALA E ENGINE SHUTDOWN Y ENGINE STOPPAGE AP APPROACH 1 SO 27 128DL 59780 24078 102006 DURING DESCENT INTO MCO, RT ENG FAILED. UNKNOWN REASON FOR FAILURE NO VIBRATION OR NOISES NO BY CREW. A/C WAS LEVEL AT 11000 FEET RUNNING FINE. CLEARED TO 9000 FEET RT ENGINE FAILED TO RESPOND AT 9000 FT. CARD MESSAGE. T/S PER FIM BORO SCOPED HPC ALL NML. PERFORMED BORESCOPE INSPECTION OF HPC PER FIM 71-05-00. NO DAMAGE FOUND REMOVED AND STARTED INSTAL LATION OF NEW MEC. REMOVED FUEL PUMP AND STARTED INSTALL PER AMM. FOUND FUEL FILTER BOWL ASSY DAMAGED. PERFORMED WIND MILL CHECK ALL NML. FOUND TO PWR RUN. ALL TESTS NORMAL. 2 L 7 2 4F 4 F RT A1NM E13NE 2007021200034 20070212 00034 NM 2007 2 12 DL777070089 1 20070206 A 2120 UNKNOWN BOEING 777 777232 1385232 NM CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 865DA 29737 102006 FLT ATTN OBL REPORTS ODOR AT FWD B/E CABIN LEFT SIDE. POSS BURNING SMELL. NO SMOKE OR FIRE NOTED. FLT ATTN OBL COULD NOT IDENTIFY SMELL OR SOURCE. OBL DID NOT KNOW IF IT WAS A BURNING SMELL OR NOT. FLT CREW DID NOT SMELL ANY UNUSUAL OD OR EN ROUTE. RAN PACKS AT FULL HOT AND NO ABNORMAL SMELL. NO UNUSUAL SMELL IN ENTIRE CABIN. IFE EQUIP ON AND NO SMELL NOTED. INSPECT E/E COMPARTMENT AND NO SMELL NOTED. FWD CARGO BIN NO SMELL NOTED. 2 L 7 2 4F RT T00001SE 2007021200035 20070212 00035 NM 2007 2 12 DL757070090 1 20070207 A 3397 WIRE BOEING 757 757232 1384965 NM EMERGENCY LIGHTS BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 623DL 22913 102006 EMERGENCY LIGHT WIRE BROKEN AT 24DEF. REPAIRED WIRE PULLED FROM CONNECTOR. NOW OPS NORMAL. 2 L 7 2 4F RT A2NM 2007021200036 20070212 00036 NM 2007 2 12 DL757070091 1 20070207 A 2121 6067723 FAN BOEING 757 757232 1384965 NM RT A/C SYS SEIZED A DALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 699DL 29970 102006 EN ROUTE TO ATL AT FL 350 RT RECIRC FAN EICAS MESSAGE. RAN QRH CHECKLIST FOR RECIRC FAN. SMELLED ELECT SCENT IN COCKPI T AND CABIN. DECLARED EMERGENCY AND CONDUCTED SMOKE FUMES ELECTRICAL, AIR CONDITIONING AND REMOVAL QRH PROCEDURES FOUND RT RECIRC FAN SEIZED AND EXH NOZZLE MELTED. REMOVED AND REPLACED PER M/M, OPS CKS GOOD. ALSO REPLACED RT/LT FILTERS. 2 L 7 2 4F RT A2NM 2007021200037 20070212 00037 NM 2007 2 12 DLM88070093 1 20070207 A 5330 5911401179 SKIN DOUG MD88 MD88 3023688 NM FS 218 L18R PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 978DL 53259 FUSELAGE SKIN PUNCTURED FROM CONTACT WITH GSE EQUIPMENT. DAMAGE LOCATED AT FS 218, ABV L-18R. CUT OUT DAMAGE AND INSTA LL MODIFIED REPAIR PER MD-88 SRM 53-04 FIG 12B CLASS III REPAIR. 2 L 7 2 4F RT A6WE 2007021200038 20070212 00038 NM 2007 2 12 QXEA200700142 1 20070207 A 5610 80260006 WINDSHIELD BOMBDR DHC8 DHC8402 1390042 NM COCKPIT FAILED A QXEA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 09 414QX 12216 4061 FCA-SEA FLIGHT NR 2348: RT WINDSHIELD SPIDER WEBBED AT 24,000 FT CRUISE. WINDSHIELD HEAT ON. NO CAUTION LIGHTS. FLIGH T WAS DIVERTED TO GEG. MAINTENANCE REPLACED RT WINDSHIELD IAW AMM 56-10-01 PAGES 401-405. DRAIN HOLES WERE SEALED PER MCN 653302-001. OPS TESTS GOOD. AIRCRAFT REMAINS CAT III. 2 H 7 2 4T RT A13NM 2007021200040 20070212 00040 NE 2007 2 12 N93A30012007 2 20070130 A 7532 EB100045D BLEED VALVE GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE ENGINE STICKING E N93A A UNSCHED LANDING E B J VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 13 516QS 4690 658 11431 ENGINE VIBRATION ABOVE IDLE, ACRID SMELL IN CABIN. ENGINE WAS BORESCOPED WITH NO DISCREPANCY FOUND. MAINTENANCE FOUND B LEED AIR VALVE STICKING AND REPOSITIONED TWO (V) BAND CLAMPS.AIRCRAFT WAS DISPATCHED ON AN EVALUATION FLIGHT WITH NO FUR THER DISCREPANCIES. 2 L 7 2 4F 4 F RT A12EA E00057EN 2007021200041 20070212 00041 SW 2007 2 12 PNSA070103 1 20070117 A 3297 WIRE SWRNGN SA227 SA227AC 8780603 SW CONTROL VALVE DAMAGED A PNSA L A ABORTED APPROACH UNSCHED LANDING J WARNING INDICATION LD LANDING 1 AL 03 41NE AC741B LANDING GEAR WOULD NOT EXTEND ELECTRICALLY, GEAR EXTENDED MANUALLY AND LANDED AT AKN. ANC MX ISSUED A FERRY PERMIT AND AIRCRAFT RETURNED TO ANC GEAR DOWN. ANC MX FOUND NO POWER TO THE GEAR SELECTOR CONTROL VALVE, REPAIRED WIRING AND OPS C HECK GEAR SYSTEM NORMAL. 2 L 7 2 4T RT A8SW 2007021200042 20070212 00042 EA 2007 2 12 PNSA070105 2 20070130 A 8550 LINE PIPER PA32 PA32301 7103207 SO LYC O540 IO540K1G5 41532 EA ENGINE OIL LOOSE E PNSA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AL 03 82455 328006079 L1466348 WHILE EN ROUTE FROM AKN TO DLG, THE PILOT NOTICED OIL PRESSURE WAS ON THE LOW REDLINE AND THE OIL ANNUNCIATOR WAS ON. AI RCRAFT LANDED NORMALLY IN DLG AND PILOT FOUND EXCESSIVE OIL ON BELLY AND THE OIL LEVEL REMAINING WAS 2 QUARTS. MAINTENA NCE FOUND THE OIL VALVE COVER RETURN LINES LOOSE ON 3 CYLINDERS AND ONE CYLINDER IT WAS OFF. THIS ENGINE WAS 16 HOURS S INCE LYCOMING FACTORY OVERHAUL. ENGINE OIL FILTER WAS CHECKED OK, ENGINE OIL ADDED TO FULL AND ENGINE GROUND RAN NORMAL . OIL FILTER RECHECKED AFTER 10 HOURS AND FOUND NORMAL. 1 L 7 1 3O 3 O A3SO 1E4 2007020600182 20070206 00182 NM 2007 2 6 AT0700098 1 20070129 A 5347 SEAT TRACK BOEING 737 73776N 13844CH NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 184AT 32656 SEAT ROW 14 INOPERATIVE DUE TO SEAT TRACK DAMAGE. REPAIRED SEAT TRACK IAW 737 SRM 53-00-52 REPAIR 4. THIS COMPLIES WI TH SECTION 3 OF EA 37-25-00264 REV A. THIS IS CLASS A REPAIR AND THERE ARE NO REINSPECT REQUIREMENTS FOR THIS REPAIR. 2 L 7 2 4F RT A16WE 2007020600184 20070206 00184 NM 2007 2 6 USAASB07010 1 20070130 A 4960 38762594 SPEED SWITCH BOEING 737 7374B7 1384702 NM AFT CABIN FAULTY A USAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 444US 17427 17427 24862 CLT FLT 1081 FLIGHT DEPARTED PIT EN ROUTE TO FLL WITH THE NR 2 GENERATOR/CSD INOPERATIVE. DURING CRUISE, AT FL340, THE APU OVERSPEED LIGHT ILLUMINATED AND THE APU AUTO SHUTDOWN. WITH ONLY ONE GENERATOR REMAINING, CREW DIVERTED FLIGHT TO C LT WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE WAS UNABLE TO DUPLICATE APU AUTO SHUTDOWN. INSPECTED APU WIRING AND KNOWN PROBLEM AREAS. NO DEFECTS OBSERVED. REMOVED AND REPLACED 3 SPEED SWITCH PER MM 49-61-22-4, AS PRECAUT IONARY. OPERATIONAL CHECK GOOD. ALSO, REMOVED AND REPLACED APU CONTROL UNIT (M280 BOX). FOUND THE FREQUENCY TO BE LOW (OUT OF LIMITS) ON THE NR 2 ENGINE CSD. ADJUSTED FREQUENCY PER MM 24-11-11. OPERATION CHECK NORMAL. CHECKED AND REPL 2 L 7 2 4F RT A16WE 2007020600189 20070206 00189 NM 2007 2 6 F3LA200700016 1 20070202 A 5321 D5367180500400 FLOORBOARD AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 5911 1943 DURING C-3 CHECK, INSPECTION REPORTED FLOORBOARDS 261FF AND 262FF CORRODED. REPLACED FLOORBOARDS 261FF AND 262FF PER AM M 53-42-12-400-002. 2 L 7 2 4F RT A28NM 2007020600206 20070206 00206 NM 2007 2 6 07FDEA00241 1 20070202 A 5713 STRINGER DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 CRACK FOUND (APPROX 0.5" LONG) DURING HFEC INSPECTION ON LEFT WING TANK AT THE END OF UPPER STRINGER 37 (XORS 938). CRA CK ON LEFT HAND WING TANK AT THE END OF UPPER STRINGER 37 (XORS 938) REPAIRED AS PER FEDEX E.A. 1-5720-105613, REPAIR CL ASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020600210 20070206 00210 2007 2 6 07FDEA00245 4 20070202 A 2220 SERVO BOEING 727 727277 138408S NM AUTO PILOT UNKNOWN A FDEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 491FE 21529 AFTER DEPARTING MIA WHILE CLEANING UP AIRCRAFT STAB CRUISE TRIM CIRCUIT BREAKER POPPED. CLIMBING THROUGH 17500 IT WAS D ISCOVERED AIRCRAFT COULD NOT BE TRIMMED DOWN BELOW 0. REVIEWED QRH FOR GUIDANCE AND CONTACTED GOC AND MOCC FOR SUGGESTI ONS. DECISION WAS MADE TO RETURN TO MIA BECAUSE OF AIRSPEED/ALTITUDE RESTRICTIONS, MODERATE TURBULENCE EN ROUTE AND UN CERTAINTY OF AIRCRAFT MALFUNCTION. REMOVED AND REPLACED AUTO PILOT STAB TRIM SERVO MOTOR PER MM 22-11-021-2, OPS CKS G OOD ON GROUND PER MM 22-11-021-2. 2 L 7 3 4F RT A3WE 2007020600212 20070206 00212 2007 2 6 MWEA070026 4 20070202 A 2565 100503119 SLIDE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE AFT LOW PRESSURE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 810ME 48072 AFT EVACUATION SLIDE PRESSURE IS LOW AT 1500 PSI. REMOVED AND REPLACED AFT SLIDE. 2 L 7 2 4F 4 F A6WE E2EA 2007020700024 20070207 00024 EU 2007 2 7 07FDEA00284 1 20070203 A 5320 A5397312923000 PLATE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CHAFED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 FOUND CHAFING MARKS ON TORSION PLATE C86 RT. REPLACEMENT WAS PERFORMED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007020700025 20070207 00025 EU 2007 2 7 07FDEA00285 1 20070203 A 5310 A5397847620000 CROSSBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 FOUND CROSS BEAM ATTACHMENT PROFILE (SRM 53-17-15 FIG.10 ITEM 455) AT C61 RT CORRODED REPLACEMENT OF RELATED PART WAS PE RFORMED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007020700027 20070207 00027 NM 2007 2 7 07FDEA00288 1 20070203 A 5320 CHANNEL BOEING 727 727233 138408A NM BS 990-1010 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 AFT PIT STR 29R CORRODED IN U-CHANNEL AT SPLICE BETWEEN STA 990-1010. REMOVED CORROSION, HFEC BLEND AREA, FLAP PEENED, ALODINED AND PRIMED, INSTALLED FASTENERS WET W/ SEALANT, APPLIED CIC TO AREA, REF EA NR 7-5310-107615 AND AAR EA NR I070 076. 2 L 7 3 4F RT A3WE 2007020700028 20070207 00028 NM 2007 2 7 07FDEA00289 1 20070203 A 5740 6521658Y29 ATTACH ANGLE BOEING 727 727233 138408A NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 RT WING LOWER T/E WING PANEL BELOW NR 12 SPOILER, OTBD ATTACH, LOWER INBD ATTACH ANGLE IS CRACKED AT ROD ATTACH AREA. R EMOVED CRACKED ANGLE, VERIFIED NEW ANGLE TO BE INSTALLED AS P/N 65-21658Y29. DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED NEW ANGLE REF SRM 51-30-2, PG 2-3 AND 10-13, SRM 51-10-1, PG 12, BOEING DWG NR 65-21658, MM 51-20-021-7/51 -20-031-7, SRM 51-30-4 PG 2. 2 L 7 3 4F RT A3WE 2007020700036 20070207 00036 NM 2007 2 7 07FDEA00297 1 20070203 A 5311 FRAME BOEING 727 727233 138408A NM BS 620 S3-4L TOOL DAMAGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 MAIN CABIN BS 620 BETWEEN STR S-3L AND S-4L UPPER SILL TO FRAME SPLICE AREA HAS 2. MISDRILLED HOLES AND 1 OVER CHAMFERE D HOLE (VIEW FROM AFT SIDE) COMPLIED WITH EA NR 7-5310-106977 (WRI53108462) AND AAR WO NR 11701/2400/0004 PART 1, ITEM 1 THRU 10 ACCOMPLISHED. FINAL EA WO NR 53108484/ EA NR 7-5310-106977 ALSO COMPLIED WITH. 2 L 7 3 4F RT A3WE 2007020700040 20070207 00040 NM 2007 2 7 07FDEA00301 1 20070205 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 RIGHT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION ON R IGHT HAND WING - INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE REPAIRED AS PER FEDEX E.A. 1-5750-107780 PT1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007020700058 20070207 00058 NM 2007 2 7 SWAA070564 1 20070202 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007020700061 20070207 00061 NM 2007 2 7 SWAA070577 1 20070203 A 3350 307IBPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 797MX 27890 DURING SCHEDULED MV1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 9 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007020700066 20070207 00066 NM 2007 2 7 SWAA070558 1 20070202 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 500 S17R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 17R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007020700083 20070207 00083 NM 2007 2 7 SWAA070584 1 20070203 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020700099 20070207 00099 NM 2007 2 7 SWAA070576 1 20070203 A 3350 PH22300L LIGHT BOEING 737 7373Q8 1384670 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 ABC. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007020700101 20070207 00101 CE 2007 2 7 DXTA200701887 1 20070129 A 3220 LANDING GEAR CESSNA 680 680CE 2076811 CE NOSE UNKNOWN E DXTA O OTHER S J AFFECT SYSTEMS WARNING INDICATION CL CLIMB 1 GL 07 370QS 6800099 DURING NOSEGEAR RETRACTION, STRONG BANGING AND FLASHING UNSAFE LIGHT DURING MULTIPLE ATTEMPTS ON OCF. ALSO; GRINDING OR RUBBING SOUND DURING ALL GEAR RETRACTIONS ON TAKE OFF AND LEVEL FLIGHT. PERFORMED OPS CK PER CESSNA 680 MM 32-60-00. COU LD NOT DUPLICATE. REMOVED BRAKE METERING VALVE P/N 9914652-6 S/N 208 AND INSTALLED SERVICEABLE BRAKE METERING VALVE P/N 9914652-6 S/N 298. PERFORMED OPS CK & LEAK CK GOOD I/A/W CESSNA 680 M/M 32-42-30 2 L 7 2 4F RC T00012WI 2007020700145 20070207 00145 NM 2007 2 7 UPS07449100 1 20070111 A 5320 65B091911 SUPPORT FITTING BOEING 747 747123 1384873 NM BS 980 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT AFT FIXED STOP SUPPORT FITTING LWR SURFACE FOUND CRACK AT STA 980 RBL 45. CRACK LENGT H 2 INCHES. FWD CARGO COMPT AFT FIXED STOP SUPPORT FITTING REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 5 1-30-02. 2 L 7 4 4F A20WE 2007020700146 20070207 00146 NM 2007 2 7 UPS07549076 1 20070104 A 5311 146N102848 FRAME BOEING 757 75724APF 1384969 NM BS 1260 S25-26R DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 417UP 23904 INSPECTION TYPE:C AFT PIT RIGHT SIDE STA 1260 BETWEEN STR 25-26 FRAME DENTED. COMPLIED WITH EA 757-5362-27-A1567 AND UP S EO B757-5310-26027-A. 2 L 7 2 4F RT A2NM 2007020700158 20070207 00158 EU 2007 2 7 UPS07149103 1 20070202 A 5270 SWITCH AIRBUS A300 A300F4622R 3930360 EU CARGO DOOR MALFUNCTIONED A IPXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 147UP 0830 INSPECTION TYPE:N/A ATB - WHILE PASSING ABOUT 1,000 FT ON T/O RECEIVED AN ECAM MSG, FWD CARGO NOT CLOSED. MESSAGE STAYE D ON ABOUT 5 MINUTES THEN WENT OUT FOR REMAINDER OF FLT. INDICATION ON ECAM MSG INOP TO AMC. VERIFIED DOOR CLOSED. DE FERRED M343378. REPETITIVE INSP REQUIRED PRIOR TO EACH FLT. REMOVED AND REPLACED SWITCH 14WS PER AMM 52-71-11-05, CHEC KS GOOD. THIS CLOSES M343378. PLACARD REMOVED. 2 L 7 2 4F RT A35EU 2007020700172 20070207 00172 NM 2007 2 7 ZZDA070123101 1 20070123 A 5311 FRAME BOEING 717 717200 1383700 NM BS 37 CRACKED A ZZDA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. FORMER ANGLE, WEB AND SEAL CRACKED AND BROKEN BEYOND REPAIR. REPLACED S TA 37.0 FORMER ANGLE, WEB AND SEAL PER MDC DRAWING 991 1500 REV DL DATED 4/24/01. 2 L 7 2 4F TR A6WE 2007020700173 20070207 00173 NM 2007 2 7 ZZDA070123102 1 20070123 A 5280 DOOR FRAME BOEING 717 717200 1383700 NM NLG DENTED A ZZDA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. NLG FWD DOOR JAMB DENTED AND BENT BEYOND REPAIR. REPLACED NLG FWD DOOR JAMB PER MDC DRAWINGS 5912852 REV B DATED 06/27/81. 2 L 7 2 4F TR A6WE 2007020700175 20070207 00175 NM 2007 2 7 ZZDA070123104 1 20070123 A 5311 FRAME BOEING 717 717200 1383700 NM BS 76 CRACKED A ZZDA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. LEFT SIDE FRAME AT STA 76.0 CRACKED AND BENT BEYOND REPAIR. REPLACED LE FT SIDE FRAME AT STA 76.0 PER 991 1504 REV L DATED 7/10/98. 2 L 7 2 4F TR A6WE 2007020700181 20070207 00181 NM 2007 2 7 CALA0700047 1 20070128 A 5320 141T5134146 FLOOR SUPPORT BOEING 767 767424ER 1385270 NM BS 303-325 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76062 29457 INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 303-325, LBL 30. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02, PAGE 8. 2 L 7 2 4F RT A1NM 2007020700182 20070207 00182 NM 2007 2 7 CALA0700048 1 20070128 A 5315 141T5107 FLOORBEAM BOEING 767 767424ER 1385270 NM BS 303 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76062 29457 INSPECTION FOUND FLOORBEAM CORRODED AT BS 303, LBL 25 - LBL 40. THE CORROSION WAS REMOVED AND THE FLOORBEAM WAS REPAIRE D IAW SRM 53-00-51, REPAIR 1, FIGURE 201. 2 L 7 2 4F RT A1NM 2007020700199 20070207 00199 NM 2007 2 7 ZZDA070123113 1 20070123 A 5244 DOOR FRAME BOEING 717 717200 1383700 NM ACCESSORY BAY DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. ACCESSORY COMPARTMENT DOOR JAMB DAMAGED. REPLACED ACCESSORY COMPARTMENT DOOR JAMB PER MDC DRAWING 5910343 REV AL DATED 01/24/06. 2 L 7 2 4F TR A6WE 2007020700203 20070207 00203 NM 2007 2 7 ZZDA070123117 1 20070123 A 5330 SKIN PANEL BOEING 717 717200 1383700 NM BS 110-229 DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. LOWER SKIN PANEL FROM STA 110.0 TO STA 229.0 DAMAGED. REPLACED LOWER SK IN PANEL FROM STA 110.0 TO STA 229.0 PER MDC DRAWING 5911401 REV DW DATED 1/7/04. 2 L 7 2 4F TR A6WE 2007020800004 20070208 00004 NM 2007 2 8 SWAA070634 1 20070206 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM BS 944 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007020900001 20070209 00001 NM 2007 2 9 UPS07449125 1 20070103 A 5310 65B38600113 TENSION TIE BOEING 747 747123 1384873 NM BS 840 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D- RIGHT BS 840 TENSION TIE TO FRAME CONNECTION FOUND 1EA HOLE CRACK AT TIE CLIP APPROX 0.040 INCH R UNNING UP. M/D RIGHT BS 840 TENSION TIE TO FRAME CONNECTION TIE CLIP REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51 -30-02. 2 L 7 4 4F A20WE 2007020900009 20070209 00009 NM 2007 2 9 SWAA070622 1 20070206 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020900012 20070209 00012 NM 2007 2 9 SWAA070623 1 20070206 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020900026 20070209 00026 EA 2007 2 9 COMA0760132 1 20070204 A 2752 852D10021 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 01 479CA 11413 7675 FLIGHT 5390 - DURING JFK APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WIT HOUT INCIDENT. REPLACED THE LEFT INBOARD FLAP INBOARD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2007020900027 20070209 00027 EA 2007 2 9 COMA0760133 1 20070204 A 2752 852D10021 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 01 479CA 11480 7675 FLIGHT 5390 - DURING JFK APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WIT HOUT INCIDENT. REPLACED THE LEFT INBOARD FLAP OUTBOARD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2007020900038 20070209 00038 NE 2007 2 9 DXTA200701917 2 20070206 A 7200 ENGINE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LEFT MALFUNCTIONED E DXTA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 336QS 5600336 LT ENGINE SHUTDOWN DURING SPEED BRAKE RETRACTION TEST. N2 WAS 11 PERCENT. N1 WAS 7 PERCENT AND ITT STARTED TO RISE TO 550. 2 L 7 2 4F 4 F RT A22CE E25EA 2007020900040 20070209 00040 NM 2007 2 9 AMTA200700051 1 20070201 A 4900 UNKNOWN BOEING 757 75733N 1384931 NM APU UNKNOWN A AMTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 552TZ 32586 APU AUTO SHUTDOWN DUE TO LOW OIL QTY APPROX 2 HOURS IN TO FLIGHT. INSPECTED APU OIL FILLER CAP, ALL LINES AND TAIL PIPE FOR SIGNS OF LEAK AND NO LEAKS WERE FOUND. RAN APU FOR 4 HOURS AND NO LEAKS WERE NOTED. PERFORMED BITE AND NO FAULTS FOUND. (M) 2 L 7 2 4F RT A2NM 2007020900041 20070209 00041 EA 2007 2 9 COMA0760150 1 20070206 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 528CA 7841 FLIGHT 5115 - DURING YUL APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAG E -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTIO N MESSAGES. 2 L 7 2 4F RT A21EA 2007020900042 20070209 00042 NM 2007 2 9 CALA0700054 1 20070206 A 5311 6546538 FRAME BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE BS 597 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 INSPECTION FOUND A .5 INCH CRACK IN FRAME AT STA 597, S13L. THE FRAME WAS REPAIRED IAW SRM 53-00-07, PAGE 203, FIGURE 20 1. 2 L 7 2 4F 4 F RT A16WE E2GL 2007020900114 20070209 00114 NM 2007 2 9 07FDEA00332 1 20070205 A 5320 FLOOR SUPPORT BOEING 727 727233 138408A NM BS 277-266 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 FLT DECK FLOOR SUPPORT UPPER SURFACE CORRODED BETWEEN BS 277-266.75 AT RBL 13 REMOVED CORROSION REF SRM 51-10-1 PG 5. M AT LOSS IS .007''. HFEC IAW AAR EA I070063 REF FED EX EA NR 7-5310-107610/ WO#35039. 2 L 7 3 4F RT A3WE 2007020900115 20070209 00115 EU 2007 2 9 07FDEA00333 1 20070205 A 5313 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 CORROSION ON STRINGER P56 LT BETWEEN C70 AND C71. REPAIR ON STRINGER P56 LT WAS PERFORMED IAW SRM 53-10-14, FIG 201. 2 L 7 2 4F RT A35EU 2007021200016 20070212 00016 EA 2007 2 12 VNAA0701011 1 20070129 A 5230 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CARGO DOOR UNSECURE A VNAA C ABORTED TAKEOFF W J INADEQUATE Q C WARNING INDICATION TO TAKEOFF 1 GL 05 245PS 7919 CREW REPORTED A CARGO DOOR CAS MESSAGE ON TAKEOFF ROLL. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCID ENT. MAINTENANCE RESECURED THE CARGO DOOR HANDLE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 52-70-02-710-801. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007021200019 20070212 00019 NM 2007 2 12 AWXA200700187 1 20070130 A 5320 65479738 SHEAR WEB BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED SHEAR WEB, BS 577, S17R, WL 208. REPLACED SHEAR WEB, BS 577, S17R, WL 208 IAW B737-300 SRM 51-40-02 . 2 L 7 2 4F RT A16WE 2007021200022 20070212 00022 NM 2007 2 12 AWXA200700190 1 20070202 A 5340 D53112198200 FITTING AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 831AW 1576 SAL - FOUND CORROSION ON L1 DOOR CUT OUT LOWER SILL CENTER FITTING, FR 16 - FR 20, S23L. REPLACED L1 DOOR CUT OUT LOWER SILL CENTER FITTING, FR 16 - FR 20, S23L IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007021200023 20070212 00023 NM 2007 2 12 AWXA200700191 1 20070202 A 5320 D53112198201 FITTING AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 831AW 1576 SAL - FOUND CORROSION ON R1 DOOR CUT OUT LOWER SILL CENTER FITTING, FR 16 - FR 20, S23R. REPLACED R1 DOOR CUT OUT LOWER SILL CENTER FITTING, FR 16 - FR 20, S23R IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007021200030 20070212 00030 NE 2007 2 12 DLM8K070082 2 20070204 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 MAKING METAL A DALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 915DE 36616 726003 53420 726003 NR TWO ENG LOUD BAND ON TAKEOFF ROLL. METAL FOUND IN TAIL PIPE. FOUND SMALL METAL PARTICLES IN TAIL PIPE. REPLACED NR 2 ENG PER TRANSMITAL CARDS. 2 L 7 2 4F 4 F RT A6WE E9NE 2007021200039 20070212 00039 NM 2007 2 12 QXEA200700143 1 20070207 A 2420 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM A/C BUSS UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 405QX 4047 BOI FLIGHT NR 2391: R AC BUSS CAUTION LIGHT AFTER PUSHBACK. MAINTENANCE CYCLED NR 2 AC GENERATOR. FAULT EXTINGUISHED. ALL INDICATIONS NORMAL. NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007021200052 20070212 00052 2007 2 12 SWAA070642 4 20070207 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 429WN 33658 R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007021200053 20070212 00053 2007 2 12 SWAA070641 4 20070207 A 2565 63551101 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 417WN 29822 L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007021200054 20070212 00054 NM 2007 2 12 SWAA070646 1 20070207 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 503 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 8R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007021200055 20070212 00055 NM 2007 2 12 SWAA070645 1 20070207 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 506D S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506D, STR 7R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007021200056 20070212 00056 NM 2007 2 12 SWAA070647 1 20070207 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 706 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 706, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007021200057 20070212 00057 NM 2007 2 12 SWAA070662 1 20070207 A 5330 6545768 SKIN BOEING 737 7375H4 138449D NM BS 378 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING DUCT CUTOUT BS 378.5, LBL 2.8. REPAIRED SKI N PER SWA EA. 2 L 7 2 4F RT A16WE 2007021200058 20070212 00058 NM 2007 2 12 SWAA070653 1 20070207 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 742 S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 742D, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007021200059 20070212 00059 NM 2007 2 12 SWAA070652 1 20070207 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 743D S23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 743D, STR 23L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007021200060 20070212 00060 NM 2007 2 12 SWAA070659 1 20070207 A 5315 6545834 WEB BOEING 737 7373H4 1384600 NM BS 339-353 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 339 TO BS 353, LBL 60. REMOVED AND REPLACED CREASE BEA M WEB PER SRM. 2 L 7 2 4F RT A16WE 2007021200061 20070212 00061 NM 2007 2 12 SWAA070657 1 20070207 A 3233 654610918 ARM BOEING 737 7373H4 1384600 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED 12Y CHECK, FOUND RIGHT MLG WALKING BEAM ACTUATOR ARM CORRODED. REMOVED AND REPLACED ACTUATOR ARM PER M M. 2 L 7 2 4F RT A16WE 2007021200062 20070212 00062 NM 2007 2 12 SWAA070660 1 20070207 A 5753 6546435278 SKIN BOEING 737 7373L9 1384470 NM TE FLAPS DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED C2 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED OUTBOARD T/E END. REMOVED AND REPLACED AF T FLAP PER MM. 2 L 7 2 4F RT A16WE 2007021200063 20070212 00063 2007 2 12 YENA2007008 4 20070206 A 3415 2015G2H2H7A PROBE EMB ERJ190 ERJ190100IGW 3260408 EU NR 3 ADS FAULTED A YENA B EMER. DESCENT S AFFECT SYSTEMS DE DESCENT 1 EA 15 258JB 967 19000047 FLIGHT MANAGEMENT DISABLED, ADS 3 FAIL AND OVERSPEED ANNUNCIATION IN DESCENT AT 17000FT, UNRELIABLE AIRSPEED INDICATIONS AND MULTIPLE EICAS MESSAGES AT 17,000 FT. UNABLE TO RE-ENGAGE AP/AT, APPR 2 NOT AVAIL DISPLAYED ON EICAS AT FL180 WITH 30.20 SET ON ALL 3 ALTIMETERS AND ILS 22L (JFK) CRS TUNED CORRECTLY ON BOTH CA AND FO SIDES. AP/AT UNCOMMANDED DISENGA GE AT 17,000 FT. PMA CLEARED ON BOTH CA/FO SIDE. MULTIPLE EICAS MESSAGES ILLUMINATED. CA AIRSPEED UNRELIABLE BEFORE A ND AFTER MANUAL REVERSION TO ADS3. AP/AT WOULD NOT RE-ENGAGE ONLY LOC/GS WOULD ARM ON THE FMA. NOTHING ELSE WOULD ARM. OVERSPEED ANNUNCIATED AND DISPLAYED ON BOTH CA/FO AIRSPEED TAPES BEFORE AND AFTER MANUAL REVERSION TO ADS 3. STICK SH 2 L 7 2 4F RT A57NM 2007021200064 20070212 00064 NM 2007 2 12 DU4R2007033 1 20070107 A 5330 SKIN BOEING 757 757232 1384965 NM BS 1500-1520 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 FOUND CORROSION RT AIRFONE ANTENNA MOUNT SURFACE FUSELAGE SKIN. CUT OUT CORRODED AREA 5/8" ROUND. FABRICATED AND INSTA LLED REPAIR DOUBLER FROM 2024-T3 .063" AND FILLER 2024-T3 .040" IAW B757 SRM 51-20-1, 51-40-02. 2 L 7 2 4F RT A2NM 2007021200065 20070212 00065 NM 2007 2 12 DU4R2007048 1 20070131 A 5320 FLOOR SUPPORT BOEING 757 757232 1384965 NM BS 1445-1535 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION AFT CARGO BS 1470 RBL 2.90 CARGO FLOOR SUPPORT STRINGER CORROSION AROUND NUTPLATES HOLES. FABRICATED AND INST ALLED FLOOR SUPPORT FROM BAC1510-1087 AND FLOOR SUPPORT FROM BAC 1517-22-9 7075-T6 .063", 7075-T6511 SPLICE PLATE 6" BY 10" BY 3" WIDE FROM 60-122 EXTRUSION 7075T6511 IAW B757 SRM 53-60-53, 51-70-12 FIG 1, AND 51-20-01 PG 3 - 7, 21. 2 L 7 2 4F RT A2NM 2007021200066 20070212 00066 NM 2007 2 12 DU4R2007050 1 20070130 A 5322 SHEAR TIE BOEING 757 757232 1384965 NM CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION ON BASE OF FRAME AT BS 1400, B/L 2L IN BILGE OF THE AFT CARGO PIT. REMOVED CORRODED SHEAR TIES. REMOVED CORR OSION ON FRAME, WITHIN LIMITS IAW B757 SRM 51-10-02, 53-60-07, 53-00-07. FABRICATED AND INSTALLED 2 NEW SHEAR TIES 4.0 BY 2.0 FROM 7075-T6 .050 IAW B757 SRM 51-40-05, 51-20-01 AND 51-30-01. 2 L 7 2 4F RT A2NM 2007021200067 20070212 00067 NM 2007 2 12 DU4R2007052 1 20070129 A 5310 146N852257 BEAM BOEING 757 757232 1384965 NM BS 1375-1440 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION AFT CARGO COMPT LOCATED BS 1375 - BS 1440 RBL 21 ON TOP OF DOOR CUT OUT THRESHOLD BEAM (LOWER SILL INNER CHORD ). REMOVED AND REPLACED CORRODED CHORD WITH P/N 146N8522-57 AND FITTING P/N 69-45578-7 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007021200068 20070212 00068 NM 2007 2 12 DU4R2007053 1 20070128 A 5330 SPLICE BOEING 757 757232 1384965 NM BS 1400 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION ON SKIN SPLICE AT BS 1400 S-29L TO 30 IN AFT CARGO COMPARTMENT. FABRICATED AND INSTALLED SKIN SPLICE 36.0" BY 4.0" FROM 7075-T6 .071" IAW B757 SRM 51-40-02 AND BAC146N8522. 2 L 7 2 4F RT A2NM 2007021200069 20070212 00069 NM 2007 2 12 DU4R2007055 1 20070130 A 5310 HOUSING BOEING 757 757232 1384965 NM LAV DRAIN CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION ON TOP OF LAV DRAIN HOUSING IN E/E BAY BS 418 TO BS 440 S-26L TO S-28L. FABRICATED AND INSTALLED DOUBLER 6-12 /" BY 9-1/4" FROM 2024-T3 .040", SUPPORT 16" BY 9-3/4" FROM 2024-T3 .050" IAW B757 SRM 51-20-01, B757 DWG 141N631 AND 51 -40-02. 2 L 7 2 4F RT A2NM 2007021200070 20070212 00070 EU 2007 2 12 07FDEA00334 1 20070203 A 3230 DAMPER AIRBUS 300 A300B4622R 3930312 EU MLG DISCHARGED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 728FD 581 L/G WOULD NOT RETRACT USING EITHER SYS 1 OR 2. PERFORMED SERVICE OF LT BOOGIE PITCH DAMPER WITH NITROGEN PER AMM 12-12- 32-0 PARAGRAPH 10. FOUND THAT PITCH DAMPER ONLY HAD A 400 PSI PRECHARGE. CURRENT LIMITS PER CHART FIG 11 IS 1300 PSI. RECHARGED PITCH DAMPER TO SERVICABLE LIMITS PER AMM 12-12-32-0. DECAY CHECK WITH NO PRESSURE DROP OVER A ONE HOUR PERI OD OF TIME PER SMP. A/C OK FOR CONTINUED SERVICE. 2 L 7 2 4F RT A35EU 2007021200071 20070212 00071 EU 2007 2 12 07FDEA00335 1 20070203 A 3230 DAMPER AIRBUS 300 A300B4622R 3930312 EU MLG DISCHARGED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 728FD 581 GEAR WOULD NOT RETRACT IN FLIGHT. SWITCHED POSITION DETECTORS, NO AVAIL. REFERENCE MTSI 32-30 / 1119. BWI MX, REMOVED AND REPLACED PROXIMITY DETECTOR UNIT 54GB AS PER A300 M/M 32-31-71-4. REMOVED AND REPLACED LT BOGIE PITCH DAMPER AS PE R A300 M/M 32-11-15-4. SERVICED PITCH DAMPER AS REQ'D. OK FOR SVC PER MTSI INSTRUCTIONS, PLACED A/C LDG GEAR RETRACT S YSTEM ON MEL, WITH L/G VOM/MMO SWITCH ACTIVATED TO LDG GEAR DOWN MEL (ITEM NBRS 32-30/1123 AND 32-60/1122). FLT TO MEM, MEM MX, PERFORMED GEAR SWING, CLOSED ALL ITEMS. 2 L 7 2 4F RT A35EU 2007021200072 20070212 00072 NM 2007 2 12 07FDEA00336 1 20070205 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 277 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 FLT DECK FLOORBEAM AT BS 277 UPPER SURFACE OF UPPER CHORD GOUGED AT LBL 14.5 BLEND DAMAGE, ORIGINAL THICKNESS .090'' AMO UNT REMAINING 0.075'' HFEC IAW EA# I070063, ROTO PEENED, TREATED, PRIMED, REF FED EX EA NR 7-5310-107610. 2 L 7 3 4F RT A3WE 2007021200073 20070212 00073 NM 2007 2 12 07FDEA00337 1 20070205 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 277 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 FLT DECK FLOORBEAM AT BS 277 HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE BETWEEN RBL 13 AND LBL 13. REMOVED CORROSI ON REF SRM 51-10-1 PG 5, MAT LOSS =.007'' HFEC, ROTO PEENED, TREATED, PRIMED, REF EA NR 7-5310-107610 AND AAR EA NR I 070063. 2 L 7 3 4F RT A3WE 2007021200074 20070212 00074 NM 2007 2 12 07FDEA00338 1 20070205 A 5410 STRUCTURE BOEING 727 727233 138408A NM NR 1 NACELLE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 NR 1 PYLON HOLE ''E'' IS CONICAL IN SHAPE AND ITS MAXIMUM HOLE DIAMETER IS OUT OF LIMITS. NDT HOLE, REAMED, FABRICATED CONICAL WASHER AND INSTALLED WASHER AND FASTENER REF WRI NR 54508487 AND EA NR 7-5450-106973. 2 L 7 3 4F RT A3WE 2007021200076 20070212 00076 NM 2007 2 12 SWAA070661 1 20070207 A 5755 FITTING BOEING 737 7373L9 1384470 NM NR 4 SPOILER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED C2 CHECK, FOUND LT WING NR 4 SPOILER OUTBOARD FITTING BROKEN. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007021200077 20070212 00077 NM 2007 2 12 SWAA070655 1 20070207 A 5755 654645262A HINGE FITTING BOEING 737 7373H4 1384600 NM NR 4 SPOILER LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED 122Y CHECK, FOUND LEFT WING NR 4 GROUND SPOILER CENTER HINGE ATTACH POINT LOOSE. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007021200078 20070212 00078 NM 2007 2 12 SWAA070648 1 20070207 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 847 S25R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, STR 25R. REMOVED AND REPLACED FRAME SECTION PER SR M. 2 L 7 2 4F RT A16WE 2007021200079 20070212 00079 NM 2007 2 12 SWAA070658 1 20070207 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007021200080 20070212 00080 NM 2007 2 12 SWAA070649 1 20070207 A 5315 6546811 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, RBL 30 TO RBL 35. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007021200081 20070212 00081 NM 2007 2 12 SWAA070650 1 20070207 A 5551 6551524 FITTING BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND RT AND LT HORIZONTAL STAB FITTING CLEVIS LUG FACES CORRODED. REPAIRED STAB FITTING PE R SRM. 2 L 7 2 4F RT A16WE 2007021200082 20070212 00082 NM 2007 2 12 SWAA070639 1 20070207 A 2120 65515752 DUCT BOEING 737 7373H4 1384600 NM A/C BAY CRACKED A SWAA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SW 29 378SW 26585 DIVERSION - F/A REPORTED EXHAUST FUME ODOR IN CABIN, TURNED GASPER AND RECIRC FANS OFF, NO HELP. FOUND RIGHT PACK DUCT CRACKED. REMOVED AND REPLACED DUCT PER MM. 2 L 7 2 4F RT A16WE 2007021200083 20070212 00083 NM 2007 2 12 SWAA070663 1 20070207 A 5512 65C25727 SKIN BOEING 737 7375H4 138449D NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED C4 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED AT AFT SPAR STA 87. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007021200084 20070212 00084 NM 2007 2 12 SWAA070651 1 20070207 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 787 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787. STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021200085 20070212 00085 NM 2007 2 12 SWAA070656 1 20070207 A 5755 69432271 ATTACH FITTING BOEING 737 7373H4 1384600 NM NR 6 SPOILER LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED 122Y CHECK, FOUND RIGHT WING NR 6 GROUND SPOILER ACTUATOR ATTACH POINT LOOSE. REMOVED AND REPLACED SPO ILER PER MM. 2 L 7 2 4F RT A16WE 2007021200086 20070212 00086 NM 2007 2 12 SWAA070664 1 20070207 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 404WN 27892 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 11 ABC. REMOVED & REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007021200087 20070212 00087 2007 2 12 SWAA070654 4 20070207 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007021200088 20070212 00088 NM 2007 2 12 SWAA070665 1 20070207 A 3350 PH22300L STRIP BOEING 737 7377H4 1384404 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 779SW 27884 DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 8 ABC TO ROW 11 ABC. REMOVED AND REPLACED ST RIP PER MM. 2 L 7 2 4F RT A16WE 2007021200089 20070212 00089 NM 2007 2 12 WRLA2007022 1 20070111 A 5320 AAA70881 FITTING DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE LONGERON CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 41081 48632 DURING 2C+12A+150M CHECK, MECHANIC FOUND CENTER ACCESS COMPARTMENT DOOR FWD AREA LONGERON 52L END FITTING CORRODED AT ST A Y=6-74.750 TO Y=6-90. FABRICATE THE NEW PARTS IAW E1 NR W2007P53B-029 REV.00 AND MFG DRAWING NR AAA7088. CONDITION C HECK NORMAL. (EGAT NRC NR U05084). 2 L 7 3 4F 4 F RT A22WE E24NE 2007021200090 20070212 00090 NM 2007 2 12 WRLA2007023 1 20070112 A 5313 ARB1567116171 LONGERON DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 41081 48632 DURING 2C+12A+150M CHECK, MECHANIC FOUND CENTER CARGO INTERNAL RT SIDE LONGERON CORRODED BETWEEN STA Y=1621 TO Y=1681 L3 8R. EGAT NRC U05086. PN ARB1567-1 AND ARB1617-1. 2 L 7 3 4F 4 F RT A22WE E24NE 2007021200091 20070212 00091 NM 2007 2 12 WRLA2007024 1 20070112 A 5313 ARB1567116171 LONGERON DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 41081 48632 DURING 2C+12A+150M CHECK, MECHANIC FOUND CENTER CARGO INTERNAL RT SIDE LONGERON CORRODED BETWEEN STA Y=1621 TO Y=1681 L3 9R. EGAT NRC U05086. PN ARB1567-1 AND ARB1617-1. 2 L 7 3 4F 4 F RT A22WE E24NE 2007021200092 20070212 00092 NM 2007 2 12 WRLA2007019 1 20070112 A 5315 AEA03971 FLOORBEAM DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE ZONE 100 CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 41081 48632 DURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND M/D CARGO FLOORBEAM CORRODED AT STA Y=1321,X= -8 TO -25 AREA. FABRICATED THE NEW PARTS IAW E1 NR W2007P53B-056 REV. 00 AND APPROVED DOCUMENT MFG CONTROL NR PO209366. INSTALLED THE NEW FABRICATE D PARTS IAW MD-11F SRM VOL II 51-35-01 REV.38. APPLY CHEMICAL PROTECTIVE COATINGS AND CONDITION CHECK NORMAL. EGAT NRC N R U05094. 2 L 7 3 4F 4 F RT A22WE E24NE 2007021200093 20070212 00093 EA 2007 2 12 TRAX200700130 1 20070130 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 753EV 10169 THE 2ND FROM AFT CEILING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007021200094 20070212 00094 NM 2007 2 12 WRLA2007020 1 20070106 A 5320 ANB75955 STIFFENER DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE WING TO BODY CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 41081 48632 DURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND FUSELAGE LT WING TO BODY FAIRING SUPPORT STIFFENER CORRODED AT STA Y=5-30, X=80 TO 100 AREA. ACCOMPLISHED REPAIR, THE STIFFENER CORROSION IAW EGAT E1 NR W2007P53B-054 REV 00 AND IAW MD-11F SRM 51 -35-01 REV.38 AND APPROVED DOCUMENT MFG MESSAGE NR 1-271697095-2. APPLY CHEMICAL PROTECTIVE COATING, CONDITION CHECK NO RMAL(EGAT NRC NR U05019). 2 L 7 3 4F 4 F RT A22WE E24NE 2007021200095 20070212 00095 NM 2007 2 12 WRLA2007021 1 20070111 A 5320 AAA70881 FITTING DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 41081 48632 DURING 2C+12A+150M CHECK, MECHANIC FOUND CENTER ACCESS COMPARTMENT DOOR FWD AREA LONGERON 51L END FITTING CORRODED AT ST A Y=6-74.750 TO Y=6-90. FABRICATED THE NEW PARTS IAW E1 NR W2007P53B-029 REV.00 AND MFG DRAWING NR AAA7088. CONDITION CHECK NORMAL. (EGAT NRC NR U05084). 2 L 7 3 4F 4 F RT A22WE E24NE 2007021200096 20070212 00096 SO 2007 2 12 N93A02022007 1 20070202 A 2810 16F123 VALVE GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU TANK VENT UNKNOWN E N93A A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 13 411QS 9593 1311 AFTER TAKEOFF, IT WAS NOTICED THAT FUEL WAS EXITING FROM RT WING TANK VENT. 2 L 7 2 4F 4 F RT A12EA E25NE 2007021200097 20070212 00097 2007 2 12 IXXA070004O 4 20070126 A 3422 FIBER OPTIC GYRO DOUG DC8 DC862 3021970 WP NR 2 PRECESSES A IXXA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 11 799AL 79529 140 45918 APPROXIMATELY 1.5 HOURS AFTER TAKEOFF FROM WSAP THE NR 2 COMPASS STARTED PROCESSING AT THE RATE OF 60° TO 70° PER HOUR, DG MODE PROCESSING AT THE RATE OF 25° PER HOUR. THE CREW ELECTED TO RETURN TO WASP AND LANDED WITHOUT INCIDENT. MAINT ENANCE FOUND AND CLEANED MOISTURE IN THE FIBER OPTIC GYRO CONNECTORS, WIRE BUNDLE BURNDY BLOCKS, BELOW GYROS AND LEFT FO RWARD SIDE OF THE GYRO BAY. MAINTENANCE ALSO CLEANED MOISTURE FROM THE WIRE SPLICE CONNECTORS ON THE GYRO SYSTEM. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2007021200098 20070212 00098 WP 2007 2 12 0700509992 1 20070201 A 2150 COUPLING DOUG DC9 DC931 3022065 WP ACM DETACHED A NWAA O OTHER O OTHER CR CRUISE 1 GL 01 896OE 45869 WHILE IN CRUISE FLIGHT AT 33,000 FEET, THE RED "CABIN PRESS" ANNUNCIATOR ILLUMINATED WHEN THE CABIN ALTITUDE REACHED 10, 000 FEET. CREW COMPLIED WITH COM PROCEDURES AND FOLLOWED THE RED BOARDED CHECKLIST. A DESCENT TO FL210 WAS PERFORMED W HERE THE CREW WAS ABLE TO REGAIN CONTROL OF CABIN PRESSURIZATION. THE AIRCRAFT REMAINED AT FL210 AND THE CABIN MAINTAIN ED AN ALTITUDE OF 9500 FEET FOR THE REST OF THE FLIGHT. THE LANDING AT MEM WAS NORMAL AND UNEVENTFUL. MAINTENANCE FOUN D A BLOWN DUCT COUPLING OFF THE RIGHT SIDE OF THE ACM, A BLOWN PERI-SEAL OFF THE LEFT SIDE OF THE CROSSOVER DUCT, AND SO ME OTHER DUCT LEAK DISCREPANCIES. ALL REPAIRS WERE COMPLETED, A LEAK CHECK OF THE SYSTEM WAS GOOD, AND THE AIRCRAFT HAS 2 L 7 2 4F A6WE 2007021200099 20070212 00099 2007 2 12 YENA2007007 4 20070206 A 2330 50402100001 VIDEO DISPLAY AIRBUS 320 A320232 3930326 EU ROW 20E ODOR A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 EA 15 585JB 2539 1439 2159 FLIGHT ATTENDANT - DETECTED A POSSIBLE SMOKEY ODOR AROUND ROW 20 PRIOR TO LANDING, C/W TSM NR 23-39-00-810-801. REMOVED AND REPLACED VDU AT 20E IAW LTV MM 23-39-00. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 2007021200100 20070212 00100 EA 2007 2 12 TRAX200700131 1 20070130 A 7810 ACCESS PANEL CNDAIR CL600 CL6002B19 1900309 EA EXHAUST NOZZLE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 833AS 7246 LEFT EXHAUST NOZZLE FAIRING ACCESS PANEL AT 6:00 POS INNER DOUBLER IS CRACKED. 2 L 7 2 4F RT A21EA 2007021200101 20070212 00101 EA 2007 2 12 TRAX200700132 1 20070130 A 7810 ACCESS PANEL CNDAIR CL600 CL6002B19 1900309 EA EXHAUST NOZZLE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 833AS 7246 LEFT EXHAUST NOZZEL FAIRING ACCESS PANEL AT 9:00 POS, INNER DOUBLERS IS CRACKED. 2 L 7 2 4F RT A21EA 2007021200102 20070212 00102 EA 2007 2 12 TRAX200700133 1 20070130 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 844AS 7317 AFT PRESSURE BULKHEAD IS CRACKED ADJACENT TO THE CARGO COMPARTMENT DOOR LINTEL ATTACHMENT FITTING. COMPLIED WITH N/R-0 0001 AFT PRESSURE BULKHEAD REPAIR AT LINTED ATTACH FITTING, IAW REO 601R-53-61-1230. COMPLIED WITH EC/TC REO 601R-53-61 -1230. 2 L 7 2 4F RT A21EA 2007021200103 20070212 00103 EA 2007 2 12 TRAX200700134 1 20070130 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 889AS 7538 EMERGENCY FLOOR LIGHT AT ENTRY DOOR LAMPS INOP. 2 L 7 2 4F RT A21EA 2007021200104 20070212 00104 EA 2007 2 12 TRAX200700135 1 20070130 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 924EV 7830 RECEIVED FLAPS FAIL WHEN SELECTING FLAPS FROM 0 TO 8 DEGREES. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007021200105 20070212 00105 EA 2007 2 12 TRAX200700136 1 20070131 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA CABIN DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 CREW EMERGENCY EXIT EXTERIOR EMERGENCY EXIT PLACARD FADED. REMOVED AND REPLACED CREW EMERGENCY ESCAPE HATCH PLACARD IAW CRJ 700 AMM 11-00. NO OTHER DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2007021200106 20070212 00106 EA 2007 2 12 TRAX200700137 1 20070131 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA O OTHER J WARNING INDICATION DE DESCENT 1 SO 27 840AS 7290 FLAPS FAIL MSG AT ZERO. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007021200107 20070212 00107 EA 2007 2 12 TRAX200700138 1 20070131 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION DE DESCENT 1 SO 27 840AS 7290 FLAPS FAIL AT 0. EMERGENCY EQUIPMENT ON STANDBY. CHANGED BPSU, PDU, LUBED FLEX CABLES, AND RIGGING FLAPS 2 L 7 2 4F RT A21EA 2007021200108 20070212 00108 EA 2007 2 12 TRAX200700139 1 20070131 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 857AS 7411 RECEIVED FLAPS FAIL ON APPROACH WHEN SELECTING FLAPS FROM 0 TO 8. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007021200109 20070212 00109 EA 2007 2 12 TRAX200700140 1 20070131 A 3250 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING UNKNOWN A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 856AS 7404 AFTER ROTATION -STEERING INOP- CAUTION. AFTER LANDING ROLLOUT TURNED ON NWS PER MX CTL. STEERING INOP MSG CAME ON AGAI N. EMERGENCY EQUIPMENT ON STANDBY. FLTS 4785, 4762 CX. 2 L 7 2 4F RT A21EA 2007021200110 20070212 00110 EA 2007 2 12 TRAX200700141 1 20070131 A 5300 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 379-977 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 CORROSION AND CHAFING ON LEFT AND RIGHT SIDE SEAT RAILS AS MARKED FROM FS 379.00 TO FS 977.00. 2 L 7 2 4F RT A21EA 2007021200111 20070212 00111 EA 2007 2 12 TRAX200700142 1 20070131 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 908EV 7654 STA 280 BULKHEAD WEB CRACKED AFT SIDE JUST OUTBOARD OF RBL 9 (MARKED). 2 L 7 2 4F RT A21EA 2007021200112 20070212 00112 EA 2007 2 12 REXA200700043 1 20070206 A 2611 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA LAVATORY UNKNOWN A REXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 8980A 7980 SMOKE IN TOILET CAUTION MSG DURING TAKEOFF. LANDING UNEVENTFUL. PERFORMED OPERATIONAL CHECK OF LAVATORY SMOKE DETECTOR IAW BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 26-16-00, OPERATIONALLY CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007021200113 20070212 00113 EA 2007 2 12 COMA0770013 1 20070202 A 2780 SLAT SYSTEM CNDAIR CL600 CL6002C10 1390015 EA MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 690CA 10182 FLIGHT 4994 - DURING CVG APPROACH RECEIVED A SLAT FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WIT HOUT INCIDENT. PERFORMED FIM PROCEDURE 27-81-09-810-A01, NO MESSAGES PRESENT. SLAT OPERATION SATISFACTORY. 2 L 7 2 4F RT A21EA 2007021200114 20070212 00114 NM 2007 2 12 ASMF200702001 1 20070203 A 3220 UNKNOWN DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NLG UNKNOWN W ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 161PL 49764 AIRCRAFT RETURNED, NOSE LANDING GEAR DID NOT RETRACT. LUBRICATION SERVICE TO NOSE LANDING GEAR STRUT WAS ACCOMPLISHED IA W MM 32-21-02. CABLES, PULLEYS AND CONNECTIONS WERE CHECKED AND LUBRICATION WAS ACCOMPLISHED, ALL CORRECT. OVER WEIGHT I NSPECTION WAS NOT NECESSARY DUE TO THE AIRPLANE LANDED WITH 121,583 POUNDS AND MAXIMUM LANDING WEIGHT IS 139,500 POUNDS. DURING OVERNIGHT CHECK, TEST WAS PERFORMED IAW MM 32-30-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007021200115 20070212 00115 NM 2007 2 12 WRLA2007030 1 20070208 A 5340 SUPPORT DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE HYD REGULATOR CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 62911 48407 DURING 3C + 12A CHECK, EGAT MECHANIC FOUND CRACK AT RIGHT W/W NR 3 HYD SYSTEM REGULATOR SUPPORT CRACK 2.5 INCHES. PERFO RM RT WW NR 3 HYD SYSTEM REGULATOR INTERCOSTAL SUPPORT CRACK REPAIRED PER ENGINEERING INSTRUCTION NR W2007A53-094 REV:00 & EI NR W2006 P20A-124 REV:00. 2 L 7 3 4F 4 F RT A22WE E24NE 2007021200116 20070212 00116 SO 2007 2 12 N93A08022007 1 20070208 A 2610 UNKNOWN GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU UNKNOWN E N93A H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 13 460QS 1360 SMOKE IN LAV CASS MESSAGE ILLUMINATED. MAINTENANCE WAS UNABLE TO DUPLICATE DISCREPANCY. POWERED UP ALL ACCESSORIES AND C HECKED DETECTION SYSTEM. ALL CHECKED GOOD. 2 L 7 2 4F 4 F RT A12EA E25NE 2007021200117 20070212 00117 NM 2007 2 12 07FDEA00381 1 20070208 A 5210 WEB BOEING 727 727233 138408A NM L1 DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 MAIN ENTRY DOOR L1, INTERNAL SKIN WEB DAMAGED LOCATED AFT EDGE JUST ABOVE 8TH STOP PIN FROM THE TOP. REMOVED DAMAGE, FA BRICATED REPAIR PIECES, TREAT, AND PRIMED AND INSTALLED REPAIR PARTS REF SRM 51-40-2. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007021200118 20070212 00118 NM 2007 2 12 07FDEA00382 1 20070208 A 5220 50797872 ANGLE BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 LT AFT OW EMERGENCY EXIT HATCH 5 EACH SEAL ANGLES ARE CORRODED BLENDED 4 EACH SEAL ANGLES AND FOUND WITHIN LIMITS AND TR EATED AND PRIMED. REMOVED AND REPLACED 1 EACH SEAL ANGLE REF SRM 51-10-6 PAGE 2, SRM 51-30-2 PAGE 2 AND SRM 51-10-1 PAG E 7. 2 L 7 3 4F RT A3WE 2007021200119 20070212 00119 NM 2007 2 12 07FDEA00383 1 20070208 A 5220 ANGLE BOEING 727 727233 138408A NM ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 RT FORWARD O/W EMERGENCY EXIT HATCH, 5 EACH SEAL ANGLES ARE CORRODED. VERIFIED ORIGINAL MATERIAL ON ALL 5 ANGLES TO BE .040". THE FOLLOWING ANGLES WERE OUT OF LIMITS: P/N'S 50-7978-65 AT .031", 50-7978-67 AT .029", 50-7978-72 AT .029". ANGLE P/N'S 50-7978-68 AT .032" AND 50-7978-71 AT .033" WERE WITHIN LIMITS. TREATED AND PRIMED REF SRM 52-00-2 FIG 1, MM 51-20-021-7, MM 51-20-031-7. 2 L 7 3 4F RT A3WE 2007021200120 20070212 00120 NM 2007 2 12 07FDEA00384 1 20070208 A 5220 50797826 ANGLE BOEING 727 727233 138408A NM ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 RT AFT WO EMERGENCY EXIT HATCH SEAL ANGLE HAS 5 EACH HOLES THAT ARE CRACKED OUT ALONG FWD EDGE OF HATCH. FABRICATED NEW SEAL ANGLE REF DWG 50-7978. TREATED AND PRIMED ANGLE REF SRM 51-10-2 AND MM 51-20-031-7 AND INSTALLED ANGLE REF SRM 51 -30-2. 2 L 7 3 4F RT A3WE 2007021200121 20070212 00121 NM 2007 2 12 07FDEA00385 1 20070208 A 5220 507978 ANGLE BOEING 727 727233 138408A NM ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 RT FWD O/W EMERGENCY EXIT HATCH SEAL ANGLE UPPER FORWARD CORNER 3 EACH HOLES ARE CRACKED OUT. REMOVED AND REPLACED 1 ANGLE. REMOVED, FABRICATED, HEAT TREATED AND PRIMED 1 ANGLE. REF SRM 51-30-2 PGS 1-7. REPAIR CLASSIFIED AS MAJOR. RE F SRM 51-10-2 PAGE 2. INSTALLED FABRICATED ANGLE REF SRM 51-30-2 PAGE 2, 50-7978-24 AND -26. 2 L 7 3 4F RT A3WE 2007021200122 20070212 00122 NM 2007 2 12 07FDEA00386 1 20070208 A 5220 507978 ANGLE BOEING 727 727233 138408A NM ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 LT AFT W/W EMERGENCY EXIT HATCH SEAL ANGLE FLANGE HAS 2 CRACKED OUT FASTENERS HOLES ONE LOCATED UPPER SEAL ANGLE, ANOT HER LOCATED LOWER AFT SEAL ANGLE. REMOVED AND REPLACED 1 ANGLE. REMOVED FABRICATED, HEAT TREATED, TREATED AND PRIMED 1 ANGLE REF SRM 51-30-2 PAGES 1-7. REPAIR CLASSIFIED AS MAJOR. INSTALLED FABRICATED ANGLE REF SRM 51-30-2 PAGE 2. 2 L 7 3 4F RT A3WE 2007021200123 20070212 00123 NM 2007 2 12 07FDEA00387 1 20070208 A 5230 INTERCOSTAL BOEING 727 727233 138408A NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 MAIN CARGO DOOR INTERCOSTAL IS CRACKED AT DOME NUT FOR UPPER BOLT TO FORWARD UPPER HOIST ATTACH POINT. INSTALLED NEW IN TERCOSTAL REF SRM 51-30-2 PAGE 2 ITEM 4B. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007021200124 20070212 00124 NM 2007 2 12 07FDEA00388 1 20070208 A 5230 WEB BOEING 727 727233 138408A NM CARGO DOOR TOOL DAMAGE A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 284FE 22621 MAIN CARGO DOOR UPPER AFT CORNER WEB BS.590-640 HAS MULTIPLE TOOLING MARKS ON INNER SURFACE REMOVED GILL LINER AND PARTI ALLY REMOVED INNER SKIN WEB FOR ACCESS. REMOVED REPAIR DOUBLER REF SRM 51-30-2, CUT OUT DAMAGE AREA REF. 51-10-1 HFEC C UT OUT, IAW B727 NDT MANUAL PART 6, 51-00-00, NO DEFECTS NOTED. FABRICATED FILLER REF SRM 51-40-02 FIGURE 1. ALODINED FILLER REF SRM 51-10-2 PAGES 6-7. PRIMED FILLER REF MM 51-20-031-7. INSTALLED FILLER, DOUBLER, INNER SKIN WEB AND CEIL ING SUPPORT COMMON TO WEB REF SRM 51-30-2. INSTALLED GILL LINER REF MM 25-52-00-2. ALSO WORKED WITH EA 7- 5330-106966 . CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007021200125 20070212 00125 NM 2007 2 12 07FDEA00389 1 20070209 A 5330 ACA3850501 SKIN DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LOWER FUSELAGE EXTERIOR, NR 1 AIRCON EXHAUST CUTOUT CORNER FOUND CRACKED. REPAIRED AS PER SRM 53-50-00 VOLUME I, FIGURE 16. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007021200126 20070212 00126 WP 2007 2 12 07FDEA00390 1 20070209 A 5711 SPAR DOUG MD10 MD1010F 3022112 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 372FE 46610 ON FRAME STA 1841 LEFT SIDE STRINGER 9L FOUND CRACK FROM ONE FASTNER HOLE THRU THE SECOND FASTENER HOLE (APROX 2"). REM OVED DOUBLER 2 CLIPS AND 2 INTERCOASTALS. RECEIVED FROM FAB ON T7/661087 AND T7/661086 2 DOUBLERS 7075T6 .080 T20631,19 3413. FAB 2 CLIPS FROM 60-19980 7075T6 8877871. LOCATED DRILLED REMOVED CRACK, TREATED AND PRIMED. INSTALLED 2 DOUBLE RS, 2 CLIPS AND 2 INTERCOASTALS IAW EA8-5310-102019. 2 L 7 3 4F RT A22WE 2007021200127 20070212 00127 EU 2007 2 12 U30A200700001 1 20070202 A 3350 32145420 POWER SUPPLY AIRBUS 320 A320214 3930316 EU EMERGENCY LIGHTS DISCHARGED A U30A K NONE L NO TEST IN INSP/MAINT 1 EA 17 269AV 2187 AT GATE - THE REAR EMERGENCY EXIT LIGHTS WILL NOT ILLUMINATE, BOTH LT AND RT SIDES. MAINTENANCE REPLACED EPSU (EMERGENCY POWER SUPPLY UNIT)13WL, IAW AMM 33-51-38PB401, OP'S CK'D OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2007021200128 20070212 00128 EA 2007 2 12 TRAX200700143 1 20070131 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 RIGHT & LEFT 280 BULKHEAD WEBS CRACKED. REMOVED AND REPLACED LT AND RT 280 BULKHEAD WEBS IAW IS 670531100026 AND SRM 51 -40-11 AND REO 670-53-11-052. 2 L 7 2 4F RT A21EA 2007021200129 20070212 00129 EA 2007 2 12 TRAX200700144 1 20070131 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 CENTER FS 280 FLOOR SUPPORT CRACKED AND CORRODED. COMPLIED WITH EO 700-53-0061 AND MODSUM IS67053110026. 2 L 7 2 4F RT A21EA 2007021200130 20070212 00130 EA 2007 2 12 TRAX200700145 1 20070131 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSLEAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 908EV 7654 FWD FLOOR SUPPORT ANGLE AT STA BETWEEN LBL 9 AND RBL 9 HAS SURFACE CORROSION. 2 L 7 2 4F RT A21EA 2007021200131 20070212 00131 EU 2007 2 12 TRAX200700146 1 20070201 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 PAX DOOR STAIR EMERGENCY FLOODLIGHT INOP. 2 H 7 2 4T RT 2007021200132 20070212 00132 EU 2007 2 12 TRAX200700147 1 20070201 A 2750 FLAP SYSTEM AEROSP ATR72 ATR72 EU TE FLAPS MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 27 641AS 387 DURING APPROACH AFTER SELECTING FLAPS 30 DEG RECEIVED FLAP UNLOCK WENT AROUND RAN QRH. EN ROUTE TO PEN A/C DIVERTED TO MGM. EMERGENCY DECLARED. FLT 4450 CX. 2 H 7 2 4T RT 2007021200133 20070212 00133 NM 2007 2 12 USAA070081 1 20070205 A 5347 415N40014 GALLEY TRACK BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 941UW 27806 AFT GALLEY RT OUTBOARD MOUNTS 2 EA HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER BOEING DWG 415N40C2; CORR LEVEL 1; TASK JL-58-5316, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A2NM 2007021200134 20070212 00134 NM 2007 2 12 USAA070080 1 20070205 A 5753 65C263207 SKIN BOEING 737 7374B7 1384702 NM TE FLAP CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 460UW 25024 OUTBOARD END OF LEFT WING OUTBOARD MID FLAP CHAFED. REMOVED DAMAGED AREA, INSTALLED DOUBLER PER SRM 57-53-03, DEFECT SI ZE: 1 X 2 INCHES. 2 L 7 2 4F RT A16WE 2007021200152 20070212 00152 NM 2007 2 12 07FDEA00374 1 20070208 A 5713 ARB75092 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 CRACK FOUND AT STRINGER END 9R (XORS 819), APPROX 11 INCHES LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. CRACK ON RT WING AT STRINGER END 9R (XORS 819) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007021200153 20070212 00153 WP 2007 2 12 07FDEA00375 1 20070208 A 5743 SUPPORT BEAM DOUG MD10 MD1010F 3022112 WP LT WING ROOT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 LT WING ROOT UPPER TE MLG SUPPORT BEAM UPPER SURFACE IS FRETTED AT WING PNL INTERFACE BS 938-944, SEE SNRM N00178. BLE NDED AREA REF SRM 51-10-03 FIG ITEM 7. TREATED AND PRIMED, AND TEFLON PAINTED AREA REF WRI 32108492 AND EA NR 7-32-7-10 7630. 2 L 7 3 4F RT A22WE 2007021200154 20070212 00154 CE 2007 2 12 2007F00018 1 20070201 A 2121 903840311 BLOWER MOTOR BEECH 90 C90 1152913 CE PWA PT6 PT6A21 52043 EA HARTZL HCE4N HCE4N3 NE VENT SEIZED E A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 25 326PT 1446 1446 LJ1581 PCEPE02810 HH2359HH794 VENT BLOWER ASSEMBLY SEIZED DURING FLIGHT CAUSING SMOKE IN THE COCKPIT. UNIT IS A PART THAT IS CHANGED (ON CONDITION). PART HAS BEEN ON AIRCRAFT SINCE NEW. 1 L 7 2 3T 4 T 3A20 E4EA 5 C P10NE 2007021200155 20070212 00155 EA 2007 2 12 REXA200700044 1 20070207 A 2611 SMOKE WARNING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LAVATORY ACTIVATED A REXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 8970D 7970 TOILET SMOKE MESSAGE AFTER TAKEOFF, PILOT DELCARED EMERGENCY, PERFORMED QRH, LANDING UNEVENTFULL. DEFERRED APU IAW MEL. 2 L 7 2 4F 4 F RT A21EA E15NE 2007020700095 20070207 00095 NM 2007 2 7 SWAA070555 1 20070202 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 360 S26L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 26L. REPAIRED SHEAR TIE PER ER. 2 L 7 2 4F RT A16WE 2007020700106 20070207 00106 CE 2007 2 7 AM1070103027 1 20070106 A 5540 SUPPORT BEAM BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RUDDER DAMAGED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 146ZV UE146 PROBLEM DISCOVERED DURING MAINTENANCE INSPECTION. RUDDER BELLCRANK SUPPORT BEAM REPAIRED IAW AERODESIGN AIRCRAFT ENGINE ERING, INC REPORT NR 6496-1 REV. 1 SHEET 1 THROUGH 33. DATED 01/04/2007. 2 L 7 2 4T 4 T RT A24CE E26NE 2007020700107 20070207 00107 SO 2007 2 7 C2XA07TY003 1 20070205 A 3220 LANDING GEAR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NOSE UNKNOWN A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14568 145628 THIS WAS AN AIR RETURN ON A REPO FLIGHT FOR A LANDING GEAR AIR/GROUND FAIL MESSAGE AND A T/R DISAGREE MESSAGE. MAINTENAC E SERVICED THE NLG IAW AMM 32-20-01. OPS CHECKED GOOD AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007020700109 20070207 00109 NM 2007 2 7 2007UALA00216 1 20070126 A 3260 UPLOCK SENSOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU MLG FAULTED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 336UA 24240 RTFL DUE TO A LANDING GEAR INDICATION. FOUND FAULTY LOCK SENSOR. REPLACED LOCK SENSOR PER AMM 32-61-41. 2 L 7 2 4F 4 F RT A16WE E21EU 2007020700113 20070207 00113 NM 2007 2 7 AALA20070144 1 20070121 A 2530 COFFEEMAKER BOEING 777 777223 1385213 NM GALLEY INOPERATIVE A AALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 SW 21 792AN 30253 LHR INLIGHT - SMOKE CREW REST MAIN MESSAGE ILLIMINATED AND FLIGHT ATTENDANT ADVISED A STRONG ODOR AND HIGH TEMPERATURE W AS IN THE AREA OF COFFEEMAKERS 10, 11, 12, AND 13. COFFEEMAKERS WERE IMMEDIATELY SHUT OFF AND THE ODOR AND HEAT SUBSIDE D. LANDED LHR WITHOUT INCIDENT. INSPECTED AREA BEHIND COFFEEMAKERS AND ABOVE CREW REST WITH NO EVIDENCE OF SMOKE OR BU RNING. REPLACED NUMBER 10, 11, 12, AND 13 COFFEEMAKERS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007020700118 20070207 00118 NM 2007 2 7 2007UALA00219 1 20070126 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 947 S24L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 LOWER FUSELAGE SKIN EXTERIOR SKIN CRACKED AT STA 947 STR 24L. MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER PER SRM 53-00-01 REPAIR 31 DETAIL VIII. 2 L 7 2 4F 4 F RT A16WE E21EU 2007020700119 20070207 00119 NM 2007 2 7 2007UALA00220 1 20070126 A 5510 CLEVIS BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZONTAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 LEFT HORIZONTAL STAB CENTER SECTION FWD CLEVIS LOWER AFT LUG CORRODED. MAJOR REPAIR: REMOVED BUSHING AND REMOVED CORRO SION. SPOT FACED PER EA I070072 REV IR AND INSTALLED THE BUSHING. 2 L 7 2 4F 4 F RT A16WE E21EU 2007020700130 20070207 00130 NM 2007 2 7 AALA20070149 1 20070121 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 602AN 27053 MIA - FOUND EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A2NM 2007020700139 20070207 00139 NM 2007 2 7 AWXA200700138 1 20070122 A 5340 69353502 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND STRINGER CLIP CRACKED, BS 500A, S16R. REPLACED STRINGER CLIP, BS 500A, S16R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020700141 20070207 00141 NM 2007 2 7 UPS07449096 1 20070109 A 5313 STRINGER BOEING 747 747123 1384873 NM BS 920-930 S28L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT STRINGER FOUND CORROSION AT STA 920-930 S28L. CORROSION BLEND OUT 0.035 X .5 X 10 INC HES EXCEED SRM LIMIT. STRINGER 28L REPAIRED AS PER SRM 53-10-01 FIG 1, JUST BETWEEN BS 890-950. 2 L 7 4 4F A20WE 2007020700143 20070207 00143 NM 2007 2 7 UPS07449098 1 20070110 A 5313 STRINGER BOEING 747 747123 1384873 NM BS 2150-2160 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C BULK CARGO COMPT STRINGER FOUND CORRODED AT STA 2150 TO 2160 S31L. CORROSION BLEND OUT 0.080 X .375 X 1.5 INCH EXCEED SRM LIMIT. STRINGER 31L REPAIRED AS PER SRM 53-10-03 FIG 2, JUST BETWEEN BS 2156 AND BS 2170. 2 L 7 4 4F A20WE 2007020700144 20070207 00144 NM 2007 2 7 UPS07449099 1 20070110 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM BS 957-964 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT RIGHT SIDE SEAT TRACK LWR SURFACE FOUND CORROSION AT STA 957 TO 964 RBL 45. CORROSION BLEND OUT 0.045 X .5 X 7 INCHES EXCEED SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 5, JUST AT RBL 45 BETWEE N BS 930 AND 967. 2 L 7 4 4F A20WE 2007020700164 20070207 00164 NM 2007 2 7 UPS07449081 1 20070111 A 5340 65B15085329 ANGLE BOEING 747 747123 1384873 NM BS 1480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C AFT CARGO COMPT STA 1480 BULKHEAD LOWER ANGLE FOUND CORRODED AT LBL 25. CORROSION BLEND OUT 0.053 X . 5 X 2 INCHES EXCEED SRM LIMIT. ANGLE REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007020700167 20070207 00167 NM 2007 2 7 UPS07449084 1 20070103 A 5740 ATTACH ANGLE BOEING 747 747123 1384873 NM LT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LEFT WING - NOSE UPPER CHORD ATT ANGLE AT WS 1112 FOUND CRACKED. CRACK LENGTH 1.125 INCH. LEFT WING NOSE UPPER CHORD REPAIRED AS PER SRM 57-20-03 FIG 7. 2 L 7 4 4F A20WE 2007020700171 20070207 00171 NM 2007 2 7 ZZDA070123100 1 20070123 A 5350 RADOME BOEING 717 717200 1383700 NM BS 37 CRACKED A ZZDA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. RIGHT AND LEFT RADOME LATCH ASSEMBLIES AND FORWARD LOWER SKIN CRACKED AN D BROKEN BEYOND REPAIR. REPLACED RIGHT AND LEFT RADOME LATCH ASSEMBLIES AND FORWARD LOWER SKIN AT STA 37.0 PER MDC DRAW ING 5911400 REV CM DATED 05/03/01. 2 L 7 2 4F TR A6WE 2007020700179 20070207 00179 NM 2007 2 7 ZZDA070123108 1 20070123 A 5310 STRUCTURE BOEING 717 717200 1383700 NM BS 110 CRACKED A ZZDA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. TEE CAP AT STA 110 CRACKED AND BENT BEYOND REPAIR. REPAIRED TEE CAP AT STA 110 PER MDC DRAWING 9911509 REV L DATED 5/13/02 AND PER BOEING ENGINEERING ROD/SKETCH NUMBER 06-12-10-003-001, 8100- 9 APPROVED ON 01-07-07. 2 L 7 2 4F TR A6WE 2007020700183 20070207 00183 NM 2007 2 7 CALA0700049 1 20070101 A 5315 FLOORBEAM BOEING 737 737724 13844BY NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16732 28948 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 25.5. REPAIRED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 2007020700192 20070207 00192 NM 2007 2 7 DU4R2007037 1 20070124 A 5320 INTERCOSTAL BOEING 757 757232 1384965 NM BS 1400-1420 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION ON INTERCOSTAL WEB BS 1400 TO BS 1420 LBL 3 ON LOWER LEG. REMOVED CORRODED INTERCOSTAL WEB. FABRICATED AND I NSTALLED REPAIR WEB 19.5" BY 8.6" FROM 7075-T6 .032" IAW B757 SRM 53-60-04, 51-30-01 AND 51-40-02. 2 L 7 2 4F RT A2NM 2007020700196 20070207 00196 NM 2007 2 7 DU4R2007042 1 20070122 A 5320 PANEL BOEING 757 757232 1384965 NM BS 1530-1640 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 CORROSION ON UPPER SURFACE OF AFT PIT RT TRANSITION PANEL FROM BS 1530 TO BS 1640. CUT OUT CORRODED AREA. FABRICATED A ND INSTALLED DOUBLER 16.0" BY 5.0" FROM 7075-T6 .063" IAW B757 AMM 53-88-01-801, B757 SRM 51-20-01, 53-00-53, 53-60-53 A ND 51-40-05. 2 L 7 2 4F RT A2NM 2007020700198 20070207 00198 NM 2007 2 7 ZZDA070123112 1 20070123 A 5311 FRAME BOEING 717 717200 1383700 NM BS 133 DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. LOWER FRAME AT STA 133.4 DAMAGED. REPLACED LOWER FRAME AT STA 133.4 PER MDC DRAWING 9911512 REV T DATED 09-01-99. 2 L 7 2 4F TR A6WE 2007020800002 20070208 00002 NM 2007 2 8 SWAA070617 1 20070206 A 3233 65448106 ACTUATOR BOEING 737 7373H4 1384600 NM MLG FAULTY A SWAA O OTHER J WARNING INDICATION CL CLIMB 1 SW 29 636WN 27709 LEFT MLG UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF. CYCLED GEAR NO HELP. LEFT MLG DID NOT RETRACT. REMOVED AND REPLACED LEFT MLG RETRACT ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2007020900002 20070209 00002 EA 2007 2 9 TRAX200700161 1 20070203 A 2741 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA PITCH TRIM UNKNOWN A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 930EV 8014 PITCH TRIM RAN AWAY WHILE HAND FLYING AFTER T/O. DISCONNECTED TRIM, TRIM RAN NOSE DOWN 2.6 DEGREES. AIRCRAFT RETURNED TO ABE AFTER T/O. EMERGENCY EQUIPMENT ON STANDBY. 2 L 7 2 4F RT A21EA 2007020900003 20070209 00003 EA 2007 2 9 TRAX200700162 1 20070203 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 937EV 8042 LEFT OVERWING EMERGENCY LIGHTS INOP. 2 L 7 2 4F RT A21EA 2007020900005 20070209 00005 SO 2007 2 9 C2XA07CL020 1 20070207 A 3241 15622101 SWITCH EMB 145 EMB145LR 3260212 SO BRAKE SYSTEM LEAKING A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 27 14960 145100 EWR FLIGHT 2996 THE CREW REPORTED HYDRAULIC SYSTEM NR 2 FAILURE. TOTAL LOSS OF SYSTEM NR 2 FLUID. THE AIRCRAFT DIVERTE D INTO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE NR 2 SYSTEM BRAKE PRESSURE SWITCH L EAKING. THE SWITCH WAS REPLACED AND THE HYDRAULIC SYSTEM WAS SERVICED. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007020900006 20070209 00006 NM 2007 2 9 AMTA200700048 1 20070201 A 4900 UNKNOWN BOEING 737 73783N 13844HI NM APU UNKNOWN A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 317TZ 28246 APU LIGHT ON WHEN RECALL PUSHED WHEN APU IS RUNNING. PERFORMED MASTER CAUTION RESET PER FIM 31-52-00-810-801. FAULT CL EARED, NO FURTHER DEFECTS NOTED. (M) 2 L 7 2 4F RT A16WE 2007020900014 20070209 00014 NM 2007 2 9 SWAA070625 1 20070206 A 5743 6582770 FITTING BOEING 737 7373H4 1384600 NM LT MLG SUPPORT CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND LEFT MLG SUPPORT BEAM AFT STAB FITTING CORRODED. REMOVED AND REPLACED AFT STAB FITTIN G PER MM. 2 L 7 2 4F RT A16WE 2007020900023 20070209 00023 2007 2 9 F3LA200700021 4 20070206 A 2565 60592101 RESERVOIR AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE EMERGENCY SLIDE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 5911 1943 DURING C-3 CHECK, INSPECTION REPORTED CABLE END ON LT OVERWING EMERGENCY SLIDE INFLATION BOTTLE BROKEN OFF. REPLACED LT INFLATION RESERVOIR OVER-WING ESCAPE SLIDE IAW AMM 25-62-46-000-001 AND 25-62-46-400-001. CONNECTED LT OVERWING ESCAPE SLIDE CABLE IAW 25-62-43-400-001. 2 L 7 2 4F 4 F RT A28NM E37NE 2007020900024 20070209 00024 EA 2007 2 9 COMA0760128 1 20070204 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 973CA 7146 FLIGHT 5256 - DURING DESCENT INTO YYZ RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007020900033 20070209 00033 NM 2007 2 9 WRLA2007017 1 20070111 A 5347 AEA73255 SEAT TRACK DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 41081 48632 DURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND MAIN DECK CARGO SEAT TRACK FLANGE CORRODED AT STA Y=1329, X=29. CUT AND F ABRICATE REPAIR THE CORRODED SEAT TRACK SECTION AND SPLICE HAT PER MD-11F SRM VOL 1 53-70-00 REV 38. CONDITION CHECK NO RMAL. (MAJOR REPAIR). 2 L 7 3 4F 4 F RT A22WE E24NE 2007020900048 20070209 00048 CE 2007 2 9 AMWA82479BC 1 20070205 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER DISCHARGED A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 126YV 13799 448 UE126 BATTERY CHARGE LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED BATTERY TO CLEAR THE DISCREPANCY. THIS BATTERY CHARGE LIGHT ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS. 2 L 7 2 4T 4 T RT A24CE E26NE 2007020900049 20070209 00049 EA 2007 2 9 COMA0760140 1 20070205 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 987CA 7199 FLIGHT 4936 - DURING ALB APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAG E -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007020900058 20070209 00058 NM 2007 2 9 EIA2007001 1 20070105 A 2612 30284R9B SMOKE DETECTOR BOEING 747 747230B 1384889 NM CARGO BAY MALFUNCTIONED A EIAA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 487EV 23286 FIRE BELL SOUNDED 3 TIMES DURING LEVEL FLIGHT, ACCOMPANIED WITH WARNING LIGHTS ON P-10 AND P-12 PANELS, AND MAIN DECK CA RGO SMOKE DETECTOR NR 5 ON FE P-4 UPPER." TRANSFERRED TO DMI.328. REMOVED AND REPLACED NR 5 A AND B SMOKE DETECTORS AND SMOKE DETECTOR AMP NR 5, OPS CHK PER MM 26-14-02 AND PERFORMED SMOKE DETECTOR WIRING CONNECTION TEST, NO FAULTS FOUND P ER MM 26-14-00. 2 L 7 4 4F A20WE 2007020900064 20070209 00064 CE 2007 2 9 DXTA200701914 1 20070201 A 3230 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LANDING GEAR UNKNOWN E DXTA A UNSCHED LANDING S J AFFECT SYSTEMS WARNING INDICATION CL CLIMB 1 GL 07 950QS 7500050 AFTER TAKEOFF, GEAR DID NOT RETRACT. SHORTLY THERE AFTER RECEIVED (HYD PUMP FAIL A) CAS MESSAGE. SECONDS LATER THE (PT U FAIL) CAS MESSAGE BEGAN CYCLING. WHILE RUNNING THE (HYD PUMP FAIL A) CHECKLIST THE GEAR RETRACTED ON ITS OWN AND THE CAS MESSAGES EXTINGUISHED. THE HYDRAULIC QUANTITY WAS 95 PERCENT (LT SIDE) AND 81 PERCENT IN FLIGHT. THE HYDRAULIC A PS I WAS 300 PSI DURING THE CAS MESSAGES ILLUMINATION. GEAR CYCLED DOWN OK AND ALL SYSTEM OPERATED NORMAL FOR LANDING AFTE R PUMP AND PTU STARTED WORKING AGAIN. ACCOMPLISHED HYD SYS A AND B SYS BLEED IAW MM 12-10-00. ACCOMPLISHED LT AND RT B RAKES BLEED IAW MM 32-42-00. LEAK AND OPS CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007020900112 20070209 00112 EU 2007 2 9 07FDEA00330 1 20070205 A 5310 CROSSBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 CORRODED CROSS BEAM AT C57.2 LT / AD AND C61 RT/AD. REPAIR WAS PERFORMED IAW SRM 53-10-15, FIG 208 AT CROSSBEAM 57.2 AN D IAW SRM 53-10-15, FIG 207 AT CROSSBEAM C61. 2 L 7 2 4F RT A35EU 2007020900113 20070209 00113 NM 2007 2 9 07FDEA00331 1 20070205 A 5330 SKIN BOEING 727 727233 138408A NM BS 1422 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 EXTERNAL FUSELAGE, STA 1422 LT SIDE. SKIN DENTED 4.0'' BELOW VERTICAL FIN Y=.080'' A=1.25'' A/Y = 15, REMOVED DAMAGE, FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR, REF SRM 51-40-2, PG 1-6. 2 L 7 3 4F RT A3WE 2007021200009 20070212 00009 WP 2007 2 12 ASMF200702002 1 20070203 A 5330 SKIN DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE BS 198 S20-21L DAMAGED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 216AM 49586 DURING OVERNIGHT CHECK AND ACCOMPLISHMENT OF EO 985362, A CRACK OF .1250 LENGTH AT STA Y 198 BETWEEN LONGERONS L20L AND L21L, WAS DETECTED ON THE MAIN STAIRS DOOR. DAMAGED SKIN SECTION WAS REMOVED AND A DOUBLER (PERMANENT REPAIR) WAS INSTAL LED IAW SRM 53-05 FIGURE 57A CONFIGURATION 7001, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007021200011 20070212 00011 EA 2007 2 12 VNAA0701006 1 20070122 A 5230 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE CARGO BAY UNSECURE A VNAA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 GL 05 716PS 10171 CREW REPORTED THE AIRCRAFT WOULD NOT PRESSURIZE AFTER DEPARTING ALBANY. CREW DIVERTED TO DAY AND LANDED WITHOUT INCIDEN T. MAINTENANCE INSPECTED AND FOUND THE AFT CARGO DOOR NOT PROPERLY CLOSED. CARGO DOOR WAS INSPECTED IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 52-31-00-220-801. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007021200018 20070212 00018 NM 2007 2 12 AWXA200700186 1 20070207 A 5753 6546431255 SKIN BOEING 737 73733A 1384673 NM FORE FLAP DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 PHX - LEFT WING OUTBOARD FOREFLAP HAS A DISBONDED AREA MIDSPAN, WBL 246.50 - WBL 354.70. REPLACED LEFT WING OUTBOARD FO REFLAP IAW AWA TASK CARD R3M27022. 2 L 7 2 4F RT A16WE 2007021200025 20070212 00025 CE 2007 2 12 GLBA20060890 1 20070205 A 5730 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RT WING DAMAGED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 192GL UE192 RT WING SKIN TRAILING EDGE RIVETS LOOSE AND RIVET HOLES ELONGATED AT TRAILING EDGE BETWEEN WS 124.6 TO WS 136.6. 2 L 7 2 4T 3 T RT A24CE E2NE 2007021200026 20070212 00026 CE 2007 2 12 GLBA20060889 1 20070201 A 5340 ANGLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA WING TO FUSELAGE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 192GL UE192 RT WING TO FUSELAGE CLOSING ANGLE CRACKED AT FS 288.0. CRACK 1.750 INCHES IN LENGTH. 2 L 7 2 4T 3 T RT A24CE E2NE 2007021200032 20070212 00032 GL 2007 2 12 DL764070087 2 20070206 A 7200 CF680C2B8F ENGINE BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 1 FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 832MH 17798 29704 706433 ENGINE FAILED OPN 5039 BORO. NR 1 ENG S/N 706433 REMOVED PER TRANSMITTAL 14T103. INSTALLED NR1 ENG S/N PER TRANS 14T10 3. 2 L 7 2 4F 4 F RT A1NM E23EA 2007021200157 20070212 00157 NM 2007 2 12 ASAA0741431 1 20070202 A 5242 6545830131 SKIN BOEING 737 737490 1384715 NM E/E BAY DOOR PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 713AS 30161 E&E COMPARTMENT DOOR PUNCTURED AT EXTERNAL SKIN REPAIRED PER SRM 52-00-01 FIG 201. 2 L 7 2 4F RT A16WE 2007021200158 20070212 00158 NM 2007 2 12 ASAA0741432 1 20070202 A 5347 655384421 CARGO TRACK BOEING 737 737490 1384715 NM BS 787 WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 713AS 30161 AFT CARGO PIT TIE DOWN TRACK WORN. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2007021200159 20070212 00159 NM 2007 2 12 ASAA0741433 1 20070202 A 5330 65C457921 SKIN BOEING 737 737490 1384715 NM GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 713AS 30161 FUSELAGE SKIN GOUGED WHERE DORSAL FIN SITS. REPAIRED PER EA 5330 02178. 2 L 7 2 4F RT A16WE 2007021200160 20070212 00160 NM 2007 2 12 ASAA0741434 1 20070202 A 5311 6545808244 FRAME BOEING 737 737490 1384715 NM BS 2945 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 713AS 30161 FUSELAGE FRAME CRACKED ON LWR FLANGE. REPAIRED WITH REPAIR PART PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007021200161 20070212 00161 NM 2007 2 12 ASAA0741435 1 20070203 A 5330 65C32355 SKIN BOEING 737 7374Q8 138447Q NM BS 460-480 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 763AS 25100 FUSELAGE EXTERIOR DENTS. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 53-00-01 FIG 201 DETAIL X. 2 L 7 2 4F RT A16WE 2007021200162 20070212 00162 NM 2007 2 12 ASAA0741436 1 20070204 A 5330 65C32355 SKIN BOEING 737 7374Q8 138447Q NM BS 490-510 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 763AS 25100 FUSELAGE SKIN PANEL DENTED 2.5 INCHES FROM EXISTING REPAIR. REMOVED EXISTING REPAIR INSTALLED NEW REPAIR IAW PEMCO EA P D37 53 693C AND ASA EA 5330 02514. 2 L 7 2 4F RT A16WE 2007021200163 20070212 00163 NM 2007 2 12 ASAA0741437 1 20070201 A 5753 6546486144 SKIN BOEING 737 737490 1384715 NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 THE LEFT WING I/B MIDFLAP T/E IS DENTED AND GOUGED AT THE AFT EDGE ON THE LWR SURFACE. PREPARED THE LWR SKIN FOR BONDIN G, APPLIED POTTING COMPOUND, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 12, 15, 18 AND 20. 2 L 7 2 4F RT A16WE 2007021200164 20070212 00164 NM 2007 2 12 ASAA0741438 1 20070201 A 5753 654643583 SKIN BOEING 737 737490 1384715 NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 THE RIGHT WING O/B AFT FLAP HAS A LARGE DENT JUST BELOW THE SECOND CARRIGE FROM THE O/B END. REMOVED THE DAMAGED AREA O F LWR SKIN AND CORE FABRICATED AND INSTALLED A CORE PLUG SKIN FILLER AND TWO REPAIR DOUBLERS IAW SRM 51-70-10 PARA 7, 8, 9, 11, 15, 18 AND 20. 2 L 7 2 4F RT A16WE 2007021200165 20070212 00165 NM 2007 2 12 ASAA0741439 1 20070205 A 5753 65C3570516 SKIN BOEING 737 737490 1384715 NM TE FLAP PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 THE RIGHT WING O/B FORE FLAP IS PUNCTURED ON THE LWR SURFACE NEAR THE I/B END. REMOVED DAMAGED AREA OF LWR SKIN, FABRIC ATED AND INSTALLED A SKIN FILLER AND A REPAIR DOUBLER IAW SRM 51-70-10 APRA 7, 11, 15, 18 AND 20. 2 L 7 2 4F RT A16WE 2007021200166 20070212 00166 NM 2007 2 12 ASAA0741441 1 20070205 A 5753 654645137 SKIN BOEING 737 737490 1384715 NM TE FLAP PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 RIGHT WING NR 6 SPOILER SURFACE IS PUNCTURED 8 INCHES FROM THE T/E, 12 INCHES FROM THE O/B EDGE (UPPER SURFACE). PREPPE D THE DAMAGED AREA OF UPPER SKIN FOR BONDING, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 51-70-10 REPAIR 2. 2 L 7 2 4F RT A16WE 2007021200167 20070212 00167 EA 2007 2 12 COMA0760122 1 20070202 A 3297 TR17300600000 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA RT MLG FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 918CA 7018 FLIGHT 5020 - DURING TAXI-OUT TO THE RUNWAY RECEIVED AN ANTI-SKID CAUTION MESSAGE, AIRCRAFT RETURNED TO THE GATE. REPLA CED THE RIGHT MLG OUTBOARD TRANSDUCER WIRING HARNESS. 2 L 7 2 4F RT A21EA 2007021200168 20070212 00168 EA 2007 2 12 COMA0760127 1 20070204 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 924CA 7026 FLIGHT 5149 - DURING CVG APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WIT HOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007021200169 20070212 00169 EU 2007 2 12 UPS07149122 1 20070203 A 5210 LEVER AIRBUS A300 A300F4622R 3930360 EU PAX DOOR STICKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 140UP 0823 CREW ENTRY DOOR ARMING LEVER CATCHES APPROX 2" FROM THE DISARMED POSITION WHEN MOVING LEVER FROM ARMED TO DISARMED. C/W FUNCTIONAL TEST NOTED TO OPERATE NORMAL IN REF TO AMM 52-10-30. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2007021200170 20070212 00170 EU 2007 2 12 UPS07149123 1 20070204 A 5210 HANDLE AIRBUS A300 A300F4622R 3930360 EU PAX DOOR STICKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 140UP 0823 WHEN DISARMING MAIN ENTRANCE DOOR ITS HANDLE HANGS UP STARTING AT THE GREEN DISARM BAND. REPEAT WRITE UP. CLEANED AND LUBED FLOOR FITTING FOR GIRT BAR. PERFORMED FUNCTIONAL TEST FWD ENTRY DOOR SLIDE MECHANISM AS PER MM 52-10-30-05. CKS GOOD. 2 L 7 2 4F RT A35EU 2007021200171 20070212 00171 EU 2007 2 12 UPS07149124 1 20070204 A 5220 HANDLE AIRBUS A300 A300F4622R 3930360 EU CO-PILOT WINDOW MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 140UP 0823 ON TAXI OUT, CO-PILOTS WINDOW SAFE INDICATION POPPED UP TO UNSAFE. THE RED UNSAFE INDICATOR WILL NOT STOW. RESEATED OU TSIDE EMERGENCY ESCAPE SLIDE HANDLE WINDOW. CKS GOOD. 2 L 7 2 4F RT A35EU 2007021200172 20070212 00172 NM 2007 2 12 UPS07449116 1 20070109 A 5310 69B122411 DOUBLER BOEING 747 747123F NM MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C L/G - LT WLG W/W AT BS1245 LBL0 HYD TUBE CUTOUT DOUBLER FOUND CORRODED CRACKED. CORROSION BLEND OUT 0 .045" BY 1/2" BY 4" EXCEED SRM LIMIT. DOUBLER REPLACED AS PER SRM 51-10-01 P9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007021200173 20070212 00173 NM 2007 2 12 UPS07449117 1 20070131 A 5330 SKIN BOEING 747 747123 1384873 NM BS 203 PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FX- BS 203 RBL 3" EXTERIOR SKIN FOUND PUNCTURED, CRACK LENGTH 1/2". FX EXTERIOR SKIN REPAIRED AS PER SRM 53-30-03 FIG 1, JUST BETWEEN BS 195 AND 208 STR -1L AND STR -1R. 2 L 7 4 4F A20WE 2007021200174 20070212 00174 NM 2007 2 12 UPS07449121 1 20070206 A 2520 PANEL BOEING 747 747212B 1384886 NM CABIN MISINSTALLED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 520UP 21943 FOUND EMERGENCY LIGHT M301 INOP. FOUND CEILING PANEL INSTALLED IN WRONG LOCATION. SWAP TO CORRECT. SWAPPED CEILING PA NELS, HOOKED UP CORRECT C/P TO EMERG LIGHT MODULE. OPS CK GOOD. 2 L 7 4 4F A20WE 2007021200201 20070212 00201 EU 2007 2 12 R61A20070001 1 20070125 A 2913 5116402 PUMP EMB ERJ170 ERJ170100 EU GE CF34 CF348E5 30015 NE HYDRAULIC SYSTEM CRACKED A R61A O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 11 828MD 3661 17000048 CREW REPORTED ON APPROACH THEY HAD AN EICAS MESSAGE HYDRAULIC QUANTITY 2 LOW. THEY FOLLOWED QRH AND LANDED WITHOUT INCID ENT TAXIED TO THE GATE. MAINTENANCE WAS DISPATCHED TO THE AC AND FOUND NUMBER 2 ENGINE HYDRAULIC PUMP LEAKING. MAINTENAN CE REPLACED PUMP AND RETURNED AC TO SERVICE. 2 L 7 2 4F 4 F RT A56NM E00063EN 2007021200202 20070212 00202 SO 2007 2 12 ECI10513 1 20070121 A 2751 1159SCC2121 SWITCH GULSTM G1159 GIV 3980115 SO GE CF34 CF348E5 30015 NE FLAP ASYMMETRY MISALIGNED E E0XA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 35 919CT 1051 FLAPS WILL NOT RETRACT AFTER LANDING. FLAP ASYMMETRY SWITCHES FOUND TO BE OUT OF ADJUSTMENT. 2 L 7 2 4F 4 F RT A12EA E00063EN 2007021200204 20070212 00204 EU 2007 2 12 0700513227 1 20070206 A 3260 UPLOCK SENSOR AIRBUS 320 A320211 3930320 EU LT MLG MALFUNCTIONED A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 327NW 297 AT FLIGHT LEVEL 370, ECAM MSG: L/G DOORS NOT CLOSED, WHEELS PAGE INDICATED ALL THREE GEAR DOORS OPEN. ECAM THEN INDICAT ED ALL GEAR DOORS OPEN AND LEFT GEAR UNSAFE. AIRCRAFT DESCENDED TO FLIGHT LEVEL 200 AND 215 KNOTS, TO PERFORM COM RECYC LE PROCEDURE. BEFORE ATTEMPTING COM, THE GEAR DOORS CLOSED AND INDICATIONS WERE NORMAL. FLIGHT CONTINUED TO MSP AT LOW ER THAN PLANNED ALTITUDE, UNDER EXPEDITED ATC HANDLING DO TO INCREASED FUEL USAGE. FLIGHT LANDED UNEVENTFULLY WITHOUT F URTHER INCIDENT. CORRECTED BY REPLACING LEFT LANDING GEAR UPLOCK SENSOR, AND NR 2 LGCIU. 2 L 7 2 4F RT A28NM 2007021200205 20070212 00205 2007 2 12 2007UALA00226 4 20070126 A 2565 HARNESS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE BUCKLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 554UA 26644 SLIDE ASSY HARNESS BUCKLES AT DOOR 1L WILL NOT LATCH SLIDE PACK CORRECTLY ONTO DOOR ASSY. REPLACED SLIDE ASSY HARNESS AS WELL AS SLIDE ASSY. CAUSE OF FAILURE NOT ESTABLISHED AT THE TIME. 2 L 7 2 4F 4 F RT A2NM E17NE 2007021200206 20070212 00206 NM 2007 2 12 2007UALA00227 1 20070128 A 3350 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 641UA 25091 EMERGENCY OVERWING EXIT SIGNS INOP ALL POSITIONS. REPLACED BATTERY AND BASE; OPS CHECKED OK . 2 L 7 2 4F 4 F RT A1NM E24NE 2007021200207 20070212 00207 NM 2007 2 12 2007UALA00228 1 20070126 A 3397 WIRE HARNESS BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 EMERGENCY FLOOR LIGHT IN FIRST CAM OUT OF TRACK. FOUND 2 EEL STRIPS INOP AT FWD DOOR AND CROSSOVER. REPAIRED HARNESSES PER GNMM 2-0-15-005. ALL GROUND CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007021200208 20070212 00208 NM 2007 2 12 2007UALA00229 1 20070126 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 30024 MAIN CABIN SEAT 14 RIGHT EEL STRIP IS BROKEN. REPLACED STRIP PER MM33-51 -00, OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007021200209 20070212 00209 NM 2007 2 12 2007UALA00230 1 20070126 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE ROW 11RH MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 30024 SEAT ROW 11 RIGHT MISSING EEL LIGHT STRIP. INSTALLED NEW EEL LIGHT STRIP AND OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007021200210 20070212 00210 NM 2007 2 12 07FDEA00356 1 20070207 A 5330 NDA631353 SKIN DOUG MD11 MD11F 3023600 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 529FE 48624 DURING ACCOMPLISHING EO, NEW EXTERNAL SKIN (P/N ADA 7030Y1) FOUND WITH 2 MISDRILLED HOLES AND 11 EXTRA HOLES BEING TRANS FERRED AFTER TRANSFERRED HOLES FROM EXISTING EXTERNAL HOLES AT STA 853 TO STA 875, L-37R TO L-41R. REPAIR CARRIED OUT P ER STEP 31 AND 32 OF E.A 1-5330-104764. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007021200211 20070212 00211 EU 2007 2 12 07FDEA00357 1 20070207 A 5230 BEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 TWO OVERSIZED AND DAMAGED HOLES ON THE END OF THE LONGITUDINAL BEAM AT THE LOWER SIDE ON BULK CARGO DOOR NEAR TO C67 BET WEEN STRINGER P`45 / P`47 RT. REPAIR WAS PERFORMED BY REPLACE A NEW BEAM (A539-73100-200-51) IAW SRM 51-72-10, FIG 8, S HEET 8. 2 L 7 2 4F RT A35EU 2007021200212 20070212 00212 EU 2007 2 12 07FDEA00359 1 20070207 A 5340 BRACKET AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 CORRODED BRACKET UNDER PRESSURE MEMBRANE AT TRACK 5 LT C54. CORRODED HOLE AFTER COUNTERSINK OF PRESSURE MEMBRANE AT TRA CK 5 RT, C54. REPAIR WAS PERFORMED BY INSTALLING FITTING P/N A538-13311-201-EF ON LHS AND INSTALLING A COUNTERSUNK BUSH IN THE AFFECTED HOLE ON RHS WITH REINSTALLING NOMINAL FASTENER. REPAIR IS APPROVED BY RAS 049222/008/2006 ISSUE A AND EA 6-5315-106392. 2 L 7 2 4F RT A35EU 2007021200213 20070212 00213 EU 2007 2 12 07FDEA00361 1 20070207 A 5320 WEB AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DENTED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 WEB PLATES OF BULK CARGO DOOR TORSION BOX FWD AND AFT C68 BETWEEN P33 AND P36 RH DENTED AND SCRATCHED. REPAIR WAS PERFO RMED BY DRESSED BACK DENTS AND REWORK OF AFFECTED WEB PLATES IAW RAS/DAHAM/4021476/2006 AND EA 6-5317-106348. 2 L 7 2 4F RT A35EU 2007021200214 20070212 00214 NM 2007 2 12 07FDEA00362 1 20070207 A 5753 SKIN BOEING 727 727233 138408A NM LT FORE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 LT IB FOREFLAP AT IB END UPPER SURFACE IS WORN AND DELAMINATED REPAIRED LT IB FOREFLAP REF SRM 51-40-20 PGS 1-63 AND RE BONDED RUBSTRIP REF SRM 51-20-4 PGS 1 AND 2. TAP CHECKS GOOD. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007021300003 20070213 00003 EU 2007 2 13 07FDEA00428 1 20070209 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 MDCC - FLOORBEAM FR 63 HAS CORROSION FROM SEAT TRACK 5L TO 5R. REPAIRED FLOORBEAM AT FR 63 FROM SEAT TRACK 5L TO 5R IAW A310 SRM 51-40-21 AND 53-10-15 FIG 201 SH 17. 2 L 7 2 4F RT A35EU 2007021300004 20070213 00004 2007 2 13 0700529620 4 20070205 A 2565 SLIDE DOUG DC9 DC932 3022066 WP TAILCONE INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 620NW 47533 LOCAL VENDOR AT SYR ATTEMPTED TO STOW TAIL CONE RELEASE HANDLE AND INADVERTENTLY JETTISONED THE TAIL CONE. SEE LP NR 38 32775. THE TAIL CONE EMERGENCY ESCAPE SLIDE DID NOT DEPLOY AND DID NOT INFLATE. NO OBVIOUS REASON FOR FAILURE OF THE S LIDE TO DEPLOY AS DESIGNED. THE AIRCRAFT WAS FERRIED TO DTW WHERE THE TAIL CONE WAS REPLACED. THE SLIDE WAS, AT THAT T IME, MODIFIED PER EO 2561-01275 TO INSTALL THE IMPROVED COVER AND INSPECTED AS REQUIRED. THE AIRCRAFT HAS RETURNED TO S ERVICE. 2 L 7 2 4F A6WE 2007021300005 20070213 00005 EU 2007 2 13 07FDEA00429 1 20070209 A 5753 SKIN AIRBUS 310 A310203 3930313 EU TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 LT WING OUTBD FLAP TE HAS AREA OF DELAMINATION O/B OF FLAP RIB NR 3, 7" BY 1.5", FOUND DURING AGING ACFT INSP. REPAIRE D DAMAGED SKIN ON LT O/B FLAP IAW EA 6-5750-107644 2 L 7 2 4F RT A35EU 2007021300007 20070213 00007 NM 2007 2 13 07FDEA00431 1 20070209 A 5320 SILL BOEING 727 727233 138408A NM BS 385-410 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 FOUND MAIN DECK 1R DR CUTOUT LWR SILL CREASE BEAM SCUFF PLATE IB SUPPORT UPPER FLANGE IS CORRODED. BLENDED CORROSION, H FEC, NO DEFECTS NOTED. ALODINED AND PRIMED, REF EA NR 7-5310-106989, PART 1. 2 L 7 3 4F RT A3WE 2007021300008 20070213 00008 EU 2007 2 13 07FDEA00432 1 20070209 A 5280 DOOR AIRBUS 310 A310203 3930313 EU MLG CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 2 CHAFE MARKS EXIST AT LT MLG PRIMARY DOOR AFT LWR POSITION BLENDED AND SMOOTHED CHAFE MARKS IAW A310-200 AMM 51-73-10-8 . REPAIRED AREA IAW A310-20 0 AMM 51-73-10 AND EA 6-5280-106329. 2 L 7 2 4F RT A35EU 2007021300012 20070213 00012 SO 2007 2 13 SWIA200717788 1 20070201 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO CABIN SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 226SW 120296 AT THE GATE, HAD SMOKE IN THE COCKPIT. RAN LEFT PACK FOR 10 MINUTES WITH NO SMOKE/ODOR IN THE COCKPIT. OPERATIONAL CHE CKS GOOD. 2 L 7 2 4T RT A31SO 2007021300013 20070213 00013 SO 2007 2 13 SWIA200717789 1 20070201 A 3350 D36604001 BATTERY EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 292SW 11133 2192 120319 ALL EMERGENCY LIGHTS AFT OF ROW 8 INOP. REPLACED THE AFT EMERGENCY LIGHT BATTERY IAW AFM 33-50-02. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007021300014 20070213 00014 EA 2007 2 13 SWIA200717790 1 20070206 A 2120 UNKNOWN CNDAIR CL600 CL6002D24 1390016 EA CABIN ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 804SK 15067 VERY STRONG FUEL SMELL IN COCKPIT/CABIN ABOUT 3 MINUTES AFTER APU START. PERFORMED OPS CHECK OF THE ENGINE, APU AND PAC KS. COULD NOT DUPLICATE DISCREPANCY. 2 L 7 2 4F RT A21EA 2007021300015 20070213 00015 EA 2007 2 13 SWIA200717791 1 20070205 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 970SW 7881 AT APPROXIMATELY 2000 AGL, COULD HEAR A BUZZING/CLICKING NOISE FROM CBP NR 2 AND AT TIMES COULD SMELL AN 'OVERHEATING' T YPE ODOR. INSPECTED CB PANEL NR 2. NO DEFECTS/ODOR. UNABLE TO DUPLICATE DISCREPANCY. 2 L 7 2 4F RT A21EA 2007021300016 20070213 00016 SO 2007 2 13 SWIA200717792 1 20070204 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 213SW 13635 13635 120277 FOUND EXIT ROW LIGHTS INOP. REPLACED CENTER BATTERY PACK IAW EMB MM 33-50-02. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007021300018 20070213 00018 EA 2007 2 13 TRAX200700164 1 20070130 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT NO TEST A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 908EV 7654 RIGHT EMERGENCY EXIT DOOR FAILS PULL TEST (MTC). 2 L 7 2 4F RT A21EA 2007021300019 20070213 00019 EU 2007 2 13 TRAX200700165 1 20070201 A 5710 PLATE AEROSP ATR72 ATR72 EU RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 RIGHT WING BOX AT FR 28 FACE PLATE CRACKED. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SP 663 AND FAR 43 APPENDIX A REPAIR ACCOMPLISHED IAW SRM 51-25-01 2 H 7 2 4T RT 2007021300020 20070213 00020 EA 2007 2 13 TRAX200700167 1 20070204 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA BS 559-574 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 908EV 7654 CORROSION ON THE BOTTOM SIDE OF SEAL RAIL BEAM RBL 27.0 BETWEEN FLOORBEAMS FS 559.00+112 AND FS 574.00 AS MARKED. 2 L 7 2 4F RT A21EA 2007021300021 20070213 00021 EA 2007 2 13 TRAX200700168 1 20070204 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 880AS 7606 FLAP FAIL MSG AT ZERO DEGREES, WHEN SELECTED ON APPROACH. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007021300023 20070213 00023 NM 2007 2 13 F3LA200700018 1 20070206 A 3350 321431 BATTERY AIRBUS A319 A319111 3930336 NM EMERGENCY LIGHTS INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 918FR 1943 DURING C-3 CHECK, INSPECTION REPORTED FWD EMERGENCY LIGHTING BATTERY FAILED DURING OPS CHECK. REPLACED FWD EPSU BATTERY (10WL) IAW AMM 33-51-38-400-002. 2 L 7 2 4F RT A28NM 2007021300024 20070213 00024 NM 2007 2 13 F3LA200700017 1 20070206 A 3350 321430 BATTERY AIRBUS A319 A319111 3930336 NM EMERGENCY LIGHTS DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 918FR 5911 1943 DURING C-3 CHECK, INSPECTION REPORTED AFT EMERGENCY LIGHTING BATTERY FAILED DURING OPS CHECK. REPLACED AFT EPSU BATTERY (13WL) IAW AMM 33-51-38-400-002. 2 L 7 2 4F RT A28NM 2007021300025 20070213 00025 EU 2007 2 13 F3LA200700020 1 20070206 A 3350 321431 BATTERY AIRBUS A318 A318111 3940019 EU EMERGENCY LIGHTS DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 918FR 5911 1943 DURING C-3 CHECK, INSPECTION REPORTED RT OVERWING EMERGENCY LIGHTING BATTERY FAILED DURING OPS CHECK. REPLACED RT OVERW ING EPSU BATTERY IAW AMM 33-51-38-400-002. 2 L 7 2 4F RT 2007021300027 20070213 00027 NM 2007 2 13 USAASB07011 1 20070208 A 2751 2061141 INDICATOR BOEING 737 7374B7 1384702 NM TE FLAPS FAULTY A USAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 19 456UW 45020 45020 25020 BDL FLT 1067 - AFTER TAKEOFF AND FLAP SELECTION TO 1, CREW REPORTED A FLAP ASYMMETRY LOCKOUT. POINTERS ON FLAP POSITION INDICATOR WERE LEFT AT 2 AND RIGHT AT 5. AIRCRAFT CIRCLED BDL TO BURN OFF FUEL TO AVOID AN OVERWEIGHT LANDING. FLIGHT RETURNED TO FIELD AT BDL AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. ON ARRIVAL, MAINTENANCE VISU ALLY CHECKED FLAPS AND FOUND FLAPS SYMMETRICALLY DEPLOYED. NOTED TRAILING EDGE FLAP INDICATION CIRCUIT BREAKER IN OPEN POSITION AND INDICATIONS FROM POINTERS AS REPORTED BY FLIGHT CREW. RESET CIRCUIT BREAKER AND INDICATIONS RETURNED TO NO RMAL. OPS CHECK OF FLAPS AND INDICATION NORMAL. NO DEFECTS NOTED. TESTED FLAP ASYMMETRY PROTECTION PER MM 27-51-00-71 2 L 7 2 4F RT A16WE 2007021300029 20070213 00029 NM 2007 2 13 UPS07449129 1 20070103 A 5311 FRAME BOEING 747 747123 1384873 NM BS 840 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D - RIGHT BS 840 TENSION TIE TO FRAME CONNECTION FOUND 2EA HOLES CRACK AT FRAME (0.040" & 0.060"). M/D RIGHT BS 840 TENSION TIE TO FRAME CONNECTION I/B & O/B 2EA HOLES OVERSIZED BY INCREMENTS TO 0.309" DIA. CRACK FREE INSPECTED BY HFEC PER NTM PART 6 51-00-00 FIG 16, FASTENERS INSTALLED AS PER UPS EO B747-5310-23715 APP B. 2 L 7 4 4F A20WE 2007021300030 20070213 00030 NM 2007 2 13 UPS07449130 1 20070103 A 5311 FRAME BOEING 747 747123 1384873 NM BS 920 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LEFT BS 920 FRAME TENSION TIE ATTACHMENT AREA FOUND 1EA FASTENER HOLE CRACKED AT FRAME APPROX 0.040" R UNNING UPWARD AND DOWNWARD. M/D LEFT BS 920 FRAME 1EA HOLE OVERSIZED BY INCREMENTS TO 0.247" DIA. CRACK FREE INSPECTED BY HFEC PER NTM PART 6 51-00-00 FIG 16, FASTENER INSTALLED AS PER UPS EO B747-5310-23715 APPENDIX B. 2 L 7 4 4F A20WE 2007021300031 20070213 00031 NM 2007 2 13 UPS07449131 1 20070103 A 5310 TENSION TIE BOEING 747 747123 1384873 NM BS 840 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D LEFT BS 840 TENSION TIE TO FRAME CONNECTION FOUND 1EA HOLE CRACK AT FWD CHANNEL APPROX 0.060" RUNN ING UP. M/D LEFT TO RIGHT TENSION TIE FWD CHANNEL REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 & SRM 51-30-02 & UPS EO B747-5310-23715 APPENDIX B. 2 L 7 4 4F A20WE 2007021300034 20070213 00034 NM 2007 2 13 UPS07449140 1 20070104 A 5310 PLATE BOEING 747 747123 1384873 NM BS 920 MISREPAIRED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D RIGHT BS 920 TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D RIGHT BS 920 TENSION TIE AT TACH STEEL PLATE SHORT EDGE MARGIN REPAIRED AS PER RS R53-25-35716. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35 716 AND UPS EO B747-5310-25932. 2 L 7 4 4F A20WE 2007021300036 20070213 00036 NM 2007 2 13 UPS07449142 1 20070104 A 5310 PLATE BOEING 747 747123 1384873 NM BS 800 MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D RIGHT BS 800 TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D RIGHT BS 800 TENSION TIE AT TACH STEEL PLATE SHORT EDGE MARGIN REPAIRED AS PER RS R53-25-35710. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35 710 AND UPS EO B747-5310-25925. 2 L 7 4 4F A20WE 2007021300040 20070213 00040 EU 2007 2 13 TRAX200700169 1 20070204 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 EMERGENCY LIGHTS WILL NOT EXTINGUISH. FLT 4101 DEL 83 MINS. 2 H 7 2 4T RT 2007021300041 20070213 00041 EA 2007 2 13 TRAX200700170 1 20070204 A 3250 SWITCH CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING UNKNOWN A ASOA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 881AS 7496 A -STEERING INOP- CAUTION MESSAGE AFTER T/O. FOLLOWED QRH, MESSAGE WENT OUT WITH NWS SWITCH OFF. STEERING RE-SET WITH SWITCH AFTER LANDING. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007021300042 20070213 00042 EA 2007 2 13 TRAX200700171 1 20070204 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 920EV 7810 LEFT OVERWING EMERGENCY AFT EXT LIGHT INOP. 2 L 7 2 4F RT A21EA 2007021300043 20070213 00043 EA 2007 2 13 TRAX200700172 1 20070204 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 909EV 7658 FLAP HALF SPEED FOLLOWED BY FLAP FAIL. EMERGENCY DECLARED. FLT 4879 CX. REMOVED AND REPLACED PDU IAW AMM OPS CHECK G OOD. 2 L 7 2 4F RT A21EA 2007021300044 20070213 00044 EA 2007 2 13 TRAX200700173 1 20070204 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 837AS 7271 FLAPS FAIL CAUTION MSG AT 0 DEG ON APPROACH TO YYZ, FOLLOWED QRH, LANDED UNEVENTFUL. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007021300049 20070213 00049 NM 2007 2 13 DL757070097 1 20070206 A 5330 141N343115 SKIN BOEING 757 757232 1384965 NM BS 435 S20R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 6712B 30484 FUSELAGE SKIN WAS FOUND DENTED, CREASED, AND GOUGED AT STA 435 AT THE S-20R LAP JOINT. CUTOUT THE DAMAGED SKIN AND INST ALLED A REPAIR DOUBLER. 2 L 7 2 4F RT A2NM 2007021300050 20070213 00050 NM 2007 2 13 DL738070098 1 20070129 A 5320 147A56602 FLOOR SUPPORT BOEING 737 737832 13844CF NM BS 950 RBL 52 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 381DA 30350 DURING PSV 8, FOUND CORROSION WHICH WAS OUT OF LIMITS ON AFT RIGHT LAVATORY FLOOR SUPPORT AT STA 950 RBL 52. DAMAGE WAS LIMITED TO AN AREA .080 DIA AND .013 DEEP. REPAIR ACCOMPLISHED ON NR 235. PART REPLACED WAS MPN 147A5660-2. 2 L 7 2 4F RT A16WE 2007021300051 20070213 00051 NM 2007 2 13 DL757070099 1 20070209 A 2120 UNKNOWN BOEING 757 757232 1384965 NM CABIN/COCKPIT SMOKE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 643DL 23997 ON LAND ROLLOUT, SMOKE VISIBLE IN COCKPIT AND CABIN. POSSIBLE SULPHUR SMELL. ALSO NOTICED OUTSIDE A/C BY GROUND CONTRO L. NO UNUSUAL ODOR NOTED. INSPECTED ENGS AND PACKS. RAN BOTH ENGINES WITH PACKS ON ALL OK. 2 L 7 2 4F RT A2NM 2007021300053 20070213 00053 2007 2 13 DL76L070101 2 20070209 A 7597 CONNECTOR BOEING 767 767332 1382001 NM IDG CONTAMINATED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 174DN 24802 L IDG VLV STATUS MSG AFTER ENG START. MX FOUND ELECTRICAL CONNECTOR CONTAMINATED. CLEANED RESEATED CONNECTOR AND MSG C LEARED. RAN ENG AT IDLE NO MSG. 2 L 7 2 4F RT A1NM 2007021300054 20070213 00054 NM 2007 2 13 DL76L070102 1 20070209 A 2740 285T009917 MODULE BOEING 767 767332 1382001 NM P-50 PANEL UNKNOWN A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 193DN 28450 ON T/O UNSCHED STAB TRIM LIGHT ILLUMINATED RETURNED TO GATE. LEFT SAM FAULT STCM REPLACED FSPM CARD M838 LEFT SIDE RAN TEST PER AMM TEST GOOD. 2 L 7 2 4F RT A1NM 2007021300056 20070213 00056 NM 2007 2 13 USAABB07016 1 20070209 A 3260 SENSOR BOEING 767 767201 1385125 NM MLG MALFUNCTIONED A USAA O OTHER J WARNING INDICATION CR CRUISE 1 EA 19 250AY 23902 FLIGHT 1443, AMS-PHL: DURING CRUISE, CREW RECEIVED A LANDING GEAR MONITOR MESSAGE AND A LEFT GEAR DOWN AND LOCKED GREEN LIGHT WITH ALL GEAR UP AND LOCKED. ALL OTHER INDICATIONS NORMAL. FLIGHT CONTINUED TO PHL WITH NO DIFFICULTIES. CONDU CTED A TOWER FLY BY AT PHL TO ENSURE GEAR WAS DOWN. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE S258 SIDE BRACE DOWN SENSOR. 2 L 7 2 4F RT A1NM 2007021300061 20070213 00061 EU 2007 2 13 MAC020701 1 20070209 A 2911 54079 ACCUMULATOR AEROSP ATR42 ATR42320 8680930 EU HYD SYSTEM LEAKING A MTNA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 904FX 21359 259 DURING DEPARTURE, THE GREEN HYDRAULIC SYSTEM LIGHT ILLUMINATED. 2 H 7 2 4T RT A53EU 2007021300062 20070213 00062 EU 2007 2 13 TRAX200700166 1 20070201 A 5714 ANGLE AEROSP ATR72 ATR72 EU WING BOX CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 RIGHT WING BOX AT FR 28 ANGLE BEHIND FACE PLACED CRACKED. NEW SHEETMETAL BENT INSTALLED IAW SRM 51-25-01 AT FR28 WING BOX. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SR663 AND FAR 43 APPENDIX A REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01. 2 H 7 2 4T RT 2007021300065 20070213 00065 NM 2007 2 13 ZZDA070115135 1 20070115 A 5210 SKIN BOEING 717 717200 1383700 NM L1 DOOR DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 967AT 55028 L1 DOOR LOWER FWD CORNER OUTER SKIN DAMAGED. INSTALLED DOULBER REPAIR PER SRM 52-10-01 FIG 201, 14" X 2 1/7" 2024T3. 05 0. 2 L 7 2 4F TR A6WE 2007021300066 20070213 00066 EU 2007 2 13 XN0A1361 1 20070208 A 4997 CONNECTOR AIRBUS 300 A300B4203 3930306 EU APU DIRTY A XN0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 472AS 125 APU QUIT AT 22,000 FEET, RUNNING ON ONE GENERATOR TRIED TO RESTART, APU WOULD NOT START. DROPPED TO 20,000 FEET, RESTAR TED APU AND IT QUIT AGAIN AT 20,000 FEET. RETURNED TO VHHH. CLEANED AND RESECURED CONNECTIONS AT ECB, APU OPS CHECKS G OOD ON GROUND IAW A300 AMM CHAPTER 49-10-00. 2 L 7 2 4F RT A35EU 2007021300068 20070213 00068 NM 2007 2 13 DL76S070105 1 20070210 A 5313 STRINGER BOEING 767 767332 1382001 NM BS 412-434 S35R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 FOUND STRINGER 35R AT STA 412-434 CORRODED. REPAIRED PER SRM 53-30-03, FIG 201, REPAIR 1. 2 L 7 2 4F RT A1NM 2007021300069 20070213 00069 NM 2007 2 13 DL76S070106 1 20070210 A 5313 STRINGER BOEING 767 767332 1382001 NM BS 412-456 S36R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 FOUND STRINGER 36R STA 412-456 CORRODED. REPAIRED PER SRM 53-30-03 FIGURE 201 REPAIR 1. 2 L 7 2 4F RT A1NM 2007021300070 20070213 00070 NM 2007 2 13 DL76S070107 1 20070210 A 5313 STRINGER BOEING 767 767332 1382001 NM BS 412-434 S37R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 FOUND STRINGER 37R STA 412-434 CORRODED. REPAIRED PER SRM 53-30-03 FIG 201 REPAIR 1. 2 L 7 2 4F RT A1NM 2007021300074 20070213 00074 WP 2007 2 13 ABXA070037 1 20070128 A 5311 9923409502 FRAME DOUG DC9 DC941 302207N WP BS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 RIGHT FORWARD MAIN FRAME WAS CORRODED IN FORWARD UPPER FLANGE BETWEEN POINTS G & J OF ES01144, STA 737. REPAIRED MAIN F RAME IAW EA 53400120-001-2. 2 L 7 2 4F A6WE 2007021300075 20070213 00075 WP 2007 2 13 ABXA070038 1 20070128 A 5347 S2914913M24000 SEAT TRACK DOUG DC9 DC941 302207N WP BS 225-256 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 SEAT TRACK CORRODED, RIGHT BUTT LINE 54, STA 225 TO 256. REMOVED AND REPLACED SEAT TRACK FS 200 - 300 AT RIGHT BUTT LIN E 54. 2 L 7 2 4F A6WE 2007021300078 20070213 00078 NM 2007 2 13 WRLA2007032 1 20070209 A 5753 SKIN DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE TE FLAPS DELAMINATED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 62911 48407 DURING 3C + 12A CHECK, EGAT MECHANIC FOUND RIGHT OUTBOARD FLAP UPPER SURFACE TRAILING EDGE WEDGE IS DELAMINATED. REMOVE RT WING OUTBD FLAP WEDGE. PERFORM THE ENGINEERING INSTRUCTION NO.W2007A57B-095 REV.00, PAGE 1 OF 3 ITEM 1~7, PAGE 2 OF 3 ITEM 8~10. INSTALLED RT WING OUTBD FLAP WEDGE. 2 L 7 3 4F 4 F RT A22WE E24NE 2007021300081 20070213 00081 NE 2007 2 13 NACA20070005 2 20070210 A 8530 356993 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 18 BURNED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 AL 03 43872 1955 1955 533294 33325 NR 4 ENGINE SHUT DOWN DUE TO NR 18 CYLINDER FAILURE. REMOVED AND REPLACED NR 18 CYLINDER DUE TO BURN THROUGH ON SIDE OF CYLINDER, REF: DC-6MM SECT V PG 16 AND 16A, CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2007021300086 20070213 00086 CE 2007 2 13 DXTA200701922 1 20070208 A 3260 INDICATOR BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE MLG NO INDICATION E DXTA O OTHER P NO WARNING INDICATION DE DESCENT 1 GL 07 120QS RK293 WHEN GEAR WAS PLACED IN DOWN POSITION. THE RT GREEN R DID NOT ILLUMINATE. OHMED OUT GEAR INDICATOR HARNESS NO DEFECTS W ERE NOTED. ACCESSED CONNECTOR P272 IN R/H WHEEL WELL OHMED OUT DOWN LOCK SWITCH FOUND HIGH RESISTANCE THROUGH CLOSED CON TACTS ON SWITCH. NOTIFIED LMCC. ALSO OHMED OUT DOOR SWITCH AND GEAR UPLOCK SWITCH NO DEFECTS WERE NOTED. REMOVED DOWNLOC K SWITCH AND INSTALLED NEW CUSTOMER SUPPLIED SWITCH PER 400XP WDM 32-61-00 AND MM 32-10-00 OPS CHECKED NO DEFECTS WERE N OTED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007021300089 20070213 00089 CE 2007 2 13 DXTA200701925 1 20070208 A 3260 INDICATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG NO INDICATION E DXTA O OTHER P NO WARNING INDICATION DE DESCENT 1 GL 07 983QS 7500083 NOSE WHEEL DOWN GREEN LIGHT DID NOT ILLUMINATED WITH GEAR SELECTED TO DOWN/ EXTENDED POSITION. EMERG CHECK LIST COMPLETE D AND GEAR WAS BLOWN DOWN. LIGHT STILL FAILED TO ILLUMINATE NO OTHER NEGATIVE INDICATIONS NOTES. LIGHT TESTED SATISFACTO RY W/ ROTARY TEST. BLED GEAR, SERVICED NITROGEN BOTTLE. TROUBLESHOT TO NOSE DOWNLOCK SWITCH. REMOVED AND REPLACED DOWNL OCK SWITCH RAN GEAR. OPS CHECK GOOD. WORK DONE IAW CESSNA 750 MM CH 32-30-03. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007021300094 20070213 00094 NM 2007 2 13 AMTA200700053 1 20070202 A 4990 32895042 VALVE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE APU OIL SYS UNSERVICEABLE A AMTA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 11 552TZ 20124 20124 32586 LEVELED OFF AT CRUISE 20 MIN AFTER DEPARTURE, APU LEVELED OFF AT CRUISE 20 MIN AFTER DEPARTURE, APU OIL QTY SHOWED FULL. 30 MINUTES LATER OIL QTY SHOWED 50. REMOVED AND REPLACED GEARBOX PRESSURE REG VALVE IAW AMM 49-27-12-4. RAN APU 1 HR , APU OPS CHS NORMAL NO LEAKS NOTED. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007021300096 20070213 00096 2007 2 13 07FDEA00427 4 20070208 A 3418 COMPUTER BOEING 727 72722 1384002 NM STALL WARNING MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 191FE 19084 CAPT STICK SHAKER ACTIVATED ON ROTATION. SHAKER SPEED WAS ABNORMALLY SLOW, ABOUT 1/3 NORMAL RATE DURING TEST. SHAKER C ONTINUED FOR APPROX 3 MINUTES AND SLOWED GRADUALLY UNTIL IT STOPPED. AIRCRAFT FLEW NORMALLY. REMOVED AND REPLACED NR 1 STALL WARNING COMPUTER. OPS CKS NORMAL PER AMM34-18-000-5. 2 L 7 3 4F A3WE 2007021300099 20070213 00099 NE 2007 2 13 NACA20070006 2 20070209 A 8520 CLUTCH DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 2 ENGINE FAILED A NACA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AL 03 2907F 1710 1710 533265 CP450668 NR 2 ENGINE DROP IN BMEP, MAP DROPPED TO BAROMETRIC PSI, PRECAUTIONARY ENGINE SHUT DOWN. REPLACED NR 2 ENGINE DUE TO CL UTCH FAILURE REF: DC-6MM SECT V PG. 3-8. 2 L 7 4 4R 4 R A781 5E8 2007021300104 20070213 00104 NM 2007 2 13 UPS07449145 1 20070104 A 5310 TENSION TIE BOEING 747 747123 1384873 NM BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D LEFT BS 940 TENSION TIE TO FRAME CONNECTION FOUND 1EA HOLE CRACK AT TENSION TIE AFT CHANNEL RUNNIN G UP THRU THICKNESS APPROX 0.060 INCH, CRACK LENGTH 0.060 INCH. M/D LT BS 940 TENSION TIE LT AFT CHANNEL REPAIRED AS PE R RS R53-25-35712. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35712 AND UPS EO B747-5310-25927. 2 L 7 4 4F A20WE 2007021300107 20070213 00107 NM 2007 2 13 UPS07449148 1 20070103 A 5310 TENSION TIE BOEING 747 747123 1384873 NM BS 920 S8-9L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 920 STR 8-9L TENSION TIE LEFT O/B AFT CHANNEL FOUND CRACK. CRACK LENGTH .125 INCH. M/D BS 920 STR 8-9L TENSION TIE LEFT O/B AFT CHANNEL REPAIRED AS PER RS R53-25-35716. CONTINUE INSPECTION IS REQUIRED AS PER RS R 53-25-35716 AND UPS EO B747-5310-25932. 2 L 7 4 4F A20WE 2007021300109 20070213 00109 NM 2007 2 13 UPS07449150 1 20070109 A 5311 FRAME BOEING 747 747123 1384873 NM BS 2180 S25-26R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 2180 STR 25-26R FRAME CRACKED. CRACK LENGTH .5 INCH. M/D BS 2180 STR 25-26R FRAME REPAIRED AS PER RS R53-62-35728 AND UPS EO B747-5310-26045. 2 L 7 4 4F A20WE 2007021300110 20070213 00110 NM 2007 2 13 UPS07449151 1 20070111 A 5313 STRINGER BOEING 747 747123 1384873 NM BS 2177 S28R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C AFT OF BULK CARGO COMPT - FX STRINGER FOUND CRACK AT BS 2177 STR 28 RIGHT AS MARKED. CRACK LENGTH 1.2 5 INCH. AFT OF BULK CARGO COMPT FX STRINGER S28R AT BS 2177 AREA REPAIRED AS PER RS R53-62-35735 AND UPS ENGINEERING FI LE NR 747-53-20377. 2 L 7 4 4F A20WE 2007020800007 20070208 00007 EA 2007 2 8 COMA0760130 1 20070204 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 999CA 7230 FLIGHT 5142- DURING CVG APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITH OUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007020800008 20070208 00008 EA 2007 2 8 COMA0760131 1 20070204 A 2752 854D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 01 479CA 11480 7675 FLIGHT 5390 - DURING JFK APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WIT HOUT INCIDENT. REPLACED THE LEFT OUTBOARD FLAP OUTBOARD ACTUATOR. 2 L 7 2 4F RT A21EA 2007020800009 20070208 00009 SO 2007 2 8 GUUA02050701 1 20070205 A 3297 12041125001 WIRE HARNESS EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE ZONE 700 KINKED A GUUA O OTHER N FALSE WARNING CL CLIMB 1 SO 29 282AS 120226 FLIGHT 9212, AFTER TAKEOFF LANDING GEAR RETRACTED NOSE LANDING GEAR A SYSTEM (B) LIGHTS AND B SYSTEM (B) LIGHTS REMAINED ILLUMINATED CYCLED LANDING GEAR INDICATION REMAINED THE SAME. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. REPLACE D B SYSTEM DOWNLOCK PROXIMITY SENSOR HARNESS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 2007020800010 20070208 00010 CE 2007 2 8 GUUA02050702 1 20070205 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FUSELAGE CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 69547 UE189 AT SCHEDULED INSPECTION, DISCOVERED ONE CRACK AT AFT COMM ANTENNA (FS400) CRACK 3.0 INCHES RUNNING LONGITUDINALLY FORWAR D FROM FS 400. STOP DRILLED CRACK AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW STRUCTURALREPAIR MANUAL 51-70-06. 2 L 7 2 4T 4 T RT A24CE E26NE 2007020800011 20070208 00011 WP 2007 2 8 AMTA200700037 1 20070125 A 5710 BEAM LKHEED 1011 10113853 5265020 WP RT WING CRACKED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 162AT 1220 RIGHT WING TE BAT STRUCTURE AREA UPPER LATERAL BEAM FOUND CRACKED AT TWO LOCATIONS, ONE CRACK 2 INCHES AND ONE CRACK .5 INCHES. RIGHT WING TE BAT STRUCTURE CAP REPLACED PER L1011 SRM 51-10-01 AND 51-40-01. (M) 10-17-07 CARRIED OUT P AINT TOUCH UP, UPPER AND LOWER SIDE IAW AMM 20-51-08. (K) 2 L 7 3 4F A23WE 2007020800012 20070208 00012 WP 2007 2 8 AMTA200700035 1 20070125 A 5343 BUSHING LKHEED 1011 10113853 5265020 WP ATTACH FITTING MIGRATED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 162AT 1220 RT MAIN LANDING GEAR TRUNNION FITTING FORWARD AND AFT LANDING GEAR ATTACHING LUG BUSHINGS FOUND MIGRATED AT IWS 346. RE PAIRED IAW EER 13226 WO 319386. REMOVED GEAR AMM 32-11-02, BUSHINGS REMOVED FWD AND AFT LUG AMM 20-71-10, CORROSION REWO RK SRM 51-21-01, NDT NIL FINDINGS, NEW BUSHINGS, CAD PLATE, SRM 51-21-01, INST BUSHINGS SRM 57-14-00, INSTALL GEAR AMM 3 2-11-02, RETRACT CHECK AMM 32-32-00. (K) 2 L 7 3 4F A23WE 2007020800013 20070208 00013 EA 2007 2 8 COMA0760135 1 20070204 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 01 507CA 7796 FLIGHT 5026 - DURING CRUISE FLIGHT RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND LANDED AT YYZ WI THOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007020800014 20070208 00014 EA 2007 2 8 A6WA200740030 1 20070117 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 449AW 7818 WHEN SELECTING FLAPS 30 DEGREES ON APPROACH, FLAP FAIL CAUTION MESSAGE ILLUMINATED, FLAPS REMAINED AT 20 DEGREES. LOCAL MAINTENANCE VISUAL INSPECTED FLAPS RESET C/B`S PER AMM SUPPLEMENT 98-018A, FLAPS OPERATE NORMALLY. PLACED ON 72 HOUR W ATCH. (M) 2 L 7 2 4F RT A21EA 2007020800015 20070208 00015 EA 2007 2 8 COMA0760129 1 20070204 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 986CA 7174 FLIGHT 5507 - DURING DTW APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WIT HOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007020800016 20070208 00016 EA 2007 2 8 TRAX200700156 1 20070203 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 ASD BOTTOM STEP IS CRACKED. 2 L 7 2 4F RT A21EA 2007020800017 20070208 00017 EA 2007 2 8 TRAX200700157 1 20070203 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA RT OVERWING INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 754EV 10173 RIGHT OVERWING AFT EMERGENCY LIGHT IS INOP. 2 L 7 2 4F RT A21EA 2007020800018 20070208 00018 EA 2007 2 8 TRAX200700158 1 20070203 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA BS 330 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 PAX DOOR LOWER SILL, FLOOR SUPPORT LOWER LEG IS CORRODED FS 330. BLEND IS WITHIN LIMITS (MATERIAL THICKNESS .063 , REMO VAL .001 REMAINING 062) :INSTALLED FASTENERS AND RESTORED REWORKED AREA. PER CRJ 700 SMR51-42-06 AND SRM 51-21-23. 2 L 7 2 4F RT A21EA 2007020900008 20070209 00008 NM 2007 2 9 GAIA0701OP 1 20070117 A 3210 STRUT BOEING 727 727214 138407R NM MLG BROKEN A GAIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 750US 21512 FLIGHT 360 - MCO-ATL - DURING TAXI TO PARKING IN ATL THE RIGHT MAIN LANDING GEAR WARNING LIGHT ILLUMINATED WITH SUBSEQUE NT DOOR WARNING LIGHT ON GEAR ANNUNCIATOR PANEL AND F/E ANNUNCIATOR PANEL. POST FLIGHT INSPECTION FOUND THE RIGHT MAIN LANDING GEAR SIDE STRUT BROKEN. REMOVED AND REPLACED THE BROKEN SIDE STRUT AND PERFORMED GEAR SWING IAW BOEING 727 AMM CH 32-11-41. OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2007020900044 20070209 00044 NM 2007 2 9 AWXA200700185 1 20070129 A 5320 654797321 SHEAR WEB BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND SHEAR WEB CRACKED, BS 635, S17L. REPLACED SHEAR WEB, BS 635, S17L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007020900045 20070209 00045 NM 2007 2 9 SWAA070636 1 20070206 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 447WN 33720 DURING SCHEDULED HC1 CHECK, LEFT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK P ER MM. 2 L 7 2 4F RT A16WE 2007020900046 20070209 00046 NM 2007 2 9 SWAA070637 1 20070206 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 447WN 33720 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2007020900047 20070209 00047 NM 2007 2 9 SWAA070635 1 20070206 A 3350 MS155721 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 251WN 32510 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007020900055 20070209 00055 NM 2007 2 9 AMTA200700042 1 20070130 A 7830 1074944 CONTROLLER BOEING 757 75723N 1384973 NM THRUST REVERSER FAILED A AMTA K NONE J WARNING INDICATION IN INSP/MAINT 1 GL 11 518AT 27974 EICAS MSG L ENG BLEED OFF DISPLAYED L ENG BLEED AIR OFF LGT ILLUMINATED WITH ENG RUNNING AND SW ON. DUCT PRESS WENT TO 5 PSI. REMOVED AND REPLACED REVERSE FLOW CHECK CONTROLLER PER AMM 36-11-18-4. OPS CHECK IAW 36-11-00-5. OPS CHECK OK. (M) 2 L 7 2 4F RT A2NM 2007020900059 20070209 00059 NM 2007 2 9 EIA2007002 1 20070109 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482EV 20713 FOUND EMERGENCY LIGHT ON DOOR 5L INOP. REMOVED AND REPLACED LIGHT ASSEMBLY IAW MM33-51-00 PG 501, CHECKED NORMAL. 2 L 7 4 4F A20WE 2007020900065 20070209 00065 2007 2 9 A6WA200740036 4 20070122 A 3416 WL102AMS5 INDICATOR CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A A6WA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 31 449AW 13678 7818 DURING TAKEOFF STANDBY INDICATED AIRSPEED INDICATED 0 TO 80 KNOTS. ABORTED TAKEOFF. MAX BTMS READINGS WERE 4444 WEIGHT = 43,000 LBS IAS NR 1 AND NR 2 INDICATED NORMAL. REMOVED AND REPLACED STANDBY ALT/IAS IAW 34-12-01, PERFORMED PITOT ST ATIC LEAK CHECK, OPS CHECK GOOD IAW AMM 34-11-00. (M) 2 L 7 2 4F RT A21EA 2007020900075 20070209 00075 SO 2007 2 9 RAIA00702003 1 20070204 A 2720 15793101 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO RUDDER MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 841HK 145382 FLT NR 8023 - IAD - AUTO PILOT FAIL FOLLOWED BY RUDDER SYS 1-2 INOP MESSAGE IN FLIGHT. MAINTENANCE REMOVED AND REPLACED RELAYS K0775, K0111, AND K0363. THE NR 1 AND NR 2 RUDDER LOW PRESSURE SWITCHES WERE REMOVED AND REPLACE ALSO. 2 L 7 2 4T RT T00011AT 2007020900076 20070209 00076 SO 2007 2 9 RAIA00702002 1 20070203 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 850HK 145003 PRE FLT NR 7957 - IAD - EMERGENCY LIGHT INOP AT ROW 7. MAINTENANCE FOUND THAT FLOOR STRIP HAD BECOME LOOSE. REPOSITION ED THE STRIP AND LIGHTS FUNCTIONED PROPERLY. 2 L 7 2 4T RT T00011AT 2007020900077 20070209 00077 SO 2007 2 9 C2XA07TY004 1 20070207 A 5320 14522459003 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13949 145057 DURING A CURRENT 1C/5C INSPECTION CORROSION WAS FOUND ON BOTH ENDS OF A COMPOSITE CROSSMEMBER FLOOR SUPPORT AT FR PANEL 231FF. MAINTENANCE REPAIRED THE OMEGA BEAM AT THE DESIGNATED AREA IAW SRM 53-00-10.REMOVED AND REPLACED THE RAMP ANGLE IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007020900078 20070209 00078 EU 2007 2 9 07FDEA00376 1 20070208 A 5280 DOOR AIRBUS 300 A300B4622R 3930312 EU ZONE 700 DELAMINATED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 THE FWD LOWER CORNER OF THE RT NOSE LANDING GEAR DOOR WAS DAMAGED. REPAIR WAS PERFORMED IAW RAS/CASA/5273/2007 ISSUE: A, APPROVED BY EA 6-5282-106412. 2 L 7 2 4F RT A35EU 2007020900079 20070209 00079 EU 2007 2 9 07FDEA00377 1 20070208 A 5730 SKIN AIRBUS 300 A300B4622R 3930312 EU LT WING DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 ON LT WING LOWER SKIN PANEL AFT FROM PYLON NR 1 ARE ELONGATED HOLES ON HYDRAULIC FITTINGS. REPAIR WAS PERFORMED IAW RAS /BAE/1003815/2006 ISSUE: A, APPROVED BY EA 6-5720-103392. 2 L 7 2 4F RT A35EU 2007020900080 20070209 00080 EU 2007 2 9 07FDEA00378 1 20070208 A 5280 DOOR AIRBUS 300 A300B4622R 3930312 EU ZONE 800 DENTED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 DENT ON RT MAIN LANDING GEAR DOOR. REPAIR WAS PERFORMED IAW RAS 048387/0082006 ISSUE: A, APPROVED BY EA 6-5281-103396. 2 L 7 2 4F RT A35EU 2007020900081 20070209 00081 EU 2007 2 9 07FDEA00379 1 20070208 A 7830 UNKNOWN AIRBUS 300 A300B4622R 3930312 EU GE CF6 CF680 30025 NE THRUST REVERSER UNKNOWN A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 668FE 772 705225 ON T/O ROLL ECAM SHOWED NR 2 ENGINE REVERSER PRESSURIZED. CYCLED REVERSER WITH NO HELP. RELEASED FOR SERVICE PER MEL/C DL: 78-30-01-A CATEGORY: C EXPIRATION: 18FEB07 "MEL 78-30-01-A: ENGINE NR 2 THRUST REVERSER INOP. THRUST REVER SER IS DEACTIVATED IN FORWARD THRUST POSITION." MXP AND FADEC CK, PLEASE WORK IN CONJUNCTION WITH TSI: 78-30 9440. 2 L 7 2 4F 4 F RT A35EU E13NE 2007020900082 20070209 00082 EU 2007 2 9 07FDEA00380 1 20070208 A 2840 A2151041500300 DOOR AIRBUS 310 A310324 3930206 EU MISSING A FDEA O OTHER D INFLIGHT SEPARATION LD LANDING 1 SO 25 811FD 457 UPON LANDING INTO PWM DISCOVERED FUELING PANEL MISSING. FOUND PANEL ON RUNWAY. REPLACED R/COOLING AIR INLET FAIRING CT R SECTION ASSY IAW AMM 53-15-73-4. 2 L 7 2 4F RT A35EU 2007020900083 20070209 00083 NM 2007 2 9 KCSA071062 1 20070206 A 5347 SEAT TRACK BOEING 747 747209F 1384800 NM PWA JT9 JT9D7R4G2 52054 NE BS 320 WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 F/E'S OUTBOARD SEAT TRACK WORN BEYOND LIMITS 2 L 7 4 4F 4 F RT A20WE E3NE 2007020900087 20070209 00087 WP 2007 2 9 ABXA070034 1 20070125 A 5340 595591240 ATTACH ANGLE DOUG DC9 DC915F 3022037 WP WING TO FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 229DE 45826 WING TO FUSELAGE ATTACH ANGLE CRACKED PAST STOP DRILL, RIGHT SIDE. REPLACED ANGLE IAW DC9 SRM. 2 L 7 2 4F A6WE 2007020900088 20070209 00088 WP 2007 2 9 ABXA070028 1 20070122 A 5313 27779223 LONGERON DOUG DC9 DC915F 3022037 WP BS 313 L2R CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 229DE 45826 FS 313, LONGERON 2 RIGHT, CRACKED. REPAIRED CRACKED LONGERON IAW DC9 SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 2007020900089 20070209 00089 WP 2007 2 9 ABXA070033 1 20070125 A 5530 49567712 FITTING DOUG DC9 DC915F 3022037 WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 229DE 45826 RIGHT KEEL BEAM CLOSE-OUT PANEL STRUCTURE, FORWARD LOWER FITTING, CRACKED ON INTERIOR SECTION. REMOVED AND REPLACED FIT TING IAW DC9 SRM 51-30-3 AND 51-30-1. 2 L 7 2 4F A6WE 2007020900090 20070209 00090 WP 2007 2 9 ABXA070031 1 20070122 A 5322 99577397 SHEAR TIE DOUG DC9 DC915F 3022037 WP BS 800 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 229DE 45826 SHEAR TIE CRACKED AT FS 800 ON AFT SIDE, BETWEEN LONGERON 15 RIGHT AND 16 RIGHT. REMOVED AND REPLACED SHEAR TIE AT STA 800 IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2007020900091 20070209 00091 NE 2007 2 9 ABXA070035 2 20070203 A 7200 JT8D15 ENGINE DOUG DC9 DC941 302207N WP PWA JT8 JT8D15 52051 NE LEFT DAMAGED A ABXA E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 GL 23 955AX 3271 47619 686246 FLIGHT 509, ILN - JAX, AT CRUISE POWER SETTING, LEFT EPR HAD SUDDEN DROP OF .4 EPR. LOUD POPPING SOUND. MODERATE VIBRA TION, THROTTLED BACK, VIBRATION WORSENED. SHUT LEFT ENGINE DOWN. AIRCRAFT LANDED WITHOUT INCIDENT AT JAX. FOUND TURBI NE DAMAGED. REMOVED AND REPLACED LEFT ENGINE IN WO 600265419, JOB CARD 9090010. 2 L 7 2 4F 4 F A6WE E2EA 2007020900092 20070209 00092 WP 2007 2 9 ABXA070030 1 20070122 A 5313 27779223 LONGERON DOUG DC9 DC915F 3022037 WP BS 525 L9L CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 229DE 45826 FS 525, LONGERON 9 LEFT, CRACKED. REPAIRED LONGERON IAW DC9 SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 2007020900093 20070209 00093 WP 2007 2 9 ABXA070029 1 20070122 A 5313 27779223 LONGERON DOUG DC9 DC915F 3022037 WP BS 446 L3R CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 229DE 45826 FS 446, LONGERON 3 RIGHT, CRACKED. REPAIRED CRACKED LONGERON IAW DC9 SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 2007020900094 20070209 00094 WP 2007 2 9 ABXA070032 1 20070123 A 5313 591140929 LONGERON DOUG DC9 DC915F 3022037 WP BS 332 L16R CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 229DE 45826 LONGERON 16 RIGHT CRACKED AT FRAME FS 332. REMOVED AND REPLACED LONGERON IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 2007020900095 20070209 00095 NM 2007 2 9 AMTA200700047 1 20070131 A 2613 902864 DETECTOR BOEING 737 73783N 13844HI NM NR 2 UPPER UNSERVICEABLE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 308TZ 28244 NR 2 ENGINE OVERHEAT DET WILL NOT TEST IN A MODE. WORKS OK IN B. REMOVED AND REPLACED NR 2 ENG UPPER FAN FIRE DETECTOR IWA AMM 26-11-01-4 SYSTEM TESTS NORMAL, NO FAULTS. (M) 2 L 7 2 4F RT A16WE 2007022300269 20070223 00269 NE 2007 2 23 2007UALA00464 2 20070214 A 7320 EEC BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE FAILED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 597UA 28750 726644 LOSS OF NR 2 ENGINE INDICATION, ENGINE SHUT DOWN. NR 2 ENG FLAMED OUT,30 MINUTES OUT OF HNL. ALL INDICATIONS WENT TO ZE RO. NO N2 INDICATION. ENGINE WIND MILLED FOR 30 MINUTES WITH NO OIL PRESSURE INDICATED. FOUND EEC ROTOR DISINTEGRATED. REPLACED EEC ROTOR AND STATOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007020900096 20070209 00096 EA 2007 2 9 COMA0760145 1 20070205 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 812CA 7381 FLIGHT 5567 - DURING BTR APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WIT HOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007020900097 20070209 00097 NM 2007 2 9 AMTA200700050 1 20070201 A 2150 SENSOR BOEING 757 75723N 1384973 NM A/C PACK MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 517AT 27973 EICAS MSG R PACK OFF AND PACK TEMP DISPLAYED RESET PACK IN STANDBY, OPS NORMAL. REMOVED AND REPLACED COMPRESSOR DISCHAR GE TEMP SENSOR PER MM 21-51-06, OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A2NM 2007020900098 20070209 00098 EA 2007 2 9 COMA0760148 1 20070206 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 929CA 7035 FLIGHT 4973 - DURING PREFLIGHT INSPECTION RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTIO N MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLA P CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007020900099 20070209 00099 EA 2007 2 9 COMA0760149 1 20070206 A 2760 SPOILER SYS CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 812CA 7381 FLIGHT 9459 - DURING TAKEOFF ROLL RECEIVED A CONFIG SPOILER MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORME D SYSTEM RESET WITH NO FURTHER DISCREPANCIES. 2 L 7 2 4F RT A21EA 2007020900100 20070209 00100 CE 2007 2 9 6017802062007 1 20070206 A 3260 SWITCH LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE MLG OUT OF ADJUST E J7SA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SW 05 244FX 178 LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. AIRCRAFT IS IN MAINTENANCE AT THIS TIME. SO FAR, GROUND GEAR SWINGS HAVE NOT DUPLICATED PROBLEM WHILE RINGING OUT WIRING AND SWITCHES, FOUND THE RT GEAR SQUAT SWITCH ADJUSTED ALL THE WAY IN, THUS MAKING THE SWITCH AT ALL TIMES. HOWEVER, THIS SHOULD HAVE PRECLUDED ALL GEAR MOVEMENT, WHICH IS NOT THE CASE FOUND DURIN G GROUND RUNS. 2 L 7 2 4F 4 F RT A10CE E35NE 2007020900102 20070209 00102 EU 2007 2 9 07FDEA00319 1 20070205 A 5313 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DENTED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 OLD DENT REPAIR ON FWD CARGO DOOR SURROUNDING PANEL, C23, P 44 RT DAMAGE ARE ACCEPTABLE IAW RAS/DABRE/00688/ 2000 ISS.B 2 L 7 2 4F RT A35EU 2007020900103 20070209 00103 EU 2007 2 9 07FDEA00320 1 20070205 A 5310 FAILSAFE AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 FWD RIGHT PAX DOOR FAIL/SAFE RING CORRODED IN FWD UPPER CORNER. REPAIR WAS PERFORMED IAW RAS/AS/103/2003 (REWORK OF COR ROSION, INSTALLATION OF NEW FASTENERS). 2 L 7 2 4F RT A35EU 2007020900104 20070209 00104 EU 2007 2 9 07FDEA00321 1 20070205 A 5330 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DENTED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 OLD FLUSH REPAIR DOUBLER ON FUSELAGE AT C76/77, P26/27 LT. REPAIR WAS PERFORMED IAW RAS-DA/HAM 1207/96 ISSUE B AND IS A PPROVED BY EA 6-5318-106345. 2 L 7 2 4F RT A35EU 2007020900105 20070209 00105 NM 2007 2 9 07FDEA00322 1 20070205 A 5230 HANDLE BOEING 727 727233 138408A NM CARGO DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 FUSELAGE LOWER LOBE, NR 1 CARGO DOOR EXT HANDLE HAS EXCESSIVE PLAY AT CONTROL ROD FWD END REPLACED DOOR REF MM 52-35-011 -4, PG 3 B. OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 2007020900106 20070209 00106 EU 2007 2 9 07FDEA00323 1 20070205 A 5330 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 300 DENTED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 OLD EXTERNAL DOUBLER REPAIR ON FUSELAGE AT C89, P39-42. REPAIR WAS PERFORMED IAW SRM 53-10-12, FIG 215. 2 L 7 2 4F RT A35EU 2007020900107 20070209 00107 EU 2007 2 9 07FDEA00324 1 20070205 A 5753 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 DAMAGED A FDEA O OTHER O OTHER UK UNKNOWN 1 SO 25 748FD 633 OLD REPAIR ON LT INBOARD FLAP ON TOP SKIN CLOSE TO TRACK 2 RIB 7. REPAIR WAS PERFORMED IAW RAS/FOK/064/2003 ISSUE B. 2 L 7 2 4F RT A35EU 2007020900108 20070209 00108 EU 2007 2 9 07FDEA00326 1 20070205 A 5100 UNKNOWN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 UNKNOWN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 OLD REPAIR ON RT INBOARD FLAP AT LOWER AND UPPER SKIN BETWEEN RIB 12/14 TRAILING EDGE (PATCH REPAIR). REPAIR WAS PERFOR MED IAW RAS/FOK/060/2003 ISSUE A. 2 L 7 2 4F RT A35EU 2007020900109 20070209 00109 EU 2007 2 9 07FDEA00327 1 20070205 A 5100 UNKNOWN AIRBUS 310 A310222 3930315 EU AILERONS UNKNOWN A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 449FE 217 IN FLIGHT AIRCRAFT WANTED TO TURN RIGHT. REQUIRED 3 UNITS AILERON DEFLECTION TO FLY STRAIGHT. REQUIRED 14 UNITS OF RI GHT RUDDER TRIM TO LEVEL OUT AILERONS. NO CHANGES FROM CLIMB POWER TO IDLE POWER. NO CHANGE YAW DAMPERS ON OR OFF. NO CHANGES AUTOPILOT ON OR OFF. FUEL TANKS AND FOUND FUEL LOAD TO BE SYMMETRICAL. RUDDER NEUTRAL AND FOUND AT ZERO. CH ECKED AILERON CABLE TENSION AND ADJUSTMENT AND FOUND OK. CHECKED AILERON DROOP, AILERON TRIM ADJUSTMENT AND FOUND ALL WITHIN PARAMETERS. CHECKED AILERON NEUTRAL AND FOUND TO BE OK REF A310-200AMM 27-11-00-5. OPERATED AILERON SYSTEM SE VERAL TIMES WITH NO DEFECTS NOTED. REMOVED AND REPLACED LT DROOP ACTUATOR PER A310-200 MM 27-11-71-4 , OPS CHECK AND L 2 L 7 2 4F RT A35EU 2007020900110 20070209 00110 EU 2007 2 9 07FDEA00328 1 20070205 A 5730 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 OLD REPAIR ON LT/RT OUTBOARD WING TIP UNDERNEATH STATIC DISCHARGER. REPAIR WAS PERFORMED IAW RAS/FOK/247/2000 ISSUE B. 2 L 7 2 4F RT A35EU 2007020900111 20070209 00111 EU 2007 2 9 07FDEA00329 1 20070205 A 5101 UNKNOWN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 UNKNOWN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 OLD REPAIR ON TOP CAP BEAM AT C62 LT. REPAIR WAS RENEWED IAW SRM 53-10-15, FIG 207. 2 L 7 2 4F RT A35EU 2007021200002 20070212 00002 WP 2007 2 12 UPS07849118 1 20070121 A 5730 57573183 SKIN DOUG DC8 DC871F 302199D WP LWS 195 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 WHILE GETTING OK TO INSTALL LT AUX TANK. FOUND CRACK ON LT STUB WING LE UPPER IB SIDE. REPAIRED LT LE IB SLOT SUPPORT STRUCTURE SKIN STA XFS-195 IAW RAA DC8-57-20205 A. 2 L 7 4 4F RT 4A25 2007021200008 20070212 00008 CE 2007 2 12 020507N505CS1 1 20070205 A 3233 SWITCH TEIJINSEIKI CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG ACTUATOR FAILED E Z5FA L A ABORTED APPROACH UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 NE 03 505CS 0575 5605252 ON APPROACH, GEAR SELECTED DOWN, THE LT MAIN LANDING GEAR DOWN AND LOCK INDICATION LIGHT DID NOT ILLUMINATE. THE INDICAT OR LIGHT TEST WAS GOOD. THE FLIGHT CREW FOLLOWED THE EMERGENCY CHECKLIST AND UTILIZED THE EMERGENCY BOTTLE TO BLOW DOWN THE GEAR. THE FLIGHT CREW DIVERTED TO MSP AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDING WAS UNEVENTFUL. MAINTENANCE TR OUBLE SHOT THE PROBLEM TO A BAD LT MAIN LANDING GEAR ACTUATOR SWITCH. THE GEAR ACTUATOR WAS REPLACED AND FUNCTIONAL CHEC K WAS GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007021200010 20070212 00010 NM 2007 2 12 ASMF200702003 1 20070204 A 3213 7220MT987N SEAL DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NLG STRUT BROKEN W ASMF A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 SW 23 161PL 49764 AIRCRAFT RETURNED, DURING TAKEOFF, THE NOSE LANDING GEAR DID NOT RETRACT, TRANSPONDER DID NOT WORK AND PRESSURIZATION FA ILED. ADDITIONALLY, STABILIZER, SPOILERS AND AUTOBRAKES LANDING GEAR ALARMS WERE ACTIVATED, AS WELL AS A STRONG NOISE IN THE NOSE LANDING GEAR. NOSE LANDING GEAR STRUT AND SEAL WERE REPLACED IAW MM 32-21-02, LUBRICATION SERVICE AND TEST WER E PERFORMED IAW MM 12-21-04 AND 32-30-00, ALL CORRECT. OVERWEIGHT INSPECTION WAS NOT NECESSARY DUE TO AIRCRAFT LANDED WI TH 17,200 POUNDS AND MAXIMUM LANDING WEIGHT IS 139,500 POUNDS. 2 L 7 2 4F 4 F RT A6WE E9NE 2007021200028 20070212 00028 CE 2007 2 12 GUUA01140703 1 20070114 A 5510 1016200111BW HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT STABILIZER CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 17541 4977 UE203 AT SCHEDULED ROUTINE MAINTENANCE LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED LT OB ELEVATOR HINGE BRACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 2007021200043 20070212 00043 NM 2007 2 12 DU4R2007057 1 20070202 A 5320 SHEAR WEB BOEING 757 757232 1384965 NM BS 1700 S17L CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 6705Y 30397 CORROSION ON SHEAR DECK BS 1700L LBL 50. REPAIRED BY FABRICATING AND INSTALLING REPAIR DOUBLER 16-1/8 BY 15-5/8 BY 8-3/ 8 BY 8-1/8 FROM 2024-T3 .063 IAW B757 SRM 53-60-51, 51-20-01 AND 53-60-57. 2 L 7 2 4F RT A2NM 2007021200044 20070212 00044 NM 2007 2 12 DU4R2007058 1 20070124 A 5320 SHEAR WEB BOEING 757 757232 1384965 NM BS 1683 S17R CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 6705Y 30397 CORROSION ON SHEAR WEB BS 1683 RBL 8. CUT OUT CORRODED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER 9.75" BY 15" BY 8 -1/4" XFROM 2024-T3 .080 AND FILLER FROM 20240-T3 .071" IAW B757 SRM 53-60-51, AND 51-20-01. 2 L 7 2 4F RT A2NM 2007021200045 20070212 00045 NM 2007 2 12 DU4R2007059 1 20070122 A 5320 SHEAR WEB BOEING 757 757232 1384965 NM BS 1699 S17R CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 6705Y 30397 FOUND CORROSION AT BS 1699 RBL 50. FABRICATED AND INSTALLED REPAIR DOUBLER 6-1/4" BY 10.5" BY 6-1/2" FROM 2024-T3 .063 IAW B757 SRM 53-60-51, AND 51-20-01. 2 L 7 2 4F RT A2NM 2007021200047 20070212 00047 CE 2007 2 12 020207N542CS1 1 20070202 A 3233 SWITCH TEIJINSEIKI CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG ACTUATOR FAILED E Z5FA L A ABORTED APPROACH UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 NE 03 542CS 0843 5605523 ON APPROACH, GEAR SELECTED DOWN, THE LT MAIN LANDING GEAR DOWN AND LOCK LIGHT FAILED TO ILLUMINATE FOLLOWED BY THE GEAR AURAL WARNING HORN. THE INDICATOR LIGHT TEST WAS GOOD. THE FLIGHT CREW FOLLOWED THE EMERGENCY CHECKLIST AND UTILIZED THE EMERGENCY BOTTLE TO BLOW DOWN THE GEAR. THE FLIGHT CREW DIVERTED AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDING WAS UN EVENTFUL. MAINTENANCE TROUBLESHOT THE PROBLEM TO A BAD LT MAIN LANDING GEAR ACTUATOR SWITCH. THE ACTUATOR WAS REPLACED A ND FUNCTIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007021200048 20070212 00048 2007 2 12 YENA2007006 4 20070203 A 3140 70265421901 MODULE EMB ERJ190 ERJ190100IGW 3260408 EU FAILED A YENA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 216JB 1897 19000026 ON CLIMB-OUT, EICAS DISPLAYED AVNX ASCB FAULT AND SEVERAL OTHER MESSAGES THAT COULDN'T READ IN TIME DROPPED AUTO PILOT, AUTO THROTTLES, ETC. REMOVED AND REPLACED NIC/PROC MODULE NR 5 IAW E190 TASK 31-41-04. ALL OPS NORMAL. 2 L 7 2 4F RT A57NM 2007021200049 20070212 00049 NM 2007 2 12 SWAA070644 1 20070207 A 3350 417A5600201 SIGN BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 493WN 32477 MID CABIN EMERGENCY EXIT SIGN LOOSE. SECURED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007021200050 20070212 00050 NM 2007 2 12 SWAA070643 1 20070207 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 464WN 32468 EEPLS COVER LOOSE AT ROW 22 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007021200051 20070212 00051 NM 2007 2 12 SWAA070640 1 20070207 A 3210 544482517 ACTUATOR BOEING 737 7373H4 1384600 NM RT MLG FAULTY A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 321SW 23342 DIVERSION - RIGHT MLG UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF. CYCLED GEAR, NO HELP. RIGHT MLG DID NOT RETRACT. REMOVE D AND REPLACED RIGHT MLG LOCK ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2007021200135 20070212 00135 NM 2007 2 12 MZZA0700001 1 20070205 A 5610 58935841 WINDSHIELD BOEING 737 737824 13844BZ NM COCKPIT CRACKED A MZZA O OTHER O OTHER NR NOT REPORTED 1 WP 13 26232 26017 28942 THE L-5 COCKPIT WINDOW SHATTERED IN FLIGHT. NO OTHER PROBLEMS WERE REPORTED TO BE ASSOCIATED WITH THE OCCURRENCE. MAINTE NANCE FOUND THAT THE WINDOW HAD ALSO SEPARATED AND LIFTED AWAY FROM THE FUSELAGE FRAME. THE L-5 WINDOW WAS REMOVED AND R EPLACED IAW MM 56-11-31-400-801. THE L-4 WINDOW WAS ALSO REPLACED AS A PRECAUTION DUE TO DELAMINATION. BOTH WINDOWS WERE LEAK CHECKED IAW MM 05-51-91 AND ALL CHECKED GOOD. A WINDOW HEAT SYSTEM OPERATIONAL TEST WAS ALSO PERFORMED IAW MM 30-4 1-00-710-801 AND ALL CHECKED GOOD. 2 L 7 2 4F RT A16WE 2007021200136 20070212 00136 SO 2007 2 12 SIMA200703804 1 20070206 A 2710 14521026427 CONTROL CABLE EMB 145 EMB145LR 3260212 SO AILERONS WORN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 655AE 13348 4800 145452 FOUND RIGHT OUTBOARD AILERON CABLE WORN AT FRAME 35 FAIRLEAD. REMOVED AND REPLACED AILERON CABLE IAW EMB AMM 27-11-01. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007021200137 20070212 00137 EU 2007 2 12 SIMA200703802 1 20070206 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 253AE 12252 495 340B253 EMERGENCY PROXIMITY FLOOR LIGHT AT ROW 8 INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY AT POSITION 24LN IAW SAAB AMM 3 3-50-10. OPERATIONAL CHECK GOOD, RETURNED BACK TO SERVICE. 2 L 7 2 4T RT A52EU 2007021200138 20070212 00138 SO 2007 2 12 SIMA200703803 1 20070206 A 2910 UNKNOWN EMB 145 EMB145 3260210 SO HYD SYSTEM UNKNOWN A SIMA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 611AE 145074 HYDRAULIC SYSTEM 1 QUANTITY LEVEL WENT TO AMBER WITH LOW QUANTITY MESSAGE, ENGINE 1 HYDRAULIC SYSTEM PUMP FAIL MESSAGE, INTERMITTENT HYDRAULIC 1 FAIL MESSAGE, EMERGENCY DECLARED. POST INSPECTION FOUND HYDRAULIC FLUID ON NUMBER 1 ENGINE COW L. 2 L 7 2 4F RT T00011AT 2007021200139 20070212 00139 SO 2007 2 12 SIMA200703808 1 20070206 A 2710 14521026431 CONTROL CABLE EMB 145 EMB145LR 3260212 SO AILERONS WORN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 655AE 13348 4800 145452 FOUND LEFT OUTBOARD AILERON CABLE WORN AT FRAME 35 FAIRLEAD. REMOVED AND REPLACED AILERON CABLE IAW EMB AMM 27-11-01. O PERATIONAL CHECKED GOOD - RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007021200140 20070212 00140 SO 2007 2 12 SIMA200703801 1 20070205 A 2760 UNKNOWN EMB 145 EMB145LR 3260212 SO SPOILERS UNKNOWN A SIMA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 931AE 14500912 SPOILER FAILED, EMERGENCY DECLARED. PERFORMED SPOILER OPERATIONAL CHECK IAW EMB AMM 27-63-01 WITH NO DEFECTS NOTED, RET URNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007021200141 20070212 00141 SO 2007 2 12 SIMA200703806 1 20070206 A 5320 14521718007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 655AE 13348 4800 145452 FOUND ANGLE ON LEFT OMEGA BEAM CORRODED AT FRAME 20. REMOVED AND REPLACED ANGLE IAW EMB SRM 51-40-02. RETURNED AIRCRAF T TO SERVICE. 2 L 7 2 4T RT T00011AT 2007021200142 20070212 00142 SO 2007 2 12 SIMA200703805 1 20070206 A 2710 CONTROL CABLE EMB 145 EMB145LR 3260212 SO AILERONS WORN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 655AE 13348 4800 145452 FOUND LEFT INBOARD AILERON CABLE WORN AT FRAME 25 FAIRLEAD. REMOVED AND REPLACED AILERON CABLE IAW EMB AMM 27-11-01. O PERATIONAL CHECK GOOD, RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007021200143 20070212 00143 SO 2007 2 12 SIMA200703807 1 20070131 A 5320 14521725401 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 655AE 13348 4800 145452 FOUND CORROSION BEYOND LIMITS ON FORWARD SERVICE DOOR SILL. REPAIRED SILL IAW SRM 53-21-10, FIGURE 204, PAGE 216. INSTA LLED NEW DOUBLER IAW EMB IC2007-145/00685, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007021200144 20070212 00144 NM 2007 2 12 07FDEA00365 1 20070207 A 5100 UNKNOWN BOEING 727 727233 138408A NM UNKNOWN A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 267FE 21673 ON DEP AT 200'AGL (APPROX) RED WINDSHEAR WARNING LIGHT AND AURAL WARNING. PERFORMED ESCAPE MANV. FIREWALL POWER SET FO R ABOUT 3-5 SECONDS. WINDSHEAR WARN STOPPED AND LIGHT WENT OUT. RETURNED TO MEM. NO ENG PARAMETERS APPEARED TO BE EX CEEDED. AIRSPEED WAS STABLE AND A SMOOTH CLIMB-OUT. PERFORMED GPWS LEVEL 1, 2 AND 3 SELF TEST, NO CURRENT SYS FAULTS OR FLIGHT HISTORY FAULTS FOR LAST FLT LEG. REF 727-200 M/M 34-52-000-1. 2 L 7 3 4F RT A3WE 2007021200145 20070212 00145 NM 2007 2 12 07FDEA00367 1 20070207 A 5713 ARB75132 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 CRACK FOUND AT STRINGER END 13R (XORS 577), APPROX 13.5 INCHES LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. CRACK ON RIGHT HAND WING AT STRINGER END 13R (XORS 577) REPAIRED AS PER SRM 57-20- 00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007021200146 20070212 00146 NM 2007 2 12 07FDEA00368 1 20070207 A 5713 ARB75142 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 CRACK FOUND AT STRINGER END 14R (XORS 521), APPROX 14.5 INCHES LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. CRAC K ON RIGHT HAND WING AT STRINGER END 14R (XORS 521) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED A S MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007021200147 20070212 00147 NM 2007 2 12 07FDEA00369 1 20070207 A 5713 ARB75121 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 CRACK FOUND AT STRINGER END 12L (XORS 642), APPROX 12 INCHES LENGTH ON LT WING TANK DURING HFEC INSPECTION. CRACK ON LT WING AT STRINGER END 12L (XORS 642) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007021200148 20070212 00148 NM 2007 2 12 07FDEA00370 1 20070207 A 5713 ARB75131 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 CRACK FOUND AT STRINGER END 13L (XORS 577), APPROX 13 INCHES LENGTH ON LEFT HAND WING TANK DURING HFEC INSPECTION. CR ACK ON LT HAND WING AT STRINGER END 13L (XORS 577) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007021200149 20070212 00149 NM 2007 2 12 07FDEA00371 1 20070208 A 5713 ARB75141 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 CRACK FOUND AT STRINGER END 14L (XORS 521), APPROX 13 INCHES LENGTH ON LT WING TANK DURING HFEC INSPECTION. CRACK ON LT WING AT STRINGER END 14L (XORS 521) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007021200150 20070212 00150 NM 2007 2 12 07FDEA00372 1 20070208 A 5713 ARB75112 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 CRACK FOUND AT STRINGER END 11R (XORS 704), APPROX 13 INCHES LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. CRACK ON RT WING AT STRINGER END 11R (XORS 704) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR P ER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007021200151 20070212 00151 NM 2007 2 12 07FDEA00373 1 20070208 A 5713 ARB75102 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 CRACK FOUND AT STRINGER END 10R (XORS 760), APPROX 12 INCHES LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. REPAIRED AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007021200175 20070212 00175 NM 2007 2 12 USAA070089 1 20070206 A 4910 ATTACH ANGLE BOEING 757 7572B7 1384964 NM APU DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 941UW 27806 TOP, LWR & FWD SIDES OF APU INTAKE DOOR ON 3 ATTACH ANGLES HAS CORROSION. MFG ANGLES PER BOEING DWG 148N3152 & SRM 53-0 0-07, DEFECT SIZE: 10 SQ INCHES. 2 L 7 2 4F RT A2NM 2007021200176 20070212 00176 NM 2007 2 12 USAA070088 1 20070206 A 5320 146N5323U5 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM FUSLEAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 941UW 27806 AROUND NUT PLATE HOLES (90 PERCENT) CTR FLOOR SUPPORT BL 0 STA 1640-1681.8 HAS CORROSION. REPLACED CHANNELS PER SRM 51- 40-02; CORR TASK JL-58-53516; LEVEL 1, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A2NM 2007021200177 20070212 00177 NM 2007 2 12 USAA070087 1 20070206 A 5340 415N40014 MOUNT BOEING 757 7572B7 1384964 NM AFT GALLEY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 941UW 27806 AFT GALLEY LEFT OUTBOARD MOUNTS 2 EA AROUND BARREL NUT HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENT PART PER BOEIN G DWG 415N40C2; CORR LEVEL 1; TASK JL-58-53516, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A2NM 2007021200178 20070212 00178 NM 2007 2 12 USAA070086 1 20070206 A 5340 415N40014 MOUNT BOEING 757 7572B7 1384964 NM AFT GALLEY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 941UW 27806 AFT GALLEY RIGHT OUTBOARD MOUNTS 2 EA AROUND BARREL NUT HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER BOEING DWG 415N40C2; CORR LEVEL 1; TASK JL-58-5316, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A2NM 2007021200179 20070212 00179 NM 2007 2 12 USAA070085 1 20070206 A 5414 SKIN BOEING 737 7374B7 1384702 NM LT NACELLE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 24811 LEFT ENGINE PYLON PANEL OPENING 572L AT O/B AFT CORNER OF OPENING CRACKED. STOP DRILLED CRACK & INSTALLED REPAIR DOUBLE R PER TYP REP 54-30-07, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007021200180 20070212 00180 NM 2007 2 12 USAA070084 1 20070206 A 5320 INTERCOSTAL BOEING 737 7374B7 1384702 NM BS 360 S11L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 STA 360 & S-11L CRACKED. REMOVED DAMAGE & INSTALLED FABRICATED REPAIR PARTS PER BOEING DWG 65-17685, DEFECT SIZE: 1 IN CH. 2 L 7 2 4F RT A16WE 2007021200181 20070212 00181 NM 2007 2 12 USAA070083 1 20070206 A 5340 ANGLE BOEING 737 7374B7 1384702 NM BS 360 S13L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 BS 360 S-13L CRACKED. REMOVED & REPLACED WITH FABRICATED PART PER BOEING DWG 65-17685, DEFECT SIZE: .250 INCH. 2 L 7 2 4F RT A16WE 2007021200182 20070212 00182 NM 2007 2 12 USAA070082 1 20070206 A 5340 ANGLE BOEING 737 7374B7 1384702 NM BS 360 S8L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 INTERCOSTAL ANGLE STA 360 AND S-8L CRACKED. MANUFACTURED PART PER DWG 69-48985, DEFECT SIZE: .75 INCH. 2 L 7 2 4F RT A16WE 2007021200185 20070212 00185 EU 2007 2 12 LGP3219N14834 1 20070206 A 2612 FIRE LOOP AEROSP ATR42 ATR42320 8680930 EU NR 2 NACELLE MALFUNCTIONED A HYIA O OTHER N FALSE WARNING LD LANDING 1 NE 01 14834 193 NR 2 ENGINE FIRE LOOP A MEL'D, JUST PRIOR TO LANDING, CREW REPORTED NR 2 ENGINE FIRE WARNING. CREW VERIFIED NO FIRE, TH IS SAME PROBLEM OCCURRED ON PREVIOUS FLIGHT. MX REMOVED AND REPLACED LOOP A HARNESS, REPOSITIONED LOOP B HARNESS CLAMP CUSHIONS, MEL RESTORED. 2 H 7 2 4T RT A53EU 2007021200191 20070212 00191 EU 2007 2 12 0500070001 1 20070203 A 2612 FIRE LOOP AEROSP ATR42 ATR42320 8680930 EU NR 2 NACELLE MALFUNCTIONED A HYIA E ENGINE SHUTDOWN N FALSE WARNING LD LANDING 1 NE 01 14834 193 JUST PRIOR TO LANDING, CREW RECEIVED NR 2 ENGINE FIRE WARNING ON FIRE HANDLE AND CONDITION LEVER. CREW VERIFIED NO FIRE , SHUT DOWN AFTER LANDING AS A PRECAUTION. MX FOUND NR 2 ENGINE LOOP A FAULT AT 40 PERCENT POWER. MEL NR 2 LOOP A AND RELEASED AIRCRAFT BACK TO SERVICE. 2 H 7 2 4T RT A53EU 2007021200192 20070212 00192 EU 2007 2 12 04328N14834 1 20070203 A 2612 FIRE LOOP AEROSP ATR42 ATR42320 8680930 EU NR 2 NACELLE MALFUNCTIONED A HYIA O OTHER N FALSE WARNING LD LANDING 1 NE 01 14834 193 NR 2 ENGINE FIRE LOOP MEL'D, JUST PRIOR TO LANDING, CREW REPORTED NR 2 ENGINE FIRE WARNING. CREW VERIFIED NO FIRE, THIS SAME PROBLEM OCCURRED ON PREVIOUS FLIGHT. 2 H 7 2 4T RT A53EU 2007021200195 20070212 00195 NM 2007 2 12 07FDEA00347 1 20070206 A 5730 6521656854 PANEL BOEING 727 727233 138408A NM ZONE 600 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 RT WING INBD TE LWR SURFACE PANEL JUST OB OF MLG FWD TRUNNION, DELAMINATED ON UPPER SURFACE FWD EDGE. OIL SOAKED REMOV ED DAMAGED PANEL ASSY. TRIED TO REMOVE DAMAGE REF SRM 51-40-9 PG 4 AND DAMAGE WAS MORE THEN 25% OF PANEL, BEYOND REPAIR ABLE LIMITS REF SRM 51-40-9 PG 25. REPLACED AND REINSTALLED NEW PANEL ASSY (AA2923) REF SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007021200196 20070212 00196 NM 2007 2 12 AT0700014 1 20070127 A 5230 PAN BOEING 717 717200 1383700 NM AFT CARGO DOOR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 967AT 55028 AFT CARGO DOOR FWD CAM CUTOUT CRACK. INSTALLED ANGLE REPAIR 2024T3 .063 X 30 X 7.0 PER B717 SRM 52-30-02 FIG 201 REPAIR 4. 2 L 7 2 4F TR A6WE 2007021200197 20070212 00197 NM 2007 2 12 07FDEA00348 1 20070206 A 5314 STIFFENER BOEING 727 727233 138408A NM KEELBEAM CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 LT MLG WHEEL WELL KEEL BEAM STIFFENER IS CRACKED AT BL 0, STA 930, WL 198. REMOVED CRACKED STIFFENER, FABRICATED AND IN STALLED NEW STIFFENER REF SRM 51-30-2 PG 2. CLASSIFIED AS MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007021200198 20070212 00198 NM 2007 2 12 07FDEA00349 1 20070206 A 5411 RIB BOEING 727 727233 138408A NM NR 3 NACELLE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 NR 3 ENGINE UPPER COWL 2ND FROM FWD END RIB IS GOUGED ACCOMPLISHED TYPICAL FORMED REPAIR ON NR 3 ENG UPPER COWL REB REF SRM 51-43-3, PG 1-3 FIG 1. REINSTALLED NR 3 ENG UPPER COWL REF MM 71-10-011-4. 2 L 7 3 4F RT A3WE 2007021200199 20070212 00199 NM 2007 2 12 07FDEA00350 1 20070206 A 5710 6521656142 STRUCTURE BOEING 727 727233 138408A NM RT WING FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 RT WING INBD T/E WAFFLE BOARD HAS PANEL FASTENERS PULLED THROUGH AT LWR SPAR FLANGE JUST FWD OF MLG MAIN ACTUATOR REMOVE D DAMAGE WAFFLE BOARD AND INSTALLED NEW SEAL AND WAFFLE BOARD IN AREA, REF SRM 51-30-2 PG 2-5. 2 L 7 3 4F RT A3WE 2007021200200 20070212 00200 NM 2007 2 12 07FDEA00351 1 20070206 A 5321 FLOOR PANEL BOEING 727 727233 138408A NM CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 LWR AFT CARGO COMPT NR 4 FLOOR PANEL HAS SEVERAL DEEP GOUGES AND IS CRACKED THROUGH AT BS 1035 BL ''0'' CUT SHEETMATAL T O FORM OF OLD FLOOR PNL. JOGGLED EDGED, TRANSFERED FASTENER HOLES FOR PANEL, PRIMED BACK (UNDERSIDE) OF PNL. INSTALLED FASTENERS SECURING FLOOR PNL. 2 L 7 3 4F RT A3WE 2007021300011 20070213 00011 EA 2007 2 13 SWIA200717787 1 20070205 A 2913 887055 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM FAILED A SWIA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 07 960SW 7853 AT FLAP 8 DEGREES GOT HYDRAULIC 1B PUMP CAUTION MESSAGE FOLLOWED BY HYDRAULIC 1B LOW PRESSURE. SYSTEM RAN DRY FOR 20 MI NUTES. REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW AMM 29-11-01 AND REPLACED NR 1 ACMP IAW AMM 29-11-03. OPERATIONA L CHECKS GOOD, SN OFF: MX666036. ACMP PN OFF: 848847 SN OFF: MX666036. 2 L 7 2 4F RT A21EA 2007021300022 20070213 00022 NM 2007 2 13 F3LA200700019 1 20070206 A 3350 321431 BATTERY AIRBUS A319 A319111 3930336 NM EMERGENCY LIGHT DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 918FR 5911 1943 DURING C-3 CHECK, INSPECTION REPORTED LT OVERWING EMERGENCY LIGHTING BATTERY FAILED DURING OPS CHECK. REPLACED LT OVERW ING EPSU BATTERY (11WL) IAW AMM 33-51-38-400-002. 2 L 7 2 4F RT A28NM 2007021300052 20070213 00052 NM 2007 2 13 DL76S070100 1 20070209 A 5313 STRINGER BOEING 767 767332 1382001 NM BS 434-456 S34R DEFORMED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 FOUND STRINGER 34R DEFORMED AT STA 434-456. REPAIRED PER SRM 53-30-03 FIG 201 REPAIR 1. 2 L 7 2 4F RT A1NM 2007021300071 20070213 00071 NM 2007 2 13 DL76S070108 1 20070210 A 5313 STRINGER BOEING 767 767332 1382001 NM BS 500-522 S38R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 FOUND STRINGER 38R STA 500-522 CORRODED. STRINGER REPAIRED PER SRM 53-00-03 FIG 201, REPAIR 2. 2 L 7 2 4F RT A1NM 2007021300072 20070213 00072 EU 2007 2 13 R61A20070004 1 20070208 A 3240 900005831PR BRAKE ASSY EMB ERJ170 ERJ170100 EU MLG FROZEN A R61A O OTHER O OTHER LD LANDING 1 GL 11 814MD 3145 8 17000033 CREW REPORTED TIRE HAD BLOWN ON LANDING. MAINTENANCE REPORTED RIGHT HAND OUTBOARD BRAKE FROZEN/LOCKED-UP. MAINTENANCE REPLACED THE RIGHT HAND OUTBOARD BRAKE ASSEMBLY (ABSC) AND THE NR 3 AND NR 4 MLG WHEEL ASSEMBLIES. 2 L 7 2 4F RT A56NM 2007021300077 20070213 00077 WP 2007 2 13 ABXA070040 1 20070131 A 5320 991050131 CUSP WEB DOUG DC9 DC941 302207N WP BS 224 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 CUSP WEB CRACKED AT RIGHT BUTT LINE 54, STA 224. REPAIRED CUSP WEB AT RIGHT BUTT LINE 54, STA 224 IAW DC9 SRM 53-01, FI GURE 2. 2 L 7 2 4F A6WE 2007021300083 20070213 00083 CE 2007 2 13 DXTA200701919 1 20070208 A 3240 UNKNOWN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE BRAKES UNKNOWN E DXTA O OTHER O OTHER LD LANDING 1 GL 07 358QS 5600455 RT SEAT BRAKE PEDALS REQUIRE EXCESSIVE TRAVEL BEFORE BRAKING ACTION OCCURS. BRAKING ACTION APPEARS NORMAL AND BRAKES HO LD ACFT STATIONARY AT HIGH POWER SETTINGS. VERIFIED DISCREPANCY. INSPECTED MASTER CYLINDERS AND CHECKED TIGHTNESS OF F ITTINGS. NO DEFECTS NOTED. BLED BRAKE SYSTEM AND SERVICED RESERVOIR PER CESSNA 560 M/M 32-42-00. OPS AND LEAK CHECK G OOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2007021300087 20070213 00087 CE 2007 2 13 DXTA200701923 1 20070208 A 3240 BRAKE ASSY CESSNA 680 680CE 2076811 CE MLG HOT E DXTA O OTHER M J OVER TEMP WARNING INDICATION LD LANDING 1 GL 07 365QS 6800057 UPON APPLIED BRAKES A/C PULL TO THE LT. AT SHUTDOWN, LT INSIDE BRAKE WAS SMOKING AND VERY HOT. TAXI TIME WAS GREATER T HAN 5 MIN. BRAKES DID NOT PULL AT TAXI SPEED. INSPECTED BRAKES. NO DEFECTS NOTED. TAXIED AIRCRAFT. FOUND BRAKE SYSTEM TO BE OPERATING NORMAL. UNABLE TO DUPLICATE DISCREPANCY. NO FURTHER ACTION REQUIRED. WORK PERFORMED I.A.W. CHAPTER 32 -41-00 OF THE CITATION 60 MM. 2 L 7 2 4F RC T00012WI 2007021300088 20070213 00088 CE 2007 2 13 DXTA200701924 1 20070208 A 3260 INDICATOR BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE MLG INTERMITTENT E DXTA O OTHER N FALSE WARNING DE DESCENT 1 GL 07 125QS RK433 BOTH LT AND RT MAIN GEAR INDICATOR LIGHTS WERE INTERMITTENT AND AT TIMES WOULD NOT ILLUMINATE AT ALL WHEN GEAR WAS SELEC TED DOWN, ALL OTHER INDICATIONS WERE, CORRECT. ACCOMPLISHED CHECKLIST AND LANDED NORMALLY ALTERNATE GEAR EXTENSION WAS N OT USED. TROUBLESHOT FOUND LIGHT ASSEMBLY FOR THE GEAR INDICATOR TO BE FAULT. REMOVED AND REPLACED GEAR INDICATOR LIGHT ASSEMBLY IWTH NEW UNIT. OPERATION CHECK IS GOOD. ALL WORK PERFORMED I.A.W. HAWKER 400XP AMM 32-60-00. 2 H 7 2 4F 4 F RT A16SW E25EA 2007021300097 20070213 00097 EU 2007 2 13 07FDEA00426 1 20070209 A 5730 SKIN AIRBUS 300 A300B4622 3930401 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 717FD 361 L/T WING BOTTOM SKIN UPPER SURFACE CORROSION ADJACENT TO HYD PRESSURE LINE THROUGH HOLE. AREA WHERE HYD LINE AT WING T/ E PASS THROUGH TO NR 1 PYLON. AFTER CORROSION REMOVAL, HYDRAULIC LINE PASS, THROUGH HOLES WERE FOUND TO BE ELONGATED. HYDRAULIC BULKHEAD FITTINGS WORN. REPLACED BULKHEAD 2 FITTINGS P/N A9348226020400. REPAIRED WING SKIN PASS-THROUGH HOL ES REF: FED-EX EA 6-5730-102780, SEE FED-EX N/R N00656 OF W/O 00035272. 2 L 7 2 4F RT A35EU 2007021300101 20070213 00101 EA 2007 2 13 A6WA200740016 1 20070110 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 412AW 7582 RIGHT FS 621 FLOOR SUPPORT ANGLE IS CRACKED .5 INCH LONG IN OUTBOARD RADIUS. MAINTENANCE REPAIRED FLOOR SUPPORT IAW BOM BARDIER REO 601R-53-61-117 REV C. (M) 2 L 7 2 4F RT A21EA 2007021300105 20070213 00105 NM 2007 2 13 UPS07449146 1 20070104 A 5310 PLATE BOEING 747 747123 1384873 NM BS 780 MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D LEFT BS 780 TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D LEFT BS 780 TENSION TIE ATTA CH STEEL PLATE SHORT EDGE MARGIN REPAIRED AS PER RS R53-25-35713. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-3571 3 AND UPS EO B747-5310-25938. 2 L 7 4 4F A20WE 2007021300113 20070213 00113 NM 2007 2 13 CALA0700058 1 20070209 A 5330 141N3841 SKIN BOEING 757 757224 1384958 NM BS 202 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12125 28967 INSPECTION FOUND LIGHTNING DAMAGE AT FASTENER BS 202 BETWEEN S18L AND S19L. AN INTERIM REPAIR WAS PERFORMED IAW ECRA 53 30-03537, REV A, PART 1A. A DIP WAS ISSUED TO REINSPECT THE AREA PRIOR TO ACCOMPLISHMENT OF 37,500 FLIGHT CYCLES AND TH EREAFTER AT INTERVALS NOT TO EXCEED 12,000 FLIGHT CYCLES. 2 L 7 2 4F RT A2NM 2007021300115 20070213 00115 NM 2007 2 13 CALA0700060 1 20070210 A 5315 6546812 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 INSPECTION FOUND FLOORBEAM CORRODED AT NUT PLATES ON TOP AND BOTTOM, STA 1016, LBL 6 TO LBL 34. THE FLOORBEAM CHORD WA S REMOVED AND REPLACED IAW ECRA 5310-03851. 2 L 7 2 4F RT A16WE 2007021300118 20070213 00118 EU 2007 2 13 USAA070093 1 20070209 A 5322 D5347112420000 SHEAR TIE AIRBUS A321 A321211 3930370 EU CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 169UW 1455 FR 69 - 70 AT Y1162.5 HAS CORROSION. REPLACED SHEAR TIE PER SRM 51-72-11; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 4 SQ INCHES. 2 L 7 2 4F RT A28NM 2007021300120 20070213 00120 NM 2007 2 13 USAA070091 1 20070209 A 5330 SKIN BOEING 737 737301 1384611 NM BS 745 S24 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 STA 745 AND S-24R CRACKED. INSTALLED DOUBLER PER SRM 51-00-01 REPAIR 3 DETAIL XI, DEFECT SIZE: 1.25 INCH. 2 L 7 2 4F RT A16WE 2007021300122 20070213 00122 EA 2007 2 13 TRAX200700176 1 20070205 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 THE 2ND FROM AFT RIGHT EXTERNAL EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007021300124 20070213 00124 EA 2007 2 13 TRAX200700178 1 20070205 A 3250 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING UNKNOWN A ASOA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 27 933EV 8022 NWS INOP MESSAGE. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007021300128 20070213 00128 EA 2007 2 13 TRAX200700182 1 20070202 A 5320 INTERCOSTAL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 ASD LOWER AFT INTERCOSTAL CRACKED INSIDE SHOOT BOLT ACCESS PANEL 832BR. REMOVED AND REPLACED INTERCOSTAL IAW CRJ 700 SR M 51-42-06 OPS CK GOOD IAW CRJ 700 MM 52-11-00. 2 L 7 2 4F RT A21EA 2007021300129 20070213 00129 EA 2007 2 13 TRAX200700183 1 20070203 A 5260 HANDLE CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 ASD OUTER HANDLE CRACKED IN RADIUS (MARKED). REMOVED DOOR HANDLE AND TRANSFERED HARDWARE (NOT SAFTIED). PER AMM 52-11-0 0. PRIMED AND PAINTED NEW OUTER PAX DOOR HANDLE PER CRJ 700 SRM 51-21-16. SAFTIED HARDWARE PER CRJ 700 AMM 20-00-00 OK T O INSTALL OUTER PAX DOOR HANDLE INSTALLD NEW OUTER PAX DOOR HANDLE PER CRJ 700 AMM 52-11-00. 2 L 7 2 4F RT A21EA 2007021300130 20070213 00130 NM 2007 2 13 SWAA070684 1 20070208 A 5311 141A1140 FRAME BOEING 737 7377H4 1384404 NM BS 330 S6R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 DURING SCHEDULED 6Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 330, STR 6R. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007021300131 20070213 00131 NM 2007 2 13 SWAA070679 1 20070208 A 5315 141A55045 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 708SW 27842 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 19 TO RBL 57. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007021300006 20070213 00006 EU 2007 2 13 07FDEA00430 1 20070209 A 5420 SUPPORT BRACKET AIRBUS 310 A310203 3930313 EU NR 2 NACELLE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 5 ELONGATED HOLES EXIST AT NR 2 ENGINE PYLON UNDERNEATH HYD SUPPORT BRACKET ACCESS PNL NR 483 CL. REPAIRED PYLON IAW 6- 5450-106327. 2 L 7 2 4F RT A35EU 2007021300009 20070213 00009 EU 2007 2 13 07FDEA00433 1 20070209 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 FOUND CRACK IN FLOORBEAM UNDER CLS ADAPTER AT FR 58 BETWEEN TRACK 4R AND 5R COMPLIED WITH EA 6-5310-106317 PG 1 REF 4. 2 L 7 2 4F RT A35EU 2007021300010 20070213 00010 EU 2007 2 13 07FDEA00434 1 20070209 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 MDC SEAT TRACK NR 3 R AT FR 68 R HAS CORROSION REPAIRED SEAT TRACK IAW A310-200 SRM 53-10-16. 2 L 7 2 4F RT A35EU 2007021300017 20070213 00017 EA 2007 2 13 TRAX200700163 1 20070130 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT NO TEST A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 908EV 7654 LEFT EMERGENCY EXIT DOOR FAILS PULL TEST (MTC). 2 L 7 2 4F RT A21EA 2007021300026 20070213 00026 2007 2 13 F3LA200700022 4 20070206 A 2565 L32A319160001 CONTROL CABLE AIRBUS A319 A319111 3930336 NM ESCAPE SLIDE STUCK A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 5911 1943 DURING C-3 CHECK, INSPECTION REPORTED RT FLEXIBLE CONTROL CABLE FOR OVERWING SLIDE INFLATION BOTTLES WOULD NOT RETRACT. REPLACED RT FLEXIBLE CONTROL CABLE FOR OVERWING SLIDE INFLATION BOTTLE IAW AMM 25-62-43-000-001, AMM 25-62-43-400-001, MM 25-23-43, PB 401, AND MM 25-23-48, PB 401. 2 L 7 2 4F RT A28NM 2007021300028 20070213 00028 EU 2007 2 13 UG8A2007GM001 2 20070129 A 7230 STATOR RROYCE 6118C GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU COMPRESSOR CRACKED E UG8A K NONE O OTHER IN INSP/MAINT 1 GL 23 5115 718 85053 4019 85053 DURING VOLUNTARY COMPLIANCE WITH MFG SB 72-1706 (BORESCOPE INSPECTION OF HP COMPRESSOR 7TH STAGE STATOR VANE) A CRACKED STATOR VANE WAS DISCOVERED. 2 L 7 2 4F 4 F RT A12EA E25NE 2007021300032 20070213 00032 NM 2007 2 13 UPS07449133 1 20070103 A 5310 TENSION TIE BOEING 747 747123 1384873 NM BS 840 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D RIGHT BS 840 TENSION TIE TO FRAME CONNECTION FOUND 1EA HOLE CRACK AT TENSION TIE FWD CHANNEL (CRAC K LENGTH 0.060"). M/D LEFT TO RIGHT TENSION TIE FWD CHANNEL REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 & SRM 51-30 -02 & UPS EO B747-5310-23715 APPENDIX B REFER HX NRC AFF502047 FOR WORKING DETAIL. 2 L 7 4 4F A20WE 2007021300033 20070213 00033 NM 2007 2 13 UPS07449139 1 20070207 A 2916 SWIVEL BOEING 747 747123 1384873 NM NR 4 RESERVOIR LEAKING A IPXA O OTHER K FLUID LOSS NR NOT REPORTED 1 SO 01 676UP 20101 INSPECTION TYPE:N/A COMPLETE LOSS OF HYD QTY IN FLIGHT, ON SYSTEM NR 4. NOTE: RESERVOIR NR 4 INDICATED 1 GALLON. FOUN D RIGHT MAIN GEAR DOWNLOCK ACTUATOR FWD HOSE NEAR UPPER FITTING AT SWIVEL LEAKING. REMOVED AND REPLACED HOSE ASSY, SERV ICED NR 4 HYD QTY PRESSURIZED & OPERATED SYSTEM REF MM 32- 32-15. NO LEAKS NOTED. RAN NR 4 ENG HYD PUMP & ADP OK. 2 L 7 4 4F A20WE 2007021300035 20070213 00035 NM 2007 2 13 UPS07449141 1 20070104 A 5310 TENSION TIE BOEING 747 747123 1384873 NM BS 780 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D RIGHT BS 780 TENSION TIE TO FRAME CONNECTION FOUND 1EA HOLE CRACK AT TENSION TIE CHANNEL RUNNING U P AND DOWN APPROX .0625 INCH CRACK LENGTH .125 INCH. M/D RIGHT BS 780 TENSION TIE FWD CHANNEL REPAIRED AS PER RS R53-25 -35713, CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35713 AND UPS EO B747-5310-25938. 2 L 7 4 4F A20WE 2007021300037 20070213 00037 NM 2007 2 13 UPS07449143 1 20070104 A 5310 PLATE BOEING 747 747123 1384873 NM BS 800 MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D LEFT BS 800 TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D LEFT BS 800 TENSION TIE ATTA CHED STEEL PLATE SHORT EDGE MARGIN REPAIRED AS PER RS R53-25-35710. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35 710 AND UPS EO B747-5310-25925. 2 L 7 4 4F A20WE 2007021300038 20070213 00038 NM 2007 2 13 ZZDA070113133 1 20070113 A 5330 SKIN BOEING 717 717200 1383700 NM FS 218 L17L DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 992AT 55136 FUSELAGE HAS DENT AT FS 218 LONG 17 LT. REWORKED DENT AND INSTALLED INTERNAL DOUBLER REPAIR 2024T3 .032 PER SRM 53-00-0 1 REPAIR 2 PG 217. 2 L 7 2 4F TR A6WE 2007021300039 20070213 00039 NM 2007 2 13 DU4R2007056 1 20070121 A 5340 6945555Y11 SUPPORT FITTING BOEING 757 757232 1384965 NM BS 580 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 684DA 27104 FOUND CORROSION ON THE TIE BLOCK SUPPORT BRACKET NR 3 FROM FWD, AT FWD CARGO DOOR LWR SILL, ZONE 122. REMOVED BRACKET. INSTALLED TIE DOWN BLOCK FITTING P/N 69-45555Y11IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007021300045 20070213 00045 EA 2007 2 13 TRAX200700174 1 20070204 A 3250 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING UNKNOWN A ASOA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 980EV 7759 RECEIVED -STEERING INOP- CAUTION MESSAGE AFTER GEAR RETRACTION. RAN QRH, LANDED WITH NWS OFF. RESET BREAKERS ON GROUND AND NWS RESET. TAXIED TO GATE AS NORMAL. EMERGENCY DECLARD. FLTS 4423, 4430 CX. 2 L 7 2 4F RT A21EA 2007021300046 20070213 00046 EA 2007 2 13 TRAX200700175 1 20070204 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA RT OVERWING INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 821AS 7194 RIGHT OVERWING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007021300047 20070213 00047 NM 2007 2 13 DL76S070094 1 20070207 A 5415 112T7003 FITTING BOEING 767 767332 1382001 NM PYLON SCORED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 DURING THE ACCOMPLISHMENT OF BOEING S/B 767-54-0081 R1 WHILE IN HMV AT ACTS THE OUTBOARD PYLON SIDE LOAD FITTING BORE WA S WITH DEEP SCORE MARKS AND OVERSIZED TO 2.244" WHICH EXCEEDS S/B CLEANUP LIMITS. THIS IS SUBJECT TO AD 2004-16-12. THE DAMAGE WAS CLEANED UP AND A REPAIR BUSHING WAS INSTALLED. AN AMOC WAS RECIEVED AND DOCUMENTED PER ER/A 459797-14. 2 L 7 2 4F RT A1NM 2007021300048 20070213 00048 NM 2007 2 13 DL76L070095 1 20070207 A 2410 IDG BOEING 767 767332 1382001 NM RIGHT UNKNOWN A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 196DN 28453 RT GEN OFF ILLUMINATED. FOUND GEN DIODE FAULT ON BPCU-TRIED GCU NO HELP. REINSTALLED ORIG, REPLACED AND TESTED RT IDG PER MM ALL CHKS NORMAL. 2 L 7 2 4F RT A1NM 2007021300064 20070213 00064 NM 2007 2 13 ZZDA070115134 1 20070115 A 5230 SKIN BOEING 717 717200 1383700 NM AFT CARGO DOOR DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 967AT 55028 DENT ON AFT CARGO DOOR CENTER OF DOOR. INSTALLED FLUSH REPAIR PER SRM 52-00-01 FIG 204, PERFORMED NDT NO CRACK NOTED. 2 L 7 2 4F TR A6WE 2007021300073 20070213 00073 WP 2007 2 13 ABXA070036 1 20070126 A 5313 5924878501 LONGERON DOUG DC9 DC941 302207N WP BS 794 L30 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 LONGERON 30 CORRODED AT FS 794. REPAIRED IAW REA D953-55365 MR AND DC9 SRM 55-02, FIGURE 12. 2 L 7 2 4F A6WE 2007021300076 20070213 00076 WP 2007 2 13 ABXA070039 1 20070128 A 5347 S4925848M12000 SEAT TRACK DOUG DC9 DC941 302207N WP BS 636-655 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 CENTER TRACK CORRODED BETWEEN FS 636 - 655. REMOVED AND REPLACED CENTER TRACK STA 590 - 972 IAW DC9 SRM 51-30-1 AND 51- 10-4. 2 L 7 2 4F A6WE 2007021300079 20070213 00079 NM 2007 2 13 WRLA2007031 1 20070209 A 5753 SKIN DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE TE FLAPS DEBONDED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 62911 48407 DURING 3C + 12A CHECK, EGAT MECHANIC FOUND LEFT WING OUTBOARD FLAP WEDGE INBOARD SIDE DISBOND ABOUT 4 INCHES. CHECK THE DAMAGE AREA AND CLEANUP. BONDED FIBERGLASS FABRIC USE WET LAYUP AT TEMP 160 DEGREE F, 90 MINS VACUUM;22 INCH/HG CURE P ER MD11F SRM VOL 57-90-00 & VOL II 51-62-01 REV.38. TAP TEST & CONDITION CHK WAS SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2007021300085 20070213 00085 CE 2007 2 13 DXTA200701921 1 20070208 A 2120 VENT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CABIN AIR SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 967QS 7500067 SMOKE WAS DETECTED COMING FROM AIR VENT IN COCKPIT AND CABIN. REPLACED FORWARD ACM IAW CE-750 M/M CHAPTER 21-51-00. OPE RATIONAL AND LEAK CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007021300091 20070213 00091 NM 2007 2 13 QXEA200700157 1 20070209 A 6120 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM ENGINE UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 418QX 4143 PDX FLIGHT NR 2356: RECEIVED A POWER PLANT MESSAGE WHEN REDUCED NP. MAINTENANCE INTEROGATED CDS AND FOUND CODE 494. CL EARED FAULT IAW AMM 61-20-36-070-801. AFTER NO FAULTS WERE FOUND, C/W FIM TASK 61-20-10-810-826 AND PERFORMED AUTO FEAT HER TEST. TESTED GOOD. NO PARTS REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007021300093 20070213 00093 NM 2007 2 13 AMTA200700046 1 20070131 A 2410 727792M GENERATOR BOEING 757 75733N 1384931 NM RROYCE RB211 RB211* 54555 NE LEFT UNSERVICEABLE A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 552TZ 15441 3762 32586 LT GEN DRIVE LGT DID NOT ILLUMINATE WITH ENGINE SHUTDOWN. REMOVED AND REPLACED LT ENG. IDG IAW M57-24-01. OPS CHECK A ND LEAK CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM A12EU 2007021300095 20070213 00095 NM 2007 2 13 AMTA200700057 1 20070202 A 2420 GENERATOR BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE FAILED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 552TZ 32586 HMG WILL NOT PROVIDE ELECTRICAL POWER WHEN OPERATED. REMOVED AND REPLACED HMG IAW MM 24-25-02-4. HMG OPS GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007021300098 20070213 00098 CE 2007 2 13 DXTA200701926 1 20070208 A 3213 STRUT CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE RT MLG DISCHARGED E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 347QS 5600357 DURING GEAR EXTENSION , DID NOT ACHIEVE A GREEN( LOCKED INDICATION) ON THE RIGHT MAIN GEAR. RAN THE GEAR WILL NOT EXTEN D CHECKLIST. GEAR WAS DOWN BUT NOT LOCKED. ACHIEVED A GREEN LIGHT AS RESULT OF CHECKLIST. JACK A/C DEPLETED NITROGEN IN LANDING GEAR, LUBE AND INSPECTED RT MAIN GEAR, SERVICED EMERGENCY NITROGEN BOTTLE, RAN GEAR 10X AND MORE OPS AND LEA K CHECK GOOD ALL WORK DONE IAW CE560 M/M 32-30-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007021300100 20070213 00100 NM 2007 2 13 QXEA200700156 1 20070209 A 3297 471515 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM MLG UNKNOWN A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 415QX 305 4081 SEA TO MFR FLIGHT NR 2457: AFTER TAKEOFF, ALL THREE GEARS FAILED TO RETRACT. THREE RED AND THREE GREEN LIGHTS REMAINED I LLUMINATED. RAN CHECKLIST. NO HELP. HANDLE DID ILLUMINATED AMBER. FLIGHT WAS DIVERTED TO PDX. MAINTENANCE REMOVED N LG WOW 2 CENTERING WIRING HARNESS IAW 32-31-11-000-801AND REPLACED IAW INSTALLATION AMM TASK 32-21-11-400-801. OPS CHEC K GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007021300102 20070213 00102 EA 2007 2 13 A6WA200740017 1 20070110 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 412AW 7582 FOUND LEFT FS 621 FLOOR SUPPORT ANGLE IS CRACKED .5 INCH LONG IN OUTBOARD RADIUS. MAINTENANCE REPAIRED FS 621 FLOOR SUP PORT ANGLE IAW BOMARDIER REO 601R-53-61-117. (M) 2 L 7 2 4F RT A21EA 2007021300103 20070213 00103 EA 2007 2 13 A6WA200740022 1 20070110 A 5320 6003106819 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 460 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 412AW 7582 FOUND FS 460 FLOOR SUPPORT FITTING CRACKED OUTBOARD SIDE OF RBL 9, APPROX 1 INCH LONG. MAINTENANCE REMOVED AND REPLACED FITTING P/N 600-31068-19 AT FS 460.0 RBL 9,0 IAW CRJ SRM 51-40-11, 51-42-06 AND 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007021300106 20070213 00106 NM 2007 2 13 UPS07449147 1 20070104 A 5310 PLATE BOEING 747 747123 1384873 NM BS 900 MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D RIGHT BS 900 TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D RIGHT BS 900 TENSION TIE A TTACH STEEL PLATE SHORT EDGE MARGIN REPAIRED AS PER RS R53-25-35715. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-3 5715 AND UPS EO B747-5310-25936. 2 L 7 4 4F A20WE 2007021300108 20070213 00108 NM 2007 2 13 UPS07449149 1 20070109 A 5311 FRAME BOEING 747 747123 1384873 NM BS 2140 S25-26L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 2140 STR 25-26L FRAME FOUND CRACK. CRACK LENGTH .5 INCH. M/D BS 2140 BEWTEEN STR 25-26L FRAME REPAIRED AS PER RS R53-62-35726. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-62-35726 AND UPS EO B747-5310-26041. 2 L 7 4 4F A20WE 2007021300111 20070213 00111 NM 2007 2 13 UPS07449152 1 20070109 A 5311 FRAME BOEING 747 747123 1384873 NM BS 1800 S22-23R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D BS 1800 STR 22-23R FRAME I/B CHORD FOUND CRACK. CRACK LENGTH .5 INCH. M/D BS 1800 STR 22-23R FRA ME I/B CHORD REPAIRED AS PER RS R53-62-35721 AND UPS EO B747-5310-26036. 2 L 7 4 4F A20WE 2007021300114 20070213 00114 NM 2007 2 13 CALA0700059 1 20070209 A 5311 FRAME BOEING 737 7373T0 1384582 NM BS 616 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 INSPECTION FOUND A 1 INCH CRACK IN LT FRAME AT STA 616, S17L TO S18L BELOW FLOOR LINE. THE CRACKED AREA OF FRAME WAS RE MOVED AND A REPAIR ANGLE AND FILLER WAS INSTALLED IAW ECRA 5311-01158. 2 L 7 2 4F RT A16WE 2007021300116 20070213 00116 NM 2007 2 13 CALA0700061 1 20070211 A 5311 FRAME BOEING 737 7373T0 1384582 NM BS 616 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 INSPECTION FOUND A 1 INCH CRACK IN RT MAIN FRAME AT STA 616 BELOW FLOOR LINE. THE CRACKED AREA OF FRAME WAS REMOVED AND A REPAIR ANGLE WAS INSTALLED IAW ECRA 5311-01158. 2 L 7 2 4F RT A16WE 2007021300117 20070213 00117 NM 2007 2 13 NWAA070546302 1 20070207 A 2497 RECEPTACLE BOEING 747 747451 1384940 NM LAVATORY BURNED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 662US 23720 DURING CRUISE, FLIGHT ATTENDANT REPORTED LIGHTS IN LAV BY DOOR 2L INOP AND STRONG ELECTRICAL BURNING SMELL. AIRCRAFT WA S DIVERTED TO ANC, AND AN EMERGENCY WAS DECLARED. LANDING WAS UNEVENTFUL. MAINTENANCE FOUND CHARRING IN ELECTRIC SOCKE T. BALLAST WIRING WAS DISCONNECTED AND SECURED. LAV WAS MEL’D PER 38-30-1A, AND AIRCRAFT WAS RETURNED TO SERVICE. BAL LAST 63-3300-3-0185 IS ON ORDER AND ASSIGNED TO BE INSTALLED 09FEB07 IN NRT. 2 L 7 4 4F RT A20WE 2007021300119 20070213 00119 EU 2007 2 13 USAA070092 1 20070209 A 5322 D5347112420100 SHEAR TIE AIRBUS A321 A321211 3930370 EU FUSLEAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 169UW 1455 FR 69 - 70 AT Y1162.5 HAS CORROSION. REPLACED SHEAR TIE PER SRM 51-72-11; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 3 SQ INCHES. 2 L 7 2 4F RT A28NM 2007021300121 20070213 00121 NM 2007 2 13 USAA070090 1 20070209 A 5320 651768537 ANGLE BOEING 737 7374B7 1384702 NM BS 348 S15L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 BS 348 S-15L CRACKED. REPLACED WITH IDENTICAL PART PER BOEING DWG 64-17685-37, DEFECT SIZE: .250 INCH. 2 L 7 2 4F RT A16WE 2007021300123 20070213 00123 EA 2007 2 13 TRAX200700177 1 20070205 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 684BR 7708 WHEN ATTEMPTING TO EXTEND FLAPS TO 8 DEG, FAILED AT 0 DEG. EN ROUTE TO ERI A/C DIVERTED TO CLE DUE TO MTC. EMERGENCY D ECLARED. FLT 4266 CX & ON 02/0607 FLTS 4634, 4847 CX. 2 L 7 2 4F RT A21EA 2007021300126 20070213 00126 EA 2007 2 13 TRAX200700180 1 20070205 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF ADJUST A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 841AS 7300 PAX DOOR WILL NOT CLOSE PROPERLY, OUTER HANDLE INDICATES OUT WITH NORMAL PROCEDURES. FLT 4634 DEL 39 MINS. 2 L 7 2 4F RT A21EA 2007021300127 20070213 00127 EA 2007 2 13 TRAX200700181 1 20070131 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 CREW EMERGENCY EXIT EXTERIOR EMERGENCY EXIT PLACARD FADED. REMOVED AND REPLACED CREW EMERGENCY ESCAPE HATCH PLACARD IAW CRJ 700 AMM 11-00. NO OTHER DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2007021300132 20070213 00132 NM 2007 2 13 SWAA070677 1 20070208 A 3350 20121 CHARGER BOEING 737 7375H4 138449D NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED SERVICE CHECK, FOUND LT AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK AND BA TTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007021300133 20070213 00133 NM 2007 2 13 SWAA070680 1 20070208 A 5311 6517684 FRAME BOEING 737 7373T5 1384608 NM BS 303 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303.9, STR 16L. REPAIRED FRAME SECTION PER ER. 2 L 7 2 4F RT A16WE 2007021300134 20070213 00134 NM 2007 2 13 QXEA200700160 1 20070212 A 3010 4100S00502 VALVE BOMBDR DHC8 DHC8402 1390042 NM DEICE SYS MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 410QX 1220 4053 SEA FLIGHT NR 2484: DEICE PRESSURE CAUTION. AIRCRAFT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED NR 2 DDV IAW AMM 30-11-16 PAGES 401-406. OPS CHECK GOOD IAW AMM 30-11-00-720-801. SEALED PANEL 613AR. RII WAS C/W. AIRCRAFT WAS R ETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007021300143 20070213 00143 EA 2007 2 13 COMA0760151 1 20070204 A 3097 3530358 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE SYS FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 983CA 7169 FLIGHT 5204 - LEFT AND RIGHT ANTI-ICE DUCT MESSAGE ON TAKEOFF ROLL. LEFT AND RIGHT ANTI-ICE BLEED LOOPS SHORTED TO GROU ND. REPLACED RIGHT AFT BAY BLEED LOOP CONNECTOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007021300145 20070213 00145 WP 2007 2 13 IXXA07SMN045S 1 20070119 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER LEADING EDGE CORRODED AT STATION XFS304.000. REMOVED FASTENER S AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS . CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS AS NEEDED. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR P ARTS AND NEW FASTENERS FROM STATION XFS304.000 TO STATION XFS341.000 IAW DC8 SRM 57-2-1, FIG 44, TR NR 57-102 DATED 10/1 5/2003, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-0, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 57-2-1 FIG 2G, DC8 SRM 57 -2-1 FIG 44, DC8 SRM 57-3-1 PAGE 8, FIG 4 ITEM "A", DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 57-2-1, FIG. 44, DC8 SRM 5 2 L 7 4 4F RT 4A25 2007021300149 20070213 00149 EU 2007 2 13 07FDEA00457 1 20070213 A 5313 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 CORROSION ON MILLED STRINGER P56 RT/LT BETWEEN C76/77 AND ON OUTER SKIN BETWEEN C76/77, FOUND AFTER REMOVING TAIL BUMPER . REPAIR WAS PERFORMED IAW RAS/DATLS/0003476/2006 ISSUE: B AND EA 6-5318-103383. 2 L 7 2 4F RT A35EU 2007021300151 20070213 00151 EU 2007 2 13 07FDEA00460 1 20070213 A 5414 PANEL AIRBUS 300 A300B4622R 3930312 EU NR 2 NACELLE CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 FOUND CRACK AT PYLON NR 2 RT ON AREA AT LOWER SIDE PANEL AT RIB 18 INBOARD. REPAIR WAS PERFORMED IAW RAS 048245/005/200 6 ISSUE: A AND EA 6-5451-103394. 2 L 7 2 4F RT A35EU 2007021300153 20070213 00153 NM 2007 2 13 07FDEA00463 1 20070213 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 LEFT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), CLEVIS ASSEMBLY BORE FOUND CORRODED. REPAIRED AS PER FEDEX E.A.1-57 50-107786, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007021300154 20070213 00154 NM 2007 2 13 07FDEA00464 1 20070213 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 RIGHT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), CLEVIS ASSEMBLY BORE FOUND CORRODED. REPAIRED AS PER FEDEX E.A.1-5 750-107787, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007021300155 20070213 00155 WP 2007 2 13 IXXA07SMN036S 1 20070119 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 500 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER SKIN HAS A NON STANDARD REPAIR FROM STATION XW104.000 T O STATION XW110.000. REMOVED EXISTING SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN AS NEEDED. APPLIED SEALANT TO FAYING SURFACES. INSTALLED PLATING IAW DC8 SRM 57-7-1 FIG 1 PAGE 2, D C8 SRM 57-1-0 PAGE 1, DC8 SRM 57-7-1 FIG 1 PAGE 2 ITEM "D", DC8 SRM 51-1-8B, DC8 SRM 51-1-11 AND DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007021300156 20070213 00156 EA 2007 2 13 COMA0760156 1 20070205 A 2752 853D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS BINDING A COMA L ABORTED APPROACH J WARNING INDICATION DE DESCENT 1 SO 01 595SW 13002 7297 FLIGHT 5075 - FLAP FAIL MESSAGE ON DESCENT, DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. REMOVED AND REPLACED OUTBOARD FLAP INBOARD ACTUATOR. 2 L 7 2 4F RT A21EA 2007021300157 20070213 00157 NM 2007 2 13 MWEA070029 1 20070210 A 3350 LAMP BOEING 717 717200 1383700 NM EMERGENCY LIGHT INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 927ME 55193 TAIL CONE SLIDE EMERGENCY LIGHTS INOPERATIVE. REPLAMPED EMERGENCY LIGHT. 2 L 7 2 4F TR A6WE 2007021300162 20070213 00162 EA 2007 2 13 COMA0760155 1 20070205 A 2752 852D10021 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS BINDING A COMA L ABORTED APPROACH J WARNING INDICATION DE DESCENT 1 SO 01 595SW 2040 7297 FLIGHT 5075 - FLAP FAIL MESSAGE ON DESCENT, DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT INBOARD FLAP OUTBOARD ACTUATOR. 2 L 7 2 4F RT A21EA 2007021300163 20070213 00163 2007 2 13 MWEA070027 4 20070206 A 2565 D29982225 SLIDE BOEING 717 717200 1383700 NM PAX DOOR DETACHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 918ME 55180 DOOR SLIDE FORWARD ENTRY DOOR DISCONNECTED FROM HANGER. REINSTALLED FORWARD ENTRY DOOR SLIDE. 2 L 7 2 4F TR A6WE 2007021300167 20070213 00167 NM 2007 2 13 CALA0700062 1 20070211 A 5315 654680977 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 947 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 INSPECTION FOUND FLOORBEAM CORRODED AT STA 947, RBL 6 TO LBL 6. A FLOORBEAM REPAIR WAS INSTALLED IAW SRM 53-00-51, FIGU RE 201. 2 L 7 2 4F RT A16WE 2007021300168 20070213 00168 NM 2007 2 13 CALA0700063 1 20070209 A 2421 761574B IDG BOEING 737 737824 13844BZ NM NR 2 ENGINE LEAKING A CALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 14237 20040 28802 LIGHT SMOKE ENTERED THE CABIN AND COCKPIT AFTER TAKEOFF FROM CLE. THE AIRCRAFT WAS RETURNED TO CLE. THE SMOKE DISSIPAT ED BY THE TIME THE AIRCRAFT RETURNED TO CLE. MAINTENANCE FOUND THE NR 2 IDG DRIVE SHAFT LEAKING AND IDG EMPTY. THE NR 2 IDG AND IDG OIL COOLER WAS REPLACED IAW MM 24-11-11-400-400-801. 2 L 7 2 4F RT A16WE 2007021300169 20070213 00169 WP 2007 2 13 IXXA07SMN058S 1 20070131 A 5244 SKIN DOUG DC8 DC871F 302199D WP ACCESSORY DOOR CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 46065 DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD ACCESSORY COMPARTMENT DOOR SKIN CRACKED. REMOVED DAMAGED SKIN. FABRIC ATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN. INSTALLED NEW SKIN IAW DC8 SRM 52-8-1 FIG 1 SHEET 1, DC8 SRM 52-1-0 PAGE 1, DC8 SRM 52-8-1 FIG 1 SHEET 1 ITEM "E", DC8 SRM 51-9-0 FIG 68A, DC8 SRM 51-1-8B AND DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007021300171 20070213 00171 EA 2007 2 13 COMA0760158 1 20070205 A 2750 1104SD100201 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS BENT A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 436CA 7482 FLIGHT 5294 - FLAP FAIL ON DESCENT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED RIGHT WING NR 2 FLEX DRIVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007021300175 20070213 00175 NM 2007 2 13 UPS07449154 1 20070103 A 5753 PANEL BOEING 747 747123 1384873 NM TE FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LEFT WING INBOARD T/E MID FLAP LWR AFT INBOARD PANEL SEVERAL LOCATION FOUND DELAMINATED. FIBERGLASS R EPAIRED AS PER BOEING MESSAGE 1-2716766520-2 AND RS R57-55-35719 AND UPS ENGINEERING FILE 747-57-20133. 2 L 7 4 4F A20WE 2007021300178 20070213 00178 NM 2007 2 13 AWXA200700193 1 20070208 A 5753 SKIN BOEING 737 73733A 1384673 NM TE FLAP DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 PHX - RIGHT WING OUTBOARD AFT FLAP, INBOARD END WEDGE IS DISBONDED, WBL 204.40. REPLACED RIGHT WING OUTBOARD AFT FLAP I AW AWA TASK CARD R3M27034. 2 L 7 2 4F RT A16WE 2007021300180 20070213 00180 NM 2007 2 13 AWXA200700195 1 20070122 A 5313 654577128 STRINGER BOEING 737 73733A 1384673 NM BS 500C S16R CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED STRINGER, BS 500C + 15", S16R. REPAIRED STRINGER, BS 500C + 15", S16R IAW AWA ER 03-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2007021300181 20070213 00181 NM 2007 2 13 AWXA200700196 1 20070202 A 5321 D5367180500400 FLOORBOARD AIRBUS A319 A319132 3930340 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 831AW 1576 SAL - FOUND CORROSION ON MAIN CABIN FLOORBOARD, 261 FF, FR 66 - FR 68, +Y1292. REPLACED MAIN CABIN FLOORBOARD, 261 FF, FR 66 - FR 68, +Y1292 IAW A319 SRM 53-12-12. 2 L 7 2 4F RT A28NM 2007021300182 20070213 00182 NM 2007 2 13 UPS07449155 1 20070103 A 5753 PANEL BOEING 747 747123 1384873 NM TE FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LEFT WING INBOARD T/E MID FLAP INBOARD FWD PANEL SEVERAL LOCATION FOUND DELAMINATED. FIBERGLASS REPAI RED AS PER BOEING MESSAGE 1-2716766520-2 AND RS R57-55-35719 AND UPS ENGINEERING FILE 747-57-20133. 2 L 7 4 4F A20WE 2007021300183 20070213 00183 WP 2007 2 13 UPS07849135 1 20070207 A 3350 BATTERY DOUG DC8 DC871F 302199D WP EMERGENCY EXIT NO TEST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:N/A ON PREFLIGHT A/C FAILED EMERGENCY EXIT LIGHT PREFLIGHT TEST. REPLACED EMERGENCY LIGHTING BATTERY AN D RELAY UNIT IAW DC-8 AMM 33-50-01-2. OPS TEST GOOD. 2 L 7 4 4F RT 4A25 2007021300184 20070213 00184 WP 2007 2 13 UPS07849137 1 20070207 A 3350 LAMP DOUG DC8 DC873F 302199F WP EMERGENCY EXIT BURNED OUT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:N/A EMERGENCY EXIT DISARM LIGHT BURNED OUT. EMERGENCY EXIT DISARM LIGHT RELAMPED IAW DC8 AMM 33-50-02-2 . 2 L 7 4 4F RT 4A25 2007021300186 20070213 00186 WP 2007 2 13 UPS07849158 1 20070208 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY BATTERY PACK IAW 33-50-01-2. 2 L 7 4 4F RT 4A25 2007021300187 20070213 00187 NM 2007 2 13 UPS07M49156 1 20070208 A 3350 UNKNOWN DOUG MD11 MD11F 3023600 NM EMERGENCY LIGHTS UNKNOWN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 285UP 48457 INSPECTION TYPE:N/A EMERGENCY LIGHT BATTERY LOW ALERT DISPLAYED. EMERGENCY LIGHTING SYSTEM DEFERRED PER MEL 33-50-4, PL ACARD INSTALLED M343837. 2 L 7 3 4F RT A22WE 2007021300188 20070213 00188 WP 2007 2 13 NWAA070539762 1 20070207 A 3040 CONTROLLER DOUG DC9 DC941 302207N WP WINDSHIELD HEAT FAILED A NWAA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 GL 01 762NW 47395 DURING GROUND TIME, THE CAPTAINS WINDSHIELD HEAT MALFUNCTIONED WINDSHIELD SHATTERED THE WINDSHIELD AND IGNITED THE TRIM/ SEALANT AT THE BASE OF THE WINDSHIELD. THE FIRST OFFICER PUT OUT THE FIRE WITH THE PORTABLE FIRE EXTINGUISHER (SEE LP N R 3979492). NO PASSENGERS WERE ONBOARD AT THE TIME. THE FLIGHT WAS CANCELLED. MAINTENANCE HAS REPLACED ALL APPLICABLE COMPONENTS AND WINDSHIELD AND THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007021300192 20070213 00192 2007 2 13 DXTA200701927 4 20070209 A 2210 COMPUTER RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP AFCS MALFUNCTIONED E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 838QS 258338 AUTO PILOT PITCHED OVER FROM LEVEL FLIGHT AT FL360 AND MACH .78 OR 260 KTS IND. WE LOST 450 FT UPON THE VIOLENT PITCHIN G MOMENT AND VERY ABRUPT TAIL FLUTTER. THIS HAPPENED ON THE L-AFCS, FLIGHT DIRECTOR VERY ERRATIC IN ALL MODES AFTER PITC HING MOMENT. REPLACED FLAP COMPENSATOR TRANSMITTER (POTENTIOMETER) PERFORMED CALIBRATION CHECK PER HAWKER 800 XP M/M 34-22-60-501 AND OP'S CHECKED IAW HAWKER SERIES COMMUNIQUE NR 22-07. NO OTHER FAULTS NOTED AT THIS TIME. 2 L 7 2 4F 4 F RT A3EU E6WE 2007021300193 20070213 00193 CE 2007 2 13 DXTA200701928 1 20070209 A 7810 EXHAUST DUCT CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE RT ENGINE FIRE E DXTA E ENGINE SHUTDOWN A J FLAME/FIRE WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 839QS 5600690 DURING A RT ENG START A TAILPIPE FIRE INDICATED. DURING ENG START, NOTED ITT SPIKED TO NEARLY 300 DEGREES RIGHT AS THRO TTLE WAS MOVED OUT OF CUTOFF. MOVED THROTTLE TO CUTOFF & CONTINUED TO MOTOR. INSPECTED RT ENG EXHAUST & AFT END OF ENG, WTIH NO DEFECT NOTED. PERFORMED A VISUAL INSPECTION OF THE HORIZONTAL STABS, RT LE, NO DEFECTS NOTED. COMPLIED WITH ANOT HER START OF RT ENG WITHOUT INCIDENT. ALLOWED ENG TO IDLE FOR 10 MINS & NOTED ITT NEVER SURPASSED 500 DEGREES, ALL OTHER ENG PARAMETERES REMAINED NORMAL, COMPLIED WITH A NORMAL SHUTDOWN WITHOUT INCIDENT. COMPLIED WITH ANOTHER ENG START & SH UTDOWN WITH OUT INCIDENT. ENG INDICATIONS REMAINED NORMAL. MX PERFORMED REFERENCING CITATION 560 ENCORE AMM 71-00-00. 2 L 7 2 4F 4 F RT A22CE E00053EN 2007021300194 20070213 00194 CE 2007 2 13 DJFA2007017 1 20070207 A 5511 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 790TA RK252 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE RT IB HORIZONTAL STA BILIZER, THE RT RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. SDR WILL BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION. 2 H 7 2 4F 4 F RT A16SW E25EA 2007021300200 20070213 00200 NM 2007 2 13 HNAA0700028 1 20070211 A 5347 85320019 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 201-222 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838EX 29736 29736 220 SEAT TRACK RIGHT HAND CENTER FROM X201.15 TO X222.00 IS CORRODED. REPLACED SEAT TRACK. 2 H 7 2 4T RT A13NM 2007021400002 20070214 00002 EA 2007 2 14 QXEA200700055 1 20070113 A 5330 RIVET CNDAIR CL600 CL6002C10 1390015 EA BS 469 BURNED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - REPLACE BURNED RIVET LOCATED 10" AFT OF FS 469.6 6" BELOW WL 79.5 RTS. REPAIRED IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007021400003 20070214 00003 EA 2007 2 14 QXEA200700057 1 20070116 A 5310 DOOR FRAME CNDAIR CL600 CL6002C10 1390015 EA BS 292 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - REPLACE BURNED RIVET LOCATED AT FS 292.2 12" BELOW TOP OF MAIN CABIN DOOR FRAME. REPAIRED IAW SRM 51-42-06 AND 53-21-01. 2 L 7 2 4F RT A21EA 2007021400006 20070214 00006 EA 2007 2 14 QXEA200700060 1 20070113 A 5330 RIVET CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - REPLACE BURNED RIVET AT FS 417.3 11" BELOW WL 79.5, RHS. REPAIRED IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007021400007 20070214 00007 EA 2007 2 14 QXEA200700052 1 20070119 A 5330 SILL CNDAIR CL600 CL6002C10 1390015 EA CARGO DOORWAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - LIGHT CHAFFING ON AFT CARGO DOOR FORWARD UPPER AND LOWER SILL AREAS ON AIRCRAFT WITH SEVERAL LOCATIONS OF MINOR NICKS, SCRATCHES, AND MISSING PAINT FOUND AROUND SILL. REPAIRED IAW SRM 53-00-01, 53-61-23, AND REO670-53-61-308. 2 L 7 2 4F RT A21EA 2007021400008 20070214 00008 EA 2007 2 14 QXEA200700053 1 20070116 A 5751 SKIN CNDAIR CL600 CL6002C10 1390015 EA AILERONS CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - LOWER LEADING EDGE SKIN OF RIGHT AILERON IS CHAFED ALONG ENTIRE LENGTH BY THE WING TRAIL EDGE PANELS. REPAIRED IAW SRM 51-42-06 AND 51-42-21. 2 L 7 2 4F RT A21EA 2007021400009 20070214 00009 EA 2007 2 14 QXEA200700062 1 20070117 A 5321 FLOOR PANEL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FLIGHT COMPARTMENT FLOOR PANEL 221ALF, AFT SUPPORT, APPEARS CRACKED AT 2 PLACES. VIEWED FROM FORWARD SIDE, ADJ ACENT TO CABIN SEAT TRACK. REPAIRED IAW SRM 51-42-00, 51-40-11. 2 L 7 2 4F RT A21EA 2007021400012 20070214 00012 NM 2007 2 14 ABXA070042 1 20070210 A 3250 161T11452 PIN BOEING 767 767281 1385109 NM LT BOGIE PIVOT DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 795AX 6472 23145 DURING COMPLIANCE WITH AD 2006-07-14, AMENDMENT 39-14541, ABX JOB CARD JEA32100002-001, THE LEFT MAIN LANDING GEAR BOGIE PIVOT PIN WAS FOUND TO HAVE BRONZE TRANSFER. REMOVED AND REPLACED LEFT MAIN LANDING GEAR BOGIE PIVOT PIN IAW B767 MM. 2 L 7 2 4F RT A1NM 2007021400015 20070214 00015 SO 2007 2 14 RAIA00702011 1 20070207 A 3397 WIRE EMB 145 EMB145 3260210 SO EMERGENCY LIGHT DAMAGED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 803HK 145077 PRE FLT NR 3554 - RIC - EMERGENCY FLOOR LIGHT STRIP INOP. MAINTENANCE REPAIRED EMERGENCY LIGHT AT ROW 12 BY SOLDERING W IRES TO STRIP. 2 L 7 2 4F RT T00011AT 2007021400016 20070214 00016 SO 2007 2 14 RAIA0702013 1 20070207 A 3350 RPS1B BATTERY EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT DISCHARGED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 808HK 145157 PRE FLT NR 5501 - STL - EMERGENCY LIGHT AT MAIN DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE NR 1 BATTERY POWER SUPP LY. 2 L 7 2 4F RT T00011AT 2007021400017 20070214 00017 SO 2007 2 14 RAIA00702009 1 20070207 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 813HK 145044 PRE FLT 5467 - STL - EMERGENCY LIGHT AT MAIN DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BULB. 2 L 7 2 4T RT T00011AT 2007021400019 20070214 00019 2007 2 14 RAIA00702015 4 20070211 A 2310 RADIO EMB 145 EMB145LR 3260212 SO NR 1 INOPERATIVE A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 823HK 145475 FLT NR 7986 - BTV - NR 1 COMM UNIT WILL NOT HOLD FREQUENCY AND CAN NOT CHANGE NR 2 FREQUENCY. MAINTENANCE REMOVED AND R EINSTALLED THE NR 1 COMMUNICATION UNIT. 2 L 7 2 4T RT T00011AT 2007021400021 20070214 00021 WP 2007 2 14 IXXA07SMN066S 1 20070131 A 5753 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT UPPER OUTBOARD FLAP HAS A NON STANDARD REPAIR AT STATION XF350.000. REMO VED EXISTING SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN. CLEANED TREATED AND PRIMED AREA AND NEW SKIN AS NEEDE D. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN IAW DC8 SRM 57-7-1 FIG 4 PAGE 2 TR NR 57-94 DATE 10-01-2002, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-7-1 FIG 4 PAGE 2 ITEM "B", DC8 SRM 51-1-8B, DC8 SRM 51-1-11 AND DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007021400022 20070214 00022 EA 2007 2 14 QXEA200700065 1 20070116 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSLEAGE LIGHTNING STRIKE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD JUST BELOW ADG DOOR AT FS 170. REPAIRED IAW SRM 51-42-06, 51-25-01, AND 51-40-00. 2 L 7 2 4F RT A21EA 2007021400024 20070214 00024 EA 2007 2 14 QXEA200700069 1 20070117 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE LIGHTNING STRIKE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON LEFT SIDE OF FUSELAGE AT FS 288 AND STRINGER 26L. REPAIRED IAW S RM 53-21-01, 51-21-06, AND 51-25-16. 2 L 7 2 4F RT A21EA 2007021400025 20070214 00025 EA 2007 2 14 QXEA200700070 1 20070116 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE LIGHTNING STRIKE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 407 AND STRINGER 20R. REPAIRED IAW SRM 51-2-06, 51-25-01. 2 L 7 2 4F RT A21EA 2007021400026 20070214 00026 EA 2007 2 14 QXEA200700071 1 20070115 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE LIGHTNING STRIKE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD JUST LEFT OF LOWER RED ANTI COLLISION LIGHT AT FS 486. REPAIRED IAW SRM 53-00-01, AND 51-21-11, 51-25-01. 2 L 7 2 4F RT A21EA 2007021400030 20070214 00030 2007 2 14 BAQA200700003 2 20070111 A 7250 TURBINE WHEEL TMECA ARRIEL2C AEROSP AS365 AS365N2 8680815 EU ENGINE DAMAGED E BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 520CF 24003 6537 DURING MAINTENANCE GROUND RUNS, STARTED NR 1 ENGINE AND NR 2 ENGINES TO PERFORM REQUIRED MAINTENANCE CHECKS AFTER INSPEC TION OF AIRCRAFT AND ENGINES. SHUTDOWN ENGINES TO MAKE TAILROTOR BLADE WEIGHT CHANGE. ATTEMPTED TO START NR 1 ENGINE AND IT WOULD NOT TURN. ATTEMPTED TO MANUALLY ROTATE COMPRESSOR AND COULD NOT. REMOVED STARTER/GENERATOR AND ATTEMPTED TO TURN COMPRESSOR. STILL WOULD NOT TURN. AFTER ENGINE COOLED DOWN, WAS ABLE TO TURN COMPRESSOR BY HAND AND HEARD TURBINE RUB. HP TURBINE DISK IS RUBBING. CHANGING MODULE 2 AND 3 OF AFFECTED ENGINE. PILOT REPORTED NO ABNORMITIES DURING FIR ST RUN OF NR 1 ENGINE. 1 G 7 2 3U RT H10EU 2007021400031 20070214 00031 WP 2007 2 14 IXXA07SMN071S 1 20070131 A 5310 1616757 LONGERON DOUG DC8 DC871F 302199D WP ZONE 200 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND A CRACKED LONGERON AT STATION 1776.000 LONGERON 17 RIGHT. REMOVED DAMAGED LONG ERON. FABRICATED NEW LONGERON. CLEANED, TREATED AND PRIMED AREA AND NEW LONGERON. INSTALLED NEW LONGERON IAW DC8 SRM 53-5-1 FIG 7 SHEET 1 PAGE 22, DC8 SRM 53-1-0 PAGE 1, DC8 SRM 51-1-8B, DC8 SRM 51-2-0 FIG 50, DC8 SRM 51-1-21, DC8 SRM 51 -1-20D AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007021400035 20070214 00035 NM 2007 2 14 PIDA07006 1 20070202 A 5340 STRINGER CLIP BOEING 737 7372K5 138448X NM BS 727B CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 STRINGER TIE CLIP CRACKED AT BS 727B AT STR 4LT. REPLACED TIE CLIP. 2 L 7 2 4F RT A16WE 2007021400036 20070214 00036 NM 2007 2 14 PIDA07007 1 20070202 A 5340 STRINGER CLIP BOEING 737 7372K5 138448X NM BS 747 CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 STRINGER TIE CLIP CRACKED AT BS 747 AT STR 7LT. REPLACED TIE CLIP. 2 L 7 2 4F RT A16WE 2007021400037 20070214 00037 WP 2007 2 14 ASAA0781444 1 20070205 A 2410 696233B CSD DOUG DC9 DC983 3022083 WP LT ENGINE OVERTEMP A ASAA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 02 977AS 37340 1984 53453 LEFTHAND ENGINE CSD TEMPERATURE IN RED DURING CLIMB FROM ANC. SHUTDOWN CSD AND DIVERTED TO FAI. REPLACED CSD. 2 L 7 2 4F RT A6WE 2007021400039 20070214 00039 NM 2007 2 14 NOCA01507 1 20070119 A 3350 LAMP BOEING 767 767306 1385148 NM EMERGENCY LIGHT INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 760NA 29898 EXTERIOR EMERGENCY LIGHT AT DOOR 3R INOP. RELAMPED R3 DOOR LIGHT AS PER MM 33-51-06. 2 L 7 2 4F RT A1NM 2007021400044 20070214 00044 NM 2007 2 14 SWAA070681 1 20070208 A 5311 6545856 FRAME BOEING 737 7373T5 1384608 NM BS 992 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 992, RBL 50, WL 209. REPAIRED FRAME SECTION PER ER. 2 L 7 2 4F RT A16WE 2007021400045 20070214 00045 NM 2007 2 14 SWAA070667 1 20070208 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 S18R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 18R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007021400047 20070214 00047 NM 2007 2 14 SWAA070683 1 20070208 A 5311 6546568 FRAME BOEING 737 7373T5 1384608 NM BS 1016 S6R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD FRAME CRACKED AT BS 1016, STR 6R. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2007021400048 20070214 00048 NM 2007 2 14 SWAA070682 1 20070208 A 5322 6546569 SHEAR TIE BOEING 737 7373T5 1384608 NM BS 986 S19R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986.5, STR 19R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007021400049 20070214 00049 2007 2 14 SWAA070670 4 20070208 A 2565 6557463 GIRT BAR BOEING 737 7373H4 1384600 NM R2 DOOR SLIDE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 633SW 27936 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CRACKED. REMOVED AND REPLACED AFT G IRT BAR FITTING PER MM. 2 L 7 2 4F RT A16WE 2007021400050 20070214 00050 NM 2007 2 14 SWAA070669 1 20070208 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 420-513A CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND STRINGER 27L CORRODED AT BS 420 TO BS 513A. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007021400051 20070214 00051 2007 2 14 SWAA070666 4 20070208 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM L1 DOOR DISLODGED A SWAA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 SW 29 663SW 23256 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007021400052 20070214 00052 NM 2007 2 14 SWAA070675 1 20070208 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 736SA 27868 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2007021400053 20070214 00053 NM 2007 2 14 SWAA070672 1 20070208 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 736SA 27868 DURING SCHEDULED HC1 CHECK, LT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007021400056 20070214 00056 NM 2007 2 14 SWAA070676 1 20070208 A 3350 PH22300L STRIP BOEING 737 7373L9 1384470 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 5 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007021400062 20070214 00062 NM 2007 2 14 HNAA0700004 1 20070119 A 5320 85300016115 ANGLE DHAV DHC8 DHC8102 2809003 NM FUSLEAGE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838EX 29736 29736 220 CRACKS FOUND ON CLOSING ANGLE BETWEEN STR 5S AND 6S. REPLACED ANGLE. 2 H 7 2 4T RT A13NM 2007021400067 20070214 00067 NM 2007 2 14 HNAA0700030 1 20070211 A 5347 85310926 ANGLE DHAV DHC8 DHC8102 2809003 NM BS 136 CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838EX 29736 29736 220 CRACK FOUND ON ANGLE AT X136.80 AND STR 14P. REPLACED ANGLE. 2 H 7 2 4T RT A13NM 2007021400068 20070214 00068 NM 2007 2 14 HNAA0700017 1 20070211 A 5347 85320490 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838EX 29736 29736 220 RIGHT HAND INBOARD SEAT RAIL HAS CORROSION AT PAX SEAT LEG LOCATIONS. REPLACED RAIL. 2 H 7 2 4T RT A13NM 2007021400070 20070214 00070 NM 2007 2 14 HNAA0700021 1 20070211 A 5347 85320019 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838EX 29736 29736 220 LEFT HAND INBOARD SEAT RAIL HAS CORROSION AT SEAT LEG LOCATIONS. REPLACED SEAT RAIL. 2 H 7 2 4T RT A13NM 2007021400071 20070214 00071 NM 2007 2 14 HNAA0700022 1 20070211 A 5347 85330469001 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838EX 29736 29736 29736 RIGHT HAND INBOARD AFT SEAT RAIL HAS CORROSION AT SEAT LEG LOCATIONS. REPLACED SEAT RAIL. 2 H 7 2 4T RT A13NM 2007021400073 20070214 00073 NM 2007 2 14 HNAA0700018 1 20070211 A 5347 85330164117 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838EX 29736 29736 220 RIGHT HAND INBOARD MIDDLE SEAT RAIL HAS CORROSION AT SEAT LEG LOCATIONS. REPLACED SEAT RAIL. 2 H 7 2 4T RT A13NM 2007021400074 20070214 00074 EU 2007 2 14 UG8A2007PA002 1 20070206 A 5753 SKIN HAWKER BAE125 BAE125700B 7450007 EU GARRTT TFE731 TFE731* 01518 WP TE FLAPS CORRODED E UG8A K NONE O OTHER IN INSP/MAINT 1 GL 23 241FB 10724 257129 LT FLAP IB TOP SKIN HAS A SPOT OF CORROSION. PERFORMED FIELD REPAIR IAW MFG AIRCRAFT COMPANY DRAWING NR FR-HK-03161 REV . 2 DATED 2-8-07 APPROVED BY FAA DERY 635772-CE AND DERY-230161-CE ON FAA FORM 8110-3 DATED FEB 7, 2007. SUBMITTED REQU EST FOR ENGINEERING DISPOSITION TO MFG ON JAN 31/07 AND FEB 1/07. 2 L 7 2 4F 4 F RT A3EU E6WE 2007021400075 20070214 00075 NM 2007 2 14 HNAA0700029 1 20070211 A 5347 85320019 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 240-291 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838EX 29736 29736 220 SEAT TRACK RIGHT HAND CENTER FROM X240.50 TO 291.40 HAS AREAS OF CORROSION. REPLACED SEAT TRACK. 2 H 7 2 4T RT A13NM 2007021400076 20070214 00076 NM 2007 2 14 HNAA0700031 1 20070201 A 5320 85310310103 STIFFENER DHAV DHC8 DHC8102 2809003 NM BS 182 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838EX 29736 29736 220 CORROSION ON FRAME X182.00 ON HORIZONTAL BEAM ADJACENT TO SEAT TRACK ON THE RIGHT SIDE. REPLACED HORIZONTAL STIFFENER. 2 H 7 2 4T RT A13NM 2007021400084 20070214 00084 NM 2007 2 14 MWEA070028 1 20070209 A 3213 STRUT BOEING 717 717200 1383700 NM NLG FROZEN A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 916ME 55178 GEAR UNSAFE LIGHT CAME ON. REPLACED NOSE LANDING GEAR SEALS AND FLUID. 2 L 7 2 4F TR A6WE 2007021400085 20070214 00085 EA 2007 2 14 A6WA200740014 1 20070110 A 5315 601R3111357 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 412AW 7582 FOUND LEFT FS 280 FLOOR SUPPORT CLIP, P/N 601R31113-57 CRACKED APPROX .1 INCH LONG OUTBOARD SIDE LBL 9.0. REMOVED CRACK ED ANGLE. FITTED AND INSTALLED NEW ANGLE P/N 601R31113-57 IAW CRJ SRM 51-42-06, 51-42-13-51-40-11, 51-42-21 AND BSC STA NDARD REPAIR 601R-53-0057A. (M) 2 L 7 2 4F RT A21EA 2007021400086 20070214 00086 NM 2007 2 14 07FDEA00366 1 20070207 A 5713 ARB75122 STRINGER DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48421 CRACK FOUND AT STRINGER END 12R (XORS 642), APPROX 13 INCHES LENGTH ON RIGHT HAND WING TANK DURING HFEC INSPECTION. CRA CK ON RIGHT HAND WING (XORS 642) AT STRINGER END 12R REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007021400087 20070214 00087 EA 2007 2 14 TRAX200700153 1 20070202 A 5260 STEP CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 ASD LOWER STEP CRACKED. ASD LOWER STEP REMOVED & REPLACED IAW CRJ 700 AMM 52-10-00. 2 L 7 2 4F RT A21EA 2007021400088 20070214 00088 EA 2007 2 14 COMA0770014 1 20070205 A 5310 CC670341757 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 368CA 11048 10075 FLOOR SUPPORT CROSSBEAM IS CRACKED. REPAIRED CROSSBEAM I/A/W REO 670-53-11-047. 2 L 7 2 4F RT A21EA 2007021400089 20070214 00089 NM 2007 2 14 SWAA070725 1 20070210 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007021400090 20070214 00090 NM 2007 2 14 SWAA070741 1 20070212 A 5312 6546568 FRAME BOEING 737 7373H4 1384600 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED OTS CHECK, FOUND BULKHEAD FRAME CORRODED AT BS 1016, BL 0. REPAIRED BULKHEAD FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007021400091 20070214 00091 NM 2007 2 14 SWAA070738 1 20070212 A 5230 6547952 SKIN BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT OUTER DOOR HANDLE CUTOUT. REPAIRED CARGO DOOR PER SWA E A. 2 L 7 2 4F RT A16WE 2007021400092 20070214 00092 NM 2007 2 14 SWAA070712 1 20070210 A 5330 6550570 BEAR STRAP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT L2 DOOR CUTOUT LOWER FWD CORNER. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007021400093 20070214 00093 2007 2 14 SWAA070720 4 20070210 A 2565 6557463 GIRT BAR BOEING 737 7373H4 1384600 NM L1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007021400094 20070214 00094 2007 2 14 SWAA070719 4 20070210 A 2565 6557463 GIRT BAR BOEING 737 7373H4 1384600 NM L1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007021400095 20070214 00095 NM 2007 2 14 SWAA070744 1 20070212 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 727A S6L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021400096 20070214 00096 NM 2007 2 14 SWAA070743 1 20070212 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 616 S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021300112 20070213 00112 NM 2007 2 13 UPS07449153 1 20070103 A 5730 PANEL BOEING 747 747123 1384873 NM LT WING DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C LEFT WING INBOARD TRAILING EDGE MID FLAP LWR OUTBOARD AFT PANEL SEVERAL LOCATION FOUND DELAMINATED. F IBERGLASS REPAIRED AS PER BOEING MESSAGE 1-2716766520-2 AND RS R57-55-35719 AND UPS ENGINEERING FILE 747-57-20133. 2 L 7 4 4F A20WE 2007021300125 20070213 00125 EA 2007 2 13 TRAX200700179 1 20070205 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 900EV 7608 FLAP FAIL AT ZERO ON APPROACH. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007021300152 20070213 00152 NM 2007 2 13 07FDEA00462 1 20070213 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 624FE 48443 LEFT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), CLEVIS ASSEMBLY BORE FOUND CORRODED. REPAIRED AS PER FEDEX E.A.1-5 750-107785, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007021300158 20070213 00158 EA 2007 2 13 COMA0760153 1 20070204 A 5610 601R3303321 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA O OTHER O OTHER NR NOT REPORTED 1 SO 01 779CA 12842 7306 FLIGHT 5297 - CAPTAIN'S WINDSHIELD CRACKED. REPLACED WINDSHIELD. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007021300172 20070213 00172 NE 2007 2 13 AMTA200700045 2 20070131 A 7261 MO6524 MODULE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE NR 1 ENGINE UNSERVICEABLE A AMTA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 11 164AT 55570 55570 1238 14820 ON CLIMBOUT NR 1 ENGINE QTY STARTED DECREASING, OIL QTY WENT TO ZERO, OTHER INDICATIONS NORMAL AT LEVEL OFF OIL PRESSURE STARTED FLUCTUATINGS OIL PRESSURE STARTED DECREASING. SHUTDOWN ENG IAW AOM REPLACED HIGH SPEED GEAR BOX (06 MODULE). OPS CHECK NORMAL. ENG OIL QTY CHECK NORMAL. (K) 2 L 7 3 4F 4 F A23WE E12EU 2007021300190 20070213 00190 NM 2007 2 13 AMTA200700054 1 20070202 A 3020 PROBE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE UNKNOWN A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 560TZ 33525 EICAS MSG LT ENG PROBE HEAT DISPLAYED. PERFORMED FIM 30-40-00 FIG 103, MSG CLEARED. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007021300191 20070213 00191 NM 2007 2 13 SWAA070668 1 20070208 A 5310 6517685 DOOR FRAME BOEING 737 7373Q8 1384670 NM BS 348 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR FRAME WEB CRACKED AT BS 348, STR 16L. REPAIRED FRAME WEB PER EA. 2 L 7 2 4F RT A16WE 2007021300195 20070213 00195 NM 2007 2 13 HNAA0700002 1 20070125 A 5320 85300317 ANGLE DHAV DHC8 DHC8102 2809003 NM FUSLEAGE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838 29736 29736 220 CRACK FOUND ON RIGHT HAND CLOSING ANGLE ON FASTENERS AT VERTICAL FLANGE BETWEEN STR 4S AND 5S. REPLACED CLOSING ANGLE. 2 H 7 2 4T RT A13NM 2007021400005 20070214 00005 EA 2007 2 14 QXEA200700059 1 20070113 A 5330 RIVET CNDAIR CL600 CL6002C10 1390015 EA FUSLEAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - REPLACE BURNED RIVET AT FS 412.8 12" BELOW WL 79.5 RHS. REPAIRED IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007021400011 20070214 00011 WP 2007 2 14 ABXA070041 1 20070209 A 2740 591096231 JACKSCREW DOUG DC9 DC932F 3022067 WP HORIZONTAL STAB OBSTRUCTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 905AX 4579 47147 HORIZONTAL STABILIZER JACKSCREW FOUND TO BE HITTING MECHANICAL STOPS DURING OPERATION. REMOVED AND REPLACED JACKSCREW I AW DC9 MM, REF WORK ORDER 600265725. 2 L 7 2 4F A6WE 2007021400029 20070214 00029 EA 2007 2 14 QXEA200700066 1 20070115 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE LIGHTNING STRIKE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FORWARD FUSELAGE AT FS 243 AND STRINGER 22R. REPAI RED IAW SRM 51-42-06, 51-40-00, AND 51-25-01. 2 L 7 2 4F RT A21EA 2007021400033 20070214 00033 NM 2007 2 14 PIDA07003 1 20070131 A 5340 STRINGER CLIP BOEING 737 7372K5 138448X NM BS 420 CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 STRINGER TIE CLIP CRACKED AT BS 420 AT STR 5LT. REPLACED TIE CLIP. 2 L 7 2 4F RT A16WE 2007021400041 20070214 00041 EA 2007 2 14 PNSA070107 2 20070203 A 8500 ENGINE PIPER PA32 PA32301 7103207 SO LYC O540 IO540* 41532 EA MAKING METAL E PNSA K NONE O OTHER IN INSP/MAINT 1 AL 03 8305H 328106017 L1906148A DURING ROUTINE INSPECTION FOUND METAL IN FILTER. SUSPECT METAL FROM CAM AND LIFTERS. LYCOMING RECOMMENDED ENGINE BE RE MOVED AND SENT TO FACTORY FOR WARRANTY. ENGINE OVERHAULED BY LYCOMING 3/10/06. TSO 384.3 1 L 7 1 3O 3 O A3SO 1E4 2007021400059 20070214 00059 NM 2007 2 14 HNAA0700005 1 20070119 A 5320 85310310103 STIFFENER DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838EX 29736 29736 220 HORIZONTAL STIFFENER CORRODED WHERE RIGHT SEAT RAIL ATTACHES. REPLACED STIFFENER. 2 H 7 2 4T RT A13NM 2007021400065 20070214 00065 NM 2007 2 14 HNAA0700024 1 20070211 A 5315 85311097103 FLOORBEAM DHAV DHC8 DHC8102 2809003 NM BS 182 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838EX 29736 29736 220 FORWARD CENTER FLOORBOARD SUPPORT AT FRAME X182.00 IS CORRODED. REPLACED SUPPORT. 2 H 7 2 4T RT A13NM 2007021400066 20070214 00066 NM 2007 2 14 HNAA0700026 1 20070211 A 5330 85330022011 SKIN PANEL DHAV DHC8 DHC8102 2809003 NM BS 424-488 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838EX 29736 29736 220 STRINGER 30 IS DISBONDED DUE TO CORROSION FROM X424.124 TO X488.50. REPLACED SKIN PANEL FROM X424 TO 488 AND FROM STR 2 9R TO 29S. 2 H 7 2 4T RT A13NM 2007021400069 20070214 00069 NM 2007 2 14 HNAA0700020 1 20070211 A 5347 8533028 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838EX 29736 29736 220 LEFT HAND INBOARD MIDDLE SEAT RAIL HAS CORROSION AT SEAT LEG LOCATIONS. 2 H 7 2 4T RT A13NM 2007021400080 20070214 00080 NM 2007 2 14 HNAA0700025 1 20070211 A 5347 85320689105 SUPPORT FITTING DHAV DHC8 DHC8102 2809003 NM THRESHOLD CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838EX 29736 29736 220 FLOOR PANEL SUPPORT AT PAX DOOR THRESHOLD IS CORRODED. 2 H 7 2 4T RT A13NM 2007021400097 20070214 00097 NM 2007 2 14 SWAA070742 1 20070212 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 747 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021400098 20070214 00098 NM 2007 2 14 SWAA070748 1 20070212 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 907 S3R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021400099 20070214 00099 NM 2007 2 14 SWAA070746 1 20070212 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 747 S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021400100 20070214 00100 NM 2007 2 14 SWAA070745 1 20070212 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 727E S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021400101 20070214 00101 NM 2007 2 14 SWAA070747 1 20070212 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 500A S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 9L. REMOVED AND REPLACD STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021400102 20070214 00102 WP 2007 2 14 AALA20070189 1 20070126 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 415AA 49326 LGA - EMERGENCY LIGHTS AT FORWARD FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007021400103 20070214 00103 WP 2007 2 14 AALA20070190 1 20070126 A 3350 AML8095100GPL BULB DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 965TW 53615 LGA - FOUND EMERGENCY SEAT MOUNTED LIGHTS AT SEAT ROW 7 INOPERATIVE. RELAMPED EMERGENCY SEAT MOUNTED LIGHTS AT SEAT ROW 7. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007021400104 20070214 00104 2007 2 14 AALA20070184 4 20070125 A 2565 SLIDE BOEING 757 757223 1384957 NM L1 DOOR INOPERATIVE A AALA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 633AA 24591 MIA - LEFT NUMBER ONE DOOR SLIDE FELL OUT OF HOUSING WHEN DOOR OPENED. UNSUCCESSFUL DEPLOYMENT. FOUND DEBRIS AT GIRT B AR. CLEARED DEBRIS FROM GIRT BAR AREA AND REINSTALLED LEFT NUMBER ONE DOOR SLIDE AND POWER ASSIST BOTTLE. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007021400105 20070214 00105 NM 2007 2 14 AALA20070196 1 20070127 A 3397 CONNECTOR DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9413T 53188 SFO - FOUND EMERGENCY LIGHTS AT SEAT 28D INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHTS AT SEAT 28D. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2007021400106 20070214 00106 NM 2007 2 14 AALA20070197 1 20070128 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 369AA 25196 LGA - EMERGENCY LIGHT AT SEAT 25A INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 25A. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A1NM 2007021400107 20070214 00107 WP 2007 2 14 AALA20070200 1 20070127 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7508 49802 LGA - BATTERY PACKS FOR EMERGENCY LIGHTS IN MID CABIN FAILED FUNCTIONAL TEST. REPLACED BATTERY PACKS AT AB52 AND AB53 F OR EMERGENCY LIGHTS IN MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007021400108 20070214 00108 WP 2007 2 14 AALA20070186 1 20070125 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 76202 53292 LGA - EMERGENCY LIGHT AT AFT STAIRWELL FORWARD INOPERATIVE. REPINNED CONNECTOR FOR EMERGENCY LIGHT AT AFT STAIRWELL FOR WARD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007021400109 20070214 00109 WP 2007 2 14 AALA20070183 1 20070125 A 3350 BULB DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 439AA 49457 BOS - EMERGENCY LIGHT LAMP AT ROW 12AB SIDEWALL BROKEN BY PASSENGER. RELAMPED EMERGENCY LIGHT AT ROW 12AB SIDEWALL. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007021400110 20070214 00110 WP 2007 2 14 AALA20070185 1 20070125 A 2150 HEAT EXCHANGER DOUG DC9 DC982 3022082 WP AIR CONDITIONING INOPERATIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 456AA 49561 ORD INFLIGHT T366/25JAN - REPORTED FUMES IN COCKPIT AND FLIGHT ATTENDANTS REPORTED BLUISH GREY SMOKE COMING OUT OF VENTS . HIGH TEMPERATURE PACK LIGHT ILLUMINATED. SMOKE SUBSIDED WHEN PACK TURNED OFF. RETURNED TO ORD AND LANDED WITHOUT IN CIDENT. REPLACED RIGHT MOTOR PRIMARY AND SECONDARY HEAT EXCHANGER. ACCOMPLISHED PACK SYSTEM BURN OUT. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007021400127 20070214 00127 EA 2007 2 14 SIMA200704410 1 20070212 A 3310 2LA00691307 LIGHT CNDAIR CL600 CL6002C10 1390015 EA FLIGHT DECK MELTED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 509AE 9747 10078 SMOKE AND SPARKS OBSERVED COMING FROM THE GLARESHIELD AREA ABOVE THE TILLER WHEEL DURING AIRCRAFT BOARDING. AIRCRAFT PO WER DOWN. REMOVED AND REPLACED FLOOD LIGHT ASSEMBLY IAW EMB AMM 33-11-05. 2 L 7 2 4F RT A21EA 2007021400128 20070214 00128 SO 2007 2 14 SIMA200704411 1 20070212 A 5320 14522178005 SILL EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 803AE 13064 4800 145483 FOUND SERVICED DOOR FRAME LOWER CENTER SILL FOUND CORRODED. REMOVED EXISTING SILL, CLEANED AND TREATED REPAIR AREA. IN STALLED NEW SILL IAW EMB EMB SRM 51-40-02. RESTORED PROTECTED FINISH, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007021400129 20070214 00129 NM 2007 2 14 SWAA070749 1 20070212 A 5753 65C30462 SKIN BOEING 737 7373Q8 1384670 NM FORE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007021400130 20070214 00130 NM 2007 2 14 SWAA070717 1 20070210 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM BS 910 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 910, STR 4R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007021400131 20070214 00131 NM 2007 2 14 SWAA070715 1 20070210 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM BS 908 S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 908, STR 5R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007021400132 20070214 00132 NM 2007 2 14 SWAA070735 1 20070212 A 5311 69265553 FRAME BOEING 737 7373H4 1384600 NM BS 348 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED SPV CHECK, FOUND FRAME WEB CRACKED AT BS 348, STR 16L. REPAIRED FRAME WEB PER SRM AND EA. 2 L 7 2 4F RT A16WE 2007021400133 20070214 00133 NM 2007 2 14 SWAA070733 1 20070211 A 3350 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007021400134 20070214 00134 2007 2 14 SWAA070736 4 20070212 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007021400135 20070214 00135 NM 2007 2 14 SWAA070732 1 20070211 A 3350 MS155721 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 6 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007021400136 20070214 00136 NM 2007 2 14 SWAA070731 1 20070211 A 2560 P4010021 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 481WN 29853 DURING SCHEDULED RON CHECK, FOUND FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2007021400137 20070214 00137 NM 2007 2 14 SWAA070734 1 20070211 A 5552 REP4M6 BEARING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TORQUE TUBE HORN BEARING PER MM. 2 L 7 2 4F RT A16WE 2007021400138 20070214 00138 NM 2007 2 14 SWAA070739 1 20070212 A 5552 REP4M6 BEARING BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TORQUE TUBE HORN BE ARING PER MM. 2 L 7 2 4F RT A16WE 2007021400139 20070214 00139 NM 2007 2 14 SWAA070724 1 20070210 A 3397 W115006220 WIRE BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. FOUND BROKEN WIRE, REPAIRED WIRE W1150-06 2-20 PER WDM. 2 L 7 2 4F RT A16WE 2007021400140 20070214 00140 NM 2007 2 14 MZZA0700002 1 20070212 A 2560 61020 BATTERY BOEING 737 737824 13844BZ NM CFMINT CFM56 CFM567B26US NE FLASHLIGHT INOPERATIVE A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 14235 28947 INSPECTION FOUND FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOPERATIVE. THE FLASHLIGHT BATTERY WAS REPLACED IAW MM 2 5-64-00. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007021400141 20070214 00141 WP 2007 2 14 AALA20070195 1 20070126 A 3350 AML8095100GPL BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 561AA 53091 LAX - EMERGENCY SEAT MOUNTED LIGHT AT SEAT ROW 11 BROKEN. RELAMPED EMERGENCY SEAT MOUNTED LIGHT AT SEAT ROW 11. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007021400142 20070214 00142 CE 2007 2 14 FCPR20070004 1 20070213 A 3411 CM29337 STATIC PORT CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE RIGHT LEAKING B FCPR K NONE O OTHER IN INSP/MAINT 1 NM 09 77PR 150 5500211 FOUND RT STATIC PORT P/N CM2933-7 CRACKED DURING LEAK TEST. 1 L 7 2 4F 4 F A22CE E1NE 2007021400144 20070214 00144 CE 2007 2 14 68DA2 1 20070213 A 2750 1005240731 MOTOR BEECH 100 B100 1152919 CE GARRTT TPE331 TPE331* 01514 WP TE FLAP FAULTY B ODAR O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 21 68DA BE14 ON APPROACH, NO PAX, PILOT NOTICED A SMELL OF ELECTRICAL SMOKE, CONCURRENTLY WITH A POPPED FLAP MOTOR CIRCUIT BREAKER PO PPING. ON INSPECTION, MAINTENANCE FOUND AN INOP FLAP MOTOR. 1 L 7 2 4T 3 T A14CE E2WE 2007021500002 20070215 00002 CE 2007 2 15 DXTA200701930 1 20070212 A 3220 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG UNKNOWN E DXTA O OTHER E VIBRATION/BUFFET CR CRUISE 1 GL 07 979QS 7500079 A MODERATE THUMP (THAT SOUNDS AND FEELS LIKE IT IS COMING FROM THE NOSE WHEEL AREA) EXPERIENCED DURING CLIMB AND IN CRUI SE- CO PILOT'S FEET ON FLOOR. REMOVED & REPLACED NLG UPLOCK SWITCH IAW CESSNA 750 M/M CHPT 32-30-05. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007021500003 20070215 00003 SO 2007 2 15 C2XA07SH009 1 20070212 A 5320 14532637401 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15983 145239 DURING C-CHECK CENTER OMEGA BEAM LOWER FLANGE WAS FOUND WITH CORROSION BETWEEN FRMS 23 AND 29. MAINTENANCE REPAIRED CENT ER OMEGA BEAM AT FRM 24 IAW SRM 53-00-10; RESTORED ORIGINAL FINISH TO BLEND AREAS AT FRMS 23 TO 29 IAW EMB 145 CPM 51-21 -07. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007021500004 20070215 00004 SO 2007 2 15 C2XA07SH008 1 20070212 A 5320 14521713003 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15983 145239 DURING C-CHECK CENTER OMEGA BEAM WAS FOUND WITH CORROSION AT FR 18 TO FR 20. MAINTENANCE REPLACED THE CENTER OMEGA BEAM AT FR 17 TO 24 IAW SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007021500009 20070215 00009 EA 2007 2 15 QXEA200700095 1 20070115 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 320-477 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND RIGHT INBOARD CABIN SEAT TRACK IS CORRODED BETWEEN FS 320 AND FS 477. REPAIRED IAW CRJ TASK 53-00-49-000 -801-A03. 2 L 7 2 4F RT A21EA 2007021500011 20070215 00011 EA 2007 2 15 QXEA200700093 1 20070115 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 540 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND RIGHT INBOARD SEAT TRACK HAS SURFACE CORROSION INSIDE AND ON TOP OF THE TRACK AT FS 540. REPAIRED IAW RE O670-53-00-013. 2 L 7 2 4F RT A21EA 2007021500012 20070215 00012 EA 2007 2 15 QXEA200700096 1 20070115 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 394-477 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND LEFT INBOARD CABIN SEAT TRACK HAS LIGHT CORROSION AT MULTIPLE LOCATIONS BETWEEN FS 394 AND FS 477. REPAI RED IAW REO670-53-00-013. 2 L 7 2 4F RT A21EA 2007021500014 20070215 00014 WP 2007 2 15 AALA20070201 1 20070128 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 483A 49676 PHX - BATTERY PACKS FOR EMERGENCY LIGHTS IN FORWARD CABIN STATION 211 CENTER FAILED FUNCTIONAL TEST. REPLACED BATTERY P ACKS FOR EMERGENCY LIGHTS IN FORWARD CABIN STATION 211 CENTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007021500016 20070215 00016 WP 2007 2 15 AALA20070199 1 20070127 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7508 49802 LGA - EMERGENCY EXIT LIGHT AT RIGHT AFT OVERWING EMERGENCY DOOR INOPERATIVE. REPLACED BATTERY PACK AT POSITION AB54 FOR EMERGENCY EXIT LIGHT AT RIGHT AFT OVERWING EMERGENCY DOOR. 2 L 7 2 4F A6WE 2007021500018 20070215 00018 WP 2007 2 15 AALA20070206 1 20070127 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 480AA 49655 SFO - OVERWING EMERGENCY EXIT LIGHTS AT AFT LEFT AND RIGHT INOPERATIVE. REPLACED BATTERY PACK FOR OVERIWNG EMERGENCY EX IT LIGHTS AT AFT LEFT AND RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007021500019 20070215 00019 NM 2007 2 15 AALA20070222 1 20070129 A 3040 CONTROLLER BOEING 737 737823 13844BZ NM WINDOW HEAT INOPERATIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 942AN 30084 MSY INFLIGHT T2036/29JAN DFW TO MIA - CAPTAINS LEFT NUMBER TWO SLIDING WINDOW BEGAIN ARCING AND WINDOW CRACKED. LANDED MSY WITHOUT INCIDENT. REPLACED LEFT NUMBER TWO WINDOW AND HEAT CONTROLLER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007021500021 20070215 00021 EU 2007 2 15 AALA20070204 1 20070127 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 90070 513 JFK - FOUND EMERGENCY LIGHTS AT SEATS 19C TO 28C INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEATS 19C T O 28C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007021500024 20070215 00024 EU 2007 2 15 AALA20070213 1 20070128 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 MIA - EMERGENCY LIGHT AT SEAT 23G INOPERATIVE. REPLACED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 23G. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007021500025 20070215 00025 NM 2007 2 15 AALA20070208 1 20070128 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 782AN 30003 ORD - FOUND EMERGENCY LIGHT AT SEAT 22C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007021500026 20070215 00026 NM 2007 2 15 AALA20070211 1 20070128 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 782AN 30003 ORD - FOUND EMERGENCY LIGHT AT SEAT 40C MISSING LAMP. RELAMPED EMERGENCY LIGHT AT SEAT 40C. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT T00001SE 2007021500029 20070215 00029 WP 2007 2 15 AALA20070218 1 20070129 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 457AA 49562 ORD EMERGENCY LIGHT AT SEAT 19D HAS MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 19D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F A6WE 2007021500030 20070215 00030 NM 2007 2 15 AALA20070209 1 20070128 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 782AN 30003 ORD - FOUND EMERGENCY LIGHT AT SEAT 22C MISSING LAMPS. RELAMPED EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT T00001SE 2007021500031 20070215 00031 NM 2007 2 15 AALA20070210 1 20070128 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 782AN 30003 ORD - FOUND EMERGENCY LIGHT AT SEAT 40C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 40C. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007021500032 20070215 00032 NM 2007 2 15 AALA20070214 1 20070128 A 3350 0201804002 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 968AN 30095 MIA - FOUND EMERGENCY LIGHT AT SEAT 13F MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 13F. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007021500034 20070215 00034 WP 2007 2 15 AALA20070219 1 20070129 A 3350 SHIELD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 457AA 49562 ORD - FOUND EMERGENCY LIGHT AT SEAT 24D HAS MISSING SHIELD. REPLACED SHIELD FOR EMERGENCY LIGHT AT SEAT 24D. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007021500036 20070215 00036 WP 2007 2 15 AALA20070221 1 20070129 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 457AA 49562 ORD - FOUND EMERGENCY LIGHT AT SEAT 24D HAS MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007021500038 20070215 00038 EA 2007 2 15 QXEA200700082 1 20070115 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 584 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 584 AND BETWEEN STRINGER 22R A ND STRINGER 23R. REPAIRED IAW SRM 51-42-06, 53-00-01, 51-21-11, AND 51-25-01. 2 L 7 2 4F RT A21EA 2007021500040 20070215 00040 EA 2007 2 15 QXEA200700080 1 20070115 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 600 S17R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 600 AND STRINGER 17R. REPAIRE D IAW SRM 51-42-06, 53-00-01, AND 51-25-01. 2 L 7 2 4F RT A21EA 2007021500043 20070215 00043 EA 2007 2 15 QXEA200700084 1 20070117 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - DUE TO NUMEROUS DISCREPANCIES, FS 280 FLOORBEAM REQUIRES REPLACEMENT, REF NON ROUTINE 00162, NONROUTINE 00163 A ND NON ROUTINE 00171. REPLACED IAW SRM 51-42-00, 51-40-11, AND REO670-53-11-047. 2 L 7 2 4F RT A21EA 2007021500044 20070215 00044 EA 2007 2 15 QXEA200700085 1 20070115 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 259 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD AT FS 259 STRINGER 23. REPAIRED IAW SRM 51-42-06, 53-00-01, 5 1-21-11, AND 51-25-01. 2 L 7 2 4F RT A21EA 2007021500046 20070215 00046 EA 2007 2 15 QXEA200700087 1 20070115 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 265 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD AT FS 265 STRINGER 22R. REPAIRED IAW SRM 51-42-06, 53-00-01, 51-21-11, 51-25-01. 2 L 7 2 4F RT A21EA 2007021500047 20070215 00047 EA 2007 2 15 QXEA200700088 1 20070115 A 5310 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA BS 273 S22R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD AT FS 273 STRINGER 22R. REPAIRED IAW SRM 51-42-06, 53-00-01, 51-21-11, 51-25-01. 2 L 7 2 4F RT A21EA 2007021500049 20070215 00049 SO 2007 2 15 C2XA07IA032 1 20070211 A 3350 1317 BULB EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHTS BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13936 145025 IAH - DURING PREFLIGHT INSPECTION, THE EMERGENCY EXIT LIGHT AT THE CABIN DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007021500050 20070215 00050 NE 2007 2 15 MWEA070030 2 20070211 A 7200 BR700715A130 ENGINE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE RIGHT FAILED A MWEA C ABORTED TAKEOFF Y J ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 GL 13 916ME 55178 RIGHT ENGINE FAILURE. REMOVED AND REPLACED RIGHT ENGINE. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007021500053 20070215 00053 EU 2007 2 15 TRAX200700201 1 20070209 A 2750 FLAP SYSTEM AEROSP ATR72 ATR72212 8680945 EU TE FLAPS MALFUNCTIONED A ASOA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 27 634AS 370 ON SHORT FINAL, RECEIVED FLAP UNLOCK LIGHT. PERFORMED MISSED APPROACH. FOLLOWED QRH. A MADE FLAP '0' LANDING IN CHA. EMERGENCY EQUIPMENT ON STANDBY. 2 H 7 2 4T RT A53EU 2007021500054 20070215 00054 EA 2007 2 15 TRAX200700202 1 20070209 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 DURING PREFLIGHT INSPECTION, FOUND EXTERIOR EMERGENCY LIGHTS INOP/CREW RESET CB, NO HELP. 2 L 7 2 4F RT A21EA 2007021500056 20070215 00056 EA 2007 2 15 QXEA200700103 1 20070117 A 5551 BOLT CNDAIR CL600 CL6002C10 1390015 EA HORIZONTAL STAB CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND HORIZONTAL STABILIZER MOUNT BOLT ANTI-ROTATION TAB ON LEFT HAND SIDE IS CHAFED AT BOTH ENDS. REPAIRED IA W REO670-55-11-064 AND SRM 51-21-16. 2 L 7 2 4F RT A21EA 2007021500057 20070215 00057 EA 2007 2 15 QXEA200700097 1 20070115 A 5320 ANGLE CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND LEFT LOWER 90 DEGREE VERTICAL ANGLE IS CRACKED AT BOTTOM END THROUGH RIVET HOLES AT FS 280, LBL 25.5. RE PAIRED IAW SRM 51-42-06 AND 51-42-00. 2 L 7 2 4F RT A21EA 2007021500060 20070215 00060 EA 2007 2 15 QXEA200700102 1 20070124 A 5551 BOLT CNDAIR CL600 CL6002C10 1390015 EA HORIZONTAL STAB CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND HORIZONTAL STABILIZER MOUNT BOLT ANTI-ROTATION TAB ON RIGHT SIDE CHAFED AT AFT END. REPAIRED IAW REO670- 55-11-064 AND SRM 51-21-16. 2 L 7 2 4F RT A21EA 2007021500061 20070215 00061 SO 2007 2 15 C2XA07IA033 1 20070211 A 3350 74441 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13956 145078 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHT AT THE FLIGHT ATTENDANT STATION WAS INOPER ATIVE. MAINTENANCE RESET THE CONNECTOR ON THE SIGN, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVE D FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007021500062 20070215 00062 SO 2007 2 15 C2XA07IA034 1 20070209 A 3350 2013BR BATTERY EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17108 6996 4121 145655 IAH - DURING PREFLIGHT INSPECTION, A CABIN EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN T O SERVICE. 2 L 7 2 4F RT 2007021500063 20070215 00063 SO 2007 2 15 C2XA07IA035 1 20070208 A 3350 78241 INVERTER EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27523 145389 LCH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THE EMERGENCY EXIT LIGHT ON THE RIGHT WINDSCREEN TO BE INOPERATIV E. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, A ND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007021500064 20070215 00064 SO 2007 2 15 C2XA07IA036 1 20070213 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145EP 3260221 SO CARGO BAY INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16927 8771 194 145006 MEM - DURING MAINTENANCE INSPECTION THE BAGGAGE FIRE DETECTOR WAS FOUND TO BE INOPERATIVE. THE DETECTOR WAS PLACED ON M EL 26-23-00 CAT C CONTROL NUMBER 115843, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IA H ON FLIGHT 4930 WHERE MAINTENANCE REMOVED AND REPLACED THE BAGGAGE SMOKE DETECTOR, OPERATIONALLY CHECKED WITH NO DEFECT S, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007021500066 20070215 00066 EU 2007 2 15 2007UALA00295 1 20070204 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 487UA 1669 EPSU UNIT FWD LEFT FAILS EMERGENCY LIGHT TEST. REPLACED EPSU AND REPAIRED WIRING SHORTED TO SEAT TRACK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007021500068 20070215 00068 NM 2007 2 15 2007UALA00297 1 20070203 A 5320 INTERCOSTAL BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE BS 294 S16L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 912UA 25290 FOUND LT FUSELAGE INTERNAL INTERCOSTAL IS CRACKED AT STR 16L. JUST AFT OF FRAME AT BS 294.5. REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2007021500070 20070215 00070 2007 2 15 2007UALA00299 4 20070202 A 2565 GIRT BAR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 913UA 25291 FOUND PASSENGER DOOR L1 SLIDE GIRT IS NOT PROPERLY STOWED ON THE SLIDE. REPACKED GIRT BAR MATERIAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007021500071 20070215 00071 NM 2007 2 15 2007UALA00300 1 20070204 A 5330 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU BS 847 S24R DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 913UA 25291 AFT CARGO DOOR CUTOUT AFT LOWER CORNER HAS SKIN DELAMINATION AT STR 24R BS 847. INSTALLED EXTERNAL FUSELAGE SKIN DOUBLE R TRIPLER REPAIR PER SRM 53-00-01 REPAIR 32 DETAIL XVI AND V. 2 L 7 2 4F 4 F RT A16WE E21EU 2007021500072 20070215 00072 NM 2007 2 15 2007UALA00301 1 20070203 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 303UA 23644 FOUND AFT CABIN EEL LIGHTS INOPERATIVE. REPLACED EEL STRIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007021500073 20070215 00073 NM 2007 2 15 2007UALA00302 1 20070205 A 5310 STRUCTURE BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 105UA 26473 FOUND DENT AND SCRATCH BELOW AND FWD OF R5 DOOR ON BLUE STRIPE. DENT MEASURES 3 INCHES BY 4 INCHES BY .125 INCH DEEP, AREA BURNISHED AND INSPECTED FOR CRACKS, NONE NOTED. CONT OF AMIS ITEM 53120 -AREA BLENDED AND HFEC ACP REF UA-EVA-60656 , INSTALLED DOUBLER REPAIR. SET UP REPEAT FOLLOW-UP INSP. SUSPECT IMPACT BY GROUND EQUIPMENT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007021500076 20070215 00076 2007 2 15 2007UALA00305 4 20070203 A 2565 LIFTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GIRT BAR WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 FOUND DOOR 4R AND 4L AFT GIRT BAR LIFTERS HAVE WORN AREAS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007021500080 20070215 00080 NM 2007 2 15 2007UALA00309 1 20070203 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 644UA 25094 FOUND EEL LIGHTS COME ON INTERMITTENTLY AT SEATS 15 THRU TO REAR OF AIRCRAFT, LEFT AISLE. CLEANED CONNECTOR AT EMERGENC Y EXIT LIGHT BATTERY CHARGER OUTBOARD OF SEAT 18A. LIGHTS OPERATE NORMALLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007021500082 20070215 00082 NM 2007 2 15 2007UALA00311 1 20070202 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 669UA 30025 EMERGENCY CEILING LIGHTS FOUND INOPERATIVE. SPLICED IN SERVICEABLE FEEDER AND REPLACED BATTERY PACKS. SYSTEM OP CHEC KS OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007021500086 20070215 00086 2007 2 15 2007UALA00315 4 20070203 A 2565 CABLE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE R4 DOOR SLIDE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 793UA 26946 FLIGHT ATTENDANTS REPORT DOOR 4 RIGHT IS FROZEN AND WILL NOT DISARM. DOOR 4R UNABLE TO DISARM. RAISED TEMP IN AC TO TH AW DOOR ARMING CABLE. CYCLED DOOR AND ARM DISARM LEVER NUMEROUS TIMES. APPLIED ICE RELEASE TO DOOR AND GIRT BAR MECH. P ROBLEM REPEATED IN DEN. REPLACED ARMING PUSH PULL CABLE. OP CHKS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007021500088 20070215 00088 EU 2007 2 15 2007UALA00318 1 20070205 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 402UA 439 FOUND EMERGENCY EXIT LIGHTS INOP AT ROWS 1, 2, 3, 6. REPAIR SHORTED WIRES UNDER SEAT 6ABC. ALL EMERGENCY LIGHTS TES TED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007021500089 20070215 00089 EU 2007 2 15 2007UALA00319 1 20070205 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 402UA 439 FOUND EMERGENCY EXIT PATH LIGHT IS INOP AT SEAT 18. REPAIRED WIRING UNDER SEAT 18ABC, AT PATH LIGHT CONNECTOR. OPS CHEC KED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007021500090 20070215 00090 EU 2007 2 15 2007UALA00320 1 20070205 A 5314 KEELBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 410UA 463 FOUND LEFT AND RIGHT KEELBEAM TO BELLY FAIRING SUPPORT FAIRING ATTACH ANGLES ARE CRACKED AT FRAME 46. MAJOR REPAIR ACCO MPLISHED: MFG'D & INSTALLED REPAIR ANGLE SECTION. 2 L 7 2 4F 4 F RT A28NM E40NE 2007021500091 20070215 00091 SO 2007 2 15 C2XA07BT015 1 20070208 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO CABIN ODOR A C2XA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 11127 145697 EWR LOG SQUAWK FLT NR 2323, STRONG FUEL ODOR ON TAKEOFF ROLL THROUGH 600 FT. INSPECTED AFT COWLING AND FOUND VERY SMALL AMOUNT OF RESIDUAL FUEL AND STRONG SMELL OF FUEL, MEL'D APU IAW MEL 49-00-00. LATER REMOVED AND REPLACED ANTI SURGE VA LVE IAW EMB145 MM 49-55-01. OPS CHECK GOOD. ODOR STILL PRESENT. APU REMAINS ON MEL. 2 L 7 2 4F RT 2007021500092 20070215 00092 SO 2007 2 15 C2XA07BT016 1 20070211 A 3350 20131A BATTERY EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS WEAK A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14143 14504 5830 145739 EWR LOG SQUAWK FLT NR 1206, FOUND SEVERAL CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY IAW EMB-145XR AMM 33-50-04. OPS CHECK GOOD CLOSED 2 L 7 2 4F RT 2007021500093 20070215 00093 SO 2007 2 15 ECI10515 1 20070212 A 2752 1159SC21216 ACTUATOR GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6108 NE RT TE FLAPS ERRATIC E E0XA K NONE O OTHER IN INSP/MAINT 1 SO 35 919CT 1051 FLAPS FAILED IN THE UP POSITION WHEN INSPECTED BY MAINTENANCE. THE FLAPS WERE FOUND TO BE BINDING ON THE RT FLAP. THE OB FLAP ACTUATOR WAS FOUND TO BE FAULTY AND REPLACED. ALL RIGGING CHECKS AND ASYMMETRY CHECKS WERE COMPLIED WITH. FLAP S WERE OPERATED 35 TIMES WITH NO DISCREPANCIES. 2 L 7 2 4F 4 F RT A12EA E25NE 2007021500097 20070215 00097 NM 2007 2 15 2007UALA00323 1 20070205 A 5210 LATCH BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU R2 DOOR DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 937UA 26668 DOOR 2R IS VERY DIFFICULT TO DISARM. THE CAUSE WAS DIRTY LATCHES. CLEANED LATCHES. 2 L 7 2 4F 4 F RT A16WE E21EU 2007021500099 20070215 00099 NM 2007 2 15 2007UALA00325 1 20070206 A 3350 LAMP BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 FOUND EEL'S INOPERATIVE AT SEATS 3A-AFT, 4A-AFT, 5A-AFT, 5F-AFT. RELAMPED EACH SEAT POSITION, ALL OP CHECKED OK FOR SER VICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007021500102 20070215 00102 CE 2007 2 15 DJFA2007018 1 20070209 A 2510 SEAT RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP COCKPIT CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 813CW 258413 DURING A SCHEDULED MAINTENANCE EVENT A CRACK WAS DISCOVERED ON THE COPILOT'S SEAT WEB. THE CRACK WAS APPROX 2.5 INCHES LONG AND EXCEEDED THE APPROVED REPAIR REQUIREMENTS OF 2.15 INCHES. THE SDR WILL BE UPDATED UPON COMPLETION OF THE CORRE CTIVE ACTION. 2 L 7 2 4F 4 F RT A3EU E6WE 2007021500104 20070215 00104 NE 2007 2 15 I5HA0724002 2 20070111 A 7261 SHAFT CVAC STC STC240 PWA R2800 CB17 52026 NE SCAVENGE PUMP SHEARED A I5HA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 23 150PA 2944 278 P36486 ON APPROACH, (EIS) THE CREW NOTED THE RT ENGINE OIL QUANTITY DROPPING. THE RT ENGINE WAS SHUTDOWN AS A PRECAUTIONARY ME ASURE. THE AIRCRAFT LANDED WITHOUT INCIDENT AND MAINTENANCE FOUND NO EVIDENCE OF EXTERNAL OIL LEAKAGE. FURTHER INVESTI GATION INDICATED THE FRONT SCAVENGE OIL PUMP HAD FAILED AND THE OIL WAS POOLED IN THE FRONT GEARBOX. THE FORWARD SCAVEN GE PUMP WAS REMOVED AND THE DRIVE MECHANISM WAS INSPECTED. NO DAMAGE WAS FOUND. OIL SCREENS WERE INSPECTED AND THERE W AS NO INDICATION OF METAL IN THE OIL SCREENS. THE FORWARD SCAVENGE PUMP WAS REPLACED AND THE ENGINE RUN WITH NO ABNORMA LITIES. THE AIRCRAFT WAS RETURNED TO SERVICE. THE ENGINE SCREENS WERE RECHECKED FOR METAL WITH NO FINDINGS. THE AIRCR 2 L 7 2 4R 4 R A793 E264 2007021500105 20070215 00105 NE 2007 2 15 WRLA2007035 2 20070210 A 7200 TORQUE BOX DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 1 ENGINE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 62911 48407 DURING 3C + 12A CHECK, EGAT MECHANIC FOUND ENG 2 LT TORQUE BOX LOWER SIDE CASCADE FWD RING CAP OUTER CRACK APPROX 1". R EF CMM 78-32-35 PAGE 1021 ITEM 505. 2 L 7 3 4F 4 F RT A22WE E24NE 2007021500106 20070215 00106 EU 2007 2 15 USAA070098 1 20070213 A 5315 D5347218920400 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 169UW 1455 FOUND 2 AREAS, TOP SIDE OF FLOORBEAM Y1292 FR 64-49. INSTALLED NEW BEAMS PER SRM 51-42-11; CORROSION LEVEL 1; TASK JA-2 60-53500, DEFECT SIZE: 1.5" BY 1.5". 2 L 7 2 4F RT A28NM 2007021500108 20070215 00108 EU 2007 2 15 USAA070096 1 20070213 A 5315 D53472075001 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSLEAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 169UW 1455 FOUND FLOORBEAM CORRODED, -Y1732 BNTH TAB FITTING AFT RT DOOR. MODIFIED PART INSTALLED PER SRM 53-41-14; CORROSION LEVE L 1; TASK NR JA-260-53500 DEFECT SIZE: 1" BY 1". 2 L 7 2 4F RT A28NM 2007021500111 20070215 00111 GL 2007 2 15 I5HA0758003 2 20070115 A 7320 6809643 RELAY CVAC 580 580 2422806 WP ALLSN 501D 501D13 03004 GL RT ENGINE FAILED A I5HA C ABORTED TAKEOFF X J ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 GL 23 581P 29 CAE501388 ON TAKEOFF ROLL, RT ENGINE TURBINE INLET TEMPERATURE (TIT) REACHED 880 DEGREES AND BEGAN TO DETERIORATE. CREW NOTED A L OUD BANG (COMPRESSOR STALL) AND THE ENGINE SPOOLED DOWN. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO BASE. SU BSEQUENT ATTEMPT TO RESTART THE ENGINE FAILED. THE ENGINE WOULD NOT ROTATE. INITIAL INSPECTION BY MAINT DID NOT INDICA TE ANY OBVIOUS PROBLEM. A FURTHER DETAILED INSPECTION INCLUDING BOROSCOPE OF THE TURBINE AND VISUAL INSPECTION OF THE C OMPRESSOR ALSO DID NOT INDICATE ANY PROBLEM OR DAMAGE. THE ENGINE WAS SUCCESSFULLY STARTED AND RUN AT HIGH POWER SETTIN GS. WITH THE TEMPERATURE DATUM (TD) SYSTEM CIRCUIT BREAKER IN, THE ENGINE FUEL FLOW, RPM AND HORSE POWER WOULD DETERIOR 2 L 7 2 4T 4 T RT E282 2007021500112 20070215 00112 NM 2007 2 15 SWAA070737 1 20070212 A 3350 1010427 COVER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 FOUND BULL NOSE EMERGENCY EXIT LIGHT COVER MISSING AT ROW 21 ABC. INSTALLED LIGHT COVER PER MM. 2 L 7 2 4F RT A16WE 2007021500113 20070215 00113 NM 2007 2 15 SWAA070729 1 20070211 A 3350 300432 LIGHT BOEING 737 7375H4 138449D NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED MV1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT OUT OF POSITON AT ROW 3 ABC. REPOSITIONED LIGHT PER MM . 2 L 7 2 4F RT A16WE 2007021500114 20070215 00114 NM 2007 2 15 SWAA070727 1 20070211 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 6 ABC. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007021500117 20070215 00117 NM 2007 2 15 SWAA070723 1 20070210 A 2730 6545187 TORQUE TUBE BOEING 737 7373H4 1384600 NM RT ELEVATOR FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, RT ELEVATOR BUSS LINKAGE FAILED TEST. REMOVED AND REPLACED ELEVATOR OUTPUT TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007021500120 20070215 00120 NM 2007 2 15 SWAA070728 1 20070211 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 450 S17R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 FOUND FUSELAGE SKIN CRACKED AT BS 450, STR 17R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007021500121 20070215 00121 NM 2007 2 15 SWAA070713 1 20070210 A 5753 6546430121 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD FORE FLAP DELAMINATED AT UPPER SURFACE. REMOVED AND REPLACED FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2007021500122 20070215 00122 NM 2007 2 15 SWAA070726 1 20070210 A 5322 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM BS 500B S27L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007021500123 20070215 00123 NM 2007 2 15 SWAA070740 1 20070212 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM BS 616 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 616, STR 16R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007021500124 20070215 00124 NM 2007 2 15 SWAA070721 1 20070210 A 5311 6546540 FRAME BOEING 737 7373H4 1384600 NM BS 639 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 8R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007021500125 20070215 00125 NM 2007 2 15 SWAA070722 1 20070210 A 5311 6546540 FRAME BOEING 737 7373H4 1384600 NM BS 663 S3L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 663, STR 3L. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 2007021500127 20070215 00127 EA 2007 2 15 QXEA200700075 1 20070115 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 534 S19R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 534 AND STRINGER 19R. REPAIRE D IAW SRM 53-00-01, 51-42-06, 51-25-01. 2 L 7 2 4F RT A21EA 2007021500128 20070215 00128 EA 2007 2 15 QXEA200700076 1 20070116 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 534 S23R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 534 AND STRINGER 23R. REPAIRE D IAW SRM 51-42-06, 53-00-01, 51-25-01. 2 L 7 2 4F RT A21EA 2007021500129 20070215 00129 EA 2007 2 15 QXEA200700077 1 20070115 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 547 S20R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 547 AND STRINGER 20R. REPAIRE D IAW SRM 51-42-06, 53-00-01, 51-25-01. 2 L 7 2 4F RT A21EA 2007021500130 20070215 00130 EA 2007 2 15 QXEA200700074 1 20070115 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 525 S19R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 525 AND STRINGER 19R. REPAIRE D IAW SRM 53-00-01, 51-42-06, 51-25-01. 2 L 7 2 4F RT A21EA 2007021500134 20070215 00134 NE 2007 2 15 WRLA2007034 2 20070210 A 7200 TORQUE BOX DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 2 ENGINE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 62911 48407 DURING 3C + 12A CHECK, EGAT MECHANIC FOUND ENG 2 RT TORQUE BOX LOWER SIDE CASCADE FWD RING CAP OUTER CRACK APPROX 1" AND DOOR AND CRACK ABOUT 1.5". REF CMM 78-32-35 PAGE 1007 ITEM 121 AND PAGE 1021 ITEM 505. PER ENGINEERING INSTRUCTION NO: W2007A78B-110 REV:00 REPAIRED CRACK AREA ON NR 2 RT T/R OUTER CAP ANGLE AND DOOR LAND SUPPORT. JOB COMPLETED AND CONDIT ION CHECK NORMAL. 2 L 7 3 4F 4 F RT A22WE E24NE 2007021500137 20070215 00137 NM 2007 2 15 QXEA200700158 1 20070209 A 3020 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM NR 1 ENGINE UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 408QX 4050 EUG FLIGHT NR 2408: ENG ADPT HEAT 1 CAUTION AFTER ENGINE START. MAINTENANCE CYCLED POWER TO NR 1 ENGINE. ADPT HEATER C AUTION LIGHT EXTINGUISHED. ALL OPS NORMAL. NO PARTS REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007021500139 20070215 00139 EA 2007 2 15 A6WA200740011 1 20070109 A 5320 601R7526215T BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT MLG BAY CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 412AW 7582 HYDRAULIC TRANSDUCER HOT CHANNEL IN RIGHT MLG BAY CEILING CRACKED APPROXIMATELY .2 INCHES LONG, BRACKET P/N 601R75262-15 7. MAINTENANCE DRILLED OFF, REMOVED CRACKED BRACKET. DRILLED UP AND INSTALLED NEW BRACKET P/N 601R-75262-15T WET USING PR1422B SEALANT AN MS20470AD5-6 SOLID RIVETS, PRIMED, PAINTED DINOTROLED REPAIR AREA IAW CRJ 200 SRM. (M) 2 L 7 2 4F RT A21EA 2007021500140 20070215 00140 EA 2007 2 15 COMA0760157 1 20070205 A 2752 854D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA RT WING BINDING A COMA L ABORTED APPROACH J WARNING INDICATION DE DESCENT 1 SO 01 595SW 9227 7297 FLIGHT 5075 - FLAP FAIL MESSAGE ON DESCENT, DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RT OUTBOARD FLAP OUTBOARD ACTUATOR. 2 L 7 2 4F RT A21EA 2007021500141 20070215 00141 EU 2007 2 15 R61A20070003 1 20070206 A 2780 SLAT SYSTEM EMB ERJ170 ERJ170100 EU LE SLATS UNKNOWN A R61A O OTHER J WARNING INDICATION LD LANDING 1 GL 11 801MA 17000012 CREW REPORTED A SLAT FAIL MESSAGE ON LANDING. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT TO TROUBLESHOOT. MAINTENANCE CLEARED THE SLAT ACE INHIBITS TEST AND BRAKE RELEASE TEST. INSPECTED SLAT TRACKS, ACTUATORS, SKEW SENSORS AND DRIVE SHA FTS. PERFORMED FUNCTIONAL/OPERATIONAL TEST SYSTEM OPS CHECK GOOD. NO OTHER DEFECTS NOTED. 2 L 7 2 4F RT A56NM 2007021500142 20070215 00142 EA 2007 2 15 A6WA200740018 1 20070110 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 412AW 7582 FOUND RIGHT ANGLE AT FS 484 RBL 27 CRACKED APPROXIMATELY .25 INCHES LONG. MAINTENANCE REMOVED AND REPLACED CLIP IAW CRJ SRM 51-42-06 AND 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007021300138 20070213 00138 NM 2007 2 13 AALA20070073 1 20070113 A 2121 FAN BOEING 737 737823 13844BZ NM CABIN LOOSE A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 927AN 30077 SJO INFLIGHT T2164/13JAN - CABIN PRESSURIZATION LOSS. EMERGENCY DECLARED. LANDED SJO WITHOUT INCIDENT. NO MASKS DEPLO YED. FOUND GASPER FAN AT 23B LOOSE. SECURED GASPER FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007021300144 20070213 00144 EA 2007 2 13 QXEA200700072 1 20070115 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 492 S19R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 492 AND STRINGER 19R. REPAIRED IAW SRM 51-42-06, 51-40-00, AND 51-25-01. 2 L 7 2 4F RT A21EA 2007021300146 20070213 00146 EA 2007 2 13 COMA0760154 1 20070205 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS BINDING A COMA L ABORTED APPROACH J WARNING INDICATION DE DESCENT 1 SO 01 595SW 6904 7297 FLIGHT 5075 - FLAP FAIL MESSAGE ON DESCENT, DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT INBOARD FLAP INBOARD ACTUATOR. 2 L 7 2 4F RT A21EA 2007021300147 20070213 00147 EU 2007 2 13 07FDEA00455 1 20070213 A 5330 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 740FD 559 AFTER REMOVAL OF AN OLD FLUSH DOUBLER BETWEEN C70/71, P45/46 RT, AN OLD CORRODED REWORKED AREA WAS FOUND AT INNER SKIN S HEET. REPAIR WAS PERFORMED IAW SRM 53-10-12, FIG 229 SHEET 1 AND SRM 53-10-14, FIG 201 SHEET 1, APPROVED BY EA 6-5317 -106349. 2 L 7 2 4F RT A35EU 2007021300148 20070213 00148 WP 2007 2 13 IXXA070007O 1 20070208 A 3260 SWITCH DOUG DC8 DC871F 302199D WP MLG CONTAMINATED A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 829BX 91544 1872 45973 DURING TAKEOFF FROM KTOL, THE DOORS NOT LATCHED LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. THE CREW ACCOMPLISHED THE U NSATISFACTORY UP-LATCH PROCEDURE AND THE DOORS NOT LATCHED LIGHT REMAINED ON. THE CREW CONTINUED THE FLIGHT TO KLAX AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE WIRES ON THE LANDING GEAR DOOR WARNING IAW W/D 32-01-00. ALL WIRES RESISTANCE CHECKS WERE GOOD. MAINTENANCE FOUND BOTH SWITCHES HAD RESIDUAL DE-ICE FLUID THAT WAS CLEANED. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF DOOR WARNING SYSTEM SEVERAL TIMES. THE OPERATIONAL CHECK WAS GOOD IAW UAL MM 32-60-02 . THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2007021300150 20070213 00150 EU 2007 2 13 07FDEA00459 1 20070213 A 2697 WIRE HARNESS AIRBUS 300 A300B4622R 3930312 EU FIRE LOOP UNKNOWN A FDEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 662FE 761 REJECTED T/O DUE TO NR 2 ENGINE LOOP B FAULT AT 20KTS. NR 2 LOOP B INOP, VERIFY AND RECORD IN AML/EAML THAT REMAINING L OOP OPERATES NORMALLY PRIOR TO EACH FLIGHT. R & R NR 2 ENG "B" FIRE LOOP UPPER CORE WIRE HARNESS IN REF TO A300-600 AM M 71-52-01-4. 2 L 7 2 4F RT A35EU 2007021300159 20070213 00159 EU 2007 2 13 MALA070025 1 20070208 A 3620 SENSOR SAAB SF340 340B 7860101 EU MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 423XJ 340B423 DURING FLIGHT, THE CREW INFORMED DISPATCH THAT THE LT BLEED LEAK LIGHT ILLUMINATED. THE FLIGHT WAS DIVERTED TO FWA AND LANDED WITHOUT FURTHER INCIDENT. REPLACED SENSING ELEMENT AND ASSOCIATED CLAMPS. REF SAAB AMM CH 36-23-00. REF CONT C ARDS FOR DETAILS. 2 L 7 2 4T RT A52EU 2007021300166 20070213 00166 NE 2007 2 13 Z3S2007F00000 2 20070131 A 7321 FUEL CONTROL CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LT ENGINE MALFUNCTIONED E Z3SA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 13 905LC 5600334 DURING THROTTLE UP ON TAKEOFF, LT ENGINE DID NOT PRODUCE POWER BEYOND IDLE THRUST. ABORTED TAKEOFF QUICKLY AFTER BRAKE RELEASE THEN TAXIED CLEAR OF THE RUNWAY, SHUT THE ENGINE DOWN AND RESTARTED. AT THIS POINT, THE PROBLEM COULD NOT BE DU PLICATED AND NORMAL POWER RUNS WERE ACCOMPLISHED WITH NO FURTHER PROBLEMS. AFTER RETURNING TO HOME BASE WE HAD MAINTENA NCE DO SOME FURTHER TESTING AND THE LT ENGINE IS RESPONDING A LITTLE SLOWER THAN NORMAL. WE HAVE GROUNDED THE AIRCRAFT AND ARE WAITING FOR TESTING TO BE ACCOMPLISHED ON THE FUEL CONTROL UNIT. THE TESTS SHOULD BE FINISHED TODAY AND WE WILL MOVE FORWARD BASED ON THESE CONCLUSIONS. (K) 2 L 7 2 4F 4 F RT A22CE E25EA 2007021300170 20070213 00170 EA 2007 2 13 A6WA200740015 1 20070110 A 5300 601R3111358 NUT CLIP CNDAIR CL600 CL6002B19 1900309 EA FS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 412AW 7582 RIGHT FS 280 FLOOR SUPPORT CLIP P/N 601R31113-58 CRACKED APPROX .3 INCHES LONG INBOARD SIDE RBL 9.0. MAINTENANCE REMOVE D CRACKED ANGLE. FITTED AND INSTALLED NEW ANGLE P/N 601R31113-58 IAW CRJ SRM 51-42-06, 51-42-21, 51-42-13, 51-40-11 AND BSC STANDARD REPAIR 601R-53-0057A. (M) 2 L 7 2 4F RT A21EA 2007021300173 20070213 00173 NM 2007 2 13 AMTA200700056 1 20070204 A 2410 727792J GENERATOR BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE LT UNSERVICEABLE A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 552TZ 17575 17575 32586 ON TAXI OUT LT GENERATOR DRIVE LIGHT ILLUMINATED. REMOVED AND REPLACED LT IDG IAW M57-24-01. SYSTEM CHECKS GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007021300179 20070213 00179 NM 2007 2 13 AWXA200700194 1 20070122 A 5313 6545771573 STRINGER BOEING 737 73733A 1384673 NM BS 500C S16L CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CRACKED STRINGER, BS 500C + 15", S16L. REPAIRED STRINGER, BS 500C + 15", S16L IAW AWA ER 03-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2007021300185 20070213 00185 2007 2 13 UPS07849138 4 20070207 A 2565 GIRT BAR DOUG DC8 DC873F 302199F WP ESCAPE SLIDE STIFF A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:N/A THE EMERGENCY ESCAPE SLIDE GIRT BAR IS VERY DIFFICULT TO ENGAGE & DISENGAGE. REPACKED EMERGENCY ESC APE SLIDE IN ITS CONTAINER. GIRT BAR STOWS OK. 2 L 7 4 4F RT 4A25 2007021300198 20070213 00198 NM 2007 2 13 HNAA0700015 1 20070210 A 5320 85330934 FLOOR SUPPORT DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838EX 29736 29736 220 RIGHT HAND FLOORBOARD SUPPORT ANGLE AT X600.00 IS CORRODED. REPLACED ANGLE. 2 H 7 2 4T RT A13NM 2007021300199 20070213 00199 NM 2007 2 13 HNAA0700023 1 20070211 A 5310 85320019 TENSION TIE DHAV DHC8 DHC8102 2809003 NM BS 387 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838EX 29736 29736 220 FOUND CORROSION AT FRAME STATION X387.35 AND STRINGER 31S. REPLACED TENSION FITTING. 2 H 7 2 4T RT A13NM 2007021400001 20070214 00001 EA 2007 2 14 QXEA200700056 1 20070113 A 5330 RIVET CNDAIR CL600 CL6002C10 1390015 EA BS 469 BURNED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - REPLACE BURNED RIVET LOCATED 11" AFT OF FS 469.6 6" BELOW WL 79.5 RTS. REPAIRED IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007021400004 20070214 00004 EA 2007 2 14 QXEA200700058 1 20070113 A 5330 RIVET CNDAIR CL600 CL6002C10 1390015 EA FUSLEAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - REPLACE BURNED RIVET AT FS 349. 13" BELOW TOP OF MAIN CABIN DOOR, AFT OF MAIN CABIN DOOR FRAME. REPAIRED IAW S RM 51-42-06. 2 L 7 2 4F RT A21EA 2007021400010 20070214 00010 EA 2007 2 14 QXEA200700061 1 20070117 A 5330 RIVET CNDAIR CL600 CL6002C10 1390015 EA FUSLEAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - REPLACE BURNED RIVET AT FS 437 10" BELOW WL 79.5, RHS. REPAIRED IAW SRM 51-42-06, 51-21-16, AND REO670-53-21-2 48. 2 L 7 2 4F RT A21EA 2007021400013 20070214 00013 SO 2007 2 14 RAIA00702008 1 20070206 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 824HK 145498 PRE FLT NR 5526 - STL - EMERGENCY LIGHTS FROM FRONT ROW OF AIRCRAFT TO ROW 8 INOP. MAINTENANCE CHARGED THE EMERGENCY LI GHTS SYSTEM BY RUNNING THE APU. LIGHTS OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007021400014 20070214 00014 SO 2007 2 14 RAIA00702012 1 20070207 A 3260 PROXIMITY SWITCH EMB 145 EMB145 3260210 SO MLG OUT OF ADJUST A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 802HK 145066 FLT NR 3574 - STL - AFTER TAKEOFF, "LG AIR/GND FAIL" MESSAGE APPEARED ON THE EICAS. MAINTENANCE ADJUSTED THE LT AND RT NR 1 PROXIMITY SWITCHES. 2 L 7 2 4F RT T00011AT 2007021400018 20070214 00018 SO 2007 2 14 RAIA00702010 1 20070207 A 3610 O-RING EMB 145 EMB145LR 3260212 SO NR 2 BLEED WORN A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 813HK 145044 FLT NR 5501 - STL - BLEED 2 LEAK INDICATION ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE BLEED LINE O-RINGS. 2 L 7 2 4T RT T00011AT 2007021400020 20070214 00020 SO 2007 2 14 RAIA00702014 1 20070209 A 3397 WIRE EMB 145 EMB145 3260210 SO EMERGENCY LIGHT DAMAGED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 803HK 145077 PRE FLT NR 3542 - STL - EMERGENCY FLOOR STRIP WILL NOT LIGHT. MAINTENANCE RESOLDERED WIRES TO FLOOR STRIP. 2 L 7 2 4F RT T00011AT 2007021400023 20070214 00023 EA 2007 2 14 QXEA200700068 1 20070115 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSLEAGE LIGHTNING STRIKE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 316 AND STRINGER 22R. REPAIRED IAW SRM 51-40-00, 51-42-06, AND 51-25-01. 2 L 7 2 4F RT A21EA 2007021400027 20070214 00027 EA 2007 2 14 QXEA200700063 1 20070117 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FLIGHT COMPARTMENT FLOOR PANEL 221ALF, AFT SUPPORT IS CORRODED ON TOP FLANGE UPPER SURFACE. REPAIRED IAW REF N ON ROUTINE 00164 FOR REPLACEMENT OF FLOOR SUPPORT. 2 L 7 2 4F RT A21EA 2007021400028 20070214 00028 EA 2007 2 14 QXEA200700064 1 20070116 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - VERTICAL WEB IS CORRODED AT STATION 280 FLOORBEAM, LBL12-LBL16 AND LBL30. REPAIRED IAW REO670-53-11-052, AND S RM 51-40-11, 51-40-02. 2 L 7 2 4F RT A21EA 2007021400032 20070214 00032 NM 2007 2 14 PIDA07005 1 20070202 A 5340 STRINGER CLIP BOEING 737 7372K5 138448X NM BS 767 CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 STRINGER TIE CLIP CRACKED AT BS 767 AT STR 6 LT. REPLACED TIE CLIP. 2 L 7 2 4F RT A16WE 2007021400034 20070214 00034 NM 2007 2 14 PIDA07004 1 20070202 A 5340 STRINGER CLIP BOEING 737 7372K5 138448X NM BS 787 CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 STRINGER TIE CLIP CRACKED AT BS 787 AT STR 6LT. REPLACED TIE CLIP. 2 L 7 2 4F RT A16WE 2007021400038 20070214 00038 2007 2 14 NOCA02007 4 20070120 A 3441 HG1050A010 IRU BOEING 767 767324 1385203 NM UNKNOWN A NOCA O OTHER J WARNING INDICATION LD LANDING 1 EA 15 767NA 27569 CTR IRS FAULT EICAS MESSAGE ILLUMINATED UPON LANDING. PERFORMED FIM TASK 34-21-00. REMOVED AND REPLACED CTR IRU AS PER MM 34-21-00, OPS CHECK OK. 2 L 7 2 4F RT A1NM 2007021400043 20070214 00043 NM 2007 2 14 SWAA070678 1 20070208 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM BS 931 S25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 931, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007021400046 20070214 00046 NM 2007 2 14 SWAA070671 1 20070208 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007021400054 20070214 00054 NM 2007 2 14 SWAA070673 1 20070208 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 736SA 27868 DURING SCHEDULED HC1 CHECK, LT OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007021400055 20070214 00055 NM 2007 2 14 SWAA070674 1 20070208 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 736SA 27868 DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM . 2 L 7 2 4F RT A16WE 2007021400058 20070214 00058 NM 2007 2 14 HNAA0700003 1 20070117 A 5320 85300319 ANGLE DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838EX 29736 29736 220 CRACKS FOUND ON REAL CLOSING ANGLE BETWEEN STR 4P AND 5P CRACKED AT FASTENER. REPLACED ANGLE. 2 H 7 2 4T RT A13NM 2007021400061 20070214 00061 NM 2007 2 14 HNAA0700016 1 20070210 A 5315 85330934 FLOORBEAM DHAV DHC8 DHC8102 2809003 NM ZONE 100 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838EX 29736 29736 220 LEFT HAND FLOORBOARD SUPPORT CAP ANGLE AT X600.000 IS CORRODED. 2 H 7 2 4T RT A13NM 2007021400072 20070214 00072 SO 2007 2 14 UG8A2007PA01O 1 20070208 A 2820 1159SCP002005 EJECTOR GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE RT WING ICED E UG8A B EMER. DESCENT F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 23 661GA 4451 561 DURING CRUISE THE CREW REPORTED GETTING AN AMBER FUEL TANK TEMP ILLUM WITH ACTUAL TEMP -4/-5 FOLLOWED BY L-R FUEL LOW L EVEL WITH MORE THAT 9000 LBS REMAINING. AN EMERGENCY LANDING WAS MADE. UPON ACCESSING THE FUEL EJECTOR PUMPS IN BOTH W INGS, ICE WAS FOUND AROUND THE EJECTOR PUMP FUEL INLET. IT WAS DETERMINED THAT THIS ICE WAS RESTRICTING THE FLOW OF FUE L INTO THE PUMP RESULTING IN A LOW LEVEL OF FUEL IN BOTH WING HOPPER TANKS. GAC ASC 135A INSTALLS SCREENS OVER THE EJE CTOR PUMP WHICH HELPS PREVENT THIS PROBLEM. PLACED THE AIRCRAFT IN A HEATED HANGER AND ALLOWED WINGS TO WARM UP AND REM OVED ALL SIGNS OF WATER FROM INSIDE BOTH WINGS. CLOSED THE PANELS USED FOR ACCESS AND FUELED AIRCRAFT. OPERATED THE EJ 2 L 7 2 4F 4 F RT A12EA E00057EN 2007021400077 20070214 00077 NM 2007 2 14 HNAA0700013 1 20070210 A 5340 85330220 FITTING DHAV DHC8 DHC8102 2809003 NM BS 531-545 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838EX 29736 29736 220 CORROSION ON TENSION FITTING. REPLACED TENSION FITTING. 2 H 7 2 4T RT A13NM 2007021400078 20070214 00078 NM 2007 2 14 HNAA0700014 1 20070210 A 5320 85323116001 MOUNT DHAV DHC8 DHC8102 2809003 NM ANTENNA CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838EX 29736 29736 29736 CORROSION ON ANTENNA MOUNTING BOX. REMOVED AND REPLACED MOUNTING BOX. 2 H 7 2 4T RT A13NM 2007021400079 20070214 00079 NM 2007 2 14 HNAA0700019 1 20070211 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838EX 29736 29736 220 LEFT HAND INBOARD AFT SEAT RAIL HAS CORROSION AT SEAT LEG LOCATIONS. REPLACED SEAT RAILS. 2 H 7 2 4T RT A13NM 2007021400081 20070214 00081 NM 2007 2 14 HNAA0700027 1 20070211 A 5330 85330022011 SKIN PANEL DHAV DHC8 DHC8102 2809003 NM BS 424-488 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 838EX 29736 29736 220 FOUND CORROSION BETWEEN FRAME STATION 424.124 AND 434.50 JUST OUTBOARD OF STR 31S ON SKIN PANEL. 2 H 7 2 4T RT A13NM 2007021400082 20070214 00082 EA 2007 2 14 HNAA0700032 1 20070211 A 5330 85332750 SKIN PANEL DHAV DHC8 DHC8311 1386006 EA BS 445-467 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 335EN 29195 29195 220 UPON REMOVAL OF THE NR 2 DME ANTENNA CORROSION WAS FOUND ON THE SKIN PANEL UNDER THE ANTENNA. CORROSION WAS LOCATED AT THE AIRCRAFT CENTER LINE BETWEEN X445 AND 467. REPAIRED PER ENGINEERING ORDER. 2 H 7 2 4T RT A13NM 2007021400111 20070214 00111 WP 2007 2 14 AALA20070191 1 20070126 A 3350 AML8095100GPL BULB DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 965TW 53615 LGA - EMERGENCY SEAT MOUNTED LIGHT AT SEAT ROW 11 INOPERATIVE. RELAMPED EMERGENCY SEAT MOUNTED LIGHT AT SEAT ROW 11. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007021400112 20070214 00112 WP 2007 2 14 AALA20070192 1 20070126 A 3350 AML8095100GPL BULB DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 965TW 53615 LGA - FOUND EMERGENCY SEAT MOUNTED LIGHT AT SEAT ROW 17 INOPERATIVE. RELAMPED EMERGENCY SEAT MOUNTED LIGHT AT SEAT ROW 17. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007021400113 20070214 00113 WP 2007 2 14 AALA20070193 1 20070126 A 3350 AML8095100GPL BULB DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 965TW 53615 LGA - EMERGENCY SEAT MOUNTED LIGHT AT SEAT ROW 21 INOPERATIVE. RELAMPED EMERGENCY SEAT MOUNTED LIGHT AT SEAT ROW 21. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007021400114 20070214 00114 WP 2007 2 14 AALA20070188 1 20070126 A 2131 CONTROLLER DOUG DC9 DC983 3022083 WP CABIN PRESSURE INOPERATIVE A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 572AA 49458 STL INFLIGHT T335/26JAN ORD TO SAT. UNABLE TO MAINTAIN PRESSURIZATION MANUALLY. BOTH PRESSURIZATION AUTO CONTROLLERS WERE INOPERATIVE. ALL OXYGEN MASKS DROPPED. LANDED STL WITHOUT INCIDENT. REPLACED NUMBER ONE AND TWO CABIN PRESSURE C ONTROLLERS AND OUTFLOW VALVE ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007021400115 20070214 00115 WP 2007 2 14 AALA20070194 1 20070126 A 3350 AML8095100GPL BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 561AA 53091 LAX - EMERGENCY SEAT MOUNTED LIGHT AT SEAT ROW 10 BROKEN. RELAMPED EMERGENCY SEAT MOUNTED LIGHT AT SEAT ROW 10. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007021400116 20070214 00116 EA 2007 2 14 SIMA200704401 1 20070207 A 5610 601R3303318 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE FLIGHT DECK CRACKED A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 511AE 9453 10107 FO'S WINDSHIELD CRACKED, DIVERTED. REMOVED AND REPLACED WINDSHIELD IAW AMM 56-10-05. PERFORMED PRESSURIZATION CHECKS WI TH NO DEFECTS, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007021400117 20070214 00117 SO 2007 2 14 SIMA200704403 1 20070207 A 5350 CLAMP EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL RADOME OUT OF ADJUST A SIMA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SW 21 652RS 145432 NOSE VIBRIBATION IN FLIGHT. READJUSTED RADOME ATTACHMENT CLAMPS, PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS NOT ED, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007021400118 20070214 00118 2007 2 14 SIMA200704404 2 20070207 A 7261 23073567 CARBON SEAL EMB 145 EMB145LR 3260212 SO ENGINE FAILED A SIMA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 941LT 4184 14500926 LAVATORY SMOKE MESSAGE WITH A BLUE HAZE IN THE CABIN ON CLIMB-OUT, DECLARED EMERGENCY, RETURNED TO ORD. REMOVED AND REP LACED ZERO CARBON SEAL NUMBER 2. 2 L 7 2 4T RT T00011AT 2007021400119 20070214 00119 SO 2007 2 14 SIMA200704402 1 20070207 A 4940 23080013A STARTER HAMSTD EMB 145 EMB145LR 3260212 SO APU SEIZED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 665BC 5123 88 SPE0314621 145783 ACID SMELL IN CABIN AND FLIGHT DECK FOLLOWED BY INTERMITTENT APU GENERATOR OFF BUSS MESSAGE ON EICAS. COULD NOT DUPLICA TE SMELL IN CABIN OR FLIGHT DECK. PERFORMED ELECTRICAL SYSTEM INSPECTION ON WINDSHIELD CONTROLLER TERMINALS WITH NO DEF ECTS. FOUND APU STARTER GENERATOR SEIZED. REMOVED AND REPLACED APU STARTER GENERATOR IAW AMERICAN EAGLE WORK CARD 24-8 00-01. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007021400120 20070214 00120 GL 2007 2 14 SIMA200704406 2 20070208 A 7261 AE3007A1 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 LEAKING A SIMA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 696AE 13775 3129 14500874 CAE311444 LAVATORY SMOKE WARNING AFTER TAKEOFF. REMOVED AND REPLACED NUMBER TWO ENGINE IAW EMB AMM 72-00-00. PERFORMED OPERATION AL CHECKS WITH NO DEFECTS, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007021400121 20070214 00121 SO 2007 2 14 SIMA200704414 1 20070209 A 5311 12010732001 FRAME EMB 135 EMB135KL 3260302 SO FUSELAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 803AE 13064 4800 145483 FOUND LOWER SECTION OF FRAME 81 GOUGED. PERFORM BLEND AND NDT INSPECTION OF GOUGE. FABRICATED INTERNAL AND EXTERNAL RE PAIR DOUBLERS. INSTALLED DOUBLERS IAW EMB SRM 53-32-04 AND C2007-145/00878. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007021400122 20070214 00122 SO 2007 2 14 SIMA200704405 1 20070208 A 3620 UNKNOWN EMB 135 EMB135KL 3260302 SO BLEED SYSTEM UNKNOWN A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 857AE 145752 BLEED ONE LEAK WARNING MESSAGE, DECLARED AN EMERGENCY. RETURNED TO MIA. PERFORMED ENGINE RUNS IAW FAULT ISOLATION TASK 36-20-00-810-801-A WITH NO LEAKS NOTED OR FAULTS NOTED. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007021400123 20070214 00123 EU 2007 2 14 SIMA200704408 1 20070210 A 7810 UNKNOWN SAAB SF340 340B 7860101 EU TAIL PIPE UNKNOWN A SIMA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 286AE 340B286 LEFT TAIL PIPE LIGHT WOULD NOT ILLUMINATE DURING TEST. PERFORMED OPERATIONAL CHECK OF FIRE TEST SYSTEM WITH NO DEFECT N OTED IAW SAAB AMM 33-10-00. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007021400124 20070214 00124 SO 2007 2 14 SIMA200704409 1 20070211 A 3350 WIRE EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 707EB 145195 FOUND EMERGENCY LIGHTS STAY ON ALL THE TIME. REPAIRED BROKEN GROUND WIRE AT GS8008 IAW EMB AMM 20-13-21. OPERATIONAL C HECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007021400125 20070214 00125 SO 2007 2 14 SIMA200704407 1 20070209 A 3040 NP15731111 WINDSHIELD EMB 135 EMB135KL 3260302 SO FLIGHT DECK FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 850AE 9277 145722 STRONG ELECTRICAL SMELL IN CABIN AND FLIGHT DECK, NUMBER ONE WINDSHIELD HEAT DE-ICE LIGHT CAME ON. REMOVED AND REPLACED CAPTAINS WINDSHIELD IAW EMB 56-10-01. PERFORMED PRESSURIZATION CHECKS WITH NO DEFECTS, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007021400126 20070214 00126 SO 2007 2 14 SIMA200704412 1 20070209 A 5320 14522178005 SILL EMB 135 EMB135LR 3260305 SO DOOR FRAME CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 735TS 13412 4800 145386 FOUND SERVICE DOOR FRAME LOWER SILL FOUND CORRODED. REMOVED EXISTING SILL. CLEANED AND TREATED REPAIR AREA. INSTALLED NEW SILL IAW EMB SRM 51-40-02. RESTORE PROTECTIVE FINISH, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007021500005 20070215 00005 SO 2007 2 15 C2XA07BT014 1 20070206 A 2611 47357913 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CARGO BAY MALFUNCTIONED A C2XA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 27 15574 10498 145639 EWR M602 SQUAWK FLT NR 2882 BAGGAGE FIRE BOTTLES BLOWN IN FLIGHT. BAG SMOKE WARNING. REMOVED AND REPLACED THE AFT BAGG ABE SMOKE DETECTOR IAW AMM 26-15-01. OPS CHECK GOOD, CLOSED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007021500006 20070215 00006 EA 2007 2 15 QXEA200700090 1 20070117 A 5340 ATTACH FITTING CNDAIR CL600 CL6002C10 1390015 EA SEAT TRACK CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND RIGHT INBOARD CABIN SEAT RAIL ATTACH FITTING TO FS 280 BEAM IS CRACKED. REPAIRED IAW SRM 51-42-00, 51-40 -11. 2 L 7 2 4F RT A21EA 2007021500010 20070215 00010 EA 2007 2 15 QXEA200700094 1 20070116 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND VERTICAL WEB IS CORRODED AT FS 280 BEAM RBL 14 JUST ABOVE CABIN FLOOR LEVEL. REPAIRED IAW SRM 51-40-11, REO670-53-11-052. 2 L 7 2 4F RT A21EA 2007021500013 20070215 00013 WP 2007 2 15 AALA20070198 1 20070127 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7508 49802 LGA - EMERGENCY LIGHTS BETWEEN SEAT ROWS 18 TO 20 INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS BETWEEN SEAT ROWS 18 T 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007021500023 20070215 00023 EU 2007 2 15 AALA20070212 1 20070128 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 MIA - EMERGENCY LIGHT AT SEAT 20G INOPERATIVE. REPLACED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 20G. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007021500039 20070215 00039 EA 2007 2 15 QXEA200700089 1 20070115 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 960 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND LEFT SIDE UPPER SEAT RAIL GOUGED AT FS 960.00. REPAIRED IAW REO670-53-00-013. 2 L 7 2 4F RT A21EA 2007021500041 20070215 00041 EA 2007 2 15 QXEA200700081 1 20070115 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 565 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 565 AND BETWEEN STRINGER 23R AND STR INGER 24R. REPAIRED IAW SRM 51-42-06, 53-00-01, 51-25-01, AND 51-21-11. 2 L 7 2 4F RT A21EA 2007021500042 20070215 00042 EA 2007 2 15 QXEA200700083 1 20070115 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 942 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 942 AND STRINGER 17R. REPAIRE D IAW SRM 51-42-06, 53-00-01, 51-21-11, AND 51-25-01. 2 L 7 2 4F RT A21EA 2007021500058 20070215 00058 EA 2007 2 15 QXEA200700098 1 20070117 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - LIGHT FRETTING CORROSION ON FUSELAGE SKIN AT MOUNTING SURFACE FOR NR 2 VHF ANTENNA. REPAIRED IAW SRM 51-21-11 AND 51-21-01. 2 L 7 2 4F RT A21EA 2007021500059 20070215 00059 EA 2007 2 15 QXEA200700101 1 20070118 A 5242 SKIN CNDAIR CL600 CL6002C10 1390015 EA E/E BAY DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND MAIN AVIONICS COMPARTMENT DOOR CUTOUT INTERNAL LOWER SKIN HAS LIGHT SURFACE CORROSION AROUND SKIN TO DOOR CONTACTING SURFACE. REPAIRED IAW SRM 51-21-06, 53-21-01, REO670-53-21-250, AND SRM 51-25-01. 2 L 7 2 4F RT A21EA 2007021500067 20070215 00067 EU 2007 2 15 2007UALA00296 1 20070202 A 3350 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 491UA 1741 AFT EMERGENCY LIGHT BATTERY FAILED 3SVC TEST. REPLACED AFT EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD 2 L 7 2 4F 4 F RT A28NM E40NE 2007021500079 20070215 00079 NM 2007 2 15 2007UALA00308 1 20070204 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 643UA 25093 FOUND TWO EXTERIOR EMERGENCY EXIT LIGHTS OUT ON LEFT. TROUBLESHOT AND REPLACED BATTERY PACKS AT M736 AND M738. OPS CHEC K GOOD 2 L 7 2 4F 4 F RT A1NM E24NE 2007021500081 20070215 00081 NM 2007 2 15 2007UALA00310 1 20070203 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 644UA 25094 FOUND EMERGENCY EXIT LIGHTS CAME ON ONCE IN FLIGHT IN LEFT REAR OF CABIN. REPLACED BATTERY PACK AT POWER SUPPLY M739. EEL OPS CK OK 2 L 7 2 4F 4 F RT A1NM E24NE 2007021500085 20070215 00085 NM 2007 2 15 2007UALA00314 1 20070204 A 3350 BATTERY BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 787UA 26939 FOUND SEAT MOUNTED EMERGENCY LIGHT AT ZONE B FWD STAY ON. REPLACED BATTERY & TESTED OK PER MM 33-51-00. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007021500094 20070215 00094 CE 2007 2 15 020907N300CS1 1 20070209 A 3260 INDICATION SYS CESSNA 500 550 2076604 CE PWA 530 PW530A NE MLG MALFUNCTIONED E Z5FA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 NE 03 300CS 5500818 ON FINAL APPROACH, WHEN LANDING GEAR WAS EXTENDED, THE LT MAIN GEAR GREEN DOWN LIGHT FAILED TO ILLUMINATE. CREW ABORTED APPROACH AND CLIMBED TO SAFE ALTITUDE TO ADDRESS SITUATION. AN EMERGENCY WAS DECLARED, CREW FOLLOWED AFM EMERGENCY PROCE DURES AND BLEW GEAR DOWN. AIRCRAFT LANDED WITHOUT INCIDENT. AFTER LANDING ROLL OUT AIRCRAFT WAS TOWED TO FBO. THE AIRCRA FT IS PRESENTLY IN MAINTENANCE. 1 L 7 2 4F 4 F A22CE E00053EN 2007021500095 20070215 00095 NE 2007 2 15 2007UALA00321 2 20070205 A 7200 ENGINE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 1 OVERHEATED A UALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 WP 29 836UA 1460 V10784 RTFL DUE TO NR 1 ENGINE OVERHEAT. [SUP 05-08-07] REPLACED HIGH PRESSURE BLEED VALVE ON NR 1 ENGINE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007021500096 20070215 00096 NM 2007 2 15 2007UALA00322 1 20070206 A 3350 BATTERY PACK BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 903UA 25003 FOUND EMERGENCY LIGHTS INOP IN FOLLOWING LOCATIONS: ROWS 1-2 EEL LTS, EXIT SIGN ABOVE DOOR 1R, SLIDE LT FOR DOOR 1L, AND EXIT SIGN ABOVE ENTRANCE TO FLT DECK. REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007021500098 20070215 00098 NM 2007 2 15 2007UALA00324 1 20070205 A 2120 UNKNOWN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 127UA 28813 FLT ATTENDANT REPORTED ELECTRICAL ODOR IN CABIN WITH SOME HAZE. ODOR & HAZE IN CABIN AT ROWS 22-44. SWITCHED OFF ALL RE -CIRC FANS AND ODOR DISSIPATED. OPS CHECKED NORMAL, COULD NOT DUPLICATE ON GROUND, OK FOR CONTINUE IN SERVICE 2 L 7 4 4F 4 F RT A20WE E24NE 2007021500100 20070215 00100 NM 2007 2 15 2007UALA00326 1 20070206 A 3350 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE C ZONE AT LAV 11 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 FOUND EEL INOP, C ZONE AT LAV 110 SIDEWALL. FOUND EEL STRIP BROKEN. REPLACED EEL STRIP, OP CHECKED OK 2 L 7 4 4F 4 F RT A20WE E24NE 2007021500103 20070215 00103 WP 2007 2 15 I5HA0658016 1 20070207 A 5754 900623401 SKIN CVAC 340 340CVAC 242270A WP LT WING LE DAMAGED A I5HA B EMER. DESCENT E VIBRATION/BUFFET AP APPROACH 1 GL 23 584E 24 ON APPROACH, THE CREW FELT A VIBRATION AND A SEVERE PULL TO THE LT. THEY DECLARED AND EMERGENCY. AFTER LANDING AND GOIN G TO THE PARKING SPOT, THE CREW DETERMINED THAT THEY HAD A BIRD STRIKE ON THE LT IB WING (LEADING EDGE). MAINTENANCE WA S CALLED AND THEY MADE A COMPLETE INSPECTION OF THE AIRCRAFT. NO OTHER DAMAGE WAS NOTED. MAINTENANCE REMOVED AND REPLA CED THE LT LEADING EDGE AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4R 6A6 2007021500109 20070215 00109 NM 2007 2 15 USAA070095 1 20070213 A 5320 WEB BOEING 737 737301 1384611 NM BS 351-360 S16L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 FOUND WEB CRACKED, BS 351-360 S-16L. FAB'S PARTS PER SRM 53-10-04, DEFECT SIZE: .250". 2 L 7 2 4F RT A16WE 2007021500116 20070215 00116 NM 2007 2 15 SWAA070718 1 20070210 A 5311 6517684 FRAME BOEING 737 7373H4 1384600 NM BS 303 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 16L. REPAIRED FRAME PER ER AND SB. 2 L 7 2 4F RT A16WE 2007021500118 20070215 00118 NM 2007 2 15 SWAA070716 1 20070210 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 500B S26R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 26R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007021500126 20070215 00126 EA 2007 2 15 QXEA200700073 1 20070116 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 449 S24R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 499 AND STRINGER 24R. REPAIRE D IAW SRM 53-00-01, 51-40-00, AND 51-25-01. 2 L 7 2 4F RT A21EA 2007021500131 20070215 00131 EA 2007 2 15 QXEA200700078 1 20070115 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 956 S17R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD ON RIGHT SIDE OF FUSELAGE AT FS 956 AND STRINGER 17R. REPAIRE D IAW SRM 53-00-01, 51-42-06, 53-51-03, AND 51-25-01. 2 L 7 2 4F RT A21EA 2007021500133 20070215 00133 EU 2007 2 15 MALA070027 1 20070212 A 3610 HOSE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE BLEED AIR RUPTURED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 448XJ 340B448 RT BLEED AIR LEAK LIGHT CAUTION LIGHT ILLUMINATED DURING FLIGHT AT APPROXIMATELY 10,000, FT RAN THE QRH. CAUTION LIGHT WHEN OUT INITIALLY THEN CAME ON INTERMITTENTLY WITH BLEED AIR AND HP VALVES CLOSED, THIS CONTINUED UNTIL DESCENT, WHEN P OWER WAS AT A LOW SETTING. AIR RETURNED, FOUND BLEED AIR HOSE (ORANGE) AT RT FUSELAGE RUPTURED. REMOVED AND REPLACED F USELAGE BLEED AIR HOSE. PN ON AND OFF 9303688-100 IAW CHAP 36 OPS CHECK IS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2007021500136 20070215 00136 NM 2007 2 15 QXEA200700155 1 20070211 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM AFT PAX STUCK A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 414QX 4061 SEA FLIGHT NR 2414: AFT PASSSENGER DOOR WON'T OPEN. MAINTENANCE UNSTUCK AFT PASSENGER DOOR. PERFORMED OPERATIONAL CHEC K IAW AMM 52-12-00-710-801. NO DEFECTS NOTED. PERFORMED GVI ON DOOR STOPS AND ROLLERS. NO DEFECTS NOTED. NO PARTS RE PLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007021500153 20070215 00153 NM 2007 2 15 DL76S070117 1 20070211 A 5320 146T005126 SILL BOEING 767 767332 1382001 NM R2 DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 FOUND R2 DOORWAY LWR SILL, FLOOR SUPPORT TEE (REF P/N 146T0051-26) VERTICAL FLANGE EXFOLIATED BETWEEN MIDDLE AND AFT SEC TION. REPLACED FLOOR SUPPORT TEE PER SRM 51-40-02 PG 1. 2 L 7 2 4F RT A1NM 2007021500154 20070215 00154 NM 2007 2 15 DL76S070118 1 20070211 A 5320 FLOOR SUPPORT BOEING 767 767332 1382001 NM BS 785-977 WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 FOUND STA 785.9 TO STA 977, RBL 34, FLOORBEAM UPPER CHORD SCREW HOLES WORN BY CLIPNUTS. BLENDED DAMAGE PER SRM 53-00-04 , FIG 101. TREATED AND PAINTED. LOCATION AT STA 941 REPAIRED PER SRM 53-50-51, FIG 201, REPAIR 4. 2 L 7 2 4F RT A1NM 2007021500155 20070215 00155 NM 2007 2 15 DL76S070119 1 20070211 A 5315 FLOORBEAM BOEING 767 767332 1382001 NM BS 698 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 FOUND CORROSION ON FWD CARGO FLOORBEAM UPPER SURFACE AT STA 698, LBL 19. REPLACED UPPER CHORD SECTION PER SRM 51-40-02, PG 1. 2 L 7 2 4F RT A1NM 2007021500156 20070215 00156 NM 2007 2 15 DL76S070120 1 20070211 A 5315 143T10605 FLOORBEAM BOEING 767 767332 1382001 NM BS 632 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 FOUND CORROSION ON FWD CARGO FLOORBEAM UPPER CHORD AT STA 632, LBL 18. REPLACED CHORD SECTION 142T1060-5 PER DWG 143T12 09 AND SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007021500157 20070215 00157 NM 2007 2 15 DL76S070122 1 20070209 A 2550 WIRE BOEING 767 767332 1382001 NM CARGO LOADING SY SHORTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 FOUND C2 BAG BIN LOADING SYS INOP, 5 BREAKERS BLOWN. SUSPECT SHORT UNDER BAG BIN FLOOR. FOUND WIRE HARNESS MELTED BETW EEN 6L AND 6R PDU STA 1230. REPAIRED 10 EACH TRIPLE WIRE PDU POWER WIRES AND 9 EACH SINGLE PDU CONTROL WIRES UNDER 6L P DU PER BSWPM CHPT 20. AFT CARGO LOADING SYS OPS CK NORMAL. REMOVED MCO AND PLAC. 2 L 7 2 4F RT A1NM 2007021500158 20070215 00158 CE 2007 2 15 148J020807 1 20070208 A 2420 45AS888019 GCU MTSBSI MU300 MU300 5780602 CE PWA JT15 JT15D4 52112 NE RT ENGINE SHORTED E UVCA O OTHER H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 CE 03 148J 5740 A033SA RT ENGINE WOULD NOT START. STARTER WOULD NOT ROTATE ENGINE AND TRIP CIRCUIT BREAKER. FOUND GCU BAD. 2 H 7 2 4F 4 F RT A14SW E1NE 2007021500159 20070215 00159 EA 2007 2 15 A6WA200740019 1 20070110 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 412AW 7582 RIGHT INTERCOSTAL AT FS 484 RBL 36 CRACKED APPROXIMATELY .3 INCHES LONG MAINTENANCE CUT AWAY DAMAGED SECTION OF INTERCOS TAL FLANGE, PERFORMED EDDY CURRENT, FABRICATED REPAIR PARTS AND INSTALLED IAW BOMBARDIER REO 601R-53-41-059 REV A AND BS C STANDARD REPAIR 601R-53-0030A. (M) 2 L 7 2 4F RT A21EA 2007021500161 20070215 00161 EA 2007 2 15 A6WA200740012 1 20070109 A 5320 601R75262159 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 412AW 7582 HYDRAULIC TRANSDUCER HOT CHANNEL IN LEFT MLG BAY CEILING CRACKED APPROXIMATELY .2 INCHES LONG, BRACKET P/N 601R75262-159 . MAINTENANCE DRILLED OFF REMOVED CRACKED BRACKET, DRILLED UP AND INSTALLED NEW BRACKET P/N 601R75262-159 WET USING PR1 422B SEALANT AND MS 20470AD5-6 SOLID RIVETS, PRIME, PAINTED DINOTROLED REPAIR AREA IAW CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007021500162 20070215 00162 EA 2007 2 15 A6WA200740021 1 20070110 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 412AW 7582 FOUND LEFT ANGLE AT FS 484 LBL 27 CRACKED APPROXIMATELY .2 INCHES LONG. MAINTENANCE REMOVED AND REPLACED CLIP IAW CRJ S RM 51-42-06, 51-40-11 AND 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007021500163 20070215 00163 EU 2007 2 15 MALA070026 1 20070209 A 3620 SENSOR SAAB SF340 340B 7860101 EU MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 448XJ 340B448 ON CLIMB-OUT FROM MEM, THE RIGHT BLEED AIR LEAK ILLUMINATED WITH THE LP AND HP VALVES CLOSED. THE CREW FOLLOWED THE QRH AND THE BLEED AIR CAUTION LIGHT REMAINED ON. PULLED POWER BACK TO 50 PERCENT AND THE LIGHT EXTINGUISHED. THE FLIGHT R ETURNED TO MEM AND LANDED WITHOUT FURTHER INCIDENT. REPLACED FUSELAGE LOWER SENSOR LOOP P/N 51533-377 IAW AMM 35-23-10- 02 AND RAN AT HIGH POWER SETTINGS TO VERIFY FIX. BLEED LEAK LIGHT DID NOT ILLUMINATE. OPS CHECK OF SENSOR LOOK GOOD IA W AMM 36-23-00. DISC 1: SUSPECT WEU AT FAULT. SLAVED IN SERVICEABLE WEU. OPS CHECK NO GOOD. RE-INSTALLED ORIGINAL P ART. INSPECTED SENSOR LOOPS ON WING AND FUSELAGE. FOUND RIGHT FUSELAGE 54: SENSOR LOOP CHAFFED. REPLACED RIGHT FUSELA 2 L 7 2 4T RT A52EU 2007021500164 20070215 00164 EA 2007 2 15 A6WA200740027 1 20070110 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 412AW 7582 FOUND LEFT FS 280 FLOOR SUPPORT CLIP P/N 601R31113-57 CRACKED APPROX .2 INCH LONG INBOARD SIDE LBL 9.0. MAINTENANCE REM OVED AND CRACKED ANGLE, FITTED AND INSTALLED NEW ANGLE P/N 601R31113-57 IAW CRJ SRM 51-42-06, 51-42-21, 51-42-13, 51-40- 11 AND BSC STANDARD REPAIR 601R-53-0057A. (M) 2 L 7 2 4F RT A21EA 2007021500165 20070215 00165 EA 2007 2 15 A6WA200740028 1 20070111 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 202 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 412AW 7582 FOUND LEFT SIDE FORWARD FACE OF FORWARD PRESSURE BULKHEAD FS 202.75 CRACKED APPROX .2 INCH LONG AT HYDRAULIC SYSTEM NR 3 RT INBOARD BRAKE FITTING. MAINTENANCE REPAIRED CRACKED AREA IAW BOMBARDIER SERVICES CORP EO 601R-53-10650. (M) 2 L 7 2 4F RT A21EA 2007021500167 20070215 00167 EU 2007 2 15 200702121 1 20070208 A 2710 AILERON EMB ERJ170 ERJ170100SE 3260406 EU FROZEN A UHLA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 17 631R 17000007 FLIGHT 7549 IAD TO ROC DURING CRUISE THE AUTOPILOT DISCONNECTED. THE CREW BEGAN TO HAND FLY THE A/C AND FOUND THE AILER ONS FROZEN. WITHIN 2-3 SECONDS THE CONTROLS MOVED FREELY AGAIN, WITH SLIGHTLY -HEAVY- FEEL. THIS REOCCURRED ON TWO OTH ER OCCASIONS DURING THE FLIGHT. THE CREW LANDED WITHOUT INCIDENT. CONTRACT MAINTENANCE REMOVED THE FORWARD CARGO COMPA RTMENT FLOOR AND ICE WAS FOUND SURROUNDING THE CONTROL CABLES FOR THE AILERONS. MAINTENANCE USED HEATED AIR TO MELT ICE AND CLEARED THE FUSELAGE DRAINS. AFTER THE ICE HAD MELTED AND WATER DRAINED FROM THE A/C, THE CONTROLS MOVED FREELY. 2 L 7 2 4F RT A56NM 2007021500168 20070215 00168 EU 2007 2 15 R61A20070002 1 20070126 A 2780 UNKNOWN EMB ERJ170 ERJ170100 EU GE CF34 CF348E5 30015 NE SLATS UNKNOWN A R61A O OTHER J WARNING INDICATION DE DESCENT 1 GL 11 809MD 17000022 DURING A/C DECENT SETTING UP FOR APPROACH CREW REPORTED A SLAT FAIL MESSAGE ON EICAS. CREW DECLARED AN EMERGENCY AND LAN DED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE A/C. MAINTENANCE CLEARED SF-ACE INHIBITS, SYSTEM OPERATIONAL CH ECK GOOD AND A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A56NM E00063EN 2007021500170 20070215 00170 EA 2007 2 15 COMA0760159 1 20070205 A 2750 1104SD100201 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS BENT A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 436CA 7482 FLIGHT 5294 - FLAP FAIL ON DESCENT. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED LEFT WING NR 2 FLEX DRIVE . NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007021500171 20070215 00171 2007 2 15 2007UALA00231 4 20070127 A 2565 HOSE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE ESCAPE SLIDE CRUSHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 30024 RIGHT OVERWING ESCAPE SLIDE UPPER PRESSURE HOSE FOUND COLLAPSED INSIDE PANEL 196ER. HOSE REPLACED AND NEW 8130-3 ISSUED . SAME SLIDE REINSTALLED. OK FOR RETURN TO SERVICE. SUSPECT PANEL INSTALLATION CRUSHED HOSE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007021500172 20070215 00172 NM 2007 2 15 2007UALA00232 1 20070127 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 30024 SEAT EEL CONNECTOR AT SEATS 25ABC & 26ABC ARE BROKEN. REPAIRED SEAL EEL CONNECTOR AT BOTH SEAT LOCATIONS; 25ABC & 26 AB C. OPS CHECKS NORMALLY. RETURN TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007021500173 20070215 00173 NM 2007 2 15 2007UALA00233 1 20070127 A 3397 JUMPER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 30024 EEL JUMPER AT SEAT 20AB HAS BROKEN CONNECTOR. REPAIRED EEL JUMPER AT SEAT 20AB. OPS CHECKS NORMALLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007021500174 20070215 00174 NM 2007 2 15 2007UALA00234 1 20070127 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 30024 EMERGENCY LIGHT FOR LEFT FWD DOOR, 1L, LIGHT L388 INOP. FOUND BATTERY PACK HAD LOW CAPACITY. REPLACED BATTERY PACK. OPS CHECKS OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007021500175 20070215 00175 NM 2007 2 15 2007UALA00235 1 20070127 A 3397 TERMINAL BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 EMERGENCY ESCAPE PATH LIGHTS INOP AT SEATS 38H AND 39H. RESEATED TERMINAL ON SEAT 38H. OPS CHECKS NORMALLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007021500176 20070215 00176 NM 2007 2 15 2007UALA00236 1 20070128 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SEATS 16 & 17HJ INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 30024 SEATS 16 AND 17HJ, IN-SEAT EEL INOP. REMOVED AND REPLACED EEL STRIP AT SEATS 16HJ AND 17HJ PER MM 33-51-10 AND OPS CHE CK GOOD FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007021500178 20070215 00178 NM 2007 2 15 2007UALA00238 1 20070127 A 2611 RELAY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE AFT CARGO SMOKE FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 DURING THE AFT BLOWER CHECK C, -AFT DET FAN- MESSAGE DOES NOT SHOW ON EICAS. NR 2 FAN DOES NOT START UP AND -CARGO DET AIR- MESSAGE STAYS. FOUND BAD RELAY K334 AFT CARGO SMOKE DET BLOWER TDC RELAY. REPLACED PER B767 WDM 26-16-21. OPS CH ECKS NORMAL. SUSPECT RELAY DAMAGED BY REPEATED CYCLING. 2 L 7 2 4F 4 F RT A1NM E24NE 2007021500179 20070215 00179 NM 2007 2 15 2007UALA00239 1 20070128 A 3510 TRANSDUCER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CREW O2 FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 O2 PANEL INDICATOR READS 1550 WHEN O2 BOTTLE IS FULL, ALSO COCKPIT GAUGE READS 1550. SERVICED CREW BOTTLE TO FULL MID- RANGE RED ON BOTTLE, AND O2 QTY ON CREW SERVICE PANEL OR EICAS WILL NOT READ OVER 1700PSI. QTY READING ABOUT 200PSI LOW. REMOVED AND REPLACED CREW O2 PRESSURE TRANSDUCER WHICH FAILED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007021500180 20070215 00180 NM 2007 2 15 2007UALA00240 1 20070129 A 5420 WEB BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 2 NACELLE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 217UA 30550 NR 2 NACELLE AFT FAIRING LWR WEB HAS HEAT DAMAGE OF 44 PERCENT IACS AT AREA NR 3 & 4. REMOVED DAMAGED WEB BACK TO SECT ION 5 AND INSTALLED NEW IAW SRM 51-70-13 REPAIR 4. READY FOR SERVICE. SUSPECT PREVIOUS HEAT RELEASE INTO FAIRING DUE TO LEAKAGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007021500181 20070215 00181 EU 2007 2 15 2007UALA00241 1 20070129 A 2910 HYDRAULIC SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FAILED A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 405UA 452 YELLOW HYDRAULIC SYSTEM FAILURE. ECAM CAUTION MESSAGE - Y SYS LO PR MESSAGE INOP - HYD. CREW COMMENTS: YELLOW HYDRAULI C SYSTEM LOW QTY WARNING ECAM. FOUND ENGINE 2 HYDRAULIC FLEX HOSE, JUST ABOVE PRESSURE SWITCH, ON LEFT SIDE APROX 3 O'C LOCK POSITION LEAKING. REPLACED LINE AND ACCOMPLISHED ENGINE RUN LEAK CHECKS. HYDRAULIC RESERVISED TO FULL AS NECESSAR Y. OPS AND LEAK CHECKS GOOD. AS PRECAUTIONARY ACCOMPLISHED HYDRAULIC YELLOW SYSTEM CHECKS AND PUMP OPS CHECK AS REQUIR ED FOR POSSIBLE CAVITATION. ALL CHECKS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007021500182 20070215 00182 NM 2007 2 15 2007UALA00242 1 20070127 A 5610 WINDOW AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT OVERHEATED A UALA O OTHER M J OVER TEMP WARNING INDICATION CR CRUISE 1 WP 29 835UA 1426 CAPTS SLIDING WINDOW OVERHEATED TO POINT OF DISTORTING WINDOW AND BUBBLING WITHOUT ANY OVERHEAT MESSAGE OR INDICATION TO CREW, SUSPECT PROBLEM WITH WINDOW HEAT SYSTEM. REPLACED CAPTAINS SLIDING WINDOW. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007021500183 20070215 00183 NE 2007 2 15 2007UALA00243 2 20070128 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 SPARKS A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 470UA 1427 V10077 NR 2 ENG NO ROTATION, WITH SPARKS REPORTED COMING FROM BOTTOM OF COWLING. REPLACED STARTER AND START VALVE. OPS CHECKE D OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007021500184 20070215 00184 EU 2007 2 15 2007UALA00244 1 20070128 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS CUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 410UA 463 EMERGENCY LIGHT TEST INDICATES EPSU COM FWD L AND EPSU EXT LOAD FWD L ON CIDS 1 GROUND SCANNING. EPSU SHOWS FAULT EXT L OADS. FOUND BAD SPLICE ON WIRE 5109, REPLACED WIRE BETWEEN 2871VC AND 2819VC. WIRE 5109 OPERATION TEST FOR EPSU OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007021500185 20070215 00185 EA 2007 2 15 COMA0760168 1 20070206 A 2750 SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS LACK OF LUBE A COMA O OTHER W J INADEQUATE Q C WARNING INDICATION AP APPROACH 1 SO 01 966CA 7132 FLIGHT 5542 - FLAPS FAILED DURING APPROACH. REMOVED, INSPECTED, LUBRICATED AND REINSTALLED ALL FLEX DRIVE SHAFTS. 2 L 7 2 4F RT A21EA 2007021500186 20070215 00186 NM 2007 2 15 SWAA070708 1 20070210 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 445WN 29841 EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2007021500187 20070215 00187 NM 2007 2 15 SWAA070693 1 20070209 A 5313 65176856 STRINGER SPLICE BOEING 737 7373H4 1384600 NM BS 348 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 348, STR 16L. REMOVED AND REPLACED STRINGER SPLICE PER ACO. 2 L 7 2 4F RT A16WE 2007021500188 20070215 00188 NM 2007 2 15 SWAA070691 1 20070209 A 2730 6545187 TORQUE TUBE BOEING 737 7373H4 1384600 NM RT ELEVATOR FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED SPV CHECK, RIGHT ELEVATOR BUSS LINKAGE FAILED CHECK. REMOVED AND REPLACED ELEVATOR OUTPUT TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007021500189 20070215 00189 NM 2007 2 15 SWAA070710 1 20070210 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007021500190 20070215 00190 NM 2007 2 15 SWAA070709 1 20070210 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM BS 269 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 269, STR 15R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007021500191 20070215 00191 NM 2007 2 15 SWAA070689 1 20070209 A 5315 6545815 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, RBL 9 TO LBL 50. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007021500192 20070215 00192 NM 2007 2 15 SWAA070699 1 20070209 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM BS 380 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007021500193 20070215 00193 NM 2007 2 15 SWAA070687 1 20070209 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 9L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007021500194 20070215 00194 NM 2007 2 15 SWAA070703 1 20070209 A 5311 6546526 FRAME BOEING 737 7373Q8 1384670 NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007021500195 20070215 00195 NM 2007 2 15 SWAA070694 1 20070209 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007021500196 20070215 00196 NM 2007 2 15 SWAA070702 1 20070209 A 5322 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM BS 500C S28L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 28L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007021500197 20070215 00197 NM 2007 2 15 SWAA070696 1 20070209 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007021500198 20070215 00198 NM 2007 2 15 SWAA070688 1 20070209 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM BS 559 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 9L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007021500001 20070215 00001 CE 2007 2 15 DXTA200701929 1 20070212 A 2731 INDICATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE ELEVATOR TRIM OUT OF ADJUST E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 632QS 5605132 RECEIVED A NO TAKEOFF MESSAGE AROUND 40KTS, ABORTED TAKEOFF. FOUND ELEVATOR TRIM INDICATOR STRIP AND PROX SWITCH FOR NO TAKEOFF SYSTEM OUT OF ADJUSTMENT. ADJUSTED ELEVATOR TRIM STRIP INDICATOR AND PROX SWITCH IAW CH 27-31-00 OF THE CE 560 XL M.M. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007021500007 20070215 00007 EA 2007 2 15 QXEA200700091 1 20070115 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 510 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - RIGHT INBOARD SEAT TRACK HAS A GOUGE INSIDE THE TRACK WITH SURFACE CORROSION INSIDE AND ON TOP OF THE TRACK AT FS 510. REPAIRED IAW REO670-53-00-013. 2 L 7 2 4F RT A21EA 2007021500008 20070215 00008 EA 2007 2 15 QXEA200700092 1 20070117 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FS 280 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND LEFT INBOARD CABIN SEAT RAIL ATTACH FITTING TO FS 280 BEAM IS CRACKED. REPAIRED IAW REO670-53-11-047 AND SRM 51-42-00. 2 L 7 2 4F RT A21EA 2007021500015 20070215 00015 WP 2007 2 15 AALA20070203 1 20070128 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 483A 49676 PHX - BATTERY PACKS FOR EMERGENCY LIGHTS IN AFT CABIN STATION 1190 RIGHT FAILED FUNCTIONAL TEST. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS IN AFT CABIN STATION 1190 RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007021500017 20070215 00017 WP 2007 2 15 AALA20070205 1 20070127 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 480AA 49655 SFO OVERWING EMERGENCY EXIT LIGHTS ON FORWARD LEFT AND RIGHT SIDE INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMER GENCY EXIT LIGHTS ON FORWARD LEFT AND RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007021500020 20070215 00020 WP 2007 2 15 AALA20070202 1 20070128 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 483A 49676 PHX - FOUND EMERGENCY LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK AT STATION 902 RIGHT FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007021500022 20070215 00022 WP 2007 2 15 AALA20070207 1 20070128 A 3350 P2010031303 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 487AA 49680 LGA - FOUND EMERGENCY LIGHT AT AFT GALLEY SERVICE DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT AFT GALLEY SER VICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007021500027 20070215 00027 WP 2007 2 15 AALA20070216 1 20070129 A 3350 SHIELD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 457AA 49562 ORD - FOUND EMERGENCY LIGHT AT SEAT 19D HAS MISSING SHIELD. REPLACED SHIELD FOR EMERGENCY LIGHT AT SEAT 19D. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007021500028 20070215 00028 WP 2007 2 15 AALA20070217 1 20070129 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 457AA 49562 ORD - FOUND EMERGENCY LIGHT AT SEAT 19D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 19D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007021500033 20070215 00033 EU 2007 2 15 AALA20070215 1 20070129 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14068 511 MIA - FOUND EMERGENCY LIGHT AT SEAT 13G INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 13G. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007021500035 20070215 00035 WP 2007 2 15 AALA20070220 1 20070129 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 457AA 49562 ORD - FOUND EMERGENCY LIGHT AT SEAT 24D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007021500037 20070215 00037 WP 2007 2 15 AALA20070187 1 20070125 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 422AA 49334 BOS - FOUND EMERGENCY LIGHTS AT OVERHEAD LEFT AND RIGHT FORWARD AUXILIARY OVERWING EXIT AT SEAT ROW 20DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD LEFT AND RIGHT FORWARD AUXILIARY OVERWING EXIT AT SEAT ROW 20DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007021500045 20070215 00045 EA 2007 2 15 QXEA200700086 1 20070115 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 265 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVET HEAD AT FS 265 STRINGER 23R. REPAIRED IAW SRM 51-42-06, 53-00-01, 51-21-11, 51-25-01. 2 L 7 2 4F RT A21EA 2007021500048 20070215 00048 SO 2007 2 15 C2XA07IA031 1 20070211 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15555 145594 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE CABIN EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007021500051 20070215 00051 EA 2007 2 15 TRAX200700199 1 20070209 A 2750 SLAT SYSTEM CNDAIR CL600 CL6002C10 1390015 EA LE SLATS FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 724EV 10138 ON APPROACH, RECEIVED SLATS FAIL MSG, EMERGENCY DECLARED, FLT 4147 DEL 26 MINS. 2 L 7 2 4F RT A21EA 2007021500052 20070215 00052 EU 2007 2 15 TRAX200700200 1 20070209 A 3350 LIGHT AEROSP ATR72 ATR72212 8680945 EU ASD INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 FOUND EMERGENCY EXIT ON LAST STEP OF ASD INOP. 2 H 7 2 4T RT A53EU 2007021500055 20070215 00055 SO 2007 2 15 SIMA200704413 1 20070211 A 5320 14530645411 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 803AE 13064 4800 145483 PREVIOUS REPAIR ON LEFT OMEGA BEAM AT FRAME 20 CORRODED. REMOVED EXISTING REPAIR, CLEANED AND TREATED REPAIR AREA. FAB RICATED AND INSTALLED REPAIR DOUBLER IAW EMB SRM 53-00-10. RESTORED PROTECTIVE FINISH, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007021500065 20070215 00065 EU 2007 2 15 2007UALA00294 1 20070203 A 3260 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MLG DOOR UNKNOWN A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 429UA 539 RTFL WITH A LANDING GEAR DOOR WARNING MESSAGE. PROBLEM REOCCURED ON SUBSEQUENT FLIGHT. [SUP 05-08-07] AFTER RTFL OF F LIGHT 543, FAULT WAS ORIGINALLY TRACED TO A LOOSE PROXIMITY SWITCH. SWITCH WAS SECURED AND OPS CHECKED OK. ON NEXT FLIGH T, SAME WARNING MESSAGE OCCURRED FOLLOWED BY ANOTHER RTFL EVENT. SUBSEQUENT FAULT TRACING FOUND THE DOOR CLOSE SAFETY VA LVE TO BE DEFECTIVE. SAFETY VALVE WAS REPLACED AND GEAR WAS CYCLED 5 TIMES DURING A VERIFICATION FLIGHT TO ENSURE PROPER OPERATION. 2 L 7 2 4F 4 F RT A28NM E40NE 2007021500069 20070215 00069 NM 2007 2 15 2007UALA00298 1 20070203 A 5340 BRACKET BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU BS 360 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 912UA 25290 LT FUSELAGE INTERNAL AFT BRACKET IS CRACKED IN RADIUS FOR INTERCOSTAL A STR 11L JUST FWD OF BS 360, VIEW FROM LWR SURFAC E. INSTALLED NEW BRACKET. 2 L 7 2 4F 4 F RT A16WE E21EU 2007021500074 20070215 00074 NM 2007 2 15 2007UALA00303 1 20070203 A 3350 SWITCH BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS OUT OF POSITION A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 FOUND EMERGENCY EXIT LIGHTS COME ON WHEN COCKPIT SWITCH IS IN OFF. FOUND DR L1 SWITCH IS ON. REPOSITIONED SWITCH. OPS CHKD OK NO FAULT, SWITCH LEFT IN "ON" POSITION. 2 L 7 4 4F 4 F RT A20WE E24NE 2007021500078 20070215 00078 NM 2007 2 15 2007UALA00307 1 20070204 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 643UA 25093 FOUND OVERHEAD EMERGENCY EXIT LIGHTS OUT LEFT AISLE. RELAMPED BULBS FOR OVERHEAD EMERG LIGHTS, LEFT AISLE PER MM 33-5 1-00 OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007021500083 20070215 00083 NM 2007 2 15 2007UALA00312 1 20070204 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SEAT 13HJ & 14HJ MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 676UA 30028 FOUND EEL STRIP LIGHTS AT SEATS 13HJ AND 14HJ ARE MISSING. REPLACED EEL STRIP IN BOTH LOCATIONS. EEL OPS CK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007021500084 20070215 00084 NM 2007 2 15 2007UALA00313 1 20070202 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 2E DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 774UA 26936 FOUND SEAT 2E HAS A DAMAGED EEL PATH LIGHT. REPLACED EEL PATH LIGHT PER STANDARD PRACTICES AND TESTED NORMALLY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007021500101 20070215 00101 NM 2007 2 15 2007UALA00327 1 20070206 A 3350 LAMP BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 FOUND DOOR 1L EMERGENCY SLIDE ILLUMINATION LIGHT INOP. RELAMPED, OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007021500107 20070215 00107 EU 2007 2 15 USAA070097 1 20070213 A 5340 FITTING AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 169UW 1455 FOUND Y1732 LT BATH TUB FITTING AFT LT DOOR. REMOVED AND REPLACED MODIFIED PART INSTALLED PER SRM 53-41-14; CORROSION L EVEL 1; TASK JA-260-53500, DEFECT SIZE: 1" BY 1". 2 L 7 2 4F RT A28NM 2007021500110 20070215 00110 NM 2007 2 15 QXEA200700163 1 20070213 A 3040 SYLZ50970 CONTROLLER DHAV DHC8 DHC8202 2809007 NM WINDSHIELD MALFUNCTIONED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 367PH 7022 511 SEA FLIGHT NR 2251, SMOKE COMING FROM WINDSHIELD HEATING UNIT CAPTAINS SIDE SMOKE STOPPED AFTER UNIT TURNED OFF. MAINTE NANCE REPLACED CAPTAINS WINDSHIELD AND HEAT CONTROLLER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007021500115 20070215 00115 NM 2007 2 15 SWAA070730 1 20070211 A 3350 417N5253 CAP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 249WN 34951 FOUND FWD RT EEPLS END CAP BROKEN. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 2007021500119 20070215 00119 NM 2007 2 15 SWAA070714 1 20070210 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 578 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 578, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007021500132 20070215 00132 EA 2007 2 15 QXEA200700079 1 20070115 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 573 S17L DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10128 C2 PDX - FOUND EVIDENCE OF LIGHTNING STRIKE ON RIVETHEAD ON LEFT SIDE OF FUSELAGE ABOVE FORWARD CARGO DOOR AT FS 573 AND STRINGER 17L. REPAIRED IAW SRM 53-00-01, 51-21-11, AND 51-25-01. 2 L 7 2 4F RT A21EA 2007021500135 20070215 00135 NM 2007 2 15 WRLA2007033 1 20070210 A 5414 SKIN PANEL DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 1 NACELLE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 62911 48407 FOUND NR 1 PYLON PRECOOLER TORQUE BOX SKIN PANEL GOUGE. PERFORM NR 1 PYLON PRECOOLER TORQUE BOX SIDE SKIN PANEL GOUGE A REA DOUBLER INSTALL REPAIR PER MD-11 SRM VOL 1, 54-00-01 FIG 3 REV:38. 2 L 7 3 4F 4 F RT A22WE E24NE 2007021500138 20070215 00138 NM 2007 2 15 QXEA200700159 1 20070210 A 2750 FLAP SYSTEM BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 421QX 4149 SEA FLIGHT NR 2328: FLAP POWER CAUTION LIGHT ILLUMINATED DURING PUSH BACK. RESET C/B PER EA CHECKLIST. LIGHT WAS STILL ILLUMINATED. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE PERFORMED Q400 FIM TASK 27-50-00-810-802 AND OPS TEST OF THE WIN G FLAPS IAW Q400 AMM TASK 27-50-00-710-801. OPERATIONAL TEST IS GOOD WITH NO DISCREPANCIES AND NO REOCCURRENCE OF FLAP POWER CAUTION LIGHT. NO PARTS REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007021500151 20070215 00151 NM 2007 2 15 DL76S070115 1 20070211 A 5311 FRAME BOEING 767 767332 1382001 NM BS 1725 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 FOUND SMALL CRACK AFT SIDE OF FRAME AT STA 1725.5 2:00 POSITION. REPAIRED PER SRM 53-80-01 REPAIR 5 FIG 201 DETAIL 3. 2 L 7 2 4F RT A1NM 2007021500152 20070215 00152 NM 2007 2 15 DL76S070116 1 20070211 A 5330 SKIN BOEING 767 767332 1382001 NM BS 1772-1776 WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 FOUND AFT FUSELAGE, SEC 48, STAINLESS RUBSTRIP WORN THROUGH UNDER HORIZONTAL STAB AT STA 1772-1776, STR 21L. REPAIRED A ND INSTALLED SKIN PANEL PER SRM 53-80-01, FIG 201, REPAIR 3. 2 L 7 2 4F RT A1NM 2007021500199 20070215 00199 NM 2007 2 15 SWAA070701 1 20070209 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM BS 747 S8R-8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007021500200 20070215 00200 NM 2007 2 15 NWAA070556310 1 20070209 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670US 24225 DURING OVERNIGHT LINE CHECK, EMERGENCY LIGHT EXIT SIGN 3R WAS INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OPE RATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007021600009 20070216 00009 NM 2007 2 16 DL76L070127 1 20070213 A 3250 BYPASS VALVE BOEING 767 767332 1382001 NM NLG STEERING LEAKING A DALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 193DN 28450 AT PUSH BACK, STEERING BYPASS VALVE NOTICED LEAKING. FOUND UNION TUBE ON BYPASS VALVE LOOSE. TIGHTENED UNION TUBE TUBE , OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2007021600011 20070216 00011 NM 2007 2 16 DL76L070129 1 20070213 A 2410 755359 IDG BOEING 767 767332 1382001 NM RIGHT UNKNOWN A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 188DN 27583 R GEN DRIVE MESSAGE ILLUMINATED. PERFORMED BITE ON BPCU. FAULTED RT GCU. REPLACE RT GCU. PERFORMED BITE. NO FAULTS. RESET GENERATOR DISCONNECT. RAN ENG ON IDLE AT GATE. NO VOLTS OR FREQS. REMOVED AND PLACED R IDG IAW M/M. RAN ENG AT GATE. DISCONNECTED IDG. RESET DRING AND RE-RAN ENGINE. OPS CHECK NML MPN 755359. 2 L 7 2 4F RT A1NM 2007021600013 20070216 00013 2007 2 16 DHL2007780003 2 20070214 A 7200 UNKNOWN BOEING 727 727223 1384074 NM ENGINE UNKNOWN A DHLA C ABORTED TAKEOFF E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 SO 01 780DH 22006 RTO INFO 146800 LBS 80 KTS -11C, PA 1077, NORMAL AT 80 KTS, HEARD A THUMP, SAW A FLASH, ENG FAIL LIGHTS ILLUMINATED, AUT O PACK TRIP ACTIVATED. TAKEOFF WAS REJECTED. INSPECTED ENG INLET/ C-1. NO DAMAGE NOTED. SUSPECT X-WIND COND 24 KTS N OTED, PER AOM CH 1 8 PG 5 . 2 L 7 3 4F A3WE 2007021600017 20070216 00017 NM 2007 2 16 2007UALA00331 1 20070205 A 3350 BATTERY PACK BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 784UA 26951 DOOR 1L EPAS BATTERY PACK TEST LIGHT IS INOPERATIVE. REPLACED BOTH EPAS 9 VOLT BACKUP BATTERIES AT DOOR 1L AFTER REPL ACEMENT OF DOOR 1L EPAS BATTERY PACK, EPAS TESTED OK. A/C RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007021600018 20070216 00018 EU 2007 2 16 2007UALA00332 1 20070205 A 5340 ATTACH FITTING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 431UA 571 FWD FRAME CLIP AND STRINGER FASTENERS HAVE CORROSION FROM FRAME 31 TO 35 AND FROM STR 38R TO 38L. REPLACED 752 CORRODED RIVETS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007021600022 20070216 00022 2007 2 16 2007UALA00336 4 20070206 A 2565 LEVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR SLIDE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 DOOR 1R DISARM LEVER HARD TO DISARM. CREW REPORTS LEVER MOVED FORCEFULLY TO DISARM AND HEARD UNUSUAL NOISE, DOOR APPEAR S TO BE DISARMED. CLEANED DEBRIS AND ICE FROM GIRT BAR SENSOR AREA. ARM LEVER NOW NORMAL. NO COMPONENTS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007021600023 20070216 00023 NM 2007 2 16 2007UALA00337 1 20070206 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN MISLOCATED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 643UA 25093 EEL TRACK IS MISLOCATED UNDER FIRST CLASS SEATS. RELOCATED LT EEL TRACK IN A=ZONE PER DWG 15F6786. OPS CHECK GOOD 2 L 7 2 4F 4 F RT A1NM E24NE 2007021600024 20070216 00024 NM 2007 2 16 2007UALA00338 1 20070206 A 3350 SWITCH BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS DEFECTIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 666UA 29238 ALL AIRCRAFT EMERGENCY LIGHTS COME ON WHEN POWER REMOVED FROM AIRCRAFT. FOUND EMERGENCY LIGHT SWITCH S1 DEFECTIVE. REP LACED SWITCH. OP CHECKS NORMALLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007021600026 20070216 00026 NM 2007 2 16 2007UALA00340 1 20070131 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 SKIN PUNCTURED 1 X 2 INCHES JUST FORWARD OF FWD LAV SERVICE PANEL CAUSED BY LAV TRUCK. MAJOR REPAIR, INSTALLED REPAIR P ARTS REF SRM 53-10-01 RPR 11 DETAIL V AND DETAIL VII. 2 L 7 2 4F 4 F RT A16WE E21EU 2007021600027 20070216 00027 NE 2007 2 16 2007UALA00341 2 20070207 A 7230 BLADE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COMPRESSOR FAILED A UALA C ABORTED TAKEOFF X J ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 WP 29 809UA 825 V10091 CREW REPORTS ON TAKEOFF ROLL JUST BELOW 80 KNOTS, AUDIBLE COMPRESSOR STALL & REPORT OF FLAME FROM EXHAUST. [5-1-07] BO RESCOPE INSPECTION OF THE HPC REVEALED DAMAGE STARTING WITH THE R3 BLADE (THE FIRST STAGE). SUSPECT ANOTHER R3 CLAPPER FAILURE RESULTING IN A LIBERATED BLADE. KNOWN PROBLEMS WITH FIRST STAGE BLADES. 2 L 7 2 4F 4 F RT A28NM E40NE 2007021600028 20070216 00028 EU 2007 2 16 2007UALA00342 1 20070208 A 5320 ANGLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 419UA 487 RIGHT AFT BELLY FAIRING SUPPORT STRUCTURE ANGLE CRACKED AT ATTACH TO FUSELAGE SKIN BELOW KEEL BEAM AT FRAME 46. MAJOR RE PAIR ACCOMPLISHED: REPLACED DAMAGE SECTION OF ANGLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007021600029 20070216 00029 EU 2007 2 16 2007UALA00343 1 20070208 A 5320 ANGLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 419UA 487 LEFT AFT BELLY FAIRING SUPPORT STRUCTURE ANGLE CRACKED AT ATTACH TO FUSELAGE SKIN BELOW KEELBEAM AT FRAME 46. MAJOR REPA IR ACCOMPLISHED: REPLACED DAMAGE SECTION OF ANGLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007021600030 20070216 00030 EU 2007 2 16 2007UALA00344 1 20070207 A 5210 LEVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 422UA 503 DOOR 2R ARM LEVER WON'T GO ALL THE WAY DOWN WHEN IN THE ARMED POSITION. [SUP 05-08-07] LOOSE EMERGENCY SLIDE COVER WAS INTERFERING WITH MOTION OF DOOR LEVER. FULL MOTION RESTORED AFTER SLIDE COVER WAS SECURED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007021600050 20070216 00050 NM 2007 2 16 SWAA070805 1 20070214 A 2121 215201 FAN BOEING 737 7373H4 1384600 NM E&E BAY FAULTY A SWAA O OTHER O OTHER NR NOT REPORTED 1 SW 29 390SW 26593 F/A REPORT ELECTRICAL SMELL IN MID CABIN. TURNED OFF GASPER FAN SMELL DISSIPATED. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2007021600051 20070216 00051 NM 2007 2 16 SWAA070859 1 20070214 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED MV3 CHECK, FOUND EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007021600053 20070216 00053 NM 2007 2 16 SWAA070860 1 20070214 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 494WN 33868 DURING SCHEDULED MV1 CHECK, FOUND LT FWD CABIN EEPLS END CAP BROKEN. REMOVED AND REPLACED EEPLS END CAP PER MM. 2 L 7 2 4F RT A16WE 2007021600057 20070216 00057 NM 2007 2 16 SWAA070816 1 20070214 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM BS 793 S19L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 793, STR 19L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007021600058 20070216 00058 NM 2007 2 16 SWAA070855 1 20070214 A 5753 6546435 SKIN BOEING 737 7373Q8 1384670 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING OUTBOARD AFT FLAP LOWER T/E SURFACE DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007021600059 20070216 00059 NM 2007 2 16 SWAA070819 1 20070214 A 5753 6546486 SKIN BOEING 737 7373Q8 1384670 NM TE FLAP DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD MID FLAP T/E LOWER SURFACE DISBONDED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007021600060 20070216 00060 NM 2007 2 16 SWAA070815 1 20070214 A 5753 6546486129 SKIN BOEING 737 7373G7 1384595 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED MV1 CHECK, FOUND LEFT WING INBOARD MID FLAP OUTBOARD T/E DELAMINATED. REMOVED AND REPLACED MID FLAP PE R MM. 2 L 7 2 4F RT A16WE 2007021600061 20070216 00061 NM 2007 2 16 SWAA070807 1 20070214 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S9LR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 9L AND STR 9R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007021600067 20070216 00067 EU 2007 2 16 AALA20070227 1 20070130 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70054 461 MIA - FOUND EMERGENCY LIGHT AT SEAT 26G INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 26G. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007021600070 20070216 00070 WP 2007 2 16 AALA20070244 1 20070202 A 2560 STRAP DOUG DC9 DC983 3022083 WP FLASHLIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 970TW 53620 LGA - EMERGENCY FLASHLIGHTS AT BOTH FORWARD POSITIONS HAVE SAFETY STRAPS BROKEN. REPLACED SAFETY STRAPS FOR EMERGENCY F LASHLIGHTS AT BOTH FORWARD POSITIONS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007021600071 20070216 00071 NM 2007 2 16 AALA20070239 1 20070202 A 3350 SHIELD BOEING 767 767323 1385205 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AA 25201 CDG - FOUND EMERGENCY LIGHT AT SEAT 20CEG BULKHEAD HAS A LOOSE COVER. SECURED EMERGENCY LIGHT COVER AT SEAT 20CEG BULKH EAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007021600076 20070216 00076 WP 2007 2 16 AALA20070228 1 20070131 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 297AA 49309 LGA - FOUND OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK IN AFT CARGO FOR OVERWING EMERGENCY LIGHTS SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007021600079 20070216 00079 NM 2007 2 16 SWAA070812 1 20070214 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM BS 360 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007021600080 20070216 00080 NM 2007 2 16 SWAA070821 1 20070214 A 5753 65522111 TORQUE TUBE BOEING 737 7373Q8 1384670 NM TE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007021600081 20070216 00081 NM 2007 2 16 SWAA070820 1 20070214 A 5753 65522112 TORQUE TUBE BOEING 737 7373Q8 1384670 NM TE FLAPS CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQU E TUBE PER MM. 2 L 7 2 4F RT A16WE 2007021600082 20070216 00082 NM 2007 2 16 SWAA070856 1 20070214 A 5753 6573731 SKIN BOEING 737 7373Q8 1384670 NM TE FLAPS DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD AFT FLAP INBOARD T/E LOWER SURFACE DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007021600083 20070216 00083 NM 2007 2 16 SWAA070808 1 20070214 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM BS 500C S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 9R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007021600084 20070216 00084 NM 2007 2 16 SWAA070809 1 20070214 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM BS 727D S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 9R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007021600086 20070216 00086 NM 2007 2 16 SWAA070827 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 727B S3R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600087 20070216 00087 NM 2007 2 16 SWAA070826 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 727C S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600088 20070216 00088 NM 2007 2 16 SWAA070825 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 727C S6R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600089 20070216 00089 NM 2007 2 16 SWAA070824 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 727C S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600092 20070216 00092 NM 2007 2 16 SWAA070829 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 706 S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600093 20070216 00093 NM 2007 2 16 SWAA070823 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 727C S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600095 20070216 00095 NM 2007 2 16 SWAA070854 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 500 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600096 20070216 00096 NM 2007 2 16 SWAA070853 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 500B S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007021600099 20070216 00099 NM 2007 2 16 SWAA070850 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 500C S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600101 20070216 00101 NM 2007 2 16 SWAA070848 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 500D S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600104 20070216 00104 NM 2007 2 16 SWAA070845 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 559 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600105 20070216 00105 NM 2007 2 16 SWAA070830 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 706 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600106 20070216 00106 NM 2007 2 16 SWAA070837 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 597 S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600108 20070216 00108 NM 2007 2 16 SWAA070834 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 685 S6R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600112 20070216 00112 NM 2007 2 16 SWAA070843 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 559 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600116 20070216 00116 NM 2007 2 16 SWAA070841 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 578 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600117 20070216 00117 NM 2007 2 16 SWAA070842 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 559 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600118 20070216 00118 NM 2007 2 16 CALA0700064 1 20070214 A 5320 141A5410U23 INTERCOSTAL BOEING 737 737824 13844BZ NM BS 344-360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14237 28802 INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT STA 344-360, LBL 0. THE INTERCOSTAL WAS REPAIRED IAW ECRA 5321-01446. 2 L 7 2 4F RT A16WE 2007022000001 20070220 00001 CE 2007 2 20 DXTA200701931 1 20070213 A 3213 STRUT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG DISCHARGED E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 999QS 7500203 VIOLENT NOSE WHEEL SHIMMY DURING T/O ROLL (VERBAL FROM CREW STARTED AT 80KTS AND CONTINUED DOWN TO ABOUT 40 KTS). UPON ARRIVING AT AIRCRAFT FOUND NOSE STRUT FLAT. REMOVED LOWER & UPPER BARREL ASSY AND FOUND INTERNAL DAMAGE. RMVD AND REPLAC ED UPPER & LOWER BARREL ASSY. NO HYD LINES WERE REMOVED. RE-SECURED ALL ACCESS ITEMS. GEAR SWINGS/TAXI SWINGS/TAXI CHECK GOOD I/A/W CE750 C/M/M 32-20-02 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007022000020 20070220 00020 NM 2007 2 20 ASAA0741442 1 20070206 A 5753 65C3570541 SKIN BOEING 737 737490 1384715 NM LT FORE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 THE LEFT WING O/B FORE FLAP L/E IS CHAFED OUT OF LIMITS AT THE O/B END. FABRICATED AND INSTALLED AN EXTERNAL REPAIR DOU BLER IAW ASA EA 5750 02325. 2 L 7 2 4F RT A16WE 2007022000024 20070220 00024 EA 2007 2 20 TRAX200700148 1 20070130 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 FS 280.00 CENTER FWD, FLOORPANEL SUPPORT ANGLE CORRODED. 2 L 7 2 4F RT A21EA 2007022000026 20070220 00026 EU 2007 2 20 TRAX200700149 1 20070201 A 5320 INTERCOSTAL AEROSP ATR72 ATR72 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 RIGHT WING BOX DTW FR 244 24 INTERCOSTAL FOUND CRACKED. REPAIRED IAW SRM 51-25-01. 2 H 7 2 4T RT 2007022000028 20070220 00028 EU 2007 2 20 TRAX200700150 1 20070201 A 5320 PLATE AEROSP ATR72 ATR72 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 LEFT WING BOX AT FR 28A FACE PLATE CRACKED. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SP633 AND FAR 43 APPENDIX A REPAIR ACCOMPLISHED IAW SRM 51-25-01 2 H 7 2 4T RT 2007022000029 20070220 00029 EU 2007 2 20 TRAX200700151 1 20070201 A 5320 ANGLE AEROSP ATR72 ATR72 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 LEFT WING BOX AT FR 28 ANGLE BEHIND FACE PLATE CRACKED. LT WING BOX AT FR28 ANGLE BEHIND FACE PLATE REPLACED PER SRM 51 -25-01. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW S.P. 663 AND FAR 43 APPENDIX A REPAIR ACCOMPLISHED IAW SRM 51-25- 01. 2 H 7 2 4T RT 2007022000033 20070220 00033 WP 2007 2 20 N921R40407 1 20070105 A 5311 FRAME SPLICE DOUG DC8 DC863F 302198F WP BS 520 L17R CORRODED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 921R 46145 MAIN CARGO COMPARTMENT STA 520, L-17R FRAME SPLICE WITH CORROSION. REMOVED FRAME SPLICE IAW DPS 3-67-29. FABRICATED NE W FRAME SPLICE IAW DPS 3-69-4, PRIMED SPLICE IAW DC8 SRM 51-1-8. INSTALLED FRAME SPLICE IAW DC8 SRM 51-1-27 CPCP 5730-0 551. 2 L 7 4 4F 4A25 2007022000035 20070220 00035 EA 2007 2 20 TRAX200700155 1 20070202 A 2612 WARNING MESSAGE CNDAIR CL600 CL6002C10 1390015 EA FIRE WARNING ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 718EV 10095 LEFT FIRE SYSTEM FAIL CAUTION MSG. AIRCRAFT RETURNED TO ATL AFTER T/O. FLTS 4209, 4899 CX. 2 L 7 2 4F RT A21EA 2007022000036 20070220 00036 WP 2007 2 20 N921R53905 1 20070108 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 720 L17L CORRODED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 921R 46145 LOWER FUSELAGE EXTERIOR STA 720 L-17L SKIN WITH CORROSION. OPENED SKIN AREA IAW DPS 3-67-27, FOUND CORRODED INNER DOUBL ER, REMOVED INNER DOUBLER IAW DPS 3-67-27. FABRICATED NEW INNER DOUBLER IAW DC8 SRM 53-5-3 & DPS 3-69-4. TREATED AND P RIMED AREA AND NEW DOUBLER IAW DC8 SRM 57-1-81. INSTALLED NEW INNER DOUBLER IAW DC8 SRM 51-1-21 AND CLOSED SKIN AREA IA W DC8 SRM 51-1-21 CPCP 5000-0552. 2 L 7 4 4F 4A25 2007022000042 20070220 00042 EU 2007 2 20 TRAX200700214 1 20070211 A 3350 LIGHT AEROSP ATR72 ATR72 EU PAX DOOR STEP INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 636AS 375 PAX DOOR LOWER STEP LIGHT INOP. 2 H 7 2 4T RT 2007022000046 20070220 00046 EA 2007 2 20 TRAX200700203 1 20070208 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR STEP UNSERVICEABLE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 820AS 7188 THE -EXIT- PLACARD ON PAX DOOR STEP 832 BT IS UNSERVICEABLE. 2 L 7 2 4F RT A21EA 2007022000048 20070220 00048 EA 2007 2 20 TRAX200700205 1 20070209 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 820AS 7188 FLOOR SUPPORT FITTING AT FS 460.5 O/B OF LBL 9.0 CRACKED MID TOP MARKED. REMOVED CRACKED FITTING IAW CRJ SRM 51-42-21. DRILLED AND LOCATED NEW FITTING P/N 600-31068-19 IAW CRJ SRM 51-40-11. OK TO INSTALL. (INSP RA333) INSTALLED SERVICEA BLE FITTING IAW CRJ SRM 51-42-21. (EMP 699) OK TO PAINT. (INSP RA323) TOPCOATED REPAIR AREA IAW CRJ SRM 51-25-16. (EM P699 - INSP RA333). SUPPLEMENTAL - SDR CLOSED 02/15/07. 2 L 7 2 4F RT A21EA 2007022000049 20070220 00049 EA 2007 2 20 TRAX200700206 1 20070209 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 820AS 7188 FS 484 ANGLE CRACKED I/B SIDE OF FLOORBEAM AT LBL 27.0. 2 L 7 2 4F RT A21EA 2007022000052 20070220 00052 EA 2007 2 20 TRAX200700209 1 20070209 A 5320 FLOOR SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 820AS 7188 PRESSURE FLOOR SKIN UNDER FLOORBOARD 261 DLF HAS SEVERAL AREAS OF SURFACE CORROSION I/B OF DADO PANEL. 2 L 7 2 4F RT A21EA 2007022000054 20070220 00054 EA 2007 2 20 TRAX200700211 1 20070210 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 840AS 7290 FLAPS FAILED AT 0 DEGREES ON APP INTO GRR. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007022000055 20070220 00055 EA 2007 2 20 TRAX200700212 1 20070210 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 880AS 7606 FLAPS FAIL ON APPROACH. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007022000056 20070220 00056 EU 2007 2 20 TRAX200700213 1 20070210 A 2120 UNKNOWN AEROSP ATR72 ATR72 EU CABIN ODOR A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 633AS 344 ON DESCENT UNUSUAL SMELL FROM VENTS, FLIGHT COMP TEMP (PACKS). 2 H 7 2 4T RT 2007022000057 20070220 00057 EA 2007 2 20 TRAX200700185 1 20070206 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 906EV 7642 REFER TO AFDL 322776 ITEM 2 FLAP FAIL AT O DEG. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007022000058 20070220 00058 EA 2007 2 20 TRAX200700186 1 20070206 A 3250 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA STEERING SYS ACTIVATED A ASOA K NONE J WARNING INDICATION CL CLIMB 1 SO 27 917EV 7769 STEERING INOP MSG AFTER GEAR RETRACTION, COMPLIED WITH QRH, SYSTEM RESET AFTER LANDING. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007022000059 20070220 00059 EA 2007 2 20 TRAX200700187 1 20070206 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 ENTRANCE DOOR WILL NOT CLOSE. 2 L 7 2 4F RT A21EA 2007022000060 20070220 00060 EA 2007 2 20 TRAX200700188 1 20070206 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 870AS 7530 FLAP FAIL AT 8 DEGREES ON APPROACH. EMERGENCY DECLARED. FLT 4093 CX. 2 L 7 2 4F RT A21EA 2007022000061 20070220 00061 EA 2007 2 20 TRAX200700189 1 20070206 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 699BR 7801 F/O FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007022000063 20070220 00063 WP 2007 2 20 N921R19512 1 20070103 A 5313 STRINGER SPLICE DOUG DC8 DC863F 302198F WP BS 680 L4R CRACKED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 921R 46145 FOUND MAIN CARGO COMPARTMENT STA 680, L4R AFT SPLICE FITTING WITH CRACK. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-2 0 AND 53-4-1 CPCP 5730-0553. 2 L 7 4 4F 4A25 2007022000064 20070220 00064 WP 2007 2 20 N921R53309 1 20070108 A 5100 NONE DOUG DC8 DC863F 302198F WP FUSELAGE NONE A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 921R 46145 FUSELAGE STA 8 NLG WW DOOR JAMB LT CORNER SKIN WITH TEMPORARY REPAIR. REPAIRED SKIN IAW FLIGHT VEHICLES CONSULTING INC DWG NR 53-07030-1 REV NEW 01-25-09 PAGE 1/3. ISSUED FAA FORM 8110-3. CPCP 4000 0551 2 L 7 4 4F 4A25 2007022000067 20070220 00067 EU 2007 2 20 TRAX200700192 1 20070207 A 2560 FLASHLIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 632AS 338 FLIGHT ATTENDANT FLASHLIGHT INOP. 2 H 7 2 4T RT 2007022000068 20070220 00068 WP 2007 2 20 N921R72213 1 20070103 A 5313 LONGERON DOUG DC8 DC863F 302198F WP BS 520 L17R CORRODED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 921R 46145 FOUND FUSELAGE STA 1540 L29L SKIN RIVETS SHEARED AND LONGERON 29L WITH CORROSION. REPAIRED LONGERON 29L AT FS 1540 IAW DC8 SRM 53-2-2 FIGURE 8. 2 L 7 4 4F 4A25 2007022000069 20070220 00069 WP 2007 2 20 N921R63501 1 20070109 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 78 L17-18L DENTED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 921R 46145 FOUND FUSELAGE EXTERIOR STA 78 BTW L17L AND L18L SKIN WITH DENT. REPAIRED SKIN OF FUSELAGE EXTERIOR STA 78 BTW L-17L AN D L-18L IAW DC8 SRM 53-2-0, TR NR 53-170 CPCP 5000 0551. 2 L 7 4 4F 4A25 2007022000072 20070220 00072 EU 2007 2 20 NSVA20070001 1 20070101 A 2613 WARNING SYSTEM SAAB SF340 SF340A 7850100 EU RT ENG TAILPIPE MALFUNCTIONED A NSVA K NONE N FALSE WARNING IN INSP/MAINT 1 EA 27 121CQ 121 FOUND LEFT ENGINE TAILPIPE HOT LIGHT ILLUMINATED. PERFORMED AN ENG RUN COULD NOT DUPLICATE PROB, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2007022000077 20070220 00077 EA 2007 2 20 TRAX200700194 1 20070207 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 874AS 7551 FLAPS FAIL AT ZERO. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007021500143 20070215 00143 EA 2007 2 15 A6WA200740020 1 20070110 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 412AW 7582 FOUND LEFT INTERCOSTAL AT FS 484 LBL 36 CRACKED APPROXIMATELY .2 INCHES LONG. MAINTENANCE CUT AWAY DAMAGED SECTION OF I NTERCOSTAL FLANGE, PERFORM EDDY CURRENT, FABRICATED REPAIR PARTS AND INSTALLED IAW BOMBARDIER REO 601R-53-41-059 REV A A ND BSC STANDARD REPAIR 601R-53-0030A. (M) 2 L 7 2 4F RT A21EA 2007021500145 20070215 00145 NM 2007 2 15 DL76S070109 1 20070210 A 5313 STRINGER BOEING 767 767332 1382001 NM BS 412-434 S38R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 FOUND STRINGER 38R STA 412-434 CORRODED. REPAIRED PER SRM 53-00-03 FIG 201 REPAIR 2. 2 L 7 2 4F RT A1NM 2007021500146 20070215 00146 NM 2007 2 15 DL76S070110 1 20070210 A 5313 STRINGER BOEING 767 767332 1382001 NM BS 434-456 S37L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 FOUND STRINGER 37L STA 434-456 CORRODED. REPAIRED PER SRM 53-30-03 FIG 201 REPAIR 1. 2 L 7 2 4F RT A1NM 2007021500147 20070215 00147 NM 2007 2 15 DLM88070111 1 20070210 A 2910 CONTROL VALVE DOUG MD88 MD88 3023688 NM HYD SYSTEM LOOSE A DALA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 974DL 53242 SMOKE AND FUMES IN CABIN AFTER EXTENDED RAMP DELAY. AFT SMOKE DETECTOR SOUNDED. FUMES SMELLED OF RUBBER WERE NOXIOUS A ND BURNED EYES. AFTER BLOCK IN NR 1 HYD QTY DOWN TO 1 QT AND A LARGE POOL OF FLUID DISCOVERED ON RAMP. FOUND B-NUT LOO SE ON THRUST REVERSER CONTROL VALVE. TIGHTENED SAME. PERFORMED OPS 5088 2903 AND 5090. REPLACED BOTH WATER SEPARATOR BAGS. SERVICED HYD TO FULL. CLEANED 48 SEC OF EXCESS HYD FLUID. RAN PACKS WITH ENG AIR AT TAKEOFF POWER. 2 L 7 2 4F RT A6WE 2007021500149 20070215 00149 NM 2007 2 15 DL76S070113 1 20070211 A 5313 STRINGER BOEING 767 767332 1382001 NM BS 413-434 S35L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 FOUND STRINGER 35L CORRODED BETWEEN STA 412-434. INSTALLED STRINGER SECTION PER SRM 53-00-03, FIG 201, REPAIR NR 2. 2 L 7 2 4F RT A1NM 2007021500150 20070215 00150 NM 2007 2 15 DL76S070114 1 20070211 A 5313 STRINGER BOEING 767 767332 1382001 NM BS 434-456 S34L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 FOUND STRINGER 34L CORRODED BETWEEN STA 434-456. INSTALLED STRINGER SPLICE PER SRM 51-40-02, PG 1. 2 L 7 2 4F RT A1NM 2007021600001 20070216 00001 SO 2007 2 16 SIMA200704501 1 20070213 A 5320 14525480603 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 712AE 15662 4800 145247 FOUND CARGO DOOR FRAME LOWER SILL CORRODED. REMOVED EXISTING SILL, CLEANED AND TREATED REPAIR AREA. INSTALLED NEW SILL IAW EMB SRM 51-40-02. RESTORED PROTECTIVE FINISH. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007021600010 20070216 00010 NM 2007 2 16 DL76G070128 1 20070213 A 2613 233N620512 CONTROL PANEL BOEING 767 767332 1382001 NM OVERHEAT LIGHT NO TEST A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1602 29694 FOUND LT ENG OVERHEAT LIGHT WOULD NOT TEST. REPLACED FIRE PANEL W/LIKE FROM A/C 173 PER MCC M. CHECKS GOOD PER MM 26-2 1-02. 2 L 7 2 4F RT A1NM 2007021600016 20070216 00016 2007 2 16 2007UALA00330 4 20070205 A 2565 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SEATS 17G, 9F FW INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 784UA 26951 EMERGENCY LIGHTS INOP AT SEATS 17G, 9F FWD LT & 2F AFT LT. REPLACED EEL LIGHT ASSY'S AT SEATS 17G, 9F-FWD LT, & SEAT 2F -AFT LT. ALL POSITIONS OP CHECKED GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007021600019 20070216 00019 EU 2007 2 16 2007UALA00333 1 20070206 A 5340 ATTACH FITTING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 431UA 571 FWD PIT HAS CORROSION ON STRINGER AND FRAME CLIP FASTENERS FROM FRAME 24 THRU 31 AND FROM STRINGER 39R TO 40L. REPLACED 1098 RIVETS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007021600020 20070216 00020 NM 2007 2 16 2007UALA00334 1 20070205 A 5220 LATCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT OVERWING DOOR WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 RIGHT OVERWING DOOR LATCHES FAILED INTEGRATOR TORQUE CHECK. TORQUE WAS 230 LBS, MAX IS 170 LB. REPLACED RT OVERWING DO OR LATCHES,4 EA.PER MM 25-65-98 AND ACCOMPLISHED LATCHING SYSTEM ADJUSTMENT CHECK. PERFORMED INTEGRATOR TORQUE CHECK PE R MM 25-65-98. TEST OK FOR SERVICE. LATCHES ARE METAL ON METAL & IN LATCHED POSITION VIBRATION CAUSES THEM TO FRET AGAI NST EACH OTHER. 2 L 7 2 4F 4 F RT A1NM E24NE 2007021600025 20070216 00025 NM 2007 2 16 2007UALA00339 1 20070207 A 5330 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE BS 432 NICKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 229UA 30557 A NICK WAS FOUND ON FUSELAGE SKIN, STA 432, ABOUT .600 INCH INBOARD OF STR 47R. TECHNICIAN DRILLED OUT NICK, ACCOMPLIS HED HEFC INSP, NO OTHER CRACK DISCOVERED. ACCOMPLISHED REPAIR PER SRM 53-00-01. A/C READY FOR SERVICE. SUSPECT DAMAGED RESULTED FROM CONTACT WITH GROUND EQUIPMENT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007021600032 20070216 00032 NM 2007 2 16 2007UALA00346 1 20070207 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 1006 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 AFT CABIN FLOORBEAM UPPER CHORD CORRODED AROUND FASTENER HOLE BS 1006 LBL 10, WL 208. MAJOR REPAIR, REMOVED DAMAGE. A CCOMPLISHED NESTED ANGLE AND FILLER REPAIR PER MM 53-10-95. 2 L 7 2 4F 4 F RT A16WE E21EU 2007021600049 20070216 00049 EA 2007 2 16 COMA0760166 1 20070207 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 443CA 7539 FLIGHT 9453 - FLAP CAUTION MESSAGE RECEIVED ON APPROACH. LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAU TION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C) FLAP SYSTEM WAS RESET WITH NO FURTHER ME SSAGES. 2 L 7 2 4F RT A21EA 2007021600052 20070216 00052 NM 2007 2 16 SWAA070858 1 20070214 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED MV3 CHECK, FOUND EEPLS COVER MISSING AT ROW 16 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007021600055 20070216 00055 NM 2007 2 16 SWAA070813 1 20070214 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 500C S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007021600056 20070216 00056 NM 2007 2 16 SWAA070861 1 20070214 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 731D S19L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 731D, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007021600062 20070216 00062 NM 2007 2 16 SWAA070817 1 20070214 A 5322 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM BS 500C S27R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007021600063 20070216 00063 NM 2007 2 16 SWAA070818 1 20070214 A 5322 6546546 SHEAR TIE BOEING 737 7373Q8 1384670 NM BS 747 S25L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007021600064 20070216 00064 EU 2007 2 16 AALA20070263 1 20070203 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70072 515 MIA - FOUND EMERGENCY LIGHT AT SEAT 30C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 30C. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A35EU 2007021600065 20070216 00065 EU 2007 2 16 AALA20070225 1 20070131 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 MIA - FOUND EMERGENCY SEAT MOUNTED AND DOOR LIGHTS FROM RIGHT NUMBER ONE DOOR TO RIGHT NUMBER TWO DOOR INOPERATIVE. REP LACED BATTERY PACK FOR EMERGENCY SEAT MOUNTED AND DOOR LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007021600066 20070216 00066 WP 2007 2 16 AALA20070226 1 20070130 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9681B 53631 LGA - FOUND EMERGENCY LIGHTS AT LOCATION B5102 BETWEEN STATIONS 900 AND 1000 INOPERATIVE. REPLACED BATTERY PACK FOR EME RGENCY LIGHTS AT LOCATION B5102 BETWEEN STATIONS 900 AND 1000. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007021600068 20070216 00068 NM 2007 2 16 AALA20070242 1 20070202 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - FOUND EMERGENCY LIGHT OVERHEAD SEAT 31C INOPERATIVE. RELAMPED EMERGENCY LIGHT OVERHEAD SEAT 31C. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007021600069 20070216 00069 NM 2007 2 16 AALA20070243 1 20070202 A 3397 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - FOUND EMERGENCY LIGHT AT SEAT 30C INOPERATIVE. SECURED LOOSE PIN ON CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT T00001SE 2007021600074 20070216 00074 EU 2007 2 16 AALA20070266 1 20070203 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70072 515 MIA - FOUND EMERGENCY LIGHT ASSEMBLY AT SEAT 25G IS BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 25G. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007021600075 20070216 00075 NM 2007 2 16 AALA20070267 1 20070203 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 658AA 24616 MIA - FOUND EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. RELAMPED EXTERIOR EMERGENCY LIGHT AT LEFT NU MBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007021600090 20070216 00090 NM 2007 2 16 SWAA070822 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 727E S3R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600091 20070216 00091 NM 2007 2 16 SWAA070833 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 685 S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600094 20070216 00094 NM 2007 2 16 SWAA070844 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 559 S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600097 20070216 00097 NM 2007 2 16 SWAA070852 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 500B S3R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600098 20070216 00098 NM 2007 2 16 SWAA070851 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 500B S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600103 20070216 00103 NM 2007 2 16 SWAA070831 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 706 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600109 20070216 00109 NM 2007 2 16 SWAA070835 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 639 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600110 20070216 00110 NM 2007 2 16 SWAA070846 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 520 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600113 20070216 00113 NM 2007 2 16 SWAA070838 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 597 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600114 20070216 00114 NM 2007 2 16 SWAA070839 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 578 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600115 20070216 00115 NM 2007 2 16 SWAA070840 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 578 S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600119 20070216 00119 NM 2007 2 16 CALA0700065 1 20070215 A 5330 65C35794 SKIN BOEING 737 7373T0 1384582 NM BS 947-967 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT R-2 FORWARD LOWER CORNER ON DOOR LOWER TORQUE TUBE ACCESS, STA 947.5 -967, S14R TO S15R. REPAIRED IAW SRM 53-60-01, FIGURE 201, PAGE 201. 2 L 7 2 4F RT A16WE 2007022000032 20070220 00032 EU 2007 2 20 TRAX200700154 1 20070202 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 642AS 395 EMERGENCY FLOOR TRACK LIGHTING BETWEEN ROWS 5 & 6AB HAS LIGHTS INOP. 2 H 7 2 4T RT 2007022000034 20070220 00034 WP 2007 2 20 N921R28211 1 20070104 A 5330 FINGER DOUBLER DOUG DC8 DC863F 302198F WP BS 480 L31R CORRODED A U2RA K NONE O OTHER LD LANDING 1 GL 23 921R 46145 FWD CARGO COMPARTMENT STA. 480, L31R FINGER DOUBLER WITH CORROSION. CLEANED CORROSION IAW DC8 SRM 51-1-8. FOUND TO BE WITHIN LIMITS IAW DC8 SRM 53-2-0. TREATED & PRIMED AREA IAW DC8 SRM 51-1-8 CPCP 557R 0551. 2 L 7 4 4F 4A25 2007022000037 20070220 00037 WP 2007 2 20 N921R50502 1 20070106 A 5542 SKIN DOUG DC8 DC863F 302198F WP RUDDER DENTED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 921R 46145 RUDDER ZR 138 LEFT SKIN AFT SECTION WITH DENT. REMOVED LT SKIN SECTION IAW DPS 3.67-27. FABRICATED NEW SKIN IAW DPS 3. 69-4. TREATED AND PRIMED AREA AND NEW SKIN IAW DC8 SRM 51-1-8. INSTALLED NEW SKIN IAW DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 2007022000038 20070220 00038 EA 2007 2 20 TRAX200700195 1 20070208 A 3250 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA STEERING SYS ACTIVATED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 848AS 7339 AFTER SELECTING GEAR DOWN FOR APPROACH, STEERING INOP MSG APPEARED. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007022000039 20070220 00039 WP 2007 2 20 N921R53506 1 20070108 A 5280 SKIN DOUG DC8 DC863F 302198F WP NLG DOOR DAMAGED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 921R 46145 FUSELAGE STA 32 NLG DOOR SKIN HAS 2 NICKS. REPAIRED SKIN OF FUSELAGE STA 32 NLG RT DOOR IAW DC8 SRM 52-2-0 CPCP 4000 05 51. 2 L 7 4 4F 4A25 2007022000043 20070220 00043 EA 2007 2 20 TRAX200700215 1 20070211 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 828AS 7213 LEFT FWD EXTERIOR EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007022000045 20070220 00045 EA 2007 2 20 TRAX200700217 1 20070211 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT LOW A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 878AS 7590 CAPTAINS FLASHLIGHT IS VERY DIM. 2 L 7 2 4F RT A21EA 2007022000047 20070220 00047 EA 2007 2 20 TRAX200700204 1 20070209 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 820AS 7188 FS 484 ANGLE CRACKED O/B SIDE OF FLOORBEAM AT LBL 27.0 (MARKED). 2 L 7 2 4F RT A21EA 2007022000051 20070220 00051 EA 2007 2 20 TRAX200700208 1 20070209 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 820AS 7188 RIGHT WING PLANK CRACKED ON WS 148 COMMON TO AFT SPAR FLANGE. PERFORMED REPAIR ON R/H LOWER WING PLANK AFT AT WS 148.01 9, IAW REO 601R-57-21-130. (EMP 752 - INSP RA333) ALL WORK DONE IAW ASA EO 600-57-13402. (EMP 818 - INSP RA189) FUEL LEA K CHECK REQUIRED. LEAK CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. (INSP RA318) (RII - 5000528 - FOR REPAIR.) (RII - 5001 437 - FOR FUEL LEAK CHECK) 2 L 7 2 4F RT A21EA 2007022000053 20070220 00053 EA 2007 2 20 TRAX200700210 1 20070209 A 5320 FLOOR SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 820AS 7188 PRESSURE FLOOR SKIN UNDER FLOORBOARD 261 DRF HAS SEVERAL AREAS OF SURFACE CORROSION I/B OF DADO PANEL. 2 L 7 2 4F RT A21EA 2007022000062 20070220 00062 EA 2007 2 20 TRAX200700190 1 20070207 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 976EV 7601 FLOOR EMERGENCY TRACK LIGHTING INOP. 2 L 7 2 4F RT A21EA 2007022000065 20070220 00065 EA 2007 2 20 TRAX200700191 1 20070207 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA CABIN SMOKE A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 755EV 10185 AFTER TAKEOFF FROM MCN CABIN FILLED WITH BURNING OIL SMELL AND HAZE. FWD LAV SMOKE CAME ON. CABIN CLEARED OF SMELL. W HEN POWER REDUCED TO DESCEND INTO ATL, SMOKE CAME BACK, WENT AWAY ON APU BLEED. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007022000066 20070220 00066 WP 2007 2 20 N921R53410 1 20070108 A 5310 DOOR FRAME DOUG DC8 DC863F 302198F WP NLG DOOR CRACKED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 921R 46145 FUSELAGE STA 8 NLG W/W DOOR JAMB RT CORNER SKIN WITH 1" CRACK. REPAIRED SKIN IAW FLIGHT VEHICLES CONSULTING INC DWG NR 51-07030-1 REV NEW 01-25-07 PAGE 1 AND 2. ISSUED FAA FORM 8110-3 CPCP 4000 0551. 2 L 7 4 4F 4A25 2007022000076 20070220 00076 EA 2007 2 20 TRAX200700193 1 20070207 A 5210 LATCH CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 841AS 7300 MAIN DOOR LATCH VERY HARD TO DISENGAGE AND HANDLE VERY HARD TO TURN FROM OUTSIDE THE AIRCRAFT. 2 L 7 2 4F RT A21EA 2007022000078 20070220 00078 NM 2007 2 20 CALA0700055 1 20070207 A 5315 7075T76511 FLOORBEAM BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18243 28806 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 50 TO RBL 50. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01443. 2 L 7 2 4F RT A16WE 2007022000079 20070220 00079 NM 2007 2 20 CALA0700056 1 20070207 A 5330 6545800 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14358 23943 INSPECTION FOUND A 1.875 INCH CRACK IN FORWARD GALLEY DOOR CUTOUT LOWER CORNER FUSELAGE FRAME SKIN, STA 330, L17R. AN I NTERIM REPAIR WAS PERFORMED IAW ECRA 5331-01286 AND A DIP WAS ISSUED TO ACCOMPLISH A REPEAT INSPECTION WITH AN INTERVAL NOT TO EXCEED 60,000 FLIGHT CYCLES AND AT SUBSEQUENT INTERVALS NOT TO EXCEED 24,000 FLIGHT CYCLES. 2 L 7 2 4F RT A16WE 2007022000082 20070220 00082 NM 2007 2 20 CALA0700068 1 20070215 A 5315 147A5506 FLOORBEAM BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14237 28802 INSPECTION FOUND FLOORBEAM CORRODED AROUND FASTENER HOLES AT STA 986, BL 0 TO LBL 31. THE FLOORBEAM WAS REPAIRED IAW EC RA 5321-01445. 2 L 7 2 4F RT A16WE 2007022000083 20070220 00083 NM 2007 2 20 CALA0700066 1 20070215 A 5313 6545769 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 INSPECTION FOUND CENTER OF STRINGER 27L CORRODED AROUND NUT PLATE IN FORWARD BAGGAGE BIN AT STA 500D. THE STRINGER WAS REPAIRED IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 2007022000084 20070220 00084 EA 2007 2 20 COMA0760161 1 20070206 A 2752 854D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA RT FLAP FAULTY A COMA K NONE J WARNING INDICATION CR CRUISE 1 SO 01 812CA 9861 7381 FLIGHT 5331 - EN ROUTE BOS-YHZ RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOU T INCIDENT. REPLACED THE RIGHT OUTBOARD FLAP OUTBOARD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2007022000085 20070220 00085 EA 2007 2 20 COMA0760162 1 20070206 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA RT FLAP FAULTY A COMA K NONE J WARNING INDICATION CR CRUISE 1 SO 01 812CA 11909 7381 FLIGHT 5331 - EN ROUTE BOS-YHZ RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOU T INCIDENT. REPLACED THE RIGHT BRAKE POSITION SENSING UNIT. 2 L 7 2 4F RT A21EA 2007022000086 20070220 00086 EU 2007 2 20 NSVA20070005 1 20070109 A 7931 UNKNOWN SAAB SF340 340B 7860101 EU OIL PRESS SYS UNKNOWN A NSVA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 204CJ 204 L ENGINE OIL PRESSURE LIGHT ILLUMINATED ON TAKEOFF ROLL. TAKEOFF ABOUT AT LOW SPEED APPROX 20KTS. CHECKED ENGINE OIL A DDED 1 QUART AT 2380 TO BRING ENGINE OIL TO FULL LINE. CHECKED GEAR BOX OIL SIGHT GLASS NO SERVICE NEEDED. CLEANED OIL PRESSURE SENSORS CONNECTEOR WITH CONTRACT CLEANER AND RECONNECTED ENGINE RUN UP BY CREW SHOWED NORMAL OIL PRESSURE AND NO WARNING LIGHT SENSORS CHECKED AND REPLACED IAW 79-30-05-05 AND 79-30-05-10. 2 L 7 2 4T RT A52EU 2007022000087 20070220 00087 EU 2007 2 20 NSVA20070006 1 20070110 A 7931 IPTE119100200 PRESSURE SWITCH SAAB SF340 340B 7860101 EU LT ENGINE MALFUNCTIONED A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 204CJ 204 LEFT ENG OIL PRESS LIGHT ILLUMINATED. REMOVED AND REPLACED PGB PRESSURE SWITCH IAW SAAB AMM 79-30-05-04. OPS CHECK GOO D MEL NR 23579. 2 L 7 2 4T RT A52EU 2007022000088 20070220 00088 EU 2007 2 20 NSVA20070007 1 20070112 A 3230 D49412001 CONTROL PANEL SAAB SF340 340B 7860101 EU MLG UNKNOWN A NSVA O OTHER J WARNING INDICATION CL CLIMB 1 EA 27 339CJ 339 GEAR IN TRAN LIGHT WOULD NOT EXTINGUISH, FL 112262. ALSO HAD TO USE DOWN LOCK RELEASE TO GET THE GEAR UP. ALL THREE GEAR LIGHT (GREEN) LIGHT REMAINED ON. FOUND GEAR CONTROL CB POPPED RESET AND SWING GEAR SEVERAL TIMES WITHOUT FAILURE R EPLACED LANDING GEAR CONTROL PANEL IAW MM 32-31-05. RETRACTION FUNCTIONAL TEST GOOD IAW MM 32-30-00, PN ON/OFF D494-12- 001, SN ON 0631084 SN OFF 3321190. 2 L 7 2 4T RT A52EU 2007022000090 20070220 00090 EA 2007 2 20 COMA0760163 1 20070207 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 926CA 7027 FLIGHT 5528 - FLAP FAIL MESSAGE RECEIVED ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH AD 20 06-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C) FLAP SYSTEM WAS RESET WI TH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2007022000091 20070220 00091 EA 2007 2 20 COMA0760164 1 20070207 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 931CA 7037 FLIGHT 5120 - FLAP FAIL MESSAGE RECEIVED ON APPROACH, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH AD 200 6-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C) FLAP SYSTEM WAS RESET WI TH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2007022000093 20070220 00093 EA 2007 2 20 COMA0760165 1 20070207 A 5210 SEAL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OBSTRUCTED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 810CA 7370 FLIGHT 5233 - VERY LOUD HISS COMING FROM BOTTOM OF MAIN CABIN DOOR. RETURNED TO JFK, LANDED WITHOUT INCIDENT. FOUND IC E ON PAX DOOR SEAL. REMOVED ICE FROM SEAL AND PERFORMED PRESSURIZATION CHECK. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007022000095 20070220 00095 EA 2007 2 20 COMA0760170 1 20070208 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA LT FLAP FAILED A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 987CA 9029 7199 FLIGHT 5306 - FLAPS FAIL MESSAGE ON GROUND, FLAPS FAILED AT 0 DEGRESS. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATORS (FAILED LOW TEMP TORQUE CHECK). 2 L 7 2 4F RT A21EA 2007022000096 20070220 00096 EA 2007 2 20 COMA0760171 1 20070208 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA LT FLAP FAILED A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 987CA 9029 7199 FLIGHT 5306 - FLAPS FAIL MESSAGE ON GROUND, FLAPS FAILED AT 0 DEGREES. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATORS . FAILED LOW TORQUE CHECK. 2 L 7 2 4F RT A21EA 2007022000097 20070220 00097 EA 2007 2 20 COMA0760117 1 20070131 A 2752 853D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA LT WING FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 806CA 2966 7359 FLIGHT 5375 - DURING YHZ APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. REPLACED THE LEFT OUTBOARD FLAP OUTBOARD ACTUA TOR. 2 L 7 2 4F RT A21EA 2007022000098 20070220 00098 EA 2007 2 20 COMA0760125 1 20070203 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 477CA 7670 FLIGHT 5237 - AFTER LANDING AT CVG RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSA GE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTIO N MESSAGES. 2 L 7 2 4F RT A21EA 2007022000099 20070220 00099 EA 2007 2 20 COMA0760126 1 20070203 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 479CA 7675 FLIGHT 5480 - DURING MSN APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WIT HOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007022000101 20070220 00101 EA 2007 2 20 COMA0760173 1 20070209 A 2916 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYS CONTAMINATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 814CA 7387 FLIGHT 5579 - RECEIVED HYD SYSTEM NR 3 LOW PRESSURE WARNING ON TAKEOFF ROLL. ABORTED TAKEOFF BELOW 80 KTS. RETURNED TO GATE WITHOUT INCIDENT. FOUND EXCESSIVE AIR IN NR 3 HYD RESERVOIR. BLED AND SERVICED RESERVOIR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007022000107 20070220 00107 EA 2007 2 20 COMA0760160 1 20070205 A 2752 1104SD100501 FLEX DRIVE CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP BENT A COMA K NONE J WARNING INDICATION DE DESCENT 1 SO 01 436CA 7482 FLIGHT 5294 - FLAP FAIL ON DESCENT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LEFT WING NR 5 FLEX DRIVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007022000110 20070220 00110 EU 2007 2 20 NSVA20070011 1 20070115 A 7931 CONNECTOR SAAB SF340 340B 7860101 EU OIL PRESS XDUCER DIRTY A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 204CJ 204 FOUND LEFT ENGINE OIL PRESSURE LIGHT ON DURING TAKEOFF. REMOVED, CLEANED AND REINSTALLED ENG LT OIL PRESSURE TRANSDUCER CONNECTOR. PERFORMED OPS CHECK IAW AMM 72-00-00. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2007022000112 20070220 00112 WP 2007 2 20 AALA20070249 1 20070203 A 3213 STRUT DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 586AA 53249 ORD INFLIGHT T1766/03FEB - DURING GEAR RETRACTION GEAR HANDLE WOULD ONLY COME UP HALF WAY. ON THIRD ATTEMPT TO RAISE GE AR THE HANDLE CAME FULL UP AND THE NOSE GEAR RED INDICATION LIGHT ILLUMINATED. GEAR DOOR OPEN LIGHT WAS EXTINGUISHED. HEARD LOUD NOISE COMING FROM NOSE GEAR AREA. AFTER A FEW MINUTES NOISE STOPPED AND ALL INDICATION LIGHTS EXTINGUISHED. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. INSPECTED AND REPACKED NOSE STRUT. SYSTEM GROUND CHECKED NORMAL OPERATIO N. 2 L 7 2 4F A6WE 2007022000113 20070220 00113 NM 2007 2 20 AALA20070238 1 20070202 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 919AN 29520 MIA - FOUND EMERGENCY EXIT LIGHT AT AFT LEFT OVERWING LIGHT BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY FOR EMERGENCY EXI T LIGHT AT AFT LEFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007022000114 20070220 00114 WP 2007 2 20 AALA20070245 1 20070202 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 970TW 53620 LGA - FOUND EMERGENCY PORTABLE LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY PORTABL E LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007022000115 20070220 00115 NM 2007 2 20 AALA20070246 1 20070202 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 974AN 30098 MIA - FOUND EMERGENCY LIGHT AT SEAT 8D INOPERATIVE. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 8D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007022000116 20070220 00116 WP 2007 2 20 AALA20070240 1 20070202 A 3213 59632541 PISTON DOUG DC9 DC983 3022083 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 983TW 53633 ORD INFLIGHT T1637/02FEB - RECEIVED UNSAFE NOSE GEAR UP INDICATION. COULD HEAR LOUD NOISE WHEN GEAR WAS RETRACTED. SU SPECTED GEAR DOORS WERE OPEN. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR STRUT PISTON. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007022000117 20070220 00117 WP 2007 2 20 AALA20070231 1 20070131 A 3213 STRUT DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 255AA 49287 ORD INFLIGHT T2329/31JAN - GEAR UNSAFE LIGHT ILLUMINATED DURING RETRACTION. CYCLED GEAR WITH NO HELP. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. DOWN AND LOCKED INDICATIONS WERE GOOD. REPLACED NOSE LANDING GEAR STRUT. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007022000118 20070220 00118 EA 2007 2 20 COMA0760123 1 20070202 A 3097 WIRE CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYSTEM CHAFED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 983CA 7169 FLIGHT 5104 - DURING TAKE-OFF ROLL RECEIVED AN ANTI-ICE DUCT CAUTION MESSAGE, ABORTED TAKE-OFF AND RETURNED TO THE GATE. REPAIRED CHAFED WIRING AT SENSOR SW25K IN THE LEFT WING AND REPOSITION TERMINAL LUG TO PREVENT CHAFING. 2 L 7 2 4F RT A21EA 2007022000119 20070220 00119 WP 2007 2 20 AALA20070229 1 20070131 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 588AA 53251 SFO - FOUND EMERGENCY LIGHT AT SEAT 18D INOPERATIVE. REPINNED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007022000122 20070220 00122 EA 2007 2 20 COMA0760124 1 20070203 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 916CA 7014 FLIGHT 5453 - DURING DSM APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WIT HOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007022000123 20070220 00123 WP 2007 2 20 AALA20070232 1 20070131 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 967TW 53617 LGA - EMERGENCY ESCAPE PATH SEAT LIGHT IN FORWARD SECTION OF CABIN INOPERATIVE. REPLACED BATTERY PACK AT AB5-2 FOR EMER GENCY ESCAPE PATH SEAT LIGHT IN FORWARD SECTION OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007022000124 20070220 00124 NM 2007 2 20 AALA20070252 1 20070203 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 760AN 31477 DFW - WALL MOUNTED EMERGENCY LIGHT AT LEFT AFT GALLEY WALL HAS MISSING LENS. REPLACED LENS FOR WALL MOUNTED EMERGENCY L IGHT AT LEFT AFT GALLEY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007022000125 20070220 00125 EA 2007 2 20 COMA0760181 1 20070212 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 940CA 7048 FLIGHT 5448 - DURING BGR APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAG E -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C) FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2007022000126 20070220 00126 EA 2007 2 20 COMA0760182 1 20070212 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 818CA 2042 7408 FLIGHT 5550 - EMERGENCY LIGHTING FAILED TEST. REPLACED EMERGENCY LIGHTING BATTERY PACK. 2 L 7 2 4F RT A21EA 2007022000128 20070220 00128 WP 2007 2 20 AALA20070241 1 20070202 A 2130 VALVE DOUG DC9 DC982 3022082 WP AIR CONDITIONING INOPERATIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 90511 49805 DFW INFLIGHT T1119/02FEB RECEIVED PRESSURE FLOW INDICATION FOLLOWED BY REPORT FROM FLIGHT ATTENDANTS OF SMELL AND HAZE IN MAIN CABIN AREA. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED LEFT PACK REGULATORY SHUT OFF VALVE AND ACCO MPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007022000130 20070220 00130 EA 2007 2 20 COMA0760183 1 20070212 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 818CA 17299 7408 FLIGHT 5550 - EMERGENCY LIGHTING FAILED TEST. REPLACED EMERGENCY LIGHTING BATTERY PACK. 2 L 7 2 4F RT A21EA 2007022000131 20070220 00131 NM 2007 2 20 AALA20070247 1 20070202 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 974AN 30098 MIA - FOUND EMERGENCY LIGHT AT SEAT 8D INOPERATIVE. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 8D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007022000132 20070220 00132 WP 2007 2 20 AALA20070233 1 20070131 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 967TW 53617 LGA - FOUND EMERGENCY ESCAPE PATH SEAT LIGHTS IN AFT CABIN SECTION INOPERATIVE. REPLACED BATTERY PACK AT AB53 FOR EMERG ENCY ESCAPE PATH SEAT LIGHTS IN AFT CABIN SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007022000133 20070220 00133 EA 2007 2 20 COMA0760184 1 20070212 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 818CA 19405 7408 FLIGHT 5550 - EMERGENCY LIGHTING FAILED TEST. REPLACED EMERGENCY LIGHTING BATTERY PACK. 2 L 7 2 4F RT A21EA 2007022000134 20070220 00134 WP 2007 2 20 AALA20070234 1 20070131 A 2560 STRAP DOUG DC9 DC983 3022083 WP FLASHLIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 967TW 53617 LGA - EMERGENCY FLASHLIGHT FORWARD STRAP BROKEN. REPLACED EMERGENCY FLASHLIGHT FORWARD STRAP. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A6WE 2007022000135 20070220 00135 WP 2007 2 20 AALA20070235 1 20070131 A 3350 P4010051111 MODULE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 436AA 49454 LGA - FOUND AFT EMERGENCY EXIT FLOOR LIGHT FROM AFT MODULE AB54 INOPERATIVE. REPLACED CONTROL MODULE AND BATTERY FOR AF T EMERGENCY EXIT FLOOR LIGHT FROM AFT MODULE AB54. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007022000137 20070220 00137 EA 2007 2 20 COMA0760185 1 20070212 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 818CA 13394 7408 FLIGHT 5550 - EMERGENCY LIGHTING FAILED TEST. REPLACED EMERGENCY LIGHTING BATTERY PACK. 2 L 7 2 4F RT A21EA 2007022000139 20070220 00139 EU 2007 2 20 AALA20070257 1 20070203 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70072 515 MIA - FOUND EMERGENCY LIGHT AT SEAT 11C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 11C. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A35EU 2007022000140 20070220 00140 EU 2007 2 20 AALA20070260 1 20070203 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70072 515 MIA - FOUND EMERGENCY LIGHT AT SEAT 23G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 23G. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A35EU 2007022000141 20070220 00141 EU 2007 2 20 AALA20070256 1 20070203 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70072 515 MIA - FOUND EMERGENCY LIGHT AT SEAT 5C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 5C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007022000143 20070220 00143 EU 2007 2 20 AALA20070259 1 20070203 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70072 515 MIA - FOUND EMERGENCY LIGHT AT SEAT 10G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 10G. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A35EU 2007022000144 20070220 00144 EU 2007 2 20 AALA20070261 1 20070203 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70072 515 MIA - FOUND EMERGENCY LIGHT AT SEAT 37C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 37C. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A35EU 2007022000145 20070220 00145 EA 2007 2 20 COMA0760172 1 20070209 A 5270 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DIRTY A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 989CA 7215 FLIGHT 5463 - AIRCRAFT RETURNED TO JFK AFTER TAKEOFF DUE TO A RED CABIN DOOR WARNING MESSAGE. CLEANED THE CABIN DOOR PR OXIMITY SWITCH AND CLEANED THE UPPER DOOR CAM ROLLERS. 2 L 7 2 4F RT A21EA 2007022000146 20070220 00146 EU 2007 2 20 AALA20070262 1 20070203 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70072 515 MIA - FOUND EMERGENCY LIGHT AT SEAT 34C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 34C. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A35EU 2007022000148 20070220 00148 WP 2007 2 20 AALA20070255 1 20070203 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7547A 53029 LGA - FOUND EMERGENCY PATH LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY PATH LIGHTS IN FORW ARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007022000149 20070220 00149 EA 2007 2 20 COMA0760175 1 20070211 A 3510 OXYGEN SYSTEM CNDAIR CL600 CL6002B19 1900309 EA LEAKING A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 710CA 7241 FLIGHT 4941- EN ROUTE YYZ-JFK DISCOVERED A CREW OXYGEN SUPPLY LEAK, FLIGHT DIVERTED TO AVP. SERVICED THE CREW OXYGEN SY STEM. 2 L 7 2 4F RT A21EA 2007022000150 20070220 00150 WP 2007 2 20 AALA20070248 1 20070202 A 3213 SEAL DOUG DC9 DC983 3022083 WP NLG STRUT INOPERATIVE A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 966TW 53616 DTW INFLIGHT T2265/02FEB - NOSE LANDING GEAR FAILED TO RETRACT. RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING HEAR SHOCK STRUT SEAL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007022000151 20070220 00151 NM 2007 2 20 AALA20070224 1 20070130 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 358AA 24039 MIA - FOUND EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007022000152 20070220 00152 NM 2007 2 20 DHL2007781001 1 20070214 A 5310 WINDOW POST BOEING 727 727227 1384078 NM BS 219 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 781DH 21996 CAPT'S WINDSHIELD EXT, O/B POST UPPER CORNER IS CRACKED. GAINED ACCESS AS REQ TO ACCOMPLISH REPAIR. STOP DRILLED CRACK , .250" HOLE, PER B727 SRM 51-10-1. VERIFIED CRACK TERMINATION, HFEC METHOD, PER B727 SDT MAN PT 6, 51-00-00. FABRICAT ED REPAIR DOUBLER FROM 2024-T0, .090" BY 9" BY 7", PO NR 991753, PER B727 SRM 53-30-3 FIG 8. HEAT TREATED DOUBLER TO T4 CONDITION PER FASI FORM FAS0113 REV 6. TREATED, PRIMED, AND INSTALLED DOUBLER PER B727 SRM 51-10-2, AND 53-30-3 FIG 8. RETURNED AREA TO NORMAL. 2 L 7 3 4F A3WE 2007022000155 20070220 00155 NM 2007 2 20 AWXA200700207 1 20070205 A 5755 D5755104020000 HINGE PIN AIRBUS A319 A319132 3930340 NM ZONE 600 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 831AW 1576 SAL - FOUND RIGHT WING NR 2 SPOILER OUTBOARD HINGE PIN WORN. REPLACED RIGHT WING NR 2 SPOILER OUTBOARD HINGE PIN IAW AW A TASK CARD C3R57323. 2 L 7 2 4F RT A28NM 2007022000157 20070220 00157 EU 2007 2 20 07FDEA00466 1 20070213 A 7830 UNKNOWN AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680 30025 NE THRUST REVERSER UNKNOWN A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 662FE 761 705239 ON TAKEOFF ROLL, ECAM MESSAGE ENG NR 2 REV PRESSURIZED APPEARED, STOPPED TAKEOFF AND RETURNED GATE. ACN RELEASED FOR SE RVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 23FEB07 "MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) 2 THRUST REVERSE R, INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION. A/C DEPARTED TUL. 2 L 7 2 4F 4 F RT A35EU E13NE 2007022000159 20070220 00159 EA 2007 2 20 COMA0760178 1 20070211 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 804CA 7352 FLIGHT 5052 - RECEIVED FLAPS FAIL MESSAGE ON APPROACH. LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTI ON MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C) FLAP SYSTEM WAS RESET WITH NO FURTHER MESS AGES. 2 L 7 2 4F RT A21EA 2007022000160 20070220 00160 EU 2007 2 20 07FDEA00469 1 20070213 A 5310 STRUCTURE AIRBUS 310 A310203 3930313 EU FUSELAGE MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 PREVIOUS REPAIR, AFT CABIN UNDERFLOOR BEHIND BULK CARGO HAS REPAIR ON STR 56 RT, WITH 1. REPAIR SPLICE MEASURING 7.7 IN LONG AND STRINGER REPAIR SECTION MEASURES 26.5 IN LONG BETWEEN FR72 AND FR74 ZONE 170 REPAIR WAS NOT IAW A310 SRM 53-10 -14 FIG 201. AREA REPAIRED CORRECTLY IAW A310 SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007022000161 20070220 00161 EU 2007 2 20 07FDEA00470 1 20070213 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 407FE 254 PREVIOUS REPAIR, MAIN CABIN SEAT TRACK 4 RT HAS REPAIR WITH 2 EACH REPAIR ANGLES MEASURING 9.5 IN LONG EACH, BETWEEN FR7 4 AND FR75 ZONE 260. REPAIR AREA WAS NOT IAW A310 SRM 53-10-16 FIG 201. AREA REPAIRED CORRECTLY IAW A310 SRM 53-10-1 6 FIG 201 AND COMPLIED WITH EA 6-5320-107640. 2 L 7 2 4F RT A35EU 2007022000162 20070220 00162 EU 2007 2 20 07FDEA00471 1 20070213 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 407FE 254 PREVIOUS REPAIR MAIN CABIN FLOORBEAM FR 54.3 HAS FLOORBEAM SPLICE SECT REPAIR BETWEEN SEAT TRACKS 3 AND 5 LT, SPLICE SEC TION MEASURES 19.9 IN LONG 4EACH REPAIR SPLICE ANGLES 8.8 IN LONG EACH LOCATED ON THE AFT FACE ONLY OF FLOORBEAM ZONE 15 0. REPAIR AREA WAS NOT IAW A310 SRM SUPPLEMENT 53-10-15 FIG 201 SHEET 8. AREA REPAIRED CORRECTLY IAW A310 SRM SUPPLEME NT 53-10-15 FIG 201 SHEET 8 AND EA 6-5310-107661. 2 L 7 2 4F RT A35EU 2007022000163 20070220 00163 EU 2007 2 20 07FDEA00472 1 20070213 A 5347 60224577075T6511 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 MDC FOUND SEAT TRACK NR 2 LT FR 67 IS CORRODED AND GOUGED. REPAIRED SEAT TRACK IAW A310 SRM 53-10-16 FIG 208 SHEET 1. SPLICE REPAIR. 2 L 7 2 4F RT A35EU 2007022000164 20070220 00164 EU 2007 2 20 07FDEA00473 1 20070213 A 5347 60224577075T6511 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 MDC FOUND SEAT TRACK NR 2 LT BTN FR72.5 TO FR 73.5 HAS CORROSION. REMOVED CORROSION IAW A310 SRM 51-74-10 AND CHECKED L IMITS PER SRM 53-10-16 AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK NR 3L FR71.5 - FR73.5 IAW A310- 200 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007022000166 20070220 00166 EU 2007 2 20 07FDEA00474 1 20070213 A 5330 SKIN AIRBUS 310 A310203 3930313 EU FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 407FE 254 PREVIOUS REPAIR, LWR RT SIDE FUS SKIN BELOW BULK CARGO DOOR EXTERNAL REPAIR DOUBLER BETWEEN FR67 AND FR68 STR 49 RT TO S TR 52 RT, MEASURING 8.8 IN BY 8.4 IN ZONE 160. REPAIR AREA WAS NOT IAW A310 SRM 53-10-12 FIG 225 SHEET 1. AREA REPAIRE D CORRECTLY IAW A310 SRM 53-10-12 FIG 225 SHEET 1. 2 L 7 2 4F RT A35EU 2007021500202 20070215 00202 EA 2007 2 15 TRAX200700184 1 20070206 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 640 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 886AS 7531 SUSPECT CRACK ON LEFT SIDE FS 640 FRAME. 2 L 7 2 4F RT A21EA 2007021600007 20070216 00007 NM 2007 2 16 DL777070121 1 20070211 A 3320 285W00294 ELECTRONIC UNIT BOEING 777 777232 1385232 NM 3R DOOR O/H INOPERATIVE A DALA O OTHER O OTHER CR CRUISE 1 SO 27 865DA 29737 WORK LIGHTS INOPERATIVE AT 3L/3R. OEU M23406 AT 3R DOOR FAILED ON CABIN ALL TEST. FOUND OEU SHOWS EVIDENCE OF BURN MAR K. REMOVED AND REPLACED OEU. COULD NOT COMPLETE SOFTWARE UPLOAD. FWD OEU SOFTWARE LOAD TOMCO AND PLAC PER MEL 25-20-0 1I. LOADED CONFIG AND DATABASE SOFTWARE TO OEU LIGHTS OP NORMAL MCO AND PLACARD REMOVED. 2 L 7 2 4F RT T00001SE 2007021600008 20070216 00008 NM 2007 2 16 DLM90070123 1 20070211 A 5510 BOLT DOUG MD90 MD9030 3023690 NM RT HORZ STAB BROKEN A DALA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 SO 27 907DA EFS005 53387 RT MANUAL REVERSION CYLINDER HOUSING BOLTS BROKE AND THE HOUSING BODY CAME APART CAUSING BOTH HYDRAULIC SYSTEMS TO LOSE QUANTITY. THIS RESULTED IN LOSS OF STEERING AND BRAKING DURING TAXI TO GATE AFTER LANDING. AIRCRAFT WAS MET ON THE TAX IWAY AND TOWED TO THE GATE BY MAINTENANCE. REMOVED RT REVERSION CYL 453597. INSTALLED MANUAL REVERSION ACTUATOR PER MM 27-33-09-420-801 TO STEP G 223122. OPS CK LEAK FUNCTIONAL RTS PER MMR. INSP C/W QC50. 2 L 7 2 4F RT A6WE 2007021600012 20070216 00012 NM 2007 2 16 DLM88070130 1 20070214 A 2720 PULLEY DOUG MD88 MD88 3023688 NM LT RUDDER PEDAL OBSTRUCTED A DALA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 27 931DL 49718 DURING FLIGHT CONTROL CHECK, LEFT RUDDER PEDAL WAS STUCK. RIGHT PEDAL DEFLECTION NORMAL. NOSE WHEEL STEERING NORMAL. ALL HYD PRESS GOOD. PEDAL CAME FREE WITH A LOUD SNAP INSIDE RUDDER HOUSING ON CAPTS SIDE. NOW CHECKS NORMAL OPEN NOSE GEAR DOORS AND NOSE GEAR COMPARTMENT FOR INSPECTION OF RUDDER PEDAL. ALSO, REMOVED INSULATION WALL FOR INSPECTION 71324 9 FOUND AND REMOVED DEBRIS FROM BOTH LOCKOUT CAM/ROD ASSY AND PULLEY. CK CABLES PULLEYS ETC. NO OTHER DISCREPANCIES 2 L 7 2 4F RT A6WE 2007021600015 20070216 00015 NM 2007 2 16 2007UALA00329 1 20070205 A 5315 STRAP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FLOORBEAM CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 87UA 26713 LEFT NOSE TUNNEL BS 365, LBL 24, CABIN FLOORBEAM STRAP CRACKED 2 PLACES, JUST FWD OF PRIOR REPAIR. FABRICATED AND INS TALLED REPAIR DOUBLER-STRAP USING UA SPECIFICATION AND BACO DWG. 2 L 7 2 4F 4 F RT A2NM E17NE 2007021600031 20070216 00031 NM 2007 2 16 2007UALA00345 1 20070207 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 947 MISDRILLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 349UA 24253 AFT CABIN AREA CREASE BEAM WEB HAS A MISDRILLED HOLE 6 INCHES AFT OF BS 947 RBL 55. MAJOR REPAIR, REMOVED DAMAGE AND IN STALLED DOUBLER REPAIR PER SRM 51-70-13 PAGES 1-3. 2 L 7 2 4F 4 F RT A16WE E21EU 2007021600054 20070216 00054 2007 2 16 SWAA070806 4 20070214 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 423WN 29827 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007021600072 20070216 00072 EU 2007 2 16 AALA20070264 1 20070203 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70072 515 MIA - FOUND EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A35EU 2007021600073 20070216 00073 EU 2007 2 16 AALA20070265 1 20070203 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70072 515 MIA - FOUND EMERGENCY LIGHT ASSEMBLY AT SEAT 13G IS BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 13G. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007021600077 20070216 00077 NM 2007 2 16 SWAA070810 1 20070214 A 5311 6546564 FRAME BOEING 737 7373H4 1384600 NM BS 986 S27L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 986, STR 27L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007021600078 20070216 00078 NM 2007 2 16 SWAA070857 1 20070214 A 5315 6546812 FLOORBEAM BOEING 737 7373T5 1384608 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM WEB CORRODED AT BS 986, RBL 50. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007021600085 20070216 00085 NM 2007 2 16 SWAA070828 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 727A S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600100 20070216 00100 NM 2007 2 16 SWAA070849 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 500C S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600102 20070216 00102 NM 2007 2 16 SWAA070847 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 520 S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600107 20070216 00107 NM 2007 2 16 SWAA070832 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 685 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007021600111 20070216 00111 NM 2007 2 16 SWAA070836 1 20070214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 616 S2R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000018 20070220 00018 2007 2 20 AMTA200700058 4 20070203 A 3460 4058650950 CDU BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT UNSERVICEABLE A AMTA K NONE J WARNING INDICATION IN INSP/MAINT 1 GL 11 519AT 27975 RT CDU INOPERATIVE. REPLACED CDU REF MM 34-61-02. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007022000022 20070220 00022 NM 2007 2 20 ASAA0741445 1 20070209 A 2560 66242731 STOP BOEING 737 7374Q8 138447Q NM R2 DOOR WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 R2 SLIDE PACK LOOSE. R2 SLIDE PACK LOWER ATTACH FITTING DOES NOT ENGAGE FITTING ON DOOR. REMOVED AND REPLACED R2 SLIDE ASSY PER MM 25-61-35. REMOVED AND REPLACED R2 DOOR LINER ASSY PER MM 52-41-31. SHIMMED R2 DOOR SLIDE SUPPORT ASSY STO P EO 2560 01395. SLIDE ASSY SEATED AGAINST DOOR LINER. 2 L 7 2 4F RT A16WE 2007022000030 20070220 00030 WP 2007 2 20 N921R63504 1 20070109 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 78 S17-18L DENTED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 921R 46145 FOUND FUSELAGE EXTERIOR STA 78 BTW L-17L AND L-18L SKIN WITH DENT. REPAIRED SKIN OF FUSELAGE EXTERIOR STA 78 BTW L-17L AND L-18L IAW DC8 SRM 53-2-0, TR NR 53-170 CPCP 5000-0551. 2 L 7 4 4F 4A25 2007022000031 20070220 00031 EA 2007 2 20 TRAX200700152 1 20070202 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA CABIN WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 ASD EXIT PLACARD WORN AND PEELING. 2 L 7 2 4F RT A21EA 2007022000040 20070220 00040 EA 2007 2 20 TRAX200700196 1 20070208 A 2560 MEGAPHONE CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 744EV 10157 MSP--MEGAPHONE INOP. FLT 4215 CX. 2 L 7 2 4F RT A21EA 2007022000041 20070220 00041 EA 2007 2 20 TRAX200700197 1 20070208 A 2930 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYS ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 858AS 7417 HYD SYS 2 LO PRESS MSG, HYD SYS 2 QTY INDS ZERO. EN ROUTE TO HSV, A/C DIVERTED TO GSO DUE TO MTC. EMERGENCY DECLARED. FLTS 4539, 4586 CX. 2 L 7 2 4F RT A21EA 2007022000044 20070220 00044 EA 2007 2 20 TRAX200700216 1 20070211 A 7900 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE FLUCTUATES A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 875AS 7559 RIGHT ENGINE OIL PRESSURE FLUX. AIRCRAFT RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. FLTS 4084, 4401 CX. 2 L 7 2 4F RT A21EA 2007022000050 20070220 00050 EA 2007 2 20 TRAX200700207 1 20070209 A 5312 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 820AS 7188 CRACK THRU 2 FASTENERS ON AFT PRESS BULKHEAD INTERCOSTAL AT FS 623.00 LBL 51.5 STR 13L VERT FANGE OF INTERCOSTAL REQ'S C RACK LENGTH VERIFICATION. SERVICE BULLETIN 601R-53-048, FUSELAGE GENERAL VISUAL INSPECTION OF THE INTERCOSTAL MEMBERS AT FS 621/FS625.3 INCORPATED. CRACK MEASURES LESS THAN 1.50 IN LENGTH. OK FOR CONTINUED SERVICE PER REO 601R-53-61-105 A ND SERVICE BULLETIN 601R-53-048. MDA 1064 2-21-07. RA333. 2 L 7 2 4F RT A21EA 2007022000075 20070220 00075 EU 2007 2 20 NSVA20070004 1 20070107 A 2611 CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY NO TEST A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 202SR 202 FOUND CARGO SMOKE TEST FAILED. REMOVED AND REPLACED CARGO AFT SMOKE DETECTOR, OM CARGO OM REF WITH SMM 26-13-15-4. OPS CHECK GOOD, PN ON/OFF CGAB1201-01, SN ON 981, SN OFF 1079. 2 L 7 2 4T RT A52EU 2007022000080 20070220 00080 NM 2007 2 20 CALA0700057 1 20070207 A 5320 147A5660Y21 INTERCOSTAL BOEING 737 737724 13844BY NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24736 28803 INSPECTION FOUND INTERCOSTAL CORRODED AT STA 946-967 (DRAIN SUPPORT), LBL 49. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007022000111 20070220 00111 EU 2007 2 20 NSVA20070012 1 20070116 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 334CJ 334 RT SIDE EMERG EXIT LTS INOP RT SIDE, ROW EMERG FLOOR LTS ROWS 2-7 INOP, LT EMERG FLOOR LTS ROW 7 INOP. EMERGENCY EXIT L IGHTS WERE LEFT ON CAUSING POWER IN BATTERIES TO FALL BELOW MINIMUM VOLTAGE. SUPPLY PC WITH 28 VOLTS EXTERNAL POWER TO CHARGE BATTERIES OPS CHECK OF ALL LIGHTS IS GOOD. 2 L 7 2 4T RT A52EU 2007022000120 20070220 00120 WP 2007 2 20 AALA20070230 1 20070131 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 588AA 53251 SFO - FOUND EMERGENCY LIGHT AT SEAT 27D INOPERATIVE. REPINNED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007022000127 20070220 00127 WP 2007 2 20 AALA20070251 1 20070202 A 4990 5940405503 APU DOUG DC9 DC982 3022082 WP LEAKING A AALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 7536A 49990 TUS INFLIGHT T1926/02FEB - FLIGHT ATTENDANT REPORTED SMOKE IN CABIN FROM COCKPIT TO SEAT ROW 12. TURNED OFF RECIRCULATI ON FAN AND FLIGHT ATTENDANTS THOUGHT SMOKE BEGAN TO DISSIPATE. RETURNED TO TUS AND LANDED WITHOUT INCIDENT. FOUND RIGH T AIR CYCLE MACHINE OIL LEAK AND APU LEAKING OIL. PERFORMED PACK BURN AND FERRIED AIRCRAFT TO DFW FOR REPAIRS. REPLACE D APU AND ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007022000136 20070220 00136 NM 2007 2 20 AALA20070253 1 20070203 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 760AN 31477 DFW - WALL MOUNTED EMERGENCY LIGHT AT LEFT AFT GALLEY BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY FOR WALL MOUNTED LIGHT AT LEFT AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007022000156 20070220 00156 EU 2007 2 20 F3LA200700023 1 20070211 A 3350 321430 BATTERY PACK AIRBUS A318 A318111 3940019 EU EMERGENCY LIGHT DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 805FR 1660 DURING HEAVY CHECK, INSPECTION REPORTED EMERGENCY LIGHT FAILED TEST, 14RU MCDU. REPLACED BATTERY PACK 10WL. OPS CHECKE D GOOD. REF AMM 33-51-38-000-002 AND 33-51-38-400-002. 2 L 7 2 4F RT 2007022000158 20070220 00158 EU 2007 2 20 07FDEA00468 1 20070213 A 5330 SKIN AIRBUS 310 A310222 3930315 EU FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 422FE 346 PREVIOUS REPAIR, LWR RT SIDE FUSELAGE SKIN BELOW BULK CARGO DOOR HAS EXTERNAL REPAIR DOUBLER BETWEEN FR 67 AND FR 68, ST R49 RT TO STR 52 RT, MEASURING 8.8 IN BY 8.4 IN ZONE 160. REPAIR AREA WAS NOT IAW A310 SRM 53-10-12 FIG 225 SHEET 1. A REA REPAIRED CORRECTLY IAW A310 SRM 53-10-12 FIG 225 SHEET 1. 2 L 7 2 4F RT A35EU 2007022000167 20070220 00167 NM 2007 2 20 07FDEA00475 1 20070214 A 5313 ADA8090503 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 FORWARD CARGO COMPARTMENT: BILGE AREA LONGERON 52 AT STA 979 UPPER FLANGE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-533 0-105625, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007022000171 20070220 00171 NM 2007 2 20 QXEA200700137 1 20070130 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 415QX 4081 C2 PDX - UPON REMOVAL OF NR 9 SEAT RAIL FOUND CORROSION AT X781 AROUND RIVET HOLE. REPAIRED IAW SRM 51-14-00, 51-21-10, AND 51-25-10. 2 H 7 2 4T RT A13NM 2007022000172 20070220 00172 NM 2007 2 20 QXEA200700138 1 20070201 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 415QX 4081 C2 PDX - FOUND SEAT TRACK NR 11 HAS LIGHT SURFACE CORROSION AT Y10.5 TO Y13.5. REPAIRED IAW SRM 51-40-15, 51-42-05. 2 H 7 2 4T RT A13NM 2007022000176 20070220 00176 NM 2007 2 20 QXEA200700132 1 20070202 A 5321 FLOOR SKIN BOMBDR DHC8 DHC8402 1390042 NM BS 698 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 415QX 4081 C2 PDX - FOUND SUBFLOOR SKIN AROUND THE SCREW HOLE BETWEEN THE LEFT INBOARD MAIN AND AUXILARY SEAT TRACKS AT STATION X69 8. REPAIRED IAW SRM 51-14-00, 51-42-15 AND 51-42-05. 2 H 7 2 4T RT A13NM 2007022000177 20070220 00177 EA 2007 2 20 SWIA200717793 1 20070209 A 2120 UNKNOWN CNDAIR CL600 CL6002D24 1390016 EA CABIN ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 806SK 15070 FUEL ODOR IN CABIN WHEN STARTING APU. INSPECTED PACKS AND APU. COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECKS GO OD. 2 L 7 2 4F RT A21EA 2007022000178 20070220 00178 EA 2007 2 20 COMA0760180 1 20070212 A 2120 01649803 SENSOR CNDAIR CL600 CL6002B19 1900309 EA FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 933CA 7040 FLIGHT 5542 - DISPLAY COOK CAUTION MESSAGE RECEIVED. INSPECTED DUCTING, CLEANED FLOW SENSOR CONNECTOR, REPLACED FLOW SE NSOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007022000181 20070220 00181 EA 2007 2 20 SWIA200717794 1 20070211 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 408SW 7055 FOUND LAST EMERGENCY OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED AFT MOST CEILING EMERGENCY LIGHT. OPERATIONAL CHECKS GO OD. 2 L 7 2 4F RT A21EA 2007022000182 20070220 00182 SO 2007 2 20 SWIA200717795 1 20070205 A 7712 30005000057 SIGNAL COND UNIT EMB 120 EMB120ER 3260203 SO ENG TORQUE MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 218SW 120287 ON TAKEOFF, THE "AUTOFEATHER" SYSTEM WOULD NOT ARM. ABORTED T/O. REPLACED LEFT ENGINE TORQUE SIGNAL CONDITIONER. OPER ATIONAL CHECKS GOOD. S/N OFF: 4713. 2 L 7 2 4T RT A31SO 2007022000183 20070220 00183 EA 2007 2 20 SWIA200717796 1 20070208 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 448SW 7678 NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. REPLACED NR 2 OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007022000186 20070220 00186 EA 2007 2 20 SWIA200717799 1 20070207 A 3350 SIGN CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 746SK 10202 LIGHTED "EXIT" PLACARD ON GALLEY SERVICE DOOR FAILS TO LIGHT. SECURED CONNECTION AT GALLEY SERVICE DOOR TOP EXIT SIGN L IGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007022000187 20070220 00187 EA 2007 2 20 SWIA200717800 1 20070204 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 934SW 7722 FOUND OVERHEATING ODOR IN VICINITY OF ROW 9C-10C. RAN PACK AND COULD NOT DETECT ANY ODOR IN CABIN. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007022000189 20070220 00189 EA 2007 2 20 SWIA200717802 1 20070212 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 461SW 7811 FOUND INNER CORE OF CAPTAIN'S WINDSHIELD SHATTERED AT FL330. REPLACED CAPTAIN'S WINDSHIELD WITH A SERVICEABLE WINDSHIEL D IAW 56-11-01 AND RII 56-220-1000. OPERATIONAL CHECKS GOOD, PN: 139321-5 SN OFF: 03357H2307. 2 L 7 2 4F RT A21EA 2007022000190 20070220 00190 SO 2007 2 20 SWIA200717803 1 20070204 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 233SW 120307 FOUND FORWARD CABIN EMERGENCY LIGHT FAILED. REPLACED FORWARD EMERGENCY BATTERY PACK. OPERATIONAL CHECKS GOOD, SN OFF 2 22. 2 L 7 2 4T RT A31SO 2007022000201 20070220 00201 SO 2007 2 20 RAIA00702006 1 20070205 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO CABIN NOT SEATED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 820HK 145064 PRE FLT NR 5502 - STL - EMERGENCY LIGHT AT RT OVERWING EXIT IDENTIFIER INOP. MAINTENANCE RESEATED THE CONNECTOR TO THE LIGHT ASSEMBLY. 2 L 7 2 4F RT T00011AT 2007022000202 20070220 00202 SO 2007 2 20 RAIA00702007 1 20070206 A 3350 RPS1B BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 850HK 145003 POST FLT NR 7916 - STL - EMERGENCY LIGHTS CAME ON IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY. 2 L 7 2 4T RT T00011AT 2007022000203 20070220 00203 NM 2007 2 20 SWAA070697 1 20070209 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007022000207 20070220 00207 2007 2 20 SWAA070804 4 20070214 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007022000208 20070220 00208 NM 2007 2 20 SWAA070700 1 20070209 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007022000211 20070220 00211 NM 2007 2 20 SWAA070690 1 20070209 A 5743 6552235 FITTING BOEING 737 7373H4 1384600 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED 12Y CHECK, FOUND LT MLG STABILIZER FITTING CORRODED. REMOVED AND REPLACED MLG STABILIZER FITTING PER M M. 2 L 7 2 4F RT A16WE 2007022000213 20070220 00213 NM 2007 2 20 SWAA070685 1 20070209 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 464WN 32468 L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007022000218 20070220 00218 2007 2 20 SWAA070705 4 20070210 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007022000219 20070220 00219 NM 2007 2 20 SWAA070704 1 20070209 A 2560 PH22300L GLOWSTRIP BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND RIGHT FWD CABIN EEPLS PHOTOLUMINESCENT STRIP LOOSE. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007022000220 20070220 00220 NM 2007 2 20 SWAA070588 1 20070204 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007022000222 20070220 00222 NM 2007 2 20 SWAA070591 1 20070204 A 5322 6546546 SHEAR TIE BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007022000223 20070220 00223 NM 2007 2 20 SWAA070590 1 20070204 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007022000224 20070220 00224 NM 2007 2 20 SWAA070601 1 20070204 A 5330 6546881 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1050, STR 25L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007022000225 20070220 00225 NM 2007 2 20 SWAA070608 1 20070205 A 5320 6547980 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 827 TO BS 847, LBL 70. REMOVED AND REPLACED CREASE BEA M WEB PER SRM. 2 L 7 2 4F RT A16WE 2007022000228 20070220 00228 NM 2007 2 20 SWAA070923 1 20070216 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 445, STR 26L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007022000230 20070220 00230 NM 2007 2 20 SWAA070925 1 20070216 A 5322 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007022000231 20070220 00231 NM 2007 2 20 SWAA070991 1 20070217 A 5311 6546552 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 9R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007022000233 20070220 00233 NM 2007 2 20 SWAA070931 1 20070217 A 2752 65512714 GEARBOX BOEING 737 7373H4 1384600 NM T/E FLAP WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 606SW 27926 DURING SCHEDULED SERVICE CHECK, FOUND RIGHT 90 DEGREE FLAP DRIVE ANGLE GEARBOX TO FLAP DRIVE MOTOR TORQUE TUBE WORN. RE MOVED AND REPLACED RIGHT 90 DEGREE FLAP DRIVE ANGLE GEARBOX PER MM. 2 L 7 2 4F RT A16WE 2007022000234 20070220 00234 NM 2007 2 20 SWAA070993 1 20070217 A 2750 65522111 TORQUE TUBE BOEING 737 7373Q8 1384670 NM T/E FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND LEFT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007022000236 20070220 00236 NM 2007 2 20 SWAA070918 1 20070216 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM L2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2007022000237 20070220 00237 NM 2007 2 20 SWAA070924 1 20070216 A 5523 65C25797 SKIN BOEING 737 7373Q8 1384670 NM ELEVATOR TAB DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND LEFT ELEVATOR TAB SKIN DELAMINATED AT UPPER SURFACE. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007022000238 20070220 00238 NM 2007 2 20 SWAA070949 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000239 20070220 00239 NM 2007 2 20 SWAA070948 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000242 20070220 00242 NM 2007 2 20 SWAA070946 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000243 20070220 00243 NM 2007 2 20 SWAA070950 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000247 20070220 00247 NM 2007 2 20 SWAA070955 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000248 20070220 00248 NM 2007 2 20 SWAA070944 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000249 20070220 00249 NM 2007 2 20 SWAA070934 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000250 20070220 00250 NM 2007 2 20 SWAA070953 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000251 20070220 00251 NM 2007 2 20 QXEA200700193 1 20070213 A 2520 PSU BOMBDR DHC8 DHC8402 1390042 NM ROW 7 D, E DISLODGED A QXEA D RETURN TO BLOCK D INFLIGHT SEPARATION TX TAXI/GRND HDL 1 NM 09 400QX 4030 SEA FLIGHT NR 2476: PSU OVER ROW 7DE CAME DOWN. AIRCRAFT RETURNED TO GATE. MAINTENANCE REINSTALLED PSU AT ROW 7DE AS R EQUIRED. READING LIGHTS, GASPERS, CALL BUTTON AND SPEAKER ALL OPS CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED T O SERVICE. 2 H 7 2 4T RT A13NM 2007022000254 20070220 00254 NM 2007 2 20 F3LA200700025 1 20070212 A 2120 UNKNOWN AIRBUS A319 A319111 3930336 NM CABIN ODOR A F3LA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 03 925FR 2103 BLOCK TURN BACK, FLIGHT CREW REPORTED APU AUTO SHUTDOWN, EMERGENCY SHUTDOWN DUE TO BURNING SMELL. MAINTENANCE PERFORMED AN INSPECTION AND OPERATIONAL CHECKS OF THE APU PER AMM 49-00-81-810-803. NO INDICATION OF BURNING SMELL WAS FOUND. R II INSPECTION PER GMM 85.07. RAN APU AND PACKS IAW 12-33-21-618-001. NO BURNING SMELL DETECTED. 2 L 7 2 4F RT A28NM 2007022000255 20070220 00255 NM 2007 2 20 SWAA070941 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000256 20070220 00256 NM 2007 2 20 SWAA070940 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000260 20070220 00260 NM 2007 2 20 SWAA070939 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000262 20070220 00262 NM 2007 2 20 SWAA070938 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000263 20070220 00263 NM 2007 2 20 SWAA070937 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000266 20070220 00266 NM 2007 2 20 SWAA070956 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000267 20070220 00267 EU 2007 2 20 07FDEA00477 1 20070214 A 5315 FLOORBEAM AIRBUS 310 A310222 3930315 EU ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 422FE 346 PREVIOUS REPAIR LOCATED ON MAIN CABIN FLOORBEAM FRAME 37 AND BETWEEN SEAT TRACKS 4 AND 5 LT HAS 2 REPAIR ANGLES MEASURIN G 16.8" BY 1.7" LONG LOCATED AT THE UPPER FLANGE AREA, FWD AND AFT SIDE OF FLOORBEAM. PREVIOUSLY INSTALLED REPAIR LOCAT ED ON MAIN CABIN FLOORBEAM FRAME 37 BETWEEN SEAT TRACKS 4 AND 5 LT UPPER FLANGE AREA WAS DETERMINED NOT TO BE IAW A310 S RM SUPPLEMENT 53-10-15 FIG 201 SHEET 2, DUE TO MISSING 2 EACH HILOCKS AT TOP FLANGE ON FWD AND AFT CENTER ANGLES AT THE CLS ADAPTER BETWEEN THE FASTENERS WITH A PITCH OF 2.800". DRILLED, COUNTERSUNK, AND INSTALLED 2 HILOCKS PER A310 SRM SU PPLEMENT 53-10-15 FIG 201 SHEET 2. 2 L 7 2 4F RT A35EU 2007022000268 20070220 00268 NM 2007 2 20 SWAA070933 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007022000270 20070220 00270 EU 2007 2 20 07FDEA00478 1 20070214 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 422FE 346 PREVIOUS REPAIR LOCATED ON MAIN CABIN SEAT TRACK 5R BETWEEN FRAMES 35 TO 37 HAS A REPAIR WITH 4 EACH REPAIR ANGLES MEASU RING 8.8" LONG EACH AND THE SEAT TRACK REPAIR SECTION IS 20" LONG. PREVIOUSLY INSTALLED REPAIR LOCATED AT MAIN CABIN SE AT TRACK 5R BETWEEN FRAMES 35 TO 37 WAS DETERMINED NOT TO BE IAW A310 SRM 53-10-16 FIG 208 SHEET 1, DUE TO FASTENER PITC H INCORRECT. COMPLIED WITH REPAIR PER FED EX EA6-5310-107668. 2 L 7 2 4F RT A35EU 2007022000271 20070220 00271 NM 2007 2 20 SWAA070936 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000273 20070220 00273 NE 2007 2 20 07FDEA00480 2 20070215 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D15 52051 NE NR 1 DAMAGED A FDEA A UNSCHED LANDING E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 25 483FE 35696 35696 21465 700479 AFTER TAKEOFF AT 1000 FT, CREW FELT A VERY PRONOUNCED THUMP ACCOMPANIED BY A LOUD NOISE. AUTO PACK TRIP ILLUMINATED. E NGINE INSTRUMENTS CHECKED NORMAL. WHILE TROUBLESHOOTING THE PROBLEM AND CLIMBING THROUGH 18,000FT. ANOTHER LOUD THUMP AND NOISE OCCURRED AND THE NR 1 ENGINE EPR DECREASED TO 1.5 EPR. RETARDED NR 1 THROTTLE RAN THE QRH CHECKLIST AND RETU RNED TO PHL. FOUND APPROX 6 BLADES ON NR 1 ENGINE FAN DAMAGED CHECKING DAMAGE LIMITS. 2 L 7 3 4F 4 F A3WE E2EA 2007022000276 20070220 00276 NM 2007 2 20 SWAA070954 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000278 20070220 00278 NM 2007 2 20 SWAA070978 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000280 20070220 00280 NM 2007 2 20 SWAA07979 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000281 20070220 00281 NM 2007 2 20 SWAA070980 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000282 20070220 00282 NM 2007 2 20 NWAA070585638 1 20070208 A 3397 WIRE BOEING 757 757251 1384970 NM EMERGENCY EXIT BROKEN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 538US 26485 EXIT INDICATOR EMERGENCY LIGHT INOPERATIVE. TROUBLE SHOT PER WDM 33-51-21. REPAIRED BROKEN WIRES AND REPLACED POWER UN IT M732. OPS CHECKS GOOD. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2007022000284 20070220 00284 NM 2007 2 20 SWAA070957 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000285 20070220 00285 NM 2007 2 20 SWAA070983 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000290 20070220 00290 NM 2007 2 20 SWAA070988 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000291 20070220 00291 NM 2007 2 20 SWAA070989 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000292 20070220 00292 NM 2007 2 20 SWAA070990 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000294 20070220 00294 NM 2007 2 20 SWAA070982 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000295 20070220 00295 NM 2007 2 20 SWAA070965 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000300 20070220 00300 NM 2007 2 20 SWAA070962 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007022000301 20070220 00301 NM 2007 2 20 SWAA070977 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000304 20070220 00304 NM 2007 2 20 SWAA070966 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000305 20070220 00305 NM 2007 2 20 SWAA070967 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000307 20070220 00307 NM 2007 2 20 SWAA070969 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000308 20070220 00308 NM 2007 2 20 SWAA070970 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000309 20070220 00309 EA 2007 2 20 A6WA200740043 1 20070125 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 447AW 7812 FOUND RIGHT SIDE CARGO FLOOR ANGLE AT FS 621 BULKHEAD CRACKED APPROX .5 INCH LONG. (M) MAINTENANCE REPAIR CRACK IAW RE O 601R-53-61-117 REV C BY INSTALLING REPAOR ANGLE AND STRAPS. (K) 2 L 7 2 4F RT A21EA 2007022000312 20070220 00312 NM 2007 2 20 SWAA070972 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000314 20070220 00314 NM 2007 2 20 AWXA200700198 1 20070119 A 5752 654645521SP TAB BOEING 737 73733A 1384673 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND LEFT WING AILERON TAB UPPER SKIN TRAILING EDGE CRACKED, WS 433.25, 16" FROM INBOARD EDGE. REPAIRED LEFT WIN G AILERON TAB UPPER SKIN TRAILING EDGE, WS 433.25, 16" FROM INBOARD EDGE IAW B737-300 SRM 51-70-07. 2 L 7 2 4F RT A16WE 2007022000315 20070220 00315 NM 2007 2 20 SWAA070973 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000322 20070220 00322 NM 2007 2 20 ZZDA070123118 1 20070123 A 5330 SKIN PANEL BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. LOWER SKIN PANEL AND HINGE DAMAGED. REPLACED LOWER SKIN PANEL AND HINGE INSTALLATION AT AFT NLG WHEEL WELL PER MDC DRAWING 5913421 REV W DATED 12/04/99. 2 L 7 2 4F TR A6WE 2007022000326 20070220 00326 NM 2007 2 20 ZZDA070123119 1 20070123 A 5244 ACCESS DOOR BOEING 717 717200 1383700 NM ACC BAY DAMAGED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. ACCESSORY COMPARTMENT ACCESS DOOR DAMAGED. REPLACED ACCESSORY COMPARTME NT ACCESS DOOR PER MDC DRAWING 5910083 REV AY DATED 01/24/06. 2 L 7 2 4F TR A6WE 2007022000328 20070220 00328 NM 2007 2 20 AWXA200700203 1 20070126 A 5754 65C26602257SP SKIN BOEING 737 7373S3 1384711 NM ZONE 500 DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND LEFT WING NR 2 SLAT UPPER SURFACE, INBOARD END HAS AN AREA DISBONDED, SS 126. REPAIRED LEFT WING NR 2 SLAT UPPER SURFACE, INBOARD END, SS124.40 - SS 127.40 IAW B737-300 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 2007022000329 20070220 00329 NM 2007 2 20 AWXA200700204 1 20070201 A 5340 69389722 STRINGER CLIP BOEING 737 7373S3 1384711 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND STRINGER TO FRAME BRACKET CRACKED, BS 312, S28L. REPLACED STRINGER TO FRAME BRACKET, BS 312, S28L IAW B737- 300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007022000331 20070220 00331 EA 2007 2 20 A6WA200740035 1 20070123 A 8012 005900083 CHECK VALVE CNDAIR CL600 CL6002B19 1900309 EA AIR STARTER LEAKING A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 446AW 8594 7806 RAMP AGENTS REPORTED ELECTRICAL ODOR IN CARGO BIN. CREW INSPECTED AND FOUND HOT SPOT ADJACENT TO GROUND SUPPLY AIR CONN ECTION. FOUND GROUND AIR START CHECK VALVE IS LEAKING. REMOVED AND REPLACED GROUND AIR START CHECK VALVE IAW AMM 36-11 -27. NO ELECTRICAL ODOR PRESENT. OPS CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007022000334 20070220 00334 EA 2007 2 20 A6WA200740032 1 20070118 A 3000 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 465AW 7893 ANTI-ICE DUCT MESSAGE WITH DUCT FAIL IN SWITCH LIGHT WITH WING ANTI-ICE LIGHT ON. COMPLIED WITH QRH, SELECTED 14TH STAG E BLEEDS AND WING ANTI-ICE OFF. MESSAGE CLEARED. WHEN 14TH STAGE BLEEDS SELECTED ON AND WING ANTI-ICE TO STANDBY, MESS AGE DID NOT REAPPEAR. REMOVED AND REPLACED SENSING ELEMENT A47WK REF AMM 36-21-04, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007022000335 20070220 00335 NM 2007 2 20 QXEA200700139 1 20070204 A 2430 11521086 GCU BOMBDR DHC8 DHC8402 1390042 NM NR 1 MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 407QX 6422 4049 SEA FLIGHT NR 2328: NR 1 DC GEN ILLUMINATED. CHECKLIST WAS RUN. RESET NR 1 GEN AND IT REMAINED ONLINE. MAINTENANCE RE MOVED AND REPLACED NR 1 DC GCU IAW Q400 AMM 24-31-06, PAGES 401-406. PERFORMED OPERATIONAL TEST OF THE DC GCU IAW Q400 AMM 24-31-06 PAGES 501-504. OPS TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007022000081 20070220 00081 NM 2007 2 20 CALA0700067 1 20070215 A 5312 6546568519 STIFFENER BOEING 737 7373T0 1384582 NM AFT BULKHEAD CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 INSPECTION FOUND TWO CHANNEL STIFFENERS CORRODED ON FORWARD FACE OF APB LOWER SECTION. THE STIFFENERS WERE REMOVED AND NEW SECTIONS WERE SPLICED IN IAW BOEING DRAWING 65C28106. 2 L 7 2 4F RT A16WE 2007022000089 20070220 00089 2007 2 20 NSVA20070008 4 20070113 A 3420 INDICATOR BEECH 1900 1900D 1154162 CE EHSI MALFUNCTIONED A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 243CJ UE43 COMPARATOR FLAG ILLUMINATED ON TAKEOFF, HEADING FLAG ON CAPTAIN EHSI. PERFORMED OPS CK OF SYSTEM DID NOT FIND ANY FAULT S, OPS CK GOOD REF 34-20-00. 2 L 7 2 4T RT A24CE 2007022000092 20070220 00092 EA 2007 2 20 COMA0760169 1 20070207 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 987CA 7199 FLIGHT 5363 - SMOKE TOILET MESSAGE ON CLIMBOUT. AIRCRAFT DIVERTED BACK TO EWR AND LANDED SAFELY. DEFERRED PER MEL 26-1 6-01. 2 L 7 2 4F RT A21EA 2007022000094 20070220 00094 EA 2007 2 20 COMA0760167 1 20070207 A 3350 BA50933901 CHARGER CNDAIR CL600 CL6002B19 1900309 EA CABIN FAULTY A COMA K NONE O OTHER CR CRUISE 1 SO 01 526CA 7824 FLIGHT 5347 - EMERGENCY LIGHT SIGN AT MAIN CABIN DOOR FLOOR LEVEL EXIT AND AISLE OVERHEAD FLICKERING WHILE THE SWITCH IS IN THE OFF POSITION. REPLACED NR 2 CHARGER ASSEMBLY. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007022000100 20070220 00100 EA 2007 2 20 COMA0770015 1 20070209 A 3810 9819101 VALVE CNDAIR CL600 CL6002C10 1390015 EA LAVATORY FAUCET LEAKING A COMA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 01 369CA 2464 10079 FLIGHT 5328 - EN ROUTE CVG-PBI DISCOVERED THE FORWARD AND AFT LAVATORY WERE LEAKING POTABLE WATER INTO THE CABIN, FLIGHT RETURNED TO CVG. REPLACED THE FORWARD LAVATORY FAUCET. 2 L 7 2 4F RT A21EA 2007022000102 20070220 00102 EA 2007 2 20 COMA0760174 1 20070210 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 915CA 22928 7013 FLIGHT 5184 - DURING BUF APPROACH RECEIVED A LANDING GEAR DOWN DISAGREE CAUTION, ABORTED APPROACH, THEN LANDED WITHOUT I NCIDENT ON SECOND ATTEMPT. REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2007022000103 20070220 00103 CE 2007 2 20 NSVA20070009 1 20070114 A 7931 1013890235 TRANSDUCER BEECH 1900 1900D 1154162 CE OIL PRESSURE MALFUNCTIONED A NSVA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 243CJ UE43 RT OIL PRESS FLUCTUATION INFLIGHT 115-160 PSI>1800 LBS TQ. REMOVED AND REPLACED RT OIL PRESS TRANSDUCER IAW BMM 79-30-0 0 P/N 101-389023-5 S/N ON 5405-A-37, S/N OFF 40910. OPS CK GOOD. 2 L 7 2 4T RT A24CE 2007022000104 20070220 00104 EU 2007 2 20 NSVA20070010 1 20070115 A 2612 NONE SAAB SF340 340B 7860101 EU LT TAILPIPE UNKNOWN A NSVA O OTHER N FALSE WARNING CL CLIMB 1 EA 27 339CJ 339CJ LT TAILPIPE HOT LIGHT ILLUMINATED IN FLIGHT. COULD NOT DUPLICATE DISCREPANCY, OPS CHECK GOOD IAW SA MM 26-11-00. 2 L 7 2 4T RT A52EU 2007022000121 20070220 00121 NM 2007 2 20 AALA20070250 1 20070202 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 797AN 30012 DFW - FOUND EMERGENCY LIGHT AT SEAT 25C HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 25C SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007022000129 20070220 00129 NM 2007 2 20 AALA20070236 1 20070101 A 2530 46700017 COFFEEMAKER BOEING 777 777223 1385213 NM GALLEY MALFUNCTIONED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 798AN 30797 LAX INFLIGHT T170/01FEB - CAPTAIN REPORTED SEEING SMOKE AROUND NUMBER 10 AND 11 COFFEE MAKERS AND SMELL OF BURNING INSUL ATION. CIRCUIT BREAKERS POPPED. FOUND THE NUMBER 11 COFFEE MAKER BLEW TWO HEATING ELEMENTS OUT OF WATER TANK SPRAYING WHITE POWDER ALL BEHIND AND AROUND THE COFFEE MAKER NUMBER 10 AND 11. CLEANED UP AREA AND REPLACED NUMBER 11 COFFEE MAK ER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007022000138 20070220 00138 WP 2007 2 20 AALA20070223 1 20070130 A 3230 PSEU DOUG DC9 DC983 3022083 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 983TW 53633 EWR INFLIGHT T429/30JAN - GEAR UNSAFE LIGHT ILLUMINATED DURING LANDING GEAR RETRACTION. CYCLED GEAR WITH NO HELP. RETU RNED TO EWR AND LANDED WITHOUT INCIDENT. REPLACED PROXIMITY SENSOR ELECTRONIC UNIT FOR NOSE LANDING GEAR. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007022000142 20070220 00142 EU 2007 2 20 AALA20070258 1 20070203 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70072 515 MIA - FOUND EMERGENCY LIGHT AT SEAT 11G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 11G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007022000147 20070220 00147 WP 2007 2 20 AALA20070254 1 20070203 A 3213 STRUT DOUG DC9 DC983 3022083 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 979TW 53629 ORD INFLIGHT T309/03FEB - NOSE GEAR WOULD NOT RETRACT. RECEIVED RED LIGHT INDICATION AND HEARD NOISE. CYCLED GEAR WITH SAME RESULTS. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. SERVICED LANDING GEAR STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007022000153 20070220 00153 NM 2007 2 20 AWXA200700205 1 20070130 A 5340 693535214 STRINGER CLIP BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED STRINGER CLIP, BS 616,S4R. REPLACED STRINGER CLIP, BS 616,S4R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007022000154 20070220 00154 EA 2007 2 20 COMA0760176 1 20070211 A 2530 5003272 RACK CNDAIR CL600 CL6002B19 1900309 EA GALLEY DIRTY A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 629BR 7251 FLIGHT 5008 - EN ROUTE RSW-CMH CREW REPORTED THE PRESENCE OF STRONG ELECTRICAL SMOKE SMELL IN THE COCKPIT, FLIGHT DIVERT ED TO MCO. REPLACED THE COFFEEMAKER RACK. 2 L 7 2 4F RT A21EA 2007022000165 20070220 00165 EA 2007 2 20 COMA0760179 1 20070211 A 5610 NP1393225 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 477CA 11580 7670 FLIGHT 5573 - FOUND THE CAPTAINS SIDE WINDOW CRACKED DURING WALK-AROUND INSPECTION. REPLACED THE CAPTAINS SIDE WINDOW. 2 L 7 2 4F RT A21EA 2007022000174 20070220 00174 NM 2007 2 20 QXEA200700134 1 20070124 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 467 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 415QX 4081 C2 PDX - FOUND LEFT OUTBOARD SEAT TRACK HAS LIGHT CORROSION INSIDE TRACK AT STATION X467. REPAIRED IAW RD8/4-53-884 AND SRM 51-21-10. 2 H 7 2 4T RT A13NM 2007022000185 20070220 00185 EA 2007 2 20 SWIA200717798 1 20070209 A 5210 ANCHOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 927SW 7693 AFT PAX DOOR ANCHOR CRACKED, DISCOVERED DURING SERVICE CHECK. REPLACED AFT PAX DOOR ANCHOR AND SWIVEL IAW CRJ200 MM 52- 11-17. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007022000204 20070220 00204 NM 2007 2 20 SWAA070811 1 20070214 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 502D, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007022000205 20070220 00205 2007 2 20 SWAA070814 4 20070214 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED 12Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007022000206 20070220 00206 2007 2 20 SWAA070803 4 20070214 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007022000209 20070220 00209 NM 2007 2 20 SWAA070698 1 20070209 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007022000212 20070220 00212 NM 2007 2 20 SWAA070706 1 20070210 A 2560 6557463 FITTING BOEING 737 7377H4 1384404 NM R1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 231WN 32499 R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED GIRT BAR FITTING PER MM. 2 L 7 2 4F RT A16WE 2007022000214 20070220 00214 NM 2007 2 20 SWAA070686 1 20070209 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 464WN 32468 R2 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007022000215 20070220 00215 NM 2007 2 20 SWAA070707 1 20070210 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 419WN 29824 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007022000216 20070220 00216 NM 2007 2 20 SWAA070692 1 20070209 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED SPV CHECK, FOUND STRINGER 26R CORRODED AT BS 442. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007022000217 20070220 00217 2007 2 20 SWAA070711 4 20070210 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007022000221 20070220 00221 NM 2007 2 20 SWAA070609 1 20070205 A 5322 6546546 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007022000229 20070220 00229 NM 2007 2 20 SWAA070922 1 20070216 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007022000232 20070220 00232 NM 2007 2 20 SWAA070992 1 20070217 A 5311 6546554 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007022000235 20070220 00235 NM 2007 2 20 SWAA070994 1 20070217 A 2750 65522112 TORQUE TUBE BOEING 737 7373Q8 1384670 NM T/E FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND LEFT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007022000240 20070220 00240 NM 2007 2 20 SWAA070947 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000244 20070220 00244 NM 2007 2 20 SWAA070951 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000245 20070220 00245 NM 2007 2 20 SWAA070952 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000246 20070220 00246 EA 2007 2 20 A6WA200740045 1 20070124 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 447AW 7812 FOUND LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT HOLE NR 2 (PNL 510AB, HAS MINOR PITTING AT INBOARD END IN AN AR EA APPROX 3 INCHES LONG BY .005 INCH DEEP IN NON-CRITICAL AREA. (M) MAINTENANCE REPAIRED WING PLANK HOLE NR 2 (510AB) IAW REO 601R-57-21-030 REV F AND AWAC EO E06/021/457 REV A. (K) 2 L 7 2 4F RT A21EA 2007022000252 20070220 00252 NM 2007 2 20 SWAA070943 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000253 20070220 00253 NM 2007 2 20 SWAA070942 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000264 20070220 00264 EU 2007 2 20 07FDEA00476 1 20070214 A 5511 SPAR AIRBUS 310 A310203 3930313 EU ZONE 300 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 PREVIOUS REPAIR LOCATED ON RT THS UPPER REAR SPAR CHORD AT RIB 4 HAS A REPAIR STRAP APPROXIMATELY 10.3" BY 1.0" LONG PRE VIOUSLY INSTALLED REPAIR LOCATED AT RT THS UPPER CHORD AT RIB 4 WAS DETERMINED NOT TO BE IAW A310 SRM 55-11-21 FIG 217 , DUE TO INCORRECT FASTENERS AND PITCH INSTALLED. COMPLIED WITH FED EX EA6-5510-107667. 2 L 7 2 4F RT A35EU 2007022000265 20070220 00265 NM 2007 2 20 SWAA070935 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000272 20070220 00272 NM 2007 2 20 SWAA070984 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000274 20070220 00274 NM 2007 2 20 SWAA070976 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000277 20070220 00277 EU 2007 2 20 07FDEA00482 1 20070215 A 5340 A5397432100051 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 FOUND CORROSION ON CORNER FITTING C63, P43 LT AND ON CROSSBEAM C61, P45 LT AND C58, P47 RT. REPAIR WAS PERFORMED BY REP LACE A NEW FITTING IAW SRM 51-72-10 AND SRM 53-17-15, FIG 5. CROSSBEAM REPAIR WAS PERFORMED IAW SRM 53-10-15/FIG 208 SE E ALSO SRM 53-16-15 / FIG 5 AND SRM 53-10-15 FIG 208 SEE ALSO SRM 53-17-15 FIG 10. 2 L 7 2 4F RT A35EU 2007022000283 20070220 00283 NM 2007 2 20 SWAA070981 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000286 20070220 00286 NM 2007 2 20 SWAA070975 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000287 20070220 00287 NM 2007 2 20 SWAA070985 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000288 20070220 00288 NM 2007 2 20 SWAA070986 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000293 20070220 00293 NM 2007 2 20 SWAA070995 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000296 20070220 00296 NM 2007 2 20 SWAA070958 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007022000298 20070220 00298 NM 2007 2 20 SWAA070960 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007022000299 20070220 00299 NM 2007 2 20 SWAA070961 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000302 20070220 00302 NM 2007 2 20 SWAA070964 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000303 20070220 00303 NM 2007 2 20 SWAA070974 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000306 20070220 00306 NM 2007 2 20 SWAA070968 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000310 20070220 00310 NM 2007 2 20 SWAA070971 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000318 20070220 00318 NM 2007 2 20 ZZDA070130136 1 20070130 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 910AT 55086 DENT ON RT SIDE AFT OF R1 DOOR STA 212 BETWEEN LONG 15 AND 16 RT. INSTALLED FLUSH REPAIR PER B717 SRM 53-00-01 FIG 204 REPAIR 2. 2 L 7 2 4F TR A6WE 2007022000320 20070220 00320 NE 2007 2 20 NACA20070004 2 20070207 A 8530 356993 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 16 CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 43872 1682 1682 533294 510152 NR 1 ENGINE WOULD NOT TAKE A LEAN IN CRUISE FLIGHT. PERFORMED PRECAUTIONARY SHUTDOWN. REMOVED AND REPLACED NR 16 CYLIN DER DUE TO CRACKED HEAD, REF: NAC DC-6MM SEC V, PG 16. RUN UP CHECKED GOOD, NO LEAKS. 2 L 7 4 4R 4 R A781 5E8 2007022000321 20070220 00321 NM 2007 2 20 AWXA200700199 1 20070121 A 5311 65465485 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND FRAME ANGLE CRACKED, BS 747, S13L. REPAIRED FRAME ANGLE, BS 747, S13L IAW B737-330 SRM 51-70-11. 2 L 7 2 4F RT A16WE 2007022000323 20070220 00323 WP 2007 2 20 IXXA07SMN035S 1 20070119 A 5753 SKIN DOUG DC8 DC871F 302199D WP TE FLAP MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER SKIN HAS A NON STANDARD REPAIR FROM STATION XW132.000 T O STATION XW135.000. REMOVED EXISTING SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN AS NEEDED. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN IAW DC8 SRM 57-1-0, PAGE 1, DC8 S RM 51-1-21, DC8 SRM 57-7-1 FIGURE 1 PAGE 2 ITEM "F" DC8 SRM 51-1-8B DC8 SRM 51-1-11 AND DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007022000324 20070220 00324 NM 2007 2 20 AWXA200700200 1 20070121 A 5311 65465632 FRAME BOEING 737 73733A 1384673 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CORROSION ON FRAME LOWER ATTACH, BS 967, INBOARD OF S28L. REPLACED FRAME LOWER ATTACH, BS 967, INBOARD OF S 28L IAW B737-300 SRM 53-00-07-2R7. 2 L 7 2 4F RT A16WE 2007022000325 20070220 00325 NM 2007 2 20 AWXA200700201 1 20070122 A 5347 6546813508 SEAT TRACK BOEING 737 73733A 1384673 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - FOUND CORROSION ON MAIN CABIN SEAT TRACK, BS 328 - BS 344, RBL 45. REPLACED MAIN CABIN SEAT TRACK, BS 328 - BS 34 4, RBL 45 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007022000330 20070220 00330 EA 2007 2 20 A6WA200740034 1 20070120 A 2741 601R517063 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 420AW 7404 7640 STAB TRIM AND MACH TRIM CAUTION INFLIGHT NEITHER CHANNEL 1 AND 2 WOULD RE-ENGAGE COMPLIED WITH QRH. REMOVED AND REPLACE D STAB TRIM AND MACH TRIM CONTROL PANEL IAW CRJ AMM 27-41-25, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007022000332 20070220 00332 WP 2007 2 20 AMTA200700036 1 20070125 A 5280 STRUCTURE LKHEED 1011 10113853 5265020 WP NLG DOOR CRACKED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 162AT 1220 NOSE LANDING GEAR RT DOOR FOUND CRACKED ON UPPER EDGE BETWEEN MID AND AFT HINGE. NLG RT FWD DOOR REMOVED, ROUTED TO SHO P IAW AMM 32-22-01. NLG DOOR CRACK BEYOND REPAIRABLE LIMITS IAW SRM 52-82-00 AND EER NR 13225. INST NEW DOOR IAW AMM 3 2-22-01. NOSE GEAR EXT., RETRACT. ADJUST TEST AMM 32-30-00, AND 32-22-01. (K) 2 L 7 3 4F A23WE 2007022000333 20070220 00333 EU 2007 2 20 AWXA200700197 1 20070211 A 2530 OVEN AIRBUS 320 A320232 3930326 EU GALLEY FIRE A AWXA F ACTIVATE FIRE EXT. W A INADEQUATE Q C FLAME/FIRE CR CRUISE 1 WP 28 678AW 2482 OVEN FIRE, F/A REPORTED FIRE IN OVEN NR 4, CARDBOARD FROM FOOD TRAY CAUGHT FIRE. THE F/A EXTINGUISHED WITH PORTABLE HAL ON FIRE EXTINGUISHER. MX REMOVED AND REPLACED AFT GALLEY HALON EXTINGUISHER AND PLACED THE OVEN ON MEL. 2 L 7 2 4F RT A28NM 2007022000336 20070220 00336 NM 2007 2 20 NWAA070566310 1 20070209 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670US 24225 DURING OVERNIGHT LINE CHECK, EXTERIOR EMERGENCY LIGHTS RT OVERWING 2 FWD LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007022000343 20070220 00343 NE 2007 2 20 QXEA200700125 2 20070204 A 7320 CIRCUIT BREAKER DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE BETA LOCKOUT TRIPPED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 368PH 512 SEA FLIGHT NR 2031 - ON TAXI, NR 2 ENGINE MANUAL CAUTION LIGHT ILLUMINATED. MAINTENANCE RESET BETA LOCKOUT CIRCUIT BREA KER. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007022000355 20070220 00355 NM 2007 2 20 ZZDA070123121 1 20070123 A 3230 BUNGEE BOEING 717 717200 1383700 NM NLG DAMAGED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. NLG COLLASPED (AFT DIRECTION) APPORX 18 INCHES EXPOSED (WHEEL ASSEMBLE). REMOVED AND REPLACED NLG ASSY AND RETRACT CYCLE AND BUNGEE PER JAC 717-5044-559532001-01 PER MDC DRAWING 5940760 REV T DATED 01/24/06. 2 L 7 2 4F TR A6WE 2007022000356 20070220 00356 NM 2007 2 20 ZZDA070123122 1 20070123 A 5280 DOOR BOEING 717 717200 1383700 NM NLG DAMAGED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. LEFT FWD AND AFT NOSE GEAR DOOR DAMAGED. REPLACED NLG FWD AND AFT DOORS PER MDC DRAWING 5910086 REV AF DATED 01/24/06. 2 L 7 2 4F TR A6WE 2007022000360 20070220 00360 NM 2007 2 20 AALA20070172 1 20070122 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 921AN 29522 TUL - BATTERY PACK FOR EMERGENCY LIGHTS IN COACH FAILED FUNCTIONAL TEST. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007022000361 20070220 00361 NM 2007 2 20 AALA20070174 1 20070105 A 5330 SKIN BOEING 767 767323 1385205 NM BS 883-873 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 371AA 25198 AFW - FUSELAGE SKIN BETWEEN STATION 883.5 AND STATION 873 BETWEEN STRINGER 1 RIGHT AND STRINGER 2 RIGHT IN AN AREA OF 1 INCH BY 0.5 INCH WITH AT DEPTH OF .0.76 INCH HAD GOUGES. BLENDED GOUGES PER SRM 530001 FIGURE 101 AND PERFORMED HIGH FR EQUENCY EDDY CURRENT INSPECTION FOR CRACKS AND ALODINED. 2 L 7 2 4F RT A1NM 2007022000362 20070220 00362 WP 2007 2 20 AALA20070177 1 20070124 A 2130 1173T0691 SWITCH DOUG DC9 DC983 3022083 WP AIR CONDITIONING INOPERATIVE A AALA O OTHER O OTHER CR CRUISE 1 SW 21 436AA 49454 LGA INFLIGHT T1142/24JAN - EN ROUTE TO LGA EXPERIENCED PRESSURIZATION LOSS. INITIATED EMERGENCY DESCENT AND PASSENGER OX YGEN MASKS DROPPED WITH EXCEPTION OF SEAT 23DEF AND FLIGHT ATTENDANT STATION. REPLACED LEFT PACK FLOW CONTROL VALVE, TE MPERATURE CONTROL VALVE, RIGHT PACK AUTO TEMPERATURE CONTROLLER, PACK DISCHARGE SWITCH, AUTO TRIP SWITCHES, AND REPLACED OXYGEN MASKS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007022000363 20070220 00363 NM 2007 2 20 ZZDA070123126 1 20070123 A 2910 HYDRAULIC LINE BOEING 717 717200 1383700 NM NLG CRACKED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. NLG HYDRAULIC PIPING AND RELATED SUPPORTS CRACKED. REMOVED AND REPLACED NLG HYDRAULIC PIPING AND RELATED SUPPORTS PER MDC DRAWING 5963926 REV T DATED 06/28/00. 2 L 7 2 4F TR A6WE 2007022000364 20070220 00364 NM 2007 2 20 ZZDA070123127 1 20070123 A 5320 PANEL BOEING 717 717200 1383700 NM FUSELAGE CRACKED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. DISCONNECT PANEL ASSEMBLY CRACKED. REMOVED AND REPLACED DISCONNECT PANE L ASSEMBLY AND DETAILS PER MDC DRAWING 5971435 REV F DATED 03/03/03 AND PER DRAWING 7970776 REV J DATED 01/24/06. 2 L 7 2 4F TR A6WE 2007022000365 20070220 00365 NM 2007 2 20 ZZDA070123128 1 20070123 A 5320 BATTERY BOX BOEING 717 717200 1383700 NM E&E BAY DAMAGED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. MAIN BATTERY INSTALLATION STRUCTURE DAMAGED. REPLACED DAMAGED DETAILS O F MAIN BATTERY INSTALLATION STRUCTURE PER MDC DRAWING 9971381 REV Y DATED 0711 3/04 AND DRAWING 5971382 REV P DATED 09/1 6/02. 2 L 7 2 4F TR A6WE 2007022000366 20070220 00366 NM 2007 2 20 ZZDA070123129 1 20070123 A 3260 SWITCH BOEING 717 717200 1383700 NM NLG DAMAGED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. GROUND SENSING INTERLOCK SWITCH DAMAGED. REPLACED GROUND SENSING INTERL OCK SWITCH PER MDC DRAWING 7940768 REV AP DATED 01/24/06. 2 L 7 2 4F TR A6WE 2007022000369 20070220 00369 2007 2 20 ZZDA070123132 4 20070123 A 2312 5658262DC10A ANTENNA BOEING 717 717200 1383700 NM NR 1 VHF COMM DAMAGED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 956AT 55018 AIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. NR 1 VHF COMMUNICATION ANTENNA DAMAGED. REPLACED NR 1 VHF COMMUNICATION ANTENNA PER 717 AMM CHAPTER 23-12-03 REV 27 DATED 01/01/07. 2 L 7 2 4F TR A6WE 2007022000370 20070220 00370 EU 2007 2 20 SA07013 1 20070215 A 2560 CABLE AIRBUS A319 A319112 3930323 EU L1 DOOR MISROUTED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 703UW 0904 PIT - MAINTENANCE REPORTED THE L1 DOOR ESCAPE SLIDE CABLE ROUTED INCORRECTLY. MAINTENANCE REROUTED THE CABLE TO PROPER POSITION FOR LEFT-HAND DOOR INSTALLATION. 2 L 7 2 4F RT A28NM 2007022000372 20070220 00372 NM 2007 2 20 2007UALA00347 1 20070207 A 5241 NUT PLATE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU GALLEY DOOR BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 327UA 24147 FWD GALLEY DOOR INTERIOR HANDLE TRIM CRACKED ALSO DOOR SLIDE ATTACH POINT HAS BROKEN NUT PLATE. MAJOR REPAIR. REMOVED AND REPLACED DOOR HANDLE COVER PER MM 52-41-31. ALSO, REPLACED NUT PLATE PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022000375 20070220 00375 NM 2007 2 20 2007UALA00350 1 20070207 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 544UA 25322 DOOR 4 RIGHT DISARM OPERATION FAILS CHECK WHEN ATTEMPTING TO OPEN FROM OUTSIDE. THE GIRT BAR DOES NOT DISENGAGE. NOTE: CONDITION OCCURS WHEN OPENING SLOWLY IN ARMED POSITION. THE DISCREPANCY WAS TAKEN CARE OF BY CABLE ADJUSTMENT. NO CO MPONENT NEEDED TO BE REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022000378 20070220 00378 NE 2007 2 20 2007UALA00354 2 20070205 A 7314 PUMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2 ENGINE LOW PRESSURE A UALA D RETURN TO BLOCK Y ENGINE STOPPAGE TX TAXI/GRND HDL 1 WP 29 198UA 28716 727704 ON TAXI OUT, AFTER 30 MINS OF OPERATION, NR 2 ENG SHUTDOWN WITH NO FAULTS INDICATED. REPLACED BOTH ENGINE FUEL PUMP & F MU. BOTH FUEL PUMP & FMU TESTED "AS-RECEIVED" IN THE COMPONENT SHOP. ONLY DISCREPANCY FOUND IN FUEL PUMP. LOW DISCHAR GE FLOW 2583 PPH, VERSUS A MINIMUM LIMIT OF 2688 PPH. THIS SMALL DISCREPANCY SHOULD NOT HAVE CAUSED A FLAMEOUT. FMU PA SSED "AS-RECEIVED" TESTING. BOTH UNITS WERE FULLY DISASSEMBLED, & NO ABNORMALITIES FOUND. ENGINE EXPERIENCED NO FURTHE R PROBLEMS SINCE FUEL PUMP & FMU REPLACEMENT. [SUP 4-17-07] DATA ON THE FUEL PUMP IS INCLUDED BELOW, AS IT WAS SLIGHTLY OUT OF LIMIT AT THE LOW FLOW TEST POINT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022000384 20070220 00384 NM 2007 2 20 QXEA200700202 1 20070205 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 415QX 4081 C2 PDX - THERE IS A DENT OR WAVE IN THE SKIN IN THE RIGHT FUSELAGE SKIN ABOUT 6" LONG 1/2 " WIDE THAT STARTS ABOUT 1" AB OVE STRINGER 16 RT AND GOES TO ABOUT 1" BELOW STRINGER 17 RT. REPAIRED IAW RD8/4-53-1821. 2 H 7 2 4T RT A13NM 2007022000385 20070220 00385 NM 2007 2 20 QXEA200700203 1 20070131 A 5340 ANCHOR BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 415QX 4081 C2 PDX - UPPER TCAS FORWARD LEFT ANCHOR NUT IS CORRODED. REPAIRED IAW SRM 51-42-05, 51-21-10. 2 H 7 2 4T RT A13NM 2007022000386 20070220 00386 NM 2007 2 20 QXEA200700204 1 20070201 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 415QX 4081 C2 PDX - FOUND SEAT TRACK NR 10 HAS SURFACE CORROSION AT Y1.0-Y3.0. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007022000391 20070220 00391 NM 2007 2 20 AWXA200700215 1 20070217 A 5523 65C2638428 TAB BOEING 737 7373G7 1384595 NM ZONE 300 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 PHX - FOUND RIGHT ELEVATOR TRIM TAB PUSH ROD ATTACH POINT FITTING CRACKED. REPLACED RIGHT ELEVATOR TRIM TAB, ELEVATOR S TATION 32.075 - ELEVATOR 124.047 IAW AWA TASK CARD 6RC27007. 2 L 7 2 4F RT A16WE 2007022000392 20070220 00392 EU 2007 2 20 AWXA200700216 1 20070216 A 5320 D53480043202 SILL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 652AW 953 SAL - FOUND CORROSION ON MAIN CABIN SILL BEAM, +Y1732, FR 67+16". REPAIRED MAIN CABIN SILL BEAM, +Y1732, FR 67+16" IAW A320 SRM 53-41-14. 2 L 7 2 4F RT A28NM 2007022000393 20070220 00393 EU 2007 2 20 AWXA200700217 1 20070215 A 5320 D5347217220500 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 652AW 953 SAL - FOUND CORROSION ON MAIN CABIN LONGITUDINAL BEAM, -Y1292, FR 66 + 4" TO FR 68 - 4". REPLACED MAIN CABIN LONGITUDIN AL BEAM, -Y1292, FR 66 + 4" TO FR 68 - 4" IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007022000395 20070220 00395 NM 2007 2 20 QXEA200700169 1 20070210 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - GOUGE ON THE INNER SKIN OF THE BAGGAGE DOOR 37 3/4 FROM THE TOP AND 2 1/2 FROM THE AFT SIDE. REPAIRED IAW SRM 51-20-11, 51-20-16, AND 51-20-36. 2 H 7 2 4T RT A13NM 2007022000399 20070220 00399 NM 2007 2 20 QXEA200700165 1 20070210 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - GOUGE ON THE STRAP ON THE INNER SKIN OF THE BAGGAGE DOOR 9" FROM THE BOTTOM AND 71/2" FROM THE AFT SIDE. REPAI RED IAW SRM 51-20-11, 51-20-16, AND 51-20-36. 2 H 7 2 4T RT A13NM 2007022000400 20070220 00400 NM 2007 2 20 QXEA200700166 1 20070213 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - GOUGE ON THE INNER SKIN OF THE BAGGAGE DOOR 21/2" FROM THE BOTTOM AND 24" FROM THE FORWARD SIDE. REPAIRED IAW SRM 51-20-11, AND RD8-52-884. 2 H 7 2 4T RT A13NM 2007022000402 20070220 00402 NM 2007 2 20 AWXA200700208 1 20070204 A 5755 D5155104020000 HINGE PIN AIRBUS A319 A319132 3930340 NM ZONE 500 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 831AW 1576 SAL - FOUND LEFT WING NR 2 SPOILER HINGE PIN WORN. REPLACED LEFT WING NR 2 SPOILER HINGE PIN IAW AWA TASK CARD C3L57322 . 2 L 7 2 4F RT A28NM 2007022000403 20070220 00403 NM 2007 2 20 AWXA200700209 1 20070204 A 5755 D57551039200000 HINGE PIN AIRBUS A319 A319132 3930340 NM ZONE 500 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 831AW 1576 SAL - FOUND LEFT WING NR 4 SPOILER CENTER HINGE PIN WORN. REPLACED LEFT WING NR 4 SPOILER CENTER HINGE PIN IAW AWA TAS K CARD C3L57322. 2 L 7 2 4F RT A28NM 2007022000404 20070220 00404 NM 2007 2 20 QXEA200700184 1 20070213 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 487 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - RIGHT INBOARD SEAT TRACK NR 8 HAS CORROSION IN CENTER OF TRACK AND ON EDGES OF CLAWS AT STATION X487. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2007022000408 20070220 00408 NM 2007 2 20 QXEA200700186 1 20070213 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 437 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - RIGHT INBOARD SEAT TRACK NR 8 HAS CORROSION ON THE INBOARD FLANGE AT STATION X437. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2007022000409 20070220 00409 NM 2007 2 20 QXEA200700185 1 20070213 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 440-452 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - RIGHT INBOARD SEAT TRACK NR 8 HAS GOUGE IN CENTER OF TRACK AT STATION X440 TO X452. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2007022000412 20070220 00412 NM 2007 2 20 XEA200700188 1 20070213 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 510 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - RIGHT OUTBOARD SEAT TRACK NR 12 HAS CORROSION ON TOP OF TRACK AT STATION X510. REPAIRED IAW RD8-53-3644. 2 H 7 2 4T RT A13NM 2007022000413 20070220 00413 NM 2007 2 20 QXEA200700182 1 20070211 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 450-465 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - LEFT SEAT TRACK NR 2 HAS CHAFE STATION 450 AND NICKS STATION 465. REPAIRED IAW RD8-53-1342. 2 H 7 2 4T RT A13NM 2007022100001 20070221 00001 SO 2007 2 21 SWIA200717804 1 20070213 A 3350 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 295SW 120322 FOUND EXIT ROW 6 RIGHT SIDE LIGHT INOP. RELAMPED EXIT ROW 6 EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007022100005 20070221 00005 SO 2007 2 21 SWIA200717808 1 20070212 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 227SW 120304 FOUND EMERGENCY EXIT SIGN AT ROW 9 IS INOP. REPAIRED BROKEN WIRE ON EXIT SIGN AT ROW 9 ON OVERHEAD BIN. OPERATIONAL C HECKS GOOD. 2 L 7 2 4T RT A31SO 2007022100007 20070221 00007 EA 2007 2 21 SWIA200717809 1 20070214 A 2913 887055 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA O OTHER K FLUID LOSS CR CRUISE 1 NM 07 910EV 7727 HYDRAULIC SYSTEM LOST ALL QUANTITY EN ROUTE. REPLACED LEFT ENGINE EDP IAW 29-13-00 AND CARBON SEALS ON EDP, AIR TURBINE STARTER AND IDG IAW RII 72-900-1000 AND MM 25-61-00. OPERATIONAL AND LEAKS CHECKS GOOD, S/N OFF MX-574191. 2 L 7 2 4F RT A21EA 2007022100008 20070221 00008 2007 2 21 2007UALA00355 4 20070208 A 2565 PROXIMITY SWITCH AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE L2 DOOR SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 845UA 1585 DOOR 2L SLIDE DOES NOT INDICATE AN ARMED IND WHEN ARMED. RECYCLED 2 TIMES, NO LUCK. [SUP 05-08-07] FAULTY PROXIMITY SWITCH. REPLACED SWITCH AND ADJUSTED TO PROPER CLEARANCE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100009 20070221 00009 NM 2007 2 21 2007UALA00358 1 20070206 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 DOOR 1R LWR GATE BOTTOM MID PORTION GATE FRAME CRACKED, FOUND AFTER REMOVING DOOR PRESSURE SEAL. REPLACED GATE ON DOOR FRAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100012 20070221 00012 NM 2007 2 21 2007UALA00361 1 20070208 A 5420 ANGLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 NR 2 PYLON MIDSPAR FITTING CLOSE-OUT ANGLE IS CRACKED, VERIFIED BY HFEC. STOPPED DRILLED CRACK AND INSTALLED STRAP REPA IR PER REO-G11942 REV C. PER UAL EVA-70073. MUST REPLACE CLOSE OUT ANGLE AT C-16-HMV VISIT. A/C RETURNED TO SERVICE. SUS PECT VIBRATION & HEAT ADD TO EARLY CRACKING OF CLOSE-OUT ANGLE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022100018 20070221 00018 SO 2007 2 21 SWIA200717814 1 20070216 A 5610 WINDSHIELD EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA O OTHER O OTHER LD LANDING 1 NM 07 299SW 120329 CAPTAIN'S WINDSHIELD PANE AND FO'S WINDSHIELD PANE SHATTERED ON LANDING ROLLOUT. REPLACED CAPTAIN'S WINDSHIELD IAW EMB1 20 AMM REF NR 56-10-01, P/N NP-151311-1 S/N OFF 04149146184. REPLACED FIRST OFFICER'S WINDSHIELD IAW EMB120 MM 56-10-01 AND RII 56-200-1000, P/N NP-151311-2, S/N OFF 1526H3005. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007022100019 20070221 00019 EA 2007 2 21 SWIA200717815 1 20070216 A 5610 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 758SK 10222 CAPTAIN'S WINDSHIELD CRACKED DURING LANDING ROLLOUT. REPLACED CAPTAINS WINDSHIELD IAW CRJ700 MM 56-11-01 AND PER RII 56 -220-1000, P/N OFF NP-139321-003 S/N 05089H4605. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007022100020 20070221 00020 NE 2007 2 21 2007UALA00363 2 20070208 A 7230 COMPRESSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE STALLED A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 482UA 1584 V11076 RTFL DUE TO NR 2 ENGINE COMPRESSOR STALL. [5-1-07] STALL OCCURRED AT TOP-OF-CLIMB AFTER TURNING-OFF THE ANTI-ICE VALVE . ALL CHECKS WERE PERFORMED PER THE AIRBUS TSM WITH NO FINDINGS. THE ENGINE PASSED POWER ASSURANCE RUN AND WAS RETURNE D TO SERVICE. SUSPECT THE STALL OCCURRED DUE TO A SIMULATANEOUS OCCURANCE OF THE SHUTTING OFF OF THE ANTI-ICE VALVE AND SOME ATMOSPHERIC EFFECTS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100021 20070221 00021 EA 2007 2 21 SWIA200717816 1 20070216 A 5610 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 754SK 10215 LEFT SIDE WINDOW SHATTERED ON TAKEOFF OUT OF DENVER. CAPTAINS WINDSHIELD CRACKED UPON INSTALLATION OF LEFT SIDE WINDOW. REPLACED CAPTAINS SIDE WINDOW IAW AMM 56-11-01 AND RII 56-220-1000, P/N OFF 601R33033-19, S/N 04329H3190. REPLACED CA PTAINS WINDSHIELD IAW AMM 56-11-01 AND RII 56-220-1000, P/N OFF 601R33033-17 S/N 04308H1158. 2 L 7 2 4F RT A21EA 2007022100023 20070221 00023 EA 2007 2 21 SWIA200717817 1 20070216 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 939SW 7742 PILOT'S LEFT WINDOW CRACKED DURING TAKEOFF. REPLACED LEFT SIDE WINDOW REFERENCE AMM 56-12-01 C/W RII 56-220-1000, P/N O FF 601R33053-11, S/N OFF 02269H6696. 2 L 7 2 4F RT A21EA 2007022100024 20070221 00024 EA 2007 2 21 SWIA200717818 1 20070216 A 5610 WINDSCREEN CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 410SW 7066 FIRST OFFICER'S WINDSCREEN SHATTERED ON PUSH BACK. REPLACED FIRST OFFICER'S WINDSCREEN IAW AMM 56-11-01 AND RII 56-220- 1000, PN OFF: NP-139321-6, SN OFF: NSN. 2 L 7 2 4F RT A21EA 2007022100025 20070221 00025 NM 2007 2 21 QXEA200700189 1 20070211 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 309-420 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - LEFT SEAT TRACK NR 1 HAS NICKS AND CHAFE DAMAGE AT STATION X309, STATION X342, STATION X366, STATION X420. REP AIRED IAW RD8-53-1342. 2 H 7 2 4T RT A13NM 2007022100026 20070221 00026 EU 2007 2 21 2007UALA00365 1 20070208 A 3350 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 449UA 851 EMERGENCY LIGHTS INOP AT DOOR 1L AND 1R, SEATS ROW 1, 2 AND 3 ABC. REPLACED BATTERY PACK AT DOOR 1L. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100027 20070221 00027 NM 2007 2 21 2007UALA00366 1 20070208 A 3397 CABLE BOEING 737 737322 1384676 NM IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 312UA 23673 AFT CABIN EEL LIGHTS INOP FROM ROW 15 AFT UP TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT. REPLACED EEL CABLE (560-0809) AND STRIP (560-0857). 2 L 7 2 4F 4 F RT A16WE E40NE 2007022100028 20070221 00028 NM 2007 2 21 2007UALA00367 1 20070208 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN MISINSTALLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 EEL STRIP IN FRONT OF FWD GALLEY CART STOWAGE COMPARTMENT INSTALLED UPSIDE DOWN. REINSTALLED EEL STRIP CORRECTLY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022100030 20070221 00030 NM 2007 2 21 2007UALA00369 1 20070208 A 3350 SIGN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 590UA 28708 LEFT FWD OVERWING EMERGENCY EXIT EMERGENCY SIGN INOPERATIVE MOUNTED ON SIDEWALL. REPLACED EXIT SIGN FWD OF FWD LT OVE RWING HATCH. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100031 20070221 00031 NM 2007 2 21 QXEA200700172 1 20070210 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - GOUGE ON INNER SKIN OF THE BAGGAGE DOOR 37" FROM THE TOP AND 2 1/2" FROM FORWARD SIDE. REPAIRED IAW SRM 51-20- 11, 51-20-16, AND 51-20-36. 2 H 7 2 4T RT A13NM 2007022100032 20070221 00032 NM 2007 2 21 QXEA200700171 1 20070210 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - GOUGE ON INNER SKIN OF THE BAGGAGE DOOR 20" FROM THE TOP AND 2 1/2" FROM THE AFT SIDE. REPAIRED IAW SRM 51-20- 11, 51-20-16, AND 51-20-36. 2 H 7 2 4T RT A13NM 2007022100033 20070221 00033 NM 2007 2 21 2007UALA00370 1 20070208 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 590UA 28708 EEL LIGHT IN FRONT OF MID LAV INOPERATIVE. SPLICED NEW PINS ONTO ENCAPSULATED LAMP WITH AMP CRIMPER. REPLACED EEL LIGHT LENS AND ENDCAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100034 20070221 00034 NM 2007 2 21 QXEA200700176 1 20070213 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - AIRCRAFT SKIN HAS CORROSION AROUND LOWER TCAS ANTENNA O-RING MATING AREA AND SCREW HOLES. REPAIRED IAW SRM 51- 20-11, 51-20-16. 2 H 7 2 4T RT A13NM 2007022100035 20070221 00035 NM 2007 2 21 QXEA200700175 1 20070210 A 5310 WINDOW POST DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - WINDSHIELD CENTER POST HAS THREE NUTPLATES CORRODED. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007022100041 20070221 00041 NM 2007 2 21 QXEA200700179 1 20070211 A 5340 FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - CORROSION FOUND AT THE AFT END OF THE FITTING CONNECTING SKIN TO THE VERTICAL SEAT TRACK SUPPORT LOCATED AT STR INGER 31S FORWARD OF FRAME STATION X201. REPAIRED IAW SRM 51-20-26. 2 H 7 2 4T RT A13NM 2007022100042 20070221 00042 2007 2 21 2007UALA00373 4 20070208 A 2565 SQUIB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 RIGHT OVERWING INTEGRATOR SQUIB FAILED SQUIB TEST. TROUBLESHOT SYSTEM TO BAD TIME DELAY RELAY (M1) ON RIGHT OFF-WING EXCAPE SYSTEM MODULE. REPLACED RELAY 10167-2001BT PER MM 25-65-00 AND 25-65-12 AND OPS CHECK GOOD. SLIDE PROBLEM ROOT C AUSE: RELAY DIRTY & STICKS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022100043 20070221 00043 NM 2007 2 21 QXEA200700180 1 20070211 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 201 S31S CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FRAME LOWER FLANGE AND VERTICAL KEEL BEAM AT STATION X201.15 AND STRINGER 31S ARE CORRODED NEAR FITTING AND ARO UND RIVETS. REPAIRED IAW SRM 51-20-36, 51-20-16, AND 51-20-26. 2 H 7 2 4T RT A13NM 2007022100044 20070221 00044 NM 2007 2 21 QXEA200700178 1 20070211 A 5510 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND FRAME CRACKED. LOCATED IN REAR FUSELAGE AT STRINGER NR 4 PORT. REPAIRED IAW SRM 51-20-16 AND 51-20-36, RD/8-55-199. 2 H 7 2 4T RT A13NM 2007022100045 20070221 00045 EA 2007 2 21 SWIA200717819 1 20070217 A 5610 601R3303320 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 724SK 9 9 10189 FIRST OFFICER'S SIDE WINDOW BROKEN. REPLACED FIRST OFFICER'S SIDE WINDOW REF CRJ 700 MM 56-12-07 AND RII 56-220-1000 ST EPS 1 THROUGH 7 AND 9, P/N ON 601R33033-12 P/N OFF 601R33033-20 S/N ON 06312H7366 S/N OFF 04199H1301. 2 L 7 2 4F RT A21EA 2007022100048 20070221 00048 NM 2007 2 21 QXEA200700208 1 20070215 A 5270 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM DOOR WARNING UNKNOWN A QXEA O OTHER N FALSE WARNING AP APPROACH 1 NM 09 421QX 4149 SEA FLIGHT NR 2379: FUSELAGE DOOR WARNING ON APPROACH AND ON TAXI. LEFT REAR BAGGAGE DOOR. LANDED WITHOUT INCIDENT. M AINTENANCE FOUND NO FAULTS ON THE PROX SENSOR COMPUTER. PROX SENSOR COMPUTER SHOWS ALL AFT BAGGAGE SENSORS GOOD WHEN DOO R CLOSED AND LOCKED. NO VISUAL DISCREPANCIES WITH DOOR OR DOOR HANDLE. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RE TURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007022100049 20070221 00049 NM 2007 2 21 AALA20070269 1 20070203 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 904AN 29506 MIA - EMERGENCY LIGHT AT SEAT 9D INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007022100050 20070221 00050 EU 2007 2 21 AALA20070278 1 20070203 A 3350 OL3229BPE BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70073 516 MIA - EMERGENCY LIGHT AT SEAT 20G INOPERATIVE. RELAMPED EMERGENCY LIGHT AS SEAT 20G. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A35EU 2007022000168 20070220 00168 NM 2007 2 20 QXEA200700192 1 20070113 A 2420 RELAY DHAV DHC8 DHC8202 2809007 NM NR 2 AC GEN MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 363PH 520 PDX FLIGHT 2048 - NR 2 AC GENERATOR CAUTION ILLUMINATED DURING CLIMB-OUT. RAN EMERGENCY CHECKLIST AND NR 2 AC GENERATOR CAUTION LIGHT REMAINED ILLUMINATED. RETURNED TO FIELD. MAINTENANCE REPLACED RELAY 2421-K2 IN RIGHT CONTACTOR BOX. OP ERATIONAL CHECK GOOD AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007022000169 20070220 00169 NM 2007 2 20 QXEA200700136 1 20070130 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 415QX 4081 C2 PDX - LEFT INBOARD SEAT TRACK IS CORRODED ON THE ENTRY FLOOR FLANGE FROM STATION X000-X032. REPAIRED IAW RD8/4-53-88 4 AND SRM 51-42-05, 51-42-90. 2 H 7 2 4T RT A13NM 2007022000170 20070220 00170 NM 2007 2 20 QXEA20070131 1 20070201 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 415QX 4081 C2 PDX - THERE IS HEAVY PITTING AT THE AFT SEAT TRACK LUGS AT X789.102 ON THE LEFT INBOARD SEAT RAIL. REPAIRED IAW RD8/ 4-53-884 AND SRM 51-40-07, 51-42-05, 51-40-15. 2 H 7 2 4T RT A13NM 2007022000173 20070220 00173 NM 2007 2 20 QXEA200700133 1 20070129 A 5320 FLOOR SUPPORT BOMBDR DHC8 DHC8402 1390042 NM BS 664-698 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 415QX 4081 C2 PDX - FLOOR PANEL ATTACH ANGLE JUST INBOARD OF THE AFT STAIRWAY TRACK AT THE AFT PASSENGER DOOR STATION X664 - X698 H AS VERY LIGHT SURFACE CORROSION IN SPOTS. REPAIRED IAW SRM 51-25-10 AND 51-42-35. 2 H 7 2 4T RT A13NM 2007022000175 20070220 00175 NM 2007 2 20 QXEA200700135 1 20070201 A 5320 SILL BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY EXIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 415QX 4081 C2 PDX - FOUND EMERGENCY EXIT LOWER SILL IS CORRODED AROUND BOTH LOWER LATCH FITTINGS. REPAIRED IAW SRM 51-21-00, RD8/4 -53-1829. 2 H 7 2 4T RT A13NM 2007022000184 20070220 00184 EA 2007 2 20 SWIA200717797 1 20070207 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 925SW 7682 FOUND LEFT EMERGENCY EXIT LOWER EXIT SIGN DOES NOT ILLUMINATE. REPLACED LEFT OVERWING LOWER EXIT LIGHTED SIGN AS REQUIR ED. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007022000188 20070220 00188 EA 2007 2 20 SWIA200717801 1 20070207 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 773SK 10236 FOUND EMERGENCY FLOOD LIGHT POD AT ROW 7 IS INOP. RELAMPED EMERGENCY LIGHTING CEILING FLOOD LIGHT AT ROW 7 PER 33-51-09 . OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007022000210 20070220 00210 NM 2007 2 20 SWAA070695 1 20070209 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007022000226 20070220 00226 NM 2007 2 20 SWAA070593 1 20070204 A 5313 6551698 STRINGER SPLICE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER S RM. 2 L 7 2 4F RT A16WE 2007022000227 20070220 00227 NM 2007 2 20 SWAA070598 1 20070204 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000241 20070220 00241 NM 2007 2 20 SWAA070945 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000257 20070220 00257 NM 2007 2 20 F3LA200700024 1 20070214 A 2121 EVT3454H BLOWER AIRBUS A319 A319111 3930336 NM AIR DISTRIBUTION DAMAGED A F3LA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NM 03 927FR 294 2209 ON SHORT FINAL, FLIGHT CREW REPORTED AN ELECTRICAL SMOKE SMELL IN THE COCKPIT AND LOUD SOUND OF FAN POWERING DOWN ALONG WITH A VENT BLOWER FAULT LIGHT. PER TSM 24-00-00-810-823, IDENTIFIED AVIONICS BLOWER FAN AS SOURCE OF SMELL. REPLACED AVIONICS BLOWER FAN REF MM 21-26-51, PG 401. OPS CHECKED GOOD, VENT BLOWER FAULT CLEARED. 2 L 7 2 4F RT A28NM 2007022000269 20070220 00269 NM 2007 2 20 SWAA070932 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000275 20070220 00275 EU 2007 2 20 07FDEA00481 1 20070215 A 5320 PLATE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 740FD 559 FOUND OLD REPAIR ON REAR CARGO DOOR SEALING PLATE C60-C60A IN FUSELAGE ABOVE DOOR. OLD REPAIR WAS VERIFICATION THAT IT IS PERFORMED IAW RAS DA/HAM-1083/98 ISSUE B. 2 L 7 2 4F RT A35EU 2007022000289 20070220 00289 NM 2007 2 20 SWAA070987 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 579, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007022000297 20070220 00297 NM 2007 2 20 SWAA070959 1 20070217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007022000327 20070220 00327 NM 2007 2 20 AWXA200700202 1 20070125 A 5753 6546435238 SKIN BOEING 737 7373S3 1384711 NM ZONE 600 DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND RIGHT WING OUTBOARD AFT FLAP LOWER SKIN HAS AREA OF DELAMINATION, WS 248.10 - WS 251.40, 19" FROM INBOARD E DGE. REPAIRED RIGHT WING OUTBOARD AFT FLAP LOWER SKIN WS 248.10 - WS 251.40, 19" FROM INBOARD EDGE IAW B737-300 SRM 51- 70-10-2R3. 2 L 7 2 4F RT A16WE 2007022000340 20070220 00340 NM 2007 2 20 QXEA200700126 1 20070204 A 3040 SYLZ50970 CONTROLLER DHAV DHC8 DHC8202 2809007 NM WINDSHIELD HEAT MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 365PH 12603 526 PDX FLIGHT 2260 - ON TAXI LEFT WINDSHIELD HOT CAUTION LIGHT ILLUMINATED. OAT WAS +5C. WINDSHIELD DID NOT FEEL HOT TO T HE TOUCH. MAINTENANCE REPLACED THE LEFT WINDSHIELD HEAT CONTROLLER AND COMPLIED WITH OPERATIONAL TEST OF THE WINDSHIELD HEATING SYSTEM IAW DHC-8 AMM TASK 30-41-00-710-801. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007022000342 20070220 00342 NM 2007 2 20 QXEA200700124 1 20070203 A 3240 21599 BRAKE ASSY DHAV DHC8 DHC8202 2809007 NM MLG VIBRATION A QXEA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 NM 09 350PH 77130 795 488 SEA FLIGHT NR 2010, VIBRATION COMING FROM LEFT SIDE BRAKES. MAINTENANCE REPLACED NR 1 AND NR 2 BRAKE ASSEMBLIES. BLED AND LEAK CHECKED BRAKES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007022000344 20070220 00344 NM 2007 2 20 QXEA200700130 1 20070205 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM MALFUNCTIONED A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 367PH 14797 413 511 SEA FLIGHT NR 2057 - INTERMITTENT SMOKE WARNING LIGHT. MAINTENANCE REPLACED NR 1 AND NR 2 SMOKE DETECTOR. OPERATIONAL CHECK PER 26-15-00-710-801. CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007022000347 20070220 00347 EU 2007 2 20 07FDEA00352 1 20070206 A 7830 UNKNOWN AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680 30025 NE THRUST REVERSER UNKNOWN A FDEA F C ACTIVATE FIRE EXT. ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 683FE 801 705228 ON PUSHING POWER UP FOR TAKEOFF, AFTER SELECTING TOGA, GOT NR 1 ENGINE REVERSER PRESSURIZED AT 50 KIAS. TAXIED BACK TO RAMP. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 16FEB07 "MEL 78-30-01-A: ENGINE NR 1 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION." 2 L 7 2 4F 4 F RT A35EU E13NE 2007022000350 20070220 00350 WP 2007 2 20 07FDEA00355 1 20070206 A 5712 ARB22172 RIB DOUG MD10 MD1010F 3022112 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 368FE 46606 WINGS, LT WING LOWER RIB CAP CRACKED AT XORS 402 STGR 35-36 REPAIR: DURING "C" CHECK INSPECTION WHILE ACCOMPLISHING ALI CARD 57X1203ALI-P2 BUTTERFLY CLIPS WERE FOUND TO BE CRACKED AND A 1" CRACK WAS FOUND IN THE SUBJECT ARB2217-2 RIB CAP BE TWEEN STRINGER35 AND 36. THE SUBJECT CRACKED CAP LOCATION IS SHOWN IN FIGURE 1. THE 4 BUTTERFLY CLIPS ARE LOCATED AT S TA XORS 402 STRINGERS 36L, 36R, AND 37L AND STA XORS 372 STRINGER 43R EA NR 8-5710-102778 HAS BEEN COMPLIED WITH AT TI MCO BY EMPLOYEE NR 7951 ON N/R'S N00809, N00811, N00813, N00827, N00814. 2 L 7 3 4F RT A22WE 2007022000371 20070220 00371 EU 2007 2 20 SA07011 1 20070211 A 3230 664700500A4D CONTROL UNIT AIRBUS 320 A320214 3930316 EU NR 2 FAULTY A USAA O OTHER O OTHER CL CLIMB 1 EA 19 124US 20304 1314 BOS FLT 1262 EN ROUTE CUN TO BOS. AFTER TAKEOFF AND GEAR RETRACTION, THE NOSE GEAR DID NOT COME UP AND THE MAIN GEAR DO ORS DID NOT CYCLE. THE GEAR WAS RECYCLED, AND THE GEAR RETRACTED NORMALLY. THE FLIGHT CONTINUED WITHOUT FURTHER INCIDE NT. MAINTENANCE REPLACED THE NR 2 LGCIU. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2007022000374 20070220 00374 NM 2007 2 20 2007UALA00349 1 20070207 A 5320 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 MID CABIN STA 616L INNER CHORD IS CRACKED AT LOWER FASTENER, FRAME TO STUB BEAM JOINT. MAJOR REPAIR. REMOVED DAMAGE. FABRICATED ANGLE REPAIR AND FILLER PER MM 53-11-89. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022000394 20070220 00394 EU 2007 2 20 AWXA200700218 1 20070214 A 5321 D5367180500500 FLOOR PANEL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 652AW 953 SAL - FOUND CORROSION ON MAIN CABIN FLOORBOARD 262 FF, FS 66 - FS 68, -Y1292 TO -Y1732. REPLACED MAIN CABIN FLOORBOARD 262 FF, FS 66 - FS 68, -Y1292 TO -Y1732 IAW AWA TASK CARD C1C53303. 2 L 7 2 4F RT A28NM 2007022000397 20070220 00397 NM 2007 2 20 QXEA200700170 1 20070213 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - GOUGE ON THE INNER SKIN OF THE BAGGAGE DOOR 28 3/4" FROM THE TOP AND 2 1/2" FROM THE AFT SIDE. REPAIRED IAW SR M 51-20-11, AND RD8-52-884. 2 H 7 2 4T RT A13NM 2007022000398 20070220 00398 NM 2007 2 20 QXEA200700164 1 20070210 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - CORROSION AROUND THE FASTENER HOLE ON THE FORWARD LOWER STRAP ON THE INNER SKIN OF THE BAGGAGE DOOR. REPAIRED IAW SRM 51-20-11, 51-20-16, AND 51-20-36. 2 H 7 2 4T RT A13NM 2007022000401 20070220 00401 NM 2007 2 20 QXEA200700167 1 20070210 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - GOUGE ON THE INNER SKIN OF THE BAGGAGE DOOR 3" FROM THE BOTTOM AND 21/2" FROM THE AFT SIDE. REPAIRED IAW SRM 5 1-20-11, 51-20-16, AND 51-20-36. 2 H 7 2 4T RT A13NM 2007022000405 20070220 00405 NM 2007 2 20 QXEA200700190 1 20070207 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 376-380 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - RIGHT INBOARD SEAT TRACK NR 7 HAS CORROSION IN THE CENTER OF TRACK AT STATION X376 TO X380. REPAIRED IAW RD8-5 3-1339. 2 H 7 2 4T RT A13NM 2007022000406 20070220 00406 NM 2007 2 20 2007UALA00357 1 20070206 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 DOOR L1 LOWER GATE HAS CORROSION. FOUND AFTER RUB STRIP REMOVED. CONFIRMED CORROSION. NEEDED TO REPLACE LOWER GATE ON DOOR FRAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022000407 20070220 00407 NM 2007 2 20 QXEA200700191 1 20070207 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 262 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - RIGHT SEAT TRACK NR 7 HAS CORROSION ON THE EDGE OF CLAWS AT STATION X262. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2007022100003 20070221 00003 EA 2007 2 21 SWIA200717806 1 20070213 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 410SW 7066 AFT EMERGENCY CEILING LIGHT INOP. REPLACED LAMP IN AFT CEILING EMERGENCY LIGHT AS NEEDED. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007022100004 20070221 00004 SO 2007 2 21 SWIA200717807 1 20070213 A 2597 CONNECTOR EMB 120 EMB120ER 3260203 SO COFFEEMAKER ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 296SW 120325 FOUND OVERHEATED ELECTRICAL SMELL IN CABIN. REPLACED CONNECTOR ON HOT JUG. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007022100006 20070221 00006 2007 2 21 2007UALA00353 4 20070207 A 2565 PROXIMITY SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT AFT SLIDE OUT OF ADJUST A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 427UA 512 LEFT AFT SLIDE INDICATION INOP ON DOOR-OXY SYSTEM ECAM PAGE - DOOR-OXY. [SUP 05-08-07] OUT OF ADJUSTMENT PROXIMITY SWI TCH. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100014 20070221 00014 EA 2007 2 21 SWIA200717811 1 20070216 A 5610 601R3303317 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 753SK 10214 AT 100 KNOTS ON TAKEOFF LEFT WINDSHIELD AND LEFT SIDE WINDOW CRACKED/SHATTERED. REPLACED LEFT WINDSHIELD AND LEFT SIDE WINDOW PER AMM 56-11-01 AND 56-12-01 AND RII CARDS RII 56-220-1000. WINDSHIELD S/N OFF: 04348H4434. LEFT SIDE WINDOW P/N OFF: 601R33033-19 S/N OFF: 04334H3285 2 L 7 2 4F RT A21EA 2007022100016 20070221 00016 EA 2007 2 21 SWIA200717812 1 20070216 A 5610 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 746SK 10202 ON CLIMB-OUT ABOUT FL190, THE F/O WINDSHIELD CRACKED. REPLACED RIGHT WINDSHIELD PER AMM 56-12-01. OPS CHECK GOOD, P/N OFF: NP139321-003, S/N OFF: 04231H3790. 2 L 7 2 4F RT A21EA 2007022100022 20070221 00022 2007 2 21 2007UALA00364 4 20070208 A 2565 INDICATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE READS LOW A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 549UA 25397 THE 1L SLIDE PACK NEEDLE READS LOW. ALLOWED INFLATION CYLINDER TEMP TO STABILIZE. PRESSURE GAUGE NEEDLE IS WITHIN LIMI TS. REPLACED MED 1L SLIDE. ALL SAFETY PINS WERE REMOVED AND STOWED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100051 20070221 00051 NM 2007 2 21 AALA20070279 1 20070204 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 962AN 30858 MIA - FOUND EMERGENCY LIGHT AT SEAT 7D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007022100052 20070221 00052 WP 2007 2 21 AALA20070280 1 20070204 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9629H 53599 LGA - OVERHEAD EMERGENCY LIGHTS IN COCKPIT INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007022100053 20070221 00053 EU 2007 2 21 AALA20070288 1 20070205 A 3350 OL3229BPE BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 MIA - EMERGENCY LIGHT AT SEAT ROW 1G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT ROW 1G. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A35EU 2007022100054 20070221 00054 WP 2007 2 21 AALA20070270 1 20070203 A 2530 2510000405 OVEN DOUG DC9 DC982 3022082 WP GALLEY INOPERATIVE A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 21 419AA 49331 ORD INFLIGHT FERRY FLIGHT T1173/03FEB - ON SHORT FINAL, CREW REPORTED ELECTRICAL BURNING SMELL AND SMOKE IN FIRST CLASS GALLEY. ALL OVENS WERE OFF. TURNED GALLEY POWER AND RECIRCULATION FANS OFF WITH NO HELP. LANDED ORD WITHOUT INCIDENT. REPLACED FIRST CLASS GALLEY OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007022100055 20070221 00055 WP 2007 2 21 AALA20070283 1 20070204 A 3350 BATTERY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT UNSECURE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 593AA 53256 SFO - EMERGENCY LIGHTS IN CEILING AT SEAT ROWS 23 TO 27 INOPERATIVE. RESEATED BATTERIES IN POWER SUPPLY FOR EMERGENCY L IGHTS IN CEILING AT SEAT ROWS 23 TO 27. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007022100056 20070221 00056 NM 2007 2 21 AALA20070272 1 20070203 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 177AN 32396 DFW - EXTERNAL EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. RELAMPED EXTERNAL EMERGENCY LIGHT AT LEFT NUMBER F OUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007022100057 20070221 00057 EU 2007 2 21 AALA20070282 1 20070204 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 33069 512 MIA - EMERGENCY LIGHTS FROM SEAT ROWS 19G TO 28G INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT ROWS 19G TO 28G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007022100063 20070221 00063 NM 2007 2 21 AALA20070180 1 20070124 A 3397 WIRE HARNESS BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 612AA 24488 MIA - EMERGENCY LIGHTS AT SEAT ROWS 26 TO 36 INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHTS AT SEAT ROWS 26 TO 36. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007022100065 20070221 00065 NE 2007 2 21 AALA20070181 2 20070124 A 7261 FILTER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RT ENGINE OIL CLOGGED A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 7519A 49896 717870 DFW INFLIGHT T1141/24JAN - RIGHT ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED IN FLIGHT AT FLIGHT LEVEL 300. OIL TEMPERA TURE 114 DEGREES. SHUT DOWN RIGHT ENGINE AND DESCENDED. ENGINE WINDMILLED FOR 38 MINUTES. FOUND METAL IN OIL SCREEN A ND FILTER. REPLACED RIGHT ENGINE ON 25 JAN AT DFW. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007022100072 20070221 00072 EA 2007 2 21 QXEA200700145 1 20070122 A 5754 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA RT SLAT DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 611QX 10041 C3 OKC - FOUND RIGHT SLAT PANEL 622CB HAS DAMAGE AT LEADING EDGE. REPAIRED IAW SRM 53-00-00, 51-20-08 AND 51-21-11. 2 L 7 2 4F RT A21EA 2007022100074 20070221 00074 EU 2007 2 21 AALA20070274 1 20070203 A 3350 BR964814 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70073 516 MIA - EMERGENCY LIGHT ASSEMBLY AT SEAT 14C BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 14C. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007022100076 20070221 00076 NM 2007 2 21 AALA20070290 1 20070205 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 632AA 24590 DFW - OVERWING EMERGENCY EXIT SIGN LIGHT AT MID CABIN CEILING IS MISSING LENS. REPLACED LENS FOR THE OVERWING EMERGENCY EXIT SIGN LIGHT AT MID CABIN CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007022100077 20070221 00077 NM 2007 2 21 AALA20070285 1 20070205 A 3350 0202503001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 773AN 29583 NRT - EMERGENCY EXIT LIGHT AT FIRST CLASS CLOSET MISSING LENS. REPLACED LENS FOR EMERGENCY EXIT LIGHT AT FIRST CLASS CL OSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007022100080 20070221 00080 WP 2007 2 21 AALA20070291 1 20070205 A 3213 STRUT DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 474 49649 ORD INFLIGHT T1349/05FEB - NOSE GEAR RED UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF DURING GEAR RETRACTION. CYCLED LANDING GEAR WITH NO CHANGE. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. PERFORMED NOSE LANDING GEAR STRUT INSPECTION AND SER VICE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007022100081 20070221 00081 EU 2007 2 21 AALA20070275 1 20070203 A 3350 BR964814 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70073 516 MIA - FOUND EMERGENCY LIGHT ASSEMBLY AT SEAT 21G BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 21G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007022100082 20070221 00082 EU 2007 2 21 AALA20070276 1 20070203 A 3350 OL3229BPE BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70073 516 MIA - EMERGENCY LIGHT AT SEAT 13G INOPERATIVE. RELAMPED EMERGENCY LIGHT AS SEAT 13G. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A35EU 2007022100083 20070221 00083 EU 2007 2 21 2007UALA00374 1 20070208 A 7830 FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 REVERSER CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 431UA 571 NR 2 INBOARD REVERSER AT 7:00 POS FRAME IS CRACKED IN HALF. AFT END OF CASCADE VANES ATTACH TO FRAME. [5-1-07] REPLACE D FRAME DURING HMV. FRAME HAS HISTORY IN THE INDUSTRY OF CRACKING, SERVICE BULLETIN IAE V2500-NAC-78-0209 ADDRESSES PART OF THE ISSUE . THE ROOT CAUSE IS VIBRATION INDUCED FATIQUE DUE TO LOOSE LOWER AND UPPER ATTACHMENT POINTS. A THRUST REV ERSER HEALTH CHECK TO CHECK THE SUPPORT BUSHINGS EVERY CCK IS BEING INSTITUTED. SERVICE BULLETIN 78-0209 IS ALSO INCORPO RATED INTO THE HEALTH CHECK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100086 20070221 00086 EU 2007 2 21 AALA20070277 1 20070203 A 3350 OL3229BPE BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70073 516 MIA - FOUND EMERGENCY LIGHT AT SEAT 19C INOPERATIVE. RELAMPED EMERGENCY LIGHT AS SEAT 19C. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A35EU 2007022100088 20070221 00088 NM 2007 2 21 2007UALA00375 1 20070207 A 7130 FIRESEAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 2 ENGINE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 309UA 23670 NR 2 ENGINE PYLON FIRE SEAL ASSY AT FWD END OF REVERSER HAS HOLE WORN IN IT AT CENTER LINE OF PYLON. MAJOR REPAIR. REM OVED DAMAGE. INSTALLED WEB REPAIR PER SRM 51-70-13. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022100090 20070221 00090 2007 2 21 UIEA200700066 4 20070204 A 3416 19039253 CADC BOEING 747 7472D7B 1384803 NM ALTIMETER STICKING A UIEA O OTHER J WARNING INDICATION CR CRUISE 1 EA 15 528MC 22472 DURING CLIMB CAPT ALTIMETER NEEDLE WOULD STICK IN POSITION CAUSING PULL-UP TERRAIN WARNINGS, DON’T SINK WARNING AUDIBLES , ALTIMETER READ 37.0, ATC 36.8. PERFORMED STATIC SYSTEM LEAK CHECK NORMAL AS PER MM 34-11-00. FOUND NR 1 CADC DEFECTI VE. REMOVED AND REPLACED CADC PER MM 34-12-01. SYSTEM TEST NORMAL AND IAWS TEST NORMAL AS PER 34-11-00/34-46-01. 2 L 7 4 4F RT A20WE 2007022100095 20070221 00095 EU 2007 2 21 2007UALA00175 1 20070123 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 468UA 1363 BOTH PILOTS REPORTED A NAUSEOUS FEELING INFLIGHT. CREW COMMENTS: STRONG DISINFECTANT ODOR IN CABIN. ODOR PRESENT DURI NG INITIAL PACK RUN. AFTER ENGINE RUN AND SWITCHING BLEED SOURCE BETWEEN APU AND ENGINE, SMELL DISSIPATED AND DID NOT R ETURN. RAN PACKS ON HOT AND HIGH FLOW TO GENERATE ODOR, NO ODOR. CONFIRMED WITH CAPTAIN AND CAPTAIN AGREED NO ODOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100096 20070221 00096 NM 2007 2 21 UIEA200700062 1 20070129 A 5311 FRAME BOEING 747 747341 13848AM NM GE CF6 CF650E2 30018 NE BS 420 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 CRACK FOUND ON DOUBLER NEAR MAIN DECK FRAME WEB STRINGER CUT-OUT AT STATION 420R STRINGER 14 RT. REPAIRED, REMOVED STRI NGER CLIPS AND PERFORMED DVI. ALL HOLES NDT INSPECTED. FABRICATED AND INSTALLED FLAT REPAIR DOUBLER AND INSTALLED PER BOEING MESSAGE 1-273634952-2. 2 L 7 4 4F 4 F RT A20WE E23EA 2007022100097 20070221 00097 NM 2007 2 21 2007UALA00415 1 20070209 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 799UA 26926 EMERGENCY LIGHT STRIP AT 1L LOOSE. FOUND LIGHT OPERATIONAL BUT LOOSE. SECURED FWD SEAT 1F EMERG LIGHT, LIGHT CHECKS O K. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007022100098 20070221 00098 NM 2007 2 21 AWXA200700177 1 20070114 A 5210 507945236 SKIN BOEING 737 7373S3 1384711 NM ZONE 800 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 MCN - L1 DOOR INNER SKIN CRACKED, BS 347.30, BETWEEN BEAM 12 - BEAM 13 AT NR 6 STOP PIN FITTING FROM TOP. REPAIRED L1 D OOR INNER SKIN, BS 347.30, BETWEEN BEAM 12 - BEAM 13 AT NR 6 STOP PIN FITTING FROM TOP IAW AWA ER 03-5211-07035-TH3. 2 L 7 2 4F RT A16WE 2007022100099 20070221 00099 NM 2007 2 21 AWXA200700178 1 20070114 A 5210 501945259 SKIN BOEING 737 7373S3 1384711 NM ZONE 800 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 MCN - L1 DOOR AFT FRAME CRACKED, BS 347.30, BETWEEN BEAM 12 - BEAM 13 AT NR 6 AND NR 7 STOP PIN HOLES FROM TOP. REPAIR ED L1 DOOR AFT FRAME, BS 347.30, BETWEEN BEAM 12 - BEAM 13 AT NR 6 AND NR 7 STOP PIN HOLES FROM TOP IAW AWA ER 03-5211-0 7035-TH3. 2 L 7 2 4F RT A16WE 2007022100100 20070221 00100 NM 2007 2 21 AWXA200700179 1 20070121 A 5340 69429494 STRINGER CLIP BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 MCN - CRACKED STRINGER CLIP, BS 807, S26R. REPLACED STRINGER CLIP, BS 807, S26R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007022100101 20070221 00101 NM 2007 2 21 AWXA200700180 1 20070201 A 5330 6545775594 SKIN PANEL BOEING 737 7373S3 1384711 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 MCN - FUSELAGE SKIN CRACKED, B/S 754, S25R. REPAIRED FUSELAGE SKIN, B/S 754, S25R IAW B737-300 SRM 53-00-01-2R-31 FIGUR E 201. 2 L 7 2 4F RT A16WE 2007022100103 20070221 00103 NM 2007 2 21 AWXA200700181 1 20070121 A 5340 69429495 STRINGER CLIP BOEING 737 7373S3 1384711 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 MCN - CRACKED STRINGER CLIP, BS 827, S26R. REPLACED STRINGER CLIP, BS 827, S26R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007022100104 20070221 00104 NM 2007 2 21 AWXA200700182 1 20070115 A 5320 6551629501 REVEAL BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 MCN - CRACKED R1 DOOR CUTOUT REVEL, BS 296, S10R. REPLACED R1 DOOR CUTOUT REVEL, BS 296, S10R IAW B737-300 SRM 51-40-05 . 2 L 7 2 4F RT A16WE 2007022100105 20070221 00105 NM 2007 2 21 2007UALA00417 1 20070209 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 DOOR 2R UPPER GATE, INBOARD GATE FRAME CRACKED. WELD REPAIR ACCOMPLISHED FOR 2 EA CRACKS ON DOOR GATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100110 20070221 00110 NM 2007 2 21 2007UALA00418 1 20070209 A 5241 PLATE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 327UA 24147 FWD GALLEY DOOR BODY TORQUE TUBE LOWER HINGE UPPER STOP PLATE HAS A GAP. REPLACED UPPER AND LOWER TORQUE TUBE BEARINGS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022100117 20070221 00117 EU 2007 2 21 2007UALA00420 1 20070212 A 2597 WIRE HARNESS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EVAC SLIDE MISROUTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 441UA 751 DOOR 1R MED EVACUATION SLIDE ELECTRICAL HARNESS IS INCORRECTLY ROUTED. [SUP 05-16-07] REINSTALLED ELECTRICAL HARNESS C ORRECTLY. SLIDE IS ORIGINAL EQUIPMENT FROM WHEN AIRCRAFT WAS DELIVERED AND THERE IS NO EVIDENCE OF THE SLIDE EVER BEING SERVICED TO THE EXTENT THAT DISTURBANCE OF THE WIRING HARNESS WAS REQUIRED. UNABLE TO DETERMINE IF THE HARNESS MISROUTE IS AN ERROR FROM THE FACTORY OR DUE TO AN INTERMEDIATE SERVICING. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100122 20070221 00122 NM 2007 2 21 UIEA200700009 1 20070118 A 5311 65B01838136 FRAME BOEING 747 7472D7B 1384803 NM BS 488 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 NR 1R BS 488 CUTOUT FRAME WEB AT STOP NR 1 FOUND CRACKED. NR 1R BS 488 FRAME REPAIRED PER SRM 53-10-04 FIG 92. 2 L 7 4 4F RT A20WE 2007022100125 20070221 00125 NM 2007 2 21 UIEA200700005 1 20070110 A 5311 65B01838135 FRAME BOEING 747 7472D7B 1384803 NM BS 488 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 DURING PERFORMANCE OF EO NR 4753A531 AS PER AD 2005-22-06, AS PER NON ROUTINE CARD NR 212 CRACK FOUND DURING HFEC AT BS 488 MAIN ENTRY DOOR 1R CUT OUT FRAME WEB AT STOP 9. BS 488 MED FRAME REPAIRED AS PER SRM 53-10-04 FIG 121. 2 L 7 4 4F RT A20WE 2007022100126 20070221 00126 NM 2007 2 21 UIEA200700011 1 20070122 A 5730 SKIN BOEING 747 7472D7B 1384803 NM LT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 527MC 22471 LT WING, UPPER SURFACE, TRAILING EDGE PANEL, AFT OF REAR SPAR, WBL 445 IS CRACKED AROUND FASTENER HOLE. ACCOMPLISHED PE RMANENT REPAIR AS PER B747-200 SRM 51-40-09 FIG 2, SHEETS 1 THRU 5. REPAIR AREA IS 4.0 INCH BY 4.0 INCH ALSO, REFERENCE ATLAS AIR EO NR 4757A339. 2 L 7 4 4F RT A20WE 2007022100130 20070221 00130 NM 2007 2 21 UIEA200700014 1 20070123 A 7830 9059M72G03 COWLING BOEING 747 7472D7B 1384803 NM THRUST REVERSER CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 AS PER N/R 746, NR 3 ENG RT T/REV TRANSLATING COWL UPPER FAIRING (BEAVER TAIL) INTERIOR SKIN FOUND CRACKED. REPAIRED AC COMPLISHED AS PER EO NR 4778A089 AND FAA FORM 8110-3 DATED 12 JAN, 2007. 2 L 7 4 4F RT A20WE 2007022100131 20070221 00131 NM 2007 2 21 UIEA200700015 1 20070123 A 5310 65B04913428 CREASE BEAM BOEING 747 7472D7B 1384803 NM BS 940-960 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 M/DECK STA 940-960 S-7R TO S-8R CREASE BEAM WEB FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER SRM 51-10-01. 2 L 7 4 4F RT A20WE 2007022100132 20070221 00132 NM 2007 2 21 UIEA200700016 1 20070124 A 5712 65B149153 RIB BOEING 747 7472D7B 1384803 NM LT WING LE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 96210 21783 LT WING INBOARD FIXED LEADING EDGE RIB AT ILES 1024.45 FOUND CRACKED IN THE INTEGRAL STIFFENER ATTACHING THE UPSTOP FITT ING INTERCOSTAL. INTERIM REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-271219411 AND FAA FORM 8100-9. 2 L 7 4 4F RT A20WE 2007022100133 20070221 00133 NM 2007 2 21 UIEA200700034 1 20070129 A 5414 65B9405315 SKIN BOEING 747 7472D7B 1384803 NM NR 3 NACELLE CHAFED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 NR 3 PYLON RT ACCESS PANEL 473AR CUTOUT AT NAC STA 286 TO STA 300 FOUND CHAFING. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-272049267 AND FAA FORM 8110-9. 2 L 7 4 4F RT A20WE 2007022100134 20070221 00134 EU 2007 2 21 2007UALA00422 1 20070212 A 2150 A/C PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 OVERHEATED A UALA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 404UA 450 PACK 2 OVERHEAT DISPLAYED ON UPPER ECAM SCREEN. AIR CREW COMMENTS: FLIGHT ATTENDANT OBSERVED VERY FAINT SMOKE IN BACK AS WELL AS ODOR. [SUP 05-16-07] DETERMINED THAT AIR CYCLE MACHINE IN PACK 2 HAD SEIZED DUE TO FAILED BEARINGS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100135 20070221 00135 NM 2007 2 21 2007UALA00424 1 20070212 A 3350 COVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 596UA 28749 EEL STRIP COVER IS DAMAGED JUST FWD OF AFT FWD LAV APPROX 1.500 FT DAMAGED. REPLACED 25' SECTION OF EEL STRIP COVER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100136 20070221 00136 NM 2007 2 21 2007UALA00425 1 20070212 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 596UA 28749 AFT RT OVERWING EXIT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100140 20070221 00140 NM 2007 2 21 2007UALA00430 1 20070213 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT LIGHT INOP AT DOOR 2 RIGHT CEILING ENTRY. RELAMPED. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022100141 20070221 00141 NM 2007 2 21 2007UALA00431 1 20070213 A 3350 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 P5 EMERGENCY STANDBY LIGHTING FAILS TO ILLUM MODULES BACKLIGHTING. REPLACED DIMMING MODULE FUSE, CHKS OK 2 L 7 4 4F 4 F RT A20WE E24NE 2007022100143 20070221 00143 2007 2 21 2007UALA00433 4 20070212 A 2565 FASTENER BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EVAC SLIDE LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 910UA 25254 VELCRO LOOSE 2R SLIDE. UNDETERMINED CAUSE. SECURED VELCRO. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022100144 20070221 00144 2007 2 21 2007UALA00434 4 20070209 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT OVERWING FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 404UA 450 FOUND AT PTP PANEL TEST LEFT INTER EXTERNAL FAULTS. [SUP 05-16-07] REPLACED THE LT OVERWING SLIDE ASSEMBLY. AT OVERHAU L, DETERMINED THAT THE PACK BOARD WAS FAULTY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100145 20070221 00145 NM 2007 2 21 2007UALA00435 1 20070209 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 AFT PIT CENTER LINE FLOOR SUPPORT CHANNEL BETWEEN STA 1400 AND 1420 CRACKED. MAJOR REPAIR ACCOMPLISHED. STOP DRILLED CRACKS. APPLIED CORROSION INHIBITING COMPOUND. TO REINSPECT AT A-CHECK. TO REPAIR OR REPLACE STRINGER AT C-CHECK. TO CONTACT ENGINEERING IF ANY CRACKS ARE DETECTED AT A-CK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100147 20070221 00147 EU 2007 2 21 2007UALA00437 1 20070213 A 5314 ATTACH ANGLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 430UA 568 KEEL BEAM LWR RIGHT WEB UPPER ATTACH ANGLE IS CRACKED JUST FWD OF FR 47. MAJOR REPAIR ACCOMPLISHED: REPLACED ANGLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100150 20070221 00150 NM 2007 2 21 2007UALA00440 1 20070213 A 2121 FAN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN SMOKE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 781UA 26945 CREW REPORTED SMOKE IN THE CABIN AROUND DOORS 2 LT & RT WITH ELECTRICAL ODOR. RAN PACKS, GALLEY CHILLERS, COFFEE MAKERS AND OVENS IN BUSINESS CLASS GALLEY. NO DEFECTS FOUND. IDENTIFIED LOWER LT RECIRCULATION FAN FAILURE AS CAUSE OF STRONG ELECTRICAL ODOR AND SMOKE. FAN REPLACED. SYSTEM OP CHECKED OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007022100152 20070221 00152 EU 2007 2 21 2007UALA00442 1 20070213 A 5313 FASTENER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FWD CARGO BAY CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 430UA 568 FWD PIT STRINGER ATTACH FASTENERS ARE CORRODED FROM FRAME 29 TO 34 BETWEEN STR 38R AND 38L. REPLACED 562 CORRODED FASTE NERS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100153 20070221 00153 NM 2007 2 21 2007UALA00443 1 20070213 A 3397 CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 311UA 23672 AFT 15 FEET OF EEL LIGHT INOPERATIVE. REPLACED EEL CABLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022100155 20070221 00155 NM 2007 2 21 2007UALA00445 1 20070213 A 3397 CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 346UA 24250 AFT CABIN EEL LIGHT STRIPS INOP FROM ROW 15 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTME NT. REPLACED CABLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022100159 20070221 00159 EU 2007 2 21 2007UALA00245 1 20070127 A 5210 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 479UA 1538 FLIGHT ATTENDANT ADVISES BOTTLE PRESSURE AT DOOR 1L READS LOW. REPLACED DOOR 1L DOOR-DAMPER AND EMERGENCY-OPERATION CYL INDER. COMPLETE INSPECTION OF REPLACED BOTTLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100164 20070221 00164 EU 2007 2 21 2007UALA00250 1 20070129 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 438UA 678 AFT RIGHT DOOR SILL PLATE IS CORRODED BEYOND LIMITS AT FWD AND AFT ENDS. MAJOR REPAIR. REPLACED R2 DOOR SILL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100165 20070221 00165 NM 2007 2 21 2007UALA00251 1 20070129 A 2621 FIRE BOTTLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 ENGINE OBSTRUCTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 824UA 965 NR 2 ENGINE FIREX DISCHARGE LINE 4 EA OPENINGS ALL CAPPED WITH FLEX HOSE AND PLUG TEST EQUIPMENT. FIREX LINE IS DIRECTL Y ABOVE ENGINE FAN CASE. TEST EQUIPMENT WAS FOUND DURING OPEN UP. [SUP 05-16-07] THE INSTALLED CAPS, FLEX HOSE AND TE ST EQUIPMENT ARE USED DURING A PRESSURIZED LEAK TEST OF THE EXTINGUISHER DISCHARGE SYSTEM. THIS TEST WAS LAST PERFORMED ON THE AFFECTED AIRCRAFT DURING A REGULARLY SCHEDULED C-CHECK ON 8/29/2005. AT THAT TIME, THE MECHANICS WHO PERFORMED TH E TEST FAILED TO PUT THE DISCHARGE SYSTEM BACK INTO A FLIGHT WORTHY CONDITION AND THE ERROR WAS NOT DISCOVERED TILL THE MOST RECENT C-CHECK WAS PERFORMED ON 1/29/2007. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100166 20070221 00166 2007 2 21 2007UALA00252 4 20070129 A 2565 CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EVAC SLIDE MISROUTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 376UA 24641 DOOR 2R DOOR SLIDE GIRT BAR INFLATION CABLE ROUTED INCORRECTLY. GIRT BAR INFLATION CABLE ROUTED INCORRECTLY. ROUTED CAB LE CORRECTLY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022100167 20070221 00167 NM 2007 2 21 2007UALA00253 1 20070129 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 EXT FUSELAGE SKIN BENT & DAMAGED AT AFT GALLEY DOOR LOWER HINGE CUTOUT. MAJOR REPAIR: FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIR PER SRM 53-60-01 REPAIR NR 7. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022100168 20070221 00168 NM 2007 2 21 2007UALA00254 1 20070129 A 5320 RIVET BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 TWO EA RIVET HEADS ARE BROKEN AND CRACKED LOCATED ON FWD ROW OF BUTT SPLICE STA 259.5 AND LWR TWO ROWS OF STR 19L LAP SP LICE. MAJOR REPAIR: REPLACED FASTENERS PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022100170 20070221 00170 NM 2007 2 21 2007UALA00256 1 20070129 A 5420 WEB BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 1 NACELLE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 217UA 30550 NR 1 NACELLE AFT FAIRING LWR WEB HAS 45 PERCENT IACS AT AREA NR 2. REPAIRED PER SRM 51-20-13. REPAIR COMPLETE. OK FOR RETURN TO SERVICE. SUSPECT PREVIOUS HEAT RELEASE INTO FAIRING DUE TO LEAKAGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007022100175 20070221 00175 NM 2007 2 21 2007UALA00261 1 20070131 A 3350 276005 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BATTERY CHARGER BLOWN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY OVERWING LIGHT RIGHT 2 BOTTOM LIGHT INOP. *S/D* REPLACED BATTERY CHARGER FUSE. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022100178 20070221 00178 NM 2007 2 21 2007UALA00264 1 20070131 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN UNKNOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 EMERGENCY EXIT LIGHTS COME ON & GO OFF IN BUSINESS CLASS. TESTED EEL LIGHTS SEVERAL TIMES AND FOUND NO DEFECTS IN OPERA TION. UNABLE TO DUPLICATE.A/C RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022100180 20070221 00180 NM 2007 2 21 2007UALA00266 1 20070201 A 3350 LAMP BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 RIGHT OVERWING AFT EMERGENCY ILLUM LIGHT INOPERATIVE. RELAMPED, OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022100182 20070221 00182 NM 2007 2 21 2007UALA00268 1 20070201 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EEL INOP AT ROWS 50 & 59 RIGHT. REPLACED LAMP ASSY IN BOTH POSITIONS. BOTH OP CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022100186 20070221 00186 EU 2007 2 21 2007UALA00272 1 20070131 A 5210 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR OUT OF LIMITS A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 447UA 836 DOOR 2L BOTTLE PRESSURE IS OUT OF LIMITS. [SUP 05-08-07] THE DOOR 2L ASSIST BOTTLE BEING BELOW LIMITS WAS A REGULAR OC CURRENCE ON THIS AIRCRAFT. AT THE NEXT OCCURRENCE OF THE SAME FAULT, IT WAS DETERMINED THAT THE DOOR DAMPER CYLINDER WAS FAULTY AND IT WAS REPLACED. OVERHAUL OF THE DAMPER CYLINDER FOUND A PUNCTURED DIAPHRAGM, WHICH WAS ALLOWING A SLOW LEAK IN THE SYSTEM AND RESULTED IN THE CHRONIC LOW ASSIST BOTTLE CONDITION. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100187 20070221 00187 NE 2007 2 21 2007UALA00273 2 20070131 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 STALLED A UALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 WP 29 442UA 780 V10497 ENGINE 2 STALL ECAM MSG MOMENTARY AT SAME TIME OF LIGHTNING STRIKE. CREW ADVISED OF AUDIO POP AT SAME TIME AS LIGHTNING STRIKE. EVENT OCCURRED ACFT TURNING FINAL. ENGINE PARAMETERS NORMAL BEFORE AND AFTER STALL EVENT. COMPRESSOR STALL N EAR LIGHTENING STRIKES IS NOT UNCOMMON. THIS IS DUE TO THE TUBULENCE CREATED BY THE LIGHTENING. THIS ENGINE WAS INSPEC TED PER THE AIRBUS TSM AND NO DISCREPANCIES WERE FOUND. AS A PRECAUSTION, THE VSV SYSTEM WAS LUBRICATED. THE ENGINE PA SSED ITS POWER ASSURANCE RUN AND RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100188 20070221 00188 NM 2007 2 21 2007UALA00274 1 20070131 A 3397 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 657UA 27112 EEL STRIP LEFT FWD CABIN INOPERATIVE. REPAIRED EEL CABLE. A/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022100189 20070221 00189 NM 2007 2 21 2007UALA00275 1 20070131 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 305UA 23666 ROW 16 ON BACK, EMERGENCY EXIT LIGHTS DON'T WORK. REPLACED POWER STRIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007030100122 20070301 00122 NM 2007 3 1 UIEA200700069 1 20070211 A 2913 4205401 PUMP BOEING 747 74747UF 1384949 NM GE CF6 CF680C2B2 30025 NE HYD SYSTEM UNSERVICEABLE A UIEA O OTHER K FLUID LOSS CR CRUISE 1 EA 15 409MC 30558 30558 HYD QTY LOW NR 2 EICAS MSG QTY 0. FOUND HYD FLUID LEAKING FROM NR 2 EDP (FLUID STILL IN SYSTEM). REMOVED AND REPLACED NR 2 EDP PER MM 29-11-08, OPS, LEAK CHECK OK AND ALL INDICATION ON PRESSURE NORMAL. REMOVED AND REPLACED NR 2 CASE DRAI N FILTER PER MM 29-11-14 CHECKED OK PER MM 29-11-14. 2 L 7 4 4F 4 F RT 1384945 E13NE 2007022100194 20070221 00194 NM 2007 2 21 2007UALA00281 1 20070201 A 5210 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 FORWARD GALLEY DOOR S/N 1113, AFT FRAME IS CRACKED AT OPENING FOR 3RD STOP FITTING ON INBOARD SIDE. MAJOR REPAIR: REMO VED DAMAGE. INSTALLED NEW REPAIR ANGLE PER SM 90-52-40-14-JD PAGE 24 FIGURE 10 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022100195 20070221 00195 NM 2007 2 21 2007UALA00282 1 20070201 A 5347 ATTACH FITTING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 MAIN CABIN FLOOR SEAT TRACK ATTACH PLATE CORRODED AT FLOORBEAM UPPER CHORD, BS 365, RBL 28, WL 208. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100197 20070221 00197 NM 2007 2 21 UIEA200700020 1 20070125 A 5414 SKIN BOEING 747 7472D7B 1384803 NM NR 1 NACELLE DEBONDED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC MCB02130 21783 NR 1 ENGINE RT T/REV TRANSLATING COWL UPPER EDGE SKIN FOUND DEBOND. REPAIR ACCOMPLISHED AS PER EO NR 4778A088 AND FAA F ORM 8110-3. 2 L 7 4 4F RT A20WE 2007022100201 20070221 00201 2007 2 21 2007UALA00287 4 20070201 A 2565 CYLINDER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE OUT OF TOLERANCE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 RIGHT & LEFT OFFWING SLIDE CYLINDERS ARE OUT OF TOLERANCE. RT OFFWING SLIDE CYLINDER LIMIT OVERDUE, DATE OF MANUFACTURE 4-92. CYLINDER NOT OUT OF DATE DOD, 26JAN07, BUT WILL NOT HAVE 20 MONTHS REMAINING. REPLACED CYLINDER. OPS CHECK SQU IB TEST FOR NORMAL READING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100202 20070221 00202 NM 2007 2 21 2007UALA00288 1 20070201 A 3350 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 LEFT SEAT 26 EMERGENCY LIGHT BULB MISSING. INSTALLED A NEW BULB. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100203 20070221 00203 NM 2007 2 21 2007UALA00289 1 20070201 A 3397 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 GALLEY 1B EMERGENCY LIGHT CONNECTOR BROKEN. REPAIRED EEL CONNECTOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100204 20070221 00204 NM 2007 2 21 2007UALA00290 1 20070201 A 5210 SPRING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 DOOR 4R HAS ARMING FLIP DOOR SPRING NOT HOLDING DOOR CLOSED. REPOSITIONED SPRING AND MADE READJUSTMENTS TO DOOR RIG. N O COMPONENTS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022100205 20070221 00205 NM 2007 2 21 2007UALA00291 1 20070202 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY EXIT LIGHTS AT DOOR 5L X AISLE, THE UPPER DECK SIDE WALL ADJACENT TO LAVS, 2J FWD & AT 2J AFT ARE INOPERATIVE. RESECURED EEL FEEDER CONNECTOR IN EACH POSITION. OP CHECKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022100206 20070221 00206 NM 2007 2 21 2007UALA00292 1 20070202 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY LIGHT AT DOOR 3R SLIDE LIGHT DIM AND THE EMERGENCY LIGHTS AT 32 RT CEILING & AT ROWS 16 & 17 ARE INOPERATIVE. RELAMPED EMERGENCY LIGHT AT EACH POSITION. ALL EEL OP CK NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022100211 20070221 00211 EA 2007 2 21 A6WA200740044 1 20070124 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 447AW 7812 FOUND LT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT HOLE NR 16 PN. 550HB, HAS MINOR PITTING AT IB END IN AN AREA APPR OX 3.25 INCH LONG BY .003 INCH DEEP IN NON-CRITICAL AREA. (M) MAINTENANCE REPAIRED WING PLANK HOLE NR 16 (550 HB) IAW REO 601R-57-21-030 REV F AND EO E06/021/457, REV A. (K) 2 L 7 2 4F RT A21EA 2007030200026 20070302 00026 NM 2007 3 2 EIA2007018 1 20070215 A 5320 PAC1504100506 INTERCOSTAL BOEING 747 747273C 1384896 NM BS 2280-2320 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 FOUND INTERCOSTAL MOUNTING SCREW HOLE FLANGE AREA CRACKED AT STA 2280 TO 2320 AT LBL 76. CRACKED INTERCOSTAL REPLACED I AW B747 SRM 51-10-01 PG 6-9 AND SRM 51-30-02 PG 5-9. NEW INTERCOSTAL MADE FROM BAC 1509-100506, 7075-76. 2 L 7 4 4F A20WE 2007030200027 20070302 00027 NM 2007 3 2 EIA2007020 1 20070222 A 2611 30231R7 SMOKE DETECTOR BOEING 747 747121 1384871 NM NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480EV 20348 FOUND LOWER DECK NR 4 SMOKE DETECTOR WILL NOT TEST. REPLACED SMOKE DETECTOR IAW MM 26-16-00, ALL TESTS OK. 2 L 7 4 4F A20WE 2007030200029 20070302 00029 NM 2007 3 2 SWAA071122 1 20070226 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 336, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030500011 20070305 00011 NM 2007 3 5 NOCA03107 1 20070207 A 3350 S417T51013 LIGHT BOEING 767 767300 1385204 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 768NA 29898 FWD GALLEY RT SIDE ELECTRO LUMINESCENT E-PATH LIGHT STRIP INOP. REPLACED LUMINESCENT E-PATH STRIP PER AMM 33-00-00. 2 L 7 2 4F RT A1NM 2007030500025 20070305 00025 EU 2007 3 5 AWXA200700206 1 20070112 A 3260 SENSOR AIRBUS 320 A320232 3930326 EU NLG OUT OF ADJUST A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 605AW 543 FLIGHT 297: MSP - LAS - AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT. CREW LOWERED LDG GEAR HANDLE PER ECAM AND THE "L/G GEAR NOT UPLOCKED" ECAM MSG REMAINED. DECLARED EMERGENCY AND RETURNED TO MSP, THE LANDING WAS UNEVENTFUL. MX REMOVED A ND REPLACED L/G SELECTOR VALVE PER MM 32-31-12-000-001. PERFORMED LANDING GEAR SWING/NORMAL CHECK PER AWA TASK CARD F4M 32301 (INSTALLED LOAN BORROW PART #114079015 S/N 05291). SYSTEM OPS CHECK WAS GOOD. A/C WAS BEING MX FERRIED TO PHX FO R NLG ISSUES WHEN SHORTLY AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT. SOC AND MOC REQUESTED THE CREW TO RETURN TO M SP. THE LANDING WAS UNEVENTFUL. MX PERFORMED A BORESCOPE OF THE NLG UPPER SUPPORT ANTI-ROTATION LUGS, NO DEFECTS NOTED 2 L 7 2 4F RT A28NM 2007030500028 20070305 00028 SO 2007 3 5 SIMA200705002 1 20070215 A 5320 14529063003 ANGLE EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 848AE 9680 4800 145710 FOUND ANGLE FROM FLOOR SUPPORT TO SERVICE DOOR SILL CORRODED. REMOVED AND REPLACED IAW EMB SRM 51-40-02. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007030500031 20070305 00031 EU 2007 3 5 07FDEA00511 1 20070216 A 5315 FLOORBEAM AIRBUS 310 A310222 3930315 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 FOUND FWD CARGO COMPT, FR 38, FLOORBEAM, LBL66, (1) EA CRACK IN RADIUS 0.380 INCH LENGTH. REPAIRED FLOORBEAM PER A310-2 00 SRM 53-10-15. 2 L 7 2 4F RT A35EU 2007030500035 20070305 00035 EU 2007 3 5 07FDEA00515 1 20070216 A 5347 SEAT TRACK AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 FOUND SEAT TRACK AT R-5 2EA SPOTS OF CORROSION BETWEEN FR 38.2 AND 40/41. REMOVED AND REPLACED SEAT TRACK IAW A310 SRM 51-40-21 AND 53-10-16. 2 L 7 2 4F RT A35EU 2007030500042 20070305 00042 WP 2007 3 5 AALA20070293 1 20070206 A 2820 SEAL DOUG DC9 DC982 3022082 WP LT TANK ACCESS LEAKING A AALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 21 469AA 49599 SFO INFLIGHT T1514/06FEB SJC TO DFW - AFTER TAKEOFF FELT WING INBALANCE. FUEL GAGE HAD LEFT MAIN 450, RIGHT MAIN 9250 A ND CENTER 14700. UNWANTED FUEL TRANSFER FROM LEFT WING TO CENTER TANK. LANDED SFO WITHOUT INCIDENT. FOUND FUEL LEAK F ROM LEFT WING FUEL BOOST PUMP COVER PLATE. REPLACED TANK ACCESS COVER SEAL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007030500049 20070305 00049 NM 2007 3 5 AALA20070349 1 20070216 A 3350 D71701001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 907AN 29509 LGA - FOUND EMERGENCY LIGHT AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FOWARD CABIN. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007030500051 20070305 00051 WP 2007 3 5 AALA20070346 1 20070216 A 3222 STRUT DOUG DC9 DC983 3022083 WP NLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 110HM 49787 IND INFLIGHT T1077/16FEB - NOSE LANDING GEAR WOULD NOT RETRACT. RETURNED TO IND AND LANDED WITHOUT INCIDENT. REPACKED NOSE LANDING GEAR STRUT AND ACCOMPLISHED FULL SERVICE OF NOSE LANDING GEAR STRUT. SYSTEM GROUND CHECKED NORMAL OPERATIO N. 2 L 7 2 4F RT A6WE 2007030500056 20070305 00056 EA 2007 3 5 TRAX200700264 1 20070220 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 FOUND RT CABIN SIDEWALL SEAT TRACKS HAVE MINOR CORROSION IN SEVERAL LOCATIONS AS MARKED. 2 L 7 2 4F RT A21EA 2007030500062 20070305 00062 EA 2007 3 5 TRAX200700270 1 20070220 A 2930 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA COCKPIT ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 354CA 10064 HYD SYS NR 1 HIGH TEMP MSG. AIR RETURN, AIRCRAFT RETURNED TO ATL AFTER T/O, EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007030500064 20070305 00064 EA 2007 3 5 TRAX200700272 1 20070221 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 935EV 8037 FOUND LT FORWARD MOST EXTERNAL EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007030500074 20070305 00074 EA 2007 3 5 TRAX200700258 1 20070220 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 FOUND LT CABIN FLOOR SEAT TRACK CORRODED AT FS 364. 2 L 7 2 4F RT A21EA 2007030500078 20070305 00078 NM 2007 3 5 AWXA200700302 1 20070201 A 5320 6517684639 INTERCOSTAL BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED INTERCOSTAL, BS 294.5, S9L. REPLACED INTERCOSTAL, BS 294.5, S9L IAW AWA ER 03-5312-07054-HF4. 2 L 7 2 4F RT A16WE 2007030500086 20070305 00086 NM 2007 3 5 AWXA200700272 1 20070217 A 5320 65528942 CHANNEL BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND CRACKED MAIN CABIN FLOOR STRUCTURE CHANNEL ASSEMBLY, BS 540, BL0 - RBL 24.5, WL 208. REPLACED MAIN CABIN F LOOR STRUCTURE CHANNEL ASSEMBLY, BS 540, BL0 - RBL 24.5, WL 208 IAW B737-300 SRM 51-40-04. 2 L 7 2 4F RT A16WE 2007030500102 20070305 00102 NM 2007 3 5 AWXA200700310 1 20070131 A 5320 69489852 FITTING BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED INTERCOSTAL CLIP, BS 360, S8L. REPLACED INTERCOSTAL CLIP, BS 360, S8L IAW AWA ER 03-5312-0754-HF4. 2 L 7 2 4F RT A16WE 2007030500121 20070305 00121 NM 2007 3 5 SWAA071171 1 20070301 A 5330 6545857 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007030500122 20070305 00122 NM 2007 3 5 SWAA071153 1 20070228 A 5210 6545871 SKIN BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED SPV CHECK, FOUND R1 DOOR SKIN CRACKED AT BS 304, STR 15R. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2007030500123 20070305 00123 NM 2007 3 5 SWAA071170 1 20070301 A 5753 6546434 FLAP BOEING 737 7375H4 138449D NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED BRDG CHECK, FOUND LEFT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007030500155 20070305 00155 WP 2007 3 5 DHL2007802515 1 20070118 A 5753 ANGLE DOUG DC8 DC873 302199C WP T/E FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 FOUND LT INBD FLAP T/E ANGLE 1.500" CRACK STA XW 129.000. REMOVED CRACKED REINFORCING ANGLE IAW SRM 51-1-21. FABRICATE D NEW REINFORCING ANGLE (AL2024"0" 0.050") IAW SRM 57-7-1 FIG 2 SHEET 1. HEAT TREATED FROM "0" TO AL2024T4 IAW SRM 51-1 -1 PG 1-13-17. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW REINFORCING ANGLE IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007030500156 20070305 00156 WP 2007 3 5 DHL2007802516 1 20070130 A 5712 FRAME DOUG DC8 DC873 302199C WP LT WING BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 FOUND LT WING CTR L/E UPPER INTERNAL FORMER BROKEN 1" STA XS 521.000. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED DO UBLER (AL7075"0" 0.063") IAW SRM 57-3-3 FIG 4. HEAT TREATED FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007030500171 20070305 00171 EU 2007 3 5 07FDEA00490 1 20070215 A 3610 9787345 VALVE AIRBUS 300 A300B4605R 3930308 EU BLEED AIR SYS MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 677FE 791 NR 2 BLEED FAULT DURING CLIMB-OUT. FAULT DUE TO OVERHEAT. PRESSURED CHECKED MUSCLE LINE ON FAN AIR VALVE TO HP VALVE. CHECKED GOOD. REPLACED FAN AIR VALVE IAW MM 36-11-16-4-02. RAN NR 2 ENGINE AT POWER PER JRH. WITH ENGINE STABILIZED AT POWER THE BLEED PRESSURE WAS 42 PSI AND DUCT TEMP WAS 180C. NO OVERHEAT FAULTS, ALL INDICATIONS NORMAL. 2 L 7 2 4F RT A35EU 2007030500175 20070305 00175 NM 2007 3 5 QXEA200700278 1 20070214 A 5322 ANGLE DHAV DHC8 DHC8202 2809007 NM FWD LAVATORY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND LAVATORY MOUNT ANGLE IS CORRODED ON TOP FLANGE AT RIGHT HAND SIDEWALL Y42.5 AND STATION X222. REPAIRED I AW SRM 51-20-11, RD8-53-9469, AND 51-20-36. 2 H 7 2 4T RT A13NM 2007030500177 20070305 00177 NM 2007 3 5 QXEA200700279 1 20070214 A 5322 ANGLE DHAV DHC8 DHC8202 2809007 NM GALLEY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND UPPER FLANGE OF GALLEY MOUNT ANGLE RIGHT HAND SIDEWALL Y 42.5 AT STATION X240 IS CORRODED. REPAIRED IAW SRM 51-20-11, RD8-53-9469, AND 51-20-36. 2 H 7 2 4T RT A13NM 2007030500195 20070305 00195 NM 2007 3 5 AWXA200700316 1 20070126 A 5330 654576972 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED FUSELAGE SKIN, BS 407, S28L - S28R. REPAIRED FUSELAGE SKIN, BS 407, S28L - S28R IAW AWA EO 5331-010 24 AND AWA TASK CARD M2A53002. 2 L 7 2 4F RT A16WE 2007030500196 20070305 00196 NM 2007 3 5 AWXA200700317 1 20070126 A 5313 6546877 STRINGER BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CRACKED STRINGER, BS 727, S18A LEFT. REPAIRED STRINGER, BS 727, S18A LEFT IAW AWA ER 03-5361-07058-SS3. 2 L 7 2 4F RT A16WE 2007030500206 20070305 00206 NM 2007 3 5 CALA0700090 1 20070222 A 5320 69489856 SUPPORT ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 SUPPORT ANGLE CRACKED AT 360 AND STRINGER S11L. REPAIRED IAW ECRA 5311-01297. 2 L 7 2 4F RT A16WE 2007030500207 20070305 00207 NM 2007 3 5 CALA0700091 1 20070223 A 5200 PAN BOEING 737 7373T0 1384582 NM DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 UPPER FWD PAN CRACKED AT FWD SPLICE. INSTALLED SERVICEABLE PAN. 2 L 7 2 4F RT A16WE 2007030500208 20070305 00208 NM 2007 3 5 CALA0700092 1 20070223 A 5230 65C2518022 PAN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 C2 DOOR FWD SIDE PAN CRACKED AT SPLICE POINT. INSTALLED NEW PAN IAW SRM 52-30-02. 2 L 7 2 4F RT A16WE 2007030600002 20070306 00002 NM 2007 3 6 2007UALA00591 1 20070226 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 FUSELAGE FRAME HAS DEEP GOUGES STA 1720 BETWEEN STR 29L TO JUST O/B OF STR 29R. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030600011 20070306 00011 NM 2007 3 6 2007UALA00600 1 20070227 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 G5 GALLEY, G1A GALLEY LT, STAIRWAY & SEAT 17AB CEILINGS EMERGENCY LIGHT LAMPS ARE BURNED OUT. REPLACED NEW LAMPS AND CH ECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030600012 20070306 00012 NM 2007 3 6 2007UALA00601 1 20070227 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 OVERWING EMERGENCY 3RD LIGHT WAS OUT AT RT WING TO BODY AFT AREA. REPLACED WITH NEW LAMP & THEN OP CHECKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030600031 20070306 00031 NM 2007 3 6 SWAA071138 1 20070227 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030600045 20070306 00045 NM 2007 3 6 SWAA071134 1 20070227 A 5315 6546811 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 11 TO LBL 13. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2007030600046 20070306 00046 NM 2007 3 6 SWAA071139 1 20070227 A 5310 6547959 DOOR FRAME BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT LOWER CORNER. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007030600050 20070306 00050 NM 2007 3 6 SWAA071118 1 20070226 A 3350 MS155721 LAMP BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 718SW 27852 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007030600055 20070306 00055 NM 2007 3 6 SWAA071148 1 20070226 A 2910 65C26839 LINE BOEING 737 7373H4 1384600 NM HYDRAULIC SYS RUPTURED A SWAA K NONE K FLUID LOSS AP APPROACH 1 SW 29 399WN 27693 DECLARED EMERGENCY, LOSS OF HYDRAULIC B-SYSTEM ON APPROACH. REMOVED AND REPLACED B-SYSTEM MODULE LINE PER MM. 2 L 7 2 4F RT A16WE 2007030600056 20070306 00056 NM 2007 3 6 SWAA071156 1 20070228 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 476WN 32475 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007030600077 20070306 00077 2007 3 6 AMTA200700066 4 20070210 A 3160 C16221KA02 DISPLAY BOEING 737 73783N 13844HI NM COCKPIT INOPERATIVE A AMTA K NONE O OTHER CR CRUISE 1 GL 11 319TZ 30643 ISFD INOPERATIVE. REMOVED AND REPLACED ISFD IAW MM 34-24-02-4, OPS CHECK NORMAL. (K) 2 L 7 2 4F RT A16WE 2007030600078 20070306 00078 NM 2007 3 6 AMTA200700067 1 20070210 A 2613 OVERHEAT SYS BOEING 737 73783N 13844HI NM LT WING MALFUNCTIONED A AMTA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 321TZ 28249 LT WING BODY OVERHEAT LIGHT ILLUMINATED AFTER ENGINE START, ACCOMPLISHED RESET LIGHT WOULD NOT RESET. INSPECTED AFT CAR GO FOR RUPTURED DUCT NO DEFECTS NOTED PERFORMED BITE PROCEDURE FOR WHEEL WELL, WING AND BODY OVERHEAT DET CONTROL MODULE . ALARM CODE 44 DISPLAYED. PERFORMED FIM, NO DEFECTS FOUND. CLEARED CODE. (K) 2 L 7 2 4F RT A16WE 2007030600100 20070306 00100 NM 2007 3 6 AWXA200700322 1 20070227 A 5320 D5348004820200 SILL AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 803AW 931 SAL - FOUND CORROSION ON L2 DOOR CUT OUT SILL BEAM SHAPE SILL, FR 60 - FR 68, S23L. REPLACED L2 DOOR CUT OUT SILL BEAM SHAPE SILL, FR 60 - FR 68, S23L IAW B737-300 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007030600101 20070306 00101 NM 2007 3 6 DL76L070163 1 20070227 A 4990 OIL COOLER BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE APU DEFECTIVE A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 171DN 39317 24759 P266 APU SHUTDOWN AFTER ENG START. PERFORMED APU BITE. BITE SHOWS HIGH OIL TEMP. REPLACED OIL TE SWITCH PER M/M. APU SHUT S DOWN AFTER 10 MIN. T/S PER FIM 49-11-00 FIG 110 DOWN TO SHEET 4 STEP 9 155986. CONT T/S NE OIL COOLER BYPASS VALVE 15 5986. REPLACED AIR/OIL COOLER ASS P/N 160126-2 PER M/M AND IPC APU RAN 30 MIN WITH NO FAULTS MCO/PLAC REMOVED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007030600102 20070306 00102 NM 2007 3 6 DL76G070164 1 20070227 A 5610 SEAL BOEING 767 767332 1382001 NM COCKPIT WINDOW DIRTY A DALA O OTHER O OTHER CR CRUISE 1 SO 27 16065 30199 WINDOW SQUEAL LEAKY WINDOW SEAL CAPT SIDE. CAPT SLIDE WINDOW SEAL CLEANED AND LUBRICATED. A/C PRESSURIZE AS REQUIRED B Y MCC AND ACCORDING AMM 05-51-24-782-001. NO LEAK FOUND. 2 L 7 2 4F RT A1NM 2007030600103 20070306 00103 NE 2007 3 6 DL76G070165 2 20070226 A 7200 CF680C2B6F ENGINE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 MALFUNCTIONED A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 1604R 31177 8164 704887 30180 704887 ENGINE REPLACED DUE TO HOC NR 2. REPLACED NR 2 ENG PER TRANS 1T161. 2 L 7 2 4F 4 F RT A1NM E13NE 2007030600104 20070306 00104 NM 2007 3 6 DLM88070166 1 20070221 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 938DL 49811 THE FUSELAGE SKIN WAS CORRODED FROM FS 564 TO 588, L22R-L26R. THE DAMAGED FUSELAGE SKIN WAS CUT OUT AND A REPAIR DOUBLE R WAS INSTALLED. 2 L 7 2 4F RT A6WE 2007030600125 20070306 00125 NM 2007 3 6 EIA2007037 1 20070222 A 5753 SPAR BOEING BOEING 747 747273C 1384896 NM T/E FLAP CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 CORROSION FOUND AT RT WING INBOARD FLAP (65B02070-2) MOST INBOARD INTERNAL STRUCTURE, REPAIR TO FIBERGLASS WEDGE. TRIM AFFECTED AREA OF THE REAR SPAR TO REMOVE CORROSION. FABRICATE AND INSTALL A SPAR SECTION AND SPLICE CHANNEL. REPAIR TR AILING EDGE WEDGE SECTION CORE AND SKIN. RESTORE ASSEMBLY FINISH CONDUCT DVI AND TEST TAP INSP. 2 L 7 4 4F A20WE 2007030600126 20070306 00126 NM 2007 3 6 EIA2007035 1 20070222 A 2120 65B409915 DUCT BOEING 747 747273C 1384896 NM A/C BAY DENTED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 FOUND A DENT APPROX 1" AT CENTER AREA OF DUCT FROM BYPASS VALVE TO ACM, NR 3 PACK. CARRIED OUT PENETRANT INSP, ADD ALUM INUM DOUBLER, WELD AND ALODINE REPAIR PER ECRA 471-51-256-1 2 L 7 4 4F A20WE 2007030600127 20070306 00127 NM 2007 3 6 EIA2007038 1 20070222 A 5754 SEAL BOEING 747 747273C 1384896 NM L/E FLAP UNKNOWN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 REQUIRE ADDITION OF ADDITIONAL FLAP SEAL MATERIAL FOR LT WING LEADING EDGE KRUEGER FLAP SEALS (RAIN EROSION SHIELDS) REP AIR. REPAIRED NR 11-13 KRUEGER FLAPS MOLDING SEALS PER BOEING DOC D6-13625. 2 L 7 4 4F A20WE 2007030600128 20070306 00128 NM 2007 3 6 EIA2007039 1 20070222 A 5330 SKIN BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 FOUND FORWARD CARGO CEC CUTOUT BILGE SKIN UNDER DOUBLER FOUND CORRODED AND FWD RIGHT DOUBLER CRACKED OFF. REMOVED DAMA GED FUSELAGE SKIN, C/W HFEC, PREP NEW SKIN SECTION AND INSTALL PER ECRA 471-51-256-1. 2 L 7 4 4F A20WE 2007030600140 20070306 00140 EU 2007 3 6 NSVA20070017 1 20070122 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 184CJ 184 FOUND ARM LT ON EMERG LT SYS NOT ACTIVATING. REMOVED AND REPLACED LIGHT BULB, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2007030700006 20070307 00006 NM 2007 3 7 07FDEA00622 1 20070301 A 5711 ARB74141 SPAR CAP DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 FOUND LT WING, REAR SPAR LOWER CHORD AT STA 1063 - 1075 CORROSION. LT WING, REAR SPAR LOWER CHORD AT STA 1063 - 1075 RE PAIRED AS PER FEDEX EA NR 1- 5710- 105615, WINGS, LEFT WING LOWER SPAR CAP AFT FLANGE CORROSION BETWEEN XORS=1063 AND XORS=1075 - REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007030700013 20070307 00013 NM 2007 3 7 07FDEA00448 1 20070212 A 5313 A5A70361 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 CENTER CARGO COMPARTMENT BILGE AREA LONGERON 52 AT STA 1531 FOUND CORRODED REPAIR CARRIED OUT PER FEDEX EA 1-5310-10562 3, FUSELAGE, LONGERON L52 AT STA 5-102, SRM SPLICE CLASSIFICATION. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007030700014 20070307 00014 NM 2007 3 7 07FDEA00451 1 20070212 A 5310 AGA7026503 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 AFT CARGO COMPARTMENT RT TUNNEL AREA, LONGERON 38R AT STA 1863 FOUND CRACKED. REPAIRED AS PER SRM 53-10-00 VOLUME I, F IGURE 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007030700015 20070307 00015 NM 2007 3 7 07FDEA00623 1 20070301 A 5710 ARB74131 CAP DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LT WING, REAR SPAR UPPER CHORD AT STA 1035-1043 FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5710-105616, CLASSIFIED AS MA JOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007030700020 20070307 00020 NM 2007 3 7 ASAA0741497 1 20070227 A 5753 STRUCTURE BOEING 737 7374Q8 138447Q NM T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 RIGHT I/B MID FLAP IS DENTED AT PREVIOUS REPAIR. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007030700029 20070307 00029 NM 2007 3 7 ASAA0741490 1 20070223 A 5320 654587512 ATTACH ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 R1 DOORWAY LOWER SILL CHORD ATTACHMENT ANGLE CORRODED. ATTACHMENT ANGLE REPLACED WITH NEW PART IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007030700032 20070307 00032 NM 2007 3 7 ASAA0741493 1 20070227 A 5320 65C235831 WEB BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 FLOOR WEB HAS 2 EACH SHARP DENTS. REMOVED FABRICATED NEW AND INSTALLED WEB IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007030700033 20070307 00033 NM 2007 3 7 ASAA0741494 1 20070227 A 5320 65C335822 SHEAR WEB BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 SHEAR WEB AT L2 DOOR MOP SILL IS BENT AND CRACKED. REMOVED FABRICATED NEW WEB AND INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007030700040 20070307 00040 EA 2007 3 7 TRAX200700286 1 20070223 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 STA 364 FRAME HAS SURFACE CORROSION BETWEEN STR 26 LT AND 26 RT. REPAIRED IAW ALL PERTINENT SRM`S AND OR EO`S. 2 L 7 2 4F RT A21EA 2007030700041 20070307 00041 EA 2007 3 7 TRAX200700287 1 20070223 A 5320 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 FS 280 CROSSBEAM HAS CORROSION ON UPPER FLANGE. REPLACE BEAM PER CUSTOMER. REMOVED ALL REQUIRED FASTENERS ON LEFT FS 2 80. CROSSBEAM, REMOVED LBL 9 CLIP, REMOVED LEFT FS 280 CROSSBEAM. ALL WORK DONE IAW CRJ SRM 51-42-06, 51-42-13, 51-42- 21. LOCATED HOLES ON SERVICEABLE BEAM P/N CC670-34175-7 IAW CRJ SRM 51-40-11 MH715. OK TO INSTALL LEFT 280 CROSSBEAM. OK TO INSTALL LBL 9 CLIP. INSTALLED LBL 9 WITH HI-LOKS, INSTALLED LEFT FS 280 CROSSBEAM WET W/ HI-LOKS, SOLID FASTENER S, CHERRY RIVETS IAW CRJ SRM 51-42-06, 51-42-13, 51-42-21 MH715, REQUIRES 1 EA. CHERRY FASTENERS 2ND IN FROM O/B REQUIR ES CHANGING. REMOVED CHERRY FASTENER 2ND IN FROM O/B REQUIRES CHANGING. REMOVED CHERRY FASTENER & INSTALLED HI-LOK IAW 2 L 7 2 4F RT A21EA 2007030700042 20070307 00042 EA 2007 3 7 TRAX200700289 1 20070223 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 LEFT LOWER FS 280 WEB HAS CORROSION BEYOND LIMITS OF REO 670-53-11-052. REMOVED LT LOWER FS 280 WEB. REF STEPS OF FORM 412 FOR DUPLICATION OF WEB. OK TO INSTALL STRAP TO DOUBLER. INSTALLED 2 EA. LOWER ROWS OF FASTENERS W/ WET SOLID FASTEN ERS IAW CRJ SRM 51-42-6 MH715. OK TO INSTALL LT 280 WEB. INSTALLED LT 280 WEB IAW CRJ 7001900 SRM 51-42-06, 51-42-13, 51 -42-21. TOPCOATED INTERIOR WALL / GRAY WITH AXWF-3-G3G IAW CRJ 700/900 SRM 51-25-00 WR586 2-26-07. APPLIED WHITE TOPCOA T TO REMAINING FASTENERS IAW CRJ 700/900 SRM 51-25-16. WR586 2-26-07. 2 L 7 2 4F RT A21EA 2007030700043 20070307 00043 EA 2007 3 7 TRAX200700290 1 20070223 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 RT LOWER FS 280 WEB HAS CORROSION BEYOND LIMITS OF REO 670-53-11-052. REMOVED RT 280.00 WEB. DUPLICATED WEB 0.040 7075 T-6. LOCATE ALL HOLES EXCEPTING THOSE FROM RBL 42.50 OUTBOARD. DEBURR ALL ALODINE, PRIME TOPCOAT, IAW REO 670-53-11-05 2. DUPLICATED STRAP RT. STRAP ATTACHED TO WEB, IAW REO 670-53-11-052. REMOVED STRAP FROM WEB TO ACCOMMODATE REO 670-5 3-11-201 REPAIR. OK TO INSTALL WEB ASSY ON RT 280. INSTALLED A LARGE PORTION OF RT 280 WEB, IAW REO 670-53-11-052. INS TALLED REQUIRED FASTENERS IN RT 280 WEB, IAW REO 670-53-11-052. ALL FASTENERS INSTALLED IN RT 280.00 WEB, IAW REO 670-5 3-11-052. OK TO PRIME / TOPCOAT PRIMED / TOPCOATED WEB FASTENERS, IAW CRJ 700/900 SRM 51-25-06, 51-25-16 AND 51-25 2 L 7 2 4F RT A21EA 2007030700044 20070307 00044 NM 2007 3 7 CALA0700098 1 20070221 A 5320 BAC15181211 BEAM BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27239 28951 CORRODED BEAM AT STA 986.5. REPAIRED IAW ECRA 5321-01450. 2 L 7 2 4F RT A16WE 2007030700045 20070307 00045 NM 2007 3 7 CALA0700099 1 20070225 A 5320 141A52111 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 26210 28770 CENTER FLOOR PANEL SUPPORT MEMBER CORRODED. REPAIRED IAW ECRA 5310-04614. 2 L 7 2 4F RT A16WE 2007030700046 20070307 00046 NM 2007 3 7 CALA0700109 1 20070301 A 5320 141A52111 INTERCOSTAL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17244 28954 INTERCOSTAL FWD OF STA 277 AND AFT COCKPIT CORRODED. REPLACED INTERCOSTAL IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007030700048 20070307 00048 NM 2007 3 7 CALA0700111 1 20070301 A 5310 654795978 DOOR FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69603 27316 ABB DOOR CUTOUT FWD FRAME CRACKED AT SECOND STOP FROM THE BOTTOM. REPLACED FRAME IAW BOEING DRAWING 65-47959. 2 L 7 2 4F RT A16WE 2007030700049 20070307 00049 NM 2007 3 7 CALA0700112 1 20070301 A 3230 273A25011 UPLOCK ACTUATOR BOEING 737 737824 13844BZ NM RT MLG MALFUNCTIONED A CALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 27 14237 28802 RT MAIN GEAR CAME DOWN IN FLIGHT. REPLACED RT MAIN GEAR UPLOCK ACTUATOR. 2 L 7 2 4F RT A16WE 2007030700051 20070307 00051 NM 2007 3 7 CALA0700114 1 20070302 A 5311 654654049 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 LEFT MAIN FRAME CRACKED AT STA 639. REPAIRED IAW ECRA 5311-01299. 2 L 7 2 4F RT A16WE 2007030700053 20070307 00053 NM 2007 3 7 SWAA071202 1 20070303 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 203WN 32483 EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007030700056 20070307 00056 NM 2007 3 7 SWAA071178 1 20070302 A 5330 6545576 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 985, STR 21R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007030700057 20070307 00057 NM 2007 3 7 SWAA071184 1 20070302 A 2560 65457463 FITTING BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007030700058 20070307 00058 NM 2007 3 7 SWAA071183 1 20070302 A 2560 65457463 FITTING BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007030700060 20070307 00060 NM 2007 3 7 SWAA071182 1 20070302 A 5330 6545800 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 277, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007030700061 20070307 00061 NM 2007 3 7 SWAA071179 1 20070302 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 253, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007030700062 20070307 00062 NM 2007 3 7 SWAA071175 1 20070302 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 9R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030700063 20070307 00063 NM 2007 3 7 SWAA071185 1 20070302 A 5322 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 538, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007030700064 20070307 00064 NM 2007 3 7 SWAA071197 1 20070302 A 5311 6546538 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030700067 20070307 00067 NM 2007 3 7 SWAA071192 1 20070302 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030700069 20070307 00069 NM 2007 3 7 SWAA071177 1 20070302 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 947, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007030700070 20070307 00070 NM 2007 3 7 SWAA071186 1 20070302 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030700072 20070307 00072 NM 2007 3 7 SWAA071189 1 20070302 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030700074 20070307 00074 NM 2007 3 7 SWAA071193 1 20070302 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030700075 20070307 00075 NM 2007 3 7 SWAA071194 1 20070302 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030700076 20070307 00076 NM 2007 3 7 SWAA071195 1 20070302 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030700077 20070307 00077 NM 2007 3 7 SWAA071196 1 20070302 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030700079 20070307 00079 NM 2007 3 7 SWAA071205 1 20070303 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030700083 20070307 00083 NM 2007 3 7 SWAA071181 1 20070302 A 5313 BAC1498 STRINGER BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED 18Y CHECK, FOUND STRINGER 7L CRACKED AT BS 597. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007030700087 20070307 00087 NM 2007 3 7 SWAA071214 1 20070303 A 2560 6557463 FITTING BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CRACKED. REPAIRED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007030700089 20070307 00089 NM 2007 3 7 SWAA071217 1 20070303 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030700090 20070307 00090 NM 2007 3 7 SWAA071233 1 20070305 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030700091 20070307 00091 NM 2007 3 7 SWAA071213 1 20070303 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 14R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007030700093 20070307 00093 NM 2007 3 7 SWAA071218 1 20070303 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030700095 20070307 00095 NM 2007 3 7 SWAA071220 1 20070303 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, LBL 14. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030700098 20070307 00098 NM 2007 3 7 SWAA071210 1 20070303 A 3350 OL3071BPEGL LIGHT BOEING 737 7373TO 138447G NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED MV1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 21 DEF. REMOVED AND REPLACED LIGHT BULB PE R MM. 2 L 7 2 4F RT A16WE 2007030700099 20070307 00099 NM 2007 3 7 SWAA071228 1 20070305 A 2560 P4010021 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 235WN 34630 AFT INBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2007030700100 20070307 00100 NM 2007 3 7 SWAA071229 1 20070305 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED A2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP MISSING AT ROW 8 ABC TO ROW 10 ABC. INSTALLED STRIP PER M M. 2 L 7 2 4F RT A16WE 2007030700101 20070307 00101 NM 2007 3 7 SWAA071223 1 20070304 A 2612 100012001 CONTROL PANEL BOEING 737 7373H4 1384600 NM COCKPIT FAULTY A SWAA K NONE N FALSE WARNING NR NOT REPORTED 1 SW 29 304SW 22944 ALL LIGHTS ON CARGO FIRE PANEL ILLUMINATED WITH MASTER FIRE WARNING LIGHT AND BELL. CARGO FIRE PANEL LIGHTS STAYED ON F OR 15 MINUTES, THEN WENT OFF. REMOVED AND REPLACED CARGO FIRE PANEL CONTROL PANEL PER MM. 2 L 7 2 4F RT A16WE 2007030700102 20070307 00102 NM 2007 3 7 SWAA071235 1 20070305 A 3350 101073 COVER BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 FWD CABIN EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT COVER PER MM. 2 L 7 2 4F RT A16WE 2007030700104 20070307 00104 NM 2007 3 7 SWAA071211 1 20070303 A 3350 101331 LENS BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED THRU CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007030700105 20070307 00105 NM 2007 3 7 SWAA071209 1 20070301 A 3244 26066712 TIRE BOEING 737 7373H4 1384600 NM RT MLG RUPTURED A SWAA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 29 319SW 23340 DIVERSION / DECLARED EMERGENCY. NR 3 MAIN TIRE RUPTURED ON TAKEOFF. REMOVED AND REPLACED NR 3 WHEEL AND TIRE ASSY, RIG HT WING INBOARD GROUND SPOILER, FORE FLAP AND MID FLAP PER MM. 2 L 7 2 4F RT A16WE 2007030700106 20070307 00106 2007 3 7 SWAA071225 4 20070304 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 733SA 27865 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007030700114 20070307 00114 NM 2007 3 7 SWAA071222 1 20070303 A 5322 6546546 SHEAR TIE BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 726SW 27858 DURING SCHEDULED 8Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, STR 24L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007030700117 20070307 00117 CE 2007 3 7 DXTA200701958 1 20070220 A 3213 STRUT CESSNA 750 750 2076810 CE NLG DISCHARGED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 971QS 7500071 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. GEAR HANDLE WOULD NOT RAISE. PERFORMED GEAR SWING 10 TIMES GEAR OPS CHECK ED GOOD ALL 10 TIMES. FOUND NOSE STRUT LOW ON SERVICE. SERVICED NOSE STRUT IAW CE-750 M/M CHPT 12-10-38. PERFORMED GE AR SWING 5 MORE TIMES OPS CHECK GOOD. 2 L 7 2 4J RT T00007WI 2007030700118 20070307 00118 CE 2007 3 7 DXTA200701959 1 20070220 A 3241 ANTI-SKID SYS CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG MALFUNCTIONED E DXTA D RETURN TO BLOCK S J AFFECT SYSTEMS WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 628QS 5605305 DURING TAXI CAPTAINS RIGHT BRAKE PEDAL BECOMES VERY "SPONGY". PERFORMED ANTI-SKID BRAKE BLEEDING PROCEDURE IAW CESSNA 56 0XL MM 32-42-00. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007030700119 20070307 00119 CE 2007 3 7 DXTA200701960 1 20070221 A 3233 278882 ACTUATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG INTERMITTENT E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 996QS 5096 7500196 LANDING GEAR RED UNSAFE LIGHT CAME ON WITH GEAR EXTENDED ALONG WITH (3) GREEN GEAR LIGHTS. ACCOMPLISHED CHECKLIST ITEMS. RED UNSAFE LIGHT BECAME INTERMITTENT FOR (5) MINUTES AND THEN EXTINGUISHED. BLEW LANDING GEAR DOWN AND LANDED NORMALL Y. REMOVED & REPLACED NOSE LANDING GEAR ACTUATOR CK & OPS CK GOOD I.A.W. CESSNA M/M CH 32-30-03. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007030700120 20070307 00120 CE 2007 3 7 DXTA200701961 1 20070222 A 3233 99121114 ACTUATOR CESSNA 500 560CESSNA 2076750 CE MLG INTERMITTENT E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 347QS 6224 5600357 RH MAIN GEAR LIGHT WOULD NOT ILLUMINATE AFTER 2 CYCLES OF LANDING GEAR. AFTER GO AROUND AND VERIFICATION FROM TOWER WAS RECEIVED, RIGHT HAND GEAR LIGHT ILLUMINATED. NO OTHER INDICATIONS THAT GEAR WAS NOT DOWN ADN LOCKED EXISTED. ROTARY TEST REVIELD THAT THE BULB WAS NOT INOP. AS A PRECAUTION, EMERG GEAR EXT WAS ACCOMPLISHED AND NITROGEN BACK UP WAS ACTIVATED . REMOVED RT MAIN LANDING GEAR ACTUATOR AND INSTALLED REPAIRED MAIN LANDING GEAR ACTUATOR IN THE R/H POSITION. PERFORME D GEAR OPERATIONAL CHECK. ALL CHECKS WERE GOOD. ALL WORK DONE I.A.W. CESSNA 560 ULTRA AMM 32-31-04 2 L 7 2 4F RT A22CE 2007030700121 20070307 00121 CE 2007 3 7 DXTA200701962 1 20070223 A 3233 281262 ACTUATOR CESSNA 680 680CE 2076811 CE MLG INTERMITTENT E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 362QS 1201 6800051 RT MAIN GEAR SAFE LIGHT DID NOT ILLUMINUTE AND RED GEAR UNSAFE LIGHT ILLUMNATED WHEN THE GEAR HANDLE WAS SELECTED DOWN. THE GEAR WAS BLOW DOWN BUT INITALLY DID NOT INDICATE SAFE APPROX 5 MINUTES AFTER COMPLETION OF THE EP, THE GEAR INDICATE D SAFE. REMOVED & REPLACE RT MAIN LANDING GEAR ACTUATOR IAW CE680 MM 32-30-40. OPERATIONALY CHECKS GOOD. 2 L 7 2 4F RC T00012WI 2007030700122 20070307 00122 CE 2007 3 7 DXTA200701964 1 20070224 A 3213 PACKING CESSNA 750 750 2076810 CE NLG STRUT DAMAGED E DXTA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 GL 07 966QS 7500166 AFTER TAKE-OFF GEAR HANDLE COULD NOT BE MOVED TO " GEAR UP POSITION". HANDLE WAS LOCKED IN " GEAR DOWN POSITION." JACK ED AIRCRAFT AND CYCLED GEAR SEVERAL TIMES. GEAR HANDLE FUNCTIONED NORMALLY. FOUND NOSE GEAR SERVICE LOW. REMOVED AND DIS ASSEMBLED LOWER NOSE GEAR STRUT. INSTALLED ALL NEW PACKINGS AND SEALS, REASSEMBLED AND INSTALLED ON A/C, SERVICED NOSE S TRUT. CYCLED GEAR SEVERAL MORE TIMES. NO PROBLEMS NOTED. ALL WORK DONE IAW CE750 MM CH 32-20-02. DOWN JACKED A/C 2 L 7 2 4J RT T00007WI 2007030700123 20070307 00123 CE 2007 3 7 DXTA200701965 1 20070225 A 3260 SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG DIRTY E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 876QS 258586 RT MLG INDICATES GREEN AND RED UPON RETRACTION. GEAR SELECTED DOWN RT MLG INDICATES GREEN NOT RED. JACKED AIRCRAFT AND APPLIED HYDRAULIC POWER. CLEANED LT & RT MAIN GEAR SWITCHES DUE TO EXCESSIVE DIRT BUILDUP. VERIFIED RT GEAR MICROSWITCHE S WIRING AND TERMINAL INSTALLATIONS. CYCLED GEAR NUMEROUS TIMES, ALL OPERATIONAL CHECKS GOOD. WORK PERFORMED IAW HAWKER 800XPC MAINT. MAN. SEC. 32-10-00. 2 L 7 2 4F 4 F RT A3EU E6WE 2007030700124 20070307 00124 CE 2007 3 7 DXTA200701966 1 20070225 A 3230 HOOK CESSNA 750 750 2076810 CE MLG UPLOCK OUT OF ADJUST E DXTA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 GL 07 971QS 7500071 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. GEAR HANDLE WOULD NOT MOVE TO "RETRACT POSITION". GEAR HANDLE LOCKED IN D OWN POSITION INFLIGHT. ADJUSTED NLG UPLOCK HOOK ASSY IAW 400A M/M 32-20-00. OPS CHECKED GOOD 2 L 7 2 4J RT T00007WI 2007030700125 20070307 00125 CE 2007 3 7 GLBA20060914 1 20070219 A 3252 1148200523 SHIMMY DAMPENER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NLG MISSING A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 220GL UE220 UPON PRE-FLIGHT INSPECTION, PILOT REPORT OF SHIMMY DAMPENER DAMAGE/MISSING AND SUSPECTED DAMAGE TO STRUCTURE IN SURROUND ING AREA WAS ALSO REPORTED. MAINTENANCE REMOVED AND REPLACED THE SHIMMY DAMPER IAW B1900D MM 32-20. MAINENANCE REMOVED AND REPLACED STEERING BELLCRANK CENTERING MECHANISM IAW B1900 MM 32-51. MAINTENANCE REMOVED AND REPLACED NOSE DRAG BRACE IAW B1900 MM 32-10. SUBSEQUENT OPERATIONAL CHECKS GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2007030700127 20070307 00127 2007 3 7 SA07015 2 20070226 A 7322 1348M79P12 HMU CFMINT AIRBUS A321 A321211 3930370 EU NR 1 ENGINE FAILED A USAA E ENGINE SHUTDOWN E M A VIBRATION/BUFFET OVER TEMP FLAME/FIRE DE DESCENT 1 EA 19 181UW 20911 575223 1531 CLT FLT 1408 EN-ROUTE SFO - CLT. DURING DESCENT, AT APPROXIMATELY FL 290, A RUMBLING SOUND DEVELOPED WITH A COINCIDIN G RISE IN EGT TO THE REDLINE LIMIT OF THE NUMBER 1 ENGINE. PASSENGERS REPORTED SEEING FLAMES COMING OUT OF THE NUMBER O NE ENGINE TO THE CABIN CREW. THE FLIGHT CREW ELECTED TO SHUT DOWN THE NUMBER ONE ENGINE AND DECLARE AN EMERGENCY INBOUN D TO CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 18 MINUTES. INITIAL MAINTENANCE INSPEC TION REVEALED OIL IN THE TAILPIPE. A BORESCOPE INSPECTION REVEALED NO FINDINGS CONSISTENT WITH THE ENGINE SHUTDOWN. TH E OIL IN THE TAILPIPE WAS FOUND TO BE A NORMAL CONDITION FOR AN ENGINE THAT HAS BEEN WINDMILLING. MAINTENANCE TROUBLESH 2 L 7 2 4F RT A28NM 2007030700128 20070307 00128 EA 2007 3 7 TRAX200700275 1 20070221 A 5321 PRESSURE PANEL CNDAIR CL600 CL6002B19 1900309 EA BS 409-559 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 CORROSION ON PRESSURE FLOOR IN SEVERAL LOCATIONS AT LBL45 FROM FS 409+112 TO FS559. TREATED, PRIMED, PAINTED AND DYNATUR ALED FASTENERS AND PRESSURE DECK ALL WORK IAW REO 601R-53-41-491. BM24222. 02-27-07 JOB COMPLETE. 2 L 7 2 4F RT A21EA 2007030700129 20070307 00129 EA 2007 3 7 TRAX200700276 1 20070221 A 5321 PRESSURE PANEL CNDAIR CL600 CL6002B19 1900309 EA BS 513 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 FOUND CORROSION ON PRESSURE FLOOR AT RBL 45 AT FS 513. TREATED, PRIMED, PAINTED AND DYNATURALED FASTENERS AND PRESSURE DECK ALL WORK IAW REO 601R-53-41-491. BM24222. 02-27-07 JOB COMPLETE. 2 L 7 2 4F RT A21EA 2007030700130 20070307 00130 EA 2007 3 7 TRAX200700277 1 20070221 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 473 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 FRAME AT FS 473.15 HAS CORROSION AT LBL45 REMOVED 3 SOLID RIVITS AND INSTALLED 3 HST110AG6-7 HI-LOCKS.TREATED, PRIMED, PAINTED AND DYNATURALED FASTENERS AND PRESSURE DECK ALL WORK IAW REO 601R-53-41-491. BM24222. 02-27-07 JOB COMPLETE. 2 L 7 2 4F RT A21EA 2007031500001 20070315 00001 WP 2007 3 15 UPS07849342 1 20070221 A 5347 6015176 SEAT TRACK DOUG DC8 DC873F 302199F WP FS 1510 RBL 45 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C1 SEAT TRACK HEAVILY CORRODED STA 1510 RBL 45. REMOVED SEAT TRACK FROM STA 1490-1550 RBL 45. FABRICAT ED AND INSTALLED REPLACEMENT SEAT TRACK IAW SRM 51-3-0, 53-07-03 FIG 7-3 FIG 003. 2 L 7 4 4F RT 4A25 2007030700159 20070307 00159 NM 2007 3 7 QXEA200700268 1 20070209 A 5320 SILL DHAV DHC8 DHC8202 2809007 NM FUSLEAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND CORROSION ON BEAM UNDER MAIN CABIN DOOR LOWER SILL PLATE BY NUTPLATES. REPAIRED IAW SRM 51-20-16 AND 51- 20-36. 2 H 7 2 4T RT A13NM 2007030700160 20070307 00160 NM 2007 3 7 QXEA200700259 1 20070214 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM LT WING LE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - LEFT LEADING EDGE UPPER SPAR FLANGE HAS GOUGE AT STATION YW 288.0. REPAIRED IAW RD8-57-1119 AND RD8-57-3584. 2 H 7 2 4T RT A13NM 2007030700161 20070307 00161 NM 2007 3 7 QXEA200700269 1 20070211 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - LEFT INBOARD FLAP TRACK NR 1 HAS 2 DIVOTS ON UPPER RAMP AND 2 DIVOTS ON LOWER RAMP. REPAIRED IAW RD8-57-985. 2 H 7 2 4T RT A13NM 2007030700162 20070307 00162 NM 2007 3 7 QXEA200700270 1 20070209 A 5320 SILL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND CORROSION ON BEAM UNDER MAIN CABIN DOOR LOWER SILL WHERE DOOR SEAL AIR SUPPLY TUBE GOES THROUGH. REPAIRE D IAW SRM 51-20-11 AND 51-20-36. 2 H 7 2 4T RT A13NM 2007030700163 20070307 00163 NM 2007 3 7 QXEA200700272 1 20070211 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - LEFT OUTBOARD FLAP NR 3 FLAP TRACK HAS 2 DIVOTS ON UPPER RAMP AND 2 DIVOTS ON LOWER RAMP. REPAIRED IAW RD8-57- 1166 AND RD8-57-987. 2 H 7 2 4T RT A13NM 2007030700166 20070307 00166 EU 2007 3 7 07FDEA00393 1 20070209 A 5330 SKIN AIRBUS 310 A310203 3930313 EU BS 904-926 MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 409FE 273 PREVIOUS REPAIR FOUND LOCATED RT, FS 904-926, FS 7-8. REPAIR LOCATED AROUND OXYGEN DISCHARGE INDICATOR. REPAIR REQUIRE S EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. OPEN /CLOSE ACCE SS PER AMM 25-71-00 EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISH ED PER FEDEX ENG AUTH 6-5330-106692. REPAIR EVALUATED AND CLASSIFIED AS PER GMM 6-2-100 AS "MAJOR". 2 L 7 2 4F RT A35EU 2007030700167 20070307 00167 EU 2007 3 7 07FDEA00395 1 20070209 A 5330 SKIN AIRBUS 310 A310203 3930313 EU BS 3408-3461 MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 409FE 273 PREVIOUS REPAIR FOUND LOCATED RT, FS 3408-3461, FS 63-64 AND STR 40-43. REPAIR AFT OF AFT CARGO DOOR. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED IN ACCORDANCE WITH FEDEX ENG AUTH NR 6-5330--1 06691. REPAIR EVALUATED AND CLASSIFIED AS PER GMM 6-2-100 AS "MAJOR". 2 L 7 2 4F RT A35EU 2007030700169 20070307 00169 EU 2007 3 7 07FDEA00398 1 20070209 A 5330 SKIN AIRBUS 310 A310203 3930313 EU BS 4941-4956 MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 409FE 273 PREVIOUS REPAIR FOUND LOCATED RT, FS 4941-4956, FR 97 AND STR 4-6. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINA TION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTI NG SRM REPAIR. NEW REPAIR ACCOMPLISHED PER FEDEX ENG AUTH NR 6-5330-106690. REPAIR EVALUATED AND CLASSIFIED AS PER GMM 6-2-100 AS "MINOR". 2 L 7 2 4F RT A35EU 2007030700170 20070307 00170 EU 2007 3 7 07FDEA00401 1 20070209 A 5512 SKIN AIRBUS 310 A310203 3930313 EU HORIZONTAL STAB MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 409FE 273 PREVIOUS FLUSH REPAIR FOUND LOCATED ON THE LEADING EDGE OF THE RT HORIZONTAL STABILIZER LEADING EDGE PANEL 341CB. REPAI R REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIR PER SRM 55-12-12 FIG 201 AND REPLACED RIB 26 P/N A5517805020100 AND SRM 51-72-10. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR". 2 L 7 2 4F RT A35EU 2007030700171 20070307 00171 EU 2007 3 7 07FDEA00406 1 20070209 A 5755 SKIN AIRBUS 310 A310203 3930313 EU NR 7 SPOILER MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 409FE 273 PREVIOUS COMPOSITE REPAIR LOCATED ON THE LT WING, NR 7 SPOILER, LOWER SIDE OUTBD OF ACTUATOR. REPAIR REQUIRES EVALUATIO N FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUN D NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER EA 6-5740-106682. REPAIR EVALUATED AND CLASSIF IED AS PER GMM 6-2-100 AS "MAJOR". 2 L 7 2 4F RT A35EU 2007030700172 20070307 00172 2007 3 7 2007UALA00569 4 20070221 A 2565 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 MAIN CABIN L-4 DOOR GIRT BAR IS OUT OF ADJUSTMENT. ADJUSTED L-4 GIRT BAR FOR PROPER ENGAGEMENT OF GIRT BAR SLIDERS. DO OR L-4 ARM-DISARM OPERATIONAL TEST WAS ACCOMPLISHED FOR ASSURING PROPER FUNCTIONALITY. NO COMPONENTS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030700173 20070307 00173 NM 2007 3 7 2007UALA00570 1 20070221 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 SIGNS OF CORROSION (WHITE POWDER) AT DME (RIGHT) ANTENNA MOUNTING AT BS 668.5 BETWEEN STR 28L TO 29L. REMOVED ANTENNA FOR EVALUATION OF LEVEL 1 SKIN CORROSION. REPLACED ANTENNA MOUNT AND ANTENNA. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030700174 20070307 00174 NM 2007 3 7 2007UALA00571 1 20070221 A 5310 UNKNOWN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE VIBRATION A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 843UA 1573 LITE LATERAL VIBRATION - NOISE ENCOUNTERED IN CLIMB AND AT FL360. [SUP 05-16-07] PERFORMED A RUDDER FREEPLAY CHECK AFT ER LANDING AND FOUND ALL THREE RUDDER ACTUATOR ROD ENDS WORN BEYOND LIMITS. REPLACED ALL RUDDER ACTUATOR ROD ENDS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007030700175 20070307 00175 EU 2007 3 7 07FDEA00412 1 20070209 A 5310 CROSSBEAM AIRBUS 310 A310203 3930313 EU BS 1817 MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 409FE 273 PREVIOUS REPAIR FOUND LOCATED ON FWD PIT CROSSBEAM, RT, FS 1817, FR 33 AND Y69. REPAIR REQUIRES EVALUATION FOR MAJOR MI NOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 53-10-15 FIG 201 SHEET 4A. REPAIR EVALUATED AND CLA SSIFIED AS PER GMM 6-2-100 AS "MAJOR". 2 L 7 2 4F RT A35EU 2007030700176 20070307 00176 NM 2007 3 7 HALA0700072 1 20070228 A 3397 CONNECTOR BOEING 767 76733A 1385209 NM EMERGENCY LIGHTS UNKNOWN A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 583HA 25531 FOUND FWD GALLEY X-OVER AISLE FLOOR PROX LIGHTS INOP. REPLACED CONNECTOR STRIP OPN CK GOOD. 2 L 7 2 4F RT A1NM 2007030700177 20070307 00177 NM 2007 3 7 HALA0700073 1 20070228 A 3397 CONNECTOR BOEING 767 767300 1385204 NM EMERGENCY LIGHTS LOOSE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 586HA 24259 FOUND EMERGENCY FLOOR LIGHTS FROM MID GALLEY AFT TO OVERWING EXIT ACFT LEFT INOP. RETERMINATED LOOSE CONNECTOR AT OVERW ING EXIT. LIGHTS OPERATE NORMAL. 2 L 7 2 4F RT A1NM 2007030500128 20070305 00128 WP 2007 3 5 DU4R2007068 1 20070227 A 5320 STRUCTURE DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED B BWIA K NONE O OTHER IN INSP/MAINT 1 SO 15 789BV 49789 FOUND TRIMMED OUT AREA AT FS 157 ALONG THE AFT EDGE OF THE E/E BAY DOOR CUTOUT. REPAIRED BY FABRICATING AND INSTALLING REPAIR 22 BY 10.5 FROM 6AL-4V .032 IAW TIMCO REO-L00681 REV IR DATED 11/10/03 APPROVED BY FAA FORM 8110-3. 2 L 7 2 4F RT A6WE 2007030500131 20070305 00131 NM 2007 3 5 DHL2007781012 1 20070227 A 5313 STRINGER BOEING 727 727227 1384078 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 781DH 21996 FOUND FWD CARGO, BS 690, STR 27R, HAS SMALL SPOT OF CORROSION IN CHANNEL. CORROSION OUT OF LIMITS PER B727 SRM 53-10-1 FIG 1. CUT OUT DAMAGED PORTION OF STRINGER, 8" APPROX, FABRICATED, STR SPLICE OUT OF BAC1498-132, 20.5" LONG, PO NR 711 4294; SHIM OUT OF 7075-T6, .050' BY 8", PO NR 9003817, ALL PER B727 SRM 53-10-3 FIG 1. TREATED, PRIMED, AND INSTALLED REPAIR PARTS PER B727 SRM 51-10-2 AND 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2007030500137 20070305 00137 WP 2007 3 5 DHL2007802531 1 20070208 A 5310 DOOR FRAME DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 86868 46076 "B" CARGO DOOR AFT LWR JAMB CORNER 0.750" CRACK STA 560.000 L-31R TO L-32R. PERFORMED MAJOR REPAIR IAW AD2005-18-07 S/B 53-078 REV 1 JAN 25-01, FAA FORM 8100-9 DATED 02-05-07, BOEING MSG 1-274569547-4 DATED 02-05-07. REMOVED EXISTING REPA IR DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW BOEING MS 1-274569547-4, SEMAN DWG ED4428. PERFO RMED NDT INPS IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK OR CORROSION FOUND. FABRICATED REPAIR DOUBLER (AL7075T6 0.09 0") REPAIR TRIPLER (AL7075T6 0.125") 2 FILLERS (AL7075T6 0.080") IAW BOEING MSG 1-274569547-4, SEMAN DWG ED4428. CLEANE D, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTA 2 L 7 4 4F RT 4A25 2007030500159 20070305 00159 NM 2007 3 5 EIA2007019 1 20070222 A 2612 CLAMP BOEING 747 747230B 1384889 NM FIRE LOOP OPEN A EIAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 09 487EV 23286 ON TAKEOFF ROLL, NR 4 ENGINE NACELLE TEMP "A" LOOP TEMP WAS READING 8.2 UNITS WITH P2 PANEL AMBER LIGHT "FIRE DET" LIGHT ILLUM. ABORTED TAKEOFF. MX FOUND LOOP CLAMP OPEN WITH "A" LOOP (L/H BOTTOM) CONTACTING BEARING OIL SCAVENGE LINE. IN SPECTED FIRE LOOP AND SECURED CLIP AND VERIFIED CLEARANCE IAW MM 26-11-02. C/W ENGINE RUN, NO DEFECTS NOTED. 2 L 7 4 4F A20WE 2007030500160 20070305 00160 NM 2007 3 5 EIA2007021 1 20070222 A 5230 BEAM BOEING 747 747273C 1384896 NM CARGO DOOR CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 FOUND FORWARD CARGO DOOR LOWER CLOSE OUT BEAM CORROSION AT SCREW HOLES FROM STA 567 TO 662. CORRODED BEAM WEB REPLACED AND INSTALLED FASTENERS WITH SHORT EDGE MARGINS WERE REPAIRED. FASTENERS WITH SHORT EDGE MARGINS WERE TRIMMED OUT AND R EPAIR DOUBLERS WERE INSTALLED. 2 L 7 4 4F A20WE 2007030500166 20070305 00166 NM 2007 3 5 F3LA200700032 1 20070216 A 5415 D5451007900000 BEARING AIRBUS A319 A319111 3930336 NM LT PYLON CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 929FR 4725 2240 DURING C-2 CHECK, INSPECTION REPORTED LT PYLON PANEL 473BL, ONE SPHERICAL BEARING CORRODED. REPLACED SPHERICAL BEARING PER AMM 51-42-11. 2 L 7 2 4F RT A28NM 2007030500169 20070305 00169 NM 2007 3 5 F3LA200700029 1 20070216 A 5610 WINDSHIELD AIRBUS A319 A319111 3930336 NM COCKPIT CRACKED A F3LA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 927FR 2149 2209 AIR TURN BACK, BOTH FWD WINDSHIELDS CRACKED AT 20:00Z. ANTI-ICE LT AND RH WINDHIELDS. NO IMPACT ON WINDSHIELDS. OCCUR RED ON CLIMB-OUT AT 7000 MSL. REPLACED BOTH NR 1 AND NR 2 WINDSHIELDS IAW AMM 56-11-11, PB401. PART NUMBERS AND SERIAL NUMBERS ARE AS FOLLOWS: NR 1 WINDSHIELD - P/N STA320-1-7-1A (MFG SULLY), S/N 56343; NR 2 WINDSHIELD, P/N NP165311-8 ( MFG - PPG IND.), S/N 05028H8440. 2 L 7 2 4F RT A28NM 2007030500170 20070305 00170 EU 2007 3 5 F3LA200700031 1 20070216 A 5610 NP1653117 WINDSHIELD AIRBUS A318 A318111 3940019 EU COCKPIT CRACKED A F3LA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 807FR 8576 2276 AIR TURN BACK, CAPTAIN'S FWD WINDSHIELD SHATTERED. REPLACED CAPTAINS FWD WINDSHIELD IAW 56-11-11, PB401. 2 L 7 2 4F RT 2007030500174 20070305 00174 NM 2007 3 5 QXEA200700282 1 20070214 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND RIGHT OUTBOARD SEAT TRACK NR 11 HAS CORROSION IN CENTER OF TRACK AND ON EDGE OF CLAWS AT STATION X495. R EPAIRED IAW RD8-53-1342. 2 H 7 2 4T RT A13NM 2007030500178 20070305 00178 NM 2007 3 5 QXEA200700281 1 20070208 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND CORROSION ON FRAME CASTELLATION AT STATION X434.5 BETWEEN STRINGER 27S AND 28S. REPAIRED IAW SRM 51-20-1 1, 51-20-16, AND 51-20-36. 2 H 7 2 4T RT A13NM 2007030500182 20070305 00182 NM 2007 3 5 QXEA200700273 1 20070219 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND LEFT INBOARD FLAP TRACK NR 2 HAS 2 DIVOTS ON UPPER RAMP AND 2 DIVOTS ON LOWER RAMP. REPAIRED IAW RD8-57- 986. 2 H 7 2 4T RT A13NM 2007030500200 20070305 00200 NM 2007 3 5 SWAA071164 1 20070301 A 5312 6546578 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 13L. REPAIRED BULKHEAD WEB PER ER. 2 L 7 2 4F RT A16WE 2007030500214 20070305 00214 NM 2007 3 5 SWAA071162 1 20070301 A 5312 6546578 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6L. REPAIRED BULKHEAD WEB PER ER. 2 L 7 2 4F RT A16WE 2007030600005 20070306 00005 EU 2007 3 6 2007UALA00594 1 20070225 A 3350 LIGHTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 409UA 462 THE 2L EXIT SIGN HAS 1 BULB, 2R EXIT SIGN HAS 4 BULBS & RIGHT OVERWING EXIT SIGN HAS 1 BULB INOPERATIVE. [5-1-07] REP LACED LAMPS OPS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007030600016 20070306 00016 NM 2007 3 6 2007UALA00605 1 20070226 A 3350 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 557UA 26653 EMERGENCY STRIP LIGHTS ROW 23 INOPERATIVE. [SUP 4-17-07] TROUBLESHOT EMERGENCY STRIP AT SEAT ROW 23. FOUND WIRE PULLED FROM CONNECTOR, REPAIRED CONNECTOR 2 L 7 2 4F 4 F RT A2NM E17NE 2007030600022 20070306 00022 NE 2007 3 6 2007UALA00611 2 20070227 A 7230 CHECK VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE MALFUNCTIONED A UALA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS AP APPROACH 1 WP 29 662UA 27159 727334 LANDED UNDER AMBER ALERT DUE TO NR 1 ENGINE AT FLIGHT IDLE DUE TO COMPRESSOR STALL AND HIGH EXHAUST GAS TEMPERATURE. EM ERGENCY EQUIPMENT CALLED AS PRECAUTION. TROUBLESHOOTING IDENTIFIED FAILED 8TH STAGE PNEUMATIC CHECK VALVE. AFTER EXTE NSIVE TROUBLESHOOTING, IDENTIFIED CAUSE AS 8TH STAGE PNEUMATIC CHECK VALVE. REPLACED VALVE & CORRECTED RESULTANT DAMAGE . VALVE FAILED RELEASING THE POPPET SHAFT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007030600033 20070306 00033 NM 2007 3 6 SWAA071141 1 20070227 A 3350 MS155721 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007030600037 20070306 00037 NM 2007 3 6 SWAA071130 1 20070227 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 487WN 33854 EEPLS COVER BROKEN AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007030600067 20070306 00067 NM 2007 3 6 AMTA200700070 1 20070214 A 5320 MOUNT BRACKET BOEING 737 73783N 13844HI NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 323TZ 30033 CORROSION AT LT FLOOR SPLICE MOUNT BRACKET STA 727J IN AFT PIT, LBL 22. REMOVED CORROSION AT LT FLOOR SPLICE MOUNT BRAC KET, ORIG MAT THK .050 MAT LOSS .004 FOUND TO BE WITHIN LIMITS IAW SRM, FIG 103, TREATED AND PRIMED IAW SRM. (K) 2 L 7 2 4F RT A16WE 2007030600068 20070306 00068 NM 2007 3 6 AMTA200700071 1 20070214 A 5320 MOUNT BRACKET BOEING 737 73783N 13844HI NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 323TZ 30033 CORROSION RT FLOOR SPLICE MOUNT STA 727J, RBL 22. REMOVED CORROSION ON RT FLOOR SPLICE MOUNT BRACKET, ORIG MAT THK .050 MAT LOSS .003 FOUND TO BE WITHIN LIMITS IAW SRM, FIG 103, TREATED AND PRIMED IAW 51-20-01. (K) 2 L 7 2 4F RT A16WE 2007030600073 20070306 00073 2007 3 6 AMTA200700101 4 20070213 A 2565 416N222032 BOTTLE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE EVAC SLIDE UNSERVICEABLE A AMTA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 11 550TZ 13567 66 32584 RT EMERGENCY ESCAPE TEST LT IS ILLUMINATING (DIM) AT ALL TIMES. REPLACED RT EMER ESCAPE BOTTLE IAW AMM 25-65-02. CHECK S NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007030600083 20070306 00083 NM 2007 3 6 AMTA200700063 1 20070211 A 4990 380029817 APU BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE APU BAY UNSERVICEABLE A AMTA H DEACTIVATE SYST/CIRCUITS K FLUID LOSS CR CRUISE 1 GL 11 552TZ 20124 32586 APU OIL QTY WENT TO .50 AFTER 47 MIN INTO FLIGHT 27 MIN. ABOVE 20K CRUISE AT 35K. MANUALY SHUT APU DOWN. REMOVED AND R EPLACED APU USING M57-49-02. OPS CHECK OK. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007030600087 20070306 00087 NM 2007 3 6 2007UALA00617 1 20070301 A 5320 ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RT MLG WW CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 364UA 24533 RIGHT BS 695 INNER CHORD ANGLE CRACKED AT INNER RADIUS IN RT WW AREA AFT OF MLG UPLOCK. 21 MARCH 07, SUPPLEMENTAL D ATA UPDATE MAJOR REPAIR: REMOVED DAMAGE. INSTALLED NEW ANGLE REF MM 53-10-98 & SRM 51-40-02 PAGE 1. 2 L 7 2 4F 4 F RT A16WE E21EU 2007030600089 20070306 00089 NM 2007 3 6 2007UALA00619 1 20070227 A 2730 ACTUATOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE ELEVATOR MALFUNCTIONED A UALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 29 834UA 1420 RTFL UNDER AMBER ALERT DUE TO LOSS OF ELEVATOR CONTROL. POST FLIGHT REPORT SHOWS THS ACTUATOR POSITION ERROR 9CE REPORT ED BY SEC1 ELAC 2. SUPPLEMENTAL DATA UPDATE TRIMMABLE HORIZONTAL STABILIZER (THS) ACTUATOR LOCKED UP AND WOULD NOT RESPO ND TO INPUTS. WHILE FAULT TRACING PER TSM, FOUND THAT DISCONNECTING CERTAIN CONNECTORS ON THE THS ACTUATOR WOULD FREE UP THE MOTOR, SO SUSPECT THAT THS ACTUATOR ELECTRONICS ARE FAULTY. REPLACED THS ACTUATOR AND ALSO REPLACED ELAC 2 AS A PRE CAUTIONARY MEASURE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007030600090 20070306 00090 EU 2007 3 6 2007UALA00620 1 20070228 A 2520 SEAT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 420UA 489 PAX SEAT ROW 10R FOUND INSTALLED TOO FAR FWD AND INTERFERES WITH THE REMOVAL OF THE FWD RIGHT OVERWING EMERGENCY EXIT HA TCH. ERROR WAS MADE WHEN ATTACHMENT SCREWS FOR SEATS 10DEF WERE REMOVED FOR USE ON ANOTHER AIRCRAFT ON 1/19/2007 AT IA D. SEAT ROW WAS ACCIDENTALLY SHIFTED AND THEN RESECURED TOO FAR FORWARD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007030600091 20070306 00091 NM 2007 3 6 2007UALA00621 1 20070301 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EEL(S) AT 1A FWD, 4A FWD, 33ABC, 38 ABC & 49HJK ARE INOPERATIVE. RELAMPED. OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030600092 20070306 00092 NM 2007 3 6 2007UALA00622 1 20070301 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY CEILING LIGHT AT ROW 8 RT & ROW 53 LT ARE INOPERATIVE. RELAMPED. CKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030600094 20070306 00094 NM 2007 3 6 2007UALA00624 1 20070301 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 DOOR 3L FWD EMERGENCY SILL LIGHT INOP. RELAMPED. CKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030600095 20070306 00095 2007 3 6 2007UALA00625 4 20070228 A 2565 LOCK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 588UA 26717 RIGHT OVERWING SLIDE CARRIER LOCK RELEASE TRIGGER IS OUT OF ADJUSTMENT, DOOR WILL NOT LATCH. [SUP 05-18-07] TROUBLESHO T AND FOUND INNER LOCK TUBE WAS NOT CLOCKED PROPERLY WITH LOCK BASE RETAINER PREVENTING CONTACT WITH BEARING. ADJUSTED LOCK BASE RETAINER AND COMPLETED FORCE CHECK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030600119 20070306 00119 NM 2007 3 6 EIA2007028 1 20070222 A 5230 SKIN BOEING 747 747273C 1384896 NM CARGO DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 FWD CARGO DOOR LOWER CORNER VIEW PORT FOUND 3 CRACKS ON DOOR SKIN. REMOVED EXISTING REPAIR AND CUT OUT DAMAGED PART OF SKIN. FABRICATE NEW REPAIR DOUBLER AND FILLER, CARRIED OUT HFEC ON CUT EDGES AND ALL FASTENER HOLES. APPLY CHEM COATIN G AND PRIMER TO ALL PARTS, SKIN, AND FASTENERS WIT BMS 5-95. 2 L 7 4 4F A20WE 2007030600134 20070306 00134 NM 2007 3 6 07FDEA00620 1 20070301 A 5330 651842016 SKIN BOEING 727 727225 1384077 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FOUND LOWER FUSELAGE AT BS 178, LBL 0 - LBL 1 SKIN EDGE IS BENT, CRACKED AND KNIFE EDGED. REPAIRED DAMAGED LOWER FUSELA GE SKIN AT BS 178, LBL 0 - LBL 1 REF SRM 53-30-1, FIGURE 1. 2 L 7 3 4F A3WE 2007030600135 20070306 00135 NM 2007 3 6 07FDEA00621 1 20070301 A 5340 654531314 STRINGER CLIP BOEING 727 727225 1384077 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 MAIN DECK BODY FRAME STRINGER CLIP IS CRACKED AT BS 950C STR 9R. REPLACED STRINGER CLIP REFERENCE SRM 51-30-2. CLASSIF IED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007030700004 20070307 00004 NM 2007 3 7 ASAA0741502 1 20070227 A 5210 65648373 FITTING BOEING 737 737490 1384715 NM L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 713AS 30161 L1 DOOR HARD TO CLOSE AND LOCK. ADJUSTED L1 DOOR UPPER AFT CAM FITTING. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2007030700019 20070307 00019 NM 2007 3 7 ASAA0741496 1 20070227 A 5753 SKIN BOEING 737 7374Q8 138447Q NM T/E FLAP PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 RIGHT O/B AFT FLAP LOWER SURFACE IS PUNCTURED. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007030700027 20070307 00027 NM 2007 3 7 ASAA0741488 1 20070223 A 5315 654581094 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 CABIN STA 312 FLOORBEAM UPPER CHORD CORRODED. FLOORBEAM UPPER CHORD REPAIR ACCOMPLISHED IAW SRM 53-10-51 REPAIR 5. 2 L 7 2 4F RT A16WE 2007030700035 20070307 00035 EA 2007 3 7 TRAX200700281 1 20070222 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 937EV 8042 ASD BTM STEP BROKEN. 2 L 7 2 4F RT A21EA 2007030700038 20070307 00038 EA 2007 3 7 TRAX200700284 1 20070222 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 STA 333 FRAME CORRODED AFT SIDE AT STR 27 (MARKED). BLENDED CORROSION ON FS 333 FRAME, REMOVED 14 RIVETS IAW CRJ 200 SR M 53-21-15 AND 53-00-00 MS 7022223. SUPPLEMENTAL - SDR CLOSED 03/01/07. 2 L 7 2 4F RT A21EA 2007030700039 20070307 00039 EA 2007 3 7 TRAX200700285 1 20070223 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 CORROSION ON FRAME STATION 319.7 WL 0, AS REPORTED BY MAINTENANCE. 2 L 7 2 4F RT A21EA 2007030700050 20070307 00050 NM 2007 3 7 CALA0700113 1 20070302 A 5320 654654043 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 CRACKED AT WEB STA 639 ABOVE FLOOR LINE. REPAIRED IAW ECRA 5311-01299. 2 L 7 2 4F RT A16WE 2007030700054 20070307 00054 NM 2007 3 7 SWAA071200 1 20070302 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 424WN 29828 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 6 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007030700065 20070307 00065 NM 2007 3 7 SWAA071206 1 20070303 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 13R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030700073 20070307 00073 NM 2007 3 7 SWAA071191 1 20070302 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 908, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030700081 20070307 00081 NM 2007 3 7 SWAA071198 1 20070302 A 5322 69353656 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007030700084 20070307 00084 NM 2007 3 7 SWAA071176 1 20070302 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER 25R CRACKED AT BS 945. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007030700086 20070307 00086 2007 3 7 SWAA071174 4 20070302 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 L2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007030700126 20070307 00126 SO 2007 3 7 GLBA20060916 1 20070226 A 2121 FAN EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT A/C PACK INOPERATIVE A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 03 96ZK 120096 GROUND/TAXI - PILOT REPORT OF LT PACK BLOWING SMOKE IN THE COCKPIT. MAINTENANCE PLACED THE ITEM ON MEL 21-51-2 CATEGORY C. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND GROUND COOLING FAN IAW EMB-120 MM 21-51. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2007030700148 20070307 00148 NM 2007 3 7 HALA0700082 1 20070306 A 2913 PRESSURE SWITCH BOEING 767 767300 1385204 NM HYD PUMP DIRTY A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, CENTER HYD PUMP 2 LOW PRESS LIGHT IS ILLUMINATED. EICAS MSG C HYD PRIM 2 IS ALSO ILLUMINATED. CENTER HYD PRESS IS NORMAL. CLEANED AND RESECURED C2 HYD PUMP PRESSURE SWITCH (S34) PERFORMED FIM 29-11-00 FIG 108. OPS CKS NORMAL. 2 L 7 2 4F RT A1NM 2007030700149 20070307 00149 NM 2007 3 7 HALA0700080 1 20070305 A 2497 CONNECTOR BOEING 767 767300 1385204 NM IDG LOOSE A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 590HA 33467 ETOPS SIGNIFICANT SYSTEM, RT GEN DRIVE LT -ON, RT GEN OFF LT -ON. FOUND IDG SERVICE QUICK DISCONNECT POPPET NOT SEATED, SERVICED IDG, RAN ENG. POPPET SEALED NORMALLY, IDG OPERATION NORMAL. IDG FILTER INDICATOR NOT POPPED RESET RT GENERAT OR CONTROL IDG VOLTS FREQS NORMAL. NO LEAKS FOUND. OK FOR SERVICE PER AMM 12-13-03, AMM 24-11-00. 2 L 7 2 4F RT A1NM 2007030700150 20070307 00150 NM 2007 3 7 HALA0700084 1 20070306 A 2150 UNKNOWN BOEING 767 767300 1385204 NM A/C PACK UNKNOWN A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 590HA 33467 ETOPS SIGNIFICANT SYSTEM, LEFT PACK INOP LIGHT ILLUM. EICAS MESSAGE ,LEFT PACK TEMP DISPLAYED, OPERATED WARM AFTER STAN DBY SELECTED. PERFORMED BITE CHECK PER FIM 21-51-00, NO FAULT NOTED. 2 L 7 2 4F RT A1NM 2007030700151 20070307 00151 NM 2007 3 7 QXEA200700323 1 20070224 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - AFT CARGO DOOR RIVET ON INNER SKIN DAMAGED, AFT MIDDLE SECTION OF DOOR. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007030700152 20070307 00152 NM 2007 3 7 QXEA200700324 1 20070226 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 245 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND FUSELAGE EXTERIOR BELLY SKIN HAS CORROSION AT STATION FS X245. REPAIRED IAW SRM 51-20-11. 2 H 7 2 4T RT A13NM 2007030700153 20070307 00153 NM 2007 3 7 QXEA200700325 1 20070222 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND CHAFE ON EXTERIOR SKIN DOUBLER AROUND LAVATORY SERVICE DOOR AT AFT SIDE OF DOOR CUTOUT. REPAIRED IAW SRM 51-20-11. 2 H 7 2 4T RT A13NM 2007030700154 20070307 00154 NM 2007 3 7 QXEA200700326 1 20070224 A 5753 HANGER ASSY DHAV DHC8 DHC8202 2809007 NM NR 4 FLAP TRACK CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND LEFT NR 4 FLAP TRACK INBOARD HANGER UPPER BOLT BUSHING IS CORRODED. REPAIRED IAW SRM 57-50-42. 2 H 7 2 4T RT A13NM 2007030700155 20070307 00155 EU 2007 3 7 SIMA200700601 1 20070301 A 2612 899052 CONTROL UNIT SAAB SF340 340B 7860101 EU FIRE DETECTION FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 286AE 21869 340B286 LEFT TAIL PIPE HOT WILL NOT TEST. REMOVED AND REPLACED LEFT FIRE DETECTION CONTROL UNIT IAW SAAB AMM 26-11-00. OPERATI ONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007030700156 20070307 00156 NM 2007 3 7 EIA2007015 1 20070218 A 2612 580258003 CABLE BOEING 747 747230B 1384889 NM RELIEF VALVE BROKEN A EIAA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CR CRUISE 1 NM 09 487EV 0167 23286 AFTER TAKEOFF, IN CLIMB, AT F1120 PILOTS FIRE WARNING ANNUNCIATOR ILLUMINATED WITH FLIGHT ENGINEER'S NR 1 ENG A & B LOOP S AT TOP OF BAND. ENGINE WAS SHUT DOWN AND RT FIRE BOTTLE DISCHARGED. FIRE DETECTION RETURNED TO NORMAL AND AIRCRAFT R ETURNED TO TLV. TROUBLESHOOTING LED TO VARIABLE BYPASS VALVE, CABLE AND BELLCRANK NEEDING TO BE REPLACED. THE VBV CABL E WAS BROKEN AND THE BELLCRANK WAS BENT. 2 L 7 4 4F A20WE 2007030700157 20070307 00157 NM 2007 3 7 QXEA200700319 1 20070303 A 6123 30005000056 CONTROL UNIT DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 358PH 4288 506 PDX FLIGHT NR 2092 - AUTO FEATHER FAILED TO ARM DURING DAILY TEST. MAINTENANCE REPLACED A/F SELECT SWITCH NO HELP. RE PLACED NR 1 AND NR 2 TSCU'S BOTH REPLACED IAW P&W 123 MM 72-01-10 PAGE 240-424, PARAGRAPH 7A AND B. ALL CHECK ARE GOOD. PERFORMED THE AUTO FEATHER/POWER UP TRIM TEST 21 TIMES, ALL WORKED IAW TASK CARD 9720018, P/N 30005-0000-49, S/N 3461, TSR 675.04. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030700158 20070307 00158 NM 2007 3 7 QXEA200700258 1 20070214 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM LT WING LE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - LEFT LEADING EDGE UPPER SPAR FLANGE HAS GOUGE AT STATION YW 306.5. REPAIRED IAW RD8-57-3584 AND RD8-57-1119. 2 H 7 2 4T RT A13NM 2007030700178 20070307 00178 NM 2007 3 7 HALA0700074 1 20070228 A 2841 100800201 INDICATOR BOEING 767 76733A 1385209 NM COCKPIT MALFUNCTIONED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 587HA 16847 16847 33521 ETOPS SIGNIFICANT SYSTEM - FUEL GAUGE ON OVERHEAD PANEL, RT SIDE UNREADABLE. REPLACED FUEL INTEGRATED FUEL QTY INDICATI ON PER AM 28-41-04-004-003, OPS CHECK GOOD SECURITY CONDITION GOOD. 2 L 7 2 4F RT A1NM 2007030700179 20070307 00179 NM 2007 3 7 HALA0700071 1 20070228 A 2710 UNKNOWN BOEING 767 76733A 1385209 NM UNKNOWN A HALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM - "AILERON LOCKOUT" EICAS MESSAGE ILLUMINATED AT HIGH SPEED, MOMENTARILY DURING CLIMB A/C >=290 KIAS. T/S PER FIM 27-11-00/101 FIG 104 BLKS 1-5-10-15. SYS IS OK. 2 L 7 2 4F RT A1NM 2007030700180 20070307 00180 WP 2007 3 7 NWAA070709763 1 20070227 A 2910 VALVE DOUG DC9 DC941 302207N WP HYD SYSTEM LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 763NW 47396 FLIGHT CREW NOTICED THE RIGHT HYDRAULIC SYSTEM HAD LOST ALL FLUID AND PRESSURE WHILE AT CRUISE. COM PROCEDURES WERE COM PLIED WITH AND VERIFIED SYSTEM INOPERATIVE. THE FLIGHT RETURNED TO A NORMAL SAFE LANDING BACK AT DEPARTURE AIRPORT AND WAS TOWED TO THE GATE. MAINTENANCE AT DTW FOUND THE RT HYDRAULIC SYSTEM VACUUM BREAKER VALVE LEAKING AND REPLACED IT. STANDARD COMPONENT REPLACEMENT DUE TO LOSS OF FLUID ALSO ACCOMPLISHED. FUNCTIONAL CHECKS OF RELATED SYSTEMS, INCLUDING GEAR SWINGS, PERFORMED SATISFACTORILY, LEAK CHECKS WERE ALL GOOD, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007030700181 20070307 00181 EU 2007 3 7 NSVA20070018 1 20070123 A 2841 INDICATOR SAAB SF340 340B 7860101 EU FUEL FLOW FAILED A NSVA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 EA 27 347CJ 347 FOUND LT FUEL FLOW GAUGE FAILED DURING TAKEOFF ROLL. CYCLED C/B PERFORMED, OPS CHECK FUEL FLOW GAUGE, GROUND RAN OK OPS CK GOOD. 2 L 7 2 4T RT A52EU 2007030700182 20070307 00182 EU 2007 3 7 NSVA20070020 1 20070128 A 7712 6071T20P16 DCU SAAB SF340 340B 7860101 EU LT ENGINE MALFUNCTIONED A NSVA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 341CJ 341 FOUND LT ENG IGNITION ILLUMINATED WITH TQ FLUX FULL SCALE AND ENGINE SURGING. REPLACED LEFT TORQUE SPEED SENSOR IAW GE MM 74-00-00, PN: 5066T92G05SN ON: 1253B, SN OFF: 51M0190B. REPLACED LEFT ENG DECU IAW GE MM CH 74-00-00. OPS CHECK GOO D. NO PROBLEMS NOTED, PN: 6071T20P16, SN ON: ECOT1599 SN OFF: ECOT1613. 2 L 7 2 4T RT A52EU 2007030700183 20070307 00183 CE 2007 3 7 NSVA20070021 1 20070129 A 2910 SHUTTLE VALVE BEECH 1900 1900D 1154162 CE HYD SYSTEM FAULTED A NSVA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 155CJ UE55 FOUND LANDING GEAR WOULD NOT COME UP DURING TAKEOFF. TROUBLESHOT GEAR IAW BE AMM 32-30-00-101 CHART 101, FOUND HYDRAULI C FLUID LOW AND RISUAL VERY CLOUDY DRAINED HYDRAULIC FLUID AND INSPECTED FILTER FOUND NO DEFECTS WITH FILTER. RESERVICE D POWER PACK IAW BE AMM 32-30-00. CLEANED FILTER IAW W/C 32-30-02 AND CONDUCTED GEAR SWING IAW 32-30-01. OPS CHECK SAT . PERFORMED W/C 32-30-02 LANDING GEAR POWER PACK FILTER AND SCREENS. PERFORMED W/C 32-30-01 LANDING GEAR RETRACTION, O PS CHECK. LANDING GEAR OPS CHECKS, FOUND LG HYDRAULIC PACK TO HAVE A FAULTY SHUTTLE VALVE. REPLACED LANDING GEAR HYDRA ULIC POWER PACK IAW BE AMM 32-30-02. PERFORMED LANDING GEAR RETRACTION OPERATIONAL CHECK IAW W/C 32-30-01 AND FOUND TO 2 L 7 2 4T RT A24CE 2007030700218 20070307 00218 NM 2007 3 7 DLM88070181 1 20070301 A 5330 5924802517 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 FS 260, LONG 17-18, GROUND DAMAGE CUTOUT REPAIR. THE FUSELAGE SKIN WAS DAMAGED BY THE JET WAY. THE DAMAGE WAS REMOVED WITH A 8" BY 11" SKIN CUTOUT AND A SECTION OF LONGERON 17 REMOVED. THE SKIN WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPA IR DOUBLER AND THE LONGERON REPAIRED WITH AN FORMED ALUMINUM REPAIR SECTION PER THE MD-88 SRM. THE REPAIRS WERE DOCUME NTED PER ER/A 460339-14. 2 L 7 2 4F RT A6WE 2007030700219 20070307 00219 NM 2007 3 7 DL76L070182 1 20070301 A 4990 388019010 PUMP BOEING 767 767332 1382001 NM APU MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 183DN 27110 ON ENG START APU FAULT LIGHT ILLUM AND AUTO S/D ON PUSH BACK. APU ECU FAULTED LOW OIL PRESS SW PREV REPLACED. REPLACED OIL LUBE PUMP AND ECU APU NOW STARTS AND RUNS. ATTEMPTED ENG ST WAS SUCCESSFUL LEAK CHECK OK A/C RTS WITH FULL SERVICE APU PUMP MFG NR 3880190-10. 2 L 7 2 4F RT A1NM 2007030700220 20070307 00220 NM 2007 3 7 DLM88070183 1 20070301 A 5512 5922578515 SKIN DOUG MD88 MD88 3023688 NM HORIZ STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 984DL 53311 HORIZONTAL STABILIZER/RT/UPPER AFT SKIN PANEL CRACK REPAIR. THE UPPER AFT SKIN OF THE RT HORIZONTAL STABILIZER WAS FOUN D WITH A .625" CRACK NEAR INBD AFT EDGE OF THE PANEL. THE CRACK WAS ROUTED OUT WITH A SMALL CUTOUT ON A TIME LIMITE D BASIS PER ER/A 460410-14. PERMANENT REPAIR REQUIRES REPLACEMENT OF THE SKIN PANEL. 2 L 7 2 4F RT A6WE 2007030700221 20070307 00221 NM 2007 3 7 DLM88070184 1 20070302 A 5512 5922578515 SKIN DOUG MD88 MD88 3023688 NM HORIZ STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 905DE 53410 HORIZONTAL STABILIZER/RT/UPPER AFT SKIN PANEL, CRACK REPAIR. THE UPPER AFT SKIN PANEL OF THE RT HORIZONTAL STABILIZER W AS FOUND WITH A .25" CRACK NEAR THE INBD AFT EDGE OF THE PANEL. THE CRACK WAS STOP DRILLED ON THE FWD END AND ROUTED OU T TO THE AFT EDGE OF THE PANEL ON A TIME LIMITED BASIS. THE PERMANENT REPAIR REQUIRES REPLACEMENT OF THE SKIN PANEL. T HE REPAIR WAS ACCOMPLISHED PER ER/A 460409-14. 2 L 7 2 4F RT A6WE 2007030700222 20070307 00222 2007 3 7 DL764070186 4 20070303 A 3445 6228971500 COMPUTER BOEING 767 767432ER 1385134 NM TCAS MALFUNCTIONED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 840MH 137016 29717 TCAS FAILED IN FLT. INSTALLED PROCESSOR FROM A/C 1821, CKS GOOD. 2 L 7 2 4F RT A1NM 2007030700223 20070307 00223 GL 2007 3 7 DL764070188 2 20070305 A 7230 COMPRESSOR BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 1 ENGINE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 829MH 22126 29700 702247 ON DESCENT, RECEIVED A BLEED HPSOV AND N2 VIBS INCREASED TO 5 UNITS. INLET AND EXHAUST OK CHECK CHIP DETECTORS OK RUN E NG AGAIN VIBS RETURNED. BOROSCOPE COMPRESSOR FOUND 6TH STAGE DAMAGE. BORO AND FOUND HPC 6TH AND 7TH STAGE DAMAGE BEYON D MM LIMITS. REMOVED BOROSCOPE PLUGS B 1-5 B 1-6 NR 1 ENG. ENG REMOVAL R REPLACED NR 1 ENG PER TRANS 1RT103. 2 L 7 2 4F 4 F RT A1NM E23EA 2007030700224 20070307 00224 NM 2007 3 7 DLM88070189 1 20070303 A 5512 5922578515 SKIN DOUG MD88 MD88 3023688 NM HORIZ STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 942DL 49815 702247 FOUND HORIZONTAL STABILIZER/RT/UPPER AFT SKIN PANEL, CRACK REPAIR. THE UPPER AFT SKIN PANEL OF THE RT HORIZONTAL STABIL IZER WAS FOUND WITH A 1.85" CRACK NEAR THE INBD AFT END OF THE PANEL. THE CRACK WAS STOP DRILLED ON A TIME LIMITED BASI S. THE PERMANENT REPAIR WILL REPLACE THE SKIN PANEL WITH A NEW PANEL. THE REPAIR IS DOCUMENTED PER ER/A 460477-14. 2 L 7 2 4F RT A6WE 2007030700225 20070307 00225 NM 2007 3 7 07FDEA00519 1 20070217 A 3260 656021123 MODULE BOEING 727 727233 138408A NM E&E BAY FAULTY A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CL CLIMB 1 SO 25 284FE 22621 ON TAKEOFF WHEN GEAR RETRACTED, RED DOOR AND ALL RED GEAR LIGHTS WITH GEAR WARNING HORN. DOORS LIGHT EVENTUALLY GO OUT, BUT RED GEAR LIGHTS AND AURAL HORN STAYS ON. TROUBLESHOT SYSTEM REF MM 32-61-001-1. REPLACED LGAU MODULE REF MM 32-09 -121-4. LANDING GEAR POSITION AND WARNING SYSTEM TEST GOOD REF WDM 33-19-01 P2 AND MM 32-61-001-5. 2 L 7 3 4F RT A3WE 2007030700226 20070307 00226 NM 2007 3 7 07FDEA00520 1 20070216 A 3233 39140165505 ACTUATOR DOUG MD11 MD11F 3023600 NM RT MLG BROKEN A FDEA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 25 588FE 21017 21017 48490 AFTER GEAR RETRACTION ON TAKEOFF (FROM ALA RWY 05) RECEIVED RED UNSAFE GEAR INDICATION ON RT MAINS INDICATED ON GEAR HAN DLE INDICATORS AS WERE AS CONF SYNOPTIC. RAN RED TABS. RETURNED TO ALA AFTER DUMPING AP PXLY 100.000 LBS CONFIG SYNOPT IC SHOWED RIGHT GEAR TEMPS COLD VS ALL OTHERS. TEMPS WERE -2 SAME AS OAT. AT WALK AROUND, FOUND RIGHT MAIN LANDING GEA R UNLOCK ACTUATOR BROKEN. THE UNLOCK ACTUATOR FROM RIGHT MLG REMOVED PER MD-11 MM 32-33-02-4. INSTALLED NEW RT MLG UNL OCK ACTUATOR PER AMM 32-33-02-4. CHECK ACCOMPLISHED PER AMM OK. NO LEAKS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F RT A22WE 2007030700227 20070307 00227 NM 2007 3 7 07FDEA00521 1 20070216 A 2910 HYDRAULIC LINE DOUG MD11 MD11F 3023600 NM HYDRAULIC SYS LEAKING A FDEA O OTHER J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SO 25 612FE 48605 HYD 3 FAIL, QTY .1 LOWERED GEAR VIA ALTERNATE EXTENSION FOUND LEAK IN CENTER GEAR AT HYD LINE ADJACENT TO RMPS. REPAIRE D CRACK AT FERREL WITH RYNGLOK PER MM 20-10-01-2. SERVICED NR 3 HYD RESERVOIR TO FULL AND LEAK CHKS OK PER SMP. NEED A LTERNATE RELEASE CONTROL LEVER NOSE/MAIN GEAR STOWED. RESET ALTERNATE GEAR EXTENSION LEVER PER REF TO MD-11 WORK CARD 3 2T3601 REVISION NR 0001, 11-FEB-2004. SYSTEM OKAY FOR SERVICE AT THIS TIME. 2 L 7 3 4F RT A22WE 2007030700228 20070307 00228 NM 2007 3 7 07FDEA00522 1 20070217 A 2120 DUCT DOUG MD11 MD11F 3023600 NM A/C BAY DISCONNECTED A FDEA F ACTIVATE FIRE EXT. J WARNING INDICATION CR CRUISE 1 SO 25 606FE 48602 INTMT LVL 3 APU FIRE ALERT AFTER 1 50, EN ROUTE-SUSPECTED BLEED/DUCT LEAK COMPLIED W/QRH, BOTTLE BLOWN INSTALLED SERVICE ABLE FIREX CONTAINER AND CARTRIDGE IN THE NR 1 POSITION AND REINSTALLED FIREX CONTAINER IN THE NR 2 POSITION IN REF FOUN D FLEX DUCT AT EXHAUST DISCONNECTED AND CLAMP MISSING. RAN APU FOUND AIR LEAKING AT PRESS REG VALVE CLAMP, TIGHTENED CL AMP. RAN NR 2 ENG AND COULD HEAR A MASSIVE AIR LEAK RUMBLE, WITH ENG RUNNING SHUT DOWN APU AND FOUND AT THE FORWARD FIR EWALL THE NR 2/APU MANIFOLD LEAKING AT THE CLAMP. TIGHTENED CLAMP AND AIR LEAK STOPPED. CLAMP WAS EXTREMELY LOOSE. AL L OTHER CLAMPS AND CONNECTIONS LEAK CHECK GOOD. 2 L 7 3 4F RT A22WE 2007030700229 20070307 00229 NM 2007 3 7 07FDEA00523 1 20070218 A 3260 656021123 ACCESSORY UNIT BOEING 727 727233 138408A NM E&E BAY FAILED A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CL CLIMB 1 SO 25 284FE 22621 DURING GEAR RETRACTION, AN AUDIO HORN SOUNDS WITH A CORRESPONDING RED GEAR LIGHTS AND RED DOOR LIGHT. NOTE: RED DOOR LI GHT EXTINGUISHES AFTER AN APPROPRIATE TIME. BEFORE TAKEOFF, AIRCREW CYCLED FLAPS TO 30 DEGREES AND BACK TO 15 DEGRE ES. TRIED SAME SEQUENCE OF EVENTS SEVERAL TIMES WITH NORMAL AND NOT NORMAL RESULTS. JACKED AC AND TESTED LANDING GEAR WARN SYSTEM. CONFIRMED OPERATION OF THROTTLE, FLAP AND L/G SWITCHES PER MM 31-26-000-5 P3 STEP 4D. ALL CHECK GOOD. RE PLACED L/G POS/WARN ACCESS UNIT PER MM 32-09-121-4 P1 AND TESTED ACCESS UNIT PER MM 32-09-121-5 P 1-4 ALL CHECKS OK INCL UDING L/G WARN HORN. DOWN JACKED PER MM 7-11-000-2. 2 L 7 3 4F RT A3WE 2007030700230 20070307 00230 NM 2007 3 7 07FDEA00639 1 20070304 A 5713 STRINGER DOUG MD11 MD11 3023602 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 CRACK FOUND AT STRINGER END 9R (XORS 819), APPROX 13" LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. (SUPPLEMENTAL 23 MARCH 07) CRACK AT STRINGER END 9R (XORS 819) ON RIGHT HAND WING TANK TRIMMED OUT AND REPAIRED WITH SPLICES AS PE R SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007030700231 20070307 00231 NM 2007 3 7 07FDEA00640 1 20070304 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 CRACK FOUND AT STRINGER END 12R (XORS 642), APPROX. 9" LENGTH ON RIGHT WING TANK, DURING HFEC INSPECTION. (SUPPLEMENTAL 23 MARCH 07) CRACK AT STRINGER END 12R (XORS 642) ON RIGHT HAND WING TANK CARRIED OUT REPAIR AS PER SRM 57-20-00 FIGUR E 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007030700232 20070307 00232 NM 2007 3 7 07FDEA00641 1 20070304 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 CRACK FOUND AT STRINGER END 13R (XORS 577), APPROX 11" LENGTH ON RIGHT WING TANK, DURING HFEC INSPECTION. (SUPPLEMENTAL 23 MARCH 07) CRACK AT STRINGER END 13R (XORS 577) ON RIGHT HAND WING TANK TRIMMED OUT 2 BAY AND REPAIRED WITH SPLICES AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007030700233 20070307 00233 NM 2007 3 7 07FDEA00642 1 20070304 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 CRACK FOUND AT STRINGER END 14R (XORS 521), APPROX 14" LENGTH ON RIGHT WING TANK, DURING HFEC INSPECTION. (SUPPLEMENTAL 23 MARCH 07) CRACK AT STRINGER END 14R (XORS 521) ON RIGHT HAND WING TANK TRIMMED OUT AND REPAIRED WITH SPLICES AS P ER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007030700234 20070307 00234 EU 2007 3 7 07FDEA00643 1 20070304 A 5320 A5378193720100 ADAPTER AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 669FE 774 FOUND MAIN CABIN ADAPTER TRACK CORRODED FRAME 36 RBL32. REMOVED AND REPLACED ADAPTER TRACK. 2 L 7 2 4F RT A35EU 2007030700235 20070307 00235 EU 2007 3 7 07FDEA00644 1 20070304 A 5320 A5351293420000 CROSSBEAM AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 669FE 774 MAIN CABIN ADAPTER TRACK CORRODED FRAME 48 RBL 32 REMOVED CORROSION IAW A300-600 SRM 51-22-10. ORIGINAL SCALLOP OPENING 0.421 IAW A300-600 SRM 53-15-15 FIG 9 AND A300-600 SRM 51-31-20 FIG 36. REMAINING SCALLOP OPENING .475 FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-1-15 FIG 107. REMOVED AND REPLACED CROSSBEAM P/N A5351293420000 IAW A300-600 SRM 51-40-2 1 PAR 5, A300-600 SRM 51-40-00 PG 95/96 AND A300-600 SRM 51-49-00 PAR 3. 2 L 7 2 4F RT A35EU 2007030700236 20070307 00236 EU 2007 3 7 07FDEA00645 1 20070304 A 5315 A5327828820300 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 669FE 774 MAIN CARGO COMPT FLOORBEAM AT FRAME 62, 32 RIGHT OF B/L SUPPORT ANGLE HAS CORROSION AROUND FASTENER HOLES. REMOVED AND REPLACED ADAPTER SEAT TRACK. 2 L 7 2 4F RT A35EU 2007030700238 20070307 00238 NM 2007 3 7 07FDEA00647 1 20070305 A 5340 65453131 STRINGER CLIP BOEING 727 727225 1384077 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FOUND MAIN CABIN STATION 620, STR 3R, STRINGER CLIP IS DAMAGED REPLACED STRINGER CLIP REF SRM 51-30-2. 2 L 7 3 4F A3WE 2007030700239 20070307 00239 WP 2007 3 7 07FDEA00579 1 20070227 A 5310 DOOR FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 FOUND EXISTING REPAIR MAIN CABIN R3 DOOR JAMB FROM STA 1305 TO STA 1315 BETWEEN LONGERONS 26 AND 27 RT. REMOVED OLD REP AIR IAW SRM 51-33-01 PAR 6-10 VOL 2. INSTALLED NEW REPAIR DOUBLER IAW SRM 53-50-00 FIG 19 VOL 1. FABRICATED PART IAW D ETAIL PART TRAVELER I036055/N01055 AND IAW SRM 53-50-00 FIG 19 DETAIL -9 VOL 1. 2 L 7 3 4F A22WE 2007030700241 20070307 00241 WP 2007 3 7 07FDEA00581 1 20070227 A 5311 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 FOUND EXISTING FRAME REPAIR AT STA 1761 BETWEEN LONGERONS 11 AND 12 RT. REMOVED RIVETS AND INSTALLED HI LOCKS FIRST OVE RSIZE IAW SRM 53-30-00 FIG 5 SHT 2 VOL 1 AND SRM 51-33-01 PAR 6-10 VOL 2. 2 L 7 3 4F A22WE 2007030700242 20070307 00242 WP 2007 3 7 07FDEA00582 1 20070227 A 5311 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 FOUND EXISTING FRAME REPAIR AT STA 1781 BETWEEN LONGERONS 11 AND 12 RT. REMOVED RIVETS AND INSTALLED HI LOCKS FIRST OVE RSIZE IAW SRM 53-30-00 FIG 5 SHT 2 VOL 1 AND SRM 51-33-01 PAR 6-10 VOL 2. 2 L 7 3 4F A22WE 2007030700243 20070307 00243 WP 2007 3 7 07FDEA00583 1 20070227 A 5311 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 FOUND EXISTING FRAME REPAIR AT STA 1701 BETWEEN LONGERONS 11 AND 12 RT. REMOVED RIVETS AND INSTALLED HI LOCKS IAW SRM 5 3-30-00 FIG 5 SHT 2 VOL 1, USED FIRST OVERSIZE FASTENERS AS REQUIRED IAW SRM 51-33-01 VOL 2. 2 L 7 3 4F A22WE 2007030700244 20070307 00244 WP 2007 3 7 07FDEA00584 1 20070227 A 5311 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 FOUND EXISTING FRAME REPAIR AT STA 1721 BETWEEN LONGERONS 11 AND 12 RT. REMOVED RIVETS AND INSTALLED HI LOCKS IAW SRM 5 3-30-00 FIG 5 SHT 2 VOL 1, USED OVERSIZE FASTENERS AS REQUIRED IAW SRM 51-33-01 VOL 2. 2 L 7 3 4F A22WE 2007030700245 20070307 00245 WP 2007 3 7 07FDEA00585 1 20070227 A 5311 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 FOUND EXISTING FRAME REPAIR AT STA 1741 BETWEEN LONGERONS 11 AND 12 RT. REMOVED RIVETS AND INSTALLED HI LOCKS IAW SRM 5 3-30-00 FIG 5 SHT 2 VOL 1, USED OVERSIZE FASTENERS AS REQUIRED IAW SRM 51-33-01 VOL 2. 2 L 7 3 4F A22WE 2007030700246 20070307 00246 WP 2007 3 7 07FDEA00586 1 20070227 A 5311 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 373FE 46611 FOUND EXISTING FRAME REPAIR AFT CARGO COMPARTMENT AT STA 1856 BETWEEN LONGERONS 52 AND 51 RT. PERFORMED INSPECTION OF R EPAIR AND NOT FOUND INCOMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-P2 BECAUSE FOUND 20 RIVETS INSTEAD OF HI L OCKS IAW SRM 53-30-00 PAGE 15 FIG 5 SHT 1 VOL 1. REMOVED RIVETS AND INSTALLED HI LOCKS OVERSIZE IAW SRM 53-30-00 PAGE 1 5 FIG 5 SHT 1 VOL 1 AND SRM 51-33-01 VOL 2. 2 L 7 3 4F A22WE 2007030700247 20070307 00247 WP 2007 3 7 07FDEA00587 1 20070227 A 5311 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 FOUND EXISTING FRAME REPAIR AT STA 1741 BETWEEN LONGERONS 11 AND 12 LT. REMOVED RIVETS AND INSTALLED HI LOCKS IAW SRM 5 3-30-00 FIG 5 SHT 2 VOL 1, USED OVERSIZE FASTENERS AS REQUIRED IAW SRM 51-33-01 VOL 2. 2 L 7 3 4F A22WE 2007030700248 20070307 00248 WP 2007 3 7 07FDEA00588 1 20070227 A 5311 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 FOUND EXISTING FRAME REPAIR AT STA 1721 BETWEEN LONGERONS 11 AND 12 LT. REMOVED RIVETS AND INSTALLED HI LOCKS IAW SRM 5 3-30-00 FIG 5 VOL 1, USED OVERSIZE FASTENERS AS REQUIRED IAW SRM 51-33-00 VOL 2. 2 L 7 3 4F A22WE 2007030700249 20070307 00249 WP 2007 3 7 07FDEA00589 1 20070227 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 RT AIR CONDITIONING COMPT CRACK 1" LONG ON INTERNAL VERTICAL BULKHEAD AT STA 495 Z= -58. REMOVED PORTION OF BROKEN WEB, AND REPAIRED IAW SRM 53-40-00 VOL 1 FIG 34. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I035881/N00881 AND IAW SRM 53-4 0-00 VOL 1. 2 L 7 3 4F A22WE 2007030700250 20070307 00250 WP 2007 3 7 07FDEA00590 1 20070227 A 5310 DOOR FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 MAIN CABIN FOUND NR 1 CRACK 1" LONG ON LOWER SIDE WEB JAMB DOOR L 3 AT STA 1256 LONG NR 26 LT SIDE. REMOVED EXISTING DO UBLER IAW SRM 51-35-01 VOL 2 PAR 1-5. INSTALLED NEW DOUBLER. REPAIRED IAW SRM 53-50-00 FIG 10 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER I035547/N00547 AND IAW SRM 53-50-01 FIG 10 SHT 1 VOL 1. 2 L 7 3 4F A22WE 2007030700251 20070307 00251 WP 2007 3 7 07FDEA00591 1 20070227 A 5310 DOOR FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 MAIN CABIN FOUND NR 1 CRACK 0.40" LONG ON LOWER SIDE WEB JAMB DOOR R 3 AT STA 1256 LONG NR 26 RT SIDE "UNDER EXISTING RE PAIR". REMOVED EXISTING DOUBLER IAW SRM 51-35-01 PAR 1-5 / 51-33-01 PAR 6-10 VOL 2. INSTALLED NEW REPAIR DOUBLER IAW S RM 53-50-00 FIG 19 SHT 1 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER I035540/N00540 AND IAW SRM 53-50-00 FIG 19 SHT 1 VOL 1. 2 L 7 3 4F A22WE 2007030700254 20070307 00254 WP 2007 3 7 07FDEA00594 1 20070227 A 5313 LONGERON SPLICE DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 FOUND FWD CARGO COMPT LONG NR 51 LT AT STA 989 TO STA 1009 EXISTING LONG SPLICE REPAIRS. REMOVED 2 SPLICES IAW SRM 51-3 0-00 VOL 2. INSTALLED 2 NEW LONGERON SPLICES IAW SRM 53-10-00 FIG 1 AND FIG 2 VOL 1. FABRICATED PARTS IAW DETAIL PART TRAVELER N01190 AND SRM 53-10-00 FIG 1 FIG 2 VOL 1. 2 L 7 3 4F A22WE 2007030800001 20070308 00001 WP 2007 3 8 07FDEA00595 1 20070227 A 5754 RIB DOUG DC10 DC1010 3022110 WP L/E SLAT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 RT WING L/E TRACK SUPPORT RIB AT STA XOS 1005 EXISTING REPAIR ANGLE. REMOVED SLAT TRACK DOOR FOR ACCESS IAW MM 57-21-01 -2. REPLACED DAMAGED RIB IAW DWG ARB1096. REINSTALLED SLAT TRACK DOOR IAW MM 57-21-01-2. 2 L 7 3 4F A22WE 2007030800002 20070308 00002 WP 2007 3 8 07FDEA00596 1 20070227 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 FOUND LOWER EXT FUSELAGE FOUND DENT 6" BY 4" DEPTH .066" FROM STA 1901 TO STA 1910 LONG NR 33 - 35 RT. DENT EVALUATED A ND FOUND TO BE OUT OF LIMITS IAW PROVISION 1A OF SRM 53-20-00 VOL 1 FIG 13. DENTS AREA LESS THAN 3" A PART. REPAIR PER FORMED IAW SRM 53-20-00 VOL 1 FIG 6 SHT 3-6. 2 L 7 3 4F A22WE 2007030800005 20070308 00005 WP 2007 3 8 07FDEA00599 1 20070227 A 5730 DOUBLER DOUG DC10 DC1010 3022110 WP RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 RT WING LOWER SURFACE AT XORS 264 ON BEAVER TAIL DOUBLER AROUND NR 15 HEAD FASTENERS FOUND LIGHT CORROSION WITH EXFOLIAT ION. TAPER LOCKS REMOVED IAW SRM 51-34-01 PAGE 1-7 VOL 2. CORROSION REMOVED IAW SRM 57-10-00 FIG 69 VOL 1, AREA OUT OF LIMITS TRIMMED OUT (SEE JPF). RECOMMENDED ACTION EA NR 8-5710-103696 ACCOMPLISHED. 2 L 7 3 4F A22WE 2007030800006 20070308 00006 WP 2007 3 8 07FDEA00600 1 20070227 A 5312 PRESSURE PANEL DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 MAIN CABIN BTWN STA 535 AND 555 X= 90 BTWN HORIZ PRESS PANEL AND FINGER DOUBLER FOUND CORROSION. REMOVED FINGER DOUBLER AND CORROSION IAW SRM 51-35-01 PAGE 1-13 VOL 2 AND SRM 51-21-01 PAR 34. PERF INSP IAW NDTSPM04 FOUND NOM THK.050", MIN .036" IS OUT OF LIMIT. TRIMMED OFF CORRODED WEB AREA IAW EA NR 8-5310-103736. REMOVED PARTS FOR ACCESS. REMOVED THE EXISTING REPAIR PANEL SECTION AND SPLICING, TRIMMED OUT SECTION OF THE P/N NCA6048-3 PANEL, FOUND OLD REPAIR ANGLE ON NC A6048-83 "T" AT STA 535 NOT PERFORMED FOR SRM 53-00-01 FIG 2 SHT 2 VOL 1. CUT OUT DAMAGED AREA IAW SRM 53-00-01 FIG 9. PERFORMED EA NR 8-5310-103736. FAB PART IAW DETAIL PART TRAVELER N01777/I026777 IAW EA NR 8-5310-103736. 2 L 7 3 4F A22WE 2007030800007 20070308 00007 WP 2007 3 8 07FDEA00602 1 20070227 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 FOUND LT AIR CONDITIONING COMPT, SEVERE CORROSION W/EXFOLIATION ON LONGERON FROM STA 560 TO STA 595 X= 28. REMOVED CORR OSION IAW SRM 53-10-00 FIG 4 SHT 1 (36 PERCENT). REMOVED FASTENERS ON SKIN, CUT AND REMOVED LONG IAW SRM 53-10-00 FIG 6 VOL 1 AT STA 595. REMOVED FASTENERS ON SKIN AND CLEANED AREA FOR ACCESS TO REINSTALL FASTENERS IS NECESSARY TO REMOVE OR CUT AN SECTION ON FRAME STA 588 IAW SRM 53-10-00 FIG 6 VOL1. REMOVED CORROSION (4.1%) IS IN LIMIT IAW SRM 53-00-01. REMOVED FRAME IAW SRM 51-33-01 VOL 2. REMOVED PARTS AND CUT FRAME IAW DWG ACA0050. INSTALLED NEW SECTION OF LONG NR 4 8 LT AND REINST FASTENERS ON FRAME IAW SRM 51-33-01 PAGE 34/47 VOL 2. STOP DRILLED ON CRACKED SKIN. FAB NEW DOUBLER AN 2 L 7 3 4F A22WE 2007030800010 20070308 00010 WP 2007 3 8 07FDEA00606 1 20070227 A 5310 DOOR FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 FOUND INTERNAL FUSELAGE AT STA 1250 TO STA 1257 LONGS NR 26 RT AND 27 RT DOOR JAMB FRAME EXISTING DOUBLER REPAIR. PERFO RMED INSPECT REPAIR IAW FEDEX EA NR 8-5350-105644 P1, INSTRUCTION 2. 2 L 7 3 4F A22WE 2007030800013 20070308 00013 NM 2007 3 8 07FDEA00632 1 20070303 A 5754 DUCT DOUG MD11 MD11 3023602 NM L/E SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RIGHT WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT FOUND CRACKED. (SUPPLEMENTAL 23 MARCH 07) CRACK AT RIGHT HAND WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57 -10-00 FIGURE 42 VOLUME I. REPAIR CLASSIFIED AS MAJ OR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007030800017 20070308 00017 NM 2007 3 8 07FDEA00636 1 20070303 A 5713 STRINGER DOUG MD11 MD11 3023602 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 CRACK FOUND AT STRINGER END 44L (XORS 523), APPROX 1" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. (SUPPLEMENTAL 23 MARCH 07) CRACK AT STRINGER END 44L (XORS 523) ON LEFT HAND WING TANK SLOTTED OUT AND REPAIRED WITH NEW REPAIR S PLICE AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007030800019 20070308 00019 NM 2007 3 8 07FDEA00638 1 20070304 A 5713 STRINGER DOUG MD11 MD11 3023602 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 CRACK FOUND AT STRINGER END 10R (XORS 760), APPROX. 13" LENGTH ON RIGHT WING TANK, DURING HFEC INSPECTION. (SUPPLEMENTA L 23 MARCH 07) CRACK AT STRINGER END 10R (XORS 760) ON RIGHT HAND WING TANK SLOTTED OUT AND ANGLE REPAIR CARRIED OUT A S PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007030800020 20070308 00020 NM 2007 3 8 07FDEA00518 1 20070217 A 3610 DUCT DOUG MD11 MD11F 3023600 NM A/C BAY DISCONNECTED A FDEA F ACTIVATE FIRE EXT. J WARNING INDICATION CR CRUISE 1 SO 25 606FE 48602 INTERMITTENT LEVEL 3 APU FIRE ALERT AFTER 150 EN ROUTE-SUSPECTED BLEED/DUCT LEAK-COMPLIED W/QRH, BOTTLE BLOWN. FOUND FL EX DUCT AT EXHAUST DISCONNECTED AND CLAMP MISSING, DUCT COMES FROM THE GEN COOLING SHROUD. RAN APU FOUND AIR LEAKING AT PRESS REG VALVE CLAMP, TIGHTENED CLAMP. RAN NR 2 ENG AND COULD HEAR A MASSIVE AIR LEAK RUMBLE, WITH ENG RUNNING SHUT D OWN APU AND FOUND AT THE FORWARD FIREWALL THE NR 2/APU MANIFOLD LEAKING AT THE CLAMP. TIGHTENED CLAMP AND AIR LEAK STOP PED. CLAMP WAS EXTREMELY LOOSE. ALL OTHER CLAMPS AND CONNECTIONS LEAK CHECK GOOD. SAFETIED THE FIRE BOTTLES ELE CONNE CTIONS AND SQUIBS. SYSTEM OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2007030800022 20070308 00022 NM 2007 3 8 HALA0700075 1 20070303 A 4920 APU BOEING 767 76733A 1385209 NM APU BAY SHUTDOWN A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 591HA 33423 ATB - APU AUTO SHUTDOWN CLIMBING THRU FL350, FAULT LIGHT ILL AND EICAS MESSAGE "APU FAULT" DISPLAYED. ACCOMPLISHED ECU BITE, FOUND "OVERSPEED" FAULT W/NO MINI FLAGS. ACCOMP FIM 49-11-00 FIG 111. CHECKED P2 SENSE LINES. NO DEFECTS NOTED. AS PER POWERPLANT ENG, REPLACED P2 SENSOR PER AMM 49-61-04. REPLACED FCU PER AMM 49-31-01. RERACKED ECU, GND RUN-UP AND LEAK FCU/P2 SENSOR OK. 2 L 7 2 4F RT A1NM 2007030800024 20070308 00024 NM 2007 3 8 HALA0700078 1 20070303 A 2722 3790011107 ACTUATOR BOEING 767 767300 1385204 NM RUDDER LEAKING A HALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 584HA 24258 RUDDER RATIO CHANGER ACTUATOR LEAKING FROM PISTON DYNAMIC SEAL. REPLACED RRCA PER AMM 27 21 42 024, TASK ALL TESTS AND LEAK CKS OK. 2 L 7 2 4F RT A1NM 2007030800026 20070308 00026 NM 2007 3 8 HALA0700069 1 20070227 A 3350 LIGHT BOEING 767 76733A 1385209 NM CABIN INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 589HA 33422 FOUND CEILING EMERGENCY LIGHT AT 28B INOP. RELAMPED, OPS NML. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007030800027 20070308 00027 NM 2007 3 8 HALA0700066 1 20070226 A 2421 745329 IDG BOEING 767 76733A 1385209 NM NR 2 MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, FOUND NR 2 ENGINE IDG DPI EXTENDED. FILTER INSP PER AMM 24-11-01-286-076, PARTICLES FOUND REQ UIRES IDG REPLACEMENT, NO OIL DISCOLOR, OR OVRHT, NO CHEMICAL CONTAMINATION. REMOVED AND REPLACED IDG ER AMM 24-11-01-4 04-002-004/001-004, TASK CARD 767-3-4250 01, 767-3-405001 LEAK, OPS CHECK OK. 2 L 7 2 4F RT A1NM 2007030800030 20070308 00030 NM 2007 3 8 HALA0700067 1 20070226 A 4960 233T3233212 CONTROL PANEL BOEING 767 767300 1385204 NM COCKPIT FAULTY A HALA K NONE O OTHER CR CRUISE 1 WP 13 584HA 32 32 24258 ETOPS SIGNIFICANT SYSTEM, APU DID NOT START ON VERIFICATION FLT. TROUBLE SHOT PER FIM 49-11-00. REPLACED APU CONTROL P ANEL PER 49-41-81-404-007. OPS CKS NORMAL. 2 L 7 2 4F RT A1NM 2007030800032 20070308 00032 WP 2007 3 8 IXXA07SMN006S 1 20070113 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2944 46065 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION FS172, LONGERON 35 RIGHT. REMOVED EXISTING REPAIR D OUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATE D REPAIR DOUBLER. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 51-3-1, DC8 SRM 51-3-0, DC8 S RM 51-1-21, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-11, SEMAN DRAWING NUMBER ED-4412 DATE 01-17-07 AND COMPLETED FAA FORM 8110-3 NUMBER 07019 DATED 01-18-07. 2 L 7 4 4F RT 4A25 2007030800033 20070308 00033 WP 2007 3 8 IXXA07SMN028S 1 20070113 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2944 46065 DURING ROUTINE C CHECK INSPECTION FOUND RIGHT HAND WING UPPER SKIN CRACKED AT STATION XRS105.000, STRINGER 14.REMOVED FA STENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND, AFT ER DAMAGE REMOVED. FABRICATED REPAIR PARTS. CLEANED TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYI NG SURFACES. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1 -8B, DC8 SRM 51-1-12, DC8 SRM 51-3-1 AND SEMAN DRAWING NUMBER ED-4408. COMPLETED FAA FORM 8110-3 NUMBER 07021 DATED 01/ 19/07. 2 L 7 4 4F RT 4A25 2007030800035 20070308 00035 WP 2007 3 8 IXXA07SMN025S 1 20070113 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2944 46065 DURING ROUTINE C CHECK INSPECTION, FOUND AN IMPROPER REPAIR AT STATION FS1694, LONGERON 27 RIGHT. REMOVED EXISTING REPA IR DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRI CATED REPAIR CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS DC8. INSTALLED REPAIR PARTS IAW DOUGLAS DRAWING SR085300 32, BOEING MESSAGE NUMBER 1-288540577-7, SEMAN DRAWING ED-4469 DATED 02-16-07, BOEING MESSAGE NUMBER 1-288540577-5 DATED 02-15-07, ATI ENGINEERING ORDER NUMBER 53-DC8-3729 DATED 02-05-07, AD-DC8-2007-02-02, SB-DC8-53A080, DC8 SRM 51-1-21, D C8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001 AND SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007030800037 20070308 00037 WP 2007 3 8 IXXA07SMN005S 1 20070113 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK, FOUND EXISTING REPAIR AT STATION FS174, LONGERON 34 RIGHT, DOES NOT MEET DTA REQUIREMENTS OF MDC 91K0262 REPORT. REMOVED EXISTING REPAIR REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND . AFTER DAMAGE REMOVAL. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 51-3-0, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-1 0-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-3-0, DC8 SRM 51-3-1 AND SEMAN DRAWING NUMBER ED-4412 DATED 01-17- 07. COMPLETED FAA FORM 8110-3 NUMBER 07019 DATED 01-18-07. 2 L 7 4 4F RT 4A25 2007030800041 20070308 00041 WP 2007 3 8 IXXA07SMN013S 1 20070113 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2944 46065 DURING ROUTINE C CHECK, FOUND AN IMPROPER REPAIR AT STATION FS 545, LONGERON 35 RIGHT. REMOVED EXISTING REPAIR. TRIMME D OUT DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATED REPAIR PA RTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IA W DC8 SRM 51-1-20D, DC8 SRM 51-1-21, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-3-1 AND SEMAN DRAWING NUMBER ED-4417 DATED 01-11-07. COMPLETED FAA FORM 8110-3 NUMBER 07012 DATED 01-15-07. 2 L 7 4 4F RT 4A25 2007030800042 20070308 00042 WP 2007 3 8 IXXA07SMN012S 1 20070113 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2944 46065 DURING ROUTINE C CHECK, FOUND EXISTING REPAIR IS IMPROPER AT STATION FS 403, LONGERON 35 LEFT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATED REPAI R PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PART S IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 51-1-20D, DC8 NDT SPM PART 06-10-01-001,DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-3-1 AND SEMAN DRAWING NUMBER ED-4416 DATED 01-15-07, FAA FORM 8110-3 NUMBER 07012 DATED 01-15-07. 2 L 7 4 4F RT 4A25 2007030800043 20070308 00043 WP 2007 3 8 IXXA07SMN018S 1 20070113 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND AN IMPROPER REPAIR AT FS 1282, LONGERON 35 RIGHT. REMOVED EXISTING REPAIR DOUB LER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATED R EPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS FROM STATION FS1265.000 TO STATION FS1282.000 IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-1-20D, DC8 NDT SPM P ART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-3-1 AND SEMAN DRAWING NUMBER ED-4418 DATED 01-12-07. FAA FORM 8110-3 NUMBER 07012 DATED 01-15-07. 2 L 7 4 4F RT 4A25 2007030800044 20070308 00044 WP 2007 3 8 IXXA07SMN023S 1 20070113 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND AN IMPROPER REPAIR AT STATION FS 1682, LONGERON 35 RIGHT. REMOVED EXISTING IMP ROPER REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND DAMAGE REMOVED. FABRICATE D REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-3-1 AND SEMAN DRAWING NUMBER ED-4442 DATED 01-25-07. COMPLETED FAA FORM 8110-3 NUMBER 07031 DATED 01-26-07. 2 L 7 4 4F RT 4A25 2007030800045 20070308 00045 WP 2007 3 8 IXXA07SMN032S 1 20070119 A 5753 SKIN DOUG DC8 DC871F 302199D WP T/E FLAP MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND A NON STANDARD REPAIR ON THE LEFT OUTBOARD FLAP FROM STATION XF169.000 TO STATI ON XF174.000. REMOVED EXISTING SKIN PANEL WITH NON STANDARD REPAIR. FABRICATED NEW SKIN PANEL AND BONDED DOUBLER. BON DED BOTH PARTS WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN PANEL INTERNAL SURFACE. APPLIED SEALANT TO FA YING SURFACES. INSTALLED NEW SKIN PANEL IAW DC8 SRM 51-1-21, DC8 SRM 57-7-1 FIGURE 4 TR NUMBER 57-94 DATED 10-01-02, DC 8 SRM 57-1-0 PAGE 1, DC8 SRM 57-7-1 FIGURE 4 ITEMS "P" AND "Q", DC8 SRM 51-1-9, DC8 SRM 51-1-8B AND DC8 SRM 51-1-11. 2 L 7 4 4F RT 4A25 2007030800046 20070308 00046 WP 2007 3 8 IXXA07SMN015S 1 20070113 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND EXISTING REPAIR AT STATION FS 1143, LONGERON 35 RIGHT, DOES NOT MEET THE DTA RE QUIREMENTS OF MDC 91K0262 REPORT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, T REATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 51-3-1 , DC8 SRM 53-2-1 FIGURE 7 SHEET 1 AND 3,DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 53-4-1 FIGURE 16 ITEM D, DC8 SRM 51-1 -8B AND DC8 SRM 51-1-11. 2 L 7 4 4F RT 4A25 2007030800047 20070308 00047 WP 2007 3 8 IXXA07SMN003S 1 20070113 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND EXISTING REPAIR AT STATION FS 76, LONGERON 35 RIGHT, DOES NOT MEET THE DTA REQU IREMENTS OF MDC 91K0262 REPORT. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVAL. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR P ARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 NDT SPM PA RT 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND DC8 SRM 51-3-1. SEMAN DRAWING NUMBER ED-4411 DATED 01-11-07. COM PLETED FAA FORM 8110-3, NUMBER 07012, DATED 01-15-07. 2 L 7 4 4F RT 4A25 2007030800048 20070308 00048 WP 2007 3 8 IXXA07SMN007S 1 20070113 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK, FOUND AN IMPROPER REPAIR REPAIR AT STATION FS 222.000, LONGERON 35 RIGHT. REMOVED EXISTING REPA IR DOUBLER. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIE D SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-1 FIGURE 7 SHEET 1 AND 3, DC8 SRM 51-1-21, DC8 SR M 51-1-20D, DC8 SRM 53-4-1 FIGURE 1 ITEM "B", DC8 SRM 51-9-0 FIGURE 68A, DC8 SRM 51-1-8B, DC8 SRM 51-1-11 AND DC8 SRM 51 -3-1. 2 L 7 4 4F RT 4A25 2007030800049 20070308 00049 WP 2007 3 8 IXXA07SMN009S 1 20070113 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND AN IMPROPER REPAIR AT FS 330, LONGERON 30 RIGHT. REMOVED EXISTING REPAIR. PER FORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVAL. FABRICATED REPAIR PARTS. CLEANED, TREATED AN D PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-21, DC8 SR M 51-1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-3-1. AD 2005-18-07, BOEING MESSA GE NR 1-274569452-5 DATED 01-17-07 BOEING MESSAGE NR 1-290998891-2 AND SEMAN DRAWING ED-4414-1 DATED 01-17-07. COMPLETE D FAA FORM 8100-9 DATED 02-17-07. 2 L 7 4 4F RT 4A25 2007030800051 20070308 00051 WP 2007 3 8 IXXA07SMN030S 1 20070113 A 5753 SKIN DOUG DC8 DC871F 302199D WP T/E FLAP MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 46065 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING OUTBOARD FLAP HAS A NON STANDARD REPAIR ON UPPER SURFACE FROM STATION XF216.000 TO STATION XF220.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION . NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATED NEW SKIN AND REPAIR PARTS. CLEANED, TREATED AND PRIME D AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN AND REPAIR PARTS IAW DC8 SRM 51-3-0, D C8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-1 AND SE MAN DRAWING, NUMBER ED-4409 DATED 01-13-07. 2 L 7 4 4F RT 4A25 2007030800052 20070308 00052 WP 2007 3 8 IXXA07SMN001S 1 20070113 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND AN IMPROPER REPAIR AT STATION FS 280 LONGERON 30 REMOVED EXISTING REPAIR. PERF ORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND, AFTER DAMAGE REMOVED. FABRICATED REPAIR PARTS. CLEANED, TREATED A ND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAWDC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01 -001, DC8 SRM 51-1-8B, DC8 SRM 51-3-1, AD 2005-18-07, BOEING MESSAGE NUMBER 1-274569452-5 DATED 01-17-07, BOEING MESSAGE NUMBER 1-290998891-2 DATED 01-17-07, SEMAN DRAWING NUMBER ED-4414 DATED 01-17-07 AND ATI ENGINEERING ORDER 53-DC8-2452. COMPLETED FAA FORM 8110-9 DATED 02-17-07. 2 L 7 4 4F RT 4A25 2007030800053 20070308 00053 WP 2007 3 8 IXXA07SMN022S 1 20070113 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND INTERIM REPAIR AT FS 1542, LONGERON 35 LEFT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVAL. FABRICATED EXTERNAL REPAI R DOUBLER AND INTERNAL FINGER DOUBLER. CLEANED TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SUR FACES. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-3-1 AND SEMAN DRAWING NUMBER ED-4419 DATED 01-19-07. COMPLETED FAA FORM 8110- 3 NUMBER 07026 DATED 01-22-07. 2 L 7 4 4F RT 4A25 2007030800054 20070308 00054 WP 2007 3 8 IXXA07SMN014S 1 20070113 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND INTERIM REPAIR AT STATION FS 518, LONGERON 31 RIGHT. REMOVED EXISTING REPAIR P ERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. FABRICATED REPAIR PARTS CLEANED, TREATED AND PRIMED AREA AND RE PAIR PARTS. INSTALLED REPAIR PARTS IAW DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-21, DC8 SRM 51-1-20 D, DC8 SRM 51-3-0, DC8 SRM 51-3-1, SERVICE BULLETIN DC8-53-078, AD-2005-18-07 BOEING MESSAGES NUMBER 1-274569706-5, 1-27 4569706-7 DATED 01-17-07 AND SEMAN DRAWING ED-4422-1 DATED 02-05-07. COMPLETED FAA FORM 8110-9 DATED 02-05-07. 2 L 7 4 4F RT 4A25 2007030800055 20070308 00055 WP 2007 3 8 IXXA07SMN017S 1 20070113 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND AN IMPROPER REPAIR AT STATION FS1265, LONGERON 35 RIGHT. REMOVED EXISTING REPA IR DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRI CATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS FROM STATION FS1265.000 TO STATION FS1282.000, LONGERON 35 RIGHT IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 S RM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-3-1 AND SEMAN DRAWING NUMBER ED -4418 DATED 01-12-07. COMPLETED FAA FORM 8110-3 NUMBER 07012 DATED 01-15-07. 2 L 7 4 4F RT 4A25 2007030800062 20070308 00062 WP 2007 3 8 IXXA07SMN037S 1 20070119 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2944 46065 DURING ROUTINE C CHECK INSPECTION, FOUND AN IMPROPER REPAIR AT STATION FS 1692, LONGERON 36. REMOVED EXISTING REPAIR DO UBLER. FABRICATED REPAIR PARTS. CLEANED TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, DC8 SRM 53-2-1 FIGURE 7 SHEETS 1, 4 AND, 5DC8 SRM 51-1-21, DC8 SRM 53-5-1 FIGURE 1 PAGE 2 ITEM "E" AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007030800063 20070308 00063 WP 2007 3 8 IXXA070009S 1 20070223 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING-EXTERNAL UPPER SKIN CRACKED AT STATION XRS74.000 STRINGER 12. REMOVE D FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATED REPAIR DOUBLER AND FILLERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPL IED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW DC8 SRM 57-2-1 FIGURE 10 SHEET 3, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 57-3-1 FIGURE 10 PAGE 17 ITEM "A", DC8 SRM 51-10-0, FIGURE 1 SHEET 6, D C8 SRM 51-1-8B, DC8 SRM 51-1-12 AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007030800065 20070308 00065 WP 2007 3 8 IXXA07SMN038S 1 20070119 A 5330 PN564932975N1 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2944 46065 DURING ROUTINE C CHECK INSPECTION, FOUND AN IMPROPER REPAIR AT STATION FS 1696, LONGERON 36. REMOVED EXISTING SKIN WITH IMPROPER REPAIR. CLEANED TREATED AND PRIMED AREA. TREATED AND PRIMED NEW SKIN PLATING. APPLIED SEALANT TO FAYING SUR FACE. INSTALLED NEW SKIN PLATING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, DC8 SRM 53-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 53-5-1 FIGURE 1 ITEM "E", DC8 SRM DC8 51-1-11 AND BOEING MESSAGE NUMBER 1-271850875-2 DATED 01-10-07. 2 L 7 4 4F RT 4A25 2007030800066 20070308 00066 EU 2007 3 8 MALA070028 1 20070214 A 3350 74331 LIGHT SAAB SF340 340B 7860101 EU CABIN BROKEN A MALA K NONE O OTHER UK UNKNOWN 1 GL 15 415XJ 340B415 FOUND EMERGENCY LIGHT STRIP BROKE AND INOP. REPLACED LIGHT ASSEMBLY, P/N 7433-1. 2 L 7 2 4T RT A52EU 2007030600041 20070306 00041 NM 2007 3 6 SWAA071133 1 20070227 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 793, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007030600043 20070306 00043 NM 2007 3 6 SWAA071137 1 20070227 A 5210 6545871 SKIN BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED SPV CHECK, FOUND R1 DOOR SKIN CRACKED AT BS 316, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007030600054 20070306 00054 NM 2007 3 6 SWAA071165 1 20070301 A 5754 65C26602 SKIN BOEING 737 7373H4 1384600 NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED C2 CHECK, FOUND RIGHT WING NR 4 L/E SLAT LOWER T/E SKIN CRACKED. REPAIRED SLAT PER SWA EA. 2 L 7 2 4F RT A16WE 2007030600062 20070306 00062 NM 2007 3 6 AMTA200700091 1 20070217 A 5551 PIN BOEING 737 73783N 13844HI NM HORIZ STAB CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 323TZ 30033 LT STAB LOWER AFT STAB PIN CORRODED. REMOVED AND REPLACED 180A1612-4 IAW EO 737-55AD-2935 REV B. (K) 2 L 7 2 4F RT A16WE 2007030600063 20070306 00063 NM 2007 3 6 AMTA200700068 1 20070214 A 5321 FLOOR PANEL BOEING 737 73783N 13844HI NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 323TZ 30033 FWD CARGO COMPARTMENT FLOOR PANEL 120AF CORRODED THE LENGTH OF THE THRESHOLD, STA 440-490, RBL 22. REMOVED CORROSION ON FWD CARGO FLOOR PANEL 120AF. ORIG MAT THK IS .073 MAT LOSS .002. FOUND TO BE WITHIN LIMITS IAW SRM. (K) 2 L 7 2 4F RT A16WE 2007030600071 20070306 00071 NM 2007 3 6 AMTA200700060 1 20070206 A 3350 D71702001 POWER SUPPLY BOEING 737 73783N 13844HI NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 315TZ 28245 RT OVERWING EXCAPE GROUND ILLUMINATION LIGHT AND AFT OVERWING ESCAPE LIGHT INOPERATIVE. REMOVED AND REPLACED PWR SUPPLY IAW MM, OPS CHECK NORMAL. (K) 2 L 7 2 4F RT A16WE 2007030600074 20070306 00074 NM 2007 3 6 AMTA200700107 1 20070221 A 2560 GIRT BAR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE L4 DOOR LACK OF LUBE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 518AT 27974 ON DISARMING DOOR 4L, FOUND TUBE STIFF DIFFICULT TO MOVE. CLEANTED AND LUBED GIRT BAR AS REQUIRED, NO DEFECTS NOTED. O K FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007030600082 20070306 00082 NM 2007 3 6 AMTA200700098 1 20070218 A 2560 LIGHT BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE EVAC SLIDE INOPERATIVE A AMTA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 11 519AT 27975 GIRT BAR ENGAGE LGT EXTN WITH EVACUATION SLIDE ARMING LEVER IN ARMED POS AT ENTRY DOOR DR 4L. RELAMPED SLIDE LIGHT OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007030600096 20070306 00096 NM 2007 3 6 2007UALA00626 1 20070301 A 5320 ATTACH FITTING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 122UA 29168 FOUND GUIDE MOUNT ATTACHMENT AT TORQUE BOX HAS DAMAGE TO THE PRIMARY STRUCTURE. UPON REMOVAL OF FLOOR BOARD FOR FLOOR M OUNT CENTER GUIDE INSTALLATION, FOUND DAMAGE AREA JUST AFT OF THE CENTER GUIDE MOUNT BOLTS, STA 1800 CENTER LINE BEAM. REMOVED DAMAGED MOUNT ASSY & MFGED REPAIR PARTS FOR DAMAGED WEB. ASSEMBLED MOUNT & INSTALLED 2 EA. CENTER GUIDES. A/C R EADY FOR RETURN TO SERVICE. SUSPECT DMG CAUSED BY LD3 IMPACT ON FLOOR FITTING. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030600106 20070306 00106 2007 3 6 DL76G070169 4 20070227 A 3497 WIRE BOEING 767 767332 1382001 NM COCKPIT SHORTED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 173DZ 29692 RTB DUE TO NO DATA FROM LEFT IRU. FOUND W161-9009B-22 SHORTED TO SHIELD AT D4769P. REPLACED WIRE IRUS FMC TCAS, ALL CK NORMAL. 2 L 7 2 4F RT A1NM 2007030600107 20070306 00107 2007 3 6 DLM90070170 4 20070226 A 2565 BOTTLE 100505201 DOUG MD90 MD9030 3023690 NM EVAC SLIDE DISCHARGED A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 908DA D9A011 53388 FLIGHT ATTENDANT WAS ARMING SLIDE AT POSITION 2E WHEN HEARD A LOUD HISSING SOUND (NOT INTENTIONAL). THE BOTTLE DEPLETED BUT THE SLIDE DID NOT INFLATE AT ALL. THE AMT'S OPENED THE PARACHUTE PINS TO INSPECT THE SLIDE PACK AND SUSPECT TH AT THE DEFLATION VALVE WAS PARTIALY OPENED, P/N 100505-201 S/N D9A011 ROUTED TO REPAIR SUPPLIER USING REPAIR PO 48000286 00. SLIDE WAS REPLACED ON THE A/C. 2 L 7 2 4F RT A6WE 2007030600108 20070306 00108 NM 2007 3 6 DL757070172 1 20070228 A 5330 148N32145 SKIN BOEING 757 757232 1384965 NM FUSELAGE PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 DENT AND PUNCTURE IN THE FUSELAGE SKIN AT STA 1720-1770, STR27L-27R. REMOVED AND REPLACED DAMAGED SKINS AND STRINGERS. FRAMES AND STA 1720 BULKHEAD REPAIRED PER SRM. REMOVED AND REPLACED PARTS PREVIOUSLY REPAIRED PER 221765-14. 2 L 7 2 4F RT A2NM 2007030600109 20070306 00109 NM 2007 3 6 DU4R2007070 1 20070215 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM FUSELAGE CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 6706Q 30422 FOUND CORROSION ON TOP CENTER OF AFT CABIN FLOORBEAM AT FS 1640. REPAIRED BY CUTTING OUT CORRODED AREA OF UPPER CAP IA W B757 SRM 53-00-51D FIG 206. FABRICATED AND INSTALLED REPAIR PARTS 28” FROM BAC1505-100617, 7.5 FROM BAC1490-2738, DOU BLER 7.5 FROM 7075-T6 .050, 4.0” FROM 7075-T6 .125, 6.0 FROM 7075-T6 .090, 6.0 FROM 7075-T6 .063 IAW B757 SRM 53-60-51- 2-205D, 51-40-02, 53-60-51 AND 51-40-03. 2 L 7 2 4F RT A2NM 2007030600110 20070306 00110 NM 2007 3 6 DL764070150 1 20070223 A 2933 INDICATION SYS BOEING 767 767432ER 1385134 NM HYDRAULIC SYS MALFUNCTIONED A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 825MH 29696 DURING TAXI FOR T/O, EICAS MESSAGE RT HYD QTY ON STATUS PAGE. RT HYD SYS IND 1.02. FWD TO MCO AND PLACARD PER MEL 29-33 -02. PERFORM REP CK RT HYD QTY CKS FULL, NO MSGS AND NO DISCREPANCIES NOTED RT HYD QTY SYS NORMAL MCO/PLAC REMOVED. 2 L 7 2 4F RT A1NM 2007030700018 20070307 00018 NM 2007 3 7 ASAA0741495 1 20070227 A 5753 SKIN BOEING 737 7374Q8 138447Q NM T/E FLAP PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 RIGHT O/B AFT FLAP LOWER SURFACE IS PUNCTURED. REMOVED DAMAGED SECTION FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-40-10. 2 L 7 2 4F RT A16WE 2007030700022 20070307 00022 NM 2007 3 7 ASAA0741499 1 20070227 A 5755 SKIN BOEING 737 7374Q8 138447Q NM NR 4 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 LWR SURFACE OF NR 4 GROUND SPOILER HAS MULITPLE DENTS. PREPPED DENTED AREAS, FABRICATED AND INSTALLED REPAIR DOUBLERS I AW SRM 51-70-10 REPAIR 2. 2 L 7 2 4F RT A16WE 2007030700059 20070307 00059 NM 2007 3 7 SWAA071203 1 20070303 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 973, STR 5R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007030700068 20070307 00068 NM 2007 3 7 SWAA071188 1 20070302 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030700071 20070307 00071 NM 2007 3 7 SWAA071187 1 20070302 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030700080 20070307 00080 NM 2007 3 7 SWAA071190 1 20070302 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 908, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030700082 20070307 00082 NM 2007 3 7 SWAA071208 1 20070303 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER 17R CRACKED AT BS 810.5. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007030700088 20070307 00088 NM 2007 3 7 SWAA071234 1 20070305 A 3350 65C27093 LIGHT BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 682SW 23496 L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007030700094 20070307 00094 NM 2007 3 7 SWAA071219 1 20070303 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030700097 20070307 00097 NM 2007 3 7 SWAA071232 1 20070305 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030700111 20070307 00111 NM 2007 3 7 SWAA071215 1 20070303 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 294, STR 10L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007030700112 20070307 00112 NM 2007 3 7 SWAA071221 1 20070303 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 10L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007030700113 20070307 00113 NM 2007 3 7 SWAA071230 1 20070305 A 5322 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 28L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007030700135 20070307 00135 NM 2007 3 7 07FDEA00628 1 20070302 A 5340 654531315 STRINGER CLIP BOEING 727 727225 1384077 NM BS 540 S1L DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FOUND MAIN CABIN STRINGER CLIP DAMAGED AT FS 540 STR 1. REPLACED STRINGER CLIP REF SRM 51-30-2 AND SRM 51-30-5. CLASSI FIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007030700216 20070307 00216 NM 2007 3 7 DLM88070179 1 20070301 A 5511 SPAR CAP DOUG MD88 MD88 3023688 NM HORIZ STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948DL 49879 HORIZONTAL STABILIZER/LT/UPPER AFT SKIN AND REAR SPAR : CRACK REPAIR. THE UPPER AFT SKIN PANEL OF THE LT HORIZ STAB WAS FOUND WITH A 1.85" LONG CRACK NEAR THE INBD AFT EDGE OF THE PANEL. UPON REMOVAL OF THE CRACKED PANEL, THE UPPER SPAR C AP WAS FOUND WITH A 5/8" CRACK NEAR THE INBD END IN THE VERTICAL FLANGE OF THE CAP. BOTH THE SKIN AND SPAR CAP ARE B EING REPLACED PER OEM DRAWINGS AND DOCUMENTED PER ER/A 460237-14. 2 L 7 2 4F RT A6WE 2007030700217 20070307 00217 NM 2007 3 7 DL757070180 1 20070106 A 5330 141N382118 SKIN BOEING 757 757232 1384965 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 690DL 27585 THE FUSELAGE SKIN AT STA 265 TO 297 AND RBL 30-60 HAD DENTS IN 8 LOCATIONS. SOME DENTS WERE CUT OUT AND A DOUBLER INSTA LLED AND SOME DENTS WERE WITHIN ALLOWABLE LIMITS. 2 L 7 2 4F RT A2NM 2007030700252 20070307 00252 WP 2007 3 7 07FDEA00592 1 20070227 A 5511 SPAR CAP DOUG DC10 DC1030 3023501 WP HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 DURING HFEC INSP, ON LT HORIZONTAL STAB, AFT SPAR CAP, FOUND CRACK, ON UPPER SURFACE AND INNER SURFACE OF ONE BARREL NUT . RETAINER IS INSTALLED IN BARREL NUT HOLE. REMOVE FOR TOTAL CRACK LONGEST. REMOVED L/E CTR SECTION HORIZ STAB IAW MM 55-10-02. REMOVED ACCESS DOOR 331AZ IAW MM 6-33-00 AND REMOVED I/B ELEVATOR AND ATTACHING PARTS IAW MM 27-30-01. REMO VED AND DISCONNECTED HYD PIPES LINE ALK7009-596/614/556 AND CUT ALK7014-501 IAW MM 20-10-01-2. REPLACE CAP ALC7472-1 IAW SRM 51-33-01 AND 51-35-01 VOL 2 AND DWG ALC7463. REPLACED ALL PARTS DAMAGED AND CLOSED AREA IAW SB DC10-55-18. ACC OMPLISHED EA NR 8-5510-103679. 2 L 7 3 4F A22WE 2007030700253 20070307 00253 WP 2007 3 7 07FDEA00593 1 20070227 A 5512 SKIN DOUG DC10 DC1030F 3023504 WP HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 LT HORIZ STAB OUTER SECTION UPPER AFT SKIN PANEL FOUND 1 CRACK 2, 5" LONG. REPAIRED CRACKED SKIN PANEL IAW SB 55-18 AND EA NR 8-5510-103679. WORKED IN CONJUNCTION WITH NRC N00898/I030898. 2 L 7 3 4F RT A22WE 2007030800003 20070308 00003 WP 2007 3 8 07FDEA00597 1 20070227 A 5720 STRINGER DOUG DC10 DC1010 3022110 WP WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 FOUND LT AND RT WING STRINGER NR 8 FUEL COMPENSATOR FASTENER HOLES OF THE ARB0903 DOUBLER, EXISTING REPAIRS. FOR SUSPEC T CRACK STRIP PAINT AREA WITH CHEMICAL METHOD FOR PERFORMED PENETRANT INSP STRIPPED PAINT IAW SRM 51-21-01 PAGE 26 VOL 2 . PERFORMED INSP IAW NDTSPM 08 ON EDGE AND SURFACE OF STR NR 8 LT AND RT WING, NO CRACK FOUND. INSPECTED STRINGER NR 8 LT AND RT IAW FEDEX EA NR 8-5720-103624, NO CRACK FOUND. 2 L 7 3 4F A22WE 2007030800004 20070308 00004 WP 2007 3 8 07FDEA00598 1 20070227 A 5310 DOOR FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 FOUND AFT LOWER CARGO COMPT FWD JAMB DOOR FRAME, EXISTING REPAIR AT STA 1781 LONG NR 40 TO 42 LT. REMOVED 2 PLATE CONTA INER GUIDE AND 2 SUPPORT LINING SUPPORT AND WEB COVER IAW SRM 51-30-00 VOL 2. PERFORMED GVI, FOUND IN COMPLIANCE WITH C RITERIA REQUEST BY EO NR 8-5100-7-5001 P2. ACCOMPLISHED FEDEX EA NR 8-5350-105644 PART 1 INSTRUCTION 1. REINSTALLED RE MOVED PART IAW SRM 51-30-00 VOL 2. 2 L 7 3 4F A22WE 2007030800011 20070308 00011 WP 2007 3 8 07FDEA00607 1 20070227 A 5310 DOOR FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 FOUND INTERNAL FUSELAGE AFT MAIN CABIN AT STA 1306 TO STA 1317 LONGS NR 26 RT AND 27 RT DOOR JAMB FRAME EXISTING DOUBLER REPAIR. PERFORMED INSPECT REPAIR IAW FEDEX EA NR 8-5350-105644 P1, INSTRUCTION 3. 2 L 7 3 4F A22WE 2007030800012 20070308 00012 WP 2007 3 8 07FDEA00630 1 20070302 A 5230 FITTING DOUG DC10 DC1010 3022110 WP CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 MAIN CARGO DOOR LOWER DOOR FITTINGS (SPOOLS) HAVE EVIDENCE OF CORROSION AT SERRATED PLATE ATTACH POINTS. (04 APRIL 07) REQUIRE REMOVAL FOR FURTHER INSPECTION ,ALL 7 SPOOL FITTINGS. FOUND SPOOLS 1-7 WITH CRACK INDICATIONS, AND A CRACK IN NR 7 LOWER LATCH SUPPORT FITTING BELOW WEB. REMOVED AND REPLACED NR 1-7 SPOOL FITTINGS IAW DC10-10 SRM 51-33-01. REAMED ATTACH HOLES IN NR 7 JAMB BEAM TO REMOVE CRACK, VERIFIED CRACK REMOVAL IAW NDT SPM 06-10-01.003, NO CRACK INDICATION. INSTALLED REPAIR BUSHINGS PER SRM 53-50-00 VOL I, 51-39-01 VOL II P4. RIGGED AND OPS CHECKED MCD IAW DC 10-10 AMM 52-34 -00-5. OPS CHECK GOOD. 2 L 7 3 4F A22WE 2007030800016 20070308 00016 NM 2007 3 8 07FDEA00635 1 20070303 A 5713 STRINGER DOUG MD11 MD11 3023602 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 CRACK FOUND AT STRINGER END 14L (XORS 521), APPROX 13" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. CRACK AT STRING ER END 14L (XORS 521) ON LEFT HAND WING TANK TRIMMED OUT AND REPAIRED WITH SPLICE REPAIR AS PER SRM 57-20-00 FIGURE 10 V OLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007030800021 20070308 00021 2007 3 8 HALA0700077 4 20070303 A 2565 RELAY BOEING 767 767332 1382001 NM EVAC SLIDE UNKNOWN A HALA K NONE L NO TEST NR NOT REPORTED 1 WP 13 596HA 23276 DURING SQUIB TEST 1 LEFT EMER ESCAPE SLIDE INDICATOR LGT REMAINED EXTINGUISHED. DEAMRED LT/RT OVERWING SLIDES PER AMM 2 5-65-60, REPLACED LEFT DOOR SLIDE RELAYS K1 AND K3 ON M1135 MODULE. REPLACED BATTERIES FOR M961 AND M962. SQUIB TEST G OOD PER AMM 25-65-00, ARMED LT/RT OVERWING SLIDES SYSTEM PER 25-65-00 TEST OKAY. 2 L 7 2 4F RT A1NM 2007030800028 20070308 00028 NM 2007 3 8 HALA0700070 1 20070226 A 5414 ACCESS DOOR BOEING 767 767332 1382001 NM NR 1 PYLON MISSING A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 NR 1 ENG PYLON NACELLE STRUT ACCESS DOOR MISSING (I/B). INSTALLED ACCESS DOOR IN NR 1 ENG PYLON NACELLE STRUT SEC, CK O K. 2 L 7 2 4F RT A1NM 2007030800031 20070308 00031 WP 2007 3 8 IXXA07SMN020S 1 20070113 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK, FOUND AN IMPROPER REPAIR AT STATION FS 1384, LONGERON 35 RIGHT. REMOVED EXISTING REPAIR. REMOV ED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYIN G SURFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-1 FIGURE 7 SHEET 1 AND 3, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SR M 53-4-1 FIGURE 16 SHEET 2 ITEM "B", DC8 SRM 51-9-0 FIGURE 68A, DC8 SRM 51-1-8B, DC8 SRM 51-1-11 AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007030800050 20070308 00050 WP 2007 3 8 IXXA07SMN051S 1 20070131 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND AN IMPROPER REPAIR AT STATION FS367, LONGERON 20 LEFT. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-1 FIGURE 7 SHEET 1, 4 AND 5, DC8 SRM 51-1-21, DC8 S RM 51-1-20D, DC8 SRM 53-4-1 FIGURE 6 ITEM "B", DC8 SRM 51-9-0 FIGURE 68A, DC8 SRM 51-1-8B, DC8 SRM 51-1-11 AND DC8 SRM 5 1-3-1. 2 L 7 4 4F RT 4A25 2007030800067 20070308 00067 WP 2007 3 8 NACA20070007 1 20070214 A 3230 2248988 BUNGEE DOUG DC6 DC6A 3021706 WP LT MLG BROKEN A NACA O OTHER N FALSE WARNING LD LANDING 1 AL 03 6174C 44075 LEFT MAIN GEAR LIGHT DID NOT ILLUMINATE ON LANDING. RED TRANSIT LIGHT WAS ON. MADE VISUAL INSPECTION FROM CAPTAINS WIN DOW AND A LOW PASS FOR MAINTENANCE TO INSPECT. FOUND INBD BUNGEE/SPRING BROKEN, REPLACED. LMLG DOOR SLIDER ROD BENT, R EPLACED ROD AND RIGGED. REF: DOUGLAS MM CH 26-9-3. OP CHECKED GOOD. 2 L 7 4 4R 6A3 2007030800068 20070308 00068 NE 2007 3 8 NACA20070008 2 20070228 A 7420 10884251 HARNESS PWA CB3 DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 2 ENGINE CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 2907F 1570 1570 31026 533265 31026 NR 2 ENGINE SHUT DOWN, WOULD NOT TAKE A LEAN AND BACKFIRES IN RICH. FOUND CRACKED IGNITION HARNESS. REPLACED HARNESS R EF: PURDUE MB 24-1-1. DISTRIBUTOR REPLACED IN REF: PW 2800MM CH 6 1/2. LEAK AND OP CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2007030800070 20070308 00070 EU 2007 3 8 NSVA20070013 1 20070117 A 3350 BATTERY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 294CJ 294 FOUND FWD CABIN EMERGENCY LIGHTS INOP. RECHARGED BATTERY 21LN W/GPU,OPS CHK GOOD IAW SMM 33-50-00. 2 L 7 2 4T RT A52EU 2007030800071 20070308 00071 EU 2007 3 8 NSVA20070014 1 20070118 A 6123 AUTOCOARSEN SYS SAAB SF340 340B 7860101 EU MALFUNCTIONED A NSVA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 339CJ 339 AUTO COARSEN LIGHT ILLUMINATED ON TAKEOFF ROLL. RETURNED TO GATE AND PERFORMED AN OP'S TEST OF SYSTEM IAW AUTO COURZEN P3 TEST, AS PER MX CONTROL. SYSTEM OPERATES NORMAL. 2 L 7 2 4T RT A52EU 2007030800073 20070308 00073 CE 2007 3 8 NSVA20070016 1 20070122 A 7920 LINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE OIL SYSTEM LEAKING A NSVA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 171CJ UE71 FOUND SMOKE IN CABIN DURING FLIGHT. SMOKE DISSIPATED BEFORE LANDING. MAINTENANCE FOUND LEAKING OIL COOLER HOSE ON THE LT ENGINE, A SMALL AMOUNT OF OIL MIGRATED INTO THE ENVIRONMENTAL SYSTEM THAT CAUSED THE CABIN SMOKE. THE OIL LINES WERE REPLACED AND IT TOOK A FEW ENGINE RUNS TO BURN THE RESIDUAL OIL FROM THE ENVIRONMENTAL SYSTEM. 2 L 7 2 4T 4 T RT A24CE E26NE 2007030800077 20070308 00077 EU 2007 3 8 NSVA20070041 1 20070218 A 2913 4018502 PUMP SAAB SF340 340B 7860101 EU HYDRAULIC SYS INTERMITTENT A NSVA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 193CJ 193 HYDRAULIC LIGHT CAME ON ON TAXI INOP IN AUTO AND MANUAL MODE THEN WORKED LATER. HYD PUMP WAS FOUND TO WORK INTERMITTENT LY AND OPERATION WAS WEAK. REMOVED AND REPLACED HYD PUMP IAW CWC 29-10-07S AND OPS CHECK GOOD IAW 29-10-10-04 PN 40185- 02 SN OFF EQ21 SN ON ID72. 2 L 7 2 4T RT A52EU 2007030800080 20070308 00080 EU 2007 3 8 NSVA20070031 1 20070207 A 3234 D49412002 CONTROL HANDLE SAAB SF340 340B 7860101 EU COCKPIT FAULTY A NSVA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 350CJ 350 FOUND LANDING GEAR FAILED TO RETRACT. REPLACED LANDING GEAR CONTROL HANDLE IAW MM 32-31-05. OPS CHECK GOOD, PN ON D494 -12-001, SN ON 2150788, PN OFF D494-12-002, SN OFF 3030590. 2 L 7 2 4T RT A52EU 2007030800081 20070308 00081 CE 2007 3 8 NSVA20070034 1 20070209 A 3234 1013880083 SELECTOR VALVE BEECH 1900 1900D 1154162 CE LANDING GEAR MALFUNCTIONED A NSVA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 27 155CJ UE55 FOUND LANDING GEAR CIRCUIT BREAKER POPPED ON GEAR RETRACTION, UPON EXTENSION BREAKER POPPED AGAIN BEFORE NOSE SHOWED DOW N AND LOCKED. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE PN ON/OFF 101-388008-3, SN ON 1886, SN OFF 1825 IAW B-19 00MM CHAPTER 32-30-00-201 LEAK AND OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 2007030800084 20070308 00084 NM 2007 3 8 NWAA070715808 1 20070304 A 3350 POWER SUPPLY BOEING 757 757351 1384991 NM CABIN SHORTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 588NW 32988 FLIGHT ATTENDANTS REPORTED EMERGENCY EXIT LIGHT TURNING ON AND OFF WITH SWITCHES IN NORMAL POSITION. REMOVED AND REPLAC ED FIRST CLASS POWER SUPPLY. REPLACED COCKPIT TOGGLE SWITCH FOR EMERGENCY LIGHTS NO HELP. FIRST CLASS AND CABIN EMERGE NCY LIGHTS WORKING OPPOSED EACH OTHER IN THE ARM POSITION CABIN LIGHT ON, FIRST CLASS OFF. UPON FURTHER TROUBLESHOOTING FOUND POWER SUPPLY M11612 BATTERY PACK LEAKING AND POWER SUPPLY SHORTED. REMOVED AND REPLACED M11612 POWER SUPPLY AND BATTERY. REMOVED AND REPLACED M43 EMERGENCY LIGHT/PASS OXY PANEL DUE TO LOOSE CONNECTION ON WIRE TERMINAL IAW MM 33-51- 07 AND 33-51-08. A/C OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2007030800085 20070308 00085 WP 2007 3 8 NWAA070729984 1 20070212 A 5730 PANEL DOUG DC9 DC932 3022066 WP LT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 984US 47383 DURING "L" CHECK, FOUND CRACK IN LT WING LEADING EDGE PANEL NR 1590 APPROXIMATELY 4 INCHES AFT OF NR 3 FLAP HINGE. REPA IRED PER EA 99-208468. 2 L 7 2 4F A6WE 2007030800086 20070308 00086 NM 2007 3 8 NWAA070706746 1 20070228 A 3241 CONTROL UNIT BOEING 747 747222B 1384904 NM ANTI-SKID SYS MALFUNCTIONED A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 646NW 23737 TAKEOFF ABORTED AT 115 KNOTS DUE TO ANTI-SKID LIGHT ILLUMINATED ON FORWARD ANNUNCIATOR PANEL, AND BRAKES DID NOT FEEL NO RMAL ON ABORT. MAINTENANCE REMOVED AND REPLACED ANTI-SKID CONTROL UNIT, AND CONNECTORS OF ANTI-SKID UNIT. OPERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007030800087 20070308 00087 NM 2007 3 8 0700103152 1 20070113 A 3350 BATTERY AIRBUS A319 A319114 3930350 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 352NB 1828 DURING EMERGENCY ELECTRICAL CHECK, FOUND EPSU LEFT FAILURE. CORRECTED BY REPLACING EPSU BATTERY. CHECKS NORMALLY. 2 L 7 2 4F RT A28NM 2007030800090 20070308 00090 NE 2007 3 8 NWAA070766729 2 20070304 A 7310 FUEL FILTER BOEING 747 747251F 1384898 NM PWA JT9 JT9D7Q 52054 NE NR 2 ENGINE DIRTY A NWAA K NONE X ENGINE FLAMEOUT CR CRUISE 1 GL 01 629US 22388 702271 DURING CRUISE AT FL390, IN CODE 5 TURBULENCE, NR 2 ENGINE FLAMED OUT. DESCENDED TO FL270 AND SUCCESSFULLY RESTARTED ENG INE. FLIGHT CONTINUED TO NRT AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED TO FUEL FILTER. THE ENGINE WAS INSPECTED, TESTED AND RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E3NE 2007030800091 20070308 00091 NE 2007 3 8 NWAA070733172 2 20070301 A 7314 SHAFT AIRBUS A319 A319114 3930350 NM GE CFM56 CFM56* 13802 NE FUEL PUMP SHEARED A NWAA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 GL 01 372NB 2369 DURING DESCENT, AT 14,000 FT., NR 1 ENGINE FLAMED OUT. THE FLIGHT CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE FUEL PUMP SHAFT SHEARED. THE FUEL PUMP AND FCU WERE REPLACED, THE ENGINE TRIMMED, TES TED AND RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E2GL 2007030800094 20070308 00094 NM 2007 3 8 NWAA070786717 1 20070225 A 5310 TENSION TIE BOEING 747 747251F 1384898 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 617US 21121 DURING "L" CHECK, FOUND CRACKS IN FRAME TENSION TIE WEB FASTENER HOLES AT BS 880 STRINGER 6L TO STRINGER 12L. REPAIRED PER EA 67-208619 SECTIONS I AND II. 2 L 7 4 4F A20WE 2007030800095 20070308 00095 NM 2007 3 8 NWAA070806305 1 20070227 A 5311 FRAME BOEING 747 747451 1384940 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 665US 23820 DURING "M" CHECK, FOUND CRACK ON THE BS 1256 FRAME WEB AT STRINGER 26R. INTERIM REPAIR WAS ACCOMPLISHED PER SECTION I OF EA 63-208895. REPETITIVE INSPECTIONS PER SECTION II TO BE ACCOMPLISHED EVERY 2000 CYCLES. SECTION III WILL BE BASED O N SECTION II FINDINGS. 2 L 7 4 4F RT A20WE 2007030800097 20070308 00097 NM 2007 3 8 NWAA070796305 1 20070227 A 5411 FRAME BOEING 747 747451 1384940 NM PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 665US 23820 DURING "M" CHECK, FOUND CRACK IN AFT LOWER SIDE OF PYLON FRAME OUTBOARD CUTOUT FOR PANEL 484ER. REPAIRED PER EA 63-2089 00. 2 L 7 4 4F RT A20WE 2007030800098 20070308 00098 NM 2007 3 8 NWAA070816305 1 20070227 A 5311 FRAME BOEING 747 747451 1384940 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 665US 23820 DURING "M" CHECK, FOUND CRACK IN LT FRAME WEB AT BS 1265 STRINGER 26L. REPAIRED PER EA 63-208883 SECTION I. REPETITIVE INSPECTIONS PER SECTION II TO BE ACCOMPLISHED EVERY 2000 CYCLES. SECTION III WILL BE BASED ON SECTION II FINDINGS. 2 L 7 4 4F RT A20WE 2007030800100 20070308 00100 NM 2007 3 8 NWAA070656740 1 20070222 A 2697 WIRE BOEING 747 747251F 1384898 NM FIRE PROTECTION BROKEN A NWAA E ENGINE SHUTDOWN N FALSE WARNING NR NOT REPORTED 1 GL 01 640US 23888 DURING FLIGHT, NACELLE TEMP INDICATOR FLUCTUATING CAUSING FIRE WARNING BELL TO SOUND AND FIRE WARNING LIGHTS TO ILLUMINA TE, AND WIND MILLING OIL PRESSURE. SHUT DOWN NR 1 ENGINE DUE TO INTERMITTENT FIRE WARNING ON LOOP A, B LOOP IS INOP (AL READY ON MEL). DECISION WAS MADE TO DIVERT TO MSP, AND LANDING WAS UNEVENTFUL. MAINTENANCE FOUND PULLED OR BROKEN WIRE S, AND OTHER WIRES ARE TOO LONG FOR PLUG. REMOVED AND REPLACED PLUG D0017J. ALSO FOUND FORWARD DUCT ASSEMBLY SEALS, AN D MUSCLE LINE ON PYLON VALVE (PRSOV) LEAKING. REMOVED AND REPLACED SEALS AND PYLON VALVE. ALSO, REMOVED AND REPLACED N R 1 ENGINE OUTBOARD FIRE EXTINGUISHING BOTTLE. OPERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F A20WE 2007030800101 20070308 00101 NE 2007 3 8 NWAA070749751 2 20070303 A 7321 FCU DOUG DC9 DC941 302207N WP PWA JT8 JT8D11 52044 NE NR 1 ENGINE MALFUNCTIONED A NWAA K NONE X ENGINE FLAMEOUT DE DESCENT 1 GL 01 751NW 47115 676170 DURING DESCENT, AT 14,000 FT, NR 1 ENGINE FLAMED OUT. THE FLIGHT CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE FUEL PUMP SHAFT SHEARED. THE FUEL PUMP AND FCU WERE REPLACED, THE ENGINE TRIMMED, TEST ED AND RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 2007030800103 20070308 00103 NM 2007 3 8 NWAA070636623 1 20070220 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 623US 21705 DURING OVERNIGHT CHECK, FOUND EXIT SIGNS INOP AT DOOR 4 LEFT. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. OPERATION AL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F A20WE 2007030800105 20070308 00105 NM 2007 3 8 NWAA070676309 1 20070224 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING OVERNIGHT CHECK, FOUND UPPER DECK EMERGENCY TRACK LIGHTING INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007030800106 20070308 00106 GL 2007 3 8 P5CA0701511 2 20070104 A 7230 COMPRESSOR BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL NR 3 ENGINE DAMAGED A P5CA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 15 451PA 30809 706215 DURING TREND MONITORING OF NR 3 ENGINE, A SHIFT IN PARAMETERS WAS NOTICED. AN INSPECTION ON THE NR 3 ENGINE WAS REQUEST ED AND THE AIRCRAFT WAS DIVERTED TO PIK FOR A BORESCOPE INSPECTION. INSPECTED NR 3 ENGINE AND FOUND 11TH STAGE DAMAGE. REMOVED AND REPLACED NR 3 ENGINE PER POLAR WORK CARDS P71-00-00-1A/2A, P71-71-002A, P78-34-02-2A, P7200-101, P7100-002. 2 L 7 4 4F 4 F RT A20WE E23EA 2007030800107 20070308 00107 NM 2007 3 8 P5CA0701512 1 20070218 A 7330 WARNING MESSAGE BOEING 747 74746NF 13848BT NM COCKPIT ACTIVATED A P5CA O OTHER J WARNING INDICATION UK UNKNOWN 1 EA 15 454PA 30812 NR 4 ENGINE FUEL VALVE STATUS MESSAGE WITH CMC 74574. DEFERRED PER DDPG 73-31-2. 2 L 7 4 4F RT A20WE 2007030800109 20070308 00109 2007 3 8 QXEA200700213 4 20070218 A 2340 CONNECTOR BOMBDR DHC8 DHC8402 1390042 NM INTERPHONE SYS CORRODED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 413QX 4060 SEA FLIGHT NR 2376, COCKPIT TO GROUND CREW FORWARD LIGHT REMAINS ILLUMINATED WHEN DOOR IS CLOSED. COCKPIT TO GROUND INT ERPHONE INOP. AIRCRAFT RETURNED TO GATE. MAINTENANCE CLEANED CORROSION FROM INTERPHONE JACK SYSTEM. ALL CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030800110 20070308 00110 EU 2007 3 8 QXEA200700214 3 20070221 A 6140 WARNING SYSTEM BOMBDR DHC8 DHC8402 1390042 NM ROTOL R408 CR4086123F17 EU COCKPIT MALFUNCTIONED A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 421QX 4149 SEA FLIGHT NR 2334: AS THE AIRCRAFT ONTO THE RUNWAY, THE POWER PLANT MESSAGE APPEARED ON THE ED. AIRCRAFT RETURNED TO B LOCK. MAINTENANCE UPON INTERROGATION OF THE CDS FOR ENGINE FAULTS FOUND NR 2 ENGINE LANE B FAULT 130. C/W FIM TASK 61- 20-03-810-815. AFTER FAULT CODE CLEARED, RAN NR 2 ENGINE TWICE IN BETA RANGE. FAULT DID NOT RETURN. NO PARTS REPLACED . AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 6 C P17BO 2007030800114 20070308 00114 NM 2007 3 8 QXEA200700211 1 20070218 A 2421 31708001A GENERATOR DHAV DHC8 DHC8202 2809007 NM NR 2 FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 346PH 22933 1249 477 PDX FLIGHT NR 2149 - ON CLIMB-OUT, JUST AFTER TURNING THE ICING EQUIPMENT ON, WE GOT A ELEVATOR HORN HEAT. THE ENGINE M ADE A RUMBLE AND GOT THE NR 2 AC GEN LIGHT. RAN THE CHECKLIST AND LIGHT STAYED ON. MAINTENANCE REPLACED NR 2 AC GENER ATOR IAW AMM Q200 TASKS 2421-00-000-801 AND 24-21-00-400-801. 2 H 7 2 4T RT A13NM 2007030800116 20070308 00116 NM 2007 3 8 QXEA200700261 1 20070210 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - RIGHT WING INBOARD FLAP TRACK NR 1 UPPER TRACK UPPER SURFACE HAS 2 DIVOTS AT ROLLER POSITIONS ZERO AND 5 DEGREE S. REPAIRED IAW RD8-57-985. 2 H 7 2 4T RT A13NM 2007030800117 20070308 00117 NM 2007 3 8 QXEA200700262 1 20070216 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND THREE DENTS IN THE LEFT FUSELAGE SKIN JUST BELOW THE LEFT HAND ICE SHIELD AT STATIONS X297.5, X300.5 AND X303.5 BETWEEN STRINGERS 18 AND 19 LEFT. REPAIRED IAW RD8-53-5384 AND RD8-53-9471. 2 H 7 2 4T RT A13NM 2007030800118 20070308 00118 NM 2007 3 8 QXEA200700263 1 20070214 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - PROTRUDING DENT IN LOWER FUSELAGE SKIN AT STATION X349 AND STRINGER 30 LEFT. REPAIRED IAW RD8-53-2181 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007030800120 20070308 00120 NM 2007 3 8 QXEA200700265 1 20070214 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - THERE IS A GROUP OF DENTS LOCATED X329.00 BETWEEN STRINGER 11L AND 13L. REPAIRED IAW RD8-53-9468 AND SRM 51-10 -11. 2 H 7 2 4T RT A13NM 2007030800123 20070308 00123 NM 2007 3 8 QXEA200700271 1 20070209 A 5210 STRUCTURE DHAV DHC8 DHC8202 2809007 NM PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND ON MAIN CABIN DOOR LOWER FORWARD CORNER COVER PIECE WHERE CONNECTED TO MAIN CABIN DOOR LOWER SILL PLATE J UST AFT OF FORWARD GOOSENECK, THERE IS CORROSION ON BOTTOM SIDE. REPAIRED IAW SRM 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 2007030800124 20070308 00124 NM 2007 3 8 QXEA200700267 1 20070209 A 5210 STRUCTURE DHAV DHC8 DHC8202 2809007 NM PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND MAIN CABIN DOOR AFT LOWER CORNER COVE PIECE HAS CORROSION ON UNDER SIDE WHERE CONNECTED TO DOOR LOWER SIL L PLATE. REPAIRED IAW SRM 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 2007030800126 20070308 00126 NM 2007 3 8 QXEA200700332 1 20070228 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND MAIN CABIN DOOR THRESHOLD CORROSION AROUND NUTPLATE HOLES. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007030800130 20070308 00130 NM 2007 3 8 QXEA200700334 1 20070302 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND DENT IN FUSELAGE SKIN AT STATION X315.00 AND BETWEEN STRINGER 3L AND 4L. REPAIRED IAW RD8-53-9488. 2 H 7 2 4T RT A13NM 2007030800132 20070308 00132 NM 2007 3 8 QXEA200700329 1 20070222 A 5610 NUT PLATE DHAV DHC8 DHC8202 2809007 NM WINDSHIELD CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - RUSTED GANG CHANNEL NUTPLATES ON COPILOT AND PILOT WINDSHIELD CENTER AND LOWER FRAMES. REPAIRED IAW SRM 51-40- 11. 2 H 7 2 4T RT A13NM 2007030800133 20070308 00133 NM 2007 3 8 QXEA200700328 1 20070223 A 5347 CARGO TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - ON SEAT TRACK NR 6 IN FORWARD CARGO BAY THERE IS PITTING IN INBOARD FLOOR BOARD SUPPORT FROM STATION X550 TO X5 97. REPAIRED IAW RD8-53-784 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2007030800134 20070308 00134 NM 2007 3 8 QXEA200700336 1 20070303 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND RIGHT WING NR 3 FLAP TRACK HAS A LARGE DIVOT ON BOTTOM SODE OF UPPER TRACK. REPAIRED IAW RD8-57-987. 2 H 7 2 4T RT A13NM 2007030800136 20070308 00136 NM 2007 3 8 QXEA200700309 1 20070222 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - LAV PAN EXTERNAL SKIN APERTURE IS CHAFED AT AFT LOWER EDGE. REPAIRED IAW SRM 51-20-11. 2 H 7 2 4T RT A13NM 2007030800137 20070308 00137 NM 2007 3 8 QXEA200700315 1 20070224 A 5230 RIVET DHAV DHC8 DHC8202 2809007 NM CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - AFT CARGO DOOR RIVET ON INNER SKIN DAMAGED, AFT MIDDLE SECTION OF DOOR. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007030800138 20070308 00138 NM 2007 3 8 QXEA200700316 1 20070226 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND FUSELAGE EXTERIOR BELLY SKIN HAS CORROSION AT FS X245. REPAIRED IAW SRM 51-20-11. 2 H 7 2 4T RT A13NM 2007030800139 20070308 00139 NM 2007 3 8 QXEA200700311 1 20070223 A 5347 CARGO TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - ON SEAT TRACK SIX IN FORWARD CARGO BAY THERE IS PITTING ON INBOARD FLOORBOARD SUPPORT FROM STATION X550 TO X597 . REPAIRED IAW RD8-53-784 AND SRM 51-20-16, 51-20-36. 2 H 7 2 4T RT A13NM 2007030800142 20070308 00142 EA 2007 3 8 SWIA200717865 1 20070228 A 3350 INVERTER CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 411SW 7067 FOUND FLOOR EMERGENCY LIGHT AT RIGHT EXIT INOP. REPLACED INVERTER. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007030800149 20070308 00149 NM 2007 3 8 QXEA200700339 1 20070222 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND SCRATCH AND DENT IN FUSELAGE AT STATION 186.00 AND BETWEEN STRINGER 27L AND 26L. REPAIRED IAW RD8-53-538 4. 2 H 7 2 4T RT A13NM 2007030800151 20070308 00151 NM 2007 3 8 QXEA200700337 1 20070224 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND LEFT NR 2 FLAP TRACK HAS 2 DIVOTS ON UPPER RAMP AND 2 DIVOTS ON LOWER RAMP. REPAIRED IAW RD8-57-986. 2 H 7 2 4T RT A13NM 2007030800168 20070308 00168 EA 2007 3 8 SWIA200717886 1 20070115 A 5220 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7853 FOUND RT EMERGENCY EXIT DOOR UPPER LT CORNER LOOKING FROM INSIDE OF DOOR HAS CORNER METAL LIP BENT AND CRACKED INWARDS A T PRESSURE SEAL ATTACHMENT AREA, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLE AS PER REO 601R-52-21-042 SHEET 1-3 NOTE 7-8. 2 L 7 2 4F RT A21EA 2007030800169 20070308 00169 EA 2007 3 8 SWIA200717887 1 20070115 A 5220 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7853 FOUND LT EMERGENCY EXIT DOOR LOWER RT CORNER LOOKING FROM THE INSIDE OF THE DOOR HAS CORNER LIP OF PRESSURE SEAL ATTACHM ENT AREA BENT AND CRACKED INWARDS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLE AS PER REO 601R-52-21-0 43 SHEET 1-3 NOTE 7-8. 2 L 7 2 4F RT A21EA 2007030800171 20070308 00171 EA 2007 3 8 SWIA200717889 1 20070115 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7853 FOUND RBL 9 LOWER FLOOR SUPPORT STA280 CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE, CLIP, FILLER AND ANGLE FILLER IAW REO 601R-53-11-171 REV C. 2 L 7 2 4F RT A21EA 2007030800172 20070308 00172 EA 2007 3 8 SWIA200717890 1 20070115 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7853 AFT WEB CRACKED ON PAX DOOR NR 2 STEP FROM TOP, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS IN ZONE 2 AT AFT PAX DOOR PER CRJ200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007030800174 20070308 00174 NM 2007 3 8 QXEA200700347 1 20070302 A 2133 88060B010002 OUTFLOW VALVE BOMBDR DHC8 DHC8402 1390042 NM CABIN PRESSURE CONTAMINATED A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 424QX 1237 4006 SJC FLIGHT: DESCENDING TO 8000 FT WITH POWER AT IDLE, PRESSURIZATION PEGGED AT 3000 FPM. CLIMB FOR ABOUT 20 SECONDS THA N PEGGED TO 3000 FPM DESCENT. WHEN CABIN CAUGHT US AT ABOUT 7000 FT, IT DESCENDED WITH ME 1000-15000 FPM TO AIRPORT. M AINTENANCE INTERROGATED CDS AND FOUND NO REPORTING FAULTS, PSEU SHOWS NO FAULTS. FOUND OUTFLOW VALVE FOULED WITH WHAT L OOKS LIKE NICOTINE. REPLACED OUTFLOW VALVE PER Q400 AMM 21-31-16-000-801 AND 21-31-16-400-801. PERFORMED FUNCTIONAL TE ST OF THE PRESSURIZATION CONTROL PER 21-31-00-720-801. TESTS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030800176 20070308 00176 NM 2007 3 8 QXEA200700304 1 20070228 A 2740 WARNING SYSTEM BOMBDR DHC8 DHC8402 1390042 NM COCKPIT MALFUNCTIONED A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 416QX 4083 SEA FLIGHT NR 2338: FOUND PITCH TRIM CAUTION LIGHT WAS ILLUMINATED AFTER ENGINE START. LIGHT WENT OUT AFTER AIRCRAFT WA S BACK AT GATE ON EXTERNAL POWER. MAINTENANCE C/W Q400 FIM TASK 27-30-00-810-803. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030800177 20070308 00177 EA 2007 3 8 SWIA200717856 1 20070116 A 5345 ANGLE CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIP BAY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 967SW 7872 AFT EQUIP BAY ANGLE IS CRACKED RT BELOW THE RIGHT PACK (PART OF THE PACK AND HYD EQUIP MOUNTING STRUCTURE, DISCOVERED DU RING C-CHECK INSPECTION. INSTALLED NEW ANGLE AFT EQUIPMENT BAY AT RT PACK HYD MOUNT STRUCTURE AS PER CRJ200 SRM 51-42-0 6 PG 10-19. 2 L 7 2 4F RT A21EA 2007030800179 20070308 00179 EA 2007 3 8 SWIA200717858 1 20070116 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 967SW 7872 FOUND CRACK IN CLIP ON LEFT SIDE AT STRINGER 15 LT AND FS 624.0 ON AFT SIDE OF AFT PRESSURE BULKHEAD, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW LT CLIP AS PER REO 601R-53-61-422. 2 L 7 2 4F RT A21EA 2007030800181 20070308 00181 EA 2007 3 8 SWIA200717860 1 20070116 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 967SW 7872 FOUND CRACK IN CLIP ON FLOORBEAM FS 280.0 AND FLOOR SUPPORT (RIGHT) RBL9 INBOARD SIDE BELOW WL 730.00, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIP ON FLOORBEAM FS 280 AND FLOOR SUPPORT RBL 9 INBD SIDE PER STANDARD REPAIR 601R 53-0 057A. 2 L 7 2 4F RT A21EA 2007030800182 20070308 00182 EA 2007 3 8 SWIA200717861 1 20070116 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 967SW 7872 FOUND CRACK IN CLIP ON FLOORBEAM FS280.00 AND FLOOR SUPPORT (LEFT) LBL9 INBOARD AND OUTBOARD SIDES BELOW WL 73.00, DISCO VERED DURING C-CHECK INSPECTION. INSTALLED CLIP ON FLOORBEAM FS 280 AND FLOOR SUPPORT LBL9 INBD AND OTBD SIDE PER STAND ARD REPAIR 601R 53-0057A. 2 L 7 2 4F RT A21EA 2007030800183 20070308 00183 EA 2007 3 8 SWIA200717862 1 20070116 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 967SW 7872 PAX DOOR, FORE AND AFT WEBS ARE CRACKED UNDER THE HANDRAIL STOW BRACKET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLE D DOUBLER AND ANGLE AT PASSENGER DOOR FORE AND AFT WEBS PER CRJ200 REO 601R-52-11-702. 2 L 7 2 4F RT A21EA 2007030800184 20070308 00184 EA 2007 3 8 SWIA200717863 1 20070116 A 5210 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 967SW 7872 PAX DOOR, CRACKED INTERCOSTAL INSIDE THE DOOR, AFT EDGE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW INTERCOSTA L INSIDE PAX DOOR AFT EDGE IAW CRJ200 SRM 51-42-21 PG 17 AND SRM 51-42-06 PG 11. 2 L 7 2 4F RT A21EA 2007030800185 20070308 00185 EA 2007 3 8 SWIA200717864 1 20070116 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 967SW 7872 PAX DOOR, OUTER HANDLE IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW PAX DOOR OUTER HANDLE ASSY P/N 6 01R31763-1 PO NR 7872-01-24 IAW CRJ200 AMM 52-11-03-400-802. 2 L 7 2 4F RT A21EA 2007030800186 20070308 00186 EA 2007 3 8 SWIA200717843 1 20070222 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 441SW 7602 FOUND CAPTAIN'S WINDSHIELD CRACKED. REPLACED LEFT WINDSHIELD IAW CRJ MM 56-11-01. OPERATIONAL CHECKS GOOD, SN OFF: 012 29H5810. 2 L 7 2 4F RT A21EA 2007030900009 20070309 00009 EA 2007 3 9 SWIA200717893 1 20070115 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7853 FOUND PAX DOOR FWD STAIR SUPPORT WEB CRACKED IN RADIUS BETWEEN SECOND AND THIRD STEP, DISCOVERED DURING C-CHECK INSPECTI ON. INSTALLED DOUBLER AND ANGLES IAW REO 601R-52-11-702 REV A. 2 L 7 2 4F RT A21EA 2007030900011 20070309 00011 EA 2007 3 9 SWIA200717895 1 20070123 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 970SW 7881 FOUND PAX DOOR OPENING LOWER AFT SILL AREA AFT STEP PLATE HAS 4 EA CORRODED RUSTED BOLTS BOLTS ATTACH ANCHOR FITTING TO STEP PLATE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW BOLTS AND SCREWS ON PASSENGER DOOR COUNTER BALANCE ANCH OR FITTING PER CRJ200 AMM 52-11-17-400-804. 2 L 7 2 4F RT A21EA 2007030900012 20070309 00012 EA 2007 3 9 SWIA200717896 1 20070123 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 970SW 7881 FOUND PAX DOOR OUTER HANDLE CRACKED AT RADIUS, DISCOVERED DURING C-CHECK INSPECTION. REPLACED OUTER PAX DOOR HANDLE PER CRJ200 AMM 52-11-03-000-802/400-802. 2 L 7 2 4F RT A21EA 2007030900014 20070309 00014 EA 2007 3 9 SWIA200717898 1 20070123 A 5340 NUT CLIP CNDAIR CL600 CL6002B19 1900309 EA FLOOR SUPPORT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 970SW 7881 FOUND STA 280 LBL 9.0 OTBD CLIP ON FLOOR SUPPORT IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED OTBD CLIP A T FS 280 AS PER CRJ200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007030900015 20070309 00015 EA 2007 3 9 SWIA200717899 1 20070123 A 5340 NUT CLIP CNDAIR CL600 CL6002B19 1900309 EA FLOOR SUPPORT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 970SW 7881 FOUND STA 280 RBL 9.0 INBD AND OTBD CLIPS ON FLOOR SUPPORT ARE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED RT OTBD CLIP AT STA 280 RBL 9.0 PER CRJ200 SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007030900016 20070309 00016 EA 2007 3 9 SWIA200717900 1 20070123 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 970SW 7881 FOUND PAX DOOR AFT WEB CRACKED AT STAIR 832DT AND 832CT RADIUS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLES AND DOUBLER IAW REO 601R-52-11-702. 2 L 7 2 4F RT A21EA 2007030900017 20070309 00017 EA 2007 3 9 SWIA200717901 1 20070123 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 970SW 7881 FOUND STA 621 BULKHEAD TO FLOOR ATTACH ANGLE CRACKED LT OTBD SIDE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SPLI CE, REPAIR ANGLES AND STRAP AS PER REO 601R-53-61-117. 2 L 7 2 4F RT A21EA 2007030900018 20070309 00018 EA 2007 3 9 SWIA200717902 1 20070123 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 970SW 7881 FOUND FS 484 LBL 28 INTERCOSTAL, BRACKET CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP P/N 601R3117 1-17 TO FS 484 INTERCOSTAL LBL 28 PER CRJ200 SRM 51-42-06 PG 11 AND 51-42-21 PG 17. 2 L 7 2 4F RT A21EA 2007030900020 20070309 00020 EA 2007 3 9 SWIA200717904 1 20070123 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 970SW 7881 FOUND PAX DOOR FWD WEB IS CRACKED AT HANDRAIL DOWN STOP BRACKET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED 2 ANGL ES AND 1 DOUBLER ON PAX DOOR FWD WEB IAW REO 601R-52-11-702A PAGE 4 ITEM 8. 2 L 7 2 4F RT A21EA 2007030900023 20070309 00023 NM 2007 3 9 QXEA200700340 1 20070228 A 5320 SILL DHAV DHC8 DHC8202 2809007 NM PAX DOORWAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - THE MAIN CABIN DOOR SILL LOWER AFT CORNER FITTING HAS CORROSION ON THE INBOARD SIDE. REPAIRED IAW SRM 51-40-11 . 2 H 7 2 4T RT A13NM 2007030900024 20070309 00024 2007 3 9 DXTA200702002 4 20070306 A 3417 ACM CESSNA 750 750 2076810 CE CFE CFE73811B NE CABIN ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 07 970QS 7500070 5 MINUTES BEFORE LANDING CABIN SMELLED OF SMOKE AFTER LANDING, SWITCHED CAB PAC SWITCH TO OFF AND SMOKE DISAPPEARED. NO DIVERT. FOUND FWD ACM SEIZED. R & R FWD ACM, OPS CHECKS GOOD. I/A/W 750 MM 21-51-00. 2 L 7 2 4J 4 F RT T00007WI E44NE 2007030900026 20070309 00026 NM 2007 3 9 QXEA200700341 1 20070301 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - THE MAIN CABIN DOOR ENTRY FLOOR BOARD LANDING AT THE DOOR SILL EXHIBITS CORROSION BETWEEN THE MAIN CABIN DOOR G OOSE NECKS, PRIMARILY AT THE NUTPLATES. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007030900027 20070309 00027 NM 2007 3 9 QXEA200700342 1 20070222 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND DENTS AND SCRATCHES ON FUSELAGE SKIN, LOCATED FORWARD OF 121AL, 13" FORWARD AND BETWEEN STRINGER 27L AND 26L. REPAIRED IAW RD8-53-5384. 2 H 7 2 4T RT A13NM 2007030900028 20070309 00028 NM 2007 3 9 QXEA200700343 1 20070223 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 411 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND LEFT OUTBOARD SEAT TRACK NR 1 IS GOUGED AT STATION X411. REPAIRED IAW SRM 51-20-36 AND RD8-53-1342. 2 H 7 2 4T RT A13NM 2007030900030 20070309 00030 NM 2007 3 9 QXEA200700344 1 20070223 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 543 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND LEFT INBOARD SEAT TRACK IS GOUGED AT STATION X543. REPAIRED IAW RD8-53-4936 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2007030900031 20070309 00031 NM 2007 3 9 QXEA200700346 1 20070225 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 223-250 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX -THE LEFT INBOARD SEAT TRACK NR 4 HAS CORROSION AT THE PANEL LANDING ON THE OUTBOARD SIDE BETWEEN STATION X223 AN D X250. REPAIRED IAW RD8-53-1102 AND RD8-53-4473. 2 H 7 2 4T RT A13NM 2007030900034 20070309 00034 2007 3 9 070052 4 20070226 A 3497 CONNECTOR DOUG DC9 DC983 3022083 WP VHF NAVIGATION LOOSE A WX0A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 19 869GA 53294 FLIGHT 474 LAS/FSD - APPROXIMATELY 40 MINUTES AFTER TAKEOFF, THE FLIGHT CREW REPORTED THAT THE NR 2 VHF NAV HAD BECOME I NOPERATIVE. DISPATCH AND MAINTENANCE CONTROL ASSURED THE CREW THAT THE WEATHER AT FSD WAS ADEQUATE TO CONTINUE THE FLIG HT. HOWEVER, THE CREW OPTED TO RETURN TO LAS VEGAS WHERE THE AIRPLANE LANDED WITHOUT INCIDENT. LAS VEGAS MAINTENANCE D ISCOVERED A LOOSE J2 ELECTRICAL CONNECTOR AT THE VHF NAV CONTROL PANEL. A SATISFACTORY RETURN-TO-SERVICE CHECK WAS ACCO MPLISHED PER AMM 22-01-05. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007030900035 20070309 00035 CE 2007 3 9 DJFA2007023 1 20070225 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZ STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 755TA 4896 RK324 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE RT IB HORIZONTAL STA BILIZER, THE RT RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. MAINTENANCE REPLACED THE RIB ASSEMBLY. 2 H 7 2 4F 4 F RT A16SW E25EA 2007030900037 20070309 00037 WP 2007 3 9 070045 1 20070219 A 3010 AYLF97321 SENSOR DOUG DC9 DC983 3022083 WP OUT OF ADJUST A WX0A H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 WP 19 861GA 49557 FLIGHT 516 IDA/LAS - FLIGHT CREW REPORT "L ICE PROTECT TEMP HIGH" ANNUNCIATOR ILLUMINATED WITH AIRFOIL ANTI-ICE ON. QRH PROCEDURE APPLIED AND LIGHT EXTINGUISHED. LAS VEGAS MAINTENANCE TROUBLESHOT THE SYSTEM TO A FAULTY LT TEMPERATURE SENS OR. REMOVED AND REPLACED TEMP SENSOR PER AMM 30-10-06. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER 30-10-00. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007030900038 20070309 00038 WP 2007 3 9 070044 1 20070218 A 5210 SKIN DOUG DC9 DC983 3022083 WP L1 DOOR GOUGED A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 871GA 53296 FLIGHT 5184 IFP/SJC - DURING THE PRE-FLIGHT WALKAROUND A PILOT NOTICED WHAT APPEARED TO BE A GOUGE IN THE FUSELAGE ABOVE L1 MAIN PASSENGER DOOR. INVESTIGATION REVEALED SKIN DAMAGE BEGINNING APPROXIMATELY 24 INCHES ABOVE THE L1 DOOR AND CON TINUING LATERALLY ACROSS THE FUSELAGE APPROXIMATELY 10 INCHES WHERE THE GOUGE TERMINATED IN A PUNCTURE. THE DEPTH ATTAI NED WAS APPROXIMATELY 1 INCH NEAR THE PUNCTURE. NO PRESSURIZATION, NOISE OR DRIPPING FLUID ISSUES HAVE BEEN REPORTED AG AINST THIS AIRPLANE SO DETERMINATION OF ORIGIN OF THE DAMAGE IS NOT POSSIBLE. THE AIRPLANE WAS FERRIED TO TULSA WHERE A MERICAN AIRLINES PERFORMED A TEMPORARY REPAIR APPROXIMATELY AT STATION 220, LONGERON 3L IN-ACCORDANCE-WITH AA ESO NR 805 2 L 7 2 4F RT A6WE 2007030900039 20070309 00039 WP 2007 3 9 070043 1 20070216 A 3350 408822101 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 881GA 49708 DURING A ROUTINE OVERNIGHT SERVICE CHECK LAS VEGAS, MAINTENANCE REPORTED THAT THE EMERGENCY EXIT OVERHEAD SIGNS WOULD NO T TEST. REPLACED THE BATTERY PACK IN B5-27 POWER SUPPLY. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33- 51-12. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007030900048 20070309 00048 2007 3 9 070050 4 20070224 A 3422 25883024 GYRO DOUG DC9 DC983 3022083 WP NR 2 DIRECTIONAL MALFUNCTIONED A WX0A O OTHER J WARNING INDICATION CR CRUISE 1 WP 19 866GA 49910 FLIGHT 431 SHV/LAS - FLIGHT CREW REPORTED THAT DURING CRUISE, HEADING FAIL ON BOTH FMS'S. 30 DEGREE SPLIT BETWEEN F/O'S NAV DISPLAY AND RMI, QRH 31.2 PROCEDURE APPLIED. LAS VEGAS MAINTENANCE REPORT THAT THEY REMOVED AND REPLACED THE NR 2 D IRECTIONAL GYRO. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 34-21-09. THE AIRPLANE HAS RETURNED TO SERV ICE. 2 L 7 2 4F RT A6WE 2007030700047 20070307 00047 NM 2007 3 7 CALA0700110 1 20070226 A 5315 141T5107 FLOORBEAM BOEING 767 767424ER 1385270 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69063 29458 FLOORBEAM CORRODED AT BS 303, LBL 25. REPAIRED IAW SRM 53-00-51 FIG 201. 2 L 7 2 4F RT A1NM 2007030700052 20070307 00052 NM 2007 3 7 SWAA071199 1 20070302 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 424WN 29828 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007030700055 20070307 00055 NM 2007 3 7 SWAA071201 1 20070303 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 17 DEF. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007030700066 20070307 00066 NM 2007 3 7 SWAA071180 1 20070302 A 5340 65C27134 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 440, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030700078 20070307 00078 NM 2007 3 7 SWAA071204 1 20070303 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030700085 20070307 00085 NM 2007 3 7 SWAA071207 1 20070303 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER 16R CRACKED AT BS 401. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007030700092 20070307 00092 NM 2007 3 7 SWAA071216 1 20070303 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030700096 20070307 00096 NM 2007 3 7 SWAA071231 1 20070305 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 20R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007030700103 20070307 00103 NM 2007 3 7 SWAA071224 1 20070304 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 222WN 34290 R2 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007030700107 20070307 00107 NM 2007 3 7 SWAA071236 1 20070305 A 5210 6397861 LINK BOEING 737 7373H4 1384600 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 L1 DOOR WILL NOT COMPLETELY OPEN. REMOVED AND REPLACED CRACKED LOWER GUIDE ARM LINK, REINSTALLED PIN PER MM. 2 L 7 2 4F RT A16WE 2007030700108 20070307 00108 NM 2007 3 7 SWAA071226 1 20070304 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 690, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007030700109 20070307 00109 NM 2007 3 7 SWAA071227 1 20070304 A 5320 6545801 TEE FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED MV1 CHECK, FOUND OUTBOARD TEE CHORD CORRODED AT FWD HORIZONTAL FLANGE BS 227, LBL 3. REPAIRED CHORD PE R SWA EA. 2 L 7 2 4F RT A16WE 2007030700110 20070307 00110 NM 2007 3 7 SWAA071212 1 20070303 A 5310 6545834 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM CORRODED AT BS 344, STR 17R. REMOVED AND REPLACED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2007030700115 20070307 00115 NE 2007 3 7 G60A200700002 2 20070221 A 7320 441790 HYDROMECH UNIT DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE NR 1 ENGINE UNKNOWN A G60A O OTHER X ENGINE FLAMEOUT CR CRUISE 1 EA 27 701GC 48434 702497 DURING CRUISE AT FL310 NR 2 ALERT -ENG 1 RPM LOW- ENGINE FLAMED OUT. SELECTED IGNITION OVERRIDE, ENGINE CAME BACK ON LI NE. REPLACED HMU. 2 L 7 3 4F 4 F RT A22WE E31N3 2007030700131 20070307 00131 EU 2007 3 7 07FDEA00624 1 20070302 A 2612 CG7G011 SMOKE DETECTOR AIRBUS 300 A300F4605R 3930327 EU E/E BAY MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 651FE 3917 3917 728 CLIMB-OUT APPROACHING 2000' , CRC ECAM FLASHED FOR MIN EQUIP BAY SMOKE. SMOKE LIGHT CAME ON AND LIGHT EXTINGUISHED IN A FEW SECONDS. MIN EQUIP BAY SNIFFER CHECK, NEGATIVE. PASSED 11,000' SAME HAPPENED AGAIN, LIGHT STAYED ON. SNIFFER C HECK WAS NEGATIVE. DECLARED EMERG, RAN CHKLISTS AND CAME BACK. LIGHT EXTINGUISHED AGAIN, DON'T KNOW WHEN. REMOVED AND REPLACED SMOKE DETECTOR 12WA; OPS CK OK. PREMATURE REMOVAL/INSTALLATION OFF MFG CG7G0-11, POS AV2 SRL AB1227,TAG 390B 62, ON MFG CG7G0-11, SRL 144, TAG 6565A4. REMOVED AND REPLACED LEFT AND RIGHT COALESCER BAGS PRECAUTIONARY. 2 L 7 2 4F RT A35EU 2007030700133 20070307 00133 NM 2007 3 7 07FDEA00626 1 20070125 A 5312 BULKHEAD BOEING 727 727233 138408A NM BS 1183 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 COMPLY WITH FEDEX EA 7-5330-102012, FUSELAGE - BS 11 83 BULKHEAD WEB CRACK REPAIR AT WL 225, BL61. COMPLIED WITH EA 7-5 330-102012, RII:575461. 2 L 7 3 4F RT A3WE 2007030700136 20070307 00136 NM 2007 3 7 QXEA200700302 1 20070228 A 3110 DISPLAY BOMBDR DHC8 DHC8402 1390042 NM COCKPIT MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 410QX 4053 SMF FLIGHT NR 2410: ALT FAILURE ON FO'S PFD. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE PULLED AND RESET ICP2 (C6) CIRCUI T BREAKER. ALL INDICATIONS ON FO'S PFD NORMAL. COMPLETED OPS CHECK OF ICP IAW MTC 6316103. ALL CHECKS ARE GOOD. A/C IS CAT I AND PLACARD REFLECTS CAT I. MAINTENANCE CONTROL WAS BEEN NOTIFIED. NO PARTS REPLACED. AIRCRAFT WAS RETURNED T O SERVICE. 2 H 7 2 4T RT A13NM 2007030700137 20070307 00137 NM 2007 3 7 QXEA200700303 1 20070228 A 5210 HANDLE BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR DAMAGED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 421QX 4149 SEA FLIGHT NR 2378: FOUND MAIN CABIN DOOR EXTERIOR OPEN HANDLE RECESSES TOO DEEP, CANNOT OPEN DOOR FROM OUTSIDE. MAINTE NANCE SHIMMED EXTERIOR DOOR HANDLE STOP BUMPER AS REQUIRED FOR FLUSH FIT OF HANDLE. DOOR OPERATES NORMALLY OPENING AND CLOSING. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030700138 20070307 00138 NM 2007 3 7 07FDEA00611 1 20070227 A 2821 HDA3F011 RELAY DOUG MD11 MD11 3023602 NM ZONE 100 BURNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 ELECTRICAL ARCING AT NR 1 EPC BAY LT TOP SIDE RELAY R2-53, R2-57, R2-102 AND R2-252 AFFECTED. REMOVED AND REPLACED 4 R ELAYS R2-53, R2-57, R2-102 AND R2-252 AS PER STANDARD WIRING PRACTICES MANUAL. WIRINGS SPLICE REPAIRED AS PER STANDARD WIRING PRACTICES MANUAL. WIRINGS CONTINUITY CHECKED AS PER WDM 28-22-01, WDM 28-22-02, WDM 28-22-04 AND WDM 28-22-05, F OUND SATISFACTORY BOOST PUMPS. OPS CHECK CARRIED OUT AS PER AMM 28-22-01-5, FOUND SATIS. 2 L 7 3 4F RT A22WE 2007030700139 20070307 00139 WP 2007 3 7 07FDEA00612 1 20070228 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP BS 1481-1491 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 CLG WW FOUND 1 CRACK 1.25" LONG ON HORIZONTAL BULKHEAD BETWEEN STA 1481 AND 1491 X= 30 RT. TRIMMED OUT DAMAGED PORTION OF WEB AND INSTALLED FILLER AND REPAIR DOUBLER IAW SRM 53-00-01 FIG 4 SHT 2 VOL 1. REPLACED INTERCOSTAL IAW SRM 51-35-0 1 VOL 1 PAR 1-5. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I026749/N01749 IAW SRM 53-00-01 FIG 4 SHT 2 VOL 1. 2 L 7 3 4F A22WE 2007030700140 20070307 00140 WP 2007 3 7 07FDEA00613 1 20070228 A 5310 DOOR FRAME DOUG DC10 DC1010 3022110 WP BS 889 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 554FE 46708 FOUND FWD LOWER CARGO COMPT, FWD DOOR JAMB AT STA 889 LONGS NR 43 RT AND 40 RT, EXISTING REPAIR AT WEB AND DOOR FRAME. REMOVED WEB REPAIR, FRAME SPLICE REPAIR TWO INTERNAL ANGLE SPLICE AND OPEN WEB AS REQ`D FOR ACCESS IAW SRM 51-30-00 VOL 2. REMOVED AND REPLACED INTERCOSTAL IAW DWG ADA0056. INSTALLED FRAME, ANGLE AND WEB REPAIR IAW SRM 53-50-00 FIG 1 VOL 1 AND DWG ADA0055. FABRICATED PARTS IAW DETAIL PART TRAVELER N01168 AND SRM 53-50-00 FIG 1 VOL 1. 2 L 7 3 4F A22WE 2007030700141 20070307 00141 WP 2007 3 7 07FDEA00614 1 20070228 A 5300 UNKNOWN DOUG DC10 DC1010 3022110 WP BS 1156 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 CAC 2 EA CRACKS 1.5" LONG AND 3" LONG ON STRIP AT STA 1156 Z= -74 X= -6 AND X= 6. STRIPPED PAINT FROM DAMAGED AREA IAW SRM 51-21-01 PAR C PAG 26 VOL 2. PERFORM NDI CONTROL AND CONFIRMED LENGTH AND END OF CRACK. PERFORMED REPAIR IAW SRM 5 3-40-00 FIG 17. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I027579/N02579 AND IAW SRM 53-40-00, FIG 17 VOL 1. 2 L 7 3 4F A22WE 2007030700142 20070307 00142 WP 2007 3 7 07FDEA00615 1 20070228 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 1099 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 CAC CIRCUMFERENTIAL FRAME AT STA 1099 BETWEEN STRINGER NR 39 LT TO 45 RT EXISTING FRAME REPAIRS AND REPAIRS CHANNEL IN D IF LOCATIONS. REMOVED OLD REPAIR CHANNEL SPLICE AT L NR 52, CUT CAP FRAME AT L NR 41 R. REMOVED SECTION FRAME BTWN L NR 47 L TO 46 R. REMOVED SHEAR CLIPS BTWN L NR 44 R TO 49 R. INSTALLED REPAIR PARTS P/N`S I026182-1A TO -13 IAW SRM 5 3-30-00-FIG 5 VOL 1, SRM 51-35- 01 VOL 2 AND SRM 51-33-01 VOL 2. SEALING AREA IAW SRM 51-41-02 VOL 2. FABRICATED PART S IAW DETAIL PART TRAVELER N01182 AND SRM 53-30-00 FIG 5 VOL 1. 2 L 7 3 4F A22WE 2007030700143 20070307 00143 NM 2007 3 7 QXEA200700349 1 20070304 A 7921 800600M03 ACTUATOR BOMBDR DHC8 DHC8402 1390042 NM NR 1 OIL COOLER MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 401QX 2007 4031 BOI FLIGHT NR 2422: AFTER TAKEOFF, OIL TEMP CONTINUED TO CLIMB THRU ABOUT 15000 FT. TEMP WAS ABOUT 90 DEG. AFTER LEVEL OFF WITH CRUISE POWER SET, TEMP FLUCTUATED FROM 97 TO 86 AT ABOUT 1 MINUTE AT A TIME. IT WAS ABOVE 90 FOR THE FIRST 30 MINUTES OF FLIGHT. AFTER THAT IT STABLIZED AT 77-78. DURING TAXI IN, IT CLIMBED AGAIN TO 88. MAINTENANCE REMOVED AND REPLACED THE NR 1 OIL COOLER AIR OUTLET FLAP ACTUATOR IAW Q400 AMM 79-21-31-000-801 AND 79-21-31-400-801. OPS CHECK OF THE ACTUATOR WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030700144 20070307 00144 NM 2007 3 7 QXEA200700350 1 20070304 A 2120 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM CABIN ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 411QX 4055 MFR FLIGHT NR 2420: PAX REPORTED BURNING RUBBER ODOR AT SEAT 1AB. TURNED OFF NR 1 ACM AND ODOR WENT AWAY. MAINTENANCE PERFORMED EXTENSIVE GROUND RUN OF A/C OPERATING ACM'S TOGETHER AND INDIVIDUALLY SELECTED VARIED TEMPERATURE SETTINGS DUR ING OPS CHECK. NO FUMES NOTED AT ANY TIME. UTILIZED INPUT INSTRUCTIONS OF SERVICE LETTER DH8-400-SL-21-012A AS A PRECA UTIONARY MEASURE, AGAIN NO FUMES NOTED. NO PARTS REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030700145 20070307 00145 2007 3 7 HALA0700085 4 20070304 A 2210 066500291101 RECEIVER BOEING 767 767300 1385204 NM NR 1 MALFUNCTIONED A HALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 590HA 15602 15602 33467 ETOPS SIGNIFICANT SYSTEM, "NO LAND 3" DISPLAYED ON ASA WITH APP MODE NOT SELECTED AND AUTOPILOT/FD ENGAGED OR NOT ENGAGE D (ASA NO LAND 3 DISPLAYED IN CRUISE FL 340 NO RESET), (ON APP AMBER LOC AND G/S FLAG CAPT ADI. REPLACED NR 1 MMR, OPS CK OK PER MM 34-31-01. PERFORMED MCDP TEST 30 TO RETAIN "LAND 3" STATUS TEST PASSED. 2 L 7 2 4F RT A1NM 2007030700146 20070307 00146 NM 2007 3 7 HALA0700083 1 20070304 A 3350 LIGHT BOEING 767 767300 1385204 NM SEAT 1H INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 587HA 33421 FOUND OVERHEAD EMER LIGHT AT 1H IS INOP. REPLACED LIGHT ASSY FOR OVERHEAD EMER LIGHT AT SEAT 1H OPS NML. 2 L 7 2 4F RT A1NM 2007030700147 20070307 00147 NM 2007 3 7 HALA0700081 1 20070306 A 2160 UNKNOWN BOEING 767 767300 1385204 NM TEMP CONTROL UNKNOWN A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, TEMP CONTROL ON GROUND IN HNL WAS INADEQUATE. COOLED CABIN TO 80-83 UNABLE TO COOL TO 75, IN AIR TEMP CONTROL WAS NORMAL. ACCOMPLISHED BITE CHECK AT BOTH PACK TEMP CONTROLLERS AND ZONE TEMP CONTROLLER. NO FAULTS FOUND. CLEANED AND RESECURED CONNECTORS AT BOTH PACK TEMP CONTROL VLVS. OPS CHECKS NORMAL. 2 L 7 2 4F RT A1NM 2007030700165 20070307 00165 EA 2007 3 7 COMA0760213 1 20070226 A 3020 5399001 ANTI-ICE VALVE CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 932CA 7630 7038 FLIGHT 5056 - ON CLIMBOUT, RECEIVED ANTI-ICE CAUTION MESSAGE. REPLACED COWL ANTI-ICE VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007030700168 20070307 00168 NM 2007 3 7 2007UALA00568 1 20070221 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 556UA 26650 EMERGENCY LIGHT AT DOOR 4 LEFT EXTERIOR INOPERATIVE. RELAMPED. OPS CHK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030700184 20070307 00184 EU 2007 3 7 NSVA20070022 1 20070129 A 2770 ACTUATOR SAAB SF340 SF340A 7850100 EU GUST LOCK LEAKING A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 35SZ 03070002 35 FOUND RUDDER GUST LOCK WILL NOT ENGAGE. THIS RUDDER GUST LEAK ACTUATOR, VERIFIED 28 VOL AT RUDDER GUST LOCK ACTUATOR IA W SMR 27-72-00. PLACED GUST LOCK HANDLE IN DISENGAGED POSITION. REMOVED AND REPLACED RUDDER GUST LOCK ACTUATOR IAW AMM 27-72-10, P/N 8618M16 S/N OFF 03070002, S/N ON 98070048. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2007030700185 20070307 00185 2007 3 7 NSVA20070023 2 20070202 A 7297 WIRE SAAB SF340 340B 7860101 EU ENGINE BROKEN A NSVA O OTHER O OTHER LD LANDING 1 EA 27 311CE 214 FLIGHT IDLE STOP LIGHT CAME ON DURING LANDING. TS IAW AMM 76-10-60 AND FOUND TWO BROKEN WIRES AT 6GA-J1 PINS L AND N RE QUIRED WIRES IAW SAAB WM 20-20-00. REPAIRED BROKEN WIRING AT 6GA-J1 PINS L AND N IAW SWM 20-20-00. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 2007030700186 20070307 00186 CE 2007 3 7 NSVA20070024 1 20070202 A 2612 FIRE LOOP BEECH 1900 1900D 1154162 CE LT NACELLE MALFUNCTIONED A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 124CJ UE24 WHEN TESTING THE LT FIRE LOOP THE LEFT T HANDLE ILLUMINATED AND THE ANN DID NOT ILLUMINATE. REPOSITIONED LT FIRE LOOP N EAR LT EXHAUST STACK, INSPECTED FWD DIRE SEAL CONNECTIONS AND AFT GROUND, NDN, INSPECTED CONNECTIONS AT AMP NG AND PERFO RMED ALL OPS CHECKS, OPS CHECKS NORMAL IAW 1900 MM 26-10-01. 2 L 7 2 4T RT A24CE 2007030700187 20070307 00187 EU 2007 3 7 NSVA20070026 1 20070202 A 5210 7253741257 SEAL SAAB SF340 340B 7860101 EU PAX DOOR LEAKING A NSVA O OTHER O OTHER CR CRUISE 1 EA 27 237MJ 237 FOUND LOUD WHISTLING NOISE COMING FROM MAIN CABIN DOOR IN FLIGHT. INSPECTED CABIN DOOR AND FOUND PRESSURE SEAL TO BE IN TACT AND IN PROPER POSITION. REMOVED AND REPLACED LOWER DOOR SEAL REST IAW SRM 51-40-02. OPS CHECK GOOD, P/N 7253741-2 57. 2 L 7 2 4T RT A52EU 2007030700188 20070307 00188 EU 2007 3 7 NSVA20070027 1 20070202 A 7600 UNKNOWN SAAB SF340 340B 7860101 EU UNKNOWN A NSVA O OTHER O OTHER TO TAKEOFF 1 EA 27 350CJ 350 AFTER TAKEOFF THE FLT IDLE STOP LIGHT ILLUMINATED. PERFORMED OPERATIONAL CHECK OF FLIGHT IDLE STOP MECHANISM AS PER SAM M 76-10-60-05. NO FAULTS NOTED, OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2007030700189 20070307 00189 EU 2007 3 7 NSVA20070028 1 20070205 A 7600 531624 CONTROL QUADRANT SAAB SF340 340B 7860101 EU ENGINE UNKNOWN A NSVA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 242CJ 242 FOUND FLIGHT IDLE OPEN LIGHT ILLUMINATED AFTER TAKEOFF. REPLACED CONTROL QUADRANT IAW SA AMM 76-10-05 FUNCTIONAL TEST R EQUIRED, PN: 531624, SN ON: 023 SN OFF: 061. PERFORMED OPERATIONAL CHECK OF QUADRANT CONTROL IAW SA MM 71-00-00. OPERA TIONAL CHECK GOOD. 2 L 7 2 4T RT A52EU 2007030700190 20070307 00190 EU 2007 3 7 NSVA20070029 1 20070205 A 7697 WIRE SAAB SF340 340B 7860101 EU ENGINE BROKEN A NSVA O OTHER O OTHER TO TAKEOFF 1 EA 27 339CJ 339 FLIGHT IDLE STOP OPEN LIGHT ILLUMINATED AFTER TAKEOFF, OVERRIDE KNOB IS IN. T/S IAW 76-10-60 AND FOUND A BROKEN WIRE ON 6GA-J1 PIN N. REPAIRED WIRE IAW MM 20-20-00, OPS CHECKED GOOD IAW AMM 76-10-60. 2 L 7 2 4T RT A52EU 2007030700191 20070307 00191 EU 2007 3 7 2007UALA00573 2 20070223 A 7200 ENGINE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 2 FAILED A UALA A E UNSCHED LANDING ENGINE SHUTDOWN E K VIBRATION/BUFFET FLUID LOSS CL CLIMB 1 WP 29 372UA 24637 856264 RTFL DUE TO FAILURE OF NR 2 ENGINE. [SUP 05-16-07] MISSING NUT ON HPC IGV CAUSED ONE VANE TO ROTATE OUT OF SCHEDULE. T HIS CREATED AN AERODYNAMIC 1/REV ON THE HPC R1 BLADES. THIS EXCITATION RESULTED IN THE HCF FAILURE AT THE ROOT OF ONE OF THE BLADES. THE LIBERATED BLADE DESTROYED THE OPERABILITY OF THE ENGINE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007030700192 20070307 00192 EU 2007 3 7 NSVA20070030 1 20070206 A 3260 DOWNLOCK SWITCH SAAB SF340 340B 7860101 EU MLG DIRTY A NSVA O OTHER J WARNING INDICATION CL CLIMB 1 EA 27 350CJ 350 FOUND DOWN LOCK LIGHT SLOW TO EXTINGUISH DURING RETRACTION. FLIGHT CREW REPORTS 2 NORMAL GEAR EXT/RET CYCLES AFTER INI TIAL DISCREPANCY EVALUATED DOWN AND UPLOCK SWITCHES VISUALLY AND CLEANED DEBRIS FROM SWITCH AREA. 2 L 7 2 4T RT A52EU 2007030700193 20070307 00193 NM 2007 3 7 2007UALA00574 1 20070222 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 512UA 24809 SEATS 5, 6 AND 7 LEFT EMERGENCY LIGHTS INOPERATIVE. RESEATED SEAT 5L CONNECTOR AND OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030700194 20070307 00194 NM 2007 3 7 2007UALA00575 1 20070222 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 512UA 24809 DOOR 4R EMERGENCY LIGHT INOPERATIVE. RELAMPED R-4 DOOR EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030700195 20070307 00195 NM 2007 3 7 QXEA200700297 1 20070216 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 389-395 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND THREE PROTRUDING DENTS IN THE LOWER FUSELAGE SKIN AT STATIONS X389.5, X393.5 AND X395.0 AND STRINGER 30LT . REPAIRED IAW RD8-53-5384 AND RD8-53-9475. 2 H 7 2 4T RT A13NM 2007030700196 20070307 00196 NM 2007 3 7 2007UALA00576 1 20070222 A 2997 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT MLG WW BURNED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 771UA 26932 CONNECTOR DM29311A BURNED FOR THE NR 2 ACMP (CENTER PUMP) RIGHT WHEEL WELL. PUMP REPLACED. CONNECTOR IS TAPED AND TIED OFF IN THE AREA. REPLACED CONNECTOR AND PINS. SYSTEM OP CHECKS OK FOR SERVICE. SUSPECT PUMP ARMATURE DETERIORATION CA USED GREATER THAN NORMAL CURRENT FLOW, RESULTING IN BURNED CONNECTOR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007030700197 20070307 00197 NM 2007 3 7 QXEA200700295 1 20070209 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND RIGHT INBOARD FLAP TRACK NR 1 HAS 2 DIVOTS ON UPPER RAMP AND 2 DIVOTS ON LOWER RAMP. REPAIRED IAW RD8-57 -985. 2 H 7 2 4T RT A13NM 2007030700198 20070307 00198 NM 2007 3 7 QXEA200700296 1 20070209 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND RIGHT INBOARD FLAP TRACK NR 2 HAS 2 DIVOTS ON UPPER RAMP AND 2 DIVOTS ON LOWER RAMP. REPAIRED IAW RD8-57 -986. 2 H 7 2 4T RT A13NM 2007030700199 20070307 00199 EU 2007 3 7 200703051 1 20070228 A 2120 UNKNOWN EMB ERJ170 ERJ170100SE 3260406 EU COCKPIT ODOR A UHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 11 872RW 17000143 FLIGHT 6503 LGA TO DCA BURNT SMELL IN COCKPIT AFTER ENGINE SHUTDOWN. OCM VERIFIED NO C/B'S TRIPPED, NO SMELL WITH POWER ON, PERFORMED VISUAL IN FWD AVNX BAY, NO DEFECTS NOTED. OCM RAN ENGINES AND NO SMELL NOTED. NO REPEAT DISCREPANCIES TO THIS DATE 03/05/2007. 2 L 7 2 4F RT A56NM 2007030700200 20070307 00200 NM 2007 3 7 QXEA200700292 1 20070218 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - LEFT INBOARD FLAP TRACK NR 2 HAS A DIVOT ON LOWER RAMP LOWER SURFACE 3" AFT OF FORWARD EDGE. REPAIRED IAW RD8- 57-986. 2 H 7 2 4T RT A13NM 2007030700201 20070307 00201 EA 2007 3 7 COMA0760212 1 20070225 A 3260 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA LANDING GEAR MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 416CA 7450 FLIGHT 5089 - AFTER TAKEOFF FROM BWI RECEIVED A LEFT MLG DISAGREE WARNING MESSAGE, CREW DECLARED AN EMERGENCY AND DIVERT ED TO PIT. FLIGHT LANDED WITHOUT INCIDENT. INSPECTED THE LEFT MLG SWITCHES AND TARGETS; NO DEFECTS NOTED. CYCLED THE LANDING GEAR MULTIPLE TIMES WITH PUMP 3A AND 3B INDEPENDENTLY. DISCREPANCY COULD NOT BE DUPLICATED. 2 L 7 2 4F RT A21EA 2007030700202 20070307 00202 EU 2007 3 7 Y2PA200700022 1 20070222 A 7160 INLET AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D 30010 NE NR 1 ENGINE DAMAGED A Y2PA A UNSCHED LANDING C F.O.D. CL CLIMB 1 GL 23 827AA 298 249J109 WEATHER CLEAR - VFR - CLIMBING THROUGH 8000' CREW HEARD A LOUD NOISE FROM REAR AND FELT AN IMPACT. CREW NOTICED LEFT EN GINE EPR CLIMB AND OIL PRESSURE DECREASING. AFTER CREW CONFIRMED SECONDARY INDICATIONS AN ENGINE SHUTDOWN WAS INITIATED USING APPROVED USA JET PROCEDURES FOR DA-20 AIRCRAFT. CREW DECLARED EMERGENCY WITH HOUSTON CENTER , APPROVED TO DIVERT TO SAT FOR LONG RUNWAY AND EMERGENCY ASSISTANCE. FIRE TRUCKS WERE CALLED OUT AS PRECAUTION BUT NOT NEED, CREW WERE ABL E TO TAXI ON THE ONE ENGINE TO THE FOB WITH NO FURTHER DAMAGE. MAINTENANCE WAS SENT FROM USA JET MAIN MAINTENANCE BASE TO INVESTIGATE AND FOUND NR 1 ENGINE SUSTAINED A BIRD STRIKE WITH INLET DAMAGE. MAINTENANCE PERSONAL PERFORMED BOROSCOP 2 L 7 2 4F 4 F A7EU E7EA 2007030700203 20070307 00203 EU 2007 3 7 NSVA20070039 1 20070214 A 7600 531624 CONTROL QUADRANT SAAB SF340 340B 7860101 EU ENGINE UNKNOWN A NSVA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 202SR 202 CONFIG WARNING ON TAKEOFF ROLL. VERIFIED POWER TO RELAY 8 GA W PINX1. VERIFIED GROUND TO RELAY AT 8GA PIN X2.5. VERIF IED GROUNDS FROM RELAY 8GA PINS D1 AND A2. VERIFIED OPERATION OF L POWER LEVER QUADRANT SWITCH PINS 5 AND 6 AT P1. VER IFIED OPERATION OF R POWER LEVER QUADRANT SWITCH PINS 5 &6 AT P2. VERIFIED OPERATION OF R CONDITION LEVER QUADRANT SWIT CH PINS AT 5&6 PE. FOUND L CONDITION LEVER QUADRANT SWITCH STAYS IN OPEN POTIONS WHEN LEVER IS MOVED CHECKED PINS A 5 & 6 AT RH P1. REMOVED CONTROL QUADRANT IAW SAB 340 AMM 76-10-05-04 TROUBLESHOOT SYSTEM USING WM 76-10-00. VERIFIED CONTI NUITY BETWEEN LT BOARD WOW SWITCH AND RELAY AT 8GA. SWAPPED RELAY AT 8 GA NO FIX . INSTALLED NEW CONTROL QUADRANT IAW 2 L 7 2 4T RT A52EU 2007030700204 20070307 00204 EU 2007 3 7 NSVA20070025 1 20070202 A 3220 LANDING GEAR SAAB SF340 340B 7860101 EU NOSE ICED A NSVA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 252CJ 252 DURING GEAR RETRACTION IN TRANSIT, LIGHT REMAINED ON WITH GEAR SELECTED UP. RAN ABNORMAL CHECKLIST RETURNED TO AIRPORT, AIRCRAFT REQUIRES CHECK FLIGHT TO VERIFY PROPER OPERATION OF GEAR. AIRCRAFT RELEASED FOR OPS CHECK FLIGHT PURPOSES ONL Y. REMOVED 3/8" ICE FROM NOSE GEAR UPLOCK PAD, ALSO REMOVED EXCESSIVE ICE BUILD UP FROM NOSE AND MAIN GEAR. INSTRUCTED CREW TO DE-ICE GEAR AT DE-ICE PAD PRIOR TO TAKEOFF, SEE LOG PAGE 103867 ITEM 1M FOR TEST FLIGHT ENTRY TO VERIFY GEAR OP ERATION. OPERATION CHECK FLIGHT SATISFACTORY. 2 L 7 2 4T RT A52EU 2007030700205 20070307 00205 EU 2007 3 7 NSVA20070042 1 20070218 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU LAVATORY MALFUNCTIONED A NSVA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 360PX 220 LAV SMOKE DETECTOR LIGHT COMES ON INTERMITTANTLY. REMOVED AND REPLACED SMOKE DETECTOR, IAW SMM 26-13-06. OPS CHECK GOO D. 2 L 7 2 4T RT A52EU 2007030700206 20070307 00206 EA 2007 3 7 COMA0760214 1 20070227 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 934CA 9184 7042 FLIGHT 5443 - SEVERAL EMERGENCY LIGHTS OUT, BOTH ROWS OF TRACK LIGHTING. REMOVED AND REPLACED EMERGENCY BATTERY PACK. 2 L 7 2 4F RT A21EA 2007030700207 20070307 00207 EA 2007 3 7 COMA0760217 1 20070227 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 934CA 17216 7042 FLIGHT 5443 - SEVERAL EMERGENCY LIGHTS OUT, BOTH ROWS OF TRACK LIGHTING. REMOVED AND REPLACED EMERGENCY BATTERY PACK. 2 L 7 2 4F RT A21EA 2007030700208 20070307 00208 EA 2007 3 7 COMA0760215 1 20070227 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 934CA 24466 7042 FLIGHT 5443 - SEVERAL EMERGENCY LIGHTS OUT, BOTH ROWS OF TRACK LIGHTING. REMOVED AND REPLACED EMERGENCY BATTERY PACK. 2 L 7 2 4F RT A21EA 2007030700209 20070307 00209 EA 2007 3 7 COMA0760216 1 20070227 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 934CA 13292 7042 FLIGHT 5443 - SEVERAL EMERGENCY LIGHTS OUT, BOTH ROWS OF TRACK LIGHTING. REMOVED AND REPLACED EMERGENCY BATTERY PACK. 2 L 7 2 4F RT A21EA 2007030700210 20070307 00210 EA 2007 3 7 COMA0770017 1 20070220 A 2150 GG6700950093 ACM CNDAIR CL600 CL6002C10 1390015 EA A/C BAY FAILED A COMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 379CA 4144 10102 FLIGHT 5044 - DURING TAXI F/A REPORTED SMOKE IN CABIN, THEN RIGHT PACK AUTO FAIL CAUTION MESSAGE. A/C RETURNED TO GATE. REMOVED AND REPLACED RIGHT PACK ACM. 2 L 7 2 4F RT A21EA 2007030700211 20070307 00211 NM 2007 3 7 CALA0700115 1 20070302 A 5320 6562285531 DRAG ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 LEFT UPPER WING TO BODY DRAG ANGLE CRACKED FWD OF A/C DOOR 3302L. REPAIRED IAW ECRA 5311-01300. 2 L 7 2 4F RT A16WE 2007030700212 20070307 00212 EU 2007 3 7 NSVA20070037 1 20070214 A 2697 CONNECTOR SAAB SF340 340B 7860101 EU OVERHEAT SYS DEFECTIVE A NSVA O OTHER N FALSE WARNING IN INSP/MAINT 1 EA 27 339CJ 339 LH TAILPIPE HOT LIGHT ILLUMINATED ON GROUND. INSP TAILPIPE AREA, NO FAULTS FOUND. REMOVED 3 DETECTORS AND SECURED WIRI NG AND CAPPED CONNECTOR. RE-INSTALLED (3EA) SPOT DETECTORS ON EXHAUST FAIRING IAW AMM 26-12-05. REMOVED AND REPLACED C ONNECTOR IAW MM 20-20-00, OPS CHECK GOOD. LOG PAGE 119451 STATES CLEARING DMI 7470 APPLIED SEALANT TO LT NG TAILPIPE HO T DETECTOR IAW COLGAN WORK CARD 26-21-19-1, OPS CHECK GOOD, P/N ON TF2219-5. REMOVED AND REPLACED CONNECTOR IAW MM 20-2 0-10 CWC 26-21-09, P/N 1953723-PWT000 SN REFER TO 5M FOR SEALANT ON SOT DETECTORS, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2007030700213 20070307 00213 EU 2007 3 7 NSVA20070040 1 20070215 A 2752 TP100010 ACTUATOR SAAB SF340 340B 7860101 EU T/E FLAP MALFUNCTIONED A NSVA O OTHER O OTHER IN INSP/MAINT 1 EA 27 193CJ 193 FOUND FLAPS FAILED TO RETRACT UNLESS HYD PUMP IS IN OVERRIDE. REMOVED AND REPLACED RT FINE ACTUATOR BLEED HYDS SYSTEM A ND OPS CHECK GOOD IAW 27-51-25-04 PN TP1000-10 SN OFF 486 SN ON 503. 2 L 7 2 4T RT A52EU 2007030700214 20070307 00214 NE 2007 3 7 DL76S070173 2 20070228 A 7200 CF680A2 ENGINE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 1 MAKING METAL A DALA E ENGINE SHUTDOWN R E PARTIAL RPM/PWR LOSS VIBRATION/BUFFET DE DESCENT 1 SO 27 135DL 39368 4656 25145 580370 LT ENG INOP, ON DESCENT LOUD BOOM AND SERVERE VIBS-ENG CONT TO RUN UNTIL SHUTDOWN-THRUST LOST. FOUND METAL IN TAILPIPE. REMOVED AND REPLACED NR 1 ENGINE ON ROUNTINE CARD TRANSMITTAL. 2 L 7 2 4F 4 F RT A1NM E13NE 2007030700215 20070307 00215 NM 2007 3 7 DL76L070177 1 20070227 A 5414 PANEL BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 PYLON MISSING A DALA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 SO 27 188DN 27583 723843 ON WAC FOUND RIGHT ENG INBD PYLON TRAPEZOID PANEL MISSING. FWD TO MCO AS PER CDL 54-53-02 CHECKED TIGHTENING BOLTS ON ALL OTHER PYLON ACCESS PANEL ON BOTH ENGINE. INSTALLED RT ENG PYLON OTBD TRAPEZOID PANEL MCO AND PLAC REMOVED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007030800008 20070308 00008 WP 2007 3 8 07FDEA00603 1 20070227 A 5730 SKIN DOUG DC10 DC1010 3022110 WP RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 RT WING LOWER SURFACE AT STA XW 486 ON SKIN TANK BOX FOUND SEVERE CORROSION WITH EXFOLIATION. FASTENERS REMOVED AND REI NSTALLED IAW SRM 51-33-01. CORROSION REMOVED IAW SRM 57-10-00 FIG 59 VOL 1 O/B FLAP I/B HINGE SUPPORT REMOVED AND REINS TALLED IAW SRM 51-33-01 VOL 2 PAGE 34/47, EA NR 8-5730-103699 ACCOMPLISHED (SEE JPF). 2 L 7 3 4F A22WE 2007030800015 20070308 00015 NM 2007 3 8 07FDEA00634 1 20070303 A 5713 STRINGER DOUG MD11 MD11 3023602 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 CRACK FOUND AT STRINGER END 42L (XORS 629), APPROX 1" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. (SUPPLEMENTAL 2 3 MARCH 07) CRACK AT STRINGER END 42L (XORS 629) ON LEFT HAND WING TANK SLOTTED OUT AND REPAIRED WITH NEW REPAIR SPL ICE AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007030800018 20070308 00018 NM 2007 3 8 07FDEA00637 1 20070303 A 5713 STRINGER DOUG MD11 MD11 3023602 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 CRACK FOUND AT STRINGER END 11R (XORS 704), APPROX 12.5" LENGTH ON RIGHT WING TANK, DURING HFEC INSPECTION. CRACK AT S TRINGER END 11R (XORS 704) ON RIGHT HAND WING TANK TRIMMED OUT AND REPAIRED WITH SPLICES AS PER SRM 57-20-00 FIGURE 10 V OLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2- 100. 2 L 7 3 4F RT A22WE 2007030800023 20070308 00023 NM 2007 3 8 HALA0700076 1 20070303 A 2120 CDU BOEING 767 767300 1385204 NM MALFUNCTIONED A HALA K NONE O OTHER NR NOT REPORTED 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM, E/E COOLING MOTOR L FMC COOLING BAIL DOES NOT INDICATE COOLING FLOW. RESEATED CAPT MCDU. OPS CKS OK. 2 L 7 2 4F RT A1NM 2007030800025 20070308 00025 NM 2007 3 8 HALA0700079 1 20070303 A 3150 WARNING SYSTEM BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE COCKPIT MALFUNCTIONED A HALA K NONE O OTHER NR NOT REPORTED 1 WP 13 596HA 23276 ETOPS SIGNIFICANT SYSTEM - L FWD BOOST PUMP LOW PRESS LIGHT FAILED TO ILLUM AND EICAS MSG FAILED TO DISPLAY WITH SW OFF. PERFORMED FIM 28-22-00 FIG 110. FOUND SYSTEM OPERATES NORMALLY WITH APU NOT RUNNING. 2 L 7 2 4F 4 F RT A1NM E24NE 2007030800029 20070308 00029 NM 2007 3 8 HALA0700068 1 20070226 A 7830 CLAMP BOEING 767 767300 1385204 NM NR 1 ENGINE BROKEN A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 584HA 24258 ETOPS SIGNIFICANT SYSTEM, NR 1 ENG LT REVERSER BAN CLAMP BROKEN. REPLACED BAN LATCH PER AMM TASK 78-31-02-404-008-N00, CHECKED GOOD. 2 L 7 2 4F RT A1NM 2007030800036 20070308 00036 WP 2007 3 8 IXXA07SMN046S 1 20070119 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING DAMAGED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD LEADING EDGE HOLES ELONGATED AT STATION XFS 710.000. REMOV ED FASTENERS AS NEEDED. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMO VED. FABRICATED REPAIR PARTS, CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51- 1-8B, DC8 SRM 51-1-11, DC8 SRM 51-3-1 AND SEMAN DRAWING NUMBER ED-4426 DATED 01-20-07. 2 L 7 4 4F RT 4A25 2007030800040 20070308 00040 WP 2007 3 8 IXXA07SMN016S 1 20070113 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2944 46065 DURING ROUTINE C CHECK INSPECTION, FOUND AN IMPROPER REPAIR AT STATION FS1290, LONGERON 15 RIGHT. REMOVED EXISTING REPA IR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATED REP AIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PA RTS IAW DC8 SRM 51-1-20D, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1- 11, DC8 SRM 51-3-1 AND SEMAN DRAWING NUMBER ED4423 DATED 01-26-07. COMPLETED FAA FORM 8110-3 NUMBER 07077 DATED 02-13-0 7. 2 L 7 4 4F RT 4A25 2007030800060 20070308 00060 WP 2007 3 8 IXXA07SMN033S 1 20070119 A 5753 SKIN DOUG DC8 DC871F 302199D WP T/E FLAP MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP UPPER SKIN HAS A NON STANDARD REPAIR FROM STATION XF326.000 TO STATION XF333.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK S OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11SEMAN DRAWING NUMBER ED-4410 DATED 01-13-07. COMPLETED FAA FORM 8110-3 NUMBER 07021 DATED 01-19-07. 2 L 7 4 4F RT 4A25 2007030800072 20070308 00072 EU 2007 3 8 NSVA20070015 1 20070120 A 6123 AUTOCOARSEN SYS SAAB SF340 340B 7860101 EU MALFUNCTIONED A NSVA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 321CJ 321 AUTOCOARSEN LIGHT DID NOT ILLUMINATE WHEN TURNED ON. RESET ALL C/B'S IN SYS ROW ENG'S CHECKED SYS IAW 61-22-00, OP CHEC KED NORMAL ON GROUND. 2 L 7 2 4T RT A52EU 2007030800074 20070308 00074 EU 2007 3 8 NSVA20070019 1 20070127 A 6123 M835366022M RELAY SAAB SF340 340B 7860101 EU AUTOCOARSEN SYS FAILED A NSVA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 EA 27 299CJ 299 FOUND AUTOCOARSEN WILL NOT TEST. REMOVED AND REPLACED RELAYS 113 AND 114P/N: M83536-6-022M, IAW AMM 39-40-45. 2 L 7 2 4T RT A52EU 2007030800075 20070308 00075 EU 2007 3 8 NSVA20070044 1 20070223 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 196CJ 196 FOUND 4 EMERGENCY LIGHTS ON FLOOR AND 3 ON LT SIDE OVERHEAD ARE INOP. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT POWER S UPPLY IAW AMM 33-50-04. OPS CHECK GOOD PN ON/OFF 60-1321-1 SN ON 19332 OFF 17063. 2 L 7 2 4T RT A52EU 2007030800076 20070308 00076 CE 2007 3 8 NSVA20070036 1 20070211 A 2620 1183890051 SHUTOFF VALVE BEECH 1900 1900D 1154162 CE LT ENGINE INOPERATIVE A NSVA O OTHER O OTHER IN INSP/MAINT 1 EA 27 60MJ UE60 FOUND LT ENGINE FIREWALL SHUTOFF VALVE IS INOP. REMOVED AND REPLACED LT ENGINE FIREWALL SHUTOFF VALVE PN/OFF/ON 118-389 005-1, SN/OFF 9307076 SN/ON9031512, OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 2007030800079 20070308 00079 EU 2007 3 8 NSVA20070033 1 20070207 A 3350 22LN BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 334CJ 334 FOUND NUMEROUS EMERGENCY LIGHTS IN CABIN OUT. REMOVED AND REPLACED NR 3 (22LN) BATT POWER SUPPLY IAW AMM 33-50-10-4 PN ON 60-1321-1 SN ON 8405 SN OFF 1880, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2007030800082 20070308 00082 EU 2007 3 8 NSVA20070038 1 20070214 A 2750 HP14161005 CONTROL VALVE SAAB SF340 340B 7860101 EU T/E FLAP MALFUNCTIONED A NSVA O OTHER O OTHER AP APPROACH 1 EA 27 193CJ 193 FLAPS WOULD NOT EXTEND ON APPROACH. NO WARNINGS AURAL OR VISUAL. FLAPS TAKE 10 SECONDS TO EXTEND WHEN ACTUATED WITH H ANDLE. TESTED IAW AMM 27-51-00-05 AND OPERATIONAL CHECK GOOD. PERFORMED ADJUSTMENT AND TEST OF FLAP CONTROL IAW 27-51- 00-05 PROCEDURE 3 ELECTRICAL RIGGING OF FLAP CONTROL POTENTIOMETER L/R FLAP POTENTIOMETERS. ADJUSTED POTENTIOMETERS WIT HIN SPECS. ALL ELECTRICAL POTENTIOMETERS NOW WITH LIMITS. REMOVED AND REPLACED FLAP CONTROL VALVE IAW AMM 27-51-15-04 PN ON AND OFF HP1416100-5 SN ON 51540 OFF 1539. OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 2007030800089 20070308 00089 WP 2007 3 8 NWAA070759855 1 20070302 A 2160 CIRCUIT BREAKER DOUG DC9 DC951 3022051 WP CABIN TEMP FAILED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 764NC 47717 FLIGHT ATTENDANT REPORTED SMOKE CIRCULATING IN THE PASSENGER CABIN AREA DURING THE TAKEOFF CLIMB. APPROPRIATE COM PROCE DURES WERE COMPLIED WITH AND THE FLIGHT CREW STATED THAT THE SMOKE DISSIPATED AFTER THEY SHUTDOWN THE RIGHT PACK. THE A IRCRAFT RETURNED TO A NORMAL SAFE LANDING BACK AT MEM. MAINTENANCE DID NOT FIND ANY CONFIRMED SOURCE FOR SMOKE. DISCOV ERED THAT THE CABIN TEMPERATURE CONTROL CIRCUIT BREAKER HAD FAILED INTERNALLY AND REPLACED IT. COALESCER BAGS WERE REPL ACED, PACK BURNOUT PROCEDURES PERFORMED, NO FURTHER EVIDENCE OF SMOKE OR SMELL NOTED SO THE AIRCRAFT WAS RETURNED TO SER VICE. 2 L 7 2 4F RT A6WE 2007030800092 20070308 00092 WP 2007 3 8 NWAA070849941 1 20070306 A 2120 CLAMP DOUG DC9 DC932 3022066 WP RT ACM STRIPPED A NWAA B EMER. DESCENT O OTHER CR CRUISE 1 GL 01 3324L 47103 AT FL340, THE CABIN TEMPERATURE BEGAN TO INCREASE. THE LEFT PACK WENT TO FULL HOT IN AUTO AND FLIGHT CREW SELECTED FULL COLD. THEN THE RIGHT PACK WENT TO FULL HOT IN AUTO AND FULL COLD WAS SELECTED IN MANUAL. CREW NOTICED THAT THE AIRCRA FT WAS LOSING CABIN PRESSURE AND APPLIED COM PROCEDURES, INCLUDING STARTING A DESCENT. STILL UNABLE TO CONTROL CABIN PR ESSURE AN EMERGENCY DESCENT TO 10,000 FEET WAS ACCOMPLISHED. MASKS DID NOT DEPLOY, THE AIRCRAFT CONTINUED TO SCHEDULED DESTINATION AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RIGHT ACM OUTLET DUCT HAD A LOOSE CLAMP WITH STR IPPED THREADS AND REPLACED IT. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007030800096 20070308 00096 NM 2007 3 8 NWAA070826305 1 20070204 A 5311 FRAME BOEING 747 747451 1384940 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 665US 23820 DURING "M" CHECK, FOUND CRACK ON BS 340 BL 0 FRAME. REPAIRED PER EA 63-208887. 2 L 7 4 4F RT A20WE 2007030800102 20070308 00102 NM 2007 3 8 NWAA070616623 1 20070220 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 623US 21705 DURING OVERNIGHT CHECK, FOUND EXIT SIGNS INOP AT DOOR 5 LEFT. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. OPERATION AL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F A20WE 2007030800111 20070308 00111 EA 2007 3 8 QXEA200700354 2 20070306 A 7310 312242604 FUEL FILTER BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA NR 1 DIRTY A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 420QX 127 4147 RDM FLIGHT NR 2329: NR 1 FUEL FILTER BYPASS. MAINTENANCE REMOVED AND REPLACED NR 1 FUEL FILTER IAW Q400 MM TASK 73-11-3 1-000-801 AND 73-11-31-400-801. NO DEFECTS NOTED. NO LEAKS. REMOVED AND REPLACED THE NR 1 FUEL FILTER IMPENDING BYPAS S SWITCH IAW Q400 AMM TASK 73-31-06-000-801 AND 73-31-06-400-801. OPS CHECK GOOD WITH NO LEAKS NOTED. AIRCRAFT RETURNE D TO SERIVCE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2007030800112 20070308 00112 NM 2007 3 8 QXEA200700257 1 20070216 A 2913 6617302 PUMP BOMBDR DHC8 DHC8402 1390042 NM NR 1 MAKING METAL A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 406QX 6958 4048 YLW FLIGHT NR 2477: NR 1 HYD SYSTEM FAILED, LOST FLUID AND PRESSURE WITH ZERO FLUID QUANTITY. NR 1 HYD SYSTEM INTERMITT ENTLY INDICATED 500-700 PSI PRESSURE BUT NO BRAKES WERE AVAILABLE ON LANDING. MAINTENANCE PERFORMED STEPS 5A, 5B AND 5C OF Q400 AMM 05-54-00 PG 604. REMOVED PRESSURE RETURN AND CARE DRAIN MANIFOLD FILTERS. INSPECTED AND FOUND METALLIC DE BRIS PARTICLES IN THE PRESSURE AND CARE DRAIN FILTERS. INSTALLED NEW HYD SYS NR 1 PRESSURE RETURN AND CASE DRAIN FILTER ELEMENTS IAW Q400 AMM 29-11-32 PGS 401-407. PERFORMED FLUSH OF THE NR 1 HYD SYSTEM IAW AMM TASK 29-10-00-617-802 PARA 1-4J (1)(A) THRU (AP). INSPECTED AND FOUND SOURCE OF HYD LEAK TO BE THE BOOTSTRAP PRESSURE LINE. REMOVED AND REPLACED 2 H 7 2 4T RT A13NM 2007030800121 20070308 00121 NM 2007 3 8 QXEA200700260 1 20070211 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND RIGHT WING INBOARD FLAP TRACK NR 2 UPPER TRACK UPPER SURFACE HAS 2 DIVOTS AT ROLLER POSITIONS ZERO AND 5 DEGREES. REPAIRED IAW RD8-57-986. 2 H 7 2 4T RT A13NM 2007030800122 20070308 00122 NM 2007 3 8 QXEA200700266 1 20070209 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND RIGHT OUTBOARD FLAP TRACK NR 3 HAS 2 DIVOTS ON UPPER RAMP AND 2 DIVOTS ON LOWER RAMP. REPAIRED IAW RD8-5 7-987. 2 H 7 2 4T RT A13NM 2007030800125 20070308 00125 NM 2007 3 8 QXEA200700331 1 20070228 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND 2 DENTS IN FUSELAGE SKIN AT STATION X311.00 AND 2.5" ABOVE THE LEFT HAND ICE SHIELD, BETWEEN STRINGER 4L AND 5L. REPAIRED IAW RD8-53-9488. 2 H 7 2 4T RT A13NM 2007030800129 20070308 00129 NM 2007 3 8 QXEA200700333 1 20070303 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND RIGHT FLAP TRACK NR 3 HAS A WEAR AREA ON UPPER RAMP BOTTOM SIDE1.5" FROM THE FORWARD END OF THE TRACK. R EPAIRED IAW RD8-57-987. 2 H 7 2 4T RT A13NM 2007030800131 20070308 00131 NM 2007 3 8 QXEA200700327 1 20070223 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND UPPER LEFT LEADING EDGE BRACKET AT YW 137.0 IS CRACKED. REPAIRED IAW SRM 51-40-00 AND 51-40-11. 2 H 7 2 4T RT A13NM 2007030800135 20070308 00135 NM 2007 3 8 QXEA200700310 1 20070222 A 5610 NUT PLATE DHAV DHC8 DHC8202 2809007 NM WINDSHIELD CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - RUSTED GANG CHANNEL NUTPLATES ON CO-PILOT AND PILOT WINDSHIELD CENTER AND LOWER FRAMES. REPAIRED IAW SRM 51-40 -11. 2 H 7 2 4T RT A13NM 2007030800148 20070308 00148 EA 2007 3 8 SWIA200717871 1 20070224 A 3350 AD20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA CABIN DISCHARGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 614SK 8285 8285 10051 FOUND EMERGENCY LIGHTING BATTERY PACKS NR 1 AND NR 2 FAIL WHEN TESTED. REPLACED BATTERY PACKS NR 1 AND NR 2 IAW MM 33-5 1-17. OPERATIONAL CHECKS GOOD. NR 2 BATTERY PACK S/N OFF - 80518. 2 L 7 2 4F RT A21EA 2007030800165 20070308 00165 2007 3 8 QXEA200700351 4 20070306 A 3160 6229810204 DISPLAY CNDAIR CL600 CL6002C10 1390015 EA COCKPIT MALFUNCTIONED A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 606QX 11230 10023 SEA - AFTER TAKEOFF FOR FLIGHT 2542, FIRST OFFICER'S MULTI FUNCTION DISPLAY WENT BLANK. RETURNED TO THE FIELD AND LANDE D WITHOUT INCIDENT. MAINTENANCE REPLACED THE DISPLAY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007030900006 20070309 00006 NM 2007 3 9 DXTA200702001 1 20070306 A 5312 SEAL AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE NLG WW PANEL WORN E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 275QS 75 LOUD GRINDING NOISE DURING GEAR DOWN CYCLE. DURING CYCLE, 20 SECOND WARNING LIGHT STARTED FLASHING. 3 GREEN/ NO RED WAS INDICATED APPROXIMATELY 10 SECONDS AFTER 20 SECOND WARNING FLASHER. INSPECTED MLG, MLG DOORS NOSE CONE. NO DEFECTS NOTED . PERFORMED MLG SWINGS. NO DEFECTS NOTED. INSPECTED NLG WW ACCESS PANEL SEAL. FOUND SEAL WORN. PLACED SEAL. NLG WHEEL WE LL PANEL PLACED. ALL WORK DONE IAW F-2000 M/M CH 52-40-00-3/11/07. 2 K 7 2 4F 4 F RT A50NM E44NE 2007030900007 20070309 00007 EU 2007 3 9 NSVA20070043 1 20070220 A 3297 CONNECTOR SAAB SF340 340B 7860101 EU MLG DOWNLOCK DAMAGED A NSVA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 237MJ 237 FLIGHT IDLE STOP LIGHT DOES NOT GO OFF AFTER GEAR RETRACTION. TAKES 40 SEC FOR IT TO GO OFF AFTER GEAR ARE FULLY RETRAC TED CAN NOT BE DUPLICATED IN ANY OTHER PHASE OF FLIGHT OR GROUND. REF FLT FORM 119905. FOUND STRAY GROUND BETWEEN RT M LG DOWNLOCK CONNECTOR PIN N AND PIN Y ON CONNECTOR 132 VP PZ. REPAIRED WIRE IN MLG WELL AREA REF SAAB MM 76-10-00 AND 3 2-30-00, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2007030900021 20070309 00021 EA 2007 3 9 SWIA200717906 1 20070123 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA BS 5280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 970SW 7881 FOUND CRACK ON FS 5280 WEB AT RBL10 LOWER PART OF BEAM AT INTERSECTION POINT WITH FLOOR POST AND WEB, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE PER CRJ200 SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007030900036 20070309 00036 2007 3 9 070053 4 20070226 A 2565 SLIDE DOUG DC9 DC987 3022087 WP PAX DOOR DISLODGED A WX0A O OTHER O OTHER TX TAXI/GRND HDL 1 WP 19 948GA 49778 FLIGHT 826 PIA/PIE - AFTER TAXI TO THE GATE AND ENGINE SHUT-DOWN, THE CABIN CREW ATTEMPTED TO OPEN THE MAIN ENTRY DOOR. THEY NOTICED THAT THE EVACUATION SLIDE HAD BECOME DISMOUNTED FROM THE DOOR. ST. PETERSBURG MAINTENANCE REPORT HOLDING THE SLIDE AND DISCONNECTING THE GIRT BAR TO ALLOW THE PASSENGERS TO DEPLANE. THEY FURTHER REPORT SECURELY RE-MOUNTING T HE SLIDE TO THE MAIN ENTRY DOOR PER AMM 25-62-00. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007030900045 20070309 00045 WP 2007 3 9 070049 1 20070223 A 3350 BATTERY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS SEPARATED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 871GA 53296 DURING A ROUTINE OVERNIGHT MAINTENANCE SERVICE CHECK LAS VEGAS MAINTENANCE REPORTED THAT THE FORWARD OVERWING HATCH EXIT SIGNS WOULD NOT TEST. FURTHER REPORT THAT THE BATTERY HAD BECOME PARTIALLY DISMOUNTED FROM THE POWER SUPPLY. A SATISF ACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007030900047 20070309 00047 2007 3 9 N93A05032007 4 20070305 A 3418 C36602 STICK SHAKER GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU COCKPIT BROKEN E N93A K NONE O OTHER IN INSP/MAINT 1 SO 13 441QS 3864 1341 DURING SCHEDULED MAINTENANCE, THE PILOTS STICK SHAKER WAS FOUND BROKEN OFF AND LAYING IN THE BELLY OF THE AIRCRAFT. 2 L 7 2 4F 4 F RT A12EA E25NE 2007030900054 20070309 00054 NM 2007 3 9 QXEA200700307 1 20070223 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 411 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND LEFT OUTBOARD SEAT TRACK NR 1 IS GOUGED AT STATION X411. REPAIRED IAW SRM 51-20-36 AND RD8-53-1342. 2 H 7 2 4T RT A13NM 2007030900055 20070309 00055 NM 2007 3 9 QXEA200700314 1 20070223 A 5740 BRACKET DHAV DHC8 DHC8202 2809007 NM LT WING LE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND UPPER LEFT LEADING EDGE BRACKET AT YW 137.0 IS CRACKED. REPAIRED IAW SRM 51-40-00, 51-40-11. 2 H 7 2 4T RT A13NM 2007030900059 20070309 00059 EA 2007 3 9 SWIA200717837 1 20070226 A 2120 UNKNOWN CNDAIR CL600 CL6002D24 1390016 EA CABIN ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 806SK 15070 WHEN STARTING THE APU GET A FUEL ODOR. PERFORMED SEVERAL APU STARTS BUT COULD NOT DUPLICATE AND NO FUEL LEAKS NOTED. O PERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007030900060 20070309 00060 EA 2007 3 9 SWIA200717838 1 20070222 A 2913 887055 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 430SW 5849 5849 7523 HYD 2 LOW PRESSURE MESSAGE, LOST ALL QUANTITY SYSTEM NR 2. DIVERTED RNO. REPLACED NR 2 HYDRAULIC PUMP IAW 29-11-01. O PS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2007030900062 20070309 00062 EA 2007 3 9 SWIA200717839 1 20070220 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 969SW 7876 FOUND CEILING EMERGENCY LIGHT AT ROW 5 NOT WORKING. REPLACED CEILING LAMP AT ROW 5 IAW AMM 33-51-16. OPERATIONAL CHECK S GOOD. 2 L 7 2 4F RT A21EA 2007030900063 20070309 00063 EA 2007 3 9 SWIA200717840 1 20070223 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCONNECTED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 917SW 7641 FOUND EMERGENCY EXIT SIGN AT FLOOR AND MAIN CABIN DOOR DOES NOT ILLUMINATE. SECURED CONNECTOR TO EMERGENCY EXIT AND PAX ENTRY FLOOR SIGN. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007030900066 20070309 00066 EA 2007 3 9 SWIA200717842 1 20070221 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 944SW 7764 FOUND CEILING LEVEL EMERGENCY FLOOD LIGHT JUST FORWARD OF LAV INOP. RELAMPED CEILING EMERGENCY FLOODLIGHT IAW AMM 33-42 -04. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007030900067 20070309 00067 SO 2007 3 9 ECI10517 1 20070221 A 2752 1159SCC21215 ACTUATOR GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6108 NE T/E FLAP MALFUNCTIONED E E0XA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 35 919CT 673 1051 ON TEST FLIGHT, FLAPS RETRACTED WITH LOUD NOISE AND CAME OUT OF ASYMMETRY. REMOVED AND REPLACED LT OB ACTUATOR. 2 L 7 2 4F 4 F RT A12EA E25NE 2007030900068 20070309 00068 SO 2007 3 9 SIMA200705901 1 20070224 A 5280 14537886401 DOOR EMB 145 EMB145LR 3260212 SO MLG DAMAGED A SIMA O OTHER O OTHER LD LANDING 1 SW 21 648AE 15883 145225 UPON LANDING AT APPROXIMATELY 90 KNOTS A HEAVY CROSS WIND BLEW THE AIRCRAFT OFF THE RUNWAY. PASSENGERS WERE DEPLANED BY AIRSTAIRS, POST INSPECTION REVEALED DAMAGED TO THE LEFT AND RIGHT NOSE LANDING GEAR DOORS AND TO THE NR 2 VHF ANTENNA. PERFORMED HIGH SIDE LOAD INSPECTION IAW AMERICAN EAGLE WORK CARD 05-200-02 WITH NO DEFECTS NOTED. REMOVED AND REPLACED BOTH NOSE LANDING GEAR DOORS IAW EMB AMM 32-20-05, OPERATIONAL CHECKED GOOD. REMOVED AND REPLACED NUMBER 2 VHF ANTENNA IAW EMB AMM23-12-04, OPERATIONAL CHECK GOOD. RECONTOURED DENT AFT OF NUMBER 2 VHF ANTENNA IAW EMB IC2007-145/01374. P ERFORMED OPERATIONAL CHECK OF EXTENSION/RETRACTION SYSTEM WITH NO DEFECTS NOTED. PERFORMED FUNCTIONAL CHECK OF LANDING 2 L 7 2 4T RT T00011AT 2007030900071 20070309 00071 SO 2007 3 9 SIMA200705902 1 20070227 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 909AE 4803 14500899 FOUND OMEGA BEAM CORRODED AT FRAME 20. FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS. CLEANED, TREATED AND REST ORED PROTECTIVE FINISH IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007030900074 20070309 00074 GL 2007 3 9 DJFA2007024 2 20070226 A 7230 23066437 FAN BLADE EMB 135 EMB135BJ 3260306 SO ALLSN AE300 AE3007A GL NR 2 ENGINE DAMAGED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 910LX 1014 14500952 CAE312906 ON A WALK AROUND MX FOUND 2 ENGINE FAN BLADES ON NR 2 ENGINE WITH THE TIPS CURLED. MX REMOVED 4 ENGINE FAN BLADES PN NR 23065323 AND INSTALLED 2 - KITS OF MATCHED PAIRS OF BLADES PN 23066437. 2 L 7 2 4F 4 F RT TE6CH 2007030900075 20070309 00075 CE 2007 3 9 DJFA2007025 1 20070228 A 7830 ARM BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE THRUST REVERSER CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 408CW RK108 DURING A SCHEDULED MAINTENANCE EVENT, MAINTENANCE DISCOVERED A LARGE CRACK ON THE UPPER OB THRUST REVERSER ARM OF THE LT ENGINE. SDR WILL BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION. 2 H 7 2 4F 4 F RT A16SW E25EA 2007030900076 20070309 00076 NM 2007 3 9 AMTA200700112 1 20070216 A 4920 APU BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE APPU BAY SHUTDOWN A AMTA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 560TZ 33525 APU AUTO SHUTDOWN. OIL QTY, EICAS MSG (APU OIL QTY). REMOVED AND REPLACED APU IAW M57-49-02. OPS AND LEAK CHECKED GOO D. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007030900077 20070309 00077 NE 2007 3 9 DXTA200702003 2 20070307 A 7297 TERMINAL CESSNA 680 680CE 2076811 CE PWA JT15 JT15D5 52112 NE ENGINES BROKEN E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 384QS 6800110 (HIGH PRESS VALVE FAIL -R) CAS MESSAGE ILLUMINATED PRIOR TO ROTATION DURING TAKEOFF. CAS MESSAGE ONLY REMAINED ILLUMINAT ED FOR APPROX 15 MINS. DURING CLIMB-OUT, NR 1 ENG BEGAN TO SURGE WITH N1 FLUCTUATIONS OF 10-15 PERCENT FOR APPROX 20-30 SECONDS. ENG ANTI -ICE SWITCH ON. DURING CLIMB-OUT, NR 2 ENG BEGAN TO SURGE WITH N1 FLUCTUATIONS OF 10-15 PERCENT FOR A PPROX 20-30 SECS. ENG ANTI-ICE SWITCH ON. DURING APPROACH FLAPS FAILED AT 7 DEGREES & COULD NOT BE RESET. DUE TO AN EM ERGENCY, OVERWEIGHT LANDING MADE AT 27,600 LBS. REPLACED BROKEN GROUND TERMINAL GE-003 IAW 680 M/M 20-10-06 OPS CHECK GO OD. 2 L 7 2 4F 4 F RC T00012WI E25EA 2007030900078 20070309 00078 EA 2007 3 9 N6WA00702002 1 20070223 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE CABIN INOPERATIVE A N6WA K NONE L NO TEST IN INSP/MAINT 1 CE 03 156GJ 10227 CEILING LEVEL EMERGENCY LIGHT INOPERATIVE, DEFERRED LIGHT IAW MEL 33-51-01-2A. 2 L 7 2 4F 4 F RT A21EA E15NE 2007030900080 20070309 00080 WP 2007 3 9 I5HA0758004 1 20070207 A 5754 900623401 SLAT CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13 03004 GL WING BIRD STRIKE A I5HA B EMER. DESCENT E F VIBRATION/BUFFET FLT CONT AFFECTED AP APPROACH 1 GL 23 584 24 ON APPROACH, THE CREW FELT A VIBRATION AND A SEVERE PULL TO THE LEFT. THEY DECLARED AN EMERGENCY. AFTER LANDING AND GO ING TO THE PARKING SPOT, THE CREW DETERMINED THAT THEY HAD BEEN STRUCK BY A BIRD ON THE LT IB WING (LEADING EDGE). MAIN TENANCE WAS CALLED AND THEY MADE A COMPLETE INSPECTION OF THE AIRCRAFT. NO OTHER DAMAGE WAS NOTED. MAINTENANCE REMOVED AND REPLACED THE LT LEADING EDGE AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4R 4 T 6A6 E282 2007030900081 20070309 00081 CE 2007 3 9 DXTA200701967 1 20070226 A 3260 WARNING LIGHT BEECH MU300 400A 1155402 CE COCKPIT ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 123QS RK486 RED LIGHT ON GEAR HANDLE REMAINS ON WHEN GEAR IS RETRACTED. GEAR WAS CYCLED AND RED LIGHT REMAINED ILLUMINATED. 2 H 7 2 4F RT A16SW 2007030900082 20070309 00082 CE 2007 3 9 DXTA200701969 1 20070227 A 3243 982813 MASTER CYLINDER CESSNA 560 560XL 2076702 CE PWA 530 PW535A NE BRAKE SYS BYPASSING E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 639QS 5988 5605139 CAPTAINS LT BRAKE IS VERY SPONGY BUT WILL CATCH AFTER ALMOST FULL DEPRESSION. REMOVED AND REPLACED PILOT'S LT AND RT BR AKE MASTER CYLINDERS AND BLED SYSTEM IAW MM 32-42, OPS AND LEAK CHECK GOOD. PERFORMED TAXI CHECK, NO DEFECTS FOUND. 2 L 7 2 4F 4 F RT A22CE E00053EN 2007030900084 20070309 00084 NM 2007 3 9 NWAA070605502 1 20070218 A 2130 UNKNOWN BOEING 757 757251 1384970 NM UNKNOWN A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 502US 23191 AFTER LEVEL OFF AT FL350 CABIN ALTITUDE HORN AND LIGHT CAME ON. CABIN ALTITUDE WAS OBSERVED TO BE CLIMBING THROUGH 11,0 00 FEET. EMERGENCY DESCENT WAS ACCOMPLISHED. OVERWEIGHT LANDING ACCOMPLISHED AT 202,500 LBS. TROUBLESHOT PER FIM 21-5 1-00. PERFORMED PACK CONTROLLER BITE TEST. NO DEFECTS NOTED. RESET PACK CONTROLLERS. PACKS OPERATE NORMALLY IAW AMM 21-51-00. CHECKED AIRFRAME FOR LEAKS IAW AMM 05-51-24, NO SIGNIFICANT LEAKS NOTED. AIRCRAFT PRESSURIZES NORMALLY ON GR OUND. RAN ENGINES AT IDLE TO VERIFY SUFFICIENT BLEED AIR SUPPLY. NO DEFECTS NOTED. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2007030900085 20070309 00085 EA 2007 3 9 SWIA200717827 1 20070220 A 5610 601R330331 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 NM 07 416SW 11 11 7089 FOUND LEFT WINDSHIELD CRACKED. REPLACED LEFT WINDSHIELD IAW RII 56-220-1000. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007030900087 20070309 00087 EA 2007 3 9 SWIA200717829 1 20070220 A 2120 UNKNOWN CNDAIR CL600 CL6002D24 1390016 EA CABIN ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 608SK 10252 AFTER STARTING APU A STRONG FUEL ODOR FILLS CABIN. OPERATED THE APU FOR SEVERAL MINUTES BUT UNABLE TO DUPLICATE. OPERA TIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007030900089 20070309 00089 EA 2007 3 9 A6WA200740057 1 20070213 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA LT & RT DIRTY A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 407AW 7424 SMOKE TOILET CAUTION MESSAGE DURING CLIMB-OUT. COMPLIED WITH QRH, AIR RETURN TO PHL. NO OVERWEIGHT LANDING 41,000 LBS, NO VISUAL SMOKE IN LAV OR CABIN. INSPECTED LAV, FOUND SMOKE DETECTOR OK. PERFORMED OPS CHECK IAW AMM 26-16-01-710-80 1. NO DEFECTS NOTED. REMOVED AND REPLACED LEFT AND RIGHT COALESCER BAGS IAW AMM 21-51-13. OPS CHECK GOOD. NO SMOKE N OTED. (M) 2 L 7 2 4F RT A21EA 2007030900090 20070309 00090 SO 2007 3 9 SWIA200717831 1 20070223 A 5410 SUPPORT EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 232SW 120306 FOUND LEFT NACELLE WHEEL WELL LOWER SUPPORT FRAME (STRINGER NR 1) IS CRACKED, DISCOVERED DURING ROUTINE INSPECTION. REP LACED LOWER OUTBOARD SUPPORT FRAME IAW EMB 120 SRM 51-10-02. 2 L 7 2 4T RT A31SO 2007030900092 20070309 00092 EA 2007 3 9 A6WA200740076 1 20070222 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 450AW 7823 FOUND LT FLOOR SUPPORT ANGLE IS CRACKED 1 INCH AT FS 621, WL 73, LBL 41. (M) MAINTENANCE REPAIRED CRACKED FLOOR SUPPOR T ANGLE BY REMOVING DAMAGED AREA AND INSTALLING REPAIR ANGLE AND STRAP IAW REO 601R-53-61-117 REV C. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007030900093 20070309 00093 EA 2007 3 9 A6WA200740070 1 20070221 A 5320 S6144A14 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT FS484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 448AW 7814 FOUND FS 484 ANGLE IS CRACKED AT RBL 36. (M) MAINTENANCE REPLACED ANGLE IAW REO 601R-53-41-059. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007030900096 20070309 00096 SO 2007 3 9 SWIA200717833 1 20070102 A 5310 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 393SW 120330 FOUND CORROSION AT PASSENGER DOOR ENTRANCE BUTTSTRAP, DISCOVERED DURING C-CHECK INSPECTION. REPLACED BUTTSTRAP AT PASSE NGER DOOR ENTRANCE IAW SRM 51-10-02 PG 3 SEC 3A. 2 L 7 2 4T RT A31SO 2007030900097 20070309 00097 SO 2007 3 9 SWIA200717834 1 20070102 A 5310 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 393SW 120330 FOUND CORROSION AT CARGO DOOR ENTRANCE BUTTSTRAP, DISCOVERED DURING C-CHECK INSPECTION. REPLACED BUTTSTRAP AT CARGO DO OR ENTRANCE IAW SRM 120 51-10-02 PG 3 SEC 3A. 2 L 7 2 4T RT A31SO 2007030900098 20070309 00098 EA 2007 3 9 A6WA200740075 1 20070221 A 2910 601R75262159 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 450AW 7823 FOUND LT MLG WHEEL WELL HYDRAULIC TRANSDUCER HAT CHANNEL P/N 601R75262-159 CRACKED APPROX .05 INCH LONG. (M) MAINTENAN CE REMOVED AND REPLACED CHANNEL PN 601R75262-159 IAW SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007030900099 20070309 00099 SO 2007 3 9 SWIA200717835 1 20070102 A 5310 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 393SW 120330 FOUND CORROSION AT RIGHT AND CENTER BUTTSTRAPS NEAR LAV AREA, DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT AND CENTER BUTTSTRAPS NEAR LAV AREA IAW SRM 120 51-10-02 PG 3 SEC 3A. 2 L 7 2 4T RT A31SO 2007030900100 20070309 00100 SO 2007 3 9 SWIA200717836 1 20070102 A 5210 STRUCTURE EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 393SW 120330 PAX DOOR HAS A CRACK UNDER LOCK FASTENER FWD AND AFT STRINGER NEXT TO 3RD STEP, DISCOVERED DURING C-CHECK INSPECTION. R EPLACED CRACKED BRACKETS ON PAX DOOR SECURED IAW EMB 120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2007030900102 20070309 00102 EA 2007 3 9 A6WA200740069 1 20070221 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 448AW 7814 FOUND FS 484 ANGLE IS CRACKED AT LBL 36. (M) MAINTENANCE REPLACED ANGLE IAW REO 601R-53-41-059. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007030900104 20070309 00104 EA 2007 3 9 A6WA200740073 1 20070221 A 2910 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE RT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 450AW 7823 FOUND RT MLG WHEEL WELL HYDRAULIC LINE SUPPORT BRACKET P/N 601R75262-155 CRACKED APPROX .1 INCH LONG. (M) MAINTENANCE REMOVED AND REPLACED BRACKET ASSY PN 601R75262-153 IAW SRM 51-42-06. 2 L 7 2 4F 4 F RT A21EA E15NE 2007030700240 20070307 00240 WP 2007 3 7 07FDEA00580 1 20070227 A 5310 DOOR FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 FOUND EXISTING REPAIR MAIN CABIN L3 DOOR JAMB FROM STA 1305 TO STA 1315 BETWEEN LONGERONS 26 AND 27 LT. AFTER AN ASSES SMENT OF THIS REPAIRED WAS DETERMINATED DOEN`T COMPLY WITH SRM REQUIREMENTS, THEREFORE, REMOVED AND DISCARDED REPAIRED. FABRICATED AND INSTALLED NEW REPAIR IAW SRM 53-50-00 FIG 19 VOL 1. 2 L 7 3 4F A22WE 2007030800009 20070308 00009 WP 2007 3 8 07FDEA00605 1 20070227 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 FOUND EXTERNAL FUSELAGE AT STA 1219 BTWN LONG NR 51 LT TO 51 RT EXISTING REPAIR DOUBLER. REMOVED EXISTING DOUBLER IAW S RM 51-35-01 VOL2. REPAIRED IAW SRM 53-20-00 FIG 6 SHT 3-4 VOL 1 AND INSTALLED DOUBLER AND FITTING IAW SRM 51-35-01 PAG 1-13 VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I026042/N01042 AND SRM 53-20-00 FIG 6 VOL 1. 2 L 7 3 4F A22WE 2007030800014 20070308 00014 NM 2007 3 8 07FDEA00633 1 20070303 A 5713 STRINGER DOUG MD11 MD11 3023602 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 CRACK FOUND AT STRINGER END 9L (XORS 819), APPROX 10" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. SUPPLEMENTAL 21 MARCH 07, CRACK ON STRINGER END 9L (XORS 819) SLOTTED OUT AND REPAIRED WITH ANGLES AS PER SRM 57-20 -00 FIGURE 10 VO LUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007030800034 20070308 00034 WP 2007 3 8 IXXA07SMN024S 1 20070113 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND AN IMPROPER REPAIR AT STATION FS 1693, LONGERON 27 LEFT. REMOVED EXISTING REPA IR REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATED REPA IR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW DOUGLAS DRAWING SR08530032 WIT H APPROVED DEVIATIONS, SEMAN DRAWING ED-4469 DATED 02-16-07, BOEING MESSAGE NUMBER 1-288540577-7 DATED 02-15-07, ATI ENG INEERING ORDER NUMBERDC8-3729 DATED 02-05-07, AD-DC8-2007-02-02,SB-DC8-53A080, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 ND T SPM PART 06-10-01-001 AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007030800038 20070308 00038 WP 2007 3 8 IXXA07SMN004S 1 20070113 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND EXISTING REPAIR AT STATION FS104, LONGERON 35 LEFT DOES NOT MEET DTA REQUIREMEN TS OF MDC91K0262 REPORT. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TR EATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-1 FIGURE 7 SHEET 1 AND 2, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 53-4-1 FIGURE 1 ITEM "C", DC8 SRM 51-9-0 FIGURE 68A, DC8 SRM 51-1-8B, DC8 SRM 51-1-11 AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007030800039 20070308 00039 WP 2007 3 8 IXXA07SMN026S 1 20070113 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND AN IMPROPER REPAIR FROM STATION FS 290 TO STATION FS 330 LONGERON 30, REMOVED E XISTING REPAIR. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND, AFTER DAMAGE REMOVED. FABRICATED REPAIR PARTS . CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS. IAWDC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-3-1, AD 2005-18-07, BOEING MESSAGE NUMBER 1-274569452-5 DATED 01- 17-07, BOEING MESSAGE NUMBER 1-290998891-2 DATED 01-17-07, SEMAN DRAWING NUMBER ED-4414 DATED 01-17-07 AND ATI ENGINEERI NG ORDER 53-DC8-2452. COMPLETED FAA FORM 8110-9 DATED 02-17-07. 2 L 7 4 4F RT 4A25 2007030800061 20070308 00061 WP 2007 3 8 IXXA07SMN034S 1 20070119 A 5753 SKIN PANEL DOUG DC8 DC871F 302199D WP T/E FLAP MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP SKIN PANEL HAS A NON STANDARD REPAIR FROM STATION XW104.000 T O STATION XW108.000. REMOVED SKIN PANEL WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN PANEL AND INTERNAL BOND ED DOUBLERS. BONDED REPAIR PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN PANEL INTERNAL SU RFACE. APPLIED SEALANT TO FAYING SURFACES. INSTALLED PANEL IAW DC8 SRM 57-7-1 FIGURE 1 PAGE 2, DC8 SRM 57-1-0, PAGE 1, DC8 SRM 51-1-21, DC8 SRM 57-7-1 FIGURE 1 PAGE 2 ITEM "A", "L" AND "R" DC8 SRM 51-1-9, DC8 SRM 51-1-8B AND DC8 SRM 51-1- 11. 2 L 7 4 4F RT 4A25 2007030800064 20070308 00064 WP 2007 3 8 IXXA070010S 1 20070223 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING-EXTERNAL UPPER SKIN CRACKED AT STATION XRS74.000 STRINGER 14. REMOVE D FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATED REPAIR DOUBLER AND FILLERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPL IED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW DC8 SRM 57-2-1 FIGURE 10 SHEET 3, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 57-3-1 FIGURE 10 PAGE 17 ITEM "A", DC8 SRM 51-10-0, FIGURE 1 SHEET 6, D C8 SRM 51-1-8B, DC8 SRM 51-1-12 AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007030800069 20070308 00069 EU 2007 3 8 NSVA20070035 1 20070213 A 2697 CONNECTOR SAAB SF340 340B 7860101 EU OVERHEAT SYS DIRTY A NSVA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 EA 27 339CJ 339 FOUND LT ENG TAILPIPE HOT LIGHT ILLUMINATED. REDUCED POWER LIGHT DID NOT GO OUT. CLOSED BLEEDS LIGHT STILL NOT OUT. SHUT ENGINE DOWN LIGHT STILL ON. CLEANED ALL CONNECTION TO OVERHEAT DETECTORS, PERFORMED ADJ/TEST IAW AMM 25-12-00, OPS CHECK GOOD. NO FAULTS AT THIS TIME. 2 L 7 2 4T RT A52EU 2007030800108 20070308 00108 2007 3 8 QXEA200700353 4 20070306 A 3417 7000700976 ADC DHAV DHC8 DHC8202 2809007 NM NR 2 MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 366PH 19586 19586 510 PDX - ON FLIGHT 2096, RETURNED TO FIELD, FO'S ALTIMETER FLAGGED OFF AND FD DADC MESSAGE WITH ADC INPUT FAIL MESSAGE FROM FMS. SAME SEQUENCE OCCURRED TWICE. MAINTENANCE REMOVED AND REPLACED THE NR 2 ADC. OPERATIONAL TEST GOOD. AIRCRAFT R ETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030800113 20070308 00113 2007 3 8 QXEA200700210 4 20070218 A 3452 626523205 CONTROL HEAD DHAV DHC8 DHC8202 2809007 NM ATC TRANSPONDER MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 357PH 8186 504 SEA FLIGHT NR 2262 - ATC ADVISED THEY HAD NO TRANSPONDER ON RADAR. TRANSPONDER TRIED IS ON, NR 1 AND NR 2 POSITION, REP LY LIGHT NORMAL. MAINTENANCE REPLACED ATC CONTROL HEAD UNIT. PERFORMED ATCBS/MODE-S TRANSPONDER TEST IAW TASK CARD 934 5001. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030800115 20070308 00115 NM 2007 3 8 QXEA200700209 1 20070216 A 2760 SWITCH DHAV DHC8 DHC8202 2809007 NM SPOILER SYS MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 351PH 490 SEA FLIGHT NR 2020 - ROLL SPOILER HYDRAULIC CAUTION LIGHT ILLUMINATED ON TAXI OUT. MASTER CAUTION UNABLE TO BE RESET. ALL HYDRAULIC INDICATIONS NORMAL. MAINTENANCE REPLACED NR 1 ROLL SPOILER LOW PRESSURE SWITCH. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030800128 20070308 00128 NM 2007 3 8 QXEA200700330 1 20070228 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND 2 DENTS IN FUSELAGE SKIN AT STATION X302.00 AND 1.25" ABOVE THE LEFT ICE SHIELD, BETWEEN STRINGER 4L AND 5L. REPAIRED IAW RD8-53-9488. 2 H 7 2 4T RT A13NM 2007030800140 20070308 00140 NM 2007 3 8 QXEA200700312 1 20070222 A 5330 DOUBLER DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - CHAFE ON EXTERIOR SKIN DOUBLER AROUND LAVATORY SERVICE DOOR AT AFT SIDE OF DOOR CUTOUT. REPAIRED IAW SRM 51-20 -11. 2 H 7 2 4T RT A13NM 2007030800141 20070308 00141 NM 2007 3 8 QXEA200700313 1 20070224 A 5753 BUSHING DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND LEFT NR 4 FLAP TRACK INBOARD HANGER UPPER BOLT BUSHING IS CORRODED. REPAIRED IAW DHC-8 200 AMM 57-50-42. 2 H 7 2 4T RT A13NM 2007030800143 20070308 00143 EA 2007 3 8 SWIA200717866 1 20070301 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 907SW 7511 AN EMERGENCY LIGHT INOP IN MAIN CABIN CEILING. RELAMPED EMERGENCY LIGHT BETWEEN ROW 4 AND 5 AS REQUIRED, OPS CHECK GOOD . 2 L 7 2 4F RT A21EA 2007030800144 20070308 00144 SO 2007 3 8 SWIA200717867 1 20070301 A 2450 RELAY EMB 120 EMB120ER 3260203 SO E&E BAY NOISY A SWIA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 213SW 120277 FOUND NOISE FROM RELAY IN RIGHT SIDE ELEC BAY, LAV SMOKE ALARM WENT OFF ALONG WITH OVERHEATED SMELL IN CABIN. REPLACED RELAY K0194, NR 2 SHOCK RELAY. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007030800145 20070308 00145 EA 2007 3 8 SWIA200717868 1 20070301 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 405SW 7029 FOUND FLOOR LEVEL EMERGENCY LIGHTS AFT OF ROW 8 ARE INOP. SECURED CONNECTOR AT ROW 12. OPERATIONAL CHECKS GOOD.. 2 L 7 2 4F RT A21EA 2007030800147 20070308 00147 EA 2007 3 8 SWIA200717870 1 20070228 A 3222 SEAL CNDAIR CL600 CL6002B19 1900309 EA NLG STRUT LEAKING A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 927SW 7693 UPON ROTATION GOT NOSE GEAR DOOR WARNING AND GEAR DISAGREE. CYCLED GEAR WITH NO CHANGE. RETURNED TO DEN REPACKED NOSE STRUT SEALS PER CRJ 200 MM 32-21-20 AND SERVICED STRUT IAW 12-12-32. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007030800164 20070308 00164 EA 2007 3 8 QXEA200700352 1 20070306 A 3250 523506 ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA NLG STEERING MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 604QX 13624 10019 SEA - FLIGHT 2480 - AFTER TAKEOFF RECEIVED A GEAR DISAGREE WARNING MESSAGE AND PROX SYSTEM FAULT MESSAGE. RETURNED TO T HE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE PERFORMED A GENERAL VISUAL INSPECTION WITH NO DEFECTS NOTED . ALSO, PERFORMED A HEAVY LANDING INSPECTION WITH NO DEFECTS NOTED. PLACED INDICATION ON MEL 32-30-1. MEL CLEARED 3/7 /07 BY REPLACING THE STEERING ACTUATOR AND THE SWIVEL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007030800166 20070308 00166 EA 2007 3 8 SWIA200717884 1 20070115 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7853 FOUND LBL9 UPPER FLOOR SUPPORT CRACKED AT RIVET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FILLER AND SPLICES AT STA 280 LBL9 UPPER FLOOR SUPPORT PER BOMBARDIER REO 601R-53-11-138. 2 L 7 2 4F RT A21EA 2007030800173 20070308 00173 EA 2007 3 8 SWIA200717891 1 20070115 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7853 FOUND FLOOR SUPPORT ANGLE CRACKED LT CORNER, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED STRAP AND ANGLE PER CRJ200 REO 601R-53-61-117 REV C. 2 L 7 2 4F RT A21EA 2007030900008 20070309 00008 EA 2007 3 9 SWIA200717892 1 20070115 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7853 FOUND FLOOR SUPPORT ANGLE CRACKED RT CORNER FS 621.0 WL 73.50, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE AN D STRAP PER CRJ200 REO 601R-53-61-117 REV C. 2 L 7 2 4F RT A21EA 2007030900010 20070309 00010 EA 2007 3 9 SWIA200717894 1 20070115 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7853 FOUND PAX DOOR AFT DRAG ANGLE IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS ON AFT SIDE OF P AX DOOR PER REO 601R-52-11-513. 2 L 7 2 4F RT A21EA 2007030900019 20070309 00019 EA 2007 3 9 SWIA200717903 1 20070123 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 970SW 7881 FOUND FS 484 LBL 36 INTERCOSTAL BRACKET CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE AT FS 484 PER RE O 601R-53-41-059 REV A. 2 L 7 2 4F RT A21EA 2007030900033 20070309 00033 NM 2007 3 9 QXEA200700338 1 20070305 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM TE FLAP UNKNOWN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND LEFT OUTBOARD FLAP UPPER INBOARD SURFACE HAS CHAFE ON PREVIOUS REPAIR. REPAIRED IAW SRM 51-20-91, 51-20- 11, AND RD8-57-1734. 2 H 7 2 4T RT A13NM 2007030900040 20070309 00040 WP 2007 3 9 070042 1 20070215 A 3397 POWER SUPPLY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS MISWIRED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 863GA 49911 DURING A ROUTINE OVERNIGHT SERVICE CHECK LAS VEGAS MAINTENANCE REPORTED THAT THE OVERWING HATCH EXIT SIGNS WOULD NOT SHU T OFF. FOUND POWER SUPPLY (NOT IDENTIFIED) MISWIRED AT THE TERMINAL STRIP. CORRECTED WIRING. OPERATIONAL CHECK GOOD P ER AMM 33-53-00. AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007030900052 20070309 00052 WP 2007 3 9 070047 1 20070222 A 5210 SKIN DOUG DC9 DC983 3022083 WP PAX DOOR GROUND DAMAGE A WX0A O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 WP 19 865GA 49998 FLIGHT 461 PIA/LAS - AFTER PASSENGER LOADING, BEFORE PUSHBACK, AN EFFORT WAS MADE TO CLOSE THE MAIN ENTRY DOOR BUT IT WA S RESTING ON THE JETWAY DECK. THE JETWAY OPERATOR RETRACTED THE JETWAY WITHOUT LOWERING IT. AS A RESULT, THE L1 DOOR S KIN SUSTAINED A .5 BY .6 INCH AREA OF DAMAGE. THE AIRPLANE WAS PREPARED FOR FERRY AND WAS DELIVERED TO TULSA WHERE AMER ICAN AIRLINES ACCOMPLISHED A PERMANENT REPAIR OF THE L1 DOOR IN ACCORDANCE WITH ESO NR 80559 DATED 22 FEB, 2007. HFEC I NSPECTION REVEALED NO CRACKS. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007030900056 20070309 00056 NM 2007 3 9 QXEA200700308 1 20070223 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 543 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND LEFT INBOARD SEAT TRACK IS GOUGED AT STATION X543. REPAIRED IAW RD8-53-4936 AND SRM 51-20-16 AND 51-20-3 6. 2 H 7 2 4T RT A13NM 2007030900069 20070309 00069 EA 2007 3 9 SIMA200705904 1 20070128 A 5315 CC670341757 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 519AE 7877 4800 10131 FOUND FLOORBEAM AT STATION 280 CORRODED ALONG BUTT LINE 24L TO 42R. SPLICED IN FRAME 280 AND EXTENSION MOUNTS IAW AMERI CAN EAGLE ENGINEERING ORDER CR-53-MR-105. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007030900086 20070309 00086 EA 2007 3 9 SWIA200717828 1 20070221 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN BURNED OUT A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 806SK 15070 NR 6 OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED MID CABIN EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007030900088 20070309 00088 EA 2007 3 9 SWIA200717830 1 20070216 A 5610 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 724SK 10189 ALL WINDSHIELD AND SIDE WINDOWS CRACKED ON THE TAKEOFF ROLL. REPLACED ALL FOUR COCKPIT WINDOWS IAW CRJ MM 56-11-01, 56- 12-07 AND RII 56-220-1000 STEPS 1 THROUGH 7 AND 9. LEFT WINDSHIELD P/N OFF: 601R33033-17 S/N OFF: 04202H1409. RIGHT WI NDSHIELD P/N OFF: 601R33033-18 S/N OFF: 04135H4893. LEFT SIDE WINDOW P/N OFF: 601R33033-19, S/N OFF: 0419H9504. RIGHT SIDE WINDOW P/N OFF: 601R33033-20 S/N OFF: 04199H1301. 2 L 7 2 4F RT A21EA 2007030900095 20070309 00095 EA 2007 3 9 A6WA200740074 1 20070221 A 2910 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE RT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 450AW 7823 FOUND RIGHT MLG WHEEL WELL HYDRAULIC TRANSDUCER HAT CHANNEL P/N 601R75262-157 CRACKED APPROX .1 INCH LONG. (M) MAINTENA NCE REMOVED AND REPLACED BRACKET PN 601R75262-157 IAW SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007030900103 20070309 00103 EA 2007 3 9 A6WA200740077 1 20070222 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 450AW 7823 FOUND RT FLOOR SUPPORT ANGLE IS CRACKED 1 INCH AT FS 621, WL 73, RBL 41. (M) MAINTENANCE REPAIRED FLOOR SUPPORT ANGLE AT FS 621 IAW REO 601R-53-61-117 REV C. 2 L 7 2 4F 4 F RT A21EA E15NE 2007030900107 20070309 00107 EA 2007 3 9 A6WA200740078 1 20070222 A 5320 S6144A14 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LH FS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 450AW 7823 FOUND FS 484 INTERCOSTAL CRACKED APPROX .1 INCH LONG AT LBL 36. (M) MAINTENANCE REMOVED DAMAGED FLANGE AND INSTALLED R EPAIR ANGLE IAW REO 601R-53-41-059 REV A AND BSC STANDARD REPAIR 601R-53-0030A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007030900108 20070309 00108 EA 2007 3 9 A6WA200740079 1 20070222 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 450AW 7823 FOUND FS 484 INTERCOSTAL ANGLE CRACKED APPROX .1 INCH LONG AT BL 27. (M) MAINTENANCE REMOVED AND REPLACED ANGLE IAW BS C STANDARD REPAIR 601-53-0029B. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007030900110 20070309 00110 EA 2007 3 9 A6WA200740072 1 20070224 A 5711 SPAR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE WING MISDRILLED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 448AW 7814 WHILE PERFORMING E03/062/457 MODIFICATION LT AND RT WING REAR SPARS, A FASTENER HOLE WAS MISDRILLED. HOLE DIAMETER .213 INCH AT TRAILING EDGE WS 129, 2 INCHES IB OF JACKING PAD POINT ON RT WING. (M) MAINTENANCE REAMED HOLE TO ACCOMMODATE .25 INCH HOLE TO BE COLD WORKED AND INSTALLED HST11A68 HI-LITE IAW BSC EO 601R-57-10936. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007030900121 20070309 00121 EA 2007 3 9 SWIA200717848 1 20070108 A 5310 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 336 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 PAX DOOR FRAME FS336 HAS A CRACK ON INNER FLANGE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW FRAME PER CRJ200 SRM 51-42-06 AND SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007030900123 20070309 00123 EA 2007 3 9 SWIA200717849 1 20070108 A 5310 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 321 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 PAX DOOR FRAME FS321.5 IS CRACKED ON INNER FLANGE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FRAME INSERT, SPLICE S, SHIM AND CLEAT PER REO 601R-52-11-402. 2 L 7 2 4F RT A21EA 2007030900124 20070309 00124 EA 2007 3 9 SWIA200717850 1 20070108 A 5310 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 323 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 PAX DOOR FRAME FS 323.5 IS CRACKED ON INNER FLANGE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW FRAME PER CRJ20 0 SRM 31-42-06 AND SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007030900125 20070309 00125 EA 2007 3 9 SWIA200717851 1 20070108 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 625 S14R CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FOUND RT STRINTER 14 AT STATION 625 CLIP IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CRACKED CLIP AT RT STRINGER 14STD625 AND WITH INTERCOSTAL PER CRJ200 SRM 51-42-06 PG 11. 2 L 7 2 4F RT A21EA 2007030900128 20070309 00128 EA 2007 3 9 SWIA200717852 1 20070108 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 625 S14L CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FOUND LT STR14 AT STATION 625 CLIP IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CRACKED CLIP AT LT STRING ER STA 625 AND WITH INTERCOSTAL PER CRJ200 SRM 51-42-06 PG 11,18. 2 L 7 2 4F RT A21EA 2007030900130 20070309 00130 EA 2007 3 9 SWIA200717854 1 20070108 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 625 S13R CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FOUND CRACK IN RADIUS OF CLIP AT STA625.00 STR 13R, BL 50.000 REF DRAWING 601-35012, DISCOVERED DURING C-CHECK INSPECTIO N. REPLACED CLIP PN 601-35012-45 PO 75630 AT STA 625-00 STR13R, BL50.000 PER CRJ200 SRM 51-40-06 PG 12. 2 L 7 2 4F RT A21EA 2007030900136 20070309 00136 EA 2007 3 9 SWIA200717910 1 20070128 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 446SW 7666 PAX DOOR AFT WEB/CRACKED UNDER HANDRAIL, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED HANDRAIL SUPPORT FITTING FOR P AX DOOR AFT WEB PER SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007030900137 20070309 00137 EA 2007 3 9 SWIA200717911 1 20070128 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 FWD SIDE OF PAX DOOR CRACK TOP OF DOOR OPEN BENEATH TOP FOLDING STEP, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED R EPAIR ANGLE AND FILLER AT PAX DOOR FWD SIDE TOP STEP PER CRJ200 REO 601R-52-11-279. 2 L 7 2 4F RT A21EA 2007030900138 20070309 00138 EA 2007 3 9 SWIA200717912 1 20070128 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 PAX DOOR HANDLE CRACKED OUTER, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED OUTER HANDLE ASSY, SPLINED SHAFT AND HAN DLE FLAP IAW CRJ200 AMM 52-11-03-400-802. 2 L 7 2 4F RT A21EA 2007030900139 20070309 00139 EA 2007 3 9 SWIA200717913 1 20070128 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 LBL9 STA 280 UPPER FLOOR SUPPORT HAS CRACK, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FILLER ANGLE AND REPAIR SPL ICE ANGLE PER REO 601R 53-11-136 REV 'C' SHT 1-4. 2 L 7 2 4F RT A21EA 2007030900141 20070309 00141 EA 2007 3 9 SWIA200717914 1 20070128 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 LBL9 STA 280 LWR FLOOR SUPPORT HAS CRACK, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE, REPAIR ANGLE, CLIPS AN D FILLERS PER REO 601R-53-11-171 REV C SHEET 1-2. 2 L 7 2 4F RT A21EA 2007030900142 20070309 00142 EA 2007 3 9 SWIA200717915 1 20070128 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 RBL9 LWR FRAME CRACKED AT FS 280, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR FILLER ANGLE AND SPLICE AT FS 280 RBL 9 AS PER REO 601R-53-11-136 REV C SHEET 1-4. 2 L 7 2 4F RT A21EA 2007030900144 20070309 00144 EA 2007 3 9 SWIA200717917 1 20070128 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 FS 625 RT SIDE CLIPS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP DW 9310 P/N 601-35012-52 P/O 720 55 PER REO 601R-53-61-422. 2 L 7 2 4F RT A21EA 2007030900146 20070309 00146 EA 2007 3 9 SWIA200717919 1 20070128 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 STA 484 RBL 36 INTERCOSTAL CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLE TO FS 484 INTERCOSTAL RBL36 PER CRJ200 SRM 51-42-06 PG 11 AND 51-42-21 PG 17. 2 L 7 2 4F RT A21EA 2007030900151 20070309 00151 CE 2007 3 9 DXTA200701981 1 20070301 A 3230 ROLLER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG LACK OF LUBE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 331QS 5600331 AFTER GEAR RETRACTION, GEAR UNSAFE AND HYDRAULIC PRESS ON LIGHT REMAINED ILLUMINATED. NORMAL INDICATIONS ON GEAR EXTENSI ON. JACKED AIRCRAFT & DUPLICATED FAULT FOUND LH MLG UPLOCK ROLLER NOT COMPLETELY ENGAGED ON UPLOCK HOOK. CLEANED & LUB ED UPLOCK ROLLER & ADJUSTED LT MLG DOOR. CYCLED GEAR 10 TIMES WITH NO FAULTS IAW CE560XL M/M 32-11-01/32-31-05. 2 L 7 2 4F 4 F RT A22CE E25EA 2007030900153 20070309 00153 CE 2007 3 9 DXTA200701982 1 20070301 A 3200 UNKNOWN BEECH MU300 400A 1155402 CE MLG WARNING LIGHT E DXTA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 07 122QS RK467 UPON GEAR RETRACTION AFTER MISSED APPROACH IN KASE. RED LIGHT ON GEAR HANDLE REMAINED ON. DRAGGING NOISE DURING REMAINDE R OF FLIGHT TO GRAND JUNCTIONS. GEAR EXTENSION WAS NORMAL. JACKED AIRCRAFT. PERFORMED 15 FAULT FREE GEAR SWINGS IAW 400 A MM 32-00-00. NO DEFECT FOUND AT THIS TIME. CLEANED ALL LANDING GEAR UPLOCK AND DOWN LOCK SWITCHES. DOWNJACKED AIRCRAFT AND SERVICED HYD. SYS I.A.W BEECHJET 400A M/M CH 12 2 H 7 2 4F RT A16SW 2007030900156 20070309 00156 CE 2007 3 9 DXTA200701983 1 20070301 A 2700 UNKNOWN CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE UNKNOWN E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 664QS 5605264 STAB MISCOMPARE AND HYD PRESS LIGHT CAME ON OUT OF APPROX 3000 FT WITH THE GEAR UP AND FLAPS UP SPEED APPROX 220 KTS. R AN CHECKLIST . PULLED HYD CONTROL CB. HYD CONTROL CB. HYD PRESS WENT OUT. CONFIGURED FOR LANDING . WITH FLAPS 15 STAB MISCOMP WENT OUT. PERFORMED TWO-PISTON HORIZONTAL STAB OPERATIONAL CHECK. PERFORMED AIRSPEED SWITCH AND HORIZONTAL STAB OPERATIONAL CHECK. NO DEFECTS NOTED. ALL WORK PERFORMED IAW CESSNA CITATION 560XL MM 27-40-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007030900158 20070309 00158 CE 2007 3 9 DXTA200701984 1 20070301 A 3297 CONNECTOR CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE MLG DIRTY E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 837QS 5600685 WHEN GEAR SELECTED DOWN WE HAS A NOSE AND LT MAIN DOWN INDICATION BUT NO RT AND A GEAR UNLOCK LIGHT STAYED ON. GEAR RE TRACTED ON GO AROUND. WHEN RETRACTED ON GO AROUND. WHEN SELECTING GEAR DOWN AGAIN TO RUN CHECKLIST WE STILL GET NO RIGH T INDICATION AND GEAR UNLOCK LIGHT STAYED ON. PULLED ALT GEAR CONTROL AND BLEW BOTTLE THEN HAD 3 GREEN AND NO RED. SERV ICED EMERG BOTTLE TO RESET & SAFETIED, INSPECTED RT DOWN LOCK CONNECTOR & FOUND VERY DIRTY, CLEANED & BLED HYDRAULIC SYS TEM THEN FROZE SWITCH & CYCLED MANY TIMES WITH NO DEFECTS & PROPER SEQUENCE OBSERVED IAW CESSNA 560 MM 32-01-00 2 L 7 2 4F 4 F RT A22CE E00053EN 2007030900159 20070309 00159 CE 2007 3 9 DXTA200701985 1 20070301 A 2720 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RUDDER UNKNOWN E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 912QS 7500012 AIRCRAFT REQUIRED YAW AND RUDDER TRIM OUTSIDE OF T/O LIMIT IN CRUISE (APPROX 25 PERCENT LT OF CENTER) AND YAWS LT AND RT OUT OF TRIM FOR NO APPARENT REASON IN CRUISE (APPROX .5 BALL). PERFORMED RUDDER TRIM DIRECTION TEST PER CE-750 M/M 27- 14-00 AND VERIFIED PROPER RUDDER RIGGING PER CE-750 M/M 27-20-00. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007030900160 20070309 00160 CE 2007 3 9 DXTA200701986 1 20070301 A 3260 SQUAT SWITCH CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG OUT OF RIG E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 960QS 7500160 DURING TAKEOFF THE GEAR INITIALLY WOULD NOT RETRACT (GEAR HANDLE WOULD NOT MOVE). TRIED SEVERAL TIMES AND IT RETRACTED. FOUND RT SQUAT SWITCH OUT OF RIG. RERIGGED IAW CESSNA 750. MM. CH. 32-60-00. OPS CHECKS GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007030900168 20070309 00168 CE 2007 3 9 DXTA200701980 1 20070228 A 2612 UNKNOWN RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP CARGO FIRE DET UNKNOWN E DXTA O OTHER N FALSE WARNING AP APPROACH 1 GL 07 874QS 258474 BAG FIRE ANNUNCIATOR ILLUMINATED INTERMITTENTLY BELOW 1000 FT AGL ON FINAL APPROACH WENT OUT DURING LANDING, REMAINED OU T DURING TAXI TO RAMP- NO VISUAL INDICATION OR SMELL OF SMOKE. INSPECTED AND CLEANED BAG FIRE SMOKE DETECTOR AS REQUIRE D. PERFORMED SMOKE DETECTION SYSTEM ADJUSTMENT TEST IAW 800XP REPS 26-11-00 REV 36A. MM 800XP REV 13 9/06. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A3EU E6WE 2007030900170 20070309 00170 CE 2007 3 9 GLBA20060913 1 20070219 A 5210 SKIN BEECH 1900 1900D 1154162 CE PAX DOOR DELAMINATED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 195GL UE195 MAJOR REPAIR - UPON ROUTINE INSPECTION MAINTENANCE FOUND A DELAMINATION ON THE AIRSTAIR DOOR SKIN BELOW THE EXTERIOR DOO R HANDLE. MAINTENANCE REPAIRED AIRSTAIR DOOR SKIN IAW BEECH 1900D SRM 52-10. RII COMPLIED WITH PER TC 8.2.1. 2 L 7 2 4T RT A24CE 2007030900171 20070309 00171 CE 2007 3 9 DXTA200701973 1 20070227 A 3213 65415204 STRUT CESSNA 500 560CESSNA 2076750 CE MLG BINDING E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 807QS 3408 5600617 AFTER T/O THE GEAR WOULD NOT RETRACT. INDICATIONS WERE THREE GREEN, UNSAFE DOOR LIGHT AND GEAR HANDLE UP-GEAR HANDLE WAS PLACED BACK DOWN AND WE HAD THREE GREEN, NO RED.JACKED AIRCRAFT AND FOUND RH OLEO STRUT HANGING UP AND NOT ALLOWING RH SQUAT SWITCH TO CONTACT. REPLACED FAULTY OLEO STRUT WITH CUSTOMER SUPPLIED INSPECTED OLEO STRUT. SERVICED STRUT WITH NI TROGEN. CYCLED LANDING GEAR SEVERAL TIMES, OPS TEST GOOD. ALL WORK IAW 560 MM 32-11-02 AND 12-14-01. NOTE: INSTALLED STR UT HAS 781 CYCLES 2 L 7 2 4F RT A22CE 2007030900173 20070309 00173 SO 2007 3 9 C2XA07SH012 1 20070205 A 2611 SMOKE WARNING EMB 145 EMB145LR 3260212 SO CARGO BAY MALFUNCTIONED A C2XA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 27 15574 145639 FL 3130 IAH TO STL - BAGGAGE SMOKE IN FLIGHT AT FL 290 CREW DISCHARGED BOTTLES AND DIVERTED TO SHV. MX INSPECTED THE BA GGAGE COMPARTMENT AREA AND FOUND NO EVIDENCE OF FIRE OR SMOKE. MX R&R FIRE BOTTLES AND PERFORMED OPERATIONAL CHECKS SUC CESSFULLY. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007030900176 20070309 00176 CE 2007 3 9 DXTA200701974 1 20070228 A 2710 991444015 PCU CESSNA 750 750 2076810 CE AILERONS INOPERATIVE E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 948QS 5765 7500149 ON LANDING A "FLIGHT CONTROL FAULT" MESSAGE APPEARED AND THE 'AILERON FLIGHT CONTROL SHUTOFF LIGHT BLINKED. REPLACED "B" PCU (AILERON) , ADJUSTMENT & OPS. IAW. CE 750. M/M CE750. 27-11-05. 2 L 7 2 4J RT T00007WI 2007030900177 20070309 00177 2007 3 9 C2XA07BT023 4 20070301 A 2300 7013270965 RMU EMB 145 EMB145LR 3260212 SO COCKPIT BURNED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 15574 10648 145639 EWR LOG SQUAWK FLT NR 3064 SMOKE DISPERSED FROM DASH FOR 3-5 SECS, THEN STOPPED. FOUND RMU NR 2 BURNT. REMOVED AND REP LACED NR 2 RMU IAW EMB 145 MM 23-81-01. OPS CHECK GOOD. CLOSED 2 L 7 2 4T RT T00011AT 2007030900178 20070309 00178 CE 2007 3 9 DXTA200701979 1 20070228 A 2730 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL ELEVATOR CLACKER UNKNOWN E DXTA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 990QS 7500190 ELEVATOR TRIM AUDIO (CLACKER) BEGINS RUNNING CONTINUOUSLY DURING FLIGHT WITH AUTOPILOT ON BUT NO TRIMMING ACTUALLY OCCUR S. THIS ONLY HAPPENS WHEN FLIGHT GUIDANCE (B) IS SELECTED AND THE AUDIO STOPPED WHEN FLIGHT GUIDANCE TO (A). THIS HAS OCCURRED DURING CRUISE AT HIGH ALTITUDE AND ALSO AT LOW ALTITUDE DURING APPROACH. CONNECTED EXTERNAL POWER. BROUGHT UP AVIONICS SYSTEM "CLACKER" OPS CHECKS GOOD. RAN AUTOPILOT AT INTERVALS OVER A 2 HR PERIOD. COULD NOT DUPLICATE. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007030900179 20070309 00179 CE 2007 3 9 DXTA200701987 1 20070302 A 3231 DOOR BEECH MU300 400A 1155402 CE MLG OUT OF RIG E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 122QS RK467 UPON GEAR RETRACTION RED LIGHT ON GEAR HANDLE REMAINS ON. DRAGGING NOISE HEARD FROM COCKPIT. SOUNDS LIKE GEAR DOORS DID NOT CLOSE. JACKED AIRCRAFT AND CONNECTED MULE AND GROUND POWER UNIT. PERFORMED GEAR CYCLE AND FOUND RIGGING OF NOSE GEA R DOORS PREVENTING NOSE GEAR FROM GOING INTO THE UP AND LOCKED POSITION AT REDUCED HYDRAULIC PRESSURES. RIGGED NOSE GEAR DOORS IAW 400A MM 32-20-00. PERFORMED NUMEROUS GEAR CYCLES WITH NO FURTHER PROBLEMS NOTED. SERVICED HYDRAULIC RESERVOIR IAW 400A M/M 12-10-00. DOWNJACKED AIRCRAFT. 2 H 7 2 4F RT A16SW 2007030900180 20070309 00180 CE 2007 3 9 DXTA200701989 1 20070302 A 2720 991455812 ACTUATOR CESSNA 750 750 2076810 CE VERTICAL STAB INOPERATIVE E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 944QS 274 7500144 RUD LIMIT FAIL "B' AMBER EICAS MESSAGE CTRL POS SHOWS RUDDER LIMT 86%.CHECKED SYTEM FOR PROPER OPERATION. COULD NOT DUPL ICATE. REMOVED AND REPLACED RUDDER LIMITER ACTUATOR "B" OPS CHECKED GOOD IAW 750 M/M CH 27-20-00 2 L 7 2 4J RT T00007WI 2007030900183 20070309 00183 CE 2007 3 9 GLBA20060910 1 20070219 A 5330 SKIN BEECH 1900 1900D 1154162 CE BS 228 CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 195GL UE195 MAJOR REPAIR - UPON ROUTINE MAINTENANCE, EVIDENCE OF CORROSION WAS FOUND ON THE BELLY OF THE AIRCRAFT AT APPROXIMATELY F S 228.25, 1.5 INCHES ON RT SIDE OF STRINGER 16. MAINTENANCE REPAIRED THE BELLY SKIN FROM APPROXIMATELY F.S. 228.25 ON RI GHT HAND SIDE OF STRINGER 16 I.A.W. BEECH 1900D SRM 51-70. RII INSPECTION COMPLIED WITH PER TC 8.2.1. 2 L 7 2 4T RT A24CE 2007030900186 20070309 00186 2007 3 9 C2XA07CL026 4 20070301 A 3140 701700082430 COMPUTER EMB 145 EMB145XR 3260214 SO COCKPIT SHORTED A C2XA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 10156 15302 145786 YUL FLIGHT NR 2034 THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN. THEY ALSO REPORTED LOSE OF CAPTAINS MFD, PVD, AND EICAS. THE AIRCRAFT RETURNED TO YUL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 I C-600. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT 2007030900189 20070309 00189 SO 2007 3 9 C2XA07SH013 1 20070305 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12157 145787 SHV DURING C-CHECK LT OMEGA BEAM CORRODED AT FR 20. MAINTENANCE REPAIRED LT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 51-40-0 2. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2007030900190 20070309 00190 SO 2007 3 9 C2XA07BT025 1 20070305 A 3350 GE1317 LIGHT EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 10156 145786 BTV 3A CHECK FLT NR 2414 FOUND LEFT HAND OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LAMP FOR LEFT HAND OVERWIN G EMERGENCY LIGHT IAW EMB145 AMM 33-50-07. OPS CHECK GOOD. CLOSED 2 L 7 2 4F RT 2007030900192 20070309 00192 SO 2007 3 9 C2XA07BT026 1 20070306 A 3350 110049 CHARGER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16981 145208 BTV ROUTINE CHECK FLT NR 2043 FOUND COCKPIT CEILING, CEILING AT ROW 3ABC, AND LEFT FWD WING TO FUSELAGE FAIRING EMERGENC Y LIGHTS INOP. REMOVED AND REPLACED NR 1 EMERGENCY BATTERY LIGHT BASE CHARGER IAW EMB145 AMM 33-50-04. OPS CHECK GOOD. CLOSED 2 L 7 2 4T RT T00011AT 2007030900194 20070309 00194 SO 2007 3 9 C2XA07BT024 1 20070305 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN DIRTY A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 12996 145296 EWR LOG SQUAWK FLT 2347 FORWARD OVERHEAD EMERGENCY EXIT LOCATER SIGN AT ROW 11 OUT. CLEANED CONNECTOR AND RESECURED FOR WARD EMERGENCY EXIT LOCATER AT ROW 11 IAW EMB145 AMM 33-50-13. OPS CHECK GOOD. CLOSED 2 L 7 2 4T RT T00011AT 2007030900195 20070309 00195 SO 2007 3 9 C2XA07TY009 1 20070304 A 3260 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO LT MLG OUT OF ADJUST A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 13956 145078 JAX-CLE FLT NR 2050- LANDING GEAR/AIR GROUND FAIL MESSAGE ANNUNCIATED DURING FLIGHT. DIVERTED TO TYS WITHOUT INCIDENT. THE LT MLG TRAILING ARM PROX SWITCH WAS ADJUSTED IAW EMB 145 AMM 32-63-05 AND OPS CHECKED GOOD. THE A/C WAS RETURNED T O SERVICE. 2 L 7 2 4T RT T00011AT 2007030900196 20070309 00196 CE 2007 3 9 DXTA200701970 1 20070227 A 3213 STRUT CESSNA 750 750 2076810 CE NLG UNDERSERVICED E DXTA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 GL 07 960QS 7500160 LANDING GEAR WOULD NOT RETRACT. SERVICED NOSE STRUT IAW CE-750 MM CHP 12-10-38 PERFORMED 7 FAULT FREE GEAR SWINGS. OPERA TIONAL CHECK GOOD. 2 L 7 2 4J RT T00007WI 2007030900197 20070309 00197 SO 2007 3 9 C2XA07CL028 1 20070302 A 2612 FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY FAULTY A C2XA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 27 13550 11868 145575 DURING ROUTINE MAINTENANCE THE LAV SMOKE MESSAGE WAS ON THE ECIAS. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DET ECTOR. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007030900198 20070309 00198 CE 2007 3 9 DXTA200701971 1 20070227 A 3260 CABLE CESSNA 560 560XL 2076702 CE MLG OUT OF ADJUST E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 694QS 5605194 GEAR 'UNLOCK' LIGHT ILLUMINATED AFTER GEAR RETRACTION. CYCLED GEAR TWICE WITH SAME RESULT. HYD SYSTEM REMAINED PRESSURIZ ED UNTIL GEAR SELECTED DOWN. ADJUSTED & CHECKED FREE FALL CABLE IAW CESSNA 560XL M/M CHPT 32-30-08 2 L 7 2 4F RT A22CE 2007030900200 20070309 00200 CE 2007 3 9 DXTA200701988 1 20070302 A 2700 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL UNKNOWN E DXTA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 07 962QS 7500126 ON 2 SEPERATE T/O ROLLS AT 60-70 KTS BOTH YD AND MACH TRIM CAME OFF. T.O.S WERE BOTH ABORTED . NOTE: PITOT HEAT INDICA TED WORKING AND WAS LT ON FROM TAXI OUT TO T/O ROLL. (EST 20-25 MIN BY 2ND T.O. ATTEMPT) PLANE WAS SITTING IN HEAVY RA IN FOR SEVERAL HRS. PURGED PITOT/STATIC SYSTEMS AS REQUIRED. YAW DAMPER AND MACH TRIM SYSTEM FUNCTIONING NORMAL AT THIS TIME. ALL WORK DONE IAW 750 MM CHAPTERS 22, 30, 34 & 23. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007030900202 20070309 00202 2007 3 9 DXTA200701990 4 20070302 A 3417 8220374412 ADC AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE NR 1 INOPERATIVE E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 227QS 231 127 MACH TRIM LIGHT ILLUMINATED ON PFD. DUPLICATED DISCREPANCY. CLEARED FADEC FAULTS I.A.W. THE FALCON 2000 M.M. 45-000. NR 1 ADC REMOVED AND REPLACED DUE TO PILOT REPORT OF LOSS OF AIRSPEED. SYSTEM OPS CHECKS NORMAL I/A/W THE FALCON 2000 M.M. 34-103. 2 K 7 2 4F 4 F RT A50NM E44NE 2007030900204 20070309 00204 SO 2007 3 9 C2XA07IA048 1 20070226 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11547 6146 2606 145563 DURING SCHEDULED MAINTENANCE THE LEFT FORWARD FAIRING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. THE NR 1 EMERGE NCY LIGHT BATTERY PACK WAS REMOVED AND REPLACED, THE SYSTEM OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED. 2 L 7 2 4T RT T00011AT 2007030900205 20070309 00205 SO 2007 3 9 C2XA07IA049 1 20070227 A 2611 M8373110271 SWITCH EMB 145 EMB145LR 3260212 SO SMOKE WARNING SHORTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 15574 145639 DURING PUSHBACK FROM THE TERMINAL THE CREW REPORTED THAT THE BAG SMOKE WARNING ILLUMINATED. MAINTENANCE REMOVED AND REP LACED THE BAGGAGE SMOKE DETECTION TEST SWITCH, OPERATIONALLY TESTED THE SYSTEM AND CLEARED THE DISCREPANCY. 2 L 7 2 4T RT T00011AT 2007030900207 20070309 00207 SO 2007 3 9 C2XA07IA045 1 20070221 A 3222 M834611236 PACKING EMB 145 EMB145LR 3260212 SO NLG STRUT WORN A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13970 145146 FLIGHT 2830 - CREW REPORTED A LANDING GEAR AIR/GROUND FAIL INDICATION FOLLOWED BY ENGINE 1/2 REVERSER DISAGREE MESSAGES. THE AIRCRAFT RETURNED TO IAH WHERE MAINTENANCE FOUND THE NOSE GEAR STRUT TO BE FLAT. THE NLG STRUT WAS DISASSEMBLED A ND PACKING WAS REPLACED. THE STRUT WAS THEN REASSEMBLED, LANDING GEAR OPERATIONAL AND LEAK CHECKS PERFORMED AND THE DIS CREPANCY WAS CLEARED. 2 L 7 2 4T RT T00011AT 2007030900208 20070309 00208 NM 2007 3 9 NWAA070916305 1 20070201 A 5310 DOOR FRAME BOEING 747 747451 1384940 NM BS 1990 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 665US 23820 DURING "M" CHECK, FOUND CORROSION ON BULK CARGO DOOR REVEAL WEB AT BS 1990. REPAIRED PER EA 63-208888. 2 L 7 4 4F RT A20WE 2007030900209 20070309 00209 SO 2007 3 9 C2XA07IA046 1 20070222 A 3350 BA50933901 POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16559 11648 2887 145603 DURING SCHEDULED MAINTENANCE THE AFT CABIN EMERGENCY LIGHTS WOULD NOT ILLUMINATE WHEN TESTED. MAINTENANCE REMOVED AND R EPLACED THE NR 6 POSITION EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREP ANCY. 2 L 7 2 4T RT T00011AT 2007030900211 20070309 00211 SO 2007 3 9 C2XA07TY008 1 20070223 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14952 145067 602 NR 110291- AIRCRAFT IN FOR C-CHECK. CORROSION ON LT OMEGA BEAM AT FRM 20. SPLICED IN NEW SECTION OF BEAM, ALODINED , PRIMED AND PAINTED. REPAIRS MADE IAW EC5320-01229 AND EMB145 CPM 51-21-07. 2 L 7 2 4T RT T00011AT 2007030900212 20070309 00212 NM 2007 3 9 NWAA070906717 1 20070223 A 5310 TENSION TIE BOEING 747 747251F 1384898 NM BS 860 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 617US 21121 DURING "L" CHECK, FOUND CRACKS IN LT AND RT TENSION TIE FASTENER HOLES AND FRAME AT BS 860 UPPER LOBE. REPAIRED PER EA 67-208623. 2 L 7 4 4F A20WE 2007030900214 20070309 00214 NM 2007 3 9 NWAA070896717 1 20070225 A 5310 TENSION TIE BOEING 747 747251F 1384898 NM BS 840 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 617US 21121 DURING "L" CHECK FOUND CRACKS IN LT AND RT TENSION TIE FASTENER HOLES AND FRAME AT BS 840 UPPER LOBE. REPAIRED PER EA 6 7-208624. 2 L 7 4 4F A20WE 2007030900215 20070309 00215 NM 2007 3 9 NWAA070886717 1 20070223 A 5310 TENSION TIE BOEING 747 747251F 1384898 NM BS 820 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 617US 21121 DURING "L" CHECK, FOUND CRACKS IN LT AND RT TENSION TIE FASTENER HOLES, FRAME AND FAIL/SAFE CHORD AT BS 820. REPAIRED P ER EA 67-208625. 2 L 7 4 4F A20WE 2007030900216 20070309 00216 NM 2007 3 9 NWAA070876717 1 20070225 A 5310 TENSION TIE BOEING 747 747251F 1384898 NM BS 900 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 617US 21121 DURING "L" CHECK, FOUND CRACKS IN LT AND RT TENSION TIE FASTENER HOLES, FRAME AND FAIL/SAFE CHORD AT BS 900. REPAIRED P ER EA 67-208626. 2 L 7 4 4F A20WE 2007030900217 20070309 00217 NM 2007 3 9 NWAA070856717 1 20070217 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 2140 S25-26L CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 617US 21121 DURING "L" CHECK, FOUND CRACK IN FRAME WEB AT BS 2140 BETWEEN S25L AND S26L. REPAIRED PER EA 67-208624. 2 L 7 4 4F A20WE 2007030900218 20070309 00218 NM 2007 3 9 NWAA070866717 1 20070222 A 5310 TENSION TIE BOEING 747 747251F 1384898 NM BS 920 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 617US 21121 DURING "L" CHECK, FOUND CRACKS IN LT AND RT TENSION TIE FASTENER HOLES, FRAME AND FAIL SAFE CHORD AT BS 920. REPAIRED P ER EA 67-208627. 2 L 7 4 4F A20WE 2007030900220 20070309 00220 NM 2007 3 9 F3LA200700039 1 20070225 A 5313 STRINGER AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 930FR 2241 DURING C-2 CHECK INSPECTION, REPORTED FWD CARGO COMPARTMENT STRINGER 42R AT THE AFT END OF ZONE 131, INBD OF CARGO DOOR FROM F24 TO F28, HAD EXFOLIATION/CORROSION AROUND RIVETS. REMOVED CORRODED RIVETS IAW SRM 51-42-11. PERFORMED HFEC INS PECTION OF HOLES IAW NTM 51-10-01, PAGE 612. NO DEFECTS NOTED. OVERSIZED HOLES AND INSTALLED RIVETS PER SRM 51-42-11. 2 L 7 2 4F RT A28NM 2007030900222 20070309 00222 NM 2007 3 9 F3LA200700030 1 20070301 A 3510 MXP80110 STOWAGE BOX AIRBUS A319 A319111 3930336 NM CREW OXYGEN NO TEST A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 931FR 4727 2253 DURING C-2 CHECK, INSPECTION REPORTED 3RD CREW O2 STOWAGE BOX DID NOT FUNCTION DURING PUSH-TO-TEST. REPLACED 3RD CREW O 2 STOWAGE BOX IAW 35-12-41, PB 401. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A28NM 2007030900223 20070309 00223 SO 2007 3 9 C2XA07IA055 1 20070306 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13988 5212 484 145265 MAF - FLIGHT 2760, DURING PREFLIGHT THE CREW REPORTED THE AFT THREE EMERGENCY LIGHT STRIPS TO BE INOPERATIVE. THE CREW C HARGED THE EMERGENCY LIGHTS SYSTEM, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE RVICE. 2 L 7 2 4T RT T00011AT 2007030900224 20070309 00224 NM 2007 3 9 NWAA070936717 1 20070221 A 5313 STRINGER BOEING 747 747251F 1384898 NM BS 2160-2180 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 617US 21121 DURING "L" CHECK, FOUND CRACK IN STRINGER 46L, BS 2160-2180. REPAIRED PER EA 67-208981. 2 L 7 4 4F A20WE 2007030900225 20070309 00225 NM 2007 3 9 NWAA070946717 1 20070222 A 5313 STRINGER BOEING 747 747251F 1384898 NM BS 1482-1486 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 617US 21121 DURING "L" CHECK, FOUND CRACK IN STRINGER 16L, BS 1482-1486. REPAIRED PER EA 67-208979. 2 L 7 4 4F A20WE 2007030900226 20070309 00226 NM 2007 3 9 NWAA070956717 1 20070227 A 5313 STRINGER BOEING 747 747251F 1384898 NM BS 1960-1980 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 617US 21121 DURING "L" CHECK, FOUND CRACK ON STRINGER 48R, BS 1960-1980. REPAIRED PER EA 67-208978. 2 L 7 4 4F A20WE 2007030900227 20070309 00227 NM 2007 3 9 NWAA070966305 1 20070131 A 5414 SKIN BOEING 747 747451 1384940 NM LT NACELLE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 665US 23820 DURING "M" CHECK, FOUND CRACK IN NR 4 PYLON LT INBOARD SKIN NAC STA 276, NWL 170, PANEL 482EL CUTOUT. REPAIRED PER EA 6 3-208898. 2 L 7 4 4F RT A20WE 2007030900229 20070309 00229 EA 2007 3 9 SWIA200717924 1 20070129 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 920SW 7660 PAX DOOR AFT DRAG ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLE AND SPLICE ANGLES PER CRJ 200 REO 601-R52-11-513 STEP 6-10. 2 L 7 2 4F RT A21EA 2007030900230 20070309 00230 EA 2007 3 9 SWIA200717925 1 20070129 A 5210 ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 920SW 7660 PAX DOOR NR 5 STEP FWD STEP ANGLE CRACKED AT DOOR RAIL FITTING, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER AND REPAIR ANGLES PER CRJ200 REO 601-R52-11-702 (REV-) RII 52-900-1001 AND REO 601R-52-11-702. 2 L 7 2 4F RT A21EA 2007030900231 20070309 00231 EA 2007 3 9 SWIA200717926 1 20070129 A 5210 ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 920SW 7660 PAX DOOR NR 5 STEP AFT ANGLE CRACKED AT DOOR RAIL FITTING AND AT BOTTOM OF NR 4 STEP AFT WEB, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PART AND AFT GAS SPRING MOUNT BRACKET PER CRJ200 REO 601R-53-11-702 ZONES 2,2 AND 4 REPAIR STEPS 8, 10, 13, 16 AND 17. 2 L 7 2 4F RT A21EA 2007030900232 20070309 00232 EA 2007 3 9 SWIA200717927 1 20070129 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 920SW 7660 PAX DOOR BOTTOM FOLDING STEP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW PAX DOOR BOTTOM FOLDING STEP PER CRJ200 AMM 52-11-04-400-802. 2 L 7 2 4F RT A21EA 2007030900233 20070309 00233 SO 2007 3 9 C2XA07IA051 1 20070304 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145EP 3260221 SO CARGO BAY INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16927 12135 12135 145006 IAH - DURING MAINTENANCE INSPECTION THE BAGGAGE SMOKE DETECTOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE BAGGAGE SMOKE DETECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN T O SERVICE. 2 L 7 2 4F RT T00011AT 2007030900234 20070309 00234 EA 2007 3 9 SWIA200717928 1 20070129 A 5320 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA BS 640 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 920SW 7660 RT STA 640 REINFORCEMENT DOUBLER BETWEEN STR 9 AND STR 12 FOUND TO BE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. IN STALLED FS 640 RHS DOUBLER IAW CRJ200 SRM 51-42-06 PG 11 FIG 8 SRM 51-42-21 PG 17 AND REO 601R-53-61-2056 A. 2 L 7 2 4F RT A21EA 2007030900235 20070309 00235 EA 2007 3 9 SWIA200717929 1 20070129 A 5340 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 920SW 7660 AFT EQUIPMENT COMPARTMENT DIRECTLY UNDER RT ACM, ANGLE BRACKET IS CRACKED IN 2 PLACES, DISCOVERED DURING C-CHECK INSPECT ION. INSTALLED ANGLE BRACKET UNDER RT AC IN AFT EQUIPMENT COMPARTMENT PER CRJ200 SRM 51-42-06 PG 18 AND CRJ200 SRM 51-4 2-20 PG 12 FIG-7. 2 L 7 2 4F RT A21EA 2007030900236 20070309 00236 EA 2007 3 9 SWIA200717930 1 20070129 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 920SW 7660 FS 280 FLOOR SUPPORT BEAM CRACKS FOUND AT RBL12 AND LBL12, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED PARTS PER CR J200 REO 601R-53-11-171 REV C AND COMPLIED WITH SKYWEST RII 53-900-1001. 2 L 7 2 4F RT A21EA 2007030900237 20070309 00237 SO 2007 3 9 C2XA07IA052 1 20070304 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145EP 3260221 SO CARGO BAY MALFUNCTIONED A C2XA F A ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 16927 11582 570 145006 IAH - FLIGHT 2811, THE CREW REPORTED A BAGGAGE SMOKE INDICATION IN FLIGHT. THE CREW DISCHARGED BOTH BAGGAGE FIRE BOTTLES , AND RETURNED TO IAH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND RE PLACED THE BAGGAGE SMOKE DETECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE RVICE. 2 L 7 2 4F RT T00011AT 2007030900238 20070309 00238 EA 2007 3 9 SWIA200717932 1 20070129 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 920SW 7660 ENGINE SUPPORT BEAM LOWER WEB FOUND TO BE CRACKED AT FWD INBD CORNER OF LT ACCESS PANEL, DISCOVERED DURING C-CHECK INSPE CTION. INSTALLED REPAIR AT LT LOWER WEB OF ENG SUPPORT BEAM FWD INBD CORNER OF ACCESS PN CUTOUT PER REO 601R 53-61-358. 2 L 7 2 4F RT A21EA 2007030900239 20070309 00239 EA 2007 3 9 SWIA200717933 1 20070129 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 920SW 7660 ENGINE SUPPORT BEAM LOWER WEB FOUND TO BE CRACKED AT FWD INBD WEB CORNER OF RT ACCESS PANEL CUTOUT, DISCOVERED DURING C- CHECK INSPECTION. INSTALLED REPAIR PARTS TO LOWER WEB RT ENG SUPPORT BEAM PER CRJ200 SRM 51-42-06 PG 11 SRM 51-42-20 PG 23. 2 L 7 2 4F RT A21EA 2007030900240 20070309 00240 EA 2007 3 9 SWIA200717934 1 20070129 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 920SW 7660 CABIN 280 BULKHEAD BELOW THE FLOOR AT STRINGER 9L AND 9R EACH HAVE A CRACK, DISCOVERED DURING C-CHECK INSPECTION. INSTA LLED CLIPS AT RBL9 AND LBL9. 2 L 7 2 4F RT A21EA 2007030900241 20070309 00241 EA 2007 3 9 SWIA200717935 1 20070131 A 5210 BRACKET CNDAIR CL600 CL6002B19 1900309 EA DOOR ASSIST MOTR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 869AS 7479 FOUND PAX DOOR-DOOR ASSIST MOTOR MOUNTING BRACKET CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED PAX DOOR ASS IST MOTOR MOUNTING BRACKET PER CRJ200 SRM 51-42-06 PG 4/SRM 51-41-02 PG 5. 2 L 7 2 4F RT A21EA 2007030900242 20070309 00242 EA 2007 3 9 SWIA200717936 1 20070131 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 869AS 7479 FOUND PASSENGER DOOR OUTER HANDLE IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED PAX DOOR OUTER HANDLE PER CRJ200 SRM 51-42-20 PG 24 . 2 L 7 2 4F RT A21EA 2007030900244 20070309 00244 SO 2007 3 9 C2XA07IA054 1 20070304 A 3697 W400000124WH WIRE EMB 135 EMB135LR 3260305 SO RT PYLON CHAFED A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 27 27523 145389 MGM - FLIGHT 2362, THE CREW REPORTED A ENGINE TWO BLEED LEAK IN FLIGHT. THE CREW SHUT DOWN THE NUMBER TWO ENGINE AS A PR ECAUTION AND THE AIRCRAFT DIVERTED TO MGM WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REPAIRED A CHAFED WIRE IN THE NUMBER TWO PYLON, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007030900245 20070309 00245 SO 2007 3 9 C2XA07BT022 1 20070228 A 3350 110049 CHARGER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 48901 145501 EWR MX LOG SQUAWK FLT NR 3005 FOUND EMERGENCY LIGHTS (RT WING FUSELAGE FRONT FAIRING AND ISLE LIGHT NR 2) INOP. REMOVED AND REPLACED CHARGER ASSEMBLY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. CLOSED 2 L 7 2 4T RT T00011AT 2007030900248 20070309 00248 2007 3 9 C2XA07SH015 4 20070309 A 3140 701700082430 COMPUTER EMB 145 EMB145XR 3260214 SO COCKPIT MALFUNCTIONED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 10156 145786 FL 2128 - XNA TO IAH- SMOKE IN COCKPIT (ELEC) LOST CAPT MFD, PFD, ICAS, CREW DIVERTED TO DAL. MX INSPECTED AND FOUND IC- 600 NR 1 TO HAVE A BURNING SMELL. REMOVED AND REPLACED IC 600 NR 1 IAW EMB 145 AMM 31-42-01 OPS CHECK GOOD. NO OTHER SMO KE, BURNING, FIRE DAMAGE DEFECT FOUND IN COCKPIT AT THIS TIME. INSPECTED CAPTS MFD, PFD AND THE EICAS FOR NORMAL OPERATI ON AND FUNCTIONALITY AS REQUIRED. NO DEFECT NOTED AT THIS TIME. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE 2 L 7 2 4F RT 2007030900249 20070309 00249 NM 2007 3 9 SWAA071238 1 20070306 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 464WN 32468 EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007030900251 20070309 00251 NM 2007 3 9 SWAA071240 1 20070306 A 5310 6519603 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM CHORD CRACKED AT BS 639, LBL 70. REMOVED AND REPLACED CREASE BEAM CHORD P ER ER. 2 L 7 2 4F RT A16WE 2007030900252 20070309 00252 NM 2007 3 9 SWAA071253 1 20070306 A 5311 6545805 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007030900253 20070309 00253 NM 2007 3 9 SWAA071241 1 20070306 A 5753 6546430189 STRUCTURE BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED C2 CHECK, FOUND LEFT WING INBOARD FORE FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FORE FLA P PER MM. 2 L 7 2 4F RT A16WE 2007030900254 20070309 00254 NM 2007 3 9 SWAA071243 1 20070306 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030800078 20070308 00078 2007 3 8 NSVA20070032 4 20070207 A 3418 WARNING LIGHT SAAB SF340 340B 7860101 EU STALL WARNING FALSE ACTIVATION A NSVA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 346CJ 346 FOUND PUSHER DISARM LIGHT ILLUMINATED. RESET PUSHER DISARM SWITCH, OPS CHECK GOOD. NO FAULTS NOTED AT THIS TIME IAW SA MM 27-35-00. 2 L 7 2 4T RT A52EU 2007030800088 20070308 00088 NM 2007 3 8 NWAA070626623 1 20070220 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 623US 21705 DURING OVERNIGHT CHECK, FOUND C ZONE FLOOR EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. OPERAT IONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F A20WE 2007030800093 20070308 00093 NM 2007 3 8 NWAA070776717 1 20070225 A 5310 TENSION TIE BOEING 747 747251F 1384898 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 617US 21121 DURING "L" CHECK, FOUND CRACKS IN FRAME TENSION TIE WEB DOUBLER FASTENER HOLES. REPAIRED PER EA 67-208621 SECTION I AND II. 2 L 7 4 4F A20WE 2007030800099 20070308 00099 NM 2007 3 8 NWAA070836305 1 20070131 A 5310 TENSION TIE BOEING 747 747451 1384940 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 665US 23820 DURING "M" CHECK, FOUND CRACK IN BS 1220 RT TENSION TIE DOUBLER AT STRINGER 8R AND STRINGER 9R AND A EXISTING TRIM OUT O N THE FRAME DOUBLER AT STRINGER 9R. REPAIRED PER EA 63-208886 SECTION I AND II. 2 L 7 4 4F RT A20WE 2007030800104 20070308 00104 NM 2007 3 8 NWAA070693149 1 20070227 A 2911 O-RING AIRBUS A319 A319114 3930350 NM HYD ACCUMULATOR UNKNOWN A NWAA K NONE K FLUID LOSS CR CRUISE 1 GL 01 349NB 1815 TOTAL LOSS OF FLUID IN YELLOW HYDRAULIC SYSTEM. COM 2.29.33 USED TO SECURE SYSTEM. PUMP SHUTOFF IMMEDIATELY PER FIRST OFFICER. AN EMERGENCY WAS DECLARED AT DESTINATION, THE LANDING AND TAXI TO GATE WAS UNEVENTFUL. CORRECTION WAS REPLACEM ENT OF O-RING ON FITTING, ON TOP OF YELLOW HYDRAULIC SYSTEM ACCUMULATOR. LEAK AND OPS CHECK OK. 2 L 7 2 4F RT A28NM 2007030800119 20070308 00119 NM 2007 3 8 QXEA200700264 1 20070218 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 C4 PDX - FOUND 3 SMALL DENTS LOCATED 2" FORWARD OF A YELLOW DOTTED DENT BETWEEN STATION X126 AND 28 BETWEEN RIBS 31 AND 32 RIGHT. REPAIRED IAW RD8-53-5384 AND RD8-53-9474. 2 H 7 2 4T RT A13NM 2007030800127 20070308 00127 NM 2007 3 8 QXEA200700335 1 20070303 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND RIGHT WING NR 4 FLAP TRACK OUTBOARD VERTICAL SIDE HAS PITTING AT FORWARD POINT. REPAIRED IAW RD8-57-1167 . 2 H 7 2 4T RT A13NM 2007030800146 20070308 00146 EA 2007 3 8 SWIA200717869 1 20070303 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR LACK OF LUBE A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 955SW 7817 CREW REPORTS SERVICE DOOR OUTER HANDLE WON'T COME OUT. CLEANED AND LUBED THE SERVICE DOOR HANDLE/LATCH ASSEMBLY. OPERA TIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007030800150 20070308 00150 NM 2007 3 8 QXEA200700345 1 20070222 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - FOUND LAV PAN EXTERNAL SKIN APERTURE IS CHAFED AT AFT LOWER EDGE. REPAIRED IAW SRM 51-20-11. 2 H 7 2 4T RT A13NM 2007030800152 20070308 00152 SW 2007 3 8 01302007 1 20070130 A 3710 3P207 PUMP GULSTM 500 500B 0141106 SW LYC O540 IO540E1A5 41532 EA VACUUM SYS DAMAGED E ZJWA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 CE 05 610BW 277 1523185 RL199248 LEFT VACUUM PUMP LOOSENED FROM ENGINE AND CAUSED A LOOSE OF OIL PRESSURE. THE VACUUM PUMP DRIVE WAS DAMAGED IN THAT THE GEAR WAS ROUNDED OFF. IT WAS HARD TO DETERMINE IF THE GEAR WORE AND CREATED STRESS TO WORK IT LOOSE FROM THE ENGINE OR IT WORKED LOOSE AND THEN DAMAGED THE GEAR. 1 H 7 2 3O 3 O 6A1 1E4 2007030800167 20070308 00167 EA 2007 3 8 SWIA200717885 1 20070115 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7853 FOUND 3RD STEP AFT WEB SUPPORT CRACKED DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS IN ZONE 3 AT AFT WE B PAX DOOR IAW CRJ200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007030800170 20070308 00170 EA 2007 3 8 SWIA200717888 1 20070115 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7853 FOUND LBL 9 OUTBD 280 CLIP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIP AT STA 280 LBL9 O/R PER CRJ200 SRM 51-42-21 PG 17, 18 FIG 10. 2 L 7 2 4F RT A21EA 2007030800175 20070308 00175 NM 2007 3 8 QXEA200700348 1 20070304 A 3060 697071272 HARNESS BOMBDR DHC8 DHC8402 1390042 NM PROPELLER DE-ICE BROKEN A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 413QX 4060 SEA FLIGHT NR 2484 - PROP DEICE CAUTION ON CLIMB. MAINTENANCE FOUND NR 2 PROP NR 2 BLADE DEICE LEAD BROKEN. REMOVED AN D INSTALLED SERVICEABLE NR 2 PROP NR 2 BLADE PROP DEICE LEAD IAW Q400 AMM 61-10-06-000-805 AND 61-10-06-400-805. OPS CH ECK IAW Q400 AMM 30-61-00-720-802. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030800178 20070308 00178 EA 2007 3 8 SWIA200717857 1 20070116 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 967SW 7872 FOUND CRACK IN CLIP ON RIGHT SIDE AT STRINGER 14 RT AND FS 624.0 ON AFT SIDE OF AFT PRESSURE BULKHEAD, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP PER REO 601R-53-61-422. 2 L 7 2 4F RT A21EA 2007030800180 20070308 00180 EA 2007 3 8 SWIA200717859 1 20070116 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 967SW 7872 FOUND CRACK IN CLIP ON FLOORBEAM FS280.0 AND FLOOR SUPPORT (RIGHT) RBL9 OUTBOARD SIDE BELOW WL 73.00, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIP ON FLOORBEAM FS 280 AND FLOOR SUPPORT RBL 9 OTBD SIDE PER STANDARD REPAIR 601R 53-00 57A. 2 L 7 2 4F RT A21EA 2007030900013 20070309 00013 EA 2007 3 9 SWIA200717897 1 20070123 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 970SW 7881 FOUND PAX DOOR AFT DRAG ANGLE CRACKED AT CABLE EXIT FOR PULL IN MOTOR, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE SECTION AND SPLICE ANGLE IAW REO 601R-52-11-513. 2 L 7 2 4F RT A21EA 2007030900022 20070309 00022 EA 2007 3 9 SWIA200717907 1 20070123 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT MLG WW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 970SW 7881 FOUND LT WHEEL WELL TRANSDUCER BRACKET CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT WHEEL WELL TRANSDUC ER BRACKET PER CRJ200 SRM 51-42-06 AND 51-80-00. 2 L 7 2 4F RT A21EA 2007030900029 20070309 00029 SO 2007 3 9 GLBA20060921 1 20070305 A 2130 CABIN PRESSURE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE MALFUNCTIONED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 299UX 120299 AIR RETURN, PILOT REPORTED THAT PRESSURIZATION WAS NOT WORKING IN THE MANUAL MODE SETTING ABOVE 10,000 FEET AND THE AIRC RAFT WAS ALREADY ON MEL FOR THE AUTO FUNCTION. MAINTENANCE PERFORMED GROUND OPERATIONAL CHECKS IAW MM 21-30 WITH NO ABN ORMALITIES NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 2007030900049 20070309 00049 WP 2007 3 9 070046 1 20070221 A 3350 79116 BATTERY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 869GA 53294 DURING A ROUTINE OVERNIGHT SERVICE CHECK LAS VEGAS MAINTENANCE REPORTED THAT THE TAIL CONE AREA EMERGENCY LIGHTS WOULD N OT TEST. THEY FURTHER REPORT THE REPLACEMENT OF THE BATTERY PACK AT POWER SUPPLY B5-28. A SATISFACTORY OPERATIONAL CHE CK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007030900051 20070309 00051 EU 2007 3 9 BAQA20070006 1 20070228 A 2697 320551 TERMINAL AEROSP AS355 AS355F1 8680810 EU ALLSN 250C 250C20 03013 GL FIRE DETECTION BROKEN E BAQA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 03 5797X 5182 CAE841010 DURING CRUISE FLIGHT PILOT OBSERVED THE NR 2 ENGINE FIRE LIGHT ILLUMINATE . PILOT DID A PRECAUTIONARY LANDING AT AIRPORT . MECHANIC DISPATCHED AND FOUND WIRE ON TERMINAL LUG ON FIRE DETECTOR BROKEN. REPLACED TERMINAL LUG AND COMPLIED WITH A N OPERATION CHECK OF THE FIRE DETECTION SYSTEM AND FOUND NO DEFECTS AT THIS TIME. AIRCRAFT WAS FROM OUR BASE SITE. 1 G 7 2 3U 3 U H11EU E4CE 2007030900053 20070309 00053 NM 2007 3 9 QXEA200700306 1 20070225 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 223-250 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 C4 PDX - THE LEFT INBOARD SEAT TRACK NR 4 HAS CORROSION AT THE PANEL LANDING ON THE OUTBOARD SIDE BETWEEN STATION X223 A ND X250. REPAIRED IAW RD8-53-1102 AND RD8-53-4473, SRM 51-40-00, 51-40-11. 2 H 7 2 4T RT A13NM 2007030900057 20070309 00057 NM 2007 3 9 QXEA200700317 1 20070301 A 3150 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 406QX 4048 PDX FLIGHT NR 2170: ON TAXI OUT, THE T/O WARNING HORN CAME ON WITH THE TEST. MAINTENANCE CYCLED POWER FOR STAB TRIM. OPS CHECK GOOD IAW TASK 31-52-00-720-801. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007030900101 20070309 00101 2007 3 9 A6WA200740058 2 20070213 A 7200 REGULATOR VALVE CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE MALFUNCTIONED A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 407AW 7424 SMOKE TOILET CAUTION MESSAGE ON TAKEOFF CLIMB, COMPLIED WITH QRH, AIR RETURNED TO PHL NO OVERWEIGHT LANDING WTW 41,000 L BS. NO VISUAL SMOKE IN LAV OR CABIN. (M) REMOVED AND REPLACED PRESS REGULATING VALVE ASSY ON RT ENG IAW AMM 25-31-05. PERFORMED COMP WASH AND POWER RUNS NO SMELLS NOTED AND NO SMOKE NOTED THROUGH ALL POWER RANGES, OK FOR SERVICE. (K) 2 L 7 2 4F RT A21EA 2007030900118 20070309 00118 EA 2007 3 9 SWIA200717846 1 20070108 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FOUND CLIP CRACKED AT RBL9 ON AFT SIDE OF STA 280 AT FLOOR LEVEL, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW C LIP, AT FS 280 RBL 9 INBD AFT SIDE OF FLOORBEAM AS PER CRJ200 SRM 51-42-21 PG 1-19 AND SRM 51-42-06 PG 1-18. 2 L 7 2 4F RT A21EA 2007030900131 20070309 00131 EA 2007 3 9 SWIA200717855 1 20070116 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 967SW 7872 PAX DOOR - AFT DRAG ANGLE CRACKED ADJACENT TO THE ASSIST CABLE PULLEY, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SPLICE ANGLES PER REO 601R-52-11-513 REV A. 2 L 7 2 4F RT A21EA 2007030900135 20070309 00135 EA 2007 3 9 SWIA200717909 1 20070128 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 PAX DOOR FWD WEB CRACKED UNDER HANDRAIL, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS TO REPAIR CRACKED PAX DOOR FWD WEB AS PER REO 601R-52-11-702 REV A. 2 L 7 2 4F RT A21EA 2007030900149 20070309 00149 EA 2007 3 9 SWIA200717922 1 20070128 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BRAKE TRANSDUCER CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 LT BRAKE TRANSDUCER BRACKET CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW BRACKET LT SIDE PER SRM 51-42- 06. 2 L 7 2 4F RT A21EA 2007030900150 20070309 00150 EA 2007 3 9 SWIA200717923 1 20070129 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 920SW 7660 PAX DOOR OTBD HANDLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED PAX DOOR OUTER HANDLE AS PER CRJ200 AMM 52 -11-03-000-802 AND 52-11-03-400-802. 2 L 7 2 4F RT A21EA 2007030900187 20070309 00187 SO 2007 3 9 C2XA07CL029 1 20070306 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 27 11113 145662 MKE FLIGHT NR 2745 THE CREW REPORTED A ELECTRICAL BURNING SMELL IN THE COCKPIT AND CABIN UPON LANDING. MAINTENANCE INSP ECTED CIRCUIT BREAKERS AND RELAYS AND FOUND NO DEFECTS. RAN THE ENGINES WITH BLEEDS ON AND NO ODOR WAS DETECTED. THE A IRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT 2007030900191 20070309 00191 SO 2007 3 9 C2XA07BT027 1 20070307 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN DISCONNECTED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13913 145438 BTV ROUTINE CHECK FLT NR 2043 FOUND SERVICE DOOR EMERGENCY LIGHT(EXTERIOR) INOP. RECONNECTED SERVICE DOOR EMERGENCY LIG HT CONNECTER IAW EMB145 AMM STANDARD PRACTICES. OPS CHECK GOOD. CLOSED 2 L 7 2 4T RT T00011AT 2007030900203 20070309 00203 SO 2007 3 9 C2XA07IA044 1 20070220 A 2612 FIRE WARNING EMB 145 EMB145LR 3260212 SO APU MALFUNCTIONED A C2XA F ACTIVATE FIRE EXT. N FALSE WARNING UK UNKNOWN 1 SW 27 36915 145421 FLIGHT 2600 - THE CREW REPORTED THAT AN APU FIRE WARNING INDICATION HAD ILLUMINATED WHILE THE AIRCRAFT WAS PARKED AT THE AIRPORT TERMINAL. THE APU FIRE BOTTLE WAS DISCHARGED AS A RESULT OF THE WARNING. MAINTENANCE INSPECTED THE APU AN FOU ND NO EVIDENCE OF A FIRE OR SMOKE. THE FIRE BOTTLE WAS REPLACED AND OPERATIONAL CHECKS OF THE APU AND IT'S ASSOCIATED F IRE DETECTION SYSTEM WERE PERFORMED. THE OPERATIONAL CHECKS PROVED SATISFACTORY AND THE DISCREPANCY WAS CLEARED. 2 L 7 2 4T RT T00011AT 2007030900206 20070309 00206 SO 2007 3 9 C2XA07BT020 1 20070223 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN SMOKE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 15973 145159 EWR LOG SQUAWK FLT NR 2292 ON CLIMB AT 8000 FT. WE GOT LAV SMOKE WARNING. THE FA CONFIRMED SMOKE IN THE CABIN. INSPEC TED ALL OVERHEAD LIGHTS IN CABIN AND LAV. NO DEFECTS NOTED. PERFORMED RR FIM TASK 72-00-00-810-814. RAN BOTH ENGINES INDIVIDUALLY WITH BLEED AND PACKS ON FOR 20 MINUTES AT FULL POWER. COULD NOT DUPLICATE. OPPS CHECK GOOD CLOSED 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007030900255 20070309 00255 NM 2007 3 9 SWAA071244 1 20070306 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030900256 20070309 00256 NM 2007 3 9 SWAA071245 1 20070306 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030900258 20070309 00258 NM 2007 3 9 SWAA071247 1 20070306 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030900259 20070309 00259 NM 2007 3 9 SWAA071242 1 20070306 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030900260 20070309 00260 NM 2007 3 9 SWAA071249 1 20070306 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030900262 20070309 00262 NM 2007 3 9 SWAA071255 1 20070307 A 2530 41610019 COFFEEMAKER BOEING 737 7375H4 138449D NM CABIN FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 527SW 26569 F/A REPORTS BURNING SMELL FROM FWD COFFEEMAKER. REMOVED AND REPLACED COFFEEMAKER PER MM. 2 L 7 2 4F RT A16WE 2007030900263 20070309 00263 NM 2007 3 9 SWAA071262 1 20070307 A 5310 6516352 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 18Y CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007030900264 20070309 00264 NM 2007 3 9 SWAA071267 1 20070307 A 5753 6543430129 STRUCTURE BOEING 737 7373G7 1384595 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED C3 CHECK, FOUND LEFT WING INBOARD FORE FLAP DELAMINATED AT UPPER INBOARD END. REMOVED AND REPLACED FOR E FLAP PER MM. 2 L 7 2 4F RT A16WE 2007030900265 20070309 00265 NM 2007 3 9 SWAA071263 1 20070307 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 23R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007030900266 20070309 00266 NM 2007 3 9 SWAA071270 1 20070307 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030900267 20070309 00267 NM 2007 3 9 SWAA071261 1 20070307 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030900272 20070309 00272 NM 2007 3 9 SWAA071260 1 20070307 A 5310 6546958 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 440 TO BS 460, STR 17L. REMOVED AND REPLACED CREASE BE AM WEB PER SRM. 2 L 7 2 4F RT A16WE 2007030900275 20070309 00275 NM 2007 3 9 SWAA071266 1 20070307 A 2750 65522111 TORQUE TUBE BOEING 737 7373H4 1384600 NM T/E FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD MID FLAP TORQUE TUBE OUTBOARD END CORRODED. REMOVED AND REPLACED TORQ UE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007030900276 20070309 00276 NM 2007 3 9 SWAA071259 1 20070307 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM L2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. REMOVED AND REPLACED GIRT BAR H OOK PER MM. 2 L 7 2 4F RT A16WE 2007030900280 20070309 00280 NM 2007 3 9 SWAA071258 1 20070307 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM R1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. REMOVED AND REPLACED GIRT BAR H OOK PER MM. 2 L 7 2 4F RT A16WE 2007030900283 20070309 00283 NM 2007 3 9 USAA070155 1 20070227 A 5320 FLOOR SUPPORT BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 FLOOR SUPPORT, STA 770 LBL 6 HAS CORROSION. DRILLED HOLES, TREATED, PRIMED, INSTALLED PLATES PER TR 53-10-06B, SRM 51-4 0-02, COR TASK C53-208-01, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007030900285 20070309 00285 NM 2007 3 9 SWAA071248 1 20070306 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007030900289 20070309 00289 NM 2007 3 9 SWAA071251 1 20070306 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007030900294 20070309 00294 NM 2007 3 9 SWAA071252 1 20070306 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 433LV 33716 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007030900298 20070309 00298 2007 3 9 SWAA071264 4 20070307 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM EVAC SLIDE MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 615SW 27698 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2007030900299 20070309 00299 NM 2007 3 9 SWAA071269 1 20070307 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND STRINGER 8L CRACKED AT BS 1010. REMOVED AND REPLACED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007030900301 20070309 00301 NM 2007 3 9 SWAA071268 1 20070307 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 424WN 29828 DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007030900305 20070309 00305 NM 2007 3 9 USAA070144 1 20070227 A 5230 6547952166M DOOR FRAME BOEING 737 737401 1384701 NM AFT CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 AFT CARGO DOOR FWD SIDE FR STA 795.23 S 22R HAS CRACK. REPLACED DOOR PER IMM 52-31-00-4, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007030900306 20070309 00306 NM 2007 3 9 USAA070145 1 20070227 A 5330 DOUBLER BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 500 B-C AT NR 2 ANTENNA DOUBLER HAS CORROSION. REMOVED DOUBLER & INSTALLED FAB'D DOUBLER PER SRM 51-10-02; CORR LEV EL 2; TASK C53-208-01, DEFECT SIZE: 6 INCHES. 2 L 7 2 4F RT A16WE 2007030900307 20070309 00307 NM 2007 3 9 USAA070146 1 20070227 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 294.5 - 312, RBL 16 HAS CORROSION. REMOVED DAMAGED PART & INSTALLED NEW PER SRM 53-00-04; CORR LEVEL 1; TASK C53-10 7-02, DEFECT SIZE: 18 INCHES. 2 L 7 2 4F RT A16WE 2007030900308 20070309 00308 NM 2007 3 9 USAA070147 1 20070227 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 727D & 727G STR 25R HAS CORROSION. REMOVED DAMAGE & INSTALLED FAB'D PARTS PER SRM BAC SPEC 1496-377; CORR LEVEL 2; TASK C53-202-01, DEFECT SIZE: 10 INCHES. 2 L 7 2 4F RT A16WE 2007030900309 20070309 00309 NM 2007 3 9 USAA070148 1 20070227 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 727G-767 JUST ABOVE STR 25R HAS CORROSION. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER SRM BAC SPEC 1496-377; CORR LEVEL 2; TASK C53-202-01, DEFECT SIZE: 40 INCHES. 2 L 7 2 4F RT A16WE 2007030900310 20070309 00310 NM 2007 3 9 USAA070149 1 20070227 A 5320 SUPPORT BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 947-967 LBL 25 HAS CORROSION. REMOVED DAMAGE & INSTALLED FAB'D REPAIR PARTS PER SRM 53-60-51; CORR LEVEL 2; TASK C5 3-107-02, DEFECT SIZE: 20 INCHES. 2 L 7 2 4F RT A16WE 2007030900311 20070309 00311 NM 2007 3 9 USAA070150 1 20070227 A 5320 ATTACH FITTING BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 328 LBL 45 HAS CORROSION. REMOVED DAMAGE & INSTALLED FAB'D PARTS PER BOEING DWG 65-45834; CORR LEVEL 1; TASK C53-20 2-01, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007030900312 20070309 00312 NM 2007 3 9 USAA070151 1 20070227 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 T-CAP SECTION FROM LBL 9-RBL 52, REUSING SPLICES LBL 13-RBL 6, 6 SPOTS CORROSION. REMOVED DAMAGE, INSTALLED CAP PER TR 53-60-01 REV A; CORR LEVEL 2; TASK C53-107-02, DEFECT SIZE: 2 INCHES DIA AT 6 SPOTS. 2 L 7 2 4F RT A16WE 2007030900313 20070309 00313 NM 2007 3 9 USAA070152 1 20070227 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 947-996 HAS CORROSION. REMOVED DAMAGED Z AND INSTALLED NEW PER SRM 51-40-02; CORR LEVEL 2; TASK C53-107-01, DEFECT SIZE: 50 INCHES. 2 L 7 2 4F RT A16WE 2007030900314 20070309 00314 NM 2007 3 9 USAA070142 1 20070227 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 850-890 STR 2R - 2L, SKIN DEEPLY GOUGED/CHAFED AT FRONT OF DORSAL MOUNT. INSTALLED DOUBLER & TRIPLER PER EA 98446, DEFECT SIZE: 16"L X 1"W X .010"D. 2 L 7 2 4F RT A16WE 2007030900315 20070309 00315 NM 2007 3 9 USAA070154 1 20070227 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 312 LBL 8-0, AROUND NUT PLATES ON FLOORBEAM HAS CORROSION. REMOVED T-CUP, PICKED UP HOLES, TREATED, PRIMED, INSTALL ED NUT PLATES PER SRM 53-10-51; CORR TASK C53, DEFECT SIZE: .5 INCH 2 L 7 2 4F RT A16WE 2007030900316 20070309 00316 EU 2007 3 9 USAA070166 1 20070227 A 5321 FLOOR PANEL AIRBUS A321 A321211 3930370 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 167US 1442 FLOOR PANEL 262 HG CRACKED. MANUFACTURED REPLACEMENT PART PER MCGILL IRM 9701, REV F, DEFECT SIZE: 6 INCHES. 2 L 7 2 4F RT A28NM 2007030900317 20070309 00317 NM 2007 3 9 USAA070156 1 20070227 A 5320 FLOOR SUPPORT BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 UNDER SIDE OF FLOOR SUPPORT, STA 770, LBL 23 HAS CORROSION. REINSTALLED REPAIR & NUT PLATES PER TR 53-10-06B, DRM 51-40 -02; CORR TASK C53-208-01, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007030900318 20070309 00318 NM 2007 3 9 USAA070157 1 20070227 A 5320 FLOOR SUPPORT BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 770, LBL 16 ON FLOOR SUPPORT HAS CORROSION. INSTALLED NUT PLATES PER TR 53-10-06B, SRM 51-40-02; CORR TASK C53-208- 01, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007030900319 20070309 00319 NM 2007 3 9 USAA070158 1 20070227 A 5320 FLOOR SUPPORT BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 FLOOR SUPPORT, STA 770, LBL 12 HAS CORROSION. TREATED, PRIMED & REINSTALLED NUT PLATES PER TR 53-10-06B, SRM 51-40-02; CORR TASK C53-208-01, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007030900320 20070309 00320 NM 2007 3 9 USAA070159 1 20070227 A 5320 FLOOR SUPPORT BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 AFT CARGO COMPARTMENT STR 28R HAS CORROSION. REMOVED DAMAGE, INSTALLED REPAIR PARTS PER TR 53-10-06B; CORR TASK C53-208 -01, DEFECT SIZE: 3 INCHES. 2 L 7 2 4F RT A16WE 2007030900321 20070309 00321 NM 2007 3 9 USAA070160 1 20070227 A 5340 STRINGER CLIP BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STRINGER CLIP, STA 847 S24R HAS CORROSION. REMOVED & REINSTALLED CLIP PER DWG 65-47960; CORR TASK C53-208-01; LEVEL 2, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007030900322 20070309 00322 NM 2007 3 9 USAA070161 1 20070227 A 5320 ATTACH ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 500G S28I HAS CORROSION. REMOVED ANGLE, FAB'D NEW, TREATED & PRIMED PER SRM 51-10-02; CORR TASK C53-208-01, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007030900323 20070309 00323 NM 2007 3 9 USAA070162 1 20070227 A 5347 CARGO TRACK BOEING 737 737401 1384701 NM CARGO BAY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 400-500G AT S26R CARGO TIE DOWN TRACKS. MADE NEW TIE DOWN TRACK, TREATED & PRIMED PER SRM 53-00-53, 53-10-02; CORR TASK C53-202-01, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007030900324 20070309 00324 NM 2007 3 9 USAA070163 1 20070227 A 5320 STRAP BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STRAP BETWEEN BS 748-787 HAS CORROSION. FAB'D STRAP PER BOEING DWG 65-47957 & SRM 51-20-01; CORR TASK C53-202-01; LEVEL 2, DEFECT SIZE: 3 X 4 INCHES. 2 L 7 2 4F RT A16WE 2007030900325 20070309 00325 NM 2007 3 9 USAA070164 1 20070227 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 847-867 S26R ON TRANSITION ANGLE HAS CORROSION. REMOVED & INSTALLED NEW INTERCOSTAL PER SRM 53-60-53, 51-10-01, 51- 20-01; CORR TASK C53-208-01, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007030900326 20070309 00326 NM 2007 3 9 USAA070165 1 20070227 A 5320 SUPPORT ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 787 S-27-S26R ON FRAME TO SKIN ATTACH POINT SUPPORT ANGLES HAVE CORROSION. REPLACED SUPPORT ANGLE, TREATED, PRIMED, INSTALLED PER SRM 53-00-01, 53-00-07; CORR TASK C53-202-01, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007030900327 20070309 00327 NM 2007 3 9 USAA070153 1 20070227 A 5320 SUPPORT ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 STA 727D-727E ABOVE S25L, AROUND SCREW HOLES ON SUPPORT ZEE HAVE CORROSION. FOUND CORROSION OUT OF LIMITS, CHANGED ZEE PER SRM 53-60-53, 53-20-01; CORR LEVEL 2; TASK C53-202-01, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007030900328 20070309 00328 NM 2007 3 9 USAA070169 1 20070228 A 5310 DOOR FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 23933 AFT FRAME OF FWD CARGO DOOR CUTOUT STA 492.4, RT S-24R HAS CRACK. CUT OUT DAMAGE, FAB'D DOUBLER, INSTALLED REPAIR PER E A 98508, DEFECT SIZE: 0.125 INCH. 2 L 7 2 4F RT A16WE 2007030900329 20070309 00329 NM 2007 3 9 USAA070168 1 20070228 A 5310 DOOR FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 23933 FWD FRAME OF FWD CARGO DOOR CUTOUT STA 440 RT NR 2 STOP HAS CRACK. CUT OUT DAMAGE, FAB'D DOUBLER & INSTALLED PER EA 985 09, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007030900330 20070309 00330 EU 2007 3 9 USAA070167 1 20070228 A 5321 D5367019500400 FLOOR PANEL AIRBUS A321 A321211 3930370 EU FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 163US 1417 PANEL 251 AG FRAME 47-47.5 DAMAGED. MANUFACTURED NEW PANEL PER MCGILL IRM 9701 REV F, DEFECT SIZE: 2 X 1 INCH. 2 L 7 2 4F RT A28NM 2007030900331 20070309 00331 NM 2007 3 9 BB07019 1 20070302 A 3397 WIRE BOEING 767 7672B7 1385107 NM CABIN DAMAGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 256AY 26847 MAINTENANCE FOUND FLOOR LEVEL EMERGENCY LIGHTS BETWEEN ROWS 3 AND 5 RIGHT INOPERATIVE. REPAIRED WIRING. NO FURTHER FAU LTS. 2 L 7 2 4F RT A1NM 2007030900332 20070309 00332 NM 2007 3 9 BB070019 1 20070302 A 3397 WIRE BOEING 767 7672B7 1385107 NM CABIN DAMAGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 256AY 26847 MAINTENANCE FOUND FLOOR LEVEL EMERGENCY LIGHTING INOPERATIVE BETWEEN ROWS 3 AND 5 RIGHT. ACCOMPLISHED REPAIR TO WIRING. NO FURTHER FAULTS. 2 L 7 2 4F RT A1NM 2007030900333 20070309 00333 EU 2007 3 9 SA07016 1 20070228 A 3350 32145410 EPSU AIRBUS 320 A320214 3930316 EU CABIN BURNED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 121UW 21260 21260 1294 CLT - DURING WEEKLY CHECK, WHILE PERFORMING EPSU TEST, MAINTENANCE FOUND THE BATTERY AND BATTERY CHARGER UNITS AT FIN WL 11 BURNED, CAUSING EPSU TEST TO FAIL. MAINTENANCE REMOVED AND REPLACED THE CHARGER AND BATTERY AT WL 11. OPERATIONAL C HECK GOOD PER MM 33-51-38. 2 L 7 2 4F RT A28NM 2007030900338 20070309 00338 NM 2007 3 9 SB07020 1 20070228 A 3397 WIRE BOEING 737 737401 1384701 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 405US 23885 DCA - MAINTENANCE FOUND THE FLOOR PROXIMITY EMERGENCY LIGHTS AT THE LAST TWO ROWS OF SEATS, LEFT-HAND SIDE, INOPERATIVE. MAINTENANCE REPAIRED WIRING. OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD. 2 L 7 2 4F RT A16WE 2007030900339 20070309 00339 NE 2007 3 9 SA07019 2 20070302 A 7260 624912 PACKING AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE LT ENGINE CUT A USAA A UNSCHED LANDING W K INADEQUATE Q C FLUID LOSS CR CRUISE 1 EA 19 715UW 1051 575201 CLT - FLT 864 EN-ROUTE TPA TO PIT. DURING CRUISE, AND APPROXIMATELY 50 MILES SOUTH OF CLT, THE FLIGHT CREW REPORTED THA T THE LEFT ENGINE OIL QUANTITY WAS AT 2 QUARTS. OIL PRESSURE WAS FOUND NORMAL. THE FLIGHT DIVERTED TO CLT AND DECLARED AN EMERGENCY. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A CUT PACKING ON THE NUMBER ONE ENGINE DR IVEN HYDRAULIC PUMP SPLINE SHAFT. MAINTENANCE REPLACED THE PACKING, RAN AND LEAK CHECKED THE ENGINE. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A28NM E37NE 2007030900340 20070309 00340 EU 2007 3 9 SA07020 1 20070303 A 3397 PIN AIRBUS A319 A319112 3930323 EU WIRE HARNESS BENT A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 705UW 0929 DCA - THE TEST OF THE EMERGENCY EXIT LIGHT SYSTEM FAILED, FAULTING EPSU EXT LOAD L ON THE FORWARD CIDS PANEL. MAINTENAN CE REPLACED THE AFT LEFT EMERGENCY POWER SUPPLY BATTERY, WHICH DID NOT FIX THE PROBLEM. THE AIRCRAFT WAS RELEASED ON ME L. SUBSEQUENTLY, MAINTENANCE FOUND AND CORRECTED A BENT PIN IN THE AFT, RIGHT SLIDE ELECTRICAL HARNESS. OK FOR SERVICE . 2 L 7 2 4F RT A28NM 2007030900341 20070309 00341 2007 3 9 SA07017 4 20070228 A 2565 D30664105 SLIDE AIRBUS 320 A320214 3930316 EU PAX DOOR FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 106US 17443 3971 1044 PHL - THE FRONT ENTRY DOOR WAS OPENED INADVERTENTLY AFTER IT WAS ARMED. THE SLIDE DID NOT DEPLOY. MAINTENANCE REPLACED THE FORWARD, LEFT ENTRY DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2007030900342 20070309 00342 2007 3 9 SA07018 4 20070301 A 2565 D30665105 SLIDE AIRBUS 320 A320214 3930316 EU PAX DOOR FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 102UW 0844 PIT - DURING OPERATIONAL TEST OF THE LEFT HAND, AFT DOOR EMERGENCY ESCAPE SLIDE, THE DOOR ONLY OPENED HALF-WAY, THE DOOR ASSIST BOTTLE DID NOT WORK, THE SLIDE COVER DID NOT FULLY RELEASE, AND THE BOTTOM HALF (UNDERSIDE) OF THE SLIDE DID NOT INFLATE. MAINTENANCE REPLACED THE LEFT HAND, AFT DOOR EMERGENCY ESCAPE SLIDE. 2 L 7 2 4F RT A28NM 2007030900343 20070309 00343 NM 2007 3 9 BB07020 1 20070307 A 3397 WIRE BOEING 767 7672B7 1385107 NM CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 252AU 24765 EMERGENCY LIGHTS INOPERATIVE FORWARD OF SEAT 12F. MAINTENANCE RECONNECTED WIRING. NO FURTHER FAULTS. 2 L 7 2 4F RT A1NM 2007030900344 20070309 00344 2007 3 9 SB07021 4 20070304 A 2565 D17978113 BOTTLE BOEING 737 737401 1384701 NM EVAC SLIDE LOW PRESSURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 1351 23991 PHL - CREW REPORTED THE RIGHT AFT SERVICE DOOR EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE APPEARS TO BE IN THE RED. MAINTEN ANCE REMOVED AND REPLACED THE RIGHT AFT SERVICE DOOR EMERGENCY ESCAPE SLIDE PER MM 25-61-35-422-004. 2 L 7 2 4F RT A16WE 2007030900345 20070309 00345 SO 2007 3 9 RAIA00702036 1 20070223 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN UNKNOWN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 810HK 145231 PRE FLT NR 5535 - STL - EMERGENCY EXIT LIGHT INOP AT ROW 12. MAINTENANCE REMOVED AND REPLACED NR 6 INVERTER. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007030900346 20070309 00346 SO 2007 3 9 RAIA00702038 1 20070224 A 4950 BLEED AIR SYS EMB 145 EMB145LR 3260212 SO APU UNKNOWN A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 842HK 14500830 FLT NR 7986 - IAD - ENGINE WON'T START OFF APU BLEED. MAINTENANCE DEFERRED APU BLEED PER MEL. 2 L 7 2 4T RT T00011AT 2007030900347 20070309 00347 NM 2007 3 9 DHL2007751509 1 20070304 A 5320 INTERCOSTAL BOEING 727 727264 138408M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 751DH 22982 IN "C" CHECK, AFT CARGO COMPT INTERCOSTAL BETWEEN STA 1050-1070 STR 27L CORRODED. REMOVED INTERCOSTAL UPPER ANGLE IAW B 727 SRM 51-30-2. FAB NEW ANGLE IAW B727 SRM 53-10-2 USING 2024T3 .050 PO NR 9004174 DIM 19" BY 2" ALODINE AND PRIME PAR T IAW B727 IAW B727 SRM 51-10-2. INSTALLED ANGLE IAW B727 SRM 51--30-2. 2 L 7 3 4F A3WE 2007030900348 20070309 00348 NM 2007 3 9 DHL2007751512 1 20070226 A 5311 FRAME BOEING 727 727264 138408M NM FUSELAGE PUNCTURED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 751DH 22982 IN "C" CHECK, AFT CARGO COMPT FRAME AT STA 1090 IS PUNCTURED IN UPPER FLANGE RADIUS ABOVE STR 27L. REMOVAL TRANSITION P ANEL FOR ACCESS IAW B727 SRM 51-30-2, FAB FRAME REPAIR FROM 7075-0 .063 PO NR 9004384 DIM 8" BY 3 1/2"BY 1" BY 1" IAW B7 27 SRM 53-10-2 FIG 1. HEAT TREATED PART TO T6 IAW FAS ENGINEERING REPORT NR 2-37153-801 REV IR. TREATED AND PRIMED PAR TS IAW B727 SRM 51-10-2. INSTALLED FRAME REPAIR AT AFT CARGO COMPT FRAME STA1090 ABOVE STR.27L IAW B727 SRM 51-30-2. R EINSTALLED TRANSITION PANEL IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007030900349 20070309 00349 NM 2007 3 9 DHL2007751513 1 20070226 A 5311 FRAME BOEING 727 727264 138408M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 751DH 22982 A/C IN "C" CHECK, AFT CARGO COMPT FRAME AT STA 950C IS CORRODED AT BOTTOM BETWEEN STR 29L-28L. REPLACED DAMAGED SHEAR T IE AT BS 950C BETWEEN STR 29L-28L. FABRICATED NEW PART 7075-0 .080 PO NR 9002619 IAW B727 SRM 53-10-4 FIG 15 AND 53-10- 2 FIG 5. HEAT TREATED IAW B727 SRM 51-10-3 AND FAS0115. TREATED, PRIMED AND INSTALLED IAW B727 SRM 51-10-2 & 51-30-2, S RM 53-10-4 FIG 15 DIMENSION OF NEW PART 2" BY 6". 2 L 7 3 4F A3WE 2007031200003 20070312 00003 SO 2007 3 12 RAIA00702046 1 20070227 A 3397 WIRE EMB 145 EMB145 3260210 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 804HK 145082 PRE FLT NR 3507 - PIT - FLOOR EMERGENCY PROXIMITY LIGHTS INOP. MAINTENANCE RESECURED WIRE TO FLOOR PROX STRIP. OPS CHE CKS GOOD. 2 L 7 2 4F RT T00011AT 2007031200004 20070312 00004 SO 2007 3 12 RAIA00702044 1 20070226 A 5210 CABLE EMB 145 EMB145LR 3260212 SO PAX DOOR OUT OF ADJUST A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 831HK 145232 PRE FLT NR 7901 - ROA - PAX DOOR WILL NOT CLOSE. MAINTENANCE ADJUSTED DOOR CABLES FOR EXTERIOR AND INTERIOR HANDLE AND LUBED DOOR. 2 L 7 2 4T RT T00011AT 2007031200008 20070312 00008 SO 2007 3 12 RAIA00702039 1 20070225 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN DIRTY A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 841HK 145382 PRE FLT NR 8046 - IAD - FWD EMERGENCY LIGHT STRIP FLOOR PROXIMITY LIGHT INOP. MAINTENANCE CLEANED CONNECTOR ON FWD STRI P. 2 L 7 2 4T RT T00011AT 2007031200010 20070312 00010 CE 2007 3 12 DXTA200701999 1 20070304 A 2435 STARTER GEN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE UNKNOWN E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 342QS 5600324 AT VARIOUS STAGES OF FLIGHT LT FUEL FLOW INDICATION WAS ERRATIC AND ACCOMPANIED BY A RUMBLE. REMOVED & REPLACED LT STAR TER/GENERATOR IAW CE 560 M.M. 80-11-01. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2007031200014 20070312 00014 NE 2007 3 12 DXTA200701993 2 20070303 A 7321 MOTOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE NR 2 ENGINE FAILED E DXTA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 07 690QS 5605090 NR 2 ENGINE EEC FAILED AFTER DEPARTURE PASSING THROUGH 10,000 FEET. AFTER CHECKLIST ITEMS WERE COMPLETE ENGINE COMPRESS OR STALLS CONTINUED. VERIFIED DISCREPANCY. INSPECTED AND FOUND DEBRIS INSIDE BOV TORQUE MOTOR AND SECONDARY ORIFICE. RE MOVED AND REPLACED WITH OVERHAULED UNIT. LEAK CHECK GOOD. OPS CHECK GOOD. WORK DONE IAW & PWC 545A M.M. CHAPTER 75-30-01 . 2 L 7 2 4F 4 F RT A22CE E00059EN 2007031200015 20070312 00015 CE 2007 3 12 DXTA200701994 1 20070303 A 3246 WHEEL CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG VIBRATES E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 905QS 7500105 NOSE WHEEL SHIMMY ON TAKEOFF. ABORTED TAKEOFF. REMOVED THE LT AND RT NOSE WHEEL ASSEMBLIES AND REPLACED BOTH WITH OVERH AULED ASSEMBLIES IAW THE CE-750 M.M CHAP. 32-41-01. SERVICED LT & RT TIRES IAW CE-750 M.M CHAP. 12-10-30. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007031200018 20070312 00018 CE 2007 3 12 DIXA200700001 1 20070222 A 2497 ELECTRICAL SYS BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE COCKPIT ODOR E DIXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 05 314TL 2719 RK181 FLIGHT CREW REPORTED HEARING A POPPING SOUND FROM BEHIND THE COCKPIT LT SIDEWALL AREA FOLLOWED BY A SLIGHT ELECTRICAL OD OR FOR A PERIOD OF 15 SECONDS. NO SYSTEMS WERE AFFECTED AS ALL WERE OPERATING NORMALLY FOR THE DURATION OF THE FLIGHT (1 .2 HRS). MFG AIRCRAFT SERVICES TECHNICIANS WERE DISPATCHED AND REMOVED ALL LT SIDEWALL PANELS FOR ACCESS. INSPECTION OF ALL ELECTRICAL COMPONENTS, CONNECTORS, AND WIRING REVEALED NO DEFECTS. SUBSEQUENT FLIGHTS WERE ALL UNEVENTFUL. 2 H 7 2 4F 4 F RT A16SW E25EA 2007031200020 20070312 00020 NE 2007 3 12 ASMF200702008 2 20070227 A 7321 76960615 FUEL CONTROL DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE RT ENGINE FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 169PL 31130 8493 53175 718246 AIRCRAFT RETURNED TO PLATFORM DUE TO RT ENGINE DID NOT ACCELERATE. THE PARAMETERS WERE RT ENGINE N2 54 PERCENT, N1 29 PE RCENT AND LT ENGINE N2 56 PERCENT, N1 26 PERCENT, EGT 472 RT AND 462 LT AND FUEL FLOW 87 RT AND 53 LT. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK, THE RT FCU WAS REPLACED IAW MM 73-20-01 AND BOTH THRUST LEVERS WERE ADJUSTED IAW MM 76-11-00; FINALLY TRIM AND TEST WERE PERFORMED TO BOTH ENGINES IAW MM 71-00-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007031200021 20070312 00021 NM 2007 3 12 ASMF200703001 1 20070301 A 2910 7936913814 LINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE RT HYDRAULIC SYS LEAKING W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 158PL 49761 DURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE AFT CARGO COMPARTMENT. DURING MAINTENANCE CHECK, THE AFT RT C ARGO COMPARTMENT WALLS WERE REMOVED, DETECTING A HYDRAULIC LEAK IN THE HYDRAULIC LINE. THE HYDRAULIC LINE WAS REPLACED I AW MM 20-10-13, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007031200023 20070312 00023 SO 2007 3 12 RAIA00703005 1 20070301 A 3350 78812 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 803HK 145077 PRE FLT NR 3502 - PIT - EMERGENCY LIGHT INOP, FLOOR PROXIMITY LIGHT OVERWING AREA. MAINTENANCE REPLACED EMERGENCY FLOOR LIGHT STRIP. 2 L 7 2 4F RT T00011AT 2007031200024 20070312 00024 2007 3 12 BUE2007F00001 4 20070130 A 3418 COMPUTER BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE STALL WARNING FAULTED E BUEA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 9PW RK007 STICK SHAKER ACTIVATED SHORTLY AFTER ROTATION, STAYED ACTIVATED UNTIL 240KIAS. INDICATOR AND ANGLE OF ATTACK (AOA) INDE XER READ NORMAL. FLAPS WERE AT 10 DEGREES, LANDING GEAR WAS DOWN. AOA HEAT WAS SELECTED. AIRCRAFT HAD DEICE FLUID APP LIED. INSP OF EMPENNAGE UPON LANDING AND CLOSER INSP IN HANGAR SHOWS NO ICE OR OTHER ISSUES. VERIFIED FUNCTION OF AOA PROBES, VERIFIED FUNCTION OF FLAP FOLLOW UP SWITCHES. CHECKED PROBES FOR FREEDOM OF MOVEMENT, FLUID INGRESS AT CONNECTO R PLUGS, AND THAT THEY WOULD PROPERLY TRACK IN AIRSTREAM. CHECKED PROBES FOR GROUND AND AIR HEAT MODE PROPER FUNCTIONIN G. CANNOT FIND ANY REASON FOR STICK SHAKER ACTIVATING. LOGICALLY THE FAULT MUST BE IN THE RT SIDE. SWAPPED LT AND RT 2 H 7 2 4F 4 F RT A16SW E25EA 2007031200025 20070312 00025 CE 2007 3 12 AWM083022 1 20070303 A 3240 13275478 B-NUT BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BRAKE LINE LOOSE A AMWA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CE 07 176YV UE176 WHEN CREW ARRIVED AT DESTINATION THEY CALLED INTO MAINT CONTROL AND WROTE UP THE LT BRAKES NOT GETTING FULL BRAKING ACTI ON. TIGHTENED B-NUT, CLEANED AND BLED BRAKES, OPS CK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007031200027 20070312 00027 SO 2007 3 12 RAIA00703004 1 20070301 A 3620 WARNING SYSTEM EMB 145 EMB145EP 3260221 SO BLEED AIR SYS MALFUNCTIONED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 827HK 145021 FLT NR 5593 - STL - AFTER TAKEOFF GOT BLEED 2 OVERTEMP. MAINTENANCE PERFORMED GROUND MAINTENANCE OPS CHECK, NO DEFECTS AT THIS TIME. 2 L 7 2 4F RT T00011AT 2007031200029 20070312 00029 SO 2007 3 12 RAIA00703003 1 20070301 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 811HK 145256 PRE FLT NR 5549 - STL - EMERGENCY LIGHT OUT, AISLE FLOOD LIGHT. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BULB. 2 L 7 2 4T RT T00011AT 2007031200031 20070312 00031 SO 2007 3 12 C2XA07IA029 1 20070206 A 3350 276005 FUSE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL POWER SUPPLY BLOWN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11565 145621 DURING MAINTENANCE INSPECTION THE RT FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED A FUSE IN THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007031200034 20070312 00034 SO 2007 3 12 RAIA00702052 1 20070228 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 830HK 145313 POST FLT NR 5558 - STL - AISLE FLOOD LIGHT AFT SECTION INOP. MAINTENANCE RELAMPED AISLE FLOOD LIGHT, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007031200035 20070312 00035 NM 2007 3 12 CALA0700052 1 20070205 A 3350 D71702030 BATTERY PACK BOEING 767 767424ER 1385270 NM GE CF6 CF680C2* GL BS 533 INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76055 29450 THE EMERGENCY LIGHTS AT STA 533 DID NOT ILLUMINATE DURING TEST OF EMERGENCY LIGHT BATTERY PACK REPLACEMENT. THE POWER SU PPLY WAS REMOVED AND REPLACED IAW MM 33-61-07. 2 L 7 2 4F 4 F RT A1NM E23EA 2007031200036 20070312 00036 NM 2007 3 12 CALA0700053 1 20070205 A 3350 D71702030 BATTERY PACK BOEING 767 767424ER 1385270 NM GE CF6 CF680C2* GL BS 1545 INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76055 29450 THE EMERGENCY LIGHTS AT F/A SEAT STA 1545 DID NOT ILLUMINATE DURING TEST OF EMERGENCY LIGHT BATTERY PACK REPLACEMENT. PO WER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-51-07. 2 L 7 2 4F 4 F RT A1NM E23EA 2007031200039 20070312 00039 SO 2007 3 12 C2XA07CL019 1 20070202 A 5240 14533417405 CABLE EMB 145 EMB145EP 3260221 SO ALLSN AE300 AE3007A GL GALLEY DOOR FAULTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14940 145033 CLE FLIGHT NR 3107 THE CREW REPORTED THEY WERE UNABLE TO CLOSE GALLEY DOOR. MAINTENANCE INSPECTED AND REPLACED THE SERV ICE DOOR LOCKBOX CABLE AND BUSHINGS. THE DOOR WAS RE-RIGGED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007031200040 20070312 00040 NE 2007 3 12 DJFA2007019 2 20070213 A 7230 SEAL BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE COMPRESSOR LEAKING E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 23 898TA RK295 TRIP NR 1141843 CREW REPORTED A NOXIOUS OILY SMELL WHEN ENGINE IS AT HIGH POWER SETTINGS CONTINUING THROUGH CLIMB THEN D ISSIPATING DURING CRUISE. MAINTENANCE FOUND BROWN RESIDUE INTO BLEED DUCT WITH SOME CRYSTALLIZATION AND SUSPECTS LEAKIN G AT CENTRIFUGAL COMPRESSOR SEAL ON THE NR 2 ENGINE. ENGINE IS BEING CHANGED. TEARDOWN OF THE ENGINE REVEALED A CRACK AT THE NR 3 BEARING SCAVENGE OIL TUBE. RESIDUAL OIL WAS FOUND ON THE GAS GENERATOR ASSEMBLY NEAR THE CRACKED LINE. 2 H 7 2 4F 4 F RT A16SW E25EA 2007031200041 20070312 00041 CE 2007 3 12 GLBA2006910 1 20070219 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 228 CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 195GL UE195 UPON ROUTINE MAINTENANCE, EVIDENCE OF CORROSION WAS FOUND ON THE BELLY OF THE AIRCRAFT AT APPROXIMATELY FS 228.25, 1.5 I NCHES ON RT SIDE OF STRINGER 16. 2 L 7 2 4T 4 T RT A24CE E26NE 2007030900050 20070309 00050 WP 2007 3 9 070051 1 20070225 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS LOOSE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 871GA 53296 DURING A ROUTINE OVERNIGHT MAINTENANCE SERVICE CHECK LAS VEGAS MAINTENANCE REPORTED THAT THE ELECTROLUMINESCENT EGRESS P ATH LIGHTING WOULD NOT TEST BETWEEN ROWS 21 AND 24. FURTHER REPORT THAT TIGHTENED THE ELECTROLUMINESCENT STRIP ELECTRIC AL CONNECTION. A SATISFACTORY OPERATIONAL TEST WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE . 2 L 7 2 4F RT A6WE 2007030900064 20070309 00064 2007 3 9 SWIA200717841 4 20070220 A 2340 BUTTON CNDAIR CL600 CL6002B19 1900309 EA PA SYSTEM STUCK A SWIA O OTHER M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 932SW 7714 PA BUTTON IS STUCK IN THE ON POSITION AND OVERHEATING ODOR IS PRESENT. REPLACED TB 431-2 IAW UDM 20-18-00, P/N M81714/2 -DC1. 2 L 7 2 4F RT A21EA 2007030900065 20070309 00065 CE 2007 3 9 DXTA200701978 1 20070228 A 5330 PANEL CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE FUSELAGE DEPARTED E DXTA A UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 GL 07 639QS 5605139 ACCESS PANEL JUST AFT OF LT LANDING LIGHT IN JUST IN FRONT OF WING CAME OFF DURING FLIGHT. INSTALLED ACCESS PANEL UNDER LT WING IAW CE560XL MM CHP 53-30-00 2 L 7 2 4F 4 F RT A22CE E00059EN 2007030900070 20070309 00070 EA 2007 3 9 SIMA200705903 1 20070125 A 5320 67053110521 WEB CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 519AE 7787 4000 10131 FOUND WEB AT STATION 280 CORRODED AT FLOOR MATING AREA. SPLICED IN NEW WEB AT STATION 280 IAW AMERICAN EAGLE ENGINEERIN G ORDER CR-53MR-106. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007030900072 20070309 00072 2007 3 9 DXTA200701963 4 20070224 A 2210 WARNING SYSTEM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL AUTOPILOT SYS MALFUNCTIONED E DXTA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 07 990QS 7500190 AFTER ONE HOUR OF CRUISE FLIGHT THE TRIM CLACKER ACTIVATED AND RAN CONTINUOUSLY (AUTO-PILOT WAS NOT TRIMMING) AT LOWER A LTITUDES AND HIGHER TEMPS THE CLACKER SILENCED AND WORKED NORMALLY. C/W AUTOPILOT GROUND FUNCTIONAL CHECKS. SYSTEM OPS C HECKS GOOD ON GROUND IAW 750 MM 22-10-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007030900079 20070309 00079 SO 2007 3 9 ECI10518 1 20070218 A 2752 1159SCC2102 DRIVE UNIT GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6108 NE T/E FLAP ERRATIC E E0XA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 35 919CT 1051 FLAPS WOULD NOT EXTEND FOR THIRD TAKEOFF OF THE DAY. REMOVED AND REPLACED FLAP DRIVE UNIT. 2 L 7 2 4F 4 F RT A12EA E25NE 2007030900083 20070309 00083 CE 2007 3 9 DXTA200701972 1 20070226 A 3243 991205016 MASTER CYLINDER CESSNA 560 560XL 2076702 CE PWA 530 PW535A NE BRAKE SYS MALFUNCTIONED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 628QS 3051 5605305 LT SEAT RT BRAKE PEDAL IS SOFT REALITIVE TO LT BRAKE PRESSURE WHEN BRAKES ARE APPLIED. REMOVED AND REPLACED CAPTAINS RT MASTER CYLINDER IAW MM 32-42. BLEED OPS AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00053EN 2007030900091 20070309 00091 SO 2007 3 9 SWIA200717832 1 20070102 A 5411 FRAME EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 393SW 120330 FOUND LEFT NACELLE FRAME 1 CRACKED AT INBOARD WEB, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW LEFT FRAME NR 1 IAW EMB 120 SRM 51-40-02, SB 120-54-0036 PART II AND RII 54-900-1000. 2 L 7 2 4T RT A31SO 2007030900094 20070309 00094 EA 2007 3 9 A6WA200740071 1 20070222 A 5720 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE WING DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 448AW 7814 FOUND NR 15 HOLE AT WS 148 LHS IS ELONGATED TO .230 INCH. (M) MAINTENANCE REPAIRED BY CLEANING UP HOLE AND INSTALLING FREEZE PLUG IAW EO 601R57-10925A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007030900105 20070309 00105 EA 2007 3 9 SIMA200705005 1 20070217 A 7500 670960111 SEAL CNDAIR CL600 CL6002C10 1390015 EA BLEED AIR SYS BLOWN A SIMA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SW 21 518AE 8250 10126 CABIN SIDE WALL AT SEAT 17A FELT HOT TO THE TOUCH, EMERGENCY DECLARED, DIVERTED TO CMH. REPLACED RISER DUCT GAS KIT BEH IND CABIN SIDE IAW CRJ AMM. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007030900106 20070309 00106 SO 2007 3 9 SIMA200705101 1 20070213 A 5320 14525480603 SILL EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 712AE 15662 4800 145247 BAGGAGE DOOR FRAME LOWER SILL FOUND CORRODED. REMOVED EXISTING SILL, CLEANED AND TREATED AREA. INSTALLED NEW SILL IAW EMB SRM 51-40-02. RESTORED PROTECTIVE FINISH. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007030900109 20070309 00109 NM 2007 3 9 TSAA0732013 1 20070222 A 2760 CONTROL ROD BOEING 737 7372X6C 1384552 NM SPOILER INTERLOC FAILED A TSAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 13 747AS 23124 FLIGHT 924 HNLOGG - AFTER TAKEOFF, THE CREW WAS UNABLE TO MOVE THE LANDING GEAR HANDLE TO THE UP POSITION. CREW FOLLOWE D QRH PROCEDURES AND RETURNED TO HNL. MAINTENANCE REMOVED AND REPLACED THE GROUND SPOILER INTERLOCK VALVE CABLE ROD END PER AMM 27-62-51. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007030900111 20070309 00111 NM 2007 3 9 TSAA0732014 1 20070226 A 3244 26066712 TIRE BOEING 737 7372K5 138448X NM NR 2 MLG FLAT A TSAA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 WP 13 250TR 22597 FLIGHT 210 LIH-HNL - ON LANDING, ATC OBSERVED SMOKE FROM THE LEFT MAIN LANDING GEAR. CREW FOUND NORMAL BRAKING AND NO L OSS OF CONTROL. CREW REQUESTED THE AIRPORT FIRE EQUIPMENT AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NR 2 MAIN TIRE FLAT. MAINTENANCE REMOVED AND REPLACED BOTH THE NR 1 AND NR 2 MAIN WHEEL ASSEMBLIES PER AMM 3 2-45-11. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007030900113 20070309 00113 EA 2007 3 9 SIMA200706001 1 20070228 A 2150 A/C PACK CNDAIR CL600 CL6002C10 1390015 EA LEFT SEIZED A SIMA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 506AE 10056 SMOKE APPEARED FROM AIR CONDITIONING VENTS AS LEFT THROTTLE WAS ADVANCED. RECEIVED LEFT ENGINE BLEED CAUTION MESSAGE. FOUND LEFT PACK SEIZED, DEFERRED PER AMERICAN EAGLE CRJ MEL 21-12. 2 L 7 2 4F RT A21EA 2007030900143 20070309 00143 EA 2007 3 9 SWIA200717916 1 20070128 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 FS 280 RBL9 UPPER FLOOR SUPPORT HAS SUSPECT CRACK, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED RT I/B SUPPORT CLIP PER REO 601R-53-11-136 REV NC. 2 L 7 2 4F RT A21EA 2007030900145 20070309 00145 EA 2007 3 9 SWIA200717918 1 20070128 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 FS 625 LT SIDE CLIPS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP P/N 601-35012-51 P/O 71471 PER R EO 601R-53-61-422. 2 L 7 2 4F RT A21EA 2007030900147 20070309 00147 EA 2007 3 9 SWIA200717920 1 20070128 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 FOUND STA 484 LBL36 AND LBL27 INTERCOSTAL CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLE TO FS 4 84 INTERCOSTAL RBL 36 PER CRJ200 SRM 51-42-06 PG 11 AND 51-42-21 PG 17. 2 L 7 2 4F RT A21EA 2007030900148 20070309 00148 EA 2007 3 9 SWIA200717921 1 20070128 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BRAKE TRANSDUCER CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 RT FWD BRAKE TRANSDUCER BRACKET IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW BRACKET RT SIDE PER SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007030900181 20070309 00181 SO 2007 3 9 C2XA07CL025 1 20070301 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13970 145146 CLE FLIGHT NR 2401 THE CREW REPORTED A BURNING SMELL IN THE COCKPIT. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE AIRCRAFT ELECTRICAL SYSTEM. NO DEFECTS WERE FO UND AND NO SMELL WAS NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007030900188 20070309 00188 SO 2007 3 9 C2XA07IA047 1 20070226 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 14953 145071 IAH - FLT NR 3116, DURING A TEST THE EMERGENCY EXIT LIGHTING FAILED TO ILLUMINATE. MAINTENANCE RESET THE EMERGENCY LIGH TING SYSTEM AND OPERATIONALLY TESTED THE SYSTEM. THE DISCREPANCY COULD NOT BE DUPLICATED AND WAS THEN CLEARED. 2 L 7 2 4T RT T00011AT 2007030900199 20070309 00199 SO 2007 3 9 C2XA07CL027 1 20070302 A 3260 80069425 WARNING HORN EMB 145 EMB145LR 3260212 SO COCKPIT FAULTY A C2XA K NONE N FALSE WARNING DE DESCENT 1 SW 27 13956 22470 145078 CLE FLIGHT NR 2485 THE CREW REPORTED DESCENDING THRU 25000 FEET THEY HAD A AUDIBLE LANDING GEAR WARNING UNTIL LANDING GE AR WAS DOWN AND LOCKED. MAINTENANCE INSPECTED AND REPLACED THE AURAL WARNING UNIT. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007030900201 20070309 00201 SO 2007 3 9 C2XA07TY010 1 20070302 A 3350 110049 POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11565 145621 602 NR 482585- RT FWD EXTERIOR EMERGENCY LIGHT AND NR 2 AISLE CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 2 B ATTERY POWER SUPPLY UNIT IAW EMB 145AMM 33-50-04 OPS CK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007030900213 20070309 00213 SO 2007 3 9 C2XA07IA057 1 20070223 A 2612 FIRE WARNING EMB 145 EMB145XR 3260214 SO APU FALSE ACTIVATION A C2XA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 27 11140 145732 DEN - FLIGHT 3086, THE CREW REPORTED AN APU FIRE WARNING DURING ENGINE START WITH AN AUTOMATIC SHUTDOWN OF THE APU. NO SMOKE MESSAGE APPEARED IN RELATION TO THIS EVENT, AND WARNING EXTINGUISHED WHEN THE APU SHUT DOWN. DENVER MX INSPECTED THE AIRCRAFT AND PLACED THE APU ON MEL 49-00-00 "C", AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH ON THE SAME FLIGHT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND OPERATIONALLY CHECKED THE APU WITH NO DEFE CTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007030900221 20070309 00221 SO 2007 3 9 C2XA07IA058 1 20070307 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145EP 3260221 SO CARGO BAY MALFUNCTIONED A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 27 16927 1310 1310 145006 IAH FLT 2903, THE CREW REPORTED A BAGGAGE SMOKE WARNING IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAI NTENANCE REMOVED AND REPLACED THE AFT CARGO SMOKE DETECTOR, OPERATIONALLY CHECKED WIT NO DEFECTS, AND THE AIRCRAFT WAS A PPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007030900247 20070309 00247 SO 2007 3 9 C2XA07SH014 1 20070309 A 5230 14531545003 ANGLE EMB 145 EMB145XR 3260214 SO CARGO DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12157 145787 SHV DURING C-CHECK CORROSION DAMAGE WAS FOUND AT THE CARGO DOOR BOTTOM INBOARD "L" ANGLE NUTPLATES. MAINTENANCE REPAIRED CARGO DOOR BOTTOM INBOARD "L" ANGLE IAW EC5230-01144. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2007030900250 20070309 00250 NM 2007 3 9 SWAA071239 1 20070306 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 779SW 27884 EEPLS COVER LOOSE AT ROW 6 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007030900269 20070309 00269 EA 2007 3 9 SWIA200717937 1 20070131 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 869AS 7479 PAX DOOR AFT DRAG ANGLE IS CRACKED ADJACENT TO DOOR ASSIST CABLE PULLEY BRACKET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE SECTION PER CRJ200 REO 601R 52-11-513 REV 'A' SHEET 2. 2 L 7 2 4F RT A21EA 2007030900270 20070309 00270 EA 2007 3 9 SWIA200717938 1 20070131 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 869AS 7479 PAX DOOR,THE FWD WEB IS CRACKED UNDER THE HANDRAIL STOW BRACKET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FABRIC ATED REPAIR PARTS ON PAX DOOR FWD SIDE PANEL WEB IAW IAW CRJ200 REO 601R-52-11-702, REV NC & C/W SKYWEST RII 52-900-1001 CABIN DOOR REPAIR. 2 L 7 2 4F RT A21EA 2007030900271 20070309 00271 EA 2007 3 9 SWIA200717939 1 20070131 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 869AS 7479 PAX DOOR, THE AFT WEB IS CRACKED UNDER THE HANDRAIL STOW BRACKET AND IN THE RADIUS BETWEEN THE 3RD AND 4TH FIXED STEPS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED 3RD STEP AND REPAIR STOW BRACKET PER CRJ200 SRM 51-42-20 PG 23. 2 L 7 2 4F RT A21EA 2007030900273 20070309 00273 EA 2007 3 9 SWIA200717940 1 20070131 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 869AS 7479 FOUND CLIP CRACKED AFT SIDE OF 621 BULKHEAD LT, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP 601-35012-51 P/O 71 471 AT STA621 STR 14 IAW CRJ200 SRM 51-42-21 PG 17-21 51-40-11 PG 4,15. 2 L 7 2 4F RT A21EA 2007030900274 20070309 00274 EA 2007 3 9 SWIA200717941 1 20070131 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 869AS 7479 FS 280 LBL9-13 CRACKS BOTH FLOORBEAM SUPPORT ATTACH CLIPS AND 280 BEAM UPPER AND LOWER, DISCOVERED DURING C-CHECK INSPEC TION. INSTALLED REPAIR PARTS AT FS280 LBL9-13 UPPER/LOWER BEAM REPAIR PER REO 601R 53-11-138 AND REO 601R 53-11-171. 2 L 7 2 4F RT A21EA 2007030900277 20070309 00277 EA 2007 3 9 SWIA200717943 1 20070131 A 5420 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 869AS 7479 ENG BEAM RBL8.0 UPPER WEB SUPPORT ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW SUPPORT ANGLE AT R BL8.0 UPPER WEB PER CRJ200 SRM 51-42-06 PG 13. 2 L 7 2 4F RT A21EA 2007030900278 20070309 00278 EA 2007 3 9 SWIA200717944 1 20070131 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT MLG WW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 869AS 7479 LT WHEEL WELL HAS THE BRAKE TRANSDUCER BRACKET CRACKED/BROKEN AT TOP MID OF THE WHEEL WELL, DISCOVERED DURING C-CHECK IN SPECTION. REPLACED BRAKE TRANSDUCER BRACKET AT LT SIDE WHEEL WELL IAW CRJ200 SRM 51-77-00 PG 1 PARA 3. 2 L 7 2 4F RT A21EA 2007030900279 20070309 00279 EA 2007 3 9 SWIA200717945 1 20070131 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT MLG WW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 869AS 7479 RT WHEEL WELL HAS THE BRAKE TRANSDUCER BRACKET CRACKED/BROKEN AT TOP MID OF THE WHEEL WELL, DISCOVERED DURING C-CHECK IN SPECTION. REPLACED BRAKE TRANSDUCER BRACKET AT RT SIDE WHEEL WELL IAW CRJ200 SRM 51-77-00 PG 1 PARA 3. 2 L 7 2 4F RT A21EA 2007030900281 20070309 00281 NM 2007 3 9 DHL2007751507 1 20070226 A 5311 FRAME BOEING 727 727264 138408M NM BS 700 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 751DH 22982 IN "C" CHECK, FWD CARGO COMPT FRAME STA 700 HAS 3 DENTS AT UPPER FLANGE BETWEEN STR 24L-25L. CUT OUT DAMAGED AREA APPRO X 1" BY 3/4" IAW B727 SRM 51-40-3 FIG 1. FAB REPAIR ANGLE FROM 7075-0 .063 PO NR 9004384 APPROX DIM 11.7" BY 4" IAW B72 7 SRM 51-40-3 FIG 1 AND SRM 53-10-2 FIG 3. HEAT TREATED MAT. TO T6 CONDITION IAW FAS FORM NR FAS0115 REV 10. INSTALLED REPAIR ANGLE AT FWD CARGO COMPT BS 700 STR 24L-25L IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2007030900282 20070309 00282 NM 2007 3 9 DHL2007751508 1 20070226 A 5311 FRAME BOEING 727 727264 138408M NM BS 660 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 751DH 22982 IN "C", FWD CARGO COMPT FRAME STA 660 HAS DEEP DENT AT UPPER FLANGE BETWEEN STR.23R-24R. CUT OUT DAMAGED AREA APPROX DI M 1 1/4" IAW B727 SRM 51-40-3. FAB DOUBLER REPAIR FROM 7075-0 .063 PO NR 9004384 APPROX DIM 13" IAW B727 SRM 51-40-3 PA GE 1 AND 3 AND SRM 53-10-2 FIG 3. HEAT TREATED MAT. TO T6 CONDITION IAW FAS FORM FAS0115 REV 10. INSTALLED DOUBLER REP AIR AT FWD CARGO COMPT FRAME STA 660 BETWEEN STR 23R-24R IAW B727 SRM 51-30-2 AND 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2007030900286 20070309 00286 2007 3 9 BAQA200700004 2 20070221 A 7321 0319858020 FUEL CONTROL TMECA UROCOP EC135 EC135T1 5620026 EU NR 1 ENGINE INOPERATIVE E BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 135MF 1063 32056 0281 DURING AN 800 HOUR INSPECTION, FOUND NR 1 ENGINE FUEL DEGRADE LIGHT WOULD NOT ILLUMINATE WHEN ENGINE PUT IN MANUAL MODE AND TWIST GRIP WAS ENGAGED. REMOVED AND REPLACED FCU 3 TIMES BEFORE TEST WOULD PASS. FUEL CONTROL P/N 0319858090 S/N AN R855, P/N 0319858240 S/N 578B BOTH FAILED THE FUNCTIONAL TEST. INSTALLED P/N 031985820 S/N 658B AND PROBLEM WAS CURED. 1 G 7 2 3U H88EU 2007030900288 20070309 00288 2007 3 9 DXTA200701991 4 20070302 A 2200 STATIC INVERTER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE AUTOPILOTS SYS DISCONNECTED E DXTA O OTHER S AFFECT SYSTEMS CR CRUISE 1 GL 07 314QS 5600441 RT PFD FAILURE ATTITUDE AND HEADING FLASH RAPIDLY ATT ANNUNCIATOR ON LT PFD FLASHES. HAPPENS INTERMITTENTLY. AUTOPILOT D ISCONNECTS FREQUENTLY WHEN COUPLED TO RT SIDE NR 2 RT PFD DISPLAY WORKS. R & R NR 1 & 2 STATIC INVERTER. OPS CHECK GOOD IAW MM 24-20-04. 2 L 7 2 4F 4 F RT A22CE E25EA 2007030900290 20070309 00290 CE 2007 3 9 DXTA200702004 1 20070307 A 3243 MASTER CYLINDER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE BRAKES MALFUNCTIONED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 325QS 5600425 LT BRAKE ON RT SIDE TRAVELS ALMOST TO FLOOR DURING BRAKE APPLICATIONS. REMOVED CO-PILOTS IB AND OB BRAKE MASTER CYLINDE RS AND INSTALLED NEW MASTER CYLINDERS IAW C560 MM 32-42-02. BLED BRAKES AS REQUIRED. 2 L 7 2 4F 4 F RT A22CE E25EA 2007030900292 20070309 00292 NM 2007 3 9 DXTA200702005 1 20070307 A 3150 UNKNOWN GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE UNKNOWN E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 727QS 113 30 SECONDS AFTER TAKEOFF WE GOT STALL SYS FAIL ELEV FEEL AND STICK PUSHER FAIL, ALL CB,S WERE IN. REMOVED AND REPLACED THE SPQC WITH AN INSPECTED UNIT AND PERFORMED A COMPLETE FUNCTIONAL TEST I/A/W G200 MM 34-15-00. COMPLIED WITH CMP'S 34 1601 AND 2703030. 2 L 7 2 4F 4 F RT A53NM E35NE 2007030900293 20070309 00293 GL 2007 3 9 BAQA200700005 2 20070301 A 7200 6890550 COMPRESSOR ALLSN AEROSP AS355 AS355F2 8680812 EU ALLSN 250C 250C20F 03013 GL ENGINE SEIZED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 942MS 13675 898 CAT40126 5498 CAE840394 PILOT WENT TO START NR 1 ENGINE. ENGINE WOULD NOT TURN. FOUND ENGINE SEIZED. REMOVED AND REPLACED ENGINE ASSEMBLY. BROU GHT ENGINE TO ARC, DISASSEMBLED ENGINE AND FOUND 2 (6TH STAGE) COMPRESSOR BLADES BROKEN AND SEIZED THE COMPRESSOR, ALSO REMOVED THE TURBINE ASSEMBLY DUE TO FOD. WILL REPLACE THE COMPRESSOR ASSEMBLY AND TURBINE ASSEMBLY. 1 G 7 2 3U 3 U H11EU E4CE 2007030900295 20070309 00295 NM 2007 3 9 SWAA071257 1 20070307 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. REMOVED AND REPLACED GIRT BAR H OOK PER MM. 2 L 7 2 4F RT A16WE 2007030900296 20070309 00296 CE 2007 3 9 DXTA200701997 1 20070304 A 3260 SQUAT SWITCH CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG OUT OF RIG E DXTA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 GL 07 319QS 5600519 SQUAT SWITCH INOPERATIVE ON TAKEOFF , LANDING GEAR WOULD NOT RETRACT, FLIGHT TIMER INOPERATIVE, AOA INDEXER INOPERATIVE, LOW SPEED AWARENESS, TAPE INOPERATIVE. FOUND SQUAT SWITCH ON LT MLG "H" BLOCK MOVED DURING SAFETYING. RIGGED SQUAT SWI TCH I/A/W 560 MM 32-61-00. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2007030900297 20070309 00297 CE 2007 3 9 DXTA200701996 1 20070303 A 3240 ACCUMULATOR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE BRAKES OVERSERVICED E DXTA O OTHER W S INADEQUATE Q C AFFECT SYSTEMS TX TAXI/GRND HDL 1 GL 07 341QS 5600341 UPON LANDING FELT PULSING IN BRAKE PEDALS AND PEDALS WERE HARD TO PRESS. BRAKE PRESSURE ACCUMULATOR PUMP (NOSE) CYCLES O N APPROXIMATELY EVERY 20-30 SECONDS. PUMP MOTOR SEEMS TO CYCLE ON MORE FREQUENTLY THAN NORMAL. TROUBLE SHOT SYSTEM. DET ERMINED BRAKE ACCUMULATOR OVER SERVICED, SERVICED ACCUMULATOR TO PROPER LEVEL OPS CK GOOD ALL WORK DONE I/A/W CITATION U LTRA M/M CHAPTER 12-13-02 2 L 7 2 4F 4 F RT A22CE E25EA 2007030900300 20070309 00300 2007 3 9 SWAA071254 4 20070307 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007031200012 20070312 00012 SO 2007 3 12 RAIA00703008 1 20070302 A 3350 7287580507 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 831HK 145232 PRE FLT NR 7899 - IAD - LAST STRIP OF EMERGENCY LIGHTS INOP (FLOOR PROXIMITY LIGHT). MAINTENANCE REPLACED EMERGENCY EXI T LIGHT STRIP LOCATED AFT (FLOOR PROXIMITY LIGHT), OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007031200042 20070312 00042 CE 2007 3 12 GLBA20060909 1 20070219 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 303-309 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 210UX UE210 UPON ROUTINE INSPECTION MAINTENANCE FOUND A 6 INCH CRACK 27.5 INCHES RT OF THE BELLY CENTERLINE FROM FS 303.75 TO FS 309 .75.MAINTENANCE REPAIRED THE 6 INCH CRACK 27.5 INCHES RT OF THE BELLY CENTERLINE FROM FS 303.75 TO 309.75 IAW SRM 51-7 0 AND TC 8.2.1. REPAIR DIMENSIONS 6.375 INCHES BY 15.750 INCHES. INSERT 11.750 INCHES BY 4.375 INCHES. 2 L 7 2 4T 4 T RT A24CE E26NE 2007031200044 20070312 00044 SO 2007 3 12 RAIA00702054 1 20070228 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 802HK 145066 PRE FLT NR 3571 - PIT - AISLE FLOOD LIGHT INOP, AFT SECTION. MAINTENANCE REMOVED AND REPLACED BULB, OPS CHECKS GOOD AT THIS TIME. 2 L 7 2 4F RT T00011AT 2007031200050 20070312 00050 SO 2007 3 12 RAIA00703011 1 20070304 A 2720 UNKNOWN EMB 145 EMB145LR 3260212 SO RUDDER MALFUNCTIONED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 836HK 145695 FLT NR 7959 - DEN - RUDDER 2 INOP/ABORTED T/O. MAINTENANCE RESET C/B AS PER FAULT ISOLATION MANUAL & PERFORMED AN OPS C HECK OF THE RUDDER SYS IAW MM PROCEDURES, NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2007031200051 20070312 00051 NM 2007 3 12 SWAA071283 1 20070308 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031200052 20070312 00052 NM 2007 3 12 SWAA071287 1 20070308 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031200053 20070312 00053 NM 2007 3 12 SWAA071286 1 20070308 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031200054 20070312 00054 NM 2007 3 12 SWAA071284 1 20070308 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031200055 20070312 00055 NM 2007 3 12 SWAA071275 1 20070308 A 5310 6546958 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 460 TO BS 480, STR 17L. REMOVED AND REPLACED CREASE BE AM WEB PER SRM. 2 L 7 2 4F RT A16WE 2007031200056 20070312 00056 NM 2007 3 12 SWAA071274 1 20070308 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 359, STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007031200057 20070312 00057 EU 2007 3 12 XN0A1359 1 20070201 A 2420 GCU AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE NR 2 FAULTED A XN0A D RETURN TO BLOCK G MULTIPLE FAILURE TX TAXI/GRND HDL 1 GL 23 472AS 125 NR 1 PITCH TRIM TRIPPED BEFORE TAXI. ALL COCKPIT LIGHTS STARTED FLASHING WITH POWER-UP FOR TAXI. LOST VSI INDICATORS T EMPORARILY. LOST TAWS INDICATIONS. FOUND NR 1 GCU CAUSING POWER INTERRUPTIONS. R/R NR 1 GCU AND DISCONNECTED NR 2 CSD, OPS CK GOOD IAW AMM CHAPTER 22-12-34. (2) R/R NR 1 GCU AND DISCONNECTED NR 2 CSD, OPS CK GOOD IAW AMM CHAPTER 24-21-12.( 3) R/R NR 1 GCU AND DISCONNECTED NR 2 CSD, OPS CK GOOD IAW AMM CHAPTER 34-11-50. R/R NR 1 GCU AND DISCONNECTED NR 2 CSD , OPS CK GOOD IAW CMM ST3400. WHILE T/S ITEMS NR 1 THRU NR 4, FOUND NR 2 ENGINE GCU FAULTY. R/R NR 2 ENGINE GCU. CSD R ECONNECTED, OPS CHECKS GOOD IAW AMM CHAPTER 24-21-12. DMI NR 7005 CLEARED. (STATUS:SUPP/CLOSED) 2 L 7 2 4F 4 F RT A35EU E23EA 2007031200059 20070312 00059 NE 2007 3 12 ASMF200702004 2 20070212 A 7321 76960615 FUEL CONTROL DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE LT SIDE FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 169PL 8453 2731 53175 728194 AIRCRAFT RETURNED TO PLATFORM, LT ENGINE DID NOT STABILIZE IN IDLE, THE PARAMETERS WERE THE FOLLOWING: EPR´S 1.03, N1 20 , EGT´S 486 DEGREE C, N2 44, FF 9700 POUND. LT ENGINE WAS TRIMMED IN IDLE WITH EPR´S 1.03, N1 27, EGT´S 460, N2 55, FF 1160 IAW MM 71-00-00 PAGES 514 AND 544, TESTED CORRECT. DURING OVERNIGHT CHECK, LT FCU WAS REPLACED AND TESTED IAW MM 73 -20-01 AND 71-00-01, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007031200061 20070312 00061 SO 2007 3 12 C2XA07IA027 1 20070124 A 3397 M8353610024L RELAY EMB 145 EMB145EP 3260221 SO ALLSN AE300 AE3007A GL LAVATORY LIGHT SHORTED A C2XA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 27 14942 145037 FLIGHT 1281, PILOT REPORTED THAT A LAV SMOKE INDICATION ILLUMINATED DURING CLIMB OUT. A VISUAL INSPECTION WAS PERFORMED AND SMOKE, FIRE AND/OR UNUSUAL ODORS WERE NOT NOTICED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE LAV SMOKE WARNING SYST EM OPERATIONALLY TESTED GOOD. DURING TROUBLESHOOTING RELAY K8100 FOR THE LAVATORY LIGHT ASSEMBLY WAS FOUND TO BE SHORTED . THE RELAY WAS REPLACED AND THE DISCREPANCY CLEARED. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007031200063 20070312 00063 CE 2007 3 12 ACE02050702 1 20070205 A 2750 1005240731 MOTOR BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA TE FLAP FAILED E YADA O OTHER B S SMOKE/FUMES/ODORS/SPARKS AFFECT SYSTEMS AP APPROACH 1 AL 03 113AX 994 UC41 FLAPS STOPPED AT TAKEOFF. RETRACTED TO UP ON THE GROUND. THE SMELL OF HOT ELECTRICAL WAS STRONG. REPLACED FAILED FLAP MOTOR AND GEAR BOX. 2 L 7 2 4T 4 T RT A24CE E4EA 2007031200065 20070312 00065 CE 2007 3 12 GLBA20060885 1 20070112 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 289 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 122UX UE122 RT FUSELAGE LOWER SKIN, FORWARD SPAR FLANGE HAS (2) PULLED RIVETS WITH 1.2500 INCH CRACK AT F.S. 289.0 AND W.S. 29.06. REPAIRED CRACK AND RIVETS IAW SRM 53-90-18. 2 L 7 2 4T 4 T RT A24CE E26NE 2007031200067 20070312 00067 EU 2007 3 12 U0GA114076 1 20070212 A 2612 FIRE WARNING UROCOP EC135 EC135P2 5620027 EU PWA PW206 PW206B 0 NE ACTIVATED E U0GA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 605SS 0471 10 MINUTES INTO THE FLIGHT, FIRE WARNING AUDIO WAS HEARD FOR A SHORT PERIOD OF TIME IN THE HEADSET. AIRCRAFT WAS RETURN ING TO DEPARTURE LOCATION AND THE AUDIO WAS HEARD ONCE MORE FOR A SHORT PERIOD OF TIME. NO LIGHTS ILLUMINATED ONLY AUDI O SOUND. 1 G 7 2 3U 3 U H88EU E42NE 2007031200072 20070312 00072 NM 2007 3 12 SWAA071291 1 20070308 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007031200074 20070312 00074 NM 2007 3 12 SWAA071279 1 20070308 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007031200077 20070312 00077 SO 2007 3 12 RAIA00702043 1 20070226 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 813HK 145044 POST FLT NR 5564 - STL - EMERGENCY ROW EXIT LIGHTS NOT WORKING AT 1A & 2A. MAINTENANCE REPAIRED WIRE ON LIGHT TRACK AT 1A AND 2A. LIGHTS CHECK OK. 2 L 7 2 4T RT T00011AT 2007031200078 20070312 00078 WP 2007 3 12 ABXA070067 1 20070303 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 973AX 47511 EMERGENCY LIGHTS FAILED TO TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00-8. 2 L 7 2 4F A6WE 2007031200080 20070312 00080 WP 2007 3 12 200700299 1 20070110 A 3350 7027181 SIGN DOUG DC9 DC9 3022002 WP CABIN FAILED B ERKR K NONE L NO TEST IN INSP/MAINT 1 WP 07 941AA 48155 SELF-ILLUMINATING EXIT LIGHT ON UPPER ANTI-COLLISION LIGHT ACCESS PANEL 5801A FAILED TEST IAW MM 11-00 PAGES 203 AND 20 4. REPLACED SELF-ILLUMINATING EXIT LIGHT ON UPPER ANTI-COLLISION LIGHT ACCESS PANEL, REF SRM 51-30-01 PG. 1 2 L 7 2 4F A6WE 2007031200084 20070312 00084 NM 2007 3 12 AWXA200700336 1 20070220 A 5340 D53231336202 FITTING AIRBUS A319 A319132 3930340 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 803AW 931 SAL - FOUND CORROSION ON FORWARD CARGO COMPARTMENT DOOR CUT OUT THRESHOLD CORNER FITTING, FR 24A, S37R. REPLACED FORWAR D CARGO COMPARTMENT DOOR CUT OUT THRESHOLD CORNER FITTING, FR 24A, S37R IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007031200090 20070312 00090 NM 2007 3 12 DHL2007751511 1 20070228 A 5311 FRAME BOEING 727 727264 138408M NM BS 318 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 751DH 22982 FOUND INTERIOR E/E COMPARTMENT, BS 318, RBL 18-24, WL 160, LEVELING COMPOUND BLOWN UP AT FASTENERS BY FRAME WALKWAY BEAM INTERSECTION. REMOVED LEVELING COMPOUND FOR CORROSION EVAL IAW B727 SRM 51-10-6. CORROSION FOUND OUT OF LIMITS AT FRA ME SHEAR TIE IAW B727 SRM 53-10-1, FIG 1. CUT OUT DAMAGE ON SHEAR TIE DIM. 5.5" BY 1" IAW B727 SRM 53-10-4, FIG 11. FA B SHEAR TIE USING 7075T6, .063, 5.5" BY .25" IAW B727 SRM 53-10-2, FIG 1. TREATED AND PRIMED PARTS AND AREA IAW B727 SR M 51-10-2. INSTALLED NEW SHEAR TIE IAW B727 SRM 51-30-2 AND 53-10-4, FIG 11. REAPPLIED LEVELING COMPOUND IAW B727 AMM 51-30-00. 2 L 7 3 4F A3WE 2007031200094 20070312 00094 NM 2007 3 12 AWXA200700324 1 20070302 A 5320 D53480043204 SILL AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 803AW 931 SAL - FOUND CORROSION ON L2 DOOR CUT OUT LOWER SILL, FR 67 + 19", +Y1250. REPAIRED L2 DOOR CUT OUT LOWER SILL, FR 67 + 19", +Y1250 IAW A319 SRM 53-41-14. 2 L 7 2 4F RT A28NM 2007031200096 20070312 00096 EU 2007 3 12 AWXA200700325 1 20070227 A 5347 D57130147200 SEAT TRACK AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 627AW 66 SAL - FOUND CORROSION ON MAIN CABIN SEAT TRACK, +Y765, FR 36, FR 36 + 17", FR 37 + 2", FR 38 + 9", FR 39 + 2" AND FR 40 + 16". REPLACED MAIN CABIN SEAT TRACK , +Y765, FR 36 - FR 41 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007031200097 20070312 00097 EA 2007 3 12 TRAX200700306 1 20070228 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 821AS 7194 LEFT FS 484 INTERCOSTAL CRACKED ON O/B SIDE. 2 L 7 2 4F RT A21EA 2007031200099 20070312 00099 NM 2007 3 12 AWXA200700327 1 20070214 A 5312 6545409245 PRESSURE PANEL BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND LEFT WHEEL WELL CEILING PRESSURE WEB CRACKED, BS 664 - BS 675, LBL 30 - LBL 35, WL 208. REPAIRED LEFT WHEEL WELL CEILING PRESSURE WEB, BS 664 - BS 675, LBL 30 - LBL 35, WL 208 IAW B737-300 SRM 53-60-51-2R4. 2 L 7 2 4F RT A16WE 2007031200101 20070312 00101 NM 2007 3 12 AWXA200700329 1 20070302 A 5313 6546877142 WEB BOEING 737 7373S3 1384711 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - FOUND CORROSION AROUND 2 FASTENERS ON S18A RIGHT WEB, UPPER SURFACE BETWEEN BS 695 - BS 706. REPAIRED S18A RIGHT WEB, BS 695 - BS 706 IAW AWA ER 03-5361-07052-SS5. THIS PART MUST BE REPLACED ON OR BEFORE 6,000 FLIGHT CYCLES OR 24 MO NTHS WHICHEVER COMES FIRST. 2 L 7 2 4F RT A16WE 2007031200102 20070312 00102 NM 2007 3 12 AWXA200700331 1 20070215 A 5754 65C26602217SP WEDGE BOEING 737 7373S3 1384711 NM ZONE 500 DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND LEFT WING NR 2 SLAT TRAILING EDGE WEDGE DELAMINATED, SS 139.65. REPAIRED LEFT WING NR 2 SLAT TRAILING EDGE WEDGE, SS 139.65 IAW B737-300 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 2007031200103 20070312 00103 NM 2007 3 12 AWXA200700332 1 20070215 A 5754 65C26601179SP WEDGE BOEING 737 7373S3 1384711 NM ZONE 500 DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND LEFT WING NR 1 SLAT WEDGE DEBONDED, SS 269. REPAIRED LEFT WING NR 1 SLAT WEDGE, SS 254.53 - SS 272.78 IAW B 737-300 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 2007031200104 20070312 00104 NM 2007 3 12 AWXA200700333 1 20070214 A 5753 6546431286 SKIN BOEING 737 7373S3 1384711 NM ZONE 600 DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND RIGHT WING OUTBOARD FORE FLAP, UPPER SURFACE DEBONDED, WS 282 - WS 303. REPAIRED RIGHT WING OUTBOARD FORE F LAP, UPPER SURFACE, WS 282 - WS 303 IAW B737-300 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 2007031200105 20070312 00105 NM 2007 3 12 AWXA200700334 1 20070214 A 5753 6546486150 WEDGE BOEING 737 7373S3 1384711 NM ZONE 600 DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND RIGHT WING INBOARD MID FLAP TRAILING EDGE WEDGE UPPER AND LOWER SURFACES DEBONDED, WBL 109 - WBL 168. REPAI RED RIGHT WING INBOARD MID FLAP TRAILING EDGE WEDGE UPPER AND LOWER SURFACES, WBL 109 - WBL 168. 2 L 7 2 4F RT A16WE 2007031200108 20070312 00108 EU 2007 3 12 TRAX200700308 1 20070301 A 3230 LANDING GEAR AEROSP ATR72 ATR72 EU NLG & MLG MALFUNCTIONED A ASOA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 640AS 405 LANDING GEAR WILL NOT RETRACT AFTER TAKEOFF. FLT 4858 CX ON 3/2/07. A/C RETURNED TO AGS AFTER T/O. LANDING GEAR RETRA CTION SYSTEM. 2 H 7 2 4T RT 2007031200109 20070312 00109 NM 2007 3 12 AWXA200700343 1 20070214 A 5210 SKIN BOEING 737 7373S3 1384711 NM ZONE 800 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 961 24060 MCN - FOUND CRACKED L1 DOOR SKIN AT THE 6TH AND 7TH STOP PIN CUT OUT FROM THE TOP, BEAM 12 AND BEAM 13. REPAIRED L1 DOO R SKIN AT THE 6TH AND 7TH STOP PIN CUT OUT FROM THE TOP, BEAM 12 AND BEAM 13 IAW ER 03-5200-07065-SS2. 2 L 7 2 4F RT A16WE 2007031200113 20070312 00113 NM 2007 3 12 HALA0700087 1 20070307 A 2150 WARNING LIGHT BOEING 767 76733A 1385209 NM ISOLATION VALVE UNKNOWN A HALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 13 587HA 33421 ETOPS SIGNIFICANT SYSTEM, L ISOLATION VALVE LIGHT ON WILL NOT GO OUT, PER M/M 36-11-00-715-149. OPS CHECK ISOLATION VAL VE OK. 2 L 7 2 4F RT A1NM 2007031200115 20070312 00115 EA 2007 3 12 TRAX200700311 1 20070302 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 821AS 7194 CRACK AT INTERCOSTAL FUSELAGE STA 559 CARGO BAY ENTRY DOOR UNDER PANEL 281LLF (MARKED). 2 L 7 2 4F RT A21EA 2007031200116 20070312 00116 NM 2007 3 12 HALA0700088 1 20070307 A 5100 NONE BOEING 767 76733A 1385209 NM NONE NONE A HALA O OTHER N FALSE WARNING CR CRUISE 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, " AIL LOCK LGT ILLUM AT ALL SPEEDS EICAS MSG AILERON LOCKOUT DISPLAYED. TROUBLE SHOT PER FIM 27-11-00. SYSTEM CK'S OUT OK. AIL LOCK LIGHT AND EICAS MSG EXTINGUISHED. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007031200117 20070312 00117 NM 2007 3 12 HALA0700091 1 20070224 A 5712 RIB BOEING 767 767300 1385204 NM LT WING CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 588HA 33466 LT WING FIXED LE BULLNOSE RIB IS CRACKED JUST I/B OF NR 4 I/B ROTARY ACTUATOR. REMOVED SLAT CURTAIN AT NR 4 SLAT I/B RO TARY ACT. REMOVED AND REPLACED BULLNOSE RIB AERO DYNAMIC FORMER (NOSE) REINSTALLED SLAT CURTAIN. ALL WORK DONE IAW SRM 51-40-02 PAR 4 AND 7 AND M/M 27-81-024-001 STEP 2 E (2) AND M/M 27-81-424-019 STEP 3 (6). 2 L 7 2 4F RT A1NM 2007031200121 20070312 00121 NM 2007 3 12 EIA2007026 1 20070128 A 5755 HINGE FITTING BOEING 747 747273C 1384896 NM WS 1028 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 INSTALLATION OF SPOILER HINGE FITTING AT WS1028.525 REQUIRES RIVETS AND TAPER LOOKS DUE TO DIFFICULTIES IN INSTALLING RI VETS, REPLACEMENT NEEDED. USE BACB30NX8K*Y HILOCKS WITH BACC30AC8 COLLARS PER BOEING MESSAGE 1-280951.970-8 DATED 5 FEB 07 2 L 7 4 4F A20WE 2007031200123 20070312 00123 NE 2007 3 12 DL757070192 2 20070308 A 7261 POWERPLANT BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 OVERSERVICED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 669DN 25142 P2803 ON TAKEOFF, SMOKE DETECTED IN CABIN FUMES IN COCKPIT CREW DONNED MASKS LAVATORY SMOKE DETECTORS HEARD A/C LANDED AND RET URNED TO GATE UNDER POWER OIL ODOR DETECTED IN CABIN BY MAINTENANCE WHEN ENTERED AFTER PAX DOOR OPENED. FOUND NR 2 ENG OIL OVERSERVICED AND OIL DRAINED 5 PINTS OF OIL FROM TANK. ODOR IMPROVED AND OIL PRESS IMPROVED. PERFORMED REMOVAL OF OIL CONTAMINATION FROM AIR CONDITIONING PNEUMATIC SYSTEMS PER MM. NO SMOKE OR ODOR NOTED. ADJUSTED OIL PRESS DOWN ON N R 2 ENG, 950841 OK FOR SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007031200124 20070312 00124 NM 2007 3 12 DL76L070193 1 20070307 A 4920 491003096 TURBINE BOEING 767 767332 1382001 NM APU MAKING METAL A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 199DN 31474 28456 P2119 APU FAILED TO START AT DEPARTURE. FOUND METAL ON CHIP DETECTOR. REPLACED APU. 2 L 7 2 4F RT A1NM 2007031200128 20070312 00128 EU 2007 3 12 07FDEA00420 1 20070209 A 5310 CROSSBEAM AIRBUS 310 A310203 3930313 EU BS 3302 MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 409FE 273 PREVIOUS REPAIR FOUND LOCATED ON THE AFT PIT CROSSBEAM, RT, FS 3302, FR 61 AND Y160. REPAIR REQUIRES EVALUATION FOR MAJ OR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CO NFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 53-10-15 FIG 206 (SHEET3) AND USING FEDEX ENG AUTH 6 -5310-106688. REPAIR EVALUATED AND CLASSIFIED AS PER GMM 6-2-100 AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031200130 20070312 00130 NM 2007 3 12 07FDEA00648 1 20070305 A 5330 6518214 SKIN BOEING 727 727225 1384077 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FUSELAGE AT LT WING LEADING EDGE ROOT AT BS 720D, 10" - 14" AT STRINGER 19L, LAP AREA IS WORN FROM PANEL CONTACT. BLEN DED DAMAGED AREA REF 53-30-1 PAGE 2A. FOUND TO BE OUT OF LIMITS REF SRM 53-30-1 PG 2C. REPAIRED AREA WITH DOUBLER AND FILLER REF SRM 53-30-3 FIG 5. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007031200132 20070312 00132 NM 2007 3 12 07FDEA00650 1 20070305 A 5340 65453132 STRINGER CLIP BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FOUND MAIN CABIN FS 540, STR 3 R STRINGER CLIP HAS NO RADIUS AND HAS SHARP EDGES ON TOP SIDE. REPLACED STRINGER CLIP AT STA 540, STR 3R REFERENCE SRM 51-30-2. CLASSIFIED AS MAJOR REPAIR. 2 L 7 3 4F A3WE 2007031200133 20070312 00133 NM 2007 3 12 07FDEA00651 1 20070305 A 5340 654531314 STRINGER CLIP BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FOUND MAIN DECK BODY FRAME STRINGER CLIP IS CRACKED AT BS 950D, SRT 9R. REPLACED STRINGER CLIP REF SRM 51-30-2. CLASSI FIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007031200134 20070312 00134 NM 2007 3 12 07FDEA00652 1 20070305 A 5280 651756396 DOOR BOEING 727 727225 1384077 NM NLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FOUND NLG RT FWD DOOR INNER SKIN IS CRACKED AT INBD EDGE, FORWARD END CUT OUT DAMAGE. INSTALLED TYPICAL WEB REPAIR, REF SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 2007031200136 20070312 00136 NM 2007 3 12 07FDEA00653 1 20070305 A 5753 652163091 SKIN BOEING 727 727225 1384077 NM FORE FLAP MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 463FE 22551 FOUND REPAIR AT LT WING INBD FOREFLAP LE SKIN 21" FROM IB END (EXTERNAL REPAIR). REPAIR REQUIRES EVALUATION FOR MAJOR/M INOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED REPAIR, FOUND NOT TO CONFORM TO SR M 57-50-4 FIG 1. REMOVED EXISTING REPAIR, PICKED UP ONE ADDITIONAL ROW OF FASTENERS TO CONFORM TO SRM REPAIR 57-50-4 FI G 7. REPAIR CLASSIFIED AS MAJOR. 2 L 7 3 4F A3WE 2007031200137 20070312 00137 WP 2007 3 12 07FDEA00654 1 20070305 A 5230 FITTING DOUG MD10 MD1010F 3022112 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 566FE 46989 FOUND MAIN CARGO DOOR NR 1 SPOOL FITTING HAS CRACK INDICATION. REMOVED SPOOL FITTING IAW DC10/MD10 SRM 51-33-01 VOL 2 D RILLED UP NEW FITTING IAW DAC DWG AFA 7132 REV J INSTALLED FITTING IAW DC10/MD10 SRM 51-33-01 VOL 2 DOOR TO BE RIGGED ON FEDEX N/R N00712. 2 L 7 3 4F RT A22WE 2007031200139 20070312 00139 WP 2007 3 12 07FDEA00656 1 20070305 A 5230 FITTING DOUG MD10 MD1010F 3022112 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 566FE 46989 FOUND MAIN CARGO DOOR NR 3 SPOOL FITTING HAS CRACK INDICATION. 2 L 7 3 4F RT A22WE 2007031200141 20070312 00141 NM 2007 3 12 AWXA200700339 1 20070306 A 7714 3301KGAMS1 TACH GENERATOR BOEING 757 7572G7 1384963 NM RT SIDE FAILED A AWXA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 WP 28 909AW 24522 DURING CRUISE FLIGHT, THE CREW DOCUMENTED THE FOLLOWING FAULTS ON LPS 7446894, 7446895, 7446896. CREW REPORTED THE FOLL OWING: RIGHT CENTER FUEL PUMP WAS INOPERATIVE. RIGHT ENGINE BLEED INOPERATIVE. RIGHT ENGINE N3 INDICATION INOPERATIVE. MX REPLACED THE N3 TACH GENERATOR AND THE NR 2 ENGINE SPEED CARD. OPERATIONAL CHECK WAS GOOD DURING ENGINE RUN. 2 L 7 2 4F RT A2NM 2007031200142 20070312 00142 EA 2007 3 12 TRAX200700314 1 20070219 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 PAX DOOR AFT DRAG ANGLE, (SUSPECTED CRACK) AS PER DOUG. 2 L 7 2 4F RT A21EA 2007031200145 20070312 00145 NM 2007 3 12 F3LA200700041 1 20070306 A 5313 D5347218820200 LONGERON AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 919FR 4679 1980 DURING C-3 CHECK, INSPECTION REPORTED CORROSION FOUND UNDER NUT CLIPS LT BEAM Y1292 BETWEEN CROSS BEAMS FR 58 AND FR 69 PROFILE 80. BURNISHED SURFACE CORROSION AND OVERSIZED HOLES TO REMOVE CORROSION IAW SRM 51-22-00, PAGE 11, AND EA A9-53 R-11805. 2 L 7 2 4F RT A28NM 2007031200147 20070312 00147 EU 2007 3 12 AWXA200700340 1 20070307 A 5347 D5311278220 SEAT TRACK AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 PHX - FOUND CORROSION ON MAIN CABIN SEAT TRACK, FR 20, -Y765, AT THE RIGHT FORWARD WINDSCREEN. REPAIRED MAIN CABIN SEAT TRACK, FR 20, -Y765, AT THE RIGHT FORWARD WINDSCREEN IAW A320 SRM 53-00-15 FIGURE 201. 2 L 7 2 4F RT A28NM 2007031200148 20070312 00148 EU 2007 3 12 AWXA200700341 1 20070307 A 5347 D5311278220 SEAT TRACK AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 PHX - FOUND CORROSION ON MAIN CABIN SEAT TRACK, FR 20, -Y1292, AT THE RIGHT FORWARD WINDSCREEN. REPAIRED MAIN CABIN SEA T TRACK, FR 20, -Y1292, AT THE RIGHT FORWARD WINDSCREEN IAW A320 SRM 53-00-15 FIGURE 201. 2 L 7 2 4F RT A28NM 2007031200149 20070312 00149 NM 2007 3 12 DHL2007751515 1 20070309 A 5311 FRAME BOEING 727 727264 138408M NM BS 1148 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 751DH 22982 AFT CARGO COMPT FRAME AT STA 1148 IS CORRODED AT BOTTOM BETWEEN STR 29R AND 30R. CUT OUT DAMAGED AREA 4" BY 1" BY 1". FABRICATED REPAIR SHEAR TIE (.063" BY 4.875" BY 3.5" BY 1") AND SHIM (.063" BY 3.5" BY 1.2") FROM 7075-T6 PO NR 9004690; TREATED AND PRIMED REPAIR PARTS AS REQ; AND INSTALLED REPAIR PARTS, ALL PER B727 SRM 53-10-4 FIG 14, 51-10-2, AND 51-3 0-2. 2 L 7 3 4F A3WE 2007031200150 20070312 00150 EA 2007 3 12 TRAX200700304 1 20070227 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 748EV 10158 SIDEWALL LIGHT INOP, CEILING ROW 1. FLT 4685 DEL 23 MINS N/C FLTS 4157, 4914, 4326 CX CABIN EMERGENCY LIGHTS - CEILING LEVEL FLOODLIGHTS. 2 L 7 2 4F RT A21EA 2007031200151 20070312 00151 NM 2007 3 12 SWAA071276 1 20070308 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007031200153 20070312 00153 NM 2007 3 12 KNNA200700010 1 20070125 A 5312 BULKHEAD BOEING 737 737297 1384480 NM PWA JT8 JT8D9 52048 NE BS 178 CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 147AW 22630 FOUND STA 178 BULKHEAD IS CRACKED AT W/L 234,RBL 9-RBL 10. FOUND PROVIDE INSTRUCTIONS ON REPAIR OF BULKHEAD AT STA 178 RBL 9-RBL 10 . 2 L 7 2 4F 4 F A16WE E2EA 2007031200155 20070312 00155 NM 2007 3 12 KNNA200700012 1 20070125 A 5312 2024T3 BULKHEAD BOEING 737 737297 1384480 NM PWA JT8 JT8D9 52048 NE BS 178 CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 147AW 22630 FOUND STA 178 BULKHEAD IS CRACKED AT STA 178 W/L 213.5, RBL1, W/L 224, LBL-1-RBL1, W/L 227, RBL 1. PROVIDE INSTRUCTIONS ON REPAIR OF BULKHEAD AT STA 178 W/L 213.5, RBL 1, 2 L 7 2 4F 4 F A16WE E2EA 2007031200156 20070312 00156 NM 2007 3 12 KNNA200700013 1 20070119 A 5242 SKIN BOEING 737 737297 1384480 NM PWA JT8 JT8D9 52048 NE E/E BAY DOOR DAMAGED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 147AW 22630 E/E BAY ACCESS DOOR EXTERIOR SURFACE, RT EDGE BEND. PROVIDE INSTRUCTIONS ON REPAIR OF E/E BAY DOOR . 2 L 7 2 4F 4 F A16WE E2EA 2007031200159 20070312 00159 NM 2007 3 12 HALA0700097 1 20070309 A 2710 550030019 ACTUATOR BOEING 767 76733A 1385209 NM AILERON UNKNOWN A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, "AILERON LOCKOUT" DISPLAYED ON EICAS. T/S PER FIM 27-11-00, FIG 104 AND THE RIGHT SAM FAULTED "R AIL LOCK ACT". PER FIM BLOCK 35, RESET AND FAULT DID NOT RETURN. FOR PRECAUTIONARY T/S, REMOVED AND REPLACED RIGHT AILERON LOCK-OUT ACTUATOR PER AMM 27-11-44 AND SYS OPS CKS GOOD. NO EICAS MSG'S. OK TO CONTINUE. 2 L 7 2 4F RT A1NM 2007031200162 20070312 00162 GL 2007 3 12 SWAA071294 2 20070308 A 7530 7064004 MOTOR BOEING 737 7373A4 1384585 NM CFMINT CFM56 CFM563B1US GL NR 2 ENGINE SHEARED A SWAA K NONE R PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 29 676SW 23288 AT FL 370 NR 2 ENGINE WILL NOT ATTAIN MAX CLIMB POWER. FOUND VBV MOTOR SHAFT SHEARED. REMOVED AND REPLACED VBV DRIVE M OTOR PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2007031200163 20070312 00163 NM 2007 3 12 SWAA071295 1 20070308 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND STRINGER 4L CRACKED AT BS 1010. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007031200166 20070312 00166 NM 2007 3 12 MWEA070040 1 20070228 A 5350 4913354501 RELEASE MECH BOEING 717 717200 1383700 NM TAILCONE OUT OF ADJUST A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 909ME 55173 TAIL CONE DID NOT DEPLOY WHEN THE AFT PRESSURE BULKHEAD DOOR TEST WAS PERFORMED. CLEANED AND ADJUSTED RELEASE CLIP. 2 L 7 2 4F TR A6WE 2007031200167 20070312 00167 NM 2007 3 12 ABXA070066 1 20070227 A 5754 114T020136 PANEL BOEING 767 767232 1385132 NM L/E SLAT MISSING A ABXA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 GL 23 745AX 22222 RIGHT WING SLAT ANTI-ICE DUCT PANEL MISSING. REPLACED RIGHT WING ANTI-ICE DUCT SEAL DOOR IAW BOEING S/B 767-57-0045 AND AMM 57-41-58. 2 L 7 2 4F RT A1NM 2007031200175 20070312 00175 2007 3 12 MWEA070037 4 20070225 A 3417 102JD2FE PROBE BOEING 717 717200 1383700 NM RAM AIR TEMP FAILED A MWEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 13 917ME 55179 RAM AIR TEMPERATURE FAIL ON THE ANNUNCIATOR. REMOVED AND REPLACED RAM AIR TEMPERATURE PROBE. 2 L 7 2 4F TR A6WE 2007031200176 20070312 00176 WP 2007 3 12 ABXA070060 1 20070215 A 5730 591214425 SKIN PANEL DOUG DC9 DC941 302207N WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 CRACK ON LEFT LOWER WING SKIN PANEL JUST FORWARD OF BUTE DOOR 1501. REMOVED AND REPLACED SKIN FORWARD OF BUTE DOOR IAW DC9 SRM 51-30-1, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2007031200181 20070312 00181 NM 2007 3 12 ABXA070058 1 20070213 A 5420 313T3380244 ANGLE BOEING 767 767281 1385109 NM NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 CRACKS AT FASTENER HOLES LEFT AND RIGHT ON ANGLE INSIDE OF STRUT LOOKING UP THROUGH LIGHTNING HOLE ON AFT END. REMOVED A ND REPLACED CRACKED ANGLE IAW B767 SRM 51-40. 2 L 7 2 4F RT A1NM 2007031200184 20070312 00184 WP 2007 3 12 ABXA070059 1 20070215 A 5730 591214426 SKIN PANEL DOUG DC9 DC941 302207N WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 CRACK ON RIGHT LOWER WING SKIN PANEL JUST FORWARD OF BUTE DOOR 1601. REMOVED AND REPLACED SKIN PANEL IAW DC9 SRM. 2 L 7 2 4F A6WE 2007031200185 20070312 00185 NM 2007 3 12 ABXA070055 1 20070212 A 5713 113T14076 FRAME BOEING 767 767281 1385109 NM RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 RIGHT WING T-FRAME JUST INBOARD OF INBOARD FLAP HINGE HAD CORROSION. REPAIRED RIGHT WING T-FRAME IAW B767 SRM 57-51-02. 2 L 7 2 4F RT A1NM 2007031200186 20070312 00186 NM 2007 3 12 ABXA070057 1 20070212 A 5420 313T336079 ANGLE BOEING 767 767281 1385109 NM NR 1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 NR 1 PYLON TRAILING EDGE PANEL HAS CRACKED ANGLE ON INBOARD SIDE AND BROKEN NUT PLATE ON FORWARD OUTBOARD SIDE. REMOVED AND REPLACED ANGLE ON NR 1 PYLON TRAILING EDGE PANEL ON INBOARD SIDE AND REPLACED NUT PLATE IAW B767 SRM. 2 L 7 2 4F RT A1NM 2007031200190 20070312 00190 NM 2007 3 12 SWAA071292 1 20070308 A 5330 6545768 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007031200191 20070312 00191 NM 2007 3 12 SWAA071273 1 20070308 A 5312 6545819 PRESSURE PANEL BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND NLG WHEEL WELL WEB CRACKED AT BS 251, RBL 7.75. REPAIRED WEB PER ACO. 2 L 7 2 4F RT A16WE 2007031200192 20070312 00192 NM 2007 3 12 SWAA071289 1 20070308 A 5753 6546435277 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED C4 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED AFT F LAP PER MM. 2 L 7 2 4F RT A16WE 2007031200193 20070312 00193 NM 2007 3 12 SWAA071288 1 20070308 A 5753 6546435336 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2007031200195 20070312 00195 NM 2007 3 12 SWAA071281 1 20070308 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031200199 20070312 00199 EA 2007 3 12 TRAX200700317 1 20070303 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 PAX DOOR HANDLE BROKEN. 2 L 7 2 4F RT A21EA 2007031200200 20070312 00200 EA 2007 3 12 TRAX200700318 1 20070303 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 748EV 10158 REFER TO AFDL 335624 ITEM NR 1 EMERGENCY LIGHT AT ROW 1 OUT. 2 L 7 2 4F RT A21EA 2007031200202 20070312 00202 NM 2007 3 12 KNNA200700014 1 20070125 A 5311 KIT65C3785243 FRAME BOEING 737 737297 1384480 NM PWA JT8 JT8D9 52048 NE BS 178 CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 147AW 22630 FOUND STA 178 RT SIDE FRAME IS CRACKED AT WL 207. PROVIDE INSTRUCTION TO REPAIR CRACK BY INSTALLING A SPLICE OVER THE ( RIGHT SIDE) SIDE CHORD AT WL 212. 2 L 7 2 4F 4 F A16WE E2EA 2007031200203 20070312 00203 NM 2007 3 12 KNNA200700015 1 20070125 A 5312 2024T3 BULKHEAD BOEING 737 737297 1384480 NM PWA JT8 JT8D9 52048 NE BS 178 CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 147AW 22630 FOUND STA 178 BULKHEAD IS CRACKED AT WL-234, LBL-8 TO LBL-9. PROVIDE INSTRUCTION ON REPAIR OF BULKHEAD AT STA 178 LBL 8 - LBL 9 AND LBL-10-LBL 12. 2 L 7 2 4F 4 F A16WE E2EA 2007031200204 20070312 00204 NM 2007 3 12 KNNA200700016 1 20070112 A 5313 1498163 STRINGER SPLICE BOEING 737 737297 1384480 NM PWA JT8 JT8D9 52048 NE BS 663 ACTIVE A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 147AW 22630 FOUND CRACKED CHORD OF STRINGER 14L AT BS 663.75. PROVIDE INSTRUCTION ON REPAIR OF S14L AT BS 663.75. 2 L 7 2 4F 4 F A16WE E2EA 2007031200205 20070312 00205 EA 2007 3 12 TRAX200700288 1 20070223 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 FS 280 FWD CENTER FLOOR SUPPORT ANGLE CORRODED. REMOVED FS 280 FWD CENTER FLOOR SUPPORT ANGLE MH715 LOCATED HOLES IN SE RVICEABLE ANGLE P/N CC670-33292-13 IAW CRJ SRM 51-40-11 MH715. OK TO INSTALL. INSTALLED FWD CENTER FLOOR SUPPORT IAW C RJ CRM 51-42-06 & 51-42-21 JA10220 2-27-07. OK TO TOPCOAT. TOPCOATED IAW CRJ SRM 51-25-16 JA10220 2-27-07. REINSTALLE D AVIONICS COMPARTMENT LIGHT TO FS 280 SUPPORT ANGLE IAW CRJ 200 SRM 51-42-06. MDA1064 2-27-07. SUPPLEMENTAL - SDR CLO SED 03/01/07. 2 L 7 2 4F RT A21EA 2007031200206 20070312 00206 NM 2007 3 12 KNNA200700017 1 20070125 A 5312 65C3760716 VERTICAL BEAM BOEING 737 737297 1384480 NM PWA JT8 JT8D9 52048 NE BS 178 CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 147AW 22630 FOUND LBL 5.7 VERTICAL BEAM IS CRACKED BOTH FLANGES AT STA 178 BULKHEAD. PROVIDE INSTRUCTIONS ON REPAIR OF LBL 5.7 VERT ICAL CHORD AT STA 178. 2 L 7 2 4F 4 F A16WE E2EA 2007030900112 20070309 00112 NM 2007 3 9 TSAA0726015 1 20070226 A 2612 899929 FIRE LOOP BOEING 737 737236 1384476 NM NR 2 NACELLE FAILED A TSAA E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 837AL 23169 FLIGHT 246 HNL- ITO, DURING CLIMB, THE NR 2 ENGINE HAD AN OVERHEAT INDICATION. THE CREW SHUT DOWN THE NR 2 ENGINE AND A CTIVATED THE ENGINE FIRE EXTINGUISHING BOTTLES. THE AIRCRAFT RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REM OVED AND REPLACED THE NR 2 ENGINE FIRE LOOP ELEMENT PER AMM 26-11-1; REMOVED AND REPLACED THE FORWARD AND AFT ENGINE FIR E BOTTLES PER AMM 26-21-4. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007030900115 20070309 00115 SO 2007 3 9 SWIA200717844 1 20070217 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS UNSECURE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 227SW 120304 FOUND EXIT SIGN ON BIN DOOR ABOVE SEATS 9B-C DOES NOT ILLUMINATE. SECURED WIRE AT EXIT SIGN AT BIN 9B-C. OPERATIONAL C HECKS GOOD. 2 L 7 2 4T RT A31SO 2007030900117 20070309 00117 EA 2007 3 9 SWIA200717845 1 20070108 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FOUND RT GEAR WELL AILERON QUADRANT LOWER MOUNT HAS CRACK ON BULKHEAD, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR DOUBLER, SHIMS AND BUTT STRAP PER CRJ200 REO 601R-53-41-26 STEPS 7 AND 8. 2 L 7 2 4F RT A21EA 2007030900120 20070309 00120 EA 2007 3 9 SWIA200717847 1 20070108 A 5310 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 388 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 PAX DOOR FRAME FS388 HAS A CRACK ON INNER FLANGE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FRAME INSERT, SPLICES , SHIM AND NEW CLEAT PER REO 601R-52-11-402. 2 L 7 2 4F RT A21EA 2007030900129 20070309 00129 EA 2007 3 9 SWIA200717853 1 20070108 A 7120 BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE ATTACH CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FOUND LT UPPER OTBD BRACKET TOP WEB OF ENG BEAM TO FUSE SKIN. BRACKET CRACKED ON AFT RADIUS, DISCOVERED DURING C-CHECK INSPECTION. NEW ANGLE INSTALLED PER CRJ200 SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007030900134 20070309 00134 EA 2007 3 9 SWIA200717908 1 20070128 A 5210 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR ASSIST CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 PAX DOOR ASSIST MOTOR ATTACH ANGLE/LOWER CRACKED RADIUS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW ANGLE 601R -317745-7 IAW CRJ200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007030900162 20070309 00162 CE 2007 3 9 GLBA20060911 1 20070220 A 5330 SKIN BEECH 1900 1900D 1154162 CE BS 298 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 195GL UE195 UPON ROUTINE INSPECTION MAINTENANCE FOUND THE BELLY SKIN CRACKED AT APPROXIMATELY F.S. 298.0, B.L. 27.0. MAINTENANCE REP AIRED BELLY SKIN AT APPROXIMATELY F.S.298.0 B.L. 27.0 PER BEECH SRM 51-70. RII INSPECTION COMPLIED WITH PER TC 8.2.1. 2 L 7 2 4T RT A24CE 2007030900163 20070309 00163 EU 2007 3 9 07FDEA00601 1 20070227 A 7830 PILOT VALVE AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680 30025 NE UNKNOWN A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 672FE 779 705201 AFTER APPLYING TAKEOFF POWER ON RUNWAY, ECAM ALERT NR 2 ENG REVERSER PRESSURIZED. REJECTED TAKEOFF ABOUT 70 KTS. ACN R ELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 09MAR07. INSPECTED T/R ON NR 2 ENGINE NO DEFECTS FO UND. REMOVED AND REPLACED DIRECTIONAL PILOT VALVE ON WORK INSTRUCTION CARD E.O. 9-7830-7-5000A ,OPS CHECK GOOD IAW WOR K INSTRUCTION CARD E.O 9-7830-7-5000A AND A300 JRH REV CHECK.INOP STICKER REMOVED RII:098042. 2 L 7 2 4F 4 F RT A35EU E13NE 2007030900164 20070309 00164 EU 2007 3 9 07FDEA00604 1 20070227 A 7830 LOCK AIRBUS 310 A310 EU PWA JT9 JT9D7R4D 52054 NE NR 2 ENGINE UNKNOWN A FDEA O OTHER X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 SO 25 450FE 162 707738 DURING LANDING AT KBUR, THRUST REVERSER LEVERS EXTREMELY STIFF, F/O LOWERED REVERSER OR ATTEMPTED TO STOW AND LEVERS WER E SO STIFF COULD NOT STOW REVERSERS. ALL BETWEEN 80-60 KTS, AT ABOUT 65 KTS CAPT COMMANDED F/O TO MOVE HAND FROM THROT TLE AND POUNDED AND SLAMMED REVERSERS OUT PRIOR TO GETTING REVERSERS STOWED NR 2 ENGINE COMPRESSOR STALLED AND FLAMED O UT. EXCESSIVE FORCE TO DISCONNECT AUTO BRAKES. ACCOMPLISHED HPT AND COMBUSTION CHAMBER BORESCOPE. REMOVED & REPLACED SYNCHRONOUS SHAFT LOCK ASSY. RT SIDE PER AMM 78-31-41-4. OP'S CK OK. 2 L 7 2 4F 4 F RT A35EU E3NE 2007030900165 20070309 00165 CE 2007 3 9 GLBA20060919 1 20070226 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 126-131 MISREPAIRED A GLBA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 03 195GL UE195 UPON ROUTINE INSPECTIONS MAINTENANCE FOUND THAT A REPAIR MUST CONFORM WITH SRM TECHNICAL DATA SPECIFICATIONS AT FS 126 T O FS 131.3 STRINGER 3R TO APPROXIMATELY 3 INCHES IB OF STRINGER 2R ABOVE PILOTS WINDSHIELD. MAINTENANCE REPAIRED THE AF FECTED AREA AT FS 177.3 RT STRINGER 9AL RELIEF HOLE PER BEECH 1900D SRM 51-70 AND TC 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007030900166 20070309 00166 CE 2007 3 9 DXTA200701975 1 20070228 A 2120 UNKNOWN CESSNA 650 650 2076802 CE GARRTT TFE731 TFE7314R 01518 WP CABIN/COCKPIT SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 795QS 6507095 DISTINCT SMELL OF ELECTRICAL SMOKE IN CABIN AND COCKPIT AND A NOTICEABLE HAZE OF SMOKE VISIBLE. OPERATED GROUND TEST AP U TWICE FOR APPROX 20-25 MIN IAW 650 MM 49-10-00. NO NOTICEABLE SIGNS OF SMOKE IN CABIN. RAN CABIN TEMP TO FULL HOT AND COLD. BITE CHECKED BOX. NO FAULTS FOUND PER 650 MM 49-00-00. VISUALLY CHECKED BOTH ACM OIL LEVELS, COALESCERS, COCKPIT & CABIN TEMP SENSORS, COCKPIT CIRCUIT BREAKER PANELS & OPS CHECK ALL INTERLIGHTING IAW 650 IMM CHAPTERS 21-00-000, 12-00 -00, 24-00-00 & 33-00-00. NO DEFECTS NOTED. 2 L 7 2 4F 4 F A9NM E6WE 2007030900167 20070309 00167 CE 2007 3 9 DXTA200701976 1 20070228 A 2760 SPEED BRAKE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE RIGHT SLOW E DXTA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 07 131QS RK431 ON APPROACH HAD A UNCOMMANDED TURN TO THE RT WITH SPEED BRAKES EXTENDED. AIRCRAFT WAS AT APPROACH SPEED. CHECKED LEFT AND RIGHT SPOILER CABLE TENSIONS FOUND NORMAL AT 82 FOUND IAW HAWKER 400XP M.M. CH 27-60-00 CHART 201. FOUND LEFT SIDE S PEEDBRAKE EXTENDING SLIGHTLY SLOWER THAN RIGHT. CLEANED AND LUBRICATED FRICTION POINTS IN SPOILER MIXER. OPERATIONAL CHE CK GOOD ON GROUND. PERFORMED IAW 400XP MM CH 27-60-00 PG 203 2 H 7 2 4F 4 F RT A16SW E25EA 2007030900174 20070309 00174 SO 2007 3 9 C2XA07SH011 1 20070302 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12157 145787 SHV DURING C-CHECK CENTER OMEGA BEAM CORRODED AT FR 20. MAINTENANCE REMOVED AND REPLACED OMEGA BEAM LOCATED AT FR 20 IA W EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVE TO RETURN FOR SERVICE 2 L 7 2 4F RT 2007030900210 20070309 00210 SO 2007 3 9 C2XA07SH010 1 20070224 A 5320 12302681001 CROSSBEAM EMB 145 EMB145EP 3260221 SO NLG WW CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 SHV-DURING C-CHECK MAINTENANCE FOUND CROSS BEAM AT FRM 5 (NLG WHEEL WELL) CRACKED AT SUPPORT HOUSING. MAINTENANCE INSTA LLED REPAIR DOUBLER IAW EC 5320-01352. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007030900219 20070309 00219 SO 2007 3 9 C2XA07IA056 1 20070307 A 5210 14531380401 LOCK EMB 145 EMB145LR 3260212 SO PAX DOOR DEFECTIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13955 145075 IAH - THE CREW REPORTED THAT THE MAIN CABIN DOOR WOULD NOT CLOSE NORMALLY. MAINTENANCE REMOVED AND REPLACED THE FORWARD PAX DOOR LOCK BOX ASSEMBLY, RIGGED AND OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RE TURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007030900243 20070309 00243 SO 2007 3 9 C2XA07IA053 1 20070304 A 4920 4504113A APU EMB 145 EMB145EP 3260221 SO APU BAY MALFUNCTIONED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 12934 1900 1900 145019 IAH - FLIGHT 2984, THE CREW REPORTED SMOKE IN THE CABIN DURING FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITH OUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND PLACED THE APU ON MEL 49-00-00 CTL NUMBER 116866, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. FLIGHT 2272 OUT OF IAH THE CREW REPORTED A SMOKE SMELL AND LAV SMOKE INDICATION, TH E AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED TH E APU, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS NOTED. THE MEL WAS REMOVED, AND THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE 2 L 7 2 4F RT T00011AT 2007030900246 20070309 00246 SO 2007 3 9 C2XA07BT021 1 20070225 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO CABIN ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 11164 14500817 EWR LOG SQUAWK FLT NR 2059 AFTER TURNING ON PACK NR 2 DURING BOARDING THERE WAS A STRONG SMELL OF ELECTRICAL WIRE BURNIN G. RAN NR 1 AND NR 2 PACKS IAW EMB145 AMM 21-51-00. NO SMELL NOTED . CLOSED 2 L 7 2 4F RT 2007030900284 20070309 00284 NM 2007 3 9 USAA070143 1 20070227 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 BS 440 S-24R WL 160 HAS CRACK. REMOVED DAMAGE & INSTALLED FAB'D REPAIR PARTS PER EA 98455, DEFECT SIZE: .250 INCH. 2 L 7 2 4F RT A16WE 2007031200207 20070312 00207 EA 2007 3 12 TRAX200700292 1 20070226 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 CORROSION ON SHEAR CLIP LEG AT FS 605, STR 27 - 26 LT. 2 L 7 2 4F RT A21EA 2007031200208 20070312 00208 NM 2007 3 12 KNNA200700018 1 20070125 A 5311 65C3785243 FRAME BOEING 737 737297 1384480 NM PWA JT8 JT8D9 52048 NE BS 178 CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 147AW 22630 FOUND STA 178, LT SIDE FRAME IS CRACKED AT W/L 195. PROVIDE INSTRUCTION ON REPAIR CRACK BY INSTALLING A SPLICE OVER THE (LEFT SIDE) SIDE CHORD AT WL 212. 2 L 7 2 4F 4 F A16WE E2EA 2007031200212 20070312 00212 EA 2007 3 12 TRAX200700294 1 20070226 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 905EV 7632 AFT RIGHT EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007031200213 20070312 00213 EU 2007 3 12 TRAX200700295 1 20070227 A 3350 SIGN AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 634AS 370 FWD EMERGENCY SIGN OUT. 2 H 7 2 4T RT 2007031200214 20070312 00214 EA 2007 3 12 TRAX200700296 1 20070227 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNLOCKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 PAX DOOR LOCK NOT LOCKING. FLT 4273 DEL 35 MINS. 2 L 7 2 4F RT A21EA 2007031200215 20070312 00215 EA 2007 3 12 TRAX200700320 1 20070304 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 834AS 7254 ASD BOTTOM STEP IS CRACKED. 2 L 7 2 4F RT A21EA 2007031200217 20070312 00217 EA 2007 3 12 TRAX200700322 1 20070304 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 884AS 7513 LEFT AND RIGHT EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007031200222 20070312 00222 NM 2007 3 12 FDKA200702046 1 20070205 A 3350 82410162001 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A FDKA K NONE L NO TEST NR NOT REPORTED 1 SW 07 803LR 322 FDM 6175 JFK (0758 PHX LCL) CAPTAIN REPORTED THAT NO EMERGENCY LIGHT WOULD TURN ON. MX REMOVED AND REPLACED EMERGENCY C ONTROL BOX. 2 H 7 2 4T RT A13NM 2007031200226 20070312 00226 NM 2007 3 12 HNAA0700045 1 20070227 A 3350 OL3071BPEGPL LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 934HA 47479 70 134 EMERGENCY LIGHTING AIRSTAIR DOOR EMERGENCY EXIT SIGN CENTER LAMP IS INOP. RELAMPED LIGHT. 2 H 7 2 4T RT A13NM 2007031200227 20070312 00227 2007 3 12 MWEA070042 4 20070205 A 2565 3961899501 CABLE BOEING 717 717200 1383700 NM EVAC SLIDE DETACHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 902ME 55166 FORWARD ENTRANCE DOOR ESCAPE SLIDE CABLE DETACHED. RESECURED LOWER LATCH FOR FORWARD ENTRANCE DOOR SLIDE. 2 L 7 2 4F TR A6WE 2007031200229 20070312 00229 EA 2007 3 12 TRAX200700299 1 20070228 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 821AS 7194 PASSENGER DOOR EMERGENCY ILLUMINATION STRIPS REQUIRES REPLACEMENT (8EA) MARKED. [SUP 05-02-07] REMOVED AND REPLACED 1 PASSENGER DOOR EMERGENCY ILLUMINATION STRIP ON STEP 832CT AFT SIDE WITH NEW SERVICEABLE EMERGENCY ILLUMINATION STRIP IAW CRJ CMM 11-30-00, REMOVED AND REPLACED 7 PASSENGER DOOR EMERGENCY ILLUMINATION STRIPS ON STEPS 832BT, 832CT, AND CENTER TWO STEPS IAW CRJ AMM 11-30-00, 2 L 7 2 4F RT A21EA 2007031200230 20070312 00230 EA 2007 3 12 TRAX200700300 1 20070228 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 821AS 7194 PAX DOOR STEP 832AT -EXIT- PLACARD REQUIRES REPLACEMENT. 2 L 7 2 4F RT A21EA 2007031200232 20070312 00232 EA 2007 3 12 TRAX200700302 1 20070301 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 741EV 10155 AFT MOST CEILING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007031200233 20070312 00233 EA 2007 3 12 TRAX200700303 1 20070301 A 3010 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 875AS 7559 AFTER TAKEOFF, RECEIVED A WING OVERHEAT WARNING MSG, CYCLES CONTINUOUSLY. RETURNED TO ATL. REPEAT WRITE-UP. EMERGENCY DECLARED. FLT 4257 CX. 2 L 7 2 4F RT A21EA 2007031200234 20070312 00234 WP 2007 3 12 ABXA070054 1 20070226 A 3260 313 LIGHT DOUG DC9 DC933F 302207A WP COCKPIT INOPERATIVE A ABXA O OTHER O OTHER AP APPROACH 1 GL 23 933AX 47291 ON APPROACH, WHEN LANDING GEAR WAS EXTENDED, THE NOSE GEAR UNSAFE LIGHT DID NOT ILLUMINATE INITIALLY, THEN IT DID ILLUMI NATE. WHEN GEAR WAS EXTENDED, THE NOSE GEAR GREEN LIGHT WAS INOPERATIVE. RECYCLED GEAR WITH NO IMPROVEMENT. REPLACED NLG INDICATOR BULBS AND INDICATION WORKED NORMAL. COULD NOT DUPLICATE THE DISCREPANCY. FOUND PIN NR 2 TO NOSE GEAR DOW N AND LOCKED SWITCH SLIGHTLY RECESSED. RESEATED NR 2 PIN AND REPLACED THE DOWNLOCK SWITCH AS A PRECAUTION IAW DC9 MM 32 -60-01-2-0. 2 L 7 2 4F A6WE 2007031200244 20070312 00244 2007 3 12 NOCA04907 4 20070227 A 3441 HG1050A004 IRU BOEING 757 75728A 1384976 NM RIGHT MALFUNCTIONED A NOCA K NONE J WARNING INDICATION LD LANDING 1 EA 15 756NA 32448 AUTOBRAKES DISARMED ON LANDING. PERFORMED ANTI-SKID AUTOBRAKES BITE PER FIM 32-42-00 FOUND IRS R AT FAULT REMOVED AND R EPLACED R IRU PER MM 34-21-01, OPS CHECKED AUTOBRAKES PER FIM 32-42-00. OPS CHECKS OK. 2 L 7 2 4F RT A2NM 2007031200252 20070312 00252 NM 2007 3 12 NOCA05007 1 20070301 A 3297 WIRE BOEING 757 75728A 1384976 NM BRAKE SYS BROKEN A NOCA K NONE J WARNING INDICATION NR NOT REPORTED 1 EA 15 754NA 29381 AUTOBRAKES FAILED TO LATCH ON ANY SETTING DEFERRED PER 32-42-4, AUTOBRAKES INOP OPENED TO ORIGINAL DATE 2-20-07/ANTI-SKI D STATUS MSG ALT ANTI-SKID VALVE INOP MANUAL BRAKING VERIFIED RE-OPENED ITEM TO ORIGINAL DATE 2-20-07. TROUBLESHOT PER AWM 32-42-11 AND FIM 32-42-00 FOUND BROKEN WIRE AT TB209 REPINNED WIRE AT TB209 AND REPLACED TB209 PER SWPM ACCOMPLISHED ANTISKID/ AUTOBRAKE TEST PER MM 32-42-00, OPS CHECKS NORMAL. 2 L 7 2 4F RT A2NM 2007031200255 20070312 00255 SO 2007 3 12 N3B2007F00000 2 20070215 A 8500 TSIO520EB ENGINE CESSNA 402 402B 207590P CE CONT O520 TSIO520EB 17040 SO MCAULY 3AF32C 3AF32C* GL LEFT SHUTDOWN A N3BA O OTHER Y ENGINE STOPPAGE TX TAXI/GRND HDL 1 SW 01 593DM 432 402B1228 18222072ER DURING LANDING (AT DESCISION HEIGHT) LT ENGINE SHUTDOWN CAUSING AIRCRAFT TO LAND WITH A YAW TO THE LT, PUTTING EXCESSIVE LOAD ON RT LANDING GEAR. AFTER LANDING, LT ENGINE WAS RESTARTED AND AIRCRAFT CONTINUED ITS TAXI, WHEN AC TURNED OFF RU NWAY. RT LANDING GEAR TORQUE LINK ASSY CENTER SECTION FAILED AT DESIGNED CONNECTION POINT. THIS CAUSED DAMAGE TO OB LA NDING GEAR DOOR AND LOWER WING SKIN WERE GEAR DOOR ATTACHED. AC WAS NOT QUITE OFF RUNWAY WHEN THIS HAPPENED. AIRCRAFT HAD DESCENDED THRU HEAVY SNOW AND RAIN JUST PRIOR TO LANDING AND SUSPECT THAT THIS PLAYED A CONSIDERABLE FACTOR IN ENGIN E PERFORMANCE. (K) 1 L 7 2 3O 3 O A7CE E8CE 5 C P22EA 2007110500209 20071105 00209 NM 2007 11 5 CALA0700616 1 20071026 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM BS 827 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11612 27325 INSPECTION FOUND A .5 INCH CRACK AT FASTENER HOLE OF FRAME AT STA 827 BETWEEN STRINGERS 8L AND 9L. THE FRAME WAS REPAIR ED IAW ECRA 5310-04668. 2 L 7 2 4F RT A16WE 2007031200257 20070312 00257 SO 2007 3 12 FXG2007F00001 1 20070201 A 3230 19559 BUSHING MESSIER EMB 120 EMB120FC 3260204 SO PWA 118 PW118 NE LT MLG TIGHT G FXGA O OTHER O OTHER CL CLIMB 1 AL 01 1110J RT478LT479 120110 ON GEAR RETRACTION RED GEAR LIGHTS A AND B REMAINED ON AND LT MAIN GEAR DOOR WOULD NOT SHUT. MAINTENANCE INVESTIGATION REVELED THAT THE PN 19659 BUSHINGS IN BOTH THE LT AND RT UP-LOCK HOOK SUPPORT ASSY. PN 19552 WERE AT MINIMUM OVERHAUL T OLERANCES. IN COLD TEMPERATURES (-35F TO -40F) THESE CLEARANCES WERE TOO TIGHT. BUSHINGS WERE REAMED TO THE UPPER O/H CLEARANCE LIMITS. ASSY REASSEMBLED AND OPERATIONALY CHECKED. AC RETURNED TO SERVICE WITH NO ADDITIONAL PROBLEMS. (K) 2 L 7 2 4T 4 T RT A31SO E20NE 2007031200259 20070312 00259 SW 2007 3 12 EOP2007F00000 1 20070116 A 5302 206023129101P FITTING BELL BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ELEVATOR OUT OF ALIGNMENT E EOPA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 01 360AL 51462 NEW FITTING WAS ORDERED TO REPLACE WORN FITTING. WHEN NEW FITTING WAS INSTALLED AND ELEVATOR WAS BEING REINSTALLED IT W AS OUT OF ALIGNMENT AND BINDING. THE NEW FITTING WAS THEN COMPARED TO THE OLD FITTING, THE NEW FITTING WAS FOUND TO BE OUT OF ALIGNMENT BY .1250 INCH FROM THE OLD FITTING. (K) 1 G 7 1 3U 3 U H2SW E1GL 2007031200260 20070312 00260 SO 2007 3 12 C4S2007F00000 1 20070212 A 5730 467 SKIN GULSTM G1159 G1159A 3970109 SO RT WING CORRODED E C4SA K NONE O OTHER IN INSP/MAINT 1 SW 05 400WY 467 DURING A WING INSPECTION ACCOMPLISHED APRIL 9, 2006, CORROSION WAS NOTED IN THE UPPER RT WING PLANK AT FS 452 AND BL33. THE CORROSION DID NOT REQUIRE REPLACEMENT OF THE PART AND DID NOT REQUIRE BLENDING THAT EXCEEDED THE MFG ALLOWANCES. M FG ENGINEERING ALLOWED CONTINUED OPERATION WITH A RE-INSPECT DUE AT 12 MONTHS. OPTED TO ACCOMPLISH ASC 229 WHICH REMOVE THE CORROSION ON THE PLANK AND INSTALLS A DOUBLER PLATE AND NEW STYLE WING ATTACH PIN AND REMOVES AHT 12 MONTH RE-INSPE CTION REQUIREMENT. (K) 2 L 7 2 4F A12EA 2007031200261 20070312 00261 NM 2007 3 12 BJNA070101 1 20070124 A 2560 P4010021 BATTERY BOEING 737 7378Q8 13844BX NM FLASHLIGHT DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 GXLAJ 30703 AFT GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT BATTERY. (K) 2 L 7 2 4F RT A16WE 2007031200264 20070312 00264 NM 2007 3 12 AMTA200700143 1 20070213 A 5551 PIN BOEING 737 73783N 13844HI NM HOEIZ STAB CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 323TZ 30033 RT AFT CENTER STAB PIN CORRODED. REMOVED AND REPLACED PIN PN 180A1612-4 IAW EO 737-55AD-2935, REV B. (K) 2 L 7 2 4F RT A16WE 2007031200265 20070312 00265 EA 2007 3 12 SWIA200717958 1 20070207 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 426SW 7468 PAX DOOR AFT WEB AT 2ND STAIR CRACKED. (DISCOVERED DURING C-CHECK INSPECTION)INSTALLED REPAIR DOUBLER & SHIMS PER CRJ20 0 REO 601R-52-11-1188 REV A ON PAX DOOR AFT WEB STEP 2. 2 L 7 2 4F RT A21EA 2007031200266 20070312 00266 EA 2007 3 12 SWIA200717959 1 20070207 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 426SW FS280 LT/RT CLIPS CRACKED. (DISCOVERED DURING C-CHECK INSPECTION)INSTALLED NEW BRACKET ANGLES AT FS280 LT/RT PER CRJ200 SRM 51-42-06 PG 11 (9) 51-42-21 PG 17. 2 L 7 2 4F RT A21EA 2007031200267 20070312 00267 EA 2007 3 12 SWIA200717960 1 20070207 A 5320 SUPPORT FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 426SW BRACKET SUPPORT CLIP CRACKED RT RBL27 OTBD AND FS484 UNDER FLOORBD. (DISCOVERED DURING C-CHECK INSPECTION) INSTALLED NE W CLIP SUPPORT BRACKET AT RT RBL27 FS484 UNDER FLOORBOARD PER CRJ200 SRM51-42-06 PG 11 AND SRM 51-42-21 PG 17. 2 L 7 2 4F RT A21EA 2007031200269 20070312 00269 EA 2007 3 12 SWIA200717962 1 20070208 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 863AS PAX DOOR - THE OUTER HANDLE IS CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED PAX DOOR OUTER HANDLE AS PER CR J200 AMM 52-11-03-000-802 7 52-11-03-400-802. 2 L 7 2 4F RT A21EA 2007031200272 20070312 00272 EA 2007 3 12 SWIA200717965 1 20070208 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 863AS CRACK AT LOWER FLOORBEAM ST280 LT BL10. (DISCOVERED DURING C-CHECK INSPECTION) INSTALLED REPAIR ANGLE, CLIPS AND FILLER S AT STA 280, LBL10.0 IAW CRJ200 REO 601R-53-11-171, REV C, REPAIR SCHEME A. 2 L 7 2 4F RT A21EA 2007031200273 20070312 00273 EA 2007 3 12 SWIA200717966 1 20070208 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 863AS CRACK AT LOWER FLOORBEAM ST280 RBL10. (DISCOVERED DURING C-CHECK INSPECTION) INSTALLED REPAIR ANGLE, FILLER & NEW CLIP AT STA 280, RBL10.0 IAW CRJ200 REO 601R-53-11-171 REV C REPAIR SCHEME A. 2 L 7 2 4F RT A21EA 2007031200274 20070312 00274 EA 2007 3 12 SWIA200717972 1 20070213 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 705SK 10145 PAX DOOR AFT WEB 2ND & 3RD CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) INSTALLED REPAIR PARTS AS PER 670-52-11-104 REO REV B. 2 L 7 2 4F RT A21EA 2007031200275 20070312 00275 EA 2007 3 12 SWIA200717973 1 20070213 A 5210 STEP CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 705SK PAX DOOR FWD WEB 2ND STEP CRACKED. (DISCOVERED DURING C-CHECK INSPECTION)INSTALLED DOUBLER AND REPAIR ANGLES PER REO 67 0-52-11-104. 2 L 7 2 4F RT A21EA 2007031200276 20070312 00276 EA 2007 3 12 SWIA200717974 1 20070213 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 705SK PAX DOOR OUTER HANDLE CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) INSTALLED NEW HANDLE ASSY PER CRJ700/900 AMM 52-1 1-03-400-801-A01. 2 L 7 2 4F RT A21EA 2007031300004 20070313 00004 WP 2007 3 13 07FDEA00664 1 20070306 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 FOUND MAIN CARGO COMPARTMENT STA 535 RBL 28, SEAT TRACK GOUGED. REMOVED AND REPLACED SEAT TRACK SECTION IAW DC/MD10 SRM 53-70-00 PAGE 21 VOL I, 51- 31-0 VOL II PG 1,53-70-00 VOL I FIG 1 PG 4. 2 L 7 3 4F A22WE 2007031300005 20070313 00005 2007 3 13 07FDEA00665 2 20070225 A 7397 WIRE HARNESS AIRBUS 300 A300B4622 3930401 EU FUEL PUMP FAULTED A FDEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 716FD 358 RT INNER TANK NR 2 PUMP FAULTED DURING TAXI OUT. (SUPP DATE: 15 MARCH 2007) RAN COMPLETE NEW WIRE RUN FROM 50QA PINS A, B,&C TO 62VC PINS H,G & F PER WDM 28-21-10 PG 2. ALL LT INNER BOOST PUMPS ADJUSTMENT /TESTS ARE NORMAL. IAW MM 28-21- 12-5 A/C OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2007031300007 20070313 00007 NM 2007 3 13 07FDEA00667 1 20070306 A 5740 MOUNT DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LEFT WING LOWER WINGLET AFT MOUNTING FORWARD HOLE (WINGSIDE) FOUND CORRODED. SUPPLEMENTAL 21 MARCH 07; CORROSION ON LEF T HAND WING LOWER WINGLET AFT MOUNTING FORWARD HOLE (WINGSIDE) REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5730-107 803, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007031300008 20070313 00008 NM 2007 3 13 07FDEA00668 1 20070306 A 5740 MOUNT DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LEFT WING LOWER WINGLET AFT MOUNTING AFT HOLE (WINGSIDE) FOUND CORRODED. SUPPLEMENTAL 21 MARCH 07; CORROSION ON LEFT H AND WING LOWER WINGLET AFT MOUNTING AFT HOLE (WINGSIDE) REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5730-107803, R EPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007031300010 20070313 00010 NM 2007 3 13 07FDEA00670 1 20070306 A 5343 FITTING DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 NOSE LANDING GEAR LEFT HAND FITTING FOUND CRACKED. (SUPPLEMENTAL 28 MARCH 07) TRIMMED OUT AS PER FEDEX EA 1-5310-10781 2, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO SNRM N01285 FOR FITTING REPLACEMENT. 2 L 7 3 4F RT A22WE 2007031300011 20070313 00011 EU 2007 3 13 07FDEA00671 1 20070307 A 5310 CROSSBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 FOUND CORROSION ON CROSSBEAM C67 RT. REPAIR WAS PERFORMED IAW SRM 53-10-15, FIG 207. 2 L 7 2 4F RT A35EU 2007031300013 20070313 00013 EU 2007 3 13 07FDEA00673 1 20070307 A 5330 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 OLD GRINDING MARK BETWEEN C70-71, P48-49 LT. REPAIR WAS PERFORMED IAW TD/K4/S1/21674/2006 ISS A, APPROVED BY RAS/DAHAM/ 4021674/2006 ISS A. 2 L 7 2 4F RT A35EU 2007031300014 20070313 00014 EU 2007 3 13 07FDEA00674 1 20070307 A 5310 BEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 CORROSION AT ATTACHMENT HOLES ON SILL BEAM BETWEEN C25 AND 25A AT FWD CARGO DOOR. REPAIR WAS PERFORMED IAW TD/K7/S1/073 72/2006 ISS A AND EA 6-5313-106401 AND IS APPROVED BY RAS/DABRE/7007372/2006 ISS A. 2 L 7 2 4F RT A35EU 2007031300017 20070313 00017 EU 2007 3 13 07FDEA00397 1 20070209 A 5330 SKIN AIRBUS 310 A310203 3930313 EU BS 4937-4947 MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 409FE 273 PREVIOUS REPAIR FOUND LOCATED RT, FS 4937-4947, FR 96 AND STR 2. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATI ON AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER FEDEX ENG. AUTH. 36-5330-106690. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIF IED AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031300077 20070313 00077 NM 2007 3 13 SWAA071312 1 20070310 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031300078 20070313 00078 NM 2007 3 13 SWAA071311 1 20070310 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031300079 20070313 00079 NM 2007 3 13 SWAA071313 1 20070310 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 500C S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031300080 20070313 00080 NM 2007 3 13 SWAA071304 1 20070307 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, LBL 65, WL 201. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007031300081 20070313 00081 NM 2007 3 13 SWAA071306 1 20070308 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031300082 20070313 00082 NM 2007 3 13 SWAA071307 1 20070308 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031300083 20070313 00083 NM 2007 3 13 SWAA071308 1 20070308 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 996 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE RIGHT CREASE BEAM CORRODED AT BS 996. REMOVED AND REPLACED CREASE BEAM SECTI ON PER SRM. 2 L 7 2 4F RT A16WE 2007031300084 20070313 00084 NM 2007 3 13 SWAA071302 1 20070309 A 3350 65C27093 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 207WN 34012 L1 DOOR EMERGENCY EXIT DOOR LIGHT LENS LOOSE. REMOVED AND REPLACED LENS COVER PER MM. 2 L 7 2 4F RT A16WE 2007031300085 20070313 00085 WP 2007 3 13 IXXA07SMN042S 1 20070119 A 5720 VANE DOUG DC8 DC871F 302199D WP RT WING ELONGATED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 46065 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD SLOT VANE HOLES ELONGATED AT STATION XS520.168. REMOVED EX ISTING INTERNAL DOUBLER. REMOVED OUT DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAG E REMOVED. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFA CES. INSTALLED REPAIR PARTS IAW, DC8 SRM 51-3-0, DC8 SRM 51-3-1, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06 -10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SEMAN DRAWING NUMBER ED-4424 DATED 01-16-07. COMPLETED FAA FORM 8110-3 NU MBER 07019 DATED 01-18-07. 2 L 7 4 4F RT 4A25 2007031300086 20070313 00086 WP 2007 3 13 IXXA07SMN057S 1 20070131 A 5340 4705984501 FITTING DOUG DC8 DC871F 302199D WP ZONE 100 CRACKED B IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND A CRACKED FITTING AT STATION FS 240.000, LONGERON 33 RIGHT. REPLACED CRACKED F ITTING IAW DC8 SRM 51-1-20D AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007031300087 20070313 00087 NM 2007 3 13 CALA0700116 1 20070301 A 5340 65522643 FITTING BOEING 737 7373T0 1384582 NM BS 616 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 INSPECTION FOUND A .5 INCH CRACK IN UPPER RADIUS OF FITTING AFT OF FRAME JUST BELOW STRINGER 17L AND CREASE BEAM AT STA 616. A NEW FITTING WAS INSTALLED IAW SRM 51-10-2 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007031300088 20070313 00088 EA 2007 3 13 COMA0760218 1 20070301 A 3260 16600101 UPLOCK CNDAIR CL600 CL6002B19 1900309 EA NLG WW FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 927CA 31343 7031 FLIGHT 5157 - RECEIVED GEAR DISAGREE MESSAGE ON APPROACH. DECLARED EMERGENCY. PERFORMED QRH. NOSE GEAR EXTENDED. LAN DED WITHOUT INCIDENT. REPLACED NLG SELECTOR VALVE AND NLG UPLOCK ASSEMBLY. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007031300089 20070313 00089 EA 2007 3 13 COMA0760220 1 20070301 A 2750 7455001 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 01 721CA 9182 7259 FLIGHT 5686 - FLAP FAIL MESSAGE AFTER LANDING. REPLACED FLAP CONTROL HANDLE AS INDICATED BY FECU INTERROGATION. ALSO P ERFORMED EO 27-046AD. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007031300090 20070313 00090 NM 2007 3 13 CALA0700124 1 20070308 A 5310 147A85401 DOOR FRAME BOEING 737 737824 13844BZ NM STA 947-987 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14242 28805 INSPECTION FOUND CORROSION AROUND FASTENER HOLES ON L-2 CHORD AT STA 947-987, LBL 53 TO LBL 54. THE CHORD WAS REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007031300091 20070313 00091 WP 2007 3 13 IXXA07SMN072S 1 20070131 A 5340 3779762U501 FITTING DOUG DC8 DC871F 302199D WP ZONE 200 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND A CRACKED FITTING AT STATION FS680.000, LONGERON 2 LEFT. REMOVED CRACKED FITTI NG CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21 SRM 51-1-20D, DC8 SRM 51-3-1 PAGE 2A AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007031300092 20070313 00092 EA 2007 3 13 COMA0760229 1 20070306 A 5610 601R3303324 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA O OTHER O OTHER DE DESCENT 1 SO 01 592SW 2674 7279 FLIGHT 9438 - F/O'S SIDE WINDOW CRACKED PASSING THROUGH 26,000 FT. REPLACED WINDOW. 2 L 7 2 4F RT A21EA 2007031300093 20070313 00093 EA 2007 3 13 COMA0760225 1 20070305 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS OUT OF RIG A COMA O OTHER O OTHER LD LANDING 1 SO 01 999CA 7230 FLIGHT 4956 - FLAPS FAIL MESSAGE WHEN FLAPS WERE SELECTED TO 45 DEGREES. INSPECTED AND FOUND RIGHT BPSU OUT OF RIG. RI GGED RIGHT AND LEFT BPSU'S, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007031300094 20070313 00094 EA 2007 3 13 COMA0760226 1 20070305 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 933CA 7040 FLIGHT 5559 - FLAPS FAIL AT GATE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PA RAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007031300095 20070313 00095 WP 2007 3 13 IXXA07SMN074S 1 20070131 A 5522 SKIN DOUG DC8 DC871F 302199D WP ZONE 300 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR LOWER PANEL HAS A NON STANDARD REPAIR FROM STATION XE55.062 TO S TATION XE65.156. REMOVED SKIN PANEL WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN PANEL AND REPAIR PARTS. BO NDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN PANEL INNER SURFACE. APPLIED SEALANT TO FAYING SURFACE. INSTALLED NEW SKIN PANEL AND REPAIR PARTS. PERFORMED RIGHT ELEVATOR BALANCING. FOUND WITHIN TOLERANC E, MOMENT 1471.4 IN-LBS IAW DC8 SRM 51-4-4 PAGE 1-4, DC8 SRM 55-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 55-4-1 FIGURE 1 SHE ETS 1-2 ITEM "E” AND "F", DC8 SRM 51-1-9, DC8 SRM 51-1-8B, DC8 SRM 51-1-11 AND DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007031300096 20070313 00096 EA 2007 3 13 COMA0760230 1 20070306 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 987CA 28403 7199 FLIGHT 5512 - FLAP FAIL CAUTION MESSAGE RECEIVED. DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. PERFORMED EO 27-046AD INCLUDING FLAP REJUVE, LT, REPLACED PDU. 2 L 7 2 4F RT A21EA 2007031300097 20070313 00097 EA 2007 3 13 COMA0760232 1 20070306 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 784CA 7319 FLIGHT 5620 - RECEIVED FLAPS FAIL MESSAGE ON APPROACH, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH AD 20 06-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2007031300098 20070313 00098 EA 2007 3 13 COMA0760233 1 20070306 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 436CA 7482 FLIGHT 5045 - RECEIVED FLAPS FAIL CAUTION MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006- 12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WIT H NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2007031300099 20070313 00099 WP 2007 3 13 IXXA07SMN075S 1 20070131 A 5522 SKIN PANEL DOUG DC8 DC871F 302199D WP ZONE 300 DELAMINATED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR UPPER SKIN PANEL IS DELAMINATED AT STATION XE50.000. REMOVED DA MAGED SKIN PANEL. FABRICATED NEW SKIN PANEL AND REPAIR PARTS. BONDED REPAIR PARTS AS NEEDED WITH HYSOL. CLEANED, TREA TED AND PRIMED AREA AND NEW SKIN PANEL AND REPAIR PARTS AS NEEDED. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW S KIN PANEL AND REPAIR PARTS FROM STATION XAR0.00 TO STATION XE132.000. PERFORMED RIGHT ELEVATOR BALANCING FOUND WITHIN T OLERANCE, MOMENT 1471.4 IN-LBS IAW DC8 SRM 51-4-4 PAGE 1-4, DC8 SRM 55-4-1 FIGURE 1 SHEETS 1 AND 2, ITEMS "E" AND "F".DC 8 SRM 55-1-0 PAGE 1, DC8 SRM 51-1-9, DC8 SRM 51-1-8B, DC8 SRM 51-1-11 AND DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007031300103 20070313 00103 NM 2007 3 13 CALA0700122 1 20070306 A 5310 147A8540U8 DOOR FRAME BOEING 737 737824 13844BZ NM BS 947-995 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14242 28805 INSPECTION FOUND CORROSION AROUND FASTENER HOLES ON R-2 FRAME AT BS 947-995, RBL 43 TO RBL 63. THE CHORD WAS REMOVED AN D REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007031300104 20070313 00104 NM 2007 3 13 CALA0700123 1 20070307 A 5340 69489856 ATTACH FITTING BOEING 737 737524 1384721 NM BS 344-360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69603 27316 INSPECTION FOUND A 1 INCH CRACK I/B OF AFT END OF STRINGER 11L ATTACHMENT CLIP AFT OF L-1 DOOR CUTOUT, STA 344-360. THE CLIP WAS REPLACED IAW ECRA 5311-01301. A DIP WAS INITIATED TO REINSPECT THE AREA AT INTERVALS NOT TO EXCEED 6,000 FLIG HT CYCLES. 2 L 7 2 4F RT A16WE 2007031300105 20070313 00105 NE 2007 3 13 IXXA070012O 2 20070307 A 7300 CABLE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C1 13802 NE NR 4 VSV OUT OF ADJUST A IXXA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 11 605AL 42283 7986 46106 693556 DURING TAKEOFF ROLL AT ABOUT 90 KNOTS, THE CREW HEARD TWO LOUD POPPING NOISES. THE CREW ABORTED THE TAKEOFF. ENGINE AN TI-ICE WAS ON. MAX POWER WAS SET 87 PERCENT N1. THE CREW RETURNED TO PARKING. MAINTENANCE INSPECTED THE AIRCRAFT AND COMPLIED WITH CFM56 MM 71-00 CODE 41. AN ADJUSTMENT WAS MADE TO NUMBER 4 ENGINE VSV FEEDBACK CABLE. NO OTHER DEFECTS W ERE FOUND. MAINTENANCE PERFORMED AN ACCELERATION CHECK AND MAX POWER RUN ALL ENG PARAMETERS WERE NORMAL IAW ATI ERH 70. 01. TAXIED THE AIRCRAFT IAW ATI ERH 9.01.1. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2007031300106 20070313 00106 WP 2007 3 13 IXXA07SMN055S 1 20070131 A 5330 SKIN DOUG DC8 DC871F 302199D WP ZONE 100 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND A NON STANDARD REPAIR AT STATION FS12.000 LONGERON 27 RIGHT. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. AFTER DAMAGE REMOV ED. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. I NSTALLED REPAIR PARTS IAW UNITED AIRLINES DC8 MM 53-30-09 PAGES 201-209, DC8 SRM 51-1-21, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-20D AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007031300107 20070313 00107 EA 2007 3 13 COMA0770018 1 20070302 A 5100 NONE CNDAIR CL600 CL6002C10 1390015 EA NONE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 378CA 10097 FLIGHT 5526 - ELEVATOR SPLIT CAUTION MESSAGE ON CLIMBOUT. AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. INSPECTED A IRCRAFT, NO FAULTS IN MDC, NO HISTORY IN TRAX OR AIRCRAFT LOG BOOK. PERFORMED OPS CHECK WITH NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2007031300108 20070313 00108 EA 2007 3 13 COMA0760219 1 20070301 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 927CA 16264 7031 FLIGHT 5157 - RECEIVED GEAR DISAGREE MESSAGE ON APPROACH. DECLARED EMERGENCY. PERFORMED QRH. NOSE GEAR EXTENDED. LAN DED WITHOUT INCIDENT. REPLACED NLG SELECTOR VALVE AND NLG UPLOCK ASSEMBLY. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007031300109 20070313 00109 EA 2007 3 13 COMA0760223 1 20070303 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS UNKNOWN A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 987CA 7199 FLIGHT 5009 - UPON SELECTING FLAPS 8 DEGREES FLAPS FAILED AT ZERO DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MES SAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUT ION MESSAGES. 2 L 7 2 4F RT A21EA 2007031300110 20070313 00110 EA 2007 3 13 COMA0760224 1 20070304 A 3397 59465 JUMPER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS FAILED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 991CA 7216 FLIGHT 9420 - EMERGENCY LIGHTS NEAR PAX AND SERVICE DOORS INOPERATIVE. REMOVED AND REPLACED JUMPER CABLE. 2 L 7 2 4F RT A21EA 2007031300111 20070313 00111 EA 2007 3 13 COMA0760228 1 20070306 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS UNKNOWN A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 936CA 7043 FLIGHT 5063 - FLAPS FAIL CAUTION MESSAGE RECEIVED. ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. COMPLIED WITH AD 20 06-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2007031300112 20070313 00112 EA 2007 3 13 COMA0760231 1 20070306 A 2750 601R93106101 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS WORN A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 987CA 7199 FLIGHT 5512 - FLAP FAIL CAUTION MESSAGE RECEIVED. DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. REPLACED LEFT NR 1 FLE X DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2007031300113 20070313 00113 EA 2007 3 13 COMA0760234 1 20070306 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS UNKNOWN A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 471CA 7655 FLIGHT 5020 - RECEIVED A FLAP FAIL MESSAGE. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-2 1 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2007031300159 20070313 00159 NM 2007 3 13 2007UALA00589 1 20070225 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 644UA 25094 OVERWING EXIT EMERGENCY LIGHTS FLASHING WITH EMERGENCY LIGHTS ARMED. REPLACED EEL BATTERY PACK AT ROW 17A. EEL SYSTEM O P CHECKED OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007031300160 20070313 00160 NM 2007 3 13 2007UALA00590 1 20070226 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY CEILING LIGHT ABOVE ROW 18 INOPERATIVE. RELAMPED CEILING EEL .OP CHECKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007031300168 20070313 00168 EU 2007 3 13 MALA070039 1 20070305 A 3260 UPLOCK SAAB SF340 340B 7860101 EU MLG OUT OF ADJUST A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 448XJ 340B448 DURING DEPARTURE FROM MSP, THE CREW EXPERIENCED AN ABNORMAL GEAR RETRACTION INDICATION DURING DEPARTURE. THE CREW FOLLO WED THE QRH AND RETURNED TO MSP LANDING WITHOUT FURTHER INCIDENT. ON TAKEOFF BROUGHT GEAR HANDLE UP ALL 3 GEAR LIGHTS E XTINGUISHED, BUT DISAGREEMENT LIGHT HANDLE REMAINED ON AS WELL AS HYD PUMP CONTINUED TO RUN. PERFORMED QRH GEAR CAME UP WHEN RECYCLED AND DISAGREEMENT LIGHT EXTINGUISHED. ADJUSTED LEFT AND RIGHT MAIN LANDING GEAR UPLOCKS IAW 32-32-00-05. ADJUSTED LEFT AND RIGHT UPLOCK SWITCHES IAW 32-61-15-02. ADJUSTED RIGHT O/B MAIN LANDING GEAR DOOR IAW 32-12-15-02. P ERFORMED GEAR SWINGS IAW 32-30-00-05. FUNCTIONAL TEST GOOD. NO DEFECTS FROM 409-301796. 2 L 7 2 4T RT A52EU 2007031300169 20070313 00169 EU 2007 3 13 MALA070036 1 20070220 A 3260 CONTROL UNIT SAAB SF340 340B 7860101 EU MLG MALFUNCTIONED A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 449XJ 340B449 WHEN THE LANDING GEAR IS SELECTED UP, THE INTRANSIT LIGHT DOES NOT ILLUMINATE. TESTED TRANSIT LIGHT WHILE GEAR WAS UP A ND LIGHT BULB WORKS. REPLACED LANDING GEAR CONTROL UNIT WITH SERVICEABLE UNIT, P/N OFF AND ON: D494-12-001, S/N OFF: 614 /091-96, S/N ON: 645/09-97. OPS CKS GOOD, DONE PER SAAB AMM 32-31-05-02 AND 32-30-00-05. 2 L 7 2 4T RT A52EU 2007031300170 20070313 00170 EU 2007 3 13 MALA070035 1 20070207 A 3297 WIRE HARNESS SAAB SF340 340B 7860101 EU MLG UNKNOWN A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 437XJ 340B437 UPON GEAR EXTENSION IN EAU, LT MAIN GEAR DOWNLOCK INDICATOR DID NOT SHOW GREEN, INTRANSIT LIGHT EXTINGUISHED NORMALLY, 2 0 SECONDS LATER, LEFT GEAR GREEN LIGHT ILLUMINATED BY ITSELF. INSPECTED MAIN GEAR ACTUATOR AND DOWNLOCK, FOUND OK. PIN NED GEAR TO INSURE DOWN AND LOCKED. REMOVED GEAR PINS. INSP A/C FOUND TO BE SAFE FOR ONE-TIME FERRY FLIGHT FROM EAU TO MSP WITH GEAR DOWN, NOT PINNED. MAX SPEED 200 KNOTS, AND FLOWN NO ICE CONDITION. REMOVED AND REPLACED LT MLG PER 32-6 1-05-02. GEAR SWING CHECKS GOOD. 2 L 7 2 4T RT A52EU 2007031300171 20070313 00171 2007 3 13 2007UALA00630 4 20070301 A 2565 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 1L READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 576UA 26690 SLIDE AT DOOR 1L BOTTLE PRESSURE LOW. [SUP 05-08-07] WATER VALVE TESTED FOR LEAKS. FOUND THE SEAL WAS BROKEN INSIDE T HE GAUGE AND BECAME NON-SERVICEABLE. REMOVED AND REPLACED GAUGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007031300172 20070313 00172 NM 2007 3 13 2007UALA00631 1 20070302 A 5280 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT NLG DOOR DAMAGED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 781UA 26945 LIGHTNING STRIKE DAMAGE TO RIGHT NLG DOOR. REPAIRED LIGHTNING STRIKES REF SRM 52-80-01. REPAIR TAP CKS GOOD. A/C OK FO R SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007031300174 20070313 00174 EU 2007 3 13 MALA070033 1 20070303 A 3397 CONNECTOR SAAB SF340 340B 7860101 EU EMERGENCY LIGHT BROKEN A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 437XJ 340B437 FOUND EMERGENCY FLOOR TRACK LIGHTING DISCOVERED INSECURE AT THE 1A/2A AREA. UPON INSPECTION, FOUND CONNECTORS BROKEN. REPLACED EMERGENCY FLOOR TRACK LIGHTING STRIP AT ROW 2A-3A WITH SERVICEABLE UNIT, P/N 6636-2 IAW SF340MM 33-50-20. 2 L 7 2 4T RT A52EU 2007031300175 20070313 00175 EU 2007 3 13 MALA070034 1 20070307 A 7500 BLEED AIR SYS SAAB SF340 340B 7860101 EU ENGINE UNKNOWN A MALA O OTHER J WARNING INDICATION DE DESCENT 1 GL 15 407XJ 340B407 ON DESCENT INTO DSM, RIGHT BLEED LEAK LIGHT ILLUMINATED, COMPLETED QRH, LIGHT EXTINGUISHED. VISUALLY INSPECTED RT BLEED AIR DUCTS AND OVERHEAT DETECT LOOP. NO DEFECTS NOTED. PERFORMED OPERATIONAL TEST OF THE BLEED AIR DUCT LEAK DETECTION SYSTEM IAW AMM CHAP 36-23-00-05. OPS CHECK GOOD. CHECKED FOR BLEED LEAKS USING SHOP AIR AND BLEED AIR FROM LT ENGINE, NO LEAKS NOTED. RAN RT ENGINE FOR APPROX 30 MINUTES WITH LP AND HP ON, NO FAULTS NOTED. 2 L 7 2 4T RT A52EU 2007031300200 20070313 00200 NM 2007 3 13 AALA20070363 1 20070217 A 3350 P4010049 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 322AA 22323 LAX - SEAT MOUNTED EMERGENCY LIGHTS AT LEFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT LEFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007031400001 20070314 00001 CE 2007 3 14 AMW083149 1 20070308 A 2700 50534387231 SPRING BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE UNKNOWN BROKEN A AMWA O OTHER F FLT CONT AFFECTED LD LANDING 1 CE 07 162ZV 17348 UE162 AFTER LANDING, THE CAPT REPORTED THAT THE AIRCRAFT PULLED TO THE RIGHT. AIRCRAFT WAS TAKEN OUT OF SERVICE AND REPAIRED. REMOVED AND REPLACED INTERCONNECT SPRING. 2 L 7 2 4T 4 T RT A24CE E26NE 2007031400011 20070314 00011 NM 2007 3 14 UPS07449283 1 20070214 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1601 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C AFT CARGO RIGHT STA 1601 S37R STRINGER FOUND CRACKED. CRACK LENGTH .25 INCH. AFT CARGO COMPT BS 1590 TO BS 1630 S37R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007031400016 20070314 00016 NM 2007 3 14 UPS07449294 1 20070216 A 5320 SUPPORT BOEING 747 747121 1384871 NM BS 1940-2045 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C BULK CARGO COMPT SLOPE PANEL SUPPORT SEVERAL LOCATION FOUND SURFACE CORROSION AT STA 1940 TO STA 2045 LBL 60 ANCHOR NUT AREA. CORROSION BLEND OUT 0.025" X .5" X 2" EXCEED SRM 53-10-01 FIG 1 LIMITS. SLOPE PNL SUPPORT BS 1 940-2010 COR REMOVED & REPROTECTED AS PER SRM 51-10-01 & 51-10-02 ORG 0.050" BLEND OUT 0.005" X .5" X 1" WITHIN SRM 53-1 0-01 FIG 1 LIMITS. BS 2010-2070 COR SUPPORT REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02. 2 L 7 4 4F A20WE 2007031400022 20070314 00022 NM 2007 3 14 AALA20070375 1 20070220 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 691AA 25697 LAX - SEAT MOUNTED EMERGENCY LIGHTS AT AFT CABIN FAILED TEST. SECURED WALL SEAT CONNECTOR FOR SEAT MOUNTED EMERGENCY LI GHTS AT SEAT 27DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007031400033 20070314 00033 CE 2007 3 14 AMW082600 1 20070211 A 2750 1185210551 SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE TE FLAPS DIRTY A AMWA O OTHER F FLT CONT AFFECTED CL CLIMB 1 CE 07 167YV 20113 UE167 AFTER T/O, FLAPS STUCK AT 17 DEGREES. CREW CALLED IT IN AND TOWER DECLARED EMERGENCY. EMERGENCY WAS THEN IMMEDIATELY T ERMINATED A/C FLEW ITS ROUTE, ARRIVED ON TIME, NO FURTHER INCIDENT. (DIRECTED BY FAA TO ENTER AS AN SDR, INITIALLY ENTE RED AS AN MIS) CLEANED LT/RT FLAP SAFETY SWITCHES ADJUSTED RT SAFETY SWITCHES, OPS CK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007031400034 20070314 00034 CE 2007 3 14 DXTA200702015 1 20070312 A 3260 UNKNOWN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG UNKNOWN E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 311QS 5600311 AFTER TAKEOFF THE GEAR UNLOCKED LIGHT REMAINED ILLUMINATED. THE LANDING GEAR HANDLE WAS CYCLED TWICE WITH NORMAL INDICA TIONS. INSPECTED GEAR & C/W GEAR SWINGS, ALL OPERATIONS & INDICATIONS WERE NORMAL NO DEFECTS NOTED AT THIS TIME. ALL W ORK ACCOMPLISHED IAW CE560 MM CHAPTER 32-30-00 & 32-30-00 FOR TROUBLESHOOTING. 2 L 7 2 4F 4 F RT A22CE E25EA 2007031400037 20070314 00037 EA 2007 3 14 FFKA114 2 20070226 A 7414 10682016 GEAR CONTIN D3000 PIPER PA32 PA32R300 7103213 SO LYC O540 IO540K1G5 41532 EA MAGNETO DAMAGED B FFKA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 05 5454F 754 754 G05LA102R 32R7780012 L2399248A PILOT REPORTED THAT THE ENGINE IS RUNNING ROUGH DURING TAXI AND HAD A BAD MAGNETO DROP. MAINTENANCE INVESTIGATED AND FO UND THE GEAR TEETH P/N 10-682016 BROKEN OFF OF BOTH THE LEFT AND RIGHT GEAR ASSEMBLIES. AFTER FURTHER INVESTIGATION OF THE MAGNETO, IT WAS ALSO FOUND THAT ONE OF THE RETAINER SNAP RINGS P/N 10-92815-37 TO BE DISCOLORED AND SPREAD APART. 1 L 7 1 3O 3 O A3SO 1E4 2007031400043 20070314 00043 NM 2007 3 14 AALA20070354 1 20070217 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 MIA - FOUND EMERGENCY LIGHT ABOVE SEAT 3D INOPERATIVE. RELAMPED EMERGENCY LIGHT ABOVE SEAT 3D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007031400048 20070314 00048 NM 2007 3 14 07FDEA00683 1 20070307 A 5340 9078139 FITTING BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 MAIN CABIN FS 340 STR 8L DOOR STOP FITTING FOR FWD ENTRY HAS A MISDRILLED HOLE. REMOVED OLD FITTING, DRILLED AND INSTALL ED NEW STOP FITTING REF SRM 51-30-02 PG 4, MM 52-11-011-8 PG 1, POLY PAINTED FITTING REF MM 51-20-103-7, PG 1. 2 L 7 3 4F A3WE 2007031400049 20070314 00049 NM 2007 3 14 07FDEA00684 1 20070307 A 5321 FLOOR SKIN BOEING 727 727225 1384077 NM BS 435 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 E/E COMPT RT O/B FLOOR PNL WEB HAS CORROSION FS - 435, REMOVED AND REPLACED DAMAGED WEB AT STA 435 IAW SRM 51-30-2. NEW WEB MADE ON TRAVELER T7/665341. 2 L 7 3 4F A3WE 2007031400050 20070314 00050 NM 2007 3 14 DXTA200702010 1 20070309 A 3210 UNKNOWN AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE MLG UNKNOWN E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 281QS 81 AFTER TAKEOFF, UPON GEAR RETRACTION, LT MAIN GEAR DOOR LIGHT REMAINED RED. NO NOISE OR VIBRATION TO INDICATE DOOR WAS NO T CLOSED. ALL OTHER GEAR LIGHTS NORMAL. RETURNED TO AIRPORT, LANDED AND RED LIGHT STAYED ON. REMOVED & REPLACED DEFECTI VE LMLG DOOR LATCH W/ REPAIRED UNIT. JACKED AIRCRAFT CYCLED GEAR W/ NO DEFECTS NOTED. ALL WORK IAW F2000 M/M 32-130. 2 K 7 2 4F 4 F RT A50NM E44NE 2007031400051 20070314 00051 NM 2007 3 14 07FDEA00685 1 20070307 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM 740-840 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 FOUND MAIN DECK SEAT TRACK STA 740-850 RBL-45 HAS AREA OF BARE METAL AND CORROSION. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2007031400053 20070314 00053 NM 2007 3 14 07FDEA00687 1 20070307 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 620-720F CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 CABIN SEAT TRACK HAS CORROSION SPOTS FS 620-720F LBL 45, REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2007031400058 20070314 00058 WP 2007 3 14 07FDEA00693 1 20070307 A 3243 BRAKE ASSY DOUG MD10 MD1010F 3022112 WP MLG LOCKED A FDEA O OTHER F FLT CONT AFFECTED LD LANDING 1 SO 25 358FE 46633 NR 2 AND NR 3 MAIN BRAKES LOCKED UP AT HIGH SPEED LANDING. REMOVED AND REPLACED NR 2 AND NR 3 MAIN BRAKES PER MD10-10 A MM 32-43-01-4. VISUALLY INSPECTED ALL TIRES AND BRAKES, NO DEFECT FOUND. 2 L 7 3 4F RT A22WE 2007031400061 20070314 00061 NM 2007 3 14 UPS07449274 1 20070214 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1652 S32R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C AFT CARGO RIGHT STA 1652 STR 35R STRINGER FOUND CORROSION CRACKED. CRACK LENGTH .75 INCH. AFT CARGO COMPT BS 1650 TO BS 1670 STR 35R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007031400062 20070314 00062 NM 2007 3 14 UPS07449275 1 20070212 A 5340 65B0794132 ATTACH FITTING BOEING 747 747121 1384871 NM BS 260 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 260 LBL 11 NLG TOP BOX ATT CLIP FOUND CRACKED. CRACK LENGTH .25 INCH. M/D BS 260 LBL 11 NLG T OP BOX ATT CLIP REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007031400063 20070314 00063 NM 2007 3 14 UPS07449276 1 20070212 A 5320 FLOOR SUPPORT BOEING 747 747121 1384871 NM BS 340 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 340 RIGHT O/B FLOOR SUPPORT FOUND CRACKED. CRACK LENGTH .5 INCH. M/D BS 340 RIGHT O/B FLOOR S UPPORT REPAIRED AS PER SRM 51-40-04 FIG 2. 2 L 7 4 4F A20WE 2007031400068 20070314 00068 CE 2007 3 14 DJFA2007026 1 20070306 A 7160 INLET BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE RT ENGINE CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 686TA RK328 PCEJA0430 DURING A SCHEDULED MAINTENANCE EVENT MAINTENANCE FOUND A CRACK ON THE RT ENGINE INLET RING AT THE 12 O'CLOCK POSITION. THE CRACK IS ABOUT .25 INCH LONG. MAINTENANCE REPLACED THE INLET. 2 H 7 2 4F 4 F RT A16SW E25EA 2007031400069 20070314 00069 NM 2007 3 14 DXTA200702007 1 20070308 A 3240 7G1042 PRESSURE SWITCH AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE BRAKES OUT OF TOLERANCE E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 277QS 4946 177 BRAKE PRESS ANNUNCIATOR TRIGGERED T/O CONFIG DURING TAKEOFF BEFORE 50 KTS. TROUBLESHOT BRAKE SYSTEM TO NR 2 SYSTEM BRAK E PRESSUE SWITCH. REMOVED AND REPLACED NR 2 SYSTEM BRAKE PRESSURE SWITCH WITH A (NEW) UNIT IAW MM 32-42-00. 2 K 7 2 4F 4 F RT A50NM E44NE 2007031400070 20070314 00070 CE 2007 3 14 DXTA200702008 1 20070308 A 2611 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL SMOKE DETECTION UNKNOWN E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 902QS 7500002 DURING CRUISE FLT AT FL430 THE BAGGAGE SMOKE MESSAGE AND MASTER WARNING CAME ON FOR APPROX 3 SECONDS AND WENT OUT. AFTE R A SHORT TIME IT CAME ON AGAIN FOR APPROX 3 SECONDS AND WENT OUT. FOUND BAGGAGE VENT BLOCKED BY CARPET RESECURED CARPET TO CLEAR BAGGAGE VENT IAW CE750 M/M CH 26-90-14 OPS CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007031400072 20070314 00072 CE 2007 3 14 AMW061222025A 1 20070212 A 5310 1294200343 DOOR FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FUSLAGE CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 10675 19467 UE229 AIRSTAIR DOOR FRAME ANGLE CRACKED. REPAIRED IAW REPORT 6512-1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007031400078 20070314 00078 NM 2007 3 14 UPS07549281 1 20070302 A 3020 VALVE BOEING 757 75724APF 1384969 NM ANTI ICE SYS INOPERATIVE A IPXA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 01 458UP 25479 INSPECTION TYPE:N/A DIVERSION - RIGHT ENG ANTI-ICE VALVE WILL NOT OPEN GOING INTO ICING CONDITIONS. REMOVED AND REPLACE D RIGHT ENG ANTI-ICE VALVE IAW 30-21-03-4. ALL OPS CHECK NORMAL THIS CLEARS M345383. 2 L 7 2 4F RT A2NM 2007031400079 20070314 00079 NM 2007 3 14 07FDEA00733 1 20070309 A 3220 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 NOSE LANDING GEAR, RT TRUNNION FITTING FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5310-105635. STOP DRILL DEVIATION FROM SRM AND SRM 53-40-00 FIG. 22 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007031400080 20070314 00080 EA 2007 3 14 SWIA200717971 1 20070208 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 863AS 7487 LT MLG WHEEL WELL HAS BRAKE TRANSDUCER BRACKET CRACKED BROKEN ON TOP MID AREA OF WHEEL WELL, DISCOVERED DURING C-CHECK I NSPECTION. INSTALLED NEW PART PER CRJ200 SRM 51-40-06 PG 1-3; 15-17. 2 L 7 2 4F RT A21EA 2007031400082 20070314 00082 EA 2007 3 14 SWIA200717977 1 20070213 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 705SK 10145 FS 280 FLOOR SUPPORT ANGLES CRACKED LBL9, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED 2 'T' BRACKETS PER MODSUM 156 7053110026. 2 L 7 2 4F RT A21EA 2007031400083 20070314 00083 EA 2007 3 14 SWIA200717978 1 20070213 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 705SK 10145 280 FLOOR SUPPORT BEAM CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED LT INBD AND OTBD INTERCOSTALS, RT OTBD INTERCOSTAL AND FASTENERS IN RT FLOORBEAM REO 670-53-11-047 REV 'D' P/N 670-53-11-047-5 AND MODSUM DWG I567053110026 REV 'B1'. 2 L 7 2 4F RT A21EA 2007031400084 20070314 00084 EU 2007 3 14 07FDEA00741 1 20070312 A 5754 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 SOME PARTS IN KRUEGER FLAP AREA AT FWD FAIRING HEAVY CORRODED, PARTS REPLACED IAW SRM 57-45-11, KEEL BEAM PN A535-10215- 201, BRACKET A535-10219-201 AND FITTING A535-10561-201. 2 L 7 2 4F RT A35EU 2007031400086 20070314 00086 NM 2007 3 14 07FDEA00735 1 20070309 A 3234 HANDLE DOUG MD11 MD11F 3023600 NM MLG STUCK A FDEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 521FE 48478 AFTER T/O COULD NOT RAISE GEAR HANDLE. REPEATED ATTEMPTS. HANDLE FINALLY RAISED WITH RIGHT MAIN GEAR UNSAFE. RED LIGH T IN BOTH PRIMARY AND SECONDARY. LOWERED GEAR & LANDED FUEL DUMP APPROX 110,000 LBS FOUND RT MLG DOOR MOUNTED SENSOR TARGET DAMAGED. REPLACED TARGET ASSEMBLY. GEAR SWING ACCOMPLISHED WITH NO DEFECTS FOUND. REMOVED AND REPLACED RT MLG TRUCK TRIM ACTUATOR AND RT MLG ACTUATOR RESTRICTORS PRECAUTION. FOUND GEAR HANDLE RELEASE BUTTON BROKEN. REPLACED. FOU ND RT MLG DOOR LWR FWD RAMP HANDLE ASSY DAMAGED/BENT. REPLACED. LUBRICATED LT AND RT MLG TRUCK BEAM PIVOT POINTS. GE AR SWING AND ALTERNATE RELEASE SYSTEM CHECKS GOOD. 2 L 7 3 4F RT A22WE 2007031200017 20070312 00017 CE 2007 3 12 DXTA200702000 1 20070305 A 3213 STRUT CESSNA 650 650 2076802 CE GARRTT TFE731 TFE7314R 01518 WP NLG UNDERSERVICED E DXTA A UNSCHED LANDING W S INADEQUATE Q C AFFECT SYSTEMS CL CLIMB 1 GL 07 715QS 6507105 LANDING GEAR WOULD NOT RETRACT (HANDLE WOULD NOT COME UP) AFTER TAKEOFF. TROUBLESHOT NOSE LANDING GEAR - FOUND NOSE STRU T NOT FULLY SERVICED - SERVICED STRUT WITH FLUID AND NITROGEN IAW CESSNA M/M 12-10-38 FUNCTIONALLY TESTED GEAR - NO DEFE CTS NOTED AT THIS TIME 03-05-07 2 L 7 2 4F 4 F A9NM E6WE 2007031200019 20070312 00019 CE 2007 3 12 GLBA20060918 1 20070226 A 5313 STRINGER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 177 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 195GL UE195 UPON ROUTINE INSPECTIONS, MAINTENANCE FOUND A STRINGER RELIEF HOLE CRACKED AT FS 177.3 RT STRINGER 9AL. MAINTENANCE RE PAIRED THE AFFECTED AREA AT FS 177.3 RT STRINGER 9AL RELIEF HOLE IAW SRM 51-70 AND TC 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007031200026 20070312 00026 2007 3 12 RAIA00703002 4 20070301 A 3441 7510100631 INU EMB 145 EMB145LR 3260212 SO NR 1 MALFUNCTIONED A RAIA O OTHER O OTHER LD LANDING 1 CE 03 844HK 6287 14500838 FLT NR 8095 - IAD - LOST NAV 1 /NAV 2 ON ILS APPROACH TO IAD. MAINTENANCE REMOVED AND REPLACED NR 1 INU, OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT T00011AT 2007031200046 20070312 00046 SO 2007 3 12 C2XA07BT013 1 20070131 A 3240 BRAKE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL PARKING MALFUNCTIONED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11536 145520 IND LOG SQUAWK FLT NR 2951 WITH PARKING BRAKE SET AIRCRAFT ROLLS. CYCLED NORMAL BRAKES SEVERAL TIMES AND PERFORMED OPS CHECK OF PARKING BRAKE SYSTEM IAW AMM 32-44-07. OPS CHECK GOOD. CLOSED 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007031200076 20070312 00076 NM 2007 3 12 SWAA071277 1 20070308 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 12R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007031200081 20070312 00081 CE 2007 3 12 213200744AS 1 20070213 A 5730 SKIN CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE LT WING DAMAGED E VQMA K NONE O OTHER IN INSP/MAINT 1 NM 03 44AS 5500047 PULLED FASTENERS AND CRACK IN LT WING LOWER SKIN. 1 L 7 2 4F 4 F A22CE E1NE 2007031200085 20070312 00085 NM 2007 3 12 DHL2007751510 1 20070227 A 5753 SKIN BOEING 727 727264 138408M NM TE FLAPS DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 751DH 22982 IN "C", RT WING OB FORE FLAP UPPER SURFACE HAS 3" GOUGE, HITTING SCREWS ON SPOILERS, WS 575. CUT OUT GOUGED/DELAMINATED AREA ON RT OB FORE FLAP UPPER SURFACE APPROX 2" BY 4". FAB FILLER APPROX 2" BY 4" AND DOUBLER APPROX 6"BY 6 3/4" FROM 2024T3 .016 PO NR 9004174. CLEANED, PREPPED, BONDED, CLEANED, TREATED, PRIMED, AND SEALED EDGES IAW B727 SRM 57-50-2 FI G 4 AND 51-40-24 FIG 1. 2 L 7 3 4F A3WE 2007031200087 20070312 00087 NM 2007 3 12 AWXA200700335 1 20070305 A 2560 BATTERY BOEING 737 7373G7 1384595 NM FLASHLIGHT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 302AW 24009 PHX - AFT GALLEY EMERGENCY FLASHLIGHT HAS A DEAD BATTERY. MX REPLACED THE FLASHLIGHT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2007031200091 20070312 00091 NM 2007 3 12 F3LA200700042 1 20070306 A 5313 D5347218820200 LONGERON AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 919FR 4679 1980 DURING C-3 CHECK, INSPECTION REPORTED CORROSION FOUND UNDER NUT CLIPS LT BEAM Y1292 BETWEEN CROSSBEAMS FR67 AND FR68 PRO FILE 195. REPLACED BEAM IAW SRM 51-42-11 AND SRM 53-41-14. 2 L 7 2 4F RT A28NM 2007031200100 20070312 00100 NM 2007 3 12 AWXA200700328 1 20070214 A 5753 6546486150 WEDGE BOEING 737 7373S3 1384711 NM ZONE 600 DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND RIGHT WING INBOARD MID FLAP TRAILING EDGE WEDGE UPPER SURFACE DEBONDED, WS 109 - WS 111. REPAIRED RIGHT WIN G INBOARD MID FLAP TRAILING EDGE WEDGE UPPER SURFACE, WS 109 - WS 111 IAW B737-300 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 2007031200110 20070312 00110 EA 2007 3 12 TRAX200700309 1 20070302 A 5320 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 921EV 7819 LEFT SIDE 640 DOUBLER SUSPECT CRACKED. FLT 4538 CX. 2 L 7 2 4F RT A21EA 2007031200114 20070312 00114 NM 2007 3 12 HALA0700089 1 20070307 A 2121 UNKNOWN BOEING 767 767300 1385204 NM RECIRC FAN UNKNOWN A HALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM, UPON ARRIVAL AND PWR SWAP RT RECIRC FAN FAILED WITH EICAS MSG. RESET RT RECIRC FAN, OPS NORMA L MSG CLEARED AMM 21-58-00. 2 L 7 2 4F RT A1NM 2007031200120 20070312 00120 NM 2007 3 12 HALA0700095 1 20070308 A 5100 NONE BOEING 767 767300 1385204 NM NONE NONE A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, EICAS STATUS MSG R ENG OH LP 2 DISPLAYED. DOWN POWER AIRCRAFT, RERACKED R ENG OH LP 2 CARD ON P54, RESTORED POWER, EICAS STATUS MESSAGE CLEARED. 2 L 7 2 4F RT A1NM 2007031200122 20070312 00122 NM 2007 3 12 DL76L070190 1 20070306 A 4900 331200ER APU BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE APU BAY CONTAMINATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 185DN 6602 27961 P2803 ATB - CREW REPORTED SMOKE IN CABIN ALONG WITH SMOKE DETECTOR SOUNDING IN MID LT LAV. RAN BOTH ENGS AT POWER. COULD NO T DUPLICATE WITH ENG BLD WITH APU BLEED ODOR SENSED IN CABIN. REPLACED APU PER JIC 7952. RAN APU NO LEAKS NOTED AIR AN D GEN OPS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007031200125 20070312 00125 NM 2007 3 12 DL738070194 1 20070308 A 5753 113A270015 SKIN BOEING 737 737832 13844CF NM LT WING FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 380DA 30266 P2119 A BLOWN TIRE CAUSED LARGE DAMAGE TO THE LOWER SKIN AND CORE OF THE INBD AFT FLAP. REPAIRED PER DELTA ERA 460616-14. 2 L 7 2 4F RT A16WE 2007031200127 20070312 00127 NM 2007 3 12 EIA2007017 1 20070215 A 5310 DOOR FRAME BOEING 747 747273C 1384896 NM CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 NR 3 MAIN ENTRY DOOR FRAME IS PRONE TO CRACKING FROM FATIGUE, INSPECTION REVEALED THE REQUIREMENT TO REPAIR/MODIFY BS 12 65 FRAME WEB AND CHORD PER EO 53-747-1580-00 REV E. CARRIED OUT MODIFICATION OF INTERCOSTAL AND FRAME AND INSTALLED NEW INNER CHORD AS PER SB 747-53A2416, REV 3. 2 L 7 4 4F A20WE 2007031200161 20070312 00161 NM 2007 3 12 SWAA071293 1 20070308 A 3260 65C28034 SENSOR BOEING 737 7373H4 1384600 NM NLG W/W OUT OF RIG A SWAA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SW 29 609SW 27929 DIVERSION/DECLARED EMERGENCY. ON APPROACH NLG UNSAFE LIGHT ILLUMINATED, AND NO MLG INDICATIONS. FERRY TO PHX FOR TROUB LESHOOTING. REMOVED AND REPLACED MLG LOGIC CARDS PER MM. RIGGED NLG LOCK SENSOR PER MM. 2 L 7 2 4F RT A16WE 2007031200170 20070312 00170 NM 2007 3 12 NOCA00207 1 20070102 A 3260 321004258 PSEU BOEING 767 76736N 1385152 NM E&E BAY MALFUNCTIONED A NOCA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 15 768NA 29898 TCAS FAIL LANDING GEAR INDICATING DOWN. PERFORMED FIM 32-09-03 PSEU AT FAULT, REMOVED AND REPLACED PSEU PER MM 32-09-04 , OPS OK. PERFORMED SYS TEST PER 32-09-04, TEST OK. 2 L 7 2 4F RT A1NM 2007031200171 20070312 00171 NM 2007 3 12 NOCA00307 1 20070102 A 3270 321004258 PSEU BOEING 767 76736N 1385152 NM TAIL SKID MALFUNCTIONED A NOCA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 15 768NA 29898 TAIL SKID LIGHT ON. REMOVED AND REPLACED PSEU PERFORMED FIM TASK 32-71-00, LIGHT AND MESSAGE OPERATE NORMAL. 2 L 7 2 4F RT A1NM 2007031200177 20070312 00177 WP 2007 3 12 ABXA070064 1 20070219 A 5322 99162701 SHEAR TIE DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 CRACKED SHEAR TIE FITTING IN KEEL AREA AT STA 655 LONGERON 29 LEFT. REMOVED AND REPLACED SHEAR TIE FITTING FS 655, LONG ERON 29 LEFT IAW DC9 SRM 51-30-5 AND 51-10-4. 2 L 7 2 4F A6WE 2007031200182 20070312 00182 WP 2007 3 12 ABXA070061 1 20070215 A 2740 591096235 JACKSCREW DOUG DC9 DC941 302207N WP HORIZ STAB MAKING METAL A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 HORIZONTAL STABILIZER JACKSCREW HAD WORN THREADS AND METAL IN THE GREASE. REMOVED AND REPLACED JACKSCREW AND ACME NUT. 2 L 7 2 4F A6WE 2007031200187 20070312 00187 WP 2007 3 12 MWEA070041 1 20070305 A 5350 29633 LATCH DOUG DC9 DC982 3022082 WP TAILCONE BROKEN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 810ME 48072 AFT TAIL CONE DOOR ARMING, DISARMING GUARD WILL NOT REMAIN DOWN AND LOCKED ON PLACE. REMOVED AND REPLACED LATCH. 2 L 7 2 4F A6WE 2007031200194 20070312 00194 NM 2007 3 12 SWAA071285 1 20070308 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031200197 20070312 00197 EA 2007 3 12 TRAX200700326 1 20070305 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE J WARNING INDICATION DE DESCENT 1 SO 27 924EV 7830 FLAPS FAIL AT 0. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007031200198 20070312 00198 EA 2007 3 12 TRAX200700316 1 20070226 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA AIR STAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 709EV 10068 ASD EXTERNAL HANDLE CRACKED. 2 L 7 2 4F RT A21EA 2007031200201 20070312 00201 EA 2007 3 12 TRAX200700319 1 20070302 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DEFECTIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 709EV 10068 NR 1 EMERGENCY BATTERY PACK WILL NOT KEEP A CHARGE. 2 L 7 2 4F RT A21EA 2007031200209 20070312 00209 EA 2007 3 12 REXA200700045 1 20070304 A 2110 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA ODOR A REXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 824AY 8024 ON TAKEOFF GOT SMOKE AND SWEET BURNING ODOR. QRH FOLLOWED RETURNED TO AIRPORT. FOUND TO BE RESIDUAL DE-ICE FLUID IN EC S SYSTEM. ENGINE RUNS PERFORMED OPERATIONAL CHECKED GOOD 2 L 7 2 4F RT A21EA 2007031200210 20070312 00210 EA 2007 3 12 REXA20070046 1 20070304 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA CONTAMINATED A REXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 8907A 8907 AFTER TAKEOFF GOT SMOKE IN CABIN. FOLLOWED QRH AND RETURNED TO AIRPORT. SYSTEM TESTED AND FOUND TO RESIDUAL DE-ICE FLU ID IN ECS PACKS. HIGH POWER ENGINE RUNS OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2007031200211 20070312 00211 2007 3 12 REXA920070048 4 20070308 A 2562 4535000 G SWITCH ARTEX CNDAIR CL600 CL6002B19 1900309 EA ELT INOPERATIVE A REXA K NONE O OTHER IN INSP/MAINT 1 SO 25 08460 8029 ELT G-SWITCH FOUND INOP DURING SCHEDULED INSPECTION. 2 L 7 2 4F RT A21EA 2007031200225 20070312 00225 2007 3 12 ZZDA070225140 4 20070225 A 2565 3961899501 LANYARD BOEING 717 717200 1383700 NM EVAC SLIDE BROKEN A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 923AT 55051 L1 DOOR GIRT BAR LANYARD BROKEN (WHERE GIRT BAR SLIDES THROUGH LANYARD). REPLACED LANYARD IAW MM 25-61-01. 2 L 7 2 4F TR A6WE 2007031200235 20070312 00235 2007 3 12 REXA920070047 4 20070308 A 2562 4535000 G SWITCH ARTEX CNDAIR CL600 CL6002B19 1900309 EA ELT INOPERATIVE A REXA K NONE L NO TEST IN INSP/MAINT 1 SO 25 08460 8029 G-SWITCH FOUND INOP DURING SCHEDULED INSPECTION. 2 L 7 2 4F RT A21EA 2007031200236 20070312 00236 WP 2007 3 12 07FDEA00658 1 20070305 A 5230 FITTING DOUG MD10 MD1010F 3022112 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 566FE 46989 FOUND MAIN CARGO DOOR NR 7 SPOOL FITTING HAS CRACK INDICATION. 2 L 7 3 4F RT A22WE 2007031200237 20070312 00237 NM 2007 3 12 07FDEA00659 1 20070306 A 5280 651756395 DOOR BOEING 727 727225 1384077 NM ZONE 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FOUND NLG LEFT FORWARD DOOR, INBOARD INNER CHORD IS CORRODED THRU AT AFT END REPLACED LEFT FWD NLG DOOR. REF MM 32-22-0 01-4, PG 1. DOOR ADJUSTMENT AND TEST ACCOMPLISHED ON ROUTINE CARD 71C130-00 SEQ# 98. 2 L 7 3 4F A3WE 2007031200238 20070312 00238 NM 2007 3 12 07FDEA00660 1 20070306 A 5340 654531313 STRINGER CLIP BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FOUND MAIN DECK BODY FRAME STR CLIP IS CRACKED AT BS 970, STR 9L REMOVED AND REPLACED CRACKED STRINGER ATTACH CLIP AT S TRINGER 9L, BS 970 PER SRM 51-30-02 PG 8. 2 L 7 3 4F A3WE 2007031200239 20070312 00239 EU 2007 3 12 07FDEA00394 1 20070209 A 5300 UNKNOWN AIRBUS 310 A310203 3930313 EU BS 1446-1461 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 409FE 273 PREVIOUS REPAIR FOUND LOCATED RT, FS 1446-1461, FR 20-20A AND STR 38-41. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DET ERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIR ACCOMPLISHED PER FEDEX EA NR 6-5310-105667. REPAIR EVALUATED AND CLASSIFIED AS PER GMM 6 -2-100 AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031200241 20070312 00241 EU 2007 3 12 07FDEA00402 1 20070209 A 5100 UNKNOWN AIRBUS 310 A310203 3930313 EU UNKNOWN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 409FE 273 PREVIOUS COMPOSITE REPAIR FOUND LOCATED ON THE RT ELEVATOR LOWER SURFACE TRAILING EDGE STA 473. REPAIR REQUIRES EVALUAT ION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED PER SRM 55-21-11 AND EA 6-5510-106683. REPAIR EVALUATED AND CLASSIFIED AS PER GMM 6-2-100 AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031200242 20070312 00242 NM 2007 3 12 NOCA04807 1 20070227 A 2611 033638500 BLOWER BOEING 757 75728A 1384976 NM SMOKE DETECTOR MALFUNCTIONED A NOCA K NONE J WARNING INDICATION NR NOT REPORTED 1 EA 15 752NA 28174 FWD DET FAN STATUS ON EICAS. PERFORMED FIM TASK 26-16-00 FOUND SMOKE DET BLOWER M10462 AT FAULT REMOVED AND REPLACED BL OWER PER MM 26-16-02. OPS CHECKS OK. 2 L 7 2 4F RT A2NM 2007031200243 20070312 00243 EU 2007 3 12 07FDEA00403 1 20070209 A 5512 SKIN AIRBUS 310 A310203 3930313 EU HORIZONTAL STAB MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 409FE 273 PREVIOUS FLUSH REPAIR FOUND LOCATED ON THE LEADING EDGE OF THE LT HORIZONTAL STABILIZER LEADING EDGE PANEL 331CB. REPAI R REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 55-12-12 FIG 203. REPAI R EVALUATED AND CLASSIFIED AS PER GMM 6-2-100 AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031200250 20070312 00250 CE 2007 3 12 SAI020701 1 20070220 A 5711 SPAR CESSNA 402 402B 207590P CE WING CRACKED B EATA K NONE O OTHER IN INSP/MAINT 1 GL 09 33NC 10642 402B0825 CRACKS WERE LOCATED OUT OF THE RADIUS GOING TO A RIVET ON ALL FOUR LOCATIONS OF THE MAIN SPAR WEB ABOVE THE UPPER MAIN S PAR CAP AT FS 154.50. THE FWD AND AFT MAIN SPAR WEB EXTENDS ABOVE THE CAP WHEN IT EXITS THE FUSELAGE AND FORMS A FLANGE WHERE THE UPPER SKINS ATTACH. REPAIR WAS COMPLETED WITH A DER. 1 L 7 2 3O A7CE 2007031300003 20070313 00003 WP 2007 3 13 07FDEA00663 1 20070306 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 600 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 FOUND MAIN CARGO COMPARTMENT STA 795 RBL 48,SEAT TRACK IS GOUGED. REMOVED AND REPLACED SEAT TRACK SECTION IAW DC/MD10 S RM 53-70-00 FIG 1 VOL.I, 51-21-01 VOL II PG1-18. MAJOR REPAIR, MECH 2579, QC227. 2 L 7 3 4F A22WE 2007031300015 20070313 00015 EU 2007 3 13 07FDEA00675 1 20070307 A 5300 LATCH AIRBUS 300 A300B4622R 3930312 EU UNKNOWN CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 FOUND CORROSION ON Y-Z LATCH SUPPORT AT C25A RT. REPAIR WAS PERFORMED IAW SRM 53-13-13, FIG 204, SHEET 1, 2. 2 L 7 2 4F RT A35EU 2007031300031 20070313 00031 EU 2007 3 13 07FDEA00425 1 20070209 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 409FE 273 PREVIOUS REPAIR FOUND LOCATED ON THE LT SEAT TRACK, FR 20-21 AND Y246. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETE RMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFOR M TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER FEDEX EA 6-5310-10669. REPAIR EVALUATED PER GMM 6-2-100 AND C LASSIFIED AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031300032 20070313 00032 NM 2007 3 13 07FDEA00530 1 20070220 A 5313 AJC72081 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 EMPENNAGE, AFT FUSELAGE COMPARTMENT APPROX STA 2023 LONGERON 45L FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5310-106597, F USELAGE MAINFRAME LONGERON 45 (L/H). REPAIR AT BODY STATION Y = 2007 - Y = 2033/STANDARD REPAIR DRAWING (NR SR10530090) EMBODIMENT. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007031300033 20070313 00033 2007 3 13 AMTA200700135 4 20070303 A 2310 9640453011 COUPLER BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE LT HF SYS UNSERVICEABLE A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 561TZ 33526 LT TRANSMISSION INTERMITTENT AT ALL CREW STATIONS. REMOVED AND REPLACED LT HF COUPLER IAW MM. INSTALLATION TEST NORMAL . (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007031300034 20070313 00034 EU 2007 3 13 YENA2007012 1 20070301 A 2797 190143401 WIRE HARNESS EMB ERJ190 ERJ190100IGW 3260408 EU NR 2 SLAT DAMAGED A YENA O OTHER J WARNING INDICATION AP APPROACH 1 EA 15 183JB 3256 19000007 AT 1500 FT FLAPS SELECTED 5. SLATS TRAVELLED TO FULL ON EICAS WHILE FLAPS INDICATED SOMEWHERE BETWEEN 1/2 AND FULL. EX ECUTED QRH CHECKLIST. AFTER CHECKLIST COMPLETED, SLATS INDICATED FULL WHILE FLAPS WERE AT 5. NORMAL LANDING. FOUND SL AT NR 2 HARNESS W611 ON RIGHT WING DAMAGED. REMOVED AND REPLACED HARNESS IAW W611 27-83-07-400-801A. OPS CHECK NORMAL & WING THERMAL ANTI-ICE, OPS NORMAL. 2 L 7 2 4F RT A57NM 2007031300035 20070313 00035 NM 2007 3 13 UPS07449293 1 20070212 A 5347 SEAT TRACK BOEING 747 747121 1384871 NM BS 1500-1520 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 1500-1520 LBL 97 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.028" X .5" X 8" E XCEEDS SRM 53-10-01 FIG 1 LIMITS, M/D BS 1483 - 1550 LBL 97 - 99" SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2007031300036 20070313 00036 WP 2007 3 13 070056 1 20070227 A 3350 LAMP DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 860GA 49786 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE REPORTED THAT THE EGRESS PATH LIGHTING AT ROW 36 WOULD NOT TEST. REPORTED RELAMPED THE FIXTURE. A SATISFACTORY OPERATIONAL TEST WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPL ANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007031300037 20070313 00037 WP 2007 3 13 070055 1 20070226 A 3350 1001191 PORTABLE LIGHT DOUG DC9 DC983 3022083 WP L1 DOOR MALFUNCTIONED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 871GA 53296 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION LAS VEGAS MAINTENANCE REPORTED THAT THE MAIN PASSENGER DOOR (L1) POR TABLE EMERGENCY LIGHT WOULD NOT EXTINGUISH. LAS VEGAS MAINTENANCE REMOVED AND REPLACED THE PORTABLE LIGHT ASSY AT THE L 1 DOOR. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007031300038 20070313 00038 WP 2007 3 13 070064 1 20070311 A 3350 60030431 POWER SUPPLY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 863GA 49911 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION LAS VEGAS MAINTENANCE REPORTED THAT THE CEILING EMERGENCY EXIT SIGNS AT THE OVERWING EXIT HATCHES WOULD NOT TEST. LAS VEGAS MAINTENANCE REPORT THE REMOVAL AND REPLACEMENT OF THE APPROPRIA TE EMERGENCY LIGHT POWER SUPPLY UNIT. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007031300039 20070313 00039 2007 3 13 070063 4 20070309 A 3418 STALL WARNING DOUG MD80 MD83 3023681 NM UNKNOWN A WX0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 19 874GA 49643 FLIGHT 462 LAS/PIA - FLT CREW REPORT THAT THE STALL INDICATION FAILURE ANNUNCIATOR ILLUMINATED AFTER FLAP/SLAT RETRACTIO N. DURING CLIMB-OUT, BOTH SYSTEMS TESTED GOOD AND THE ANNUNCIATOR EXTINGUISHED DURING APPROACH WHEN FLAPS WERE EXTENDED TO 11 AND 15 DEGREES. RETURNED TO POINT OF DEPARTURE & LANDED WITHOUT FURTHER INCIDENT. R & R STALL WARNING COMPUTER PER AMM 34-19-02. R & R LT AOA TRANSDUCER PER AMM 34-19-01. R & R RT AOA TRANSDUCER PER AMM 34-19-01. TESTED STALL WA RNING SYSTEM PER AMM 34-19-00. TEST FAILED. DURING TEST, STICK PUSHER WAS HEARD MAKING EXCESSIVE NOISE. R & R STICK PU SHER SERVO DRIVE. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 34-19-00. SUBSEQUENTLY, THE STALL INDICATI 2 L 7 2 4F RT 2007031300123 20070313 00123 EA 2007 3 13 COMA0770019 1 20070306 A 5610 NP13932110 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A COMA O OTHER O OTHER CR CRUISE 1 SO 01 378CA 10371 10097 FLIGHT 5280 - F/O WINDSHIELD CENTER PANE AT FL 390. LANDED WITHOUT INCIDENT. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 2007031300124 20070313 00124 NM 2007 3 13 SWAA071305 1 20070308 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 380 S2L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 2L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007031300125 20070313 00125 NM 2007 3 13 SWAA071300 1 20070309 A 2120 65C29582 DUCT BOEING 737 7373H4 1384600 NM KEELBEAM LOOSE A SWAA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 SW 29 359SW 26596 DECLARED EMERGENCY, CABIN PRESS WARNING HORN SOUNDED. FOUND A/C DISTRIBUTION KEEL BEAM DUCT BOOT CLAMP LOOSE. SECURED DUCT CLAMP PER MM. 2 L 7 2 4F RT A16WE 2007031300126 20070313 00126 NM 2007 3 13 SWAA071296 1 20070307 A 5520 6959227 BUSHING BOEING 737 7375H4 138449D NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED MV2 CHECK, FOUND EXCESSIVE PLAY AT RIGHT ELEVATOR TAB. REMOVED AND REPLACED RIGHT ELEV TAB CONTROL MEC HANISM OUTBOARD BUSHING. 2 L 7 2 4F RT A16WE 2007031300127 20070313 00127 NM 2007 3 13 SWAA071301 1 20070309 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN FLOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 436WN 32456 EEPLS TRACK BROKEN WITH WIRES EXPOSED AT FWD END. REMOVED AND REPLACED EEPLS TRACK SECTION PER MM. 2 L 7 2 4F RT A16WE 2007031300128 20070313 00128 EA 2007 3 13 COMA0760237 1 20070307 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS UNKNOWN A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 986CA 7174 FLIGHT 5251 - RECEIVED FLAP FAIL MESSAGE. LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -F IRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2007031300129 20070313 00129 NM 2007 3 13 CALA0700125 1 20070308 A 2530 8201110000A OVEN BOEING 737 737724 13844BY NM GALLEY OVERHEATED A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 54711 26912 28782 THE NR 1 OVEN OVERHEATED AND BECAME VERY HOT WITH SMOKE COMING FROM THE OVEN. THE FLIGHT ATTENDANT PULLED THE OVEN CIRC UIT BREAKER AND THE SMOKE CEASED. THE FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEM. THE NR 1 OVEN WAS REMOVED AND REPL ACED IAW IFM 25-36. OPERATION CHECKED NORMAL. 2 L 7 2 4F RT A16WE 2007031300130 20070313 00130 NM 2007 3 13 CALA0700126 1 20070310 A 5210 141T66622 PAWL BOEING 767 767424ER 1385270 NM L2 DOOR BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76062 29457 THE L-2 DOOR WOULD NOT ARM PRIOR TO PUSHBACK. THE EXTERIOR PAWL WAS FOUND BROKEN. THE INTERLOCK PAWL WAS REPLACED IAW MM 52-11-26. 2 L 7 2 4F RT A1NM 2007031300131 20070313 00131 WP 2007 3 13 IXXA07SMN054S 1 20070131 A 5330 SKIN DOUG DC8 DC871F 302199D WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT STATION FS1400.00 LONGERON 33 RIGHT. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND, AFTER DAMAGE REMOVED. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC 8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-21, DC8 SRM 51-1-20B, DC8 SRM 51-1-20D, DC8 SRM 51-3-1, DOUGLAS DRAWING NUMBER SR08530019, AD-2005-18-07,S.B DC8-53-078 AND DOUGLAS DRAWING NUMBER 5750776. 2 L 7 4 4F RT 4A25 2007031300132 20070313 00132 NM 2007 3 13 SWAA071309 1 20070310 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 380 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007031300133 20070313 00133 NM 2007 3 13 SWAA071310 1 20070310 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 380 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007031300134 20070313 00134 WP 2007 3 13 IXXA07SMN069S 1 20070131 A 5340 4641324N FITTING DOUG DC8 DC871F 302199D WP BS 1690 S24L CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND A CRACKED FITTING AT STATION FS 1690.000, LONGERON 24 LEFT. REMOVED CRACKED FI TTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1 AND DC8 SRM 51-1-8 B. 2 L 7 4 4F RT 4A25 2007031300135 20070313 00135 WP 2007 3 13 IXXA07SMN059S 1 20070131 A 5340 FITTING DOUG DC8 DC871F 302199D WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION FOUND A CRACKED FITTING AT STATION FS 824.000 LONGERON 14 RIGHT. REMOVED CRACKED FITT ING. FABRICATED FITTING. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND FITTING. INSTALLED FITTING IAW DC8 SRM 51-3-1, DC8 SRM 51-1-20D, DC8 NDT SPM PART 08-00-02 TO 07, DC8 SRM 51-1-8B AND DOUGLAS DRAWING NUMBER 4751643. 2 L 7 4 4F RT 4A25 2007031300136 20070313 00136 WP 2007 3 13 IXXA07SMN067S 1 20070131 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP ZONE 100 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND EXISTING INTERNAL DOUBLER CORRODED FROM STATION FS 1640.000 TO STATION FS 1660. 000 AND FROM LONGERON 29 RIGHT TO LONGERON 33 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND, AFTER DAMAGE REM OVED. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS AND NEW FAST ENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 53-2-0 PAGE 2P, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51 -1-8B, DC8 SRM 51-1-20D, DC8 SRM 51-3-1, SEMAN DRAWING NUMBER ED-4431 DATED 01-23-07 AND COMPLETED FAA FORM 8110-3 NR 07 2 L 7 4 4F RT 4A25 2007031300137 20070313 00137 EA 2007 3 13 COMA0760227 1 20070305 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 781CA 19836 7312 FLIGHT 5374 - LEFT WINDSHIELD CRACKED AND ARCED. RETURNED TO AIRPORT. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED LEFT WINDSHIELD. 2 L 7 2 4F RT A21EA 2007031300138 20070313 00138 WP 2007 3 13 IXXA07SMN061S 1 20070131 A 5340 FITTING DOUG DC8 DC871F 302199D WP ZONE 200 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX * 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND A CRACKED FITTING AT STATION FS702.000 LONGERON 14 RIGHT. REMOVED CRACKED FITT ING. FABRICATED FITTING. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA AND FITTING. INSTALLED FITTING I AW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, DC8 NDT SPM PART 08-00-02-07, DC8 SRM 51-1-8B, DOUGLAS DRAWING NUMBER 3779978. 2 L 7 4 4F RT 4A25 2007031300139 20070313 00139 WP 2007 3 13 IXXA07SMN086S 1 20070131 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 500 MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LEADING EDGE HAS A NON STANDARD REPAIR FROM STATION XFS422.000 TO STA TION XOLDI6.220. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND, AFTER DAMAGE REMOVED. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. AP PLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 51.3.1, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 5 1-1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11,SEMAN DRAWING ED-4436 DATED 01-18-07, COMPLETED FAA FORM 8110-3 NUMBER 07026 DATED 01-22-07. 2 L 7 4 4F RT 4A25 2007031300140 20070313 00140 WP 2007 3 13 IXXA070013O 1 20070308 A 3230 UNKNOWN DOUG DC8 DC871F 302199D WP MLG MALFUNCTIONED A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 829BX 91635 1963 45994 DURING CLIMB-OUT OF KTOL, THE GEAR DOOR WARNING LIGHT ILLUMINATED AFTER A SATISFACTORY GEAR UP-LATCH CHECK. THE CREW RE TURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE MAIN LANDING GEAR DOOR SYSTEM AND REPLACED THE DOOR ACTUA TORS, CONTROL VALVES, DOOR WARNING SWITCHES AND RIGGED BOTH LEFT AND RIGHT MAIN LANDING GEAR DOORS. THE OPERATIONAL CHE CK AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2007031300141 20070313 00141 WP 2007 3 13 IXXA07SMN078S 1 20070131 A 2730 FASTENER DOUG DC8 DC871F 302199D WP ZONE 300 WRONG PART B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR LOWER SKIN PANEL HAS IMPROPER FASTENERS FROM STATION XE306.062 TO STATION XE273.875. REMOVED EXISTING SKIN PANEL WITH IMPROPER FASTENERS. FABRICATED NEW SKIN PANEL AND FINGER DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN PANEL INNER SURFACE. INSTALLED NEW SKIN PANEL FROM STATION XE246.000 TO STATION XH285.000. PERFORMED BALANCE, FOUND WITHIN TOLERANCE MOMENT 1454.8 INCH PO UNDS IAW DC8 SRM 51-4-4 PAGES 1-4, DC8 SRM 55-4-1 FIGURE 1 SHEETS 1 AND 2 ITEMS E AND F, DC8 SRM 55-1-0 PG 1, DC8 SRM 51 -1-21, DC8 SRM 51-1-9 AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007031300142 20070313 00142 WP 2007 3 13 IXXA07SMN077S 1 20070131 A 5522 SKIN DOUG DC8 DC871F 302199D WP ZONE 300 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR LOWER SKIN PANEL HAS A NON STANDARD REPAIR FROM STATION XE79.531 TO STATION XE89.718. REMOVED EXISTING SKIN PANEL WITH NON STANDARD REPAIR. FABRICATED NEW SKIN PANEL AND FINGER DOUBL ER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN PANEL INTERNAL SURFACE. APPLIED S EALANT TO FAYING SURFACES. INSTALLED NEW SKIN PANEL FROM STATION XAR0.00 TO STATION XE132.000. PERFORMED BALANCE, FOUN D WITHIN TOLERANCE, MOMENT 1454.8 INCH POUNDS. IAW DC8 SRM 51-4-4 PAGES 1-4, DC8 SRM 55-4-1 FIGURE 1 SHEETS 1 AND 2, ITE MS "E" AND "F", DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-9, DC8 SRM 51-1-8B, DC8 SRM 51-1-11 AND DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007031300143 20070313 00143 WP 2007 3 13 IXXA07SMN080S 1 20070131 A 5313 LONGERON DOUG DC8 DC871F 302199D WP ZONE 100 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND LONGERON 25 RIGHT CORRODED AT STATION 1620.000. REMOVED FASTENERS. REMOVED CO RROSION. FOUND OUT OF LIMITS. REMOVED CORRODED LONGERON SECTION AND FABRICATED NEW LONGERON SECTION. PERFORMED HEAT T REATMENT. PERFORMED NDT INSPECTION. FABRICATED SPLICES. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-2 FIGURE 4A, DC8 SRM 51-1-8 PAGES 17 AND 18, DC8 SRM 53-2-0 PAGE 2P, DC8 SRM 53-2-2 FIGUR E 4A, DC8 SRM 53-4-1 FIGURE 42 SHEET 2 ITEM "E", DC8 SRM 51-2-0 FIGURE 50, DC8 SRM 51-1-1 PAGES 1, 13 AND 17, DC8 NDT SP M PART 08-00-02, DC8 SRM 53-2-2 FIGURE 10 SHEET 1 AND 3, TR NUMBER 53-153, DATED 12-10-02, DC8 SRM 53-2-2 FIG 10 SHEET 4 2 L 7 4 4F RT 4A25 2007031300144 20070313 00144 WP 2007 3 13 IXXA07SMN081S 1 20070131 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING LOWER CENTRAL LEADING EDGE HAS A NON STANDARD REPAIR FROM STATION XF S304.000 TO XFS316.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRAC K OR CORROSION FOUND, AFTER DAMAGE REMOVED. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS . APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, DC8 SRM 51-1-21, DC 8 SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SEMAN DRAWING NUMBER ED-4433 DATED 01-22- 07 AND COMPLETED FAA FORM 8110-3 NUMBER 07031 DATED 01-26-07. 2 L 7 4 4F RT 4A25 2007031300145 20070313 00145 WP 2007 3 13 IXXA07SMN084S 1 20070131 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 500 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LEADING EDGE HAS A NON STANDARD REPAIR FROM STATION XFS304.000 TO STA TION XFS310.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND, AFTER DAMAGE REMOVED. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS AS N EEDED. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, DC8 SRM 51-1-2 1, DC8 SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001,DC8 SRM 51-18B, DC8 SRM 51-1-11. SEMAN DRAWING NUMBER ED-4435 DATED 01 -20-07 AND COMPLETED FAA FORM 8110-3 NUMBER 07026 DATED 01-22-07. 2 L 7 4 4F RT 4A25 2007031300146 20070313 00146 WP 2007 3 13 IXXA07SMN085S 1 20070131 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 500 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LEADING EDGE HAS A NON STANDARD REPAIR FROM STATION XFS416.000 TO STA TION XOLDI6.220. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS AS NE EDED. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 51.3.1, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SEMAN DRAWING ED-4436 DATED 01-18-07, COMPLETED FAA FORM 8110-3 NUMBER 07026 DATED 01-22-07. 2 L 7 4 4F RT 4A25 2007031300147 20070313 00147 EA 2007 3 13 COMA0770020 1 20070307 A 5610 NP1393225 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 331CA 11505 10061 FLIGHT 5656 - LEFT WINDSHIELD SHATTERED AT FL 360. DECLARED EMERGENCY, DIVERTED TO ATL. LANDED WITHOUT INCIDENT. REPL ACED LEFT WINDSHIELD. 2 L 7 2 4F RT A21EA 2007031300148 20070313 00148 EA 2007 3 13 COMA0760222 1 20070303 A 3010 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA LT WING ANTI ICE UNKNOWN A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 951CA 7091 FLIGHT 5047 - DURING TAKEOFF AT 60 KTS RECEIVED A LEFT WING ANTI-ICE CAUTION MESSAGE, ABORTED TAKEOFF. DEFERRED PER MEL 30-12-03-01. 2 L 7 2 4F RT A21EA 2007031300149 20070313 00149 WP 2007 3 13 IXXA07SMN079S 1 20070131 A 5340 3779978U1 FITTING DOUG DC8 DC871F 302199D WP ZONE 200 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND A CRACKED FITTING AT STATION FS 702.000, LONGERON 19 RIGHT. REMOVED CRACKED FI TTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D DC8 SRM 51-3-1 AND DC8 SRM 51-1-8B . 2 L 7 4 4F RT 4A25 2007031300150 20070313 00150 EA 2007 3 13 COMA0760221 1 20070302 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS UNKNOWN A COMA O OTHER O OTHER AP APPROACH 1 SO 01 796CA 7338 FLIGHT 5270 - FLAPS FAIL CAUTION MESSAGE AT 24 DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007031300151 20070313 00151 EU 2007 3 13 2007UALA00577 1 20070225 A 2497 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE UNKNOWN SHORTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 401UA 435 FOUND SHORTED WIRE BETWEEN SEC AND ACTUATOR. [SUP 05-16-07] FLT RTBL WITH EFCS TEST 1 FAILURE MESSAGE. EFCS FAULTED SE C 2. INITIALLY SWAPPED SEC 2 WITH SEC 3 TO DETERMINE IF FAULT WAS WITH THE SEC UNIT ITSELF. POST SWAP OPS CHECK FAILED, SO STARTED TO PERFORM RESISTANCE CHECKS ON CONNECTORS PER TSM. FOUND SEC 2 PIN 15D HAD 8 OHM RESISTANCE WITH GROUND AND TSM SPECIFIES THAT SHOULD HAVE HAD AT LEAST 100 MEGAOHM. UNWRAPPED WIRING BUNDLE FOR RT ELEVATOR OUTBOARD SERVO AND FOUN D RED WIRE 5954-PF20 TO BE SHORTING UNDERNEATH THE CARGO COMPARTMENT FORWARD MOST FLOORBOARD. REPAIRED WIRE WITH ENVIRON MENTAL SPLICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007031300152 20070313 00152 NM 2007 3 13 2007UALA00578 1 20070226 A 5100 UNKNOWN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SMOKE A UALA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 786UA 26938 222023 SMOKE COMING FROM FWD OUTFLOW VALVE AFTER ENGINE START. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007031300153 20070313 00153 NM 2007 3 13 2007UALA00579 1 20070223 A 2750 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU TE FLAPS UNKNOWN A UALA O OTHER O OTHER AP APPROACH 1 WP 29 340UA 24244 ON FLAP EXTENSION FLAPS DID NOT EXTEND TO SELECTED SETTING, 10 DEG SELECTED ON HANDLE. INDICATOR SPLIT WITH LEFT INDICA TING BETWEEN 0 AND 1, RIGHT INDICATING 1, RIGHT INDICATING. CAUSED BY A FAULTY LEFT HAND FLAP TRANSMITTER. REPLACED LEF T HAND FLAP TRANSMITTER. FOUND TRANSMITTER OUT OF TOLERANCE. ADJUSTED TO MAKE SERVICEABLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007031300154 20070313 00154 NM 2007 3 13 2007UALA00580 1 20070223 A 5313 STRINGER BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU BS 287 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 914UA 25381 BODY STA 287 STRINGER UPPER CROWN LT SIDE. MAJOR REPAIR: REMOVED DAMAGE. INSTALLED PERMANENT REPAIR PER SRM 53-00-01 RE PAIR 31 DETIAL XIX, INSTALLED DOUBLER, TRIPLER, AND FILLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007031300155 20070313 00155 NM 2007 3 13 2007UALA00581 1 20070223 A 5310 DOOR FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 914UA 25381 FWD CARGO CUTOUT AFT FRAME IS CRACKED ON AFT SIDE OF FRAME AT UPPER RADIUS AT I/B CORNER OF LOWER STOP FITTING. MAJOR R EPAIR: REMOVED DAMAGE. INSTALLED REPAIR ANGLES PER MM 53-30-75. 2 L 7 2 4F 4 F RT A16WE E21EU 2007031300156 20070313 00156 NM 2007 3 13 2007UALA00582 1 20070223 A 2432 CHARGER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE MAIN BATTERY FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 779UA 26941 BATTERY MAIN CHARGER STATUS MESSAGE. MAIN BATTERY CHARGER FAILURE MESSAGE. ACTIVE ES HARD FAULT. AFTER TROUBLESHOOT ING, REPLACED MAIN BATTERY. SYSTEM CHECKS OK 2 L 7 2 4F 4 F RT T0001SE E46NE 2007031300157 20070313 00157 NM 2007 3 13 2007UALA00583 1 20070223 A 5610 WINDOW BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT ARCED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 366UA 24535 CAPTAIN SLIDING SIDE WINDOW ELEC ARCING AT MESH WIRE ON AFT SIDE OF WINDOW. FOUND WIRING IN HARNESS LEADING TO WINDOW D AMAGED CAUSING RESISTANCE BUILD UP. REPLACED WINDOW, WINDOW HEAT CONTROLLER, AND REPAIRED WIRING HARNESS AT CAPT SLIDIN G WINDOW POSITION. ALL SYSTEMS CHECK GOOD AFTER WORK ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007031300176 20070313 00176 2007 3 13 NWAA071009855 2 20070311 A 7261 FITTING DOUG DC9 DC951 3022051 WP RT ENGINE LEAKING A NWAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 01 764NC 47717 THE FLIGHT ATTENDANT REPORTED ACCUMULATION OF SMOKE IN THE CABIN DURING CLIMB. COM PROCEDURES WERE COMPLIED WITH AND TH E AIRCRAFT RETURNED TO A NORMAL LANDING. MAINTENANCE AT DTW COULD NOT DUPLICATE THE SMOKE USING APU AIR OR ENGINE AIR ( IDLE AND HIGH POWER). THE RIGHT ACM AND THE COALESCER BAGS WERE ALL CHANGED BUT NO DEFECTS NOTED. A LEAKING FITTING ON THE RIGHT ENGINE NR 4 BEARING BREATHER LINE WAS SECURED, A LEAKING LEFT ENGINE OIL TANK TRANSFER TUBE WAS REPLACED, AND THE RIGHT ENGINE FUEL FLOW TRANSMITTER WAS REPLACED DUE TO SPRAYING FUEL. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007031300177 20070313 00177 CE 2007 3 13 GUUA02190701 1 20070219 A 7120 12991004717 TRUSS BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE ZONE 400 CHAFED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81536 UE152 AT SCHEDULED ROUTINE MAINTENANCE DISCOVERED ENGINE TRUSS TUBE PN 129-910032-101 CHAFING DAMAGE AT 2.5 INCHES AFT OF FIRE SEAL FLANGE ON IB SIDE. PERFORMED TRUSS REPAIR TO CHAFFED AREA IAW APPROVED DATA CONTAINED IN THE MFG AIRLINER SERIES STRUCTURAL REPAIR MANUAL, CHAPTER 71-91-05. 2 L 7 2 4T 4 T RT A24CE E26NE 2007031300178 20070313 00178 WP 2007 3 13 AALA20070355 1 20070216 A 3213 STRUT DOUG DC9 DC982 3022082 WP NOSE GEAR LEAKING A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 468AA 49598 ORD INFLIGHT - UNABLE TO RETRACT LANDING GEAR. THREE GREEN INDICATION AT ALL TIMES. GEAR HANDLE WOULD NOT MOVE FULL RA NGE. LANDED ORD WITHOUT INCIDENT. FOUND NOSE LANDING GEAR STRUT NOT FULLY EXTENDING. REPACKED NOSE LANDING GEAR STRUT . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007031300179 20070313 00179 NM 2007 3 13 AALA20070356 1 20070218 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 774AN 29581 NRT - FOUND EMERGENCY LIGHT AT FIRST CLASS CLOSET LEFT CORNER BROKEN. REPLACED EMERGENCY LIGHT AT FIRST CLASS CLOSET LE FT CORNER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007031300180 20070313 00180 EU 2007 3 13 AALA20070368 1 20070218 A 3297 WIRE HARNESS AIRBUS 300 A300B4605R 3930308 EU MLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 33069 512 JFK INFLIGHT - LANDING GEAR WOULD NOT RETRACT. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED GIRT MAIN LANDING GEAR HARNESS ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007031300181 20070313 00181 NM 2007 3 13 AALA20070369 1 20070218 A 3350 101331101 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 675AN 29425 SEA - EMERGENCY LIGHT AT LEFT OVERWING EXIT HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LEFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007031300182 20070313 00182 NM 2007 3 13 AALA20070367 1 20070218 A 3097 WIRE BOEING 767 767323 1385205 NM ANTI ICE RELAY INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 393AN 29430 DFW INFLIGHT T239/18FEB SJU TO LAX - AFTER TAKEOFF CREW HAD RIGHT WING ANTI-ICE INDICATION AND RIGHT WING ANTI-ICE VAL VE INDICATION. LANDED DFW WITHOUT INCIDENT. REPLACED RELAY BASE K1155 AND REPAIRED BROKEN WIRE. REINSTALLED RELAY. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007031300183 20070313 00183 WP 2007 3 13 AALA20070361 1 20070217 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 214AA 49162 DFW - EMERGENCY LIGHTS AT AFT CABIN CEILING AND TAIL COMPARTMENT LOWER SLIDE FLOOD LIGHT INOPERATIVE. REPOSITIONED BATT ERIES IN THE BATTERY PACK CLIPS FOR EMERGENCY LIGHTS IN AFT CABIN CEILING AND TAIL COMPARTMENT LOWER SLIDE FLOOD LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007031300184 20070313 00184 WP 2007 3 13 AALA20070362 1 20070217 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 214AA 49162 DFW - EMERGENCY EXIT LIGHT AT AFT LEFT OVERWING HATCH HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY EXIT LIGHT AT AFT LE FT OVERWING HATCH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007031300185 20070313 00185 NE 2007 3 13 AALA20070364 2 20070218 A 7230 BLADE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LEFT ENGINE FAILED A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 562AA 49344 708524 DFW INFLIGHT T1511/18FEB - DURING CLIMB, LEFT ENGINE SPOOLED TO IDLE POWER WITH EXCESSIVE VIBRATION AND ENGINE GAS TEMP ERATURE AT 800 DEGREES. SHUT DOWN LEFT ENGINE AND LANDED DFW WITHOUT INCIDENT. REPLACED LEFT ENGINE DUE TO COMPRESSOR BLADE FAILURE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A6WE E9NE 2007031300186 20070313 00186 EU 2007 3 13 NWAA070973258 1 20070308 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320212 3930322 EU EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 358NW 18385 18385 832 FOUND "EPSU UNIT FWD L" MESSAGE ON CIDS PANEL, EMERGENCY LIGHT POWER 10WL. REPLACE 10WL EPSU, OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 2007031300187 20070313 00187 EU 2007 3 13 NWAA070983263 1 20070307 A 3610 SEAL AIRBUS 320 A320212 3930322 EU BLEED SYS DAMAGED A NWAA B EMER. DESCENT O OTHER DE DESCENT 1 GL 01 363NW 0923 AT FLIGHT LEVEL 190, AIR R WING LEAK ANNUNCIATED. LOST PRESSURIZATION DUE TO LEFT PACK PREVIOUSLY PLACED ON MEL. PER CO M PROCEDURE AN EMERGENCY WAS DECLARED AND EMERGENCY DESCENT EXECUTED. SHORTLY FOLLOWING THE BLEED FAULT EXTINGUISHED, W ITH SYSTEM RECOVERING. EMERGENCY CANCELLED WITH ATC AND FLIGHT CONTINUED TO DESTINATION WITHOUT FURTHER INCIDENT. REPL ACED DUCT SEALS LOCATED BETWEEN FLOW CONTROL VALVE AND PACK HEAT EXCHANGER. LEAK CHECKED GOOD. 2 L 7 2 4F RT A28NM 2007031300188 20070313 00188 SO 2007 3 13 FFKA115 2 20070306 A 7414 10682016 GEAR CONTIN D3000 PIPER PA32 PA32R300 7103213 SO LYC 0540 IO540K1G5D 41532 SO MAGNETO DAMAGED B FFKA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 05 333TG 56 F140008CR 32R7680320 RL2752848A PILOT REPORTED THAT THE ENGINE IS RUNNING ROUGH DURING TAXI AND HAD A BAD MAGNETO DROP. MAINTENANCE INVESTIGATED THE PR OBLEM AND DETERMINED THAT THE MAGNETO P/N 10-682560-13 NEEDED TO BE REPLACED. UPON FURTHER INVESTIGATION OF THE MAGNETO , FOUND THAT 2 EACH OF P/N 10-682016 HAD BROKEN TEETH ON THE GEAR ASSEMBLIES. 1 L 7 1 3O 3 O A3SO 1E4 2007031300189 20070313 00189 CE 2007 3 13 GUUA02260701 1 20070226 A 7120 12991004717 TRUSS BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE ZONE 400 CHAFED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 69547 UE189 AT SCHEDULED ROUTINE MAINTENANCE DISCOVERED ENGINE TRUSS TUBE PN 129-910032-101 CHAFING DAMAGE AT 2.5 INCHES AFT OF FIRE SEAL FLANGE ON IB SIDE. PERFORMED TRUSS REPAIR TO CHAFFED AREA IAW APPROVED DATA CONTAINED IN THE DWG NR 070226,DERT 5 10305-CE. 2 L 7 2 4T 4 T RT A24CE E26NE 2007031300190 20070313 00190 CE 2007 3 13 GUUA03030701 1 20070303 A 2697 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE ZONE 400 LOOSE A GUUA O OTHER J WARNING INDICATION CR CRUISE 1 SO 29 69547 UE189 FLIGHT:9253 TBI/FLL DURING FLIGHT RT ENGINE FIRE EXTINGUISHER DISCHARGE ANNUNCIATOR ILLUMINATED. SECURED WIRE ON RT ENG INE FIRE BOTTLE. 2 L 7 2 4T 4 T RT A24CE E26NE 2007031300191 20070313 00191 EU 2007 3 13 UPS07149268 1 20070228 A 3230 PROXIMITY SENSOR AIRBUS A300 A300F4622R 3930360 EU MLG MALFUNCTIONED A IPXA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 SO 01 172UP 0005 INSPECTION TYPE:N/A ATB - LANDING GEAR WOULD NOT RETRACT & STBY PITOT HEAT INOP. REMOVED AND REPLACED NOSE GEAR PROX DE TECTOR SSGB PER TECH SUPPORT M/M 32-00-00-04, SEC E, PARA D. OPS CHECK GEAR PER MM 32-31-00-05. OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2007031300192 20070313 00192 NM 2007 3 13 UPS07449269 1 20070301 A 3240 BRAKE BOEING 747 747123 1384873 NM MLG FAILED A IPXA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 672UP 20324 INSPECTION TYPE:N/A BTB - BRAKES BOTTOMED OUT DURING TAXI. BLED BRAKE SYS IAW 32-41-00. CK'D CABLE TENSION IAW AMM 32- 41-00, PG 501. CABLE TENSION CKS GOOD. TAXIED A/C BRAKES OPERATE NORMAL IAW AMM 32-41-00 PG 1. OK FOR SERVICE. 2 L 7 4 4F A20WE 2007031300193 20070313 00193 NM 2007 3 13 UPS07449273 1 20070214 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1640 S32L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C AFT CARGO LEFT STA 1640 STR 32L STRINGER FOUND CRACK APPROX .125 INCH AS MARKED. AFT CARGO LEFT STRIN GER S32L REPAIRED AS PER SRM 53-10-03 FIG 1, JUST BETWEEN STA 1630 AND 1670. 2 L 7 4 4F A20WE 2007031300194 20070313 00194 NE 2007 3 13 2007UALA00633 2 20070301 A 7200 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ENGINE UNKNOWN A UALA O OTHER O OTHER DE DESCENT 1 WP 29 454UA 1104 V11015 ENG NR 1 STALL ON POWER REDUCTION DESCENDING OUT OF FL 380, 1 SECONDS THUD HEARD AND STALL ECAM FOR 5 SECONDS. THEN ALL INDICATIONS NORMAL. [SUP 05-18-07] INITIALLY ATTRIBUTED TO POSSIBLE 7TH OR 10TH STAGE BLEED VALVE SOLENOID FAILURE. D ID FIND THAT 7TH STAGE VALVE SOLENOID WAS NOT CLOSING CORRECTLY AND WAS REPLACED. HOWEVER AFTER SIMILAR EVENT OCCURRED O N FLIGHT 472 APRIL 8TH, FURTHER INVESTIGATION CORRECTLY DETERMINED THAT THE ROOT CAUSE OF THE CONDITION WAS A FAULTY VAR IABLE STATOR VANE ACTUATOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007031300195 20070313 00195 NM 2007 3 13 2007UALA00634 1 20070302 A 3397 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 547UA 25368 A-ZONE FLOOR EEL INOP FROM SEAT 3 TO SEAT 6. REPAIRED CABLE. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007031400002 20070314 00002 CE 2007 3 14 DJFA2007027 1 20070308 A 2700 UNKNOWN BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE UNKNOWN E DJFA O OTHER F FLT CONT AFFECTED CR CRUISE 1 EA 23 454LX RK327 TRIP NR 1152283/ CREW REPORTED AT FLIGHT LEVEL 380 IN CLEAR SKYS AND SMOOTH AIR A LOUD NOISE SOUNDED AND RANG OUT THROUG HOUT THE AIRCRAFT. AIRCRAFT PITCHED DOWN MOMENTARILY AND CREW DISENGAGED THE AP AFTER WHICH THE AIRCRAFT RETURNED TO NO RMAL LEVEL FLIGHT. MAINTENANCE IS INVESTIGATING THE DISCREPANCY. MAINTENANCE PERFORMED AN EXTENSIVE INSPECTION OF THE F LIGHT CONTROL SYSTEM, TRIM SYSTEM, AND THE AUTOPILOT SYSTEM. NO DISCREPANCIES WERE NOTED. THE DISCREPANCY HAS NOT RET URNED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007031400003 20070314 00003 CE 2007 3 14 AMW083151BC 1 20070308 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FALSE INDICATION A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 138YV 22649 541 UE138 DURING FLT, BATTERY CHARGE ANNUN ILLUM. THIS BC ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACT ION TO THE PILOTS. BATTERY WAS REPLACED WITH NO FURTHER INCIDENT. 2 L 7 2 4T 4 T RT A24CE E26NE 2007031400004 20070314 00004 CE 2007 3 14 200700001 1 20070206 A 2160 66004238 MOTOR LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE7313A 01518 WP STICKS E DELA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 522WK 088 AMBER DUCT OVHT ANNUNCIATOR ILLUMINATED ABOVE FL300 APPROXIMATELY 20 MINUTES INTO FLIGHT. CREW NOTICED THAT THE CREW TEM P INDICATOR READ 4 ON THE SCALE WITH SYSTEM IN MANUAL AND TEMP CONTROL SELECTED TO FULL COLD. CREW INITIATED THE APPROPR IATE ABNORMAL CHECKLIST PROCEDURES WITH CHANGE IN INDICATIONS. THE CREW DECIDED TO RETURN TO THE DEPARTURE AIRPORT AND C HANGE TO LOWER FL. AT FL260, THE CREW TEMP INDICATOR SCALE READING REDUCED AND THE DUCT OVHT ANNUNCIATOR EXTINGUISHED. 2 L 7 2 4F 4 F A10CE E6WE 2007031400007 20070314 00007 CE 2007 3 14 DXTA200702013 1 20070311 A 3297 WIRE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG DAMAGED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 960QS 7500160 AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT MOVE FROM THE DOWN POSITION, UNABLE TO RETRACT GEAR. REMOVED AND REPLACED NOSE GEAR SQUAT SWITCH, WIRING AND CONNECTOR JG019. ADJUSTED NOSE LANDING GEAR SQUAT SWITCH REF. CE-750 M/M CHPT 32-60-0 0. SWUNG LANDING GEAR SEVERAL TIMES, OPS CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007031400009 20070314 00009 NM 2007 3 14 DXTA200702012 1 20070310 A 3220 LANDING GEAR AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE NOSE NOISY E DXTA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 07 275QS 75 ON TAKEOFF GEAR RETRACTION, LOUD NOISE HEARD FROM NOSE AREA LIKE GEAR DOOR NOT CATCHING OR BINDING SHOOK NOSE OF AIRPLAN E. ON GEAR EXTENSION LOUD NOISE THIS TIME GRINDING SOUND LIKE WHEN TWO GEARS NOT MESHING TOGETHER RIGHT. POSITIONED AIRC RAFT IN HANGAR. INSPECTED GEAR, GEAR DOORS NOSE CONE. NO DEFECTS NOTED. PERFORMED NUMEROUS GEAR SWINGS. NO DEFECTS NOTED . INSPECTED NOSE WHEEL WELL ACCESS PANEL SEAL. FOUND SEAL WORN.REMOVED OLD SEAL P/N FGFB291600003 FROM WHEEL WELL ACCESS PANEL AND CLEANED PANEL. NOTE ALL WORK DONE IAW F-2000 M/M CH 52-40-00-3/11/07. 2 K 7 2 4F 4 F RT A50NM E44NE 2007031400010 20070314 00010 CE 2007 3 14 AWM061222025B 1 20070212 A 5712 11811005010 RIB BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE ZONE 600 CORRODED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 10675 19467 UE229 BIO CORROSION RT WING RIB AT WS124. REPAIRED IAW REPORT AERODESIGN REPORT 6497-1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007031400013 20070314 00013 NM 2007 3 14 UPS07449287 1 20070213 A 5347 SEAT TRACK BOEING 747 747121 1384871 NM BS 908-910 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 908-910 LBL 11 SEAT TRACK BOTH SIDE FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.022" X .75" X 3" IS EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 890-930 LBL 11" SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14. 2 L 7 4 4F A20WE 2007031400014 20070314 00014 NM 2007 3 14 UPS07449291 1 20070216 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 1940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C BULK CARGO COMPT M/D FLOORBEAM LOWER WEB FOUND CRACK AT 1940 RBL 64". CRACK LENGTH .5 INCH. BULK CAR GO COMPT M/D FLOORBEAM LOWER WEB REPAIRED AS PER SRM 51-40-02 FIG 1, JUST AT STA 1940 RBL 64 AREA. 2 L 7 4 4F A20WE 2007031400015 20070314 00015 NM 2007 3 14 UPS07449292 1 20070210 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C EQUIPMENT COOLING OUTLET FOUND ONE EACH FASTENER HOLE CRACKED AT SKIN APPROX .125 INCH LONG RUNNING FW D & APPROX .375 INCH LONG RUNNING TO EDGE. FUSELAGE SKIN AT BS 575 EQUIPMENT COOLING OUTLET REPAIRED AS PER UPS EO B747 -5330-6909 APPENDIX B. 2 L 7 4 4F A20WE 2007031400017 20070314 00017 NM 2007 3 14 UPS07449295 1 20070216 A 5320 FLOOR SUPPORT BOEING 747 747121 1384871 NM BS 1920-1940 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C BULK CARGO COMPT LEFT STA 1920 TO STA 1940 LBL 55" FLOOR SUPPORT UNDER ANCHOR NUT FOUND CORRODED AS MA RKED. CORROSION BLEND OUT 0.025" X .5" X 1" EXCEED SRM 53-10-01 FIG 1 LIMITS. BULK CARGO COMPT LEFT BS 1920 TO 1970 LB L 55" FLOOR SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02. 2 L 7 4 4F A20WE 2007031400019 20070314 00019 CE 2007 3 14 AMW070206033 1 20070226 A 5711 1181000131 SPAR CAP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE ZONE 600 CORRODED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 143YV 21923 UE143 BIO-CORROSION ON RT SPAR CAP FLANGE AT WS124. REPAIRED IAW AERODESIGN ENGINEERING REPORT NR6556-1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007031400023 20070314 00023 NM 2007 3 14 AALA20070352 1 20070217 A 5610 58935733 WINDOW BOEING 737 737823 13844BZ NM COCKPIT CRACKED A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 915AN 29516 LIT- DFW - YYZ - FOUND COCKPIT LEFT NUMBER FOUR WINDOW PANE CRACKED. LANDED LIT WITHOUT INCIDENT. REPLACED COCKPIT LEF T NUMBER FOUR WINDOW. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007031400025 20070314 00025 WP 2007 3 14 AALA20070377 1 20070220 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 33414 49325 LGA - FOUND EMERGENCY LIGHT IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK IN FIRST CLASS OVERHEAD PANEL FOR EMERGE NCY LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007031400026 20070314 00026 EU 2007 3 14 AALA20070379 1 20070221 A 3350 0L3229BPE BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 JFK - FOUND EMERGENCY LIGHT AT SEAT 20G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 20G. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A35EU 2007031400028 20070314 00028 WP 2007 3 14 AALA20070358 1 20070217 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 214AA 49162 DFW - FOUND EMERGENCY LIGHT SHROUD AT SEAT 23D BROKEN. REPLACED EMERGENCY LIGHT SHROUD AT SEAT 23D. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007031400029 20070314 00029 WP 2007 3 14 AALA20070359 1 20070217 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 214AA 49162 DFW - FOUND EMERGENCY SEAT MOUNTED LIGHTS FROM FORWARD CABIN TO SEAT ROW 21 INOPERATIVE. REPLACED BATTERY PACKS AND MOD ULES AT AB51 AND AB52 FOR EMERGENCY SEAT MOUNTED FROM FORWARD CABIN TO SEAT ROW 21. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F A6WE 2007031400030 20070314 00030 WP 2007 3 14 AALA20070360 1 20070217 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 214AA 49162 DFW - FOUND EMERGENCY EXIT LIGHTS FROM FORWARD CABIN TO SEAT ROW 21 INOPERATIVE. REPLACED BATTERY PACKS AND MODULES AT AB51 AND AB52 FOR EMERGENCY EXIT LIGHTS FROM FORWARD CABIN TO SEAT ROW 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007031400031 20070314 00031 WP 2007 3 14 AALA20070376 1 20070220 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9629H 53599 LGA - FOUND EMERGENCY LIGHT AT SEAT ROW 22 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 22. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007031400035 20070314 00035 NE 2007 3 14 DXTA200702016 2 20070312 A 7200 ENGINE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LEFT OUT OF RIG E DXTA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 396QS 5600396 PCE500019 AFTER SPEED BRAKE TEST RETARDED THROTTLE ON LT ENGINE TO THE IDLE STOP AND ENGINE QUIT ON ITS OWN. RIGGED LT ENG SO IT DOES NOT SHUTDOWN AT IDLE. ENG OPS CHECKS GOOD AT THIS TIME. ALL WORK DONE IAW CESSNA 560 M.M. CHAPTER 76-11-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007031400036 20070314 00036 SO 2007 3 14 FFKA117 1 20070312 A 2730 091028600 INSULATOR KING KS272 PIPER PA34 PA34200T 7103406 SO TRIM SERVO PUNCTURED B FFKA O OTHER C F.O.D. NR NOT REPORTED 1 SO 05 86BW 1970 347770340 SMALL HOLE IN INSULATOR CAUSED BY DEBRIS AT INITIAL ASSEMBLY, RESULTED IN THE TRIM SERVO CLUTCH TO BE ENGAGED WHENEVER A IRCRAFT POWER WAS ON. TIME ON PART IS UNKNOWN. 1 L 7 2 3O A7SO 2007031400038 20070314 00038 EU 2007 3 14 NWAA070993303 1 20070311 A 2530 4306800000 OVEN AIRBUS 330 A330323 3930335 EU GALLEY SMOKE A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 803NW 542 DURING CRUISE FLIGHT ATTENDANTS REPORTED SMOKE AT CEILING AREA ABOVE AFT GALLEY, PULLED CIRCUIT BREAKERS AND SMOKE APPEA RED TO STOP. DIVERTED TO LGW AND LANDING WAS UNEVENTFUL. TESTED ALL HOT PLATES, COFFEE MAKERS, BUN WARMERS, CHILLERS, OVENS AND FOUND NR 2 OVEN TO OVER TEMP AND WAS REPLACED AND CHECKS OK. 2 L 7 2 4F RT A46NM 2007031400039 20070314 00039 WP 2007 3 14 AALA20070370 1 20070219 A 4990 OIL SYSTEM DOUG DC9 DC982 3022082 WP APU LEAKING A AALA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 297AA 49309 AFTER TAKEOFF, CREW REPORTED SMOKE AND FUMES IN CABIN. LANDED MCI WITHOUT INCIDENT. FOUND AUXILLIARY POWER UNIT (APU) LEAKING OIL AND INGESTING OIL INTO INLET. REPLACED APU ON 27 FEB AT RDU. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007031400040 20070314 00040 NM 2007 3 14 AALA20070371 1 20070219 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 959AN 30828 MIA - FOUND EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007031400041 20070314 00041 WP 2007 3 14 AALA20070372 1 20070219 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 453AA 49558 DFW - FOUND EMERGENCY LIGHTS NEAR SEAT 28D DAMAGED BY CART. REPLACED LIGHT LENS, TRIM AND BULBS FOR DAMAGED EMERGENCY L IGHTS NEAR SEAT 28D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007031400042 20070314 00042 NM 2007 3 14 AALA20070353 1 20070217 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 MIA - EMERGENCY LIGHT ABOVE SEAT 3A INOPERATIVE. RELAMPED EMERGENCY LIGHT ABOVE SEAT 3A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007031400044 20070314 00044 WP 2007 3 14 UPS07849271 1 20070222 A 3350 CONTROL UNIT DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:N/A COCKPIT EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK CONTROL UNIT PER MM 33-50-02-2 . 2 L 7 4 4F RT 4A25 2007031400046 20070314 00046 CE 2007 3 14 AMW082671 1 20070215 A 3233 11238002223 ACTUATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG FALSE INDICATION A AMWA O OTHER N FALSE WARNING LD LANDING 1 CE 07 126YV 16560 10136 UE126 ON APPROACH TO LANDING THE NOSE GEAR INDICATOR D/N SHOW GEAR DOWN AND LOCKED. CREW PERFORMED EMERGENCY CHECKLIST AND DE CLARED AN EMERGENCY. A FLY-BY OF THE TOWER CONFIRMED GEAR WAS DOWN. THE INTRANSIT LIGHT IN THE GEAR HANDLE WAS ALSO OU T. SO CREW LANDED SAFELY WITH NO FURTHER INCIDENT. REMOVED AND REPLACED NOSE GEAR ACTUATOR, OPS CHECKED GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2007031400047 20070314 00047 NM 2007 3 14 07FDEA00682 1 20070307 A 5220 507978U24 ANGLE BOEING 727 727225 1384077 NM ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FOUND LT FWD EMERGENCY EXIT UPPER FWD SEAL RETAINER ANGLE IS CRACKED AT FASTENER HOLE. REMOVED LT FWD EMERGENCY EXIT UP PER FWD SEAL RETAINER ANGLE AND INSTALLED NEW RETAINER ANGLE PER SRM 51-30-02 PG 2. REMOVED LINER AND REINSTALLED LINER PER SRM 51-30-02 PG 4. 2 L 7 3 4F A3WE 2007031400052 20070314 00052 NM 2007 3 14 07FDEA00686 1 20070307 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 620-700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 CABIN SEAT TRACK HAS CORROSION SPOTS FS 620 - 700 RBL 24. REMOVED AND REPLACED SEAT TRACK FS 620 - 700 RBL 24 IAW SRM 5 1-30-2. 2 L 7 3 4F A3WE 2007031400054 20070314 00054 WP 2007 3 14 07FDEA00689 1 20070307 A 5511 SPAR CAP DOUG DC10 DC1010 3022110 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 FOUND RIGHT AFT OUTBOARD SPAR CAP CRACKED FROM HOLE TO HOLE AND INSIDE THE BOREHOLE (NOTIFY STRUCTURES ENGINEERING PRIOR TO FURTHER FLIGHT). E8-5510-7-3310 PT.4. REPAIRED RIGHT AFT OUTBOARD SPAR CAP IAW FEDEX EA 8-5510-105170-STABLIZER HOR IZ.- AD92-22-10-R/H UPPER AFT SPAR SPLICE-REPAIR. MECH 4315 QC364 MAJOR REPAIR 2 L 7 3 4F A22WE 2007031400056 20070314 00056 WP 2007 3 14 07FDEA00691 1 20070307 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 FOUND MAIN CABIN SEAT TRACK FROM STA 1507 TO 1587 AT LBL 48. REMOVED AND REPLACED SEAT TRACK SECTION IAW MD/DC1 SRM 53- 70-00 FIG 2A VOLI, 51-31-01 VOLII PG 1 AND 51-21-01 VOLII . MAJOR REPAIR. 2 L 7 3 4F A22WE 2007031400057 20070314 00057 2007 3 14 07FDEA00692 4 20070307 A 3452 DOWNLOCK SWITCH AIRBUS 300 A300B4622R 3930312 EU MLG UNKNOWN A FDEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 25 725FD 572 ON FINAL, 400 AGL, RECEIVED A "TO LOW GEAR" VERBAL WARNING, LDG GEAR POSITION DETECTION SYS WAS IN POS "1", SWITCHED TO SYS "2" AND CONTINUED PERFORMED GO-AROUND. ON SECOND ATTEMPT, THERE WAS NO WARNING, ALL SYSTEMS SHOWED GEAR DOWN, AND LANDED. IND R PER TSM AND GPWS SELF TEST, LEVEL NR 5, FLT LEG HISTORY INDICATED, EXT FAULT GEARSWITCH FAULT (79GB). DO WNLOCK SWITCH P/N OF OLD/REMOVED SWITCH AS FOLLOWS-(141FLO1D3--DATE 6/92, CPN# 2310526). REMOVED AND REPLACED SAME PER A300-600 MM NR 32-00-00-4, OPS CHK NORMAL PER A300-600 MM NR 34-48-00-5-02. 2 L 7 2 4F RT A35EU 2007031200216 20070312 00216 EA 2007 3 12 TRAX200700321 1 20070304 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 906EV 7642 LEFT SIDE EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007031200218 20070312 00218 EA 2007 3 12 TRAX200700297 1 20070227 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 885AS 7521 EXTERIOR EMERGENCY FWD OVERWING LIGHT INOP. 2 L 7 2 4F RT A21EA 2007031200219 20070312 00219 EA 2007 3 12 TRAX200700298 1 20070228 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 759EV 10211 CEILING EMERGENCY LIGHT 1 EA INOP. 2 L 7 2 4F RT A21EA 2007031200228 20070312 00228 NM 2007 3 12 NOCA04707 1 20070227 A 2612 TERMINAL BOEING 767 76736N 1385152 NM FIRE LOOP DEFECTIVE A NOCA K NONE N FALSE WARNING UK UNKNOWN 1 EA 15 768NA 29898 RIGHT ENGINE FIRE LOOP 1 STATUS MESSAGE. REPLACED TERMINAL END AT LOWER FWD LOOP 1 DETECTOR PER 26-11-21 WDM. OPS CHEC KS OK. 2 L 7 2 4F RT A1NM 2007031200245 20070312 00245 EU 2007 3 12 07FDEA00408 1 20070209 A 5753 SKIN AIRBUS 310 A310203 3930313 EU TE FLAP MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 409FE 273 PREVIOUS REPAIR FOUND LOCATED ON THE RT INBOARD FLAP, LOWER SURFACE, TRAILING EDGE, RIB 4. REPAIR REQUIRES EVALUATION F OR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIR ACCOMPLISHED PER FEDEX EA 6-5710-106681. REPAIR EVALUATED AND CLASSIFI ED AS PER GMM 6-2-100 AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031200246 20070312 00246 EU 2007 3 12 07FDEA00409 1 20070209 A 5753 SKIN AIRBUS 310 A310203 3930313 EU TE FLAP MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 409FE 273 PREVIOUS REPAIR FOUND LOCATED ON THE RT INBOARD FLAP, LOWER SURFACE, TRAILING EDGE BETWEEN RIB 19-21. REPAIR REQUIRES E VALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AN D FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER FEDEX E.A. Nº 6-5710-106681. REPAIR EVAL UATED AND CLASSIFIED AS PER GMM 6-2-100 AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031200247 20070312 00247 EU 2007 3 12 07FDEA00410 1 20070209 A 5753 SKIN AIRBUS 310 A310203 3930313 EU TE FLAP MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 409FE 273 PREVIOUS REPAIR FOUND LOCATED ON THE RT OUTBOARD FLAP, UPPER SURFACE BETWEEN TRACK 3-4. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIR ACCOMPLISHED PER FEDEX EA Nº 6-5710-106684. REPAIR EVALUATED AND CLASSI FIED AS PER GMM 6-2-100 AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031200248 20070312 00248 EU 2007 3 12 07FDEA00411 1 20070209 A 5310 DOOR FRAME AIRBUS 310 A310203 3930313 EU BS 1461 MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 409FE 273 PREVIOUS REPAIR FOUND LOCATED ON THE FWD CARGO DOOR FRAME, FS 1461, FR 20A AND STR 34. REPAIR REQUIRES EVALUATION FOR M AJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER FEDEX EA Nº 6-5310-105667. REPAIR EVALUATED AND CLASSIF IED AS PER GMM 6-2-100 AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031200249 20070312 00249 EU 2007 3 12 07FDEA00415 1 20070209 A 5310 CROSSBEAM AIRBUS 310 A310203 3930313 EU BS 1976 MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 409FE 273 PREVIOUS REPAIR FOUND LOCATED ON THE FWD PIT CROSSBEAM, RT, FS 1976, FR 36 AND ?Y69. REPAIR REQUIRES EVALUATION FOR MAJ OR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CO NFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 53-10-15 FIG 201 SHEET 2A AND SHEET 3. REPAIR EVALUAT ED AND CLASSIFIED AS PER GMM 6-2-100 AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031200268 20070312 00268 EA 2007 3 12 SWIA200717961 1 20070208 A 5210 MOUNT BRACKET CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 863AS 7487 PAX DOOR - THE DOOR ASSIST MOTOR MOUNTING BRACKET IS CRACKED. (DISCOVERED DURING C-CHECK INSPECTION)INSTALLED NEW STIFF ENER IAW CRJ200 SRM 51-40-11 & SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007031200270 20070312 00270 EA 2007 3 12 SWIA200717963 1 20070208 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 863AS PAX DOOR - THE AFT WEB IS CRACKED UNDER THE HANDRAIL STOW BRACKET AND IN THE RADIUS BETWEEN THE 3RD & 4TH FIXED STEPS. (DISCOVERED DURING C-CHECK INSPECTION) INSTALLED REPAIRS TO PAX DOOR STEP 2 & 3 AFT SIDE WALL IAW CRJ200 REO 601R-52-11- 702 REV A "REPAIR FOR MULTI-SITE DAMAGES: ZONE 2,3,4" (SHEET 8). 2 L 7 2 4F RT A21EA 2007031200277 20070312 00277 EA 2007 3 12 SWIA200717975 1 20070213 A 5210 STIFFENER CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 705SK PAX DOOR AFT WEB EXTRUDED ANGLE STIFFENER CRACKED AT 2ND STEP. (DISCOVERED DURING C-CHECK INSPECTION) INSTALLED REPAI R DOUBLER AND FILLER PER CRJ700/900 SRM 51-71-59-001-001-A01. 2 L 7 2 4F RT A21EA 2007031300016 20070313 00016 NM 2007 3 13 07FDEA00676 1 20070307 A 3210 65179974 CRANK ASSY BOEING 727 7272S2F 1384O81 NM RT MAIN GEAR BROKEN A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 208FE 22930 RED RIGHT GEAR DOOR LIGHTS ILLUMINATED WITH LANDING GEAR HANDLE IN UP POSITION. RAN GEAR UNSAFE AND/ON DOOR LIGHT ILLUM INATED-GEAR HANDLE-UP, BOTH RED LIGHTS REMAINED ILLUMINATED. PLACED GEAR HANDLE DOWN AND ACHIEVED ALL GEAR DOWN AND LOC KED IN THE GREEN. LANDED UNEVENTFULLY AT MEM. FOUND VALVE ACTUATING CRANK BROKE ON RT MAIN GEAR DOOR SEQUENCE VALVE. REMOVED AND REPLACED THE VALVE ACTUATING CRANK IN REF TO 727-200 AMM 32-32-021-4. PERFORMED GEAR SWINGS, SYSTEM OPERAT ED NORMALLY, A/C IS OK FOR CONTINUE SERVICE. 2 L 7 3 4F A3WE 2007031300067 20070313 00067 WP 2007 3 13 IXXA07SMN041S 1 20070119 A 5320 PLATE DOUG DC8 DC871F 302199D WP BS 902 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2944 46065 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT MAIN LANDING GEAR WHEEL WELL PLATE UPPER SIDE CORRODED AT STATION FS902.0 00. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED PLATE. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW PLAT. IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 53-2-0 PAGE 2P AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007031300068 20070313 00068 WP 2007 3 13 IXXA07SMN050S 1 20070131 A 5330 564932975N1 SKIN DOUG DC8 DC871F 302199D WP ZONE 100 DAMAGED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 6994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND LOWER FUSELAGE SKIN HAS SCRATCHES AND SMALL DENT AT STATION FS1870 LONGERON 36. REMOVED DAMAGED SKIN PANEL. CLEANED TREATED AND PRIMED AREA AND NEW SKIN PANEL. APPLIED SEALANT TO FAYING SURFACES I NSTALLED NEW SKIN PANEL FROM STATION FS 1696 TO STATION 1890, LONGERON 28 RIGHT TO LONGERON 28 LEFT IAW DC8 SRM 51-1-20D , DC8 SRM 51-3-1, DC8 SRM 53-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 53-5-1 FIGURE 1 ITEM "E", DC8 SRM 51- 1-8B, DC8 SRM 51-1-11, BOEING MESSAGE NUMBER 1-271850875-2 DATED 01-10-07. 2 L 7 4 4F RT 4A25 2007031300069 20070313 00069 WP 2007 3 13 IXXA07SMN052S 1 20070131 A 5330 564932975N1 SKIN DOUG DC8 DC871F 302199D WP ZONE 100 MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2944 46065 DURING ROUTINE C CHECK INSPECTION FOUND A IMPROPER REPAIR AT STATION FS1762, LONGERON 34 LEFT. REMOVED DAMAGED SKIN PAN EL CLEANED TREATED AND PRIMED AREA AND NEW SKIN PANEL. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN PANEL FR OM STATION 1696 TO STATION 1890, FROM LONGERON 28 RIGHT TO LONGERON 28 LEFT IAW DC8 SRM 51-1-21 SRM 51-1-20D, SRM 51-3-1 , DC8 SRM 53-1-0 PAGE 1, DC8 SRM 51-1-8B, DC8 SRM 53-5-1 FIG 1 ITEM "E", DC8 SRM 51-1-8B, DC8 SRM DC8 51-1-11. BOEING M ESSAGE NUMBER 1-271850875-2 DATED 01-10-07. 2 L 7 4 4F RT 4A25 2007031300100 20070313 00100 WP 2007 3 13 IXXA07SMN060S 1 20070131 A 5340 3779978U1 FITTING DOUG DC8 DC871F 302199D WP BS 824 L19L CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND A CRACKED FITTING AT STATION FS824.000 LONGERON 19 LEFT. REPLACED CRACKED FITT ING IAW DC8 SRM 51-1-20D AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007031300101 20070313 00101 WP 2007 3 13 IXXA07SMN062S 1 20070131 A 5340 3753235U1 FITTING DOUG DC8 DC871F 302199D WP BS 980 L22R CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND A CRACKED FITTING AT STATION FS 980.000 LONGERON 22 RIGHT. REMOVED CRACKED FI TTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1 AND DC8 SRM 51-1-8 B. 2 L 7 4 4F RT 4A25 2007031300102 20070313 00102 WP 2007 3 13 IXXA07SMN065S 1 20070131 A 5753 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT OUTBOARD FLAP HAS A NON STANDARD REPAIR AT STATION XF240.000. REMOVED EX ISTING REPAIR. REMOVED DAMAGED SKIN. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FA BRICATED NEW SKIN AND REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA, NEW SKIN AND REPAIR PARTS. INSTALLED NEW SKIN AN D REPAIR PARTS IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC 8 SRM 51-3-1, AND SEMAN DRAWING NUMBER ED-4430 DATED 01-13-07. COMPLETED FAA FORM 8110-3 NUMBER 07021 DATED 01-19-07 2 L 7 4 4F RT 4A25 2007031300161 20070313 00161 WP 2007 3 13 IXXA07SMN087S 1 20070131 A 5753 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD FLAP UPPER SKIN PANEL HAS A NON STANDARD REPAIR FROM STATIO N XF169.000 TO STATION XF172.000. REMOVED EXISTING SKIN PANEL WITH NON STANDARD REPAIR. FABRICATED NEW SKIN PANEL AND REPAIR PARTS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA, NEW SKIN PANEL AND REPAIR PARTS AS N EEDED. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN PANEL IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SR M 57-7-1 FIGURE 4 PAGE 2 TR NR 57-94 DATED 10-01-02, ITEM "P" AND "Q", DC8 SRM 51-1-9, DC8 SRM 51-1-8B AND DC8 SRM 51-1- 11. 2 L 7 4 4F RT 4A25 2007031300162 20070313 00162 NM 2007 3 13 2007UALA00584 1 20070224 A 2750 UNKNOWN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU TE FLAPS UNKNOWN A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 913UA 25291 AFTER TAKEOFF, FLAPS WOULD NOT RETRACT. AFTER SEVERAL ATTEMPTS FLAPS FINALLY RETRACTED NORMALLY. FLAP TRANSMITTERS OUT OF TOLERANCE. ADJUSTED TRANSMITTERS. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007031300163 20070313 00163 NM 2007 3 13 2007UALA00585 1 20070224 A 2150 A/C PACK BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE INOPERATIVE A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 213UA 30219 LOST RIGHT PACK AFTER DEPARTURE. REPLACED RIGHT SYSTEM LOWER SHUTOFF-PACK FLOW CONTROL VALVE PER MM 21-51-02, PASSED T EST & CLEARED MESSAGE 21-24304 . SUSPECT VALVE STUCK DUE TO FRICTIONAL-INDUCED WARE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007031300164 20070313 00164 NM 2007 3 13 2007UALA00586 1 20070224 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 277-287 S2-4L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 364UA 24533 EXTERIOR FUSELAGE UPPER CROWN BODY STATION S277 TO 287, BETWEEN STRINGERS 2 AND 4 LEFT. FUSELAGE SKIN SCRATCHED, MARKED . SUPPLEMENTAL DATA UPDATE 21 MARCH 07, MAJOR REPAIR: REMOVED DAMAGE. ACCOMPLISHED DOUBLER, TRIPLER AND FILLER REPAIR PE R SRM 53-00-01 REPAIR 31 DETAIL XIX. 2 L 7 2 4F 4 F RT A16WE E21EU 2007031300165 20070313 00165 NM 2007 3 13 2007UALA00587 1 20070224 A 3510 OXYGEN SYSTEM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 774UA 26936 CREW OXYGEN PRESSURE AT ZERO. FOUND LEAKING OXYGEN PRESSURE TRANSDUCER. REPLACED X-DUCER. SERVICED CREW OXYGEN. CHECK ED SYSTEM AND FOUND NO LEAKS. SUSPECT LEAKING AT TRANSDUCER CAUSED BY SEAL LEAKAGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007031300166 20070313 00166 EU 2007 3 13 MALA070037 1 20070301 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297-320 MISREPAIRED A MALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 15 441XJ 340B441 FOUND CABIN SEAT TRACK AT LBL 18.3 HAS AN INCORRECT REPAIR, BETWEEN FS297 AND 320. THE PREVIOUS REPAIR HAS BEEN REMOVED AND NEW REPAIR INSTALLED IAW MESABA EO NR S53060. REF: EAMS WORK ORDER 215609 TASK 1504. 2 L 7 2 4T RT A52EU 2007031300167 20070313 00167 EU 2007 3 13 MALA070038 1 20070305 A 3260 UNKNOWN SAAB SF340 340B 7860101 EU MLG UNKNOWN A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 448XJ 340B448 GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FOLLOWED QRH, RECYCLED GEAR. NO CHANGE. PUT GEAR DOWN, 3 GREEN A ND LANDED AT TVF INSPECTED AIRCRAFT AND FOUND SAFE FOR ONE FERRY TIME FERRY FLIGHT FROM TVF TO MSP FOR TROUBLE SHOOTING AND REPAIR. FERRY AIRCRAFT FROM TVF TO MSP FOR REPAIR OF GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION FOLLOWED Q RH RECYCLED GEAR, NO CHANGE, PUT GEAR DOWN 2 GREEN, LANDED AT TVF W/GEAR DOWN. COMPLETED SEVERAL GEAR SWINGS CND PROBLE M, CLEARED AND VISUALLY INSPECTED UP-LOCK SWITCHES, NO DEFECTS NOTED. 2 L 7 2 4T RT A52EU 2007031300196 20070313 00196 NM 2007 3 13 2007UALA00635 1 20070301 A 3397 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 588UA 26717 EEL FEEDER AT ROW 28 DAMAGED. REPLACED EEL LEAD IN AND OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007031300198 20070313 00198 NM 2007 3 13 AALA20070365 1 20070217 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 379AA 25448 DFW - EMERGENCY LIGHT AT LEFT AFT OVERWING INOP. RELAMPED EMERGENCY LIGHT AT LEFT AFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007031300199 20070313 00199 NM 2007 3 13 AALA20070366 1 20070217 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 379AA 25448 DFW - FOUND EMERGENCY LIGHT AT SEAT 5H INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 5H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007031400006 20070314 00006 2007 3 14 DXTA200702014 4 20070311 A 3140 DISPLAY CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL COCKPIT INOPERATIVE E DXTA A UNSCHED LANDING P G NO WARNING INDICATION MULTIPLE FAILURE CR CRUISE 1 GL 07 905QS 7500105 IN CRUISE NR 1, 2, AND 3 DU'S WENT BLANK WITH RED X'S. NR 1 FMS WENT BLANK. WE SWITCHED TO SG2 AND DU 1, 2, AND 3 CAME BACK WITH RT SIDES INFO. CYAN (FGC A FAIL) AND (FADEC FAULT R-A) WAS OBSERVED IN CAS BOX. THE FADECS WOULD NOT RESET. 30 MINUTES LATER ON APPROACH LT SIDE INFO CAME BACK. GPWS NR 1 FAIL CAS MESSAGE, STAYS ON FROM 1000 FT UNTIL A/C SHUTD OWN. TROUBLESHOT TO PILOT'S SIDE IAC AND REPLACED PILOT'S IAC WITH A SERVICEABLE UNIT. MAINTENANCE IAW CE750 MM CHAPTE R 34-25-01. OPS CHECKS GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007031400008 20070314 00008 CE 2007 3 14 DXTA200702011 1 20070310 A 2760 UNKNOWN RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP AIRBRAKES UNKNOWN E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 816QS 258416 AIRCRAFT ROLLS TO THE RT 2 DEG PER SEC WHEN AIRBRAKES DEPLOYED. DECREASED LT UPPER AIRBRAKE PANEL ANGLE DEFLECTION AND I NCREASED RT UPPER AIRBRAKE PANEL ANGLE DEFLECTION IAW MM 27-61-02. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A3EU E6WE 2007031400012 20070314 00012 NM 2007 3 14 UPS07449286 1 20070303 A 3242 UNKNOWN BOEING 747 747123 1384873 NM ANTI SKID SYS UNKNOWN A IPXA O OTHER O OTHER LD LANDING 1 SO 01 672UP 20324 DURING LANGING GEAR ROLL AT APPROX 95 KNOTS APPLIED MAXIMUM BRAKING EFFORT (BRAKE PEDALS PUSHED TO END OF THROW) AND THE ANTI SKID DID NOT CYCLE. ACCOMPLISHED HYD BRAKE SYS. ADJ/TEST MM 32-41-00. NO FAULT NOTED. ALL SATISFACTORY. CHECK ED CABLE TENSIONS PER MM 32-41-00. CABLE TENSION CHECKED OK. TAXIED AIRCRAFT AND TESTED BRAKES. NO FAULTS NOTED WITH ALL SYSTEMS. 2 L 7 4 4F A20WE 2007031400018 20070314 00018 NM 2007 3 14 UPS07449297 1 20070216 A 5320 FLOOR SUPPORT BOEING 747 747121 1384871 NM BS 1940 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C BULK CARGO COMPT LEFT STA 1940 LBL 55 FLOOR SUPPORT FOUND CORRODED CRACK AS MARKED. CORROSION BLEND O UT 0.025" X .5" X 1" EXCEED SRM 53-10-01 FIG 1 LIMITS. BULK CARGO COMPT FLOOR SUPPORT REPLACED WITH EXISTING SPLICE FRO M BS 1920-1970 LBL 55 PER SRM 51-10-01 PG 9 & INSTALLED PER SRM 51-30-02 REF NRC NO AFQ516607 FOR DETAIL. 2 L 7 4 4F A20WE 2007031400020 20070314 00020 2007 3 14 DXTA200702006 4 20070307 A 3160 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL PITCH FEEL UNKNOWN E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 962QS 7500126 AMBER (PITCH FEEL FAIL) CAME ON DESCENDING OUT OF 4000 FT FOR 3000 FT AUTOPILOT ON 220 KTS: COMPLIED WITH CHECKLIST. A FTER ABOUT 5 MINS OF HAND FLYING. LIGHT WENT OUT JUST PRIOR TO LANDING. COULD NOT DUPLICATE FLIGHT CREWS DISCREPANCY. R AN SYSTEM WITH PITOT/STATIC TEST EQUIPMENT SEVERAL TIMES, OPERATIONALY CHECKS GOOD. IAW: MM 27-30-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007031400021 20070314 00021 NM 2007 3 14 AALA20070374 1 20070220 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 689AA 25731 LAX - SEAT MOUNTED EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACKS M00735 AND M10699 FOR SEAT MOUNTED EME RGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007031400024 20070314 00024 WP 2007 3 14 AALA20070373 1 20070220 A 3260 SENSOR DOUG DC9 DC983 3022083 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 434AA 49452 LAX INFLIGHT T452/20FEB - RED NOSE GEAR LIGHT ILLUMINATED AFTER TAKEOFF. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. SERVICE NOSE STRUT, REPLACED SHRADER VALVE, AND REPLACED D1 NOSE GEAR PISTON SENSOR AND REPACKED LOWER PISTON. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007031400027 20070314 00027 NM 2007 3 14 AALA20070357 1 20070217 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39356 24037 SFO - FOUND EMERGENCY SEAT MOUNTED LIGHTS AT SEATS 4AB INOPERATIVE. RELAMPED EMERGENCY SEAT MOUNTED LIGHTS AT SEATS 4AB . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007031400032 20070314 00032 NM 2007 3 14 AALA20070378 1 20070221 A 3213 162N11222 CYLINDER BOEING 757 757223 1384957 NM NOSE GEAR INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 650AA 24608 DFW INFLIGHT T1276/21FEB - ARRIVED DFW WITH RIGHT NOSE TIRE/WHEEL ASSEMBLY MISSING. PASSENGERS DEPLANED VIA PORTABLE STAIRS AND BUSSED TO TERMINAL. REPLACED NOSE GEAR PISTON AXLE ASSEMBLY, TIRES AND WHEELS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007031400045 20070314 00045 WP 2007 3 14 UPS07849280 1 20070215 A 5310 SAA28920862 SUPPORT ANGLE DOUG DC8 DC871F 302199D WP FS 740 L22R MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C3 MAIN CABIN CENTER WING BOX SUB FLOOR FRAME FITTING SUPPORT ANGLE MISSING AT STA 740 L22R. FABRICATED AND INSTALLED SUPPORT ANGLE IAW SRM 51-3-2, 51-1-20D AND DWG 2892086. 2 L 7 4 4F RT 4A25 2007031400055 20070314 00055 WP 2007 3 14 07FDEA00690 1 20070307 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 FOUND MAIN CARGO COMPARTMENT STA.999 48RBL SEAT TRACK GOUGED. REMOVED AND REPLACED SEAT TRACK SECTION IAW DC/MD SRM 51- 31-01 VOL II PG 1, 53-70--00 VOL1 PG 5, 51-21-01 VOL II PG1-18. 2 L 7 3 4F A22WE 2007031400059 20070314 00059 WP 2007 3 14 07FDEA00694 1 20070307 A 2780 UNKNOWN DOUG MD10 MD1010F 3022112 WP SLAT HANDLE UNKNOWN A FDEA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 25 358FE 46633 ON APPROACH TO TJSJ, SLAT HANDLE WOULD NOT MOVE. FLAPS OPERATE NORMAL AFTER FLAP/SLAT HANDLE SEPARATED. MADE NO SLAT W ITH FLAPS, 22DEG LANDING. GROSS WT OF 346,00 0 LBS. APPROACH SPEED 198. BRAKE LOCKED AFTER CLEARING RUNWAY,WHILE AW AITING GROUND TUG FOR TOW TO RAMP. AFTER TOW A/C TO FEDEX RAMP. VISUALLY INSPECTED SLAT MECHANISM AT PEDESTAL AND CAC. NO DEFECT FOUND, PERFORMED FLAPS/SLATS OPERATION SEVERAL TIMES, SYS CKS NORMAL AT THIS TIME, AS PRECAUTIONARY LUB SLAT ACTUATOR AT CAC. WORK DONE PER MD10-10 AMM 27-00-00-2. 2 L 7 3 4F RT A22WE 2007031400060 20070314 00060 NM 2007 3 14 07FDEA00695 1 20070308 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1481 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 CABIN STA 1481 TO STA 5-33, X = -47.5 SEAT TRACK FOUND CORRODED. (SUPPLEMENTAL 23 MARCH 07) CORRODED SEAT TRACK AT STA 1481 TO STA 5-33, X = -47.5 REPAIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007031400064 20070314 00064 NM 2007 3 14 UPS07449277 1 20070212 A 5347 BAC15201566 SEAT TRACK BOEING 747 747121 1384871 NM BS 400-420 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 400-420 LBL 90 SEAT TRACK I/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.022" X .5" X 10" I S EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 410-460 LBL 90" SEAT TRACK REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 A ND 51-30-02. 2 L 7 4 4F A20WE 2007031400065 20070314 00065 NM 2007 3 14 UPS07449278 1 20070212 A 5347 BAC15201566 CARGO TRACK BOEING 747 747121 1384871 NM BS 480-500 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D LBL 33 BS 480-500 TIE DOWN TRACK I/B FLANGE CORRODED. CORROSION BLEND OUT 0.052" X .5" X 10" EXCE EDS SRM 53-10-01 FIG 1 LIMITS. M/D BS 460-530 LBL 33" TIE DOWN TRACK REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS P ER SRM 51-30-02. 2 L 7 4 4F A20WE 2007031400066 20070314 00066 NM 2007 3 14 UPS07449279 1 20070213 A 5311 FRAME BOEING 747 747121 1384871 NM BS 360 S24-26L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 360 STR 24AL-26L FRAME AFT FACE ATT DOUBLER FOUND CRACK. LENGTH .75 INCH. M/D BS 360 BETWEEN STR 24AL & 27L FRAME AFT FACE ATT DOUBLER REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007031400067 20070314 00067 NM 2007 3 14 UPS07449282 1 20070302 A 3242 BRAKE BOEING 747 747123 1384873 NM MLG STIFF A IPXA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 672UP 20324 BTB - APPLIED MAX BRAKING EFFORT AT 15 KNOTS GROUND SPEED. A/C CAME TO A SLOW GENTLE STOP. BRAKE PEDAL TRAVEL AND RESI STANCE IS INCONSISTANT WITH NORMAL BRAKING FEEL. T/S HYD BRAKE SYS IAW MM 32-41-00. CLEANED AND LUBED CABLE QUADRANTS. OPS CHECK NORMAL. A/C HAS NORMAL RESPONSE METERING VALVES INSTALLED. 2 L 7 4 4F A20WE 2007031400071 20070314 00071 CE 2007 3 14 DXTA200702009 1 20070309 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 344QS 5600344 LITTLE OR NO BRAKE PRESSURE ON RT SIDE (FO SEAT). NO LEAKING FLUID NOTED. BLED SYSTEM SEVERAL TIMES AND REMOVED ALL AI R IN THE SYSTEM IAW MM, CH 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007031400073 20070314 00073 WP 2007 3 14 UPS07849266 1 20070216 A 5311 FRAME DOUG DC8 DC871F 302199D WP FS1040 L35-35L/R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C3 C-PIT STA 1040 FRAME FROM L35L-L35R HAS EXFOLIATION CORROSION. REMOVED DAMAGED AREA OF FRAME CAP AT STA 1040 IAW SRM 51-1-21, AND DWG 53A-011-A. FABRICATED AND INSTALLED REPAIR ANGLE AND STRAP AT STA 1040 FROM L35L-L35R IAW DWG 2537716, DWG DC8-53A-011 AND SRM 51-1-4, 51-1-20D. 2 L 7 4 4F RT 4A25 2007031400074 20070314 00074 NM 2007 3 14 UPS07649302 1 20070303 A 3243 AUTOBRAKE SYS BOEING 767 76734AF 1385212 NM MLG INOPERATIVE A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 316UP 27744 RTO PORTION OF AUTOBRAKES WOULD NOT ENGAGE AFTER PUSHBACK. PERFORMED ANTISKID/AUTOBRAKE SYSTEM INSP/CHECK PER B767 AMM 32-42-00 -6. SYSTEM CHECKED OUT NORMAL. NO FAULTS DETECTED. A/C OK CONTINUE SERVICE IN CAT IIIB. 2 L 7 2 4F RT A1NM 2007031400075 20070314 00075 WP 2007 3 14 UPS07849288 1 20070220 A 5330 SKIN DOUG DC8 DC871F 302199D WP FS1600 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C3 HFEC & VISUAL INSPECTION DETECTED A CRACK ON THE R-2 DOOR FWD UPPER CORNER APPROX .50 INCH IN LENGTH. CUT OUT DAMAGED AREA OF THE R-2 DOOR FWD UPPER CORNER IAW SRM 53-02-00 FIG 16, FABRICATED AND INSTALLED DOUBLER, TRIPL ER, AND FILLER IAW SRM 53-02-00 FIG 16 AND SRM TR 53-197. 2 L 7 4 4F RT 4A25 2007031400076 20070314 00076 NM 2007 3 14 UPS07M49335 1 20070306 A 3350 BATTERY DOUG MD11 MD11F 3023600 NM EMERGENCY LIGHT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 285UP 0832 48457 ON AS-N FOUND EMERGENCY LIGHT BATTERY LOW WARNING DURING EMERGENCY LIGHT TEST. REMOVED AND REPLACED EMERGENCY BATTERY P OWER SUPPLY IAW MM 33-52-01. OPS CHECK NORMAL. 2 L 7 3 4F RT A22WE 2007031400077 20070314 00077 NM 2007 3 14 UPS07549270 1 20070301 A 2910 HYDRAULIC SYSTEM BOEING 757 75724APF 1384969 NM LEFT UNKNOWN A IPXA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 01 423UP 25325 INSPECTION TYPE:N/A DECLARED AN EMERGENCY & DIVERTED TO FWA AFTER RECEIVING LEFT HYD SYS IND. COMPLY WITH REPETITIVE IN SP PER MEL 29-33-2. LEFT HYD QTY IND INOP / INTERMITTENT. PLACED ITEM ON DEFERRAL PER MEL 29-33-2. M345299. REMOVED A ND REPLACED MONITOR UNIT HYD FLUID QTY PER M/M 29-33-51-4. NO FAULTS. THIS CLEARS DEFERRAL M345299. 2 L 7 2 4F RT A2NM 2007031400081 20070314 00081 EA 2007 3 14 SWIA200717976 1 20070213 A 5210 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 705SK 10145 PAX DOOR AFT DRAG ANGLE IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER REO 670-52-11-072. 2 L 7 2 4F RT A21EA 2007031400085 20070314 00085 NM 2007 3 14 07FDEA00734 1 20070309 A 3220 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 NOSE LANDING GEAR, LT TRUNNION FITTING FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5310-105634. STOP DRILL DEVIATION FROM SRM AND SRM 53-40-00 FIG. 22 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007031400088 20070314 00088 EU 2007 3 14 07FDEA00743 1 20070312 A 5310 A53974268200 CROSSBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 FOUND CORROSION ON CROSSBEAMS C56 AND C58. PARTS REPLACED IAW SRM 71-52-10. 2 L 7 2 4F RT A35EU 2007031400091 20070314 00091 WP 2007 3 14 UPS07849341 1 20070226 A 5313 3750257U503 LONGERON SPLICE DOUG DC8 DC873F 302199F WP FS 1050 L31R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C1 LONGERON SPLICE FITTING CRACKED AT STA 1050 L31R. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-3-0 , 51-1-20D. 2 L 7 4 4F RT 4A25 2007031400094 20070314 00094 NM 2007 3 14 UPS07449318 1 20070213 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 960 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 960 RBL 9 TO 11 FLOORBEAM WEB FOUND CRACKED. CRACK LENGTH .75 INCH. M/D FLOORBEAM WEB REPAIRE D AS PER SRM 53-10-07 FIG 11, JUST AT BS 960 BETWEEN RBL 6 AND RBL16 AREA. 2 L 7 4 4F A20WE 2007031400096 20070314 00096 NM 2007 3 14 UPS07449320 1 20070214 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1601 S34R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C AFT CARGO RIGHT STA 1601 S34R STRINGER FOUND CRACKED. CRACK LENGTH .3125 INCH. AFT CARGO COMPT BS 15 90 TO BS 1630 STR 34R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007031400097 20070314 00097 NM 2007 3 14 UPS07449324 1 20070305 A 3231 DOOR BOEING 747 747123 1384873 NM NLG MALFUNCTIONED A IPXA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 672UP 20324 NOSE GEAR DOORS OPENING DURING FLIGHT. REMOVED AND REPLACED NOSE GEAR DOOR SEQUENCE VALVE. OPS CHECK NORMAL. OK FOR C ONTINUED SERVICE. 2 L 7 4 4F A20WE 2007031400103 20070314 00103 WP 2007 3 14 UPS07849322 1 20070220 A 5313 4772397U1 FITTING DOUG DC8 DC873F 302199F WP FS 1763 L17R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C1 CRACK IN END FITTING, L17R, STA 1763, MAIN CABIN. REMOVED L17R END FITTING AT STA 1763 IAW SRM 51-1- 20D. LOCATED, DRILLED UP, AND INSTALLED L17R END FITTING AT STA 1763 IAW SRM 51-3-2, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007031400104 20070314 00104 WP 2007 3 14 UPS07849323 1 20070220 A 5313 4772397U1 FITTING DOUG DC8 DC873F 302199F WP FS 1763 L10R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C1 L10R END FITTING CRACKED AT STA 1763, MAIN CABIN. REMOVED CRACKED END FITTING AT STA 1763 L10R IAW S RM 51-1-20D. LOCATED, DRILLED UP, AND INSTALLED END FITTING AT STA 1763 L10R IAW SRM 51-3-2, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007031400107 20070314 00107 EA 2007 3 14 SWIA200717991 1 20070216 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSLEAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 CABIN FLOOR SUPPORT INBD OF PAX DOOR, 6" FROM AFT OF DOOR IS CORRODED, 5 FASTENER FITTING, DISCOVERED DURING C-CHECK INS PECTION. INSTALLED NEW BRACKETS IAW CRJ200 SRM CH 51-42-06, PG 11, PARA 9. 2 L 7 2 4F RT A21EA 2007031400108 20070314 00108 EA 2007 3 14 SWIA200717992 1 20070216 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 CRACK IN CLIP AT AFT SIDE 280 FLOORBEAM, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP AT SIDE OF 280.0 FLOO RBEAM AND INBD SIDE OF FLOOR SUPPORT RBL-09 PER CRJ200 SRM 51-42-06 PG 4, 51-42-21 PG AND 53-28-00 FIG 11. 2 L 7 2 4F RT A21EA 2007031400109 20070314 00109 EA 2007 3 14 SWIA200717996 1 20070216 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 589 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 FUSE TO INTERCOSTAL ATTACH CLIP CRACKED AT STATION 589.0 UNDER CARGO DOOR SILL FWD SIDE, DISCOVERED DURING C-CHECK INSPE CTION. INSTALLED CLIP AT STA 589 UNDER CARGO DOOR SILL PLATE PER CRJ200 SRM 51-45-00 PG 2, 51-42-21 PG 17, AND 51-42-13 PG 2. 2 L 7 2 4F RT A21EA 2007031400112 20070314 00112 EA 2007 3 14 SWIA200717872 1 20070301 A 2910 LINE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 NM 07 912SW 7595 ON LANDING, LOST ALL HYD FLUID IN NR 2 SYSTEM. REPAIRED NR 2 ENGINE CASE DRAIN RETURN LINE IN AFT EQUIPMENT BAY IAW CRJ MM 20-22-00. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007031400113 20070314 00113 EA 2007 3 14 SWIA200717946 1 20070303 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 438SW 7574 FOUND 1.2" CRACK AT ENGINE SUPPORT BEAM AFT, TOP, MID SECTION OF BEAM DURING AD 2004-10-3/01. FABRICATED AND INSTALLED AN ALUMINUM REPAIR IN THE CRACKED ENGINE SUPPORT BEAM IAW CRJ REO NRS 601R-53-61-345 AND 601R-53-61-368. 2 L 7 2 4F RT A21EA 2007031400114 20070314 00114 EA 2007 3 14 SWIA200717947 1 20070204 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 923SW 7664 PAX DOOR AFT WEB HAS 1.25" CRACK BENEATH COUNTER BALANCE GAS STRUT FRAME, MID DOOR AREA, DISCOVERED DURING C-CHECK INSPE CTION. INSTALLED REPAIR PARTS IAW REO 601R-52-11-702 REV A. 2 L 7 2 4F RT A21EA 2007031400115 20070314 00115 EA 2007 3 14 SWIA200717948 1 20070204 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 923SW 7664 CRACK IN STEP WEB BEHIND FWD HANDRAIL DOWN LOCK SUPPORT BRACKET ON PAX DOOR, DISCOVERED DURING C-CHECK INSPECTION. INST ALLED DOUBLER (-5) REPAIR ANGLES (-8 AND -10) PER REO 670-52-11-104. 2 L 7 2 4F RT A21EA 2007031400116 20070314 00116 EA 2007 3 14 SWIA200717949 1 20070204 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 923SW 7664 FOUND RT AND LT WHEEL WELL BOTH HYDRAULIC PRESSURE TRANSDUCER BRACKETS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. I NSTALLED NEW TRANSDUCER BRACKETS LT AND RT WHEEL WELL PN 601R75262-157 AND 159 AS PER CRJ200 SRM 51-42-06 PGS 11-18. 2 L 7 2 4F RT A21EA 2007031400120 20070314 00120 EA 2007 3 14 SWIA200717953 1 20070204 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 623 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 923SW 7664 CLIP AT FS 623 STR 14 LEFT CRACK, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP AT FS 623 STR 14 LEFT PER CRJ200 SRM 51-42-06 AND 51-42-21. 2 L 7 2 4F RT A21EA 2007031400122 20070314 00122 EA 2007 3 14 SWIA200717955 1 20070207 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 426SW 7468 PAX DOOR STEP 832DT HAS CRACK ON FWD RADIUS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLES AND DOUBLER PER REO 601R-52-11-702 REV A REPAIR ZONE 2 AND CRJ200 SRM 51-42-06,51-42-21 AND 51-23-00. 2 L 7 2 4F RT A21EA 2007031400123 20070314 00123 EA 2007 3 14 SWIA200717956 1 20070207 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 426SW 7664 PAX DOOR STEPS HAVE CRACKS AT STEP 832DT AND 832CT AFT RADIUS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR P ER BOMBARDIER REO 601R-52-11-702 AND CRJ200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007031400124 20070314 00124 EA 2007 3 14 SWIA200717957 1 20070207 A 5210 BRACKET CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 426SW 7468 PAX DOOR PULL-IN MOTOR BRACKET CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SIDE PNL STIFFENER PER CRJ200 5 1-42-06 PG 11. 2 L 7 2 4F RT A21EA 2007031400126 20070314 00126 EA 2007 3 14 SWIA200717979 1 20070305 A 3350 AD20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 457SW 15 15 7773 REAR FACING AFT CEILING LEVEL LIGHTED EXIT SIGN INOP. REPLACED BATTERY PACK. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007031400127 20070314 00127 SO 2007 3 14 SWIA200717980 1 20070228 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS BROKEN A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 298SW 120328 FOUND EMERGENCY EXIT ROW LIGHT/SIGN ON 9B OVERHEAD BIN WILL NOT ILLUMINATE. REPAIRED WIRE ON EMERGENCY EXIT LIGHT AT R OW 9B/C OVERHEAD BIN. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007031400128 20070314 00128 SO 2007 3 14 SWIA200717981 1 20070307 A 2120 UNKNOWN EMB 120 EMB120 3260201 SO CABIN ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 250YV 120250 WITH APU RUNNING AND PACKS SET TO APU, FIRE DETECTOR GOES OFF IN LAV WITH AN OVERHEATED ODOR. UNABLE TO DUPLICATE. 2 L 7 2 4T RT A31SO 2007031400131 20070314 00131 EA 2007 3 14 SWIA200717984 1 20070306 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 719SK 10188 FOUND RIGHT MID FUSELAGE LOWER EMERGENCY LIGHT PLACARD WON`T ILLUMINATE. REPLACED NR 4 EMERGENCY LIGHT BATTERY PACK. O PERATIONAL CHECKS GOOD IAW CRJ 200 MM 33-51-00. 2 L 7 2 4F RT A21EA 2007031400133 20070314 00133 SO 2007 3 14 SWIA200717986 1 20070308 A 3233 2060500005 ACTUATOR EMB 120 EMB120ER 3260203 SO NLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 576SW 11734 11734 120345 AFTER TAKEOFF, NOSE GEAR WOULDN'T RETRACT. RETURNED TO FIELD. REPLACED NOSE GEAR ACTUATOR WITH SERVICEABLE IAW EMB 120 MM CH 37-32-11. OPERATIONAL CHECKS GOOD, PN 20605-000-05, SN/ON B51, SN/OFF 4S. 2 L 7 2 4T RT A31SO 2007031400135 20070314 00135 EU 2007 3 14 UPS07849300 2 20070301 A 7200 ENGINE DOUG DC8 DC873F 302199F WP CFMINT CFM56 CFM562AFR 13802 EU NR 4 FLAMED OUT A IPXA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION NR NOT REPORTED 1 SO 01 852UP 46052 INSPECTION TYPE:N/A AT FL370, NR 4 ENGINE FLAMED OUT. NOTED NR 4 BOOST PUMP OFF. RESTARTED AFTER SECOND ATTEMPT. REMO VED AND REPLACED NR 4 MAIN FUEL FILTER IAW DC8 MM 73-10-02-4. FILTER WAS CLEAN. INSP CHIP DETECTOR IAW DC8 MM 79-20-05 -2. RAN ENG. STARTED AND RAN OK. CHECKED EDP PRESS & IDLE (19 PSI) PER DC8 MM 73-10-01-2. COULD NOT DUPLICATE PROBLE M. 2 L 7 4 4F 4 F RT 4A25 E21EU 2007031400137 20070314 00137 EA 2007 3 14 SWIA200717968 1 20070208 A 5340 ATTACH BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 863AS 7487 FOUND RT STA484 BL27 CLIP CRACKED UPPER RADIUS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIPS AT BL27 AND BL36 PER REO 601R 53-41-059 NOTES 1-4. 2 L 7 2 4F RT A21EA 2007031400138 20070314 00138 EA 2007 3 14 SWIA200717969 1 20070208 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 863AS 7487 625 14L AND 14R CLIPS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CRACKED CLIPS AT 14L & 14R ZONE 625 AS PE R CRJ200 SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007031400142 20070314 00142 NM 2007 3 14 UPS07449305 1 20070213 A 5347 SEAT TRACK BOEING 747 747121 1384871 NM BS 2130-2140 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 2130-2140 LBL 85 SEAT TRACK O/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.029" X .5" X 20" EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 2110-2150 LBL 85" SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2007031500004 20070315 00004 NM 2007 3 15 UPS07M49338 1 20070104 A 5754 SKIN DOUG MD11 MD11F 3023600 NM RT WING LE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE:C RIGHT WING UNDERSIDE FIXED L/E SKIN AT ENG PYLON O/B SIDE FOUND GROOVE CAUSED BY PYLON FAIRING. RIGHT WING UNDERSIDE FIXED L/E SKIN AT ENG PYLON O/B SIDE GROOVE REMOVED ORIG THK 0.063 INCH MATL REMOVED 0.018 INCH MATL REM AIN 0.045 INCH FOUND EXCEED LIMIT PER SRM 57-00-01 FIG 3 VOL 1 REV 38. REWORKED AREA REPROTECTED PER SRM 51-21-01 VOL 2 REV 38. FPI CUT OUT ON REWORKED AREA & FOUND NO CRACK EVIDENT. NEW DOUBLER INSTALLED PER EN1064-07 & SRM 51-35-01 VOL II REV38. 2 L 7 3 4F RT A22WE 2007031500006 20070315 00006 EA 2007 3 15 A6WA200740090 1 20070302 A 2410 HA4A039 RELAY CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ADG DAMAGED A A6WA O OTHER N FALSE WARNING AP APPROACH 1 GL 31 448AW 7814 ON AC SYNOPTIC PAGE, ADG BUSS DISPLAYED IN WHITE. AC1 AND AC2 BUSS SHOW WHITE LINES TO ESS BUSS, ESS BUSS IS GREEN. RE MOVED AND REPLACED ADG ESSENTIAL TRANSFER CONTACTOR (KX2D). PERFORMED OPS CHECK, OPS CHECK GOOD. REF AMM 24-51-31. (K ) 2 L 7 2 4F 4 F RT A21EA E15NE 2007031500007 20070315 00007 NM 2007 3 15 UPS07M49356 1 20070129 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM BS 2140 L45R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE:C RIGHT AFT FX, STA 2140, RIGHT LONGERON 45, FOUND WITH EXFOLIATION CORROSION. FASTENERS & ATTACHING PA RTS REMOVED PER SRM 51-31-01 VIIR38. DAMAGED AREA TRIMMED OFF PER EN1088-07 & REPROTECTED PER SRM 51-21-01VIIR38. HFEC C/O IAW DACNDTSPMR12PT06-10-01.001 NO CRACK. FILLERS & DOUBLERS FAB PER EN1088 -07. INSTALLED PER SRM 51-33-01VIIR38 & EN1088-07. ATTACHED PARTS & FASTENERS INSTALLED PER SRM 51-31-01VIIR38. PAINT TOUCHUP PER SRM 51-21-01VIIR38. 2 L 7 3 4F RT A22WE 2007031500011 20070315 00011 EU 2007 3 15 07FDEA00744 1 20070312 A 5330 SKIN AIRBUS 310 A310324 3930206 EU ZONE 200 UNKNOWN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 OLD DOUBLER REPAIR ON SKIN BETWEEN C73A/C74, P28/29 RT VERIFICATION OF REPAIR, PERFORMED IAW RAS/DAHAM/4018650/2004 ISSU E: A. FOR NEW REQUIREMENTS SEE DR394 (EA6-5318-103411). 2 L 7 2 4F RT A35EU 2007031500013 20070315 00013 EU 2007 3 15 07FDEA00746 1 20070312 A 5312 PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 UNKNOWN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 OLD CORROSION REPAIR ON FRONT PANEL OF NOSE LANDING GEAR BAY. REPAIR VERIFICATION, PERFORMED IAW RAS/AS/073/02 ISSUE: A , EA FOR TRACKING: 6-5312-103346. 2 L 7 2 4F RT A35EU 2007031500014 20070315 00014 CE 2007 3 15 BSAASDR0704 1 20070307 A 3297 G10A22 WIRE BEECH 1900 1900D 1154162 CE MLG CHAFED A BSAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 NM 05 139ZV UE139 WHEN THE GEAR WAS SELECTED DOWN, THE GEAR DIDN'T EXTEND. THE RED GEAR HANDLE LIGHT DIDN'T COME ON & THE GREEN GEAR DOWN LIGHTS DIDN'T COME ON. THE 2AMP GEAR RELAY CONTROL CB WAS FOUND POPPED. THE CREW ABORTED THE LANDING AND DECLARED AN E MERGENCY. EMERGENCY CHECKLIST PROCEDURES WERE FOLLOWED AND THE GEAR WAS MANUALLY PUMPED DOWN WITH NORMAL GEAR DOWN INDI CATIONS. CREW LANDED WITH NO FURTHER INCIDENT. WIRE G10A22 FOR THE LANDING GEAR SERVICE VALVE WAS FOUND CHAFED ON THE EDGE OF THE LANDING GEAR SERVICE PRESSURE RELIEF VALVE ALUMINUM PLACARD PLATE. THE WIRE WAS WITH 5 OTHER WIRES FOR THE S AME SWITCH, COVERED WITH A CLEAR PLASTIC SHEATH AND SPIRAL WRAP. THE EDGE OF THE PLATE CHAFED IN BETWEEN THE SPIRAL WRA 2 L 7 2 4T RT A24CE 2007031500016 20070315 00016 NM 2007 3 15 UPS07449309 1 20070213 A 5340 65B3874422 ATTACH FITTING BOEING 747 747121 1384871 NM BS 960-980 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 960 TO 980 RBL 11 INTERCOSTAL WEB FWD ATT FITTING FOUND CRACKED. CRACK LENGTH .375 INCH. M/D BS 960 TO 980 RBL 11 INTERCOSTAL WEB FWD ATT FITTING REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02 . 2 L 7 4 4F A20WE 2007031500017 20070315 00017 NM 2007 3 15 UPS07449310 1 20070216 A 5320 65B10026136 WEB BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C U/D RIGHT CREW DOOR SILL AREA I/B VERTICAL WEB AND ANGLE FOUND CRACKED. CRACK LENGTH .5 INCH. VERTIC AL WEB AND ANGLE REPLACED PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007031500018 20070315 00018 NM 2007 3 15 UPS07449311 1 20070212 A 5347 SEAT TRACK BOEING 747 747121 1384871 NM BS 1640 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 1640 LBL 11 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.019" X .5" X .5" EXCEE D SRM LIMIT. M/D BS 1590-1690 LBL 11 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14, REFER NRC 50765 FOR DETAIL. 2 L 7 4 4F A20WE 2007031500020 20070315 00020 NM 2007 3 15 UPS07449314 1 20070214 A 5310 RIB BOEING 747 747121 1384871 NM BS 1500-1520 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C AFT CARGO LEFT STA 1500-STA 1520 S34L WEB 3 RIBS DAMAGED AT LOWER EDGE AS MARKED. REPLACED THE 3 RIBS AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007031500021 20070315 00021 NM 2007 3 15 UPS07449315 1 20070214 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1620 S35L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C AFT CARGO LEFT STA 1620 S35L FOUND CORROSION CRACK AS MARKED. CORROSION BLEND OUT 0.030" X .5" X .5" EXCEED SRM LIMIT. AFT CARGO COMPT BS 1610 TO BS 1630 STR 35L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007031500022 20070315 00022 EU 2007 3 15 07FDEA00736 1 20070309 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 409FE 273 SEAT TRACK FOUND WITH DAMAGED "TOOTH" BETWEEN FR 20 AND FR 21 AT Y 2462. REPAIRED IAW FEDEX EA 6-5310-106699. 2 L 7 2 4F RT A35EU 2007031500023 20070315 00023 EU 2007 3 15 07FDEA00737 1 20070309 A 5414 PANEL AIRBUS 310 A310203 3930313 EU ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 409FE 273 NR 1 PYLON, RT SIDE PANEL AT RIB 8 FOUND CRACKED REPAIRED IAW SRM 54-51-31 FIG 201 SHT 1 AND 2. 2 L 7 2 4F RT A35EU 2007031500026 20070315 00026 NM 2007 3 15 07FDEA00740 1 20070311 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 CRACK FOUND AT STRINGER END 20R (XORS 152), APPROX 10" LENGTH ON RT WING TANK, DURING HFEC INSPECTION. REPAIR CARRIED O UT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007031500027 20070315 00027 WP 2007 3 15 UPS07849327 1 20070305 A 3350 BATTERY DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY IAW MM 33-50-01. 2 L 7 4 4F RT 4A25 2007031500028 20070315 00028 NM 2007 3 15 07FDEA00757 1 20070312 A 5313 LONGERON SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 CTR CARGO BILGE AREA LONGERON 49R SPLICE AT STA 1531 SUSPECT CRACKED. CTR CARGO BILGE AREA LONGERON 49R SPLICE AT STA 1 531 REMOVED & REPLACED AS PER SRM 51-33- 01 VOL.II. THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007031500035 20070315 00035 NM 2007 3 15 07FDEA00760 1 20070312 A 5100 TORQUE BOX BOEING 727 727225 1384077 NM BS 1238 UNKNOWN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 462FE 22550 FOUND EXTERNAL DOUBLER, SECTION 48, RT LOWER TORQUE BOX STA 1238, RBL20, WL 183. COMPLIED WITH ATTACHMENT "B" OF EO 7-5 100-7-5005 PT2. 2 L 7 3 4F A3WE 2007031500036 20070315 00036 NM 2007 3 15 07FDEA00761 1 20070312 A 5310 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 CTR CARGO BILGE AREA LONGERON 41L SPLICE AT STA 1531 SUSPECT CRACKED. CTR CARGO BILGE AREA LONGERON 41L SPLICE AT STA 1 531 REMOVED & REPLACED AS PER SRM 51-33- 01 VOL.II. THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007031500037 20070315 00037 NM 2007 3 15 07FDEA00762 1 20070312 A 5714 SKIN DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 FOUND UPPER CARGO COMPARTMENT, CENTER WING UPPER SKIN CORRODED AT STA 1229, RBL 98. COMPLIED WITH FEDEX EA 1-5720-10984 0. CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6- 2-100. 2 L 7 3 4F RT A22WE 2007031500038 20070315 00038 NM 2007 3 15 07FDEA00763 1 20070312 A 5714 SKIN DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 FOUND UPPER CARGO COMPARTMENT, CENTER WING TANK UPPER SKIN CORRODED AT STA 1229, RBL 75. COMPLIED WITH FEDEX EA 1-5720- 109840, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007031500039 20070315 00039 NM 2007 3 15 07FDEA00764 1 20070312 A 5311 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 FOUND UPPER CARGO COMPARTMENT, RT SIDEWALL FRAME AT STA 1701 INNER CHORD DENTED AT L-12R. UPPER CARGO COMPARTMENT, RT S IDEWALL FRAME AT STA 1701 AT L-12R REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG.1 VOL.I. REPETITIVE INSPECTION REQUIRED . INITIAL INSPECTION AT 14500 CYCLES AND THEREAFTER 9500 CYCLES, INSPECTION TO BE CARRIED OUT AS PER SRM 53-30 -00 F IG. 1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. ITEM TRANSFERRED TO OPEN ITEMS LIST CONTROL NR 0311190 . 2 L 7 3 4F RT A22WE 2007031500040 20070315 00040 NM 2007 3 15 07FDEA00765 1 20070312 A 5311 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 FOUND UPPER CARGO COMPARTMENT, RT SIDEWALL FRAME AT STA 1661 INNER CHORD DENTED AT L- 12R. UPPER CARGO COMPARTMENT, RH SIDEWALL FRAME AT STA 1661 INNER CHORD AT L-12R REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG.1 VOL.I. REPETITIVE INSPECTIO N REQUIRED - INITIAL INSPECTION AT 14500 CYCLES AND THEREAFTER 9500 CYCLES, INSPECTION TO BE CARRIED OUT AS PER SRM 53 -30 -00 FIG. 1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. ITEM TRANSFERRED TO OPEN ITEMS LIST CONTRO L NO. 0311189. 2 L 7 3 4F RT A22WE 2007031500041 20070315 00041 NM 2007 3 15 07FDEA00766 1 20070312 A 5100 TORQUE BOX BOEING 727 727225 1384077 NM BS 1237 UNKNOWN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 462FE 22550 FOUND EXTERNAL DOUBLER, SECTION 48, RT LOWER TORQUE BOX STA 1237, RBL 20, WL 189. COMPLIED WITH ATTACHMENT "B" OF EO 7- 5100-7-5005 PT2, MAJOR REPAIR. 2 L 7 3 4F A3WE 2007031500042 20070315 00042 NM 2007 3 15 07FDEA00767 1 20070312 A 5311 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 FOUND UPPER CARGO COMPARTMENT, LT SIDEWALL FRAME AT STA 1701 INNER CHORD DENTED AT L- 12L. UPPER CARGO COMPARTMENT, LT SIDEWALL FRAME AT STA 1701 AT L-12L REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG.1 VOL.I. REPETITIVE INSPECTION REQUIRED - INITIAL INSPECTION AT 14500 CYCLES AND THEREAFTER 9500 CYCLES, INSPECTION TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. 1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. ITEM TRANSFERRED TO OPEN ITEMS LIST CONTROL NR 0311188 . 2 L 7 3 4F RT A22WE 2007031500043 20070315 00043 NM 2007 3 15 07FDEA00768 1 20070312 A 5311 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 FOUND UPPER CARGO COMPARTMENT, LT SIDEWALL FRAME AT STA 1681 DENTED AT L- 12L. UPPER CARGO COMPARTMENT, LT SIDEWALL FR AME AT STA 1681 AT L-12L REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG.1 VOL.I. REPETITIVE INSPECTION REQUIRED - INITIA L INSPECTION AT 14500 CYCLES AND THEREAFTER 9500 CYCLES, INSPECTION TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. 1 V OL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. ITEM TRANSFERRED TO OPEN ITEMS LIST CONTROL NR 031191 2 L 7 3 4F RT A22WE 2007031500044 20070315 00044 NM 2007 3 15 07FDEA00769 1 20070312 A 5311 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 FOUND UPPER CARGO COMPARTMENT, LT SIDEWALL FRAME AT STA 1641 INNER CHORD DENTED AT L-12L. UPPER CARGO COMPARTMENT, LH S IDEWALL FRAME AT STA 1641 AT L-12L. REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG.1 VOL.I. REPETITIVE INSPECTION REQUIRED - INITIAL INSPECTION AT 14500 CYCLES AND THEREAFTER 9500 CYCLES, INSPECTION TO BE CARRIED OUT AS PER SRM 53-30 - 00 FIG. 1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. ITEM TRANSFERRED TO OPEN ITEMS LIST CONTROL NR 0311192. 2 L 7 3 4F RT A22WE 2007031500045 20070315 00045 NM 2007 3 15 SWAA071315 1 20070310 A 3350 079123 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 241WN 32504 EEPLS LENS LOOSE AT FWD END. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007031500046 20070315 00046 NM 2007 3 15 SWAA071317 1 20070309 A 5330 6523693 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 251.5, STR 24L. REPAIRED SKIN PER SWA EA & SRM. 2 L 7 2 4F RT A16WE 2007031500048 20070315 00048 NM 2007 3 15 SWAA071320 1 20070311 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 791 S17L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 791, STR 17L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007031500049 20070315 00049 NM 2007 3 15 SWAA071321 1 20070311 A 5330 6545775 SKIN BOEING 737 737317 138447P NM BS 420 S17R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 420, STR 17R. REPAIRED SKIN PER SWA EA & SRM. 2 L 7 2 4F RT A16WE 2007031500050 20070315 00050 NM 2007 3 15 SWAA071336 1 20070312 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031500051 20070315 00051 NM 2007 3 15 SWAA071334 1 20070312 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM BS 520 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031500052 20070315 00052 NM 2007 3 15 SWAA071323 1 20070312 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM BS 520 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031500053 20070315 00053 NM 2007 3 15 SWAA071326 1 20070312 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031500054 20070315 00054 NM 2007 3 15 SWAA071328 1 20070312 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031500055 20070315 00055 NM 2007 3 15 SWAA071327 1 20070312 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031500056 20070315 00056 NM 2007 3 15 SWAA071329 1 20070312 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM BS 867 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031500057 20070315 00057 NM 2007 3 15 SWAA071332 1 20070312 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031500058 20070315 00058 NM 2007 3 15 SWAA071324 1 20070312 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM BS 727B S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031500059 20070315 00059 NM 2007 3 15 07FDEA00770 1 20070312 A 5311 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 FOUND UPPER CARGO COMPARTMENT, RT SIDEWALL FRAME AT STA 1761 INNER CHORD DENTED AT L-12R. UPPER CARGO COMPARTMENT, RH S IDEWALL FRAME AT STA 1761 INNER CHORD DENTED AT L-12R REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG.1 VOL.I. REPETITIVE INS PECTION REQUIRED. INITIAL INSPECTION AT 14500 CYCLES AND THEREAFTER 9500 CYCLES, INSPECTION TO BE CARRIED OUT AS PER SR M 53-30-00 FIG. 1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. ITEM TRANSFERRED TO OPEN ITEMS LIST CONTRO L NR 0311193. 2 L 7 3 4F RT A22WE 2007031500060 20070315 00060 NM 2007 3 15 07FDEA00771 1 20070312 A 5310 TORQUE BOX BOEING 727 727225 1384077 NM BS 1227 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 EXTERNAL DOUBLER SECTION 48, RT LOWER TORQUE BOX, ATA 1227.5,RBL 20, WL 190. COMPLY WITH ATTACHMENT "B" OF EO 7-5100- 7-5005 PT2. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR. 2 L 7 3 4F A3WE 2007031500061 20070315 00061 NM 2007 3 15 07FDEA00772 1 20070312 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 1050-1070 UNKNOWN A FDEA K NONE O OTHER NR NOT REPORTED 1 SO 25 462FE 22550 AFT PIT FUSE STRINGER REPAIR, STA 1050- 1070,S20R. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR. 2 L 7 3 4F A3WE 2007031500062 20070315 00062 NM 2007 3 15 07FDEA00773 1 20070312 A 5100 STRINGER BOEING 727 727225 1384077 NM UNKNOWN A FDEA K NONE O OTHER NR NOT REPORTED 1 SO 25 462FE 22550 AFT PIT, FUSE STRINGER REPAIR, STA 1070- 1090,S20R. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR. 2 L 7 3 4F A3WE 2007031500063 20070315 00063 NM 2007 3 15 07FDEA00774 1 20070312 A 5100 STRINGER BOEING 727 727225 1384077 NM UNKNOWN A FDEA K NONE O OTHER NR NOT REPORTED 1 SO 25 462FE 22550 AFT PIT, FUSE STRINGER REPAIR STA 1130- 1166,S29. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR. 2 L 7 3 4F A3WE 2007031500064 20070315 00064 NM 2007 3 15 07FDEA00775 1 20070312 A 5100 FRAME BOEING 727 727225 1384077 NM UNKNOWN A FDEA K NONE O OTHER NR NOT REPORTED 1 SO 25 462FE 22550 FOUND AFT PIT FRAME REPAIR STA 950, ABOVE S24L TO S25L. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REP AIR. 2 L 7 3 4F A3WE 2007031500065 20070315 00065 NM 2007 3 15 07FDEA00776 1 20070312 A 5100 FRAME BOEING 727 727225 1384077 NM UNKNOWN A FDEA K NONE O OTHER NR NOT REPORTED 1 SO 25 462FE 22550 FOUND AFT PIT FRAME REPAIR, STA 970, ABOVE S23L TO S24L. COMPLY WITH ATTACHMENT "B" OF EO 7- 5100-7-5005 PT2. COMPLIE D WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR. 2 L 7 3 4F A3WE 2007031500067 20070315 00067 EU 2007 3 15 07FDEA00782 1 20070313 A 5315 A53773651210 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CORROSION ON TOP CAP BEAM, UPPER FLANGE, C25 AD. REPAIR WAS PERFORMED IAW SRM 53-10-15, FIG 207 AND SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007031500068 20070315 00068 EU 2007 3 15 07FDEA00783 1 20070313 A 5310 CROSSBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 813FD 500 OLD CROSSBEAM REPAIR AT C62 WHICH IS NOT CONFORM TO THE SRM. REPAIR PERFORMED IAW SRM 53-10-15, FIG 207, PERFORMED WITH FOLLOW DR511. 2 L 7 2 4F RT A35EU 2007031400087 20070314 00087 EU 2007 3 14 07FDEA00742 1 20070312 A 5340 A53773405200 STRINGER CLIP AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 FOUND CLIP AT FRAME 22 AD HEAVY CORRODED. NEW PART INSTALLED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007031400089 20070314 00089 WP 2007 3 14 UPS07849339 1 20070220 A 5340 3779659U501 FITTING DOUG DC8 DC873F 302199F WP FS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C1 MAIN CABIN FWD OF THE 857.123 L6L END FITTING CRACKED. REMOVED AND REPLACED END FITTING IAW SRM 51-1 -20D AND 51-3-0. 2 L 7 4 4F RT 4A25 2007031400090 20070314 00090 WP 2007 3 14 UPS07849340 1 20070220 A 5340 SAA577384443 BRACKET DOUG DC8 DC873F 302199F WP FS 1766 L6L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C1 APB BRACKET CRACKED STA 1766 L6L MAIN CABIN. REMOVED, FABRICATED AND INSTALLED APB BRACKET IAW SRM 5 1-1-21, 51-1-2 0D AND DWG 5773844. 2 L 7 4 4F RT 4A25 2007031400092 20070314 00092 NM 2007 3 14 UPS07449316 1 20070215 A 5320 SUPPORT BOEING 747 747121 1384871 NM BS 2080-1260 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C BULK CARGO COMPT RIGHT SLOPE PANEL SUPPORT SEVERAL LOCATION CORROSION AT STA 2080 TO STA 2160 RBL 60 A NCHOR NUT AREA. CORROSION BLEND OUT 0.026" X 1" X 1" EXCEED SRM LIMIT. BULK CARGO COMPT BS 2040 - 2160 RBL 60 SLOPE PA NEL SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007031400095 20070314 00095 NM 2007 3 14 UPS07449319 1 20070216 A 5320 65B091911 SUPPORT FITTING BOEING 747 747121 1384871 NM BS 980 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C FWD CARGO COMPT AFT FIXED END STOP SUPPORT FITTING FOUND CRACK AT STA 980 RBL 45. CRACK LENGTH .75 IN CH. FWD CARGO COMPT AFT FIXED END STOP SUPPORT FITTING REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30 -02, JUST AT STA 980 RBL 45. 2 L 7 4 4F A20WE 2007031400098 20070314 00098 NM 2007 3 14 UPS07449325 1 20070305 A 3350 LIGHT BOEING 747 747200 1384847 NM ESCAPE SLIDE INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP AT ESCAPE SLIDE DOOR FRAME AND EXIT SIGN ABOVE SLIDE. REMOVED AND REPLACED PO WER SUPPLY MODULE FOR EXIT SIGN PER MM 33-51-04. EXIT SIGN OPS CHECKS NORMAL. LIGHTS IN ESCAPE DOOR FRAME STILL INOP. NEEDS MODULE X327, RELAMPED IAW MM-33-51-05. OPS IAW MM 33-51-00. OPS NORMAL OK FOR SERVICE. 2 L 7 4 4F RT A20WE 2007031400099 20070314 00099 NM 2007 3 14 UPS07449330 1 20070213 A 5347 SEAT TRACK BOEING 747 747121 1384871 NM BS 1520-1530 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D STA 1520-1530 RBL 96 SEAT TRACK I/B FLANGE CORRODED. CORROSION BLEND OUT 0.035" X .5" X 1" EXCEED SRM 53-10-09 FIG 1, LIMITS. M/D BS 1480-1570 RBL 96 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2007031400100 20070314 00100 NM 2007 3 14 UPS07549301 1 20070216 A 5311 146N100527 FRAME BOEING 757 75724APF 1384969 NM BS 1280 S26L DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 461UP 28265 INSPECTION TYPE:C DENT IN AFT CARGO FRAME STA 1280, S26L. REPAIRED PER FINAL EA 757-5362-27-A1608 AND UPS EO B757-5310- 262 69-A. 2 L 7 2 4F RT A2NM 2007031400101 20070314 00101 NM 2007 3 14 UPS07549328 1 20070305 A 3350 POWER SUPPLY BOEING 757 75724APF 1384969 NM EMERGENCY LIGHT NO TEST A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 433UP 25464 INSPECTION TYPE:N/A EMERGENCY LIGHTS TEST FAILED PER PS CK STEP 15 G. REPLACED POWER SUPPLY IAW AMM 33-51-07-2. 2 L 7 2 4F RT A2NM 2007031400102 20070314 00102 NM 2007 3 14 UPS07649333 1 20070306 A 2910 O-RING BOEING 767 76734AF 1385212 NM HYD FILTER LEAKING A IPXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 308UP 27761 CREW REPORTED VIA ACARS, LOSING HYDRAULIC QUANTITY IN THE CENTER SYSTEM. C-HYD QUANTITY DECREASED TO .09 ON ARRIVAL. R EPLACED FILTER PLUG O-RING ON NR 10 ACTUATOR. LEAK CHECK OK. 2 L 7 2 4F RT A1NM 2007031400105 20070314 00105 EA 2007 3 14 SWIA200717988 1 20070227 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 763SK 10228 PAX DOORS FWD WEB 2ND & 3RD TOP STEP RADIUS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER PER 670-52 -11-104 IN CONJUNCTION WITH DEVIATION REO 670-52-11-252. 2 L 7 2 4F RT A21EA 2007031400106 20070314 00106 EA 2007 3 14 SWIA200717989 1 20070227 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 763SK 10228 PAX DOOR AFT WEB TOP STEP AND MIDSTEP RADIUS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. COMPLIED WITH REO 670-52-11 -104. 2 L 7 2 4F RT A21EA 2007031400110 20070314 00110 EA 2007 3 14 SWIA200717997 1 20070216 A 5300 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA BS 654 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 AFT EQUIP BAY AT FS 654.50 STR12R CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP AT FS 654.50 STR 12 IAW CRJ200 SRM 51-42-20 PG 23. 2 L 7 2 4F RT A21EA 2007031400111 20070314 00111 EA 2007 3 14 SWIA200717998 1 20070216 A 5420 ANGLE CNDAIR CL600 CL6002B19 1900309 EA RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 RT PYLON, THERE IS A CRACK IN THE LWR PYLON STRUCTURE AT FS 605, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FORMED ANGLE REPAIR AT RT PYLON LOWER PYLON SECONDARY STRUCTURE SUPPORT ANGLE PER CRJ200 51-71-59 PG 2 SEC 2A. 2 L 7 2 4F RT A21EA 2007031400117 20070314 00117 EA 2007 3 14 SWIA200717950 1 20070204 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 923SW 7664 FS 280 CRACKED ANGLE CLIP AT LH BL9, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP AS PER CRJ200 SRM 51-42-2 1. 2 L 7 2 4F RT A21EA 2007031400118 20070314 00118 EA 2007 3 14 SWIA200717951 1 20070204 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 923SW 7664 FS 280 CRACKED ANGLE CLIP AT RT BL9, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP AS PER CRJ200 SRM 51-42-2 1. 2 L 7 2 4F RT A21EA 2007031400119 20070314 00119 EA 2007 3 14 SWIA200717952 1 20070204 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 923SW 7664 FS 280 BEAM HAS CRACK AT RT BL9, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER, FILLER AND CLIP PER REO 601R- 53-11-171 REV (C). 2 L 7 2 4F RT A21EA 2007031400121 20070314 00121 EA 2007 3 14 SWIA200717954 1 20070204 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 625 S14R CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 923SW 7664 CLIP AT FS 625 STR 14R IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP AT STA 625.0 STR 14R PER CR J200 SRM 51-42-21 PGS 15-17. 2 L 7 2 4F RT A21EA 2007031400129 20070314 00129 EA 2007 3 14 SWIA200717982 1 20070308 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A SWIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 07 865AS 7507 FOUND CRACK ON TOP OF MAIN ENG SUPPORT BEAM BELOW LEFT CARGO FIRE BOTTLE ON RIGHT CORNER OF FIRE DETECTION LOOP BRACKET, DISCOVERED DURING SERVICE CHECK INSPECTION. TEMPORARILY REPAIRED WITH DOUBLER IAW CRJ REO 601R-53-61-2093 . 2 L 7 2 4F RT A21EA 2007031400130 20070314 00130 EA 2007 3 14 SWIA200717983 1 20070310 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT FAILED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 945SW 7770 FOUND ROW 8 AND AFT EMERGENCY FLOOR LIGHTING STRIP OUT. REPLACED POWER STRIP ON EMERGENCY LIGHT FLOOR STRIP ROW 8 AND B ACK IAW CRJ AMM 33-51-01. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007031400132 20070314 00132 SO 2007 3 14 SWIA200717985 1 20070309 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENC Y LIGHT DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 298SW 13014 13014 120328 FOUND FORWARD EMERGENCY LIGHT BATTERY PACK IS DEAD. REPLACED FORWARD EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007031400134 20070314 00134 WP 2007 3 14 UPS07849289 1 20070217 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FS 1580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C3 HEAVY CORROSION ON TOP OF FLOORBEAM AFT ACCY COMPT STA 1580 RBL 50-60, FWD SIDE. CUT OUT CORRODED AR EA ON FLOORBEAM AT STA 1580 RBL 50-60 IAW SRM TR 51-2-1. FABRICATED AND INSTALLED REPAIR FILLER, REPAIR ANGLES AND SPLI CE ANGLES IAW SRM TR 51-2-1. 2 L 7 4 4F RT 4A25 2007031400136 20070314 00136 EA 2007 3 14 SWIA200717967 1 20070208 A 5340 ATTACH BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 863AS 7487 FOUND LT STA484 BL27 AND BL36 CLIPS CRACKED UPPER RADIUS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE, CLIP A ND PULLEY GUIDE PER REO 601R 53-41-059. 2 L 7 2 4F RT A21EA 2007031400139 20070314 00139 EA 2007 3 14 SWIA200717970 1 20070208 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 863AS 7487 RT MLG WHEEL WELL BRAKE TRANSDUCER BRACKET CRACKED BROKEN ON TOP MID AREA OF WHEEL WELL, DISCOVERED DURING C-CHECK INSPE CTION. INSTALLED NEW PART PER CRJ200 SRM 51-42-06 PG 1-3, 15-17. 2 L 7 2 4F RT A21EA 2007031400140 20070314 00140 NM 2007 3 14 UPS07449303 1 20070216 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 360-380 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 380 S14EL FOUND CRACK. CRACK LENGTH .25 INCH. M/D BS 360-380 STRINGER S14EL REPLACED AS PER S RM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007031400141 20070314 00141 NM 2007 3 14 UPS07449304 1 20070214 A 5320 INTERCOSTAL BOEING 747 747121 1384871 NM BS 2220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 2220 RBL 58 INTERCOSTAL WEB VERTICAL ANGLE FOUND CRACKED. CRACK LENGTH .5 INCH. M/D BS 2220 R BL 58 INTERCOSTAL WEB VERTICAL ANGLE REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007031400143 20070314 00143 NM 2007 3 14 UPS07449306 1 20070214 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1650 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C AFT CARGO RIGHT STA 1650 S38R STRINGER FOUND CRACK. CRACK LENGTH .375 INCH. AFT CARGO COMPT BS 1630 TO BS 1650 STR 38R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007031400144 20070314 00144 NM 2007 3 14 UPS07449307 1 20070214 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1650 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C AFT CARGO - RIGHT STA 1650 S37R STRINGER FOUND CRACKED. CRACK LENGTH .375 INCH. AFT CARGO COMPT BS 1 630 TO BS 1670 STR 37R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007031500002 20070315 00002 WP 2007 3 15 UPS07849343 1 20070220 A 5410 SAA5801007508 ATTACH FITTING DOUG DC8 DC871F 302199D WP NR 4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C3 1ST CLIP FROM FWD C/S IS CRACKED NR 4 PYLON O/B SKATE ANGLE. REMOVED, FABRICATED AND INSTALLED CLIP IAW SRM 51-1-20D, DWG 5804007. 2 L 7 4 4F RT 4A25 2007031500003 20070315 00003 WP 2007 3 15 UPS07849344 1 20070212 A 5730 561134017 SKIN DOUG DC8 DC871F 302199D WP XFS 107 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C3 LEFT WING UPPER SKIN 1 INCH CRACK AT XRS 107.000 UPPER FRONT SPAR SKIN. REPAIRED UPPER WING SKIN AT XRS 107.000 FRONT SPAR IAW SAA EA 008-5710-01-A0685 AND UPS RAA DC8-57-20211. 2 L 7 4 4F RT 4A25 2007031500005 20070315 00005 NM 2007 3 15 UPS07M49355 1 20070126 A 5730 ARB75582 SKIN DOUG MD11 MD11F 3023600 NM RT WING CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE:C RIGHT WING TOPSIDE FIXED L/E XORS 1093.629 CANTED AREA FOUND CHAFE MARK. AREA SMOOTHEN MATL REMAIN 0. 083 EXCEED LIMIT PER SRM 57-00-01 FIG 3 VIR38. L/E SKIN REMOVED PER SRM 51-33-01VIIR38. TRIMMED OUT PER EN1085-07. HF EC C/O PER NDTSPMR1206-10-01.001 NO CRACK. NEW SKIN FAB PER EN. HEAT TREATED PER DPS7.00-1 & HRB54.7 PER DPS1.05-3 & E N. SKIN WELD PER EN SH1OF3 1TO6. FPI C/O PER NDTSPMR12PT08 NO CRACK. REINSTALLED PER SRM 51-33-01 VIIR38. 2 L 7 3 4F RT A22WE 2007031500010 20070315 00010 NM 2007 3 15 UPS07M49361 1 20070118 A 5330 SKIN DOUG MD11 MD11F 3023600 NM BS 2140 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE:C AFT BODY (RIGHT), EXTENDED SKIN, STA 2140 (FWD OF APU EXHAUST DOOR) FOUND CORRODED. AFT FX RIGHT STA 2140 FWD OF APU EXHAUST DOOR, CORRODED EXTERIOR SKIN REPAIR CARRIED OUT AS PER EN1067-07. 2 L 7 3 4F RT A22WE 2007031500012 20070315 00012 EU 2007 3 15 07FDEA00745 1 20070312 A 5347 A5381314100000 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU BS 3407-3460 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 669FE 774 CABIN SEAT TRACK CORRODED BETWEEN FR 54.1 AND 54.2 LBL18 REMOVED CORROSION ON SEAT TRACK FOUND TO BE OUT OF LIMITS IAW A 300-600 SRM 53-10-16 FIG 102. REMOVED CORRODED (DAMAGED) SEAT TRACK, RECEIVED NEW SEAT TRACK SECTION AND INSTALLED IA W A300-600 SRM 51-40-21 MINOR REPAIR PO 564077.5. 2 L 7 2 4F RT A35EU 2007031500015 20070315 00015 NM 2007 3 15 UPS07449308 1 20070214 A 5410 65B90468911 BAFFLE BOEING 747 747121 1384871 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C NR 2 PYLON NAC STA 180 VERT FLANGE L/R LOWER CLEATS BROKEN AND CRACKED. CRACK LENGTH .375 INCH. NR 2 PYLON NAC STA 180 VERTICAL BAFFLE AND CLEATS REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007031500019 20070315 00019 NM 2007 3 15 UPS07449312 1 20070212 A 5347 SEAT TRACK BOEING 747 747121 1384871 NM BS 1595 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 1595 LBL 11 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.025" X .5" X 1" EXCEED SRM LIMIT. M/D BS 1590-1690 LBL 11 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14. 2 L 7 4 4F A20WE 2007031500024 20070315 00024 EU 2007 3 15 07FDEA00738 1 20070310 A 5210 SKIN AIRBUS 310 A310203 3930313 EU ZONE 800 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 409FE 36674 273 PREVIOUS REPAIR FOUND LOCATED ON LOWER SECTION OF NR 2 RT DOOR. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATIO N AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN E XISTEING SRM REPAIR. NEW REPAIR ACCOMPLISHED IAW SRM 52-10-00, FIG 204. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIE D AS MAJOR. 2 L 7 2 4F RT A35EU 2007031500025 20070315 00025 EU 2007 3 15 07FDEA00739 1 20070310 A 2910 UNKNOWN AIRBUS 300 A300F4605R 3930327 EU HYD SYSTEM UNKNOWN A FDEA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 25 674FE 781 IN FLIGHT ECAM GREEN HYD SYS LO PRESS WARNING GREEN FLUID LEVEL ON OVERHEAD AND ECAM INDICATED TOTAL FLUID LOSS. COMPLI ED WITH QRH. CRANKED GEAR. AT SOME TIME AFTER GEAR DOWN, FLUID GAGE INDICATED NORMAL. TUGGED IN BLUE AND YELLOW FLUID GAGES SHOWED OVERSERVICED BEFORE BLOCKOUT. MEM MX SAID AIR IN SYSTEM AND SHOULD CLEAR, IT DID. BLEED ALL 3 HYD SYSTEM PER A300-600 AMM 29-00-00-4. RESERVICED ALL 3 SYSTEMS PER A300-600 AMM 29-00-00-3 AND 12-12-29-0. RAN ENGINES PER F DX JRH AND OPERATED ALL FLIGHT CONTROLS NO ABNORMAL INDICATIONS IN FLIGHT DECK AT THIS TIME. REFER TO WRI 29-30-8090 F OR MOCC CONFERENCE CALL WITH MGMT. 2 L 7 2 4F RT A35EU 2007031500029 20070315 00029 WP 2007 3 15 UPS07849329 1 20070306 A 3350 LIGHT DOUG DC8 DC873F 302199F WP COCKPIT ILLUMINATED A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 852UP 46052 INSPECTION TYPE:N/A DURING FLIGHT - EMERGENCY LIGHTS ILLUMINATED, UNABLE TO RESET. TRIED RESETTING ALL 3 CIRCUIT BREAKE RS WITHOUT SUCCESS, TURNED EMERGENCY LIGHTS TO DISARM THEN OFF. RESET EMERGENCY EXIT LIGHT CONTROL C/B, ELIMINATED DISC REPANCY. ALL SYSTEMS NORMAL. 2 L 7 4 4F RT 4A25 2007031500030 20070315 00030 2007 3 15 UPS07849334 4 20070306 A 2565 GIRT BAR DOUG DC8 DC871F 302199D WP ESCAPE SLIDE MALFUNCTIONED A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 772UP 46072 INSPECTION TYPE:N/A GIRT BAR WILL NOT LATCH IN PLACE TO ARM THE SLIDE CHUTE WHEN DOOR IS CLOSED. REPOSITIONED SLIDE ON DOOR PER MM 25-60-00. OPS CHECK OK. 2 L 7 4 4F RT 4A25 2007031500032 20070315 00032 NM 2007 3 15 UPS07M49326 1 20070306 A 3350 6044115 BATTERY PACK DOUG MD11 MD11F 3023600 NM EMERGENCY LIGHTS DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 285UP 48457 INSPECTION TYPE:N/A EMERGENCY LIGHT BATTERY 1 LOW WARNING (LVL 1) PRESENT DURING EMERGENCY LIGHT TEST (PREFLIGHT). T/S AS PER FIM 33-51-02-00, FOUND POWER SUPPLY FAULTY. REMOVED AND REPLACED FAULTED BATTERY, EMERGENCY LIGHT OPS CHECKED SA TISFACTORY PER MM 33-51-01-4. 2 L 7 3 4F RT A22WE 2007031500033 20070315 00033 NM 2007 3 15 07FDEA00758 1 20070312 A 5313 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 CTR CARGO BILGE AREA LONGERON 43L SPLICE AT STA 1531 SUSPECT CRACKED. CTR CARGO BILGE AREA LONGERON 43L SPLICE AT STA 1 531 REMOVED & REPLACED AS PER SRM 51-33- 01 VOL.II. THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007031500034 20070315 00034 NM 2007 3 15 07FDEA00759 1 20070312 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 CTR CARGO BILGE AREA LONGERON 44L SPLICE AT STA 1531 SUSPECT CRACKED. CTR CARGO BILGE AREA LONGERON 44L SPLICE AT STA 1 531 REMOVED & REPLACED AS PER SRM 51-33- 01 VOL.II. THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007031500083 20070315 00083 NM 2007 3 15 07FDEA00801 1 20070313 A 5280 6521636159 STRUCTURE BOEING 727 727225 1384077 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FOUND LMLG WING DOOR LWR AFT EDGE ANGLE IS CRACKED. REPAIRED LMLG WING DOOR LWR AFT EDGE ANGLE REF SRM 51-40-3 FIGURE 1 . 2 L 7 3 4F A3WE 2007031500084 20070315 00084 EU 2007 3 15 07FDEA00802 1 20070313 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 412FE 360 MDCC SEAT TRACK 5L GOUGED BLENDED GOUGES IAW A310-200 SRM 51-74-10. FOUND TO BE IN LIMITS. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2 L 7 2 4F RT A35EU 2007031500085 20070315 00085 EU 2007 3 15 07FDEA00803 1 20070313 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 412FE 360 MDCC SEAT TRACK 3L GOUGED CUT OUT AND REPLACED GOUGED SECTION OF SEAT TRACK. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2 L 7 2 4F RT A35EU 2007031500086 20070315 00086 EU 2007 3 15 07FDEA00805 1 20070313 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 669FE 774 MAIN CABIN SEAT TRACK CORRODED OVER FS 15A AT BL Y593 REMOVED CORROSION IAW A300-600 SRM 51-74-10, SEAT TRACK FOUND TO B E OUT OF LIMITS IAW A300-600 SRM 53-10-16 FIG 101. REMOVED AND REPLACED SEAT TRACK P/N A53612524200 IAW A300-600 SRM 51 -40-21, PO 565252.1. 2 L 7 2 4F RT A35EU 2007031500092 20070315 00092 NM 2007 3 15 SWAA071316 1 20070309 A 3350 BULB BOEING 737 7373Q8 1384670 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT BULBS INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2007031500093 20070315 00093 NM 2007 3 15 SWAA071331 1 20070312 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500C S25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 25R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007031500094 20070315 00094 NM 2007 3 15 SWAA071318 1 20070311 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 482WN 29852 DURING SCHEDULED MV2 CHECK, FOUND EEPLS BROKEN AT FWD END. RELAMPED AND REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007031500095 20070315 00095 2007 3 15 SWAA071314 4 20070311 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 L2 DOOR EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2007031500118 20070315 00118 NM 2007 3 15 2007UALA00642 1 20070304 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 277-360 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 364UA 24533 FWD CABIN AREA RIGHT CREASE BEAM CHORD IS CORRODED FROM BS 277 TO BS 360 STR 17R, WL 208. *S/D* MAJOR REPAIR: REPLACE D CREASE BEAM REF SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2007031500119 20070315 00119 NM 2007 3 15 2007UALA00643 1 20070305 A 5740 FITTING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE WING CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 119UA 28812 CORROSION - BOTH BORES OF THE DSB UNDERWING FITTING AT NUMBER 4 NACELLE STRUT ATTACH AREA. ACCOMPLSHED BORING OF THE D UAL SIDE BRACE UNDERWING FITTING AT NUMBER 4. BOTH HOLES PER BOEING SB 747-54A2218 (FINAL HOLE DIA AFTER HONE = 2.2450). SUSPECT CORROSION RESULT OF COMBINATION OF HEAT IN SVCE & CONDENSATION IN NACELLE-PYLON AREA. 2 L 7 4 4F 4 F RT A20WE E24NE 2007031500120 20070315 00120 NM 2007 3 15 2007UALA00644 1 20070302 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LAVATORY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 530UA 25043 EEL LIGHT BAR AT THE MID LAV IS INOPERATIVE. REPAIRED EEL LIGHT BAR AT MID LAV. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007031500121 20070315 00121 NM 2007 3 15 2007UALA00645 1 20070303 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 540UA 25252 NOTICED BURNING PLASTIC ODOR ON DESCENT OUT OF 240. TURNING OFF RIGHT RECIRC FAN NO CHANGE. PER CREW, ODOR IN FLT DECK AREA, WENT AWAY AT APPROX 8000 FT. [SUP 05-18-07] CHECKED MEC FOR ELEC MODULE FAULTS OR ODOR IN AREA AND NONE FOUND. CHECKED WINDOW HEAT CONNECTIONS FOR EVIDENCE OF LOOSE OR OVERHEATING AND ALL CHECKED OK. NO PROTECTIVE CAPS MELTED. NO E ICAS MESSAGES FOUND. RIGHT HALF OF THE VNAV SWITCH IS BURNED OUT. RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007031500122 20070315 00122 NM 2007 3 15 2007UALA00646 1 20070302 A 2550 INSULATION BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1365 S28L BURNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 AFT CARGO COMP HEAT DUCT BURNED INSULATION BLANKETS. BLANKETS CONTACT AFT CARGO COMPARTMENT HEAT DUCT IN AFT CARGO PIT, BS 1365 AND BETWEEN STR 28L TO STR 32R, (2 PIECES OF INSULATION). REPLACED & CHKD POSITION OF 2 PIECES OF INSULATION I N A/C BELLY NEAR AFT CARGO COMP HOT AIR DUCT. POSITIONED BLANKETS SO THEY DO NOT CONTACT HEATER DUCT. OK FOR SERVICE. SUSPECT DUCT RUN HOT WHEN CREW SELECTS MAX TEMP TO AFT CARGO COMPARTMENT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007031500123 20070315 00123 2007 3 15 2007UALA00647 4 20070303 A 2565 SLIDE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT OVERWING BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 RIGHT OVERWING SLIDE PACK UNLACE TRIGGER IS BROKEN OFF. REPLACED SLIDE. A/C RETURNED TO SERVICE. SLIDE PROBLEM ROOT CA USE: UNLACE TRIGGER FITTING BROKEN BY SIGNIFICANT IMPACT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007031500124 20070315 00124 NM 2007 3 15 2007UALA00648 1 20070303 A 5347 145T5213 SEAT TRACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 745-758 FRACTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 FRACTURED SEAT TRACK SCALLOPES AT RBL 88.0, STA 745 TO 758. *S/D* REPLACED SEAT TRACK SECTION REF SRM 51-40-02. FABRI CATED TRACK PER BOEING AC DWG. A/C READY FOR SERVICE. SUSPECT SERVICE CART DAMAGE COMBINED WITH FLIGHT ATTENDANT/ PAX TRAFFIC. 2 L 7 2 4F 4 F RT A1NM E24NE 2007031500125 20070315 00125 EU 2007 3 15 07FDEA00711 1 20070308 A 5414 SKIN AIRBUS 310 A310203 3930313 EU NR 2 PYLON CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 409FE 273 NR 2 PYLON PRECOOLER HOUSING RT SIDE SKIN SURFACE FOUND CRACKED AT RIB 5A UPPER AREA INSTALLED NEW WALL P/N A54611393203 00 PER SRM 51-72-10. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031500126 20070315 00126 NM 2007 3 15 2007UALA00649 1 20070302 A 2597 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE AFT GALLEY DAMAGED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 653UA 25391 F/A REPORTS BEING SHOCKED WHEN TOUCHING A GALLEY CART. FOUND CONNECTOR DAMAGED. REPLACED DAMAGED AFTER-GALLEY P53 P IGTAIL CORD CONNECTOR. CART CHECKED FOR VOLTAGE TO GROUND. CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007031500128 20070315 00128 NM 2007 3 15 2007UALA00651 1 20070302 A 3350 1317 LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 773UA 26929 EXTERIOR EMERGENCY LIGHTS INOPERATIVE AT DOOR 3L. CLEANED SOCKET, RELAMPED AND CHECKED PER MM 33-51-04. CHECKS NORMALL Y. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007031500130 20070315 00130 NM 2007 3 15 2007UALA00653 1 20070304 A 3350 LAMP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 798UA 26928 EEL LIGHT OUT AT 18 C&G. RELAMPED. TESTED GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007031500131 20070315 00131 NM 2007 3 15 2007UALA00654 1 20070302 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE SEAT 11C FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 846UA 1600 SEAT 11C AISLE WAY EEPM LIGHT INOPERATIVE WITH EMERGENCY LIGHTS SWITCHED TO ON. REPLACED SEAT LIGHT ASSY. OPS CHECK OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007031500132 20070315 00132 NM 2007 3 15 2007UALA00655 1 20070302 A 3397 CONTACT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT OUT OF ALIGNMENT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 572UA 26682 EMERGENCY SLIDE LIGHT INOP AT DOOR 1R. [SUP 4-17-07] FOUND CENTER CONTACT POPPED OUT OF LIGHT ASSEMBLY. REINSTALLED CE NTER CONTACT OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007031500133 20070315 00133 EU 2007 3 15 2007UALA00657 1 20070303 A 3510 OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 487UA 1669 F/O'S OXYGEN HARNESS FAILS TO INFLATE (LEAKING). DOES NOT TEST CORRECTLY WHEN PRESS TO TEST IS PUSHED. [SUP 05-24-07] REPLACED FIRST OFFICER'S MASK WITH A NEW UNIT. AT REPAIR, MASK WAS FOUND TO HAVE A LEAKING AIR BLADDER INSIDE THE HARN ESS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007031500134 20070315 00134 NM 2007 3 15 2007UALA00658 1 20070303 A 5210 BOTTLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE DOOR 2L READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 855UA 1737 DOOR BOTTLE AT 2L REPORTED LOW. [SUP 05-24-07] SERVICED BOTTLE TO PROPER PRESSURE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007031500135 20070315 00135 NM 2007 3 15 2007UALA00660 1 20070302 A 2120 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 653UA 25391 BURNING ODOR NOTICED IN CABIN BY CREW. TROUBLE SHOOTING IDENTIFIED PROBLEM AS OVERHEATING OF FWD E & E COMPARTMENT COOL ING FAN. REPLACED FWD EXHAUST FAN AS PER MM 21-58-06. TESTED OKAY. SUSPECT DIRT BUILD-UP CAUSED FAN TO DRAG & REQUIRED MORE CURRENT TO OVERCOME FRICTION. LED TO OVERHEATED MOTOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2007031500136 20070315 00136 NM 2007 3 15 2007UALA00661 1 20070302 A 4900 APU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SHUTDOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 APU AUTO SHUTDOWN AFTER APPROX 15-20 MINS OF OPERATION. ALL CHIP DETECTORS ARE OKAY AND NOTED OIL SYSTEM EXTREMELY HOT. [5-1-07] HISTORY SHOWS COOLING FAN AND OIL COOLER RECENTLY REPLACED. REPLACED APU. 2 L 7 2 4F 4 F RT A2NM E17NE 2007031500137 20070315 00137 NM 2007 3 15 UIEA200700093 1 20070227 A 5330 65B041042 SKIN BOEING 747 7472D3B 1384805 NM BS 690 MISREPAIRED A UIEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 15 505MC 21251 FUSELAGE BS 690 S31L HAS 14" BY 12" EXTERNAL DOUBLER TO LT UPPER STATIC PORT PREVIOUS REPAIRED PER SRM 51-70-00 PG 8E AN D F FIG 3 SHEET 6 AND 7. THIS REPAIR IS BEYOND THE LIMIT. REPAIRED ACCOMPLISHED AS PER SRM 53-30-03 FIG 1 AND 51-70-00 FIG 3. 2 L 7 4 4F RT A20WE 2007031500138 20070315 00138 NM 2007 3 15 UIEA200700094 1 20070228 A 5313 STRINGER BOEING 747 7472D3B 1384805 NM BS 895 S7R CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 M/DECK STA 895 STR 7R FOUND CRACKED. STRINGER REPAIRED ACCOMPLISHED AS PER SRM 53-10-03 FIG 4. 2 L 7 4 4F RT A20WE 2007031500139 20070315 00139 NM 2007 3 15 UIEA200700095 1 20070228 A 5310 65B04913428 CREASE BEAM BOEING 747 7472D3B 1384805 NM BS 960 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 FOUND M/DECK STA960, S-7R CREASE BEAM SUPPORT ANGLE FOUND CRACKED. CREASE BEAM SUPPORT WEB REPLACED AS PER SRM 51-10-0 1. 2 L 7 4 4F RT A20WE 2007031500140 20070315 00140 NM 2007 3 15 UIEA200700096 1 20070228 A 5313 65B0436655 STRINGER BOEING 747 7472D3B 1384805 NM BS 980 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 FOUND FWD CARGO COMPT STA 980, STR 43R IS CORRODED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F RT A20WE 2007031500141 20070315 00141 NM 2007 3 15 UIEA200700097 1 20070228 A 5310 CREASE BEAM BOEING 747 7472D3B 1384805 NM BS 940 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 M/DECK RTH SIDE STA 940, S-8R CREASE BEAM WEB FOUND CRACKED. CREASE BEAM WEB REPLACED AS PER SRM 51-10-01 AND 51-30-02. 2 L 7 4 4F RT A20WE 2007031500142 20070315 00142 NM 2007 3 15 UIEA200700098 1 20070228 A 5313 STRINGER BOEING 747 7472D3B 1384805 NM BS 875 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 M/DECK LT SIDE STA 875, STR9L FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03, FIG.4 2 L 7 4 4F RT A20WE 2007031500143 20070315 00143 NM 2007 3 15 UIEA200700099 1 20070228 A 5753 SKIN BOEING 747 7472D3B 1384805 NM TE FLAP PUNCTURED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 002212 21251 NR 20 VC FLAP FOLDING NOSE I/B END SKIN PUNCHED. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-290202458-1 THRU -3 AND FAA FORM 8100-9. 2 L 7 4 4F RT A20WE 2007031500144 20070315 00144 NM 2007 3 15 UIEA200700100 1 20070228 A 5414 65B94280185 SKIN BOEING 747 7472D3B 1384805 NM NR 3 NACELLE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 NR 3 ENGINE LT CORE COWL SKIN BOND DOUBLER CRACKED AT AIR EXHAUST DUCT AFT LOWER PORTION. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-286833874-1 THRU -6, DWG 65B94280 AND FAA FORM 8100-9. 2 L 7 4 4F RT A20WE 2007031500145 20070315 00145 NM 2007 3 15 UIEA200700101 1 20070228 A 5322 65B0963111 SHEAR TIE BOEING 747 7472D3B 1384805 NM BS 840 CRACKED A UIEA O OTHER O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 RT STA 840 FWD CHANNEL TENSION TIE AT 12 O'CLOCK FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER BOEING SR ID 1-288425027-1 AND -6, 1-289012875-1, SB747-53-2502 AND FAA FORM 8100-9. 2 L 7 4 4F RT A20WE 2007031500146 20070315 00146 NM 2007 3 15 UIEA200700106 1 20070301 A 5314 65B15069354 KEELBEAM BOEING 747 7472D3B 1384805 NM BS 1450 BULGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 FOUND KEEL BEAM BOTH SIDES WEB BULGE FOUND AT BS 1450. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-286690602-1 THRU -10. 2 L 7 4 4F RT A20WE 2007031500147 20070315 00147 NM 2007 3 15 UIEA200700102 1 20070228 A 5315 FLOORBEAM BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE BS 340 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 21784 UPPER DECK FLOORBEAM AT BS 340L ONE FASTENER HOLE CRACK AT FRAME WEB. THE CRACK WAS TRIMMED OUT AND REPAIRED PER BOEING MESSAGE AND SRM 53-10-04 FIG 102. 2 L 7 4 4F 4 F RT A20WE E23EA 2007031500148 20070315 00148 NM 2007 3 15 UIEA200700103 1 20070228 A 5315 FLOORBEAM BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE BS 420 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 21784 FOUND UPPER DECK FLOORBEAM AT BS 420R ONE FASTENER HOLE CRACK AT FRAME WEB. THE CRACK WAS TRIMMED OUT AND REPAIRED PER BOEING MESSAGE AND SRM 53-10-04 FIG 107. 2 L 7 4 4F 4 F RT A20WE E23EA 2007031500149 20070315 00149 NM 2007 3 15 UIEA200700107 1 20070301 A 5313 65B04366213 STRINGER BOEING 747 7472D3B 1384805 NM BS 905 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 M/DECK ZONE "C" LT SIDEWALL STRUCTURE STA 905, STR-10L FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER SRM 53-10-03, FIG 4. 2 L 7 4 4F RT A20WE 2007031500150 20070315 00150 NM 2007 3 15 UIEA200700120 1 20070302 A 5347 BAC15201566 SEAT TRACK BOEING 747 747243B 1384830 NM BS 1816 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 FOUND MAIN CARGO COMPARTMENT SEAT TRACK AT STATION 1816, LBL 99 HAS CRACK CROWN LUGS. ACCOMPLISHED PERMANENT REPAIR AS PER 747-200 SRM 53-10-05 FIG 1A, ALSO, REFERENCE ATLAS AIR EO 4753A921. 2 L 7 4 4F A20WE 2007031500151 20070315 00151 EU 2007 3 15 07FDEA00712 1 20070308 A 5210 STRUCTURE AIRBUS 310 A310203 3930313 EU R1 DOOR DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 409FE 273 FOUND ON R1 PASS DOOR, AT THE LOWER LT CORNER, SEVERAL SPOTS WITH MISSING MATERIAL (SHEET METAL) REPAIRED PER SRM 52-11- 00 FIG 206. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031500152 20070315 00152 EU 2007 3 15 07FDEA00713 1 20070308 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 409FE 273 FWD CARGO COMPARTMENT UPPER FLAP AT BEAM/FLOOR OF CABIN FOUND CRACK AT FR 38 AND Y1700 REPAIRED PER SFEDEX EA 6-5310-106 694. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031500153 20070315 00153 EU 2007 3 15 07FDEA00714 1 20070308 A 5313 SKIN AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CORROSION SPOTS ON FUSELAGE SKIN PANEL AT BUTT-STRAP C18 BETWEEN P26-27 LT. REPAIR WAS PERFORMED IAW TD942.04740 8/017/2006A (EA 6-5312-103399) AND APPROVED BY RAS/AS/165/2006 ISSUE:A. SEE ALSO DR 186 WHICH IS PERFORMED WITH MENTIONE D RAS. 2 L 7 2 4F RT A35EU 2007031500154 20070315 00154 EU 2007 3 15 07FDEA00715 1 20070308 A 5330 SKIN AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CORROSION SPOTS AFTER REMOVAL OF OLD EXTERNAL DOUBLER AT C18, P16/18 LT. REPAIR WAS PERFORMED IAW RAS/AS/165/2006 ISS.A ( EA 6-5312-103399) DR 508 IS ALSO COVERED BY MENTIONED RAS. 2 L 7 2 4F RT A35EU 2007031500155 20070315 00155 EU 2007 3 15 2007UALA00662 1 20070305 A 2130 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN PRESSURE UNKNOWN A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 472UA 1435 RTFL DUE TO BLEED 1 & 2 EMAC FAULT ON CLIMB. RESET BMC, BLEED 1 RESTORED IMMEDIATELY FOLLOWED BY BLEED 2 IN FLIGHT. SUPP LEMENTAL DATA UPDATE ON ENGINE NR 1, BITE TEST INDICATED FAULT OF EITHER FAN AIR VALVE, CONTROL THERMOSTAT OR SENSE LINE . FOUND FILTER FOR CONTROL THERMOSTAT SENSE LINE COMPLETELY CLOGGED. REPLACED FILTER AND THERMOSTAT AS A PRECAUTIONARY M EASURE. ON ENGINE NR 2, BITE TEST INDICATED FAULT OF BLEED REGULATED PRESSURE TRANSDUCER AND OVER PRESSURE VALVE. REPLAC ED OVER PRESSURE VALVE AND PRESSURE REGULATING VALVE AS A PRECAUTIONARY MEASURE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007031500156 20070315 00156 EU 2007 3 15 2007UALA00663 1 20070305 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSLEAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 477UA 1514 CABIN FLOORBEAM EXFOLIATED, STA FRAME C21 TO C22, LBL 9 IN. [SUP 05-24-07] REMOVED AND REPAIRED DAMAGED AREA IN ACCORD ANCE WITH SRM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007031500158 20070315 00158 NM 2007 3 15 2007UALA00665 1 20070305 A 5410 STRUCTURE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 NACELLE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 119UA 28812 CORROSION ON BOTH DIAGONAL SIDE BRACE FITTING BORES AT NUMBER 4 NACELLE STRUT. ACCOMPLISHED BORING THE DUAL SIDE BRAC E FITTING ON THE NACELLE STRUT AT NUMBER 4. BOTH HOLES DRESSED OUT PER COA AND SB 747-54A 2218 (FINAL HOLE DIA AFTER HON E=2.2454"). REASSEMBLED & INSPECTED. READY FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007031500159 20070315 00159 NM 2007 3 15 2007UALA00666 1 20070306 A 5410 STRUCTURE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 1 NACELLE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 119UA 28812 CORROSION - BOTH DIAGONAL SIDE BRACE FITTING BORES AT NR 1 NACELLE. MAJOR REPAIR. CORROSION - BOTH DUAL SIDE BRACE FI TTING BORES AT NUMBER 1 NACELLE. ACCOMPLISHED BORING THE DSB NACELLE STRUT AT NR 1. BOTH HOLES IN SPEC PER COA AND SB 7 47-54A2218 (FINAL HOLE DIA AFTER HONE INBD = 2.2449" OUTBD = 2.2448". REASSEMBLED AFTER CLEANUP. READY FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007031500160 20070315 00160 NM 2007 3 15 2007UALA00667 1 20070306 A 5710 STRUCTURE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 1 NACELLE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 119UA 28812 CORROSION - INBOARD BORE OF THE DIAGONAL SIDE BRACE UNDER WING FITTING AT NR 1 NACELLE STRUT ATTACH AREA. FOUND CORRO SION - INBD BORE OF THE DIAGONAL SIDE BRACE UNDER WING FITTING AT NUMBER 1 NACELLE STRUT ATTACH AREA. ACP BORING THE D SB UNDER WING FITTING AT NR 1 INBD HOLE PER COA 899993010. CLEANED UP UNDER-FITTING AREA & REASSEMBLED. READY FOR SER VICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007031500161 20070315 00161 NM 2007 3 15 2007UALA00668 1 20070306 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT CUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EEL LIGHT CABLE CUT AT SEATS 4A & 5E. REPLACED WITH NEW EMER LIGHT SEGMENTS (2 POSITIONS). EEL SYSTEM CHECKED NORMALLY . 2 L 7 4 4F 4 F RT A20WE E24NE 2007031500162 20070315 00162 2007 3 15 2007UALA00669 4 20070305 A 2565 MODULE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SLIDE INTERMITTENT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 F/A REPORTS UPPER DECK LEFT DOOR SLIDE LIGHT INOP. FOUND DOOR ANNUNCIATOR MODULE WORKING INTERMITTENTLY. NEEDS MODULE M 7035. NO PCN ONLY P-N 65B48538-2. SEE IPC 52-23-15-001 ITEM 20. REPLACED MODULE. TESTED & FOUND OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007031500163 20070315 00163 NM 2007 3 15 2007UALA00670 1 20070305 A 2560 FLASHLIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 RED LED FOR HI-INTENSITY EMERGENCY FLASHLIGHT (OUTBOARD) IS NOT FLASHING AT ATTENDANT'S SEAT NEAR NR 3 LEFT MAIN ENTRY D OOR. REMOVED AND REPLACED HI -INTENSITY EMERGENCY FLASHLIGHT (OUTBOARD) AND BATTERY KIT NEAR NR 3 LT MAIN ENTRY DOOR. OPERATIONAL CHECKED - NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007031500164 20070315 00164 NM 2007 3 15 2007UALA00671 1 20070305 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 549UA 25397 EXTERIOR EMERGENCY LIGHT INOP AFT RIGHT OVERWING. [SUP 5-1-07] RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007031500165 20070315 00165 NM 2007 3 15 2007UALA00672 1 20070305 A 5347 145T5212 SEAT TRACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 785 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 MAIN CABIN SEAT TRACK CRACKED AT BS 785 AND RBL 56. REMOVED DAMAGED SEAT TRACK SECTION AND FABRICATED SPLICE SECTION AN D SPLICE CHANNELS AND INSTALLED PER SRM 53-00-52, DETAIL IV AND V, PG 206 AND SRM 51-40-2. SUSPECT COMBINATION OF SERVI CE CART LOADING AND PAX/ FLIGHT ATTENDANT TRAFFIC. 2 L 7 2 4F 4 F RT A1NM E24NE 2007031500166 20070315 00166 NM 2007 3 15 2007UALA00673 1 20070305 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SEAT 1E UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 792UA 26934 WIRE HANGING OUT ON AISLE SIDE OF SEAT 1E POSSIBLY FROM EMERGENCY LIGHTING. RESECURED EMERGENCY LIGHT STRIP TO MOVEABLE ARMREST AND EMERGENCY LIGHTS OPERATION TESTED NORMALLY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007031500167 20070315 00167 EU 2007 3 15 2007UALA00674 1 20070305 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 433UA 589 EMERGENCY LIGHT TEST FAILED -EXT LOADS AFT L- NO GREEN SYS OK LIGHT CIDS RESET, NO HELP. [SUP 05-24-07] FAULT TRACED T O A FAULTY SLIDE PACK AT DOOR 2L. OVERHAUL OF THE SLIDE PACK FOUND THE GREEN SYSTEM LIGHTS TO BE DAMAGED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007031500176 20070315 00176 NE 2007 3 15 2007UALA00678 2 20070306 A 7230 COMPRESSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE STALLED A UALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 29 518UA 24871 727193 RTFL DUE TO NR 2 ENGINE COMPRESSOR STALLS. [SUP 05-18-07] BOROSCOPE NR 2 ENG SERIAL NR 727193, FOUND SEVERE DAMAGES ON COMPRESSOR STAGES 16 & 17 THROUGH AP8. FOUND RT ENGINE BLADE 1 & 2 GOUGES IN LEFT EDGES. BLADES 1 AND 2 OK. REPLACEM ENT OF NR 2 ENG NR 4 BEARING SCAVENGE VALVE. ENGINE RUN - ALL PARAMETERS WITHIN NORMAL RANGE. REPLACED NR 2 ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007031500177 20070315 00177 NM 2007 3 15 2007UALA00679 1 20070306 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 23671 EMERGENCY FLOOR LIGHTING INOP FROM ROW 16 TO DOOR 2L. REPLACED LIGHT POWER STRIP FROM SEAT 16 TO FWD EDGE OF AFT GALLEY , LIGHTING CHECK OK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007031500178 20070315 00178 NM 2007 3 15 2007UALA00680 1 20070307 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY EXIT CEILING LIGHT INOP AT TOP OF UPPER DECK STAIRS. RELAMPED, OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007031500179 20070315 00179 NM 2007 3 15 2007UALA00681 1 20070307 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY LIGHTS INOP AT EXIT STAIR ILLUMINATION TO UPPER DECK AND AT ROW 59 LEFT. REPLACED LAMPS, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007031500180 20070315 00180 NM 2007 3 15 2007UALA00682 1 20070307 A 3350 276005 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 104UA 26902 FOUR EACH EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP ON LEFT SIDE. REPLACED FUSES IN EPSU. CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007031500181 20070315 00181 NM 2007 3 15 2007UALA00684 1 20070306 A 5330 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU BS 552 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 919UA 25386 UPPER CROWN HAS LIGHTNING STRIKE BS 552 AT STRINGER 2L. MAJOR REPAIR: REMOVED DAMAGE, FABRICATED AND INSTALLED EXTERNA L DOUBLER, TRIPLER, AND FILLER REPAIR REF SRM 53-00-01 REPAIR 31 PROCEDURE V PAGE 201-240. 2 L 7 2 4F 4 F RT A16WE E21EU 2007031600001 20070316 00001 WP 2007 3 16 AALA20070391 1 20070223 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 234AA 49181 LGA - FOUND EMERGENCY LIGHT AT OVERWING INOPERATIVE. RESEATED CONNECTOR ON POWER SUPPLY FOR EMERGENCY LIGHT AT OVERWING . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007031600002 20070316 00002 NM 2007 3 16 AALA20070384 1 20070222 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 649AA 24607 DFW - FOUND EMERGENCY LIGHT AT SEAT ROW 12 INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 12. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007031600003 20070316 00003 WP 2007 3 16 AALA20070387 1 20070223 A 2121 6054578 FAN DOUG DC9 DC982 3022082 WP AIR CONDITIONING INOPERATIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 274AA 49271 SDF INFLIGHT - CREW REPORTED SMOKE AND FUMES FROM AIR CONDITIONING PACKS. LANDED SDF WITHOUT INCIDENT. FOUND RECIRCULA TION FAN BREAKERS POPPED. REPLACED RECIRCULATION FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007031600018 20070316 00018 EA 2007 3 16 SWIA200718002 1 20070309 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 913EV 7731 OVERHEAD MID CABIN EMERGENCY LIGHT INOP. REPLACED OVER HEAD MID CABIN EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007031600019 20070316 00019 SO 2007 3 16 SWIA200718003 1 20070211 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 566SW 120341 SEAT TRACK FOR SEAT 11A HAS CORROSION AT SEAT, DISCOVERED DURING C-CHECK INSPECTION. REPLACED FLOOR SEAT TRACK AT SEAT 11A PER EMBRAER APPROVED REPAIR NO EST 186/96. 2 L 7 2 4T RT A31SO 2007031600021 20070316 00021 SO 2007 3 16 SWIA200718005 1 20070211 A 5411 RIB EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 566SW 120341 LEFT MLG MID COWL FIRST RIB AFT OF DOOR FRAME CRACKED AT STRINGER CUT OUT, DISCOVERED DURING C-CHECK INSPECTION. REPAIR ED RIB IAW SRM 51-70-05 AND RII 54-900-1000. 2 L 7 2 4T RT A31SO 2007031600024 20070316 00024 EA 2007 3 16 SIMA200707201 1 20070312 A 3520 OXYGEN MASK CNDAIR CL600 CL6002C10 1390015 EA CABIN UNWANTED DEPLOY A SIMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 21 522AE 10147 ALL PASSENGER OXYGEN MASKS DEPLOYED DURING TAXI. RESTOWED PASSENGER OXYGEN MASKS IAW CRJ AMM. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007031600030 20070316 00030 CE 2007 3 16 DXTA200702017 1 20070313 A 7931 TRANSMITTER CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LT ENG OIL PRESS MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 696QS 5605296 PCEDB0702 DURING POWER REDUCTION TO IDLE AT 10.000 FT, LT ENGINE OIL PRESSURE DROPPED TO BELOW 20 PSI AND JUMPED BACK AND FORTH TO 40 PSI. ON POWER INCREASE, PRESSURE STAYED AROUND 30 PSI. ENGINE WAS LEFT AT IDLE UNTIL COMPLETION OF FLIGHT. LOWERED NR 1 ENGINE COWLING. INPSECTED FOR OIL LEAKS. NO LEAKS NOTED. REMOVED AND REPLACED OIL PRESSURE TRANSMITTER. ADDED .5 QT S OF OIL (2380) RAN NR 1 AND 2 ENGINES. OPS CHECK GOOD IAW CE560XL M/M 79-30-00, AND MM 05-10-00. LEAK CHECK GOOD. CLOSE D COWLING. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007031600031 20070316 00031 NM 2007 3 16 WRLA2007042 1 20070312 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE BS 840-855 CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271WA 48518 DURING C-04 CHECK, FOUND SEAT TRACK AREA Y=840-855 X=44 CORRODED. INSTALLED SEAT TRACK AND SPLICE PER MD-11 SRM VOL.II 51-33-01 REV.38. 2 L 7 3 4F 4 F RT A22WE E24NE 2007031600032 20070316 00032 NM 2007 3 16 WRLA2007043 1 20070312 A 5313 LONGERON DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE BS 1953 L40R CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271WA 48518 DURING C-04 CHECK, FOUND LONGERON L40R CORRODED STA Y=1953. PERFORM LONGERON REPAIR PER MD-11 SRM VOL.I 53-10-00 FIG.2 TABLE I R=5. 2.INSTALLED REPAIR FITTING AND REPAIR LONGERON PER MD-11 SRM VOL.II 51-33-01 & 51-35-01 REV.38. 2 L 7 3 4F 4 F RT A22WE E24NE 2007031600034 20070316 00034 NM 2007 3 16 WRLA2007044 1 20070312 A 5313 LONGERON DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE BS 1953 L42R CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271WA 48518 DURING C-04 CHECK, FOUND LONGERON L42R CORRODED STA Y=1953. PERFORM LONGERON REPAIR PER MD-11 SRM VOL.I 53-10-00 FIG.2 TABLE 1 R=5. 2. INSTALLED REPAIR FITTING AND LONGERON PER SRM VOL.II 51-33-01,51-35-01 REV.38. 2 L 7 3 4F 4 F RT A22WE E24NE 2007031600037 20070316 00037 EU 2007 3 16 BAQA20070007 1 20070308 A 6320 355A530500164 LINE AEROSP AS355 AS355F2 8680812 EU ALLSN 250C 250C20 03013 GL OIL CUT E BAQA K NONE K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 EA 03 942MS 6361 170 5498 DURING POST FLIGHT WALK AROUND INSPECTION FOUND MAJORITY OF TAILBOOM OF AIRCRAFT COVERED IN BLACK OIL. REPAIRED CUT OIL LINE. 1 G 7 2 3U 3 U H11EU E4CE 2007031600038 20070316 00038 EU 2007 3 16 07FDEA00817 1 20070314 A 5524 FITTING AIRBUS 310 A310324 3930206 EU ZONE 300 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 OLD REPAIR ON LT ELEVATOR, AT INNER FITTING NR 2, A LUG IS BROKEN OFF TO INSTALL A SAFETY COTTER PIN. VISUAL VERIFICATI ON OF REPAIR, ACCOMPLISHED IAW RAS/CASA/2363/2002 ISSUE "A". 2 L 7 2 4F RT A35EU 2007031600039 20070316 00039 EU 2007 3 16 07FDEA00818 1 20070314 A 5524 FITTING AIRBUS 310 A310324 3930206 EU ZONE 500 MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 813FD 500 OLD REPAIR ON CENTER WING FITTING C47, DEVIATION OF HOLE 1 AND 41 WITH SB 57-2047. VERIFICATION OF REPAIR, PERFORMED IA W RAS 013464/014/2001 ISSUE "A" AND SIA-EN: 10EN-57-7681. 2 L 7 2 4F RT A35EU 2007031600040 20070316 00040 NM 2007 3 16 AWXA200700352 1 20070214 A 5743 6549488503 FITTING BOEING 737 7373S3 1384711 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND LEFT WING MAIN LANDING GEAR SUPPORT BEAM FITTING CRACKED, WBL 157. REPLACED LEFT WING MAIN LANDING GEAR SUP PORT BEAM FITTING IAW AWA ER 03-5722-07065-SS. 2 L 7 2 4F RT A16WE 2007031600042 20070316 00042 NM 2007 3 16 AWXA200700355 1 20070312 A 5320 651768469 INTERCOSTAL BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND CRACKED INTERCOSTAL, BS 294.5 - BS 303.9, S13L. REPLACED INTERCOSTAL, BS 294.5 - BS 303.9, S13L IAW AWA E R 03-5312-07067-ES1. 2 L 7 2 4F RT A16WE 2007031600045 20070316 00045 NM 2007 3 16 AWXA200700358 1 20070312 A 5313 6561777503 STRINGER BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND CRACKED STRINGER CHANNEL, BS 360, S14L. REPLACED STRINGER CHANNEL, BS 360, S14L IAW AWA ER 03-5312-07066-E S2. 2 L 7 2 4F RT A16WE 2007031600046 20070316 00046 NM 2007 3 16 AWXA200700359 1 20070312 A 5340 6916920501 ATTACH ANGLE BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND CRACKED ATTACH CLIP, BS 348.20, S15L. REPLACED ATTACH CLIP, BS 348.20, S15L IAW AWA ER 03-5312-07066-ES2. 2 L 7 2 4F RT A16WE 2007031600047 20070316 00047 NM 2007 3 16 AWXA200700360 1 20070312 A 5320 65176859 COVER BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND CRACKED WEB COVER, BS 348.20 - BS 351.2, S15L - S17L. REPLACED WEB COVER, BS 348.20 - BS 351.2, S15L - S17L IAW AWA ER 03-5312-07066-ES2. 2 L 7 2 4F RT A16WE 2007031600048 20070316 00048 NM 2007 3 16 AWXA200700361 1 20070312 A 5320 65176856 STRAP BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND CRACKED TIE STRAP, BS 348.20, S16L. REPLACED TIE STRAP, BS 348.20, S16L IAW AWA ER 03-5312-07066-ES2. 2 L 7 2 4F RT A16WE 2007031600051 20070316 00051 NM 2007 3 16 AWXA200700364 1 20070312 A 5340 69265552 STRINGER CLIP BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND CRACKED CLIP, BS 348.20, S16L. REPLACED CLIP, BS 348.20, S16L IAW AWA ER 03-5312-07066-ES2. 2 L 7 2 4F RT A16WE 2007031600054 20070316 00054 EU 2007 3 16 USAA070177 1 20070309 A 5321 D5361011700295 FLOOR PANEL AIRBUS A321 A321211 3930370 EU FUSELAGE DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 167US 1442 SEPARATION OF COMPOSITE, AFT EDGE OF COCKPIT FLOOR PANEL 211FF. FABRICATED NEW BOARD PER MCGILL IRM 979 REV F, DEFECT S IZE: 1 X 3 INCHES. 2 L 7 2 4F RT A28NM 2007031600055 20070316 00055 EU 2007 3 16 USAA070176 1 20070309 A 5347 D5311278220201 SEAT TRACK AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 167US 1442 RIGHT O/B SEAT TRACK 2 INCHES FWD OF FR 23 2 GALLEY MOUNT HAS CORROSION. REMOVED & REPLACED PER SRM 53-11-15, DEFECT SI ZE: 6 X 4 INCHES. 2 L 7 2 4F RT A28NM 2007031600056 20070316 00056 EU 2007 3 16 USAA070175 1 20070309 A 5320 D5347218820400 FLOOR SUPPORT AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 167US 1442 LEFT FLOOR SUPPORT Y1292 FR 67-68 HAS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-72-11; CORR TASK JA-260 -53500; LEVEL 1, DEFECT SIZE: 3 SQ INCHES. 2 L 7 2 4F RT A28NM 2007031600057 20070316 00057 WP 2007 3 16 07FDEA00828 1 20070314 A 5711 SPAR DOUG MD10 MD1010F 3022112 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 360FE 46636 RIGHT WING REAR SPAR IS CRACKED AT NR 3 AFT FUEL BOOST PUMP, REMOVED PARTS. FABRICATED REPAIR DOUBLER AND INSTALLED REP AIR PARTS IAW SRM 57-10-00, FIG 52, VOL I. 2 L 7 3 4F RT A22WE 2007031600059 20070316 00059 NM 2007 3 16 07FDEA00832 1 20070314 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 CABIN FWD RT GALLEY DOOR EXT UPPER HINGE CUT OUT DOOR SKIN HAS A CRACK. STOPPED DRILLED CRACK IAW SRM IAW SRM 52-00-3 F IG 3. FABRICATED REPAIR DOUBLER FROM 2024 T-3 .080C. INSTALLED REPAIR IAW SRM 52-00-3 FIG 3. REPAIR CLASSIFIED AS A M AJOR REPAIR. 2 L 7 3 4F A3WE 2007031600062 20070316 00062 EU 2007 3 16 07FDEA00835 1 20070314 A 5730 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CORROSION ON RT WING TOP SKIN AT TRAILING EDGE AREA OUTER SHROUD BOX. REPAIR PERFORMED IAW EA 6-5720-103382. 2 L 7 2 4F RT A35EU 2007031600066 20070316 00066 WP 2007 3 16 07FDEA00839 1 20070314 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 360FE 70707 46636 FOUND FUSELAGE SKIN DENT AT LE OF RT STATIC PORT (PRIMARY) CREATING A GAP BETWEEN SKIN AND COMPENSATOR PLATE REPAIRED ST ATIC PORT REGION IAW SRM VOL I 53-20-00 FIG 9. CLASS "B" REPAIR REQUIRES REINSPECTION AND FOLLOWUP INSPECTIONS. INITIA L INSPECTION AT 34,000 AND REPETITIVE AT 23,000 IAW SRM VOL I 53-20-00 FIG 9. 2 L 7 3 4F RT A22WE 2007031500069 20070315 00069 EU 2007 3 15 07FDEA00784 1 20070313 A 5310 CROSSBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 OLD CROSS BEAM REPAIR WHICH WAS NOT CONFORM TO SRM. THE SRM REPAIR IN SOURCE DR330 ISN'T APPLICABLE. ANOTHER CROSSBEAM REPAIR WAS NECESSARY. CROSSBEAM REPAIR PERFORMED IAW SRM 53-10-15, FIG.207. 2 L 7 2 4F RT A35EU 2007031500070 20070315 00070 EU 2007 3 15 07FDEA00785 1 20070313 A 5313 A53970701388 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND HEAVY CORROSION ON STRINGER WITH COUPLING AT C54.3, P49. REPAIR IS PERFORMED IAW SRM 53-10-14, FIG 201. 2 L 7 2 4F RT A35EU 2007031500071 20070315 00071 EU 2007 3 15 07FDEA00786 1 20070313 A 5313 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND HEAVY CORROSION ON P44 RT BETWEEN C38.2-C39. REPAIR PERFORMED IAW SRM 53-10-14, FIG 201. 2 L 7 2 4F RT A35EU 2007031500072 20070315 00072 EU 2007 3 15 07FDEA00787 1 20070313 A 5313 A53777250 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND HEAVY CORROSION ON STRINGER P30 RT BETWEEN C33 AND C34. REPAIR IS PERFORMED IAW RAS/DABRE/7007241/2006 ISSUE:A (E A 6-5314-103372). 2 L 7 2 4F RT A35EU 2007031500073 20070315 00073 EU 2007 3 15 07FDEA00788 1 20070313 A 5313 A53777250 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND HEAVY CORROSION ON STRINGER P30 RT BETWEEN C33 AND C34. REPAIR IS PERFORMED IAW RAS/DABRE/7007241/2006 ISSUE:A (E A 6-5314-103372). 2 L 7 2 4F RT A35EU 2007031500074 20070315 00074 EU 2007 3 15 07FDEA00789 1 20070313 A 5313 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 OLD DAMAGED STRINGER P37 LT BETWEEN C55/58 AND C59. STRINGER REPAIR PERFORMED IAW SRM 53-10-14, FIG 201. 2 L 7 2 4F RT A35EU 2007031500075 20070315 00075 NM 2007 3 15 07FDEA00790 1 20070313 A 5343 FITTING DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 DURING REPLACEMENT OF LEFT NOSE LANDING GEAR FITTING INBOARD BUSHING FOUND FITTING BORE WITH CORROSION. (SUPPLEMENTAL 28 MARCH 07) CORRODED FITTING ON NOSE LANDING GEAR LEFT HAND REMOVED AND REPLACED WITH NEW FITTING AS PER SRM 51- 31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007031500076 20070315 00076 EU 2007 3 15 07FDEA00791 1 20070313 A 2910 FITTING AIRBUS 310 A310324 3930206 EU ZONE 400 LOOSE A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 HYD FITTING GREEN PRESSURE PIPE AND BLUE SUCTION PIPE LOOSE IN FEED THROUGH ON LT WING. REPAIR PERFORMED IAW AI-INSTRUC TION: R572-49184 ISSUE: C (EA 6-5720-103398). 2 L 7 2 4F RT A35EU 2007031500077 20070315 00077 EU 2007 3 15 07FDEA00792 1 20070313 A 5755 SKIN AIRBUS 310 A310324 3930206 EU ZONE 500 DELAMINATED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 AT LOWER SKIN ON SPOILER 2 LT TRAILING EDGE WAS AN AREA DELAMINATED. REPAIR PERFORMED IAW EA 6-5770-103369. 2 L 7 2 4F RT A35EU 2007031500078 20070315 00078 NM 2007 3 15 UPS07449369 1 20070215 A 5230 FRAME BOEING 747 747121 1384871 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D L4 DOOR LOWER AFT CORNER FRAME FOUND CRACKED. CRACK LENGTH 1.5 INCH. FRAME REPAIRED AS PER SRM 5 2-10-02 FIG 10 AT M/D L4 DOOR AFT VERTICAL FRAME CORNER AREA. 2 L 7 4 4F A20WE 2007031500079 20070315 00079 NM 2007 3 15 UPS07449376 1 20070216 A 5210 SKIN BOEING 747 747121 1384871 NM L3 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D L3 DOOR SKIN FOUND CRACKED APPROX AT CTR LOWER PORTION. CRACK LENGTH .75 INCH. L3 DOOR SKIN REPA IRED AS PER SRM 52-10-02 FIG 9. 2 L 7 4 4F A20WE 2007031500080 20070315 00080 NM 2007 3 15 UPS07449377 1 20070212 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 760 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D - LBL 75-97 BS 760 FLOORBEAM CORRODED. CORROSION BLEND OUT 0.044" X 1" X 2" EXCEED SRM 53-10-01 F IG 1 LIMITS. M/D BS 760 LBL 67 TO MOST LEFT O/B FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 3. 2 L 7 4 4F A20WE 2007031500081 20070315 00081 EU 2007 3 15 07FDEA00795 1 20070313 A 5415 SKIN AIRBUS 310 A310324 3930206 EU ZONE 400 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 PYLON SUPPORT BRACKET HOLES ON LT/RT WING BOTTOM SKIN DAMAGED. REPAIR PERFORMED IAW EA 6-5720-103398. 2 L 7 2 4F RT A35EU 2007031500082 20070315 00082 EU 2007 3 15 07FDEA00798 1 20070313 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 669FE 774 CABIN SEAT TRACK GOUGED BETWEEN FR 40-50 LBL 18 REPLACED SEAT TRACK FROM FR40 TO FR54 AT LBL18 IAW AIRBUS DWG A53812912. TREATED SEAT TRACK IAW FEDEX A300-600 SRM 51-21-10, PO NR 564624.4. 2 L 7 2 4F RT A35EU 2007031500087 20070315 00087 NM 2007 3 15 SWAA071335 1 20070312 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM BS 727B S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031500088 20070315 00088 NM 2007 3 15 SWAA071330 1 20070312 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 344 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 344, LBL 10. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007031500089 20070315 00089 NM 2007 3 15 SWAA071333 1 20070312 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM BS 500C S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031500090 20070315 00090 NM 2007 3 15 SWAA071325 1 20070312 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM BS 727D S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031500091 20070315 00091 NM 2007 3 15 SWAA071322 1 20070311 A 5754 65C26602301 SKIN BOEING 737 7375H4 138449D NM NR 2 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED MV1 CHECK, FOUND NR 2 L/E SLAT DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED NR 2 L/E SLAT ASSY PE R MM. 2 L 7 2 4F RT A16WE 2007031500096 20070315 00096 WP 2007 3 15 IXXA07SMN132S 1 20070303 A 5512 SKIN DOUG DC8 DC871F 302199D WP ZONE 300 DAMAGED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER HAS ELONGATED HOLES AT LEADING EDGE STATION XFS 285 .000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CO RROSION FOUND AFTER DAMAGE REMOVED. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PASTS AS NEED ED. APPLIED SEALANT TO FAYING SURFACE. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, DC8 SRM 51-1-21, DC8 SRM 51-3-0 DC8 NDT PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SEMAN DRAWING NUMBER ED 4443 DATED 01-24-07 AND COMPLETED FAA FORM 8110-3 NUMBER 07031 DATED 01-26-07. 2 L 7 4 4F RT 4A25 2007031500097 20070315 00097 CE 2007 3 15 BSAASDR0703 1 20070301 A 3230 1143640681 CIRCUIT BOARD BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A BSAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 05 139ZV UE139 WHEN GEAR HANDLE WAS SELECTED DOWN DURING APPROACH, THE GEAR DIDN'T EXTEND, THE RED UNSAFE LIGHT CAME ON, AND THE GREEN GEAR DOWN LIGHTS STAYED OFF. CREW FOUND THE 2 AMP CONTROL CB POPPED. GEAR HANDLE WAS PUT BACK UP, THE CB WAS RESET, AN D THE CB POPPED AGAIN, WITH THE SAME INDICATION. GEAR WAS THEN PUMPED DOWN BY HAND, WITH THREE GREEN GEARDOWN LIGHTS. MAINTENANCE TROUBLESHOT AND REPLACED PC BOARD A316, GEAR WAS CYCLED MULTIPLE TIMES WITH NO FURTHER PROBLEMS. THERE WAS ONE PREVIOUS INCIDENT OF THE SAME FAILURE ON WITH THE SAME PC BOARD. 2 L 7 2 4T RT A24CE 2007031500098 20070315 00098 NM 2007 3 15 07FDEA00688 1 20070307 A 5330 6518385 SKIN BOEING 727 727225 1384077 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 LOWER FUSELAGE AT BS 1148 TO 1170 BETWEEN STR 19R AND 20R, SKIN IS CREASED. REMOVED DAMAGE AND MANUFACTURED REPAIR PARTS REF SRM 53-30-3, PG 5. TREAT AND PRIMED REPAIR PARTS AND REPAIR AREA ON A/C SKIN REF SRM 51-10-2 PG 7. INSTALLED FAST ENERS REF SRM 51-30-02 PG 8 AND SRM 53-30-3 PG 5, ITEM 12. 2 L 7 3 4F A3WE 2007031500099 20070315 00099 NM 2007 3 15 07FDEA00696 1 20070308 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 CABIN STA 1521 TO STA 5-93, X = -8.5 SEAT TRACK FOUND CORRODED. CORRODED SEAT TRACK AT STA 1521 TO STA 5-93, X = -8.5 R EPAIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007031500100 20070315 00100 NM 2007 3 15 07FDEA00697 1 20070308 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 CABIN STA 1521 TO STA 5-73, X = 47.5 SEAT TRACK FOUND CORRODED. CORRODED SEAT TRACK AT STA 1521 TO STA 5-73, X = 47.5 RE PAIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007031500101 20070315 00101 EU 2007 3 15 07FDEA00698 1 20070308 A 5330 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CORROSION AT MANHOLE FITTING ( C38-C38.1) AND EXTERNAL SKIN AREA FWD OF C39. REPAIR WAS PERFORMED IAW TD/K7/S1/07 107 ISS.A (EA 6-5314-106384A), APPROVED BY RAS/DABRE/7007107/2006 ISS.:A. 2 L 7 2 4F RT A35EU 2007031500102 20070315 00102 EU 2007 3 15 07FDEA00699 1 20070308 A 5312 BULKHEAD AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 OLD CORROSION REPAIR IN FUSELAGE CENTER SECTION AT C39 AND CORROSION AT PRESSURE BULKHEAD. REPAIR WAS VERIFIED AND PERF ORMED IAW RAS: 047609/013/2006 ISSUE:A. 2 L 7 2 4F RT A35EU 2007031500103 20070315 00103 EU 2007 3 15 07FDEA00700 1 20070308 A 5753 SKIN AIRBUS 310 A310203 3930313 EU TE FLAP DELAMINATED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 409FE 273 OUTB FLAP RT, DELAMINATION FOUND ON THE INBD AREA, INNER SKIN SURFACE REPAIRED PER FEDEX ENG AUTH 6-5710-106684. REPAI R EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031500104 20070315 00104 EU 2007 3 15 07FDEA00701 1 20070308 A 5730 PANEL AIRBUS 310 A310203 3930313 EU RT WING CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 409FE 273 RT WING, WING LWR SKIN SURFACE NEXT TO TOP INB OF PNL 681AB FOUND CRACKED REPAIRED PER FEDEX ENG AUTH 6-5710-106686. RE PAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031500105 20070315 00105 EU 2007 3 15 07FDEA00703 1 20070308 A 5510 BEARING AIRBUS 310 A310203 3930313 EU RUDDER HINGE DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 409FE 273 RUDDER HINGE ARM NR 4 WITH FWD BEARING DAMAGED. BEARING REPLACED PER SB NO A310-55-2025 PG 27/28 DATE OCT 12/98 REVISIO N NO 3 APR 08/04 FEDEX EA 6-5510-106687. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031500106 20070315 00106 EU 2007 3 15 07FDEA00704 1 20070308 A 5330 SKIN AIRBUS 310 A310203 3930313 EU FUSELAGE DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 409FE 273 FUSELAGE SKIN SURFACE FOUND DENTED BETWEEN FS 68 AND FS 69 RT AND BETWEEN STR 2 AND STRG 3 REPAIRED PER SRM 53-10-12 FIG 225 (SHEET 1). REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031500107 20070315 00107 EU 2007 3 15 07FDEA00705 1 20070308 A 5755 FITTING AIRBUS 310 A310203 3930313 EU NR 3 SPOILER CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 409FE 273 LT WING NR 3 SPOILER INB SEATING FITTING FOUND CRACKED REPAIRED PER SRM 57-51-11 FIG 204 SHEET 1. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031500108 20070315 00108 EU 2007 3 15 07FDEA00706 1 20070308 A 5321 FLOOR PANEL AIRBUS 310 A310203 3930313 EU CARGO BAY CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 409FE 273 FOUND FWD CARGO COMP´T CABIN FLOOR UPPER FLAP CRACKED AT FR 25 AND AT -Y690. REPAIRED PER SRM 53-10-15 FIG 201 SHEET 4A . REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031500109 20070315 00109 EU 2007 3 15 07FDEA00707 1 20070308 A 5410 FERRULE AIRBUS 310 A310203 3930313 EU NR 2 PRECOOLER CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 409FE 273 NR 2 PYLON PRECOOLER FERRULE WITH SEVERAL CRACKS. INSTALLED NEW FERRULE P/N A5461270000000 PER SRM 51-72-10. REPAIR EV ALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031500110 20070315 00110 EU 2007 3 15 07FDEA00709 1 20070308 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 409FE 273 MDCC- FOUND TRACK -Y953 WITH CORROSION BETWEEN FRAMES 53 AND 54. REPAIRED PER SRM 53-10-16. REPAIR EVALUATED PER GMM 6 -2-100 AND CLASSIFIED AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031500111 20070315 00111 EU 2007 3 15 07FDEA00710 1 20070308 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 409FE 273 MDCC- FOUND TRACK -Y1456 WITH CORROSION BETWEEN FRAMES 46 AND 54. REPAIRED PER SRM 53-10-16 FIG 205. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR". 2 L 7 2 4F RT A35EU 2007031500112 20070315 00112 NM 2007 3 15 2007UALA00572 1 20070220 A 3220 1225P0089 SWITCH BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NLG INOPERATIVE A UALA O OTHER E VIBRATION/BUFFET AP APPROACH 1 WP 29 777UA 26916 ABOUT 5 SECONDS AFTER GEAR HANDLE TO DOWN POSITION HEARD LOUD BANG IN VICINITY OF NOSE GEAR. ABOUT 2 SECONDS LATER GOT NORMAL GEAR DOWN INDICATION. *S/D* FOUND STRUT PRESS-EXTENSION LOW. NO FLUID LEAKS. REPLACED NOSE GEAR PRESSURE SWIT CH SYSTEM CHECKED NORMALLY. A/C RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007031500113 20070315 00113 NM 2007 3 15 2007UALA00636 1 20070302 A 5320 FLOOR SUPPORT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 802UA 690 CORROSION FOUND ON FLOOR STRUCTURE UNDER AFT GALLEY. (SUP 05-24-07] ATTEMPT TO BLEND OUT CORROSION RESULTED IN EXCESSI VE MATERIAL LOSS AND STRUCTURE OUTSIDE OF ALLOWABLE DAMAGE LIMITS. AFFECTED FLOOR STRUCTURE WAS CUTOUT AND REPAIRED IN A CCORDANCE WITH SRM. SUSPECT CLOGGED CHILLER DUCT DRAIN, WHICH WOULD HAVE ALLOWED EXCESS MOISTURE TO BUILDUP IN THE FLOOR STRUCTURE UNDERNEATH AND AROUND THE GALLEY. REPLACED INTERCOSTAL. INSTALLED NEW FLOOR BEAMS. MFG & INSTALLED NEW FLOOR PANELS. REPLACED R2 DOOR SILL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007031500114 20070315 00114 NM 2007 3 15 2007UALA00638 1 20070302 A 5230 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FWD CARGO DOOR FWD FRAME IS CRACKED AT LWR STOP FITTING. *S/D* MAJOR REPAIR: ACCOMPLISHED NESTED ANGLE REPAIR PER MM 53-30-75 PAGE 801-813. 2 L 7 2 4F 4 F RT A16WE E21EU 2007031500115 20070315 00115 NM 2007 3 15 2007UALA00639 1 20070302 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FWD CARGO DOOR AFT FRAME IS CRACKED IN UPPER FLANGE AT LOWER STOP FITTING. MAJOR REPAIR: REMOVED DAMAGE. INSTALLED NE W FRAME SECTION PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2007031500116 20070315 00116 NM 2007 3 15 2007UALA00640 1 20070302 A 5510 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RUDDER DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 RUDDER S/N -099 LEFT SIDE JUST ABOVE COUNTER BALANCE AREA HAS GROOVE WEAR DAMAGE. *S/D* MAJOR REPAIR: ACCOMPLISHED CO MPOSITE REPAIR PER AAR EA-I070152 & SRM 51-70-17. 2 L 7 2 4F 4 F RT A16WE E21EU 2007031500168 20070315 00168 NM 2007 3 15 UIEA200700136 1 20070310 A 5730 SKIN PANEL BOEING 747 747243B 1384830 NM LT WING DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 LT WING UPPER TRAILING EDGE SKIN PANEL HAS A 6.0 INCH BY 6.0 INCH AREA OF DELAMINATION AND FASTENERS ARE PULLING THRU TH E SKIN, AT WBL 239.00 INBOARD OF NR 6 SPOILER AND 62.0 INCHES FROM AFT EDGE. PERMANENT REPAIR WAS ACCOMPLISHED AS PER 7 47-200 SRM 51-40-09, FIG 2, TABLE 1 AND 747-200 SRM 51-40-12. ALSO, REFERENCE ATLAS AIR EO NR 4757A352. 2 L 7 4 4F A20WE 2007031500169 20070315 00169 NM 2007 3 15 UIEA200700137 1 20070310 A 5730 SKIN PANEL BOEING 747 747243B 1384830 NM RT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 RT WING UPPER TRAILING EDGE COMPOSITE PANEL HAS A 2.0 INCH CRACK, INBOARD OF INBOARD AILERON AT WBL 445.00, 10.0 INCHES FROM AFT EDGE. PERMANENT REPAIR WAS ACCOMPLISHED AS PER 747-200 SRM 51-40-09, FIG 2, TABLE 1 AND 747-200 SRM 51-40-12. ALSO, REFERENCE ATLAS AIR EO NR 4757A352. 2 L 7 4 4F A20WE 2007031500170 20070315 00170 NM 2007 3 15 UIEA200700110 1 20070306 A 5414 SKIN BOEING 747 7472D7B 1384803 NM NR 1 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 21784 NR 1 PYLON PRECOOLER EXHAUST CUT-OUT SKIN ASSEMBLY AND DOUBLER FOUND CRACKED. SKIN ASSEMBLY TRIMMED OFF FILLER FABRICAT ED AND INSTALLED AS PER BOEING MESSAGE 1-289015678-4 AND REMOVED FASTENERS INSTALLED AS PER BOEING MESSAGE 1-289015678-8 AND FAA FORM 8100-9. 2 L 7 4 4F RT A20WE 2007031500171 20070315 00171 NM 2007 3 15 UIEA200700126 1 20070302 A 5320 INTERCOSTAL BOEING 747 7472D3B 1384805 NM BS 420 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 UPPER DECK FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 420, LBL 50. U/DECK FLOOR SUPPORT INTERCOSTAL AT BS420, LBL 50 REPLA CED AS PER SRM 51-30-02. 2 L 7 4 4F RT A20WE 2007031500172 20070315 00172 NM 2007 3 15 UIEA200700127 1 20070302 A 5313 STRINGER BOEING 747 7472D3B 1384805 NM BS 978 S47L CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 FWD CARGO COMPARTMENT STA 978, STR 47L FOUND CORRODED. FWD CARGO COMPARTMENT STA978, STR47L REPLACED AS PER SRM 51-10-0 1. 2 L 7 4 4F RT A20WE 2007031500173 20070315 00173 EU 2007 3 15 2007UALA00675 1 20070305 A 2621 EXTINGUISHER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 411UA 464 NR 1 ENGINE FWD FIRE EXTINGUISHER BOTTLE SAFETY RELIEF VALVE FOUND WITH A METAL CAP STILL INSTALLED. [SUP 05-27-07] RE MOVED METAL CAP AND REINSTALLED FIRE EXTINGUISHER BOTTLE. AT THE PREVIOUS C-CHECK ON 9/13/2005, THE NR 1 ENGINE FWD BOTT LE WAS ACCIDENTALLY DISCHARGED AND REPLACED WITH A NEW ONE. INSPECTION OF THE NEW BOTTLE WAS INADEQUATE, ALLOWING THE AI RCRAFT TO RETURN TO SERVICE WITH THE METAL CAP LEFT ON THE RELIEF VALVE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007031500174 20070315 00174 NM 2007 3 15 2007UALA00676 1 20070306 A 7160 DUCT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE LOOSE A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 524UA 24977 717989 RTFL DUE TO SIGNIFICANT VIBRATION IN LEFT ENGINE AFTER TAKEOFF. COULD NOT ADVANCE POWER W/O VIBRATION INCREASING. 3RD STAGE LPT BLADE FRACTURED. THE 3RD STAGE LPT BLADES AND VANES WERE SULFIDED. DURING DISASSEMBLY A BOLT FOR THE OUTER DUCT WAS FOUND FRACTURED. THE LOOSE DUCT REDUCED AIRFLOW TO THE BLADES AND THE ON-GOING BLADE SULFIDATION CAUSED THE FA ILURE OF BLADE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007031600004 20070316 00004 NM 2007 3 16 AALA20070392 1 20070223 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 934AN 29531 MIA - FOUND EMERGENCY LIGHTS AT SEAT 7D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007031600005 20070316 00005 NM 2007 3 16 AALA20070403 1 20070225 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 DFW - FOUND EMERGENCY LIGHT AT SEAT 26G HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007031600006 20070316 00006 NM 2007 3 16 AALA20070406 1 20070226 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 358AA 24039 MIA - EMERGENCY LIGHT AT SEAT 20H BULKHEAD FORWARD OF SEAT INOPERATIVE. FOUND PIN PUSHED BACK. RESECURED PIN TO CONNECT OR FOR E EMERGENCY LIGHT AT SEAT 20H BULKHEAD FORWARD OF SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007031600007 20070316 00007 NM 2007 3 16 AALA20070396 1 20070224 A 2897 RELAY BOEING 737 737823 13844BZ NM BOOST PUMP INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 912AN 29513 IAH INFLIGHT T2163/24FEB - AFTER TAKEOFF LEFT TANK CONFIGURATION LIGHT ILLUMINATED. BOTH LEFT FUEL PUMPS BOTH RIGHT BOO ST FUEL PUMPS AND RIGHT CENTER FUEL PUMP WAS ON. LEFT CENTER PUMP AS PLACARDED INOPERATIVE AND OFF. COULD NOT MAINTAIN BALANCE USING STANDARD PROCEDURES. LANDED IAH WITHOUT INCIDENT. CHECKED OPERATION OF CROSSFEED SYSTEM AND BALANCED FU EL LOAD. SYSTEM GROUND CHECKED NORMAL OPERATION. REPLACED CENTER LEFT BOOST PUMP RELAY IN DCA ON 27 FEB 2007. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007031600008 20070316 00008 NM 2007 3 16 AALA20070397 1 20070224 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 772AN 29580 ORD- EMERGENCY EXIT CEILING LIGHT IN FIRST CLASS LEFT AISLE INOPERATIVE. RELAMPED EMERGENCY EXIT CEILING LIGHT IN FIRS T CLASS AT LEFT AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007031600009 20070316 00009 NM 2007 3 16 AALA20070400 1 20070225 A 2820 14057 VALVE BOEING 777 777223 1385213 NM FUEL DIST INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 767AJ 33539 DFW INFLIGHT - DURING CLIMB, RECEIVE ENGINE FUEL VALVE RT NR 4 EICAS MESSAGE. RETURNED TO DFW AND LANDED WITHOUT INCIDE NT. REPLACED SPAR RT VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007031600010 20070316 00010 NM 2007 3 16 AALA20070401 1 20070225 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 DFW - FOUND EMERGENCY LIGHT AT SEAT 23C HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007031600011 20070316 00011 NM 2007 3 16 AALA20070402 1 20070225 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 DFW - FOUND EMERGENCY LIGHT AT SEAT 20C HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007031600012 20070316 00012 WP 2007 3 16 AALA20070404 1 20070225 A 3397 WIRE HARNESS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 432AA 49350 LGA - FOUND EMERGENCY LIGHTS IN AFT STAIRWAY INOPERATIVE. REPLACED SPLICE ON HARNESS FOR EMERGENCY LIGHTS IN AFT STAIRW AY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007031600013 20070316 00013 EU 2007 3 16 AALA20070405 1 20070225 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 3075A 606 MIA - FOUND EMERGENCY LIGHT AT SEAT 29G INOPERATIVE. SECURED LOOSE CONNECTOR UNDER SEAT FOR EMERGENCY LINGT AT SEAT 29G . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007031600014 20070316 00014 NM 2007 3 16 AALA20070408 1 20070226 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 766AN 32880 MIA - EMERGENCY LIGHT AT SEAT 25C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT T00001SE 2007031600015 20070316 00015 EA 2007 3 16 SWIA200717999 1 20070305 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 764SK 10229 PAX DOOR FWD WEB CRACKED AT STEP 5 BASE END ADJACENT TO STEP 4 FROM THE BOTTOM, DISCOVERED DURING C-CHECK INSPECTION. I NSTALLED DOUBLER AND REPAIR ANGLES PER REO 690-52-11-104 REV B REPAIR ZONE 2 REO 670-52-11-104 REV B COMPLETE. 2 L 7 2 4F RT A21EA 2007031600016 20070316 00016 EA 2007 3 16 SWIA200718000 1 20070305 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 764SK 10229 PAX DOOR AFT WEB CRACKED AT STEP 4 BASE END, ADJACENT TO STEP 3 FROM THE BOTTOM AND STEP 5 AT THE BASE STEP 4 CRACKED, D ISCOVERED DURING C-CHECK INSPECTION. COMPLIED WITH REO 670-52-11-104 REV B. 2 L 7 2 4F RT A21EA 2007031600017 20070316 00017 SO 2007 3 16 SWIA200718001 1 20070312 A 3230 SEQUENCE VALVE EMB 120 EMB120ER 3260203 SO MLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 565SW 120340 LEFT MAIN GEAR DID NOT RETRACT PROPERLY WITH RED AND GREEN A&B REMAINING LIT. RETURNED TO FIELD. REPLACED BOTH LEFT GE AR DOOR SEQUENCE VALVES. OPERATIONAL CHECKS GOOD IAW 32-32-04. 2 L 7 2 4T RT A31SO 2007031600020 20070316 00020 SO 2007 3 16 SWIA200718004 1 20070211 A 5410 MOUNT EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 566SW 120341 RIGHT NACELLE DECK AT OUTBOARD AFT TAIL PIPE MOUNT CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ON R IGHT NACELLE DECK AT OUTBOARD AFT TAIL PIPE MOUNT PER SRM 54-20-01 AND RII 54-900-1000 AND SRM 51-40-02 . 2 L 7 2 4T RT A31SO 2007031600022 20070316 00022 SO 2007 3 16 SIMA200707101 1 20070310 A 3000 C1460093 ANTI-ICE VALVE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL NR 1 ENGINE FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 845AE 15396 1120 145685 CAE311166 ENGINE ONE ANTI-ICE MESSAGE, ATC DIVERSION, EMERGENCY DECLARED FOR LOW FUEL. REMOVED AND REPLACED ENGINE ONE ANTI-ICE V ALVE IAW EMB AMM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007031600023 20070316 00023 NM 2007 3 16 AALA20070409 1 20070226 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 766AN 32880 MIA - FOUND EMERGENCY LIGHT AT SEAT 25C HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007031600025 20070316 00025 EA 2007 3 16 SIMA200707202 1 20070312 A 2130 GG670980019 CONTROL PANEL CNDAIR CL600 CL6002C10 1390015 EA CABIN PRESSURE FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 522AE 7190 5666 10147 DURING CLIMB-OUT, HEARD A "POP" SOUND LIKE AN ELECTRICAL RELAY OPENING. ALL PASSENGER OXYGEN MASKS IN CABIN DEPLOYED FO LLOWED BY O2 SWITCH LIGHT. AIRCRAFT RETURNED TO DFW. REMOVED AND REPLACED CABIN PRESSURE CONTROL PANEL IAW CRJ AMM 21- 33-01. OPERATIONAL CHECK GOOD, PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007031600026 20070316 00026 SO 2007 3 16 SIMA200707104 1 20070309 A 3243 39807 CONTROL VALVE EMB 145 EMB145LR 3260212 SO BRAKES FAILED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 627AE 17546 145121 OUTBOARD BRAKE INOPERATIVE MESSAGE ON TAKEOFF ROLL, ABORTED TAKEOFF. REMOVED AND REPLACED OUTBOARD BRAKE CONTROL VALVE IAW EMB AMM TASK 32-41-06-000-801-A AND TASK 32-41-06-400-801-A. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007031600027 20070316 00027 NM 2007 3 16 AALA20070410 1 20070226 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 358AA 24039 MIA - FOUND EMERGENCY LIGHT AT SEAT 6H INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 6H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007031600028 20070316 00028 CE 2007 3 16 DXTA200702018 1 20070313 A 3230 SWITCH CESSNA 650 650 2076802 CE GARRTT TFE731 TFE7314R 01518 WP MLG CENTERING OUT OF ADJUST E DXTA A UNSCHED LANDING S J AFFECT SYSTEMS WARNING INDICATION CL CLIMB 1 GL 07 715QS 6507105 LANDING GEAR WOULD NOT RETRACT. AFTER TAKEOFF. GEAR HANDLE WOULD NOT MOVE. TROUBLESHOT TO NOSE CENTERING SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH IAW 650 MM 32-60-00. OPS CHECK GOOD IAW SAME. 2 L 7 2 4F 4 F A9NM E6WE 2007031600033 20070316 00033 NM 2007 3 16 WRLA2007045 1 20070312 A 5313 LONGERON DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE BS 1541 L52 CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271WA 48518 DURING C-04 CHECK, FOUND LONGERON L52 CORRODED STA Y=1541. REPAIRED PER MD-11 SRM VOL II 51-33-01 REV.38. 2 L 7 3 4F 4 F RT A22WE E24NE 2007031600035 20070316 00035 EU 2007 3 16 BAQA20070009 1 20070308 A 2497 BUSS TIE UROCOP EC135 EC135T1 5620026 EU SHORTED E BAQA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 03 135CJ 25 0495 INFLIGHT, BUSS TIE CAUTION LIGHT ILLUMINATED FOLLOWED BY GENERATOR DISCONNECT LIGHT AND SLIGHT ODOR OF ELECTRICAL BURNIN G. 1 G 7 2 3U H88EU 2007031600036 20070316 00036 WP 2007 3 16 ASAA0781503 1 20070227 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 950AS 53023 OVERHEAD OVERWING EMERGENCY EXIT LIGHT FOUND INOPERATIVE. REPLACED LIGHT BATTERY PACK. 2 L 7 2 4F RT A6WE 2007031600041 20070316 00041 NM 2007 3 16 AWXA200700354 1 20070219 A 5311 654795961 FRAME BOEING 737 7373S3 1384711 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND CORROSION AND CRACK ON AFT CARGO COMPARTMENT DOOR CUT OUT FORWARD FRAME, BS 794, S22R - S26R. REPAIRED AFT CARGO COMPARTMENT DOOR CUT OUT FORWARD FRAME, BS 794, S22R - S26R IAW AWA ER 03-5362-07072-SS2. 2 L 7 2 4F RT A16WE 2007031600043 20070316 00043 NM 2007 3 16 AWXA200700356 1 20070312 A 5320 6517684638 INTERCOSTAL BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND CRACKED INTERCOSTAL WEB, BS 294.5 - BS 303, S12L. REPLACED INTERCOSTAL BS 294.5 - BS 303, S12L IAW AWA ER 03-5312-07066-ES2. 2 L 7 2 4F RT A16WE 2007031600044 20070316 00044 NM 2007 3 16 AWXA200700357 1 20070312 A 5340 69489853 ATTACH FITTING BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND CRACKED INTERCOSTAL WEB CLIP, BS 360, S9L. REPLACED INTERCOSTAL WEB CLIP, BS 360, S9L IAW AWA ER 03-531 2-07066-ES2. 2 L 7 2 4F RT A16WE 2007031600049 20070316 00049 NM 2007 3 16 AWXA200700362 1 20070312 A 5340 69165096 STRINGER CLIP BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND CRACKED STRINGER CLIP, BS 348.20, S16L. REPLACED STRINGER CLIP, BS 348.20, S16L IAW AWA ER 03-5312-07066-E S2. 2 L 7 2 4F RT A16WE 2007031600050 20070316 00050 NM 2007 3 16 AWXA200700363 1 20070312 A 5340 69265553 STRINGER CLIP BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND CRACKED CLIP, BS 348.20 - S16L. REPLACED CLIP, BS 348.20 - S16L IAW AWA ER 03-5312-07066-ES2. 2 L 7 2 4F RT A16WE 2007031600052 20070316 00052 EU 2007 3 16 AWXA200700365 1 20070306 A 5347 D5311209220539 SEAT TRACK AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 627AW 66 SAL - FOUND CORROSION ON MAIN CABIN SEAT TRACK, FR 21 + 12" AND FR 20 + 1", -Y765 . REPLACED MAIN CABIN SEAT TRACK, FR 20 - FR 24, -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007031600053 20070316 00053 NM 2007 3 16 P5CA0701514 1 20070125 A 5200 HANDLE BOEING 747 74746NF 13848BT NM DOOR UNSECURE A P5CA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 451PA 30809 HIGH SPEED REJECT DUE TO OVERHEAD DOOR OPEN INDICATION. INSIDE HANDLE WAS AJAR. CHECKED OPERATION OF HANDLE AND HATCH. OPERATION NORMAL. 2 L 7 4 4F RT A20WE 2007031600058 20070316 00058 NM 2007 3 16 07FDEA00831 1 20070314 A 5753 SUPPORT BRACKET BOEING 727 727225 1384077 NM NR 2 FLAP TRACK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 NR 2 FLAP TRACK AFT SUPPORT BRACKET IS CRACKED OTBD AFT END. REMOVED AND REPLACED BRACKET IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2007031600061 20070316 00061 EU 2007 3 16 07FDEA00834 1 20070314 A 5753 SLAT TRACK AIRBUS 310 A310324 3930206 EU ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CORROSION ON SLAT TRACK NR 7 INBOARD AT INNER LOWER SKIN. REPAIR PERFORMED IAW EA 6-5720-103412. 2 L 7 2 4F RT A35EU 2007031600063 20070316 00063 WP 2007 3 16 07FDEA00836 1 20070314 A 5315 ADA364515 FLOORBEAM DOUG DC10 DC1010 3022110 WP ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 397FE 46631 DURING ACF MODIFICATION, FOUND TO FWD CARGO COMPARTMENT BILGE STA 1090 FLOORBEAM WITH CRACK 2" LONG. REPLACE FLOORBEAM FOR SRM 51-31-01 VOIL II P/N AFA0039-5N E TEE ADA3645-15. 2 L 7 3 4F A22WE 2007031600064 20070316 00064 WP 2007 3 16 07FDEA00837 1 20070314 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 397FE 46631 DURING ACF MODIFICATION, FOUND TO AFT PRESSURE BULKHEAD AT STA 595 LONG 9 LT WITH CRACK 1". REPLACED LONGERON CLIP FOR SRM 51-31-01 VOL II. 2 L 7 3 4F A22WE 2007031600065 20070316 00065 WP 2007 3 16 07FDEA00838 1 20070314 A 5510 SUPPORT DOUG DC10 DC1010 3022110 WP ZONE 300 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 397FE 46631 DURING ACF MODIFICATION , FOUND ON HORIZ STAB ON SUPPORT NOTED 1 HOLE OVALIZATION DIA, 0.2720" HOLE NOMINAL: 0.1870". R EPAIRED FOR EA FEDEX 8-5340-97792 REV A DATE 02-02-07. 2 L 7 3 4F A22WE 2007031600067 20070316 00067 NM 2007 3 16 S2YA07002 1 20070223 A 4990 38004983 APU DORNER DO32 DO328300 NM APU BAY OIL CONSUMPTION A S2YA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 352 11432 435 3111 DURING CLIMBOUT OF FLIGHT 2189 MKE-CLE THE CREW NOTE AN AMBER APU LIMIT EXCEEDANCE MESSAGE. THE SYSTEMS PAGE INDICATED LOW OIL PRESSURE. IT WAS DETERMINED THAT SINCE THE RIGHT DC GENERATOR WAS ALREADY ON MEL THAT THE AIRCRAFT WOULD HAVE T O RETURN TO MKE. THE CREW PERFORMED AN AIR TURNBACK TO MKE. MAINTENANCE REPLACED THE APU AND RETURNED THE AIRCRAFT TO SERVICE. 2 H 7 2 4T RT A55NM 2007031600068 20070316 00068 NM 2007 3 16 07FDEA00840 1 20070314 A 5330 6554585 SKIN BOEING 727 727225 1384077 NM BS 720C-720D MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 463FE 22551 FOUND EXTERNAL REPAIR APPROX BETWEEN STA 720C AND 720D, BETWEEN STR 7R-8R, TO BE INSTALLED WITH BLIND FASTENERS, AND DOU BLER ENDS ON STRUCTURE. REMOVED AND REPLACED DOUBLER BETWEEN STA 720C AND 720D. SEALED AND PAINTED. REF SRM 53-30-3 F IG 1. 2 L 7 3 4F A3WE 2007031600070 20070316 00070 EU 2007 3 16 07FDEA00843 1 20070314 A 5330 SKIN AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 412FE 360 AVIONICS BAY HAD A 2.5" BY 1.5" AREA OF CORROSION BETWEEN FRAMES 17 AND 18 AND STRINGERS 50L AND 51L. CORROSION OUT OF LIMITS. COMPLIED WITH EA 6-5330-107691. 2 L 7 2 4F RT A35EU 2007031600074 20070316 00074 NM 2007 3 16 ASAA0741506 1 20070309 A 5753 SKIN BOEING 737 7374Q8 138447Q NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 THE LEFT I/B FORE FLAP LWR SURFACE HAS MULTIPLE DENTS. PREPARED FORE FLAP ASSY LWR SURFACE FOR BONDING FABRICATED AND I NSTALLED TWO REPAIR DOUBLERS IAW SRM 51-70-10 PARA 7, 8, 12, 15, 18 AND 20. 2 L 7 2 4F RT A16WE 2007031600075 20070316 00075 NM 2007 3 16 ASAA0741507 1 20070309 A 5755 654645267 SKIN BOEING 737 7374Q8 138447Q NM NR 4 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 THE LEFT NR 4 SPOILER HAS MULTIPLE DENTS ON THE LWR SURFACE FROM THE PANEL CENTER TO THE I/B EDGE. PREPARED THE LWR SUR FACE OF THE SPOILER PANEL FOR BONDING FABRICATED AND INSTALLED TWO REPAIR DOUBLERS IAW SRM 51-70-10 REPAIR 4. 2 L 7 2 4F RT A16WE 2007031600077 20070316 00077 NM 2007 3 16 ASAA0741510 1 20070309 A 5522 65C2575376 SKIN BOEING 737 7374Q8 138447Q NM RT ELEVATOR PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 THE RIGHT ELEVATOR IS PUNCTURED ON THE UPPER SURFACE 5 INCHES FROM THE T/E AT STA 110. REMOVED THE DAMAGED PLIED FROM T HE UPPER SKIN PANEL PREPARED AND APPLIED REPAIR PLIES IAW SRM 51-70-04 PG 4, 33, 37 AND 55-20-01 FIG 201. 2 L 7 2 4F RT A16WE 2007031600079 20070316 00079 EU 2007 3 16 AWXA200700366 1 20070310 A 5321 D5367180500400 FLOOR PANEL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 672AW 2193 SAL - FOUND CORROSION ON L2 DOOR WAY FLOOR PANEL 261 FF, FR 66 - FR 68, +Y1550. REPLACED L2 DOOR WAY FLOOR PANEL 261 F F, FR 66 - FR 68, +Y1550 IAW AWA TASK CARD C1C53303. 2 L 7 2 4F RT A28NM 2007031600082 20070316 00082 EU 2007 3 16 USAA070173 1 20070309 A 5322 D5347112420000 SHEAR TIE AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 167US 1442 LEFT SHEAR TIE FR 70, Y1292 HAS CORROSION. REMOVED AND REPLACED SHEAR TIE PER SRM 51-72-11, CORR TASK JA-260-53500; LEV EL 1, DEFECT SIZE: 2 SQ INCHES. 2 L 7 2 4F RT A28NM 2007031600083 20070316 00083 EU 2007 3 16 USAA070172 1 20070309 A 5315 D5311282600101 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSLEAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 167US 1442 FLOORBEAM AT Y505 HAS CORROSION. REMOVED & REPLACED BEAM PER SRM 51-72-11; CORR TASK JA-220-53500; LEVEL 1, DEFECT SI ZE: 1 X 8 INCHES. 2 L 7 2 4F RT A28NM 2007031600085 20070316 00085 EU 2007 3 16 USAA070170 1 20070309 A 5315 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 167US 1442 RIGHT FLOORBEAM -Y1732 AT FR 66 AT NUT PLATE HOLE HAS CORROSION. INSTALLED NEW REPAIR ANGLES & FILLER PER SRM 53-41-14; CORR TASK JA-260-53500, LEVEL 1, DEFECT SIZE: 0.750 X 0.750 INCH. 2 L 7 2 4F RT A28NM 2007031600087 20070316 00087 EA 2007 3 16 A6WA200740091 1 20070304 A 2700 FLT CONTROLS CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE UNKNOWN A A6WA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 31 470ZW 7927 ABORTED TAKEOFF AT 110 KNOTS. FLIGHT CONTROLS FELT UNRESPONSIVE IN ROLL, CONTROL YOKE FULL LT DEFLECTION, AIRCRAFT STIL L WANTED TO ROLL RT. MAX BTMS = 5, TOW =40,800. INSPECTED AILERON RUDDER, ELEVATOR FLAPS, SPOILERONS, STAB TRIM, RUDDE R TRIM AND AILERON TRIM FOR TRAVEL AND OPERATION. CHECKED HYDRAULIC FLUID LEVELS AND ALL CIRCUIT BREAKERS IN-CHECK GOOD . ALL FLIGHT COTROLS OPERATE NORMAL. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007031600091 20070316 00091 NM 2007 3 16 SWAA071356 1 20070313 A 5754 SKIN BOEING 737 7373H4 1384600 NM NR 4 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN PA774 27694 DURING SCHEDULED C2 CHECK, FOUND NR 4 L/E SLAT DELAMINATED AT INBOARD UPPER SURFACE WEDGE. REMOVED AND REPLACED NR 4 L/ E SLAT PER MM. 2 L 7 2 4F RT A16WE 2007031600092 20070316 00092 WP 2007 3 16 UPS07849367 1 20070213 A 5730 5611360167 SKIN DOUG DC8 DC871F 302199D WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 LEFT WING UPPER SKIN AT XW 408 TP CANT 508 BETWEEN STR 6 AND REAR SPAR REQUIRES REPAIR. REPAIR WING UPPER SKIN IAW SAA EA 008-5730-01-A0660 AND UPS EO DC8-5 730-26300-A. 2 L 7 4 4F RT 4A25 2007031600093 20070316 00093 WP 2007 3 16 UPS07849370 1 20070217 A 5315 9753798503 FLOORBEAM DOUG DC8 DC871F 302199D WP FS 1260 LBL 59 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C3 HEAVY CORROSION & EXFOLIATION ON AFT SIDE OF FLOORBEAM, C-PIT TUNNEL LT SIDE STA 1260 LBL 59. REPAIR ED FLOORBEAM AT STA 1260 LBL 59 IAW SAA EA 008-5310-01-A0693 UPS RAA DC8-53-20612, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007031600096 20070316 00096 WP 2007 3 16 UPS07849405 1 20070221 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C1 EXTERIOR FUSELAGE, L-1 DOOR HOLD OPEN RECEPTICAL CUTOUT HAS .375 INCH CRACKED IN AFT LWR CORNER. TRI MMED OUT DAMAGED AREA L-1 DOOR HOLD OPEN CUTOUT AFT LWR CORNER IAW SRM ADDENDUM DC8-5330-19684-A. FABRICATED AND INSTAL LED REPAIR DOUBLER AT THE L-1 DOOR HOLD OPEN CUTOUT AFT LWR CORNER IAW SRM ADDENDUM DC8-5330-19684-A. 2 L 7 4 4F RT 4A25 2007031600098 20070316 00098 WP 2007 3 16 UPS07849409 1 20070306 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C1 EXFOLIATED CORROSION ON WEB AT STA -99 - -80 RBL 30-50. REMOVED CORROSION ON WEB AT STA -99 TO -80 R BL 30-50 IAW SRM 51-1-8 FABRICATED AND INSTALLED SPLICE DOUBLER AND REPAIR DOUBLER AT STA -80 TO -90 RBL 30-50 IAW SRM 5 1-1-20D, AND DWG 5612298. 2 L 7 4 4F RT 4A25 2007031600099 20070316 00099 WP 2007 3 16 UPS07849410 1 20070220 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FS1618 L15R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C1 R2 DOOR JAMB WEB CRACKED, 2 PLACES, AT DOOR SNUBBER, STA 1618 L15R TO L16R. REMOVED WEB FROM R2 DOOR JAMB AT FS 1618 L15R-L16R IAW SRM 51-1-21. FABRICATED AND INSTALLED WEB AT STA 1618 L15R-L16R IAW DWG 5772656 AND SRM 51-3-2 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007031600101 20070316 00101 NM 2007 3 16 UPS07M49374 1 20070118 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1239-1321 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C MAIN DECK: BS 1239 TO BS 1321 RT MOST O/B SEAT TRACK FLANGE AREAS AND CROWN AREAS CORRODED. REMOVED SEAT TRACK FROM BS 1229-1371 RT MOST O/B PER SRM 51-31-01V2.R.38. REWORKED NEW SEAT TRACK & PICKED UP HOLES & PAINTED P ER SRM 51-21-01V2 R38, NEW SEAT TRACK, OK TO INSTALL. NEW SEAT TRACK, INSTALLED PER SRM 53-70-00 F1 V1R 38, FOUND SATIS FACTORY. 2 L 7 3 4F RT A22WE 2007031600103 20070316 00103 NM 2007 3 16 AWXA200700344 1 20070212 A 5310 65C80735183 DOOR FRAME BOEING 737 7373S3 1384711 NM BS 442 S24R CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND FORWARD CARGO DOOR, FORWARD FRAME CRACKED, BS 442.55, S24R. REPLACED FORWARD CARGO DOOR, FORWARD FRAME, BS 442.55, S24R IAW B737-300 SRM 51-40-04 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007031600104 20070316 00104 NM 2007 3 16 AWXA200700345 1 20070213 A 5330 654576987 SKIN BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND FUSELAGE SKIN CRACKED, BS 414, S2R. REPAIRED FUSELAGE SKIN, BS 414, S2R IAW AWA TASK CARD M2A53002. 2 L 7 2 4F RT A16WE 2007031600105 20070316 00105 NM 2007 3 16 AWXA200700346 1 20070306 A 5311 65207235 FRAME BOEING 737 7373S3 1384711 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND FRAME UPPER INNER FLANGE STRAP CRACKED, BS 492, S22R. REPLACED FRAME UPPER INNER FLANGE STRAP, BS 492, S22R IAW B737-300 SRM 51-40-02 AND 51-40-05. 2 L 7 2 4F RT A16WE 2007031600118 20070316 00118 SO 2007 3 16 SIMA200707102 1 20070311 A 2150 8151138 COUPLING EMB 135 EMB135LR 3260305 SO ACM BLOWN A SIMA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SW 21 729AE 14458 145343 LOW PITCH VIBRATION HEARD CYCLING ON AND OFF IN FLIGHT COMING FROM AIR CYCLE MACHINE AREA. REMOVED AND REPLACED COUPLIN G AT NUMBER TWO INLET TO DUAL TEMPERATURE CONTROL VALVE IAW EMB AMM 21-51-03. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007031600122 20070316 00122 NM 2007 3 16 USAA200703001 1 20070312 A 5512 SKIN BOEING 737 7374B7 1384702 NM HORIZONTAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 441US 24812 A 2.25 INCH CRACK FOUND AT LT HORIZONTAL STAB LWR SKIN STA 115. INSTALLED DOUBLER PER SRM 55-10-01. 2 L 7 2 4F RT A16WE 2007031900001 20070319 00001 NM 2007 3 19 UPS07449412 1 20070217 A 5312 PRESSURE PANEL BOEING 747 747121 1384871 NM LT MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT BODY LANDING GEAR W/W PRESSURE DECK ATT WEB FOUND SURFACE CORROSION AT STA 1403 LBL 125. CORROSI ON BLEND OUT 0.034 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. LEFT BODY LANDING GEAR W/W PRESSURE DECK ATT WEB REPA IRED AT STA 1403 LBL 125 AREA AS PER SRM 53-10-07 FIG 2, SUBSEQUENT INSPECTION IS REQ'S AS PER SRM 53-10-07 FIG 2 SHT 7 TABLE 2. 2 L 7 4 4F A20WE 2007031900002 20070319 00002 NM 2007 3 19 UPS07449416 1 20070216 A 5310 65B05091847 DOOR FRAME BOEING 747 747121 1384871 NM L5 DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D L5 DOOR UPPER FRAME FOUND CRACKED AT SEVERAL FASTENER HOLE AREA. CRACK LENGTH .375 INCH. M/D L5 DOOR UPPER FRAME REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02. 2 L 7 4 4F A20WE 2007031900003 20070319 00003 NM 2007 3 19 UPS07449417 1 20070213 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 860 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 860 LBL 80-97 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.040 X 2 X 2 INCHES EXCEED SRM 53 -10-01 FIG 1 LIMITS. M/D BS 860 LBL 65 TO MOST LEFT O/B FLOORBEAM REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 5 1-30-02. 2 L 7 4 4F A20WE 2007031900005 20070319 00005 NM 2007 3 19 UPS07449419 1 20070216 A 5710 SHEAR TIE BOEING 747 747121 1384871 NM LWS 469 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT WING WS 469.8 FWD OF UPPER STR 29 SHEAR TIES FOUND CRACKED AS MARKED. CRACK LENGTH .5 INCH. LEF T WING WS 469.8 FWD OF UPPER STR 29 SHEAR TIE REPAIRED AS PER SRM 57-10-05 FIG 7. 2 L 7 4 4F A20WE 2007031900006 20070319 00006 NM 2007 3 19 UPS07449420 1 20070213 A 5311 65B01711638 FRAME BOEING 747 747121 1384871 NM BS 360 S14-16R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 360 STR 14-16R FRAME AFT FACE O/B AREA FOUND CRACKED. CRACK LENGTH .375 & .25 INCH. M/D BS 36 0 STR 13R TO STR 18R FRAME REPAIRED AS PER SRM 51-40-03 FIG 2. 2 L 7 4 4F A20WE 2007031900008 20070319 00008 NM 2007 3 19 UPS07449422 1 20070213 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 340 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT BS 340 U/D FLOORBEAM UPPER CHORD TO FRAME CONNECTION AREA FOUND 1EA FASTENER HOLE CRACKED AT U/D FLOORBEAM WEB APPROX .125 INCH. RIGHT BS 340 U/D FLOORBEAM WEB REPAIRED AS PER SRM 53-10-07 FIG 11, JUST BETWEEN RBL 5 2 AND RIGHT MOST O/B END. 2 L 7 4 4F A20WE 2007031900009 20070319 00009 NM 2007 3 19 UPS07449423 1 20070227 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 820-840 S10R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 820-840 S10 RIGHT STRINGER ATT WEB FOUND CRACK. CRACK LENGTH .625 INCH. M/D BS 820-840 STR 10 R ATTACH WEB REPAIRED AS PER SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 2007031900011 20070319 00011 NM 2007 3 19 UPS07449425 1 20070227 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 820-840 S10L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 820-840 STR 10 LT STRINGER ATT WEB FOUND CRACKED. CRACK LENGTH .75 INCH. M/D BS 820-840 STR 1 0 LT ATTACH WEB REPAIRED AS PER SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 2007031900012 20070319 00012 EA 2007 3 19 COMA0760248 1 20070312 A 7830 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER UNKNOWN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 914CA 7012 FLIGHT 5122 - LEFT REV UNLOCK MASTER CAUTION CAME ON AFTER TAKEOFF. AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. D EFERRED PER MEL 78-30-01. 2 L 7 2 4F RT A21EA 2007031900013 20070319 00013 EA 2007 3 19 COMA0760249 1 20070313 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 783CA 19835 7315 FLIGHT 5443 - HYD PUMP 3A HIGH TEMP, FOLLOWED QRH HYD PUMP 3A OFF 3B ON THEN RECEIVED GEAR DISAGREE WARNING DURING GEAR EXTENSION WITH 3B HYD PUMP ONLY. REMOVED AND REPLACED HYD PUMP 3B FOR GEAR DISAGREE. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007031900014 20070319 00014 EA 2007 3 19 COMA0760251 1 20070313 A 2760 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA SPOILER UNKNOWN A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 815CA 7397 FLIGHT 5429 - CONFIG SPOILER MESSAGE ON TAKEOFF ROLL. ABORTED TAKEOFF AT 20 KTS, RETURNED TO GATE. PERFORMED FIM RESET AND PERFORMED SPOILER TEST AND GROUND FUNCTIONAL CHECK. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007031900015 20070319 00015 NM 2007 3 19 UPS07449426 1 20070213 A 5320 STIFFENER BOEING 747 747121 1384871 NM BS 1500 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D STA 1500 RBL 58 FLOOR SUPPORT INTERCOSTAL WEB ATT STIFFENER FOUND CRACKED. CRACK LENGTH .25 INCH. SUPPORT STIFFENER REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007031900018 20070319 00018 WP 2007 3 19 UPS07849413 1 20070213 A 5711 FRAME DOUG DC8 DC871F 302199D WP RWS 252 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C3 CRACK IN DRILL START IN FRAME ON OUTBOARD LWR SIDE OF NR 3 ENG STUB WING. STOP DRILLED CRACK IN FRAM E AT RIGHT STUB WING STA 252.351 IAW SRM 54-2-0, AND SRM TR 54-38. FABRICATED AND INSTALLED REPAIR ANGLE AND DOUBLER AT RIGHT STUB WING STA 252.351 IAW DWG 97532964, AND SRM 54-2-0 FIG 3 AND SRM TR 54-40. 2 L 7 4 4F RT 4A25 2007031900020 20070319 00020 WP 2007 3 19 UPS07849428 1 20070314 A 3350 LIGHT DOUG DC8 DC871F 302199D WP COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 750UP 45950 ON CREW PREFLIGHT, FOUND EMERGENCY LIGHTS INOP AWAITING CLOSING LP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT IAW MM 33 -50-01-2. CHECKS GOOD. 2 L 7 4 4F RT 4A25 2007031900021 20070319 00021 NM 2007 3 19 UPS07M49415 1 20070313 A 3350 BATTERY DOUG MD11 MD11F 3023600 NM EMERGENCY LIGHTS DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 285UP 48457 PREFLIGHT - WHEN TESTING EMERGENCY LIGHT SYSTEM, MESSAGE SAYS -NO 1 BAT LO-. REMOVED AND REPLACED EMERGENCY LIGHTS POWE R SUPPLY PER AMM 33-51-01-4. FOLLOWED FIM 33-51-02-00. REMOVED AND REPLACED MSC PRECAUTIONARY AS PER AMM 31-42-01-4. EMERGENCY LIGHTS AND MSC TEST GOOD. 2 L 7 3 4F RT A22WE 2007031900023 20070319 00023 EA 2007 3 19 TRAX200700341 1 20070311 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 928EV 8006 CABIN AFT MOST CEILING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007031900026 20070319 00026 EA 2007 3 19 TRAX200700346 1 20070312 A 5260 BRACKET CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 ASD AFT TREAD SKIN TO INNER SKIN L-BRACKET CRACKED IN A PREVIOUSLY REPAIRED AREA, LOCATION MARKED. 2 L 7 2 4F RT A21EA 2007031900027 20070319 00027 EA 2007 3 19 TRAX200700347 1 20070311 A 2760 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA SPOILERS UNKNOWN A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 354CA 10064 OUTBOARD SPOILERONS & OUTBOARD FLT SPLRS CAUTION MSG. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007031900028 20070319 00028 EA 2007 3 19 COMA0760252 1 20070313 A 2740 SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM DIRTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 685BR 7712 FLIGHT 5266 - ON CLIMBOUT STAB AND MACH TRIM ABNORMAL MESSAGES. RAN QRH, NO CHANGE. AIRCRAFT RETURNED BACK TO RIC AND LANDED SAFELY. CLEANED STAB TRIM DISCONNECT SWITCHES ON BOTH YOKE ASSEMBLIES. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2007031900029 20070319 00029 2007 3 19 YENA2007016 4 20070228 A 2330 3042865102 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU ROW 1DEF ODOR A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 15 586JB 16060 12965 2160 FLT 718, SJU TO JFK, PRIOR TO TOP OF DESCENT. F/A REPORTED BURNING SMELL IN AREAS OF ROW 1-5 AIRCRAFT RIGHT. REQUESTED LIVE TV TO BE SHUT OFF. SMELL DISAPPEARED. C/W TSM 23-39-00-810-801. REMOVED AND REPLACED VDU'S AT 1DEF AND SEB AT R OW 1 RT AS PRECAUTIONARY IAW LTV MM 23-39-00. OPS CHECK OK. 2 L 7 2 4F RT A28NM 2007031900030 20070319 00030 EA 2007 3 19 COMA0760253 1 20070314 A 5340 88308 POST CNDAIR CL600 CL6002B19 1900309 EA BS 559 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 938CA 7046 DURING INSPECTION FOUND BULKHEAD POST LOWER END CRACKED, FS 559, RBL 9. REMOVED DAMAGE AND INSTALLED DOUBLER PER BOMBAR DIER REO 601R-53-41-057. 2 L 7 2 4F RT A21EA 2007031900031 20070319 00031 NM 2007 3 19 CALA0700128 1 20070315 A 5330 6555074 SKIN BOEING 737 7373T0 1384582 NM BS 211-219 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 77303 23354 INSPECTION FOUND A .5 INCH CRACK AT UPPER O/B CORNER OF FLIGHT COMPARTMENT R-1 WINDSHIELD CUTOUT, STA 211.8-219.8, S5R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-10-01. 2 L 7 2 4F RT A16WE 2007031600069 20070316 00069 EU 2007 3 16 07FDEA00842 1 20070314 A 5330 SKIN AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 412FE 360 AVIONICS BAY SKIN FWD OF FRAME 17 BETWEEN STRINGERS 48L AND 50L HAS 5" BY 5" AREA OF CORROSION AREA OUT OF LIMITS. COMP LIED WITH EA 6-5330-107691. 2 L 7 2 4F RT A35EU 2007031600071 20070316 00071 EU 2007 3 16 07FDEA00844 1 20070314 A 5410 FERRULE AIRBUS 310 A310203 3930313 EU NR 1 PRECOOLER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 412FE 360 NR 1 PYLON PRECOOLER FERRULE PAN CRACKED BETWEEN RIBS 4 AND 8. ACCOMPLISHED PERMANENT REPAIR IAW SB A310-54-2028. 2 L 7 2 4F RT A35EU 2007031600072 20070316 00072 EU 2007 3 16 07FDEA00845 1 20070314 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 412FE 360 PREVIOUS REPAIR ON CABIN FLOORBEAM FRAME 37 REPAIR ANGLES IMPROPERLY INSTALLED. CORRECTED REPAIR IAW EA 6-5310-107701. 2 L 7 2 4F RT A35EU 2007031600073 20070316 00073 NM 2007 3 16 ASAA0741505 1 20070309 A 5754 STRUCTURE BOEING 737 7374Q8 138447Q NM TE FLAP DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 THE RIGHT O/B AFT FLAP IS DAMAGED ON THE O/B TRAILING EDGE. REMOVED DAMAGED AREA OF T/E ASSY SKIN AND CORE FABRICATED A ND INSTALLED A CORE REPAIR SECTION SKIN FILLER AND DOUBLER IAW SRM 51-70-10 PARA 7, 8, 9, 11, 15, 18 AND 20. 2 L 7 2 4F RT A16WE 2007031600076 20070316 00076 NM 2007 3 16 ASAA0741509 1 20070309 A 5522 65C2575362 SKIN BOEING 737 7374Q8 138447Q NM RT ELEVATOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 THE RIGHT ELEVATOR IS DENTED ON THE LWR SURFACE I/B OF THE NR 5 HINGE. REMOVED DAMAGED PLIES FROM LWR SKIN PNL, PREPARE D AND APPLIED REPAIR PLIES IAW SRM 51-70-04 PG 4, 33, 37 AND 55, 20, 01 FIG 201. 2 L 7 2 4F RT A16WE 2007031600078 20070316 00078 NM 2007 3 16 ASAA0741511 1 20070309 A 5523 65C2579718 TAB BOEING 737 7374Q8 138447Q NM RT ELEVATOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 THE RIGHT ELEVATOR TAB UPPER SURFACE IS CRACKED AT THE I/B SIDE OF THE SECOND FROM O/B HINGE CUTOUT. PREPARED THE DAMAG ED SURFACE FOR BONDING PREPARED AND APPLIED GRAPHITE REPAIR PLIES IAW SRM 51-70-17 REPAIR 11. 2 L 7 2 4F RT A16WE 2007031600080 20070316 00080 NM 2007 3 16 AWXA200700353 1 20070311 A 3240 CZ9DM6A TRANSDUCER AIRBUS A319 A319132 3930340 NM RT MLG BRAKE FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 WP 28 802AW 924 LAS - DIVR - DURING APPROACH, THE CREW DISCOVERED THE RIGHT BRAKE PRESSURE INDICATED 500 PSI - 3000 PSI. THE CREW DIVER TED TO LAX, DECLARED AN EMERGENCY. THE PAX DID NOT BRACE. THE LANDING WAS UNEVENTFUL. MX REPLACED 62GG ALTERNATE BRAK E TRANSDUCER IAW AMM 32-44-18. OPERATIONAL CHECK WAS GOOD. THE A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2007031600081 20070316 00081 2007 3 16 DXTA200702020 4 20070314 A 2210 TRIM SYSTEM GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE PITCH UNKNOWN E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 708QS 069 DURING CLIMB WITH THE AUTOPILOT ENGAGED THE AUTOPILOT DISENGAGED ALONG WITH ILLUMINATION OF THE A/P PITCH TRIM CAUTION M ESSAGE 3 TIMES AFTER THE THIRD FAILURE THE PRIMARY PITCH TRIM WOULD NOT FUNCTION. PERFORMED HORIZONTAL TRIM SYSTEM FUNC TIONAL TEST AND RAN OUT SYSTEM WIRING FINDING NO DEFECTS. APPLIED HYDRO AND REPEATED ABOVE TESTS WITH NO DEFECTS NOTED. REF: G200 WO 27-40-11 AND G200 MM 27-40-00. SEE GAC SAV WO SC108327-6.1 2 L 7 2 4F 4 F RT A53NM E35NE 2007031600084 20070316 00084 EU 2007 3 16 USAA070171 1 20070309 A 5315 D5311281820401 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 167US 1442 SEVERAL AREAS, FLOORBEAM AT Y254 BETWEEN FR C14 & C23 HAS CORROSION. REMOVED & REPLACED BEAM PER SRM 51-72-11; CORR TAS K JA-220-53500, DEFECT SIZE: 1 X 1 INCH. 2 L 7 2 4F RT A28NM 2007031600088 20070316 00088 NM 2007 3 16 BB07023 1 20070312 A 3397 WIRE BOEING 767 7672B7 1385107 NM EMERGENCY LIGHTS BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AY 24764 PHL - MAINTENANCE REPORTED THE AFT LEFT-HAND SIDE OF LOW LEVEL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND A WIRE B ROKEN AT LIGHT CONNECTION. REPAIRED WIRE AND REINSTALLED LIGHT COVER. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A1NM 2007031600089 20070316 00089 NM 2007 3 16 SWAA071372 1 20070313 A 5340 6557463 ATTACH FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED BRDG CHECK, L1 DOOR EVACUATION SLIDE GIRT BAR AFT FLOOR ATTACH FITTING CORRODED. REMOVED AND REPLACED AFT FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007031600090 20070316 00090 NM 2007 3 16 SWAA071361 1 20070313 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM BS 360 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031600094 20070316 00094 WP 2007 3 16 UPS07849371 1 20070213 A 5343 BOSS DOUG DC8 DC871F 302199D WP SHOCK STRUT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP UP36617 45938 INSPECTION TYPE:C3 LEFT MLG RETRACT PIN BOSS HAS PITTING AND TOOLING MARKS. REMOVED AND REPLACED LEFT MLG SHOCK STRUT A SSY IAW 32-11-00, RETRACT AND EXTENSION CHECKS GOOD IAW 32-11-00. 2 L 7 4 4F RT 4A25 2007031600095 20070316 00095 WP 2007 3 16 UPS07849372 1 20070215 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FS 280 RBL 48 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C3 CRACKED END FITTING ON FLOORBEAM AT STA 280, RBL 48 A-PIT DOORWAY UPPER FWD CORNER REMOVED FLOORB EAM END FITTING AT STA 280, RBL 48 A-PIT DOORWAY UPPER FWD CORNER IAW SRM 51-1-20D. FABRICATED AND INSTALLED FLOORBEAM END FITTING AT STA 280 RBL 48 IAW DWG 974022 AND SRM 51-3-2 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007031600097 20070316 00097 WP 2007 3 16 UPS07849408 1 20070222 A 5340 ATTACH FITTING DOUG DC8 DC873F 302199F WP FS 857 L19R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C1 MAIN CABIN ATTACH FITTING CRACKED AT STA 857.125 L19R. REMOVED FITTING AT STA 857.125 L19R IAW SRM 5 1-1-20D. FABRICATED AND INSTALLED REPAIR FITTING AT STA 857.125 L19R IAW SRM 51-03-02 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007031600100 20070316 00100 NM 2007 3 16 UPS07M49373 1 20070201 A 5311 AGA71704 FRAME DOUG MD11 MD11F 3023600 NM BS 1841 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C CTR CARGO BILGE AREA STA 1841 FRAME WEB ABOVE LONGERON 45R FOUND CRACKED AS MARKED. ATTACHED CRACK WE B SUPPORTS & FASTENERS REMOVED FOR ACCESS. NEW WEB P/B AGA7170-4 FAB & FASTENERS HOLE PICKED UP PER SRM 51-31-01V 2 REV 38. REWORKED & PAINTING CUTOUT ON NEW WEB FOUND SATISFACTORY & OK TO INSTALL. NEW WEB INSTALLED PER SRM 51-31-01 V2 R3 8, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007031600102 20070316 00102 NM 2007 3 16 UPS07M49375 1 20070126 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM BS 1119 L51R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C FWD CARGO COMPT FROM BS 1119 (BS 6-00) TO BS 6-10, LONGERON 51R FOUND CORRODED. LONGERON & ATTACHED P ARTS REMOVED FOR ACCESS PER SRM 51-31-01V2 R38. REPAIR LONGERON & FAB PER SRM 53-10-01 V1 R38. REPAIR PARTS PROTECTED PER SRM 51-21-01V2 R38. REPAIRED LONGERON, OK TO INSTALL PER SRM 53-10-00 F2V1 R38. 2 L 7 3 4F RT A22WE 2007031600106 20070316 00106 NM 2007 3 16 AWXA200700347 1 20070216 A 5414 301A10701 SKIN BOEING 737 7373S3 1384711 NM ZONE 400 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - NR 2 PYLON STRUT SKIN CRACKED, EXTENDS BEYOND STOP DRILL HOLE, AT PANEL NR 5828R, NAC STATION 196.70 -NAC STATION 254.525. REPAIRED NR 2 PYLON STRUT SKIN, NAC STATION 196.70 -NAC STATION 254.525 PER AWA ER 03-5400-07065-SS3. 2 L 7 2 4F RT A16WE 2007031600107 20070316 00107 NM 2007 3 16 AWXA200700348 1 20070216 A 5744 65C252466 FITTING BOEING 737 7373S3 1384711 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND LEFT WING NR 4 GROUND SPOILER INBOARD ACTUATOR FITTING CRACKED, WBL 79.75. REPLACED LEFT WING NR 4 GROUND S POILER PANEL ASSEMBLY IAW B737-300 AMM 27-62-12-4. 2 L 7 2 4F RT A16WE 2007031600116 20070316 00116 NE 2007 3 16 SA07021 2 20070309 A 7532 1324M12P10 ACTUATOR AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4P NE ZONE 400 LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 113UW 20392 5411 1141 575141 PIT FLT 914 EN ROUTE, SFO TO PHL. DURING IN-FLIGHT CHECKS, IT WAS DETERMINED THAT THE AIRCRAFT HAD BURNED 4,000 LBS OF FUEL MORE THAN EXPECTED. A FUEL LEAK FROM THE RIGHT SIDE FUEL SYSTEM WAS SUSPECTED. THE FLIGHT DIVERTED TO PIT AND LA NDED WITHOUT FURTHER INCIDENT. MAINTENANCE ISOLATED THE LEAK TO THE NUMBER TWO ENGINE, OUTBOARD, VARIABLE STATOR VANE ( VSV) ACTUATOR. THE VSV ACTUATOR WAS REPLACED. SYSTEM OPERATIONALLY AND LEAK CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E38NE 2007031600117 20070316 00117 NM 2007 3 16 SCNA07004 1 20070312 A 5220 DOOR BOEING 737 737800* NM EMERGENCY EXIT UNKNOWN A SCNA O OTHER O OTHER CR CRUISE 1 GL 15 PHHZG 28379 CREW REPORTED AFT OVERWING EXIT AT SEAT F (AFT RIGHT) APPEARS TO BE LEAKING WATER AROUND EXIT DOOR SEAL. MAINTENANCE OP ENED BOTH RT SIDE OVERWING EXITS. INSPECTED DOOR SEALS, BOTH OK. REMOVED CONDENSATION, INSULATION BLANKETS ARE DRY, RE -SECURED BOTH RT OVERWING EXIT DOORS. 2 L 7 2 4F RT A16WE 2007031600119 20070316 00119 SO 2007 3 16 SIMA200707103 1 20070309 A 5315 14521700007 FLOORBEAM EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 849AE 9413 4800 145716 FOUND LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. PERFORMED CUT OUT, FABRICATED AND INSTALLED REPAIRS PARTS I AW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007031600120 20070316 00120 EA 2007 3 16 SIMA200707105 1 20070226 A 5311 67053110522 FRAME CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 518AE 8286 4308 10126 FOUND WEB AT STATION 280 RIGHT SIDE CORRODED AT FLOORBEAM MATING AREA. SPLICED IN NEW WEB AT STATION 280 IAE AMERICAN E AGLE ENGINEERING ORDER CR-53MR-109. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007031600121 20070316 00121 EA 2007 3 16 SIMA200707106 1 20070226 A 5315 CC670341757 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 518AE 8286 4307 10126 FOUND STATION 280 FLOORBEAM CORRODED ALONG TOP FLANGE. SPLICED IN FRAME 280 AND EXTENSION MOUNTS IAW AMERICAN EAGLE ENG INEERING ORDER CR-53MR-108. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007031900004 20070319 00004 NM 2007 3 19 UPS07449418 1 20070212 A 5740 ATTACH ANGLE BOEING 747 747121 1384871 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT WING L/E NOSE BEAM WEB ATT ANGLE AT ILES 1117 FOUND CRACKED. CRACK LENGTH .375 INCH. LEFT WING L/E NOSE BEAM WEB ATT ANGLE AT ILES 1117 REPAIRED AS PER SRM 57-20-03 FIG 7. 2 L 7 4 4F A20WE 2007031900007 20070319 00007 NM 2007 3 19 UPS07449421 1 20070213 A 5311 65B01711638 FRAME BOEING 747 747121 1384871 NM BS 360 S17-18R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 360 STR 17-18R FRAME AFT FACE O/B AREA FOUND CRACKED. CRACK LENGTH .25 & .3125 INCH. M/D BS 3 60 STR 13R TO STR 18R FRAME REPAIRED AS PER SRM 51-40-03 FIG 2. 2 L 7 4 4F A20WE 2007031900010 20070319 00010 NM 2007 3 19 UPS07449424 1 20070213 A 5310 65B0500065 REVEAL BOEING 747 747121 1384871 NM L5 DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D L5 DOOR CUTOUT REVEAL FOUND CRACKED AT LOCK RELEASE LEVER AREA. CRACK LENGTH .5 INCH. M/D L5 DOO R CUTOUT REVEAL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007031900016 20070319 00016 NM 2007 3 19 UPS07449427 1 20070213 A 5712 65B078405 RIB BOEING 747 747121 1384871 NM LWS 1349 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT WING - 3VC FLAP I/B ACTUATOR ATTACH L/E RIB AT OLES 1349.25 CD LINK PTD AREA FOUND CRACK. CRACK LENGTH 0.375 INCH. LEFT WING NR 3VC FLAP I/B ACTUATOR O/B RIB AT OLES 1349.25 REPAIRED AS PER HX RS R57-42-35766, & UPS EO B747-5740-15105. 2 L 7 4 4F A20WE 2007031900017 20070319 00017 NM 2007 3 19 UPS07449429 1 20070313 A 5512 SKIN BOEING 747 747200 1384847 NM HORIZONTAL STAB DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 HOLE IN FUSELAGE TAIL SECTION LEFT SIDE ABOVE HORIZONTAL STABILIZIER/ ELEVATOR APPROX 5 X 7 INCHES. FABRICATED AND INST ALLED SHEET METAL DOUBLER PER 747 SRM 53-30-03. 2 L 7 4 4F RT A20WE 2007031900019 20070319 00019 WP 2007 3 19 UPS07849414 1 20070221 A 5311 75898332 FRAME DOUG DC8 DC873F 302199F WP FS 80 L20R DAMAGED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C1 MAIN CABIN LONGERON FRAME AND SHEAR TIE HAS DRILLED STOP MARK AND FRAME HAS SEVERAL OPEN HOLES AT STA 80 L20R. REMOVED DAMAGED SECTION OF FRAME. FABRICATED 2 EACH REPAIR SPLICES, 1 FRAME SECTION AND 1 SHEAR TIE. INSTAL LED IAW SRM 53-02-00-0 FIG 002, 51-3-2. 2 L 7 4 4F RT 4A25 2007031900022 20070319 00022 EA 2007 3 19 COMA0760242 1 20070309 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 987CA 7199 FLIGHT 5587 - DURING TAKEOFF ROLL, THE LAVATORY SMOKE DETECTION SYSTEM ACTIVATED, ABORTED TAKEOFF AND RETURNED TO THE GA TE. DEFERRED THE LAVATORY SMOKE DETECTION SYSTEM PER MEL 26-16-01. 2 L 7 2 4F RT A21EA 2007031900024 20070319 00024 EA 2007 3 19 TRAX200700343 1 20070312 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 EMERGENCY BATTERY PACKS FAILED OPS TEST. 2 L 7 2 4F RT A21EA 2007031900025 20070319 00025 EA 2007 3 19 TRAX200700345 1 20070312 A 5260 HANDLE CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 ASD OUTER HANDLE CRACKED IN WEB AS MARKED. REMOVED AND REPLACED ASD OUTER HANDLE IAW CRJ 700 SRM 52-11-03. SUPPLEMENTA L - SDR CLOSED 03/15/07. 2 L 7 2 4F RT A21EA 2007031900033 20070319 00033 NM 2007 3 19 CALA0700130 1 20070315 A 3350 D71701100 BATTERY PACK BOEING 737 737824 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12225 28934 THE SEAT MOUNTED EMERGENCY PATH LIGHTS FROM ROW 15-24 WERE FOUND INOPERATIVE. THE BATTERY PACK AT ROW 20ABC WAS REPLACE D IAW MM 33-51-06-960-805. 2 L 7 2 4F RT A16WE 2007031900037 20070319 00037 NM 2007 3 19 SWAA071367 1 20070313 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 779SW 27884 DURING SCHEDULED MV1 CHECK, FOUND EEPLS LOOSE BETWEEN ROW 8 ABC & 10 ABC. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2007031900038 20070319 00038 NM 2007 3 19 SWAA071357 1 20070313 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 766SW 29806 DURING SCHEDULED MV2 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007031900039 20070319 00039 WP 2007 3 19 UPS07849411 1 20070309 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 498 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 SKIN CORROSION/PULLED FASTENER FWD OF PIT 32 DOOR OPENING. CLASS II REPAIR CARRIED OUT TO LOWER BELLY SKIN AT STATION 4 98 (LONGERON 36) IAW DC8 SRM 53-02-01-0. 2 L 7 4 4F RT 4A25 2007031900041 20070319 00041 EA 2007 3 19 TRAX200700328 1 20070306 A 2750 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS UNKNOWN A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 978EV 7723 FLAP FAIL AT ZERO ON APPROACH. EMERGENCY EQUIPMENT ON STANDBY. 2 L 7 2 4F RT A21EA 2007031900042 20070319 00042 EA 2007 3 19 TRAX200700329 1 20070307 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 LEFT FORWARD MOST EXTERNAL EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007031900043 20070319 00043 EA 2007 3 19 TRAX200700330 1 20070307 A 2750 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS UNKNOWN A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 920EV 7810 FLAP FAIL AT ZERO ON APPROACH. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007031900044 20070319 00044 EU 2007 3 19 TRAX200700331 1 20070307 A 5220 DOOR AEROSP ATR72 ATR72 EU EMERGENCY EXIT STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 EMERGENCY EXIT AT 1A IS DIFFICULT TO OPEN. 2 H 7 2 4T RT 2007031900048 20070319 00048 EA 2007 3 19 TRAX200700342 1 20070312 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 640 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 SUSPECT CRACK ON LEFT DOUBLER AT FRAME 640. PERFORMED EDDY CURRENT INSPECTION OF SUSPECT AREA PER MTC REQUEST. LEFT FS 640 DOUBLER IS CRACKED. 2 L 7 2 4F RT A21EA 2007031900049 20070319 00049 EA 2007 3 19 TRAX200700344 1 20070312 A 5260 HANDLE CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 ASD OUTER HANDLE CRACKED. 2 L 7 2 4F RT A21EA 2007031900050 20070319 00050 EU 2007 3 19 BA07001 1 20070312 A 3230 005LG005B CONTROL UNIT AIRBUS 330 A330323 3930335 EU MLG FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 270AY 32858 332 0315 PHL FLT 1071 ON CLIMBOUT FROM PHL, EN ROUTE TO SJU, CREW RECEIVED ECAM L/G LGCIU 1 FAULT. CREW TRIED TO RESET FAULT ON OVERHEAD PANEL WITH NO HELP. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DEC LARED. MAINTENANCE REMOVED AND REPLACED THE NR 1 LGCIU PER MM 32-31-71-000-801. PERFORMED SATISFACTORY FUNCTIONAL CHEC K. 2 L 7 2 4F RT A46NM 2007031900051 20070319 00051 NM 2007 3 19 ZZDA070208143 1 20070208 A 5330 SKIN BOEING 717 717200 1383700 NM BS 235 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 915AT 55085 SMOOTH SKIN DENT AT FS 235, 6 INCHES ABOVE CUSP LINE WITHIN LIMITS PER SRM 53-00 ON LEFT SIDE. 3 INCHES IN DIA BY .125 I NCH DEPTH. INSTALLED DOUBLER REPAIR AT FS 235, 6 INCHES ABOUT AS PER B717 SRM 53-00-01 REPAIR 6. 2 L 7 2 4F TR A6WE 2007031900053 20070319 00053 EU 2007 3 19 AWXA200700349 1 20070307 A 2121 EVT3454H FAN AIRBUS 320 A320232 3930326 EU E/E BAY FAILED A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 669AW 24440 12401 1792 TPA - CREW DETECTED A SMOKE ODOR IN THE CABIN AND FLIGHT DECK. THE CREW DIVERTED TO TLH. MX INSPECTED THE A/C AND DETER MINED IT WAS A BAD EXTRACT FAN (18HQ). MX PLACED SYSTEM ON MEL. THE FLIGHT CONTINUED. A FUP WAS GENERATED TO REPLACE THE EXTRACT FAN (18HQ). MX REPLACED THE FAN, OPS CHECK WAS GOOD. MX CLEARED THE MEL. 2 L 7 2 4F RT A28NM 2007031900055 20070319 00055 EA 2007 3 19 TRAX200700348 1 20070311 A 3250 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA NLG STEERING INOPERATIVE A ASOA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 761ND 10213 AFTER TAKEOFF, GOT NOSE STEERING INOP. FOLLOWED QRH, TURNED STEERING OFF. AFTER LANDING RESET NWS 1-G2, 2-G2. FURTHER OPERATIONS NORMAL. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007031900057 20070319 00057 NM 2007 3 19 ASAA0771514 1 20070312 A 5340 143A9485Y35 ATTACH ANGLE BOEING 737 737790 13844CN NM BS 500D CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 FWD CARGO PIT ATTACH ANGLE CORRODED AT BS 500D. REMOVED AND REPLACED WITH P/N 143A9485435. 2 L 7 2 4F RT A16WE 2007031900061 20070319 00061 NM 2007 3 19 ASAA0771518 1 20070312 A 5315 146A75036 FLOORBEAM BOEING 737 737790 13844CN NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 AFT CARGO CORROSION FOUND ON CARGO FLOORBEAM AT BS 767. REPAIRED IAW EA5320 01793. 2 L 7 2 4F RT A16WE 2007031900062 20070319 00062 NM 2007 3 19 ASAA0771519 1 20070312 A 5315 FLOORBEAM BOEING 737 737790 13844CN NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 AFT CARGO CORROSION FOUND ON CARGO FLOORBEAM AT BS 767+4. REPAIRED IAW EA 5320 01793. 2 L 7 2 4F RT A16WE 2007031900067 20070319 00067 EA 2007 3 19 COMA0760244 1 20070309 A 7700 6030T40P01 THERMOCOUPLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LT ENGINE FAULTY A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 815CA 7397 807656 FLIGHT 5693 - DURING TAKEOFF ROLL THE NR 1 ITT INDICATION FLUCTUATED, ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACE D THE LEFT ENGINE OUTBOARD THERMOCOUPLE ASSEMBLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2007031900071 20070319 00071 2007 3 19 YENA2007014 4 20070311 A 3460 C13042BA01 COMPUTER AIRBUS 320 A320232 3930326 EU FLT MANAGE UNKNOWN A YENA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 621JB 6675 2491 FLT 515 EWR-FLL, ON ROTATION, -WARNING LANDING GEAR NOT DOWN- LOST SPEED A-THR, AP DISCONNECT. LOSS OF DATA ON PDF COND UCTED. AIR RETURN TO EWR, OVERWEIGH LANDING. INTERROGATED PFR. T/S CENTRAL WARNING SYS AMM 31-50-00. NO DEFECTS. PE RFORMED AFS/LAND TEST. NO DEFECTS. REPLACED FMGC 1 1CA1& 1CA2 PRECAUTIONARY PER AMM 22-83-34, PERFORMED OVERWEIGHT LAN DING CHECK PER AMM 05-51-11. NO DEFECTS. 2 L 7 2 4F RT A28NM 2007031900072 20070319 00072 EA 2007 3 19 COMA0760238 1 20070308 A 2420 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 2 UNDERSERVICED A COMA C ABORTED TAKEOFF W INADEQUATE Q C TO TAKEOFF 1 SO 01 927CA 7031 FLIGHT 5576 - GEN NR 2 DROPPED OFF LINE AS AIRCRAFT BEGAN TAKEOFF ROLL, ABORTED TAKEOFF. SERVICED NR 2 IDG, OPS CHECK G OOD. 2 L 7 2 4F RT A21EA 2007031900073 20070319 00073 GL 2007 3 19 SIMA200706701 2 20070307 A 7200 AE3007A1 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 ODOR A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 624AE 15512 4269 145111 CAE311351 "SUP" FOUL ODOR IN CABIN AND COCKPIT. REMOVED AND REPLACED NR 1 ENGINE IAW AMERICAN EAGLE WORK CARD 72-000-00. OPERATI ONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007031900075 20070319 00075 SO 2007 3 19 SIMA200706710 1 20070303 A 5320 14525480603 SILL EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 847AE 9685 4800 145707 FOUND BAGGAGE DOOR LOWER SILL FOUND CORRODED. REMOVED AND REPLACED SILL IAW EMB SRM 51-40-02, 51-40-06 AND 51-20-03. 2 L 7 2 4F RT T00011AT 2007031900076 20070319 00076 SO 2007 3 19 SIMA200706711 1 20070227 A 3220 14524475003 BEARING CAP EMB 135 EMB135KL 3260302 SO ZONE 700 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 807AE 13140 4800 145506 NOSE LANDING GEAR DRAG BRACE RIGHT LOWER BEARING CAP FOUND CORRODED. REMOVED AND REPLACED BEARING CAP IAW EMB AMM 32-20 -02. PERFORMED RETRACTION/EXTENSION CHECK WITH NO DEFECTS, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007031900077 20070319 00077 SO 2007 3 19 SIMA200706712 1 20070227 A 5320 14521721009 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 807AE 9685 4800 145506 GALLEY FOWARD DIGITAL FOUND CORRODED. CUT OUT DAMAGE AREA, SPLICED IN REPAIR SECTION IAW EMB SRM 53-21-10. RETURNED AI RCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007031900079 20070319 00079 SO 2007 3 19 SIMA200706705 1 20070226 A 5315 14521700007 FLOORBEAM EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 804AE 13150 4800 145487 LEFT OMEGA BEAM FOUND CORRODED AT FRAME 25. PERFORMED CUT OUT OF CORROSION, FABRICATED REPAIR PARTS AND INSTALLED REPAI R PARTS IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007031900080 20070319 00080 SO 2007 3 19 SIMA200706702 1 20070304 A 3350 20131A BATTERY PACK EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHTS DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 814AE 10576 1215 145541 FOUND EMERGENCY BATTERIES FAILED TO TEST. REMOVED AND REPLACED EMERGENCY BATTERIES IAW EMB AMM 33-50-04. OPERATIONAL C HECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007031900083 20070319 00083 SO 2007 3 19 SIMA200706708 1 20070301 A 5310 14521413605 BEAM EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 807AE 13140 4800 145506 RIGHT HAT BEAM FOUND CORRODED AT FRAMES 22 AND 23. BLENEDED CORRODED AREA AND FILLED WITH EA934NA RESIN. FABRICATED AN D INSTALLED DOUBLER IAW EMB IC2007-145/01376, DATED 02/26/07. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007031900084 20070319 00084 SO 2007 3 19 SIMA200706709 1 20070303 A 5320 14522178005 SILL EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 847AE 9685 4800 145707 SERVICE DOOR CENTER SILL FOUND CORRODED. BLENDED DAMAGED AREA AND FILLED WITH EA934NA RESIN. FABRICATED AND INSTALLED A DOUBLER IAW EMB SRM 53-21-02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007031900085 20070319 00085 NM 2007 3 19 UPS07449378 1 20070216 A 5320 65B382182 SUPPORT BOEING 747 747121 1384871 NM BS 1960 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C BULK CARGO COMPT - STA 1960 LEFT SIDEWALL SUPPORT ANCHOR NUT AREA FOUND CORRODED AS MARKED. CORROSION BLEND OUT 0.049" X .5" X 1" EXCEED SRM 53-10-01 FIG 1 LIMITS. BULK CARGO COMPT - STA 1960 LEFT SIDEWALL SUPPORT REPAIR ED AS PER SRM 51-40-04 FIG 1. 2 L 7 4 4F A20WE 2007031900086 20070319 00086 NM 2007 3 19 UPS07449388 1 20070216 A 5210 65B05091848 FRAME BOEING 747 747121 1384871 NM R5 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D R5 DOOR UPPER FRAME FOUND CRACKED AT SEVERAL FASTENER HOLE AREA. CRACK LENGTH .75 INCH. FRAME RE PLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007031900087 20070319 00087 NM 2007 3 19 UPS07449401 1 20070216 A 5320 65B382253 SUPPORT BOEING 747 747121 1384871 NM BS 2080 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C BULK CARGO COMPT - STA 2080 LT SIDEWALL SUPPORT ANCHOR NUT AREA FOUND CORRODED AS MARKED. CORROSION B LEND OUT 0.038" X 1" X 1" EXCEED SRM 53-10-01 FIG 1 LIMITS. BULK CARGO COMPT BS 2080 LEFT SIDEWALL SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 1. 2 L 7 4 4F A20WE 2007031900091 20070319 00091 WP 2007 3 19 UPS07849364 1 20070213 A 5730 5611360167 SKIN DOUG DC8 DC871F 302199D WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 LEFT UPPER WING SKIN AT CANT 495 TO XRS 554 BETWEEN STR 5 AND 8 REQUIRES REPAIR. REPAIRED UPPER WING SKIN IAW SAA EA 008-5730-01-A0658 AND UPS EO DC8-5730-26300-A. 2 L 7 4 4F RT 4A25 2007031900097 20070319 00097 CE 2007 3 19 GUUA03110701 1 20070311 A 2910 LINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HYDRAULIC SYS PUNCTURED A GUUA O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 29 81535 UE147 FLIGHT: 9137, AIRCRAFT SMELLS LIKE OIL, COMING FROM THE OVERHEAD BLOWERS RETURNED DEPARTURE, LANDED WITHOUT INCIDENT. I NSPECTED AIRCRAFT FOUND PUNCTURED HYDRAULIC BRAKE LINE JUST FORWARD OF SEAT 4F, REPAIRED DAMAGED HYDRAULIC LINE. ENVIRON MENTAL SYSTEM OPERATIONAL CHECK NORMAL NO LEAKS OR SMELL DETECTED. 2 L 7 2 4T 4 T RT A24CE E26NE 2007031900098 20070319 00098 NM 2007 3 19 AWXA200700350 1 20070312 A 5330 6545775 SKIN BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 PHX - FOUND CRACKED FUSELAGE SKIN, BS 887, S25R AT LAP SEAM. REPAIRED FUSELAGE SKIN, BS 887, S25R AT LAP SEAM IAW B737- 300 SRM 53-00-01-2R 2 L 7 2 4F RT A16WE 2007031900100 20070319 00100 EA 2007 3 19 COMA0760243 1 20070309 A 3260 750009000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 804CA 18895 7352 FLIGHT 5436 - AFTER DEPARTURE FROM LGA RECEIVED A GEAR UP DISAGREE MESSAGE, NOSE GEAR REMAINED DOWN. CREW DECLARED AN E MERGENCY AND FLIGHT LANDED AT LGA WITHOUT INCIDENT. REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2007031900102 20070319 00102 NM 2007 3 19 USAA070190 1 20070313 A 5340 69775191 STRINGER CLIP BOEING 737 737401 1384701 NM BS 727A S11L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 BS 727A S-11L STRINGER TO FRAME TIE CLIP CRACKED. FABBED & INSTALLED NEW CLIP PER SRM 51-01-02, BOEING DWG 6977519 , DE FECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007031900104 20070319 00104 EA 2007 3 19 TRAX200700332 1 20070308 A 5310 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 LEFT FS 280 CROSSBEAM HAS CORROSION ON UPPER FLANGE. REMOVED LEFT 280.00 CROSSBEAM IAW 700/900 SERIES SRM 51-42-06, 51- 42-13, 51-42-21. LOCATED HOLES ON SERVICEABLE CROSSBEAM P/N CC670-34175-7, IAW CRJ 700 SRM 51-40-11. INSTALLED LEFT 28 0.00 CROSSBEAM SECTION, SOLID FASTENERS, AND HI-LITES AND CHERRY FASTENERS AS REQUIRED IAW CRJ 200 SRM 51-42-06, 51-42-1 3, AND 51-42-21. RE-INSTALLATION OF LBL 20.00 AND LBL 37.00 INTERCOSTALS. O/B UPPER FLANGE FASTENERS REQUIRE INSTALLAT ION FOR COMPLETION OF REPAIR. INSTALLED REMAINING FASTENERS AS REQUIRED IAW CRJ 700 SRM 51-42-06. TOPCOATED REPAIR ARE A IAW CRJ 700 SRM 51-25-16. APPLIED DINITROL AV8 TO REPAIR AREA IAW CRJ 700 SRM 51-21-11. LOCATED FASTENER HOLES FOR F 2 L 7 2 4F RT A21EA 2007031900105 20070319 00105 EA 2007 3 19 TRAX200700333 1 20070308 A 5310 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 RIGHT FS 280 CROSSBEAM HAS CORROSION ON UPPER FLANGE. [SUP 05-02-07] REMOVED RT 280.00 CROSSBEAM IAW CRJ 700/900 SERIES SRM 51-42-06. 51-42-13, 51-42-21. LOCATED ALL HOLES IN NEW SERVICEABLE R CROSSBEAM. 2 L 7 2 4F RT A21EA 2007031900111 20070319 00111 EA 2007 3 19 COMA0760255 1 20070314 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 739CA 7273 FLIGHT 5460 - RECEIVED FLAPS FAIL CAUTION MESSAGE WHILE PARKED AT GATE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAG E -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007031900112 20070319 00112 EA 2007 3 19 COMA0760256 1 20070314 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 811CA 7380 FLIGHT 5441 - FLAPS FAIL MESSAGE AT 30 DEGREES ON CLIMBOUT, AIRCRAFT RETURNED BACK TO JAX AND LANDED SAFELY. COMPLIED W ITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM W AS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007031900113 20070319 00113 NM 2007 3 19 BB07022 1 20070310 A 3350 20121 CHARGER BOEING 757 757225 1384959 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 923UW 22203 FLL - MAINTENANCE REPORTED THE AFT RIGHT EMERGENCY EXIT SIGN AND THE LEFT EMERGENCY EXIT LOCATOR SIGN INOPERTIVE. MAINTE NANCE REMOVED AND REPLACED THE AFT RIGHT BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 2007031900114 20070319 00114 EA 2007 3 19 COMA0760247 1 20070311 A 3610 ISOLATION VALVE CNDAIR CL600 CL6002B19 1900309 EA ENGINE FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 786CA 7333 FLIGHT 5199 - DURING CRUISE FLIGHT THE 10TH STAGE ISOLATION VALVE FAILED TO CLOSE. PERFORMED AN OPERATIONAL CHECK OF TH E 10TH STAGE ISOLATION VALVE, DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE. 2 L 7 2 4F RT A21EA 2007031900117 20070319 00117 NM 2007 3 19 USAA070188 1 20070313 A 5320 69735272 ANGLE BOEING 737 737401 1384701 NM BS 500G S28R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 BS 500G, S-28R CRACKED. REMOVED CRACKED ANGLE & FAB'D & INSTALLED NEW PER SRM 51-10-02, BOEING DWG 6973527, DEFECT SIZE : .5 INCH. 2 L 7 2 4F RT A16WE 2007031900119 20070319 00119 NM 2007 3 19 USAA070186 1 20070313 A 5340 6935352U14 STRINGER CLIP BOEING 737 737401 1384701 NM BS 727F S7R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 BS 727F, S-7R CRACKED. REMOVED CRACKED TIE & INSTALLED NEW ONE PER SRM 51-10-02, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007031900120 20070319 00120 NM 2007 3 19 USAA070185 1 20070313 A 5340 6935352U14 STRINGER CLIP BOEING 737 737401 1384701 NM BS 727F S8R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 BS 727F S-8R CRACKED. REMOVED CRACKED TIE & INSTALLED NEW ONE PER SRM 51-10-02, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007031900121 20070319 00121 NM 2007 3 19 USAA070184 1 20070313 A 5340 6935352U14 STRINGER CLIP BOEING 737 737401 1384701 NM BS 727C S7R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 BS 727C S-7R CRACKED. REMOVED CRACKED TIE AND INSTALLED NEW ONE PER SRM 51-10-02, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007031900124 20070319 00124 NM 2007 3 19 USAA070181 1 20070313 A 5340 STRINGER CLIP BOEING 737 737401 1384701 NM 663 S10R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 TIE CLIP AT STA 663 STR S10R CRACKED. REPLACED TIE CLIP WITH NEW PER SRM 51-10-02, DEFECT SIZE: .025 INCH. 2 L 7 2 4F RT A16WE 2007031900126 20070319 00126 EU 2007 3 19 USAA070179 1 20070313 A 5320 SILL AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 171US 1465 AFT RIGHT DOOR SILL AT FR 66 HAS CORROSION. REMOVED CORROSION, INSTALLED REPAIR ANGLES PER SRM 53-41-14; CORR LEVEL 1; TSK JA-260-53500, DEFECT SIZE: .5 X .5 INCH. 2 L 7 2 4F RT A28NM 2007031900127 20070319 00127 NM 2007 3 19 USAA070178 1 20070313 A 5311 FRAME BOEING 737 737301 1384611 NM BS 492 S24R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 589US 23934 BS 492 S-24R CRACKED. FAB'D & INSTALLED REPAIR ANGLES PER EA 98533, DEFECT SIZE: .5 INCH CRACK. 2 L 7 2 4F RT A16WE 2007031900128 20070319 00128 CE 2007 3 19 6017802072007 1 20070207 A 3260 1EN18 SWITCH LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE MLG DOOR MALFUNCTIONED E J7SA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 05 244FX 178 UPON SELECTING LANDING GEAR UP, HAD (2) RED INDICATIONS, BUT ALSO (3) GREEN, AND THE LANDING GEAR WOULD NOT RETRACT. AI R RETURN WITH UNEVENTFUL LANDING AND TAXI. 02/08/07 REMOVED AND REPLACED LT AND RT GEAR DOOR SWITCHES. OPS CHECK GOOD . 02/14/07 AIRCRAFT HAS FLOWN 17 ADDITIONAL LEGS WITH NO REPEAT EVENT. 2 L 7 2 4F 4 F RT A10CE E35NE 2007031900130 20070319 00130 CE 2007 3 19 DJFA2007028 1 20070309 A 2916 RESERVOIR BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HYD SYSTEM EMPTY E DJFA O OTHER J WARNING INDICATION LD LANDING 1 EA 23 790TA RK252 TRIP NR 1153226, ON LANDING, CREW REPORTED HYDRAULIC LOW ANNUNCIATOR ILLUMINATED AND LOSS OF HYDRAULIC PRESSURE. EMERGE NCY BRAKING WAS USED. MAINTENANCE DICOVERED HYDRAULIC RESERVOIR EMPTY. MAINTENANCE DISCOVERED THE HYDRAULIC PRESSURE LI NE ON THE RIGHT HAND TR RUPTURED. THE LINE WAS REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007031900131 20070319 00131 NM 2007 3 19 SWAA071344 1 20070311 A 3350 079123 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 448WN 33721 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER MISSING AT 23 DEF. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007031900132 20070319 00132 NM 2007 3 19 SWAA071341 1 20070312 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS ASSY PER MM. 2 L 7 2 4F RT A16WE 2007031900134 20070319 00134 NM 2007 3 19 SWAA071342 1 20070310 A 5320 6545410 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM BS 706-712 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED BETWEEN BS 706 TO BS 712, BL 0. REPAIRED FLOORBEAM PER BFG ER. 2 L 7 2 4F RT A16WE 2007031900135 20070319 00135 NM 2007 3 19 SWAA071343 1 20070310 A 5320 6545410 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM BS 707 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 707, LBL 25. REPAIRED FLOORBEAM PER BFG ER & SRM . 2 L 7 2 4F RT A16WE 2007031900138 20070319 00138 NM 2007 3 19 SWAA071352 1 20070313 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM BS 706 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706 STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031900139 20070319 00139 NM 2007 3 19 SWAA071354 1 20070313 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM BS 747 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747 STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031900141 20070319 00141 NM 2007 3 19 SWAA071353 1 20070313 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907 STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031900144 20070319 00144 NM 2007 3 19 SWAA071337 1 20070311 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN FLOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 485WN 32473 EEPLS TRACK LOOSE AT 4 ABC. SECURED EEPLS TRACK PER MM. 2 L 7 2 4F RT A16WE 2007031900145 20070319 00145 NM 2007 3 19 ASAA0741512 1 20070309 A 2150 22051702 ACM BOEING 737 7374Q8 138447Q NM RIGHT LEAKING A ASAA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 NM 02 772AS 25105 RIGHT PACK TRIP AND FILLED CABIN WITH SMOKE. SMOKE REMOVED FROM CABIN PER AMM 21-00-01. FOUND RIGHT ACM LEAKING BETWEE N TURBINE AND COMPRESSOR SECTIONS. REMOVED AND REPLACED ACM O2 FILTER AND COMPLETED CONDITIONAL INSPECTION. 2 L 7 2 4F RT A16WE 2007031900146 20070319 00146 NM 2007 3 19 ASAA0711513 1 20070312 A 3350 1104461 MODULE BOEING 737 737290C 138448V NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 742AS 23136 L1 & R1 AND HATCH COVER EMERGENCY EXIT MARKER LIGHTS OUT. REPLACED MODULE M7331, OPS NORMAL. 2 L 7 2 4F A16WE 2007031900150 20070319 00150 NM 2007 3 19 07FDEA00732 1 20070309 A 5713 ARB75442 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT WING TANK, APPROX 3/4 INCHES CRACK FOUND AT STRINGER END 44R (XORS 253) DURING HFEC INSPECTION. REPAIR CARRIED OUT AS PER SRM 57- 20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007031900151 20070319 00151 NM 2007 3 19 07FDEA00808 1 20070314 A 5414 SKIN DOUG MD11 MD11F 3023600 NM ZONE 400 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 PYLON NR 3: ABOVE ENGINE DRAIN PAN APPROX STA YN230 RT LOWER PYLON SKIN FOUND WITH SEVERAL GOUGES. COMPLIED WITH FEDEX EA 1-5450-109841, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007031900152 20070319 00152 NM 2007 3 19 07FDEA00809 1 20070314 A 5414 SKIN DOUG MD11 MD11F 3023600 NM ZONE 400 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 PYLON NR 3: ABOVE ENGINE DRAIN PAN APPROX STA YN=230LH LOWER PYLON SKIN FOUND WITH SEVERAL GOUGES. COMPLIED WITH FEDEX EA 1-5450-109842, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007031900154 20070319 00154 EU 2007 3 19 07FDEA00811 1 20070314 A 5730 SKIN AIRBUS 310 A310324 3930206 EU ZONE 500 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 OLD REPAIR ON LT WING ON TOP SKIN, REAR SPAR, BETWEEN RIB 4-5. VISUAL INSPECTION FOR FURTHER CORROSION AND CORRECT TAPE RLOCK INSTALLATION IAW AMM570000/601/PARA 2, SRM514021/001/PARA 9 AND RAS/BAE/0439/98 ISSUE "B". (FURTHER DR422). 2 L 7 2 4F RT A35EU 2007031900157 20070319 00157 NM 2007 3 19 SB07023 1 20070314 A 5610 5893543130 WINDSHIELD BOEING 737 737401 1384701 NM COCKPIT ARCED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 420US 20819 20819 23987 CLT - FLT9180 EN ROUTE FROM BNA TO CLT, THE FIRST OFFICER'S R1 WINDSHIELD BEGAN ARCING IN THE UPPER LEFT CORNER. WINDOW WENT COLD. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT AT CLT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOV ED AND REPLACED THE FIRST OFFICER'S R1 WINDSHIELD PER JOB CARD J356-11-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007031900158 20070319 00158 NM 2007 3 19 USAA070192 1 20070314 A 5210 507945264 SKIN BOEING 737 737401 1384701 NM L1 DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 L1 DOOR AT NUMBER 6 STOP PIN CRACKED. INSTALLED DOUBLER PER TR 52-10-16, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007032000001 20070320 00001 NM 2007 3 20 USAA070207 1 20070315 A 5313 STRINGER SPLICE BOEING 737 737401 1384701 NM BS 908 S4L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 S4L SPLICE CRACKED AROUND 2 RIVETS AT STA 908L. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-10, DEFECT SIZE: .250 INCH. 2 L 7 2 4F RT A16WE 2007032000002 20070320 00002 NM 2007 3 20 USAA070193 1 20070315 A 5210 507945264 PIN BOEING 737 737401 1384701 NM L1 DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 L1 DOOR AT NR 5 STOP PIN CRACKED. INSTALLED DOUBLER PER TR 52-10-16, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007032000006 20070320 00006 NM 2007 3 20 USAA070197 1 20070315 A 5410 ANGLE BOEING 737 737401 1384701 NM NR 1 NACELLE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 NR 1 ENGINE PYLON AFT AREA, ANGLE TIE CRACKED. FABRICATED & INSTALLED NEW ANGLE PER BOEING DWG 65C26300 & SRM 51-10-02, DEFECT SIZE: 3 INCHES. 2 L 7 2 4F RT A16WE 2007032000009 20070320 00009 NM 2007 3 20 USAA070200 1 20070315 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 STR 11L INTERCOSTAL AFT TURN DOWN ANGLE CRACKED. REMOVED DAMAGED ANGLE, FABRICATED & INSTALLED NEW ANGLE PER BOEING DWG 69-48985 & SRM 51-10-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007032000010 20070320 00010 NM 2007 3 20 USAA070201 1 20070315 A 5310 FRAME BOEING 737 737401 1384701 NM 727B S8R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 BS 727B S-8R CRACKED. REMOVED DAMAGE & INSTALLED DOUBLERS PER TR 53-10-20E, DEFECT SIZE: .500 INCH. 2 L 7 2 4F RT A16WE 2007032000012 20070320 00012 NM 2007 3 20 USAA070203 1 20070315 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 328 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 STA 328 LBL 45 FWD SIDE OF FLOORBEAM, FLOORBEAM SUPPORT CRACKED. REMOVED DAMAGE & INSTALLED FABRICATED REPAIR PARTS PER SRM 53-15-01, BOEING DWG 65C33942, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007032000013 20070320 00013 NM 2007 3 20 USAA070204 1 20070315 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 328 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 STA 328 LBL 45, FLOORBEAM SUPPORT CRACKED. INSTALLED FABRICATED REPAIR PARTS PER SRM 53-15-01, BOEING DWG 65C33942, DEF ECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007032000014 20070320 00014 EU 2007 3 20 HAEA200700199 1 20070313 A 5697 MIL22759168 WIRE AMD FALC20 FALCON 2720302 EU GE CF700 CF700* 30010 NE WINDSHIELD SHORTED E HAEA H D DEACTIVATE SYST/CIRCUITS RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 05 232TW 16542 16542 32 ON TAXI OUT, COPILOTS WINDSHIELD HEAT PRODUCED SMOKE. MAINTENANCE REMOVED WINDOW FACIA AND DISCOVERED SHORTED WIRES. REP AIRED WIRES AND TESTED SYSTEM. OPERATIONS NORMAL. [CLOSED] 2 L 7 2 4F 4 F A7EU E7EA 2007032000015 20070320 00015 NM 2007 3 20 USAA070206 1 20070315 A 5313 STRINGER SPLICE BOEING 737 737401 1384701 NM BS 908 S4L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 STA 908, S4L CRACKED. REMOVED & REPLACED WITH NEW, TREATED & PRIMED PER SRM 53-10-02, 53-20-01, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007032000018 20070320 00018 NM 2007 3 20 UPS07M49383 1 20070121 A 5313 AEA0165 LONGERON DOUG MD11 MD11F 3023600 NM BS 1361-1381 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C MAIN DECK:FROM BS 1361 TO 1381 LONGERON 20R FOUND CORRODED. REMOVED LONGERON NR 20R FROM 1361 TO 1381 PER SRM 51-31-01 V2 R38. NEW FAB LONGERON 20R PER DWG AEA0165 & PROTECTED PER SRM 51-21-01 V2 R38. NEW LONGERON NR 20 R RE-INSTALLED PER SRM 51-31-01 V2 R38. FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007032000019 20070320 00019 NM 2007 3 20 UPS07M49384 1 20070131 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM BS 1541 L43R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C CTR CARGO STA 5-113-1541 STR 43-R BILGE AREA STRINGER FOUND CORRODED AS MARKED. ATT/PARTS REMOVED FOR ACCESS ON STRINGER SPLICE PER SRM 51-31-01 V2 R38. CORROSION LONGERON REMOVED PER SRM 53-10-00 F2 V1 R38. REPAIR LONG ERON PARTS & FAB PER SRM 53-10-00 F2 V2 R38. REPAIR PARTS PROTECTED PER SRM 51-21-01 V2 R38. REPAIR LONGERON ATT/PARTS RE-INSTALLED PER SRM 53-10-00 F2 V2 R38, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007032000020 20070320 00020 NM 2007 3 20 UPS07M49385 1 20070126 A 5313 AGA7115 LONGERON DOUG MD11 MD11F 3023600 NM BS 630-650 L45R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C FWD CARGO COMPT: FROM BS 6-30 TO 6-50 LONGERON 45R FOUND CORRODED. CORRODED LONGERON & ATTACHED PARTS REMOVED FOR ACCESS. CORROSION LONGERON PROTECTED PER SRM 51-31-01 V2 R38. NEW LONGERON FAB PER DWG AGA7115.F PI CUTOU T ON NEW FAB LONGERON FOUND NO CRACK EVIDENT. NEW LONGERON RE-PROTECTED PER SRM 51-21-01 V2 R38. OK TO INSTALL. NEW L ONGERON & ATT/PARTS RE-INSTALLED PER SRM 51-31-01 V2 R38 & DWG: AGA7115, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007032000021 20070320 00021 NM 2007 3 20 UPS07M49386 1 20070203 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM BS 1541 L38L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C CTR CARGO STA 1541 LONGERON 38L FOUND CORRODED AS MARKED. CORROSION LONGERON ATT/PARTS REMOVED FOR AC CESS PER 51-31-01 V2 R38 STA 1561 LONGERON 38L CORROSION LONGERON REMOVED PER SRM 53-10-00 F2 V1 R38. REPAIR LONGERON P ARTS FAB PER SRM 53-10-00 F2 V2 R38 PER SRM 51-21-01 V2 R38. OK TO INSTALL. REPAIR LONGERON & AREA FASTENERS REINSTALL ED PER SRM 53-10-00 FIG 2 VOL 1 REV 38, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007032000022 20070320 00022 NM 2007 3 20 UPS07M49387 1 20070131 A 5313 AGA7115 LONGERON DOUG MD11 MD11F 3023600 NM BS 1139 L44R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C FROM STA 6-90 TO STA 1139 LONGERON 44R CORRODED. CORRODED LONGERON ATT/PARTS REMOVED FOR ACCESS PER S RM 51-31-01 V2 R38. NEW LONGERON SPLICE P/N AGA7115U511, FAB PER DWG: AGA7115.FPI CUTOUT ON NEW FAB LONGERON FOUND NO E VIDENT OF CRACK. NEW SPLICE P/N AGA7115 & FASTENER PICK UP HOLES PER DWG: AGA7115 & SRM 51-31-01 V2 R38. OK TO INSTALL , INSTALLATION PER SRM 51-31-01 V2 R38 & DWG: AGA7115 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007032000025 20070320 00025 CE 2007 3 20 GLBA20060922 1 20070308 A 5260 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE AIRSTAIR DOOR DELAMINATED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 100UX UE100 AIRSTAIR DOOR EXTERIOR SKIN DELAMINATING AROUND DOOR HANDLE AREA. MX REMOVED CORROSION IN AFFECTED AREA AND REPAIRED PE R B1900 SRM 52-10-05 FIGURE NR 1.RII INSPECTION COMPLIED WITH PER TC 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007032000028 20070320 00028 NM 2007 3 20 USAA070220 1 20070315 A 5320 FLOOR SUPPORT BOEING 737 737401 1384701 NM BS 328-344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 BETWEEN STA 328-344 RBL 55 HAS CORROSION. REMOVED PART & REPLACED WITH IDENTICAL PART PER DWG 65C80735, DEFECT SIZE: 3 X 16 INCHES. 2 L 7 2 4F RT A16WE 2007032000030 20070320 00030 NM 2007 3 20 USAA070209 1 20070315 A 5711 SPAR BOEING 737 737401 1384701 NM RT WING DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 RT WING UNDER SIDE FIRST 3 FASTENERS INBOARD AT ATTACH Z-ANGLE BELOW FWD SPAR HAS HOLES. REAMED HOLES TO .263 & INSTALL ED FASTENERS PER SRM 51-40-09, DEFECT SIZE: .213 DIA. 2 L 7 2 4F RT A16WE 2007032000035 20070320 00035 NM 2007 3 20 UPS07M49397 1 20070109 A 5730 SKIN DOUG MD11 MD11F 3023600 NM LT WING CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE:C LEFT WING UNDERSIDE FIXED L/E SKIN ABOVE ENG PYLON I/B EDGE SKIN FOUND CHAFF MARK. LEFT WING UNDERSID E FIXED L/E SKIN ABOVE ENG PYLON I/B EDGE SKIN CHAFF MARK REMOVED AND REPROTECTED PER SRM 51-21-01 V-II R38. FOUND EXCE ED LIMIT PER SRM 57-00-01 FIG 3 VI R38. HFEC INSP CUTOUT PER DAC NDTSPM R12 06-10-0 1.001 ON REWORKED AREA & FOUND NO C RACK EVIDENT. NEW DOUBLER FAB & INSTALLED PER EN 1061-07. 2 L 7 3 4F RT A22WE 2007032000036 20070320 00036 NM 2007 3 20 UPS07M49398 1 20070110 A 5410 LONGERON DOUG MD11 MD11F 3023600 NM RT NACELLE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE:C NR 1 ENG RIGHT CORE COWL AFT LWR EDGE FOUND WITH CHAFE MARK AS MARKED. DAMAGED LONGERON AT NR 1 ENG R IGHT CORE COWL AFT LWR EDGE AREA REMOVED PER SRM 51-31-01 V-II R38. NEW LONGERON FAB PER EN 1093-07. HOLES ON FAB LONG ERON PICKED UP AS PER SRM 51-31-01 V-II R38. PAINT TOUCHED UP ON REWORK AREA PER SRM 51-21-01 V-II R38. NEW LONGERON A T NR 1 ENG RIGHT CORE COWL AFT LWR EDGE AREA INSTALLED PER SRM 51-21-01 V-II R38. 2 L 7 3 4F RT A22WE 2007032000037 20070320 00037 NM 2007 3 20 UPS07M49399 1 20070116 A 5753 HINGE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE:C RIGHT WING O/B FLAP, I/B AFT HINGE FOUND PIVOT POINT BUSHINGS 2EA CORRODED. RIGHT AFT O/B FLAP I/B HI NGE PIVOT POINT BUSHINGS REMOVED PER BSOPM 20-20 -7 R56. RIGHT AFT O/B FLAP I/B HINGE PIVOT BORE & SPOTFACE CORROSION R EMOVED & FOUND EXCEED LIMIT PER CMM57-52-04 PG 621-622. FPI CUTOUT IAW DAC NDT SPM R12 PT 8 ON REWORKED AREA & FOUND NO CRACK & NO CORROSION EVIDENT. BUSHINGS FAB & INSTALLED PER EN 1082-07. 2 L 7 3 4F RT A22WE 2007032000039 20070320 00039 NM 2007 3 20 WRNA200700015 1 20070310 A 5330 SKIN BOEING 747 747212B 1384886 NM BS 560 S37-38R GOUGED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, 2 GOUGES IN SKIN WERE FOUND OUT OF LIMITS AT FUSELAGE STA 560 BETWEEN STR 37R AND STR 38R. BLENDED OUT DAMAGE AREA OF OUTER SKIN IAW EA 01-07013. 2 L 7 4 4F A20WE 2007032000040 20070320 00040 NM 2007 3 20 WRNA200700016 1 20070210 A 2810 FUEL TANK BOEING 747 747212B 1384886 NM BS 1265 CORRODED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, CORROSION WAS FOUND AT LOWER CENTER TANK SKIN AT STA 1265 LBL 117. REPAIRED IAW SRM 57-30-01 AND EA 01- 07018. 2 L 7 4 4F A20WE 2007032000041 20070320 00041 NM 2007 3 20 WRNA200700017 1 20070213 A 5414 SKIN BOEING 747 747212B 1384886 NM NR 3 NACELLE DAMAGED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, NR 3 PYLON INBOARD SKIN DOUBLER WAS FOUND WORN UNDER FORESHIELD NEAR NAC STA 221. FABRICATED AND INSTAL LED REPAIR PARTS IAW EA 01-07019. 2 L 7 4 4F A20WE 2007032000042 20070320 00042 NM 2007 3 20 WRNA200700018 1 20070210 A 5330 SKIN BOEING 747 747212B 1384886 NM BS 1770-1850 DAMAGED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, EXTERNAL FUSELAGE SKIN WAS FOUND CREASED FROM STA 1770 TO STA 1850 & 41L TO 46L. REPLACED SKIN SECTION IAW SRM 53-30-03 FIG 19 AND EA 01-07014. 2 L 7 4 4F A20WE 2007032000043 20070320 00043 NM 2007 3 20 WRNA200700019 1 20070210 A 5330 SKIN BOEING 747 747212B 1384886 NM BS 2348 S51R BULGED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, FUSELAGE SKIN WAS FOUND BULGED AT STA 2348 AT STRINGER 51R. REPAIRED STRINGER, FAILSAFE STRAP, SHEAR TI E, FRAME WEB AND FRAME IAW SRM, 53-10-02, 53-10-03 FIG 1, 51-40-04, MM 51-21-00, KM DRAWING 531007003-1 AND EA 01-07017. 2 L 7 4 4F A20WE 2007032000044 20070320 00044 CE 2007 3 20 021607N511CS1 1 20070216 A 3233 SWITCH CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE ACTUATOR FAILED E Z5FA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NE 03 511CS 0697 5605324 ON APPROACH INTO BTV THE RT MLG LIGHT DID NOT ILLUMINATE FOLLOWED BY THE RED GEAR UNSAFE INDICATION. THE CREW FOLLOWED T HEIR CHECKLIST THE EMERGENCY GEAR/BRAKE BOTTLE WAS USED AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE TROUBLESHOT THE FAILURE TO A BAD RT MLG ACTUATOR SWITCH. THE ACTUATOR WAS REPLACED GEAR OPERATION WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007032000045 20070320 00045 CE 2007 3 20 GUUA03140701 1 20070314 A 2916 RESERVOIR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HYD SYSTEM OVERSERVICED A GUUA O OTHER W K B INADEQUATE Q C FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 29 190YV UE190 FLIGHT: 9199, AFTER TAKEOFF PINK FLUID LEAKAGE AND ODOR FOUND ON FIRST OFFICERS FLOORBOARD. RETURNED TO DEPARTURE AND LA NDED WITHOUT INCIDENT. FOUND RESIDUAL HYDRAULIC FLUID DUE TO BRAKE RESERVOIR OVERSERVICE. CLEANED RESIDUAL HYDRAULIC FL UID. INSPECTED FIRST OFFICERS BRAKE MASTER CYLINDER AND BRAKE LINES NO LEAKS NOTED. 2 L 7 2 4T 4 T RT A24CE E26NE 2007032000046 20070320 00046 NM 2007 3 20 SWAA071375 1 20070313 A 3350 071702001 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS WEAK A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 706SW 27840 DURING SCHEDULED HC1 CHECK, RIGHT CENTER EMERGENCY EXIT LIGHT BATTERY PACK FAILED TIME TEST. REMOVED AND REPLACED BATTE RY PACK PER MM. 2 L 7 2 4F RT A16WE 2007031900032 20070319 00032 NM 2007 3 19 CALA0700129 1 20070315 A 5320 6517688U175 ANGLE BOEING 737 737524 1384721 NM BS 277-344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14605 27318 INSPECTION FOUND Z-ANGLE CORRODED AT L-1 DOOR, STA 277-344, BL 0. A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007031900036 20070319 00036 NM 2007 3 19 SWAA071358 1 20070313 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727B S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007031900045 20070319 00045 NM 2007 3 19 UPS07M49379 1 20070125 A 5313 AFA77821 LONGERON DOUG MD11 MD11F 3023600 NM L42R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C FWD CARGO BETWEEN STA 6-10 AND STA 6-30 LONGERON 42R FOUND CORRODED. CORRODED LONGERON REMOVED FOR AC CESS PER SRM 51-31-01 V2 R38. NEW LONGERON P/N AFA7782-1 FAB PER DWG: AFA7782, FOUND SATIS. FPI CUTOUT ON NEW FAB LONG ERON & FOUND NO CRACK EVIDENT. NEW LONGERON FASTENERS & PICK HOLES UP HOLES PER DWG: AFA7782 & SRM 51-31-01 V2 R38. OK TO INSTALL NEW LONGERON & ATT/PARTS RE-INSTALLED PER DWG: AFA7782 & SRM 51-31-01 V1 R38. 2 L 7 3 4F RT A22WE 2007031900054 20070319 00054 WP 2007 3 19 ASMF200703003 1 20070310 A 5330 SKIN DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE BS 389 L25-26R DENTED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 216AM 49586 DURING TRANSIT CHECK, A DENT WAS DETECTED IN THE RT STATIC PORT AREA. DENT WAS LOCATED AT STATION 389 AND LONGERONS 25 A ND 26 RT SIDE AND WAS INSPECTED IAW MM 34-11-01, BEING WITHIN LIMITS. 2 L 7 2 4F 4 F RT A6WE E9NE 2007031900059 20070319 00059 NM 2007 3 19 ASAA0771516 1 20070312 A 5315 146A75036 FLOORBEAM BOEING 737 737790 13844CN NM BS 737 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 AFT CARGO CORROSION FOUND ON CARGO FLOORBEAM AT BS 767+4. REPAIRED IAW EA 5320 01793. 2 L 7 2 4F RT A16WE 2007031900060 20070319 00060 NM 2007 3 19 ASAA0771517 1 20070312 A 5315 146A75032 FLOORBEAM BOEING 737 737790 13844CN NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 AFT CARGO CORROSION FOUND ON CARGO FLOORBEAM AT BS 767. 2 L 7 2 4F RT A16WE 2007031900063 20070319 00063 NM 2007 3 19 ASAA0771520 1 20070312 A 5320 CHANNEL BOEING 737 737790 13844CN NM BS 500B CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 FWD CARGO PIT Z-CHANNEL IS CORRODED AT BS 500D. REPAIRED IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2007031900064 20070319 00064 NM 2007 3 19 ASAA0771521 1 20070312 A 5320 146A75022 SUPPORT BOEING 737 737790 13844CN NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 AFT CARGO PIT RIGHT Z-ANGLE AT BS 727+4 CORRODED. REPAIRED IAW BS 727+4. 2 L 7 2 4F RT A16WE 2007031900090 20070319 00090 WP 2007 3 19 UPS07849363 1 20070213 A 5730 5611360167 SKIN DOUG DC8 DC871F 302199D WP XRS 589 STR 1 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 LEFT UPPER WING SKIN AT XRS 589 BETWEEN STR 1 TO REAR SPAR REQUIRES REPAIR. REPAIRED WING UPPER SKIN IAW SAA EA 008-5730-01-A0656 AND UPS EO DC8-5730-26300-A. 2 L 7 4 4F RT 4A25 2007031900092 20070319 00092 WP 2007 3 19 UPS07849365 1 20070213 A 5730 5611360067 SKIN DOUG DC8 DC871F 302199D WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 LEFT WING UPPER SKIN AT CANT 495 TO XW408 OVER CENTER SPAR REQUIRES REPAIR. REPAIRED WING UPPER SKIN IAW SAA EA 008-5730-01-A0659 AND UPS EO DC8-5730-26300-A. 2 L 7 4 4F RT 4A25 2007031900099 20070319 00099 NM 2007 3 19 AWXA200700351 1 20070219 A 5340 693535222 STRINGER CLIP BOEING 737 7373S3 1384711 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND CRACKED STRINGER CLIP, BS 787, S24R. REPLACED STRINGER CLIP, BS 787, S24R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007031900116 20070319 00116 NM 2007 3 19 USAA070189 1 20070313 A 5340 6935352U14 STRINGER CLIP BOEING 737 737401 1384701 NM BS 727C S4R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 BS 727C, S-4R CRACKED. REMOVED TIE AND INSTALLED NEW ONE PER SRM 51-10-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007031900118 20070319 00118 NM 2007 3 19 USAA070187 1 20070313 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM BS 348 S16L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 TWO CRACKS, MAIN ENTRY DOOR INTERCOSTAL, BS 348, S-16L. FAB'D & INSTALLED TEE, FILLER & STRAP PER EO E5305V203, DEFECT SIZE: 2 INCHES (2 EA). 2 L 7 2 4F RT A16WE 2007031900122 20070319 00122 NM 2007 3 19 USAA070183 1 20070313 A 5340 6935352U14 STRINGER CLIP BOEING 737 737401 1384701 NM BS 727C S7R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 BS 727C S-7R CRACKED. REMOVED CRACK TIE & INSTALLED NEW PER SRM 51-10-02, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007031900123 20070319 00123 NM 2007 3 19 USAA070182 1 20070313 A 5322 SHEAR TIE BOEING 737 737401 1384701 NM BS 360 S14-15L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 STA 360, S14L-S15L CRACKED. FAB'D & INSTALLED NEW SHEAR TIE PER BOEING DWG 69-48204, DEFECT SIZE: .250 INCH. 2 L 7 2 4F RT A16WE 2007031900140 20070319 00140 NM 2007 3 19 SWAA071351 1 20070313 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787 STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031900147 20070319 00147 NM 2007 3 19 07FDEA00722 1 20070308 A 5713 ARB75401 STRINGER DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LEFT WING TANK, APPROX 1/2 INCH LENGTH CRACK FOUND AT STRINGER END 40L (XORS 747), DURING HFEC INSPECTION. (SUPPLEMENTAL 28 MARCH 07) STRINGER END 40L (XORS 747) ON LHW TANK REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007031900148 20070319 00148 NM 2007 3 19 07FDEA00727 1 20070309 A 5753 VANE DOUG MD11 MD11F 3023600 NM TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48470 LEFT WING, INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED. (SUPPLEMENTAL 28 MARCH 07) COMPLIED WITH FEDEX EA 1-5750 -105636, REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007031900149 20070319 00149 NM 2007 3 19 S2YA07001 1 20070211 A 2421 ALT3524 ALTERNATOR DORNER DO32 DO328300 NM ENGINE DAMAGED A S2YA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 GL 13 355SK 14982 797 3124 DURING FLIGHT 2473 MKE-OMA THE CREW CONTACTED MAINTENANCE AND REPORTED A LEFT ALTERNATOR FAIL INDICATION. THE CREW SUCC ESSFULLY RESET THE SYSTEM IN FLIGHT ONLY TO HAVE THE PROBLEM RETURN SHORTLY. IT WAS DETERMINED THAT THE AIRCRAFT SHOULD PERFORM AN AIR TURNBACK TO MKE. A SHORT TIME LATER THE CREW REPORTED A LEFT ENGINE VIBRATION. THE FLIGHT WAS DIVERTED TO MSN. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LEFT ALTERNATOR BEARING AND PART OF THE END CAP HAD BEEN SEVE RELY DAMAGED. THE VIBRATION WAS MOST LIKELY CAUSED BY THE ARMATURE SPINNING LOOSELY IN THE ALTERNATOR CASE CAUSING MORE DAMAGE. 2 H 7 2 4T RT A55NM 2007031900155 20070319 00155 NM 2007 3 19 2007UALA00696 1 20070308 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE 40 HJK & 48 ABC INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EEL 40 HJK & 48 ABC ARE INOPERATIVE. RELAMPED, CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007031900156 20070319 00156 NM 2007 3 19 2007UALA00697 1 20070308 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE 7R & AT DOOR 3R INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY CEILING LIGHTS AT 7R & DOOR 3R ARE INOPERATIVE. RELAMPED, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032000004 20070320 00004 NM 2007 3 20 USAA070195 1 20070315 A 5340 693532U14 STRINGER CLIP BOEING 737 737401 1384701 NM BS 727D S6R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 BS 727D, S6R CRACKED. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-10-02, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007032000007 20070320 00007 NM 2007 3 20 USAA070198 1 20070315 A 5311 FRAME BOEING 737 737401 1384701 NM BS 520 S9R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 BS 520 S-9R, FRAME CRACKED. REPAIRED PER TYPICAL REPAIR 53-10-20D, DEFECT SIZE: .250 INCH. 2 L 7 2 4F RT A16WE 2007032000016 20070320 00016 NM 2007 3 20 UPS07M49381 1 20070131 A 5313 AGA7115 LONGERON DOUG MD11 MD11F 3023600 NM BS 1139 S46R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C FROM STA 6-90 TO 1139, LONGERON 46R CORRODED. CORRODED LONGERON REMOVED FOR ACCESS PER SRM 51-31-01 V 2 R38. NEW LONGERON FAB PER DWG: AGA7115.FPI CUTOUT, ON NEW FAB LONGERON FOUND NO CRACK EVIDENT. NEW FAB LONGERON, OK TO INSTALL. NEW LONGERON & ATT/PARTS RE-INSTALLED PER SRM 51-31-01 V2 R8 & DWG: AGA7115. 2 L 7 3 4F RT A22WE 2007032000017 20070320 00017 NM 2007 3 20 UPS07M49382 1 20070131 A 5313 AGA67137 LONGERON DOUG MD11 MD11F 3023600 NM BS 1139 S47R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C STA 6-90 TO STA 1139, LONGERON 47R CORRODED. CORRODED LONGERON ATT/PARTS REMOVED FOR ACCESS PER SRM 5 1-31-01 V2 R38. NEW LONGERON FAB PER DWG: AGA6713, P/N: AGA6713-7. NEW LONGERON PROTECTED PER SRM 51-21-01 V2 R38. N EW LONGERON OK TO INSTALL. NEW LONGERON & ATT / PARTS RE-INSTALLED PER DWG: AGA6713 & SRM 51-31-01 V2 R38, FOUND SATISF ACTORY. 2 L 7 3 4F RT A22WE 2007032000048 20070320 00048 NM 2007 3 20 SWAA071376 1 20070313 A 3350 079123 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 487WN 33854 EEPLS COVER LOOSE AND WIRES EXPOSED AT FWD END. SECURED EEPLS COVER & REPOSITIONED WIRES PER MM. 2 L 7 2 4F RT A16WE 2007032000049 20070320 00049 NM 2007 3 20 SWAA071393 1 20070314 A 3350 101114 LENS BOEING 737 7373T5 1384608 NM EMERGENCY LIGHTS CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED C2 CHECK, FOUND LT LOWER AFT EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007032000050 20070320 00050 NM 2007 3 20 SWAA071397 1 20070315 A 2121 215201 GASPER FAN BOEING 737 7377H4 1384404 NM A/C COMPT FAULTY A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 29 444WN 29839 FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. BOTH A/C PACKS ON, GASPER FAN ON, RECIRC FAN OFF. REMOVED AND REPLACED G ASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2007032000052 20070320 00052 NM 2007 3 20 SWAA071395 1 20070314 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 434 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 434, STR 16R. REPAIRED SKIN PER SRM & EA. 2 L 7 2 4F RT A16WE 2007032000054 20070320 00054 NM 2007 3 20 SWAA071386 1 20070314 A 5311 6546525 FRAME BOEING 737 7373Y0 1384671 NM BS 369 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 369, STR 9L. REPAIRED FRAME PER EA. 2 L 7 2 4F RT A16WE 2007032000056 20070320 00056 NM 2007 3 20 SWAA071390 1 20070314 A 5310 6547952 DOOR FRAME BOEING 737 7373Q8 1384670 NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR UPPER FRAME CRACKED AT PULLEY BRACKET LOCATION. REMOVED AND REPLACED D OOR FRAME PER SRM & BAC DRAWING. 2 L 7 2 4F RT A16WE 2007032000057 20070320 00057 NM 2007 3 20 SWAA071391 1 20070314 A 5310 6547952 DOOR FRAME BOEING 737 7373Q8 1384670 NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR LOWER FRAME CRACKED AT PULLEY BRACKET LOCATION. REMOVED AND REPLACED D OOR FRAME PER SRM & BAC DRAWING. 2 L 7 2 4F RT A16WE 2007032000060 20070320 00060 EU 2007 3 20 YENA2007015 1 20070310 A 5230 FITTING EMB ERJ190 ERJ190100IGW 3260408 EU CARGO DOOR DAMAGED A YENA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 15 187JB 19000009 AFT CARGO DOOR OPEN INDICATION AFTER TAKEOFF AT 500 FEET. RETURNED TO JFK AT 5000FT & 210 KIAS. STARTED FEELING VIBRAT IONS WHEN ACCELERATING TO 190 KIAS. VB WENT AWAY AT 180 KIAS. VISUAL INDICATION THAT DOOR WAS OPEN. LANDED UNEVENTFUL LY. INSPECTED AFT CARGO DOOR & SURROUNDING STRUCTURE AS PER EA E-07-088. REPAIRED DAMAGED AFT CARGO DOOR AFT FRAME ROL LER FITTING & ACCESS COVER AS PER EA E-07-089 & EA E-07-090B PART 1 DOOR FRAME INSPECTION. OPERATION & INDICATOR CHECKE D NORMAL. OK FOR SERVICE. 2 L 7 2 4F RT A57NM 2007032000062 20070320 00062 NM 2007 3 20 SWAA071378 1 20070314 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 294 S13L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007032000065 20070320 00065 NM 2007 3 20 PIDA07010 1 20070305 A 5754 SKIN BOEING 757 757236 1384971 NM NR 5 SLAT DELAMINATED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 757BJ 22176 DURING INSPECTION FOUND LEADING EDGE OF LEFT WING AT THE NR 5 SLAT DELAMINATED SIX INCHES FROM THE OUTBOARD END ON THE U PPER SURFACE. REPAIRED AREA PER SRM 57-41-01 AND SRM 51-70-17 WITH MINOR DEVIATIONS PER EA 57-046. 2 L 7 2 4F RT A2NM 2007032000066 20070320 00066 NM 2007 3 20 SWAA071379 1 20070314 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 597 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 4L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007032000067 20070320 00067 NM 2007 3 20 SWAA071381 1 20070314 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 616 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007032000069 20070320 00069 NM 2007 3 20 SWAA071383 1 20070314 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 277 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007032000071 20070320 00071 NM 2007 3 20 SWAA071385 1 20070314 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727D S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007032000072 20070320 00072 NM 2007 3 20 SWAA071387 1 20070314 A 5313 BAC1498 STRINGER BOEING 737 7373Y0 1384671 NM BS 706 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER 9L CRACKED AT BS 706. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007032000073 20070320 00073 NM 2007 3 20 SWAA071377 1 20070313 A 3350 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 793SA 27888 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT 11 ABC. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2007032000077 20070320 00077 EA 2007 3 20 COMA0760240 1 20070308 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 685BR 7712 FLIGHT 5564 - FLAPS FAIL CAUTION MESSAGE WHEN SELECTED FROM ZERO DEGREES ON APPROACH. A/C LANDED SAFELY. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007032000078 20070320 00078 2007 3 20 DJFA2007003 4 20070101 A 3460 C500 EFB RAYTHN DH125 HAWKER800XP 7150012 CE COCKPIT BURNED E DJFA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 813CW 258413 TRIP NR 1124325, CREW REPORTED THAT RT ELECTRONIC FLIGHT BAG (EFB) GOT HOT. SMELLED AND SMOKE WAS EVIDENT COMING FROM TH E UNIT. FLIGHT CONTINUED TO DESTINATION USING SECOND EFB. MAINTENANCE CONFIRMED THE FAILED UNIT AND THE RT FUJITSU WAS REPLACED WITH A SERVICEABLE UNIT. 2 L 7 2 4F RT A3EU 2007032000079 20070320 00079 NM 2007 3 20 CALA0700127 1 20070313 A 3350 ADD71701100 BATTERY PACK BOEING 737 737724 13844BY NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24706 28767 INSPECTION FOUND AFT HALF SECTION OF AISLE PATH LIGHTING INOPERATIVE DURING RON. THE BATTERY PACK FOR M1672 CHARGER WAS FOUND AT FAULT, REF W/D 33-51-11. THE BATTERY PACK WAS REPLACED. 2 L 7 2 4F RT A16WE 2007032000080 20070320 00080 NM 2007 3 20 UIEA200700129 1 20070302 A 5330 65B04193601 SKIN BOEING 747 7472D3B 1384805 NM BS 1241 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 FOUND M/DECK STA1241 FRAME AND SKIN SPLICE AREA HAS HOLE, CRACKED AND CORRODED. REPAIRED ACCOMPLISHED AS PER BOEING MES SAGE NR 1-29020776-1 AND -6 AND FAA FORM 8100-9. 2 L 7 4 4F RT A20WE 2007032000082 20070320 00082 NM 2007 3 20 UIEA200700135 1 20070305 A 5280 STRUCTURE BOEING 747 747243B 1384830 NM MLG DOOR CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 000300 23300 DURING WALK AROUND, FOUND LEFT WING GEAR INBOARD SHOCK STRUT DOOR DAMAGED ALONG THE LOWER 27" OF THE T/E WITH APPROX 7" DAMAGE ON DOOR FAIRING. LEFT WING GEAR INBOARD CHOCK STRUT DOOR ASSY REMOVED IAW CDL 32-12-1. REPLACED LOWER STRUT DOO R AND FAIRING AS PER AMM 32-12-05 AND 32-12-06, PERFORMED LOWER GEAR RETRACTION DOOR ADJUSTMENTS AND LOWER GEAR EXTENSIO N AS PER AMM 32-32-00 & 32-72-00, ALL OPS TEST WERE OK. 2 L 7 4 4F A20WE 2007032000083 20070320 00083 NM 2007 3 20 UIEA200700111 1 20070306 A 5414 SKIN BOEING 747 7472D7B 1384803 NM `NR 4 NACELLE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 21784 NR 4 PYLON PRECOOLER EXHAUST CUT-OUT SKIN ASSEMBLY AND DOUBLERS CRACKED. PYLON REPAIRED AS PER BOEING MESSAGE 1-2890156 78-8. 2 L 7 4 4F RT A20WE 2007032000086 20070320 00086 NM 2007 3 20 UIEA200700128 1 20070302 A 5730 65B9081352 DOUBLER BOEING 747 7472D3B 1384805 NM RT WING SEPARATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 NR 3 PYLON FWD FIXED FAIRING LT EXTERIOR SURFACE AFT CORNER SKIN DOUBLER SEPARATED. FAIRING REPLACED BUT NUMEROUS FASTE NERS HOLES FOUND MISALIGNED. TIME LIMIT REPAIRED ACCOMPLISHED AS PER BOEING MESSAGE NR 1-292185930-1 THRU -14, DWG 65B9 0813-52 AND FAA FORM 8100-9. 2 L 7 4 4F RT A20WE 2007032000088 20070320 00088 NM 2007 3 20 2007UALA00685 1 20070306 A 3260 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NLG WARNING UNKNOWN A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 510UA 24780 ON CLIMBOUT, RECEIVED EICAS STATUS MSG: NOSE A-G DISAGREE. [SUP 05-18-07] CREW SAID, NOSE A-G DISAGREE DISPLAYED DURI NG CLIMB & REMAIN DISPLAYED, NO OTHER DISCREPANCY NOTED. REPLACED LT NOSE GEAR NOT COMPRESSED SENSORS 2 L 7 2 4F 4 F RT A2NM E17NE 2007032000092 20070320 00092 CE 2007 3 20 DXTA200702023 1 20070315 A 3230 LANDING GEAR BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE RIGHT INOPERATIVE E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 131QS RK431 COULD NOT GET RT MAIN GEAR LIGHT USED ALTERNATE GEAR EXTENSION. TROUBLESHOT SYSTEM AND FOUND RT MLG DOWNLOCK SWITCH TO BE SHORTED AND NOT REPORTING POSITION. REMOVED AND INSTALLED NEW SWITCH IAW HAWKER 400XP MM 32-60-00. OPS CHECK OF SYSTE M SHOWS NORMAL OPERATION OF GEAR AND EMER DOOR CLOSE HANDLE. ALL WORK IAW HAWKER MM 400XP 32-60 AND 32-10. 2 H 7 2 4F 4 F RT A16SW E25EA 2007032000093 20070320 00093 NM 2007 3 20 DXTA200702024 1 20070315 A 3230 DCU GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE RT MLG INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 706QS 131 RT MAIN LANDING GEAR WOULD NOT COME UP YELLOW INDICATOR THEN RED. CYCLED ONE TIME DID NOT CHANGE. DCU INOP. REMOVED DC U AND INSTALLED AN INSPECTED UNIT IAW CH 31-50-00 OF THE G-200 MM OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A53NM E35NE 2007032000094 20070320 00094 CE 2007 3 20 DXTA200702025 1 20070315 A 2700 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL STAB UNKNOWN E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 990QS 7500190 WHEN SWITCHING FROM FGS (A) TO FGS (B) THE CLACKER COMES ON IMMEDIATELY AND DOES NOT STOP. THE STAB DOES NOT MOVE. SWITC HING BACK TO FGS (A) CANCELS THE CLACKERS. REMOVE AND REPLACED FGC CONTROLLER WITH REPAIRED UNIT FROM HONEYWELL RS LV2R 992K PER CESSNA 750 MAINT. MANUAL CHAPTER 22-10-03. GROUND OP'S CHECKED GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007032000095 20070320 00095 CE 2007 3 20 DXTA200702026 1 20070315 A 2720 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RUDDER LIMIT UNKNOWN E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 902QS 7500002 RUDDER LIMIT (B) FAIL CAS MESSAGE CAME ON IN CRUISE AT FL300/ .85/ 21 PERCENT. REMOVED & REPLACED "B" RUDDER LIMITER AC TUATOR, OPERATIONALY CHECK'S GOOD IAW CE750 MM 27-20-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007032000096 20070320 00096 CE 2007 3 20 DXTA200702027 1 20070316 A 2611 SMOKE DETECTOR RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP CARGO BAY CONTAMINATED E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 872QS 258472 RED (BAGGAGE FIRE) ANNUNCIATOR ILLUMINATED MOMENTARILY (3) TIMES DURING DESCENT. NO SMOKE OR VISUAL INDICATION OF FIRE P RESENT. CLEANED SMOKE DETECTOR GRILLS AND BLEW OUT DUST INSIDE UNITS. PERFORMED TEST OF SMOKE DETECTOR UNITS PER HAWKER 800XP MMA 26-11-00-001 NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A3EU E6WE 2007032000099 20070320 00099 CE 2007 3 20 DXTA200702030 1 20070316 A 2720 YAW DAMPER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL INOPERATIVE E DXTA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 07 949QS 7500049 DURING TAKEOFF ACCELERATION THE LOWER YAW DAMPER THEN KICKED OFF AND THE TAKEOFF WAS DISCONTINUED. REPLACE NR 2 NOSEWHE EL PER MAINTENANCE CONTROL. (NR 1 ALSO REPLACED DUE TO IMPROPER TORQUE) IAW CESSNA 750 MM 32-41-01 (NOSE WHEEL ASSY. W/T IRE) 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007032000100 20070320 00100 NM 2007 3 20 2007UALA00689 1 20070306 A 3810 OUTFLOW VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN WATER STUCK A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 213UA 30219 FLIGHT DIVERTED DUE TO NO WATER PRESSURE. PRE-SELECT OVERFLOW VALVE FOUND TO STICK IN SEMI-CLOSED POSITION. PRIOR TO R EPLACEMENT- CHECKED LINKAGES, INDICATION & VALVE OPERATION. VLV OPERATION NORMAL WITH PRE-SELECT KNOB MOVEMENT AT FWD S ERVICE PANEL. PRECAUTIONARY: REPLACED PRE-SELECT OVERFLOW VALVE. OPS CHECK OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007032000101 20070320 00101 SO 2007 3 20 N93A06032007A 1 20070306 A 3260 SWITCH GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU MLG OUT OF ADJUST E N93A O OTHER J WARNING INDICATION LD LANDING 1 SO 13 405QS 275 4054 NOSE STEERING INOP ON LANDING. ADJUSTED WEIGHT ON WHEELS SWITCH, PERFORMED TAXI CHECK AND TOUCH AND GO LANDINGS. NO FURT HER DEFECTS. 2 L 7 2 4F 4 F RT A12EA E25NE 2007032000102 20070320 00102 EU 2007 3 20 2007UALA00690 1 20070306 A 3010 BLEED AIR SYS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT WING LEAKING A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 410UA 463 DIVERTED DUE TO A LEFT WING BLEED LEAK. LT WING LEAK DISPLAYED ON UPPER ECAM SCREEN-AIR. FOUND LOOSE DUCTING AND CL AMPS JUST ABOVE THE EXTERNAL AIR CART HOOK UP. RESEATED DUCT AND RESECURED CLAMPS NO FURTHER DEFECTS NOTED. ACCOMPLISH ED LEAK CHECK OF DUCK AND NO LEAKS NOTED. ECAM MESSAGE GONE AND SYSTEM OPS CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032000119 20070320 00119 NM 2007 3 20 2007UALA00711 1 20070308 A 5210 BEARING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT PAX DOOR WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 364UA 24533 AFT ENTRY DOOR FUSELAGE TORQUE TUBE UPPER AND LOWER SERPENTINE PLATE BEARINGS ARE WORN. MAJOR REPAIR ACCOMPLISHED: REM OVED & REPLACED UPPER & LOWER BEARINGS. INSTALLED PLATES. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032000120 20070320 00120 2007 3 20 2007UALA00712 4 20070308 A 2565 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE/RAFT READS LOW A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 543UA 25698 TWO EACH CABIN LIFE RAFTS, CYLINDER PRESSURE GAUGE NEEDLES ARE IN RED BAND (LOW PRESSURE). [SUP 05-18-07] LOW BOTTLE P RESSURE ATTRIBUTED TO A LEAKING GAUGE O-RING, WHICH APPARENTLY FAILED TO SEAL. FILL VALVE WAS FOUND LOOSE. TIGHTENED VA LVE AND RETESTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032000121 20070320 00121 NM 2007 3 20 2007UALA00713 1 20070308 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 DENT IN FUSELAGE LEFT SIDE JUST FWD OF LAV SERVICE PANEL. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED & FABRICATED & IN STALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032000122 20070320 00122 NM 2007 3 20 2007UALA00714 1 20070308 A 5313 STRINGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1210-1219 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 AFT PIT STR 36L AT STA 1210 TO 1219 IS CORRODED. MAJOR REPAIR ACCOMPLISHED: FORMED NEW STRINGER SECTION. INSTALLED N EW SECTION WITH SPLICES, ANGLES AND CHORD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007032000123 20070320 00123 EU 2007 3 20 2007UALA00715 1 20070308 A 2913 PUMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYD SYSTEM FAILED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 487UA 1669 LANDED UNDER AMBER ALERT DUE TO LOSS OF GREEN HYDRAULIC ENGINE PUMP. [SUP 05-29-07] REPLACED ENG NR 1 HYDRAULIC PUMP A ND CASE DRAIN FILTER. HYDRAULIC PUMP WAS OVERHAULED, BUT NOTHING WAS FOUND TO BE OUT OF SPEC. SEVERAL FLIGHTS LATER, THE ERROR MESSAGE REOCCURRED. FURTHER FAULT TRACING DETERMINED THAT THE GREEN HYDRAULIC SYSTEM PRESSURE SWITCH WAS FAULTY A ND REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032000124 20070320 00124 SO 2007 3 20 N93A06032007 1 20070306 A 2820 1159P4201139 LINE GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU FUEL SYS DAMAGED E N93A O OTHER J WARNING INDICATION CR CRUISE 1 SO 13 477QS 7156 1377 UNCOMMANDED FUEL TRANSFER FROM ONE WING TO ANOTHER. MAINTENANCE FOUND FUEL TUBE DAMAGED. 2 L 7 2 4F 4 F RT A12EA E25NE 2007032000125 20070320 00125 NM 2007 3 20 2007UALA00716 1 20070308 A 2820 FUEL SYS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUEL TRANSFER MALFUNCTIONED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 121UA 29167 UNWANTED FUEL TRANSFER FROM CTR INTO NR 2 MAIN TANK IN FIRST HOUR OF FLIGHT. TANK ENTRY & TROUBLESHOOTING IDENTIFIED FUE L JETTISON PUMP CHECK VALVE NOT FULLY CLOSING. REPLACED VALVE & AIRCRAFT RETURNED TO SERVICE. SUSPECT VALVE WEAR LED TO HANG-UP WHICH PREVENTED CLOSING. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032000126 20070320 00126 2007 3 20 2007UALA00717 4 20070308 A 2565 5A29011 ASPIRATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ESCAPE SLIDE UNSERVICEABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA PF0115 25392 BOTH ASPIRATORS DID NOT CLOSE SHUT WHEN DEPLOYED. SLIDE REPLACED. AIRCRAFT OK FOR SERVICE. REPLACED BOTH ASPIRATORS I N RIGHT O/W SLIDE. SUSPECT ASPIRATORS SUFFERED CRUSHED FLEX-CYLINDER DURING INSTALLATION. 2 L 7 2 4F 4 F RT A1NM E24NE 2007032000127 20070320 00127 NM 2007 3 20 2007UALA00718 1 20070308 A 8011 STARTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 523UA 24932 726622 DURING RT ENG START, NO N2, NO N1, RAMP REPORTED SPARKS FROM RIGHT ENGINE. [SUP 05-18-07] REPLACED STARTER DUE TO LOW OIL. ALSO REPLACED STARTER VALVE DUE TO FOD FROM STARTER FAILURE. OP CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032000128 20070320 00128 NM 2007 3 20 UIEA200700118 1 20070302 A 5414 SKIN BOEING 747 747243B 1384830 NM NR 3 NACELLE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 NR 3 PYLON TOP SKIN, AFT EDGE, ABOVE LINK FITTING HAS A 0.375 INCH CRACK. TRIMMED OUT SKIN TO REMOVE CRACK AS PER 747 S RM 51-10-01. ACCOMPLISHED HFEC INSPECTION TO VERIFY REMOVAL OF CRACK AS PER 747 NDT MANUAL PAR 6 SECTION 51-00-00 FIG 4 . ALSO, REFERENCE ATLAS AIR XEO NR 54-022807. 2 L 7 4 4F A20WE 2007032000129 20070320 00129 NM 2007 3 20 UIEA200700119 1 20070302 A 5730 PANEL BOEING 747 747243B 1384830 NM RT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 RIGHT WING, UPPER TRAILING EDGE PANEL, OUTBOARD OF NR 8 SPOILER HAS A 7.0 INCH LONG BY 1.5 INCH WIDE CRACK. PERMANENT R EPAIR WAS ACCOMPLISHED AS PER 747-200 SRM 51-40-09, FIG 2, TABLE 1 AND SRM 51-40-12. ALSO, REFERENCE ATLAS AIR XEO NR 5 7-030107. 2 L 7 4 4F A20WE 2007032000130 20070320 00130 EA 2007 3 20 COMA0760246 1 20070310 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 951CA 7091 FLIGHT 4975 - DURING GRR APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAG E -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007032000131 20070320 00131 NM 2007 3 20 UIEA200700123 1 20070302 A 5720 22173831 ANGLE BOEING 747 747243B 1384830 NM RT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 VERTICAL "L" EXTRUSION ANGLE CRACKED AT RIGHT WING UPPER SURFACE, BELOW GAP PANEL 611CT FOR NR 3 PYLON AT INBOARD SIDE, FORWARD CORNER, WING STATION 670.25. REMOVED AND REPLACED "L" ANGLE EXTRUSION P/N 221738-3-1 AS PER 747-200 SRM 51-30-0 2 AND SRM 51-10-02. ALSO, REFERENCE ATLAS AIR XEO NR 57-030107-1. 2 L 7 4 4F A20WE 2007032000132 20070320 00132 NM 2007 3 20 USAA200703002 1 20070307 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 727E S24L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 531AU 24478 SKIN CRACK 2.5 INCH LONG LT FUSELAGE STA 727E, STRINGER 24L. CUT OUT DAMAGE, APPLIED REPAIR DOUBLER PER SRM 53-00-01, R EP 31, & TYP REP 53-60-03A. 2 L 7 2 4F RT A16WE 2007032000133 20070320 00133 EA 2007 3 20 COMA0760245 1 20070310 A 2410 7578137101 FILTER CNDAIR CL600 CL6002B19 1900309 EA RT IDG CLOGGED A COMA C ABORTED TAKEOFF J H WARNING INDICATION ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SO 01 927CA 7031 FLIGHT 5671 - DURING THRUST INCREASE FOR TAKEOFF RECEIVED A 2 IDG CAUTION MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE G ATE. REPLACED THE RIGHT IDG FILTER ELEMENT. 2 L 7 2 4F RT A21EA 2007032000134 20070320 00134 NM 2007 3 20 UIEA200700125 1 20070302 A 5330 65B082416 SKIN BOEING 747 7472D3B 1384805 NM BS 1319 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 M/DECK RT NR 3 MED CUTOUT AFT UPPER CORNER SKIN STA1319, STR 17R-18R FOUND CORRODED. REPAIRED ACCOMPLISHED AS PER BOEIN G MESSAGE NR 1-289657194-1, 747 SRM 53-30-03 FIG 44 AND FAA FORM 8100-9. 2 L 7 4 4F RT A20WE 2007032000135 20070320 00135 NM 2007 3 20 UIEA200700121 1 20070302 A 5411 FRAME BOEING 747 747243B 1384830 NM NR 1 NACELLE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 NR 1 PYLON AFT UPPER BULKHEAD "T" FRAME HAS A CRACK AT AFT FLANGE AND A SECOND CRACK AT FORWARD FLANGE, OUTBOARD OF NR 1 PYLON FRONT SPAR CHORD ASSEMBLY. AFT FLANGE CRACK IS 0.750 INCH LONG. FORWARD FLANGE CRACK IS 0.375 INCH LONG AT NACEL LE STATION 270.00. ACCOMPLISHED INTERIM REPAIR AS PER 747-200 SRM 51-30-02 AND ATLAS AIR XEO NR 54-030107, FAA FORM 8110 -3 ISSUED AND APPROVED. PERMANENT REPAIR TO BE ACCOMPLISH AT NEXT "C" CHECK. 2 L 7 4 4F A20WE 2007032000136 20070320 00136 NM 2007 3 20 UIEA200700105 1 20070302 A 5322 SHEAR TIE BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE BS 860 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 21784 BS 860L TENSION TIE ATTACHMENT FOUND ONE HOLE CRACKED. TENSION TIE REPAIRED AS PER BOEING MESSAGE DRAWING 1-283852979-4 . 2 L 7 4 4F 4 F RT A20WE E23EA 2007032000137 20070320 00137 NM 2007 3 20 UIEA200700104 1 20070301 A 5330 DOUBLER BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE BS 800 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 21784 BS 800 STR 19R DOOR CUTOUT DOUBLER FOUND CRACKED. REPAIRED PER BOEING MESSAGE 1-285788451-4. TRIMMED AND REMOVED DAMAG ED FRAME STRAP NDT AREA. FABRICATED REPAIR STRAP AND DOUBLER. ALODINED AND COATED WITH BMS 5-95 BETWEEN MATING SURFACE . INSTALLED HI LOCKS WET WITH BMS 5-95. 2 L 7 4 4F 4 F RT A20WE E23EA 2007032000138 20070320 00138 NM 2007 3 20 UIEA200700115 1 20070302 A 5714 SKIN BOEING 747 7472D7B 1384803 NM BS 1240 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 21784 FOUND BS 1240 LBL 99 WING CENTER SECTION SKIN CORRODED. CORROSION REMOVED PER SRM 51-10-01. AREA HFEC INSPECTED AND FL AT PEENED. REPAIR DOUBLER WERE FABRICATED AND INSTALLED PER 8100-9. 2 L 7 4 4F RT A20WE 2007032000139 20070320 00139 NE 2007 3 20 UIEA200700132 2 20070302 A 7261 6506606 OIL FILTER BOEING 747 747228F 1384895 NM GE CF6 CF650E2 30018 NE NR 2 ENGINE UNSERVICEABLE A UIEA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 EA 15 809MC 20887 528106 NR 2 OIL FILTER BY PASS LIGHT ILLUMINATED DURING DESCENT, LIGHT REMAINED AT IDLE THRUST, SHUT DOWN NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE OIL FILTER AS PER MM 79-21-04. PERFORMED ENGINE RUN NO LEAK NOTED. 2 L 7 4 4F 4 F A20WE E23EA 2007032000140 20070320 00140 NM 2007 3 20 UIEA200700116 1 20070302 A 5330 BEAR STRAP BOEING 747 7472D7B 1384803 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 21784 FOUND CRACK IN BEARSTRAP HOLE FORWARD CARGO DOOR FORWARD UPPER CORNER. REAMED HOLE COMMON TO SKIN AND BEARSTRAP TO REMO VE CRACK INDICATION AND INSTALLING FREEZE PLUG AND OVERSIZED FASTENER AS PER BOEING MESSAGE 1-285675404-1 AND 8100-9. 2 L 7 4 4F RT A20WE 2007032000141 20070320 00141 2007 3 20 UIEA200700133 4 20070302 A 2211 2591415905 VALVE BOEING 747 747243B 1384830 NM NR 3 PYLON UNSERVICEABLE A UIEA O OTHER J WARNING INDICATION CR CRUISE 1 EA 15 517MC 23300 WHEN "A" AUTOPILOT IS CONNECTED THE ACF GOES INTO A STEEP DIVE WITH STAB TRIM "A" LIGHT ON ALL ATTITUDE. WHEN AUTOPILOT "B" IS CONNECTED A/C PORPOISES + - 1,200 FRM WITH STAB TRIM "B" LIGHT ON. THIS HAPPENED ABOVE FL 27.0. IF FLYING AT 27 .0 IT MAINTAINED A GOOD LEVEL CRUISE, TX DMI M07-028 PER MEL 22-1 PLACARD INSTALLED. REMOVED AND REPLACED AUTO STAB TRI M UNIT IAW 22-14-01, OPS CHECK OK. REMOVED AND REPLACED NR 3 PYLON VALVE IAW MM 36-11-04, OPS CHECK OK. PERFORMED OPS CHECK OF NR 4 PYLON VALVES AS PER MM 36-00-00, OPS CHECK NORMAL. 2 L 7 4 4F A20WE 2007032000142 20070320 00142 NM 2007 3 20 UIEA200700117 1 20070302 A 5311 FRAME BOEING 747 7472D7B 1384803 NM BS 360 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 21784 CRACK FOUND IN THE FRAME WEB AT STATION 360 STR 14ER CUTOUT. THE CRACK IN THE FRAME WEB WERE INSPECTED AND A .063" DOUB LER WAS INSTALLED AS PER BOEING MESSAGE 1-28580146-3/5 AND 8100-9. 2 L 7 4 4F RT A20WE 2007032000143 20070320 00143 NM 2007 3 20 UIEA200700108 1 20070303 A 5310 WINDOW FRAME BOEING 747 7472D7B 1384803 NM BS 340 S8L CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 21784 NR 3L WINDOW FRAME FOUND CRACK AT STATION 340 STR 8L SKIN LOWER CORNER. SKIN REPAIRED AS PER BOEING MESSAGE 1-289012478 -7 AND 12 AND 8100-9. 2 L 7 4 4F RT A20WE 2007032000144 20070320 00144 NM 2007 3 20 UIEA200700134 1 20070302 A 5330 BEAR STRAP BOEING 747 7472D7B 1384803 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 21784 NR 3L DOOR CUT-OUT FORWARD LOWER BEAR STRAP CRACKED. NR 3L DOOR CUT-OUT FORWARD LOWER BEAR STRAP CRACK REPAIRED AS PER EO4753A751 OPTION 2. INSTALLED WITH LARGE DOUBLER. 2 L 7 4 4F RT A20WE 2007032000145 20070320 00145 NM 2007 3 20 UIEA200700114 1 20070302 A 5313 LONGERON SPLICE BOEING 747 7472D7B 1384803 NM BS 2598 L11R CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 21784 BS 2598 OUTER CHORD STR 11R FWD AND AFT LOWER LONGERON SPLICE FITTING FOUND BOLT HOLE CORROSION CRACK. FORWARD AND AFT SPLICE FITTING REPLACED PER SRM 51-10-01 PAGE 9 AND SB 74753A2410. 2 L 7 4 4F RT A20WE 2007032000146 20070320 00146 CE 2007 3 20 031707N319CS1 1 20070317 A 3260 MS25237327 BULB CESSNA 500 550 2076604 CE MLG INDICATOR INOPERATIVE E Z5FA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 63 319CS 5501036 DURING APPROACH, WHEN GEAR WAS EXTENDED THERE WAS NO GREEN DOWN INDICATION FOR LT MAIN GEAR. ABORTED APPROACH AND CLIMBE D TO SAFE ALTITUDE, PERFORMED AFM EMERGENCY CHECK LIST PROCEDURES. LANDING GEAR WAS BLOWN DOWN AND CREW DECLARED EMERGE NCY AND LANDED UNEVENTFULLY. ON SITE MAINTENANCE FOUND LEFT GEAR DOWN LIGHT BULB INOPERATIVE. BULB REPLACED, GEAR SWUNG AND SYSTEM OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 4F A22CE 2007032000147 20070320 00147 2007 3 20 SA07022 4 20070312 A 2565 GIRT BAR AIRBUS A321 A321211 3930370 EU ZONE 200 OUT OF ADJUST A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 163US 1417 PHL - THE CABIN CREW STATED THAT THE EMERGENCY ESCAPE SLIDE ARMING LEVER AT DOOR 4L KEEPS POPPING OUT. MAINTENANCE ADJU STED THE GIRT BAR FITTING. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2007032000148 20070320 00148 NM 2007 3 20 ASAA0771522 1 20070312 A 5320 146A75021 ANGLE BOEING 737 737790 13844CN NM BS 727-849 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 AFT CARGO PIT Z-ANGLE AT BS 727+4 FOUND CORRODED. REPAIRED IAW SRM 53-00-53 FIG 502. 2 L 7 2 4F RT A16WE 2007032000149 20070320 00149 NM 2007 3 20 ASAA0771523 1 20070312 A 5347 146A75011 CARGO TRACK BOEING 737 737790 13844CN NM BS 787 WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 AFT CARGO PIT LEFT TIE DOWN TRACK WORN AT BS 787. REPAIRED IAW 53-00-53 FIG 201. 2 L 7 2 4F RT A16WE 2007032000150 20070320 00150 NM 2007 3 20 ASAA0771524 1 20070312 A 5347 146A750125 CARGO TRACK BOEING 737 737790 13844CN NM BS 794 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 AFT CARGO RIGHT TIE DOWN TRACK CORRODED AT BS 794. REPAIRED IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2007032000151 20070320 00151 NM 2007 3 20 ASAA0771525 1 20070312 A 5311 146A126241 FRAME BOEING 737 737790 13844CN NM BS 787 MAINT ERROR A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 AFT CARGO PIT FRAME AT BS 787 DOUBLE DRILLED. REPAIRED IAW SRM 51-70-11. 2 L 7 2 4F RT A16WE 2007032000152 20070320 00152 NM 2007 3 20 ASAA0771526 1 20070312 A 5315 146A940121 FLOORBEAM BOEING 737 737790 13844CN NM BS 887 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 AFT CARGO PIT FLOORBEAM CORRODED AT BS 887. REPAIRED IAW SRM 53-60-53 FIG 2. 2 L 7 2 4F RT A16WE 2007032000153 20070320 00153 NM 2007 3 20 ASAA0771527 1 20070312 A 5320 146981571 FLOOR SUPPORT BOEING 737 737790 13844CN NM BS 767-787 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 AFT CARGO PIT FLOOR SUPPORT AT BS 767 CORRODED. REPAIRED IAW SRM 53-60-15 FIG 5. 2 L 7 2 4F RT A16WE 2007032000154 20070320 00154 NM 2007 3 20 ASAA0771528 1 20070312 A 5347 146A75011 CARGO TRACK BOEING 737 737790 13844CN NM BS 787 WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 AFT CARGO PIT LEFT TIE DOWN TRACK WORN AT BS 787. REPAIRED IAW SRM 53-60-53. 2 L 7 2 4F RT A16WE 2007032000155 20070320 00155 NM 2007 3 20 WRLA2007046 1 20070312 A 5315 FLOORBEAM DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE BROKEN A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271WA 48518 DURING C-04 CHECK, FOUND FLOORBEAM BULKHEAD BROKEN AT STA Y=1841 X=42. REPAIRED PER SRM VOL.III 53-16-01 REV.38 AND SRM 53-00-01 VOL.I FIG.10 REV.38 2 L 7 3 4F 4 F RT A22WE E24NE 2007032000156 20070320 00156 NM 2007 3 20 2007UALA00728 1 20070309 A 3350 78671 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EMERGENCY LIGHT INOP ROW 35 ABC. REPLACED LAMP. OP CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032000158 20070320 00158 EU 2007 3 20 2007UALA00737 1 20070312 A 3230 CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MLG MALFUNCTIONED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 410UA 463 GEAR DID NOT RETRACT PROPERLY ON DEPARTURE. ALL OK ON 2ND ATTEMPT. [SUP 05-29-07] REPLACED NR 2 LANDING GEAR CONTROL AND INDICATING UNIT AND LANDING GEAR SELECTOR VALVE. AT OVERHAUL, NOTHING WAS FOUND TO BE OUT OF SPEC WITH THE LGCIU OR THE SELECTOR VALVE. LATER IT WAS DETERMINED THAT THE PROXIMITY SENSOR WAS FAULTY AFTER THE SAME FAULT OCCURRED SEVERAL F LIGHTS LATER. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032000159 20070320 00159 NM 2007 3 20 2007UALA00738 1 20070310 A 2730 ROD END AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE ELEVATOR WORN A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 848UA 1647 LOUD RAPPING NOISE IN TAIL SECTION ON TAKEOFF. WENT AWAY BUT FOLLOWED BY MODERATE VIBRATION IN AFT CABIN. [SUP 05-29-0 7] VISUALLY CHECKED THE HORIZONTAL STABILIZER JACKSCREW COMPARTMENT AND DID NOT FIND ANY MECHANICAL DEFECTS. ALSO CHECK ED ELEVATORS AND FOUND ALL 4 CONTROL SERVOS TO BE OUT OF ADJUSTMENT. ADJUSTED ALL CONTROL SERVOS TO NEUTRAL CONDITION, B UT STILL FOUND LEFT ELEVATOR TO HAVE EXCESSIVE FREEPLAY. REPLACED BOTH GREEN AND BLUE SYSTEM ELEVATOR CONTROL SERVOS. AT OVERHAUL, FOUND WORN ROD END ASSEMBLIES ON BOTH CONTROL SERVOS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032000160 20070320 00160 EU 2007 3 20 WRNA200700014 1 20070309 A 3240 286467100 SERVO VALVE AIRBUS 300 A300B4203 3930306 EU NR 3 BRAKE ASSY FAILED A WRNA O OTHER M J OVER TEMP WARNING INDICATION LD LANDING 1 SO 05 506TA 207 AFTER LANDING, NR 3 BRAKE TEMP, WENT TO 700C. INSPECTED IAW 05-51-16, FOUND HEAT DAMAGE REQUIRING BOGIE BEAM REPLACEMEN T. TEST OF NR 3 SERVO VALVE INDICATED SERVO VALVE TO BE FAULTY. REPLACED BOGIE BEAM IAW MM 32-11-14, PG 401-411. REPL ACED NR 3 BRAKE IAW 32-42-27 CONF NR 2 PG 401, NR 3 SERVO VALVE IAW 32-42-48 PG 401, 3 & 4 TIRES IAW 12-37-32 CONF NR 2 PG 401 AND 3 & 4 TACH GENERATORS IAW 32-42-57 PG 401. ALL SYSTEMS CHECKS NORMAL, ACCOMPLISHED GEAR RETRACTION AND TAXI TEST, ALL CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A35EU 2007032000161 20070320 00161 SO 2007 3 20 RAIA00703016 1 20070308 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN DISLODGED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 845HK 14500842 POST FLT NR 7953 - IAD - EMERGENCY FLOOR LIGHT BY GALLEY CAME OFF. MAINTENANCE SECURED LIGHT STRIP, CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT T00011AT 2007032000162 20070320 00162 SO 2007 3 20 RAIA00703019 1 20070309 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 818HK 145059 PRE FLT NR 5479 - STL - EMERGENCY LIGHT, FLOOR PROXIMITY LIGHTS AND COCKPIT FLOODLIGHT ARE OUT. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY, CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007032000163 20070320 00163 SO 2007 3 20 RAIA00703017 1 20070308 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 817HK 145058 PRE FLT NR 5555 - STL - OVERHEAD EMERGENCY LIGHT IN THE CABIN (AISLE FLOODLIGHT) INOP. MAINTENANCE REMOVED AND REPLACED BULB, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007032000164 20070320 00164 SO 2007 3 20 RAIA00703020 1 20070309 A 2720 FADEC EMB 145 EMB145EP 3260221 SO MALFUNCTIONED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 827HK 145021 FLT NR 5566 - RIC - RUDDER HARDOVER PROTECTION MESSAGE ON EICAS. MAINTENANCE RESET FADEC, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007032000165 20070320 00165 SO 2007 3 20 RAIA00703018 1 20070309 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 824HK 145498 PRE FLT NR 5467 - STL - EMERGENCY LIGHT (FWD SIDE AFT CEILING EXIT LOCATOR) IS OUT. MAINTENANCE REPLACED LIGHT, OPS CHE CK GOOD. 2 L 7 2 4T RT T00011AT 2007032000166 20070320 00166 NM 2007 3 20 SB07022 1 20070313 A 3350 20131ASMI BATTERY PACK BOEING 737 7373B7 1384580 NM AFT CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 23380 BOS - MAINTENANCE REPORTED THE AFT RIGHT GALLEY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT R IGHT BATTERY SUPPLY PACK IN ASSOCIATION WITH MAINTENANCE MANUAL. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007032000167 20070320 00167 NM 2007 3 20 2007UALA00739 1 20070312 A 3397 WIRE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 337UA 24241 EMERGENCY EXIT LIGHTS NEAR AFT GALLEY INOP AND A PLUG SEEMS DISCONNECTED. REPAIRED BROKEN WIRE AT AFT GALLEY LAST LIGHT STRIP FOR PERMANENT REPAIR. OPS GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032000168 20070320 00168 NM 2007 3 20 2007UALA00740 1 20070312 A 5230 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CARGO DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 DENT AFT PIT DOOR 16 INCHES AFT OF FWD EDGE 27 INCHES DOWN FROM TOP EDGE, 1.250 INCHES DIA .750 IN WIDTH AND .031 DEPTH. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGED AREA. FABRICATED & INSTALLED DOUBLER & FILLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032100001 20070321 00001 2007 3 21 2007UALA00741 4 20070311 A 2565 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 4R MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 UNABLE TO DISARM SLIDE PACK WITH SAFETY PIN DOOR 4R. [SUP 05-18-07] FOUND DOOR 4R GIRT BAR AFT FOOT MISSING AND SLIDE NOT SERVICEABLE WHILE WORKING INBOUND GRIPE. REPLACED SLIDE AND GIRT BAR FOOT. GIRT BAR IS MOVING WHEN TRYING TO ARM. U NABLE TO DISARM SLIDE PACK WITH SAFETY PIN DOOR 4R. REPLACED SLIDE AS PRECAUTION DUE TO GIRT BAR MALFUNCTION. ADJUSTED GIRT BAR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032100002 20070321 00002 2007 3 21 2007UALA00742 4 20070312 A 2565 TORQUE TUBE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 GIRT BAR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 508UA 24744 L-1 DOOR LOWER GIRT BAR LINKAGE TORQUE TUBE IS GOUGED AND CORRODED. [SUP 05-22-07] L-1 DOOR LOWER GIRT BAR LINKAGE T ORQUE TUBE IS GOUGED AND CORRODED. REPLACED TORQUE TUBE DURING DOOR OVERHAULS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032100003 20070321 00003 NM 2007 3 21 2007UALA00743 1 20070312 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 365 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 508UA 24744 RIGHT FWD MAIN CABIN FLOOR STRUCTURE, FLOORBEAM UPPER CHORD ON UPPER AND LOWER SURFACES CORRODED AROUND FASTENER HOLES I N MULTIPLE PLACES, BS 365.25, RBL 0 TO RBL 64. MAJOR REPAIR ACCOMPLISHED: RMV'D CORROSION. FABRICATED & INSTALLED REPA IR ANGLE & STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032100004 20070321 00004 NM 2007 3 21 2007UALA00744 1 20070312 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1562 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 AFT GALLEY AREA, MAIN FLOORBEAM STA 1562, RBL 48 AREA, TOP BEAM FLANGE CORRODED AND BLEND OUT EXCEEDS LIMITS. MAJOR REP AIR ACCOMPLISHED: CUT-OUT DAMAGED AREA. FABRICATED & INSTALLED UPPER CHORD ANGLE SPLICE SECTION. 2 L 7 2 4F 4 F RT A1NM E24NE 2007032100005 20070321 00005 NM 2007 3 21 2007UALA00745 1 20070312 A 2750 SENSOR BOEING 737 737522 138449F NM TE FLAPS FAULTED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 918UA 25385 RTFL AND LANDED UNDER AMBER ALERT DUE TO A LEADING EDGE SLAT INDICATION. [SUP 05-16-07] FOUND FAULTY NR 3 FLAP EXTEND S ENSOR. REPLACED FLAP EXTEND SENSOR. 2 L 7 2 4F RT A16WE 2007032100007 20070321 00007 2007 3 21 2007UALA00747 4 20070312 A 2565 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR SLIDE NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 526UA 24994 2R EMERGENCY ESCAPE SLIDE FAILS TEST. [SUP 05-22-07] REMOVED AND REPLACED BOTTLE ASSY. OPERATIONAL TEST OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032100008 20070321 00008 NM 2007 3 21 2007UALA00748 1 20070310 A 5300 STRUCTURE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE BS 1226 S42 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 837UA 1474 STA 12267, STR 42 RIVET HAS LIGHTNING DAMAGE. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA & INSTALLED DOUBLER REPAI R. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032100009 20070321 00009 NM 2007 3 21 2007UALA00749 1 20070313 A 5330 SKIN BOEING 737 737322 1384676 NM BS 861-867 GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 364UA 24533 UPPER FUSELAGE SKIN HAS 2 EA GOUGE-TOOLING MARKS APPROX BS 861-867 BL0. MAJOR REPAIR ACCOMPLISHED: INSTALLED EXTERNAL F USELAGE SKIN DOUBLER-TRIPLER, INTERNAL TEAR STRAP DOUBLERS & WEAR STRIPS UNDER THE DORSAL LANDING. 2 L 7 2 4F RT A16WE 2007032100010 20070321 00010 NM 2007 3 21 2007UALA00750 1 20070313 A 5300 UNKNOWN BOEING 737 737322 1384676 NM BS 875-887 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 364UA 24533 UPPER FUSELAGE FROM APPROX STA 875 TO STA 887 LBL 4 TO LBL 5 AND RBL 3 TO RBL 4 2EA LONG GOUGES-WEAR. MAJOR REPAIR ACCO MPLISHED: INCORPORATED INTO SAME REPAIR AS PTT 0922100 - (INSTALLED EXTERNAL FUSE SKIN DOUBLER-TRIPLER, INTERNAL TEAR ST RAP DOUBLERS & WEAR STRIPS UNDER DORSAL LANDING) 2 L 7 2 4F RT A16WE 2007032100011 20070321 00011 NM 2007 3 21 2007UALA00751 1 20070314 A 3397 7945243 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY EXIT LIGHT INOPERATIVE AT SEAT 2J & AT DOOR 5L GALLEY CROSS-AISLE. SUPPLEMENTAL DATA UPDATE FOUND LOOSE CONNE CTION, RESECURED. EEL CHECKS OK 2 L 7 4 4F 4 F RT A20WE E24NE 2007032100012 20070321 00012 NM 2007 3 21 2007UALA00752 1 20070314 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY EXIT CEILING LIGHT INOP JUST AFT OF FWD GALLEY RIGHT SIDE. RELAMPED. OP CHECKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032100013 20070321 00013 NM 2007 3 21 2007UALA00753 1 20070314 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY EXIT LIGHT INOPERATIVE AT SEAT 42L. REPLACED LAMP ASSY. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032100014 20070321 00014 NM 2007 3 21 2007UALA00754 1 20070314 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY EXIT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EXTERIOR EMERGENCY OVERWING EXIT LIGHTS INOPERATIVE ON LEFT SIDE TWO MOST AFT ASSEMBLIES. REPLACED FUSE IN EMERGENCY PO WER SUPPLY UNIT, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032100015 20070321 00015 NM 2007 3 21 2007UALA00755 1 20070314 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 SEAT EEL AT SEATS 2J, 4E (AFT) & 5E (AFT) ARE FAULTY. REPLACED EEL AT THREE POSITIONS WITH NEW EMERGENCY LIGHT. EEL SYS TEM OP CHECKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032100016 20070321 00016 NM 2007 3 21 2007UALA00756 1 20070314 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 20UAÊ 29166 FLIGHT DECK EMERGENCY LIGHT LAMP BURNED OUT. REPLACED WITH NEW FLIGHT DECK EMERG LIGHT LAMP. EMERG LIGHTS CHKED NORMAL LY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032100017 20070321 00017 NM 2007 3 21 2007UALA00757 1 20070313 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 549UA 25397 RIGHT OVERWING EXIT EMERGENCY LIGHT INOPERATIVE. [SUP 4-17-07] RELAMPED L563 SLIDE LIGHT AT RIGHT AFT OVERWING EXIT , BUT LIGHT STILL INOP. REPLACED RT WING BATTERY PACK AND OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2007032100018 20070321 00018 EU 2007 3 21 2007UALA00758 1 20070312 A 5270 UNKNOWN AIRBUS 320 A320232 3930326 EU DOOR WARNING UNKNOWN A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 426UA 510 FLIGHT DIVERTED DUE TO A FLIGHT DECK DOOR UNLOCK INDICATION. [SUP 06-01-07] FAULT TRACED TO A FAULTY COCKPIT SYSTEM CO NTROL UNIT. UNIT WAS REPLACED AND KEYPAD WAS REPROGRAMMED. 2 L 7 2 4F RT A28NM 2007032100036 20070321 00036 WP 2007 3 21 UPS07849517 1 20070221 A 5313 LONGERON SPLICE DOUG DC8 DC873F 302199F WP FS45-55 L24R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C1 HEAVY CORROSION UNDER SPLICE FITTING, L24R STA 45. REMOVED CORRODED LONGERON SPLICE FITTING AT STA 4 5-55 L24R IAW SRM 51-1-21. FABRICATED AND INSTALLED L24R SPLICE FITTING AND STIFFENER AT STA 45-55 IAW SRM 53-3-3 FIG 2 , 51-3-2, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007032100037 20070321 00037 WP 2007 3 21 UPS07849518 1 20070305 A 5710 SPLICE DOUG DC8 DC873F 302199F WP WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C1 CRACK AT NR 4 ALT LWR FRONT SPLICE PLATE BETWEEN XRS 428 AND XRS 463. REMOVED CRACKED SPLICE FITTING AT NR 4 ALT TANK LWR FRONT SPAR CAP BETWEEN XRS 428-XRS 463 IAW SRM 51-01-20D. FABRICATED AND INSTALLED REPAIR SPLICE FITTING IAW DWG 3644046, AND SRM 51-03-02, 51-01-20D. 2 L 7 4 4F RT 4A25 2007032100038 20070321 00038 WP 2007 3 21 UPS07849519 1 20070220 A 5311 FRAME DOUG DC8 DC873F 302199F WP FS 1707 L21R GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C1 CANTED FRAME CAP DENTED/GOUGED BEYOND LIMITS, MAIN CABIN STA 1707 L21R. REMOVED DAMAGED FRAME CAP AT STA 1707 L21R IAW SRM 51-1-21. FABRICATE AND INSTALLED FRAME CAP AT STA 1707 L21R IAW SRM 53-2-0, 51-1-20D AND DWG 561 2146. 2 L 7 4 4F RT 4A25 2007032100039 20070321 00039 WP 2007 3 21 UPS07849521 1 20070307 A 5330 SKIN DOUG DC8 DC873F 302199F WP FS 1710 L20L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C3 BULGING SKIN ON EXTERNAL FUSELAGE AT STA 1710 L20L. CUT OUT DAMAGED AREA ON SKIN AT STA 1710 L20L IA W SRM 53-02-01-0 FIG 7. FABRICATED & INSTALLED REPAIR DOUBLER, FILLER, AND FINGER DOUBLER AT STA 1710 L20L IAW SRM 53-0 2-01-0 FIG 7. 2 L 7 4 4F RT 4A25 2007031900034 20070319 00034 NM 2007 3 19 SWAA071368 1 20070313 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 400 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND STR CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007031900035 20070319 00035 NM 2007 3 19 SWAA071370 1 20070313 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 663 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED BRDG CHECK, FOUND STR CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007031900040 20070319 00040 EA 2007 3 19 TRAX200700327 1 20070306 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 718EV 10095 LEFT FUSELAGE 1 EXTERIOR EMERGENGY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007031900058 20070319 00058 NM 2007 3 19 ASAA0771515 1 20070312 A 5315 146A75039 FLOORBEAM BOEING 737 737790 13844CN NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 AFT CARGO CORROSION FOUND ON CARGO FLOORBEAM AT BS 767. REPAIRED IAW EA 5320 01793. 2 L 7 2 4F RT A16WE 2007031900088 20070319 00088 NM 2007 3 19 UPS07449402 1 20070214 A 5210 DOUBLER BOEING 747 747121 1384871 NM R1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D - R1 DOOR SKIN ATT DOUBLER FOUND CRACKED AT LOWER LINK AREA. M/D - R1 DOOR SKIN DOUBLER REPLACED AND INSTALLED AS PER SRM 52-10-02 FIG 11. 2 L 7 4 4F A20WE 2007031900089 20070319 00089 NM 2007 3 19 UPS07449403 1 20070215 A 5740 69B116408 ATTACH FITTING BOEING 747 747121 1384871 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT WING L/E RIB TO FRONT SPAR UPPER CHORD ATT FITTING AT ILES 340 FOUND CRACKED. CRACK LENGTH .375 INCH. RIGHT WING L/E RIB TO FRONT SPAR UPPER CHORD ATTACH AT ILES 340 REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 AN D 51-30-02. 2 L 7 4 4F A20WE 2007031900093 20070319 00093 WP 2007 3 19 UPS07849366 1 20070213 A 5730 5611360167 SKIN DOUG DC8 DC871F 302199D WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 LEFT WING UPPER SKIN AT XRS650 TO XRS659 OVER STR 7 REQUIRES REPAIR. REPAIR WING UPPER SKIN IAW SAA EA3 008-5730-01-A0655 AND UPS EO DC8-57 30-26300-A. 2 L 7 4 4F RT 4A25 2007031900094 20070319 00094 CE 2007 3 19 DXTA200702022 1 20070314 A 3230 UNKNOWN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE WARNING LIGHT UNKNOWN E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 311QS 5600311 AFTER TAKEOFF THE GEAR UNLOCKED LIGHT AND THE HYDRAULIC PRESS ON LIGHT REMAINED ILLUMINATED AFTER RETRACTING THE LANDING GEAR. REMOVED & REPLACED LT UPLOCK ACTUATOR ASSY SPRING AND LT UPLOCK SWITCH. CYCLED GEAR MULTIPLE TIMES. OPS CHECKS G OOD IAW CE560 MM 32-31-05. 2 L 7 2 4F 4 F RT A22CE E25EA 2007031900101 20070319 00101 NM 2007 3 19 USAA070191 1 20070313 A 5311 FRAME BOEING 737 737401 1384701 NM BS 500A S9L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 STA 500A, S9L CRACKED. FAB'D & INSTALLED DOUBLER REPAIR PARTS PER TR 53-10-20D, DEFECT SIZE: .50 INCH. 2 L 7 2 4F RT A16WE 2007031900109 20070319 00109 EA 2007 3 19 TRAX200700337 1 20070309 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 PAX DOOR OUTER HANDLE CRACKED. REMOVED PAX DOOR LATCH MECHANISM TO FOM. REMOVED PAX DOOR OUTER HANDLE JB422. INSTALLED SERVICEABLE FLAP HANDLE ONTO SERVICEABLE HANDLE MECHANISM PN 601R31763-1 IAW CRJ SRM 51-42-04. OK TO PRIME & PAINT PAX D OOR OUTER HANDLE. PAINTED AND PRIMED PAX DOOR OUTER HANDLE IAW CRJ 700 SRM 51-25-01 INSTALLED OUTER HANDLE IAW CRJ 700 A MM 52-11-02. REQUIRES OPS CK. PERFORMED OPS & LEAK CHECK OF PAX DOOR IAW CRJ MM 52-11-02. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007031900110 20070319 00110 EA 2007 3 19 TRAX200700338 1 20070309 A 5347 CARGO TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 AFT CARGO BAY FWD TRACK SUPPORT ANGLE MIDDLE CHANNEL CRACKED (MARKED). [SUP 05-02-07] REPAIRED IAW ALL SRM`S. 2 L 7 2 4F RT A21EA 2007031900115 20070319 00115 WP 2007 3 19 I5HA0758005 1 20070309 A 6120 REGULATOR CVAC 580 580 2422806 WP ALLSN 501D 501D13 03004 GL ALLSN A6441 A6441FN606 GL PROPELLER FAILED A I5HA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 23 582 475 HC2769 WHILE ENROUTE, MAINTENANCE BASE (LCK)TO THE OUT STATION, THE CREW OBSERVED THE LT PROPELLER RPM OVERSPEED. THE CREW WAS UNABLE TO REGAIN NORMAL RPM AND ELECTED TO SHUTDOWN THE ENGINE. THE AIRCRAFT LANDING UNEVENTFULLY. AT THIS TIME THE CAUSE OF THE OVERSPEED IS STILL TO BE DETERMINED. THE PROPELLER GOVERNOR AND NTS VALVE WERE REMOVED AND REPLACED BUT DI D NOT FIX THE PROBLEM. THE PROPELLER REGULATOR ASSEMBLY IS BEING CHANGED. THE PROPELLER REGULATOR WAS REMOVED AND REPL ACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT E282 6 C P898 2007031900125 20070319 00125 NM 2007 3 19 USAA070180 1 20070313 A 5340 STRINGER CLIP BOEING 737 737401 1384701 NM BS 727C S9R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 TIE CLIP AT STA 727C S-9R CRACKED. REPLACED TIE CLIP WITH NEW PER SRM 51-10-02, DEFECT SIZE: .025 INCH. 2 L 7 2 4F RT A16WE 2007031900129 20070319 00129 CE 2007 3 19 4514702062007 1 20070206 A 3260 66323003001001 LIMIT SWITCH LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE7312 01518 WP MLG DOOR MALFUNCTIONED E J7SA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 05 425FX 147 MAIN GEAR DOORS INDICATED (OPEN) OR (IN-TRANSIT) IN FLIGHT. AIR RETURN WITH UNEVENTFUL LANDING AND TAXI. 02/07/07 REM OVED AND REPLACED LT AND RT LANDING GEAR UP LIMIT SWITCHES. OPS CHECK GOOD. 02/08/07 MAINTENANCE CHECK FLIGHT SATISFA CTORY. 02/14/07 AIRCRAFT HAS FLOWN SEVEN ADDITIONAL LEGS SINCE REPAIR WITH NO REPEAT EVENT. 2 L 7 2 4F 4 F RT T00008WI E6WE 2007031900136 20070319 00136 NM 2007 3 19 SWAA071348 1 20070313 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031900137 20070319 00137 NM 2007 3 19 SWAA071349 1 20070313 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440 STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031900153 20070319 00153 EU 2007 3 19 07FDEA00810 1 20070314 A 5714 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 INOPERATIVE A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 ELONGATED HOLES IN PYLON SUPPORT BRACKET AND BOTTOM SKIN, RT WING. REPAIR PERFORMED IAW AI-INSTRUCTION: R571-50532 ISSU E "A" AND EA 6-5720-106407. 2 L 7 2 4F RT A35EU 2007032000003 20070320 00003 NM 2007 3 20 USAA070194 1 20070315 A 5320 69735271 ANGLE BOEING 737 737401 1384701 NM BS 500G S28L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 BS 500G, S-28L CRACKED. FABRICATED & INSTALLED NEW ANGLE PER SRM 51-10-02, BOEING DWG 69-73527, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007032000008 20070320 00008 NM 2007 3 20 USAA070199 1 20070315 A 5310 9078224 STRAP BOEING 737 737401 1384701 NM BS 294-305 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 STRAP BETWEEN BS 294.5 & 305, BETWEEN S-9L & S-10L CRACKED. REMOVED DAMAGE & INSTALLED NEW & FABRICATED REPAIR PARTS PE R 51-10-02; BOEING DWG 65-17684, DEFECT SIZE: .750 INCH. 2 L 7 2 4F RT A16WE 2007032000034 20070320 00034 NM 2007 3 20 UPS07M49394 1 20070104 A 5311 FRAME DOUG MD11 MD11F 3023600 NM BS 1256 L1L/R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE:C CABIN - CRACK ALONG THE GRAINS OF FRAME FLANGE AT STA 1256 L1 LEFT TO L1 RIGHT. GRAINS OF FRAME FLANG E CRACK AREA TRIMMED OUT AT STA 1256 L1 LEFT TO L1 RIGHT PER SRM 53-30-00 VI R38. HFEC INSP CUTOUT PER DAC NDTSPM R12 0 6-10.0 1.001 ON TRIMMED AREA AND FOUND NO CRACK EVIDENT. NEW DOUBLER & FILLER, STRAP & SHIM FAB PER EN EN1042-07. NEW DOUBLER FILLER STRAP & SHIM INSTALLED PER SRM 51-35-01 & 51-33-01 V-II R38 & EN 1042-07. 2 L 7 3 4F RT A22WE 2007032000047 20070320 00047 NM 2007 3 20 SWAA071394 1 20070314 A 3350 079123 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 221WN 34259 DURING SCHEDULED C2 CHECK, FOUND EEPLS LENS MISSING. INSTALLED EEPLS LENS PER MM 2 L 7 2 4F RT A16WE 2007032000059 20070320 00059 NM 2007 3 20 SWAA071380 1 20070314 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 616 S2R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007032000061 20070320 00061 NM 2007 3 20 BB07021 1 20070310 A 4910 BACR13CF2AB RELAY BOEING 757 7572B7 1384964 NM APU DOOR FAULTY A USAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 934UW 27200 DEN - FLT773 EN ROUTE FROM PHL TO LAS, CREW REPORTED, LOST THE NR 2 ENGINE IDG AND WERE UNABLE TO START THE APU. CREW D ECLARED AN EMERGENCY AND DIVERTED TO DEN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE K176 APU DOOR INLET RELAY PER WDM CHAPTER 20. PERFORMED FOUR SUCCESSFUL APU STARTS. OPERATIONALLY CHECKED APU DOOR IN LET PER MM 49-15-06 AND PERFORMED ECU BITE CHECK. NO FAULTS NOTED. ALSO, REMOVED AND REPLACED NR 2 ENGINE IDG AND OIL COOLER PER MM 24-11-01 AND MM 24-11-04. OPERATIONAL CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT A2NM 2007032000070 20070320 00070 NM 2007 3 20 SWAA071384 1 20070314 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727B S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007032000097 20070320 00097 CE 2007 3 20 DXTA200702028 1 20070316 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 395QS 5600496 BRAKES ARE MUSHY THROUGH THE FIRST 75 PERCENT OF PRESSURE APPLICATION. DON'T START TO FEEL BRAKING UNTIL PAST THE 75 PE RCENT MARK. IMPROVES SLIGHTLY IF YOU PUMP THE BRAKES. BLED LT & RT BRAKES, INSPECTED BRAKES FOR DEFECTS, BRAKE WEAR F OUND WITHIN LIMITS, NO OTHER DEFECTS NOTED. SERVICED BRAKE RESERVOIR TO FULL LEVEL. PERFORMED GROUND RUN & TAXI CHECK OF BRAKES, BRAKES FOUND TO FUNCTION PROPERLY FROM PILOT & CO-PILOT POSITIONS WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GO OD. MAINT PERFORMED IAW CE-560 MM CH 32-42-00 2 L 7 2 4F 4 F RT A22CE E00053EN 2007032100040 20070321 00040 NM 2007 3 21 UPS07M49511 1 20070131 A 5315 ADA797123 FLOORBEAM DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C FWD CARGO COMPT ALONG STA 6-0, FROM LBL 0 TO LBL 27, FLOORBEAM SUPPORT CORRODED. CORROSION FLOORBEAM SUPPORT REMOVED PER SRM 51-3501 V2 R38. NEW FLOORBEAM SUPPORT & FASTENERS HOLE PICKED UP PER SRM 51-31-01 V2 R38. NEW SUPPORT REPROTECTED PER SRM 51-21-01 V2 R38. NEW SUPPORT PAINTED PER SRM 51-21-01 V2 R38 AND OK TO INSTALLED. NEW BEAM SUPPORT INSTALLED PER SRM 51-35-01 V2 R38, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007032100041 20070321 00041 NM 2007 3 21 UPS07M49512 1 20070207 A 5320 71703 WEB DOUG MD11 MD11F 3023600 NM BS 1841 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C CENTER CARGO COMPT CENTER CARGO DOOR ENTRYWAY BILGE AREA AT STA 1841 RT PARTITION PLATE BETWEEN CENTER & AFT CARGO ADJACENT TO LONGERON 46L CRACKED. ATTACH CRACK WEB REMOVED FOR ACCESS PER SRM 51-31-01 V2 R38. FAB NEW WE B P/N AGA7170-3, PER DWG P/N AGA7170, & FRAME HOLES PICKED UP PER SRM 51-31-01 V2 R38. NEW WEB INSTALLED & ATTACHED WE B PARTS REINSTALLED PER DWG AGA 7170 & SRM 51-31-01 V2 R38. OK TO TOUCH TOPCOAT. ON REPLACED AREA PAINT TOUCHED UP PER SRM 51-21-01 V2 R38. 2 L 7 3 4F RT A22WE 2007032100042 20070321 00042 NM 2007 3 21 KCSA071066 1 20070316 A 5315 VERTICAL SUPPORT BOEING 747 747236B 1384804 NM BS 2000 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 AFT BILGE FLOORBEAM VERTICAL SUPPORT IS CRACKED AT STA 2000, RBL 49, AFT SIDE. 2 L 7 4 4F A20WE 2007032100043 20070321 00043 WP 2007 3 21 MWEA070044 1 20070316 A 5710 5930494501 VANE DOUG DC9 DC981 3022081 WP LT WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 805ME 48031 LEFT WING MOST INBOARD FIXED VANE HAS A SMALL HOLE IN LOWER SURFACE SKIN, CENTER OF VANE. FABRICATED AND INSTALLED DOUB LER. 2 L 7 2 4F A6WE 2007032100044 20070321 00044 WP 2007 3 21 UPS07849430 1 20070220 A 5311 DC853A01117 FRAME DOUG DC8 DC873F 302199F WP FS 1600 L9R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C1 HOLE DRILLED THRU EDGE OF FRAME, INTO RADIUS, MAIN CABIN STA 1600 L9R. REMOVED SPLICE ANGLE AND CUT OUT DAMAGE, FABRICATED AND INSTALLED -J- DOUBLER AND FILLER IAW EO DC8-5310-11728B AND DWG DC-853A-011A. 2 L 7 4 4F RT 4A25 2007032100045 20070321 00045 WP 2007 3 21 UPS07849431 1 20070309 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C3 LEFT WING OUTBOARD LWR RIB CRACKED AT XFS 790. CRACK TERMINATES AT FASTENER HOLE PER HFEC INSP NDTSP M 06-10-01-001 FABRICATED AND INSTALLED REPAIR DOUBLERS AND ANGLES AT LEFT WING OUTBOARD LEADING EDGE STA XFS 790 IAW SR M 57-03-03 FIG 7, AND SRM 57-2-0. 2 L 7 4 4F RT 4A25 2007032100046 20070321 00046 2007 3 21 UPS07849499 4 20070314 A 2565 INDICATOR DOUG DC8 DC871F 302199D WP DOOR SLIDE DISLODGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 DOOR SLIDE PRESS INDICATOR SLIDE OUT OF SIGHT. CANNOT READ. REPACKED/REPOSITIONED SLIDE INDICATOR, NOW IN VIEW. 2 L 7 4 4F RT 4A25 2007032100047 20070321 00047 WP 2007 3 21 UPS07849501 1 20070315 A 3350 BULB DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS BURNED OUT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 PILOTS OVERHEAD PANEL EMERGENCY LIGHTS DISARMED LIGHT INOP. FOUND BULB BURNED OUT. REPLACED BULB, CHECKS OK. 2 L 7 4 4F RT 4A25 2007032100048 20070321 00048 EA 2007 3 21 TRAX200700350 1 20070314 A 5313 STRINGER CNDAIR CL600 CL6002C10 1390015 EA BS 333-349 S26L CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 CORROSION ON STR 26L BETWEEN FS 333.00 AND FS 349 (MARKED). 2 L 7 2 4F RT A21EA 2007032100049 20070321 00049 EA 2007 3 21 TRAX200700351 1 20070314 A 5313 STRINGER CNDAIR CL600 CL6002C10 1390015 EA BS 333-349 S26R CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 CORROSION ON STR 26R BETWEEN FS 333.00 AND FS 349 (MARKED). (SUPPLEMENTAL 28 MARCH 07) C/W EC/TC REO 670-52-21-262 NO FUTHER ACTION REQUIRED AT THIS TIME 2 L 7 2 4F RT A21EA 2007032100050 20070321 00050 EA 2007 3 21 TRAX200700352 1 20070314 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 295 S26L/R CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 CORROSION ON ANTENNA MOUNT PLATE/DOUBLER BETWEEN STG 26L AND 26R BETWEEN FS 295.00 AND FS 310.00 (MARKED). REMOVED AND REPLACED ANTENNA MOUNT PLATE DOUBLER ASSEMBLY IAW CRJ 700 SRM 51-42-06. INSTALLED LOWER TCAS ANTENNA IAW CRJ 700 MM 34 -43-07 SYS OPS CK GOOD. 2 L 7 2 4F RT A21EA 2007032100051 20070321 00051 EA 2007 3 21 TRAX200700353 1 20070314 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 CORROSION ON FLOORBOARD SUPPORT ANGLE AT FS 280.00 IN AVIONICS CRAWLWAY. 2 L 7 2 4F RT A21EA 2007032100052 20070321 00052 EA 2007 3 21 TRAX200700354 1 20070314 A 5321 FLOORBOARD CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 CORROSION AT COCKPIT FLOORBOARD AFT LAND AT FS 280.00. (SUPPLEMENTAL 28 MARCH 07) REPAIR ON FLOOR BOARD AFT LAND AT F S 280.00 IAW REO 670-53-11-046. 2 L 7 2 4F RT A21EA 2007032100053 20070321 00053 EA 2007 3 21 TRAX200700355 1 20070314 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 928EV 8006 RIGHT EMERGENCY EXIT PLACARD WORN. 2 L 7 2 4F RT A21EA 2007032100054 20070321 00054 EA 2007 3 21 TRAX200700356 1 20070314 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA OVERWING EXIT DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 928EV 8006 RIGHT SIDE OVERWING EXIT NIGHT GLOW PLACARD UNREADABLE. 2 L 7 2 4F RT A21EA 2007032100055 20070321 00055 EA 2007 3 21 TRAX200700357 1 20070315 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 CORROSION ON FLOOR SUPPORT ANGLE ON ASD SILL. REMOVED FWD, MID, AFT ANGLE, LOWER ASD ANGLE AND FWD AND AFT STAIR RAIL F ITTINGS. DRILLED, COUNTERSANK, DEBURRED AND ALODINED NEW MID CAP ANGLE PER CRJ 700 SRM 51-42-06. DRILLED, DEBURRED AND COUNTERSANK NEW KICKPLATE PER CRJ 700 SRM 51-40-00. FINISHED INSTALLING NEW KICKPLATE, INSTALLED NEW MID CAP ANGLE AND FWD AND AFT STAIR RAIL FITTINGS AND SEALED AND RESTORED FINISH TO REPAIR AREA PER CRJ 700 SRM 51-42-03, 51-23-00 AND 5 1-25-16. 2 L 7 2 4F RT A21EA 2007032100056 20070321 00056 NM 2007 3 21 PIDA07016 1 20070206 A 5753 SKIN BOEING 757 757236 1384971 NM LT WING TE FLAP DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 757BJ 22176 DURING INSPECTION, DAMAGE FOUND ON UPPER SURFACE OF THE LEADING EDGE OF THE LEFT WING O/B FLAP. REPAIRED DAMAGE PER SRM 57-53-01 FIGURE 201 REPAIR 2. 2 L 7 2 4F RT A2NM 2007032100057 20070321 00057 EA 2007 3 21 TRAX200700364 1 20070315 A 5313 STRINGER CNDAIR CL600 CL6002C10 1390015 EA BS 364 S26L/R CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 CORROSION ON STR 26L AND 26R AT FS 364.00. (SUPPLEMENTAL 28 MARCH 07) REMOVED FASTNERS AND BLENDED CORRISION IAW CRJ 700 SRM 51-42-06. DAMAGE IS OUT OF LIMITS, REMOVED .025 FROM S26R BETWEEN FS 349 AND FS 364. DAMAGE ON S26L IS WITH IN LIMIT, REMOVED .006 IAW CRJ 700 SRM 53-21-03-101-006-A01. S26R HAS BEEN REMOVED AND REPLACED ATFS 364 FOR ALL WORK ACCOMPLISHED REFER TO W/O 53023 N/R-00161. INSTALLED RIVETS ON S26L AT FS 364 TREATED, PRIMED AND PAINTED REWOKED AREA IAW CRJ 700 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007032100058 20070321 00058 EA 2007 3 21 TRAX200700365 1 20070315 A 5313 STRINGER CNDAIR CL600 CL6002C10 1390015 EA BS 294-333 S26R CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 CORROSION ON STR 26R BETWEEN FS 294.00 AND FS 333.00. DAMAGE IS OUT OF LIMITS, REMOVED .018 FROM STRG 26R BETWEEN FS 2 95 AND FS 319.70 IAW CRJ 700 SRM 53-21-03-101-002-A01. CUT STRINGER 26R AT FS 300 THRU FS 312 AND REMOVED DAMAGED SECTIO N OF STR. 26 R FROM FS 295 TO FS 364 IAW CRJ 700 SRM 53-00-03. FABRICATED NEW SECTION OF STRINGER AND SHIM AND DOUBLER OUT OF EXTRUSION FOR FS 295 THRU 312, IAW CRJ SRM 53-00-03. PERFORMED EDDY CURRENT INSPECTION OF CUT LINES PER MTC REQ UEST, IAW CRJ 700 NDTM PART 1. 51-20-006. NO DEFECTS NOTED. FABRICATED BACKSIDE Z ANGLE DOUBLER FOR BOTH CUTLINES OUT O F EXTRUSION, ALL PARTS DEBURED AND PRIMED IAW CRJ 700 SRM 53-00-03. OK TO INSTALL. 2 L 7 2 4F RT A21EA 2007032100059 20070321 00059 EA 2007 3 21 TRAX200700366 1 20070315 A 3350 COVER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 EMERGENCY EXIT LIGHT COVER ABOVE SERVICE DOOR CRACKED (MARKED). 2 L 7 2 4F RT A21EA 2007032100060 20070321 00060 NM 2007 3 21 USAA070222 1 20070319 A 5311 FRAME BOEING 737 7374B7 1384702 NM BS 440 S24R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 445US 24863 STA 440 STR 24R O/B RADIUS OF FRAME CRACKED. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER EA 98545, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007032100061 20070321 00061 NM 2007 3 21 USAA070221 1 20070319 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 986 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 589US 23934 STA 986 HAS CORROSION. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER EA 98538; CORR TASK C53-107-02; LEVEL 2, DEFECT SIZE : .5 INCH DIA. 2 L 7 2 4F RT A16WE 2007032100062 20070321 00062 EA 2007 3 21 TRAX200700367 1 20070315 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR EXIT WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 PAX DOOR -EXIT- PLACARD WORN. REPAIRED IAW ALL REFERENCE MATERIAL. 2 L 7 2 4F RT A21EA 2007032100063 20070321 00063 EA 2007 3 21 TRAX200700368 1 20070315 A 3250 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING UNKNOWN A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 883AS 7504 STEERING INOP MESSAGE FOLLOWED BY GEAR DISAGREE MESSAGE, NOSE GEAR WOULD NOT RETRACT, RETURNED TO ATL. EMERGENCY DECLAR ED BY TOWER. FLTS 4603, 4639 CX. 2 L 7 2 4F RT A21EA 2007032100064 20070321 00064 SO 2007 3 21 C2XA07CL031 1 20070315 A 3231 M835362024M RELAY EMB 145 EMB145LR 3260212 SO MLG FAULTY A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 15555 145594 CLE FLIGHT 2736 THE CREW REPORTED THE NOSE GEAR DOORS WOULD NOT RETRACT AFTER TAKEOFFF. MAINTENANCE INSPECTED AND REPLA CED THE NOSE GEAR SEQUENCE DOOR RELAY KO642. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007032100065 20070321 00065 EA 2007 3 21 TRAX200700358 1 20070315 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA BS 295 S27 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 FRAME CORRODED AT FS 295 STRINGER 27. 2 L 7 2 4F RT A21EA 2007032100066 20070321 00066 NM 2007 3 21 ASAA0741530 1 20070312 A 2150 22051702 ACM BOEING 737 7374Q8 138447Q NM RIGHT LEAKING A ASAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 02 772AS 25105 RIGHT PACK TRIP AND CABIN FILLED WITH SMOKE. SMOKE REMOVED FROM CABIN PER AMM 21 00 01. FOUND RT ACM LEAKING BETWEEN T URBINE AND COMPRESSOR SECTIONS. REMOVED AND REPLACED ACM HEPA FILTERS AND COMPLETED CONDITIONAL INSPECTION. 2 L 7 2 4F RT A16WE 2007032100114 20070321 00114 NM 2007 3 21 USAA200703003 1 20070319 A 5330 SKIN BOEING 737 737301 1384611 NM BS 500D-520 S12L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 503UW 23237 A 4.75 INCH CRACK FOUND LONGERON 12L BETWEEN STA 500D AND 520. CRACK REMOVED & REPAIRED PER EA 84260 & SRM 53-00-01 2 L 7 2 4F RT A16WE 2007032100115 20070321 00115 NM 2007 3 21 USAA070210 1 20070315 A 5740 ATTACH ANGLE BOEING 737 737401 1384701 NM RT WING DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 RIGHT WING UNDER SIDE INBOARD ATTACH Z-ANGLE AT FWD SPAR. REAMED HOLES TO .263 & INSTALLED FASTENERS PER SRM 51-40-09, DEFECT SIZE: .213 DIA. 2 L 7 2 4F RT A16WE 2007032100116 20070321 00116 NM 2007 3 21 USAA070211 1 20070315 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 500F-500G CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 RIGHT TRANSITION ANGLE STA 500F - 500G IN AFT CARGO AREA. INSTALLED FABRICATED ANGLE PER TR 53-20-04; CORR TASK C53-208 -01, LEVEL 2, DEFECT SIZE: 10 INCHES. 2 L 7 2 4F RT A16WE 2007032100117 20070321 00117 NM 2007 3 21 USAA070212 1 20070315 A 5320 WEB BOEING 737 737401 1384701 NM BS 794-847 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 STA 794.3 TO 847 AT S21R HAS CORROSION. REMOVED & REPLACED WEB, TREATED, PRIMED PER SRM 53-60-15, 53-10-02, 53-20-01; C ORR TASK C53-202-01. 2 L 7 2 4F RT A16WE 2007032100118 20070321 00118 NM 2007 3 21 USAA070213 1 20070315 A 5320 STRAP BOEING 737 737401 1384701 NM BS 767-847 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 SURFACE CORROSION ON STRAP THAT RUNS FROM STA 767-847 HAS CORROSION. REMOVED & REPLACED STRAP, TREATED, PRIMED PER BOEI NG DWG 65-47957, SRM 53-60-15, CORR TASK C53-202-01, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007032100119 20070321 00119 NM 2007 3 21 USAA070214 1 20070315 A 5310 CREASE BEAM BOEING 737 737401 1384701 NM BS 270-360 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 RIGHT CREASE BEAM INNER CHORD ANGLE, STA 270-360 RIGHT SIDE HAS CORROSION. REPLACED NEW ZEE ANGLE PER SRM 51-10-02; DWG 65-45875; CORR TASK C53-107-01; LEVEL 2, DEFECT SIZE: 38 X 2 INCHES. 2 L 7 2 4F RT A16WE 2007032100120 20070321 00120 NM 2007 3 21 USAA070215 1 20070315 A 5310 STRUCTURE BOEING 737 737401 1384701 NM NLG VIEW PORT CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 NOSE GEAR VIEW PORT WINDOW HAS CORROSION. REMOVED DAMAGE & INSTALLED FAB'D REPAIR PARTS PER SRM 51-70-12, DEFECT SIZE: 8 INCHES. 2 L 7 2 4F RT A16WE 2007032100121 20070321 00121 NM 2007 3 21 USAA070216 1 20070315 A 5320 FLOOR SUPPORT BOEING 737 737401 1384701 NM BS 870-947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 BS 870-947.5, RBL 12 HAS CORROSION. REMOVED DAMAGED AREA & INSTALLED NEW STRINGER PER SRM 53-0-53; CORR TASK C53-202-01 ; LEVEL 2, DEFECT SIZE: 78 INCHES. 2 L 7 2 4F RT A16WE 2007032100128 20070321 00128 WP 2007 3 21 ABXA070070 1 20070315 A 3260 BULB DOUG DC9 DC941 302207N WP MLG INDICATOR INOPERATIVE A ABXA O OTHER P NO WARNING INDICATION LD LANDING 1 GL 23 979AX 47492 LEFT MAIN GEAR GREEN DOWNLOCK LIGHT FAILED TO COME ON FOR LANDING. ALT GEAR LIGHT INDICATED GEAR DOWN. RECYCLED LANDIN G GEAR AND LIGHT CAME ON AFTER A TIME. FOUND BOTH LEFT GEAR INDICATION LIGHT BULBS MUSHROOMED AT CONTACTS. RELAMPED BU LB AS REQUIRED. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2007032100129 20070321 00129 NM 2007 3 21 ABXA070071 1 20070315 A 3350 20131A BATTERY BOEING 767 767231 1385131 NM EMERGENCY LIGHTS DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 708AX 22571 ON PRE-DEPARTURE CHECK, FOUND WHEN EMERGENCY LIGHT SWITCH SELECTED TO ON, LIGHTS ILLUMINATED MOMENTARILY, THEN EXTINGUIS HED. SWAPPED SPARE AND ACTIVE EMERGENCY POWER SUPPLIES. OPS CHECKED GOOD IAW B767 MM 33-51-07-2. 2 L 7 2 4F RT A1NM 2007032100130 20070321 00130 NM 2007 3 21 BB07025 1 20070315 A 3350 LIGHT BOEING 767 7672B7 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 256AY 26847 FLOOR LEVEL EMERGENCY LIGHTS FOUND INOPERATIVE ON A/C LEFT SIDE, MID SECTION. MAINTENANCE REPLACED A LIGHT ASSEMBLY. N O FURTHER FAULTS. 2 L 7 2 4F RT A1NM 2007032100131 20070321 00131 NM 2007 3 21 PIDA07014 1 20070309 A 5330 SKIN BOEING 757 757236 1384971 NM BS 1620 S17L DENTED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 757BJ 22176 DURING INSPECTION, A DENT WAS FOUND IN THE FUSELAGE SKIN AT BS 1620 JUST ABOVE STR 17LT. DENT REPAIRED IN ACCORDANCE WI TH BOEING MESSAGE 1-295219323-1, -4, -5, -7, -8, AND -9 WITH FAA DOA APPROVED 8100-9 DATED 13 MARCH 2007. 2 L 7 2 4F RT A2NM 2007032100132 20070321 00132 NM 2007 3 21 PIDA07015 1 20070314 A 5314 KEELBEAM BOEING 757 757236 1384971 NM BS 1146-1154 CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 757BJ 22176 DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT KEEL BEAM HORIZONTAL LEG UPPER SURFACE BETWEEN BS 1146 AND BS 1154 I N THE RIGHT MLG WHEEL WELL. REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH EA 53-069 DATED 03/11/07 WITH FAA DER APPROVED 8 110-3 DATED MARCH 11, 2007. 2 L 7 2 4F RT A2NM 2007032100133 20070321 00133 NM 2007 3 21 UPS07449442 1 20070210 A 5340 65B38600113 STRINGER CLIP BOEING 747 747121 1384871 NM BS 880 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT BS 880 TENSION TIE ATT NR 10 FASTENER HOLE CRACK AT TIE CLIP, CRACKS RUNNING UP .25 INCH AND RUN NING DOWN .1875 INCH APPROX. RIGHT SIDE BS 880 TENSION TIE ATT TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007032100134 20070321 00134 NM 2007 3 21 ZZDA070313143 1 20070313 A 3350 8039251 BATTERY PACK BOEING 717 717200 1383700 NM EMERGENCY LIGHT INOPERATIVE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 946AT 55009 EMERGENCY EXIT LIGHT OVER THE TAIL CONE EXIT IS INTERMITTENTLY ON WHEN IT SHOULD BE OFF. REPLACED EMERGENCY LIGHT PACK ASSY OVER AFT FLIGHT ATTENDANT`S SEAT PER M/M 33-51, OPS CHECKS NORMAL. P/N OFF/ON 803925-1, S/N OFF 21144, S/N ON 2031 6. 2 L 7 2 4F TR A6WE 2007032100135 20070321 00135 NM 2007 3 21 UPS07449443 1 20070216 A 5210 SKIN BOEING 747 747121 1384871 NM R3 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D R3 DOOR SKIN FOUND CRACKED APPROX AT CTR LOWER PORTION. CRACK LENGTH .375 INCH. M/D R3 DOOR SKIN AT CTR LOWER PORTION AREA REPAIRED AS PER SRM 52-10-02 FIG 9. 2 L 7 4 4F A20WE 2007032100136 20070321 00136 NM 2007 3 21 UPS07449444 1 20070210 A 5311 FRAME BOEING 747 747121 1384871 NM BS 840 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT SIDE BS 840 TENSION TIE ATTACHMENT AREA NR 13 AND NR 14 FASTENER HOLE CRACK AT FRAME DOUBLER. CR ACK LENGTH .25 INCH. M/D BS 840 LT FRAME ATTACH DOUBLER REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-3 0-02. 2 L 7 4 4F A20WE 2007032100137 20070321 00137 NM 2007 3 21 UPS07449447 1 20070210 A 5320 CHANNEL BOEING 747 747121 1384871 NM BS 800 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT BS 800 TENSION TIE ATTACHMENT AREA NR 7 FASTENER HOLE CRACK FOUND AT AFT CHANNEL RUNNING UP APPR OX .0625 INCH IN LENGTH. RIGHT BS 800 TENSION TIE ATT AFT CHANNEL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PE R SRM 51-30-02. 2 L 7 4 4F A20WE 2007032100138 20070321 00138 NM 2007 3 21 UPS07449448 1 20070210 A 5320 CHANNEL BOEING 747 747121 1384871 NM BS 800 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT BS 800 FRAME TENSION TIE ATTACHMENT AREA AT HOLE NR 5 CRACK FOUND AT FWD CHANNEL RUNNING UPPER AN D LOWER BOTH CRACK APPROX .125 INCH IN LENGTH. LEFT BS 800 FRAME TENSION TIE ATT FWD CHANNEL REPLACED AS PER SRM 51-10- 01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007032100139 20070321 00139 NM 2007 3 21 UPS07449449 1 20070210 A 5320 CHANNEL BOEING 747 747121 1384871 NM BS 800 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT BS 800 FRAME TENSION TIE ATTACHMENT AREA AT FASTENER HOLE NR 7 CRACK FOUND AT AFT CHANNEL RUNNING UPPER APPROX .0625 INCH IN LENGTH. LEFT BS 800 FRAME TENSION TIE ATT AFT CHANNEL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007032100140 20070321 00140 NM 2007 3 21 UPS07449450 1 20070210 A 5310 CHANNEL BOEING 747 747121 1384871 NM BS 800 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT BS 800 TENSION TIE ATTACHMENT AREA NR 5 AND NR 12 FASTENER HOLE CRACK AT FWD CHANNEL. CRACK LEN GTH .125 INCH. RIGHT BS 800 TENSION TIE FWD CHANNEL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02 . 2 L 7 4 4F A20WE 2007032100141 20070321 00141 NM 2007 3 21 UPS07449451 1 20070211 A 5320 CHANNEL BOEING 747 747121 1384871 NM BS 780 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT BS 780 FRAME TENSION TIE ATTACHMENT AREA AT FASTENER HOLE NR 5 FOUND CRACK AT FWD CHANNEL AT 12: 00 O/C POSITION APPROX .125 INCH LONG. M/D BS 780 LT TO RT FRAME ATTACH TENSION TIE FWD CHANNEL REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007032100142 20070321 00142 NM 2007 3 21 UPS07449452 1 20070211 A 5320 CHANNEL BOEING 747 747121 1384871 NM BS 780 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT BS 780 FRAME TENSION TIE ATTACHMENT AT FASTENER HOLE NR 7 CRACK AT AFT CHANNEL RUNNING UPPER APPR OX .0625 INCH IN LENGTH. M/D BS 780 LT FRAME ATTACH TENSION TIE AFT CHANNEL REPAIRED AS PER RS R53-25-35745. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35745 AND UPS EO B747-5310-26128. 2 L 7 4 4F A20WE 2007032100143 20070321 00143 SO 2007 3 21 C2XA07IA059 1 20070308 A 3350 2013BR BATTERY PACK EMB 135 EMB135LR 3260305 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 29515 7341 4482 145309 IAH - DURING MAINTENANCE INSPECTION THE AFT AISLE PATH EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007032100144 20070321 00144 SO 2007 3 21 C2XA07IA060 1 20070308 A 4920 M4504113A APU EMB 145 EMB145EP 3260221 SO APU BAY INOPERATIVE A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 12934 5306 10 145019 DFW - FLIGHT 2811, THE CREW REPORTED A LAV SMOKE INDICATION AFTER TAKEOFF. THE AIRCRAFT RETURNED TO DFW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE APU ON MEL 49-00-00 CTL 117353, AND THE AIRCRAFT W AS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT CAME TO IAH ON 03/09/07 WHERE MAINTENANCE REMOVED AND REPLACED THE APU, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007032100145 20070321 00145 SO 2007 3 21 C2XA07IA061 1 20070311 A 4920 M4504113A APU EMB 135 EMB135LR 3260305 SO APU BAY BURNED A C2XA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 SW 27 16525 11761 11761 145403 BTR - FLIGHT 2679, THE CREW REPORTED AN APU FIRE AT THE GATE AFTER AN UNSUCCESSFUL RESET. MAINTENANCE INSPECTED THE AIR CRAFT AND PLACED THE APU ON MEL 49-00-00 CAT C CTL 117499, AND 26-22-00 CAT C CTL 117498. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO IAH ON FLIGHT 2574 ON 03/11/07 AND MAINTENANCE REMOVED AND REPLACED THE AP U, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL'S, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007032100153 20070321 00153 SO 2007 3 21 C2XA07TY012 1 20070313 A 5751 14569009410 ATTACH BRACKET EMB 145 EMB145EP 3260221 SO RT AILERON WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 RIGHT AILERON ATTACH BRACKET WORN AT THE HOLES FOR THE HAT BUSHINGS. REMOVED AND REPLACED AILERON PCA BRACKET IAW EC575 0-01177. AIRCRAFT IS STILL IN C-CHECK. 2 L 7 2 4F RT T00011AT 2007032100154 20070321 00154 SO 2007 3 21 C2XA07TY011 1 20070311 A 5751 14569009409 ATTACH BRACKET EMB 145 EMB145EP 3260221 SO LT AILERON DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 LEFT AILERON PCA ATTACH BRACKET HAS DAMAGED HAT BUSHING HOLES. REMOVED AND REPLACED BRACKET IAW EC5750-01177. AIRCRAFT IS STILL IN C-CHECK. 2 L 7 2 4F RT T00011AT 2007032100155 20070321 00155 NM 2007 3 21 KCSA071068 1 20070317 A 5315 FLOORBEAM BOEING 747 747236B 1384804 NM BS 1920 DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 AFT BILGE FLOORBEAM STANCHION AT BOTTOM NEAR CARGO DOOR IS DENTED AT STA 1920, RBL 64. 2 L 7 4 4F A20WE 2007032200001 20070322 00001 EA 2007 3 22 COMA0760260 1 20070315 A 5310 60034017595 CROSSBEAM CNDAIR CL600 CL6002B19 1900309 EA FS 280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 797CA 7344 FS 280 CROSSBEAM CORRODED. REPAIRED CROSSBEAM IAW REO 601R-53-21-069. 2 L 7 2 4F RT A21EA 2007032200002 20070322 00002 EA 2007 3 22 COMA0760261 1 20070315 A 5610 NP13932111 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA O OTHER O OTHER CR CRUISE 1 SO 01 528CA 8967 7841 CAPTAIN'S WINDSHIELD INNER PANEL SHATTERED. PROCEEDED TO CVG WITHOUT INCIDENT. REPLACED CAPTAIN'S WINDSHIELD. 2 L 7 2 4F RT A21EA 2007032200005 20070322 00005 NE 2007 3 22 DXTA200702037 2 20070318 A 7200 ENGINE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE RIGHT SHUTDOWN E DXTA E D ENGINE SHUTDOWN RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 335QS 5600335 PCE500168 RT ENG SPOOLED DOWN TO 10-15 PERCENT N1 APPROX 2 MIN AFTER START WITH NO THROTTLE MOVEMENT, RAPID INCREASE IN ITT AT THE SAME TIME BUT NOT ABOVE LIMITATIONS. ALSO, ENG STARTED ON THIRD ATTEMPT, NO FUEL SPILL. REMOVED FUEL INLET LINE TO FLO W DIVIDER & MOTORED ENG OVER. FUEL SPRAYED OUT AT HIGH VOLUME. PERFORMED 2 NORMAL ENG STARTS AND TOOK ENG TO N1 OF THE DAY. ALL READINGS NORMAL. WAITED A HOUR & TOOK ENG TO N1 OF THE DAY AGAIN WITH NORMAL RESULTS. VISUALLY INSPECTED AL L ADJUSTMENT POINTS FOR SECURITY. RECOWLED NR 2 ENG & PERFORMED 1 MORE START & VERIFIED BOTH ENG STARTED NORMALLY, NO E RRATIC READINGS. COULD NOT DUPLICATE SQUAWK. WORK DONE IAW CITATION 560 AMM SECTION 73-10-00, PWA JT15-5D EMM 3040342. 2 L 7 2 4F 4 F RT A22CE E25EA 2007032200006 20070322 00006 CE 2007 3 22 DXTA200702032 1 20070317 A 3210 LANDING GEAR CESSNA 680 680CE 2076811 CE RIGHT MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 350QS 6800036 RT MAIN MOUNT FAILED TO INDICATE DOWN AND LOCKED, (RED UNSAFE LIGHT) WAS ILLUMINATED. FOLLOWED CHECKLIST PROCEDURE, BLE W DOWN GEAR AND LANDED UNEVENTFULLY. REPLACED DOWN LOCK SWITCH ON RIGHT MAIN GEAR OPS CHECK GOOD IAW CE680 MM CHAP 32-3 0-40. 2 L 7 2 4F RC T00012WI 2007032200007 20070322 00007 CE 2007 3 22 DXTA200702033 1 20070317 A 2701 CONTROL COLUMN CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE COCKPIT VIBRATION E DXTA O OTHER E VIBRATION/BUFFET CR CRUISE 1 GL 07 643QS 5605588 NOTICEABLE VIBRATION OF CONTROL COLUMN DURING TAKEOFF,CLIMB,REDUCED DURING. CRUISE AND BEGINS TO BE MORE NOTICEABLE DURI NG DECENT AND LANDING. TROUBLESHOT ELEVATOR SYSTEM. FOUND LEFT AND RIGHT ELEV. TRIM TAB BEARINGS TO HAVE EXCESSIVE PLAY . REMOVED AND REPLACED L/R TRIM TAB BEARINGS WITH NEW UNITS. SYSTEM CHECKS GOOD AT THIS TIME. IAW CE560 XLS M/M 2 L 7 2 4F 4 F RT A22CE E00059EN 2007032200008 20070322 00008 CE 2007 3 22 DXTA200702034 1 20070317 A 3240 BRAKE ASSY CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG WEAK E DXTA O OTHER S AFFECT SYSTEMS LD LANDING 1 GL 07 915QS 7500015 ON LANDING, BRAKE PEDALS FELT MUSHY NEEDED TO USE MORE BRAKE PEDAL THAN NORMAL. PERFORMED POWER BRAKE AND ANTISKID SYST EM BLEEDING ON EACH BRAKE ASSEMBLY IN ACCORDANCE WITH TASK 32-42-00-721 OF THE CE750 MM LEAK CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007032200009 20070322 00009 EA 2007 3 22 COMA0760258 1 20070315 A 5700 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA LT WING UNKNOWN A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 989CA 7215 FLIGHT 5576 - LEFT WING OVERHEAT ON BEGINNING OF TAKEOFF THRUST. DEFERRED PER MEL 30-12-03-1. 2 L 7 2 4F RT A21EA 2007032200010 20070322 00010 NM 2007 3 22 NOCA05607 1 20070310 A 3350 BULB BOEING 767 767306 1385148 NM EMERGENCY LIGHT INOPERATIVE A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 768NA 29898 E-PATH LIGHT INSIDE R4 DOOR JAMB AREA INOP. REPLACED LIGHT AND RECONNECTED WIRE AS PER MM 33-51-00. 2 L 7 2 4F RT A1NM 2007032200011 20070322 00011 NM 2007 3 22 NOCA05707 1 20070310 A 3397 WIRE BOEING 767 767306 1385148 NM EMERGENCY LIGHT BROKEN A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 768NA 29898 RED E-PATH LIGHT INOP 26AB - 26GH. REPINNED BROKEN WIRE AS PER MM 33-51-00. 2 L 7 2 4F RT A1NM 2007032200013 20070322 00013 NM 2007 3 22 NOCA05807 1 20070310 A 3350 3071 BULB BOEING 767 767306 1385148 NM EMERGENCY LIGHT INOPERATIVE A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 768NA 29898 E-PATH LIGHT BY LEFT LAV INOP. REPLACED LIGHT AS PER MM 33-51-00. 2 L 7 2 4F RT A1NM 2007032200015 20070322 00015 2007 3 22 NOCA06307 4 20070314 A 3445 751790010003 COMPUTER BOEING 767 767306 1385148 NM TCAS MALFUNCTIONED A NOCA O OTHER J WARNING INDICATION AP APPROACH 1 EA 15 765NA 28098 TCAS/TCAS OFF EICAS INTERMITTENT DURING APPROACH. REPLACED TCAS COMPUTER PER MM 34-45-01, OPS CHECK OK. 2 L 7 2 4F RT A1NM 2007032200016 20070322 00016 NM 2007 3 22 NOCA05907 1 20070314 A 2121 033638500 FAN BOEING 757 75728A 1384976 NM UNKNOWN A NOCA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 15 752NA 28174 FORWARD DET FAN ON STATUS. REPLACED BLOWER PER MM 26-16-02. 2 L 7 2 4F RT A2NM 2007032200017 20070322 00017 NM 2007 3 22 NOCA06007 1 20070314 A 3241 ANTI-SKID SYS BOEING 767 76739H 1385311 NM MLG UNKNOWN A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 760NA 26257 ANTI-SKID SYSTEM ONE CHANNEL INOP DUE TO NR 8 TRANSDUCER FAULT. MEGGERED WIRES FROM ANTI-SKID MODULE TO NR 8 TRANSDUCER , CHECKED FOR POWER RESIST AT NR 8 TRANSDUCER. SUSPECT BAD WIRE AT J2 BOX ON RT LANDING DUE TO FAULT NR 7 TRANSDUCER OC CURRED WHEN DISTURBING WIRES AT J2 FOUND WIRE 2688-201B-20 OPEN TO NR 7 TRANSDUCER. RE-PINNED PLUG 02024, ALL CHECKS GO OD BITE ON AS/AB CONTROLLER NO FAULTS, ACCOMPLISHED ANTI-SKID AUTO BRAKE TEST PER MM 32-42-00, NO FAULTS. 2 L 7 2 4F RT A1NM 2007032200018 20070322 00018 2007 3 22 NOCA06107 4 20070314 A 3461 COMPUTER BOEING 757 75728A 1384976 NM TCAS INOPERATIVE A NOCA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 754NA 29381 TCAS INOP EICAS ON TAKEOFF ROLL. ABORTED BELOW 60 KNOTS. OPENED CI 34-01 FOR TCAS INOP PER MEL 34-61-2 AND ACCOMPLISHE D A HIGH ENERGY STOP PER MM 5-51-14. SDR STILL OPEN PREFORMED FIM 34-45-00 FOUND RA DISP AT FAULT REPLACED TCAS COMPUT ER IAW 34-45-01 OPS CHECK OK 2 L 7 2 4F RT A2NM 2007032200019 20070322 00019 2007 3 22 NOCA06507 4 20070314 A 3442 6225132633 TRANSCEIVER BOEING 757 75728A 1384976 NM WINDSHEAR UNKNOWN A NOCA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 15 755NA 30043 WINDSHEAR SYSTEM MESSAGE ON EICAS. PERFORMED FIM TASK 24-43-00 REPLACED WX XCVR PER MM 34-43-01, OPS CHECK OK. 2 L 7 2 4F RT A2NM 2007032200021 20070322 00021 NM 2007 3 22 NOCA06207 1 20070314 A 5270 SENSOR BOEING 767 767306 1385148 NM PAX DOOR OUT OF ADJUST A NOCA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 15 765NA 28098 LEFT FWD ENTRY DOOR EICAS MESSAGE. ADJUSTED S194 SENSOR PER MM 52-71-00, TEST OK. 2 L 7 2 4F RT A1NM 2007032200022 20070322 00022 2007 3 22 NOCA06407 4 20070314 A 3457 8221152002 RECEIVER BOEING 767 767306 1385148 NM GPS MALFUNCTIONED A NOCA O OTHER J WARNING INDICATION CR CRUISE 1 EA 15 765NA 28098 RIGHT GPS EICAS MSG ILLUMINATED IN FLIGHT. REPLACED RIGHT MMR PER MM 34-3101, OPS CHECK OK. 2 L 7 2 4F RT A1NM 2007032200024 20070322 00024 NM 2007 3 22 CALA0700132 1 20070317 A 5330 6545775 SKIN BOEING 737 7373T0 1384582 NM BS 727E S24L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 77303 23354 INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT STA 727E, S24L. A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 201. 2 L 7 2 4F RT A16WE 2007032200026 20070322 00026 CE 2007 3 22 AMW082983BC 1 20070301 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER FALSE INDICATION A AMWA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 176YV 25114 370 UE176 WHILE IN FLT, THE BATTERY CHARGE ANNUN ILLUMINATED. CREW PROCEEDED TO DESTINATION, LANDED SAFELY WITH NO FURTHER INCIDE NT. THIS BATTERY CHARGE LIGHT ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS. REMOVED AND REPLACED BATTERY 2 L 7 2 4T 4 T RT A24CE E26NE 2007032200028 20070322 00028 CE 2007 3 22 AMW083289BC 1 20070315 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER FALSE INDICATION A AMWA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 159YV 18322 325 UE159 BATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT, CREW RAN THE ABNORMAL CHECKLIST, BATTERY CHARGE RATES DECREASED, ANNUN CIATOR EXTINGUISHED, FLIGHT CONTINUED TO DESTINATION W/NO FURTHER INCIDENT. THIS BC ILLUMINATION IS CONSIDERED A NUISANC E WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS. RESET A130 PCB - OPS CHECKED GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2007032200029 20070322 00029 CE 2007 3 22 AWM070223021C 1 20070306 A 5311 1294400333 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 451 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 146ZV 26382 UE146 RT FUSELAGE FRAME DAMAGED BY CHAFING. REPAIRED IAW ENGINEERING REPORT 6593-1, REV IR (MAR 5, 2007).. 2 L 7 2 4T 4 T RT A24CE E26NE 2007032200031 20070322 00031 CE 2007 3 22 AWM070223021A 1 20070306 A 5311 1294300311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 258 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 146ZV 26382 UE146 LT FUSELAGE FRAME DAMAGED BY CHAFING. REPAIRED IAW ENGINEERING REPORT 6593-1, REV IR DATED 5 MAR 07.. 2 L 7 2 4T 4 T RT A24CE E26NE 2007032200032 20070322 00032 CE 2007 3 22 AWM083043BC 1 20070305 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER FALSE INDICATION A AMWA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 159YV 18322 247 UE159 BATTERY CHARGE ANNUN ILLUM IN FLT. UPON ARRIVAL AT DESTINATION, BATTERY WAS REPLACED WITH NO INCIDENT. THIS BATTERY CH ARGE ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS. 2 L 7 2 4T 4 T RT A24CE E26NE 2007032200035 20070322 00035 CE 2007 3 22 AMW082669BC 1 20070215 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER FALSE INDICATION A AMWA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 133YV 16181 350 UE133 WHILE IN FLT, THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED. CREW PROCEEDED TO DESTINATION, LANDED SAFELY WITH NO FURTHER INCIDENT. THIS BATTERY CHARGE LIGHT ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE P ILOTS. REPLACED BATTERY, RAN ACFT SYS, OPS CKS NORMAL, COULDN'T DUPLICATE. 2 L 7 2 4T 4 T RT A24CE E26NE 2007032200038 20070322 00038 CE 2007 3 22 DJFA2007029 1 20070315 A 5514 HINGE BRACKET CESSNA 750 750 2076810 CE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 701LX 7500114 DURING A SCHEDULED MAINTENANCE INSPECTION, THE LT IB HORIZONTAL STABILIZER ELEVATOR HINGE BRACKET WAS FOUND CRACKED. MA INTENANCE WILL REPLACE THE BRACKET IAW MFG ENGINEERING. (SUPPLEMENTAL 28 MARCH 07) THE CRACK WAS .2" ON THE INBD HORIZ ONTAL HINGE HALF. THE BRACKET WAS REPLACED PER CESSNA DRAWING 6732030 DATED 8-30-95. 2 L 7 2 4J RT T00007WI 2007032200039 20070322 00039 SO 2007 3 22 RAIA00703028 1 20070313 A 3350 100865 BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 847HK 2535 14500857 PRE FLT NR 8022 - STL - EMERGENCY LIGHTS (COCKPIT FLOODLIGHT AND FWD AISLE FLOODLIGHTS) INOP. MAINTENANCE REMOVED AND R EPLACED NR 1 EMERGENCY LIGHT BATTERY PACK, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007032200041 20070322 00041 SO 2007 3 22 RAIA00703030 1 20070314 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN MALFUNCTIONED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 807HK 145119 PRE FLT NR 5549 - STL - DOOR EMERGENCY LIGHTS INOP, MAIN DOOR EXIT MARKER. MAINTENANCE RESET POWER TO EMERGENCY LIGHTS, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007032200045 20070322 00045 SO 2007 3 22 RAIA00703032 1 20070315 A 2750 FLAP SYSTEM EMB 145 EMB145LR 3260212 SO TE FLAPS OUT OF ADJUST A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 816HK 145055 FLT NR 5587 - STL - FLAP FAIL MESSAGE ON EICAS. MAINTENANCE RIGGED FLAP SYSTEM, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007032200047 20070322 00047 SO 2007 3 22 RAIA00703027 1 20070312 A 2750 FLAP SYSTEM EMB 145 EMB145LR 3260212 SO TE FLAPS FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 816HK 145055 FLT NR 5558 - ALT - FLAP FAIL. MAINTENANCE RESET FLAP SYSTEM, SYSTEM OPS CHECKS NORMAL. 2 L 7 2 4T RT T00011AT 2007032200049 20070322 00049 EA 2007 3 22 COMA0760266 1 20070316 A 5610 NP1393225 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A COMA O OTHER O OTHER CR CRUISE 1 SO 01 936CA 13040 7043 FLIGHT 5091 - CAPTAIN'S SIDE WINDOW CRACKED AND SHATTERED OUTER LAYER IN FLIGHT AT FL320. AIRCRAFT LANDED SAFELY IN CVG . REMOVED AND REPLACED CAPTAIN'S SIDE WINDOW. 2 L 7 2 4F RT A21EA 2007032200051 20070322 00051 EA 2007 3 22 COMA0760268 1 20070319 A 3240 BRAKE ASSY CNDAIR CL600 CL6002B19 1900309 EA RT MLG OVERHEATED A COMA O OTHER M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 989CA 7215 FLIGHT 5204 - LEFT BRAKE INOPERATIVE WHILE THE RIGHT BRAKE INDICATED HOT DURING ARRIVAL AT BOS. RECONNECTED THE LEFT ML G INBOARD AND OUTBOARD BRAKE QUICK DISCONNECT FITTINGS. 2 L 7 2 4F RT A21EA 2007032200052 20070322 00052 EA 2007 3 22 COMA0760259 1 20070315 A 3260 16600103 UPLOCK CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 594SW 19914 7285 FLIGHT 5013 - NOSE GEAR DISAGREE ON APPROACH, NOSE GEAR SHOWED WHITE BOX, RAN QRH NOSE GEAR DOWN AND LOCKED. PERFORMED EMERGENCY LANDING IN JFK. AIRCRAFT LANDED SAFELY. UPLOCK FAULTY. 2 L 7 2 4F RT A21EA 2007032200054 20070322 00054 WP 2007 3 22 ABXA070075 1 20070315 A 5312 99155613 BULKHEAD DOUG DC9 DC941 302207N WP AFT CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 AFT LOWER CARGO, AFT BULKHEAD WEB EXFOLIATED AT LEFT BUTT LINE 18 INCHES AT TOP. REPAIRED DAMAGE IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 2007032200056 20070322 00056 NE 2007 3 22 COMA0760269 2 20070319 A 7261 388700320153 CHECK VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENG OIL PUMP FAULTY A COMA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 01 451CA 7562 873763 FLIGHT 9456 - EN ROUTE LGA-CVG RECEIVED A LEFT ENGINE WARNING MESSAGE, CREW DECLARED AN EMERGENCY AND PERFORMED AN INFLI GHT SHUTDOWN OF THE LEFT ENGINE. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT ENGINE OIL PUMP CHECK VALVE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007032200057 20070322 00057 WP 2007 3 22 ABXA070072 1 20070315 A 3397 WIRE DOUG DC8 DC863F 302198F WP CABIN LIGHTS DAMAGED A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 816AX 46093 DURING SERVICE CHECK FOUND ELECTRICAL ODOR COMING FROM OVERHEAD LIGHT. FOUND ONE FLUORESCENT LIGHT RECEPTACLE CORRODED AT TERMINAL ENDS AND SHORTING. CLEANED RECEPTACLE AND REPLACED BOTH TERMINAL ENDS ON WIRES COMING TO RECEPTACLE. REPLA CED LAMP AND OPS CHECKED GOOD IAW DC8 AMM 33. 2 L 7 4 4F 4A25 2007032200058 20070322 00058 CE 2007 3 22 032007N300CS1 1 20070320 A 3233 SWITCH CESSNA 500 550 2076604 CE PWA 530 PW530A NE MLG ACTUATOR MALFUNCTIONED E Z5FA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 63 300CS 5500818 AFTER TAKEOFF, THE LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. THE LT MAIN GEAR GREEN LIGHT ILLUMINATED ABOUT 10 SECONDS LATER FOLLOWED BY THE RT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A BAD SWITCH IN THE RT MAIN L ANDING GEAR ACTUATOR. THE ACTUATOR WAS REPLACED GEAR SWINGS WERE PERFORMED AND SYSTEM OPS OK. AIRCRAFT WAS RETURNED TO S ERVICE. 1 L 7 2 4F 4 F A22CE E00053EN 2007032200059 20070322 00059 NE 2007 3 22 2007UALA00719 2 20070310 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 551UA 25399 726553 DIVERTED FLIGHT DUE TO LOSS OF NR 1 ENGINE. LEFT ENGINE FAILED INFLT FL330 N2 ZERO OIL PRESSURE. ENGINE WINDMILLING INSPECTION. CREW REPORTED ENGINE WINDMILLED FOR 40 MINS WITH ZERO OIL QTY INDICATED. CONDUCTED OIL FILTER AND MAG PLUG S INSP AND NO CONTAMINATION WAS FOUND. FILTER REPLACED. REPLACED EEC ALTERNATOR AND STATOR. ROOT CAUSE ATTRIBUTED TO A FAILED ROTOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032200060 20070322 00060 NM 2007 3 22 2007UALA00720 1 20070311 A 5310 DOOR FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 918UA 25385 FWD CARGO DOOR CUTOUT AFT DOORWAY FRAME IS CRACKED ON AFT SIDE OF FRAME IN RADIUS AT UPPER I/B CORNER AT DOOR LOWER BOTT OM STOP FITTING. MAJOR REPAIR ACCOMPLISHED: INSTALLED NESTED ANGLE DOUBLER FRAME REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032200062 20070322 00062 NM 2007 3 22 2007UALA00722 1 20070311 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 280 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 RIGHT SIDE STA 280 FLOORBEAM HAS CORROSION AND BLEND-OUT EXCEEDS LIMITS. MAJOR REPAIR ACCOMPLISHED: REMOVED SECTION OF T-CAP. FABRICATED & INSTALLED NEW SECTION OF T-CAP CHORD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007032200064 20070322 00064 NM 2007 3 22 2007UALA00724 1 20070310 A 5210 TORQUE TUBE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU PAX DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 918UA 25385 FWD ENTRY DOOR BODY TORQUE TUBE SLEEVE ON LOWER SPIGOT CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED AND REPLACED FUSEL AGE TORQUE TUBE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032200065 20070322 00065 NM 2007 3 22 2007UALA00725 1 20070310 A 5210 LINER BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU PAX DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 918UA 25385 FWD ENTRY DOOR LINER AFT LOWER CORNER CRACKED WITH A SHARP EDGE STICKING OUT. MAJOR REPAIR ACCOMPLISHED: FABRICATED A ND INSTALLED A DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032200067 20070322 00067 NM 2007 3 22 2007UALA00726 1 20070309 A 3350 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 338UA 24242 LEFT AFT OVERWING EMERGENCY EXIT LIGHT ON EXTERIOR OF ACFT INOPERATIVE. RELAMPED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032200070 20070322 00070 NE 2007 3 22 ANCF200600046 2 20070312 A 7200 ENGINE BOEING 757 7572T7 1384914 NM RROYCE RB211 RB211535E437 54555 NE LEFT FAILED W ANCF A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 23 513NA 23895 30748 LT ENGIINE SURGED DURING CONSTANT POWER DURING CLIMB AT 6.000 FT. ENGINE OPS NORMAL AFTER SURGE AT LOW THRUST. BOROSCO PE INSPECTION ACCOMPLISHED TO INTERMEDIATE PRESSURE COMPRESOR, HIGH PRESSURE COMPRESOR, COMBUSTION CHAMBER, HIGH PRESSUR E TURBINE BLADES, LOW PRESSURE TURBINE BLADES AND INTERMEDIATE PRESSURE TURBINE FOUND IN LIMITS. IAW AMM 71-00-00-PAGIN A 201 & EWO 75-72-7179. REPLACED NR 1 ENGINE. TEST RUN UP WAS SATISFACTORY IAW AMM 71-00-00 PAG 501. LT ENGINE REPLACEME NT & FIRE DETECTION CARDS CONFIGURATION, FIRE DETECTOR CARDS M681 Y M682 REPLACED IAW EWO 75-72-7179 INSTRUCTIONS & AMM 26-10-01 PAG 401. LT ENGINE REPLACEMENT, HP2 & HP6 HIGH PRESSURE DUCTS REPLACED IAW AMM 36.11-01 PAGE 401 & OPS TEST ACC 2 L 7 2 4F 4 F RT A2NM E12EU 2007032200094 20070322 00094 NM 2007 3 22 UPS07449453 1 20070212 A 5311 FRAME BOEING 747 747121 1384871 NM BS 820 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT BS 820 TENSION TIE TO FRAME CONNECTION NR 4 AND NR 10 FASTENER HOLE FOUND CRACK AT FRAME WEB DOUB LER RUNNING UP THRU THICKNESS. CRACK LENGTH .125 INCH. LEFT BS 820 TENSION TIE TO FRAME WEB ATT DOUBLER REPLACED AS PE R SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007032200095 20070322 00095 NM 2007 3 22 UPS07449454 1 20070216 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 2185 S51R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C BULK CARGO COMPT STRINGER FOUND CRACK AT STA 2185 STR 51R. CRACK LENTH .375 INCH. BULK CARGO COMPT B S 2185 STR 51R REPAIRED AS PER RS R53-11-35768 AND UPS ENGINEERING FILE NUMBER 747-53-20407. 2 L 7 4 4F A20WE 2007032200096 20070322 00096 NM 2007 3 22 UPS07449455 1 20070214 A 5311 65B0500272 FRAME BOEING 747 747121 1384871 NM BS 800 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT BS 800 FRAME FOUND 2EA FASTENER CRACKS AT STRAP LAYER. CRACK LENGTH 0.125 INCH AND 0.025 INCH. FRAME REPAIRED AS PER RS R53-12-35762 AT BS 800 STR 16R TO STA 18R STRAP AREA AND REFER UPS EO B747-5310-26131. 2 L 7 4 4F A20WE 2007032200097 20070322 00097 CE 2007 3 22 AMW070223021 1 20070315 A 5542 1295240003 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RUDDER DENTED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 146ZV 26417 UE146 (2) DENTS IN RUDDER; (1) ON THE LT SIDE AND (1) ON THE RT LOWER END CAP. REPAIRED IAW 1900-27-00-0001. 2 L 7 2 4T 4 T RT A24CE E26NE 2007031900046 20070319 00046 NM 2007 3 19 UPS07M49380 1 20070131 A 5313 AFA7719501 LONGERON DOUG MD11 MD11F 3023600 NM BS 1139 L43R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C FROM STA 6-90 TO STA 1139, LONGERON NR 43R CORRODED. CORRODED LONGERON & ATT/PARTS REMOVED FOR ACCESS PER SRM 51-31-01 V2 R38. NEW LONGERON P/N AFA7719-501, FAB PER DWG AFA7719. FPI C/OT ON NEW FAB PART FOUND NO EVIDENT OF CRACK. NEW LONGERON FRAME HOLES PICKED UP PER DW G:AFA7719 & SRM 51-31-01 V2 R38. INSTALLATION OF LONGERON PER DWG 7719 & SRM 51-31-01 V2 R38, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007031900052 20070319 00052 NM 2007 3 19 ZZDA070310141 1 20070310 A 3350 4TL115 SWITCH BOEING 717 717200 1383700 NM EMERGENCY LIGHTS INOPERATIVE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 946AT 55009 CABIN EMERGENCY LIGHTS WILL NOT ILLUMINATE WITH SWITCH ON. REMOVED AND REPLACED R2-5086 RELAY, NO HELP. REMOVED AND RE PLACED COCKPIT EMERGENCY LIGHT SWITCH IAW M/M 20-30-06. OPS CHECKS GOOD IAW M/M 33-51-00. 2 L 7 2 4F TR A6WE 2007031900065 20070319 00065 EA 2007 3 19 COMA0760254 1 20070314 A 3213 STRUT CNDAIR CL600 CL6002B19 1900309 EA NLG DISCHARGED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 989CA 7215 FLIGHT 9426 - AFTER TAKEOFF, SELECTED GEAR UP, MAINS RETRACTED BUT NOSE GEAR HAD A LOUD CONTINUOUS BANGING NOISE WITH ON INDICATION OF GEAR UP OR DOWN. SERVICED OIL AND NITROGEN OF NLG STRUT. PERFORMED EXTENSION / RETRACTION TEST, OPS TES T GOOD. 2 L 7 2 4F RT A21EA 2007031900068 20070319 00068 EA 2007 3 19 COMA0760239 1 20070308 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 969CA 7141 FLIGHT 5375 - FLAPS FAILED AT ZERO DEGREES PRIOR TO LANDING. A/C LANDED SAFELY. COMPLIED WITH AD 2006-12-21 FLAP CAUTI ON MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLA P CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007031900069 20070319 00069 NM 2007 3 19 0312200701 1 20070312 A 2910 AS115080326 HOSE BOEING 747 747200B NM GE CF6 CF650* 30018 NE HYD SYSTEM WORN A OZYA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 29 535FC 21833 AFTER TAKEOFF, WITH LG RETRACTED, OBSERVED HYDRAULIC SYSTEM NR 4 LOOSE WITH BOTH NR 4 EDP, ADR LOW PRESSURE ON. AOM 2- 2-55 AND 2-2-59 FOLLOWED, RETURNED TO DEPARTURE.FOUND LT WING GEAR DOOR ACTUATOR HYDRAULIC LINE WORN. REMOVED AND REPLA CED HYDRAULIC LINE, AND REWORKED NR 4 EDP IAW MM 29-11-05, INSTALLING EDP DISPATCH KIT IAW MM29-11-03, SERVICE, AND LEAK CHECK OK. EDP PLACED ON MEL IAW MEL 29-1. AIRCRAFT RETURNED TO SERVICE. 1 L 7 4 4F 4 F RT A20WE E23EA 2007031900070 20070319 00070 2007 3 19 YENA2007017 4 20070314 A 2330 3042865102 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU UNKNOWN A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 519JB 7691 1398 FLT 752, CUN/JFK. F/A SMELLED ELECTRICAL BURNING ODOR EMITTING FROM VICINITY ROW 7 DEF C/C RIGHT. F/A FELT CONTROL BO X 7D, IT FELT VERY WARM. THERE WAS NO SMOKE. ELECTED TO TURN OVERHEAD GALLEY 1 C/B PANEL LIVE TV MASTER SWITCH OFF FOR REMAINDER OF FLIGHT. F/A STATED SMELLING ELECTRICAL BURNING ODOR AT ROW 7DEF AS WELL AS FEELING THE SEB WARMER THAN US UAL. NO LOSS OF VIDEO WAS REPORTED AND SYSTEM WAS IMMEDIATELY TURNED OFF. PERFORMED TSM TASK 23-39-00-810-801 OF LTV A MM 23-39-33. NO DISCREPANCIES NOTICED IN IMMEDIATE AREA OF SUSPICIOUS ODOR. REMOVED AND REPLACED SEB 7 D PRECAUTIONARY . REACTIVATED LTV SYSTEM. 2 L 7 2 4F RT A28NM 2007031900074 20070319 00074 SO 2007 3 19 SIMA200706703 1 20070305 A 3350 20131A POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 623AE 10152 21 145109 FOUND EMERGENCY FLOOR STRIP BETWEEN ROW 8 AND 12 INOPERATIVE, OVERWING EXIT WALL LIGHTS INOPERATIVE. REMOVED AND REPLAC ED NUMBER 3 BATTERY POWER SUPPLY IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007031900078 20070319 00078 SO 2007 3 19 SIMA200706704 1 20070225 A 5315 14521413605 FLOORBEAM EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 804AE 13150 4800 145487 FOUND CENTER OMEGA BEAM CORRODED AT FRAME 23. PERFORMED CUT TO REMOVE CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007031900082 20070319 00082 SO 2007 3 19 SIMA200706707 1 20070301 A 5315 14521413605 FLOORBEAM EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 807AE 13140 4800 145506 CENTER OMEGA BEAM FOUND CORRODED AT FRAME 25. PERFORMED CUT OUT TO REMOVE CORROSION, FABRICATED AND INSTALLED REPAIR PA RTS IAW EMB SRM 53-00-01. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007031900096 20070319 00096 EA 2007 3 19 COMA0760257 1 20070315 A 5312 601R3202650 POST CNDAIR CL600 CL6002B19 1900309 EA BULKHEAD CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 938CA 7046 DURING INSPECTION FOUND BULKHEAD VERTICAL POST, LOWER END CRACKED, FS 559, RBL 18. REMOVED DAMAGE AND INSTALLED DOUBLER PER BOMBARDIER REO 601R-53-41-067. 2 L 7 2 4F RT A21EA 2007031900103 20070319 00103 NM 2007 3 19 PIDA07013 1 20070309 A 5753 FAIRING BOEING 757 757236 1384971 NM TE FLAPS DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 757BJ 22176 DURING INSPECTION, FOUND CORROSION ON LOWER SURFACE OF LEFT WING AT THE FORWARD ATTACH POINT FOR THE I/B FLAP TRACK FAIR ING (WING STA 285.65). REPAIRED PER BOEING MESSAGES 1-281963543-1 AND 1-281963543-9 WITH FAA DOA APPROVED 8100-9 DATED 3-6-2007. 2 L 7 2 4F RT A2NM 2007031900106 20070319 00106 EA 2007 3 19 TRAX200700334 1 20070308 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 FS 280 FWD CENTER FLOOR SUPPORT ANGLE CORRORED. REPAIRED IAW ALL SRM`S. 2 L 7 2 4F RT A21EA 2007031900107 20070319 00107 EA 2007 3 19 TRAX200700335 1 20070308 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 LEFT LOWER FS 280 WEB HAS CORROSION. REMOVED LEFT 280 WEB SPLICE DOUBLER. REMOVED LEFT 280 LOWER CORRODED WEB IAW CRJ 700, 51-42-06. RE-INSTALLED SPLICE WET WITH SOLID FASTENERS; BOTTOM 2EA ROWS TO LOWER LEFT 280 WEB IAW CRJ SRM 51-42-02 . STARTED INSTALLATION OF FASTENERS IN LEFT 280 WEB AND SPLICE DOUBLER IAW REO 670-53-11-052. COMPLETED INSTALLATION O F LEFT FS 280.00 LOWER WEB FASTENERS IAW BOMBARDIER REO 670-53-11-052. FILLET SEALED REPAIR AREA IAW CRJ 700 SRM 51-23- 00. TOPCOATED REPAIR AREA IAW CRJ 700 SRM 51-25-16. SUPPLEMENTAL - SDR CLOSED 03/15/07. 2 L 7 2 4F RT A21EA 2007031900108 20070319 00108 EA 2007 3 19 TRAX200700336 1 20070308 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 RIGHT LOWER FS BULKHEAD WEB HAS CORROSION. REPLACED WEB. 2 L 7 2 4F RT A21EA 2007031900133 20070319 00133 NM 2007 3 19 SWAA071347 1 20070312 A 2121 215201 FAN BOEING 737 7375H4 138449D NM A/C BAY FAULTY A SWAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 SW 29 512SW 24189 DIVERSION, ELECTRICAL ODOR IND PAX CABIN. GASPER FAN C/B TRIPPED. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2007031900142 20070319 00142 NM 2007 3 19 SWAA071350 1 20070313 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM BS 727D S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007031900143 20070319 00143 NM 2007 3 19 SWAA071345 1 20070311 A 3350 ADD71701 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 448WN 33721 DURING SCHEDULED HC1 CHECK, LEFT FWD CABIN EMERGENCY EXIT LIGHT BATTERY PACK FAILED THE LONG CHECK. REMOVED AND REPLACE D BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007032000005 20070320 00005 NM 2007 3 20 USAA070196 1 20070315 A 5712 654544555 RIB BOEING 737 737401 1384701 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 LEFT WING, WBL 235.5 IN SPAR RIB, LOWER CHORD BETWEEN STRINGERS 2 & 3 CRACKED. CUT OUT CRACKED SECTION OF LOWER CHORD, FAB'D & INSTALLED REPAIR FILLERS & TEE PER EA 98492, DEFECT SIZE: 0.6 INCH. 2 L 7 2 4F RT A16WE 2007032000011 20070320 00011 NM 2007 3 20 USAA070202 1 20070315 A 5340 66235743 STRINGER CLIP BOEING 737 737401 1384701 NM BS 706 S11L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 BS 706 S-11L, STRINGER TIE CLIP CRACKED. REMOVED CRACKED TIE CLIP & INSTALLED NEW PER SRM 51-10-02, DEFECT SIZE: .5 INC H. 2 L 7 2 4F RT A16WE 2007032000027 20070320 00027 CE 2007 3 20 031307N425CS1 1 20070313 A 2611 47359717 SMOKE DETECTOR CESSNA 525 525 2076601 CE CARGO BAY DIRTY E Z5FA O OTHER N FALSE WARNING DE DESCENT 1 EA 63 425CS 525B0132 ON DESCENT FL110 THE BAGGAGE SMOKE LIGHT ILLUMINATED ON THE ANNUNCIATOR PANEL. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. NO SMOKE OR SMELL WAS NOTICED IN THE CABIN BY THE FLIGHT CREW. MAINTENANCE TROUBLESHOT THE SYSTEM FOU ND DUST ON THE CEILING AREA AND SMOKE DETECTOR IN THE AFT BAGGAGE COMPARTMENT. CEILING AND SMOKE DETECTOR WAS CLEANED. N O EVIDENCE OF SMOKE OR BURNING WAS FOUND. SYSTEM TEST WAS GOOD. 1 L 7 2 4F RT A1WI 2007032000029 20070320 00029 NM 2007 3 20 USAA070208 1 20070315 A 5320 REVEAL BOEING 737 737401 1384701 NM SERVICE DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 FWD SERVICE DOOR SEAL REVEAL AT FWD UPPER CORNER STA 300 S7R CRACKED. INSTALLED NEW REVEAL & FAIRING COMPOUND & PRIMED PER BOEING DWG 65-53595 & SRM 53-10-02, DEFECT SIZE: 1.5 INCH. 2 L 7 2 4F RT A16WE 2007032000053 20070320 00053 NM 2007 3 20 SWAA071389 1 20070314 A 5330 6545890 SKIN BOEING 737 7373Q8 1384670 NM BS 291 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 291, NEXT TO R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PE R SRM. 2 L 7 2 4F RT A16WE 2007032000055 20070320 00055 NM 2007 3 20 SWAA071392 1 20070314 A 5315 6546804 FLOORBEAM BOEING 737 7373Q8 1384670 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, LBL 65 TO RBL 65. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2007032000063 20070320 00063 NM 2007 3 20 PIDA07012 1 20070219 A 5240 FRAME BOEING 757 757236 1384971 NM L4 DOOR CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 757BJ 22176 DURING INSPECTION FOUND CORROSION ON AN INTERNAL FRAME WEB ON THE FORWARD SIDE OF THE L4 DOOR WINDOW. CUT INNER SKIN OF DOOR FOR ACCESS AND REPLACED DAMAGED FRAME SECTION PER SRM 51-70-11 FIGURE 1 AND DWG 146N6100 AND REPAIRED INNER DOOR S KIN PER EA 52-031. 2 L 7 2 4F RT A2NM 2007032000068 20070320 00068 NM 2007 3 20 SWAA071382 1 20070314 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 616 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007032000074 20070320 00074 NM 2007 3 20 2007UALA00659 1 20070302 A 2910 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE HYD SYSTEM UNKNOWN A UALA O OTHER J WARNING INDICATION LD LANDING 1 WP 29 661UA 27158 LANDED UNDER AMBER ALERT DUE TO HYDRAULIC QUANTITY INDICATION. AIRCRAFT TOWED TO GATE. REPLACED O-RING NR 2 ELECTRIC P UMP PRESSURE REDUCER FITTING, REFILLED & PRESSURIZED SYSTEM. NO LEAKS NOTED. RETURN TO SERVICE. SUSPECT NORMAL WEAR IN S ERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007032000081 20070320 00081 NM 2007 3 20 UIEA200700124 1 20070302 A 5312 65B07992121 BULKHEAD BOEING 747 7472D3B 1384805 NM BS 1250 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 BS 1250, L WLG W/W CANTED PRESSURE BULKHEAD, NR 2 PACK COOLING DUCT CUTOUT FOUND CORROSION. REPAIRED ACCOMPLISHED AS P ER BOEING SR ID NR 1-289645346-1 THRU -5 AND FAA FORM 8100-9. 2 L 7 4 4F RT A20WE 2007032000085 20070320 00085 NM 2007 3 20 UIEA200700112 1 20070302 A 5311 FRAME BOEING 747 7472D7B 1384803 NM BS 840 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 21784 FOUND BS 840 FRAME TO TENSION TIE CONNECTION FOUND 1 HOLE CRACKED. REPAIR ACCOMPLISHED PER BOEING DRAWING ON MESSAGE 1- 283852403-4. 2 L 7 4 4F RT A20WE 2007032000087 20070320 00087 NM 2007 3 20 UIEA200700122 1 20070302 A 5414 SKIN BOEING 747 747243B 1384830 NM NR 4 NACELLE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 NR 4 PYLON CUT-OUT FOR PRE-COOLER EXHAUST AIR, RT SIDE OF PYLON AT NACELLE STATION 248.0 HAS A 2.625 INCH CRACK AT AFT, LOWER CORNER. ACCOMPLISHED INTERIM REPAIR, LOCATED CRACK AS PER NDT 747 MANUAL 51-00-00 PAR 6 AND STOP DRILLED BY REAMI NG EXISTING HI-LOCK HOLE TO .312 INCH DIAMETER AS PER 747 SRM 51-10-01 AND SRM 51-30-02. VERIFIED CRACK HIT HOLE AND IN STALLED HI-LOCK AS PER 747 SRM 51-30-02. REFERENCE ATLAS AIR XEO 54-030207. 2 L 7 4 4F A20WE 2007032000090 20070320 00090 NM 2007 3 20 2007UALA00687 1 20070306 A 5414 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 NR 2 PYLON OUTBOARD SKIN IS CRACKED AT FWD HOLE. [SUP 4-24-07] MAJOR REPAIR ACCOMPLISHED. HFEC INSP AT END OF CRACK. INSTALLLED 301 HALF 0.050" DOUBLERS AS A UA APPROVED REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032000103 20070320 00103 EU 2007 3 20 2007UALA00691 1 20070307 A 2910 O-RING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYD SYSTEM FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 498UA 1865 RTFL DUE TO GREEN HYDRAULIC SYSTEM FAILURE. GEAR WAS MANUALLY EXTENDED. REPLACED NR 1 ENGINE HYDRAULIC PUMP, AND NR 1 ENGINE HYDRAULIC PUMP CASE DRAIN FILTER PRECAUTIONARY. LEAK WAS DETERMINED TO BE CAUSED BY A CHECK VALVE PACKING IN THE NR 1 ENGINE PYLON. REPLACED O-RING. LEAK CHECKED GOOD. NFF ON PUMP BY THE SHOP. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032000104 20070320 00104 EU 2007 3 20 2007UALA00692 1 20070307 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 403UA 442 EMERGENCY LIGHT TEST FAULTED LEFT UNIT. REPLACED EPSU. OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007120600006 20071206 00006 EU 2007 12 6 07FDEA04966 1 20071130 A 3260 RELAY AIRBUS 300 A300F4605R 3930327 EU MLG INDICATOR FAILED A FDEA L ABORTED APPROACH N S FALSE WARNING AFFECT SYSTEMS AP APPROACH 1 SO 25 731FD 709 AT 200' AGL RECEIVED "TOO LOW GEAR" GPWS WARNING. LOG GEAR POS DET SYS 1. EXECUTED GO AROUND, SWITCH TO SYSTEM 2 AND LA NDED UNEVENTFULLY. HAD GOOD INDICATIONS ON ALL 3 GEAR INDICATORS. ACN RELEASED FOR SERVICE PER MEL/CDL: 32-61-01-B CA TEGORY: B EXPIRATION: 03DEC07 "MEL 32-61-01-B: OVHD LANDING GEAR INDICATOR PANEL - INOP." NO FAULTS LOGGED ON PROX BOX OR FACE OF EGPWS. USED TSM 32-61-00 FOR TS. REPLACED RELAY 99GB PER SMP. ACCOMPLISHED TEST OF GROUND PROX WARNING SYSTE M PER A300 MM 34-48-00-5-02. TEST GOOD. 2 L 7 2 4F RT A35EU 2007032000105 20070320 00105 NM 2007 3 20 2007UALA00694 1 20070308 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EEL AT 5E, 5F & DOOR 5L XAISLE ARE INOPERATIVE. SECURED LOOSE FEEDER CABLE IN ONE POSITION AND SPLICED CABLE IN THE OTH ER. EEL LIGHTS OP CHECKED OK FOR SERVICE. SUSPECT DAMAGE CAUSED BY PAX TRAFFIC & CARRY-ON BAGGAGE IMPACT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032000106 20070320 00106 NM 2007 3 20 2007UALA00695 1 20070308 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EEL AT 4E & 4F ARE INOPERATIVE. SECURED LOOSE FEEDER CONNECTOR. EEL OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032000107 20070320 00107 NM 2007 3 20 2007UALA00698 1 20070307 A 5414 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 NR 2 PYLON INBOARD SIDE SKIN CRACKED AT FWD HOLE. MAJOR REPAIR ACCOMPLISHED: REPAIRED SIDE SKIN WITH 3 EACH REPAIR DO UBLERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032000108 20070320 00108 NM 2007 3 20 2007UALA00700 1 20070308 A 3233 ACTUATOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE MLG UNKNOWN A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 175UA 24382 LANDING GEAR WON'T RETRACT; RTFL & LANDED UNDER AMBER ALERT. REPLACED RT BODY TILT ACTUATOR. CYCLED GEAR, OP CHECKED O K. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032000109 20070320 00109 EU 2007 3 20 2007UALA00701 2 20070305 A 7230 COMPRESSOR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU NR 1 ENGINE STALLED A UALA O OTHER R E J PARTIAL RPM/PWR LOSS VIBRATION/BUFFET WARNING INDICATION DE DESCENT 1 WP 29 932UA 26658 726356 ON DESCENT NR 1 ENG COMPRESSOR STALLED WITH AUDIBLE BANGS. TWO BANGS WHEN THROTTLE RETARDED AT FL370, ENG BANGED LIGHTL Y DOWN TO FL 150 AND BETWEEN FL 150-100 VIBRATION AND NOISE INCREASED. [07-03-07] FOUND MINOR DAMAGE TO THE 3RD STAGE BLADES AND VANES, WITH HEAVY DAMAGE ON THE 4TH STAGE BLADES AND VANES. MINOR DAMAGE ON THE 5TH THROUGH 9TH STAGE BLADES AND VANES. REPLACED ENGINE. REPLACED BLADES ON REMOVED ENGINE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032000110 20070320 00110 EU 2007 3 20 2007UALA00702 1 20070308 A 2913 PUMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYD SYSTEM FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 406UA 454 GREEN HYDRAULIC PUMP FAILURE JUST AFTER DEPARTURE. REPLACED NR 1 ENGINE PUMP PRESSURE SWITCH. RAN ENGINE PRESSURE AND INDICATION NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032000111 20070320 00111 NM 2007 3 20 2007UALA00703 1 20070308 A 2750 UNKNOWN BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE TE FLAP UNKNOWN A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 668UA 30024 AMBER ALERT DECLARED DUE TO FLAP PROBLEM. AIRCRAFT ARRIVED WITH NO TE FLAPS DISAGREE EICAS OR STATUS MSG DISPLAYED. A CP FSEU BITE PER FIM 27-51-00-101. FSEU TEST OK, NO FAULTS NOTED. FLAPS OPS CHECK OK ON GROUND. UNABLE TO DUPLICATE PROB LEM ON GROUND. 2 L 7 2 4F 4 F RT A1NM E24NE 2007032000112 20070320 00112 NM 2007 3 20 2007UALA00704 1 20070308 A 3350 CHARGER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EPSU 1L FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 849UA 1649 EPSU 1L FAULT ON CIDS. REPLACED EPSU 1L CHARGER AND BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032000113 20070320 00113 NM 2007 3 20 2007UALA00705 1 20070308 A 2131 CONTROLLER BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN PRESSURE FAULTED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 930UA 26655 CABIN PRESSURIZATION ELECTRONIC SYSTEM IN STANDBY, CABIN PRESSURE SURGES (OSCILLATING CABIN ALTITUDE) IN DESCENT. OUTFL OW VALVE INDICATOR IS NOT OSCILLATING. OK IN MANUAL. CABIN PRESSURE CONTROLLER FAULTY. REPLACED CPC, PERFORMED PRESS URE TEST--PASSED. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032000114 20070320 00114 2007 3 20 2007UALA00706 4 20070308 A 2565 SLIDE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU DOOR 1R UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 942UA 26679 SLIDE PACK 1R FELL OUT OF DOOR PACK BUT DID NOT ACTIVATE. [SUP 05-16-07] REINSTALLED SLIDE PACK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032000115 20070320 00115 NM 2007 3 20 2007UALA00707 1 20070308 A 5320 SILL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R2 DOORWAY CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 802UA 690 R-2 DOOR SILL PLATE HAS CORROSION AT CLIP NUT HOLE BETWEEN FR 65 AND 66. MAJOR REPAIR ACCOMPLISHED: REPLACED SILL PLATE . 2 L 7 2 4F 4 F RT A28NM E40NE 2007032000116 20070320 00116 EU 2007 3 20 2007UALA00708 1 20070309 A 3597 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN SEATS 3AB, DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 421UA 500 CABIN SEATS 3AB, 3CD, 17ABC FAILED O2 MASK RELEASE CHECK. [SUP 05-29-07] ADJUSTED THE OXYGEN CONTAINER DOOR SPACERS AND REPLACED THE RELEASE SOLENOIDS AS A PRECAUTIONARY MEASURE. AT SEATS 17ABC, FOUND THE ELECTRICAL CONNECTOR DISCONNECT ED. RECONNECTED & PERFORMED DROP TEST. TESTS OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032000117 20070320 00117 NM 2007 3 20 2007UALA00709 1 20070308 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 616 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 364UA 24533 FUSELAGE BS 616 LT SIDE OVERWING FRAME INNER CHORD CRACKED LBL 65. MAJOR REPAIR ACCOMPLISHED: ACCOMPLISHED ANGLE, FILL ER & SHIM REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032000118 20070320 00118 NM 2007 3 20 2007UALA00710 1 20070308 A 5210 TORQUE TUBE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU PAX DOOR WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 364UA 24533 AFT ENTRY DOOR FUSELAGE TORQUE TUBE LOWER SPIGOT WORN. MAJOR REPAIR ACCOMPLISHED: REMOVED AND REPLACED FUSELAGE TORQUE TUBE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032100019 20070321 00019 2007 3 21 2007UALA00759 4 20070313 A 2565 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR OUT OF ADJUST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 588UA 26717 DOOR 1L WILL NOT ARM. ADJUSTED GIRT BAR FLOOR LOCK, DOOR OPS CHECK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032100020 20070321 00020 2007 3 21 2007UALA00760 4 20070313 A 2565 GIRT BAR AIRBUS A319 A319131 3930317 NM DOOR SLIDE OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 802UA 690 AFT GIRT BAR FLOOR FITTING CLEARANCE OUT OF ADJUSTMENT. [SUP 06-01-07] FOUND THAT THE GIRT BAR FLOOR FITTINGS WERE OUT OF ADJUSTMENT AND NOT ALLOWING THE GIRT BAR TO FREELY MOVE FROM THE DOOR FITTINGS TO THE SILL FITTINGS. THE FLOOR STRUC TURE AROUND DOOR 2R WAS OPENED UP A FEW DAYS EARLIER FOR A CORROSION REPAIR (REF SDR 2007UALA00636). THE GIRT BAR FLOOR FITTINGS WERE NOT PROPERLY ADJUSTED AFTER THE REPAIR WAS FINISHED. 2 L 7 2 4F RT A28NM 2007032100021 20070321 00021 NM 2007 3 21 2007UALA00761 1 20070313 A 5330 SKIN BOEING 737 737322 1384676 NM FUSELAGE PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 PUNCTURE RT SIDE OF FUSELAGE BELOW FWD LAV SVC DOOR. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SKIN. INSTALLED DOUBLE R-TRIPLER & FILLER REPAIR. 2 L 7 2 4F RT A16WE 2007032100022 20070321 00022 NM 2007 3 21 2007UALA00762 1 20070314 A 2150 8102044 VALVE BOEING 777 777222 1385219 NM RT A/C PACK STICKING A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 212UA 30218 FLIGHT DIVERTED DUE TO RIGHT A/C PACK PROBLEM. TROUBLESHOOTING IDENTIFIED PARTIALLY OPEN PACK FLOW CONTROL VALVE. REPLA CED RIGHT HAND FLOW CONTROL VALVE. A/C PACK SYSTEM OP CHECKED OK FOR SERVICE. 2 L 7 2 4F RT T0001SE 2007032100023 20070321 00023 NM 2007 3 21 2007UALA00763 1 20070314 A 5330 SKIN BOEING 737 737322 1384676 NM BS 941-945 S24L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 EXTERNAL FUSELAGE SKIN CRACKED ABOVE STR 24LT AT FUSELAGE STA 941 TO 945. [SUP 4-17-07] MAJOR REPAIR ACCOMPLISHED PER EVA 70120. 2 L 7 2 4F RT A16WE 2007032100024 20070321 00024 NM 2007 3 21 2007UALA00764 1 20070315 A 2810 UNKNOWN BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE FUEL SYS UNKNOWN A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 105UA 26473 UNWANTED FUEL TRANSFER. FOUND NR 3 AFT OVERRIDE PUMP DISCHARGE CHECK VALVE MISSING PIN FOR DRAIN HOLE. REQ PER MM 28-31 -11 ITEM 1D. REPLACED CK VLV WITH PIN INSTALLED. PROBLEM PERSISTED. PERFORMED TANK ENTRY & TROUBLESHOOTING. FINALLY RE PLACED DENSITOMETER, COMPENSATOR & TANK PROBE. RETURNED TO SERVICE WITH NO RECURRENCE OF UNWANTED FUEL TRANSFER. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032100025 20070321 00025 NM 2007 3 21 2007UALA00765 1 20070315 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHTS FROM ROWS 22GH TO 26GH & 35HJK TO 44HJK ARE INOPERATIVE. BATTERY PACK INOPERATIVE. REPLACED BATTERY PA CKS IN BOTH POSITIONS. ALL EEL OP CHECK NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032100026 20070321 00026 NM 2007 3 21 2007UALA00766 1 20070315 A 3350 LAMP BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE DOOR SLIDE 5L INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY DOOR SLIDE LIGHT 5L & 5R INOP. RELAMPED SLIDE LIGHT, BOTH POSITIONS. BOTH OP CHECK NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032100027 20070321 00027 NM 2007 3 21 2007UALA00767 1 20070314 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LAVATORY FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 549UA 25397 EEL LIGHT BAR IN FRONT OF THE AFT LAV IS INOPERATIVE. REPAIRED AFT LAV LIGHT BAR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032100029 20070321 00029 NM 2007 3 21 2007UALA00769 1 20070315 A 3350 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 199UA 28717 ZONE "E" ALL EMERGENCY LIGHTS TURN ON AND OFF. [SUP 4-17-07] REPLACED POWER SUPPLY M6010, 6011, 6012 AND 6013 PER MM 3 3-51-04 P201. OPS CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032100030 20070321 00030 2007 3 21 2007UALA00770 4 20070313 A 3442 SCANNER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE WX RADAR SYS FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 651UA 25389 FLIGHT DIVERTED DUE TO WEATHER RADAR FAILURE. REPLACED SCANNER ASSY PER MM34-43-05. PERFORMED OPERATIONAL TEST OF WEA THER RADAR. TEST SUCCESSFUL PER MM 34-43-00 2 L 7 2 4F 4 F RT A1NM E24NE 2007032100031 20070321 00031 NM 2007 3 21 2007UALA00771 1 20070314 A 3397 58644 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 652UA 25390 EMERGENCY EEL LIGHTS INOP FROM SEATS 30HJ TO AFT GALLEY. SUPPLEMENTAL DATA UPDATE REPAIRED EEL STRIPS FEEDING LEFT REAR OF AIRCRAFT. OP CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007032100032 20070321 00032 NM 2007 3 21 2007UALA00772 1 20070314 A 3350 362624 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 3F INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 771UA 26932 FWD EEL LIGHT AT SEAT 3F IS INOPERATIVE. REPLACED LIGHT ASSY. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007032100033 20070321 00033 NM 2007 3 21 2007UALA00773 1 20070314 A 3350 1317 LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 771UA 26932 SEAT 43D EEL LIGHT IS INOPERATIVE. RELAMPED. OPS CHECKS GOOD . 2 L 7 2 4F 4 F RT T0001SE E46NE 2007032100034 20070321 00034 NM 2007 3 21 2007UALA00774 1 20070314 A 5412 BULKHEAD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 NACELLE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 NR 2 ENGINE STRUT BULKHEAD CRACKED AT MAIN FUEL LINE CLAMP BLOCK CONNECTION AT NAC STA 102.1. MAJOR REPAIR ACCOMPLISHED : REMOVED 3 ANGLES, 2 FILLER, 2 SEALS AND VBAND. REMOVED WEB. INSTALLED NEW WEB, ANGLES AND FILLERS. INSTALLED VBAND R ETAINER AND 2 SEALS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032200012 20070322 00012 NM 2007 3 22 NOCA05507 1 20070310 A 3213 161T11455 PIVOT ASSY BOEING 767 767306 1385148 NM LT MLG CRACKED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 768NA 29898 LEFT MLG BOGIE PIVOT PIN CRACKED. REPLACED MLG BOGIE PIVOT PIN AS PER EO 767-32-007. 2 L 7 2 4F RT A1NM 2007032200014 20070322 00014 NM 2007 3 22 NOCA05407 1 20070310 A 3350 1317 BULB BOEING 767 767306 1385148 NM EMERGENCY LIGHT INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 768NA 29898 E-PATH LIGHTING ABOVE 14AB INOP. REPLACED LIGHT AS PER MM 33-51-00. 2 L 7 2 4F RT A1NM 2007032200020 20070322 00020 NM 2007 3 22 NOCA05107 1 20070304 A 7830 SLEEVE BOEING 767 767306 1385148 NM THRUST REVERSER DAMAGED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 765NA 28098 DURING THE POST FLIGHT INSPECTION, DAMAGE WAS FOUND ON THE NR 2 ENGINE OUTBOARD THRUST REVERSER TRANSCOWL SLEEVE. 2 L 7 2 4F RT A1NM 2007032200033 20070322 00033 CE 2007 3 22 AMW082976BC 1 20070301 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER FALSE INDICATION A AMWA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 138YV 22399 223 UE138 WHILE IN FLT, THE BATTERY CHARGE ANNUN ILLUMINATED. CREW PROCEEDED TO DESTINATION, LANDED SAFELY WITH NO FURTHER INCIDE NT. THIS BATTERY CHARGE LIGHT ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS. REMOVED AND REPLACED BATTERY 2 L 7 2 4T 4 T RT A24CE E26NE 2007032200036 20070322 00036 EA 2007 3 22 COMA0760262 1 20070316 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS OBSTRUCTED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 796CA 7338 FLIGHT 9429 - FLAPS FAIL CAUTION MESSAGE AFTER FLAP RETRACTION, FLAPS FAILED AT ZERO DEGREES. FOUND A LARGE AMOUNT OF P ACKED SNOW AND ICE IN THE LEFT INBOARD FLAP COVE AREA OF THE WING TRAILING EDGE. AFTER REMOVING DEBRIS, FLAPS RESET. I NSPECTED LEFT FLAP SYSTEM, NO DEFECTS. FLAP SYSTEM, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007032200040 20070322 00040 2007 3 22 RAIA00703029 2 20070313 A 7200 UNKNOWN EMB 145 EMB145LR 3260212 SO ENGINE UNKNOWN A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 825HK 145510 FLT NR 5486 - DEN - E2 NO MARGIN MSG. MAINTENANCE PERFORMED ENGINE RUN, COULD NOT REPRODUCE PROBLEM AT THIS TIME ENGINE STAYED WITHIN LIMITS. 2 L 7 2 4T RT T00011AT 2007032200043 20070322 00043 SO 2007 3 22 RAIA00703021 1 20070309 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT UNSECURE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 833HK 145240 PRE FLT NR 8022 - STL - LEFT EMERGENCY OVERWING EXIT MARKER LIGHT INOP. MAINTENANCE RESCURED LEFT EMERGENCY LIGHT CONNE CTOR, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007032200044 20070322 00044 SO 2007 3 22 RAIA00703023 1 20070309 A 3350 BULB EMB 145 EMB145 3260210 SO EMERGENCY LIGHT LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 820HK 145064 PRE FLT NR 5587 - STL - EMERGENCY LIGHT RIGHT EMERGENCY DOOR FLOODLIGHT IS OUT. MAINTENANCE RESEATED LAMP AND OPS CHECK . 2 L 7 2 4F RT T00011AT 2007032200053 20070322 00053 WP 2007 3 22 ABXA070074 1 20070315 A 5312 991556153 BULKHEAD DOUG DC9 DC941 302207N WP AFT CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 AFT LOWER CARGO, AFT BULKHEAD WEB AND ANGLE EXFOLIATED AT RIGHT BUTT LINE 4 INCHES AT BOTTOM SIDE. REPAIRED DAMAGED IAW ABX ENGINEERING TO DUPLICATE PRODUCTION SPLICE IAW DACO DWG 9915561 AND DC9 SRM 51-30-0. 2 L 7 2 4F A6WE 2007032200063 20070322 00063 NM 2007 3 22 2007UALA00723 1 20070309 A 3350 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 844UA 1581 RIGHT OVERWING FAILS EMERGENCY LIGHT TEST. REPLACED POWER SUPPLY AND BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032200071 20070322 00071 EA 2007 3 22 TRAX200700340 1 20070311 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA CABIN WORN A AOSA K NONE O OTHER IN INSP/MAINT 1 SO 27 885AS 7521 ASD -EXIT- PLACARD WORN. 2 L 7 2 4F RT A21EA 2007032200072 20070322 00072 NM 2007 3 22 USAA200703004 1 20070320 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 525 S11L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 503UW 23237 HFEC INDICATES .125 INCH CRACK IN STRINGER S-11L BS 525. DETECTED BY ROTATING EDDY CURRENT. REMOVED CRACKED STRINGER & REPAIRED PER EA 84289 & SRM 51-70-12. 2 L 7 2 4F RT A16WE 2007032200073 20070322 00073 NM 2007 3 22 ASMF200703004 1 20070312 A 2410 729825J IDG BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE LEFT LEAKING W ASMF C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SW 23 805AM 17443 10629 26272 AIRCRAFT REJECTED TAKEOFF AT 80 KNOTS DUE TO (L GEN) LIGHT TURNED ON IN EICAS. DURING MAINTENANCE CHECK, THE LT IDG WAS DETECTED WITH LOW OIL LEVEL. FAILURE WAS DEFERRED BY MEL 24-00-1, THE LANDING GEAR AND BRAKES WERE CHECKED BY CONDITION, BEING ALL CORRECT. THE REJECTED TAKEOFF INSPECTION WAS PERFORMED IAW MM 05-51-14, ALL CORRECT. DURING OVERNIGHT CHECK, THE LT IDG WAS REPLACED IAW MM 24-11-01, TESTED CORRECT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032200076 20070322 00076 NM 2007 3 22 2007UALA00731 1 20070309 A 2497 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FWD CARGO BAY BURNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 FOUND BURNED WIRE BUNDLES & SHIELDED WIRES DAMAGED ALONG WITH INTERCOSTAL AND FLOOR STRUCT AT STA 680 FWD PIT CEILING. FOUND WIRES W4104-0082-20 & W4104-0090-20 SHORTED TO GROUND. RIGHT RECIRC FAN CIRCUIT BREAKER C337 ON P37 PANEL TRIPPED . PUSHING C/B IN ACFT RESULTED IN LOSS OF RT BUSS POWER. FOUND WIRES W4104-0082-20 & W4104-0090-20 SHORTED TO GRND. (3 50 OHMS & 1.26 KOHMS) ORDERED WTR HEATER TAPE (B118) GOES TO WIRE W4104-0090-20. STILL NEED TO ISOLATE WIRES FROM SPLICE (SP285)TO LOCATE PROBLEM WITH MID FWD TOILET DRAIN HTR GASKET (B10112) OR MID FWD DRAIN LINE HTR TAPE. FLOORBEAM SUPPO RT MFG AND INSTD. RMVD DMG INTERCOSTAL. MAIN ACFT BATTERY MAIN POWER CONNECTOR SAFETIED WITH BREAK AWAY WIRE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032200099 20070322 00099 CE 2007 3 22 DJFA2007030 1 20070316 A 3260 DOWNLOCK SWITCH BEECH MU300 400A 1155402 CE MLG OUT OF RIG E DJFA O OTHER N FALSE WARNING LD LANDING 1 EA 23 466LX RK507 ON ROLLOUT, AFTER LANDING, THE LT MAIN GEAR COLLAPSED. INITIAL INSPECTION REVEALED THE LT DOWN LOCK SWITCH OUT OF RIG AN D THE OVER CENTER PIVOT JOINT APPEARED TO BE BINDING DUE TO LACK OF LUBRICATION. THE AIRCRAFT HAS NOT REACHED ITS FIRST SCHEDULED MAINTENANCE EVENT. [SUP 05-21-07] MAINTENANCE DISCOVERED THE LEFT MLG DOWNLOCK SWITCH OUT OF ADJUSTMENT. THE MLG DOWNLOCK SWITCH WAS ADJUSTED. 2 H 7 2 4F RT A16SW 2007032200100 20070322 00100 CE 2007 3 22 DJFA2007031 1 20070321 A 3210 PIN BEECH MU300 400A 1155402 CE MLG MISSING E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 471LX RK506 UPON INSPECTION OF THE RT MAIN LANDING GEAR MAINTENANCE DISCOVERED THE UPPER TORQUE LINK PIVOT PIN WAS MISSING ITS RETAI NING PIN. THE PIVOT PIN HAD SLID OUT ABOUT .5 INCHES. ADDITIONALLY, IT APPEARS THAT THE GEAR HAS NOT BEEN PROPERLY LU BRICATED. AIRCRAFT HAS NOT REACHED ITS FIRST SCHEDULED MAINTENANCE EVENT. THE PIVOT PIN WAS ADJUSTED AND A ROLL PIN IN STALLED. THE GEAR WAS LUBRICATED. 2 H 7 2 4F RT A16SW 2007032200101 20070322 00101 NM 2007 3 22 UPS07449456 1 20070214 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D R3 DOOR CUTOUT FWD LOWER CORNER SKIN AND STRAP FOUND CRACKED. CRACK LENGTH 2.5 INCHES. RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS R53-41-35782. 2 L 7 4 4F A20WE 2007032200102 20070322 00102 NM 2007 3 22 UPS07449457 1 20070228 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER 1EA FASTENER HOLE (IDENT I) FOUND CRACK THRU THICKNESS AT 5:00 O/C POSITION (LOOKING I/B) CRACK LENGTH 2.5 INCH. RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS R53-41-35782. 2 L 7 4 4F A20WE 2007032200103 20070322 00103 NM 2007 3 22 UPS07449458 1 20070211 A 5311 FRAME BOEING 747 747121 1384871 NM BS 900 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT BS 900 FRAME TENSION TIE ATTACHMENT AREA AT FASTENER HOLE NR 1 THREE CRACKS FOUND AT FRAME LAYER . CRACK LENGTH .0625 AND 0.030 INCH. M/D BS 900 RIGHT FRAME BETWEEN STR 6R TO STR 11-5R REPAIRED AS PER RS R53-10-3575 0. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-10-35750 AND UPS EO B747-5310-26134. 2 L 7 4 4F A20WE 2007032200104 20070322 00104 NM 2007 3 22 UPS07449459 1 20070210 A 5311 FRAME BOEING 747 747121 1384871 NM BS 880 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT BS 880 TENSION TIE ATTACHMENT AREA NR 13 FASTENER HOLE CRACK AT FRAME WEB THRU THICKNESS APPROX .0625 INCH. M/D RIGHT BS 880 TENSION TIE ATTACH FRAME AT STR 6R TO STR 12R REPAIRED AS PER RS R53-25-35752 AND UPS EO B 747-5310-26133. 2 L 7 4 4F A20WE 2007032200105 20070322 00105 NM 2007 3 22 UPS07449460 1 20070212 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 640 RBL 100-108 FLOORBEAM FOUND CORROSION. CORROSION BLEND 0.136 X 1 X 2 INCH EXCEED SRM LIMIT . M/D BS 640 RBL 100-108 FLOORBEAM FITTING REPAIRED AS PER RS R53-25-35757 AND UPS ENGINEERING FILE NUMBER 747-53-20405 . 2 L 7 4 4F RT A20WE 2007032200106 20070322 00106 NM 2007 3 22 UPS07449461 1 20070210 A 5311 FRAME BOEING 747 747121 1384871 NM BS 940 S7-8L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 940 STR 7-8L FRAME O/B FLANGE FOUND CRACK. CRACK LENGTH 0.875 INCH. M/D BS 940 LEFT BETWEEN S TR 5L TO STR 12L FRAME REPAIRED AS PER RS R53-25-35756 AND UPS EO B747-5310-14767. 2 L 7 4 4F A20WE 2007032200107 20070322 00107 NM 2007 3 22 UPS07449462 1 20070213 A 5311 FRAME BOEING 747 747121 1384871 NM BS 380 S14-15L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 380 STR 14-15L FRAME FWD FACE FOUND CRACK. CRACK LENGTH 1 INCH. M/D BS 380 STR 14-15L FRAME F WD FACE REPAIRED AS PER RS R53-10-35758. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-10-35758 AND UPS EO B747-5310-26 303. 2 L 7 4 4F A20WE 2007032200108 20070322 00108 NM 2007 3 22 UPS07449463 1 20070210 A 5311 FRAME BOEING 747 747121 1384871 NM BS 880 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT SIDE BS 880 TENSION TIE ATTACHMENT AREA NR 10 FASTENER HOLE CRACK FOUND AT FRAME DOUBLER APPROX .0625 INCH IN LENGTH. M/D BS 880 RIGHT FRAME ATTACH DOUBLER REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007032200109 20070322 00109 NM 2007 3 22 UPS07449464 1 20070211 A 5311 FRAME BOEING 747 747121 1384871 NM BS 780 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT BS 780 FRAME TENSION TIE ATTACHMENT AREA AT FASTENER HOLE NR 5 CRACK AT FWD CHANNEL RUNNING UPPER APPROX .125 INCH IN LENGTH. M/D BS 780 LT TO RT FRAME ATTACH TENSION TIE FWD CHANNEL REPLACED AND 51-30-02. 2 L 7 4 4F A20WE 2007032200110 20070322 00110 NM 2007 3 22 UPS07449465 1 20070211 A 5311 FRAME BOEING 747 747121 1384871 NM BS 820 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RT BS 820 FRAME TENSION TIE ATTACHMENT AREA AT FASTENER HOLE NR 11 CRACK AT FRAME UPPER APPROX .0625 I NCH IN LENGTH RUNNING AT 5:00 O/C POSITION. RIGHT BS 820 FRAME REPAIRED BETWEEN STR 8R AND STA 11-5R AS PER RS R53-25-3 5751. 2 L 7 4 4F A20WE 2007032200111 20070322 00111 NM 2007 3 22 2007UALA00776 1 20070314 A 5520 BEARING BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU ELEVATOR OUT OF LIMITS A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 934UA 26662 LOW FREQUENCY VIBRATIONS FELT AFTER GEAR RETRACT. STOPPED AT 1ST LEVEL OFF FL24. DID NOT RETURN IN CLIMB. FOUND ROTB ELEV TRIM TAB BEARING OUT OF LIMITS- REPLACED BEARINGS AND PERFORMED INSPECTIONS OF ALL SURFACES AND DRAINS FOR ABNORMA L CONDITIONS. NO FURTHER VIBES NOTED AFTER THESE ACTIONS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032200113 20070322 00113 NE 2007 3 22 2007UALA00778 2 20070315 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 DAMAGED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING C J F.O.D. WARNING INDICATION CL CLIMB 1 WP 29 662UA 27159 727334 RTFL UNDER AMBER ALERT WITH NR 1 ENGINE SHUT DOWN DUE TO BIRD STRIKE (TOWED TO GATE). A/C ENCOUNTERED A FLOCK OF DUCKS. BOTH ENGINES HAD COMPRESSOR SURGES DUE TO INGESTION. NR 1 WAS MUCH MORE SEVERELY DAMAGED & ENGINE WAS REPLACED. NR 2 E NGINE BORESCOPED & PLACED ON 25 HOUR LIMIT TO BE REPLCD AT GSO. NUMEROUS SHEET METAL DAMAGE SITES INCLUDING 1 X 2 FT DE NT ON LEFT SIDE OF FUSELAGE, DMG TO STA 132.5 AT STR 212R, STA 204.5 AT STR 32L, STA 266.5 AT STR 11R. ALSO DMGED WERE BOTH NOSE GEAR DOORS, NR 1 ENG NOSE COWL & PITOT STATIC PROBES. DAMAGE FROM FOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007032200114 20070322 00114 NM 2007 3 22 2007UALA00779 1 20070315 A 5310 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE VIBRATION A UALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 29 518UA 24871 FLIGHT DIVERTED DUE TO AN AIRFRAME VIBRATION. UNIDENTIFIED RUMBLE- VIBRATION VERY STRONG AFT GALLEY MIDDLE FLOOR. FOUN D WATER FILL VALVE OPEN, CLOSED VALVE. SERVICE PANEL HAD ICE CHUNKS BANGING AROUND INSIDE CAUSING NOISE. CLEANED OUT PAN EL AND CLOSED. REMOVED AFT CARGO CENTER WALL PANEL AND INSPECTED AREA AROUND WATER TANK, NO LEAKS FOUND. NO WATER PRESS URE, PULLED CB'S TO POT WATER COMPRESSOR. VIBRATION IN CTRLINE IN AFT GALLEY CONTINUES AND GETS WORSE AT TIMES. FOUND FILL VALVE IN SERVICE PANEL OPEN. CLOSED PANEL, AIR COMPRESSOR BUILDS PRESSURE AND SHUTS OFF AS NORMAL. MAINTENANCE TO ENSURE FILL VLV IS CLOSED, WATER PRESSURE AVAILABLE IN CABIN AND COMPRESSOR IS SILENT PRIOR TO RE-DISPATCHING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032200115 20070322 00115 NM 2007 3 22 2007UALA00780 1 20070315 A 5347 SEAT TRACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 488 LBL 11 GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 MAIN CABIN SEAT TRACK GOUGED AT BS 488 AND LBL 11. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF SEAT TRACK A ND EXISTING FWD REPAIR SPLICE AT BS 422. FABRICATED NEW SEAT TRACK AND REPAIR SPLICES. 2 L 7 2 4F 4 F RT A1NM E24NE 2007032200116 20070322 00116 NM 2007 3 22 2007UALA00781 1 20070315 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 654 RBL 77 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 ELONGATED HOLE ON FLOORBEAM AT BS 654+88, RBL 77.0. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF UPPER CHORD FLANGE. FABRICATED & INSTALLED CHORD ANGLE AND SPLICE STRAPS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007032200117 20070322 00117 NM 2007 3 22 2007UALA00782 1 20070315 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 654 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 DOUBLE DRILLED FIGURE 8 HOLES ON FLOORBEAM UNDER CABIN FLOOR AT BS 654+22, RBL 66 TO RBL 77, 2 PLACES. MAJOR REPAIR AC COMPLISHED: FABRICATED AND INSTALLED 2 EACH FREEZE PLUGS AND REPAIR STRAPS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007032200118 20070322 00118 NM 2007 3 22 2007UALA00783 1 20070315 A 5720 WEB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 RIGHT WING LEADING EDGE CAVITY, WEB CRACKED AT LES 588. DAMAGE TO WING FIXED LEADING EDGE NOSE BEAM WEB. AFFECTED SRM REPAIR PROCEDURE. VERIFIED CRACK CONTAINED BY STOP DRILLS PER HFEC NDT 51-00-19, PRT 6. FABRICATED REPAIR PARTS AND I NSTALLED PER SRM 57-41-13. A/C READY FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007032200119 20070322 00119 NM 2007 3 22 2007UALA00784 1 20070315 A 5512 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE HORIZONTAL STAB DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 780UA 26944 RIGHTT HORIZONTAL STABILIZER LOWER SKIN HAS IMPACT DAMAGE. RT HORIZONTAL STABILIZER REPAIR ACCOMPLISHED PER UAL EVA 701 28. A/C READY FOR RETURN TO SERVICE. SUSPECT DAMAGED BY GROUND EQUIPMENT OR RUNWAY KICK-UP FOREIGN OBJECT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007032200120 20070322 00120 EU 2007 3 22 2007UALA00785 1 20070316 A 5100 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE VIBRATION A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 443UA 820 HIGH FREQ LATERAL VIBRATION FROM TAIL OF ACFT DURING CLIMBOUT. VIBRATION DECREASES WITH DECREASE IN AIR SPEED. [SUP 06 -01-07] REPLACED YELLOW HYDRAULIC SYSTEM RT ELEVATOR SERVO VALVE AFTER FINDING OSCILLATIONS TO BE OUT OF LIMITS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032200121 20070322 00121 EU 2007 3 22 2007UALA00786 1 20070316 A 5100 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE VIBRATION A UALA O OTHER E VIBRATION/BUFFET CR CRUISE 1 WP 29 446UA 834 HIGH FREQUENCY VIBRATION STARTED 23,500- 330 KNOTS WENT AWAY 24,500-300 KNOTS RETURNED AGAIN 25,000-315 KNOTS AND STOPP ED 30,500-290 KNOTS .76 MACH. VIBRATION VERY NOTICEABLE THROUGHOUT CABIN. FLT CONTROLS SEEMED OK. CREW REPORTED UP & DOWN OSCILLATION THROUGHOUT AC. [SUP 06-01-07] PERFORMED ELEVATOR FREEPLAY AND OSCILLATION CHECKS. RT ELEVATOR SERVO V ALVE FAILED OSCILLATION TEST AND WAS REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032200122 20070322 00122 NM 2007 3 22 UPS07449466 1 20070211 A 5311 FRAME BOEING 747 747121 1384871 NM BS 780 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT BS 780 FRAME TENSION TIE ATTACHMENT AREA AT FASTENER HOLE NR 1 AND NR 9 BOTH FOUND CRACK AT FAIL SAFE CHORD AT 5:00 O/C POSITION. APPROX .0625 & .125 INCH LONG. M/D BS 780 RIGHT FRAME BELOW STR 11R FAILSAFE CHORD RE PLACED AS PER RS R53-25-35745 AND UPS EO B747-5310-26128. 2 L 7 4 4F A20WE 2007032200123 20070322 00123 EU 2007 3 22 2007UALA00788 1 20070315 A 2910 HYDRAULIC SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN SYSTEM READS LOW A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 412UA 465 GREEN HYDRAULIC LOW LEVEL QTY ECAM ON FINAL. PRESSURE STILL GOOD ON GREEN SYSTEM. EMERGENCY DECLARED. AMBER ALERT. [SUP 06-01-07] PERFORMED A LEAK CHECK WITH ELECTRIC AND ENGINE DRIVEN PUMPS OPERATING AND DID NOT FIND ANY LEAKS. 2 DAY S PRIOR, NR 2 ENGINE DRIVEN PUMP WAS REPLACED. IT WAS ALSO NOTED AS PART OF THE SAME MAINTENANCE ACTIVITY THAT THE YELLO W AND GREEN SYSTEMS WERE OVER SERVICED AND WERE SLIGHTLY DRAINED TO BRING LEVELS WITHIN NORMAL SPECS. SUSPECT THAT TOO M UCH FLUID WAS DRAINED AND/OR DID NOT ACCOUNT FOR NEW EDP NOT BEING FULL OF FLUID YET. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032200153 20070322 00153 NM 2007 3 22 ABXA070073 1 20070318 A 3610 FLANGE BOEING 767 767232 1385132 NM LT ENGINE LOOSE A ABXA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 GL 23 740AX 22213 ON CLIMBOUT, EICAS MESSAGE LEFT ENGINE OVERHEAT DISPLAYED WITH ENGINE OVERHEAT LIGHT ILLUMINATED. LIGHT REMAINED ILLUMI NATED AFTER THRUST REDUCTION. ENGINE WAS SHUTDOWN. DID AIR TURNBACK TO STA SAL. OPENED NR 1 ENGINE COWL, INSPECTED BL EED AIR DUCTING. FOUND LOOSE DUCT FLANGE NEAR TURBINE LOOSE. TIGHTENED FLANGE HARDWARE. RUN-UP NR 1 ENGINE TO 60 - 80 PERCENT N2 LIGHTS AND EICAS MESSAGE REMAINED OUT. ALSO REPLACED FIRE DETECTION CARD IAW DC9 MM 26-10-01. OVERHEAT LOO PS 1 & 2 SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2007032200154 20070322 00154 NM 2007 3 22 UPS07449492 1 20070228 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD COVER CORNER 1EA FASTENER HOLE (IDENT B) FOUND CRACKED AT BEAR STRAP .0 625 INCH TO FWD AT 5 O/C POSITION (LOOKING I/B). CRACK LENGTH .0625 INCH. RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS R53-41-35782. WORK DETAIL REFER NRC 51916 AND UPS EO B747-5330-15047-A. 2 L 7 4 4F A20WE 2007032200155 20070322 00155 EU 2007 3 22 USAA070230 1 20070320 A 5315 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 172US 1472 Y-1732 BETWEEN FR 65 & 66 CORRODED. CUT OUT DAMAGE, INSTALLED REPAIR ANGLES & FILLER PER SRM 53-41-14; CORR TASK JA-260 -53500; LEVEL 1, DEFECT SIZE: 1 INCH DIA. 2 L 7 2 4F RT A28NM 2007032200156 20070322 00156 NM 2007 3 22 UPS07449493 1 20070228 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER 1EA FASTENER HOLE (IDENT E) FOUND CRACKED AT SKIN AND BEAR STRAP .125 INCH TO UPWARD AT 12 O/C POSITION (LOOKING I/B). RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS R53-41-35782. WORK DETAIL REFER NRC51976 AND UPS EO B747-5330-15047-A. 2 L 7 4 4F A20WE 2007032200157 20070322 00157 NM 2007 3 22 UPS07449494 1 20070228 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER 1E FASTENER HOLE (IDENT F) FOUND CRACKED AT BEAR STRAP .12 5 INCH APPROX RUNNING UPWARD AT 12 O/C POSITION (LOOKING I/B). CRACK LENGTH .125 INCH. RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS R53-41-35782. WORK DETAIL REFER NRC 51976 AND UPS EO B747-5330-1504 7. 2 L 7 4 4F A20WE 2007032200158 20070322 00158 NM 2007 3 22 UPS07449495 1 20070228 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER 1EA FASTENER HOLE (IDENT D) FOUND CRACKED AT SKIN .125 INC H APPROX RUNNING FWD AT 5 O/C POSITION (LOOKING I/B). RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP R EPAIRED AS PER RS R53-41-35782. WORK DETAIL REFER NRC 51976 AND UPS EO B747-5330-15047. 2 L 7 4 4F A20WE 2007032200159 20070322 00159 NM 2007 3 22 UPS07449496 1 20070228 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER 1EA FASTENER HOLE (IDENT G) FOUND CRACKED AT BEAR STRAP .1 25 INCH TO UPWARD AT 11 O/C POSITION (LOOKING I/B). RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REP AIRED AS PER RS R53-41-35782. WORK DETAIL REFER NRC51976 AND UPS EO B747-5330-15047. 2 L 7 4 4F A20WE 2007032200160 20070322 00160 NM 2007 3 22 UPS07449497 1 20070228 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER 1EA FASTENER HOLE (IDENT H) FOUND THROUGH THICKNESS CRACKE D AT 7 O/C POSITION AND .0625 INCH CRACKED TO FWD AT BOTTOM OF HOLES BORE AT 5 O/C POSITION (LOOKING I/B). RIGHT NR 3 P AX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS R53-41-35782. WORK DETAIL REFER NRC51976 AND UPS EO B747-5330-15047. 2 L 7 4 4F A20WE 2007032200161 20070322 00161 EU 2007 3 22 USAA070229 1 20070320 A 5315 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 172US 1472 Y1732 FR 66 - FR 65, CORROSION AROUND SCREW HOLE CORRODED. CUT OUT DAMAGE & INSTALLED REPAIR ANGLES & FILLER PER SRM 53 -41-14; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1 INCH DIA. 2 L 7 2 4F RT A28NM 2007032200162 20070322 00162 CE 2007 3 22 DXTA200702038 1 20070320 A 3150 WARNING LIGHT CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE INOPERATIVE E DXTA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 GL 07 603QS 5605203 NO TAKEOFF LIGHT ILLUMINATED ON TAKEOFF ROLL. FLAPS, TRIM AND SPEEDBRAKES WERE ALL VERIFIED IN CORRECT POSITION, ABORTED TAKEOFF. (SUPPLEMENTAL 23 MARCH 07) FOUND DURING OP'S CHECK NO TAKEOFF LIGHT WOULD ILLUMINATE BY JUST BUMPING ELEVATO R TRIM WHEEL, REMOVED ELEVATOR TRIM WHEEL AND FOUND EXCESSIVE GREASE AND BALL OF LINT ON TRIM POINTER PROX SWITCH CAUSIN G INTERMITTEN NO TAKEOFF LIGHT TO ILLUMINATE CLEANED IAW CE560XL MM. CH 27-31-00 AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007032200167 20070322 00167 EA 2007 3 22 VNAA0702013 1 20070223 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS INOPERATIVE A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 05 250PS 7929 CREW REPORTED A FLAP FAIL MESSAGE DISPLAYED AFTER TAKEOFF. CREW ELECTED TO CONTINUE FLIGHT AND LAND IN CLT WITHOUT INCI DENT. MAINTENANCE INSPECTED AND CYCLED CIRCUIT BREAKERS IN ACCORDANCE WITH THE AIRCRAFT SERVICE LETTER. AIRCRAFT WAS R ELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007032200168 20070322 00168 EA 2007 3 22 VNAA0702014 1 20070226 A 3000 5399001 ANTI-ICE VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 NACELLE FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 206PS 443 7860 CREW REPORTED A NR 2 COWL ANTI-ICE CAS MESSAGE AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT . MAINTENANCE REMOVED AND REPLACED THE NR 2 ANTI-ICING VALVE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCR AFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007032200169 20070322 00169 EA 2007 3 22 VNAA0703001 1 20070304 A 3310 2LA00691307 LIGHT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE CABIN SHORTED A VNAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 05 702PS 10135 CREW REPORTED THE PANEL FLOODLIGHT SHORTED/SMOKED AND POPPED THE CIRCUIT BREAKER AFTER TAKEFOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE COCKPIT FLOODLIGHT IN ACCORDANCE WITH THE AIR CRAFT MAINTENANCE MANUAL. MAINTENANCE ALSO REPLACED THE FLOOD POTENTIOMETER IN ACCORDANCE WITH THE CMM 33-12-16. AIRCR AFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007032300002 20070323 00002 CE 2007 3 23 DXTA200702031 1 20070316 A 3220 UNKNOWN CESSNA 750 750 2076810 CE NLG NOISY E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 901QS 7500102 NOSEGEAR MAKES OCCASIONAL BUMPING NOISE IN FLIGHT.COMPLIED WITH GEAR BUMP TROUBLESHOOTING PER C750 MM 32-30-00. ALL CLE ARANCES AND OPERATIONAL CHECKS TEST GOOD. 2 L 7 2 4J RT T00007WI 2007032300004 20070323 00004 CE 2007 3 23 DXTA200702040 1 20070321 A 2120 UNKNOWN BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE CABIN ODOR E DXTA G O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 161QS RK435 UNIDENTIFIED ENVIROMENTAL SYSTEM ODOR BEGAN ENTERING THE CABIN PASSING 7000 FT WITH THE THROTTLES NEAR IDLE IN DESCENT. VISUALLY INSPECTED RT AND LT ENGINE INTAKE AND EXHAUST, NO DISCREPANCIES WERE NOTED. GAINED ACCESS TO THE REFRIGERATION UNIT AND VISUALLY INSPECTED, NO DISCREPANCIES WERE NOTED. OPERATED LT AND RT ENGINES AND ACCOMPLISHED REFRIGERATION UNI T OPERATIONAL CHECK TWO SEPARATE TIMES AT 1/2 HOUR EACH, SWITCHED PRESSURE SOURCE FROM LT RNGINE TO RT ENGINE AND NO UNU SUAL ODERS WERE NOTED IN THE COCKPIT OR CABIN. OPERATIONAL CHECK WAS FOUND TO BE SATISFACTORY. NO DISCREPANCY WAS NOTED AT THIS TIME. REINSTALLED REMOVED PANELS TO GAIN ACCESS. ACCOMPLISHED IAW HAWKER 400XP MM 21-50-00. 2 H 7 2 4F 4 F RT A16SW E25EA 2007032300005 20070323 00005 CE 2007 3 23 DXTA200702041 1 20070321 A 2170 COALESCER BAG CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CABIN AIR ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 943QS 7500043 EXTREME CABIN ODOR WHEN BLEED AIR TURNED ON. REMOVED BOTH COALESCER SOCKS & INSTALLED 2 NEW SOCKS. RAN APU & BOTH ENGIN ES SEPERATELY & TOGETHER, W/ BLEED AIR, NO ODOR PRESANT THROUGHOUT A/C. WORK PERFORMED IAW CE-750 MM CHPT. 21-30-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007032300006 20070323 00006 NM 2007 3 23 QXEA200700376 1 20070315 A 6120 78249050 PCU DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 2 ENGINE MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 352PH 303 494 SEA FLIGHT NR 2092 AUTOFEATHER ARMED LIGHT DID NOT ILLUMINATE UNTIL ABOUT 80 PERCENT TORQUE ON TAKEOFF ROLL. AFTER ARMI NG LIGHT EXTINGUISHED AT APPROXIMATELY 80 KTS, MAINTENANCE REPLACED NR 2 ENGINE PCU. GROUND RUNS AND OPERATIONAL CHECK G OOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007032300007 20070323 00007 SO 2007 3 23 SIMA200707808 1 20070311 A 5320 14525480603 SILL EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 849AE 9413 4800 145716 CARGO DOOR LOWER SILL CORRODED. REMOVED AND REPLACED CARGO LOWER SILL IAW EMB SRM 51-40-03. RETURN AIRCRAFT TO SERVICE . 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007032300008 20070323 00008 SO 2007 3 23 SIMA200707806 1 20070318 A 5347 14530659011 SEAT TRACK EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 652RS 13322 4800 145432 LT FWD IB SEAT TRACK CORRODED FROM FRAME 17 TO 24. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCR AFT TO SERVICE 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007032300009 20070323 00009 SO 2007 3 23 SIMA200707810 1 20070314 A 5315 14521413605 FLOORBEAM EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 849AE 9413 4800 145716 CENTER OMEGA BEAM WAS FOUND CORRODED AT FRAME 25. PERFORMED CUTOUT TO REMOVE CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007032300010 20070323 00010 SO 2007 3 23 SIMA200707807 1 20070318 A 5320 14521725025 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 652RS 13322 4800 145432 AFT SERVICE DOOR SILL CORRODED. REPAIRED DOOR SILL BY CUTTING OUT DAMAGE AND INSTALLED DOUBLER IAW SRM 53-21-10. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007032300011 20070323 00011 SO 2007 3 23 SIMA200707809 1 20070314 A 5315 14521700007 FLOORBEAM EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 849AE 9413 4800 145716 LT OMEGA BEAM CORRODED AT FRAME 27. PERFORMED A CUTOUT TO REMOVE CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW I C2007-145/01665, DATED 03-08-07. RETURNED AIRCRAFT TO SERVICE 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007032300012 20070323 00012 NM 2007 3 23 SWAA071469 1 20070321 A 3350 101073 LENS BOEING 737 7373K2 13844BA NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED C2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007032300013 20070323 00013 NM 2007 3 23 SWAA071495 1 20070321 A 3350 10107451 SIGN BOEING 737 7373TO 138447G NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED C1 CHECK, FOUND FWD CABIN EMERGENCY EXIT SIGN LENS CRACKED. REMOVED AND REPLACED EMERGENCY EXIT SIGN P ER MM. 2 L 7 2 4F RT A16WE 2007032300014 20070323 00014 NM 2007 3 23 SWAA071474 1 20070321 A 3350 101331 LENS BOEING 737 7373T0 1384582 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED HC1 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007032300015 20070323 00015 NM 2007 3 23 SWAA071492 1 20070321 A 3350 101331 LENS BOEING 737 7375H4 138449D NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED MV1 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007032300016 20070323 00016 NM 2007 3 23 SWAA071501 1 20070321 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007032300017 20070323 00017 NM 2007 3 23 SWAA071498 1 20070321 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 706SW 27840 DURING SCHEDULED MV2 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007032300018 20070323 00018 NM 2007 3 23 SWAA071497 1 20070321 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 210WN 34162 DURING SCHEDULED HC1 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007032300021 20070323 00021 NM 2007 3 23 SWAA071489 1 20070321 A 5312 6517582 VERTICAL BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED 10Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 184, RBL 17.1. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007032000051 20070320 00051 NM 2007 3 20 SWAA071396 1 20070314 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 727E S18R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 18R. REPAIRED SKIN PER SRM & EA. 2 L 7 2 4F RT A16WE 2007032000058 20070320 00058 NM 2007 3 20 SWAA071388 1 20070314 A 5330 6547952 SKIN BOEING 737 7373Q8 1384670 NM BS 303 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 303.9, WL 259.88 NEXT TO L1 DOOR UPPER HINGE CUTOUT. REPA IRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007032000064 20070320 00064 NM 2007 3 20 PIDA07011 1 20070305 A 5754 114N40003111 SKIN BOEING 757 757236 1384971 NM NR 2 SLAT CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 757BJ 22176 DURING INSPECTION FOUND THE LEFT WING NR 2 SLAT LOWER SURFACE HAS CORROSION 46 INCHES FROM THE INBOARD END. REPAIRED AR EA PER EA 57-032. 2 L 7 2 4F RT A2NM 2007032000089 20070320 00089 2007 3 20 2007UALA00686 4 20070305 A 2200 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE AUTOPILOT UNKNOWN A UALA O OTHER O OTHER CL CLIMB 1 WP 29 534UA 25129 IN CLIMB CENTER A-P DISCONNECTED FOUND C/B E21 POPPED. FLIGHT CONTROL COMPUTER SERVO CENTER. [SUP 05-18-07] FOUND CEN TER FCC WITH INTERNAL FAILURE FOR OUTPUT TO SOCKET 18 POWER TO CENTER LATERAL CONTROL SERVO . REPLACED A-P CENTER LATER AL CONTROL SERVO AFTER CONFIRMING IT WAS THE CAUSE OF THE C-B TRIP. ALSO REPLACED CENTER FCC AND ACCOMPLISHED MCDP TEST 07 NUMEROUS TIMES WITH NO FAULTS OR ELECTRICAL SMELL OR C-B TRIPS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032000098 20070320 00098 CE 2007 3 20 DXTA200702029 1 20070316 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE MLG INOPERATIVE E DXTA O OTHER O OTHER LD LANDING 1 GL 07 801QS 5600601 LOST BRAKE PRESSURE DURING LANDING ROLL. CONFIRMED N2 PRESSURE AT BOTH PILOT STATIONS. USED EMER PRESS LEVER TO STOP. 2 L 7 2 4F 4 F RT A22CE E00053EN 2007032100067 20070321 00067 NM 2007 3 21 ASAA0711531 1 20070313 A 3350 1104461 MODULE BOEING 737 737290C 138448V NM EMERGENCY LIGHTS INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 742AS 23136 L1, R1 AND HATCH COVER EMERGENCY EXIT MARKER LIGHTS OUT. REPLACED MODULE M7331. OPS NORMAL. 2 L 7 2 4F A16WE 2007032100068 20070321 00068 NM 2007 3 21 ASAA0741532 1 20070315 A 5210 69169542 PLATE BOEING 737 7374Q8 138447Q NM L1 DOOR WRONG PART A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 FLIGHT ATTENDANT REPORTED L1 DOOR HARD TO OPEN FOUND INCORRECT BEARING PLATE INSTALLED WHICH APPEARED TO BE CATCHING ON DOOR DURING LAST 1 INCH OF DOOR CLOSING. AFTER REPLACING PLATE FOUND THE UPPER TORQUE ROD CONTROL LEVER ROLLER NOT ENGA GING CAM AT DOOR HANDLE. RIGGED DOOR, CHECKS GOOD. 2 L 7 2 4F RT A16WE 2007032100122 20070321 00122 NM 2007 3 21 USAA070217 1 20070315 A 5313 STRINGER BOEING 737 737401 1384701 NM BS 300 S14L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 STRINGER CHANNEL AT STA 360 AT S14L HAS CRACK. REMOVED STRINGER CHANNEL, TREATED, PRIMED & INSTALLED PER SRM 51-10-02; 51-40-43, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007032100123 20070321 00123 NM 2007 3 21 USAA070218 1 20070315 A 5311 FRAME BOEING 737 737401 1384701 NM BS 727B S8-9R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 BS 727B BETWEEN STRINGERS 8R & 9R AT RAIL ATTACH POINT CRACKED. REMOVED DAMAGE & INSTALLED FAB'D REPAIR PARTS PER T/R 5 3-10-20E, DEFECT SIZE: .250 INCH. 2 L 7 2 4F RT A16WE 2007032100125 20070321 00125 NM 2007 3 21 USAA070219 1 20070315 A 5347 69773083 MOUNT BOEING 737 737401 1384701 NM BS 947 S17R CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 STA 947 S-17R JUST FWD OF R-2 DOOR, ON AFT LAV MOUNT HAS CORROSION. REPLACED MOUNT WITH NEW ONE & SECURED BEAM PER SRM 51-10-02; CORR TASK C53-107-02; LEVEL 2, DEFECT SIZE: LESS THAN 1 INCH. 2 L 7 2 4F RT A16WE 2007032100126 20070321 00126 NM 2007 3 21 USAA070205 1 20070315 A 5347 SEAT TRACK BOEING 737 737401 1384701 NM BS 727B-727C CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 BETWEEN BS 727B & 727C, RBL 24.75 HAS CRACK. FABRICATED & INSTALLED NEW TRACK SECTION & SPLICE REPAIR PER SRM 53-00-52- 2R-3 FIG 201, REPAIR 3, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007032100127 20070321 00127 GL 2007 3 21 C2XA07CL030 2 20070312 A 7261 CARBON SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 ENGINE LEAKING A C2XA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 27 15973 145159 CAE311984 EWR FLIGHT 3068 THE CREW REPORTED A LAV SMOKE INDICATION AFTER TAKEOFF. THE AIRCRAFT RETURNED TO EWR AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND RAN BOTH ENGINES. THE NR 1 ENGINE WAS FOUND TO BE THE CAUSE OF THE LAV IN DICATION AND SMOKEY ODOR. THE NR 1 ENGINE WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE ROOT CAUSE OF THE HAZE IN THE CABIN WAS THE NR 4 CARBON SEAL.THE SEGMENTS AND THE TEFLON SEAL NO LONGER RETAINED OIL FROM SEEPING OUT TO THE TIP OF THE FRONT SUMP HOUSING AND INTO THE HP COMPRESSOR"S AIR STREAM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007032100149 20070321 00149 NM 2007 3 21 KCSA071069 1 20070320 A 5412 BULKHEAD BOEING 747 747246F 1384850 NM NR 3 NACELLE CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 NR 3 PYLON HAS HYD PRESSURE LINE FITTING CHAFED THROUGH NAC STA 221.9 BULKHEAD WEB. 2 L 7 4 4F RT A20WE 2007032100150 20070321 00150 NM 2007 3 21 KCSA071067 1 20070316 A 5347 SEAT TRACK BOEING 747 747236B 1384804 NM BS 1600 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 MAIN DECK SEAT TRACK IS DAMAGED AT STA 1600, RBL 65. 2 L 7 4 4F A20WE 2007032100151 20070321 00151 NM 2007 3 21 KCSA071065 1 20070315 A 5315 FLOORBEAM BOEING 747 747236B 1384804 NM BS 180 PUNCTURED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 MAIN DECK FLOORBEAM WEB IS PUNCTURED AT STA 180, LBL 49, WL 195. 2 L 7 4 4F A20WE 2007032100152 20070321 00152 WP 2007 3 21 MWEA070043 1 20070314 A 3397 0200413003 GROUND WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 809ME 48071 OVERHEAD EMERGENCY LIGHT, ROW 9 IS INOPERATIVE. REPAIRED GROUND WIRE AT LIGHT SOCKET. 2 L 7 2 4F A6WE 2007032200003 20070322 00003 CE 2007 3 22 DXTA200702035 1 20070318 A 2810 FLAPPER VALVE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CENTER TANK OBSTRUCTED E DXTA A UNSCHED LANDING C K J F.O.D. FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 07 912QS 7500012 5 MINUTES AFTER LEVEL OFF, AMBER (WING TANK O'FULL - L) CAS ILLUMINATED. FUEL WAS OBSERVED VENTING OUT OF LT WING TANK. FUEL IN MAIN TANKS 3250 EACH, CENTER TANK EMPTY. AFTER SEVERAL BANK AND YAW MANEUVERS, VENTING CONTINUED. AFTER A 18 0 DEGREE LT TURN, VENTING SLOWED. STARTED DESCENT, VENTING STOPPED. (SUPPLEMENTAL 23 MARCH 07) INSPECTED LT WING OUTER FUEL VENT SYSTEM AND FOUND SURGE TANK DRAIN LINE FLAPPER VALVE WITH DEBRIS STUCK IN FLAPPER, CLEANED FLAPPER AND VISUAL LY INSPECTED VENT FLOAT VALVE, PLUMBING AND TANK AREA. NO OTHER DEFECTS NOTED. ALL WORK DONE IAW 750 MM 28-10-04. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007032200004 20070322 00004 CE 2007 3 22 DXTA200702036 1 20070318 A 3210 UNKNOWN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG UNKNOWN E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 311QS 5600311 UPON DEPARTURE AND GEAR RETRACTION THE GEAR UNSAFE LIGHT ILLUMINATED ON AND HYD PRESS LIGHT ILLUMINATED. WITH ACCELERATI ON NOISE INCREASED ABNORMALLY, AS IF ONE OR MORE GEAR REMAINED DOWN. REMOVED LT MAIN GEAR ACTUATOR & INSTALLED A RENTAL ACTUATOR THAT WAS INSPECTED BY CESSNA AIRCRAFT COMPANY CRS CNQR18C IAW 560 M.M. CHAP. 32-31-04. 2 L 7 2 4F 4 F RT A22CE E25EA 2007032200023 20070322 00023 NM 2007 3 22 CALA0700131 1 20070316 A 5330 65C337556 SKIN BOEING 737 7373T0 1384582 NM BS 328 S17R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 77303 23354 INSPECTION FOUND A 1.5 INCH CRACK IN R-1 DOOR CUTOUT LOWER AFT CORNER, STA 328, S17R. REPAIR DOUBLERS AND FILLERS WERE INSTALLED IAW SRM 53-10-01. 2 L 7 2 4F RT A16WE 2007032200055 20070322 00055 EA 2007 3 22 COMA0760263 1 20070317 A 3230 46193 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 932CA 31105 7038 FLIGHT 4992 - NOSE GEAR DISAGREE. REMOVED AND REPLACED MLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2007032200069 20070322 00069 NM 2007 3 22 2007UALA00729 1 20070309 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 WALL EEL INOP BETWEEN MID LAVS. REPLACED LAMP, EEL OP CHECKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032200077 20070322 00077 NM 2007 3 22 2007UALA00733 1 20070309 A 2597 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 526UA 24994 EMERGENCY ESCAPE SQUIB TEST INOP, RIGHT SQUIB TEST POSN TWO. [SUP 05-22-07] CLEANED CONNECTOR. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032200078 20070322 00078 2007 3 22 2007UALA00734 4 20070308 A 2565 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 3L LACK OF LUBE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 569UA 26677 THE 3L DOOR WILL NOT DISARM. [SUP 05-18-07] LUBED GIRT BAR, OP'S CHECKED NORMAL ON GROUND. FOUND WATER UNDER GIRT BAR AREA INDICATING POSSIBLE ICE BUILD-UP IN THE AREA. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032200079 20070322 00079 EU 2007 3 22 2007UALA00735 1 20070310 A 3350 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 473UA 1469 OVERWING EXIT LIGHT IN CEILING AND LEFT OVERWING EXIT LIGHT ON SIDEWALL FLICKER WITH SWITCH IN OFF-ON-ARMED POSITIONS. REPLACED EMERGENCY LIGHT BATTERY ON LEFT SIDE OVERWING. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032200080 20070322 00080 NM 2007 3 22 2007UALA00736 1 20070310 A 3350 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 812UA 850 EPSU EMERGENCY LEFT FAULTING TEST. REPLACED EPSU. OP CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032200082 20070322 00082 NM 2007 3 22 ASMF200703005 1 20070312 A 4920 38003681 APU DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE APU BAY FAILED W ASMF A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 23 169PL 10506 53175 AIRCRAFT RETURNED DUE TO FUEL ODOR IN THE CABIN AT 28,000 FEET. THE UPPER AND LOWER WING PANELS AND APU WERE CHECKED AND NO LEAKS WERE DETECTED. NEVERTHELESS, THE AIR CONDITIONING WATER SEPARATORS AND ENGINES WERE CHECKED BY CONDITION AND L EAKS AND NO ODOR NEITHER LEAKS WERE DETECTED, THEREFORE AIRCRAFT WAS DISPATCHED. OVERWEIGHT INSPECTION WAS NOT NECESSARY DUE TO AIRCRAFT LANDED WITH 123,300 POUNDS AND MAXIMUM LANDING WEIGHT IS 139,500 POUNDS. DURING OVERNIGHT CHECK, THE FU EL AND OIL ODOR CONTINUED WITH AIR CONDITIONING SUPPLIED BY APU. AIR CONDITIONING WATER SEPARATORS, APU FUEL HEATER AND APU WERE REPLACED IAW MM 21-20-02, 49-31-01 AND 49-10-00 TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007032200084 20070322 00084 NM 2007 3 22 CALA0700133 1 20070317 A 5320 147A5506 STRUCTURE BOEING 737 737824 13844BZ NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17245 28955 INSPECTION FOUND STRUCTURE CORRODED AT STA 986.6, LBL 42. A REPAIR STRAP WAS INSTALLED ALONG WITH REQUIRED NUT PLATES I AW ECRA 5310-01459. 2 L 7 2 4F RT A16WE 2007032200085 20070322 00085 NM 2007 3 22 CALA0700134 1 20070320 A 3350 ADD71701100 BATTERY PACK BOEING 737 737724 13844BY NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23708 28769 THE LEFT OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE DURING TEST. THE LEFT OVERWING BATTERY PACK WAS REPLACED IA W MM 33-51-06-960-804. 2 L 7 2 4F RT A16WE 2007032200086 20070322 00086 NM 2007 3 22 CALA0700135 1 20070319 A 5330 6555074 SKIN BOEING 737 7373T0 1384582 NM BS 211-219 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 77303 23354 INSPECTION FOUND A 0.75 INCH CRACK AT UPPER O/B CORNER OF FLIGHT COMPARTMENT L-1 WINDSHIELD CUTOUT, STA 211.8-219.8, S5L . A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-10-01, FIGURE 201. 2 L 7 2 4F RT A16WE 2007032200087 20070322 00087 NM 2007 3 22 CALA0700136 1 20070319 A 5330 6545775 SKIN BOEING 737 7373T0 1384582 NM BS 765 S21R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 77303 23354 INSPECTION FOUND A 1.7 INCH CRACK IN FUSELAGE SKIN AT STA 765, S21R. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-00-01. 2 L 7 2 4F RT A16WE 2007032200090 20070322 00090 WP 2007 3 22 WX0A070069 1 20070315 A 2700 FLT CONTROLS DOUG DC9 DC983 3022083 WP UNKNOWN A WX0A O OTHER F FLT CONT AFFECTED DE DESCENT 1 WP 19 863GA 49911 FLIGHT 461 PIA/LAS. THE FLIGHT CREW REPORT, INFLIGHT AP DISCONNECT DUE TO ROLL CONTROL (YOKE) STUCK DISCOVERED ROLL CON TROL TRIM STUCK (UNTIL 1000 FT AGL LAST CHECK OF THIS FUNCTION. UPON LANDING AFTER TOUCHDOWN, FULL RIGHT AILERON CONTRO L WAS MADE WITH LEFT ROLL TENDENCY UNTIL AUTO SPOILERS STOWED. THE AIRPLANE LANDED WITHOUT FURTHER INCIDENT. MAINTENAN CE REPORT OPENING THE LEFT AND RIGHT WING AFT SPAR ACCESS PANELS TO INSPECT THE LEFT AND RIGHT AILERONS, CONTROL TABS AN D TRIM TABS CABLES, PULLEYS, HINGES, ETC FOR WEAR, FRAYING OR BINDING. NO DEFECTS FOUND, CLOSED ACCESS PANELS. INSPECT ED LEFT AND RIGHT WHEEL WELL AREAS FOR EVIDENCE OF CONTROL TAB OR TRIM TAB CABLE OR PULLEY DAMAGE OR BINDING. NO DEFECT 2 L 7 2 4F RT A6WE 2007032200124 20070322 00124 NM 2007 3 22 2007UALA00789 1 20070315 A 5310 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 THE 2L MED UPPER HINGE FRAME CUTOUT LWR RADIUS CRACKED. MAJOR REPAIR ACCOMPLISHED: COMPLETED A DOUBLER REPAIR ACCORDI NG TO A BOEING APPROVED REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032200125 20070322 00125 NM 2007 3 22 2007UALA00790 1 20070315 A 2121 BEARING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RECIRC FAN FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 341UA 24245 RECIRC FAN ABOVE 7 IS GRINDING & HAS A BURNING ODOR. [SUP 05-29-07] RECIRCULATION FAN INOP. REPLACED RECIRCULATION FA N AND FILTER. UNIT HAD BAD BEARINGS. REPLACED BEARING AND BALANCED ROTOR AND IMPELLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032200126 20070322 00126 EU 2007 3 22 2007UALA00791 1 20070316 A 2420 IDG AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 LEAKING A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 401UA 435 RTFL DUE TO A IDG LOW OIL PRESSURE PROBLEM. [SUP 06-01-07] REPLACED NR 1 IDG. AT OVERHAUL, FOUND A LEAKING SEAL THAT W AS ALLOWING FLUID TO ESCAPE THE SYSTEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032200127 20070322 00127 NM 2007 3 22 2007UALA00792 1 20070312 A 5751 65B022496 WEDGE BOEING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RT WING AILERON DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 104UA 000440 26902 HAIL DAMAGE TO T/E WEDGE UPPER SKIN OF T/E DAMAGED. T/E REPAIRED. T/E WEDGE REMOVED FOR REPAIR AND REINSTALLED. UPPER SKIN FWD OF T/E SEAM DAMAGED. SEAM DAMAGE REPAIRED. AIRCRAFT READY FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032200128 20070322 00128 NM 2007 3 22 UPS07449467 1 20070227 A 5311 FRAME BOEING 747 747121 1384871 NM BS 820 S11-12R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 820 STR 11-12R FRAME FOUND CRACK. CRACK LENGTH .875 - 1 INCH. M/D BS 820 STR 11-12R FRAME REP AIRED AS PER RS R53-12-35770. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-12-35770 AND UPS EO B747-5310-26322. 2 L 7 4 4F A20WE 2007032200129 20070322 00129 NM 2007 3 22 UPS07449468 1 20070211 A 5320 PLATE BOEING 747 747121 1384871 NM BS780 MISMANUFACTURED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 780 LEFT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 780 LEFT TENSION TIE ATT STEEL PLATE REPAIRED AS PER RS R53-25-35745. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35745 AND UPS EO B747-531 0-26128. 2 L 7 4 4F A20WE 2007032200130 20070322 00130 NM 2007 3 22 UPS07449469 1 20070211 A 5311 FRAME BOEING 747 747121 1384871 NM BS 820 S8-11R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT BS 820 FRAME TENSION TIE ATTACHMENT AREA AT FASTENER HOLE NR 10 CRACK AT FRAME LAYER RUNNING LOW ER APPROX .0625 IN LENGTH. RIGHT BS 820 FRAME REPAIRED AT BETWEEN STR 8R AND STR 11.5R AS PER RS R53-25-35751 AND UPS E O B747-5310-26129. 2 L 7 4 4F A20WE 2007032200131 20070322 00131 NM 2007 3 22 UPS07449470 1 20070211 A 5320 PLATE BOEING 747 747121 1384871 NM BS 820 MISMANUFACTURED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 820 LEFT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 820 LEFT TENSION TIE ATT STEEL PLATE REPAIRED AS PER RS R53-25-35751. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35751 AND UPS EO B747-531 0-26129. 2 L 7 4 4F A20WE 2007032200132 20070322 00132 NM 2007 3 22 UPS07449471 1 20070211 A 5320 PLATE BOEING 747 747121 1384871 NM BS 860 MISMANUFACTURED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 860 LEFT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 860 LEFT TENSION TIE ATT STEEL PLATE REPAIRED AS PER RS R53-25-35746. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35746 AND UPS EO B747-531 0-26132. 2 L 7 4 4F A20WE 2007032200133 20070322 00133 NM 2007 3 22 UPS07449472 1 20070211 A 5320 PLATE BOEING 747 747121 1384871 NM BS 800 MISMANUFACTURED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 800 LEFT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 800 LEFT TENSION TIE ATT STEEL PLATE REPAIRED AS PER RS R53-25-35755. CONTINUE INSPECTION IS REQUIRED PER RS R53-35-35755 AND UPS EO B747-5310-1 4973. 2 L 7 4 4F A20WE 2007032200134 20070322 00134 NM 2007 3 22 UPS07449473 1 20070211 A 5320 PLATE BOEING 747 747121 1384871 NM BS 880 MISMANUFACTURED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 880 LEFT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 880 LEFT TENSION TIE ATT STEEL PLATE REPAIRED AS PER RS R53-25-35752. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35752 AND UPS EO B747-531 0-26133. 2 L 7 4 4F A20WE 2007032200135 20070322 00135 NM 2007 3 22 UPS07449474 1 20070211 A 5320 PLATE BOEING 747 747121 1384871 NM BS 920 MISMANUFACTURED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 920 LEFT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 920 TENSION TIE ATT STEEL PLATE REPAIRED AS PER RS R53-25-35761. CONTINUE INSPECTION IS REQUIRED AS PER R53-25-35761 AND UPS EO B747-5310-14932. 2 L 7 4 4F A20WE 2007032200136 20070322 00136 NM 2007 3 22 UPS07449475 1 20070211 A 5320 PLATE BOEING 747 747121 1384871 NM BS 780 MISMANUFACTURED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 780 RIGHT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 780 RIGHT TENSION TIE AT T STEEL PLATE REPAIRED AS PER RS R53-25-35745. CONTINUE INSPECTION IS REQUIRED AS PER R53-25-35745 AND UPS EO B747-5310 -26128. 2 L 7 4 4F A20WE 2007032200137 20070322 00137 NM 2007 3 22 UPS07449476 1 20070211 A 5320 PLATE BOEING 747 747121 1384871 NM BS 800 MISMANUFACTURED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 800 RIGHT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 800 RIGHT TENSION TIE AT T STEEL PLATE REPAIRED AS PER RS R53-25-35755. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35755 AND UPS EO B747-5 310-14973. 2 L 7 4 4F A20WE 2007032200138 20070322 00138 NM 2007 3 22 UPS07449477 1 20070211 A 5320 PLATE BOEING 747 747121 1384871 NM BS 860 MISMANUFACTURED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 860 RT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 860 RT TENSION TIE ATT STEE L PLATE REPAIRED AS PER RS R53-25-35746. CONTINUE INSPECTION IS REQUIRED AS PER R53-25-35746 AND UPS EO B747-5310-26132 . 2 L 7 4 4F A20WE 2007032200139 20070322 00139 NM 2007 3 22 UPS07449478 1 20070211 A 5320 PLATE BOEING 747 747121 1384871 NM BS 820 MISMANUFACTURED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 820 RT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 820 RIGHT TENSION TIE ATT S TEEL PLATE REPAIRED AS PER RS R53-25-35751. CONTINUE INSPECTION IS REQUIRED AS PER R53-25-35751 AND UPS EO B747-5310-26 129. 2 L 7 4 4F A20WE 2007032200141 20070322 00141 NM 2007 3 22 UPS07449479 1 20070211 A 5320 PLATE BOEING 747 747121 1384871 NM BS 880 MISMANUFACTURED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 880 RT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 880 RT TENSION TIE ATTACH S TEEL PLATE REPAIRED AS PER RS R53-25-35752. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35752 AND UPS EO B747-5310 -26133. 2 L 7 4 4F A20WE 2007032200142 20070322 00142 NM 2007 3 22 UPS07449480 1 20070211 A 5320 PLATE BOEING 747 747121 1384871 NM BS 920 MISMANUFACTURED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 920 RT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 920 RT TENSION TIE ATT STEE L PLATE REPAIRED AS PER RS R53-25-35761. CONTINUE INSPECTION IS REQUIRED AS PER R53-25-35761 AND UPS EO B747-5310-14932 . 2 L 7 4 4F A20WE 2007032200143 20070322 00143 NM 2007 3 22 UPS07449481 1 20070211 A 5320 PLATE BOEING 747 747121 1384871 NM BS 940 MISMANUFACTURED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 940 RT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 940 RIGHT TENSION TIE ATT S TEEL PLATE REPAIRED AS PER RS R53-25-35756. CONTINUE INSPECTION IS REQUIRED AS PER R53-25-35756 AND UPS EO B747-5310-14 767. 2 L 7 4 4F A20WE 2007032200144 20070322 00144 NM 2007 3 22 UPS07449484 1 20070212 A 5311 FRAME BOEING 747 747121 1384871 NM BS 820 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LT BS 820 TENSION TIE TO FRAME CONNECTION NR 2, 4, 10 AND 13 FASTENER HOLE FOUND CRACK AT WEB RUNNING DOWN THRU THICKNESS. LT BS 820 FRAME WEB REPAIRED AT BETWEEN STR 8L AT STA 11.5L AS PER RS R53-25-35751 AND UPS EO B747 -5310-26129. 2 L 7 4 4F A20WE 2007032200145 20070322 00145 NM 2007 3 22 UPS07449485 1 20070211 A 5730 PANEL BOEING 747 747121 1384871 NM LT WING DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT WING I/B MID FLAP UPPER PANEL 577LT INTERNAL FOUND DELAMINATION. LEFT WING I/B MID FLAP UPPER PA NEL 577LT REPAIRED AS PER RS R57-55-35711 AND US EO B747-5730-15355. 2 L 7 4 4F A20WE 2007032200146 20070322 00146 NM 2007 3 22 UPS07449486 1 20070211 A 5753 PANEL BOEING 747 747121 1384871 NM RT WING TE FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT WING I/B FORE FLAP I/B LWR PANEL FWD AREA FOUND DELAMINATION. RIGHT WING I/B FORE FLAP I/B LWR PANEL REPAIRED AS PER RS R57-55-35769 AND UPS EO B747-5750-26318. 2 L 7 4 4F A20WE 2007032200147 20070322 00147 NM 2007 3 22 UPS07449487 1 20070209 A 5412 FIRESHIELD BOEING 747 747121 1384871 NM NR 2 PYLON DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C DMI D341139 - NR 2 PYLON FIRESHIELD DAMAGED AT NAC STA 261.5 AND STA 275.3. NR 2 PYLON FIRESHIELD REP AIRED AT NAC STA 261.5 TO NAC STA 290.5 AREA AS PER RS R54-54-35772 AND UPS ENGINEERING FILE 747-54-20058. 2 L 7 4 4F A20WE 2007032200148 20070322 00148 NM 2007 3 22 UPS07449488 1 20070301 A 5320 FLOOR SUPPORT BOEING 747 747121 1384871 NM BS 1220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 1220 LBL 98.8 FLOOR WEB SUPPORT FOUND CRACK AS MARKED. CRACK LENGTH .375 INCH. M/D BS 1220 LB L 98.8 FLOOR WEB SUPPORT REPAIRED AS PER RS R53-15-35777 AND UPS ENGINEERING FILE 747-53-20406. 2 L 7 4 4F A20WE 2007032200149 20070322 00149 NM 2007 3 22 UPS07449489 1 20070215 A 5714 SKIN BOEING 747 747121 1384871 NM BS 1210-1220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 1210-1220 LBL 97 WING CTR SECTION TOP SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.043 X .5 X 2 INCHES EXCEED SRM LIMIT. M/D BS 1210-1220 LBL 97 WING CTR SECTION TOP SKIN REPAIRED AS PER RS R57-14-35765 AND UPS EO B747-5730-15819. 2 L 7 4 4F A20WE 2007032200150 20070322 00150 NM 2007 3 22 UPS07449490 1 20070228 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER 1EA FASTENER HOLE (IDENT C) FOUND CRACKED AT BEAR STRAP .0 625 INCH AT 11 O/C POSITION AND ANOTHER CRACK AT SKIN AND BEAR STRAP .0625 INCH AT 5 O/C POSITION (LOCKING I/B). RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER R R53-41-35782. WORK DETAIL REFER NRC51976 AN D UPS EO B747-5330-15047. 2 L 7 4 4F A20WE 2007032200151 20070322 00151 NM 2007 3 22 UPS07449491 1 20070228 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C 1EA FASTENER HOLE (IDENT A) FOUND CRACKED AT RIGHT NR 3 PAX DOOR CUTOUT AREA FWD LOWER CORNER AT SKIN I/B FACE CRACK LENGTH 0.040 INCH APPROX WHICH RUNNING FWD AT 5 O/C POSITION (LOOKING I/B). RIGHT NR 3 PAX DOOR CUTOUT F WD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS R53-41-35782. WORK DETAIL REFER NRC51976 AND UPS EO B747-5330-15 047. 2 L 7 4 4F A20WE 2007032200152 20070322 00152 WP 2007 3 22 070068 1 20070313 A 3350 60030431 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 871GA 53296 DURING A ROUTINE OVERNIGHT SERVICE CHECK MAINTENANCE INSPECTION. MAINTENANCE REPORTED THAT THE EMERGENCY EGRESS PATH LI GHTING FROM ROW 20 TO 24, BOTH FORWARD LEFT AND RIGHT OVERWING ESCAPE HATCH EMERGENCY EXIT SIGNS AND BOTH AFT LEFT AND R IGHT OVERWING ESCAPE HATCH EMERGENCY EXIT SIGNS WOULD NOT TEST. MAINTENANCE FURTHER REPORT THAT A BATTERY PACK AT POSIT ION BS-600S WAS REMOVED AND REPLACED FOR THE EGRESS PATH ISSUE AND THAT A POWER SUPPLY AND BATTERY PACK AT POSITION BS-4 9 WERE REMOVED AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-51-13. THE AIRPLANE HAS RETU RNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007032300019 20070323 00019 2007 3 23 SWAA071465 2 20070320 A 7310 5332A0042 LINE BOEING 737 7373H4 1384600 NM FUEL SYSTEM COLLAPSED A SWAA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 29 619SW 28035 INFLIGHT SHUTDOWN / DIVERSION / DECLARED EMERGENCY. DURING CRUISE AT 34000 FT WITH FUEL TRANSFER FROM NR 1 TANKS, NR 2 FUEL PUMPS OFF/CROSSFEED OPEN, NR 2 ENGINE FLAMED OUT SMOOTHLY. NR 2 ENGINE RESTARTED SUCCESSFULLY PER QRH. INSPECTED FUEL SYSTEM FOUND PARTIALLY COLLAPSED FUEL LINE FROM PYLON TO FUEL PUMP. REMOVED AND REPLACED FUEL LINE PER MM. 2 L 7 2 4F RT A16WE 2007032300020 20070323 00020 NM 2007 3 23 SWAA071490 1 20070321 A 5312 6517582 VERTICAL BEAM BOEING 737 7373H4 1384600 NM BS 184 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED 10Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 184, LBL 17.1. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007032300022 20070323 00022 NM 2007 3 23 QXEA200700368 1 20070310 A 3250 4603000501 CONTROL UNIT BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA NLG STEERING FAULTED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 411QX 6734 4055 FLIGHT NR 2333: DURING ROLL OUT, NOSE STEERING CAUTION ILLUMINATED. DID ABNORMAL CHECKLIST. TAXIED TO GATE. MAINTENANCE CHECK NWS ECU FOR FAULTS AND FOUND FAULTS VDT1, VDT2, SCU, PWR, PHC, P-SW AND SCUT. CLEARED FAULTS. TAXIED AIRCRAFT. NOS EWHEEL STEERING OPERATED NORMALLY. NO CAUTION LIGHTS ILLUMINATED. NO FAULTS RETURNED. REPLACED NOSE WHEEL STEERING ELE CTRONIC CONTROL UNIT FOR PRECAUTIONARY MEASURES IAW MM TASK 32-51-01-000-801 AND 32-51-01-400-801 BECAUSE OF BEING ONLY COMMON LRU TO ALL FAULTS IAW Q400 FIM TASK 32-50-00-810-801 PAR 2A. NOSEWHEEL STEERING SYSTEM OPS TEST GOOD IAW Q400 MM TASK 32-50-00-710-801. TAXIED AIRCRAFT MAKING NUMEROUS LT AND RT TURNS WITH TILLER AND RUDDER PEDALS. NOSE WHEEL STEERIN 2 H 7 2 4T 4 T RT A13NM E00062EN 2007032300023 20070323 00023 NM 2007 3 23 07FDEA01062 1 20070321 A 5311 65453132 FRAME BOEING 727 727200 138407E NM BS 640 S5R DAMAGED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 463FE 22551 MAIN DECK BODY, FRAME WEB AND SHEAR TIE HAVE 2 EA SHORT PITCH (0.25 INCH) MISDRILLED FASTENER HOLES BS 640, STR 5R. REM OVED DAMAGE FROM WEB, FABRICATED AND INSTALLED REPAIR AND NEW SHEAR TIE. TREATED AND PRIMED REPAIR PARTS REF EA 7-5310- 107003. 2 L 7 3 4F RT A3WE 2007032300024 20070323 00024 EU 2007 3 23 07FDEA01063 1 20070321 A 5311 FRAME AIRBUS 300 A300F4605R 3930327 EU BS 1870 S7-9L GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 669FE 774 UPPER FUSELAGE FRAME 28 GOUGED 3 EACH PLACES BETWEEN STR 9L AND STR 7L COMPLIED WITH FEDEX EA 6-5310-105185 TITLE FUSELA GE - MINOR NICKS IN FRAME 28 STRINGER 7L TO 9L REPAIR. BLENDED 3 AREAS WITH A MAXIMUM DEPTH OF .063 ON THE INBOARD CORN ER AS NOTED IN FIGURE 1 ARE STRUCTURALLY ACCEPTABLE PROVIDED A MIN 63 MICRO FINISH IS MAINTAINTED TOUCH UP ALODINE AND F R PRIMER PER SRM CHAPTER 51. 2 L 7 2 4F RT A35EU 2007032300025 20070323 00025 WP 2007 3 23 07FDEA01064 1 20070321 A 5347 607158 SEAT TRACK DOUG MD10 MD1010F 3022112 WP BS 1541-1681 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 571FE 47830 MAIN CARGO COMPT SEAT TRACK AT STA 1541-1681 LBL 8 DAMAGED BEYOND REPAIRABLE LIMITS. REMOVED AND REPLACED DAMAGED SEAT TRACK. 2 L 7 3 4F RT A22WE 2007032300026 20070323 00026 NM 2007 3 23 SWAA071425 1 20070319 A 3350 0L3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 437WN 29832 EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007032300027 20070323 00027 NM 2007 3 23 SWAA071437 1 20070320 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 241WN 32504 DURING SCHEDULED MV1 CHECK, FOUND EEPLS COVER BROKEN AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007032300028 20070323 00028 NM 2007 3 23 SWAA071438 1 20070320 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 245WN 32506 EEPLS COVER MISSING AT ROW 3 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007032300029 20070323 00029 NM 2007 3 23 SWAA071428 1 20070318 A 5610 5717623122 WINDOW BOEING 737 737301 1384611 NM COCKPIT ARCED A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 660SW 23230 FLIGHT DECK R2 WINDOW ARCHED. REMOVED AND REPLACED R2 WINDOW PER MM. 2 L 7 2 4F RT A16WE 2007032300030 20070323 00030 2007 3 23 SWAA071439 4 20070320 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 456WN 32463 R1 DOOR EMERGENCY EVAC SLIDE OUT OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007032300031 20070323 00031 2007 3 23 SWAA071440 4 20070320 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 708SW 27842 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007032300032 20070323 00032 2007 3 23 SWAA071436 4 20070320 A 2565 BOTTLE BOEING 737 7375H4 138449D NM L1 DOOR SLIDE LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 0621 24188 L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007032300033 20070323 00033 2007 3 23 SWAA071426 4 20070319 A 2565 BOTTLE BOEING 737 7377H4 1384404 NM L2 DOOR SLIDE LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 759GS 0015A 30544 DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPL ACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007032300034 20070323 00034 2007 3 23 SWAA071427 4 20070316 A 2565 BOTTLE BOEING 737 7377H4 1384404 NM L2 DOOR SLIDE LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 417WN 0224A 29822 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPL ACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007032300035 20070323 00035 2007 3 23 SWAA071433 4 20070318 A 2565 BOTTLE BOEING 737 7377H4 1384404 NM L2 DOOR SLIDE LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 774SW 0094A 27882 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPL ACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007032300036 20070323 00036 NM 2007 3 23 SWAA071430 1 20070321 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 520 S28R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007032300037 20070323 00037 NM 2007 3 23 SWAA071446 1 20070320 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 572 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 572, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007032300038 20070323 00038 NM 2007 3 23 SWAA071444 1 20070320 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 563 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 563, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007032300039 20070323 00039 WP 2007 3 23 ASMF200703006 1 20070317 A 5730 698640 SEAL DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE LT WING PANEL LEAKING W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 803ML 49726 DURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED IN AN UPPER PANEL OF THE LT WING. MAINTENANCE PERSONNEL RELOCATED THE SEA L AND APPLIED SEALANT IAW SRM 51-20-04 AND 51-22-2A, LEAK WAS CORRECTED. AS A PRECAUTIONARY ACTION, DURING OVERNIGHT CH ECK THE SEAL WAS REPLACED, SEALANT WAS APPLIED AND A LEAK TEST WAS PERFORMED IAW MM 28-10-01 PAGE 601, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007032300040 20070323 00040 SO 2007 3 23 SWIA200718015 1 20070119 A 5712 PRESSURE PANEL EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT MLG WW ERODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 221SW LT WHEEL WELL FWD OB WEB PANEL ERODED FROM INSPECTION PANELS. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED LT WHEEL WELL OB WEBBING, SECURED IAW SRM 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 2007032300041 20070323 00041 SO 2007 3 23 SWIA200718016 1 20070119 A 2572 RACK EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE E/E BAY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 221SW AVIONICS EQUIPMENT RACK IN AVIONICS COMPARTMENT IS CRACKED IN (2) AREAS. (DISCOVERED DURING C-CHECK INSPECTION) (2) NEW BRACKETS INSTALLED IAW SRM 120 51-10-02 PG. 3 SEC. 3A. 2 L 7 2 4T 4 T RT A31SO E20NE 2007032300042 20070323 00042 SO 2007 3 23 SWIA200718017 1 20070119 A 5411 FRAME EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 221SW 120290 LT NACELLE FRAME NR 1 CRACKED AT WEBBING. (DISCOVERED DURING C-CHECK INSPECTION) COMPLIED WITH SB 120-54-0036 REV. 02 0 9 JUN 99 TO LT ENGINE NACELLE FRAME NR 1. 2 L 7 2 4T 4 T RT A31SO E20NE 2007032300043 20070323 00043 SO 2007 3 23 SWIA200718018 1 20070119 A 5753 BRACE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT NACELLE FLAP CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 221SW RT NACELLE FLAP INTERNAL BRACING HAS A CRACK AT A STIFFENER. (DISCOVERED DURING C-CHECK INSPECTION) NEW STIFFENER INSTA LLED IAW SRM 120 51-10-02 PG. 3 SEC. 3A. 2 L 7 2 4T 4 T RT A31SO E20NE 2007032300044 20070323 00044 SO 2007 3 23 SWIA200718019 1 20070119 A 5411 RIB EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 221SW 120290 LT IB NACELLE RIB CRACKED BENEATH WING. (DISCOVERED DURING C-CHECK INSPECTION) DOUBLER INSTALLED IAW SRM 120 51-10-02 P G 2 SEC. 2B. 2 L 7 2 4T 4 T RT A31SO E20NE 2007032300045 20070323 00045 SO 2007 3 23 SWIA200718020 1 20070119 A 5320 BRACKET EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 221SW 120290 BRACKET BETWEEN FRAMES AFT OF DV WINDOW CAPTAIN'S SIDE COCKPIT CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPLACE D BRACKET BETWEEN FRAME IAW SRM 51-10-02 PG. 3 SEC 3A AND RII 53-500-1000. 2 L 7 2 4T 4 T RT A31SO E20NE 2007032300046 20070323 00046 SO 2007 3 23 SWIA200718021 1 20070119 A 5330 SKIN EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 221SW 120290 FUSELAGE SKIN CORRODED AT FUSELAGE FRAME STATION 22 BETWEEN STRINGERS 21.5R TO 21.5L. (DISCOVERED DURING C-CHECK INSPEC TION)NEW SKIN INSTALLED IAW SRM 51-10-02 PG. 3 SECT 3A AND RII CARD 53-800-1000. 2 L 7 2 4T 4 T RT A31SO E20NE 2007032300047 20070323 00047 SO 2007 3 23 SWIA200718022 1 20070119 A 5310 WINDOW POST EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 221SW 120290 CRACK ON CAPTAIN'S SIDE LOWER DV WINDOW BEAM AT VERTICLE WINDOW POST AREA. (DISCOVERED DURING C-CHECK INSPECTION) REPLA CED CAPTAIN'S SIDE DV WINDOW BEAM IAW SRM 51-10-02 PG SEC. 3A AND RII 53-800-1000. 2 L 7 2 4T 4 T RT A31SO E20NE 2007032300048 20070323 00048 SO 2007 3 23 SWIA200718023 1 20070119 A 5311 FRAME EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE FUSLEAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 221SW 120290 CROSS MEMBER OF FRAME (16) CRACKED. (DISCOVERED DURING C-CHECK INSPECTION NEW CROSS MEMBER INSTALLED IAW SRM 51-10-02 PG. 3 SEC. 3A P/N 120-06962-601. 2 L 7 2 4T 4 T RT A31SO E20NE 2007032300050 20070323 00050 NE 2007 3 23 FE5F200700001 2 20070311 A 7250 JT8D219 ENGINE DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE LEFT SURGES W FE5F A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 03 28025 22988 2164 9853602 P726041 B-28025(SN:53602), 0345(UTC) DEPARTING FROM RCTP (TPE TAIWAN), CLIMBING THROUGH 11000 NR,ENCOUNTERING SURGING CONTINUALL Y, A/T OFF, LT THROTTLE IDLE AND ADJUST TO EPR 1.4 AND INSTRUMENT SHOWING STABLE, READJUST EPR TO 1.75 ,SURGING HAPPENED AGAIN. REQUESTED APPROACH FOR LANDING, DESCENT THROUGH 6000 INCH (IDLE) SURGING HAPPENED AGAIN. LT FUEL LEVEL OFF. LAND ING TPE AIRPORT AT 0414 (UTC). 2 L 7 2 4F 4 F RT E9NE 2007032300051 20070323 00051 CE 2007 3 23 GUUA03180701 1 20070318 A 5510 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT STABILIZER CORRODED A GUUA O OTHER O OTHER IN INSP/MAINT 1 SO 29 69549 5043 UE194 AT SCHEDULED ROUTINE MAINTENANCE LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED LT OB ELEVATOR HINGE BRACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 2007032300052 20070323 00052 SO 2007 3 23 C2XA07IA063 1 20070315 A 3230 355022002MOD4 ELECTRONIC UNIT EMB 145 EMB145EP 3260221 SO LT MLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13935 14139 14139 145022 IAH - FLT 2103, DURING CLIMB THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WH ERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT (LGEU), OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007032300053 20070323 00053 SO 2007 3 23 C2XA07IA064 1 20070315 A 2150 8152403 ACM EMB 145 EMB145LR 3260212 SO NR 1 FROZEN A C2XA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 13968 145138 IAH - FLIGHT 2082, DURING TAKEOFF ROLL, THE CREW REPORTED A STRONG SMOKE ODOR INVADED THE CABIN AND FLIGHT DECK. THE CR EW ABORTED TAKEOFF AND RETURNED TO THE GATE WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ACM, OPERATIONALLY CHE CKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032300054 20070323 00054 SO 2007 3 23 C2XA07IA065 1 20070318 A 3231 DOOR EMB 135 EMB135LR 3260305 SO MLG MALFUNCTIONED A C2XA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SW 27 28518 145334 IAH - FLIGHT 2620, THE CREW REPORTED THAT THE NOSE LANDING GEAR DOORS OPENED IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITH OUT INCIDENT, WHERE MAINTENANCE INSPECTED THE AIRCRAFT, AN OPERATIONALLY CHECKED THE LANDING GEAR EXTENSION AND RETRACTI ON SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007032300055 20070323 00055 SO 2007 3 23 C2XA07IA066 1 20070318 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12957 145080 IAH - DURING A-CHECK INSPECTION THE SECOND AISLE PATH LIGHTING STRIP FROM THE FRONT EMERGENCY EXIT WAS FOUND TO BE INOPE RATIVE. MAINTENANCE OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032300056 20070323 00056 SO 2007 3 23 C2XA07IA067 1 20070318 A 5610 SEAL EMB 135 EMB135LR 3260305 SO WINDSHIELD LEAKING A C2XA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 27 28518 145334 IAH - FLIGHT 3137, THE CREW REPORTED THAT THE AIRCRAFT MAKES NOISE AT SPEED WITH NOSE PITCH UP OR DOWN, NOSE GEAR DOORS DO NOT CLOSE ALL THE WAY. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE LANDING GEAR, OPE RATIONALLY CHECKED WITH NO DEFECTS, DISCOVERED THE WINDSHIELD HUMP SEAL TO BE THE SOURCE OF THE NOISE. MAINTENANCE REPA IRED THE CAPTAINS WINDSHIELD HUMP SEAL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TOP SERVICE. 2 L 7 2 4F RT T00011AT 2007032300057 20070323 00057 SO 2007 3 23 C2XA07IA068 1 20070319 A 2810 14569701403 VALVE EMB 145 EMB145XR 3260214 SO LT WING TANK LEAKING A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 27 17159 145792 VER - FLIGHT 4916, THE CREW REPORTED THE LEFT WING LEAKING FUEL IN FLIGHT. THE AIRCRAFT DIVERTED TO VER WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND OUTBOARD FLAPPER VALVE, LEAK CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007032300058 20070323 00058 SO 2007 3 23 C2XA07CL032 1 20070317 A 3231 21180100401 ACTUATOR EMB 145 EMB145LR 3260212 SO NLG LEAKING A C2XA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 27 16561 11385 145610 CLE FLIGHT 2464 THE CREW REPORTED A VERY LOUD WIND NOISE UNDER NOSE OF AIRCRAFT FOR SEVERAL MINUTES AFTER TAKEOFF. THE CREW SUSPECTED THE NOSE GEAR DOORS DID NOT FULLY CLOSE. NO INDICATION WAS NOTED ON THE EICAS. MAINTENANCE INSPECTED AN D REPLACED THE LEFT HAND NOSE GEAR DOOR ACTUATOR. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007032300059 20070323 00059 SO 2007 3 23 C2XA07BT028 1 20070308 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NLG DOOR INOPERATIVE A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 14573 145638 EWR LOG SQUAWK FLT 3128 SOUNDS LIKE NLG DOORS ARE OPEN IN FLT. MAINTENANCE FOUND NLG DOORS WERE NOT CLOSING. REMOVED A ND REPLACED NLG DOOR SEQUENCE PROX SWITCH IAW EMB145 MM 32-61-01. OPS CHECK GOOD IAW EMB145 MM 32-30-00. 2 L 7 2 4T RT T00011AT 2007032300060 20070323 00060 SO 2007 3 23 C2XA07BT031 1 20070318 A 2752 ACTUATOR EMB 145 EMB145XR 3260214 SO TE FLAPS LACK OF LUBE A C2XA O OTHER J WARNING INDICATION DE DESCENT 1 SW 27 12157 145787 EWR FLT 3084 LOG SQUAWK FLAP FAIL DURING APPROACH. LUBRICATED ALL 8 FLAP SCREW JACK ACTUATORS IAW EMB145XR AMM 27-51-00 AND REMOVED AND REPLACED FLAP SELECTOR LEVER IAW EMB145XR AMM 27-53-03. OPS CHECK FLAP SYSTEM. NO FAULT FOUND. 2 L 7 2 4F RT 2007032300061 20070323 00061 SO 2007 3 23 C2XA07BT029 1 20070310 A 2611 FAU751A4 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY FALSE ACTIVATION A C2XA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 27 12540 145537 EWR LOG SQUAWK FLT 2490 LAV SMOKE MESSAGE ON EICAS. REMOVED AND REPLACED SMOKE DETECTOR TEST PANEL IAW EMB145 CMM 26-14 -01. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007032300062 20070323 00062 SO 2007 3 23 C2XA07BT030 1 20070311 A 3350 AD20131A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 13988 4930 743 145265 EWR LOG SQUAWK FLT 2325 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY IAW EMB145 AMM 33-50-04. O PS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007032300079 20070323 00079 CE 2007 3 23 GLBA20060924 1 20070322 A 2121 1143800284 BLOWER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BROKEN A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 245GL UE245 FLIGHT 5066 - PILOTS REPORTED THE ODOR OF SMOKE OR FUMES. NO INDICATIONS OF FIRE OR SMOKE REPORTED. MAINTENANCE INSPECT ED AFFECTED AREAS AND REMOVED AND REPLACED THE AFT VENT BLOWER IAW MM 21-20-00. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2007032300088 20070323 00088 SO 2007 3 23 GLBA20060925 1 20070322 A 2197 WIRE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE TEMP CONTROL SWT DISCONNECTED A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 71GL 120071 FLIGHT 5022 - PILOTS REPORTED THE ODOR OF SMOKE OR FUMES THROUGHOUT THE CABIN. NO INDICATIONS OF FIRE OR SMOKE REPORTE D. MAINTENANCE PLACED THE ITEM ON MEL IAW 21-50-2 CATEGORY C. MAINTENANCE RECONNECTED WIRES ON THE TEMPERATURE CONTROL S WITCH IAW EMB-120 21-60. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2007032300089 20070323 00089 NM 2007 3 23 KCSA071073 1 20070322 A 5330 BEAR STRAP BOEING 747 747236B 1384804 NM BS 1314 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 MAIN DECK ENTRY DOOR OPENING BEAR STRAP DOUBLER CRACKED AT AFT UPPER CORNER BS 1314, WL 275. 2 L 7 4 4F A20WE 2007032300090 20070323 00090 NM 2007 3 23 KCSA071074 1 20070322 A 5347 SEAT TRACK BOEING 747 747236B 1384804 NM BS 1700 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 CORROSION ON MAIN DECK SEAT TRACK FLANGE AT BS 1700, RBL 12, WL 200. 2 L 7 4 4F A20WE 2007032300091 20070323 00091 NM 2007 3 23 KCSA071075 1 20070322 A 5414 SKIN BOEING 747 747236B 1384804 NM NR 3 PYLON WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 NR 3 PYLON I/B SKIN AND FIRESHIELD WORN ON LOWER SKIRT AT NAC STA 233. 2 L 7 4 4F A20WE 2007032300092 20070323 00092 NM 2007 3 23 KCSA071076 1 20070322 A 5414 SKIN BOEING 747 747236B 1384804 NM NR 4 PYLON WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 NR 4 PYLON O/B SKIN WORN AT LOWER SKIRT AT NAC STA 236. 2 L 7 4 4F A20WE 2007032300093 20070323 00093 WP 2007 3 23 BSYA200700007 2 20070320 A 7210 307009312 BEVEL GEAR LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP GEARBOX DAMAGED E BSYA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 GL 07 98LC 077 P74225 EN ROUTE FROM DAL TO APA AT FLIGHT LEVEL 36,000 FEET LEFT ENGINE COMPUTER FAIL LIGHT CAME ON AND THE ENGINE SHUT DOWN. RECYCLED COMPUTER AND IT CAME BACK ON LINE ATTEMPTED A START, WOULD NOT RELIGHT. LANDED APA NO PROBLEMS. FOUND 90 DEGR EE GEAR BOX BEVELED GEAR DAMAGED, REMOVED AND REPLACED 90 DEGREE GEAR BOX. 2 L 7 2 4F 4 F A10CE E6WE 2007032300094 20070323 00094 EA 2007 3 23 VNAA0703003 1 20070304 A 2420 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 IDG LOW A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 251PS 7931 CREW REPORTED A NR 2 IDG CAS MESSAGE ON TAKEOFF ROLL. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE IDG NR 2 OIL LEVEL LOW. MAINTENANCE PROPERLY SERVICED THE OIL LEVEL IAW MM. AIRCRA FT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007032300095 20070323 00095 EA 2007 3 23 VNAA0703006 1 20070306 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAA O OTHER J WARNING INDICATION DE DESCENT 1 GL 05 202PS 7858 CREW REPORTED A FLAPS FAIL CAS MESSAGE ON DESCENT. MAINTENANCE INSPECTED AND COMPLIED WITH THE SERVICE LETTER 00-001. SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007032600003 20070326 00003 NM 2007 3 26 SWAA071499 1 20070321 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 503D S12R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 12R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007032600008 20070326 00008 EA 2007 3 26 SWIA200718038 1 20070319 A 2497 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ELECTRICAL SHORTED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 864AS 7502 AFTER TAKEOFF ACCESS BUSS CAUTION MESSAGE AND FOLLOWED BY SEVERAL CAUTIONS MESSAGES. FOUND ADG XFER K2XD CONTACTOR HAD A SHORTED TERMINAL. REPLACED CONTACTOR, TERMINAL AND ESSENTIAL TRU 1. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2007032600009 20070326 00009 EA 2007 3 26 TRAX200700388 1 20070316 A 5300 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 STA 484 RBL 36 INTERCOSTAL REPAIR ANGLE CRACKED IN RADIUS. 2 L 7 2 4F RT A21EA 2007032600010 20070326 00010 EA 2007 3 26 TRAX200700389 1 20070317 A 5230 BRACKET CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 CARGO DOOR STRUCTURE AFT ANGLE BRACKET IS CRACKED. 2 L 7 2 4F RT A21EA 2007032600011 20070326 00011 EA 2007 3 26 TRAX200700390 1 20070318 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 CORROSION FOUND ON FWD SUPPORT FLOOR ANGLE OF THE 280. REMOVED FWD 280 FLOOR SUPOPRT AGNLE DUE TO CORROSION ALL WORK D ONE IAW CRJ 200 SRM 51-42-06. REMOVED AND REPLACED FWD FLOOR SUPPORT ANGLE ON 280 IAW REO 601R-53-11-926. TASK COMPLETE D ON TASK CARD N/R-00169. 2 L 7 2 4F RT A21EA 2007032600012 20070326 00012 EA 2007 3 26 TRAX200700391 1 20070318 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 349 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 CORROSION AT FS 349 LBL 37 ASD AFT ANGLE. REMOVED TEFLON STRIP AND REMOVED CORROSION AT FS349 LBL37 ASD AFT ANGLE. DAM AGE WITHIN LIMITS. TREATED PRIMED AND PAINTED.REINSTALLED TEFLON STRIP. WORK DONE IAW CRJ 200 SRM 51-21-06 AND 51-42-13. 2 L 7 2 4F RT A21EA 2007032600014 20070326 00014 EA 2007 3 26 TRAX200700393 1 20070318 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA ASD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 929EV 8007 ASD BOTTOM STEP CRACKED. 2 L 7 2 4F RT A21EA 2007032600017 20070326 00017 NM 2007 3 26 SWAA071467 1 20070321 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 714 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 714, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600018 20070326 00018 NM 2007 3 26 SWAA071476 1 20070321 A 5330 6545767 SKIN BOEING 737 7373Q8 1384670 NM BS 410 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA. CUT OUT BS 410, BL 0. REPAIRED SKI N PER ER. 2 L 7 2 4F RT A16WE 2007032600019 20070326 00019 NM 2007 3 26 SWAA071477 1 20070321 A 5330 6545767 SKIN BOEING 737 7373Q8 1384670 NM BS 430 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA. CUTOUT BS 430, BL 0. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007032600020 20070326 00020 NM 2007 3 26 SWAA071478 1 20070321 A 5330 6545767 SKIN BOEING 737 7373Q8 1384670 NM BS 450 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA . CUT OUT BS 450, BL 0. REPAIRED SK IN PER ER. 2 L 7 2 4F RT A16WE 2007032600025 20070326 00025 NM 2007 3 26 SWAA071491 1 20070321 A 5210 6545871 SKIN BOEING 737 7373Y0 1384671 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR SKIN CRACKED AT LOWER DOOR HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600026 20070326 00026 NM 2007 3 26 SWAA071475 1 20070321 A 5753 6546430167 SKIN BOEING 737 7373T0 1384582 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED HC1 CHECK, FOUND LEFT WING INBOARD FORE FLAP DELAMINATED INBOARD UPPER SURFACE. REMOVED AND REPLACED F ORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2007032600029 20070326 00029 NM 2007 3 26 SWAA071482 1 20070321 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM BS 520 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600030 20070326 00030 NM 2007 3 26 SWAA071487 1 20070321 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 S8 L/R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600031 20070326 00031 NM 2007 3 26 SWAA071486 1 20070321 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600032 20070326 00032 NM 2007 3 26 SWAA071488 1 20070321 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM BS 867 S8L/R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600033 20070326 00033 NM 2007 3 26 SWAA071485 1 20070321 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600034 20070326 00034 NM 2007 3 26 SWAA071483 1 20070321 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM BS 360 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600035 20070326 00035 NM 2007 3 26 SWAA071484 1 20070321 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM BS 727D S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600036 20070326 00036 NM 2007 3 26 SWAA071504 1 20070321 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 360 S11L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007032600037 20070326 00037 NM 2007 3 26 SWAA071503 1 20070321 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 360 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007032600040 20070326 00040 NM 2007 3 26 SWAA071496 1 20070321 A 5313 BAC1498 STRINGER BOEING 737 7373T5 1384608 NM BS 747 S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED MV2 CHECK, FOUND STRINGER 24L CRACKED AT BS 747. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007032600045 20070326 00045 NM 2007 3 26 SWAA071472 1 20070321 A 5520 DAS623B BEARING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, LEFT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED INBOARD HORN BEARING PER MM. 2 L 7 2 4F RT A16WE 2007032100069 20070321 00069 NM 2007 3 21 UPS07449432 1 20070211 A 5310 FILLER BOEING 747 747121 1384871 NM BS 780 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT BS 780 FRAME TENSION TIE ATTACHMENT AREA AT FASTENER HOLE NR 4 FOUND CRACK AT FILLER RUNNING 1:0 0 O/S POSITION APPROX .0625 INCH LONG. RIGHT BS 780 FRAME TENSION TIE ATT FILLER REPLACED AS PER SRM 51-10-01 PG 9. 2 L 7 4 4F A20WE 2007032100070 20070321 00070 NM 2007 3 21 UPS07449433 1 20070305 A 5330 BEAR STRAP BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER CRACK REVEALED AT THE EDGE OF BEAR STRAP. CRACK LENGTH 2. 5 INCHES APPROX. RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS R53-41-35782 AND UP S EO B747-5330-15047. 2 L 7 4 4F A20WE 2007032100071 20070321 00071 NM 2007 3 21 UPS07449434 1 20070213 A 5712 65B708285 RIB BOEING 747 747121 1384871 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT WING NR 5 VC FLAP I/B ACTUATOR ATT L/E SUPPORT RIB AT OLES 1205 ORIGINAL CRACK EXTENDED TOWARD O/ B. CRACK LENGTH .25 INCH. LEFT WING NR 5 VC FLAP I/B ACTUATOR L/E SUPPORT RIB AT OLES 1205 REPAIRED AS PER RS R57-42-3 5767. REPEAT INSPECTION IS REQUIRED AS PER RS R57-42-35767 AND UPS EO B747-5740-26319. 2 L 7 4 4F A20WE 2007032100072 20070321 00072 NM 2007 3 21 UPS07449435 1 20070212 A 5714 65B106718 STIFFENER BOEING 747 747121 1384871 NM BS 1241 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT WING RIGHT WLG WW CTR SECTION REAR SPAR STIFFENER BS 1241 AT RBL 85 30 INCHES BELOW CEILING FOUN D CORRODED. CORROSION BLEND OUT 0.150 X .5 X 5 INCH EXCEED SRM LIMIT. RIGHT WING RIGHT WLG W/W CTR SECTION REAR SPAR S TIFFENER AT BS 1241 RBL 85 REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND RS R53-43-35776 AND UPS EO B747-5710-1642 1. 2 L 7 4 4F A20WE 2007032100073 20070321 00073 NM 2007 3 21 UPS07449436 1 20070216 A 5310 DOOR FRAME BOEING 747 747121 1384871 NM BS 2231 S24-25R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT BS 2231 FRAME AT DOOR NR 5 BETWEEN S24R-25R FOUND 2EA HOLE CRACK. CRACK LENGTH .125 INCH, .25 I NCH AND .1875 INCH. M/D RIGHT BS 2231 FRAME REVEAL, STRAP AND CHORD REPAIRED AS PER RS R53-62-35764. CONTINUE INSPECTI ON IS REQUIRED PER RS R53-62-35764 AND UPS EO B747-5310-26334. 2 L 7 4 4F A20WE 2007032100074 20070321 00074 NM 2007 3 21 UPS07449437 1 20070215 A 5320 REVEAL BOEING 747 747121 1384871 NM BS 2231 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT BS 2231 FRAME AREA 2EA FASTENER HOLE CRACK FOUND AT REVEAL BETWEEN S25R AND S26R. CRACK LENGTH .25 INCH, .125 INCH, AND .1875 INCH. M/D RIGHT BS 2231 FRAME REVEAL, STRAP AND CHORD REPAIRED AS PER RS R53-62-3764. C ONTINUE INSPECTION IS REQUIRED AS PER RS R53-62-35764 AND UPS EO B747-5310-26334. 2 L 7 4 4F A20WE 2007032100075 20070321 00075 NM 2007 3 21 UPS07449439 1 20070210 A 5320 CHANNEL BOEING 747 747121 1384871 NM BS 840 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C M/D BS 840 LEFT TENSION TIE AFT CHANNEL FOUND CRACK. CRACK LENGTH .5 INCH. M/D BS 840 LEFT TENSION T IE AFT CHANNEL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007032100076 20070321 00076 NM 2007 3 21 UPS07449440 1 20070211 A 5320 CHANNEL BOEING 747 747121 1384871 NM BS 820 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C RIGHT BS 820 FRAME TENSION TIE ATTACHMENT AREA AT FASTENER HOLE NR 4 CRACK AT FWD CHANNEL RUNNING UPPE R AND LWR BOTH CRACK APPROX .0625 IN LENGTH. RIGHT BS 820 FRAME TENSION TIE FWD CHANNEL REPAIRED AS PER RS R53-25-35751 . CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35751 AND UPS EO B747-5310-26129. 2 L 7 4 4F A20WE 2007032100077 20070321 00077 NM 2007 3 21 SWAA071399 1 20070316 A 5610 59717623121 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT ARCED A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 383SW 26589 FLIGHT DECK L2 WINDOW ARCHED. REMOVED AND REPLACED L2 WINDOW PER MM. 2 L 7 2 4F RT A16WE 2007032100078 20070321 00078 2007 3 21 SWAA071420 4 20070317 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 749SW 29801 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007032100079 20070321 00079 NM 2007 3 21 SWAA071403 1 20070316 A 5330 6545896 SKIN BOEING 737 7373H4 1384600 NM BS 528 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT AIR CONDITIONING DOOR CUTOUT RT FWD CORNER BS 528. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007032100080 20070321 00080 NM 2007 3 21 SWAA071413 1 20070316 A 5753 6546434 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 18Y CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT LOWER OUTBOARD END. REPAIRED FLAP PER SRM . 2 L 7 2 4F RT A16WE 2007032100081 20070321 00081 NM 2007 3 21 SWAA071401 1 20070316 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM BS 380 S13R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 13R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007032100082 20070321 00082 NM 2007 3 21 SWAA071404 1 20070316 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM BS 380 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007032100083 20070321 00083 NM 2007 3 21 SWAA071414 1 20070316 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S26R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 26R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007032100084 20070321 00084 NM 2007 3 21 SWAA071417 1 20070316 A 5311 6546551 FRAME BOEING 737 7373Q8 1384670 NM BS 807 S25L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, STR 25L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007032100085 20070321 00085 NM 2007 3 21 SWAA071415 1 20070316 A 5311 6546552 FRAME BOEING 737 7373Q8 1384670 NM BS 827 S25L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 827, STR 25L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007032100086 20070321 00086 NM 2007 3 21 SWAA071416 1 20070316 A 5311 6546554 FRAME BOEING 737 7373Q8 1384670 NM BS 847 S25L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, STR 25L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007032100087 20070321 00087 2007 3 21 ABXA070069 4 20070313 A 3497 WIRE DOUG DC8 DC863F 302198F WP COCKPIT CHAFED A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 816AX 46093 ACRID ODOR OF ELECTRICAL SMOKE BY ALL 3 CREW MEMBERS, SOURCE NOT IDENTIFIED. ODOR COMES AND GOES. FOUND LOAD CALCULATO R WIRES CHAFING ON PANEL. ROUTED PANEL AREA OUT AND REPAIRED WIRES IAW DC8 MM CHAPTER 20. NO OTHER DEFECTS NOTED AT TH IS TIME. 2 L 7 4 4F 4A25 2007032100088 20070321 00088 NM 2007 3 21 SWAA071411 1 20070316 A 5310 6546957 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 510 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 510, LBL 68. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2007032100089 20070321 00089 NM 2007 3 21 SWAA071412 1 20070316 A 5310 6547979 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 816 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 816, RBL 68. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2007032100090 20070321 00090 NM 2007 3 21 SWAA071410 1 20070316 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 400 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007032100091 20070321 00091 NM 2007 3 21 SWAA071405 1 20070316 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727C S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007032100092 20070321 00092 NM 2007 3 21 SWAA071406 1 20070316 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727D S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007032100093 20070321 00093 NM 2007 3 21 SWAA071407 1 20070316 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007032100094 20070321 00094 NM 2007 3 21 SWAA071409 1 20070316 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 400 S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007032100095 20070321 00095 NM 2007 3 21 SWAA071408 1 20070316 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 440 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007032100096 20070321 00096 NM 2007 3 21 SWAA071419 1 20070317 A 3350 767 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 207WN 34012 DURING SCHEDULED MV2 CHECK, FOUND LEFT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007032100097 20070321 00097 NM 2007 3 21 SWAA071400 1 20070316 A 3350 8200548401 LIGHT BOEING 737 7377H4 1384404 NM EMERGENCY EXIT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 485WN 32473 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007032100098 20070321 00098 2007 3 21 SWAA071398 4 20070316 A 2565 D31354 SLIDE BOEING 737 7373L9 1384470 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007032100099 20070321 00099 NM 2007 3 21 SWAA071402 1 20070316 A 3350 MS155721 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007032100100 20070321 00100 NM 2007 3 21 SWAA071418 1 20070316 A 3350 MS155721 LAMP BOEING 737 737317 138447P NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007032100101 20070321 00101 EA 2007 3 21 TRAX200700359 1 20070315 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA BS 319 S27 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 FRAME CORRODED AT FS 319 STRINGER 27. 2 L 7 2 4F RT A21EA 2007032100102 20070321 00102 EA 2007 3 21 TRAX200700360 1 20070315 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA BS 333 S27 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 FRAME CORRODED AT FS 333 STRINGER 27. REMOVED FASTNERS AND BLENDED CORRISION IAW CRJ 700 SRM 51-42-06. PERFORMED THICK NESS MEASUREMENT OF BLEND AREA AT FS 333, STR 27 IAW CRJ 700 NDTM 51-20-004. MINIMUM THICKNESS IS .047". SUBMITTED AND RECIEVED REO 670-53-21-260 FOR FS 333 AT STR27. BLENDOUT IS WITHIN LIMITS OF REO 670-53-21-260 ITEM 12. PERFORMED EDDY CURRENT INSPECTION OF BLEND AREA AT FS 333, STR. 27 IAW REO 670-53-21-260 PER CRJ 700 NDTM 51-20-006. NO DEFECTS NOTED. INSTALLED NEW FASTENERS WHERE THEY WERE REMOVED FOR CORROSION REMOVAL IAW CRJ 700 SRM 51-42-06. TREATED, PRIMED AND P AINTED SKIN WHERE RIVETS WERE REMOVED IAW CRJ 700 SRM 51-26-01. JOB COMPLETE. 2 L 7 2 4F RT A21EA 2007032100103 20070321 00103 EA 2007 3 21 TRAX200700361 1 20070315 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA BS 349 S27 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 FRAME CORRODED AT FS 349 STRINGER 27. 2 L 7 2 4F RT A21EA 2007032100104 20070321 00104 EA 2007 3 21 TRAX200700362 1 20070315 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 SURFACE CORROSION AT COCKPIT AFT RT WEB FS 280.00 AFT FACE BOTTOM SIDE AT APPROX RBL 26. (SUPPLEMENTAL 28 MARCH 07) B LENDED CORROSION ON LEFT AND RIGHT FS 280 WEB TO THE MAX DEPTH OF .004" BLEND OUT WAS FOUND WITHIN LIMITS IAW 670-53-11- 052. 2 L 7 2 4F RT A21EA 2007032100105 20070321 00105 EA 2007 3 21 TRAX200700363 1 20070315 A 5313 STRINGER CNDAIR CL600 CL6002C10 1390015 EA BS 294-333 S25R CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 CORROSION ON S25R BETWEEN FS 294 AND FS 333. DAMAGE IS OUT OF LIMITS, REMOVED .025 FROM STRG 25R BETWEEN FS 294 AND FS 333 IAW CRJ 700 SRM 53-21-03-101-002-A01. RECIEVED REO 670-53-21-260. FABRICATED REPAIR ANGLE AND SHIM IAW REO 670-53-2 1-260. PERFORMED NDT PER NDTM 51-20-08 IAW REO 670-53-21-260. INSTALLED REPAIR ANGLE AND SHIM IAW REO 670-53-21-260. INSTALLED CLEAT FOR S26R AND APPLIED CORROSION INHIBITOR TO AREA BETWEEN FS 280 AND FS 349 PER CRJ 700 SRM 51-21-01. 2 L 7 2 4F RT A21EA 2007032100106 20070321 00106 NM 2007 3 21 ASAA0771536 1 20070316 A 5244 148A38202 HINGE BOEING 737 737790 13844CN NM APU DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 APU ACCESS DOOR HINGE AREA DAMAGED REPAIRED IAW SRM 53-80-01. 2 L 7 2 4F RT A16WE 2007032100107 20070321 00107 NM 2007 3 21 ASAA0771535 1 20070316 A 5340 ATTACH FITTING BOEING 737 737790 13844CN NM BS 243-260 LOOSE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 NOSE LANDING GEAR RETRACT ACTUATOR UPPER ATTACH LUG BEARING IS LOOSE AND MIGRATING REPAIRED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007032100108 20070321 00108 NM 2007 3 21 ASAA0771533 1 20070316 A 5321 147A581023 FLOOR PANEL BOEING 737 737790 13844CN NM BS 976-986 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 CABIN FLOOR PANEL 241AAF IS GOUGED AT FWD LEFT CORNER REPAIRED IAW EA5320 100. 2 L 7 2 4F RT A16WE 2007032100109 20070321 00109 NM 2007 3 21 ASAA0771534 1 20070316 A 5321 147A581023 FLOORBOARD BOEING 737 737790 13844CN NM CABIN DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 CABIN FLOORBOARD AT 967 DAMAGED REPAIRED IAW SRM 53-00-50 REPAIR 2. 2 L 7 2 4F RT A16WE 2007032100110 20070321 00110 NM 2007 3 21 ASAA0771537 1 20070316 A 5321 147A5810136 FLOORBOARD BOEING 737 737790 13844CN NM CABIN DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 CABIN FLOORBOARD IS DAMAGED AT 951 REPAIRED IAW SRM 53-00-50. 2 L 7 2 4F RT A16WE 2007032100111 20070321 00111 NM 2007 3 21 ASAA0771538 1 20070316 A 5321 147A581020 FLOORBOARD BOEING 737 737790 13844CN NM CABIN DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 CABIN FLOORBOARD HAS DAMAGE AT 927 REPAIRED IAW SRM 53-00-50 REPAIR 9. 2 L 7 2 4F RT A16WE 2007032100112 20070321 00112 NM 2007 3 21 ASAA0771539 1 20070316 A 5320 147A56602 INTERCOSTAL BOEING 737 737790 13844CN NM BS 967 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 FLOORBOARD SUPPORT INTERCOSTAL IS CORRODED AT BS 967 REPAIRED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007032100113 20070321 00113 NM 2007 3 21 ASAA0771540 1 20070316 A 5315 147A5506 FLOORBEAM BOEING 737 737790 13844CN NM BS 986 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 FLOORBEAM UPPER TEE IS CORRODED AT BS 986 REPAIRED IAW EA 5310 02703. 2 L 7 2 4F RT A16WE 2007032100146 20070321 00146 GL 2007 3 21 C2XA07IA062 2 20070309 A 7200 AE3007A1P ENGINE EMB 145 EMB145EP 3260221 SO ALLSN AE300 AE3007A GL RIGHT LEAKING A C2XA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 27 12934 15422 15422 145019 IAH - FLIGHT 2703 THE CREW REPORTED A LAV SMOKE WARNING ON ROTATION WITH A STRONG SMOKE SMELL BUT NO VISUAL INDICATION O F SMOKE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TW O ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007032100147 20070321 00147 EA 2007 3 21 A6WA200740105 1 20070307 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 421ZW 7346 FLAPS FAIL CAUTION MESSAGE FLAPS FAILED ZERO. INSPECTED FLAPS FOUND NO EVIDENCE OF TWISTING SKEWING, OR ABNORMAL DEFORM ATION, NO FAULTS FOUND, SYSTEM RESET AND SYSLED FLAPS IAW SUPPLEMENTAL 98-018A. (K) 2 L 7 2 4F RT A21EA 2007032100148 20070321 00148 NM 2007 3 21 BB07024 1 20070312 A 3397 WIRE BOEING 767 7672B7 1385107 NM EMERGENCY LIGHT BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 251AY 24764 FLOOR LEVEL EMERGENCY LIGHTS FOUND INOPERATIVE ON A/C LEFT SIDE. MAINTENANCE REPAIRED BROKEN WIRING. NO FURTHER FAULTS . 2 L 7 2 4F RT A1NM 2007032200034 20070322 00034 CE 2007 3 22 AMW082683 1 20070216 A 2750 1185210552 LINK BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE TE FLAP WORN A AMWA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CE 07 133YV 22126 UE133 AFTER TAKEOFF, FLAPS STUCK AT 17 DEGREES. THE CAPTAIN RETURNED TO FIELD AND DECLARED AN EMERGENCY. ACFT LANDED AND FLA PS RETRACTED TO ZERO WITH NO FURTHER INCIDENT. REMOVED AND REPLACED RT FLAP SAFETY SWITCH LINKS AND BUSHINGS. OPS CK N ORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007032200042 20070322 00042 SO 2007 3 22 RAIA00703024 1 20070310 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 814HK 145046 PRE FLT NR 5536 - DEN - EMERGENCY LIGHT, RIGHT EMERGENCY DOOR FLOODLIGHT IS OUT. MAINTENANCE RELAMPED, CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007032200046 20070322 00046 SO 2007 3 22 RAIA00703025 1 20070310 A 2750 CONTROL SYSTEM EMB 145 EMB145LR 3260212 SO TE FLAPS MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 816HK 145055 FLT NR 5546 - AUS - FLAP FAIL, STUCK AT 9 DEGREES. MAINTENANCE RESET FLAP CONTROL SYSTEM AND PERFORMED OPS CHECK, OPS C HECK GOOD AT THIS TIME. 2 L 7 2 4T RT T00011AT 2007032200068 20070322 00068 NM 2007 3 22 2007UALA00727 1 20070310 A 2621 SQUIB BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FIRE BOTTLE FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 AFT CARGO FIRE BOTTLE A FWD SQUIB TEST BAD. REPLACED SQUIB AND TESTED PER MMOV 26-23-02 . TESTED OK FOR SERVICE. SUS PECT INTERNAL DETERIORATION OF SQUIB. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032200088 20070322 00088 WP 2007 3 22 WX0A070072 1 20070317 A 3350 57761 BATTERY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 880GA 49625 DURING A ROUTINE OVERNIGHT SERVICE CHECK MAINTENANCE INSPECTION. MAINTENANCE REPORTED THAT THE EMERGENCY EGRESS PATH LI GHTING FROM ROW 25 TO ROW 32 WOULD NOT TEST. MAINTENANCE FURTHER REPORT THE REMOVAL AND REPLACEMENT OF AN EMERGENCY LI GHT POWER SUPPLY BATTERY PACK AT ROW 26 OVERHEAD. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007032200089 20070322 00089 WP 2007 3 22 WX0A070070 1 20070316 A 2410 CSD DOUG DC9 DC983 3022083 WP LEFT UNKNOWN A WX0A O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 WP 19 861GA 49557 FLIGHT 2305 DPC/MKE. FLIGHT CREW REPORT THAT THE LEFT CSD OIL TEMP WENT TO RED LINE - DISCONNECTED LEFT CSD. MAINTENAN CE REPORT, FLUSHED THE LEFT CSD AND SERVICED IT TO THE CORRECT LEVEL WITH OIL. A SATISFACTORY OPERATIONAL CHECK WAS ACC OMPLISHED PER AMM 24-10-00. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007032200163 20070322 00163 NM 2007 3 22 DXTA200702039 1 20070320 A 3230 LANDING GEAR GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE RIGHT MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 706QS 131 RT MAIN LANDING GEAR WOULD NOT RETRACT. HAD RED UNSAFE EICAS INDICATION. CONFIRMED DISCREPANCY. TROUBLESHOT AND DISCOVE RED CONNECTOR 44G1J TO HAVE AMPLE AMOUNT OF WATER IN IT. CLEANED AND DRIED CONNECTOR AND RECONNECTED. SWUNG GEAR THROUGH SEVERAL CYCLES WITH NO DEFECTS NOTED. APPLIED SEALANT TO BACK OF CONNECTOR TO PREVENT WATER INTRUSION. C/W CMP 323001 N ORMAL FUNCTIONAL TEST. WORK DONE IAW G200 REF 32-10-10 & 32-10-15. 2 L 7 2 4F 4 F RT A53NM E35NE 2007032200164 20070322 00164 EU 2007 3 22 PO72007F00001 1 20070301 A 6220 109011211105 ROD END AGUSTA A109 A119 0261102 EU PWA PT6 PT6* 52043 EA M/R DAMPER DAMAGED L PO7L O OTHER O OTHER NR NOT REPORTED 1 WP 07 198FB 429 0088 14509 PCEPU0068 DURING A WALK AROUND INSPECTION, NOTICED THAT ONE MAIN ROTOR DAMPER HAD A BEARING WHICH IS ROTATING WITHIN THE ROD END. ACCORDING TO THE FORM 8130-3 THIS PART HAD BEEN REPAIRED ON SEPT 7, 2006. (K) 1 G 7 2 3U 3 T H7EU E2NE 2007032200165 20070322 00165 SO 2007 3 22 UG8A2007GM03O 1 20070319 A 2910 D10021A04 FITTING GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU NLG LOOSE E UG8A O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 23 5117 641 4026 UPON EXTENSION OF THE LANDING GEAR DURING APPROACH IT WAS NOTED THAT THE LT HYDRAULIC QUANTITY BEGAN TO DECREASE. HYDRA ULIC QUANTITY IN THE LT SYSTEM WAS DOWN TO .3 GALLONS UPON SHUTDOWN OF THE AIRCRAFT AFTER PARKING. AFTER DEPARTING THE AIRCRAFT IT WAS NOTED THAT HYDRAULIC FLUID WAS LEAKING FROM THE NOSE WHEEL WELL AREA. TIGHTENED LOOSE NOSE GEAR DOWN LO CK HYDRAULIC LINE (B) NUT AT SWIVEL FITTING, RESERVICED HYDRAULIC FLUID AND PERFORMED SEVERAL GEAR SWINGS. NO FURTHER L EAKS WERE NOTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A12EA E25NE 2007032200166 20070322 00166 EU 2007 3 22 PO72007F00000 1 20070302 A 6220 BEARING AGUSTA A109 A119 0261102 EU PWA PT6 PT6* 52043 EA M/R DAMPER INOPERATIVE L PO7L O OTHER O OTHER NR NOT REPORTED 1 WP 07 195FB 220 0145 14502 PCEPU0059 DURING A WALK AROUND INSPECTION WE NOTICED THAT ONE MAIN ROTOR DAMPER HAD A BEARING WHICH IS ROTATING AND PULLING AWAY F ROM WITHIN THE ROD END. (K) 1 G 7 2 3U 3 T H7EU E2NE 2007032300096 20070323 00096 NM 2007 3 23 KCSA071070 1 20070320 A 5313 STRINGER BOEING 747 747236B 1384804 NM BS 480 S38L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STA 480 STRINGER 38L HAS CRACK .25 INCH. 2 L 7 4 4F A20WE 2007032300097 20070323 00097 NM 2007 3 23 KCSA071071 1 20070320 A 5313 STRINGER BOEING 747 747236B 1384804 NM BS 518 S37L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STA 518 STRINGER 37L HAS 1.75 INCH CRACK. 2 L 7 4 4F A20WE 2007032300098 20070323 00098 NM 2007 3 23 KCSA071072 1 20070320 A 5347 SEAT TRACK BOEING 747 747236B 1384804 NM BS 570 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 FWD BILGE SEAT TRACK AT STA 570 HAS 1 INCH CRACK. 2 L 7 4 4F A20WE 2007032600004 20070326 00004 SO 2007 3 26 SWIA200718034 1 20070319 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE EMERGENCY EXIT DISLODGED A SWIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 07 223SW 120291 EMERGENCY EXIT PLACARD OVER SEATS 9BC CAME OFF. REPLACED EMERGENCY EXIT SIDEWALL LIGHT AT 9BC. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2007032600006 20070326 00006 SO 2007 3 26 SWIA200718036 1 20070317 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 584SW 120352 RT WING IB FIRST PANEL FROM NACELLE HAS SEVERAL LEAKING RIVETS . FOUND STRINGER 8 CRACKED BETWEEN RIBS 7 AND 8. C/W STRI NGER 8R REPAIR IAW SRM 57-20-03 AND IAW RII 57-900-1000. 2 L 7 2 4T 4 T RT A31SO E20NE 2007032600021 20070326 00021 NM 2007 3 26 SWAA071468 1 20070321 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 714 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 714, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600022 20070326 00022 NM 2007 3 26 SWAA071494 1 20070321 A 5330 6545774 SKIN BOEING 737 7373TO 138447G NM BS 759 S19R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 759, STR 19R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600028 20070326 00028 NM 2007 3 26 SWAA071481 1 20070321 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600038 20070326 00038 NM 2007 3 26 SWAA071502 1 20070321 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM BS 310 S18R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 310, STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600039 20070326 00039 NM 2007 3 26 SWAA071500 1 20070321 A 3350 767 LAMP BOEING 737 7373G7 1384595 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED SERVICE CHECK, FOUND RIGHT FWD FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007032600041 20070326 00041 2007 3 26 SWAA071463 4 20070321 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007032600043 20070326 00043 NM 2007 3 26 SWAA071479 1 20070321 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT NO TEST A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 786SW 29811 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007032600047 20070326 00047 NM 2007 3 26 AALA20070423 1 20070302 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 905AN 29507 MIA - EMERGENCY LIGHTS FROM SEAT ROWS 15 TO 21 INOPERATIVE. REPLACED BATTERY PACK AT SEAT 20E FOR EMERGENCY LIGHTS FROM SEAT ROWS 15 TO 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007032600049 20070326 00049 NM 2007 3 26 AALA20070428 1 20070303 A 3350 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 753AN 30261 MIA - EMERGENCY LIGHT AT SEAT ROW 43 TO AFT CABIN INOPERATIVE. SECURED LOOSE CONNECTION FOR EMERGENCY LIGHT AT SEAT ROW 43 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032600050 20070326 00050 NM 2007 3 26 AALA20070429 1 20070304 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 753AN 30261 MIA - EMERGENCY SEAT MOUNTED LIGHT AT SEAT 24C HAS MISSING LENS. REPLACED LENS CAP ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032600053 20070326 00053 NM 2007 3 26 AALA20070436 1 20070305 A 3397 L317 WIRE HARNESS BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 359AA 24040 LAX - EMERGENCY LIGHT AT SEAT 4B INOPERATIVE. REPAIRED WIRE CONNECTION FOR EMERGENCY LIGHT AT SEAT 4B. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007032600055 20070326 00055 EA 2007 3 26 TRAX200700383 1 20070317 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 837AS 7271 LEFT FS 484 LBL 36 ANGLE CRACKED. [SUP 05-02-07] COMPLIED WITH REPAIR TO INTERCOSTAL AT F.S. 484, LBL 36, IAW REO 601R- 53-41-059, PRESSURIZATION CHECK GOOD, IAW CRJ MM 21-30-00. 2 L 7 2 4F RT A21EA 2007032600056 20070326 00056 EA 2007 3 26 TRAX200700384 1 20070317 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 920EV 7810 FLAPS FAIL 0 DEGREES. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007032600058 20070326 00058 EA 2007 3 26 TRAX200700386 1 20070317 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 838AS 7276 FLAPS FAIL CAUTION WHEN SELECTED FROM 0 TO 8 INDICATION SHOWED ALL FLAPS AT 0. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007032600059 20070326 00059 EA 2007 3 26 TRAX200700387 1 20070317 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 834AS 7254 FLIGHT ATTENDANT`S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007032600061 20070326 00061 NM 2007 3 26 AALA20070444 1 20070306 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 796AN 30796 DFW - OVERHEAD EMERGENCY LIGHT AT SEAT 20C MISSING. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD SEAT 20C. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032600063 20070326 00063 NM 2007 3 26 AALA20070432 1 20070304 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 394AN 29431 MIA - EMERGENCY LIGHT AT SEAT 25G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 25G. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A1NM 2007032600067 20070326 00067 WP 2007 3 26 AALA20070424 1 20070302 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7544A 53026 SFO - EMERGENCY LIGHT AT SEAT 16D HAS MISSING BULB. RELAMPED EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007032600068 20070326 00068 WP 2007 3 26 AALA20070425 1 20070302 A 3350 BEZEL DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7544A 53026 SFO - EMERGENCY LIGHT AT SEAT 16D HAS MISSING BEZEL. REPLACED BEZEL FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007032600071 20070326 00071 WP 2007 3 26 AALA20070420 1 20070303 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9625W 53595 LGA - SEAT MOUNTED EMERGENCY LIGHT IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR AFT SEAT MOUNTED EMERGENCY LIGHT IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007032600072 20070326 00072 NM 2007 3 26 AALA20070422 1 20070302 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 905AN 29507 MIA - EMERGENCY LIGHT AT RIGHT HAND AFT OVERWING OUTSIDE INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT HAND AFT OVERWI NG OUTSIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007032600082 20070326 00082 NM 2007 3 26 AALA20070437 1 20070305 A 3350 MODULE BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR AISLE EXIT SIGN INOPERATIVE. REPLACED LIGHT MODULE FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR AISLE EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032600083 20070326 00083 WP 2007 3 26 AALA20070415 1 20070301 A 7931 1163P0041 PRESSURE SWITCH DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RT ENGINE OIL INOPERATIVE A AALA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 SW 21 577AA 53154 725673 DFW - INFLIGHT ON APPROACH RIGHT ENGINE CLOGGED STRAINER INDICATION ILLUMINATED. CREW PERFORMED IN FLIGHT SHUTDOWN. LA NDED DFW WITHOUT INCIDENT. ALL CHECKS NORMAL. INSTALLED NEW FILTER AND OIL FILTER DIFFERENTIAL PRESSURE SWITCH. DRAIN ED AND REPLENISHED OIL TANK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007032600087 20070326 00087 EA 2007 3 26 TRAX200700370 1 20070313 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 ASD (PAX DOOR) OUTER HANDLE CRACKED. PAX DOOR OUTER HANDLE REMOVED AND REPLACED. 2 L 7 2 4F RT A21EA 2007032600088 20070326 00088 EA 2007 3 26 TRAX200700371 1 20070316 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 640 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 LEFT SIDE 640 FRAME CRACKED FWD SIDE BETWEEN STR 9 AND ENGINE SUPPORT BEAM WEB AFT OF ENGINE SUPPORT BEAM UPPER OUTBOARD ATTACH ANGLE. 2 L 7 2 4F RT A21EA 2007032600089 20070326 00089 EA 2007 3 26 TRAX200700372 1 20070316 A 5310 FRAME CNDAIR CL600 CL6002C10 1390015 EA BS 310 S26L/R CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 CORROSION ON FRAME LEG AT FS 310 BETWEEN STR 26L TO 26R. 2 L 7 2 4F RT A21EA 2007032600091 20070326 00091 EA 2007 3 26 TRAX200700374 1 20070316 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 837AS 7271 EMERGENCY EXIT ARROW ON WARDROBE WORN. REMOVED WORN EMERGENCY EXIT ARROW. INSTALLED SERVICEABLE EMERGENCY EXIT ARROW IA W CRJ AMM 11-30-02. 2 L 7 2 4F RT A21EA 2007032600092 20070326 00092 EA 2007 3 26 TRAX200700375 1 20070316 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 837AS 7271 EXIT PLACARD ON 2ND STAIR WORN (PAX DOOR). REMOVED EXIT PLACARD FROM 2ND STAIR ON PAX DOOR INSTALLED SERVICEABLE EXIT P LACARD P/N S1594-18, ON 2ND STAIR OF PAX DOOR IAW CRJ 200 AMM 11-30-00-944-001. SUPPLEMENTAL - SDR CLOSED 03/22/07. 2 L 7 2 4F RT A21EA 2007032600093 20070326 00093 EA 2007 3 26 TRAX200700376 1 20070316 A 5310 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 338 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 837AS 7271 PAX DOOR FRAME CRACKED AT FS 338. REPAIRED PAX DOOR FRAME IAW EO'S REO 601R-52-11-1205 AND REO 601R-52-11-402. 2 L 7 2 4F RT A21EA 2007032600104 20070326 00104 NM 2007 3 26 2007UALA00388 1 20070210 A 2420 756603D GCU BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RIGHT FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 225UA 18944 30554 CREW RECEIVED EICAS MSG FOR LEFT AC BUS TIE FAILED, AND STATUS MSG SHOWING BOTH LEFT AND RIGHT FAILED. *S/D* ELEC BUSS ISOLATION MSG L AND R EICAS. RIGHT BUSS TIE ISOLATION LIGHT ONLY OVERHEAD. RESTORED ELMS EU'S, RAN BOTH ENGINES AND T RANSFERRED PWR BETWEEN ENG GENERATORS, APU AND EXTERNAL PWR, LEFT & RIGHT BUSS TIES OPERATE NORMALLY, PER MAINT TIPS. A IRCRAFT OK FOR SERVICE. ENGRNG REQUESTED UNIT REMOVAL. KNOWN PROB WITH GCU & EXISTING SERVICE BULLETIN CORRECTS. MOD DONE BY ATTRITION. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007032600105 20070326 00105 WP 2007 3 26 UPX2007F00000 1 20070304 A 6200 BEARING ROBSIN R44 R44RAVENII 7640122 WP LYC O540 IO540* 41532 EA CLUTCH LACK OF LUBE E UPXC O OTHER O OTHER NR NOT REPORTED 1 AL 03 74435 1347 3087 10718 CLUTCH MAKING UNUSUAL NOISES ON COAST DOWN. UPON REMOVAL THE BEARINGS IN THE CLUTCH FELT ROUGH AND DRY. COMPONENT RETU RNED TO MFG FOR O/H. (K) 1 G 7 1 3O 3 O H11NM 1E4 2007032600108 20070326 00108 EA 2007 3 26 VNAA0703007 1 20070310 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT TE FLAP FAILED A VNAA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 GL 05 249PS 6867 7926 CREW REPORTED A FLAPS FAIL CAS MESSAGE ON DESCENT. CREW LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLAC ED THE BRAKE AND POSITION SENSOR UNIT IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SER VICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007032600110 20070326 00110 EA 2007 3 26 VNAA0703010 1 20070315 A 7100 1211508003 ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE VG LEAKING A VNAA O OTHER K FLUID LOSS NR NOT REPORTED 1 GL 05 708PS 6669 10160 CREW REPORTED FUEL RUNNING OUT OF RIGHT ENGINE NACELLE. MAINTENANCE INSPECTED AND FOUND THE LEAK OCCURING AT THE VG ACT UATOR WITH THE FUEL PUMP ON. MAINTENANCE REMOVED AND REPLACED THE NR 2 VG MASTER ACTUATOR IN ACCORDANCE WITH THE AIRCRA FT MAINTENANCE MANUAL. NO FURTHER DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007032600112 20070326 00112 WP 2007 3 26 WX0A070066 1 20070312 A 3350 AD4002P BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 861GA 49557 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MILWAUKEE MAINTENANCE REPORTED THAT THE FLIGHT DECK EMERGENCY LIGHTS WOULD NOT TEST. MILWAUKEE MAINTENANCE FURTHER REPORT THE REMOVAL AND REPLACEMENT OF THE BATTERY PACK AT EMERGENCY LIGH T POWER SUPPLY BS-23. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007032600114 20070326 00114 WP 2007 3 26 03200701 2 20070320 A 7200 ENGINE GULSTM 690TP 690A 0141722 SW GARRTT TPE331 TPE3315 01514 WP HARTZL HCB3T HCB3T* GL RIGHT SHUTDOWN E O9IA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION NR NOT REPORTED 1 NM 09 290PF 11290 0677706015 WHILE ON SHORT FINAL (APPROX .2500 MILE), PILOT REPORTED THE RT ENGINE SHUTDOWN. AS HE WAS ON SHORT FINAL HE DID NOT NO TICE IF THERE WAS A CORRESPONDING INITIATION OF THE NTS SYSTEM OR IF THE ENGINE/PROP BEGAN TO FEATHER. WHEN THE PROBLEM WAS NOTICED THE PILOT ATTEMPTED TO ADVANCE POWER ON THE NR 1 ENGINE WITH NO EFFECT. LT ENGINE HAD ALSO SHUTDOWN. BOTH ENGINES/PROPS WERE PULLED BACK INTO FEATHER AND THE AIRCRAFT LANDED. AFTER DEBRIEFING THE CAPTAIN MOTORED THE ENGINES, RESTARTED THEM, TAXIED THE AIRCRAFT, ADVANCED POWER TO 100 PERCENT TO ACTIVATE THE EPA KITS, AND SHUT THE AIRCRAFT DOWN . FUEL TANKS WERE SUMPED WITH NO NOTICEABLE CONTAMINATION OR WATER. FUEL FILTERS WERE REMOVED AND INSPECTED. NO NOTIC 1 H 7 2 3T 4 T 2A4 E4WE 6 C P15EA 2007032600117 20070326 00117 NM 2007 3 26 UPS07549503 1 20070222 A 5311 146N102886 FRAME BOEING 757 75724APF 1384969 NM BS 1340 S26R DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 418UP 23905 INSPECTION TYPE:C DENT IN AFT CARGO COMPARTMENT FUSELAGE FRAME STA 1340 STR 26R. COMPLIED WITH EA 757-5262-27-A1614, & UPS EO B757-5310-26361-A. 2 L 7 2 4F RT A2NM 2007032600119 20070326 00119 NM 2007 3 26 UPS07549505 1 20070222 A 5311 14N102489 FRAME BOEING 757 75724APF 1384969 NM BS 720 S24-25L DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 418UP 23905 INSPECTION TYPE:C DENT IN FORWARD CARGO COMPARTMENT FUSELAGE FRAME STA 720, BETWEEN S24L TO S25L. COMPLIED WITH EA 757- 5332-27-A1610 & UPS EO B757-5310-26369-A. 2 L 7 2 4F RT A2NM 2007032600124 20070326 00124 NM 2007 3 26 UPS07549510 1 20070226 A 5412 311N3271 BULKHEAD BOEING 757 75724APF 1384969 NM NR 2 PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 418UP 23905 INSPECTION TYPE:C NR 2 PYLON LOWER I/B CORNER OF MIDSPAR BULKHEAD IS HEAVILY CHAFED. COMPLIED WITH EA 757-5453-27-A1615 WITH NO DEVIATIONS AND EO B757- 410-26326. 2 L 7 2 4F RT A2NM 2007032800226 20070328 00226 NM 2007 3 28 QXEA200700422 1 20070314 A 5415 MOUNT DHAV DHC8 DHC8202 2809007 NM LT MLG CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - LEFT MAIN LANDING GEAR ACTUATOR LOWER MOUNT ON H MEMBER HAS FRETTING CORROSION AROUND LOWER BOLT HOLES. REPAIR ED IAW RD8-54-1178. 2 H 7 2 4T RT A13NM 2007032600126 20070326 00126 SO 2007 3 26 C2XA07TY013 1 20070321 A 5540 NUT PLATE EMB 145 EMB145EP 3260221 SO RUDDER MISSING A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 TYS - DURING A CURRENT 1C INSPECTION FOUND A MISSING NUT PLATE FOR THE PROTRACTOR ATTACHMENT ON RUDDER 2. MAINTENANCE R EPAIRED RUDDER 2 IAW EC 5540-01063. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. 2 L 7 2 4F RT T00011AT 2007032600129 20070326 00129 NM 2007 3 26 SWAA071445 1 20070320 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 582 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 582, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600130 20070326 00130 NM 2007 3 26 SWAA071443 1 20070320 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 584 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 584, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600131 20070326 00131 NM 2007 3 26 SWAA071429 1 20070321 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 410 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT NR 2 RADIO ALTIMETER ANTENNA CUTOUT BS 410, BL 0. REPAIRED SK IN PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600132 20070326 00132 NM 2007 3 26 SWAA071442 1 20070320 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 460 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 460, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600133 20070326 00133 NM 2007 3 26 SWAA071441 1 20070320 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 450 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 450, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600134 20070326 00134 NM 2007 3 26 SWAA071424 1 20070318 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 767 S20L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 20L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600137 20070326 00137 NM 2007 3 26 SWAA071422 1 20070318 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM BS 727 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600138 20070326 00138 NM 2007 3 26 SWAA071459 1 20070320 A 5753 6546430121 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 DURING SCHEDULED C4 CHECK, FOUND LEFT WING INBOARD FORE FLAP DELAMINATED AT UPPER INBOARD SURFACE. REMOVED AND REPLACED FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2007032600139 20070326 00139 NM 2007 3 26 SWAA071453 1 20070320 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 400 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 16R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007032600140 20070326 00140 NM 2007 3 26 SWAA071452 1 20070320 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 520 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 16L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007032600143 20070326 00143 NM 2007 3 26 SWAA071461 1 20070320 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007032600146 20070326 00146 SO 2007 3 26 FDKA200703094 1 20070301 A 3350 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 840MJ 145429 FDM 6017 MCO-BNA (1845 PHX LCL). FLOOR EMERGENCY LIGHTS OUT AT ROW 12. MX REPAIRED WIRE AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007032600148 20070326 00148 NM 2007 3 26 FDKA200703100 1 20070308 A 3350 1317 LAMP DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHT INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 926HA 114 FDM 6190 JFK-BDL (0803 PHX LCL). MAIN CABIN DOOR EMERGENCY EXIT LIGHT INOP. MX REPLACED BULB. 2 H 7 2 4T RT A13NM 2007032600149 20070326 00149 NM 2007 3 26 SWAA071435 1 20070320 A 3350 6556633 SIGN BOEING 737 7373H4 1384600 NM EMERGENCY EXIT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2007032600150 20070326 00150 NM 2007 3 26 SWAA071450 1 20070320 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 807 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 18L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007032600151 20070326 00151 NM 2007 3 26 SWAA071447 1 20070320 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 767 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007032600152 20070326 00152 NM 2007 3 26 SWAA071449 1 20070320 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 747 S13R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 13R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007032600153 20070326 00153 NM 2007 3 26 SWAA071448 1 20070320 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 747 S18R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 18R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007032600154 20070326 00154 NM 2007 3 26 SWAA071457 1 20070320 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727B S26R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007032600155 20070326 00155 NM 2007 3 26 DL757070218 1 20070320 A 5330 143N34714 SKIN BOEING 757 757232 1384965 NM FS 606-614 S27R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 636DL 23763 DURING CURRENT HMV, INSPECTION NOTED A SLIGHT GAP BETWEEN THE RIGHT RADIO ALTIMETER RECEIVER ANTENNA FAIRING AND THE FUS ELAGE SKIN AT FS 610 AND S-27R. UPON REMOVAL OF THE ANTENNA FAIRING A DENT WITH CRACK WAS DISCOVERED. THE DENT AND CRA CK WAS TRIMMED OUT FROM FS 606 TO 614, RIGHT ALONG THE PAD UP AT S-27R. THE TRIM OUT MEASURED 4.7 INCHES BY 8 INCHES. A BOEING APRPOVED REPAIR WAS INSTALLED PER ERA 457354-14. 2 L 7 2 4F RT A2NM 2007032600157 20070326 00157 NM 2007 3 26 DL76L070220 1 20070320 A 5311 145T138212 FRAME BOEING 767 767332 1382001 NM FS 903 RBL 90 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 184DN 27111 DURING CURRENT HMV, A CRACK WAS FOUND ON THE INNER CHORD LOWER END OF THE RHS FRAME SEGMENT AT FS 903.5 AND RBL 90. THE CRACK IS LOCATED AT WL 190, AND WAS LOCATED AT THE 0.25 IN RADIUS TRANSITION BETWEEN THE CHORD FLANGES. A BOEING APPRO VED REPAIR AND FOLLOW UP REPETITIVE INSPECTIONS WERE SET UP PER ERA 460452-14AD. 2 L 7 2 4F RT A1NM 2007032600158 20070326 00158 NM 2007 3 26 DL76L070221 1 20070320 A 5311 145T138211 FRAME BOEING 767 767332 1382001 NM FS 903 LBL 90 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 184DN 27111 DURING CURRENT HMV, A CRACK WAS FOUND ON THE INNER CHORD LOWER END OF THE LBL 90 FRAME SEGMENT AT FS 903.5. THE CRACK W AS AT WL 190, AND WAS AT THE 0.25 INCH RADIUS TRANSITION BETWEEN THE CHORD FLANGES. A BOEING APPROVED REPAIR AND FOLLOW UP INSPECTIONS WERE INSTALLED PER 460453-14AD 2 L 7 2 4F RT A1NM 2007032600161 20070326 00161 NM 2007 3 26 DL76L070224 1 20070320 A 3350 CONNECTOR BOEING 767 767332 1382001 NM EMERGENCY LIGHT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 197DN 28454 EMERGENCY LIGHTS STAY ON WHEN COCKPIT SWITCH SET TO OFF. REPAIRED PUSHED BACK PIN AT PIN 33 OF PLUG D1650 AFT FLT ATTEN DANT PANEL. EMERGENCY LIGHTS OPS CHK OK. 2 L 7 2 4F RT A1NM 2007032600163 20070326 00163 NM 2007 3 26 DL757070226 1 20070321 A 7997 TRANSMITTER BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE FAULTED A DALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 27 674DL 20026 728776 25979 728776 THE RT ENG HAD LOW OIL PRESSURE AND FOLLOWED THE THROTTLE MOVEMENT. ENG T/S TEAM FOUND THE NR 2 ENG OIL PRESS TRANSMITT ER TO BE AT FAULT. REPLACED SAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032300063 20070323 00063 2007 3 23 200703211 4 20070318 A 3415 2015G2H2H7A PROBE EMB ERJ170 ERJ170100SE 3260406 EU NR 4 DEFECTIVE A UHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 863RW 17000100 FLIGHT 6482 ATL TO MDW AT ABOUT 90 KTS ACCELERATING, CREW RECEIVED AMBER -IAS- COMPARATOR MESSAGES ON THE AIRSPEED TAPES . CREW REJECTED THE TAKEOFF AND RETURNED TO GATE. MAINT CYCLED POWER AND ADSP BIT RAN OK, NO SPLIT, RESECURED BRAKE TE MP SENSOR AT RIGHT O/B BRAKE, OPS CHECK GOOD. REPEAT DISCREPANCY 03/19 FLIGHT 6459 HOU TO ATL IAS FLAG APPEARED ON BOT H PFD DURING TAKEOFF ROLL. TAKEOFF WAS ABORTED 80-90 KIAS. FLT CREW RESET A/C POWER, OCM REPORTED NO FAULT CODES FOUND , GETTING DOWNLOAD IN ATL. DOWNLOAD INDICATES NR 4 ADS PROBE AS POTENTIAL PROBLEM. REMOVED AND REPLACED NR 4 ADS PROBE . OPS CHECK GOOD. 2 L 7 2 4F RT A56NM 2007032300064 20070323 00064 EU 2007 3 23 YENA2007018 1 20070318 A 7100 COWLING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE DETACHED A YENA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 EA 15 635JB 2725 V12220 FLT 830, PBI-JFK, AIR RETURN TO PBI. ENGINE COWL SEPARATED FROM ENGINE NR 1. DAMAGE NOTED ON INBOARD LEADING EDGE ON L EFT WING AND OTHER AREA'S OF ENGINE COWL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032300065 20070323 00065 NM 2007 3 23 ANCF200600047 1 20070228 A 5753 113T23018A SKIN BOEING 767 767259 1385136 NM PWA 4056 PW4056 NE TE FLAP DELAMINATED W ANCF K NONE O OTHER IN INSP/MAINT 1 SO 23 986AN 72243 24835 NON ROUTINE WRITEUP. N: 448686-135: RT IB FLAP. AFT FLAP LOWER SKIN WITH DELAMINATION. DELAMINATION WAS FOUND ON THE WED GE LOWER AND UPPER SKIN BETWEEN STA:IFS 277 TO ISF 293 AREA LONG 15.5 INCHES WIDE 11.5 INCHES. IN RT IB WING FLAP. THE AFT FLAP WAS REPLACED IAW 27-51-06 PAGES 201 TO 217. 2 L 7 2 4F 4 F RT A1NM E24NE 2007032300066 20070323 00066 EU 2007 3 23 AALA20070412 1 20070228 A 3350 MODULE AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14061 471 MIA - EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR INOPERATIVE. REPLACED BATTERY PACK AND MODULE ASSEMBLY FOR INOPERATIVE EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007032300067 20070323 00067 WP 2007 3 23 AALA20070413 1 20070228 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 561AA 53091 LGA - EMERGENCY EXIT LIGHT AT RIGHT AFT LOWER OVERWING INOPERATIVE. REPLACED BATTERY PACKS AT BOTH MID AND AFT FOR LOWE R OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007032300068 20070323 00068 EU 2007 3 23 AALA20070411 1 20070227 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 90070 513 MIA - EMERGENCY LIGHTS FROM SEAT ROWS 7C TO 18C INOPERATIVE. REPLACED OVERHEAD LIGHT ASSEMBLIES FOR EMERGENCY LIGHTS FR OM SEAT ROWS 7C TO 18C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007032300069 20070323 00069 NM 2007 3 23 AALA20070417 1 20070302 A 3397 PIN BOEING 767 767323 1385205 NM CONNECTOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 370AA 25197 DFW - EMERGENCY LIGHTS AT SEAT 17B INOPERATIVE. RESEATED WALL TO SEAT CONNECTOR PIN AT SEAT 17B FOR INOPERATIVE EMERGEN CY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007032300070 20070323 00070 NM 2007 3 23 AALA20070418 1 20070302 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 370AA 25197 DFW - EMERGENCY LIGHT AT SEAT ROW 23B INOPERATIVE. RELAMPED OVERHEAD EMERGENCY LIGHT AT ROW 23B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007032300071 20070323 00071 EA 2007 3 23 TRAX200700380 1 20070316 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 838AS 7276 FLAPS FAIL AT 0 ON APP. EMERGENCY DECLARED. FLT 4762 DEL 35 MINS. 2 L 7 2 4F RT A21EA 2007032300072 20070323 00072 EA 2007 3 23 TRAX200700381 1 20070317 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 STA 280 AFT FLOOR SUPPORT ANGLE HAS SURFACE CORROSION AT BL 0. ALL WORK DONE IAW REO 601R-53-11-926 2 L 7 2 4F RT A21EA 2007032300073 20070323 00073 SO 2007 3 23 C2XA07CL033 1 20070318 A 2530 500064001 COFFEEMAKER EMB 145 EMB145EP 3260221 SO GALLEY SMOKE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 17928 145007 CMH FLIGHT 2930 THE CREW REPORTED THE COFFEE POT WAS SMOKING WHEN TURNED ON.THE COFFEE POT WAS PLACED ON MEL AND THE AIR CRAFT WAS RELEASED FOR SERVICE. MAINTENANCE INSPECTED AND REPLACED THE NR 2 COFFEE POT BREWER.OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2007032300074 20070323 00074 WP 2007 3 23 ABXA070076 1 20070320 A 2120 UNKNOWN DOUG DC9 DC932 3022066 WP COCKPIT ODOR A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 982AX 47317 AIRCRAFT HAS STRONG ODOR OF FUEL OR SOLVENT IN COCKPIT AND CARGO AREA. NO FUEL LEAK OR ODOR NOTED IAW DC9 MM 28-00-00. 2 L 7 2 4F A6WE 2007032300075 20070323 00075 NM 2007 3 23 ASAA0771542 1 20070320 A 5330 143A325216 SKIN BOEING 737 737790 13844CN NM BS 365-420 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 RIGHT SIDE OF FUSELAGE FWD OF FWD CARGO DOOR HAS A DENT ON LOWER CENTER. BS 365 REPAIRED IAW EA 53 30 02188. 2 L 7 2 4F RT A16WE 2007032300076 20070323 00076 NM 2007 3 23 ASAA0741541 1 20070320 A 5320 6517684638 INTERCOSTAL BOEING 737 7374Q8 138447Q NM BS 294-303 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 INTERCOSTAL CRACKED. REPLACED INTERCOSTAL PER SRM 51-40-01 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007032300077 20070323 00077 WP 2007 3 23 ABXA070078 1 20070315 A 5311 99118777 FRAME DOUG DC9 DC941 302207N WP FS 1209 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 FS 1209 CANTED FRAME CRACKED BETWEEN LONGERON 14 AND 15 LEFT SIDE. REPAIRED IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 2007032300078 20070323 00078 WP 2007 3 23 ABXA070077 1 20070315 A 5330 5910228187 SKIN DOUG DC9 DC941 302207N WP BS 1197 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 AFT FUSELAGE SKIN CRACKED 2 PLACES APPROXIMATELY FS 1197, LEFT SIDE. REPAIRED AREA IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 2007032600002 20070326 00002 NM 2007 3 26 SWAA071493 1 20070321 A 5330 6545765 SKIN BOEING 737 7373TO 138447G NM BS 503C S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503C, STR 11R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600005 20070326 00005 EA 2007 3 26 SWIA200718035 1 20070319 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EMERGENCY LIGHTS DISCONNECTED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 908SW 7540 LAST PART EMERGENCY LIGHTS WILL NOT ILLUMINATE.SECURED STRIP CONNECTION. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2007032600007 20070326 00007 SO 2007 3 26 SWIA200718037 1 20070316 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE EMERGENCY LIGHTS DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 563SW 11839 11839 120338 A GOOD PORTION OF THE EMERGENCY LIGHT SYSTEM DOES NOT TEST. REPLACED NR 2 BATTERY PACK IAW MM 33-50-02. OPERATIONAL CHE CKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2007032600013 20070326 00013 EA 2007 3 26 TRAX200700392 1 20070318 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 349 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 CORROSION AT FS 349 RBL 37 SERVICE DOOR AFT ANGLE. 2 L 7 2 4F RT A21EA 2007032600015 20070326 00015 EA 2007 3 26 TRAX200700394 1 20070318 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 914EV 7752 EXTERNAL EMERGENCY LIGHT INOP NEAR RT WING MOST FORWARD. 2 L 7 2 4F RT A21EA 2007032600016 20070326 00016 EA 2007 3 26 TRAX200700395 1 20070318 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 838AS 7276 FLAPS AGAIN FAILED AT ZERO. PERFORMED ZERO FLAP LANDING ON 41,000 LB CARD. REPEAT WRITE-UP. EMERGENCY DECLARED. FLTS 4913, 4818, 4683 CX. 2 L 7 2 4F RT A21EA 2007032600023 20070326 00023 NM 2007 3 26 SWAA071471 1 20070321 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 706 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 DURING SCHEDULED C4 CHECK, FOUND RIGHT KEEL BEAM SKIN CRACKED AT BS 706, LBL 6.50. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007032600051 20070326 00051 NM 2007 3 26 AALA20070431 1 20070304 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 394AN 29431 MIA - EMERGENCY LIGHT AT SEAT 27B INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 27B. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A1NM 2007032600062 20070326 00062 NM 2007 3 26 AALA20070445 1 20070306 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 968AN 30095 MIA - EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A16WE 2007032600077 20070326 00077 NM 2007 3 26 AALA20070446 1 20070306 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 968AN 30095 MIA - EMERGENCY LIGHT AT SEAT 15D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A16WE 2007032600080 20070326 00080 NM 2007 3 26 AALA20070442 1 20070306 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 796AN 30796 DFW - OVERHEAD EMERGENCY LIGHT AT SEAT 30C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT OVERHEAD SEAT 30C. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032600084 20070326 00084 NM 2007 3 26 AALA20070416 1 20070301 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 907AN 29509 MIA - EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT NUMBER FO UR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007032600094 20070326 00094 EA 2007 3 26 TRAX200700377 1 20070316 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 461 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 FLOORBEAM FITTING CRACKED AT UPPER AFT CORNER STA 461 RBL 9 INBOARD FITTING. (SUPPLEMENTAL 28 MARCH 07) INSTALLED N EW REPLACEMENT FITTING IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007032600095 20070326 00095 EA 2007 3 26 TRAX200700378 1 20070316 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 461 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 STA 461 FLOORBEAM FITTING CRACKED RBL 9 OUTBOARD SIDE. INSTALLED NEW FITTING COMPLETE WITH LOCK FASTENERS IAW CRJ 200 SRM 51-42-21 . 2 L 7 2 4F RT A21EA 2007032600102 20070326 00102 EA 2007 3 26 COMA0760264 1 20070317 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 430CA 7461 FLIGHT 9438 - FLOOR FORWARD EMERGENCY LIGHT INOP. REPAIRED WIRE AT CONNECTOR, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007032600115 20070326 00115 WP 2007 3 26 070067 1 20070313 A 3350 AD4002P BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 861GA 49557 DURING A ROUTINE OVERNIGHT MAINTENANCE INSPECTION MAINTENANCE REPORTED THAT THE AISLE EMERGENCY LIGHTS AT ROWS 7 THROUGH 11 WOULD NOT TEST. MILWAUKEE MAINTENANCE FURTHER REPORT THE REMOVAL AND REPLACEMENT OF AN EMERGENCY LIGHT POWER SUPPLY BATTERY PACK AT FUSELAGE STATION 500. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLAN E HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007032600123 20070326 00123 NM 2007 3 26 UPS07549509 1 20070226 A 5412 311N3271 BULKHEAD BOEING 757 75724APF 1384969 NM NR 2 PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 418UP 23905 INSPECTION TYPE:C NR 2 PYLON LOWER O/B CORNER OF MIDSPAR BULKHEAD IS HEAVILY CHAFED. COMPLIED WITH EA 757-5453-27-A1615 WITH NO DEVIATIONS AND EO B757- 5410-18134B. 2 L 7 2 4F RT A2NM 2007032600135 20070326 00135 NM 2007 3 26 SWAA071423 1 20070318 A 5330 6545778 SKIN BOEING 737 7373H4 1384600 NM BS 955 S24R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 955, STR 24R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600136 20070326 00136 NM 2007 3 26 SWAA071421 1 20070318 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM BS 264 S14R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 264, STR 14R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600147 20070326 00147 SO 2007 3 26 FDKA200703098 1 20070306 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 FDM 6173 RDG (1157 PHX LCL) OVERHEAD EXIT LIGHT INOP ON ONE SIDE. MX RESET, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007032600162 20070326 00162 2007 3 26 DL777070225 4 20070321 A 2397 CONNECTOR BOEING 777 777232 1385232 NM VIDEO MONITOR LOOSE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 861DA 29952 IFE MONITOR AT 52G HAD A PUFF OF SMOKE COME OUT OF IT DURING DESCENT. FOUND POWER HARNESS MONITOR CONNECTOR LOOSE. SEC URED CONNECT INSPECTED ALL CONNECTORS AND WIRING AT ROWS 51, 52 AND 53. REMOVED AD REPLACED SUSPECT MONITOR AT SEAT 52G . OPS CKD ALL EFX ENTERAINMENT AT SEAT 52G. OPS CK NORMAL P/N RD-KW7670-04 S/N OFF D308354 S/N D306137. REMOVED PLACA RD A/P 1984218. 2 L 7 2 4F RT T00001SE 2007032600164 20070326 00164 NM 2007 3 26 DL738070227 1 20070322 A 5330 SKIN BOEING 737 737832 13844CF NM FS 268 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3755D 29627 THE FUSELAGE SKIN WAS GOUGED AND DENTED JUST ABOVE THE LAP JOINT AT S-24L AT FS 268. WHILE REMOVING THE DAMAGE TO THE F USELAGE SKIN, THE STRINGER 24L INCURRED TOOLING DAMAGE. A STRINGER REPAIR AND AN EXTERNAL SKIN REPAIR WERE INSTALLED PE R 460778-14. 2 L 7 2 4F RT A16WE 2007032600167 20070326 00167 NM 2007 3 26 CALA0700138 1 20070322 A 5315 6545410199 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 727B CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 77303 23354 INSPECTION FOUND A .25 INCH CRACK IN FLOORBEAM AT STA 727B, LBL 44. THE FLOORBEAM WAS REPAIRED IAW ECRA 5311-01303. 2 L 7 2 4F RT A16WE 2007032600170 20070326 00170 EA 2007 3 26 COMA0760271 1 20070320 A 3397 64645 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT FAULTY A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 914CA 7012 FLIGHT 5199 - EMERGENCY LIGHTS INOP FROM ROW 8 THROUGH 12. EMERGENCY LIGHT STRIP CRACKED AT ROW 11. REPLACED POWER SUP PLY STRIP. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007032600172 20070326 00172 NM 2007 3 26 AWXA200700379 1 20070305 A 5754 65C267995 SKIN BOEING 737 7373G7 1384595 NM NR 1 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - LEFT WING NR 1 SLAT LOWER SURFACE CRACKED, SS 340. REPAIRED LEFT WING NR 1 SLAT LOWER SURFACE, SS 340 IAW B737-30 0 SRM 57-43-01 ON LOG PAGE 5939533. 2 L 7 2 4F RT A16WE 2007032600173 20070326 00173 NM 2007 3 26 AWXA200700380 1 20070310 A 5340 69353521 STRINGER CLIP BOEING 737 7373G7 1384595 NM BS 500D S25R CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED FORWARD CARGO COMPARTMENT STRINGER CLIP, BS 500D, S25R. REPLACED FORWARD CARGO COMPARTMENT STRINGER CLIP, BS 500D, S25R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007032700005 20070327 00005 EA 2007 3 27 SWIA200718041 1 20070321 A 5610 NP13932210 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 418SW 7446 AT FL330, CO-PILOTS WINDOW SHATTERED. REPLACED RIGHT SIDE WINDOW IAW RII 56-220-1000 AND MM 56-12-01. OPERATIONAL CHEC KS GOOD. 2 L 7 2 4F RT A21EA 2007032700006 20070327 00006 EA 2007 3 27 SWIA200718042 1 20070223 A 5310 BOLT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 864AS 7502 FOUND CORROSION ON WARDROBE FLOOR BOLTS, DISCOVERED DURING C-CHECK INSPECTION. REPLACED 4 WARDROBE FLOOR BOLTS IAW CRJ2 00 AMM 20-21-00-910-801. 2 L 7 2 4F RT A21EA 2007032700009 20070327 00009 EA 2007 3 27 SWIA200718045 1 20070223 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 864AS 7502 FS 280 9L AND 9R BRACKETS ANGLES CRACKED INBOARD AND OUTBOARD (ALL 4, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED C LIPS AND FILLER PER CRJ200 SRM 51-40-2 AND BOMBARDIER REO 601R-53-11-171 REV C. 2 L 7 2 4F RT A21EA 2007032700010 20070327 00010 EA 2007 3 27 SWIA200718025 1 20070316 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 752SK 10209 ONE CABIN EMERGENCY LIGHT INOP. RELAMPED AFT CABIN EMERGENCY LIGHT IAW MM CH 33-51-09. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007032700011 20070327 00011 EA 2007 3 27 SWIA200718026 1 20070313 A 5210 MECHANISM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CONTAMINATED A SWIA O OTHER C F.O.D. TX TAXI/GRND HDL 1 NM 07 903SW 7425 FOUND MAIN CABIN DOOR WILL NOT OPEN FROM INSIDE/OUTSIDE. REMOVED EXCESSIVE LUBRICATION FROM HANDLE MECHANISM. OPERATIO NAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007032700013 20070327 00013 NM 2007 3 27 752006 1 20070315 A 3610 8988061 REGULATOR VALVE BOEING 747 747228F 1384895 NM GE CF6 CF650E2 30018 NE NR 1 ENGINE LEAKING A Q2SA O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 63 752SA 21255 530291 NR 1 ENGINE MAXIMUM TAKEOFF POWER. PILOT'S PANEL ENGINE LOOP FAULT LIGHT ILLUMINATED INTERMITTENTLY FOLLOWED BY INTERMI TTENT FIRE WARNING. NACELLE TEMPERATURE FLUCTUATED 5 TO FULL SCALE. SET CLIMB POWER. NACELLE TEMPERATURE A & B SETTLE D TO 2.0. TAKEOFF POWER 111.2 AT 14 DEGREES C. 2997, EGT 913 DEGREES C CONTINUED TO PANC. FOUND PRSOV AT FAULT. REMOVE D AND REPLACED PRSOV IN ACCORDANCE WITH AMM 36-11-19. LEAK CHECK GOOD IN ACCORDANCE WITH AMM 71-00-00. OPERATIONAL CHE CK GOOD IN ACCORDANCE WITH AMM 36-11-00. 2 L 7 4 4F 4 F A20WE E23EA 2007032700016 20070327 00016 NM 2007 3 27 DL764070199 1 20070311 A 4950 BLEED VALVE BOEING 767 767432ER 1385134 NM APU INOPERATIVE A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 836MH 10903 29709 032704 APU BLEED VALVE WILL NOT OPEN. REPLACED APU BLEED VLV PER MM 36-11-10-404-014. LEAK CKS GOOD. 2 L 7 2 4F RT A1NM 2007032700017 20070327 00017 NM 2007 3 27 DL76L070207 1 20070314 A 4920 380029817 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE APU FAILED A DALA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 SO 27 175DN 9110 P2699 24803 P2699 THE APU FAILED TO START WHILE TAXIING IN AT BU. THE APU FAULT LIGHT ILLUMINATED. REPLACED APU AND APU ECU AS PER AMM R AN APU NO LEAKS NOTED. ECU SHOWS NML SHUTDOWN NO FAULTS NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007032700022 20070327 00022 2007 3 27 HALA0700113 4 20070316 A 2350 MICROPHONE BOEING 717 717200 1383700 NM COCKPIT INOPERATIVE A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 478HA 55123 BTB: FIRST OFFICER`S BOOM MIC INOPERATIVE. REPLACED FIRST OFFICER`S BOOM MIC GROUND CHECK OKAY. 2 L 7 2 4F TR A6WE 2007032700023 20070327 00023 NM 2007 3 27 HALA0700114 1 20070317 A 2450 734285C BPCU BOEING 767 767300 1385204 NM ELECTRICAL FAILED A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 594HA 34994 34994 23275 BTB. LOSS L AND R UTIL BUSSES ON TAXI OUT. CHECK BPCU, NO TEST. DOWN POWERED AND CHECK BITE BPCU FOUND REPLACE BPCU. REPLACED BPCU PER AMM 24-41-03-004-001. OPS CHECK, BITE CHECK GOOD. 2 L 7 2 4F RT A1NM 2007032700024 20070327 00024 NM 2007 3 27 HALA0700112 1 20070316 A 2410 GENERATOR BOEING 767 767332 1382001 NM RIGHT INOPERATIVE A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 598HA 23278 BTB - ETOPS SIGNIFICANT SYSTEM, AFTER START RIGHT GENERATOR DID NOT COME ON LINE. RESET RIGHT ENGINE GENERATOR, RAN ENG INE, OP`S CK GOOD PER AMM 24-11-01-404-003-001. 2 L 7 2 4F RT A1NM 2007032700026 20070327 00026 NM 2007 3 27 DL76L070201 1 20070311 A 2432 893003 CHARGER BOEING 767 767332 1382001 NM MASTER INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 171DN 24759 AT CRUISE, MAIN BAT CHG STATUS MSG BAT VOLTS 25, AFTER APPROX 45 MINS MSG DISAPPEARED. VOLTS WENT TO 28 AND DC-A WENT T O 11. REPLACED A/C MAIN BATTERY AND MAIN BATTERY CHARGER PER AMM. TEST OK. 2 L 7 2 4F RT A1NM 2007032700028 20070327 00028 NM 2007 3 27 DL764070203 1 20070311 A 2530 OVEN BOEING 767 767432ER 1385134 NM GALLEY CONTAMINATED A DALA K NONE W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 841MH 29714 OVEN POS 401 SMOKES SO MUCH IT IS UNUSABLE FOUND PLASTIC SHEET ON TOP OF OVEN FAN. REMOVED DEBRIS. NOW OVEN OPERATES G OOD. 2 L 7 2 4F RT A1NM 2007032700031 20070327 00031 NM 2007 3 27 AWXA200700392 1 20070312 A 5340 69353523 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - FOUND CRACKED STRINGER CLIP, BS 947, S26R. REPLACED STRINGER CLIP, BS 947, S26R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007032700033 20070327 00033 NM 2007 3 27 AWXA200700394 1 20070311 A 5340 69414372 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - FOUND CRACKED STRINGER CLIP, BS 706, S2L. REPLACED STRINGER CLIP, BS BS 706, S2L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007032700034 20070327 00034 NM 2007 3 27 AWXA200700395 1 20070311 A 5340 69414372 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - FOUND CRACKED STRINGER CLIP, BS 663.75, S10L. REPLACED STRINGER CLIP, BS 663.75, S10L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007032700035 20070327 00035 NM 2007 3 27 AWXA200700396 1 20070311 A 5340 69353521 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - FOUND CRACKED STRINGER CLIP, BS 706, S2R. REPLACED STRINGER CLIP, BS 706, S2R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007032700037 20070327 00037 NM 2007 3 27 AWXA200700398 1 20070311 A 5340 69353521 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - FOUND CRACKED STRINGER CLIP, BS 616, S6R. REPLACED STRINGER CLIP, BS 616, S6R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007032700038 20070327 00038 NM 2007 3 27 AWXA200700399 1 20070320 A 5310 REVEAL BOEING 737 7373G7 1384595 NM CARGO DOORWAY CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 PHX - AFT CARGO DOOR FORWARD FRAME INTERNAL DOUBLER CRACKED AND DAMAGED. REPLACED AFT CARGO COMPARTMENT DOOR FORWARD FR AME DOUBLER IAW B737-300 SRM 51-40-02. DISCREPANT PART INFORMATION AND LOCATION WILL BE ADDED AFTER MAJOR REPAIR FORM I S RECEIVED AND REVIEWED. [SUP 05-15-07] UPON FURTHER REVIEW IT WAS DETERMINED THAT THE DISCREPANT PART WAS NOT THE AFT CARGO DOOR FORWARD FRAME INTERNAL DOUBLER BUT WAS A SIDEWALL ATTACHMENT REVEAL NEAR THE FORWARD FRAME OF THE AFT CARGO DOOR CUT OUT WHICH IS CLASSIFIED AS SECONDARY STRUCTURE AND IS NOT A SERVICE DIFFICULTY REPORTABLE EVENT. 2 L 7 2 4F RT A16WE 2007032700039 20070327 00039 CE 2007 3 27 GUUA03130701 1 20070313 A 2120 FILTER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE VENT BLOWER CONTAMINATED A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 29 81535 UE147 FLIGHT: 9286, DURING FLIGHT AIRCRAFT HAS NAUSEATING OIL SMELL COMING FROM VENTS. REPLACED FORWARD AND AFT VENT BLOWER F ILTERS. 2 L 7 2 4T 4 T RT A24CE E26NE 2007032700040 20070327 00040 CE 2007 3 27 AMW083435 1 20070321 A 5270 1013644662 SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA CARGO DOOR OUT OF ADJUST A AMWA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 142ZV UE142 DURING CLIMBOUT, CARGO DOOR ANNUN ILLUM, A/C RETURNED TO FIELD WITH NO FURTHER INCIDENT.ADJUSTED SWITCH. 2 L 7 2 4T 3 T RT A24CE E2NE 2007032700041 20070327 00041 EA 2007 3 27 SIMA200708501 1 20070323 A 3597 WIRE CNDAIR CL600 CL6002C10 1390015 EA CABIN CHAFED A SIMA G A O2 MASK DEPLOYED UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 522AE 10147 PASSENGER MASK DEPLOYED DURING CLIMB-OUT, RETURNED TO DFW. REPAIRED CHAFED WIRE FBH6463, EIGHT INCHES FROM CONNECTOR JB 10 IAW CRJ WRM. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007032700042 20070327 00042 SO 2007 3 27 SIMA200708502 1 20070325 A 2160 DUCT EMB 135 EMB135KL 3260302 SO CABIN AIR DISCONNECTED A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 845AE 145685 CABIN WOULD NOT COOL AND SMOKE REPORTED IN CABIN. RESECURED DUCT UNDER FLOOR IAW EMB AMM. PERFORMED ENGINE RUNS WITH N O DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007032700046 20070327 00046 SO 2007 3 27 SIMA200708507 1 20070314 A 5320 14522178005 SILL EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 738NR 13393 4800 145401 SERVICE DOOR SILL FOUND CORRODED. REMOVED AND REPLACED SERVICE DOOR SILL IAW EMB SRM 51-20-01, 51-20-03, 51-40-02, 51-4 0-04 AND 51-40-06. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007032700047 20070327 00047 SO 2007 3 27 SIMA200708503 1 20070314 A 5310 14522460015 GUSSET EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 738NR 13393 4800 145401 GALLEY FORWARD GUSSET FOUND TO BE CORRODED. BLENDED THE AREA REMOVING CORROSION, FABRICATED AND INSTALLED REPAIR DOUBLE R IAW EMB IC2007-145/01751, DATED 3-12-07. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007032700049 20070327 00049 EA 2007 3 27 SWIA200718046 1 20070223 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 864AS 7502 FS 280 FLOORBEAM IS CRACKED AT RBL TO (LWR), DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS FS 280 FLOORB EAM PER REO 601R-53-71-171 REV C. 2 L 7 2 4F RT A21EA 2007032700050 20070327 00050 EA 2007 3 27 SWIA200718047 1 20070223 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 864AS 7502 FS 280 FLOORBEAM IS CRACKED AT LBL10 (LWR), DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS ON FLOORBEAM S TA 280 LBL10 PER REO 601R-53-11-176 REV C. 2 L 7 2 4F RT A21EA 2007032700051 20070327 00051 EA 2007 3 27 SWIA200718048 1 20070223 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 864AS 7502 AFT PAX DOOR STEPS CRACKED CORNERS 4/5, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS, PAX DOOR AFT WEB PER REO 601R-52-11-702 REV A. 2 L 7 2 4F RT A21EA 2007032700052 20070327 00052 EA 2007 3 27 SWIA200718049 1 20070223 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 864AS 7502 FWD PAX DOOR STEPS 4/5 CRACKS FOUND IN CORNERS, DISCOVERED DURING C-CHECK INSPECTION. C/W CRJ200 REO 601R-52-11-702 REV A REPAIR FOR MULTI SITE DAMAGE ZONES 2 AND 3. 2 L 7 2 4F RT A21EA 2007032700057 20070327 00057 EA 2007 3 27 SWIA200718054 1 20070223 A 5340 NUT CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 864AS 7502 RT 484 INBOARD/OUTBOARD CLIPS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP 601R31171-9 AND 601R-53 -41-059-2 TO RT FS 484 AT RBL 27 AND 36 PER CRJ200 SRM 51-42-06 P11 AND 51-42-21 P17. 2 L 7 2 4F RT A21EA 2007032700061 20070327 00061 NM 2007 3 27 DHL2007751518 1 20070320 A 5320 651986220 SUPPORT ANGLE BOEING 727 727264 138408M NM BS 300 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 751DH 22982 INT E/E AT BS 300, ON RT CRAWLWAY HAS I/B CORRODED ON LOWER SURFACE (NLG TRUNNION SUPPORT). GAINED ACCESS, REMOVED CORR OSION, WITH MATERIAL LOSS EXCEEDING LIMITS AS PER B727 SRM 53-10-1 (MAT REMOVED <.085"). REMOVED AND REPLACED RT MID CH ORD ANGLE PER B727 SRM 51-30-2 AND 51-20-1. RETURNED AREA TO NORMAL. 2 L 7 3 4F A3WE 2007032700064 20070327 00064 SO 2007 3 27 SIMA200707402 1 20070312 A 5347 14530659003 SEAT TRACK EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 14572 4800 145234 CORRISION FOUND ON LEFT LOWER BOTTOM CABIN SEAT TRACK BETWEEN FRAMES 30 TO 35. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032700065 20070327 00065 SO 2007 3 27 SIMA200707414 1 20070312 A 5347 14532606001 SEAT TRACK EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 15742 4800 145234 CORROSION ON LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 24 TO 30. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RE TURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032700070 20070327 00070 EA 2007 3 27 SWIA200718006 1 20070315 A 2910 O-RING CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 430SW 7523 IN FLIGHT "HYD 2 LO PRESS" CAUTION MESSAGE AND SYNOPTIC PAGE SHOWED ZERO QUANTITY. DIVERTED TO MTJ. REPLACED BROKEN O- RING AT MANIFOLD GROUND PRESSURE LINE B NUT REF 29-11-05. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007032700071 20070327 00071 EA 2007 3 27 SWIA200718007 1 20070313 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN FAILED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 925SW 7682 FOUND FLOOR EMERGENCY LIGHT AT ROW 5 INOP. REPLACED LIGHT STRIP AT ROW 5. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007032700072 20070327 00072 SO 2007 3 27 SWIA200718008 1 20070311 A 2150 A/C PACK EMB 120 EMB120ER 3260203 SO RIGHT ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 218SW 120287 RIGHT PACK GIVES SLIGHT OVERHEATED ODOR IMMEDIATELY AFTER TAKEOFF. OPERATED RIGHT PACK FOR SEVERAL MINUTES AND COULD NO T DUPLICATE. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007032700074 20070327 00074 SO 2007 3 27 SWIA200718010 1 20070119 A 5210 WEB EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 221SW 120290 FOUND CRACK CENTER AFT OF PAX DOOR ON UNDERSIDE OF WEBBING, DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CENTER AFT S UPPORT IAW SRM 52-10-02 AND RII 52-800-1000. 2 L 7 2 4T RT A31SO 2007032700075 20070327 00075 SO 2007 3 27 SWIA200718011 1 20070119 A 5210 WEB EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 221SW 120290 FOUND CRACK CENTER FORWARD OF PAX DOOR ON UNDERSIDE OF WEBBING, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CRACKED FRAME IAW SRM 51-10-02 PG 3 SEC 3A AND RII 52-800-1000. 2 L 7 2 4T RT A31SO 2007032700077 20070327 00077 SO 2007 3 27 C2XA07RI007 1 20070320 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13988 145265 RIC - MX DURING SCHEDULE ROUTINE MAINTENANACE, MX FOUND 02 EMERGENCY AISLE LIGHTS INOP. MX REMOVED AND REPLACED NR 4 EM ERGENCY LIGHT INVERTER. MX PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032700078 20070327 00078 NM 2007 3 27 SWAA071505 1 20070322 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 406WN 27894 EEPLS LIGHT COVER BROKEN AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007032700079 20070327 00079 EU 2007 3 27 SA07024 2 20070321 A 7261 3051125000 SEAL AIRBUS A321 A321211 3930370 EU CFMINT CFM56 CFM563BFR 13802 EU LT ENGINE LEAKING A USAA E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CR CRUISE 1 EA 19 189UW VJ1676 1425 779509 ABQ FLT 1596 EN ROUTE. WHILE IN CRUISE FLIGHT, THE NR 1 ENGINE BEGAN TO LOOSE OIL PRESSURE. THE CREW SHUTDOWN THE NR 1 ENGINE AND THE FLIGHT DIVERTED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. THERE WAS 20 MINUTES OF SINGLE ENGINE TI ME. MAINTENANCE REPLACED THE TRANSFER GEARBOX ADAPTER SEAL. ENGINE OPERATIONALLY AND LEAK CHECKS OK. (K) 2 L 7 2 4F 4 F RT A28NM E21EU 2007032700080 20070327 00080 NM 2007 3 27 HALA0700119 1 20070320 A 3246 165T010039 WHEEL BOEING 767 76733A 1385209 NM MLG DAMAGED A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 593HA 1649 1649 33424 BTB - ON PUSH BACK, HEARD LOUD POP FROM LT TRUCK. FOUND WHEEL LUG LAYING IN VICINITY OF WHERE A/C WAS PARKED. INSPECTE D LT WHEEL ASSY'S FOUND LUG ON NR 5 WHEEL ASSY SHEARED. REMOVED AND REPLACED NR 5 WHEEL AND TIRE ASSY PER HAL M295-767 SPIN CHKS OK. 2 L 7 2 4F RT A1NM 2007032700081 20070327 00081 NE 2007 3 27 HALA0700120 2 20070320 A 7320 EEC BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE NR 1 UNKNOWN A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM - BTB - LEFT ENG EEC C-1 STATUS MSG DISPLAYED. PERFORMED FIM 73-21-00 FIG 115 SHEET 1 ALL PASS ED NO INBOUND OR HISTORY. CLEARED MIC SHEET PULLED PLACARD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007032700082 20070327 00082 NM 2007 3 27 HALA0700121 1 20070320 A 2150 A/C PACK BOEING 767 76733A 1385209 NM LEFT UNKNOWN A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, TAXI IN LT PACK OFF LIGHT ON WITH PACKS SELECTED ON. GOOD APU AIR. NO FAULTS FOUND AND PERFO RMED FIM 21-51-00 FIG 3 SHEET 1 THRU 5 SYSTEM CKS OK. 2 L 7 2 4F RT A1NM 2007032700087 20070327 00087 NE 2007 3 27 AALA20070462 2 20070309 A 7210 779150 GEARBOX DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RIGHT ENGINE LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 245AA 49257 718470 DFW TO GDL, DURING CRUISE RIGHT ENGINE OIL QUANTITY WENT FROM 12 QUARTS TO 4 QUARTS IN TWO HOURS. OIL PRESSURE AND TEMP ERATURE NORMAL. CREW SHUTDOWN RIGHT ENGINE AND LANDED MTY WITHOUT INCIDENT. FOUND NUMBER TWO GEARBOX LEAKING OIL. REP LACED NUMBER TWO GEARBOX. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007032700088 20070327 00088 EU 2007 3 27 AALA20070467 1 20070310 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 40064 507 MIA - FOUND EMERGENCY LIGHT AT SEAT 28G INOPERATIVE. FOUND PIN ON CONNECTOR PUSHED BACK. SECURED CONNECTOR FOR EMERGEN CY LIGHT AT SEAT 28G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007032700089 20070327 00089 WP 2007 3 27 AALA20070471 1 20070311 A 7931 OIL SYSTEM DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LEFT ENGINE LOW PRESSURE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 578AA 53155 718508 ORD INFLIGHT - LEFT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED FOLLOWED BY OIL QUANTITY DEGRADING. CREW SHUTDOWN ENGINE. NO HIGH OIL TEMPERATURES OR ENGINE GAS TEMPERATURES OBSERVED. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. SINGLE EN GINE TIME APPROXIMATELY 20 MINUTES. REPLACED NUMBER ONE ENGINE ON 11 MARCH 2007 AT ORD DUE TO OIL PRESSURE OUT OF LIMIT S. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007032700090 20070327 00090 EU 2007 3 27 AALA20070463 1 20070310 A 2780 JACKSCREW AIRBUS 300 A300B4605R 3930308 EU SLAT INOPERATIVE A AALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SW 21 70079 619 JFK INFLIGHT - DURING APPROACH CONFIGURATION SLATS SYSTEM ONE AND TWO FAULTED. LANDED JFK WITHOUT INCIDENT WITH NO SLAT S AND FLAPS AT 40. REPLACED LEFT WING NUMBER TWO SLAT JACKSCREW AND RESET TORQUE LIMITER FOR LEFT SLAT SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007032700091 20070327 00091 NE 2007 3 27 AALA20070464 2 20070310 A 7250 TURBINE BLADES BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE RT ENGINE FAILED A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 710TW 28169 727217 LAS INFLIGHT - DURING CLIMB CREW EXPERIENCED SEVERAL RIGHT ENGINE COMPRESSOR STALLS AT ROTATION AND LOUD BANGS. ENGINE GAS TEMPERATURE TO 664. SHUTDOWN ENGINE AND LANDED LAS WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE ON 12 MARCH 2007 D UE TO TURBINE BLADE FAILURE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032700092 20070327 00092 NE 2007 3 27 AALA20070465 2 20070310 A 7510 2028TP DUCT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE ZONE 500 DAMAGED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 410AA 49321 728240 DFW INFLIGHT - DURING CLIMB, LEFT ENGINE FIRE LOOP ILLUMINATED. AFTER ACCOMPLISHING CHECKLIST THE FIRE LOOP WARNING EXT INGUISHED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE ANTI ICE BLEED LINE. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007032700093 20070327 00093 EU 2007 3 27 AALA20070468 1 20070310 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 40064 507 MIA - FOUND EMERGENCY LIGHT AT SEAT 23C INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007032700094 20070327 00094 EU 2007 3 27 AALA20070476 1 20070311 A 3350 BR9664103 LIGHT AIRBUS 300 A300B4605R 3930308 EU SEAT 1D INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 JFK - FOUND EMERGENCY FLOODLIGHT FORWARD OF SEAT 1D INOPERATIVE. REPLACED EMERGENCY FLOODLIGHT FORWARD OF SEAT 1D. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007032700097 20070327 00097 NM 2007 3 27 AALA20070447 1 20070306 A 2121 FAN BOEING 757 757223 1384957 NM AIR CONDITIONING INOPERATIVE A AALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 177AN 32396 ORD INFLIGHT - FLIGHT ATTENDANT REPORTED ELECTRICAL SMELL/HAZE AFTER TAKEOFF. RETURNED TO ORD AND LANDED WITHOUT INCIDE NT. DURING TAXI IN EQUIPMENT COOLING OVERHEAT LIGHT ILLUMINATED. REPLACED EQUIPMENT COOLING FAN. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007032700098 20070327 00098 NM 2007 3 27 AALA20070469 1 20070310 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 182AN 29592 DFW - FOUND EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 25D. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007032700099 20070327 00099 NM 2007 3 27 AWXA200700400 1 20070304 A 5330 655298881 SKIN BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED FUSELAGE SKIN, BS 951, S10L AT THE L2 DOOR UPPER HINGE CUT OUT. REPAIRED FUSELAGE SKIN, BS 951, S10 L AT THE L2 DOOR UPPER HINGE CUT OUT IAW B737-300 SRM 53-60-01. 2 L 7 2 4F RT A16WE 2007032700102 20070327 00102 NE 2007 3 27 AWXA200700403 2 20070320 A 7321 FMU560MK1 FUEL CONTROL AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE LEFT ENGINE FAILED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 830AW 9113 9102 1565 SAN - ABTO - CREW ABORTED THE TAKEOFF AT 100 KTS DUE TO LEFT ENGINE FUEL CONTROL FAULT. THE CREW SHUT DOWN THE LEFT ENG INE AND RETURNED TO THE GATE. MX REPLACED THE FUEL METERING UNIT PER AMM 73-22-52-000-01. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032700106 20070327 00106 EA 2007 3 27 TRAX200700407 1 20070319 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 CO-PILOTS FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007032700107 20070327 00107 EA 2007 3 27 TRAX200700408 1 20070319 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 839AS 7284 F/O'S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007032700108 20070327 00108 EA 2007 3 27 TRAX200700409 1 20070319 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 934EV 8028 PAX DOOR WOULD NOT OPEN. 2 L 7 2 4F RT A21EA 2007032700110 20070327 00110 EA 2007 3 27 TRAX200700411 1 20070319 A 2750 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS UNKNOWN A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 882AS 7503 PILOT REPORTED, AFTER TAKEOFF ON FLAP RETRACTION, GOT -FLAPS FAIL- MSG. EICAS SHOWS LEFT AT 18 & RIGHT AT 20. EN ROUTE TO ATL, A/C DIVERTED TO BTR DUE TO MTC. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007032700111 20070327 00111 EA 2007 3 27 TRAX200700412 1 20070319 A 3350 SIGN CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 724EV 10138 FORWARD BULKHEAD EXIT SIGN INOP. FLTS 4536, 4781 CX. 2 L 7 2 4F RT A21EA 2007032700112 20070327 00112 2007 3 27 SWAA071522 4 20070322 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 720WN 27854 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007032700113 20070327 00113 NM 2007 3 27 SWAA071537 1 20070322 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM BS 188 S17L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007032700116 20070327 00116 NM 2007 3 27 SWAA071541 1 20070322 A 5311 6517684 FRAME BOEING 737 7373H4 1384600 NM BS 303 S17L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 303.9, STR 17L. REMOVED AND REPLACED FRAME WEB PER S RM. 2 L 7 2 4F RT A16WE 2007032700118 20070327 00118 NM 2007 3 27 SWAA071520 1 20070322 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM BS 763 S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 763, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007032700119 20070327 00119 NM 2007 3 27 SWAA071542 1 20070322 A 5311 6545810 FRAME BOEING 737 7373H4 1384600 NM BS 312 S6L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 312, STR 6L. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2007032700120 20070327 00120 NM 2007 3 27 SWAA071543 1 20070322 A 5310 6545834 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 192 S17R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 192.5, STR 17R. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007032700121 20070327 00121 NM 2007 3 27 SWAA071533 1 20070322 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM BS 537 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 18Y CHECK, FOUND RIGHT KEEL BEAM CORRODED AT BS 537, LBL 6. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2007032700124 20070327 00124 NM 2007 3 27 SWAA071515 1 20070322 A 5753 6546434 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED SERVICE CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER S RM. 2 L 7 2 4F RT A16WE 2007032700125 20070327 00125 NM 2007 3 27 SWAA071525 1 20070322 A 5753 6546434 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED 10Y CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER SURFACE. REPAIRED FLAP P ER SRM. 2 L 7 2 4F RT A16WE 2007032700127 20070327 00127 NM 2007 3 27 DLM88070206 1 20070314 A 2800 UNKNOWN DOUG MD88 MD88 3023688 NM FUEL SYSTEM UNKNOWN A DALA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 27 936DL 49723 AIRCRAFT DEVELOPED 2000LB IMBALANCE HALF WAY THRU FLIGHT. (RIGHT WING LOW) ACCOMPLISHED FUEL LEAK CHECKLIST. FUEL CON T TO DECLINE TO 1900 LBS ON RT GAUGE, WHEN RIGHT ENGINE FAILED. FUEL AT SHUTDOWN - 4200LT, 2000RT, 6300 TOTAL. ENGINE FLAMED OUT DESCENDING THRU 10000FT. NO RESTART ATTEMPTED. ENGINE SHUTDOWN CHECKLIST ACCOMPLISHED. LANDED APPROX 8 MIN UTES AFTER FLAMEOUT. REPLACED COMP PROBE, REPLACED NR 6 PROBE. REPLACED JUNCTION PROBE. PERFORMED A FUEL QTY TEST WIT H DIP STICK PER MM AND FUELING MANUAL AND CHECKED FUEL QTY SYS PER MM 28-40-00-101-1 AND ALL COMPONENTS CHECKED GOOD. 2 L 7 2 4F RT A6WE 2007032700128 20070327 00128 NM 2007 3 27 DL76S070211 1 20070316 A 4940 STARTER BOEING 767 767332 1382001 NM GE CF6 CF680C2* GL APU INOPERATIVE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 125DL 29393 24075 P1375 STRONG SMELL NOTICED BOTH INSIDE AND OUTSIDE AIRCRAFT SMELL STARTED AFTER POWER TRANSFER TO APU AND PACKS WERE TURNED ON . GROUND PERSONNEL ALSO REPORTED STRONG SMELL AND REPORTED SMOKE COMING OUT OF AN APU VENT. INSP APU AREA FOUND STARTE R MOTOR W/STRONG BURNT ELEC ODOR. REPLACED STARTER ALSO FOUND RELAY STUCK CLOSED K197 REPLACED K19 AND K117 RELAYS. AL SO, REPLACED APU BATT. RAN APU, OPS CK OK. REMOVED MCO/PLAC. 2 L 7 2 4F 4 F RT A1NM E23EA 2007032700130 20070327 00130 NM 2007 3 27 DL777070213 1 20070317 A 3240 BRAKE ASSY BOEING 777 777232 1385232 NM RROYCE RB211 RB211TRENT89 NE MLG CONTAMINATED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 863DA 29735 P1375 TOWER REPORTED SMOKE COMING FROM AIRCRAFT MAIN GEAR AFTER VERY SMOOTH LANDING. FOUND RESIDUAL DEICING FLUID ON WHEELS A ND BRAKES. CLEANED BRAKES. OK FOR SERVICE. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT T00001SE E00050EN 2007032700132 20070327 00132 NM 2007 3 27 DL76G070215 1 20070318 A 2530 251005193 COFFEEMAKER BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE GALLEY ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 1612T 30575 P1375 STRONG ELEC SMELL IN AFT CABIN DURING CLIMB-OUT. INSPECTED A/C DURING VERIFICATION FLT. TURNED ON ALL OVENS/COFFEE MAK ERS/AND CHILLERS IN AFT GALLEY. OPENED UP CEILING PANELS IN AFT GALLEY/CABIN. CHECKED DOOR HEATERS DUCTING/OXY/CANISTE RS AND FANS. CHECKED ENTIRE CABIN/COCKPIT/LWR E/E AND FWD CARGO. CHECKED CHILLER VENTS, NO ODOR PRESENT. ONLY ODOR NO TICED WAS A BURNT SMELL FROM COFFEE MAKER 1/2. REMOVED COFFEE MAKER AND FOUND HEAVY CRUD NEAR HEAT ELEMENT. REMOVED AL L COFFEE MAKERS AND CLEANED UNDERBASES NR 1 AND 2 WERE REPLACED. 2 L 7 2 4F 4 F RT A1NM E13NE 2007032700134 20070327 00134 NM 2007 3 27 DL738070217 1 20070318 A 5753 BACB30US81K3 BOLT BOEING 737 737832 13844CF NM FLAP BELLCRANK SHEARED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3741S 30487 LEFT WING O/B FLAP I/B FLAP TRACK FAIRING PUNCHED BY SHEARED AFT FLAP ACTUATING ROD. REPLACED LT O/B FLAP BELLCRANK BOT H AFT FLAP PUSHRODS AND FL FAIRING. REPLACED RODS P/N 113A3920-5, P/N 113A3920-7. BELLCRANK 113A3910-3 AND FAIRING 113 A9250-13. REPLACED AND ADJUSTED PER M/M 27-51-18-400-802. CYCLED FLAPS SEVERAL TIMES, OPN CHECKS OK. 2 L 7 2 4F RT A16WE 2007032700135 20070327 00135 NM 2007 3 27 SWAA071521 1 20070322 A 5753 6546435278 SKIN BOEING 737 7373Q8 1384670 NM RT TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED HC1 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP UPPER OUTBOARD SURFACE DELAMINATED. REMOVED AND REPL ACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2007032700137 20070327 00137 NM 2007 3 27 SWAA071518 1 20070322 A 5311 6546540 FRAME BOEING 737 7373Q8 1384670 NM BS 639 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 15R. REPAIRED FRAME PER ER AND BOEING SB. 2 L 7 2 4F RT A16WE 2007032700138 20070327 00138 NM 2007 3 27 SWAA071528 1 20070322 A 5311 6546555 FRAME BOEING 737 7373Y0 1384671 NM BS 867 S14R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 14R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007032700139 20070327 00139 NM 2007 3 27 SWAA071535 1 20070322 A 5312 6546568 STIFFENER BOEING 737 7373H4 1384600 NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 18Y CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT BS 1016, STR 4R. REPAIRED STIFFENER PER SR M. 2 L 7 2 4F RT A16WE 2007032700140 20070327 00140 NM 2007 3 27 SWAA071544 1 20070322 A 5312 6546568 STIFFENER BOEING 737 7373H4 1384600 NM BS 1016 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT BS 1016, STR 9L. REPAIRED STIFFENER PER SR M. 2 L 7 2 4F RT A16WE 2007032700143 20070327 00143 NM 2007 3 27 SWAA071534 1 20070322 A 5312 6546568 STIFFENER BOEING 737 7373H4 1384600 NM BS 1016 S3R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 18Y CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT BS 1016, STR 3R. REPAIRED STIFFENER PER SR M. 2 L 7 2 4F RT A16WE 2007032700144 20070327 00144 NM 2007 3 27 SWAA071540 1 20070322 A 5315 6546811 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CRACKED AT BS 986.5, RBL 5. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2007032700145 20070327 00145 NM 2007 3 27 SWAA071539 1 20070322 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM BS 360 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007032700146 20070327 00146 NM 2007 3 27 SWAA071508 1 20070322 A 2750 6573271 TORQUE TUBE BOEING 737 7373Y0 1384671 NM RT WING TE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD MIDFLAP TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007032700147 20070327 00147 NM 2007 3 27 SWAA071512 1 20070322 A 5220 657913183 LINER BOEING 737 7373Y0 1384671 NM EMERGENCY DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED 20Y CHECK, LEFT OVERWING EMERGENCY EXIT HATCH, FORCE TO OPEN HANDLE FAILED. ADJUSTED LINING PER MM. 2 L 7 2 4F RT A16WE 2007032700149 20070327 00149 NM 2007 3 27 SWAA071509 1 20070322 A 5523 65C26384 TAB BOEING 737 7373Y0 1384671 NM LT ELEVATOR DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED 20Y CHECK, FOUND LEFT ELEVATOR TAB DISBONDED AT STA 25. REPAIRED TAB PER MM AND BOEING DRAWING. 2 L 7 2 4F RT A16WE 2007032700151 20070327 00151 NM 2007 3 27 SWAA071519 1 20070322 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 867 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007032700153 20070327 00153 NM 2007 3 27 SWAA071530 1 20070322 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 380 S27L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 380, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007032700155 20070327 00155 NM 2007 3 27 SWAA071513 1 20070322 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 987 S27L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND STRINGER 27L CORRODED AT BS 987. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007032700156 20070327 00156 NM 2007 3 27 SWAA071526 1 20070322 A 5313 BAC1498 STRINGER BOEING 737 7373Y0 1384671 NM BS 290 S14R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER 14R CRACKED AT BS 290. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007032300080 20070323 00080 NE 2007 3 23 HNAA0700050 2 20070317 A 7320 HMU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE FAILED A HNAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 EA 07 816 329 120438 AT 13,000 FEET HEARD MUFFLED BOOM FROM NR 1 ENGINE FOLLOWED BY NR 1 ENGINE MANUAL CAUTION LIGHT AND OIL PRESSURE WARNING . SHUT DOWN ENGINE. REPLACED HMU AND FUEL PUMP. 2 H 7 2 4T 4 T RT A13NM E20NE 2007032300081 20070323 00081 NM 2007 3 23 MWEA070045 1 20070316 A 5350 RELEASE MECH BOEING 717 717200 1383700 NM TAIL CONE FAILED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 920ME 55182 TAIL CONE FAILED TO DROP WHEN USING AFT PRESSURE BULKHEAD DOOR PULL PER TASK 53-52-00-03. CLEANED AND ADJUSTED RELEASE CLIPS IN AFT ACCESSORY COMPARTMENT. 2 L 7 2 4F TR A6WE 2007032300082 20070323 00082 NM 2007 3 23 USAA070228 1 20070320 A 5751 SKIN BOEING 737 7374B7 1384702 NM RT AILERON PUNCTURED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 452UW 24979 RIGHT AILERON, UPPER SURFACE, 10.5 INCHES INBOARD OF OUTBOARD EDGE PUNCTURED. REMOVED DAMAGE, LAYED UP PLIES PER EA 985 60, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007032300083 20070323 00083 NM 2007 3 23 USAA070227 1 20070320 A 5311 FRAME BOEING 737 7374B7 1384702 NM BS 492 S24R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 445US 24863 BS 492 S-24R HAS CRACK. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER EA 98545, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007032300084 20070323 00084 NM 2007 3 23 USAA070226 1 20070320 A 5311 FRAME BOEING 737 737301 1384611 NM BS 492 S24R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 589US 23934 BS 492, S-24R HAS CRACK. FABRICATED & INSTALLED REPAIR ANGLES PER EA 98533, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007032300085 20070323 00085 NM 2007 3 23 USAA070225 1 20070320 A 5310 STRUCTURE BOEING 737 737401 1384701 NM BS 760 S4R DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 STA 760, S4R, SKIN FASTENER & STRINGER SECTION HAS HOLE. CUT OUT SECTION OF STRINGER, FAB'S SPLICE, NEW CLIP & INSTALLE D PER SRM 53-00-03, FIG 201 REP 3, DEFECT SIZE: .1875 INCH. 2 L 7 2 4F RT A16WE 2007032300086 20070323 00086 NM 2007 3 23 USAA070224 1 20070320 A 5320 ANGLE BOEING 737 737401 1384701 NM FROM STA 305-344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 FROM STA 305-344 S-17L HAS CORROSION. INSTALLED NEW CHORD ANGLE PER SRM 51-10, 51-40-03; CORR TASK C53-107-02; LEVEL 2, DEFECT SIZE: 1 X 18 INCHES. 2 L 7 2 4F RT A16WE 2007032300087 20070323 00087 NM 2007 3 23 USAA070223 1 20070320 A 5712 RIB BOEING 737 737401 1384701 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 LEFT WING IN WBL 135.5 RIB UPPER CHORD ABOUT 6 INCHES FWD OF REAR SPAR. SPLICED IN REPAIR ANGLE & DOUBLERS PER EA 98495 , DEFECT SIZE: 0.5 INCH. 2 L 7 2 4F RT A16WE 2007032300099 20070323 00099 EA 2007 3 23 COMA0760152 1 20070204 A 3010 356202255 LOOP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE FUSELAGE LT SIDE FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 983CA 7169 FLIGHT 5204 - LT AND RT ANTI-ICE DUCT MESSAGE ON TAKEOFF ROLL. LT AND RT ANTI-ICE BLEED LOOPS SHORTED TO GROUND. REPLA CED LT FUSELAGE BLEED LOOP. NO FURTHER DEFECTS. 2 L 7 2 4F 4 F RT A21EA E15NE 2007032600001 20070326 00001 NM 2007 3 26 SWAA071466 1 20070321 A 2761 CASE BOEING 737 7375H4 138449D NM ACTUATOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 7669 25153 LEFT WING NR 4 SPOILER INBOARD ACTUATOR CASE CRACKED. REMOVED AND REPLACED SPOILER ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2007032600024 20070326 00024 NM 2007 3 26 SWAA071470 1 20070321 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 706 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 DURING SCHEDULED C4 CHECK, FOUND RIGHT KEEL BEAM SKIN CRACKED AT BS 706, RBL 6.50. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007032600027 20070326 00027 NM 2007 3 26 SWAA071480 1 20070321 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007032600042 20070326 00042 2007 3 26 SWAA071464 4 20070321 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007032600044 20070326 00044 NM 2007 3 26 SWAA071473 1 20070321 A 5520 DAS623B BEARING BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, RIGHT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED INBOARD HORN BEARING PER MM. 2 L 7 2 4F RT A16WE 2007032600046 20070326 00046 EU 2007 3 26 2007F00022 1 20070305 A 2130 1032788 SAFETY VALVE ISRAEL 1124 1124A 4500103 EU GARRTT TFE731 TFE731* 01518 WP CABIN PRESSURE LEAKING E A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 325LW 5961 334 AIRCRAFT PRESSURIZATION INTERMITTENT. PRESSURIZATION WILL WORK WITH NO DEFECTS ON ONE FLIGHT; THE VERY NEXT FLIGHT, SYST EM WOULD NOT WORK AT ALL. CLEANED OUTFLOW AND SAFETY VALVES; STILL INTERMITTENT. INSTALLED NEW SAFETY AND OUTFLOW SOLENO ID VALVES (A AND B), INSTALLED OVERHAULED SAFETY VALVE, AND RIGGED LT MLG GROUND CONTACT SWITCH IAW MM. PERFORMED SEVERA L FUNCTIONAL CHECK FLIGHT, NO DEFECTS NOTED. 2 M 7 2 4F 4 F A2SW E6WE 2007032600057 20070326 00057 EA 2007 3 26 TRAX200700385 1 20070317 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 874AS 7551 CAPT FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007032600065 20070326 00065 NM 2007 3 26 AALA20070421 1 20070302 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 905AN 29507 MIA - OUTSIDE EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR SLIDE INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007032600069 20070326 00069 WP 2007 3 26 AALA20070426 1 20070302 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7544A 53026 SFO - EMERGENCY LIGHT AT SEAT 16D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007032600070 20070326 00070 NM 2007 3 26 AALA20070427 1 20070303 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 391AA 27451 DFW - EMERGENCY LIGHT AT COCKPIT EXIT SIGN INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT COCKPIT EXIT SIG N. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007032600073 20070326 00073 NM 2007 3 26 AALA20070430 1 20070304 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 753AN 30261 MIA - EMERGENCY SEAT MOUNTED LIGHT AT SEAT 25C HAS MISSING LENS. REPLACED LENS CAP ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032600075 20070326 00075 NM 2007 3 26 AALA20070438 1 20070305 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032600076 20070326 00076 NM 2007 3 26 AALA20070439 1 20070305 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - EMERGENCY LIGHT AT RIGHT NUMBER THREE DOOR EXIT SIGN INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT NUMBER THREE DOOR EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032600079 20070326 00079 NM 2007 3 26 AALA20070441 1 20070306 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39356 24037 DFW - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR OUTSIDE INOPERATIVE. RELAMPED OUTSIDE EMERGENCY LIGHT AT RIGHT NUMBER F OUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007032600081 20070326 00081 NM 2007 3 26 AALA20070443 1 20070306 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 796AN 30796 DFW - EMERGENCY LIGHT AT SEAT 24G HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 24G. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032600086 20070326 00086 EA 2007 3 26 TRAX200700369 1 20070313 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 640 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 SUSPECT CRACK ON LEFT DOUBLER AT FRAME 640. PERFORMED EDDY CURRENT INSPECTION OF SUSPECT AREA PER MTC REQUEST IAW CRJ 2 00 NDTM PART 1, 51-20-06. LEFT FS 640 IS CRACKED. REMOVED DAMAGE ON LT DOUBLER FRAME 640. AND PERFORMED EO 600-53-059 PART B ESB MOD. ALL WORK ACCOMPLISHED ON N/R 13,14,15 AND DEVIATION TO EO 059 PART B. 2 L 7 2 4F RT A21EA 2007032600096 20070326 00096 EA 2007 3 26 TRAX200700379 1 20070316 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 EMERGENCY LIGHTS TURNED ON INTERMITTENTLY DURING FLIGHT. 2 L 7 2 4F RT A21EA 2007032600103 20070326 00103 EA 2007 3 26 COMA0760265 1 20070318 A 5270 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX UNKNOWN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 597SW 7293 FLIGHT 5549 - PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE, FOLLOWED BY A PAX DOOR WARNING MESSAGE. AIRCRAFT RETURNED BA CK TO BWI AND LANDED SAFELY. DEFERRED PER MEL 52-70-01-1. 2 L 7 2 4F RT A21EA 2007032600106 20070326 00106 NE 2007 3 26 CALA0700137 2 20070320 A 7200 SHAFT BOEING 777 777224 1385225 NM GE GE90 GE9090B NE NR 2 ENGINE FAN FAILED A CALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 27 78017 31679 900238 TAKEOFF WAS ABORTED AT 160 KNOTS DUE TO NR 2 ENGINE FAILURE. N1 WENT FROM 104 PERCENT TO 34 PERCENT. INITIAL EXAMINATI ON OF THE NR 2 ENGINE REVEALED METAL IN THE TAILPIPE. THERE WAS NO EVIDENCE OF INGESTION OR BLADE DAMAGE ON THE INLET A REA AND THE ENGINE CASE AND COWL WERE NOT DAMAGED. THE NR 2 ENGINE WAS REMOVED AND REPLACED. [07-25-07] A BOROSCOPE O F THE ENGINE FOUND THE FAN MID SHAFT(FMS) SEPARATED IN THE AXIAL ZONE IN LINE WITH THE HPC STAGE 3 DISK. INVESTIGATION B Y ENGINEERING AND GE CONCLUDED THAT AN OMNI SEAL WAS NOT INSTALLED DURING ENGINE BUILDUP AND THAT THIS CAUSED ACCELERATE D CORROSION OF THE FMS AND SUBSEQUENT FAILURE. 2 L 7 2 4F 4 F RT T00001SE E00049EN 2007032600109 20070326 00109 EA 2007 3 26 VNAA0703009 1 20070314 A 2910 MM67075294005 LINE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE HYD SYSTEM LEAKING A VNAA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 05 702PS 10135 CREW REPORTED THE NR 2 HYDRAULIC SYSTEM FLUID QUANTITY WENT TO 0 PERCENT IN FLIGHT ALONG WITH LOW PRESSURE CAS MESSAGES DURING DESCENT. CREW DECLARED AN EMERGENCY AND LANDED IN SAV WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE NR 2 HYDRAULIC PRESSURE LINE CHAFED AND LEAKING. MAINTENANCE REMOVED AND REPLACED THE NR 2 HYDRAULIC SYSTEM PRESSURE LINE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. NO FURTHER DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007032600111 20070326 00111 EA 2007 3 26 VNAA0703011 1 20070316 A 5200 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE GROUND POWER OPEN A VNAA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 GL 05 723PS 10181 CREW REPORTED A LOUD NOISE OUTSIDE OF AIRCRAFT UPON INITIAL CLIMB. CREW RETURNED TO MSY AND LANDED WITHOUT INCIDENT. M AINTENANCE INSPECTED AND FOUND THE GROUND POWER DOOR OPEN. MAINTENANCE CLOSED AND SECURED DOOR. NO FURTHER DEFECTS NOT ED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007032600118 20070326 00118 NM 2007 3 26 UPS07549504 1 20070222 A 5311 143N1024122 FRAME BOEING 757 75724APF 1384969 NM BS 840 S23-24R DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 418UP 23905 INSPECTION TYPE:C DENT IN FWD CARGO CARGO COMPARTMENT FUSELAGE FRAME STA 840, BETWEEN S23R TO 24R REPAIR AT FRAME ST A 840, S23R TO S24R HAS BEEN ACCOMPLISHED PER EA 757-5332-27-A1613, WITH NO DEVIATIONS AND PER UPS EO B757-5310 26350-A. 2 L 7 2 4F RT A2NM 2007032600120 20070326 00120 NM 2007 3 26 UPS07549506 1 20070222 A 5311 146N102911 FRAME BOEING 757 75724APF 1384969 NM BS 1460 S25-26R DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 418UP 23905 INSPECTION TYPE:C DENT IN AFT CARGO COMPARTMENT FUSELAGE FRAME STA 1460, BETWEEN S25R TO 26R. COMPLIED WITH EA 757-5362 -27-A1612, & UPS EO 5310-26359-A. 2 L 7 2 4F RT A2NM 2007032600121 20070326 00121 NM 2007 3 26 UPS07549507 1 20070222 A 5311 146N103074 FRAME BOEING 757 75724APF 1384969 NM BS 1580 S26L DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 418UP 23905 INSPECTION TYPE:C DENT IN AFT CARGO COMPARTMENT FUSELAGE FRAME STA 1580, S26L. REPAIR AT FRAME STA 1580, S26L HAS BEEN ACCOMPLISHED PER EA 757-5362-27-A1611, WITH NO DEVIATIONS AND PER UPS EO B757-5310- 26344-A. 2 L 7 2 4F RT A2NM 2007032600122 20070326 00122 NM 2007 3 26 UPS07549508 1 20070226 A 5412 311N3271 BULKHEAD BOEING 757 75724APF 1384969 NM NR 1 PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 418UP 23905 INSPECTION TYPE:C NR 1 PYLON O/B LOWER CORNER OF MIDSPAR BULKHEAD IS HEAVILY CHAFED. COMPLIED WITH EA 757-5453-27-A1615 WITH NO DEVIATIONS AND EO B757-5410-18134B. 2 L 7 2 4F RT A2NM 2007032600142 20070326 00142 NM 2007 3 26 SWAA071460 1 20070320 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM BS 616 S17L/R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, STR 17L AND STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007032600156 20070326 00156 NM 2007 3 26 DL76L070219 1 20070318 A 5415 FITTING BOEING 767 767332 1382001 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 172DN 24775 THE NR 2 PYLON MIDSPAR FITTING WAS FOUND WITH A CRACK IN ONE FASTENER HOLE. THE FASTENER HOLE WAS OVERSIZED TO REMOVE T HE CRACK. REF AD 2005-19-23; 01-074944-12AD. 2 L 7 2 4F RT A1NM 2007032600168 20070326 00168 NM 2007 3 26 CALA0700139 1 20070321 A 5313 65617775 STRINGER SPLICE BOEING 737 7373T0 1384582 NM BS 351-365 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 77303 23354 INSPECTION FOUND A .5 INCH CRACK IN STRINGER 16L SPLICE CHANNEL AT STA 351-365. A NEW STRINGER SPLICE CHANNEL WAS INSTA LLED IAW ECRA 5311-01302. 2 L 7 2 4F RT A16WE 2007032600174 20070326 00174 NM 2007 3 26 AWXA200700381 1 20070312 A 5340 69353521 STRINGER CLIP BOEING 737 7373G7 1384595 NM BS 747 S25L CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - FOUND CRACKED AFT CARGO COMPARTMENT STRINGER CLIP, BS 747, S25L. REPLACED AFT CARGO COMPARTMENT STRINGER CLIP, BS 747, S25L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007032700001 20070327 00001 WP 2007 3 27 IXXA070017S 1 20070322 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 87731 1836 45811 DURING ROUTINE CPCP INSPECTION, FOUND RIGHT WING UPPER SKIN CRACKED AT STATION XRS 74 STRINGER 16. REMOVED DAMAGE AREA, NO CRACK'S OR CORROSION FOUND AFTER DAMAGE REMOVED. MANUFACTURED REPAIR PARTS. TREATED AND PRIMED AREA AND REPAIR PAR TS. INSTALLED REPAIR PARTS IAW DACO DC8 SRM57-2-1 FIGURE 10. 2 L 7 4 4F RT 4A25 2007032700004 20070327 00004 SO 2007 3 27 SWIA200718040 1 20070320 A 5311 FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 LEFT HYDRAULIC BAY OUTBOARD FRAME HAS A CRACK IN IT, DISCOVERED DURING SERVICE CHECK INSPECTION. REPLACED OUTBOARD FRAM E IAW EMB SRM 51-40-02. 2 L 7 2 4T RT A31SO 2007032700007 20070327 00007 EA 2007 3 27 SWIA200718043 1 20070223 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 864AS 7502 LT ENG FWD MOUNT UPPER LINK HAS CORROSION ON UPPER BEARING, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT ENGINE FORWARD MOUNT UPPER LINK P/N 601-37016-5 S/N 5064. 2 L 7 2 4F RT A21EA 2007032700008 20070327 00008 EA 2007 3 27 SWIA200718044 1 20070223 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 864AS 7502 LT ENG FWD YOKE MOUNT HAS CORROSION IN BEARING, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT ENGINE FORWARD YOKE MOUNT P/N 601-37015-7 S/N RJ SWA/070301BTAC03. 2 L 7 2 4F RT A21EA 2007032700012 20070327 00012 NM 2007 3 27 752005 1 20070314 A 2612 CIRCUIT CARD BOEING 747 747228F 1384895 NM GE CF6 CF650E2 30018 NE FIRE WARNING MALFUNCTIONED A Q2SA O OTHER N FALSE WARNING CL CLIMB 1 EA 63 752SA 21255 530291 MAXIMUM POWER TAKEOFF OUT OF PANC, N1 SET AT 105.8 PERCENT. AFTER TAKEOFF PASSING THRU 1000 FEET, NR 1 ENGINE NACELLE F AULT LIGHT ILLUMINATED INTERMITTENTLY ACCOMPANIED BY FIRE WARNING. BELL ALSO RANG INTERMITTENTLY. NACELLE INDICATORS A & B WERE FLUCTUATING BETWEEN 3 AND 5. FOLLOWED QRH AND ALL INDICATION RETURN TO NORMAL. CONTINUED FLIGHT. INSPECTED ENGINE BLEED SYSTEM. NO VISIBLE DAMAGE. PNEUMATIC LEAK CHECK OF ENGINE. NO LEAKS NOTED IN ACCORDANCE WITH AMM 71-00-0 0. CLEANED AND INSPECTED FIRE LOOP CONNECTORS, FIRE LOOP WARNING CARDS IN ACCORDANCE WITH AMM 26-11-00. NO FAULT FOUND . 2 L 7 4 4F 4 F A20WE E23EA 2007032700015 20070327 00015 NM 2007 3 27 DL738070205 1 20070313 A 3350 ADD7170110 BATTERY BOEING 737 737832 13844CF NM EMERGENCY LIGHTS DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3733Z 30539 L1 EMERG LIGHTS INOP. REPLACED BATTERY PACK. 2 L 7 2 4F RT A16WE 2007032700019 20070327 00019 2007 3 27 DL76G070209 4 20070315 A 3442 ANTENNA BOEING 767 767332 1382001 NM WX RADAR SYS INOPERATIVE A DALA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 27 173DZ 29692 RECEIVED NO GROUND OR WEATHER RETURNS ON WX RADAR INFLT. REPLACED T/R NO HELP. REPLACED WXR ANTENNA, NO HELP. TRIED A NOTHER TRANSCEIVER. SYS CHECKS OK. 2 L 7 2 4F RT A1NM 2007032700020 20070327 00020 NM 2007 3 27 DL757070210 1 20070314 A 5330 143N34714 SKIN BOEING 757 757232 1384965 NM FS 606-614 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 636DL 23763 DURING CURRENT VISIT, A GAP BETWEEN THE RIGHT RADIO ALTIMETER RECEIVER ANTENNA FAIRING AND THE FUSELAGE SKIN AT APPROXIM ATELY BODY STATION 610 S-27R JUST UNDER THE C1 CARGO DOOR CARGO DOOR OPENING WAS FOUND. UPON REMOVAL OF THE FAIRING, A DENT WITH GOUGES AND RESULTING CRACK WAS DISCOVERED. THIS RESULTED IN A TRIM OUT OF THE CRACKED FUSELAGE SKIN AND A BOE ING APPROVED REPAIR INSTALLED PER 460758-14. 2 L 7 2 4F RT A2NM 2007032700027 20070327 00027 NM 2007 3 27 DL76G070202 1 20070311 A 2710 2828001009 ACTUATOR BOEING 767 767332 1382001 NM LT I/B AILERON MALFUNCTIONED A DALA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SO 27 1613B 32776 ON CLIMB-OUT WITH A/P ON NOTICED CONTROL WHEEL DEFECTED 2 DEGREES RIGHT WITH A/P OFF RUDDER TRIM PLACED 7 DEGREES RIGHT TO CENTER WHEEL. REMOVED LEFT INBD AIL PCA OUTBD PCA LT SYS OK TO INSTALL PCA S/N 3666. INSTALLED LEFT INBD AIL OUTBD P CA INSTALLATION OK. ADJ TEST OK. SAFTY AND SECURITY CHECK OK RII INSPECTIONS C/W MM 27-11-48 FOR REMOVAL AND INSTALLATI ON OF LT I/B AILERON PCA. 2 L 7 2 4F RT A1NM 2007032700029 20070327 00029 NM 2007 3 27 MZZA0700005 1 20070314 A 5210 BACB10FK6F6HS BEARING BOEING 737 737824 13844BZ NM L1 DOOR FROZEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 27246 28956 THE L-1 DOOR WAS DIFFICULT TO OPEN AND CLOSE. MAINTENANCE FOUND THE CAM FOLLOWER BEARING FROZEN. THE BEARING WAS REPLA CED. OPERATIONAL CHECKS WERE GOOD IAW MM 52-11-00. 2 L 7 2 4F RT A16WE 2007032700030 20070327 00030 NM 2007 3 27 AWXA200700391 1 20070315 A 5315 6545834107 STRAP BOEING 737 7373G7 1384595 NM FLOORBEAM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - FOUND CRACKED LOWER FLOORBEAM STRAP, BS 312, RBL 46. REPAIRED LOWER FLOORBEAM STRAP, BS 312, RBL 46 IAW B737-300 SRM 51-70-11. 2 L 7 2 4F RT A16WE 2007032700036 20070327 00036 NM 2007 3 27 AWXA200700397 1 20070310 A 5340 693533521 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - FOUND CRACKED STRINGER CLIP, BS 500C, S27L. REPLACED STRINGER CLIP, BS 500C, S27L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007032700043 20070327 00043 SO 2007 3 27 SIMA200708506 1 20070313 A 3220 14524475003 BEARING CAP EMB 135 EMB135LR 3260305 SO ZONE 700 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 738NR 13393 4800 145401 RIGHT NOSE LANDING GEAR BEARING CAP FOUND CORRODED. REMOVED AND REPLACED BEARING CAP IAW EMB AMM 32-20-02. RETURNED AI RCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007032700054 20070327 00054 EA 2007 3 27 SWIA200718051 1 20070223 A 5210 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 864AS 7502 DOUBLER CRACKED INSIDE PNL832AR OF PAX DOOR, DISCOVERED DURING C-CHECK INSPECTION. INSTALL NEW PAX DOOR DOUBLER PER CRJ 200 SRM 51-42-06 PG 11, 51-42-21 PG 17 AND 51-23-00 PG 21. 2 L 7 2 4F RT A21EA 2007032700056 20070327 00056 EA 2007 3 27 SWIA200718053 1 20070223 A 5340 NUT CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 864AS 7502 LT 484 INBOARD AND OUTBOARD CLIPS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIP P/N 601R31171-17 ST LT STA 484 BL 27.00 PER REO 601R-53-41-059 AND ANGLE AT LT STA 484 BL 36.00 PER REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2007032700058 20070327 00058 EA 2007 3 27 SWIA200718055 1 20070223 A 7830 TRACK CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 864AS 7502 RT T/R NR 4 MAIN TRACK CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT THRUST REVERSER LOWER I/B MAIN TRA CK PER CRJ200 MM TASK 78-34-11-400-801. 2 L 7 2 4F RT A21EA 2007032700059 20070327 00059 EA 2007 3 27 SWIA200718056 1 20070223 A 7830 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 864AS 7502 LEFT ENGINE T/R BOX UPPER INBOARD CRACKED AT LOWER FORWARD CORNER, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED LEFT ENGINE UPPER INBOARD CASCADE PER CRJ200 MM SUBTASK 78-33-01-869-001 AND 78-33-01-920-001 TUC 1233 2 L 7 2 4F RT A21EA 2007032700066 20070327 00066 SO 2007 3 27 SIMA200707403 1 20070312 A 5347 14530659007 SEAT TRACK EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 15742 4800 145234 CORROSION ON LEFT LOWER BOTTOM CABIN SEAT TRACK BETWEEN FRAME 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53- 01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032700067 20070327 00067 SO 2007 3 27 SIMA200707413 1 20070213 A 5347 14532606003 SEAT TRACK EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 15742 4800 145234 CORROSION ON LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 30 TO 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RE TURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032700068 20070327 00068 SO 2007 3 27 SIMA200707421 1 20070312 A 5347 14532606017 SEAT TRACK EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 15742 4800 145234 FOUND CORROSION ON LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-0 6. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032700069 20070327 00069 SO 2007 3 27 SIMA200707410 1 20070312 A 5347 14530658001 SEAT TRACK EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 15742 4800 145234 FOUND CORROSION ON RIGHT FORWARD LOWER CABIN SEAT TRACK BETWEEN FRAME 24 TO 30. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032700073 20070327 00073 SO 2007 3 27 SWIA200718009 1 20070119 A 2711 CHAIN EMB 120 EMB120ER 3260203 SO RT AILERON TRIM CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 221SW 15210 15210 120290 RIGHT AILERON TRIM CHAIN IS RUSTED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT AILERON TRIM TAB ACTUATOR ASSY IAW EMB 120 MM 27-12-01. 2 L 7 2 4T RT A31SO 2007032700076 20070327 00076 NM 2007 3 27 DHL2007751517 1 20070320 A 5343 SUPPORT FITTING BOEING 727 727264 138408M NM LT NLG TRUNNION CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 751DH 22982 LT NLG TRUNNION FITTING AND LOWER CAP HAVE SURFACE CORROSION. REMOVED SURFACE CORROSION AT FITTING PER B727 SRM 53-40-1 FIG 2; ORIG BORE DIA 2.498", FINAL BORE DIA 2.587", REWORK WITHIN CONTINUED SERV LIMITS PER B727 SRM 53-40-1 FIG 2. R EWORK SURFACE TREATED AS REQ PER B727 SRM 53-40-1 FIG 2. 2 L 7 3 4F A3WE 2007032700083 20070327 00083 NM 2007 3 27 HALA0700122 1 20070320 A 2150 A/C PACK BOEING 767 76733A 1385209 NM LEFT UNKNOWN A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, LT PACK OFF LIGHT CAME ON PRIOR TO PUSH BACK. BITE ON PACK CONTROLER HAD NO FAULTS. CLEANED AND SECURED C/P ON LT PACK SENSORS, RAN PACK WITH NO FAULTS, OK FOR SERVICE PER FIM 21-51-00 PACK BITE. 2 L 7 2 4F RT A1NM 2007032700084 20070327 00084 NM 2007 3 27 HALA0700123 1 20070320 A 2160 UNKNOWN BOEING 767 767332 1382001 NM TEMP UNKNOWN A HALA O OTHER O OTHER CR CRUISE 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, FA'S COMPLAIN THAT THE FORWARD FIRST CLASS AREA OF THE CABIN IS VERY COLD. WARMED THE FWD CAB IN TO INDICATION OF 79 DEGREE F TO 80 DEGREE F. FA'S STILL SAY ITS VERY COLD. PERFORMED ZONE TEMP CONTROL BIT IAW DAL FIM 21-61-00 FIG 103 CONFIG 2. NO FAULTS. SYS NORMAL PER BLOCK 7. OPS CHECK PACKS OPS NML. COULD NOT DUPLICATE. 2 L 7 2 4F RT A1NM 2007032700100 20070327 00100 NM 2007 3 27 AWXA200700401 1 20070308 A 5340 69353521 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED STRINGER CLIP, BS 706, S2L. REPLACED STRINGER CLIP, BS 706, S2L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007032700101 20070327 00101 NM 2007 3 27 AWXA200700402 1 20070308 A 5340 69353521 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED STRINGER CLIP, BS 685, S2L. REPLACED STRINGER CLIP, BS 685, S2L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007032700105 20070327 00105 EA 2007 3 27 TRAX200700406 1 20070319 A 5410 COWLING CNDAIR CL600 CL6002B19 1900309 EA NR 1 NACELLE MISSING A ASOA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 SO 27 829AS 7232 TOP COWLING ON LEFT ENGINE NR 1 MISSING ON POSTFLIGHT. COWLING WAS PRESENT ON PREFLIGHT. IT WAS CHANGED IN MCN MTC OVE RNIGHT. 2 L 7 2 4F RT A21EA 2007032700109 20070327 00109 EA 2007 3 27 TRAX200700410 1 20070319 A 3220 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA NLG UNKNOWN A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 905EV 7632 AFTER T/O NOSE GEAR DISAGREE, NOSE GEAR SLOW TO RETRACT. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. FLTS 4278 , 4648 CX. 2 L 7 2 4F RT A21EA 2007032700117 20070327 00117 NM 2007 3 27 SWAA071506 1 20070322 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 691 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 691, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007032700126 20070327 00126 NM 2007 3 27 DL76L070200 1 20070311 A 2933 TRANSMITTER BOEING 767 767332 1382001 NM HYD SYSTEM FAILED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 199DN 28456 A/C RTB DUE TO R HYD QTY DROPPING. FWD TO MCO AND PLAC MEL 29-33-02. IND JUMPED TO 1.15. R HYD QTY IND INOP. REPLACED RT HYD QTY TRANSMITTER RESERVOIR OPS CK PER M/M 29-33-02. OK REMOVED MCO/PLAC. 2 L 7 2 4F RT A1NM 2007032700129 20070327 00129 NM 2007 3 27 DL757070212 1 20070316 A 2741 TRIM SYSTEM BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE STAB OUT OF POSITION A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 675DL 25980 P1375 ABORTED T/O DUE CONFIG WARNING. CREW STATED STAB TRIM OUT OF GREEN BAND. REPOSITIONED STAB TRIM T/O WARN, OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032700157 20070327 00157 NM 2007 3 27 SWAA071524 1 20070322 A 2910 NAS1611215 O-RING BOEING 737 7373H4 1384600 NM -A-HYD SYS LEAKING A SWAA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 29 355SW 25250 AIR TURNBACK/DECLARED EMERGENCY. TOTAL -A- SYSTEM HYDRAULIC FLUID AND PRESSURE LOSS. REMOVED AND REPLACED NR 2 SPOILER ACTUATOR O-RING PER MM. 2 L 7 2 4F RT A16WE 2007032700160 20070327 00160 NM 2007 3 27 HALA0700099 1 20070309 A 4900 HOUSING BOEING 767 76733A 1385209 NM GENERATOR CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 582HA 1070 28139 ETOPS SIGNIFICANT SYSTEM, FOUND APU GENERATOR HOUSING CRACK. REMOVED AND REPLACED APU GENERATOR, PER AMM 24-21-01. OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT A1NM 2007032700161 20070327 00161 WP 2007 3 27 IXXA070015O 1 20070317 A 3260 H141003 DOWNLOCK SWITCH DOUG DC8 DC873F 302199F WP ZONE 700 DEFECTIVE A IXXA O OTHER N FALSE WARNING CL CLIMB 1 SW 11 604BX 87093 2121 46046 DURING LANDING INTO KTOL WHEN THE GEAR HANDLE WAS PLACED IN DOWN POSITION LEFT GEAR GREEN LIGHT DID NOT ILLUMINATE, RED LIGHT CYCLE ON AND OFF. THE CREW RECYCLED THE GEAR AND GEAR OPERATED NORMALLY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LEFT GEAR DOOR AND FOUND THE LEFT MAIN LANDING GEAR DOWN LOCK SWITCH DEFECTIVE. MAINTENANCE REPLACED THE SWITCH AND OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2007032700162 20070327 00162 WP 2007 3 27 IXXA070016O 1 20070317 A 3260 0080004002 PROXIMITY SENSOR DOUG DC8 DC871F 302199D WP ZONE 700 DEFECTIVE A IXXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 11 820BX 89111 32 46065 DURING CLIMB OUT OF KTOL AFTER GEAR WAS RETRACTED THE DOOR LIGHT REMAINED ON AFTER UPLATCH CHECK. THE CREW DID ALL NECE SSARY PROCEDURES AND RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PROXIMITY CONTROL SWITCH FAILED BI TE TEST. MAINTENANCE REPLACED PROXIMITY CONTROL SWITCH AND OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2007032700163 20070327 00163 EU 2007 3 27 USAA070232 1 20070323 A 5315 D5347208900400 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 163US 1417 RIGHT FLOORBEAM TOP FLANGE FROM FR 64-FR 69, -Y1160 TO -Y1192 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM PER SRM 51- 72-11; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1.5 SQ INCH. 2 L 7 2 4F RT A28NM 2007032700167 20070327 00167 NE 2007 3 27 TRAX200700413 2 20070319 A 7200 ENGINE AEROSP ATR72 ATR72 EU PWA 120 PW120 NE LEFT FAILED A ASOA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 27 635AS 372 LEFT ENGINE FAILURE IN FLT. EMERGENCY DECLARED. 2 H 7 2 4T 4 T RT E20NE 2007032700171 20070327 00171 WP 2007 3 27 UPS07849537 1 20070321 A 3240 BRAKE ASSY DOUG DC8 DC873F 302199F WP NR 6 WHEEL BROKEN A IPXA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 894UP 46094 INSPECTION TYPE:N/A BTB 20:10Z REASON FOR BTB IS BLOWN TIRE ON T/O ROLL. PERFORMED REJECTED TAKEOFF. FOUND NR 6 WHEEL ASSY BROKEN (RIM). REPLACED NR 6 BRAKE ASSY AND WHEEL ASSY PER MM 32-42-01-4 AND MM 32-40-01-2. NO OTHER DAMAGE FOUND. 2 L 7 4 4F RT 4A25 2007032700173 20070327 00173 WP 2007 3 27 UPS07849542 1 20070322 A 3350 LIGHT DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A IPXA O OTHER O OTHER CL CLIMB 1 SO 01 851UP 46051 AFTER TAKEOFF, EMERGENCY LIGHTS CAME ON AND WOULD NOT EXTINGUISH EXCEPT TO DISARM EMERGENCY LIGHTS. FOUND C/B PULLED. RESET C/B AND PERFORMED EMERGENCY LIGHTS. OPS CHECK PER MM 33-50-01-2. EMERGENCY LIGHTS, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2007032700174 20070327 00174 NM 2007 3 27 UPS07M49539 1 20070123 A 5710 STRAP DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C RIGHT WING L/E LWR COMPT STA XORP562 FOUND UPPER STRAP CRACK AS MARKED. AS ABOVE STATED AREA, STRINGE R SPLICE REMOVED PER EN1060-07. DAMAGED STRINGER TRIMMED PER EN1060-07. HFEC CUTOUT FOUND SATISFACTORY. NEW STRINGER & SPLICE FAB PER EN1060-07. NEW FAB STRINGER & SPLICE DRILLED HOLES PER EN106 0-07. NEW PARTS OK TO INSTALL. RIGHT WI NG L/E LWR COMPT STA XORS 562 REPAIR PARTS INSTALLED AS PER EN1060-07, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007032700176 20070327 00176 NE 2007 3 27 AALA20070448 2 20070306 A 7210 GEARBOX DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LEFT ENGINE SEIZED A AALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SW 21 7549A 53031 718496 MEM INFLIGHT, AT FLIGHT LEVEL 350 LEFT ENGINE SHUTDOWN. LANDED MEM WITHOUT INCIDENT. FOUND NUMBER ONE ENGINE GEARBOX SEIZED. REPLACED NUMBER ONE ENGINE ON 08 MARCH 2007 AT MEM. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007032700177 20070327 00177 NE 2007 3 27 DXTA200702048 2 20070325 A 7261 OIL SYSTEM BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE RT ENGINE OVERTEMP E DXTA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 GL 07 142QS RK432 PCEJA0654 ON TAKEOFF, NOTICED YAW JUST BEFORE ROTATION. NORMAL TAKEOFF. WHEN LEVEL AT 3000 FT - 200KTS NOTICED RT ENGINE OIL TEMP IN RED. REDUCED THRUST OIL TEMP OUT OF RED, LANDED. FOUND RIGHT ENGINE OIL TEMP/PRESS GAUGE INCORRECT. REMOVED RIGHT ENGINE OIL TEMP/PRESSURE GAUGE AND INSTALLED AN OVERHAULED INDICATOR. ALL WORK PERFORMED IAW HAWKER 400XP MM 31-10-00. 2 H 7 2 4F 4 F RT A16SW E25EA 2007032700179 20070327 00179 NM 2007 3 27 AALA20070472 1 20070311 A 3350 P4010051112 MODULE BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA O OTHER O OTHER TO TAKEOFF 1 SW 21 676AN 29426 MIA - EMERGENCY LIGHT ALONG FLOOR AT LAST 10 ROWS OF COACH FLICKERED DURING TAKEOFF AND REMAINED OFF DURING CLIMB. ALL INDICATIONS NORMAL. REPLACED MODULE FOR EMERGENCY LIGHTS AT LAST 10 ROS OF COACH. SYSTEM GROUND CHECKED NORMAL OPERATI ON. 2 L 7 2 4F RT A2NM 2007032700180 20070327 00180 NM 2007 3 27 AALA20070473 1 20070311 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 777AN 29585 DFW - EMERGENCY SEAT MOUNTED LIGHT AT SEAT 26C IS MISSING BULB. RELAMPED EMERGENCY SEAT MOUNTED LIGHT AT SEAT 26C. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032700181 20070327 00181 NM 2007 3 27 AALA20070450 1 20070307 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 791AN 30254 MIA - EMERGENCY LIGHTS AT SEAT 21C HAS MISSING LENS. REPLACED LENS CAP FOR EMERGENCY LIGHTS AT SEAT 21C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032700185 20070327 00185 NM 2007 3 27 AALA20070470 1 20070310 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 182AN 29592 DFW - EMERGENCY LIGHT ON EXTERIOR OF RIGHT NUMBER THREE DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT ON THE EXTERIOR OF R IGHT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007032700186 20070327 00186 NM 2007 3 27 AALA20070453 1 20070307 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 788AN 30011 DFW - EMERGENCY LIGHT AT ELECTRICAL ACCESS IN FORWARD GALLEY BROKEN. REPLACED EMERGENCY LIGHT AT L105 AT ELECTRICAL ACC ESS IN FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032700190 20070327 00190 NM 2007 3 27 AALA20070458 1 20070307 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 795AN 30257 DFW - EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT T00001SE 2007032700191 20070327 00191 NM 2007 3 27 AALA20070459 1 20070307 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 795AN 30257 DFW - EMERGENCY LIGHT AT SEAT 22C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032700193 20070327 00193 CE 2007 3 27 DXTA200702046 1 20070323 A 2750 FLAP SYSTEM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS MALFUNCTIONED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED DE DESCENT 1 GL 07 960QS 7500160 AT 16000 FEET AND 230 KIAS, FLAPS WERE SELECTED TO 5 DEGREES, SLATS EXTENDED BUT FLAPS STUCK AT 3 DEGREES AND THE AMBER (FLAPS FAIL) CAS ILLUMINATED. REMOVED & REPLACED FLAP POWER DRIVE UNIT, ACCOMPLISHED COMPLETE FLAP SYSTEM RIG IAW CE750 MM 27-50-00. OPERATIONALY CHECKS GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007032700194 20070327 00194 NE 2007 3 27 NWAA071096315 2 20070318 A 7200 ENGINE BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE NR 2 FAILED A NWAA J A DUMP FUEL UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 01 675NW 33001 717559 DURING CRUISE, AT FL330, NR 2 ENGINE FLAMED OUT. FLIGHT CREW DECLARED AN EMERGENCY, DUMPED 30,000 POUNDS OF FUEL AND RE TURNED TO NRT. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND METAL CONTAMINATION IN THE OIL FILTER A ND ON THE CHIP DETECTORS. REMOVED AND REPLACED THE NR 2 ENGINE, TESTED AND RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032700195 20070327 00195 NM 2007 3 27 AALA20070456 1 20070307 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 618AA 24526 DFW - EMERGENCY LIGHT AT FORWARD RIGHT WING INOPERATIVE. RELAMPED EMERGENCY LIGHT AT FORWARD RIGHT WING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007032800028 20070328 00028 SO 2007 3 28 C2XA07IA071 1 20070326 A 2530 COFFEEMAKER EMB 145 EMB145XR 3260214 SO GALLEY ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 14116 145672 IAH FLIGHT 2560, THE CREW REPORTED THAT THE COFFEEMAKER HAD A BURNING SMELL IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHO UT INCIDENT WHERE MAINTENANCE INSPECTED THE COFFEEMAKER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APP ROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007032700196 20070327 00196 EA 2007 3 27 REXA200700050 1 20070325 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT STUCK A REXA K NONE L NO TEST IN INSP/MAINT 1 SO 25 8683B 7683 RIGHT SIDE EMERGENCY OVERWING EXIT JAMMED. OPERATIONALLY CHECKED GOOD RIGHT SIDE OVERWING EXIT IAW AIRCRAFT MAINTENANCE MANUAL (AMM) 52-20-00. 2 L 7 2 4F RT A21EA 2007032700197 20070327 00197 NM 2007 3 27 NWAA071105508 1 20070319 A 5414 SKIN BOEING 757 757251 1384970 NM NR 2 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 506US 23195 DURING SCHEDULED ENGINE REPLACEMENT INSPECTION REVEALED CRACK IN THE NR 2 PYLON RT SKIN. REPAIRED PER EA 55-209137. 2 L 7 2 4F RT A2NM 2007032700198 20070327 00198 NM 2007 3 27 DU4R2007073 1 20070223 A 2750 113N21052 TORQUE TUBE BOEING 757232 BOEING 757 757232 1384965 NM FLAP CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 636DL 000175 23763 FOUND CORROSION INSIDE LT I/B T/E FLAP TORQUE TUBE. REPAIRED BY REMOVING AND REPLACING TORQUE TUBE WITH P/N 117N2105-1 NSN, CARRIAGE ASSY WITH P/N 113N2100-13 S/N 248, FAIL SAFE AND P/N 113N2108-1 NSN IAW DELTA EA 06-097981-14 REV A. 2 L 7 2 4F RT A2NM 2007032700199 20070327 00199 NM 2007 3 27 DU4R2007072 1 20070224 A 2750 113N21051 TORQUE TUBE BOEING 757232 BOEING 757 757232 1384965 NM FLAP ASSY CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 636DL 000175 23763 FOUND CORROSION INSIDE LT I/B T/E FLAP TORQUE TUBE. REPAIRED BY REMOVING AND REPLACING TORQUE TUBE WITH P/N 117N2105-1 NSN, CARRIAGE ASSY WITH P/N 113N2100-13 S/N 248, FAIL SAFE AND P/N 113N2108-1 NSN IAW DELTA EA 06-097981-14 REV A. 2 L 7 2 4F RT A2NM 2007032700205 20070327 00205 NM 2007 3 27 USAA070241 1 20070327 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 STA 727D - 727F LEFT SIDE OF CARGO COMPARTMENT HAS CORROSION. INSTALLED FAB'D REPAIR PARTS PER SRM 53-60-53; CORR TASK C53-107-02; LEVEL 2, DEFECT SIZE: 40 INCHES. 2 L 7 2 4F RT A16WE 2007032700207 20070327 00207 NM 2007 3 27 HNAA0700052 1 20070325 A 3397 CONNECTOR DHAV DHC8 DHC8101 2809002 NM CABIN BURNED A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 07 812EX 38014 38014 312 SMOKE COMING FROM FILLER PANEL FORWARD RIGHT HAND SIDE ABOVE EMERGENCY EXIT. REMOVED AND REPLACED P40 MALE AND FEMALE C ONNECTORS. 2 H 7 2 4T RT A13NM 2007032700208 20070327 00208 NM 2007 3 27 HNAA0700053 1 20070325 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE O OTHER UK UNKNOWN 1 EA 07 912HA 40 EMERGENCY LIGHT SWITCH ON FLIGHT ATTENDANTS PANEL IS NOT ILLUMINATED. RELAMPED SWITCH. 2 H 7 2 4T RT A13NM 2007032700209 20070327 00209 WP 2007 3 27 ABXA070083 1 20070307 A 5313 5914259501 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 949AX 47325 LONGERON 20 INBOARD AT LEFT WHEEL WELL CORRODED AT STA 718. REMOVED LONGERON 20. DRILLED LONGERON 20 P/N 5914259-501AX , IAW DOUGLAS DWG 5914579 AND DC9 SRM 51-10-4. REINSTALLED LONGERON 20 IAW DWG 5914579, DC9 SRM 51-30-5 AND 51-30-1. 2 L 7 2 4F A6WE 2007032700211 20070327 00211 WP 2007 3 27 ABXA070079 1 20070228 A 5311 59114481 FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 949AX 47325 FORWARD LOWER CARGO FRAME CORRODED AT FS 465 BETWEEN LONGERON 28 LEFT AND LONGERON 28 RIGHT. REMOVED CORROSION AND REPL ACED SECTION OF FRAME IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 2007032700213 20070327 00213 WP 2007 3 27 ABXA070081 1 20070302 A 5320 99577263 INTERCOSTAL DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 949AX 47325 CORROSION AT AND AROUND INTERCOSTAL STA 737 - 756, LEFT BUTT LINE 22. INSTALLED INTERCOSTAL IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2007032700214 20070327 00214 WP 2007 3 27 ABXA070082 1 20070302 A 5347 S2914913M24000 SEAT TRACK DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 949AX 47325 LOWER LEG OF SEAT TRACK CORRODED AT STA 699, RIGHT BUTT LINE 10. BLENDED OUT OF LIMITS. REMOVED SEAT TRACK FROM STA 66 3 - 763 AND FLOOR PANEL 8F. REINSTALLED NEW SEAT TRACK IAW DC9 SRM DWG K05482. RE-INSTALLED FLOOR PANEL 8F IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 2007032700217 20070327 00217 SO 2007 3 27 RAIA00703036 1 20070316 A 3260 ELECTRONIC UNIT EMB 145 EMB145LR 3260212 SO LANDING GEAR MALFUNCTIONED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 843HK 14500822 FLT NR 7962 - ORD - LANDING GEAR/GRD FAIL MESSAGE. MAINTENANCE RESET LANDING GEAR ELECTRICAL UNIT NO FURTHER MSG DISPLA YED CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT T00011AT 2007032700218 20070327 00218 SO 2007 3 27 RAIA00703037 1 20070317 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 830HK 145313 PRE FLT NR 5549 - STL - EMERGENCY LIGHTS OUT AT MAIN DOOR EXIT MARKER AND GALLEY WALL EXIT LOCATOR. CYCLED POWER SYSTEM CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007032700219 20070327 00219 SO 2007 3 27 RAIA00703038 1 20070317 A 8097 CONNECTOR EMB 145 EMB145LR 3260212 SO ENGINE DIRTY A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 812HK 145373 FLT NR 5571 - STL - NR 1 ENGINE WILL NOT START. MAINTENANCE CLEANED CONNECTOR TO ENGINE START CONTROL VALVE, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007032800001 20070328 00001 EA 2007 3 28 TRAX200700401 1 20070319 A 5720 ANGLE CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 837AS 7271 UPPER ATTACH ANGLE BETWEEN LT WING INBOARD AND MIDDLE LE`S ARE CRACKED. REMOVED DAMAGED ANGLE ON LT WING LE AND DUPLICA TED USING 0.040, 2024-T3 PER CRJ SRM 51-24-21 AND 51-40-11. OK TO ALODINE, PRIME, AND INSTALL. ALODINED AND PRIMED ANGLE IAW CRJ SRM 51-25-06 AND INSTALLED IAW CRJ SRM 51-42-06 AND 51-42-13. 2 L 7 2 4F RT A21EA 2007032800002 20070328 00002 EA 2007 3 28 TRAX200700402 1 20070319 A 5740 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 837AS 7271 RT. WING I/B L/E, O/B ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED RT WING L/E ATTACH ANGLE (P/N 600-12025-8), IAW CRJ SRM 51-40-11 PG 1-3, CRJ SRM 51-41-02 PG 1-5. 2 L 7 2 4F RT A21EA 2007032800003 20070328 00003 EA 2007 3 28 TRAX200700403 1 20070319 A 5740 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 837AS 7271 RT WING MIDDLE L/E,I/B ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED RT WING ATTACH ANGLE L/E, IAW CRJ SRM 51-40-11 PG 1-3, CRJ SRM 51-41-02 PG 1-5, P/N 600-12045-12. 2 L 7 2 4F RT A21EA 2007032800004 20070328 00004 EA 2007 3 28 TRAX200700399 1 20070319 A 5740 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 837AS 7271 UPPER ATTACH ANGLE BETWEEN RT WING I/B AND MIDDLE L/E'S IS CRACKED. REMOVED DAMAGED UPPER ATTACH ANGLE BETWEEN RT WING I/B AND MIDDLE L/E'S AND DUPLICATED USING 0.040, 2024-T3, PO 10054 PER CRJ SRM 51-24-36, 51-24-21, AND 51-40-11. INSTAL LED SERVICEABLE DUPLICATED UPPER ATTACH ANGLE BETWEEN RT WING I/B AND MIDDLE L/E'S PER CRJ SRM 51-45-00 AND 51-23-00. 2 L 7 2 4F RT A21EA 2007032800005 20070328 00005 SO 2007 3 28 RAIA00703039 1 20070317 A 2760 SPOILER SYS EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 835HK 145670 PRE FLT NR 7922 - DAY-SPOILER FAIL MGS. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL TEST OF SPOILER SYSTEM, OPS CHE CK NORMAL, NO MSG. 2 L 7 2 4T RT T00011AT 2007032800006 20070328 00006 EA 2007 3 28 TRAX200700400 1 20070319 A 5740 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 837AS 7271 LT WING MIDDLE L/E,I/B ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED LEFT WING L/E I/B ATTACH ANGLE, WITH NEW ONE, P/ N 600-12045-11, IAW CRJ SRM 51-41-02 PG 1-5, AND 51-40-11 PG 1-3. 2 L 7 2 4F RT A21EA 2007032800008 20070328 00008 SO 2007 3 28 RAIA00703043 1 20070318 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 824HK 145498 POST FLT NR 5542 - STL - AISLE FLOOD LIGHT EMERGENCY LIGHT INOP. MAINTENANCE RE-BULBED EMERGENCY CEILING WASH LIGHT, OP S CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007032800009 20070328 00009 SO 2007 3 28 RAIA00703044 1 20070319 A 3350 LIGHT EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 827HK 145021 PRE FLT NR 5553 - STL - EMERGENCY LIGHTS ON STAIRS INOP. MAINTENANCE REMOVED AND REPLACED LIGHT BULB, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007032800010 20070328 00010 CE 2007 3 28 DXTA200702042 1 20070322 A 3260 SQUAT SWITCH CESSNA 750 750 2076810 CE NLG OUT OF RIG E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 971QS 7500071 UPON T/O MEM, GEAR WOULD NOT RETRACT. RETRACTED HANDEL INIATIALLY. RED GEAR LITE CAME ON, GEAR DID NOT COME UP. PLACED G EAR HANDEL DOWN , 3 GREEN NO RED , RETURNED TO MEM.FOUND NOSE GEAR SQUAT SWITCH OUT OF RIG. RIGGED NOSE GEAR SQUAT SWITC H IAW CESSNA 750 MM 32-60-00. GEAR OPS CHECK GOOD ON NUMEROUS CYCLES. 2 L 7 2 4J RT T00007WI 2007032800011 20070328 00011 SO 2007 3 28 RAIA00703045 1 20070319 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN DIRTY A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 810HK 145231 PRE FLT NR 7912 - IAD - EMERGENCY LIGHT AT RIGHT HAND OVERWING EXIT IDENTIFIER IS INOP. MAINTENANCE CLEANED CONNECTORS FOR EMERGENCY LIGHT, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007032800012 20070328 00012 NM 2007 3 28 07FDEA00730 1 20070309 A 5713 ARB75132 STRINGER DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT HAND WING TANK - APPROX 13 INCHES CRACK FOUND AT STRINGER END 13R (XORS 577) DURING HFEC INSPECTION STRINGER EN D 13R (XORS 577)AT RIGHT HAND WING TANK REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007032800013 20070328 00013 NM 2007 3 28 07FDEA00731 1 20070309 A 5713 ARB75142 STRINGER DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT HAND WING TANK - APPROX 15.5 INCHES LENGTH CRACK FOUND AT STRINGER END 14R (XORS 521) DURING HFEC INSPECTION ST RINGER END 14R (XORS 521)AT RIGHT HAND WING TANK REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLAS SIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007032800014 20070328 00014 SO 2007 3 28 RAIA00703046 1 20070319 A 5270 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT ACTIVATED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 831HK 145232 FLT NR 8028 - IAD - CARGO DOOR WARNING CAP CAME ON, DURING TAKEOFF ROLL. MAINTENANCE DEFERRED PER MEL. 2 L 7 2 4T RT T00011AT 2007032800017 20070328 00017 SO 2007 3 28 RAIA00703047 1 20070319 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN MALFUNCTIONED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 802HK 145066 POST FLT NR 3545 - STL - EMERGENCY LIGHT ON FLOOR ADJACENT TO SEAT 3A (FLOOR PROXIMITY LIGHT) INOP. MAINTENANCE PERFORM ED SEVERAL OPS CHECK OF EMERGENCY LIGHTING, ALL FLOOR LIGHTS OPS CHECKED GOOD. NO DEFECTS NOTED. 2 L 7 2 4F RT T00011AT 2007032800018 20070328 00018 EU 2007 3 28 UPS07149545 1 20070323 A 3350 CM1864 LIGHT AIRBUS A300 A300F4622R 3930360 EU COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 167UP 0862 INSPECTION TYPE:PS DURING TEST OF GLARESHIELD EMERGENCY LIGHTS FOUND LAMP 133LE INOP. RELAMPED AND CHECKS GOOD PER PS C K METHODS STEP 10 AND MM 33-12-00-09. 2 L 7 2 4F RT A35EU 2007032800019 20070328 00019 NM 2007 3 28 UPS07549553 1 20070323 A 3350 LIGHT BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 402UP 23724 INSPECTION TYPE:N/A EMERGENCY LIGHTS DISARM LIGHT HAS 1 INOP BULB. RELAMPED, OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2007032800021 20070328 00021 WP 2007 3 28 UPS07849551 1 20070312 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C3 DEEP CREASED DENT 3 INCHES LONG ON LEADING EDGE O/B RIGHT WING. FABRICATED AND INSTALLED REPAIR DOUB LER IAW SRM 57-02-01-00 FIG 002H. 2 L 7 4 4F RT 4A25 2007032800025 20070328 00025 SO 2007 3 28 C2XA07IA073 1 20070322 A 2150 A/C PACK EMB 145 EMB145EP 3260221 SO CABIN SMOKE A C2XA H DEACTIVATE SYST/CIRCUITS C B F.O.D. SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 16927 145006 IAH - FLIGHT 2372, THE CREW REPORTED AN OVERWHELMING SMELL OF SMOKE IN THE CABIN AND COCKPIT THAT GOT BETTER WITH THE PA CKS OFF. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND DISCOVERED THAT THE N UMBER ONE ENGINE HAD SUFFERED A BIRD STRIKE. MAINTENANCE CLEANED THE RESIDUE FROM THE ENGINE, BORESCOPE INSPECTED AND O PERATIONALLY CHECKED WITH NO DEFECTS/SMELL NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007032800031 20070328 00031 NM 2007 3 28 KCSA071079 1 20070323 A 5420 ANGLE BOEING 747 747236B 1384804 NM NR 2 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 NR 2 PYLON STA 219 ANGLE CRACKED .75 INCH. 2 L 7 4 4F A20WE 2007032800032 20070328 00032 NM 2007 3 28 KCSA071080 1 20070323 A 5412 FIRESHIELD BOEING 747 747236B 1384804 NM NR 4 PYLON GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 NR 4 PYLON I/B SIDE FIRESHIELD GOUGE NAC STA 180. 2 L 7 4 4F A20WE 2007032800035 20070328 00035 SO 2007 3 28 RAIA00703054 1 20070321 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 818HK 145059 POST FLT NR 5556-STL - EMERGENCY LIGHT AT COCKPIT STEP EXIT IDENTIFIER IS INOP. MAINTENANCE FOUND LOOSE WIRE ON EXIT. REPAIRED WIRE, OPS CHECKED EMERGENCY LIGHTING GOOD. 2 L 7 2 4T RT T00011AT 2007032800036 20070328 00036 SO 2007 3 28 RAIA00703053 1 20070320 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 841HK 145382 POST FLT NR 8045 - STL - FLOOR PROXIMITY LIGHT EMERGENCY FLOOR STRIP LIGHT INOP. MAINTENANCE REMOVED AND REPLACED FORWA RD LIGHT BULBS ABOVE 1A, OPS CHECK GOOD. PERFORMED OPS CHECK ON FLOOR PROX LIGHT, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007032800037 20070328 00037 NM 2007 3 28 SCNA07005 1 20070324 A 2560 COVER BOEING 737 7378Q8 13844BX NM CABIN MISSING A SCNA K NONE O OTHER UK UNKNOWN 1 GL 15 806SY 28215 FLIGHT CREW FOUND ROW 12F EXIT SIGN COVER MISSING. MAINTENANCE THEN REPLACED THE COVER. 2 L 7 2 4F RT A16WE 2007032800041 20070328 00041 NM 2007 3 28 CALA0700141 1 20070323 A 5320 147A8540U7 STRUCTURE BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13248 28808 INSPECTION FOUND L-2 DOOR CHORD CORRODED AT STA 947-986.5, LBL 52. THE CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007032800043 20070328 00043 NM 2007 3 28 CALA0700144 1 20070324 A 5314 6562125 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 77303 23354 INSPECTION FOUND LT KEEL BEAM I/B LOWER FLANGE CORRODED AT STA 537, S28L, O/B AND AFT OF A/C GROUND CONNECTION. A KEEL BEAM SPLICE REPAIR WAS INSTALLED IAW SRM 53-60-12, FIGURE 201. 2 L 7 2 4F RT A16WE 2007032800045 20070328 00045 NM 2007 3 28 CALA0700146 1 20070325 A 5310 6520723U66 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 77303 23354 INSPECTION FOUND A .75 INCH CRACK IN FORWARD CARGO DOOR CUTOUT AFT FRAME LOWER STOP PAD, STA 480, S24R. THE AFT FRAME W AS REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007032800047 20070328 00047 NM 2007 3 28 CALA0700148 1 20070323 A 5320 141T5134146 FLOOR SUPPORT BOEING 767 767424ER 1385270 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76064 29459 INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 303-325, LBL 31. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-02, PAGE 8 AND SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007032800050 20070328 00050 NM 2007 3 28 CALA0700151 1 20070325 A 3350 ADD71701100 BATTERY PACK BOEING 737 737724 13844BY NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13718 28937 THE AFT OVERHEAD EMERGENCY LIGHT BATTERY PACK WAS FOUND INOPERATIVE DURING SERVICE CHECK. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-06-960-805. 2 L 7 2 4F RT A16WE 2007032800052 20070328 00052 NM 2007 3 28 KCSA07027 1 20070324 A 2121 FAN BOEING 747 747209B 138489B NM COCKPIT DEFECTIVE A KCSA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 715CK 22447 LOUD RUMBLE DURING CRUISE ACCOMPANIED BY ACRID ODOR. TURNED OFF FLIGHT DECK FAN. RUMBLE IMMEDIATELY STOPPED, ODOR DISS IPATED IN APPROXIMATELY THREE MINUTES. 2 L 7 4 4F RT A20WE 2007032600048 20070326 00048 WP 2007 3 26 AALA20070414 1 20070301 A 3213 STRUT DOUG DC9 DC982 3022082 WP NOSE GEAR DAMAGED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7543A 53025 YYC - INFLIGHT NOSE LANDING GEAR WOULD NOT RETRACT. RETURNED TO YYC AND LANDED WITHOUT INCIDENT. REPACK NOSE GEAR SHOC K STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007032600052 20070326 00052 EU 2007 3 26 AALA20070434 1 20070304 A 2910 90G1182 PRESSURE SWITCH AIRBUS 300 A300B4605R 3930308 EU HYD SYSTEM INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SW 21 41063 506 SJU - INFLIGHT DURING APPROACH LOST GREEN HYDRAULIC SYSTEM. LOW QUANTITY, LOW PRESSURE INDICATOR ON AND HYDRAULIC LOW P RESSURE CAUTION LIGHT ILLUMINATED. MANUALLY LOWERED LANDING GEAR. LANDED WITHOUT INCIDENT. REPLACED HYDRAULIC PRESSUR E SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007032600054 20070326 00054 EA 2007 3 26 TRAX200700382 1 20070317 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 PAX DOOR HANDLE IS CRACKED. PAX DOOR STEP NR 2 REMOVED IAW AMM 20-21-00. HANDLE REMOVED IAW AMM 52-11-03. HANDLE INSTA LLED IAW AMM 52-11-03. PAX DOOR STEP NR 2 INSTALLED IAW AMM 20-21-00. PAX DOOR FUNCTIONAL TEST C/OUT IAW AMM 52-11-03. PAX DOOR OPS TEST C/OUT IAW AMM 52-11-03. 2 L 7 2 4F RT A21EA 2007032600064 20070326 00064 NM 2007 3 26 AALA20070419 1 20070302 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 766AN 32880 MIA - EMERGENCY LIGHT AT SEAT 21C BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 21C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032600066 20070326 00066 NM 2007 3 26 AALA20070433 1 20070304 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 952AA 30088 MIA - EMERGENCY LIGHT RED LENS IN CABIN BROKEN. REPLACED RED LENS FOR EMERGENCY LIGHT IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007032600074 20070326 00074 NM 2007 3 26 AALA20070435 1 20070305 A 3040 WIRE BOEING 757 757223 1384957 NM WINDOW HEAT BURNED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 187AN 32381 LAX - INFLIGHT RETURNED TO LAX DUE TO SMOKE AND ELECTRICAL ODOR IN COCKPIT. LANDED WITHOUT INCIDENT. FOUND WIRE TO LEF T NUMBER ONE WINDOW HEAT CONNECTION BURNED. REPAIRED WIRE AND REPLACED LEFT NUMBER ONE WINDOW. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007032600078 20070326 00078 NM 2007 3 26 AALA20070440 1 20070305 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 776AN 29582 DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR AT FLOOR 1 103 INOPERATIVE. REPLACED EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032600090 20070326 00090 EA 2007 3 26 TRAX200700373 1 20070316 A 5313 STRINGER CNDAIR CL600 CL6002B19 1900309 EA BS 333-349 S27 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 CORROSION ON STR 27 FROM FS 333 TO 349. (SUPPLEMENTAL 28 MARCH 07) COMPLIED WITH EC/TC REO 670-53-21-261 NO FURTHER ACTION REQUIRED. 2 L 7 2 4F RT A21EA 2007032600097 20070326 00097 CE 2007 3 26 45AX022607 1 20070226 A 2620 331000211 FIRE BOTTLE LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE731* 01518 WP TAIL CONE FALSE INDICATION E K NONE N FALSE WARNING IN INSP/MAINT 1 SW 15 45AX 1858 206 FIRE BOTTLE GAUGE HAS INACCURATE INDICATION, FOUND TO INDICATE (0) ON PREFLIGHT. THE BOTTLE WAS REMOVED AND DETERMINED TO BE FULL OF AGENT AND NOTICED ROTATING THE BOTTLE MOVED THE PRESSURE GAUGE. BY HAND SHAKING THE BOTTLE THE PRESSURE I NDICATION WOULD MOVE FROM A (0) INDICATION UP TO 800 PSI. THE BOTTLE WAS REPLACED WITH AN O/H UNIT. 2 L 7 2 4F 4 F RT T00008WI E6WE 2007032600100 20070326 00100 EA 2007 3 26 2007F00023 1 20070306 A 2612 24412086 FIRE LOOP CNDAIR CL600 CL6001A11 1900302 EA LYC ALF502 ALF502* 41580 EA LT ENGINE SHORTED E A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 403WY 8054 1059 FLIGHT CREW REPORTED LT ENGINE FIRE DETECTION FAIL LIGHT CAME ON JUST PRIOR TO ROTATION, THEN FIRE WARNING CAME ON AT 1, 500 FEET DURING CLIMB. STAYED ON AFTER DISCHARGING BOTH FIRE BOTTLES. RETURNED TO BASE, AFTER LANDING, APPEARED TO BE NO FIRE. FOUND LT ENGINE PYLON FIRE LOOP BAD AND LT ENGINE CORE FIRE LOOP BAD. REPLACED IAW M/M. PERFORMED FIRE DETECTION SYSTEM OP'S CHECK, NO DEFECTS NOTED 2 L 7 2 4F 4 F RT A21EA E6NE 2007032600113 20070326 00113 NM 2007 3 26 UIEA200700130 1 20070304 A 5310 65B050021411 STRAP BOEING 747 7472D3B 1384805 NM GE CF6 CF650* 30018 NE BS 800 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 CRACKS FOUND ON BS 800 LT STRAP AND INNER CHORD AT NR 2 MAIN ENTRY DOOR. REPAIRED ACCOMPLISHED IAW SR ID NR 1-289052431 AND FAA FORM 8100-9. 2 L 7 4 4F 4 F RT A20WE E23EA 2007032600141 20070326 00141 NM 2007 3 26 SWAA071462 1 20070320 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007032600159 20070326 00159 NM 2007 3 26 DL76L070222 1 20070320 A 5415 311T31271 ANGLE BOEING 767 767332 1382001 NM NR 1 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 172DN 24775 THE NR 1 PYLON MIDSPAR FITTING CLOSEOUT ANGLE WAS FOUND CRACKED. THE CRACKED ANGLE WAS REPLACED, REF AD 2005-19-23, 01- 074944-12AD. 2 L 7 2 4F RT A1NM 2007032600160 20070326 00160 NM 2007 3 26 DL76L070223 1 20070319 A 5415 311T31571 ANGLE BOEING 767 767332 1382001 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 172DN 24775 THE NR 2 PYLON MIDSPAR FITTING CLOSEOUT ANGLE WAS FOUND CRACKED. THE CRACKED ANGLE WAS REPLACED, REF AD 2005-19-23. 2 L 7 2 4F RT A1NM 2007032700002 20070327 00002 WP 2007 3 27 IXXA070018S 1 20070322 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 87731 1836 45811 DURING ROUTINE CPCP INSPECTION, FOUND RIGHT WING UPPER SKIN CRACKED AT STATION XRS 74 STRINGER 9. REMOVED DAMAGE AREA, NO CRACK'S OR CORROSION FOUND AFTER DAMAGE REMOVED. MANUFACTURED REPAIR PARTS. TREATED AND PRIMED AREA AND REPAIR PART S. INSTALLED REPAIR PARTS IAW DACO DC8 SRM 57-2-1 FIGURE 10. 2 L 7 4 4F RT 4A25 2007032700003 20070327 00003 EA 2007 3 27 SWIA200718039 1 20070321 A 5610 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 611SK 10035 FIRST OFFICERS SIDE WINDOW CRACKED IN FLIGHT. REPLACED FIRST OFFICER'S SIDE WINDOW IAW RII 56-220-1000 AND AMM 56-11-01 . OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007032700014 20070327 00014 NM 2007 3 27 DLM88070204 1 20070312 A 2432 021904000 BATTERY DOUG MD88 MD88 3023688 NM MASTER UNSERVICEABLE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 912DL 49543 ON TAXI IN RAMP REPORTED SMOKE/STEAM COMING FROM UNDER A/C. CALLED MTC TO INVESTIGATE SAME. FOUND SHIPS BATTERIES OVER HEATED. NO DAMAGE TO A/C, BATTERIES OR CHARGER. REPLACED MAIN BATTERIES AND CHARGER. OP AND SYSTEM TESTS OK. 2 L 7 2 4F RT A6WE 2007032700025 20070327 00025 NM 2007 3 27 DLM90070196 1 20070307 A 5342 591214186 ATTACH ANGLE DOUG MD900 MD900 3027375 NM VERTICAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 916DN 53396 THE RT FUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE WAS FOUND WITH A CRACK NEAR THE AFT END OF THE ANGLE. THE CRACK MEA SURED 1" LONG AND IS TYPICAL OF CRACKS DOCUMENTED PER BAC S/B MD90-53-027. THE CRACK WAS TRIMMED OUT AND REPAIRED WITH A REPAIR ANGLE PER THE S/B AND PER DAL ER/A 460482-14. 1 G 7 2 3U NC H19NM 2007032700044 20070327 00044 SO 2007 3 27 SIMA200708505 1 20070311 A 5320 14521718007 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 738NR 13393 4800 145401 LEFT OMEGA BEAM RAMP SUPPORT IN GALLEY FOUND CORRODED. REMOVED AND REPLACED RAMP SUPPORT IAW EMB SRM 51-40-02. RETURNE D AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007032700045 20070327 00045 SO 2007 3 27 SIMA200708504 1 20070311 A 5320 14590082003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 738NR 13393 4800 145401 CENTER BEAM RAMP SUPPORT IN GALLEY AREA FOUND TO BE CORRODED. REMOVED AND REPLACED THE RAMP SUPPORT IAW EMB SRM 51-40-0 2. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007032700085 20070327 00085 EU 2007 3 27 AALA20070460 1 20070308 A 2780 JACKSCREW AIRBUS 300 A300B4605R 3930308 EU SLATS INOPERATIVE A AALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 21 14061 471 JFK INFLIGHT - SLATS DID NOT EXTEND FOR LANDING. LANDED JFK WITHOUT INCIDENT. REPLACED NUMBER SIX LEFT JACKSCREW. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007032700086 20070327 00086 WP 2007 3 27 AALA20070461 1 20070309 A 4910 5940405503 APU DOUG DC9 DC983 3022083 WP APU BAY UNKNOWN A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 569AA 49351 LAX INFLIGHT - AFTER TAKEOFF, FLIGHT ATTENDANTS REPORTED LIGHT SMOKE AND ODOR IN CABIN. RETURNED TO LAX AND LANDED WITH OUT INCIDENT. REPLACED APU AT LGA ON 15 MAR 2007. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007032700103 20070327 00103 2007 3 27 AWXA200700404 4 20070323 A 2565 SLIDE BOEING 757 7572S7 1384962 NM L4 DOOR NO TEST A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 905AW 23567 PHX - EES - L-4 DOOR SLIDE DEPLOYMENT FAILED DUE TO THE SLIDE COVER. MX REPOSITIONED THE SLIDE COVER, DEPLOYMENT WAS NO RMAL. 2 L 7 2 4F RT A2NM 2007032700104 20070327 00104 NM 2007 3 27 NWAA071116309 1 20070321 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 OVERNIGHT MAINTENANCE FOUND RT OVERWING 3 EA EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OPERATIO NAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007032700131 20070327 00131 NM 2007 3 27 DL764070214 1 20070316 A 2611 SMOKE DETECTOR BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL LAVATORY FALSE ACTIVATION A DALA O OTHER N FALSE WARNING CR CRUISE 1 SO 27 831MH 29702 P1375 REAR SMOKE ALARM WENT OFF IN FLT, TESTED SMOKE ALARM SYSTEM. TESTED OK. NO PROBLEMS FOUND. 2 L 7 2 4F 4 F RT A1NM E23EA 2007032700133 20070327 00133 NM 2007 3 27 DL777070216 1 20070319 A 2120 UNKNOWN BOEING 777 777232 1385232 NM CABIN ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 861DA 29952 FLT 17 FROM MAN REPORTED AN ELEC ODOR BY F/A BETWEEN 2L AND 3L ON CAPTS SIDE. NOT CONFIRMED. CHECKED ALL IFE VSEB AND CONNECTOR AT LT SIDE OF AFT OF L2 DOOR ALL OPS CHECK NORMAL/116167 PANASONIC/CHECK AREA FOUND NO ABNORMAL ODORS. CKD WI TH PACKS RUNNING HYDS ON RAN IFE OVENS ETC FOUND ALL NORMAL. 2 L 7 2 4F RT T00001SE 2007032700136 20070327 00136 NM 2007 3 27 SWAA071527 1 20070322 A 5311 6546538 FRAME BOEING 737 7373Y0 1384671 NM BS 597 S14R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 14R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007032700141 20070327 00141 NM 2007 3 27 SWAA071529 1 20070322 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 18Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 10 O`CLOCK POSITION. REPAIRED WEB PER E R. 2 L 7 2 4F RT A16WE 2007032700142 20070327 00142 NM 2007 3 27 SWAA071511 1 20070322 A 5312 6546568 BULKHEAD BOEING 737 7373Y0 1384671 NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 17R. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007032700152 20070327 00152 NM 2007 3 27 SWAA071531 1 20070322 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 380 S28L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007032700166 20070327 00166 NM 2007 3 27 NWAA071136314 1 20070321 A 2530 OVEN BOEING 747 747451 1384940 NM NR 2 GALLEY CONTAMINATED A NWAA F ACTIVATE FIRE EXT. W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 674US 30269 DURING CRUISE, THE FLIGHT ATTENDANTS NOTICED AN ODOR AT GALLEY 2. SMOKE SEEN COMING OUT OF THE OVEN, (NO FIRE), PER F/A INCIDENT REPORT "SPARKLES" OBSERVED AT BOTTOM OF OVEN. 4 HALOGEN FIRE BOTTLES WERE DISCHARGED. CIRCUIT BREAKERS WERE PULLED. NO EMERGENCY WAS DECLARED, FLIGHT CONTINUED ON AND LANDED WITHOUT INCIDENT. FLIGHT ATTENDANT FOUND HIDDEN PIEC E PAPER IN OVEN WAS CAUSE OF SMOKE. MAINTENANCE FOUND BAR ALIGNMENT MISSING. REMOVED AND REPLACED OVEN, OVEN CONTROLLE R, 4 HALOGEN FIRE BOTTLES, AND 2 PBE’S (PROTECTIVE BREATHING EQUIPMENT). OPERATIONAL CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007032700184 20070327 00184 WP 2007 3 27 AALA20070449 1 20070306 A 2913 PUMP DOUG DC9 DC983 3022083 WP RIGHT INOPERATIVE A AALA O OTHER J WARNING INDICATION DE DESCENT 1 SW 21 964TW 53614 SAN INFLIGHT - RIGHT HYDRAULIC PRESSURE WENT TO ZERO. USED ALTERNATE GEAR EXTENSION LEVER. LANDED SAN WITHOUT INCIDENT . REPLACED RIGHT ENGINE HYDRAULIC DRIVEN PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007032700189 20070327 00189 NM 2007 3 27 AALA20070457 1 20070307 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 618AA 24526 DFW - OVERHEAD EMERGENCY LIGHT AT ROW 4AB INOPERATIVE. RELAMPED OVERHEAD EMERGENCY LIGHT AT ROW 4AB. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007032700201 20070327 00201 NM 2007 3 27 USAA070246 1 20070327 A 5313 STRINGER BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 STA 947 2 STR 18L IN CARGO COMPARTMENT; CORR TASK C53-107-02; LEVEL 2. INSTALLED FAB'D REPAIR PART PER SRM 53-00-53; CO RR TASK C53-107-02; LEVEL 2, DEFECT SIZE: 6 INCH AREA. 2 L 7 2 4F RT A16WE 2007032800016 20070328 00016 SO 2007 3 28 C2XA07CL034 1 20070326 A 3350 602024 LIGHT EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 24128 145700 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT AT THE COCKPIT DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT AT THE COCKPIT DOOR. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2007032800048 20070328 00048 NM 2007 3 28 CALA0700149 1 20070323 A 5320 141T5107 FLOOR SUPPORT BOEING 767 767424ER 1385270 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76064 29459 INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 303, LBL 21 TO LBL 31. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 53-00-51, R EPAIR 1, FIGURE 201. 2 L 7 2 4F RT A1NM 2007032800049 20070328 00049 NM 2007 3 28 CALA0700150 1 20070321 A 5347 151N62947 SEAT TRACK BOEING 777 777224 1385225 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 74007 29477 INSPECTION FOUND SEAT TRACK CORRODED AT STA 1510-1586, RBL 108. REPAIRED IAW SRM 53-00-52, REPAIR 4, FIGURE 202. 2 L 7 2 4F RT T00001SE 2007032800051 20070328 00051 NM 2007 3 28 HNAA0700054 1 20070323 A 3231 ROD DHAV DHC8 DHC8102 2809003 NM MLG OUT OF ADJUST A HNAA D RETURN TO BLOCK E VIBRATION/BUFFET CL CLIMB 1 EA 07 934HA 139 FLIGHT ATTENDANT REPORTS FORWARD MAIN LANDING GEAR DOOR SHAKING AND WHEN CLOSED DOOR IS GAPPED. FLIGHT RETURNED TO FIEL D, NO EMERGENCY WAS DECLARED BUT RESCUE VEHICLES WERE DISPATCHED TO ESCORT AIRCRAFT TO GATE. ADJUSTED LEFT HAND FORWARD GEAR DOOR ACTUATOR ATTACH ROD. 2 H 7 2 4T RT A13NM 2007032800053 20070328 00053 SO 2007 3 28 C2XA07SH016 1 20070327 A 5512 14532235401 SKIN EMB 135 EMB135LR 3260305 SO HORIZ STAB CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16520 145372 SHV DURING C-CHECK LEFT HORIZONTAL STABALIZER LEADING EDGE HAS PITTING CORROSION. MX REPAIRED LEFT HORIZONTAL STABALIZE R IAW EC 5530-01116. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 2007032800054 20070328 00054 EA 2007 3 28 COMA0760270 1 20070320 A 3350 363782 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN CRACKED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 914CA 7012 FLIGHT 5199 - EMERGENCY LIGHTS INOP FROM ROW 8 THROUGH 12. EMERGENCY LIGHT STRIP CRACKED AT ROW 11. REPLACED ARROW LIG HTED STRIP. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007032800056 20070328 00056 EU 2007 3 28 USAA070174 1 20070309 A 5315 D5347209001100 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 163US 1417 RIGHT FLOORBEAM TO FLANGE FROM FR 64-68; -Y1160 TO -Y1292 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM PER SRM 51-72-1 1; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1 SQ INCH. 2 L 7 2 4F RT A28NM 2007032800057 20070328 00057 2007 3 28 COMA0760272 4 20070320 A 2215 6224404101 SERVO CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT SYS FAULTY A COMA K NONE E VIBRATION/BUFFET CL CLIMB 1 SO 01 785CA 20323 7326 FLIGHT 5042 - AFTER TAKEOFF ENGAGED AUTO PILOT AT 12000 FT, AT 20000 FT FELT SLIGHT VIBRATION AND YAW MOTION. EICAS SHO WED AILERON FLUTTERING. REPLACED AILERON SERVO, INSPECTED AILERON AND RUDDER CONTROL SYSTEMS AND PERFORMED AUTO PILOT O PERATIONAL CHECKS. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007032800060 20070328 00060 NM 2007 3 28 KCSA071084 1 20070326 A 5347 SEAT TRACK BOEING 747 747236B 1384804 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 MAIN DECK SEAT TRACK CORRODED AT BS 1930, RBL 11. 2 L 7 4 4F A20WE 2007032800061 20070328 00061 2007 3 28 BB07026 4 20070301 A 2565 101651303 LIGHT BOEING 767 767201 1385125 NM EVAC SLIDE FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 245AY 59540 11747 23897 DURING ACCOMPLISHMENT OF JOB CARD J825-60-10, ESCAPE SLIDE LIGHTS FAILED TO ILLUMINATE. CHECK MAINTENANCE REPLACED THE SLIDE ASSEMBLY. 2 L 7 2 4F RT A1NM 2007032800063 20070328 00063 NM 2007 3 28 USAA070235 1 20070327 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 STA 360 AT STR 9L HAS CRACK. REMOVED DAMAGED ANGLE & INSTALLED FABRICATED ANGLE PER BOEING DWG 69-48985, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007032800064 20070328 00064 NM 2007 3 28 USAA070236 1 20070327 A 5512 SKIN BOEING 737 737401 1384701 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 LEFT HORIZONTAL STAB, LOWER SURFACE AFT T/E SKIN BETWEEN STA 157.5 & 184.7 HAS CRACK. INSTALLED REPAIR DOUBLERS PER EA 98564 & SRM 55-10-07, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007032800065 20070328 00065 NM 2007 3 28 USAA070237 1 20070327 A 5320 WEB BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 STA 294.5 AT S15L HAS CRACK. REMOVED CRACKED WEB & FAB'D NEW & REINSTALLED PER SRM 51-10-02, DWG 65-17684, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007032800066 20070328 00066 NM 2007 3 28 USAA070238 1 20070327 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 BS 907 BETWEEN S-8L AND S-9L HAS CRACK. INSTALLED REPAIR ANGLES PER TYP REP 53-10-20E, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007032800068 20070328 00068 NM 2007 3 28 USAA070240 1 20070327 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 MAIN SVC DOOR Z-ANGLE AT STA 294-35 HAS CORROSION. REMOVED & INSTALLED NEW Z-ANGLE PER BOEING DWG 65C80735; CORR TASK C 53-107-02; LEVEL 2, DEFECT SIZE: 5 INCHES. 2 L 7 2 4F RT A16WE 2007032800070 20070328 00070 NM 2007 3 28 USAA070234 1 20070327 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 FUSELAGE SKIN AT AFT RIGHT DOOR AT UPPER HINGE CUTOUT HAS CRACK. INSTALLED REPAIR DOUBLER PER SRM 53-60-01, DEFECT SIZE : .125 INCH LONG. 2 L 7 2 4F RT A16WE 2007032800072 20070328 00072 EU 2007 3 28 USAA070250 1 20070327 A 5320 FITTING AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 173US 1481 FR 66 AT Y1732 HAS CORROSION. INSTALLED FILLER/DOUBLER PER SRM 53-41-14; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1 SQ INCH. 2 L 7 2 4F RT A28NM 2007032800073 20070328 00073 NM 2007 3 28 USAA070244 1 20070327 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 STA 727F - 767 RT SIDE OF CARGO COMPARTMENT HAS CORROSION. INSTALLED FAB'D REPAIR PARTS PER SRM 53-60-53; CORR TASK C53 -107-02; LEVEL 2, DEFECT SIZE: 40 INCH AREA. 2 L 7 2 4F RT A16WE 2007032800075 20070328 00075 NM 2007 3 28 USAA070245 1 20070327 A 5330 DOUBLER BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 SKIN DOUBLER, STA 787-807 BETWEEN 27L AND 27R HAS CORROSION. INSTALLED FAB'D REPAIR DOUBLER PER SRM 51-40-02; CORR TASK C53-208-01; LEVEL 2, DEFECT SIZE: 20 X 20 INCH AREA. 2 L 7 2 4F RT A16WE 2007032800076 20070328 00076 EA 2007 3 28 TRAX200700396 1 20070319 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 901EV 7616 SECOND FROM AFT CEILING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007032800077 20070328 00077 NE 2007 3 28 TRAX200700397 2 20070319 A 7250 TURBINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 837AS 7271 CRACK FOUND ON NR 2 ENGINE LPT AT 9 O'CLOCK POSITION MEASURING 0.300 INCH MARKED PER SB CF34-3B1-72-A022 01. 2 L 7 2 4F 4 F RT A21EA E15NE 2007032800078 20070328 00078 EA 2007 3 28 TRAX200700398 1 20070319 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 935EV 8037 CLIP CRACKED UNER CARGO DOOR THRESHOLD AT FS 589.00. [SUP 05-09-07] INSTALLED 4EA LOCK FASTENERS THROUGH FS 589.00 FRA ME AND CLIP. PRESSURIZATION CHECK GOOD IAW CRJ MM 21-31-00. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2007032800081 20070328 00081 NM 2007 3 28 SWAA071516 1 20070322 A 3350 101073 LENS BOEING 737 737301 1384611 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED BRDG CHECK, FOUND AFT CABIN EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED SIGN LENS PER MM. 2 L 7 2 4F RT A16WE 2007032800082 20070328 00082 NM 2007 3 28 SWAA071523 1 20070322 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 MID CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007032800083 20070328 00083 NE 2007 3 28 HNAA0700047 3 20070311 A 6197 CONNECTOR DHAV DHC8 DHC8102 2809003 NM HAMSTD 14SF 14SF7 NE TORQUE MOTOR DISCONNECTED A HNAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 07 808EX 299 NR 2 PROP FLUXES PLUS OR MINUS 10 RPM DURING CLIMB WITH TORQUE FOLLOWING. FOUND CONNECTOR NOT CONNECTED TO TORQUE MOTOR ON NR 1 ENGINE. 2 H 7 2 4T RT A13NM 6 C P7NE 2007032800084 20070328 00084 NM 2007 3 28 UPS07649543 1 20070323 A 2910 PRESSURE SWITCH BOEING 767 76734AF 1385212 NM HYD SYSTEM MALFUNCTIONED A IPXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 302UP 27240 LOST CENTER HYDRAULIC PRESSURE WHILE ENROUTE. FLIGHT CREW FOLLOWED AOM CHECKLIST AND CONTINUED TO OAK. DECLARED EMERGENC Y. A/C TAXIED TO GATE UNDER OWN POWER. ACCOMPLISHED OPERATIONAL TEST OF CENTER HYDRAULIC SYSTEM PER B767 MM 29-11-00-5. NO FAULTS NOTED. CHANGED CENTER SYSTEM AND ADP PRESSURE SWITCHES PER B767 MM 29-31-01-4. EICAS MSG CLEARED. 2 L 7 2 4F RT A1NM 2007032800085 20070328 00085 NM 2007 3 28 HNAA0700056 1 20070315 A 2540 ANGLE DHAV DHC8 DHC8102 2809003 NM AFT LAVATORY CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 824EX 27985 27985 389 LAVATORY LOWER AFT FLOOR STRUCTURE ANGLE FOUND CORRODED. REPLACED ANGLE. 2 H 7 2 4T RT A13NM 2007032800090 20070328 00090 NM 2007 3 28 HNAA0700055 1 20070323 A 2910 82970009325 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM HYDRAULIC SYS BROKEN A HNAA K NONE K J FLUID LOSS WARNING INDICATION DE DESCENT 1 EA 07 943 46161 46161 167 ON DESCENT NR 2 ENGINE HYDRAULIC PUMP CAUTION LIGHT CAME ON WITH ISOLATION VALVE CAUTION LIGHT ASSOCIATED WITH NR 2 HYDR AULIC QUANTITY READING ZERO. FLIGHT TIME TO GATE APPROX 5 MINS. FOUND ENGINE DRIVEN PRESSURE LINE INTO PRESSURE MANIFO LD BROKEN OFF. REPLACED LINE. 2 H 7 2 4T RT A13NM 2007032800091 20070328 00091 SO 2007 3 28 RAIA00703055 1 20070321 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 815HK 145048 PRE FLT NR 5573 - STL - AISLE FLOOD LIGHT EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED EMERGENCY LIGHT CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007032800092 20070328 00092 SO 2007 3 28 RAIA00703050 1 20070320 A 2560 GLOWSTRIP EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 832HK 145771 POST FLT NR 7950 - IAD - PHOTO ILLUMINESCENT STRIP CAME LOOSE AROUND ROW 10. MAINTENANCE SECURED STRIP, CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007032800094 20070328 00094 SO 2007 3 28 RAIA00703061 1 20070322 A 2150 A/C PACK EMB 145 EMB145LR 3260212 SO NR 2 OVERHEATED A RAIA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 CE 03 842HK 14500830 FLT NR 7876 - TYS - PACK 2 OVERHEAT. MAINTENANCE DEFERRED NR 2 PACK SYSTEM. 2 L 7 2 4T RT T00011AT 2007032800095 20070328 00095 GL 2007 3 28 RAIA00703060 2 20070321 A 7200 AE3007A11 ENGINE EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL LEFT SHUTDOWN A RAIA C ABORTED TAKEOFF R Y PARTIAL RPM/PWR LOSS ENGINE STOPPAGE TO TAKEOFF 1 CE 03 805HK 14549 6911 145096 FLT NR 3552 - PIT - LEFT ENGINE STALL AND UNCOMMAND SHUT DOWN ON TAKEOFF ROLL. MAINTENANCE REMOVED AND REPLACED NR 1 EN GINE, OPS AND LEAK CHECKS GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007032800099 20070328 00099 SO 2007 3 28 RAIA00703057 1 20070321 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 830HK 145313 PRE FLT NR 5559 - STL - EMERGENCY LIGHTS FLOOR PROXIMITY LIGHT IS INOP. MAINTENANCE PERFORMED OPS CHECK, NO DISCREPANCY FOUND. 2 L 7 2 4T RT T00011AT 2007032800102 20070328 00102 SO 2007 3 28 RAIA00703049 1 20070320 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 810HK 145231 PRE FLT NR 3542 - STL - AISLE FLOOD LIGHT, FLOOR STRIP EMERGENCY LIGHT INOP. MAINTENANCE OPS CHECK, REMOVED AND REPLACE D LAMP, CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007032800104 20070328 00104 NM 2007 3 28 ABXA070085 1 20070327 A 5220 HANDLE BOEING 767 767232 1385132 NM EMERGENCY EXIT MISSING A ABXA K NONE O OTHER UK UNKNOWN 1 GL 23 745AX 22222 EMERGENCY EGRESS HANDLE WAS MISSING FROM THE L2 WINDOW. INSTALLED EMERGENCY EGRESS HANDLE AS REQUIRED IAW B767 AMM 56-1 1-04. CHECKED GOOD. 2 L 7 2 4F RT A1NM 2007032800108 20070328 00108 NM 2007 3 28 BB07027 1 20070322 A 3397 GROUND WIRE BOEING 767 7672B7 1385107 NM CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 252AU 24765 MAINTENANCE FOUND EMERGENCY LIGHTS INOPERATIVE AT ROW 1R. RECONNECTED GROUND WIRE. NO FURTHER FAULTS. 2 L 7 2 4F RT A1NM 2007032800109 20070328 00109 NM 2007 3 28 SWAA071559 1 20070323 A 3350 079123 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 430WN 33659 DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS CRACKED AT ROW 11. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007032800110 20070328 00110 NM 2007 3 28 SWAA071552 1 20070323 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 AFT OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007032800111 20070328 00111 2007 3 28 SWAA071550 4 20070323 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR UNWANTED DEPLOY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 786SW 29811 L1 DOOR EVACUATION SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2007032800112 20070328 00112 NM 2007 3 28 SWAA071551 1 20070324 A 5330 6545768 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 FUSELAGE SKIN CRACKED AT BS 450, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007032800114 20070328 00114 NM 2007 3 28 SWAA071548 1 20070323 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING MV2 CK, FOUND FUSELAGE SKIN CRACKED AT BS 415, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007032800117 20070328 00117 NM 2007 3 28 SWAA071556 1 20070321 A 5322 6546551 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 27L & 27R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007032800118 20070328 00118 NM 2007 3 28 SWAA071558 1 20070323 A 5534 6546872 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND RT VERTICAL STAB FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA. 2 L 7 2 4F RT A16WE 2007032800119 20070328 00119 NM 2007 3 28 SWAA071557 1 20070323 A 5534 6547450 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND LT VERTICAL STAB FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA. 2 L 7 2 4F RT A16WE 2007032800120 20070328 00120 NM 2007 3 28 07FDEA00847 1 20070314 A 5330 SKIN BOEING 727 727225 1384077 NM BS 950D-950E CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 461FE 22548 AFT BAG BIN FUSE SKIN CORRODED ADJACENT TO STR 29L BETWEEN FS 950D TO 950E. CUT OUT DAMAGE, FABRICATED REPAIR PLATE AND FILLER FROM MAT 2024-T3. TREATED AND PRIMED IAW SRM 51-10-2 AND INSTALLED REPAIR IAW SRM 53-30-3, FIG 3. MAJOR REPAIR . 2 L 7 3 4F A3WE 2007032800121 20070328 00121 NM 2007 3 28 SWAA071554 1 20070323 A 5313 6551698 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER FITTING CRACKED AT BS 727, STR 24L. REMOVED AND REPLACED STR FITTING PER SRM . 2 L 7 2 4F RT A16WE 2007032800123 20070328 00123 NM 2007 3 28 07FDEA00848 1 20070314 A 5330 SKIN BOEING 727 727225 1384077 NM BS 1087-1096 MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 461FE 22548 EXTERNAL DOUBLER LOCATED AT STA 1087- 1096, STR 22R - 23R, DOES NOT COMPLY WITH FAA APPROVED DATA. REMOVED EXISTING R EPAIR, FABRICATED NEW REPAIR DOUBLER AND FILLER FROM MAT 2024-T3, .071. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3, FIG 1. MAJOR REPAIR. 2 L 7 3 4F A3WE 2007032800124 20070328 00124 NM 2007 3 28 07FDEA00849 1 20070314 A 3230 BOLT BOEING 727 727227 1384078 NM MLG LOOSE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 489FE 21492 AFTER T/O LANDING GEAR FAILED TO RETRACT RAN THE "LANDING GEAR LEVER LATCH FAILED TO RELEASE" CHECKLIST TEST NR 1 FAIL, TEST 2&3 PASSED. RETURN TO MEMPHIS NORMAL LANDING. FOUND LEFT MAIN GEAR SAFETY SENSOR ACTUATOR CENTER PIVOT BOLT LOOSE AND NUT BACKED OFF TO LAST THREAD CAUSING EXCESSIVE GAP TO SENSORS. REPLACED NUT AND IAW B727-200 AMM 32-09-221-4. GA P NOW WITHIN LIMITS. SWUNG GEAR IAW B727-200 AMM 32-61-001-5, ALL CHECKS GOOD. 2 L 7 3 4F A3WE 2007032800126 20070328 00126 EU 2007 3 28 07FDEA00850 1 20070315 A 5344 A52834027003 HINGE AIRBUS 310 A310304 3930339 EU ZONE 800 MISINSTALLED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 816FD 593 RT MLG FITTING BUSH, WRONG INSTALLATION. REPAIR WAS PERFORMED IAW EA 6-5281-106381 AND RAS/CASA/5328/2007 ISSUE "A" AND RAS/AS/228/95 ISSUE "A". 2 L 7 2 4F RT A35EU 2007032800127 20070328 00127 EU 2007 3 28 07FDEA00851 1 20070315 A 5730 SKIN AIRBUS 310 A310304 3930339 EU WING DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 ELONGATED HOLES IN LT BOTTOM WING SKIN AT PYLON SUPPORT BRACKET. REPAIR WAS PERFORMED IAW EA 6-5720-106422, DRAWING R57 2-49184 AND RAS/BAE/1004144/2007 ISSUE "A". 2 L 7 2 4F RT A35EU 2007032800129 20070328 00129 EU 2007 3 28 07FDEA00852 1 20070315 A 5730 SKIN AIRBUS 300 A300B4622R 3930312 EU LT WING CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 LT WING TIP, CORROSION UNDER ONE STATIC DISCHARGER AND CRACK ON NAVIGATION LIGHT BRACKET. REPAIR WAS PERFORMED IAW EA 6 -5730-106400 AND RAS/FOK/004/2007 ISSUE "A". 2 L 7 2 4F RT A35EU 2007032800130 20070328 00130 EA 2007 3 28 TRAX200700414 1 20070315 A 5320 SILL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 RIGHT FLOOR SILL PLATE CORRODED AT FS 280.0. 2 L 7 2 4F RT A21EA 2007032800153 20070328 00153 EA 2007 3 28 TRAX200700415 1 20070320 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 683BR 7692 ASD DOOR HANDLE CRACKED. 2 L 7 2 4F RT A21EA 2007032800155 20070328 00155 EA 2007 3 28 TRAX200700417 1 20070320 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 759EV 10211 EMERGENCY LIGHT STRIP SECTION NOT WORKING. 2 L 7 2 4F RT A21EA 2007032800156 20070328 00156 2007 3 28 TRAX200700418 4 20070320 A 3425 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A ASOA K NONE J WARNING INDICATION CR CRUISE 1 SO 27 906EV 7642 EFIS COMP MON CAUTION MSG APPEARS REPEATEDLY THROUGHOUT FLT, ALL PHASES (REPEAT). TOWER DECLARED EMERGENCY. FLT 4517 D EL 65 MINS. 2 L 7 2 4F RT A21EA 2007032800157 20070328 00157 EA 2007 3 28 TRAX200700419 1 20070321 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 684BR 7708 RIGHT FWD EMERGENCY LIGHT OUT. 2 L 7 2 4F RT A21EA 2007032800158 20070328 00158 EA 2007 3 28 TRAX200700420 1 20070322 A 5313 STRINGER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 FLOOR SUPPORT STRINGER AT PAX DOOR OPENING STA 310 TO 349 LEFT CORRODED. REMOVED CENTER TITANIUM FLOOR SUPPORT ANGLE, D OOR PROX SWITCH SENSOR, FWD AND AFT HANDRAIL FITTINGS & BONDING WIRE CONNECTIONS, & BLENDED CORROSION OUT OF LIMITS OF C RJ 200 SRM 53-00-00 ON FLOOR SUPPORT STRINGER. FLOOR SUPPORT STRINGER REQUIRES REMOVE & REPLACE. FINISHED REMOVING FLOO R SUPPORT STRINGER, LOCATED HOLES & DRILLED NEW STRINGER, STARTED INSTALLING TOP FLOOR SUPPORT, IAW SRM 51-40-11/ 51-42- 06. INSTALLED BONDING WIRES AND PROX SWITCH OPS CK GOOD IAW CRJ 200 AMM 52-70-00 AND WDM 20-00-00 2 L 7 2 4F RT A21EA 2007032800159 20070328 00159 EA 2007 3 28 TRAX200700422 1 20070322 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 713EV 10081 F/O`S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007032800163 20070328 00163 NM 2007 3 28 SWAA071432 1 20070318 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 378, STR 26L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007032800165 20070328 00165 NM 2007 3 28 SWAA071451 1 20070320 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007032800166 20070328 00166 NM 2007 3 28 SWAA071454 1 20070320 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER 15R CRACKED AT BS 489. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007032800167 20070328 00167 NM 2007 3 28 SWAA071431 1 20070318 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007032800168 20070328 00168 NM 2007 3 28 SWAA071456 1 20070320 A 2560 PH22300L GLOWSTRIP BOEING 737 737301 1384611 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED BRDG CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 13 ABC. REMOVED AND REPLACED EEPLS STRIP PE R MM. 2 L 7 2 4F RT A16WE 2007032800169 20070328 00169 NM 2007 3 28 SWAA071455 1 20070320 A 2560 PH22300L GLOWSTRIP BOEING 737 737301 1384611 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED BRDG CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 16 DEF. REMOVED AND REPLACED EEPLS STRIP PE R MM. 2 L 7 2 4F RT A16WE 2007032800171 20070328 00171 2007 3 28 SWAA071340 4 20070312 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVACUATION SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2007032800173 20070328 00173 2007 3 28 SWAA071338 4 20070311 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 L1 DOOR EVACUATION SLIDE LOOSE. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2007032800174 20070328 00174 2007 3 28 SWAA071346 4 20070313 A 2312 G6076 CONTROL PANEL BOEING 737 7373H4 1384600 NM NR 2 VHF COMM MALFUNCTIONED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 29 654SW 28399 SMALL AMOUNT OF VISIBLE SMOKE FROM CENTER CONSOLE NR 2 VHF NAV COMM RECEIVER. REMOVED AND REPLACED NR 2 VHF NAV COMM PA NEL PER MM. 2 L 7 2 4F RT A16WE 2007032800184 20070328 00184 NM 2007 3 28 WRLA2007041 1 20070309 A 5730 SKIN DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE LT WING CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271WA 48518 DURING C-04 CHECK FOUND CRACK LT WING FIXED LEADING EDGE ACCESS DOOR CUTOUT BOTH UPPER SIDE XOS:464 TO XOS:470, NR 3 SLA T. PERFORM REPAIR PER MD-11 SRM 57-10-00 FIG 42 VOL 1 REV 38 TR 57-8 2 L 7 3 4F 4 F RT A22WE E24NE 2007032800185 20070328 00185 NM 2007 3 28 SWAA071374 1 20070314 A 3350 071702001 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 247WN 32508 PAX CABIN EMERGENCY EXIT LIGHT C/B TRIPPED. REMOVED AND REPLACED RIGHT AFT EMERGENCY EXIT LIGHT BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007032800186 20070328 00186 NM 2007 3 28 SWAA071373 1 20070314 A 3350 6104781 BATTERY PACK BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED SERVICE CHECK, FOUND RIGHT CEILING MID CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY P ACK PER MM. 2 L 7 2 4F RT A16WE 2007032800188 20070328 00188 NM 2007 3 28 SWAA071366 1 20070313 A 5753 6546486128 FLAP BOEING 737 7375H4 138449D NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED C1 CHECK, FOUND LEFT WING INBOARD MIDFLAP DELAMINATED AT INBOARD EDGE. REMOVED AND REPLACED LEFT WING INBOARD MIDFLAP PER MM. 2 L 7 2 4F RT A16WE 2007032800189 20070328 00189 NM 2007 3 28 SWAA071369 1 20070313 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED BRDG CHECK, FOUND STR FUSELAGE FRAME CRACKED AT BS 380, STR 15R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007032800190 20070328 00190 NM 2007 3 28 SWAA071359 1 20070313 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, BETWEEN STR 13R & STR 14R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007032800191 20070328 00191 NM 2007 3 28 SWAA071364 1 20070313 A 5315 6546804 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 996, LBL 65 TO RBL 65. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2007032800193 20070328 00193 NM 2007 3 28 SWAA071362 1 20070313 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE CREASE BEAM CORRODED AT BS 996 LEFT SIDE. REPAIRED CREASE BEAM SECTION PER S RM. 2 L 7 2 4F RT A16WE 2007032800198 20070328 00198 NM 2007 3 28 UPS07549522 1 20070316 A 3350 LIGHT BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 442UP 27387 INSPECTION TYPE:N/A 1 BULB INOP IN EMERGENCY LIGHTS ARMED/DISARMED ANNUN LIGHT. RELAMPED, OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2007032800201 20070328 00201 NM 2007 3 28 2007UALA00656 1 20070303 A 2997 BACC63BN105SN CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE HYDRAULIC SYS FAULTY A UALA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 WP 29 175UA 24382 RTFL UNDER AMBER ALERT DUE TO HYDRAULIC OVERHEAT MESSAGE. REPLACED TEMPERATURE TRANSMITTER FOR ENG NR 1 HYD SYSTEM PER A MM 29-32-02. NO LEAKS. AFTER REPLACEMENT INDICATION IS BLANK. SUSPECT CONNECTOR. REPLACED CONNECTOR. SYSTEM TEST OK. SUSPECT VIBRATION CAUSE INTERNAL CONNECTOR WEAR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032800203 20070328 00203 WP 2007 3 28 07FDEA00857 1 20070315 A 5730 SKIN DOUG DC10 DC1030F 3023504 WP LT WING LE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 FOUND LT WING L/E FOUND CORROSION WITH EXF ON SKIN FIXED PANEL AT STA XOS 910-930. REPAIRED SACRIFICIAL DOUBLER IAW SRM 57-10-00 FIG 19D SHT 1 VOL 1. TOUCHED UP IAW SRM 51-21-01 VOL 2 PAG 21-25 AND SRM 51-21-02 VOL 2. FABRICATED PARTS IA W DETAIL PARTS TRAVELER I030694-1 SACRIFICIAL DOUBLER, I030694-3 ( 2EA ) INTERNAL REPAIR STRAP 3, I030694-4 (2EA) INTERN AL STRAP 4, I030694-2 ( 2EA ) INTERNAL REPAIR STRAP 2, I030694-1B (2EA) IAW SRM 57-10-00 FIG 19 VOL 1. 2 L 7 3 4F RT A22WE 2007032800204 20070328 00204 WP 2007 3 28 07FDEA00858 1 20070315 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 1801-1821 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 LWR FUSELAGE EXT ZONA FOUND DEEP DENT ON SKIN DIMENSION: 2" BY 1.25" DEEP 0.09" BTWN STA 1801 AND STA 1821 FROM LONG NR 42 TO LONG NR 43 RT SIDE. REMOVED EXTERNAL DOUBLER AND INTERNAL FINGER DOUBLERS IAW SRM 53-20-00 FIG 6 VOL 1. REPAIRE D IAW SRM 53-20-00 FIG 6 VOL 1 SHT 3. PAINTED AREA IAW SRM 51-21-01 VOL 2. 2 L 7 3 4F A22WE 2007032800205 20070328 00205 EU 2007 3 28 2007UALA00796 1 20070318 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GALLEY SMOKE A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 408UA 457 FLIGHT CREW REPORTING SMOKE IN AFT GALLEY IN OVEN AREA. [SUP 06-01-07] REMOVED BOTH OVENS, CEILING PANELS AND CIRCUIT BREAKER PANEL AND FOUND NO EVIDENCE OF FIRE. OPERATED OVENS, HOT PLATES AND CHILLERS FOR 4.5 HOURS ON GROUND AND DID NOT NOTICE ANY SMOKE OR BURNING ODOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032800206 20070328 00206 WP 2007 3 28 07FDEA00859 1 20070315 A 5540 RUDDER DOUG DC10 DC1030F 3023504 WP TAIL DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 DURING AUTOPILOT TEST DAMAGED LOWER RUDDER AFT T/E. REPAIRED T/E SECTION IAW SRM 55-30-00 VOL 1 FIG 2. FABRICATED PART S IAW DETAIL PARTS TRAVELER I031562/N01562 AND IAW SRM 55-30-00 VOL 1 FIG 2. 2 L 7 3 4F RT A22WE 2007032800207 20070328 00207 EU 2007 3 28 07FDEA00860 1 20070315 A 5730 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 CHAFED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 CHAFING MARKS TO LEADING EDGE 'D' NOSE SKIN, BOTH WINGS. LT WING BETWEEN TRACK 5 AND TRACK 6, LT WING BETWEEN TRACK 9 A ND TRACK 10, RT WING BETWEEN TRACK 5 AND TRACK 6 AND RT WING AREA OF TRACK 1. REPAIR WAS PERFORMED IAW EA 6-5741-103419 AND RAS/BAE/1003686/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007032800208 20070328 00208 EU 2007 3 28 07FDEA00861 1 20070315 A 5754 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 CHAFED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 CHAFING MARKS TO LEADING EDGE 'D' NOSE SKIN, BOTH WINGS. LT WING BETWEEN TRACK 5 AND TRACK 6, LT WING BETWEEN TRACK 9 A ND TRACK 10, RT WING BETWEEN TRACK 5 AND TRACK 6 AND RT WING AREA OF TRACK 1. REPAIR WAS PERFORMED BY BLENDING AND REPL ACMENT IAW EA 6-5741-103419 AND RAS/BAE/1003686/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007032800209 20070328 00209 EU 2007 3 28 07FDEA00862 1 20070315 A 5751 A57242795200 SKIN AIRBUS 310 A310324 3930206 EU ZONE 500 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 CRACKS AT 2 FASTENER HOLES AT AILERON HINGE RIB BOTTOM SKIN, LT WING. REPAIR WAS PERFORMED IAW EA 6-5720-103409 AND RAS /BAE/1003670/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007032800212 20070328 00212 2007 3 28 2007UALA00801 4 20070317 A 2565 SLIDE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 918UA 25385 DOOR 1L SLIDE FELL OUT WHEN DOOR WAS OPENED. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032800215 20070328 00215 NM 2007 3 28 2007UALA00803 1 20070319 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 20UAÊ 29166 DOOR 5 CREW REST ROOM EMERGENCY LIGHT NOT ON (STAIRWAY AREA). REPLACED WITH SERVICABLE EMERGENCY LIGHT ASSY AND THEN OP CHECKED ON GROUND. SYSTEM OP CHECKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032800219 20070328 00219 NM 2007 3 28 QXEA200700375 1 20070314 A 2420 115221884 GENERATOR BOMBDR DHC8 DHC8402 1390042 NM NR 1 INOPERATIVE A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 400QX 10476 1076 4030 SEA FLIGHT NR 2348: NR 1 AC GEN, AFTER START, COULD NOT RESET. MAINTENANCE REMOVED AND REPLACED NR 1 AC GEN IAW MTC 624 2101. OPS CHECK GOOD. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032800220 20070328 00220 NM 2007 3 28 QXEA200700452 1 20070324 A 3620 8209074 SWITCH BOMBDR DHC8 DHC8402 1390042 NM BLEED TEMP MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 409QX 5746 5746 4051 SEA FLIGHT NR 2392: NR 2 BLEED HOT CAUTION ILLUMINATED ON TAXI OUT. MAINTENANCE REMOVED AND REPLACED THE RIGHT BLEED OV ER TEMP SWITCH IAW AMM TASK 36-11-16-000-801 AND 36-11-16-400-801. RBLD TMP SW FAULT CLEARED. CAUTION LIGHT CLEARED. BLEED AIR SYSTEM OPS CHECK GOOD IAW AMM TASK 36-11-00-710-802. 2 H 7 2 4T RT A13NM 2007032800221 20070328 00221 NM 2007 3 28 QXEA200700453 1 20070325 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM MAIN PAX UNKNOWN A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 413QX 4060 SMF FLIGHT NR 2430: FLIGHT ATTENDANT REPORTS THAT THE AFT PASSENGER DOOR IS DIFFICULT TO OPEN. MAINTENANCE CLEANED AND INSPECTED SEAL. NO DEFECTS NOTED. C/W Q400 AMM TASK 52-12-00-710-802. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032800222 20070328 00222 NM 2007 3 28 QXEA200700454 1 20070325 A 3097 697071272 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM PROP DEICE DAMAGED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 405QX 4047 SEA FLIGHT NR 2495: PROP DEICE CAUTION ILLUMINATED IN THE CLIMB. RAN THE CHECKLIST. LIGHT BACK ON AFTER RESET (ILLUMIN ATED WHEN NR 1 PROP ENERGIZED). AIRCRAFT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED NR 1 PROP NR 6 BLADE DEIC E WIRING HARNESS IAW AMM TASK 61-10-06-000-805 AND 61-10-06-400-805. FUNCTIONAL TEST OF THE PROP DEICE SYSTEM CHECKS GO OD IAW AMM TASK 30-61-00-720-801. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032800224 20070328 00224 NM 2007 3 28 QXEA200700424 1 20070314 A 5310 DOOR FRAME DHAV DHC8 DHC8202 2809007 NM EMERGENCY EXIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - ANGLE CONNECTING FORWARD RIGHT EMERGENCY DOOR FRAME BY 240.5 TO GALLEY MOUNT ANGLE HAS CORROSION AROUND NUTPLAT E LOWER SIDE OF ANGLE. REPAIRED IAW SRM 51-20-11, RD8-53-9512. 2 H 7 2 4T RT A13NM 2007032600166 20070326 00166 2007 3 26 BA07002 4 20070322 A 3441 46502003030316 ADIRU AIRBUS 330 A330323 3930335 EU NR 1 FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 273AY 23876 0337 FLIGHT 1592, CLT-FRA: CREW RECEIVED ADIRU 1 FAULT. DIVERTED TO PHL. MAINTENANCE REPLACED ADIRU 1. NO FURTHER FAULTS. 2 L 7 2 4F RT A46NM 2007032600171 20070326 00171 NM 2007 3 26 F3LA200700043 1 20070309 A 5321 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 919FR 4679 1980 DURING C-3 CHECK, INSPECTION REPORTED FWD CARGO PIT FLOOR COVER SHEET CORRODED AROUND SEVERAL HOLES, AFT COVER SHEET NR 131CG. FOUND CORROSION IN FWD PIT AT Y692 TRANSITION SUPPORT PLATE RUNNING FROM FR 28 TO FR 34 AT THE FASTENER HOLES. FABRICATED AND INSTALLED TRANSITION PLATE AND COVER SHEET IAW A319 SRM 51-42-11. 2 L 7 2 4F RT A28NM 2007032700018 20070327 00018 NM 2007 3 27 DL76G070208 1 20070313 A 4920 380029817 ENGINE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE APU MALFUNCTIONED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 16065 38335 30199 P265C DUE TO HOC REPLACE APU. REMOVED AND REPLACED APU PER MM, OPS CKS OK. 2 L 7 2 4F 4 F RT A1NM E13NE 2007032700021 20070327 00021 NM 2007 3 27 AWXA200700382 1 20070225 A 5320 INTERCOSTAL BOEING 737 7373S3 1384711 NM ZONE 100 BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - INTERCOSTAL ATTACH ANGLE HAS PIECE BUSTED OUT, BS 500D + 4", BL 0, WL 207. REPLACED INTERCOSTAL ATTACH ANGLE, BS 500D + 4", BL 0, WL 207 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007032700032 20070327 00032 NM 2007 3 27 AWXA200700393 1 20070312 A 5320 65566542 WEB BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - FOUND AFT CARGO COMPARTMENT DOOR CUT OUT WEB CRACKED, BS 847, RBL 36, WL 150. REPAIRED AFT CARGO COMPARTMENT DOOR CUT OUT WEB, BS 847, RBL 36, WL 150 IAW B737-300 SRM 51-70-02. 2 L 7 2 4F RT A16WE 2007032700048 20070327 00048 SO 2007 3 27 CHQA200700008 1 20070321 A 3411 CS500060D4A RELAY EMB 145 EMB145LR 3260212 SO PITOT STATIC BURNED A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 562RP 145451 FLIGHT 6248 - STL-CVG - EN ROUTE AT 27,000 FEET, RECEIVED PITOT 2 FAIL MESSAGE. RAN QRH AND STARTED SMELLING AN ODOR. CABIN WAS HAZY. RAN MEMORY ITEMS FOR SMOKE AND FIRE COCKPIT AND QRH. DECLARED EMERGENCY, DIVERTED TO EVV. MAINTENANCE REPLACED RELAYS K0494 (PN CS500-060-D4A), K0054 (PN CS500-060-D4A), AND K0055 (PN MS27743-18) AND ASSOCIATED RELAY SOCK ETS IAW EMB MM 20-13-02. OPS CHECK GOOD IAW MM 30-31-00. 2 L 7 2 4T RT T00011AT 2007032700053 20070327 00053 EA 2007 3 27 SWIA200718050 1 20070223 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 864AS 7502 PAX DOOR EXTERNAL HANDLE IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED PAX DOOR EXTERNAL HANDLE P/N 601R31 763-1 IAW CRJ200 SRM 51-42-21 PG 1-21. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007032700055 20070327 00055 EA 2007 3 27 SWIA200718052 1 20070223 A 7160 NOSE COWL CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 864AS 7502 RT ENGINE NOSE COWL HAS A CRACKED BRACKET AT 4 O'CLOCK POSITION AND XN122.72, DISCOVERED DURING C-CHECK INSPECTION. INS TALLED NEW BRACKET RT ENGINE NOSE COWL AT 4 O'CLOCK POSITION PER ENGINEERING ORDER 601R-71-11031. 2 L 7 2 4F RT A21EA 2007032700060 20070327 00060 NM 2007 3 27 HALA0700103 1 20070315 A 5330 DOUBLER BOEING 717 717200 1383700 NM FUSELAGE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 481HA 55126 DURING LIGHTNING STRIKE INSPECTION FOUND UPPER TCAS ANTENNA DOUBLER SEVERELY CORRODED PN 5962773-1. REPAIRED PER HAL M1 05 FILE NR 481094. 2 L 7 2 4F TR A6WE 2007032700062 20070327 00062 SO 2007 3 27 SIMA200707409 1 20070312 A 5347 14530659001 SEAT TRACK EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 15742 4800 145234 CORROSION ON LEFT LOWER CABIN SEAT TRACK BETWEEN FRAME 24 TO 30. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 A ND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032700063 20070327 00063 SO 2007 3 27 SIMA200707415 1 20070312 A 5347 14532606009 SEAT TRACK EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 15742 4800 145234 CORROSION ON LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 53 TO 58. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RE TURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032700095 20070327 00095 NM 2007 3 27 AALA20070474 1 20070311 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 777AN 29585 DFW - EMERGENCY SEAT MOUNTED LIGHT AT SEAT 26C IS MISSING LENS. REPLACED LENS FOR EMERGENCY SEAT MOUNTED LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032700096 20070327 00096 NM 2007 3 27 AALA20070475 1 20070311 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 627AA 24585 MIA - EMERGENCY LIGHT UNARMED ANNUNCIATOR HAS ONE BULB INOPERATIVE. RELAMPED EMERGENCY LIGHT UNARMED ANNUNCIATOR. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007032700114 20070327 00114 NM 2007 3 27 SWAA071538 1 20070322 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM BS 188 S17R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007032700115 20070327 00115 NM 2007 3 27 SWAA071536 1 20070322 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM BS 188 S17R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007032700122 20070327 00122 NM 2007 3 27 SWAA071532 1 20070322 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM BS 505D S28R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 18Y CHECK, FOUND RIGHT KEEL BEAM CORRODED AT BS 505D, STR 28R. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2007032700123 20070327 00123 NM 2007 3 27 SWAA071507 1 20070322 A 5753 6546430 SKIN BOEING 737 7373Y0 1384671 NM LT WING TE FLAP DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED 20Y CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DISBONDED AT LOWER INBOARD END. REPAIRED FLAP PER SRM . 2 L 7 2 4F RT A16WE 2007032700148 20070327 00148 NM 2007 3 27 SWAA071510 1 20070322 A 5523 65C26384 TAB BOEING 737 7373Y0 1384671 NM LT ELEVATOR DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED 20Y CHECK, FOUND LEFT ELEVATOR TAB SKIN CRACKED AT STA 94. REPAIRED TAB PER SRM. 2 L 7 2 4F RT A16WE 2007032700150 20070327 00150 NM 2007 3 27 SWAA071514 1 20070322 A 5754 65C26602 SKIN BOEING 737 7373H4 1384600 NM LT WING SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED C3 CHECK, FOUND LEFT WING NR 2 L/E SLAT CRACKED AT INBOARD ACTUATOR. REPAIRED SLAT PER SWA EA. 2 L 7 2 4F RT A16WE 2007032700154 20070327 00154 NM 2007 3 27 SWAA071517 1 20070322 A 5322 69353656 SHEAR TIE BOEING 737 7373Q8 1384670 NM BS 360 S28R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 360, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007032700164 20070327 00164 EU 2007 3 27 USAA070231 1 20070323 A 5315 D5347217220500 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 163US 1417 RIGHT FLOORBEAM TOP FLANGE FROM FR 64-69, -Y1160-Y1292 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM PER SRM 51-72-11; CORR TASK JA-260-53500, LEVEL 1, DEFECT SIZE: 1.5 SQ INCH. 2 L 7 2 4F RT A28NM 2007032700165 20070327 00165 2007 3 27 P5CA0701516 4 20070323 A 2397 8220987003 COUPLER BOEING 747 74746NF 13848BT NM HF SYSTEM FAILED A P5CA O OTHER G MULTIPLE FAILURE CR CRUISE 1 EA 15 450PA 30808 LEFT AND RIGHT HF TRANSMITTERS WENT INOPERATIVE. REPLACED LEFT AND RIGHT HF COUPLERS. OPERATIONAL CHECKS GOOD. 2 L 7 4 4F RT A20WE 2007032700168 20070327 00168 NM 2007 3 27 UPS07549536 1 20070222 A 5311 146N1015N1030 FRAME BOEING 757 75724APF 1384969 NM BS 1480 S26L DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 418UP 23905 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1480, BETWEEN S25L TO S26L. FRAME REPAIR AT STA 1480, S26L HAS B EEN ACCOMPLISHED PER EA 757-5362 -27-A1618 WITH -NO DEVIATIONS-, AND PER UPS EO B757-5310-26389-A. 2 L 7 2 4F RT A2NM 2007032700172 20070327 00172 WP 2007 3 27 UPS07849540 1 20070313 A 5330 FINGER DOUBLER DOUG DC8 DC873F 302199F WP FS960-980 RBL65 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C3 CENTER WING BOX SUBFLOOR FINGER DOUBLER CORRODED AT STA 960-980 RBL 65. REMOVED FINGER DOUBLER AT ST A 960-980 RBL 65 IAW SRM 51-1-21. FABRICATED AND INSTALLED FINGER DOUBLER AT STA 960-980 RBL 65 IAW SRM 53-7-3, AND SRM 53-07-03-0. 2 L 7 4 4F RT 4A25 2007032700175 20070327 00175 NM 2007 3 27 UPS07M49541 1 20070118 A 5730 ARB39546 PANEL DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C RIGHT L/E LWR COMPT FOUND CRACK AT UPPER DOUBLER PANEL AND STRAP AS MARKED APPROX STA XORS 562. OPEN UP FOR ACCESS, PER DEFECT STATED ABOVE AREA PER SRM 51-31-01 V2 R38. RIGHT WING L/E LWR, STA XORS 562 BEADED DOUBLER TR IMMED PER 57-10-00.F.25B TEMP R29. DOUBLER P/N ARB3954-6 FAB PER USING DWG ARB3594. REPAIR FILLER & DOUBLER & ANGLES P ER SRM F.25B & 57-10-00 TEMP R29. RIGHT WING L/E LWR STA XORS 562 DOUBLER & RIB INSTALLED PER SRM 51-31-01 V2 R38, SATI SFACTORY. 2 L 7 3 4F RT A22WE 2007032700182 20070327 00182 WP 2007 3 27 AALA20070451 1 20070307 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 279AA 49295 LGA - EMERGENCY LIGHTS AT SEAT ROWS 22 TO 26 INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 26 FOR EMERGENCY LIGHTS AT SEAT ROWS 22 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007032700188 20070327 00188 NM 2007 3 27 AALA20070452 1 20070307 A 3350 BEZEL BOEING 777 777223 1385213 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 788AN 30011 DFW - EMERGENCY LIGHT ADJACENT TO LEFT NUMBER THREE DOOR AT GALLEY BULKHEAD HAS BROKEN BEZEL. REPLACED EMERGENCY LIGHT AT L308 FOR BROKEN BEZEL AT GALLEY BULKHEAD ADJACENT TO LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032700200 20070327 00200 WP 2007 3 27 NWAA071069941 1 20070219 A 5754 SKIN DOUG DC9 DC932 3022066 WP LE FLAP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING "H" CHECK, FOUND CRACKS IN LT FLAP NOSE SKIN AT XFS 235 AND 252. REPAIRED PER EA 99-208467. 2 L 7 2 4F A6WE 2007032700203 20070327 00203 NM 2007 3 27 USAA070248 1 20070327 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 STA 727B-727D IN CARGO AREA HAS CORROSION. INSTALLED FAB'D REPAIR PART PER SRM 53-60-53; CORR TASK C53-107-02; LEVEL 2, DEFECT SIZE: 12 INCH AREA. 2 L 7 2 4F RT A16WE 2007032700204 20070327 00204 NM 2007 3 27 USAA070249 1 20070327 A 5320 SUPPORT ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 STA 304-330 RBL 55 WL 209 FWD SERVICE DOOR THRESHOLD HAS CORROSION. REPLACED THRESHOLD SUPPORT PER SRM 51-10-02; CORR T ASK C53-107-01; LEVEL 2, DEFECT SIZE: 1 X 20 INCHES. 2 L 7 2 4F RT A16WE 2007032700210 20070327 00210 WP 2007 3 27 ABXA070084 1 20070307 A 5330 591141611 DOUBLER DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 949AX 47325 DOUBLER ATTACHED TO FUSELAGE SKIN AT FUEL SHROUD WAS CORRODED, LONGERON 20 AREA. REMOVED AND INSTALLED NEW DOUBLER IAW DC9 SRM. 2 L 7 2 4F A6WE 2007032700215 20070327 00215 SO 2007 3 27 RAIA00703034 1 20070315 A 3350 78241 INVERTER EMB 145 EMB145 3260210 SO CABIN MALFUNCTIONED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 820HK 145064 PRE FLT NR 5485 - STL - EMERGENCY LIGHT OUT AT RIGHT HAND OVERWING EXIT MARKER. MAINTENANCE REMOVED AND REPLACED EMERGE NCY LIGHT INVERTER, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007032700216 20070327 00216 SO 2007 3 27 RAIA00703035 1 20070316 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 818HK 55 145059 PRE FLT NR 5491 - STL - EMERGENCY LIGHT OUT AT COCKPIT FLOODLIGHT. MAINTENANCE REMOVED AND REPLACED NR 1 BATTERY POWER SUPPLY, SYSTEM CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007032700220 20070327 00220 SO 2007 3 27 RAIA00703040 1 20070317 A 3020 C1460092 ANTI-ICE VALVE EMB 145 EMB145LR 3260212 SO NR 1 ENGINE MALFUNCTIONED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 813HK 21015 145044 FLT NR 5571 - STL - NR 1 ENGINE ANTI-ICE FAIL. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE ANTI-ICE VALVE, OPS CHECK G OOD. 2 L 7 2 4T RT T00011AT 2007032800007 20070328 00007 SO 2007 3 28 RAIA00703041 1 20070317 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN DIRTY A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 817HK 145058 PRE FLT NR 5555 - STL - EMERGENCY LIGHT INOP AT FWD SIDE AFT CEILING EXIT LOCATOR. MAINTENANCE CLEANED EMERGENCY LIGHT INVERTER CONNECTOR, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007032800022 20070328 00022 NM 2007 3 28 BB07029 1 20070322 A 5610 141T480150 WINDSHIELD BOEING 757 7572B7 1384964 NM COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 930UW 21101 27145 FLIGHT 888, LAS-FLL: IN CRUISE, 1R WINDOW DEVELOPED EXTENSIVE SPIDERWEB CRACKING. FLIGHT DIVERTED TO PHX. MAINTENANCE REPLACED THE WINDSHIELD ASSEMBLY AND THE HEAT CONTROLLER. 2 L 7 2 4F RT A2NM 2007032800023 20070328 00023 SO 2007 3 28 C2XA07IA072 1 20070324 A 3350 7287580501 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13968 145138 IAH FLIGHT 2305, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE LAST ROW OF AISLE PATH LIGHTING WAS INOPERATIV E. MAINTENANCE REMOVED AND REPLACED THE LAST SECTION OF AISLE PATH LIGHTING, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032800033 20070328 00033 NM 2007 3 28 KCSA071081 1 20070323 A 5320 WEB BOEING 747 747236B 1384804 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 AFT PIT STA 1800 RBL 10 WEB CREASED WL 116. 2 L 7 4 4F A20WE 2007032800039 20070328 00039 NE 2007 3 28 MAC030701 2 20070322 A 7323 8210161C GOVERNOR AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE NR 2 ENGINE INTERMITTENT A MTNA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 33 904FX 21001 6140 259 120474 NR 2 ENGINE SURGE DURING CLIMB. 2 H 7 2 4T 4 T RT A53EU E20NE 2007032800044 20070328 00044 NM 2007 3 28 CALA0700145 1 20070324 A 5311 654655418 BELTFRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 77303 23354 INSPECTION FOUND FRONT SIDE OF BELTFRAME CORRODED IN AFT CARGO COMPARTMENT AT STA 847 BETWEEN S27L AND S27R. A NEW FRAM E WAS INSTALLED IAW SRM 51-40-02 AND 51-10-02. 2 L 7 2 4F RT A16WE 2007032800046 20070328 00046 NM 2007 3 28 CALA0700147 1 20070325 A 5310 6520722U70 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 77303 23354 INSPECTION FOUND A .75 INCH CRACK IN FORWARD CARGO DOOR CUTOUT FORWARD FRAME LOWER STOP PAD AT STA 440, S24R. THE FRAME WAS REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007032800062 20070328 00062 NM 2007 3 28 USAA070243 1 20070327 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 STA 727F - 787 HAS CORROSION. REMOVED & INSTALLED FAB'D REPAIR PARTS PER SRM 53-50-53; CORR TASK C53-107-02; LEVEL 2, D EFECT SIZE: 70 INCHES. 2 L 7 2 4F RT A16WE 2007032800067 20070328 00067 NM 2007 3 28 USAA070239 1 20070327 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 STA 787 - 807 LEFT SIDE CARGO COMPARTMENT HAS CORROSION. INSTALLED FAB'D REPAIR PARTS PER SRM 51-40-02; CORR TASK C53-1 07-01; LEVEL 2, DEFECT SIZE: 40 INCHES. 2 L 7 2 4F RT A16WE 2007032800069 20070328 00069 EU 2007 3 28 EMB07001 1 20070320 A 7500 BLEED AIR SYS EMB ERJ190 ERJ190100IGW 3260408 EU NR 1 ENGINE LEAKING A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 944UW 339 19000058 FLIGHT 1212, DFW-PHL: DURING CLIMB, RECEIVED ENGINE 1 FIRE WARNING. SHUT DOWN NUMBER 1 ENGINE AND RETURNED TO FIELD. NO EVIDENCE OF FIRE NOTED. HEAT DAMAGE FROM BLEED LEAK TO ENGINE HARNESSES WAS NOTED. MAINTENANCE FERRIED TO PHL. REPLAC ED THE NUMBER ONE ENGINE. 2 L 7 2 4F RT A57NM 2007032800074 20070328 00074 CE 2007 3 28 DXTA200702043 1 20070322 A 3240 215672 BRAKE CESSNA 750 750 2076810 CE MLG LEAKING E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 945QS 140 140 7500029 SMOKE REPORTED COMING FROM RT MLG BY TOWER ON DEPARTURE AND GROUND CREW ON TAXI INTO RAMP.INSPECTED RT MAIN GEAR, BRAKE AND WHEEL ASSYS. NO VISUAL DEFECTS NOTED. REMOVED RT IB AND RT OB BRAKE ASSYS AND INSTALLED OVERHAULED IB AND OR BRAKE A SSYS. BLED BRAKE SYSTEM.TAXI AND LEAK CHECKS GOOD. ALL WORK DONE IAW. IAW. CHAPTER 32-42-01 OF THE 750 M.M. 2 L 7 2 4J RT T00007WI 2007032800080 20070328 00080 EA 2007 3 28 TRAX200700405 1 20070319 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 854AS 7382 LEFT AFT OVERWING EMERGENCY LIGHT IS INOP. 2 L 7 2 4F RT A21EA 2007032800098 20070328 00098 SO 2007 3 28 RAIA00703056 1 20070321 A 5610 163500111 WINDSHIELD EMB 145 EMB145LR 3260212 SO COCKPIT DELAMINATED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 837HK 9694 12 145255 FLT NR 8001 - STL - CAPT WINDSHIELD DELAMINATED IN FLIGHT ABOVE 10K FT AROUND HEATING ELEMENT. MAINTENANCE REMOVED AND REPLACED CAPTS WINDSHIELD, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007032800113 20070328 00113 NM 2007 3 28 SWAA071549 1 20070323 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING MV2 CK, FOUND FUSELAGE SKIN CRACKED AT BS 485, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007032800116 20070328 00116 NM 2007 3 28 SWAA071546 1 20070323 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 FUSELAGE SKIN CRACKED AT BS 475, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007032800131 20070328 00131 EU 2007 3 28 07FDEA00854 1 20070315 A 5712 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 FOLDING NOSE LT INTERNAL RIB CRACKED. REPAIR WAS PERFORMED IAW EA 6-5710-106358 AND SB A300-57-6067. 2 L 7 2 4F RT A35EU 2007032800132 20070328 00132 NM 2007 3 28 07FDEA01102 1 20070322 A 5210 659315567 DOOR BOEING 727 727227 1384078 NM MAIN PAX LEAKING A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 491FE 21529 APPEARED TO LOOSE PRESSURIZATION PASSING 12,000' LEVELED AT 14,000' CABIN AT 9500, DESCENDED TO 10,000 AND WAS UNABLE T O GET PRESSURE IN CABIN BELOW 8,000. HEARD LOUD AIR NOISE, CHECKED MAIN CABIN DOOR, FOUND AIR LEAKING AROUND DOOR. RET URNED TO MEM. ADJUSTED UPPER DOOR GUIDE ARM 1/2 TURN OUT IAW B727-200 AMM 52-411-001-5. REMOVED AND REPLACED THE TEFLO N RUB STRIP AND MID CENTERING GUIDE ADJUSTED UPPER DOOR GUIDE ARM ROD END, REF 727-200MM 52-11-001-5. REINSTALLED ESCAP E SLIDE. OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2007032800133 20070328 00133 EU 2007 3 28 07FDEA01105 1 20070323 A 5210 A53611511205 GUSSET AIRBUS 300 A300B4622R 3930312 EU PAX DOOR CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 FUSELAGE NOSE SECTION-CORROSION ON FWD PAX DOOR FRAME AREA, RT LOWER CORNER, GUSSET A536-11517-205 REPAIR PERFORMED BY R EPLACEMENT OF GUSSET AND REWORK IAW EA 6-5312-106395 AND RAS/AS/010/2007 ISS.B 2 L 7 2 4F RT A35EU 2007032800134 20070328 00134 SO 2007 3 28 SWIA200718012 1 20070119 A 5411 FRAME EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 221SW 120290 LEFT NACELLE FRAME CRACKED AT AFT OUTBOARD DOOR AFT HINGE ATTACH POINT FORWARD BOSS, DISCOVERED DURING C-CHECK INSPECTIO N. REPLACED LEFT NACELLE FRAME AFT DOOR FORWARD HINGE ATTACH POINT IAW SRM 120 51-10-02 PG 2 SEC 2B. 2 L 7 2 4T RT A31SO 2007032800135 20070328 00135 SO 2007 3 28 SWIA200718013 1 20070119 A 2572 RACK EMB 120 EMB120ER 3260203 SO E/E BAY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 221SW 120290 AVIONICS BAY; RIGHT RADIO RACK CRACKED MIDWAY, DISCOVERED DURING C-CHECK INSPECTION. NEW RACK INSTALLED IAW SRM 120 51- 10-02 PG 23 SEC 3A. 2 L 7 2 4T RT A31SO 2007032800136 20070328 00136 SO 2007 3 28 SWIA200718014 1 20070119 A 5712 PRESSURE PANEL EMB 120 EMB120ER 3260203 SO LT MLG WW ERODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 221SW 120290 LEFT WHEEL WELL FORWARD INBOARD WEB PANEL ERODED FROM INSPECTION PANELS, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT WHEEL WELL FORWARD INBOARD WEB IAW EMB 120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2007032800137 20070328 00137 WP 2007 3 28 AALA20070515 1 20070319 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 298AA 49310 MSP - EMERGENCY EXIT ARROW LIGHT AT AISLE OUTSIDE OF FORWARD LAVATORY BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXI T ARROW LIGHT AT AISLE OUTSIDE OF FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007032800138 20070328 00138 NE 2007 3 28 AALA20070529 2 20070320 A 7320 LJ35801 TUBE BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4B3 NE LEFT ENGINE EPR BROKEN A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 696AN 26976 31037 SJU - AT TOP OF CLIMB LEFT ENGINE ROLLED BACK. ENGINE PRESSURE RATIO REMAINED STEADY AND ENGINE POWER DROPPED TO IDLE. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE ENGINE PRESSURE RATIO SENSOR TUBE. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2007032800139 20070328 00139 NM 2007 3 28 AALA20070516 1 20070319 A 3350 1318 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 SFO - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007032800140 20070328 00140 WP 2007 3 28 AALA20070532 1 20070321 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT MOUNT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 483A 49676 LGA - AFT FORWARD EMERGENCY FLASHLIGHT STRAP BROKEN. REPLACED STRAP FOR AFT FORWARD EMERGENCY FLASHLIGHT. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007032800141 20070328 00141 NM 2007 3 28 AALA20070534 1 20070321 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 781AN 29586 DFW - EMERGENCY LIGHT AT SEAT 3D HAS BULB MISSING. RELAMPED EMERGENCY LIGHT AT SEAT 3D. SYSTEM GROUND CHECKED NORMAL O PERATION. 2 L 7 2 4F RT T00001SE 2007032800142 20070328 00142 NM 2007 3 28 AALA20070518 1 20070320 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 796AN 30796 NRT - EMERGENCY LIGHT AT FIRST CLASS CLOSET DOOR JAMB IS BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FIRST C LASS CLOSET DOOR JAMB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032800143 20070328 00143 WP 2007 3 28 AALA20070519 1 20070320 A 3350 P2010031701 LIGHT DOUG DC9 DC982 3022082 WP CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 403A 49314 ORD - EMERGENCY EXIT LIGHT AT FORWARD GALLEY WALL FLOOR MISSING. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT FORWARD GALL EY WALL FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007032800144 20070328 00144 NM 2007 3 28 AALA20070510 1 20070316 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 939AN 30883 MIA - EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. SECURED CONNECTOR AT SIDEWALL FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007032800145 20070328 00145 EU 2007 3 28 AALA20070517 1 20070319 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 80057 465 MIA - EMERGENCY LIGHT AT SEAT 3G MISSING. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 3G. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007032800146 20070328 00146 NM 2007 3 28 AALA20070533 1 20070321 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 781AN 29586 DFW - EMERGENCY LIGHT AT SEAT 3D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 3D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032800147 20070328 00147 WP 2007 3 28 AALA20070530 1 20070320 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 437AA 49455 LGA - EMERGENCY LIGHTS AT FIRST CLASS SECTION INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS SE CTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007032800148 20070328 00148 NM 2007 3 28 AALA20070531 1 20070320 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 775AN 29584 DFW - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032800149 20070328 00149 NM 2007 3 28 AALA20070528 1 20070320 A 3397 WIRE BOEING 767 767323 1385205 NM EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 359AA 24040 MIA - EMERGENCY LIGHT AT SEAT 21H INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT AT SEAT 21H. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007032800150 20070328 00150 NM 2007 3 28 AALA20070511 1 20070317 A 7930 PUMP BOEING 777 777223 1385213 NM RROYCE RB211 RB211TRENT89 NE LEFT ENGINE FAILED A AALA A UNSCHED LANDING J K B WARNING INDICATION FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 756AM 30264 51166 DURING CLIMB NUMBER ONE ENGINE INDICATED ZERO OIL PRESSURE. CREW SHUT DOWN NUMBER ONE ENGINE. SMOKE ODOR IN CABIN AFTER ENGINE SHUT DOWN AND FLIGHT ATTENDANT REPORTED CREW REST SMOKE ALARM SOUNDED FOR BRIEF PERIOD AND NOTED LIGHT SMOKE FOR WARD OF FIRST CLASS SECTION. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME 21 MINUTES. REPLACED NUM BER ONE ENGINE DUE TO OIL PRESSURE PUMP FAILURE AND OIL PRESSURE OUT OF LIMITS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT T00001SE E00050EN 2007032800151 20070328 00151 WP 2007 3 28 07FDEA00855 1 20070315 A 5753 SKIN DOUG DC10 DC1030 3023501 WP LT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 FOUND 3 CRACKS AND LOOSE RIVETS ON SKIN OF OUTBOARD FLAP LT WING LWR AND UPPER SURFACE BETWEEN STA XOF 533 & XOF 462. C UT OUT DAMAGED AREA IAW SRM 57-10-00 FIG 85 VOL 1. FOUND ON "C" 2 CRACKS 1" LONG AND .25" LONG. REMOVED TO GAIN ACCESS T/E PROFIL UP AND LOWER SKIN. REMOVED SECTION OF OUTBOARD FLAP IAW SRM 51-31-01 PAG 36/41 VOL 2. REMOVED CLOSURE CHAN NEL ARC1951-5 IAW DWG ARC1951, ARC1652 AND SRM 51-35-01 VOL 2. FOUND 7 HOLES OVALIZED MAX DIAM .028". REPLACED LWR SK IN PANEL IAW DWG ARC1949 AND ARC1652. INSTALLED RIVETS IAW SRM 51-35-01 VOL 2. REINSTALLED T/E PROFIL UP AND LOWER SK IN FLAP IAW SRM 51-35-01 VOL 2. REINSTALLED OUTBOARD SECTION FLAP IAW SRM 51-31-01 VOL 2. FAB PART IAW DETAIL TRAV FX- 2 L 7 3 4F A22WE 2007032800152 20070328 00152 NM 2007 3 28 C1HA200775001 1 20070314 A 3010 CLAMP BOEING 727 727225 1384077 NM ANTI-ICE SYSTEM LOOSE A C1HA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 675MG 22553 EN ROUTE HAD LOWER AFT BODY HEAT LIGHT ILLUMINATE. RAN COM.2.36.5- AFTER SHUTTING OFF LEFT NR 1 BLEED VALVE, LIGHT EXTI NGUISHED. AFTER SHUTTING OFF ENGINE NR 1 BLEED VALVE FOLLOWED BY LT A/C PACK, RT PACK WOULD NOT HOLD PRESSURIZATION, HA D TO DESCENT TO 1100, TO KEEP CABIN UNDER. FOUND LEAK AT NR 1 ENGINE WING ANTI-ICE VALVE CLAMP. REPOSITIONED AND SECUR ED. RAN ENGINE AT SEVERAL POWER SETTINGS. NO LEAKS FOUND AND NO LIGHT ILLUMINATED. TIGHTEN CLAMPS AT RT FLOW CONTROL SHUTOFF VALVE. ACCOMPLISHED CABIN DECAY CHECK REF MM 05-51-101, CHECKS WITHIN LIMITS. 2 L 7 3 4F A3WE 2007032800154 20070328 00154 EA 2007 3 28 TRAX200700416 1 20070320 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 ASD INNER HANDLE CRACKED AT SHAFT CONNECTION (LOCATION MARKED). REMOVED AND REPLACED ASD INNER HANDLE IAW AMM 52-11-02. 2 L 7 2 4F RT A21EA 2007032800162 20070328 00162 NM 2007 3 28 SWAA071458 1 20070320 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 270, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007032800187 20070328 00187 NM 2007 3 28 SWAA071360 1 20070313 A 5320 6545819 WEB BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND NLG W/W WEB CRACKED AT BS 251, LBL 7.75. REPAIRED WEB PER ER. 2 L 7 2 4F RT A16WE 2007032800196 20070328 00196 NM 2007 3 28 SWAA071371 1 20070313 A 2560 6557463 ATTACH FITTING BOEING 737 7373H4 1384600 NM L1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED BRDG CHECK, L1 DOOR EVACUATION SLIDE GIRT BAR FWD FLOOR ATTACH FITTING CORRODED. REMOVED AND REPLACED FWD FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007032800197 20070328 00197 NM 2007 3 28 ASAA0741543 1 20070321 A 3520 289801240 ATTACH FITTING BOEING 737 737490 1384715 NM O2 MASKS CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 799AS 29270 DURING C-CHECK MAINTENANCE FOUND RELEASE CBL LANYARD ATTACH EYELET ON SEVERAL O2 MASK ASSYS CRACKED/BROKEN, WHICH IN THE EVENT OF CABIN DEPRESSURIZATION AND MASK DEPLOYMENT WOULD PREVENT THE O2 GENERATOR RELEASE PIN FROM BEING PULLED. INSP ECTION CARRIED OUT ON ALL PSU O2 MASK ASSYS. ALL O2 MASK ASSYS IDENTIFIED AS UNSERVICEABLE WERE REPLACED WITH SERVICEAB LE ASSYS. 2 L 7 2 4F RT A16WE 2007032800200 20070328 00200 NM 2007 3 28 WRLA2007048 1 20070325 A 5754 SKIN DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE L/E SLAT GOUGED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271WA 48518 DURING C-04 CHECK, RIGHT WING NR 8 SLAT INTERNAL SURFACE SKIN GOUGE STATION XOS 1009. REPAIRED PER MD-11 SRM 57-10-00 F IG.=10 VOL.1 REV.38 2 L 7 3 4F 4 F RT A22WE E24NE 2007032800217 20070328 00217 NM 2007 3 28 2007UALA00804 1 20070319 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 20UAÊ 29166 DOOR SLIDE EMERGENCY LIGHT NOT ON DOOR R2. REPLACED WITH SERVICEABLE SLIDE EMER LT (DR R2, R4). ON GRD, DOOR R2, R4 SLI DE EMERGENCY LIGHT OP CHECKED NORMAL. READY FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032800229 20070328 00229 NM 2007 3 28 2007UALA00807 1 20070318 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EEL AT 2A & 4F FWD, 5A AFT, 33C, & 44 RIGHT ARE INOP. RELAMPED EACH OF THE FIVE POSITIONS. ALL OP CHECKED OK FOR SERVI CE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032800233 20070328 00233 NM 2007 3 28 2007UALA00811 1 20070316 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 508UA 24744 MAIN CABIN FLOORBEAM T-CAP CORROSION, STA 1640 RBL 56-59. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION. INSTALL ED NEW T-CAP SECTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032800234 20070328 00234 NM 2007 3 28 2007UALA00812 1 20070316 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 508UA 24744 FWD CARGO LEFT SIDE WALL LAV SERVICE PORT UPPER SKIN CORRODED AROUND DUCT AT STA 705-711, STR 19L-21. MAJOR REPAIR ACCO MPLISHED. REPLACED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032800235 20070328 00235 NM 2007 3 28 2007UALA00813 1 20070317 A 5322 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 508UA 24744 AFT PIT STA 1360 BETWEEN STR 29R-28R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED NEW TIE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032800236 20070328 00236 NM 2007 3 28 2007UALA00814 1 20070316 A 3397 7956243 WIRE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 779UA 26941 BOTH EEL PROX LIGHTS AT 1F ARE INOPERATIVE. REPAIRED WIRE TO EEL LIGHTS. ALSO RELAMPED, OP CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007032800237 20070328 00237 NM 2007 3 28 2007UALA00815 1 20070316 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 779UA 26941 THE AFT EEL PROX LIGHT AT SEAT 3F IS INOP. REPLACED LAMP ASSEMBLY. OP CHECKS OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007032800239 20070328 00239 NM 2007 3 28 2007UALA00817 1 20070319 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 846UA 1600 COCKPIT DOME LIGHT IS INOP WHEN SWITCH IS IN DIM AND DIM WHEN SWITCH IS IN BRIGHT. [SUP 5-1-07] FOUND 1 OPERATING LAMP IN EACH FIXTURE. RELAMPED ALL 8 BULBS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032800240 20070328 00240 SO 2007 3 28 C2XA07IA070 1 20070326 A 2150 8152403 ACM EMB 145 EMB145XR 3260214 SO NR 1 MALFUNCTIONED A C2XA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 27 16183 5522 5522 14500914 IAH - FLIGHT 2281, AFTER TAKEOFF WHEN PACKS SELECTED ON, COCKPIT AND CABIN IMMEDIATELY FILLED WITH SMOKE AND PACK 2 VALV E FAIL ADV ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER 1 ACM, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. 2 L 7 2 4F RT 2007032800241 20070328 00241 EU 2007 3 28 2007UALA00818 1 20070319 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 443UA 820 EMERGENCY LIGHTS TEST FAILED. REPLACED EPSU AND BATTERY 11WL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032800242 20070328 00242 NM 2007 3 28 2007UALA00819 1 20070319 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 305UA 23666 EMERGENCY SLIDE LIGHT INOP AT DOOR 1L. [SUP 4-17-07] RELAMPED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032800243 20070328 00243 NM 2007 3 28 2007UALA00820 1 20070319 A 3397 58781 CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 305UA 23666 EEL LIGHTS INOP AFT OF ROW 16. CLEANED LIQUID FROM EEL TRACK. REPLACED RIBBON CABLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032800247 20070328 00247 NM 2007 3 28 2007UALA00824 1 20070316 A 2612 MODULE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FIRE DETECTION FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 304UA 23665 FIRE TEST FAILED. SWTCH LEFT, ENG 1 AND APU FIRE HANDLES DO NOT ILLUMINATE. FOUND FAULTY FIRE/OVERHEAT DTECTOR CONTROL MODULE. REPLACED THE FIRE/OVERHEAT DTECTOR CONTROL MODULE. [SUP 4-17-07] SHOP FOUND NO FAULTS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032800248 20070328 00248 NM 2007 3 28 2007UALA00827 1 20070320 A 5320 SILL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 AFT ENTRY DOOR CUTOUT LOWER SILL HAS SEVERAL AREAS OF CORROSION. [SUP 4-17-07] MAJOR REPAIR: ACCOMPLISHED REPAIR PER S RM 51-70-11 FIGURE 1 PAGE 1 THRU 6. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032800249 20070328 00249 NM 2007 3 28 2007UALA00828 1 20070320 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 AFT GALLEY DOOR INNER CHORD OF CREASE BEAM CORRODED STA 967-977 LBL 45-49, WL 208-208. REMOVED CORROSION. REFERENCE SRM 53-60-51 PAGE 6 ITEM 105 THRU 113. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032800250 20070328 00250 NM 2007 3 28 2007UALA00829 1 20070320 A 5320 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 PASSENGER CABIN FWD ENTRY DOOR BELOW THRESHOLD STA 312 TO 344 LBL 60 WL 208.1 HAS NUMEROUS AREAS OF CORROSION AROUND SCR EW HOLES. REMOVED CORROSION. REFERENCE SRM 53-10-51 PAGE 6 ITEM 105 THRU 115. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032800252 20070328 00252 2007 3 28 2007UALA00832 4 20070317 A 2565 COVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EVAC SLIDE OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 402UA 439 THE 2L SLIDE COVER FELL OFF. [SUP 05-18-07] SECURED SLIDE COVER. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032800253 20070328 00253 NM 2007 3 28 2007UALA00833 1 20070317 A 2560 GIRT BAR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 910UA 25254 DOOR 1L EVAC SLIDE GIRT MATERIAL HANGING LOOSE FROM CONTAINER. SECURED AND STOWED BOTTOM PORTION OF SLIDE. INSPECTION ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032800254 20070328 00254 2007 3 28 2007UALA00834 4 20070317 A 2565 SLIDE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE R1 DOOR LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 DOOR 1R SLIDE PRESSURE READS BELOW SERVICEABLE LIMIT. REPLACED R1 DOOR SLIDE PER MM 25-66-01. CAUSED BY SUSPECT SEAL L EAKAGE AT BOTTLE CONNECTION. 2 L 7 2 4F 4 F RT A1NM E24NE 2007032800256 20070328 00256 NM 2007 3 28 2007UALA00836 1 20070321 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY LIGHT INOP AT ROW 6GH AND 7GH. WIRE BROKEN BETWEEN SEAT 7H AND 8H CAUSING BOTH EEL LOSS. REPAIRED WIRE AND ALL SEAT EEL OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032800257 20070328 00257 NM 2007 3 28 2007UALA00837 1 20070321 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY CEILING LIGHT ABOVE ROW 17 INOP. RELAMPED LIGHT. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041600117 20070416 00117 NM 2007 4 16 2007UALA01035 1 20070404 A 2821 FUEL FILTER BOEING 737 737322 1384676 NM UNKNOWN A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 301UA 23642 NR 2 FUEL TANK FILTER BYPASS LITE ILLUMINATED ON INITIAL CLIMBOUT. FOUND FUEL FILTER CLEAN. DIFFERENTIAL PRESSURE SWIT CH WARNING TEST CHECKED GOOD. REPLACED FUEL FILTER. 2 L 7 2 4F RT A16WE 2007041700002 20070417 00002 CE 2007 4 17 GLBA20060935 1 20070411 A 2130 FILTER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE PRESSURE RELAY DIRTY A GLBA O OTHER J WARNING INDICATION CR CRUISE 1 NM 03 208GL UE208 AIR RETURN, FLIGHT 5141 ENROUTE, CABIN "ALTITUDE HIGH" ILLUMINATED AND NORMAL PRESSURIZATION APPEARED TO HAVE FAILED. M X CLEANED FILTERS ON THE CABIN PRESSURE RELAY AND CHECKED ALL REMAINING FILTERS FOR ANOMALIES IAW REF MM 21-30. GROUND O PERATIONAL TESTS OK. 2 L 7 2 4T 4 T RT A24CE E26NE 2007032900001 20070329 00001 NM 2007 3 29 QXEA200700420 1 20070314 A 5415 MOUNT DHAV DHC8 DHC8202 2809007 NM MLG ACTUATOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - FOUND LEFT MAIN LANDING GEAR ACTUATOR UPPER MOUNT POINT ON H MEMBER HAS FRETTING CORROSION ABOVE BOLT HOLE. RE PAIRED IAW RD8-54-1178. 2 H 7 2 4T RT A13NM 2007032900002 20070329 00002 NM 2007 3 29 QXEA200700425 1 20070314 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - NR 7 SEAT TRACK HAS CORROSION AROUND A CAMLOCK RECEPTICAL AT X202, INBOARD FLANGE. REPAIRED IAW RD8-53-4698 AN D SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007032900003 20070329 00003 NM 2007 3 29 QXEA200700418 1 20070310 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 436-526 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - SEAT TRACK NR 8 HAS MINOR SCRATCHES AND CHAFES AT STATION 436 TO 486, 465, 472 TO 486, 508 TO 521, 526. REPAIR ED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2007032900006 20070329 00006 NM 2007 3 29 QXEA200700419 1 20070310 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 456-490 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - SEAT TRACK NR 11 HAS MINOR SCRATCHES AT STATION 456, 487, 490. REPAIRED IAW RD8-53-1342. 2 H 7 2 4T RT A13NM 2007032900007 20070329 00007 2007 3 29 FDKA200702074 4 20070218 A 3418 0861DT5MOD1 AOA EMB 145 EMB145LR 3260212 SO STALL WARNING MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 839MJ 11662 145416 FDM 6151 CAK-ATL (0512 PHX LCL). SPS 2 INOP AND SPS ADVANCE MESSAGES. MX REPLACED THE RIGHT AOA VANE AND OPS CHECK NOR MAL. 2 L 7 2 4T RT T00011AT 2007032900010 20070329 00010 SO 2007 3 29 FDKA200703102 1 20070308 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6038 ATL-CLT (1224 PHX LCL). MAIN CABIN DOOR WILL NOT CLOSE COMPLETELY. MX LUBED ROLLERS, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007032900013 20070329 00013 SO 2007 3 29 FDKA200701055 1 20070129 A 5320 14521725013 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 CORROSION ON FWD AND AFT SERVICE DOOR SILLS BETWEEN FR22, FR23, FR18 AND FR20. REPLACED SILLS. 2 L 7 2 4T RT T00011AT 2007032900014 20070329 00014 SO 2007 3 29 FDKA200701057 1 20070129 A 5320 14521721005 SPLICE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 CORROSION ON BUTT SPLICE BL 0 BETWEEN FR15 AND FR18. REPLACED BUTT STRAP. 2 L 7 2 4T RT T00011AT 2007032900015 20070329 00015 NM 2007 3 29 QXEA200700444 1 20070322 A 3150 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 421QX 4149 POWER PLANT MESSAGE OCCURRED DURING TAXI OUT. AIRCRAFT RETURNED TO GATE. MAINTENANCE INTERROGATED CDS AND FOUND PEC FA ULT CODE 130B ON NR 2 PEC. CLEARED FAULT IAW Q400 AMM TASK 61-20-36-070-801. C/W OPS CHECK OF AUTO FEATHER (FAULT OCCU RRED DURING A/F TEST WHILE TAXING) IAW Q400 AMM TASK 61-20-00-710-805. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RE TURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900016 20070329 00016 NM 2007 3 29 QXEA200700450 1 20070324 A 3150 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 422QX 4150 DU BAD ON ED. PERFORMED CHECKLIST PROCEDURE. MESSAGE REMAINS. MAINTENANCE CYCLED AIRCRAFT POWER AND REINITIALIZED DIS PLAY UNITS. ALL INDICATIONS NORMAL WITH NO REOCCURRENCE OF MESSAGE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900018 20070329 00018 NM 2007 3 29 QXEA200700468 1 20070327 A 3350 XD4N RELAY BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY LIGHTS INOPERATIVE A QXEA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 NM 09 421QX 4149 PDX - ON FLIGHT 2362, RETURNED TO GATE. CREW REPORTS CABIN EMERGENCY LIGHTS WILL NOT TURN OFF WHILE ARMED. MAINTENANCE REPLACED 3351 K2 RELAY. OPERATIONAL CHECK GOOD AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900019 20070329 00019 NM 2007 3 29 QXEA200700469 1 20070327 A 2913 6618202 PUMP BOMBDR DHC8 DHC8402 1390042 NM HYD SYSTEM INOPERATIVE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 403QX 14985 14985 4037 PDX - ON FLIGHT 2449, RETURNED TO GATE NR 3 HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED AFTER ENGINE START PRIOR TO TAXI. THE LIGHT ILLUMINATED RIGHT AFTER BRAKE RELEASE FOR TAXI. MAINTENANCE REMOVED AND REPLACED NR 3 HYDRAULIC PUMP. OPERAT IONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900020 20070329 00020 EU 2007 3 29 07FDEA00866 1 20070315 A 5415 ATTACH FITTING AIRBUS 310 A310324 3930206 EU ZONE 500 DENTED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 NICK IN PYLON ATTACH FITTTING AND PYLON REINFORCEMENT PLATE. REPAIR WAS PERFORMED IAW EA 6-5720-103365 AND RAS/BAE/1003 600/2006 ISSUE "A" (BLEND OUT). 2 L 7 2 4F RT A35EU 2007032900021 20070329 00021 NM 2007 3 29 QXEA200700449 1 20070326 A 6120 301450301 PSEU BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 424QX 4050 4050 4006 EUG FLIGHT NR 2421: FLIGHT DIVERTED TO PDX AFTER TAKEOFF FROM LAX. POWER PLANT MESSAGE ON ED ABOUT 2 OR 3 MINUTES AFTER TAKEOFF FROM LAX. MAINTENANCE REPLACED PSEU IAW 32-61-01-000-801 AND 32-61-01-400-801. ALSO, C/W FIM 61-20-07-810-814 , STEPS 1-5(3) FOR FAULT 336 A & B. OCF PERFORMED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900025 20070329 00025 SO 2007 3 29 FDKA200701028 1 20070127 A 2750 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO T/E FLAP MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 840MJ 145429 FDM 6109 MCO-PNS (0432 PHX LCL). CREW REPORTED FLAP 1 LOW SPEED MESSAGE. MAINTENANCE RESET THE SYSTEM. 2 L 7 2 4T RT T00011AT 2007032900026 20070329 00026 EU 2007 3 29 07FDEA00867 1 20070315 A 5730 SKIN AIRBUS 310 A310324 3930206 EU LT WING CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CORROSION ON LT WING TOP SKIN. REPAIR WAS PERFORMED BY BLEND OUT IAW EA 6-5720-106356 AND RAS/BAE/1003742/2006 IS SUE "A". 2 L 7 2 4F RT A35EU 2007032900028 20070329 00028 SO 2007 3 29 FDKA200701016 1 20070118 A 7830 83990168 SWITCH EMB 145 EMB145LR 3260212 SO THRUST REVERSER FAULTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 7558 145214 FDM 6111 BMI - ATL (0611 PHX LCL). ABORTED T/O DUE TO E2 REV DISAGREE MESSAGE ON T/O. MX REMOVED AND REPLACED LOWER ST OW SWITCHES. 2 L 7 2 4T RT T00011AT 2007032900031 20070329 00031 EU 2007 3 29 07FDEA00871 1 20070315 A 5320 PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CORROSION AT SERVICE BOX PANEL DOUBLER C12-12A LT. REPAIR WAS PERFORMED BY BLEND OUT IAW EA 6-5312-103410 AND RAS /AS/177/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007032900033 20070329 00033 SO 2007 3 29 FDKA200701017 1 20070118 A 7830 83990168 SWITCH EMB 145 EMB145LR 3260212 SO THRUST TREVERSER FAULTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 847MJ 8745 145517 FDM 6085 MCO-NAS (0918 PHX LCL). CREW ABORTED T/O DUE TO E1 TR REV DISAGREE MESSAGE. MX REMOVED AND REPLACED LOWER TRA NSIT SWITCH. 2 L 7 2 4T RT T00011AT 2007032900034 20070329 00034 EU 2007 3 29 07FDEA00873 1 20070315 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 412FE 360 FOUND CRACK FR 38 PROFILE MDCC FLOORBEAM LT FWD CARGO COMPARTMENT BETWEEN SEAT TRACKS L-4 & L-5, REF SRM 53-10-00 AND SR M 53-10-15. REPAIRED FR 38 MDCC FLOORBEAM BETWEEN SEATRACKS L-4 AND L-5 IAW A310-200 SRM 53-10-15, FIG 201, SHT 6A. 2 L 7 2 4F RT A35EU 2007032900035 20070329 00035 EU 2007 3 29 07FDEA00874 1 20070315 A 5330 A53610602211 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CORROSION AT AFT NOSE LANDING GEAR PANEL C17-18, P52-53 RT. REPAIR WAS PERFORMED IAW EA 6-5312-103408 REV A AND R AS/AS/176/2006 ISSUE "A", SEE ALSO DRW R536-11104, CHANGED STRINGER, EXTERNAL DOUBLER INSTALLED AND DENT ACCEPTED. 2 L 7 2 4F RT A35EU 2007032900036 20070329 00036 EU 2007 3 29 07FDEA00875 1 20070315 A 5320 PROFILE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CORROSION AT L-PROFILE, C73-76, P26 RT. REPAIR WAS PERFORMED BY REMOVING CORROSION IAW EA 6-5318-103403 REV A AND RAS/DAHAM/4021374/2006 ISSUE "C". 2 L 7 2 4F RT A35EU 2007032900037 20070329 00037 2007 3 29 FDKA200701030 4 20070129 A 2210 AUTOPILOT SYS DHAV DHC8 DHC8101 2809002 NM COCKPIT MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 805LR 039 FDM 6137 JFK-ORF (0744 PHX LCL). AUTO PILOT WILL NOT ENGAGE. RESET SYSTEM, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007032900038 20070329 00038 EU 2007 3 29 07FDEA00876 1 20070315 A 5730 SKIN AIRBUS 310 A310203 3930313 EU LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 412FE 360 LT WING LOWER SKIN SURFACE HAS A CRACK OF APPROX 1 INCH LONG AT AFT END OF RIB 11, 4 INCHES AFT OF REAR SPAR, FWD INBD E ND OF CUTOUT FOR ACCESS PANEL 581AB. CRACK RUNS THROUGH 1 FASTENER HOLE. ACCOMPLISHED RIB 11 PERMANENT REPAIR IAW FED EX EA 6-5710-107675 AND SB A310-57- 2066. LEAK CHECK GOOD IAW A310-200 AMM 28-11-00-5. 2 L 7 2 4F RT A35EU 2007032900041 20070329 00041 EU 2007 3 29 07FDEA00879 1 20070315 A 5315 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND TOP CAP BEAM C25 AD UPPER FLANGE A537-73651-210 CORRODED. REPAIR WAS PERFORMED IAW SRM 53-10-15/FIG 207. 2 L 7 2 4F RT A35EU 2007032900042 20070329 00042 NM 2007 3 29 07FDEA00880 1 20070315 A 5340 651593516 STRINGER CLIP BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 MAIN CABIN FS 640, STR 3R STRINGER CLIP IS DAMAGED. FABRICATED STRINGER CLIP, TREATED, PRIMED AND INSTALLED CLIP REF SR M 51-10-2 PG 3, SRM 51-30-2 PG 3, AND DWG 65-15935-16. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007032900043 20070329 00043 NM 2007 3 29 FDKA200701009 1 20070110 A 2910 FLUID DHAV DHC8 DHC8101 2809002 NM HYDRAULIC SYS LOW A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 808LR 073 FDM 6137 BTV-JFK (0450 PHX LCL). LOSS OF BRAKES DUE TO HYD ISOL VALVE CAUTION LIGHT. MX SERVICED HYD AND RAN ENG NO DE FECTS NOTED. 2 H 7 2 4T RT A13NM 2007032900048 20070329 00048 EU 2007 3 29 07FDEA00883 1 20070315 A 5315 A53773651218 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 MAINT ERROR A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 813FD 500 MISDRILLED HOLE IN THE FLOOR STRUCTURE OF FWD CARGO COMPARTMENT C22 RT. REPAIR WAS PERFORMED IAW EA 6-5313-103406 AND R AS/DABRE/7007121/2006 ISSUE "A". REPAIR ANGLE INSTALLED. 2 L 7 2 4F RT A35EU 2007032900049 20070329 00049 EU 2007 3 29 07FDEA00884 1 20070315 A 5300 UNKNOWN AIRBUS 310 A310203 3930313 EU BS 1315 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 412FE 360 FOUND CORROSION EXIST AT AVIONICS COMPARTMENT STA 1315/ FR 17 STGR 45 LT 2' BY 2' INCHES BELOW ACCESS PNL 121 PF ZONE 12 0 COMPLIED WITH EA 6-5330-107691. 2 L 7 2 4F RT A35EU 2007032900051 20070329 00051 EU 2007 3 29 07FDEA00886 1 20070315 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU BS 2612-2877 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 669FE 774 MAIN CABIN SEAT TRACK CORRODED IN AREAS FROM FRAME 40 TO FRAME 45 RBL 77. REMOVED CORROSION ORIGINAL THICKNESS .145 REM OVED .033 REMAINING MAT IS .112. FOUND TO BE OUT OF LIMITS IAW A300-600 53-10-16 TOOL NR TWS 58329B. REMOVED SEAT TRAC K IAW FEDEX A300-600 SRM 51-40-21 PG7. FABRICATED NEW SEAT TRACK IAW ABS5456C580EPART MARKED REF FEDEX GMM 7-0-1000. I NSTALLED SEAT TRACK IAW FEDEX A300-600 SRM 51-40-21 PG 6-7. 2 L 7 2 4F RT A35EU 2007032900052 20070329 00052 EU 2007 3 29 07FDEA00887 1 20070315 A 5340 A53773643205 ATTACH FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CORRODED CLIP AT C35, P43-44 RH. CLIP REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007032900054 20070329 00054 EU 2007 3 29 07FDEA00889 1 20070315 A 5330 SKIN AIRBUS 310 A310203 3930313 EU BS 1315 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 412FE 360 FOUND CORROSION EXIST AT AVIONIC COMPARTMENT AT STA 1315/FR 16 AND 17 STGR 46 ON FUSELAGE SKIN TOTAL 2 BY 2 INCHES BELOW ACCESS PNL 121 PF ZONE 120 COMPLIED WITH FEDEX EA 6-5330-107691. 2 L 7 2 4F RT A35EU 2007032700158 20070327 00158 NE 2007 3 27 NWAA071129880 2 20070320 A 7310 629195 MANIFOLD DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE FUEL SYSTEM CRACKED A NWAA O OTHER K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 GL 01 675MC 47651 696721 DURING TAKEOFF, THE TOWER REPORTED EXCESSIVE SMOKE FROM THE NR 1 ENGINE. FLIGHT CREW ALSO REPORTED HIGHER FUEL FLOW FRO M THE NR 1 ENGINE. THE FLIGHT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A CRACKED PRIMARY FUEL M ANIFOLD. REMOVED AND REPLACED THE NR 1 ENGINE, TESTED AND RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A6WE E2EA 2007032700159 20070327 00159 NM 2007 3 27 HALA0700098 1 20070312 A 2750 834503 SWITCH BOEING 767 76733A 1385209 NM TE FLAPS MALFUNCTIONED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 580HA 28140 ATB - EICAS "L/E SLAT ASYM" AND "LEADING EDGE " LIGHT ON WITH FLAP LEVER IN UP POSITION AND THRU FLAPS 30 POSITION. FLA P INDICATOR POINTERS SHOWED 1 WITH LEVER UP. REPLACED L/E SLAT SENSOR SWITCH PER MM 27-88-01. OPS CHK OK. BITE FSEU HA D FAULT CODE 27-81021. BITE PSEU FAULTED S284 PROX SWITCH CHECK S284 OK. REPLACED S284 PRECAUTIONARY PER TEXT SERVICE. CHECK OK PER TASK 27-88-01-722. 2 L 7 2 4F RT A1NM 2007032700169 20070327 00169 NM 2007 3 27 UPS07549544 1 20070322 A 2560 65B4028912 HARNESS BOEING 757 75724APF 1384969 NM COCKPIT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 407UP 23729 EMERGENCY HARNESS ASSY SOAKED AND UNUSEABLE. REPLACED EMERGENCY HARNESS WITH SERVICEABLE ONE. 2 L 7 2 4F RT A2NM 2007032700170 20070327 00170 WP 2007 3 27 UPS07849535 1 20070313 A 5330 FINGER DOUBLER DOUG DC8 DC873F 302199F WP FS 935 RBL65 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C3 SUBFLOOR FINGER DOUBLER HEAVY CORRODED AT STA 935 RBL 65. REMOVED, FABRICATED AND INSTALLED REPLACEM ENT FINGER DOUBLER IAW SRM 53-2-0 FIG 1F, 53-07-03 AND 51-3-02. 2 L 7 4 4F RT 4A25 2007032700183 20070327 00183 EU 2007 3 27 AALA20070466 1 20070310 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 40064 507 MIA - EMERGENCY LIGHT AT SEAT 24G INOPERATIVE. FOUND PIN PUSHED BACK ON CONNECTOR. SECURED PIN ON CONNECTOR. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007032700187 20070327 00187 WP 2007 3 27 AALA20070454 1 20070307 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AA 49271 LGA - EMERGENCY ESCAPE PATH LIGHT IN CABIN HAS LENS MISSING. REPLACED LENS FOR EMERGENCY ESCAPE PATH LIGHT IN CABIN. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007032700192 20070327 00192 NE 2007 3 27 AALA20070455 2 20070308 A 7261 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RIGHT LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 486AA 49679 728231 TPA INFLIGHT - RSW TO DFW, DURING CRUISE RIGHT ENGINE OIL QUANTITY AND PRESSURE DROPPED. CREW PERFORMED RIGHT ENGINE S HUTDOWN AND DIVERTED TO TPA. LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME 15 MINUTES. FOUND RIGHT ENGINE LEAKING OIL. PERFORMED FLIGHT DATA RECORDER DOWNLOAD. REPLACED NUMBER TWO ENGINE AT TPA ON 10 MAR 2007. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007032700202 20070327 00202 NM 2007 3 27 USAA070247 1 20070327 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 SKIN DOUBLER, STA 747-767, BETWEEN 27L-28R HAS CORROSION. INSTALLED REPAIR PARTS PER SRM 51-40-02; CORR TASK C53-208-01 ; LEVEL 2, DEFECT SIZE: 20 INCH AREA. 2 L 7 2 4F RT A16WE 2007032700206 20070327 00206 NE 2007 3 27 HNAA0700048 2 20070318 A 7310 FUEL FILTER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE NR 2 ENGINE DIRTY A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 934HA 139 NR 2 FUEL FILTER BYPASS CAUTION LIGHT ILLUMINATED AFTER TAKEOFF. INSPECTED WIRE HARNESS NO DEFECT NOTED. INSPECTED AND REPLACED THE HP FUEL FILTER. INSPECTED AND CLEANED THE L/P FUEL FILTER. RAN AIRCRAFT AT POWER SETTINGS, NO DEFECT NOT ED. 2 H 7 2 4T 4 T RT A13NM E20NE 2007032700212 20070327 00212 WP 2007 3 27 ABXA070080 1 20070228 A 5320 99577093 INTERCOSTAL DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 949AX 47325 INTERCOSTAL AT LONGERON 29 RIGHT CORRODED BETWEEN LONGERON 29 RIGHT AND INTERCOSTAL FROM STA 965 - 980, BULGED ON INBOAR D LEGS. REMOVED AND REPLACED INTERCOSTAL LONGERON 29 RIGHT, FS 965 TO 980 IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2007032800015 20070328 00015 NM 2007 3 28 HNAA0700051 1 20070325 A 3320 BA08006281 BALLAST DHAV DHC8 DHC8102 2809003 NM CABIN DEFECTIVE A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 07 812EX 38014 38014 312 SMOKE COMING FROM AROUND RIGHT FWD FILLER PANEL ABOVE EMERGENCY EXIT DOOR. TROUBLESHOT TO SHORTED BALLAST ON RIGHT FORW ARD FILLER PANEL PERFORMED HIDDEN DAMAGE INSPECTION NO DEFECTS NOTED. REPLACED BALLAST ASSEMBLIES (2). 2 H 7 2 4T RT A13NM 2007032800020 20070328 00020 WP 2007 3 28 UPS07849550 1 20070308 A 5320 SAA5615530191 STIFFENER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C3 HEAVY CORROSION AT BASE OF VERTICAL STIFFENER ON STA 8 BULKHEAD IN A/C COMP'T, LEFT SIDE, ABOVE L28. REMOVED, FABRICATED AND INSTALLED STIFFENER AND SPLICE REPAIR IAW SRM 51-1-21, 51-1-20D AND DWG 5615530. 2 L 7 4 4F RT 4A25 2007032800024 20070328 00024 SO 2007 3 28 GLBA20060926 1 20070322 A 3244 314461 TIRE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE MLG FAILED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 96ZK 120096 FLT 5044- PILOT HAD A REPORT THAT THE NR 1 TIRE HAD SEPERATED FROM THE WHEEL ASSY UPON TAKEOFF. SUBSEQUENT LANDING RESU LTED IN THE NR 2 IB TIRE FAILING AS WELL. UPON LANDING IN DEN. MX PERFORMED HIGH DRAG SIDE LOAD LANDING INSPECTION PER EMB-120 MM 5-50-03 , NR 1 AND 2 BRAKE INSPECTION PER GLA TC 120-3244.02, HUBCAP INSPECTION PER AD 2004-12-12. ALL CHECK S GOOD. MX R & R SHOCK ABSORBER SENSOR PER EMB MM31-10. MX R & R LT AFT INBOARD LANDING GEAR DOOR IAW EMB120 MM 52-81. M X R & R LT SEQUENCE VALVE HYD LINE IAW EMB120 MM 20-10-03. OPS CHECK GOOD IAW EMB-120 32-32-00. MX R & R LT OUTBOARD AFT DOOR SUPPORTS IAW 52-21. MX R & R LT AFT OUTBOARD GEAR DOOR ACTUATOR ROD IAW EMB120 MM52-81. MX R & R LT AFT INBOARD G 2 L 7 2 4T 4 T RT A31SO E20NE 2007032800026 20070328 00026 WP 2007 3 28 07FDEA01132 1 20070326 A 5230 SPOOL DOUG MD10 MD1010F 3022112 WP CARGO DOOR CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 566FE 46989 MAIN CARGO DOOR NR 3 SPOOL FITTING HAS CRACK INDICATIONS. NR 3 SPOOL FITTING HAS CRACK INDICATIONS ON FWD INBD HOLE. R EAMED HOLE TO .453 IAW DC/MD10 SRM 53-50-01 FIG 17, VOL 1. PERFORMED BHEC IAW NDT SPM 06-10-01.003. NO CRACKS NOTED. DOOR TO BE RIGGED ON FEDEX, N/R N00712. 2 L 7 3 4F RT A22WE 2007032800034 20070328 00034 NM 2007 3 28 CALA0700152 1 20070323 A 5330 6545774 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 77303 23354 INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT STA 876 BETWEEN S23L AND S24L. A REPAIR WAS INSTALLED IAW SRM 53- 00-01, REPAIR 31, FIGURE 201. 2 L 7 2 4F RT A16WE 2007032800040 20070328 00040 NM 2007 3 28 CALA0700140 1 20070323 A 5313 BAC1498146 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 77303 23354 INSPECTION FOUND STRINGER 27L CORRODED NEAR VHF ANTENNA DOME NUT, STA 500. THE CORRODED SECTION OF STRINGER WAS REMOVED AND REPAIR STRINGER AND SPLICES WERE INSTALLED IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2007032800042 20070328 00042 NM 2007 3 28 CALA0700142 1 20070323 A 5320 147A8540U8 STRUCTURE BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13248 28808 INSPECTION FOUND R-2 DOOR CHORD CORRODED FROM STA 947.5-1000, RBL 52. THE CHORD WAS REMOVED AND REPLACED IAW SRM 51-40- 02. 2 L 7 2 4F RT A16WE 2007032800079 20070328 00079 EA 2007 3 28 TRAX200700404 1 20070319 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 837AS 7271 LEFT BONDED SKIN COMMON TO FS 640 FRAME IS CRACKED. COMPLIED WITH REO 601R-53-61-506 REPAIR TO SKIN BUTT STRAP L/H SIDE FS 640.00 STR 8-13. 2 L 7 2 4F RT A21EA 2007032800086 20070328 00086 NM 2007 3 28 07FDEA00723 1 20070308 A 5713 ARB75111 STRINGER DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LT WING TANK - APPROX NINE (9) INCHES LENGTH CRACK FOUND AT STRINGER END 11L (XORS 704) DURING HFEC INSPECTION STRI NGER END 11L (XORS 704)AT LT WING TANK REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007032800087 20070328 00087 NM 2007 3 28 07FDEA00724 1 20070309 A 5713 ARB75141 STRINGER DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LT WING TANK - APPROX 12 INCHES LENGTH CRACK FOUND AT STRINGER END 14L (XORS 521) DURING HFEC INSPECTION STRINGER END 14L (XORS 521) AT LT WING TANK REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS P ER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007032800088 20070328 00088 NM 2007 3 28 07FDEA00728 1 20070309 A 5753 NRC67622 VANE DOUG MD11 MD11 3023602 NM ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT HAND WING - INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED COMPLIED WITH FEDEX EA 1-5750-109837, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007032800089 20070328 00089 NM 2007 3 28 07FDEA00729 1 20070309 A 5713 ARB75122 STRINGER DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT HAND WING TANK - APPROX 13 INCHES CRACK FOUND AT STRINGER END 12R (XORS 642) DURING HFEC INSPECTION STRINGER EN D 12R (XORS 642) RIGHT HAND WING TANK REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007032800093 20070328 00093 WP 2007 3 28 ASTAR200700015 1 20070323 A 2497 LEAD DOUG DC8 DC873 302199C WP NR 1 GENERATOR DAMAGED A DHLA K NONE O OTHER DE DESCENT 1 GL 05 805DH 46125 ON APPROACH TO IAH, NR 1 "GEN UNPARALLELED" LIGHT ILLUMINATED 20-30 SECONDS LATER THERE WAS A BURNING ODOR , THEN CLEARE D. TRANSFERRED TO DMI LOG ITEM NR 28522 IAW DC8 MEL 24-1 CAT "C" SP PROC. C/W; NR 1 GEN DISCONNECTED. PLACARDS INSTAL LED, SOURCE OF ODOR IDENTIFIED, NR 1 GENERATOR LEAD. 2 L 7 4 4F RT 4A25 2007032800097 20070328 00097 SO 2007 3 28 RAIA00703052 1 20070320 A 3350 SIGN EMB 145 EMB145 3260210 SO CABIN MALFUNCTIONED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 821HK 145068 POST FLT NR 5550 - STL - EMERGENCY LIGHT FWD CEILING EXIT LOCATOR IS INOP. MAINTENANCE RESET POWER TO OVERHEAD EXIT MAR KER ADJACENT TO GALLEY, OPS CHECK GOOD OF EMERGENCY LIGHT SYSTEM. 2 L 7 2 4F RT T00011AT 2007032800100 20070328 00100 SO 2007 3 28 RAIA00703059 1 20070321 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 830HK 145313 POST FLT NR 5560 - STL - EMERGENCY LIGHT INOP AT GALLEY WALL EXIT LOCATOR. MAINTENANCE CYCLED POWER SYSTEM CHECKED GOOD . 2 L 7 2 4T RT T00011AT 2007032800103 20070328 00103 SO 2007 3 28 RAIA00703058 1 20070321 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 814HK 145046 POST FLT NR 5566 - STL - EMERGENCY LIGHT INOP AT FLOOR PROXIMITY LIGHT. MAINTENANCE RESEATED CONNECTOR, SYSTEM CHECK GO OD. 2 L 7 2 4T RT T00011AT 2007032800115 20070328 00115 NM 2007 3 28 SWAA071547 1 20070323 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING MV2 CK, FOUND FUSELAGE SKIN CRACKED AT BS 425, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007032800122 20070328 00122 NM 2007 3 28 SWAA071555 1 20070323 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 502C, STR 20L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007032800128 20070328 00128 2007 3 28 MWEA070046 4 20070323 A 3140 40815070909 ELECTRONIC UNIT BOEING 717 717200 1383700 NM NR 2 FAULTED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 918ME 55180 LEVEL 1 ALERT -VIA FAIL- ILLUMINATED. REMOVED AND REPLACED NR 2 VIA. 2 L 7 2 4F TR A6WE 2007032800160 20070328 00160 EA 2007 3 28 TRAX200700425 1 20070322 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SO 27 838AS 7276 FLAPS AGAIN, FAILED AT 0 DEG PERFORMED 0 DEG FLAP LANDING ON 41,000 CARD. REPEAT WRITE UP. EMERGENCY EQUIPMENT ON STAN DBY. 2 L 7 2 4F RT A21EA 2007032800164 20070328 00164 NM 2007 3 28 SWAA071434 1 20070315 A 5330 65C385871 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 763, STR 25L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007032800183 20070328 00183 EA 2007 3 28 CHQA200700007 1 20070310 A 7830 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER MALFUNCTIONED A CHQA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 GL 11 702BR 7462 FLIGHT 3276 - IAH-MCI - EN ROUTE AT FL310 -R REV UNLOCKED- MESSAGE APPEARED. REDUCED THRUST ON RIGHT ENGINE TO IDLE AND RAN QRH. DETERMINED REVERSER DID NOT DEPLOY. DECLARED AN EMERGENCY. APPROACH AND LANDING WERE UNEVENTFUL. MAINTENAN CE DEFERRED THRUST REVERSER. 2 L 7 2 4F RT A21EA 2007032800192 20070328 00192 NM 2007 3 28 SWAA071355 1 20070313 A 5210 6547952 SKIN BOEING 737 7373H4 1384600 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR SKIN CRACKED AT UPPER AFT CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007032800194 20070328 00194 NM 2007 3 28 SWAA071365 1 20070313 A 5310 6547978 CREASE BEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND RIGHT CREASE BEAM CORRODED AT BS 948. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2007032800195 20070328 00195 NM 2007 3 28 SWAA071363 1 20070313 A 5314 6547978 KEELBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND LEFT KEEL BEAM CORRODED BETWEEN BS 500C & BS 510. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2007032800199 20070328 00199 WP 2007 3 28 UPS07849502 1 20070220 A 5313 3779658U502 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C1 MAIN CABIN LONGERON END FITTING CRACKED STA 900 L10L. REMOVED AND REPLACED END FITTING IAW SRM 51-1- 20D AND 51-2-15. 2 L 7 4 4F RT 4A25 2007032800202 20070328 00202 EU 2007 3 28 2007UALA00793 1 20070317 A 3250 CONTROL MODULE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG STEERING MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 454UA 1104 RTFL DUE TO NW STEERING FAULT DISPLAYED ON UPPER ECAM SCREEN. REQUESTED TOW. [SUP 06-01-07] REPLACED NOSE STEERING SE RVO CONTROL MODULE. AT OVERHAUL, FOUND A CRUSHED ELECTRICAL CONNECTOR AND SIGNIFICANT CORROSION DAMAGE ON ELECTRO SELECT OR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032800213 20070328 00213 EU 2007 3 28 07FDEA00864 1 20070315 A 5730 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 BOTTOM SKIN REWORK CAUSED BY CORROSION AT RIB 8, P19, RT OUTER WING REPAIR WAS PERFORMED IAW EA 6-5721-106402 AND RAS/BA E/1004132/2007 ISS A (BLEND OUT CORROSION, FASTENER REPLACEMENT. 2 L 7 2 4F RT A35EU 2007032800216 20070328 00216 EU 2007 3 28 07FDEA00865 1 20070315 A 5320 ANGLE AIRBUS 310 A310324 3930206 EU ZONE 300 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 CORROSION BETWEEN C91 AND C92 BILGE AREA AT OUTER FLANGE C91, SOME ANGLES C92 AND AT DOUBLER P23 C92. REPAIR WAS PERFOR MED BY REMOVING CORROSION IAW SRM51-74-10 AND REPLACEMENT OF CORRODED STRUCTURE PARTS IAW SRM 51-72-10, SRM 53-19-18/FIG 9 AND SRM 5319-13/FIG 11/12. 2 L 7 2 4F RT A35EU 2007032800218 20070328 00218 NM 2007 3 28 2007UALA00805 1 20070319 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENGY LIGHT ON DOOR 4R IS INOP. REPLACED WITH SERVICEABLE DOOR 4R EMERGENCY LIGHT. OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032800223 20070328 00223 NM 2007 3 28 QXEA200700455 1 20070325 A 5230 HANDLE BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR UNSECURE A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 401QX 4031 BOI FLIGHT NR 2399: TAKEOFF ABORTED DUE TO FUSELAGE DOORS MASTER WARNING AFTER TAKEOFF POWER APPLIED. MAINTENANCE FOUND AFT CARGO DOOR HANDLE NOT SEATED CORRECTLY. CLEANED AND LUBED AFT CARGO DOOR HANDLE LOCKING MECHANISM. OPS CHECK NORM AL IAW AMM TASK 52-31-00-710-801. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032800227 20070328 00227 NM 2007 3 28 QXEA200700423 1 20070310 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 525-535 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - FOUND SEAT TRACK NR 12 HAS MINOR SCRATCHES AT STATION 525 TO 535, 548. REPAIRED IAW RD8-53-1342. 2 H 7 2 4T RT A13NM 2007032800230 20070328 00230 NM 2007 3 28 2007UALA00808 1 20070318 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 DOOR 1R EMERGENCY SLIDE LIGHT INOP. REPLACED LIGHT ASSY. TESTED GOOD FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032800244 20070328 00244 NM 2007 3 28 2007UALA00821 1 20070319 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 305UA 23666 EEL LAMP INOP ROW 15. REPLACED EEL LAMP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032800255 20070328 00255 2007 3 28 2007UALA00835 4 20070318 A 2565 SLIDE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE L1 DOOR LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 809UA 825 DOOR 1L PRESSURE IS LOW. [SUP 06-01-07] REPLACED SLIDE PACK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032900029 20070329 00029 EU 2007 3 29 07FDEA00869 1 20070315 A 5730 SKIN AIRBUS 310 A310324 3930206 EU RT WING CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND TWO DAMAGED HOLES (HOLE NR 4 RIB 17 AND HOLE NR 4 RIB 3-4) ON RT WING TOP SKIN AND CORROSION ON WING TOP SKIN. RE PAIR WAS PERFORMED IAW EA 6-5720-106356 AND RAS/BAE/1003742/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007032900032 20070329 00032 EU 2007 3 29 07FDEA00872 1 20070315 A 5280 A32313021000 ATTACH FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 LT NOSE GEAR DOOR ATTACHMENT FITTING DAMAGED. REPLACEMENT OF ATTACHMENT FITTING IAW AMM 32-31-16. 2 L 7 2 4F RT A35EU 2007032900039 20070329 00039 EU 2007 3 29 07FDEA00877 1 20070315 A 5320 A26270471 BRACKET AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND BRACKET A262-70471-200 BETWEEN CROSS BEAM C26/32 AND C33 CRACKED. BRACKET A262-70471-202 BETWEEN CROSS BEAM C33 A ND 34 CRACKED. NEW PARTS INSTALLED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007032900044 20070329 00044 NM 2007 3 29 QXEA200700386 1 20070315 A 6120 AUTOFEATHER SYS BOMBDR DHC8 DHC8402 1390042 NM NR 1 PROPELLER MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 402QX 4032 SEA FLIGHT NR 2341: PRIOR TO TAXI, AFTER BRINGING CONDITION LEVERS OUT OF START/FEATHER, NR 1 PROP WAS AT 750, NR 2 ENGI NE WAS AT 800 RPM. PRIOR TO RETURNING TO GATE AND SHUTTING DOWN ENGINES THE CREW DESELECTED THE AUTOFEATHER AND BOTH PR OPS RPM WENT TO NORMAL. MAINTENANCE INTERROGATED CDS SYSTEM FOR POSSIBLE FAULTS. FOUND CHANNEL B 797 STATUS CODE ON CH ANNEL B FOR ED. TORQUE IN MAINTENANCE MODE. CLEARED FAULTS IAW FIM TASK 73-20-00-810-889. FAULT DID NOT REAPPEAR AFTE R ENGINE RUNS. CYCLED INTO AUTOFEATHER SELECT MODE OVER 5 TIMES DURING ENGINE RUN WITH NO PROBLEMS NOTED. NO PARTS REP LACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900045 20070329 00045 2007 3 29 2007UALA00841 4 20070320 A 2565 5A29011 ASPIRATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 641UA PK0157 25091 BOTH ASPIRATORS LEAKING BETWEEN JET PLATE ASSEMBLY AND SENSING TUBE. REPLACED BOTH ASPIRATORS. SUSPECT SIDE LOAD ON AS PIRATORS DURING PACKING CAUSED LEAKS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007032900046 20070329 00046 EU 2007 3 29 07FDEA00881 1 20070315 A 5311 FRAME AIRBUS 310 A310203 3930313 EU BS 1315 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 412FE 360 FOUND CORROSION EXIST AT AVIONIC COMPARTMENT AT STA 1315/ FRAME 16 AND 17 BETWEEN S47 AND 48 BELOW ACCESS PNL 121 PF ZON E 120 COMPLIED WITH EA 6- 5330-107691. 2 L 7 2 4F RT A35EU 2007032900050 20070329 00050 EU 2007 3 29 07FDEA00885 1 20070315 A 5330 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 SCRATCHES CLOSE TO STATIC PORT C27-29, P41 RT. REPAIR WAS PERFORMED BY BLEND OUT IAW EA 6-5314-103422 AND RAS/DATLS/000 3445/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007032900057 20070329 00057 EU 2007 3 29 07FDEA00892 1 20070315 A 5347 A5327541120390 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU BS 3991-4044 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 669FE 774 MAIN CARGO DECK SEAT TRACK ADAPTER AT FR61/Y-1456 IS CRACKED REMOVED SEAT TRACK ADAPTER AT FR 61,Y-1456 REF TO A300-600 SRM 51-40-21 PARAGRAPH 7 LOCATED AND DRILLED NEW SEAT TRACK ADAPTER REF TO A300600 SRM 51-40-44 PAR 2. ALODINED, PRIMED NEW SEAT TRACK ADAPTER REF TO A300-600 SRM 51-21-10 PARA 2. INSTALLED SEAT TRACK ADAPTOR AT FR 61, Y-1456 REF TO A300- 600 SRM 51-40-21 PARA 7 PO 565656.3 MINOR REPAIR. 2 L 7 2 4F RT A35EU 2007032900060 20070329 00060 EU 2007 3 29 07FDEA00895 1 20070315 A 5730 SKIN AIRBUS 310 A310324 3930206 EU ZONE 500 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND DAMAGED HOLES ON LT WING TOP SKIN, REAR SPAR, RIB 4-5. REPAIR WAS PERFORMED BY REAMING UP HOLE 248 IAW EA 6-5720- 103430 AND RAS/BAE/1003766/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007032900065 20070329 00065 EU 2007 3 29 07FDEA00900 1 20070315 A 5310 STRUCTURE AIRBUS 310 A310324 3930206 EU ZONE 300 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CORRODED L-SECTION AT C95. REPAIR WAS PERFORMED BY FRAME CUT AND SPLICE IAW EA 6-5319-103401 AND RAS/DATLS/000341 1/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007032900066 20070329 00066 EU 2007 3 29 07FDEA00901 1 20070315 A 5711 SPAR AIRBUS 310 A310324 3930206 EU CENTER WING BOX CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 CENTER WING BOX, CRACKS IN FLANGE SPAR NR 4 RT, C44.1. REPAIR WAS PERFORMED BY CUT OUT AND MANUFACTURE AND REPAIR ANGLE IAW EA 6-5710-103404 AND RAS/047737/009/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007032900067 20070329 00067 EU 2007 3 29 07FDEA00902 1 20070315 A 5330 SKIN AIRBUS 310 A310324 3930206 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 412FE 360 AVIONICS BAY CORROSION AROUND FASTENERS FS 16 TO 17, STR 44L TO 45L REPAIRED PER EA 6-5330-107691. 2 L 7 2 4F RT A35EU 2007032900068 20070329 00068 EU 2007 3 29 07FDEA00903 1 20070315 A 5311 A53989505202 FRAME AIRBUS 310 A310324 3930206 EU ZONE 300 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CORROSION AT FRAME SECTION C102. PART REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007032900069 20070329 00069 EU 2007 3 29 07FDEA00904 1 20070315 A 5310 CROSSBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CORROSION AT CROSS BEAM C63 LT. CROSS BEAM REPAIRED IAW SRM 53-10-15, PAGE 241/242. 2 L 7 2 4F RT A35EU 2007032900070 20070329 00070 EU 2007 3 29 07FDEA00905 1 20070315 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 412FE 360 MDCC - FLOORBEAM FRAME 36 CRACKED (PREVIOUS REPAIR NOT PER SRM). REWORKED PREVIOUS REPAIR IAW EA 6-5321-29042. 2 L 7 2 4F RT A35EU 2007032900071 20070329 00071 EU 2007 3 29 07FDEA00906 1 20070315 A 5313 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CORROSION ON COUPLING BETWEEN C54.2-54.3, P51 LT AND ON STRINGER P51 LT, C54.2. REPAIR WAS PERFORMED IAW SRM 53-10 -14 AND SRM 51-72-10, STRINGER REPAIR AND COUPLING REPLACEMENT. 2 L 7 2 4F RT A35EU 2007032900074 20070329 00074 EU 2007 3 29 07FDEA00909 1 20070315 A 5313 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CORROSION AT STRINGER P56, C54.1-54.3. STRINGER REPAIR PERFORMED IAW SRM 53-10-14/FIG 201A AND NEW COUPLING INSTA LLED. 2 L 7 2 4F RT A35EU 2007032900075 20070329 00075 NM 2007 3 29 07FDEA00910 1 20070315 A 5210 DOOR BOEING 727 727233 138408A NM MAIN PAX UNSECURE A FDEA B A EMER. DESCENT UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SO 25 269FE 21675 AFTER TAKEOFF IN IAD CABIN ALTITUDE WENT ABOVE 10,00 0' RAN QRH PROCEDURES CABIN ALTITUDE WENT TO 11,500' WENT ON O2 R ETURNED TO IAD. NOTICE FORWARD ENTRY DOOR WAS NOT SEATED PROPERLY OPEN AND SECURED DOOR SEVERAL TIMES, PERFORMED FORWAR D ENTRY DOOR INSPECTION REF: M/M 52-11-001-6 CHECKED NORMAL. A/C OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2007032900076 20070329 00076 NM 2007 3 29 07FDEA00911 1 20070315 A 5730 SKIN BOEING 727 727225 1384077 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 RIGHT WING LOWER SURFACE HAS CORROSION AT NR 6 FLAP TRACK MID ATTACH POINT. ACCOMPLISHED REPAIR OF ATTACH POINT, REF EA 7-5730-107001, WRI 57309127. 2 L 7 3 4F A3WE 2007032900077 20070329 00077 NM 2007 3 29 07FDEA00912 1 20070315 A 5320 BRACKET BOEING 727 727225 1384077 NM NLG WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 NLG W/W CEILING THRU LT ACCESS PNL LT SUPPORT HAS CRACKS ON BOTH ENDS FS 259.50. REMOVED SEAT TRACK FOR ACCESS IAW SRM 51-30-2. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-30-2. REINSTALLED SEAT TRACK IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2007032900081 20070329 00081 WP 2007 3 29 07FDEA00917 1 20070315 A 5730 SKIN DOUG DC10 DC1010 3022110 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 RIGHT WING UPPER SKIN HAS SEVERAL AREAS OF SURFACE CORROSION XW118- XORS 264 (32 AREAS MARKED). REMOVED CORRODED AREAS NR 1 THRU NR 32 IAW DC10 SRM 57-10-00 FIG 59 VOL I AREAS NR 1 THRU NR 21 AND NR 23, NR 25, THRU NR 32 FOUND TO BE WITHI N LIMITS IAW DC10 SRM 57-10-00 FIG 59 VOL I AND 57-10-00 FIG 61 VOL I. AREA NR 22 STR 6 STA XORS 152, ORIG THICKNESS .2 30, MATERIAL REMOVED .027, REMAINING THICKNESS .0203 AREA NR 24 STR 24 STA XORS 139.5 ORIG THICKNESS .225, MAT. REMOVED .026, REMAINING THICKNESS .199 FOUND TO BE OUT OF LIMITS. REWORKED OUT OF LIMITS AREAS PER EA 8-5730-105174-WINGS, RT UPPER WING SKIN CORROSION AT STRG 6 XORS 139.5 AND 152 -REPAIR. 2 L 7 3 4F A22WE 2007032900083 20070329 00083 NM 2007 3 29 2007UALA00842 1 20070321 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 AFT CARGO PIT AT BS 1197+132 TO BS 1219 AT STR 36L SKIN AT LAP SPLICE & CIRCUMFERENTIAL JOINT IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED & INSTALLED REPAIR FILLER AND 3 EACH DOUBLERS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007032900084 20070329 00084 NM 2007 3 29 QXEA200700434 1 20070314 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - NR 1 DME MATING SURFACE ON THE AIRCRAFT HAS MULTIPLE GOUGES FROM PREVIOUS ANTENNA REMOVAL. REPAIRED IAW RD8-53 -9518. 2 H 7 2 4T RT A13NM 2007032900085 20070329 00085 NM 2007 3 29 2007UALA00843 1 20070321 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 DURING DEPARTURE A/C OVER-ROTATED STRIKING THE RUNWAY AT BS 1715-1787. AFT SKIN PANEL & FWD SKIN PANEL ABRAIDED 100 PER CENT AT STA 1720. STA 1720 FWD CHORD & AFT CHORD WERE ABRAIDED AT LEAST 30 PERCENT, AND THE AFT PRESSURE BULKHEAD LWR W EB WAS FOUND BUCKLED COMMON TO STA 1720 FWD & AFT CHORDS. [06-14-07] MAJOR REPAIR ACCOMPLISHED. CHORD REPAIRS 3 EA ARE PERMANENT REPAIRS, AFT SKIN REPLACEMENT WAS A PERMANENT REPAIR. FORWARD SKIN REPAIR WAS CATEGORY B INTERIM REPAIR PE R UA ENGINEERING SPECIFICATIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032900086 20070329 00086 NM 2007 3 29 QXEA200700436 1 20070314 A 2497 JUMPER DHAV DHC8 DHC8202 2809007 NM DOOT TO FUSELAGE MISINSTALLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - REWORK REQUIRED. CORROSION ON LAV PAN DOUBLER AT BONDING STRAP FUSE TO DOOR DUE TO BONDING JUMPER ATTACH POINT AT FUSE END IS NOT ATTACHED TO BRACKET AS OUTLINED IN RD8-53-3299. REPAIRED IAW RD8-53-3299. 2 H 7 2 4T RT A13NM 2007032900088 20070329 00088 NM 2007 3 29 2007UALA00844 1 20070321 A 5312 BULKHEAD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE BUCKLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 AFT PRESSURE BULKHEAD STA 1720 HAS A BUCKLE IN ITS WEB, ABOUT ONE QUARTER INCH DEFLECTION BY 18 INCHES LONG. FIVE INCHE S FROM THE BOTTOM, BETWEEN THE TWO VERTICAL BEAMS AT LBL 9.20 AND RBL 9.20 DAMAGE TO FOLLOWING AREAS: GOUGES STA 1720 S TR 29L TO OUTBOARD STR 29R DEEP GOUGE, 4 INCH CRACK STA 1743 BETWEEN STR 29L & 29R. GOUGES FROM STA 1720 TO 1780 OUTBOA RD STR 29L TO OUTBOARD OF 29R. FUS FRAME SHEAR TIE STA 1743 BENT STR 29L & 29R. [06-14-07] MAJOR REPAIR ACCOMPLISHED. CHORD REPAIRS 3 EA ARE PERMANENT REPAIRS, AFT SKIN REPLACEMENT WAS A PERMANENT REPAIR. FORWARD SKIN REPAIR WAS CATEGOR Y B INTERIM REPAIR PER UA ENGINEERING SPECIFICATIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032900090 20070329 00090 NM 2007 3 29 QXEA200700427 1 20070314 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 19061 C4 PDX - FLAP TRACK 4 ON LEFT WING HAS PITTING THE FULL LENGTH OF ROLLER TRAVEL ON TRACK E ON INBOARD SIDE. REPAIRED IA W DHC-8 AMM 27-51-11-830-801. 2 H 7 2 4T RT A13NM 2007032900097 20070329 00097 NM 2007 3 29 QXEA200700432 1 20070314 A 5340 ANGLE DHAV DHC8 DHC8202 2809007 NM WING TO FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - LEFT OUTBOARD AFT WING TO FUSELAGE CLOSING ANGLE IS CRACKED AT LAST 2 OUTBOARD HILOCKS. REPAIRED IAW RD8-53-51 92. 2 H 7 2 4T RT A13NM 2007032900101 20070329 00101 NM 2007 3 29 AALA20070512 1 20070317 A 1100 PLACARD BOEING 757 757223 1384957 NM EMERGENCY EXIT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 173AN 32399 MIA - EMERGENCY LIGHT AT FORWARD LEFT WING EXIT SIGN AT SEAT BOTTOM LEVEL HAS DIRECTIONAL DECAL FALLING OFF. REPLACED D ECAL FOR EMERGENCY LIGHT AT FORWARD LEFT WING EXIT SIGN AT SEAT BOTTOM LEVEL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007032900103 20070329 00103 NM 2007 3 29 2007UALA00848 1 20070322 A 3350 GUARD BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT OUT OF ADJUST A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EXIT LIGHTS ON RIGHT SIDE OF ACFT CAME ON INFLIGHT. LEFT SIDE STAYED OFF. UNABLE TO DUPLICATE ON GRD. TESTED LIGHTS VIA FLT DECK SWITCH AND OPS NML ON BOTH SIDES. CHECKED VIA SWITCH AT 1L ATTENDANT SEAT AND OPS NORMAL. NOTE: SW ITCH GUARD NOT POSITIONED CORRECTLY AND MAY HAVE CAUSED PARTIAL ACTIVATION BY ATTENDANT LEANING ON SEAT IN AREA OF SWITC H. THIS PARTIAL ACTIVATION HAS OCCURRED PREVIOUSLY ON OTHER A/C. GUARD REPOSITIONED. NO REPEAT OCCURRENCE AFTER RETURN TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032900108 20070329 00108 NM 2007 3 29 QXEA200700456 1 20070307 A 5412 FIREWALL DHAV DHC8 DHC8202 2809007 NM NR 2 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 C4 OKC - NR 2 NACELLE AFT FIREWALL CRACKED, OUTBOARD SIDE AT EXHAUST ATTACH FLANGE JUST ABOVE FIRE LOOP BRACKET. REPAIR ED IAW RD8-54-806. 2 H 7 2 4T RT A13NM 2007032900113 20070329 00113 NM 2007 3 29 AALA20070513 1 20070319 A 3350 233T321042 CONTROL PANEL BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA O OTHER O OTHER CR CRUISE 1 SW 21 687AA 25695 OVERHEAD EMERGENCY EXIT LIGHTS AND OVERWING EMERGENCY EXIT LIGHTS IN COACH CABIN ILLUMINATED FOR APPROXIMATELY ONE HOUR AND THEN WENT OFF. REPLACED EMERGENCY LIGHTS OVERHEAD PANEL IN COCKPIT AND FLIGHT ATTENDANT PANEL SWITCH. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007032900114 20070329 00114 NM 2007 3 29 AALA20070507 1 20070315 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 697AN 26977 DFW - EMERGENCY LIGHT AT RIGHT AFT SERVICE DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT AFT SERVICE DOOR. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007032900117 20070329 00117 NM 2007 3 29 AALA20070506 1 20070315 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 697AN 26977 DFW - EMERGENCY LIGHT AT SEAT ROW 24D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT ROW 24D. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A2NM 2007032900118 20070329 00118 NM 2007 3 29 NWAA071045511 1 20070314 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 511US 23199 DURING MAINTENANCE LINE CHECK, ALL FLOOR PROXIMITY LIGHTS ILLUMINATE DIM WHEN EMERGENCY LIGHTS ARE SELECTED OFF. REPLAC ED EMERGENCY LIGHT POWER SUPPLIES PER B757 MM 33-51-07. LIGHTS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007032900120 20070329 00120 EU 2007 3 29 NWAA071053214 1 20070314 A 2120 UNKNOWN AIRBUS 320 A320211 3930320 EU UNKNOWN ODOR A NWAA A UNSCHED LANDING B N SMOKE/FUMES/ODORS/SPARKS FALSE WARNING CR CRUISE 1 GL 01 314US 160 CRUISE FLIGHT 380, FLIGHT CREW DETECTED FOUL ODOR, NOTICED FWD AND AFT CARGO FIRE EXTINGUISHING DISCHARGE LIGHTS BOTH IL LUMINATED, WITH NO ASSOCIATED INDICATIONS. NO SMOKE WAS DETECTED IN CABIN, ODOR WAS REPORTED BY FLIGHT ATTENDANT. FLIG HT DIVERTED INTO TLH, LANDING UNEVENTFULLY. REPLACED ELECTRICAL CONNECTORS 1154VCA AND 1156VCA, REPLACED LAVATORY EXTRA CT FAN 32-2120-9-0021 AND CABIN RECIRCULATION FAN 32-2120-9-0021 (L/P 3976012, 3976018). 2 L 7 2 4F RT A28NM 2007032900121 20070329 00121 NM 2007 3 29 AWXA200700367 1 20070315 A 5310 652072354 DOOR FRAME BOEING 737 7373S3 1384711 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - FOUND FORWARD CARGO COMPARTMENT DOOR CUT OUT FORWARD FRAME CRACKED, BS 492, S24R - S25R, AT THE LOWER DOOR STOP FI TTING. REPAIRED FORWARD CARGO COMPARTMENT DOOR CUT OUT FORWARD FRAME, BS 492, S24R - S25R, AT THE LOWER DOOR STOP FITTI NG IAW AWA ER 03-5331-07073-ES3. 2 L 7 2 4F RT A16WE 2007032900122 20070329 00122 NM 2007 3 29 AWXA200700368 1 20070213 A 5311 65458076 FRAME BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MCN - R1 DOOR CUT OUT FORWARD UPPER STUB FRAME CRACKED, BS 297.5, RBL 47, WL 269.06 AT THE TOP STOP PAD FITTING. REPLAC ED R1 DOOR CUT OUT FORWARD UPPER STUB FRAME, BS 297.5, RBL 47, WL 269.06 AT THE TOP STOP PAD FITTING IAW B737-300 SRM 51 -40-02. 2 L 7 2 4F RT A16WE 2007032900127 20070329 00127 NM 2007 3 29 2007UALA00853 1 20070319 A 5310 UNKNOWN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE VIBRATION A UALA O OTHER E VIBRATION/BUFFET AP APPROACH 1 WP 29 924UA 26645 EXCESSIVE VIBRATION ON APPROACH FLAPS 5. FOUND E&E DOOR SEAL DAMAGED AT TWO PLACES AND FREEPLAY AT ELEV TRIM TAB IS OU T OF LIMITS. REPLACED E&E DOOR SEAL AND REPLACED THE FLANGED BUSHINGS ON ELEVATOR FITTING FOR TAB ATTACH HINGE AT POSIT IONS NR 1, 3, AND 4. ACCOMPLISHED FREE PLAY CHECK NO FURTHER VIBRATIONS NOTED ON SUBSEQUENT FLIGHTS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032900129 20070329 00129 NE 2007 3 29 2007UALA00855 2 20070321 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 HUNG START A UALA E ENGINE SHUTDOWN M OVER TEMP NR NOT REPORTED 1 WP 29 453UA 1001 V10110 NR 2 ENG HAD A OVERTEMP. EGT WAS 738C ON ECAM. N1 6-7%, N2 41-42%. ENG APPEARED TO HAVE A HUNG START AND WAS OVER 635 C FOR APPROX 6-8 SECONDS BEFORE SHUTTING DOWN. [06-14-07] REPLACED NR 2 ENGINE DUE TO POSSIBLE DAMAGE TO TURBINES AND DOWNSTREAM ITEMS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032900131 20070329 00131 2007 3 29 2007UALA00857 4 20070322 A 2565 D31039201 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE UNDERSERVICED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 542UA 25276 LOW PRESSURE ON CYLINDER. [SUP 05-16-07] BOTTLE WAS UNDERFILLED. FILLED BOTTLE TO SPECIFICATIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032900132 20070329 00132 2007 3 29 2007UALA00858 4 20070323 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR DISCHARGED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 426UA 510 SLIDE DISCHARGED 1L. [SUP 06-01-07] REPLACED DOOR 1L SLIDE AND ASSIST MECHANISM SEALING DIAPHRAGM. FILLED ASSIST BOTTL E TO PROPER PRESSURE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032900133 20070329 00133 NM 2007 3 29 2007UALA00859 1 20070322 A 5320 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 STA 727E STR 23L-24L IS DAMAGED. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACK DAMAGE. INSTALLED DOUBLER/TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032900134 20070329 00134 NM 2007 3 29 2007UALA00860 1 20070322 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 LOWER FUSELAGE BS 827 STR 25L FRAME GOUGED ON UPPER FWD RADIUS. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE & INSTALLED STRAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032900135 20070329 00135 NM 2007 3 29 AWXA200700371 1 20070308 A 5312 651758243 VERTICAL BEAM BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED VERTICLE BEAM WEB, BS 178, RBL 17.1, WL 240. REPAIRED VERTICLE BEAM WEB, BS 178, RBL 17.1, WL 240 I AW B737-300 SRM 53-10-08 FIGURE 201. 2 L 7 2 4F RT A16WE 2007032900136 20070329 00136 NM 2007 3 29 2007UALA00861 1 20070322 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 AFT CARGO COMPARTMENT STA 727D AT STR 23L STRINGER CLIP IS CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED STRI NGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032900137 20070329 00137 NM 2007 3 29 AWXA200700372 1 20070309 A 5320 69353654 SUPPORT ANGLE BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED MAIN CABIN SUPPORT ANGLE, BS 380 - BS 400, BL 0, WL 208.1. REPLACED MAIN CABIN SUPPORT ANGLE, BS 38 0 - BS 400, BL 0, WL 208.1 IAW B737-300 SRM 51-40-02 AND 51-40-05. 2 L 7 2 4F RT A16WE 2007032900138 20070329 00138 NM 2007 3 29 AWXA200700373 1 20070305 A 5754 65C26602107 SKIN BOEING 737 7373G7 1384595 NM ZONE 500 DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND LEFT WING NR 2 SLAT WEDGE UPPER SURFACE DEBONDED, SS 223. REPAIRED LEFT WING NR 2 SLAT WEDGE UPPER SURFACE, SS 220.9 - SS 225.9, IAW B737-300 SRM 51-70-10-2R, FIGURE 203. 2 L 7 2 4F RT A16WE 2007032900139 20070329 00139 NM 2007 3 29 AWXA200700374 1 20070308 A 5312 651758243 VERTICAL BEAM BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED VERTICAL WEB, BS 178, LBL 17.1, WL 230. REPAIRED VERTICAL WEB, BS 178, LBL 17.1, WL 230 IAW B737-30 0 SRM 53-10-08 FIGURE 201. 2 L 7 2 4F RT A16WE 2007032900141 20070329 00141 NM 2007 3 29 AWXA200700375 1 20070308 A 5312 65175829 BULKHEAD BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED VERTICAL WEB, BS 178, RBL 5.7, WL 180. REPAIRED VERTICAL WEB, BS 178, RBL 5.7, WL 180 IAW B737-300 SRM 53-10-08 FIGURE 201. 2 L 7 2 4F RT A16WE 2007032900144 20070329 00144 NM 2007 3 29 2007UALA00865 1 20070323 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY EEL LIGHT INOP AT SEAT 23 LEFT AFT. REPLACED LAMP. EEL OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032900145 20070329 00145 NM 2007 3 29 2007UALA00866 1 20070323 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY EEL LIGHT INOP AT SEAT 34 RIGHT. SECURED LOOSE CONNECTOR. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032900148 20070329 00148 NM 2007 3 29 2007UALA00868 1 20070322 A 5210 CHAIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR MISROUTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 596UA 28749 MED 1LH HARNESS LATCH CHAIN MISROUTED OVER HARNESS FITTING. [06-14-07] ACCOMP'D ROUTINE JC'S TO RESTORE DOOR AND SLID E TO NORMAL SAFE CONDITION. REROUTED CHAIN TO CORRECT POSITION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032900153 20070329 00153 2007 3 29 2007UALA00871 4 20070321 A 2565 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 DOOR 1L SLIDE PACK FELL OUT OF HOUSING UPON OPENING OF DOOR INTACT. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032900154 20070329 00154 SO 2007 3 29 C2XA07TY014 1 20070321 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16561 145610 RIGHT FUSELAGE SKIN CRACKED AROUND RIVET AT FR 79, STR 6R. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER. ALODINE PRIME D AND PAINTED IAW EC5330-01676. AIRCRAFT IS STILL IN MOD LINE MAINTENANCE. 2 L 7 2 4T RT T00011AT 2007032900158 20070329 00158 WP 2007 3 29 070075 1 20070324 A 2410 696233B CSD DOUG DC9 DC987 3022087 WP LT GENERATOR UNSERVICEABLE A WX0A H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CR CRUISE 1 WP 19 945MA 49725 FLIGHT 842 GSP/PIE - THE FLIGHT CREW REPORTED THAT THE LT GENERATOR FREQUENCY WENT TO 0 [ZERO]. LEFT CSD OIL OUTLET TEM PERATURE ROSE RAPIDLY. DISCONNECTED LEFT CSD AT [OIL TEMPERATURE] REDLINE PER QRH. THE AIRPLANE COMPLETED THE FLIGHT W ITHOUT FURTHER INCIDENT. A "CRUISE" FLIGHT PHASE IS ASSUMED IN THE ABSENCE OF A FLIGHT CREW STATEMENT. ST. PETERSBURG MAINTENANCE PLACARDED THE LEFT GENERATOR SYSTEM INOPERATIVE IN ACCORDANCE WITH MEL 24-1-1 AND COMPLIED WITH THE 'M' PROC EDURE. ON 25 MARCH, 2007, ST. PETERSBURG MAINTENANCE REMOVED AND REPLACED THE LEFT CSD. SATISFACTORY OPERATIONAL AND L EAK CHECKS WERE ACCOMPLISHED PER AMM 24-10-01. THE MEL WAS CLEARED PER COMPANY PROCEDURES, THE PLACARDS WERE REMOVED AN 2 L 7 2 4F RT A6WE 2007032900160 20070329 00160 NM 2007 3 29 DHL2007750002 1 20070112 A 7500 652245113 DUCT BOEING 727 7272M7 138407S NM ENGINE LEAKING A DHLA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 750DH 21951 NR 1 FIRE HANDLE INTERMITTENTLY GOES OFF AFTER TAKEOFF. FOUND SIX STAGE DUCT LEAKING AT FIREWALL ABOVE FIRELOOP REMOVED AND REPLACED DEFECTIVE DUCTING IAW B727 M/M 36-00-01. PERFORMED ENG RUN NO LEAKS NOTED IAW ASTAR JRHCHPT 7. REMOVED A ND REPLACED FIRE LOOP DETECTION. 2 L 7 3 4F A3WE 2007032900162 20070329 00162 NM 2007 3 29 AALA20070481 1 20070312 A 3350 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9412W 53187 DFW - FOUND EMERGENCY LIGHT AT OVERWING INOPERATIVE. REPLACED BATTERY PACK AT B5 125 FOR EMERGENCY LIGHT AT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2007032900167 20070329 00167 NM 2007 3 29 AALA20070493 1 20070313 A 3350 PBS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST CR CRUISE 1 SW 21 399AN 29606 LAX - EMERGENCY LIGHTS AT CEILING AND FLOOR AT LEFT AISLE SEAT ROWS 30 TO AFT OF CABIN INTERMITTENTLY ON AND OFF THROUGH OUT FLIGHT. LANDED LAX WITHOUT INCIDENT. REPLACED BATTERY PACK AND CHARGER AT SEAT 39AB FOR EMERGENCY LIGHTS AT CEILI NG AND FLOOR AT LEFT AISLE SEAT ROWS 30 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007032900168 20070329 00168 NM 2007 3 29 AALA20070494 1 20070313 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 343AN 33082 SFO - EMERGENCY LIGHT AT SEAT 25H CEILING INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 25H CEILING. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007032900171 20070329 00171 NM 2007 3 29 AALA20070496 1 20070313 A 3350 P4010049 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 325AA 22326 JFK - SEAT MOUNTED EMERGENCY LIGHTS ON RIGHT SIDE OF FIRST CLASS AND BACK TO HALF OF BUSINESS CLASS INOPERATIVE. REPLAC ED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS ON RIGHT SIDE OF FIRST CLASS AND BACK TO HALF OF BUSINESS CLASS. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007032900172 20070329 00172 NM 2007 3 29 AALA20070477 1 20070312 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 779AN 29955 DFW - OVERHEAD EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR INOPERATIVE. RELAMPED OVERHEAD EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032900173 20070329 00173 NM 2007 3 29 AALA20070479 1 20070312 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 619AA 24577 MIA - EMERGENCY LIGHT AT FORWARD OVERWING INOPERATIVE. RELAMPED EMERGENCY LIGHT AT FORWARD OVERWING. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007032900174 20070329 00174 NM 2007 3 29 AALA20070487 1 20070313 A 3350 0202365001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 783AN 30004 LHR EMERGENCY LIGHT AT FIRST CLASS CLOSET AREA NEAR LEFT NUMBER ONE DOOR HAS MISSING LENS. REPLACED LIGHT ASSEMBLY AT F IRST CLASS CLOSET AREA NEAR LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032900175 20070329 00175 NM 2007 3 29 AALA20070498 1 20070313 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 695AN 26975 DFW - EMERGENCY LIGHT AT SEAT 12D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007032900178 20070329 00178 NM 2007 3 29 DHL2007762501 1 20070323 A 5310 TORQUE BOX BOEING 727 7272B7 138407L NM AIRSTAIRS GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 762AT 22162 LEFT AFT AIR STAIRS TORQUE BOX LIGHTING HOLE GOUGED BS 1320. ROUTED OUT GOUGED AREA, MATERIAL LOSS .008 IAW B727 SRM 53 -30-1 FIG 1. FAB REPAIR DOUBLER 4" BY 2.5" BY .050, 7075T6 IAW B727 SRM 53-10-2 FIG 6 AND 51-40-1, FIG 1. TREATED ALOD INE AND PRIMED IAW B727 SRM 52-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM 51-40-2. 2 L 7 3 4F A3WE 2007032900179 20070329 00179 NM 2007 3 29 DHL2007762502 1 20070323 A 5320 7075T6 SUPPORT ANGLE BOEING 727 7272B7 138407L NM AIR STAIR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 762AT 22162 FOUND CRACK IN LT AFT AIR STAIRS TORQUE BOX ON UPPER WEB SUPPORT ANGLE, APPROX BS 1253. MADE TWO EACH CUT OUTS FOR ACCE SS, 4 BY 4 AT UPPER WEB IAW B727 SRM 51-10-1. REMOVED CRACKED SUPPORT ANGLE IAW B727 SRM 51-30-2. FABRICATED NEW SUPPO RT ANGLE USING 7075T6, .040 BY 29.25 BY 4.5 IAW B727 SRM 53-10-2 FIG 6 AND 51-20-1 FIG 7. FABRICATED ACCESS COVERS FROM 7075T6, 4 DIA BY .040 IAW B727 SRM 51-20-1. FABRICATED SPLICE RING FROM 7075T6, 6 DIA BY .050” IAW B727 SRM 51-20-1. ALODINE AND PRIMED SUPPORT ANGLE AND ALL REPAIR PARTS IAW B727 SRM 52-10-2. INSTALLED NEW SUPPORT ANGLE IAW B727 SRM 51 -30-2. INSTALLED REPAIR DOUBLER AND ACCESS COVERS AT BS 1250 LBL 45.5 AND BS 1267 LBL 45.5 IAW B727 SRM 51-20-2 AND 51- 2 L 7 3 4F A3WE 2007032900180 20070329 00180 NM 2007 3 29 QXEA200700366 1 20070311 A 3620 8209074 SWITCH BOMBDR DHC8 DHC8402 1390042 NM RT BLEED SYS MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 421QX 4149 OAK/SUN FLIGHT NR 2409: DURING LEVEL CRUISE FLIGHT AT 25,000 FT, NR 2 BLEED HOT CAUTION ILLUMINATED AND REMAINED ILLUMIN ATED WITH NR 2 BLEED SWITCH OFF FOR DURATION. FLIGHT DIVERTED TO BOI. MAINTENANCE FOUND CDS MESSAGE B BLD ANA OT. REM OVED AND REPLACED RIGHT BLEED OVER TEMP SWITCH AND RIGHT PRECOOLER TEMP SWITCH (P/N 820907-5). REF Q400 FIM 36-11-16-81 0-802 PARA 1 THROUGH 4A, STEPS (1) AND (2) AND PARA 5. NO CDS FAULTS. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900181 20070329 00181 NM 2007 3 29 AALA20070483 1 20070312 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 786AN 30250 DFW - EMERGENCY LIGHT AT SEAT 22C HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032900182 20070329 00182 2007 3 29 QXEA200700442 2 20070322 A 7260 CARBON SEAL DHAV DHC8 DHC8202 2809007 NM OIL BREATHER UNKNOWN A QXEA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 NM 09 366PH 510 PDX FLIGHT NR 2156 EN ROUTE EUG TO SEA, JUST PASSING PDX, CAPTAIN AND FO SMELLED SMOKE, FLIGHT ATTENDANT MENTIONED HAZE IN THE CABIN, ESPECIALLY NEAR THE REAR OF THE AIRCRAFT. RAN APPROPRIATE CHECKLIST. BLEED NR 1 ON AND BLEED NR 2 OFF SE EMED TO CLEAR SMOKE. NORMAL LANDING. FIRST SMELLED SMOKE AT 22,000 FEET. MAINTENANCE REPLACED THE NR 2 OIL BREATHER T UBE CARBON SEAL. OPERATIONAL CHECK FLIGHT GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900183 20070329 00183 2007 3 29 QXEA200700443 4 20070321 A 2350 HANDSET DHAV DHC8 DHC8202 2809007 NM INTERCOM INOPERATIVE A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 361PH 516 PDX FLIGHT NR 2227 - FA UNABLE TO HEAR COMMUNICATION FROM FLIGHT DECK. CAPTAIN AND FO PA WORK OK. FLIGHT DECK ABLE TO HEAR FA. MAINTENANCE REPLACED FA HANDLE ASSEMBLY. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900188 20070329 00188 NM 2007 3 29 AALA20070499 1 20070314 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7375A 25202 DFW - EMERGENCY SEAT MOUNTED LIGHTS AT SEAT 23AB IS DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY SEAT MOUNTED LIGHTS AT SEAT 23AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007032900189 20070329 00189 NM 2007 3 29 AALA20070500 1 20070314 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7375A 25202 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23AB INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007032900190 20070329 00190 WP 2007 3 29 AALA20070502 1 20070315 A 3230 HANDLE DOUG DC9 DC982 3022082 WP MLG BYPASS PULLED A AALA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 SW 21 291AA 49303 MCO - LANDING GEAR WOULD NOT RETRACT. RETURNED TO MCO AND LANDED WITHOUT INCIDENT. FOUND MAIN LANDING GEAR DOOR BYPASS LEVER PULLED. STOWED HANDLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007032900191 20070329 00191 NM 2007 3 29 AALA20070488 1 20070313 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39356 24037 MIA - EMERGENCY LIGHT AT OVERHEAD AISLE AT SEAT 17F INOPERATIVE. RELAMPED EMERGENCY LIGHT AT OVERHEAD AISLE AT SEAT 17F . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007032900194 20070329 00194 EU 2007 3 29 AALA20070492 1 20070313 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4605R 3930308 EU LAVATORY INOPERATIVE A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 21 70079 619 SMOKE DETECTOR ALARM SOUNDED IN AFT LAVATORY AFTER TAKEOFF AND A STRONG ODOR PRESENT UNTIL LEFT PACK TURNED OFF. FOUND LAVATORY SMOKE DETECTOR DEFECTIVE. REPLACED AFT LAVATORY SMOKE DETECTOR AND ACCOMPLISHED PACK BURN. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007032900195 20070329 00195 NM 2007 3 29 AALA20070478 1 20070312 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 619AA 24577 MIA - EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007032900197 20070329 00197 WP 2007 3 29 AALA20070491 1 20070313 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 570AA 49352 SFO - EMERGENCY LIGHT AT SEAT 4E INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 4E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007032900201 20070329 00201 NM 2007 3 29 QXEA200700439 1 20070318 A 3230 NAS77B11040P BUSHING BOMBDR DHC8 DHC8402 1390042 NM MLG WORN A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 400QX 4030 RDD FLIGHT NR 2310: LEFT AND RIGHT MAIN LANDING GEAR AMBER DOORS AND LEFT RED GEAR UNSAFE LIGHT ILLUMINATED IN CRUISE FO R 2 SECONDS. FELT GEAR BEGIN TO CYCLE AND THEN RETRACT AND LIGHT WENT OUT. THEN THE DOOR AMBER LIGHT CONTINUED TO CYCL E AT 2 SECOND INTERVALS. AIRCRAFT LANDED WITHOUT INCIDENT AND WAS FERRIED TO PDX. MAINTENANCE PERFORMED THE FOLLOWING: LT AFT MLG DOOR MECHANISM WORN PARTS WERE REMOVED AND REPLACED. REF DHC-8 400 AMM TASKS 32-31-31-000-801 AND 32-31-31- 400-801. PERFORMED OPS CHECK OF THE MLG EXTENSION/RETRACTION. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900204 20070329 00204 EA 2007 3 29 REXA200700049 1 20070316 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A REXA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 25 8923A 7923 FLAPS FAILED AT ZERO ON APPROACH. QRH FOLLOWED UNEVENTFUL ZERO FLAP LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH P ER AD 2006-12-21 2 L 7 2 4F RT A21EA 2007032900206 20070329 00206 SO 2007 3 29 KY7A003 1 20070313 A 5340 BRACKET PIPER PA31 PA31350 7103110 SO BULKHEAD LOOSE E KY7A K NONE O OTHER IN INSP/MAINT 1 NM 03 411BJ 317952043 DURING INSPECTION WHILE MOVING ELEVATOR MANUALLY AT THE TAIL, A NOISE WAS HEARD NEAR THE CENTER ELEVATOR HINGE. THE NOI SE WAS FROM THE MOVEMENT OF THE BULKHEAD P/N 40638.00 AT FS 352 RELATIVE TO THE SUPPORTING BRACKETS P/N 40646-00 AND 406 46-01 DUE TO POPPED RIVETS SECURING THE BRACKETS TO THE BULKHEAD. 1 L 7 2 3O A20SO 2007032900210 20070329 00210 SO 2007 3 29 FDKA200701035 1 20070130 A 2133 2097K021100 OUTFLOW VALVE EMB 145 EMB145LR 3260212 SO CABIN PRESSURE MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 853MJ 10954 145464 FDM 6004 ATL-LIT (2026 PHX LCL). AIRCRAFT WOULD NOT PRESSURIZE. MX REMOVED AND REPLACED OUT FLOW VALVE AND PRESSURE CO NTROLLER. 2 L 7 2 4T RT T00011AT 2007032800058 20070328 00058 NM 2007 3 28 KCSA071082 1 20070326 A 5315 STIFFENER BOEING 747 747236B 1384804 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 AFT PIT, BS 1800, RBL 10 FLOORBEAM VERTICAL SUPPORT CRACKED 2 INCHES BELOW UPPER CAP. 2 L 7 4 4F A20WE 2007032800059 20070328 00059 NM 2007 3 28 KCSA071083 1 20070326 A 5315 STIFFENER BOEING 747 747236B 1384804 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 AFT PIT, BS 1800, RBL 4, FLOORBEAM VERTICAL SUPPORT CRACKED 2 INCHES BELOW UPPER CAP. 2 L 7 4 4F A20WE 2007032800071 20070328 00071 NM 2007 3 28 USAA070242 1 20070327 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 STA 727D - 727G RT SIDE OF CARGO COMPARTMENT HAS CORROSION. INSTALLED FAB'D REPAIR PARTS PER SRM 53-60-53; CORR TASK C5 3-107-02; LEVEL 2, DEFECT SIZE: 80 INCHES AREA. 2 L 7 2 4F RT A16WE 2007032800096 20070328 00096 SO 2007 3 28 RAIA00703051 1 20070320 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 807HK 145119 PRE FLT NR 3535 - RIC - EMERGENCY LIGHT NR 1 ON PAX DOOR INOP. MAINTENANCE DEFERRED EMERGENCY AIRSTAIR LIGHT PER MEL. 2 L 7 2 4F RT T00011AT 2007032800101 20070328 00101 SO 2007 3 28 RAIA00703048 1 20070320 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 845HK 14500842 POST FLT NR 7914 - IAD - EMERGENCY LIGHT STRIP NEAR GALLEY INOP. MAINTENANCE SECURED EMERGENCY EXIT LIGHT STRIP, OPS CH ECK GOOD. 2 L 7 2 4T RT T00011AT 2007032800105 20070328 00105 NE 2007 3 28 C8GA20070004 2 20070320 A 7260 717000 GEARBOX BOEING 727 727223 1384074 NM PWA JT8 JT8D9A 52048 NE NR 2 LEAKING A C8GA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 29 708AA 63646 22465 656951 FLT 715 FROM HRL TO MEM. DURING CRUISE OPERATION NR 2 LOW OIL PSI LIGHT ILLUMINATED FOLLOWED BY A DECREASE IN OIL PSI AN D OIL QUANTITY. PERFORMED APPROPRIATE CHECKLIST AND SHUT DOWN NR 2 ENGINE. AIRCRAFT DIVERTED TO IAH WHERE IT LANDED WI THOUT INCIDENT. POST FLIGHT INSP REVEALED HEIL COILS PULLED FROM GEARBOX ON OIL RETURN LINE. REMOVED AND REPLACED GEAR BOX PERFORMED, OPS AND LEAK CHECKS, NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2007032800106 20070328 00106 NM 2007 3 28 07FDEA01087 1 20070322 A 5320 NCA6046115 STIFFENER DOUG MD11 MD11F 3023600 NM ZONE 700 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 WITH REFERENCE TO SNRM N01285: LEFT NOSE LANDING GEAR OLD FITTING ASSEMBLY FOUND WITH EXISTING FREEZE PLUG. EXISTING FR EEZE PLUG ON NOSE LANDING GEAR LEFT FITTING ASSEMBLY STA 579. REMOVED AND NEW BUSHING INSTALLED AS PER FEDEX EA NR 1-53 40-106606, TITLE: FUSELAGE ATTACH FITTINGS, LEFT NOSE LANDING GEAR TRUNNION FITTING (ACA7017-501)/STRUCTURE BUSHING/ PLUG REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007032800107 20070328 00107 NM 2007 3 28 07FDEA01090 1 20070322 A 5330 6518386 SKIN BOEING 727 727225 1384077 NM BS 1148-1166 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 463FE 22551 FOUND EXTERNAL FUSELAGE REPAIR AT APPROX STA 1148-1166, STR 29L-29R. REPAIR REQUIRED EVALUATION FOR MAJOR/MINOR DETER MINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. DOUBLER HAS NUMEROUS AD RIVETS WHICH WERE REPLACED W ITH D RIVETS TO CONFORM TO SRM 53-30-3 FIG 3. A MINOR REWORK TO A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007032800125 20070328 00125 NM 2007 3 28 SWAA071553 1 20070322 A 3350 BR20123 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 437WN 29832 EEPLS INOP AT FWD END. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007032800161 20070328 00161 NM 2007 3 28 BB07028 1 20070322 A 3350 TERMINAL BOEING 767 7672B7 1385107 NM CABIN LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 255AY 25257 MAINTENANCE FOUND FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE AT ROWS 1G-4G. SECURED TERMINALS AT LIGHT ASSEMBLY 3G. NO F URTHER FAULTS. 2 L 7 2 4F RT A1NM 2007032800170 20070328 00170 NM 2007 3 28 P5CA0701513 1 20070307 A 2740 160200103 CONTROL MODULE BOEING 747 74746NF 13848BT NM HORIZ STAB FAILED A P5CA K NONE F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 EA 15 454PA 30812 DUAL SRM FAILURE: CMC MSGS 27201 AND 27001. REPLACED RIGHT STAB TRIM CONTROL MODULE PER MM 27-41-04. 2 L 7 4 4F RT A20WE 2007032800172 20070328 00172 2007 3 28 SWAA071339 4 20070312 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2007032800225 20070328 00225 NM 2007 3 28 QXEA200700426 1 20070314 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - DENT ON LEFT SIDE JUST AFT OF ICE SHIELD BETWEEN STRINGER 13 AND 14. DENT IS 1" IN DIAMETER AND .07" DEEP. DE NT IS TO BE REPAIRED AT NEXT C CHECK. REPAIRED IAW RD8-53-9511. 2 H 7 2 4T RT A13NM 2007032800228 20070328 00228 NM 2007 3 28 2007UALA00806 1 20070318 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY CEILING LIGHT AT ROW 4 RIGHT INOP. RELAMPED. OP CHECKED GOOD FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032800238 20070328 00238 NM 2007 3 28 2007UALA00816 1 20070317 A 3350 1317 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 782UA 26948 EMERGENCY SEAT LIGHT OUT AT 1E. *S/D* RELAMPED, EEL SYSTEM TESTED GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007032800246 20070328 00246 NM 2007 3 28 2007UALA00823 1 20070319 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 774UA 26936 AFT EMERGENCY LIGHT INOP AT SEATS 1E & 2E. REPLACED LAMP IN AFT EMERGENCY LIGHTS AT SEATS 1E & 2E. OP CHECKS NORMALLY . 2 L 7 2 4F 4 F RT T0001SE E46NE 2007032900005 20070329 00005 NM 2007 3 29 QXEA200700417 1 20070311 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 542-597 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 DX - LEFT INBOARD SEAT TRACK NR 6 CORRODED AT STATION 542.0, 545.0, 565.0, 597.0. REPAIRED IAW RD8-53-4936, SRM 51-2 0-16, 51-20-36, AND 51-40-11. 2 H 7 2 4T RT A13NM 2007032900011 20070329 00011 NM 2007 3 29 QXEA200700466 1 20070327 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY MALFUNCTIONED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 352PH 1338 494 SMOKE WARNING LIGHT CAME ON DURING TAKEOFF. THE LIGHT CAME ON AND OFF AND CONTINUED TO BE INTERMITTENT. MAINTENANCE RE MOVED NR 1 SMOKE DETECTOR IN BAGGAGE COMPARTMENT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900022 20070329 00022 NM 2007 3 29 QXEA200700451 1 20070324 A 3620 8209074 SWITCH BOMBDR DHC8 DHC8402 1390042 NM BLEED SYS MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 418QX 13920 13920 4143 BOI FLIGHT NR 2320: NR 1 BLEED HOT CAUTION LIGHT ON AFTER START UP. TURNED OFF BLEED SWITCH PER CHECKLIST AND CAUTION L IGHT STAYED ON. MAINTENANCE REPLACED NR 1 PRECOOLER TEMP SWITCH IAW AMM TASK 36-11-11-000-801 AND 36-11-11-400-801 AND NR 1 BLEED OVER TEMP SWITCH IAW AMM TASK 36-11-16-000-801 AND 36-11-16-400-801. GROUND RAN AIRCRAFT AT VARIOUS POWER SE TTINGS AND BLEED SETTINGS FOR 30 MINUTES. NO BLEED CAUTIONS. CHECKED CDS FOR ECS FAULTS. NO FAULTS NOTED. AIRCRAFT R ETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900024 20070329 00024 NM 2007 3 29 QXEA200700370 1 20070311 A 2720 RUDDER PEDAL BOMBDR DHC8 DHC8402 1390042 NM COCKPIT FOD A QXEA D RETURN TO BLOCK C F.O.D. TX TAXI/GRND HDL 1 NM 09 417QX 4086 SEA FLIGHT NR 2426: NOTICED RUBBING NOISE WITH RUDDER PEDAL MOVEMENT DURING CONTROL CHECK. MAINTENANCE FOUND A PIECE OF RAW ALUMINUM STOCK ON LT SIDE OF CAPTAIN'S RUDDER PEDALS. REMOVED RAW ALUMINUM STOCK PIECE FROM CAPTAIN'S RUDDER PEDAL S. PERFORMED MOVEMENT CHECK OF CAPTAIN'S RUDDER PEDALS. NOSE GONE AND COMPLETE FREEDOM OF MOVEMENT. OPS CHECK GOOD. GVI SHOWS NO FURTHER DEFECTS. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900040 20070329 00040 EU 2007 3 29 07FDEA00878 1 20070315 A 5310 A53978476202 CROSSBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CROSSBEAM C62 RT CORRODED. REPAIR WAS PERFORMED BY REPLACEMENT OF CROSS BEAM IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007032900047 20070329 00047 WP 2007 3 29 07FDEA00882 1 20070315 A 5347 SEAT TRACK DOUG MD10 MD1010F 3022112 WP BS 908-949 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 566FE 46989 FOUND UPPER FUSELAGE CABIN SEAT TRACK AT LBL 47 STA 910 GOUGED. REMOVED DAMAGED SEAT TRACK SECTION AND INSTALLED NEW SE AT TRACK SECTION FROM STA 908 TO STA 949, LBL 47 IAW DC10/MD10 SRM 53-70-00 FIG 1 VOL 1, AND D RW SP10510179 REV D ZONE F-8. 2 L 7 3 4F RT A22WE 2007032900056 20070329 00056 EU 2007 3 29 07FDEA00891 1 20070315 A 5330 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 SCRATCHES ON SKIN AT C33-34, P54 RT TO P54 LT. REPAIR WAS PERFORMED BY INSTALLING AN EXTERNAL DOUBLER IAW EA 6-5314-103 373 AND RAS/DABRE/7007106/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007032900063 20070329 00063 EU 2007 3 29 07FDEA00898 1 20070315 A 5313 A53986219 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 DEFORMATION OF STRINGER AT C65, P38 LT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007032900073 20070329 00073 EU 2007 3 29 07FDEA00908 1 20070315 A 5330 SKIN AIRBUS 310 A310324 3930206 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 412FE 360 AVIONICS BAY, CORROSION BELOW FRAME 17 AT STR 44L REPAIRED IAW EA 6-5330-107691. 2 L 7 2 4F RT A35EU 2007032900080 20070329 00080 NM 2007 3 29 07FDEA00916 1 20070315 A 5315 651759325 FLOORBEAM BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FLIGHT DECK FLOOR SUPPORT CHANNEL IS CRACKED ON TOP OF CHANNEL LOCATED AT BS 285, LBL 6.5. INSTALLED NEW SUPPORT CHANNE L PER SRM 51-30-2 PG 2. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007032900082 20070329 00082 NM 2007 3 29 QXEA200700433 1 20070310 A 5730 PANEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - GOUGE UNDER PANEL 521AT. REPAIRED IAW SRM 51-20-11, 51-20-36. 2 H 7 2 4T RT A13NM 2007032900094 20070329 00094 NM 2007 3 29 2007UALA00846 1 20070321 A 3350 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 819UA 893 EMERGENCY LIGHTS FAILED 3 SVC CHECK. REPLACED AFT LEFT EPSU AND BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032900095 20070329 00095 NM 2007 3 29 QXEA200700430 1 20070312 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM PAX DOORWAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - POSSIBLE CORROSION ON MAIN CABIN DOOR APPERATURE LOWER INBOARD THRESHOLD MEMBER AROUND AIR INLET FOR DOOR SEAL. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007032900096 20070329 00096 NM 2007 3 29 QXEA200700431 1 20070309 A 5340 ANGLE DHAV DHC8 DHC8202 2809007 NM WING TO FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - RIGHT FORWARD OUTBOARD WING TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW RD8-53-5192. 2 H 7 2 4T RT A13NM 2007032900106 20070329 00106 NM 2007 3 29 QXEA200700459 1 20070306 A 5313 STRINGER SPLICE DHAV DHC8 DHC8202 2809007 NM BS 531 S25R CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 C4 OKC - LIGHT CORROSION ON STRINGER SPLICE AT STATION X 531.50 AND STRINGER 25R. REPAIRED IAW SRM 51-40-00, AND 51-40- 11. 2 H 7 2 4T RT A13NM 2007032900107 20070329 00107 NM 2007 3 29 QXEA200700457 1 20070303 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 182-215 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 C4 OKC - RIGHT FORWARD FLOOR SUPPORT SEAT TRACK HAS 2 SPOTS OF CORROSION AT STATION X 182.00 TO X 215.5. REPAIRED IAW R D8-53-4698. 2 H 7 2 4T RT A13NM 2007032900109 20070329 00109 2007 3 29 AALA20070520 4 20070320 A 2330 WIRE BOEING 777 777223 1385213 NM ENTERTAIN SYS DAMAGED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 775AN 29584 SEAT 11J TV SCREEN HAS EXPOSED WIRES AND SPARKED WHEN USED BY PASSENGER. FOUND SEAT 11J VIDEO ARM CABLE FRAYED. REPLA CED VIDEO ARM, SCREEN, AND AUDIO UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032900115 20070329 00115 NM 2007 3 29 AALA20070508 1 20070316 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 939AN 30883 MIA - EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007032900119 20070329 00119 NM 2007 3 29 2007UALA00849 1 20070321 A 3397 POWER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN OUT OF POSITION A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 647UA 25284 EEL LIGHTING 1EF AND 2EF RIGHT SIDE WIRES STICKING UP AND NOT WORKING. REINSTALLED & RESECURED LIGHT STRIP AND POWER CA BLE, BOTH POSITON EEL OP CHECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007032900126 20070329 00126 NM 2007 3 29 2007UALA00852 1 20070322 A 2897 PIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUEL GAUGE CONNE SHORTED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 203UA 24718 COCKPIT FUEL GAUGES INOPERATIVE. FMC FUEL QUANTITY DOES NOT MATCH. DISPLAYED ERROR NR 4 ON NR 2 TANK COCKPIT FUEL QTY GAUGE. CAUSED BY FOUND PIN 6 ON CONNECTOR D4578P INTERNALLY SHORTED TO PIN 16. REPLACED CONNECTOR D4578P. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032900142 20070329 00142 NM 2007 3 29 2007UALA00863 1 20070322 A 5241 BEARING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT GALLEY DOOR EXCESS PLAY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 AFT GALLEY DOOR HAS PLAY IN UPPER TORQUE TUBE BEARING. REMOVED & REPLACED UPPER TORQUE TUBE BEARING. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032900149 20070329 00149 WP 2007 3 29 070077 1 20070325 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN NO TEST A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 883GA 49710 DURING A ROUTINE OVERNIGHT RON CHECK MAINTENANCE INSPECTION, LAS VEGAS MAINTENANCE REPORTED A FORWARD EMERGENCY EXIT POR TABLE LIGHT WOULD NOT TEST. LAS VEGAS MAINTENANCE FURTHER REPORT THE REMOVAL AND INSTALLATION OF AN EMERGENCY EXIT PORT ABLE LIGHT. A SATISFACTORY OPERATIONAL TEST WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007032900151 20070329 00151 2007 3 29 070076 4 20070325 A 2565 375321321 RETAINER DOUG DC9 DC983 3022083 WP ESCAPE SLIDE BROKEN A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 880GA 49625 FLIGHT 9880 FAT/LAS - FLIGHT CREW REPORTED THAT THE MAIN PASSENGER ENTRY DOOR (L1) ESCAPE SLIDE NEEDS TO BE RE-ATTACHED TO THE DOOR. LAS MAINTENANCE REPORT THE REMOVAL AND REPLACEMENT OF A RETAINING CLIP AT L1 DOOR AND THE RE-MOUNTING OF T HE ESCAPE SLIDE PER AMM 25-62-00. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007032900152 20070329 00152 NM 2007 3 29 2007UALA00870 1 20070321 A 3310 BULB BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT OVERHEATED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 329UA 24149 CREW REPORTS THE LIGHT ON THE AFT COCKPIT BULKHEAD ON THE CAPT'S SIDE HAS OVERHEATED, CREW SMELLED BURNING PLASTIC IN CO CKPIT THAT DISSIPATED WHEN THE RIGHT PACK WAS SECURED. ODOR COULD NOT BE DUPLICATED. SUSPECT COCKPIT BULB THAT OVERHEAT ED. REPLACED COCKPIT BULB. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032900155 20070329 00155 SO 2007 3 29 C2XA07TY015 1 20070321 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16561 145610 LEFT FUSELAGE SKIN IS CRACKED AROUND RIVET AT FRAME 77 STR 6L. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER. ALODINE P RIMED AND PAINTED IAW EC5330-01676. AIRCRAFT IS STILL IN MOD LINE MAINTENANCE. 2 L 7 2 4T RT T00011AT 2007032900156 20070329 00156 NM 2007 3 29 FDKA200702091 1 20070227 A 2720 7G773 PRESSURE SWITCH DHAV DHC8 DHC8102 2809003 NM RUDDER MALFUNCTIONED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 801LR 1033 047 FDM 6131 JFK-PWM (1008 PHX LCL). RUDDER PRESSURE CAUTION LIGHT ILLUMINATED IN FLIGHT. MX REMOVED AND REPLACED PRESSURE SWITCH P3 AND P4. 2 H 7 2 4T RT A13NM 2007032900165 20070329 00165 NM 2007 3 29 AALA20070503 1 20070315 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 369AA 25196 SFO - EMERGENCY LIGHT AT SEAT 29H INOPERATIVE. RECONNECTED WIRE AT CONNECTOR FOR EMERGENCY LIGHT AT SEAT 29H. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007032900169 20070329 00169 NM 2007 3 29 FDKA200702063 1 20070210 A 2910 HYDRAULIC LINE DHAV DHC8 DHC8101 2809002 NM NR 2 ENGINE LOOSE A FDKA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 802LR 205 FDM 6175 SYR-JFK (0600 PHX LCL). NR 2 ENGINE SMOKING FROM COWLING AFTER ENGINE SHUTDOWN. MX TIGHTENED HYD LINE TO EDP. 2 H 7 2 4T RT A13NM 2007032900170 20070329 00170 NM 2007 3 29 AALA20070495 1 20070313 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 631AA 24589 DFW - EMERGENCY SEAT MOUNTED LIGHTS AT FORWARD SECTION OF COACH INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY SEAT M OUNTED LIGHTS AT FORWARD SECTION OF COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007032900199 20070329 00199 WP 2007 3 29 AALA20070489 1 20070313 A 3233 ACTUATOR DOUG DC9 DC983 3022083 WP NLG INOPERATIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 434AA 49452 NOSE GEAR FAILED TO EXTEND NORMALLY. RECYCLED THREE TIMES WITH NO HELP. MANUALLY EXTENDED GEAR. LANDED ORD WITHOUT IN CIDENT. REPLACED NOSE LANDING GEAR BUNGEE ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007032900221 20070329 00221 SO 2007 3 29 FDKA200701036 1 20070131 A 2752 3632001003 PDU EMB 145 EMB145LR 3260212 SO T/E FLAP FAILED A FDKA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 840MJ 13487 145429 FDM 5975 TY-MCO (0530 PHX LCL). FLAP FAIL MESSAGE ON TAXI OUT. MX FERRY AIRCRAFT TO MCO WITH FLAPS AT 9 DEGREES. MCO MX REPLACED THE FLAP PDU. 2 L 7 2 4T RT T00011AT 2007032900223 20070329 00223 WP 2007 3 29 NWAA071019989 1 20070302 A 5322 SHEAR TIE DOUG DC9 DC931 3022065 WP BS 332 S23-25L DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8945E 47181 DURING GROUND OPERATIONS, BELT LOADER IMPACTED FUSELAGE CAUSING DAMAGE TO SHEAR TIE AT S23L-25L BS 332. REPAIRED PER EA 99-206447. 2 L 7 2 4F A6WE 2007032900230 20070329 00230 NM 2007 3 29 QXEA200700390 1 20070223 A 2430 80053533 ANNUNCIATOR DHAV DHC8 DHC8202 2809007 NM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 358PH 17097 119 506 SEA FLIGHT NR 2244, NR 2 DC GENERATOR HOT CAUTION LIGHT FLICKERED FAINTLY AND INTERMITTENTLY. CREW PERFORMED EA CHECKLI ST AND TURNED OFF NR 2 DC GEN SWITCH. NR 2 DC GEN CAUTION LIGHT CONTINUED TO FLICKER BEFORE TURNED OFF THE NR 2 DC GENE RATOR. MAINTENANCE PERFORMED GVI OF NR 2 DC GEN HOT WIRING FROM P-16 TO CONNECTOR. REPLACED ANNUNCIATOR PANEL AND DC S TARTER/GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900232 20070329 00232 SO 2007 3 29 SWIA200718028 1 20070314 A 2150 CONTROL VALVE EMB 120 EMB120ER 3260203 SO LT A/C PACK SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 308SW 120326 SELECTED PACKS TO NORMAL AND LEFT PACK FAILED WITH AIR CONDITION SMOKE. REPLACED LEFT PACK TEMPERATURE CONTROL VALVE IA W 21-60-01. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007032900233 20070329 00233 SO 2007 3 29 SWIA200718029 1 20070315 A 2121 EVAC2322C2 COOLING FAN EMB 120 EMB120ER 3260203 SO SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 220SW 5277 5277 120288 APU BLEED AIR CAUSES PACKS TO SMOKE. REPLACED LEFT GROUND COOLING FAN. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007032900235 20070329 00235 EA 2007 3 29 SWIA200718030 1 20070318 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 744SK 10200 FOUND OVERHEAD CEILING EMERGENCY LIGHT AT ROW 7 IS INOP. RELAMPED EMERGENCY FLOOD LIGHT AT ROW 7 IAW CRJ 700 AMM 33-51- 00. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007032900236 20070329 00236 2007 3 29 SWIA200718031 4 20070316 A 3417 8220372445 ADC CNDAIR CL600 CL6002B19 1900309 EA NR 2 FAILED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 965SW 5927 5927 7871 RECEIVED RED "IAS", "ALT" AND "V/S" FLAGS ON FO SIDE PFD IN FLIGHT. PURGED P1, P2 SYSTEMS IAW AMM 34-11-00 AND REPLACED ADC 2 IAW AMM 34-13-01. 2 L 7 2 4F RT A21EA 2007032900237 20070329 00237 EA 2007 3 29 SWIA200718032 1 20070315 A 3397 WIRE CNDAIR CL600 CL6002C10 1390015 EA CHART LIGHT SHORTED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 703SK 10139 FO'S CHART HOLDER LIGHT SPARKED, THEN WENT OUT. REPAIRED CHART LIGHT POWER SUPPLY IAW WDM 20-33-00 AND ALSO REPLACED LA MP CONTROL ASSEMBLY. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007032900243 20070329 00243 SO 2007 3 29 SIMA200707408 1 20070312 A 5347 14530658003 SEAT TRACK EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 15742 4800 145234 FOUND CORROSION ON RIGHT FORWARD LOWER BOTTOM CABIN SEAT TRACK BETWEEN FRAME 30 TO 50. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032900245 20070329 00245 SO 2007 3 29 SIMA200707417 1 20070312 A 5347 14532605001 SEAT TRACK EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 15742 4800 145234 FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 24 TO 30. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01- 06. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032900246 20070329 00246 SO 2007 3 29 SIMA200707416 1 20070312 A 5347 14530658007 SEAT TRACK EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 15742 4800 145234 FOUND CORROSION ON RIGHT INBOARD SEAT TRACK BETWEEN FRAME 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-0 6. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032900247 20070329 00247 SO 2007 3 29 SIMA200707418 1 20070312 A 5347 14532605015 SEAT TRACK EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 15742 4800 145234 FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 36 TO 45. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01- 06. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032900248 20070329 00248 SO 2007 3 29 SIMA200707419 1 20070312 A 5347 14532605017 SEAT TRACK EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 15742 4800 145234 FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01- 06. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032900249 20070329 00249 SO 2007 3 29 SIMA200707420 1 20070312 A 5347 14532606015 SEAT TRACK EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 15742 4800 145234 FOUND CORROSION ON LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 36 TO 45. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-0 6. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032900250 20070329 00250 SO 2007 3 29 SIMA200707401 1 20070312 A 5347 14530658005 SEAT TRACK EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 15742 4800 145234 CORROSION FOUND ON RIGHT LOWER BOTTOM CABIN SEAT TRACK BETWEEN FRAMES 36 TO 45. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 51-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032900252 20070329 00252 NM 2007 3 29 MZZA0700004 1 20070308 A 5330 SKIN BOEING 737 737824 13844BZ NM STA 500D-500G DAMAGED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 14235 28947 INSPECTION FOUND SEVERAL AREAS OF LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN CROWN AREA AT STA 500D-500G FORWARD OF UPPER ANTI-COLLISION LIGHT. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR B. 2 L 7 2 4F RT A16WE 2007032900255 20070329 00255 NM 2007 3 29 07FDEA01123 1 20070324 A 5347 FLOORBEAM BOEING 727 727225 1384077 NM BS 720A CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 CABIN FLOORBEAM FS 720A, RBL 24.75 TO BL -0, HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION, REMOVED FLOORBEAM DAMAG E IAW SRZ 27-53-034. FABED NEW ANGLES AND FILLER REPAIR IAW SRZ 27-53-034. INSTALLED REPAIR PARTS IAW SRM 51-30-2. MI NOR REPAIR. 2 L 7 3 4F A3WE 2007032900262 20070329 00262 NE 2007 3 29 FDKA200702081 2 20070224 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MALFUNCTIONED A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 810LR 003 FDM 6175 SYR-JFK (0427 PHX LCL). AIRCRAFT RETURNED TO GATE DUE TO BOTH ENGINES WOULD NOT START CABIN FILLED WITH SMOKE. MX RAN ENGINES, CLEARED DUCT AND OPS CHECKED GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2007032900263 20070329 00263 SO 2007 3 29 FDKA200702066 1 20070211 A 3240 CONTROL UNIT EMB 145 EMB145LR 3260212 SO BRAKE SYS MALFUNCTIONED A FDKA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 848MJ 145530 FDM 5976 MCO-HSV (1556 PHX LCL). ABORTED T/O DUE TO BRAKE O/B INOP MESSAGE. MX RESET BRAKE CONTROL UNIT, OPS CHECKED G OOD. 2 L 7 2 4T RT T00011AT 2007032900266 20070329 00266 NM 2007 3 29 07FDEA01124 1 20070324 A 3230 LANDING GEAR DOUG MD11 MD11F 3023600 NM RIGHT INOPERATIVE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 596FE 48554 RMLG WOULD NOT RETRACT ON TAKE OFF. ALL OTHER GEAR GOOD. GOOD DOWN AND LOCKED INDICATIONS FOR LDG T/S IN PROGRESS ON I NITIAL VISUAL INSP, NO SIGN OF LEAKS/DAMAGE ON ANY GEAR/PROX SENSORS/HYD LINES. SELF TEST OF PSEU, SHOWS CODE '99' ONLY , (NIL FAULTS). FOLLOWED FIM T/S TREE CHAPTER 32-30-03.. STEPS 1, 2, 3, 5 AND 7 CARRIED OUT SUCCESSFULLY AMM-32-34-03, 32-61-15, AND 32-33-22. AS PER LAST STAGE OF STEP 7, 'NO LEAKAGE OR OBVIOUS DAMAGE' TO ANY OF THE VALVES/CYLINDER ON R T MLG. 2 L 7 3 4F RT A22WE 2007032900267 20070329 00267 NM 2007 3 29 07FDEA01125 1 20070323 A 2750 4059001908 COMPUTER DOUG MD11 MD11F 3023600 NM FLT CONTROL FAILED A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 595FE 38137 30827 48553 PDIS : FLAPS DID NOT RETRACT WHEN FLAP HANDLE RAISED AFTER T/O, PER QRH, MATCHED FLAP HANDLE TO INDICATED POSITION (15DE G) BUT FLAP INDICATION SHOWED FLAPS CONTINUING TO COME UP. EVENTUALLY INDICATED "0", MATCHED FLAP HANDLE AGAIN. RTB WI TH NO PROBLEM ON FLAP EXTENSION AND NORMAL LANDING. PERFORMED INSPECTION OF FLAPS AND CONTROLS, NO OBVIOUS DISCREPANCY FOUND. PERFORMED FCC RTS, FCC1 FAILS. CYCLED FLAPS FROM UP POSITION TO 50 DEG POSITION, OPERATIONS AND INDICATIONS NOR MAL, SENSOR READ OUT INDICATIONS WITHIN LIMITS. INITIAL FCC RTS SHOWED FAULT CODE N124.12, N124.13,N124.14, ON FCC1. R EMOVED AND REPLACED FCC1. PERFORMED RTS ON FCC1 AND FLAP OPERATIONAL, FLAP OPERATION AND INDICATIONS NORMAL. 2 L 7 3 4F RT A22WE 2007032900268 20070329 00268 NM 2007 3 29 07FDEA01126 1 20070324 A 2750 CONTROL VALVE DOUG MD11 MD11F 3023600 NM TE FLAPS UNKNOWN A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 595FE 48553 PDIS: FLAPS FROZE AT 22-23 DEG ON RETRACTION, RETURN FLAP HANDLE TO 25DEG FLAPS EXTENDED BACK TO 25 DEG, NO ASYMMETRY NO TED, ON 2ND ATTEMPT TO RETRACT FLAPS, FLAPS MOVED SLOWER THAN NORMAL AND FLAPS FULLY RETRACTED. ON LANDING FLAPS EXTEND NORMALLY. AFTER LANDING LOB FLAP MOVES SLOWER THAN OTHERS. NO DEFECTS NOTED ON GROUND OPERATIONAL CHECK. PRECAUTIONA RY REPLACED INBD, CENTER AND OUTBD WING FLAP CONTROL VALVES AND RESTRICTORS. OPERATIONAL TEST CARRIED OUT, OPERATION NO RMAL. A/C OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2007032900270 20070329 00270 NM 2007 3 29 QXEA200700404 1 20070320 A 5210 85290102001 SEAL BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR LEAKING A QXEA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 09 407QX 4049 BOI - ON FLIGHT 2343, IN LEVEL FLIGHT AT 220 NR 2 AFT CABIN DOOR SEAL STARTED LEAKING PER FA, VERY LOUD NOISE DOOR LOWER FORWARD PORTION AT THE DOOR. MAINTENANCE REMOVED AND REPLACED CARGO DOOR SEAL. PRESSURIZED AIRCRAFT, NO LEAKS OR SQUE ALS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900271 20070329 00271 NM 2007 3 29 QXEA200700405 1 20070314 A 6120 697072003 GOVERNOR BOMBDR DHC8 DHC8402 1390042 NM NR 2 OVERSPEED INOPERATIVE A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 424QX 411 411 4006 BOI - ON FLIGHT 2300, RETURNED TO GATE, NR 2 ENGINE TOOK 28 SECONDS TO COME OUT OF FEATHER. MAINTENANCE REMOVED AND REP LACED NR 2 OVERSPEED GOVERNOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900272 20070329 00272 EA 2007 3 29 QXEA200700406 2 20070317 A 7200 312162701 ENGINE BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA NR 1 DAMAGED A QXEA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 NM 09 402QX 2006 2006 4032 SUN-ON FLIGHT 2408 ABORTED TAKEOFF, POWER LEVERS WERE ADVANCED TO RATING DETENT TAKEOFF TORQUE WAS ACHIEVED ON BOTH ENGI NES AT ABOUT 70 KIAS HEARD LOAD BANG. AIRCRAFT VEERED OFF CENTERLINE TO LEFT, ABORTED TAKEOFF, AS I BROUGHT POWER BACK NOTICED "UPTRIM" DISPLAYED ON ED IN REVERSE VIDEO MOMENTARILY. AS WE PULLED OFF RUNWAY, ENGINE INDICATIONS WERE NORMAL. NOTICED ODOR OF SMOKE IN COCKPIT, AS WE RETURNED TO GATE, FA'S REPORTED SOME SMOKE IN THE CABIN, BUT IT WAS DISSIPATING . BOTH ENGINE APPEARED TO RUN NORMALLY AFTER ABORTED TAKEOFF. MAINTENANCE BOROSCOPE REVEALED INTERNAL DAMAGE TO NR 1 ENGINE, REPLACED ENGINE. ALL POST MAINTENANCE CHECKS TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2007032900275 20070329 00275 NM 2007 3 29 QXEA200700395 1 20070319 A 2530 UNKNOWN DHAV DHC8 DHC8202 2809007 NM GALLEY ODOR A QXEA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 355PH 500 SEA FLIGHT NR 2017, BURNING RUBBER ODOR FROM MAPCO, GALLEY EQUIPMENT INOP. MAINTENANCE PLACED MAPCO ON MEL. 2 H 7 2 4T RT A13NM 2007032900277 20070329 00277 NM 2007 3 29 QXEA200700403 1 20070319 A 6123 AUTOFEATHER SYS DHAV DHC8 DHC8202 2809007 NM NR 1 NO TEST A QXEA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 NM 09 358PH 506 SEA FLIGHT NR 2203, NR 1 WOULD NOT AUTOFEATHER DURING AUTOFEATHER TEST. MAINTENANCE COMPLIED WITH AUTOFEATHER SYSTEM AN D POWER UPTRIM TEST. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900278 20070329 00278 2007 3 29 QXEA200700391 4 20070318 A 3420 7004544314 SYMBOL GENERATOR DHAV DHC8 DHC8202 2809007 NM MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 362PH 6678 518 PDX FLIGHT NR 2096, SHORTLY AFTER TAKEOFF, YD FAIL MESSAGE OCCURRED. LESS THAN A MINUTE LATER RECEIVED AHRS DATA INVALI D, ADI PITCH/ROLL MISMATCH. FO'S ADI SHOWED 15 DEGREES BANK OF OPPOSITE OF CAPTAINS AND FO ADI ALSO PITCHED TO 30-35 DE GREES NOSE UP WITH CAPTAINS AT 10 DEGREES NOSE UP. MAINTENANCE REPLACED THE SYMBOL GENERATOR AND NR 2 AHRS COMPUTER. O PERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900279 20070329 00279 NE 2007 3 29 QXEA200700392 2 20070318 A 7200 UNKNOWN DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 1 ENGINE UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 356PH 502 PDX FLIGHT NR 2030 ON TAXI OUT, NR 1 ENGINE MANUAL CAUTION LIGHT ILLUMINATED DURING BETA BACKUP FIRST FLIGHT OF DAY CHEC K. MAINTENANCE C/W REST PROCEDURE IAW AIRCRAFT FLIGHT STANDARDS MANUAL. CAUTION LIGHT EXTINGUISHED. NO DEFECT NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007032900281 20070329 00281 NM 2007 3 29 NWAA070116309 1 20070321 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 OVER NIGHT MAINTENANCE FOUND RT OVERWING 3 EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OPERATIONA L CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007032900283 20070329 00283 EU 2007 3 29 07FDEA01128 1 20070326 A 5330 SKIN AIRBUS 310 A310304 3930339 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 816FD 593 OLD EXTERNAL DOUBLER REPAIR AT C38/38A, P44 RT REPAIR WAS PERFORMED IAW LHT SDR 0226/007536, APPROVED BY EA 6-5314-10641 4 AND RAS/DABRE/7005488/2005 ISS.A 2 L 7 2 4F RT A35EU 2007032900285 20070329 00285 EU 2007 3 29 07FDEA01129 1 20070326 A 5350 A53510703000 FAIRING AIRBUS 310 A310304 3930339 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 REPAIR DAMAGE TO FAIRING 577EL REPAIR WAS PERFORMED BY WET LAY-UP REPAIR IAW EA 6-5317-106416 AND RAS/DAHAM/4021689/2007 ISS.A 2 L 7 2 4F RT A35EU 2007032900286 20070329 00286 EU 2007 3 29 07FDEA01130 1 20070326 A 5410 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 400 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 CORROSION ON AFT BEAM (RIB 8) OF PYLON NR 1, REPAIR WAS PERFORMED BY OVERSIZING IAW EA 6-5451-106439 AND RAS/050001/005/ 2007 ISS.A 2 L 7 2 4F RT A35EU 2007032900288 20070329 00288 EU 2007 3 29 07FDEA01133 1 20070326 A 5411 RIB AIRBUS 310 A310203 3930313 EU NR 2 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 PYLON NR 2 AT AFT SPAR SECTION PYLON TORQUE BOX INNER SURFACE HAS SEVERAL WORKING RIVETS. VISIBLE THRU OPEN ACCESS DOOR NR 484CR. UPON FURTHER INVESTIGATION CRACKS CONTINUING PAST STOP DRILLED ON RIB 20. REMOVED RIB ASSY IAW SRM 51-40- 21. FABBED AND RECEIVED PARTS ON MAE TRAV NR T7/668674,T7/669337 AND T7/669336. LOCATED AND DRILLED IAW SRM 51-40-44. TREATED AND PRIMED PAINTED NEW PARTS IAW SRM 51-21-10 AND INSTALLED RIB ASSY AND REPLACED WORKING RIVETS IAW SRM 51-40- 21. 2 L 7 2 4F RT A35EU 2007032900289 20070329 00289 NM 2007 3 29 DHL2007786501 1 20070314 A 5330 7075T6 SKIN BOEING 727 727214 138407R NM BS 1323-1342 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 61473 21692 AFT AIR STAIRS OUTER SKIN HAS A CREASE FWD OF BS 1323-1342, RBL 17-24. CUT OUT DAMAGED AREA 2" BY 1.5" IAW B727 SRM 52- 10-2 FIG 3. FAB DOUBLER 16" BY 6.375" BY .050, 7075T6 AND FILLER 2" BY .75'BY .040" IAW B727 SRM 52-10-1 AND 52-10-2. TREATED ALODINE AND PRIMED IAW B727 SRM 52-10-2. INSTALLED DOUBLER REPAIR AT AFT AIRSTAIRS IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007032900300 20070329 00300 EA 2007 3 29 A6WA200740084 1 20070225 A 7110 COWLING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENGINE DEPARTED A A6WA K NONE D INFLIGHT SEPARATION CL CLIMB 1 GL 31 456ZW 7849 TOP OF LT ENGINE COWLING DETACHED FROM ENGINE IN FLIGHT STRIKING VERTICAL AND HORIZONTAL STABILIZERS. REMOVED AND REPLA CED UPPER NOSE COWL IAW AMM 71. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900301 20070329 00301 EA 2007 3 29 A6WA200740066 1 20070217 A 5320 601350125X ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT, RT, FS625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 448AW 7814 LT AND RT FS 625.00 OBLIQUE ANGLES ARE CRACKED .5 INCH LONG ON AFT RADIUS. (K) MAINTENANCE DRILLED OFF, REMOVED CRACKE D OBLIQUE ANGLES LT AND RT FS 625 DRILLED UP, ALODINED AND INSTALLED ANGLES PN 601-35012-51 (LT AND 601-35012-529 (RT). OBLIQUE ANGLES INSTALLED WET USING PR1422BY2 SEALANT AND MS2D470AD-5 AND -6 SOLID RIVETS, PRIMED AND PAINTED. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900304 20070329 00304 EA 2007 3 29 A6WA200740053 1 20070204 A 5320 6013501251 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 421ZW 7346 LT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. MAINTENANCE REM OVED AND REPLACED INTERCOSTAL PN 6013501251 IAW SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900305 20070329 00305 EA 2007 3 29 A6WA200740054 1 20070206 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 421ZW 7346 VERTICLE BEAM AT FS 559.0, RBL 9 CRACKED APPROX .300 INCH LONG AT LOWER OB FLANGE. MAINTENANCE REPAIRED FS 559.0 BULKHE AD POST AT RBL 9, LOWER OB FLANGE IAW REO 601R53-41-057 (A). (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900307 20070329 00307 EA 2007 3 29 A6WA200740063 1 20070216 A 5320 601R75262159 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT MLG BAY CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 448AW 7814 HYDRAULIC TRANSDUCER HAT CHANNEL CRACKED APPROX .1 INCH LONG LT MLG WHEEL WELL CEILING. (K) MAINTENANCE INSTALLED NEW HAT CHANNEL IAW SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900308 20070329 00308 EA 2007 3 29 A6WA200740116 1 20070303 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RIGHT MALFUNCTIONED A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 461AW 7846 7870 CABIN FILLED WITH VISIBLE SMOKE. SHUTDOWN PACKS, SMOKE DISSIPATED. TROUBLESHOT SYSTEM FOUND RT AIR CYCLE MACHINE BAD. REMOVED AND REPLACED RT AIR CYCLE MACHINE IAW 21-51-10. OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900311 20070329 00311 EA 2007 3 29 A6WA200740136 1 20070317 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 415AW 7593 RT WING PLANK ACCESS HOLE AT FUEL PANEL 650CB HAS MINOR CORROSION AROUND APPROX 90 PERCENT OF BONDING AREA. (K) [SUP 0 6-05-07] MAINTENANCE SANDED CORRODED AREA TO REMOVE DAMAGE MAX BLEND .004 IAW BSC EO NR 601R-57-11217. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900312 20070329 00312 EA 2007 3 29 A6WA200740062 1 20070216 A 5320 601R75262157 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT MLG BAY CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 448AW 7814 HYDRAULIC TRANSDUCER HAT CHANNEL APPROX .1 INCH LONG RT MLG WHEEL WELL CEILING. (K) MAINTENANCE INSTALLED NEW HAT CHANNE L IAW SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900313 20070329 00313 EA 2007 3 29 A6WA200740094 1 20070305 A 5240 SERVICE DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE MALFUNCTIONED A A6WA K NONE O OTHER NR NOT REPORTED 1 GL 31 410AW 7490 SERVICE DOOR WILL NOT OPEN. CYCLED DOOR, OPENED NORMAL. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900314 20070329 00314 EA 2007 3 29 A6WA200740133 1 20070317 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 415AW 7593 FS 280.0 FLOOR SUPPORT CLIPS PN 601R3113-58 CRACKED APPROX .1 INCH LONG AT IB AND OB SIDE RBL 9.0. (K) [SUP 05-17-07] MAINTENANCE REPLACED INBOARD AND OUTBOARD CLIPS AT FS 280 RBL9 IAW CRJ SRM 51-40-11, 52-42-06 AND 51-42-21. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900316 20070329 00316 EA 2007 3 29 A6WA200740056 1 20070206 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 421ZW 7346 RT WING LOWER PLANK FUEL ACCESS PANEL 640AB HOLE NR 4 AT WS 54.681 HAS MINOR CORROSION ON AFT FLANGE APPROX .003 INCH DE EP AND 3 INCHES LONG IN CRITICAL AREA. MAINTENANCE REPAIRED FUEL WING PLANK CUTOUT HOLE NR 4 (640AB) IAW REO 601R-57-21 -030 REV (F). 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900318 20070329 00318 EA 2007 3 29 A6WA200740064 1 20070217 A 5340 601R3111357 FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT IB, OB FUSELA CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 448AW 7814 FS 280.00 CLIPS ARE CRACKED .2500 INCH IN UPPER RADIUS IB AND OB OF LBL 9. (K) MAINTENANCE REMOVED AND REPLACED FS 280 CLIPS IB AND OB OF LBL 9 IAW MFG STANDARD REPAIR NR 601R-53-0057A STEPS 1 THRU 4. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900320 20070329 00320 EA 2007 3 29 A6WA200740067 1 20070219 A 5340 FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FLOORBEAM RT IB CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 450AW 7823 IB AND OB CLIPS AT FS 280, RBL 9.0, FLOOR SUPPORT BEAM ARE CRACKED IN RADIUS APPROX .30 INCHES LONG EACH. (K) MAINTENANC E REMOVED AND REPLACED IB AND OB CLIPS PN 601R31113-58 IAW SRM 51-42-06, SRM 51-42-20 AND BSC STANDARD REPAIR 601R-53-00 57A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900321 20070329 00321 NM 2007 3 29 F3LA200700044 1 20070309 A 3243 A253130021 SELECTOR VALVE AIRBUS A319 A319111 3930336 NM BRAKES UNKNOWN A F3LA O OTHER N FALSE WARNING DE DESCENT 1 NM 03 920FR 4339 1997 DURING DESCENT, FLIGHT CREW REPORTED BRAKES AUTO BRAKE FAULT. REPLACED BRAKE SELECTOR VALVE 23GG AS PRECAUTIONARY MEASU RE DUE TO NO FAULTS PRESENT, REF AMM 32-42-11, PB401. 2 L 7 2 4F RT A28NM 2007032900324 20070329 00324 EU 2007 3 29 07FDEA00918 1 20070316 A 5320 A53988724 STRUT AIRBUS 310 A310324 3930206 EU ZONE 300 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CORROSION ON CROSS STRUTS AT C87 RT AND LT. REPAIR PERFORMED BY REPLACEMENT WITH NEW PARTS IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007032900325 20070329 00325 EU 2007 3 29 07FDEA00919 1 20070316 A 5730 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 OLD CORROSION REPAIRS ON TOP WING SKIN LT BETWEEN RIB 8 AND RIB 19, P12-15. OLD BLEND REPAIRS ARE WITHIN LIMITS GIVEN F ROM AI EA 6-5720-103417 AND RAS/BAE/1003706/2006 ARE VALID FOR THIS SUBJECT. 2 L 7 2 4F RT A35EU 2007032900329 20070329 00329 EA 2007 3 29 A6WA200740113 1 20070311 A 2750 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT ACTIVATED A A6WA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 31 417AW 7610 WHEN SELECTING FLAPS FROM 8 DEGREES TO 20 DEGREES, A FLAP CAUTION MESSAGE OCCURRED IN FLIGHT. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900331 20070329 00331 EA 2007 3 29 A6WA200740068 1 20070219 A 5340 601R3111357 FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT IB, OB CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 450AW 7823 IB AND OB CLIPS AT FS 280, LBL 9.0, FLOOR SUPPORT BEAM ARE CRACKED IN RADIUS APPROX .30 INCH LON EACH. (K) MAINTENANCE REMOVED AND REPLACED IB AND OB CLIPS PN 601R31113-57 IAW SRM 51-42-06, SRM 51-42-20 AND BSC STANDARD REPAIR 601R-53-005 7A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900332 20070329 00332 EA 2007 3 29 A6WA200740081 1 20070223 A 4950 15A102103 DUCT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE APU CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 405AW 7362 INSPECTED APU AND FOUND UPPER AND LOWER INTAKE DUCTS CRACKED BEYOND LIMITS IAW AMM 49-14-01. REMOVED AND REPLACED UPPER AND LOWER APU INTAKE DUCTS. OPERATIONAL CHECK GOOD IAW 49-52-01. UPPER DUCT TSN = 7728, LOWER DUCT TSN = 11740. 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900335 20070329 00335 EA 2007 3 29 A6WA200740055 1 20070206 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 421ZW 7346 FS 484.0 INTERCOSTAL CRACKED AT RBL 36 APPROX .4 INCH IN UPPER RADIUS. MAINTENANCE REPAIRED INTERCOSTAL IAW REO 601R-53 -41-059 REV (A) AND BSC STANDARD REPAIR 601R-53-0030A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900338 20070329 00338 EA 2007 3 29 A6WA200740132 1 20070317 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 415AW 7593 FS 280.0 FLOOR SUPPORT ANGLE PN 600-34017-595 CRACKED APPROX .2 INCHES LONG ON AFT SIDE FS 280.0 OB OF RBL 9.0. (K) [SU P 05-17-07] MAINTENANCE DAMAGED SECTION DRILLED NEW SECTION OF ANGLE AND SPLICES IAW BOMBARDIER REO 601R-53-11-136. (M ) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900340 20070329 00340 EA 2007 3 29 A6WA200740052 1 20070204 A 5320 6013501252 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 421ZW 7346 RT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STRINGER 14R IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. MAINTENANCE REM OVED AND REPLACED INTERCOSTAL PN 601-35012-52 IAW SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900341 20070329 00341 EA 2007 3 29 A6WA200740112 1 20070312 A 3297 WIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LANDING GEAR DAMAGED A A6WA O OTHER N FALSE WARNING LD LANDING 1 GL 31 408AW 7568 PROXIMITY SYSTEM FAULT WHITE STATUS MESSAGE. INSTALLED NEW WIRES FROM P4MB TO PROXIMITY SWITCH S38. WIRES INSTALLED WE RE RED AND BLUE IAW WDM 20-12-00. OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900345 20070329 00345 SO 2007 3 29 FDKA200703128 1 20070319 A 5241 UNKNOWN EMB 145 EMB145LR 3260212 SO GALLEY DOOR MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 FDM RON CAE (1656 PHX LCL). GALLEY SERVICE DOOR HARD TO CLOSE FROM INSIDE THE CABIN. MX IS CURRENTLY TROUBLESHOOTING. 2 L 7 2 4T RT T00011AT 2007032900346 20070329 00346 NE 2007 3 29 FDKA200703132 2 20070325 A 7261 OIL SYSTEM DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE LOW A FDKA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 07 804LR 324 FDM 6193 JFK (2056 PHX LCL). CREW ABORTED THE TAKEOFF AFTER EXPERIENCING A LOSS OF OIL PRESSURE IN THE NR 1 ENGINE. MX FOUND THE OIL LEVEL LOW AND SERVICED IT. 2 H 7 2 4T 4 T RT A13NM E20NE 2007032900347 20070329 00347 SO 2007 3 29 FDKA200703133 1 20070325 A 5210 HANDLE EMB 145 EMB145LR 3260212 SO PAX DOOR UNKNOWN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 837MJ 145367 FDM RON CAE. MAIN CABIN DOOR WILL NOT OPEN. MX REINSTALLED THE DOOR HANDLE AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2007032900350 20070329 00350 SO 2007 3 29 FDKA200702039 1 20070202 A 4940 23080013A STARTER GEN EMB 145 EMB145LR 3260212 SO APU MALFUNCTIONED A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 833MJ 8628 145327 FDM 6001 LEX-ATL (1001 PHX LCL). APU WAS SHUTDOWN DUE TO BLUE SMOKE COMING OUT WITH NO FIRE INDICATION. MX REMOVED AND REPLACED STARTER GEN, OPS GOOD. 2 L 7 2 4T RT T00011AT 2007032900353 20070329 00353 2007 3 29 FDKA200702061 4 20070208 A 8300 HOUSING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE LOOSE A FDKA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 SW 07 803LR 41550 322 120383 FDM 6023 JFK-MHT (1621 PHX LCL). CREW EXPERIENCED A LOSS OF OIL PRESSURE IN THE NR 1 ENGINE. COMPLETED AN IN FLIGHT SH UTDOWN AND FEATHERED THE PROPELLER. CONTRACT MX FOUND THE RGB SCAVANGE OIL FILTER HOUSING LOOSE AND THE FILTER MISSING. MX REMOVED AND REPLACED THE ENGINE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007032900354 20070329 00354 NM 2007 3 29 FDKA200702076 1 20070220 A 3240 LINE DHAV DHC8 DHC8102 2809003 NM NR 4 BRAKE CRACKED A FDKA O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 07 804LR 324 FDM 6166 JFK-MHT (1722 PHX LCL). NR 2 HYDRAULIC QUANTITY DROPPED TO 2 QUARTS. MX FOUND NR 4 BRAKE LINE CRACKED. MX RE PLACED THE BRAKE LINE ON THE NR 4 BRAKE, OPS/LEAK CHECK GOOD. 2 H 7 2 4T RT A13NM 2007032900357 20070329 00357 NE 2007 3 29 FDKA200702084 2 20070224 A 7320 311246302 VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE P3 MALFUNCTIONED A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 810LR 400 003 FDM 6121 JFK (1200 PHX LCL). CAPT REPORTS SMOKE IN CABIN AND COCKPIT ON APPROACH. MX REMOVED AND REPLACED P3 VALVE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007032900358 20070329 00358 SO 2007 3 29 FDKA200702085 1 20070224 A 3260 852701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO LANDING GEAR MALFUNCTIONED A FDKA O OTHER O OTHER CR CRUISE 1 SW 07 828MJ 1496 145218 FDM 6103 MCO-FLL (0550 PHX LCL). CREW RETURNED TO THE FIELD DUE TO LANDING GEAR WOULD NOT RETRACT. MX SERVICED THE NLG STRUT, REPLACED THE RIGHT TRAILING ARM PROX SENSOR AND REPLACED THE LEFT SHOCK ABSORBER PROX SENSOR. OPS CHECK NORMAL, GEAR SWINGS GOOD. 2 L 7 2 4T RT T00011AT 2007032900360 20070329 00360 NM 2007 3 29 FDKA200702090 1 20070227 A 2711 LA11A2118 ACTUATOR DHAV DHC8 DHC8102 2809003 NM AILERON MALFUNCTIONED A FDKA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 SW 07 804LR 5880 324 FDM 6201 JFK-PWM (1128 PHX LCL). AILERON TRIM WILL GO FULL LEFT AND WILL NOT RETURN TO NEUTRAL. MX REMOVED AND REPLACE D ACTUATOR. 2 H 7 2 4T RT A13NM 2007032800231 20070328 00231 NM 2007 3 28 2007UALA00809 1 20070318 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EEL BETWEEN LAVS AT DOORS 3R & 3L XAISLE INOP. SECURED LAMP CONNECTOR. EEL TESTED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032800232 20070328 00232 NM 2007 3 28 2007UALA00810 1 20070318 A 5753 BOLT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE T/E FLAP DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 LEFT WING, OUTBOARD FLAP, OUTBOARD FLAP DRIVE, FOREFLAP ATTACH FITTING, 3 OF 4 BOLTS MISSING, BROKEN, WITH FITTING SEPAR ATING FROM ITS MOUNTING POINT (4TH LOCK FASTENER IS LOOSE AND ABOUT TO SHEAR). [SUP 06-14-07] REMOVED AND REINSTALLED FITTING WITH OVERSIZED FASTENERS PER UA ENGINEERING SPECIFICATIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032800245 20070328 00245 NM 2007 3 28 2007UALA00822 1 20070319 A 5210 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR INADEQUATE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 508UA 24744 DOOR 2R FWD FRAME IS INADEQUATE. MAJOR REPAIR ACCOMPLISHED: INSTALLED FWD FRAME STEEL DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032800258 20070328 00258 NM 2007 3 28 2007UALA00838 1 20070320 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 218UA 30222 AFT SEAT MOUNTED EMERGENCY LIGHT AT SEAT 2E IS MISSING. REPLACED AFT SEAT 2E EEL LIGHT ASSY. EEL LIGHTING SYSTEM CHECK S OK 2 L 7 2 4F 4 F RT T0001SE E46NE 2007032900027 20070329 00027 NM 2007 3 29 07FDEA00868 1 20070315 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 463FE 22551 FOUND FLUSH REPAIR AT APPROX FUSELAGE STATION 1110-1130 BETWEEN STR 13L-14L DID NOT CONFORM TO EA NR 7-5330-107007. REM OVED EXISTING INTERNAL PLUG DOUBLER PER EA NR 7-5330-107007. FABRICATED .090" INTERNAL DOUBLER TO COMFORM TO EA TREATED AND PRIMED, AND INSTALLED PLUG AT AFT GALLEY VENT LOCATION. 2 L 7 3 4F A3WE 2007032900030 20070329 00030 NM 2007 3 29 07FDEA00870 1 20070315 A 5310 651628065 BEAM BOEING 727 727225 1384077 NM BS 745-765 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 AC BAY LBL 13 BEAM LOWER CHORD HAS CORROSION AROUND GROUND STUDS AND CLAMP SCREW BS 745-765, WL 140 ACCOMPLISHED REPAIR AT A/C BAY LBL 13 BEAM LOWER CHORD BS 745-765 REF SRM 51-40-3 PG 1-6. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007032900053 20070329 00053 EU 2007 3 29 07FDEA00888 1 20070315 A 5320 A53611674201 SPLICE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CORRODED SPLICE AT C19 P48 LT. PART REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007032900058 20070329 00058 EU 2007 3 29 07FDEA00893 1 20070315 A 5730 SKIN AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 OVERSIZED HOLES FOUND DURING ACCOMPLISHMENT OF SB A310-53-2072 ON WING CENTER SECTION UPPER SURFACE STIFFENER 9 AND 10. REPAIR CONSISTS OF INSTALLING OF BOTH HOLES EN 6115-V5X IN TRANSITION FIT IAW EA 6-5315-103426 AND RAS 048117/009/200 6 ISSUE "A". 2 L 7 2 4F RT A35EU 2007032900059 20070329 00059 EU 2007 3 29 07FDEA00894 1 20070315 A 5340 ANGLE AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FUSELAGE CENTER SECTION, CRACKED HOLE AT PICK UP ANGLE, C39-40 RT. REPAIR WAS PERFORMED BY OVERSIZING AND BUSHING INSTA LLATION IAW EA 6-5315-103413 AND RAS/AS/0212/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007032900062 20070329 00062 EU 2007 3 29 07FDEA00897 1 20070315 A 5710 PLATE AIRBUS 310 A310324 3930206 EU ZONE 600 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 NICK IN PYLON REINFORCEMENT PLATE RT. REPAIR WAS PERFORMED BY BLEND OUT IAW EA 6-5720-103365. 2 L 7 2 4F RT A35EU 2007032900072 20070329 00072 EU 2007 3 29 07FDEA00907 1 20070315 A 5311 A53978267208 CROSSBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CORROSION AT CROSSBEAM C67 RT. PART REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007032900079 20070329 00079 WP 2007 3 29 07FDEA00915 1 20070315 A 5730 SKIN DOUG DC10 DC1010 3022110 WP ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 RIGHT WING L/EDGE FWD OF PRESSURE "REFUEL" PANEL AT XORS 510 TO XORS 538 DENTED 2 AREAS. REMOVED, REPLACED, FABBED AND INSTALLED DOUBLER IAW DC10 SRM 57-00-01 FIG 4 SHEET 2 VOL I, ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL II. 2 L 7 3 4F A22WE 2007032900098 20070329 00098 WP 2007 3 29 NWAA071079918 1 20070226 A 5711 SPAR DOUG DC9 DC932 3022066 WP LT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 940N 47572 DURING "L" CHECK, FOUND CRACK IN LT WING TE SPAR EXISTING TEMPORARY REPAIR AT WS 267. SECTION I OF EA 99-208475 REMOVES EXISTING TEMPORARY REPAIR AND REINSTALLATION OF NEW TEMPORARY REPAIR. SECTION II OF EA REQUIRES PERMANENT REPAIR TO BE INSTALLED WITHIN 2 YEARS OR 3,000 CYCLES. 2 L 7 2 4F A6WE 2007032900102 20070329 00102 NM 2007 3 29 QXEA200700458 1 20070306 A 5313 STRINGER SPLICE DHAV DHC8 DHC8202 2809007 NM BS 531 S26R CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 C4 OKC - FOUND LIGHT CORROSION ON STRINGER SPLICE AT STATION X 531.50 AND STRINGER 26R. REPAIRED IAW SRM 51-40-00, 51-4 0-11. 2 H 7 2 4T RT A13NM 2007032900104 20070329 00104 NM 2007 3 29 QXEA200700460 1 20070228 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 510 S24L CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 C4 OKC - FOUND LIGHT CORROSION AT STATION X 510.00 AND STRINGER 24L. REPAIRED IAW SRM 51-40-00, AND 51-40-11. 2 H 7 2 4T RT A13NM 2007032900105 20070329 00105 NM 2007 3 29 QXEA200700461 1 20070226 A 5210 PLATE DHAV DHC8 DHC8202 2809007 NM PAX DOOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 364PH 524 C4 OKC - FOUND PASSENGER DOOR FORWARD UPPER GUIDE PLATE IS WORN. REPAIRED IAW SRM 52-00-16. 2 H 7 2 4T RT A13NM 2007032900110 20070329 00110 WP 2007 3 29 AALA20070504 1 20070315 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 246AA 49258 LGA - EMERGENCY EXIT SIGNS AT OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGNS AT OVERWING EXI T. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007032900111 20070329 00111 NM 2007 3 29 AALA20070505 1 20070315 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 917AN 29518 MIA - EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR SLIDE INOPERTIVE. RELAMPED EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007032900116 20070329 00116 NM 2007 3 29 AALA20070509 1 20070316 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 939AN 30883 MIA - EMERGENCY LIGHTS AT SEAT 13D INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OP ERATION. 2 L 7 2 4F RT A16WE 2007032900124 20070329 00124 EU 2007 3 29 AWXA200700369 1 20070313 A 5753 D57571302202 STRUT AIRBUS 320 A320231 3930325 EU ZONE 600 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 627AW 66 SAL - FOUND CORROSION ON RIGHT WING INBOARD FLAP, INTERCONNECTION STRUT FITTING HOLE, WS 3758/RIB 7. REPLACED RIGHT WIN G INBOARD FLAP, INTERCONNECTION STRUT FITTING, WS 3758/RIB 7 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007032900125 20070329 00125 NM 2007 3 29 AWXA200700370 1 20070309 A 5320 654654039 ANGLE BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED VERTICAL ANGLE, BS 640, RBL 45.6, WL 207. REPLACED VERTICAL ANGLE, BS 640, RBL 45.6, WL 207 IAW B73 7-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007032900159 20070329 00159 NM 2007 3 29 FDKA200702088 1 20070227 A 2421 23088008 GENERATOR DHAV DHC8 DHC8102 2809003 NM NR 1 ENGINE MALFUNCTIONED A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 847EX 718 333 FDM 6138 MHT-JFK (1219 PHX LCL). SMOKE COMING FROM RIGHT SIDE OF NR 1 ENGINE COWL. MX REMOVED AND REPLACED NR 1 S/G, G CU, RELAYS K1 AND K5 AND REPAIRED WIRING. 2 H 7 2 4T RT A13NM 2007032900161 20070329 00161 SO 2007 3 29 FDKA200702062 1 20070208 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 837MJ 145367 FDM RON RDU (1846 PHX LCL). MAIN CABIN DOOR HARD TO CLOSE. MX LUBED DOOR ROLLERS. 2 L 7 2 4T RT T00011AT 2007032900163 20070329 00163 NM 2007 3 29 AALA20070485 1 20070312 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 786AN 30250 DFW - FOUND EMERGENCY LIGHT AT SEAT 25C HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032900184 20070329 00184 NM 2007 3 29 AALA20070484 1 20070312 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 786AN 30250 DFW - EMERGENCY LIGHT AT SEAT 22C HAS MISSING BULB. REPLACED BULB FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032900185 20070329 00185 NM 2007 3 29 FDKA200702040 1 20070203 A 3230 M390166105L RELAY DHAV DHC8 DHC8101 2809002 NM LANDING GEAR MALFUNCTIONED A FDKA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 926HA 114 FDM 6186 JFK - BWI (2245 PHX LCL). LANDING GEAR INOP CAUTION LIGHT IN FLIGHT. MX REMOVED AND REPLACED NOSE LANDING & L EFT , RIGHT LANDING GEAR SEQUENCE RELAY. 2 H 7 2 4T RT A13NM 2007032900186 20070329 00186 WP 2007 3 29 AALA20070497 1 20070313 A 2131 21171803 CONTROLLER DOUG DC9 DC982 3022082 WP AIR CONDITIONING INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 208AA 49159 DFW TO ATL DIVERTED TO LIT DUE TO PRESSURIZATION LOSS AT 29000 FEET. DEPLOYED OXYGEN MASKS. PRESSURIZATION RETURNED A T 20000 BUT DIVERTED TO LIT DUE TO DEPLETED PASSENGER OXYGEN. LANDED LIT WITHOUT INCIDENT. REPLACED BOTH NUMBER ONE AN D NUMBER TWO PRESSURIZATION CONTROLLERS AND OUTFLOW VALVE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007032900187 20070329 00187 SO 2007 3 29 FDKA200702041 1 20070203 A 2752 3632501003 MOTOR EMB 145 EMB145LR 3260212 SO T/E FLAP MALFUNCTIONED A FDKA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 SW 07 840MJ 13504 145429 FDM 6169 MCO-PNS (0504 PHX LCL). FLAP LOW SPEED MESSAGE. MX REPLACED THE RIGHT FLAP MOTOR. 2 L 7 2 4T RT T00011AT 2007032900192 20070329 00192 NM 2007 3 29 AALA20070490 1 20070313 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 639AA 24597 SFO - EMERGENCY LIGHT AT SEAT 28D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007032900198 20070329 00198 NM 2007 3 29 AALA20070480 1 20070312 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 619AA 24577 MIA - EMERGENCY LIGHT AT SEAT 35D INOPERATIVE. RESET CONNECTION FOR INOPERATIVE LIGHT AT SEAT 35D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007032900211 20070329 00211 SO 2007 3 29 FDKA200701011 1 20070114 A 2150 8152916 SWITCH EMB 145 EMB145LR 3260212 SO NR 2 PACK MALFUNCTIONED A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 852MJ 3069 145567 FDM 6123 ATL-PHF (1830 PHX LCL) CABIN AND COCKPIT WAS FILLING UP WITH SMOKE WHEN PACK 2 WAS RUNNING. MX REMOVED AND REP LACED OVERTEMP SWITCH. 2 L 7 2 4T RT T00011AT 2007032900217 20070329 00217 NM 2007 3 29 FDKA200701015 1 20070118 A 2720 INDICATOR DHAV DHC8 DHC8102 2809003 NM COCKPIT OUT OF ADJUST A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 803LR 322 FDM 6195 JFK-PWM (0335 PHX LCL) ELEV TRIM WILL NOT GO FULL RANGE OF MOTION. MX ADJUSTED INDICATOR ON CONT WHEEL. 2 H 7 2 4T RT A13NM 2007032900222 20070329 00222 WP 2007 3 29 NWAA071039989 1 20070221 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 285 L29-30L DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8945E 47181 DURING GROUND OPERATIONS, BELT LOADER IMPACTED FUSELAGE DAMAGING L29L AND L30L AT BS 285. REPAIRED PER EA 99-206445. 2 L 7 2 4F A6WE 2007032900238 20070329 00238 EA 2007 3 29 SWIA200718033 1 20070318 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 954SW 7815 AFT EMERGENCY "POD" LIGHT IS BURNED OUT. REPLACED AFT OVERHEAD EMERGENCY LAMP. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007032900241 20070329 00241 SO 2007 3 29 SIMA200707406 1 20070312 A 5347 14530659009 SEAT TRACK EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 15742 4800 145234 FOUND CORROSION ON LEFT LOWER BOTTOM CABIN SEAT TRACK BETWEEN FRAME 36 TO 45. REMOVED AND REPLACED SEAT TRACK IAW EMB A MM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032900276 20070329 00276 NM 2007 3 29 QXEA200700402 1 20070319 A 3240 21599 BRAKE ASSY DHAV DHC8 DHC8202 2809007 NM NLG MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 360PH 13978 465 515 SEA FLIGHT NR 2070, NOSE LANDING GEAR VIBRATION WHEN BRAKES ARE APPLIED. MAINTENANCE REPLACED BOTH BRAKE ASSEMBLY. OPE RATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900282 20070329 00282 NM 2007 3 29 07FDEA01127 1 20070325 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 620 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 CABIN FLOORBEAM UPPER SURFACE HAS CORROSION, FS 620, LBL 24.75, TO RBL 24.75. REMOVED CORROSION IAW SRM 51-10-6. FABRI CATED REPAIR PARTS ON MAE TRAV NR T7/669488,T7/669489, AND T7/668025 AND INSTALLED REPAIR PARTS IAW SRM 51-30-2. MAJOR REPAIR. 2 L 7 3 4F A3WE 2007032900302 20070329 00302 EA 2007 3 29 A6WA200740093 1 20070307 A 4930 69254517 SOLENOID CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE APU LEAKING A A6WA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 31 449AW 5481 7818 FUEL LEAK AND RUNNING DOWN BELLY SURFACE UNDER TAIL. FOUND APU FUEL SOLENOID LEAKING DRAINING OUT FUSELAGE BELLY DRAIN. DEACTIVATED APU, NO LEAK NOTED, REMOVED AND REPLACED FUEL SOLENOID AND O-RING AT LOWER ELBOW FITTING IAW AMM 49-31, NO LEAKS NOTED. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900306 20070329 00306 EA 2007 3 29 A6WA200740083 1 20070223 A 2750 POTENTIOMETER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE T/E FLAP OUT OF ADJUST A A6WA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 31 469AW 7917 FLAPS FAIL CAS MSG AT ZERO DEGREES, LANDING WEIGHT 40,000 LBS, TOUCHDOWN SPEED 160 KNOTS, MAX BRAKE TEMP = 6.0 FLAP LAND ING PERFORMED RIG CHECK OF BPSU`S, IAW AMM 27-51-10, FOUND NR 6 AND NR 7 POTENTIOMETERS OUT OF ADJUSTMENT. ADJUSTED PO TENTIOMETERS AND PERFORMED CHECK AGAIN. FOUND TEST TO BE COMPLETE. AC GOOD FOR RETURN TO SERVICE. ADDITIONAL: UPON F URTHER INSPECTION OF FLAPS IN HANGAR, FOUND SLUSH AND ICE PACKED INSIDE RT IB FLAP WING TRAILING EDGE APPROX .7500 INCH THICK AND 36 INCHES LONG. ICE MELTED OUT ON RT IB FLAP, DEPOWERED AND REPOWERED AC AND FLAP SYS RESET IAW SUPP 98-018A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900310 20070329 00310 EA 2007 3 29 A6WA200740080 1 20070223 A 3297 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE MLG WOW DEFECTIVE A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 406AW 7402 APPROXIMATELY 17,000 AGL (STEERING INOP) CAS MESSAGE ILLUMINATED MOMENTS LATER (WOW INPUT) MESSAGE ILLUMINATED. COMPLIE D WITH QRH. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED MLG WOW NR 1 ELECTRICAL HARNESS. OPS CHECK GOOD AT THIS TIM E, IAW AMM 32-61-05. 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900327 20070329 00327 NM 2007 3 29 07FDEA00921 1 20070316 A 5710 DUCT DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LT WING FIXED L/E COMPT FOUND TELESCOPING DUCT PASSAGE CUTOUT ON EXTERNAL UPPER SURFACE CORNER CRACKED. REPAIR CARRIE D OUT ON PASSAGE CUTOUT EXTERNAL UPPER SURFACE CORNER OF THE LT WING FIXED L/E COMPT TELESCOPING DUCT AS PER SRM 57-10-0 0 FIGURE 42 VOLUME I TR 57-8. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007032900330 20070329 00330 EA 2007 3 29 A6W2007F00000 1 20070323 A 4950 15A103101 DUCT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE APU CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 405AW 7362 INSPECTED APU AND FOUND UPPER AND LOWER INTAKE DUCTS CRACKED BEYOND LIMITS IAW AMM 49-14-01. REMOVED AND REPLACED UPPER AND LOWER APU INTAKE DUCTS. OPERATIONAL CHECK GOOD IAW 49-52-01. UPPER DUCT, TSN 7728, LOWER DUCT, TSN 11740. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900359 20070329 00359 SO 2007 3 29 FDKA200702086 1 20070224 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6134 ATL-BMI (1720 PHX LCL). GALLEY DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MX CYCLED THE SWITCH AND OPS CHECKE D GOOD. 2 L 7 2 4T RT T00011AT 2007032900361 20070329 00361 SO 2007 3 29 FDKA200703103 1 20070308 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 840MJ 145429 FDM 6123 MCO-ATL (1912 PHX LCL). FLOOR EMERGENCY LIGHTS INOP. MX RESET LIGHT SWITCH, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007032900362 20070329 00362 SO 2007 3 29 MASA200703109 1 20070312 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA K NONE L NO TEST NR NOT REPORTED 1 SW 07 840MJ 145429 FDM 5958 MCO-BTR (0503 PHX LCL). AFT EMERGENCY EXIT FLOOR LIGHTING INOP. MX RESET, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007032900363 20070329 00363 SO 2007 3 29 FDKA200703110 1 20070312 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN DISCONNECTED A FDKA K NONE L NO TEST NR NOT REPORTED 1 SW 07 840MJ 145429 FDM 6018 BNA-MCO (1050 PHX LCL). AFT EMERGENCY EXIT FLOOR LIGHTING INOP. MX RECONNECTED AND OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007032900369 20070329 00369 NM 2007 3 29 FDKA200701008 1 20070109 A 3260 PROXIMITY SENSOR DHAV DHC8 DHC8101 2809002 NM MLG DIRTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 805LR 039 FDM 6077 JFK-PWM (1505 PHX LCL). BOTH MAIN GEAR DOOR AND LANDING GEAR WOULD NOT COME DOWN UNTIL SECOND TRY. MX CLEANED PROX SENSORS. 2 H 7 2 4T RT A13NM 2007032900371 20070329 00371 NM 2007 3 29 FDKA200701024 1 20070124 A 7110 87140011001 COWLING DHAV DHC8 DHC8102 2809003 NM NR 2 ENGINE DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 926HA 57 114 FDM 6212 SYR-JFK (1824 PHX LCL). APPARENT ICE DAMAGE TO NR 2 INLET COWL FIBER GLASS IS TORN. MX CHANGED THE LOWER COWL ING. 2 H 7 2 4T RT A13NM 2007032900375 20070329 00375 SO 2007 3 29 FDKA200701026 1 20070126 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 832MJ 145310 FDM 6147 FLL-TLH (0818 PHX LCL). CREW REPORTED A BURNING SMELL IN THE COCKPIT WITH NO SMOKE AT ALL. MX INSPECTED THE C OCKPIT AND ELECTRICAL AREAS WITH THE FLIGHT CREW AND FOUND NO DEFECTS NOTED AT ALL. 2 L 7 2 4T RT T00011AT 2007032900376 20070329 00376 SO 2007 3 29 FDKA200703096 1 20070305 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6089 TYS-MCO (1621 PHX LCL). FUEL SMELL IN COCKPIT DURING APU STARTUP. MX TROUBLESHOT AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007032900380 20070329 00380 SO 2007 3 29 FDKA200701053 1 20070128 A 5320 14521721009 SPLICE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 12813 145481 CORROSION IN BUTT SPLICE BL 0 BETWEEN FRAMES 15 & 16. MX REPLACED STRAP. 2 L 7 2 4T RT T00011AT 2007032900381 20070329 00381 SO 2007 3 29 FDKA200701054 1 20070128 A 5320 14526437001 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 RIGHT BUTT STRAP SPLICE IS CORRODED AT FR 61 RBL 24. MX REMOVED AND REPLACED DIGITAL. 2 L 7 2 4T RT T00011AT 2007032900382 20070329 00382 SO 2007 3 29 FDKA200701059 1 20070131 A 2844 211C119168 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO RT WING CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 12813 145481 RIGHT WING FUEL PRESSURE SWITCH & LINE IS PITTED FROM CORROSION. MX REPLACED FUEL PRESSURE SWITCH AND LINE. 2 L 7 2 4T RT T00011AT 2007032900388 20070329 00388 SO 2007 3 29 FDKA200702069 1 20070213 A 2750 3634001019 SHAFT EMB 145 EMB145LR 3260212 SO T/E FLAP UNKNOWN A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 840MJ 13549 145429 FDM 6109 MCO (1523 PHX LCL). CREW REPORTED FLAP FAIL MESSAGE. MX REMOVED AND REPLACED HARNESS W170, RIGHT BRACKET FLEX SHAFT. 2 L 7 2 4T RT T00011AT 2007032900389 20070329 00389 SO 2007 3 29 FDKA200701058 1 20070129 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 12813 145481 CORRODED AFT CARGO DOOR SILL. MX REMOVED AND REPLACED CARGO DOOR SILL. 2 L 7 2 4T RT T00011AT 2007032900390 20070329 00390 SO 2007 3 29 FDKA200702052 1 20070207 A 2750 3634001023 SHAFT EMB 145 EMB145LR 3260212 SO T/E FLAP UNKNOWN A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 840MJ 9593 145429 FDM 6011 MCO. FLAP FAIL MESSAGE. MX REPLACED THE RIGHT WING FLEX SHAFT AND REINSTALLED THE LEFT WING FLEX SHAFT. 2 L 7 2 4T RT T00011AT 2007033000001 20070330 00001 NM 2007 3 30 ASTAR20070011 1 20070316 A 3310 RHEOSTAT BOEING 727 727227 1384078 NM COCKPIT LIGHTS SHORTED A DHLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 05 782DH 21998 FOUND STRONG ODOR ON FLT DECK IN FLT. FOUND S/O BACK GROUND LIGHTING RHEOSTAT SHORTED INTERNALLY AND CAUSING STRONG ODO R. REMOVED AND REPLACED RHEOSTAT, F/E'S BACK GROUND LIGHTING, OPS NORMAL IAW B-MM 33-10-01 2 L 7 3 4F A3WE 2007033000004 20070330 00004 NM 2007 3 30 DLM90070242 1 20070317 A 5315 FLOORBEAM DOUG MD90 MD9030 3023690 NM FS 1364 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 FOUND CABIN FLOORBEAM FS 1364 CORRODED. REPAIR PER SRM 51-70-01 FIG 1. 2 L 7 2 4F RT A6WE 2007033000005 20070330 00005 NM 2007 3 30 DLM90070244 1 20070314 A 5230 PAN DOUG MD90 MD9030 3023690 NM CARGO DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 FOUND FWD CARGO DOOR INNER PAN CRACKED AT AFT LATCH. REPAIR IAW SRM 52-30-02D FIG 3 REF N/R 8100-0038. 2 L 7 2 4F RT A6WE 2007033000006 20070330 00006 NM 2007 3 30 DLM90070245 1 20070307 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FS 607 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 FOUND RT CUSP WEB AT STA 607 OUT OF LIMITS. REPLACED CUSP WEB IAW SRM 51-30-02 REF N/R 2700-0221 AT HMV2. 2 L 7 2 4F RT A6WE 2007033000007 20070330 00007 NM 2007 3 30 DLM90070246 1 20070307 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FS 645-654 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 FOUND RT CUSP WEB OUT OF LIMITS FS 645. REPLACED CUSP WEB IAW SRM 51-30-02 REF NR 2700-0224. 2 L 7 2 4F RT A6WE 2007033000008 20070330 00008 NM 2007 3 30 FDKA200703104 1 20070309 A 2750 WARNING SYSTEM DHAV DHC8 DHC8102 2809003 NM FLAP SYSTEM MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 801LR 047 FDM 6165 PWM-JFK (0917 PHX LCL) FLAP DRIVE CAUTION MESSAGE. MX TROUBLESHOT SYSTEM AND OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2007033000009 20070330 00009 NM 2007 3 30 DL76L070247 1 20070324 A 2131 211738813 CONTROLLER BOEING 767 767332 1382001 NM CABIN PRESSURE MALFUNCTIONED A DALA D RETURN TO BLOCK G J MULTIPLE FAILURE WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 179DN 25144 CABIN ALT AUTO 1 AND AUTO 2 STATUS MSG APPEAR ON, TAXI OUT AND CABIN PRESSURIZATION ERRATIC AND UNCOMFORTABLE. REPLACED CPC 1 AND CPC 2. BITE TESTS VERIFY NO FAULTS. MSGS ERASED. 2 L 7 2 4F RT A1NM 2007033000010 20070330 00010 NM 2007 3 30 DL76L070248 1 20070324 A 4910 APU BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE APU BAY SHUTDOWN A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 172DN 24934 24775 P1711 APU AUTO SHUTDOWN AFTER ENGINE START. REMOVED AND REPLACED APU ASSY PER AMM. LK CK OPS CK GOOD. REMOVED MCO AND PLAC. 2 L 7 2 4F 4 F RT A1NM E24NE 2007033000011 20070330 00011 NM 2007 3 30 FDKA200703105 1 20070309 A 3230 LANDING GEAR DHAV DHC8 DHC8102 2809003 NM MALFUNCTIONED A FDKA O OTHER O OTHER CR CRUISE 1 SW 07 810LR 003 FDM 6212 JFK-PWM (2142 PHX LCL) CREW RETURNED TO THE FIELD DUE TO THE LANDING GEAR NOT RETRACTING. MX PERFORMED MLG SWI NG AND NO DEFECTS NOTED. 2 H 7 2 4T RT A13NM 2007033000012 20070330 00012 NM 2007 3 30 DL76G070249 1 20070323 A 3240 BRAKE ASSY BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE MLG DAMAGED A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 1610D 30594 P1711 OUTSIDE REAR LT BRAKE TEMP EXTREMELY HOT REACHING 9 MLG TIRE 5 FOUND DEFLATED UPON ARRIVAL. AFTER TIRE REMOVAL FOUND BR AKE ASSY DAMAGED BRAKE PAD FALLING APART ACP CONDITIONAL INSPECTION AS PER AMM 05-51-14-212-094. NOTHING ABNORMAL FOUND . REPLACED BRAKE ASSEMBLY AS PER AMM. 2 L 7 2 4F 4 F RT A1NM E13NE 2007033000013 20070330 00013 SO 2007 3 30 FDKA200703106 1 20070309 A 2720 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO RUDDER SYS MALFUNCTIONED A FDKA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 SW 07 841MJ 145448 FDM 9961 ATL-MCO (1635 PHX LCL). WHEN RUDDER SYSTEM 1 IS DEACTIVATED THERE IS NO ASSOCIATED EICAS MESSAGE. MX RESET TH E SYSTEM AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2007033000015 20070330 00015 NM 2007 3 30 DLM90070251 1 20070314 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 798 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 RT CUSP WEB OUT OF LIMITS STA 798 FOUND AT HMV2. REPAIRED PER SRM 53-05D FIG 827 REF N/R 2700-0223. 2 L 7 2 4F RT A6WE 2007033000018 20070330 00018 NM 2007 3 30 DLM90070254 1 20070317 A 5320 WEB DOUG MD90 MD9030 3023690 NM FS 370 S26L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 FOUND FWD PIT WEB FS 370 BELOW L26 CORRODED OUT OF LIMITS. FABBED AND REP PER SRM 51-30-02 ,51-30-05,51-30-04 REF N/R 1 400-0325 AT HMV2. 2 L 7 2 4F RT A6WE 2007033000019 20070330 00019 NM 2007 3 30 DLM90070255 1 20070318 A 5230 PAN DOUG MD90 MD9030 3023690 NM AFT CARGO DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 AFT CARGO DOOR INNER PAN CRACKED UNDER 2ND FROM BOTTOM STOP FITTING. REPAIRED PER SRM 52-30-02D. 2 L 7 2 4F RT A6WE 2007033000020 20070330 00020 GL 2007 3 30 FDKA200703107 2 20070309 A 7261 GARLOCK SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 ENGINE LEAKING A FDKA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 838MJ 145384 FDM 6146 MCO-PFN (1650 PHX LCL). NR 1 ENGINE LOW OIL PRESSURE MESSAGE IN FLIGHT AND LEAKING ON THE GROUND. IN-FLIGHT S HUT DOWN OF THE NR 1 ENGINE AND AN EMERGENCY WAS DECLARED. MX REMOVED AND REPLACED ATS GARLOCK SEAL. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007033000025 20070330 00025 2007 3 30 FDKA200703111 4 20070312 A 2210 AUTOPILOT SYS EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 825MJ 145179 FDM 5969 AVL-ATL (0329 PHX LCL). AUTO PILOT AND YAW DAMP FAIL MESSAGES AT POWER UP. CYCLED AIRCRAFT POWER AND FAULT CL EARED. 2 L 7 2 4T RT T00011AT 2007033000026 20070330 00026 SO 2007 3 30 FDKA200702112 1 20070224 A 5347 14532606017 SEAT TRACK EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 849MJ 145534 RIGHT O/B SEAT TRACKS ARE CORRODED OUT OF LIMITS THE ENTIRE LENGTH OF THE A/C. THE SEAT TRACKS HAVE BEEN REMOVED AND RE PLACED. 2 L 7 2 4T RT T00011AT 2007033000030 20070330 00030 NM 2007 3 30 DLM90070262 1 20070325 A 5310 PAN DOUG MD90 MD9030 3023690 NM FWD CARGO DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 FOUND LWR FLANGE OF FWD CARGO DOOR CUTOUT CORRODED. REPAIR PER SRM 51-70-01 FIG 1 REF N/R 1400-0343 AT HMV 2. 2 L 7 2 4F RT A6WE 2007033000031 20070330 00031 NM 2007 3 30 DLM90070263 1 20070322 A 5311 FRAME DOUG MD90 MD9030 3023690 NM FS 1379 L30 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 FOUND AFT B/B FRAME AT STA 1379 LONG 30 CORRODED. REPAIR PER SRM 53-10-02D. 2 L 7 2 4F RT A6WE 2007033000032 20070330 00032 NM 2007 3 30 DLM90070264 1 20070325 A 5730 SKIN DOUG MD90 MD9030 3023690 NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 RT WING L/E SKIN CRACKED AT O/B END OF THE REFUELING PANEL CUT OUT. REPAIR PER SRM 57-20-01 FIG 2 HMV 2 REF N/R 6200-00 02. 2 L 7 2 4F RT A6WE 2007033000033 20070330 00033 SO 2007 3 30 FDKA200703116 1 20070313 A 2750 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO FLAP SYSTEM MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 831MJ 145273 FDM 6099 ATL-LEX (0642 PHX LCL). FLAP LOW SPEED MESSAGE. MX RESET THE FLAP SYSTEM AND OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007033000040 20070330 00040 NM 2007 3 30 HALA0700131 1 20070325 A 3150 UNKNOWN BOEING 767 767300 1385204 NM ISOLATION VALVE UNKNOWN A HALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 13 584HA 24258 ETOPS SIGNIFICANT SYSTEM, APU ISOLATION VALVE ADVISORY LIGHT ON. APU ISLN VAL MSG CLEARED. RAN APU ISOLATION VALVE OPE NED NORMALLY. RAN BOTH PACKS CK'S NML. MESSAGE DID NOT RETURN FIM REF 28-25-00 FIG 104. 2 L 7 2 4F RT A1NM 2007033000041 20070330 00041 SO 2007 3 30 FDKA200703122 1 20070315 A 2742 3622009015 ACTUATOR EMB 145 EMB145LR 3260212 SO HORIZ STAB DEFECTIVE A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 842MJ 11159 145457 FDM 5968 CAK-ATL. PITCH TRIM MAIN CAUTION. MX REMOVED AND REPLACED PITCH TRIM ACTUATOR. 2 L 7 2 4T RT T00011AT 2007033000042 20070330 00042 NE 2007 3 30 HALA0700133 2 20070323 A 7230 BLADE BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 ETOPS SIGNIFICANT SYSTEM, NR 1 ENG BLADE 5 FOD. BLENDED NR 1 ENG NR 5 BLADE PER AMM 72-31-02. NO CRACKS NOTED. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007033000045 20070330 00045 NM 2007 3 30 HALA0700135 1 20070324 A 3150 UNKNOWN BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE UNKNOWN A HALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, ENG EEC C1 MSG DISPLAYED ON EICAS STATUS PG L ENG EEC C1 MSG STATUS ON. EICAS CLEARED, DID NO T RETURN, DID BITE CHECK ON L PIMU . NO FAULTS LPIMU MSG, ALSO CLEARED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007033000046 20070330 00046 NM 2007 3 30 DHL2007786502 1 20070315 A 5512 SKIN BOEING 727 727214 138407R NM HORIZONTAL STAB DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 RT HORIZ STAB LWR SURFACE HAS A DENT, STAB STA 144, 11 AFT OF L/E. CUT OUT DAMAGED AREA AT RT HORIZ STAB LWR, MEASUREME NTS, 1.25 BY 1.75 IAW B727 SRM 55-10-3. FABRICATED DOUBLER REPAIR FROM 2024T3, .080, 7.875 BY 5.375 IAW B727 SRM 55-10- 3, FIG 3. TREATED ALODINE AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR WITH SOLID FSTNRS IAW B727 SRM 51- 30-2. 2 L 7 3 4F A3WE 2007033000047 20070330 00047 2007 3 30 ANCF200600048 4 20070325 A 3440 AHRS DOUG DC9 DC983 3022083 WP NR 1 FAILED W ANCF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 836RA 53046 AFTER T/O TO 30º AHRS DIFERENCE WAS PRESENTED. AFTER THAT TOTAL AHRS FAILURE CHECK LIST WAS PERFORMED UNSATISFACTORY IA W AMM 34-20-00 PAGE 401 WAS SWAPPED THE AHRS NR 1 WITH ANRS NR 2 AND PERFORMED BITE PROCEDURE AMM 34-22 03 PAGE 201. TE ST ON GROUND SATISFACTORY, P/N ON 460800-03-06 S/N POS 1 ON 1548 ON S/N POS 2 ON 1135 ON P/N ON - OFF:460800-03-06 S/N OFF: POS (1)1135 S/N OFF: POS (2) 1548. 2 L 7 2 4F RT A6WE 2007033000050 20070330 00050 NM 2007 3 30 DHL2007786509 1 20070316 A 5347 BAC1520792 SEAT TRACK BOEING 727 727214 138407R NM BS 486-492 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 PITTING CORROSION IN LWR SECTION OF SEAT TRACK CUTOUT AT RT BS 486 TO 492.5, RBL 45. EVAL FOUND SEAT TRACK PITTING CORR OSION BEYOND LIMITS. REMOVED SEAT TRACK FROM BS 480 TO 690 IAW B727 SRM 53-10-5, FIG 1. FABRICATED AND TRIMMED AS REQU IRED NEW SEAT TRACK SECTION P/N BAC 1520-792 IAW B727 SRM 53-10-5, FIG 1. TREATED, PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED SEAT TRACK IAW B727 SRM 53-10-5, FIG 1. 2 L 7 3 4F A3WE 2007033000051 20070330 00051 EA 2007 3 30 SWIA200718057 1 20070324 A 3350 CHARGER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 719SK 10188 FLOOR-LEVEL LIGHTED EXIT SIGN AT ROW 18 ON RIGHT SIDE IS OUT. REPLACED BATTERY CHARGER PER AMM 33-51-17. OPERATIONAL C HECKS GOOD. 2 L 7 2 4F RT A21EA 2007033000056 20070330 00056 EA 2007 3 30 SWIA200718060 1 20070320 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCONNECTED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 917SW 7641 FOUND FORWARD ENTRY EMERGENCY LIGHT INOP. SECURED CONNECTOR AT FORWARD EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GO OD. 2 L 7 2 4F RT A21EA 2007033000061 20070330 00061 NM 2007 3 30 DLM88070230 1 20070323 A 5330 593600731 SKIN DOUG MD88 MD88 3023688 NM FS 1322 MISREPAIRED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 943DL 49816 DURING THE CURRENT VISIT, AN UNIDENTIFIED REPAIR WAS REPORTED ON THE FUSELAGE SKIN AT FS 1322 BETWEEN L25R AND L26R. A BOEING APPROVED REPAIR WAS INSTALLED PER 460142-14. 2 L 7 2 4F RT A6WE 2007033000063 20070330 00063 NM 2007 3 30 DLM88070231 1 20070323 A 5330 59670631 SKIN DOUG MD88 MD88 3023688 NM FS 1437 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 943DL 49816 DURING CURRENT VISIT, TWO CRACKS WERE REPORTED IN THE FUSELAGE SKIN AT FS 1437, BETWEEN L1 AND L-4L. THE CRACKS WERE 0. 5" IN LENGTH. THE DAMAGE WAS CUTOUT AND A BOEING APPROVED REPAIRED INSTALLED PER 460141-14 2 L 7 2 4F RT A6WE 2007033000068 20070330 00068 NM 2007 3 30 DL764070235 1 20070323 A 3150 UNKNOWN BOEING 767 767432ER 1385134 NM UNKNOWN A DALA D RETURN TO BLOCK G J MULTIPLE FAILURE WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 834MH 29707 CHECKING EICAS RECALL ON BEFORE T/O CHECKLIST ALL WARNINGS AND CAUTIONS DISPLAYED AS IF ACFT WAS SHUTDOWN. DOWN POWERED ACFT AND RESET POWER. ALL INDICATIONS NORMAL. 2 L 7 2 4F RT A1NM 2007033000069 20070330 00069 NM 2007 3 30 DL757070236 1 20070323 A 3230 LINE BOEING 757 757232 1384965 NM MLG HYD SYS RUPTURED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 615DL 22822 AFTER T/O THE GEAR HANDLE WOULD NOT RAISE. AS PER QRH NR 6 OVRD PROCEDURE ACCOMPLISHED AND RT MAIN STAYED DOWN AND GRN. LT MAIN AND NOSE CAME UP WITH GEAR DISAGREE LIGHT. LOWERED GEAR HANDLE AND HAD 3 GRN LANDED UNEVENTLY. FOUND RUPTURE D HYD FLEX LINE NEAR RIGHT GEAR STRUT TRUNNION FOR RIGHT TRUCK POSITIONER SHUTTLE VALVE. REPLACED FLEXLINE. LEAK CHECK OK. NO FURTHER TROUBLE FOUND. ALSO, PERFORMED SHUTTLE TEST PER M/M 32-32-17-404-012. CHECKS OK. 2 L 7 2 4F RT A2NM 2007033000071 20070330 00071 NM 2007 3 30 DLM90070238 1 20070316 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FS 1192-1231 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 AT HMV 2, FOUND CUSP WEB CORRODED LT STA 1193-1231. FABBED 2 DOUBLERS IAW MD90 SRM 53-00-01 AND 51-10-03 REF N/R 2400-0 239. 2 L 7 2 4F RT A6WE 2007033000072 20070330 00072 NM 2007 3 30 DLM90070239 1 20070318 A 5551 ATTACH ANGLE DOUG MD90 MD9030 3023690 NM FS 1475 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 RT DORSAL TO FUSELAGE ATTACH ANGLE CRACKED 2 PLACES STA 1475HMV2. REPLACED ANGLE PER SRM 51-30-05 PG 10A AND 15 REF N/R 3300-0076. 2 L 7 2 4F RT A6WE 2007033000073 20070330 00073 NM 2007 3 30 HALA0700124 1 20070320 A 3246 165T010039 WHEEL BOEING 767 767300 1385204 NM MLG DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 588HA 2799 2799 33466 NR 4 MLG WHEEL HOT THERMALED UPON ARRIVAL REQUIRES REPLACEMENT. REMOVED AND REPLACED NR 4 MLG WHEEL ASSY PER TASK CARD 32-45-01-004 AND 32-45-01-404-027. 2 L 7 2 4F RT A1NM 2007033000074 20070330 00074 NM 2007 3 30 HALA0700125 1 20070320 A 3240 BRAKE ASSY BOEING 767 767300 1385204 NM MLG HOT A HALA K NONE M OVER TEMP IN INSP/MAINT 1 WP 13 588HA 3451 3451 33466 UPON WALK AROUND, FOUND MAIN LANDING GEAR WHEEL BRAKES NR 3 RED HOT AND SMOKING MAIN LANDING GEAR MLG THERMALED WENT FLA T REQUIRE REPLACEMENT. REMOVED AND REPLACED NR 3 MLG AS PER MM TASK CARD 32-45-01-004-001 AMD TASK CARD 32-45-01-404-02 7. 2 L 7 2 4F RT A1NM 2007033000075 20070330 00075 2007 3 30 HALA0700126 4 20070321 A 2310 9640452012 RECEIVER BOEING 767 76733A 1385209 NM HF SYSTEM MALFUNCTIONED A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 581HA 2875 2875 28141 ETOPS SIGNIFICANT SYSTEM, L HF RECEPTION WEAK XMIT OK, IN DATA MODE, ALL FREQ SHOW "POOR" QUALITY NO COMM. REPLACED NR 1 HF XCVR. OPS CHECK OK PER MM 23-11-03. 2 L 7 2 4F RT A1NM 2007033000080 20070330 00080 NM 2007 3 30 DHL2007786508 1 20070316 A 5347 SEAT TRACK BOEING 727 727214 138407R NM BS 1096-1103 GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 NUMEROUS DENTS AN GOUGES IN RT SEAT TRACK AT RT STA 1096-1103. MARKED IN RED. REMOVED SEAT TRACK AT RT RBL 45-STA 1050 -1130 IAW B727 SRM 51-30-2. FABBED NEW SEAT TRACK SECTION MAT USED BAC 1520-792-792-7178T6511. PO NR 9003963, DIM 5 FT . 7" LONG IAW B727 SRM 53-10-5 FIG 1. TREATED AND PRIMED AREA IAW B727 SRM B727 SRM 51-10-2. INSTALLED NEW SEAT TRACK S ECTION IAW B727 SRM 53-10-5 FIG 1 AND 51-30-2. 2 L 7 3 4F A3WE 2007033000081 20070330 00081 NM 2007 3 30 DHL2007786506 1 20070322 A 5542 SKIN BOEING 727 727214 138407R NM RUDDER DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 FOUND TWO DENTS ON UPPER RUDDER LT T/E SKIN AT LOWER HINGE BS 1540. NO DENTS ALLOWED. FOUND OUT OF LIMITS IAW B727 SRM 55-40-1 FIG, 61. REMOVED LT T/E SKIN AT UPPER RUDDER BS 1540 IAW B727 SRM 51-30-2. FABBED LT T/E SKIN AT RUDDER BS 15 40 MATERIAL USED 2024T3 .025 PO NR 9004384 DIM 45 3/4" BY 7" IAW B727 SRM 55-40-2 FIG 2. TREATED ALODINE AND PRIMED IAW B727 SRM 51-10-2. INSTALLED LT T/E SKIN AT UPPER RUDDER IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007033000082 20070330 00082 NM 2007 3 30 QXEA200700393 1 20070318 A 2497 WIRE DHAV DHC8 DHC8202 2809007 NM NR 2 DC GEN CHAFED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 354PH 498 SEA FLIGHT 2070 SHORTLY AFTER LIFTOFF NR 2 DC GENERATOR DC GEN HOT CAUTION ILLUMINATED. CAUTION REMAINED ON FOR ENTIRE DURATION OF FLIGHT EVEN AFTER TURNING OFF NR 2 DC GENERATOR. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND WIRES, 77A20N, 71 5D20, 78A20, 76A16, AND 75A20 INSULATION CHAFED APPROXIMATELY 3 FEET FROM NR 2 STARTER GENERATOR CONNECTOR P16. REPAIRE D WIRES IAW PRATT AND WHITNEY MM 72-01-10. NO PARTS REPLACED OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007033000086 20070330 00086 NM 2007 3 30 QXEA200700410 1 20070305 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 263-424 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - LEFT OUTBOARD SEAT TRACK NR 1 CORRODED AT STATION 263.0 TO 266.0, STATION 269.0, 284.0, 297.0 TO 301.0, 342.0 T O 345.0, 362.0, 374.0, 376.0, 378.0, 405.0, 424.0. REPAIRED IAW RD8-53-1342. 2 H 7 2 4T RT A13NM 2007033000088 20070330 00088 NM 2007 3 30 QXEA200700412 1 20070309 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 518-528 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - LEFT OUTBOARD SEAT TRACK NR 3 CORRODED AT STATION 518.0, 528.0. REPAIRED IAW RD8-53-3644. 2 H 7 2 4T RT A13NM 2007033000090 20070330 00090 NM 2007 3 30 QXEA200700414 1 20070314 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 493 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - LEFT INBOARD SEAT TRACK NR 5 CORRODED AT STATION 493.0. REPAIRED IAW RD8-53-9519. 2 H 7 2 4T RT A13NM 2007033000091 20070330 00091 NM 2007 3 30 QXEA200700407 1 20070314 A 5411 FRAME DHAV DHC8 DHC8202 2809007 NM RT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - RIGHT NACELLE INBOARD FRAME INSIDE WHEELWELL HAS CHAFE LEFT FORWARD CORNER AT STATION ZN 15.00 AND XN 130.06. REPAIRED IAW SRM 51-20-16, 51-20-36, AND 51-20-51, RD8-54-2370. 2 H 7 2 4T RT A13NM 2007033000092 20070330 00092 NM 2007 3 30 QXEA200700408 1 20070318 A 5530 BRACKET DHAV DHC8 DHC8202 2809007 NM VERTICAL STAB MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - INTERIOR OF VERTICAL STABILIZER LEADING EDGE UNDER PANEL 321CL. THE BRACKET FOR THE HOT AIR DUCTING IS MISSING A FASTENER. REPAIRED IAW RD8-55-1813. 2 H 7 2 4T RT A13NM 2007033000093 20070330 00093 NM 2007 3 30 QXEA200700409 1 20070309 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 258 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - LEFT OUTBOARD SEAT TRACK NR 1 GOUGED AT STATION 258.0. REPAIRED IAW RD8-53-1342. 2 H 7 2 4T RT A13NM 2007033000095 20070330 00095 NM 2007 3 30 QXEA200700416 1 20070309 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 330-424 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - SEAT TRACK NR 10 HAS MINOR SCRATCHES AND CHAFES AT STATION 330, 342, 360 TO 370, 388 TO 424. REPAIRED IAW RD8- 53-1342. 2 H 7 2 4T RT A13NM 2007033000097 20070330 00097 NM 2007 3 30 QXEA200700441 1 20070318 A 7712 304725201 SENSOR BOMBDR DHC8 DHC8402 1390042 NM ENGINE TORQUE MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 425QX 3343 3343 4039 SMF FLIGHT NR 2410: POWER PLANT MESSAGE ON ED AFTER PROPS CAME OUT OF FEATHER. AIRCRAFT RETURNED TO THE GATE. MAINTENA NCE REQUESTED REMOVAL AND REPLACEMENT OF NR 2 PECU (P/N 699018002, S/N 1046) IAW AMM TASK 61-20-36-000-801 AND 61-20-36- 400-801. OPS TEST FAILED. DID NOT FIX PROBLEM. AFTER TROUBLE SHOOTING, SWAPPED THE TORQUE SENSOR 'A' CONNECTOR P11 FR OM NR 1 TO NR 2 AND VICE VERSA. PROBLEM FOLLOWED FROM NR 2 ENGINE TO NR 1 ENGINE. SWAPPED TORQUE SENSORS BACK TO ORIGI NAL POSITIONS IAW TASKS 77-11-06-000-801 AND 77-11-06-400-801. REMOVED AND REPLACED NR 2 ENGINE TORQUE SENSOR 'A' CONNE CTOR P11 WITH NEW FROM STOCK. FAULT CODE CLEARED. ALL OPS CHECKS COMPLETED FOR THE NR 1 AND NR 2 ENGINES. FADEC AND P 2 H 7 2 4T RT A13NM 2007033000098 20070330 00098 EU 2007 3 30 07FDEA00923 1 20070316 A 5710 FLANGE AIRBUS 310 A310324 3930206 EU ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 CORROSION AT HOLES 34A AND 36A OF RT OUTBOARD HORIZONTAL FLANGE OF LOWER TEE SECTION. REPAIR CONSISTS OF OVERSIZING HOL ES UP TO CORROSION REMOVAL AND INSTALLING REPAIR FASTENERS IAW EA 6-5710-103425 AND RAS/048047/009/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007033000100 20070330 00100 EU 2007 3 30 07FDEA00925 1 20070316 A 5230 A52378043230 BEAM AIRBUS 310 A310324 3930206 EU ZONE 800 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 CRACKS IN 2 STAY, PROFILES AT C67A AND C68 RT BETWEEN BEAM 3-5, SHOWN IN SRM 52-34-00/FIG 2/PG 8) REPAIR PERFORMED BY RE PLACEMENT OF AFFECTED STRUCTURE COMPONENT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007033000101 20070330 00101 EU 2007 3 30 07FDEA00927 1 20070316 A 5313 A53986212 STRINGER AIRBUS 310 A310304 3930339 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 FOUND CORRODED STRINGER P52 AND P53, C65-66. REPAIR WAS PERFORMED IAW SRM 53-10-14. 2 L 7 2 4F RT A35EU 2007033000104 20070330 00104 SO 2007 3 30 FDKA200703095 1 20070304 A 2720 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO RUDDER SYS MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 852MJ 145567 FDM 6043 ATL (2043 PHX LCL). RUDDER HARD OVER SYSTEM FAIL MESSAGE. MX RESET AND MESSAGE CLEARED. 2 L 7 2 4T RT T00011AT 2007033000107 20070330 00107 NM 2007 3 30 QXEA200700381 1 20070219 A 3350 3017426 LIGHT BOMBDR DHC8 DHC8402 1390042 NM CABIN MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 425QX 4039 PDX - ON FLIGHT 2286, ON PREFLIGHT FOUND FLOOR TRACK PIECE AT 1 AB WITH THE SMALL RED SQUARES INDICATING AN EMERGENCY EX IT IS MISSING. MAINTENANCE REMOVED AND REPLACED FLOOR TRACK STRIP. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007033000108 20070330 00108 NM 2007 3 30 QXEA200700380 1 20070215 A 3620 8209712 SHUTOFF VALVE BOMBDR DHC8 DHC8402 1390042 NM ENGINE INOPERATIVE A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 424QX 12646 12646 4006 PDX - NR 1 AND NR 2 BLEED HOT LIGHTS ILLUMINATED ON 2-3 MILE FINAL. LIGHTS EXTINGUISHED WHEN BLEEDS SELECTED OFF PER EM ERGENCY CHECKLIST. MAINTENANCE REMOVED AND REPLACED NR 1 AND NR 2 ENGINE HPSOV. GROUND RAN BOTH ENGINES THROUGH ALL PO WER SETTINGS FAULT DID NOT RE-OCCUR. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007033000110 20070330 00110 SO 2007 3 30 FDKA200702047 1 20070205 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 842MJ 145457 FDM 6022 ATL-CAK (0538 PHX LCL). CREW REPORTED A BURNING SMELL IN THE COCKPIT THE DISSIPATED. MX FOUND NO DEFECTS. 2 L 7 2 4T RT T00011AT 2007033000112 20070330 00112 NM 2007 3 30 QXEA200700382 1 20070309 A 3350 M8373110341 SWITCH BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY LIGHTS MALFUNCTIONED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 421QX 4149 SEA - ON FLIGHT 2476, EMERGENCY LIGHT ILLUMINATED WHEN POSITIONED TO ARM RECYCLED SWITCH. NO GOOD. MAINTENANCE REMOVED AND REPLACED FA'S EMERGENCY LIGHT SWITCH. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007033000113 20070330 00113 NM 2007 3 30 QXEA200700379 1 20070312 A 4910 APU BOMBDR DHC8 DHC8402 1390042 NM APU BAY FAILED A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 409QX 4051 PDX FLIGHT NR 2409: DURING START AND ATTTEMPT TO START APU. THERE WAS A LOUD BANG ALONG WITH A FAIL MESSAGE ON THE POWE R SELECTOR SWITCH. MAINTENANCE DETERMINED LOUD 'BANG' WAS ASSOCIATED WITH A FAILURE OF THE APU AND APU ENCLOSURE. REMOV ED AND REPLACED TAIL CONE ASSEMBLY, APU ASSY. AND APU DOORS. ALL CHECKS WERE GOOD WITH NO DEFECTS NOTED. AIRCRAFT RETURN ED TO SERVICE 2 H 7 2 4T RT A13NM 2007033000116 20070330 00116 NM 2007 3 30 FDKA200702089 1 20070227 A 2597 CONNECTOR DHAV DHC8 DHC8102 2809003 NM GALLEY DIRTY A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 805LR 039 FDM 6212 JFK-PWM (2024 PHX LCL). F/A SMELLED STRONG ODOR IN GALLEY IN FLIGHT. MX CLEANED HOT JUGS OUT & CLEANED THE CO NNECTORS, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007033000117 20070330 00117 NM 2007 3 30 HALA0700116 1 20070319 A 3150 UNKNOWN BOEING 767 76733A 1385209 NM UNKNOWN A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 587HA 33421 ETOPS SIGNIFICANT SYSTEM, EICAS STATUS ALERT. CENTER FUEL TANK AND TOTAL FUEL QTY INDICATORS BLANK. EICAS MSG 'FUEL QT Y IND' DISPLAYED. FUEL QTY TEST NORMAL, DISPLAYS REMAINED BLANK AFTER TEST. PERFORMED FUEL QTY TEST. FUEL BITE AND SE LF TEST ON FQIS PROCESSOR. SYSTEM TEST PASS. NO FURTHER ACTION REQUIRED PER FIM 28-41-00 FIG 104 116 AND 114. 2 L 7 2 4F RT A1NM 2007032900055 20070329 00055 EU 2007 3 29 07FDEA00890 1 20070315 A 5330 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 DOUBLE HOLE IN SKIN AT C73-74, P28 LT. REPAIR WAS PERFORMED BY REAM UP THE HOLE IAW EA 6-5318-103397 AND RAS/DATLS/0003 407/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007032900061 20070329 00061 EU 2007 3 29 07FDEA00896 1 20070315 A 5411 SPAR AIRBUS 310 A310324 3930206 EU NR 2 PYLON CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 CRACKED HOLE ON PYLON NR 2 AT RIB 8 UPPER SPAR. REPAIR WAS PERFORMED IAW SRM 54-51-31/FIG 201 AND APPROVED BY EA 6-5451 -103400. 2 L 7 2 4F RT A35EU 2007032900064 20070329 00064 EU 2007 3 29 07FDEA00899 1 20070315 A 5340 A53980161201 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 MAINT ERROR A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 813FD 500 OLD MISDRILLED HOLE AT FITTING C74, P26 RT. PART REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007032900087 20070329 00087 NM 2007 3 29 QXEA200700437 1 20070315 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - 4 INCHES BELOW UPPER APERTURE OF LEFT UNDER WING EMERGENCY EXIT AT THE AFT EDGE THERE ARE 9 FASTENERS PULLED TH ROUGH THE WING TO FUSELAGE FAIRING. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007032900089 20070329 00089 NM 2007 3 29 QXEA200700435 1 20070314 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSLEAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - THE SKIN UNDER LOWER VHF COMM ANTENNA HAS CORROSION BY 57803. AVIONICS REQUEST. REPAIRED IAW RD8-53-9518. 2 H 7 2 4T RT A13NM 2007032900091 20070329 00091 NM 2007 3 29 QXEA200700428 1 20070314 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - FLAP TRACK 4 ON LEFT WING HAS PITTING ON OUTBOARD SIDE ON TRACK E. REPAIRED IAW EA 2-57-216A AND DHC-9 TASK 27 -51-11-830-801. 2 H 7 2 4T RT A13NM 2007032900092 20070329 00092 NM 2007 3 29 QXEA200700429 1 20070314 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - FLAP TRACK NR 5 ON LEFT WING HAS PITTING ON OUTBOARD SIDE ON TRACK E. REPAIRED IAW EA 2-57-217A AND DHC-8 TASK 27-51-11-830-801. 2 H 7 2 4T RT A13NM 2007032900099 20070329 00099 WP 2007 3 29 NWAA071089758 1 20070302 A 5310 DOOR FRAME DOUG DC9 DC941 302207N WP CARGO DOORWAY DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 758NW 47286 DURING "H" CHECK, FOUND FORWARD CARGO DOOR JAMB DOUBLER WITH MULTIPLE OVERSIZED HOLES. REPAIRED PER EA 97-208465 SECTIO N I. SECTION II REQUIRES INSPECTIONS AT "L" CHECK INTERVALS. 2 L 7 2 4F A6WE 2007032900112 20070329 00112 NE 2007 3 29 AALA20070514 2 20070319 A 7230 COMPRESSOR DOUG MD80 MD83 3023681 NM PWA JT8 JT8D217 52053 NE RT ENGINE STALLED A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 9420D 49824 708559 DURING CLIMB, AIRCRAFT EXERIENCED LOUD BANK AND FIVE DEGREES OF YAW AT 2600 FEET. CREW RETURNED TO MSP AND LANDED WITHO UT INCIDENT. CREW REPORTED NUMBER TWO ENGINE GIVING LITTLE MORE THAN IDLE THRUST ON SHORT FINAL. REPLACED NUMBER TWO E NGINE ON 20 MARCH AT MSP DUE TO STALLS DURING CLIMB POWER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT E9NE 2007032900123 20070329 00123 NM 2007 3 29 2007UALA00851 1 20070320 A 3097 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE WINDOW HEAT BURNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 663UA 27160 F/O`S NR 1 WINDOW & CAPT'S SIDE WINDOW HEAT INOP. FOUND WINDOW HEAT WIRES BURNT BEHIND E2-1 RACK AT CONN D4294P, REF WD M 30-41-12. CONTROL SENSOR FOR LEFT WINDOW 2 MELTED AND OTHER WIRES HAVE HEAT DAMAGE. PWR WIRE W1120-203B-12 EXTENSIVELY DAMAGED. WIRES WERE REPAIRED AND HARNESS REINSTALLED IN A/C. HARNESS OPERATED OK. SUSPECT LOOSE PINS CAUSED HIGH CURRE NT DRAW & C-B FAILED TO OPEN SOON ENOUGH TO PROTECT WIRES. 2 L 7 2 4F 4 F RT A1NM E24NE 2007032900128 20070329 00128 NM 2007 3 29 2007UALA00854 1 20070320 A 5522 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU RT ELEVATOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 927UA 26649 ELEVATOR SKIN IS CRACKED. MAJOR REPAIR ACCOMPLISHED REPAIR PER SRM. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032900140 20070329 00140 NM 2007 3 29 2007UALA00862 1 20070322 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 AFT PIT BS 827 JUST ABOVE STR 25, SHEAR TIE DAMAGED AT LWR INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLE R REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032900143 20070329 00143 NM 2007 3 29 2007UALA00864 1 20070323 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY EXIT CEILING ENTRY LIGHT INOP AT DOORS 1R & 3R. RELAMPED CEILING ENTRY EMERGENCY LIGHTS, BOTH POSITIONS. BO TH OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032900146 20070329 00146 NM 2007 3 29 2007UALA00867 1 20070323 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY EEL LIGHT INOPERATIVE AT SEAT 56 RIGHT. REPLACED LIGHT ASSY. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032900147 20070329 00147 WP 2007 3 29 070074 1 20070320 A 5280 DOOR DOUG DC9 DC983 3022083 WP MLG DAMAGED A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 879GA 53486 DURING A ROUTINE OVERNIGHT SERVICE CHECK MAINTENANCE INSPECTION SANFORD MAINTENANCE REPORTED THAT THE RIGHT MAIN LANDING GEAR DOOR WAS DAMAGED WHEN IT (THE DOOR) VIOLENTLY CONTACTED THE GROUND. THE GEAR DOORS WERE BEING OPENED AS A ROUTINE PART OF THE SERVICE CHECK. THE AIRPLANE HAS BEEN DECLARED NOT AIRWORTHY AS A RESULT OF ENGINEERING EVALUATION OF THE D AMAGE. THE EVIDENCE AT THIS POINT SEEMS TO INDICATE THAT THE DOOR HAS BEEN ALLOWED TO "FREE FALL" TO THE GROUND REPEATE DLY BY MAINTENANCE TECHNICIANS OVER AN EXTENDED PERIOD OF TIME AT VARIOUS STATIONS. THE AIRPLANE WILL ONLY RETURN TO SE RVICE UPON INSTALLATION OF A SERVICEABLE RIGHT MAIN LANDING GEAR DOOR. 2 L 7 2 4F RT A6WE 2007032900157 20070329 00157 NM 2007 3 29 FDKA200702087 1 20070226 A 2720 7G773 PRESSURE SWITCH DHAV DHC8 DHC8102 2809003 NM RUDDER MALFUNCTIONED A FDKA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 801LR 249 047 FDM 6060 ORF-JFK (1855 PHX LCL). CAPTAIN REPORTED A RUDDER FULL PRESS CAUTION LIGHT ILLUMINATED INTERMITTENTLY THROUGHO UT ALL PHASES OF FLIGHT. MX REMOVED AND REPLACED PRESSURE SWITCHES. 2 H 7 2 4T RT A13NM 2007032900164 20070329 00164 NM 2007 3 29 AALA20070486 1 20070312 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 786AN 30250 DFW - EMERGENCY LIGHT AT SEAT 25C HAS MISSING BULB. REPLACED BULB FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007032900166 20070329 00166 WP 2007 3 29 AALA20070501 1 20070315 A 3350 LIGHT DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 582AA 53159 DEN - SEAT MOUNTED EMERGENCY LIGHTS BY GALLEY CART BROKEN. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHTS BY GALLEY CART. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007032900176 20070329 00176 NM 2007 3 29 AALA20070482 1 20070312 A 3350 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9412W 53187 DFW - EMERGENCY LIGHTS ABOVE SLIDE AND AT CAT WALK IN AFT ACCESSORY COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK AT B 5 28 FOR EMERGENCY LIGHTS ABOVE SLIDE AND AT CAT WALK IN AFT ACCESSORY COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F RT 2007032900177 20070329 00177 NM 2007 3 29 DU4R2007074 1 20070317 A 5311 146N1006 FRAME BOEING 757 757232 1384965 NM BS 1300 S26-27R CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 636DL 23763 FOUND CORROSION IN AFT PIT MAIN FRAME UPPER CAP AT BS 1300 S-26 27R. REPAIRED BY FABRICATING AND INSTALLING REPAIR 12 B Y 2 FROM 7075-T6 .071 IAW B757 SRM 53-00-07 FIG 201. 2 L 7 2 4F RT A2NM 2007032900196 20070329 00196 SO 2007 3 29 FDKA200701032 1 20070129 A 5210 14553170005 SEAL EMB 145 EMB145LR 3260212 SO PAX DOOR TORN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 850MJ 145568 FDM RON MCO (1626 PHX LCL). PAX DOOR SEAL TORN AT THE TOP AND SQUEALS IN FLIGHT. MX REPLACED THE DOOR SEAL. 2 L 7 2 4T RT T00011AT 2007032900202 20070329 00202 2007 3 29 FDKA200701033 4 20070129 A 2215 7002260723 SERVO DHAV DHC8 DHC8101 2809002 NM AUTOPILOT SYS MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 805LR 801 039 FDM 6077 JFK-BWI (2111 PHX LCL). AUTO PILOT INOP. MX REMOVED AND REPLACED SERVO. 2 H 7 2 4T RT A13NM 2007032900203 20070329 00203 NM 2007 3 29 DHL2007751519 1 20070320 A 5314 KEELBEAM BOEING 727 727264 138408M NM BS 870-873 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 751DH 22982 LT FWD KEEL BEAM, BS 870, HAS A CRACK BETWEEN TWO FASTENERS. VERIFIED CRACK FROM BS 870 TO BS 873. GAINED ACCESS AS RE Q, CUT OUT DAMAGED AREA 1.875" BY 1" PER SB B727-53-0208. FABRICATED REPAIR DOUBLER FROM 15.5 PH STEEL, .071" BY 8.5" B Y 3.75", PO NR 6522231 PER SB B727-53-0208. HEAT TREATED DOUBLER TO HRC 40.61, KSI 170 AND CADMIUM PLATED PER SB B727-5 3-0208, AMS-H-6875A, AMS27591-3D, AND FASI FORM FAS0036 REV 4. INSTALLED DOUBLER PER SB B727-53-0208. RETURNED ARE TO NORMAL. 2 L 7 3 4F A3WE 2007032900205 20070329 00205 SO 2007 3 29 FDKA200702070 1 20070214 A 5210 14525311401 SEAL EMB 145 EMB145LR 3260212 SO PAX DOOR TORN A FDKA O OTHER O OTHER CR CRUISE 1 SW 07 850MJ 145568 FDM 6146 ATL (1912 PHX LCL). LOUD NOISE IN FLIGHT FROM GALLEY OR PAX DOOR. MX FOUND THE PAX DOOR SEAL WAS TORN. FERRI ED TO CAE WHERE MX REPLACED THE DOOR SEAL. 2 L 7 2 4T RT T00011AT 2007032900216 20070329 00216 SO 2007 3 29 FDKA200701014 1 20070117 A 2797 CONNECTOR EMB 145 EMB145LR 3260212 SO AILERON DIRTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 854MJ 145490 FDM 5969 AVL-ATL (0620 PHX LCL) AILERON SYSTEM 2 INOP. MX CLEANED CONNECTOR & RESECURED AT HYD MANIFOLD. 2 L 7 2 4T RT T00011AT 2007032900226 20070329 00226 NM 2007 3 29 C1HA200778001 1 20070316 A 3610 LINE BOEING 727 727225 1384077 NM CONTROL VALVE LOOSE A C1HA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 678MG 22555 ON CLIMB-OUT FROM DEN, NR 3 EPR STARTED SURGING UP AND DOWN 10 TO 15 PERCENT, SHUT OFF RT PACK, SURGING STOPPED. MADE P RECAUTIONARY LANDING BACK IN DEN CONFIRMED FAULT FOUND 10 SENSE LINES LOOSE ON RT FLOW CONTROL VALVE. TIGHTENED PER STD PRACTICES REF MM 36-12-01. OPS CHECK NORMAL MX FUEL BURN 2780 LBS. 2 L 7 3 4F A3WE 2007032900227 20070329 00227 NM 2007 3 29 QXEA200700388 1 20070228 A 2900 UNKNOWN DHAV DHC8 DHC8202 2809007 NM UNKNOWN A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 350PH 488 SEA FLIGHT NR 2077 INFLIGHT, NR 2 SPU AUX POWER CAUTION LIGHT ILLUMINATED RAN APPROPRIATE CHECKLIST NO OTHER CAUTION LIG HTS AT THE TIME. MAINTENANCE GROUND RAN ENGINES FOR AC POWER 2 SPU AUX POWER CAUTION LIGHT REMAINS EXTINGUISHED WITH AC GEN POWER APPLIED. UNABLE TO INDUCE LIGHT IN NORMAL CONFIGS. CHECK GOOD HYDRAULIC PRESS FROM 2 STBY GOOD. NO PARTS R EPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900228 20070329 00228 NM 2007 3 29 QXEA200700389 1 20070226 A 2910 UNKNOWN DHAV DHC8 DHC8202 2809007 NM HYD SYSTEM UNKNOWN A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 353PH 496 YVR FLIGHT NR 2029, AFTER TAKEOFF DURING FLAP RETRACTION GOT NR 1 ENGINE HYD PUMP CAUTION LIGHT. PRESSURE INDICATED 200 0 PSI ON BOTH STANDBY AND MAIN NR 1 HYDRAULIC PRESSURE GAUGES. WHEN FLAPS WERE UP ALL INDICATIONS WENT BACK TO NORMAL. NO OTHER CAUTION LIGHTS NOTED. PERFORMED EA CHECKLIST. MAINTENANCE INSPECTED NR 1 HYDRAULIC SYSTEM FOR LEAKS. NO LEA KS NOTED. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900240 20070329 00240 SO 2007 3 29 SIMA200707405 1 20070312 A 5347 14530658009 SEAT TRACK EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 15742 4800 145234 FOUND CORROSION ON RIGHT LOWER BOTTOM CABIN SEAT TRACK BETWEEN FRAME 53 TO 58. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032900242 20070329 00242 SO 2007 3 29 SIMA200707407 1 20070312 A 5347 14530659009 SEAT TRACK EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 15742 4800 145234 FOUND CORROSION ON LEFT FORWARD CABIN SEAT TRACK BETWEEN FRAME 18 TO 24. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53 -01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032900254 20070329 00254 NM 2007 3 29 07FDEA01122 1 20070324 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 720D CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 CABIN FLOORBEAM HAS CORROSION ON UPPER SURFACE FS 720D, LBL 24.75 TO LBL 65. REMOVED CORROSION, REMOVED DAMAGE PORTION SR 27-53-034. FABED NEW PARTS PER SR 27-53-034. INSTALLED NEW ANGLES AND NEW FILLER REPAIR IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2007032900287 20070329 00287 EU 2007 3 29 07FDEA01131 1 20070326 A 7830 BULKHEAD AIRBUS 310 A310203 3930313 EU THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 NR 2 ENG RT TR AT DEPLOYED POSN AFT BULKHEAD SUPPORT WEB ON UPPER BALLSCREW CUT OUT CRACKED 2 PLACES. REMOVED DAMAGED S ECTION OF WEB IAW CMM 78-32-02. FABRICATED WEB FROM 2024-0, 0.050C AND HEAT TREATED LOT NR 20410 ON MAE TRAV NR T7/6675 89, DOUBLER FABBED FROM 2024-T3 .063C IAW CMM 78-32-02 FIG 602. INSTALLED WEB IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007032900309 20070329 00309 EA 2007 3 29 A6WA200740114 1 20070311 A 2752 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE T/E FLAP LACK OF LUBE A A6WA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 31 421ZW 7346 FLAPS FAILED AT 20 AFTER DEPARTURE. CLEANED AND LUBRICATED ALL RT FLAP DRIVE SHAFTS. OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900333 20070329 00333 EA 2007 3 29 A6WA200740059 1 20070209 A 5320 601R35050109 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 421ZW 7346 CARGO DOOR SUPPORT BEAM ANGLE THAT ATTACHES TO REAR PRESSURE BULKHEAD FS 621. CRACKED APPROX 1 INCH LONG (ANGLE PN 601R 35050-109). MAINTENANCE DRILLED OFF, REMOVED CRACKED BRACKET, INSTALLED NEW SUPPORT ANGLE PN 601R35050-109 USING HST10A G-6 AND HST110AG-6 HILITES IAW SRM 51-40-11 AND 51-42-21. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900334 20070329 00334 EA 2007 3 29 A6WA200740131 1 20070317 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 415AW 7593 FS 280.0 FLOOR SUPPORT ANGLE PN 600-34017-595 CRACKED APPROX .2 INCHES LONG ON AFT SIDE FS 280.0 OB OF LBL 9.0. (K) [S UP 05-17-07] MAINTENANCE REPAIRED DAMAGED SECTION, DRILLED NEW SECTION OF ANGLE AND SPLICES IAW REO 601R-53-11-136 STEP S 1-6 ANGLE P/N 600-34017-595. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900337 20070329 00337 EA 2007 3 29 A6WA200740060 1 20070209 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 421ZW 7346 LT MLG BATT RIB CRACKED 1 INCH LONG UPPER AFT CORNER MAINTENANCE REPAIRED BATT RIB IWA REO 601R-57-51-046. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900339 20070329 00339 EA 2007 3 29 A6WA200740095 1 20070306 A 5270 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR DEFECTIVE A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 404AW 7294 INFLIGHT, PAX DOOR WARNING MESSAGE. COMPLIED WITH QRH CHECKLIST, LANDED AT 46,000. REMOVED AND REPLACED PS5MB AND PS6M B PROXIMITY SWITCHES IAW AMM 52-70-04. OPS CHECK OF PASSENGER DOOR GOOD. PSEU FOUND NO FAULTS. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900342 20070329 00342 NE 2007 3 29 FDKA200703124 2 20070316 A 7261 OIL SYSTEM DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE LOW A FDKA D RETURN TO BLOCK J WARNING INDICATION NR NOT REPORTED 1 SW 07 805LR 039 FDM 6195 PWM-JFK (0342 PHX LCL). AIRCRAFT RETURNED TO THE GATE DUE TO NR 1 ENGINE LOW OIL PRESSURE WARNING LIGHT ON TAK EOFF ROLL. MX SERVICED OIL. 2 H 7 2 4T 4 T RT A13NM E20NE 2007032900344 20070329 00344 SO 2007 3 29 FDKA200703127 1 20070319 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 849MJ 145534 FDM 6126 ATL-CAK (0904 PHX LCL). PAX DOOR WILL NOT SHUT. MX CHECKED ALIGNMENT OF DOOR AND LUBED DOOR ROLLERS, OPS CHEC K GOOD. 2 L 7 2 4T RT T00011AT 2007032900365 20070329 00365 SO 2007 3 29 FDKA200703120 1 20070314 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA K NONE L NO TEST NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6123 MCO-ATL (1520 PHX LCL). SERVICE DOOR EMERGENCY LIGHT INOP. MX REPLACED THE LIGHT BULB AND OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007032900374 20070329 00374 SO 2007 3 29 FDKA200703093 1 20070301 A 2150 8152912 SWITCH EMB 145 EMB145LR 3260212 SO A/C PACK MALFUNCTIONED A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 851MJ 11648 145572 FDM 5967 ATL-PHF (1606 PHX LCL). CREW REPORTED A PACK 2 OVERLOAD IN FLIGHT AND HAD A SMOKE SMELL WHEN THE PACK WAS ON. MX REMOVED AND REPLACED PACK OVERLOAD SWITCH. 2 L 7 2 4T RT T00011AT 2007032900387 20070329 00387 NE 2007 3 29 FDKA200702068 2 20070212 A 7261 OIL SYSTEM DHAV DHC8 DHC8101 2809002 NM PWA 120 PW120 NE NR 1 ENGINE LOW A FDKA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 805LR 039 FDM 6160 BTV-JFK (1738 PHX LCL). ABORTED TAKEOFF WITH NR 1 ENGINE LOW OIL PRESS WARNING. MX SERVICED WITH 3 QTS OF OIL AND IT OPS CHECKED GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2007033000016 20070330 00016 NM 2007 3 30 DLM90070252 1 20070313 A 5280 SKIN DOUG MD90 MD9030 3023690 NM NLG DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 FUSELAGE CRACKED AND RIVETS PULLED THROUGH AT LT NOSE GEAR STRUT DOOR AFT HINGE CUT OUT. REPAIR PER SRM 53-05D REF FIG 62 PG1 REF N/R 1000-0004 AT HMV2. 2 L 7 2 4F RT A6WE 2007033000021 20070330 00021 NM 2007 3 30 DLM90070256 1 20070312 A 5230 SKIN DOUG MD90 MD9030 3023690 NM AFT CARGO DOOR DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 FOUND AFT CARGO DOOR SKIN DENTED 2 AREAS. REPAIR IAW SRM 53-30-02 PG 20 FIG 7 SH1 REF N/R 8300-0015. 2 L 7 2 4F RT A6WE 2007033000028 20070330 00028 NM 2007 3 30 DLM90070260 1 20070323 A 5311 FRAME DOUG MD90 MD9030 3023690 NM FS 1364 L26-30R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 AFT CARGO PIT STA 1364 AFT SIDE OF FRAME CORRODED LONG 26-30R. REPAIR PER SRM 53-00-01 REF N/R 1600-0286. 2 L 7 2 4F RT A6WE 2007033000029 20070330 00029 2007 3 30 FDKA200703115 4 20070313 A 2215 4006719906 SERVO EMB 145 EMB145LR 3260212 SO AUTOPILOT SYS MALFUNCTIONED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 855MJ 10563 145614 FDM 6007 HPN- ATL . AUTO PILOT FAIL MESSAGE. MX REMOVED AND REPLACED AILERON AND ELEVATOR SERVO. 2 L 7 2 4T RT T00011AT 2007033000036 20070330 00036 SO 2007 3 30 FDKA200703117 1 20070313 A 5210 MECHANISM EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 831MJ 145273 FDM 6099 ATL-LEX (0642 PHX LCL). MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE. MX LUBED AND ADJUSTED THE MAIN CABIN DOOR AND OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007033000044 20070330 00044 NM 2007 3 30 HALA0700134 1 20070326 A 3150 UNKNOWN BOEING 767 76733A 1385209 NM UNKNOWN A HALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 13 581HA 28141 ETOPS SIGNIFICANT SYSTEM, WXR FAIL DISPLAY ON HSI WITH L SYSTEM SELECTED. WXR TEST DISPLAY WXR FAIL RT ON HSI. PERFORM ED FIM 34-43-00. BITE TEST PASSED, NO FAULTS NOTED. MSG CLEARED. 2 L 7 2 4F RT A1NM 2007033000049 20070330 00049 NM 2007 3 30 DHL2007786505 1 20070328 A 5754 65172941314 RIB BOEING 727 727214 138407R NM NR 3 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 NR 3 SLAT IB AND OB RIBS WS 515 AT ACT ATTACH ARE CRACKED IN THE AFT LOWER CORNERS. REMOVED AND REPLACED RIBS I/B AND O /B AT NR 3 SLAT WS 515 IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007033000057 20070330 00057 SO 2007 3 30 SWIA200718061 1 20070320 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 299SW 12268 12268 120329 FIRST SECTION OF EMERGENCY FLOOR LIGHTING DOES NOT ILLUMINATE. REPLACED FORWARD EMERGENCY LIGHTING BATTERY PACK. OPERA TIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007033000058 20070330 00058 EA 2007 3 30 SWIA200718062 1 20070324 A 2150 A/C PACK CNDAIR CL600 CL6002C10 1390015 EA LEFT SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 709SK 10159 FOUND LEFT PACK PRODUCES SMOKE/HAZE IN COCKPIT AND CABIN. COULD NOT DUPLICATE DISCREPANCY. 2 L 7 2 4F RT A21EA 2007033000059 20070330 00059 EA 2007 3 30 SWIA200718063 1 20070323 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 776SK 10241 FOURTH EMERGENCY LIGHT POD INOP. REPLACED FOURTH CEILING EMERGENCY FLOOD LIGHT IAW AMM 33-51-09. OPERATIONAL CHECKS GO OD. 2 L 7 2 4F RT A21EA 2007033000060 20070330 00060 NM 2007 3 30 DL76G070229 1 20070322 A 2530 828450407M0DA OVEN BOEING 767 767332 1382001 NM AFT GALLEY INOPERATIVE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 173DZ 29692 FOUND GALLEY REAR CENTER OVEN INOP, FWD TO MCO AND PLACARD PER MEL 25-20-01H CB PULLED AND COLLARED DUE TO AFT GALLEY OV EN NR 6 CB POPPED WITH REPORT OF VISABLE ELECTRIC FLASH. REPLACED OVEN CKS GOOD REMOVED MCO AND PLAC. 2 L 7 2 4F RT A1NM 2007033000099 20070330 00099 EU 2007 3 30 07FDEA00924 1 20070316 A 5340 A53974003236 ATTACH FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 813FD 500 OLD MISDRILLED HOLE IN THE CLIP AT C68 LT, P42-P43, CLIP SHOWN IN SRM 553-17-13/FIG.9/SH.13/ITEM420. REPAIR PERFORMED B Y REPLACEMENT OF AFFECTED STRUCTURE COMPONENT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007033000102 20070330 00102 EU 2007 3 30 07FDEA00928 1 20070316 A 5310 DOOR FRAME AIRBUS 310 A310304 3930339 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 OLD MARKS ON FWD CARGO DOOR FRAME FWD LOWER CORNER. REPAIR WAS PERFORMED BY BLEND OUT WITH LHT SDR. 2 L 7 2 4F RT A35EU 2007033000118 20070330 00118 NM 2007 3 30 HALA0700115 1 20070319 A 2150 285T01771 SENSOR BOEING 767 76733A 1385209 NM RT A/C PACK MALFUNCTIONED A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 582HA 28139 BLX TURN BACK, ETOPS SIGNIFICANT SYSTEM, RT PACK INOP. REMOVED AND REPLACED OUTLET COMPRESSOR TEMP SENSOR AUTO SIDE PER TASK 21-51-06-404-011. OPS CK GOOD. 2 L 7 2 4F RT A1NM 2007033000119 20070330 00119 GL 2007 3 30 HALA0700118 2 20070319 A 7510 2790583108 VALVE BOEING 767 767332 1382001 NM GE CF6 CF680C2* GL ANTI ICE SYS FAILED A HALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 13 598HA 24656 24656 23278 ETOPS SIGNIFICANT SYSTEM, AFTER ENG START RT ENG ANTI-ICE VALVE FAIL TO OPEN ALSO EICAS MESSAGE RT ENG ANTI-ICE. REMOVE D, REPLACED FUNCTIONAL AND LEAK CHECKED GOOD THE NR 2 ENGINE ANTI-ICE VALVE IAW MM 30-21-03. 2 L 7 2 4F 4 F RT A1NM E23EA 2007033000124 20070330 00124 NM 2007 3 30 QXEA200700371 1 20070313 A 3250 STEERING SYS DHAV DHC8 DHC8202 2809007 NM NLG INOPERATIVE A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 360PH 515 SEA FLIGHT NR 2234, LOUD NOISE FROM NOSE WHEEL STEEERING, NOSE WHEEL STEERING INOP. MAINTENANCE PLACED ON MEL 2 H 7 2 4T RT A13NM 2007033000125 20070330 00125 SO 2007 3 30 FDKA200702077 1 20070221 A 4920 APU EMB 145 EMB145LR 3260212 SO APU BAY ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 831MJ 145273 FDM 6118 DAY-MCO (0643 PHX LCL). CREW REPORTED APU FIRE MESSAGE WITH SMOKE SMELL FROM APU. MX INSPECTED APU NO DEFECTS FOUND, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007033000127 20070330 00127 EA 2007 3 30 QXEA200700377 1 20070214 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA MAIN PAX LACK OF LUBE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 601QX 10009 DEN - ON FLIGHT 4340, MAIN CABIN DOOR HARD TO OPEN. MAINTENANCE INSPECTED AND FOUND INNER HANDLE DETENT ASSY DIRTY. CL EANED AND LUBED ASSY. OPERATIONAL CHECKED GOOD. NO DEFECTS OR FAULT NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS RE PLACED. 2 L 7 2 4F RT A21EA 2007033000130 20070330 00130 SO 2007 3 30 FDKA200702043 1 20070204 A 2750 3634001019 SHAFT EMB 145 EMB145LR 3260212 SO T/E FLAP UNKNOWN A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 840MJ 13549 145429 FDM 5971 TRI-MCO (1353 PHX LCL). CREW REPORTED FLAPS FAIL AND FLAP LOW SPEED MESSAGE. MX REMOVED AND REPLACED FLEX SHA FTS AND ADJUSTED O/B ACTUATOR. 2 L 7 2 4T RT T00011AT 2007033000131 20070330 00131 NM 2007 3 30 FDKA200702045 1 20070204 A 3150 WARNING SYSTEM DHAV DHC8 DHC8102 2809003 NM MALFUNCTIONED A FDKA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 804LR 324 FDM 208 JFK-PVD (2136 PHX LCL). ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN SOUNDED. MX TROUBLESHOT AND OPS CHECKED GO OD. 2 H 7 2 4T RT A13NM 2007033000133 20070330 00133 SO 2007 3 30 FDKA200701025 1 20070125 A 2810 2810051102 VENT EMB 145 EMB145LR 3260212 SO FUEL SYSTEM MALFUNCTIONED A FDKA O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 07 829MJ 7604 145228 FDM 5964 ATL-HPN (1603 PHX LCL). FUEL COMING FROM VENT WHILE SINGLE POINT REFUELING. MX REPLACED VENT VALVE. 2 L 7 2 4T RT T00011AT 2007033000135 20070330 00135 2007 3 30 FDKA200701003 4 20070105 A 2210 YAW DAMPER CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT SYS DISENGAGED A FDKA O OTHER O OTHER TO TAKEOFF 1 SW 07 806LR 093 FDM 6189 BDL-JFK (0520 PHX LCL). ABORTED TAKEOFF DUE TO THE YAW DAMPNER SYSTEM DISENGAGING WHEN INITIATING TAKEOFF ROLL . MX TROUBLESHOT AND OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2007033000136 20070330 00136 SO 2007 3 30 FDKA200701004 1 20070106 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT SMOKE A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 9936 ATL-HSV (0511 PHX LCL). CREW REPORTED SMOKE IN THE CABIN AND FLIGHT DECK. MX SET NR 2 PACK ON FULL HOT AND NO SMOKE NOTED. 2 L 7 2 4T RT T00011AT 2007033000137 20070330 00137 NM 2007 3 30 FDKA200702072 1 20070216 A 3150 7002537 CONTROL BOX DHAV DHC8 DHC8101 2809002 NM COCKPIT MALFUNCTIONED A FDKA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 809LR 1190 083 FDM 6185 JFK-PHL (1313 PHX LCL). AIRCRAFT REJECTED TAKEOFF DUE TO MASTER WARNING LIGHT ILLUMINATED. MX REMOVED AND REP LACED ADV LIGHT CONT BOX. 2 H 7 2 4T RT A13NM 2007033000138 20070330 00138 NM 2007 3 30 FDKA200702073 1 20070217 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM LAVATORY MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 810LR 003 FDM 6190 JFK-BDL (1255 PHX LCL). LAVATORY SMOKE DETECTOR BEEPED. PILOT DE-POWERED AND RE-POWERED THE ACFT AND THE FLIG HT ATTENDANT TESTED THE SMOKE DETECTOR AND NO DEFECTS WERE NOTED. 2 H 7 2 4T RT A13NM 2007033000141 20070330 00141 NM 2007 3 30 AWXA200700384 1 20070317 A 2720 65C370539 PCU BOEING 737 7373B7 1384580 NM RUDDER FAILED A AWXA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 28 332AW 46718 1824 23384 PHX - CREW REPORTED DURING CLIMB THEY HAD TO INPUT 5 DEG LEFT RUDDER TO MAINTAIN WINGS LEVEL FLIGHT. MX REPLACED THE RU DDER PCU AND RIGGED IAW MM 27-21-00-5. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2007033000142 20070330 00142 NM 2007 3 30 AWXA200700410 1 20070307 A 5320 69165096 INTERCOSTAL BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED INTERCOSTAL CLIP, BS 348.2, S16L. REPLACED INTERCOSTAL CLIP, BS 348.2, S16L IAW AWA ER 03-5312-0708 3-ES1. 2 L 7 2 4F RT A16WE 2007033000148 20070330 00148 NM 2007 3 30 AWXA200700415 1 20070307 A 5320 66142081 INTERCOSTAL BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED INTERCOSTAL WEB, BS 294.5, S11L. REPLACED INTERCOSTAL WEB, BS 294.5, S11L IAW AWA ER 03-5312-07083- ES1. 2 L 7 2 4F RT A16WE 2007033000149 20070330 00149 NM 2007 3 30 AWXA200700416 1 20070307 A 5320 6517684638 INTERCOSTAL BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED INTERCOSTAL WEB, BS 294.5, S12L. REPLACED INTERCOSTAL WEB, BS 294.5, S12L IAW AWA ER 03-5312-07083- ES1. 2 L 7 2 4F RT A16WE 2007033000151 20070330 00151 NM 2007 3 30 AWXA200700418 1 20070307 A 5320 65176856 INTERCOSTAL BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED INTERCOSTAL STRAP, BS 348.2, S16L. REPLACED INTERCOSTAL STRAP, BS 348.2, S16L IAW AWA ER 03-5312-07 083-ES1. 2 L 7 2 4F RT A16WE 2007033000152 20070330 00152 NM 2007 3 30 AWXA200700419 1 20070307 A 5340 69482042 ATTACH FITTING BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED FRAME VERTICLE CLIP, BS 360, S14L - S15L. REPLACED VERTICLE CLIP, BS 360, S14L - S15L IAW AWA ER 0 3-5312-07083-ES1. 2 L 7 2 4F RT A16WE 2007033000154 20070330 00154 NE 2007 3 30 FDKA200702083 2 20070224 A 7261 OIL SYSTEM DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ENGINE LOW A FDKA C ABORTED TAKEOFF J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 07 810LR 003 FDM 6175 SYR-JFK (0615 PHX LCL). CREW ABORTED T/O AND RETURNED TO THE GATE FOR NR 1 ENGINE LOW OIL PRESSURE WARNING LIG HT ILLUM AND SMOKE IN THE CABIN. MX SERVICED ENG OIL 5 QTS RIGHT AND 3 QTS LEFT. PERFORMED POWER RUNS WITH NO LEAKS NO TED. 2 H 7 2 4T 4 T RT A13NM E20NE 2007033000155 20070330 00155 EU 2007 3 30 07FDEA00929 1 20070316 A 5280 SKIN AIRBUS 310 A310304 3930339 EU ZONE 800 DELAMINATED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD C1581 593 OLD REPAIR ON LT MLG DOOR, DELAMINATED SKIN. REPAIR WAS PERFORMED BY FILL OUT THE DELAMINATED AREA IAW LHT SDR. 2 L 7 2 4F RT A35EU 2007033000157 20070330 00157 NM 2007 3 30 DHL2007786504 1 20070328 A 5310 TORQUE BOX BOEING 727 727214 138407R NM BS 1329 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 756AT 21692 CRACK AT LIGHTENING HOLE, RT LOWER TORQUE BOX STA 1329. STOPPED DRILLED 0.250" DIAMETER HOLE AT LIGHTENING HOLE RT LOWE R TORQUE BOX STA 1329 IAW B727 SRM 51-40-2. NDT C/W HFEC FOR CRACK STOP VERIFED, IAW B727 NDTM, PT6 51-00-00 FIG 23. F ABRICATED DOUBLER REPAIR AT LIGHTENING HOLE RT LOWER TORQUE BOX STA 1329 MATERIAL USED 7075T6 .040 PO NR 9003110 SIZE 5 3/4" BY 3 1/2" IAW B727 SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. TREATED ALODINE AND PRIMED PART AND AREA IAW B727 SRM 51-1 0-2. INSTALLED DOUBLER REPAIR AT LIGHTENING HOLE STA 1329 IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007033000172 20070330 00172 NM 2007 3 30 FDKA200703099 1 20070307 A 2120 UNKNOWN DHAV DHC8 DHC8102 2809003 NM COCKPIT SMOKE A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 803LR 322 FDM 6189 BDL-JFK (0745 PHX LCL). SMOKE INTO THE COCKPIT AND CABIN DURING TAXI OUT. GROUND RAN AIRCRAFT WITH BLEED ON A ND NO DEFECTS NOTED. 2 H 7 2 4T RT A13NM 2007033000173 20070330 00173 SO 2007 3 30 FDKA200701012 1 20070116 A 2750 FLAP EMB 145 EMB145LR 3260212 SO WING MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 840MJ 145429 FDM 6068 ATL. FLAP FAIL AT ZERO DEGREES IN FLIGHT. MX RESET THE FLAP SYSTEM AND OPS CHECK NORMAL ON THE GROUND. 2 L 7 2 4T RT T00011AT 2007033000174 20070330 00174 EU 2007 3 30 07FDEA00932 1 20070316 A 5230 SKIN AIRBUS 310 A310304 3930339 EU ZONE 800 DENTED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 OLD DENT REPAIR ON BULK CARGO DOOR OUTER SKIN BETWEEN BEAM 1-2 AND BEAM 4-5. REPAIR WAS PERFORMED BY INSTALLING EXTERNA L DOUBLER BETWEEN BEAM 4-5 AND BLEND OUT BETWEEN BEAM 1-2 IAW LHT SDR. 2 L 7 2 4F RT A35EU 2007033000176 20070330 00176 GL 2007 3 30 FDKA200701013 2 20070116 A 7261 4252070 GARLOCK SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 ENGINE LEAKING A FDKA O OTHER O OTHER CR CRUISE 1 SW 07 845MJ 145502 FDM 9963 BNA-JFK (1610 PHX LCL). NR 2 ENG SHUTDOWN IN FLIGHT DUE TO LOW OIL PRESSURE ON CLIMBOUT. MX REMOVED AND REPLA CED NR 2 GEN GARLOCK SEAL. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007033000178 20070330 00178 EU 2007 3 30 07FDEA00938 1 20070316 A 4910 LONGERON AIRBUS 310 A310304 3930339 EU ZONE 800 BENT A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 APU ACCESS DOOR LT/RT LOWER LONGERON, OLD BENT REPAIR. REPAIR WAS PERFORMED BY CUT OUT AND INSTALLATION OF NEW LONGERON SECTION. 2 L 7 2 4F RT A35EU 2007033000180 20070330 00180 SO 2007 3 30 FDKA200701021 1 20070123 A 2750 3633501003 SENSOR EMB 145 EMB145LR 3260212 SO T/E FLAP MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 840MJ 145429 FDM 9962 BNA-RDU (1007 PHX LCL). FLAP LOW SPEED EICAS MESSAGE. MX REPLACED FLAP VELOCITY SENSOR. 2 L 7 2 4T RT T00011AT 2007033000181 20070330 00181 SO 2007 3 30 FDKA200702092 1 20070227 A 2742 3622001015 ACTUATOR EMB 145 EMB145LR 3260212 SO HORIZ STAB MALFUNCTIONED A FDKA O OTHER O OTHER CR CRUISE 1 SW 07 826MJ 145214 FDM 6004 LEX-ATL (1831 PHX LCL). AUTOPILOT FAILED IN FLIGHT ON CLIMBOUT. MX REMOVED AND REPLACED HORIZONTAL STAB ACTUA TOR. 2 L 7 2 4T RT T00011AT 2007033000182 20070330 00182 SO 2007 3 30 FDKA200701018 1 20070120 A 2750 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO FLAP SYSTEM MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 831MJ 145273 FDM 5969 ATL-DAY (0918 PHX LCL). FLAP LOW SPEED MESSAGE. MX RESET SYSTEM. 2 L 7 2 4T RT T00011AT 2007033000183 20070330 00183 NM 2007 3 30 SWAA071573 1 20070325 A 2710 6940081 CONTROL ROD BOEING 737 7373H4 1384600 NM LT AILERON WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED 14Y CHECK, LEFT AILERON FAILED THE FREEPLAY CHECK. REMOVED AND REPLACED LEFT AILERON CONTROL ROD ASSY. 2 L 7 2 4F RT A16WE 2007033000184 20070330 00184 NM 2007 3 30 SWAA071577 1 20070326 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 469WN 33859 EEPLS SECTION OUT OF RECEPTACLE AT FWD END. REINSTALLED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2007033000185 20070330 00185 NM 2007 3 30 SWAA071581 1 20070326 A 3350 PL2230LH00 STRIP BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 227WN 34450 DURING SCHEDULED HC2 CHECK, FOUND EEPLS STRIP CRACKED AT ROW 1 ABC. REMOVED AND REPLACED EEPLS STRIP SECTION PER MM. 2 L 7 2 4F RT A16WE 2007033000186 20070330 00186 NM 2007 3 30 SWAA071561 1 20070324 A 3350 079123 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 406WN 27894 EEPLS LENS LOOSE AT FWD END. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007033000187 20070330 00187 NM 2007 3 30 SWAA071560 1 20070324 A 3350 079123 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 247WN 32508 EEPLS LIGHT LENS LOOSE AT FWD END. REMOVED AND REPLACED LENS ASSY PER MM. 2 L 7 2 4F RT A16WE 2007033000188 20070330 00188 NM 2007 3 30 SWAA071565 1 20070324 A 3350 6042221 BATTERY PACK BOEING 737 737301 1384611 NM CABIN FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED BRDG CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY PACK M9137 FAULTY. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2007033000190 20070330 00190 NM 2007 3 30 SWAA071567 1 20070324 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E+17, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007033000191 20070330 00191 NM 2007 3 30 SWAA071566 1 20070324 A 5330 6545774 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 793, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007033000192 20070330 00192 NM 2007 3 30 SWAA071563 1 20070324 A 5753 6546434 FLAP BOEING 737 7373H4 1384600 NM LT WING DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND LEFT WING INBOARD AFT T/E FLAP DISBONDED AT AFT EDGE. REPAIRED FLAP PER SRM & BAC DRA WING. 2 L 7 2 4F RT A16WE 2007033000193 20070330 00193 NM 2007 3 30 SWAA071562 1 20070324 A 5311 6546532 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, STR 26R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007033000197 20070330 00197 NM 2007 3 30 SWAA071570 1 20070325 A 3350 079123 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 217JC 34232 EEPLS LENS BROKEN AT FWD END. REMOVED AND REPLACED LENS ASSY PER MM. 2 L 7 2 4F RT A16WE 2007033000201 20070330 00201 NM 2007 3 30 SWAA071585 1 20070327 A 5330 6545768 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007033000202 20070330 00202 NM 2007 3 30 SWAA071583 1 20070326 A 5330 6545877 SKIN BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER AFT CORNER CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007033000203 20070330 00203 NM 2007 3 30 SWAA071578 1 20070326 A 5755 6546452 SKIN BOEING 737 7373H4 1384600 NM SPOILER PUNCTURED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED SERVICE CHECK, FOUND NR 4 GROUND SPOILER PUNCTURED AT UPPER SURFACE. REMOVED AND REPLACED SPOILER ASSY PER MM. 2 L 7 2 4F RT A16WE 2007033000204 20070330 00204 NM 2007 3 30 SWAA071584 1 20070327 A 5330 6550531 SKIN BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 715SW 27849 FUSELAGE SKIN CRACKED AT EXTERNAL POWER ACCESS DOOR AFT LOWER CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007033000205 20070330 00205 NM 2007 3 30 SWAA071576 1 20070326 A 2560 6557463 HOOK BOEING 737 7377H4 1384404 NM R1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 454WN 29851 R1 DOOR EVACUATION SLIDE GIRT BAR ATTACH HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2007033000207 20070330 00207 NM 2007 3 30 SWAA071579 1 20070326 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 6 ABC. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2007033000209 20070330 00209 2007 3 30 ASAA0781550 4 20070313 A 2565 D29984213 SLIDE DOUG DC9 DC983 3022083 WP TAILCONE MALFUNCTIONED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 969AS 52326 2986 53063 AFT ACCY COMPARTMENT EMERGENCY ESCAPE SLIDE FAILED TO DEPLOY DURING DEPLOYMENT TEST. INDICATION WAS THAT THE TAIL CONE STRAP (LANYARD) DETACHED FROM THE SLIDE COVER VELCRO TAB BEFORE THE COVER COULD BE PULLED OPEN. REPLACED COVER VELCRO T AB AND RETESTED SUCCESSFULLY ON 3-26-07. ENGINEERING IS NOW CONSIDERING ESTABLISHMENT OF A TAB CONDITION CHECK. 2 L 7 2 4F RT A6WE 2007033000212 20070330 00212 WP 2007 3 30 ASAA0781553 1 20070328 A 5321 99365533 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 CABIN FLOOR PANEL CORRODED. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007033000214 20070330 00214 WP 2007 3 30 ASAA0781555 1 20070328 A 5321 99365465 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 CABIN FLOOR PANEL PUNCTURED. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007033000215 20070330 00215 WP 2007 3 30 ASAA0781556 1 20070328 A 5321 993053867 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 CABIN FLOOR PANEL WEB IS CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-70. 2 L 7 2 4F RT A6WE 2007033000217 20070330 00217 NM 2007 3 30 HALA0700104 1 20070314 A 3350 LIGHT BOEING 767 76733A 1385209 NM CABIN INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 581HA 28141 FLOOR PROXIMITY EMERGENCY ESCAPE PATH, LIGHTING AT 1L DOOR CROSS AISLE INOPERATIVE. REPLACED CROSS PATH LIGHTING IN F/C CABIN BETWEEN, 1L AND 1R DOOR. OPS CHECK NORMAL, OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007033000221 20070330 00221 WP 2007 3 30 ASAA0781560 1 20070329 A 5330 595305077 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 FUSELAGE SKIN DENTED. REMOVED DAMAGED AREA. INSTALLED SKIN FILLER INTERNAL FINGER DOUBLERS INTERNAL REPAIR DOUBLERS AN D INTERNAL REPAIR STRAPS PER SRM 53-04. 2 L 7 2 4F RT A6WE 2007033000223 20070330 00223 WP 2007 3 30 ASAA0781562 1 20070329 A 5347 593054765 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE N FALSE WARNING IN INSP/MAINT 1 NM 02 969AS 53063 CABIN SEAT TRACK CORRODED. REMOVED DAMAGED SECTION OF TRACK. INSTALLED REPAIR TRACK AND SPLICE PER SRM 53-05. 2 L 7 2 4F RT A6WE 2007033000224 20070330 00224 NM 2007 3 30 HALA0700105 1 20070314 A 7830 SPRING BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE T/R BLOCKER DOOR BROKEN A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, ON ARRIVAL PDX FOUND NR 1 ENG RT THRUST REVERSER BLOCKER DOOR 4TH FROM TOP BLOCKER DOOR SPRING BROKEN. REMOVED AND REPLACED DOOR IAW MM78-31-14-004-002-N00. INSTALLED NEW SPRING, REINSTALLED BLOCKER DOOR IAW MM 7 8-31-14-404-011-N00, OPERATED T/R SEVERAL TIMES OPS NML. 2 L 7 2 4F 4 F RT A1NM E24NE 2007033000225 20070330 00225 NM 2007 3 30 HALA0700110 1 20070315 A 8011 35054367 STARTER BOEING 767 767300 1385204 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE LEAKING A HALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 592HA 9625 9625 33468 ETOPS SIGNIFICANT SYSTEM, NR 2 ENG STARTER LEAKING OIL. REMOVED AND REPLACED NR 2 ENG STARTER PER AMM 80-11-01, LEAK AN D SECURITY CHECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007033000226 20070330 00226 WP 2007 3 30 ASAA0781563 1 20070329 A 5753 591004241 DOUBLER DOUG DC9 DC983 3022083 WP FLAP VANE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 LEFT WING OUTBOARD FLAP CENTER VANE IS CHAFED ON EXISTING REPAIR DOUBLER. REPLACED DOUBLER PER SRM 51-70-2. 2 L 7 2 4F RT A6WE 2007033000229 20070330 00229 WP 2007 3 30 ASAA0781564 1 20070329 A 5753 59304964 DOUBLER DOUG DC9 DC983 3022083 WP FLAP VANE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 RIGHTHAND OUTBOARD FLAP VANE LEADING EDGE IS GOUGED AT PREVIOUS REPAIR. REPLACED EXISTING REPAIR DOUBLER PER SRM 51-70- 2. 2 L 7 2 4F RT A6WE 2007033000230 20070330 00230 NM 2007 3 30 HALA0700109 1 20070315 A 8012 9798585 START VALVE BOEING 767 767300 1385204 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE STUCK A HALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 13 592HA 11818 11818 33468 ETOPS SIGNIFICANT SYSTEM, NR 2 ENG START VALVE DOES NOT OPEN. REMOVED AND REPLACED NR 2 ENG START VALVE PER AMM80-11-02 LEAK AND SECURITY CHECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007033000231 20070330 00231 WP 2007 3 30 ASAA0781565 1 20070329 A 5753 591004336 VANE DOUG DC9 DC983 3022083 WP T/E FLAP GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 RIGHTHAND OUTBOARD FLAP OUTBOARD VANE IS GOUGED. INSTALLED REPAIR DOUBLER PER SRM 51-70-2. 2 L 7 2 4F RT A6WE 2007033000235 20070330 00235 EU 2007 3 30 07FDEA00944 1 20070316 A 5742 ATTACH FITTING AIRBUS 310 A310304 3930339 EU ZONE 400 CHAFED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 PYLON NR 2, CHAFING MARKS ON INBOARD SIDE OF PYLON-TO-ENGINE ATTACH FITTING. REPAIR WAS PERFORMED BY BLEND OUT AND REST ORE PROTECTION. 2 L 7 2 4F RT A35EU 2007033000236 20070330 00236 NM 2007 3 30 ASAA0741544 1 20070326 A 5320 6517684678 STRAP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 STRINGER 16L STRAP ON INTERCOSTAL BROKEN. REPLACED STRAP IAW SRM 53-10-14. 2 L 7 2 4F RT A16WE 2007033000237 20070330 00237 EU 2007 3 30 07FDEA00945 1 20070316 A 5754 WEB AIRBUS 310 A310304 3930339 EU ZONE 500 CHAFED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 CHAFING MARK AT BACK WALL OF KRUEGER FLAP CHAMBER. REPAIR WAS PERFORMED BY BLEND OUT AND REPROTECT. 2 L 7 2 4F RT A35EU 2007033000238 20070330 00238 EU 2007 3 30 07FDEA00946 1 20070316 A 5712 RIB AIRBUS 310 A310304 3930339 EU ZONE 600 CHAFED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 KRUEGER BOX RT, DAMAGED REPAIR, ABRASION IN AN SUPPORT FLANGE OF RIB 2B. REPAIR WAS PERFORMED BY BLEND OUT. 2 L 7 2 4F RT A35EU 2007033000239 20070330 00239 NM 2007 3 30 ASAA0741545 1 20070326 A 5320 6517684Y642 INTERCOSTAL BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 STRINGER 7L INTERCOSTAL CRACKED. REPLACED INTERCOSTAL IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007033000240 20070330 00240 EU 2007 3 30 07FDEA00947 1 20070316 A 5730 SKIN AIRBUS 310 A310304 3930339 EU ZONE 600 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 RT WING BOTTOM SKIN PANEL NR 2, AFT OF REAR SPAR INBOARD OF RIB 11 CRACKED. REPAIR WAS PERFORMED IAW REPAIR DRAWING R57 2-49152-001 AND SB A310-57-2066 (DOUBLER INSTALLED). 2 L 7 2 4F RT A35EU 2007032900220 20070329 00220 NM 2007 3 29 FDKA200702064 1 20070211 A 2910 HYDRAULIC LINE DHAV DHC8 DHC8101 2809002 NM NR 2 ENGINE LOOSE A FDKA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 802LR 205 FDM 6199 JFK-BDL (1138 PHX LCL). NUMBER 2 ENGINE SMOKES AFTER SHUT DOWN. MX TIGHTENED HYD LINE FROM EDP. 2 H 7 2 4T RT A13NM 2007032900225 20070329 00225 WP 2007 3 29 NWAA071029989 1 20070221 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 288-375 DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8945E 47181 DURING GROUND OPERATIONS, BELT LOADER IMPACTED FUSELAGE CAUSING DAMAGE TO LOWER BELLY SKIN L26R-L26L AT BS 288-375 AND U PPER LT FUSELAGE SKIN L26L-L23L AT BS 305-361. REPAIRED PER EA 99-206446. 2 L 7 2 4F A6WE 2007032900229 20070329 00229 NM 2007 3 29 QXEA200700387 1 20070225 A 3010 UNKNOWN DHAV DHC8 DHC8202 2809007 NM DE ICE SYS UNKNOWN A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 347PH 480 PSC FLIGHT NR 2121, LEFT INBOARD DEICE LIGHT CONTINUOUSLY ILLUMINATED ON WING EVEN LIT ON GROUND AFTER TERMINATING CHECK LIST COMPLETE. MAINTENANCE PERFORMED FUNCTIONAL TEST OF AIRFRAME DEICING SYSTEM. NO DEFECTS NOTED. NO PARTS REPLACED . AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900231 20070329 00231 SO 2007 3 29 SWIA200718027 1 20070315 A 5413 STRINGER EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 215SW 120281 LEFT ENGINE MID COWL FORWARD OUTBOARD STRINGER CRACKED, DISCOVERED DURING E-6 INSPECTION. REPLACED FORWARD OUTBOARD STR INGER AT LEFT ENGINE MID COWL IAW SRM 51-40-02 SEE RII 54-900-1000. 2 L 7 2 4T RT A31SO 2007032900239 20070329 00239 SO 2007 3 29 SIMA200707404 1 20070312 A 5347 14530659009 SEAT TRACK EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 15742 4800 145234 FOUND CORROSION ON LEFT LOWER BOTTOM CABIN SEAT TRACK BETWEEN FRAME 53 TO 58. REMOVED AND REPLACED SEAT TRACK IAW EMB A MM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R1. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032900244 20070329 00244 SO 2007 3 29 SIMA200707411 1 20070312 A 5347 14532605003 SEAT TRACK EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 15742 4800 145234 FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 30 TO 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01- 06. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032900251 20070329 00251 SO 2007 3 29 SIMA200707412 1 20070312 A 5347 14532606011 SEAT TRACK EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 649PP 15742 4800 145234 FOUND CORROSION ON LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 18 TO 24. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-0 6. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007032900253 20070329 00253 WP 2007 3 29 07FDEA01117 1 20070323 A 5743 ARB0622 BOLT DOUG MD10 MD1010F 3022112 WP LT MLG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 LT MAIN LANDING GEAR SUPPORT FITTING-FWD TRUNNION BOLT DOES NOT TAKE GREASE AND IS FROZEN. UPON REMOVAL, FOUND BOLT COR RODED. REPAIRED BOLT PER SEQ NR 13 EA 8-5710-10593 "LT MLG SUPPORT FITTING, FWD TRUNNION BOLT (FROZEN)". 2 L 7 3 4F RT A22WE 2007032900261 20070329 00261 NM 2007 3 29 FDKA200702080 1 20070223 A 2120 UNKNOWN DHAV DHC8 DHC8102 2809003 NM CABIN SMOKE A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 803LR 322 FDM 6209 JFK (2342 PHX LCL). AIRCRAFT RETURNED TO THE FIELD WITH SMOKE HAZE IN THE CABIN. MX RAN ENG, OPERATED THE PAC KS AND ALL OPS CHECKS WERE GOOD. 2 H 7 2 4T RT A13NM 2007032900274 20070329 00274 NM 2007 3 29 QXEA200700396 1 20070319 A 6123 AUTOFEATHER SYS DHAV DHC8 DHC8202 2809007 NM NR 1 NO TEST A QXEA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 NM 09 358PH 506 SEA FLIGHT NR 2203, NR 1 WOULD NOT AUTOFEATHER DURING AUTOFEATHER TEST. MAINTENANCE COMPLIED WITH AUTOFEATHER SYSTEM AN D POWER UPTRIM TEST NUMEROUS TIMES. OPERATION CHECK GOOD EACH TIME. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007032900303 20070329 00303 EA 2007 3 29 A6WA200740140 1 20070318 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 416AW 7603 RT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX .8 INCHES LONG. (K) [SUP 05-09-07] MAINTENANCE REMOVED AND REPLACED RIGHT FS 625 INTERCOSTAL AT STRINGER 14R IAW CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900319 20070329 00319 EA 2007 3 29 A6WA200740065 1 20070217 A 5340 601R3111357 FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT IB, OB CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 448AW 7814 FS 280.00 CLIPS ARE CRACKED .2500 INCH IN UPPER RADIUS IB AND OB RBL 9. (K) MAINTENANCE REMOVED AND REPLACED FS 280 CL IPS IB AND OB OF RBL 9 MFG STANDARD REPAIR NR 601R-53-0057A, STEPS 1 THRU 4. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900322 20070329 00322 EA 2007 3 29 A6WA200740134 1 20070317 A 5340 FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 415AW 7593 FS 280.0 FLOOR SUPPORT CLIPS PN 601R31113-57 CRACKED APPROX .1 INCH LONG AT IB AND OB SIDE LBL 9.0. (K) [SUP 06-05-07] MAINTENANCE REPLACED INBOARD AND OUTBOARD CLIPS AT FS 280 LBL 9 IAW CRJ 200 SRM 51-40-11, 51-42-02, 51-42-21. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032900323 20070329 00323 NM 2007 3 29 AWXA200700376 1 20070309 A 5320 654654039 ANGLE BOEING 737 7373G7 1384595 NM BS 640 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED VERTICAL ANGLE, BS 640, LBL 45.6, WL 208.1. REPLACED VERTICAL ANGLE, BS 640, LBL 45.6, WL 208.1 IA W B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007032900343 20070329 00343 SO 2007 3 29 FDKA200703126 1 20070319 A 5241 ROLLER EMB 145 EMB145LR 3260212 SO GALLEY DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 FDM 6082 TRI-ATL (0730 PHX LCL). GALLEY SERVICE DOOR WILL NOT CLOSE. MX CLEANED AND LUBED DOOR ROLLERS, OPS CHECK GOOD . 2 L 7 2 4T RT T00011AT 2007032900351 20070329 00351 NM 2007 3 29 FDKA200701027 1 20070127 A 2721 TRIM SYSTEM DHAV DHC8 DHC8101 2809002 NM RUDDER STUCK A FDKA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 SW 07 808LR 073 FDM 6194 JFK-BTV (0722 PHX LCL). RUDDER TRIM STUCK FULL RIGHT WHEN MAINTENANCE WAS REPOSITIONING AIRCRAFT TO GATE. MX RESET SYSTEM. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007032900364 20070329 00364 NM 2007 3 29 FDKA200703118 1 20070314 A 3350 1317 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 847EX 333 FDM 6140 JFK-MHT (0855 PHX LCL). EMERGENCY EXIT FLOOR PATH LIGHTING STAYS ON. MX RELAMPED. 2 H 7 2 4T RT A13NM 2007032900366 20070329 00366 NM 2007 3 29 FDKA200703129 1 20070320 A 3350 1317 LIGHT DHAV DHC8 DHC8102 2809003 NM EXTERIOR INOPERATIVE A FDKA K NONE L NO TEST NR NOT REPORTED 1 SW 07 804LR 324 FDM 5979 BWI-JFK (1912 PHX LCL). RIGHT EMERGENCY DOOR EXTERIOR LIGHT INOP. MX RELAMPED, OP CHECK GOOD. NO OTHER DEFEC TS NOTED. 2 H 7 2 4T RT A13NM 2007032900367 20070329 00367 SO 2007 3 29 FDKA200703101 1 20070308 A 7830 THRUST REVERSER EMB 145 EMB145LR 3260212 SO NR 2 ENGINE MALFUNCTIONED A FDKA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 846MJ 145507 FDM 6151 CAK-ATL (0610 PHX LCL). CREW ABORTED TAKEOFF FOR E2 REVERSER DISAGREE. MX PLACED E2 REVERSER ON MEL. 2 L 7 2 4T RT T00011AT 2007032900370 20070329 00370 SO 2007 3 29 FDKA200702065 1 20070211 A 2750 3631001011 CONTROL UNIT EMB 145 EMB145LR 3260212 SO T/E FLAP MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 840MJ 12471 145429 FDM 6018 BNA-MCO (0616 PHX LCL). FLAPS FAIL MESSAGE AT 0 DEGREES. MX REMOVED AND REPLACED FECU, PERFORMED RIGGING, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007032900383 20070329 00383 SO 2007 3 29 FDKA200701060 1 20070131 A 2844 211C119168 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO LT WING CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 LEFT WING FUEL PRESSURE SWITCH LINE IS PITTED FROM CORROSION. MX REMOVED AND REPLACED PRESSURE SWITCH TUBE ASSY. 2 L 7 2 4T RT T00011AT 2007032900384 20070329 00384 SO 2007 3 29 FDKA200701020 1 20070122 A 2760 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO SPOILER SYS MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 833MJ 145327 FDM 6134 ATL-BMI (1906 PHX LCL). SPOILER FAIL MESSAGE. MX RESET SPOILER SYSTEM AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007032900386 20070329 00386 NM 2007 3 29 FDKA200702067 1 20070212 A 2797 WIRE DHAV DHC8 DHC8101 2809002 NM AILERON DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 806LR 093 FDM 6181 ALB-JFK (1356 PHX LCL). CONTROL YOKE DIFFICULT TO MOVE IN AIR TO RIGHT AND AILERON TRIM INOP. MX SPLICED WIRE ON AILERON TRIM POT. 2 H 7 2 4T RT A13NM 2007033000002 20070330 00002 NM 2007 3 30 DLM90070240 1 20070317 A 5310 DOOR FRAME DOUG MD90 MD9030 3023690 NM FS 200 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 FOUND FWD ENTRY DOOR JAMB AFT WEB CRACKED FS 200. FAB AND INST REPAIR IAW SRM 51-11-01 PG 05. 2 L 7 2 4F RT A6WE 2007033000017 20070330 00017 NM 2007 3 30 DLM90070253 1 20070317 A 5320 WEB DOUG MD90 MD9030 3023690 NM FS 370 L26R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 FOUND FWD PIT WEB SURFACE CORROSION AT STA 370 LONG 26R. FABBED AND INSTALLED REPAIR PER SRM 53-00-01AT HMV2 REF N/R 14 00-0073. 2 L 7 2 4F RT A6WE 2007033000022 20070330 00022 NM 2007 3 30 DLM90070257 1 20070320 A 5330 SKIN DOUG MD90 MD9030 3023690 NM FS 185 S23-24R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 FOUND FUSE SKIN DENTED AT FS 185 BETWEEN LONG 23R AND 24R. REPAIR PER SRM 53-30-02 FIG 07. 2 L 7 2 4F RT A6WE 2007033000027 20070330 00027 NM 2007 3 30 DLM90070259 1 20070323 A 5313 LONGERON SPLICE DOUG MD90 MD9030 3023690 NM BS 1136-1155 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 FOUND AFT CARGO PIT LONG CORRODED AT STA 1136-1155. REPAIR PER SRM 51-30-05 REF N/R 1600-0151. 2 L 7 2 4F RT A6WE 2007033000034 20070330 00034 NM 2007 3 30 DL76S070265 1 20070326 A 2120 UNKNOWN BOEING 767 767332 1382001 NM CABIN ODOR A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 128DL 24078 FLIGHT ATTENDANTS REPORT BURNING SMELL IN CABIN. ELECTRICAL COMPONENT ODOR, SUSPECTED POSSIBLE LIGHTING PROBLEM. INSPE CTED A/C CABIN MID SECTION WITH NO DISCREPANCIES NOTED CHECKED LOWER CARGO COMP ALL OK. 2 L 7 2 4F RT A1NM 2007033000039 20070330 00039 NE 2007 3 30 HALA0700132 2 20070322 A 7230 FAN BLADE BOEING 767 767300 1385204 NM PWA 4060 PW4060 52119 NE LT ENGINE DENTED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 584HA 24258 ETOPS SIGNIFICANT SYSTEM, DURING L ENG INSPECTION FOUND DENT DAMAGE APPROX .030-.035 INCH NBR 4 FAN BLADE, 1 INCH FROM T IP AREA A. PERFORMED BLENDING PER AMM 72-31-02-308-003-N00 AND OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007033000064 20070330 00064 NM 2007 3 30 DL76L070232 1 20070323 A 3240 26124121A BRAKE ASSY BOEING 767 767332 1382001 NM LT MLG DAMAGED A DALA O OTHER M J OVER TEMP WARNING INDICATION LD LANDING 1 SO 27 189DN 25990 ON LANDING NOTICED HIGH BRAKE TEMP ON LT MLG FIM PROCEDURE 32-46-00/104 FIG 103 AND FIM PROCEDURE 32-46-00/105 FIG 104 C /OUT. NO FAULTS FOUND ON BRAKES TEMPERATURE INDICATION SYSTEM AND NO ANTISKID OR AUTOBRAKE FAILURE FOUND. NO FAI LURE FOUND ON WHEEL 4 AND INDICATION NORMAL. AT A/C ARRIVAL FOUND WHEEL 6 WITH TEMP INDICATION A UNIT. HIGH ENERGY STO P INSPECTION PERFORMED 05-51-14. NO FUSE MELTED. FOUND BRAKE 6 DAMAGED. BRAKE 6 DO NOT TURN FREE. BRAKE 6 REMOVED AN D REPLACED IAW AMM 32-41-08 CHECKED FOR LEAKAGE NIL FOUND. A/C RTS ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL T O ETOPS. 2 L 7 2 4F RT A1NM 2007033000067 20070330 00067 NM 2007 3 30 DL76G070234 1 20070322 A 4910 DOOR BOEING 767 767332 1382001 NM GE CF6 CF680 30025 NE APU BAY MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 171DZ 39502 29690 P153C AFTER APU SHUTDOWN GOT STATUS MSG AND APU DOOR MSG ON EICAS. FWD TO MCO AND PLAC PER MEL 49-15-01B. APU DOOR LOCKED IN FULLY OPEN POSITION. 2 L 7 2 4F 4 F RT A1NM E13NE 2007033000076 20070330 00076 NM 2007 3 30 HALA0700127 1 20070321 A 2410 OIL SYSTEM BOEING 767 76733A 1385209 NM RT IDG LOW A HALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, EICAS MSG "R GEN DRIVE" LIGHT ILL. GEN DRIVE DISCONNECTED. INSPECTED NR 2 IDG DPI, CHECK GOO D ON ARRIVAL. BITE CHECK BPCU, RT IDG OIL LOW. SERVICED AND RAN ENG LEAK AND DPI CHECK OK. RECONNECTED, OPS CHECK GOO D. MAINTENANCE ACCOMPLISHED PER AMM 24-11-01. 2 L 7 2 4F RT A1NM 2007033000077 20070330 00077 NM 2007 3 30 HALA0700128 1 20070323 A 2612 472565 FIRE LOOP BOEING 767 76733A 1385209 NM NR 1 NACELLE UNKNOWN A HALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 589HA 33422 AFTER LANDING RCVD EICAS ADVISORY MSG "L ENG FIRE LOOP". REMOVED AND REPLACED NR 1 ENG FIRE LOOP PER AMM 26-11-02 (UPPE R AFT). OPS CHK OK. NO MESSAGE NOTED. 2 L 7 2 4F RT A1NM 2007033000083 20070330 00083 NM 2007 3 30 QXEA200700394 1 20070316 A 3250 POTENTIOMETER DHAV DHC8 DHC8202 2809007 NM STEERING TILLER OUT OF ADJUST A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 349PH 486 SEA FLIGHT NR 2243 WHEN NOSE WHEEL STEERING SELECTED ON, WITH TILLER CENTERED, NOSE WHEEL TURNS FULL LEFT, NOSE WHEEL ST EERING INOP. MAINTENANCE RESECURED LINKAGE BETWEEN TILLER HANDLE AND RVDT ADJUSTED POT NO PARTS REPLACED. AIRCRAFT RET URNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007033000084 20070330 00084 NM 2007 3 30 ASTAR20070014 1 20070321 A 7830 SWITCH BOEING 727 727223 1384074 NM THRUST REVERSER OUT OF ADJUST A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 752DH 22466 WHEN THRUST LEVERS WERE BEING ADVANCED FOR T/O NR 3 ENG THRUST REVERSER LIGHT ILLUMINATED. REJECTED T/O AT ABOUT 20 KTS . PERFORMED RTO CHECKLIST AND ABNORMAL PROCEDURE. NORMAL OPERATION RESTORED. ADJUSTED NR 3 THRUST REV OPERATING LIGHT SWITCH IAW B727 MM 78-30-91. OPS CHECK GOOD THROUGH SEVERAL CYCLES DURING NR 3 ENG RUN REF: JRH 5.2 2 L 7 3 4F A3WE 2007033000096 20070330 00096 NM 2007 3 30 QXEA200700440 1 20070321 A 3150 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 402QX 4032 LAX FLIGHT NR 2442: ALT FAIL MESSAGE ON PFD AFTER START. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE CYCLED AIRCRAFT PO WER. ALT FAIL MESSAGE CLEARED WITH NO FAULTS FOUND. NO PARTS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007033000111 20070330 00111 NM 2007 3 30 QXEA200700384 1 20070220 A 3150 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 416QX 4083 SEA - ON FLIGHT 2362, NR 1 AND NR 2 BLEED HOT CAUTION LIGHTS ILLUMINATED AT 500' AFTER TAKEOFF. FIFTEEN MINUTES AFTER T AKEOFF, FIFTEEN MINUTES AFTER CONDUCTING RAM AIR CHECKLIST, BOTH BLEED HOT CAUTION WENT OUT. MAINTENANCE CHECKED CDS FO R FAULTS, CLEARED FAULTS, PERFORMED BLEED AIR OPERATIONAL TEST, TEST GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPL ACED. 2 H 7 2 4T RT A13NM 2007033000115 20070330 00115 NM 2007 3 30 HALA0700117 1 20070318 A 2150 62594610 CONTROLLER BOEING 767 767332 1382001 NM RT A/C PACK MALFUNCTIONED A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 596HA 35191 35191 23276 ETOPS SIGNIFICANT SYSTEM, WITH PNEU PRESS NORMAL A/C PACKS WOULD NOT COOL CABIN BELOW 81 DEGREES F. ATTEMPTED SELECTING WARM TEMP THEN PACK TO COLD, NO HELP. BITE CHECKED TEMP CONTROLLER PER MM 21-61-00 REPLACED RT PACK TEMP CONTROLLER PE R MM 21-61-03-400-005, OPS CK OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007033000147 20070330 00147 NE 2007 3 30 FDKA200702082 2 20070224 A 7261 OIL SYSTEM DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE LOW A FDKA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 804LR 324 FDM 6204 PVD-JFK (0500 PHX LCL). CREW ABORTED T/O AND RETURNED TO THE GATE FOR NR 2 ENGINE LOW OIL PRESSURE WARNING LIG HT ILLUMINATED. WHEN THE CAPT THROTTLED BACK LIGHT WENT OUT AND PRESSURE INCREASED. MX SERVICED OIL WITH 2 QUARTS AND NO FURTHER DEFECTS NOTED. 2 H 7 2 4T 4 T RT A13NM E20NE 2007033000150 20070330 00150 NM 2007 3 30 AWXA200700417 1 20070307 A 5320 69265553 INTERCOSTAL BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED INTERCOSTAL WEB, BS 348.2, S16L. REPLACED INTERCOSTAL WEB, BS 348.2, S16L IAW AWA ER 03-5312-07083- ES1. 2 L 7 2 4F RT A16WE 2007033000153 20070330 00153 NM 2007 3 30 AWXA200700420 1 20070307 A 5340 69620541 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED STRINGER CLIP, BS 294.5, S11L. REPLACED STRINGER CLIP, BS 294.5, S11L IAW AWA ER 03-5312-07083-ES1. 2 L 7 2 4F RT A16WE 2007033000158 20070330 00158 EU 2007 3 30 07FDEA00930 1 20070316 A 5210 SHAFT AIRBUS 310 A310304 3930339 EU ZONE 800 CHAFED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 OLD CHAFING MARK ON PAX DOOR NR 1 RT AT LOCKING CONTROL SHAFT. REPAIR WAS PERFORMED BY BLEND OUT IAW LHT SDR. 2 L 7 2 4F RT A35EU 2007033000164 20070330 00164 NM 2007 3 30 FDKA200701022 1 20070124 A 2750 FLAP DHAV DHC8 DHC8102 2809003 NM WING MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 926HA FDM 6204 PVD-JFK (0500 PHX LCL). FLAPS STUCK AT ZERO. MX RESET THE SYSTEM AND ALL OPS CHECKS WERE GOOD. 2 H 7 2 4T RT A13NM 2007033000167 20070330 00167 NM 2007 3 30 FDKA200702038 1 20070201 A 3233 8300101 ACTUATOR DHAV DHC8 DHC8101 2809002 NM NLG MALFUNCTIONED A FDKA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 805LR 30757 039 FDM 6188 JFK-SYR (2030 PHX LCL). DURING GEAR EXTENSION RUD PRESS & NR 2 RUD HYD CAUTION LIGHT & NR 2 PSI DROPPED BELOW 2000 PSI. MX REMOVED AND REPLACED NLG ACTUATOR. 2 H 7 2 4T RT A13NM 2007033000177 20070330 00177 EU 2007 3 30 07FDEA00936 1 20070316 A 5315 FLOORBEAM AIRBUS 310 A310304 3930339 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 AFT CARGO COMP FLOORBEAM AT C63 LT, Y 445 CORRODED. REPAIR WAS PERFORMED IAW SRM 53-10-15/FIG 207 BY LHT SDR. 2 L 7 2 4F RT A35EU 2007033000189 20070330 00189 NM 2007 3 30 SWAA071564 1 20070324 A 3350 6042221 BATTERY PACK BOEING 737 737301 1384611 NM CABIN FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED BRDG CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY PACK M9132 FAULTY. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2007033000195 20070330 00195 NM 2007 3 30 SWAA071568 1 20070325 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 469WN 33859 EEPLS LOOSE AT FWD END. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2007033000198 20070330 00198 NM 2007 3 30 SWAA071574 1 20070325 A 3350 100031 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 773SA 27881 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT SIDE LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT BALLAST PER M M. 2 L 7 2 4F RT A16WE 2007033000199 20070330 00199 NM 2007 3 30 SWAA071582 1 20070326 A 3350 101114 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 227WN 34450 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR SIDEWALL EMERGENCY EXIT LIGHT ASSY LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007033000208 20070330 00208 NM 2007 3 30 SWAA071572 1 20070325 A 5720 6937877 BAR BOEING 737 7373H4 1384600 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED SERVICE CHECK, FOUND RIGHT WING STABILIZER BAR CORRODED. REMOVED AND REPLACED RIGHT WING STABILIZER BA R PER MM. 2 L 7 2 4F RT A16WE 2007033000227 20070330 00227 2007 3 30 HALA0700107 4 20070314 A 3460 UNKNOWN BOEING 767 76733A 1385209 NM UNKNOWN A HALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 13 587HA 33421 ETOPS SIGNIFICANT SYSTEM, EPR COMMAND BUG ON BOTH EPR INDICATORS IS GREEN W/VNAV THRUST COMMAND MODE ACTIVE. MAX ALTITU DE AVAIL ON CLIMB PAGE WAS 23000 FT ALL PERF/DISTANCE PARAMETERS NORMAL. REF FIM 22-00-03 AND 34-61-00 MCDP SHOWS, NO L AST FLT FAULTS RAN MCDP TEST 2, 10, 30 AND 40 ALL SUCCESSFUL RAN BITE ON FMS COMPUTERS ALL TESTS OK. 2 L 7 2 4F RT A1NM 2007033000228 20070330 00228 NE 2007 3 30 HALA0700108 2 20070315 A 7261 ENGINE BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE NR 1 LEAKING A HALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM, NR 1 ENGINE 4.0 PINTS ADDED, NEED TO ACCOMPLISH HIGH OIL CONSUMPTION CHECK PER FIM 71-08-00 FI G 113. ACCOMPLISHED FIM 71-08-00 FIG 113 LEAKAGE CHECK, NO LEAKS NOTED. PRECAUTIONARY REPLACEMENT OF OIL TANK CAP PACK ING. OK TO CONTINUE IN SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007033000245 20070330 00245 NM 2007 3 30 ASAA0741548 1 20070327 A 5347 655384416 CARGO TRACK BOEING 737 7374Q8 138447Q NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 25112 CORROSION FOUND BEYOND LIMITS ON THE RT CARGO TIE DOWN TRACK. REPLACED WITH NEW PART IAW SRM 53-00-53 REPAIR 2 FIG 201. 2 L 7 2 4F RT A16WE 2007033000246 20070330 00246 EU 2007 3 30 07FDEA00952 1 20070316 A 5310 A53978267208 CROSSBEAM AIRBUS 310 A310304 3930339 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 FOUND CORRODED CROSSBEAM AT C67, Y-1070-1115. PART REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007033000248 20070330 00248 NM 2007 3 30 ASAA0741549 1 20070327 A 5347 655384415 FITTING BOEING 737 7374Q8 138447Q NM CARGO BAY WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 25112 AFT CARGO PIT NET TIE DOWN FITTING WORN AT BS 787 LBL 18. AFT CARGO NET TIE DOWN TRACK AT BS 727G+10 807+12 IAW SRM 53- 00-53 REPAIR 2 (LBL 18). 2 L 7 2 4F RT A16WE 2007033000253 20070330 00253 NM 2007 3 30 CALA0700153 1 20070327 A 5730 65C2670110 SKIN BOEING 737 7373T0 1384582 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 77303 23354 INSPECTION FOUND A 1.5 INCH CRACK IN RT WING FIXED LEADING EDGE LOWER SKIN AT PYLON O/B MIDSPAR FITTING. A DOUBLER WAS INSTALLED IAW ECRA 5731-01302. 2 L 7 2 4F RT A16WE 2007033000254 20070330 00254 NM 2007 3 30 CALA0700154 1 20070328 A 5320 5622492 STRUCTURE BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33203 30613 INSPECTION FOUND R-2 DOOR CHORD CORRODED AT STA 958-994, RBL 43. THE CHORD WAS REMOVED AND A NEW CHORD WAS INSTALLED IA W SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007033000255 20070330 00255 NM 2007 3 30 CALA0700155 1 20070328 A 5320 65C80735 ANGLE BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14604 27317 INSPECTION FOUND R-2 DOORWAY Z-ANGLE CORRODED JUST AFT OF DOORWAY AT STA 986.5, RBL 46. THE Z-ANGLE WAS REMOVED AND REP LACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007033000256 20070330 00256 EA 2007 3 30 COMA0760283 1 20070324 A 2750 860D10018ABCD CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAULTY A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 629BR 20756 7251 FLIGHT 5257 - FLAP FAIL MESSAGE RECEIVED AT START-UP. REPLACED FECU. ALSO PERFORMED EO 27-046AD. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007033000257 20070330 00257 NM 2007 3 30 HALA0700139 1 20070327 A 5753 STRUCTURE BOEING 767 76733A 1385209 NM TE FLAP DAMAGED A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 587HA 33421 AIRCRAFT ARRIVED WITH IMPACT DAMAGE TO LEFT OUTBOARD FLAP. IMPACT LOCATION IS 48" OUTBOARD WBL 955.0 2.5 FT FWD OF TRAI LING EDGE, 2 FT INBOARD OF FLAP CANOE. DIMENSIONS 5.5" IN LENGTH, 1/72" IN WIDTH AND 1/8" IN.DEPTH. ACCOMPLISHED INTE RIM REPAIR PER HAL M105 FILE 587034 1 CYC LIMITATION. 2 L 7 2 4F RT A1NM 2007033000258 20070330 00258 NM 2007 3 30 HALA0700144 1 20070327 A 3240 26124121A BRAKE ASSY BOEING 767 767300 1385204 NM NR 3 DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 590HA 10269 10269 33467 NR 3 MLG BRAKE ASSY SHOWS EVIDENCE OF HIGH HEAT. REMOVED AND REPLACED NR 3 MLG BRAKE ASSY IAW 32-41-68. OPS CKS AND LE AK CKS GOOD. PERFORMED AXLE INSPECTION FOR HEAT DAMAGE IAW MM 05-51-14. INSPECTION FOUND OK. 2 L 7 2 4F RT A1NM 2007033000259 20070330 00259 NE 2007 3 30 HALA0700140 2 20070328 A 7200 ENGINE BOEING 767 767300 1385204 NM PWA 4060 PW4060 52119 NE LEFT SURGES A HALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 WP 13 581HA 28141 ETOPS SIGNIFICANT SYSTEM, LEFT ENGINE SURGING EPR .01 TO .02 N1 .1 TO .3 TENTHS IN CRUISE FLT LEVEL 350. FOLLOWED PROCE DURES IN FIM 73-21-00 TESTED PIMU NO FAULTS NOTED. CHECKED FUEL FILTER AND EGT HARNESS NO FAULTS NOTED NOTIFIED MOC . OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007033000261 20070330 00261 NE 2007 3 30 HALA0700142 2 20070328 A 7250 NOZZLE BOEING 767 767300 1385204 NM PWA 4060 PW4060 52119 NE 1ST STAGE HPT CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, 1ST STAGE HPT NOZZLE INNER PLATFORM HAVE CRACKS AND BURN THRU THE PLATFORM ON NR 1 ENG FOUND D URING BORESCOPE. INSPECTED AREA CRACKS AND BURN THROUGHS ARE WITHIN LIMITS PER CF6-80A CARD NR 767-3-411024 ITEM NR 9, PAGE 8 OF 37 PER ENGINEERING. 2 L 7 2 4F 4 F RT A1NM E24NE 2007033000267 20070330 00267 SO 2007 3 30 SIMA200707801 1 20070315 A 3297 CONNECTOR PARKERHANFIN EMB 145 EMB145LR 3260212 SO PROXIMITY SWITCH DAMAGED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 662EH 8030 3382 145777 AIR/GROUND MESSAGE ILLUMINATED ON TAKEOFF, GEAR HANDLE WOULD NOT COME UP, MESSAGE WENT WENT AWAY ON LANDING. FOUND PIN "A" BROKEN ON PROXIMITY SWITCH. REMOVED AND REPLACED NOSE LANDING GEAR PROXIMITY SWITCH IAW EMB AMM 32-63-05. PERFORME D EXTENSION AND RETRACTION CHECKS WITH NO DEFECTS. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007033000268 20070330 00268 EA 2007 3 30 SIMA200707803 1 20070318 A 2621 4331000 GUARD CNDAIR CL600 CL6002C10 1390015 EA FLIGHT DECK FAILED A SIMA E ENGINE SHUTDOWN Y ENGINE STOPPAGE LD LANDING 1 SW 21 513AE 9670 10114 ON LANDING ROLL OUT, CREW PUSH LEFT FIRE ARM PBA, LEFT ENGINE SHUT DOWN. REMOVED AND REPLACED LEFT FIRE PUSH BUTTON LIG HT GUARD IAW CRJ AMM 31-14-01. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007033000270 20070330 00270 NE 2007 3 30 COMA0760274 2 20070321 A 7314 6078T3P04 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LT ENGINE MALFUNCTIONED A COMA K NONE X ENGINE FLAMEOUT AP APPROACH 1 SO 01 810CA 11499 7370 807042 FLIGHT 5428 - LEFT ENGINE FLAMED OUT ON APPROACH, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED LEFT FUEL PU MP. NO FURTHER DEFECTS. 2 L 7 2 4F 4 F RT A21EA E15NE 2007033000273 20070330 00273 WP 2007 3 30 N921R54017 1 20070108 A 5330 SPLICE DOUG DC8 DC863F 302198F WP SKIN CORRODED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 921R 46145 LWR FUSELAGE EXTERIOR STA 1766 L-33L MANUFACTURING SPLICE WITH CORROSION. REMOVED SPLICE IAW DPS 3.67.27, FABRICATED NE W SPLICE IAW DC8 SRM 53-4-1 AND DPS 3.69.4. PRIMED NEW SPLICE IAW DC8 SRM 51-1-8 AND INSTALLED NEW SPLICE IAW DC8 SRM 5 1-1-21 CPCP 5000 0552. 2 L 7 4 4F 4A25 2007033000274 20070330 00274 NM 2007 3 30 F3LA200700045 1 20070318 A 3230 664700500A4D CONTROL UNIT AIRBUS A319 A319111 3930336 NM MLG INOPERATIVE A F3LA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 03 908FR 3363 1759 FLIGHT CREW REPORTED ECAM L/G LGCIU2 FAULT ON APPROACH. PERFORMED GO-AROUND AND AIRCRAFT LANDED WITHOUT INCIDENT. REPL ACED NR 2 LANDING GEAR CONTROL INTERFACE UNIT (LGCIU) IAW 32-31-71-400-001 AND TESTED GOOD. 2 L 7 2 4F RT A28NM 2007033000275 20070330 00275 SO 2007 3 30 SIMA200708204 1 20070321 A 3350 20131A POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMEGENCY LIGHTS FAILED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 623AE 5148 17 145109 FOUND EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED NUMBER THREE EMERGENCY POWER SUPPLY ASSEMBLY IAW EMB AMM 33-50 -04. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007033000276 20070330 00276 EA 2007 3 30 COMA0760278 1 20070323 A 3234 7455025 CONTROL LEVER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 932CA 336 7038 FLIGHT 5615 - RECEIVED GEAR DISAGREE MESSAGE, MAINS STUCK IN UP POSITION. ABORTED APPROACH, DECLARED EMERGENCY, MANUALL Y DEPLOYED GEAR. LANDED WITHOUT INCIDENT. REPLACED GEAR SELECTOR LEVER. ALSO FOUND MLG SELECTOR VALVE CAP LOOSE AND S ECURED. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007033000277 20070330 00277 EA 2007 3 30 COMA0760286 1 20070324 A 2613 355862255 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA OVERHEAT SYS MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 436CA 7482 FLIGHT 9965 - RECEIVED RIGHT FUSELAGE ANTI-ICE DUCT MESSAGE. ABORTED TAKEOFF AT 90 KTS, RETURNED TO GATE WITHOUT INCIDE NT. PERFORMED MEGAOHN CHECK OF ALL LOOPS IN RIGHT FUSELAGE CIRCUIT. NO DISCREPANCIES. REPLACED LOOP A18WK FOR TROUBLE SHOOTING. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007033000278 20070330 00278 2007 3 30 COMA0760287 4 20070325 A 3170 6229820009 DCU CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 931CA 21365 7037 FLIGHT 5429 - RECEIVED DCU NR 2 INOP MESSAGE ON CLIMB. RETURNED TO CVG AND LANDED WITHOUT INCIDENT. REPLACED NR 2 DCU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007033000281 20070330 00281 SO 2007 3 30 FDKA200701010 1 20070111 A 2760 SWITCH EMB 145 EMB145LR 3260212 SO COCKPIT FAULTY A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 842MJ 145457 FDM 6071 DAY-ATL (1236 PHX LCL). SPOILER FAIL CAUTION MESSAGE IN FLIGHT. MX ADJUSTED NR 4 THROTTLE LEVER MICRO SWITCH, NO FUTHER DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2007033000282 20070330 00282 EA 2007 3 30 COMA0760291 1 20070328 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 403CA 7428 DURING MID CHECK INSPECTION FOUND FS 202.75 BULKHEAD CRACKED, BL 23.71 AT CUTOUT FOR HYDRAULIC LINE. REMOVED DAMAGE AND INSTALLED DOUBLER PER BOMBARDIER REO 601R-53-11-563. 2 L 7 2 4F RT A21EA 2007033000284 20070330 00284 EA 2007 3 30 COMA0760290 1 20070326 A 5210 FLAPPER VALVE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OBSTRUCTED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 812CA 7381 FLIGHT 5244 - RECEIVED PAX DOOR CAUTION AND CABIN PRESSURE INCREASE ON CLIMBOUT. PERFORMED QRH. RETURNED TO PIT AND LA NDED WITHOUT INCIDENT. CLEARED FOD FROM PAX DOOR FLAPPER VALVE. INSPECTED DOOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007033000286 20070330 00286 EA 2007 3 30 COMA0760288 1 20070326 A 2760 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA SPOILER SYS MALFUNCTIONED A COMA K NONE N FALSE WARNING AP APPROACH 1 SO 01 917CA 7017 FLIGHT 5667 - RECEIVED SPOILER CAUTION DURING DESCENT. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. RESET SPOILER S YSTEM. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007033000288 20070330 00288 EA 2007 3 30 COMA0760281 1 20070323 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 739CA 14956 7373 FLIGHT 5542 - RECEIVED FLAP FAIL CAUTION MESSAGE DURING TAXI. RETURNED TO GATE. REPLACED RIGHT BPSU. NO FURTHER DEFEC TS. 2 L 7 2 4F RT A21EA 2007033000289 20070330 00289 EA 2007 3 30 COMA0760282 1 20070324 A 2752 601R93106505 FLEX DRIVE CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP BENT A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 629BR 7251 FLIGHT 5257 - FLAP FAIL MESSAGE RECEIVED AT START-UP. REPLACED LEFT NR 5 FLEX DRIVE. ALSO PERFORMED EO 27-046AD. NO F URTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007033000292 20070330 00292 NE 2007 3 30 COMA0760275 2 20070321 A 7321 8063483 FUEL CONTROL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LT ENGINE MALFUNCTIONED A COMA K NONE X ENGINE FLAMEOUT AP APPROACH 1 SO 01 810CA 22170 7370 807042 FLIGHT 5428 - LEFT ENGINE FLAMED OUT ON APPROACH, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE FUEL CONTROL. NO FURTHER DEFECTS. 2 L 7 2 4F 4 F RT A21EA E15NE 2007033000297 20070330 00297 NM 2007 3 30 KCSA071091 1 20070328 A 5315 FLOORBEAM BOEING 747 747236B 1384804 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE BENT A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 AFT PIT FLOORBEAM UPPER CAP BENT AT BS 1580, RBL 54. 2 L 7 4 4F 4 F A20WE E3NE 2007033000301 20070330 00301 NM 2007 3 30 KCSA071095 1 20070228 A 5312 BULKHEAD BOEING 747 747236B 1384804 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 AFT PRESSURE BULKHEAD HAS SEVERAL SMALL DENTS RBL 55, WL 220, STA 2400. 2 L 7 4 4F 4 F A20WE E3NE 2007033000303 20070330 00303 NM 2007 3 30 KCSA071096 1 20070329 A 5313 STRINGER BOEING 747 747236B 1384804 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STA-2380 STR-46R HAS GOUGE. 2 L 7 4 4F 4 F A20WE E3NE 2007033000304 20070330 00304 NM 2007 3 30 KCSA071097 1 20070329 A 5315 FLOORBEAM BOEING 747 747236B 1384804 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STA 1720 RBL 46 FLOORBEAM UPPER CAP DENTED WL 118. 2 L 7 4 4F 4 F A20WE E3NE 2007033000305 20070330 00305 NM 2007 3 30 KCSA071098 1 20070329 A 5315 FLOORBEAM BOEING 747 747236B 1384804 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 UPPER DECK FLOORBEAM STA 420 RBL 5 HAS ELONGATED FASTENER HOLE IN UPPER CHORD FWD SIDE. 2 L 7 4 4F 4 F A20WE E3NE 2007033000309 20070330 00309 NM 2007 3 30 KCSA071085 1 20070327 A 5320 SHEAR WEB BOEING 747 747236B 1384804 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 MAIN DECK SLOPING, SHEAR WEB CRACKED AT FORWARD IB CORNER AFT OF TENSION TIE AT BS 820, RBL 77, STR 9R. 2 L 7 4 4F 4 F A20WE E3NE 2007033000311 20070330 00311 NM 2007 3 30 KCSA071088 1 20070327 A 5322 SHEAR TIE BOEING 747 747236B 1384804 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 MAIN DECK FUSELAGE FRAME SHEAR TIE CRACKED ON BOTH SIDES OF STR 11L. 2 L 7 4 4F 4 F A20WE E3NE 2007033000313 20070330 00313 NM 2007 3 30 AMTA200700129 1 20070304 A 5551 PIN BOEING 737 73783N 13844HI NM HORIZ STAB CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 321TZ 28249 RT AFT UPPER HORIZ STAB ATTACHMENT PIN HAS CORROSION, ITT ING FUSE 1147. REMOVED AND REPLACED HORIZ STAB PIN WITH NEW P IN PN 180A1612-3 IAW EO 737-55AD-2935 REV B. (K) 2 L 7 2 4F RT A16WE 2007033000318 20070330 00318 NM 2007 3 30 AMTA200700159 1 20070323 A 2540 MOUNT BOEING 737 73783N 13844HI NM AFT LAVATORY CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 301TZ 28239 LT AFT LAV OB MOUNT CORRODED (ON LAV) BS 952, LBL 49.5. REMOVED AND REPLACED LT AFT MOUNT IAW SRM 25-46-99. REPLACEMEN T MOUNT FABRICATED IAW EA 737-2500-09-A0716. (K) 2 L 7 2 4F RT A16WE 2007033000319 20070330 00319 NM 2007 3 30 AMTA200700169 1 20070323 A 2540 MOUNT BOEING 737 73783N 13844HI NM AFT LAVATORY CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 301TZ 28239 RT AFT LAV OB AFT CORNER MOUNT FITTING AND 2 EACH BLOCKS ARE CORRODED BS 952, RBL 49.5. CW EA 737-2500-00A0726, PARTS F AB IAW EA. (K) 10-26-07 REMOVED AND REPLACED MOUNT AND BLOCKS SPM 25-46-99. (M) 2 L 7 2 4F RT A16WE 2007033000322 20070330 00322 NM 2007 3 30 AMTA200700148 1 20070316 A 3350 20131A BATTERY PACK BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE CABIN DISCHARGED E AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 517AT 27973 EMERGENCY EXIT SIGN LIGHT AT ROW 16 CEILING INOPERATIVE. REPLACED BATTERY PACK IAW MM 33-51-07-2. OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007033000323 20070330 00323 NM 2007 3 30 AMTA200700145 1 20070309 A 4940 5198587 STARTER BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE APU FAULTY A AMTA K NONE J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 11 561TZ 12534 12534 33526 APU FAILED TO START 10 PERCENT RPM, 756 ECU FAULT (ABORTED START). APU COPARTMENT FULL OF ELECTRICAL SMOKE. REMOVED AN D REPLACED APU STARTER IAW AMM 49-41-01, OPS CHECK NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007033000324 20070330 00324 WP 2007 3 30 AMTA200700126 1 20070301 A 3350 LIGHT LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE CABIN INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 162AT 1220 AFT GALLEY EGRESS STRIP INOPERATIVE. REMOVED AND REPLACED AFT GALLEY EGRESS STRIP OPS CHECKS NORMAL. (K) 2 L 7 3 4F 4 F A23WE E12EU 2007033000325 20070330 00325 NM 2007 3 30 AMTA200700130 1 20070304 A 5551 PIN BOEING 737 73783N 13844HI NM HORIZ STAB CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 321TZ 28249 RT AFT CENTER (FAIL SAFE) HORIZ STAB ATTACHMENT PIN HAS CORROSION PITTING FUSE STA 1147. REMOVED AND REPLACED HORIZ STA B PIN WITH NEW PN 180A1612-4 IAW EO 737-55AD-2935, REV B. 2 L 7 2 4F RT A16WE 2007033000326 20070330 00326 SO 2007 3 30 SIMA200708202 1 20070321 A 2120 UNKNOWN EMB 135 EMB135LR 3260305 SO CABIN SMOKE A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 712AE 145247 SMOKE REPORTED IN CABIN AFTER NR 1 ENGINE START. PERFORMED VISUAL INSPECTION OF NR 1 ENGINE, APU AND BOTH PACKS WITH NO DEFECTS NOTED. PERFORMED ENGINE START OF NR 1 ENGINE. ALL PARAMETERS NORMAL WITH NO EICAS MESSAGES OR EVIDENCE OF SMO KE, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007033000327 20070330 00327 NM 2007 3 30 AMTA200700146 1 20070312 A 5610 141T480013 WINDOW BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT FAULTY A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 CAPTAINS NR 1 WINDOW ARCING. REMOVED AND REPLACED CAPTAINS WIND SHIELD IAW AMM CH 56-11-01-04. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007033000328 20070330 00328 NM 2007 3 30 AMTA200700089 1 20070217 A 5551 PIN BOEING 737 73783N 13844HI NM HORIZ STAB CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 323TZ 30033 LLT AFT UPPER VERT STAB PIN CORRODED AND GALLED. REPLACED PIN 180A16123 IAW EO 737-55AD-2935, REV B. (K) 2 L 7 2 4F RT A16WE 2007033000329 20070330 00329 NM 2007 3 30 AMTA200700128 1 20070304 A 5551 PIN BOEING 737 73783N 13844HI NM HORIZ STAB CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 321TZ 28249 RT AFT LOWER HORIZ STAB ATTACHMENT PIN HAS CORROSION PITTING FUSE STA 1147. REMOVED AND REPLACED HORIZ STAB PIN WITH NE W PIN PN 180A1612-4 IAW EO 737-55AD-2935, REV B M-30 ATTACHED TO EO. (K) 2 L 7 2 4F RT A16WE 2007033000333 20070330 00333 NM 2007 3 30 AMTA200700134 1 20070304 A 4970 APU BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE APU BAY MALFUNCTIONED A AMTA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 550TZ 32584 APU INOPERATIVE. PERFORMED BITE ON ECU, FOUND 2 ABORTED STARTS AND 1 DOOR SYSTEM FAULT. RAN APU SEVERAL TIMES APU RAN FINE NO FAULTS. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007033000334 20070330 00334 WP 2007 3 30 AMTA200700171 1 20070324 A 5210 SWITCH LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE R2 DOOR SHORTED A AMTA K NONE O OTHER TX TAXI/GRND HDL 1 GL 11 161AT 1219 R-2 DOOR WILL NOT OPEN ELECTRICALLY. FOUND R2 CLOSE SWITCH SHORTED INTERNALLY. REPLACED SWITCH IAW CH 20 STANDARD PRAC TICE OPS CHECK GOOD. (K) 2 L 7 3 4F 4 F A23WE E12EU 2007033000335 20070330 00335 NM 2007 3 30 AMTA200700110 1 20070223 A 3610 32143068 SHUTOFF VALVE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE BLEED AIR SYS MALFUNCTIONED A AMTA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 518AT 27974 LT ENGINE BLEED OFF LIGHT ILLUMINATED AT TAXI INTO INDY WITH ASSOCIATED EICAS MSG. REPLACED PROSOV AND HIGH STAGE PILOT IAW AMM. RAN LT ENGINE, OPS CHECKED LT BLEED REF MM. BLEED OPERATION NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007033000337 20070330 00337 NM 2007 3 30 AMTA200700133 1 20070304 A 5551 PIN BOEING 737 73783N 13844HI NM HORIZ STAB CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 321TZ 28249 LT AFT LOWER HORIZ STAB ATTACHMENT PIN HAS CORROSION PITTING. REMOVED AND REPLACED STAB PIN PN 180A1612-4 IAW EO 737-55 AD-2935 REV B. (K) 2 L 7 2 4F RT A16WE 2007033000338 20070330 00338 NM 2007 3 30 NOCA07007 1 20070312 A 3350 1315 LIGHT BOEING 767 767306 1385148 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 765NA 28098 EMERGENCY EXIT LIGHT IN COCKPIT ABOVE COCKPIT DOOR INOP. REPLACED LIGHT AS PER MM 33-51-04, OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2007033000339 20070330 00339 NM 2007 3 30 NOCA06607 1 20070320 A 4920 APU BOEING 767 767324 1385203 NM APU BAY MALFUNCTIONED A NOCA K NONE O OTHER CL CLIMB 1 EA 15 767NA 27569 APU IN FLIGHT START UNSUCCESSFUL AFTER THREE ATTEMPTS. A/C OFF E-TOPS. 2 L 7 2 4F RT A1NM 2007033000340 20070330 00340 NM 2007 3 30 NOCA07407 1 20070323 A 2610 033638500 DETECTOR BOEING 757 75728A 1384976 NM DETECTION SYS MALFUNCTIONED A NOCA K NONE J WARNING INDICATION UK UNKNOWN 1 EA 15 755NA 30043 FWD DET FAN/AIR ON EICAS. REPLACED FWD DET FAN PER MM 26-16-02. 2 L 7 2 4F RT A2NM 2007033000341 20070330 00341 NM 2007 3 30 NOCA06907 1 20070315 A 2751 18196917 TRANSMITTER BOEING 757 75728A 1384976 NM T/E FLAP FAULTY A NOCA K NONE N FALSE WARNING LD LANDING 1 EA 15 752NA 28174 EICAS MSG AFTER LANDING T/E FLAP ASYM. REMOVED AND REPLACED LEFT FLAP POSITION TRANSMITTER PER AMM 27-58-03 AND 27-58-0 0. OPS CHECKS NORMAL. 2 L 7 2 4F RT A2NM 2007033000342 20070330 00342 NM 2007 3 30 NOCA06807 1 20070314 A 3350 1315 LIGHT BOEING 767 767306 1385148 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 765NA 28098 EMERGENCY EXIT LIGHT IN COCKPIT ABOVE DOOR INOP. RELAMPED, OPS CHECKS OK. 2 L 7 2 4F RT A1NM 2007033000344 20070330 00344 NM 2007 3 30 NOCA07307 1 20070321 A 2751 751790010003 TRANSMITTER BOEING 757 75728A 1384976 NM T/E FLAP FAULTY A NOCA K NONE N FALSE WARNING UK UNKNOWN 1 EA 15 750NA 26277 TRAILING EDGE FLAP ASYM UPON FLAP RETRACTION. REMOVED AND REPLACED FLAP POS TRANSMITTER PER MM 27-58-03. 2 L 7 2 4F RT A2NM 2007033000345 20070330 00345 NM 2007 3 30 SWAA071587 1 20070327 A 2697 726SW727SW WIRE HARNESS BOEING 737 7373K2 13844BA NM APU BAY CHAFED A SWAA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 SW 29 340LV 23738 DECLARED EMERGENCY, APU FIRE WARNING LIGHT & HORN INDICATIONS. APU FIRE EXTINGUISHER BOTTLE DISCHARGED. FOUND APU FIRE WARN HARNESSES CHAFING. REMOVED AND REPLACED HARNESSES PER MM. 2 L 7 2 4F RT A16WE 2007033000347 20070330 00347 NM 2007 3 30 SWAA071602 1 20070327 A 3350 PL2230LH00 STRIP BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 481WN 29853 DURING SCHEDULED HC2 CHECK, FOUND EEPLS STRIP CRACKED BETWEEN ROWS 7 ABC & 14 ABC. REMOVED AND REPLACED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 2007033000351 20070330 00351 NM 2007 3 30 SWAA071598 1 20070327 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007033000358 20070330 00358 NM 2007 3 30 AALA20070536 1 20070322 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 967AN 29545 MIA - EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 13DEF DAMAGED. RELAMPED EMERGENCY LIGHT AT SEAT ROW 13DEF. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007033000360 20070330 00360 NM 2007 3 30 AALA20070524 1 20070322 A 3397 DBD3610501 WIRE HARNESS BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 359AA 24040 SFO - EMERGENCY SEAT MOUNTED LIGHT AT SEAT 32B INOPERATIVE. REPLACED HARNESS FOR EMERGENCY SEAT MOUNTED LIGHT AT SEAT 3 2B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007033000361 20070330 00361 NM 2007 3 30 AALA20070537 1 20070322 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 967AN 29545 MIA - EMERGENCY LIGHT AT SEAT ROW 13DEF HAS LENS DAMAGED. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 13DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007033000364 20070330 00364 EU 2007 3 30 07FDEA01065 1 20070321 A 5311 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 669FE 774 LT SIDE INSIDE FUSE, FS 47, BETWEEN STR 12L AND 13L GOUGED FRAME. COMPLIED WITH FEDEX EA NR 6-5310-105186 TITLE FUSELAG E, MINOR NICKS IN FRAME 47 STRINGER 12L-13L AND 12R - 13R REPAIR, BLENDED 2 AREAS WITH A MAXIMUM DEPTH OF .077 ON THE INBD CORNER AS NOTED IN FIGURE 1 ARE STRUCTURALLY ACCEPTABLE PROVIDED A MIN 63 MICRO INCH FINISH IS MAINTAINED, TOUCH UP ALODINE AND FR PRIMER PER SRM CHAPTER 51. 2 L 7 2 4F RT A35EU 2007033000366 20070330 00366 WP 2007 3 30 07FDEA01067 1 20070321 A 5610 NBA604724 WINDOW DOUG MD10 MD1010F 3022112 WP COCKPIT OPEN A FDEA C ABORTED TAKEOFF W INADEQUATE Q C TO TAKEOFF 1 SO 25 567FE 46994 REJECTED T/O FOR F/O OPEN WINDOW 90KTS. OPEN AND RECLOSED WINDOW LOCKED AND LATCHED A/C OK TO CONTINUE. 2 L 7 3 4F RT A22WE 2007033000367 20070330 00367 NM 2007 3 30 AALA20070546 1 20070324 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 369AA 25196 MIA - EMERGENCY LIGHT ASSEMBLY AT SEAT 12H MISSING. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 12H. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007033000369 20070330 00369 EU 2007 3 30 AALA20070548 1 20070324 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70054 461 MIA - EMERGENCY LIGHT AT SEAT 7G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 7G. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F RT A35EU 2007033000371 20070330 00371 EU 2007 3 30 07FDEA01069 1 20070321 A 5315 FLOORBEAM AIRBUS 310 A310222 3930315 EU FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 421FE 342 PREVIOUS REPAIR LOCATED ON MAIN CABIN FLOORBEAM FRAME 35 BETWEEN SEAT TRACKS 2 AND 3 RT FWD AND AFT UPPER FLANGE HAS 2 E ACH REPAIR ANGLES THE FWD ANGLE IS 10.3" BY 1" AND THE AFT ANGLE IS 12.4" BY 1.82". REPAIR FOUND NOT TO BE IAW EA6-5321 -29300. REMOVED EXISTING REPAIR ANGLES AND REPAIRED FLOORBEAM PER FEDEX EA6-5310-107718. 2 L 7 2 4F RT A35EU 2007040200001 20070402 00001 NM 2007 4 2 SWAA071597 1 20070327 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, WL 204 LT SIDE. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007040200003 20070402 00003 EU 2007 4 2 07FDEA00976 1 20070316 A 2611 CG7G011 SMOKE DETECTOR AIRBUS 300 A300F4605R 3930327 EU E/E BAY CONTAMINATED A FDEA O OTHER N FALSE WARNING LD LANDING 1 SO 25 678FE 792 AT 240 DESCENDING TO OAKLAND RECEIVED RED ECAM FOR AVIONICS SMOKE. REOCCURRED 3 TIMES. PER CREW DEBRIEF, CREW NEVER SM ELLED SMOKE IN COCKPIT, NOR SMELLED SMOKE VIA SNIFFER TUBE. INSPECTED MIN EQUIP BAY, RT AND LT AVIONICS RACKS, NO EVI DENCE OF SMOKE/FIRE OR SMOKE ODORS. AVIONICS SMOKE LIGHT. DURING TROUBLESHOOTING, FOUND WATER DRIPPING ON SMOKE DETECT OR 11WA. REPLACED DETECTOR. REMOVED AND REPLACED 11WA SMOKE DETECTOR PER MM 26-15-12-4, ON MFG CGDU2000-00, SRL 5565 T AG 7A3346. 2 L 7 2 4F RT A35EU 2007040200005 20070402 00005 WP 2007 4 2 07FDEA00978 1 20070318 A 5347 SEAT TRACK DOUG MD10 MD1010F 3022112 WP BS 1079-1089 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 566FE 46989 MAIN CABIN COMPT SEAT TRACK AT STA 1079, RBL 27.5 IS CRACK. REMOVED DAMAGED SECTION OF SEAT TRACK AND SPLICED IAW DC10/ MD10 SRM 53-70-00. FAB`D NEW EXTRUSION IAW DRG ADA8019 REV J. INSTALLED EXTRUSION IAW DC10/MD10 SRM 51-33-01 VOL. 11. ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL11. INSTALLED REMOVED FLOOR PANELS IAW DC10 SRM 51-31-01 VOL 11. 2 L 7 3 4F RT A22WE 2007040200007 20070402 00007 WP 2007 4 2 07FDEA00980 1 20070318 A 5730 SKIN DOUG MD10 MD1010F 3022112 WP RT WING DENTED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 566FE 46989 RT WING O/B FLAP O/B END LOWER SKIN DENTED, JUST I/B OF EXISTING REPAIR. REMOVED DAMAGED DOUBLER IAW MD10/DC10 SRM 51-3 1-01 VOL11 MAT ID FOR REPAIR DOUBLER 2024-T3 0.040 IAW DC10/MD10 SRM 57-52-01 VOL 111. PO NR 557785.5 AND PO NR 541694. 2. FAB`D PARTS IAW MD10/DC10-10 SRM 57-10-00. ALODINED AND PRIMED PARTS IAW MD10/DC10-10 SRM 51-21-01 VOL 11. INSTALL ED REPAIR IAW MD10/DC10-10 SRM 57-10-00 VOL 1. 2 L 7 3 4F RT A22WE 2007032900368 20070329 00368 SO 2007 3 29 FDKA200702071 1 20070214 A 5610 14553170005 SEAL EMB 145 EMB145LR 3260212 SO COCKPIT DETACHED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 850MJ 145568 FDM RON CAE. CAPTAIN’S EMERGENCY WINDOW SEAL IS DETACHED. MX REPLACED THE SEAL. 2 L 7 2 4T RT T00011AT 2007033000003 20070330 00003 NM 2007 3 30 DLM90070241 1 20070320 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FS 788-807 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 AT HMV2, CUSP WEB AT STA 788-807 LT CORRODED. REPAIRED IAW ERA 398191-14MA REF N/R 2400-0214. 2 L 7 2 4F RT A6WE 2007033000014 20070330 00014 NM 2007 3 30 DL76G070250 1 20070324 A 3240 BRAKE ASSY BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE MLG DAMAGED A DALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 1602 29694 P1711 NR 8 BRAKE TEMP READ SEVEN AFTER PARKING. REPLACED BRAKE ASSY. LEAK AND OPS CK C/W GOOD. PERFORMED AXLE HI-TEMP INSPE CTION. NO DEFECTS FOUND ON AXLE. 2 L 7 2 4F 4 F RT A1NM E13NE 2007033000024 20070330 00024 NM 2007 3 30 DLM90070258 1 20070322 A 5230 STRUCTURE DOUG MD90 MD9030 3023690 NM CARGO DOOR GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 C-1 DOOR HAS DENT 15IN ABOVE LWR AFT CORNER GOUGED. REPAIR PER SRM 53-30-01 FIG REF8000-0001. 2 L 7 2 4F RT A6WE 2007033000035 20070330 00035 NM 2007 3 30 HALA0700136 1 20070327 A 3150 UNKNOWN BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE UNKNOWN A HALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, L ENG EEC C1 STATUS MSG. BITE CK PER FIM 73-21-00 FIG 115. MSG CLEARED OK FOR SERVICE TEST E EC L MAINT. PANEL P-61 OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007033000037 20070330 00037 NM 2007 3 30 HALA0700137 1 20070327 A 3150 UNKNOWN BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE UNKNOWN A HALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM - L PIMU MAINT MSG. BITE CK PER FIM 73-21-00 FIG 115. FAULTS CH A MSG CLEARED. OK FOR SERVIC E. 2 L 7 2 4F 4 F RT A1NM E24NE 2007033000038 20070330 00038 SO 2007 3 30 FDKA200703121 1 20070314 A 5210 SEAL EMB 145 EMB145LR 3260212 SO PAX DOOR UNKNOWN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 831MJ 145273 FDM 6116 PFN-MCO (1705 PHX LCL). MAIN CABIN DOOR HARD TO OPEN. MX PERFORMED RIG AND REMOVED AND REPLACED DOOR SEAL. 2 L 7 2 4T RT T00011AT 2007033000043 20070330 00043 SO 2007 3 30 FDKA200703123 1 20070315 A 5210 DOOR EMB 145 EMB145LR 3260212 SO OUT OF RIG A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 831MJ 145273 FDM 6017 MCO-BNA (2209 PHX LCL). MAIN CABIN DOOR HARD TO OPEN. MX RE-RIGGED DOOR. 2 L 7 2 4T RT T00011AT 2007033000052 20070330 00052 EA 2007 3 30 SWIA200718058 1 20070320 A 3320 BALLAST CNDAIR CL600 CL6002C10 1390015 EA CABIN LIGHTS FAILED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 773SK 10236 FOUND SMOKE IN THE CABIN WITH LIGHTS FLICKERING AT ROWS 2 AND 3 AB SIDE. REPLACED LIGHT BALLAST AT ROW 3. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007033000054 20070330 00054 EA 2007 3 30 SWIA200718059 1 20070320 A 3310 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CHART HOLDER SHORTED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 957SW 7829 CAPTAIN'S CHART HOLDER/YOKE LIGHT EMITTED SPARKS. REPLACED CAPTAIN'S LIGHTED CHART HOLDER IAW AMM 33-13-13. OPERATIONA L CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007033000065 20070330 00065 NM 2007 3 30 DL76L070233 1 20070322 A 7797 CIRCUIT CARD BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 176DN 25061 724638 AFTER LEFT ENG START STATUS MESSAGE L ENG SPEED CARD. CHECKED L ENG SPEED CARD OK INT CHANGED L AND R SPEEDCARDS. MSG RE-APPEARED AFTER ENG RUN NOW RT SIDE. REMOVED AND REPLACED RT SPEEDCARD IAW MM 77-12-01. 2 L 7 2 4F 4 F RT A1NM E24NE 2007033000070 20070330 00070 NM 2007 3 30 DLM90070237 1 20070314 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FS 735-750 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 DURING HMV 2 FOUND CUSP WEB FS 735-750 OUT OF LIMITS. REPAIRED PER ERA 398191-14MA ON N/R 2700-0222. 2 L 7 2 4F RT A6WE 2007033000078 20070330 00078 NM 2007 3 30 HALA0700129 1 20070325 A 3150 UNKNOWN BOEING 767 76733A 1385209 NM RUDDER UNKNOWN A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 580HA 28140 BTB - ETOPS SIGNIFICANT SYSTEM - AFTER ENG START "RUDDER RATIO" EICAS LIGHT REMAINED ON. PERFORMED FIM27-21-00-104 AND RRCM BITE PER FIM27-09-106B. ALL TEST PASSED. NO FAULTS NOTED. RUDDER RATIO MSG CLEARED. 2 L 7 2 4F RT A1NM 2007033000079 20070330 00079 NM 2007 3 30 HALA0700130 1 20070322 A 3350 LIGHT BOEING 767 76733A 1385209 NM CABIN INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 583HA 25531 FOUND EMERGENCY PATH LIGHTS INOP AT 17 A, B 18 A, B 19A, B. REPLACED LIGHTS STRIP CHECKS OK. 2 L 7 2 4F RT A1NM 2007033000085 20070330 00085 WP 2007 3 30 ASTAR20070017 1 20070324 A 2420 GENERATOR DOUG DC8 DC873 302199C WP NR 4 FAILED A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 05 805DH 46125 NR 4 GEN HAD TO BE RESET AFTER ENG START BEFORE IT CAME ON LINE. WITHIN 2 MIN OF PARALLELING GENS, AND PULLING OUT OF T HE BLOCKS, NR 4 GEN UNPARALLELED LIGHT ILLUM. ABNORMAL PROC WAS COMPLETED, RESTORING NR 4 GEN TO THE PARALLELED STATUS. WITHIN 2 MIN OF RESTORING THE NR 4 GEN, NR 4 GEN UNPARALLELED LIGHT ILLUM AGAIN. WITH BOTH FAILURES, THERE WAS A LOUD BANG HEARD FROM THE ELEC DIST CENTER AND ALSO SOME SMOKE SMELLED. TRANSFERRED TO DMI LIST NR 28550 PER MEL 24-1-1 SP 2 4-1 C/W PLACARD INST. 2 L 7 4 4F RT 4A25 2007033000087 20070330 00087 NM 2007 3 30 QXEA200700411 1 20070309 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 438-502 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - LEFT OUTBOARD SEAT TRACK NR 2 CORRODED AT STATION 438.0, 461.0, 469.0, 488.0,502.0. REPAIRED IAW RD8-53-1342. 2 H 7 2 4T RT A13NM 2007033000089 20070330 00089 NM 2007 3 30 QXEA200700413 1 20070312 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 182-344 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - LEFT INBOARD SEAT TRACK NR 4 CORRODED AT STATION 182.0, 205.0, 218.0, 226.0, 230.0 TO 255.0, 268.0, 284.0, 298. 0, 314.0, 344.0. REPAIRED IAW RD8-53-1102, RD8-53-4473, AND SRM 51-30-26. 2 H 7 2 4T RT A13NM 2007033000094 20070330 00094 NM 2007 3 30 QXEA200700415 1 20070309 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 505-511 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - LEFT INBOARD SEAT TRACK NR 5 GOUGED AT STATION 505.0 TO 511.0. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2007033000109 20070330 00109 NM 2007 3 30 QXEA200700383 1 20070222 A 5270 PROXIMITY SWITCH BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR FROZEN A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 419QX 4145 PDX - ON FLIGHT 2452, ON CLIMB-OUT FROM SJC, MASTER WARNING AND THE FUSELAGE DOOR WARNING LIGHT ILLUMINATED ON MFD. AFT PASSENGER DOOR SHOWED OPEN, FA CONFIRMED VISUALLY DOOR WAS CLOSED AND PRESSURIZATION WAS NORMAL PER CHECKLIST. MAINTEN ANCE FOUND AFT PASSENGER DOOR PROX SWITCH SLIDING BRACKET FULL OF ICE AND H2O. CLEANED AND LUBED BRACKET. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007033000114 20070330 00114 NM 2007 3 30 AWXA200700409 1 20070307 A 5322 66142101 SHEAR TIE BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED INTERCOSTAL CLIP (SHEAR TIE), BS 294.5, S11L. REPLACED INTERCOSTAL CLIP (SHEAR TIE), BS 294.5, S11L IAW AWA ER 03-5312-07083-ES1. 2 L 7 2 4F RT A16WE 2007033000120 20070330 00120 NM 2007 3 30 QXEA200700372 1 20070314 A 2120 UNKNOWN DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE COCKPIT ODOR A QXEA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 362PH 518 PDX FLIGHT NR 2169, AFTER ENGINE STARTS WITH BLEEDS BOTH ON STRONG BURNING ODOR NOTED ON FLIGHT DECK AND IN THE CABIN. AFTER BLEEDS SELECTED OFF THE ODOR DISSIPATED SLIGHTLY. IN THE CABIN THE ODOR WAS STRONGEST IN THE AFT. MAINTENANCE CO MPLIED WITH FAULT ISOLATION FIGURE 119 OF PWC MM 72-00-01. NO DEFECTS NOTED. STARTED BOTH ENGINES NUMEROUS TIMES SELEC TING BLEEDS ON ONE AT A TIME AND TOGETHER NO BURNING ODOR OR SMOKE NOTED IN FLIGHT DECK OR CABIN. NO PARTS REPLACED. A IRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007033000129 20070330 00129 EU 2007 3 30 AWXA200700383 1 20070316 A 3350 321431 BATTERY PACK AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHT NO TEST A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 626AW 65 LAS - RT EPSU BATTERY PACK FAILED TEST. MX REMOVED AND REPLACED BATTERY PACK WITH SERVICABLE UNIT. OPERATIONAL CHECK W AS GOOD. 2 L 7 2 4F RT A28NM 2007033000146 20070330 00146 NM 2007 3 30 AWXA200700414 1 20070307 A 5320 6517684629 INTERCOSTAL BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED INTERCOSTAL WEB, BS 294.5, S8L. REPLACED INTERCOSTAL WEB, BS 294.5, S8L IAW AWA ER 03-5312-07083-ES 1. 2 L 7 2 4F RT A16WE 2007033000163 20070330 00163 NM 2007 3 30 FDKA200701034 1 20070130 A 2721 TRIM SYSTEM DHAV DHC8 DHC8102 2809003 NM RUDDER SYS MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 847EX 333 FDM 6055 SYR-JFK (1248 PHX LCL). RUDDER TRIM INOP. MX RESET SYSTEM AND OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2007033000166 20070330 00166 NM 2007 3 30 FDKA200702044 1 20070204 A 2760 DSC1823 RELAY DHAV DHC8 DHC8101 2809002 NM RUDDER SYS FAILED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 926HA 114 FDM 6080 JFK (1626 PHX LCL). ROLL SPOILERS FAILED TO STOW. MX REMOVED AND REPLACED 2760-K1 RELAY. 2 H 7 2 4T RT A13NM 2007033000194 20070330 00194 NM 2007 3 30 SWAA071569 1 20070325 A 2560 6557463 HOOK BOEING 737 7373Q8 1384670 NM R2 DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 R2 DOOR EVACUATION SLIDE GIRT BAR FWD ATTACH HOOK BROKEN. REMOVED AND REPLACED R2 DOOR SLIDE COVER ASSY PER MM. 2 L 7 2 4F RT A16WE 2007033000196 20070330 00196 NM 2007 3 30 SWAA071575 1 20070326 A 3350 079123 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 226WN 32494 EEPLS LENS MISSING AT ROW 17. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007033000206 20070330 00206 NM 2007 3 30 SWAA071580 1 20070326 A 3350 65C27093 LENS BOEING 737 7373A4 1384585 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED 22Y CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN AT ROW 2. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007033000211 20070330 00211 WP 2007 3 30 ASAA0781552 1 20070328 A 5321 99365439 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 CABIN FLOOR PANEL CORRODED. REPLACED PANEL PER SRM 51-10-3 AND DAC DWG 9932816. 2 L 7 2 4F RT A6WE 2007033000213 20070330 00213 WP 2007 3 30 ASAA0781554 1 20070328 A 5321 993653711 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 CABIN FLOOR PANEL PUNCTURED. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007033000218 20070330 00218 WP 2007 3 30 ASAA0781557 1 20070328 A 5321 993053839 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 CABIN FLOOR WEB IS CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-70-4. 2 L 7 2 4F RT A6WE 2007033000219 20070330 00219 WP 2007 3 30 ASAA0781558 1 20070328 A 5321 993653927 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 CABIN FLOOR PANEL PUNCTURED. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007033000220 20070330 00220 WP 2007 3 30 ASAA0781559 1 20070328 A 5321 993658211 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 CABIN FLOOR PANEL PUNCTURED. REMOVED DAMAGED SECTION. APPLIED FILLER PLIES. 2 L 7 2 4F RT A6WE 2007033000222 20070330 00222 WP 2007 3 30 ASAA0781561 1 20070329 A 5330 595305077 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 FUSELAGE DENTED. REMOVED DAMAGED AREA. INSTALLED SKIN FILLER INTERNAL REPAIR DOUBLERS REPAIR STRAPS AND FINGER DOUBLER S PER SRM 53-04. 2 L 7 2 4F RT A6WE 2007033000232 20070330 00232 2007 3 30 HALA0700111 4 20070312 A 2312 6226827002 CONTROL PANEL BOEING 767 767332 1382001 NM HF RADIOS MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 598HA 5 5 23278 ETOPS SIGNIFICANT SYSTEM, RIGHT HF WILL NOT TURN OFF. REMOVED AND REPLACED RIGHT HF CONTROL PANEL, CKS GOOD PER MM 23-1 1-02. 2 L 7 2 4F RT A1NM 2007033000233 20070330 00233 NM 2007 3 30 AWXA200700421 1 20070307 A 5313 6561777503 STRINGER SPLICE BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED STRINGER SPLICE CHANNEL, BS 360, S14L. REPLACED STRINGER SPLICE CHANNEL, BS 360, S14L IAW AWA ER 03 -5312-07083-ES1. 2 L 7 2 4F RT A16WE 2007033000234 20070330 00234 WP 2007 3 30 ASAA0781566 1 20070329 A 5753 591004335 VANE DOUG DC9 DC983 3022083 WP T/E FLAP GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 LEFTHAND OUTBOARD FLAP OUTBOARD VANE IS GOUGED. INSTALLED REPAIR DOUBLER PER SRM 51-70-2. 2 L 7 2 4F RT A6WE 2007033000241 20070330 00241 EU 2007 3 30 07FDEA00948 1 20070316 A 5720 STIFFENER AIRBUS 310 A310304 3930339 EU ZONE 600 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 RT WING, SHROUD BOX F/S SPAR, DAMAGE BY MAIN BARREL PIN. REPAIR WAS RENEWED BY REPLACEMENT OF VERTICAL STIFFENER. 2 L 7 2 4F RT A35EU 2007033000242 20070330 00242 NM 2007 3 30 ASAA0741546 1 20070326 A 5311 65C32351 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 FRAME CRACKED. REPAIRED CRACKED FRAME IAW SRM 53-00-07 FIG 201. 2 L 7 2 4F RT A16WE 2007033000263 20070330 00263 NM 2007 3 30 HALA0700100 1 20070312 A 7720 902515 THERMOCOUPLE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE TURBINE MALFUNCTIONED A HALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 13 478HA 55123 BTB - ENG R SYS FAULT AFTER STARTING R ENG TURBINE BEARING O/H CHANNEL AND B FAULT. CURRENT FAULT "TURBINE BEARING OVER HEAT SENSOR A/B CHANNEL DISAGREE" 772204. REMOVE AND REPLACE TURBINE OVERHEAT DETECTION THERMOCOUPLE PER AMM77-23-01, O PS CK OK. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007033000269 20070330 00269 EA 2007 3 30 COMA0760284 1 20070324 A 2613 355962255 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA OVERHEAT SYS MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 436CA 7482 FLIGHT 9965 - RECEIVED RIGHT FUSELAGE ANTI-ICE DUCT MESSAGE. ABORTED TAKEOFF AT 90 KTS, RETURNED TO GATE WITHOUT INCIDE NT. PERFORMED MEGAOHN CHECK OF ALL LOOPS IN RIGHT FUSELAGE CIRCUIT. NO DISCREPANCIES. REPLACED LOOP A38WK FOR TROUBLE SHOOTING. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007033000272 20070330 00272 NM 2007 3 30 UIEA200700109 1 20070302 A 5320 REVEAL BOEING 747 7472D7B 1384803 NM R4 DOORWAY CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 21784 FOUND R4 DOOR CUTOUT UPPER FORWARD REVEAL CRACKED: CRACK WAS STOPPED DRILLED AND DOUBLER ADDED AS PER BOEING MESSAGE 1-2 94125025-3 AND 8100-9. 2 L 7 4 4F RT A20WE 2007033000291 20070330 00291 NE 2007 3 30 COMA0760277 2 20070322 A 7261 6087T04P06 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENGINE FAULTY A COMA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 SO 01 451CA 2575 7562 876763 FLIGHT 9476 - EN ROUTE CVG-GRR LEFT ENGINE OIL PRESSURE INDICATION WAS ERRATIC, CREW DECLARED AN EMERGENCY AND PERFORMED AN IN-FLIGHT SHUTDOWN. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT ENGINE LUBRICATION MODULE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007033000293 20070330 00293 WP 2007 3 30 UPS07849568 1 20070315 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C3 L30R AT STA 1700 HAS CORROSION. CORROSION EXTENDS UNDER END FITTING. REMOVED EXFOLIATED AND CRACKED END FITTING AT STA 1700 L30R IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT LONGERON SEGMENT AT STA 1700 L30R I AW SRM 53-02-002 FIG 10. 2 L 7 4 4F RT 4A25 2007033000294 20070330 00294 WP 2007 3 30 UPS07849569 1 20070314 A 5313 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C3 LONGERON END FITTING CRACKED AT STA 1260 TO 1280 L34L. REMOVED LONGERON SPLICE FITTING AT STA 1260-1 280 L34L IAW SRM 51-1-20D. LOCATED, DRILLED AND INSTALLED LONGERON SPLICE FITTING AT STA 1260-1280 L34L IAW SRM 51-3-2, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007033000302 20070330 00302 NM 2007 3 30 KCSA071089 1 20070328 A 5347 SEAT TRACK BOEING 747 747236B 1384804 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE BENT A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 AFT PIT SEAT TRACK FLANGE BENT AT BS 1905, LBL-25 2 L 7 4 4F 4 F A20WE E3NE 2007033000314 20070330 00314 NM 2007 3 30 AMTA200700155 1 20070323 A 5320 FLOOR SUPPORT BOEING 737 73783N 13844HI NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 301TZ 28239 CORROSION ON AFT FLOOR SUPPORT STRAP AT STA 771, LBL 21 TO RBL 21 AT BOTTOM AND TOP OF FASTENER HOLES. REMOVED CORROSIO N IAW 51-10-02, FOUND OUT OF LIMITS, FABRICATED SUPPORT STRAP IAW 53-60-53-01-2, DRILLED AND INSTALLED NUT PLATES IAW 53 -60-53-01, 51-40-02, INSTALLED IAW 51-40-02. (K) 2 L 7 2 4F RT A16WE 2007033000317 20070330 00317 NM 2007 3 30 AMTA200700132 1 20070304 A 5551 PIN BOEING 737 73783N 13844HI NM HORIZ STAB CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 321TZ 28249 LT AFT CENTER HORIZ STAB ATTACHMENT PIN HAS CORROSION PITTING FUSE STA 1147. REMOVED AND REPLACED PIN IAW EO 737-55AD-2 935, REV B.(K) 2 L 7 2 4F RT A16WE 2007033000332 20070330 00332 NM 2007 3 30 AMTA200700125 1 20070228 A 3350 D71702001 POWER SUPPLY BOEING 737 73783N 13844HI NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 310TZ 28243 AFT RT WING OVER WING EMERGENCY EXTERIOR LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AT STA 727. LI GHT OPS CHECK GOOD. (K) 2 L 7 2 4F RT A16WE 2007033000336 20070330 00336 2007 3 30 AMTA200700111 4 20070225 A 3160 4058650950 CDU BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT INOPERATIVE A AMTA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 519AT 27975 F/O CDU INOPERATIVE. REMOVED AND REPLACED CDU F/O`S SIDE IAW AMM. CDU WAS HARD FAILED (BLANK), NOW OPS NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007033000343 20070330 00343 NM 2007 3 30 NOCA07207 1 20070323 A 2913 32687929 PUMP BOEING 767 76739H 1385311 NM HYDRAULIC SYS MALFUNCTIONED A NOCA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 760NA 26257 C-HYD SYS PRESS EICAS C-SYS PRESS LIGHT ILLUMINATED, AIR PRESS LIGHT ILLUMINATED, AIRCRAFT DUMPED 18.8K LBS OF FUEL. AI RCRAFT HAD AIR TURNBACK TO DFW. REPLACED ADP PUMP ASSY. REPLACED CENTER HYD PRESS SWITCH S35. REPLACED AIR HYD PUMP P RESS SWITCH S28. REPLACED AIR HYD PUMP CONTROL PRESS SWITCH S29AS PER MM 29-11-04. 2 L 7 2 4F RT A1NM 2007033000348 20070330 00348 NM 2007 3 30 SWAA071600 1 20070327 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 10R. REPAIRED SKIN PER SRM & EA. 2 L 7 2 4F RT A16WE 2007033000354 20070330 00354 NM 2007 3 30 SWAA071589 1 20070327 A 5311 6546526 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 420, STR 26R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007033000355 20070330 00355 NM 2007 3 30 NWAA071155635 1 20070315 A 5347 SEAT TRACK BOEING 757 757251 1384970 NM BS 685-740 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 535US 26482 DURING "M" CHECK, FOUND CORROSION ON SEAT TRACK AT BS 685-740 RBL 45. REPAIRED PER EA 56-208812. 2 L 7 2 4F RT A2NM 2007033000356 20070330 00356 WP 2007 3 30 AALA20070542 1 20070323 A 2560 BATTERY DOUG DC9 DC983 3022083 WP FLASHLIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 591AA 53254 LGA - EMERGENCY FLASHLIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT LEFT NUMBE R TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007033000359 20070330 00359 NM 2007 3 30 AALA20070525 1 20070322 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 181AN 29591 MIA - EMERGENCY EXTERIOR LIGHT AT LEFT NUMBER THREE DOOR INOPERATIVE. RELAMPED EMERGENCY EXTERIOR LIGHT AT LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007033000362 20070330 00362 2007 3 30 AALA20070538 2 20070323 A 7200 INDICATION SYS DOUG DC9 DC982 3022082 WP COCKPIT INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 218AA 49168 RIGHT ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED AT FLIGHT LEVEL 370. LIGHT STAYED ON AT IDLE. CREW SHUT DOWN RIGHT HA ND ENGINE. ENGINE WINDMILLED FOR 27 MINUTES WITH NORMAL OIL PRESSURE AND QUANTITY. RETURNED TO TPA AND LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE OIL FILTER. FILTER CHECKED CLEAN. PLACARDED RIGHT ENGINE OIL STRAINER INDICATION INOPERATIVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007033000363 20070330 00363 NM 2007 3 30 AALA20070539 1 20070323 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7667A 25301 MIA - EMERGENCY LIGHTS AT ROW 17D TO 25D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROW 17D TO 25D. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007033000365 20070330 00365 EU 2007 3 30 07FDEA01066 1 20070321 A 5311 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 669FE 774 RT SIDE INSIDE FUSE FR47 BETWEEN STR 12R AND 13R GOUGED FRAME COMPLIED WITH FEDEX EA NR 6-5310-105186 TITLE FUSELAGE MIN OR NICKS IN FRAME 47 STRINGER 12L-13L AND 12R-13R REPAIR, BLENDED 2 AREAS WITH A MAXIMUM DEPTH OF .077 ON THE INBD COR NER AS NOTED IN FIGURE 1 ARE STRUCTURALLY ACCEPTABLE PROVIDED A MIN 63 MICRO INCH FINISH IS MAINTAINED. TOUCH UP ALODIN E AND FR PRIMER PER SRM CHAPTER 51. 2 L 7 2 4F RT A35EU 2007040200006 20070402 00006 WP 2007 4 2 07FDEA00979 1 20070318 A 5347 SEAT TRACK DOUG MD10 MD1010F 3022112 WP BS 1086-1095 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 566FE 46989 UPPER CARGO DOOR COMPARTMENT SEAT TRACK SCALLOPS DAMAGED BETWEEN STA 1086 AND STA 1095, RBL 48. REMOVED DAMAGED SEAT TR ACK IAW DC/MD10-10 SRM 51-31-01 VOL 11 PG 1. FAB`D NEW SEAT TRACK IAW DC/MD10-10 SRM 53-70-00 VOL 1 AND DWG SP10S10179 REV`D, ALODINED AND PRIMED NEW SEAT TRACK IAW DC/MD10-10 SRM 51-21-01 VOL2 PG 2. INSTALLED NEW SEAT TRACK IAW DC/MD10-1 0 SRM 53-70-00 VOL 1 AND DWGSP10S10179 REV D. 2 L 7 3 4F RT A22WE 2007040200010 20070402 00010 NM 2007 4 2 07FDEA00983 1 20070318 A 5320 INTERCOSTAL BOEING 727 727225 1384077 NM BS 348-360 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 FOUND INTERCOSTAL CORRODED FS 348 TO 360, AT STR 12L. REMOVED CORRODED, CHECKED AND FOUND TO BE OUT OF LIMITS IAW SRM 5 3-10-1, FIG 1, SHEET 2. FAB`D NEW FILLER AND DOUBLER FROM 7075-T6, .040C BATCH 1120917, AND 7075-T6, .050C BATCH 761741 IAW SRM 51-40-2, FIG 1, PAGE 1-6. INSTALLED FILLER AND DOUBLER IAW SRM 51-40-2, FIG 1, PG 1-6. 2 L 7 3 4F A3WE 2007040200012 20070402 00012 EU 2007 4 2 07FDEA00989 1 20070319 A 5330 SKIN AIRBUS 310 A310304 3930339 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 DOUBLE HOLE ON FUSELAGE SKIN AT C67, P35 RHS REPAIR WAS PERFORMED BY BUSH REPAIR IAW SRM 51-40-51, APPROVED BY EA 6-5317 6-106410 AND RAS/DAHAM/4021719/2007 ISS. A 2 L 7 2 4F RT A35EU 2007040200013 20070402 00013 EU 2007 4 2 07FDEA00990 1 20070319 A 5330 SKIN AIRBUS 310 A310304 3930339 EU ZONE 200 CHAFED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 CHAFE MARKS ON C38.1, P14-15 LT SIDE. REPAIR WAS PERFORMED BY BLEND OUT IAW EA 6-5314-106417 AND RAS/DATLS/0003560/2007 ISS. B 2 L 7 2 4F RT A35EU 2007040200015 20070402 00015 EU 2007 4 2 07FDEA00992 1 20070319 A 5320 A53974276206 SILL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 CORROSION ON SILL BEAM C59-63A, RT REPAIR WAS PERFORMED BY CUT OUT AT C60 AND C63 IAW SRM 53-17-18 AND REWORK AT SILL BE AM EDGE IAW EA 6-5317-106399 AND RAS/DAHAM/4021663/2006 ISS. A 2 L 7 2 4F RT A35EU 2007040200016 20070402 00016 EU 2007 4 2 07FDEA00993 1 20070319 A 5720 ANGLE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 CRACK FINDINGS IN ANGLE (HOLE 11, 13, 42, 45, 160, 180, 191, ALL LT SIDE) DURING ACCOMPLISHMENT OF EO 6-5710-7-3305, SB A300-57-6050 REV.03, AD 2005-23-08 REPAIR WAS PERFORMED BY REAM OUT, OVERSIZING AND COLD WORKING IAW EA 6-5710-106435 A ND RAS/049856/032/2007 ISS. A 2 L 7 2 4F RT A35EU 2007040200017 20070402 00017 NM 2007 4 2 07FDEA00994 1 20070319 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 571FE 71749 47830 MAIN CARGO COMPARTMENT SEAT TRACK HAS GOUGED AREAS AT F/S 1079 - 1109 LBL8 BLENDED AREA IAW SRM 53-70-00 FIG 5. BEGINNI NG THICKNESS OF MATERIAL 0.145; REMOVED 0.060; OUT OF LIMITS IAW SRM 53-70-00 FIG 5. RECIEVED FROM FAB ON MAE TRAVLER N R T7/666714, SEAT TRACK; RECEIVED FROM FAB ON MAE TRAVLER NR T7/666715, SPLICE HAT AND SPLICE PLATE. INSTALLED NEW SEAT TRACK, HAT, AND SPLICE IAW SRM 53-70-00 FIG 1. 2 L 7 3 4F RT A22WE 2007040200018 20070402 00018 WP 2007 4 2 07FDEA00995 1 20070319 A 5347 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 571FE 71749 47830 MAIN CARGO COMPARTMENT SEAT TRACK HAS GOUGED AREAS AT FS 1139 - 1239 RBL 8. BLENDED SEAT TRACK IAW SRM 53-70-00 FIG 5, FOUND TO BE OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 53-70-00 FIG 1. SEAT TRACK FABRICATED ON MAE TRAVELER NR T7/666 718. SPLICE PLATE AND HAT FABRICATED ON MAE TRAVLER NR T7/666719. 2 L 7 3 4F RT A22WE 2007040200019 20070402 00019 WP 2007 4 2 07FDEA00996 1 20070319 A 5347 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 571FE 71749 47830 MAIN CARGO COMPARTMENT SEAT TRACK HAS GOUGED AREAS AT F/S 909 - 1039 RBL 75. BLENDED AREA IAW SRM 53-70-00 FIG 5. SEAT TRACK EXCEEDED LIMITS IAW SRM 53-70-00 FIG 5. REMOVED DAMAGED AREA STA 930-1030 RBL 75 IAW SRM 53-70-00 FIG 4. FABRIC ATED NEW SEAT TRACK ON MAE TRAVELER NR T7/666392. FABRICATED HAT AND SPLICE FOR SEAT TRACK ON MAE TRAVELER NR T7/666393 . INSTALLED NEW SEAT TRACK, SPLICE, AT HAT IAW SRM 53-70-00 FIG 1. 2 L 7 3 4F RT A22WE 2007040200021 20070402 00021 EU 2007 4 2 07FDEA00998 1 20070319 A 5330 DOUBLER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 OLD GRINDING MARK AT INTERNAL DOUBLER, C70-71, P48-49 LHS REPAIR WAS PERFORMED BY BLEND OUT THE DAMAGE IAW EA 6-5317-106 396 AND RAS/DAHAM/ 4021674/2006 ISS. A. 2 L 7 2 4F RT A35EU 2007040200023 20070402 00023 NM 2007 4 2 07FDEA01001 1 20070319 A 5230 FITTING DOUG MD11 MD11F 3023600 NM CARGO DOOR CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 566FE 46989 MAIN CARGO DOOR NR 6 SPOOL FITTING HAS CRACK INDICATION. REMOVED SPOOL FITTING IAW MD/DC10 SRM 51-33-01 VOL11 PR=G,47. BHEC WAS PERFORMED IAW NDTSPM 06-10-01. ON NR 6 LOWER JAMB WEB HOLES. NO CRACKS FOUND. LOCATED AND DRILLED NEW FITTI NG IAW DAC DWG AFA7132 REV B. INSTALLED NEW SPOOL FITTING IAW MD/DC10 SRM 51-33-01 VOL 11 PG, 34 PARAG 6. 2 L 7 3 4F RT A22WE 2007040200026 20070402 00026 EU 2007 4 2 NWAA071143205 1 20070324 A 3350 BATTERY PACK AIRBUS 320 A320211 3930320 EU EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 305US 041 AFT EMERGENCY ESCAPE PATH LIGHTS INOP. CORRECTED BY REPLACING AFT BATTERY PACK (12WL). OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 2007040200028 20070402 00028 NM 2007 4 2 07FDEA01004 1 20070319 A 5330 SKIN BOEING 727 727225 1384077 NM BS 298-307 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 461FE 22548 REPAIR AT STA 298-307, STR 21R TO 23R DOES NOT COMPLY WITH FAA APPROVE DATA. REMOVED REPAIR, FAB`D NEW REPAIR DOUBLER IA W SRM 53-30-3, FIG 3, TABLE 1, MAT 2024-T3, .063C, AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3, FIG 3. 2 L 7 3 4F A3WE 2007040200029 20070402 00029 EU 2007 4 2 07FDEA01007 1 20070320 A 5210 A52120753001A SKIN AIRBUS 310 A310324 3930206 EU ZONE 800 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 FOUND CORROSION ON RT FWD PASSENGER DOOR ARM ASSEMBLY. REPAIR PERFORMED BY BLEND OUT WITH DOUBLER INSTALLATION AND REPL ACEMENT OF CORRODED PARTS IAW EA 6-5211-101326 AND IS APPROVED BY RAS 045586/005/2006. 2 L 7 2 4F RT A35EU 2007040200030 20070402 00030 NM 2007 4 2 07FDEA01012 1 20070320 A 5220 50797824 RETAINER BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 RIGHT AFT EMERGENCY EXIT HATCH AFT LOWER SECTION HAS CRACKED SEAL RETAINER. REMOVED RETAINER REF SRM 51-20-2. FABRICAT ED NEW SEAL RETAINER REF BAC DWG 50-07978-53. INSTALLED NEW SEAL REF SRM 51-20-2 PG 4. 2 L 7 3 4F A3WE 2007040200031 20070402 00031 EU 2007 4 2 07FDEA01013 1 20070320 A 5311 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 DENTED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 DENT (RIVETING MARK) AT C23, P41 LT. REPAIR PERFORMED BY INSTALLING FLUSH DOUBLER AND SPLICED STRINGER IAW EA 6-5313-10 1261, SRM 53-10-12/FIG 27 AND SRM 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007040200032 20070402 00032 EU 2007 4 2 07FDEA01014 1 20070320 A 5330 A53778731206 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CORROSION AT INNER DOUBLER A537-78731-206 OF GROUND SERVICE CONDITIONED AIR CONNECTION BETWEEN C37-38.1 LT IS OUT OF LIM IT IAW SRM 53-10-00. REPAIR PERFORMED IAW EA 6-5314-101290 AND RAS/DATLS/0003182/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040200035 20070402 00035 EU 2007 4 2 07FDEA01019 1 20070320 A 5330 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 814FD 534 OLD REPAIR, EXTERNAL DOUBLER BETWEEN C66/67, P33/34 RT AND NOT CONFORM TO REPAIR REF: SRM53-10-12/FIG 203. REPAIR PERFO RMED BY INSTALLING NEW DOUBLER IAW EA 6-5317-101260 AND SRM 53-10-12/FIG 225. 2 L 7 2 4F RT A35EU 2007040200036 20070402 00036 EU 2007 4 2 07FDEA00953 1 20070316 A 5320 FLOOR SUPPORT AIRBUS 310 A310304 3930339 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 FOUND CORROSION AT MAIN DECK FLOOR STRUCTURE PARTS C74-75, P26 LT/RT (CONNECTING SECTION P/N A539-80458-200-90, P/N A5 39-80464-200-51 AND P/N A539-80464-201-00). PARTS REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007040200038 20070402 00038 EU 2007 4 2 07FDEA00955 1 20070316 A 5530 ATTACH FITTING AIRBUS 310 A310304 3930339 EU ZONE 300 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 V/S TAPERED ATTACH FITTINGS LT REAR, RT REAR AND RT CENTER BRONZE PLATING MISSING. PARTS REPLACED IAW AMM 55-30-11/401, P/N A555-72151-000-00 (1 EA.) AND P/N A555-72201-000- 00 (2 EA.) 2 L 7 2 4F RT A35EU 2007040200039 20070402 00039 EU 2007 4 2 07FDEA00956 1 20070316 A 5714 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 DEVIATIONS DURING ACCOMPLISHMENT OF SB A310-57-2035 REV 8 AT INTERNAL ANGLE OF CENTER WING BOX. REPAIR PERFORMED BY OVE RSIZING AFFECTED HOLES IAW EA 6-5710-103421 AND RAS/048070/031/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040200041 20070402 00041 EU 2007 4 2 07FDEA00958 1 20070316 A 5330 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 SKIN HAS DAMAGED AREA AROUND HOLE NR 12, C73-76, P26 RT, REPAIR WAS PERFORMED BY REAMING UP AND INSTALL A FREEZE PLUG IA W EA 6-5318-103403 REV A AND RAS/DAHAM/4021374/2006 ISSUE "C". 2 L 7 2 4F RT A35EU 2007040200042 20070402 00042 EU 2007 4 2 07FDEA00959 1 20070316 A 5710 STRUCTURE AIRBUS 310 A310324 3930206 EU ZONE 500 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 OUTER WING, CORROSION ON OVERWING REFUELING PORT LT. REPAIR WAS PERFORMED BY CORROSION REWORK IAW EA 6-5720-103412 AND RAS/BAE/1003838/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040200043 20070402 00043 EU 2007 4 2 07FDEA00960 1 20070316 A 5313 A53543033207 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FWD KARMAN STRUCTURE C36-37 MISDRILLED HOLE AT STRINGER A535-43033-207. REPAIR WAS PERFORMED IAW EA 6-5314-103429 AND R AS/SA/111/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040200047 20070402 00047 EU 2007 4 2 07FDEA00965 1 20070316 A 5754 SLAT TRACK AIRBUS 310 A310324 3930206 EU ZONE 500 WORN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 WEAR AT SLAT NR 3 LT, TRACK NR 9. REPAIR WAS PERFORMED IAW SRM 57-40-00 PB 101 AND APPROVED BY EA 6-5741-103381. 2 L 7 2 4F RT A35EU 2007040200050 20070402 00050 EU 2007 4 2 07FDEA00968 1 20070316 A 5311 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 CORROSION IN THE AIR CONDITIONING COMPARTMENT AT C42, P50-51 LT. REPAIR WAS PERFORMED BY CUT OUT AND INSTALLING A REPAI R ANGLE AND A NEW PICK UP ANGLE IAW EA 6-5315-103434 AND RAS/048419/005/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040200051 20070402 00051 EU 2007 4 2 07FDEA00969 1 20070316 A 5311 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 CORROSION IN THE AIR CONDITIONING COMP, C43-44, P47 RT. REPAIR WAS PERFORMED BY REWORK OF CORRODED AREA IAW EA 6-5315-1 03434 AND RAS/048419/005/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040200054 20070402 00054 WP 2007 4 2 07FDEA00972 1 20070316 A 5310 DOOR FRAME DOUG DC10 DC1010 3022110 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 FWD PIT BILGE STA 879 LWR SURFACE OF TOP FLANGE OF WEB CORRODED AT LONGERON 43R. ACCOMPLISHED REPAIR PER EA FUSELAGE FW D LOWER CARGO DOOR JAMB FRAME STA 866 CHORD REPAIR {8-5310-105181}. 2 L 7 3 4F A22WE 2007040200055 20070402 00055 WP 2007 4 2 07FDEA00973 1 20070316 A 5320 SILL DOUG DC10 DC1010 3022110 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 FWD CARGO DOOR CUT-OUT AFT SILL SEAL RETAINER DENTED STA 959 LONGERON 38R. REPAIRED IAW DC/MD SRM 53-50-00 VOL I, PAGE 132 AND EA 8-5310-105180 FUSELAGE FWD LOWER CARGO DOOR JAMB FRAME STA 959 CHORD AND SKIN REPAIR. 2 L 7 3 4F A22WE 2007040200056 20070402 00056 EU 2007 4 2 07FDEA00974 1 20070316 A 2721 RUDDER AIRBUS 300 A300B4622R 3930312 EU BINDING A FDEA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 SO 25 716FD 358 ON TAKEOFF ROLL, TOGA SELECTED PUSHED RUDDER FOR FREEDOM OF MOVEMENT AND THEY WOULD NOT MOVE LEFT AND RIGHT VERY STIFF, (FELT LIKE TRYING TO OVERRIDE THE AUTOPILOT ON AN AUTOLAND AUTO PILOT ON WITH ROLLOUT ON LANDING AND TRYING TO USE MANUA L RUDDER WITH A/P ON. ABORTED TAKEOFF. I/W RAN BOTH ENGINES PER JRH, TAXI A/C WHILE MOVING RUDDER PEDALS, FOUND NO BIN DING. PERFORMED ARTIFICIAL FEEL AND RUDDER TRAVEL LIMITING ADJUSTMENT TEST ACCORDING TO AMM 27-23-00-5 WITH THE EXCEPTI ON OF THE TEST OF THE VARIABLE STOP UNIT CYLINDER EXTENSION AND RUDDER DEFLECTION, PG 519 STEP D. ALL TESTS PASS AND IN DICATIONS ARE NORMAL. 2 L 7 2 4F RT A35EU 2007040200057 20070402 00057 NM 2007 4 2 NWAA071183156 1 20070328 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319114 3930350 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 356NB 12357 12357 1866 EMERGENCY EXIT LIGHT ON LEFT OVERWING EXIT NOT WORKING. REPLACED LEFT OVERWING EPSU, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 2007040200061 20070402 00061 NM 2007 4 2 AALA20070521 1 20070321 A 2420 430101 GCU BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4 54555 NE NR 1 GENERATOR INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SW 21 606AA 27057 31095 ON APPROACH INDICATION SHOWED OIL PRESSURE FOR NUMBER ONE ENGINE DROPPING. CREW SHUT LEFT ENGINE DOWN AT ABOUT 16 POUND S PER SQUARE INCH. LANDED TUL WITHOUT INCIDENT. SINGLE ENGINE TIME APPROXIMATELY THREE MINUTES. REPLACED BLEED VALVE CONTROL UNIT AND BOTH DEDICATED GENERATOR CONTROL UNITS FOR LEFT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2007040200062 20070402 00062 NM 2007 4 2 AALA20070527 1 20070322 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 346AN 33085 SFO - EMERGENCY LIGHT AT LEFT AFT DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT LEFT AFT DOOR. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007040200064 20070402 00064 WP 2007 4 2 AALA20070541 1 20070323 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 591AA 53254 LGA - EMERGENCY LIGHTS AT OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007040200065 20070402 00065 NM 2007 4 2 AALA20070526 1 20070322 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 631AA 24589 MIA - EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A2NM 2007040200066 20070402 00066 NM 2007 4 2 AALA20070523 1 20070322 A 3350 LENS BOEING 757 757231 1384950 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 705TE 28479 DFW - EMERGENCY FLOOR TRACK LIGHT IN FRONT OF LAVATORY D HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY FLOOR TRACK LIGHT IN FRONT OF LAVATORY D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007040200067 20070402 00067 NM 2007 4 2 AALA20070535 1 20070322 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 346AN 33085 SFO- EMERGENCY LIGHT AT LEFT FORWARD DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT LEFT FORWARD DOOR. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007040200068 20070402 00068 SO 2007 4 2 SIMA200708201 1 20070319 A 3350 78241 INVERTER EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT FAILED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 709GB 15936 145211 FOUND EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED NUMBER ONE INVERTER IAW EMB AMM 33-50-01. OPERATIONAL CHECK G OOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007040200070 20070402 00070 EA 2007 4 2 SIMA200708206 1 20070322 A 3520 M220D4N RELAY CNDAIR CL600 CL6002C10 1390015 EA COCKPIT FAILED A SIMA G O2 MASK DEPLOYED J WARNING INDICATION DE DESCENT 1 SW 21 522AE 7419 10147 FLAPS SELECTED TO 45 DEGREES ON FINAL RECEIVED PAX OXY ON CAUTION MESSAGE, PASSENGER PUSH LIGHT ON. PASSENGER OXYGEN MA SK DEPLOYED IN CABIN. REMOVED AND REPLACED RELAYS K130 AND K131. PERFORMED OPERATIONAL CHECK, RETURNED AIRCRAFT TO SER VICE. 2 L 7 2 4F RT A21EA 2007040200071 20070402 00071 EU 2007 4 2 07FDEA01046 1 20070320 A 2120 UNKNOWN AIRBUS 310 A310203 3930313 EU CABIN ODOR A FDEA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 25 442FE 353 AFTER LIFTOFF ON KMEM 18L, HEAVY ARID FUMES FILLED COCKPIT FOLLOWED MAY RED MAIN DECK SMOKE WARNING AND CRC CHIMES. DEC LARED EMERGENCY AND LANDED ON RUNWAY 27. FUMES STILL HEAVY. EVACUATED AIRCRAFT ON RUNWAY. RAN PACKS ON GROUND. NOTE D THE ODOR OF OIL WHILE PACKS ARE RUNNING WITH APU AIR INSP DUCT AT THE OUTLET SIDE OF APU LOAD BLEED VALVE. NO OIL NO TED. REINSTALLED DUCT AND CLAMP. RAN APU. LEAK CHECK GOOD. REMOVED AND REPLACED AVIONICS COOLING AIR FILTER AS PRECA UTIONARY PER SMP. REPLACED COALESCER BAGS (PRECAUTIONARY). PERFORMED ENG RUNS AT PWR PER A310 JRH. NO ODOR NOTED DURI NG ENG RUNS. NO DEFECTS NOTED AT THIS TIME REINSTALLED PACK BAY PANEL PER SMP. 2 L 7 2 4F RT A35EU 2007040200072 20070402 00072 2007 4 2 IXXA070019O 4 20070324 A 2310 5220536016 HF COMM DOUG DC8 DC862F 3021972 WP NR 1 DEFECTIVE A IXXA O OTHER O OTHER CR CRUISE 1 SW 11 41CX 81558 718 46129 DURING FLIGHT FROM KBWI THE NR 1 AND NR 2 HF SYSTEM FAILED. THE CREW DID ALL NECESSARY PROCEDURES AND RETURNED TO KBWI LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NR 1 AND NR 2 HF SYSTEM, RESEATED THE NR 1 HF SYSTEM OPERATIONAL CHE CK GOOD. REPLACED NR 2 HF ACC COUPLER OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2007040200073 20070402 00073 EU 2007 4 2 MALA070040 1 20070311 A 3610 DUCT SAAB SF340 340B 7860101 EU BLEED AIR SYS LEAKING A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 422XJ 340B422 AIRCRAFT DID AN AIR RETURN FOR THE RT BLEED LEAK INDICATION COMING ON AFTER TAKEOFF. THE CREW FOLLOWED THE QRH AND LAND ED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED RT ELBOW AT FWD DUCT (RED HOSE) IAW AMM 21-20-00. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2007040200075 20070402 00075 EU 2007 4 2 07FDEA00747 1 20070312 A 5313 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CORROSION, OLD STRINGER REPAIR AT C42/43, P50 RT. VERIFICATION SHOWS THAT REPAIR IS NOT CONFORM TO SRM 53-10-14, FIG 201A, SEC.A-A. 2 L 7 2 4F RT A35EU 2007040200077 20070402 00077 NM 2007 4 2 07FDEA00752 1 20070312 A 5347 BAC1520792 SEAT TRACK BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 MAIN DECK FLOOR SEAT TRACK OTBD FLANGE IS CORRODED AT BS 950 ,10 TO 950A 8, LBL 25, WL 208. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS REF SRM 53-10-1 FIG 3. REPAIRED SEAT TRACK REF SRM 53-10-5 FIG 7. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007040200078 20070402 00078 EU 2007 4 2 AWXA200700385 1 20070227 A 5754 D5746020000500 SKIN AIRBUS 320 A320231 3930325 EU ZONE 600 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 627AW 66 SAL - WORN AREA ON RIGHT WING NR 2 SLAT, LOWER SURFACE TRAILING EDGE, WS 4862. REPAIRED RIGHT WING NR 2 SLAT, LOWER SUR FACE TRAILING EDGE, WS 4862 IAW AWA ER 26-5743-07072-SS1. 2 L 7 2 4F RT A28NM 2007040200079 20070402 00079 EU 2007 4 2 AWXA200700386 1 20070227 A 5753 D57571307200 ANGLE AIRBUS 320 A320231 3930325 EU ZONE 500 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 627AW 66 SAL - FOUND CORROSION ON LEFT WING INBOARD FLAP, INTERCONNECTION STRUT FITTING HOLE, WS 4067/RIB 8. REPLACED LEFT WING INBOARD FLAP, INTERCONNECTION STRUT FITTING, WS 4067/RIB 8 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007040200080 20070402 00080 EU 2007 4 2 AWXA200700387 1 20070228 A 5522 D55281232000 SKIN AIRBUS 320 A320231 3930325 EU ZONE 300 DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 627AW 66 SAL - FOUND RIGHT ELEVATOR UPPER SKIN PANEL HAS EVIDENCE OF TRAPPED WATER AND IS DEBONDED, BETWEEN RIB 1 AND RIB 4. REP AIRED RIGHT ELEVATOR UPPER SKIN PANEL BETWEEN RIB 1 AND RIB 4 IAW A320 SRM 51-77-13 PARAGRAPH 2A(2), FIGURE 2. 2 L 7 2 4F RT A28NM 2007040200081 20070402 00081 NM 2007 4 2 AWXA200700388 1 20070307 A 5340 69353521 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED STRINGER CLIP, BS 597, S8R. REPLACED STRINGER CLIP, BS 597, S8R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007040200082 20070402 00082 NM 2007 4 2 AWXA200700389 1 20070307 A 5340 69353521 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED STRINGER CLIP, BS 663, S10L. REPLACED STRINGER CLIP, BS 663, S10L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007040200085 20070402 00085 NM 2007 4 2 UIEA200700138 1 20070314 A 2780 PDU BOEING 747 74747UF 1384949 NM FLAP DAMAGED A UIEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 15 492MC 70010 29253 EICAS "FLAP DRIVE" LEFT MID LEADING EDGE DID NOT RETRACT, THEN MID AND INBOARD LEADING EDGE DID NOT EXTEND. REMOVED AND REPLACED NR 3 LEFT LEADING EDGE PDU AS PER MM 27-81-03. GROUND OPERATION NORMAL. 2 L 7 4 4F RT 1384945 2007040200088 20070402 00088 NM 2007 4 2 SWAA071595 1 20070327 A 5311 6546540 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 15R TO STR 16R. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2007040200089 20070402 00089 NM 2007 4 2 AWXA200700406 1 20070312 A 5340 69353521 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - FOUND CRACKED STRINGER CLIP, BS 727E, S24L. REPLACED STRINGER CLIP, BS 727E, S24L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007040200090 20070402 00090 NM 2007 4 2 SWAA071594 1 20070327 A 5311 6546541 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663.75, STR 1. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2007040200091 20070402 00091 NM 2007 4 2 SWAA071592 1 20070327 A 5315 6548804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 1016 UPPER SURFACE. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007040200092 20070402 00092 NM 2007 4 2 SWAA071588 1 20070327 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 27L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007040200093 20070402 00093 NM 2007 4 2 SWAA071593 1 20070327 A 5753 65C30462 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP PUNCTURED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD FORE FLAP PUNCTURED AT LOWER SURFACE. REPAIRED FORE FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007040200094 20070402 00094 NM 2007 4 2 AWXA200700407 1 20070311 A 5340 69353521 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - FOUND CRACKED STRINGER CLIP, BS 706, S1. REPLACED STRINGER CLIP, BS 706, S1 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007040200095 20070402 00095 NM 2007 4 2 AWXA200700408 1 20070311 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - FOUND CRACKED STRINGER CLIP, BS 616, S8R. REPLACED STRINGER CLIP, BS 616, S8R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007040200097 20070402 00097 EU 2007 4 2 2007UALA00896 1 20070324 A 2930 WARNING SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYDRAULIC SYS ACTIVATED A UALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 407UA 456 AFTER TAKEOFF RECEIVED ECAM FOR GREEN HYDRAULIC LOW LEVEL. AMBER ALERT AND EMERGENCY DECLARED WITH ATC WITH EMERGENCY E QUIPMENT MEETING FLIGHT AT PLANNED DESTINATION. [SUP 06-01-07] A HYDRAULIC PRESSURE LINE IN THE UPPER FORWARD LT PYLON WORN THROUGH FROM CONTACT WITH ADJACENT HYDRAULIC RETURN LINE. MANUFACTURED AND INSTALLED NEW PRESSURE AND RETURN LINES WITH PROPER CLEARANCE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007040200098 20070402 00098 NM 2007 4 2 2007UALA00897 1 20070325 A 3297 CIRCUIT CARD BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU MLG MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 340UA 24244 RIGHT MLG RED LIGHT ON WITH HANDLE DOWN AND LOCKED, GEAR DOWN AND LOCKED. FAULTY DOWN LOCK CARD. REPLACED M981 RT MLG D OWN LOCK CARD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007040200099 20070402 00099 NM 2007 4 2 QXEA200700446 1 20070323 A 6123 3014403 TSCU DHAV DHC8 DHC8202 2809007 NM AUTOFEATHERING MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 358PH 8818 126 506 EUG FLIGHT NR 2218, FAILURE ON AUTOFEATHER ARM LIGHT TO ILLUMINATE. MAINTENANCE REPLACED NR 1 AND NR 2 TACU. AUTOFEATH ER ARM LIGHT ILLUMINATED AND AUTOFEATHER OPERATES NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007040200100 20070402 00100 NM 2007 4 2 QXEA200700447 1 20070325 A 3320 COVER DHAV DHC8 DHC8202 2809007 NM CABIN LIGHT DISLODGED A QXEA D RETURN TO BLOCK D INFLIGHT SEPARATION TX TAXI/GRND HDL 1 NM 09 352PH 494 PDX FLIGHT NR 2248, DURING TAXI OUT, PLASTIC LIGHT COVER FELL DOWN. MAINTENANCE REINSTALLED PLASTIC LIGHT COVER. NO PA RTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007040200102 20070402 00102 WP 2007 4 2 AALA20070381 1 20070221 A 3350 WIRE HARNESS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 246AA 49258 YUL - EMERGENCY EXIT LIGHT AT SEAT 5EF INOPERATIVE. REPAIRED HARNESS FOR EMERGENCY LIGHT AT SEAT 5EF. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007040200103 20070402 00103 NM 2007 4 2 2007UALA00898 1 20070325 A 2613 CIRCUIT CARD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 657UA 27112 RIGHT FUEL CUT OFF SWITCH FIRE TEST INOPERATIVE. [SUP 4-20-07] AFTER TROUBLESHOOTING FOUND LOGIC TEST FIRE OVERHEAT CA RD M10274 AT FAULT. REPLACED CARD PER MM26-10-0 1, OP CHECKS GOOD. RETURN TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007040200104 20070402 00104 WP 2007 4 2 AALA20070386 1 20070223 A 3230 SCHRADER VALVE DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 253AA 49286 LAX INFLIGHT - AFTER TAKEOFF CAPTAIN WAS UNABLE TO RAISE NOSE LANDING GEAR. RETURNED TO LAX AND LANDED WITHOUT INCIDEN T. REMOVED PISTON AND INSPECTED. REPLACED STRUT. INSTALLED NEW SCHRADER VALVE AND O-RING. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F A6WE 2007040200105 20070402 00105 WP 2007 4 2 AALA20070399 1 20070225 A 7830 ACCUMULATOR DOUG DC9 DC983 3022083 WP THRUST REVERSER LEAKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 590AA 53253 DFW INFLIGHT - DURING CLIMB CREW COULD SMELL ODOR IN COCKPIT. FLIGHT ATTENDANT REPORTED SMELL AND SMOKE IN CABIN. TUR NED PACKS TO COLD AND RETURNED TO DFW AND LANDED WITHOUT INCIDENT. SMOKE CLEARED PRIOR TO LANDING. FOUND LEFT THRUST R EVERSER ACCUMULATOR LEAKING. REPLACED LEFT THRUST REVERSER ACCUMULATOR. PERFORMED BURN OUT OF HIGH PRESSURE PNEUMATIC DUCTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007040200107 20070402 00107 NM 2007 4 2 AALA20070395 1 20070224 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 354AA 24035 DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007040200108 20070402 00108 NM 2007 4 2 AALA20070398 1 20070223 A 3397 FUSE BOEING 777 777223 1385213 NM BATTERY PACK FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 DFW - EMERGENCY EXIT LIGHT AT LEFT NUMBER THREE DOOR INOPERATIVE. REPLACED FUSE IN EMERGENCY PATTERY PACK M33406 FOR EM ERGENCY EXIT LIGHT AT LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007040200110 20070402 00110 EU 2007 4 2 AALA20070407 1 20070226 A 3297 WIRE AIRBUS 300 A300B4605R 3930308 EU NR 2 BRAKES INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7055A 462 SJU INFLIGHT - CREW RECEIVED HIGH TEMPERATURE INDICATION FOR BRAKE NUMBER TWO DURING TAKEOFF. RETURENED TO SJU AND LAND ED WITHOUT INCIDENT. REPLACED WIRING FOR NUMBER ONE AND TWO BRAKE FAN AND TRANSDUCERS. SYSTEM GROUND CHECKED NORMAL OP ERATION. 2 L 7 2 4F RT A35EU 2007040200111 20070402 00111 WP 2007 4 2 AALA20070385 1 20070223 A 3231 DOOR DOUG DC9 DC982 3022082 WP NOSE GEAR INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 443AA 49469 ORD INFLIGHT - AFTER TAKEOFF CREW RETRACTED NOSE GEAR AND EXPERIENCE A SEVERE NOSE GEAR DOOR VIBRATION. LOWERED GEAR AN D VIBRATION REDUCED. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. FOUND LEFT NOSE GEAR DOORS DOWN. PERFORMED NOSE GEA R DOOR INSPECTION WITH NO DEFECTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007040200113 20070402 00113 WP 2007 4 2 AALA20070380 1 20070222 A 3010 13277505 DUCT DOUG DC9 DC982 3022082 WP ANTI ICE SYSTEM BLOWN A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 484AA 49677 TPA INFLIGHT - LEFT FIRE WARNING ACTIVATED AFTER DURING CLIMB. RETURNED TO TPA AND LANDED WITHOUT INCIDENT. FIRE WARNI NG STOPPED AFTER REDUCING THROTTLE TO IDLE. REPLACED ANTI-ICE DUCT AND UPPER COWLING. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F A6WE 2007040200114 20070402 00114 NM 2007 4 2 AALA20070394 1 20070223 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 191AN 32385 DFW - EMERGENCY LIGHT AT SEAT 23D INOPERATIVE. REPLACED BROKEN CONNECTOR AT SIDEWALL FOR EMERGENCY LIGHT AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007033000122 20070330 00122 NM 2007 3 30 AWXA200700377 1 20070310 A 5340 693535012 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND FORWARD CARGO COMPARTMENT STRINGER CLIP CRACKED, BS 500, S20R. REPLACED FORWARD CARGO COMPARTMENT STRINGER CLIP, BS 500, S20R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007033000123 20070330 00123 NM 2007 3 30 AWXA200700378 1 20070305 A 5754 65C267995 SKIN BOEING 737 7373G7 1384595 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND LEFT WING NR 1 SLAT LOWER SURFACE CRACKED, SS 357. REPAIRED LEFT WING NR 1 SLAT LOWER SURFACE, SS 288 - SS 363 IAW B737-300 SRM 57-43-01. 2 L 7 2 4F RT A16WE 2007033000128 20070330 00128 EA 2007 3 30 QXEA200700378 1 20070217 A 3020 54011485 VALVE CNDAIR CL600 CL6002C10 1390015 EA ANTI ICE INOPERATIVE A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 604QX 3478 3478 10019 SEA - ON FLIGHT 2543, RIGHT COWL ANTI ICE MESSAGE APPEARED APPROX 15 SECONDS AFTER SELECTING COWL ANTI ICE PAGE SHOWED M AGNETIC RING AROUND VALVE AS PER CHECKLIST. RECYCLED RIGHT COWL ANTI ICE SWITCH SYSTEM OPERATED NORMALLY FOR ABOUT 20 S ECONDS THEN RIGHT COWL ANTI ICE MESSAGE APPEARED AGAIN. MAINTENANCE REMOVED AND REPLACED RIGHT COWL ANTI ICE VALVE. OP ERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007033000143 20070330 00143 NM 2007 3 30 AWXA200700411 1 20070307 A 5320 69265552 INTERCOSTAL BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED UPPER INTERCOSTAL CLIP, BS 348.2, S16L. REPLACED UPPER INTERCOSTAL CLIP, BS 348.2, S16L IAW AWA ER 03-5312-07083-ES1. 2 L 7 2 4F RT A16WE 2007033000144 20070330 00144 NM 2007 3 30 AWXA200700412 1 20070307 A 5320 69489854 INTERCOSTAL BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED INTERCOSTAL CLIP, BS 360, S10L. REPLACED INTERCOSTAL CLIP, BS 360, S10L IAW AWA ER 03-5312-07083-ES 1. 2 L 7 2 4F RT A16WE 2007033000145 20070330 00145 NM 2007 3 30 AWXA200700413 1 20070307 A 5320 6517684642 INTERCOSTAL BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED INTERCOSTAL WEB, BS 294.5, S7L. REPLACED INTERCOSTAL WEB, BS 294.5, S7L IAW AWA ER 03-5312-07083-E S1. 2 L 7 2 4F RT A16WE 2007033000200 20070330 00200 2007 3 30 SWAA071571 4 20070325 A 2565 416A2200 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 449WN 32469 L1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2007033000210 20070330 00210 WP 2007 3 30 ASAA0781551 1 20070328 A 5320 990777013 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 AFT ACCESSORY INTERCOSTAL CRACKED. REPLACED INTERCOSTAL PER SRM 51-10-4 AND 51-30-2. 2 L 7 2 4F RT A6WE 2007033000216 20070330 00216 NM 2007 3 30 HALA0700106 1 20070316 A 2410 BEARING BOEING 767 76733A 1385209 NM NR 2 IDG WORN A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, NUMBER 2 IDG OVERFILL PORT COVER RETAINING BEARINGS WORN OUT. REPLACED COVER ENGAGES NORMALLY . 2 L 7 2 4F RT A1NM 2007033000243 20070330 00243 NM 2007 3 30 ASAA0741547 1 20070326 A 5311 65C22910 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 FRAME CRACKED. REPAIRED FRAME IAW SRM 53-00-07 FIG 201. 2 L 7 2 4F RT A16WE 2007033000247 20070330 00247 NM 2007 3 30 AWXA200700422 1 20070307 A 5320 651768470 INTERCOSTAL BOEING 737 7373G7 1384595 NM ZONE 200 CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND INTERCOSTAL WEB CHAFED, BS 301, S13L - S14L. REPLACED INTERCOSTAL WEB, BS 301, S13L - S14L IAW AWA ER 03-53 12-07083-ES1. 2 L 7 2 4F RT A16WE 2007033000250 20070330 00250 NM 2007 3 30 F3LA200700046 1 20070319 A 3350 2LA00541401 LIGHT AIRBUS A319 A319111 3930336 NM EXTERIOR OVWING INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 936FR 2392 MAINTENANCE REPORTED RT AFT EMERGENCY OVERWING OUTSIDE LIGHT (62WL) INOP. REPLACED LIGHT ASSY (62WL) IAW 33-51-15-400-0 01. 2 L 7 2 4F RT A28NM 2007033000251 20070330 00251 EU 2007 3 30 MALA070042 1 20070321 A 3350 COVER SAAB SF340 340B 7860101 EU EMEGENCY LIGHT WRONG PART A MALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 15 430XJ 340B430 ON LC1, NOTED RT FORWARD EMERGENCY EXIT COVER WAS WRONG PART. REPLACED RT FORWARD EMERGENCY EXIT COVER WITH CORRECT PAR T NUMBER 43-206-2 IAW SF340 AMM 52-20-05-02. 2 L 7 2 4T RT A52EU 2007033000252 20070330 00252 NM 2007 3 30 CALA0700143 1 20070323 A 5320 141A8310U31 STRUCTURE BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 36247 28807 INSPECTION FOUND R-1 DOOR CHORD CORRODED AT STA 277-344, RBL 61 TO RBL 64. THE CHORD WAS REMOVED AND REPLACED IAW SRM 5 1-40-02. 2 L 7 2 4F RT A16WE 2007033000264 20070330 00264 NM 2007 3 30 DHL2007786507 1 20070322 A 5260 AIRSTAIR BOEING 727 727214 138407R NM BS 1329 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 FOUND CRACK AT LIGHTENING HOLE RT LWR TORQUE BOX STA 1329. STOP DRILLED .250 DIA HOLE AT LIGHTENING HOLE RT LWR TORQUE BOX STA 1329 IAW B727 SRM 51-40-2. HFEC FOR CRACK STOP VERIFIED IAW B727 NDTM PT6 51-00-00 FIG 23. FABRICATED DOUBLER REPAIR AT LIGHTENING HOLE FROM 7075T6, .040, 5.75 BY 3.50 IAW B727 SRM 53-10-2, FIG 6 AND 51-40-2 FIG 1. TREATED ALODIN E AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR AT LIGHTENING HOLE IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007033000265 20070330 00265 EA 2007 3 30 QXEA200700445 1 20070324 A 2611 4462534 SMOKE DETECTOR CNDAIR CL600 CL6002C10 1390015 EA LAVATORY MALFUNCTIONED A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 290RB 3524 10029 BUR - LAVATORY AFT SMOKE DETECTOR CAME ON THREE TIMES. MAINTENANCE REPLACED THE LAVATORY SMOKE DETECTOR. OPERATIONAL C HECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007033000271 20070330 00271 SO 2007 3 30 SIMA200707805 1 20070317 A 3320 BR90002 BALLAST EMB 145 EMB145LR 3260212 SO CABIN LIGHTS FAILED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 21 642AE 16456 145193 SEVERAL OVERHEAD CABIN LIGHTS INOPERATIVE ABOVE ROWS 16 AND 17A, SMOKE SMELL REPORTED. REMOVED AND REPLACED BALLAST FOR CEILING LIGHTS AT 16 AND 17A IAW EMB AMM 33-21-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007033000287 20070330 00287 EA 2007 3 30 COMA0760280 1 20070323 A 5270 840534 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 936CA 7043 FLIGHT 5111 - RECEIVED PAX DOOR OUTER HANDLE WARNING MESSAGE. PERFORMED QRH, DID NOT RESET. DECLARED EMERGENCY, DIVERT ED TO TYS AND LANDED WITHOUT INCIDENT. HANDLE WAS OBSERVED TO BE STOWED ON GROUND. REPLACED PROX SENSOR DI-17. NO FUR THER DEFECTS. 2 L 7 2 4F RT A21EA 2007033000295 20070330 00295 WP 2007 3 30 UPS07849571 1 20070328 A 2910 PACKING DOUG DC8 DC873F 302199F WP HYDRAULIC SYS LEAKING A IPXA O OTHER K FLUID LOSS CR CRUISE 1 SO 01 803UP 46073 AT CRUISE FL 350 HYD PRESS SENT TO ZERO AND HYD QTY WENT TO EMER/AUX POSITION. LOSS OF HYD QTY AND PRESS CHECKLIST ACCOM PLISHED. REPLACED PACKINGS & RETAINER RINGS REF IPC 29-11-24 ITEM 175,180,185 ON WING SLOT CONTROL VALVE IAW MM 27-80- 04-2. LEAK AND OPS CHECKED GOOD. NO CONTROL VALVE ARM WAS DISCONNECTED OR ADJUSTED. 2 L 7 4 4F RT 4A25 2007033000299 20070330 00299 NM 2007 3 30 KCSA071093 1 20070328 A 5315 FLOORBEAM BOEING 747 747236B 1384804 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STA 360 FLOORBEAM UPPER CHORD HAS AREA OF CORROSION AT LBL 34, WL 312. 2 L 7 4 4F 4 F A20WE E3NE 2007033000306 20070330 00306 NM 2007 3 30 KCSA071099 1 20070329 A 5312 BULKHEAD BOEING 747 747236B 1384804 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 AFT PRESSURE BULKHEAD HAS 2 DENTS STA 2382, WL 190, RBL 40. 2 L 7 4 4F 4 F A20WE E3NE 2007033000307 20070330 00307 NM 2007 3 30 KCSA071100 1 20070329 A 5311 FRAME BOEING 747 747236B 1384804 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STA 1720 RBL 46 BOTTOM OF FRAME WEB HAS 2 SMALL HOLES FROM CHAFING. 2 L 7 4 4F 4 F A20WE E3NE 2007033000315 20070330 00315 NM 2007 3 30 AMTA200700131 1 20070304 A 5551 PIN BOEING 737 73783N 13844HI NM HORIZ STAB CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 321TZ 28249 LT AFT UPPER HORIZ STAB ATTACHMENT PIN HAS CORROSION PITTING FUSE 1147. REMOVED AND REPLACED HORIZ STAB PIN PN 180A161- 3 IAW EO 737-55AD-2935. (K) 2 L 7 2 4F RT A16WE 2007033000316 20070330 00316 2007 3 30 AMTA200700144 4 20070309 A 2310 HF COMM BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE LEFT MALFUNCTIONED A AMTA K NONE L NO TEST CR CRUISE 1 GL 11 560TZ 33525 LT HF WILL NOT TUNE OR TRANSMITT. RECEPTION NORMAL. PERFORMED STATIS BITE CHECK OF LT HF TXCR IAW FIM 23-11-00. NO FA ULTS NOTED PERFORMED A STATIS COMMS CHECK OF LT HF SYSTEM. OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007033000320 20070330 00320 WP 2007 3 30 AMTA200700170 1 20070323 A 2597 WIRE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE COFFEEMAKER SHORTED A AMTA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 161AT 1219 APPROX 6 MINUTES AFTER T/O, SFA REPORTED HEARING ARCING AND SEE SMOKE IN AREA OF LT FWD COFFEEMAKERS. TURNED OFF GALLEY POWER AND MUX ARCING AND SMOKE STOPPED. FOUND WIRES SHORTED ON TOP OF COFFEE MAKER. REMOVED AND REPLACED LT FWD IB CO FFEEMAKER OPS CHECK GOOD NO FAULTS NOTED. (K) 2 L 7 3 4F 4 F A23WE E12EU 2007033000321 20070330 00321 NM 2007 3 30 AMTA200700147 1 20070312 A 3350 S417N5101007 COVER BOEING 737 73783N 13844HI NM CABIN MISSING A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 319TZ 30643 AFT GALLEY L-2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED NEW EXIT SIGN ASSY, OPS CHECK NORMAL IAW M M33-5-1-01. (K) 2 L 7 2 4F RT A16WE 2007033000346 20070330 00346 NM 2007 3 30 SWAA071586 1 20070327 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 309SW 22948 FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2007033000349 20070330 00349 NM 2007 3 30 SWAA071599 1 20070327 A 5330 6545766 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16L. REPAIRED SKIN PER SRM & EA. 2 L 7 2 4F RT A16WE 2007033000350 20070330 00350 NM 2007 3 30 SWAA071601 1 20070327 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 413 TO BS 433, LBL 3 TO RBL 3. REPAIRED SKIN PER E A. 2 L 7 2 4F RT A16WE 2007033000352 20070330 00352 NM 2007 3 30 SWAA071591 1 20070327 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 912, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007033000353 20070330 00353 NM 2007 3 30 SWAA071590 1 20070327 A 5753 6546431 WEDGE BOEING 737 7373Y0 1384671 NM T/E FLAP DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED 20Y CHECK, FOUND LEFT WING OUTBOARD FORE FLAP T/E WEDGE DISBONDED. REMOVED AND REPLACED FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2007033000370 20070330 00370 EU 2007 3 30 07FDEA01068 1 20070321 A 5315 STIFFENER AIRBUS 310 A310222 3930315 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 MDCC - FLOORBEAM C37, FWD FACE, VERTICAL STIFFENER AT TOP HAS .5 INCH CRACK LOCATED BETWEEN NR 4L AND 5L SEAT TRACK RO UTED OUT CRACKED VERTICAL STIFFENER IAW A310/200 SRM 53-10-15 NDT VERIFIED CRACK. REMOVAL FABRICATED REPAIR ANGLES IAW A310/200 SRM, 53-10-15. INSTALLED REPAIR ANGLES IAW A310/200 SRM 53-10-15. 2 L 7 2 4F RT A35EU 2007040200002 20070402 00002 NM 2007 4 2 07FDEA00975 1 20070317 A 2150 A/C PACK DOUG MD11 MD11 3023602 NM CONTAMINATED A FDEA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 25 579FE 48470 AT 100KTS ON T/O ROLL RECEIVED LEVEL-3 CABIN SMOKE ALERT. TAKEOFF ABORTED. LIGHT REMAINED ON 3 SECONDS AND NEVER REILL UMINATED. ALL OTHER INDICATIONS OF FIRE NEGATIVE. COMPLIED WITH RTS ON ESC ALL RTS PASS. A/C WAS DEICED PRIOR TO A/C DEPERATURE SUSPECT DEICING FLUID INGESTED INTO PACKS. ALL SYSTEM CHECK GOOD. A/C OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2007040200009 20070402 00009 NM 2007 4 2 07FDEA00982 1 20070318 A 5320 INTERCOSTAL BOEING 727 727225 1384077 NM BS 348-360 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 INTERCOSTAL CORRODED FS 348 TO 360 AT STR 9L. REMOVED CORROSION, CHECKED LIMITS, IAW SRM 53-104-1, FIG 1, SHEET 2. FAB `D NEW FILLER AND DOUBLER FROM 7075-T6, .040C BATCH 1107917 AND 7075-T6, .050C BATCH 76174. IAW SRM 51-40-2, FIG 1. INS TALLED FILLER AND DOUBLER IAW SRM 51-40-2, FIG 1, PG 1-6. 2 L 7 3 4F A3WE 2007040200037 20070402 00037 EU 2007 4 2 07FDEA00954 1 20070316 A 5320 FLOOR SUPPORT AIRBUS 310 A310304 3930339 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 CORROSION AT MAIN DECK FLOOR STRUCTURE PARTS C74-75, P26 LT/RT, CONNECTING SECTION P/N A539-80458-200-90, P/N A539-80464 -200-51 AND P/N A539-80464-201-00. PARTS REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007040200040 20070402 00040 EU 2007 4 2 07FDEA00957 1 20070316 A 5714 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 DEVIATIONS DURING ACCOMPLISHMENT OF SB A310-57-2035 REV.8 AT INTERNAL ANGLE OF CENTER WING BOX. REPAIR PERFORMED BY OVE RSIZING AFFECTED HOLES IAW EA 6-5710-103421 AND RAS/048070/031/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040200045 20070402 00045 EU 2007 4 2 07FDEA00963 1 20070316 A 5311 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CORROSION IN THE AIR CONDITIONING COMP, C42, P50-51 RT. REPAIR WAS PERFORMED BY CUT OUT AND INTALLING A REPAIR AN GLE AND A NEW PICK UP ANGLE IAW EA 6-5315-103434 AND RAS/048419/005/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040200046 20070402 00046 EU 2007 4 2 07FDEA00964 1 20070316 A 5320 A25775030004 TRACK AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 MISDRILLED HOLE ON ROLLERTRACK AT C62 RT, Y-1470. REPAIR WAS PERFORMED BY REAM UP AND INSTALL FREEZE PLUGS IAW EA 6-531 7-106354 REV A AND RAS/DATLS/0003496/2006 ISSUE "B". 2 L 7 2 4F RT A35EU 2007040200048 20070402 00048 EU 2007 4 2 07FDEA00966 1 20070316 A 5311 A53989505202 FRAME AIRBUS 310 A310324 3930206 EU ZONE 300 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FUSELAGE TAIL SECTION, CORROSION AT C102, BETWEEN P13 LT AND P13 RT. REPAIR WAS PERFORMED BY TRIM THE FRAME OUTER FLANG E TO ALLOW FASTENER INSTALLATION. 2 L 7 2 4F RT A35EU 2007040200052 20070402 00052 WP 2007 4 2 07FDEA00970 1 20070316 A 5330 DOUBLER DOUG DC10 DC1010 3022110 WP ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 EXTERNAL FUSELAGE FROM FWD TO AFT SIDE LOWER EDGE CARGO DOOR CUT-OUT, SKIN DAMAGED ALONG SILL CUT-OUT, UPPER CARGO DOOR. REMOVED AND REPLACED DOUBLERS AT STA 629, 662, 676, 693 AND 762 AT MAIN CARGO DOOR LOWER SKIN IAW DC/MD10 SRM 51-3 3-01 VOL II PAGE 1 AND DC/MD10 53-50-00 VOL I. 2 L 7 3 4F A22WE 2007040200058 20070402 00058 NM 2007 4 2 AALA20070540 1 20070323 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGE NCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 657AM 24615 MIA - FOUND EMERGENCY LIGHT AT SEAT 33D INOPERATIVE. SECURED LOOSE CONNECTOR AT SEAT 33D FOR EMERGENCY LIGHT. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007040200101 20070402 00101 SO 2007 4 2 SIMA200706801 1 20070308 A 7720 AE3007A1 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 OVERTEMP A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 682AE 6726 14500826 CAE312630 "SUP" ON CLIMB OUT OF 10,000 FT NR 1 INLET TURBINE TEMPERATURE WENT TO 920 DEGREES, RETARDED THRUST LEVER TEMPERATURE DR OPPED TO 880 DEGREES. AIRCRAFT RETURNED TO ORD. REMOVED AND REPLACED NUMBER ONE ENGINE IAW AMERICAN EAGLE WORK CARD 72 -000-00. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007040200109 20070402 00109 NE 2007 4 2 2007UALA00899 2 20070325 A 7200 CASE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 2 ENGINE WORN A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 667UA 29239 727817 NR 2 ENGINE CASE WORN. [SUP 4-20-07] NR 2 ENG CASE WORN DUE TO TOOLING FOUND LODGED UNDER UNISON RING. ALSO FOUND BREA THER TUBE CHAFING. FOUND TUBE DAMAGE TO BE LESS THAN 10 PERCENT OF WALL THICKNESS. THE TUBE DAMAGE IS WITHIN LIMITS. FOUND WEAR MARK ON THE ENG CASE TO BE NO GREATER 0.010 TO 0.015 DEEP..PER EID 72-35-40-01 P6 OF 28 WARE WITHIN LIMITS. DAMAGE EVALUATED BY ENGINEERING AT TERMINATION OF FERRY FLT. CHECKED OK FOR SERVICE. ALL DAMAGE WITHIN LIMITS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007040200112 20070402 00112 WP 2007 4 2 AALA20070383 1 20070222 A 3520 OXYGEN MASK DOUG DC9 DC982 3022082 WP CABIN DEPLOYED A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 472AA 49647 DFW INFLIGHT - AIRCRAFT EXPERIENCED PRESSURIZATION PROBLEMS DURING CLIMB AND PASSENGER OXYGEN MASKS DEPLOYED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED ALL PASSENGER OXYGEN MASKS AND OXYGEN GENERATORS REPLACED AS NECESSARY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007040200115 20070402 00115 NM 2007 4 2 AALA20070382 1 20070222 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 366AA 25193 DFW - EMERGENCY LIGHT AT LEFT OVERWING INOPERATIVE. RELAMPED EMERGENCY LIGHT AT LEFT OVERWING. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007040200116 20070402 00116 WP 2007 4 2 AALA20070388 1 20070223 A 2150 A/C PACK DOUG DC9 DC983 3022083 WP A/C BAY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 21 973TW 53623 PDX INFLIGHT - DURING APPROACH WITH TAIL DE-ICE SELECTED CREW REPORTED STRONG BURNING SMELL WITH SOME OBSTRUCTED VISIBIL ITY DUE TO SMOKY AIR. LANDED PDX WITHOUT INCIDENT. INSPECTED ENGINES, APU, AIR CONDITIONING PACKS AND SURROUNDING AREA S FOR LEAKS AND DISCREPANCIES. NO DISCREPANCIES NOTED. ACCOMPLISHED PACK BURN ON BOTH PACKS AND DUCTING. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007040200118 20070402 00118 NE 2007 4 2 QXEA200700463 2 20070327 A 7530 4120T03P04 ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE COMPRESS VG LEAKING A QXEA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 617QX 10130 DEN - ON POST FLIGHT INSPECTION NOTED FUEL LEAK AT NR 1 ENGINE. MAINTENANCE REPLACED THE SLAVE COMPRESSOR VG ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007040200120 20070402 00120 EA 2007 4 2 QXEA200700464 1 20070327 A 7410 IGNITION SYS CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE NR 2 ENGINE MALFUNCTIONED A QXEA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 613QX 10045 SEA - DURING START OF NR 2 ENGINE RECEIVED A RIGHT IGNITION "A" FAULT STATUS MESSAGE. PUSHBACK OPERATOR NOTICED EXCESSI VE SMOKE AND FLAME FROM THE ENGINE. THE ENGINE STARTED NORMALLY. MAINTENANCE PLACED THE "A" IGNITION SYSTEM ON MEL 74- 11-1A. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007040200121 20070402 00121 NM 2007 4 2 AALA20070390 1 20070224 A 5220 HANDLE BOEING 767 767323 1385205 NM EMERGENCY EXIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 357AA 24038 CDG - FOUND EMERGENCY EXIT HANDLE AT SEAT 20J PANEL INOPERATIVE. REINSTALLED EMERGENCY EXIT HANDLE AT SEAT 20J PANEL. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007040200122 20070402 00122 NM 2007 4 2 07FDEA00721 1 20070308 A 5347 BAC1520702 SEAT TRACK BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FOUND MAIN DECK FLOOR SUPPORT SEAT TRACK OUTBD FLANGE IS CORRODED AT BS 1080 - 1090, RBL 1, WL 208. REMOVED DAMAGED/COR RODED OUT OF LIMIT SEAT TRACK FROM STA 1010 TO STA 1130, BL0 AND INSTALLED NEW SEAT TRACK REF SRM 53-10-2 FIGURE 7A SHEE T 16 PAGE 16 AND SRM 51- 30-02. CLASSIFIED AS MAJOR REPAIR. 2 L 7 3 4F A3WE 2007040200123 20070402 00123 EU 2007 4 2 200703261 1 20070322 A 7732 4120T14P02 ACCELEROMETER EMB ERJ170 ERJ170100SE 3260406 EU GE CF34 CF348E5 30015 NE NR 2 ENGINE DEFECTIVE A UHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 635RW 17000056 GEE193234 FLIGHT 7542 IAD TO YUL - DURING CLIMBOUT AND DURING CRUISE CREW REPORTED AN NR 2 ENG LP SPOOL VIBE 4.1 DURING CLIMB AND WENT TO 4.0 AT CRUISE. PERFORMED QRH PROCEDURE AND RETURNED TO FIELD. OCM REMOVED AND REPLACED FWD ACCELEROMETER. PE RFORMED ENGINE RUNS AT ALL POWER SETTINGS TO INCLUDE TOGA, NO ABNORMAL VIBES DETECTED. DISCREPANCY REPEATED 03/27/2007. FERRIED TO IND. MAINT ACCOMPLISHED BLADE LUBE AND INSTALLED NEW BLADE BUMPERS. 2 L 7 2 4F 4 F RT A56NM E00063EN 2007040200125 20070402 00125 SO 2007 4 2 GUUA03220701 1 20070322 A 3260 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE MLG UNKNOWN A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 29 268AS 120202 FLIGHT: 9154 , DURING FLIGHT LANDING GEAR (A) SYSTEM (3) RED UNSAFE LIGHTS ILLUMINATED AND WENT OUT AFTER SEVERAL SECOND S. INSPECTED ALL LANDING GEAR SYSTEMS NO DEFECTS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 2007040200126 20070402 00126 CE 2007 4 2 4530903272007 1 20070324 A 7500 UNKNOWN LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE7312 01518 WP BLEED SYSTEM UNKNOWN E J7SA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 05 436FX 309 LT BLEED AIR LEAK IN FLIGHT WOULD NOT EXTINGUISH WITH BLEED AIR TURNED OFF. MAINTENANCE ACCESSED BLEED LINES IN AREA OF FAULT DETECT AND PERFORMED GROUND RUNS. NO FAULT FOUND. SWAPPED A76 AND A77 LEAK DETECT BOXES AND PERFORMED OPERATIONAL CHECK FLIGHT. NO DISCREPANCIES REPORTED. AIRCRAFT APPROVED FOR RETURN TO SERVICE. WILL MONITOR THE SITUATION FOR REOCCU RRENCE. 2 L 7 2 4F 4 F RT T00008WI E6WE 2007040200131 20070402 00131 CE 2007 4 2 DXTA200702053 1 20070328 A 3240 LINE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LT BRAKE ASSY CONTAMINATED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 391QS 5600493 UPON LANDING, THE FO'S LT BRAKE WAS SPONGY. IT DID PUMP UP TO HAVING BRAKE HOWEVER IT SEEMS AS THOUGH THERE IS AIR IN TH E BRAKE LINE. C/W BLEED BRAKES. TAXIED A/C OP'S CHECKS GOOD. SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME. ALL WORK DONE I.A.W. I.A.W. CE560 M/M 32-40-00 2 L 7 2 4F 4 F RT A22CE E25EA 2007040200132 20070402 00132 CE 2007 4 2 DXTA200702051 1 20070327 A 2720 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RUDDER UNKNOWN E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 971QS 7500071 WHEN RAISING FLAPS , YELLOW FLAP EICAS MESSAGE (RUDDER LIMIT FAIL - A) ILLUMINATED. FLIGHT CONTROL PAGE INDICATED 89 PE RCENT RUDDER AVAILABLE. REMOVED AND REPLACED UPPER LIMITER ACTUATOR IAW 750 MM 27-30-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007040200137 20070402 00137 2007 4 2 200703291 4 20070328 A 3418 STALL WARNING EMB ERJ170 ERJ170100SE 3260406 EU COCKPIT MALFUNCTIONED A UHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 653RW 17000076 FLIGHT 7763 DEN TO AUS - CREW REPORTS AFTER TAKEOFF AT ABOUT 100 FEET AGL RECEIVED THREE CAUTION MESSAGES: SHAKER ANTIC IPATED, AOA LIMIT FAIL, WIND SHEAR FAIL. RETURNED TO FIELD. CREW ALSO REPORTS VERY STRONG HEADWINDS AND OR WAKE TURBUL ENCE FROM A UNITED A320 THAT TOOK OFF JUST AHEAD OF THEM. MAINTENANCE ACCOMPLISHED DOWNLOAD AND CHECKED FOR FAULT CODES AND REPORTS HEAVY GUSTY WINDS IN AREA. AIRCRAFT POWER WAS RESET AND ALL MESSAGES CLEARED. 2 L 7 2 4F RT A56NM 2007040200139 20070402 00139 NM 2007 4 2 USAA20703006 1 20070326 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 525AU 23860 A 1 INCH CRACK FOUND RT SIDE OF FUSELAGE, STA 767, STR 21R. REPAIRED AS PER BAC SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2007040200140 20070402 00140 NM 2007 4 2 SB07024 1 20070328 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 459UW 25023 BDL - MAINTENANCE REPORTED THE FORWARD LEFT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007040200141 20070402 00141 NM 2007 4 2 USAA200703005 1 20070327 A 5414 SKIN BOEING 737 7374B7 1384702 NM LT PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 A .75 INCH CRACK FOUND AT LEFT PYLON AT ACCESS PANEL 5727L OPENING. STOP DRILLED & INSTALLED DOUBLER PER TYPICAL REPAIR 54-30-07. 2 L 7 2 4F RT A16WE 2007040200142 20070402 00142 NM 2007 4 2 WRLA2007053 1 20070318 A 5320 CHANNEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271WA 48518 DURING C-04 CHECK IN TPE, CRACK .55 INCH FOUND ON UPPER HORIZONTAL DECK OF FORWARD AFT FUSELAGE COMPARTMENT AT EMPENNAGE STA Y=2015, X=-14, Z=+61. INSTALLED REPAIR PER MD-11 SRM VOL.I 53-00-01 REV.38 FIG.10 2 L 7 3 4F 4 F RT A22WE E24NE 2007040200145 20070402 00145 NM 2007 4 2 WRLA2007050 1 20070311 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271WA 48518 DURING C-04 CHECK IN TPE, CENTER GALLEY AREA SEAT TRACK CORRODED AREA Y=840-850, X=27.5. INSTALLED SEAT TRACK & SPLICE PER MD-11 SRM VOL.II 51-33-01 REV.38 2 L 7 3 4F 4 F RT A22WE E24NE 2007040200146 20070402 00146 NM 2007 4 2 WRLA2007052 1 20070318 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271WA 48518 DURING C-04 CHECK IN TPE, CORROSION FOUND CABIN SEAT TRACK STA Y=855-860, X=10, Z=-18. INSTALLED SEAT TRACK AND SPLICE PER MD-11 SRM VOL.II 51-33-01 REV.38. 2 L 7 3 4F 4 F RT A22WE E24NE 2007040200148 20070402 00148 CE 2007 4 2 DXTA200702049 1 20070326 A 3246 WHEEL CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG VIBRATION E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 900QS 7500123 DURING TAKEOFF ROLL AIRCRAFT BEGAN TO SHUDDER AT APPROXIMATELY 40 KIAS AND CONTINUED THROUGHT APPROXIMATLEY 60 KIAS TAKE OFF WAS ABORTED AT THAT TIME, SHUDDER CAME FROM NOSEWHEEL. TROUBLESHOT NOSE GEAR SHIMMY TO NOSE TIRES BEING OUT OF ROUN D PER THE CITATION X NOSE SHIMMY CHECKLIST. REMOVED LEFT AND RIGHT NOSE WHEEL ASSEMBLIES AND INSTALLED OVERHAULED WHEEL ASSEMBLIES WITH NEW TIRES. WORK PERFORMED IAW CHAPTER 32-41-01 OF THE CITATION 750 M.M. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007040200149 20070402 00149 NM 2007 4 2 ZZDA070326144 1 20070326 A 2170 COALESCER BAG BOEING 737 737* NM A/C BAY DIRTY A ZZDA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 15 318AT 33931 ON CLIMBOUT A STRONG BURNING SMELL WAS REPORTED BY THE LEAD FLT ATTENDANT. THE BURNING SMELL WAS REPORTED THRU OUT THE A/C. REPLACED COALESCERS REF AMM 21-51 AND PERFORMED LEFT, RIGHT ENG RUN AT POWER, NO SMELL NOTED. 2 L 7 2 4F RT A16WE 2007040200150 20070402 00150 2007 4 2 DXTA200702050 4 20070326 A 3460 COMPUTER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL FLT GUIDANCE FAILED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 997QS 7500208 ABORTED TAKEOFF ROLL TWICE FOR SAME REASON, FADEC FAULT L AB, FADEC FAULT R AB, FLIGHT GUIDANCE COMPUTER A FAIL. YD OFF LWR, MACH TRIM OFF. CHECKED SYSTEM FOR PROPER OPERATION. C/W TWO SUCESSFUL STARTS AND RAN ENGINES TO HIGH POWER. COUL D NOT DUPLICATE SQUAWK. OPS CHECKED GOOD IAW 750 MM CH 71-00-04. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007040200152 20070402 00152 CE 2007 4 2 DXTA200702044 1 20070322 A 2741 TRIM SYSTEM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL STAB FAILED E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 944QS 7500144 PRIMARY STABILIZER TRIM FAILED IN-FLIGHT. PRIMARY TRIM ALSO DOES NOT WORK ON GROUND. REMOVED AND REPLACED FAILED MOTOR ASSEMBLY. PERFORMED OPS CHECK SATISFACTORY. WORK DONE IAW 750 MM CHAP 27-40-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007040200153 20070402 00153 NM 2007 4 2 AWXA200700423 1 20070328 A 5754 65C26753 SKIN BOEING 737 73733A 1384673 NM LE FLAP CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 PHX - FOUND LEFT WING KRUGER FLAP TO NACELLE AND STRUT DOOR CRACKED, WS 196.8461. REPLACED LEFT WING KRUGER FLAP TO NAC ELLE AND STRUT DOOR, WS 196.8461 IAW B737-300 AMM 27-81-14. 2 L 7 2 4F RT A16WE 2007040200155 20070402 00155 2007 4 2 AWXA200700424 4 20070328 A 2565 D31516317 SLIDE AIRBUS A319 A319132 3930340 NM R1 DOOR FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 801AW 20261 84 889 PHX - EES - R1 DOOR SLIDE EMERGENCY LIGHT TEST FAILED. MX REPLACED THE R1 DOOR SLIDE ASSY. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007040200156 20070402 00156 SO 2007 4 2 GLBA20060927 1 20070327 A 2161 222017011400 CONTROLLER EMB 120 EMB120ER 3260203 SO CABIN AIR TEMP FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 96ZK 120096 AIR RETURN - FLT 5111 - PILOT REPORTED THAT THE CABIN DID NOT PRESSURIZE UNTIL 10,000 FEET. CABIN MASKS DROPPED AT APPRO XIMATELY 8,000 FEET CABIN ALTITUDE. MAINTENANCE REMOVED AND REPLACED THE AUTO TEMP CONTROLLER. OPERATIONAL CHECK ON GROU ND GOOD. REFERENCE EMB-120 MM 21-30. SUBSEQUENT OPERATIONAL CHECK FLIGHT WAS SATISFACTORY. 2 L 7 2 4T RT A31SO 2007040200172 20070402 00172 EA 2007 4 2 A6WA200740148 1 20070314 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 415AW 7593 LT FS 625.00 OBLIQUE ANGLE IS CRACKED 1.5 INCHES LONG IN AFT RADIUS. (K) [SUP 06-05-07] MAINTENANCE REMOVED CRACKED A NGLE AND INSTALLED NEW SERVICEABLE ANGLE P/N 601-35012-51 IAW CRJ SRM 51-42-21 AND BSC EO 601R-53-11218. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007040200173 20070402 00173 EA 2007 4 2 A6WA200740147 1 20070316 A 5320 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 415AW 7593 HYDRAULIC TRANSDUCER HOT CHANNEL PN 601R75262-159 CRACKED APPROX .1 INCH LONG IN CEILING OF LT MLG WHEEL WELL. (K) [SU P 06-05-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R75262-159 IAW CRJ SRM 51- 42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007040200174 20070402 00174 EA 2007 4 2 A6WA200740150 1 20070320 A 5230 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CARGO DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 416AW 7603 CARGO DOOR FWD TRUCK BOTTOM U-CHANNEL CRACKED APPROX .1 INCH LONG. (K) [SUP 05-09-07] MAINTENANCE REMOVED AND REPLACE D CARGO DOOR FORWARD U-CHANNEL IAW CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007040200175 20070402 00175 EA 2007 4 2 A6WA200740141 1 20070318 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 416AW 7603 LT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. (K) [SUP 05-09-07] MAINTENANCE REMOVED AND REPLACED LEFT FS 625 INTERCOSTAL AT STRINGER 14L IAW CRJ200 SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007040200177 20070402 00177 EA 2007 4 2 A6WA200740146 1 20070316 A 2910 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 415AW 7593 HYDRAULIC TRANSDUCER BRACKET PN 601R75262-157 CRACKED APPROX .1 INCH LONG IN CEILING OF RT MLG WHEEL WELL. (K) [SUP 06 -05-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R75262-157 IAW CRJ SRM 51-42-0 6. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007040200180 20070402 00180 NM 2007 4 2 07FDEA01003 1 20070318 A 2782 651781820 ACTUATOR BOEING 727 727233 138408A NM L/E SLAT LEAKING A FDEA O OTHER K FLUID LOSS LD LANDING 1 SO 25 274FE 22039 SHORT FINAL, LOSS OF A SYSTEM, LANDED STRAIGHT AHEAD. TOWED IN. AFTER T/S FOUND NR 2 L/E FLAP ACTUATOR LEAKING. CANCE LED FIRST PART. REMOVED AND REPLACED NR 2 LE FLAP ACT IAW M/M 27-81-022-4. SERVICED HYD SYSTEM PER 12-12-000-2. 2 L 7 3 4F RT A3WE 2007040200184 20070402 00184 NM 2007 4 2 07FDEA01024 1 20070320 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A FDEA K NONE O OTHER UK UNKNOWN 1 SO 25 461FE 22548 FOUND CABIN FLOORBEAM UPPER SURFACE HAS CORROSION, FS 580, RBL 24.75, TO RBL 45.5. REWORKED IAW FEDEX EA 7-5310-102028. 2 L 7 3 4F A3WE 2007040200186 20070402 00186 NM 2007 4 2 07FDEA01026 1 20070320 A 5720 WEB BOEING 727 727225 1384077 NM RT WING CRACKED A FDEA K NONE O OTHER UK UNKNOWN 1 SO 25 461FE 22548 R/M/G WEB CRACKED AT NR 8 SPOILER MOUNT AFT OF GEAR. REMOVED AND REPLACED WEB IAW SRM 51-40-2, AND SRM 51-30-2. REMOVE D AND REPLACED EXTERNAL DOUBLER IAW SRM 51-20-1, FIG 7, AND SRM 51-30-2. 2 L 7 3 4F A3WE 2007040200188 20070402 00188 EU 2007 4 2 07FDEA01029 1 20070321 A 5330 SKIN AIRBUS 310 A310324 3930206 EU FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C UK UNKNOWN 1 SO 25 814FD 534 OLD REPAIR, AN EXTERNAL DOUBLER INSTALLED NEAR APU DOOR BETWEEN C92/93 AND BETWEEN P18/19 RT. THIS DOUBLER IS NOT CONFO RM TO SRM 53-19-12 FIG 202. REPAIR PERFORMED BY INSTALLATION OF A NEW REPAIR DOUBLER IAW SRM 53-19-12/FIG 201. 2 L 7 2 4F RT A35EU 2007040200189 20070402 00189 EU 2007 4 2 07FDEA01030 1 20070321 A 5311 FRAME AIRBUS 310 A310324 3930206 EU FUSELAGE CORRODED A FDEA K NONE O OTHER UK UNKNOWN 1 SO 25 814FD 534 FOUND CORROSION BLEND OUT ON C80/82, P5 LT AND C87, P6 RT. THESE TWO SPOTS WERE OUT OF SRM LIMITS. REPAIR PERFORMED IA W EA 6-5319-101245 AND IS APPROVED BY RAS/DAHAM/4020774/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040200190 20070402 00190 EU 2007 4 2 07FDEA01031 1 20070321 A 5320 SPLICE AIRBUS 310 A310324 3930206 EU FUSELAGE DENTED A FDEA K NONE O OTHER UK UNKNOWN 1 SO 25 814FD 534 FOUND OLD REPAIR OF AN EXTERNAL DOUBLER BETWEEN C91/92, ABOVE SKIN LAP BETWEEN P35 AND P41 LT. REPAIR VERIFICATION, PER FORMED IAW SIA-NRC: RAS/DAHAM/1020/99 ISSUE "A", EA FOR TRACKING: 6-5319-101259. 2 L 7 2 4F RT A35EU 2007040200191 20070402 00191 EU 2007 4 2 07FDEA01032 1 20070321 A 5320 STRUCTURE AIRBUS 310 A310324 3930206 EU FUSELAGE CORRODED A FDEA K NONE O OTHER UK UNKNOWN 1 SO 25 814FD 534 OLD REPAIR BY A DOUBLER AND ANGLE DOUBLERS, INSTALLED ON FWD NLG WHEEL WELL, INSIDE E/E COMPARTMENT RT. REPAIR VERIFICA TION, PERFORMED IAW RAS/AS/332/96 AND SIA-EN NO 10EN-53-6591. EA FOR TRACKING: 6-5312-101298. 2 L 7 2 4F RT A35EU 2007040200192 20070402 00192 EU 2007 4 2 07FDEA01033 1 20070321 A 5313 STRINGER AIRBUS 310 A310324 3930206 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER UK UNKNOWN 1 SO 25 814FD 534 OLD REPAIRS ON FLOOR STRUCTURE, REPAIR ANGLES ON SEVERAL STRINGERS. SPECIAL PROFILE BETWEEN C11/12, BETWEEN C/L (Y232), SPLICE REPAIR BETWEEN C14/15 (Y-953) AND SPLICE REPAIR BETWEEN C14/15 (Y-1959). REPAIR VERIFICATION, PERFORMED IAW SRM 53-12-15/FIG 207. 2 L 7 2 4F RT A35EU 2007040200193 20070402 00193 EU 2007 4 2 07FDEA01034 1 20070321 A 5320 ANGLE AIRBUS 310 A310324 3930206 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER UK UNKNOWN 1 SO 25 814FD 534 OLD REPAIRS WITH NO RECORDS AND NO SRM REFERENCE ON FLOOR STRUCTURE. Z-PROFILE REPAIR BETWEEN C11/12A (Y450/730) AND A FURTHER Z-PROFILE REPAIR BETWEEN C11/12A (1020/1200). REPAIR VERIFICATION, PERFORMED IAW RAS 045088/009/2006 ISSUE "A" AND EA 6-5312-101258. 2 L 7 2 4F RT A35EU 2007040200194 20070402 00194 EU 2007 4 2 07FDEA01035 1 20070321 A 5313 A59386217 STRINGER AIRBUS 310 A310324 3930206 EU FUSELAGE CORRODED A FDEA K NONE O OTHER UK UNKNOWN 1 SO 25 814FD 534 CORROSION BLEND OUT REPAIR CAUSES OUT OF LIMIT PER SRM 53-10-00 ON STRINGERS P52 LT, BETWEEN C54.1- C55/58; P45 LT, BET WEEN C54.1-54.2 AND P52 RT BETWEEN C61/62-C62/63. STRINGER REPAIR PERFORMED BY SRM 53-10-14 AND MILL TO STRINGER IAW SR M 53-10-14 "B-B". 2 L 7 2 4F RT A35EU 2007040200196 20070402 00196 EU 2007 4 2 07FDEA01037 1 20070321 A 5730 SKIN AIRBUS 310 A310324 3930206 EU RT WING CORRODED A FDEA K NONE O OTHER UK UNKNOWN 1 SO 25 814FD 534 FOUND CORROSION ON TOP SKIN RT WING. AFFECTED AREAS MENTIONED IN EA 6-5720-99229. REPAIR PERFORMED BY BLEND OUT AND OV ERSIZING IAW EA 6-5720-99229 AND RAS/BAE/1002732/2006. 2 L 7 2 4F RT A35EU 2007040200197 20070402 00197 NM 2007 4 2 07FDEA00913 1 20070315 A 5330 65545839 SKIN BOEING 727 727225 1384077 NM FUSELAGE MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FOUND EXTERNAL FUSELAGE REPAIR AT APPROX STA 1110-1130, AT S-20L DID NOT CONFORM TO SRM 53-30-3 FIG 5. REMOVED EXISTING REPAIR, EXTENDED FILLER AT LAP AND INSTALLED DOUBLER REF SRM 53-30-3 FIG 5. 2 L 7 3 4F A3WE 2007040200198 20070402 00198 NM 2007 4 2 DU4R2007077 1 20070321 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM FUSELAGE CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 6708D 30480 FOUND CORROSION ON FLOORBEAM UPPER CAP AT FS 1640 LBL 24. FABRICATED AND INSTALLED 63.0 LONG T CAP FROM 7075-T6 .090, 2 SUPPORT ANGLES 11.0 FROM 7075-T6 .063, 2 6.0 RADIUS FILLERS FROM 7075-T6 .125, 2 REINFORCEMENT STRAPS 8.0 FROM 7075-T 6 .090 6 IAW DELTA B757 SRM 53-60-51-2-805D FIG 205, 51-20-01. 2 L 7 2 4F RT A2NM 2007040200199 20070402 00199 NM 2007 4 2 DU4R2007076 1 20070323 A 5210 140N27514 ROD BOEING 757 757232 1384965 NM R1 DOOR CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND CORROSION ON R-1 DOOR LOWER GATE GIRT BAR CRANK PUSH ROD. REPAIRED BY REMOVING CORRODED ROD, ADJUSTED AND INSTALL ED NEW ROD P/N 140N2751-4 ON GIRT BAR MECHANISM IAW CMM 52-11-05. 2 L 7 2 4F RT A2NM 2007040200202 20070402 00202 NM 2007 4 2 DLM90070267 1 20070324 A 5230 SKIN DOUG MD90 MD9030 3023690 NM MID CARGO DOOR GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 FOUND MID CARGO DOOR SKIN AFT LWR CORNER GOUGED. REMOVED AND REPLACED DOUBLER PER SRM 51-30-02 AT HMV2 REF N/R 8000-003 5. 2 L 7 2 4F RT A6WE 2007040200203 20070402 00203 2007 4 2 DL76G070269 4 20070326 A 2565 H2052K3833 DOOR LATCH BOEING 767 767332 1382001 NM RT OVERWING DOOR MISINSTALLED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 1609 30574 RT OFF WING SLIDE COMPARTMENT DOOR LATCH 3RD FROM THE FRONT, FOUND INCORRECTLY INSTALLED. FOUND LATCH INSTALLED UPSIDE DOWN. REORIENTED LATCH. 2 L 7 2 4F RT A1NM 2007040200205 20070402 00205 NM 2007 4 2 DL76S070272 1 20070325 A 5330 146T32621 SKIN BOEING 767 767332 1382001 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 128DL 24078 FUSELAGE SKIN CRACKED AT STA 1197+99 AND BL0. CUT OUT CRACK AND INSTALLED REPAIR DOUBLER AND TRIPLER. 2 L 7 2 4F RT A1NM 2007040200206 20070402 00206 NM 2007 4 2 DL76P070275 1 20070329 A 5315 141T5111 FLOORBEAM BOEING 767 767332 1382001 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 140LL 25988 DURING HMV, FOUND STA 287 FLOORBEAM CORRODED 18 INCHES FROM BL 0 RT. CAUSE OF CORROSION WAS ENVIRONMENTAL. DAMAGE WAS REPAIRED PER SRM 53-00-51D. CORROSION WAS FOUND DURING HMV ROUTINE INSPECTION. 2 L 7 2 4F RT A1NM 2007040200208 20070402 00208 EA 2007 4 2 A6WA200740118 1 20070312 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE WING MALFUNCTIONED A A6WA K NONE F FLT CONT AFFECTED CL CLIMB 1 GL 31 465AW 7893 AFTER TAKEOFF WHILE RETRACTING FLAPS FROM 20 DEGREES. COMPLIED WITH QRH, FLAPS FAIL CAUTION MESSAGE ON ED1. COMPLIED W ITH SUPPLEMENT 98-018A, NO FLAP TWISTING, SKEWING OR DEFORMATION NOTED. RESET CIRCUIT BREAKER ONCE, MESSAGE CLEARED, FL APS OPERATE NORMALLY. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007040200210 20070402 00210 EA 2007 4 2 A6WA200740144 1 20070319 A 5320 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 416AW 7603 HYDRAULIC TRANSDUCER HOT CHANNEL (ASSY PN 601R75262-159) CRACKED APPROX .1 INCH LONG IN CEILING LT WHEEL WELL. (K) [SU P 05-09-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R75262-159 IAW BSC STANDAR D REPAIR 601R-53-0044E. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007040200211 20070402 00211 EA 2007 4 2 A6WA200740106 1 20070307 A 5270 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR MALFUNCTIONED A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 404AW 7294 CLIMBING THRU 14,000 FT GOT PAX DOOR LATCH CAUTION MESSAGE, FOLLOWED BY PAX DOOR (RED) WARNING MESSAGE, COMPLIED WITH QR H NO PRESSURIZATION PROBLEM NOTED. NO ABNORMAL NOISE OR ALIGNMENT INDICATION NOTED. DIVERTED, RED WARNING MESSAGE CLEA RED BELOW 16,000 FT, AND PAX DOOR LATCH MESSAGE RETURNED ALL MESSAGES OUT BELOW 3,000 FT. LANDING WEIGHT 45,400 LBS. S EE CROSS REFERENCE SDR A6WA200740095. (REMOVED AND REPLACED PS5MB AND PS6MB, OPS CHECK GOOD). (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007040200212 20070402 00212 EA 2007 4 2 A6WA200740117 1 20070309 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE T/E FLAP MALFUNCTIONED A A6WA K NONE J WARNING INDICATION CR CRUISE 1 GL 31 464AW 7890 FLAPS FAIL CAUTION WHILE IN FLIGHT, FAILED AT 30. COMPLIED WITH AWAC SUPPLEMENT 98-018A, NO FLAP TWISTING, SKEWING OR D EFORMATION NOTED. RESENT CIRCUIT BREAKERS ONCE, MESSAGE CLEARED. FLAPS OPERATE NORMALLY. PLACED ON 72 HOUR WATCH. (K ) 2 L 7 2 4F 4 F RT A21EA E15NE 2007040200213 20070402 00213 CE 2007 4 2 A6Y2007F00000 1 20070304 A 2121 COOLING FAN BEECH 58 58 1152740 CE CONT O520 IO520CB 17032 SO RADIO MALFUNCTIONED E A6YA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 09 8257H TH1650 APPROXIMATELY 20 MINUTES INTO THE FLIGHT PILOT SUSPECTED AN ELECTRICAL BURNING SMELL. HE NOTICED SOME SMOKE COMING FROM UNDER INSTRUMENT PANEL. AT THAT TIME HE COMPLETED THE MEMORY ITEMS FOR (ELECTRICAL SMOKE OR FIRE). AFTER 1 TO 2 MINUT ES SMOKE AND SMELL DISSIPATED. AFTER REGAINING RADIO COMMUNICATIONS WITH MINNEAPOLIS CENTER PILOT DECLARED AN EMERGENCY AND ASKED FOR VECTORS TO NEAREST AIRPORT. PILOT ACCEPTED VECTORS. FLIGHT LANDED UNEVENTFULLY. NO EMERGENCY EVAC, RAD IO COOLING FAN FOUND RUBBING BETWEEN FAN AND HOUSING, REPOSITIONED FAN. INSPECTED SIMILAR COOLING FANS ACROSS FLEET. ( K) 1 L 7 2 3O 3 O 3A16 E5CE 2007040200217 20070402 00217 NM 2007 4 2 AMTA200700150 1 20070322 A 4970 WARNING SYSTEM BOEING 757 75733N 1384931 NM GE CF34 CF343B1 NE APU MALFUNCTIONED A AMTA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 552TZ 32586 AFTER BLOCK OUT APU GEN OFF LIGHT ILLUMINATED, RESENT TURNED OFF GEN LIGHT AND APU DOOR EICAS MSG APPEARED. RESET CB AP U BATT BUS. PERFORMED APU BITE IAW FIM 49-11-00, FIG 103, NO FAULTS. RAN APU NO DEFECTS FOUND. APU DOOR CLOSES ON SHU TDOWN. (K) 2 L 7 2 4F 4 F RT A2NM E15NE 2007040200218 20070402 00218 NM 2007 4 2 AMTA200700113 1 20070226 A 4970 WARNING SYSTEM BOEING 737 73783N 13844HI NM APU MALFUNCTIONED A AMTA K NONE N FALSE WARNING CR CRUISE 1 GL 11 304TZ 30675 APU FAULT LIGHT CAME ON WHEN APU SHUTDOWN NORMALLY 1 HOUR BEFORE LANDING. FAULT LIGHT WENT OUT AFTER 5 MINUTES. PERFOR MED APU RUN-OPS CHECK NORMAL, NO FAULTS. EXISTING FAULT 49-31001 CLEARED ITSELF UPON BITE TEST AFTER OPS CHECK. (K) 2 L 7 2 4F RT A16WE 2007040200219 20070402 00219 NM 2007 4 2 AMTA200700136 1 20070301 A 3040 CIRCUIT BREAKER BOEING 737 73783N 13844HI NM COCKPIT TRIPPED A AMTA K NONE J WARNING INDICATION CR CRUISE 1 GL 11 318TZ 28247 INFLIGHT, FOUND WINDOW HEAT CB POPED FOR L2-L3-L4. ON P6-11 PANEL. PERFORMED BITE CK IAW FIM 30-40-00-810-801. RESET CIRCUIT BREAKER, OPS CK NORMAL. (K) 2 L 7 2 4F RT A16WE 2007040200221 20070402 00221 NE 2007 4 2 AXS2007F00000 2 20070220 A 7261 3022454 CARBON SEAL CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE ACCESS GEARBOX DAMAGED E AXSA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 65 731FX 5229 208B0480 19366 AIRCRAFT DEPARTED AS FLIGHT 81391 REPOSITIONING EMPTY UNDER FAR 91. 15 MINUTES INTO FLIGHT THE PIC NOTED OIL PRESSURE F LUCTUATIONS FOLLOWED BY DECREASING OIL PRESSURE. THE PIC DIVERTED AND ENROUTE NOTED TORQUE FLUCTUATIONS OF APPROXIMATEL Y 500 FT/LBS. THE PIC LANDED AND OTED OIL INSIDE EXHAUST PIPE AND ON RT SIDE OF AIRCRAFT. PRELIMINARY MAINTENANCE INSP ECTION REVEALED THAT DAMAGE OR DETERIORATION TO THE CARBON SEAL IS LIKELY THE CAUSE OF THE OIL LEAK AND SUBSEQUENT OIL P RESSURE FLUCTUATIONS. (K) 1 H 7 1 3T 3 T A37CE E4EA 2007040200223 20070402 00223 NM 2007 4 2 DHL2007786512 1 20070316 A 5347 BAC1520792 SEAT TRACK BOEING 727 727214 138407R NM FUSELAGE GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 CUTOUT AREA OF SEAT TRACK GOUGED AND WORN AT LT BS 994, LBL 25. REMOVED FLOOR BOARDS AND SEAT TRACK AT STA 950 TO 1130 IAW B727 SRM 51-30-2. FABRICATED AND TRIMMED AS REQUIRED NEW SEAT TRACK SECTION, P/N BAC 1520-792 IAW B727 SRM 53-10-5, FIG 1. TREATED, PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED SEAT TRACK IAW B727 SRM 53-10-5, FIG 1. 2 L 7 3 4F A3WE 2007040200228 20070402 00228 EU 2007 4 2 07FDEA01039 1 20070321 A 2910 FITTING AIRBUS 310 A310324 3930206 EU RT WING DAMAGED A FDEA K NONE O OTHER UK UNKNOWN 1 SO 25 814FD 534 ELONGATED HYDRAULIC FITTING HOLES IN THE LOWER SKIN PANELS OF RT WING. REPAIR BY OVERSIZING AND BUSHING HOLES AS PER R5 72-49184 ISSUE "C" IAW EA 6-5720-99228, APPROVED BY RAS/BAE/1002610/2006. 2 L 7 2 4F RT A35EU 2007040200229 20070402 00229 EU 2007 4 2 07FDEA01040 1 20070321 A 5730 SKIN AIRBUS 310 A310324 3930206 EU LT WING CORRODED A FDEA O OTHER O OTHER UK UNKNOWN 1 SO 25 814FD 534 EXTENSIVE CORROSION ON LT WING TOP SKIN. AFFECTED AREAS SHOWN ON PAGES 4 THROUGH 6 IN MENTIONED EA. REPAIR PERFORMED B Y BLEND OUT AND OVERSIZING IAW EA 6-5720-101319, APPROVED BY RAS/BAE/1003173/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040200230 20070402 00230 EU 2007 4 2 07FDEA01041 1 20070321 A 5730 SKIN AIRBUS 310 A310324 3930206 EU LT WING CORRODED A FDEA O OTHER O OTHER UK UNKNOWN 1 SO 25 814FD 534 EXTENSIVE CORROSION ON THE LT WING BOTTOM SKIN FRONT SPAR OVERHANGS. LOOK FOR AFFECTED AREAS IN MENTIONED EA. REPAIR P ERFORMED BY BLEND OUT AND/OR CUT OUT AND INSTALLING REPAIR PLATES ALL IAW EA 6-5720-99230, APPROVED BY RAS/BAE/1002584/2 006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040200232 20070402 00232 2007 4 2 07FDEA01044 4 20070320 A 2565 7A1298005 SLIDE AIRBUS 310 A310203 3930313 EU L1 DOOR MALFUNCTIONED A FDEA A UNSCHED LANDING L NO TEST TX TAXI/GRND HDL 1 SO 25 442FE 2277 353 L1 SLIDE DID NOT DEPLOY. SAFETY HAS SLIDE. REMOVED SLIDE ASSY MPN 7A1298-005, S/N WA0377, TURNED SLIDE OVER TO FLT SA FETY. 2 L 7 2 4F RT A35EU 2007040200233 20070402 00233 EU 2007 4 2 07FDEA01045 1 20070321 A 5753 RIB AIRBUS 310 A310324 3930206 EU TE FLAP DAMAGED A FDEA O OTHER O OTHER UK UNKNOWN 1 SO 25 814FD 534 OLD REPAIR AT RIB 21 INNER FLAP LT. REPLACEMENT OF END RIB 21 IAW SB A310-57-2055, APPROVED BY EA 6-5752-103333. 2 L 7 2 4F RT A35EU 2007040200234 20070402 00234 EU 2007 4 2 07FDEA01047 1 20070321 A 5540 HINGE FITTING AIRBUS 300 A300B4622R 3930312 EU RUDDER CORRODED A FDEA O OTHER O OTHER UK UNKNOWN 1 SO 25 748FD 633 FOUND CORROSION ON RUDDER HINGE FITTINGS NR 5, NR 6 AND NR7 (A554-71605-200, A554-71606-200, A554-71617-000) CORROSION R EWORK AND HFEC INSPECTION IAW EA 6-5546-106387, APPROVED BY RAS/DAHAM/4021625/2006 ISSUE "B". 2 L 7 2 4F RT A35EU 2007040300006 20070403 00006 NM 2007 4 3 DHL2007786522 1 20070315 A 5753 STRUCTURE BOEING 727 727214 138407R NM TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 A/C IN "C" CHECK AT FLIGHTSTAR A/C SERVICES, REF. ASTAR NR 080502. LT WING IB MID FLAP LOWER TE CHORD WBL100-134 HAS 5 CRACKS ON 3 CUTOUTS. REMOVED LT IB MID FLAP LOWER ACCESS PANEL FOR ACCESS IAW B727 SRM 51-30-2. FABRICATED REPAIR, MAT ERIAL USED ANGLE EXTRUSION PO NR 7157132 PN BAC1503-100046 7075T6 DIM 78" BY 2 1/4" AND 2 SPLICES MATERIAL USED EXTRUSIO N PO NR 7157132 PN BAC1503-100046 7075T6 DIM 8 3/4"BY 2 1/4" AND 7 3/4" BY 2 1/4" IAW B727 SRM 51-40-3 FIG 1 AND 57-50-2 FIG 5. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED ANGLE EXTRUSION AT LT IB MID FLAP IAW B727 SRM 51-30- 2. CLOSED ACCESS PANEL LT IB MID FLAP IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007040300008 20070403 00008 EA 2007 4 3 SIMA200708602 1 20070326 A 2910 HYDRAULIC SYSTEM CNDAIR CL600 CL6002C10 1390015 EA NR 2 LEAKING A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 519AE 10131 RECEIVED HYDRAULIC 2 LOW PRESSURE MESSAGE ON CLIMB, HYDRAULIC QUANTITY WENT TO ZERO FOLLOWED BY HYDRAULIC 2 SYSTEM FAILU RE. AIRCRAFT DIVERTED TO CMH. 2 L 7 2 4F RT A21EA 2007040300014 20070403 00014 EU 2007 4 3 07FDEA01052 1 20070321 A 5415 MOUNT AIRBUS 310 A310304 3930339 EU ZONE 400 CHAFED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 OLD CHAFING MARK ON PYLON NR 1 FWD PYLON TO ENGINE MOUNT FITTING. REPAIR PERFORMED BY INSTALLATION OF AN PROTECTION ANG LE, APPROVED BY RAS 018876/027/2002 ISSUE "A" AND EA 6-5450-106441. 2 L 7 2 4F RT A35EU 2007040300016 20070403 00016 NM 2007 4 3 07FDEA01059 1 20070321 A 5510 69701913 ATTACH FITTING BOEING 727 727225 1384077 NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 NR 2 ENGINE INLET DOGHOUSE AT BASE OF VERTICAL LEADING EDGE VERTICAL WEB ATTACH CLIP CRACKED RT SIDE INTERIOR AT STA 127 4. REMOVED AND REPLACED VERTICAL WEB ATTACH CLIP AT STA 1274 INSIDE VERTICAL STABILIZER ABOVE S DUCT ON RT SIDE, REF B7 27 SRM 51-30-2 PAGE 2. 2 L 7 3 4F A3WE 2007040300017 20070403 00017 EU 2007 4 3 07FDEA01060 1 20070321 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 669FE 774 MAIN CABIN SEAT TRACK CORROSION SEVERAL AREAS BETWEEN FRAME 38.2 AND 40, LBL 57. BLENDED AREAS OF CORROSION IAW A300-60 0 SRM 51-22-00. FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-16. RECEIVED NEW SEAT TRACK, PO NR 566271.1. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-40-21, PAR 5, 6 AND 7. 2 L 7 2 4F RT A35EU 2007040300019 20070403 00019 CE 2007 4 3 DXTA200702065 1 20070401 A 3240 UNKNOWN CESSNA 560 560XL 2076702 CE PWA JT15 JT15D5 52112 NE BRAKES CHATTERING E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TX TAXI/GRND HDL 1 GL 07 686QS 5605661 UPON RELEASING BRAKES FOR TAKEOFF AT SJC, (4) LOUD KNOCKS IN RAPID SUCCESSION WERE HEARD FROM REAR OF AIRCRAFT. ABORTED TAKEOFF AND RETURNEDTO RAMP. INSPECTED BRAKES & ENGINES & FOUND NO DEFECTS. TAXI CHECK & PERFORMED ENGINE RUN UP TO TAK E OFF POWER SEVERAL TIMES WICH NO DEFECTS NOTED. COULD NOT DUPLICATE DISCREPANCY. WORK DONE IAW CE-560XL MM CH 32-42-00 & 71-00-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007040300020 20070403 00020 CE 2007 4 3 DXTA200702058 1 20070331 A 2710 CONTROL CABLE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE AILERONS OUT OF ADJUST E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 604QS 5605204 AIRCRAFT WILL NOT FLY LEVEL IN FLIGHT AFTER AILERON RIGGING WITH CONTROLS CENTERED. ADJUSTED AILERON WING AND FAIRING C ABLE TENSION AND RIG IAW 560XL MM 27-10-00. OPS CHECK OK. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007040300021 20070403 00021 CE 2007 4 3 DXTA200702062 1 20070331 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 390QS 5600490 BRAKES ON SIC SIDE NEED TO BE PUMPED TO BE EFFECTIVE AFTER LANDING. BLED BRAKE SYSTEM ON SIC SIDE IAW CH 32-42-00 OF CE 560 M.M. 2 L 7 2 4F 4 F RT A22CE E25EA 2007040300022 20070403 00022 CE 2007 4 3 DXTA200702056 1 20070331 A 2760 UNKNOWN CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE SPEED BRAKE UNKNOWN E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 603QS 5605203 (NO TAKEOFF) LIGHT ILLUMINATED ON TAKEOFF ROLL-ABORTED-CYCLED STAB, FLAPS AND SPEED BRAKE MANY TIMES, NO CHANGE. PULLED SPEED BRAKE BREAKER AND LIGHT WENT OUT. TROUBLE SHOT SPEED BRAKE SYSTEM. FOUND EXCESSIVE MOISTURE LET SPEED BRAKE DOWN SWITCH CONNECTOR. CLEANED AND DRIED CONNECTOR & REINSTALLED CONNECTOR. TEST RUN LET ENGINE NO TAKE OFF LIGHT EXPIRED & SPEED BRAKE OPS CHECKS GOOD A-W-II 20-10-00 560XL WIRING MANUAL. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007040300024 20070403 00024 CE 2007 4 3 DXTA200702060 1 20070331 A 3240 BRAKE ASSY CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LT & RT MALFUNCTIONED E DXTA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 GL 07 930QS 7500130 BRAKES LT AND RT ARE SPONGY WILL NOT HOLD A/C ON MAX POWER STATIC TAKEOFF. INSPECTED LEFT AND RIGHT BRAKE SYSTEM AND F OUND NO DEFECTS. BLEED LEFT AND RIGHT BRAKE SYSTEMS, BLEED AIR FROM NR 1 AND 4 BRAKES, NR 2 AND 3 BRAKES HAD NO AIR. ALL WORK ACCOMPLISHED IAW CESSNA 750 MM 32-42-00. NO DEFECTS NOTED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007040300025 20070403 00025 CE 2007 4 3 DXTA200702059 1 20070331 A 2820 TRANSFER VALVE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP FUEL SYSTEM MALFUNCTIONED E DXTA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 07 862QS 258362 P107620 DURING FUEL TRANSFER AT CRUISE FL340 MOMENTARY LOSS OF THRUST WHEN RT FUEL BOOST PUMP SELECTED OFF. MONETARY INCREASE IN THRUST AND APPROXIMATELY 150 PPH FUEL FLOW WHEN RT PUMP SELECTED ON. INSTALLED OH FUEL TRANSFER VALVE WITH NEW O RINGS P/N HTE 7300N16-128 PER. 800XP MM. 28-20-61. OPS. CHECK GOOD. 2 L 7 2 4F 4 F RT A3EU E6WE 2007040300026 20070403 00026 CE 2007 4 3 DXTA200702063 1 20070401 A 3230 VALVE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 311QS 5600311 AFTER TAKEOFF, NOTICED GEAR UNLOCK LIGHT WITH HYDRAULIC PRESSURE ON ANNUNCIATOR. RAN CHECK LIST. WHEN GEAR CONTROL CIR CUIT BREAKER PULLED LT MAIN FELL WITH GREEN LIGHT. MATCHED CONDITION WITH GEAR HANDLE AND RT MAIN AND NOSE WHEEL FELL W ITH GREEN LIGHTS. USED EMER GEAR BOTTLE AND LANDED. REPLACED HYDRO RELIEF VALVE PER 560 MM, CH 29-11-06. LEAK AND OPS CHECKS GOOD 2 L 7 2 4F 4 F RT A22CE E25EA 2007040300027 20070403 00027 NM 2007 4 3 DXTA200702061 1 20070331 A 3233 ACTUATOR GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE MLG INTERMITTENT E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 706QS 131 SELECTED GEAR DOWN, THE RT MLG DID NOT SHOW DOWN & LOCKED WITH A RED INDICATION PRESENT. ON FINAL, CYCLED MLG 1 MORE TIM E & INDICATION THE SAME. FLY BY TOWER & TOLD THAT THE MLG LOOKED TO BE NORMAL. ON DOWNWIND LEG AT 1500 FT AGL RED LIGHT WENT OUT & GREEN LIGHT OF SAFE GEAR CAME ON. LANDED. REMOVED RT MLG ACTUATOR PN 27300-000-04, SN IL-069 AND INSTALLED R EPAIRED UNIT PN 27300-000-04, SN IL-141. BLED ACTUATOR & PERFORMED GEAR SWINGS, NO DEFECTS NOTED WITH LANDING OPERATION . CLOSED ALL ACCESS AND VERIFIED FALL CONNECTORS DISTURBED DURING TROUBLESHOOTING TO BE SECURE. ALL WORK ACCOMPLISHED I AW G200 AMM. 2 L 7 2 4F 4 F RT A53NM E35NE 2007033000244 20070330 00244 EU 2007 3 30 07FDEA00951 1 20070316 A 5310 A53974259202 BEAM AIRBUS 310 A310304 3930339 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 TWO LONGITUDINAL BEAMS BETWEEN C64-65, -Y 525 AND Y 805 WITH WRONG EXISTING HOLES. PARTS REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007033000249 20070330 00249 EU 2007 3 30 MALA070041 1 20070318 A 3020 HEATER SAAB SF340 340B 7860101 EU RT ENG INTAKE SEPARATED A MALA O OTHER C B J F.O.D. SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 GL 15 457XJ 340B457 ON FINAL INTO TVF ABOUT 8-10 MINUTES OUT, COCKPIT FILLED WITH A STRONG SMOKE ODOR. FA LATER REPORTED FAINT ODOR IN CABI N AND NO VISIBLE SMOKE. NOTED SHORT FINAL SHUT OFF BOTH BLEED VALVES. FOUND APPROX 2 1/2'' BY 2 1/2'' PIECE OF INTAKE HEATING MAT TO HAVE BROKEN OFF. INDICATIONS SUGGEST SOME PARTICLES MAY HAVE ENTERED THE RIGHT ENGINE. REPLACED RIGHT E NGINE LOWER FORWARD DUCT ASSY PN NH24668-081-08 SN OFF L155395 PN ON NH24668-169 SN ON L290559 IAW SAAB AMM 71-60-05. R EPLACED RIGHT ENGINE DEICE CONTROL MODULE PN 44730 SN OFF L248376 SN ON A00031 IAW SAAB AMM 30-20-15 PERFORMED GROUND RU NS, NO DEFECTS NOTED. PERFORMED BOROSCOPE INSPECTION OF COMPRESSOR IAW GE MM 72-00-00, NO DEFECTS. 2 L 7 2 4T RT A52EU 2007033000260 20070330 00260 NM 2007 3 30 HALA0700143 1 20070327 A 3246 165T010039 WHEEL BOEING 767 767300 1385204 NM NR 3 DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 590HA 4471 4471 33467 NR 3 MLG TIRE/WHEEL ASSY SHOWS EVIDENCE OF HIGH HEAT, FUSE PLUG NOT BLOWN. REMOVED AND REPLACED NR 3 MLG TIRE/WHEEL ASS Y IAW 32-45-61. 2 L 7 2 4F RT A1NM 2007033000262 20070330 00262 NM 2007 3 30 HALA0700141 1 20070327 A 4997 CONNECTOR BOEING 767 76733A 1385209 NM FLOW SENSOR LOOSE A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 593HA 33424 ETOPS SIGNIFICANT SYSTEM, PER FLIGHT CREW APU AIR INOP. BITE CHECKED APU ECU. FOUND FAULT DELTA P SENSOR AND MINI FLAG 15 PER FIM 49-11-00 CHECKED FROM FLOW SENSING MOD. FOUND CONNECTOR LOOSE, CLEANED CONNECTIONS AND RESECURED. RAN APU SEVERAL TIMES AND CYCLED APU BLEED AIR SWITCH SEVERAL TIMES, OPERATION CHECK GOOD, NO DEFECTS NOTED. 2 L 7 2 4F RT A1NM 2007033000266 20070330 00266 NM 2007 3 30 UIEA200700113 1 20070302 A 5315 FLOORBEAM BOEING 747 7472D7B 1384803 NM BS 340 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 21784 BS 340 U/D FLOORBEAM UPPER CHORD FWD AND AFT FLANGE FROM RBL 13-44 FOUND 4 HOLES CRACKED. REPAIRED AS PER SB 747-53A243 1 PART 3 FIGURE 9. 2 L 7 4 4F RT A20WE 2007033000279 20070330 00279 EA 2007 3 30 COMA0760289 1 20070326 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA MLG OUT OF ADJUST A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 712CA 7244 FLIGHT 5598 - RECEIVED GEAR DISAGREE WARNING AFTER TAKEOFF. RETURNED TO SAV AND LANDED WITHOUT INCIDENT. FOUND MLG UPL OCK PROXIMITY SENSOR OUT OF ADJUSTMENT AND TARGET LOOSE. ADJUSTED SENSOR AND SECURED TARGET. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007033000280 20070330 00280 EA 2007 3 30 COMA0760279 1 20070323 A 3230 46193 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG WW FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 932CA 9612 7038 FLIGHT 5615 - RECEIVED GEAR DISAGREE MESSAGE, MAINS STUCK IN UP POSITION. ABORTED APPROACH, DECLARED EMERGENCY, MANUALL Y DEPLOYED GEAR. LANDED WITHOUT INCIDENT. REPLACED MLG PRIORITY VALVE. ALSO FOUND MLG SELECTOR VALVE CAP LOOSE AND SE CURED. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007033000283 20070330 00283 EA 2007 3 30 COMA0760273 1 20070319 A 3222 STRUT CNDAIR CL600 CL6002B19 1900309 EA NLG LOW A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 804CA 7352 FLIGHT 5078 - AFTER RETRACTION, NLG INDICATION STAYED YELLOW THEN RECEIVED GEAR DISAGREE WARNING. FOLLOWED QRH AND PERF ORMED NORMAL LANDING. FOUND NLG REQUIRED SERVICING. SERVICED NLG, NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007033000285 20070330 00285 EA 2007 3 30 COMA0760285 1 20070324 A 2613 355523255 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA OVERHEAT SYS MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 436CA 7482 FLIGHT 9965 - RECEIVED RIGHT FUSELAGE ANTI-ICE DUCT MESSAGE. ABORTED TAKEOFF AT 90 KTS, RETURNED TO GATE WITHOUT INCIDE NT. PERFORMED MEGAOHN CHECK OF ALL LOOPS IN RIGHT FUSELAGE CIRCUIT. NO DISCREPANCIES. REPLACED LOOP A40WK FOR TROUBLE SHOOTING. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007033000290 20070330 00290 EA 2007 3 30 COMA0760276 1 20070322 A 4920 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY FIRE A COMA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 SO 01 987CA 7199 FLIGHT 5190 - APU AUTO SHUTDOWN AT GATE, SMOKE AND FLAMES REPORTED AT GATE, EMERGENCY DECLARED, FIRE SELF-EXTINGUISHED, SUSPECT RESIDUAL FUEL. DEFERRED PER MEL 49-10-01-1. 2 L 7 2 4F RT A21EA 2007033000296 20070330 00296 NM 2007 3 30 KCSA071090 1 20070328 A 5315 FLOORBEAM BOEING 747 747236B 1384804 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 AFT PIT FLOORBEAM UPPER CAP DENTED AT BS 1720, RBL 46. 2 L 7 4 4F 4 F A20WE E3NE 2007033000298 20070330 00298 NM 2007 3 30 KCSA071092 1 20070328 A 5312 BULKHEAD BOEING 747 747236B 1384804 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 AFT PRESSURE BULKHEAD HAS (2) SMALL DENTS LBL 45, WL 210, STA 2400. 2 L 7 4 4F 4 F A20WE E3NE 2007033000300 20070330 00300 NM 2007 3 30 KCSA071094 1 20070228 A 5312 BULKHEAD BOEING 747 747236B 1384804 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 AFT PRESSURE BULKHEAD HAS SEVERAL SMALL DENTS RBL 30, WL 200, STA 2390. 2 L 7 4 4F 4 F A20WE E3NE 2007033000308 20070330 00308 NM 2007 3 30 KCSA071087 1 20070327 A 5347 SEAT TRACK BOEING 747 747236B 1384804 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 MAIN DECK SEAT TRACK CORRODED AT BS 1670, LBL 76, WL 200. 2 L 7 4 4F 4 F A20WE E3NE 2007033000310 20070330 00310 NM 2007 3 30 KCSA071086 1 20070327 A 5320 SHEAR WEB BOEING 747 747236B 1384804 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 MAIN DECK SLOPING SHEAR WEB CRACKED AT FORWARD I/B CORNER AFT OF TENSION TIE AT BS 820, LBL 77, STR 9L. 2 L 7 4 4F 4 F A20WE E3NE 2007033000330 20070330 00330 NM 2007 3 30 AMTA200700161 1 20070323 A 2540 MOUNT BOEING 737 73783N 13844HI NM AFT LAVATORY CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 301TZ 28239 RT AFT LAV OB CORNER MOUNT IS CORRODED (ON LAX) BS 952, RBL 49.5. REMOVED AND REPLACED RT AFT LAV MOUNT MM 25-00-00-8, REPLACEMENT PART FABRICATED 737-2500-01-8. (K) 2 L 7 2 4F RT A16WE 2007033000331 20070330 00331 SO 2007 3 30 SIMA200708203 1 20070320 A 2497 7287502609 WIRE HARNESS EMB 145 EMB145LR 3260212 SO CABIN MELTED A SIMA D RETURN TO BLOCK M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 637AE 17062 145170 SMOKE COMING FROM OVERHEAD ROW 1A, ELECTRICAL ODOR FROM SIDE WALL. FOUND ELECTRICAL HARNESS MELTED ABOVE SEAT 1A, REMOV ED AND REPLACED HARNESS ASSEMBLY IAW EMB 33-21-06. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007033000368 20070330 00368 EU 2007 3 30 AALA20070547 1 20070324 A 5210 BOTTLE AIRBUS 300 A300B4605R 3930308 EU PAX DOOR LOW PRESSURE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70054 461 MIA - EMERGENCY BOTTLE AT RIGHT NUMBER ONE DOOR HAS LOW PRESSURE. SERVICED EMERGENCY BOTTLE AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007040200004 20070402 00004 NM 2007 4 2 07FDEA00977 1 20070317 A 5320 ANGLE BOEING 727 727225 1384077 NM BS 1100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 MAIN CABIN UPPER LOBE STA 1100, "LEFT AND 1" RIGHT OF STR 1, HAS 2EA RIVETS WITH CRACKS AROUND RIVETS. REPAIRED DAMAGED AREA IAW SRM 53-30-3, FIG 3, AND SB 727-53A0204. REPAIRED DAMAGED SKATE ANGLE IAW SRM 51-40-9. PREPPED AND PAINTED ARE A IAW AMM 51-20-151-7. 2 L 7 3 4F A3WE 2007040200014 20070402 00014 NM 2007 4 2 07FDEA00991 1 20070319 A 5310 651961169 CREASE BEAM BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 CABIN LT CREASE BEAM INNER CHORD HAS 5 EA PLUGGED HOLES WL 208, BS 740 - 760. REMOVED SUPPORT ANGLE, AND INSTALLED NEW SUPPORT ANGLE, REFERENCE SRM 51-30-02. CLASSIFIED AS MAJOR REPAIR. 2 L 7 3 4F A3WE 2007040200022 20070402 00022 EU 2007 4 2 07FDEA01000 1 20070319 A 5320 FLANGE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 REPAIR DEFORMATION AND TOOL MARKS ON C74 OUTER FLANGE AT P26 LT AND RT REPAIR WAS PERFORMED BY REWORK TO SMOOTH CONTOUR ON THE OUTER FLANGE IAW EA 6-5318-106420 AND RAS/DATLS/0003545/2007 ISS. A 2 L 7 2 4F RT A35EU 2007040200027 20070402 00027 EU 2007 4 2 NWAA071173271 1 20070326 A 3350 BATTERY PACK AIRBUS 320 A320212 3930322 EU EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 371NW 1535 DURING EMERGENCY LIGHT CHECK, FOUND RIGHT EMERGENCY EPSU BATTERY INOP. REPLACED RIGHT EMERGENCY EPSU BATTERY, OPERATES GOOD. 2 L 7 2 4F RT A28NM 2007040200044 20070402 00044 EU 2007 4 2 07FDEA00962 1 20070316 A 5730 A57247242200 SKIN AIRBUS 310 A310324 3930206 EU ZONE 500 DELAMINATED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 CORROSION AND DELAMINATION ON T/E BOTTOM SURFACE LT WING. REPAIR WAS PERFORMED BY INSTALLING A NEW WEDGE SECTION AND A REPAIR PLATE IAW EA 6-5750-103433 AND RAS/BAE/1003821/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040200059 20070402 00059 NM 2007 4 2 AALA20070545 1 20070324 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39365 24046 SFO - EMERGENCY LIGHTS AT LEFT AND RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEF T AND RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007040200063 20070402 00063 NM 2007 4 2 AALA20070544 1 20070324 A 3297 CIRCUIT BREAKER BOEING 737 737823 13844BZ NM MLG TRIPPED A AALA A UNSCHED LANDING S J AFFECT SYSTEMS WARNING INDICATION CL CLIMB 1 SW 21 934AN 29531 AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. RETURNED TO MSY AND LANDED WITHOUT INCIDENT. FOUND GEAR LATCH AND PRESSUR E WARNING CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007040200069 20070402 00069 SO 2007 4 2 SIMA200708205 1 20070320 A 2741 3622001015 ACTUATOR EMB 145 EMB145LR 3260212 SO ZONE 100 FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 685AE 6724 14500836 MAIN PITCH TRIM FAILURE WARNING MESSAGE DURING CLIMB, RETURNED TO DFW. REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUA TOR IAW EMB AMM 27-40-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007040200076 20070402 00076 EU 2007 4 2 07FDEA00748 1 20070312 A 5313 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FOUND CORROSION OLD STRINGER REPAIR AT C42/43, P50 RT WASN'T ALLOWED IN AFFECTED AREA (RECHECK WITH SRM 53-10-14, FIG 20 1A). RENEW OF OLD REPAIR IAW SRM 53-10-14, FIG 201A. PERFORMED IAW RAS 048525/009/2006 ISSUE: A. (EA 6-5315-106344). 2 L 7 2 4F RT A35EU 2007040200086 20070402 00086 NM 2007 4 2 SWAA071596 1 20070327 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, WL 204 RT SIDE. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007040200096 20070402 00096 NM 2007 4 2 P5CA0701515 1 20070315 A 2840 UNKNOWN BOEING 747 747* NM FUEL UNKNOWN A P5CA D RETURN TO BLOCK J WARNING INDICATION NR NOT REPORTED 1 EA 15 496MC 29257 AT PUSHBACK OFF BLOCKS, RECEIVED STATUS MESSAGE FUEL OVRD 2 FWD. DEFER PER MEL 28-31-2. 2 L 7 4 4F RT A20WE 2007040200106 20070402 00106 NM 2007 4 2 AALA20070393 1 20070223 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 191AN 32385 DFW - EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. RESECURED LOOSE CONNECTION AT SIDEWALL FOR EMERGENCY LIGHT AT SEAT 26D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007040200117 20070402 00117 EU 2007 4 2 AALA20070389 1 20070224 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14068 511 MIA - EMERGENCY LIGHT AT SEAT 11G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 11G. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A35EU 2007040200130 20070402 00130 CE 2007 4 2 AKCA001 1 20070307 A 3210 50450181 WASHER CESSNA 414 414A 2075907 CE CONT O520 TSIO520* 17040 SO ZONE 700 SHEARED E AKCA O OTHER O OTHER LD LANDING 1 CE 05 414AN 5870 414A0819 ON LANDING AIRCRAFT VEERED TO THE RT, INSPECTION SHOWED WASHER PN 5045018-1 HAD SHEARED ALLOWING BOTTOM TORQUE LINK AND WHEEL ASSY TO TURN 180 DEGREES ROTATION. ADDITIONAL ROTATION WAS STOPPED WHEN BRAKE ASSY CONTACTED UPPER TORQUE LINK. CONSIDERING TORQUE LOADING UPON LANDING THE SPECIAL WASHERS PN 5045018-1 NEED TO BE CLOSELY INSPECTED AND CORRECT TOW OU T NEEDS TO BE MAINTAINED. THIS IS CENTER PIVOT TORQUE LINK BOLT WASHER. NOTE: WASHERS IN QUESTION MEASURE .045 - .032. 1 L 7 2 3O 3 O A7CE E8CE 2007040200136 20070402 00136 EU 2007 4 2 200703292 1 20070328 A 2120 UNKNOWN EMB ERJ170 ERJ170100SE 3260406 EU COCKPIT ODOR A UHLA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 634RW 17000055 FLIGHT 7764 ORF TO IAD - ON TAXI INTO GATE FWD LAV SMOKE DETECTOR WENT OFF. CREW REPORTS STRONG SMELL IN COCKPIT AND RE AR OF AIRPLANE. MAINTENANCE RAN ENGINES, NO TRACE OF SMOKE DETECTED. THIS IS A FIRST OCCURRENCE ON THIS AIRCRAFT AND H AS NOT REPEATED. SUSPECT SMOKE CAUSED BY STARTING OF APU. 2 L 7 2 4F RT A56NM 2007040200161 20070402 00161 WP 2007 4 2 07FDEA01118 1 20070323 A 5247 AJC771419 DIVERTER DOUG MD10 MD1010F 3022112 WP APU DOOR BENT A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 359FE 46635 PDIS: ADVISED BY GROUND MARSHALLER APU DOOR WAS OPEN AT BLOCK IN. DURING POST FLIGHT WALK AROUND NOTICED APU ACCESS DO OR WAS OPEN. LANDING WAS SMOOTH. FACT: INSPECTED DOOR AND DOOR LATCH'S ASSY,REF AMM 52-45-01-2. LATCH ASSY'S CK NORM AL. DOOR TRAILING EDGE FAIRING IS BENT AND INTERFERRING WITH CLOSING OF DOOR. SHEET METAL DEPT REPARIED FAIRING. DOOR C LOSES AND LATCHES NORMALLY. RETURNED TO SERVICE. 2 L 7 3 4F RT A22WE 2007040200162 20070402 00162 WP 2007 4 2 07FDEA01119 1 20070323 A 5512 SKIN DOUG DC10 DC1010 3022110 WP HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 RT HORIZONTAL AT STA. XE87 UPPER SKIN PLANK STRINGER 4 IS CRACKED. ACCOMPLISHED REPAIR IAW EA 8-5510-105177-STABILIZER S-HORIZ.-RT AFT OUTB. UPPER PANEL S4R CRACK AT XE 87-REPAIR. MECH 2579 2 L 7 3 4F A22WE 2007040200163 20070402 00163 WP 2007 4 2 07FDEA01120 1 20070323 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 INSPECT/REPAIR/MOD LT AND RT TEE CAPS. CARD E8-5310-7-3327 PT.3. C/W E8--5310-105179- FUSELAGE-AD 96-18-11-LT AND RT 11 56 BULKHEAD TEE AND SKIN CRACK-REPAIR. MAJOR REPAIR. 2 L 7 3 4F A22WE 2007040200165 20070402 00165 WP 2007 4 2 07FDEA01121 1 20070323 A 5312 SKIN DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 INSPECT/REPAIR/MOD LT AND RT TEE CAPS, CARD E8-5310-7-3327 PT.4. C/W FUSELAGE-AD96-18-11-LT AND RT 1156 BULKHEAD TEE AN D SKIN CRACK-REPAIR. MAJOR REPAIR. 2 L 7 3 4F A22WE 2007040200171 20070402 00171 EA 2007 4 2 A6WA200740149 1 20070314 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 415AW 7593 RT FS 625.00 OBLIQUE ANGLE IS CRACKED 1.5 INCH LONG IN AFT RADIUS. (K) [SUP 06-05-07] MAINTENANCE REMOVED CRACKED ANG LE AND INSTALLED NEW SERVICEABLE NEW SERVICEABLE ANGLE P/N 601-35012-52 IAW CRJ SRM 51-42-21 AND BSC EO 601R-53-11207. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007040200183 20070402 00183 WP 2007 4 2 07FDEA01023 1 20070320 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 FWD PIT BILGE STA-879 LOWER SURFACE OF TOP FLANGE OF OF WEB CORRODED AT LONGERON 43R. REMOVED CORROSION, TRIMMED OUT DAMAGE IAW DC/MD10 SRM 53-00-01 FIG 9 SHT 9. REMOVED FLOOR SUPPORT, STRAPS AND FILLERS IAW DC/MD 10 SRM 51-31-01 PAGE 1 VOLII. REPLACED FLOOR SUPPORT, STRAPS AND FILLERS IAW DC/MD10 SRM 51-31-01 PAGE 1 VOL II AND 53-00-01 FIG 9 SHT 9. 2 L 7 3 4F A22WE 2007040200200 20070402 00200 NM 2007 4 2 DU4R2007075 1 20070323 A 5210 10607798A ROD END BOEING 757 757232 1384965 NM R1 DOOOR CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND CORROSION ON R1 DOOR INTERNAL UPPER END CENTER CONTROL ROD WITH RUSTED ROD END. REPAIRED BY REMOVING AND REPLACIN G ROD END WITH P/N 10-60779-8A IAW BOEING CMM 52-11-05. 2 L 7 2 4F RT A2NM 2007040200215 20070402 00215 CE 2007 4 2 AJ02007F00000 1 20070206 A 3233 SWITCH CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG ACTUATOR FAULTY A AJ0A A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 EA 63 72SG 5605508 WHILE ON APPROACH, THE AC EXPERIENCED A RT MLG UNSAFE INDICATOR LIGHT AFTER THE GEAR WAS SELECTED TO THE EXTENDED POSITI ON. A SUBSEQUENT FLY-BY WAS CONDUCTED AND THE TOWER STATED THE POSITION OF THE GEAR WAS INCONCLUSIVE. THE CREW THEN CO NDUCTED THE UNSAFE GEAR/ EMERGENCY EXTENSION CHECKLIST WHICH INCLUDED BLOWING THE GEAR DOWN. THE CREW ELECTED TO DIVERT , WHICH PROVIDED MORE FAVORABLE CAPABILITIES FOR THE OCCURRENCE. ANOTHER FLY-BY WAS CONDUCTED, AND THE TOWER STATED THE GEAR (APPEARED TO BE DOWN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INVESTIGATION REVEALED NO ANOMALIES WHIL E PERFORMING A GROUND CHECK. INFORMATION RECEIVED FROM THE MFG INDICATED THAT A NUMBER OF SAME MODEL AIRCRAFT HAD EXPER 2 L 7 2 4F 4 F RT A22CE E00059EN 2007040200216 20070402 00216 NM 2007 4 2 AMTA200700172 1 20070325 A 4970 WARNING LIGHT BOEING 737 73783N 13844HI NM COCKPIT ILLUMINATED A AMTA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 318TZ 28247 ATTEMPTED START OF APU, FAULT LIGHT, NO LIGHT OFF. PERFORMED BITE IAW FIM 49-60-00-810-801-802, CURRENT FAULTS DISPLAY ED. (K) 2 L 7 2 4F RT A16WE 2007040300009 20070403 00009 EA 2007 4 3 HSYA200700001 2 20070227 A 7260 3037277 ROTOR SHAFT PWA PT6A65B BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA ZONE 600 SHEARED E HSYA B A EMER. DESCENT UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 NM 05 101UE GG32358 UC101 GG32358 UPON REACHING ALTITUDE THE RT ENGINE LOST OIL AND FUEL PRESSURE AND THE ENGINE SHUTDOWN. THE AIRCRAFT RETURNED TO DEPAR TURE AND LANDED WITHOUT FURTHER INCIDENT. THE NR 2 ENGINE WAS REMOVED AND SENT FOR TEARDOWN TO DETERMINE CAUSE OF THE FA ILURE. ON TEARDOWN THE COMPRESSOR ROTOR SHAFT (STUB SHAFT) WAS FOUND TO HAVE FAILED. ANY ADDITIONAL INFORMATION WILL BE SUBMITTED AS IT BECOMES AVAILABLE. 2 L 7 2 4T 4 T RT A24CE E4EA 2007040300013 20070403 00013 NM 2007 4 3 07FDEA01051 1 20070321 A 5310 651961169 CREASE BEAM BOEING 727 727225 1384077 NM BS 740-760 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 CABIN FLOOR CREASE BEAM RT INNER CHORD HAS 7 PLUGGED HOLES BS 740-760, REPLACED CABIN FLOOR CREASE BEAM ANGLE AT CREASE BEAM STA 740-760 ON RT SIDE AT RBL 63" REFERENCE SRM 51-30-2. 2 L 7 3 4F A3WE 2007040300018 20070403 00018 WP 2007 4 3 07FDEA01061 1 20070321 A 7120 BRACKET DOUG MD10 MD1010F 3022112 WP NR 2 ENGINE CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 566FE 46989 NR 2 ENG RT LOWER FORWARD FLANGE SHIP STAND ATTACHED POINT CRACK PAST STOP DRILL BOTH SIDES OF FLANGE. REMOVED GROUND HANDLING BRACKET IAW MD/DC 10 SRM 51-33-01 VOL 11. WELDED CRACK IN NR 2 ENG RT LOWER FORWARD FLANGE SHIP STAND IAW GE C OMMERCIAL ENGINE STANDARD PRACTICE MANUAL 72-23-01 REPAIR 1 STEP 1-4. REINSTALLED BRACKET IAW MD/DC 10 SRM 51-33-01 VOL 11. 2 L 7 3 4F RT A22WE 2007040300023 20070403 00023 CE 2007 4 3 DXTA200702057 1 20070331 A 3244 TIRE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LT MLG FAILED E DXTA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 961QS 7500061 LT MAIN TIRES ARE BLOWN, LT BRAKE POSSIBLY DRAGGING. PERFORMED OPS TEST OF NR 1 & 2 BRAKES NO DEFECTS NOTED REPLACED NR 1 BRAKE. REPLACED NR 2 BRAKE. REPLACED NR 1 MLG WHEEL & TIRE ASSY ON TIRE REPLACED NR 2 MLG WHEEL & TIRE ASSY. ALL WORK PERFORMED IAW CE750 MM 32-41-02, 32-42-01, 32-00-01 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007040300029 20070403 00029 CE 2007 4 3 DXTA200702064 1 20070401 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG WEAK E DXTA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 GL 07 339QS 5600339 RT (CO-PILOTS) BRAKE PEDALS ARE VERY SOFT. NOTE CREW REPORTS BOTH COPILOTS PEDALS ARE SOFT. NO SIGN OF FLUID ON FLOOR. [ SUP 4-26-07] PERFORMED BRAKE BLEEDING PROCEDURE I/A/W AMM 32-42-00. OPS CHECKS GOOD IN SHOP. 2 L 7 2 4F 4 F RT A22CE E25EA 2007043000173 20070430 00173 NM 2007 4 30 SWAA072054 1 20070425 A 5340 65C27314 STRINGER CLIP BOEING 737 7373L9 1384470 NM BS 685 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007040300031 20070403 00031 CE 2007 4 3 GLBA20060929 1 20070329 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE COCKPIT ODOR A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 100UX UE100 PILOTS REPORTED 30 MINUTES INTO THE FLIGHT THAT A BURNING SMELL WAS EVIDENT WITH BLOWERS IN AUTO. PILOTS SELECTED THE BL OWERS OFF AND THE SMELL WENT AWAY. MAINTENANCE INSPECTED BLOWER MOTORS FORWARD AND AFT, FLAP MOTOR, CIRCUIT BREAKER PAN ELS UNDER THE FLOOR AND OPERATIONALLY CHECKED ALL SYSTEMS IN COCKPIT AND CABIN WITH NO FAULTS FOUND. REFERENCE 24-00-00, 21-20-01, AND 27-50-03. 2 L 7 2 4T 4 T RT A24CE E26NE 2007040300038 20070403 00038 WP 2007 4 3 I5HA0758006 1 20070328 A 2120 UNKNOWN CVAC 580 580 2422806 WP ALLSN 501D 501D13 03004 GL COCKPIT SMOKE A I5HA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 23 582 475 700112 DURING ENGINE START, THE CREW OBSERVED AND SMELLED SMOKE IN THE COCKPIT. THE CREW REPORTED TO MAINTENANCE THAT THE SMOK E HAD AN OILY ODOR. MAINTENACE REMOVED ALL ENGINE DRIVEN COMPRESSOR (EDC) DUCTING AND INSPECTED FOR OIL, NONE WAS FOUND . THE EDC OIL LEVEL WAS CHECKED AND WAS NORMAL. MAINTENANCE RAN THE ENGINE AND OPERATED THE AIR CONDITIONING SYSTEM HO T AND COLD A NUMBER OF TIMES. NO SMOKE WAS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT E282 2007040300040 20070403 00040 EU 2007 4 3 1234567 1 20070328 A 2150 COMPRESSOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE AIR CONDITIONER SEIZED E A1UA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 03 123LN 4115 FUMES IN FLIGHT. LANDED ASAP, SHUTDOWN, MADE WRITE-UP IN MAINTENANCE RECORD AND WAITED FOR MECHANIC. NOTE: THE AIRCRAF T MODEL IS AS350B2 NOT EC130B4. 1 G 7 1 3U 3 U H9EU E19EU 2007040300042 20070403 00042 EA 2007 4 3 S9BA00107 2 20070307 A 7310 3011857 FUEL LINE DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA ZONE 500 CRACKED A S9BA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 29 251SA 2250 47 524 PGO266 PERFORMED PRECAUTIONARY SHUTDOWN DUE TO A MAJOR FUEL LEAK SIGHTED COMING FROM THE LT ENGINE. REPLACED FUEL LINE FROM FC U TO TOP OF START CONTROL. 1 H 7 2 3T 4 T RT A9EA E4EA 2007040300043 20070403 00043 EA 2007 4 3 S9BA00207 2 20070307 A 7230 3013411 COMPRESSOR WHEEL DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA ZONE 500 DAMAGED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 251SA 2250 51 524 PGO266 LT ENGINE VIBRATION OCCURRED WHEN MOTORED AFTER FUEL LINE REPLACEMENT. REMOVED AND HAD C/T DISK ASSEMBLY OVERHAULED INS TALLED SAME ASSEMBLY. (SULFIDATION) 1 H 7 2 3T 4 T RT A9EA E4EA 2007040300046 20070403 00046 NE 2007 4 3 ASMF200703008 2 20070327 A 7200 JT8D219 ENGINE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE LEFT OVERSPEED W ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 803ML 43316 3018 49726 716781 AIRCRAFT REJECTED TAKEOFF AT 77 KNOTS DUE TO LT ENGINE REACHED ONLY 1.6 EPR WITH N1 104 PERCENT. AIRCRAFT WAS SENT TO T HE HANGAR AND ENGINE WAS REMOVED AND SENT TO THE SHOP. THE NRC A0111096 WAS ISSUED TO CHECK ENGINE PT2 AND PT7 LINES AND MANIFOLD BY LEAKS IAW MM 72-00-03, DETECTING A PT7 LINE LEAKING AND DELAMINATED, SO IT WAS REPLACED. ENGINE OVERSPEED A ND OPERATIONAL TESTS WERE PERFORMED IAW MM 72-00-00 PAGE 516 PARAGRAPH 2H (3)(D), DETERMINING REPLACEMENT OF C1 IAW MM 7 2-00-00 AND MPCM 71-00-01, TESTED CORRECT. ADDITIONALLY, CHIP DETECTORS, EXHAUST PRESSURE PROBES, THROTTLE ADJUSTMENT AN D ENGINE TRIM WERE PERFORMED IAW MM 77-11-04, 76-00-00 AND 71-00-00, ALL CORRECT. AS A PRECAUTIONARY ACTION, LT EPR TRAN 2 L 7 2 4F 4 F RT A6WE E9NE 2007040300052 20070403 00052 NM 2007 4 3 AWXA200700442 1 20070306 A 5210 5079454 SKIN BOEING 737 7373G7 1384595 NM ZONE 800 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - L-1 DOOR INNER SKIN CRACKED, AT THE 6TH AND 7TH STOP FROM TOP, BS 347.30, BEAM 12 - BEAM 13. REPAIRED L-1 DOOR IN NER SKIN CRACKED, AT THE 6TH AND 7TH STOP FROM TOP, BS 347.30, BEAM 12 - BEAM 13 IAW AWA ER 03-5200-07084-SS1. 2 L 7 2 4F RT A16WE 2007040300053 20070403 00053 NM 2007 4 3 AWXA200700443 1 20070306 A 5320 65479573 WEB BOEING 737 7373G7 1384595 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CORROSION ON AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL WEB, BS 794 - 847, S25R. REPLACED AFT CARGO COMP ARTMENT DOOR CUT OUT LOWER SILL WEB, BS 794 - 847, S25R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007040300054 20070403 00054 NM 2007 4 3 AWXA200700444 1 20070306 A 5311 6520723 FRAME BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND FORWARD CARGO COMPARTMENT FRAME CRACKED, BS 492, S24R. REPAIRED FORWARD CARGO COMPARTMENT FRAME, BS 492, S2 4R IAW AWA ER 03-5300-07086-SS3. 2 L 7 2 4F RT A16WE 2007040300055 20070403 00055 NM 2007 4 3 AWXA200700445 1 20070305 A 5754 65C267943 SKIN BOEING 737 7373G7 1384595 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - LEFT WING NR 2 SLAT SKIN LOWER SURFACE CRACKED, SS 153.4 - SS 238.4. REPAIRED LEFT WING NR 2 SLAT SKIN LOWER SURF ACE, SS 153.4 - SS 238.4 IAW B737-300 SRM 57-43-01-2R6, FIGURE 201. 2 L 7 2 4F RT A16WE 2007040300057 20070403 00057 NM 2007 4 3 AWXA200700447 1 20070305 A 5743 654948823 FITTING BOEING 737 7373G7 1384595 NM ZONE 500 - LEFT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - LEFT WING MAIN LANDING GEAR SUPPORT BEAM FITTING CRACKED, RSS 219.5. REPLACED LEFT WING MAIN LANDING GEAR SUPPORT BEAM FITTING CRACKED, RSS 219.5 IAW AWA ER 03-5722-07086-SS4. 2 L 7 2 4F RT A16WE 2007040300064 20070403 00064 EA 2007 4 3 SIMA200708802 1 20070327 A 5610 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT FAILED A SIMA B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 512AE 10110 CAPTAIN SIDE WINDOW SHATTERED. EMERGENCY DECLARED. DIVERTED TO JAX. 2 L 7 2 4F RT A21EA 2007040300065 20070403 00065 SO 2007 4 3 SIMA200708801 1 20070327 A 2810 FUEL SYS EMB 145 EMB145LR 3260212 SO WING LEAKING A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 680AE 14500820 FOUND FUEL STREAMING FROM WING ON CLIMB-OUT. 2 L 7 2 4T RT T00011AT 2007040300067 20070403 00067 SO 2007 4 3 SIMA200708901 1 20070329 A 2121 4611028900 FAN EMB 145 EMB145LR 3260212 SO ZONE 100 SEIZED A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 656AE 15190 3603 145740 BURNING ELECTRICAL ODOR IN CABIN AND FLIGHT DECK DURING TAXI OUT, RETURNED TO BLOCK. REMOVED AND REPLACED RECIRCULATION FAN AND PACK VALVE IAW EMB AMM. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007040300068 20070403 00068 SO 2007 4 3 SIMA200708902 1 20070330 A 2820 2810051104 VALVE EMB 145 EMB145LR 3260212 SO ZONE 500 FAILED A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 922AE 4895 14500906 FLUID STREAMING FROM LEFT WING, RETURNED TO CHA. POST INSPECTION LEFT OUTBOARD WING WET FROM FLUID AND REVEALED FUEL ST RAINED AROUND VENT VALVE AND FLAME ARRESTOR. FERRIED AIRCRAFT TO CMI FOR REPAIR. REMOVED AND REPLACED VENT VALVE IAW E MB AMM. OPERATIONAL AND LEAK CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007040300070 20070403 00070 SO 2007 4 3 SIMA200708606 1 20070323 A 5320 14525480603 SILL EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 852AE 9852 4800 145736 FOUND CARGO DOOR LOWER SILL FOUND CORRODED. REMOVED AND REPLACED CARGO DOOR LOWER SILL IAW EMB SRM 51-20-03, 51-40-02, 51-40-06 AND 51-21-06. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007040300071 20070403 00071 SO 2007 4 3 SIMA200708607 1 20070323 A 5315 14521700007 FLOORBEAM EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 852AE 9852 4800 145736 LEFT OMEGA BEAM FOUND CORRODED AT FRAME 25. CUT OUT CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB IC2007-145 /01986, DATED 03-21-07. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT T00011AT 2007040300072 20070403 00072 EU 2007 4 3 SIMA200708601 1 20070326 A 3260 MS213212 UPLOCK SWITCH SAAB SF340 340B 7860101 EU ZONE 700 FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 317AE 23086 340B317 LANDING GEAR LIGHT ON AFTER TAKEOFF, HYDRAULIC PUMP RUNNING CONTINUALLY. REMOVED AND REPLACED RIGHT MAIN GEAR UPLOCK SW ITCH IAW SAAB AMM 32-61-15. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4T RT A52EU 2007040300073 20070403 00073 SO 2007 4 3 SIMA200708603 1 20070326 A 3350 7281000501 CONTROL MODULE EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS FAILED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 610AE 13 145073 DISCOVERED EMERGENCY FLOOR LIGHTING INOPERATIVE STARTING AT ROW 3A DURING CREW'S PREFLIGHT. ELECTRICAL SMELL NOTED. RE MOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW EMB 33-21-01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007040300075 20070403 00075 SO 2007 4 3 SIMA200708605 1 20070323 A 5330 14520555005 SKIN EMB 145 EMB145LR 3260212 SO ZONE 200 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 928AE 4890 4890 14500911 DENT FOUND IN FUSELAGE SKIN AFT OF FRAME 26 AND BETWEEN STRINGERS 20R AND 21R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 51-40-02 AND 53-22-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007040300077 20070403 00077 SO 2007 4 3 SIMA200709202 1 20070327 A 3220 14524475003 BEARING CAP EMB 135 EMB135LR 3260305 SO ZONE 700 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 708AE 15810 4800 145205 NOSE LANDING GEAR LEFT BEARING CAP FOUND CORRODED. REMOVED AND REPLACED BEARING CAP IAW EMB AMM 32-20-01. RETURNED AIR CRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007040300078 20070403 00078 2007 4 3 SIMA200709201 2 20070401 A 7261 4252070 CARBON SEAL EMB 145 EMB145LR 3260212 SO ENGINE 2 FAILED A SIMA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 651AE 145422 NUMBER 2 ENGINE OIL QUANTITY DROPPED TO 4 QUARTS, OIL PRESSURE STARTED TO DROP. CREW SHUTDOWN ENGINE. DIVERTED TO CID. POSTFLIGHT INSPECTION REVEALED OIL ON NUMBER 2 ENGINE COWL. REMOVED AND REPLACED NUMBER 4 GENERATOR AND CARBON SEAL A SSEMBLY PER EMB AMM 72-53-10 AND AMERICAN EAGLE WORK CARD 24-800-00. OPERATIONAL AND LEAK CHECK GOOD. RETURNED AIRCRAF T TO SERVICE. 2 L 7 2 4T RT T00011AT 2007040300085 20070403 00085 CE 2007 4 3 DJFA2007034 1 20070322 A 3260 1283600791 ANNUNCIATOR BEECH MU300 400A 1155402 CE MLG INOPERATIVE E DJFA O OTHER P NO WARNING INDICATION LD LANDING 1 EA 23 467LX 982 RK447 TRIP NR 1154624 - CREW REPORTED NO GREEN GEAR DOWN AND LOCKED LIGHTS. CREW ACCOMPLISHED EMERGENCY GEAR EXTENSION AND DE CLARED EMERGENCY. MAINTENANCE DISCOVERED THE LANDING GEAR INDICATOR CAPSULE INOPERATIVE. THE CAPSULE WAS REPLACED. 2 H 7 2 4F RT A16SW 2007040300087 20070403 00087 NM 2007 4 3 AWXA200700429 1 20070306 A 5311 65C312403 FRAME BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - AFT CARGO COMPARTMENT DOOR SURROUND FORWARD FRAME CRACKED, BS 794, S25R. REPAIRED AFT CARGO COMPARTMENT DOOR SURR OUND FORWARD FRAME CRACKED, BS 794, S25R IAW AWA ER 03-5362-07091-SS1. 2 L 7 2 4F RT A16WE 2007040300090 20070403 00090 EU 2007 4 3 AWXA200700432 1 20070323 A 5340 D53112198201 FITTING AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 FOUND CORROSION ON R1 DOOR CUT OUT LOWER SILL CENTER FITTING, -Y1860, FR 16 + 5" - FR 19 + 4". REPLACED R1 DOOR CUT OU T LOWER SILL CENTER FITTING, -Y1860, FR 16 + 5" - FR 19 + 4" IAW A320 SRM 51-42-11. 2 L 7 2 4F RT A28NM 2007040300091 20070403 00091 EU 2007 4 3 AWXA200700433 1 20070326 A 3211 D3215303200200 PIN AIRBUS 320 A320231 3930325 EU ZONE 700 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 634AW 091 SAL - CORROSION ON RIGHT MAIN LANDING GEAR REAR PINTLE PIN THREADS. REPLACED RIGHT MAIN LANDING GEAR REAR PINTLE PIN I AW AWA TASK CARD R4M32304. 2 L 7 2 4F RT A28NM 2007040300092 20070403 00092 NM 2007 4 3 AWXA200700434 1 20070317 A 5534 65537447 SUPPORT CHANNEL BOEING 737 7373G7 1384595 NM ZONE 300 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - CRACKED VERTICAL STABILIZER SUPPORT STIFFENER CHANNEL, BS 1095, RBL 8.5. REPLACED VERTICAL STABILIZER SUPPORT ST IFFENER CHANNEL, BS 1095, RBL 8.5 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007040300093 20070403 00093 NM 2007 4 3 AWXA200700435 1 20070315 A 5320 65479599 INTERCOSTAL BOEING 737 7373G7 1384595 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - CORROSION ON AFT CARGO COMPARTMENT INTERCOSTAL, BS 797, S25R. REPLACED AFT CARGO COMPARTMENT INTERCOSTAL, BS 797, S25R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007040300099 20070403 00099 NM 2007 4 3 AWXA200700441 1 20070308 A 5210 STOP FITTING BOEING 737 7373G7 1384595 NM ZONE 800 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - R1 DOOR CRACKED AT 4TH AFT STOP FITTING CUTOUT FROM TOP, BS 299, WL 246. REPAIRED R1 DOOR AT 4TH AFT STOP FITTIN G CUTOUT FROM TOP, BS 299, WL 246 IAW AWA ER 03-5211-07081-ES3. 2 L 7 2 4F RT A16WE 2007040300100 20070403 00100 CE 2007 4 3 5183246256 1 20070315 A 2720 99145586 ACTUATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RUDDER BINDING E J00A K NONE F FLT CONT AFFECTED CR CRUISE 1 EA 01 505MA 2454 2454 7500057 RUDDER MOVEMENT WAS LIMITED TO 20 PERCENT OF FULL TRAVEL. SERVICE CENTER FOUND ACTUATOR TO BE SEIZED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007040300102 20070403 00102 CE 2007 4 3 GUUA03280701 1 20070328 A 2120 1X2X136X60 FILTER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BLOWER ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 29 190YV UE190 DURING FLIGHT OIL ODOR COMING FROM BLOWERS. REPLACED AFT BLOWER MOTOR FILTERS. 2 L 7 2 4T 4 T RT A24CE E26NE 2007040300103 20070403 00103 CE 2007 4 3 DJFA2007036 1 20070328 A 5411 FRAME BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE NR 1 NACELLE CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 785TA RK239 DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND A CRACK IN THE NR 1 ENGINE AFT NACELLE SUPPORT FRAME. THE CRACK WAS AB OUT .25 INCH, LOCATED ON THE IB SIDE JUST FWD OF THE TR AND JUST ABOVE THE PYLON AT ABOUT THE 0930 POSITION LOOKING AFT. CRACK WAS REPAIRED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007040300110 20070403 00110 NM 2007 4 3 QXEA200700486 1 20070326 A 5340 ATTACH FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - FOUND UPPER CENTER ATTACH HARDWARE HOLE FOR PANEL 122AR IS ELONGATED. REPAIRED IAW RD8-53-4317. 2 H 7 2 4T RT A13NM 2007040300111 20070403 00111 NM 2007 4 3 QXEA200700487 1 20070328 A 5320 WEB DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - SUSPECT CORROSION ON WEB AND ANGLE JUST AFT AND BELOW LEFT CENTER EMERGENCY EXIT DOOR AT FLOOR LEVEL AT STATIO N Z100.032 AND X387.350. REPAIRED IAW SRM 51-20-11, 51-40-11. 2 H 7 2 4T RT A13NM 2007040300117 20070403 00117 EA 2007 4 3 QXEA200700494 1 20070328 A 2800 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 616QX 10128 DEN - ON TAXI OUT, RECEIVED A "L FADEC" CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENANCE PERFORMED A ENGINE RUN AND FOUND NO DEFECTS. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007040300120 20070403 00120 NM 2007 4 3 QXEA200700503 1 20070331 A 3150 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 416QX 4083 HLN FLIGHT NR 2322: ABORTED TAKEOFF, PRIOR TO 60 KNOTS, RECEIVED A NR 2 BLEED HOT CAUTION LIGHT. RAN CHECKLIST. NR 2 B LEED HOT CAUTION MESSAGE WENT OUT AFTER ONE MINUTE. MAINTENANCE C/W Q400 FIM TASK 36-20-00-810-802 FROM PARA 1 THRU 3 S TEP 1 THRU 3A. C/W CLOSE OUT TASK PARA 5. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007040300121 20070403 00121 NM 2007 4 3 QXEANM09401 1 20070313 A 4920 164161100 DRAIN VALVE SUNDSTRANDEM BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA APU PLUGGED G QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 BALL ON WRONG SIDE OF SPRING, WHICH ALLOWS IT TO REST IN CLOSED POSITION, NOT ALLOWING PROPER DRAINAGE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2007040300122 20070403 00122 NM 2007 4 3 QXEA200700475 1 20070326 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - SEAT TRACK NR 10 HAS CHAFE, SCRATCHES, NICKS AT STATION X260, X306, X376, X430. REPAIRED IAW RD8-53-1342. 2 H 7 2 4T RT A13NM 2007040300123 20070403 00123 NM 2007 4 3 QXEA200700481 1 20070327 A 5230 ATTACH ANGLE DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - THERES CORROSION ON VERTICAL WEB AND ATTACHED ANGLE AT STATION X600.00 AND Z99.00 JUST INSIDE CARGO DOOR AND AB OVE THE OUTBOARD AFT CORNER OF FLOORBOARD PANEL 144AZ. REPAIRED IAW SRM 51-40-11, 51-20-16, AND 51-20-11. 2 H 7 2 4T RT A13NM 2007040300126 20070403 00126 NM 2007 4 3 QXEA200700477 1 20070326 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - SEAT TRACK NR 11 HAS SCRATCHES AT STATION X438, X456, X467, X492. REPAIRED IAW RD8-53-1342. 2 H 7 2 4T RT A13NM 2007040300127 20070403 00127 NM 2007 4 3 QXEA200700478 1 20070326 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - FOUND SEAT TRACK NR 12 HAS SCRATCHES AT STATION X525, X540. REPAIRED IAW RD8-53-3644 AND RD8-53-1342. 2 H 7 2 4T RT A13NM 2007040300130 20070403 00130 NM 2007 4 3 QXEA200700474 1 20070328 A 5210 STRUCTURE DHAV DHC8 DHC8202 2809007 NM PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - CORROSION AROUND THE PASS THROUGH HOLE FOR THE MAIN CABIN DOOR SEAL INFLATION TUBE. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007040300131 20070403 00131 NM 2007 4 3 QXEA200700473 1 20070328 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - FOUND SEAT TRACK NR 7 HAS CORROSION AT STATION X236. REPAIRED IAW RD8-53-4473 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007040300132 20070403 00132 NM 2007 4 3 QXEA200700489 1 20070326 A 5551 MOUNT DHAV DHC8 DHC8202 2809007 NM HORIZONTAL STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - LEFT FORWARD HORIZONTAL STAB MOUNT/STAND-OFF HAS LIGHT SCRATCHES AND PAINT. REPAIRED IAW RD8-55-847, SRM 51-20 -16, 51-20-36, AND 51-20-51. 2 H 7 2 4T RT A13NM 2007040300133 20070403 00133 NM 2007 4 3 QXEA200700485 1 20070325 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 263 S2-3L DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - BURN MARK AT RIVET FOR FRAME X263 BETWEEN STRINGERS 2L AND 3L. REPAIRED IAW SRM 51-40-11 AND 51-20-26. 2 H 7 2 4T RT A13NM 2007040300134 20070403 00134 NM 2007 4 3 QXEA200700490 1 20070326 A 5330 PANEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - 4 HOLES ELONGATED AT PANEL 122AR APERTURE. REPAIRED IAW RD8-53-4317. 2 H 7 2 4T RT A13NM 2007040300136 20070403 00136 NM 2007 4 3 QXEA200700492 1 20070325 A 5730 ACCESS PANEL DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - FUEL TANK ACCESS PANEL 524CL HAS FRETTING ON WING STRUCTURE AT STATION YW404.00, YW387.00, YW369.00 AND YW334.0 0. REPAIRED IAW RD8-57-611. 2 H 7 2 4T RT A13NM 2007040300139 20070403 00139 WP 2007 4 3 070079 1 20070326 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 875GA 53468 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION LAS VEGAS, MAINTENANCE REPORTED THAT THE CEILING MOUNTED EMERGENCY L IGHTS FROM SEAT ROW 25 TO SEAT ROW 28 WOULD NOT TEST. LAS VEGAS MAINTENANCE FURTHER REPORT THE REMOVAL AND REPLACEMENT OF AN EMERGENCY LIGHT POWER SUPPLY BATTERY PACK AT FS 1057R. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED PER AMM 33- 53-00. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007040300141 20070403 00141 WP 2007 4 3 070081 1 20070328 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 879GA 53486 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION SANFORD MAINTENANCE REPORTED THAT BOTH AFT OVERWING ESCAPE HATCH 'EX IT' SIGNS WOULD NOT TEST. SANFORD MAINTENANCE FURTHER REPORT THE REMOVAL AND REPLACEMENT OF 2 EMERGENCY LIGHT POWER SUP PLY BATTERY PACKS. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SE RVICE. 2 L 7 2 4F RT A6WE 2007040300144 20070403 00144 EU 2007 4 3 07FDEA01073 1 20070321 A 5315 FLOORBEAM AIRBUS 310 A310222 3930315 EU FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 421FE 342 REWORK OF FR 14 REPAIR DOUBLER TO FLOOR CROSSBEAM REQUIRED DUE TO INSUFFICIENT ED ON FASTENER HOLES COMMON TO STAND OF F BRACKETS. REMOVED REPAIR DOUBLER (ANGLE) AND FILLER SHIM IAW A310-200 SRM 51-40-21. FABRICATED NEW REPAIR DOUBLER (ANGLE) AND FILLER SHIM IAW A310-200 SRM 53-12-15 FIG 201 AND 202. APPLIED SURFACE PROTECTION TO REPAIR DOUBLER (ANGLE) AND FILLER SHIM IAW A310-200 SRM 51-21-10 AND SRM 51-75-10. INSTALLED NEWLY FABRICATED REPAIR DOUBLER (ANGLE) AND FILL ER SHIM IAW A310-200 SRM 53-12-15. 2 L 7 2 4F RT A35EU 2007040300145 20070403 00145 EU 2007 4 3 07FDEA01074 1 20070321 A 5320 FLOOR SUPPORT AIRBUS 310 A310222 3930315 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 UPON REMOVAL OF CEILING PANEL 131EC FOR AGING ACFT INSPECTION, FOUND MDCC FLOOR SUPPORT C36 BETWEEN L4 AND L5 SEAT TRA CK TO BE CRACKED TOP OF VERTICAL STIFFENER LENGTH OF CRACK .400 INCH ROUTED OUT CRACK IAW A310/200 SRM 53-10-15. FABRIC ATED 2 REPAIR ANGLES AND INSTALLED IAW A310-200 SRM 53-10-15. REPROTECTED AREA IAW A310-200 SRM 51-75-10. 2 L 7 2 4F RT A35EU 2007040300146 20070403 00146 EU 2007 4 3 07FDEA01075 1 20070321 A 5315 FLOORBEAM AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 MDCC FLOORBEAM AT FR 14 LT 64 INCHES FROM CENTER HAS 1 SPOT OF CORROSION ON FORWARD BOTTOM FACE 15" LONG BY 1" WIDE. RE MOVED CORROSION IAW SRM 51-74-10 CHECKED LIMITS IAW SRM 53-12-15, OUT OF LIMITS. FABBED REPAIR IAW A310/200 SRTM 53-12- 15 PB210 FIG 201. REPROTECTED REPAIR IAW A310-200 SRM 51-75-10. INSTALLED REPAIR IAW A310-200 SRM 51-40-21 AND SRM 53- 12-15. 2 L 7 2 4F RT A35EU 2007040300147 20070403 00147 EU 2007 4 3 07FDEA01076 1 20070322 A 5320 TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 PREVIOUS REPAIR LOCATED ON AFT CARGO ROLLER TRACK LEFT NR 2 HAS A 9 INCH LONG REPAIR SECTION WITH 2 REPAIR ANGLES ON T HE OUTBD SIDE MEASURING 7 INCH LONG EACH BETWEEN FRAMES 54.3 TO55/58 PREVIOUSLY INSTALLED REPAIR WAS DETERMINED NOT TO BE IAW A310 SRM 53-10-15 FIG 203. REMOVED AND REINSTALLED 2 EACH FLOOR PANELS PER A310-200 AMM 53-10-33-4. REMOVED AND REPLACED 2 EACH REPAIR ANGLES PER A310 SRM 53-10-15 FIG 203. 2 L 7 2 4F RT A35EU 2007040300148 20070403 00148 EU 2007 4 3 07FDEA01078 1 20070322 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 FWD CARGO COMPARTMENT, OVER HEAD FLOORBEAM [ C34 ] FWD FACE OF BEAM , LOCATED BETWEEN L4 AND L5 SEAT TRACK HAS A 0.425 I NCH CRACK IN VERTICAL STIFFENER. REMOVED AND REINSTALLED FLOOR BOARD 231KF AND 231QF TO FOM REPAIR IAW A310-200 AMM 53- 10-25-4. REPAIRED FLOORBEAM C34 BETWEEN L4 AND L5 SEAT TRACK IAW A310-200 SRM 53-10-15. 2 L 7 2 4F RT A35EU 2007040300149 20070403 00149 EU 2007 4 3 07FDEA01079 1 20070322 A 5340 A53613847200 ATTACH FITTING AIRBUS 310 A310324 3930206 EU ZONE 200 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CRACK ON CROSSBEAM ATTACHMENT FITTING AT FRAME 12A THROUGH 13 LT. REPAIR PERFORMED PERFORMED BY REPLACING NEW PART IAW SB A310-53-2116 AND SOG-W8-53-00-02, REFER TO DRW A53613845. 2 L 7 2 4F RT A35EU 2007040400004 20070404 00004 NM 2007 4 4 HALA0700149 1 20070402 A 2410 UNKNOWN BOEING 767 767300 1385204 NM IDG UNKNOWN A HALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 13 581HA 28141 ETOPS SIGNIFICANT SYSTEM, IDG OUT TEMP MAINT MSG DISPLAYED. CHECKED PER FIM 24-20-00 FIG 103. NO BITE MSGS. NO OTHER EICAS MSGS. NO FURTHER ACTION REQUIRED. 2 L 7 2 4F RT A1NM 2007040400005 20070404 00005 EU 2007 4 4 07FDEA01091 1 20070322 A 5330 SKIN AIRBUS 310 A310203 3930313 EU FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 409FE 273 AREA 200 FUSELAGE SKIN SURFACE FOUND DENTED, BETWEEN FR 68 AND FR 69 RT AND BETWEEN STR 2 AND STR 3 REPAIRED IAW SRM 53- 10-12 FIG 225. REPAIR INSPECTED PER SRM 53-10-12-2-005-00. INITIAL INSP AT 32.800 FC, REPAIR AT 4400FC REPAIR EVALUAT ED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR". 2 L 7 2 4F RT A35EU 2007040400006 20070404 00006 WP 2007 4 4 07FDEA01092 1 20070322 A 5315 FLOORBEAM DOUG MD10 MD1010F 3022112 WP BS 1841 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 566FE 46989 AFT PIT TOP OF FLOORBEAM CORRODED AT STA 1841 RBL 17 TO 23. REMOVED AND REPLACED FLOORBEAM AGA3874-3, AND AFT ATTACHED ANGLE AGA3874-9 IAW DAC DWG AGA3874 REV B, AND MD/DC10 SRM 51-33-01 PG 1 VOL 11. MD/DC10 RSM 51-35-01 PG 1 VOL 11. 2 L 7 3 4F RT A22WE 2007040400007 20070404 00007 EU 2007 4 4 07FDEA01093 1 20070322 A 5310 F53271776002 BEAM AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 DURING SB: A310-53-2095, FOUND ENLARGED HOLES ON AFT CARGO DOOR ACTUATOR BEAM BETWEEN C61-C62. REPLACEMENT OF EXISTING BEAM (A537-81256-002) BY NEW ONE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007040400010 20070404 00010 NM 2007 4 4 SWAA071626 1 20070329 A 5330 6518420 SKIN BOEING 737 7373H4 1384600 NM BS 304 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT BS 304, WL 257. REPAIRED SKIN PE R ER. 2 L 7 2 4F RT A16WE 2007040400011 20070404 00011 NM 2007 4 4 SWAA071606 1 20070328 A 5330 6518420 SKIN BOEING 737 7373H4 1384600 NM BS 304 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT BS 304, WL 257. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007040400012 20070404 00012 NM 2007 4 4 SWAA071636 1 20070329 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 583 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 583, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007040400015 20070404 00015 NM 2007 4 4 SWAA071619 1 20070329 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM BS 767 S22L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 FUSELAGE SKIN CRACKED AT BS 767, STR 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007040400016 20070404 00016 NM 2007 4 4 SWAA071603 1 20070328 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 924 S23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 924, STR 23L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007040400017 20070404 00017 NM 2007 4 4 SWAA071612 1 20070328 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED SPV CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP SKIN CRACKED AT INBOARD CARRIAGE ARM CUTOUT. REPAIRE D FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007040400018 20070404 00018 NM 2007 4 4 SWAA071614 1 20070329 A 5753 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 1126 27705 DURING SCHEDULED HC2 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP UPPER AFT SURFACE DELAMINATED. REMOVED AND REPLACED A FT FLAP PER MM. 2 L 7 2 4F RT A16WE 2007040400019 20070404 00019 NM 2007 4 4 SWAA071616 1 20070329 A 5311 6546533 FRAME BOEING 737 7373Y0 1384671 NM BS 500 S26R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, STR 26R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007040400023 20070404 00023 2007 4 4 070084 4 20070331 A 3418 9650449002 COMPUTER DOUG DC9 DC983 3022083 WP STALL WARNING MALFUNCTIONED A WX0A H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 WP 19 875GA 53468 FLIGHT 502 PSP/LAS, THE FLIGHT CREW REPORT THAT THE STALL INDICATION FAILURE ANNUNCIATOR ILLUMINATED IN FLIGHT. THERE W AS NO STALL WARNING. PERFORMED QRH PROCEDURE TO DETERMINE SYSTEM 2 HAD FAILED. PULLED C/B Z-23. LAS VEGAS MAINTENANCE REPORT THE INTERROGATION OF THE STALL WARNING COMPUTERS AND BOTH REPORTED AOA VANE FAULT. REMOVED AND REPLACED AOA VAN E PER AMM 34-19-01. NEXT DAY (04-01-2007) FLIGHT 551 RDM/LAS SIF, ANNUNCIATOR REPORTED AGAIN WITH SYSTEM 2 FAULT. LAS VEGAS MAINTENANCE REPORT THE REMOVAL AND REPLACEMENT OF THE NR 2 STALL WARN COMPUTER PER AMM 34-19-02. A SATISFACTORY O PERATIONAL CHECK WAS ACCOMPLISHED. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007040400024 20070404 00024 NM 2007 4 4 AWXA200700452 1 20070311 A 5753 SKIN BOEING 737 7373G7 1384595 NM ZONE 600 DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW BN855 24710 MCN - RIGHT WING OUTBOARD FLAP UPPER SURFACE DELAMINATED, WS 316.45 - WS 326.45. REPAIRED RIGHT WING OUTBOARD FLAP UPPE R SURFACE, WS 316.45 - WS 326.45 IAW B737-300 SRM 51-70-10-2R4 FIGURE 203. 2 L 7 2 4F RT A16WE 2007040400025 20070404 00025 NM 2007 4 4 AWXA200700453 1 20070314 A 5523 65C2638428SP TAB BOEING 737 7373G7 1384595 NM ZONE 300 DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - RIGHT ELEVATOR TRIM TAB DISBONDED, ELEVATOR STATION 59 - 64. REPAIRED RIGHT ELEVATOR TRIM TAB, ELEVATOR STATION 5 9 - 64 IAW B737-300 SRM 51-70-04 FIGURE 10. 2 L 7 2 4F RT A16WE 2007040400026 20070404 00026 NM 2007 4 4 AWXA200700454 1 20070312 A 5340 69353522 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - FOUND CRACKED STRINGER CLIP, BS 727A, S20R. REPLACED STRINGER CLIP, BS 727A, S20R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007040400029 20070404 00029 EU 2007 4 4 AWXA200700457 1 20070328 A 5320 D53480020696 SHEAR WEB AIRBUS 320 A320232 3930326 EU ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 SAL - CRACKED CABIN FLOOR PLATE/SHEAR WEB TRAY, FR 68 - FR 68 + 12", +Y1250. REPLACED CABIN FLOOR PLATE/SHEAR WEB TRAY, FR 68 - FR 68 + 12", +Y1250 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007040400030 20070404 00030 NM 2007 4 4 AWXA200700458 1 20070310 A 5320 694147315 INTERCOSTAL BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - CRACKED INTERCOSTAL, BS 400, S26L. REPLACED INTERCOSTAL, BS 400, S26L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007040400031 20070404 00031 NM 2007 4 4 07FDEA01229 1 20070401 A 5711 ARB74141 SPAR CAP DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LT WING, REAR SPAR LOWER CAP UPPER SURFACE XORS 1050 FOUND WITH CORROSION. [SUP 4-20-07] COMPLIED WITH FEDEX EA 1-5710 -109848. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040400032 20070404 00032 NM 2007 4 4 07FDEA01230 1 20070402 A 5754 SLAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT WING FIXED LEADING EDGE NR 14 SLAT TRACK CUTOUT FOUND CRACKED. 4-18-07, REPAIR CARRIED OUT AS PER SRM 57-10-00 F IGURE 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040400033 20070404 00033 NM 2007 4 4 07FDEA01231 1 20070402 A 5730 SKIN DOUG MD11 MD11F 3023600 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT WING TIP LOWER SURFACE FOUND CORROSION. [SUP 4-19-07] REPAIRED AS PER FEDEX E.A. 1-5710-107829. REPAIR IS CLA SSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040400035 20070404 00035 NM 2007 4 4 SWAA071610 1 20070329 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 294 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007040400036 20070404 00036 NM 2007 4 4 SWAA071625 1 20070329 A 5330 65C381921 SKIN BOEING 737 737317 138447P NM BS 500D S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007040400040 20070404 00040 NM 2007 4 4 SWAA071623 1 20070329 A 5313 BAC1498 STRINGER BOEING 737 7373Y0 1384671 NM BS 502C S25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER 25R CRACKED AT BS 502C. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007040200008 20070402 00008 NM 2007 4 2 07FDEA00981 1 20070318 A 5330 SKIN BOEING 727 727225 1384077 NM BS 1166 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 AFT CARGO FWD OF STA 1166, FROM LBL 6 TO RBL 2, HAS CORROSION ON SKIN. REMOVED CORROSION IAW SRM 51-10-6, UT INSP PER N TM 51-00-00, PT4, MAT THICKNESS BEFORE .125 AFTER REWORK .118, FOUND TO BE WITH IN LIMITS IAW SRM 53-10-1, FIG 1, DETAIL I. TREATED AND PRIMED AREA IAW SRM 51-10-2. PREPPED AND PAINTED AREA IAW MM 51-20-151-7. 2 L 7 3 4F A3WE 2007040200011 20070402 00011 EU 2007 4 2 07FDEA00987 1 20070319 A 5753 VANE AIRBUS 310 A310304 3930339 EU ZONE 600 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 CHAFE MARK ON INBOARD FLAP VANE. REPAIR WAS PERFORMED. 2 L 7 2 4F RT A35EU 2007040200024 20070402 00024 NM 2007 4 2 07FDEA01002 1 20070319 A 5754 652170037 SKIN BOEING 727 727225 1384077 NM ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FOUND REPAIR AT LT WING FIXED LE AT IB END OF NR 3 SLAT. REPAIR REQUIRES EVALUATION FOR MAJOR/MMINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. FOUND EXISTING REPAIR DAMAGED. REMOVED DAMAGED REPAIR FILLER, FABR ICATED NEW FILLER AND INSTALLED. REFERENCE SRM 57-30-4/FIGURE 4/PAGES 6-7. ALSO BLENDED GOUGE AFT OF REPAIR FILLER AND IS WITH IN LIMITS. REFERENCE SRM 57-20-1. CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2007040200025 20070402 00025 NM 2007 4 2 NWAA071163167 1 20070326 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319114 3930350 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 367NB 2028 FOUND EMERGENCY LIGHTS INOP AT SEATS 9 AND 10. CORRECTED BY REPLACING EMERGENCY POWER SUPPLY UNIT 12WL, CHECKS GOOD. 2 L 7 2 4F RT A28NM 2007040200033 20070402 00033 EU 2007 4 2 07FDEA01017 1 20070320 A 5330 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 814FD 534 OLD EXTERNAL REPAIR DOUBLER REPAIR BETWEEN C33/34, P54 LT AND P54 RT THAT INTERFERES WITH P TO F. INSTALLATION DRW R537 B1610. DISCREPANCY PERFORMED BY INSTALLING REDESIGNED REPAIR DOUBLER IAW EA 6-5314-101241 AND IS APPROVED BY RAS/DABR E/7006565/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040200034 20070402 00034 EU 2007 4 2 07FDEA01018 1 20070320 A 5330 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 814FD 534 OLD REPAIR, EXTERNAL DOUBLER BETWEEN C66/67, P33/34 RT AND NOT CONFORM TO REPAIR REF: SRM53-10-12/FIG 203 REPAIR PERFORM ED BY INSTALLING NEW DOUBLER IAW EA 6-5317-101260 AND SRM 53-10-12/FIG 225. 2 L 7 2 4F RT A35EU 2007040200053 20070402 00053 WP 2007 4 2 07FDEA00971 1 20070316 A 5310 DOOR FRAME DOUG DC10 DC1010 3022110 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 FWD PIT BILGE STA 879 LWR SURFACE OF TOP FLANGE OF WEB CORRODED AT LONGERON 43R. ACCOMPLISHED REPAIR PER EAM FUSELAGE F WD LOWER CARGO DOOR JAMB FRAME STA 866 CHORD REPAIR {8-5310-105181}. 2 L 7 3 4F A22WE 2007040200060 20070402 00060 NM 2007 4 2 AALA20070522 1 20070322 A 3350 BATTERY PACK BOEING 757 757231 1384950 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 705TE 28479 DFW - EXTERIOR EMERGENCY SLIDE FLOOD LIGHT AT RIGHT NUMBER FOUR DOOR, RIGHT AND LEFT INTERIOR EXIT SIGN LIGHT ABOVE RIGH T NUMBER FOUR DOOR, EXIT SIGN IN THE AFT GALLEY CEILING, AND THE AISLE BULLNOSE FLOOD LIGHT AT SEAT ROW 30 INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK M736 FOR EXTERIOR EMERGENCY SLIDE FLOOD LIGHT AT RIGHT NUMBER FOUR DOOR, RIGHT AN D LEFT INTERIOR EXIT SIGN LIGHT ABOVE RIGHT NUMBER FOUR DOOR, EXIT SIGN IN THE AFT GALLEY CEILING, AND THE AISLE BULLNOS E FLOOD LIGHT AT SEAT ROW 30. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007040200074 20070402 00074 EU 2007 4 2 07FDEA00424 1 20070209 A 5230 SKIN AIRBUS 310 A310203 3930313 EU CARGO DOOR MISREPAIRED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 409FE 273 PREVIOUS REPAIR FOUND LOCATED ON THE AFT CARGO DOOR INSIDE STRUCTURE LOWER SECTION, FS 3355 BETWEEN FR 62-62A. REPAIR R EQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVA LUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMP IAW EA 6-5230-105668. REPAIR EVALUATED PE R GMM 6-2-100 AND CLASSIFIED MINOR. 2 L 7 2 4F RT A35EU 2007040200083 20070402 00083 NM 2007 4 2 DU4R2007071 1 20070312 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM BS 1681 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 6708D 30480 FOUND CORROSION ON FLOORBEAM UPPER CAP AT BS 1681 LBL 24. CUT OUT CORRODED AREAS. FABRICATED AND INSTALLED REPAIR DOUB LER 26.5 BY 2 FROM 2024-T3 .080 AND 3 FILLERS FROM 2024-T3 .071 IAW B757 SRM 53-60-51 FIG 201, 51-20-01. 2 L 7 2 4F RT A2NM 2007040200084 20070402 00084 NM 2007 4 2 UIEA200700139 1 20070315 A 2701 FLT CONTROLS BOEING 747 7472D7B 1384803 NM BINDING A UIEA O OTHER F FLT CONT AFFECTED CL CLIMB 1 EA 15 522MC 21783 AT T/O WITH FLAP 20 DEGREES THE YOKE WOULD STICK AT ABOUT THE POINT OF 2 UNITS OF RIGHT AILERON TRIM. AFT FLAP WERE AT 10 DEGREES THE YOKE WOULD STICK AT THE SAME POINT, BUT TAKE LESS PRESSURE TO OVERCOME THE PROBLEM, ON APPROACH NO INDICA TION OF STICKING WITH FLAPS UP OR AT NIL FLAPS SETTING DOWN TO 30 DEGREES. VERIFIED YOKE AND AILERONS, NOT BINDING PRIO R TO DEPARTURE WITH FLAPS UP AND FLAPS DOWN IAW MM 27-11-00. 2 L 7 4 4F RT A20WE 2007040200087 20070402 00087 NM 2007 4 2 AWXA200700405 1 20070315 A 5320 655489212 ANGLE BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - FOUND CRACKED ANGLE, BS 336, BETWEEN S22L AND S23L. REPLACED ANGLE, BS 336, BETWEEN S22L AND S23L IAW B737-300 SR M 51-40-02. 2 L 7 2 4F RT A16WE 2007040200119 20070402 00119 EA 2007 4 2 QXEA200700462 1 20070327 A 2840 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA UNKNOWN A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 602QX 10010 DEN - ON TAXI OUT FOR FLIGHT 4327, RECEIVED A "XFLOW" CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENANCE CLEARED THE F AULTS IAW CRJ-700 SERVICE LETTER SL-28-007 REVISION C. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE, NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007040200128 20070402 00128 CE 2007 4 2 03192007650Z 1 20070319 A 2910 AE4700E0075170 HOSE CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP HYD SYSTEM CRACKED E VQMA O OTHER K FLUID LOSS LD LANDING 1 NM 03 650Z 6500108 LT UPPER ACTUATOR LINE WAS FOUND TO HAVE A CRACK IN THE ELBOW, CAUSING A HYDRAULIC FLUID LEAK. MATERIAL IN THE ELBOW OF THE HOSE LOOKS GRAINY AS IS STRESSED WHILE FORMING. 2 L 7 2 4F 4 F A9NM E6WE 2007040200138 20070402 00138 NM 2007 4 2 USAA200703007 1 20070327 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA E ENGINE SHUTDOWN O OTHER IN INSP/MAINT 1 EA 19 525AU 3860 FOUND 3 INCH CRACK AT STA 767 STR 21L SKIN. REPAIRED PER SRM 53-00-01, REPAIR 31, TR 53-60-03A. 2 L 7 2 4F RT A16WE 2007040200143 20070402 00143 NM 2007 4 2 WRLA2007051 1 20070318 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271WA 48518 DURING C-04 CHECK IN TPE, CORROSION FOUND CABIN SEAT TRACK STA Y=460-470, X=-27, Z=-18. INSTALLED SEAT TRACK AND SPLICE PER MD-11 SRM VOL.II 51-33-01 REV.38. 2 L 7 3 4F 4 F RT A22WE E24NE 2007040200154 20070402 00154 NM 2007 4 2 AWXA200700426 1 20070307 A 5313 6545800801 STRINGER BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED STRINGER, BS 298, S10L. REPAIRED STRINGER, BS 298, S10L IAW AWA ER 03-5300-07083-ES3. 2 L 7 2 4F RT A16WE 2007040200176 20070402 00176 EA 2007 4 2 A6WA200740142 1 20070319 A 2910 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 416AW 7603 HYDRAULIC LINE SUPPORT BRACKET (ASSY PN 601R75262-153) CRACKED APPROX .1 INCH LONG IN CEILING RT WHEEL WELL FWD OF TRANS DUCER BRACKET. (K) [SUP 05-09-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R7 5262-153 IAW CRJ 200 SRM 51-40-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007040200178 20070402 00178 EA 2007 4 2 A6WA200740143 1 20070319 A 5320 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 416AW 7603 HYDRAULIC TRANSDUCER HOT CHANNEL (ASSY PN 601R75262-157) CRACKED APPROX 1 INCH LONG IN CEILING RT WHEEL WELL. (K) [SUP 05-09-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R75262-157 IAW BSC STANDARD REPAIR 601R-53-0044E. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007040200181 20070402 00181 WP 2007 4 2 07FDEA01021 1 20070320 A 5320 SUPPORT FITTING DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 FOUND CRACK IN SUPPORT FITTING BELOW MAIN CARGO DOOR FWD ALIGNMENT FITTING, BETWEEN LATCH ROLLERS NR 2 AND NR 3. REMOVE D AND REPLACED LOWER SUPPORT FITTING AND PLATE BETWEEN NR 2 AND NR 3 LATCH ROLLERS IAW DC/MD SRM 51-33-01 VOL II PGE 1, 51-21-01 VOL II PGE 1-19. 2 L 7 3 4F A22WE 2007040200185 20070402 00185 NM 2007 4 2 07FDEA01025 1 20070320 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C UK UNKNOWN 1 SO 25 461FE 22548 EXTERNAL DOUBLER AT STA 392- 408, STR 14L, DOES NOT COMPLY WITH FAA APPROVED DATA. REMOVED REPAIR, FAB`D NEW FILLER DO UBLER MAT 2024-T3, 0.080, BATCH 1228717, IAW SRM 53-30-3. INSTALLED REPAIR FILLER DOUBLER IAW SRM 53-30-3. 2 L 7 3 4F A3WE 2007040200225 20070402 00225 EU 2007 4 2 07FDEA01071 1 20070321 A 5315 FLOORBEAM AIRBUS 310 A310222 3930315 EU FUSELAGE MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 PREVIOUS REPAIR LOCATED ON MAIN CABIN FLOORBEAM FRAME 36 BETWEEN SEAT TRACKS 2 AND 3 RT FWD AND AFT UPPER FLANGE HAS 2 E ACH REPAIR ANGLES THE FWD ANGLE IS 10.25" BY 1 " AND THE AFT ANGLE IS 12.2" BY 1.82" PREVIOUSLY INSTALLED REPAIR LOCATED AT MAIN CABIN FLOORBEAM FRAME 36 BETWEEN SEAT TRACK 2 AND 3 RT WAS DETERMINED NOT TO BE IAW FEDEX EA6-5321-29300. REMO VED EXISTING REPAIR ANGLES AND REPAIRED FLOORBEAM PER FEDEX EA6-5310-107718. 2 L 7 2 4F RT A35EU 2007040200231 20070402 00231 EU 2007 4 2 07FDEA01043 1 20070321 A 5730 SKIN AIRBUS 310 A310324 3930206 EU RT WING CORRODED A FDEA O OTHER O OTHER UK UNKNOWN 1 SO 25 814FD 534 FOUND EXTENSIVE CORROSION ON RT WING BOTTOM FRONT SPAR OVERHANGS. LOOK FOR AFFECTED AREAS IN EA 6-5720-99230. REPAIR P ERFORMED BY BLEND AND/OR CUT OUT AND INSTALLING REPAIR PLATES ALL IAW EA 6-5720-99230, APPROVED BY RAS/BAE/1002584/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040200236 20070402 00236 EU 2007 4 2 07FDEA01049 1 20070321 A 5320 COVER PLATE AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CHAFED A FDEA O OTHER O OTHER UK UNKNOWN 1 SO 25 748FD 633 OLD TOOLING MARK ON COVER PLATE AT DOOR NR 4 RT. REPAIR PERFORMED BY REWORK AND HFEC INSPECTION IAW EA6-5318-106393 AND RAS/DAHAM/4021668/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040300007 20070403 00007 NM 2007 4 3 DHL2007786523 1 20070326 A 5753 STRUCTURE BOEING 727 727214 138407R NM TE FLAPS CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 A/C IN "C" CHECK AT FLIGHTSTAR A/C SERVICES, REF ASTAR NR NR 112916. LT OB FORE FLAP WAS FOUND TO HAVE A DEEP PUNTURE I N THE UPPER SURFACE WBL442. CUT OUT PUNTURE 1" DIA ON LT OB FORE FLAP UPPER SURFACE WBL442 AND APPLIED POTTING COMPOUND . FABRICATED DOUBLER 4" DIA FROM .016 2024T3 PO NR 9004174. BONDED DOUBLER, CLEANED, PRIMED, AND SEALED IAW B727 SRM 5 7-50-2 AND 51-40-22 FIG 3. 2 L 7 3 4F A3WE 2007040300051 20070403 00051 NM 2007 4 3 07FDEA00726 1 20070309 A 5313 A5A7114517 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 CENTER CARGO RT TUNNEL AREA, LONGERON 38R SPLICE AT STA 1531 SUSPECTED CRACKED CENTER CARGO RT TUNNEL AREA, LONGERON 3 8R SPLICE AT STA 1531. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX G MM 6-2-100. 2 L 7 3 4F RT A22WE 2007040300058 20070403 00058 EU 2007 4 3 AWXA200700448 1 20070326 A 5320 D53480020697 SHEAR WEB AIRBUS 320 A320232 3930326 EU ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - CRACKED CABIN FLOOR PLATE/SHEAR WEB TRAY, FR 68 - FR 68 + 12", -Y1250. REPLACED CABIN FLOOR PLATE/SHEAR WEB TRAY, FR 68 - FR 68 + 12", -Y1250 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007040300059 20070403 00059 NM 2007 4 3 AWXA200700449 1 20070305 A 5330 654577810 SKIN BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED FUSELAGE SKIN, BS 957, WL 208, R2 DOOR CUT OUT LOWER FORWARD CORNER. REPAIRED FUSELAGE SKIN, BS 957 , WL 208, R2 DOOR CUT OUT LOWER FORWARD CORNER IAW B737-300 SRM 53-00-01 FIGURE 201. 2 L 7 2 4F RT A16WE 2007040300060 20070403 00060 NM 2007 4 3 AWXA200700450 1 20070309 A 5311 654580761 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - R1 DOOR CUT OUT FORWARD FRAME CRACKED, BS 294, WL 207. REPLACED R1 DOOR CUT OUT FORWARD FRAME, BS 294, WL 207 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007040300061 20070403 00061 NM 2007 4 3 AWXA200700451 1 20070309 A 5311 65458076 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - CRACKED R1 DOOR CUT OUT UPPER STUB FRAME, BS 296.40, RBL 49.34,WL 265. REPLACED R1 DOOR CUT OUT UPPER STUB FRAME, BS 296.40, RBL 49.34,WL 265 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007040300063 20070403 00063 CE 2007 4 3 ACE032707 1 20070325 A 5313 STRINGER BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA BS 250 S14L CORRODED E YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 113AX UC41 LOCATED CORRODED STRINGER NR 14LH AT FS. 250. 2 L 7 2 4T 4 T RT A24CE E4EA 2007040300080 20070403 00080 SO 2007 4 3 SIMA200708608 1 20070326 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 922AE 4867 4867 14500906 LEFT OMEGA BEAM CORRODED AT FRAME 20. REPAIRED OMEGA BEAM IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007040300086 20070403 00086 CE 2007 4 3 DJFA2007035 1 20070322 A 2120 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CABIN ODOR E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 704LX 7500091 TRIP NR 1158377, CREW REPORTED BURNING ODOR IN CABIN AND CABIN PAC SELECTOR SUPPLY READ 200 DEG AND INCREASING. ACM WA S MEL'D. SDR WILL BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007040300098 20070403 00098 NM 2007 4 3 AWXA200700440 1 20070309 A 5320 69434771 CHANNEL BOEING 737 7373G7 1384595 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - CORROSION ON AFT CARGO COMPARTMENT DOOR CUT OUT CHANNEL, BS 787, S25R. REPLACED AFT CARGO COMPARTMENT DOOR CUT O UT CHANNEL, BS 787, S25R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007040300101 20070403 00101 NE 2007 4 3 0331200702 2 20070331 A 7200 ENGINE BOEING 747 747200B NM RROYCE RB211 RB211524D419 54555 NE NR 2 BIRD INGESTION A OZYA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING C E J F.O.D. VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 29 361FC 22442 12617 AT ROTATION NR 2 ENG VIB ANNUNICATOR LIGHT & ENG VIB LIGHT FOR NR 2 ENG ILLUM, ACCOMPANIED BY VIB & ABNORMAL SOUND. NR 2 ENG SECURED IAW CHECKLIST, NO VIB NOTED AFTER SHUTDOWN. FUEL JETTISON, ACFT RETURNED WITHOUT FURTHER INCIDENTS. ON POSTFLIGHT INSPECTION FOUND EVIDENCE OF A BIRDSTRIKE ON NR 2 ENGINE. ACCOMPLISH INSPECTION IAW AMM 5-51-14, & AMM 71-00 -47. BORESCOPE INSPECTION OF IPC, HPC & COMBUSTION SECTION COMPLETED, & FOUND ACCEPTABLE. DAMAGE TO NR 11, & NR 12 FAN ROTOR BLADES NOTED. CLEANED LP COMPRESSOR CASE & VANES OF BIRD RESIDUE, & REPLACED FULL SET OF ROTOR BLADES IAW AMM 72- 31-04. ACCOMPLISH RUN UP TEST & TO POWER ENGINE RUN IAW MM. FINAL INSPECTION, LEAK CHECKS SATISFACTORY, ACFT RTS. 1 L 7 4 4F 4 F RT A20WE E12EU 2007040300104 20070403 00104 CE 2007 4 3 DJFA2007037 1 20070329 A 2435 23080050 STARTER GEN BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE RT ENGINE VIBRATES E DJFA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 EA 23 454LX 376 5 RK327 TRIP NR 1161270 CREW REPORTED SEVERE AIRFRAME VIBRATION COMING FROM THE RT SIDE. DECISION WAS MADE TO DIVERT. MAINTENA NCE DISCOVERED THE RT STARTER GENERATOR AS CAUSE OF THE VIBRATION; POSSIBLE BEARING FAILURE OR WARPED STATOR ASSEMBLY. THE GENERATOR WAS REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007040300112 20070403 00112 NM 2007 4 3 QXEA200700488 1 20070326 A 5551 MOUNT DHAV DHC8 DHC8202 2809007 NM HORIZONTAL STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - RIGHT FORWARD MOUNT/STAND OFF FOR HORIZONTAL STAB HAS LIGHT SCRAPES AND MISSING PAINT. REPAIRED IAW RD8-55-847 AND SRM 51-20-16, 51-20-36, AND 51-20-51. 2 H 7 2 4T RT A13NM 2007040300118 20070403 00118 EA 2007 4 3 QXEA200700496 1 20070330 A 2840 73811812 COMPUTER CNDAIR CL600 CL6002C10 1390015 EA FUEL QTY FAILED A QXEA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 NM 09 611QX 9876 788 10041 DEN - RECEIVED A FUEL CHANNEL 1/2 FAIL CAUTION MESSAGE IN FLIGHT. RETURNED TO THE FIELD. MAINTENANCE REPLACED THE FUEL QUANTITY GAUGING COMPUTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007040300137 20070403 00137 NM 2007 4 3 QXEA200700505 1 20070331 A 5230 DOOR BOMBDR DHC8 DHC8402 1390042 NM CARGO LACK OF LUBE A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 410QX 4053 PDX FLIGHT NR 2497: RAMPERS REPORT THAT FWD BAGGAGE DOOR VERY DIFFICULT TO OPEN AND CLOSE. MAINTENANCE CLEANED AND LUBE D THE EXTERNAL DOOR HANDLE MECHANISM ON THE FWD BAGGAGE DOOR. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007040300142 20070403 00142 EU 2007 4 3 YENA2007019 1 20070322 A 2150 A/C PACK AIRBUS 320 A320232 3930326 EU IAE V2500 V2500A1 NE NR 2 ODOR A YENA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 15 589JB 2215 APRX 1645Z, NO VISIBLE SMOKE (BURNING RUBBER SMELL) DURING APPROACH QRH COMPLIED WITH MID CABIN. EMERGENCY DECLARED. SME LL SUBSIDED UPON EXITING TAXIWAY. EVACUATION WAS DEEMED NOT REQUIRED. PERFORMED TROUBLESHOOTING IAW TSM 24-00-00-810-823 AND TSM 23-39-00-810-801 FOR LTV IFE. FOUND SMELL COMING FROM NR 2 PACK SYS. INSPECTED LTV SYS IAW 23-39-00. NO FAULTS NOTED. ALL AIRCRAFT ELECTRICAL SYS CHECKS NORMALLY PERFORMED NR 2 PACK DECONTAMINATION OF ECS IAW AMM TASK 21-00-00-615- 002, NR 2 PACK CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E311NE 2007040400013 20070404 00013 NM 2007 4 4 SWAA071631 1 20070329 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 583 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 583, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007040400014 20070404 00014 NM 2007 4 4 SWAA071637 1 20070329 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 800 S17L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800, STR 17L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007040400021 20070404 00021 WP 2007 4 4 070083 1 20070329 A 2720 CONTROL VALVE DOUG DC9 DC983 3022083 WP RUDDER LEAKING A WX0A O OTHER K G J FLUID LOSS MULTIPLE FAILURE WARNING INDICATION DE DESCENT 1 WP 19 877GA 53467 FLIGHT 758 PSM/SFB, THE FLIGHT CREW REPORTED THAT THE RIGHT HYDRAULIC SYSTEM PRESSURE AND QUANTITY READINGS DROPPED BELO W THE USEABLE MINIMUMS, PHASE OF FLIGHT NOT REPORTED. ITEM NR 2 ON THE SAME LOG PAGE REPORTS THAT "DURING MANUAL GEAR E XTENSION THE NOSE GEAR WOULD NOT EXTEND. AFTER EXHAUSTING ALL OPTIONS, LANDED W/NOSE GEAR RETRACTED. SUCCESSFUL EVACUA TION FOLLOWED." THE RIGHT HYDRAULIC SYSTEM LEAK WAS DISCOVERED AT THE RUDDER CONTROL VALVE SUPPLY LINE CHECK VALVE CONN ECTION TO THE PIPING. THE CAUSE OF THE LEAK IS UNDER INVESTIGATION BY THE NTSB AND FAA. THE FAILURE WHICH PREVENTED TH E NOSE LANDING GEAR FROM EXTENDING DURING THE ATTEMPTED ALTERNATE GEAR EXTENSION OPERATION IS UNDER INVESTIGATION BY THE 2 L 7 2 4F RT A6WE 2007040400034 20070404 00034 NM 2007 4 4 AWXA200700459 1 20070310 A 5347 654681597 SEAT TRACK BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - CRACKED CABIN SEAT TRACK, BS 841, LBL 24.75. REPLACED CABIN SEAT TRACK, BS 727B - BS 947, LBL 24.75 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007040400037 20070404 00037 NM 2007 4 4 SWAA071617 1 20070329 A 5322 69353656 SHEAR TIE BOEING 737 7373Y0 1384671 NM BS 360 S14R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007040400039 20070404 00039 NM 2007 4 4 SWAA071620 1 20070329 A 5523 6963391 BOLT BOEING 737 7373H4 1384600 NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED MV2 CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED INBOARD PUSHROD END BOLT PE R SWA EA. 2 L 7 2 4F RT A16WE 2007040400041 20070404 00041 2007 4 4 SWAA071618 4 20070329 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007040400043 20070404 00043 NM 2007 4 4 SWAA071654 1 20070331 A 5330 6545776 SKIN BOEING 737 7373Y0 1384671 NM BS 950 S25L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 950, STR 25L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007040400044 20070404 00044 NM 2007 4 4 SWAA071640 1 20070331 A 5311 6545808 FRAME BOEING 737 7373Y0 1384671 NM BS 291 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 291.5, STR 16R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040400050 20070404 00050 NM 2007 4 4 07FDEA01234 1 20070402 A 5313 A5A7114543 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 CTR CARGO COMPARTMENT LT TUNNEL AREA L38L SPLICE AT STA 5-123 FOUND CRACKED. [SUP 4-20-07] R & R AS PER SRM 51-33-01 V OL II & DOUGLAS DRAWING A5A7114. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040400053 20070404 00053 NM 2007 4 4 07FDEA01237 1 20070402 A 5710 ARB11281 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LT WING, LEADING EDGE SLAT NR 15 TRACK CUTOUT FOUND CRACK. [SUP 4-20-07] REPAIR CARRIED OUT AS PER SRM 57-10- 00 FIG 21 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040400054 20070404 00054 NM 2007 4 4 07FDEA01238 1 20070402 A 5710 ARB11252 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RT WING, LEADING EDGE NR 12 SLAT TRACK CUT OUT FOUND CRACKED. [SUP 4-20-07] REPAIR CARRIED OUT AS PER SRM 57-10- 00 FI G. 21 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040400055 20070404 00055 NM 2007 4 4 07FDEA01239 1 20070402 A 5313 A5A7114531 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 CTR CARGO COMPARTMENT : RT TUNNEL AREA LONGERON 38R SPLICE AT STA 5-123 SUSPECT CRACKED. [SUP 4-20-07] REMOVED AND R EPLACED AS PER SRM 51-33-01 VOL.II AND DOUGLAS DRAWING A5A7114. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040400057 20070404 00057 EU 2007 4 4 07FDEA01241 1 20070402 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 1 CRACK EXIST IN FLOORBEAM VERTICAL STIFFENER AT FR 36 BETWEEN SEAT TRACK L4 AND L5, MEASURING 0.450" P/N 537B1041000 A3 10-200 AMM 53-10-15-6. REMOVED 1 CRACK IN FLOORBEAM VERTICAL STIFFENER AT FRAME 36 BETWEEN SEAT TRACK L4 AND L5 IAW A31 0-200 SRM 53-10-15 FIG 201. FABRICATED AND INSTALLED REPAIR IAW A310-200 SRM 53-10-15 PG 201. 2 L 7 2 4F RT A35EU 2007040400059 20070404 00059 NM 2007 4 4 07FDEA01243 1 20070402 A 5755 SKIN BOEING 727 727225 1384077 NM NR 13 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 RT WING NR 13 SPOILER T/E IS SPLIT NR 13 SPOILER REPAIRED ON WO NR 11841-6000-0005 REFERENCE SRM 51-40-20. INSTALLED NR 13 SPOILER REF MM 27-61-001-4 PG 2-3 STEP 5, TORQUE WRENCH AAR 20026 DATE 8-23-07. CTR BOLT 285 IN LB. OUTBD HINGE BO LT, 130 IN LB TORQUE WRENCH 23442 DATE 11-16-07. FLUKE KIT AAR 18259 DATE 10-5-06. FUNCTIONAL CHECK WILL BE PERFORMED ON WC 70C006-00. 2 L 7 3 4F A3WE 2007040400060 20070404 00060 NM 2007 4 4 07FDEA01244 1 20070402 A 5330 651753033 SKIN BOEING 727 727225 1384077 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 463FE 22551 FOUND EXTERNAL FUSELAGE REPAIR AT APPROX STA 1223, STR 25R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. FOUND REPAIR DID NOT CONFORM TO SRM 53-30-3 FIG 3. REMOVED EXT ERNAL DOUBLER FROM A/C REF SRM 51-30-2. MFG NEW REPAIR DOUBLER AND INSTALLED REF SRM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 2007040400064 20070404 00064 NM 2007 4 4 SWAA071615 1 20070329 A 5322 6546546 SHEAR TIE BOEING 737 7373Y0 1384671 NM BS 727E S14L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 727E, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007040400065 20070404 00065 NM 2007 4 4 SWAA071633 1 20070329 A 5311 6546549 FRAME BOEING 737 7373H4 1384600 NM BS 767 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040400066 20070404 00066 NM 2007 4 4 SWAA071632 1 20070329 A 5311 6546551 FRAME BOEING 737 7373H4 1384600 NM BS 807 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040400067 20070404 00067 NM 2007 4 4 SWAA071635 1 20070329 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040400068 20070404 00068 NM 2007 4 4 SWAA071622 1 20070329 A 5311 6546569 FRAME BOEING 737 7373H4 1384600 NM BS 1040 S25L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 1040, STR 25L. REPAIRED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2007040400069 20070404 00069 2007 4 4 SWAA071604 4 20070328 A 2565 65C16820 HOOK BOEING 737 7377H4 1384404 NM R1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 286WN 32471 R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2007040400070 20070404 00070 NM 2007 4 4 SWAA071634 1 20070329 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM BS 500C S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040400071 20070404 00071 NM 2007 4 4 SWAA071611 1 20070328 A 5754 SKIN BOEING 737 7373H4 1384600 NM NR 4 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED SPV CHECK, FOUND RIGHT WING NR 4 L/E SLAT SKIN CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007040400072 20070404 00072 NM 2007 4 4 SWAA071609 1 20070328 A 5754 SKIN BOEING 737 7373H4 1384600 NM NR 6 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED SPV CHECK, FOUND RIGHT WING NR 6 L/E SLAT SKIN CRACKED AT INBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007040400075 20070404 00075 NM 2007 4 4 SWAA071628 1 20070329 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 706 S2R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007040400076 20070404 00076 NM 2007 4 4 SWAA071629 1 20070329 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 706 S2L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007040400077 20070404 00077 NM 2007 4 4 SWAA071630 1 20070329 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 663 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007040400079 20070404 00079 NM 2007 4 4 07FDEA01084 1 20070322 A 5320 65348932 FLOOR SUPPORT BOEING 727 727225 1384077 NM BS 740-760 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 CABIN FLOOR SUPPORT WORN AT FWD END FROM CONTACT WITH SPACER BLOCK UNDER SEAT TRACK AT BS 744, RBL 63. REPLACED CABIN F LOOR SUPPORT AT STA 740-760 RBL 63 REF SRM 51-30-2. 2 L 7 3 4F A3WE 2007040400080 20070404 00080 EU 2007 4 4 07FDEA01085 1 20070322 A 5730 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CORROSION ON LOWER SKIN PANEL NR 2 AND REINFORCING STRUCTURE OF THE RT WING INBOARD RIBS 1-3. REPAIRED BY BLENDING OUT AND TRIMMING OUT EXFOLIATION CORROSION IAW EA 6-5720-99216, APPROVED BY RAS/BAE/1002613/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040400081 20070404 00081 EU 2007 4 4 07FDEA01086 1 20070322 A 5730 SKIN AIRBUS 310 A310324 3930206 EU ZONE 500 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CORROSION ON LOWER SKIN PANEL NR 2 AND REINFORCING STRUCTURE OF THE LT WING INBOARD RIB 1-3. REPAIRED BY BLENDING OUT A ND TRIMMING OUT EXFOLIATION CORROSION IAW EA 6-5720-99216, APPROVED BY RAS/BAE/1002613/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040400082 20070404 00082 EU 2007 4 4 07FDEA01088 1 20070322 A 5330 A53989510214 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 300 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 THE UPPER SKIN PANEL BETWEEN C103/104 IN AREA OF 317AL CUTOUT WAS CRACKED. REPAIR REMOVED BY REPLACED STRUCTURE. 2 L 7 2 4F RT A35EU 2007040400083 20070404 00083 EU 2007 4 4 07FDEA01089 1 20070322 A 5350 DOUBLER AIRBUS 310 A310324 3930206 EU TAIL CONE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 SEVERAL AREAS OF CORROSION ON C95, ON INTERNAL DOUBLER BETWEEN C94-C95, P14-P16 LT AND ON EXTERNAL SKIN BETWEEN C95-C96, P15 LT ON FUSELAGE TAIL CONE, LISTED IN DR 0534-01-16-0200. REPAIR PERFORMED BY BLEND OUT, REPLACEMENT, CUT OUT WITH E XTERNAL AND INTERNAL DOUBLERS IAW EA 6-5319-99217, APPROVED BY RAS/DAHAM/4020768/2006 ISSUE "A", RAS/DAHAM/4020762/2006 ISSUE "A" AND RAS/DAHAM/4020742/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040400085 20070404 00085 NM 2007 4 4 HALA0700145 1 20070330 A 2613 UNKNOWN BOEING 767 767300 1385204 NM RT ENGINE UNKNOWN A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 583HA 25531 EICAS MESSAGE R ENG OH LP1 DISPLAY. OK FOR SERVICE PER FIM 26-11-00. SECURITY CONDITION GOOD. 2 L 7 2 4F RT A1NM 2007040400087 20070404 00087 EU 2007 4 4 2007UALA00875 1 20070323 A 3397 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 438UA 678 CIDS TEST FAULTS BPSU BATTERY AFT LT. CONNECTOR DIRTY. CLEANED CONNECTION FOR BATTERY POWER SUPPLY UNIT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007040400088 20070404 00088 EU 2007 4 4 2007UALA00876 1 20070325 A 3397 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 446UA 834 INVESTIGATING SMC 003 FAULT. FOUND BOTH THE LEFT AND RIGHT OVERWING EMERGENCY EXIT EPSU UNIT CONNECTOR DISCONNECTED. [ SUP 06-01-07] ALL EMERGENCY POWER SUPPLY UNITS WERE CHANGED DURING A REGULARLY SCHEDULED HMV VISIT 2 WEEKS PRIOR. STATI ON PERFORMING HMV DID NOT PROPERLY CONNECT EPSUS LOCATED AT THE OVERWING EMERGENCY EXITS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007040400092 20070404 00092 NM 2007 4 4 SWAA071665 1 20070331 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM BS 360 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040400093 20070404 00093 NM 2007 4 4 SWAA071666 1 20070331 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM BS 500B S19L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 19L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040400094 20070404 00094 NM 2007 4 4 SWAA071660 1 20070331 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 680 S6R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 680, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007040400096 20070404 00096 NM 2007 4 4 SWAA071656 1 20070331 A 5313 BAC1498 STRINGER BOEING 737 7373Y0 1384671 NM BS 510 S23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER 23L CRACKED AT BS 510. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007040400099 20070404 00099 2007 4 4 SWAA071646 4 20070331 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007040400100 20070404 00100 NM 2007 4 4 SWAA071653 1 20070331 A 3350 MS155721 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007040400106 20070404 00106 NM 2007 4 4 SWAA071649 1 20070331 A 2121 215201 FAN BOEING 737 7377H4 1384404 NM E&E BAY FAILED A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 794SW 30605 DECLARED EMERGENCY, CREW REPORTED STRONG ELECTRICAL ODOR IN CABIN. INSPECTED AIRCRAFT, FOUND GASPER FAN HAD FAILED. RE MOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2007040400108 20070404 00108 NM 2007 4 4 SWAA071642 1 20070331 A 3350 30043233 LIGHT BOEING 737 7373H4 1384600 NM FUSELAGE DIRTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED 14Y CHECK, FOUND LEFT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. CLEANED LIGHT SOCKET PER MM. 2 L 7 2 4F RT A16WE 2007040400111 20070404 00111 NM 2007 4 4 SWAA071641 1 20070331 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 500B S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007040400112 20070404 00112 NM 2007 4 4 SWAA071639 1 20070330 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 970 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007040400113 20070404 00113 NM 2007 4 4 SWAA071655 1 20070331 A 5330 6545776 SKIN BOEING 737 7373Y0 1384671 NM BS 967 S25L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 967, STR 25L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007040400114 20070404 00114 NM 2007 4 4 DHL2007786 1 20070320 A 5322 SHEAR TIE BOEING 727 727214 138407R NM BS 1148 S28L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 AFT CARGO COMPARTMENT AT BS 1148 AND STR 28L, SHEAR TIE HAS CORROSION. CUT OUT DAMAGED AREA AT AFT CARGO COMPARTMENT SH EAR TIE, DIMENSION 4.50 BY 1.75 IAW B727 SRM 53-10-4, FIG 13. FABRICATED SHEAR TIE REPAIR FROM, FILLER 7075T6, .063, 1. 1 BY 1 BY 4.75, DOUBLER FROM 7075T6, .071, 3.10 BY 5.70 IAW B727 SRM 53-10-4, FIG 13. TREATED ALODINE AND PRIMED IAW B 727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007040400121 20070404 00121 NM 2007 4 4 2007UALA00889 1 20070325 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 700 S26L PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 508UA 24744 FUSELAGE SKIN HAS PUNCTURE AT BS 700, STR 26L. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SKIN. FABRICATED & INSTALLE D DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007040400125 20070404 00125 NM 2007 4 4 2007UALA00893 1 20070326 A 5322 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 143 S24-30R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 662UA 27159 WEB AND SHEAR TIE DAMAGE TO CIRCUMFERENTIAL AT STA 143.5 BETWEEN STR 24R & 30R. MAJOR REPAIR ACCOMPLISHED: REPLACED DA MAGED FRAME & CHORD ANGLE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007040400126 20070404 00126 NM 2007 4 4 2007UALA00894 1 20070324 A 2781 SENSOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 4 SLAT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 676UA 30028 RTFL DUE TO LEADING EDGE SLAT DISAGREE & LEADING EDGE SLAT ASSY EICAS MSG. [SUP 4-20-07] REPLACED NR 4 SLAT INBOARD S ENSOR DUE TO FAULT ON PSEU BOX. RAN FLAPS, SLATS NO EICAS MESSAGES NOTED. OP CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007040400127 20070404 00127 NM 2007 4 4 2007UALA00895 1 20070326 A 3397 WIRE HARNESS BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 776UA 26937 SEAT 25G EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. EEL FEEDER CABLE HAD FAULTY CONNECTION. REPAIRED HARNESS PER GNMM 2- 0-15-1. TESTED OK 2 L 7 2 4F 4 F RT T0001SE E46NE 2007040400130 20070404 00130 NM 2007 4 4 2007UALA00944 1 20070329 A 3350 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 810UA 843 EMERGENCY LIGHTS BATTERIES DUE CAPACITY TEST. [SUP 4-17-07] REPLACED EPSU BATTERIES. 2 L 7 2 4F 4 F RT A28NM E40NE 2007040400132 20070404 00132 NM 2007 4 4 2007UALA00946 1 20070329 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 52 FWD INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 EMERGENCY LIGHT ROW 52 FWD INOPERATIVE. RELAMPED ROW 5E EMERGENCY LIGHT. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007040400134 20070404 00134 NM 2007 4 4 2007UALA00948 1 20070330 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 EMERGENCY LIGHT BETWEEN MID LAV INOPERATIVE. RELAMPED EMERGENCY LIGHT, OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007040400138 20070404 00138 NM 2007 4 4 2007UALA00952 1 20070329 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SEAT 2F DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 209UA 30215 SEAT 2F EVACUATION LIGHT IS DAMAGED. REPAIRED LIGHT. OP CHECKS OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007040400140 20070404 00140 NM 2007 4 4 QXEA200700507 1 20070402 A 3150 LIMIT SWITCH DHAV DHC8 DHC8202 2809007 NM WARNING HORN MALFUNCTIONED A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 09 367PH 511 SEA FLIGHT NR 2236, WHEN TAKEOFF POWER APPLIED, TAKEOFF WARNING HORN SOUNDED. TAKEOFF ABORTED AT LESS THAN 60 KTS WITH ELEVATOR TRIM, FLAPS, CONDITION LEVERS, PARK BRAKE AND ECU CONFIGURED FOR TAKEOFF. TAKEOFF WARNING HORN SOUNDED AGAIN W HEN CHECKED WITH REJECTED CHECKLIST. MAINTENANCE REPLACED TAKE-OFF WARNING HORN LIMIT SWITCHES 3151-S3 AND 5131-S4. CO MPLIED WITH THE CONDITION LEVER LIMIT SWITCH RIGGING TEST. PERFORMED OPERATIONAL TEST OF THE TAKEOFF WARNING HORN IAW D 8-200 AMM TASK 31-51-01-720-801. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007040400141 20070404 00141 NM 2007 4 4 QXEA200700506 1 20070402 A 2150 78279018 ACM DHAV DHC8 DHC8202 2809007 NM ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 368PH 7677 512 MFR FLIGHT NR 2125 - UPON LEVEL OFF AT FL190, NOTICED UNUSUAL ODOR ACCOMPANIED BY AIRCRAFT NOT PRESSURIZING PROPERLY. C ABIN CONTINUED TO CLIMB AND CABIN ALTITUDE APPROACHED 8000. MAINTENANCE REPLACED AIR CYCLE MACHINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007040400143 20070404 00143 NM 2007 4 4 DHL2007786524 1 20070327 A 5753 SKIN BOEING 727 727214 138407R NM LT WING FLAP DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 A/C IN "C" CHECK AT FLIGHTSTAR A/C SERVICES, REF ASTAR NR 112921, LT WING OB FORE FLAP ASSY HAS 1 DENT UPPER SKIN. CUT OUT DENT 1" DIA ON LT OB FORE FLAP UPPER SURFACE AND APPLIED POTTING COMPOUND. FABRICATED FILLER 4" DIA FROM .016 2024T 3 PO NR 9004174. BONDED DOUBLER, CLEANED, PRIMED, AND SEALED IAW B727 SRM 57-50-2 AND 51-40-22 FIG 3. 2 L 7 3 4F A3WE 2007040400144 20070404 00144 NM 2007 4 4 DHL2007786527 1 20070315 A 5751 SKIN BOEING 727 727214 138407R NM AILERON TAB DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT ASTAR052902 21692 LEFT OUTBD AILERON TAB WBL 535 AND 567, T/E IS DEBONDED TWO PLACES. REMOVED LEFT OUTBD AILERON TAB IAW B727 M/M 27-10-4 1 AND WEIGH BEFORE REPAIR IS 3.9 LBS IAW B727 SRM 51-80-06, FIG 2. REMOVED DELAMINATION AREA 38.5" BY 5", CLEANED AND P REPPED REPAIR AREA IAW B727 SRM 51-40-20, PARA 7, FIG 3/7 AND 51-40-24, FIG 3. FABRICATED SKIN FROM 2024T3, 38.5" BY 5' BY .010 AND DOUBLER FROM 2024T3, 8" BY 5' BY .010. ANODIZED, PRIMED AND APPLIED ADHESIVE FILM IAW B727 SRM 51-40-20, P ARA 8,14,15,18 AND 57-50-2, FIG 8. INSTALLED DOUBLER AND SKIN, CURED REPAIR AREA IAW B727 SRM 51-40-20, PARA 20. FINIS HED REPAIR AREA IAW B727 SRM 51-40-20, PARA 22 AND 51-40-24, FIG 3. REWEIGH AFTER REPAIR 3.76 LBS, REBALANCE NOT REQUIR 2 L 7 3 4F A3WE 2007040400145 20070404 00145 NM 2007 4 4 DHL2007786526 1 20070315 A 5751 SKIN BOEING 727 727214 138407R NM AILERON DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT BN2511 21692 LEFT INBD AILERON OUTBD END LOWER SURFACE IS DELAMINATED, LT STAB STA 60.21. CUTOUT DELAMINATED AREA ON LT IB AILERON T AB LOWER SURFACE 4" BY 6". FABRICATED FILLER 4" BY 6" AND DOUBLER 5 1/2" BY 7" FROM .010" 2024T3 PO NR 9003621 IAW B727 SRM 57-50-2. BONDED REPAIR PARTS, CLEANED, PRIMED, AND SEALED IAW B727 SRM 51-40-20. TAB WEIGHT AFTER REPAIR 5.48 LBS WITHIN LIMITS IAW B727 SRM 51-80. REMOVED AND REINSTALLED LT IB AILERON TAB IAW B727 MM 27-10-11, OPS CHECK GOOD IAW B 727MM 27-10-11. 2 L 7 3 4F A3WE 2007040400146 20070404 00146 CE 2007 4 4 33107N128CS1 1 20070331 A 7830 ATTENUATOR CESSNA 525 525 2076601 CE THRUST REVERSER MALFUNCTIONED E Z5FA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 NE 03 128CS 5250361 AFTER ROTATION MASTER CAUTION, HYD PRESS ON AND ATTENUATOR UNLOCKED RT ILLUMINATED. THE CREW SELECTED STOW WITH NO EFFE CT AND THE ATTENUATOR COULD BE HEARD OPENING AND CLOSING IN FLIGHT. CREW NOTIFIED TOWER THEY HAD AN EMERGENCY AND REQUE STED RETURN TO ROCHESTER AIRPORT. AIRCRAFT LANDED UNEVENTFUL AND IS CURRENTLY BEING CHECKED BY LOCAL MAINTENANCE VENDOR . THRUST ATTENUATORS MEL'D AND AIRCRAFT RELOCATED TO REPAIR FACILITY. 1 L 7 2 4F RT A1WI 2007040400147 20070404 00147 NM 2007 4 4 2007UALA00901 1 20070326 A 5312 PRESSURE PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1681 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 AFT PRESSURE DECK BS 1681.80 AT RBL 40 IS DAMAGED. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED DOUBLER/FILLER RE PAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007040400148 20070404 00148 NM 2007 4 4 2007UALA00902 1 20070326 A 5210 DOOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE R1 DOOR OPEN A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 669UA 30025 RTFL DUE TO DOOR 1R PRESSURE INDICATION. [SUP 4-24-07] ON ARRIVAL FOUND DOOR OPEN APPROX 6 IN & EXTERIOR HANDLE FULLY DEPLOYED. ACCOMPLISHED DOOR OP CHECK. ARMED AND DISARMED PER 52-11-00-0601. ALL OPERATIONS NORMAL. SUSPECT DOOR WAS N OT CLOSED AND ARMED PROPERLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007040400149 20070404 00149 NM 2007 4 4 07FDEA01099 1 20070322 A 5313 BAC1498132 STRINGER BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 MAIN CABIN FS 360 AT STR 7L HAS A MIS DRILLED HOLE AT END OF STRINGER. REMOVED DAMAGE SECTION OF STRINGER 7L. FABRICAT ED AND INSTALLED STRINGER REPAIR. REINSTALLED ITEMS THAT WERE REMOVED IAW SRM 53-10-3 PG 3-4, FIG 1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2007040400150 20070404 00150 EU 2007 4 4 07FDEA00999 1 20070319 A 5730 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 DAMAGED A FDEA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 25 748FD 633 PYLON SUPPORT BRACKET AND BOTTOM WING SKIN (LT WING), ELONGATED HOLES REPAIR WAS PERFORMED IAW DRAWING R571-50532 REV A , APPROVED BY EA 6-5720-106407 AND RAS/BAE/1004134/2007 ISS A. 2 L 7 2 4F RT A35EU 2007040400151 20070404 00151 EU 2007 4 4 MALA070045 1 20070321 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 296-305 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 408XJ 340B408 DOUBLER ON SEAT TRACK, AT LBL 18.3 AND STA 296 TO 305 WAS CORRODED OUT OF LIMITS. REMOVED EXISTING REPAIR DOUBLER AND I NSTALLED NEW DOUBLER IAW MESABA EOS 53342, REF: EAMS WORK ORDER 215882 TASK 1521. 2 L 7 2 4T RT A52EU 2007040400152 20070404 00152 2007 4 4 2007UALA00903 4 20070326 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 2L MISLOCATED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 588UA 26717 DOOR 2L SLIDE PACK LANYARD NOT VISIBLE. [06-14-07] FOUND D-RING STUCK UNDER SLIDE PACK. REPLACED LANYARD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007040400153 20070404 00153 NM 2007 4 4 2007UALA00904 1 20070326 A 3350 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 844UA 1581 EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 8, 9 AND 10. [SUP 4-17-07] REPLACED PSEU AND BATTERY ON RT SIDE AT SEATS 9 A ND 10. OPS CKD EMERGENCY LITE SYSTEM. CKD OK AND REPLACED EMERGENCY LIGHT CABLE AT SEAT 8 ABC LIGHT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007040400154 20070404 00154 NM 2007 4 4 2007UALA00917 1 20070328 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C 13802 EU BS 727B S25-26R DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 AFT CARGO COMPARTMENT FRAME DENTED IN FWD RADIUS AT BS 727B BETWEEN STR S25R & STR S26R. *S/D* MAJOR REPAIR ACCOMPLISH ED. FABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007040400155 20070404 00155 NM 2007 4 4 2007UALA00918 1 20070328 A 5540 BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RUDDER INTERFERENCE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 364UA 24533 VERTICAL STAB RIGHT TRAILING EDGE BEAM EXCESSIVE MATERIAL REMOVED FROM BEAM FOR RUDDER PCU CLEARANCE. MAJOR REPAIR ACCO MPLISHED: FABRICATED & INSTALLED REPAIR STRAP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007040400156 20070404 00156 NM 2007 4 4 2007UALA00919 1 20070328 A 5313 STRINGER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 294-303 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 364UA 24533 BS 294.5 TO 303.9 STRINGER S12L HAS A 4 INCH CRACK. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE & ACCOMPLISHED NDT FOR C RACKS. CRACK FOUND IN BEARSTRAP AT 1EA FASTENER HOLE. REMOVED DAMAGE FROM BEAR STRAP THROUGH STRINGER. ACCMP'D STRING ER CHANNEL REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007040500001 20070405 00001 EU 2007 4 5 07FDEA00984 1 20070318 A 2913 3508806 PUMP AIRBUS 300 A300F4605R 3930327 EU HYD SYSTEM UNKNOWN A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 663FE 15002 300 766 UPON RAISING LANDING GEAR AFTER TAKEOFF FROM MEM, GEAR STAYED DOWN WITH AMBER DOOR LIGHTS & GOT ECAM INDICATION OF COM PLETE GREEN SYSTEM FLUID LOSS. NO NOSE WHEEL STERRING ON ROLLOUT. REMOVED AND REPLACED THE NR 2 ENGINE GREEN SYSTEM HY DRAULIC PUMP PER A300-600 MM 29-11-32-4-02, OPS AND LEAK CHECK GOOD. SERVICED THE GREEN SYSTEM HYDRAULIC PER A300-600 M M 12-12-00. 2 L 7 2 4F RT A35EU 2007040500002 20070405 00002 NM 2007 4 5 UPS07M49529 1 20070205 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM BS 1541 S38L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C CTR CARGO STA 1541 CONFIG LONGERON 38L SKIN CORROSION AS MARKED. ATTACHMENT PARTS & INNER FASTENERS R EMOVED FOR ACCESS TO EXECUTE REPAIR WORK ON 38L LONGERON PER SRM 51-31-01V2 R38. CORROSION DOUBLER MAT TRIMMED PER SRM 51-21-01 V2 R38. REPAIR FILLER & DOUBLER FAB PER EN1084-07 & DOUBLER FASTENERS HOLE PICKED UP PER SRM 51-31-01 V1 R38. REPAIR PARTS REINSTALLED PER EN1087-07 & SRM 51-31-01 V2 R38. 2 L 7 3 4F RT A22WE 2007040500003 20070405 00003 NM 2007 4 5 SWAA071693 1 20070402 A 5220 507978 DOOR BOEING 737 7373Y0 1384671 NM EMERGENCY EXIT OUT OF ADJUST A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED 20Y CHECK, RIGHT EMERGENCY EXIT DOOR RELEASE HANDLE FAILED TEST. ADJUSTED EMERGENCY EXIT DOOR PER MM. 2 L 7 2 4F RT A16WE 2007040500004 20070405 00004 2007 4 5 SWAA071698 4 20070403 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 248WN 32509 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007040500005 20070405 00005 NM 2007 4 5 SWAA071686 1 20070402 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 665 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 665, BL 0. REPAIRED BEAM PER ER. 2 L 7 2 4F RT A16WE 2007040500006 20070405 00006 NM 2007 4 5 SWAA071691 1 20070402 A 5330 6545765 SKIN BOEING 737 7373Y0 1384671 NM BS 518 S13L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518, STR 13L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007040500007 20070405 00007 NM 2007 4 5 SWAA071690 1 20070402 A 5330 6545765 SKIN BOEING 737 7373Y0 1384671 NM BS 502D S12L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 502D, STR 12L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007040500008 20070405 00008 NM 2007 4 5 SWAA071702 1 20070403 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 772 S14L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 772, STR 14L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007040500009 20070405 00009 NM 2007 4 5 SWAA071692 1 20070402 A 5330 6545768 SKIN BOEING 737 7373Y0 1384671 NM BS 394 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 394, LBL 2. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2007040500010 20070405 00010 EA 2007 4 5 TRAX200700427 1 20070317 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 AFT PRESSURE BULKHEAD FS 621 IS CRACKED AT LINTEL ATTACHMENT FITTING. 2 L 7 2 4F RT A21EA 2007040500011 20070405 00011 EA 2007 4 5 TRAX200700428 1 20070317 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 837AS 7271 RIGHT FS 484 RBL 27 ANGLE CRACKED. 2 L 7 2 4F RT A21EA 2007040500012 20070405 00012 EA 2007 4 5 TRAX200700429 1 20070325 A 2741 TRIM SYSTEM CNDAIR CL600 CL6002B19 1900309 EA AUTO TRIM FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 854AS 7382 TOTAL STAB TRIM AND MACH TRIM FAILURE ON APPROACH TO ATL WOULD NOT RE-ENGAGE. AUTOPILOT PITCH TRIM NU MSG. EMERGENCY L ANDING INTO ATL. 2 L 7 2 4F RT A21EA 2007040500013 20070405 00013 EA 2007 4 5 TRAX200700430 1 20070325 A 2913 PUMP CNDAIR CL600 CL6002B19 1900309 EA NR 2 HYD FAILED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 839AS 7284 NR 2 HYD ENGINE PUMP FAILED ON CLIMBOUT OF ATL, LOST NR 2 QUANTITY. A/C RETURNED TO ATL AFTER T/O. EMERGENCY EQUIPMENT AS PRECAUTION. FLTS 4178, 4654, 4217, 4744 CX. 2 L 7 2 4F RT A21EA 2007040500014 20070405 00014 EU 2007 4 5 07FDEA01096 1 20070322 A 5347 A5381310820000 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU BS 2506-2612 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 669FE 774 MAIN CABIN SEAT TRACK CORRODED FROM FRAME 38.2 TO 40 RBL 77 REMOVED AND REPLACED SEAT TRACK ASSY IAW A300-600 SRM 51-40- 21 PARA 6 AND A300-600 SRM 41-40-21 PARA 7, MINOR REPAIR PO 565247.1. 2 L 7 2 4F RT A35EU 2007040500015 20070405 00015 EU 2007 4 5 07FDEA01098 1 20070322 A 5730 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 FOUND CORROSION ON RT WING TOP SKIN IN AREA OF RIB 4/5 NEAR PICK UP FITTING. CORROSION REMOVED BY BLEND OUT AND INSTALL ATION OF PACKING WASHERS FOR FLAT SEATING OF LOCALIZED SPOTFACING OF OVERWING BRACKET HOLES IAW EA 6-5720-99218, APPROVE D BY RAS/BAE/1002737/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040500016 20070405 00016 EA 2007 4 5 SWIA200718064 1 20070310 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 765SK 10231 PAX DOOR AFT WEB, STEP NR 2 AND NR 3 CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS AS PER REO 6 70-52-11-104 REV B. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007040500017 20070405 00017 EA 2007 4 5 SWIA200718065 1 20070310 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 765SK 10231 PAX DOOR FWD WEB CRACKED AT TWO LOCATIONS STEP NR 2 BASE AND NR 3 STEP, FROM, TOP DOOR OPEN, DISCOVERED DURING C-CHECK I NSPECTION. INSTALLED REPAIR PARTS AS PER REO 670-52-11-104 REV B. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007040200124 20070402 00124 NM 2007 4 2 2007UALA00938 1 20070329 A 3040 THERMAL SWITCH BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU WINDSHIELD FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 309UA 23670 LIGHT BURNING ODOR FROM COCKPIT WINDOW L5, WINDOW FELT HOT. REPLACED WINDOW & THERMAL SWITCH. 2 L 7 2 4F 4 F RT A16WE E21EU 2007040200179 20070402 00179 EA 2007 4 2 A6WA200740145 1 20070316 A 2910 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 415AW 7593 HYDRAULIC LINE SUPPORT BRACKET (ASSY PN 601R75262-153) JUST FWD OF TRANSDUCER IN CEILING OF RT MLG WHEEL WELL CRACKED AP ROX .1 INCH LONG. (K) [SUP 06-05-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601 R75262-153 IAW CRJ SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007040200182 20070402 00182 NM 2007 4 2 07FDEA01022 1 20070320 A 5522 657278415 SKIN BOEING 727 727225 1384077 NM ELEVATOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 LT HORIZONTAL STAB, ELEVATOR LWR SURFACE SKIN HAS CRACKS COMING OUT OF FWD AND AFT EDGES OF FASTENER HOLES, 38.5" OB OF INBD EDGE AND 13.5" FWD OF AFT EDGE. REPAIRED BONDED SKIN REF SRM 51-40-20 PG 59, 60, COOK TICKET ATTACHED TO N00129. PRIMED/PAINTED EXTERIOR, PROTECTIVE FINISH, REF MM 51-20-151-7. 2 L 7 3 4F A3WE 2007040200187 20070402 00187 WP 2007 4 2 07FDEA01028 1 20070320 A 5415 BOLT DOUG MD10 MD1010F 3022112 WP NR 1 PYLON SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 396FE 46630 NR 1 ENG PYLON FWD LOWER ATTACH FITTING/TOMBSTONE HAS 2 BOLTS PULLED, OUT/SHEARED AT 3:00 O`CLOCK AND 9:00 O`CLOCK POSTI ON. REMOVED LOWER PLUG PLATE AND 6EA. BOLTS IN REFERANCE TO MM 54-00-01-4. INSPECTED ALL 6EA BOLT HOLES AND FOUND NO CORROSION. INSTALLED 6 EA. NEW BOLTS, PLUG PLATE AND RETAINER IAW MM 54-00-01-4. 2 L 7 3 4F RT A22WE 2007040200195 20070402 00195 EU 2007 4 2 07FDEA01036 1 20070321 A 5330 SKIN AIRBUS 310 A310304 3930339 EU FUSELAGE SCRATCHED A FDEA K NONE O OTHER UK UNKNOWN 1 SO 25 816FD 593 OLD SCRATCH REPAIR ON EXTERNAL SKIN BETWEEN C75/76, P27. REPAIR VERIFICATION, PERFORMED IAW SRM 53-18-12/FIG 102 EA FOR TRACKING: 6-5318-106413. 2 L 7 2 4F RT A35EU 2007040200201 20070402 00201 NM 2007 4 2 DLM90070266 1 20070324 A 5210 SKIN DOUG MD90 MD9030 3023690 NM L1 DOOR BENT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DA 53381 FOUND L1 DOOR LOWER AFT CORNER SKIN IS BENT. REPAIR PER SRM 52-10-01 AT HMV2 REF N/R 8000-0003. 2 L 7 2 4F RT A6WE 2007040200204 20070402 00204 NM 2007 4 2 DL76L070271 1 20070328 A 2740 271003367 CONTROL MODULE BOEING 767 767332 1382001 NM STABILIZER TRIM MALFUNCTIONED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 193DN 28450 DISCONTINUED TAKEOFF AT 65-70 KIAS FOR AN UNSCHEDULED TRIM LIGHT STAB TRIM/AILERON LOCK-OUT MODULE SAM M524 W/ FAULT BAL L STCM. FAULT BALL RESET. PRIMARY AND ALTERNATE STAB TRIM OPERATED FULLY NORMAL WITH NO FURTHER EICAS MSGS. FIM PROC 27-09-00 FIG 106A CARRIED OUT SATIS. ADC TEST L AND R CARRIED OUT SATIS IAW MM. REMOVED AND REPLACED LEFT STAB TRIM CO NTROL MODULE AS PER AMM. LEAK CHK GOOD. PERFORMED REQUIRED RII INSP PER TOPP 40-30-05 ITEM 6 AND TOPP 40-10-20 PG 3/B ITEM 2 NOTE BOX. 2 L 7 2 4F RT A1NM 2007040200207 20070402 00207 2007 4 2 DL76G070276 4 20070329 A 2330 3100362 AUDIO VIDEO UNIT BOEING 767 7673P6 1385105 NM CABIN MALFUNCTIONED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 156DL 25354 ENT SYS SHUTOFF AND BACK ON BY ITSELF. F/A INVESTIGATED AND DETECTED HOT ELECTRICAL SMELL. TURNED SYS OFF AND SMELL DI SSIPATED. PULLED CB T9/T8 AS PRECAUTION. RESET CBS AND TURNED ON SYS. VMOD IMMEDIATELY EMITTED STRONG ODOR COOLING FA N NOISY AND COOLING VENTS PARTIALLY BLOCKED. REPLACED VMOD IFE SYS CKS OK. NO FURTHER ODOR NOTED. COOLING AIRFLOW UNR ESTRICTED. 2 L 7 2 4F RT A1NM 2007040200224 20070402 00224 EU 2007 4 2 07FDEA01070 1 20070321 A 5315 FLOORBEAM AIRBUS 310 A310222 3930315 EU FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 421FE 342 PREVIOUS REPAIR LOCATED ON MAIN CABIN FLOORBEAM FRAME 34 BETWEEN SEAT TRACKS 2 AND 3 RT FWD AND AFT UPPER FLANGE HAS 2 E ACH REPAIR ANGLES THE FWD ANGLE IS 10.25" BY 1" AND THE AFT ANGLE IS 12.2" BY 1.82" PREVIOUSLY INSTALLED REPAIR LOCATED AT MAIN CABIN FLOORBEAM FRAME 34 BETWEEN SEAT TRACKS 2 AND 3 RT WAS DETERMINED NOT TO BE IAW FEDEX EA6-5321-29300. REMO VED AND REINSTALLED FLOOR PANEL PER A310/200 AMM SUPPLEMENT 53-10-23-4, REMOVED EXISTING REPAIR ANGLES AND REPAIRED FLOO RBEAM PER FEDEX EA6-5310-107718. 2 L 7 2 4F RT A35EU 2007040200226 20070402 00226 NM 2007 4 2 07FDEA01027 1 20070320 A 3244 ARG7755503 TIRE DOUG MD11 MD11F 3023600 NM NR 9 DAMAGED A FDEA K NONE O OTHER LD LANDING 1 SO 25 595FE 48553 NR 9 TIRE FAIL ALERT ON LNDG ROLLOUT CDG. NO OTHER INDICATIONS. FOUND NR 9 TIRE EXPOSED. FOUND BRAKE NR 10 HYD PRESS LINE CUT, AND BRAKE NR 9 HID FITTING BENT, NEED TO REPLACE NR 9 BRAKE. REMOVED AND REPLACED BRAKE NR 10 HYD PRESS LINE AS PER SUMP. LEAK TEST OK. REMOVED AND REPLACED MAIN TIRE NR 10 AS PER MM 32-41-01-4. CHECKED CONTINUITY TEST BETWEE N ANTI-SKID CONTROL UNIT AND WHEEL SPEED TRANSDUCER NR 9 AND 10. CHECKED WIRING CONTINUITY BETWEEN ANTI SKID MANIFOLD C TR GEAR AND ASCU, PRECAUTIONARY CHANGED ASCU AS PER MM 32-45-01-4. PERFORMED ANTI-SKID TEST AS PER MM 32-41-01-5, ALL T EST PASSED. REMOVED AND REPLACED NR 9 BRAKE ASSY AS PER MM 32-43-20-4. LEAK CHECK OK. REMOVED AND REPLACED NR 9 WHEEL 2 L 7 3 4F RT A22WE 2007040200227 20070402 00227 NM 2007 4 2 07FDEA01038 1 20070321 A 5320 FLOOR SUPPORT BOEING 727 72725 1384006 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 CABIN FLOOR SUPPORT (BEAM ) HAS CORROSION FS 620, LBL 35. FABRICATED REPAIR ANGLES PER DWG SR27-53-033 AND MAE TRAVELER T7/669736 CUT OUT DAMAGED AREA IAW DWG SR27-53-033. TREATED AND PRIMED CUT OUT DAMAGE IAW SRM 51-10- 2. FABRICATED F ILLER FROM 7075-T6 .125C BATCH NR 1046555 IAW DWG SR27-53-033. INSTALLED ANGLES AND FILLER REPAIR IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2007040300001 20070403 00001 NM 2007 4 3 DHL2007786520 1 20070321 A 5522 SKIN BOEING 727 727214 138407R NM RT ELEVATOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 DENT ON RT ELEVATOR LWR SKIN FWD OF NR 2 STATIC WICK, ELEV STA 209.96, 11" FWD OF T/E. EVALUATED DENT AND FOUND OUT OF LIMITS IAW B727 SRM 55-20-1, FIG 7. CUT OUT DAMAGED AREA 7" BY 0.50" AND FABRICATED REPAIR DOUBLER USING 2024T3, 0.032, 4" BY 2.0625 IAW B727 SRM 55-20-2, FIG 1 AND 55-20-3 FIG 5. TREATED, PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED REPA IR DOUBLER IAW B727 SRM 55-20-3, FIG 5 AND SRM 51-30-2. ELEVATOR WEIGHT AND BALANCE PERFORMED ON NR 112945. 2 L 7 3 4F A3WE 2007040300002 20070403 00002 NM 2007 4 3 DHL2007786516 1 20070321 A 5522 SKIN BOEING 727 727214 138407R NM LT ELEVATOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 LT ELEVATOR LWR T/E SKIN DENTED AT NR 1 TAB BOBWEIGHT CUTOUT, ELEV STA 99.79, FWD OF CONTROL TAB. EVALUATED TWO EACH DE NTS, NR 1, A=.50" Y=.051" A/Y=9.80, NR 2, A=.50" Y=.052" A/Y=9.61, FOUND TO BE OUT OF LIMITS IAW B727 SRM 55-20-1, FIG 1 . CUTOUT DAMAGE AREA, NR 1, 0.625" BY 0.50", NR 2, 0.625" BY 0.50" IAW B727 SRM 55-20-2, FIG 1. FAB DOUBLER REPAIR FOR M 2024T3, 0.032, 5" BY 2" AND 5" BY 1.875" IAW B727 SRM 55-20-2, FIG 1 AND 55-20-3, FIG 5. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 55-20-3, FIG 5. REBALANCED LT ELEVATOR SURFACE, REPAIR WEIGHT 0.074 LBS DIS TANCE Y=4", REPAIR MOMENT M=0.296, PREVIOUS MOMENTOUS 121.85 LBS/IN PLUS 0.296 LBS/IN = 122.15 LBS/IN. FOUND TO BE WITH 2 L 7 3 4F A3WE 2007040300003 20070403 00003 NM 2007 4 3 DHL2007786519 1 20070313 A 5344 MS20001167200 HINGE BOEING 727 727214 138407R NM CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 EXT FUSELAGE MCD HINGE AFT SEGMENT AFT MOST LOBE IS CRACKED. REMOVED HINGE AT EXT FUSE MCD AFT SEGMENT IAW AEI B727 FRE IGHTER CHAPTER 52 FIG 5201 A REVF. FABRICATED AFT SEGMENT, MATERIAL MS20001-16-7200 PO NR 9002527 DIM 18" IAW B727 FREI GHTER CHAPTER 52 FIG 5201 A REVF. TREATED AND PRIMED AREA AND PART IAW B727 SRM 51-10-2. INSTALLED NEW SEGMENT AT AFT END IAW AEI B727 FREIGHTER CHAPTER 52 FIG 5201 A REV F. 2 L 7 3 4F A3WE 2007040300004 20070403 00004 NM 2007 4 3 AWXA200700425 1 20070327 A 2750 LIMITER AIRBUS A319 A319132 3930340 NM NR 1 FLAP TORQUE TRIPPED A AWXA O OTHER J WARNING INDICATION AP APPROACH 1 WP 28 833AW 1844 LAS - EL - CREW REPORTED DURING APPROACH INTO BOS, THE FLAPS DID NOT EXTEND. CREW DECLARED AN EMERGENCY. THE PAX DID N OT BRACE. THE LANDING WAS UNEVENTFUL. MX FOUND NR 1 TORQUE LIMITER TRIPPED. MX RESET TORQUE LIMITER PER 27-50-00-991- 003. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007040300005 20070403 00005 NM 2007 4 3 DHL2007786521 1 20070315 A 5753 STRUCTURE BOEING 727 727214 138407R NM TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 A/C IN "C" CHECK AT FLIGHTSTAR A/C SERVICES REF ASTAR NR 080528. RT WING IB MID FLAP LOWER CHORD AT WBL135 SHOWS CRACK. REMOVED R/WING IB MID FLAP LOWER PANEL AND LOWER AFT CHORD WBL135 AS REQ IAW B727 SRM 51-30-2. FABRICATED ANGLE FROM B AC1503-100046 7075T6 PO NR 7157132 DIM. 68 1/2" BY 2" IAW B727 SRM 51-40-3 FIG 1 AND 57-50-2 FIG 5. TREATED AND PRIMED ANGLE AND AREA IAW B727 SRM 51-10-2. INSTALLED ANGLE AT R/WING IB MID FLAP IAW B727 SRM 51-30-2. CLOSED ACCESS PANEL A T R/WING IB MID FLAP IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007040300011 20070403 00011 SO 2007 4 3 20060927 1 20070327 A 2161 222017011400 CONTROLLER EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE AUTO TEMP FAILED A GLBA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 NM 03 96ZK 120096 AIR RETURN, PILOT REPORTED THAT THE CABIN DID NOT PRESSURIZE UNTIL 10,000 FEET. CABIN MASKS DROPPED AT APPROXIMATELY 8, 000 FEET CABIN ALTITUDE. MAINTENANCE REMOVED AND REPLACED THE AUTO TEMP CONTROLLER. OPERATIONAL CHECK ON GROUND GOOD. RE FERENCE MM 21-30. SUBSEQUENT OPERATIONAL CHECK FLIGHT WAS SATISFACTORY. 2 L 7 2 4T 4 T RT A31SO E20NE 2007040300012 20070403 00012 EU 2007 4 3 07FDEA01050 1 20070321 A 5340 FITTING AIRBUS 310 A310304 3930339 EU ZONE 100 DAMAGED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 816FD 593 MISDRILLED HOLES IN C17 AT P44 LT. REPAIR WAS PERFORMED BY BUSHING REPAIR AND NEW FITTING INSTALLATION (P/N A536-10607- 206-93, A536- 10607-207-93) IAW EA 6-5312-106418 AND RAS/AS/006/2007 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040300015 20070403 00015 EU 2007 4 3 07FDEA01053 1 20070321 A 5711 FRAME AIRBUS 310 A310304 3930339 EU ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 DEVIATIONS TO EO 6-5710-7-3322 (CRACKS IN HOLE 23 AND 62 LT). REPAIR PERFORMED BY OVERSIZING HOLE 23 AND 62 LT IAW EA 6 -5710-106423 AND RAS/049817/013/2007 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040300041 20070403 00041 CE 2007 4 3 9876543219876 1 20070315 A 2720 99145586 ACTUATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL ZONE 300 BINDING E J00A O OTHER F FLT CONT AFFECTED CR CRUISE 1 EA 01 505MA 2454 2454 7500057 RUDDER MOVEMENT WAS LIMITED TO 20 PERCENT OF FULL TRAVEL. SERVICE CENTER FOUND ACTUATOR TO BE SEIZED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007040300044 20070403 00044 CE 2007 4 3 DJFA2007038 1 20070330 A 2711 4034311 TRIM SWITCH BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE ROLL STICKING E DJFA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 23 455CW 2813 RK365 TRIP NR 1160942 CREW REPORTED ROLL TRIM RUNAWAY. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. MAINTENANCE FOUND THE ROLL TRIM SWITCH STUCK. THE SWITCH WAS REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007040300050 20070403 00050 NM 2007 4 3 07FDEA00725 1 20070309 A 5313 A5A7114519 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 FOUND CENTER CARGO RT TUNNEL AREA, LONGERON 37R SPLICE AT STA 1531 SUSPECTED CRACKED CENTER CARGO RT TUNNEL AREA LONGERO N 37R SPLICE. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-10 0. 2 L 7 3 4F RT A22WE 2007040300062 20070403 00062 NM 2007 4 3 DXTA200702054 1 20070329 A 3030 HEATER AMD FALC50 FALCON2000 2730170 NM PITOT SYS FAILED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 230QS 59 PITOT HEAT FAIL, AOA HEAT FAIL, STATIC PORT HEAT FAIL. INSPECTED BEHIND OVERHEAD C/B PANEL NO DEFECTS NOTED. FOUND AN D RESET LT PITOT HEAT C/B. PERFORMED FUNCTIONAL TEST AND GROUND RUN IAW FALCON 2000EX M/M 30-300. NO DEFECTS NOTED. IN SPECTED BEHIND OVERHEAD C/B PANEL NO DEFECTS NOTED. FOUND AND RESET LT AOA HEAT C/B. PERFORMED FUNCTIONAL TEST AND GRO UND RUN IAW FALCON 2000EX MM 30-300. NO DEFECTS NOTED. INSPECTED BEHIND OVERHEAD C/B PANEL NO DEFECTS NOTED. FOUND AN D RESET LT STATIC HEAT C/B. PERFORMED FUNCTIONAL TEST AND GROUND RUN IAW FALCON 2000EX MM 30-300. NO DEFECTS NOTED. 2 K 7 2 4F RT A50NM 2007040300074 20070403 00074 EA 2007 4 3 SIMA200708604 1 20070327 A 2731 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA PITCH FEEL UNKNOWN A SIMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 SW 21 504AE 10044 RECEIVED PITCH FEEL CAUTION MESSAGE, EMERGENCY DECLARED. PERFORMED OPERATIONAL TEST OF PITCH FEEL SYSTEM IAW EMB AMM TA SK 27-31-00-710-802-A01 AND EMB FIM TASK 27-41-00-810-805-A01 WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007040300076 20070403 00076 EA 2007 4 3 SIMA200709204 1 20070316 A 5320 67053110522 WEB CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 520DC 7739 3739 10140 WEB AT STATION 280 LEFT SIDE CORRODED AT FLOOR MATING AREA. SPLICED IN NEW WEB AT STATION 280 IAW AMERICAN EAGLE ENGINE ERING ORDER CR-53MR-112. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007040300079 20070403 00079 SO 2007 4 3 SIMA200709203 1 20070327 A 5315 13500469403 FLOORBEAM EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 708AE 15810 4800 145205 RIGHT FLOORBEAM SUPPORT FOUND CORRODED IN GALLEY AREA. REMOVED AND REPLACED SUPPORT IAW EMB SRM 51-40-02. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007040300109 20070403 00109 NM 2007 4 3 QXEA200700484 1 20070325 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 222 S2-3L DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - BURN MARK AT RIVET FOR FRAME X222 BETWEEN STRINGERS 3L ND 4L. REPAIRED IAW SRM 51-40-11, AND 51-20-26. 2 H 7 2 4T RT A13NM 2007040300116 20070403 00116 NM 2007 4 3 QXEA200700499 1 20070325 A 6120 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN A QXEA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 09 420QX 4147 SEA - ON FLIGHT 2476, RETURNED TO FIELD, DURING CLIMB AT APPROX 18,000 FT NOTICED NR 2 PROP DROP FROM 850 RPM TO 840 RPM FOR ABOUT 10 SECONDS THEN POWERPLANT MESSAGE DISPLAYED ON ED. NOTICED NR 2 OIL PRESSURE WAS FLUCTUATING FROM NEAR TOP OF NORMAL TO 3/4 DOWN IN GREEN ARC. WAS NORMAL PSI AT FLIGHT IDLE. ALL OTHER INDICATIONS WERE NORMAL TO LANDING. MAIN TENANCE TROUBLESHOOTING (FAULT CODE RETRIEVAL AND EMU DOWNLOAD) CLEARING OF FAULT CODE 158 AND PWR ASSUR CHECK IAW MTC 6 710005. REF BOMBARDIER SERVICE LETTER DH8-400-SL-61-004 FOR RETURN TO SERVICE AUTHORIZATION, PWR ASSUR CHECK GOOD. FAU LT CODE CLEARED AND DID NOT RETURN. OK FOR CONTINUED SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007040300119 20070403 00119 EA 2007 4 3 QXEA200700495 1 20070329 A 3230 9752753 VALVE CNDAIR CL600 CL6002C10 1390015 EA MLG MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 603QX 2737 10011 PDX - AFTER SELECTING THE GEAR "UP", THE MAIN GEAR REMAINED IN TRANSIT FOR A EXTENDED PERIOD OF TIME. WHEN PLACED TO "D OWN" NO ACTIVITY FOR 5 SECONDS OR SO. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACE D THE BALANCE RELIEF VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007040300128 20070403 00128 NM 2007 4 3 QXEA200700472 1 20070325 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - FOUND SEAT TRACK NR 9 HAS SCRATCHES AT STATION X535 TO X545. REPAIRED IAW RD8-53-784. 2 H 7 2 4T RT A13NM 2007040300143 20070403 00143 EU 2007 4 3 07FDEA01072 1 20070321 A 5347 SEAT TRACK AIRBUS 310 A310222 3930315 EU FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 MDCC DUMMY TRACK NR 1 FR 38.2 - FR 40 CENTER LINE OF AIRPLANE IS WORN MORE THAN .039 IAW EO6-5310-7-3322, WORN LESS THAN .078 REMOVED AND REINSTALLED FLOOR BOARDS PER A310-200 SRM 51-40-21. REMOVED AND REINSTALLED DUMMY TRACK PER A310-200 SRM 51-40-21. REPAIRED DUMMY TRACK PER A310-200 SRM 53-15-16. 2 L 7 2 4F RT A35EU 2007040400003 20070404 00003 NM 2007 4 4 HALA0700147 1 20070402 A 3397 WIRE BOEING 767 767300 1385204 NM EMERGENCY LIGHT BROKEN A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 592HA 33468 EMERGENCY PATH LIGHTING AT 20 HJ TO 27 HJ INOP. FOUND POWER LEAD WIRE BROKEN. REPLACED LEAD. PATH LIGHTING CKS OK. 2 L 7 2 4F RT A1NM 2007040400020 20070404 00020 NM 2007 4 4 SWAA071607 1 20070328 A 5322 6546536 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 540 S27R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 540, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007040400022 20070404 00022 WP 2007 4 4 070085 1 20070331 A 2410 CSD DOUG DC9 DC983 3022083 WP LEFT LOW A WX0A H DEACTIVATE SYST/CIRCUITS J J WARNING INDICATION WARNING INDICATION CR CRUISE 1 WP 19 863GA 49911 THE FLT CREW REPORTED THAT THE LT CSD OIL TEMP PEGGED OVER REDLINE. CSD DISCONNECTED. FARGO CONTRACT MAINTENANCE DEFER RED THE LEFT GENERATOR PER MEL 24-01-01 UNDER THE GUIDANCE OF MAINTENANCE CONTROL. ACFT RETURNED TO LAS VEGAS & MX SERV ICED CSD PER AMM 12-12-02. A SATISFACTORY OPS CHECK ACCOMPLISHED PER AMM 71-00-00. ACFT RETURNED TO SERVICE. THIS IS THE 2ND INCIDENT ON THIS ACFT & CSD. MAINTENANCE REPLACED THE LEFT CSD CHARGE AND SCAVENGE FILTERS IAW MM 24-10-00, REP LACED LEFT CSD OIL COOLER IAW MM 24-10-03. ALL CHECKS NORMAL,CSD RECONNECTED AND SAFETIED SWITCH. AIRCRAFT RETURNED TO S ERVICE. 2 L 7 2 4F RT A6WE 2007040400027 20070404 00027 EU 2007 4 4 AWXA200700455 1 20070319 A 5210 D52111830 COVER AIRBUS 320 A320231 3930325 EU ZONE 800 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 634AW 091 SAL - L2 DOOR FORWARD UPPER AFT CORNER INTERNAL COVER PLATE WORN. REPLACED L2 DOOR FORWARD UPPER AFT CORNER INTERNAL CO VER PLATE IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007040400028 20070404 00028 EU 2007 4 4 AWXA200700456 1 20070319 A 5210 D52111417201 COVER AIRBUS 320 A320231 3930325 EU ZONE 800 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 634AW 091 SAL - R2 DOOR AFT UPPER AFT CORNER INTERNAL COVER PLATE WORN. REPLACED R2 DOOR AFT UPPER AFT CORNER INTERNAL COVER PLA TE IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007040400038 20070404 00038 NM 2007 4 4 SWAA071621 1 20070329 A 5523 6963391 BOLT BOEING 737 7373H4 1384600 NM LT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED MV2 CHECK, LEFT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED INBOARD PUSHROD END BOLT PER SWA EA. 2 L 7 2 4F RT A16WE 2007040400042 20070404 00042 NM 2007 4 4 SWAA071624 1 20070329 A 3350 MS155721 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 491WN 33867 DURING SCHEDULED MV3 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007040400048 20070404 00048 NM 2007 4 4 07FDEA01232 1 20070402 A 5710 ARB2886504 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RT WING, LEADING EDGE ANTI-ICE TELESCOPIC DUCT CUT-OUT FOUND CRACKED APPROX 1/4" IN LENGTH. [SUP 4-20-07] AREA TRIMMED OUT AND REPAIRED AS PER SRM 57-10-00 FIG. 42 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040400056 20070404 00056 EU 2007 4 4 07FDEA01240 1 20070402 A 5320 FLOOR SUPPORT AIRBUS 310 A310203 3930313 EU CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 MDCC FWD LT FLOOR SUPPORT ANGLE ON FLOOR PANEL 221FF IS CRACKED AT 1 FASTENER HOLE. STOP DRILLED CRACK IAW SRM 51-73-10 . NDT IAW NTM 51-20-08. NO CRACK INDICATIONS PAST STOP DRILL. FABRICATED DOUBLER IAW SRM 51-71-40. MAT'L USED 2024-T 3 .063 IAW SRM 53-12-15, FIG 19, ITEM 105, PG 34, BATCH NR 1230605. LOCATED AND DRILLED DOUBLER IAW SRM 51-40-44. INST ALLED DOUBLER IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007040400061 20070404 00061 NM 2007 4 4 07FDEA01245 1 20070402 A 5754 SKIN BOEING 727 727225 1384077 NM ZONE 500 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 463FE 22551 FOUND REPAIR AT LT WING NR 1 SLAT. FLUSH REPAIR IS 15" FROM OB END ON TOP SURFACE. REPAIR REQUIRES EVALUATION FOR MAJO R/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. FOUND REPAIR DID NOT MEET CRITERIA OF SRM 57-50-3 FIG 1. AFT END OF REPAIR NOT ATTACHED TO SKIN OF SLAT. REPLACED, ADJUSTED AND OPS CHECKED LT WING NR 1 LE SLA T REF MM 27-81-011-4 PAGES 1-5. NR 1 LE SLAT, OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2007040400073 20070404 00073 NM 2007 4 4 SWAA071608 1 20070328 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 767 S26R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007040400086 20070404 00086 NM 2007 4 4 DHL2007786513 1 20070321 A 5521 7075T6 RIB BOEING 727 727214 138407R NM RT ELEVATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 RT ELEVATOR, FWD INBD RIB CRACKED AND MISSING RIVETS, ELEV STA 20. REMOVED ACCESS PANEL RT ELEVATOR LWR INBD IAW B727 S RM 51-30-2. REMOVED RIB IAW B727 SRM 51-30-2. FABRICATED NEW RIB FROM 7075T6, .040, 18.25 BY 2.50 IAW B727 SRM 55-20-2 , FIG 2. TREATED ALODINE AND PRIMED IAW B727 SRM 51-10-2. INSTALLED NEW RIB AT RT ELEVATOR INSIDE ACCESS PANEL NR 9405 IAW B727 SRM 51-30-2. INSTALLED ACCESS PANEL IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007040400101 20070404 00101 NM 2007 4 4 SWAA071645 1 20070331 A 3350 101073 LENS BOEING 737 7373K2 13844BA NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007040400105 20070404 00105 NM 2007 4 4 SWAA071638 1 20070330 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED MV1 CHECK, FOUND RIGHT FWD CABIN BULLNOSE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007040400117 20070404 00117 NM 2007 4 4 2007UALA00873 1 20070323 A 2120 UNKNOWN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 WP 29 837UA 1474 ON APPROACH ELECTRICAL ODOR. GALLEY CABIN OFF, VIDEO PLAYER OFF. ODOR DISSIPATED. [SUP 06-01-07] INSPECTED FORWARD AND AFT EE COMPARTMENTS AND FORWARD GALLEY WITH NO DEFECTS NOTED. RAN BOTH AC PACKS WITH NO NOTICABLE ODOR DETECTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007040400129 20070404 00129 EU 2007 4 4 2007UALA00943 1 20070329 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE S42L CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 432UA 587 STRINGER 42 LEFT HAS CORROSION ON THE INNER SURFACE OF THE FLANGE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007040400142 20070404 00142 NM 2007 4 4 DHL2007786528 1 20070322 A 5511 FRAME BOEING 727 727214 138407R NM BS 1303 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 EMPENNAGE INTERIOR BS 1303 WL 281, FRAME CENTER WEB AT SECOND UP RIGHT STRINGER CUTOUT IS CRACKED 1 INCH. STOP DRILLED CRACK IAW COTNEY AEROSPACE ED NR EAZ04E-1, REV IR, 8110-3 DATED 3/28/07. VISIONAL RE-INSPECTION REQUIRED AT INTERVALS N OT TO EXCEED 2400 FLIGHT CYCLES. 2 L 7 3 4F A3WE 2007040400157 20070404 00157 NM 2007 4 4 2007UALA00920 1 20070328 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 294 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 364UA 24533 A CRACK WAS FOUND AT SHEAR TIE AT BS 294.5 NEAR STR 11L & AT INTERCOSTAL WEB AT BS 294.5 NEAR STRINGER 12L. [SUP 4-17-0 7] MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS PER AAR EA I070140 AND UA EVA-70146. 2 L 7 2 4F 4 F RT A16WE E21EU 2007040400158 20070404 00158 NM 2007 4 4 2007UALA00921 1 20070329 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EMERGENCY LIGHT AT SEAT 4E INOP. RELAMPED EEL LIGHT. OP CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007040400159 20070404 00159 NM 2007 4 4 2007UALA00922 1 20070329 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE STAIRS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 STAIRS EMERGENCY LIGHT INOP. [SUP 4-17-07] SECURED CONNECTION. STAIR EMERGENCY LIGHT OP CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007040400160 20070404 00160 NM 2007 4 4 2007UALA00923 1 20070329 A 3350 20131A BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EMERGENCY LIGHTS FROM SEAT 46A UP TO 54A INOP. [SUP 4-17-07] REPLACED BATTERY. ALL EEL OPERATE NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007040400161 20070404 00161 NM 2007 4 4 2007UALA00924 1 20070329 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 53A INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EMERGENCY LIGHT INOP AT SEAT 53A. [SUP 4-17-07] REPLACED LIGHT ASSY. OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007040400162 20070404 00162 2007 4 4 2007UALA00925 4 20070328 A 2565 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE DOOR 5R FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 177UA 24384 SLIDE LACING BROKEN ON TOP EDGE OF DOOR 5R SLIDE PACK. [SUP 4-24-07] AIR-SERVE REPORTS GIRT BAR AT DOOR 5R IS HANGING OUT OF BUSTLE. LACING APPEARS BROKEN ON TOP EDGE OF DOOR 5R SLIDE. REPLACED DOOR 5 RIGHT DOOR SLIDE PER MM 25-69-01. SUSPECT IMPROPER CINCHING DURING SLIDE REFURBISHING & REINSTALLATION, AGGRAVATED BY IMPACT OF CABIN & GALLEY SERVICE EQU IPMENT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007040400163 20070404 00163 NE 2007 4 4 2007UALA00926 2 20070328 A 7200 COMPRESSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LEFT ENGINE STALLED A UALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 416UA 479 V10925 POSSIBLE ENGINE COMPRESSOR STALL ON TAKEOFF. SUSPECT LEFT ENG. NO ECAM, PFR SHOWS NR 2 ENGINE COMPRESSOR STALL. [SUP 05-18-07] QTY 2 STAGE 6 HPC BLADES LIBERATED AT MID-SPAN WITH DOWNSTREAM DAMAGE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007040400165 20070404 00165 NM 2007 4 4 2007UALA00928 1 20070328 A 3397 WIRE HARNESS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 590 RBL 30 DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 508UA 24744 AISLE LIGHT AT STA 590, RBL 30 AND AISLE LIGHT AT STA 1430, LBL 30, WIRE HARNESS DAMAGED. [SUP 4-17-07] REPAIRED EEL LIGHT AT STA 590, RBL 30 WIRE HARNESS PER BSWPM 20-30-12. REPLACED WIRE HARNESS TO AISLE EEL LIGHT AT STA 1430. 2 L 7 2 4F 4 F RT A2NM E17NE 2007040400166 20070404 00166 NM 2007 4 4 07FDEA01134 1 20070326 A 5753 66166445 BULLET BOEING 727 727225 1384077 NM FLAP TRACK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 NR 1 FLAP TRACK FAIRING ASSY BULLET IS CRACKED REMOVED AND REPLACED NR 1 FAIRING BULLET REF MM 27-31-031. 2 L 7 3 4F A3WE 2007040500018 20070405 00018 EA 2007 4 5 SWIA200718066 1 20070323 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 728SK 10192 LAST OVERHEAD EMERGENCY EXIT LIGHT IS INOP. REPLACED LAST OVERHEAD EMERGENCY EXIT LIGHT BULB IAW CRJ MM 33-51-09. OPER ATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007040500019 20070405 00019 SO 2007 4 5 SWIA200718067 1 20070325 A 5411 FRAME EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 234SW 120308 LEFT MLG OUTBOARD AFT DOOR AFT ATTACH ARM UPPER ATTACH POINT NACELLE FRAME CRACKED, DISCOVERED DURING A-CHECK INSPECTION . INSTALLED SERVICEABLE HALF-FRAME ON LEFT OUTBOARD AFT NACELLE IAW SRM 51-40-02. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007040500020 20070405 00020 EA 2007 4 5 SWIA200718068 1 20070326 A 5610 601R3303311 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 449SW 7699 PILOT'S SIDE LEFT WINDOW CRACKED AT 35,000 FT. REPLACED CAPTAIN'S LEFT WINDOW IAW CRJ 200 MM 56-12-01 AND RII 56-220-10 00. 2 L 7 2 4F RT A21EA 2007040500021 20070405 00021 SO 2007 4 5 SWIA200718069 1 20070302 A 5330 SKIN EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 229SW 120305 UNDER FLOOR BETWEEN STATION 38 AND 39 FOUND HOLE CORRODED THROUGH SKIN, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER EMB IC2007-120/1728D AND EMB 120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2007040500022 20070405 00022 SO 2007 4 5 SWIA200718070 1 20070327 A 7712 30005000052 SIGNAL COND UNIT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENG TORQUE MALFUNCTIONED A SWIA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 NM 07 298SW 5076 5076 120328 ON CLIMB-OUT, RIGHT TORQUE WENT TO 118 PERCENT. REPLACED SIGNAL CONDITIONING UNIT IAW 77-11-01 AND TORQUEMETER PICKUP P ROBE P/N 3116942-01 IAW 77-11-02 IAW 71-00-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2007040500023 20070405 00023 SO 2007 4 5 SWIA200718071 1 20070302 A 5751 BEARING EMB 120 EMB120ER 3260203 SO LT AILERON CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 229SW 120305 LEFT AILERON QUADRANT BEARINGS ARE CORRODED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED BEARINGS ON LEFT AILERON QU ADRANT ASSEMBLY. 2 L 7 2 4T RT A31SO 2007040500024 20070405 00024 NE 2007 4 5 SWIA200718072 2 20070323 A 7261 OIL SYSTEM CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE RT ENGINE LOW PRESSURE A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 744SK 10200 RECEIVED RIGHT ENGINE LOW OIL PRESSURE EMERGENCY MESSAGE. SHUT ENGINE DOWN. REPLACED RIGHT ENGINE ASSEMBLY IAW M/M 71- 00-00 AND RII 72-400-1000. OPERATIONAL CHECK GOOD, P/N: CF-348C1, S/N OFF: GE-E965640. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007040500025 20070405 00025 NE 2007 4 5 NACA20070012 2 20070328 A 8530 404481 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 1 ENGINE SEPARATED A NACA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AL 03 2907F 365 41 533265 P34459 NR 1 ENGINE BACKFIRING. ENGINE SHUT DOWN. REPLACED NR 1 ENGINE NR 8 CYLINDER DUE TO SEPERATED FINS FROM CYLINDER LINER . REF: DC-6MM SECT V PG 16 AND 16A. LEAK AND OPS CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2007040500026 20070405 00026 NM 2007 4 5 07FDEA01135 1 20070326 A 5340 66248952 ATTACH ANGLE BOEING 727 727225 1384077 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 LOWER AFT PIT FORWARD BULKHEAD VERTICAL WALL SUPPORT LOWER CLIP ANGLE IS CRACKED THAT ATTACHES TO FLOOR STRINGER AT ST A 950A, RBL 12. REMOVED AND REPLACED AFT PIT FWD BULKHEAD VERTICAL WALL SUPPORT LOWER CLIP ANGLE AT STA 950A, RBL 12, R EF DWG NR 66-24895 AND 727 SRM 51-30-02 PG 2. 2 L 7 3 4F A3WE 2007040500027 20070405 00027 EU 2007 4 5 07FDEA01136 1 20070327 A 5720 R57150404 ANGLE AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 CORROSION AND CRACK FINDINGS IN HOLES DURING SEALING ANGLES INSTALLATION-EO 6-5710-7-5002-SB A300-57-6033 REV 01-SB A300 -57-6-27 REV 6- AD98-18-02 AND AD 2006-07-07. REPAIR PERFORMED BY REAM UP AND SEALING ANGLE REPLACEMENT IAW EA 6-5720-1 06433 AND RAS/BAE/1004205/2007 ISS.A 2 L 7 2 4F RT A35EU 2007040500028 20070405 00028 NM 2007 4 5 07FDEA01137 1 20070327 A 2750 MS9391130ZE4C DRIVE UNIT BOEING 727 727233 138408A NM TE FLAPS LEAKING A FDEA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 25 285FE 22622 DESCENDING THROUGH 10,000 EN ROUTE TO KTPA, EXPERIENCED HYDRAULIC SYSTEM "A" LOSS O QUANTITY FOLLOWED BY BOTH PUMP LIGHT S ILLUMINATED. SYSTEM "A" FLUID SHUTOFF SWITCHES WERE CLOSED FOR 20 MINUTES. REMOVED AND REPLACED FLAP POWER UNIT HYD MOTOR PER M/M 27-51-062-4. SERVICED FLUID, RAN ENGINES AND CHECKED CASE DRAIN FILTERS AND PRESS FILTERS FOR METAL CONT AMINATION. NO METAL FOUND, INSTALLED NEW FILTERS, RAN ENGINES, NO FURTHER LEAKS NOTED. RECHECK FILTER IN 200 HRS OK FO R SERVICE. 2 L 7 3 4F RT A3WE 2007040500029 20070405 00029 EU 2007 4 5 07FDEA01138 1 20070327 A 5720 R57150404 ANGLE AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 CORROSION AND CRACK FINDINGS DURING SEALING ANGLE INSTALLATION- EO 6-5710-7-5002- SB A300-57-6033 REV 1- SBA300-57-6027 REV 6- AD 98-18-02 AND AD 2006-07-07 REPAIR PERFORMED BY REAM UP IAW EA 6-5720-106433 AND RAS/BAE/1004205/2007 ISS. A. 2 L 7 2 4F RT A35EU 2007040500030 20070405 00030 EU 2007 4 5 07FDEA01139 1 20070327 A 5755 STRUCTURE AIRBUS AIRBUS 300 A300B4622R 3930312 EU SPOILER DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD FX0010 633 DAMAGE ON SPOILER NR 4 LT REPAIR PERFORMED IAW SRM 57-72-11 FIG 205, APPROVED BY EA 6-5770-106440 REV A AND RAS/DABRE/70 07420/2007 ISS. A 2 L 7 2 4F RT A35EU 2007040500031 20070405 00031 EU 2007 4 5 07FDEA01140 1 20070327 A 5712 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 CRACK WAS FOUND ON MLG RIB 5 RT WING INTERIM REPAIR PERFORMED IAW, DRAWING R572-40265 AND APPROVED BY EA 6-5710-108975 A ND RAS/BAE/1004080/2006 ISS.A 2 L 7 2 4F RT A35EU 2007040500032 20070405 00032 EU 2007 4 5 07FDEA01141 1 20070327 A 5730 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 CORROSION SPOTS ON LT WING TOP SKIN RIB 1-25 REPAIR PERFORMED BY BLEND OUT IAW EA 6-5720-106376 AND RAS/BAE/1004287/2007 ISS. A. 2 L 7 2 4F RT A35EU 2007040500033 20070405 00033 EU 2007 4 5 07FDEA01142 1 20070327 A 5730 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 CORROSION SPOTS ON OUTER SHROUD BOX AND TOP SKIN REPAIR PERFORMED BY BLEND OUT IAW EA 6-5720-106376 AND RAS/BAE/1004287/ 2007 ISS. A 2 L 7 2 4F RT A35EU 2007040500034 20070405 00034 NM 2007 4 5 07FDEA01143 1 20070327 A 5315 652082755 FLOORBEAM BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 MAIN DECK AT FS 480 FLOORBEAM CORRODED BETWEEN LBL 26 AND LBL 45. REMOVED CORROSION REF SRM 53-10-01. ORIGINAL MATERIA L MEASURED AT .125 BLEND OUT MATERIAL LOSS AT DEEPEST LOCATION MEASURES .016. REMAINING MATERIAL AFTER BLEND IS .109 AND IS STRUCTURALLY ACCEPTABLE PER EA 7-5310-106996. ACCOMPLISHED HFEC INSPECTION TO EFFECTED AREA REF EA AND SOPM 20-1 0-03 WAS USED TO ACCOMPLISH FLAP PEEN TO AREA. 2 L 7 3 4F A3WE 2007040500035 20070405 00035 NM 2007 4 5 07FDEA01144 1 20070327 A 5340 69701914 ATTACH FITTING BOEING 727 727225 1384077 NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 NR 2 ENG INLET DOGHOUSE AT BASE OF VERTICAL LEADING EDGE, VERTICAL WEB ATTACH CLIP CRACKED AT INTERIOR STA 1274 LT SIDE. REMOVED AND REPLACED VERTICAL WEB ATTACH CLIP, AT STA 1274 INSIDE VERTICAL STABILIZER ABOVE S-DUCT ON LT SIDE. REF B7 27 SRM 51-30-02 PG 2. 2 L 7 3 4F A3WE 2007040500036 20070405 00036 NM 2007 4 5 07FDEA00985 1 20070318 A 5311 AFA00193 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 MAIN DECK CARGO, FRAME FOUND DENT AT STA 1721 L12 LT. REPAIR CARRIED OUT AT MAIN DECK CARGO FRAME AT STA 1721 L12 LT AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040500037 20070405 00037 NM 2007 4 5 07FDEA00986 1 20070318 A 5311 AFA00273 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 MAIN DECK CARGO FRAME, FOUND DENT AT STA 1661 L12 LT. REPAIR CARRIED OUT AT MAIN DECK CARGO FRAME AT STA 1661 L12 LT AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040500038 20070405 00038 NM 2007 4 5 07FDEA01145 1 20070327 A 5751 SKIN BOEING BOEING 727 727225 1384077 NM AILERON DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 LT WING O/B AILERON LOWER T/E SKIN IS DELAMINATED JUST O/B OF TAB. REMOVED, REPAIRED AND REINSTALLED LT O/B AILERON REF MM 27-10-031-2. REPAIR ACCOMPLISHED ON WO NR 11841-5000-0002. REMOVED TAB, REPAIRED DELAMINATED SKIN ON AILERON TE AND REINSTALLED TAB REF MM 27-10-041-4 AND SRM 51-40-20. 2 L 7 3 4F A3WE 2007040500039 20070405 00039 EU 2007 4 5 07FDEA01146 1 20070327 A 5310 CROSSBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 414FE 400 PREVIOUSLY INSTALLED REPAIR FOUND ON CROSS BEAM AT FRAME 36 YA TO YB DOES NOT FOLLOW SRM CRITERIA. REMOVED PREVIOUSLY I NSTALLED REPAIR ANGLES IAW SRM 51-40-21. FABBED NEW ANGLES IAW SRM 53-10-15 FROM 60-15 36/15 7075-0 AND HEAT TREATED ON MAE TRAV T7/670475. LOCATED AND DRILLED IAW SRM 51-40-44 AND SRM SUPPLEMENT 53-10-10. INSTALLED NEW ANGLES IAW SRM SU P 53-10-15, APPLIED CIC IAW SRM SUP 53-10-15. 2 L 7 2 4F RT A35EU 2007040500040 20070405 00040 EA 2007 4 5 TRAX200700432 1 20070327 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 CRACK FOUND ON PAX DOOR INNER SKIN AT FS 329.50 NEAR HANDLE PIVOT SHAFT. 2 L 7 2 4F RT A21EA 2007040500041 20070405 00041 EA 2007 4 5 TRAX200700433 1 20070327 A 3250 STEERING SYS CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 829AS 7232 GEAR RETRACTION RECEIVED STEERING INOP MSG FOLLOWED BY GEAR DISAGREE WARNING. NOSE GEAR BOX RED. AIRCRAFT RETURNED TO MKE AFTER T/O. EMERGENCY DECLARED BY TOWER. FLTS 4194, 4356 CX. 2 L 7 2 4F RT A21EA 2007040500042 20070405 00042 EA 2007 4 5 TRAX200700434 1 20070327 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 978EV 7723 ON CLIMBOUT OF ATL BELOW 10K BOTH F/O AND CAPT PICKED UP A MILD BURNING ODOR, PRIOR TO REACHING 10K ODOR WENT AWAY. UP ON LANDING AT FAY BOTH RECEIVED SAME ODOR. F/A REPORTED, ONLY ON TAXI IS A STRONG ODOR OF BURNING. 2 L 7 2 4F RT A21EA 2007040500043 20070405 00043 EA 2007 4 5 TRAX200700435 1 20070329 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 719EV 10099 CAPTAIN`S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007040500048 20070405 00048 WP 2007 4 5 07FDEA01100 1 20070322 A 5230 FITTING DOUG MD10 MD1010F 3022112 WP CARGO DOOR CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 566FE 46989 MAIN CARGO DOOR NR 7 SPOOL FITTING HAS CRACK INDICATION. REMOVED NR 7 SPOOL FITTING (BACK OF FITTING) IAW DC/MD10 SRM 5 1-33-01 VOL 11, PG 47. LOCATED AND DRILLED NEW FITTING IAW DAC DWG AFA7132 REV B. INSTALLED NEW FITTING IAW DC/MD10 S RM 51-33-01 VOL11 PG 34. SPOOL FITTING TO BE RIGGED ON N/R N00712. 2 L 7 3 4F RT A22WE 2007040500049 20070405 00049 NM 2007 4 5 07FDEA01101 1 20070322 A 5330 SKIN BOEING 727 727225 1384077 NM STA 232 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 461FE 22548 EXTERNAL DOUBLER AT STA 232-243.5 STR 24R DOES NOT COMPLY WITH FAA APPROVED DATA. REPAIRED AREA AT STA 232-243.5, STR 2 4R IAW SRM 53-30-3 FIG 14 SH 7. 2 L 7 3 4F A3WE 2007040500064 20070405 00064 EA 2007 4 5 COMA0760292 1 20070326 A 2711 601R5122623 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA AILERON TRIM FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 987CA 7199 FLIGHT 5689 - CONFIG AILERON MASTER WARNING MESSAGE RECEIVED. REPLACED AILERON TRIM CONTROL PANEL. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007040500065 20070405 00065 NM 2007 4 5 DHL2007786515 1 20070326 A 5322 SHEAR TIE BOEING 727 727214 138407R NM BS 950F CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 AFT CARGO COMPARTMENT BS 950F AND STR 28L, SHEAR TIE HAS CORROSION. CUT OUT DAMAGED AREA AT AFT CARGO COMPARTMENT SHEAR TIE, SIZE 6” BY 1.50 IAW B727 SRM 53-10-4, FIG 13. FABRICATED DOUBLER REPAIR FROM 7075T6, .071, 8 BY 3.50 IAW B727 SRM 53-10-4, FIG 13. TREATED ALODINE AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007040500066 20070405 00066 NM 2007 4 5 DHL2007786518 1 20070320 A 5322 SHEAR TIE BOEING 727 727214 138407R NM BS 985 S28R CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 AFT CARGO COMPARTMENT AT BS 985 AND STR 28R, SHEARTIE HAS CORROSION. CUT OUT DAMAGED AREA AT AFT CARGO COMPARTMENT BS 9 85 AND STR 28R SHEARTIE IAW B727 SRM 53-10-4, FIG 13. DIMENSION 5.25 BY 4 IAW B727 SRM 53-10-4, FIG 13. FABRICATED SHE ARTIE REPAIR FROM 7075T6, FILLER .040, 5.25 BY 4, DOUBLER, .063, 5.30 BY 4 IAW B727 SRM 53-10-4, FIG 13. TREATED ALODIN E AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007040500067 20070405 00067 EA 2007 4 5 COMA0760293 1 20070329 A 2150 ACM CNDAIR CL600 CL6002B19 1900309 EA RIGHT MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 916CA 7014 FLIGHT 5687 - DURING TAKEOFF ROLL RECEIVED A -R PACK HI PRESS- MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. DEFER RED THE RIGHT AIR CONDITIONING PACK. 2 L 7 2 4F RT A21EA 2007040500068 20070405 00068 EA 2007 4 5 COMA0760297 1 20070402 A 2840 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 821CA 7420 FLIGHT 5538 - FUEL CHANNEL 2 STATUS MESSAGE ON CLIMBOUT, AIRCRAFT RETURNED TO AGS AND LANDED SAFELY. DEFERRED PER MEL 2 8-41-03 CAT B. 2 L 7 2 4F RT A21EA 2007040500069 20070405 00069 NM 2007 4 5 07FDEA01148 1 20070327 A 5210 SHROUD BOEING 727 727225 1384077 NM L2 DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 LT AFT SERVICE DOOR FWD UPPER END SHROUD HAS CRACKS 2 PLACES APPROX 8 IN AND 6 IN FROM FWD UPPER CORNER. CONTAINED CRA CK IN SHROUD BY STOP DRILLING IAW SRM 51-10-1 PARA 10. TREATED AND PRIMED AREA IAW SRM 51-10-1. RESEALED AREA IAW DWG 65-56992 AND MM 51-30-001-1. PREPPED AND PAINTED IAW MM 51-20-151-7. 2 L 7 3 4F A3WE 2007040500070 20070405 00070 NM 2007 4 5 07FDEA01149 1 20070327 A 5230 SKIN BOEING 727 727225 1384077 NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 MCD DOOR EXTERNAL SKIN AT AFT LOWER EDGE HAS DISTORTED AND CRACKED SKIN. BLENDED AREA IAW SRM 51-10-1 AND 52-00-2, ORIG MAT'L .063IN AFTER REWORK .061IN. WITHIN LIMITS IAW SRM 52-00-2, FIG NR 1. REMOVED DAMAGED ON SKIN EDGE AMOUNT OF MA T'L. REMOVED WAS 0.003 WITHIN LIMITS IAW SRM 52-00-2 FIG NR 1. HFEC IAW NTM 51-00-00 PT6. NO CRACK NOTED. TREATED AN D PRIMED IAW SRM 51-10-2. PREPPED AND PAINTED AREA IAW MM 51- 20-151-7. CLASSIFIED AS MINOR REPAIR. 2 L 7 3 4F A3WE 2007040500071 20070405 00071 NM 2007 4 5 07FDEA01150 1 20070327 A 5740 651928090 ATTACH FITTING BOEING 727 727225 1384077 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 LT WING PANEL NR 8240 CLIP IS CRACKED REMOVED DAMAGED CLIP, VERIFIED MATERIAL AS 2024 T3-.032 REF DWG 65-19280 AND FABRI CATED REPLACEMENT CLIP REF DWG 65-19280 AND FED EX 7-0-1001 ITEM 7C. TREATED REPLACEMENT PART REF SRM 51-10-2 PG 7. PR IMED REF AMM 51-20-151-7 ITEMS 5 AND 6 AND INSTALLED REF SRM 51-30-2. 2 L 7 3 4F A3WE 2007040500072 20070405 00072 NM 2007 4 5 07FDEA01151 1 20070327 A 5754 6922882 BRACKET BOEING 727 727225 1384077 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 NR 5 FLAP TRACK OTBD AFT BRACKET FOR CENTER FAIRING IS CRACKED. REMOVED AND REPLACED NR 5 FLAP TRACK OTBD AFT BRACKET. REF SRM51-30-2 PG 4 REF BOEING DRAWING 69-22882 REF SRM 51-10-2 PG 3, 4 AND 5, REF MM 51-20-031-07 PGS 1, 2, & 3. 2 L 7 3 4F A3WE 2007040500073 20070405 00073 WP 2007 4 5 07FDEA01152 1 20070327 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 731-771 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 SEAT TRACK CRACKED NEAR NR 7 MCD LATCH FITTING REMOVED SEAT TRACK AT LBL 108 STA 731 TO 771 IAW DC/10MD10 SRM 53-70-00, VOL 1 PG 6 A. FABRICATED HAT CHANNEL AND SPLICE PLATE 7075T6 .050" PO 543247.6 HAT CHANNEL S4932154-N00 PO 563619.1 IAW DC/MD 10 SRM 53-70-00 VOL 1 PG 6. FABRICATED SEAT TRACK. REPAIR S4929149 PO 564954 IAW DC/MD10 SRM 53-70-00 VOL I PG 6. ALODINED AND PRIMED IAW DC/MD 10 SRM 51-21-01 VOL I PG 1-15. INSTALLED SEAT TRACK AND SEALED IAW DC/MD 10, SRM 53-7 0-00 VOL 1 PG 7. 2 L 7 3 4F A22WE 2007040500074 20070405 00074 NM 2007 4 5 07FDEA01153 1 20070327 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 1183 S25R CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 AFT PIT S-25R AND TENSION TIE AT 1183 STA EXFOLIATED. REMOVED STR AND TENSION TIE, FABED NEW PARTS IAW SRM 53-10-3, FIG 1, DETAIL 2. INSTALLED TENSION TIE AND STRINGER REPAIR PARTS IAW SRM 53-30-2,AND 53-10-3. 2 L 7 3 4F A3WE 2007040500075 20070405 00075 NM 2007 4 5 07FDEA01154 1 20070327 A 3210 UNKNOWN DOUG MD11 MD11 3023602 NM RT MLG UNKNOWN A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 596FE 48554 RIGHT MAIN GEAR WOULD NOT RETRACT ON TAKEOFF. LANDED DXB WITHOUT INCIDENT. RT/MLG BUNGEE ACTUATOR REMOVED AND REPLACED AND HYDRAULICS BLED C/O AND LEAK CHECK SATIS AS PER AMM 32-33-02-4. RT MLG TRIM CYLINDER REMOVED AND REPLACED AND BLEE D CHECK SATISFACTORILY AS PER AMM 32-37-01-4. RESTRICTOR FOR RT L/G RETRACT CYLINDER REMOVED AND REPLACED AND LEAK CHEC K SATIS AS PER AMM 32-33-01-4. RT MLG RETRACT CYLINDER REMOVED AND REPLACED SATIS AND LEAK/OPERATION CHECK ALL NORMAL A S PER AMM 32 -33-20-4. AIRCRAFT JACKED UP TO HEIGHT FOR MLG SWINGS AS PER AMM 07-11-00-2 MAIN GEAR WHEEL AND DOOR OPE RATIONAL TESTS CARRIED OUT SATISFACTORILY (5) FIVE TIMES AS PER AMM 32-31-00-5. OKAY FOR SERVICE. 2 L 7 3 4F RT A22WE 2007040500076 20070405 00076 EA 2007 4 5 COMA0770021 1 20070402 A 5310 CC67034175701 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FS 280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 658CA 7856 10148 FS 280.0 CROSSBEAM CORRODED. REPAIRED IAW REO 670-53-11-047. 2 L 7 2 4F RT A21EA 2007040500077 20070405 00077 EA 2007 4 5 TRAX200700426 1 20070324 A 3310 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CAPTAIN'S MAP INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 COCKPIT/FLIGHT DECK/FLIGHT COMPARTMENT AND INSTRUMENT LIGHTING SYSTEMS (EXCLUDING EFIS) - INDIVIDUAL LIGHTS, CAPT'S MAP LIGHT INOP. REMOVED AND REPLACED CAPT'S MAP LIGHT IAW AMM 33-10-01. OPS CHECK GOOD. REMOVED PLACARD. 2 L 7 2 4F RT A21EA 2007040500078 20070405 00078 EA 2007 4 5 TRAX200700431 1 20070325 A 3150 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA UNKNOWN A ASOA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 761ND 10213 UPON GEAR RETRACT -STEERING INOP- CAUTION MSG. MW STG OFF PER CHECK LIST, ON AGAIN IN FLIGHT. RESET UNSUCCESSFUL. UPO N LANDING, CYCLES G-2 C/B'S ON P1 AND P2 AND RESET GOOD. EMERGENCY DECLARED. EMERGENCY EQUIPMENT ON STANDBY. 2 L 7 2 4F RT A21EA 2007040500079 20070405 00079 EU 2007 4 5 07FDEA01155 1 20070328 A 5511 A55171814216 SPAR AIRBUS 300 A300B4622R 3930312 EU ZONE 300 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 CRACK AND BEND ON LT SIDE OF THE CENTER SPAR REINFORCING ANGLE REPAIR PERFORMED BY TRIM OUT IAW EA 6-5511-106378 AND RAS /CASA/5355/2007 ISS A. 2 L 7 2 4F RT A35EU 2007040500080 20070405 00080 NM 2007 4 5 07FDEA01005 1 20070320 A 2497 BXS700722 WIRE DOUG MD11 MD11F 3023600 NM ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 AFTER INSPECTION CARRIED OUT ON WIRING CLAMPS AND HARNESSES IN FORWARD AVIONICS BAY RIGHT FOUND WIRE B102-1004-22 (CEN TER BUNDLE) AND WIRE B102-183-22N (LOWER BUNDLE) WITH CHAFED MARKS. WIRE B102-1004-22 AND WIRE B102-183-22N FROM CENT ER AND LOWER BUNDLES IN FORWARD AV BAY REPAIRED AS PER AMM 20-30-04-2. 2 L 7 3 4F RT A22WE 2007040500081 20070405 00081 EU 2007 4 5 07FDEA01156 1 20070328 A 5711 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 CRACK FINDINGS DURING ACCOMPLISHMENT OF EO 6-5710-7-3305 REV C1, SB A300-57-6050 REV 3-AD 2005-23-08 REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW EA 6-5710-106435 AND RAS/049856/032/2007 ISS. A 2 L 7 2 4F RT A35EU 2007040500082 20070405 00082 NM 2007 4 5 DHL2007786514 1 20070321 A 5753 SKIN BOEING 727 727214 138407R NM FOREFLAP DEBONDED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 RIGHT WING, INBD FOREFLAP, UPPER SKIN INBD EDGE SHOWS INCORRECT PREVIOUS REPAIR. NR 4 LE FLAP, LE STA 130.7. REMOVED I NCORRECT PREVIOUS FIBERGLASS REPAIR APPROX 1.5 IAW B727 SRM 51-40-22 FIG 3 AND APPLIED POTTING COMPOUND. FAB DOUBLER 4" BY 5", .016, 2024T3 IAW B727 SRM 57-50-2. BONDED, CLEANED AND PRIMED IAW B727 SRM 51-40-22 FIG 3. 2 L 7 3 4F A3WE 2007040500083 20070405 00083 NM 2007 4 5 DHL2007786517 1 20070315 A 5753 SKIN BOEING 727 727214 138407R NM FOREFLAP DEBONDED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 LEFT OUTBD FOREFLAP WBL 305, HAS T/E DISBONDING. CUT OUT DAMAGED AREA APPROX 2 BY 6 ON LT OUTBD FOREFLAP WBL 305 IAW B7 27 SRM 51-40-20. FABRICATED FILLER .016 BY 2 BY 6 AND DOUBLER, .016 3.50 BY 8.50 FROM 2024T3 IAW B727 SRM 53-10-4, FIG 13. BONDED FILLER AND DOUBLER, CLEANED, PRIMED AND SEALED IAW B727 SRM 51-40-20. 2 L 7 3 4F A3WE 2007040500084 20070405 00084 EU 2007 4 5 2007UALA00877 1 20070323 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FWD CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 458UA 1163 FWD EMERGENCY EXIT LIGHTS ARE ON WITH SEAT BELT SWITCH ON. SUP.4-17-07. RESET CIDS SYS. AND LIGHTS CKD NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007040500085 20070405 00085 EU 2007 4 5 2007UALA00878 1 20070324 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LEFT WING FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 473UA 1469 MID CABIN OVERHEAD EXIT FLASHING ON-OFF; EXIT DOOR LIT TOO. REPLACED LEFT WING POWER SUPPLY UNIT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007040500086 20070405 00086 NM 2007 4 5 2007UALA00879 1 20070326 A 3350 60243 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 365UA 24534 FLOOR EEL INOP FROM ROW 15 TO AFT GALLEY. FOUND WATER SHORTING EEL CIRCUIT AT AFT GALLEY, DRIED AREA AND INSTALLED NEW LAMP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007040500087 20070405 00087 NM 2007 4 5 2007UALA00880 1 20070323 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY EXIT CEILING ENTRY LIGHT INOP AT DOOR 5R. RELAMPED. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007040500088 20070405 00088 NM 2007 4 5 2007UALA00881 1 20070324 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY CEILING LIGHT ABOVE SEAT 5A & ABOVE ROW 23 LEFT ARE INOPERATIVE. RELAMPED EMERGENCY LIGHTS IN BOTH POSITIONS. BOTH OP CHECK NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007040500089 20070405 00089 NM 2007 4 5 2007UALA00882 1 20070324 A 3350 20131A BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 RIGHT & LEFT EMERGENCY CEILING LIGHTS FROM ABOVE ROW 35 TO ROW 46 ARE INOPERATIVE. REPLACED BATTERY PACK. EEL OP CHECK NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007040500090 20070405 00090 NM 2007 4 5 2007UALA00883 1 20070324 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY LIGHT ALONG UPPER DECK STAIR INOP. RESECURED EEL CONNECTOR ALONG UPPER DECK STAIRS. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007040500125 20070405 00125 2007 4 5 2007UALA00935 4 20070329 A 2565 PROXIMITY SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 2R SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 573UA 26685 DOOR SLIDE LIGHT DOOR 2R DOES NOT ILLUM WHEN ARMED. [06-14-07] CHANGED LIGHT UNIT - NO HELP. REPLACED LIGHT BASE OP S CHECK NORMAL. REPLACED PROX SWITCH S10220 FOR ULTIMATE FIX. 2 L 7 2 4F 4 F RT A2NM E17NE 2007040500127 20070405 00127 EU 2007 4 5 2007UALA00941 1 20070328 A 3250 CONTROLLER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG STEERING MALFUNCTIONED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 428UA 523 NOSE WHEEL STEERING FAULT AT GEAR DOWN. [SUP 06-01-07] REPLACED NOSE WHEEL STEERING SERVO CONTROL 6GC. 2 L 7 2 4F 4 F RT A28NM E40NE 2007040500128 20070405 00128 NM 2007 4 5 2007UALA00937 1 20070327 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 831UA 1291 CREW OXYGEN SYSTEM LOW. [SUP 06-01-07] FAULT TRACED TO AN INTERNAL LEAK IN THE CAPTAIN'S OXYGEN MASK STOWAGE BOX. REPL ACED BOX. 2 L 7 2 4F 4 F RT A28NM E40NE 2007040500131 20070405 00131 NM 2007 4 5 SWAA071716 1 20070403 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 500 S26L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007040500132 20070405 00132 NM 2007 4 5 SWAA071673 1 20070402 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040500133 20070405 00133 NM 2007 4 5 SWAA071677 1 20070402 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040500134 20070405 00134 NM 2007 4 5 SWAA071678 1 20070402 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM BS 520 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040500135 20070405 00135 NM 2007 4 5 SWAA071694 1 20070402 A 5311 6546540 FRAME BOEING 737 7373Y0 1384671 NM BS 639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, RBL 58, WL 207. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2007040500136 20070405 00136 NM 2007 4 5 SWAA071676 1 20070402 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040500137 20070405 00137 EU 2007 4 5 07FDEA01184 1 20070329 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 1 CRACK FOUND .75" IN UPPER SUPPORT LEG ON AFT SIDE OF FLOORBEAM FR 58 BETWEEN SEAT TRACK 4L AND 5L EXTENDING INTO FLOOR BEAM WEBBING UNDER CLS ADAPTER IAW A310-200 AMM 53-16-11-6. REMOVED DAMAGED AREA AND REPAIRED IAW AB DWG R53270150 AND EA 6-5310-107708. 2 L 7 2 4F RT A35EU 2007040500138 20070405 00138 EU 2007 4 5 07FDEA01185 1 20070329 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 1 CRACK EXIST IN FLOORBEAM VERTICAL STIFFENER AT FRAME 36 BETWEEN SEAT TRACK L2 AND L3 MEASURING .5" REF R537B1041000 A3 10-200 AMM 53-10-15-6. REMOVED CRACK PER A310 SRM SUPP 53-10-15 FIG 201. NDT C/W PER NTM 51-10-08, NO CRACK INDICATIO NS NOTED. FABBED REPAIR PARTS PER A310 SRM SUPP 53-10-15, FIG 201. PROTECTED SURFACES WITH ALODINE, PRIMER, AND TOPCOA T PER A310 SRM 57-75-10. INSTALLED REPAIR COMPLETE PER A310 SRM SUPP 53-10-15, FIG 201. 2 L 7 2 4F RT A35EU 2007040500139 20070405 00139 NM 2007 4 5 SWAA071670 1 20070401 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM BS 767 S25L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007040500140 20070405 00140 NM 2007 4 5 SWAA071723 1 20070403 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 620 S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 620, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007040500141 20070405 00141 NM 2007 4 5 SWAA071710 1 20070403 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 807 S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007040500142 20070405 00142 NM 2007 4 5 SWAA071672 1 20070401 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM BS 380 S26R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007040500143 20070405 00143 NM 2007 4 5 SWAA071721 1 20070403 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500B S21R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007040500144 20070405 00144 NM 2007 4 5 SWAA071711 1 20070403 A 5753 6937206 TORQUE TUBE BOEING 737 7373H4 1384600 NM RT WING TE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQU E TUBE PER MM. 2 L 7 2 4F RT A16WE 2007040500145 20070405 00145 NM 2007 4 5 SWAA071712 1 20070403 A 5753 6937206 TORQUE TUBE BOEING 737 7373H4 1384600 NM RT WING TE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007040300028 20070403 00028 CE 2007 4 3 DXTA200702066 1 20070401 A 3230 HOOK CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG STICKING E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 651QS 5605251 GEAR UNLOCK LIGHT REMAINED ILLUMIATED AND HYDRALIC PRESSURE LIGHT REMAINED ON, RAN CHECKLIST AND LIGHTS EXTINGUISH WHEN HYDRAULIC CONTROL CIRCIUT BRAKER RESET IAW CHECKLIST. REMOVED AND REPLACED NOSE GEAR UPLOCK SWITCH WITH NEW. NOSE GEAR UPLOCK HOOK WAS STICKY. REMOVED LOCK. CLEANED AND LUBRICATED. REINSTALLED HOOK. OPERATIONAL CHECK OF SYSTEM NORMAL. WORK IAW CESSNA 560XL/XLS MM CHPT 32-30-05. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007040300045 20070403 00045 NE 2007 4 3 ASMF200703007 2 20070327 A 7200 UNKNOWN DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE ENGINE UNKNOWN W ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 803ML 49726 716781 AIRCRAFT REJECTED TAKEOFF AT 75 KNOTS DUE TO LT ENGINE REACHED ONLY 1.6 EPR WHILE RT ENGINE REACHED 2.04 EPR WITH N1 100 PERCENT, SO AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL CHECKED ENGINE INLET/OUTLET, CONTROLS, PT2 AND P T7 LINES AND MANIFOLD IAW PROPER INSTALLATION, ALL CORRECT. LT ENGINE RUNNING TEST WAS PERFORMED IAW MM 71-00-00 AT 1.65 , 1.80 AND 2.06 EPR'S, BEING SATISFACTORY. ADDITIONALLY, AUTO THROTTLE TEST WAS PERFORMED REACHING 2.06 EPR IAW MM 71-00 -00 AND MPCM 71-00-01. 2 L 7 2 4F 4 F RT A6WE E9NE 2007040300056 20070403 00056 NM 2007 4 3 AWXA200700446 1 20070305 A 5313 6546877 STRINGER BOEING 737 7373G7 1384595 NM ZONE 200 - FUSEL CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - FOUND CRACKED STRINGER, BS 727, S18A LEFT. REPAIRED STRINGER, BS 727, S18A LEFT IAW AWA ER 03-5361-07084-SS2. 2 L 7 2 4F RT A16WE 2007040300066 20070403 00066 SO 2007 4 3 SIMA200708804 1 20070328 A 7500 BLEED AIR SYS EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 ENGINE LEAKING A SIMA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 941LT 14744 2303 14500926 CAE3111214 LAVATORY SMOKE WARNING MESSAGE ON TAKEOFF WHEN PACKS SELECTED ON, EMERGENCY DECLARED. RETURNED TO ORD. REMOVED AND REP LACED NR 2 ENGINE IAW AMERICAN EAGLE WORK CARD 72-000-00. OPERATIONAL AND LEAK CHECK GOOD. RETURNED AIRCRAFT TO SERVIC E. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007040300069 20070403 00069 EU 2007 4 3 SIMA200708803 1 20070328 A 2913 4018502 PUMP SAAB SF340 340B 7860101 EU HYD SYSTEM FAILED A SIMA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 SW 21 324AE 16509 2297 340B324 LOST MAIN HYDRAULIC PUMP, MAIN SYSTEM SHOWED ZERO PRESSURE, PUMP WAS INOPERATIVE. EMERGENCY ACCUMULATOR AND PRESSURE WE RE GOOD. EMERGENCY DECLARED. LOST NOSE WHEEL STEERING ON GROUND. REMOVED AND REPLACED HYDRAULIC PUMP IAW SAAB AMM. O PERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007040300083 20070403 00083 CE 2007 4 3 DJFA2007032 1 20070322 A 5511 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 789TA RK268 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION, THE LT AND RT IB HORIZO NTAL STABILIZER, BOTH LT AND RT RIBS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. SDR WILL BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION. 2 H 7 2 4F 4 F RT A16SW E25EA 2007040300084 20070403 00084 CE 2007 4 3 DJFA2007033 1 20070322 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 741TA 7281 RK201 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION, THE LT AND RT IB HORIZO NTAL STABILIZER, BOTH LT AND RT RIBS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. MAINTENANCE REPLACED THE RIB ASSEMBLIES. 2 H 7 2 4F 4 F RT A16SW E25EA 2007040300088 20070403 00088 EU 2007 4 3 AWXA200700430 1 20070329 A 5315 D53472172203 FLOORBEAM AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 SAL - CORROSION ON CABIN FLOORBEAM, -Y1292, FR 66 + 8" - FR 68. REPLACED CABIN FLOORBEAM, -Y1292, FR 66 - FR 68 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007040300089 20070403 00089 NM 2007 4 3 AWXA200700431 1 20070329 A 5711 6545324 SPAR BOEING 737 7373G7 1384595 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - LEFT WING REAR SPAR UPPER CHORD CRACKED, RSS 221. REPAIRED LEFT WING REAR SPAR UPPER CHORD, RSS 221 IAW AWA ER 03 -5722-07086-SS4. 2 L 7 2 4F RT A16WE 2007040300094 20070403 00094 NM 2007 4 3 AWXA200700436 1 20070309 A 5320 654797321 SHEAR WEB BOEING 737 7373G7 1384595 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - CORROSION ON CABIN FLOOR SHEAR WEB, BS 639, RBL 65, WL 208.1. REPLACED CABIN FLOOR SHEAR WEB, BS 639, RBL 65, WL 208.1 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007040300095 20070403 00095 NM 2007 4 3 AWXA200700437 1 20070309 A 5320 654797321 SHEAR WEB BOEING 737 7373G7 1384595 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - CORROSION ON CABIN FLOOR SHEAR WEB, BS 616, LBL 65, WL 208.1. REPLACED CABIN FLOOR SHEAR WEB, BS 616, LBL 65, WL 208.1 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007040300096 20070403 00096 NM 2007 4 3 AWXA200700438 1 20070309 A 5312 69464661 GUSSET BOEING 737 7373G7 1384595 NM BULKHEAD CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - BS 540 BULKHEAD VERTICAL STIFFENER ATTACH ANGLE CRACKED, LBL 45, WL 208. REPLACED BS 540 BULKHEAD VERTICAL STIFF ENER ATTACH ANGLE, LBL 45, WL 208 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007040300097 20070403 00097 NM 2007 4 3 AWXA200700439 1 20070309 A 5311 65465412 FRAME BOEING 737 7373G7 1384595 NM BS 663 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 MCN - CRACKED FRAME UPPER RING, BS 663.75, S1 - S3R. REPAIRED FRAME UPPER RING, BS 663.75, S1 - S3R IAW B737-300 SRM 53 -00-07-2R9, FIGURE 201. 2 L 7 2 4F RT A16WE 2007040300105 20070403 00105 NM 2007 4 3 QXEA200700504 1 20070331 A 6120 697073002 PCU BOMBDR DHC8 DHC8402 1390042 NM NR 2 MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 424QX 7550 7550 4006 PDX FLIGHT NR 2569: POWER PLANT MESSAGE AFTER ROTATION FROM PDX. RETURNED TO FIELD. MAINTENANCE REMOVED AND INSTALLED SERVICEABLE NR 2 PCU IAW Q400 AMM TASK 61-20-11-000-801 AND TASK 61-20-11-400-801. OPS CHECK GOOD. NO MESSAGES NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007040300106 20070403 00106 NM 2007 4 3 QXEA200700493 1 20070325 A 5730 ACCESS PANEL DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - FUEL TANK ACCESS PANEL 524AT HAS FRETTING ON INBOARD AND OUTBOARD SIDE WING STRUCTURE. REPAIRED IAW RD8-57-984 . 2 H 7 2 4T RT A13NM 2007040300107 20070403 00107 NM 2007 4 3 QXEA200700483 1 20070325 A 5330 DOUBLER DHAV DHC8 DHC8202 2809007 NM BS 280 S11R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - BURN MARK IN THE DOUBLER ABOVE STRINGER 11R AT STATION X280. REPAIRED IAW SRM 51-20-26 AND 51-40-11. 2 H 7 2 4T RT A13NM 2007040300108 20070403 00108 NM 2007 4 3 QXEA200700482 1 20070327 A 5320 SILL DHAV DHC8 DHC8202 2809007 NM PAX DOORWAY CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - FOUND SUPPORT BRACKET UNDER MAIN CABIN DOOR LOWER SILL PLATE IS CRACKED IN TWO PLACES AT STATION X240. REPAIRE D IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007040300113 20070403 00113 NM 2007 4 3 QXEA200700498 1 20070328 A 5210 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM DOOR UNKNOWN A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 420QX 4147 SEA - ON FLIGHT 2378, AFT BOARDING DOOR HARD TO OPEN FROM INSIDE. MAINTENANCE PERFORMED GVI OF AFT PASSENGER DOOR LINKA GE MECHANISMS AS ACCESSED THRU INTERIOR DOOR HANDLE COVER AND LOWER VENT GRILL. NO DISCREPANCIES NOTED. CLEANED AND LU BED DOOR HANDLE SHAFT. PERFORMED OPERATIONAL TEST OF THE AFT DOOR, CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PAR TS REPLACED. 2 H 7 2 4T RT A13NM 2007040300114 20070403 00114 NM 2007 4 3 QXEA200700497 1 20070330 A 2750 C1486561 POWER UNIT BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 412QX 483 483 4059 BOI - ON FLIGHT 2389, FLAP DRIVE CAUTION LIGHT AFTER FLAP RETRACTION. MAINTENANCE REMOVED AND REPLACED FLAP POWER UNIT. FUNCTIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007040300115 20070403 00115 NM 2007 4 3 QXEA200700470 1 20070306 A 3010 4100S01806 MONITOR BOMBDR DHC8 DHC8402 1390042 NM DE ICE SYSTEM INOPERATIVE A QXEA O OTHER N FALSE WARNING DE DESCENT 1 NM 09 409QX 580 580 4051 SEA - ON FLIGHT 2338 DURING DESCENT IN ICING CONDITIONS "DEICE PRESS CAUTION" ILLUMINATED. WHEN SYSTEM WAS REENGAGED DU RING EA CHECKLIST DEICE CAUTION LIGHT EXTINGUISHED BUT BOOTS DID NOT CYCLE IN AUTO MODE. LIGHTS AND BOOTS FUNCTIONED IN MANUAL MODE ONLY, DEICE PRESS WAS NORMAL THROUGHOUT. MAINTENANCE REMOVED AND REPLACED TIMER AND MONITOR UNIT. FUNCTIO NAL TEST GOOD. DEICE PRESSURE CAUTION LIGHT DID NOT ILLUMINATE. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007040300124 20070403 00124 NM 2007 4 3 QXEA200700479 1 20070326 A 7110 HINGE BRACKET DHAV DHC8 DHC8202 2809007 NM COWL DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - 424AR RIGHT COWL DOOR HOLD OPEN ROD HINGE BRACKETS HAVE ELONGATED HOLES AT CLEVIS PIN. REPAIRED IAW SRM 51-40- 11. 2 H 7 2 4T RT A13NM 2007040300125 20070403 00125 NM 2007 4 3 QXEA200700480 1 20070327 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - THERE IS CORROSION ON AND UNDER SEVERAL NUTPLATES THAT SERVE TO SECURE CARGO FLOORBOARD PANEL 144BZ. REPAIRED IAW SRM 51-40-11, 51-20-11, AND 51-20-16. 2 H 7 2 4T RT A13NM 2007040300129 20070403 00129 NM 2007 4 3 QXEA200700476 1 20070326 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - SCRATCHES AND BARE METAL ON SEAT TRACK NR 2 BETWEEN STATION 429 AND 504. REPAIRED IAW RD8-53-1342. 2 H 7 2 4T RT A13NM 2007040300135 20070403 00135 NM 2007 4 3 QXEA200700491 1 20070325 A 5730 ACCESS PANEL DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - FUEL TANK ACCESS PANEL 524BT HAS FRETTING ON INBOARD AND OUTBOARDWING STRUCTURE. REPAIRED IAW RD8-57-633. 2 H 7 2 4T RT A13NM 2007040300138 20070403 00138 WP 2007 4 3 070078 1 20070326 A 3350 408822101 BATTERY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 875GA 53468 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION LAS VEGAS MAINTENANCE REPORTED THAT BOTH LEFT AND RIGHT AFT OVERWING HATCH 'EXIT' SIGNS WOULD NOT TEST. LAS VEGAS MAINTENANCE FURTHER REPORT THE REMOVAL AND REPLACEMENT OF THE EMERGENCY L IGHT POWER SUPPLY BATTERY PACK AT FS 990R. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIR PLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007040300140 20070403 00140 WP 2007 4 3 070080 1 20070326 A 2410 CSD DOUG DC9 DC983 3022083 WP LEFT LACK OF LUBE A WX0A H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CR CRUISE 1 WP 19 863GA 49911 FLIGHT 711 SFB/RFD, THE FLIGHT CREW REPORTED THAT DURING THE FLIGHT THEY NOTICED THE LEFT CSD OIL TEMPERATURE HIGH AND R ISING. THEY FURTHER REPORT THAT THEY FOLLOWED THE QRH PROCEDURE AND DISCONNECTED THE LEFT CSD AS THE OIL TEMP EXCEEDED REDLINE. ROCKFORD CONTRACT MAINTENANCE DEFERRED THE LEFT GEN/CSD PER MEL 24-01-01. ON 03-27-2007, LAS VEGAS MAINTENANC E REPORT SERVICING THE LEFT CSD OIL TO THE PROPER LEVEL PER AMM 12-12-02. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLI SHED PER AMM 71-00-00. MEL 24-01-01 WAS CLEARED AND THE PLACARDS REMOVED. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007040400001 20070404 00001 EU 2007 4 4 07FDEA01081 1 20070322 A 5313 LONGERON AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CORROSION ON LONGERON AT FLOOR STRUCTURE SEC 12 (Y-1959) BETWEEN C17/19 WAS OUT OF LIMIT. REPAIR PERFORMED IAW SRM 53-1 2-12/FIG 207. 2 L 7 2 4F RT A35EU 2007040400002 20070404 00002 NM 2007 4 4 07FDEA01083 1 20070322 A 5320 65348932 FLOOR SUPPORT BOEING 727 727225 1384077 NM BS 740-760 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 CABIN FLOOR SUPPORT WORN AT FWD END FROM CONTACT WITH SPACER BLOCK UNDER SEAT TRACK AT BS 744, RBL 63. REPLACED CABIN F LOOR SUPPORT AT STA 740-760 RBL 63 REF SRM 51-30-2. 2 L 7 3 4F A3WE 2007040400008 20070404 00008 2007 4 4 SWAA071605 4 20070328 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 470WN 33860 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007040400009 20070404 00009 NM 2007 4 4 SWAA071613 1 20070329 A 5330 6518420 SKIN BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR CUTOUT LOWER AFT CORNER. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007040400049 20070404 00049 NM 2007 4 4 07FDEA01233 1 20070402 A 5710 ARB2886503 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LT WING, LEADING EDGE ANTI-ICE TELESCOPIC DUCT CUT-OUT FOUND WITH CRACK APPROX 3/8" IN LENGTH. [SUP 4-20-07] AREA TRIM MED OUT AND REPAIRED AS PER SRM 57-10-00 FIG. 42 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040400051 20070404 00051 NM 2007 4 4 07FDEA01235 1 20070402 A 5313 A5A7114533 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 CTR CARGO COMPARTMENT: RT TUNNEL AREA LONGERON 39R SPLICE AT STA 5-123, FOUND CRACKED. CRACKED LONGERON SPLICE AT CENTE R CARGO COMPARTMENT RH TUNNEL AREA LONGERON 39R AT STA 5- 123 REMOVED AND REPLACED WITH NEW FABRICATED SPLICE AS PER D WG A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOL. II. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040400074 20070404 00074 NM 2007 4 4 SWAA071627 1 20070329 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 706 S1 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007040400084 20070404 00084 NM 2007 4 4 HALA0700148 1 20070331 A 2913 UNKNOWN BOEING 767 767300 1385204 NM HYD PUMP UNKNOWN A HALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 13 592HA 33468 ETOPS SIGNIFICANT SYSTEM, CENTER HYDRAULIC DEMAND PUMP EICAS MESSAGE WITH GEAR. RETRACTION AND FLAP EXTENSION. T/S, EN SURED CENTER HYD SYS WAS PROPERLY SERVICED. ACCOMPLISHED TEST OF CENTER HYD SYS PER AMM 29-11-00-715-896 AND NO DEFECTS FOUND. SYS OPS CKS GOOD. 2 L 7 2 4F RT A1NM 2007040400089 20070404 00089 NM 2007 4 4 SWAA071663 1 20070331 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 847 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040400090 20070404 00090 NM 2007 4 4 SWAA071664 1 20070331 A 5311 6546557 FRAME BOEING 737 7373H4 1384600 NM BS 887 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040400103 20070404 00103 NM 2007 4 4 SWAA071651 1 20070331 A 3350 101114 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED SPV CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007040400104 20070404 00104 NM 2007 4 4 SWAA071657 1 20070331 A 3350 101114 LAMP BOEING 737 737317 138447P NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED MV2 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007040400107 20070404 00107 NM 2007 4 4 SWAA071648 1 20070331 A 3230 284A0002 PSEU BOEING 737 7377H4 1384404 NM E/E BAY FAULTY A SWAA O OTHER J WARNING INDICATION CL CLIMB 1 SW 29 737JW 27869 DURING CLIMBOUT THE NLG EXTENDED WHEN GEAR HANDLE WAS PLACED IN OFF POSITION. CYCLED GEAR, OPERATED NORMAL. PSEU ILLUM INATED ON LANDING. FOUND THREE FAULTS 32-61003, 32-61010, 32-64004, RESET ALL FAULTS PER MM. R&R NOSE GEAR ACTUATOR AN D NOSE GEAR LOCK ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2007040400109 20070404 00109 NM 2007 4 4 SWAA071644 1 20070331 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 450WN 32470 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 2 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007040400118 20070404 00118 EU 2007 4 4 2007UALA00874 1 20070323 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 415UA 475 CABIN EEL BACKSHELLS ARE BROKEN AT CABIN FLOOR LEVEL BY LEFT SIDEWALL AT SEAT ROWS 13 AND 26. [SUP 5-1-07] BACKSHELLS REPLACED AND OP CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007040400120 20070404 00120 EU 2007 4 4 MALA070043 1 20070321 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 296-305 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 408XJ 340B408 DOUBLER ON SEAT TRACK, AT BL0.0 AND STA 296 TO 305 WAS CORRODED OUT OF LIMITS. REMOVED EXISTING REPAIR DOUBLER AND INST ALLED NEW DOUBLER IAW MESABA EOS 53342 REF: EAMS WORK ORDER 215882 TASK 1520. 2 L 7 2 4T RT A52EU 2007040400128 20070404 00128 NM 2007 4 4 2007UALA00942 1 20070329 A 5320 SILL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 817-827 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 AFT CARGO COMPARTMENT LWR SILL ASSY TOP STRAP HAS CORROSION FROM STA 817 TO 827 BETWEEN STR 25R TO 26R RBL 24 TO RBL 25. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED STRAP & REPLACED WITH NEW. 2 L 7 2 4F 4 F RT A16WE E21EU 2007040400133 20070404 00133 NM 2007 4 4 2007UALA00947 1 20070330 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 EMERGENCY CEILING LIGHT ABOVE ROW 11 INOPERATIVE. RELAMPED EMERGENCY LIGHT. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007040400135 20070404 00135 NM 2007 4 4 2007UALA00949 1 20070329 A 3350 20121 POWER SUPPLY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 531UA 25042 L-2 EMERGENCY LIGHT INOPERATIVE. [SUP 4-17-07] REPLACED EMERGENCY POWER SUPPLY CHARGER. OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007040500044 20070405 00044 EA 2007 4 5 TRAX200700436 1 20070329 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ODOR A ASOA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 882AS 7503 LEFT WINDOW HEAT CAUTION MSG, 1 RESET LIGHT CAME BACK ON AFTER 5 MIN WITH A VERY FAINT ELECTRICAL ODOR IN COCKPIT AND GA LLEY WHEN LIGHT CAME BACK ON. A/C RETURNED TO ATL AFTER T/O. FLT 4719 DEL 176 MINS. 2 L 7 2 4F RT A21EA 2007040500045 20070405 00045 EU 2007 4 5 TRAX200700437 1 20070329 A 3350 LIGHT AEROSP ATR72 ATR72 EU ASD INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 EMERGENCY LIGHT OUT ON ASD. 2 H 7 2 4T RT 2007040500046 20070405 00046 EU 2007 4 5 TRAX200700438 1 20070329 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 BOARDING DOOR EMERGENCY LIGHT INOP. 2 H 7 2 4T RT 2007040500047 20070405 00047 EU 2007 4 5 TRAX200700439 1 20070329 A 2432 CHARGER AEROSP ATR72 ATR72 EU FAULTED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 AFTER STARTING ENGINE NR 1, EMERGENCY BATTERY CHARGER FAULT LIGHT ILLUMINATED. 2 H 7 2 4T RT 2007040500050 20070405 00050 EU 2007 4 5 07FDEA01103 1 20070323 A 5330 SKIN PANEL AIRBUS 310 A310304 3930339 EU ZONE 100 GOUGED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 816FD 593 TWO MISDRILLED HOLES THROUGH THE SKIN PANEL, INTERNAL DOUBLER, C17 FLANGE AND CONNECTING FITTINGS AT P44 LT. REPAIR PER FORMED BY REPLACING CONNECTING FITTINGS P44 BY NEW ONES; INSTALLING STEEL REPAIR BUSHES IN SKIN PANEL, INTERNAL DOUBLER C17 FLANGE AND C17 FLANGE USING NEW FASTENERS NSA5022-4 ALL IAW RAS/AS/0006/2007 ISS "A" AND EA 6-5312-106418. 2 L 7 2 4F RT A35EU 2007040500051 20070405 00051 EU 2007 4 5 07FDEA01104 1 20070323 A 5320 A53611511204 GUSSET AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 25 748FD 633 FUSELAGE NOSE SECTION, CORROSION ON FWD PAX DOOR FRAME AREA C14 UPPER CORNER LT, GUSSET A536-11511-204. REPAIR PERFORME D BY REPLACEMENT OF GUSSET AND REWORK IAW EA 6-5312-106395 AND RAS/AS/010/2007 ISS.B. 2 L 7 2 4F RT A35EU 2007040500052 20070405 00052 EU 2007 4 5 07FDEA01106 1 20070323 A 5320 SPLICE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 CRACKS FOUND DURING EMBODIMENT OF EO 6-5310-7-5017-SB A300-53-6123 REV 2-AD2004-20-14, ON SPLICE FITTING C47 LT REPAIR W AS PERFORMED BY REPLACEMENT OF SPLICE FITTING AND REAM UP IAW EA 6-5315-106436 AND RAS /033769/043/2004 ISS.A 2 L 7 2 4F RT A35EU 2007040500053 20070405 00053 EU 2007 4 5 07FDEA01107 1 20070323 A 5320 SPLICE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 CRACKS FOUND DURING EMBODIMENT OF EO 6-5310-7-5017, SB A300-53-6123 REV 2, AD2004-20-14, SPLICE FITTING C47 RT REPAIR P ERFORMED BY REPLACEMENT OF FITTING AND REAM UP IAW EA 6-5315-106436 AND RAS/033769/043/2004 ISS.A, 2 L 7 2 4F RT A35EU 2007040500054 20070405 00054 EU 2007 4 5 07FDEA01110 1 20070323 A 5312 BULKHEAD AIRBUS 310 A310304 3930339 EU ZONE 100 GOUGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 SOME GOUGES FOUND AT BULKHEAD 54, APPROX Y-953 AND Z-957, REPAIR PERFORMED BY BLEND OUT IAW EA 6-5315-106419 AND RAS 049 380/2007 ISS. A 2 L 7 2 4F RT A35EU 2007040500055 20070405 00055 EU 2007 4 5 07FDEA01111 1 20070323 A 5311 A53772991 FRAME AIRBUS 310 A310304 3930339 EU ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 MILLED FRAME CRACKED, C22, P26, RHS REPAIR PERFORMED BY REPLACEMENT OF FITTING IAW EA 6-5313-106374 AND RAS/DABRE/700738 1/2007 ISS. A. 2 L 7 2 4F RT A35EU 2007040500056 20070405 00056 EU 2007 4 5 07FDEA01114 1 20070323 A 3230 224TS05Y CONTROL MODULE AIRBUS 310 A310222 3930315 EU MLG INOPERATIVE A FDEA A UNSCHED LANDING S J AFFECT SYSTEMS WARNING INDICATION CL CLIMB 1 SO 25 417FE 333 UNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF. HANDLE WOULD NOT RAISE ABOVE NEUTRAL DETENT EITHER SYS 1 OR 2. LANDING G EAR CONTROL HANDLE MODULE REPLACED AS AMM 3, 2-31-11-4. GEAR NORMAL EXTENSION/RETRACTION TEST CARRIED OUT AS PER AMM 32 -31-005. FOUND SATISFACTORY. LANDING GEAR ELECTRO VALVE INSPECTION/CHECK CARRIED OUT FOUND SATISFACTORY. WORK CARRIED OUT BY L3885, OFF MFG 224TS05Y. 2 L 7 2 4F RT A35EU 2007040500057 20070405 00057 EU 2007 4 5 07FDEA01116 1 20070323 A 2611 SMOKE DETECTOR AIRBUS 310 A310324 3930206 EU E/E BAY MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 813FD 176 176 500 ON TAKEOFF FROM IND, AT 50' FEET ROTATE MIN EQUIPMENT BAY SMOKE CAME ON. CHECKED THE SNIFFER FAN, DECLARED EMERGENCY AN D CAME BACK AND LANDED. THE ECAM ALERT WENT AWAY ON TURN TO FINAL. NO ODOR WAS NOTED IN FWD EQUIPMENT BAY OR ANY OF TH E LISTED COMPONENTS. CHECKED ALL AREAS FOR WATER. NONE FOUND. INSTALLED NEW MIN EQUIP BAY SMOKE DETECTOR 12WA PER MM 26-15-12-4 AND CHECKED GOOD PER MM 26-15-00-5. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2007040500058 20070405 00058 NM 2007 4 5 NACA20070010 1 20070219 A 5330 SKIN BOEING 737 737232 1384475 NM BS 1088 SCRATCHED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 321DL 23093 AFT FUSELAGE HAS A SCRATCH AT BS 1088, BETWEEN SR 20 AND SR 23. CUT OUT DAMAGED AREA AT AFT FUSELAGE BS 1088 BETWEEN SR 20 AND SR 23 AND FABRICATED REPAIR DOUBLER IAW JOSSAIR DRAWING NR 73R5331545 REV I/R DATED 17 FEB 2007. 2 L 7 2 4F RT A16WE 2007040500059 20070405 00059 EA 2007 4 5 COMA0760298 1 20070402 A 2797 D3899926SC98SN CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA RT WING TE FLAPS FAILED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 479CA 7675 FLIGHT 5577 - FLAPS FAILED CAUTION MESSAGE, FAILED AT 45 DEGREES. REMOVED AND REPLACED RIGHT BPSU CONNECTOR. 2 L 7 2 4F RT A21EA 2007040500060 20070405 00060 EA 2007 4 5 TRAX200700440 1 20070329 A 5312 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BULKHEAD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 830AS 7236 RIGHT OBLIQUE ANGLE AFT OF 621 BULKHEAD IS CRACKED (AS MARKED). REMOVED RT OBLIQUE ANGLE AFT OF621 BULKHEAD. OK TO TREA T AND PRIME RT OBLIQUE ANGLE AND PAINT. OK TO INSTALL. 2 L 7 2 4F RT A21EA 2007040500061 20070405 00061 EA 2007 4 5 TRAX200700441 1 20070329 A 5740 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 830AS 7236 RIGHT WING I/B LEADING EDGE O/B ATTACH ANGLE CRACKED AT RADIUS. REMOVED AND REPLACED RT WING IB LE OB ATTACH ANGLE WITH NEW SERVICEABLE ANGLE P/N 600-12025-8 IAW CRJ MM 20-21-00. 2 L 7 2 4F RT A21EA 2007040500062 20070405 00062 EA 2007 4 5 COMA0760296 1 20070330 A 3297 17300221 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 595SW 7292 FLIGHT 5347 - UPON GEAR RETRACTION RECEIVED A GEAR DISAGREE MOMENTARILY BEFORE THE GEAR SHOWED UP AND LOCKED. REMOVED A ND REPLACED NLG WOW NR 1 WIRE HARNESS. 2 L 7 2 4F RT A21EA 2007040500063 20070405 00063 NM 2007 4 5 NACA20070009 1 20070206 A 5512 SKIN BOEING 737 737232 1384475 NM HORIZONTAL STAB DAMAGED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 321DL 23093 FOUND LT HORIZONTAL STAB LOWER SURFACE DAMAGED, "HAS HOLE". REPAIRED DAMAGED AREA PER JOSSAIR DRAWING NR 73R5511546 REV A DATED 21 FEB 2007. "CUTOUT REPAIR AT STABILIZER BOTTOM SKIN-STAB STA 111.0-STA 120.0". 2 L 7 2 4F RT A16WE 2007040500156 20070405 00156 EU 2007 4 5 07FDEA01159 1 20070328 A 5720 A57965050000 FAIRING AIRBUS 310 A310304 3930339 EU ZONE 500 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 CRACKED SHIM PLATE AT INNER SIDE AFT AREA OF LT NR 3 FLAP TRACK FIXED FAIRING. REPAIR PERFORMED BY WET LAY-UP PER SRM 5 7-20-35 AND INSERT INSTALLATION, APPROVED BY EA 6-5720-106421 AND RAS/FOK/016/2007 ISS. A 2 L 7 2 4F RT A35EU 2007040500157 20070405 00157 EU 2007 4 5 07FDEA01160 1 20070328 A 5730 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 748FD 633 FOUND CORROSION FINDINGS ON RT WING TOP SKIN RIB 1-25 REPAIR PERFORMED BY BLEND IAW EA 6-5720-106375 AND RAS/BAE/1004284 /2007 ISS.A. 2 L 7 2 4F RT A35EU 2007040500158 20070405 00158 EU 2007 4 5 07FDEA01161 1 20070328 A 5720 SHROUD AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 748FD 633 FOUND CORROSION FINDING ON RT WING OUTER SHROUD BOX RIB 25-29 REPAIR PERFORMED BY BLEND OUT IAW EA 6-5720-106375 AND RAS /BAE/1004284/2007 ISS. A. 2 L 7 2 4F RT A35EU 2007040500159 20070405 00159 WP 2007 4 5 07FDEA01162 1 20070328 A 5320 RAIL DOUG DC10 DC1010 3022110 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 CENTER LOWER CARGO, CORROSION ON DOOR JAMB OUTER RAIL FS 1682 LONGERON 43R. COMPLIED WITH FEDEX EA 8-5310-105182 FUSELA GE, CENTER CARGO DOOR RAIL CORROSION AT STA 1681 REPAIR. 2 L 7 3 4F A22WE 2007040500160 20070405 00160 NM 2007 4 5 07FDEA01163 1 20070328 A 5347 BAC1520792 SEAT TRACK BOEING 727 727225 1384077 NM BS 1094-1101 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 MAIN DECK FLOOR SEAT TRACK CROWN IS GOUGED/CORRODED AT BS 1094 - 1101, RBL 25, WL 208. FABRICATED AND INSTALLED REPAIR ON SEAT TRACK, STA 1094 - 1101, RBL 25, WL 208 REF B 727 SRM 53-10-5 PG 1 FIG 1. 2 L 7 3 4F A3WE 2007040500161 20070405 00161 NM 2007 4 5 07FDEA01164 1 20070328 A 5280 69228745 ANGLE BOEING 727 727225 1384077 NM LT MLG DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 LT WING GEAR DOOR LOWER AFT EDGE OF DOOR, ANGLE IS CRACKED REMOVED AND REPLACED AFT LOWER EDGE ANGLE REF SRM 51-30-02 AN D REPLACED SEAL REF MM 32-10-03. 2 L 7 3 4F A3WE 2007040500162 20070405 00162 WP 2007 4 5 07FDEA01115 1 20070323 A 5340 NYB60428 ATTACH ANGLE DOUG MD10 MD1010F 3022112 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 550FE 75522 46521 THE "SUGAR SCOOP", P/N NYB6042-8, IS CRACKED AT THE UPPER OUTB'D CORNER. REMOVED RT "SUGAR SCOOP" (ATTACHMENT ANGLE) FR OM CAC BULKHEAD 1154 PER SRM 51-00-01. INSTALLED NEW ATTACHMENT ANGLE, P/N NYB6042-8, AND SEALED PER SRM 53-40-00. 2 L 7 3 4F RT A22WE 2007040500163 20070405 00163 NM 2007 4 5 SWAA071720 1 20070403 A 5311 6546551 FRAME BOEING 737 7373H4 1384600 NM BS 807 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040600001 20070406 00001 2007 4 6 MWEA070073 4 20070331 A 2565 113317 LANYARD DOUG DC9 DC981 3022081 WP DOOR SLIDE MISALIGNED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 805ME 48031 MAIN CABIN DOOR SLIDE COVER CAME OFF AND GIRT BAR CABLE TO TIGHT. INSPECTED DOOR SLIDE COVER. FOUND SLIDE COVER TO BE INSTALLED PROPERLY. INSPECTED LANYARD CABLE, FOUND CABLE INSTALLED OVER SLIDE GIRT. REMOVED CABLE AND INSTALLED IN COR RECT POSITION. 2 L 7 2 4F A6WE 2007040600003 20070406 00003 NM 2007 4 6 UPS07M49556 1 20070125 A 5753 SKIN DOUG MD11 MD11F 3023600 NM TE FLAP DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE: C RE SKIN LEFT I/B FLAP AFT I/B & O/B SEGMENT DUE MULTIPLE DENTS. REMOVED LEFT WING I/B FLAP SPRING CA RTRIDGE PER AMM27-51-04 R55. REMOVED I/B FLAP O/B AFT SEGMENT PER AMM20-50-02 R55. LEFT WING I/B FLAP & O/B SEGMENT LW R SKIN REMOVED PER SRM 51-31-01 R38. LEFT WING I/B FLAP I/B SEGMENT SKIN FAB PER DWG ARC2736 & ARC2444, AND HOLES PICKE D UP PER SRM 51-31-01 V2 R38. RE -INSTALLATION CUTOUT PER SRM51-31-01V2 R38. OPN CHECK CUTOUT, SATISFACTORY. 2 L 7 3 4F RT A22WE 2007040600004 20070406 00004 CE 2007 4 6 DJFA2007039 1 20070330 A 5531 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE VERTICAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 789TA RK268 DURING A SCHEDULED INSPECTION, MAINTENANCE DISCOVERED A CRACK IN A VERTICAL STABILIZER RIB ABOVE THE ELEVATOR BELLCRANK MOUNTING BRACKET. CRACK WAS .5" LONG AND TERMINATED TO A TOOLING HOLE. CRACK WAS REPAIRED IAW ENGINEERING DATA. 2 H 7 2 4F 4 F RT A16SW E25EA 2007040600008 20070406 00008 NM 2007 4 6 SWAA071699 1 20070403 A 3350 100031 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 286WN 32471 FWD CABIN EMERGENCY EXIT LIGHT LOOSE. SECURED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2007040600009 20070406 00009 NM 2007 4 6 SWAA071696 1 20070403 A 3350 10107451 SIGN BOEING 737 7373Q8 1384670 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 L1 DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007040600010 20070406 00010 NM 2007 4 6 SWAA071684 1 20070402 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007040600012 20070406 00012 NM 2007 4 6 SWAA071695 1 20070402 A 2530 41600019 COFFEEMAKER BOEING 737 7373H4 1384600 NM GALLEY FAULTY A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 373SW 26581 F/A REPORTED ELECTRICAL ODOR COMING FROM AFT GALLEY COFFEEMAKER, F/A PULLED C/B AS PRECAUTIONARY MEASURE. INSPECTED AFT GALLEY AREA ISOLATED FAULT TO NR 1 COFFEEMAKER. REMOVED AND REPLACED NR 1 COFFEEMAKER PER MM. 2 L 7 2 4F RT A16WE 2007040600014 20070406 00014 NM 2007 4 6 07FDEA01195 1 20070330 A 5347 CARGO TRACK BOEING 727 727225 1384077 NM BS 950 LBL 63 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 MAIN CABIN STA 950 AT LBL 63 HAS AREA OF CORROSION AROUND TIE DOWN. FAB NEW TIE DOWN ON TRAVELER T7/670839. REMOVED AN D REPLACED TIE DOWN IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2007040600021 20070406 00021 NM 2007 4 6 SWAA071724 1 20070403 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM BS 907 S23R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, STR 23R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007040600022 20070406 00022 NM 2007 4 6 SWAA071697 1 20070403 A 3350 6556633 SIGN BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 237WN 34632 RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007040600023 20070406 00023 NM 2007 4 6 SWAA071725 1 20070403 A 5753 TORQUE TUBE BOEING 737 7373H4 1384600 NM RT WING TE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 2014 28330 DURING SCHEDULED 10Y CHECK, FOUND RIGHT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED MID FL AP PER MM. 2 L 7 2 4F RT A16WE 2007040600024 20070406 00024 NM 2007 4 6 SWAA071726 1 20070403 A 5753 TORQUE TUBE BOEING 737 7373H4 1384600 NM RT WING TE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 2014 28330 DURING SCHEDULED 10Y CHECK, FOUND RIGHT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED MID F LAP PER MM. 2 L 7 2 4F RT A16WE 2007040600025 20070406 00025 NM 2007 4 6 SWAA071705 1 20070403 A 5754 STRUCTURE BOEING 737 7373H4 1384600 NM NR 6 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED C1 CHECK, FOUND RIGHT WING NR 6 L/E SLAT CRACKED AT OUTBOARD T/E. REPAIRED SLAT PER SWA EA. 2 L 7 2 4F RT A16WE 2007040600026 20070406 00026 NM 2007 4 6 SWAA071669 1 20070401 A 3350 65C27093 LIGHT BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 L2 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007040600027 20070406 00027 NM 2007 4 6 SWAA071668 1 20070401 A 3350 65C27093 LIGHT BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 R2 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007040600029 20070406 00029 NM 2007 4 6 SWAA071709 1 20070403 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007040600030 20070406 00030 NM 2007 4 6 SWAA071671 1 20070401 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM BS 717C S23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 717C, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007040600031 20070406 00031 NM 2007 4 6 UPS07M49581 1 20070207 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1961 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:C CABIN: LEFT SEAT TRACK AT STA 1961, X=107.25 FOUND CORRODED AS MARKED. FASTENERS AT CABIN SEAT TRACK REMOVED SRM 51-31-01 VOL II. DAMAGED AREA TRIMMED OFF SRM 53-70-00 FIG 1 VOL I. HFEC INSP CARRIED OUT & NO CRACK EVID ENT. HOLES ON NEW SEAT TRACK PICKED UP SRM 51-31-01 VOL II. SPLICE PARTS FAB, HOLES ON SPLICE PARTS PICKED UP, SPLICE PARTS PROTECTED & PAINTED. SPLICE PARTS & SEAT TRACK INSTALLED SRM 51-31-01 VOL II REV 38. 2 L 7 3 4F RT A22WE 2007040600033 20070406 00033 NM 2007 4 6 UPS07M49583 1 20070318 A 5754 ARB2850506 ATTACH FITTING DOUG MD11 MD11F 3023600 NM RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 271UP 48572 INSPECTION TYPE:3C RIGHT WING LEADING EDGE O/B SLAT TRACK NR 5 FITTING IS CRACKED. REMOVED AND REPLACED SLAT TRACK FITT ING IAW MD-11 SRM 51-31-01 & 51-35-01. 2 L 7 3 4F RT A22WE 2007040600034 20070406 00034 NM 2007 4 6 UPS07M49530 1 20070226 A 5315 FLOORBEAM DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C CTR CARGO COMPT: ALONG BS 1781, ALONG RBL 45.75 (X=-45.75) FLOORBEAM WEB UPPER TEE FOUND CORRODED; AF TER ROLLER TRAY REMOVAL. ATTACH CORROSION AREA & INNER PARTS REMOVED FOR ACCESS PER SRM 51-31-01 V2 R38. T-CHORD UPPER CORROSION MAT REMOVED PER SRM 51-21-01 V1 R38. REPAIR TEE SUPPORT & ANGLE FAB PER EN1135-07, FPI CUTOUT ON FAB TEE & A NGLE FOUND CRACK EVIDENT. OK TO INSTALL. REPAIR TEE & ANGLE, RE-INSTALLED PER EN1135-07 & SRM 51-31-01 V2 R38, FOUND S ATISFACTORY. 2 L 7 3 4F RT A22WE 2007040600039 20070406 00039 NM 2007 4 6 07FDEA01179 1 20070329 A 5510 65241892 BEAM BOEING 727 727225 1384077 NM HORIZONTAL ZONE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 LT HORIZONTAL STAB T/E LWR BEAM BESIDE NR 5 RIB FROM I/B HAS CRACK. REPAIRED LT HORIZONTAL STAB LWR BEAM IAW SRM 55-10- 6 FIG 1. PREPPED AND PAINTED. REPAIRED AREA IAW AMM 51-20-151-7. 2 L 7 3 4F A3WE 2007040600046 20070406 00046 NM 2007 4 6 SWAA071708 1 20070403 A 3350 OL3071BPEGL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 407WN 29817 DURING SCHEDULED MV3 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 13 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007040600048 20070406 00048 CE 2007 4 6 DXTA200702078 1 20070404 A 3150 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL UNKNOWN E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 912QS 7500012 RED NO TAKEOFF CAS MESSAGE ON TAKEOFF ROLL. AFTER NULLING SPEED BRAKE INDICATION , SYSTEM OPS CHECK GOOD ON ENGINE RUN IAW CE 750 MM 71-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007040600049 20070406 00049 CE 2007 4 6 DXTA200702081 1 20070404 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG NONE E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 341QS 5600341 BOTH CAPTAIN'S AND FO'S BRAKES TEND TO GRAB AND SEEM SOME WHAT SPONGY. IAW CE560MM CHAP 32-42-00 BLED THE COMPLETE BRAK E SYSTEM OPS AND LEAK CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2007040600050 20070406 00050 CE 2007 4 6 DXTA200702079 1 20070404 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG FAULTED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 363QS 5600536 F/O BRAKES LITTLE TO NO EFFECT DURING FIRST 80 PERCENT OF TRAVEL WORKED DURING LAST PART BUT SOFT. NEEDED TO BE PUMPED A T LEAST TWICE TO GET RESISTANCE BUT FADED FAST CAPT SIDE FELT NORMAL. NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A22CE E25EA 2007040600051 20070406 00051 NM 2007 4 6 UPS07449578 1 20070329 A 2910 MODULE BOEING 747 747121 1384871 NM NR 3 HYD SYSTEM UNKNOWN A IPXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 683UP 20353 HYD SYSTEM 3 FAILURE PRESSURE & QUANTITY ZERO DURING FLAP RETRACTION. HYD SYSTEM PR & QT LIGHTS ON. REMOVED AND REPLAC ED MODULAR ASSY & LEAK CHECK IAW 29-11-23. 2 L 7 4 4F A20WE 2007040600053 20070406 00053 WP 2007 4 6 UPS07849575 1 20070322 A 5311 FRAME SPLICE DOUG DC8 DC873F 302199F WP FS 1690 L24L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C3 L24L END FITTING CRACKED ON AFT SIDE OF STA 1690 FRAME SPLICE. REMOVED END FITTING AT STA 1690 L24L IAW SRM 51-1-21. DRILLED, REAMED AND INSTALLED END FITTING AT STA 1690 L24L IAW SRM 51-3-2 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007040600054 20070406 00054 WP 2007 4 6 UPS07849576 1 20070321 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FS 1790 LBL8 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C3 FLOORBEAM STA 1790 LBL 8 HAS DEEP GOUGE AND EXFOLIATED CORROSION. REMOVED FLOORBEAM AT STA 1790 LBL 8 IAW SRM 51-3-0. FABRICATED AND INSTALLED FLOORBEAM AT STA 1790 LBL 8 IAW SRM 53-7-3, AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 2007040600055 20070406 00055 WP 2007 4 6 UPS07849577 1 20070313 A 5322 SHEAR TIE DOUG DC8 DC873F 302199F WP FS 660 L35L-35R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C3 SHEAR TIE CORRODED AT STA 660 L35R TO L35L. REMOVED SHEAR TIE AT STA 660 L35R-L35L IAW SRM 51-1-21. FABRICATED AND INSTALLED SHEAR TIE AT STA 660 L35L-L35R IAW DWG 5616509, AND SRM'S 51-1-20D, AND 51-1-21. 2 L 7 4 4F RT 4A25 2007040600057 20070406 00057 NM 2007 4 6 UPS07M49579 1 20070123 A 5753 NRC6753503 FITTING DOUG MD11 MD11F 3023600 NM LT WING TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE: C, LT WING O/B TRAILING EDGE FLAP UP-STOP FITTING CRACKED AS MARKED AT O/B FLAP I/B MOUNTED HINGE AREA , LEADING EDGE AREA. ALL REMOVAL OF LEFT WING O/B FLAP I/B & O/B SUPPORT CUT OUT PER AMM 20-50-02 R55 TO GAIN ACCESS TO REMOVE & RE-INSTALL NEW O/B TRAILING EDGE FLAP ASSY, P/N NRC 6753-503. RE-INSTALL CUT OUT PER AMM 20-50-02 R55 ON LEFT WING O/B TRAILING EDGE FLAP UP-STOP FITTING, FOUND SATISFACTORY. FOR OPS CHECK DETAIL PLS CROSS REFER TO EO MD11-5750- 23556-C, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007040600058 20070406 00058 NM 2007 4 6 UPS07M49580 1 20070123 A 5753 6753504 STOP FITTING DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C RIGHT WING O/B TRAILING EDGE FLAP UP-STOP CRACKED AS MARKED AT O/B FLAP I/B FLAP MOUNT HINGE AREA, LEA DING EDGE AREA. ALL REMOVAL OF RIGHT WING O/B FLAP I/B & O/B SUPPORT CUT OUT PER AMM20-50-02 R5 R55 TO GAIN ACCESS TO R EMOVE & RE-INSTALL NEW O/B TRAILING EDGE FLAP ASSY P/N NRC6753-504. RE-INSTALL CUT OUT PER AMM20-50-02 R55 ON RIGHT WIN G O/B TRAILING EDGE FLAP UP-STOP FITTING, FOUND SATISFACTORY. FOR OPS CHECK DETAILS PLS CROSS REFER TO EO MD11-5750-235 56-C, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007040600060 20070406 00060 NM 2007 4 6 MWEA070064 1 20070327 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 286 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 701ME 49760 HOLE IN FUSELAGE, LEFT SIDE STATION 286, LONGERON 23 LEFT APPROXIMATELY 2 INCH DIAMETER. FABRICATED AND INSTALLED DOUBE LR. 2 L 7 2 4F RT A6WE 2007040600063 20070406 00063 NM 2007 4 6 07FDEA01202 1 20070330 A 5754 SKIN BOEING 727 727225 1384077 NM ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 NR 5 SLAT FENCE IS DELAMINATED ON LEADING EDGE REMOVED DAMAGE AND REPAIRED AREA REF SRM 51-40-09 PG 3-7. APPLIED CONDUC TIVE COATING REF MM 51-20-051-7. PRIMED AND PAINTED REPAIR REF MM 51-20-151-7. 2 L 7 3 4F A3WE 2007040600064 20070406 00064 NM 2007 4 6 07FDEA01203 1 20070330 A 5320 661282411 ANGLE BOEING 727 727225 1384077 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 LOWER AFT PIT LOWER LT SIDEWALL ATTACH CLIP IS CRACKED AT STA 950F ABOVE STR 26L. FABRICATED AND REPLACED BROKEN CLIP R EF BOEING DRAWING 66-12821 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2007040600065 20070406 00065 NM 2007 4 6 07FDEA01204 1 20070330 A 5315 6557567 SPLICE BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 LOWER AFT PIT FLOOR STRUCTURE FLOOR PANEL SPLICE STRAP AT STA 980 4" HAS CORROSION ON UNDERSIDE AT MANY NUTPLATES AND CRACKED AT RBL 8. MANUFACTURED STRAP PER BOEING DWG 65-57567. REMOVED AND REPLACED AFT PIT FLOOR SPLICE STRAP REF SRM 51-30-07. 2 L 7 3 4F A3WE 2007040600066 20070406 00066 NM 2007 4 6 07FDEA01205 1 20070330 A 7810 2510003 FAIRING BOEING 727 727225 1384077 NM ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 NR 1 ENGINE S/N 700479 TAIL PIPE FAIRING HAS GROOVE WORN INTO IT AT 3 O'CLOCK POSITION FROM 1" AFT OF FWD EDGE TO 18" AF T OF FWD EDGE. REPLACED DAMAGED ENG NR 1 I/B TAILPIPE FAIRING REF SRM 51-30-2 ITEM 9. 2 L 7 3 4F A3WE 2007040600069 20070406 00069 CE 2007 4 6 DXTA200702071 1 20070403 A 3397 WIRE CESSNA 750 750 2076810 CE LANDING LIGHT DAMAGED E DXTA C ABORTED TAKEOFF E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 07 951QS 7500151 APPROXIMATELY 40 KTS ON TAKEOFF ROLL AIRCRAFT SHIMMEYED VIOLANTLY TAKEOFF ABORTED YAW DAMP OFF LOWER NOTED IN NOTED IN E ICAS. VISUAL INSPECTION NOTED NOSE GEAR CENTERED 90 DEGREES RT TAXI LIGHT BROKEN. AIRCRAFT TOWED IN TO THE RAMP. INSPEC TED NOSE GEAR, FOUND TAXI LIGHT GOING AND WIRES DAMAGED ALSO FOUND BOTH TAXI LIGHT ASSY DAMAGE, FOUND BOTH NOSE TIRES CH INES WORN OFF. DETERMINED CAUSE OF DAMAGE TO BE FROM NOSE TORQUE LINK NOT PROPERLY SECURED BEFORE TAXI AND TAKEOFF. CONN ECTED TORQUE LINKS PERMORMED TAXI CHECK BEFORE REPAIRS WHERE DONE CHECK GOOD 2 L 7 2 4J RT T00007WI 2007040600072 20070406 00072 CE 2007 4 6 DXTA200702077 1 20070403 A 3240 BRAKE ASSY CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG HOT E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 668QS 5605268 RT BRAKE EXCESSIVELY GRABS AND WHEN INSPECTED IS EXTREMELY HOT. PERFORMED TAXI CHECK. FOUND EVEN APPLICATION WHEN BRAKI NG. BRAKES USUALLY EXTREMELY HOT AFTER LANDING AND TAXING. BOTH BRAKES VERY WARM. FOUND RT BRAKE WEAR INDICATOR AT .15" WHICH GIVES OUT TO 118 LANDINGS LEFT IN BRAKE. BRAKE IS IN SERVICABLE CONDITION AT THIS TIME IAW CITATION 560XL MM 32-40 0-3. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007040600073 20070406 00073 NM 2007 4 6 DXTA200702075 1 20070403 A 4900 APU AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 265QS 165 APU GIVES OIL ODOR IN CABIN. NO DIVERSION. REMOVED AND REPLACED APU IAW FALCON 2000 MM 49-00, OPS CHECK APU GOOD. 2 K 7 2 4F 4 F RT A50NM E44NE 2007040600075 20070406 00075 NM 2007 4 6 MWEA070068 1 20070330 A 3510 E7403300 LATCH BOEING 717 717200 1383700 NM OXYGEN MASK BROKEN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 920ME 55182 OXYGEN MASK LATCH BROKEN. REMOVED AND REPLACED FLIGHT ATTENDANT OXYGEN MASK DOOR LATCH. 2 L 7 2 4F TR A6WE 2007040600077 20070406 00077 NM 2007 4 6 MWEA070072 1 20070331 A 7830 DOOR BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 913ME 55176 CRACK DISCOVERED ON THE RIGHT LOWER THRUST REVERSER BUCKET DOOR APPROXIMATELY .25 INCH LONG ON THE ZEE FRAME AT STATION 26.666. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2007040600080 20070406 00080 NM 2007 4 6 07FDEA01186 1 20070329 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 680 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 CABIN FLOORBEAM FS 680,BL-0 TO RBL 24.75 CORRODED ON UPPER SURFACE. REMOVED CORROSION IAW SRM 51-10-06, ORIGINAL MATERI AL IS .125" MATERIAL LOSS IS .011", MATERIAL REMAINING IS .114", IT IS OUT OF LIMIT IAW SRM P TO F 63-10-1. REMOVED DAM AGED IAW SRM 53-10-08. RECEIVED ANGLES FABRICATED ON MAE TRAVELER T7/669483 AND T7/669482. FABRICATED STRAPS FROM MAT ID 7075-T6 .50 AND 7075-T6 .080 IAW SRM 53-10-8. LOCATE AND DRILLED PARTS IAW SRM 53-10--8 FIG 3. TREATED AND PRIMED R EPAIR PARTS IAW SRM 51-10-02. INSTALLED REPAIR PARTS IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2007040600083 20070406 00083 EU 2007 4 6 07FDEA01189 1 20070329 A 5310 FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 MAIN CARGO DECK FRAME 12A FITTING RT SIDE FOUND CRACKED. REMOVED AND REPLACED FITTING ON EO NR 6-5340-7-5002 A PART 2 A ND PART 3. 2 L 7 2 4F RT A35EU 2007040600085 20070406 00085 EU 2007 4 6 07FDEA01191 1 20070330 A 5712 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 600 MISMANUFACTURED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 748FD 633 EDGE MARGIN TO SHORT FOR TEMPORARY REPAIR ON RIB 5 IAW DR 426 REPAIR PERFORMED BY INSTALLATION ADDITIONAL FASTENER IAW E A 6-5710-108975 AND RAS/BAE/1004080/2006 A. 2 L 7 2 4F RT A35EU 2007040600086 20070406 00086 NM 2007 4 6 07FDEA01193 1 20070330 A 5343 ACA7017501 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 NLG LT TRUNNION FITTING FOUND CRACKED. [SUP 4-20-07] NLG LT TRUNNION FITTING REPAIR CARRIED OUT AS PER FEDEX EA 1-5310 -109844. LT NOSE LANDING TRUNNION WEB CRACKED, STOP DRILL DEVIATION FROM SRM & SRM 53-40-00 FIG. 22 VOL I. REPAIR CLAS SIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040600087 20070406 00087 WP 2007 4 6 AALA20070561 1 20070326 A 2530 COFFEEMAKER DOUG DC9 DC982 3022082 WP GALLEY SMOKE A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 274AA 49271 ACRID ODOR THROUGH AIR CONDITIONING SYSTEM AND SMOKE REPORTED IN CABIN BY FLIGHT ATTENDANT, PASSENGERS, AND DEADHEADING CREW DURING CLIMB-OUT. CREW TURNED OFF GALLEY POWER AND SMOKE DISSIPATED AT FLIGHT LEVEL 050. FLIGHT CONTINUED TO DFW AND LANDED WITHOUT INCIDENT. FOUND SMOKE COMING FROM NUMBER FOUR COFFEE MAKER. REPLACED NUMBER FOUR COFFEE MAKER AND C HECKED APU FOR OIL INGESTION AND OIL LEAKS. REPLACED COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007040600091 20070406 00091 NE 2007 4 6 AALA20070563 2 20070326 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RIGHT STALLED A AALA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SW 21 466AA 49596 718512 AT FLIGHT LEVEL 240, RIGHT ENGINE COMPRESSOR STALLED. ENGINE GAS TEMPERATURE ROSE TO 750. UNCOMMANDED ENGINE SHUTDOWN . DUE TO INABILITY TO MAINTAIN RUDDER CONTROL MISSED APPROACH. WAS UNABLE TO CONTROL RUDDER UNTIL POWER PULL BACK ALL THE WAY. LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME 50 MINUTES. FOUND METAL IN TAIL PIPE. REPLACED NUMBER TWO ENGIN E ON 27 MAR 2007 AT IAD AND REPLACED ISOLATORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007040600092 20070406 00092 WP 2007 4 6 AALA20070555 1 20070325 A 3020 VALVE DOUG DC9 DC983 3022083 WP ANTI-ICE SYSTEM INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 9618A 53565 RIGHT ENGINE ANTI-ICE VALVE INDICATION ILLUMINATED WITH SWITCH ON. RECYCLED SWITCH AND CIRCUIT BREAKER WITH NO HELP. R ETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED RIGHT ENGINE ANTI-ICE VALVE NOSE COWL AND PERFORMED OVE RWEIGHT LANDING INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007040600093 20070406 00093 EU 2007 4 6 AALA20070557 1 20070325 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70074 517 MIA - EMERGENCY LIGHT AT SEAT 10C IS MISSING. REPLACED EMERGENCY LIGHT AT SEAT 10C. SYSTEM GROUND CHECKED NORMAL OPERA TION. 2 L 7 2 4F RT A35EU 2007040600094 20070406 00094 NM 2007 4 6 AALA20070560 1 20070325 A 2722 658D1003 ACTUATOR BOEING 757 757223 1384957 NM RUDDER INOPERATIVE A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 695AN 26975 DURING CRUISE RUDDER TRIM WOULD NOT RESPOND LEFT OR RIGHT. DIVERTED TO LAS AND LANDED WITHOUT INCIDENT. REPLACED RUDER TRIM ACTUATOR AND OVERHEAD CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007040600096 20070406 00096 NM 2007 4 6 AALA20070549 1 20070320 A 3150 UNKNOWN BOEING 767 767223 1385123 NM TE FLAPS UNKNOWN A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 329AA 22329 WHEN SELECTING LANDING FLAPS EICAS TRAILING EDGE FLAP ASYMMETRY MESSAGE ILLUMINATED. PERFORMED CHECKLIST AND EICAS MESS AGE WENT AWAY. STATUS MESSAGE FOR TRAILING EDGE FLAP SHUTDOWN STAYED ILLUMINATED. LANDED BDA WITHOUT INCIDENT. PERFOR MED BITE TEST ON FLAP/SLAT UNIT WITH NO FAULTS NOTED. OPERATED FLAPS HYDRAULICALLY TO 30 DEGREES WITH NO STATUS MESSAGE . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007040600102 20070406 00102 NM 2007 4 6 P5CA0701517 1 20070323 A 2750 CONTROL UNIT BOEING 747 74746NF 13848BT NM TE FLAPS UNKNOWN A P5CA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 15 453PA 30811 MULTIPLE STATUS MESSAGES: "STAB AUTO TRIM," "RUDDER RATIO," "NO LAND 3," AND "FLAP CONTROL R." PERFORMED OPERATIONAL CH ECKS ASSOCIATED WITH SPECIFIC MESSAGES AND RERACKED FLAP CONTROL UNIT PER MM 27-50-00. 2 L 7 4 4F RT A20WE 2007040600106 20070406 00106 NM 2007 4 6 07FDEA01209 1 20070330 A 5532 65C1862811 PANEL BOEING 727 727225 1384077 NM ZONE 300 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 VERTICAL STABILIZER PANEL 9511 IS DELAMINATED REMOVED DAMAGE AND REPAIRED PANEL, THEN APPLIED CONDUCTIVE COAT, PRIMED AN D PAINTED REFERENCE SRM 51-40-09 PAGE 4, AND MM 51-21-121-7. 2 L 7 3 4F A3WE 2007040600107 20070406 00107 NM 2007 4 6 07FDEA01210 1 20070330 A 5753 6521630250 DOOR BOEING 727 727225 1384077 NM ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 RT IB FORE FLAP INBD UPPER HINGED LE DOOR HAS DEEP WEAR REMOVED AND REPLACED RT INBD FORE FLAP REF MM 27-51-001-4 PAGE 2 . TQ WRNCH NR AAR 19624 DUE 8-19-07. 2 L 7 3 4F A3WE 2007040600118 20070406 00118 NM 2007 4 6 AWXA200700460 1 20070310 A 5754 65C2679913 SKIN BOEING 737 7373G7 1384595 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - LEFT WING NR 1 SLAT LOWER SURFACE CRACKED, SS 255 - SS 258.87. REPAIRED LEFT WING NR 1 SLAT LOWER SURFACE, SS 25 5 - SS 258.87 IAW B737-300 SRM 57-43-01-2R6 FIGURE 201. 2 L 7 2 4F RT A16WE 2007040600119 20070406 00119 NM 2007 4 6 AWXA200700461 1 20070315 A 5311 654652525 FRAME BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - CRACKED FRAME, BS 380, S27L. REPAIRED FRAME, BS 380, S27L IAW B737-300 SRM 53-00-07-2R4, FIGURE 201. 2 L 7 2 4F RT A16WE 2007040600120 20070406 00120 EU 2007 4 6 AWXA200700462 1 20070323 A 5320 D53112198200 FITTING AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - FOUND CORROSION ON L1 DOOR CUT OUT LOWER SILL CENTER FITTING, FR 16 + 5" - FR 19 + 4". REPLACED L1 DOOR CUT OUT L OWER SILL CENTER FITTING, FR 16 + 5" - FR 19 + 4" IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007040600121 20070406 00121 EU 2007 4 6 AALA20070552 1 20070325 A 5210 BOTTLE AIRBUS 300 A300B4605R 3930308 EU PAX DOOR ASSIST LOW PRESSURE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80058 466 MIA - EMERGENCY ASSIST BOTTLE AT RIGHT NUMBER TWO DOOR HAS LOW PRESSURE. SERVICED EMERGENCY ASSIST BOTTLE AT RIGHT NUMBE R TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007040400045 20070404 00045 NM 2007 4 4 SWAA071650 1 20070331 A 5753 SKIN BOEING 737 7373H4 1384600 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 1029 24375 DURING SCHEDULED SERVICE CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT LOWER OUTBOARD END. REMOVED AND R EPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2007040400046 20070404 00046 NM 2007 4 4 SWAA071661 1 20070331 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040400047 20070404 00047 NM 2007 4 4 SWAA071662 1 20070331 A 5311 6546551 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040400052 20070404 00052 NM 2007 4 4 07FDEA01236 1 20070402 A 5710 ARB11231 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LT WING, LEADING EDGE SLAT NR 10 TRACK CUT OUT FOUND WITH CRACK. [SUP 4-20-07] TRACK CUT OUT REPAIR CARRIED OUT AS PER SRM 57-10- 00 FIG. 21 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040400058 20070404 00058 NM 2007 4 4 07FDEA01242 1 20070402 A 5751 SKIN BOEING 727 727225 1384077 NM AILERON DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 LT WING OTBD AILERON IS DELAMINATED AT THE OTBD T/E. LT OB AILERON WAS REPAIRED ON SHOP WO NR 11841-5000-0003 REFERENCE SRM 51-40-20. LT OB AILERON IS INSTALLED AND RIGGED ON SNRM NR N00554. 2 L 7 3 4F A3WE 2007040400062 20070404 00062 EU 2007 4 4 AWXA200700427 1 20070329 A 3350 321431 BATTERY AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHT FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 644AW 317 LAS - EEL - MID LEFT EMERGENCY LIGHT BATTERY FAULT. MX REPLACED THE LEFT MID EMERGENCY LIGHTING BATTERY. OPERATIONAL C HECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007040400063 20070404 00063 EU 2007 4 4 AWXA200700428 1 20070331 A 3350 321431 BATTERY AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHT FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 632AW 81 PHX - EEL - RIGHT OVERWING EMERGENCY LIGHTS FAULTED. MX REPLACED THE RIGHT OVERWING EMERGENCY LIGHT BATTERY PACK. OPER ATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007040400091 20070404 00091 NM 2007 4 4 SWAA071643 1 20070331 A 5312 6546568 BULKHEAD BOEING 737 7373Q8 1384670 NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, LBL 23, WL 193. REPAIRED WEB PER BOEING SB AND SRM. 2 L 7 2 4F RT A16WE 2007040400095 20070404 00095 NM 2007 4 4 SWAA071659 1 20070331 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 700 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 700, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007040400097 20070404 00097 2007 4 4 SWAA071647 4 20070331 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM R2 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007040400098 20070404 00098 NM 2007 4 4 DHL2007786511 1 20070320 A 5320 SHEAR ANGLE BOEING 727 727214 138407R NM BS 990 S28L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 AFT CARGO COMPARTMENT AT BS 990 AND STR 28L, SHEARTIE HAS CORROSION. REMOVED FLOOR SUPPORT LT STA 990 TO 950E. REMOVED Z ANGLE SUPPORT STA 990 IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA AFT CARGO COMPARTMENT SHEARTIE, DIMENSION 3 BY 6 IA W B727 SRM 53-10-4, FIG 13. FABRICATED SHEARTIE REPAIR FROM, 7075T6, .063, 6.50 BY 3. DOUBLER 8 BY 4.50, IAW B727 SRM 53-10-4. TREATED ALODINE, PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007040400102 20070404 00102 NM 2007 4 4 SWAA071652 1 20070331 A 3350 101114 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED SPV CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007040400110 20070404 00110 NM 2007 4 4 SWAA071658 1 20070331 A 3397 487191 CONNECTOR BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 257WN 32515 DURING SCHEDULED MV2 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2007040400115 20070404 00115 NM 2007 4 4 DHL2007786510 1 20070320 A 5322 SHEAR TIE BOEING 727 727214 138407R NM BS 1148 S28L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 AFT CARGO COMPARTMENT AT BS 1148 AND STR 28L, SHEARTIE HAS CORROSION. CUT OUT DAMAGED AREA AT AFT CARGO COMPARTMENT SHE ARTIE, DIMENSION 4.50 BY 1.75 IAW B727 SRM 53-10-4, FIG 13. FABRICATED SHEARTIE REPAIR FROM, FILLER 7075T6, .063, 1.1 B Y 1 BY 4.75, DOUBLER FROM 7075T6, .071, 3.10 BY 5.70 IAW B727 SRM 53-10-4, FIG 13. TREATED ALODINE AND PRIMED IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007040400116 20070404 00116 NM 2007 4 4 2007UALA00872 1 20070325 A 5730 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE WING DAMAGED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 127UA 28813 727897 RTFL UNDER AMBER ALERT DUE TO INFLIGHT DAMAGE TO NR 4 ENGINE INBOARD SAILBOAT FAIRING. [SUP 4-20-07] FOUND ONE SAILTAI L PANEL MISSING & ONE DAMAGED. ROBBED MISSING UNIT & INSTALLED. ACCOMPLISHED HFEC INSPECTION OF BLENDED RT LOWER WING SKIN JUST INBD OF NR 4 ENGINE PYLON SAILTAIL & SURROUNDING FUEL PLATE. NO CRACKS FOUND AND MATERIAL LOSS WITHIN SERVICE ABLE LIMITS. SURROUNDING FUEL PLATE ALSO REPLACED. A/C OK FOR SERVICE. SUSPECT PANELS WERE NOT PROPERLY SECURED & VIBRAT ED LOOSE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007040400119 20070404 00119 EU 2007 4 4 MALA070044 1 20070325 A 2150 ACM SAAB SF340 340B 7860101 EU LEFT FROZEN A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 15 420XJ 340B420 FA NOTED A SMOKE ODOR IN THE CABIN BRIEFLY DURING DESCENT. MX FOUND THE ACM FROZEN UP WHEN IT GOT IN. REPLACED LT ACM. 2 L 7 2 4T RT A52EU 2007040400122 20070404 00122 NM 2007 4 4 2007UALA00890 1 20070325 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 960 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 508UA 24744 MAIN DECK FLOORBEAM AREA, WEB IS CORRODED AT BS 960, RBL 67. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED FLOORBE AM WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2007040400123 20070404 00123 NM 2007 4 4 2007UALA00891 1 20070323 A 3350 CAP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 EEL STRIP COVER AND END MISSING AT 14B ACROSS FROM B-C GALLEY. -SUP 4-17-07- REPLACED EEL STRIP END CAP LIGHTS. EEL S YSTEM OP CHECKD NORMALLY PER MM 33-51-00. 2 L 7 2 4F 4 F RT A1NM E24NE 2007040400124 20070404 00124 NM 2007 4 4 2007UALA00892 1 20070325 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 143 S25R DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 662UA 27159 FUSELAGE DAMAGE SECTION 41 APPROX STA 143 S25R, DENT APPROX 1 FT X 2 FT. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SK IN. FABRICATED & INSTALLED SKIN SECTION & DOUBLERS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007040400136 20070404 00136 NM 2007 4 4 2007UALA00950 1 20070329 A 3397 JUMPER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 545UA 25323 CABIN FLOOR EEL LIGHT STRIP FEEDER AND JUMPER CONNECTION. REPLACED FEEDER AND JUMPER AND OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007040400137 20070404 00137 NM 2007 4 4 2007UALA00951 1 20070329 A 4990 PUMP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE APU OIL SYSTEM MALFUNCTIONED A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 666UA 29238 APU OIL CONSUMPTION IS EXCESSIVE. [SUP 4-20-07] APU WAS REMOVED FROM AIRCRAFT FOR HIGH OIL CONSUMPTION. OIL CONSUMPT ION WAS INVESTIGATED AND CONFIRMED IN THE TEST CELL. THE LRU OIL PUMP WAS REPLACED AND ALL HOC WAS GONE. WITH PROPER T ROUBLESHOOTING, THIS APU COULD HAVE BEEN REPAIRED WITH THE APU STILL IN THE AIRCRAFT. THE REMOVAL OF THIS APU WAS UNNEC ESSARY. THE OIL PUMP IS A LINE REPLACEABLE UNIT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007040400139 20070404 00139 2007 4 4 QXEA200700508 4 20070402 A 3100 LAMP DHAV DHC8 DHC8202 2809007 NM INDICATOR INOPERATIVE A QXEA D RETURN TO BLOCK P NO WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 356PH 502 PDX FLIGHT NR 2170, NR 2 TANK AUX PUMP LIGHT OUT. MAINTENANCE RELAMPED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007040500129 20070405 00129 NM 2007 4 5 07FDEA01042 1 20070321 A 5322 53FX14432 SHEAR TIE BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 MAIN DECK BODY FRAME WEB AND SHEAR TIE HAVE 2 SHORT PITCH (0.25') MISDRILLED FASTENER HOLES BS 640, STR 5R. REF SNRM N00674. REMOVED DAMAGE FROM WEB, FABRICATED AND INSTALLED REPAIR AND NEW SHEAR TIE. TREATED AND PRIMED REPAIR PARTS IA W EA 7-5310-107003. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007040500130 20070405 00130 NM 2007 4 5 SWAA071719 1 20070403 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM BS 380 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040600007 20070406 00007 CE 2007 4 6 DJFA2007041 1 20070402 A 5511 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 408CW RK108 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE RT IB HORIZONTAL STA BILIZER, THE LT AND RT RIBS AND BRACKETS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. BOTH RIB ASSEMBLIES WERE REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007040600032 20070406 00032 NM 2007 4 6 UPS07M49582 1 20070318 A 5754 ARB2850505 ATTACH FITTING DOUG MD11 MD11F 3023600 NM LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 271UP 48572 INSPECTION TYPE:3C LEFT WING FIXED LEADING EDGE I/B SLAT TRACK FITTING AT STA XOS 1005 IS CRACKED. REMOVED AND REPLACED LEFT WING FIXED LEADING EDGE I/B SLAT TRACK FITTING AT XOS 1005 IAW MD-11 SRM 51-31-01 & 51-35-01. 2 L 7 3 4F RT A22WE 2007040600035 20070406 00035 NM 2007 4 6 07FDEA01175 1 20070328 A 3233 ACG74015001 ACTUATOR DOUG MD11 MD11F 3023600 NM ZONE 700 FAILED A FDEA J A DUMP FUEL UNSCHED LANDING S J AFFECT SYSTEMS WARNING INDICATION CL CLIMB 1 SO 25 607FE 18377 18377 48547 AFTER T/O, NOSE GEAR WOULD NOT RETRACT VERIFIED DOWN LOCKED ON PRI AND SECONDARY INDICATIONS, RECYCLED GEAR NUMEROUS TIM ES IN FLIGHT. NO HELP, WRITE-UP CONTINUES ANOTHER WRI 32-30 0002077. WHILE CONFIG FOR LANDING APPROX 200 KIAS DESCEN DING FROM 7000 FT W/ GEAR HANDLE UP AND NOSE GEAR UNSAFE THE NOSE GEAR RETRACTED. TAKEOFF (RETRACT) SPEED WAS APPROX 18 0 KIAS NOSE GEAR WOULD NOT RETRACT ON APPROACH, AT 180KTS, GEAR RETRACTED OK GEAR SLOW TO RETRACT. VISUALLY CHECKED NO SE GEAR AND COMPARTMENT AND DOORS NO EVIDENCE OF LEAK OR BROKEN PARTS FOUND RETRACTING ACTUATOR VERY WARM, SUSPECT INTE RNAL ACTUATOR LEAK. REMOVED AND REPLACED NOSE GEAR ACTUATOR, REMOVED AND REPLACED NOSE GEAR UNLOCK ACTUATOR. PERFORMED 2 L 7 3 4F RT A22WE 2007040600038 20070406 00038 NM 2007 4 6 07FDEA01178 1 20070329 A 5322 FITTING BOEING 727 727225 1384077 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 LOWER AFT SUPPORT TEE HAS CORROSION ON UPPER SURFACE AT FWD END OF LOWER BODY PANEL NR 3218 (INST AFT OF BEACON LIGHT) . REMOVED STROBE LIGHT ASSY MOUNT IAW SRM 53-10-01. CHECK ALLOWABLE DAMAGE LIMITS IAW FOUND TO BE OUT OF LIMITS. FABR ICATED T-CHORD AND STIFFENER ON THE MAE TRAVELER T7/667682 AND T7/667683. FABRICATED NEW U-CHANNEL ASSY ON MAE TRAVELER T7/667684. DRILLED AND LOCATED T-CHORD, STIFFENER, U-CHANNEL IAW SRM 51-30-2. INSTALLED T-CHORD, STIFFENER AND U-CHAN NEL IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2007040600043 20070406 00043 NM 2007 4 6 SWAA071667 1 20070331 A 2420 976J4982 GENERATOR BOEING 737 7373H4 1384600 NM NR 1 FAULTED A SWAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SW 29 373SW 26581 DIVERSION, EQUIPMENT COOLING OFF LIGHT ILLUMINATED AT FL 350, SWITCHED TO ALTERNATE PER QRH. F/A REPORTED HOT ELECTRICA L ODOR, NO SMOKE IN CABIN. NR 1 GEN SHOWING LOW VOLTS AND FREQS, PUT APU ON BUSS NR 1 SIDE. REMOVED AND REPLACED NR 1 GEN AND EQUIPMENT COOLING FAN PER MM. 2 L 7 2 4F RT A16WE 2007040600047 20070406 00047 NM 2007 4 6 SWAA071688 1 20070402 A 2560 P207001 FLASHLIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 451WN 32495 DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2007040600061 20070406 00061 NM 2007 4 6 07FDEA01200 1 20070330 A 5330 651842012 SKIN BOEING 727 727225 1384077 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 LOWER FUSELAGE SKIN IS GOUGED/CREASED AT BS 294-347 STR S-21R, 6" DENT WAS DETERMINED TO BE OUT OF LIMITS. REMOVED DAMA GE, FABRICATED AND INSTALLED EXTERNAL DOUBLER REPAIR REF SRM 53-30-3 FIG 1. 2 L 7 3 4F A3WE 2007040600068 20070406 00068 NE 2007 4 6 DXTA200702070 2 20070403 A 7321 EEC CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LT ENGINE FAILED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 690QS 5605090 LT EEC FAILED TO MANUAL ON TAKEOFF ROLL AT 40 KIAS. TWO TIMES. ABORTED TAKE OFF. REMOVED BLEED SERVO AND INSTALLED NE W SERVO SN TR2508 IAW PW MM CH 75-50-01. OPERATIONAL CHECKS GOOD ON TORQUE MOTOR INSTALLED NR 40 ORIFICE IN BOV IAW PW54 5A MM CH 71-00-00. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007040600070 20070406 00070 WP 2007 4 6 DXTA200702074 2 20070403 A 7200 FAN BLADE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP RT ENGINE DAMAGED E DXTA O OTHER C F.O.D. NR NOT REPORTED 1 GL 07 893QS 258393 P107758 RT ENGINE HAS FOD DAMAGE TO MULTIPLE ENGINE FAN BLADES. [SUP 4-19-07] ALL MAINTENANCE ACCOMPLISHED. IAW HONEYWELL LMM 731-5 AND HAWKER MM. 800XP. 2 L 7 2 4F 4 F RT A3EU E6WE 2007040600071 20070406 00071 2007 4 6 DXTA200702073 4 20070403 A 3414 INDICATOR CESSNA 680 680CE 2076811 CE COCKPIT ERRATIC E DXTA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 301QS 6800010 COPILOTS AIRSPEED ERRATIC ON TAKE OFF ROLL FOUND INSECT LODGED IN RT PITOT TUBE. REMOVED RT PITOT TUBE FROM MOUNT AND R EMOVED OBSTRUCTION WITH DRY NITROGEN. REINSTALLED PITOT TUBE AND PERFORMED PILOTS AD CO-PILOTS COMBINED LEAK RATE CHECK AND NR 1 AND 2 PFD ALT., AIRSPEED AND MACH AIRSPEED CORRELATION I.A.W. CE680 M/M CH. 34-11-00-700. ALL CHECKS GOOD. 2 L 7 2 4F RC T00012WI 2007040600081 20070406 00081 NM 2007 4 6 07FDEA01187 1 20070329 A 5330 651753033 SKIN BOEING 727 727225 1384077 NM BS 1223 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 463FE 22551 FOUND EXTERNAL FUSELAGE REPAIR AT APPROX STA 1223, STR 25R. REPAIR DOES NOT CONFORM TO SRM 53-30-3 FIG 3. REMOVE EXTER NAL DOUBLER FROM A/C REF SRM 51-30-2. MFG NEW REPAIR DOUBLER REF SRM 53-30-3 FIG 3. INSTALLED NEW REPAIR DOUBLER REF S RM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 2007040600084 20070406 00084 NM 2007 4 6 07FDEA01190 1 20070329 A 5414 6521873477 SKIN BOEING 727 727225 1384077 NM ZONE 400 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FOUND REPAIR AT THE TE OF THE NR 1 ENG PYLON STUB FRAME UPPER SURFACE EXISTING. REPAIR DID NOT CONFORM TO SRM 54-30-2. REMOVED EXISTING REPAIR ON UPPER SURFACE. REMOVED DAMAGE SKIN, REMOVED DAMAGE ON LOWER SURFACE T/E SKIN. REPAIRED UPP ER AND LOWER T/E WEDGE SKIN REF WO NR 35851/EA NR 7-5480-107016, THIS REQUIRES RE-INSPECTION OF BLIND FASTENERS EVERY C- CHECK FOR CONDITION. 2 L 7 3 4F A3WE 2007040600088 20070406 00088 EU 2007 4 6 AALA20070562 1 20070326 A 3350 LENS AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 80052 460 MIA - EMERGENCY LIGHT IN FIRST CLASS AT LEFT SIDE OF GALLEY BULKHEAD MISSING COVER. REPLACED LENS FOR EMERGENCY LIGHT I N FIRST CLASS AT LEFT SIDE OF GALLEY BULKHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007040600089 20070406 00089 NM 2007 4 6 AALA20070558 1 20070325 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 948AN 30086 MIA- EMERGENCY LIGHT AT SEAT 8D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 8D. SYSTEM GROUND CHECKED NORMAL OPERATI ON. 2 L 7 2 4F RT A16WE 2007040600090 20070406 00090 NM 2007 4 6 AALA20070559 1 20070325 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948AN 30086 MIA - EMERGENCY LIGHT AT SEAT 8D HAS LENS MISSING. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 8D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007040600098 20070406 00098 2007 4 6 DXTA200702068 4 20070402 A 2397 CONNECTOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE SEAT NR 4 CONTAMINATED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 616QS 5605345 (P) SMOLDERING ELECTRICAL ODOR COMING FROM SEAT NR 4 VIDEO SCREEN RECEPTICLE WHEN SCREEN IS INSERTED. NO DIVERTION. FO UND DEBRIS ACROSS CONTACTS INSIDE SCREEN RECEPTACLE AT SEAT NR 4. REMOVED DEBRIS AND CLEANED CONTACTS AS REQUIRED. VID EO MONITOR OPS CHECK NORMAL AT SEAT NR 4. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007040600099 20070406 00099 CE 2007 4 6 DXTA200702069 1 20070402 A 2731 SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP ELEVATOR TRIM OUT OF ADJUST E DXTA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 07 815QS 258705 AT 40 KTS ON T/O AILERON/ELEVATOR TRIM LIGHT ILLUMINATED, REJECTED T/O, ELEVATOR TRIM WAS SET FOR PROPER TRIM SETTING AT 21.5 ADJUSTED LT AND RT ELEVATOR OUT OF TRIM SWITCHES IAW AMM 27-30-00. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A3EU E6WE 2007040600103 20070406 00103 2007 4 6 NWAA071203255 4 20070331 A 2565 TERMINAL AIRBUS 320 A320212 3930322 EU ESCAPE SLIDE BROKEN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 355NW 13850 5511 807 WHILE PERFORMING EMERGENCY OVERWING EXIT HATCH CHECK, THE FLEXIBLE CONTROL CABLE TERMINAL END WAS FOUND BROKEN. REPLACE D LEFT OVERWING ESCAPE SLIDE RESERVOIR, INSPECTION OK. 2 L 7 2 4F RT A28NM 2007040600117 20070406 00117 NM 2007 4 6 DHL2007786529 1 20070330 A 5754 STRUCTURE BOEING 727 727214 138407R NM NR 1 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT BN233 21692 NR 1 SLAT ASSY CRACK WHERE SLAT ACTUATOR ATTACHES TO SLAT INTERNAL. REMOVED NR 1 SLAT ASSY TO FOM REPAIR IAW B727 M/M 2 7-81-11. REMOVED 2 RIBS INBD AND OUTBD FROM NR 1 SLAT ASSY IAW B727 SRM 51-30-2. LOCATED AND DRILLED RIBS IAW B727 SRM 51-30-2. INSTALLED INBD AND OUTBD RIBS, P/N 65-17327-8 AND 65-17327-11 IN NR 1 SLAT ASSY IAW B727 SRM 51-30-2. RE-INS TALLED NR 1 SLAT ASSY IAW B727 M/M 27-81-11. OP CHECK AND LEAK CHECK GOOD IAW B727 M/M 27-81-00. 2 L 7 3 4F A3WE 2007040600124 20070406 00124 NM 2007 4 6 DHL2007786530 1 20070327 A 5753 SKIN BOEING 727 727214 138407R NM TE FLAP GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT BN605 21692 RIGHT WING INBD MID FLAP GOUGED 3 FROM INBD EDGE, WBL 73.597. CUTOUT DAMAGED AREA 1 BY 1.875. FABRICATED INTERNAL DOUB LER FROM 2024T3, .040, 7.75 BY 5.625 AND FILLER 2024T3, .040, 1 BY 1.875. TREATED, ALODINED AND PRIMED PARTS IAW B727 S RM 51-10-2. INSTALLED REPAIR IAW SRM 51-30-2, BOEING TELECON 1-308995491-11, DATED 04/01/07, BOEING 8100-9 DATED 04/03/ 07 AND ASTAR J/C EC-00273-001. 2 L 7 3 4F A3WE 2007040600126 20070406 00126 EU 2007 4 6 AALA20070551 1 20070325 A 5210 BOTTLE AIRBUS 300 A300B4605R 3930308 EU EMERGENCY ASSIST LOW PRESSURE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80058 466 MIA - EMERGENCY ASSIST BOTTLE AT RIGHT NUMBER FOUR DOOR HAS LOW PRESSURE. SERVICED EMERGENCY ASSIST BOTTLE AT RIGHT NUM BER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007040600127 20070406 00127 NM 2007 4 6 AALA20070553 1 20070325 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 678AN 29428 MIA - EMERGENCY EXIT SIGN LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT SIGN LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007040600128 20070406 00128 WP 2007 4 6 AALA20070554 1 20070325 A 2820 PUMP DOUG DC9 DC982 3022082 WP CENTER FUEL TANK INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 415AA 49326 PASSING FLIGHT LEVEL 200, FOUND FUEL BURNING OUT OF THE MAIN TANKS AND THE CENTER TANK WAS INCREASING. FLIGHT LANDED DF W WITHOUT INCIDENT. REPLACED BOTH CENTER BOOST PUMPS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007040600129 20070406 00129 EU 2007 4 6 AALA20070550 1 20070325 A 5210 BOTTLE AIRBUS 300 A300B4605R 3930308 EU L1 DOOR LOW PRESSURE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80058 466 MIA - EMERGENCY ASSIST BOTTLE AT LEFT NUMBER ONE DOOR HAS LOW PRESSURE. SERVICED EMERGENCY ASSIST BOTTLE AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007040600131 20070406 00131 EA 2007 4 6 VNAA0703013 1 20070319 A 2150 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT A/C PACK UNKNOWN A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 216PS 7882 CREW REPORTED A RIGHT PACK OFF EICAS MESSAGE ON TAKEOFF. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CLEANED THE AIR CONDITION CONTROL PANEL IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007040600134 20070406 00134 NM 2007 4 6 07FDEA01173 1 20070328 A 7500 652245031 DUCT BOEING 727 727225 1384077 NM ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 NR 2 ENGINE 6TH STAGE SADDLE DUCT IS CRACKED AT THE RIGHT DUCT TO ENGINE MOUNT FLANGE AREA AFT OUTBD END OF DUCT. REMOV ED AND REPLACED CRACKED DUCT WITH SERVICEABLE UNIT REF 727 AMM 36-00-001-2 PG 1 - 6 FIG'S 201 AND 202, 727 AMM 20-80-001 -2 FIG'S 203 AND 209 AND 727 AMM 20-10-023. LEAK CHECK PERFORMED ON WORK CARD 70C005-00. 2 L 7 3 4F A3WE 2007040600137 20070406 00137 EA 2007 4 6 VNAA0703016 1 20070323 A 3320 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LAVATORY ODOR A VNAA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 05 226JS 7895 CREW REPORTED A STRONG ELECTRICAL ODOR COMING FROM THE LAVATORY AREA. MAINTENANCE INSPECTED THE LAV AND SURROUNDING ARE A INCLUDING OPS TESTING THE LAV LIGHT IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPS TEST GOOD, NO DEFECTS NOT ED AT THIS TIME. MAINTENANCE INSPECTED AND FOUND INSULATION NEAR THE LAV LIGHT BALLAST. MAINTENANCE RE-POSITIONED THE INSULATION NEAR BALLAST. IN ADDITION, MAINTENANCE FOUND THE LAV STUFFED WITH HAND TOWELS. MAINTENANCE REMOVED TOWELS, SERVICED LAVATORY AND PERFORMED OPS TEST OF LAV WASTE DISPOSAL SYSTEM IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL . NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007040600138 20070406 00138 SO 2007 4 6 N93A01042007 1 20070401 A 3250 SEAL GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU NLG STEERING DETERIORATED E N93A O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 13 404QS 1304 NOSE STEERING WAS NOT RESPONDING CORRECTLY DURING TAXI AND WAS JERKY. MAINTENANCE FOUND SEALS LEAKING. 2 L 7 2 4F 4 F RT A12EA E25NE 2007040600140 20070406 00140 NM 2007 4 6 ANCF200600049 1 20070329 A 5610 141T483514 WINDOW BOEING 767 767383 1385214 NM PWA 4060 PW4060 52119 NE COCKPIT DAMAGED W ANCF A UNSCHED LANDING O OTHER CL CLIMB 1 SO 23 984AN 35 26 24357 WITH HANDLE POSITION HANDLE CLOSED, (LATCH HANDLE) OPERATING CRANK IN CLOSED POSITION AND WINDOW INDICATOR CLOSED, FO`S WINDOW WENT OPEN ON THE BACK OF WINDOW, JUST AFTER TAKEOFF, IAW AMM 56-11-02 PAGE 401 THE RT WINDOW WAS REMOVED AND REPL ACED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007040600142 20070406 00142 NM 2007 4 6 DHL2007786531 1 20070320 A 5330 SKIN BOEING 727 727214 138407R NM BS 620 S16-17L DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 REMOVE TEMP REPAIR AND INSTALL PERMANENT REPAIR AT FUSELAGE SKIN AT BS 620 BETWEEN STR 16L AND 17L. REMOVED EXISTING RE PAIR IAW B727 SRM 51-30-2 AND SIE EO NR SIE–N786AT-3-27-07, DATED 04/02/07. FABRICATED REPAIR DOUBLER FROM 2024T3, .063 , 28.25 BY 24 AND TRIPLER FROM 2024T3 .100, 25.50 BY 21.50 IAW SIE EO NR SIE–N786AT-3-27-07, DATED 04/02/07. TREATED AN D PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. HFEC INSPECTED FASTENER HOLES AND SKIN DOUBLER EDGES WITH NO CRACK INDICA TION NOTED IAW B727 NDT MANUAL PT6 51-00-00, F16 AND F23. INSTALLED REPAIR PARTS IAW SIE EO NR SIE N786AT-3-27-07, DATE D 04/02/07. 2 L 7 3 4F A3WE 2007040600143 20070406 00143 NM 2007 4 6 MWEA070047 1 20070327 A 3350 8039251 POWER SUPPLY BOEING 717 717200 1383700 NM EMERGENCY LIGHT INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 920ME 55182 AFT EMERGENCY LIGHT ABOVE AFT ACCESSORY DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY. 2 L 7 2 4F TR A6WE 2007040600145 20070406 00145 NM 2007 4 6 MWEA070049 1 20070325 A 7830 7150922505 RIB BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 921ME 55183 LEFT THRUST REVERSER OUTBOARD END OF RIB CRACKED 12 INCHES AFT OF LOCK PIN. FABRICATED AND INSTALLED THRUST REVERSER. 2 L 7 2 4F TR A6WE 2007040600147 20070406 00147 NM 2007 4 6 MWEA070051 1 20070325 A 7830 7150922505 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 921ME 55183 RIGHT THRUST REVERSER TOP DEFLECTOR DOOR FRAME AT STATION 35.669 HAS CRACK ON OUTBOARD END OF FRAME. FABRICATED AND INS TALLED THRUST REVERSER. 2 L 7 2 4F TR A6WE 2007040600150 20070406 00150 WP 2007 4 6 MWEA070078 1 20070405 A 5322 991152739 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 810ME 48072 SHEAR CLIP DAMAGE FROM DRILL MARK. FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F A6WE 2007040600151 20070406 00151 NM 2007 4 6 MWEA070065 1 20070328 A 7830 7159022505 CHANNEL BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 927ME 55193 LEFT TOP THRUST REVERSER DOOR HAS A CRACK ON THE INBOARD ZEE CHANNEL AT STATION 35.669 APPROXIMATELY .375 INCH LONG. FA BRICATED AND INSTALLED ZEE CHANNEL. 2 L 7 2 4F TR A6WE 2007040600152 20070406 00152 NM 2007 4 6 MWEA070066 1 20070328 A 7830 7159022505 CHANNEL BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 927ME 55193 RIGHT TOP THRUST REVERSER DOOR HAS A CRACK ON THE INBOARD ZEE CHANNEL AT STATION 26.666 APPROXIMATELY .125 INCH LONG. F ABRICATED AND INSTALLED ZEE CHANNEL. 2 L 7 2 4F TR A6WE 2007040600153 20070406 00153 NM 2007 4 6 UPS07M49525 1 20070123 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM BS 1099-1119 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C FWD CARGO COMPT: UNDER FLOOR AREA BETWEEN STA 1099 & 1119, LONGERON 48R FOUND CORRODED. LONGERON ATT ACHED PARTS & FASTENERS REMOVED FOR REPAIR WORK CUTOUT PER SRM 51-31-01 V2 R38. REPAIR LONGERON & REPAIR SPILCE FAB PER 53-10-00 F2 R38. REPAIR PARTS REPROTECTED & PAINTED PER SRM 51-21-01 V2 R38. REPAIR LONGERON PARTS REINSTALLED PER SR M 53-10-01 V1 R38, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007040600156 20070406 00156 NM 2007 4 6 DU4R2007079 1 20070327 A 5210 60B100244 BEARING BOEING 757 757232 1384965 NM L2 DOOR CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND CORROSION ON L-2 DOOR, RUST ON FWD AND CRANK ROD, ROD END. REPAIRED BY REMOVING AND REPLACING ROD END WITH P/N 60 B10024-4 IAW BOEING SOPM 20-50-03. 2 L 7 2 4F RT A2NM 2007040600159 20070406 00159 NM 2007 4 6 07FDEA01218 1 20070331 A 5315 651631182 FLOORBEAM BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FLIGHT DECK FLOORBEAM HAS CORROSION ON TOP OF BEAM LOCATED AT BS 277, RBL 10.5. REMOVED CORROSION, ALL WORK FOR BLEND W AS ACCOMPLISHED ON FED EX EA NR 7-5310-107004. 2 L 7 3 4F A3WE 2007040600164 20070406 00164 NM 2007 4 6 07FDEA01206 1 20070330 A 5320 BAC15171507 FLOOR SUPPORT BOEING 727 727225 1384077 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FWD CARGO PIT FLOOR SUPPORT AT SRA 717 ABOVE STR 27R IS CRACKED FABRICATED FLOOR SUPPORT REF DWG BAC 1517-1507 REV A. N DT REF BAC 5423, HEAT TREATED AND TESTED HARDNESS REF BAC 5602 AND BAC 5946 FEF TRACKING NR 2007-03-150. REMOVED DAMAGE D SECTION OF CARGO FLOOR SUPPORT AND SPLICED IN NEW SECTION OF SUPPORT REF SRM 53-10-05 FIGURE 4 PAGES 9 AND 10. 2 L 7 3 4F A3WE 2007040600166 20070406 00166 NM 2007 4 6 07FDEA01246 1 20070402 A 5755 SKIN BOEING 727 727225 1384077 NM ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 RT WING NR 9 SPOILER UPPER TE SURFACE HAS DELAM REMOVED NR 9 SPOILER PANEL. SPOILER REPAIRED ON SHOP WO NR 11841-6000-0 003 REF SRM 51-40-20. INSTALLED NR 9 SPOILER PANEL REF MM 27-62-001-4 STEP 3-5. ADJUSTED SPOILER REF MM 27-62-001-5 PG 1 STEP 2A-2F AND STEP 3. 2 L 7 3 4F A3WE 2007040600167 20070406 00167 NM 2007 4 6 07FDEA01247 1 20070402 A 5755 STRUCTURE BOEING 727 727225 1384077 NM ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 2366 22551 RT WING NR 14 SPOILER T/E IS SPLIT REMOVED AND REINSTALLED NR 14 SPOILER FOR T/E REPAIR REF M/M 27-61-0001-4, M/M 27-61- 001-5. SPOILER REPAIRED ON IDM WORK CARD ORDER NR 11841-6000-0004. 2 L 7 3 4F A3WE 2007040600168 20070406 00168 NM 2007 4 6 07FDEA01249 1 20070403 A 5313 AFA7105513 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 AFT CARGO TUNNEL AREA: LONGERON 38R SPLICE AT STA 1863 FOUND WITH CRACK. [SUP 4-20-07] REMOVED AND REPLACED AS PER SR M 51-33-01 VOL.II AND DOUGLAS DRAWING AFA7105. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040600169 20070406 00169 EU 2007 4 6 07FDEA01250 1 20070403 A 5311 A53980044232 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CHAFED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 FOUND CRACKED FRAME-SEGMENT AT C74, P26 LT. REPLACEMENT OF THE AFFECTED FRAME-SEGMENT. 2 L 7 2 4F RT A35EU 2007040600170 20070406 00170 EU 2007 4 6 07FDEA01251 1 20070403 A 5720 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CORROSION ON RT WING BOTTOM SKIN IN AREA OF RIB 4-5 AROUND SEVERAL FASTENERS. CRACKS WERE FOUND IN TWO HOLES. REPAIR P ERFORMED BY REMOVING CORROSION AND REMOVING CRACKS AT HOLE NR 666 AND NR 1466 BY OVERSIZING IAW EA 6-5720-101321 AND RAS /BAE/1002865/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040900001 20070409 00001 NM 2007 4 9 07FDEA01299 1 20070403 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 DEFORMED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 CABIN SEAT TRACK AT STA 1485, X = 47 FOUND DEFORMED. 4-18-07, CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUM E I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040900002 20070409 00002 NM 2007 4 9 07FDEA01300 1 20070403 A 5320 655611911 SUPPORT CHANNEL BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 LOWER AFT PIT BILGE FWD SIDE OF STA 950A, VERTICAL SUPPORT CHANNEL AT 8" LBL HAS SMALL AMOUNT OF CORROSION AT LOWER OB. REPLACED VERTICAL SUPPORT AT STA 950A. REFERENCE SRM 51-30-2 PAGE 1 - 12. 2 L 7 3 4F A3WE 2007040900003 20070409 00003 WP 2007 4 9 07FDEA01265 1 20070403 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1363 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 MAIN CABIN CTR WING SECTION UPPER SKIN CORROSION UNDER HEAD OF FASTENERS. REPAIRED IAW FEDEX EA 8-5730-103734. 2 L 7 3 4F A22WE 2007040900005 20070409 00005 WP 2007 4 9 07FDEA01268 1 20070403 A 5730 SKIN DOUG DC10 DC1010 3022110 WP LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 LT WING LOWER SURFACE NR 40 HEAD FASTENERS ON SKIN FOUND MODERATE CORROSION. REPAIRED IAW FEDEX EA 8-5730-103735. 2 L 7 3 4F A22WE 2007040900007 20070409 00007 WP 2007 4 9 07FDEA01271 1 20070403 A 5312 PRESSURE PANEL DOUG DC10 DC1010 3022110 WP RT MLG WW CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 RT MLG W/W FOUND CORROSION ON PRESSURE PANEL STA 1381 UNDER SLANT PANEL. REPAIRED IAW FEDEX EA 8-5730-103734. 2 L 7 3 4F A22WE 2007040900010 20070409 00010 NM 2007 4 9 DLM88070277 1 20070331 A 2420 976J2528 GENERATOR DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 27 992DL 53344 718105 AT 1000 FT AGL BOTH ENG GENERATORS WERE PROVIDING INTERMIT POWER. BOTH SIDES PFD AND ND WERE FLASHING ON AND OFF WITH T HE PWR CYLING. THIS WAS HAPPENING EVERY 1-2 SECS. CAPTS SIDE SWITCHED TO STBY PWR TO REGAIN INST. THE F/O SIDE CONTIN UED TO FLICKER AFTER 30 SECS WHEN THE APU WAS UP AND RUNNING PLACED THE F/O SIDE ON APU GEN AFTER TRIPPING THE RT GEN MA NUALLY. AFTER THAT WE DID THE CAPTS SIDE AND IT ALL WORKED FINE. WE HAD NO AC CROSS-TIE LOCK OUT DID NOT NOTICE FREQS O R VOLTS AT THE TIME.REPLACED RT GENERATOR AND CSD PER AMM OPS CKS OK. 2 L 7 2 4F 4 F RT A6WE E9NE 2007040900011 20070409 00011 NE 2007 4 9 DL76L070278 2 20070331 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 UNKNOWN A DALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 27 194DN 43189 28451 727679 NEAR TOP OF CLIMB, LEFT EPR DROPPED FROM 1.5 TO 1.3 ACCOMPANIED BY AIRCRAFT YAW. ENGINE QUICKLY RECOVERED AND REMAINED STABLE REST OF FLIGHT. REMOVED AND REPLACED LT ENG FMU PER MM. LEAK CHK OK. REMOVED AND REPLACED LT ENG EEC PERFORMED ALL TEST REQUIRED. OPS CHK OK. ALSO PERFORMED HIGH POWER RUN, NO FAULTS NOTED ON PIMU/ENG EPR WAS STEADY NO FLUCUATIO NS. REMOVED AND REPLACED LT ENG FMU PER MM. LEAK CHK OK. REQUIRES ENG RUN. LT ENG EEC PERFORMED ALL TEST REQUIRED. OPS CHECK OK. ALSO PERFORMED HIGH POWER RUN UP. NO FAULTS NOTED ON PIMU/ENG E WAS STEADY NO FLUCTUATIONS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007040900013 20070409 00013 NM 2007 4 9 DL76L070281 1 20070401 A 2120 UNKNOWN BOEING 767 767332 1382001 NM SEAT 5A/5B ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 188DN 27583 F/A AND PAX REPORTED ELECTRICAL ODOR FROM SEATS 5A AND 5B. FWD TO MCO AND PLACARDED PER MEL 25-20-01K ITEM XFRD TO BASE MCO OPENED MAINT PROCEDURE C/O RESET SEAT PWR MODULE. INSPECTED CONNECTIONS, CHECKS GOOD PER M/M MCO AND PLAC REMOVED. 2 L 7 2 4F RT A1NM 2007040900015 20070409 00015 NM 2007 4 9 DLM88070289 1 20070403 A 5330 5936434129 SKIN DOUG MD88 MD88 3023688 NM FS 382 L29R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 945DL 49818 DURING CURENT HMV, A SCRATCH WITH TWO CRACKS WERE FOUND ON THE RHS FUSELAGE SKIN NEAR THE FORWARD CARGO DOOR CUTOUT. TH E SUBJECT CRACKS WERE TRIMMED OUT, AND A BOEING APPROVED REPAIR INSTALLED PER 460140-14. 2 L 7 2 4F RT A6WE 2007040900016 20070409 00016 NM 2007 4 9 DL76L070290 1 20070403 A 2530 811150417 COFFEEMAKER BOEING 767 767332 1382001 NM AFT LEFT GALLEY DIRTY A DALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 192DN 28449 COFFEEMAKER ON CAPT SIDE HAS BURNING ODOR WHEN ON. REMOVED AND REPLACED BOTH REAR GALLEY COFFEEMAKERS AS PRECAUTION CAP T SIDE. FOUND COFFEEMAKER DRAINS CLOGGED WITH COFFEE GRINDS AND BURNED COFFEE ON DRAIN PLATE STRONG ODOR. OPERATED COF FEEMAKERS OVER HALF HOUR PERIOD CHECKS OK CLEARED DRAIN. 2 L 7 2 4F RT A1NM 2007040900023 20070409 00023 NM 2007 4 9 07FDEA01211 1 20070331 A 5710 DUCT DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT FOUND CRACKED. [SUP 4-19-07] CRACKED AT RIGHT HAND WING FIXED LEA DING EDGE TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57-10-00 FIGURE 42 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2 -100. 2 L 7 3 4F RT A22WE 2007040900029 20070409 00029 NM 2007 4 9 07FDEA01297 1 20070403 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 CABIN, SEAT TRACK CROWN AREA AT STA 755, X = -8 FOUND CRACKED. 4-18-07, CARRIED OUT REPAIR AS PER SRM 53-70- 00 VOL UME I. FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040900035 20070409 00035 NM 2007 4 9 07FDEA01219 1 20070331 A 5230 SKIN BOEING 727 727225 1384077 NM ZONE 800 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FWD LOWER CARGO DOOR, FWD LOWER CORNER OF SKIN WORN, GOUGED. INSTALLED REPAIR DOUBLER REF 52-00-3 PG 2, FIG 4, DETAIL F . RESTORED LEVELING, COMPOUND REF SOPM 20-60-04 PG 7. 2 L 7 3 4F A3WE 2007040900039 20070409 00039 NM 2007 4 9 07FDEA01221 1 20070331 A 5730 6521657254 PANEL BOEING 727 727225 1384077 NM ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 RT WING, UPPER SURFACE AT WBL 462, PNL, JUST O/B OF NR 14 SPOILER IS DELAMINATED. REMOVED PANEL AND SENT OUT FOR REPAIR . PANEL REPAIRED ON AAR WO NR 11841/6300/0003. REMOVED DAMAGE AND DELAMINATED SKIN, AND REPAIRED, REF SRM 51-40-20. INSTALLED PANEL REF SRM 51-30-02 PG 1. 2 L 7 3 4F A3WE 2007040900040 20070409 00040 NM 2007 4 9 07FDEA01222 1 20070331 A 5711 ARB74131 SPAR CAP DOUG MD11 MD11 3023602 NM ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LT WING, REAR SPAR UPPER CAP XORS 680 HOLE FOUND ELONGATED. [SUP 4-20-07] COMPLIED WITH FEDEX E.A. 1-5710-109851 CLASS IFIED AS MAJOR. REPAIRED IAW FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040900042 20070409 00042 NM 2007 4 9 07FDEA01224 1 20070401 A 5730 SKIN BOEING 727 727225 1384077 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 LEFT WING L/E CRACKED ABOVE NR 3 SLAT O/B TRACK. REPAIRED CRACKED ON LEFT WING ABOVE NR 3 SLAT O/B TRACK IAW SRM 57-30- 4 FIG 11. 2 L 7 3 4F A3WE 2007040900044 20070409 00044 EU 2007 4 9 07FDEA01226 1 20070401 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 FORWARD LOWER CARGO COMPARTMENT STRINGER 50L HAS CORROSION BETWEEN FR 38.1 TO FR 39. REMOVED ANGLE REINFORCING IAW SRM 51-40-21. UPON FURTHER INVESTIGATION FOUND STRINGER HAS NO CORROSION FOUND. REINFORCING ANGLE HAD CORROSION FOUND, TO BE OUT OF LIMITS. FABRICATED NEW ANGLE REINFORCING P/N 60-19193/18, BATCH #96481 IAW SRM 53-14-14. REMOVED 2 SHEAR TIE , PLATE AND ANGLE BRACKET IAW SRM 51-40-21. LOCATED AND DRILLED IAW SRM 51-40-44. TREATED AND PRIMED IAW SRM 51-21-10. INSTALLED ANGLE REINFORCING IAW SRM 51-40-21. INSTALLED ANGLE BRACKETS, 2 SHEAR TIE AND 1 PLATE IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007040900046 20070409 00046 EU 2007 4 9 07FDEA01228 1 20070401 A 5320 CASE AIRBUS 310 A310203 3930313 EU L1 DOOR DRAIN CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 DRAIN CASING AT L-1 DOOR THRESHOLD CRACKED. REMOVED CRACKED DRAIN CASING, FAB`D NEW DRAIN CASING ON TRAVELER NR T7/6706 54. INSTALLED NEW DRAIN CASING IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007040900048 20070409 00048 EU 2007 4 9 07FDEA01253 1 20070403 A 5753 A57970330003 RIB AIRBUS 310 A310304 3930339 EU TE FLAP CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 FOUND OLD CRACK REPAIR ON INBOARD FLAP RT, RIB 21 (POCKET REPAIR). REPAIR WAS PERFORMED BY REPLACEMENT OF RIB 21 IAW SB A310-57-2055, APPROVED BY EA 6-5752-106443. 2 L 7 2 4F RT A35EU 2007040900049 20070409 00049 WP 2007 4 9 07FDEA01254 1 20070403 A 5754 SLAT TRACK DOUG DC10 DC1010 3022110 WP LE SLAT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 LT WING L/E AT SLAT TRACK HOLE NR 1 FOUND SKIN EDGE CORRODED AND DISBONDED. REPAIR IAW SRM 57-10-00 FIGURE 68 VOL 1 SHT 1-3. 2 L 7 3 4F A22WE 2007040900055 20070409 00055 WP 2007 4 9 07FDEA01261 1 20070403 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1801-1806 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 LOWER EXT FUSELAGE FOUND DENT 1.5" BY 1" DEPTH 0.050". REPAIRED PER NRC IC02006. 2 L 7 3 4F A22WE 2007040900056 20070409 00056 WP 2007 4 9 07FDEA01262 1 20070403 A 5730 SKIN DOUG DC10 DC1010 3022110 WP RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 RT WING L/E AT SLAT TRACK HOLE NR 2 FOUND SKIN CORRODED. REPAIRED IAW SRM 57-10-00 FIGURE 68 SHT 1-3 VOL 1. 2 L 7 3 4F A22WE 2007040900059 20070409 00059 NM 2007 4 9 07FDEA01301 1 20070403 A 5311 65561191 FRAME BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 LOWER AFT PIT BILGE, FRAME HAS APPROX 3 SQ INCHES OF CORROSION ON AFT LOWER FACE AT STA. 950A, LBL 8". REMOVED CORROSIO N REF 51-10-2 AND 53-10-1. NDT'D FOR MATERIAL LOSS, FOUND AREA OUT OF LIMITS REF SRM 53-10-1 FIG 1. REMOVED SUPPORT BR KT, VERT SUPPORT BRKT, FAST IN PNL 3522 FOR ACCESS, AND FASTENER IN REPAIR AREA REF SRM 51-30-2. CUTOUT DAMAGED SHEAR T IE AND FABRICATED NEW PART REF SRM 53-10-4, HEAT TREATED ON WO NR 11841-1000-0006. DRILLED UP REPAIR PARTS REF SRM 53-1 0-4. TREATED AND PRIMED REF SRM 53-10-4. INSTALLED SHEAR TIE REPAIR REF SRM 53-10-4. INSTALLED SUPPORT BRACKET, VERT BLKHD SUPPORT BRKT, AND PNL 3522 FAST, REF 51-30-2. 2 L 7 3 4F A3WE 2007040900060 20070409 00060 EU 2007 4 9 07FDEA01302 1 20070403 A 5312 BULKHEAD AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 FOUND CORROSION AT FRAME 39 BULKHEAD LOWER T-PROFILE AND ON PARTS OF BULKHEAD PANEL IN AREA OF THE T-PROFILE. REPAIRS O F ALL AFFECTED AREAS MENTIONED AND PERFORMED IAW EA 6-5314-99221AND RAS 014851/020/2001 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040900062 20070409 00062 NM 2007 4 9 07FDEA01304 1 20070403 A 5315 6944559 FLOORBEAM BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 LOWER AFT PIT FLOORBEAM, VERTICAL CHANNEL HAS CORROSION AT LWR END AROUND FASTENER HEAD AT STA 950E, LBL 8 FABRICATED NE W FLOORBEAM VERTICAL CHANNEL AT STA 950E, LBL 8. HEAT TREATED AND HARDNESS TESTED FOR 7075 T6 CONDITION REF BAC DWG 69- 44559 AND BAC 5602 REV AF 28AUG01 AND BAC 5946 REV AA 9JUL06, ON SHOP WO NR 11841-1600-0003. REINSTALLED FLOOR SUPPORT REF BOEING DWG 69-44559 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2007040900063 20070409 00063 WP 2007 4 9 07FDEA01305 1 20070403 A 5320 ACA72261 WEB DOUG DC10 DC1010 3022110 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 CORROSION ON UPPER SURFACE OF WEB AT MCD CUTOUT, AROUND NR 7 DOOR LATCH FITTING. REMOVED CORROSION IAW DC10-10 SRM 51-2 1-01 PG 28 VOL II, FOUND OUT OF LIMITS IAW DC10-10 SRM 53-00-01 PG 8 VOL II. REPAIRED OUT OF LIMITS AREA IAW FED EX EA 8-5310-105173 TITLED FUSELAGE, MDCD JAMB LOWER SILL CORROSION AT SPOOL 7, REPAIR. FABRICATED AND INSTALLED REPAIR DOUBL ER AND TRIPLER IAW FED EX 8-5310-105173. 2 L 7 3 4F A22WE 2007040900064 20070409 00064 NM 2007 4 9 07FDEA01306 1 20070403 A 5320 6567251 ANGLE BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 LOWER AFT PIT FWD BULKHEAD STA 950A, LBL 12, HORIZONTAL L-ANGLE AT BASE OF WALL SUPPORT HAS CORROSION AT INBD END. REMO VED L ANGLE FROM LBL 6 TO LBL 21, STA 950A. FABRICATED NEW L ANGLE ON AAR SHOP WO NR 11841-1600-0002, BY HEAT TREATING ANGLE REF DWG 65-67251. 8130 TRACKING NR 2007-03-069. INSTALLED L ANGLE REF SRM 51-30-02. 2 L 7 3 4F A3WE 2007040900067 20070409 00067 NM 2007 4 9 UPS07549558 1 20070326 A 3350 INDICATOR BOEING 757 75724APF 1384969 NM EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 461UP 28265 EMERGENCY LTS (UNARMED) LT OUT. RELAMPED EMERGENCY LTS UNARMED LT. OPS CHECKS NORMAL AMM 33-50-00. 2 L 7 2 4F RT A2NM 2007040900068 20070409 00068 NM 2007 4 9 UPS07549561 1 20070309 A 5311 146N102911 FRAME BOEING 757 75724APF 1384969 NM BS 1460 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 441UP 27386 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1460, BETWEEN S25L TO S26L. REPAIR AT FRAME STA 1460, S25L TO S2 6L ACCOMPLISHED PER FINAL EA 757-5362-27-A1622 & UPS EO B757-5310-26417-A. 2 L 7 2 4F RT A2NM 2007040900071 20070409 00071 NM 2007 4 9 UPS07549564 1 20070309 A 5311 146N102886 FRAME BOEING 757 75724APF 1384969 NM BS 1340 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 441UP 27386 INSPECTION TYPE:C DENTS IN AFT CARGO FUSELAGE FRAME STA 1340, BETWEEN S25R TO S26R, 2EA ACCOMPLISHED REPAIR PER FINAL EA 757-5362-27-A1620 AND UPS EO B757-5310-26429-A. 2 L 7 2 4F RT A2NM 2007040900073 20070409 00073 NM 2007 4 9 UPS07549566 1 20070309 A 5311 143N1024138 FRAME BOEING 757 75724APF 1384969 NM BS 660 S24-25R DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 441UP 27386 INSPECTION TYPE:C DENT IN FWD CARGO FUSELAGE FRAME STA 660, BETWEEN S24R TO S25R. COMPLIED WITH EA 757-5332-27-A1623 AN D UPS EO B757-5310-26415-A. 2 L 7 2 4F RT A2NM 2007040900074 20070409 00074 NM 2007 4 9 UPS07549567 1 20070309 A 5311 143N1014 FRAME BOEING 757 75724APF 1384969 NM BS 700 S24L DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 441UP 27386 INSPECTION TYPE:C DENT IN FWD CARGO FUSELAGE FRAME STA 700, 24L. REPAIR COMPLETED PER EA 757-5332-27-A1624, & UPS EO B7 57-26409-A, WITH NO DEVIATIONS. 2 L 7 2 4F RT A2NM 2007040900075 20070409 00075 GL 2007 4 9 UPS07649554 2 20070327 A 7200 ENGINE BOEING 767 76734AF 1385212 NM GE CF6 CF680C2* GL LEFT UNKNOWN A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 325UP 27751 704422 INSPECTION TYPE:ETOP ENGINE OIL FUMES ENTERED CABIN. FUMES STOPPED WITH LEFT ENGINE BLEED CLOSED. ALL PARAMETERS NORMA L (STRONG ODOR) TET = 23832, TEC = 7538. LEFT ENG REQ BORESCOPE PER FIM 79-21-00. BORESCOPED PER 72-30-00. FOUND STAI NS ON BLADES & IGVS. A/C REQ LEFT ENG CHANGE PER ENGINEERING. INSTALLED BORESCOPE PLUGS & CLOSED ENG. REMOVED AND REP LACED ENG IAW TC 6002. 2 L 7 2 4F 4 F RT A1NM E23EA 2007040900077 20070409 00077 NM 2007 4 9 DU4R2007081 1 20070402 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM CORRODED CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND CORROSION AROUND HOLES AT BS 345 LBL 6 AND LBL 12 W/L 0 AROUND 2 HOLES AND B/L, TO RBL 56. REPAIRED BY REMOVING C ORROSION, FABRICATED AND INSTALLED REPAIR SECTION 32-1/2 FROM BAC1505-100617 IAW B757 53-00-51, 51-20-01, 51-10-2 AND DR D 53-10-51D. 2 L 7 2 4F RT A2NM 2007040900078 20070409 00078 NM 2007 4 9 DU4R2007082 1 20070402 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM CORRODED CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND CORROSION AT CABIN FWD FLOORBEAM UPPER SURFACE AROUND NUTPLATE HOLES AT BS 345 B/L 0 RBL 56. REPAIRED BY REMOVING CORROSION, FABRICATED AND INSTALLED REPAIR SECTION 32-1/2 FROM BAC1505-100617 IAW B757 53-00-51, 51-20-01 AND 51-10-2. 2 L 7 2 4F RT A2NM 2007040900082 20070409 00082 NM 2007 4 9 CALA0700160 1 20070402 A 5311 6520723U66 FRAME BOEING 737 737524 1384721 NM BS 482 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14604 27317 INSPECTION FOUND A .75 INCH CRACK IN FORWARD CARGO DOOR CUTOUT AFT FRAME WEB AT LOWER DOORSTOP FITTING, STA 482, WL 160, S24L. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007040900083 20070409 00083 NM 2007 4 9 CALA0700161 1 20070402 A 5340 69489856 ATTACH FITTING BOEING 737 737524 1384721 NM BS 360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14604 27317 INSPECTION FOUND A 1 INCH CRACK IN ATTACHMENT CLIP AFT OF L-1 DOOR AT STA 360, STRINGER 11L. THE ATTACHMENT CLIP WAS RE PLACED IAW ECRA 5311-01306. A DIP WAS CREATED TO REINSPECT THE CLIP AT INTERVALS NOT TO EXCEED 6,000 FLIGHT CYCLES. 2 L 7 2 4F RT A16WE 2007040900084 20070409 00084 NM 2007 4 9 CALA0700162 1 20070402 A 5310 652072298 DOOR FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14604 27317 INSPECTION FOUND A .5 INCH CRACK IN FORWARD CARGO DOOR CUTOUT FORWARD FRAME WEB AT LOWER DOORSTOP FITTING, WL 160, S24R. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007040900085 20070409 00085 EA 2007 4 9 QXEA200700502 1 20070401 A 2731 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA PITCH FEEL UNKNOWN A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 608QX 10026 PDX - FLIGHT 2565 (PDX-ONT) PITCH FEEL CAUTION MESSAGE IN CRUISE FLIGHT. LANDED WITHOUT INCIDENT WITH REDUCED FLAP SETT ING. MAINTENANCE COMPLIED WITH SSCU RESET IAW CRJ700-705-900-SL-27-052 SERVICE LETTER. OPERATIONAL CHECKS GOOD AIRCRAF T RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007040900086 20070409 00086 CE 2007 4 9 DXTA200702082 1 20070405 A 2150 A/C PACK CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL COCKPIT ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 933QS 7500133 GETTING A BURNING ODOR IN THE CABIN AND COCKPIT, POSSIBLE PACK IS FAILING. REMOVED AND INSTALLED NEW COALESCER IN BOTH T HE COCKPIT & CABIN WATER SEPERATORS. RAN APU AND OPS CHECKED AND LEAK CHECKED GOOD. WORK DONE I.A.W. CE 750 AMM CHAPTE R 21-51-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007040900087 20070409 00087 CE 2007 4 9 DXTA200702084 1 20070405 A 2701 CONTROL COLUMN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL COCKPIT UNKNOWN E DXTA O OTHER O OTHER CR CRUISE 1 GL 07 970QS 7500070 IN CRUISE FLIGHT RT ELEVATOR DEFLECTED DOWN ON EICAS. RT AILERON DEFLECTED UP ON EICAS. CONTROL COLUMN SHOWS RT TURN DUR ING STRAIGHT AND LEVEL FLIGHT. C/W AILERON RIGGING I/A/W CE 750 M/M 27-10-00. TENSIONS CHECK GOOD AND OPS CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007040900088 20070409 00088 CE 2007 4 9 DXTA200702085 1 20070405 A 3240 BRAKE ASSY CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 637QS 5605137 IMMEDIATELY UPON, LANDING, PWR BRAKE AND ANTISKID ANNUNCIATOR CAME ON WITH MASTER, CAUTION, STILL HAD PRESSURE UPON EXIT ING RUNAWAY PWR BRAKE CIRCUIT BREAKER, POPPED RESET ONCE , STILL HAD SOME PRESSURE. THEN BREAKER POPPED AGAIN AND BRAKES FAILED, USED EMERGENCY BRAKE SYSTEM. USED EMERGENCY BRAKE SYSTEM. REMOVED AND REPLACED PWR BRAKE MOTOR ASSY. AND RESET BRAKES INSTALLED AND OPS. CHECKED GOOD. IAW CE560XL MM. CHP. 32-42-06. BLEED BRAKE SYSTEM AND OPS. AND LEAK CHECK GOOD. IAW. CE560XL MM. CHP. 32-42-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007040900090 20070409 00090 NM 2007 4 9 CALA0700166 1 20070405 A 5320 6545834 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM BS 270-294 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 INSPECTION FOUND CABIN FLOOR TRACK CORRODED AT STA 270-294.5, RBL 42. A NEW SECTION OF TRACK WAS INSTALLED IAW SRM 51-1 0-02. 2 L 7 2 4F RT A16WE 2007040900092 20070409 00092 NM 2007 4 9 CALA0700168 1 20070320 A 5311 655828056 FRAME BOEING 737 737524 1384721 NM BS 360 S8L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14605 27318 INSPECTION FOUND A CRACK IN FRAME AT STA 360, S8L. THE FRAME WAS REPAIRED IAW ECRA 5310-04618. 2 L 7 2 4F RT A16WE 2007040900095 20070409 00095 NM 2007 4 9 HALA0700150 1 20070403 A 3830 VALVE BOEING 767 76733A 1385209 NM LAVATORY FLUSH STUCK A HALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 13 583HA 25531 ATB - PER FLT ATTNEDANT- AFT WASTE TANK AFT F/A PANEL DOES NOT TEST PROPERLY. REFERENCE ITEMS 93, FOUND LAV H FLUSH VAL VE STUCK IN THE OPEN POSITION, SECURED LAV H VALVE CLOSED. ALSO, RECALIBRATED AFT WASTE TANK CONTINUOUS LEVEL SENSOR PE R AMM 38-33-00 TEST OKAY. 2 L 7 2 4F RT A1NM 2007040900096 20070409 00096 NM 2007 4 9 HALA0700151 1 20070403 A 8011 35054367 START VALVE BOEING 767 76733A 1385209 NM STARTER MALFUNCTIONED A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 581HA 19597 19597 28141 BTB - ETOPS SIGNIFICANT SYSTEM, RIGHT ENG STARTER VALVE LIGHT REMAINS ILLUMINATED WITH START SELECTOR IN GROUND, ENGINE FAILED TO ROTATE. REMOVED STARTER PER AMM 80-11-01-004-NOO AND REPLACED PER AMM 80-11-01-404-014-NOO AND OPS CK OK. 2 L 7 2 4F RT A1NM 2007040900100 20070409 00100 WP 2007 4 9 UPS07849592 1 20070315 A 5330 9754011505 DOUBLER DOUG DC8 DC873F 302199F WP FS 220 L35L-L35R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C3 HEAVY CORROSION ON INTERNAL DOUBLER AT FS 220 BETWEEN L35L AND L35R A-PIT. REMOVED CORROSION AND REP AIRED INTERNAL DOUBLER AT STA 220 BETWEEN LONGERONS 35L AND 35R IAW SAA EA 008-5310-01-A0747, UPS RAA DC8- 53-20613, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007040900103 20070409 00103 WP 2007 4 9 UPS07849597 1 20070214 A 5711 5597838501 SPAR CAP DOUG DC8 DC873F 302199F WP LWS 515 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C3 DURING WING FORWARD SPAR INSPECTION FOUND 1EA ATTACHMENT HOLE CRACKED. REPAIRED LEFT WING FRONT SPAR LWR CAP BETWEEN XFS 515 AND 526.76 IAW SAA EA 008-5710-01-A0733, UPS EO DC8-5710-26430-A, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007040500091 20070405 00091 NM 2007 4 5 2007UALA00884 1 20070324 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1782 GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 FUSELAGE SEC 48 LEFT UPPER SKIN 1 INCH GOUGE AT STA 1782, APPROX 14 INCHES FROM VERT STAB. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. INSTALLED DOUBLER REPAIR & FLUSH BRILES. 2 L 7 2 4F 4 F RT A2NM E17NE 2007040500092 20070405 00092 NM 2007 4 5 2007UALA00885 1 20070323 A 3510 REGULATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 556UA 26650 OXYGEN MASK DEFECTIVE AT 1=CAPT, 2=1ST OFF, 3=1ST OBS. CREW COMMENTS: INFLATABLE HARNESS DOESN'T INFLATE. [06-14-07 ] REPLACED MASK AND REGULATOR AI NR 1 POSITION OF PILOT AND 1ST OFFICER SEATS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007040500093 20070405 00093 NM 2007 4 5 2007UALA00886 1 20070325 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 592UA 28143 FLOOR EMERGENCY LIGHTS FROM ROWS 9 - 15 NOT WORKING. SUP 4-17-07. REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007040500094 20070405 00094 NM 2007 4 5 2007UALA00887 1 20070323 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 581UA 26701 DOOR 4R EMERGENCY LIGHT INOPERATIVE. SUP 4-17-07. RELAMPED, OP CK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007040500095 20070405 00095 NM 2007 4 5 2007UALA00888 1 20070325 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 480-500 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 508UA 24744 WEB FRAME BETWEEN FRAMES 500-480, RBL 12, TOP OF WEB IS CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED WEB & TOP OF WEB. FABRICATED & INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007040500096 20070405 00096 NM 2007 4 5 DHL2007786525 1 20070315 A 5322 SHEAR TIE BOEING 727 727214 138407R NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 786AT 21692 AFT CARGO COMPARTMENT AT BS 970, BETWEEN STR 28R AND 29R, SHEAR TIE HAS CORROSION. REMOVED FLOOR SUPPORT AT STA.990 TO 950E FOR ACCESS IAW SRM 51-30-2. REMOVED INTERCOSTAL BETWEEN 970-950E FOR ACCESS IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA AT SHEAR TIE BS970 STR 29R AND 28R DIM 4" BY 2" IAW B727 SRM 53-10-4. FABRICATED SHEAR TIE DOUBLER REPAIR MATERIAL USED 7075T6 .071 PO NR 9004150 DIM 6" BY 4" IAW B727 SRM 53-10-4. TREATED ALODINE AND PRIMED IAW B727 SRM 51-10-2. IN STALLED INTERCOSTAL AND FLOOR SUPPORT AT STA 990 TO 950E IAW B727 51-30-2. 2 L 7 3 4F A3WE 2007040500097 20070405 00097 NM 2007 4 5 07FDEA00940 1 20070316 A 5730 ARB75752 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT WING, LEADING EDGE NR 7 SLAT NR 15 TRACK CUT OUT FOUND CRACK. RIGHT WING, LEADING EDGE NR 7 SLAT NR 15 TRACK CUT OUT. REPAIRED AS PER SRM 57-10-00 FIG 21 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040500098 20070405 00098 NM 2007 4 5 07FDEA00941 1 20070316 A 5730 ARB75752 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT WING, LEADING EDGE NR 7 SLAT NR 14 TRACK CUT OUT FOUND CRACK. RIGHT WING, LEADING EDGE NR 7 SLAT NR 14 TRACK CUT OUT. REPAIRED AS PER SRM 57-10-00 FIG 21 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040500099 20070405 00099 NM 2007 4 5 07FDEA00942 1 20070316 A 5730 ARB75742 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT WING, LEADING EDGE NR 4 SLAT NR 10 TRACK CUT OUT FOUND CRACK. RIGHT WING, LEADING EDGE NR 4 SLAT NR 10 TRACK CUT OUT REPAIRED AS PER SRM 57-10-00 FIG 21 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040500100 20070405 00100 NM 2007 4 5 07FDEA00943 1 20070316 A 5730 ARB75741 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LEFT WING, LEADING EDGE NR 5 SLAT NR 12 TRACK CUT OUT FOUND CRACK. LEFT WING, LEADING EDGE NR 5 SLAT NR 12 TRACK CUT OU T REPAIRED AS PER SRM 57-10-00 FIG 21 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040500101 20070405 00101 EA 2007 4 5 COMA0760295 1 20070329 A 2150 DETECTOR CNDAIR CL600 CL6002B19 1900309 EA A/C PACK DIRTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 783CA 7315 FLIGHT 9451 - EN ROUTE BNA - CVG RECEIVED A DISPLAY COOL AND EXHAUST FAIL MESSAGE, FLIGHT DIVERTED TO EVV. CLEANED THE DISPLAY AIR FLOW DETECTOR. 2 L 7 2 4F RT A21EA 2007040500102 20070405 00102 EA 2007 4 5 COMA0760294 1 20070329 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS UNKNOWN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 720SW 7297 FLIGHT 5186 - DURING CLIMBOUT OF CVG RECEIVED A FLAP FAIL MESSAGE, FLIGHT RETURNED TO CVG. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007040500104 20070405 00104 NM 2007 4 5 2007UALA00905 1 20070326 A 3350 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 364UA 24533 EXTERIOR EMERGENCY LIGHT INOP EES, JUST AFT OF DOOR 1R. RELAMPED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007040500105 20070405 00105 NM 2007 4 5 2007UALA00906 1 20070325 A 2530 CHILLER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY MALFUNCTIONED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 646UA 25283 F/A'S REPORTED C/B'S IN AFT GALLEY POPPED. F/A'S IN MID CABIN REPORTED SMELL PRIOR TO C/B POPPING. [SUP 4-20-07] ALL CART CONTROLLER CB'S REPORTED POPPED AT SAME TIME. RESET CB'S. RAN CART CONTROLLERS FOR 5 MINUTES EACH. COULD NOT REPE AT PROBLEM. SUSPECT POWER SURGE. MID GALLEY ODOR DUE TO C31 CHILLER. CHILLER OPERATES LOUDLY AND CAUSING ELECTRICAL ODOR . NEEDS NEW CHILLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2007040500106 20070405 00106 2007 4 5 2007UALA00907 4 20070327 A 2565 GIRT BAR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE DOOR 1L FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA 25158 DOOR 1L GIRT BAR COULD NOT HOOK IN TOTALLY. [SUP 4-20-07] AFTER TROUBLESHOOTING, TIGHTENED 3 STRAPS ON THE SLIDE PACK RELEASE ASSEMBLY. DOOR ARMING AND DISARMING OPERATED NORMALLY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007040500107 20070405 00107 EU 2007 4 5 2007UALA00908 2 20070325 A 7200 ENGINE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 2 ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 370UA 24539 722353 OIL ODOR IN CABIN WITH RIGHT PACK ON. OIL ODOR WITH NR 2 ENG BLEED. NR 2 ENGINE REPLACED 2 L 7 2 4F 4 F RT A16WE E21EU 2007040500108 20070405 00108 NM 2007 4 5 2007UALA00909 1 20070324 A 2897 WIRE HARNESS BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUEL QTY IND DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 773UA 26929 LEFT FUEL QTY INTERMITTENT. [SUP 4-20-07] AFTER TROUBLESHOOTING DETERMINED THAT LT MAIN FUEL QTY HARNESS NEEDED REPLACI NG. FINISHED REMOVAL AND INSTALLATION OF LT MAIN FUEL QTY HARNESS PER MM 28-41-05. DUE TO LT WING FUEL QTY HARNESS REPL ACEMENT NEED TO OPS CHECK FQIS TANK UNITS AND DENSITOMETER PER MM 28-4 1-00-710-801 AND OPS CHECK FQPU PER MM 28-41-00-7 10-802. ACCOMPLISHED ALL CKS ALONG WITH FUEL TANK PANEL LEAK CHECKS. ALL TESTS AND OP CHECKS OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007040500109 20070405 00109 NM 2007 4 5 2007UALA00910 1 20070327 A 5320 WEB BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 303-294 S11L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 364UA 24533 FUSELAGE WEB IS CRACKED BS 303 - 294 STR 11 FWD END JUST FWD OF FWD OF FWD ENTRY DOOR. MAJOR REPAIR ACCOMPLISHED: INST ALLED REPLACEMENT SHEAR TIE & WEB. 2 L 7 2 4F 4 F RT A16WE E21EU 2007040500110 20070405 00110 NM 2007 4 5 2007UALA00911 1 20070328 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY EXIT CEILING LIGHT INOP AT ROW 4 RIGHT & JUST AFT OF ROW 8 RIGHT. [SUP 4-17-07] RELAMPED BOTH POSITION. OP CH ECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007040500111 20070405 00111 NM 2007 4 5 2007UALA00912 1 20070327 A 5210 BEARING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU PAX DOOR WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 AFT ENTRY DOOR CUTOUT BOTH SPHERICAL BEARINGS WORN AT UPPER AND LOWER DOOR ATTACH FITTING ON TORQUE TUBE. REPLACED THE UPPER & LOWER BEARINGS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007040500113 20070405 00113 NM 2007 4 5 2007UALA00914 1 20070327 A 5210 BEARING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU PAX DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 387UA 24662 AFT ENTRY DOOR CUTOUT TORQUE TUBE BEARINGS HAVE PLAY. REPLACED THE UPPER & LOWER BEARINGS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007040500114 20070405 00114 NM 2007 4 5 NACA20070011 1 20070209 A 5330 SKIN BOEING 737 737232 1384475 NM BS 767-787 CORRODED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 321DL 23093 AFT CARGO COMPARTMENT BILGE AREA HAS SURFACE CORROSION AT STA 787 BETWEEN STR 27L AND STR 27R. REMOVED CORROSION, PERFO RM ULTRASONIC THICKNESS TEST AND FOUND OUT OF LIMITS PER B737 SRM 53-30-1. FABRICATED REPAIR DOUBLER AND INSTALLED AT F USELAGE SKIN BS767 - BS787, L-26L - L-26R PER JOSSAIR DRAWING NR 73R5331458 REV I/R DATED 12 JAN 2007. 2 L 7 2 4F RT A16WE 2007040500115 20070405 00115 2007 4 5 2007UALA00915 4 20070327 A 2565 BOTTLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU DOOR SLIDE UNSERVICEABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 LOW BOTTLE PRESSURE. FOUND FUSIBLE PLUG LEAKING. REPLACED BOTTLE ON A/C. REMOVED AND REPLACED FUSIBLE PLUG ON UNIT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007040500116 20070405 00116 NM 2007 4 5 2007UALA00916 1 20070328 A 2750 FLAP SYSTEM BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU TE FLAPS UNKNOWN A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 913UA 25291 RECEIVED SPLIT FLAPS ON APPROACH BETWEEN FLAP POSITION 1 AND 2. [SUP 4-20-07] REPLACED FLAP POSITION INDICATOR. NO FA ULT FOUND. COULD NOT DUPLICATE ERROR. CAUSE UNKNOWN. 2 L 7 2 4F 4 F RT A16WE E21EU 2007040500117 20070405 00117 NM 2007 4 5 2007UALA00929 1 20070328 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1440 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 508UA 24744 AFT PIT STA 1440 AT STR 26L FRAME DENTED. *S/D* MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT DAMAGED INBOARD FLANGE. INSTA LLED A NESTED J-ANGLE DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007040500118 20070405 00118 NM 2007 4 5 2007UALA00930 1 20070328 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1681 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 508UA 24744 MAIN CABIN FLOORBEAM CORRODED STA 1681, BL 0 (AFT SHEAR WEB DECK PLATE). *S/D* MAJOR REPAIR ACCOMPLISHED: REMOVED DAM AGED AREA. INSTALLED DOUBLER-TRIPLER FILLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007040500119 20070405 00119 NM 2007 4 5 2007UALA00931 1 20070328 A 5320 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1681 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 508UA 24744 MAIN CABIN SHEAR WEB CORRODED STA 1681, RBL 16 TO RBL 50. *S/D* MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA. INS TALLED DOUBLER-TRIPLER FILLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007040500120 20070405 00120 2007 4 5 2007UALA00932 4 20070328 A 2565 SPRING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SLIDE GIRT BAR WEAK A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 644UA 25094 LEFT AFT MED DEPLOYMENT BAR GAS SPRING IS WEAK. [SUP 4-24-07] AFTER TROUBLESHOOTING FOUND WEAK GAS SPRING. REPLACED G AS SPRING PER MM 25-66-03. DEPLOYMENT BAR HAS PROPER SPRING TENSION. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007040500121 20070405 00121 NM 2007 4 5 2007UALA00939 1 20070329 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 802UA 690 DOOR 2R EMERGENCY EXIT LIGHT PLATE LOWER RIGHT SIDE INOP DURING TEST. SECURED & REPLACED POWER SUPPLY BATTERY. SYSTEM OPERATES NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007040500122 20070405 00122 2007 4 5 2007UALA00940 4 20070329 A 2565 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU DOOR 1R READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 THE 1R SLIDE PRESSURE LOW. [SUP 05-16-07] REPLACED SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007040500123 20070405 00123 NM 2007 4 5 2007UALA00933 1 20070328 A 2497 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE ELECTRONIC UNIT MELTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 771UA 26932 OVERHEAD ELECTRONICS UNIT DIRECTLY BELOW CENTER VHF ANTENNA FOUND BURNT AND MELTED. [SUP 4-24-07] REPLACED OVERHEAD EL ECTRONICS UNIT CONNECTOR. SUSPECT ELECTRICAL SHORT IN OEU CONNECTOR CAUSED MOMENTARY HIGH CURRENT CONDITION. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007040500124 20070405 00124 EU 2007 4 5 2007UALA00934 1 20070328 A 3040 CONTROLLER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE WINDOW HEAT INOPERATIVE A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 474UA 1475 CAPTAIN'S SLIDING WINDOW HEATING INOPERATIVE. [SUP 06-01-07] INITIALLY REPLACED THE NR 1 WINDOW HEAT CONTROLLER BUT L ATER DETERMINED THAT SLIDING WINDOW WAS DEFECTIVE. WINDOW INTERNAL TEMPERATURE SENSORS MISREPORTING TEMP TOO LOW, CAUSIN G HEAT CONTROLLER TO OVERHEAT WINDOW. 2 L 7 2 4F 4 F RT A28NM E40NE 2007040500164 20070405 00164 NM 2007 4 5 SWAA071679 1 20070402 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040500165 20070405 00165 NM 2007 4 5 SWAA071680 1 20070402 A 5311 6546554 FRAME BOEING 737 7373H4 1384600 NM BS 847 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040500166 20070405 00166 NM 2007 4 5 SWAA071681 1 20070402 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM BS 867 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040500167 20070405 00167 NM 2007 4 5 SWAA071682 1 20070402 A 5311 6546557 FRAME BOEING 737 7373H4 1384600 NM BS 887 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040500168 20070405 00168 NM 2007 4 5 SWAA071718 1 20070403 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM BS 1016 S3R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 3R. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007040500169 20070405 00169 NM 2007 4 5 SWAA071674 1 20070402 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040500170 20070405 00170 EU 2007 4 5 07FDEA01147 1 20070327 A 2131 82010B040901 CONTROLLER AIRBUS 310 A310222 3930315 EU CABIN PRESSURE MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 417FE 333 ON CLIMB-OUT THRU 250 CAB PRESS ADVISORY V/S 2500/ MIN SWITCHED TO NR 1 REG NO HELP. NR 1 REG SYSTEM PAGE NORMAL BUT CA BIN PRESSURE STILL CLIMBING AT 2500 FT/MIN. INITIATED EMERG DTCS ECAMS INCLUDED: VENT BLOWER LO FLOW, NR 1 CAB REG FA ULT AND NR 1 CAB PRESS VALVES FAULT, NO HELP ON RED TABS, QRH, AIR TURN BACK TO VHHH MEL/CDL: 21-31-02-A. REMOVED AND R EPLACED NR 1 CABIN PRESS CONTROLLER AND SYS NR 1 AFT PRESS REGULATING VLV PER MM. 2 L 7 2 4F RT A35EU 2007040500171 20070405 00171 NM 2007 4 5 07FDEA01165 1 20070328 A 5345 69159891 SHELF BOEING 727 727225 1384077 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 E/E COMPARTMENT MIDDLE EQUIPMENT RACK LT SIDE VHF SHELF CRACKED AT LT AFT ATTACH POINT BELOW COMPARATOR WARN UNIT. F ABRICATED AND INSTALLED NEW SHELF SUPPORT ANGLE REF BOEING DRAWING 69-15989, SRM 51-10-02 PAGE 7 AND SRM 51-30-02. SYST EM OPS CHECKED GOOD REF MM 34-31-001-5, AND 34-63-011-4. 2 L 7 3 4F A3WE 2007040500172 20070405 00172 NM 2007 4 5 07FDEA01166 1 20070328 A 5320 65561701 THRESHOLD BOEING 727 727225 1384077 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FOUND FORWARD LOWER CARGO DOOR, AFT THRESHOLD IS CRACKED ON FWD END. RECEIVED REPAIRED THRESHOLD, REPAIRED REF DRAWING SR27-53-025 REV. C BY IDENTIFYING BASE METAL, PREPPED, WELDED AND INSPECTED REF WO NR 11841-1000-0001. FWD LOWER CARGO DOOR AFT THRESHOLD WILL BE INSTALLED ON W/C 71C201-02. 2 L 7 3 4F A3WE 2007040500173 20070405 00173 NM 2007 4 5 07FDEA01167 1 20070328 A 5320 66126924 ANGLE BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 AIR STAIRS AREA LT SIDE, STA 1342 INBD DUCT SUPPORT ANGLE IS CRACKED LOWER END AT LBL 40. REMOVED AND REPLACED LT SIDE STA 1342 IB DUCT SUPPORT ANGLE REF SRM 51-30-02 PAGE 1. 2 L 7 3 4F 4 F A3WE E2EA 2007040500174 20070405 00174 WP 2007 4 5 07FDEA01169 1 20070328 A 5347 FX511001N305 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 571FE 47830 DURING C CHECK AT MAE, FOUND SEAT TRACK AT FS 909-1129 LBL 28 GOUGED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-31-01. 2 L 7 3 4F RT A22WE 2007040500175 20070405 00175 NM 2007 4 5 07FDEA01170 1 20070328 A 5330 652555745 PANEL BOEING 727 727225 1384077 NM ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 LOWER FUSELAGE PANEL NR 3622 (ADF NR 2 SENSE ANTENNA) PANEL HAS MULTIPLE LARGE AREAS OF DELAM, MULTIPLE ELONGATED FASTEN ER HOLES AND PANEL IS EXCESSIVELY HEAVY. REMOVED DAMAGED PANEL ASSY AND INSTALLED SERVICEABLE PANEL ASSY REF SRM 51-30- 2 PAGE 9. VERIFIED ADF SENSE ANTENNA WAS HOOKED UP. 2 L 7 3 4F A3WE 2007040500176 20070405 00176 WP 2007 4 5 07FDEA01171 1 20070328 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 571FE 47830 FUSELAGE LOW EXTERNAL SKIN HAS EVIDENCE OF CORROSION WITH BULGED AREA AND SHEARED FASTENERS AT F/L 1851 STR 51L - 51R. REMOVED CORROSION AT STA 1851 ORIGNAL THICKNESS .063, MATERIAL LOSS .035, OUT OF LIMITS. FAB`D REPAIR DOUBLER AND FIL LER, INSTALLED DOUBLER AND FILLER. 2 L 7 3 4F RT A22WE 2007040500177 20070405 00177 NM 2007 4 5 07FDEA01172 1 20070328 A 5523 657279971 TAB BOEING 727 727225 1384077 NM ZONE 300 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 LT HORIZONTAL STAB ELEVATOR TAB UPPER SURFACE HAS SPOT OF CRUSH WITH DELAM AT 9.5" OB OF INBD EDGE, ALSO SMALL DELAM ON UPPER 1" O/B. RECEIVED SERVICEABLE TAB ASSY WAS REMOVED AND WILL BE REINSTALLED ON WC E7-5520- 7-3307, WO NR 35851. 2 L 7 3 4F A3WE 2007040500178 20070405 00178 NM 2007 4 5 SWAA071675 1 20070402 A 5311 6546595 FRAME BOEING 737 7373H4 1384600 NM BS 727A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007040500179 20070405 00179 NM 2007 4 5 SWAA071717 1 20070403 A 5511 6547507 RIB BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND RIGHT HORIZONTAL STAB RIB LOWER CHORD CRACKED AT STA 120. REMOVED AND REPLACED RIB CH ORD PER SRM. 2 L 7 2 4F RT A16WE 2007040600011 20070406 00011 NM 2007 4 6 SWAA071689 1 20070402 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 484WN 33841 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 17 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007040600015 20070406 00015 NM 2007 4 6 07FDEA01196 1 20070330 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 870-960 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 MAIN CABIN SEAT TRACK STA 870-960 RBL 45 HAS SEVERAL AREA'S OF CORROSION. REMOVED SEAT TRACK AND FLOATING TRACK IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK FROM MAE TRAVELER T7/667877, MATERIAL 60-6549/24, BATCH NR 866725. INSTALLED NEW SE AT TRACK AND FLOATING TRACK IAW 51-30-2. 2 L 7 3 4F A3WE 2007040600017 20070406 00017 NM 2007 4 6 07FDEA01198 1 20070330 A 5330 651842016 SKIN BOEING 727 727225 1384077 NM BS 277 S29R DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 NLG CUTOUT FWD EDGE SKIN BENT/CREASED, REMOVED DAMAGE AREA. FABRICATED REPAIR DOUBLER AND INSTALLED REF SRM 53-30-3 FIG 1. THIS REPAIR IS A CATEGORY '"B" REPAIR. INSPECTION THRESHOLD IS 45,000 CYCLES REF SRM 53-30-3 FIG TABLE 3. 2 L 7 3 4F A3WE 2007040600018 20070406 00018 NM 2007 4 6 07FDEA01199 1 20070330 A 5754 65162095 SKIN BOEING 727 727225 1384077 NM LT WING SLAT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 LT WING LE, AT NR 4 SLAT OB HOOK CUTOUT CRACKED REMOVED DAMAGED AREA, REF SRM -30-4, NDT AREA AFTER BLEND OUT, NO DEFECT S NOTED REF B727NDT MANUAL PART 6. FABRICATED AND INSTALLED REPAIR REF SRM 57-30-4 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2007040600019 20070406 00019 NM 2007 4 6 SWAA071714 1 20070403 A 5753 6547901 FLAP TRACK BOEING 737 7373H4 1384600 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING OUTBOARD MID FLAP INBOARD FORE FLAP TRACK CORRODED. REMOVED AND REPLACED F ORE FLAP TRACK PER MM. 2 L 7 2 4F RT A16WE 2007040600036 20070406 00036 EU 2007 4 6 07FDEA01176 1 20070329 A 5311 A53610670207 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 MISDRILLED HOLE AT FRAME 13A DURING ACCOMPLISHMENT OF DR 179. REPAIR PERFORMED BY REAM UP AND COLD WORKING IAW EA 6-531 2-106395 A AND RAS/AS/010/2007 ISS. C 2 L 7 2 4F RT A35EU 2007040600037 20070406 00037 EU 2007 4 6 07FDEA01177 1 20070329 A 5710 R57150404 ANGLE AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 CRACKS IN SEALING ANGLE AND AFT SPLICE, RT, FOUND DURING ACCOMPLISHMENT OF EO 6-5710-7-5002 PART 4 REPAIR PERFORMED BY S EALING ANGLE REPLACEMENT IAW DRAWING R571-50404, APPROVED BY EO 5-5710-7-5002. 2 L 7 2 4F RT A35EU 2007040600040 20070406 00040 NM 2007 4 6 07FDEA01180 1 20070329 A 5730 6521656702 SKIN PANEL BOEING 727 727225 1384077 NM RT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 RT WING PANEL NR 8505 OUTER SURFACE FWD EDGE I/B IS DAMAGED REMOVED PANEL REF SRM 51-30-02. REPAIRED PANEL REF SRM 51- 40-20 PAGES 12, 46, 53 THRU 62. PRIMED AND PAINTED, REF MM 51-20-151-7. INSTALLED PANEL REF 20-10-023-4 PARA 4B (2). 2 L 7 3 4F A3WE 2007040600041 20070406 00041 NM 2007 4 6 07FDEA01181 1 20070329 A 5347 6520827233 FLOORBEAM BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 UPPER MAIN CARGO FLOOR STRUCTURE HAS DEEP SCRIBE ON UPPER SURFACE TEE AT STA 720D, RBL 27" TO RBL 44" STR 17R. REMOVED UPPER TEE FROM RBL 14 TO RBL 65 AND REPAIRED WITH SUPPORT ANGLES AND REINFORCEMENT STRAP AT SPLICE REF SRM 53-10-8/ FIG NR 3 PAGES 18-23. 2 L 7 3 4F A3WE 2007040600042 20070406 00042 NM 2007 4 6 07FDEA01182 1 20070329 A 5752 652173623 TAB BOEING 727 727225 1384077 NM ZONE 500 DELAMINATED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 463FE 22551 LT WING IB AILERON TAB CONTROL ARM FAIRING IS DISBONDED AT AFT EDGE CLEANED AREA, REPAIRED FAIRING REFERENCE SOPM 20-50- 12 PAGE 11 PARA 4. 2 L 7 3 4F A3WE 2007040600045 20070406 00045 2007 4 6 SWAA071685 4 20070402 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007040600052 20070406 00052 NM 2007 4 6 UPS07649573 1 20070307 A 5330 DOUBLER BOEING 767 76734AF 1385212 NM BS 490 BL0 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 322UP 27748 INSPECTION TYPE:1C SKIN DOUBLER CORRODED AT LWR 1090 ANT BS 490 BL 0. REMOVED, FABRICATED REPLACEMENT DOUBLER AND INST ALLED PER DWG 100-82778, SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007040600059 20070406 00059 NM 2007 4 6 07FDEA01208 1 20070330 A 5751 65727344 SKIN BOEING 727 727225 1384077 NM ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 RT OTBD AILERON OTBD T/E UPPER AND LOWER SURFACE IS DELAMINATED FROM CORE. REMOVED AND REPLACED RT OTBD AILERON REF MM 27-10-031-2. 2 L 7 3 4F A3WE 2007040600079 20070406 00079 NM 2007 4 6 07FDEA01168 1 20070328 A 5730 6521795333 SKIN BOEING 727 727225 1384077 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 RT WING NR 6 MOVEABLE FAIRING SKIN FWD OB EDGE IS CRACKED. REPAIRED FAIRING REF SRM 51-10-1, 57-20-2, 51-40-2 AND MM 51 -20-151-7. 2 L 7 3 4F A3WE 2007040600082 20070406 00082 NM 2007 4 6 07FDEA01188 1 20070329 A 5330 651753033 SKIN BOEING 727 727225 1384077 NM BS 1223 S25R MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FOUND EXTERNAL FUSELAGE REPAIR AT APPROX STA1223, STR 25R. REPAIR DOES NOT CONFORM TO SRM 53-30-3 FIG 3. REMOVE EXTERN AL DOUBLER FROM A/C REF SRM 51-30-2. MFG NEW REPAIR DOUBLER REF SRM 53-30-3 FIG 3. INSTALLED NEW REPAIR DOUBLER REF S RM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 2007040600097 20070406 00097 WP 2007 4 6 MWEA070067 1 20070329 A 3350 P4010021 BATTERY DOUG DC9 DC981 3022081 WP FLASHLIGHT INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 812ME 48006 FORWARD EMERGENCY FLASHLIGHT NOT BLINKING. REMOVED AND REPLACED BATTERY. 2 L 7 2 4F A6WE 2007040600105 20070406 00105 NM 2007 4 6 NWAA071193151 1 20070328 A 2120 UNKNOWN AIRBUS A319 A319114 3930350 NM COCKPIT ODOR A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 01 351NB 1820 ON DESCENT INTO MSP, FIRST OFFICER AND CAPTAIN NOTICED A STRONG BURNING ODOR LIKE ELECTRICAL AND NO SMOKE OBSERVED. THE LEAD FLIGHT ATTENDANT ALSO NOTICED THE ODOR IN THE FORWARD CABIN AND NOTHING FOUND IN THE FORWARD OVENS. ODOR DISSIPAT ED AFTER 3 TO 5 MINUTES AND LANDING WAS UNEVENTFUL. CHECK E/E BAYS, BATTERY COMPARTMENT AND RAN OVENS, COFFEE MAKERS, A IR CONDITIONING PACKS AND CLEANED COFFEE HOT PLATES AND NO ODORS NOTED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2007040600125 20070406 00125 NM 2007 4 6 P5CA0701519 1 20070326 A 2800 UNKNOWN BOEING 747 74747UF 1384949 NM JETTISON PUMP UNKNOWN A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 496MC 29257 AFTER BLOCK OUT, MAIN TANK NR 2 FWD OVERRIDE/JETTISON PUMP FAIL STATUS MESSAGE DISPLAYED. OPENED MEL 28-31-2C, COMPLIED WITH DDG. 2 L 7 4 4F RT 1384945 2007040600139 20070406 00139 CE 2007 4 6 DXTA200702080 1 20070404 A 3320 LIGHT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LAVATORY ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 938QS 7500183 OVERHEAD LIGHTS IN LAV ARE INTERMITTENT. AFTER TURNING LIGHTS ON AND OFF SEVERAL TIMES A BURNING ODOR WAS NOTED. REMOV ED RT AND LT OVERHEAD LIGHT PANELS IN LAV. INSPECTED LIGHT AND BALLAST ASSY. FOUND R/H TOP LIGHT TO BE BURNT AND PLASTIC END MELTED. REMOVED LIGHT AND INSTALLED NEW CUSTOMER SUPPLIED LIGHT, CYCLED LAV LIGHTS SEVERAL TIMES. OPS CHECK GOOD. A LL WORK I.A.W. CESSNA CITATION 750 M/M 33-00-33 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007040600141 20070406 00141 CE 2007 4 6 MWA70316066 1 20070327 A 5711 1181000131 SPAR CAP BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA LT WING DAMAGED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 166YV UE166 DISCOVERED DURING F-CHECK, DOUBLE-DRILLED HOLE LOWER FORWARD LT SPAR CAP AT APPROXIMATELY WS 81.5. REPAIRED IAW ENGINEE RING REPORT 6631-1. 2 L 7 2 4T 3 T RT A24CE E2NE 2007040600154 20070406 00154 NM 2007 4 6 UPS07M49555 1 20070125 A 5753 ARC27362444 SKIN DOUG MD11 MD11F 3023600 NM TE FLAP DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C RE SKIN I/B FLAP LOWER AFT I/B AND O/B SEGMENTS DUE MULTIPLE DENTS. REMOVED RIGHT WING I/B FLAP CARTR IDGE PER AMM27-51-04 R55. REMOVED BOTH I/B AND O/B SEGMENT PER AMM20-50-02. RIGHT WING FLAP LWR I/B & O/B SEGMENT SKIN REMOVED PER SRM 51-31-01 R38 V2. RIGHT WING FLAP LWR AFT I/B & O/B SEGMENT LWR SKIN FAB PER DWG ARC2736 & ARC2444. NE W SKIN HOLE PICKED UP. RE-INSTALLATION CUT OUT PER SRM 51-31-01 V2 R38. OPN CUTOUT CHECK, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007040900004 20070409 00004 WP 2007 4 9 07FDEA01267 1 20070403 A 5511 SPAR CAP DOUG DC10 DC1010 3022110 WP HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 HORIZONTAL STAB SPAR CAP FOUND CRACK LONG .750" AND .800" REPAIRED IAW FEDEX EA 8-5510-96110. 2 L 7 3 4F A22WE 2007040900027 20070409 00027 WP 2007 4 9 07FDEA01215 1 20070331 A 3230 LANDING GEAR DOUG MD10 MD1010F 3022112 WP MAINS MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION DE DESCENT 1 SO 25 365FE 46601 DURING NORMAL LG EXTENSION, COCKPIT PANEL GEAR LIGHTS AND SD CONFIG LIGHTS INDICATED RED, ALL 3 LG LIGHTS WERE RED ON B OTH INDICATORS. ALTERNATE EXTENSION RESULTED IN 3 GREEN ON BOTH PANEL (COCKPIT PANEL AND CONFIG SD). WHEN THE LG HANDL E WAS PLACED DOWN, IT FELT LIKE THE GEAR EXTENDED, BUT NO GREEN INDICATIONS, RED LT WAS ON IN LG HANDLE; LG NOT DOWN WAR NING SOUNDED; "LANDING GEAR" IN ESSENTIAL ITEMS BOX PRIOR TO ALTERNATE EXTENSION. REMOVED AND REPLACED LANDING GEAR HAN DLE SWITCH S1- 431 PER MM 32-31-02-2. JACKED A/C AS PER MM 07-11- 00-2, AND PERFORMED GEAR SWING PER MM 32-30-00-0 AL INDICATIONS ARE NORMAL. 2 L 7 3 4F RT A22WE 2007040900034 20070409 00034 NM 2007 4 9 TAMF20070001S 1 20070321 A 5350 FAIRING BOEING 767 767200 1385120 NM GE CF6 CF680 30025 NE BS 1080 CRACKED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 767QT 23804 DURING INSPECTION, FOUND A CRACK AT AFT WING FAIRING WEB STA 1080, BL 62-70, LT. DAMAGED AREA WAS REPAIRED IAW MFG SERV ICE REQUEST 1-303353670 AND EWO 767-53-031. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007040900038 20070409 00038 NM 2007 4 9 07FDEA01220 1 20070331 A 5610 53FX889501 PLUG BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 THE SECOND WINDOW PLUG AFT OF THE LEFT AFT EMERGENCY ESCAPE HATCH HAS CORROSION UNDER THE SEAL AT THE FWD LOWER PLUG RET AINER REMOVED WINDOW PLUG, REF MM 56-20-000-4 PG 1. DRILLED HOLE IN THE WINDOW PLUG FOR JUMPER STRAP, REF EO NR 7-5620- 7-4304. INSTALLED WINDOW PLUG REF MM 56-20-000-4 PG 2-4. 2 L 7 3 4F A3WE 2007040900045 20070409 00045 EU 2007 4 9 07FDEA01227 1 20070401 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 MAIN CARGO DECK SEAT TRACK HAS GOUGES TWO PLACES, FRAME 61, CL - 0. REMOVED AND REPLACED SEAT TRACK, BL - 0. FROM STA 5 8 TO STA 62.5 AND REPAIRED IAW SRM 53-10-16, FIG 202. CLASSIFIED AS MINOR REPAIR. 2 L 7 2 4F RT A35EU 2007040900047 20070409 00047 EU 2007 4 9 07FDEA01252 1 20070403 A 5730 SKIN AIRBUS 310 A310324 3930206 EU ZONE 500 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 FOUND CORROSION ON LT WING BOTTOM SKIN PANEL 2 IN THE AREA OF RIB 1-4 AROUND SEVERAL FASTENERS. REPAIR PERFORMED BY BLE ND OUT CORROSION IAW EA 6-5720-101272 AND SRM 57-00-00 4.C.3(B), APPROVED BY RAS/BAE/1002868/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040900065 20070409 00065 NM 2007 4 9 DU4R2007080 1 20070327 A 5210 140N27259 ROD END BOEING 757 757232 1384965 NM L1 DOOR CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND CORROSION ON L-1 DOOR RUST ON LATCH CONTROL ROD, 2 ROD ENDS. REPAIRED BY REMOVING AND REPLACING ROD ENDS WITH P/N 140N2725-9 IAW BOEING CMM 52-11-07. 2 L 7 2 4F RT A2NM 2007040900076 20070409 00076 WP 2007 4 9 UPS07849557 1 20070326 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 EMERGENCY EXIT LIGHTS INOP, OP PRE-DEP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OP CHECKS GOOD PER MM 33-50-01-2. 2 L 7 4 4F RT 4A25 2007040900079 20070409 00079 NM 2007 4 9 DU4R2007083 1 20070402 A 5322 SHEAR TIE BOEING 757 757232 1384965 NM BS 1400 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND CORROSION IN AFT PIT ON SHEAR CLIP (AFT SIDE) BS 1400 S-29L AND S-30. REPAIRED BY REMOVING SHEAR CLIP. FABRICATE D AND INSTALLED NEW SHEAR TIE FROM 7075-T6 .063 4.7" BY 1.2" IAW B757 SRM 51-40-02 BOEING DWG 146N1011 AND 146N1603. 2 L 7 2 4F RT A2NM 2007040900104 20070409 00104 WP 2007 4 9 UPS07849598 1 20070307 A 5312 56122987 PRESSURE PANEL DOUG DC8 DC873F 302199F WP NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C3 CRACK IN NLG WHEEL WELL CEILING (PRESSURE WEB) STA -13 LBL 2. REPAIRED PRESSURE WEB IN NLG WHEEL WEL L CEILING AT STA -13 LBL 2 IAW SAA EA008-5330-01-A0745, UPS EO DC8-5330-26455-A, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007040900105 20070409 00105 WP 2007 4 9 UPS07849599 1 20070308 A 5313 5750043501 LONGERON DOUG DC8 DC873F 302199F WP FS 662 L36 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C3 L36 HEAVILY CORRODED AT STA 662. REPAIRED LONGERON 36 AT STA 662 IAW SAA EA 008-5310-01-A0734, UPS E O DC8-5310-26461-A, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007040900111 20070409 00111 NM 2007 4 9 CALA0700165 1 20070403 A 2612 4739551 MODULE BOEING 737 737800* NM FIRE DETECTION INOPERATIVE A CALA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 79279 11550 31597 THE FORWARD CARGO FIRE LIGHT ILLUMINATED ON CLIMBOUT FROM EWR AT 17,000 FEET. BOTH FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE FORWARD CARGO COMPARTMENT AND FOUND NO EVIDENCE OF FIRE. TROUBLESHOOTING WAS UNABLE TO CONFIRM FAULT. THE CARGO FIRE DETECTION CONTROL MODULE WAS R EPLACED AS A PRECAUTIONARY MEASURE IAW MM 26-00-02 AND OPERATIONAL CHECKS WERE GOOD. IN ADDITION, BOTH FIRE BOTTLES WER E REPLACED IAW MM 26-23-01. 2 L 7 2 4F RT A16WE 2007040900112 20070409 00112 EU 2007 4 9 AWXA200700464 1 20070331 A 5321 D5367005000200 FLOOR PANEL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 SAL - CORROSION ON AFT GALLEY FLOORBOARD 261 FF, FR 66 - FR 68, +Y1292 TO +Y1732. REPLACED AFT GALLEY FLOORBOARD 261 F F, FR 66 - FR 68, +Y1292 TO +Y1732 IAW AWA TASK CARD C1C53303. 2 L 7 2 4F RT A28NM 2007040900113 20070409 00113 EU 2007 4 9 AWXA200700465 1 20070331 A 5321 D5361060500100 FLOOR PANEL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 SAL - CORROSION ON FORWARD GALLEY FLOORBOARD 222 FF, FR 16 - FR 20, -Y1292 TO -Y1732. REPLACED FORWARD GALLEY FLOORBOA RD 222 FF, FR 16 - FR 20, -Y1292 TO -Y1732 IAW AWA TASK CARD C1C53302. 2 L 7 2 4F RT A28NM 2007040900114 20070409 00114 EA 2007 4 9 QXEA200700512 1 20070405 A 3830 14302211 TIMER CNDAIR CL600 CL6002C10 1390015 EA LAVATORY MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 606QX 10023 DEN - FLIGHT 4277 - ON TAXI LAVATORY RUNS ALL THE TIME AND IS LEAKING FLUID. RETURNED TO THE GATE. MAINTNEANCE REPLACE D THE GASKETS AND TIMER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007040900117 20070409 00117 EA 2007 4 9 QXEA200700500 1 20070401 A 2432 100021102 CHARGER CNDAIR CL600 CL6002C10 1390015 EA APU BATTERY FAILED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 614QX 12494 4706 10049 PDX - FLIGHT 2575, ON TAXI RECEIVED A APU BATTERY CHARGER STATUS MESSAGE. RETURNED TO THE GATE. MAINTENANCE REPLACED T HE APU BATTERY CHARGER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007040900118 20070409 00118 EA 2007 4 9 QXEA200700515 1 20070331 A 2711 CC670511143 CONTROL PANEL CNDAIR CL600 CL6002C10 1390015 EA AILERON TRIM MALFUNCTIONED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 600QX 10005 SEA- UNABLE TO TRIM THE AILERONS TO THE LEFT. MAINTENANCE REPLACED THE AILERON/RUDDER TRIM CONTROL PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007040900119 20070409 00119 NM 2007 4 9 QXEANM09410 1 20070313 A 4920 164161100 DRAIN VALVE BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA APU CLOGGED G QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 BALL ON WRONG SIDE OF SPRING CREATING CLOSED CONDITION AND NOT ALLOWING PROPER DRAINAGE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2007040900123 20070409 00123 CE 2007 4 9 DXTA200702087 1 20070406 A 3234 HANDLE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG STUCK E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 951QS 7500151 LANDING GEAR HANDLE WOULD NOT MOVE TO THE GEAR RETRACTED/ GEAR UP POSITION AFTER TAKEOFF. GEAR REMAINED EXTENDED. RIGGED NOSE LANDING GEAR SQUAT SWITCH IAW 750 MM CHP 32-60-00 LANDING GEAR SYSTEM. OPS CKED GOOD IAW 750 MM CHP 32-30-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007040900124 20070409 00124 EU 2007 4 9 MALA070048 1 20070403 A 5350 SKIN SAAB SF340 340B 7860101 EU TAIL CONE PUNCTURED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 422XJ 340B422 AIRCRAFT WAS STRUCK BY A MANLIFT IN MSP CAUSING A PUNCTURE IN THE AFT LT TAIL CONE SKIN AT STATION 825. PERMANENT REPAI R COMPLETED IAW MAL EO#S53418. 2 L 7 2 4T RT A52EU 2007040900127 20070409 00127 NM 2007 4 9 HALA0700155 1 20070405 A 4920 ECU BOEING 767 767300 1385204 NM APU MALFUNCTIONED A HALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 13 590HA 33467 ETOPS SIGNIFICANT SYSTEM, APU FAILED TO START. MAX TEMP 779 WHEN SHUT DOWN AND 25 PERCENT RPM. OIL WAS FULL AT START T HEN WENT TO .75. PERFORMED APU ECU BITE PER FIM 49-11-00, NO FAULTS NOTED. START ATTEMPT EGT WITHIN LIMITS PER AMM TSK 49-11-00. PERFORMED NORMAL APU START OPS CK GOOD. ADDED 1 PT OIL TO APU. LEAK CK GOOD. 2 L 7 2 4F RT A1NM 2007040900128 20070409 00128 NM 2007 4 9 HALA0700154 1 20070404 A 2150 UNKNOWN BOEING 767 76733A 1385209 NM RT A/C PACK UNKNOWN A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 593HA 33424 ETOPS SIGNIFICANT SYSTEM, RT PACK INOP LIGHT ILLUMINATED. PERFORMED BITE PROCEDURE AT R14 PACK TEMP CONTROLLER PER FIM 21-51-00-1 FIG 103. NO FAULTS NOTED RAN RT PACK FROM APU AIR, NO DEFECTS NOTED. OPS CK NML. 2 L 7 2 4F RT A1NM 2007040900129 20070409 00129 NM 2007 4 9 HALA0700153 1 20070404 A 8011 35054367 STARTER BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE RT ENGINE FAILED A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 582HA 7037 7037 28139 ETOPS SIGNIFICANT SYSTEM, RIGHT STARTER CUTOUT EICAS MESSAGE AFTER RIGHT ENGINE START. ACCOMPLISHED CHECKLIST. STARTER FAILED, REMOVED AND REPLACED RT ENG STARTER AND START VALVE PER AMM 80-11-01-004-001-N00/80-11-01-404-014-N00. SERVD P ER 12-13-02-603-019-003, REPLACED START VALVE PER AMM 80-11-02/401. PERFORMED ENGINE START, VERIFIED OPERATION ON N2 TA CH, COWLING CLOSED AND SECURED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007040900134 20070409 00134 CE 2007 4 9 DXTA200702090 1 20070407 A 2150 A/C PACK CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL ODOR E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 984QS 7500084 THE COCKPIT PAC TEMPERATURE IS UNCONTROLLABLE IN BOTH MANUAL AND AUTO MODES. IT GOES TO FULL HOT TEMPERATURE AND PRODUCE S A FOUL OILY ODOR IN THE CABIN. DIVERTED. [SUP 4-19-07] REMOVED & REPLACED ACM, HOUSING & ASPIRATOR IAW HAMILTON SUN STRAND CMM 21-50-03 & 750 M/M 21-51-00. OPS CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007040900135 20070409 00135 2007 4 9 DXTA200702092 4 20070407 A 2210 INDICATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TRIM OUT OF RIG E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 946QS 7500195 DURING TAXI, YD NOT CENTERED AND FGC, B FAIL CAS MESSAGE CAME ON INTERMITTENT. IN FLIGHT DURING TURBULENCE THE YD NOT C ENTER CAS MESSAGE CAME ON INTERMITTENT. [SUP 4-19-07] FOUND TRIM SWITCH INDICATOR OUT OF RIG. RIGGED IAW CE-750 M.M. 2 7-14-00. ALSO, ADJUSTED TRIM TRAVELS (OUT OF RIG) IAW CE-750 M.M. 27-20-00. RIG & OPS CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007040900136 20070409 00136 NM 2007 4 9 QXEA200700509 1 20070403 A 3150 LIMIT SWITCH DHAV DHC8 DHC8202 2809007 NM OUT OF ADJUST A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 367PH 511 PDX - ON FLIGHT 2230, TAKEOFF WARNING HORN SOUNDED DURING TAKEOFF, CONFIGURATION TEST ON TAXI OUT. CHECKED CONFIGURATIO N AND HORN STILL SOUNDED. MAINTENANCE ADJUSTED CONDITION LEVER LIMIT SWITCHES. PERFORMED FUNCTIONAL TEST OF THE TAKEOF F WARNING HORN, FUNCTIONAL TEST GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007040900139 20070409 00139 NM 2007 4 9 QXEA200700510 1 20070403 A 3010 4100S00503 VALVE BOMBDR DHC8 DHC8402 1390042 NM RT WING MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 414QX 4578 11 4061 BOI FLIGHT 2406: DEICE PRESSURE CAUTION LIGHT CAME ON DURING DESCENT. RT WING OUTBOARD LIGHT DID NOT ILLUMINATE. C/W E /A CHECKLIST. MAINTENANCE C/W FUNCTIONAL CHECK OF AIRFRAME PNEUMATIC SYSTEM IAW AMM. COULD NOT DUPLICATE PILOT REPORT. REMOVED AND REPLACED RT OUTBOARD DDV IAW AMM. REMOVED AND REINSTALLED LEADING EDGE FOR DDV R7R. SYSTEM OPS CHECKED G OOD. RII WAS C/W. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007040900140 20070409 00140 NM 2007 4 9 QXEANM09424 1 20070313 A 4920 164161100 DRAIN VALVE SUNDSTRANDAI BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA APU DAMAGED G QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 424QX 4006 BALL ON WRONG SIDE OF SPRING ALLOWING IMPROPER DRAINAGE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2007040900141 20070409 00141 NM 2007 4 9 KNNA200700020 1 20070304 A 5210 2024T3 SKIN BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE L2 DOOR DAMAGED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 326DL 23098 MAIN ENTRY DOOR L-2 EXTERIOR SURFACE, UPPER AFT CORNER, SKIN BEND. PROVIDE INSTRUCTIONS ON REPAIR OF DOOR SKIN. CUT OU T BEND CORNER AND REPAIR PER SRM 52-00-3 FIGURE 5. 2 L 7 2 4F 4 F RT A16WE E2EA 2007040900142 20070409 00142 NM 2007 4 9 KNNA200700021 1 20070309 A 5315 65554846 FLOORBEAM BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE BS 460 CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 326DL 23098 CARGO FLOORBEAM CRACKED AT BS 460, RBBL 14.5 FWD CARGO COMPARTMENT. PROVIDE INSTRUCTIONS ON REPAIR OF CARGO FLOORBEAM B S 460 RBL 14.5. REMOVED AND REPLACED CARGO DOOR FLOORBEAM SRM 53-10-5 FIGURE 11. 2 L 7 2 4F 4 F RT A16WE E2EA 2007040900143 20070409 00143 NM 2007 4 9 KNNA200700024 1 20070309 A 5330 2024T3 SKIN BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE BS 500A CORRODED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 326DL 23098 CORRODED SKIN AT BS 500A+ 10' BETWEEN STR 27L/28L. PROVIDE INSTRUCTION ON REPAIR OF CORRODED EXTERIOR SKIN STA 500A + 1 0' STR 27L/28L. 2 L 7 2 4F 4 F RT A16WE E2EA 2007040900144 20070409 00144 NM 2007 4 9 KNNA200700025 1 20070311 A 5330 2024T3 SKIN BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE BS 927 S27L/R CORRODED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 326DL 23098 AFT CARGO PIT INTERIOR BILGE, BS 927 BETWEEN STR-27L STR AND 27R, FRAME BOTTOM SIDE CORRODED. PROVIDE INSTRUCTIONS ON R EPAIR OF CORROSION AFT CARGO PIT, INTERIOR BILGE BS 927 BETWEEN STR 27L AND STR 28 R BOEING SRM 53-10-4 FIGURE 7. 2 L 7 2 4F 4 F RT A16WE E2EA 2007040900146 20070409 00146 NM 2007 4 9 KNNA200700023 1 20070301 A 5330 2024T3 SKIN BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE BS 968 S27L CORRODED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 326DL 23098 FUSELAGE, EXTERNAL SURFACE LOWER LOBE, B-STA 968, STR 27 L CORRODED. PROVIDE INSTRUCTIONS ON REPAIR OF FUSELAGE EXTERNA L SURFACE LOWER LOBE BS 968 STR 27 L. BOEING SRM 53-10-3 FIGURE 1 AND 53-30-3 FIGURE 48. 2 L 7 2 4F 4 F RT A16WE E2EA 2007040900147 20070409 00147 NM 2007 4 9 KNNA200700022 1 20070314 A 5315 FLOORBEAM BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE BS 344 CORRODED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 326DL 23098 FLOOR PANEL ATTACH POINT STA 344, LBL 12 IS CORRODED. PROVIDE INSTRUCTIONS ON REPAIR OF STA 344, LBL 12 FLOOR PANEL ATT ACH POINT. REMOVED AND REPLACED FLOORBEAM SRM 53-10-9 FIG 6. 2 L 7 2 4F 4 F RT A16WE E2EA 2007040900148 20070409 00148 CE 2007 4 9 DXTA200702088 1 20070407 A 5610 WINDSHIELD CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE COCKPIT FAILED E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 696QS 5605296 LT WINDSHIELD SHATTERED. RECEIVED LT FAULT, SELECTED OFF, LT O'HEAT WINDSHIELD, ARCED AND SHATTERED, DIVERTED. [SUP 4-19 -07] REPLACED WINDOW IAW MM 56-11-00 2 L 7 2 4F 4 F RT A22CE E00059EN 2007040900149 20070409 00149 NM 2007 4 9 CALA0700156 1 20070329 A 5330 6545775594 SKIN BOEING 737 7373T0 1384582 NM BS 727D CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 77303 23354 INSPECTION FOUND A 1.8 INCH CRACK IN SKIN AT STA 727D+8, S24R. THE SKIN WAS REPAIRED IAW ECRA 5331-01295. 2 L 7 2 4F RT A16WE 2007040900150 20070409 00150 NM 2007 4 9 CALA0700157 1 20070329 A 5240 6545849504 SKIN BOEING 737 7373T0 1384582 NM R-2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 77303 23354 INSPECTION FOUND A 1 INCH CRACK AT LIGHTENING HOLE IN R-2 DOOR INNER SKIN. A REPAIR WAS INSTALLED IAW ECRA 5241-01018. 2 L 7 2 4F RT A16WE 2007040900151 20070409 00151 WP 2007 4 9 UPS07849584 1 20070328 A 5511 FRAME DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 RT HORIZONTAL STAB LEADING EDGE LWR FORMER STA XFS32 CRACKED. STOP DRILLED CRACK, FABRICATED AND INS TALLED REPAIR DOUBLER IAW SRM 5 5-02-00-0, 51-1-20D AND DWG 5644310. 2 L 7 4 4F RT 4A25 2007040900155 20070409 00155 NM 2007 4 9 USAA070260 1 20070404 A 5754 SKIN BOEING 737 7373B7 1384580 NM NR 2 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 526AU 23861 SEVERAL .125 INCH CRACKS, NR 2 SLAT LOWER TRAILING EDGE SKIN BETWEEN HET TUBE & INBOARD AUX TRACK HAS CRACK. CUT OUT DA MAGE & INSTALLED DOUBLER PER SRM 57-43-01, DEFECT SIZE: .125 INCH. 2 L 7 2 4F RT A16WE 2007040900156 20070409 00156 EU 2007 4 9 MALA070057 1 20070403 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 442XJ 340B442 THE SEAT TRACK AT BL0, CENTER AISLE FLOOR FLANGE, IS CORRODED OUT OF LIMITS. THE DAMAGE HAS BEEN REPAIRED IAW MESABA EO NR S53342. REF: EAMS WORK ORDER 215978 TASK 1532. 2 L 7 2 4T RT A52EU 2007040900157 20070409 00157 NM 2007 4 9 USAA070255 1 20070330 A 5330 SKIN BOEING 737 737401 1384701 NM BS 787-807 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 AFT CARGO (SKIN UNDER THRESHOLD) ADJACENT TO EXISTING REP DOUBLER STA 787-807 HAS CORROSION. INSTALLED DOUBLER; PER 52- 00-01 REP 32; CORR TASK C53-202-01, DEFECT SIZE: 20 INCHES. 2 L 7 2 4F RT A16WE 2007040900159 20070409 00159 NM 2007 4 9 USAA070253 1 20070330 A 5414 SKIN BOEING 737 737401 1384701 NM PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 CRACK IN INBOARD PYLON, LOWER AFT CORNER, CUTOUT FOR ACCESS PANEL 5724L. INSTALLED DOUBLER PER TR 54-50-07, DEFECT SIZ E: .375 INCH. 2 L 7 2 4F RT A16WE 2007040900160 20070409 00160 NM 2007 4 9 USAA070252 1 20070330 A 5313 STRINGER BOEING 757 757225 1384959 NM BS 446 S22R CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918UW 22196 STA 446 STR 22R HAS CORROSION. FAB'D & INSTALLED REPAIR PARTS PER SRM 53-00-03, FIG 201, 53-00-03, FIG 101, DEFECT SIZE : .900" L X .700'W X .700"D. 2 L 7 2 4F RT A2NM 2007040900161 20070409 00161 NM 2007 4 9 USAA070251 1 20070330 A 5311 FRAME BOEING 757 757225 1384959 NM BS 900, W138 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918UW 22196 BS 900, WL 138.5 ON FRAME HAS CORROSION. FAB'D REPAIR ANGLES, T-CHORDS, INSTALLED ALL PARTS PER SRM 51-70-12, 51-40-02; DEFECT SIZE: 12"L X 1.70"W X .041"D. 2 L 7 2 4F RT A2NM 2007040900163 20070409 00163 SO 2007 4 9 SIMA200709602 1 20070403 A 5347 14530606015 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 703MR 15867 4800 145173 LEFT WALL SEAT TRACK CORRODED BETWEEN FRAME 36 AND FRAME 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007040900165 20070409 00165 NM 2007 4 9 BB07030 1 20070328 A 2120 213N11005076 DUCT BOEING 757 757225 1384959 NM RT A/C PACK BROKEN A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 923UW 22203 FLIGHT 1842, MCO-CLT: DURING FLIGHT, A BURNING ODOR AND MIST WAS NOTED IN CABIN. FLIGHT WAS GIVEN PRIORITY INTO CLT, WH ERE AN UNEVENTFUL LANDING TOOK PLACE. MAINTENANCE FOUND A FLANGE BROKEN ON THE RIGHT PACK DUCT. REPLACED DUCT. NO FUR THER FAULTS. 2 L 7 2 4F RT A2NM 2007041000004 20070410 00004 NM 2007 4 10 CNMA20070007 1 20070331 A 3350 2013A1 BATTERY PACK BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHTS DISCHARGED A CNMA K NONE L NO TEST IN INSP/MAINT 1 SW 07 369AX 28161 RT FWD EMERGENCY LIGHTS INOP AND LT AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS IAW MM 33-51 OPS CHECK GOO D. REPLACED 2 EACH BATTERY PACKS P/N 2013-A1 S/N 54166 RT FWD S/N 9695 LT AFT. 2 L 7 2 4F 4 F RT A2NM E12EU 2007041000005 20070410 00005 SO 2007 4 10 C2XA07TY018 1 20070405 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO CARGO DOORWAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16951 145063 AIRCRAFT IN FOR C-CHECK. CARGO DOOR CUTOUT LOWER SILL HAS AREAS OF CORROSION. REMOVED AND REPLACED CORRODED SILL IAW E MB 135/145 SRM 51-20-03, 51-40-02. ALODINED, PRIMED AND PAINTED IAW EMB CPM 51-21-04, 05, 06. AIRCRAFT STILL IN C-CK. 2 L 7 2 4T RT T00011AT 2007041000007 20070410 00007 SO 2007 4 10 C2XA07IA079 1 20070404 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 15973 145159 IAH - FLIGHT 2151, DURING PREFLIGHT INSPECTION THE CREW REPORTED A HOT ELECTRICAL ODOR IN THE COCKPIT. MAINTENANCE INSP ECTED THE AIRCRAFT, AND COULD NOT DUPLICATE THE DISCREPANCY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007041000009 20070410 00009 SO 2007 4 10 SIMA200709403 1 20070328 A 5315 14521700007 FLOORBEAM EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 708AE 15810 4800 145205 LEFT OMEGA BEAM AT FRAME 20 CORRODED. REMOVED CORROSION BY CUTOUT, FABRICATED AND INSTALLED NEW REPAIR PARTS IAW EMB SR M 53-00-10. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041000011 20070410 00011 EA 2007 4 10 SIMA200709405 1 20070402 A 2810 TUBE CNDAIR CL600 CL6002C10 1390015 EA FUEL SYSTEM LEAKING A SIMA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 524AE 10154 FUEL LEAK FROM THE NACA TUBE AREA. PERFORMED A VISUAL INSPECTION OF CENTER TANK FOR LEAKS WITH NO LEAKS NOTED IAW CRJ A MM 28-11-00 AND PERFORMED OPERATIONAL TEST OF VENT SYSTEM WITH NO DEFECTS NOTED IAW CRJ AMM 28-12-00. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007041000013 20070410 00013 EU 2007 4 10 NWAA071243239 1 20070405 A 2120 UNKNOWN AIRBUS 320 A320212 3930322 EU CABIN ODOR A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 339NW 367 FLIGHT ATTENDANT ADVISED BURNING PLASTIC ODOR IN CABIN, ODOR DECREASED DURING FLIGHT. WING ANTI ICE WAS ON FROM 3000MSL TO 10000MSL AND LANDING WAS UNEVENTFUL. INSPECTED CABIN, GALLEYS, LAVATORIES AND WHEEL WELLS AND NO SOURCE WAS FOUND. 2 L 7 2 4F RT A28NM 2007041000017 20070410 00017 CE 2007 4 10 DJFA2007043 1 20070405 A 5511 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 749TA RK149 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE RT IB HORIZONTAL STA BILIZER, THE RT RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUÉ' NR 70. MAINTENANCE REPLACED THE RT RIB ASSEMBLY. 2 H 7 2 4F 4 F RT A16SW E25EA 2007041000018 20070410 00018 CE 2007 4 10 DJFA2007044 1 20070405 A 2160 UNKNOWN BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE CABIN TEMP UNKNOWN E DJFA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 23 497CW RK297 TRIP NR 1161433 CREW REPORTED BURNING ODOR FROM CABIN TEMPERATURE RUNAWAY. CREW REGAINED CONTROL OF CABIN TEMP AND RETU RNED TO FIELD. MAINTENANCE TROUBLESHOT THE SYSTEM BUT WAS UNABLE TO DUPLICATE THE DISCREPANCY. THE FAILURE HAS NOT REP EATED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007041000019 20070410 00019 CE 2007 4 10 DJFA2007045 1 20070406 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 787TA 6196 RK260 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE RIGHT INBOARD HORIZO NTAL STABILIZER, THE LT AND RT RIBS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN M FG COMMUNIQUÉ' NR 70. BOTH RIBS WERE REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007041000020 20070410 00020 NM 2007 4 10 07FDEA01307 1 20070403 A 5740 EAL6897481 ATTACH ANGLE BOEING 727 727225 1384077 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 RT WING TE, LOWER PANEL BELOW NR 13 SPOILER PANEL OTBD ATTACH ANGLE OF THE INBD SET IS CRACKED AT SUPPORT ROD. FABRICAT ED REPLACEMENT ANGLE ON SHOP WO NR 11841-6300-0002. HEAT TREATED ON 8130- 3 TRACKING NR 2007-03-142. REPLACED ANGLE AT TACHMENT FOR LOWER PANEL REFERENCE SRM 51-40-3. 2 L 7 3 4F A3WE 2007041000021 20070410 00021 NM 2007 4 10 07FDEA01308 1 20070403 A 5330 6517529143 SKIN BOEING 727 727225 1384077 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FOUND REPAIR AT FUSELAGE STA 1184, LBL 10. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED REPAIR DOUBLER REF SRM 51-30-2. HFEC SKIN IAW 727 NDT MANUAL PART 6, 51 -00-00 FIG 23. FOUND CRACKS AT 2 FASTENER HOLES. REMOVED DAMAGE REF SRM 53-30-3. FABRICATED REPAIR PARTS REF SRM 53-3 0-3. TREATED AND PRIMED REPAIR PARTS REF SRM 51-10-2. INSTALLED AND FILLET SEALED REPAIR REF SRM 53-30-3 PG 12, 155-15 9. THIS IS A CATEGORY C REPAIR REF PAGE 156. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007040500146 20070405 00146 NM 2007 4 5 SWAA071706 1 20070403 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM BS 759 S18R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 759, STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007040500147 20070405 00147 NM 2007 4 5 SWAA071700 1 20070403 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 834 S20L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 834, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007040500148 20070405 00148 NM 2007 4 5 SWAA071701 1 20070403 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 854 S17L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 854, STR 17L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007040500149 20070405 00149 NM 2007 4 5 SWAA071703 1 20070403 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 839 S17L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 839, STR 17L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007040500150 20070405 00150 NM 2007 4 5 SWAA071704 1 20070403 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 757 S19R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007040500151 20070405 00151 NM 2007 4 5 SWAA071715 1 20070403 A 5315 6545833 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 294.5, LBL 53. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007040500152 20070405 00152 NM 2007 4 5 SWAA071687 1 20070402 A 5755 ATTACH FITTING BOEING 737 7375H4 138449D NM NR 4 SPOILER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED A2 CHECK, FOUND LEFT WING NR 4 SPOILER INBOARD LUG BROKEN. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007040500153 20070405 00153 NM 2007 4 5 SWAA071713 1 20070403 A 5753 6546486 WEDGE BOEING 737 7373H4 1384600 NM RT WING TE FLAP DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD MID FLAP T/E WEDGE LOWER SKIN DISBONDED AT OUTBOARD END. REMOVED A ND REPLACED T/E WEDGE PER MM. 2 L 7 2 4F RT A16WE 2007040500154 20070405 00154 EU 2007 4 5 07FDEA01157 1 20070328 A 5415 ATTACH FITTING AIRBUS 310 A310304 3930339 EU ZONE 400 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 CORROSION IN AFT PYLON ATTACH FITTING HOLE , PYLON NR 2, RIB 18 REPAIR PERFORMED WITH SB A31-52-2021, APPROVED BY EA 6-5 450-106340. 2 L 7 2 4F RT A35EU 2007040500155 20070405 00155 EU 2007 4 5 07FDEA01158 1 20070328 A 5415 ATTACH FITTING AIRBUS 310 A310304 3930339 EU ZONE 400 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 FOUND CORROSION IN AFT PYLON ATTACH FITTING HOLE , PYLON NR 2, RIB 18 REPAIR PERFORMED WITH SB A31-52-2021, APPROVED BY EA 6-5450-106340. 2 L 7 2 4F RT A35EU 2007040600002 20070406 00002 2007 4 6 MWEA070074 4 20070403 A 3418 0861EW1 TRANSMITTER BOEING 717 717200 1383700 NM AOA CONTAMINATED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 909ME 55173 STICK SHAKERS WENT OFF AND REMAINED ON UNTIL AIRCRAFT DESCENDED TO 29,000 FEET. REMOVED AND REPLACED TRANSMITTER AOA. 2 L 7 2 4F TR A6WE 2007040600005 20070406 00005 CE 2007 4 6 DJFA2007040 1 20070330 A 5530 BRACKET BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE VERTICAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 789TA RK268 DURING A SCHEDULED INSPECTION, MAINTENANCE DISCOVERED A SMALL CRACK ON THE RIB SUPPORT BRACKET FOR A RIB IN THE VERTICAL STABILIZER. THE CRACK WAS APPROX .25 INCH LONG TRANSECTING A NUTPLATE RIVET. MAINTENANCE IS REPLACING THE BRACKET. M AINTENANCE FABRICATED A NEW BRACKET AND INSTALLED IT. 2 H 7 2 4F 4 F RT A16SW E25EA 2007040600006 20070406 00006 SO 2007 4 6 DJFA2007042 1 20070331 A 2120 UNKNOWN EMB 135 EMB135BJ 3260306 SO ALLSN AE300 AE3007A GL CABIN ODOR E DJFA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 902LX 145495 TRIP NR 1162348 CREW REPORTED BURNING ODOR IN THE CABIN. THE ODOR EVENTUALLY REACHED THE COCKPIT. SEVERAL PASSENGERS A ND THE COPILOT ALSO REPORTED HEADACHES. THE AIRCRAFT WAS DIVERTED TO MBPV. ON DESCENT THE ACM WAS SWITCHED TO THE APU AND THE ODOR WENT AWAY. MAINTENANCE PLACED THE ACM ON MEL. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY. AIRCRAFT WAS RELEASED WITH NO FURTHER EVENTS. 2 L 7 2 4F 4 F RT TE6CH 2007040600013 20070406 00013 NM 2007 4 6 07FDEA01194 1 20070330 A 5754 PANEL BOEING 727 727225 1384077 NM NR 1 KRUEGER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 LEFT WING LWR SURFACE L/E PNL DELAMINATING AFT OF NR 1 KRUEGER FLAP. REMOVED DAMAGE AND BONDED REPAIR PLIES PER SRM 51- 40-9. PAINTED PER MM 51-20-151-7. 2 L 7 3 4F A3WE 2007040600016 20070406 00016 WP 2007 4 6 07FDEA01197 1 20070330 A 5730 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 571FE 71749 47830 COMPLIED WITH EA NR 8-5710-102030 WING LT WING UPPER SKIN CRACKED AT XORS 585 ADJACENT TO STR 7. ACCOMPLISH PART 2 AT S UBSEQUENT C CHECKS CONCURRENT WITH MAINTENANCE WORK CARD 57SI5503-02 MAJOR REPAIR. COMPLIED WITH EA NR 8-5710-102030 WI NG LT WING UPPER SKIN CRACKED AT XORS 585 ADJACENT TO STR 7. ACCOMPLISH PART 2 AT SUBSEQUENT C CHECKS CONCURRENT WITH MAINTENANCE WORK CARD 57SI5503-02. 2 L 7 3 4F RT A22WE 2007040600020 20070406 00020 NM 2007 4 6 SWAA071683 1 20070402 A 5330 6547955 SKIN BOEING 737 7373H4 1384600 NM BS 789 S25R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT BS 789, STR 25R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007040600028 20070406 00028 NM 2007 4 6 SWAA071722 1 20070403 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500D S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007040600044 20070406 00044 2007 4 6 SWAA071707 4 20070403 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007040600056 20070406 00056 NM 2007 4 6 UPS07M49574 1 20070130 A 5330 AGA7808 DOUBLER DOUG MD11 MD11F 3023600 NM BS 1721-1741 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C CTR CARGO STA 1721-1741 STR 51R TO 52R BILGE AREA DOUBLER FOUND WITH CORROSION AS MARKED. CTR CARGO D RUM MUST REMOVED PER AMM20-50-02 R55. CORROSION REMOVED PER SRM 51-31-01 V2 R38. CORROSION REMOVED FOUND EXCEED LIMIT PER SRM 51-21-01 V2 R38. STA 1701 TO STA 1741 LONGERON 48L TO 48R SKIN FASTENERS REMOVED PER SRM 51-31-01 V2 R38. NEW DOUBLER FASTENER HOLES PICKED UP PER DWG AGA7808 & INSTALLATION CUT OUT WITH NEW DOUBLER FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007040600062 20070406 00062 NM 2007 4 6 07FDEA01201 1 20070330 A 5410 6519686768 COWLING BOEING 727 727225 1384077 NM ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 NR 3 ENGINE FIXED COWL AFT UPPER LATCH CUTOUT IS CRACKED AT AFT END NEW COWL ASSY RECEIVED AND REPLACED REF MM 71-10-031 -4 AND REF WC 74C300-01. 2 L 7 3 4F A3WE 2007040600067 20070406 00067 NE 2007 4 6 6017803312007 2 20070331 A 7230 BLADE LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE COMPRESSOR SEPARATED E J7SA A UNSCHED LANDING E Y J VIBRATION/BUFFET ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SW 05 244FX 178 CA0194 LOUD BANG ON LT ENGINE AT FL 410 FOLLOWED BY MAJOR VIBRATION, SHUT ENGINE DOWN IN FLIGHT. PRELIMINARY INVESTIGATION: 1S T STAGE COMPRESSOR BLADE LET LOOSE. BOUNCED AROUND INSIDE CONTAINMENT RING BUT MADE ITS WAY FORWARD WHERE IT PENETRATED THROUGH THE INLET. THIS CAUSED THE OUTER COWLINGS TO BECOME PRESSURIZED WHICH POPPED THE LATCHES AND THE COWLINGS DEPART ED THE AIRCRAFT, AND MADE SLIGHT CONTACT WITH THE HORIZONTAL STABILIZER. 2 L 7 2 4F 4 F RT A10CE E35NE 2007041600113 20070416 00113 WP 2007 4 16 DXTA200702072 2 20070403 A 7200 ENGINE CESSNA 650 650 2076802 CE GARRTT TFE731 TFE7314R 01518 WP LEFT MALFUNCTIONED E DXTA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 07 713QS 6507103 P102287 LEFT ENG ROLLED BACK TO 91% N1 ON T/O ROLL (APROX 80 KNOTS). T/O ABORTED. INSP EEC FOR FAULTS NONE NOTED. RAN A/C AT ALL POWER SETTINGS IN AUTO & MANUAL MODES. NO ROLL BACK NOTED SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME ALL WORK DONE IA W CE 650 M/M 76-10-04 & HONEYWELL TFE731 M/M 76-00-00 2 L 7 2 4F 4 F A9NM E6WE 2007040600076 20070406 00076 NM 2007 4 6 MWEA070071 1 20070331 A 7830 DOOR BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 913ME 55176 CRACK DISCOVERED ON THE LEFT LOWER THRUST REVERSER BUCKET DOOR, APPROXIMATELY .25 INCH LONG ON THE ZEE FRAME AT STATION 26.666. FABRICATED AND INSTALLED REPAIRED SECTION. 2 L 7 2 4F TR A6WE 2007040600078 20070406 00078 NM 2007 4 6 MWEA070069 1 20070330 A 3520 5D03411 RELAY BOEING 717 717200 1383700 NM OXYGEN SYSTEM INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 920ME 55182 SERVICE UNIT DOOR AT ROW 8 RIGHT SIDE DID NOT OPEN AT SIMULATED 14,500 FEET. REMOVED AND REPLACED RELAY. 2 L 7 2 4F TR A6WE 2007040600095 20070406 00095 WP 2007 4 6 AALA20070556 1 20070325 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 246AA 49258 LGA - OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS IN FIRS T CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007040600104 20070406 00104 WP 2007 4 6 NWAA071229752 1 20070401 A 2916 59240355501 RESERVOIR DOUG DC9 DC941 302207N WP HYD SYSTEM LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 752NW 34092 34092 47116 THE RIGHT HYDRAULIC SYSTEM HAD DROPPED TO ABOUT TWO QUARTS WHILE IN CRUISE FLIGHT. AS THE AIRCRAFT WAS ON APPROACH FOR LANDING AND THE LANDING GEAR WAS EXTENDED THE RIGHT SYSTEM WENT TO ZERO. THE LANDING GEAR DID LOCK DOWN AND ALL SAFE IN DICATIONS ILLUMINATED. COM PROCEDURES WERE COMPLIED WITH AND THE LANDING WAS UNEVENTFUL. MAINTENANCE FOUND THE RESERVO IR RELIEF VALVE STUCK IN THE OPEN POSITION. THE RESERVOIR WAS REPLACED ALONG WITH THE AUX PUMP, ENGINE DRIVEN PUMP AND SYSTEM FILTERS. AFTER A SATISFACTORY LEAK CHECK THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007040600108 20070406 00108 NM 2007 4 6 NWAA071216313 1 20070402 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 673US 30268 DURING OVERNIGHT LINE CHECK, MAINTENANCE FOUND RIGHT OVERWING EXTERIOR EMERGENCY EXIT LIGHT THIRD ONE AFT INOP. MAINTEN ANCE REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007040600109 20070406 00109 NM 2007 4 6 NWAA071236301 1 20070404 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23719 DURING OVERNIGHT LINE CHECK, MAINTENANCE FOUND RIGHT OVERWING EXTERIOR EMERGENCY EXIT LIGHTS 3 AND 4 AFT INOP. MAINTENA NCE REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007040600122 20070406 00122 EU 2007 4 6 AWXA200700463 1 20070404 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHTS FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 627AW 27314 11405 66 PHX - EEL - MX REPORTED EMERGENCY LIGHTS ROW 13, 17, 19 INOP. MX REPLACED THE AFT POWER SUPPLY AND BATTERY. OPERATIONA L CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007040600123 20070406 00123 EA 2007 4 6 VNAA0703021 1 20070329 A 5240 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE OPEN A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 05 709PS 10165 CREW REPORTED AN EXTERNAL POWER DOOR OPEN ON CLIMBOUT. CREW ELECTED TO RETURN TO MSY AND LAND WITHOUT INCIDENT. MAINTE NANCE INSPECTED AND FOUND THE EXTERNAL POWER DOOR OPEN. MAINTENANCE CLOSED DOOR AND PERFORMED OPERATIONAL CHECKS IN ACC ORDANCE WITH AMM 53-10-00-210-807-A01. NO DAMAGE NOTED AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007040600133 20070406 00133 EA 2007 4 6 VNAA0703019 1 20070325 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE COCKPIT ODOR A VNAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 05 706PS 10150 CREW REPORTED SMELLING SMOKE IN COCKPIT AND CABIN AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDE NT. ODOR DISSIPATED AFTER LANDING. MAINTENANCE INSPECTED AND PERFORMED A GENERAL VISUAL INSPECTION OF THE FLIGHT DECK, CABIN AND AVIONICS COMPARTMENT. NO DEFECTS NOTED AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007040600135 20070406 00135 NM 2007 4 6 07FDEA01174 1 20070328 A 5320 6557990 BRACKET BOEING 727 727225 1384077 NM RT MLG WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 RT MLG WW BULB SEAL SUPPORT BRACKET ON KEEL BEAM IS CRACKED 10 INCHES FORWARD OF SAFETY BAR. REMOVED DAMAGED BRACKET AND FABRICATED NEW BRACKET. HEAT TREATED REF BOEING DWG 65-57990. TREATED, PRIMED AND INSTALLED NEW BRACKET REF SRM 51 -40-2. INSTALLED NUT PLATE REF SRM 51-30-2. 2 L 7 3 4F A3WE 2007040600136 20070406 00136 WP 2007 4 6 MWEA070070 1 20070402 A 5310 WINDOW FRAME DOUG DC9 DC981 3022081 WP COCKPIT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 805ME 48031 CENTER WINDSHIELD LOWER FRAME HAS LIGHT CORROSION. FABRICATED AND INSTALLED ZEE. 2 L 7 2 4F A6WE 2007040600146 20070406 00146 NM 2007 4 6 MWEA070050 1 20070325 A 7830 7150922505 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 921ME 55183 RIGHT THRUST REVERSER, TOP DEFLECTOR DOOR FRAME AT STATION 35.669 HAS A CRACK. FABRICATED AND INSTALLED THRUST REVERSER . 2 L 7 2 4F TR A6WE 2007040600149 20070406 00149 WP 2007 4 6 MWEA070077 1 20070404 A 5330 59364341 SKIN DOUG DC9 DC982 3022082 WP BS 541 S26-27 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 810ME 48072 EVIDENCE OF SKIN DENTED AT STATION 541 BETWEEN LONGERERON 26 AND LONGERON 27. FABRICATED AND INSTALLED FILLER. 2 L 7 2 4F A6WE 2007040900006 20070409 00006 EU 2007 4 9 07FDEA01269 1 20070403 A 5320 R53700089200 SUPPORT AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 HEAVY CORROSION ON Y-Z LATCH SUPPORT AT C25A RT. REPAIR PERFORMED IAW SRM 53-13-13/FIG 203 (PN: R537-00089-200-EF). 2 L 7 2 4F RT A35EU 2007040900009 20070409 00009 EU 2007 4 9 07FDEA01082 1 20070322 A 5730 SKIN AIRBUS 310 A310324 3930206 EU ZONE 500 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 ELONGATED HYDRAULIC FITTING HOLES IN THE LOWER SKIN PANELS OF LT WING. REPAIR PERFORMED BY OVERSIZING AND BUSHING HOLES IAW EA 6-5720-99228, APPROVED BY RAS/BAE/1002610/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040900014 20070409 00014 NM 2007 4 9 DL76G070282 1 20070331 A 2822 PUMP BOEING 767 767332 1382001 NM FUEL SYSTEM INOPERATIVE A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 177DZ 29698 LEFT CENTER FUEL PUMP INOP. PRESSURE LIGHT ON. LEFT CENTER FUEL PUMP VERIFIED TO BE OPERATING NORMAL LOW PX LIGHT INOP FWD TO MCO PLACARD PER MEL 28-42-01C. 2 L 7 2 4F RT A1NM 2007040900017 20070409 00017 NM 2007 4 9 DL76G070291 1 20070403 A 2530 828450407M0DA OVEN BOEING 767 7673P6 1385105 NM MID GALLEY ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1501P 24983 GALLEY MID CABIN CENTER OVEN WON`T HEAT PROPERLY GIVES OFF ELECTRICAL ODOR WHEN HEATING. CLEANED CHECKED OPS NORMAL. 2 L 7 2 4F RT A1NM 2007040900019 20070409 00019 NM 2007 4 9 ZZDA070329145 1 20070329 A 2170 COALESCER BAG BOEING 737 737 UTILSYS NM CABIN AIR ODOR A ZZDA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 15 309AT 33929 DURING CLIMBOUT F/A'S AND SEVERAL PAX REPORTED A SMOKE AND OIL TYPE ODOR INSIDE THE CABIN. REPLACED LEFT AND RIGHT COAL ESCER BAGS PER M/M 21-51, LEAK CHECK GOOD. 2 L 7 2 4F RT A16WE 2007040900024 20070409 00024 NM 2007 4 9 07FDEA01212 1 20070331 A 5710 DUCT DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT WING TOPSIDE FIXED LEADING EDGE AT TELESCOPING DUCT CUTOUT FOUND 2 SKIN CRACKS AT AFT CORNERS. [SUP 4-19-07] CRAC KS AT LT WING TOPSIDE FIXED LEADING EDGE AT TELESCOPIC DUCT CUTOUT CORNERS REPAIRED AS PER SRM 57-10-00 FIGURE 42 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040900025 20070409 00025 NM 2007 4 9 07FDEA01213 1 20070331 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 NOSE LANDING GEAR LEFT TRUNNION FITTING FOUND CRACKED. REPAIRED AS PER SRM 53-40- 00 FIGURE 22 VOLUME I AND FEDEX EA 1-5310-107816, REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100. 2 L 7 3 4F RT A22WE 2007040900026 20070409 00026 NM 2007 4 9 07FDEA01214 1 20070331 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 NOSE LANDING GEAR RIGHT TRUNNION FITTING FOUND CRACKED. [SUP 4-18-07] REPAIRED AS PER SRM 53-40-00 FIGURE 22 VOLUME I A ND FEDEX EA 1-5310-107815, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040900030 20070409 00030 NM 2007 4 9 07FDEA01298 1 20070403 A 5320 656725110 ANGLE BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 LOWER AFT PIR FWD BULKHEAD STA 950A, RBL 22, L ANGLE AT BASE OF WALL SUPPORTS HAVE CORROSION ON UPPER SURFACE (2 EACH) D AMAGE TO 2 L ANGLES OUT OF LIMITS. ORIGINAL MATERIAL WAS .050", REMAINING MATERIAL .035". FABRICATED 2 REPAIR ANGLES, HEAT TREATED TO T4 ON SHOP WO NR 11841-1600-0001, AND INSTALLED. 2 L 7 3 4F A3WE 2007040900031 20070409 00031 NM 2007 4 9 07FDEA01248 1 20070402 A 5730 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LT WING I/B FLAP LOWER SEGMENT UPPER SKIN FOUND PUNCTURED. LT WING I/B FLAP LOWER SEGMENT REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG 35, VOL I AND FEDEX EA 1-5750-106610, WINGS TRAILING EDGE AND TRAILING EDGE DEVICES, LT INBD FLAP UPPER SKIN REPAIR. CLASSIFIED AS A MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007040900051 20070409 00051 WP 2007 4 9 07FDEA01256 1 20070403 A 5344 HINGE DOUG DC10 DC1010 3022110 WP CARGO DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 LOWER FWD CARGO DOOR DAMAGE FOUND ON DOOR HINGE FWD HINGE LOBE AND AFT HINGE LOBE OVALIZED AND OUT OF LIMIT (DIA. 0.355" ). REPAIRED WITH BUSHING IAW SRM 52-10-00 FIG 8 VOL 1 AND CMM 52-31-03. 2 L 7 3 4F A22WE 2007040900052 20070409 00052 EU 2007 4 9 07FDEA01257 1 20070403 A 5730 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 DEVIATIONS AND CORROSION ON THE TOP SKIN PANEL OF THE CENTER WING BOX, LT/RT, FROM C42 TO C47. REPAIRS PERFORMED IAW SR M 57-10-12 FIG 101 SH 3 AND SRM 51-40-21, COVERED BY EA 6-5710-99220 AND RAS 044669/016/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007040900053 20070409 00053 WP 2007 4 9 07FDEA01258 1 20070403 A 5730 SKIN DOUG DC10 DC1010 3022110 WP RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 RT WING L/E AT SLAT TRACK HOLE NR 1 FOUND SKIN EDGE CORRODED AND DISBONDED. REPAIRED SKIN IAW SRM 57-10-00 FIGURE 68 VO L.1 SHT 1-3. 2 L 7 3 4F A22WE 2007040900057 20070409 00057 WP 2007 4 9 07FDEA01263 1 20070403 A 5753 SKIN DOUG DC10 DC1010 3022110 WP TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 LT WING INB'D FLAP DENTS ON LOWER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIGURE 4 VOL.1. 2 L 7 3 4F A22WE 2007040900066 20070409 00066 EU 2007 4 9 UPS07149560 1 20070327 A 3350 SWITCH AIRBUS A300 A300F4622R 3930360 EU EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 129UP 0813 INSPECTION TYPE:N/A WHEN MOVING EMERGENCY EXIT LIGHT SWITCH TO DISARM ON SHUTDOWN DID NOT GET YELLOW CAUTION DISARM LIGH T. LIGHT DOES TEST. CYCLED A/C POWER. PERFORMED OPS CHECK PER AMM 33-51-00-05, CHECKS GOOD. 2 L 7 2 4F RT A35EU 2007040900069 20070409 00069 NM 2007 4 9 UPS07549562 1 20070309 A 5311 146102886 FRAME BOEING 757 75724APF 1384969 NM BS . 1340 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 441UP 27386 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1340, S26L. ACCOMPLISHED REPAIR PER FINAL EA 757-5362-27-A1621 A ND UPS EO B757-5310-26418-A. 2 L 7 2 4F RT A2NM 2007040900072 20070409 00072 NM 2007 4 9 UPS07549565 1 20070309 A 5311 143N102494 FRAME BOEING 757 75724APF 1384969 NM BS 640 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 441UP 27386 INSPECTION TYPE:C DENT IN FWD CARGO FUSELAGE FRAME STA 640, S24R. REPAIR COMPLETED PER EA 757-5332-27-A1625. 2 L 7 2 4F RT A2NM 2007040900089 20070409 00089 NM 2007 4 9 DXTA200702086 1 20070405 A 2612 FIRE WARNING GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE APU BAY UNKNOWN E DXTA F A ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 729QS 118 AT FL-380 APU FIRE WARNING ILLUMINATED, RAN QRH CHECKLIST FIRED APU FIRE BOTTLE INDICATION DID NOT GO OUT. LANDED AT NEA REST AIRPORT. REPLACED APU FIRE DETECTOR P/N 3001-148-450-9, S/N 86516 WITH INSPECTED DETECTOR P/N 3001-148; S/N 87592 IAW G200 AMM SECTION 26-10-15. REMOVED RH FIRE BOTTLE P/N 473779-3; S/N 02738C AND INSTALLED ENW BOTTLE P/N 473779-3; S/ N 0377BC WITH NEW SQUIBS P/NS 446582-1; S/N 060600213; 446582-2; S/N 050600304; 446582-3, S/N 070600323 AND 2 FUSES P/N 27F650 IAW G200 AMM SECTIONS 26-10-15 AND 26-20-10, 26-20-05. OPS CHECK OK 2 L 7 2 4F 4 F RT A53NM E35NE 2007040900091 20070409 00091 NM 2007 4 9 CALA0700167 1 20070405 A 5315 6546568 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT STA 1016, RBL 9. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 2007040900102 20070409 00102 WP 2007 4 9 UPS07849594 1 20070405 A 5230 SKIN DOUG DC8 DC873F 302199F WP CARGO DOOR DENTED A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 809UP 46109 CARGO DOOR DENT OUT OF SRM LIMITS. ACCOMPLISHED INTERIM REPAIR ACTIONS AS PER EO DC8-5230-26519. ACCOMPLISHED HFEC PER DC-8 NDTM 51-00-019. NO CRACKS FOUND. OK FOR CONTINUED SERVICE. 2 L 7 4 4F RT 4A25 2007040900108 20070409 00108 CE 2007 4 9 GUUA04040701 1 20070404 A 3260 H111541 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG SHORTED A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 29 87550 UE205 AFTER TAKEOFF LANDING GEAR RETRACTION LANDING GEAR HANDLE LIGHTS REMAIN ILLUMINATED. RETURNED TO TPA LANDED WIITHOUT INC IDENT. REPLACED LT AND RT MAIN LANDING GEAR UPLOCK SWITCHES. 2 L 7 2 4T 4 T RT A24CE E26NE 2007040900131 20070409 00131 CE 2007 4 9 DXTA200702093 1 20070408 A 3260 DOWNLOCK SWITCH CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LT MLG INOPERATIVE E DXTA A UNSCHED LANDING S J AFFECT SYSTEMS WARNING INDICATION CL CLIMB 1 GL 07 970QS 7500070 AFTER TAKEOFF, LT MAIN GEAR WILL NOT RETRACT. [SUP 4-19-07] REMOVED AND REPLACED LEFT DOWN/LOCK SWITCH IAW CE 750 MM C HAP 32-30-04 OPS CHECKS GOOD C/W GEAR SWINGS. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007040900137 20070409 00137 NM 2007 4 9 CALA0700158 1 20070401 A 5330 6565775594 SKIN BOEING 737 7373T0 1384582 NM BS 727E-727D CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A 1.75 INCH CRACK IN FUSELAGE SKIN AT STA 727E-727D, S23R (AT WING AFT EMERGENCY LIGHT). DOUBLERS WERE INSTALLED IAW ECRA 5330-03659, REV A. 2 L 7 2 4F RT A16WE 2007040900138 20070409 00138 NM 2007 4 9 CALA0700159 1 20070401 A 5330 6545774575 SKIN BOEING 737 7373T0 1384582 NM BS 727D-727E CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT STA 727D-727E, S23L (AT LEFT AFT EMERGENCY LIGHT). REPAIRED IAW ECR A 5330-03658. 2 L 7 2 4F RT A16WE 2007040900152 20070409 00152 WP 2007 4 9 ABXA070089 1 20070404 A 3260 DOWNLOCK SWITCH DOUG DC9 DC931 3022065 WP MLG MALFUNCTIONED A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 947AX 47004 ON 1ST GEAR EXTENSION, GOT GEAR ABNORMAL INDICATION. NO RIGHT MAIN GEAR GREEN LIGHT (ALSO NO UNSAFE LIGHT). ON 2ND GEA R EXTENSION, ALL GEAR INDICATION WAS NORMAL. REPLACED RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH (INTERMITTENT) IAW DC9 MM 32-60-01-2-0101. 2 L 7 2 4F A6WE 2007040900154 20070409 00154 EU 2007 4 9 USAA070261 1 20070404 A 5315 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 174US 1492 AROUND SCREW HOLE, FRAME 66, RIGHT SIDE Y -1292 HAS CORROSION. CUT OUT DAMAGE, INSTALLED REPAIR ANGLES & FILLER PER SRM 53-41-14; CORR TASK JA-260-53500, LEVEL 1, DEFECT SIZE: .75 INCH DIA. 2 L 7 2 4F RT A28NM 2007041000002 20070410 00002 NE 2007 4 10 NACA20070013 2 20070403 A 8530 404482 CYLINDER HEAD DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 9 CRACKED A NACA E F D ENGINE SHUTDOWN ACTIVATE FIRE EXT. RETURN TO BLOCK A FLAME/FIRE TX TAXI/GRND HDL 1 AL 03 99330 1838 55 43576 P34218 NR 2 ENGINE FIRE ON TAXI. ENGINE SHUT DOWN LT BANK CO2 BOTTLES DISCHARGED. CREW ALSO DISCHARGED MAIN CABIN ABC, COCKPI T AND CABIN HALON BOTTLES TO EXTINGUISH FIRE. NR 2 ENGINE REPLACED AND SENT TO SHOP FOR INSPECTION: FIRE RESULTED FROM THE NR 9 CYLINDER CRACKED HEAD. FURTHER INSPECTION SHOWED MINOR DAMAGE TO INTAKE SCOOP. 2 L 7 4 4R 4 R 6A3 5E8 2007041000003 20070410 00003 NM 2007 4 10 CNMA20070005 1 20070225 A 3350 20131A BATTERY PACK BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHTS INOPERATIVE A CNMA K NONE L NO TEST IN INSP/MAINT 1 SW 07 369AX 28161 EMERGENCY PATHLIGHTS OUT ROW 7 THRU 24 (LT SIDE). REPLACED BATTERY PACK (M733) IAW MM 33-51-07 SYSTEM TEST AND OPS CHEC K GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2007041000008 20070410 00008 SO 2007 4 10 SIMA200709401 1 20070402 A 2840 367934002 FCU EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL ZONE 100 FAILED A SIMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 705AE 11934 5456 145184 NR 1 FUEL QUANITY WENT ZERO ON EICAS, DIVERTED TO RIC. REMOVED AND REPLACED FUEL CONDITIONING UNIT IAW EMB AMM. OPERAT IONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007041000023 20070410 00023 EU 2007 4 10 07FDEA01310 1 20070404 A 5311 FRAME AIRBUS 310 A310304 3930339 EU FUSELAGE CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 DEVIATION TO EO 6-5310-7-5020, SB A310-53-2124, AD 2006-02-06, CRACKS IN FRAME FEET , C45, C46 LT REPAIR PERFORMED BY CR ACK REMOVING THRU OVERSIZING IAW EA 6-5315-106424 AND RAS 049395/047/2007 ISS A. 2 L 7 2 4F RT A35EU 2007041000024 20070410 00024 EU 2007 4 10 07FDEA01311 1 20070404 A 5311 FRAME AIRBUS 310 A310304 3930339 EU ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 DEVIATION TO EO 6-5310-7-5020-SB A310-53-2124- AD 2006-020-06, CRACKS IN FRAME FEET C43, C46 RT REPAIR PERFORMED BY REMO VING THE CRACKS THRU OVERSIZING IAW EA 6-5315-106424 AND RAS 049395/047/2007 ISS. A 2 L 7 2 4F RT A35EU 2007041000030 20070410 00030 EA 2007 4 10 CHQA200700009 1 20070405 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 647BR 7399 FLIGHT 3274 - PBI-IAH - RECEIVED FLAP FAIL EICAS MESSAGE DURING CLIMB-OUT. FLAPS FAILED IN 0 DEGREE POSITION. RAN QRH. NO DIVERSION REQUIRED. DECLARED EMERGENCY AND LANDED IN IAH UNEVENTFULLY. MAINTENANCE COMPLIED WITH AD 2006-12-21 MA INTENANCE PROCEDURES. SYSTEM RESET AND OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007041000033 20070410 00033 SO 2007 4 10 SIMA200709613 1 20070403 A 5347 14530658007 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 703MR 15867 145173 RIGHT INBOARD SEAT TRACK CORRODED BETWEEN FRAME 47 AND 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETUR NED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041000034 20070410 00034 SO 2007 4 10 SIMA200709615 1 20070403 A 5347 13500412005 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 703MR 15867 4800 145173 LEFT WALL SEAT TRACK CORRODED BETWEEN FRAME 53 AND FRAME 55. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RET URNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041000039 20070410 00039 2007 4 10 TRAX200700451 4 20070402 A 2562 ELT CNDAIR CL600 CL6002B19 1900309 EA CABIN NO TEST A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 842AS 7304 ELT DOES NOT TEST. 2 L 7 2 4F RT A21EA 2007041000041 20070410 00041 EA 2007 4 10 TRAX200700453 1 20070402 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 830AS 7236 LT FS 484 INTERCOSTAL HAS CRACK IN CLIP AT LBL 27 IB. REMOVED CRACKED CLIP FROM LT 484 INTERCOSTAL IAW CRJ 200 SRM 51-4 2-20. DUPLICATE CLIP FROM SALVAGE REWORK ANGLE P/N S6144-3 IAW CRJ 200 SRM 53-41-43. 2 L 7 2 4F RT A21EA 2007041000042 20070410 00042 EA 2007 4 10 TRAX200700454 1 20070402 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 830AS 7236 FLOOR SUPPORT STRUCTURE BENEATH SERVICE DOOR THRESHOLD HAS MINOR SURFACE CORROSION. CORROSION FOUND TO BE LIMITED TO SU RFACE ONLY AND NO PITTING WAS FOUND. TREATED MINOR CORROSION PER CRJ SRM 51-21-06 AND APPLIED FINISH A023 PER CRJ SRM 51 -21-16. 2 L 7 2 4F RT A21EA 2007041000043 20070410 00043 EA 2007 4 10 TRAX200700455 1 20070402 A 3220 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA NLG UNKNOWN A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 905EV 7632 NOSE GEAR DISAGREE W/N RETRACT AFTER T/O. A/C RETURNED TO ATL AFTER T/O. TOWER DECLARED EMERGENCY. 2 L 7 2 4F RT A21EA 2007041000047 20070410 00047 EA 2007 4 10 TRAX200700459 1 20070404 A 5310 BEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 741EV 10155 THE 280 BEAM CORRODED LBL 9-14. REMOVED AND REPLACED 280 CROSSBEAM IAW IS67053110026 AND REO 670-53-11-047. 2 L 7 2 4F RT A21EA 2007041000048 20070410 00048 EA 2007 4 10 TRAX200700460 1 20070404 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 741EV 10155 COCKPIT FLOOR LAND, AFT SIDE BADLY CORRODED. ALL WORK BEING COMPLIED WITH ON TASK CARD N/R-00099 IAW EO 670-53-11-047. 2 L 7 2 4F RT A21EA 2007041000049 20070410 00049 EA 2007 4 10 TRAX200700461 1 20070404 A 5310 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 LEFT FS 280 CROSSBEAM HAS CORROSION ON UPPER FLANGE. STARTED REMOVING FASTENERS FROM LT 280 BEAM IAW CRJ 700 SRM 51-42- 21 AND 51-42-06. CONTINUED TO REMOVED FASTENERS FROM 280 CROSSBEAM IAW CRJ 700 SRM 51-42-21 AND 51-42-06. FINISHED REMOV ING FS 280 2 L 7 2 4F RT A21EA 2007041000052 20070410 00052 EA 2007 4 10 TRAX200700463 1 20070404 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 FS 280 FWD CENTER FLOOR SUPPORT ANGLE CORRODED. REMOVED 280 CENTER FLOOR SUPPORT ANGLE IAW CRJ 700, 51-42-06 AND 51-42- 21. OK TO INSTALL SERVICE ANGLE. 2 L 7 2 4F RT A21EA 2007041000053 20070410 00053 EA 2007 4 10 TRAX200700470 1 20070405 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 878AS 7590 FWD RIGHT AND LEFT OVERWING EMERGENCY LIGHTS WILL NOT WORK. 2 L 7 2 4F RT A21EA 2007041000054 20070410 00054 SO 2007 4 10 C2XA07TY017 1 20070402 A 5330 SKIN PANEL EMB 145 EMB145LR 3260212 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18556 145595 TYS - MAINTENANCE FOUND A CRACK IN THE FUSELAGE AT FR 77, FR 78 AND FR 79 AT STRINGER 6L. MAINTENANCE REMOVED THE DAMAG ED SKIN, FAB A DOUBLER, ALODINED AND REINSTALLED. ALL WORK WAS ACCOMPLISHED IAW EC5330-01680. AIRCRAFT RELEASED BACK T O SERVICE. 2 L 7 2 4T RT T00011AT 2007041000055 20070410 00055 EA 2007 4 10 TRAX200700464 1 20070404 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 RIGHT LOWER FS 280 WEB HAS CORROSION. REMOVED RT FS280 WEB IAW CRJ 700 51-42-06 AND 51-42-21. DUPLICATED R/H LWR 280 WEB . 2 L 7 2 4F RT A21EA 2007041000056 20070410 00056 EA 2007 4 10 TRAX200700465 1 20070404 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 LEFT 280 LWR WEB HAS MINOR CORROSION. 2 L 7 2 4F RT A21EA 2007041000057 20070410 00057 EA 2007 4 10 TRAX200700466 1 20070404 A 3250 TORQUE LINK CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING DISCONNECTED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 846AS 7328 ON TAKEOFF NLG W/N RETRACT RECEIVED GEAR DISAGREE, WOW INPUT, WOW OUTPUT GEAR DOOR OPEN. FOLLOWED QRH UPON LANDING HAD NO NOSE WHEEL STEERING. FOUND TORQUE LINK DISCONNECTED. A/C RETURNED TO AVP AFTER T/O. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007041000058 20070410 00058 EA 2007 4 10 TRAX200700467 1 20070404 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 923EV 7826 PAX DOOR HARD TO OPEN. ONCE OPENED, IT CLOSED ITSELF, NO HELP FROM ANYONE. TO OPEN IT AGAIN, PRESSED DOOR ASSIST BUTT ON ONCE. 2 L 7 2 4F RT A21EA 2007041000059 20070410 00059 EA 2007 4 10 TRAX200700468 1 20070405 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 CAPTAIN`S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007041000061 20070410 00061 WP 2007 4 10 ABXA070086 1 20070327 A 5240 46560541 ACCESS PANEL DOUG DC8 DC861 3021952 WP MISSING A ABXA O OTHER O OTHER NR NOT REPORTED 1 GL 23 847AX 46031 ON POST FLIGHT FOUND FIRE BOTTLE ACCESS PNL ON PRESS GAGES MISSING. (CENTER INBOARD DOOR ASSEMBLY). INSTALLED TEMPORAR Y COVER PER REA D857-55548, DEFERRED PER REA D857-55548 FOR MAINT TRACKING IAW ABX GMM 01.07.04 TO BE REPLACED ON OR BEF ORE MARCH 30, 2007. INSTALLED NEW DOOR PART 4656054-1 AS REQUIRED. 2 L 7 4 4F 4A25 2007041000063 20070410 00063 SO 2007 4 10 C2XA07RI009 1 20070322 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO LAVATORY DEFECTIVE A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 12172 1454 1454 14500864 FLT 2761 - RIC TO EWR - DURING CLIMB, CREW HAD WARNING OF LAV SMOKE. EWR MX REMOVED AND REPLACED LAV SMOKE SENSOR AND P ERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007041000067 20070410 00067 NM 2007 4 10 SB07025 1 20070329 A 2131 7638101 CONTROLLER BOEING 737 737301 1384611 NM CABIN PRESSURE FAULTY A USAA O OTHER J WARNING INDICATION DE DESCENT 1 EA 19 502UW 56853 56853 23232 DFW FLT 1105 - EN ROUTE FROM CLT TO DFW, AT FL240, CREW REPORTED A LOSS OF PRESSURIZATION AS CABIN ALTITUDE WARNING HORN SOUNDED AND CABIN CLIMBED TO 10,000 FEET. CREW MANUALLY SWITCHED TO STANDBY PRESSURIZATION AND DESCENDED TO 10,000 FEE T. AFTER FLIGHT LEVELED OFF, ALL APPEARED TO RETURN TO NORMAL. AT 4,000 FEET, FLIGHT LOST PRESSURIZATION AGAIN. FLIGH T LANDED WITHOUT PRESSURIZATION OR FURTHER INCIDENT AT DFW. NO EMERGENCY WAS DECLARED AND NO OXYGEN MASKS WERE DEPLOYED . MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER PER MM 21-31-21-4. OPERATIONAL CHECKED GOOD PER MM 21 -31-00-2-702-001. 2 L 7 2 4F RT A16WE 2007041000070 20070410 00070 NM 2007 4 10 DL76L070270 1 20070327 A 7830 THRUST REVERSER BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE FAULTED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 194DN 43189 7252 28451 727679 UPON PUSHBACK AFTER LT ENG START, LT ENG REV POS STATUS MSG BIT LT ENG PIMU. FAULTED EEC CH A/B REVR CR CK FAIL. DEACT IVATED LT ENG THRUST REVERSER PER MEL 78-31-01, MCO AND PLACARD INSTALLED. T/S PER FIM 71 PIMU INDEX FOR MSG 353-25 LVD T RES CK NORM. RAN T/R SEVERAL TIMES WITH NO FAULTS. RAN ENG NO MSG. T/R ACTIVATED MCO AND PLACARD REMOVED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007041000071 20070410 00071 NM 2007 4 10 DL76G070284 1 20070402 A 3840 COMPRESSOR BOEING 767 767324 1385203 NM POTABLE WATER UNSERVICEABLE A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 394DL 27394 BURNING ELECTRICAL SMELL IN AFT RT GALLEY DURING LEFT ENGINE START. NO SMOKE RETURNED TO GATE. LOCATED POTABLE WATER C OMPRESSOR MOTOR BURNED INOP FWD TO MCO/PLAC PER MEL 38-10-01A PULLED AND COLLARD C/B ON P33 PANEL FOR COMPRESSOR NEEDS N EW COMPRESSOR. FOUND POTABLE WATER COMPRESSOR MOTOR AT FAULT REPLACED PER AMM. OPERATION LEAK CKS GOOD. REMOVED MCO A ND PLACARD. 2 L 7 2 4F RT A1NM 2007041000072 20070410 00072 NE 2007 4 10 DL76L070286 2 20070402 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 MALFUNCTIONED A DALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 27 194DN 43189 7252 727679 28451 727679 ON CLIMB-OUT AROUND 15000 FT MSL APPROX 7 MINUTES INTO THE FLIGHT LT ENGINE ABRUPTLY ROLLED BACK TO IDLE 1.0 EPR THEN AT TEMPTED TO RECOVER CREW EMPLOYED QRH AT ARM SWITCH OFF AND RETARDED THROTTLE. REPLACED NR 1 ENG PER TRANS 1T148 . 2 L 7 2 4F 4 F RT A1NM E24NE 2007041000073 20070410 00073 NE 2007 4 10 DLM90070287 2 20070402 A 7230 V2528D5 ENGINE DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 1 FOD A DALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 27 905DA 27510 53385 020042 AT FL310, LEFT ENGINE SHUT DOWN IN FLT HEARD BANG AND FELT SHUTTER N1 RAPIDLY DECREASED, EGT INCREASED TO 730 OIL PRESS WENT TO -0-. C/W BORESCOPE INSP FOUND FOD BEYOND M/M LIMITS. DAMAGE STA AT 3RD STG HPC. STG 2.5 LPC BLADES ARE CLEAN E NG CHANGE REQUIRED. REPLACED LT ENG AS PER TRANS 2T102. 2 L 7 2 4F 4 F RT A6WE E40NE 2007041000076 20070410 00076 NM 2007 4 10 DL76G070296 1 20070405 A 5315 BAC1505101303 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 654 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 154DL 25241 BS 654 + 121 RBL 28 TO 55 FLOORBEAM UPPER CHORD CORRODED AND REPAIRED PER DRD53-00-51D FIG 201 ON NR CARD 51907. 2 L 7 2 4F RT A1NM 2007041000077 20070410 00077 NM 2007 4 10 DL76G070297 1 20070405 A 5315 BAC1505101303 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 654 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 154DL 25241 BS 654+88 RBL 28 FLOORBEAM UPPER CHORD FOUND CORRODED AND REPAIRED AS PER DRD 53-00-51D. 2 L 7 2 4F RT A1NM 2007041000080 20070410 00080 NM 2007 4 10 DL76G070300 1 20070405 A 5315 BAC50337075T6511 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 1153 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 154DL 25241 AFT CAGRO COMPARTMENT STA 1153 RBL 29 FLOORBEAM FWD FACE UNDERSIDE CORRODED AND REPAIRED AS PER SRM 53-10-07 REPAIR 4 FI GURE 201 DETAIL 3. 2 L 7 2 4F RT A1NM 2007041000082 20070410 00082 SO 2007 4 10 C2XA07IA075 1 20070324 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12567 145623 MCI - DURING MAINTENANCE INSPECTION AISLE PATH LIGHTS 6, 7 & 8 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007041000084 20070410 00084 SO 2007 4 10 C2XA07IA076 1 20070325 A 2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY MALFUNCTIONED A C2XA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 27 16987 145261 IAH - FLIGHT 2890, THE CREW REPORTED A LAV SMOKE WARNING FOR 15 SECONDS IN FLIGHT WITH NO VISUAL INDICATION OF SMOKE THR OUGHOUT FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY TES TED THE LAV SMOKE DETECTOR ALL WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007041000085 20070410 00085 SO 2007 4 10 C2XA07RI011 1 20070325 A 3350 REBC410A1001CB RELAY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12922 145338 FLT 2359 - EWR - CREW REPORTED ELECTRICAL EMERGENCY ABNORMAL AND EMERGENCY LIGHT NOT ARMED INDICATIONS CAME ON TAXI. EW R MX REMOVED AND REPLACED RELAY K0097 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERV ICE. 2 L 7 2 4T RT T00011AT 2007041000086 20070410 00086 NM 2007 4 10 SWAA071735 1 20070404 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 436WN 32456 DURING SCHEDULED HC2 CHECK, EEPLS COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2007041000087 20070410 00087 NM 2007 4 10 SWAA071729 1 20070404 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 583 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 583, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007041000089 20070410 00089 NM 2007 4 10 SWAA071732 1 20070404 A 5313 6551698 STRINGER SPLICE BOEING 737 7373Y0 1384671 NM BS 727 S22L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 727, STR 22L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007041000091 20070410 00091 NM 2007 4 10 SWAA071730 1 20070404 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 827 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007041000093 20070410 00093 NM 2007 4 10 SWAA071727 1 20070404 A 5753 65C35276 FLAP TRACK BOEING 737 7373H4 1384600 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND LEFT INBOARD MID FLAP OUTBOARD FORE FLAP TRACK CORRODED. REMOVED AND REPLACED FLAP TR ACK PER MM. 2 L 7 2 4F RT A16WE 2007041000097 20070410 00097 SO 2007 4 10 SIMA200709617 1 20070405 A 2701 12049637001 BUSHING EMB 135 EMB135LR 3260305 SO YOKE WORN A SIMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 702AE 16316 145164 CAPTAIN YOKE HAS APPROXIMATELY QUARTER INCH OF DEAD SPACE WHEN MOVING ELEVATOR. REMOVED AND REPLACED BUSHING ON ELEVATO R BELL CRANK IAW EMB AMM. PERFORMED OPERATIONAL CHECKS WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041000104 20070410 00104 SO 2007 4 10 SIMA200709604 1 20070403 A 5347 13500438003 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 703MR 15867 4800 145173 RIGHT WALL SEAT TRACK CORRODED BETWEEN FRAME 24 AND FRAME 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041000105 20070410 00105 SO 2007 4 10 SIMA200709609 1 20070403 A 5320 14521725613 SILL EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 703MR 15867 145173 FOUND SERVICE DOOR FORWARD SILL CORRODED. REPAIRED SILL BY CUTTING OUT DAMAGED AREA AND INSTALLED A DOUBLER IAW IC2007- 140/02123 AND SRM 53-21-10. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041000106 20070410 00106 SO 2007 4 10 SIMA200709605 1 20070403 A 5347 14530658005 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 703MR 15867 4800 145173 RIGHT SEAT TRACK FROM FRAME 36 TO FRAME 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB SRM 53-01-06. AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041000107 20070410 00107 SO 2007 4 10 SIMA200709606 1 20070403 A 5320 14521725613 SILL EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 703MR 15867 4800 145173 FOUND SERVICE DOOR SILL CORRODED. REPAIRED BY CUTTING OUT DAMAGED AREA AND INSTALLED A DOUBLER IAW EMB IC2007-140/02123 AND SRM 53-21-010. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041000109 20070410 00109 NM 2007 4 10 DL76G070301 1 20070405 A 5315 BAC1503100229 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 1153 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 154DL 25241 AFT COMARTMENT STA 1153 RBL 28 FLOORBEAM AFT FACE UNDERSIDE CORRODED AND REPAIRED PER SRM53-00-07 REPAIR 4 FIG 201 DETAI L V. 2 L 7 2 4F RT A1NM 2007041000110 20070410 00110 NM 2007 4 10 DL76G070302 1 20070405 A 5315 BAC1509100682 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 1197 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 154DL 25241 AFT CARGO COMPARTMENT STA 1197+66 FLOORBEAM AFT FACE UNDER SIDE CORRODED AND REPAIRED PER SRM53-00-07 REPAIR 4 FIG 201 D ETAIL VI. 2 L 7 2 4F RT A1NM 2007041000112 20070410 00112 NM 2007 4 10 DL76G070304 1 20070405 A 5315 BAC1503100229 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 1197 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 154DL 25241 AFT CARGO COMPARTMENT STA 1197+44 RBL 22.5 FLOORBEAM AFT FACE UNDERSIDE CORRODED AND REPAIRED PER SRM 53-00-07 REPAIR 4 FIG 201 DETAIL V. 2 L 7 2 4F RT A1NM 2007041000113 20070410 00113 NM 2007 4 10 DL76G070305 1 20070403 A 2150 211002344 VALVE BOEING 767 767332 1382001 NM LT A/C PACK FAILED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 1608 30573 BEFORE PUSHBACK W/L PACK OFF THE PACK OFF LIGHT WENT OUT AND THE L PACK OFF EICAS MESSAGE WAS NOT DISPLAYED. RTB, REMOV ED AND REPLACED LT PACK VALVE. OPS NORMAL. 2 L 7 2 4F RT A1NM 2007041000114 20070410 00114 NM 2007 4 10 DL764070306 1 20070405 A 3220 FITTING BOEING 767 767432ER 1385134 NM NLG DAMAGED A DALA D RETURN TO BLOCK W INADEQUATE Q C TX TAXI/GRND HDL 1 SO 27 831MH 29702 ON PUSHBACK, TOWBAR BOLT AND TOW LUG SUSTAINED DAMAGE. REMOVED TOWBAR FITTINGS FROM NOSE GEAR. INSTALLED NEW TOW BAR F ITTING PER AMM FIT CK OK. 2 L 7 2 4F RT A1NM 2007041000115 20070410 00115 2007 4 10 DL76G070307 4 20070407 A 3417 4040800912 ADC BOEING 767 767332 1382001 NM MALFUNCTIONED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 1607B 30388 DURING TAKEOFF ROLL F/O AIRSPEED INDICATOR FROZEN AT ZERO WITH NO WARNING FLAGS OR EICAS LIGHTS. ONCE AIRBORNE A/S INDI CATOR BEGAN TO MOVE AND PEGGED HIGH AT 400KTS. WITH ASSOCIATED IAS DISAGREE. RUDDER RATIO-AIL LOCKOUT AND L/R EEC MODE EICAS ILLUM. F/O SELECTED ALT AIR DATA AND A/S AND ALTIMETER RETURNED TO NORMAL. EICAS WARNS THE SAME EXCEPT FOR TAS DISAGREE OUT. REMOVED AND REPLACED RT ADC. PERFORMED TEST 30 CHKS OK. PERFORMED ADC TEST CHKS NORMAL. OK FOR SERVICE . 2 L 7 2 4F RT A1NM 2007041000116 20070410 00116 NE 2007 4 10 DL76L070308 2 20070407 A 7261 815316 OIL FILTER BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE UNKNOWN A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 187DN 27582 724166 AFTER ENGINE START R OIL FILTER CAUTION AND R OIL FILTER STATUS MSG, OIL QTY INDICATED 2QTS, SHUTDOWN ENGINE. REPLACED RT ENGINE MAIN OIL FILTER PER AMM 79-21-05. RAN ENGINE. LEAK CHECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007041000117 20070410 00117 WP 2007 4 10 ABXA070087 1 20070328 A 2170 1808492 COALESCER BAG DOUG DC9 DC941 302207N WP TAIL COMPARTMENT ODOR A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 974AX 47623 ODOR IN COCKPIT, SUSPECT COALESCER BAG. REPLACED WATER SEPARATOR COALESCER BAGS IAW DC9 MM 21-20-02-2. 2 L 7 2 4F A6WE 2007041000118 20070410 00118 NM 2007 4 10 UIEA200700146 1 20070402 A 5330 7075T60040 SKIN BOEING 747 7472D7B 1384803 NM BS 2360 S30-32R CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 527MC 22471 FUSELAGE STATION 2360 RT SIDE, BETWEEN STRINGERS 30R AND 32R HAS AN AREA OF 3.0 INCH LONG BY 11.0 INCHES WIDE OF CORROSI ON ON SKIN. ACCOMPLISHED PERMANENT REPAIR AS PER 747-200 SRM 53-30-03 FIG 1. AREA OF CORROSION WAS CUT-OUT AND HFEC WA S ACCOMPLISHED TO VERIFY ANY CRACKS AS PER 747 NDT MANUAL 51-00-00 FIG 23 PAR 6, DOUBLER AND FILLER WERE INSTALLED PER 7 47-200 SRM 53-30-03 FIG 1. ALSO, REFERENCE ATLAS AIR XEO 53-040207. 2 L 7 4 4F RT A20WE 2007041000119 20070410 00119 NM 2007 4 10 UIEA200700145 1 20070326 A 2697 WIRE BOEING 747 7472D3B 1384805 NM GE CF6 CF650E2 30018 NE NR 3 FIRE WARN CHAFED A UIEA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 EA 15 505MC 21251 517577 AFTER T/O FROM AMS, WHERE NR 3 ENGINE B LOOP WAS DEFERRED AS INOP. NR 3 ENGINE FIRE BELL AND LIGHT ILLUMINATED, NR 3 EN GINE A LOOP WAS ERRATIC AND WAS AT 10 ON THE SCALE FLUCTUATING. ENGINE SHUT DOWN AS PER ATLAS PROCEDURE USING FIRE CHEC K LIST FIRE SWITCH AT 1602Z, WIND MILL OIL PRESSURE 7-9 PSI. FOUND WIRING AT CONNECTORS DM132A AND DM214A WITH WORN INS ULATION AND CHAFING AGAINST CONNECTORS. REPLACED CONNECTORS PER SWPM 20-62-19. ALL CHECKS SATISFACTORY PER MM 26-11-00 . NO FURTHER FAULT FOUND. 2 L 7 4 4F 4 F RT A20WE E23EA 2007041000123 20070410 00123 NM 2007 4 10 UIEA200700140 1 20070304 A 5347 SEAT TRACK BOEING 747 74747UF 1384949 NM BS 1905-1920 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 496MC 29257 LOWER AFT CARGO COMPARTMENT SEAT TRACK BETWEEN STA 1905-1920, RBL 25 CRACKED. SEAT TRACK REPLACED AS PER SRM 53-00-52. 2 L 7 4 4F RT 1384945 2007041000124 20070410 00124 NM 2007 4 10 UIEA200700141 1 20070304 A 5347 SEAT TRACK BOEING 747 74747UF 1384949 NM BS 1905-1920 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 496MC 29257 LOWER AFT CARGO COMPARTMENT SEAT TRACK CRACKED STA 1905-1920, RBL 45. SEAT TRACK REPLACED AS PER SRM 53-00-52. 2 L 7 4 4F RT 1384945 2007041000126 20070410 00126 2007 4 10 QXEA200700518 2 20070408 A 7200 ENGINE BOMBDR DHC8 DHC8402 1390042 NM NR 1 MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 418QX 4143 SEA FLIGHT NR 2316: ON CLIMB-OUT AT ABOUT 13,000, NOTICED TORQUE SPLIT. NR 1 TORQUE WAS STAYING 6 PERCENT LESS THAN NR 2. ALSO, NR 1 NL AND NH WERE LOWER THAN 32. RETURNING TO SEA IN DESCENT AT LOW POWER SETTINGS, TORQUE SPLIT WOULD SEEM TO BE LESS NOTICEABLE. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INTERROGATED CDS AND NO FAULTS WERE FOUND. C/W POWER ASSURANCE RUNS IAW AMM 71-00-00-868-806. CHECKS GOOD. RAN BOTH ENGINES AT VARIOUS POWER SETTINGS WITH BLEEDS ON AND OF F WITH NO TORQUE SPLIT NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007041000127 20070410 00127 EA 2007 4 10 TRAX200700445 1 20070401 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 CABIN AFT MOST CEILING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007041000129 20070410 00129 WP 2007 4 10 07FDEA01280 1 20070403 A 5310 BEAM DOUG DC10 DC1010 3022110 WP BS 1099 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 FWD CARGO COMPT CRACK 2" ON LOWER BEAM STA 1099. REPAIRED BEAM IAW SRM 53-60-01 FIG 3 VOL 1. 2 L 7 3 4F A22WE 2007041000130 20070410 00130 WP 2007 4 10 07FDEA01282 1 20070403 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 535 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 RT AIR COND COMPT FOUND CRACK 5" LONG ON FRAME STA 535. REPAIRED FRAME IAW SRM 53-30-00 FIG 5 AND SRM 53-00-01 FIG 8 VO L 1. 2 L 7 3 4F A22WE 2007041000131 20070410 00131 WP 2007 4 10 07FDEA01285 1 20070403 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 1256 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 MAIN CABIN FOUND 1 CRACK 4" ON BEAM SUPPORT SEAT TRACK STA 1256. REPAIRED BEAM IAW SRM 53-00-01 FIG 9 VOL 1. 2 L 7 3 4F A22WE 2007041000132 20070410 00132 WP 2007 4 10 07FDEA01292 1 20070403 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP LT MLG WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 LT MLG W/W FOUND 1 CRACK 2" LONG ON VERTICAL BLKHD. REPAIRED IAW SRM 53-00-01 FIGURE 4 SHT 2 VOL 1. 2 L 7 3 4F A22WE 2007041000133 20070410 00133 2007 4 10 C2XA07RI010 4 20070301 A 2300 7013270965 RMU EMB 145 EMB145LR 3260212 SO NR 2 BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 15574 10648 10648 145639 FLT 6064 RIC - EWR, CREW REPORTED SMOKE IN COCKPIT FROM DASH BOARD FOR 3 TO 5 SECONDS THEN STOPPED. EWR MX FOUND RMU NR 2 BURNT. MX REMOVED AND REPLACED RMU NR 2 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN T O SERVICE. 2 L 7 2 4T RT T00011AT 2007041000135 20070410 00135 WP 2007 4 10 UPS07849586 1 20070403 A 5280 RELEASE MECH DOUG DC8 DC873F 302199F WP NLG DOOR CONTAMINATED A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 819UP 46019 INSPECTION TYPE:N/A DIVERSION - LEFT NOSE GEAR DOOR OPEN IN FLIGHT. FOUND LEFT NOSE GEAR DOOR RELEASE TRIGGER JAMMED WI TH DEBRIS. CLEANED TRIGGER IAW MM 32-20-00-01. GEAR DOOR LATCHES NORMALLY, A/C OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2007041000138 20070410 00138 NM 2007 4 10 UPS07M49513 1 20070226 A 5315 AFA7299 FLOORBEAM DOUG MD11 MD11F 3023600 NM BS 1701 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C CTR CARGO COMPT ALONG STA 1701 BETWEEN X=7 AND X=18, FLOORBEAM SUPPORT FOUND CORRODED, AFTER ROLLER TR AY REMOVAL. CORROSION BLENDED & FOUND EXCEED LIMIT PER SRM 53-00-01 F3 R38. DISCREPANT FLOOR SUPPORT REMOVED PER SRM 5 1-35-01 V2 R38. NEW SUPPORT RWK FROM S2929841 PER DWG P/N AFA7299. NEW SUPPORT REPROTECTED & PAINTED PER SRM 51-21-01 V2 R38. NEW SUPPORT LOCATED & INSTALLED PER DWG AFA7299, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007041000139 20070410 00139 NM 2007 4 10 UPS07M49514 1 20070118 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1239-1245 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C MAIN DECK: FROM BS 1239 TO 1245 LT MOST O/B SEAT TRACK CROWN AREAS & FLANGE FOUND CORRODED. REMOVED SEAT TRACK FROM BS 1229 - BS 1351 LT MOST O/B PER 51-31-01 V2 R38. RWK NEW SEAT TRACK & PICKED UP HOLES PER SRM 53-70-0 0 F1 R38. OK TO INSTALL. NEW SEAT TRACK PER SRM 53-70-00 F1 R38. 2 L 7 3 4F RT A22WE 2007040600130 20070406 00130 CE 2007 4 6 DXTA200702067 1 20070402 A 2731 TRIM SYSTEM CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE STUCK E DXTA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 07 603QS 5605203 (P) ON TAKEOFF TRIM STUCK JUST BETWEEN THE TOP LINE AND THE TOP OF THE (T) IN THE TAKEOFF RANGE. WE MANUALLY FORCED IT F REE AND IT BEGAN TO WORK AGAIN. DURING THE RETURN TO THE AIRPORT, THE ELECTRIC TRIM SEEMED TO DRAG IN THE TAKEOFF RANGE. PERIODICALLY MOVING FREELY AND THEN DRAGGING AGAIN. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007040600144 20070406 00144 NM 2007 4 6 MWEA070048 1 20070325 A 7830 7150922505 RIB BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 921ME 55183 RIGHT THRUST REVERSER BUCKET HAS A CRACKED RIB JUST AFT OF OUTBOARD LOCK PIN. FABRICATED AND INSTALLED THRUST REVERSER. 2 L 7 2 4F TR A6WE 2007040600148 20070406 00148 WP 2007 4 6 MWEA070076 1 20070404 A 5330 59360041 SKIN DOUG DC9 DC982 3022082 WP BS 636 S27 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 810ME 48072 LONGERON 27 AT STATION 636 EVIDENCE OF SKIN DENTED. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2007040600155 20070406 00155 NM 2007 4 6 DU4R2007078 1 20070327 A 5330 SKIN BOEING 757 757232 1384965 NM BS 418 S16L DENTED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND DENT IN EXTERIOR SKIN AT BS 418 S-16L. REPAIRED BY IAW B757 SRM 53-00-01 FIG 207 BY CUTTING OUT DENTED SKIN. HFE C CUTOUT, NO CRACKS INDICATED. FABRICATED AND INSTALLED DOUBLER 12" BY 7" FROM 2024-T3 .071 AND FILLER FROM 2024-T3 .06 3 IAW B757 DELTA SRM 53-00-01 FIG 201, 53-10-01 FIG 1, 51-20-01. 2 L 7 2 4F RT A2NM 2007040600157 20070406 00157 NM 2007 4 6 07FDEA01216 1 20070331 A 2571 65239431 BATTERY BOX BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 E/E COMPARTMENT BATTERY BOX CORRODED AT FOWARD RT AND LT CORNERS REMOVED CORROSION FROM BATTERY BOX. MATERIAL LOSS WAS OUT OF LIMITS, REF SRM 51-30-2 FIG. REPLACED WITH NEW BATTERY BOX REF MM 24-30-011-4. 2 L 7 3 4F A3WE 2007040600158 20070406 00158 NM 2007 4 6 07FDEA01217 1 20070331 A 2571 69216492 BATTERY BOX BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 E/E COMPARTMENT BATTERY TRAY AFT EDGE IS CORRODED. REMOVED, FABRICATED AND ACP HEAT TREAT PROCESS FOR 2024-T4, CONDITIO N FOR TRAY. REF BAC DWG 69-21649 REV C AND BAC5602 REV (AF) 28 AUG 01 AND BAC 5946 REV (AA) 9 JUL 01. IDENTIFIED TRAY AS FX-69-21649-1. W/O 11841-1000-0004 AND REINSTALLED REF SRM 51-30-02 PG 13. 2 L 7 3 4F A3WE 2007040600165 20070406 00165 NM 2007 4 6 07FDEA01207 1 20070330 A 5720 6521656 SUPPORT BOEING 727 727225 1384077 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 RT WING INBD TE LOWER SURFACE FWD INNER SUPPORT CLIP IS CRACKED AT ATTACH TO REAR SPAR FLANGE OFF PANEL 10" O/B OF O/B E ND OF MLG BEAM REMOVED DAMAGED CLIP, VERIFIED REPAIR MATERIAL AS 2024-T3-.040 REF DWG NR 65-21656, AND FABRICATED REPL ACEMENT CLIP REF DWG 65-21656 AND FED EX GMM 7-0-1001 ITEM 7C. TREATED REPLACEMENT CLIP REF 727 MM 51-10-2 PG 7G AND PR IMED REF 727 AMM 51-20-151-1 TMES 5 AND 6. INSTALLED REF 727 SRM 51-20-2. 2 L 7 3 4F A3WE 2007040900041 20070409 00041 NM 2007 4 9 07FDEA01223 1 20070331 A 2611 1014A RELAY BOEING 727 727233 138408A NM FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 283FE 22350 FIRE WARNING MASTER LIGHTS ILLUMINATED, INTERMITTENTLY, WITH AUDIO BELL. NO OTHER INDICATIONS. REMOVED AND REPLACED R97 RELAY AND M438, REF WIRING DIAGRAM MANUAL 49-41-01 PAGE 3. NEEDS OPS CHECKS. REF MM 26-15-000, OP CHECK APE FIRE SYST EM. CHECKS OK. 2 L 7 3 4F RT A3WE 2007040900043 20070409 00043 NM 2007 4 9 07FDEA01225 1 20070401 A 5730 65162094 SKIN BOEING 727 727225 1384077 NM LT WINGTIP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 LEFT WING SMALL CRACK AND DENT IN WING TIP L/E ADJACENT TO O/B END. REMOVED AND REPALCED WING TIP SKIN PNL IAW SRM 51-3 0-2, P/N 65-16209-4. PAINTED SKIN IAW MM 51-20-151-7. 2 L 7 3 4F A3WE 2007040900050 20070409 00050 WP 2007 4 9 07FDEA01255 1 20070403 A 5720 STRUCTURE DOUG DC10 DC1010 3022110 WP RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 RT WING SEVERE CORROSION ON UPPER BEAVER TAIL. REPAIR CORROSION IAW FEDEX EA 8-5710-103714. 2 L 7 3 4F A22WE 2007040900054 20070409 00054 WP 2007 4 9 07FDEA01260 1 20070403 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 879-887 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 LWR FUSELAGE EXT SKIN FOUND DEEP DENT 2" BY 2" DEEP 0.07". REPAIRED IAW FEDEX EA 8-5310-96119. 2 L 7 3 4F A22WE 2007040900061 20070409 00061 EU 2007 4 9 07FDEA01303 1 20070403 A 5340 ATTACH FITTING AIRBUS 310 A310304 3930339 EU NLG WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 FUSELAGE CRACKED LT NLG DOOR ACTUATOR ATTACH FITTING (EO 6-5340-7-5001). COMPLIED WITH EA 6-5340-102027 PT1 FUSELAGE CR ACKED LT NLG DOOR ACTUATOR ATTACH FITTING (EO 6-5340-7-500 1) IAW SB A310-53-2065 REV 04. 2 L 7 2 4F RT A35EU 2007040900070 20070409 00070 NM 2007 4 9 UPS07549563 1 20070309 A 5311 146N100503 FRAME BOEING 757 75724APF 1384969 NM BS 1280 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 441UP 27386 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1280, S26L. REPAIRED FRAME PER FINAL EA 757-5362-27-A1619 AND UP S EO B757-26423 7-A. 2 L 7 2 4F RT A2NM 2007040900080 20070409 00080 EU 2007 4 9 07FDEA01264 1 20070403 A 5315 A53773651212 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 HEAVY CORROSION ON TOP CAP BEAM, C38.2 IN FWD CARGO COMPARTMENT. REPLACEMENT OF TOP CAP BEAM (A537-73651-212-00) IAW 51 -72-10. 2 L 7 2 4F RT A35EU 2007041600112 20070416 00112 CE 2007 4 16 DXTA200702083 1 20070405 A 2700 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL UNKNOWN E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 990QS 7500190 CRUISING AT 9,000 FEET WITH A/P ON, THE TRIM CLACKER CAME ON CONTINUOUSLY TO FULL NOSE DOWN, THEN THE FGC A FAILED AND K ICKED OFF A/P. REPLACED FAILED ECM. OPS CHECKED OK. IAW. CE 750 M/M 27-40-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007040900093 20070409 00093 EU 2007 4 9 MALA070046 1 20070403 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 442XJ 340B442 THE SEAT TRACK AT LBL 18.3, CENTER AISLE FLOOR FLANGE, IS CORRODED OUT OF LIMIT. THE DAMAGE HAS BEEN REPAIRED IAW MESAB A EO S53342. REF: EAMS WORK ORDER 215978 TASK 1533. 2 L 7 2 4T RT A52EU 2007040900094 20070409 00094 NM 2007 4 9 KNNA200700019 1 20070331 A 5311 65C23267 FRAME BOEING 737 7372L9 1384497 NM PWA JT8 JT8D15 52051 NE BS 360 CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 464A 49673 3000 21278 3 INCH CRACK OVER BODY STATION 360 FRAME BETWEEN STRINGERS 23 TO 22. REPAIR IS IN PROGRESS IN ACCORDANCE WITH SERVICE B ULLETIN B737-53A1064 AND DRAWING NUMBER 65C23267. 2 L 7 2 4F 4 F RT A16WE E2EA 2007040900097 20070409 00097 CE 2007 4 9 MLJ2007F00000 1 20070329 A 5712 BULKHEAD CESSNA 310 310R 2074245 CE RT WING CRACKED E MLJA K NONE O OTHER IN INSP/MAINT 1 GL 11 3284M 310R1892 WHILE AC WAS IN FOR AN ANNUAL INSPECTION, A CRACK WAS FOUND IN THE REAR MOUNT BULKHEAD ON THE RT MAIN TANK. THE CRACK W AS APPROX 1.5 INCH LONG AND LOCATED IN THE UPPER IB RADIUS OF THE WEBBING, NOT THE FLANGE. THE CRACK DID NOT ORIGINATE FROM AN EDGE OR A HOLE AND WAS PERPENDICULAR TO THE RADIUS. A PROBABLE CAUSE WAS PART FATIGUE DUE TO AGE OF PART. SOME POSSIBLE CONTRIBUTING FACTORS WERE FLIGHTS INTO TURBULENT WEATHER DUE TO AIRCRAFT BEING OWNED BY A CHARTER COMPANY. A C TOTAL TIME AT TIME OF REPLACEMENT WAS 11286.4 HRS AND PART TIME IS ASSUMED TO BE THE SAME. THE PART WAS REPLACED WITH A NEW PART FROM MFG. (K) 1 L 7 2 3O 3A10 2007040900101 20070409 00101 WP 2007 4 9 UPS07849593 1 20070314 A 5347 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C3 INTERCOSTAL UNDER SEAT TRACK STA 70-80 RBL 48 HAS CORROSION. REMOVED INTERCOSTAL AT STA 65-80 IAW SR M 51-1-20D. FABRICATED INTERCOSTAL AND INSTALLED AT STA 65-80 IAW DWG 4888755, AND SRM'S 51-3-2, AND 51-1-20D. 2 L 7 4 4F RT 4A25 2007040900109 20070409 00109 NM 2007 4 9 CALA0700163 1 20070403 A 5514 6547533501 ANGLE BOEING 737 737524 1384721 NM STAB STA 83.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14604 27317 INSPECTION FOUND A .5 INCH CRACK IN LT HORIZONTAL STABILIZER LEADING EDGE WEB L-ANGLE AT STAB STA 83.5. A REPAIR WAS IN STALLED IAW ECRA 5510-01883. 2 L 7 2 4F RT A16WE 2007040900121 20070409 00121 NM 2007 4 9 QXEANM09406 1 20070313 A 4920 164161100 DRAIN VALVE BOMBDR DHC8 DHC8402 1390042 NM APU DAMAGED G QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 BALL ON WRONG SIDE OF SPRING, WHICH ALLOWS IT TO REST IN CLOSED POSITION, NOT ALLOWING PROPER DRAINAGE. 2 H 7 2 4T RT A13NM 2007040900130 20070409 00130 NM 2007 4 9 QXEANM09425 1 20070313 A 4920 164161100 DRAIN VALVE BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA APU PLUGGED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 425QX 4039 BALL ON WRONG SIDE OF SPRING ALLOWING IMPROPER DRAINAGE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2007040900164 20070409 00164 NE 2007 4 9 BB07033 2 20070402 A 7200 ENGINE BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE NR 1 VIBRATION A USAA O OTHER E VIBRATION/BUFFET CR CRUISE 1 EA 19 922UW 22202 FLIGHT 1866, FLL-PHL: DURING FLIGHT, CREW REPORTED A NUMBER ONE ENGINE VIBRATION AND NO RESPONSE TO THROTTLE MOVEMENTS. DECLARED EMERGENCY AND LANDED PHL WITH NO OTHER DIFFICULTIES. ENGINE SHUT DOWN NORMALLY AFTER LANDING. MAINTENANCE R EPLACED THE LEFT ENGINE. 2 L 7 2 4F 4 F RT A2NM E12EU 2007041000006 20070410 00006 SO 2007 4 10 C2XA07IA078 1 20070405 A 3230 UNKNOWN EMB 145 EMB145EP 3260221 SO LANDING GEAR UNKNOWN A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 15926 145005 IAH - FLIGHT 2810, THE CREW REPORTED THAT DURING CLIMB THE NOSE LANDING GEAR FAILED TO RETRACT AND STAYED IN TRANSITION FOR 15-20 SEC AFTER MAIN GEAR RETRACTED. ALSO THE NOSE LANDING GEAR DOORS DID NOT CLOSE. THE AIRCRAFT LANDED AT IAH WI THOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE EXTENSION AND RETRACTION SYSTEM WITH NO D EFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041000010 20070410 00010 SO 2007 4 10 SIMA200709402 1 20070331 A 5320 14522178005 SILL EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 708AE 15810 4800 145205 SERVICE DOOR SILL FOUND CORRODED. REMOVED AND REPLACED SERVICE DOOR SILL IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SE RVICE. 2 L 7 2 4F RT T00011AT 2007041000012 20070410 00012 SO 2007 4 10 SIMA200709404 1 20070402 A 3213 STRUT EMB 135 EMB135KL 3260302 SO NLG LOW A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 853AE 145742 RECEIVED AIR/GND FAIL MESSAGE ON EICAS. RETURNED TO DFW. PERFORMED RESERVICE OF NOSE STRUT IAW EMB AMM. PERFORMED GEA R SWING WITH NO DEFECTS. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041000014 20070410 00014 SO 2007 4 10 C2XA07CL036 1 20070407 A 2611 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL LAVATORY MALFUNCTIONED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 12172 14500864 CAE312657 CLE FLIGHT 2488 - THE CREW REPORTED A LAV SMOKE WARNING INDICATION DURING CLIMB. THE AIRCRAFT RETURNED TO CLE AND LANDE D WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE. OPERATIONAL CHECKS WERE GOOD. THE PRIMARY FAI LURE/REASON FOR REMOVAL WAS OIL LEAKING PAST NR 4 CARBON SEAL ASSEMBLY ALLOWING OIL TO ENTER THE CORE FLOWPATH AND CAUSE OIL SMELL IN THE CABIN. 2 L 7 2 4F 4 F RT TE6CH 2007041000015 20070410 00015 SO 2007 4 10 C2XA07RI008 1 20070323 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16987 145261 EWR - FLT 2882 - DURING PREFLIGHT CHECK, CREW REPORTED GALLEY EMERGENCY EXIT LIGHT INOP. EWR MAINTENANCE REMOVED AND RE PLACED NR 3 EMERGENCY LIGHT INVERTER. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO FLIG HT. 2 L 7 2 4T RT T00011AT 2007041000016 20070410 00016 SO 2007 4 10 C2XA07TY016 1 20070329 A 2530 THERMAL SWITCH EMB 145 EMB145LR 3260212 SO ZONE 900 TRIPPED A C2XA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14920 145380 FLT 2807, F/A NOTED THERMAL SWITCH FOR GALLEY POPPED IN FLIGHT WITH ASSOCIATED BURNING ODOR. AC RELEASED IAW MEL 25-60 -02 (3) CAT D. 2 L 7 2 4T RT T00011AT 2007041000022 20070410 00022 NM 2007 4 10 07FDEA01309 1 20070403 A 5415 6519686765 NACELLE BOEING 727 727225 1384077 NM ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 NR 1 ENGINE FIXED COWL UPPER SECTION CRACKED AT UPPER FWD CORNER. REPLACED FIXED COWL, NEW COWL INSTALLED ON WC 70T0001 -01. 2 L 7 3 4F A3WE 2007041000029 20070410 00029 NM 2007 4 10 QXEA200700516 1 20070406 A 6120 697072003 GOVERNOR BOMBDR DHC8 DHC8402 1390042 NM NR 2 OVERSPEED MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 409QX 6235 5084 4051 LAX FLIGHT NR 2307: UNABLE TO GET NR 2 PROP OUT OF FEATHER AFTER ENGINE STOP. MAINTENANCE REMOVED AND REPLACED THE NR 2 OVERSPEED GOVENOR PER Q400 MM 61-20-26-000-801 AND 61-20-26-400-801. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007041000040 20070410 00040 EA 2007 4 10 TRAX200700452 1 20070402 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 830AS 7236 RIGHT FS 484 INTERCOSTAL HAS CRACK IN CLIP AT RBL 27 IB. REMOVED CRACKED CLIP ON RT FS 484 INTERCOSTALS' AT RBL 27 AND DUPLICATED PER CRJ SRM 53-41-43 FIG. 1 ITEM 3. 2 L 7 2 4F RT A21EA 2007041000050 20070410 00050 EA 2007 4 10 TRAX200700462 1 20070404 A 5310 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 RIGHT FS 280 CROSSBEAM HAS CORROSION ON UPPER FLANGE. REMOVED RT FS 280 CROSSBEAM IAW CRJ 700 SRM 51-42-06 AND 51-42-21 . LOCATED NEW SERVICEABLE CROSSBEAM IAW CRJ 700 SRM 51-40-11. 2 L 7 2 4F RT A21EA 2007041000051 20070410 00051 NM 2007 4 10 BB07032 1 20070331 A 7932 8TJ146AAA1 TRANSMITTER BOEING 767 767201 1385125 NM GE CF6 CF680 30025 NE OIL QTY FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 245AY 23897 695133 FLIGHT 1015, PHL-STT: ABOUT 20 MINUTES AFTER DEPARTURE, RIGHT ENGINE OIL QUANTITY INDICATION DROPPED TO ZERO. OIL PRES SURE REMAINED NORMAL. FLIGHT RETURNED TO PHL. MAINTENANCE REPLACED THE RIGHT OIL QUANTITY TRANSMITTER. NO FURTHER FAU LTS. 2 L 7 2 4F 4 F RT A1NM E13NE 2007070300043 20070703 00043 NM 2007 7 3 070086 1 20070405 A 2131 21171802 CONTROLLER DOUG MD80 MD83 3023681 NM CABIN PRESSURE MALFUNCTIONED A WX0A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 19 874GA 49643 THE FLIGHT CREW REPORTED "FLOW LIGHT ILLUMINATED/"ON". UNABLE TO MAINTAIN CABIN ALT." NO OTHER INFORMATION AVAILABLE ON FLT LOG PAGE. ACRFT DESCENDED FROM FL320 TO APPROX 10,000 FT, CABIN PRESSURE STABILIZED. WHILE IN PROGRESS, SUPPLY DUC T PRESSURE 30PSI, "FLOW" ANNUNCIATOR ILLUMINATED & CABIN RATE-OF-CLIMB 1500 FPM. ACRFT DIVERTED TO COS & LANDED WITHOUT FURTHER INCIDENT. COS MX & FLT CREW PRESSURIZED ACRFT ON GROUND WITH LT PACK TO APPROXIMATELY 5PSI & RT PACK TO APPROX 3 .5 PSI. AIRFOIL ANTI-ICE DUCTING VERIFIED TO BE NOT LEAKING. ACRFT FERRIED TO LAS. DURING FERRY FLT NR 1 CABIN PRESSURE CONTROLLER FAILED AFTER 1 HR OF FLT. LAS MX INSPECTED ALL DUCTING/TUBING ON BOTH PACKS & OPERATED BOTH PACKS. NO FAULTS 2 L 7 2 4F RT 2007041000062 20070410 00062 NE 2007 4 10 ABXA070088 2 20070328 A 7210 717000 GEARBOX DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE LT ENGINE DEFECTIVE A ABXA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 GL 23 943AX 1776 47528 656912 ON CLIMBOUT, LEFT OIL PRESSURE BEGAN TO FLUCTUATE FOLLOWED BY 0.1 QUANTITY AMD A "L OIL PRESS LOW" ANNUNCIATOR LIGHT. E NGINE SECURING CHECKLIST COMPLETED. REPLACED ACCESSORY GEAR BOX IAW P&W JT8D MM 72-60-00. 2 L 7 2 4F 4 F A6WE E2EA 2007041000065 20070410 00065 EU 2007 4 10 USAA070257 1 20070403 A 5320 SILL AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 174US 1492 FR 66 SILL BEAM UPPER SURFACE HAS CORROSION. INSTALLED TWO BATH TUB FITTINGS PER SRM 53-41-14, DEFECT SIZE: 2"W X .075 "D. 2 L 7 2 4F RT A28NM 2007041000066 20070410 00066 EU 2007 4 10 USAA070256 1 20070403 A 5320 D53480020697 SHEAR WEB AIRBUS A321 A321211 3930370 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 174US 1492 SHEAR WEB TRAY FR 68 & 69 ATTACHING TO Y -1162 HAS CRACK. FABRICATED TRAY & INSTALLED PER SRM 51-31-00 & 51-72-11, DEFE CT SIZE: 2 INCHES. 2 L 7 2 4F RT A28NM 2007041000069 20070410 00069 NM 2007 4 10 QXEA200700517 1 20070406 A 3097 697071272 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM PROP DE ICE BROKEN A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 414QX 4061 FLIGHT NR 2329: PROP DEICE CAUTION LIGHT ILLUMINATES CONCURRENT WITH RIGHT SIDE PROP DEICE ADVISORY LIGHT ILLUMINATING. AIRCRAFT WAS DIVERTED TO PDX. MAINTENANCE REPLACED BROKEN HARNESS ON NR 2 PROP, NR 3 BLADE PER Q400 MM 61-10-06-000-8 05 AND 61-10-400-805. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007041000075 20070410 00075 NM 2007 4 10 DLM88070294 1 20070405 A 5512 SKIN PANEL DOUG MD88 MD88 3023688 NM HORIZONTAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 P234AP FOUND CRACK, HORIZONTAL STAB UPPER SKIN SPLICE, RT. 2 L 7 2 4F RT A6WE 2007041000079 20070410 00079 NM 2007 4 10 DL76G070299 1 20070405 A 5315 BAC1505101303 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 346 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 154DL 25241 BS 346 RBL 38 TO 45 FLOORBEAM FOUND CORRODED AND REPAIRED AS PER DRD53-00-51D FIG 201. 2 L 7 2 4F RT A1NM 2007041000081 20070410 00081 2007 4 10 BA07003 4 20070403 A 3140 96154570510X COMPUTER AIRBUS 330 A330323 3930335 EU DMC FAULTED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 275AY 29982 88 0370 FLIGHT 718, PHL-FCO: AT CRUISE, ENGINE PAGE DISPLAYED ON CAPTAINS NAV DISPLAY PANEL. SELECTED DMC 3 AND NR 1 DMC FAULT DISPLAYED. RESET NR 1 DMC AND PROBLEM CLEARED. RETURNED TO PHL. MAINTENANCE REPLACED THE NR 1 DMC. NO FURTHER FAULT S. 2 L 7 2 4F RT A46NM 2007041000083 20070410 00083 SO 2007 4 10 C2XA07IA077 1 20070402 A 4900 APU EMB 145 EMB145LR 3260212 SO ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 22909 145459 STL - FLIGHT 3153, DURING PREFLIGHT INSPECTION THE CREW REPORTED A SMOKEY ODOR IN THE GALLEY. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE APU ON MEL 49-00-00 CAT C CONTROL 118810, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 10-9-07 ON 04/05/07 CLE MAINTENANCE REMOVED AND REPLACED THE APU BLEED AIR VALE, OPERATIONALLY CHECKED WITH NO DEFECT S, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE 2 L 7 2 4T RT T00011AT 2007041000088 20070410 00088 NM 2007 4 10 SWAA071733 1 20070404 A 5313 6551698 STRINGER SPLICE BOEING 737 7373Y0 1384671 NM BS 727 S23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 727, STR 23L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007041000096 20070410 00096 SO 2007 4 10 SIMA200709612 1 20070403 A 5347 14532606017 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 703MR 15867 4800 145173 LEFT WALL SEAT TRACK CORRODED BETWEEN FRAME 47 AND FRAME 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RET URNED AIRCRAFT TO SERVICE 2 L 7 2 4F RT T00011AT 2007041000099 20070410 00099 SO 2007 4 10 SIMA200709614 1 20070403 A 5347 14530659007 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 703MR 15867 4800 145173 LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAME 47 AND FRAME 53. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-01-06. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041000100 20070410 00100 SO 2007 4 10 SIMA200709611 1 20070403 A 5347 13500439005 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 703MR 15867 4800 145173 FOUND LEFT SEAT TRACK CORRODED BETWEEN FRAME 18 AND FRAME 23. REMOVED AND REPLACED SEAT TRACK IAW EMB SRM 53-01-06. AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041000103 20070410 00103 SO 2007 4 10 SIMA200709601 1 20070403 A 5347 14530659005 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 703MR 15867 4800 145173 LEFT INBOARD SEAT TRACK CORRODED AT FRAME 36 TO FRAME 47. REMOVED AND REPLACED SEAT TRACK IAW EMB SRM53-01-06. RETURNE D AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041000121 20070410 00121 NM 2007 4 10 UIEA200700143 1 20070323 A 7830 FAIRING BOEING 747 74747UF 1384949 NM THRUST REVERSER MISSING A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523 21782 DURING WALK AROUND, FOUND NR 2 ENGINE INBOARD UPPER T/REV TRACK FAIRING MISSING. MISSING PIECE MEASURES- 17"X 4". TRAN SFERRED TO DMI M07-066 IAW CDL 78-32-02. 2 L 7 4 4F RT 1384945 2007041000140 20070410 00140 NM 2007 4 10 UPS07M49515 1 20070121 A 5313 AEA0407 LONGERON DOUG MD11 MD11F 3023600 NM BS 1381-1401 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C MAIN DECK: FROM BS 1381 TO 1401 LONGERON NR 20R FOUND CORRODED. REMOVED LONGERON 20R FROM BS 1381 TO 1401 PER SRM 51-31-01 V2 R38. FAB NEW LONGERON 20R PER DWG AEA0407 & PROTECTED PER SRM 51-21-01 V2 R38. NEW LONGERON 20R INSTALLED PER SRM 51-31-01 V2 R38. 2 L 7 3 4F RT A22WE 2007041000141 20070410 00141 NM 2007 4 10 UPS07M49516 1 20070126 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM BS 1119 S48R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C FWD CARGO COMPT: FROM BS 1119 BS 6-70, LONGERON 48R FOUND CORRODED. CORRODED LONGERON 48R ATTACHED P ARTS REMOVED FOR ACCESS PER SRM 1-31-01 V2 R38. REPAIR LONGERON & SPLICE FAB PER SRM 53-31-01 V2 R38. REPAIR PARTS REP ROTECTED PER SRM 51-21-01 V2 R38. REPAIR PARTS & ATTACH PARTS REINSTALLED PER SRM 53-10-01 F2 V2 R38. 2 L 7 3 4F RT A22WE 2007041000142 20070410 00142 NM 2007 4 10 UPS07M49524 1 20070118 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1960-1966 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C MAIN DECK: FROM BS 1960 TO 1966, LT MOST O/B SEAT TRACK CROWN & FLANGE AR AREAS CORRODED. REMOVED SE AT TRACK FROM BS 1966 LT MOST O/B PER SRM 51-31-01 V2 R38. RWK NEW SEAT TRACK & PICKED UP HOLES PER SRM 53-70-00 F1 V1 R38. OK TO INSTALL. NEW SEAT TRACK INSTALLED PER SRM 53-70-00 F1 V1 R38. 2 L 7 3 4F RT A22WE 2007041000144 20070410 00144 NM 2007 4 10 USAA070267 1 20070404 A 5311 FRAME BOEING 737 737401 1384701 NM BS 639 S16L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 STA 639 BELOW STR 16L HAS CRACK. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER EA 98542, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007041000146 20070410 00146 NM 2007 4 10 USAA070265 1 20070404 A 5320 WEB BOEING 737 737401 1384701 NM BS 787 S23-24R CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 STA 787 S23R & S24R HAS CORROSION. FAB'D NEW WEB PER DWG 65-61329, SRM 51-40-02; CORR TASK C53-202-01, LEVEL 2, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007041000152 20070410 00152 NM 2007 4 10 KCSA071115 1 20070404 A 5315 FLOORBEAM BOEING 747 747236B 1384804 NM BS 600 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 UPPER DECK FLOORBEAM AT STA 600 HAS DAMAGE TO UPPER CHORD AT LBL 39 WL 308. 2 L 7 4 4F A20WE 2007041000153 20070410 00153 NM 2007 4 10 KCSA071104 1 20070331 A 5315 FLOORBEAM BOEING 747 747236B 1384804 NM BS 540 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 UPPER DECK FLOORBEAM UPPER CHORD IS CORRODED AT STA 540, RBL 16. 2 L 7 4 4F A20WE 2007041000154 20070410 00154 NM 2007 4 10 KCSA071112 1 20070404 A 5330 SKIN BOEING 747 747236B 1384804 NM BS 2170 S23L DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 FUSELAGE SKIN DENTED ST BS 2170, STR 23L. 2 L 7 4 4F A20WE 2007041000160 20070410 00160 EA 2007 4 10 TRAX200700444 1 20070331 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 836AS 7263 AFT FOUR FLOOR LEVEL EMERGENCY LIGHTS INOP. 2 L 7 2 4F RT A21EA 2007041000161 20070410 00161 NM 2007 4 10 KCSA077106 1 20070402 A 5347 SEAT TRACK BOEING 747 747236B 1384804 NM BS 1870 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 MAIN DECK SEAT TRACK DAMAGED AT LUG AT BS 1870, LBL 33. 2 L 7 4 4F A20WE 2007041000163 20070410 00163 NM 2007 4 10 KCSA071107 1 20070402 A 5411 RIB BOEING 747 747236B 1384804 NM NR 2 NACELLE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 NR 2 PYLON RIB AT NAC STA 209 HAS ELONGATED FASTENER HOLE. 2 L 7 4 4F A20WE 2007041000165 20070410 00165 NM 2007 4 10 KCSA071109 1 20070402 A 5340 FITTING BOEING 747 747236B 1384804 NM BS 1241 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 RIGHT UPPER WING TO BODY KICK FITTING AT STA 1241 HAS CORROSION AROUND FASTENER HOLES. 2 L 7 4 4F A20WE 2007041000169 20070410 00169 WP 2007 4 10 07FDEA01322 1 20070404 A 5310 BEAM DOUG DC10 DC1010 3022110 WP BS 1099 S43L CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 FOUND CORROSION WITH EXFOLIATION ON BEAM AT STA 1099 LONGERON 43 LT. REPAIRED BEAM IAW SRM 53-60-01 FIGURE 3 VOL 1. 2 L 7 3 4F A22WE 2007041000172 20070410 00172 WP 2007 4 10 07FDEA01325 1 20070404 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP BS 1119 BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 FOUND A STRUT OF BULKHEAD BROKEN. REPAIRED STRUT IAW SRM 53-00-01 FIGURE 2 SHT 2 VOL 1. 2 L 7 3 4F A22WE 2007041000173 20070410 00173 NM 2007 4 10 07FDEA01327 1 20070404 A 5730 65162238 SKIN BOEING 727 727225 1384077 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 RT WING LEADING EDGE UPPER SURFACE CUTOUT AT NR 5 SLAT INBD GUIDE IS GOUGED AND CRACKED AT AFT EDGE REMOVED SLAT SEALS A ND COVER FOR ACCESS, DAMAGE REMOVED REF SRM 57-30-2. HFEC FOR CRACKS REF B727 NDT MANUAL PART 6. FABRICATED PART AND I NSTALLED REPAIR REF SRM 57-30-4 PG 26. REINSTALLED SLAT SEALS AND COVER REF SRM 51-30-02 PG 1. 2 L 7 3 4F A3WE 2007041000174 20070410 00174 WP 2007 4 10 07FDEA01329 1 20070404 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 959 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 EXTERNAL FUSELAGE SKIN DAMAGED CUT OUT AFT JAMB LOWER FWD CARGO DOOR. REPAIRED SKIN IAW SRM 53-20-00 FIGURE 6 SHT 3-6 V OL 1. 2 L 7 3 4F A22WE 2007041000175 20070410 00175 NM 2007 4 10 TAMF20070002S 1 20070406 A 5350 WEB BOEING 767 767200 1385120 NM GE CF6 CF680 30025 NE WING FAIRING CRACKED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 769QT 23801 DURING INSPECTION CHECK WAS FOUND A CRACK AT AFT WING FAIRING WEB STA 1080 BL 62-70-LT. DAMAGED AREA WAS REPAIRED IAW EW O 767 53-035 AND MFG SERVICE REQUEST 1-311853573. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUED APP ROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007041000176 20070410 00176 NM 2007 4 10 07FDEA01331 1 20070404 A 5320 SPLICE BOEING 727 727225 1384077 NM BS 1178 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 AFT PIT STR -30 APPROX STA 1178 EXFOLIATED. REMOVED AND REPLACED SPLICE IAW 51-30-2. 2 L 7 3 4F A3WE 2007041000177 20070410 00177 SO 2007 4 10 SIMA200709406 1 20070402 A 7500 14531227404 DUCT EMB 145 EMB145LR 3260212 SO ZONE 400 LEAKING A SIMA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 619AE 17889 145101 RECEIVED LAVATORY SMOKE INDICATION WITH BLEEDS ON, PACKS CLOSED AND APU OFF, SMOKE WAS NOTICED FROM PSU GASPERS. CIRCUI T BREAKERS PULLED PER AIRCRAFT OPERATING MANUAL AND SMOKE AND SMELL DISAPPEARED. RETURNED TO JFK. REMOVED AND REPLACED RIGHT HAND ENGINE DUCT ASSEMBLY IAW EMB AMM 36-11-00. OPERATIONAL CHECK GOOD WITH NO SMOKE NOTED - PERFORMED FUNCTIONAL CHECK FLIGHT. RETURNED AIRCRAFT TO SERVICE 2 L 7 2 4T RT T00011AT 2007041100010 20070411 00010 WP 2007 4 11 07FDEA01335 1 20070404 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP BS 573 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 RT AIR COND COMPT CRACK 1" LONG ON VERTICAL BULKHEAD. REPAIRED WEB IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1. 2 L 7 3 4F A22WE 2007041100018 20070411 00018 EA 2007 4 11 A6WA200740180 1 20070401 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 457AW 7854 PASSENGER DOOR AFT DRAG ANGLE CRACKED APPROX 1.5 INCH LONG. (K) [SUP 05-09-07] MAINTENANCE CUTOUT DAMAGED SECTION AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R-53-11-513 REV A. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041100019 20070411 00019 EA 2007 4 11 A6WA200740172 1 20070402 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 451AW 7832 RT FS 621.00 FLOOR SUPPORT ANGLE CRACKED APPROX .5 INCH LONG. (K) [SUP 5-1-07] MAINTENANCE REMOVED DAMAGED SECTION OF THE RIGHT FLOOR SUPPORT ANGLE AT FS 621 AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R-53-61-117. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041200001 20070412 00001 NM 2007 4 12 2007UALA01051 1 20070405 A 3350 1317 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 34C BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 781UA 26945 FOUND EEL LIGHT AT 34C BROKEN. REPLACED EEL LIGHT AT 34C. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007041200004 20070412 00004 EA 2007 4 12 A6WA200740168 1 20070402 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 451AW 7832 RT FS 484.0 ANGLE CRACKED APPROX .1 INCH LONG AT PRESSURE FLOORBEAM RBL 27.0. (K) [SUP 5-1-07] MAINTENANCE REMOVED CR ACKED ANGLE AT FS 484 RBL 27 ON THE PRESSURE FLOORBEAM AND INSTALLED A NEW SERVICEABLE ANGLE P/N 601R31171-9 IAW CRJ 200 SRM 51-42-06 AND 51-42-13. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041200005 20070412 00005 EU 2007 4 12 YENA2007021 1 20070402 A 2720 RUDDER AIRBUS 320 A320232 3930326 EU MALFUNCTIONED A YENA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 15 652JB 3039 FLIGHT 727, JFK-BQN, ON CLIMBOUT IN STRAIGHT FLIGHT THE A/C HAD TO HOLD 5 DEGREES LEFT BANK TO MAINTAIN HEADING. SAME O N AUTOPILOT OR HAND FLYING. AFTER 20 MINUTES AND SLOWING DOWN AUTOPILOT WAS ABLE TO FLY WINGS LEVEL BY TRIMMING L 3.3 D EGREES. AIRCRAFT RETURN TO JFK, RE-INDEXED ELECTRIC ZERO "0" ON RUDDER TRIM ACTUATOR (10CC) IAW AMM 27-22-51-04. ALL I NDICATIONS ARE NOW NORMAL, FUNCTIONAL TEST GOOD. OK TO CONTINUE SERVICE. 2 L 7 2 4F RT A28NM 2007041200007 20070412 00007 NM 2007 4 12 2007UALA01039 1 20070405 A 5310 ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU DOOR FRAME WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 RIGHT AC BAY OPENING O/B ANGLE WORN FROM DOOR LATCH PADS LOCATED 12 INCHES FROM FWD END AND 21 INCHES, 46 INCHES, 53 INC HES FROM AFT EDGE. *S/D* MAJOR REPAIR: BLENDED WORN AREAS SMOOTH, ROTO PEENED AND INSTALLED A FILLER PER AAR EAI07217 IR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041200008 20070412 00008 NM 2007 4 12 2007UALA01040 1 20070405 A 5551 ATTACH FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZONTAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 RIGHT HORIZONTAL FWD LUG LOWER CENTER SECTION CORRODED. MAJOR REPAIR: REMOVED CORROSION, FABRICATED AND INSTALLED NEW BUSHING. REFERENCE AAR EA I070224IR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041200010 20070412 00010 NM 2007 4 12 2007UALA01042 1 20070405 A 5320 WEB BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 294 S7L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 PASSENGER CABIN AT FWD ENTRY DOOR STR 7L STA 294.5 CRACK IN FWD CORNER OF WEB. MAJOR REPAIR: REMOVED DAMAGE, INSTALLED NEW WEB. REFERENCE AAR EAI070215 REV IR AND UA-EVA-70168. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041200011 20070412 00011 NM 2007 4 12 2007UALA01043 1 20070405 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 294 S11L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 FWD ENTRY DOOR FWD SURROUND, WEB CRACKED FRAME BS 294 STR 11. MAJOR REPAIR: REMOVED AND REPLACED SHEAR TIE WEB AT 11L STA 294.5. REFERENCE AAR EAI070215 REV IR AND UA-EVA-70168. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041200013 20070412 00013 NE 2007 4 12 2007UALA01045 2 20070405 A 7261 ENGINE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 OVERSERVICED A UALA O OTHER W K J INADEQUATE Q C FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 214UA 30220 NR 1 ENGINE HIGH OIL CONSUMPTION AND REPORTS OF OIL LEAKS UNDER COWLING IN THE VICINITY OF THE HIGH STAGE BLEED VALVE. [SUP 5-1-07] NO LEAKS DISCOVERED OR EXCESSIVE OIL ON COWLING. ENGINE OVERSERVICED AT GATE AFTER COOLDOWN. OIL CONSUMPT ION NORMAL; RETURNED TO ETOPS SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007041200014 20070412 00014 NM 2007 4 12 2007UALA01046 1 20070406 A 5350 SEAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU WING TO BODY DAMAGED A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 370UA 24539 NOTICEABLE HI FREQUENCY LO AMPLITUDE VIBRATION DURING CLIMB. REPLACED BLADE SEAL AND RESEALED BODY WING FAIRING. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041200015 20070412 00015 NM 2007 4 12 2007UALA01047 1 20070406 A 3350 BR964422 LAMP AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 848UA 1647 SEAT 18C EEL EVACUATION LIGHT HAS 1 LAMP INOP OF 2. REPLACED LAMP ASSY, OPS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041200016 20070412 00016 NM 2007 4 12 2007UALA01048 1 20070406 A 3350 COVER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 848UA 1647 SEAT 14C EEL EVACUATION LIGHT LENS BROKE OFF SHROUD. *S/D* REPLACED LENS COVER. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041200017 20070412 00017 NM 2007 4 12 2007UALA01049 1 20070406 A 2120 COFFEEMAKER BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU GALLEY CONTAMINATED A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 935UA 26663 BURNING PLASTIC ODOR REPORTED BY CREW FROM THE FIRST CLASS GALLEY. CAUSED BY FOUND PLASTIC MELTED ON COFFEE BURNER. CL EANED BURNER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041200021 20070412 00021 SO 2007 4 12 C2XA07IA080 1 20070406 A 2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO CARGO BAY FALSE ACTIVATION A C2XA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 27 14959 145091 HRL - FLIGHT 3124, THE CREW REPORTED A BAGGAGE SMOKE INDICATION ON EICAS. THE CREW INSPECTED THE AIRCRAFT AND PLACED TH E BAGGAGE SMOKE DETECTOR ON MEL 26-15-00 CAT-C CTL 119255, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIR CRAFT LANDED AT IAH WITHOUT INCIDENT FROM HRL, WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE BAGGA GE SMOKE DETECTORS WITH NO DEFECTS NOT, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007041200022 20070412 00022 SO 2007 4 12 C2XA07IA081 1 20070406 A 2820 2810051104 VALVE EMB 145 EMB145XR 3260214 SO FUEL VENT LEAKING A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 27 13161 8039 8039 14500805 MCI - FLIGHT 11, THE CREW REPORTED THAT ON TAKEOFF FROM MCI, ATC AND ANOTHER AIRCRAFT REPORTED VISUALLY SIGNIFICANT FUEL LEAKING FROM THE RIGHT WING. THE AIRCRAFT RETURNED TO MCI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND R EPLACED THE RIGHT HAND VENT VALVE, AND RIGHT HAND FLOAT VENT VALVE, LEAK & OPERATIONAL CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007041200023 20070412 00023 SO 2007 4 12 C2XA07IA082 1 20070406 A 2820 2930015101 FLOAT EMB 145 EMB145XR 3260214 SO VENT VALVE LEAKING A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 27 13161 8039 8039 14500805 MCI - FLIGHT 11, THE CREW REPORTED THAT ON TAKEOFF FROM MCI, ATC AND ANOTHER AIRCRAFT REPORTED VISUALLY SIGNIFICANT FUEL LEAKING FROM THE RIGHT WING. THE AIRCRAFT RETURNED TO MCI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND R EPLACED THE RIGHT HAND VENT VALVE, AND RIGHT HAND FLOAT VENT VALVE, LEAK & OPERATIONAL CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007041200030 20070412 00030 NM 2007 4 12 SPAA0700091 1 20070409 A 3350 110049 POWER SUPPLY BOEING 737 7372T4 1384492 NM PWA JT8 JT8D17 52049 NE ZONE 200 INOPERATIVE A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 AFT SECTION OF FLOORTRACK ESCAPE PATH LIGHTING INOP. REPLACED BATTERY POWER SUPPLY AND FUNCTIONAL CHECK SATISFACTORY IAW CMM 33-21-27. 2 L 7 2 4F 4 F A16WE E2EA 2007041200032 20070412 00032 EA 2007 4 12 QXEA200700523 1 20070408 A 2840 73811812 COMPUTER CNDAIR CL600 CL6002C10 1390015 EA FUEL QTY MALFUNCTIONED A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 614QX 1686 10049 PDX - FLIGHT 2565 - RECEIVED A XFLOW PUMP CAUTION MESSAGE AFTER XFLOW OVERRIDE SELECTED (NO CROSS FLOW ACTIVE). RESET S YSTEM WITH NO HELP. RETURNED TO THE GATE. MAINTENANCE REPLACED THE FUEL QUANTITY GAUGING COMPUTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007041200036 20070412 00036 EA 2007 4 12 COMA0760301 1 20070404 A 7500 20035008067 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA BLEED AIR SYS FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 914CA 13026 7012 FLIGHT 5349 - RECEIVED ANTI-ICE DUCT WARNING DURING CLIMB WITH WING AND COWL ANTI-ICE ON. REPLACED BLEED AIR LEAK CONTR OL UNIT. PERFORMED OPS CHECKS, NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007041200037 20070412 00037 EA 2007 4 12 A6WA200740173 1 20070330 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 457AW 7854 WING PLANK AT WS 54.897 HAS SEVERAL PITS ON AFT EDGE THE DEEPEST IS .005 INCH. (K) [SUP 05-01-07] MAINTENANCE REMOVED CORROSION AND REPAIRED AREA IAW REO 601R-57-21-030. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041200038 20070412 00038 NM 2007 4 12 QXEA200700544 1 20070309 A 5754 BRACKET DHAV DHC8 DHC8202 2809007 NM RT WING LE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - RIGHT LEADING EDGE BRACKET CRACKED AT YW138.00. REPAIRED IAW SRM 51-40-11 AND 51-40-00. 2 H 7 2 4T RT A13NM 2007041200042 20070412 00042 EU 2007 4 12 UPS07149605 1 20070404 A 5330 SKIN AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 169UP 0864 SEVERAL DENTS NEAR TAIL STAND BALL. THREE EACH DENTS/GOUGES 2 FWD OF TAIL BALL, 1 AFT OF TAIL BALL ARE BLENDED & SKIN T HICKNESS MEASURED. ALL ARE WITHIN REPAIR CATEGORY -C- OF SRM 53-10-12 PG 111/112. REPAIR DUE WITHIN 50 FLT CYCLES. TH REE GOUGES HAVE BEEN DRESSED OUT. [SUP 05-07-07] REMOVED BALL FITTING AT FRAME 85. REMOVED FASTENERS FOR REPAIR. REF A 300 S/M 53-10-12 200 PG BLK. TRANSFERRED TO ECA 010948. THIS ITEM CLEARED AT THIS TIME. SEE ECA'S 010948 AND 010949 FO R WORK ACCOMPLISHED. 2 L 7 2 4F RT A35EU 2007041200043 20070412 00043 EU 2007 4 12 UPS07149606 1 20070404 A 5330 FITTING AIRBUS A300 A300F4622R 3930360 EU FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 169UP 0864 INSPECTION TYPE:N/A THE TAIL BALL FITTING HAS A 1 INCH BY .015 X .050 AREA THAT WAS GOUGED THEN BLENDED. REPAIRED AREA PER EO A300-5330-26511-A. 2 L 7 2 4F RT A35EU 2007041200045 20070412 00045 NM 2007 4 12 UPS07M49601 1 20070305 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM BS 1119 L52 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:C FWD CARGO BILGE AREA STA 1119 LONGERON 52 FOUND WITH CORROSION. FWD CARGO LONG 52 STA 1119 AREA SPLIC E REMOVED & LONG 52 STA 1109 TO STA 6-0 6 AREA FASTENERS REMOVED. FWD CARGO LONG 52 DAMAGED AREA TRIMMED. HFEC INSP CA RRIED OUT, NO CRACK EVIDENT. LONG REPAIR SECTION & SPLICE FAB. FPI CARRIED ON FAB LONG & SPLICE NO CRACK EVIDENT. REP AIR SECTION & SPLICE PAINTED. LONG REPAIR SECTION & SPLICE INSTALLED PER SRM 51-31-01 VOL II REV 38. 2 L 7 3 4F RT A22WE 2007041200046 20070412 00046 NM 2007 4 12 UPS07M49603 1 20070407 A 3350 LIGHT DOUG MD11 MD11F 3023600 NM EMERGENCY EXIT DISLODGED A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 252UP 48768 RIGHT ENTRY EMERGENCY EXIT LIGHT FELL OFF. REINSTALLED RIGHT ENTRY EMERGENCY EXIT LIGHT PER 33-52-05-2. EMERGENCY EXIT LIGHTS OPS CHECK GOOD. 2 L 7 3 4F RT A22WE 2007041200052 20070412 00052 EU 2007 4 12 07FDEA00829 1 20070314 A 5753 A57970100027 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 DELAMINATED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 OLD DELAMINATION REPAIR ON INBOARD FLAP RT UPPER SURFACE AT TRAILING EDGE. REPAIR PERFORMED BY REPLACING THE EXISTING R EPAIR IAW SRM 57-53-12/FIG 209 APPROVED BY EA 6-5752-103367 AND RAS/DABRE/7007093/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007041200055 20070412 00055 NM 2007 4 12 07FDEA01366 1 20070406 A 5330 6554574 SKIN BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 EXT FUSELAGE BS 420 S-4R 2 PAIRS OF OVERLAPPPING RIVET HEADS AND SEVERAL RIVETS CLOSELY SPACED REMOVED 9 G NET ATTACH ST RUCTURE BETWEEN S-4R AND S-5R CUT OUT DAMAGED AREA. FABRICATED REPAIR FILL AND REPAIR DOUBLER AND INSTALLED. REFERENCE EA NR 7-5330-106995 (REVISION DATE 16 MAR 2007). 2 L 7 3 4F A3WE 2007041200056 20070412 00056 NM 2007 4 12 07FDEA01367 1 20070406 A 5320 65561751 THRESHOLD BOEING 727 727225 1384077 NM BS 950E-990 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 AFT LOWER CARGO PIT DOOR CUTOUT THRESHOLD HAS 2 CRACKS IN CURVED AREA BETWEEN 27" AND 32" AFT OF FWD EDGE WELD ACCOMPL ISHED ON SHOP N/R 11841-8300-0001. VERIFIED MATERIAL WELDED AND SMOOTHED AREA REFERENCE FED EX DWG SR27-53-025C. 2 L 7 3 4F A3WE 2007041200058 20070412 00058 NM 2007 4 12 07FDEA01369 1 20070406 A 5320 65575504 CHANNEL BOEING 727 727225 1384077 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 AFT CARGO PIT RT "Z" CHANNEL CRACKED AT RIVET HEAD AT STA 1040 FRAME REPLACED Z-ANGLE REF SRM 51-30-2. 2 L 7 3 4F A3WE 2007041200059 20070412 00059 NM 2007 4 12 07FDEA01370 1 20070406 A 5755 6521658 ANGLE BOEING 727 727225 1384077 NM NR 12 SPOILER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 RT WING, TE LOWER PANEL, BELOW NR 12 SPOILER PANEL, OTBD ATTACH ANGLE, OF THE OTBD SET IS CRACKED AT SUPPORT ROD. REMOV ED DAMAGE ANGLE, VERIFIED REPAIR MATERIAL AS 7075-T6 .050 REF IPC 57-30-00 FIG 16 AND DWG 65-21658. FABRICATED REPLACEM ENT ANGLE REF FED EX GMM 7-0-1001 ITEM 7C AND SRM 51-41-2. TREATED REF 727 SRM 51-10-2 PG 7G, AND PRIMED REF 727 AMM 51 -20-151-7 ITEMS 5 AND 6. INSTALLED REPLACEMENT PART REF 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007041200062 20070412 00062 2007 4 12 YENA2007020 4 20070328 A 2330 3042865102 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU LIVE TV FAULTY A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 EA 15 623JB 10782 2504 FLT 489, BOS TO LGB, APROX 2015Z, ON LANDING TV/SCREEN AT SEAT 10C SMOKING WITH THE SMELL OF BURNED WIRE. LIVE TV SYS S HUTDOWN. ACCOMPLISHED TSM TAS 23-39-00-810-801. FOUND VDU AT SEAT 10C SCREEN BLACK NO DISPLAY. REMOVED AND REPLACED V DU AT 10C IAW AMM 23-39-00 AND FOUND SLIGHT DISTORTION IN DISPLAYED VIDEO. REMOVED AND REPLACED SEB AT 10C OER AMM 23-3 9-00. VDU 10C OPERATES NORMAL. OPERATED SYSTEM FOR 2 HOURS. NO FURTHER DEFECTS NOTED. 2 L 7 2 4F RT A28NM 2007041200063 20070412 00063 EA 2007 4 12 A6WA200740088 1 20070228 A 5320 6013501252 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FS 621-625 S14R CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 453AW 7838 RT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX 1.2 INCH LONG. MAINTENANCE REPLACED INTERCOSTAL PN 601-35012-52 IAW SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041200064 20070412 00064 NM 2007 4 12 KCSA071101 1 20070330 A 5347 SEAT TRACK BOEING 747 747236B 1384804 NM BS 530-565 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 CORROSION ON SEAT TRACK RBL-9 STA-530 STA-565 WL-308. 2 L 7 4 4F A20WE 2007041200065 20070412 00065 NM 2007 4 12 KCSA071102 1 20070330 A 5347 SEAT TRACK BOEING 747 747236B 1384804 NM BS 550 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 CORROSION ON SEAT TRACK LBL-66 STA-550 WL-308. 2 L 7 4 4F A20WE 2007041200066 20070412 00066 NM 2007 4 12 KCSA071103 1 20070330 A 5347 SEAT TRACK BOEING 747 747236B 1384804 NM BS 480-500 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 CORROSION ON SEAT TRACK RBL-47 STA-480 TO 500 WL-308. 2 L 7 4 4F A20WE 2007041200067 20070412 00067 SO 2007 4 12 LR7A07015 1 20070401 A 5320 WEB LKHEED 382 382G 526414U SO FS 750 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 376 4763 DURING SCHEDULED A CHECK PER JOB CARD HA1200, FOUND LT SIDE RAMP WEB SKIN GOUGED AND CRACKED BETWEEN RAMP STN 0 AND STN 2 AT FS750, WL146, BL61. REPAIRED RAMP WEB SKIN IAW SMP583 FIG 51-140-12, LOG PAGE 26257 ITEM M1. 2 H 7 4 4T A1SO 2007041200068 20070412 00068 NM 2007 4 12 07FDEA01349 1 20070404 A 5320 65184425 CASTING BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 MAIN DECK 2 RIGHT DOOR CUT OUT UPPER AFT CORNER SEAL DEPRESSOR CASTING IS CRACKED AT BS 1062 WL 271. REMOVED AND DRILLE D UP R2 CORNER SEAL DEPRESSOR CASTING. INSTALLED CASTING REF 51-30-02. 2 L 7 3 4F A3WE 2007041200071 20070412 00071 NM 2007 4 12 07FDEA01353 1 20070405 A 5730 SKIN DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT WING DROOPED LEADING EDGE UPPER SURFACE FOUND CRACKED. [SUP 4-19-07] REMOVED AND REPLACED AS PER AMM 27-80-10. RE PAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007041200072 20070412 00072 NM 2007 4 12 07FDEA01354 1 20070405 A 5330 SKIN DOUG MD11 MD11F 3023600 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 FORWARD CARGO DOOR AFT CUTOUT LOWER SKIN FOUND DENT AND CHAFED. CARRIED OUT REPAIR AS PER SRM 53-50-00 FIGURE 16 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007041200073 20070412 00073 NM 2007 4 12 07FDEA01355 1 20070405 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 CABIN LEFT LONGERON 17 FOUND CRACKED AT STA 1239. 4-18-07, REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPA IR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007041200078 20070412 00078 EU 2007 4 12 07FDEA01360 1 20070405 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 FWD LOWER CARGO COMPARTMENT FLOOR SUPPORT IS CRACK LT SIDE OF FS 38.2 BETWEEN CL TO LBL 24". CRACK LENGTH .5 " CRACK LE NGTH WOULD NOT ALLOW TO SUBMIT SDR WHEN ENTERED ON BLOCK 7C. REMOVED FLOOR SUPPORT IAW SRM 51-40-44. FABBED NEW SUPPOR T, LOCATED AND DRILLED IAW SRM 51-40-44. INSTALLED FLOOR SUPPORT IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007041200079 20070412 00079 WP 2007 4 12 07FDEA01278 1 20070403 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP BS 547 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 LT AIR COND COMPT FOUND CRACK 1.5" ON HORIZONTAL ANGLE AT STA 547. REPAIRED JAMB IAW SRM 53-00-01 FIG 8 SHT 2 VOL 1. 2 L 7 3 4F A22WE 2007041200081 20070412 00081 NM 2007 4 12 WRLA2007054 1 20070405 A 2120 UNKNOWN DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE CABIN SMOKE A WRLA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 11 803DE 48474 LAD/IAH AIR TURNBACK DUE TO FLIGHT CABIN CREW REPORTED ELECTRICAL SMOKE AFT OF L2 DOOR LT SIDE ROW 15AV CABINET, F/A'S I SOLATED ELECTRICAL AND ALL SMOKE DISSIPATED. RAN CHECKLIST AND RETURNED TO FNLU. AFTER DOING A SEARCH OF THE SUSPECTED AREA OF CABIN FROM ROWS 13 FWD OF 15 AND AFT TO ROW 38 A&B, REMOVED ALL CEILING PANELS, READING LIGHTS PANELS, REMOVED VIDEO CONTROL UNIT. RAN MUX SYSTEM TEST ALL SYSTEM TESTS PASSED. CHECKED ALL C/B'S, NONE POPPED, COULD NOT FIND ANYTHI NG THAT COULD HAVE CAUSED THE ODOR. THERE ARE NO WIRES THAT LOOKED BURNED. TURNED ON EVERYTHING THE CREW REPORTED WAS ON WHEN THE PROBLEM HAPPENED, COULD NOT DUPLICATE THE PROBLEM ON THE GROUND. 2 L 7 3 4F 4 F RT A22WE E24NE 2007041200085 20070412 00085 EA 2007 4 12 A6WA200740170 1 20070402 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 451AW 7832 LT FS 484.0 INTERCOSTAL CRACKED APPROX .1 INCH LONG AT PRESSURE FLOORBEAM LBL 36.0. (K) [SUP 05-01-07] MAINTENANCE CU T OUT DAMAGED SECTION OF INTERCOSTAL AT FS 484 LBL 36 AT THE PRESSURE FLOOR SUPPORT BEAM FABBED AND INSTALLED NEW ANGLE IAW BOMBARDIER REO 601R-53-41-059 AND BSC SR 601R-53-0030A. (M) 2 L 7 2 4F RT A21EA 2007041200086 20070412 00086 EA 2007 4 12 A6WA200740171 1 20070402 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 451AW 7832 RT FS 484.0 INTERCOSTAL CRACKED APPROX .1 INCH LONG AT PRESSURE FLOORBEAM RBL 36.0. (K) [SUP 5-1-07] MAINTENANCE CUT AW AY DAMAGED ATTACHMENT FLANGE FABRICATED ANGLE FROM S6144-14 AND INSTALLED ANGLE IAW BOMBARDIER REO 601R-53-41-059A AND B SC SR 601R-53-0030A. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041200087 20070412 00087 EU 2007 4 12 07FDEA01361 1 20070405 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 FORWARD LOWER CARGO COMPARTMENT STRINGER HAS CORROSION STR 48R FR 38.2 BILGE AREA. REMOVED CORROSION IAW SRM 51-10-10 F OUND TO BE OUT OF LIMITS IAW SRM 53-14-14. REMOVED STRINGER REINFORCEMENT SUPPORT IAW SRM 51-40-21. FABBED NEW REINFOR CEMENT SUPPORT IAW SRM 53-14-14 AND SRM 51-40-44 LOCATED AND DRILLED ON MAE TRAV T7/671547. INSTALLED STR 48R REINFORCE MENT SUPPORT IAW SRM 51-40-20. 2 L 7 2 4F RT A35EU 2007041200088 20070412 00088 WP 2007 4 12 ARWA20070304 1 20070322 A 3040 NBBA6045502 WINDSHIELD DOUG DC10 DC1010 3022110 WP COCKPIT CRACKED A ARWA O OTHER O OTHER CR CRUISE 1 SO 19 68041 46900 DURING CRUISE RT WINDSHIELD CRACKED. REMOVED AND REPLACED RT WINDSHIELD PANEL IN ACCORDANCE WITH M/M 56-11-00. OPERATI ONAL CHECK PERFORMED IN ACCORDANCE WITH M/M 30-41-00 AND M/M 30-42-00, FOUND NORMAL OPERATION. 2 L 7 3 4F A22WE 2007041200093 20070412 00093 NE 2007 4 12 MWEA070081 2 20070408 A 7320 8061965 FMU BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE LT ENGINE INOPERATIVE A MWEA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 GL 13 920ME 55182 LEFT ENGINE INDICATED VERY LOW PERFORMANCE READINGS, LEFT PRESSURIZATION SYSTEM ALSO SHUT DOWN. REMOVED AND REPLACED FU EL METERING UNIT. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007041200099 20070412 00099 SO 2007 4 12 RAIA00703072 1 20070327 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 845HK 14500842 POST FLT NR 7886 - IAD - EMERGENCY LIGHT AT MAIN DOOR FLOOD LIGHT IS INOP. MAINTENANCE REPLACED LAMP AT MAIN DOOR, OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007041200102 20070412 00102 SO 2007 4 12 RAIA00703063 1 20070223 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 819HK 145062 PRE FLT NR 5578 - TUL - EMERGENCY LIGHT AT AFT SIDE AFT CEILING EXIT LOCATOR OUT. MAINTENANCE RESECURED CONNECTOR ON EM ERGENCY LIGHT. CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007041200103 20070412 00103 WP 2007 4 12 NWAA071259867 1 20070209 A 5330 SKIN DOUG DC9 DC951 3022051 WP BS 370 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 776NC 47786 DURING "H" CHECK FOUND 1/4" CRACK IN FUSELAGE SKIN AT BS 370 FORWARD CARGO DOOR CUTOUT. REPAIRED PER EA 98-208811. 2 L 7 2 4F RT A6WE 2007041200104 20070412 00104 NM 2007 4 12 HALA0700160 1 20070408 A 2160 ACTUATOR BOEING 767 767300 1385204 NM LT PACK CONTROL MALFUNCTIONED A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 588HA 33466 ETOPS SIGNIFICANT SYSTEM, LEFT PACK TEMP EICAS LIGHT CAME ON. SWITCHED TO STBY "N" LIGHT WENT OUT. PERFORMED BITE CK O N LT PACK TEMP CONTROLLER. FOUND INLET ACT FAULT, VERIFIED AND RESET, MSG CLD. OK FOR SERVICE PER FIM 21-51-00. 2 L 7 2 4F RT A1NM 2007041200105 20070412 00105 NM 2007 4 12 HALA0700161 1 20070409 A 3610 LINE BOEING 767 767300 1385204 NM ENGINE LOOSE A HALA O OTHER O OTHER DE DESCENT 1 WP 13 588HA 33466 ETOPS SIGNIFICANT SYSTEM, L ENG PRV WARNING CAME ON SEVERAL TIMES DURING DESCENT FRM FL 380. TROUBLESHOT PER FIM 36-10- 00 FIG 123. FOUND LOOSE SENSE LINE TO PRE-COOLER. TIGHTENED LINE, RAN ENGINE AND PERFORMED OPERATIONAL TEST OF PRV PER AMM 36-11-18/501. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A1NM 2007041200106 20070412 00106 NM 2007 4 12 HALA0700158 1 20070408 A 3397 CONNECTOR BOEING 767 76733A 1385209 NM EMERGENCY LIGHT DAMAGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 581HA 28141 RIGHT SIDE FIRST CLASS EMERGENCY FLOOR LIGHTS INOP. REPLACED CONNECTOR CHECKS OK. 2 L 7 2 4F RT A1NM 2007041200108 20070412 00108 NE 2007 4 12 HALA0700164 2 20070410 A 7311 21SN04269 PRESSURE SWITCH BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE RT ENGINE UNKNOWN A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 594HA 2836 2836 23275 ETOPS SIGNIFICANT SYSTEM, "R. ENG FUEL FILT" DISPLAYED ON STATUS PAGE. T/S PER FIM 73-11-00 FIG 103, REPLACED FUEL FILT ER PER AMM 73-11-02/401. FOUND FUEL FILTER CLEAN REPLACED DIFFERENTIAL PRESSURE SWITCH PER AMM 73-34-01/401, RAN ENGINE , NO MSG NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007041200110 20070412 00110 NM 2007 4 12 HALA0700162 1 20070407 A 3150 UNKNOWN BOEING 767 767300 1385204 NM LT ENGINE UNKNOWN A HALA O OTHER O OTHER DE DESCENT 1 WP 13 588HA 33466 ETOPS SIGNIFICANT SYSTEM, LT ENG PRV CAUTION EICAS DISPLAYED ON DESCENT DUCT PRESS NORMAL. T/S PER FIM 36-10-00 FIG 123 LT ENG PRV CHECKS GOOD. PERFORMED BITE CHECK OF AIR SYSTEM CONTROLLER. NO FAULTS NOTED. OK FOR CONTINUED SERVICE. 2 L 7 2 4F RT A1NM 2007041200111 20070412 00111 NE 2007 4 12 HALA0700157 2 20070407 A 7300 7300579 FMU BOEING 767 767300 1385204 NM PWA 4060 PW4060 52119 NE ENGINE MALFUNCTIONED A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 586HA 12730 12730 24259 ETOPS SIGNIFICANT SYSTEM, ENG VALVE LIGHT ILLUMNIATED WITH FUEL CONTROL SWITCH IN RUN. T/S USING FIM 73 11 00 NO EICAS MSGS VERIFIED 28 VDC TO FMU SO SOLENOID WDM 76 11 11 BLK 41 REPLACE FMU BLK 3 VERIFIED 300 PSIG FUEL PRESSURE FIM 71 08 00FIG101 REMOVED AND REPLACED NR 2 ENGINE FMU IAW B767 MM 73 21 01 004, NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007041200112 20070412 00112 NM 2007 4 12 QXEA200700526 1 20070409 A 6120 30005000056 TSCU DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER MALFUNCTIONED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 349PH 180 486 PDX AUTO FEATHER ARM SWITCH LIGHT DOES NOT EXTINGUISH, LIGHT FLICKERS ON AND OFF EN ROUTE AND EXTINGUISHES IN DESCENT. REPLACED 6121-K5 RELAY AND NR 1 AND NR 2 TSCU UNITS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007041200113 20070412 00113 SO 2007 4 12 RAIA00703065 1 20070324 A 2750 FLAP SYSTEM EMB 145 EMB145LR 3260212 SO TE FLAPS UNKNOWN A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 814HK 145046 FLT NR 3551 - PIT - FLAP FAIL MESSAGE. MAINTENANCE RESET FLAPS AND PERFORMED OPERATIONAL TEST OF FLAP SYSTEM. OPS CHEC K GOOD AT THIS TIME. 2 L 7 2 4T RT T00011AT 2007040900106 20070409 00106 NM 2007 4 9 UPS07M49591 1 20070402 A 5754 ARB287715 FITTING DOUG MD11 MD11F 3023600 NM SLAT TRACK DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 271UP 48572 INSPECTION TYPE:3C LEFT O/B SLAT TRACK FITTING DAMAGED BY SLAT CABLE BETWEEN 5 & 6 SLATS. REPAIRED DAMAGED AREA IAW SAA EA 011-5710-01-A0765 & UPS RAA MD-11-57-20106. 2 L 7 3 4F RT A22WE 2007040900107 20070409 00107 NM 2007 4 9 QXEA200700511 1 20070325 A 2752 800600M02 ACTUATOR BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS MALFUNCTIONED A QXEA O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 09 424QX 1419 1419 4006 SEA FLIGHT NR 2474: 14 MINUTES INTO CLIMB GOING THROUGH 19000 AT (TEMP -11 DEG C ISA +13 DEG). NR 1 OIL TEMP HIT 108 DE G C FOR ONE MINUTE. BYPASS DOORS WERE CLOSED PER CHECKLIST. AIRCRAFT WAS LEVELED AT 20,000 FT AND NR 1 OIL TEMP DECREA SED UNTIL STEADY AT NR 1 79 DEC AND NR 2 AT 75 DEG. UPON LANDING, NR 1 OIL TEMP WAS 90 DEG AND NR 2 WAS 84 DEG. MAINTE NANCE C/W AMM TASK 05-11-00-992-802. REMOVED AND REPLACED NR 1 OIL COOLER AIR OUTLET FLAP ACTUATOR IAW AMM 79-21-31 PG 401-409. PERFORMED OPS TEST OF THE AIR COOLED OIL COOLER FLAP DOOR ACTUATOR IAW AMM 79-21-31 PG 501-504. OPS CHECK GOO D. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007040900110 20070409 00110 NM 2007 4 9 CALA0700164 1 20070402 A 2612 4739551 CONTROL PANEL BOEING 737 737524 1384721 NM FIRE SUPPRESSION INOPERATIVE A CALA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 33608 27321 THE OVERHEAT DETECT LIGHT ON CAPTAIN'S SIX PACK ILLUMINATED WITH THE AFT CARGO COMPARTMENT AMBER B-LOOP LIGHT ALSO ILLUM INATING ON TAKEOFF FROM IAH. BOTH FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WIT HOUT INCIDENT. MAINTENANCE INSPECTED THE AFT CARGO COMPARTMENT AND FOUND NO EVIDENCE OF FIRE. THE COCKPIT FIRE SUPPRES SION PANEL WAS REPLACED AND TESTED GOOD IAW MM 26-23-10, PAGE 210. IN ADDITION, BOTH FIRE BOTTLES WERE REPLACED. 2 L 7 2 4F RT A16WE 2007040900115 20070409 00115 EA 2007 4 9 QXEA200700513 1 20070402 A 3000 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA ANTI ICE SYS UNKNOWN A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 606QX 10023 DEN - FLIGHT 4203, ON TAXI RECEIVED A "ANTI-ICE DUCT" WARNING. RETURNED TO THE GATE. MAINTENANCE CYCLED THE CIRCUIT BR EAKERS AND PERFORMED A ENGINE RUN WITH ANTI-ICE OPERATING. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS R EPLACED. 2 L 7 2 4F RT A21EA 2007040900116 20070409 00116 EA 2007 4 9 QXEA200700514 1 20070402 A 2520 PANEL CNDAIR CL600 CL6002C10 1390015 EA CABIN UNSECURE A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 601QX 10009 DEN - FLIGHT 4432 - CEILING PANEL AT ROW 10 HANGING DOWN. RETURNED TO THE GATE. MAINTENANCE RESECURED THE PANEL. NO O THER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007040900120 20070409 00120 NM 2007 4 9 QXEANM09404 1 20070313 A 4920 164161100 DRAIN VALVE SUNDSTRANDEM BOMBDR DHC8 DHC8402 1390042 NM APU DAMAGED G QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 BALL ON WRONG SIDE OF SPRING, WHICH ALLOWS IT TO REST IN CLOSED POSITION, NOT ALLOWING PROPER DRAINAGE 2 H 7 2 4T RT A13NM 2007040900122 20070409 00122 NM 2007 4 9 QXEANM09416 1 20070314 A 4920 164161100 DRAIN VALVE BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA APU PLUGGED G QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 416QX 4083 BALL ON WRONG SIDE OF SPRING ALLOWING IMPROPER DRAINAGE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2007040900126 20070409 00126 NM 2007 4 9 HALA0700156 1 20070405 A 2841 TOTALIZER BOEING 767 76733A 1385209 NM COCKPIT INOPERATIVE A HALA D RETURN TO BLOCK P NO WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 583HA 25531 BTB:ETOPS SIGNIFICANT SYSTEM, FMC FUEL TOTALIZER, BLANK. BITE CHECKED FUEL QTY PROCESSOR PER FIM 28-41-00 TABLE 101. F AULTED D1, 25, 75. ALL CLEARED EXCEPT FAULT 75 PERFORMED FUEL TEST PER 28-41-00 FIG 105 CHECKS OK. OK TO CONTINUE. 2 L 7 2 4F RT A1NM 2007040900132 20070409 00132 CE 2007 4 9 DXTA200702089 1 20070407 A 3240 BRAKE ASSY CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MALFUNCTIONED E DXTA K NONE O OTHER IN INSP/MAINT 1 GL 07 958QS 7500158 CARBON LIKE RESIDUE FOUND ON OUTSIDE OF ALL MAIN WHEELS, BRAKES SEEM A LITTLE GRABBY. INSPECTED ALL 4 BRAKE STACK HYD. PUCKS AND WEAR INDICATORS FOUND ALL 4 BRAKES SERVICABLE IAW CESSNA 750 M/M 32-42-01 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007040900133 20070409 00133 CE 2007 4 9 DXTA200702091 1 20070407 A 2150 A/C PACK CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 900QS 7500123 PUNGENT ODOR EMINATING FROM PACS SMELLS MUSTY IN CABIN AND COCKPIT WITH APU ON. REMOVED LT&RT COALESCER CLOTH WITH PAC KING. INSTALLED NEW COALESCER CLOTHS WITH PACKINGS. OPS CHECK GOOD. WORK PERFORMED IN REFERENCE TO CE750 MM CHAPTER 12 -10-01. FOR DETAILS REFER TO FAS WO 07-849. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007040900158 20070409 00158 NM 2007 4 9 USAA070254 1 20070330 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM BS 500B CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 JUST AFT OF BS 500B & S26L HAS CRACK. MFG & INSTALLED NEW INTERCOSTAL PER SRM 51-10-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007041000028 20070410 00028 2007 4 10 C2XA07IA074 2 20070327 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ODOR A C2XA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 27 14950 145061 IAH - FLIGHT 2367, THE CREW REPORTED SMOKE IN THE CABIN AND A LAV SMOKE WARNING AFTER T/O. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, PERFORMED GROUND RUNS AND FOUND THE ODOR TO BE R ESIDUAL OIL. THE AIRCRAFT WAS TEST FLOWN SATISFACTORILY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007041000031 20070410 00031 NM 2007 4 10 BB07031 1 20070330 A 4990 351T030060 APU BOEING 757 757225 1384959 NM LEAKING A USAA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 923UW 56181 2902 22203 FLIGHT 1228, FLL-CLT: DURING FLIGHT, CREW REPORTED AN OVERHEAT ODOR AND THE 2L LAV SMOKE DETECTOR SOUNDING. FLIGHT LAN DED IN CLT WITH NO DIFFICULTIES. MAINTENANCE PLACED THE LEFT PACK ON MEL 21-5101 AND REPLACED THE 2L LAV SMOKE DETECTOR . SUBSEQUENT TROUBLESHOOTING FOUND THAT THE APU HAD AN INTERNAL OIL LEAK, CAUSING CONTAMINATION OF THE AIR DISTRIBUTION SYSTEM. REPLACED APU. NO FURTHER FAULTS. 2 L 7 2 4F RT A2NM 2007041000046 20070410 00046 EA 2007 4 10 TRAX200700458 1 20070404 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 RIGHT OVERWING EMERGENCY EXIT LIGHT HAS SEVERAL INOP BULBS. 2 L 7 2 4F RT A21EA 2007041000064 20070410 00064 NM 2007 4 10 USAA070258 1 20070403 A 5320 143N55227 SUPPORT BOEING 757 7572B7 1384964 NM R2 DOOR CUTOUT B CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 200UU 27809 R2 DOOR CUTOUT BS 720-740 HAS CORROSION. REMOVED, FABRICATED & INSTALLED SUPPORT PER SRM 51-40-02, FIG 3 & 8, DEFECT SI ZE: 3 X 1 INCH. 2 L 7 2 4F RT A2NM 2007041000074 20070410 00074 NM 2007 4 10 DL75A070293 1 20070404 A 2620 33900004 FIRE BOTTLE BOEING 757 757212 1384951 NM APU BAY MALFUNCTIONED A DALA F ACTIVATE FIRE EXT. O OTHER TX TAXI/GRND HDL 1 SO 27 752AT 30712 23128 P234AP APU QUIT ON PUSHBACK AS POWER CORD WAS REMOVED SIMULTANEOUSLY APU FIRE DISCHARGE LIGHT ILLUMINATED. FOUND BOTTLE DISCHAR GED. CHECKING CIRCUITRY FOR UNCOMMANDED BOTTLE DISCHARGE. TESTED OK PER AMM. 2 L 7 2 4F RT A2NM 2007041000092 20070410 00092 NM 2007 4 10 SWAA071728 1 20070404 A 5753 65C35276 FLAP TRACK BOEING 737 7373H4 1384600 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND LEFT INBOARD MID FLAP INBOARD FORE FLAP TRACK CORRODED. REMOVED AND REPLACED FLAP TRA CK PER MM. 2 L 7 2 4F RT A16WE 2007041000094 20070410 00094 NM 2007 4 10 SWAA071731 1 20070404 A 3350 MS155721 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007041000098 20070410 00098 SO 2007 4 10 SIMA200709616 1 20070403 A 5347 13500439002 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 703MR 15867 4800 145173 LEFT WALL SEAT TRACK 2ND AFT CORRODED BETWEEN FRAME 24 AND FRAME 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01- 06. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041000102 20070410 00102 SO 2007 4 10 SIMA200709607 1 20070403 A 5347 14532605015 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 703MR 15867 4800 145173 FOUND RIGHT SEAT TRACK CORRODED BETWEEN FRAME 36 AND FRAME 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041000120 20070410 00120 NM 2007 4 10 UIEA200700142 1 20070325 A 2612 FIRE WARNING BOEING 747 74747UF 1384949 NM UNKNOWN A UIEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 412MC 30559 ON CLIMB-OUT, FIRE WARNING BELL RANG INTERMITTENT EVERY FEW SECONDS FOR 20 MINUTES OF FLIGHT. NO OTHER INDICATION. MAW EA SYS CYCLED, MAWEA OPERATION CHECK CARRIED OUT AND FOUND NORMAL AS PER AMM 31-51-00, 715-014. 2 L 7 4 4F RT 1384945 2007041000147 20070410 00147 NM 2007 4 10 USAA070264 1 20070404 A 5313 STRINGER BOEING 737 737401 1384701 NM FS 907 S4R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 FS 907 STR 4R HAS CRACK. STRINGER SPLICE REPAIR PER SRM 51-40-02, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007041000156 20070410 00156 NM 2007 4 10 KCSA071114 1 20070404 A 5312 BULKHEAD BOEING 747 747236B 1384804 NM BS2360 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 BS 2360 BULKHEAD FORWARD LOWER CHORD CORRODED AT STRINGER END FITTING HOLES FROM STR 26L TO STR 26R. 2 L 7 4 4F A20WE 2007041000158 20070410 00158 EA 2007 4 10 TRAX200700442 1 20070315 A 3350 COVER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 EMERGENCY LIGHT COVER ON F/A STATION DAMAGED (MARKED). 2 L 7 2 4F RT A21EA 2007041000162 20070410 00162 NM 2007 4 10 07FDEA01318 1 20070404 A 5532 65174754 SKIN PANEL BOEING 727 727225 1384077 NM ZONE 300 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 RT VERTICAL STAB SKIN/WEB HAS (2 EA) TOOLING GOUGES LOCATED UNDER PANEL 9706. GOUGES ARE LOCATED NEAR FASTENER ROW FOR L- ANGLE AND 23", 24" FROM FRONT OF PANEL. REMOVED DAMAGE PER EA I070144. VERIFY DAMAGED REMOVED BY HFEC IAW 727 NDT M AN, PART 6, 51-00-00, FIG 23. TOOL NR IDM-0031, 11/30/07 REF EA I070144 REV P2, PG 2 STEP 1. TREATED AND PRIMED BLENDE D AREA REF 51-10-2 PG 7 AND EA I070144. FABRICATED DOUBLER, TREATED AND PRIMED DOUBLER, INSTALLED DOUBLER AND FILLET SE ALED DOUBLER PER EA I070144 REV P2 PG 2 STEPS 3-7. 2 L 7 3 4F A3WE 2007041000164 20070410 00164 NM 2007 4 10 KCSA071108 1 20070402 A 5347 SEAT TRACK BOEING 747 747236B 1384804 NM BS 683 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 UPPER DECK STA 683 RBL 47 SEAT TRACK HAS AREA OF CORROSION WL 308. 2 L 7 4 4F A20WE 2007041000170 20070410 00170 WP 2007 4 10 07FDEA01323 1 20070404 A 5730 SKIN DOUG DC10 DC1010 3022110 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 LT WING L/E CRACK LONG 0.75" ON EXTERNAL LOWER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIGURE 68 SHT 1-3 VOL 1. 2 L 7 3 4F A22WE 2007041100011 20070411 00011 WP 2007 4 11 07FDEA01337 1 20070404 A 5320 STIFFENER DOUG DC10 DC1010 3022110 WP A/C BAY WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 LT AIR COND COMPT DEEP WEAR ON VERTICAL STIFFENER. REPAIRED STIFFENER IAW SRM 53-00-01 FIG 9 SHT 7 VOL 1. 2 L 7 3 4F A22WE 2007041100012 20070411 00012 WP 2007 4 11 07FDEA01340 1 20070404 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 FWD AVIONIC COMPT LT SIDE 2 HOLES ON SKIN. REPAIRED IAW SRM 53-30-00 FIG 4 VOL 1. 2 L 7 3 4F A22WE 2007041100013 20070411 00013 WP 2007 4 11 07FDEA01341 1 20070404 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP BS 490 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 RT AIR COND COMPT CRACK 1" LONG ON VERTICAL BULKHEAD. REPAIRED CRACK IAW SRM 53-30-00 FIG 6 SHT 8 VOL 1. 2 L 7 3 4F A22WE 2007041100014 20070411 00014 WP 2007 4 11 07FDEA01342 1 20070404 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP BS 473 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 LT AIR COND COMPT CRACK 1" LONG ON VERTICAL BULKHEAD. REPAIRED WEB IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1. 2 L 7 3 4F A22WE 2007041100015 20070411 00015 NM 2007 4 11 07FDEA01352 1 20070404 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 MAIN DECK CARGO COMPARTMENT STA 635 RBL 8 SEAT TRACK FOUND WITH CORROSION. [SUP 4-20-07] REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007041200003 20070412 00003 NM 2007 4 12 2007UALA01055 1 20070405 A 3213 CYLINDER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT MLG STRUT CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 563UA 26665 RIGHT MLG STRUT OUTER CYLINDER HAS CORROSION IN THE GLAND NUT THREAD AREA & IN THE GROOVE ABOVE THE THREADS 6 INCHES LON G ON THE FORWARD SIDE. [06-20-07] REMOVED RT MLG OUTER STRUT CYLINDER PER SFO GEAR SHOP, AND ROUTED TO GEAR SHOP FOR E VALUATION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041200028 20070412 00028 CE 2007 4 12 040807N338CS1 1 20070408 A 5210 65112092 DOOR SEAL CESSNA 500 550 2076604 CE PWA 530 PW530A NE ZONE 800 SEPARATED E Z5FA B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 NE 03 338CS 5501084 LOUD NOISE FROM CABIN DOOR AT FL370. FOUND DOOR SEAL TO BE THE CAUSE. ALERTED ATC FOR LOWER ALTITUDE. NO PRESSURIZATION PROBLEMS INDICATED, HOWEVER PRESSURIZATION CONTROLLER BEGAN TO FLUCTUATE. CREW DONNED THEIR O2 MASKS, DECLARED AN EMERGE NCY DESCENT AND DIVERTED. MAINTENANCE INSPECTED, CLEANED, AND LUBED PASSENGER DOOR SEAL. FOUND SEAL AND SEAMS NOT CONNEC TED, RECONNECTED SEAL ENDS IAW MM. FOUND INNER OR PRIMARY SEAL GOOD. LEAK CHECK GOOD. 1 L 7 2 4F 4 F A22CE E00053EN 2007041200034 20070412 00034 EU 2007 4 12 07FDEA00826 1 20070314 A 5753 A57970100026 SKIN AIRBUS 310 A310324 3930206 EU ZONE 500 DELAMINATED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 DELAMINATION ON OLD DOUBLER REPAIR, LT INBOARD FLAP, AFT OF TRACK NR 2. REPAIR PERFORMED BY REMOVING THE EXISTING REPAI R AN INSTALL SRM REPAIR PER 57-53-12, FIG 209. APPROVED BY EA 6-5752-103366 AND RAS/DABRE/7007096/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007041200035 20070412 00035 CE 2007 4 12 CIEA200700002 1 20070406 A 3320 2K40F3 RESISTOR BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA CABIN LIGHTS BURNED E CIEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 03 60PD 18527 BB58 SHUTDOWN THE ENGINES, NOTICED LIGHT SMOKE COMING FROM UNDER INSTRUMENT PANEL & AN ODOR LIKE ELECTRICAL BURNING. MAINT I NSPECTED AC & WHEN MASTER SWITCH WAS TURNED ON, A RESISTOR MOUNTED TO FWD BULKHEAD UNDER PILOTS INSTRUMENT PANEL FOUND T O BE GLOWING RED & EMITTING SMOKE. AFTER REVIEWING THE WIRING FROM THE RESISTOR IT WAS DETERMINED TO BE THE (R145) RESI STOR FOR THE FLUORESCENT LIGHTENING SYSTEM. THE WIRING SYSTEM FOR THE FLUORESCENT SYSTEM WAS INSPECTED FOR SHORTS AND THE ONLY ITEM FOUND WAS A LOOSE WIRE CONNECTION TO THE RT ELECTRICAL FILTER MOUNTED ON THE RT SIDE WALL OF THE AC UNDER THE EMERGENCY EXIT WINDOW. A NEW RESISTOR WAS INSTALLED AND THE SYS CHECKED GOOD AND THE AC WAS RETURNED TO SERVICE. I 1 L 7 2 4T 4 T A24CE E4EA 2007041200044 20070412 00044 WP 2007 4 12 UPS07849602 1 20070315 A 5315 575503271 FLOORBEAM DOUG DC8 DC873F 302199F WP FS 1723 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C3 FLOORBEAM STA 1723 RBL 30 - RBL 15 HAS POPPED RIVETS AND EXFOLIATION CORROSION. REMOVED CORROSION AN D REPAIRED FLOORBEAM AT STA 1723 RBL 30 - RBL 15 IAW SAA EA 008-5320-01-A0762, UPS RAA DC8-53-20617, AND FAA FORM 8100-9 . 2 L 7 4 4F RT 4A25 2007041200049 20070412 00049 EU 2007 4 12 AWXA200700477 1 20070408 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU EMEGENCY LIGHTS FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 627AW 47646 39 66 PHX - EEL - MX REPORTED EMERGENCY EXIT LIGHTS IN ROWS 19 AND 24 INOP. MX REPLACED THE POWER SUPPLY UNIT AND RETERMINAT ED THE CONNECTOR. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007041200069 20070412 00069 NM 2007 4 12 07FDEA01350 1 20070404 A 5330 65577941 SKIN BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FUSELAGE UPPER LOBE INTERIOR SKIN IS CRACKED ON BOTH SIDES OF STRINGER AT SKATE ANGLE FASTENERS AT BS 1097, STR 1, LBL 1 - RBL 1. REMOVED DAMAGE AND INSTALLED DOUBLER IN REFERENCE TO SRM 53-30-3, PG 12. 2 L 7 3 4F A3WE 2007041200096 20070412 00096 2007 4 12 RAIA00703062 4 20070323 A 3414 LINE EMB 145 EMB145 3260210 SO AIRSPEED CONTAMINATED A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 801HK 145053 FLT NR 3574 - RIC - AIRSPEED COMPARISON PROBLEMS. MAINTENANCE DRAINED WATER FROM PS LINES & PERFORMED PS TEST CHECKS GO OD. 2 L 7 2 4F RT T00011AT 2007041200114 20070412 00114 SO 2007 4 12 RAIA00703066 1 20070325 A 5101 UNKNOWN EMB 145 EMB145LR 3260212 SO WING UNKNOWN A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 823HK 145475 FLT NR 7901 - ROA - FLIGHT ATTENDANT & PASSENGER REPORTED LARGE STREAM OF VAPOR FROM UNDER WING DURING CLIMBOUT. TANK 2 INDICATION SHOWED GREATER LOSS OF FUEL THAN THE LEFT TANK. MAINTENANCE FUELED AIRCRAFT WITH 11290 LBS AND INSPECTED N O LEAKS NOTED. 2 L 7 2 4T RT T00011AT 2007041200116 20070412 00116 CE 2007 4 12 GUUA04050701 1 20070405 A 2697 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RT FIRE BOTTLE LOOSE A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 29 46AR UE27 FLIGHT: 6004, DURING FLIGHT RT FIRE EXTINGUISHER DISCHARGE ANNUNCIATOR ILLUMINATED. SECURED LOOSE WIRE ON RT FIRE EXTIN GUISHER BOTTLE. 2 L 7 2 4T 3 T RT A24CE E2NE 2007041200119 20070412 00119 EA 2007 4 12 A6WA200740185 1 20070402 A 2760 PCU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT SPOILER MALFUNCTIONED A A6WA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 GL 31 417AW 7610 VIBRATION NOTED AT 10,000 FT AIRSPEED 310 KNOTS, SLOWED TO 260 KNOTS, VIBRATION STOPPED. GEAR WAS UP. REMOVED AND REPL ACED RT SPOILER PCU REF AMM 27-62-01, OPS CHECK GOOD AT THIS TIME. REMOVED SPOILER PCU SER NO MAL 5041, PN 270007, TSN: 11492 CSN: 10286. SPOILER PCU SER NO MAL 5155, PN 270007, TSN: 12169, CSN: 10873. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041200120 20070412 00120 2007 4 12 IXXA070020O 4 20070408 A 2310 5221501000 TRANSCEIVER DOUG DC8 DC862F 3021972 WP HF SYSTEM DEFECTIVE A IXXA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 11 71CX 70022 1094 45961 DURING FLIGHT FROM KSUU, THE CREW NOTICE THAT BOTH NR 1 AND NR 2 HF TRANSCEIVER WAS NOT TRANSMITTING OR RECEIVEING. THE CREW RETURNED TO KSUU WITHOUT INCIDENT. MAINTENANCE FOUND BOTH NR 1 AND NR 2 HF TRANSCEIVER WERE INOP. MAINTENANCE RE PLACED BOTH HF TRANSCEIVER, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2007041200133 20070412 00133 NM 2007 4 12 ASAA0741567 1 20070328 A 5210 507945177 DOOR BOEING 737 7374Q8 138447Q NM L1 STIFF A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 L1 DOOR HARD TO CLOSE. CONFIRMED L1 DOOR HANGS UP WHEN AFT LATCH ROLLERS ENTER THE LATCH CAM FITTINGS (AFT). LUBED ALL FOUR LATCH ROLLER TORQUE TUBE BEARINGS PER AMM. ACCOMPLISHED FWD ENTRY DOOR OPS TEST PER AMM, ALL NORMAL. 2 L 7 2 4F RT A16WE 2007041200136 20070412 00136 EA 2007 4 12 A6WA200740177 1 20070331 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 457AW 7854 LT FS 484.0 INTERCOSTAL CRACKED AT LBL 36.0 APPROX .1 INCH LONG AT FLOOR SUPPORT BEAM. (K) [SUP 05-09-07] MAINTENANCE CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR FLANGE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BSC SR 601R-53-0030A. ( M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041200137 20070412 00137 EA 2007 4 12 A6WA200740179 1 20070401 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 340 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 457AW 7854 PAX DOOR ASSIST MOTOR SUPPORT FITTING (PN 601R317745-7) CRACKED APPROX .2 INCHES LONG. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041200142 20070412 00142 EU 2007 4 12 07FDEA01386 1 20070410 A 5753 A57970100027 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 DELAMINATED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 SEVERAL DENTS WITH DELAMINATION ON RT INBOARD FLAP BOTTOM SKIN, T/E. REPAIR WAS PERFORMED IAW SRM 57-53-12/FIG 208, APP ROVED BY EA 6-5752-101287 AND RAS/DABRE/7006662/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007041200143 20070412 00143 EU 2007 4 12 07FDEA01387 1 20070410 A 5740 A5724298542984 ATTACH BRACKET AIRBUS 310 A310324 3930206 EU ZONE 500 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CORROSION FOUND IN THE ATTACHMENT HOLES OF LT WING NR 3 FLAP JACK MOUNTING STRUCTURE. REPAIR PERFORMED BY OVERSIZING TH E HOLES AND BUSH INSTALLATION IAW EA 6-5751-103263 AND RAS/BAE/1003177/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007041200145 20070412 00145 EU 2007 4 12 07FDEA01389 1 20070410 A 5313 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CORROSION FOUND IN ZONE 150 AFT CARGO COMPARTMENT, C54-C62, P46-P53 LT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 / FI G 201 ON THE RELATED STRINGER; CONNECTING SECTIONS, C54.1-C55/58, P44-P51 REPLACED IAW SRM 51-72-10 AND SEVERAL CLIPS RE PLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007041200148 20070412 00148 EU 2007 4 12 07FDEA01392 1 20070410 A 5315 A53773651212 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 FOUND CORROSION ON TOP CAP BEAM (UPPER FLANGE) AT C33. REPAIR PERFORMED BY REPLACEMENT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007041200156 20070412 00156 EU 2007 4 12 07FDEA01398 1 20070410 A 5753 A57970100026 SKIN AIRBUS 310 A310324 3930206 EU ZONE 500 DELAMINATED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 TWO AREAS WITH DELAMINATION ON LT INBOARD FLAP BOTTOM SKIN T/E, RIB 3-5 AND RIB 8-9. REPAIR PERFORMED BY METAL SKINNED CORE REPAIR IAW SRM 57-53-12/FIG 207/209, APPROVED BY EA 6-5752-101288 AND RAS/DABRE/7006663/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007041200158 20070412 00158 EU 2007 4 12 07FDEA01400 1 20070410 A 5730 A57350047 SKIN AIRBUS 310 A310324 3930206 EU ZONE 500 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 IMPACT AND CORROSION AROUND ACCESS HOLES OF LT WING BOTTOM SKIN BETWEEN RIB 22-23, RIB 28A-29 AND RIB 29-30. REPAIR PER FORMED BY BLEND OUT IAW EA 6-5720-101243 ISSUE "A" AND RAS/BAE/1002786/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007041200159 20070412 00159 EU 2007 4 12 07FDEA01401 1 20070410 A 5314 KEELBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CORROSION ON KEEL BEAM BOX AND MLG DOOR ATTACHMENT BRACKETS LT/RT. REPAIR PERFORMED BY BLEND OUT AND SPOT FACING ON ALL AFFECTED FASTENER HOLES IAW EA 6-5315-103286 AND RAS 045294/020/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007041200160 20070412 00160 EU 2007 4 12 07FDEA01404 1 20070410 A 5414 PANEL AIRBUS 310 A310324 3930206 EU ZONE 400 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CORROSION ON PYLON NR 2 INBOARD SIDE PANEL, RIB 10-18. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5451-101322 AND RAS 045345 /010/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007041200161 20070412 00161 EU 2007 4 12 07FDEA01405 1 20070410 A 5411 SPAR AIRBUS 310 A310324 3930206 EU ZONE 400 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CORROSION ON UPPER SPAR OF RT PYLON AT RIB 14. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5451-101244 ISSUE "A" AND RAS 044 734/013/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007041200162 20070412 00162 EU 2007 4 12 07FDEA01406 1 20070410 A 5340 A53773644 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CORROSION ON CORNER FITTING AT C33, P44 LT/RT (P/N A537-73644-202, -203) REPAIR PERFORMED BY REPLACEMENT IAW SRM 51-72-1 0. 2 L 7 2 4F RT A35EU 2007041200163 20070412 00163 CE 2007 4 12 DXTA200702097 1 20070410 A 3260 INDICATOR BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE MLG UNKNOWN E DXTA O OTHER P NO WARNING INDICATION LD LANDING 1 GL 07 125QS RK433 AFTER EXTENDING LANDING GEAR RT MAIN GREEN LIGHT DID NOT ILLUMINATE, BULB TESTED OK. COMPLIED WITH SEVERAL LANDING GEAR HANDLE OPERATIONAL CHECKS DUE TO ONE TRANSIT LIGHT NOT ILLUMINATING. ALL GEAR HANDLE TRANSIT LIGHTS OPERATIONAL CHECKE D SATISFACTORY IAW BEECHJET 400A M/M CHAPTER 32-00-00. 2 H 7 2 4F 4 F RT A16SW E25EA 2007041200167 20070412 00167 EU 2007 4 12 07FDEA01407 1 20070410 A 5730 PANEL AIRBUS 310 A310324 3930206 EU ZONE 500 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CORROSION ON LT BOTTOM WING PANEL NR 2, RIB 28/30. REPAIR PERFORMED BY BLEND OUT IAW 6-5720-101273 AND RAS/BAE/1002867/ 2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007041200168 20070412 00168 EU 2007 4 12 07FDEA01408 1 20070410 A 5313 A53986212 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 FOUND CORROSION ON STRINGER P56, C69-C71. STRINGER REPAIR PERFORMED IAW SRM 53-10-14/FIG 201 AND CLIP (P/N A539-73791-2 24-91) REPLACEMENT ON C70 IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007041200172 20070412 00172 EU 2007 4 12 07FDEA01414 1 20070410 A 5755 A55710013007 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 DELAMINATED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 DELAMINATION ON SPOILER NR 3 LT, NR 4 RT END RIB. REPAIR PERFORMED IAW SRM 51-77-11, APPROVED BY EA 6-5772-101289 AND R AS 045027/006/2006 ISSUE "A" (NR 3 LT) AND RAS 045027/007/2006 ISSUE "A" (NR 4 RT). 2 L 7 2 4F RT A35EU 2007041200174 20070412 00174 WP 2007 4 12 NWAA071269956 1 20070328 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 1087 L10R CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 923RW 47183 DURING "H" CHECK FOUND, CRACK IN RT FUSELAGE FRAME AT BS 1087 L10R. REPAIRED PER EA 99-208472. 2 L 7 2 4F A6WE 2007041200175 20070412 00175 WP 2007 4 12 NWAA071279956 1 20070327 A 5310 DOOR FRAME DOUG DC9 DC931 3022065 WP EMERGENCY EXIT CHAFED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 923RW 47183 DURING "H" CHECK, FOUND CHAFING DAMAGE TO MAIN CABIN RT EMERGENCY EXIT LOWER JAMB AT BS 666 AND BS 707. REPAIRED PER EA 99-208476. 2 L 7 2 4F A6WE 2007041200177 20070412 00177 NM 2007 4 12 0406200701 1 20070406 A 3150 UNKNOWN BOEING 747 7472F6B 1384807 NM GE CF6 CF650* 30018 NE WARNING HORN UNKNOWN A OZYA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 29 535FC 21833 ON TAKEOFF ROLL, TAKEOFF WARNING HORN SOUNDED. LARGE SHUTTER CAUSED BY ROUGH RUNWAY OCCURRED. COULD NOT DUPLICATE WITH AIRCRAFT STOPPED. RETURNED TO RAMP. ACCOMPLISH TO AURAL WARNING TEST IAW MM 31-26-00. ALL OPS NORMAL, COULD NOT DUPLI CATE. ACCOMPLISHED HIGH ENERGY STOP INSPECTION IAW MM 5-5-10, NO DISCREPANCIES NOTED, AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E23EA 2007041200178 20070412 00178 NM 2007 4 12 F3LA200700059 1 20070330 A 5322 SHEAR TIE AIRBUS A319 A319111 3930336 NM SHEARED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED SHEAR PLATE SHEARED BETWEEN FR 68 AND FR 69, JUST OTBD OF FLOORBEAM -Y1292. REM OVED AND INSTALLED SHEAR PLATE IAW A319 SRM 53-41-14, FIG 18, 51-42-11, 51-20-00, PARA 3, AND 51-23-11. 2 L 7 2 4F RT A28NM 2007041200179 20070412 00179 NM 2007 4 12 F3LA200700063 1 20070330 A 5322 SHEAR TIE AIRBUS A319 A319111 3930336 NM CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED SUPPORT SHEAR PLATE CORRODED BETWEEN FR 69 AND FR 70, JUST BEHIND FLOORBEAM Y129 2. REMOVED AND REPLACED SHEAR PLATE SUPPORT FRAME AND SHEAR PLATE IAW A319 SRM 51-42-11, FIG. 8; 51-44-11, TABLE 3; 51- 72-11, PARA. 5.A.; 51-42-00, PARA. 6,7,10; AND AIRBUS DRAWING D53474180, ISSUE G. 2 L 7 2 4F RT A28NM 2007041200182 20070412 00182 NM 2007 4 12 SWAA071771 1 20070408 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 LEFT OVERWING EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007041200183 20070412 00183 NM 2007 4 12 SWAA071773 1 20070408 A 3350 20311A BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND BAT TERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007041200184 20070412 00184 NM 2007 4 12 SWAA071769 1 20070407 A 3350 20311A BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007041200185 20070412 00185 NM 2007 4 12 SWAA071770 1 20070407 A 3350 3071OLBPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 497WN 32479 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007041200186 20070412 00186 NM 2007 4 12 SWAA071764 1 20070406 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 440LV 29835 EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007041200187 20070412 00187 NM 2007 4 12 SWAA071763 1 20070406 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 458WN 33857 DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER MISSING AT ROW 20 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007041200188 20070412 00188 NM 2007 4 12 SWAA071767 1 20070407 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 227WN 34450 EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007041200189 20070412 00189 NM 2007 4 12 SWAA071772 1 20070408 A 5610 58935578 WINDOW BOEING 737 7373G7 1384595 NM FLIGHT DECK ARCED A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 671SW 23785 FLIGHT DECK R2 WINDOW ARCHED AND CRACKED. REMOVED AND REPLACED WINDOW AND HEAT CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 2007041200190 20070412 00190 2007 4 12 SWAA071768 4 20070407 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 791SW 27886 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007041200191 20070412 00191 NM 2007 4 12 SWAA071752 1 20070406 A 5714 6545413 WEB BOEING 737 7373H4 1384600 NM BS 610 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED C2 CHECK, FOUND WING CENTER SECTION WEB CRACKED BS 610, LBL 40.875. REPAIRED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2007041200192 20070412 00192 NM 2007 4 12 SWAA071746 1 20070406 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 500D CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 8L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007041200193 20070412 00193 NM 2007 4 12 SWAA071743 1 20070406 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 500D CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 8R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007041200194 20070412 00194 NM 2007 4 12 SWAA071747 1 20070406 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007041200199 20070412 00199 EA 2007 4 12 A6WA200740184 1 20070403 A 2163 FAN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TEMP SENSOR OBSTRUCTED A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 456ZW 7849 REQUEST INSPECTION OF ODOR IN BACK OF AIRPLANE. INSPECTED AIRCRAFT FOR ODORS, NO SIGNS OF ELECTRICAL DISCREPANCIES. CL EANED CABIN TEMP SENSOR FAN, DUE TO BLOCKAGE, FAN CHECKS OK. DETERMINED ODOR FROM LAV. OK FOR SERVICE AT THIS TIME. ( K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041200200 20070412 00200 NM 2007 4 12 QXEA200700519 1 20070405 A 2420 28B5551 GENERATOR BOMBDR DHC8 DHC8402 1390042 NM NR 2 FAILED A QXEA D RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 409QX 5569 5569 4051 PDX FLIGHT NR 2356: AFTER PUSHBACK AND CONDITION LEVER AT 1020, NO LOAD ON NR 2 AC GEN. NR 2 AC GEN LIGHT STAYED ILLUMI NATED. MAINTENANCE REMOVED AND INSTALLED FROM STOCK NR 2 POSITION AG GENERATOR IAW MTC 6242101. OPS CHECKED GOOD. LEA K CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007041300001 20070413 00001 EU 2007 4 13 07FDEA01454 1 20070412 A 5720 A57965171002 FAIRING AIRBUS 310 A310 EU PWA 4152 PW4152 NE ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 CRACK FOUND AT INNER SKIN OF NR 4 LT FLAP MOVABLE FAIRING. REPAIR PERFORMED BY BONDING IAW SRM 57-20-35 AND EA 6-5720-99 236 AND RAS/FOK/126/2006 ISSUE (A). 2 L 7 2 4F RT A35EU E24NE 2007041300002 20070413 00002 EU 2007 4 13 07FDEA01455 1 20070412 A 5714 SKIN AIRBUS 310 A310 EU PWA 4152 PW4152 NE ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 ELONGATED HOLES AT PYLON SUPPORT BRACKET AND BOTTOM OF LT WING SKIN. REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATIO N IAW. EA 6-5720-101304 AND RAS/BAE/1002914/2006 ISSUE (A). 2 L 7 2 4F RT A35EU E24NE 2007041300015 20070413 00015 EU 2007 4 13 YENA2007025 1 20070409 A 3030 1663214301 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2524 V2524A5 NE NR 3 ODOR A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 542JB 14035 1802 FLT 209, APRX 1450Z, DIVERTED, BURNING ODOR IN COCKPIT AND CABIN FOLLOWED BY ANTI-ICE-STBY L STAT, STBY R STAT. PERFORME D T/S TASK 24-00-00-00-810-823, FOUND SELL COMING FROM PROBE HEAT COMPUTER NR3. REMOVED AND REPLACED NR3 PROB HEAT COMPU TER. OPS CHECK OK 2 L 7 2 4F 4 F RT A28NM E40NE 2007041300016 20070413 00016 SO 2007 4 13 C2XA07IA083 1 20070410 A 5210 14533413401 HANDLE EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL PAX DOOR LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 24517 145332 FLIGHT 2102, THE CREW REPORTED THAT THE MAIN CABIN DOOR WOULD NOT OPEN FROM THE INSIDE. MAINTENANCE INSPECTED THE AIRCRA FT AND FOUND IT SAFE FOR A FERRY FLIGHT WHERE IT LANDED WITHOUT INCIDENT. MFG MAINTENANCE INSPECTED THE DOOR, AND RESECU RED THE INTERNAL HANDLE. OPERATIONAL CHECKES PERFORMED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007041300017 20070413 00017 CE 2007 4 13 DXTA200702098 1 20070411 A 3260 BULB CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG INDICATOR INOPERATIVE E DXTA O OTHER P NO WARNING INDICATION LD LANDING 1 GL 07 652QS 5605152 ON GEAR EXTENSION , LT MAIN HAD NO LIGHTS , COMPLETED CHECKLIST Z3 STILL NO INDICATION, GEAR BLEW DOWN. [SUP 4-19-07] JACKED AIRCRAFT, RAN LANDING GEAR UP & DOWN SEVERAL TIME NOTED LEFT MAIN GEAR DOWN & LOCKED LIGHT NOT ILUMINATING CHECK BULBS. FOUND BAD. REPLACED BULBS & CYCLED LANDING GEAR OPS CHECK GOOD REF CE560 M/M 32-01-00 2 L 7 2 4F 4 F RT A22CE E00059EN 2007041300018 20070413 00018 CE 2007 4 13 DXTA200702099 1 20070411 A 3610 WARNING LIGHT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL OVERPRESSURE ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 984QS 7500084 ON TAKEOFF ROLL HP DUCT OVERPRESS RT AMBER CAS MESSAGE CAME ON AND REMAINED ON. [SUP 4-19-07] REMOVED AND REPLACED OVE R OVER PRESS SWITCH IAW 760 MM 30-10-00 OPS END LEAK CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007041300019 20070413 00019 CE 2007 4 13 DXTA200702100 1 20070411 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 318QS 5600418 CO-PILOT LT BRAKE IS (SOFT). [SUP 4-19-07] USED BRAKE BLEED PROCEDURE FOR ANTI-SKID SYSTEM FOR CO-PILOTS LT BRAKE IAW. CESSNA 560 MM 32-42-00 CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2007041300020 20070413 00020 NM 2007 4 13 SWAA071761 1 20070406 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM BS 871 S24R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 871, STR 24R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007041300021 20070413 00021 NM 2007 4 13 SWAA071745 1 20070406 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 727C S14R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727C, STR 14R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007041300022 20070413 00022 NM 2007 4 13 SWAA071760 1 20070406 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM BS 900 S24R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 900, STR 24R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007041300023 20070413 00023 NM 2007 4 13 SWAA071765 1 20070406 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007041300024 20070413 00024 NM 2007 4 13 SWAA071738 1 20070406 A 5753 6546430100 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED HC1 CHECK, FOUND RIGHT WING INBOARD FORE FLAP UPPER AFT SURFACE DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2007041300025 20070413 00025 NM 2007 4 13 SWAA071750 1 20070406 A 5753 6546430122 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FORE FLAP PE R MM. 2 L 7 2 4F RT A16WE 2007041300026 20070413 00026 NM 2007 4 13 SWAA071757 1 20070406 A 5753 6546434 SKIN BOEING 737 7373A4 1384585 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED SPV CHECK, FOUND LEFT WING INBOARD T/E AFT FLAP DELAMINATED INBOARD END. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007041300027 20070413 00027 NM 2007 4 13 SWAA071758 1 20070406 A 5753 6546434 SKIN BOEING 737 7373A4 1384585 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED SPV CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED INBOARD END. REMOVED AND REPLACED FLAP PE R MM. 2 L 7 2 4F RT A16WE 2007041300028 20070413 00028 NM 2007 4 13 SWAA071751 1 20070406 A 5755 654645268A SKIN BOEING 737 7373H4 1384600 NM NR 4 SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED C2 CHECK, FOUND LT WING NR 4 SPOILER HINGE CRACKED AT OUTBOARD END. REMOVED AND REPLACED SPOILER PER M M. 2 L 7 2 4F RT A16WE 2007041300029 20070413 00029 NM 2007 4 13 SWAA071756 1 20070406 A 5313 6551698 STRINGER SPLICE BOEING 737 7373Y0 1384671 NM BS 908 S14R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 14R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007041300030 20070413 00030 NM 2007 4 13 SWAA071741 1 20070406 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM BS 360 S28L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 360, STR 28L. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2007041300031 20070413 00031 2007 4 13 SWAA071774 4 20070408 A 2565 65C16820 HOOK BOEING 737 7377H4 1384404 NM R1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 422WN 29826 R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM. 2 L 7 2 4F RT A16WE 2007041300032 20070413 00032 NM 2007 4 13 SWAA071753 1 20070406 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 707 S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 707, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007041300033 20070413 00033 NM 2007 4 13 SWAA071755 1 20070406 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 597 S6L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007041300034 20070413 00034 NM 2007 4 13 SWAA071754 1 20070406 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 360 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007041300035 20070413 00035 NM 2007 4 13 SWAA071742 1 20070406 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 380 S27L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 380, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007041300036 20070413 00036 2007 4 13 SWAA071739 4 20070406 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007041300037 20070413 00037 2007 4 13 SWAA071766 4 20070406 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 618WN 28034 DURING SCHEDULED A2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007041300038 20070413 00038 NM 2007 4 13 SWAA071740 1 20070406 A 3350 MS155721 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007041300039 20070413 00039 NM 2007 4 13 SWAA071762 1 20070406 A 3350 MS155721 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 247WN 32508 DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007041300040 20070413 00040 EA 2007 4 13 TRAX200700471 1 20070405 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 640 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 830AS 7236 RANRC 390. LT BONDED SKIN COMMON TO FS 640.00 FRAME IS CRACKED. COMPLIED WITH LT BONDED SKIN FS 640 REPAIR, IAW EC/TC RE O 601R-53-61-506 (JA10220/RA328) 04/12/07. 2 L 7 2 4F 4 F RT A21EA E15NE 2007041300041 20070413 00041 EA 2007 4 13 TRAX200700472 1 20070405 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 889AS 7538 FLAPS FAIL ON APPROACH WHEN SELECTING FROM 0 DEG TO 8 DEG. {EMERGENCY DECLARED} 2 L 7 2 4F 4 F RT A21EA E15NE 2007041300044 20070413 00044 NM 2007 4 13 F3LA200700055 1 20070330 A 5315 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM BETWEEN FR 67 AND FR 68 AT-Y1292. FLOORBEAM WAS FOUND TO BE OUT OF LIMITS PER A319 SRM 51-00-14, FIG 101. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-42-11. 2 L 7 2 4F RT A28NM 2007041300045 20070413 00045 NM 2007 4 13 QXEA200700525 1 20070409 A 2751 44281508011 INDICATOR DHAV DHC8 DHC8202 2809007 NM TE FLAPS MALFUNCTIONED A QXEA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 NM 09 367PH 3609 511 PDX FLIGHT NR 2156 ON TAKEOFF ROLL, TAKEOFF WARNING HORN SOUNDED AS POWER LEVERS WERE ADVANCED AND A/S BECAME ALIVE. ES TIMATED TORQUE 60 PERCENT AND A/S >40 KTS. TAKEOFF CONFIG TEST PASSED IAC E.A RE TAKEOFF CHECKLIST. MAINTENANCE INSPEC TED, CLEANED AND LUBED CLA, PARK BRAKE AND LEVATOR TRIM SWITCHES. REPLACED FLAP POSITION INDICATOR. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007041300046 20070413 00046 NM 2007 4 13 QXEA200700527 1 20070410 A 2920 UNKNOWN DHAV DHC8 DHC8202 2809007 NM NR 2 SPU UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 352PH 494 SEA FLIGHT NR 2104 - AFTER COMPLETING AUTO FEATHER TEST, NR 2 SPU AUX POWER CAUTION LIGHT ILLUMINATED AND REMAINED ILLUM INATED. MAINTENANCE RESET CIRCUIT BREAKER 2921-C/B6. OPERATIONAL CHECK GOOD NO PARTS REPLACED. AIRCRAFT RETURNED TO S ERVICE. 2 H 7 2 4T RT A13NM 2007041300047 20070413 00047 2007 4 13 QXEA200700528 2 20070410 A 7200 ENGINE DHAV DHC8 DHC8202 2809007 NM NR 2 SURGES A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 352PH 494 SEA FLIGHT NR 2162 ON TAKEOFF AT ABOUT 200', GOT A TORQUE SURGE ON THE NR 2 ENGINE AND SHUT IT DOWN AS PER DHECKLIST. M AINTENANCE FOUND NR 2 PLA SWITCH 6141 S4 INOP. REPLACED SWITCH, BETA LOCK OUT SYSTEM TEST GOOD. C/W WITH OVER TORQUE P ROCEDURES. NO FURTHER MTX NEED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007041300048 20070413 00048 NE 2007 4 13 QXEA200700529 2 20070409 A 7320 ECU DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 1 WARNING LIGHT A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 351PH 490 PDX FLIGHT NR 2200 ON TAXI OUT FOR DEPARTURE, DURING BETA BACKUP TEST NR 1 ECU CAUTION. MAINTENANCE RE-SET BETA LOCKOUT CIRCUIT BREAKER IAW FSM. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007041300082 20070413 00082 NM 2007 4 13 ANCF200600050 1 20070405 A 2731 SERVO BOEING 767 767284 1385184 NM PWA 4060 PW4060 52119 NE ELEVATOR MALFUNCTIONED W ANCF O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 23 988AN 24742 DURING DESCENT AT 15.000 FT, SPEED 290 EICAS MSG AUTOPILOT COME ON WITH CAUTION LIGHT, AUTOPILOT WAS DISENGAGED BY IT SE LF. DURING APP THE ELEVATOR WAS VERY HARD TO OPERATE, BEING NECESSARY, EXCESSIVE FORCE CONTROL BY THE PILOT. PILOT FLY ING. DURING FLARE THE ELEVATOR EFFECTIVENESS WAS COMPLETELY LOST. ACCOMPANIED BY A STRONG NOISE., TAIL NOISE. IAW FIM 22-00-02 FIG 114 BLOCKS 1,2,3,4,5,35 AND 109, DURING MCDP BITE. LAST FLIGHT FAULT A/P CTR MODE ERR CODE 244 WAS FOUND ; AND IAW AMM 22-12-01/401, THE CTR ELEVATOR A/P SERVO WAS REPLACED. IAW AMM 27-31-19/401 THE ELEVATOR FEEL COMPUTER W AS REPLACED TEST IAW AMM 27-31-00/50 AMM 34-11-00/ 201 AND 22-00-02/501 TEST SATISFACTORY. IAW AMM 31-31-01 PAGE 401, T 2 L 7 2 4F 4 F RT A1NM E24NE 2007041300083 20070413 00083 SO 2007 4 13 GUUA04070701 1 20070407 A 2710 UNKNOWN EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE AILERONS UNKNOWN A GUUA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 29 280AS 120231 FLIGHT: 0253, DURING FINAL APPROACH FLIGHT CONTROLS WILL NOT PERMIT RT AILERON INPUT. INSPECTED LT AILERON CONTROL SURF ACE REMOVED PANELS AND INSPECTED CABLES, PULLEYS, BEARING ATTACHMENTS ALSO INSPECTED AILERON CONTROL QUADRANTS UNDER THE FLOOR FOR LOOSE ITEMS CABLES PULLEYS AND CONTROL RODS NO DEFECTS NOTED CONTROLS ARE FREE NO BINDING. TEST FLIGHT SATISF ACTORY. 2 L 7 2 4T 4 T RT A31SO E20NE 2007041300084 20070413 00084 CE 2007 4 13 GUUA04060701 1 20070406 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CABIN ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 29 87557 UE246 FLIGHT: 9175, DURING FLIGHT SWEET ODOR EMINATING FROM BLOWERS. INSPECTED BOTH ENGINE OIL LINES FOR OIL LEAKS, INSPECTED BLEED AIR LINES RAN BOTH ENGINES VCM AUTO AND MANUAL NO DEFECTS NOTED. 2 L 7 2 4T 4 T RT A24CE E26NE 2007041300085 20070413 00085 CE 2007 4 13 GUUA04080701 1 20070408 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CABIN ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 29 87557 UE246 FLIGHT: 9297, DURING FINAL APPROACH STRONG SWEET ODOR OBSERVED UNTIL TOUCHDOWN. PREFORMED ENGINE RUNS FOR 20 MINUTES WI TH DIFFERENT ACM, VCM AND BLEED VALVE SETTINGS COULD NOT DUPLICATE. 2 L 7 2 4T 4 T RT A24CE E26NE 2007041300086 20070413 00086 NM 2007 4 13 QXEA200700533 1 20070323 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 500-512 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - SCRATCHES ON SEAT TRACK NR 5 BETWEEN STATION 500 AND 512. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2007041000032 20070410 00032 SO 2007 4 10 SIMA200709603 1 20070403 A 5320 14522460009 GUSSET EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 703MR 15867 4800 145173 CABIN FLOOR GUSSET ON CENTER HAT BEAM CORRODED AT FRAME 20 TO FRAME 22. REMOVED AND REPLACED GUSSET IAW EMB SRM. RETUR NED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041000044 20070410 00044 EA 2007 4 10 TRAX200700456 1 20070403 A 2560 MEGAPHONE CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 717EV 10088 FLIGHT ATTENDANT MEGAPHONE INOP. 2 L 7 2 4F RT A21EA 2007041000045 20070410 00045 EU 2007 4 10 TRAX200700457 1 20070403 A 3350 BULB AEROSP ATR72 ATR72 EU EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 ASD EMERGENCY LIGHT BULB INOP. 2 H 7 2 4T RT 2007041000060 20070410 00060 EA 2007 4 10 TRAX200700469 1 20070405 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA CABIN STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 CABIN DOOR VERY DIFFICULT TO OPEN FROM THE OUTSIDE. 2 L 7 2 4F RT A21EA 2007041000078 20070410 00078 NM 2007 4 10 DL76G070298 1 20070405 A 5315 BAC1505101303 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 14616 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 154DL 25241 BS 1461 LBL 33-40 FLOORBEAM FOUND CORRODED AND REPAIRED AS PER DRD 53-00-51D FIG 201. 2 L 7 2 4F RT A1NM 2007041000090 20070410 00090 NM 2007 4 10 SWAA071734 1 20070404 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 727 S23R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727, STR 23R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007041000095 20070410 00095 SO 2007 4 10 SIMA200709608 1 20070403 A 5347 13500412001 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 703MR 15867 4800 145173 RIGHT INBOARD SEAT TRACK CORRODED BETWEEN FRAME 53 AND FRAME 55. REMOVED AND REPLACED SEAT TRACK IAW EMB SRM 53-01-06. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041000101 20070410 00101 EA 2007 4 10 SIMA200709618 1 20070405 A 5240 DOOR CNDAIR CL600 CL6002C10 1390015 EA GROUND POWER UNSECURE A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 510AE 10105 HEARD DULL THUMP FOLLOWED BY SQUEAL DURING AIRCRAFT ROTATION, POST FLIGHT INSPECTION REVEALED GROUND POWER UNIT DOOR NOT SECURED. INSPECTED FUSELAGE AROUND EXTERNAL ELECTRICAL RECEPTACLE AND FOUND NO DAMAGE. SECURED DOOR, RETURNED AIRCRAF T TO SERVICE. 2 L 7 2 4F RT A21EA 2007041000108 20070410 00108 SO 2007 4 10 SIMA200709610 1 20070403 A 5347 14532605017 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 703MR 15867 4800 145173 RIGHT SEAT TRACK CORRODED BETWEEN FRAME 47 AND FRAME 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAF T RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041000111 20070410 00111 NM 2007 4 10 DL76G070303 1 20070405 A 5315 BAC1503100229 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 1197 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 154DL 25241 AFT COMPARTMENT STA 1197 RBL 23 TO 29 FLOORBEAM FWD OF AFT UNDER SIDE CORRODED AND REPAIRED PER SRM53-00--7 FIG 201 REPA IR 4 DETAIL V. 2 L 7 2 4F RT A1NM 2007041000122 20070410 00122 NM 2007 4 10 UIEA200700144 1 20070324 A 5330 SKIN BOEING 747 747228F 1384895 NM BS 789 S46R CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 FUSELAGE SKIN HAS A CRACK APPROX 400", AT BS 789 S46R AND RIVET PULLING THROUGH. REPAIRED ACCOMPLISHED AS PER XEO NR 53 -032207. 2 L 7 4 4F A20WE 2007041000125 20070410 00125 SO 2007 4 10 C2XA07CL035 1 20070401 A 3350 78241 INVERTER EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14940 145033 DURING ROUTINE MAINTENANCE THE OVERWING FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLAC ED THE NR 6 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2007041000128 20070410 00128 WP 2007 4 10 07FDEA01277 1 20070403 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 1671 S44R CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 CENTRAL CARGO COMPT 2 CRACKS 5" AND 7" LONG STA 1671. REPLACE LONG AFA3040-1 AND REPAIRED FRAME IAW SRM 53-30-00 FIG 5 AND 10 VOL 1. 2 L 7 3 4F A22WE 2007041000134 20070410 00134 WP 2007 4 10 UPS07849585 1 20070328 A 5511 FRAME DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 RT HORIZONTAL STAB LEADING EDGE LWR FORMER STA XFS 44 CRACKED. STOP DRILLED CRACK, FABRICATED AND IN STALLED REPAIR DOUBLER IAW SRM 55-02-00-0, 51-1-20D AND DWG 5644310. 2 L 7 4 4F RT 4A25 2007041000136 20070410 00136 WP 2007 4 10 UPS07849587 1 20070401 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:N/A FWD PASSAGEWAY AND EMERGENCY LIGHT NEXT TO EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED PASSAG EWAY AND EMERGENCY LIGHT. LIGHT OPS GOOD. 2 L 7 4 4F RT 4A25 2007041000137 20070410 00137 WP 2007 4 10 UPS07849588 1 20070402 A 3350 5708458 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT FAILED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT BATTERY PACK WILL NOT CHARGE. EMERGENCY EXIT BATTERY PACK REPLACED IAW DC8 AMM 33-50-01-2. 2 L 7 4 4F RT 4A25 2007041000143 20070410 00143 NM 2007 4 10 USAA070268 1 20070404 A 5311 FRAME BOEING 737 737401 1384701 NM BS 492 S24R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 FWD CARGO DOOR AFT FRAME LOWER DOORSTOP FITTING AREA, BS 492, S24R HAS CRACK. REMOVED & INSTALLED NEW FRAME PER BOEING DWG 65-20723 & SRM 51-40-02, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007041000148 20070410 00148 NM 2007 4 10 USAA070263 1 20070404 A 5730 65C26601198 SKIN BOEING 737 737401 1384701 NM WING LE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 RIVET HOLES IN LEADING EDGE LOWER SKIN (AFT FASTENER ROW) JUST FWD OF I/B HAS CRACKS. REMOVED DAMAGE, INSTALLED FILLER & EXTERNAL DOUBLER PER SRM 57-43-01, DEFECT SIZE: 7 INCHES TOTAL ACCUMULATIVE LENGTH, 2 EA. 2 L 7 2 4F RT A16WE 2007041000151 20070410 00151 WP 2007 4 10 07FDEA01343 1 20070404 A 5730 SKIN DOUG DC10 DC1010 3022110 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 LT WING LWR EXT SKIN L/E FOUND CRACK 0.5" LONG. REPAIRED CRACK IAW SRM 57-10-00 FIG 68 SHT 2 VOL 1. 2 L 7 3 4F A22WE 2007041000159 20070410 00159 EA 2007 4 10 TRAX200700443 1 20070331 A 3210 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA MAINS UNKNOWN A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 880AS 7606 AFTER TAKEOFF PLACED GEAR HANDLE UP, FOLLOWED BY GEAR DISAGREE AND NOSE GEAR DOOR OPENED EICAS WARNING MSG'S. C/W QRH P ROCEDURES LANDED AND GROUND PERSONNEL INSERTED GEAR PINS INTO GEAR. EMERGENCY DECLARED. A/C RETURNED TO ERI AFTER T/O. FLT 4825 CX. 2 L 7 2 4F RT A21EA 2007041000166 20070410 00166 WP 2007 4 10 07FDEA01319 1 20070404 A 5712 RIB DOUG DC10 DC1010 3022110 WP RWS 720 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 RT WING L/E INT ZONE FOUND 1 CRACK 0.50" LONG, ON RIB WITH OLD REPAIR. REMOVED OLD REPAIR, AND PERFORMED NEW REPAIR IAW SRM 57-20-00 FIGURE 1 VOL 1. 2 L 7 3 4F A22WE 2007041000168 20070410 00168 WP 2007 4 10 07FDEA01321 1 20070404 A 5712 RIB DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 RT WING L/E INTERNAL ZONE FOUND 1 CRACK 0.75" LONG ON RIB. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 1 VOL 1. 2 L 7 3 4F A22WE 2007041100002 20070411 00002 WP 2007 4 11 07FDEA01313 1 20070404 A 5740 TEE FITTING DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 RT WING L/E FOUND 1 CRACK ON FIXED TEE 1" LONG. REPAIRED TEE IAW SRM 57-10-00 FIG 49 VOL 1. 2 L 7 3 4F A22WE 2007041100003 20070411 00003 WP 2007 4 11 07FDEA01314 1 20070404 A 5740 TEE FITTING DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 RT WING L/E FOUND 1 CRACK 1" LONG ON FIXED TEE. REPAIRED TEE IAW SRM 57-10-00 FIG 49 VOL 1. 2 L 7 3 4F A22WE 2007041100004 20070411 00004 WP 2007 4 11 07FDEA01315 1 20070404 A 5740 TEE FITTING DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 RT WING L/E 1 EA CRACK 1" LONG ON FIXED TEE. REPAIRED TEE IAW SRM 57-10-00 FIG 49 VOL 1. 2 L 7 3 4F A22WE 2007041100005 20070411 00005 WP 2007 4 11 07FDEA01316 1 20070404 A 5730 SKIN DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 RT WING L/E ON EXTERNAL SKIN FOUND 1 CRACK 1" LONG. REPAIRED CRACK ON L/E SKIN IAW SRM 57-10-00 FIG 68 SHT 1 VOL 1. 2 L 7 3 4F A22WE 2007041100006 20070411 00006 WP 2007 4 11 07FDEA01317 1 20070404 A 5730 SKIN DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 RT WING DURING INSPECTION WITH EO NR 8-5100-7-5001 P2 FOUND 1 CRACK 1" LONG ON UPPER SKIN OF O/B FLAP. REPAIRED SKIN IA W SRM 57-00-01 FIG 4 SHT 2 VOL 1. 2 L 7 3 4F A22WE 2007041100007 20070411 00007 NM 2007 4 11 07FDEA01364 1 20070405 A 5730 65225557 SKIN BOEING 727 727225 1384077 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 LEFT WING FAIRING NR 3343 VERIFIED MATERIAL AS 2024-0 .050 REF DWG 65-22555 AND SRM 51-40-2 PG 1. STOPPED DRILLED CRACK REF SRM 51-10-PG 13 ITEM 10, HFEC IAW 727NDT MAN PART 6, 51-00-00 FIG 23. TOOL NR IDM 0031 11-30-07. VERIFIED CRACK T O BE CONFINED BY STOP DRILL AND MADE REPAIR DOUBLER, REF SRM 51-40-2 PG 3 HEAT TREATED REF W/O 11841-5000-0011 ACP HARDN ESS TEST, WITHIN ACCEPTABLE LIMITS FOR 2024 T4 REF BAC5946 REV 9 TREATED AND PRIMED DOUBLER/FAIRING REF SRM 51-10-2 PG 9 AND 11-12. INSTALLED DOUBLER AND FILLET SEALED REF SRM 51-40-2. PAINTED REF MM 51-20-151-7 REPAIR CLASSIFIED AS MINOR . 2 L 7 3 4F A3WE 2007041100008 20070411 00008 WP 2007 4 11 07FDEA01333 1 20070404 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 421 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 FWD AVIONIC COMPT CRACK 6" LONG ON FRAME. REPAIRED FRAME IAW SRM 53-30-00 FIGURE 5 SHT 1-2 VOL 1. 2 L 7 3 4F A22WE 2007041100009 20070411 00009 WP 2007 4 11 07FDEA01334 1 20070404 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP BS 1491 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 RT MLG W/W FOUND 1 CRACK 2" LONG ON VERTICAL BLKHD. REPAIRED BLKHD IAW SRM 53-00-01 FIGURE 4 SHT 2 VOL.1. 2 L 7 3 4F A22WE 2007041100021 20070411 00021 EA 2007 4 11 A6WA200740086 1 20070226 A 5320 6013501252 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 450AW 7823 AFT EQUIPMENT COMPARTMENT FS 625.00 OBLIQUE ANGLE. RT IS CRACKED 2 INCH LONG IN AFT RADIUS MAINTENANCE REMOVED OLD CRAC KED 625 OBLIQUE ANGLE, INSTALLED NEW SERVICEABLE ANGLE, PN 601-35012-52 IAW SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041200018 20070412 00018 NM 2007 4 12 2007UALA01050 1 20070405 A 2432 BATTERY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE MASTER FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 671UA 30026 MAIN BATTERY CHG STATUS MSG. [SUP 5-1-07] REPLACED BATTERY CHARGER. CHECKS OK FOR SERVICE. SUSPECT CHARGER SHORTED OU T. 2 L 7 2 4F 4 F RT A1NM E24NE 2007041200020 20070412 00020 SO 2007 4 12 C2XAO7SH017 1 20070405 A 5310 14524061008 DOOR FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12957 145080 SHV - DURING C-CHECK MAINTENANCE FOUND THE SVC DOOR CUTOUT AT FRM 22 WITH CORROSION AROUND TRIM NUT PLATE, BELOW LOWER A FT DOOR STOP. MAINTENANCE INSTALLED DOUBLER AT THE SVC DOOR CUTOUT FRM 22 LOWER AFT CORNER AT NUT PLATE AREA IAW EC 531 0-01373. AIRCRAFT APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007041200033 20070412 00033 EA 2007 4 12 QXEA200700524 1 20070409 A 5240 ROLLER CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR LACK OF LUBE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 606QX 10023 DEN - FLIGHT 4327- GALLEY SERVICE DOOR HARD TO UNLOCK AND OPEN. MAINTENANCE LUBED THE GALLEY DOOR ROLLERS AND HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007041200041 20070412 00041 EU 2007 4 12 UPS07149604 1 20070408 A 2560 ESCAPE ROPE AIRBUS 300 A300B4622R 3930312 EU COCKPIT MISINSTALLED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 167UP 0862 INSPECTION TYPE:N/A F/O'S ESCAPE ROPE IS NOT INSTALLED PROPERLY. PART OF ROPE IS TRAPPED IN PANEL, WON'T RELEASE FULLY, NEEDS TO FREELY BE RELEASED AND PROPERLY REPACKED. REMOVED ROPE AND REPACKED PROPERLY. 2 L 7 2 4F RT A35EU 2007041200050 20070412 00050 EU 2007 4 12 AWXA200700478 1 20070408 A 3040 41600318003 CONTROLLER AIRBUS 320 A320231 3930325 EU WINDSHIELD HEAT UNKNOWN A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 WP 28 620AW 13441 13441 052 MCO - ON APPROACH TO MCO, F/OS WINDSHIELD CRACKED AND STARTED SPARKING. CREW DECLARED AN EMERGENCY. THE PAX DID NOT BR ACE. THE LANDING WAS UNEVENTFUL. MX REPLACED THE WINDSHIELD AND AS A PRECAUTION, MX REPLACED THE WINDOW HEAT CONTROLLE R. OPERATIONAL CHECK WAS GOOD. THE A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2007041200060 20070412 00060 2007 4 12 07FDEA01371 2 20070406 A 7200 ENGINE DOUG MD10 MD1010F 3022112 WP NR 2 MALFUNCTIONED A FDEA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 SO 25 381FE 46615 NUMBER 2 ENGINE SHUT DOWN WHEN IT WOULD NOT RESPOND TO THROTTLE MOVEMENTS. NO PARAMETERS EXCEEDED. NORMAL LANDING ACCO MPLISHED PER CREW DEBRIEF THROTTLES WERE NEVER STIFF AND ENGINE WAS SHUT DOWN ABOUT 30 MINUTES IN FLIGHT. NR 2 ENG AND MOVED THROTTLE LEVER IN COCKPIT TO VERIFY MOVEMENT AT FUEL CONTROL. FUEL CONTROL LEVER MOVED ACCORDINGLY. STARTED EN G WITH THROTTLE AT IDLE. NR 2 ENG SPOOLED UP PAST FLIGHT IDLE DURING START. SUSPECT MEC, IAW MD10. 2 L 7 3 4F RT A22WE 2007041200070 20070412 00070 NM 2007 4 12 07FDEA01351 1 20070404 A 5320 58300 FITTING BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 INTERNAL FUSELAGE AT STA 259.BL0 TO RBL 2, CASTING HAS TOOLING DAMAGE REMOVE FLIGHT DECK CEILING TO GAIN ACCESS TO CASTI NG. REMOVED INTERCOSTAL AND SURROUND STRUCTURE. REMOVED CASTING, DRILLED NEW CASTING AND INSTALLED. RE-INSTALLED ALL STRUCTURE AND CEILING PANELS REF SRM 51-30-2. 2 L 7 3 4F A3WE 2007041200074 20070412 00074 NM 2007 4 12 07FDEA01356 1 20070405 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 CABIN, RIGHT LONGERON 17 FOUND CRACKED AT STA 1239. [SUP 4-18-07] REMOVED AND REPLACED AS PER SRM 51-33- 01 VOLUME II . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007041200076 20070412 00076 EU 2007 4 12 07FDEA01358 1 20070405 A 5320 FLOOR SUPPORT AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 FWD LOWER CARGO COMPARTMENT FLOOR SUPPORT IS CRACK LT SIDE OF FR 38.2 BETWEEN CL TO LBL 24". REMOVED FLOOR SUPPORT IAW SRM 51-40-44. FAB`D NEW SUPPORT, LOCATED AND DRILLED IAW SRM 51-40-44. INSTALLED FLOOR SUPPORT IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007041200077 20070412 00077 EU 2007 4 12 07FDEA01359 1 20070405 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 414FE 400 FWD LOWER CARGO COMPARTMENT FLOORBEAM IS CRACK LT SIDE OF FR 38.2 BETWEEN CL TO LBL 24". REMOVED FLOOR SUPPORT IAW SRM 51-40-44. FABBED NEW SUPPORT, LOCATED AND DRILLED IAW SRM 51-40-44. INSTALLED FLOOR SUPPORT IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007041200084 20070412 00084 EA 2007 4 12 A6WA200740089 1 20070228 A 5320 6013501251 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FS 621-625 S14L CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 453AW 7838 LT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.2 INCH LONG. MAINTENANCE REMOVED AND REPLACED LT INTERCOSTAL PN 601-35012-51 IAW SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041200091 20070412 00091 EA 2007 4 12 A6WA200740165 1 20070401 A 2741 706010 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE STAB TRIM MALFUNCTIONED A A6WA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 31 419AW 19540 7633 STAB TRIM RUNAWAY AFTER TAKEOFF, QRH COMPLIED WITH, RETURNED TO DEPARTURE. REMOVED AND REPLACED HORIZONTAL STAB TRIM CO NTROL UNIT IAW AMM REF 27-41-01 AND FOUND SERVICEABLE. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041200092 20070412 00092 WP 2007 4 12 MWEA070080 1 20070407 A 3350 60030451 BATTERY PACK DOUG DC9 DC981 3022081 WP EMERGENCY LIGHTS INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 814ME 48010 EMERGENCY LIGHT IN AFT ACCESSORY ABOVE TAIL CONE RELEASE HANDLE. REPLACED BATTERIES IN EMERGENCY BATTERY PACK. 2 L 7 2 4F A6WE 2007041200094 20070412 00094 NM 2007 4 12 MWEA070082 1 20070409 A 2170 21BC124 COALESCER BAG BOEING 717 717200 1383700 NM AFT ACCESSORY DIRTY A MWEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 13 908ME 55172 STATION PERSONAL FUMES/ ODOR FROM FORWARD ENTRY OVERHEAD VENT. PERFORMED OPERATIONAL CHECK OF BOTH LEFT & RIGHT AIRCRAF T PACKS. REMOVED AND REPLACED COALESCER BAG, PERFORMED LEAK CHECK OF THE RIGHT COALESCER AS REQUIRED. NO LEAKS NOTED A T THIS TIME. 2 L 7 2 4F TR A6WE 2007041200100 20070412 00100 SO 2007 4 12 RAIA00703071 1 20070326 A 3350 BULB EMB 145 EMB145 3260210 SO EMERGENCY LIGHT BURNED OUT A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 807HK 145119 PRE FLT NR 5595 - STL - EMERGENCY LIGHT ON STAIRWELL INOP. MAINTENANCE REMOVED AND REPLACED BULB, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007041200107 20070412 00107 NE 2007 4 12 HALA0700159 2 20070408 A 7200 GUIDE VANE BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE LT ENGINE EXIT MISSING A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, LEFT ENGINE EXIT GUIDE VANE MISSING AT 1000 O'CLOCK POSITION. INFO NOTED, OK TO CONT PER AMM 72-33-02 TABLE 602 A MAXIMUM OF 3 GUIDE VANE CAN BE MISSING OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007041200109 20070412 00109 2007 4 12 HALA0700163 4 20070407 A 3416 ALTIMETER BOEING 767 76733A 1385209 NM COCKPIT FAILED A HALA O OTHER O OTHER AP APPROACH 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM, NO LAND 3 DISPLAYED ON ASA W/APP MODE NOT SELECTED AND A/P F/D ENGAGED CENTER RADIO ALTIMETER FAIL FLAG APPEARS INTERMITTENTLY. MCDP LAST FLT FAULTS SHOWS RA CENTER 130861 BITE TEST OF CENTER R/A PASSES TEST SHOWS NO FAILURES PERFORMED MCDP TESTS 30 40 BOTH PASS AUTOLAND SYS CKS GOOD. 2 L 7 2 4F RT A1NM 2007041200117 20070412 00117 NM 2007 4 12 USAA200704001 1 20070404 A 5330 SKIN BOEING 737 7374B7 1384702 NM BS 727E CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 441US 24812 A 3 INCH CRACK FOUND ON SKIN, RIGHT SIDE AT STA 727E + 3 INCHES. REMOVED DAMAGED AREA & INSTALLED REPAIR DOUBLER PER SR M 53-00-01 REP 31. 2 L 7 2 4F RT A16WE 2007041200135 20070412 00135 WP 2007 4 12 MWEA070075 1 20070404 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 214 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 808ME 48070 DENT IN FUSELAGE SKIN AT FRAME STATION 214 JUST ABOVE LONGERON 15 RIGHT. [SUP 4/13/07] FABRICATED AND INSTALLED DOUBLER . 2 L 7 2 4F A6WE 2007041200138 20070412 00138 EA 2007 4 12 A6WA200740182 1 20070403 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621-325 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 457AW 7854 625 OBLIQUE ANGLE CRACKED IN RADIUS APPROX 1.0 INCH LONG, RT SIDE. (K) [SUP 5-1-07] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE P/N 601-35012-52, IAW CRJ SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041200140 20070412 00140 NM 2007 4 12 07FDEA01384 1 20070410 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 CORROSION FOUND ON SEAT TRACK AT STA 1853 - 1887, X= 8.5, DISCOVERED AFTER REMOVAL OF FLOOR PANEL FOR ACCESS. [SUP 4 -20-07] REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007041200141 20070412 00141 NM 2007 4 12 07FDEA01385 1 20070410 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 UPPER MAIN CARGO COMPARTMENT FOUND SEAT TRACK WITH CORROSION AT STA 1179 X= 8. [SUP 4-20-07] REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007041200157 20070412 00157 EU 2007 4 12 07FDEA01399 1 20070410 A 5730 A57350143 SKIN AIRBUS 310 A310324 3930206 EU ZONE 500 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CORROSION ON AN OLD REPAIR LT WING BOX FWD OF FRONT SPAR, BETWEEN RIB 28A-29. REPAIR PERFORMED BY REAM UP THE AFFECTED HOLES AND OVERSIZING IAW EA 6-5720-101242 AND RAS/BAE/1002718/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007041200180 20070412 00180 NM 2007 4 12 SWAA071737 1 20070406 A 3350 100031 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 244WN 34864 AFT CABIN EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007041200181 20070412 00181 NM 2007 4 12 SWAA071736 1 20070406 A 3350 101331 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 237WN 34632 RIGHT OVERWING EMERGENCY EXIT SIGN LENS FELL OFF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007041200195 20070412 00195 NM 2007 4 12 SWAA071744 1 20070406 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 416 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 416, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007041200196 20070412 00196 NM 2007 4 12 SWAA071748 1 20070406 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM BS 395 S19R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 395, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007041200197 20070412 00197 NM 2007 4 12 SWAA071749 1 20070406 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM BS 380 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, STR 8L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007041300049 20070413 00049 NM 2007 4 13 QXEA200700540 1 20070327 A 5320 SUPPORT ANGLE DHAV DHC8 DHC8202 2809007 NM FUSLEAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - GOUGES IN SUPPORT ANGLE FOR FORWARD CHANNEL OF PANEL 261GT. REPAIRED IAW SRM 51-20-11, 51-20-16, AND 51-20-36. 2 H 7 2 4T RT A13NM 2007041300050 20070413 00050 NM 2007 4 13 QXEA200700541 1 20070327 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM RT WING TOOL DAMAGE A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - RIGHT WING BOTTOM SPAR HAS TOOLING MARKS FROM LEADING EDGE REMOVAL, FROM NACELLE TO THE WING TIP. REPAIRED IAW RD8-57-1119. 2 H 7 2 4T RT A13NM 2007041300051 20070413 00051 NM 2007 4 13 QXEA200700535 1 20070402 A 5220 STOP DHAV DHC8 DHC8202 2809007 NM EMERGENCY EXIT WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - ALL 8 FUSELAGE DOOR STOPS WORN AT FORWARD EMERGENCY EXIT DOOR CUTOUT. REPAIRED IAW RD8-53-126. 2 H 7 2 4T RT A13NM 2007041300052 20070413 00052 NM 2007 4 13 QXEA200700536 1 20070402 A 5220 STOP DHAV DHC8 DHC8202 2809007 NM EMERGENCY EXIT WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - RIGHT EMERGENCY EXIT DOOR STOPS FORWARD UPPER AND LOWER AFT WORN. REPAIRED IAW RD8-52-350. 2 H 7 2 4T RT A13NM 2007041300053 20070413 00053 NM 2007 4 13 QXEA200700537 1 20070328 A 5313 STRINGER DHAV DHC8 DHC8202 2809007 NM FUSLEAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - STRINGER HAS CORROSION AT 7 RIVETS BELOW CARGO BAY THRESHOLD X567 - X576, Z93, APPROXIMATELY Y34L. REPAIRED IA W SRM 51-20-11, 51-20-36, AND 51-40-11. 2 H 7 2 4T RT A13NM 2007041300054 20070413 00054 NM 2007 4 13 QXEA200700543 1 20070330 A 5752 HINGE FITTING DHAV DHC8 DHC8202 2809007 NM RT AILERON TAB WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - RIGHT AILERON TAB, INBOARD CENTER HINGE FITTING IS WORN. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007041300055 20070413 00055 NM 2007 4 13 QXEA200700531 1 20070323 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - FOUND SEAT TRACK NR 5 HAS SCRATCHES AT STATIONS X433, X436 - X456, X467 - X488, X495 - X525. REPAIRED IAW RD8- 53-1339. 2 H 7 2 4T RT A13NM 2007041300056 20070413 00056 NM 2007 4 13 F3LA200700057 1 20070330 A 5320 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION AROUND NUTPLATE HOLE ON FLOORBEAM BETWEEN FR 66AND FR 68 AT Y1292. FL OORBEAM WAS FOUND TO BE OUT OF LIMITS IAW A319 SRM 51-00-14, FIG 8. REPLACED FLOORBEAM IAW A319 SRM 51-44-11 3B AND 51- 42-11. 2 L 7 2 4F RT A28NM 2007041300057 20070413 00057 NM 2007 4 13 F3LA200700060 1 20070401 A 5322 SHEAR TIE AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED WEB PLATE SUPPORT UNDER SHEAR PLATE BETWEEN FR 69 AND FR 70 JUST BEHIND FLOORBEA M -Y1292 SUPPORT FRAME CORRODED. FOUND WEB PLATE SUPPORT TO BE OUT OF LIMITS IAW A319 SRM 53-00-14, FIG 101. REMOVED A ND REPLACED SHEAR PLATE AND SUPPORT FRAME BETWEEN FR 69 AND FR 70 BEHIND FLOORBEAM -1292 IAW A319 SRM 51-42-11, FIG 9, 1 2, 40, 43, TABLE 22 AND 25. 2 L 7 2 4F RT A28NM 2007041300058 20070413 00058 NM 2007 4 13 F3LA200700050 1 20070330 A 5320 SILL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 1684 DURING C4/S1 CHECK, INSPECTION REPORTED NUT CLIP AREA CORRODED ON FLOORBEAM Y1732 AT FR 66, FWD OF L-2 DOOR FRAME. REMO VED FASTENERS FROM L-2 DOOR SILL IAW A319 SRM 51-42-11, PARA. 5. REPLACED L2 DOOR SILL IAW A319 SRM 51-42-11, SRM 51-75 -12, SRM 51-44-11, AND AMM 51-78-00-615-005. 2 L 7 2 4F RT A28NM 2007041300059 20070413 00059 NM 2007 4 13 QXEA200700596 1 20070410 A 3297 471515 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM NLG WOW DAMAGED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 413QX 3432 3432 4060 LAX FLIGHT NR 2444: LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. THREE GREEN, THREE RED, AMBER HANDLE LIGHTS ALL ILLUM INATED WITH GEAR SELECTED UP. MAINTENANCE REMOVED AND REPLACED NLG WOW2 CENTERING HARNESS IAW 32-21-11-000-401 AND 32-2 1-400-401, TR NR 32-203. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007041300060 20070413 00060 EA 2007 4 13 QXEA200700597 1 20070411 A 2150 A/C PACK CNDAIR CL600 CL6002C10 1390015 EA RIGHT MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 600QX 10005 PDX - FLIGHT 2555, UNABLE TO CONTROL RIGHT AIR CONDITIONING PACK TEMPERATURE IN AUTO OR MANUAL POSITIONS. RETURNED TO T HE GATE. MAINTENANCE PLACED THE AIR CONDITIONING PACK ON MEL 21-51-1B. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007041300061 20070413 00061 2007 4 13 QXEA200700594 4 20070410 A 3160 C19190AB04 DISPLAY BOMBDR DHC8 DHC8402 1390042 NM COCKPIT MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 401QX 10019 10019 4031 PDX FLIGHT NR 2449: AFTER PUSHBACK RECEIVED A HOTPFD2 MESSAGE ON THE EDU. MAINTENANCE FOUND THE CDS READS 'PFD 2 SECOND OVERHEAT' WITH NO FAN FAIL INDICATION. REMOVED AND INSTALLED NEW PFD 2 DISPLAY IAW MTC 6316104. OPS TEST GOOD. A/C O K FOR CONTINUED CAT III SERVICE AND IS PLACARD CAT III. MAINTENANCE CONTROL NOTIFIED OF STATUS. AIRCRAFT RETURNED TO S ERVICE. 2 H 7 2 4T RT A13NM 2007041300062 20070413 00062 CE 2007 4 13 BSAASDR0705 1 20070313 A 3230 MS24171D1 RELAY BEECH 1900 1900D 1154162 CE MLG ARCED A BSAA L ABORTED APPROACH J S WARNING INDICATION AFFECT SYSTEMS AP APPROACH 1 NM 05 139ZV UE139 WHEN THE GEAR WAS SELECTED DOWN DURING APPROACH THE GEAR DIDN'T EXTEND. THE CREW FOUND THE 2 AMP GEAR CONTROL CIRCUIT B REAKER POPPED. CREW ABORTED LANDING, PUT GEAR HANDLE IN UP POSITION, RESET CB, & PLACED GEAR HANDLE IN DOWN POSITION, & CB POPPED AGAIN. CREW EXTENDED GEAR USING MANUAL SYSTEM, AND DIVERTED TO MAJOR AIRPORT FOR BETTER RUNWAY CONDITIONS. CREW LANDED WITH NO FURTHER INCIDENT. INSPECTED ALL WIRING IN AREA OF PREVIOUS CHAFE, HYD POWER PACK AREA, WIRES AT CB & SUB PANEL, PCB, CONNECTOR & WIRES AT PCB, NO CHAFING OR ANY DAMAGE NOTED THAT WOULD HAVE CAUSED THE CB TO POP. REPLAC ED LANDING GEAR MOTOR RELAY PCB DUE TO GENERAL RELAY CONDITION AS A PRECAUTION, GEAR WAS CYCLED IN EXCESS OF 15 TIMES WI 2 L 7 2 4T RT A24CE 2007041300063 20070413 00063 NM 2007 4 13 AWXA200700466 1 20070404 A 5311 6520723506 FRAME BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - FORWARD CARGO COMPARTMENT DOOR CUT OUT, AFT FRAME CRACKED, BS 492.50, S24R AT LOWER STOP FITTING. REPAIRED FORWA RD CARGO COMPARTMENT DOOR CUT OUT, AFT FRAME, BS 492.50, S24R AT LOWER STOP FITTING IAW AWA ER 03-5300-07093-SS2. 2 L 7 2 4F RT A16WE 2007041300064 20070413 00064 NM 2007 4 13 AWXA200700467 1 20070323 A 5330 6545774106 SKIN BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - FUSELAGE SKIN CRACKED, BS 764, S25L. REPAIRED FUSELAGE SKIN, BS 764, S25L IAW B737-300 SRM 53-00-01-2R31. 2 L 7 2 4F RT A16WE 2007041300065 20070413 00065 NM 2007 4 13 AWXA200700468 1 20070312 A 5340 69429494 ATTACH FITTING BOEING 737 7373G7 1384595 NM ZONE 100 BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - AFT CARGO COMPARTMENT FRAME TO WEB ATTACH CLIP IS BROKEN, BS 807, S25R. REPLACED AFT CARGO COMPARTMENT FRAME TO WEB ATTACH CLIP, BS 807, S25R IAW B737-300 SRM 51-40-02 2 L 7 2 4F RT A16WE 2007041300066 20070413 00066 NM 2007 4 13 AWXA200700469 1 20070309 A 5330 654577572 SKIN BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - FUSELAGE SKIN CRACKED, BS 884, S23R - S24R. REPAIRED FUSELAGE SKIN, BS 884, S23R - S24R IAW AWA ER 03-5300-07094- ES2. 2 L 7 2 4F RT A16WE 2007041300067 20070413 00067 NM 2007 4 13 AWXA200700470 1 20070309 A 5330 6552988 SKIN BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - FUSELAGE SKIN CRACKED, BS 989, S17L, WL 280, AT L2 DOOR SURROUND UPPER AFT CORNER FASTENER HOLE. REPAIRED FUSELAG E SKIN CRACKED, BS 989, S17L, WL 280, AT L2 DOOR SURROUND UPPER AFT CORNER FASTENER HOLE IAW B737-300 SRM 53-00-01 FIGUR E 201. 2 L 7 2 4F RT A16WE 2007041300068 20070413 00068 NM 2007 4 13 AWXA200700471 1 20070312 A 5320 65176856 INTERCOSTAL BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - CRACKED INTERCOSTAL STRAP (TIE), BS 348.2, S16L. REPLACED INTERCOSTAL STRAP (TIE), BS 348.2, S16L IAW AWA ER 03-5 312-07093-SS4. 2 L 7 2 4F RT A16WE 2007041300069 20070413 00069 NM 2007 4 13 AWXA200700472 1 20070312 A 5340 69482042 ATTACH FITTING BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - CRACKED FRAME VERTICAL CLIP, BS 360, S14L - S15L. REPLACED FRAME VERTICAL CLIP, BS 360, S14L - S15L IAW AWA ER 03 -5312-07093-SS4. 2 L 7 2 4F RT A16WE 2007041300070 20070413 00070 NM 2007 4 13 AWXA200700473 1 20070312 A 5320 69265552 INTERCOSTAL BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - CRACKED INTERCOSTAL UPPER CLIP, BS 348.2, S16L. REPLACED INTERCOSTAL UPPER CLIP, BS 348.2, S16L IAW AWA ER 03-531 2-07093-SS4. 2 L 7 2 4F RT A16WE 2007041300071 20070413 00071 NM 2007 4 13 AWXA200700474 1 20070312 A 5320 69165096 INTERCOSTAL BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - CRACKED INTERCOSTAL LOWER CLIP, BS 348.2, S16L. REPLACED INTERCOSTAL LOWER CLIP, BS 348.2, S16L IAW AWA ER 03-531 2-07093-SS4. 2 L 7 2 4F RT A16WE 2007041300072 20070413 00072 NM 2007 4 13 AWXA200700475 1 20070312 A 5320 6517684629 INTERCOSTAL BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - CRACKED INTERCOSTAL WEB, BS 294.5, S8L. REPLACED INTERCOSTAL WEB, BS 294.5, S8L IAW AWA ER 03-5312-07093-SS4. 2 L 7 2 4F RT A16WE 2007041300073 20070413 00073 NM 2007 4 13 AWXA200700476 1 20070315 A 5340 6916970501 ATTACH ANGLE BOEING 737 7373G7 1384595 NM ZONE 200 - FUSEL CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - CRACKED FRAME ATTACH ANGLE (CLIP), BS 348, S15L. REPLACED FRAME ATTACH ANGLE (CLIP), BS 348, S15L IAW AWA ER 03-5 312-07093-SS4. 2 L 7 2 4F RT A16WE 2007041300074 20070413 00074 WP 2007 4 13 070088 1 20070405 A 2700 UNKNOWN DOUG DC9 DC983 3022083 WP UNKNOWN A WX0A O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 WP 19 865GA 49998 FLIGHT 479 FAR/LAS - THE FLIGHT CREW REPORTED THAT AT 250KIAS, AERODYNAMICALLY "CLEAN", THE 'ELEVATOR POWER ON' ANNUNCIA TOR ILLUMINATED MOMENTARILY. SIMULTANEOUSLY, THERE WAS A "JOLT" TO THE AIRPLANE. THE FLIGHT CONTINUED TO LAS, THE FLIG HT CREW MADE NO MENTION OF ANY PROCEDURE PERFORMED, WHERE IT LANDED WITHOUT FURTHER REPORTED INCIDENT. LAS VEGAS MAINTE NANCE REPORT AN ACCEPTABLE OPERATIONAL CHECK OF THE ELEVATOR POWER SYSTEM PER AMM27-30-07, AN ACCEPTABLE AUTO PILOT SYST EM OPERATIONAL CHECK PER AMM22-01-05 AND AN ACCEPTABLE OPERATIONAL CHECK OF THE HORIZONTAL STABILIZER TRIM SYSTEM PER AM M 27-40-00. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007041300075 20070413 00075 WP 2007 4 13 070089 1 20070406 A 3411 PITOT LINE DOUG DC9 DC982 3022082 WP DISCONNECTED A WX0A A UNSCHED LANDING G S MULTIPLE FAILURE AFFECT SYSTEMS CR CRUISE 1 WP 19 887GA 49932 FLIGHT 707 SFB/DSM. THE FLIGHT CREW REPORTED THE LOSS OF CAPT'S ALTIMETER, MACH/AIRSPEED INDICATOR, EPR BUGS AND AUTO T HROTTLE. 'NO MODE DISPLAY ON THRUST RATING PANEL. THE FLIGHT RETURNED WHERE IT LANDED WITHOUT FURTHER INCIDENT. MAINT ENANCE REPORT THAT THE PITOT LINE WAS FOUND DISCONNECTED FROM THE CADC NR 1 AT THE QUICK DISCONNECT. ATTACHED PITOT LIN E TO NR 1 CADC PER AMM34-16-01. A SATISFACTORY OPERATIONAL CHECK OF CADC NR 1 WAS ACCOMPLISHED PER AMM 34-16-00. A SAT ISFACTORY AUTO PILOT RTS CHECK PER AMM22-01-05 WAS ACCOMPLISHED. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007041300076 20070413 00076 NM 2007 4 13 QXEA200700532 1 20070323 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 472-484 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - SCRATCHES ON SEAT TRACK NR 5 BETWEEN STATION 472 AND 484. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2007041300077 20070413 00077 NM 2007 4 13 KCSA071110 1 20070402 A 5340 FITTING BOEING 747 747236B 1384804 NM BS 1241 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 LEFT UPPER WING TO BODY KICK FITTING AT STA 1241 HAS CORROSION AROUND HOLES. 2 L 7 4 4F A20WE 2007041300078 20070413 00078 WP 2007 4 13 IXXA07SMN088S 1 20070208 A 5330 SKIN DOUG DC8 DC862 3021970 WP ZONE 200 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT UPPER SKIN CORRODED AT STATION XFS1730.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, T REATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW DC8 SRM 53-2-1 FIGURE 7 SHEET 1 AND 5, DC8 SRM 51-1-21, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 53-2-0 PAGE 2P, DC8 SRM 53-5-2 FIGURE 1 ITEM "B", DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-20D AND DC8 SRM 51-3-1. 2 L 7 4 4F 4A25 2007041300079 20070413 00079 EA 2007 4 13 QXEA200700546 1 20070327 A 5320 DRAIN PAN CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - FOUND FS 280 AT RBL 9 HAS A SUSPECTED CRACK COMING OUT OF FASTENER HOLE ATTACHING DRAIN PAN. REPAIRED IAW SRM 51-40-11, 51-42-06. 2 L 7 2 4F RT A21EA 2007041300080 20070413 00080 EA 2007 4 13 QXEA200700549 1 20070328 A 5320 ANGLE CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - FS 280 AFT SIDE BETWEEN LBL 9 AND RBL 9 PREVIOUS REPAIR ANGLE HAS SUSPECT CRACK IN RADIUS. REPAIRED IAW SRM 51 -42-06. 2 L 7 2 4F RT A21EA 2007041300081 20070413 00081 WP 2007 4 13 IXXA07SMN111S 1 20070223 A 5522 SKIN DOUG DC8 DC862F 3021972 WP ZONE 300 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION FOUND LEFT HAND. ELEVATOR UPPER SKIN CORRODED AT STATION XE65.158. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND INTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYS OL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS FRO M STATION XAR0.000 TO XE132.000. BALANCED ELEVATOR. FOUND WITHIN LIMITS, MOMENT:1521.12 IN-LBS. IAW DC8 SRM 51-1-8 PAG ES 17-18, DC8 SRM 55-2-0 PAGE 12, DC8 SRM 55-1-0 PAGE 1, DC8 SRM 55-4-1 FIGURE 1 SHEET 1-2 ITEM "E" AND "F", DC8 SRM 51- 1-9 TR NUMBER 51-142 DATED 04-05-06, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-21 AND DC8 SRM 51-4-4 PAGES 1-3. 2 L 7 4 4F 4A25 2007041300087 20070413 00087 NM 2007 4 13 QXEA200700534 1 20070328 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - THERE ARE SEVERAL AREAS OF CORROSION ALONG THE CARGO FLOOR SUPPORT ANGLE, FOR FLOORBOARD NR 144AZ, AT STATION X 600.00 AND Z99.00. REPAIRED IAW SRM 51-40-11, 51-20-11, 51-20-36. 2 H 7 2 4T RT A13NM 2007041300116 20070413 00116 EA 2007 4 13 A6WA200740123 1 20070310 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 453AW 7838 RT WING PLANK ACCESS HOLE NR6 HAS MINOR PITTING IN CRITICAL AND NOT CRITICAL AREAS. MAINTENANCE REPAIRED RT WING PLANK ACCESS HOLE NR6 UNDER FUEL ACCESS PANEL 640 DB IAW REO 601R-57-21-030 REV D AND AWAC E06/021-457. (K) 2 L 7 2 4F RT A21EA 2007041600003 20070416 00003 NM 2007 4 16 F3LA200700072 1 20070409 A 5315 FLOORBEAM AIRBUS A319 A319111 3930336 NM GE CF700 CF7002D2 30010 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION IN AND AROUND FASTENER HOLES WHERE FLOORBEAM Y1292 ATTACHES TO FR68. REMOVED AND REPLACED FLOORBEAM ASSY. IAW A319 SRM 51-42-11. 2 L 7 2 4F 4 F RT A28NM E7EA 2007041600004 20070416 00004 WP 2007 4 16 070094 1 20070411 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 876GA 53469 DURING A ROUTINE OVERNIGHT SERVICE CHECK, MAINTENANCE INSPECTION, MAINTENANCE REPORTED THAT THE CEILING EMERGENCY LIGHTS BETWEEN FUSELAGE STATIONS 1133 AND 1171 WOULD NOT TEST. FURTHER REPORT THE REMOVAL AND INSTALLATION OF AN EMERGENCY LI GHT POWER SUPPLY BATTERY PACK AT FUSELAGE STATION 1190R. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED IAW AMM 33-5 3-00. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A6WE E9NE 2007041600008 20070416 00008 NM 2007 4 16 HALA0700166 1 20070411 A 2741 TRIM SYSTEM BOEING 767 767300 1385204 NM GE CF6 CF680 30025 NE STAB MALFUNCTIONED A HALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 13 598HA 23278 ETOPS SIGNIFICANT SYSTEM - STAB TRIM LEVERS SPLIT IN CLIMB AND IN CRUISE .5 INCH./RIGGED STAB TRIM LEVERS IAW AMM 27-41- 00 5639. C/W STAB TRIM CONTROL OPS TEST IAW MM 27-41-00-715-251. 2 L 7 2 4F 4 F RT A1NM E13NE 2007041600009 20070416 00009 EA 2007 4 16 QXEA200700563 1 20070329 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE BS 296 S18R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC-LIGHTNING STRIKE DAMAGE AT STRINGER 18R 7.5 INCH AFT OF FS 296.00. REPAIRED IAW REO670-53-21-257 AND SRM 51-42-06 . 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007041600010 20070416 00010 CE 2007 4 16 DATA200700002 1 20070411 A 5210 5043001811 DOOR BEECH 90 65A90 1152908 CE PWA PT6 PT6* 52043 EA MAIN PAX DISLODGED E DATA B EMER. DESCENT O OTHER CL CLIMB 1 GL 13 140PA LJ297 CLIMBING OUT, AROUND 17000 FEET, LOUD BANG AND RAPID DECOMPRESSION. MAIN CABIN DOOR BLEW OPEN BUT STAYED ATTACHED TO THE AIRCRAFT. DECLARED EMERGENCY LANDING. REPLACED MAIN DOOR ASSEMBLY. FURTHER STRUCTURAL INSPECTIONS TO BE ACCOMPLISHED A T MAJOR MAINTENANCE BASE. 1 L 7 2 3T 3 T 3A20 E2NE 2007041600011 20070416 00011 NM 2007 4 16 F3LA200700076 1 20070330 A 3220 ATTACH FITTING AIRBUS A319 A319111 3930336 NM GE CF700 CF7002D2 30010 NE NLG CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED INTERNAL CASTING AND THROUGH PIN BUSHING ON NLG UPPER TORSION LINK LUG CORRODED. REMOVED CORROSION AT UPPER TORSION LINK. TREATED, CAD PLATED AND REINSTALLED BUSHINGS IAW EA A9-32R-11842. 2 L 7 2 4F 4 F RT A28NM E7EA 2007041600014 20070416 00014 EA 2007 4 16 TRAX200700476 1 20070406 A 2750 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS UNKNOWN A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 920EV 7810 FLAPS FAIL CAUTION WHEN FLAPS SELECTED TO 8 STAYED AT 0 THE WHOLE TIME (EMERGENCY DECLARED). 2 L 7 2 4F 4 F RT A21EA E15NE 2007041600015 20070416 00015 NM 2007 4 16 USAA200704003 1 20070410 A 5512 SKIN BOEING 737 7374B7 1384702 NM GE CFM56 CFM56* 13802 NE HORIZONTAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 457UW 25021 2.5 INCH CRACK FOUND AT LOWER SKIN AT STAB ST. 98-100 (TE). INSTALLED DOUBLER IAW EA 98607 AND TR 55-10-07B. 2 L 7 2 4F 4 F RT A16WE E2GL 2007041600016 20070416 00016 SO 2007 4 16 RAIA00703074 1 20070320 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT BURNED OUT A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 822HK 145069 PRE FLT NR 5465-STL-AISLE FLOOD LIGHT AFT INOP. MAINTENANCE REMOVED AND REPLACED BULB. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007041600017 20070416 00017 NM 2007 4 16 USAA200704002 1 20070410 A 5330 SKIN BOEING 737 7374B7 1384702 NM GE CFM56 CFM56* 13802 NE BS 944 S24L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 457UW 25021 1.25 INCH CRACK FOUND ON SKIN AT STA 944 AND S-24L. REPAIR: INSTALLED DOUBLER IAW EA 98606. 2 L 7 2 4F 4 F RT A16WE E2GL 2007041600018 20070416 00018 NM 2007 4 16 SB07027 1 20070412 A 3350 1012721 LIGHT BOEING 737 737401 1384701 NM CFMINT CFM56 CFM563B2 13802 EU SEAT 20C INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 23885 MAINTENANCE REPORTED THE EMERGENCY LIGHT ON SEAT 20C INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. O PERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041600019 20070416 00019 NM 2007 4 16 SWAA071777 1 20070409 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 LEFT OVERWING EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007041600020 20070416 00020 NM 2007 4 16 SWAA071785 1 20070410 A 5524 18A80101 BOLT BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED C2 CHECK, LEFT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED INBOARD PUSHROD BOLT PER MM. 2 L 7 2 4F RT A16WE 2007041600021 20070416 00021 NM 2007 4 16 SWAA071781 1 20070409 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007041600026 20070416 00026 EA 2007 4 16 A6WA200740152 1 20070319 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 615 GROUND DAMAGE A A6WA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 432AW 7257 LAV TRUCK HIT AC - 4 INCH HOLE IN FUSELAGE FS 615, WL 73. MAINTENANCE PERFORMED A MAJOR REPAIR BY CUTTING AWAY DAMAGED SKIN AND INSTALLING A 14 INCH X 8 INCH EXTERNAL REPAIR DOUBLER IAW EO 601R-11202. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041600027 20070416 00027 EA 2007 4 16 A6WA200740153 1 20070313 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 421ZW 7346 UPON FLAP SELECTION, FLAP FAIL MESSAGE APPEARED 8 DEGREES FLAP NOTED. (K) [06-13-07] REMOVED/REPLACED FLEX DRIV ESHAFT SER NR 12973 TSN 25 CSN 23. REMOVED AND REPLACED FECU SER NR 1354 TSN 6945 CSN 6437. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041600030 20070416 00030 NM 2007 4 16 2007UALA00995 1 20070402 A 5246 ACCESS DOOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FWD LAV DUMP CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 FWD LAV DUMP ACCESS DOOR CUTOUT, FWD LAND IS CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041600031 20070416 00031 NM 2007 4 16 2007UALA00996 1 20070402 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 L1 DOOR UPPER GATE IS CRACKED AND CORRODED EXCESSIVELY. [06-14-07] REPLACED UPPER GATE ASSY. THIS IRREGULARITY IS ATTRIBUTED TO A UNFAVORABLE ENVIRONMENT LEADING TO CORROSION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041600033 20070416 00033 NM 2007 4 16 2007UALA00999 1 20070402 A 3397 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 551UA 25399 EEL STRIP AT MID LAV INOPERATIVE. SECURED EEL CONNECTION. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041600035 20070416 00035 NM 2007 4 16 2007UALA01001 1 20070402 A 3350 BATTERY PACK BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 225UA 30554 PASSENGER ENTRY DOOR 2R, EPAS BATTERY PACK GREEN TEST LIGHT NOT ON. [SUP 5-1-07] INSTALLED NEW BATTERY . GREEN TEST L IGHT ILLUMINATES. DOOR EPAS & AIRCRAFT READY FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007041600039 20070416 00039 2007 4 16 2007UALA01005 4 20070330 A 2565 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 301UA 23642 SLIDE PACK 1L HAS EXCESS FABRIC BELOW GIRT BAR DRAGGING ON FLOOR. [SUP 5-1-07] REPACKED BOTTOM SECTION OF SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041600040 20070416 00040 EU 2007 4 16 2007UALA01007 1 20070401 A 2910 LINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN SYSTEM LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 441UA 751 FLIGHT DIVERTED DUE TO LOSS OF GREEN HYD SYSTEM. A/C TOWED TO GATE. [SUP 06-01-07] FOUND A CRACKED HYDRAULIC LINE LEA DING TO THE THRUST REVERSER MANUAL ACTUATION CONTROL VALVE IN THE NR 1 ENGINE PYLON. MANUFACTURED AND INSTALLED A NEW LI NE. REPLACED HP AND PUMP CASE DRAIN FILTERS AS A PRECAUTION. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041600041 20070416 00041 NM 2007 4 16 2007UALA01008 1 20070402 A 2910 LINE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HYD SYSTEM LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 325UA 23957 DIVERTED FLIGHT UNDER AMBER ALERT DUE TO LOSS OF A-HYDRAULIC SYSTEM. [07-10-07] FOUND LEAKING HYDRAULIC RETURN LINE UN DER LEFT WING, FORWARD OF INBOARD FLAP. REPLACED HYDRAULIC LINE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041600043 20070416 00043 SO 2007 4 16 CHQA200700010 1 20070407 A 7500 403039205D O-RING EMB 145 EMB145LR 3260212 SO BLEED SYSTEM BROKEN A CHQA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 11 572RP 14500828 FLIGHT 6218 - CVG-CMH - ON DESCENT INTO CMH, RECEIVED NR 2 ENGINE BLEED LEAK. SHUT OFF ENGINE PER QRH. INTERMITTENTLY IN AND OUT OF ICING CONDITIONS, SHUTTING OFF THE BLEED CAUSED THE WING ANTI-ICE TO FAIL. DECLARED AN EMERGENCY. MAINTE NANCE FOUND LEAK AT JOINT S0237. REMOVED AND REPLACED BROKEN O-RING IAW MM 36-11-05. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007041600044 20070416 00044 EA 2007 4 16 A6WA200740178 1 20070331 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 457AW 7854 RT FS 484.0 INTERCOSTAL CRACKED AT RBL 36.0 APPROX .1 INCH LONG AT FLOOR SUPPORT BEAM. (K) [SUP 5-9-07] MAINTENANCE CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR FLANGE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BSC SR 601R-53-0030A. (M ) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041600045 20070416 00045 WP 2007 4 16 N865R623002 1 20070315 A 5312 BULKHEAD DOUG DC8 DC863F 302198F WP BS 1766 L11L CRACKED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 46088 AFT FLAT PRESSURE BULKHEAD WEB STA 1766 L11L CRACK CPCP 5730 0551. 2 L 7 4 4F 4A25 2007041600046 20070416 00046 WP 2007 4 16 N865F624003 1 20070313 A 5312 BULKHEAD DOUG DC8 DC863F 302198F WP BS 1766 L11-12R CRACKED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 46088 AFT FLAT PRESSURE BULKHEAD WEB STA 1766 L-11R-12R CRACK CPCP 5730 0551. 2 L 7 4 4F 4A25 2007041600047 20070416 00047 WP 2007 4 16 N865R1076007 1 20070323 A 5730 ACCESS DOOR DOUG DC8 DC863F 302198F WP LT WING CORRODED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 46088 LT WING XFS 836 OUTBD L/E INNER LOWER SECTION ACCESS DOOR NR 517B JAMB WITH CORROSION CPCP 107L 0552. 2 L 7 4 4F 4A25 2007041600048 20070416 00048 WP 2007 4 16 N865R1124005 1 20070326 A 5320 ANGLE DOUG DC8 DC863F 302198F WP FUSLEAGE CORRODED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 46088 COCKPIT SUBFLOOR ANGLE WITH CORROSION AT STA 32.000 L-21R CPCP455R 0552. 2 L 7 4 4F 4A25 2007041600051 20070416 00051 SO 2007 4 16 C2XA07CL037 1 20070408 A 3297 14521585403 WIRE HARNESS EMB 145 EMB145LR 3260212 SO LT MLG SHORTED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 15555 145594 CLE FLIGHT 2133 - THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT UNTIL THE DOWNLOCK RELEASE WAS USED ON THE LGEU. MAINTENANCE INSPECTED AND REPLACED THE LEFT WOW PROXIMITY SENSOR HARNESS. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007041600053 20070416 00053 EA 2007 4 16 A6WA200740158 1 20070315 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 415AW 7593 PAX DOOR AFT DRAG ANGLE IS CRACKED AT PAX DOOR ASST PULLEY BRACKET. (K) [SUP 06-05-07] CUTOUT DAMAGED SECTION AND REP AIRED IAW BOMBARDIER REO 601R-52-11-513 REV A AND BSC EO 601R-52-11280. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041600054 20070416 00054 NM 2007 4 16 F3LA200700058 1 20070330 A 5320 SUPPORT AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED LT SUPPORT FRAME CORRODED BETWEEN FR 69 AND FR 70, JUST BEHIND FLOORBEAM -Y1292. FOUND SUPPORT FRAME TO BE OUT OF LIMITS IAW A319 SRM 51-74-00. REMOVED AND REPLACED SUPPORT FRAME IAW A319 SRM 51-72- 11, PAGES 1 AND 2. 2 L 7 2 4F RT A28NM 2007041600055 20070416 00055 NE 2007 4 16 2007UALA01010 2 20070402 A 7532 SOLENOID AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE BLEED VALVE MALFUNCTIONED A UALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 493UA 1821 V11270 ENG 1 COMP STALL (LOUD BANG) 5000 FT ROLLED LEFT. [SUP 06-01-07] FOUND SEVERAL LOOSE LINES ON BLEED SOLENOID AND FAULT Y STAGE 7 BLEED VALVE. REPLACED VALVE, LUBED VARIABLE STATOR VANE MECHANISM AND TEST RAN ENGINE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041000145 20070410 00145 NM 2007 4 10 USAA070266 1 20070404 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 FLOORBEAM NUT PLATE HOLES, INTERCOSTAL, STA 967 RBL 50 - LBL 50 HAS CORROSION. FAB'D FILLER FOR INTERCOSTAL BECAUSE OF REPAIR STRAP ON BEAM PER SRM 53-60-5 TYP 53-15-01B; DEFECT SIZE: 100 INCHES. 2 L 7 2 4F RT A16WE 2007041000149 20070410 00149 NM 2007 4 10 USAA070262 1 20070404 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 727E S23L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 23380 FUSELAGE SKIN AT BS 727E, JUST ABOVE S-23L HAS CRACK. REMOVED DAMAGE & EXISTING REPAIR, FAB'D & INSTALLED DOUBLER & TRI PLER, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007041000150 20070410 00150 2007 4 10 ASMF200704001 4 20070404 A 3418 9650449002 COMPUTER DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE STALL WARNING FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 838AM 15972 49397 AIRCRAFT RETURNED TO PLATFORM DUE TO WHEN SELECTING FLAPS TO 19.5 DEGREES FOR TAKE-OFF, SLATS DISAGREE LIGHT REMAINED ON . AFTER MAINTENANCE INSPECTION, RT STALL WARNING COMPUTER WAS REPLACED IAW 34-19-02 AND TESTED IAW MM 27-81-00, ALL CORR ECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007041000155 20070410 00155 NM 2007 4 10 KCSA071113 1 20070404 A 5347 SEAT TRACK BOEING 747 747236B 1384804 NM BS 540-560 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 CORROSION ON UPPER DECK SEAT TRACK BETWEEN BS 540 AND BS 560, RBL 27. 2 L 7 4 4F A20WE 2007041000167 20070410 00167 WP 2007 4 10 07FDEA01320 1 20070404 A 5730 SKIN DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 RT WING L/E EXTERNAL SKIN FOUND 1 CRACK 1.5" LONG. REPAIRED SKIN IAW SRM 57-10-00 FIGURE 68 SHT 2 VOL 1. 2 L 7 3 4F A22WE 2007041000171 20070410 00171 WP 2007 4 10 07FDEA01324 1 20070404 A 5753 SKIN DOUG DC10 DC1010 3022110 WP TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 RT WING T/E DURING INSPECTION WITH EO 8-5100-7-5001 P2 FOUND 1 CRACK .25" LONG ON LOWER SKIN OF OUT'B FLAP. REPAIRED SK IN IAW SRM 57-00-01 FIGURE 4 SHT 2 VOL 1. 2 L 7 3 4F A22WE 2007041100016 20070411 00016 WP 2007 4 11 07FDEA01294 1 20070403 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP BS 495 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 RT AIR COND. COMP. CRACK 2" LONG ON EXTERNAL REPAIR ON VERTICAL BLKHD. REPAIRED IAW FEDEX E.A 8-5320-94639 PART 2. 2 L 7 3 4F A22WE 2007041100017 20070411 00017 EA 2007 4 11 A6WA200740176 1 20070331 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 457AW 7854 LT FS 484.0 ANGLE AT LBL 27.0 CRACKED APPROX .1 INCH LONG AT FLOOR SUPPORT BEAM. (K) [SUP 05-09-07] MAINTENANCE REMOV ED CRACKED ANGLE AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R-54-41-059 REV A AND BSC SR 601R-53-0029B. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041100020 20070411 00020 EA 2007 4 11 A6WA200740175 1 20070331 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 457AW 7854 LT FS 621.0 FLOOR SUPPORT ANGLE CRACKED APPROX .3 INCH LONG. (K) [SUP 05-01-07] MAINTENANCE CUT AWAY CRACKED ANGLE AN D INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R-53-61-117 REV C. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041200002 20070412 00002 EU 2007 4 12 2007UALA01054 1 20070405 A 2497 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 GENERATOR BURNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 456UA 1128 NR 2 GEN INOP, HAS BURNED PYLON CONNECTOR. [SUP 06-01-07] INSPECTED PYLON CONNECTOR AND FOUND PIN "C" BURNED IN CONNE CTOR & RECEPTICAL. REPLACED HARNESS AND NR 2 IDG AS A PRECAUTIONARY MEASURE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041200009 20070412 00009 NM 2007 4 12 2007UALA01041 1 20070405 A 5510 BUSHING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZONTAL STAB OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 RIGHT HORIZONTAL STAB FWD UPPER BUSHING MIGRATED. MAJOR REPAIR: REMOVED BUSHING, FABRICATED AND INSTALLED NEW BUSHING PER AAR EAI070223IR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041200019 20070412 00019 EU 2007 4 12 YENA2007024 1 20070406 A 2720 RUDDER EMB ERJ190 ERJ190100IGW 3260408 EU OUT OF RIG A YENA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 267JB 19000065 AFTER APPLICATION OF 40 PERCENT N1 ON TAKEOFF, AIRCRAFT RESPONDED OPPOSITE TO RUDDER INPUT. PRE-TAKEOFF FLIGHT CONTROL CHECK WAS GOOD. WITH ADDITIONAL INFORMATION FROM EMBRAER ENGINEERING REGARDING RUDT ALIGNMENT MARKINGS (INDEXES) ACCOMP LISHED RIGGING OF CAPTS & F/O'S RUDDER PEDALS PER MM 32-53-03, OPS CHECK OKAY. ALSO PERFORMED TAXI CHECK. TAXI CHECK W AS OK. 2 L 7 2 4F RT A57NM 2007041200029 20070412 00029 CE 2007 4 12 AMW070326046 1 20070403 A 5320 10164001111 ANGLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA FUSELAGE CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 133YV UE133 ANGLE 101-640011-11 AT CSS 69.184 AT APPROX 10.5 PERCENT CRACKED APPROX .5-1 INCH RADIATING OUT FROM THE FASTENER ON EAC H END TO THE EDGE OF ANGLE. ANGLE 101-640011-3 HAS ONE HOLE ELONGATED. REPAIRED IAW REPAIR DWG 1900D13302 REV 1R. 2 L 7 2 4T 3 T RT A24CE E2NE 2007041200031 20070412 00031 EA 2007 4 12 QXEA200700522 1 20070406 A 2721 CC670511143 CONTROL PANEL CNDAIR CL600 CL6002C10 1390015 EA RUDDER TRIM MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 290RB 10029 PDX - FLIGHT 2563, ON PUSHBACK THE RUDDER TRIM MOVED FULL SCALE LEFT. RETURNED TO THE GATE. MAINTENANCE REPLACED THE T RIM CONTROL PANEL AND THE DCU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007041200040 20070412 00040 NM 2007 4 12 07FDEA01312 1 20070404 A 5315 ADA84049 FLOORBEAM DOUG MD11 MD11F 3023600 NM BS 939 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 MAIN DECK CARGO FLOORBEAM LOWER FLANGE AT STA 939 X=-82 FOUND DENTED. [SUP 4-20-07] COMPLIED WITH FEDEX E.A. 1-5310-109 846 PART 1. 2 L 7 3 4F RT A22WE 2007041200047 20070412 00047 NM 2007 4 12 SPAA0700092 1 20070409 A 3350 110049 POWER SUPPLY BOEING 737 7372T4 1384492 NM PWA JT8 JT8D17 52049 NE EMERGENCY LIGHT INOPERATIVE A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 FORWARD SECTION OF FLOORTRACK ESCAPE PATH LIGHTING INOP. REPLACED POWER SUPPLY AND FUNCTIONALLY TESTED SATISFACTORY IAW CMM. 2 L 7 2 4F 4 F A16WE E2EA 2007041200048 20070412 00048 CE 2007 4 12 DXTA200702095 1 20070409 A 3411 PITOT TUBE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL PITOT STATIC OBSTRUCTED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 921QS 7500241 INFLIGHT, WHEN APU WAS SHUTDOWN AT ABOUT 15,000 FT MSL, THE (MACH TRIM OFF) (AMB) AND (YD LOWER OFF) AMBER MSGS ILLUMINA TED. CHECKLIST PROCEDURES WERE USED TO NO AVAIL. DURING DESCENT TO LAND, AT ABOUT 3000 FT MSL, THE (MACH TRIM OFF) MSG WENT AWAY. SHORTLY, THEREAFTER THE (YD LOWER OFF) MSG WENT AWAY. [SUP 4-19-07] SHORTLY, THEREAFTER THE "YD LOWER OFF" MSG WENT AWAY. FOUND DEBRIS IN LT AND RT PITOT TUBES. DISCONNECTED TUBES AND CLEANED. COMPLIED WITH "PITOT/STATIC SYS TEM LEAK CHECK IAW FAR 91.411, 4/09/07. WORK IAW CESSNA 750 M/M CHAP 34-11-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007041200053 20070412 00053 NM 2007 4 12 07FDEA01363 1 20070405 A 5314 65C337511 KEELBEAM BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 LOWER AFT PIT BILGE, STA 950E 10, LBL 8" O/B LWR FLANGE OF KEEL BEAM CHORD HAS CORROSION, ON PREVIOUS STRAP REPAIR. R EMOVED FLOOR SUPPORT AND SHEAR TIE FOR ACCESS, GROUND CORROSION ON EXISTING STRAP AND NDT FOR MATERIAL LOSS. FOUND TO B E OUT OF LIMITS. FABRICATED NEW REPAIR STRAP AND REPLACED SHEAR TIE AND FLOOR SUPPORT REF EA NR 7-5310-107011 PART 1. 2 L 7 3 4F A3WE 2007041200054 20070412 00054 NM 2007 4 12 07FDEA01365 1 20070405 A 5320 6519606 WEB BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 MAIN DECK FLOOR WEB UPPER SURFACE IS CORRODED BS 1147, LBL 52-63, WL 208. REMOVED DAMAGE AREA OF WEB REF SRM 51-40-2 FI G 1, STA 1147, LBL 62, THAT WAS OUT OF LIMITS REF 51-10-1, AFTER BLENDING, MFG AND INSTALLED REPAIR REF SRM 51-40-2 FIG 1 AT LBL 62 2 L 7 3 4F A3WE 2007041200075 20070412 00075 NM 2007 4 12 07FDEA01357 1 20070405 A 5310 ANGLE DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 CABIN, RT WEB ANGLE FOUND CRACKED AT STA 1219 LONGERON 27. REPAIRED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007041200080 20070412 00080 WP 2007 4 12 07FDEA01281 1 20070403 A 5720 CAP DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 RT WING L/E FOUND ONE CRACK 1" LONG ON FIXED CAP STA XORS 827. REPAIRED IAW SRM 57-10-00 FIG 49 VOL 1. 2 L 7 3 4F A22WE 2007041200089 20070412 00089 NM 2007 4 12 ARWA20070305 1 20070322 A 7830 1402302 CABLE DOUG DC10 DC1040F 3023507 NM THRUST REVERSER BROKEN A ARWA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 19 140WE 46920 ON TAKEOFF ROLL, NR 2 ENGINE REVERSER UNLOCK LIGHT CAME ON. ABORTED TAKEOFF AS SOON AS THROTTLES WERE ADVANCED. DEACTI VATED NR 2 ENGINE THRUST REVERSER AS PER MEL 78-1 (DDG) AFTER DEACTIVATION COMPLETED; CHECKED AT BLAST FENCE, VERIFIED S YSTEM AND FOUND NORMAL IN ACCORDANCE WITH M/M 71-00-00. NO LIGHT CAME ON AND M/M 78-00-00. THIS NR 2 REVERSER ENTERED ON DMI NR 20629 AS PER MEL 78-1 CATEGORY "C" (NOTE: LOCK OUT AND DEACTIVATED IN ACCORDANCE WITH DDG 78-1); REMOVED FLEX SHAFT RT ASSEMBLY AND REPLACED IN ACCORDANCE WITH M/M 78-32-07 CHECKED CABLES, FOUND PRIMARY CABLE BROKEN. REMOVED AND REPLACED CABLE ASSEMBLY, PERFORMED RIG CHECK PER M/M 78-31-16, PERFORMED TAKEOFF M/M 78-31-16, PERFORMED TAKEOFF RUN UP 2 L 7 3 4F RT A22WE 2007041200090 20070412 00090 NM 2007 4 12 07FDEA01362 1 20070405 A 5314 65C337511 KEELBEAM BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 LWR AFT PIT BILGE, STA 950A LBL 8" OB LWR FLANGE OF KEEL BEAM CHORD HAS APPROX 6 SQ INCHES OF CORROSION ON UPPER SURFACE . REMOVED CORROSION ON OUTBOARD FLANGE OF KEEL BEAM LWR AFT PIT BILGE STA 950A, 6" LBL 8" FOUND AREA OUT OF LIMITS. F ABRICATED, TREATED AND PRIMED REPAIR, STRAP/FILLER AND INSTALLED REF EO NR 7-5310-7-2356C1 PART 3, NOTE 1 OF FIG 3, PG 2 . 2 L 7 3 4F A3WE 2007041200095 20070412 00095 NM 2007 4 12 KCSA071105 1 20070331 A 5311 FRAME BOEING 747 7472B4B 138481B NM BS 560 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FORWARD BILGE FUSELAGE FRAME UPPER CHORD IS DAMAGED AT STA 560, LBL 55. 2 L 7 4 4F RT A20WE 2007041200097 20070412 00097 SO 2007 4 12 RAIA00703069 1 20070325 A 3350 BULB EMB 145 EMB145 3260210 SO EMERGENCY LIGHT BLOWN A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 821HK 145068 PRE FLT NR 5599 - STL - EMERGENCY LIGHT AT AFT CEILING EXIT LOCATOR INOP. MAINTENANCE REPLACED THE BULB AT THE EMERGENC Y LIGHT IN CEILING. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007041200098 20070412 00098 SO 2007 4 12 RAIA00703073 1 20070328 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DIRTY A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 833HK 145240 PRE FLT NR 8010 - STL - EMERGENCY LIGHT AT LEFTHAND OVERWING EXIT MARKER IS INOP. MAINTENANCE CLEANED ELECTRICAL CONNEC TION AND OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT T00011AT 2007041200101 20070412 00101 SO 2007 4 12 RAIA00703070 1 20070326 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT UNSECURE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 822HK 145069 PRE FLT NR 5564 - STL - EMERGENCY LIGHT AT FLOOR PROXIMITY LIGHT INOP. MAINTENANCE RESECURED WIRING TO FLOOR PROXIMITY LIGHT. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007041200139 20070412 00139 NM 2007 4 12 07FDEA01383 1 20070410 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 CORROSION FOUND ON SEAT TRACK AT STA 1871 X = -8.5, DISCOVERED AFTER REMOVAL OF FLOOR PANEL FOR ACCESS. [SUP 4-20-07] REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007041200144 20070412 00144 EU 2007 4 12 07FDEA01388 1 20070410 A 5720 A57242583 STIFFENER AIRBUS 310 A310324 3930206 EU ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CORROSION ON RT WING HINGE ARM FITTING AND TOP SKIN PANEL. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5722-103262 AND RAS/B AE/1003079/2006 ISSUE "A" (ALTERNATE MATERIAL DAN 26H30 IN PLACE OF 7150-T651 FOR STIFFENER A572-42583-203) AND RAS/BA E/1003026/2006 ISSUE "A" (CORROSION BLEND OUT). 2 L 7 2 4F RT A35EU 2007041200149 20070412 00149 EA 2007 4 12 A6WA200740160 1 20070327 A 5340 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSLEAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 416AW 7603 INTERCOSTAL SUPPORT FOR THE NR 1 HYDRAULIC PRESSURE/RETURN FILTERS AS CRACKED APPROX .2 INCH AT THE LOWER AFT CORNER. ( K) [SUP 05-09-07] MAINTENANCE REPAIRED SUPPORT IAW BSC EO 601R-53-11285 BY CUTTING OUT CRACK, LPI TO ENSURE CRACK REMO VED, PRIME AND PAINT. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041200150 20070412 00150 EA 2007 4 12 A6WA200740161 1 20070327 A 5340 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 718 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 416AW 7603 INTERCOSTAL SUPPORT FOR THE NR 2 HYDRAULIC PRESSURE/RETURN FILTERS IS CRACKED APPROX .2 INCH AT THE LOWER AFT CORNER. ( K) [SUP 05-09-07] MAINTENANCE REPAIRED SUPPORT IAW BSC EO 601R-53-11285 BY CUTTING OUT DAMAGE, LPI TO ENSURE CRACK REM OVED, PRIME AND PAINT. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041200154 20070412 00154 NM 2007 4 12 KCSA071136 1 20070410 A 5412 BULKHEAD BOEING 747 747212B 1384886 NM NR 4 NACELLE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 NR 4 PYLON NAC STA 221.9 BULKHEAD UPPER CHORD CRACKED IN RADIUS. 2 L 7 4 4F A20WE 2007041200169 20070412 00169 EU 2007 4 12 07FDEA01410 1 20070410 A 5310 FAILSAFE AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CORROSION ON LT FWD PAX DOOR FAIL/SAFE RING UPPER HALF. REPAIR PERFORMED BY REWORK AND OVERSIZING IAW EA 6-5312-101257 AND RAS 044737/013/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007041200170 20070412 00170 EU 2007 4 12 07FDEA01411 1 20070410 A 5310 FAILSAFE AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CORROSION ON RT FWD PAX DOOR FAIL/SAFE RING UPPER HALF. REPAIR PERFORMED BY REWORK AND OVERSIZING IAW EA 6-5312-101257 AND RAS 044737/013/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007041200198 20070412 00198 NM 2007 4 12 SWAA071759 1 20070406 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM BS 787 S23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 23L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007041300003 20070413 00003 EU 2007 4 13 07FDEA01456 1 20070412 A 5730 SKIN AIRBUS 310 A310 EU PWA 4152 PW4152 NE ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 ELONGATED HOLES AT PYLON SUPPORT BRACKET AND BOTTOM OF RT WING SKIN. REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATIO N IAW. EA 6-5720-101304 AND RAS/BAE/1002914/2006 ISSUE (A). 2 L 7 2 4F RT A35EU E24NE 2007041300004 20070413 00004 EU 2007 4 13 07FDEA01457 1 20070412 A 5532 A55371660012 PANEL AIRBUS 310 A310 EU PWA 4152 PW4152 NE ZONE 300 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 DELAMINATION AT VERTICAL STABILIZER L/E PANEL NR 3. REPAIR WAS PERFORMED BY WET LAY-UP REPAIR IAW. SRM 51-77-12 / FIG.2 11, APPROVED BY EA 6-5532-101302 AND RAS/DAHAM/4020826/2006 ISSUE (A). 2 L 7 2 4F RT A35EU E24NE 2007041300005 20070413 00005 EU 2007 4 13 07FDEA01459 1 20070412 A 5313 A53611644220 LONGERON AIRBUS 310 A310 EU PWA 4152 PW4152 NE ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 CORROSION FOUND ON LONGERON A536-11644-220, C11-C14, Y 770. REPAIR PERFORMED BY REPLACEMENT OF PART IAW. SRM 51-72-10. 2 L 7 2 4F RT A35EU E24NE 2007041300006 20070413 00006 EU 2007 4 13 07FDEA01460 1 20070412 A 5347 A53911640200 SEAT TRACK AIRBUS 310 A310 EU PWA 4152 PW4152 NE ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 CORROSION ON SEAT TRACK, C15A-C19, Y-953. REPAIR PERFORMED BY REPLACEMENT OF PART IAW. SRM 71-52-10. 2 L 7 2 4F RT A35EU E24NE 2007041300007 20070413 00007 EU 2007 4 13 07FDEA01462 1 20070412 A 5313 LONGERON AIRBUS 310 A310 EU PWA 4152 PW4152 NE ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 CORROSION ON LONGERON C11-C15A, Y-1456. REPAIR PERFORMED BY T-SPLICE REPAIR IAW SRM 53-12-15 / FIG.207. 2 L 7 2 4F RT A35EU E24NE 2007041300008 20070413 00008 EU 2007 4 13 07FDEA01463 1 20070412 A 5313 LONGERON AIRBUS 310 A310 EU PWA 4152 PW4152 NE ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 CORRODED LONGERON C12A-C14, Y1959. REPAIR PERFORMED BY T-SPLICE REPAIR IAW. SRM 53-12-15 / FIG 207. 2 L 7 2 4F RT A35EU E24NE 2007041300009 20070413 00009 WP 2007 4 13 ABXA070091 1 20070409 A 3350 60030451 POWER SUPPLY DOUG DC9 DC941 302207N WP PWA JT8 JT8D15 52051 NE EMERGENCY LIGHT DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 951AX 3293 47616 EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW MM 33-53-02-4. 2 L 7 2 4F 4 F A6WE E2EA 2007041300010 20070413 00010 WP 2007 4 13 ABXA070090 1 20070407 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP PWA JT8 JT8D15 52051 NE EMERGENCY LIGHTS DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 EMERGENCY LIGHTS WOULD NOT STAY ON. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW MM 33-53-00. 2 L 7 2 4F 4 F A6WE E2EA 2007041300011 20070413 00011 EU 2007 4 13 07FDEA01464 1 20070412 A 5313 LONGERON AIRBUS 310 A310 EU PWA 4152 PW4152 NE ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 CORRODED LONGERON C11-C15A, Y-450. REPAIR PERFORMED BY T-SPLICE REPAIR IAW. SRM 53-12-15 / FIG.207. 2 L 7 2 4F RT A35EU E24NE 2007041300012 20070413 00012 EU 2007 4 13 07FDEA01466 1 20070412 A 5315 FLOORBEAM AIRBUS 310 A310 EU PWA 4152 PW4152 NE ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 CORRODED TOP CAP FLOORBEAM AT C33 LT. REPAIR PERFORMED BY SPLICING IAW SRM 53-10-15 / FIG.207. 2 L 7 2 4F RT A35EU E24NE 2007041300013 20070413 00013 EU 2007 4 13 07FDEA01468 1 20070412 A 5313 A53610607206 STRINGER AIRBUS 310 A310 EU PWA 4152 PW4152 NE ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 CORRODED STRINGER P44 LT AND RT, C16A-C17. STRINGER REPAIR PERFORMED IAW. SRM 53-12-14 / FIG.201. (RUN OUT FITTING INS TALLATION; PN A536-10607-206, -207) 2 L 7 2 4F RT A35EU E24NE 2007041300014 20070413 00014 EU 2007 4 13 07FDEA01470 1 20070412 A 5230 A52378000036 SKIN AIRBUS 310 A310 EU PWA 4152 PW4152 NE ZONE 800 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 OLD DENT ON BULK CARGO DOOR LOWER LT CORNER WITH RAS/DATLS/0002170/2004 WITH TEMPORARY LIMIT OF ONE UNPRESSURIZED FERRY FLIGHT. PERMANENT REPAIR PERFORMED BY DOUBLER INSTALLATION IAW. EA 6-5234-101283 AND RAS/DABRE/7006682/2006 ISSUE (A) . 2 L 7 2 4F RT A35EU E24NE 2007041600028 20070416 00028 NM 2007 4 16 PIDA07017 1 20070403 A 3350 6104781 BATTERY PACK BOEING 737 737228 13844AG NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 252TR 23001 RIGHT OUTSIDE OVERWING AND AFT CARGO DOOR EMERGENCY EXIT LIGHTS ARE INOP. REPLACED BATTERY PACK IN RIGHT AFT CARGO SIDE WALL. OPS CHECKS GOOD PER MM 33-51-31. 2 L 7 2 4F RT A16WE 2007041600029 20070416 00029 EA 2007 4 16 A6WA200740163 1 20070328 A 5730 ACCESS PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 416AW 7603 LT LOWER WING PLANK FUEL ACCESS PANEL CUTOUT FOR FUEL PNL 540 CB HAS CORROSION IN NON-CRITICAL AREA APPROX 6.0 INCHES DE EP AND .020 WIDE. (K) [SUP 05-17-07] MAINTENANCE REPAIRED CORROSION BY BLENDING OUT CORROSION. PERFORMED NDT, ROTO P EENED AREA, SANDED REWORKED AREAS TO A SURFACE FINISH OF 63 MICRO INCHES. APPLIED CONVERSION COATING AND FUEL TANK COAT ING IAW BOMBARDIER REO 601R-57-21-030 REV F. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041600050 20070416 00050 WP 2007 4 16 N865F753008 1 20070319 A 5542 SKIN DOUG DC8 DC863F 302198F WP RUDDER CORRODED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 46088 RUDDER ZR 168.656 LT EXTERNAL SKIN WITH CORROSION CPCP 6820 0551. 2 L 7 4 4F 4A25 2007041600060 20070416 00060 EU 2007 4 16 2007UALA01015 1 20070403 A 5311 FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 432UA 587 FR27 HAS 1 EACH FRAME CLEAT WITH CORROSION BETWEEN STR 43R AND STR 44. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041600064 20070416 00064 EU 2007 4 16 2007UALA01020 1 20070404 A 3350 BR964421 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SEAT 7ABC INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 453UA 1001 CABIN SEAT 7ABC EMERGENCY ESCAPE PATH MARKING LIGHT IS INOPERATIVE. REPLACED LIGHT ASSY AND OP CHECKED ON WU U1013K. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041600065 20070416 00065 NM 2007 4 16 2007UALA01021 1 20070403 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 378 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 FWD LWR EXTERNAL FUSELAGE SKIN IS CRACKED AT EQ P COOLING EXHAUST PORT CUTOUT BS 378, LBL 2, WL 148. MAJOR REPAIR ACCOM PLISHED: STOP DRILLED CRACK. FABRICATED & INSTALLED EXTERNAL DOUBLER FROM BS 360-402. ALSO FABRICATED & INSTALLED EXT ERNAL RING DOUBLERS & SPACERS AT ANTENNA CUTOUT BS 410, 430, 450. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041600066 20070416 00066 NM 2007 4 16 2007UALA01022 1 20070403 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU ROW 15 AFT SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 308UA 23669 AFT CABIN EEL LIGHTS INOP FROM ROW 15 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT. F OUND EEL STRIP AT ROW 21 SHORTED, REPLACED STRIP AND SEALED TRACK COVER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041600069 20070416 00069 EA 2007 4 16 A6WA200740169 1 20070402 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 451AW 7832 LT FS 484.0 ANGLE CRACKED APPROX .1 INCH LONG AT PRESSURE FLOOR SUPPORT BEAM LBL 27.0. (K) [SUP 5-1-07] MAINTENANCE R EMOVED ANGLE AT FS 484 LT LBL 27 IAW CRJ 200 SRM 51-42-06 AND FABED A NEW ANGLE FROM S6144-14 EXTENSION AND INSTALLED NE W ANGLE IAW BSC SR 601R-53-0029B. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041600073 20070416 00073 EU 2007 4 16 2007UALA01024 1 20070404 A 3397 TERMINAL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMER LIGHT RELAY MISWIRED A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 464UA 1290 EMERGENCY LIGHTS WILL NOT TEST FROM AFT FLIGHT ATTENDANTS POSITION. [SUP 5-1-07] FOUND WIRE AT TERMINAL BLOCK 7222VT MI SWIRED. FOUND WIRE 1723 IN 3A AND 1724 IN 1H DISCONNECTED. CORRECTED WIRING. TRIED BORROWED PANEL AND GRD CHECKED NORMAL . 2 L 7 2 4F 4 F RT A28NM E40NE 2007041600074 20070416 00074 EU 2007 4 16 2007UALA01025 1 20070404 A 3350 321431 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 465UA 1341 ACFT FAILS EMERGENCY LIGHT TEST. CIDS PANEL DISPLAYS -EPSU EMERGENCY BATT L-. REPLACED EMERGENCY LIGHT BATTERY AT THE LEFT OVERWING EXIT DOORS. SYSTEM OPS CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041600077 20070416 00077 NM 2007 4 16 2007UALA01028 1 20070405 A 3350 794640 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY EEL LIGHT INOPERATIVE AT SEAT 1J AFT. SECURED CONNECTOR. OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041600078 20070416 00078 NM 2007 4 16 2007UALA01029 1 20070404 A 5310 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 R-2 DOOR FORWARD FRAME AT UPPER HINGE CUTOUT NEEDS ATTENTION. ACCOMPLISHED INSTALLATION OF STEEL DOUBLER REPAIR AS A PR EVENTIVE MAINTENANCE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041600079 20070416 00079 NM 2007 4 16 2007UALA01030 1 20070404 A 5310 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 L-2 DOOR FORWARD FRAME AT UPPER HINGE CUTOUT NEEDS ATTENTION. ACCOMPLISHED INSTALLATION OF STEEL DOUBLER REPAIR AS A PR EVENTIVE MAINTENANCE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041600080 20070416 00080 NM 2007 4 16 2007UALA01031 1 20070404 A 3350 1317 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 582UA 26702 EMERGENCY SLIDE LIGHT INOP AT DOOR 4L. *S/D* RELAMPED WITH 767 LAMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041600081 20070416 00081 NM 2007 4 16 2007UALA01033 1 20070404 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 EMERGENCY LIGHT FLOORSTRIP AT 10 E&F IS DAMAGED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007041600082 20070416 00082 NM 2007 4 16 2007UALA01034 1 20070404 A 3800 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE UNKNOWN A UALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 29 516UA 24860 NO POTABLE WATER AVAILABLE. CREW ALSO NOTICED A STRANGE NOISE AND VIBRATION IN TAIL SECTION. [06-14-07] UPON ARRI VAL FOUND SERVICE VALVE LEFT OPENED, SECURED CLOSED AND SERVICED POTABLE WATER, NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041600083 20070416 00083 NE 2007 4 16 2007UALA01036 2 20070404 A 7532 BLEED VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 445UA 826 ENG 2 BLEED FAULT DISPLAYED ON UPPER ECAM SCREEN. [SUP 06-01-07] REPLACED NR 2 ENGINE BLEED PRESSURE REGULATOR VALVE. FOUND CLOGGED FILTER ON DOWNSTREAM SENSE PORT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041600084 20070416 00084 CE 2007 4 16 2007F00028 1 20070403 A 3200 UNKNOWN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG UNKNOWN H O OTHER G MULTIPLE FAILURE DE DESCENT 1 NM 05 139ZV UE139 THIS AIRCRAFT HAS HAD MULTIPLE REOCCURRING GEAR MALFUNCTIONS. ON NUMEROUS OCCASIONS AC HAS HAD THE LANDING GEAR CIRCUIT BREAKER POP IN-FLIGHT WHICH HAS RESULTED IN A MANUAL PUMPING OF LANDING GEAR HYD SYS. AC HAS BEEN BROUGHT TO MAINTENAN CE HANGAR FOR THESE ISSUES AND HAS BEEN RETURNED TO SERVICE WITHOUT ANY REPAIR OR RESOLUTION TO PROBLEM. MAINTENANCE CO NTINUALLY SIGNS OFF AC AS (UNABLE TO DUPLICATE). MULTIPLE CREWS HAVE HAD ISSUES WITH THIS AC. FAILURE TO RESOLVE THIS ISSUE WILL EVENTUALLY RESULT IN AN AIRCRAFT ACCIDENT AND MOST LIKELY RESULT IN LOSS OF LIFE. OPERATOR IS NOT ATTEMPTING TO REMOVE THE AIRCRAFT FROM SERVICE TO FIND THE CAUSE OF THIS PROBLEM. A COMPLETE AND INTENSE INVESTIGATION NEEDS TO B 2 L 7 2 4T 4 T RT A24CE E26NE 2007041600086 20070416 00086 EA 2007 4 16 QXEA200700593 1 20070409 A 2820 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA FUEL IMBALANCE UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 610QX 10033 DEN - DURING TAXI OUT, FUEL IMBALANCE OF 600 POUNDS NOTED WITH LEFT TANK HIGHER THEN THE RIGHT. DESELECTED MANUAL CROSS FLOW. AUTO CROSSFLOW DID NOT BEGIN. SELECTED MANUAL CROSSFLOW AND FUEL STARED TO TRANSFER IN THE WRONG DIRECTION. RE SELECTED MANUAL CROSSFLOW AND IT TRANSFERRED CORRECTLY. AFTER TAKEOFF MANUAL WAS DESELECTED PER THE NORMAL CHECKLIST AN D A FUEL IMBALANCE WAS NOTED WITH THE RIGHT WING 500 POUNDS HIGHER. CROSSFLOW CONTINUED UNTIL RIGHT WING WAS 100 POUNDS HEAVY. FUEL FLOWS WERE MATCHING BUT THE RIGHT WING WAS 210 POUNDS HEAVY WITH CROSSFLOW OFF. WHEN CROSSFLOW RESTARTED, FLOW WENT THE OTHER WAY. MAINTENANCE INTERROGATED THE MDC AND FOUND NO LISTED FAULTS OR HISTORY. PERFORMED A OPERATIO 2 L 7 2 4F RT A21EA 2007041600088 20070416 00088 NM 2007 4 16 QXEA200700530 1 20070323 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 440-452 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - SCRATCHES ON SEAT TRACK NR 5 BETWEEN STATION 440 AND 452. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2007041600090 20070416 00090 EA 2007 4 16 A6WA200740102 1 20070302 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 453AW 7838 INTERCOSTAL CRACKED AT FS484.0, LBL 36.0. MAINTENANCE CUT AWAY DAMAGED FLANGE AND INSTALLED REPAIR ANGLE IAW BSC SR 601 R-53-0030A AND REO 601R-53-41-059, REV A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041600092 20070416 00092 EA 2007 4 16 A6WA200740122 1 20070308 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 453AW 7838 PAX DOOR AFT DRAG ANGLE IS CRACKED. REPAIRED IAW REO 601R-52-11-513, REV A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041600093 20070416 00093 EU 2007 4 16 2007UALA01037 1 20070405 A 3520 DOOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SEAT ROW 23RH O2 MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 412UA 465 SEAT ROW 23 RT EMERGENCY O2 COMPT DOOR OPENS IN WRONG DIRECTION, HINGE ON INBOARD SIDE. OPEN DOOR CAN IMPEDE EXITING OF PASSENGER IN OUTBOARD SEATS. [SUP 5-1-07] REMOVED AND REINSTALLED DOOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041600094 20070416 00094 2007 4 16 2007UALA01038 4 20070402 A 2565 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR SLIDE LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 590UA 28708 LOW BOTTLE PRESSURE. [SUP 05-16-07] WATER TESTED FOR LEAKS AND NO LEAK WAS FOUND. THE GAUGE STILL SHOWED IN THE GREEN. THE TECHNICIAN TOPPED OFF THE BOTTLE. SLIDE WAS IN AS A PART TIME SPARE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041600096 20070416 00096 EU 2007 4 16 SIMA200709901 1 20070408 A 3320 LIGHT SAAB SF340 340B 7860101 EU SEAT 3A SHORTED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 21 238AE 340B238 BURNING ODOR NOTICED ON LANDING COMING FROM AROUND THE MAIN DOOR AREA. INSPECTED AREA AND FOUND LIGHT ABOVE SEAT 3A SHO RTED OUT. REMOVED THE BULB AND DEFERRED PER MEL 33-02. 2 L 7 2 4T RT A52EU 2007041600097 20070416 00097 SO 2007 4 16 SIMA200709909 1 20070407 A 3610 14521182403 DUCT EMB 145 EMB145LR 3260212 SO ZONE 200 CRACKED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 649PP 15917 145234 NUMBER 1 BLEED LEAK OCCURRED CLIMBING THROUGH 13,000 FEET, RETURNED TO ORD. REMOVED AND REPLACED T-DUCT BEHIND LEFT SID E WALL IAW EMB 36-11-09. OPERATIONAL AND LEAK CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007041600101 20070416 00101 SO 2007 4 16 SIMA200709906 1 20070406 A 3350 20131A BATTERY PACK EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 735TS 9986 6694 145386 EMERGENCY PATH LIGHTS FROM ROW 6 FORWARD NO TEST. REMOVED AND REPLACED NUMBER 2 POWER SUPPLY IAW EMB AMM 33-50-04. OPE RATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041600103 20070416 00103 EU 2007 4 16 SIMA200709908 1 20070408 A 2721 UNKNOWN SAAB SF340 340B 7860101 EU RUDDER TRIM UNKNOWN A SIMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 236AE 340B236 RUDDER TRIM FLUCTUATED AND AUTOPILOT WOULD NOT ENGAGE, REQUIRED LEFT AILERON INPUT TO COMPENSATE FOR RIGHT YAW. RETURNE D TO DFW. REMOVED AND REPLACED YAW TRIM ACTUATOR IAW SAAB AMM. OPERATIONAL CHECK GOOD. RETURNED TO SERVICE 2 L 7 2 4T RT A52EU 2007041600104 20070416 00104 SO 2007 4 16 SIMA200709912 1 20070405 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 931AE 4768 14500912 LEFT OMEGA BEAM CORRODED AT FRAME 20. PERFORM CUTOUT OF CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53 -00-10. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007041600106 20070416 00106 SO 2007 4 16 SIMA200709910 1 20070403 A 5315 14521700007 FLOORBEAM EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 708AE 15810 4800 145205 LEFT OMEGA BEAM CORRODED AT FRAME 33. PERFORMED CUTOUT TO REMOVE CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW E MB SRM 53-00-10, FIGURE 202. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041600108 20070416 00108 EA 2007 4 16 COMA0760300 1 20070404 A 2613 355523255 OVERHEAT LOOP CNDAIR CL600 CL6002B19 1900309 EA LEFT WHEELWELL FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 914CA 7012 FLIGHT 5349 - RECEIVED ANTI-ICE DUCT WARNING DURING CLIMB WITH WING AND COWL ANTI-ICE ON. REPLACED LOOP A41WK. PERFORM ED OPS CHECKS, NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007041600109 20070416 00109 EA 2007 4 16 A6WA200740156 1 20070325 A 3030 7858062 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 1 HEAT MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 412AW 15241 7582 PITOT BASE HEAT CAUTION MESSAGE CAME ON AFTER TAKEOFF. QRH COMPLIED WITH, UPON LANDING TAT PROBE HEAT, LT STATIC HEAT, LT AOA HEAT, RT STATIC HEAT, AND RT AOA HEAT CAUTION MESSAGE ALL CAME ON. REMOVED AND REPLACED ADS NR1 HEAT CONTROLLER IAW AMM 30-13-15 AND PERFORMED OPS CHECK OF HEAT CONTROLLER 32 IAW AMM 30-31-15. ALL OPS CHECKS GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041600110 20070416 00110 SO 2007 4 16 C2XA07CL038 1 20070408 A 3350 66367 LIGHT EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13929 145009 CLE FLIGHT 2934 - THE CREW REPORTED THE FORWARD EMERGENCY AISLE LIGHT STRIP WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE FORWARD EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2007041600111 20070416 00111 NM 2007 4 16 AALA20070564 1 20070327 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 358AA 24039 DFW - EMERGENCY LIGHT IN UPPER LEFT NUMBER FOUR DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT IN UPPER LEFT NUMBER FOUR DO OR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007041600114 20070416 00114 NM 2007 4 16 2007UALA00963 1 20070331 A 5340 MOUNT BOEING 737 737322 1384676 NM LT GIRT BAR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 LT FWD CABIN DOOR CUTOUT FWD GIRT BAR MOUNT HAS CORROSION ON UPPER SURFACE MARKED. REMOVED CORROSION. REFERENCE SRM 51-10-02 AND SRM 51-20-01. 2 L 7 2 4F RT A16WE 2007041600115 20070416 00115 NM 2007 4 16 2007UALA01006 1 20070330 A 3234 HANDLE BOEING 737 737522 138449F NM MLG LACK OF LUBE A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 905UA 25005 ON APPROACH 3 RED LIGHTS AND 3 GREEN LIGHTS ON; TOWER SAID GEAR WAS DOWN. CLEANED OUT THE GEAR HANDLE HOUSING, SWITCH ES AND LUBED GEAR HANDLE. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A16WE 2007041600116 20070416 00116 NM 2007 4 16 2007UALA01032 1 20070404 A 3350 20131A CHARGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 644UA 25094 EEL LIGHT LEFT A-ZONE INOPERATIVE. REMOVED AND REPLACED CHARGER AND BATTERY PER MM 33-51-07 AND EEL SYSTEM OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007041700003 20070417 00003 CE 2007 4 17 AMWA083769 1 20070406 A 3240 BRAKE ASSY BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RT MLG LOCKED A AMWA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 07 146YV N146YV DURING TAXI, ACFT BRAKES (RT) LOCKED UP. ACFT RETURNED TO GATE WITH NO FURTHER INCIDENT. REMOVED AND REPLACED NR3 BRAK E ASSY AND PARKING BRAKE VALVE. 2 L 7 2 4T 3 T RT A24CE E2NE 2007041700005 20070417 00005 EA 2007 4 17 QXEA200700573 1 20070331 A 5753 SKIN CNDAIR CL600 CL6002C10 1390015 EA TE FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - 14 EACH, LOOSE RIVETS ON UPPER SKIN OF LEFT OUTBOARD FLAP. REPAIRED IAW REO670-57-53-05. 2 L 7 2 4F RT A21EA 2007041700006 20070417 00006 EA 2007 4 17 QXEA200700574 1 20070327 A 5730 ACCESS PANEL CNDAIR CL600 CL6002C10 1390015 EA LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - LEFT WING INBOARD FLAP ACCESS PANEL 584EB IS CHAFED ON OUTER SURFACE BY ACTUATOR CUTOUT. REPAIRED IAW SRM 57-5 2-01, 51-21-11, AND 51-25-06. 2 L 7 2 4F RT A21EA 2007041700008 20070417 00008 EA 2007 4 17 QXEA200700576 1 20070328 A 5730 ACCESS PANEL CNDAIR CL600 CL6002C10 1390015 EA LT WING CHAFED I QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - LEFT WING INBOARD FLAP ACCESS PANEL 584LB IS CHAFED ON OUTER SURFACE BY ACTUATOR CUTOUT. REPAIRED IAW SRM 51-2 1-11, 57-52-01. 2 L 7 2 4F RT A21EA 2007041700009 20070417 00009 SO 2007 4 17 RAIA00704020 1 20070406 A 3350 316 BULB EMB 145 EMB145 3260210 SO EMERGENCY LIGHT BURNED OUT A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 807HK 145119 PRE FLT 3574 - STL - MAIN DOOR EXTERIOR FLOOD LIGHT EMERGENCY LIGHT OUT ON HINGE OF STAIRS. MAINTENANCE REPLACED HANDRA IL EMERGENCY LIGHT AS REQUIRED, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007041700010 20070417 00010 SO 2007 4 17 RAIA00704022 1 20070406 A 2140 A/C PACK EMB 145 EMB145LR 3260212 SO NR 1 MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 CE 03 814HK 145046 FLT 5535 - DEN - NR 1 PACK WOULD NOT WARM THE COCKPIT AND HAD A PACK NR 1 OVERHEAT MESSAGE ON EICAS. MAINTENANCE DEFERR ED NR 1 PACK SYSTEM PER MEL. 2 L 7 2 4T RT T00011AT 2007041700012 20070417 00012 SO 2007 4 17 RAIA00704024 1 20070408 A 3610 O-RING EMB 145 EMB145LR 3260212 SO BLEED DIST DAMAGED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 816HK 145055 FLT 5496 - STL - FAILED PART 2, ANTI-ICE TEST FOLLOWED BY BLEED LEAK ENGINE 1 & 2 AND WING BURST MESSAGE. MAINTENANCE R EMOVED AND REPLACED BLEED O-RING & CLAMP AT JOINT NR 10 DUE TO CLOSE PROXIMITY CAUSED BLEED 1 AS WELL. NO FURTHER LEAKS NOTED. 2 L 7 2 4T RT T00011AT 2007041700017 20070417 00017 SO 2007 4 17 RAIA00704031 1 20070411 A 3260 SWITCH EMB 145 EMB145LR 3260212 SO MLG OUT OF ADJUST A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 841HK 145382 FLT 7904 - IAD - L/G AIR/GROUND FAIL MESSAGE, WITH AURAL WARNING. MAINTENANCE INSPECTED AND TESTED WOW SWITCHES CHECKS GOOD. PERFORMED WOW ADJUSTMENT, OPS CHECK GOOD. NO FURTHER MESSAGE. 2 L 7 2 4T RT T00011AT 2007041700018 20070417 00018 SO 2007 4 17 RAIA00704034 1 20070412 A 5270 UNKNOWN EMB 145 EMB145LR 3260212 SO DOOR WARNING UNKNOWN A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 831HK 145232 PRE FLT 7891 - IAD - BAG DOOR OPEN INDICATION ILLUMINATED DURING TAXI. MAINTENANCE DEFERRED BAG DOOR WARNING SYSTEM IN COMPLIANCE WITH MEL. 2 L 7 2 4T RT T00011AT 2007041700019 20070417 00019 SO 2007 4 17 RAIA00704032 1 20070412 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 829HK 145281 PRE FLT 5488 - IAD - EMERGENCY LIGHT INOP AT AFT SIDE AFT CEILING EXIT LOCATOR. MAINTENANCE RESECURED LOOSE CONNECTOR A ND OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007041700020 20070417 00020 SO 2007 4 17 RAIA00704033 1 20070412 A 3350 78241 INVERTER EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 820HK 145064 PRE FLT 5564 - OKC - EMERGENCY LIGHT MAIN DOOR EXIT MARKER INOP. MAINTENANCE REMOVED AND REPLACED NR 1 INVERTER, CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007041700021 20070417 00021 CE 2007 4 17 DJFA2007046 1 20070409 A 5514 BRACKET BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 697TA RK299 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE RT IB HORIZONTAL STA BILIZER, THE RT BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE ' NR 70. [SUP 05-04-07] MAINTENANCE REPLACED THE RIB. 2 H 7 2 4F 4 F RT A16SW E25EA 2007041700023 20070417 00023 NM 2007 4 17 ASAA0741571 1 20070413 A 5320 6517684634 INTERCOSTAL BOEING 737 7374Q8 138447Q NM BS 294-303 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 INTERCOSTAL HAS A 2.3 INCH CRACK IN THE WEB. REMOVED THE DAMAGED INTERCOSTAL LOCATED DRILLED AND INSTALLED A REPLACEMEN T INTERCOSTAL IAW EA 5310 02712 REV NEW. 2 L 7 2 4F RT A16WE 2007041700027 20070417 00027 NM 2007 4 17 ASAA0741575 1 20070413 A 5753 6546430518 SKIN BOEING 737 7374Q8 138447Q NM FORE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 THE RIGHT INBOARD FORE FLAP IS DENTED ON THE LWR INBOARD SIDE. PREPARED THE DAMAGED SURFACE OF THE LWR SKIN FOR BONDING , FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 12, 15, 18 AND 20. 2 L 7 2 4F RT A16WE 2007041700028 20070417 00028 NM 2007 4 17 ASAA0741576 1 20070413 A 5753 6546431287 SKIN BOEING 737 7374Q8 138447Q NM FORE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 THE LEFT WING OUTBOARD FORE FLAP IS CHAFED ON AN EXISTING LEADING EDGE REPAIR AT THE INBOARD END. REMOVED THE EXISTING SKIN REPAIR DOUBLER IAW SRM 57-53-01 FIG 201. 2 L 7 2 4F RT A16WE 2007041700031 20070417 00031 SO 2007 4 17 RAIA00704035 1 20070412 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 817HK 145058 POST FLT 5532 - STL - EMERGENCY LIGHT GALLEY WALL EXIT LOCATOR INOP. MAINTENANCE SECURED LOOSE WIRE ON GALLEY WALL, CHE CK GOOD. 2 L 7 2 4T RT T00011AT 2007041700033 20070417 00033 NM 2007 4 17 CALA0700173 1 20070411 A 5311 6546537 FRAME BOEING 737 7373T0 1384582 NM BS 616 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 FRAME CRACKED AT STA 616 JUST BELOW FLOOR LINE ON LEFT SIDE. REPAIRED IAW ECRA 5311-01158. 2 L 7 2 4F RT A16WE 2007041700034 20070417 00034 NM 2007 4 17 CALA0700174 1 20070411 A 5311 6546533 FRAME BOEING 737 7373T0 1384582 NM BS 500 S27-28R CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 FWD CARGO FRAME CORRODED AT STA 500 BETWEEN STRINGER 27R AND 28R. REPAIRED IAW SRM 53-00-07, REPAIR 4. 2 L 7 2 4F RT A16WE 2007041700036 20070417 00036 NM 2007 4 17 KCSA071137 1 20070410 A 5330 SKIN BOEING 747 747236B 1384804 NM BS 550 S44-45L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 FUSELAGE SKIN HAS .5 INCH LONG CRACK AT STA-550 BETWEEN S-44L AND S-45L. 2 L 7 4 4F A20WE 2007041700037 20070417 00037 NM 2007 4 17 KCSA071138 1 20070410 A 5347 SEAT TRACK BOEING 747 747236B 1384804 NM BS 630 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 UPPER DECK SEAT TRACK HAS AREA OF CORROSION AT STA-630 RBL-28 WL-308. 2 L 7 4 4F A20WE 2007041700038 20070417 00038 CE 2007 4 17 DXTA200702104 1 20070412 A 2820 UNKNOWN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE RT ENGINE UNKNOWN E DXTA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 07 325QS 5600425 DESCENDING THROUGH 11,000 FT, RT ENGINE LOW FUEL PRESSURE ANNUNCIATOR ILLUMINATED, TRIGGERING RT FUEL BOOST ANNUNCIATOR TO ILLUMINATE. RAN THE ABNORMAL CHECKLIST AND LANDED. NO ENGINE FLUCTUATIONS OR OTHER ENGINE INDICATIONS WERE NOTED. [SUP 4-19-07] SUMPED RT WING TANKS. REMOVED ENGINE FUEL FILTER AND INSTALLED A NEW FILTER. INSTALLED COWL. REMOVED RT ENGINE FUEL LOW PRESSURE SWITCH AND INSTALLED A NEW SWITCH. ALL LEAK AND OPS CHECKS GOOD. ALL WORK DONE IAW CHAPTER 73-30-02 OF THE 560 MM. 2 L 7 2 4F 4 F RT A22CE E25EA 2007041700039 20070417 00039 NM 2007 4 17 ASMF200704008 1 20070411 A 2121 034722 FAN DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE INSTRUMENT STUCK W ASMF K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 23 161PL 17842 49764 CAPTAIN REPORTED BURNING ODOR WAS DETECTED ON CABIN CREW, SO AIRCRAFT WAS SENT TO THE HANGAR AND DURING INSPECTION INSTR UMENTS FAN WAS DETECTED STUCK AND WITH BURNED ODOR. FAN WAS REPLACED AND TESTED IAW MM 21-50-01, ALL CORRECT. AS A PRECA UTIONARY ACTION, AIR CONDITIONING WATER SEPARATORS AND TURBINE COOLING WERE CHECKED FOR OIL CONTAMINATION AND DAMAGES IA W MM 21-20-02 AND 21-51-01, TESTED CORRECT IAW MM 21-00-00. 2 L 7 2 4F 4 F RT A6WE E9NE 2007041700040 20070417 00040 CE 2007 4 17 DXTA200702106 1 20070414 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LEFT LEAKING E DXTA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 GL 07 390QS 5600490 CO-PILOTS BRAKES ARE MUSHY, ESPECIALLY THE LT. FLUID NOTED ON LT BRAKE ASSEMBLY. REMOVED PILOTS LT MASTER CYLINDER & I NSTALLED IN CO-PILOTS LT POSITION. CO-PILOTS LT MASTER CYLINDER REMOVED FROM SERVICE. INSTALLED OVERHAULED MASTER CYLIND ER IN PILOTS LT POSITION. REMOVED & REPLACED CO-PILOTS RT MASTER CYLINDER WITH OVERHAULED UNIT. REPLACED PILOTS LT CYLIN DER FITTINGS & INLET HOSE WITH NEW, BLED SYSTEM, OPS & LEAK CHECKED GOOD, TAXI CHECK PERFORMED, OPS -CHECK OF BRAKE SYST EM GOOD, NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A22CE E25EA 2007041700044 20070417 00044 NM 2007 4 17 KCSA071142 1 20070412 A 5313 STRINGER BOEING 747 747236B 1384804 NM BS 2360 S48L CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 AFT OF BS 2360, STR 48L END FITTING CORRODED. 2 L 7 4 4F A20WE 2007041700045 20070417 00045 NM 2007 4 17 KCSA071143 1 20070412 A 5313 STRINGER BOEING 747 747236B 1384804 NM BS 2360 S50L CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 AFT OF BS 2360, STR 50L END FITTING CORRODED. 2 L 7 4 4F A20WE 2007041700046 20070417 00046 NM 2007 4 17 KCSA071144 1 20070412 A 5313 STRINGER BOEING 747 747236B 1384804 NM BS 2360 S44L CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 AFT OF BS 2360, STR 44L END FITTING CORRODED. 2 L 7 4 4F A20WE 2007041700047 20070417 00047 NM 2007 4 17 KCSA071145 1 20070412 A 5313 STRINGER BOEING 747 747236B 1384804 NM BS 2360 S50R CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 FWD OF BS 2360, STR 50R END FITTING CORRODED. 2 L 7 4 4F A20WE 2007041700051 20070417 00051 SO 2007 4 17 RAIA00703081 1 20070331 A 3297 D399926KA CONNECTOR EMB 145 EMB145LR 3260212 SO NLG WOW WORN A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 815HK 145048 FLT 5576 - RIC - ON GEAR RETRACTION, AIR/GROUND C/B POPPED. VARIOUS EICAS WARNINGS. MAINTENANCE REMOVED AND REPLACED T HE CONNECTOR ON NOSE GEAR WOW PROX SWITCH. 2 L 7 2 4T RT T00011AT 2007041700052 20070417 00052 SO 2007 4 17 C2XA07IA086 1 20070412 A 3210 UNKNOWN EMB 135 EMB135LR 3260305 SO LANDING GEAR UNKNOWN A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 15527 145413 IAH - FLIGHT 2922 AFTER TAKEOFF, THE CREW SELECTED GEAR LEVER TO UP POSTION BUT GEAR DID NOT RETRACT, CYCLED LEVER BACK DOWN THEN UP RETRACTED NORMAL. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED E XTENSION AND RETRACTION CHECKS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041700053 20070417 00053 SO 2007 4 17 C2XA07SH018 1 20070410 A 5315 14521700007 FLOORBEAM EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17159 145792 SHV - DURING C-CHECK MAINTENANCE FOUND SURFACE CORROSION ON THE LEFT HAND OMEGA BEAM UNDER THE CARBON FIBER CROSS BEAM A ND THE SURROUNDING AREAS. MAINTENANCE REPAIRED THE LEFT HAND OMEGA BEAM AT FRAME 20 IAW EMB 145XR SRM 53-00-10 FIG 201 SHEET 2. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007041700054 20070417 00054 2007 4 17 ASMF200704004 4 20070409 A 3440 WARNING SYSTEM DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE WINDSHEAR ALARM FAILED W ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 158PL 49761 AIRCRAFT REJECTED TAKE-OFF AT 110 KNOTS AND 121000 POUNDS DUE TO WINDSHEAR ALARM ACTIVATION. SYSTEM WAS TESTED IAW MM 3 4-47-00 CONFIRMING THE FAILURE, SO IT WAS DEFERRED IAW MEL 34-44. DURING OVERNIGHT CHECK , WIND SHEAR SELF TEST WAS PERF ORMED IAW 34-47-0, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2007041700060 20070417 00060 NM 2007 4 17 KCSA071148 1 20070413 A 3350 LIGHT BOEING 747 747236B 1384804 NM RT ESCAPE HATCH INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 701CK 21730 EMERGENCY EXIT SIGN DOES NOT ILLUMINATE AT RT ESCAPE HATCH. 2 L 7 4 4F A20WE 2007041700063 20070417 00063 NM 2007 4 17 QXEA200700602 1 20070405 A 5740 BRACKET DHAV DHC8 DHC8202 2809007 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - RIGHT WING FORWARD SPAR Z-ANGLE BRACKET AT YW 58.2 IS CRACKED. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007041700064 20070417 00064 NM 2007 4 17 QXEA200700603 1 20070405 A 5720 ANGLE DHAV DHC8 DHC8202 2809007 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - LEFT WING FORWARD SPAR Z-ANGLE AT YW 58.2 IS CRACKED. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007041700066 20070417 00066 NM 2007 4 17 QXEA200700609 1 20070405 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - CABIN SEAT TRACK NR 7 HAS MINOR SCRATCHES AT STATION X282-X302, X310-X330, X342-X366, X416-X426, X379-X387. RE PAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2007041700067 20070417 00067 NM 2007 4 17 QXEA200700606 1 20070406 A 5340 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - FOUND SEAT TRACK NR 4 HAS 4 GOUGES AT STATION X377. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2007041700068 20070417 00068 NM 2007 4 17 QXEA200700607 1 20070406 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - CORROSION ON FLOOR SUPPORT ANGLE ATTACHED TO OUTBOARD SEAT TRACK NR 4 AT STATION X222.7. REPAIRED IAW RD8-53-1 339 AND SRM 51-20-11. 2 H 7 2 4T RT A13NM 2007041700070 20070417 00070 NM 2007 4 17 QXEA200700610 1 20070405 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - CABIN SEAT TRACK NR 7 HAS CORROSION AT STATION X225. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2007041700071 20070417 00071 NM 2007 4 17 QXEA200700611 1 20070405 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - CABIN SEAT TRACK NR 7 HAS CORROSION AT STATION X218. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2007041700074 20070417 00074 NM 2007 4 17 QXEA200700613 1 20070410 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - THERE IS CORROSION ON THE SKIN BELOW THE INTERCOSTAL THAT WAS REMOVED OUTBOARD OF STRINGER 31L BETWEEN X195 AND FRAME X201. REPAIRED IAW SRM 51-20-16, 51-20-36, 51-20-11. 2 H 7 2 4T RT A13NM 2007041700075 20070417 00075 2007 4 17 ASMF200704003 4 20070409 A 3431 6223257101 VOR SYSTEM DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 FAILED W ASMF K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 23 158PL 9063 49761 DURING TRANSIT CHECK, THE VOR NR 2 FLAG WAS SHOWN ON BOTH PFD'S, RADIO ALTIMETER NR 1 AND EFIS PANEL TEST FAILED IN BOTH SIDES. TECH PERSONNEL REPLACED VHF NAV NR 2 AND RADIO ALTIMETER NR 1 IAW MM 34-32-02 AND 34-42-03 RESPECTIVELY, TESTE D CORRECT. BOTH EFIS SYSTEM SIDES WERE CHECKED, DETECTING FAILURE OF RELAY R2-124, SO IT WAS REPLACED IAW MM 32-36-00 TE STED CORRECT IAW MM 34-42-00. 2 L 7 2 4F 4 F RT A6WE E9NE 2007041700077 20070417 00077 NM 2007 4 17 ASMF200704006 1 20070410 A 2430 OIL SYSTEM DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE RT CSD EMPTY W ASMF A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 SW 23 161PL 4158 49764 696395 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT MID DUE TO CAPTAIN REPORTED RT CSD FAILED; APU DID NOT START AND BATTERIES CHARGER CIRCUIT BREAKER POPPED OUT. AT MID TECHNICAL PERSONNEL REPLACED CSD AND GENERATOR, TESTED CORRECT IAW MM 2-10-0 1 AND 24-20-01. BATTERIES CHARGER WORKED CORRECTLY IAW 24-30-02. NO OVERWEIGHT INSPECTION WAS REQUIRED DUE TO AIRCRAFT L ANDED WITH 108,737 POUNDS AND THE MAXIMUM LANDING WEIGHT IS 139,500 POUNDS. 2 L 7 2 4F 4 F RT A6WE E9NE 2007041700078 20070417 00078 EA 2007 4 17 QXEA200700585 1 20070326 A 5753 PANEL CNDAIR CL600 CL6002C10 1390015 EA RT TE FLAPS CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - RIGHT FLAP PANEL 684GB CHAFED ON LEADING EDGE. REPAIRED IAW SRM 51-25-16, 51-21-11. 2 L 7 2 4F RT A21EA 2007041700079 20070417 00079 EA 2007 4 17 QXEA200700586 1 20070326 A 5753 PANEL CNDAIR CL600 CL6002C10 1390015 EA TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - FLAP PANEL 684ET CHAFED ON LEADING EDGE. REPAIRED IAW SRM 51-25-16, 51-21-11. 2 L 7 2 4F RT A21EA 2007041700082 20070417 00082 EA 2007 4 17 QXEA200700589 1 20070325 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - FUSELAGE SKIN AT FORWARD EDGE OF PASSENGER DOOR CUTOUT LOWER SIDE HAS SEVERAL NICKS AND GOUGE. REPAIRED IAW SR M 53-00-01, 51-25-06. 2 L 7 2 4F RT A21EA 2007041700083 20070417 00083 EA 2007 4 17 QXEA200700584 1 20070331 A 5753 PANEL CNDAIR CL600 CL6002C10 1390015 EA RT TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - RIGHT FLAP PANEL 684AB CHAFED ON LEADING EDGE. REPAIRED IAW SRM 57-52-01, 51-21-11. 2 L 7 2 4F RT A21EA 2007041700084 20070417 00084 EA 2007 4 17 QXEA200700582 1 20070326 A 5720 PANEL CNDAIR CL600 CL6002C10 1390015 EA WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - BUTE DOOR PANEL 691KB HAS LIGHT SURFACE CORROSION IN FASTENER HOLES. REPAIRED IAW SRM 51-21-06, 51-25-16. 2 L 7 2 4F RT A21EA 2007041200118 20070412 00118 SO 2007 4 12 C2XA07TY020 1 20070410 A 5330 14521887001 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16951 145063 TYS - DURING A CURRENT 2C INSPECTION A CRACK WAS FOUND AT A RIVET AT FRAME 75, BETWEEN STR 1L AND 2L. MAINTENANCE CUT O UT THE DAMAGED AREA, FABRICATED DOUBLERS, INSTALLED FILLERS AND DOUBLERS, ALODINED, PRIMED AND PAINTED IAW EC 53330-0168 1. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF C-CHECK INSPECTION. 2 L 7 2 4T RT T00011AT 2007041200134 20070412 00134 EA 2007 4 12 A6WA200740167 1 20070331 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 451AW 7832 RT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX .9 INCH LONG. (K) [SUP 05-01-07] MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL FROM 621 TO 625.30 AT STRINGER 14R IAW CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041200146 20070412 00146 EU 2007 4 12 07FDEA01390 1 20070410 A 5313 A53980877 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 TWO PREVIOUS REPAIRS FOUND AT STRINGER P56 LT/RT, C76-C77 WITH NEW CORROSION ON P56 LT/RT. REPAIR PERFORMED BY CORROSIO N REMOVAL AND L-ANGLE INSTALLATION IAW EA 6-5318-101239 AND RAS/DAHAM/4020755/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007041200147 20070412 00147 EU 2007 4 12 07FDEA01391 1 20070410 A 5313 A53973079 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CORROSION ON STRINGER P46 RT, C59-C60, STRINGER REPAIR PERFORMED IAW EA 6-5317-101240 AND RAS/DAHAM/4020719/2006 ISSUE " B". 2 L 7 2 4F RT A35EU 2007041200151 20070412 00151 EA 2007 4 12 A6WA200740162 1 20070324 A 5310 VERTICAL BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 409 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 416AW 7603 FS 409.0 + 128.0 VERTICAL BEAM AT RBL 27.0 IS CRACKED .4 INCH. (K) [SUP 05-09-07] MAINTENANCE TRIMMED OUT DAMAGED ARE A, PERFORMED EDDY CURRENT, FABRICATED REPAIR ANGLE AND INSTALLED IAW BOMBARDIER REO 601R-53-41-056 REV E AND BSC EO 601R -53-11286. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041200153 20070412 00153 EU 2007 4 12 07FDEA01394 1 20070410 A 5320 LN9496A540 SILL AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CORROSION AND MATERIAL DEVIATIONS ON OLD AFT CARGO DOOR SILL BEAM REPAIR, C59-C60 RT. REPAIR PERFORMED BY CUT OUT AND R EPLACING PARTS IAW SRM 53-17-18/FIG 202 AND RAS/DAHAM/4015666/2002 ISSUE "A". 2 L 7 2 4F RT A35EU 2007041200155 20070412 00155 EU 2007 4 12 07FDEA01395 1 20070410 A 5315 A53773651212 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CORROSION ON TOP CAP BEAM UPPER FLANGE LT AT C38 AND C38.1. REPAIR PERFORMED IAW 53-10-15/FIG 207 AND SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007041200171 20070412 00171 EU 2007 4 12 07FDEA01412 1 20070410 A 5313 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CORROSION ON STRINGER P55, C70-C71. STRINGER REPAIR PERFORMED IAW SRM 53-10-14/FIG 203. 2 L 7 2 4F RT A35EU 2007041200176 20070412 00176 NM 2007 4 12 F3LA200700061 1 20070330 A 5322 SHEAR TIE AIRBUS A319 A319111 3930336 NM CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED SUPPORT FRAME (SHEAR PLATE) BETWEEN FR69 AND FR70, JUST BEHIND FLOORBEAM -Y1292 CORRODED. FOUND SHEAR PLATE TO BE OUT OF LIMITS IAW A319 SRM 53-00-14, FIG. 101. REMOVED SHEAR PLATE IAW A319 SRM 51-4 2-11, FIG 8. LOCATED AND DRILLED HOLES INTO THE NEW SHEAR PLATE IAW A319 SRM 51-72-11. INSTALLED NEW SHEAR PLATE AND S UPPORT FRAME BETWEEN FR69 AND FR70 IAW A319 SRM 51-42-11, FIG 9, 12, 40 AND 43, TABLE 22 AND 25. 2 L 7 2 4F RT A28NM 2007041600005 20070416 00005 WP 2007 4 16 070093 1 20070409 A 3260 INDICATOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NLG MALFUNCTIONED A WX0A O OTHER N FALSE WARNING CL CLIMB 1 WP 19 864GA 49912 FLIGHT 591, THE FLIGHT CREW REPORTED THAT AFTER RETRACTING THE GEAR, THE RED NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED . THE NLG INDICATOR PIN (MECHANICAL) INDICATED NOSE GEAR UP. CYCLED GEAR AND RED UNSAFE LIGHT EXTINGUISHED AND DID NOT R EOCCUR FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE REPORT THE INSPECTION OF THE MECHANICAL AND ELECTRICAL COMPONENTS OF THE NOSE GEAR WITH NO FAULTS FOUND. JACKED AIRPLANE NOSE IAW AMM 07-12-00 AND PERFORMED A SATISFACTORY NOSE GEAR SWING IAW AMM 32-30-00. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A6WE E9NE 2007041600006 20070416 00006 WP 2007 4 16 070095 1 20070411 A 3350 7732 LAMP DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE EMERGENCY LIGHT INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 948MA 49778 DURING A ROUTINE OVERNIGHT SERVICE CHECK, MAINTENANCE INSPECTION, REPORTED THAT THE EMERGENCY EGRESS PATH LIGHTING AT SE AT ROW 16 WOULD NOT TEST. FURTHER REPORT THE REMOVAL AND REPLACEMENT OF 2 (TWO) LAMPS AT ROW 16. A SATISFACTORY OPERATI ONAL CHECK WAS ACCOMPLISHED IAW AMM 33-53-01. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A6WE E9NE 2007041600007 20070416 00007 NM 2007 4 16 HALA0700165 1 20070410 A 4900 380029812 APU BOEING 767 767300 1385204 NM PWA PW4062 PW4062 NE APU BAY FAILED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 11688 11688 25531 ETOPS SIGNIFICANT SYSTEM, APU SHUTDOWN ON GATE. NOTED ALSO WITH BELLOWING SMOKE OUT OF TAILPIPE AND LOSS OIL QTY.//REPLA CED APU HAL IAW SPM AND HAL M-266-767 FORM. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007041600012 20070416 00012 EA 2007 4 16 TRAX200700474 1 20070406 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 LT ENGINE SUPPORT BEAM LOWER WEB CRACKED AT FWD IB NUT PLATE FOR ACCESS PANEL. [SUP 4-23-07] COMPLIED WITH ALL FAA APP ROVED DATA. 2 L 7 2 4F 4 F RT A21EA E15NE 2007041600049 20070416 00049 WP 2007 4 16 N865R1125006 1 20070326 A 5320 UNKNOWN DOUG DC8 DC863F 302198F WP BS 67 CORRODED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 46088 COCKPIT SUBFLOOR INNER AREA WITH CORROSION AT STA 67 L-21R CPCP 455R 0552. 2 L 7 4 4F 4A25 2007041600063 20070416 00063 NM 2007 4 16 2007UALA01019 1 20070404 A 3350 BR964421 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE SEAT 7ABC INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 804UA 759 CABIN SEAT 7ABC EMERGENCY ESCAPE PATH MARKING LIGHT INOP. REPLACED LIGHT ASSY AND OP CHECKED ON WU U1013K. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041600068 20070416 00068 EA 2007 4 16 A6WA200740166 1 20070331 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 620-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 451AW 7832 LT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. (K) MAINTENANCE REM OVED AND REPLACED THE INTERCOSTAL AT STRINGER 14L BETWEEN FS 621 AND 625.30 IAW CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041600070 20070416 00070 WP 2007 4 16 IXXA07SMN091S 1 20070208 A 5755 PANEL DOUG DC8 DC862 3021970 WP ZONE 500 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, LEFT WING OUTBORD AILERON LOWER PANEL NON STANDARD REPAIR, BETWEEN STATION XA 650.000 AND XA 693.000. REMOVED SKIN WITH EXISTING NON STANDAR REPAIR. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED PART S AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTAL LED PARTS, FROM STATION XW 546.000 TO XA 724.000. BALANCED AILERON, FOUND WITHIN TOLERANCE. MOMENT: 3345.41 IN-LBS IAW DC8 SRM 57-8-1 FIGURE 4, ITEM "E" AND "L", DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 51-1-9 TR NUMBER 51-142 DATE D 04-05-06, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND DC8 SRM 51-4-4. 2 L 7 4 4F 4A25 2007041600087 20070416 00087 EA 2007 4 16 QXEA200700591 1 20070410 A 4950 32912104 VALVE CNDAIR CL600 CL6002C10 1390015 EA APU BLEED MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 612QX 2 10042 SEA- FLIGHT 2531 - AFTER ENGINE START RECEIVED A APU BLEED CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENANCE FOUND CO DE MPE 46 IN THE MDC. REPLACED THE LOAD CONTROL VALVE IAW CRJ-700 AMM 49-51-05-000-801-A01. OPERATIONAL CHECKS GOOD. AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007041600089 20070416 00089 EA 2007 4 16 QXEA200700592 1 20070410 A 2121 AE0804A04 FAN CNDAIR CL600 CL6002C10 1390015 EA INOPERATIVE A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 619QX 3736 10246 SEA - FLIGHT 2545, AFTER TAKEOFF RECEIVED A DISPLAY COOL MESSAGE. RAN CHECKLIST BUT MESSAGE STAYED ON. RETURNED TO THE FIELD AND ACCOMPLISHED A OVERWEIGHT LANDING. MAINTENANCE REPLACED THE COOLING FAN AND PERFORMED A OVERWEIGHT LANDING I NSPECTION. OPERATIONAL CHECKS GOOD FOR THE FAN AND NO DEFECTS FOUND ON THE OVERWEIGHT INSPECTION. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007041600095 20070416 00095 NM 2007 4 16 2007UALA01053 1 20070402 A 2612 FIRE LOOP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 NACELLE SHORTED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 502UA 24623 726533 NR 1 ENGINE NR 1 FIRE LOOP SHORT ABOVE FIRE WALL DISCONNECT SHORT APPEARS TO BE IN THE PYLON. [06-14-07] NR 1 E NGINE FIRE LOOP SHORT IN PYLON. ACCOMPLISHED SHIELDING REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041600102 20070416 00102 EU 2007 4 16 SIMA200709907 1 20070407 A 3150 UNKNOWN SAAB SF340 340B 7860101 EU UNKNOWN A SIMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 21 397AE 340B397 RIGHT APR LIGHT DID NOT ILLUMINATE AFTER CTOT SELECTED TO APR, ABORTED TAKEOFF. PERFORMED OPERATIONAL CHECK OF APR SYST EM WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007041600107 20070416 00107 SO 2007 4 16 SIMA200709914 1 20070406 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 933JN 4880 4880 14500918 LEFT OMEGA BEAM CORRODED AT FRAME 20. PERFORMED CUTOUT FOR CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007041700022 20070417 00022 CE 2007 4 17 DJFA2007047 1 20070410 A 5514 BRACKET BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 452LX RK317 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE RT IB HORIZONTAL STA BILIZER, THE RT BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE ' NR 70. [SUP 05-04-07] MAINTENANCE REPLACED THE RIB. 2 H 7 2 4F 4 F RT A16SW E25EA 2007041700024 20070417 00024 NM 2007 4 17 ASAA0741572 1 20070413 A 5755 654645137 SKIN BOEING 737 7374Q8 138447Q NM NR 6 SPOILER DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 THE RIGHT WING NR 6 SPOILER UPPER SURFACE IS DELAMINATED. REMOVED TWO DAMAGED AREAS OF UPPER SKIN, FABRICATED AND INSTA LLED TWO REPLACEMENT FILLERS AND TWO REPLACEMENT DOUBLERS IAW SRM 51-70-10 REPAIR 2. 2 L 7 2 4F RT A16WE 2007041700025 20070417 00025 NM 2007 4 17 ASAA0741573 1 20070413 A 5755 654645137 SKIN BOEING 737 7374Q8 138447Q NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 THE LT WING NR 0 SPOILER UPPER SURFACE IS DENTED. REMOVED THE DAMAGED AREA OF UPPER SKIN, FABRICATED AND INSTALLED A SK IN FILLER AND A REPAIR DOUBLER IAW SRM 57-50-10 REPAIR 4. 2 L 7 2 4F RT A16WE 2007041700026 20070417 00026 NM 2007 4 17 ASAA0741574 1 20070413 A 5753 6546430517 SKIN BOEING 737 7374Q8 138447Q NM FORE FLAP PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 THE LEFT WING INBOARD FORE FLAP IS PUNCTURED ON THE LWR SURFACE 4 INCHES FROM THE TRAILING EDGE AND 20 INCHES FROM THE I NBOARD SIDE. REMOVED THE DAMAGED AREA OF LWR SKIN, FABRICATED AND INSTALLED A SKIN FILLER AND A REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 15, 18 AND 20. 2 L 7 2 4F RT A16WE 2007041700042 20070417 00042 SO 2007 4 17 C2XA07IA085 1 20070411 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 21144 145741 IAH - DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHT ON THE AFT GALLEY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE NUMBER THREE INVERTER, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007041700059 20070417 00059 NM 2007 4 17 KCSA071147 1 20070413 A 5714 SPAR BOEING 747 747236B 1384804 NM BS 980 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 VAPOR SEAL BULGING ON WING CENTER SECTION REAR SPAR WEB ADJACENT TO LOWER SPAR VERT FLANGE AT RBL 104 STA 980. 2 L 7 4 4F A20WE 2007041700061 20070417 00061 WP 2007 4 17 I5HA0758007 1 20070411 A 5270 3403150751 SPRING CVAC 580 580 2422806 WP ALLSN 501D 501D13 03004 GL PAX DOOR LOOSE A I5HA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 582P 475 WHILE EN-ROUTE, THE CABIN DOOR (OPEN) LIGHT ILLUMINATED. NO DOORS OPENED AND THERE WAS NO LOSS OF CABIN PRESSURE. THE AIRCRAFT LANDED UNEVENTFULLY WITH NO EMERGENCY OR PRECAUTIONARY PROCEDURES TAKEN. INSPECTION BY MAINTENANCE PERSONNEL, DISCOVERED A DOOR HOOK SPRING ON ONE OF THE MAIN ENTRANCE DOOR HOOKS THAT HAD COME LOOSE CAUSING THE HOOK TO MOVE AWAY F ROM THE DOOR OPEN SWITCH FAR ENOUGH TO ILLUMINATE THE LIGHT. THE SPRING WAS INSPECTED AND RE-ATTACHED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT E282 2007041700069 20070417 00069 NM 2007 4 17 QXEA200700608 1 20070409 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - CORROSION ON THE BOTTOM AROUND NUTPLATES OF THE MAIN CABIN DOOR THRESHOLD. REPAIRED IAW SRM 51-20-11, 51-40-11 , 51-20-16, AND 51-20-36. 2 H 7 2 4T RT A13NM 2007041700072 20070417 00072 NM 2007 4 17 QXEA200700605 1 20070406 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - CORROSION ON SEAT TRACK 34 AT STATION X345. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2007041700073 20070417 00073 NM 2007 4 17 QXEA200700612 1 20070408 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - CORROSION FOUND ON INTERNAL SKIN AROUND RIVET HOLES BETWEEN STRINGERS 29P AND 28P FROM STATION X136.8 TO X151.6 . REPAIRED IAW SRM 51-20-11, 51-20-16, 51-20-36. 2 H 7 2 4T RT A13NM 2007041700076 20070417 00076 CE 2007 4 17 DXTA200702103 1 20070412 A 3411 PITOT LINE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL PITOT STACTIC SY OBSTRUCTED E DXTA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 07 924QS 7500124 ON TAKEOFF, JUST PRIOR TO 80 KNOTS, GOT AMBER MASTER CAUTION AND AMBER YAW DAMPNER OFF LOWER CASE MESSAGE. [SUP 4-19-07 ] PULLED FAULT CODES 0300 05: AIRDATA MISCOMPARE. FOUND WATER IN PITOT LINES. PURGED LINES PITOT & STATIC. PERFORMED A LTITUDE CORRELATION CHECKS, OPS CHECKS GOOD IAW CE750 MM 34-60-00 & FAR 43 APPENDIX E FAR 91.411 & 91.413 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007041700080 20070417 00080 EA 2007 4 17 QXEA200700587 1 20070326 A 5753 PANEL CNDAIR CL600 CL6002C10 1390015 EA TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - FLAP PANEL 684EB CHAFED ON LEADING EDGE. REPAIRED IAW SRM 51-25-16, 51-21-11. 2 L 7 2 4F RT A21EA 2007041700081 20070417 00081 EA 2007 4 17 QXEA200700588 1 20070401 A 5280 HINGE CNDAIR CL600 CL6002C10 1390015 EA LT MLG DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - LEFT MAIN LANDING GEAR DOOR UPPER HINGE PANEL HAS FASTENERS WITH HEADS STRIPPED OUT. REPAIRED IAW SRM 51-42-02 . 2 L 7 2 4F RT A21EA 2007041700085 20070417 00085 EA 2007 4 17 QXEA200700583 1 20070326 A 5730 PANEL CNDAIR CL600 CL6002C10 1390015 EA WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - BUTE DOOR PANEL 691JB HAS LIGHT SURFACE CORROSION IN FASTENER HOLES. REPAIRED IAW SRM 51-21-06, 51-21-11, AND 51-25-16. 2 L 7 2 4F RT A21EA 2007041700086 20070417 00086 EA 2007 4 17 QXEA200700590 1 20070401 A 5220 SKIN CNDAIR CL600 CL6002C10 1390015 EA ESCAPE HATCH DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - CREW ESCAPE HATCH SKIN HAS 3 SMALL NICKS AROUND OUTER HANDLE CUTOUT RIGHT HAND SIDE. REPAIRED IAW SRM 52-00-01 , 51-21-11. 2 L 7 2 4F RT A21EA 2007041700087 20070417 00087 EA 2007 4 17 QXEA200700581 1 20070327 A 5754 SKIN CNDAIR CL600 CL6002C10 1390015 EA RT SLAT CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - RIGHT OUTBOARD SLAT INBOARD TRAILING EDGE IS CHAFED AND HAS HIGH METAL. REPAIRED IAW SRM 57-42-01. 2 L 7 2 4F RT A21EA 2007041700088 20070417 00088 SO 2007 4 17 RAIA00703082 1 20070331 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 811HK 145256 PRE FLT NR 5587 - STL - EMERGENCY LIGHT AFT CEILING EXIT LOCATOR AND AISLE FLOOD LIGHT ARE INOP. MAINTENANCE RESEATED C ONNECTOR TO CEILING LIGHT PANEL, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007041700089 20070417 00089 SO 2007 4 17 RAIA00704001 1 20070401 A 3350 UNKNOWN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS UNKNOWN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 818HK 145059 PRE FTL 5579 - STL - EMERGENCY LIGHTS COCKPIT STEP EXIT IDENTIFIER AND FWD CEILING EXIT LOCATOR ARE INOP. MAINTENANCE R ESET POWER TO SYSTEM, OPS CHECK EMERGENCY LIGHT SYSTEM GOOD. 2 L 7 2 4T RT T00011AT 2007041700090 20070417 00090 SO 2007 4 17 RAIA00704003 1 20070401 A 5210 HANDLE EMB 145 EMB145LR 3260212 SO PAX DOOR OUT OF ADJUST A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 850HK 145003 PRE FLT 8034 - IAD - PAX DOOR INTERNAL HANDLE HARD TO OPERATE. MAINTENANCE ADJUSTED MAIN DOOR STEPS DOOR, OPS CHECK GOO D. 2 L 7 2 4T RT T00011AT 2007041700091 20070417 00091 SO 2007 4 17 RAIA00704005 1 20070401 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT UNSECURE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 817HK 145058 POST FLT NR 5574 - STL - EMERGENCY LIGHT FLOOR STRIP AT ROW 11 OUT. MAINTENANCE RESECURED WIRING TO FLOOR STRIPS AT ROW 11, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007041700092 20070417 00092 SO 2007 4 17 RAIA00704006 1 20070402 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 807HK 145119 PRE FLT 7981 - ROA - PAX DOOR HANDRAIL EMERGENCY LIGHT INOP. MAINTENANCE DEFERRED EXTERNAL EMERGENCY LIGHT IN PAX HANDR AIL. 2 L 7 2 4F RT T00011AT 2007041700093 20070417 00093 SO 2007 4 17 RAIA00704007 1 20070403 A 3397 CONNECTOR EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT MALFUNCTIONED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 808HK 145157 POST FLT 5475 - STL - EMERGENCY FWD CEILING LOCATOR LIGHT AND FLOOR PROXIMITY LIGHTING INOP. MAINTENANCE RESET CONNECTI ON TO EMERGENCY LIGHT INVERTER, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007041700094 20070417 00094 SO 2007 4 17 RAIA00704009 1 20070403 A 3260 852701 SWITCH EMB 145 EMB145LR 3260212 SO RT MLG WOW SHORTED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 841HK 14660 14660 145382 FLT 8022 - STL - LANDING GEAR AIR/GROUND FAIL, NO TRIM, LANDING GEAR NOT DOWN MESSAGES. MAINTENANCE REMOVED AND REPLACE D RIGHT MAIN LANDING GEAR WOW PROX SWITCH, AFT SIDE, SYSTEM CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007041700095 20070417 00095 SO 2007 4 17 RAIA00704011 1 20070403 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 819HK 145062 POST FLT 5451 - STL - FLOOR PROXIMITY EMERGENCY LIGHT INOP. MAINTENANCE RESECURED WIRES ON EMERGENCY FLOOR LIGHTS, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007041700097 20070417 00097 SO 2007 4 17 RAIA00704013 1 20070404 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT MALFUNCTIONED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 833HK 145240 POST FLT 7922 - IAD - EMERGENCY LIGHT LEFT HAND OVERWING EXIT MARKER INOP. MAINTENANCE RESET CONNECTION BEHIND EXIT LIG HTED SIGN, RETURN TO NORMAL OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007041700098 20070417 00098 SO 2007 4 17 RAIA00704014 1 20070404 A 3350 78241 INVERTER EMB 145 EMB145 3260210 SO EMEGENCY LIGHTS INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 821HK 145068 PRE FLT 5462 - STL - EMERGENCY LIGHT AT ROW 9 & 15 INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT INVERTER, SYS TEM OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007041700099 20070417 00099 SO 2007 4 17 RAIA00704015 1 20070404 A 3020 ANTI-ICE SYSTEM EMB 145 EMB145 3260210 SO ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 807HK 145119 FLT 3505 - PIT - E2 ANTI-ICE FAIL. MAINTENANCE DEFERRED ENGINE ANTI-ICE PER MEL. 2 L 7 2 4F RT T00011AT 2007041700100 20070417 00100 NM 2007 4 17 SWAA071793 1 20070410 A 5753 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 2273 27696 DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER SURFACE. REMOVED AND REPLAC ED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2007041700102 20070417 00102 NM 2007 4 17 SWAA071800 1 20070410 A 5311 6546526 FRAME BOEING 737 7375H4 138449D NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007041700103 20070417 00103 NM 2007 4 17 SWAA071797 1 20070410 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007041700104 20070417 00104 NM 2007 4 17 SWAA071789 1 20070410 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 460 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 460, BL 0 TO RBL 3. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007041700105 20070417 00105 NM 2007 4 17 SWAA071815 1 20070411 A 3350 10107451 SIGN BOEING 737 7377H4 1384404 NM R2 DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 445WN 29841 R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007041700106 20070417 00106 NM 2007 4 17 SWAA071826 1 20070411 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 251WN 32510 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER BROKEN AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007041700108 20070417 00108 NM 2007 4 17 SWAA071833 1 20070411 A 5330 6545765 SKIN BOEING 737 7375H4 138449D NM BS 526 S27R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT GROUND AIR CONDITIONING DOOR CUTOUT BS 526, STR 27R. REPAIRE D SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007041700111 20070417 00111 NM 2007 4 17 SWAA071819 1 20070411 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 572 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 572, STR 10L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007041700112 20070417 00112 NM 2007 4 17 SWAA071823 1 20070411 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 434 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 434, LBL 1.625. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007041700113 20070417 00113 NM 2007 4 17 SWAA071816 1 20070411 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 491 S26L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 494, STR 26L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007041700114 20070417 00114 NM 2007 4 17 SWAA071824 1 20070411 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM BS 378 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING DUCT CUTOUT BS 378, LBL 2.375. REPAIRED S KIN PER SRM. 2 L 7 2 4F RT A16WE 2007041700115 20070417 00115 NM 2007 4 17 SWAA071814 1 20070411 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 765 S20L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 FUSELAGE SKIN CRACKED AT BS 765, STR 20L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007041700116 20070417 00116 NM 2007 4 17 SWAA071817 1 20070411 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 941 S22R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941, STR 22R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007041700117 20070417 00117 NM 2007 4 17 SWAA071829 1 20070411 A 5311 6546526 FRAME BOEING 737 7375H4 138449D NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007041700118 20070417 00118 NM 2007 4 17 SWAA071801 1 20070410 A 5311 6546534 FRAME BOEING 737 7375H4 138449D NM BS 520 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007041700124 20070417 00124 NM 2007 4 17 SWAA071782 1 20070409 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM BS 867 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007041700125 20070417 00125 NM 2007 4 17 SWAA071798 1 20070410 A 5311 6546558 FRAME BOEING 737 7375H4 138449D NM BS 907 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007041700126 20070417 00126 NM 2007 4 17 SWAA071805 1 20070410 A 5311 6546596 FRAME BOEING 737 7375H4 138449D NM BS 727B S8R-8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007041700129 20070417 00129 NM 2007 4 17 SWAA071788 1 20070410 A 5542 SKIN BOEING 737 7373H4 1384600 NM RUDDER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND RUDDER T/E LOWER AFT SURFACE DELAMINATED. REPAIRED RUDDER PER SRM. 2 L 7 2 4F RT A16WE 2007041700133 20070417 00133 NM 2007 4 17 ASAA0771570 1 20070408 A 5230 143A61121 SKIN BOEING 737 737790 13844CN NM CARGO DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 FWD CARGO DOOR SKIN CREASED AT STA 448. REPAIRED IAW EA 5230 01359. 2 L 7 2 4F RT A16WE 2007041700135 20070417 00135 NM 2007 4 17 SWAA071809 1 20070410 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 597 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007041700137 20070417 00137 NM 2007 4 17 SWAA071810 1 20070410 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 867 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007041700140 20070417 00140 NM 2007 4 17 SWAA071813 1 20070410 A 5320 6916500 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 787-794 S25R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND INTERCOSTAL CORRODED AT BS 787 TO BS 794, STR 25R. REMOVED AND REPLACED INTERCOSTAL P ER SRM. 2 L 7 2 4F RT A16WE 2007041700141 20070417 00141 NM 2007 4 17 SWAA071790 1 20070410 A 3350 MS157721 BULB BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED C3 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007041700142 20070417 00142 NM 2007 4 17 SWAA071776 1 20070409 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 EEPLS PHOTOLUMINESCENT STRIP MISSING AT ROW 5 DEF. INSTALLED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007041700143 20070417 00143 NM 2007 4 17 SWAA071783 1 20070410 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 16 DEF. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007041700144 20070417 00144 NM 2007 4 17 SWAA071795 1 20070410 A 2560 PH22300L GLOWSTRIP BOEING 737 7373A4 1384585 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED 22Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 21 ABC. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007041700145 20070417 00145 NM 2007 4 17 SWAA071794 1 20070410 A 2560 PH22300L GLOWSTRIP BOEING 737 7373A4 1384585 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED 22Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 19 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007041700146 20070417 00146 NM 2007 4 17 SWAA071796 1 20070410 A 5523 REP4HE8 BEARING BOEING 737 7373A4 1384585 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED 22Y CHECK, LEFT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BUSHING AND BEARING PER MM. 2 L 7 2 4F RT A16WE 2007041700148 20070417 00148 WP 2007 4 17 AALA20070566 1 20070327 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 493AA 49731 SFO - EMERGENCY LIGHT AT OVERWING EXIT AT SEAT ROW 21 LEFT AND RIGHT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY L IGHT AT OVERWING EXIT AT SEAT ROW 21 LEFT AND RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007041700149 20070417 00149 NM 2007 4 17 AALA20070567 1 20070327 A 2910 272W1592175 HOSE BOEING 777 777223 1385213 NM HYD SYSTEM LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 772AN 29580 DECLARED EMERGENCY FOR ARRIVAL DUE TO AN EN ROUTE LOSS OF HYDRAULIC QUANTITY FROM CENTER HYDRAULIC TANK. CREW USED ALTE RNATE METHOD FOR FLAP AND GEAR DEPLOYMENT. LANDED WITHOUT INCIDENT AND HAD SUFFICIENT FLUID TO TAXI TO GATE UNDER OWN P OWER. FOUND CENTER HYDRAULIC LINE LEAKING UNDER NUMBER 14 SPOILER. REPLACED LEAKING HYDRAULIC LINE. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007041700154 20070417 00154 NM 2007 4 17 AALA20070580 1 20070330 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 379AA 25448 SFO - EMERGENCY LIGHTS ON LEFT SIDE SEAT ROWS 5 TO 7 INOPERATIVE. REPLACED BATTERY PACK M379 FOR EMERGENCY LIGHTS ON LE FT SIDE SEAT ROWS 5 TO 7. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007041700156 20070417 00156 WP 2007 4 17 AALA20070569 1 20070328 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7536A 49990 LGA - EMERGENCY EGRESS LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED FORWARD EGRESS BATTERY PACK FOR EMERGENCY E GRESS LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007041700157 20070417 00157 NM 2007 4 17 AALA20070570 1 20070328 A 3397 WIRE HARNESS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 344AN 33083 SFO - FOUND EMERGENCY LIGHT AT SEAT 28H INOPERATIVE. SECURED HARNESS FOR EMERGENCY LIGHT AT SEAT 28H. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007041700158 20070417 00158 WP 2007 4 17 AALA20070571 1 20070329 A 2131 21171803 CONTROLLER DOUG DC9 DC982 3022082 WP CABIN PRESSURE INOPERATIVE A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 7518A 49895 CABIN PRESSURE ROSE AT FLIGHT LEVEL 340 AND CABIN MASKS AUTO DEPLOYED AT FLIGHT LEVEL 140. EMERGENCY DESCENT TO 10000. AFTER LEVEL AT 10000 PACK FLOW RETURNED AND BOTH PRESSURIZATION CONTROLLERS RESET. FAILURE OCCURRED JUST AFTER EXITIN G ICING CONDITIONS AND ANTI ICE SECURED. LANDED ABQ WITHOUT INCIDENT. REPLACED BOTH NUMBER ONE AND NUMBER TWO CONTROLL ERS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007041700159 20070417 00159 WP 2007 4 17 AALA20070575 1 20070330 A 2130 CONTROL VALVE DOUG DC9 DC982 3022082 WP AIR CONDITIONING INOPERATIVE A AALA O OTHER J WARNING INDICATION DE DESCENT 1 SW 21 475AA 49650 PRESSURIZATION FLOW LIGHT ILLUMINATED DURING FLIGHT. CABIN ALTITUDE SLOWLY INCREASED FROM 4 TO 6.0 AT FLIGHT LEVEL 250. DECLARED EMERGENCY AND LANDED DFW WITHOUT INCIDENT. REPLACED FLOW CONTROL VALVE. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F A6WE 2007041700160 20070417 00160 SO 2007 4 17 SWIA200718090 1 20070409 A 5610 NP1513111 WINDSHIELD EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 585SW 1527 1527 120353 CAPTAINS WINDSHIELD CRACKED IN FLIGHT. REPLACED LEFT WINDSHIELD IAW MM 56-10-01. 2 L 7 2 4T RT A31SO 2007041700161 20070417 00161 2007 4 17 SWIA200718091 4 20070407 A 3170 8221310104 DCU CNDAIR CL600 CL6002C10 1390015 EA COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 07 707SK 1558 1558 10003 ELEVATOR SPLIT CAUTION MESSAGE FOLLOWED BY A CAS MISCOMP STATUS MESSAGE IN FLIGHT, RETURNED TO ORD. REPLACED NR 1 DCU I AW CRJ MM 31-41-04. 2 L 7 2 4F RT A21EA 2007041700163 20070417 00163 2007 4 17 SWIA200718093 4 20070401 A 2210 COMPUTER EMB 120 EMB120ER 3260203 SO AUTOPILOT MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 562SW 120336 AUTOPILOT PITCHES AIRCRAFT UP AND DOWN. REPLACED NR 1 AUTOPILOT COMPUTER IAW MM 22-00-00, P/N - 622-8315-102 S/N OFF - 1303. 2 L 7 2 4T RT A31SO 2007041700164 20070417 00164 EA 2007 4 17 SWIA200718094 1 20070406 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA CABIN ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 756SK 10221 THERE IS A FUEL ODOR IN THE CABIN. RAN ENGINES WITH PACKS RUNNING OFF OF ENGINE BLEED AIR. COULD NOT DUPLICATE DISCREP ANCY, 2 L 7 2 4F RT A21EA 2007041700166 20070417 00166 2007 4 17 SWIA200718096 4 20070402 A 2216 6224404101 ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA SERVO AILERON MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 756SK 10221 AUTOPILOT TRIM LWD CAUTION INTERMITTENT WITH ASSOCIATED "A" FLAG ON BOTH PFD'S. REPLACED AILERON SERVO IAW AMM 22-11-21 . 2 L 7 2 4F RT A21EA 2007041700167 20070417 00167 NM 2007 4 17 SB07026 1 20070410 A 3350 20131ASMI BATTERY PACK BOEING 737 7373B7 1384580 NM EMERGENCY LIGHTS DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 23381 CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AFT OF SEAT ROW 16 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BA TTERY PACK FOR AFT SECTION OF SEAT MOUNTED EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007041700168 20070417 00168 NM 2007 4 17 07FDEA01372 1 20070406 A 5313 AEA75452 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 CORROSION WAS FOUND ON LONGERON 28 BETWEEN STA 1273-1289 AFTER REMOVAL OF SCUFF PLATE ON R3 DOOR. [SUP 4-20-07] REMOVE D AND REPLACED AS PER SRM 51-33-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6- 2-100. 2 L 7 3 4F RT A22WE 2007041700170 20070417 00170 NM 2007 4 17 07FDEA01374 1 20070407 A 5320 656725061 SUPPORT BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 DURING PANEL CLOSE UP ON AFT BULKHEAD IN AFT PIT, CENTER LOWER PANEL, UPPER ANGLE CORRODED AROUND FASTENER HOLES. REMOV ED CENTER BULKHEAD PANEL SUPPORT ANGLE, REPAIRED BY INSTALLING 2 ANGLES AND A FILLER. RE-INSTALLED PANEL SUPPORT ANGLE REF SRM 51-40-4/FIG NR 1 PGS 1-9. 2 L 7 3 4F A3WE 2007041700173 20070417 00173 EA 2007 4 17 A6WA200740097 1 20070302 A 5210 601R3807423 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 450AW 7823 PAX DOOR ANCHOR FITTING (FWD) PN 601R380742-3 IS CRACKED. MAINTENANCE REPLACED PAX DOOR ANCHOR FITTING (FWD) PN 601R380 7423 IAW AMM 52-11-17-400-803. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041700174 20070417 00174 EA 2007 4 17 A6WA200740174 1 20070331 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 457AW 7854 RT FS 621.0 FLOOR SUPPORT ANGLE CRACKED APPROX.3 INCH LONG. (K) [SUP 05-01-07] MAINTENANCE CUT AWAY CRACKED ANGLE AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R-53-61-117 REV C. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041700176 20070417 00176 EA 2007 4 17 QXEA200700577 1 20070328 A 5753 SKIN CNDAIR CL600 CL6002C10 1390015 EA LT TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - LEFT INBOARD FLAP INNER SKIN CHAFED BY BONDING WIRE AT 2ND FROM INBOARD FLAP VANE GUIDE BEHIND PANEL 584BB. RE PAIRED IAW SRM 51-21-11, 57-52-01. 2 L 7 2 4F RT A21EA 2007041700177 20070417 00177 EU 2007 4 17 TRAX200700447 1 20070401 A 3350 LIGHT AEROSP ATR72 ATR72 EU AIRSTAIRS INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 632AS 338 EMERGENCY LIGHT ON AIRSTAIR INOP. 2 H 7 2 4T RT 2007041700178 20070417 00178 EA 2007 4 17 QXEA200700578 1 20070328 A 5754 SKIN CNDAIR CL600 CL6002C10 1390015 EA NR 1 SLAT GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - LOWER AFT EDGE OF RIGHT NR 1 SLAT SKIN IS GOUGED/CHAFED BELOW INBOARD METAL WIRE CONDUIT. REPAIRED IAW SRM 53- 00-01, 51-12-00. 2 L 7 2 4F RT A21EA 2007041700179 20070417 00179 EA 2007 4 17 QXEA200700579 1 20070326 A 5730 PANEL CNDAIR CL600 CL6002C10 1390015 EA RT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - RIGHT WING LEADING EDGE PANEL 622AR IS GOUGED/CHAFED ON LEADING EDGE. REPAIRED IAW SRM 57-00-01, 51-12-00. 2 L 7 2 4F RT A21EA 2007041700181 20070417 00181 NM 2007 4 17 07FDEA01482 1 20070412 A 5311 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 UPPER CARGO COMPARTMENT, FRAME STA 535 FOUND WITH SCRATCHES AT LONGERON 23 LT. [4-27-07] REPAIR CARRIED OUT AS PER SR M 53-5-03. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007041700182 20070417 00182 EA 2007 4 17 TRAX200700449 1 20070401 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 824AS 7203 A -FLAPS FAIL- MSG ON APPR, A/S 155 KTS. LEFT FLAP INDICATED 39 DEG, RIGHT FLAPS INDICATED 38 DEG. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007041700183 20070417 00183 EU 2007 4 17 07FDEA01486 1 20070413 A 5411 SPAR AIRBUS 310 A310324 3930206 EU ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 A 16MM LONG CRACK WERE FOUND IN THE END OF THE STIFFENER RIB 10 ON PYLON NR 2 LOWER SPAR. REPAIR PERFORMED IAW SB A310- 54-2016, APPROVED BY EO 6-5450-7-3302 PT 6. 2 L 7 2 4F RT A35EU 2007041700184 20070417 00184 EA 2007 4 17 TRAX200700450 1 20070401 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE J WARNING INDICATION CL CLIMB 1 SO 27 824AS 7203 FLAPS FAIL AT ZERO. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007041700185 20070417 00185 EU 2007 4 17 07FDEA01489 1 20070413 A 5210 A52111410202 FITTING AIRBUS 310 A310324 3930206 EU ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 CORROSION ON FITTING LT FWD PAX DOOR (P/N A521-11301-004, S/N G-1264). REPAIR PERFORMED BY REPLACEMENT OF PART IAW EA 6 -5211-103243 AND RAS/AS/104/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007041700189 20070417 00189 SO 2007 4 17 C2XAO7ON001 1 20070408 A 3350 2013A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16561 145610 ONT- NR 1 EMERGENCY LIGHT BATTERY WILL NOT HOLD CHARGE. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY IAW EMB 145 A MM 33-50-04. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007041700190 20070417 00190 EU 2007 4 17 07FDEA01493 1 20070413 A 4910 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 SEVERAL AREAS OF CORROSION IN AIR CONDITIONING COMPARTMENT, C39-C44, P37-50 RT. REPAIR PERFORMED BY BLEND OUT IAW EA 6- 5315-101310 AND RAS/045255/008/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007041700191 20070417 00191 EU 2007 4 17 07FDEA01494 1 20070413 A 4910 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 CORROSION ON SEVERAL AREAS AT AIR CONDITIONING COMPARTMENT, C39-C47, P44-P54 LT. REPAIR PERFORMED BY BLEND OUT IAW EA 6 -5315-101310 AND RAS/045255/008/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007041700195 20070417 00195 SO 2007 4 17 C2XA07TY019 1 20070409 A 5514 14501167603 BUSHING EMB 145 EMB145LR 3260212 SO HORIZ STAB MIGRATED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16951 145063 TYS - DURING A CURRENT 5C INSPECTION THE LT HORIZONTAL STAB HINGE FITTING WAS FOUND MIGRATED. MAINTENANCE REMOVED THE L T STAB BUSHING, REWORKED HOUSING TO THE 2ND OVERSIZE DIAMETER AND INSTALLED THE 2ND SIZE BUSHING IAW EMB 135/145 SRM 55- 10-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE 5C INSPECTION. 2 L 7 2 4T RT T00011AT 2007041700196 20070417 00196 SO 2007 4 17 C2XA07CL039 1 20070410 A 3234 7455503 CONTROL LEVER EMB 135 EMB135ER 3260203 SO COCKPIT FAULTY A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 27506 145206 CLE FLIGHT 2705 - THE CREW REPORTED THE NOSE GEAR DID NOT RETRACT ON 1ST ATTEMPT DURING CLIMBOUT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2007041700197 20070417 00197 NM 2007 4 17 CALA0700169 1 20070408 A 5340 69353502 STRINGER CLIP BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 INSPECTION FOUND A .75 INCH CRACK IN STRINGER CLIP AT STA 520, STRINGER 16L. A NEW STRINGER CLIP WAS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007041700198 20070417 00198 NM 2007 4 17 CALA0700170 1 20070404 A 5320 6546568520 STIFFENER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 INSPECTION FOUND RT CHANNEL STIFFENER AT THE BOTTOM CENTER OF THE AFT PRESSURE BULKHEAD CORRODED, STA 1016, BL 0. 2 L 7 2 4F RT A16WE 2007041700201 20070417 00201 EA 2007 4 17 COMA0770023 1 20070404 A 2742 70741 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA HORIZ STAB FAULTY A COMA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 371CA 10943 10082 FLIGHT 5280 - STAB CH2 STATUS MESSAGE DISPLAYED ON AND OFF CONTINUOUSLY DURING CLIMB, CRUISE, LANDING AND TAXI. TRIM IN MOTION ORAL ON CONTINUOUSLY. ELECTRICAL SMELL IN AFT CABIN. LANDED DEN WITHOUT INCIDENT. REPLACED STAB ACTUATOR MCU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007041700204 20070417 00204 SO 2007 4 17 FDKA200703136 1 20070327 A 3350 BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6163 FLL-PNS (1400 PHX LCL). ROW 12 OVERHEAD EMERGENCY LOCATOR SIGN INOP. MX RE-SECURED BATTERY BACK AT NR 2 POSIT ION. 2 L 7 2 4T RT T00011AT 2007041700205 20070417 00205 WP 2007 4 17 UPS07849617 1 20070331 A 5541 RIB DOUG DC8 DC873F 302199F WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 18TH RIB FROM BOTTOM OF RUDDER ON L/E CRACKED. STOP DRILLED CRACK ON 18TH RIB FROM BOTTOM OF L/E IAW SRM 55-2-0. FABRICATED AND INSTALLED REPAIR DOUBLER ON 18TH RIB IAW SRM 55-06-00 FIG 028. 2 L 7 4 4F RT 4A25 2007041700206 20070417 00206 WP 2007 4 17 UPS07849618 1 20070331 A 5541 RIB DOUG DC8 DC873F 302199F WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 12TH RIB FROM BOTTOM OF RUDDER ON L/E IS CRACKED. STOP DRILLED CRACK ON 12TH RIB ON RUDDER L/E IAW S RM 55-2-0. FABRICATED AND INSTALLED REPAIR DOUBLER ON 12TH RIB ON RUDDER L/E IAW SRM 55-2-0 FIG 2 SHEET 2. 2 L 7 4 4F RT 4A25 2007041700208 20070417 00208 WP 2007 4 17 UPS07849623 1 20070414 A 3350 LIGHT DOUG DC8 DC873F 302199F WP CABIN MALFUNCTIONED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:N/A BTB - AFTER TAXI DIMMING LIGHTS NOTICED THAT EMERGENCY EXIT LIGHTING WAS ILLUMINATED IN THE ARMED PO SITION WITH A/C POWER ON AIRCRAFT. RESET C/B. OPS CHECK NORMAL PER AMM 33-50-01-2. 2 L 7 4 4F RT 4A25 2007041700210 20070417 00210 NM 2007 4 17 KCSA071117 1 20070405 A 5313 FITTING BOEING 747 747236B 1384804 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STR 48L END FITTING BOLT HOLES ARE CORRODED FWD OF BS 2360. 2 L 7 4 4F A20WE 2007041700211 20070417 00211 NM 2007 4 17 KCSA071118 1 20070405 A 5313 FITTING BOEING 747 747236B 1384804 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STR 46R END FITTING BOLT HOLES ARE CORRODED FWD OF BS 2360. 2 L 7 4 4F A20WE 2007041700214 20070417 00214 NM 2007 4 17 KCSA071121 1 20070405 A 5313 FITTING BOEING 747 747236B 1384804 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STR 51L END FITTING BOLT HOLES ARE CORRODED FWD OF BS 2360. 2 L 7 4 4F A20WE 2007041700215 20070417 00215 NM 2007 4 17 KCSA071122 1 20070405 A 5313 FITTING BOEING 747 747236B 1384804 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STR 49L END FITTING BOLT HOLES ARE CORRODED FWD OF BS 2360. 2 L 7 4 4F A20WE 2007041700217 20070417 00217 NM 2007 4 17 KCSA071126 1 20070405 A 5313 FITTING BOEING 747 747236B 1384804 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STR 38L END FITTING BOLT HOLES ARE CORRODED FWD OF BS 2360. 2 L 7 4 4F A20WE 2007041700218 20070417 00218 NM 2007 4 17 KCSA071127 1 20070405 A 5313 FITTING BOEING 747 747236B 1384804 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STR 48R END FITTING BOLT HOLES CORRODED FWD OF BS 2360. 2 L 7 4 4F A20WE 2007041700220 20070417 00220 NM 2007 4 17 KCSA071129 1 20070405 A 5230 DOOR FRAME BOEING 747 747236B 1384804 NM CARGO DOOR DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 AFT PIT DOOR FRAME DENTED AT BS 1860, STR 38R. 2 L 7 4 4F A20WE 2007041700223 20070417 00223 NM 2007 4 17 KCSA071140 1 20070411 A 5313 STRINGER BOEING 747 747236B 1384804 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STR 23L AT STA 2170 DAMAGED. 2 L 7 4 4F A20WE 2007041700224 20070417 00224 NM 2007 4 17 KCSA071141 1 20070411 A 5311 FRAME BOEING 747 747236B 1384804 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 FRAME AT STA 500 STR 26L HAS TOOLING DAMAGE. 2 L 7 4 4F A20WE 2007041700225 20070417 00225 EU 2007 4 17 07FDEA01498 1 20070413 A 5330 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 FOUND CORROSION AT UPPER SKIN PANEL C91, P4 RT. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5319-103315 AND RAS/DAHAM/402086 1/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007041700226 20070417 00226 EU 2007 4 17 07FDEA01499 1 20070413 A 5322 A57112116200 SHEAR TIE AIRBUS 310 A310324 3930206 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 FOUND CRACKED HOLES DURING ACCOMPLISHMENT OF EO 6-5310-7-5020 PT.1, LHS (C43 HOLE H2 CRACK LENGTH 9MM; C45 HOLE H22 CRAC K LENGTH 7MM; C46 HOLE H29 CRACK LENGTH 8MM). REPAIR PERFORMED BY REPLACEMENT OF FITTING A538-70064 FOR HOLE H2, OVERSI ZING HOLE H22 AND H29 AND BUSH INSTALLATION IAW EA 6-5315-101331 AND RAS/AS/0133/2006 ISSUE "B". 2 L 7 2 4F RT A35EU 2007041700227 20070417 00227 NE 2007 4 17 MAC030702 2 20070324 A 7320 3045593 PRESSURE VALVE AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE NR 1 ENGINE WORN A MTNA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 33 809FX 217 124437 NR 1 ENGINE TEMPERATURE AND TORQUE FLUCTUATING DURING DEPARTURE. THE P 2.5 AIR PRESSURE VALVE WAS REBUILT WITH KIT 3045 593. 2 H 7 2 4T 4 T RT A53EU E2ONE 2007041700228 20070417 00228 NM 2007 4 17 07FDEA01376 1 20070408 A 2810 TANK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 UPPER AUX TANK FOUND WITH CORROSION BETWEEN STA 1219 TO 1235 X= -81.170, FOUND AFTER REMOVAL OF FLOOR PANEL TO FACILITAT E NDT INSPECTION. [SUP 4-20-07] COMPLIED WITH FEDEX E.A. 1-5720-109847. CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6 -2-100. 2 L 7 3 4F RT A22WE 2007041700229 20070417 00229 NM 2007 4 17 07FDEA01377 1 20070408 A 2810 TANK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 UPPER AUX TANK FOUND WITH CORROSION BETWEEN STA 1219 TO 1235 X= -40, FOUND AFTER REMOVAL OF FLOOR PANEL TO FACILITATE ND T INSPECTION. [SUP 4-20-07] COMPLIED WITH FEDEX E.A. 1-5720-109847. CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-1 00. 2 L 7 3 4F RT A22WE 2007041700230 20070417 00230 NM 2007 4 17 07FDEA01378 1 20070408 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 UPPER MAIN CARGO COMPARTMENT FOUND SEAT TRACK CORROSION ON STA 1179 TO 1199, X= -8.5. [SUP 4-20-07] REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007041700234 20070417 00234 EU 2007 4 17 AALA20070581 1 20070331 A 5210 BOTTLE AIRBUS 300 A300B4605R 3930308 EU L1 DOOR LOW PRESSURE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 40064 507 MIA - LEFT NUMBER ONE AND RIGHT NUMBER FOUR DOOR ASSIST BOTTLE PRESSURE READS LOW. SERVICE LEFT NUMBER ONE AND RIGHT NU MBER FOUR DOOR ASSIST BOTTLES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007041700236 20070417 00236 NE 2007 4 17 NOCA07907 2 20070406 A 7412 106310451 EXCITER BOEING 767 767306 1385148 NM GE CF6 CF680C2B7 NE RT ENIGNE FAILED A NOCA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 15 765NA 28098 DURING RT ENG START NO LIGHT OFF RT ENG IGNITOR 2 EICAS. REMOVED AND REPLACED NR 2 EXCITER BOX, ALSO REMOVED AND REPLAC ED NR 1 AND 2 IGNITOR PLUGS P/N CH31772A PER MM 74-11-01 AND 74 21-02, OPS CHECK OK. 2 L 7 2 4F 4 F RT A1NM E13NE 2007041700237 20070417 00237 WP 2007 4 17 ARWA20070306 1 20070322 A 2910 HOSE DOUG DC8 DC863F 302198F WP HYD SYSTEM LEAKING A ARWA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 441J 45988 IN FLIGHT EN COUNTER A LOSS OF HYDRAULIC PRESSURE; PERFORMED EMERGENCY CHECKLIST. T/S AND FOUND RT MAIN LANDING GEAR BO GIE TRIM CYLINDER HYDRAULIC HOSE LEAKING; REMOVED AND REPLACED IN ACCORDANCE WITH DC8 M/M 32-33-1. SERVICE HYDRAULIC RE SERVOIR IN ACCORDANCE WITH DC8 M/M 12-30-1 AND PERFORMED LEAK CHECK IN ACCORDANCE WITH 29-00, NO LEAKS FOUND. 2 L 7 4 4F 4A25 2007041300088 20070413 00088 NM 2007 4 13 QXEA200700538 1 20070328 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX-FUSELAGE SKIN INTERNAL DOUBLER IS CORRODED BELOW GUSSET FITTING AT AFT LOWER CORNER OF DOOR APERATURE X598-X600, Z100, Y34L. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-20-36, AND 51-40-11. 2 H 7 2 4T RT A13NM 2007041300089 20070413 00089 NM 2007 4 13 QXEA200700539 1 20070328 A 5320 WEB DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 C4 PDX - WEBBING IS CORRODED BELOW CARGO DOOR THRESHOLD SILL AT 3 RIVETS, X593-X596, Z98.5, Y28L. REPAIRED IAW SRM 51-2 0-11, 51-20-36, AND 51-40-11. 2 H 7 2 4T RT A13NM 2007041300090 20070413 00090 NM 2007 4 13 F3LA200700070 1 20070330 A 5315 D5347209001100 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED LIGHT CORROSION AROUND NUT PLATE HOLE ON SEAT TRACK AT -Y1292, FR65. REMOVED AN D INSTALLED FLOORBEAM IAW A319 SRM 51-42-11; 51-42-11, FIG 8; 51-42-11, PARA 7; AND 51-42-11, STEP 7 B. 2 L 7 2 4F RT A28NM 2007041300091 20070413 00091 NM 2007 4 13 KCSA071111 1 20070403 A 5412 BULKHEAD BOEING 747 747249F 1384849 NM NR 3 NACELLE CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 NR 3 PYLON NAC STA 221.9 BULKHEAD WEB CHAFED AT HYD FITTINGS. 2 L 7 4 4F A20WE 2007041300092 20070413 00092 NM 2007 4 13 F3LA200700071 1 20070329 A 5320 D5347043620800 SILL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED L2 SILL PLATE UPPER SPLICE ANGLE FWD OF FR 66 AT Y1732, INBD SIDE, CORRODED. IN STALLED REPLACEMENT SPLICE ANGLE IAW A319 SRM 51-42-11. 2 L 7 2 4F RT A28NM 2007041300093 20070413 00093 NM 2007 4 13 2007UALA00997 1 20070402 A 5210 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 1R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 R-1 DOOR INTERCOSTAL CRACKED AT LIGHTNING HOLE WHERE HANDLE BOX CONTROL ROD PASSES THROUGH. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED/ INSTALLED DOUBLER FILLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041300094 20070413 00094 NM 2007 4 13 KCSA071130 1 20070406 A 5330 SKIN BOEING 747 747236B 1384804 NM BS 2650 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 CRACK IN EMPENNAGE SKIN EXTENDING THROUGH PREVIOUS REPAIR AT STA 2650 WL 315 LBL 40. 2 L 7 4 4F A20WE 2007041300095 20070413 00095 NM 2007 4 13 KCSA071131 1 20070406 A 3350 LIGHT BOEING 747 747236B 1384804 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 701CK 21730 SILL LIGHT AT RIGHT ESCAPE HATCH DOESN'T ILLLUMINATE. 2 L 7 4 4F A20WE 2007041300096 20070413 00096 WP 2007 4 13 IXXA07SMN090S 1 20070208 A 5100 SKIN DOUG DC8 DC862 3021970 WP ZONE 500 MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, LEFT OUTBOARD AILERON UPPER SKIN NON STANDARD REPAIR, STATION XA 646.000. REMOVED S KIN WITH EXISTING REPAIR. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREAT ED AND PRIMED AREA AND REPAIR PART. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIRED PARTS FROM STATION XW 546.0 00 TO XA 742.000. BALANCED AILERON, FOUND WITHIN TOLERANCE. MOMENT:3345.41 IN-LBS IAW DC8 SRM 51-1-21, DC8 SRM 57-8-1 FIGURE 4, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 57-8-1 FIGURE 4 ITEM "F" AND "G", DC8 SRM 51-1-9 TR NUMBER 51- 142 DATED 04-05-06, DC8 SRM 51-1-8B, DC8 SRM 51-1-11. 2 L 7 4 4F 4A25 2007041300097 20070413 00097 WP 2007 4 13 IXXA07SMN092S 1 20070208 A 5512 SKIN DOUG DC8 DC862 3021970 WP ZONE 300 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, RIGHT HORIZONTAL STABILIZER INBOARD LEADING EDGE OUTER SKIN CORRODED, STATION XFS 47. 500. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION NO CRACK OR CORROSION FO UND. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. APPLIED SEALANT TO F AYING SURFACES. INSTALLED REPAIR PARTS FROM STATION XFS 47.500 IAW FAA FORM 8110-3 NUMBER 07058 DATED 02-15-07, SEMAN DRAWING NUMBER ED-4459 DATED 02-14-07, EO SEMAN NUMBER 2007211 DATE 02-15-07, SEMAN NUMBER 2007211 DATE 02-15-07, SEMA N DRAWING NUMBER ED-4459 DATED 02-14-07, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-1-20D, DC8 SRM 51-3-1, DC8 NDT SP 2 L 7 4 4F 4A25 2007041300098 20070413 00098 NM 2007 4 13 F3LA200700069 1 20070329 A 5320 FITTING AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED LT AFT LAV D FWD WALL CORRODED AT OTBD ANCHOR POINT. REMOVED AND CLEANED FITTIN G AND REINSTALLED WITH NEW HARDWARE IAW CMM 25-43-51, PAGES 305, 618 AND 740. 2 L 7 2 4F RT A28NM 2007041300099 20070413 00099 NM 2007 4 13 F3LA200700067 1 20070329 A 5340 FITTING AIRBUS A319 A319111 3930336 NM CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED LT AFT LAV D, AFT WALL INBD ANCHOR POINT CORRODED. REMOVED AND CLEANED FITTING. REINSTALLED FITTING WITH NEW HARDWARE IAW CMM 25-43-51, PAGES 303, 618 AND 740. 2 L 7 2 4F RT A28NM 2007041300100 20070413 00100 WP 2007 4 13 IXXA07SMN089S 1 20070208 A 5330 SKIN DOUG DC8 DC862 3021970 WP ZONE 200 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT UPPER SKIN CORRODED AT STATION 1730.000. REMOVED FASTENERS AS NEEDED TO P ERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREA TED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-8 PA GES 17-18, DC8 SRM 53-2-0 PAGE 2P, DC8 SRM 53-5-2 FIGURE 1 ITEM "B", DC8 SRM 51-1-8B, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 53-2-1 FIGURE 7 SHEET 1 AND 5, DC8 SRM 51-1-21, DC8 SRM 51-1-20D AND DC8 SRM 51-3-1. 2 L 7 4 4F 4A25 2007041300101 20070413 00101 NM 2007 4 13 F3LA200700068 1 20070328 A 5340 FITTING AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED AFT LT LAV, AFT INBD MOUNTING HOLES IN LAV WALL WORN, ELONGATED AND CORRODED. R EMOVED AND CLEANED FITTING. REINSTALLED FITTING WITH NEW HARDWARE IAW CMM 25-43-51, PAGES 303, 618 AND 740. 2 L 7 2 4F RT A28NM 2007041300102 20070413 00102 EA 2007 4 13 A6WA200740098 1 20070304 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 202 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 450AW 7823 VISUAL INDICATION OF CRACK IN FWD PRESSURE BULKHEAD FS202.75, WL69.0, LBL23.71 (JUST BELOW PARKING BRAKE CABLE). MEASUR ES APPROX 1.0 INCH LONG. MAINTENANCE CUT-OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-11-563. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041300103 20070413 00103 WP 2007 4 13 ASAA0781568 1 20070327 A 5330 5930543 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE SCRATCHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 LARGE SCRATCHES ON LEFT FUSELAGE. REMOVED DAMAGED AREA. INSTALLED TWO EXTERNAL REPAIR DOUBLERS PER SRM 53-4. 2 L 7 2 4F RT A6WE 2007041300104 20070413 00104 EA 2007 4 13 A6WA200740101 1 20070302 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 84 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 453AW 7838 INTERCOSTAL CRACKED AT FS484.0, RBL 36.0. MAINTENANCE CUT AWAY DAMAGED FLANGE AND INSTALLED REPAIR ANGLE IAW BSC SR 601 -53-0030A AND REO 601R-53-41-059, REV A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041300105 20070413 00105 NM 2007 4 13 KCSA071132 1 20070409 A 5714 SKIN BOEING 747 747236B 1384804 NM BS 1238 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 CENTER WING SECTION UPPER SKIN PANEL CORRODED AT BS 1238, RBL 90. 2 L 7 4 4F A20WE 2007041300106 20070413 00106 NM 2007 4 13 KCSA071133 1 20070409 A 5311 FRAME BOEING 747 747236B 1384804 NM BS 820 S11L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 BS 820 FUSELAGE FRAME CRACKED AT STR 11L. 2 L 7 4 4F A20WE 2007041300107 20070413 00107 NM 2007 4 13 KCSA071134 1 20070409 A 5322 SHEAR TIE BOEING 747 747236B 1384804 NM BS 820 S11L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 BS 820 FUSELAGE FRAME SHEAR TIE CRACKED ABOVE STR 11L. 2 L 7 4 4F A20WE 2007041300108 20070413 00108 NM 2007 4 13 2007UALA00958 1 20070330 A 3397 GB6341DC GROUND STUD BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 CEILING LIGHTS AT SEAT 3E & SEAT 9D ARE OUT. FOUND EMERGENCY AREA LIGHTS INOP AT SEVERAL SEATS. TROUBLESHOOTING REVEAL ED THAT GROUND BLOCK CORROSION IS INHIBITING STRUCTURAL GROUND. REPLACED GROUNDING STUD. EEL SYSTEM OP CHECKS OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007041300109 20070413 00109 EU 2007 4 13 2007UALA00960 1 20070330 A 3350 32145410 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 458UA 1163 FWD EPSU BATTERY FAULT & EPSU BATTERY L DISPLAYED ON PTP. REPLACED BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041300110 20070413 00110 2007 4 13 2007UALA00980 4 20070330 A 2565 ORING O-RING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SLIDE ACTUATOR LEAKING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 LOW BOTTLE PRESSURE. ACTUATOR ASSEMBLY LEAKING. REPLACED WITH NEW VALVE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041300112 20070413 00112 NM 2007 4 13 F3LA200700073 1 20070330 A 5322 SHEAR TIE AIRBUS A319 A319111 3930336 NM FUSELAGE SHEARED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED SHEAR PLATE WAS SHEARED BETWEEN FR 68 AND FR 69 JUST OTBD OF FLOORBEAM Y1292. F ABRICATED AND REPLACED SHEAR PLATE IAW A319 SRM 51-42-11, FIG 7 AND 8; 53-41-14, FIG 18; 51-42-11; AND 51-20-00, PARA. 3 ; 51-23-11. 2 L 7 2 4F RT A28NM 2007041300113 20070413 00113 EA 2007 4 13 A6WA200740099 1 20070302 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 453AW 7838 FLOOR SUPPORT ANGLE AT FS621.0 IS CRACKED (LT) MAINTENANCE REPAIRED LT FS621 FLOOR SUPPORT ANGLE IAW REO 601R-53-61-117, REV C. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041300115 20070413 00115 NM 2007 4 13 2007UALA00982 1 20070401 A 3350 78941 LAMP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 206UA 30212 EMERGENCY PATH MARKING LIGHT ONE BROKEN AT SEAT 2F. REPLACED LIGHT STRIP. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007041300118 20070413 00118 EU 2007 4 13 2007UALA00984 1 20070402 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 432UA 587 FWD LEFT FUSELAGE SKIN HAS A DENT FR21, STR 23L. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. THIS REPAIR ALS O ENCOMPASSES CF9019. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041300119 20070413 00119 NM 2007 4 13 2007UALA00985 1 20070402 A 5310 DOOR FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 925UA 26646 DENT IN FUSELAGE FWD OF AFT CARGO DOOR. LOCATED ON FWD DOOR FRAME, 19 INCHES FROM BOTTOM OF DOOR. DAMAGE IS ACROSS SEV ERAL FLUSH RIVET HEADS. ALSO HAS A CRACK IN THE OUTER SKIN. *S/D* MAJOR REPAIR: DAMAGE REMOVED, FABRICATED AND INSTA LLED REPAIR PARTS. REFERENCE EVA 70158A. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041300120 20070413 00120 NM 2007 4 13 2007UALA00986 1 20070402 A 3350 582240 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY FLOOR LIGHTS FLICKER ROW 53 AFT. AFTER TROUBLESHOOTING REPLACED M6013 EMERGENCY LIGHTS POWER SUPPLY ASSY AND BATTERY AS PER MAINTENANCE PRACTICES 33-51-04. LIGHTS 53 AFT OP CHECKED OK AFTER REPLACEMENT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041300121 20070413 00121 NM 2007 4 13 2007UALA00987 1 20070403 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY CEILING LIGHT INOP AT DOOR 2L & 3R. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041300122 20070413 00122 NM 2007 4 13 2007UALA00988 1 20070403 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 180UA 25224 EEL 1A AFT, 5A AFT, 36 LT & 44 RT ARE INOPERATIVE. RELAMPED EEL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041300123 20070413 00123 NM 2007 4 13 2007UALA00989 1 20070403 A 3350 7945243 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 MID LAV CROSS AISLE EMERGENCY LIGHT INOPERATIVE. *S/D* SECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041300124 20070413 00124 NM 2007 4 13 2007UALA00990 1 20070403 A 3397 794640 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 DOOR 5R EEL CROSS AISLE INOPERATIVE. *S/D* REPAIRED FEEDER AT CROSS AISLE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041300125 20070413 00125 NM 2007 4 13 2007UALA00991 1 20070403 A 3350 80591 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L4 DOOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 MED 4L, DOOR MOUNTED EMERGENCY LIGHT INOP. REPLACED LIGHT ASSEMBLY & OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041300127 20070413 00127 NM 2007 4 13 2007UALA00993 1 20070403 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 CABIN -E- ONE LEFT CEILING EMERGENCY LIGHTS INOP. RECHARGED BATTERY PACK, OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041300128 20070413 00128 NM 2007 4 13 2007UALA00994 1 20070403 A 3397 80172424 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 SEAT EEL NOT ILLUMINATED SEAT 4F. REPLACED EEL CABLE, OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041300129 20070413 00129 EA 2007 4 13 QXEA200700550 1 20070329 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - 2 SMALL AREAS OF SUSPECTED SURFACE CORROSION ON FUSELAGE SKIN BARE METAL/FASTENER JUST FORWARD AND BELOW PAX DO OR FUSELAGE HINGE HALF FORWARD CAP. REPAIRED IAW SRM 51-21-06 AND 51-25-06. 2 L 7 2 4F RT A21EA 2007041300130 20070413 00130 EA 2007 4 13 QXEA200700551 1 20070331 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 302 S20R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - SMALL NICK IN EXTERIOR FUSELAGE SKIN, RIGHT SIDE AT FS 302.00 AND STRINGER 20R. REPAIRED IAW SRM 53-21-01. 2 L 7 2 4F RT A21EA 2007041300131 20070413 00131 EA 2007 4 13 QXEA200700553 1 20070405 A 5350 RADOME CNDAIR CL600 CL6002C10 1390015 EA NOSE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - NOSE RADOME HAS EVIDENCE OF LIGHTNING STRIKE BURN THROUGH WITH DISBONDING ON INTERNAL SURFACE. REPAIRED IAW SR M 53-81-80. 2 L 7 2 4F RT A21EA 2007041300132 20070413 00132 EA 2007 4 13 QXEA200700554 1 20070331 A 5347 MOUNT CNDAIR CL600 CL6002C10 1390015 EA GALLEY MOUNT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - FORWARD GALLEY INBOARD AFT MOUNT FOOT HAS CORROSION. REPAIRED IAW CMM 25-32-97. 2 L 7 2 4F RT A21EA 2007041300133 20070413 00133 EA 2007 4 13 QXEA200700555 1 20070401 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - UPPER TCAS ANTENNA MOUNT SKIN HAS CORROSION. REPAIRED IAW SRM 51-21-06, 53-21-01, AND 51-21-11. 2 L 7 2 4F RT A21EA 2007041300134 20070413 00134 EA 2007 4 13 QXEA200700552 1 20070403 A 5330 PANEL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE TOOL DAMAGE A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - FUSELAGE OVERWING PANEL 172BR HAS 1 FASTENER HOLE WITH TOOLING DAMAGE. REPAIRED IAW REO670-53-82-337AND SRM 51 -42-06. 2 L 7 2 4F RT A21EA 2007041300136 20070413 00136 NM 2007 4 13 NWAA071283121 1 20070410 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319114 3930350 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 321NB 17384 17384 1414 EPSU INT LOAD EMER L FAULT MESSAGE DURING EMERGENCY ESCAPE LIGHT CHECK. REPLACED EPSU 11WL. CHECKS OK. 2 L 7 2 4F RT A28NM 2007041300137 20070413 00137 NM 2007 4 13 F3LA200700074 1 20070408 A 5320 BRACKET AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C-4/S-1 CHECK, INSPECTION REPORTED BRACKET FOR ANTENNA CORRODED IN AFT PIT UNDER FLOOR PANEL 151VG, AT APPROX STR 43, BETWEEN FR 58 AND FR 59. REMOVED, FABRICATED AND INSTALLED REPLACEMENT BRACKET IAW A319 SRM 51-42-11, PARA 6 D AND FIG 8; 51-31-00, TABLE 4; 51-70-12, PARA 1E, TABLES 3 AND 4; 51-21-11, PARA 1B; 51-75-12, PARA. 4; 51-42-11, PARA. 6; A ND AIRBUS DRAWING D53910479. 2 L 7 2 4F RT A28NM 2007041600001 20070416 00001 EU 2007 4 16 07FDEA01477 1 20070412 A 5415 ATTACH FITTING AIRBUS 310 A310 EU PWA 4152 PW4152 NE ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 CORROSION ON PYLON NR 2 BEARING HOLE ON RIB 18 LOWER ATTACH FITTING. REPAIR PERFORMED BY REAM UP HOLE AND CHAMFER ON EAC H SIDE IAW SB: A310-54-2021 AND EA 6-5451-103241. 2 L 7 2 4F RT A35EU E24NE 2007041600022 20070416 00022 NM 2007 4 16 SWAA071780 1 20070409 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 402WN 29814 DURING SCHEDULED 6Y CHECK, FOUND EEPLS COVER CRACKED AT ROW 17 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007041600023 20070416 00023 NM 2007 4 16 SWAA071811 1 20070410 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 415WN 29836 DURING SCHEDULED MV3 CHECK, FOUND EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007041600024 20070416 00024 2007 4 16 SWAA071791 4 20070410 A 2565 61621469 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED C3 CHECK, R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EV AC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007041600025 20070416 00025 NM 2007 4 16 SWAA071784 1 20070410 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 767 S19L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 19L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007041600032 20070416 00032 NM 2007 4 16 2007UALA00998 1 20070402 A 5210 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR ASSIST READS LOW A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 569UA 26677 DOOR 1R ASSIST BOTTLE HAS LOW AIR PRESSURE. [06-14-07] REPLACED BOTTLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041600034 20070416 00034 NM 2007 4 16 2007UALA01000 1 20070402 A 3350 60121 COVER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT WRONG PART A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 646UA 25283 EEL LIGHTING AT ROWS 1&2 RT FOUND TORN UP AND DAMAGED. FOUND EEL CABLES DAMAGED DUE TO IMPROPER CABLE COVER. ORDERED & INSTALLED COVER STRIP OF PROPER LENGTH AND END PIECES AS WELL. OP CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007041600036 20070416 00036 NE 2007 4 16 2007UALA01002 2 20070331 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 2 VIBRATION A UALA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 215UA 30221 777104 NR 2 ENGINE VIBRATION. [SUP 5-1-07] ACCOMPLISHED TRIM BALANCE RUN PER MM72-31-00. ACCOMPLISHED INSPECTIONS OF ALL CHI P DETECTORS PER 79-22-01, AND ACCOMPLISHED INSP. PER FIM 71-05 TASK 821, ITEM B1,C2,3,4,5,6 ONLY ALL ITEMS CHECK OK. A/ C RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007041600038 20070416 00038 NM 2007 4 16 2007UALA01004 1 20070330 A 2131 CONTROLLER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN ALTITUDE MALFUNCTIONED A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 381UA 24656 DURING DESCENT AT FL230 CABIN ALT WARNING SOUNDED AND CABIN WAS AT 9800. [SUP 5-1-07] FOUND FAULTY CABIN PRESSURE CONTR OLLER. REPLACED CABIN PRESSURE CONTROLLER. SHOP FOUND LOOSE SCREW ON TRANSFORMER. BAD Q3. REPLACED Q3. REPAIRED AND TE STED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041600056 20070416 00056 NM 2007 4 16 2007UALA01011 1 20070403 A 3150 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE UNKNOWN A UALA O OTHER J WARNING INDICATION TO TAKEOFF 1 WP 29 662UA 27159 THE -L ENG PRV- EICAS MSG DISPLAYED ON TAKEOFF. [SUP 5-1-07] REPLACED PRV AND PRVC PER MM 36-11-18 AND 36-11-19. PERFO RMED SUCCESSFUL TEST OF PRV-PRC SYSTEM. NO DEFECTS OBSERVED. A/C RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007041600058 20070416 00058 NM 2007 4 16 2007UALA01013 1 20070403 A 5270 CONTROL PANEL BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE DOOR 4R MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26877 DOOR 4R EMERGENCY SIGNAL HORN SOUND IS WEAK. [SUP 5-1-07] REPLACED EMERGENCY EVACUATION SIGNAL PANEL ASSEMBLY, OP CHE CKED OK 2 L 7 4 4F 4 F RT A20WE E24NE 2007041600059 20070416 00059 EU 2007 4 16 2007UALA01014 1 20070403 A 2530 COFFEEMAKER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GALLEY SMOKE A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 480UA 1555 RTFL DUE TO CREW REPORT OF SMOKE IN THE CABIN. [SUP 05-04-07] SOURCE OF SMOKE WAS TRACED BACK TO A DEFECTIVE COFFEEMAK ER IN THE AFT GALLEY. IT WAS DETERMINED THAT A FAULTY HEATER POWER RELAY CONTINUED TO SUPPLY POWER TO THE TANK HEATER EL EMENTS EVEN THOUGH THE CONTROL CIRCUITRY COMMANDED THE HEATERS TO BE TURNED OFF. PRIOR TO THE TRIPPING OF A SAFETY THERM OSTAT, THE SMOKE POINT OF THE POTTING COMPOUND ENCASING THE WIRING WAS EXCEEDED CAUSING SMOKE TO BE RELEASED INTO THE CA BIN. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041600061 20070416 00061 NM 2007 4 16 2007UALA01016 1 20070403 A 5320 BRACKET BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 246 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 644UA 25094 PULLEY SUPPORT BRACKET CRACKED FWD FACE OF BS 246 FLOORBEAM AT RBL 14. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALL ED BRACKET STIFFENER. 2 L 7 2 4F 4 F RT A1NM E24NE 2007041600062 20070416 00062 2007 4 16 2007UALA01017 4 20070403 A 2565 COVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SLIDE PACK 1L UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 434UA 592 SLIDE PACK COVER 1L FELL OFF. [SUP 05-18-07] SECURED SLIDE COVER. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041600072 20070416 00072 NM 2007 4 16 2007UALA01023 1 20070403 A 3397 BR964321 WIRE HARNESS BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 773UA 26929 EMERGENCY LIGHTS AT SEAT 2E INOPERATIVE. FOUND HARNESS DISCONNECTED. CONNECTED HARNESS, TESTED GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007041600098 20070416 00098 SO 2007 4 16 SIMA200709913 1 20070406 A 5315 14521413605 FLOORBEAM EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 708AE 15810 4800 145205 CENTER OMEGA BEAM CORRODED AT FRAME 33. PERFORMED CUTOUT OF CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SR M 53-00-10, FIGURE 203. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041600099 20070416 00099 SO 2007 4 16 SIMA200709902 1 20070408 A 2120 UNKNOWN EMB 135 EMB135LR 3260305 SO CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 710TB 145224 STRONG FUEL ODOR NOTICED WITH BOTH PACKS RUNNING, APU WAS ONLY BLEED SOURCE ON. RAN BOTH ENGINES WITH PACKS AND NO ODOR NOTED, MEL 49-01. 2 L 7 2 4F RT T00011AT 2007041600105 20070416 00105 SO 2007 4 16 SIMA200709911 1 20070403 A 5311 1433747401 FRAME EMB 145 EMB145LR 3260212 SO ZONE 100 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 931AE 4768 4768 14500912 ADDITIONAL HOLE DRILLED DURING ACCOMPLISHMENT OF EMB SB 145-53-0068 AT FRAME 47 BETWEEN STRINGER 10L AND STRINGER 11L. FABRICATED AND INSTALLED REINFORCEMENT ON FRAME 47 BETWEEN STRINGER 10L AND 11L IAW EMB IC2007-145-02316. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007041700007 20070417 00007 EA 2007 4 17 QXEA200700575 1 20070328 A 5730 ACCESS PANEL CNDAIR CL600 CL6002C10 1390015 EA LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - LEFT WING INBOARD FLAP ACCESS PANEL 584GB IS CHAFED ON OUTER SURFACE BY ACTUATOR CUTOUT. REPAIRED IAW SRM 51-2 1-11, 57-52-01. 2 L 7 2 4F RT A21EA 2007041700013 20070417 00013 SO 2007 4 17 RAIA00704027 1 20070410 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 803HK 145077 PRE FLT 3551 - PIT - EMERGENCY LIGHT FLOOR PROXIMITY LIGHTS INOP. MAINTENANCE DEFERRED FLOOR PROXIMITY STRIP PER MEL. 2 L 7 2 4F RT T00011AT 2007041700029 20070417 00029 NE 2007 4 17 GUUA04110701 2 20070411 A 7310 AS3209009 O-RING BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NR 2 ENGINE LEAKING A GUUA E A ENGINE SHUTDOWN UNSCHED LANDING K Y J FLUID LOSS ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SO 29 81556 UE239 114291 FLIGHT 9305: AFTER TAKEOFF THE NR 2 ENGINE HAD A PARTIAL LOSS OF POWER. SHORTLY AFTER A TOTAL POWER LOSS OCCURED. SECURE D THE NR 2 ENGINE. RETURNED TO DEPARTURE LANDED WITHOUT INCIDENT. DETERMINED FUEL TRANSFER TUBE O-RING TO BE CRACKED AN D LEAKING. REPLACED TRANSFER TUBE O-RING. LEAK CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A24CE E26NE 2007041700032 20070417 00032 NM 2007 4 17 CALA0700172 1 20070410 A 5310 6520722U70 DOOR FRAME BOEING 737 7373T0 1384582 NM CARGO DOORWAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 FWD CARGO DOOR CUTOUT, FWD FRAME CRACKED AROUND THE LOWER STOP PAD FITTING. REPLACED FRAME IAW SRM 51-40-02, AND DRAWIN G 65-20722. 2 L 7 2 4F RT A16WE 2007041700035 20070417 00035 NM 2007 4 17 ASMF200704007 1 20070410 A 3610 32144464 VALVE BOEING 737 737* NM CFMINT CFM567 CFM567B22 13802 NE RT PRECOOLER FAILED W ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 997AM 12163 30283 889997 AIRCRAFT AIR-TURNED BACK DUE TO RT ENGINE BLEED TRIP OFF LIGHT, TURNED ON. AT CUU, TECH PERSONNEL DEFERRED REPORT IAW ME L 36-8. DURING OVERNIGHT CHECK; RT HIGH STAGE PRECOOLER VALVE WAS REPLACED IAW MM 36-11-06, TESTED CORRECT. OVERWEIGHT I NSPECTION WAS NOT REQUIRED DUE TO AIRCRAFT LANDED WITH 53,315 KILOGRAMS AND THE MAXIMUM LANDING WEIGHT IS 58,059 KILOGRA MS. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007041700041 20070417 00041 SO 2007 4 17 C2XA07IA084 1 20070408 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12957 145080 IAH - DURING MAINTENANCE INSPECTION, THE FIRST TWO AILSE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE NR 2 INVERTER, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS, AND THE AIRCRAFT WAS AP PROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007041700043 20070417 00043 NM 2007 4 17 CALA0700171 1 20070410 A 5311 BAC15035828 FRAME BOEING 737 7373T0 1384582 NM BS 616 S17R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 616 JUST BELOW FLOORLINE, S17R. THE CRACKED AREA OF FRAME WAS CUT OUT A ND A REPAIR ANGLE WAS INSTALLED IAW ECRA 5311-01158. 2 L 7 2 4F RT A16WE 2007041700048 20070417 00048 NM 2007 4 17 KCSA071146 1 20070412 A 5313 STRINGER BOEING 747 747236B 1384804 NM BS 2360 S38R CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 FWD OF BS 2360, STR 38R END FITTING BOLT HOLES CORRODED. 2 L 7 4 4F A20WE 2007041700050 20070417 00050 SO 2007 4 17 RAIA00703078 1 20070331 A 3340 LAMP EMB 145 EMB145LR 3260212 SO FLOOD LIGHT LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 835HK 145670 POST FLT 7931 - ORD - LEFT FWD WING/FUSELAGE FAIRING EXTERIOR FLOOD LIGHT IS INOP. MAINTENANCE RESECURED LAMP, OPS CHEC K GOOD. 2 L 7 2 4T RT T00011AT 2007041700057 20070417 00057 NM 2007 4 17 ASMF200704009 1 20070412 A 2150 20495054 COOLING TURBINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE LEFT CONTAMINATED W ASMF D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 23 162PL 24399 2783 49765 AIRCRAFT RETURNED TO PLATFORM DUE TO SMOKE DETECTORS ALARMS OF AFT LAVATORIES WERE ACTIVATED BEFORE TAKE-OFF. DURING MAI NTENANCE INSPECTION, IT WAS DETECTED OIL CONTAMINATION IN DUCTS OF COOLING TURBINE, WATER SEPARATOR AND PRIMARY AND SECO NDARY HEAT EXCHANGERS OF LT AIR CONDITIONED SYSTEM. TURBINE COOLING, WATER SEPARATOR AND HEAT EXCHANGERS WERE REPLACED I AW M/M 21-51-01, 21-20-02, 21-51-02 AND 21-51-03 RESPECTIVELY, TESTED ALL CORRECT IAW M/M 21-00-00. AS A PRECAUTIONARY A CTION, LT SMOKE DETECTOR WAS REPLACED IAW AVAS MRB 26-14-00-01 TESTED ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007041700062 20070417 00062 NM 2007 4 17 QXEA200700601 1 20070405 A 5740 BRACKET DHAV DHC8 DHC8202 2809007 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - RIGHT WING FORWARD SPAR LOWER LEADING EDGE BRACKET AT YW 138.0 IS CRACKED. REPAIRED IAW SRM 51-40-00, 51-40-11 . 2 H 7 2 4T RT A13NM 2007041700065 20070417 00065 NM 2007 4 17 QXEA200700604 1 20070406 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - CORROSION ON SEAT TRACK NR 4 AT STATION X297-X299. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2007041700107 20070417 00107 NM 2007 4 17 SWAA071834 1 20070411 A 5330 6518420 SKIN BOEING 737 7373Y0 1384671 NM BS 302-304 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 302 TO BS 304, BETWEEN WL 234 TO WL 239. REPAIRED SKIN PE R ER. 2 L 7 2 4F RT A16WE 2007041700119 20070417 00119 NM 2007 4 17 SWAA071806 1 20070410 A 5311 6546548 FRAME BOEING 737 7375H4 138449D NM BS 747 S8R-8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007041700120 20070417 00120 NM 2007 4 17 SWAA071802 1 20070410 A 5311 6546550 FRAME BOEING 737 7375H4 138449D NM BS 787 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007041700121 20070417 00121 NM 2007 4 17 SWAA071787 1 20070410 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 S13L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 13L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007041700122 20070417 00122 NM 2007 4 17 SWAA071803 1 20070410 A 5311 6546552 FRAME BOEING 737 7375H4 138449D NM BS 827 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007041700130 20070417 00130 NM 2007 4 17 SWAA071792 1 20070410 A 5754 SKIN BOEING 737 7373H4 1384600 NM NR 5 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN PA852 27696 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 5 L/E SLAT DELAMINATED AT OUTBOARD UPPER END. REMOVED AND REPLACED NR 5 SLAT PER MM. 2 L 7 2 4F RT A16WE 2007041700136 20070417 00136 NM 2007 4 17 SWAA071808 1 20070410 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 520 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007041700155 20070417 00155 WP 2007 4 17 AALA20070568 1 20070328 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7536A 49990 LGA - EMERGENCY EXIT LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT AT RIGH T NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007041700165 20070417 00165 EA 2007 4 17 SWIA200718095 1 20070402 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 865AS 7507 MAIN CABIN DOOR EMERGENCY EXIT SIGN IS INOP. RELAMPED EMERGENCY EXIT SIGN. 2 L 7 2 4F RT A21EA 2007041700175 20070417 00175 EA 2007 4 17 TRAX200700446 1 20070401 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 744EV 10157 GALLEY AREA HAS SEVERAL INOP EMERGENCY BULBS. 2 L 7 2 4F RT A21EA 2007041700180 20070417 00180 NM 2007 4 17 07FDEA01481 1 20070412 A 5311 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 UPPER CARGO COMPARTMENT, FRAME STA 535 FOUND WITH SCRATCHES AT LONGERON 19 LT. [4-27-07] REPAIR CARRIED OUT AT UPPER CA RGO COMPARTMENT, FRAME STA 535 AT LONGERON 19 LT AS PER SRZ 53-503. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007041700188 20070417 00188 CE 2007 4 17 BSAASDR0706 1 20070403 A 3297 WIRE BEECH 1900 1900D 1154162 CE LT MLG WW CHAFED A BSAA O OTHER J WARNING INDICATION AP APPROACH 1 NM 05 139ZV UE139 WHEN THE GEAR WAS SELECTED DOWN, & THE GEAR DIDN'T EXTEND, CREW FOUND 2 AMP GEAR CONTROL CB TRIPPED. CREW RESET CB, & T RIED AGAIN, THE CB TRIPPED AGAIN. CREW THEN PUMPED GEAR DOWN USING MANUAL EXTENSION SYSTEM. CREW LANDED WITH NO FURTHE R INCIDENT. THE GEAR OPERATED NORMALLY IMMEDIATELY AFTER THIS INCIDENT WHEN TROUBLESHOOTING THE PROBLEM. THE AIRCRAFT RECEIVED AN EXTENSIVE INSPECTION OF ALL WIRING CONNECTED TO THE 2 AMP GEAR CONTROL CB. THREE CHAFED WIRES WERE FOUND UN DER THE LT WHEEL WELL GRAVEL GUARD. THE RUBBER CUSHION IN THE CLAMP FOR THE WIRES TO THE UPLOCK SWITCH HAD DETERIORATED , & THREE WIRES WERE CHAFED. THE WIRES WERE REPAIRED, AND CLAMP WAS REPLACED. THE RT WHEEL WELL GRAVEL GUARD WAS REMOVE 2 L 7 2 4T RT A24CE 2007041700192 20070417 00192 EU 2007 4 17 07FDEA01495 1 20070413 A 5312 BULKHEAD AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 SCRATCH IN PRESSURE BULKHEAD AT C54, TR 4 LT. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5315-101318 AND RAS/045121/010/200 6 ISSUE "A". 2 L 7 2 4F RT A35EU 2007041700200 20070417 00200 EA 2007 4 17 COMA0770022 1 20070404 A 2742 84897132 MOTOR CNDAIR CL600 CL6002C10 1390015 EA HORIZ STAB FAULTY A COMA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 371CA 6432 10082 FLIGHT 5280 - STAB CH2 STATUS MESSAGE DISPLAYED ON AND OFF CONTINUOUSLY DURING CLIMB, CRUISE, LANDING AND TAXI. TRIM IN MOTION ORAL ON CONTINUOUSLY. ELECTRICAL SMELL IN AFT CABIN. LANDED DEN WITHOUT INCIDENT. REPLACED NR 2 STAB ACTUATOR MOTOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007041700212 20070417 00212 NM 2007 4 17 KCSA071119 1 20070405 A 5313 FITTING BOEING 747 747236B 1384804 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STR 51R END FITTING BOLT HOLES ARE CORRODED FWD OF BS 2360. 2 L 7 4 4F A20WE 2007041700213 20070417 00213 NM 2007 4 17 KCSA071120 1 20070405 A 5313 FITTING BOEING 747 747236B 1384804 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STR 36R END FITTING BOLT HOLES ARE CORRODED FWD OF BS 2360. 2 L 7 4 4F A20WE 2007041700216 20070417 00216 NM 2007 4 17 KCSA071125 1 20070405 A 5313 FITTING BOEING 747 747236B 1384804 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STR 42L END FITTING BOLT HOLES ARE CORRODED FWD OF BS 2360. 2 L 7 4 4F A20WE 2007041700222 20070417 00222 NM 2007 4 17 KCSA071139 1 20070411 A 5313 STINGER BOEING 747 747236B 1384804 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STR 42L AT STA 735 HAS DAMAGE NEAR O/B LOWER RADIUS. 2 L 7 4 4F A20WE 2007041700233 20070417 00233 EU 2007 4 17 MAC030703 1 20070327 A 7722 ST315216 TRIM STICK AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE INTERMITTENT A MTNA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 33 809FX 217 124437 NR 1 ENGINE ITT FLUCTUATED DURING DEPARTURE/CLIMB. 2 H 7 2 4T 4 T RT A53EU E2ONE 2007041700238 20070417 00238 NM 2007 4 17 NOCA07507 1 20070328 A 7603 BACR13CG2A RELAY BOEING 767 767306 1385148 NM LT ENGINE FAILED A NOCA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 15 765NA 28098 LEFT ENGINE FAILS TO START. TROUBLESHOT PER FIM 76-11-00 FIG 108. REPLACED LEFT ENG FUEL/IGN CONTROL RELAY (K1251) PER WDM 76-11-11. OPERATED LEFT ENG PER MM 71-00-00-862-088-HO1, SEVERAL TIMES. ALL STARTS NORMAL. NO FAULTS NOTED. 2 L 7 2 4F RT A1NM 2007041700239 20070417 00239 NM 2007 4 17 NOCA07607 1 20070328 A 7410 BACR13CG2A RELAY BOEING 767 767306 1385148 NM GE CF6 CF680C2B7 NE LT ENGINE FAILED A NOCA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 765NA 28098 LEFT ENG FUEL VALVE EICAS/COCKPIT LIGHT IND AFTER PUTTING LEFT FUEL CONTROL SWITCH TO RUN. REPLACED LEFT ENG IGN CONT R ELAY(K1251). ALL OPS NORMAL. 2 L 7 2 4F 4 F RT A1NM E13NE 2007041700240 20070417 00240 NM 2007 4 17 NOCA07807 1 20070402 A 2611 32V92 PRESSURE SWITCH BOEING 757 75728A 1384976 NM CARGO BAY FAULTY A NOCA K NONE N FALSE WARNING NR NOT REPORTED 1 EA 15 755NA 30043 FWD DET FAN EICAS MSG. ACCOMPLISHED FIM TASK 26-16-00 FIG 105, FOUND FWD CARGO PRESS SWITCH AT FAULT. REMOVED AND REPL ACED PRESS SWITCH PER MM 26-16-03, ALL OPS CHECKS NORMAL. 2 L 7 2 4F RT A2NM 2007041700242 20070417 00242 NM 2007 4 17 SWAA071822 1 20070411 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007041700243 20070417 00243 NM 2007 4 17 SWAA071830 1 20070411 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007041700244 20070417 00244 NM 2007 4 17 SWAA071820 1 20070411 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED SERVICE CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT BROKEN AT ROW 11 ABC. REMOVED AND REPLACED LIGHT AS SY PER MM. 2 L 7 2 4F RT A16WE 2007041700245 20070417 00245 NM 2007 4 17 SWAA071827 1 20070411 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND STRINGER 8R CRACKED AT BS 482A. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007041700246 20070417 00246 NM 2007 4 17 SWAA071831 1 20070411 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND STRINGER 4R CRACKED AT BS 360. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007041700247 20070417 00247 2007 4 17 SWAA071825 4 20070411 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007041700249 20070417 00249 2007 4 17 2007UALA00974 4 20070330 A 2565 ANNUNCIATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 508UA 24744 DOOR 2L SLIDE ARMED LIGHT INOPERATIVE. [06-14-07] REPLACED L405 GIRT BAR ANNUNCIATOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041700250 20070417 00250 2007 4 17 2007UALA00975 4 20070330 A 2565 SPRING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE BROKEN A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 508UA 24744 DOOR 4R SLIDE SPRING FOR CLIPS BROKEN. [06-14-07] REPLACED SLIDE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041700251 20070417 00251 2007 4 17 2007UALA00976 4 20070331 A 2565 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR INOPERATIVE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 508UA 24744 DOOR R1 SLIDE ARMED LIGHT ABOVE DOOR INOPERATIVE. [06-14-07] REPLACED PROXIMITY SWITCH S10217. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041700254 20070417 00254 NM 2007 4 17 2007UALA00979 1 20070330 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 644UA 25094 LIGHT STRIP IN FRONT OF THE FWD CLOSET IS INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 2007041700255 20070417 00255 EU 2007 4 17 2007UALA00961 1 20070401 A 3350 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 481UA 1559 EMERGENCY LIGHT TEST FAILED, -EMER BATT PACK LEFT- DISPLAYED. DOOR 1L BATTERY PACK WILL NOT TEST. *S/D* ACCOMPLISHED RESET POWER ON ACFT. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041700256 20070417 00256 2007 4 17 2007UALA00962 4 20070330 A 2565 SLIDE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 912UA 25290 DOOR 1L SLIDE FELL PARTIALLY OUT OF COVER. [SUP 5-1-07] CAUSE IS UNKNOWN, REPLACED SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041700257 20070417 00257 2007 4 17 2007UALA00964 4 20070329 A 2565 5A29011 ASPIRATOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EVAC SLIDE LEAKING A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 665UA PF0167 29237 ASPIRATOR LEAKING. CAUSE UNKNOWN DUE TO INTERNAL LEAKING. REPLACED ASPIRATOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2007041700258 20070417 00258 NM 2007 4 17 2007UALA00965 1 20070331 A 3397 7956329 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY EXIT EEL LIGHT INOPERATIVE AT SEATS 50R & 43L. ALSO UPPER DECK JUST AFT OF ROW 17L. SECURED CONNECTORS IN TH REE POSITIONS. ALL OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041700259 20070417 00259 NM 2007 4 17 2007UALA00966 1 20070331 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 UPPER DECK EMERGENCY EXIT CEILING LIGHT INOPERATIVE AT AISLE ROWS 12, 18 AND AT DOOR 1R ENTRY. REPLACED LAMPS AT EACH P OSITION. ALL OPS CHECK NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041700262 20070417 00262 NM 2007 4 17 2007UALA00969 1 20070331 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY EXIT EEL LIGHT INOP AT LAV 112 RIGHT HAND FLOOR. REPLACED LAMP IN TWO POSITIONS. BOTH OPS CHECK NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041700264 20070417 00264 NM 2007 4 17 2007UALA00971 1 20070331 A 3397 59193 CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY EXIT EEL LIGHT INOP AT DOOR 1R JUST BELOW VIDEO CABINET. SPLICED EEL FEEDER. OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041700265 20070417 00265 NM 2007 4 17 2007UALA00972 1 20070331 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY EXIT EEL LIGHT INOP ACROSS DOOR 3L WALL EEL. REPLACED LIGHT ASSY. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041700266 20070417 00266 NM 2007 4 17 2007UALA00973 1 20070330 A 3397 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 585UA 26709 EMERGENCY LIGHTS INOP ROW 9 THRU ROW 13. FOUND POWER STRIP DISCONNECTED. RECONNECTED STRIP AND LIGHTS ILLUMINATE CORRE CTLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041700273 20070417 00273 NM 2007 4 17 WRLA2007059 1 20070413 A 5414 SKIN DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE NR 2 COWLING CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 274WA 48633 DURING 4C+12A CHECK, EGAT MECHANIC FOUND CRACK ON NR 2 ENGINE INLET COWL INNER SKIN AT 6 O'CLOCK POSITION 1EA, 7 O'CLOCK POSITION 4EA, 8 O'CLOCK POSITION 3EA, 10 O'CLOCK POSITION 1EA, 11 O'CLOCK POSITION 2EA AND 12 O'CLOCK POSITION 1EA. [S UP 05-02-07] REPAIRED NR 2 ENGINE INLET COWL LIP INNER SURFACE CRACK AREA PER EGAT ENGINEERING INSTRUCTION NR 2007P20A- 016 REV 00 & W2007A54B-207 REV.00 & HEAT TREATMENT 22/9-0 TO 22/9-T6 PER IE ATTACHMENT SHEET NR 0028588. 2 L 7 3 4F 4 F RT A22WE E24NE 2007041700274 20070417 00274 NM 2007 4 17 WRLA2007060 1 20070412 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 274WA 48633 DURING 4C+30/60M CHECK, MAIN DECK CARGO SEAT TRACK CORROSION AT Y:627, X:-28, Z:-18. [SUP 05-02-07] REPLACED MAIN DECK CARGO SEAT TRACK PER MD-11 SRM 53-70-00 VOL.1 REV 38 FIG 1. 2 L 7 3 4F 4 F RT A22WE E24NE 2007041700275 20070417 00275 NM 2007 4 17 WRLA2007061 1 20070412 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUSELAGE WORN A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 274WA 48633 DURING 4C+30/60M CHECK, MAIN DECK CARGO SEAT TRACK WORN AT Y:630, X:-8, Z:-18. [SUP 05-02-07] REPLACED MAIN DECK CARGO SEAT TRACK PER MD-11 SRM 53-70-00 VOL.1 REV 38 FIG.1. 2 L 7 3 4F 4 F RT A22WE E24NE 2007041700276 20070417 00276 NM 2007 4 17 WRLA2007062 1 20070412 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 274WA 48633 DURING 4C+30/60M CHECK, MAIN DECK CARGO SEAT TRACK CORROSION AT Y:735, X:-8, Z:-18. [SUP 05-02-07] REPLACED MAIN DECK CARGO SEAT TRACK PER MD-11 SRM 53-70-00 VOL.1 REV 38 FIG 1 2 L 7 3 4F 4 F RT A22WE E24NE 2007041700277 20070417 00277 NM 2007 4 17 WRLA2007058 1 20070309 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 274WA 48633 DURING 4C+30/60M CHECK, MAIN DECK CARGO SEAT TRACK CRACKED AT Y:635, X:47, Z:-18. [SUP 05-02-07] REPLACED MAIN DECK CAR GO SEAT TRACK PER MD-11 SRM 53-70-00 VOL.1 REV 38 FIG.1 2 L 7 3 4F 4 F RT A22WE E24NE 2007041700278 20070417 00278 NM 2007 4 17 WRLA2007056 1 20070309 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 274WA 48633 DURING 4C+30/60M CHECK, MAIN DECK CARGO SEAT TRACK CRACKED AT Y:635, X:8.5, Z:-18. [SUP 05-02-07] REPLACE MAIN DECK CG O SEAT TRACK PER MD-11 SRM 53-70-00 VOL.1 REV 38. 2 L 7 3 4F 4 F RT A22WE E24NE 2007041700297 20070417 00297 NM 2007 4 17 UPS07M49620 1 20070327 A 2550 ROLLER TRAY DOUG MD11 MD11F 3023600 NM CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C FWD CARGO - NEAR AFT BULKHEAD, CORROSION FOUND ON ROLLER TRAY END AS MARKED AT STA 6 - 73.5, BL 0. CO RROSION ON ROLLER TRAY END AT STA 6-73 BL 0, REMOVED AS PER SRM 51-21- 01 VOL II REV 38. MEASURED THK 0.090", MATL REMO VED 0.060", MATL REMAINED 0.030" FOUND OUT OF LIMIT PER SRM 53-00-01 FIG 1A VOL I REV 38. ROLLER TRAY REMOVED FROM STA 1129 TO STA 6-73 BL 0, REMOVED AS PER SRM 51- 31-01-VOL II REV 38. NEW ROLLER TRAY INSTALLED PER SRM 51-31-01 VOL II RE V 38. 2 L 7 3 4F RT A22WE 2007041700298 20070417 00298 NM 2007 4 17 UPS07M49621 1 20070326 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C AFT CABIN SEAT TRACK SUPPORT AT STA 1996, LONGERON 27L, ADJACENT LBL 1 07.25 SEAT TRACK LOWER SURFACE FOUND CORRODED. CORROSION ON STIFFENER REMOVED PER SRM 51-21-01 VOL II REV 38. ORI THK 0.071", MATL REMOVED 0.040", MA TL REMAINED 0.031" FOUND OUT OF LIMIT PER SRM 53-00-01 FIG 3 VOL I REV 38. STIFFENER FAB USING MATL 7075-0-0 .071" AS P ER DWG ACA7145. NEW STIFFENER INSTALLED AS PER SRM 51-31-01 VOL II REV 38. 2 L 7 3 4F RT A22WE 2007041700299 20070417 00299 NM 2007 4 17 UPS07M49622 1 20070315 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C AFT CABIN - SEAT TRACK CORROSION ON FLANGES & CROWN FROM STA 1331 - ST A 1361 RIGHT RBL 75 AS MARKED. CORROSION ON SEAT TRACK FLANGES & CROWN REMOVED PER SRM 51-21-01 VOL II REV 38. ORI THK 0.080" (FLANGE AREA) STA 1351 MATL REMOVED 0.020", MATL REMAINED 0.060 FOUND OUT OF LIMIT PER SRM 53-70-00 FIG 3 VOL I REV 38. SEAT TRACK AT STA 12 6 9-1391 RBL 75 REMOVED PER SRM 51-31-01 VII REV 38. NEW SEAT TRACK RWK PER SRM 53-70-00 FIG 1 VI R38. NEW SEAT TRACK & SPLICE INSTALLED PER SRM 51-31-01 VII REV 38. 2 L 7 3 4F RT A22WE 2007041700300 20070417 00300 NM 2007 4 17 UPS07M49624 1 20070415 A 3397 WIRE DOUG MD11 MD11F 3023600 NM EMERGENCY LIGHTS DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 285UP 48457 EMERGENCY LIGHTING SYS 1 FAILED. DEFERRED PER MEL M348451. [SUP 4-20-07] REPAIRED WIRE TO CONNECTOR P1-328 BATTERY LO WER CHANGE. EMERGENCY EXIT LIGHTS TEST PASS. DEFERRAL CLOSED. 2 L 7 3 4F RT A22WE 2007041700301 20070417 00301 WP 2007 4 17 UPS07849611 1 20070331 A 5553 ATTACH ANGLE DOUG DC8 DC873F 302199F WP VERTICAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 ATTACH ANGLE FOR VERT FIN L/E TO FUSELAGE BENT AND CRACKED RIGHT SIDE FS 1690. REMOVED ATTACH ANGLE FOR VERT FIN TO FUSELAGE AT STA 1690 IAW SRM 51-3-0. FABRICATED AND INSTALLED ANGLE DOUBLER AND FILLER AT FS 1690 VERT FIN L/E TO FUSELAGE IAW SRM 53-02-05 FIG 16A. 2 L 7 4 4F RT 4A25 2007041600067 20070416 00067 NM 2007 4 16 ZZDA070405146 1 20070405 A 3350 LIGHT BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 946AT 55009 EMERGENCY EXIT LIGHTING SYSTEM LEFT ON AFTER TOWING SYSTEM FULLY DISCHARGED. C/W AMM 33-51-00, OPS CHECK GOOD. 2 L 7 2 4F TR A6WE 2007041600071 20070416 00071 NM 2007 4 16 AMTA200700176 1 20070328 A 2840 233N3206300 CONTROL PANEL BOEING 757 75723N 1384973 NM RROYCE RB211 RB211* 54555 NE FUEL MANAGE MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 519AT 27975 RT AFT FUEL BOOST PUMP LOW PRESS LIGHT INOPERATIVE, RELAMP NO HELP. REMOVED AND REPLACED FUEL MANAGEMENT CONTROL PANEL IAW AMM 28-22-14-4, TEST OK. (K) 2 L 7 2 4F 4 F RT A2NM A12EU 2007041600076 20070416 00076 NM 2007 4 16 2007UALA01027 1 20070405 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY EEL LIGHT INOPERATIVE AT SEAT 5A AFT. *S/D* 4-17-07 RELAMPED. OP CHECKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041600085 20070416 00085 NM 2007 4 16 F3LA200700049 1 20070330 A 5320 SILL AIRBUS A319 A319111 3930336 NM FUSLEAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED NUT CLIP AREA CORRODED ON FLOORBEAM -Y1732 AT FR 66, FWD OF R-2 DOOR FRAME. REM OVED AND REPLACED R-2 DOOR SILL IAW A319 SRM 51-42-11; 51-42-11, FIG 8; 51-42-11, PARA. 6; 51-21-11; 51-75-12; 51-12-11; 51-45-11, FIG 8; AND 51-42-11, 7B. 2 L 7 2 4F RT A28NM 2007041600091 20070416 00091 NM 2007 4 16 MZZA0700006 1 20070328 A 3233 273A12011 ACTUATOR BOEING 737 737824 13844BZ NM NLG INOPERATIVE A MZZA O OTHER J WARNING INDICATION CL CLIMB 1 WP 13 35236 25761 28801 THE NOSE GEAR FAILED TO RETRACT AFTER TAKEOFF FROM SAIPAN. THE GREEN DOWN AND LOCKED LIGHT REMAINED ILLUMINATED. THE N LG LOCK ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-33-01 AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2007041600100 20070416 00100 EU 2007 4 16 SIMA200709903 1 20070406 A 3260 MS213212 UPLOCK SWITCH SAAB SF340 340B 7860101 EU ZONE 700 FAILED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 317AE 23104 340B317 LANDING GEAR HANDLE SELECTED TO UP POSITION, 30 TO 45 SECONDS TO COMPLETE RETRACTION CYCLE AND LANDING GEAR DISAGREE LIG HT TO GO OUT. REMOVED AND REPLACED UPLOCK SWITCH IAW SAAB AMM, OPERATIONAL CHECK GOOD. PERFORMED FUNCTIONAL CHECK FLIG HT WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007041600118 20070416 00118 EU 2007 4 16 07FDEA01402 1 20070410 A 5414 PANEL AIRBUS 310 A310324 3930206 EU ZONE 400 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CRACK FOUND ON PYLON NR 1 LATERAL PANEL AT RIB 8 LT/RT. REPAIR WAS PERFORMED IAW SRM 54-51-31/FIG 201, APPROVED BY EA 6 -5450-101299. 2 L 7 2 4F RT A35EU 2007041600119 20070416 00119 EU 2007 4 16 07FDEA01403 1 20070410 A 5414 PANEL AIRBUS 310 A310324 3930206 EU ZONE 400 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 CRACKS ON PYLON NR 2 LATERAL PANEL AT RIB 8 RT. REPAIR WAS PERFORMED IAW SRM 54-51-31/FIG 201, APPROVED BY EA 6-5450-10 1300. 2 L 7 2 4F RT A35EU 2007041700011 20070417 00011 SO 2007 4 17 RAIA00704025 1 20070409 A 3397 TERMINAL EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DAMAGED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 814HK 145046 POST FLT 5536 - STL - EMERGENCY LIGHT STRIP INOP AT ROWS 5-7. MAINTENANCE RESECURED TERMINAL TO FLOOR STRIP LIGHTING, O PS OK. 2 L 7 2 4T RT T00011AT 2007041700014 20070417 00014 SO 2007 4 17 RAIA00704028 1 20070410 A 2150 A/C PACK EMB 145 EMB145 3260210 SO MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 804HK 145082 FLT 3551 - PIT - PACK 1 & PACK 2 OVERLOAD IN FLIGHT, COULD NOT RESET. MAINTENANCE OPS CHECK PACK 1 SYSTEM OPS CHECK GOO D. DEFERRED PACK 2 SYSTEM PER MEL. 2 L 7 2 4F RT T00011AT 2007041700015 20070417 00015 SO 2007 4 17 RAIA00704026 1 20070409 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 816HK 7689 111 145055 PRE FLT 5545 - STL - EMERGENCY LIGHTS AISLE FLOOD LIGHT AND FWD CEILING EXIT LOCATOR ARE INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY IN FWD CLOSET, OPS CHECK OK. 2 L 7 2 4T RT T00011AT 2007041700016 20070417 00016 SO 2007 4 17 RAIA00704036 1 20070412 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BURNED OUT A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 816HK 145055 PRE FLT 5497 - STL - EMERGENCY LIGHT AISLE FLOOD LIGHT IS INOP. MAINTENANCE RELAMPED, EMERGENCY LIGHT OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007041700049 20070417 00049 SO 2007 4 17 RAIA00703079 1 20070331 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BURNED OUT A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 832HK 145771 PRE FLT 7911 - MSN - EMERGENCY LIGHT ON PLUG DOOR HINGE IS OUT. MAINTENANCE REPLACED BULB, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007041700055 20070417 00055 CE 2007 4 17 DXTA200702102 1 20070412 A 3240 BRAKE ASSY CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG DAMAGED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 982QS 7500182 BRAKES ARE HARD TO PUSH AND MAKE EXCESSIVE NOISE. [SUP 4-19-07] PERFORMED TESTS AS IAW CE750 MM 32-42-00, NO FAULTS WE RE FOUND IN EITHER POWER BRAKE FUNCTIONAL OR ANTI-SKID FUNCTIONAL TESTS. REMOVED ALL 4 MLG TIRES AND CLEANED OUT THE ACC UMULATIONS OF BRAKE DUST IN ALL FOUR BRAKE ASSY'S. REINSTALLED ALL FOUND MLG TIRE ASSY'S IAW CE750 MM 32-41-02 AND BRAKE S OPS CHECKED GOOD IAW 32--42-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007041700058 20070417 00058 CE 2007 4 17 DXTA200702105 1 20070412 A 3260 INDICATION SYS CESSNA 560 560XL 2076702 CE MLG MALFUNCTIONED E DXTA B EMER. DESCENT P NO WARNING INDICATION LD LANDING 1 GL 07 634QS 5605558 NO (GREEN) LIGHT ON RT MAIN LANDING GEAR UPON EXTENSION. EMERGENCY PROCEDURES FOLLOWED AND BOTTLE WAS BLOWN, STILL NO GR EEN LIGHT. 2 L 7 2 4F RT A22CE 2007041700096 20070417 00096 SO 2007 4 17 RAIA00704012 1 20070404 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS MALFUNCTIONED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 821HK 145068 PRE FLT 5574 - PHL - EMERGENCY LIGHTS COCKPIT STEP EXIT IDENTIFIER AND FWD CEILING EXIT LOCATOR INOP. MAINTENANCE RESET CONNECTOR ON EMERGENCY LIGHT BATTERY PACK, SYSTEM CHECK NORMAL. 2 L 7 2 4F RT T00011AT 2007041700101 20070417 00101 NM 2007 4 17 SWAA071799 1 20070410 A 5311 6546525 FRAME BOEING 737 7375H4 138449D NM BS 380 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007041700110 20070417 00110 NM 2007 4 17 SWAA071818 1 20070411 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 502D S12R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 502D, STR 12R. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007041700123 20070417 00123 NM 2007 4 17 SWAA071804 1 20070410 A 5311 6546555 FRAME BOEING 737 7375H4 138449D NM BS 867 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007041700127 20070417 00127 NM 2007 4 17 SWAA071786 1 20070410 A 5551 6551524 FITTING BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND RT AND LT HORIZONTAL STAB FITTING CLEVIS LUG FACES CORRODED. REPAIRED STAB FITTING PE R SRM. 2 L 7 2 4F RT A16WE 2007041700128 20070417 00128 NM 2007 4 17 SWAA071775 1 20070409 A 3350 6556633 SIGN BOEING 737 7373H4 1384600 NM EMERGENCY EXIT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 RIGHT OVERWING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007041700138 20070417 00138 NM 2007 4 17 SWAA071812 1 20070410 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 747 S19L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 19L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007041700151 20070417 00151 NM 2007 4 17 AALA20070585 1 20070331 A 3350 SIGN BOEING 737 737823 13844BZ NM R1 DOOR BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 938AN 29533 MIA - EMERGENCY EXIT LIGHT SIGN AT RIGHT NUMBER ONE DOOR BROKEN. SECURED SIGN FOR EMERGENCY EXIT LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007041700152 20070417 00152 WP 2007 4 17 AALA20070578 1 20070330 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9615W 53562 LGA - EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007041700153 20070417 00153 WP 2007 4 17 AALA20070579 1 20070330 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 596AA 53286 LGA - EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007041700162 20070417 00162 EA 2007 4 17 SWIA200718092 1 20070407 A 5610 NP13932112 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 340CA 10062 RIGHT FRONT WINDSHIELD CRACKED IN FLIGHT. REPLACED RIGHT WINDSHIELD IAW MM 56-11-01. 2 L 7 2 4F RT A21EA 2007041700169 20070417 00169 NM 2007 4 17 07FDEA01373 1 20070406 A 5313 AEA75451 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 CORROSION WAS FOUND ON LONGERON 28 BETWEEN STA 1273-1289 AFTER REMOVAL OF SCUFF PLATE ON L3 DOOR. [SUP 4-20-07] REMOVE D AND REPLACED AS PER SRM 51-33-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007041700187 20070417 00187 EU 2007 4 17 07FDEA01491 1 20070413 A 5311 A53879305200 FRAME AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 FOUND CORROSION AT MILLED FRAME C49, P14-P15 LT. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5315-101284 AND RAS/DATLS/00032 002006 ISSUE "B". 2 L 7 2 4F RT A35EU 2007041700199 20070417 00199 NE 2007 4 17 COMA0760299 2 20070404 A 7250 CF343A1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LEFT DAMAGED A COMA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SO 01 810CA 31221 7370 807042 FLIGHT 5226 - PRONOUNCED VIBE DURING TAKEOFF. ABORTED TAKEOFF. MDC SHOWS VIBE AND ITT EXCEEDANCES. FAN CANNOT BE TURN ED BY HAND. REPLACED LEFT ENGINE ASSEMBLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2007041700202 20070417 00202 NM 2007 4 17 FDKA200703134 1 20070327 A 3350 1317 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 802LR 205 FDM 6112 JFK-BWI (0951 PHX LCL). MID CABIN EMERGENCY FLOOD LIGHT INOP. MX RELAMPED. 2 H 7 2 4T RT A13NM 2007041700203 20070417 00203 SO 2007 4 17 FDKA200703135 1 20070327 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 847MJ 145517 FDM 6173 FLL-TLH (0645 PHX LCL). BOTH EMERGENCY DOOR LIGHTS INOP. MX RE-SECURED CONNECTOR ON NR 3 POWER SUPPLY. 2 L 7 2 4T RT T00011AT 2007041700209 20070417 00209 NM 2007 4 17 KCSA071116 1 20070405 A 5313 FITTING BOEING 747 747236B 1384804 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STR 36L END FITTING BOLT HOLES ARE CORRODED FWD OF BS 2360. 2 L 7 4 4F A20WE 2007041700232 20070417 00232 NM 2007 4 17 07FDEA01381 1 20070409 A 5713 ARB75101 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 CRACK FOUND AT STRINGER END 10L (XORS 760), APPROX 9" LENGTH ON LT WING TANK DURING HFEC INSPECTION. LT WING TANK STRIN GER END 10L (XORS 760) REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG.10 VOL I. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER F EDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007041700235 20070417 00235 WP 2007 4 17 ARWA20070303 1 20070315 A 5753 SUPPORT DOUG DC10 DC1030 3023501 WP FLAP WELL CHAFED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 524MD 46999 DURING "A" CHECK INSPECTION, THE FOLLOWING WAS FOUND, LT INBD FLAP "A" SUPPORT IN FLAP WELL CHAFED. BLEND-OUT AREA FOUN D WITHIN LIMITS PER BOEING MESSAGE 1-301363052-8. 2 L 7 3 4F A22WE 2007041700248 20070417 00248 NM 2007 4 17 SWAA071821 1 20070411 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED SPV CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 10 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007041700260 20070417 00260 NM 2007 4 17 2007UALA00967 1 20070331 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EMERGENCY EXIT LIGHT INOP AT DOOR 5 RIGHT FWD SILL LIGHT. REPLACED LAMP. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041700302 20070417 00302 WP 2007 4 17 UPS07849615 1 20070322 A 5330 564932959 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:C3 EXTERIOR FUSELAGE SKIN CRACKED AT L30L STA 1690. REPAIRED FUSELAGE SKIN AT STA 1690 L30R - L28L IAW SAA EA 008-5330- 01-0750, UPS EO DC8-5330-26567-A, FAA FORM 8100-9, AND AMOC APPROVAL FOR AD 2007-02-02. 2 L 7 4 4F RT 4A25 2007041700303 20070417 00303 2007 4 17 UPS07849616 4 20070413 A 2565 SLIDE DOUG DC8 DC871F 302199D WP COCKPIT OUT OF POSITION A IPXA K NONE O OTHER NR NOT REPORTED 1 SO 01 718UP 46018 INSPECTION TYPE:N/A DOOR SLIDE FELL OUT OF CONTAINER WHEN DOOR WAS OPENED AT SDF. GIRT BAR WAS CORRECTLY STOWED. REINS TALLED SLIDE PER AMM 25-60-01-2. 2 L 7 4 4F RT 4A25 2007041700304 20070417 00304 NM 2007 4 17 UPS07M49610 1 20070318 A 5754 SKIN DOUG MD11 MD11F 3023600 NM L/E SLAT DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C LEFT WING NR 5 SLAT FRONT FACE FOUND WITH 1 EA DENT MARK AS MARKED. DENT AREA MEASURED EXCEED LIMIT P ER SRM 57-10-00 FIG 16 VI R38 DEPTH 0.080" LENGTH 2" WIDTH 1". DENTED AREA CUT OUT PER SRM 57-10-00 FIG 5 VI R38. HFEC C/O PER DACNDTSPMR13PT06.10.01.001 NO CRACK EVIDENT. REPAIR PARTS FAB PER SRM 57-10-00 FIG 5 VI R38. HOLES PICKUP PER SRM 57-10-00 FIG 5 VII R38. ALODINE & PRIMER PER SRM 51-21-01 VII R38. INSTALLED PER SRM 57-10-00 FIG 5 VI R38. 2 L 7 3 4F RT A22WE 2007041700305 20070417 00305 NM 2007 4 17 UPS07M49613 1 20070305 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:CK-C FWD CARGO BILGE AREA STA 6-06 LONGERON L41 FOUND WITH CORROSION AS MARKED. FWD CARGO BILGE AREA ST A 6-06 LONGERON L41 DAMAGED AREA REPAIRED AS PER SRM 53-10-00 FIG 2 VOL I REV 38. 2 L 7 3 4F RT A22WE 2007041700306 20070417 00306 NM 2007 4 17 UPS07M49614 1 20070319 A 5313 LONGERONR49 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:CK-C FWD CARGO STA 6-70 LONGERON R49 FOUND WITH CORROSION DURING CARRY OUT WORK ON ADJACENT AREA. CORRO DED LONGERON R49 STA 6-70 REPAIRED AS PER SRM 53-10-00 FIG 2 VOL I REV 38. 2 L 7 3 4F RT A22WE 2007041700307 20070417 00307 EU 2007 4 17 UPS07149608 1 20070410 A 5610 HANDLE AIRBUS A300 A300F4622R 3930360 EU COCKPIT LACK OF LUBE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 168UP 0863 INSPECTION TYPE:N/A CAPTAIN'S COCKPIT SIDE WINDOW LATCH INDICATION SHOWS UNLATCHED HANDLE. MUST BE PULLED UP TO RETRACT INDICATION FLAG. LUBRICATED CAPTAIN'S SLIDING WINDOW HANDLE & LATCH MECHANISM. OPERATED WINDOW SEVERAL TIMES, LATCH I NDICATOR OPERATED NORMAL. OK FOR CONTINUED SERVICE. 2 L 7 2 4F RT A35EU 2007041700308 20070417 00308 NM 2007 4 17 UPS07549609 1 20070410 A 5350 RADOME BOEING 757 75724APF 1384969 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 471UP 28842 INSPECTION TYPE:N/A RADOME HAS SEVERAL NICKS & GOUGES, POSSIBLE DELAMINATION. INSPECTED PER SRM 53-10-72-1A. DAMAGE IS OUT OF LIMITS. RADOME UNLOCKED. UPON FURTHER INSPECTION DAMAGE WAS TO THE SURFACE COATING AND BOOT. REPAIRED BOOT AN D APPLIED SURFACE COAT PER EO B757-5350-23867-A. RESECURED RADOME. 2 L 7 2 4F RT A2NM 2007041700309 20070417 00309 WP 2007 4 17 UPS07849607 1 20070408 A 2120 UNKNOWN DOUG DC8 DC871F 302199D WP COCKPIT ODOR A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 718UP 46018 INSPECTION TYPE:N/A THERE IS AN EXTREMELY FOUL -DIRTY SOCK- ODOR IN THE COCKPIT WITH PACKS ON. ACCOMPLISHED ADJ/TEST OF BOTH PACK SYSTEMS DURING ENGINE RUN. REF MM 21-50-00-5. ALL SYSTEMS CHECK NORMAL. NO ODORS NOTED. NO HISTORY. 2 L 7 4 4F RT 4A25 2007041700310 20070417 00310 EU 2007 4 17 TRAX200700480 1 20070407 A 2560 BATTERY AEROSP ATR72 ATR72 EU FLASHLIGHT DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 641AS 387 COPILOT FLASHLIGHT INOP. REMOVED AND REPLACED BATTERIES IN COPILOT FLASHLIGHT AS REQUIRED. OPS CHECK GOOD AT THIS TIME . 2 H 7 2 4T RT 2007041700311 20070417 00311 EA 2007 4 17 TRAX200700477 1 20070404 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 741EV 10155 LEFT 280 WEB CORRODED. PREVIOUSLY BLENDED ON. REMOVED AND REPLACED LEFT 280 WEB IAW CRJ 700 SRM 51-42-00 AND REO 670-5 3-11-052. SUPPLEMENTAL - SDR CLOSED 04/13/07. 2 L 7 2 4F RT A21EA 2007041700312 20070417 00312 EA 2007 4 17 TRAX200700478 1 20070404 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 741EV 10155 RIGHT 280 WEB CORRODED. PREVIOUSLY BLENDED ON. REMOVED AND REPLACED RIGHT 280 WEB IAW CRJ 700 SRM 51-24-21 AND REO670- 53-11-052. SUPPLEMENTAL - SDR CLOSED 04/13/07. 2 L 7 2 4F RT A21EA 2007041700313 20070417 00313 EA 2007 4 17 TRAX200700479 1 20070407 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 901EV 7616 LEFT FUSELAGE FWD EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007041700314 20070417 00314 EA 2007 4 17 TRAX200700483 1 20070407 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 STA 280 BULKHEAD WEB CRACKED AT LBL 9. 2 L 7 2 4F RT A21EA 2007041700315 20070417 00315 EA 2007 4 17 TRAX200700485 1 20070407 A 5340 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 STA 280 RBL 9 AND LBL 9 INBOARD CLIPS CRACKED. 2 L 7 2 4F RT A21EA 2007041700316 20070417 00316 EA 2007 4 17 TRAX200700486 1 20070407 A 2560 BATTERY CNDAIR CL600 CL6002B19 1900309 EA FLASHLIGHT DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 928EV 8006 F/O FLASHLIGHT BATTERIES INOP. 2 L 7 2 4F RT A21EA 2007041700317 20070417 00317 EA 2007 4 17 TRAX200700487 1 20070407 A 2560 BATTERY CNDAIR CL600 CL6002B19 1900309 EA FLASHLIGHT DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 873AS 7549 F/A FLASHLIGHT BATTERIES DEAD. 2 L 7 2 4F RT A21EA 2007041700318 20070417 00318 EA 2007 4 17 TRAX200700488 1 20070407 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 867AS 7463 CAPT FWD WINDSHIELD CRACKED AND ARCHING DURING DESCENT AND SHATTERED BEFORE LANDING. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007041700319 20070417 00319 EA 2007 4 17 TRAX200700489 1 20070407 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 755EV 10185 CAPT'S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007041700320 20070417 00320 EA 2007 4 17 TRAX200700490 1 20070407 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 838AS 7276 FLAPS FAIL MESSAGE ON APPROACH TO CVG. FLAPS FAILED AT 0'. BRAKE TEMPS MAXED OUT AT 4. EMERGENCY DECLARED. FLT 4863 CX AND ON 04/08/07 FLT 4421 CX. 2 L 7 2 4F RT A21EA 2007041700321 20070417 00321 EA 2007 4 17 TRAX200700497 1 20070407 A 5313 STRINGER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 FLOOR SUPPORT STRINGER AT PAX DOOR SILL CORRODED AND MISSING NUT PLATES (MARKED). BLENDED AND REMOVED STRINGER AND AFT CUP BOTH FOUND TO BE OUT OF LIMITS PER CRJ 200 SRM 53-00-00. DRILLED UP NEW PAX DOOR SILL REF CRJ-200 SRM 51-42-21, AND CRJ-200 SRM 51-42-06. ACCOMPLISHED NUTPLATE MOD AND STARTED INSTALLING SILL ON A/C PER REO 601R-52-11-577, CRJ200 SR M 51-42-21, AND 51-42-06. INSTALLED UPPER ANGLES ON ASD SILL PLATE IAW CRJ 200 SRM 51-42-06. INSTALLED DOOR PROX SWIT CH AND OPS CK GOOD IAW CRJ 200 AMM 52-70-04. 2 L 7 2 4F RT A21EA 2007041700322 20070417 00322 EA 2007 4 17 TRAX200700499 1 20070407 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 STA 349 TRANSVERSE BEAM RT SIDE CORRODED AT RBL 36 (MARKED). REMOVED CORROSION IAW CRJ200 SRM 51-21-06. 2 L 7 2 4F RT A21EA 2007041700323 20070417 00323 EA 2007 4 17 TRAX200700501 1 20070409 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 829AS 7232 F/A FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007041700324 20070417 00324 EA 2007 4 17 TRAX200700502 1 20070409 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 835AS 7258 PAX DOOR AFT ANCHOR FITTING CRACKED. [SUP 05-09-07] INSTALLED SERVICEABLE BASE PLATE P/N 600-38061-6 1EA AND SERVICEAB LE ANCHOR FITTING P/N 601R38074-51SB01 2 L 7 2 4F RT A21EA 2007041700325 20070417 00325 NM 2007 4 17 ARWA20070307 1 20070323 A 7897 CONNECTOR DOUG DC10 DC1040F 3023507 NM THRUST REVERSER LOOSE A ARWA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 140WE 46920 ON ROTATION, NR 1 ENGINE REVERSER UNLOCK LIGHT CAME ON AND REMAINED ON; SHUT ENGINE DOWN AND RETURNED TO MIAMI. PERFORM ED ELECTRICAL SYSTEM CHECK AND FOUND LOOSE CONNECTOR AT PRESSURE REG. S/O VALVE FROM PDM. TIGHTENED AND SECURED AS REQ UIRED. NEEDS SYSTEM OPERATIONAL CHECK; REMOVED AND REPLACED RT PRIMARY CABLE RIGGED AS PER M/M 78-31-16. OPERATIONAL C HECK OK. 2 L 7 3 4F RT A22WE 2007041700329 20070417 00329 EA 2007 4 17 TRAX200700506 1 20070409 A 2810 FILLERCAP CNDAIR CL600 CL6002B19 1900309 EA UNSECURE A ASOA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 878AS 7590 ON DEPARTURE F/A AND PAX REPORT LOUD NOISE COMING FROM OUTSIDE OF A/C. AIR-RETURN. AFTER PARKING FOUND FUEL CAP HANGIN G. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007041700330 20070417 00330 EA 2007 4 17 TRAX200700507 1 20070410 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 835AS 7258 PAX DOOR CRACK AT FS 320.010 ABOVE DATUM 1. [SUP 05-09-07] REPAIRED PAX DOOR FWD FRAME AT FS 320.010 IAW ASA EO REO 60 1R-52-11-402. 2 L 7 2 4F RT A21EA 2007041700331 20070417 00331 EA 2007 4 17 TRAX200700508 1 20070410 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 835AS 7258 PAX DOOR CRACK AT FS 338.00 ABOVE DATUM 1. [SUP 4-24-07] COMPLIED WITH REPAIR TO PAX DOOR AFT FRAME MEMBER AT FS 338.0 0 IAW ASA REO 601R-52-11-402. 2 L 7 2 4F RT A21EA 2007041700332 20070417 00332 EA 2007 4 17 TRAX200700510 1 20070410 A 5260 STEP CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 724EV 10138 ASD BOTTOM STEP CRACKED. 2 L 7 2 4F RT A21EA 2007041700333 20070417 00333 NE 2007 4 17 TRAX200700511 2 20070410 A 7261 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENGINE LOW A ASOA K NONE J WARNING INDICATION DE DESCENT 1 SO 27 680BR 7679 LEFT ENGINE SHUTDOWN, LOW OIL. EMERGENCY DECLARED. FLTS 4449, 4578 CX. 2 L 7 2 4F 4 F RT A21EA E15NE 2007041800002 20070418 00002 EU 2007 4 18 07FDEA01433 1 20070411 A 5350 FAIRING AIRBUS 310 A310 EU WING TO FUSE CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 801FD 539 FAIRING PANEL TO PYLON COWL OF RT CORE WITH 2 CRACKS REPAIRED THE CRACKS IAW SRM 54-56-10 CONFIG. 2 FIG 201. REPAIR EVA LUATED PER GMM 6-2-100 AND CLASSIFIED MINOR. 2 L 7 2 4F RT A35EU 2007041800003 20070418 00003 EU 2007 4 18 07FDEA01442 1 20070411 A 5350 FAIRING AIRBUS 310 A310 EU NR 1 PYLON CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 801FD 539 CRACK FOUND ON NR 1 PYLON LOWER FAIRING. REPAIR ON GOING AS SRM REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINO R. 2 L 7 2 4F RT A35EU 2007041800004 20070418 00004 EU 2007 4 18 07FDEA01443 1 20070411 A 5414 PANEL AIRBUS 310 A310 EU NR 1 PYLON CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 801FD 539 (N0535) CRACK FOUND ON NR 1 PYLON AFT FAIRING. REPAIR ON GOING AS SRM. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIE D AS MINOR. FAIRING TO PYLON COWL OF RT CORE W/ TWO CRACKS REPAIRED IAW SRM 54-56-10 CONFIG 2 FIG 201. 2 L 7 2 4F RT A35EU 2007041800005 20070418 00005 EU 2007 4 18 07FDEA01445 1 20070411 A 5330 SKIN AIRBUS 310 A310 EU FUSLEAGE DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 801FD 539 FUSELAGE LOWER FWD LOBE, REPAIR AT LT SIDE OF FUSELAGE BETWEEN FRAME 25 & 26/32 BETWEEN STR. 42 & 43 REPAIRED PER SRM 5 3-10-12 FIG. 229 (SHEET 1) PG. 406 TO 410 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS " MAJOR " 2 L 7 2 4F RT A35EU 2007041900001 20070419 00001 NM 2007 4 19 07FDEA01483 1 20070412 A 2130 32167441 CONTROL VALVE BOEING 727 727200 138407E NM RT PACK FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 280FE 22347 S/O REPERTED HEARING A SLIGHT POP PASSING 2000FT AFTER RIGHT PACK WAS TURNED ON.NORMAL INDICATION RIGHT PACK MATCHED L EFT PACK TEMP BUT AIR MIX VALVE STAYED COLD ON RIGHT PACK.CABIN STARTED A HIGHER THAN NORMAL CLIMB 71500 FT/MIN IN MAN PRESSURIZATION WITH OUTFLOW CLOSED CABIN STILL CLIMBED AT 1500 FT/MIN TRIED TO PRESSURIZE ACFT FOUND NR 2 PACK IS NOT PUTTING OUT ANY AIR OPENED SEVERAL NR 2 PACK ACCESS PANELS VERIFIED INOP RT FWD PACK VALVE. R & R SAME IAW 727-20 0 AMM 21-55-071-4. OPS CHECK NORMAL PERFORMED EXCESSIVE CABIN PRESSURE LEAK TEST IAW 727 -200 JRH. WITHIN LIMITS. OK TO CONTINUE. CHANGED LT FLOW CONTROL VALVE PRECAUTIONARY IAW 727-200AMM 36-12-061-4. OPS CHECK NORMAL. OK TO CONTINUE 2 L 7 3 4F RT A3WE 2007041900019 20070419 00019 NM 2007 4 19 2007UALA01052 1 20070405 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 300-303 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 FWD ENTRY DOOR CUTOUT STR 16L STA 294.5 CRACKED IN FWD CORNER, ALSO CRACKED INTERCOSTAL SUPPORT ANGLE STA 300-303 JUST A BOVE STR 10 FWD OF L1 DOOR, ALSO FWD ENTRY DOOR CUT OUT STR 11L STA 294.5 WEB IS CRACKED IN FWD CORNER, AND FWD ENTRY DO OR CUT-OUT STR 11L STA 360 LWR CLIP CRACKED IN CORNER. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR: REPAIR ACCOMPLISHED IAW E A I070215 AND I070216 AND UA-EVA-70168. 2 L 7 2 4F 4 F RT A16WE E2GL 2007041900020 20070419 00020 NM 2007 4 19 2007UALA01056 1 20070405 A 5210 LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DISCONNECTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 FOUND DOOR 2L EMERGENCY POWER RESERVIOR PRESSURE LINE DISCONNECTED. [06-14-07] SECURED PRESSURE LINE TO ASSIST RES ERVIOR ON DOOR 2L 2 L 7 2 4F 4 F RT A2NM E17NE 2007041900022 20070419 00022 NM 2007 4 19 2007UALA01058 1 20070406 A 2400 UNKNOWN BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE UNKNOWN A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 673UA 29241 RTFL UNDER AMBER ALERT DUE TO MULTIPLE ELECTRICAL FAULT MESSAGES. [SUP 05-08-07] REPLACED LEFT TRANSFORMER RECTIFIER U NIT PER MM24-32-01-401. TEST OK. DC-V 28 PLUS-MINUS 4. A/C READY FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007041900023 20070419 00023 NE 2007 4 19 2007UALA01059 2 20070407 A 7210 BEARING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GEARBOX FAILED A UALA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 WP 29 584UA 26706 726646 FLIGHT LANDED UNDER AMBER ALERT DUE TO ENGINE SHUT-DOWN ON FINAL. [SUP 05-24-07] THIS OCCURRENCE WAS DUE TO ANGLE GEARB OX BEARING FAILURE CAUSED BY EXCESSIVE VIBRATORY STRESS. THIS IS BELIEVED TO HAVE BEEN THE RESULT OF AN IMPROPER BALANC ING OF THE LOWER TOWER SHAFT WHICH COULD HAVE OCCURRED DURING INITIAL STAGE OF MANUFACTURE AT THE OEM. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041900024 20070419 00024 EU 2007 4 19 2007UALA01060 1 20070406 A 5311 FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 432UA 587 FRAME 30 HAS 7 EA FRAME CLEATS WITH CORROSION BETWEEN STR 40R AND STR 41L. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLAC ED CLEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900025 20070419 00025 NE 2007 4 19 2007UALA01061 2 20070406 A 7261 CARBON SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE LEAKING A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 598UA 28751 727199 NR 1 ENGINE HIGH OIL CONSUMPTION EXCEEDS LIMIT. [SUP 06-06-07] DEOILER CARBON SEAL AND OTHER SEAL RINGS REPLACED TO C ORRECT OIL CONSUMPTION. DEOILER CARBON SEAL P/N 7A0449; SEAL RING P/N 7T0541; PMA CARBON SEAL P/N 7T0530 AND SEAL RING 7T0536; STARTER CARBON SEAL P/N 7T0527. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041900026 20070419 00026 NE 2007 4 19 2007UALA01062 2 20070406 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 OIL CONSUMPTION A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 651UA 25389 724679 NR 1 ENG HIGH OIL CONSUMPTION EXCEEDS LIMIT. [SUP 05-08-07] PRECAUTIONARY REPORT. NO OIL LEAKS DISCOVERED. SUSPECT O VER SERVICING. 2 L 7 2 4F 4 F RT A1NM E24NE 2007041900027 20070419 00027 EU 2007 4 19 2007UALA01063 1 20070407 A 5311 FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 432UA 587 FRAME 32 HAS 5 EA FRAME CLEATS WITH CORROSION BETWEEN STR 42L AND STR 40R. MAJOR REPAIR ACCOMPLISHED: REPLACED CLEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900028 20070419 00028 NM 2007 4 19 MWEA070084 1 20070411 A 7830 7150922 FRAME BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 914ME 55177 RT THRUST REVERSER LOWER DOOR, ZEE CHANNEL AT STATION 26.66 CRACKED AT IB END. FABRICATED AND INSTALLLED ZEE FRAME. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007041900029 20070419 00029 NM 2007 4 19 MWEA070085 1 20070411 A 7830 7150922 FRAME BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE THURST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 914ME 55177 LT THRUST REVERSER LOWER DOOR, ZEE CHANNEL AT STATION 26.66 CRACKED AT IB END. FABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007041900031 20070419 00031 NM 2007 4 19 MWEA070087 1 20070411 A 7830 7150923 FRAME BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 914ME 55177 LT THRUST REVESER LOWER DOOR, ZEE CHANNEL AT STATION 35 CRACKED AT OB. FABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007041900032 20070419 00032 NM 2007 4 19 MWEA070088 1 20070411 A 7830 7150923 FRAME BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 914ME 55177 RT THRUST REVERSER UPPER DOOR, ZEE CHANNEL AT STATION 35 IS CRACKED ON THE OB END. FABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007041900033 20070419 00033 NM 2007 4 19 MWEA070089 1 20070411 A 7830 7150922 FRAME BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 914ME 55177 RT THRUST REVERSER UPPER DOOR, ZEE CHANNEL AT STATION 26 IS CRACKED AT THE IB END. FABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007041900034 20070419 00034 NM 2007 4 19 MWEA070090 1 20070411 A 7830 7150922 DOOR BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 914ME 55177 LT THRUST REVERSER UPPER DOOR, ZEE CHANNEL AT STATION 26 IS CRACKED AT THE IB END. INSTALLED DOOR. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007041900035 20070419 00035 NM 2007 4 19 MWEA070091 1 20070411 A 7830 7150922 DOOR BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 914ME 55177 LT THRUST REVERSER UPPER DOOR, ZEE CHANNEL AT STATION 26 IS CRACKED OB END. INSTALLED DOOR. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007041900036 20070419 00036 NM 2007 4 19 MWEA070092 1 20070411 A 7830 7150923 DOOR BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 914ME 55177 LT THRUST REVERSER UPPER DOOR, ZEE CHANNEL AT STATION 35 IS CRACKED AT THE OB END. INSTALLED DOOR. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007041900037 20070419 00037 EU 2007 4 19 2007UALA01064 1 20070407 A 5311 FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 432UA 587 FWD PIT FR 26 HAS 2 EA FRAME CLEATS WITH CORROSION BETWEEN STR 41R AND 44R. MAJOR REPAIR ACCOMPLISHED: REPLACED CLEATS . 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900038 20070419 00038 NE 2007 4 19 2007UALA01066 2 20070408 A 7230 COMPRESSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE SURGES A UALA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 454UA 1104 V11015 ENGINE NR 1 AUDIBLE COMPRESSOR SURGE. [SUP 05-18-07] DETERMINED THAT VARIABLE STATOR VANE ACTUATOR WAS MALFUNCTIONING AND WAS REPLACED. FURTHER TEARDOWN FOUND EXTENSIVE FUEL LACQUERING THROUGHOUT ACTUATOR, WHICH INTERFERED WITH PROPER OPE RATION. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900039 20070419 00039 NM 2007 4 19 2007UALA01067 1 20070408 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR UPPER DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 L-1 DOOR UPPER GATE IS CRACKED AND CORRODED EXCESSIVELY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041900041 20070419 00041 NM 2007 4 19 2007UALA01069 1 20070408 A 5210 PAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 L-1 DOOR EXTERNAL HANDLE PAN IS GOUGED. [06-14-07] REMOVED AND REPLACED HANDLE PAN PER UA ENGINEERING SPECIFICATIO NS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041900042 20070419 00042 NM 2007 4 19 2007UALA01070 1 20070408 A 3397 80541 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EEL LIGHT INOP AT DOOR 5 RIGHT AFT LOWER WALL CROSS AISLE. REPLACED LIGHT ASSY, AND POWER CABLE. CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900043 20070419 00043 NM 2007 4 19 2007UALA01071 1 20070406 A 3350 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 848UA 1647 EMERGENCY LIGHT TEST THROUGH SIDS FAULTING EPSU COMM EMER R AND L. [SUP 05-08-07] COMPLETED TSM 33-51-00-201 TEST 11WL AND 12WL OPS GOOD MESSAGE CLEAERD THROUGH CIDS 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900044 20070419 00044 EU 2007 4 19 2007UALA01072 1 20070406 A 3350 BR964421 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 423UA 504 EMERGENCY FLOOR PATH LIGHT DAMAGED AT SEAT 23ABC. REPLACED LIGHT ASSY, EMERGENCY LIGHTS OP CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900046 20070419 00046 EA 2007 4 19 COMA0760317 1 20070414 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 720SW 7297 FLAPS FAIL MSG AT 30 DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE (FIRST EVENT) MAINTENANCE ACTION, PARAGR APH (G) 1,2,3, (A,B,C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F 4 F RT A21EA E15NE 2007041900048 20070419 00048 EU 2007 4 19 AWXA200700496 1 20070402 A 3397 33511600 WIRE HARNESS AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHTS WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 634AW 091 SAL - SEAT 9L HAS A DAMAGED EMERGENCY ESCAPE PATH LIGHT WIRE. REPAIRED AND OPERATIONAL CHECKED SEAT 9L HAS A DAMAGED EM ERGENCY ESCAPE PATH LIGHT WIRE IAW AIRBUS ESPM 20-43-11 AND AWA TASK CARD C1C25312. 2 L 7 2 4F RT A28NM 2007041900049 20070419 00049 NM 2007 4 19 FDKA20703119 1 20070314 A 3350 1317 LAMP DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE EMERGENCY LIGHT INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 810LR 003 FDM 6209 JFK-ORF (1712 PHX LCL). 1 FLOOR EMERGENCY PATH LIGHT INOP. MX RELAMPED AND OPS CHECKED NORMAL. 2 H 7 2 4T 4 T RT A13NM E20NE 2007041900050 20070419 00050 SO 2007 4 19 FDKA200703147 1 20070330 A 3350 SIGN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY EXIT UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 853MJ 145464 FDM 6040 ATL-PFN (1328 PHX LCL). EMERGENCY EXIT ROW LIGHTED SIGN INOP AT ROW 12. MX SECURED THE SIGN AND OPS CHECK NOR MAL. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007041900051 20070419 00051 SO 2007 4 19 FDKA200704150 1 20070404 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY EXIT INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 838MJ 145384 FDM 6149 (1611 PHX LCL). EMERGENCY EXIT OVERHEAD LIGHT AT ROW 12 WAS INOPERATIVE. MX OPS CHECKED THE LIGHT AND OPS WER E GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007041900052 20070419 00052 SO 2007 4 19 FDKA200704152 1 20070411 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY EXIT INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 829MJ 145228 FDM 6103 (0330 PHX LCL). EMERGENCY EXIT BOTTOM ROW TRACK LIGHTS INOP. MX RESET LIGHT SYSTEM OPS CHECK GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007041900053 20070419 00053 SO 2007 4 19 FDKA200704153 1 20070412 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM 6212 (0234 PHX LCL). FLOOR EMERGENCY LIGHTS AT ROWS 8 TO 11 ARE INOPERATIVE. MX OPS CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007041900054 20070419 00054 SO 2007 4 19 FDKA200704155 1 20070415 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY EXIT INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6100 (0630 PHX LCL) . EMERGENCY EXIT FLOOR LIGHTING INOP. MX PERFORMED OPS CHECK OF THE FLOOR LIGHTS AND OPS CHECK NORMAL. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007041900055 20070419 00055 SO 2007 4 19 FDKA200704156 1 20070415 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY EXIT INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 847MJ 145517 FDM 6017 (1919 PHX LCL). RT OVERWING EXIT LIGHT INOP. MX RESET SYSTEM OPS GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007041900056 20070419 00056 NM 2007 4 19 BB07034 1 20070416 A 2613 DETECTOR BOEING 757 757225 1384959 NM UNKNOWN A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 919UW 22198 FLIGHT 1268, PHL-SJU: ON CLIMBOUT, CREW RECEIVED MASTER WARNING, FIRE WARNING, AND FIRE BELL INTERMITTENTLY. FLIGHT RE TURNED TO PHL. MAINTENANCE REPLACED THE NR 1 AND NR 2 TURBINE OVERHEAT DETECTORS ON THE RIGHT ENGINE AND FIRE/OVERHEAT CARD M10426. 2 L 7 2 4F RT A2NM 2007041900063 20070419 00063 NM 2007 4 19 HNAA0700059 1 20070411 A 4900 APU DHAV DHC8 DHC8102 2809003 NM SMOKE A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 805EX 228 BURNED PLASTIC ODOR ON FLIGHT DECK AND CABIN ALONG WITH A HAZE. RAN BOTH ENG FOR TWO HOURS, NO SMOKE IN BLEEDS, EXCESSI VE SMOKE OBSERVED WITH APU RUNNING HOT OR COLD. DEFERRED APU AT THIS TIME. 2 H 7 2 4T RT A13NM 2007041900064 20070419 00064 NM 2007 4 19 HNAA0700060 1 20070412 A 2120 UNKNOWN DHAV DHC8 DHC8102 2809003 NM CABIN ODOR A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 812EX 312 F/A REPORTS STRONG ELECTRICAL ODOR IN CABIN AT APPROX ROW 4A. REPLACED CONNECTOR J36 AND MATING P40. INSPECTED ADJACE NT WIRING AND REPLACED OVERHEATED SPLICE ON GRAY AND YELLOW/BROWN WIRES AT P40. OPERATED SYSTEMS SEVERAL HRS & NO OVERH EAT NOTED. 2 H 7 2 4T RT A13NM 2007041900065 20070419 00065 NM 2007 4 19 2007UALA01127 1 20070412 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EEL 1A AFT INOPERATIVE. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900066 20070419 00066 NM 2007 4 19 2007UALA01128 1 20070412 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 CEILING EMERGENCY LIGHT INOPERATIVE 33 LEFT. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900067 20070419 00067 NM 2007 4 19 2007UALA01129 1 20070412 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L1 DOOR SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 DOOR 1L EMERGENCY SLIDE ILLUMINATED LIGHT INOPERATIVE. [SUP 5-1-07] REPLACED LIGHT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900068 20070419 00068 NM 2007 4 19 2007UALA01130 1 20070412 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EEL AT 3R SIDEWALL INOPERATIVE. SECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900069 20070419 00069 NM 2007 4 19 2007UALA01131 1 20070412 A 3350 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY LIGHTS AT LEFT OVERWING FAIRING AFT 2 ASSEMBLIES INOPERATIVE. [SUP 5-1-07] REPLACED FUSE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900070 20070419 00070 NM 2007 4 19 2007UALA01132 1 20070412 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY EXIT SIGN AT 3L INOPERATIVE. [SUP 5-1-07] RELAMPED SIGN. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900087 20070419 00087 EU 2007 4 19 MALA070049 1 20070413 A 2620 SWITCH SAAB SF340 340B 7860101 EU TEE HANDLE INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 422XJ 340B422 FOUND LT FIRE T-HANDLE SWITCH 1 INOPERATIVE DURING FUNCTIONAL CHECK OF ENGINE FIRE BOTTLES. RESERVE CARTRIDGE ON RIGHT FIRE BOTTLE WOULD NOT FIRE DUE TO SWITCH INOPERATIVE. INSTALLED NEW LT FIRE PULL HANDLE PANEL P/N: 7239038-503, S/N ON: 941442, S/N OFF: 0704243, IAW SAAB AMM 26-21-05. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2007041900088 20070419 00088 NM 2007 4 19 2007UALA00825 1 20070316 A 2913 NAS161210 PACKING ABEX BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE HYD PUMP LEAKING A UALA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 29 781UA 26945 POSSIBLE CENTER HYDRAULIC LEAK. NO EMERGENCY DECLARED. *S/D* FOUND C2 ELECTRIC PRESSURE OUTPUT PACKING LEAKING. REPL ACED PACKING NO LEAKS NOTED. HYDRAULIC QTY LOW C CENTER HYDRAULIC SYSTEM LOW RESERVOIR QUANTITY. SERVICED CENTER HYD S YSTEM TO FULL. MSG CLEARED. A/C CLEARED FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007041900089 20070419 00089 NM 2007 4 19 2007UALA00830 1 20070316 A 5210 113W11014109 DOOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE L4 OBSTRUCTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 783UA 44464 26950 FLT ATTENDANT REPORTED UNABLE TO ARM DOOR 4L. *S/D* REMOVED FOREIGN OBJECT OPERATES NORMAL. AIRCRAFT RETURNED TO SERV ICE. SUSPECT FOREIGN OBJECT WAS PIECE OF CABIN SERVICE MATERIAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007041900090 20070419 00090 2007 4 19 2007UALA01065 4 20070407 A 2565 D31591478U1 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU R2 DOOR DISLODGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 DOOR 2R SLIDE FELL OFF THE DOOR. *S/D* REINSTALLED SLIDE PACK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041900091 20070419 00091 NM 2007 4 19 2007UALA01073 1 20070408 A 3350 LAMP AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 813UA 858 EEL LIGHT RED IN FWD CLOSET INOPERATIVE. [SUP 5-1-07] RELAMPED OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900092 20070419 00092 EU 2007 4 19 2007UALA01074 1 20070407 A 3350 SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 485UA 1617 EEL TEST FAIL WITH MSG; EPSU BATTERY AFT LT. [SUP 5-1-07] RESET EMERGENCY LIGHT SWITCH. CYCLED NSS AND FSB SIGN SW, OP S CHECK OK, NO MESSAGE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900093 20070419 00093 2007 4 19 2007UALA01075 4 20070408 A 2565 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR SLIDE READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 497UA 1847 DOOR 2R ASSIST BOTTLE LOW. [SUP 06-01-07] SERVICED ASSIST BOTTLE TO PROPER PRESSURE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900094 20070419 00094 NM 2007 4 19 2007UALA01076 1 20070407 A 3350 362624 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 306UA 23667 AFT SEAT ROWS EEL LIGHTS ARE INOPERATIVE. *S/D* RELAMPED EEL STRIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041900095 20070419 00095 NM 2007 4 19 2007UALA01077 1 20070406 A 3397 58781 WIRE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS CUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 335UA 24230 FLOOR MOUNTED EEL LIGHTS INOP FROM ROW 12 TO ROW 15. *S/D* POWER STRIP IS CUT AT SEAT 11. REPLACED POWER STRIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041900096 20070419 00096 NM 2007 4 19 2007UALA01078 1 20070407 A 3350 CIRCUIT BREAKER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS OUT OF ADJUST A UALA L ABORTED APPROACH L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 SEAT 53ABC THE EEL FLOOR STRIP LIGHT WILL NOT TURN OFF. *S/D* RESET EMERGENCY LIGHT C/B`S AND PERFORMED OP CHECK. EME RGENCY LIGHT STRIP AT 53ABC & ZONE STRIPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041700109 20070417 00109 NM 2007 4 17 SWAA071832 1 20070411 A 5330 6545765 SKIN BOEING 737 7375H4 138449D NM BS 526 S27L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT GROUND AIR CONDITIONING DOOR CUTOUT BS 526, STR 27L. REPAIRE D SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007041700131 20070417 00131 NM 2007 4 17 SWAA071779 1 20070409 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 207WN 34012 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007041700132 20070417 00132 NM 2007 4 17 SWAA071778 1 20070409 A 3350 65C27093 LIGHT BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007041700139 20070417 00139 NM 2007 4 17 SWAA071807 1 20070410 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 360 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007041700147 20070417 00147 NM 2007 4 17 AALA20070565 1 20070327 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 929AN 30078 MIA - EMERGENCY LIGHT AT SEAT 16D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A16WE 2007041700150 20070417 00150 NM 2007 4 17 AALA20070584 1 20070330 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 604AA 27055 DFW - SEAT PATH EMERGENCY LIGHT IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR SEAT PATH EMERGENCY LIGHT IN FIRS T CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007041700172 20070417 00172 EA 2007 4 17 A6WA200740096 1 20070302 A 5210 601R3807413 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 450AW 7823 PAX DOOR ANCHOR FITTING (AFT) PN 601R3807413 IS CRACKED. MAINTENANCE REPLACED PAX DOOR ANCHOR FITTING (AFT) PN 601R3807 413 IAW AMM 52-11-17-400-803. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041700186 20070417 00186 EU 2007 4 17 07FDEA01490 1 20070413 A 5220 A52271063202 ANGLE AIRBUS 310 A310324 3930206 EU ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 CRACKED ANGLE ON EMERGENCY EXIT DOOR INTERNAL STRUCTURE, UNKNOWN CRACK LENGTH. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007041700193 20070417 00193 EU 2007 4 17 07FDEA01496 1 20070413 A 5753 A57970650003 VANE AIRBUS 310 A310324 3930206 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 CHAFING MARKS AT INBOARD FLAP VANE, RHS. REPAIR WAS PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5752-101309 AND R AS/DABRE/7006736/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007041700194 20070417 00194 EU 2007 4 17 07FDEA01497 1 20070413 A 5330 SKIN AIRBUS 310 A310324 3930206 EU ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 810FD 452 DENT IN OUTER SKIN AT C20, P24-25, RHS. REPAIR PERFORMED BY SMALL BLEND OUT IAW EA 6-5313-101308 AND RAS/DABRE/7006763/ 2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007041700207 20070417 00207 WP 2007 4 17 UPS07849619 1 20070329 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 A/C COMPT FWD BULKHEAD CORRODED AT STA 8 BL 0. REMOVED CORRODED WEB AND CHANNEL AT STA 8 BL 0 IAW SR M 51-1-20D, FABRICATED AND INSTALLED REPAIR WEB, AND CHANNEL AT STA 8 BL 0 IAW SRM 51-09-00 FIG 068A, AND EO DC8-5350-78 76. 2 L 7 4 4F RT 4A25 2007041700219 20070417 00219 NM 2007 4 17 KCSA071128 1 20070405 A 5313 FITTING BOEING 747 747236B 1384804 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STR 44R END FITTING BOLT HOLES ARE CORRODED FWD OF BS 2360. 2 L 7 4 4F A20WE 2007041700221 20070417 00221 NM 2007 4 17 KCSA071135 1 20070409 A 5315 FLOORBEAM BOEING 747 747236B 1384804 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 UPPER DECK FLOORBEAM AT STA 460 HAS DOUBLE DRILLED HOLE LBL 53 WL 308. 2 L 7 4 4F A20WE 2007041700231 20070417 00231 NM 2007 4 17 07FDEA01380 1 20070409 A 5713 ARB75412 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 CRACK FOUND AT STRINGER END 41R (XORS 704) APPROX 1" IN LENGTH IN BETWEEN 2ND AND 3RD FASTENER ON RT WING TANK DURING HF EC INSPECTION. RT WING TANK STRINGER END 41R (XORS 704) REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL I. REPA IR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007041700252 20070417 00252 NM 2007 4 17 2007UALA00977 1 20070331 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 508UA 24744 DURING REWORK OF TAIL STRIKE REPAIR AT BS 1742, DAMAGE WAS INCURRED TO STR'S 29L, 29R AND REPAIRED PER EVA IMC-00680A. [06-14-07] MAJOR REPAIR ACCOMPLISHED. REPAIRED PER UA SPEC AFTER DTA RESULTS, IT HAS BEEN DETERMINED THAT THESE RE PAIR'S ARE CONSIDERED TO BE CAT 'C' TIME LIMITED. RE-INSPECTED STR 29R & 29L REPAIRS AT BS 1742 AT EACH 'C' CHK FOR COR ROSION OR DAMAGE PER REVISED INSTRUCTIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041700263 20070417 00263 NM 2007 4 17 2007UALA00970 1 20070331 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 UPPER DECK EMERGENCY EXIT EEL LIGHT INOP AT SEAT 17AB AFT EEL LIGHT ASSY. REPLACED LIGHT ASSY. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041700326 20070417 00326 EA 2007 4 17 TRAX200700503 1 20070409 A 4920 APU CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 846AS 7328 CREW REPORTED AT 10,000 FT DURING APU START UP FUMES DETECTED IN THE CABIN AND COCKPIT APU WAS SHUT DOWN AND SMOKE AND F UMES PROCEDURES WERE FOLLOWED AND THE FLIGHT LANDED SAFELY. EMERGENCY DECLARED. FLTS 4575, 4710 CX. AUXILIARY POWER U NIT APU - INTAKE DOOR DEACTIVATED CLOSED. 2 L 7 2 4F RT A21EA 2007041700327 20070417 00327 EA 2007 4 17 TRAX200700504 1 20070409 A 3350 SWITCH CNDAIR CL600 CL6002C10 1390015 EA CABIN INTERMITTENT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 355CA 10067 REPEAT WRITE-UP, EMERGENCY LIGHT SWITCH INTERMITTANT WHEN SELECTED ON (FA); TAPPING ON SWITCH ACTIVATES EMERGENCY LIGHTI NG. FLT 4606 DEL 188 MINS. 2 L 7 2 4F RT A21EA 2007041700328 20070417 00328 EU 2007 4 17 TRAX200700505 1 20070409 A 2560 FLASHLIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 630AS 336 AFT F/A'S FLASHLIGHT IS INOP. 2 H 7 2 4T RT 2007041900002 20070419 00002 2007 4 19 YENA2007023 4 20070405 A 2330 LSEBUTK1400101 ENTERTAIN SYS AIRBUS 320 A320232 3930326 EU CABIN ODOR A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 548JB 860 1868 APRROX BETWEEN 1205Z AND 1757Z, INFLIGHT CREW REPORTS BURNING RUBBER SMELL NEAR ROW 22, ODOR IS FAINT AND COMES AND GOES , LIVE TV HAS BEEN INTERMITTENT AND FINALLY QUIT WORKING, XM AND MOVIES WORKED OK. LIVE TV WAS TURNED OFF AND MASTER SWI TCH TURNED OFF. ODOR DID NOT RETURN. PERFORMED INSPECTION ON ELECTRICAL BURNING ODOR IN CABIN IAW TSM 24-00-00-810-823, NO DEFECT NOTED. PERFORMED INSPECTION IN ACCORDANCE WITH TSM 23-39-00-810-801 TASK CARD. NO ABNORMALITIES NOTED, LIVE TV AND XM OPERATED FOR 3 HOURS, NO FURTHER DEFECTS NOTED. REPLACED XEB AT 22E AS A PRECAUTIONARY REQUIREMENT. 2 L 7 2 4F RT A28NM 2007041900003 20070419 00003 NM 2007 4 19 NOCA08107 1 20070409 A 2612 7101265 FIRE LOOP BOEING 767 767306 1385148 NM RT NACELLE MALFUNCTIONED A NOCA O OTHER N FALSE WARNING CR CRUISE 1 EA 15 765NA 28098 RIGHT ENGINE FIRE LOOP 1 STATUS MESSAGE ANNUNICATED IN FLIGHT. TROUBLESHOT REMOVED AND REPLACED NR 2 ENGINE FIRE LOOP 1 LOWER AFT OUTBOARD AS PER AMM 26-11-02. OPS CHECKS NORMAL. 2 L 7 2 4F RT A1NM 2007041900004 20070419 00004 NM 2007 4 19 NOCA08207 1 20070411 A 2612 7101265 FIRE LOOP BOEING 767 767324 1385203 NM GE CF6 CF680C2B7 NE LT NACELLE FALSE ACTIVATION A NOCA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 15 767NA 27569 L ENG FIRE LOOP 1 STATUS MESSAGE. REMOVED AND REPLACED THE AFT LOWER LOOP NR 1 DETECTOR. OPS CHKS OK. 2 L 7 2 4F 4 F RT A1NM E13NE 2007041900006 20070419 00006 NM 2007 4 19 NOCA08307 1 20070413 A 2622 3460001222 FIRE BOTTLE BOEING 767 76736N 1385152 NM PWA 4060 PW4060 52119 NE APU BAY DISCHARGED A NOCA O OTHER O OTHER NR NOT REPORTED 1 EA 15 768NA 29898 APU FIRE BOTTLE ACCIDENTALLY DISCHARGED IN LEJ. REMOVED AND REPLACED APU FIRE BOTTLE IAW AMM 26-22-02. SYSTEM CHECKS N ORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007041900008 20070419 00008 NM 2007 4 19 GTIA200700007 1 20070210 A 5220 DOOR DOUG MD80 MD83 3023681 NM PWA JT8 JT8D217A 52053 NE EMERGENCY EXIT OBSTRUCTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 UNABLE TO OPEN RT AFT OVERWING EXIT. FOUND TRIM PANEL OVERLAPPING UPPER AFT CORNER PREVENTING IT FROM OPENING. 2 L 7 2 4F 4 F RT E9NE 2007041900009 20070419 00009 WP 2007 4 19 GTIA200700008 1 20070212 A 5313 LONGERON DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE BS 1320 L29R CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 AFT CARGO COMPT LONGERON 29R HAS CORROSION. MADE LONGERON REPAIR. 2 L 7 2 4F 4 F A6WE E9NE 2007041900010 20070419 00010 WP 2007 4 19 GTIA200700009 1 20070214 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE BS 160-200 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 CORROSION ON FLOOR SUPPORT. REPAIRED FLOOR SUPPORT. 2 L 7 2 4F 4 F A6WE E9NE 2007041900011 20070419 00011 WP 2007 4 19 GTIA200700010 1 20070214 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE BS 160 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 CORROSION AT FWD CABIN FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. 2 L 7 2 4F 4 F A6WE E9NE 2007041900012 20070419 00012 WP 2007 4 19 GTIA200700011 1 20070214 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE BS 200 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 CORROSION ON FLOORBEAM. INSTALLED NEW FLOORBEAM. 2 L 7 2 4F 4 F A6WE E9NE 2007041900013 20070419 00013 WP 2007 4 19 GTIA200700012 1 20070215 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE BS 1155 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 CORROSION AFT CARGO CABIN FLOORBEAM. INSTALLED NEW FLOORBEAM. 2 L 7 2 4F 4 F A6WE E9NE 2007041900014 20070419 00014 WP 2007 4 19 GTIA200700013 1 20070216 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE BS 1309 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 AFT CARGO CABIN FLOOR INTERCOSTAL CRACKED. REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F A6WE E9NE 2007041900015 20070419 00015 WP 2007 4 19 GTIA200700014 1 20070216 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE BS 200 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 CORROSION ON FLOORBEAM ANGLE. REPLACED FLOORBEAM. 2 L 7 2 4F 4 F A6WE E9NE 2007041900016 20070419 00016 WP 2007 4 19 GTIA200700015 1 20070217 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE BS 1309 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 CABIN FLOORBEAM CORRODED. REPLACED FLOOR SUPPORT BEAM. 2 L 7 2 4F 4 F A6WE E9NE 2007041900017 20070419 00017 NM 2007 4 19 HNAA0700057 1 20070408 A 3397 CONNECTOR DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS MISINSTALLED A HNAA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 EA 07 814EX 318 EXIT SIGN ABOVE F/A'S SEAT INOP. INSPECTED AND FOUND EXIT SIGN AND CEILING LIGHT CONNECTOR SWAPPED. CONNECTED TO APPRO PRIATE RECEPTACLES. 2 H 7 2 4T RT A13NM 2007041900018 20070419 00018 EU 2007 4 19 NWAA071323302 1 20070413 A 2530 3510005301 COFFEEMAKER AIRBUS 330 A330323 3930335 EU GALLEY ODOR A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 802NW 0533 DURING TAKEOFF AN ELECTRICAL ODOR FROM NR 2 GALLEY AND NR 1 COFFEEMAKER CIRCUIT BREAKER POPPED. ODOR WOULD NOT DISSIPAT E, COFFEEMAKER REMAINED HOT. LANDING WAS UNEVENTFUL. FOUND STRONG ELECTRICAL SMELL EMITTING FROM THE BACK OF NR 1 COFF EEMAKER. COFFEEMAKER WAS REMOVED AND REPLACED AND CHECKED OK. 2 L 7 2 4F RT A46NM 2007041900097 20070419 00097 NM 2007 4 19 2007UALA01079 1 20070407 A 3397 362624 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 SEAT ROW 56 RIGHT EEL LIGHT WIRE BROKEN. *S/D* REPLACED SEAT LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900098 20070419 00098 NM 2007 4 19 2007UALA01080 1 20070409 A 3350 80541 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY LIGHTS INOPERATIVE AT FWD GALLEY CEILING, COCKPIT CEILING, LEFT SIDE FWD GALLEY CEILING & ROW 15 CEILING. *S/ D* REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900099 20070419 00099 NM 2007 4 19 2007UALA01081 1 20070409 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY LIGHT INOPERATIVE AT DOORS 2R & 5L SLIDE ILLUM. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900101 20070419 00101 NM 2007 4 19 2007UALA01083 1 20070409 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EEL INOPERATIVE AT SEAT 3J AFT SECTION, ROW 39R & SEAT 32R. *S/D* RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900102 20070419 00102 NM 2007 4 19 2007UALA01084 1 20070407 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY LIGHT INOPERATIVE, UPPER DECK CEILING AT TOP OF STAIRS JUST AFT ROW 18. *S/D* RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900103 20070419 00103 NM 2007 4 19 2007UALA01085 1 20070407 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY LIGHT INOPERATIVE, UPPER DECK AFT CEILING BETWEEN DOORS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900104 20070419 00104 NM 2007 4 19 2007UALA01086 1 20070407 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 32HJK INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EEL INOPERATIVE, SEAT 32 HJK. *S/D* REPLACED EEL LIGHT, OP CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900105 20070419 00105 NM 2007 4 19 2007UALA01087 1 20070408 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 5A INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EEL LIGHT INOPERATIVE AT SEATS 5A AFT & 46 HJK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900106 20070419 00106 NM 2007 4 19 2007UALA01088 1 20070408 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EXIT CEILING LIGHT INOPERATIVE AT ROW 6 LEFT. *S/D* RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900107 20070419 00107 NM 2007 4 19 2007UALA01089 1 20070408 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 RIGHT SIDE EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE, 2 AFT LIGHT ASSEMBLIES. [SUP 5-1-07] REPAIRED BATTERY PACK, AND RELAMPED LOWER LITE ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900108 20070419 00108 NM 2007 4 19 2007UALA01090 1 20070407 A 3397 7945243 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 669UA 30025 EMERGENCY EEL LIGHTS INOP FROM SEATS 35AB TO AFT GALLEY LEFT SIDE. *S/D* REPLACED EEL FEEDER CABLE, OP CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007041900109 20070419 00109 2007 4 19 2007UALA01091 4 20070406 A 2565 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 SLIDE PACK NOT ATTACHED. DOOR 4L GIRT BAR SLIDER FELL OFF. [06-14-07] INSTALLED 2EA GIRT BAR SLIDERS ON DOOR 4L . OPS CHECK GOOD. TESTED AND CHECKED ADJUSTMENT 2 L 7 2 4F 4 F RT A2NM E17NE 2007041900110 20070419 00110 NM 2007 4 19 2007UALA01092 1 20070407 A 3510 MASK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FLIGHT ATTEND FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 804UA 759 AFT FLIGHT ATTENDANT LEFT O2 MASK CASING BRACKET BROKEN. [SUP 06-01-07] REPLACED AFT ATTENDANTS O2 MASK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900111 20070419 00111 EU 2007 4 19 2007UALA01093 1 20070406 A 2897 CIRCUIT BREAKER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUEL INDICATIONS BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 442UA 780 FUEL LIGHT TANK NR 1 PUMP LO PRESS IS ON. C/B N23 IS POPPED. [06-12-07] FOUND CB BUSS 1 103XP SPLY PHASE C LOOSE AND BURNED. REPLACED CB AND TERMINAL LUG. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900112 20070419 00112 2007 4 19 2007UALA01094 4 20070407 A 2565 STRUCTURE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE L1 DOOR SLIDE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 669UA 30025 METAL PIECE ON SLIDE PACK BENT. [SUP 05-08-07] STRAIGHTENED UPPER FWD SLIDE PACK LATCH ON DOOR 1L. LATCH FUNCTION FULL Y RESTORED AND SERVICEABLE. APPEARS METAL PIECE OF LATCH ON SLIDE PACK SNAGGED ON JET-BRIDGE OR OTHER AIRCRAFT SERVICE E QUIPMENT AND WAS DEFORMED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007041900113 20070419 00113 NM 2007 4 19 2007UALA01095 1 20070408 A 3150 WARNING LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE APU BATTERY ACTIVATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 182UA 25279 PRE-DEPARTURE CREW REPORTED APU BATTERY CHARGER STATUS MSG 24099A. [SUP 05-08-07] REPLACED APU BATTERY & OP CHECKS OK . MSG STATUS NORMAL, A/C RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900114 20070419 00114 NM 2007 4 19 2007UALA01096 1 20070408 A 4900 GEAR HONEYWELL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GEARBOX FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 589UA 6337 62549 28707 APU HAD SHUTDOWN, FAULT LIGHT ILLUM AND EICAS MSG. APU FAULT DISPLAYED. APU REMOVED FROM AIRCRAFT FOR METAL ON CHIP DE TECTOR. COMPOUND GEAR IN GEARBOX FAILED AND CAUSED AUTO SHUTDOWN. GEARBOX AND COOLING FAN TSHM=6337 HRS AND CSHM=8381. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041900115 20070419 00115 EU 2007 4 19 2007UALA01097 1 20070409 A 5311 FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 432UA 587 FRAME 33 HAS 5 EA FRAME CLEATS WITH CORROSION BETWEEN STR 39R AND STR 42L. *S/D* MAJOR REPAIR ACCOMPLISHED: REPLACED 5 EA CLEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900116 20070419 00116 EU 2007 4 19 2007UALA01098 1 20070409 A 5311 FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 432UA 587 FRAME 31 HAS 6 EA FRAME CLEATS WITH CORROSION BETWEEN STR 38R AND STR 41L. *S/D* MAJOR REPAIR ACCOMPLISHED: REPLACED 6 EA CLEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900117 20070419 00117 EU 2007 4 19 AWXA200700497 1 20070414 A 5740 D57252161000 FITTING AIRBUS 320 A320231 3930325 EU ZONE 500 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 634AW 091 SAL - CORROSION ON LEFT WING REAR SPAR ACTUATOR CYLINDER ANCHORAGE FITTING UPPER SURFACE, WS 70 - WS 141, RIB 2 - RIB 3. REPLACED LEFT WING REAR SPAR ACTUATOR CYLINDER ANCHORAGE FITTING UPPER SURFACE, WS 70 - WS 141, RIB 2 - RIB 3 IAW AWA ER 26-5726-07099-SS1. 2 L 7 2 4F RT A28NM 2007041900118 20070419 00118 NM 2007 4 19 AWXA200700498 1 20070410 A 5340 69451568 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - CRACKED STRINGER CLIP, BS 767, S11R. REPLACED STRINGER CLIP, BS 767, S11R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007041900119 20070419 00119 NM 2007 4 19 AWXA200700499 1 20070409 A 5315 654583468 FLOORBEAM BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - CRACKED FLOORBEAM STRAP, BS 328, RBL 36, WL 200. REPAIRED FLOORBEAM STRAP, BS 328, RBL 36, WL 200 IAW B737-300 SR M 53-10-51-2R4 FIGURE 201. 2 L 7 2 4F RT A16WE 2007041900120 20070419 00120 EU 2007 4 19 2007UALA01099 1 20070409 A 5311 FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 432UA 587 FRAME 28 HAS 1 EA FRAME CLEAT WITH CORROSION BETWEEN STR 43R AND STR 44. *S/D* MAJOR REPAIR ACCOMPLISHED: REPLACED CL EAT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900121 20070419 00121 EU 2007 4 19 2007UALA01100 1 20070409 A 5311 FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 432UA 587 FR 29 HAS 5 EA FRAME CLEATS WITH CORROSION BETWEEN STR 40L AND 41R. *S/D* MAJOR REPAIR ACCOMPLISHED: REPLACED 5 EA CL EATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900141 20070419 00141 EU 2007 4 19 2007UALA01120 1 20070411 A 5311 FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 432UA 587 FWD PIT FRAME 31 OUTER FLANGE IS CRACKED BETWEEN STR 43R AND 42R. *S/D* MAJOR REPAIR ACCOMPLISHED: INSTALLED ANGLE DO UBLER. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900142 20070419 00142 NM 2007 4 19 2007UALA01121 1 20070411 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 324-345 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 MAIN CABIN FLOOR SUPPORT STA 324 TO 345, RBL 60 HAS CORROSION. [SUP 05-04-07] MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED NEW FLOOR SUPPORT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041900143 20070419 00143 EU 2007 4 19 2007UALA01122 1 20070411 A 3350 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 484UA 1609 EMERGENCY LIGHT CHECK FAILED DOOR 1L. [SUP 5-1-07] REPLACED BATTERY PACK AND EPSU. SYSTEM CHECKS NORMAL AT THE GATE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900144 20070419 00144 2007 4 19 2007UALA01125 4 20070411 A 2565 D31591478U1 DISK AIRCRUISERS BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU ESCAPE SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 1057 24301 LOW BOTTLE PRESSURE. *S/D* FOUND THERMAL DISK LEAKING. REPLACED THERMAL DISK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041900146 20070419 00146 NM 2007 4 19 2007UALA00063 1 20070106 A 2130 MODULE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU UNSECURE A UALA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 913UA 25291 CABIN PRESSURE LOSS, ALTITUDE WARNING HORN SOUNDED ON CLIMBOUT. RETURN TO FIELD. *S/D* FOUND FAULTY P5 PRESSURIZATION PANEL AND UNSECURED DELTA P MODULE. REPLACED CABIN PRESSURIZATION SELECTOR PANEL AND DELTA P MODULE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007042300001 20070423 00001 NM 2007 4 23 WRLA2007064 1 20070417 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 274WA 48633 DURING 4C+30/60M CHECK, EGAT MECHANIC FOUND MAIN DECK CARGO SEAT TRACK CRACK AT Y:755, X:48, Z:-18. [SUP 05-02-07] REPL ACED MAIN DECK CARGO SEAT TRACK PER MD-11 SRM 53-70-00 VOL.1 REV 38 FIG.1. 2 L 7 3 4F 4 F RT A22WE E24NE 2007042300002 20070423 00002 NM 2007 4 23 WRLA2007063 1 20070407 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 274WA 48633 DURING 4C+30/60M CHECK, EGAT MECHANIC FOUND MAIN DECK CARGO SEAT TRACK CRACK AT Y:755, X:28, Z:-18. [SUP 05-02-07] REPLA CED MAIN DECK CARGO SEAT TRACK PER MD-11 SRM 53-70-00 VOL.1 REV 38 FIG.1. 2 L 7 3 4F 4 F RT A22WE E24NE 2007042300008 20070423 00008 WP 2007 4 23 AALA20070604 1 20070404 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 482AA 49675 LGA - EMERGENCY LIGHT AT FORWARD OVERHEAD MAIN ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK AT FORWARD OVERHEAD PANEL FOR INOPERATIVE EMERGENCY LIGHT AT FORWARD OVERHEAD MAIN ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007042300009 20070423 00009 NE 2007 4 23 AALA20070600 2 20070404 A 7530 C8E3815 CONTROL UNIT BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE MALFUNCTIONED A AALA A UNSCHED LANDING R M J PARTIAL RPM/PWR LOSS OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 197AN 32391 31494 LAX - DURING CLIMB AT 6000 FEET, LEFT ENGINE COMPRESSOR STALLED. ENGINE GAS TEMPERATURE AT 914 DEGREES. RETURNED TO LA X AND LANDED WITHOUT INCIDENT. LANDED WITH ENGINE AT IDLE. REPLACED NUMBER ONE ENGINE ON 05 APR AT LAX DUE TO BLEED VA LVE CONTROL UNIT FAULT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2007042300011 20070423 00011 WP 2007 4 23 AALA20070602 1 20070404 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9681B 53631 LGA - EMERGENCY LIGHT AT SEAT 29D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT 29D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007042300014 20070423 00014 NM 2007 4 23 AALA20070608 1 20070405 A 3350 LENS BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 662AA 25296 MIA - EMERGENCY LIGHT AT SEAT 6E MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 6E. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A2NM 2007042300015 20070423 00015 NM 2007 4 23 AALA20070609 1 20070405 A 3350 SHROUD BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 198AA 32392 DFW - EMERGENCY LIGHT AT SEAT 33D HAS MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 33D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007042300017 20070423 00017 NM 2007 4 23 AALA20070611 1 20070406 A 2910 271N61192 HYDRAULIC LINE BOEING 757 757223 1384957 NM RT MLG LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 606AA 27057 LAS - DURING CLIMB, LOST LEFT HYDRAULIC SYSTEM. RETURNED TO LAS AND LANDED WITHOUT INCIDENT. MANUALLY LOWERED LANDING GEAR. FOUND RIGHT MAIN LANDING GEAR DOWN LOCK ACTUATOR HYDRAULIC LINE LEAKING. REPLACED HYDRAULIC LINE ASSEMBLY FOR R IGHT MAIN LANDING GEAR DOWN LOCK ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007042300018 20070423 00018 WP 2007 4 23 AALA20070612 1 20070407 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP COCKPIT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 466AA 49596 LGA - EMERGENCY LIGHT AT OVERHEAD COCKPIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007042300019 20070423 00019 2007 4 23 AALA20070582 4 20070331 A 3442 ANTENNA BOEING 757 757223 1384957 NM WEATHER RADAR INOPERATIVE A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 624AA 24582 VVI INFLIGHT T922/31MAR - WEATHER RADAR INOPERATIVE. DECLARED EMERGENCY TO RECEIVE VISUAL CLEAR OF CLOUDS TO RETURN TO VVI. LANDED WITHOUT INCIDENT. REPLACED WEATHER RADAR ANTENNA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007042300021 20070423 00021 NM 2007 4 23 AALA20070576 1 20070330 A 3397 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 378AN 25447 JFK - EMERGENCY LIGHT AT SEAT 25B INOPERATIVE. RESECURED CONNECTOR AT WALL AT SEAT 25B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007042300025 20070423 00025 NM 2007 4 23 AALA20070573 1 20070329 A 3397 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 346AN 33085 LAX - EMERGENCY LIGHTS AT SEATS 24B TO 31B INOPERATIVE. SECURED LOOSE CONNECTOR AT SEAT 31A FOR EMERGENCY LIGHTS AT SEA TS 24B TO 31B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007042300026 20070423 00026 NM 2007 4 23 AALA20070574 1 20070330 A 2612 FAN BOEING 767 767323 1385205 NM FIRE DETECTION INOPERATIVE A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 344AN 33083 MIA INFLIGHT T238/30MAR LAX-SJU - CARGO COMPARTMENT FIRE DETECTION MESSAGE ILLUMINATED. UNABLE TO CLEAR. LANDED MIA W ITHOUT INCIDENT. REPLACED FORWARD CARGO FIRE DETECTOR FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007042300029 20070423 00029 EU 2007 4 23 AALA20070589 1 20070401 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70072 515 MIA - EMERGENCY LIGHT AT SEAT 34G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 34G. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A35EU 2007042300033 20070423 00033 NM 2007 4 23 AALA20070593 1 20070401 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 656AA 24614 MIA - EMERGENCY LIGHT AT SEAT 4E INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 4E. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F RT A2NM 2007042300034 20070423 00034 NM 2007 4 23 AALA20070625 1 20070411 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 370AA 25197 SFO - OVERWING EMERGENCY LIGHTS AT LEFT AND RIGHT INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHTS AT L EFT AND RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007042300035 20070423 00035 NM 2007 4 23 AALA20070627 1 20070111 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 909AN 29511 TUL- EMERGENCY LIGHT BATTERY PACK BETWEEN STATION 300 TO 400 FAILED FUNCTIONAL CHECK. REPLACED BATTERY PACK BETWEEN STA TION 300 TO 400 FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042300036 20070423 00036 NM 2007 4 23 AALA20070618 1 20070409 A 3350 LENS BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 638AA 24596 MIA - EMERGENCY LIGHT AT SEAT 6E HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 6E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007042300038 20070423 00038 NM 2007 4 23 AALA20070614 1 20070407 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 188AN 32382 TPA - EMERGENCY LIGHTS FROM SEAT ROW 26 TO AFT OF CABIN INOPERATIVE. REPLACED BATTERY PACK AT RIGHT NUMBER FOUR CEILING PANEL FOR INOPERATIVE EMERGENCY LIGHTS FROM SEAT ROW 26 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007042300039 20070423 00039 WP 2007 4 23 AALA20070615 1 20070407 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 411AA 49322 LGA - EMERGENCY LIGHT AT SEAT ROW 25 INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD BIN FOR EMERGENCY LIGHT AT SEAT ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007042300041 20070423 00041 NM 2007 4 23 AALA20070621 1 20070410 A 2530 46700017 COFFEEMAKER BOEING 767 767323 1385205 NM GALLEY MALFUNCTIONED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 21 363AA 24044 FLIGHT ATTENDANT SAW FLASH AND HEARD POP FROM COFFEEMAKER NUMBER ONE AND TWO IN FORWARD GALLEY FOLLOWED BY SMELL OF ELEC TRICAL SMOKE FOR A COUPLE OF MINUTES. PULLED BOTH CIRCUIT BREAKERS ON COFFEE MAKER. REPLACED COFFEE MAKER NUMBER ONE A ND INSPECTED WIRING WITH NO DAMAGE FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007042300043 20070423 00043 NM 2007 4 23 AALA20070628 1 20070119 A 5320 STRAP BOEING 767 767323 1385205 NM FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 387AM 27184 AFW - BLENDING ON FORWARD LARGE CARGO DOOR LOWER SILL FAIL/SAFE STRAP BEYOND LIMITS AT STATION 550. AREA OF DISCREPANCY IS 2.5 INCHES BY 1.5 INCHES WITH AT DEPTH OF .38 INCH. REPAIRED PER MRB 767 2938. 2 L 7 2 4F RT A1NM 2007042300044 20070423 00044 NM 2007 4 23 AALA20070619 1 20070409 A 3350 SHROUD BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 638AA 24596 MIA - EMERGENCY LIGHT AT SEAT 6E MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 6E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007042300045 20070423 00045 NM 2007 4 23 AALA20070620 1 20070410 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 767AJ 33539 MIA - EMERGENCY LIGHT AT FIRST CLASS GALLEY LEFT SIDE INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT FIRST CLASS GAL LEY LEFT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007042300048 20070423 00048 WP 2007 4 23 AALA20070623 1 20070410 A 3350 BUMPER BLOCK DOUG DC9 DC982 3022082 WP CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 214AA 49162 LGA - OVERHEAD EMERGENCY EXIT LIGHT AT SEAT ROW 21 RIGHT HAS MISSING BUMPER. REPLACED BUMPER FOR OVERHEAD EMERGENCY EXI T LIGHT AT SEAT ROW 21 RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007042300049 20070423 00049 NE 2007 4 23 AALA20070597 2 20070403 A 7250 TURBINE BLADES DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT ENGINE DAMAGED A AALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 21 975TW 53625 717893 TUL INFLIGHT - DURING CLIMB FELT STRONG VIBRATION FOLLOWED BY TAIL COMPARTMENT OVER TEMPERATURE INDICATION. PRESSURIZAT ION WAS HARD TO CONTROL. LANDED TUL WITHOUT INCIDENT. FOUND DAMAGE TO FOURTH STAGE LOW PRESSURE TURBINE BLADES. REPLA CED NUMBER TWO ENGINE ON 03 APRIL 2007 AT TUL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A6WE E9NE 2007042300052 20070423 00052 EU 2007 4 23 AALA20070595 1 20070402 A 2932 TRANSMITTER AIRBUS 300 A300B4605R 3930308 EU YELLOW HYD SYS FAULTY A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 14068 511 MIA INFLIGHT - CREW NOTICED BRAKE ACCUMULATOR HYDRAULIC PRESSURE LOSS DURING CLIMB. DECLARED EMERGENCY AND LANDED MIA W ITHOUT INCIDENT. AIRCRAFT WAS NOT OVERWEIGHT FOR LANDING. REPLACED YELLOW HYDRAUCLIC SYSTEM PRESSURE TRANSMITTER PER W ORK CARD 7916. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007042300054 20070423 00054 WP 2007 4 23 AALA20070599 1 20070404 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 483A 49676 MSP - EMERGENCY LIGHT AT FIRST CLASS GALLEY WALL BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY AT FORWARD FIRST CLASS GALLE Y WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007042300055 20070423 00055 WP 2007 4 23 AALA20070624 1 20070410 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 214AA 49162 LGA - EMERGENCY AFT FLASHLIGHT HAS BROKEN STRAP. REPLACED STRAP FOR EMERGENCY AFT FLASHLIGHT. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F A6WE 2007042300056 20070423 00056 2007 4 23 ARWA20060308 4 20070327 A 3442 20707090101 ANTENNA DOUG DC10 DC1030 3023501 WP WEATHER RADAR FAULTY A ARWA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 19 524MD 46999 RADAR NR 2 DOES NOT PAINT AND WEATHER IN FLIGHT TEST PATTER OK ON THE GROUND. REMOVED AND REPLACED WEATHER RADAR ANTENN A IN ACCORDANCE WITH M/M 34-41-01. OPERATIONAL CHECK GOOD IN ACCORDANCE WITH M/M 34-41-00. 2 L 7 3 4F A22WE 2007042300057 20070423 00057 WP 2007 4 23 ARWA20070302 1 20070313 A 5753 FITTING DOUG DC10 DC1030 3023501 WP T/E FLAP GOUGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 524MD 46999 DURING AN "A" CHECK INSPECTION, THE FOLLOWING WAS FOUND, LT INBD FLAP I/B THE UNIT FITTING WAS TWO GOUGES. BLEND-OUT AR EAS, FOUND WITHIN LIMITS PER BOEING MESSAGE 1-301363052-8. 2 L 7 3 4F A22WE 2007042300058 20070423 00058 EU 2007 4 23 AWXA200700493 1 20070410 A 3397 1012887 WIRE HARNESS AIRBUS 320 A320231 3930325 EU CABIN DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 634AW 091 SAL - EEL - C-5 CHECK - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT WIRE HARNESS DAMAGED AT SEATS: 2 LEFT, 10 LEFT, 19 LEFT AND 22 LEFT. REPAIRED AND OPERATIONAL CHECKED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT WIRE HARNESS AT SEATS: 2 LEFT, 10 LEFT, 19 LEFT AND 22 LEFT IAW AIRBUS ESPM 20-53-21 AND A320 AMM 33-21-00. 2 L 7 2 4F RT A28NM 2007042300059 20070423 00059 EU 2007 4 23 AWXA200700494 1 20070409 A 3397 1012887 WIRE HARNESS AIRBUS 320 A320231 3930325 EU CABIN DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 634AW 091 SAL - EEL - C-5 CHECK - EMERGENCY ESCAPE PATH LIGHT WIRE HARNESS DAMAGED AT LEFT PARTITION. REPAIRED AND OPERATIONAL CH ECKED EMERGENCY ESCAPE PATH LIGHT WIRE HANESS AT LEFT PARTITION IAW AIRBUS ESPM 20-53-21 AND A320 AMM 33-21-00. 2 L 7 2 4F RT A28NM 2007042300061 20070423 00061 NM 2007 4 23 AWXA200700479 1 20070309 A 5330 654577572 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - CRACKED FUSELAGE SKIN, BS 727D + 3", S23R - S24R. REPAIRED FUSELAGE SKIN, BS 727D + 3", S23R - S24R IAW AWA ER 03 -5300-07100-SS2. 2 L 7 2 4F RT A16WE 2007042300063 20070423 00063 NM 2007 4 23 AWXA200700481 1 20070310 A 5210 6545871515 DOOR FRAME BOEING 737 7373G7 1384595 NM L1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - CRACKED L1 DOOR AFT FRAME, BS 348, S13L - S14L, NEAR STOP PIN CUTOUTS NR 6 AND NR 7. REPAIRED L1 DOOR AFT FRAM E, BS 348, S13L - S14L, NEAR STOP PIN CUTOUTS NR 6 AND NR 7 IAW ER 03-5200-07097-ES1. 2 L 7 2 4F RT A16WE 2007042300064 20070423 00064 NM 2007 4 23 AWXA200700482 1 20070330 A 5330 654589024 BEAR STRAP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - CRACKED BEAR STRAP, BS 303, S13L, AT LOWER HINGE FITTING ATTACH POINT. REPAIRED BEAR STRAP, BS 303, S13L, AT LOWE R HINGE FITTING ATTACH POINT IAW AWA ER 03-5300-07100-SS3. 2 L 7 2 4F RT A16WE 2007042300066 20070423 00066 NM 2007 4 23 AWXA200700484 1 20070309 A 5330 65458001129 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - CRACKED FUSELAGE SKIN, BS 303.9, S13L, L1 DOOR CUT OUT FWD LOWER CORNER. REPAIRED FUSELAGE SKIN, BS 303.9, S13L, L1 DOOR CUT OUT FWD LOWER CORNER IAW AWA ER 03-5300-7100-SS3 . 2 L 7 2 4F RT A16WE 2007042300068 20070423 00068 NM 2007 4 23 AWXA200700486 1 20070314 A 5311 697818821 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - CRACKED FRAME, BS 294.5, S10L - S11L. REPAIRED FRAME, BS 294.5, S10L - S11L IAW AWA ER 03-5312-07093-SS5. 2 L 7 2 4F RT A16WE 2007042300069 20070423 00069 NM 2007 4 23 AWXA200700487 1 20070312 A 5322 66142101 SHEAR TIE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - CRACKED INTERCOSTAL SHEAR TIE CLIP, BS 294.5, S11L. REPLACED INTERCOSTAL SHEAR TIE CLIP, BS 294.5, S11L IAW AWA E R 03-5312-0793-SS4. 2 L 7 2 4F RT A16WE 2007042300070 20070423 00070 NM 2007 4 23 AWXA200700488 1 20070312 A 5320 651768465 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - CRACKED AUXILARY INTERCOSTAL, BS 294.5 - BS 299, S10L. REPLACED AUXILARY INTERCOSTAL, BS 294.5 - BS 299, S10L IAW AWA ER 03-5312-07093-SS4. 2 L 7 2 4F RT A16WE 2007042300071 20070423 00071 NM 2007 4 23 AWXA200700489 1 20070310 A 5210 6545871140 DOOR FRAME BOEING 737 7373G7 1384595 NM R1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - R1 DOOR AFT FRAME CRACKED, BS 328, S15R AT THE 5TH STOP PIN CUT OUT. REPAIRED R1 DOOR AFT FRAME, BS 328, S15R AT THE 5TH STOP PIN CUT OUT IAW AWA ER 03-5200-07098-SS1. 2 L 7 2 4F RT A16WE 2007042300072 20070423 00072 NM 2007 4 23 AWXA200700490 1 20070403 A 5330 65458001134 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - FOUND CRACKED FUSELAGE SKIN, BS 344, S13R, R1 DOOR CUT OUT LOWER AFT CORNER. REPAIRED FUSELAGE SKIN, BS 344, S13R , R1 DOOR CUT OUT LOWER AFT CORNER IAW B737-300 SRM 53-00-01-01, FIGURE 201. 2 L 7 2 4F RT A16WE 2007042300073 20070423 00073 EU 2007 4 23 AWXA200700492 1 20070413 A 2121 EVT3454H FAN AIRBUS 320 A320232 3930326 EU E&E BAY MALFUNCTIONED A AWXA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 678AW 7257 7257 2482 SJC - BS - CREW REPORTED BLOWER FAIL ECAM MESSAGE ALONG WITH A STRONG ODOR OF AN ELECTRICAL BURNING SMELL. THE CREW DEC LARED AN EMERGENCY AND DIVERTED TO LAX. MX REPLACED THE BLOWER FAN ASSY, 20QH PER AMM 21-26-51. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007042300074 20070423 00074 NM 2007 4 23 AWXA200700491 1 20070312 A 5320 654795711 STRAP BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - CORROSION ON AFT CARGO DOOR CUT OUT LOWER SILL STRAP, BS 787 - BS 857, S25R. REPLACED AFT CARGO DOOR CUT OUT LOWE R SILL STRAP, BS 787 - BS 857, S25R IAW B737-300 SRM 53-60-15-1A1 FIGURE 101. 2 L 7 2 4F RT A16WE 2007042300075 20070423 00075 NM 2007 4 23 DL777070327 1 20070412 A 3020 ANTI-ICE VALVE BOEING 777 777232 1385232 NM RROYCE RB211 RB211TRENT89 NE NR 2 ENGINE MALFUNCTIONED A DALA C ABORTED TAKEOFF J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 864DA 29736 051200 GOT ENG A/I R ON GRND WITH SWITCH TO ON POSITION. RTB, FWD TO MCO/PLAC 30-21-01B. VLV LOCKED IN OPEN POS. CONN REMOVE D FROM CONTROLLER AND TIED BACK. 2 L 7 2 4F 4 F RT T00001SE E00050EN 2007042300082 20070423 00082 NM 2007 4 23 EIA2007055 1 20070313 A 2611 2156646 SMOKE DETECTOR BOEING 747 747273C 1384896 NM CARGO BAY INOPERATIVE A EIAA O OTHER O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 MAIN CARGO DECK SMOKE DETECTOR ZONE 5, ONE DETECTOR INOP. 2 L 7 4 4F A20WE 2007042300083 20070423 00083 NM 2007 4 23 EIA2007056 1 20070316 A 3350 513561B37 LIGHT BOEING 747 747273C 1384896 NM CABIN INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 471EV 20651 UPPER DECK EMERGENCY EXIT LIGHT IN PASSAGEWAY AT DOOR INOP. REPLACED SODERBERG CEILING LIGHT PER MM 33-51-07 AT UPPER D ECK CREW DOOR. CHECK OK PER MM 33-51-00. 2 L 7 4 4F A20WE 2007042300084 20070423 00084 NM 2007 4 23 EIA2007057 1 20070317 A 3350 51356B37 LIGHT BOEING 747 747273C 1384896 NM CABIN INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 471EV 20651 UPPER DECK EMERGENCY EXIT LIGHT LEFT SIDE INOP. REPLACED UPPER DECK LEFT SIDE EMERGENCY LIGHT PER MM 33-51-07, OPS CHK GOOD PER MM 33-51-00. 2 L 7 4 4F A20WE 2007042300085 20070423 00085 NM 2007 4 23 EIA2007058 1 20070321 A 2611 2156646A SMOKE DETECTOR BOEING 747 747273C 1384896 NM CABIN FAULTY A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 471EV 20651 MAIN DECK SMOKE DETECTOR 2B WILL NOT TEST, ITEM DEFFERED PER MEL 26-11. REPLACED SMOKE DETECTOR PER MM 26-14-02. 2 L 7 4 4F A20WE 2007042300091 20070423 00091 NM 2007 4 23 EIA2007042 1 20070222 A 5720 STRUCTURE BOEING 747 747SR46 1384816 NM RT WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 RIGHT WING LEADING EDGE LOWER CHORD FORWARD FACE CORRODED AT OLES 1520, 1440 AND 1374 AND LOWER CHORD TO SKIN INTERFACE AT OLES 1405. REMOVED CORROSION, NDT AREAS, FABBED AND INSTALLED REPAIR PER B747 SRM 57-30-01 PAGES 21-22. 2 L 7 4 4F RT A20WE 2007042300092 20070423 00092 NM 2007 4 23 EIA2007043 1 20070222 A 5711 SPAR BOEING 747 747SR46 1384816 NM RT WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 RIGHT WING FRONT SPAR LOWER CHORD FORWARD SIDE HAS CORROSION ON VERTICAL FLANGE BETWEEN OLES/FSSO 1514-1521. REMOVED CO RROSION, NDT'D AERA, FABBED AND INSTALLED REPAIR PER ECRA 477-57-117-2. 2 L 7 4 4F RT A20WE 2007042300093 20070423 00093 NM 2007 4 23 EIA2007044 1 20070222 A 5730 SKIN BOEING 747 747SR46 1384816 NM RT WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 RIGHT WING LEADING EDGE LOWER SKIN UPPER SURFACE CORRODED AT OLES/FSSO 1476-1490. REMOVED CORROSION, NDT'D AREA, FABBE D AN INSTALLED REPAIR PER ECRA 477-57-117-2. 2 L 7 4 4F RT A20WE 2007042300095 20070423 00095 NM 2007 4 23 EIA2007046 1 20070222 A 5730 SKIN BOEING 747 747SR46 1384816 NM RT WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 RIGHT WING FSSO 1528-1530 HAS AREA OF PREVIOUS CORROSION REMOVAL WHICH WAS OUT OF LIMITS AT UPPER SURFACE OF LOWER SKIN, FORWARD OF FRONT SPAR LOWER CHORD. REMOVED CORROSION, FABBED AND INSTALLED REPAIR PER ECRA 477-57-116-2. 2 L 7 4 4F RT A20WE 2007042300101 20070423 00101 SO 2007 4 23 SIMA200710613 1 20070412 A 3020 14533966401 DUCT EMB 135 EMB135KL 3260302 SO NR 1 ENGINE CRACKED A SIMA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 SW 21 845AE 10322 145685 NUMBER ONE ENGINE ANTI-ICE VALVE FAIL MESSAGE, RETURNED TO ORD. REMOVED AND REPLACED ANTI-ICING DUCT IAW EMB AMM 30-21- 25. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300104 20070423 00104 SO 2007 4 23 SIMA200710607 1 20070412 A 2120 BWT138005 DUCT EMB 135 EMB135KL 3260302 SO CABIN BLOWN A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 802AE 13287 145471 LAVATORY SMOKE AURAL WARNING ON TAKEOFF, SMOKE NOTED IN CABIN. RETURNED TO LGA. REMOVED AND REPLACED DUCT IAW EMB AMM 21-22-06. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300106 20070423 00106 EA 2007 4 23 SIMA200710611 1 20070415 A 3350 YAD4F RELAY CNDAIR CL600 CL6002C10 1390015 EA CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 519AE 8250 10131 ALL EMERGENCY LIGHTS DEAD. REMOVE AND REPLACE POWER CONTROL RELAY 135 IAW CRJ AMM 20-42-00. REMOVED AND REPLACED EMERG ENCY BATTERIES AND CHARGER IAW CRJ AMM 33-51-17. ALL ITEMS OPERATIONAL CHECKED GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007042300107 20070423 00107 GL 2007 4 23 SIMA200710604 2 20070412 A 7200 AE3007A13 ENGINE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL NR 2 LEAKING A SIMA B A EMER. DESCENT UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 846AE 16996 9006 145692 CAE311135 RECEIVED LAVATORY SMOKE INDICATION ON CLIMB-OUT, NO VISUAL INDICATION OF SMOKE, FAINT SMELL NOTED. REMOVED AND REPLACED NUMBER TWO ENGINE IAW AMERICAN EAGLE WORKCARD 72-000-00. OPERATIONAL AND LEAK CHECK GOOD WITH NO DEFECTS. RETURNED AI RCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007042300108 20070423 00108 SO 2007 4 23 SIMA200710609 1 20070414 A 3350 2013BR BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 669MB 8025 145788 EMERGENCY AFT CABIN LIGHTS AND EXIT SIGN INOPERATIVE, FERRIED AIRCRAFT TO ORD. REMOVED AND REPLACED EMERGENCY BATTERY A T AFT CEILING POSITION IAW EMB AMM 33-50-04 AND EXIT SIGN IAW EMB AMM 33-50-14. BOTH ITEMS OPERATIONAL CHECK GOOD, RETU RNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007042300109 20070423 00109 EA 2007 4 23 SIMA200710603 1 20070412 A 7722 4119T30P06 SENSOR CNDAIR CL600 CL6002C10 1390015 EA NR 1 ENGINE FAILED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 516AE 11791 8332 10123 ON CLIMB-OUT RECEIVED AN LEFT ENGINE COWL ANTI-ICE DEGRADE MESSAGE, RETURNED TO ORD. REMOVED AND REPLACED NUMBER ONE EN GINE T2 SENSOR IAW CRJ AMM 77-21-01. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007042300111 20070423 00111 SO 2007 4 23 SIMA200710612 1 20070414 A 3350 110049 CHARGER EMB 135 EMB135KL 3260302 SO CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 856AE 11310 1930 145748 AFT EMERGENCY LIGHTS INOPERATIVE OVERWING. REMOVED AND REPLACED BATTERY PACK AND CHARGER IAW CRJ AMM 33-51-17. OPERATI ONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300112 20070423 00112 SO 2007 4 23 SIMA200710610 1 20070415 A 3297 CONNECTOR EMB 145 EMB145LR 3260212 SO NLG LOOSE A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 697AB 14500875 RECEIVED AIR/GROUND FAIL MESSAGE AFTER TAKEOFF, RETURNED TO MQT. TIGHTENED LOOSE CONNECTOR ON NOSE LANDING GEAR PROXIMI TY SWITCH IAW EMB AMM 32-30-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007042300113 20070423 00113 SO 2007 4 23 SIMA200710605 1 20070413 A 3350 20131A BATTERY PACK EMB 135 EMB135KL 3260302 SO CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 816AE 12451 519 145552 EMERGENCY LIGHTS NO TEST, FOUND ALL FOUR EMERGENCY BATTERIES DEAD. REMOVED AND REPLACED BATTERY PACKS IAW EMB 33-50-04. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300115 20070423 00115 SO 2007 4 23 SIMA200710710 1 20070413 A 5347 13500438003 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AE 15775 4800 145275 RIGHT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAME 24 TO 32. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300116 20070423 00116 SO 2007 4 23 SIMA200710712 1 20070413 A 5320 13500436001 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AE 15775 4800 145275 LEFT OMEGA BEAM AT CROSSMEMBER BETWEEN FRAME 33 AND 34 CORRODED. REPAIRED OMEGA BEAM IAW EMB SRM 53-00-10, FIGURE 202. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300118 20070423 00118 SO 2007 4 23 SIMA200710708 1 20070413 A 5347 14532605015 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AE 15775 4800 145275 RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 32 AND FRAME 46. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRAF T RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300119 20070423 00119 SO 2007 4 23 SIMA200710701 1 20070412 A 5320 14521413605 BEAM EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 800AE 13129 4800 145425 CENTER BEAM FOUND CORRODED AT FRAME 20. PERFORMED CUTOUT OF CORRODED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW EM B SRM 53-21-10, FIGURE 202. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300120 20070423 00120 SO 2007 4 23 SIMA200710704 1 20070404 A 5320 14521700007 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 800AE 13126 4800 145425 LEFT OMEGA BEAM CORRODED AT FRAME 25. PERFORMED CUTOUT TO REMOVE CORROSION, FABRICATE AND INSTALLED REPAIR PARTS IAW EM B SRM 53-00-01 AND 51-40-02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007041700241 20070417 00241 NM 2007 4 17 SWAA071828 1 20070411 A 5311 6546552 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007041700261 20070417 00261 NM 2007 4 17 2007UALA00968 1 20070331 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY EXIT DOOR SLIDE LIGHT INOP AT DOOR 5 LEFT. REPLACED LAMP. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041700268 20070417 00268 NM 2007 4 17 2007UALA00955 1 20070330 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE INADEQUATE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 364UA 24533 EXTERNAL FUSELAGE SKIN FROM STA 1016 TO 1088 BETWEEN STR 24L TO 24R IS INADEQUATE. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED SKIN PNL FROM STA 1016 TO 1088, STR 24L TO STR 24R. ALSO REPLACED 6EA STRINGERS 25L, 25R, 26L, 26R, 27L & 27 R. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041700269 20070417 00269 NM 2007 4 17 2007UALA00956 1 20070330 A 5320 SPLICE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE MISREPAIRED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 364UA 24533 BS 1016 AFT PRESSURE BULKHEAD EXISTING Y-CHORD SPLICE REPAIRS BETWEEN STR 26L AND STR 27R SPLICE ANGLE NOT CENTERED ON C UT LINE. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED, OBTAINED AFT CHORD SECTION & FABRICATED/INSTALLED AFT CHORD SPLIC ES. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041700270 20070417 00270 NM 2007 4 17 2007UALA00957 1 20070330 A 5312 BULKHEAD BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 364UA 24533 AFT EQUIPMENT BAY, AFT SIDE OF FRAME AND ON PRESSURE BULKHEAD STA 1016 TO 1021 RBL 0 TO RBL 8 WL 90 TO 92 STR 24R TO 25R SEALANT LIFTED WITH LARGE AMOUNT OF POWDER. ALSO FRAME AFT SIDE WEB HAS CORROSION, SAME LOCATION. MAJOR REPAIR ACCOMP LISHED: REMOVED CORRODED SECTION OF BULKHEAD & THE RADIAL STIFFENERS AT BODY LINE 0 & 13L. REPAIRED THE BULKHEAD & REP LACED THE STIFFENERS AT BODY LINE 0 & 13L. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041700271 20070417 00271 NM 2007 4 17 2007UALA00959 1 20070401 A 3350 BR964422 POWER UNIT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 842UA 1569 EMERGENCY LIGHT TEST FAULTED RIGHT SIDE. REPLACED RIGHT SIDEWALL POWER UNIT. OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041700272 20070417 00272 NM 2007 4 17 WRLA2007057 1 20070309 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 274WA 48633 DURING 4C+30/60M CHECK, MAIN DECK CARGO SEAT TRACK CRACKED AT Y:635, X:27, Z:-18. [SUP 05-02-07] REPLACED MAIN DECK C ARGO SEAT TRACK PER MD-11 SRM 53-70-00 VOL.1 REV 38 FIG 1. 2 L 7 3 4F 4 F RT A22WE E24NE 2007041700279 20070417 00279 EU 2007 4 17 YENA2007022 1 20070403 A 2910 2766GM HYDRAULIC LINE AIRBUS 320 A320232 3930326 EU HYDRAULIC SYS LEAKING A YENA B A EMER. DESCENT UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 15 528JB 22433 1591 FLT 426 AFTER TAKEOFF, HYD GREEN RSVR LO LEVEL ECAM, ZERO QTY INDICATED. FOUND HYD LINE 2766GM LEAKING. REMOVED AND RE PLACED HYD LINE 2766GM IAW AMM 32-31-00, LEAK CHECK OK. OPS CHECK NORMAL. 2 L 7 2 4F RT A28NM 2007041800001 20070418 00001 WP 2007 4 18 07FDEA01379 1 20070408 A 3234 ABH7357511 HANDLE DOUG DC10 DC1030 3023501 WP MLG DIRTY A FDEA O OTHER J WARNING INDICATION DE DESCENT 1 SO 25 310FE 48299 PUT GEAR DOWN AND HAD 4 RED LIGHTS, PUSHED ANTI-SKID TEST AND ANTI-SKID LIGHTS REMAINED BLANK.RAISED GEA R AND LOWERED GOT 4 GREEN AND ANTI-SKID TESTED.SUSPR CT THE SWITCH WHEN THE GEAR HANDLE IS PUSHED IN, DURING PREFLT CHECKS IT WAS STI CKY. JACKED ACFT AND COMPLETED GEAR SWING. FOUND THAT HANDLE SWITCH WAS STICKING OUT CAUSING RED LIGHTS TO STAY ON WI TH HANDLE IN THE DOWN POSITION. ALSO CAUSES THE ANTI SKID NOT TO TEST (UNTIL HANDLE PUSHED ALL THE WAY IN. CLEANED HANDL E RELEASE MECHANISM REF. AMM DC10-32-31-02-7. NOW OPS CK'S GOOD ON GEAR SWING. 2 L 7 3 4F A22WE 2007041900047 20070419 00047 EA 2007 4 19 COMA0760318 1 20070414 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 917CA 7017 DURING CLIMB RECEIVED AN A/ICE DUCT WARNING MSG, FLIGHT RETURNED TO JFK. PERFORMED ENGINE RUNS WITH A/ICE SYSTEM ON, DIS CREPANCY COULD NOT BE DUPLICATED. 2 L 7 2 4F 4 F RT A21EA E15NE 2007041900057 20070419 00057 NE 2007 4 19 NWAA071335807 2 20070415 A 7200 ENGINE BOEING 757 757351 1384991 NM PWA 2037 PW2037 NE NR 1 WARNING MESSAGE A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 587NW 32986 728827 DURING CRUISE MULTIPLE ENGINE NR 1 CONTROL MESSAGES ENUNCIATED AND LEFT ENGINE THRUST DID NOT RESPOND TO THRUST LEVER IN PUT. FLIGHT CREW DIVERTED TO HNL, SHUTDOWN ENGINE NR 1 AT TOD AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED ENGINE NR 1 PDIU, EEC AND THE STATOR/ALT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041900058 20070419 00058 NM 2007 4 19 2007UALA01126 1 20070412 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EEL 3J FWD & AFT INOPERATIVE. SECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900059 20070419 00059 NM 2007 4 19 HNA0700064 1 20070409 A 3350 6013211 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHT FAULTY A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 827EX 30539 30539 390 EMERGENCY LIGHTS (FRONT TWO) GLOWED AFTER EMERGENCY LIGHT SWITCH IS TURNED OFF. REPLACED EMERGENCY BATTERY PACK AT ROW 8 LEFT. 2 H 7 2 4T RT A13NM 2007041900060 20070419 00060 NM 2007 4 19 HNAA0700063 1 20070409 A 3350 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHT INOPERATIVE A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 805 228 PASSENGER EXIT SIGN, RIGHT HAND FORWARD EMERGENCY EXIT SIGN AND NR 2 OVERHEAD WHITE DOWN LIGHTS OUT. REPLACED POWER SUP PLY 3331PS1. 2 H 7 2 4T RT A13NM 2007041900061 20070419 00061 NM 2007 4 19 HNAA0700062 1 20070408 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHT UNSECURE A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 981HA 378 RIGHT HAND FORWARD AND PAX DOOR EMERGENCY LIGHTS ARE OUT. SECURED CONNECTOR AT EMERGENCY LIGHT BATTERIES AT POSITIONS P S1 AND PS2. 2 H 7 2 4T RT A13NM 2007041900062 20070419 00062 EA 2007 4 19 HNAA0700058 1 20070412 A 5420 85430022101 STIFFENER DHAV DHC8 DHC8311 1386006 EA NACELLE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 331EN 31106 31106 279 STIFFENER CRACKED ON TOP AFT NACELLE PANEL. REPLACED STIFFENER. 2 H 7 2 4T RT A13NM 2007041900071 20070419 00071 NM 2007 4 19 2007UALA01133 1 20070411 A 2530 OVEN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE GALLEY ODOR A UALA O OTHER C B F.O.D. SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 182UA 25279 OVEN 032 AUX B-C GALLEY SMOKES AND HAS BURNED PLASTIC ODOR. [SUP 05-04-07] REPLACED OVEN, OPS NORMALLY. BURN ODOR IS GONE. A/C OK FOR SERVICE.SUSPECT FOOD SERVICE WRAP FELL ON HEATING ELEMENTS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900072 20070419 00072 NM 2007 4 19 2007UALA01134 1 20070412 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE SEATS 13C & 14C INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 811UA 847 SEATS 13C AND 14C EEPM LIGHTS ONE EACH INOPERATIVE. [SUP 05-08-07] REPLACED EEPM LIGHT ASSYS. OPS TESTS FINE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900073 20070419 00073 EU 2007 4 19 2007UALA01135 1 20070412 A 3350 BULB AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 407UA 456 SEAT 22 EMERGENCY LIGHT MISSING FWD BULB SOCKET. [SUP 5-1-07] REPLACED LIGHT ASSY. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900074 20070419 00074 EU 2007 4 19 2007UALA01136 1 20070412 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 432UA 587 STRINGER 43 LT HAS CORROSION ON THE INNER SURFACE OF THE FLANGE BETWEEN FRAME 57 AND FRAME 58. MAJOR REPAIR ACCOMPLISHE D: REMOVED CORROSION & INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900076 20070419 00076 EU 2007 4 19 2007UALA01138 1 20070412 A 2612 FIRE WARNING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO BAY FALSE ACTIVATION A UALA F ACTIVATE FIRE EXT. N FALSE WARNING NR NOT REPORTED 1 WP 29 476UA 1508 CREW REPORTS AFT PIT FIRE WARNING SOUNDED. FLT ATTENDANT AND FLT CREW CONFIRMED SMOKE IN CABIN, FLT CREW FIRED CARGO BO TTLES. [SUP 06-06-07] FIRE DEPARTMENT AND FBO MECHANIC PERFORMED A COMPLETE INSPECTION OF CARGO BAYS, AVIONICS COMPART MENTS AND CABIN. DID NOT FIND ANY EVIDENCE OF FIRE OR FURTHER SMOKE. RAN BLEED AND AIR CONDITIONING SYSTEM WITH NO DEFEC TS NOTED. SUSPECT THAT DEICE FLUID FILTERED INTO AIR CIRCULATION SYSTEM AND POOLED SOMEWHERE NEAR A HEAT SOURCE. REPLACE D DISCHARGED FIRE BOTTLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900077 20070419 00077 2007 4 19 2007UALA01139 4 20070412 A 2565 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 336UA 24240 FWD GALLEY DOOR HAS LOW BOTTLE PRESS AND TORN GIRT. [SUP 5-1-07] REPLACED BOTTLE, TORN GIRT, AND SLIDE. CAUSE OF DISCR EPANCY UNKNOWN. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041900079 20070419 00079 NM 2007 4 19 HNAA0700061 1 20070404 A 3350 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHT INOPERATIVE A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 805EX 228 EMERGENCY EXIT SIGN AT ROW I D+F FLOOR LEVEL ARE INOP. REPLACED BATTERY PACK PS2. 2 H 7 2 4T RT A13NM 2007041900080 20070419 00080 NM 2007 4 19 MWEA070083 1 20070411 A 3350 LAMP BOEING 717 717200 1383700 NM EMERGENCY LIGHT INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 908ME 55172 LIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED LEFT EXTERNAL EMERGENCY LIGHT. 2 L 7 2 4F TR A6WE 2007041900081 20070419 00081 NM 2007 4 19 2007UALA01140 1 20070412 A 5512 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZONTAL STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 336UA 24240 LEFT HORIZONTAL STAB LOWER SKIN CRACKED JUST FWD OF I/B BALANCE BAY, APPROX 65 INCHES O/B OF TAIL CONE. MAJOR REPAIR A CCOMPLISHED: INSTALLED EXTERNAL SKIN DOUBLER & ACCESS HOLE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041900082 20070419 00082 NM 2007 4 19 2007UALA01141 1 20070413 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BS 1803-1810 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA 24380 EXTERNAL FUSELAGE SKIN AT AFT PIT DOOR CUTOUT FWD SIDE STA 1803 - 1810 IS DAMAGED. [SUP 05-16-07] RECHECKED EXISTING DOUBLER ON EXT FUSE SKIN AT AFT PIT DOOR CUTOUT FWD SIDE STA 1803 - 1810. REMOVED EXISTING REPAIR DOUBLERS. TRIM OUT PER FRR UAL-744-0266. HFEC PER NTM P6 51- 00-00. NO CRACKS NOTED. REINSTALLED DOUBLERS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900083 20070419 00083 NM 2007 4 19 2007UALA01142 1 20070413 A 5230 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA 24380 AFT CARGO DOOR FWD LOWER CORNER IS DAMAGED. [SUP 05-16-07] RECHECKED DOUBLER INSTALLED ON AFT CARGO DOOR FWD LOWER C ORNER. REMOVED EXISTING DOUBLER. TRIMMED OUT DAMAGED SKIN. PERFORMED HFEC PER NTM P6 51-00-00 FIG 6, NO CRACKS NOTED. FABRICATED AND INSTALLED REPAIR PARTS AND SEAL RETAINER. A/C OK FOR SERVICE. SUSPECT IMPACT BY GROUND EQUIPMENT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900084 20070419 00084 2007 4 19 2007UALA01143 4 20070413 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT OVERWING FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 464UA 1290 RIGHT OVERWING ESCAPE SLIDE CONTAINER AFT VERTICAL FRAME HAS APPROX 9 INCH CRACK FROM AFT LWR FASTENER UP TO CTR FASTENE R. [SUP 06-06-07] REPLACED RT OVERWING ESCAPE SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900085 20070419 00085 NM 2007 4 19 2007UALA00787 1 20070315 A 5200 UNKNOWN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ARMING HANDLE UNKNOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 128UA 30023 DOOR 3L WILL NOT ARM. CYCLED ARMING HANDLE, DOOR ARMS NORMALLY. UNABLE TO DUPLICATE PROBLEM. SUSPECT F/A TECHNIQUE PR OBLEM. 2 L 7 4 4F 4 F RT A20WE E24NE 2007042300004 20070423 00004 EA 2007 4 23 VNAA0704001 1 20070404 A 2421 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 IDG LOW A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 247JS 7922 CREW REPORTED THE NR 2 GENERATOR KICKED OFF LINE DURING TAKEOFF ROLL. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NR 2 ENGINE IDG. MAINTENANCE PROPERLY SERVICED THE IDG OIL LEVEL. MAINTE NANCE PERFORMED OPS AND LEAK CHECKS IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 12-13-24-610-801. NO EVIDENCE OF LEAKS NOTED AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007042300122 20070423 00122 EA 2007 4 23 SIMA200710702 1 20070404 A 5315 CC670341757 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 503AE 11405 4212 10021 STATION 280 FLOORBEAM CORRODED ALONG TOP FLANGE. SPLICE IN FRAME 280 AND EXTENTION MOUNTS IAW AMERICAN EAGLE ENGINEERIN G ORDER CR-53MR-114. 2 L 7 2 4F RT A21EA 2007042300126 20070423 00126 SO 2007 4 23 SIMA200710724 1 20070413 A 5347 14530659007 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AE 15775 4800 145275 LEFT INBOARD SEAT TRACK BETWEEN FRAME 47 TO 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNE D AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300127 20070423 00127 SO 2007 4 23 SIMA200710718 1 20070413 A 5321 MS21718007 FLOOR PANEL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AE 15775 4800 145275 LEFT FLOOR PANEL RAMP CORRODED AT FRAME 20. REMOVED AND REPLACED RAMP IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVI CE. 2 L 7 2 4F RT T00011AT 2007042300128 20070423 00128 SO 2007 4 23 SIMA200710714 1 20070413 A 5347 14530658005 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AE 15775 4800 145275 RIGHT INBOARD SEAT TRACK BETWEEN FRAME 22 AND 46 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETUR NED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300129 20070423 00129 SO 2007 4 23 SIMA200710715 1 20070413 A 5320 14521700007 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AE 15775 4800 145275 LEFT OMEGA BEAM CORRODED AT FRAME 20. REPAIRED OMEGA BEAM IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300134 20070423 00134 SO 2007 4 23 SIMA200710723 1 20070413 A 5347 14532606017 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AE 15775 4800 145275 LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETUR NED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300135 20070423 00135 SO 2007 4 23 SIMA200710719 1 20070413 A 5347 14532606015 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AE 15775 4800 145275 LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAME 32 TO 46. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURN ED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300137 20070423 00137 SO 2007 4 23 SIMA200710709 1 20070413 A 5347 13500439007 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AE 15775 4800 145275 LEFT INBOARD SEAT TRACK BETWEEN FRAMES 18L TO 23L CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300138 20070423 00138 SO 2007 4 23 SIMA200710711 1 20070413 A 5347 14530658067 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AE * 4800 145275 RIGHT INBOARD SEAT TRACK BETWEEN FRAME 47 AND 50 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB SRM 53-01-06. RETUR NED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300141 20070423 00141 EA 2007 4 23 TRAX200700498 1 20070407 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 MINOR SURFACE CORROSION STA 349 TRANSVERSE BEAM LOWER SURFACE LT SIDE AT LBL 36 (MARKED). REMOVED AND BLENDED UNDER TEF LON STRIP AND ON THE UNDERSIDE OF 349 AT LBL 36, FOUND TO BE WITHIN LIMITS, .059 MATERIAL REMAINING PER CRJ 200 SRM 53-0 0-00. SEALED AND INSTALLED TEFLON STRIP CRJ 200 SRM 51-23-00 AND 51-42-13. SUPPLEMENTAL - SDR CLOSED 04/16/07. 2 L 7 2 4F RT A21EA 2007042300146 20070423 00146 EA 2007 4 23 TRAX200700527 1 20070415 A 2560 MEGAPHONE CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 390CA 10106 MEGA PHONE IS INOP. 2 L 7 2 4F RT A21EA 2007042300147 20070423 00147 EA 2007 4 23 TRAX200700528 1 20070416 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 835AS 7258 LEFT FS 640 INNER BONDED SKIN DOULBER CRACKED AT STR 9. COMPLIED WITH EC/TC ASA RE 601R-53-61-506. RII-5001388. 2 L 7 2 4F RT A21EA 2007042300151 20070423 00151 EA 2007 4 23 TRAX200700532 1 20070416 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 659CA 10153 RIGHT LOWER FS 280.00 WEB HAS CORROSION. [SUP 05-03-07] REPAIRED IAW ALL SRM`S. 2 L 7 2 4F RT A21EA 2007042300152 20070423 00152 EA 2007 4 23 TRAX200700534 1 20070416 A 3250 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA COCKPIT ACTIVATED A ASOA K NONE J WARNING INDICATION CL CLIMB 1 SO 27 761ND 10213 AFTER T/O AND SELECTING GEAR RETRACTION GOT A NOSE WHEEL STEERING INOP MSG. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007042300154 20070423 00154 EA 2007 4 23 TRAX200700512 1 20070410 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 971EV 7528 EMERGENCY LIGHT OUT ON THE FLOOR AT SEAT 1 CD. 2 L 7 2 4F RT A21EA 2007042300156 20070423 00156 EA 2007 4 23 TRAX200700516 1 20070411 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 RIGHT SIDE FS 625 CLIP CRACKED (MARKED). INSTALLED NEW RIGHT SIDE 625 CLIP PER CRJ200 SRM 51-42-21. SUPPLEMENTAL - SDR CLOSED 04/16/07. 2 L 7 2 4F RT A21EA 2007042300157 20070423 00157 EA 2007 4 23 TRAX200700517 1 20070411 A 3350 BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA CABIN DEFECTIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 NR 3 EMERGENCY LIGHT BATTERY PACK WILL NOT HOLD CHARGE. 2 L 7 2 4F RT A21EA 2007042300161 20070423 00161 EA 2007 4 23 TRAX200700492 1 20070408 A 5312 FLOOR SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 CORROSION ON LEFT SIDE PRESSURE FLOOR SKIN FROM FS 460 TO FS 513. [SUP 4-23-07] REPAIRED IAW ALL FAA APPROVED DATA. 2 L 7 2 4F RT A21EA 2007042300163 20070423 00163 EA 2007 4 23 TRAX200700494 1 20070408 A 5320 ANGLE CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 741EV 10155 VERTICAL ANGLE RIGHT STA 280 RBL 18 APPROX 18 IS CRACKED. 2 L 7 2 4F RT A21EA 2007042300164 20070423 00164 EA 2007 4 23 TRAX200700495 1 20070408 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 920EV 7810 FLAPS FAIL IN FLT SELECTED 8 STAYED AT 0. EMERGENCY EQUIPMENT ROLLED AS A PRECAUTION. FLT 4560 (X2) CX. 2 L 7 2 4F RT A21EA 2007042300165 20070423 00165 EA 2007 4 23 TRAX200700496 1 20070408 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 909EV 7658 FLAP FAIL AT ZERO DEGREES ON APPROACH. EMERGENCY EQUIPMENT ROLLED AS A PRECAUTION. 2 L 7 2 4F RT A21EA 2007042300167 20070423 00167 EA 2007 4 23 TRAX200700481 1 20070407 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 FLOOR SUPPORT STRINGER AFT CLEAT (CUT OUT CUP FOR HANDRAIL ARM) CORRODED. BLENDED AND REMOVED AFT CUP, FOUND TO BE OUT OF LIMITS PER CRJ 200 SRM 53-00-00 BAT 23167. DRILLED UP NEW AFT CUP REF CRJ-200 SRM 51-42-06, AND ADDED NEW NUT PLATES . INSTALLED NEW CUP ON STRINGER PER CRJ 200 SRM 51-42-06, BAT23167 4/14/2007. SUPPLEMENTAL - SDR CLOSED 04/16/07. 2 L 7 2 4F RT A21EA 2007042300171 20070423 00171 NM 2007 4 23 CALA0700183 1 20070418 A 5311 65C352436 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 CORRODED AFT CARGO COMPARTMENT FRAME AT STA 847 RBL22. REPAIRED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2007042300174 20070423 00174 NM 2007 4 23 CALA0700186 1 20070416 A 2751 18173810 TRANSMITTER BOEING 737 737724 13844BY NM T/E FLAP FAULTY A CALA O OTHER O OTHER LD LANDING 1 SW 27 24736 28803 AIRCRAFT LANDED WITH FLAPS UP. REPLACED LEFT FLAP POSITION TRANSMITTER. 2 L 7 2 4F RT A16WE 2007042300176 20070423 00176 NM 2007 4 23 CALA0700176 1 20070412 A 5310 6520723U66 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19357 23841 CRACK AROUND LWR STOP PAD FITTING AT THE FWD CARGO DOOR AFT FRAME. REPAIRED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007042300177 20070423 00177 NM 2007 4 23 CALA0700177 1 20070415 A 5330 6545775 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 FUSELAGE SKIN CRACK AT STA 870 STRINGER 23RT. REPAIRED IAW SRM 53-00-01 FIG 201. 2 L 7 2 4F RT A16WE 2007042300179 20070423 00179 NM 2007 4 23 CALA0700179 1 20070417 A 5330 65C33756 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 SKIN CRACKED AT AFT LOWER CORNER OF R1 DOOR. REPAIRED IAW SRM 53-10-01 FIG 201, REPAIR 2. 2 L 7 2 4F RT A16WE 2007042300181 20070423 00181 NM 2007 4 23 CALA0700181 1 20070410 A 5210 SUPPORT BRACKET BOEING 757 757224 1384958 NM R1 DOOR UNKNOWN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13113 27555 R1 DOOR WILL NOT CLOSE AND LATCH. REPAIRED IAW AMM 52-11-04. 2 L 7 2 4F RT A2NM 2007042300186 20070423 00186 EA 2007 4 23 COMA0760330 1 20070418 A 5320 POST CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 7013 CRACK ON INBOARD FLANGE OF LBL 27 POST AT FS 409+128 AS SEEN FROM AVIONICS BAY. COMPLIED WITH REO-53-41-056 ON LBL 27 P OST AT FS 409. 2 L 7 2 4F RT A21EA 2007042300190 20070423 00190 EA 2007 4 23 COMA07700024 1 20070414 A 3097 WIRE HARNESS CNDAIR CL600 CL6002C10 1390015 EA ANTI-ICE SYS OUT OF POSITION A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 655CA 10134 DURING CRUISE FLIGHT RECEIVED A RIGHT WING ANTI-ICE CAUTION MESSAGE, FLIGHT DIVERTED TO FWA.PERFORMED AILC SELF TEST, PA SSED TEST. REPOSITIONED HARNESS FOR RIGHT WAITS AWAY FROM DUCT. 2 L 7 2 4F RT A21EA 2007042300193 20070423 00193 EA 2007 4 23 COMA0760312 1 20070410 A 5320 601R3850241 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 915CA 7013 DURING HEAVY CHECK INSPECTION FOUND INTERCOSTAL AT FS 409.00+16, BL 0 CRACKED. REPLACED SUPPORT MEMEBER AND BRACKET PER SRM 51-42-06 AND 51-42-20. 2 L 7 2 4F RT A21EA 2007042300198 20070423 00198 EA 2007 4 23 COMA0760308 1 20070409 A 2710 272953 LINK CNDAIR CL600 CL6002B19 1900309 EA LT AILERON FRACTURED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 708CA 7235 DURING A HMV5 INSPECTION, THE LEFT AILERON OUTBOARD PCU LINK WAS FOUND TO BE FRACTURED. REPLACED PCU LINK AND ACCOMPLIS HED SB601R-27-130. 2 L 7 2 4F RT A21EA 2007042400004 20070424 00004 WP 2007 4 24 07FDEA01526 1 20070418 A 5730 SKIN DOUG DC10 DC1010 3022110 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 LEFT WING TRAILING EDGE UPPER SURFACE AT STA XORS 405-415 CLOSEOUT STRAP AND REAR SPAR ARE CORRODED. . [SUP 05-06-07] REMOVED AND REPLACED CLOSE-OUT STRAP IAW DAC DRAWING ARC0771,DC10 SRM 51-31-01 VOL II AND 51-33-01 VOL II.REMOVED CORR OSION IAW DC10 SRM 51-21-01 VOL II FOUND TO BE WITHIN LIMITS IAW FEDEX EA 8-5710-109150. 2 L 7 3 4F A22WE 2007042400005 20070424 00005 EA 2007 4 24 SWIA200718136 1 20070313 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 865AS 7507 PAX DOOR FORWARD WEB IS CRACKED IN THE RADIUS OF STEP NR 2, DISCOVERED AT C-CHECK. INSTALLED REPAIR DOUBLER ON PAX DOOR FORWARD SIDE PANEL STEP NR 2 PER CRJ200 REO 601R-52-11-1207. 2 L 7 2 4F RT A21EA 2007042400006 20070424 00006 EA 2007 4 24 SWIA200718137 1 20070313 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 865AS 7507 UPPER ENGINE SUPPORT BEAM WEB CRACKED BETWEEN BL 0.0 AND RBL9.5, DISCOVERED AT C-CHECK. INSTALLED FABRICATED DOUBLER AN D FILLER ON UPPER ENGINE SUPPORT BEAM RBL 9.5 PER CRJ200 REO 601R-53-61-2114. 2 L 7 2 4F RT A21EA 2007042400008 20070424 00008 EA 2007 4 24 SWIA200718139 1 20070313 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 865AS 7507 LBL9 STATION 280 LOWER FLOOR SUPPORT ANGLE IS CRACKED AT INBOARD AND OUTBOARD CLIPS, DISCOVERED AT C-CHECK. INSTALLED R EPAIR ANGLE AND ANGLE FILLER PER CRJ200 REO 601R-53-11-171 STEPS 6 AND 7. INSTALLED CLIPS STATION 280 LBL9.0 PER CRJ200 REO 601R-53-11-171 REV D. 2 L 7 2 4F RT A21EA 2007042400009 20070424 00009 EA 2007 4 24 SWIA200718140 1 20070313 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 865AS 7507 LBL AND RBL9 AT STATION 280 UPPER FLOOR SUPPORT CRACKED, DISCOVERED AT C-CHECK. INSTALLED NEW FORWARD STATION 280 FLOOR SUPPORT ANGLE P/N 600-34017-21 ALONG WITH SPLICE ANGLE AND FILLER ANGLE IAW CRJ200 REO 601R-53-11-136, REV NC. 2 L 7 2 4F RT A21EA 2007042400012 20070424 00012 EA 2007 4 24 SWIA200718143 1 20070313 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 865AS 7507 PAX DOOR FORWARD WEB CRACKED AT TOP OF MIDDLE STEP, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLE AND DOUBLER ON FORWAR D PAX DOOR WEB PER CRJ200 REO 601R 52-11-702 REV 'A' STEPS 8-12. 2 L 7 2 4F RT A21EA 2007042400017 20070424 00017 EA 2007 4 24 SWIA200718146 1 20070313 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT MLG WW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 865AS 7507 RIGHT WHEEL WELL BRAKE TRANSDUCER BRACKET IS CRACKED, DISCOVERED AT C-CHECK. REPLACED CRACKED SUPPORT BRACKET PN 601R 7 52-62-159 IN RIGHT WHEEL WELL PER CRJ200 SRM 51-42-06 AND CRJ200 MOD IS601R 5320-0003 REV 'A'. 2 L 7 2 4F RT A21EA 2007042400018 20070424 00018 NM 2007 4 24 ASAA0741582 1 20070420 A 5311 65582801 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 FRAME CRACKED. REPAIRED CRACKED FRAME IAW SRM 53-00-07 FIG 201. 2 L 7 2 4F RT A16WE 2007042400024 20070424 00024 WP 2007 4 24 07FDEA01525 1 20070418 A 5730 SKIN DOUG DC10 DC1010 3022110 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 LEFT WING TRAILING EDGE UPPER SURFACE CLOSEOUT PANEL IS BULGED AT THE NR 3 SPOILER AREA. INSTALLED L/W T/EDGE PANELS BET WEEN NR 2 AND 5 SPOILERS. CORROSION REMOVAL TO BE ACCOMPLISHED ON FEDEX N/R N000828-SDR 07-1740. 2 L 7 3 4F A22WE 2007042400025 20070424 00025 NM 2007 4 24 ASAA0741583 1 20070420 A 5320 6517684634 INTERCOSTAL BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 INTERCOSTAL CRACKED. CRACKED INTERCOSTAL REPLACED WITH NEW ONE IAW SRM 51-40-05 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007042400028 20070424 00028 NM 2007 4 24 QXEA200700639 1 20070410 A 3297 471515 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM NR 2 NLG WOW UNKNOWN A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 403QX 10024 10024 4037 SEA FLIGHT NR 2436: LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF, RAN CHECK LIST. NO FIX. GEAR INDICATED 3 GREEN AND 3 RED WITH HANDLE UP. 3 GREEN WITH HANDLE DOWN. MAINTENANCE REMOVED AND REPLACED NLG WOW 2 HARNESS IAW Q400 AMM 32-21-1 1-000-801 AND 32-21-11-400-801 AND TASK CARD 6071001. OPS CHECK GOOD. PERFORMED GEAR SWING IAW Q400 AMM 32-31-00-867-8 01. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007042400031 20070424 00031 EA 2007 4 24 SWIA200718103 1 20070316 A 5220 SUPPORT FITTING CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 FORWARD AND AFT HINGE SUPPORT FITTING PINS ARE CORRODED ON LEFT EMERGENCY EXIT DOOR, DISCOVERED ON C-CHECK. REPLACED FO RWARD AND AFT PINS ON EMERGENCY EXIT DOOR IAW CRJ200 AMM 20-24-00-910-801 PN MS20392-4C19. 2 L 7 2 4F RT A21EA 2007042400038 20070424 00038 NM 2007 4 24 ASAA0741578 1 20070413 A 3350 20131A BATTERY PACK BOEING 737 737490 1384715 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 796AS 28891 EMERGENCY LIGHTS CAME ON MOMENTARLY THEN GOES OFF. REPEAT WRITE UP. CHANGED BATTERY PACK. 2 L 7 2 4F RT A16WE 2007042400040 20070424 00040 EA 2007 4 24 SWIA200718111 1 20070316 A 2510 SEAT BACK CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 PILOTS UPPER SEAT BACK PANEL IS CRACKED, DISCOVERED AT C-CHECK. REPLACED PILOTS UPPER SEAT BACK PANEL P/N 1B3003-5R PER SRM 51-42-13. 2 L 7 2 4F RT A21EA 2007042400042 20070424 00042 NM 2007 4 24 ASAA0741579 1 20070416 A 5330 65458001225 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 LEFT FWD EXTERIOR FUSELAGE SKIN DENTED OUT OF LIMITS AT FS 330 BETWEEN STR 27L 28L. CUT OUT DAMAGED AREA OF SKIN, FABRI CATED AND INSTALLED AN EXTERNAL REPAIR DOUBLER IAW EA 5330 02198. 2 L 7 2 4F RT A16WE 2007042400044 20070424 00044 2007 4 24 SWIA200718149 4 20070413 A 3417 8220372445 ADC CNDAIR CL600 CL6002B19 1900309 EA NR 1 FAILED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 934SW 5228 5228 7722 "EFIS COMP MON" CAUTION MESSAGE AND "IAS" FLAG ON BOTH DISPLAYS. DETERMINED ADC 1 FAILED. PURGED PITOT/STATIC SYSTEMS NR 1 AND NR 2 IAW AMM 34-11-00, AND REPLACED NR 1 ADC IAW AMM 34-13-01. 2 L 7 2 4F RT A21EA 2007042400045 20070424 00045 EA 2007 4 24 SWIA200718150 1 20070417 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 439SW 7578 FORWARD CEILING EMERGENCY LIGHT IS INOP. REPLACED LAMP IN FORWARD CEILING EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2007042400050 20070424 00050 EA 2007 4 24 COMA0760325 1 20070418 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 32349 7013 DURING HMV7 INSP FOUND 3 CRACKS AT SEMI-PRESS. BULKHEAD FS 559, RBL 18 AT NUT PLATES. REMOVED DAMAGE AND INSTALLED DOU BLER PER COMAIR SR10-5341-0001. 2 L 7 2 4F RT A21EA 2007042400054 20070424 00054 EA 2007 4 24 COMA0760315 1 20070416 A 3010 6243843 SENSOR CNDAIR CL600 CL6002B19 1900309 EA LT WING FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 816CA 7398 DURING CLIMB WITH WING ANTI-ICE SWITCHES OFF RECEIVED A WING OVERHEAT MSG WITH TRIPLE AURAL CHIME AND RED INDICATIONS ON EICAS, RETURNED TO CVG. REPLACED THE LEFT WING CONTROL SENSOR. 2 L 7 2 4F RT A21EA 2007042400059 20070424 00059 EA 2007 4 24 COMA0760327 1 20070416 A 3260 6003304337 TARGET CNDAIR CL600 CL6002B19 1900309 EA RT NLG DOOR MISSING A COMA K NONE N FALSE WARNING AP APPROACH 1 SO 01 988CA 7204 NOSE DOOR OPEN WARNING MSG ILLUMINATED. DURING GEAR EXTENSION, MSG PERSISTED AFTER CYCLING OF GEAR. FOUND RIGHT NOSE D OOR PROX SENSOR TARGET MISSING, INSTALLED NEW TARGET. 2 L 7 2 4F RT A21EA 2007042400063 20070424 00063 2007 4 24 HNAA0700070 4 20070416 A 2312 071128231 VHF COMM DHAV DHC8 DHC8102 2809003 NM COCKPIT CONTAMINATED A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 906HA 57250 70 9 16APR07 - EXPERIENCE SMOKE IN COCKPIT, SMOKE COMING FROM NR 2 COMM DURING RUN UP, SUSPECT WATER IN NR 2 COMM. 17APR07 - REMOVED AND REPLACED NR 2 COM R/T, CONTROL HEAD, ACP OPS CHECK GOOD IAW 8 M/M 23-21-00, 23-50-00. EXCESSIVE WATER FOUND IN COCKPIT COMING FROM DITCHING HATCH AND F/O'S SIDE PANEL. INSPECTED DITCH HATCH AND SEALED F/O'S SIDE WINDOW IAW SP& P 56.1.1, PRESSURIZED A/C NO LEAKS NOTED AT THIS TIME. 2 H 7 2 4T RT A13NM 2007042400064 20070424 00064 WP 2007 4 24 IXXA07SMN125S 1 20070223 A 5340 4641324U501 FITTING DOUG DC8 DC862F 3021972 WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C-CHECK INSPECTION, MAIN CARGO BATHTUB FITTING SHOWS CRACK 2" AT STA 1530, L26R. REMOVED AND REPLACED MA IN CARGO BATHTUB FITTING AT STA. 1530.000 L-26R (P/N 4641324U501) IAW DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 2007042400065 20070424 00065 NM 2007 4 24 HNAA0700065 1 20070411 A 3350 OL3071BPEGPL LIGHT GRIMES DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST UK UNKNOWN 1 EA 07 981HA 28233 70 378 THREE RED EMERGENCY LIGHTS BURNED OUT ON FLOOR NEXT TO 1D. RELAMPED EMERGENCY LIGHTS. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007042400066 20070424 00066 WP 2007 4 24 IXXA07SMN123S 1 20070223 A 5730 SKIN DOUG DC8 DC862F 3021972 WP ZONE 600 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, RT WING OTBD L/E OUTER SECTION SHOWS 1" CRACKED AT STA XFS 885.000 (NEAR EXISTING REP AIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 07110 DATE 03/14/07, SEMAN DRAWING NR ED-4463. DATE 02-15-07 AND E O SEMAN NR 2007221 DATE 03-14-07. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-3-0 AND DC8 SRM 51-1-21. CUT OUT DAMA GED AREA IAW SEMAN DRAWING NR ED-4463. PERFORMED INSPECTION NDT-IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK, NO CORROS ION, AFTER CUT OUT DAMAGED AREA ATTACHED FORM SMN 242-2. FABRICATED REPAIR DOUBLER AL7075-T6 0.063 AND INTERNAL DOUBLER AL7075-T6 0.025 AND FILLER SKIN AL 7075-T6 0.050 AND EXTERNAL FILLER AL 7075 T6 0.063 IAW SEMAN DRAWING NR ED-4463. CL 2 L 7 4 4F 4A25 2007042400067 20070424 00067 NM 2007 4 24 HNAA0700066 1 20070414 A 3320 1011801 LIGHT DHAV DHC8 DHC8102 2809003 NM AIRSTAIR STEPS MALFUNCTIONED A HNAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 981HA 28233 70 378 ON TAXI OUT - F/A REPORTED SMOKE COMING FROM AIRSTAIR DOOR STEP LIGHTS (MIDDLE 2 LIGHTS). 2 H 7 2 4T RT A13NM 2007042400068 20070424 00068 EA 2007 4 24 HNAA0700069 1 20070415 A 2434 23088008 GENERATOR DHAV DHC8 DHC8311 1386006 EA LT & RT LIGHTNING STRIKE A HNAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 07 333EN 31998 712 221 LIGHTNING STRIKE DURING CLIMB & LOST BOTH DC GENS. C/W LIGHTNING STRIKE INSP W/C. NO DEFECTS NOTED AT THIS TIME. STAR TER/GEN P/N: 23088-008, S/N-POS 1:788, POS 2:1159. NO GENERATOR CHANGED. 2 H 7 2 4T RT A13NM 2007042400072 20070424 00072 NM 2007 4 24 KCSA071158 1 20070418 A 5412 BULKHEAD BOEING 747 747123 1384873 NM NR 1 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 NR 1 PYLON HYDRAULIC PRESSURE LINE AT NAC STA 221.9 BULKHEAD IS CHAFING. 2 L 7 4 4F A20WE 2007042400079 20070424 00079 NM 2007 4 24 KCSA071155 1 20070418 A 5230 STRUCTURE BOEING 747 747236B 1384804 NM MAIN CARGO DOOR DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STA 1830 AT STR 26L MAIN CARGO DOOR HAS DAMAGE ALONG LOWER EDGE OF DOOR. 2 L 7 4 4F A20WE 2007042400082 20070424 00082 SO 2007 4 24 LR7A07016 1 20070412 A 5320 34319323 STRUT LKHEED 382 382G 526414U SO FS770 DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 339 4590 DURING SCHEDULED A CHECK PER JOB CARD HA1200, FOUND TUBE STRUT DENTED AT FS 770, WL 164, RBL 61. REPLACED TUBE STRUT IA W SMP583 51-10 PG 3G & 51-70, LOG PAGE 26232 ITEM M5. 2 H 7 4 4T A1SO 2007042400084 20070424 00084 WP 2007 4 24 MWEA070094 1 20070413 A 2560 4A30852 GIRT BAR DOUG DC9 DC982 3022082 WP AFT GALLEY STUCK A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 810ME 48072 FLIGHT ATTENDANT UNABLE TO DISARM GIRT BAR AT AFT GALLEY DOOR. DISARMED AFT GALLEY SLIDE. 2 L 7 2 4F A6WE 2007042400104 20070424 00104 CE 2007 4 24 DXTA200702096 1 20070410 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE MLG WEAK E DXTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 393QS 5600393 CO-PILOT'S BRAKES ARE SPONGY.BLED BRAKES AS REQUIRED. NO DEFECTS NOTED. ALL WORK DONE IAW CESSNA 560 MAINTENANCE MANUAL 32-42-00. 2 L 7 2 4F RT A22CE 2007042400114 20070424 00114 NM 2007 4 24 SWAA071882 1 20070416 A 3350 D71701100 BATTERY PACK BOEING 737 7377AD 1384502 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 798SW 28436 DURING SCHEDULED HC1 CHECK, RIGHT AFT CABIN EMERGENCY EXIT LIGHT FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2007042400117 20070424 00117 NM 2007 4 24 SWAA071848 1 20070413 A 3350 OL3071BPEGL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 10 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007042400120 20070424 00120 NM 2007 4 24 SWAA071933 1 20070419 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007042400121 20070424 00121 NM 2007 4 24 SWAA071946 1 20070419 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 792SW 27887 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007042400122 20070424 00122 NM 2007 4 24 SWAA071930 1 20070419 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 409WN 27896 RIGHT FWD CABIN EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007042400124 20070424 00124 NM 2007 4 24 SWAA071932 1 20070419 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 705SW 27839 EEPLS COVER MISSING AT ROW 9 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007042400126 20070424 00126 NM 2007 4 24 SWAA071929 1 20070419 A 5610 5717623122 WINDOW BOEING 737 7375H4 138449D NM COCKPIT CRACKED A SWAA K NONE O OTHER DE DESCENT 1 SW 29 505SW 24182 AT 18,000 FT FLIGHT DECK R2 WINDOW SHATTERED WITH ELECTRICAL ARCHING, NO PRESSURIZATION PROBLEMS NOTED. REMOVED AND REP LACED R2 WINDOW, WINDOW HEAT WIRING HARNESS AND HEAT CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 2007042400127 20070424 00127 NM 2007 4 24 SWAA071948 1 20070419 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 413, LBL 3. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007042400129 20070424 00129 NM 2007 4 24 SWAA071934 1 20070419 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 23R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007042400130 20070424 00130 NM 2007 4 24 SWAA071949 1 20070419 A 5311 6545810 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 312, STR 6L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007042400131 20070424 00131 NM 2007 4 24 SWAA071951 1 20070419 A 5311 6545815 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 344, STR 7L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007042400132 20070424 00132 NM 2007 4 24 SWAA071938 1 20070419 A 5312 6545819 PRESSURE PANEL BOEING 737 7373H4 1384600 NM NLG WW CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED BRDG CHECK, FOUND NLG W/W LEFT UPPER CEILING CORRODED AT BS 251.652, LBL 2. REPAIRED W/W CEILING PER E A. 2 L 7 2 4F RT A16WE 2007042400134 20070424 00134 NM 2007 4 24 SWAA071864 1 20070414 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED SPV CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS DIM WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED BATTERY PACKS AND BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007042400135 20070424 00135 NM 2007 4 24 SWAA071865 1 20070414 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED SPV CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS DIM WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED BATTERY PACKS AND BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007042400140 20070424 00140 2007 4 24 SWAA071862 4 20070416 A 2565 LANYARD BOEING 737 7377H4 1384404 NM EVAC SLIDE BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 470WN BNG5634 33860 R1 DOOR EMERGENCY EVAC SLIDE LANYARD BROKEN. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007042400142 20070424 00142 NM 2007 4 24 SWAA071879 1 20070417 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518, STR 12L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007042400144 20070424 00144 NM 2007 4 24 SWAA071870 1 20070415 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749.5, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007042400145 20070424 00145 NM 2007 4 24 SWAA071875 1 20070416 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 794, STR 19L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007042400146 20070424 00146 NM 2007 4 24 SWAA071877 1 20070416 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007042400147 20070424 00147 WP 2007 4 24 IXXA07SMN130S 1 20070223 A 5522 SKIN DOUG DC8 DC862F 3021972 WP ELEVATOR CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C-CHECK INSPECTION, FOUND LT HORIZONTAL STABILIZER ELEVATOR LOWER SKIN CORRODED & UNBONDED, BETWEEN STATI ON XE 77.000 & XE 132.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND INTE RNAL DOUBLER. BONDED SKIN AND INTERNAL DOUBLER. CLEANED, TREATED & PRIMED AREA & REPAIR PARTS. APPLIED SEALANT TO FAYIN G SURFACES. INSTALLED REPAIR PARTS.. PERFORMED BALANCE. FOUND WITHIN OF TOLERANCE LIMITS. MOMENT:1521.12 IN-LBS IAW D C8 SRM 55-4-1 FIGURE 1 SHEET 1 AND 2,DC8 SRM 51-1-8 PAGES 17 & 18, DC8 SRM 55-2-0 PAGE 12, DC8 SRM 55-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 55-4-1 FIGURE 1 SHEET 1 & 2 ITEM E & F, DC8 SRM 51-1-9 TR NR 51-142 DATED 04-05-06, DC8 SRM 51-1 2 L 7 4 4F 4A25 2007042400150 20070424 00150 NM 2007 4 24 SWAA071868 1 20070414 A 5330 6545800 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT UPPER FWD CORNER BETWEEN BS 289.5 AND BS 290.5 , WL 233 TO WL 255. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007042400151 20070424 00151 NM 2007 4 24 SWAA071884 1 20070417 A 5755 654645165A SPOILER BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 605SW 27956 DURING SCHEDULED MV1 CHECK, FOUND LT WING NR 2 SPOILER DELAMINATED AT INBOARD END. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007042400152 20070424 00152 WP 2007 4 24 IXXA07SMN131S 1 20070223 A 5522 SKIN DOUG DC8 DC862F 3021972 WP ELEVATOR CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT HAND HORIZONTAL STABILIZER ELEVATOR UPPER SKIN CORRODED FROM STATION XE 1 49.000 TO XE 222.875.REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN AND INTERNAL DO UBLER BONDED REPAIR PARTS AS NEEDED. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFA CES. INSTALLED REPAIR PARTS. PERFORM BALANCE. FOUND WITHIN OF TOLERANCE LIMITS. MOMENT:1521.12 IN-LBS.IAW DC8 SRM 55-4-1 FIGURE 1 SHEET 1 & 2 ITEM E & F DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 55-2-0 PAGE 12,DC8 SRM 55-1-0 PAGE 1, DC8 SRM 51- 1-21, DC8 SRM 51-1-9 TR NUMBER 51-142 DATED 04-05-06,DC8 SRM 51-1-8B, AND DC8 SRM 51-1-1. 2 L 7 4 4F 4A25 2007042400153 20070424 00153 CE 2007 4 24 GLBA20060937 1 20070413 A 5330 SKIN BEECH 1900 1900D 1154162 CE BS 150 S1 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 211UX UE211 MAJOR REPAIR, UPON ROUTINE INSPECTIONS A FUSELAGE SKIN CRACK AT FS 150.6 AT STRINGER 1. CRACK APPROXIMATELY 1.3 INCHES. MAINTENANCE REPAIRED THE FUSELAGE SKIN CRACK AT BS 150.6 IAW BEECH 1900D SRM 51-70 . RII INSPECTION COMPLIED WITH PER T .C. 8.2.1. 2 L 7 2 4T RT A24CE 2007042400157 20070424 00157 NM 2007 4 24 SWAA071889 1 20070417 A 5322 69353656 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007042400158 20070424 00158 NM 2007 4 24 SWAA071887 1 20070417 A 5322 69353656 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 360, BL 0. REPAIRED SHEAR TIE PER ER. 2 L 7 2 4F RT A16WE 2007042400164 20070424 00164 NM 2007 4 24 SWAA071849 1 20070413 A 3350 1619 LIGHT BOEING 737 7373Q8 1384670 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER M M. 2 L 7 2 4F RT A16WE 2007042400165 20070424 00165 2007 4 24 SWAA071836 4 20070412 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 286WN 32471 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007042400166 20070424 00166 2007 4 24 SWAA071841 4 20070412 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 789SW 29816 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007042400172 20070424 00172 NM 2007 4 24 07FDEA01502 1 20070412 A 2610 CONNECTOR BOEING 727 727200 138407E NM FIRE PROTECTION DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 NR 1 ENG FIRE DETECTION A LOOP INOP. MEL 03APR07 00:03 YOW ACN RELEASED FOR SERVICE PER MEL/CDL: 26-06-B. REMOVABL E ON P6 AREA, APU START PANEL, L/E ANNUNC. PANEL, GEN. FAULT ANNUNC. PANEL. REMOVED RELAY R730, DEPINNED PIN 9 FROM D52 20J, DEPINNED PINS 6 & 9 OF D2664P AND REMOVED ENGINE FIRE PROTECTION PANEL FOR T/S. FOUND PINS 6&9 SHORTED TOGETHER , OPENED P6-4 C/B PANEL AND FOUND WIRING BUNDLE DAMAGED. REPLACED BURNED WIRES BEHIND P-6 PANEL.TEST FLIGHT COMPLETE. 2 L 7 3 4F RT A3WE 2007042400174 20070424 00174 EU 2007 4 24 07FDEA01529 1 20070420 A 5313 A5361164220 LONGERON AIRBUS 310 A310 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 HEAVY CORROSION ON LONGERON BETWEEN C11-C15 CABIN FLOOR STRUCTURE. REPAIR PERFORMED IAW SRM53-12-15 / FIG 207. 2 L 7 2 4F RT A35EU 2007042400178 20070424 00178 NM 2007 4 24 SWAA071954 1 20070419 A 5311 6546541 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 2L. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2007042400182 20070424 00182 NM 2007 4 24 SWAA071942 1 20070419 A 5311 65C22908 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007042400185 20070424 00185 NM 2007 4 24 SWAA071957 1 20070419 A 5512 65C25727 SKIN BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 127. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007042400189 20070424 00189 2007 4 24 SWAA071839 4 20070414 A 2565 6567380 WINDOW BOEING 737 7377H4 1384404 NM EVAC SLIDE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 204WN 29855 L1 DOOR EMERGENCY EVAC SLIDE VIEWING WINDOW LOOSE. SECURED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2007042400190 20070424 00190 NM 2007 4 24 SWAA071855 1 20070413 A 5340 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007042400192 20070424 00192 NM 2007 4 24 SWAA071852 1 20070413 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007041900123 20070419 00123 NM 2007 4 19 2007UALA01102 1 20070409 A 5100 CONTROL PANEL BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FAILED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 910UA 25254 RTFL DUE TO MODE CONTROL PANEL FAILURE. [SUP 5-1-07] FOUND FAILED MODE CONTROL PANEL. REPLACED FLIGHT CONTROL COMPUTER . SHOP FOUND A "CHECK SUM ERROR" IN COMPUTER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041900124 20070419 00124 NM 2007 4 19 2007UALA01103 1 20070409 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 223 MISREPAIRED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 515UA 24840 STA 223 FRAME IS DAMAGED ON UPPER RADIUS, 6 O'CLOCK POSITION, JUST FWD OF NOSE COMPARTMENT DOOR CUTOUT. [SUP 05-16-07] MAJOR REPAIR ACCOMPLISHED. STA 223 FRAME IS DRILLED WITH A .375 INCH HOLE ON UPR RADIUS, DUE TO PREVIOUS IMPROPER REPA IR, HFEC INSPECTED ROUTED OUT HOLE AND VERIFIED NO CRACKS OR ADDITIONAL DAMAGE EXISTS. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041900125 20070419 00125 NM 2007 4 19 2007UALA01104 1 20070409 A 5754 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 5 SLAT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 CREW REPORTS THAT THERE APPEARS TO BE PHYSICAL DAMAGE TO LEFT LEADING EDGE, POSSIBLE FOD DAMAGE OR TRAILING EDGE WEDGE D AMAGE. [06-14-07] NR 5 LEADING EDGE SLAT. AUX TRACK AFT CLEVISES WERE LOOSE AND NEEDED THE PRELOAD SHIMS INSTALLE D. ACCOMPLISHED INSTALLATION OF AFT PRE LOAD BLOCKS. ACCOMPLISHED FULL RIG PER UA ENGINEERING SPECIFICATIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041900126 20070419 00126 NE 2007 4 19 2007UALA01105 2 20070409 A 7200 TUBE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 1 ENGINE COKED A UALA O OTHER A FLAME/FIRE NR NOT REPORTED 1 WP 29 812UA 850 V10070 NR 1 ENG HAD SMALL FLAME IN TAILPIPE AFTER ENG SHUTDOWN. FLAME SELF EXTINGUISHED AND NO FIRE AGENT WAS DISCHARGED INTO ENGINE. [06-12-07] FOUND TUBES IN TAILPIPE COKED. REMOVED TUBING. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900127 20070419 00127 NE 2007 4 19 2007UALA01106 2 20070410 A 7250 BLADES AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE FRACTURED A UALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 WP 29 416UA 479 V10925 ENGINE NR 2 STALLED AT FL360 MACH .78, STALL CLEARED, STALL RECURRED AND CLEARED. EMERGENCY DECLARED. LANDING WAS UNEV ENTFUL. [07-24-07] HPC BORO REVEALED QTY. 2 STAGE 6 BLADES FRACTURED AT MID SPAN. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900128 20070419 00128 NM 2007 4 19 2007UALA01107 1 20070410 A 2997 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RAM AIR TURBINE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 RAT BREAKAWAY WIRE NEEDS TO BE REPLACED. [06-14-07] RESAFETY WIRED RAM AIR TURBINE MANUAL DEPLOY SWITCH. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041900129 20070419 00129 NM 2007 4 19 2007UALA01108 1 20070410 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 570-630 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 FUSELAGE SKIN AT BS 570-630 DENTED. [SUP 06-06-07] MAJOR REPAIR ACCOMPLISHED. ACP DETAILED VISUAL INSPECTION OF THE D ENTS, BOTH INSIDE & OUTSIDE AT EACH "A" CHECK FOR CRACKS. ACP PERMANENT DOUBLER REPAIR. FABRICATED REPLACEMENT SKIN SEC TION, SPLICE DOUBLER-TRIPLER AND FILLERS PER UA ENGINEERING SPECIFICATION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041900130 20070419 00130 NM 2007 4 19 2007UALA01109 1 20070410 A 3350 80591 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 35C MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA 24380 SEAT 35C EEL MISSING. INSTALLED NEW EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900132 20070419 00132 NM 2007 4 19 2007UALA01111 1 20070410 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY EXIT CEILING ENTRY LIGHT INOPERATIVE AT DOOR 4L. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900134 20070419 00134 NM 2007 4 19 2007UALA01113 1 20070410 A 3350 9F19948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY EXIT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY EEL EXIT SIGNS INOPERATIVE AT DOOR 4L, AFT AND DOOR 4R, FWD. *S/D* REPLACED LIGHT ASSY BOTH POSITIONS. OP C HECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900135 20070419 00135 NM 2007 4 19 2007UALA01114 1 20070410 A 3397 7956329 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY EXIT EEL LIGHTS INOPERATIVE AT SEATS 46 THRU 54 HJK. *S/D* REPLACED EEL CABLE SEATS 46 THRU 54, OP CHECKS NO RMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041900136 20070419 00136 NM 2007 4 19 2007UALA01115 1 20070410 A 2910 HYDRAULIC SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE GREEN DISCHARGED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 827UA 1022 FLIGHT DIVERTED DUE TO A TOTAL LOSS OF THE GREEN SYSTEM HYDRAULICS. [SUP 06-06-07] FOUND A SPLIT HYDRAULIC LINE IN THE NR 1 ENGINE PYLON. DAMAGE WAS DUE TO EXCESS WEAR IN THE CLAMP AREA. REPLACED DAMAGED HYDRAULIC LINE. REPLACED NR 1 ENGI NE DRIVEN PUMP AND CASE DRAIN FILTER AS A PRECAUTIONARY MEASURE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900137 20070419 00137 EU 2007 4 19 2007UALA01116 1 20070410 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 442UA 780 EPSU AFT LEFT MESSAGE ON EMERGENCY LIGHT TEST. [SUP 5-1-07] REPLACED EPSU AND BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041900138 20070419 00138 NM 2007 4 19 2007UALA01117 1 20070410 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1440 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 AFT PIT BS 1440 AT STR 26L, FRAME DENTED 2 PLACES ON INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED: REPAIRED FRAME WITH A NESTED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041900139 20070419 00139 NM 2007 4 19 2007UALA01118 1 20070410 A 3350 RELAMPED LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 777UA 26916 AFT EMERGENCY LIGHT AT SEAT 8D IS OUT. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007041900140 20070419 00140 NM 2007 4 19 2007UALA01119 1 20070410 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SEAT 2E AFT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 222UA 30553 EMERGENCY LIGHT DAMAGED AT SEAT 2E. REPLACED AFT EMERGENCY LIGHT ON SEAT 2E. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007042400193 20070424 00193 NM 2007 4 24 SWAA071853 1 20070413 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007042400197 20070424 00197 NM 2007 4 24 2007UALA01202 1 20070417 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 MAIN STAIRS EEL INOPERATIVE. REPAIRED FEEDER WIRE. CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007042400199 20070424 00199 NM 2007 4 24 2007UALA01204 1 20070416 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 572UA 26682 EMERGENCY LIGHTS ARE INOP AT AISLE LIGHTS ROWS 29 & 32, DOOR 4L EXIT SIGN, DOORS 4L & 4R EXIT MARKERS, AFT GALLEY OVERHE AD EXIT SIGN. [SUP 4-24-07] REPLACED BATTERY PACK M108 18 WITH PN 2013-1. REF MM 33-51-07-201. 2 L 7 2 4F 4 F RT A2NM E17NE 2007042400200 20070424 00200 NM 2007 4 24 2007UALA01205 1 20070416 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 572UA 26682 EMERGENCY LIGHTS ARE INOP AT DOOR 2L SLIDE LIGHT, DOOR 2L EXIT SIGN, EXIT MARKERS AT DOORS 2L & 2R, EXIT SIGN ROW 8. [S UP 4-24-07] REPLACED BATTERY PACK M733 WITH PN 2013-1, REF MM 33-51-07-201. 2 L 7 2 4F 4 F RT A2NM E17NE 2007042400202 20070424 00202 NM 2007 4 24 2007UALA01207 1 20070417 A 2910 SWITCH AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE HYD SYSTEM MALFUNCTIONED A UALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 WP 29 822UA 948 FLIGHT DIVERTED DUE TO LOSS OF GREEN HYD SYSTEM. [06-22-07] OPERATIONAL CHECKS FOUND GREEN HYDRAULIC SYSTEM PRESSURE AND FLUID LEVELS TO BE NORMAL, BUT WAS REPORTING LOW. FURTHER FAULT TRACING FOUND THE WIRING IN THE NR 1 EDP PRESSURE S WITCH CONNECTOR WAS DAMAGED AND CAUSING AN INTERMITTENT SHORT. REPLACED THE SWITCH CONNECTOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007042400204 20070424 00204 EU 2007 4 24 2007UALA01209 1 20070417 A 2910 LINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYD SYSTEM MALFUNCTIONED A UALA O OTHER K FLUID LOSS TO TAKEOFF 1 WP 29 406UA 454 CREW REPORTS LOSS OF GREEN HYDRAULICS SYSTEM. ALTERNATE GEAR EXTENTION USED FOR LANDING. [06-22-07] FOUND A CRACK U NDERNEATH A CLAMP AREA ON THE HYDRAULIC LINE TO THE MAIN LANDING GEAR UPLOCK. REPLACED HYDRAULIC LINE AND REPLACED EDP A ND CASE FILTER AS A PRECAUTIONARY MEASURE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007042400206 20070424 00206 NM 2007 4 24 2007UALA01212 1 20070417 A 5311 FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 906UA 25006 FRAME DAMAGED AT BS 908 BETWEEN STRINGERS 20R AND 23R. [SUP 05-16-07] MAJOR REPAIR: ACCOMPLISHED PER UA EVA 70187. 2 L 7 2 4F 4 F RT A16WE E21EU 2007042400208 20070424 00208 NM 2007 4 24 2007UALA01214 1 20070418 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 DAMAGE BELOW AFT CARGO DOOR LOWER FUSELAGE SKIN & WEB FITTING IN AREA OF STA 807 AT STR 27L & 27R. [SUP 05-01-07] MAJ OR REPAIR ACCOMPLISHED: REMOVED DAMAGED TO SKIN & WEB. COMPLETED MANUFACTURE OF SHEAR TIE-WEB DOUBLER AND STRINGER TIE STRAPS. INSTALLED DOUBLER/TRIPLER REPAIR. REMOVED DAMAGE TO FRAMES. MFG'D & INSTALLED FRAME REPAIR SECTION. 2 L 7 2 4F 4 F RT A16WE E21EU 2007042400209 20070424 00209 NM 2007 4 24 2007UALA01215 1 20070417 A 5210 STRAP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 596UA 28749 DOOR 1R WILL NOT ARM. [06-14-07] FOUND "D" RING STRAP LOOSE, RESECURED. DOOR ARMING OPERATION PUT BACK TO NORM AL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007042400210 20070424 00210 NM 2007 4 24 2007UALA01216 1 20070417 A 2421 GENERATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LEFT UNKNOWN A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 649UA 25286 CREW REPORTS LOSS OF LEFT GENERATOR. [SUP 05-04-07] REPLACED LEFT ENGINE INTEGRATED DRIVE GENERATOR. RAN UP ENG PER J RH 2-6-1, IDG OPERATED NORMALLY. OUTBOUND TRIP DID VERIFICATION TEST AND IDG OPERATED OK. SUSPECT INTERNAL WEAR LED TO FAULTY HERTZ OUTPUT & MISMATCH WITH OTHER A/C GENERATOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2007042400212 20070424 00212 2007 4 24 2007UALA01217 4 20070418 A 2565 B14056008 O-RING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EVAC SLIDE UNSERVICEABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 336UA 1282 24240 LOW BOTTLE PRESSURE. [SUP 05-16-07] GAUGE PORT O-RING LEAKING AND LEAKING AROUND PRESSURE GAUGE THREADS. REPLACED BOTT LE AND VALVE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007042400214 20070424 00214 CE 2007 4 24 DXTA200702101 1 20070411 A 2750 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS UNKNOWN E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 997QS 7500208 DEPARTING, GOT CAS MSG ( FLAP FAIL) VISUALLY CHECKED FULLY RETRACTED, DIVERTED. CT. CHECKED SOFT START RELAY FOR LOOSE CONNECTION TO GROUND IAW CES 750- MM 27-50-00 CLEANED FLAP BUNDLE. CHECKED MEHCANICAL RIGGING, NO PROBLEMS FOUND IAW 75 0 MM 27-50-00. CHECKED ELECTRICAL RIGGING, NO PROBLEMS FOUND IAW 750 MM 27-50-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007042400215 20070424 00215 NM 2007 4 24 2007UALA01219 1 20070418 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 FWD CABIN FLOOR STRUCTURE CREASE BEAM Z-ANGLE HAS CORROSION ON UPPER SURFACE AT BS 294 TO 360 RBL 55 TO 63 AT WL 208. [ SUP 05-01-07] MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED CORRODED CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E21EU 2007042400217 20070424 00217 WP 2007 4 24 IXXA07SMN129S 1 20070223 A 5512 PANEL DOUG DC8 DC862F 3021972 WP HORIZONTAL STAB CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 45961 DURING ROUTINE C-CHECK INSPECTION, RT HORIZONTAL STABILIZER, T/E LWR PANEL, CORRODED STA XE 149.906 - STA XE 220.343. P ERFORMED MAJOR REPAIR IAW DC8 SRM 55-3-1 FIG 1, SHEET 1 AND 2. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 55-2-0, PAGE 12. REMOVED CORRODED PANEL PLATING IAW DC8 SRM 55-1-0 PAGE 1, DC8 SRM 51-1-21. FABRICATED PANEL PLATING WITH PLATING & DOUBLER, BOTH FROM (AL 7075-T6-0.025") IAW DC8 SRM 55-3-1 FIG 1, SHEET 1 AND 2, ITEM S, T. BONDED BOTH PARTS IAW DC8 SRM 51-1-9, TR 51-142, DATE 04-05-06. CLEANED, TREATED AND PRIMED AREA AND PANEL PLATING INTERNAL PART IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED PANEL PL 2 L 7 4 4F 4A25 2007042400218 20070424 00218 EU 2007 4 24 07FDEA01431 1 20070411 A 5313 STRINGER AIRBUS 310 A310324 3930206 EU FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 801FD 539 AIR COND STR 44 LT OF FR 39 TO 40 WITH CORROSION P/N A53811373200 STRINGER REPAIRED IAW FEDEX EA 6-5310-106705. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED MAJOR. 2 L 7 2 4F RT A35EU 2007042400219 20070424 00219 EU 2007 4 24 07FDEA01432 1 20070411 A 3210 BOLT AIRBUS 310 A310324 3930206 EU NLG DOOR ACT CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 801FD 539 FOUND CRACK AT NLG DOOR ACTUATOR BOLT. REPLACE BOLT PER EO 6-5340-7-5001 A4 PART 5 REPLACED BOLT IAW EO 6-5340-7-5001A4 PART 5. PERFORMED TEST CARRY OUT A DOOR GROUND OPENING AND CLOSING TEST IAW AMM 32-31-00. 2 L 7 2 4F RT A35EU 2007042400220 20070424 00220 NM 2007 4 24 2007UALA01221 1 20070418 A 5210 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 R-1 DOOR FWD FRAME AT LOWER HINGE CUTOUT IS CRACKED. [06-14-07] MAJOR REPAIR ACCOMPLISHED. REMOVED CRACK FROM LOWER HINGE BY CUTTING -238 FRAME TO MAKE A -131 AND -237 SECTIONS PER BOEING AND UA ENGINEERING SPECIFICATIONS. ALODI NED AND PRIMED AND REIDENTIFIED FRAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2007042400221 20070424 00221 NM 2007 4 24 2007UALA01222 1 20070418 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 LEFT FUSELAGE SKIN HAS 2 EA DENTS WITHIN 1 INCH OF EACH OTHER STA 1510 ABOVE STR 17L. [SUP 05-04-07] MAJOR REPAIR ACC OMPLISHED: CUTOUT DAMAGE. INSURANCE CUT ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007042400222 20070424 00222 NM 2007 4 24 2007UALA01185 1 20070416 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT OVERWING EMERGENCY LIGHT LAMPS (1ST & 2ND) & BATTERY POWER SUP PLY FUSE. OP CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007042400223 20070424 00223 NM 2007 4 24 2007UALA01186 1 20070416 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 SEAT EEL NOT ILLUMINATED AND CABLE PLUG BROKEN AT SEAT 1A. REPLACED WITH NEW CONNECTOR & EMERGENCY LIGHT. OP CHECKED N ORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007042400225 20070424 00225 NM 2007 4 24 2007UALA01188 1 20070416 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY LIGHT ROW 5A AFT & SEATS 32 HJK ARE INOP. REPLACED LAMP, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007042400226 20070424 00226 NM 2007 4 24 2007UALA01189 1 20070416 A 3397 CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY LIGHT LEFT FWD GALLEY ACROSS DOOR 1 LEFT. REPLACED EEL CABLE. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007042400228 20070424 00228 EU 2007 4 24 07FDEA01435 1 20070411 A 5311 FRAME AIRBUS 310 A310324 3930206 EU FUSELAGE MISINSTALLED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 801FD 539 FUSELAGE RIVETS BADLY INSTALLED AT PNL 40 LT FRAME 3 REPAIRED PER SRM 53-11-12 PG 217 AND 218 FIG 203 (SHT 1 AND 2). RE PAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR. 2 L 7 2 4F RT A35EU 2007042400229 20070424 00229 EU 2007 4 24 07FDEA01437 1 20070411 A 5310 DOOR FRAME AIRBUS 310 A310324 3930206 EU FUSELAGE WORN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 801FD 539 FUSELAGE, FWD CARGO COMP'T DOOR FWD FRAME WORN FR 20 STR 39. REPAIRED PER FEDEX EA NR 6-5330-106703. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR". 2 L 7 2 4F RT A35EU 2007042400238 20070424 00238 NM 2007 4 24 2007UALA01195 1 20070415 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 563UA 26665 EMERGENCY EXIT SIGN ABOVE RIGHT OVERWING EXIT IS INOP. [SUP 4-24-07] REPLACED BATTERY PACK FOR POWER SUPPLY M10568. PC N 563-1188, REF MM-33-51-07-201. 2 L 7 2 4F 4 F RT A2NM E17NE 2007042400240 20070424 00240 NM 2007 4 24 2007UALA01197 1 20070417 A 3510 BOTTLE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CREW OXYGEN LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 787UA 26939 CREW OXYGEN PRESSURE LOW 900 PSI. [SUP 05-16-07] REPLACED OXY BOTTLE. LEAK CHKD AND INDICATED OK. SUSPECT LOW PRESSUR E THE RESULT OF CREW SNIFF TESTS DURING CHECK LIST. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007042400241 20070424 00241 EU 2007 4 24 2007UALA01198 1 20070416 A 3350 SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 423UA 504 EMERGENCY EXIT LIGHT SWITCH EXTREMELY DIFFICULT TO MOVE. [SUP 4-24-07] REPLACED SWITCH. OPS NORMAL AT THIS TIME. 2 L 7 2 4F 4 F RT A28NM E40NE 2007042400242 20070424 00242 2007 4 24 2007UALA01199 4 20070416 A 2565 FLANGE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE SLIDE CONTAINER CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 806UA 788 LEFT OVERWING SLIDE CONTAINER FLANGE CRACKED 12 INCHES ON AFT VERTICAL FLANGE AND 4 INCHES IN UPPER AFT CORNER. [06-22- 07] REPLACED LT OVERWING SLIDE PACK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007042400243 20070424 00243 WP 2007 4 24 070105 1 20070417 A 2741 MODULE DOUG DC9 DC983 3022083 WP HORIZONTAL STAB OUT OF ADJUST A WX0A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 19 863GA 49911 FLIGHT 468 LAS/LAN - THE FLIGHT CREW REPORTED THAT A STABILIZER TRIM WARNING (TAKEOFF CONFIG) WAS INITIATED DURING TAKEO FF ROLL AT 90KTS. REJECTED THE TAKEOFF. LAS VEGAS MAINTENANCE REPORTED FINDING THE HORIZONTAL STABILIZER POSITION INDI CATOR MODULE OUT OF ADJUSTMENT. ADJUSTMENT AND SATISFACTORY OPERATIONAL CHECK ACCOMPLISHED PER AMM 27-40-12. THE AIRPL ANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007042400245 20070424 00245 NM 2007 4 24 DHL2007782505 1 20070405 A 5343 SUPPORT FITTING BOEING 727 727227 1384078 NM LT NLG TRUNNION CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 782DH 61330 61330 21998 NLG LT TRUNNION SUPPORT FITTING LOWER CAP PRESENTS CORROSION. REMOVED CORROSION AT NLG LT TRUNNION SUPPORT FITTING ORG DIA 2.848" FINAL DIA 2.602 MAT. REMOVED WITHIN LIMITS IAW B727 SRM 53-40-1 FIG 2. CHAMFER BORE HOLE TO .6 BY 45 DEGREE S IAW B727 SRM 53-40-1 FIG 2. PENETRANT INSPECTED MACHINE SURFACES OF TRUNNION FITTING IAW B727 MM 20-20-02. NO DEFECT S NOTED. FAB NEW BEARING HALVES FROM ALUM NICKEL BRONZE PO NR 7177170 IAW B727 SRM 53-40-1 FIG 2. PENETRANT INSPECT OF MACHINED SURFACES OF NEW HALVES BEARING IAW BOEING SOPM 20-20-02. NO DEFECTS NOTED. CAD PLATED OUTER SURFACES OF BEAR ING IAW FAS FORM FAS0036 REV 4. INSTALLED BEARING HALVES AT LT TRUNNION IAW B727 SRM 53-40-1 FIG 2. 2 L 7 3 4F A3WE 2007042400246 20070424 00246 EU 2007 4 24 MALA070050 1 20070418 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297-303 CORRODED A MALA O OTHER O OTHER IN INSP/MAINT 1 GL 15 439XJ 340B439 THE SEAT TRACK AT BL 0, BETWEEN FS 297 AND 303, HAS A PREVIOUS REPAIR TO THE AISLE SIDE FLANGE. THE PREVIOUS REPAIR IS CORRODED OUT OF LIMIT. THE REPAIR HAS BEEN REMOVED AND REPLACED IAW MESABA EO NR S53342, REF: EAMS WORK ORDER 216120 TA SK 1516. 2 L 7 2 4T RT A52EU 2007042400247 20070424 00247 NM 2007 4 24 QXEA200700650 1 20070421 A 5210 GATE BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR UNSECURE A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 408QX 4050 LAX FLIGHT NR 2424: FUSELAGE DOORS MASTER WARNING LIGHT ILLUMINATED IN FLIGHT WITH A FWD BAGGAGE DOOR OPEN INDICATION ON MFD. PRESSURIZATION REMAINED STEADY. AIRCRAFT DIVERTED TO FAT. MAINTENANCE, UPON INITIAL INSPECTION, FOUND PRESSURIZ ATION FLAPPER DOOR NO SEATED. INSPECTED LINKAGES AND CONNECTIONS TO DOOR. NO DISCREPANCY NOTED. PERFORMED OPS CHECK O F THE DOOR IAW AMM TASK 53-32-00-710-801. NO DEFECTS NOTED. OPS TEST GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO S ERVICE. 2 H 7 2 4T RT A13NM 2007042400248 20070424 00248 NM 2007 4 24 QXEA200700630 1 20070413 A 7720 10200154 SENSOR BOMBDR DHC8 DHC8402 1390042 NM NR 1 ENGINE MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 417QX 4086 SEA FLIGHT NR 2383: NR 1 FUEL TEMPERATURE STARTED FLUCTUATING IN THE 80 AND 90 DEGREE RANGE. C/W CHECKLIST. NO IMPROVE MENT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE TEMP SENSOR IAW Q400 AMM TASK 73-31-09, PAGE 401-408. FUEL TEMP OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007042400249 20070424 00249 WP 2007 4 24 IXXA07SMN114S 1 20070223 A 5313 LONGERON DOUG DC8 DC862F 3021972 WP ZONE 100 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD BELLY PIT LONGERON 30 RIGHT HAS IMPROPER REPAIR AT STATION 460.000. R EMOVED FASTENERS AS NEEDED TO PERFORM THE REPAIR. REMOVED DAMAGED LONGERON SEGMENT. FABRICATED LONGERON SEGMENT AND SP LICES. CLEANED,TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW DC8 SRM 53-2-2 F IGURE 4 PAGE 6, DC8 SRM 51-1-20D, DC8 SRM 53-2-2 FIGURE 4A, DC8 SRM 53-4-1 FIGURE 29B SHEET 1 ITEM "A", DC8 SRM 51-2-0 F IGURE 50 SHEET 51, DC8 SRM 53-2-2 FIGURE 10 SHEET 1 AND 3 TR NUMBER 53-153 DATED 12-10-02, DC8 SRM 53-2-2 FIGURE 10 SHEE T 4 TR NUMBER 53-193 DATED 03-15-04, DC8 SRM 51-2-0 FIGURE 50 SHEET 62, DC8 SRM 51-1-8B, DC8 SRM 53-2-2 FIGURE 10 TR NUM 2 L 7 4 4F 4A25 2007042400250 20070424 00250 EU 2007 4 24 USAA070269 1 20070409 A 5315 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 174US 1492 FLOORBEAM AT Y476.4 FR 16 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM PER SRM 51-72-11; CORR LEVEL 1; TASK JA-220-535 00, DEFECT SIZE: 2 SQ INCHES. 2 L 7 2 4F RT A28NM 2007042400251 20070424 00251 2007 4 24 NWAA071295502 4 20070411 A 2565 SLIDE BOEING 757 757251 1384970 NM R4 DOOR DISLODGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 502US 23191 DURING OVERNIGHT CHECK, RAMP PERSONNEL OPENED DOOR 4 RIGHT AND ESCAPE SLIDE FELL OUT OF HOLDER ONTO THE RAMP. SLIDE WAS REMOVED AND AIRCRAFT WAS MAINTENANCE FERRIED TO DTW TO HAVE A NEW SLIDE INSTALLED. MAINTENANCE INSTALLED A NEW SLIDE AN D GIRT BAR OPERATION CHECKED GOOD, REQUIRED INSPECTION ITEM COMPLETE, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007042400252 20070424 00252 EA 2007 4 24 SIMA200711301 1 20070412 A 2840 73811812 COMPUTER CNDAIR CL600 CL6002C10 1390015 EA FUEL QTY FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 509AE 8566 4307 10078 CHANNEL 2 FUEL FAIL MESSAGE, POST INSPECTION FOUND CIRCUIT BREAKER U11 POPPED. REMOVED AND REPLACED FUEL GAUGE QUANTITY GAUGING COMPUTER IAW CRJ AMM. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007042400254 20070424 00254 SO 2007 4 24 SIMA200711303 1 20070420 A 2910 368192105 PRESSURE SWITCH EMB 135 EMB135KL 3260302 SO ZONE 400 FAILED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 856AE 7372 145748 ENGINE ONE HYDRAULIC PUMP FAIL MESSAGE, ABORTED TAKEOFF. REMOVED AND REPLACED NR 1 HYDRAULIC ENGINE DRIVEN PUMP PRESSUR E SWITCH IAW EMB 29-10-19. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE 2 L 7 2 4F RT T00011AT 2007042400255 20070424 00255 EU 2007 4 24 SIMA200711304 1 20070420 A 7931 8543 PRESSURE SWITCH SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ZONE 400 FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 904AE 22926 GEE785359 340B314 GEE785359 LEFT ENGINE OIL PRESSURE LIGHT ILLUMINATED INFLIGHT, RETURNED TO DFW. REMOVED AND REPLACED LEFT ENGINE AND POWER GEAR B OX OIL PRESSURE SWITCHES IAW SAAB AMM 79-30-05. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 2007042400256 20070424 00256 SO 2007 4 24 SIMA200711302 1 20070421 A 3350 110048 POWER SUPPLY EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHT FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 826AE 14442 145592 FOUND CABIN EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED NUMBER 1 AND NUMBER 3 POWER SUPPLIES IAW AMERICAN EAGLE WORK CARD 33-700-19. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042400257 20070424 00257 NM 2007 4 24 USAA070280 1 20070412 A 5534 ANGLE BOEING 737 737401 1384701 NM VERTICAL STAB WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 BS 1006 LEFT VERTICAL STAB SKATE ANGLE WORN. FABRICATED & INSTALLED REPLACEMENT ANGLE PER SRM 51-40-02, DEFECT SIZE: 2 X 1 INCH. 2 L 7 2 4F RT A16WE 2007042400259 20070424 00259 2007 4 24 QXEA200700638 4 20070418 A 3425 AHRS BOMBDR DHC8 DHC8402 1390042 NM NR 1 OUT OF ALIGNMENT A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 403QX 4037 LAX FLIGHT NR 2420: AFTER PUSH BACK, ELEVATOR FEEL CAUTION ILLUMINATED AND FO'S PFD AND 'ATT FAIL', 'HDG FAIL' AND 'IHSI FAIL' MESSAGES. AIRCRAFT RETURNED TO GATE. MAINTENANCE REALIGNED NR 1 AND NR 2 AHRS. NO MESSAGES DISPLAYED ON NR 1 O R NR 2 PFD. NO ASSOCIATED CAUTION OR WARNING MESSAGES. INSPECTED NOSE GEAR AND TO BAR LUGS. NO DISCREPANCIES FOUND. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007042400261 20070424 00261 NM 2007 4 24 USAA070277 1 20070412 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 BS 867; 2 INCHES LEFT & 2 INCHES RIGHTT OF S-1 HAS CRACK. INSTALLED REPAIR DOUBLER (CHANNEL) PER TR 54-10-14C, DEFECT S IZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007042400262 20070424 00262 2007 4 24 MALA070052 2 20070421 A 7497 CONNECTOR SAAB SF340 340B 7860101 EU NR 2 ENGINE LOOSE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 452XJ 340B452 DURING CRUISE FLIGHT, THE FLIGHT CREW EXPERIENCED ILLUMINATION OF AN ENGINE IGNITION LIGHT ALONG WITH ENGINE POWER ROLL- BACK (TORQUE). IGNITION LIGHT ON NR 2 ENGINE ILLUMINATED TWICE AT 11000 FT (NO ICING CONDITION AT ALL) TORQUE AT ONE PO INT WENT TO 10 PERCENT + IGNITION LIGHT EXTINGUISHED. THIS OCCURRED ONCE OR TWICE MORE DURING DESCENT. THE FLIGHT RETU RNED TO DEW AND LANDED. DURING RADIO COMMUNICATION WITH PILOT, NOTED NO CHANGE IN FLIGHT CHARACTERISTICS OR CHANGE IN S OUND OF ENGINE DURING SAID EVENTS. PERFORMED PRE CHECK RUN OF ENG NO DISCREPANCY NOTED. PERFORMED PRE CHECK RUN OF ENG INE NO DISCREPANCY NOTED. PERFORMED CONTINUITY CIRCUIT CHECK OF ECU IAW GE MM 72-00-00 ENGINE TESTING NO DISCREPANCY NO 2 L 7 2 4T RT A52EU 2007042400263 20070424 00263 WP 2007 4 24 IXXA07SMN113S 1 20070223 A 5340 FITTING DOUG DC8 DC862F 3021972 WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING FRAME CRACKED AT STATION 759.000, LONGERON 18 RI GHT. REMOVED FASTENERS AS NEEDED TO PERFORM THE REPAIR. PERFORMED STOP HOLE ON CRACK END. PERFORMED NDT INSPECTION. NO CORROSION OR CRACK PROGRESSION FOUND. FABRICATED (HORIZONTAL FLANGE) (VERTICAL FLANGE). PERFORMED HEAT TREATMENT. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW FAA FORM 8110-3 NUMBER 07058 DATED 02-15-07, SEMAN DRAWING NUMBER ED-4462 DATED 02-13-07, AND EO SEMAN NUMBER 2007219 DATED 02-15-07, DC8 SRM 5 1-1-20D, DC8 SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, FORM SEMAN 242-2, DC8 SRM 51-1-1 PAGES 1, 13, 17, DC8 SRM 51-1-8 2 L 7 4 4F 4A25 2007042400264 20070424 00264 NM 2007 4 24 NWAA071316717 1 20070316 A 5230 SKIN BOEING 747 747251F 1384898 NM CARGO DOOR DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 617US 21121 DURING THRU FLIGHT NRT MAINTENANCE, FOUND MAIN DECK SIDE CARGO DOOR SKIN DAMAGE AT FORWARD LOWER ACCESS DOOR. REPAIRED PER EA 67-208937. 2 L 7 4 4F A20WE 2007042400265 20070424 00265 WP 2007 4 24 NWAA071309984 1 20070409 A 2910 LINE DOUG DC9 DC932 3022066 WP HYDRAULIC SYS FAILED A NWAA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 984US 47383 THE RIGHT HYDRAULIC SYSTEM HAD A COMPLETE LOSS OF FLUID AND PRESSURE AS THE AIRCRAFT CLIMBED THROUGH 13,000 FEET. COM P ROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT CONTINUED TO A NORMAL SAFE LANDING AT THE SCHEDULED DESTINATION. MAINTENA NCE FOUND A HYDRAULIC LINE HAD FAILED AND REPLACED IT. ALSO, REPLACED THE ENGINE DRIVEN PUMP, THE ELECTRIC PUMP, AND AL L ASSOCIATED FILTERS. THE SYSTEM WAS SERVICED AND LEAK CHECKED AND THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007042400267 20070424 00267 NM 2007 4 24 USAA070275 1 20070412 A 5754 65C26603102A SKIN BOEING 737 737401 1384701 NM L/E SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 INBOARDD SIDE OF NR 4 SLAT, UPPER SIDE OF WEDGE PANEL DELAMINATED. INSTALLED NEW CORE & SKIN PER SRM 57-43-02, 51-70-10 , DEFECT SIZE: 3 INCHES. 2 L 7 2 4F RT A16WE 2007042400269 20070424 00269 NM 2007 4 24 USAA070273 1 20070412 A 5320 SUPPORT ANGLE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 STA 360 AT S8L HAS CRACK. REMOVED & MADE NEW ANGLE PER SRM 51-10-02 BOEIGN DWG 69-48985, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007042400271 20070424 00271 NM 2007 4 24 USAA070271 1 20070412 A 5320 654534256 INTERCOSTAL BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 INTERCOSTAL CORRODED AT FLOORBOARD HOLES 1 INCH AREA. REMOVED & REPLACED INTERCOSTAL PER SRM 51-10-02; CORROSION LEVEL 2; TASK C53-107-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007042400273 20070424 00273 EA 2007 4 24 VNAA0704002 1 20070405 A 2740 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT DIRTY A VNAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 05 218PS 7885 CREW REPORTED THE STAB AND MACH TRIM FAILED ON TAKEOFF. CREW ELECTED TO RETURN TO CHO AND LANDED WITHOUT INCIDENT. MAI NTENANCE INSPECTED THE F/O'S CONTROL WHEEL. MAINTENANCE CLEANED THE HORIZONTAL STAB TRIM SWITCHES ON F/O'S CONTROL WHEE L. MAINTENANCE PERFORMED OPERATIONAL TESTS OF THE HORIZONTAL STAB TRIM SYSTEM IN ACCORDANCE WITH THE AIRCRAFT MAINTENAN CE MANUAL 27-40-00-710-801. OPS TESTS GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007042400274 20070424 00274 EA 2007 4 24 VNAA0704006 1 20070413 A 5730 WINGLET CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE RT WING LIGHTNING STRIKE A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 723PS 10181 CREW REPORTED A LIGHTNING STRIKE UPON POST FLIGHT INSPECTION. MAINTENANCE PERFORMED AN EN ROUTE LIGHTNING STRIKE INSPEC TION. MAINTENANCE INSPECTED AND FOUND DAMAGE TO THE RIGHT HAND WINGLET. MAINTENANCE REPAIRED ALL DAMAGE. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007042400276 20070424 00276 WP 2007 4 24 070096 1 20070408 A 2750 106010 SWITCH DOUG DC9 DC983 3022083 WP SLAT/FLAPS MALFUNCTIONED A WX0A O OTHER J WARNING INDICATION AP APPROACH 1 WP 19 865GA 49998 FLIGHT 485 BIL/LAS, THE FLIGHT CREW REPORTED THAT THE AUTOSLAT FAIL ANNUNCIATOR ILLUMINATED ON APPROACH WHEN FLAPS 15 WA S SELECTED. LAS VEGAS MAINTENANCE REPORT THAT TROUBLESHOOTING REVEALED FLAP/SLAT POSITION SWITCH S1-467 HAD FAILED. LA S VEGAS FURTHER REPORT THE REMOVAL AND INSTALLATION OF THE FLAP/SLAT POSITION SWITCH AT THE FLAP SELECT LEVER PER AMM 27 -80-07. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 27-80-07. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007042400277 20070424 00277 WP 2007 4 24 070097 1 20070413 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 864GA 49912 DURING A ROUTINE OVERNIGHT SERVICE CHECK MAINTENANCE INSPECTION LAS VEGAS MAINTENANCE REPORTED THAT THE CEILING EMERGENC Y LIGHTS AT SEATROWS 21 THRU 24 WOULD NOT TEST. LAS VEGAS FURTHER REPORT THE REMOVAL AND REPLACEMENT OF THE EMERGENCY L IGHT POWER SUPPLY BATTERY PACK AT FUSELAGE STATION 901. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED. THE AIRPLAN E HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007042400278 20070424 00278 NE 2007 4 24 HALA0700168 2 20070411 A 7230 FAN BLADE BOEING 767 767300 1385204 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE DAMAGED A HALA K NONE C F.O.D. IN INSP/MAINT 1 WP 13 586HA 24259 NR 1 ENG 1ST STAGE FAN BLADE NR 8 HAS A NICK IN THE LEADING EDGE 17" FROM BLADE TIP 1/16" DP BY 1/8" WD. REPAIRED NR 8 FIRST STAGE FAN BLADE BY BLENDING PERAMM 72-31-02. 2 L 7 2 4F 4 F RT A1NM E24NE 2007042400279 20070424 00279 NM 2007 4 24 ASAA0741585 1 20070420 A 5312 65C27308126 SUPPORT ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 AFT CARGO PIT RIGHT BULKHEAD PANEL LWR SUPPORT ANGLE LWR SURFACE CORRODED. CORRODED SUPPORT ANGLE REPLACED WITH FABRICA TED REPAIR PART IAW SRM 51-30-01, 51-40-02, 51-40-05. 2 L 7 2 4F RT A16WE 2007042400280 20070424 00280 NM 2007 4 24 HALA0700167 1 20070412 A 3610 UNKNOWN BOEING 767 767300 1385204 NM PHEUMATIC SYS UNKNOWN A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 592HA 33468 ETOPS SIGNIFICANT SYSTEM, LEFT PNEUMATIC SYSTEM IS NOT BEING PRESSURIZED BY L ENG. CYCLED L ENG VALVE SWITCH AND L PNEU MATIC SYSTEM OPERATES NORMAL PER FIM 36-10-00 FIG 115 SHEET 1. 2 L 7 2 4F RT A1NM 2007042400281 20070424 00281 NM 2007 4 24 HALA0700169 1 20070412 A 3010 ANTI-ICE SYSTEM BOEING 717 717200 1383700 NM WING UNKNOWN A HALA O OTHER N FALSE WARNING CR CRUISE 1 WP 13 479HA 55124 WING ICE LEFT FAIL. CHECKED PNEUMATIC BOX CLEARED ANTI-ICE MSG. OK TO CONTINUE. 2 L 7 2 4F TR A6WE 2007042400282 20070424 00282 WP 2007 4 24 IXXA07SMN100S 1 20070208 A 5753 SKIN DOUG DC8 DC862 3021970 WP ZONE 500 MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING, OUTBORD FLAP UPPER SKIN NON STANDARD REPAIR, AT STATION XF 210.000. REMOVED PANEL PLATING WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKINS AND INTERNAL DOUBLER. BONDED PARTS AS N EEDED WITH HYSOL. CLEANED, TREATED AND PRIMED PANEL PLATING INTERNAL PART AND AREA. APPLIED SEALANT TO FAYING SURFACES . INSTALLED REPAIR PARTS FROM STATION XF 210.000 IAW DC8 SRM 57-7-1 FIGURE 4 PAGE 2 TR NUMBER 57-94 DATED 10-01-02, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 57-7-1 FIGURE 4 PAGE 6 ITEM "P"AND "Q, DC8 SRM 51-1-9 TR NUMBER 51-142 DATE D 04-05-06,DC8 SRM 51-18B, DC8 SRM 51-1-11, AND DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 2007042400283 20070424 00283 WP 2007 4 24 IXXA07SMN102S 1 20070208 A 5753 SKIN DOUG DC8 DC862 3021970 WP ZONE 500 BROKEN B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP, UPPER SKIN BROKEN AT STATION XCW 64.000. REMOVED DAMAG ED PANEL PLATING. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND P RIMED AREA AND PANEL PLATING INTERNAL PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN AND REPAIR PARTS I AW DC8 SRM 57-7-1 FIGURE 1 PAGE 2, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 57-7-1 FIGURE 1 PAGE 2 ITEM "A"AND "L " DC8 SRM 51-1-9 TR NUMBER 51-142 DATED 04-05-06, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND DC8 SRM 51-1-21, DC8 SRM 51-1-21 A. 2 L 7 4 4F 4A25 2007042400284 20070424 00284 WP 2007 4 24 IXXA07SMN103S 1 20070208 A 5730 SKIN DOUG DC8 DC862 3021970 WP RT WING MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD LEADING EDGE OUTER SECTION HAS A NON STANDARD REPAIR, BETW EEN STATION XFS 710.000 AND XFS 716.250. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT IN SPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 071 10 DATED 03-14-07, SEMAN DRAWING NUMBER ED-4454 DATED 02-19-07 AND EO SEMAN NUMBER 2007198 DATED 03-14-07, DC8 SRM 51-1- 21, DC8 SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, FORM SEMAN 242-2, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-20D, 2 L 7 4 4F 4A25 2007042400285 20070424 00285 NM 2007 4 24 DLM88070330 1 20070416 A 3213 SCHRADER VALVE DOUG MD88 MD88 3023688 NM NLG STRUT DAMAGED A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 990DL 53342 AFTER GEAR RETRACTION A SEVERE VIBRATION CAME FROM NOSE GEAR AREA WITH NORMAL GEAR INDICATION/LIGHT IN COCKPIT. NOSE GE AR STRUT FLAT ON RETURN TO GATE. REMOVED AND REPLACED NLG STRUT SCHRADER VALVE AND COMPLETED SERVICING PER AMM 32-21-02 . COMPLETED NLG T/S PER OPN 50006. CKS GOOD. 2 L 7 2 4F RT A6WE 2007042400288 20070424 00288 NM 2007 4 24 F3LA200700052 1 20070330 A 5347 BUSHING AIRBUS A319 A319111 3930336 NM SEAT TRACK BROKEN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C-4/S1 CHECK, INSPECTION REPORTED LT SIDE FLOOR EXPANSION JOINT AT FRAME 35 HAD BROKEN BUSHING ON BOTH SEAT TRACK BEAMS. REPLACED BOLTS AND BUSHINGS IN THE EXPANSION JOINTS AT FS 35 ON THE LT SIDE SEAT TRACKS IAW A319 SRM 51-42-11. 2 L 7 2 4F RT A28NM 2007042400289 20070424 00289 NM 2007 4 24 F3LA200700051 1 20070330 A 5347 BUSHING AIRBUS A319 A319111 3930336 NM SEAT TRACK BROKEN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 1684 DURING C4/S1 CHECK, INSPECTION REPORTED RT SIDE FLOOR EXPANSION JOINT AT FRAME 35 HAD BROKEN BUSHING ON BOTH SEAT TRACK BEAMS. REMOVED AND REPLACED PLASTIC BUSHINGS ON BOTH RT SEAT TRACKS EXPANSION JOINTS AT FS 35 IAW A319 SRM 51-42-11, PA RA 5. 2 L 7 2 4F RT A28NM 2007042400290 20070424 00290 GL 2007 4 24 DL764070309 2 20070407 A 7320 LINE BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 2 ENGINE LEAKING A DALA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SO 27 838MH 18628 29711 704952 RT ENG FUEL FILTER LIGHT ON CLIMB ALL PARAMETERS NORMAL. REPLACED NR 2 ENG FUEL FILTER ALSO FOUND PRESSURE SW LINE M P/ N 1836M35G01 LEAKING. REPLACED SAME. OPS AND LEAK CKS OK. 2 L 7 2 4F 4 F RT A1NM E23EA 2007042400291 20070424 00291 NE 2007 4 24 DL76G070310 2 20070408 A 7261 PACKING BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 ENGINE DAMAGED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 1603 31093 29695 704823 NUMBER 2 ENGINE HAD A LOSS OF OIL AND OIL PRESSURE. IFSD WAS CARRIED OUT PER CHECKLIST AND DIV TO DUB PERFORMED. MTC F OUND PMA STATOR HOUSING COMING OUT OF GEARBOX CAUSING OIL LOSS EVALUATING DAMAGE. VISUALLY INSP NR 2 ENG FOUND PMA GEAR PACKAGE MOUNT PAD CRACK AT G/B, REMOVED PMA AND GEAR PACKAGE FOUND 2 G/B INSERTS LOO. REMOVED AND REPLACED B/B INSERTS PER MM 479849. INSTALLED NEW GEAR PACKAGE AND STATOR PER AMM RAN NR 2 ENG AT POWER PER AMM. NO LEAKS NOTED 416321. C W CDF1603-040907, 416321 ENG CHANGED ITEM 17. 2 L 7 2 4F 4 F RT A1NM E13NE 2007042400292 20070424 00292 NM 2007 4 24 DLM88070311 1 20070410 A 5743 FITTING DOUG MD88 MD88 3023688 NM MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 945DL 49818 DURING CURRENT VISIT, CORROSION WAS FOUND AT THE LHS MLG SUPPORT FITTING AT THE BORE FOR THE RETRACT CYLINDER. THE CORR OSION WAS REMOVED BY OVERSIZING THE HOLE AND INCREASING THE DEPTH OF THE BORE, AND WAS APPROVED BY BOEING, WHO ISSUED AN AMOC FAA FORM 8100. REPAIR IS DOCUMENTED IN ERA 460860-14AD. 2 L 7 2 4F RT A6WE 2007042400293 20070424 00293 2007 4 24 DL76G070312 4 20070411 A 2330 7002086001 PROJECTOR BOEING 767 7673P6 1385105 NM CABIN OVERHEATED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 153DL 24985 FLT CREW REPORTED THE FIRST CLASS OVERHEAD PROJECTOR, OVERHEATED WITH WHITE SMOKE AND BURNT ELECT SMELL. USED HALON FIR E BOTTLE TO EXTINGUISH ONBOARD AMT DEACTIVATED AND REMOVED PROJECTOR TO ENSURE FIRE WAS EXTINGUISHED. INSTALLED FWD VID EO PROJ. MID PROJ PREVIOUSLY REPLACED WITH PROJ PER EA 01-461217-14 AND FWD POSITION EMPTY. MCO AND P REMOVED. DEFEC TIVE PROJ REMOVED AND DELIVERED TO HANGAR FRO DESK FOR QUARANTINE. 2 L 7 2 4F RT A1NM 2007042400294 20070424 00294 NM 2007 4 24 DL764070313 1 20070411 A 2760 285T0017201 POWER SUPPLY BOEING 767 767432ER 1385134 NM SPOILERS OVERHEATED A DALA D RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 842MH 29715 AFTER PUSH BACK, SPOILER LIGHT ILLUMINATED. SPOILER EICAS ADVISORY MESSAGE RECEIVED. RESET CSEU POWER SUPPLY MODULE. ERASE MSG AND GOIN OUT SPOILER LIGHT IN OVERHEAD PANEL. NOW GOOD FOR FLIGHT CKD OPS OK. 2 L 7 2 4F RT A1NM 2007042400295 20070424 00295 NM 2007 4 24 ASAA0741588 1 20070420 A 5320 69353642 TIE CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 TIE CLIP CORRODED. REPLACED TIE CLIP WITH FABRICATED REPAIR PART IAW SRM 51-40-02 AND 51-40-05. 2 L 7 2 4F RT A16WE 2007042400296 20070424 00296 NM 2007 4 24 DL76G070314 1 20070411 A 3610 LINE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 ENGINE DISCONNECTED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 1603 29695 704750 ON T/O ROLL AT 70KTS, HAD R ENG PRV CAUTION MESSAGE AND BEEPER. ABORTED T/O. FOUND SENSE LINE FROM PRC DISCONNECTED. SECURED LINE. 2 L 7 2 4F 4 F RT A1NM E13NE 2007042400298 20070424 00298 NM 2007 4 24 AWXA200700503 1 20070419 A 5320 143N51974 INTERCOSTAL BOEING 757 7572S7 1384962 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - CRACKED CABIN INTERCOSTAL ANGLES, BS 660, S17L, WL 208. REPLACED CABIN INTERCOSTAL ANGLES, BS 660, S17L, WL 208 I AW B757-200 SRM 51-40-02 AND 51-30-01. 2 L 7 2 4F RT A2NM 2007042400299 20070424 00299 WP 2007 4 24 IXXA07SMN112S 1 20070223 A 5753 SKIN DOUG DC8 DC862F 3021972 WP ZONE 600 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING, INBOARD FLAP LOWER PANEL HAS A NON STANDARD REPAIR, AT STATION XW 3 .000 TO XW 50.000. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED P ARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INS TALLED REPAIR PARTS IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-7-1 FIGURE 1 PAGE 2 ITEM "B"AND "L", DC8 SRM 51-1-9 TR NUMBER 51-142 DATED 04-05-06, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 2007042400300 20070424 00300 WP 2007 4 24 IXXA07SMN108S 1 20070223 A 5753 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP LOWER SKIN HAS A NON STANDARD REPAIR AT STATION WX 84.00 0. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. FABRICATED NW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALL ED REPAIR PARTS IAW DC8 SRM 57-2-5 FIGURE 1 SHEET 1 AND 2, DC8 SRM 51-1-21,DC8 SRM 57-7-1 FIGURE 1 ITEM "B" AND "L", DC8 SRM 51-1-9 TR NUMBER 51-142 DATED 04-05-06,DC8 SRM 51-1-8B, AND DC8 SRM 51-1-11. 2 L 7 4 4F 4A25 2007042400301 20070424 00301 NM 2007 4 24 ASAA0741590 1 20070420 A 5320 6517684Y642 INTERCOSTAL BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 INTERCOSTAL CRACKED. CRACKED INTERCOSTAL REPLACED WITH NEW PART IAW SRM 51-40-05 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007042400306 20070424 00306 NM 2007 4 24 ASAA0741595 1 20070420 A 5311 6545808244 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 FRAME CRACKED AT 37L INTERCOSTAL ATTACHMENT HOLE. FRAME REPAIRED IAW EA 5310 02714. 2 L 7 2 4F RT A16WE 2007042400308 20070424 00308 NM 2007 4 24 ASAA0771600 1 20070420 A 5315 141A5505 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 FLOORBEAM AT STA 344 UPPER FLANGE CORRODED REPAIRED IAW 5310 02716. 2 L 7 2 4F RT A16WE 2007042400310 20070424 00310 WP 2007 4 24 IXXA07SMN104S 1 20070208 A 5753 VANE DOUG DC8 DC862 3021970 WP ZONE 600 DAMAGED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE SLOT VANE HOLES ELONGATED, BETWEEN STATION XOLDI 6.225 AND XS 435.789. REMOVED EXISTING INTERNAL DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK O R CORROSION FOUND. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLI ED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 07042 DATED 02-07-07, SEMAN DRAWING NU MBER ED-4458 DATED 02-02-07, EO SEMAN NUMBER 2007209 DATE 02-07-07, DC8 SRM 51-1-21, DC8 SRM 51-3-0, SEMAN DRAWING NUMBE R ED-4458,DC8 NDT SPM PART 06-10-01-001, FORM SMN 242-2, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-20D, AND DC8 SRM 2 L 7 4 4F 4A25 2007042400311 20070424 00311 NM 2007 4 24 07FDEA01508 1 20070416 A 5347 ADA83891 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 CABIN SEAT TRACK CROWN AREA FOUND CHIPPED OFF AT STA 899 X = -47. CABIN SEAT TRACK AT STA 899 X= -47 CARRIED OUT REPAIR AS PER SRM 53-70-00 VOL I FIG 1. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007042400312 20070424 00312 2007 4 24 DL76G070317 4 20070411 A 2330 7002086001 PROJECTOR BOEING 767 7673P6 1385105 NM PWA 4060 PW4060 52119 NE FWD CBN OVERHEATED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 153DL 24985 724655 MID CABIN PROJ OVERHEATED WITH WHITE SMOKE AND ELECTRICAL ODOR. INSTALLED FWD VIDEO PROJ. MID PROJ PREVIOUSLY REPLACED WITH PROJ PER EA 01-461217-14, AND FWD POSITION EMPTY. MCO AND P REMOVED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007042400313 20070424 00313 NM 2007 4 24 DL76L070320 1 20070414 A 8011 774860A4 STARTER BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE SPARKS A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 197DN 28454 727620 DURING TAXI AND START OF RT ENG, HAD NO ROTATION AND SPARKS FROM STARTER AREA AFTER START VALVE OPENED. STARTER FAILED AND ALSO DAMAGED THE START VALVE. REPLACED STARTER AND START VALVE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007042400314 20070424 00314 NM 2007 4 24 DL76L070321 1 20070414 A 3030 7705401 RELAY BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE UNKNOWN A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 173DN 24800 724142 LT ENG EEC MODE STATUS. REPLACED K402 RELAY FOR THE LT ENG PROBE HEAT. RAN ENG, OP CKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007042400315 20070424 00315 NM 2007 4 24 DL76L070322 1 20070414 A 2530 COFFEEMAKER BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE AFT GALLEY SMOKE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 196DN 28453 724142 AFT COFFEE MAKER ON CAPT'S SIDE PRODUCED SMOKE WHEN TURNED ON. SMOKE QUIT WHEN COFFEE MAKER WAS TURNED OFF. CB'S WERE PULLED. RESET C/B FOR AFT COFFEE MAKER. MADE A POT OF COFFEE FROM EACH. ALL CKS OK. NO SMOKE NOTED AT ANY TIME. 2 L 7 2 4F 4 F RT A1NM E24NE 2007042400316 20070424 00316 NM 2007 4 24 DL76L070323 1 20070414 A 7714 731703160 CIRCUIT CARD BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE ENGINE SPEED UNKNOWN A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 175DN 24803 724142 AFTER STARTING, THE RIGHT CENTER PUMP PRESS LIGHT ILLUMINATED WITH THE RIGHT CTR PUMP ON. REMOVED AND REPLACED THE RT E NG SPEED CARD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007042400318 20070424 00318 NE 2007 4 24 DL76L070325 2 20070414 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 UNKNOWN A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 195DN 28452 724639 L ENGINE WOULD NOT START. MANUAL OVERRIDE START PROCEDURE PERFORMED. FWD TO MCO PER MEL 80-00-02. CREW REPORTS GOOD S TART AT JFK. INSPECTED VLV AND CONNECTOR CHKS GOOD. RAN AND SPUN ENG SEVERAL TIMES CHKS OK MCO AND P REMOVED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007042400319 20070424 00319 NM 2007 4 24 QXEA200700631 1 20070412 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - 3 RIVETS IN RIGHT HAND OUTBOARD FLOOR SUPPORT AT SEAT TRACK NR 10 FRAMES X355.95 AND X370.9 DO NOT HAVE BUCKTAI LS SHOT TO COVER HOLES. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007042400320 20070424 00320 NM 2007 4 24 QXEA200700632 1 20070413 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 205 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - DENT IN RIGHT EXTERIOR FUSELAGE AT STATION 205.3, 7 1/2" BELOW LAV SERVICE DOOR. REPAIRED IAW RD8-53-5384 AND RD8-53-9559, SRM 51-20-16, 51-20-46, AND 51-20-51. 2 H 7 2 4T RT A13NM 2007042400321 20070424 00321 NM 2007 4 24 QXEA200700633 1 20070413 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - DENT IN RIGHT EXTERIOR FUSELAGE AT STATION 218.3 7 1/2" BELOW LAV SERVICE DOOR. REPAIRED IAW RD8-53-5384, RD8- 53-9559, SRM 51-20-11, 51-20-16, 51-20-46, AND 51-20-51. 2 H 7 2 4T RT A13NM 2007042400322 20070424 00322 NM 2007 4 24 QXEA200700634 1 20070412 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 310 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX- NR 10 SEAT TRACK HAS CORROSION AT STATION 310. REPAIRED IAW SRM 51-40-00, 51-40-11, AND RD8-53-1342. 2 H 7 2 4T RT A13NM 2007042400323 20070424 00323 NM 2007 4 24 QXEA200700635 1 20070412 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 434-387 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - CABIN SEAT TRACK NR 1 HAS SCRATCHES AT STATION X434-X456, X379-X387. REPAIRED IAW RD8-53-1342 AND SRM 51-40-11 , 51-40-00. 2 H 7 2 4T RT A13NM 2007042400324 20070424 00324 NM 2007 4 24 QXEA200700636 1 20070108 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSLEAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - SUSPECT CORROSION ON FRAME SKIN FLANGE RIVET TAILS BETWEEN STRINGER 31P AND 30P AT FRAME X136.8. REPAIRED IAW SRM 51-40-11, 51-20-16, 51-20-36, AND 51-20-51. 2 H 7 2 4T RT A13NM 2007042400325 20070424 00325 NM 2007 4 24 QXEA200700637 1 20070408 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - CORROSION FOUND ON SKIN SPLICE RIVITS BETWEEN STRINGERS 29P AND 28P FROM STATION X136.8 TO X151.6. REPAIRED IA W SRM 51-40-11, 51-20-16, 51-20-36, AND 51-20-51. 2 H 7 2 4T RT A13NM 2007042500001 20070425 00001 NM 2007 4 25 ASAA0771598 1 20070420 A 5320 145A750323 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 AFT PIT FLOOR SUPPORT CORRODED AT STA 772 REPAIRED IAW EA5320 01799. 2 L 7 2 4F RT A16WE 2007042500003 20070425 00003 NM 2007 4 25 ASAA0771601 1 20070422 A 5320 143A81225 SILL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 FWD CARGO DOOR LOWER SILL WEB IS CORRODED REPAIRED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007042500004 20070425 00004 NM 2007 4 25 ASAA0771602 1 20070422 A 5320 146A81236 SILL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 AFT CARGO DOOR LOWER SILL WEB IS CORRODED REPAIRED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007042500005 20070425 00005 EU 2007 4 25 UPS07149655 1 20070409 A 5330 SKIN AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 147UP 0830 INSPECTION TYPE:2C DENT IN LT FUSELAGE FWD OF CAPTS STBY PITOT TUBE. COMPLIED EA 300-5330-01-H0782 AND RAS 051472/014/2 007 (WITH FATIGUE/ /DAMAGE TOL. JUST, DOC:TBD WITHIN 6 MONTHS). 2 L 7 2 4F RT A35EU 2007042500009 20070425 00009 NM 2007 4 25 UPS07549650 1 20070328 A 5311 143N1024116 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 419UP 23906 INSPECTION TYPE:C DENT IN FWD CARGO FUSELAGE FRAME STA 680, BETWEEN S24R TO S25R. COMPLIED WITH EA 757-5332-27-A1630 & UPS EO B757-5310-26604-A. 2 L 7 2 4F RT A2NM 2007042500010 20070425 00010 NM 2007 4 25 DL757070332 1 20070417 A 5412 311N32712 BULKHEAD BOEING 757 757232 1384965 NM NR 1 PYLON TOOL DAMAGE A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 637DL 23760 DURING ACCOMPLISHMENT OF EA 06-070332-03AD (SIP MOD), A HOLE WAS DAMAGED BY A BROKEN DRILL BIT ON THE NR 1 PYLON AFT BUL KHEAD. THE DAMAGE REQUIRED THE HOLE TO BE OVERSIZED TO 0.640 AND OVERSIZED FASTENER INSTALLED PER BOEING APPROVAL, AS D ETAILED IN ERA 460837-14AD. 2 L 7 2 4F RT A2NM 2007042500014 20070425 00014 NM 2007 4 25 DL76G070336 1 20070417 A 2420 729825B IDG BOEING 767 767332 1382001 NM LEFT MALFUNCTIONED A DALA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 173DZ 29692 WHEN PUSHING UP THROTTLES FOR T/O LEFT GEN DROPPED OFF, LT BUSS ISOLATION AND TRU MESSAGE. RETURNED TO BLOCKS. MTC IN PROGRESS. SWAPPED TO 1601. MEGGED FEEDER CABLES CKD OK. CHANGED IDG. RAN ENG UP TO 90 PCT N1. LOADED GEN TO 75 PCT LOAD. ALL OPS NORMAL, NO FAULTS. 2 L 7 2 4F RT A1NM 2007042500017 20070425 00017 NM 2007 4 25 DLM88070339 1 20070418 A 3213 STRUT DOUG MD88 MD88 3023688 NM NLG BINDING A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 933DL UNK 49720 AIR TURN BACK AFTER TO WHEN GEAR HANDLE RAISED NOSE GEAR RED UNSAFE LIGHT REMAINED ON WITH NOISE AND VIBRATION FOLLOWED QHR PRODECURE RETURNED TO LGA. MAINTENENCE IN PROGRESS JACKED A/C VISUAL CK NOSE GEAR FOUND RT AFT DOOR ROD BINDING REM OVED DOOR ROD AND NOSE PISTON/CYL ASSY. REPLACED NOS STRUT SEALS PER MM. REPLACED RT AFT DOOR ROD INSTALLED PISTON/C YL ASSY SER NOSE STRUT PER MM SWUNG GEAR. OPS CK GOOD DOWN JACKED A/C. 2 L 7 2 4F RT A6WE 2007042500018 20070425 00018 NM 2007 4 25 UPS07549652 1 20070327 A 5311 146N102886 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 419UP 23906 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1340 S26R. COMPLIED WITH WA 757-5362-27-A1627 & UPS EO B757-5310 -23593-A. 2 L 7 2 4F RT A2NM 2007042500020 20070425 00020 WP 2007 4 25 IXXA070022O 1 20070413 A 2697 CONNECTOR DOUG DC8 DC873F 302199F WP FIRE LOOP LOOSE A IXXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 11 602AL * 1757 45991 DURING FLIGHT FROM KTOL NUMBER 3 FIRE WARNING LIGHT AND FIRE WARNING BELL CAME ON. THE CREW ACCOMPLISHED ALL NECESSARY PROCEDURES AND LANDED WITHOUT INCIDENT IN KLAS. MAINTENANCE PERFORMED VISUAL INSPECTION ON THE NUMBER 3 ENGINE FOR FIRE , NO INDICATION OF FIRE FOUND. MAINTENANCE CHECKED THE FIRE LOOP FOR SHORT, ALL LOOPS CHECKED GOOD. INSPECTED PNEUMATI C LINES FOR RUPTURES, OR LOOSE CLAMPS, NONE FOUND. MAINTENANCE FOUND RIGHT FAN FIRE LOOP FORWARD CONNECTOR LOOSE IN BAC KSHELL. REPLACED CONNECTOR IAW DACO DC8 MAINTENANCE MANUAL 20-50-1. MAINTENANCE DID OPERATIONAL CHECK ON NUMBER 3 FIRE WARNING SYSTEM, AND CHECK WAS GOOD. MAINTENANCE REPLACED BOTH NUMBER 3 AND 4 HRD FIRE BOTTLE. AIRCRAFT RETURNED TO SE 2 L 7 4 4F RT 4A25 2007042500021 20070425 00021 NM 2007 4 25 UPS07549654 1 20070328 A 5311 143N1024115 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 419UP 23906 INSPECTION TYPE:C DENT IN FWD CARGO FUSELAGE FRAME STA 680, S23L. COMPLIED WITH EA 757-5332-27-A1633 & UPS EO B757-5310 -26602-A. 2 L 7 2 4F RT A2NM 2007042500022 20070425 00022 NM 2007 4 25 UPS07549657 1 20070331 A 5412 311N3271 BULKHEAD BOEING 757 75724APF 1384969 NM NR 1 PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 419UP 23906 INSPECTION TYPE:C NR 1 PYLON AFT BULKHEAD LOWER CORNER OUTBOARD SIDE CHAFED. COMPLIED WITH EA 757-5453-27-A1637 & UPS E O B757-5410-26607-A. 2 L 7 2 4F RT A2NM 2007042500025 20070425 00025 2007 4 25 UPS07849665 4 20070421 A 2565 SLIDE DOUG DC8 DC871F 302199D WP CREW DOOR OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:N/A CREW DOOR ESCAPE SLIDE PRESSURE INDICATOR IS BELOW VIEWING WINDOW. REPOSITIONED SLIDE SO THAT PRESS URE INDICATOR IS BETTER VISIBLE. 2 L 7 4 4F RT 4A25 2007042500029 20070425 00029 NM 2007 4 25 UPS07M49645 1 20070406 A 5330 AFA7057503 SKIN DOUG MD11 MD11F 3023600 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 272UP 48571 INSPECTION TYPE:3C TRANSFERRED FROM LOG PAGE 699901 ITEM 2; DMI D344991 FUSELAGE SKIN DENT AT STA 1661, BETWEEN L32R & L 33R. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR DOUBLERS IAW SAA EA 011-5330-01-A0795. 2 L 7 3 4F RT A22WE 2007042500030 20070425 00030 WP 2007 4 25 IXXA07SMN106S 1 20070208 A 5310 DOOR FRAME DOUG DC8 DC862 3021970 WP ZONE 800 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND EXTERIOR FUSELAGE "A" DOOR AFT LOWER JAMB CORNER CRACKED. REMOVED DAMAGED AREA . PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND, AFTER TRIM OUT. FABRICATED REPAIR DOUBLER AND REPAIR TRIPLER . CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW A D-2005-18-07, SB DC8-53-078, DRAWING DOUGLAS SR08530019 AND 5750776, DRAWING DOUGLAS SR08530019, DC8 NDT SPM PART 06-10- 01-001, FORM SMN 242-2, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-1-20D, AND DC8 SRM 51-3-1. 2 L 7 4 4F 4A25 2007042500031 20070425 00031 NM 2007 4 25 UPS07549632 1 20070327 A 5311 146N102886 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 419UP 23906 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1340, S26L. FRAME REPAIR AT STA 1340, S26L, ACCOMPLISHED PER FIN AL EA 757-5362-27-A1629, WITH NO DEVIATIONS AND PER UPS EO B757-5310-26558-A. 2 L 7 2 4F RT A2NM 2007042500032 20070425 00032 NM 2007 4 25 UPS07549633 1 20070328 A 5311 146N103090 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 419UP 23906 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1560, S26R. FRAME REPAIR AT STA 1560, S26R HAS BEEN ACCOMPLISHED PER EA 757-5362-27-A1634 WITH NO DEVIATIONS AND PER UPS EO B757-5310-26562-A. 2 L 7 2 4F RT A2NM 2007042500033 20070425 00033 NM 2007 4 25 QXEA200700627 1 20070416 A 3150 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM CAUTION LIGHT UNKNOWN A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 424QX 4006 SEA FLIGHT NR 2332: NR 2 PEC CAUTION LIGHT. AIRCRAFT RETURNED TO GATE. MAINTENANCE C/W FIM TASK 61-20-05-810-817 FOR F AULT CODE 200 FOUND IN CDS. FAULT CODE CLEARED. GROUND RAN NR 2 ENGINE. FAULT CODE DID NOT REOCCUR. NO PARTS REPLACE D. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007042500035 20070425 00035 NM 2007 4 25 UPS07649629 1 20070417 A 5610 WINDOW BOEING 767 76734AF 1385212 NM COCKPIT DEFECTIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 315UP 27743 INSPECTION TYPE:N/A CREW PREFLIGHT - CAPTAIN'S SIDING WINDOW HARD TO OPEN. A/C REMOVED FROM SERVICE. REMOVED AND REPLA CED L2 WINDOW PER 56-11-02-4. 2 L 7 2 4F RT A1NM 2007042500036 20070425 00036 NM 2007 4 25 QXEA200700628 1 20070416 A 3150 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM WARNING LIGHT UNKNOWN A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 401QX 4031 PDX FLIGHT NR 2359: A/F SELECT WOULD NOT ILLUMINATE ON ED. ILLUMINATED ON PUSH ON/OFF SWITCH. AIRCRAFT RETURNED TO GAT E. MAINTENANCE SELECTED A/F 3 TIMES. TEST PASSED. GROUND RAN BOTH ENGINES. TESTED A/F AND FOUND NO DEFECTS. MESSAGE ON ED DISPLAYED. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007042500040 20070425 00040 WP 2007 4 25 UPS07849627 1 20070324 A 5310 97549441 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 REMOVE STEEL DOUBLER FROM C-3(C-PIT) DOOR JAMB LWR FWD CORNER AND REPAIR PER DC8 SRM 53-2-0, FIG 22 A ND/OR DWG SRO8530019. REPAIRED DOOR CORNER IAW SAA EA 008-5310-01-A0755. 2 L 7 4 4F RT 4A25 2007042500042 20070425 00042 WP 2007 4 25 UPS07849628 1 20070329 A 5313 3648667 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 AIR CONDITIONING COMPT LONGERON CORRODED AT STA 45 L30R AND 5 INCH LONG CRACK STA 65. REMOVED AND RE PLACED LONGERON IAW SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2007042500043 20070425 00043 WP 2007 4 25 UPS07849630 1 20070414 A 3350 LIGHT DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:N/A BTB - AFTER TAXI, DIMMING LIGHTS NOTICED THAT EMERGENCY EXIT LIGHTING WAS ILLUMINATED IN THE ARMED P OSITION WITH A/C POWER ON AIRCRAFT. RESET C/B. OPS CHECK NORMAL PER AMM 33-50-01-2. 2 L 7 4 4F RT 4A25 2007042500044 20070425 00044 WP 2007 4 25 UPS07849631 1 20070330 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 HFEC INSP DETECTED A CRACK ON THE C-4 (D-PIT) LWR AFT DOOR JAMB CORNER STARTING AT FASTENER GOING FWD TO EDGE OF DOOR CUTOUT. CUT OUT DAMAGED AREA AT D-PIT LWR AFT DOOR JAMB CORNER (STA 1440) IAW SRM 53-2-0 FIG 21. FABR ICATED AND INSTALLED REPAIR TRIPLER, DOUBLER, AND FILLER AT D-PIT LWR AFT DOOR JAMB CORNER (STA 1440) IAW SRM 53-2-0 FIG 22 TR 53-188. 2 L 7 4 4F RT 4A25 2007092700390 20070927 00390 EU 2007 9 27 07FDEA04139 1 20070825 A 5230 BEAM AIRBUS 310 A310222 3930315 EU ZONE 800 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 419FE 345 PREVIOUS REPAIR FOUND LOCATED ON RT SIDE OF BULK DOOR BETWEEN BEAM 4 AND BEAM 5, STA 3620, FR67. REPAIR REQUIRES EVAL UATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND F OUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAIR WAS ACCOMPLISHED PER SRM 52-30-00. 2 L 7 2 4F RT A35EU 2007092800003 20070928 00003 NM 2007 9 28 SWAA074754 1 20070922 A 3397 8100022607 CONNECTOR BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 474WN 33861 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT MID CABIN. FOUND LOOSE CONNECTOR. SECURED CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2007092800006 20070928 00006 NM 2007 9 28 SWAA074798 1 20070925 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED HC1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007092800018 20070928 00018 NM 2007 9 28 SWAA074805 1 20070925 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 706 S3R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092800034 20070928 00034 NM 2007 9 28 SWAA074784 1 20070924 A 5322 6546569 SHEAR TIE BOEING 737 737317 138447P NM BS 967 S26R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED OTS CHECK, FOUND SHEAR TIE CORRODED AT BS 967, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007092800043 20070928 00043 NM 2007 9 28 2007UALA03738 1 20070915 A 3320 BALLAST BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY LIGHT FAULTY A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 657UA 27112 FWD GALLEY OVERHEAD LIGHT EMITTED ODOR WHILE ON BUT WENT AWAY. LEFT IT OFF FOR REMAINDER OF FLIGHT. 10-9-07 REPLACE D BALLAST M660, OP CHECKS OK.FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092800053 20070928 00053 NM 2007 9 28 2007UALA03751 1 20070917 A 2621 METERING VALVE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FIRE BOTTLE MALFUNCTIONED A UALA F ACTIVATE FIRE EXT. J WARNING INDICATION NR NOT REPORTED 1 WP 29 312UA 23673 THE 1ST BOTTLE DISCHARGE LIGHT IS ILLUMINATED ON CARGO DETECTOR SUPPRESSION PANEL. FOUND NR 1 BOTTLE DISCHARGED AND LIN E PRESSURIZED TO THE DIVERTER VALVE. REPLACED NR 1 FIRE BOTTLE AND METERING VALVE. ALL TESTED NORMAL AFTER MTC. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092800060 20070928 00060 NM 2007 9 28 2007UALA03758 1 20070918 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 SEAT 4E AFT EEL INOP. 10-19-07 RELAMPED SEAT EEL. OP CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092800084 20070928 00084 EU 2007 9 28 UPS07150697 1 20070920 A 2780 SLAT SYSTEM AIRBUS A300 A300F4622R 3930360 EU RT WING INOPERATIVE A IPXA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 01 128UP 0812 INSPECTION TYPE:N/A ON APPROACH INTO DEN, SLATS WILL NOT EXTEND; SYSTEM 1 & 2 FAULTS ON ECAM AND OVERHEAD AMBER LIGHTS. CREW DECLARED EMERGENCY AND LANDING WAS UNEVENTFUL. A/C IS CURRENTLY OOS. *SUPPLEMENTAL SDR* FOUND RT WING NR 1 SLAT JACKSCREW TORQUE LIMITER ACTIVATED. REMOVED AND REPLACED RIGHT NR 1 L/E SLAT ACTUATOR IAW 27-84-22-04. OPS & LEAK CHEC K GOOD. 2 L 7 2 4F RT A35EU 2007092800085 20070928 00085 NM 2007 9 28 UPS07450701 1 20070920 A 3350 POWER SUPPLY BOEING 747 747123 1384873 NM EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:N/A CREW SERVICE DOOR EMERGENCY SLIDE LIGHT INOP. REMOVED & REPLACED POWER SUPPLY MODULE X327 REF WD 33 -51-12 AND MM 33-51-04, OPS CHECK GOOD. 2 L 7 4 4F A20WE 2007092800093 20070928 00093 2007 9 28 2007UALA03765 4 20070918 A 3424 INDICATOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU STBY ATTITUDE INOPERATIVE A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 381UA 24656 FLIGHT DIVERTED DUE TO AN INOP STANDBY ATTITUDE INDICATOR AND ORD WEATHER RESTRICTIONS. FOUND INOPERATIVE STANDBY ATTIT UDE INDICATOR. REPLACED STANDBY ATTITUDE INDICATOR. REPLACED STANDBY ATTITUDE INDICATOR. TEARDOWN OF STANDBY ATTITUDE INDICATOR FOUND BAD REDUCTION GEAR ASSEMBLY. REPLACED ROTOR, ALL BEARINGS, AND REDUCTION GEAR ASSEMBLY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092800100 20070928 00100 NM 2007 9 28 2007UALA03772 1 20070918 A 3350 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 558UA 26654 AFT SECTION EEL LIGHTS REMAIN ON. 10-19-07 ON T/S FOUND NOSE GEAR TEST SWITCH INTERMITTENT. REPLACED NOSE EMERGEN CY TEST LIGHT SWITCH. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092800113 20070928 00113 NM 2007 9 28 KCSA071390 1 20070923 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 320 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 MAIN DECK SEAT TRACK CRACKED AT BS 320, LBL 12. 2 L 7 4 4F RT A20WE 2007092800114 20070928 00114 NM 2007 9 28 SWAA074806 1 20070925 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 706 S2R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092800122 20070928 00122 NM 2007 9 28 UPS07M50718 1 20070629 A 5414 COVER DOUG MD11 MD11F 3023600 NM TAIL PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C TAIL PYLON COVER BEHIND THE EXHAUST NOZZLE CRACKED (6 INCHES), STOPPED DRILLED, NUMEROUS RIVETS PULLED THRU IN LT AND RT SIDE, NEEDS REPLACEMENT. FPI C/O PER DAC NDTSPM R13 PT8 & MARKED OUT CRACK END. CRACK END STOP DRIL LED PER EN 1438-07. HFEC INSP C/O PER DAC NDTSPM R13 06-10-01.001, ON REWORKED AREA & FOUND NO CRACK. WELDING C/O ON C RACKED AREA PER EN 1438-07 ITEM 4 TO 7. FPI C/O PER DAC NDT SPM R13 PT08, NO CRACK FOUND ON WELD. GVI C/O ON REPAIR AR EA, NO CRACK FOUND. FAIRING AGE HARDENED. 2 L 7 3 4F RT A22WE 2007092800128 20070928 00128 NM 2007 9 28 KCSA071396 1 20070924 A 5411 SPAR BOEING 747 7472B4B 138481B NM NR 2 NACELLE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 NR 2 PYLON NAC STA 194 LOWER SPAR WEB CRACKED .75 INCH. 2 L 7 4 4F RT A20WE 2007092800131 20070928 00131 NM 2007 9 28 SWAA074698 1 20070919 A 3350 3017BPEGPL LAMP BOEING 737 737317 138447P NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007092800132 20070928 00132 NM 2007 9 28 SWAA074704 1 20070919 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 238WN 34713 DURING SCHEDULED HC2 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007092800133 20070928 00133 NM 2007 9 28 SWAA074708 1 20070919 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED HC1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 2 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007092800134 20070928 00134 NM 2007 9 28 SWAA074709 1 20070919 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 466WN 30677 EEPLS COVER LOOSE AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007092800135 20070928 00135 NM 2007 9 28 SWAA074705 1 20070919 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 251WN 32510 EEPLS COVER BROKEN AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007092800136 20070928 00136 NM 2007 9 28 SWAA074684 1 20070916 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM BS 421 S17R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 421, STR 17R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007092800141 20070928 00141 NM 2007 9 28 SWAA074689 1 20070919 A 5230 6549889 SKIN BOEING 737 7373A4 1384585 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO DOOR INNER SKIN CRACKED AT UPPER CENTER END. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007092800145 20070928 00145 NM 2007 9 28 SWAA074693 1 20070919 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 663 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092800146 20070928 00146 NM 2007 9 28 SWAA074690 1 20070919 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 663 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092800149 20070928 00149 NM 2007 9 28 SWAA074691 1 20070919 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 706 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092800170 20070928 00170 SO 2007 9 28 LR7A07095 1 20070917 A 5230 RAMPSKINLOWER SKIN LKHEED 382 382G 526414U SO RAMP DOOR CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 646 4590 DURING SCHEDULED B-2 CHECK, PER JOBCARD HB5301, FOUND RAMP DOOR BOTTOM EXTERIOR SKIN CRACKED FROM RS0.3 TO 1.7, BL 0. REPAIR CARRIED OUT USING 2024T3 .071" IAW SMP583 FIG 51-140-12. 2 H 7 4 4T A1SO 2007092800196 20070928 00196 EU 2007 9 28 TRAX200701358 1 20070904 A 5720 ANGLE AEROSP ATR72 ATR72 EU LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 LEFT WING BOX FAIRING, ANGLE AT RIB 4 FR 25 CRACKED. 2 H 7 2 4T RT 2007092800202 20070928 00202 NM 2007 9 28 2007UALA03695 1 20070913 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 287 SCRATCHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 LEFT SIDE OF UPPER FUSELAGE ONE INCH ABOVE STRINGER 3 AND ONE INCH AFT OF STA 287 HAS A SCRATCH .001 TO .003 DEEP AND AP PROXIMATELY ONE INCH LONG. MAJOR REPAIR ACCOMPLISHED: CUT DAMAGED AREA. ACCOMPLISHED NDT & INSURANCE CUT. FABRCIATED & INSTALLED EXTERNAL DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092800203 20070928 00203 NM 2007 9 28 2007UALA03795 1 20070919 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ODOR A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 543UA 25698 FLIGHT DIVERTED DUE TO ELECTRICAL ODOR. 10-23-07 MANUAL TEST OF EQUIP COOLING SYSTEM USING TEST SWITCH ON P61 PAN EL FOUND NO FAULTS. DID NOT DETECT ANY ODOR ON FURTHER INVESTIGATION. CAUSE OF DISCREPANCY COULD NOT BE ESTABLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007100100014 20071001 00014 SO 2007 10 1 C2XA07IA211 1 20070923 A 3350 3025103 LIGHT EMB 135 EMB135LR 3260305 SO FUSELAGE INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 28518 145334 IAH - DURING MAINTENANCE INSPECTION THE RT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND OVERWING EMERGENCY LIGHT ASSEMBLY, OPERATIONALLY TESTED WITH NO DEFECTS FOUND, AND T HE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007100100021 20071001 00021 NM 2007 10 1 KCSA071400 1 20070925 A 5411 FRAME BOEING 747 747122 1384872 NM NR 1 NACELLE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 NR 1 PYLON NAC STA 235 I/B FRAME CRACKED FWD OF ACCESS PANEL. 2 L 7 4 4F A20WE 2007100100025 20071001 00025 NM 2007 10 1 USAA920070856 1 20070926 A 5347 143N5090 SEAT TRACK BOEING 757 757225 1384959 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916UW 22192 PIT - MAJOR REPAIR - C-4 CHECK, CORROSION ON CABIN SEAT TRACK, BS 710, BS 740 AND BS 757, RBL45.5. REPAIRED CABIN SEAT TRACK, BS 710 - 757, RBL 45.5 IAW B757 SRM 53-00-02 AND 53-50-52. 2 L 7 2 4F RT A2NM 2007100100053 20071001 00053 NM 2007 10 1 MASA200700538 1 20070830 A 3350 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 988HA 426 F/A EMERGENCY LIGHTS DO NOT WORK. MX CHECKED SWITCH, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007100100058 20071001 00058 EA 2007 10 1 TRAX200701364 1 20070911 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 720EV 10115 COCKPIT AFT FLOOR LAND CORRODED. 2 L 7 2 4F RT A21EA 2007100100062 20071001 00062 EA 2007 10 1 TRAX200701368 1 20070917 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 870AS 7530 FLAPS FAIL MESSAGE, FLAPS FAIL AT 20 DEGREES. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007100100064 20071001 00064 NM 2007 10 1 07FDEA04352 1 20070927 A 5315 6516338283 FLOORBEAM BOEING 727 727233 138408A NM BS 950F CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 263FE 21625 AFT CARGO STA 950F LBL 44 MAIN DECK FLOORBEAM HAS CORROSION AROUND FASTENER HOLE. REMOVED AND REPLACED T-CAP IAW SRM 51 -30 AND SRM 27-53-034. 2 L 7 3 4F RT A3WE 2007100100069 20071001 00069 EU 2007 10 1 07FDEA04323 1 20070927 A 5315 A53974268200 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 FOUND CORROSION ON CROSSBEAM AT FRAME 58, AFT CARGO COMPARTMENT. CROSSBEAM SPLICE REPAIR PERFORMED IAW SRM 53-10-15/FIG 207/SEC F-F. 2 L 7 2 4F RT A35EU 2007100100072 20071001 00072 EU 2007 10 1 07FDEA04326 1 20070927 A 5311 A53989300 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 CORRODED ANGLE SEGMENTS AT FRAME 92 BETWEEN STGR 14 LT TO RT. REPAIR PERFORMED BY REPLACEMENT OF SEGMENTS IAW SRM 51-72 -10. 2 L 7 2 4F RT A35EU 2007100100073 20071001 00073 EU 2007 10 1 07FDEA04327 1 20070927 A 5330 A53970769200 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 724FD 530 OLD EXTERNAL DOUBLER REPAIR AT FUSELAGE SKIN BETWEEN FRAME 57.3-58, STGR 35-36 RT, NOT CONFORM TO SRM 53-10-12/FIG 225 O R 203. DOUBLER REPAIR RENEWED IAW SRM 53-10-12/FIG 225. 2 L 7 2 4F RT A35EU 2007100100078 20071001 00078 EU 2007 10 1 07FDEA04280 1 20070925 A 5320 A53980195202 RETAINER AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 HEAVY CORROSION ON SEAL RETAINER ON STR 26 BETWEEN FRAME 74-75 LT, LOWER PAX DOOR. REPLACEMENT OF SEAL RETAINER IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100083 20071001 00083 NM 2007 10 1 07FDEA04285 1 20070925 A 5340 654531310 STRINGER CLIP BOEING 727 727227 1384078 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 POOR WORKMANSHIP/CUSTOMER REQUEST, STRINGER TIE CLIP ON STR 2R AT FS 334 DAMAGED FROM MISDRILLED FASTENER HOLE REMOVED D AMAGED STRINGER CLIP. VERIFIED MATERIAL AND FABRICATED NEW STRINGER CLIP. TREATED AND PRIMED STRINGER CLIP, DRILLED UP AND INSTALLED NEW STRINGER CLIP REF SRM 51-10-2, BOEING PARTS LIST PL65-45313, BOEING DRAWING 65-45313, SRM 51-30-2 THI S IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007100100087 20071001 00087 NM 2007 10 1 07FDEA04289 1 20070925 A 5340 65453134 STRINGER CLIP BOEING 727 727227 1384078 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 POOR WORKMANSHIP, STRINGER TIE CLIP ON STR NR 1 AT FS 334 BENT/CRACKED CUSTOMER REQUEST REMOVED ELECTRIC BOX (FWD ENT RY LIGHT BALLAST). REMOVED DAMAGED CLIP. FABRICATED NEW CLIP REF BOEING DWG 65-45313. TREATED PRIMED CLIP REF SRM 51- 20-1. INSTALLED CLIP REF SRM 51-30-2. INSTALLED FWD ENTRY LIGHT BALLAST ASSY MM 33-10-00. THIS REPAIR IS CLASSIFIED A S A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007100100104 20071001 00104 EU 2007 10 1 07FDEA04204 1 20070924 A 5742 A57140202 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND AT LT AFT WING TO PYLON FITTING PITTING MARKS INTO THE PYLON LUG BORE REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONT OUR AND NDT FOR CRACK FREE IAW EA 6-5720-70339 AND RAS /BAE/1352/2003 ISS A. 2 L 7 2 4F RT A35EU 2007100100107 20071001 00107 NM 2007 10 1 DHLA200700048 1 20070915 A 3411 PITOT TUBE BOEING 727 727264 138408M NM FIRST OFFICER OBSTRUCTED A DHLA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 05 751DH 22982 ON TAKEOFF ACCELERATION AT 80 KTS NO AIRSPEED INDICATION ON F/O AIRSPEED. A/C WT 131.7 AS 90KTS 27 DEGREES C ALT 0 FT COMPLETE RTO FLOW CHART BRAKE ENERGY NORMAL RANGE RWY 18R MCO. FOUND FOREIGN OBJECT IN F/O PITOT TUBE REMOVED OBJECT PE RFORMED PITOT STATIC SYSTEM LEAK CHECK LOW RANGE NO DEFECTS NOTED IAW B727 MM 34-11-0. NO SPECIAL INSPECTIONS REQUIRED DUE TO REJECTED T/O. 2 L 7 3 4F A3WE 2007100100114 20071001 00114 EU 2007 10 1 07FDEA04213 1 20070924 A 5315 A53773811206 FLOORBEAM AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND CORROSION AT STRUT OF TOP CAP BEAM C 38.2, REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100124 20071001 00124 EU 2007 10 1 07FDEA04222 1 20070924 A 5315 A53778807202 FLOORBEAM AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND CORROSION AT FLANGE OF TOP CAP BEAM C 30 LT SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 2007100100125 20071001 00125 EU 2007 10 1 07FDEA04223 1 20070924 A 5315 A53974220240 FLOORBEAM AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND CORROSION AT TOP CAP BEAM C64 SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 2007100100126 20071001 00126 NM 2007 10 1 07FDEA04224 1 20070924 A 5753 ARC27364 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 RT WING INBOARD FLAP LOWER SEGMENT FOUND WITH SEVERAL DENTS. 10-05-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 2 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007100100135 20071001 00135 EU 2007 10 1 07FDEA04234 1 20070924 A 5315 A53974219220 FLOORBEAM AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND CORROSION AT TOP CAP BEAM C63 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100138 20071001 00138 EU 2007 10 1 07FDEA04238 1 20070924 A 5313 A53973679212 STRINGER AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND CORROSION AT STRINGER SEGMENT C65 P 35 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100140 20071001 00140 EU 2007 10 1 07FDEA04240 1 20070924 A 5320 A53971025202 PROFILE AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND CORROSION AT PROFILE C 54.2-54.3 P51 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100143 20071001 00143 EU 2007 10 1 07FDEA04243 1 20070924 A 5340 A53771414202 FITTING AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND CORROSION AT FITTING OF DOOR SILL BEAM C25 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100152 20071001 00152 EU 2007 10 1 07FDEA04252 1 20070924 A 5730 A57340087224 SKIN AIRBUS 300 A300B4605R 3930308 EU ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 FOUND ELONGATED HOLES ON LT WING BOTTOM SKIN AFT OF REAR SPAR REPAIR PERFORMED BY OVERSIZING AND BUSH INSTALLATION IAW D RAWING R571-50532 AND SB 29-6058, APPROVED BY EA 6-2910-112501 AND RAS/BAE/1005314/2007 ISS A. 2 L 7 2 4F RT A35EU 2007100200004 20071002 00004 NM 2007 10 2 AMTA200700423 1 20070910 A 5320 STRUCTURE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE BS 1400-1530 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 CORROSION ON LT AFT PIT CATWALK, STA 1400-1530, AROUND SCREW HOLES LBL 20. BLENDED CORROSION ON LT AFT PIT STS 1400-153 0, AROUND SCREW HOLES, LBL 20. TREATED AND PRIMED IAW SRM 51-20-01. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007100200005 20071002 00005 NM 2007 10 2 AMTA200700429 1 20070910 A 5320 CHANNEL BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE BS 1420-1440 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 CORROSION UNDER NUTPLATES, 7 EACH ON CHANNEL LOCATED AT STA 14-20-1440, RBL 20-1440. RBL 20 AFT CARGO PIT ENTRY AREA. REMOVED CORROSION SRM 51-10-53. FAB NEW CHANNEL IAW DRWG 146N5391. REPLACED WITH NEW CHANNEL SRM 51-40-02 TREATED SRM 51-20-01 AND MM 51-21-00-7. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007100200006 20071002 00006 NM 2007 10 2 AMTA200700430 1 20070921 A 5320 STRUCTURE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE BS 1200-1310 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 CORROSION ON LT AFT PIT CATWALK, STWS 1200-1310 AROUND SCREW HOLES. REMOVED CORROSION SRM 51-10-02, FOUND 1256-1260 AND 1280-1285 OUT OF LIMITS, SRM 53-00-53-1A. REPAIRED OUT OF LIMIT AREAS IAW SRM 53-60-53-2R AND 51-70-11-0G TREATED SRM 51-20-01. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007100200008 20071002 00008 NM 2007 10 2 AMTA200700432 1 20070910 A 5320 FLOOR SUPPORT BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE BS 1640-1660 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 CORROSION ON FLOOR SUPPORT AT STA 1656, RBL 57. REMOVED CORROSION SRM 53-00-51-1A. FOUND OUT OF LIMITS IAW SRM 53-00-5 1/ REMOVED AND REPLACED FLOOR SUPPORT AT STS 1540-1660, RBL 57, IAW 51-40-02 AND 51-40-05. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007100200019 20071002 00019 NM 2007 10 2 AMTA200700419 1 20070905 A 3350 20121 BATTERY BOEING 737 737* NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS UNSERVICEABLE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 401TZ 24663 EGRESS LIGHTS AT R-2 DOOR REMAIN ON RESET, NO HELP. REMOVED AND REPLACED CHARGER IAW AMM AT R-2 DOOR O/H. OPS CHECKS G OOD. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2007100200025 20071002 00025 SO 2007 10 2 WWQ2007F00000 1 20070807 A 2731 DRIVE SHAFT GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU ELEVATOR TRIM LOOSE E WWQA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 WP 07 823GA 1005 ON AUG 7, 2007 UPON LANDING, THE CREW CALLED MAINT AND REPORTED THAT UPON DESCENT FROM 41,000 FT, THEY GOT A FGC1 FAIL M ESSAGE ALONG WITH A FWD TRIM LIMIT MESSAGE. THEY WERE UNABLE TO TRIM THE AIRCRAFT ELEVATORS. THEY COMPLIED WITH THE AC CHECKLIST TO RESET BOTH MESSAGES WITH NO SUCCESS. THEY DISCONNECTED THE AUTOPILOT AND DECLARED AN EMERGENCY WITH ATC A ND MANUALLY LANDED THE AC AT AIRPORT WITHOUT INCIDENT. REQUESTED TECH SUPPORT, TECH FOUND THAT HARDWARE ATTACHING THE E LEVATOR TRIM DRIVE SHAFT PILLOW BLOCK HAD LOOSENED CAUSING THE DRIVE SHAFT TO SEPARATE FROM THE OUTPUT SHAFT. THE TECH RESECURED THE HARDWARE AND ATTACHED THE OUTPUT SHAFT TO THE DRIVE INPUT SHAFT. THE TECHNICIAN THEN RIGGED THE ELEVATOR 2 L 7 2 4F 4 F RT A12EA E25NE 2007100200028 20071002 00028 NM 2007 10 2 ASMF200709009 1 20070923 A 5610 141A481018 WINDOW BOEING 737 73776Q 13845AA NM CFMINT CFM567 CFM567B22 13802 NE COCKPIT CRACKED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 997AM 30283 DURING TRANSIT CHECK, THE RT FIRST OFFICER LATERAL WINDOW GLASS CRACKED AND IT WAS EXTREMELY HOT. MAINTENANCE PERSONNEL REPLACED THE WINDOW IAW MM 56-12-11, TESTED CORRECT. WINDOWS HEATER WAS DEFERRED IAW MEL 30-11 CATEGORY C. LATER, FIM 3 0-41 TASK 813 PROCEDURE WAS PERFORMED, TESTED CORRECT. DEFERRED REPORT WAS CLOSED. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007100200042 20071002 00042 EU 2007 10 2 COEA0703900 1 20070828 A 5310 S53172225204 CREASE BEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 900FX 170 LEVEL 2 CORROSION IN HEAVY CHECK: FLIGHT DECK CREASE BEAM AT FRAME 10-13 RT SIDE ANGLE HAS SURFACE CORROSION. REMOVED A ND INSTALLED NEW CREASE BEAM ANGLE AT FRAME 5-13 RT SIDE. WO NR 69312, NR100016. (K) 2 H 7 2 4T RT A53EU 2007100200044 20071002 00044 EU 2007 10 2 COEA0704900 1 20070828 A 5320 S5317310200400 PANEL AEROSP ATR42 ATR42320 8680930 EU 214BF CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 900FX 170 FOUND LEVEL 2 CORROSION IN HEAVY CHECK: PANEL 214BF HAS SURFACE CORROSION. BLENDED AND REPAIRED PANEL 214BF IAW SRM. ( K) 2 H 7 2 4T RT A53EU 2007100200045 20071002 00045 EU 2007 10 2 COEA0705900 1 20070828 A 5313 S53172222258 STRINGER AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 900FX 170 FOUND LEVEL 2 CORROSION IN HEAVY CHECK: STRINGER 16L BETWEEN FRAME 9 AND 10 HAS CORROSION ON LOWER FLANGE. REMOVED AND REPLACED NEW STRINGER 16L SECTION BETWEEN FRAME 9 AND 10. (K) 2 H 7 2 4T RT A53EU 2007100200046 20071002 00046 EU 2007 10 2 COEA0706900 1 20070828 A 5311 S53572601206 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 900FX 29055 170 PERMANENT REPAIR OF HYDRAULIC CUTOUTS. PERMANENT REPAIR TO FRAME 25 LT AND RT SIDES C/W SB ATR 42-53-0121. (K) 2 H 7 2 4T RT A53EU 2007100200051 20071002 00051 NM 2007 10 2 F3LA200700245 1 20070915 A 5730 FASTENER AIRBUS A319 A319111 3930336 NM LT WING DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 INSPECTION REPORTED LIGHTNING DAMAGE TO LEFT WING UPPER SURFACE AT FASTENER INBOARD OF RIB 17 AT MID SPAR. REMOVED DAMA GED FASTENER, BLENDED DAMAGED AREA, PERFORMED REQUIRED NDT PROCESS, AND INSTALLED NEW FASTENER IAW EA A9-57R-12145. 2 L 7 2 4F RT A28NM 2007100200053 20071002 00053 NM 2007 10 2 F3LA200700246 1 20070915 A 5730 FASTENER AIRBUS A319 A319111 3930336 NM LT WING DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 5730 1943 INSPECTION REPORTED LIGHTNING DAMAGE TO LEFT WING UPPER SURFACE AFT OF NR 3 SLAT, OUTBOARD SLAT TRACK, INBOARD OF RIB 17 . REMOVED AND REPLACED DAMAGED FASTENER IAW EA A9-57R-12145. 2 L 7 2 4F RT A28NM 2007100200054 20071002 00054 2007 10 2 BB07075 4 20070920 A 3442 20412200429 CONTROL PANEL BOEING 757 757225 1384959 NM WEATHER PANEL FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 925UW 10583 814 22205 FLIGHT 1601, PHL-TPA: WEATHER RADAR FAILED EN ROUTE TO TPA. DIVERTED TO CLT. MAINTENANCE REPLACED THE WEATHER RADAR C ONTROL PANEL. 2 L 7 2 4F RT A2NM 2007100200057 20071002 00057 EA 2007 10 2 TRAX200701371 1 20070917 A 3241 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA ANTI-SKID SYSTEM ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 874AS 7551 AFTER CYCLING GEAR UP AFTER TAKEOFF RECEIVED MASTER CAUTION ANTI-SKID OUTBOARD. A/C RETURNED TO GRK AFTER T/O. EMERGEN CY DECLARED, EMERGENCY EQUIP ON STANDBY. RELATED TO DEFECT 360360-1. ANTI-SKID SYSTEM CHANNELS. 2 L 7 2 4F RT A21EA 2007100200060 20071002 00060 EA 2007 10 2 TRAX200701373 1 20070918 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 861AS 7445 DOING FIRST FLIGHT CHECKS FOUND FLOOR EMERGENCY LIGHTS OUT FROM ROW 8 BACK. 2 L 7 2 4F RT A21EA 2007100200061 20071002 00061 EA 2007 10 2 TRAX200701374 1 20070918 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 920EV 7810 F/O'S FLASHLIGHT IN COCKPIT INOP. 2 L 7 2 4F RT A21EA 2007100200062 20071002 00062 EA 2007 10 2 TRAX200701375 1 20070919 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ODOR A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 871AS 7537 STRONG SMELL OF FUEL IN COCKPIT AND CABIN IN FLT ON APU OR ENG BLEEDS. SMELL GOT WORSE ON THE GROUND WITH SEVERAL OF PA SSENGERS COMPLAINING OF NAUSEA AND HEADACHE. 2 L 7 2 4F RT A21EA 2007100200063 20071002 00063 EA 2007 10 2 TRAX200701376 1 20070919 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA PAX AIRSTAIRS INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 921EV 7819 EXIT SIGN ON PAX STAIRS NOT ILLUMINATING. 2 L 7 2 4F RT A21EA 2007100200068 20071002 00068 EU 2007 10 2 MAC090703 1 20070901 A 5751 FITTING AEROSP AEROSP ATR42 ATR42300 8680920 EU RT AILERON CORRODED A MTNA K NONE O OTHER IN INSP/MAINT 1 SO 33 923FX NT1132 135 DURING INSPECTION, LEVEL 3 CORROSION WAS FOUND ON 4 T FITTINGS INSIDE THE RIGHT WING AILERON. THE PROBABLE CAUSE IS DIS SIMILAR MATERIALS (STEEL BOLTS IN ALUMINUM FITTINGS ATTACHED TO A COMPOSITE SPAR). THE FITTINGS WERE REPLACED AT RIBS 4 , 11/12, AND 19. REFERENCE ATR 42 SRM 57-61-10 PAGE 115/116. THE TYPE OF CORROSION FOUND WAS EXFOLIATION. THE FITTING PART NUMBERS ARE: S57610025202, S57610025204, AND S57610025200. 2 H 7 2 4T RT A53EU 2007100200069 20071002 00069 EU 2007 10 2 USAA070715 1 20070921 A 5320 ANGLE AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 184US 1651 FR 66 JUST FWD OF RT AFT DOOR IN SILL PLATE UPPER ANGLE AT NUT CLIP HOLE CORRODED. INSTALLED ANGLE (BATHRUB) REPAIR PER SRM 53-41-14; CORR TASK JA-260-53500-14, DEFECT SIZE: 1 X 1 INCH. 2 L 7 2 4F RT A28NM 2007100200070 20071002 00070 EU 2007 10 2 USAA070714 1 20070921 A 5315 D5311281520200 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 184US 1651 TOPSIDE OF FLOORBEAM Y1292 HAS CORROSION. INSTALLED FILLER WITH ANGLE SPLICES ON BOTH SIDES PER SRM 53-00-14; CORR TASK JA-220-53500, DEFECT SIZE: 1.5 X 1.5 INCH. 2 L 7 2 4F RT A28NM 2007100200071 20071002 00071 EU 2007 10 2 USAA070713 1 20070921 A 5315 D5311282600101 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 184US 1651 TOPSIDE OF FLOORBEAM HAS CORROSION. REMOVED CORRODED FLOORBEAM & INSTALLED NEW BEAM PER SRM 51-72-11; CORR TASK JA-220- 53500; DEFECT SIZE: 1 X 1 INCH. 2 L 7 2 4F RT A28NM 2007100200072 20071002 00072 NM 2007 10 2 SWAA074723 1 20070920 A 3350 147A5701 COVER BOEING 737 7373K2 13844BA NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 EEPLS COVER MISSING AT ROW 10 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007100200074 20071002 00074 NM 2007 10 2 SWAA074718 1 20070920 A 3350 1619 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 283WN 36610 DURING SCHEDULED MV2 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007100200075 20071002 00075 NM 2007 10 2 SWAA074728 1 20070920 A 3350 311500 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 443WN 29838 RIGHT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007100200078 20071002 00078 NM 2007 10 2 SWAA074719 1 20070920 A 2730 6545187 TORQUE TUBE BOEING 737 7373H4 1384600 NM ELEVATOR FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, RIGHT AND LEFT ELEVATORS FAIL FREE PLAY CHECK. REMOVED AND REPLACED OUTPUT TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007100200082 20071002 00082 NM 2007 10 2 SWAA074740 1 20070920 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007100200084 20071002 00084 NM 2007 10 2 SWAA074738 1 20070920 A 5311 6546531 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 20L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007100200088 20071002 00088 NM 2007 10 2 SWAA074721 1 20070920 A 5754 65C266022 SLAT BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 5 L/E SLAT DELAMINATED AT T/E. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 2007100200091 20071002 00091 CE 2007 10 2 AOD2007F00000 1 20070424 A 3240 06111800 CYLINDER CESSNA 208 208B 2073701 CE PWA PT6 PT6* 52043 EA LT BRAKE LEAKING E AODA O OTHER K FLUID LOSS NR NOT REPORTED 1 SO 19 910HL 3152 208B1080 LT BRAKE CYLINDER LEAKING AT PISTON O-RING CAUSING LOS OF BRAKE PRESSURE AT THE LT BRAKE PEDAL. (K) 1 H 7 1 3T 3 T A37CE E2NE 2007100200093 20071002 00093 NM 2007 10 2 SWAA074730 1 20070920 A 3350 65C27093 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 R1 DOOR EMERGENCY EXIT LIGHT ASSY LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007100200094 20071002 00094 NM 2007 10 2 SWAA074726 1 20070920 A 5330 65C337568 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR FUSELAGE SKIN CRACKED AT LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007100200095 20071002 00095 NM 2007 10 2 SWAA074735 1 20070920 A 3350 65C34691 LIGHT BOEING 737 737317 138447P NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 1 DEF. REPAIRED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007100200097 20071002 00097 NM 2007 10 2 SWAA074737 1 20070920 A 3350 65C34691 LIGHT BOEING 737 737317 138447P NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 8 DEF. REPAIRED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007100200098 20071002 00098 NM 2007 10 2 SWAA074727 1 20070920 A 3350 8100517201 SOCKET BOEING 737 7377H4 1384404 NM EXTERIOR CORRODED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 412WN 29818 DURING SCHEDULED MV1 CHECK, FOUND LEFT AFT LOWER FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. CLEANED CORRODED SOCKET P ER MM. 2 L 7 2 4F RT A16WE 2007100200099 20071002 00099 NM 2007 10 2 SWAA074731 1 20070920 A 5320 907822 STRUCTURE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR UPPER HINGE BOX CRACKED. REMOVED AND REPLACED HINGE BOX PER SRM. 2 L 7 2 4F RT A16WE 2007100200100 20071002 00100 NM 2007 10 2 SWAA074732 1 20070920 A 5320 907822 STRUCTURE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR LOWER HINGE BOX CRACKED. REMOVED AND REPLACED HINGE BOX PER SRM. 2 L 7 2 4F RT A16WE 2007100200104 20071002 00104 NM 2007 10 2 ASAA0792060 1 20070921 A 5230 1036541 HOUSING BOEING 737 737990 NM CARGO DOOR GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 306AS 30014 FWD CARGO DOOR HOUSING GOUGED. REPAIRED IAW EA 5230 01123. 2 L 7 4 4F RT A16WE 2007100200106 20071002 00106 NM 2007 10 2 USAA920070845 1 20070920 A 5313 141N3270 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 920UW 22199 CLT - MAJOR REPAIR - C-3 CHECK, LEVEL 2 CORROSION ON STRINGER, BS 440, S24R. REPAIRED STRINGER BS 440, S24R IAW USAIRWA YS TYPICAL EA 98885. 2 L 7 2 4F RT A2NM 2007100200107 20071002 00107 NM 2007 10 2 USAA920070846 1 20070920 A 5322 SHEAR TIE BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 920UW 22199 CLT - MAJOR REPAIR - C-3 CHECK, LEVEL 2 CORROSION ON FRAME SHEAR TIE CLIP, BS 1440, S29L - S30L. REPLACED FRAME SHEAR T IE CLIP, BS 1440, S29L - S30L IAW B757-200 SRM 51-20-01 AND 51-10-02. 2 L 7 2 4F RT A2NM 2007100200108 20071002 00108 NM 2007 10 2 USAA920070847 1 20070921 A 5313 65617775 STRINGER SPLICE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 445US 24863 CLT - MAJOR REPAIR, CRACKED STRINGER SPLICE, BS 360, S16L. REPLACED STRINGER SPLICE, BS 360, S16L IAW B757-200 SRM 51-4 0-02. 2 L 7 2 4F RT A16WE 2007100200109 20071002 00109 NM 2007 10 2 USAA920070848 1 20070920 A 5313 140N1530 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 920UW 22199 CLT - MAJOR REPAIR - C-3 CHECK, CORROSION ON STRINGER, BS 1460, S30R. REPAIRED STRINGER, BS 1460, S30R IAW B757-200 SRM 51-00-00, 51-20-01 AND 51-40-00. 2 L 7 2 4F RT A2NM 2007100200113 20071002 00113 EU 2007 10 2 2007UALA01938 1 20070610 A 2612 FUSE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FIRE WARNING BLOWN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 476UA 1508 UPON ENGINE 1 AND 2 FIRE TEST, GETTING HALF A TEST AND OPPOSITE BOTTLE DISCHARGE LIGHT INDICATION ON OTHER ENGINE. JUST INBOARD LIGHTS ON FIRE SW COMES ON. REPLACED NR 2 XFMR (36LP) FUSE AT LOCATION (G). ALL TESTS NORMAL, NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007100200115 20071002 00115 SO 2007 10 2 RAIA00709027 1 20070920 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NR 1 & 2 MALFUNCTIONED A RAIA O OTHER N FALSE WARNING LD LANDING 1 CE 03 816HK 145055 FLT NR 5544 - STL - LANDING GEAR HANDLE DISAGREE EICAS MESSAGE ON FINAL. MAINTENANCE REMOVED AND REPLACED NR 1 & 2 RIGH T PROX SWITCHES, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007100200116 20071002 00116 SO 2007 10 2 RAIA00709024 1 20070918 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO CABIN DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 821HK 145068 POST FLT NR 5564 - STL - SERVICE DOOR EXIT MARKER EMERGENCY LIGHT INOP. MAINTENANCE RECONNECTED CONNECTOR. OPS CHECK G OOD. 2 L 7 2 4F RT T00011AT 2007100200118 20071002 00118 SO 2007 10 2 RAIA00709021 1 20070916 A 5610 SEAL EMB 145 EMB145LR 3260212 SO WINDOW LOOSE A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 850HK 145003 FLT NR 7919 - IAD - CAPT DIRECT VIEW WINDOW SEAL LOOSE. MAINTENANCE RESECURED CAPT COCKPIT EMERGENCY EXIT RUBBER TRIM S EAL, CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007100200119 20071002 00119 SO 2007 10 2 RAIA00709015 1 20070914 A 3350 100865 POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 814HK 3259 817 145046 POST FLT NR 5530 - STL - EMERGENCY LIGHT AISLE FLOOD LIGHTS FLICKERS ON/OFF. MAINTENANCE REMOVED AND REPLACED NR 1 POWE R SUPPLY, CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2007100200120 20071002 00120 SO 2007 10 2 RAIA00709020 1 20070916 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145EP 3260221 SO NLG CORRODED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 826HK 9833 8628 145016 FLT NR 5578 - TUL - LANDING GEAR AIR/GROUND DISAGREE, GEAR DID NOT RETRACT, HANDLE DID NOT GO UP. MAINTENANCE INSPECTED & FOUND CONNECTOR TO NLG WOW PROX SENSOR CORRODED. REPLACED PROX SWITCH. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007100200121 20071002 00121 SO 2007 10 2 RAIA00709026 1 20070920 A 3350 100869 POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 846HK 14500855 POST FLT NR 7938 - SYR - ALL EMERGENCY LIGHTS GO DIM DURING TEST. MAINTENANCE REMOVED AND REPLACED ALL EMERGENCY POWER SUPPLIES. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007100200123 20071002 00123 SO 2007 10 2 RAIA00709018 1 20070915 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 821HK 145068 PRE FLT NR 5575 - STL - EMERGENCY LIGHT SERVICE DOOR EXIT MARKER OUT. MAINTENANCE RESECURED CONNECTOR TO LIGHT, OPS CHE CK GOOD. 2 L 7 2 4F RT T00011AT 2007100200126 20071002 00126 NM 2007 10 2 ABXA070308 1 20070915 A 5414 311T306557 PANEL BOEING 767 767205 1385121 NM RT PYLON MISSING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 23058 ON WALKAROUND, MAINTENANCE FOUND NR 2 ENGINE INBOARD PYLON PANEL MISSING. DEFERRED 57076. C/W REA B654-56397, APPLIED SPEED TAPE. DEFERRED IAW REA B654-56397 AND GMM CHAPTER 1, SECTION 7.04 FOR MX TRACKING. CLEARED: DI 57076, INSTALLED NEW PANEL 446BL IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007100200127 20071002 00127 WP 2007 10 2 ABXA070303 1 20070907 A 5347 S2614913 CARGO TRACK DOUG DC9 DC941 302207N WP FWD CARGO ABY CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 UPPER CARGO TRACKS WERE CORRODED AT FLOOR PANEL 3F ATTACH POINTS. REPAIRED SEAT TRACK IAW REA D957-56383. 2 L 7 2 4F A6WE 2007100200128 20071002 00128 WP 2007 10 2 ABXA070302 1 20070912 A 5320 5952804511 FLOOR SUPPORT DOUG DC9 DC941 302207N WP FWD CARGO BAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 960AX 47762 FLOOR SUPPORT AT STA 351 LEFT HAD A 10 INCH CRACK ON UPPER FLANGE. REMOVED AND REPLACED ANGLE IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 2007100200132 20071002 00132 WP 2007 10 2 ABXA070305 1 20070913 A 5320 992348465 INTERCOSTAL DOUG DC9 DC941 302207N WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 INTERCOSTAL AT STA 180, LEFT BUTT LINE 19 ON BOTH SIDES OF FLOOR BEAM WAS CRACKED. REPAIRED INBOARD INTERCOSTAL STA 180, LEFT BUTT LINE 19 IAW DC9 SRM. OUTBOARD INTERCOSTAL TO BE REPAIRED ON NON ROUTINE 0523. 2 L 7 2 4F A6WE 2007100200138 20071002 00138 NM 2007 10 2 CALA0700530 1 20070923 A 5311 6546533 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70330 23460 INSPECTION FOUND A .25 INCH CRACK IN FORWARD BAGGAGE BIN FRAME WEB AT STA 500, BL 0. THE CRACKED AREA WAS REMOVED AND A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-70-11. 2 L 7 2 4F RT A16WE 2007100200140 20071002 00140 NM 2007 10 2 HNAA0700174 1 20070903 A 3260 WARNING SYSTEM DHAV DHC8 DHC8301 1386003 NM COCKPIT MALFUNCTIONED A HNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 07 333EN 221 AFTER TAKEOFF CYCLED GEAR UP, LEFT MAIN GEAR DOOR AMBER LIGHT ILLUMINATED (DOORS REMAINED OPEN). LANDING GEAR INOP CAUT ION LIGHT ILLUMINATED, PERFORMED ALT EXTENSION PROCEDURES. INSPECTED LT MAIN GEAR PROX SENSORS FOR DEFECTS AND PROPER GAPS, GEAR AND GEAR DOOR SENSORS CHECK GOOD IAW MM 32-10-00. JACKED A/C, SWUNG GEAR SEVERAL TIMES, NO DEFECTS NOTED. R EMOVED AND REPLACED PSEU AS PRECAUTIONARY, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007100200141 20071002 00141 NM 2007 10 2 UPS07550702 1 20070911 A 5311 146N1028112 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 434UP 25465 INSPECTION TYPE:C AFT CARGO FUSELAGE FRAME STA 1300, BETWEEN S25L AND S26L HAS A GOUGED/ DENTED. ACCOMPLISHED PER FINAL EA 757-5362-27-A1743 AND UPS B757-5310-27707-A. 2 L 7 2 4F RT A2NM 2007100200142 20071002 00142 NM 2007 10 2 UPS07550703 1 20070913 A 5414 146N10065 SKIN BOEING 757 75724APF 1384969 NM NR 2 NACELLE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 434UP 25465 INSPECTION TYPE:C NR 2 OUTBOARD NACELLE STRUT SKIN CRACKED ABOUT ONE INCH ALONG 443BR CUTOUT. COMPLIED WITH FINAL EA 75 7-5451-27-A1748 AND EO B757-5430-27710. 2 L 7 2 4F RT A2NM 2007100200143 20071002 00143 NM 2007 10 2 UPS07550716 1 20070914 A 3350 LIGHT BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 460UP 25481 INSPECTION TYPE:N/A EMERGENCY LIGHT UNARM LIGHT INOP. RELAMPED EMERGENCY LIGHT UNARM LIGHT. OPS CHECK NORMAL. 2 L 7 2 4F RT A2NM 2007100200144 20071002 00144 WP 2007 10 2 UPS07850705 1 20070816 A 5320 CUSP WEB DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 CUSP HAS DEEP BLEND OUT AT L21L AT STA 1130. REPAIRED CUSP AT STA 1130 L21L IAW SRM 53-02-05-0. 2 L 7 4 4F RT 4A25 2007100200147 20071002 00147 WP 2007 10 2 UPS07850708 1 20070814 A 5720 STRUCTURE DOUG DC8 DC873F 302199F WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 LEFT WING FLAPWELL FUEL DUMP CHUTE FWD AREAS CORRODED. REPAIRED LEFT WING FLAPWELL FUEL DUMP CHUTE F WD AREAS IAW SRM 51-01-08- 0, 57-02-00 FIG 007, DWG 5649654, AND SRM 51-01-21. 2 L 7 4 4F RT 4A25 2007100200150 20071002 00150 WP 2007 10 2 UPS07850711 1 20070823 A 5210 SKIN DOUG DC8 DC873F 302199F WP L1 DOOR CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 L1 DOOR OUTSIDE DOOR HANDLE IS CHAFING ON DOOR EXTERNAL SKIN. REPAIRED L1 DOOR SKIN HANDLE CUTOUT IA W UPS EO DC8-5210-8162. 2 L 7 4 4F RT 4A25 2007100200152 20071002 00152 NM 2007 10 2 UPS07M50704 1 20070816 A 5320 INTERCOSTAL DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C CABIN - C-ZONE STA 1941 - 1951 INTERCOSTAL FOUND CRACK AT L2 RIGHT AS MARKED. CABIN C-ZONE STA 1941-1 951 INTERCOSTAL FOUND CRACK AT L2 RIGHT REMOVED NEW INTERCOSTAL FABRICATED, HEAT TREATED & HARDNESS VALUES HRB 8 6.2 PER DPS 1.05-3. NEW INTERCOSTAL FASTENER HOLES PICKED UP. NEW INTERCOSTAL ALODINE CARRIED OUT, PAINTED & INSTALLED. 2 L 7 3 4F RT A22WE 2007100200154 20071002 00154 NM 2007 10 2 UPS07M50714 1 20070803 A 5313 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C CTR CARGO COMPT AT STATION 1809 LONGERON 46 RIGHT FOUND CORRODED DOUBLER AS MARKED. CTR CARGO COMPT S TA 1809 LONGERON 46 RIGHT CORRODED SPLICE DOUBLER RMVD LONGERON SPLICE MACHINED FROM S2641454-12000 HAT SECTION PER DOUG LAS DWG AFA7103. FPI C/OUT ON FABRICATED SPLICE FOUND NO CRACK. FABBED LONGERON SPLICE HOLES PICKED UP, REPROTECTED, P AINTED & INSTALLED. 2 L 7 3 4F RT A22WE 2007100200156 20071002 00156 CE 2007 10 2 BSAASDR0724 1 20070916 A 2120 1143800595 SHUTOFF VALVE BEECH 1900 1900D 1154162 CE RIGHT INOPERATIVE A BSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 05 171ZV UE171 DURING CLIMB THE LEFT ENVIROMENTAL FAIL LIGHT ILLUMINATED AND WOULD NOT RESET. UPON RETURN TO BOSTON THE DISCREPANCY WA S INITIALLY DEFERRED. AFTER RETURN TO BOSTON THE RT PRESSURE REGULATING SHUT OFF VALVE WAS REMOVED AND REPLACED. GROUN D CHECK GOOD. 2 L 7 2 4T RT A24CE 2007100200158 20071002 00158 NM 2007 10 2 USAA920070851 1 20070922 A 5320 ANGLE BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 920UW 22199 CLT - MAJOR REPAIR - C-3 CHECK, LEVEL 2 CORROSION ON ANGLE, BS 1523, 25R. REPAIRED ANGLE, BS 1523, S25R IAW B757-200 SR M 51-70-13 FIGURE 1. 2 L 7 2 4F RT A2NM 2007100200159 20071002 00159 NM 2007 10 2 HNAA0700175 1 20070902 A 2510 110821AA MECHANISM DHAV DHC8 DHC8102 2809003 NM PILOT SEAT LACK OF LUBE A HNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 07 935HA 142 DURING TAKEOFF ROLL, THE CAPTAINS SEAT BECAME DISLODGED AND FELL FROM THE TRACKS TO THE FLOOR. MTX LUBED VERTICAL ADJUS TMENT LOCK MECHANISM. 2 H 7 2 4T RT A13NM 2007100200162 20071002 00162 NM 2007 10 2 SWAA074743 1 20070922 A 5753 6546430122 REPAIR BOEING 737 7373H4 1384600 NM FOREFLAP MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 RIGHT WING INBOARD FORE FLAP PREVIOUS REPAIR PATCH MISSING. REMOVED AND REPLACED FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2007100200163 20071002 00163 NM 2007 10 2 SWAA074766 1 20070923 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007100200164 20071002 00164 NM 2007 10 2 SWAA074767 1 20070923 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007100200166 20071002 00166 NM 2007 10 2 SWAA074768 1 20070923 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007100200167 20071002 00167 NM 2007 10 2 SWAA074764 1 20070923 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007100200169 20071002 00169 NM 2007 10 2 SWAA074765 1 20070923 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007100200170 20071002 00170 NM 2007 10 2 SWAA074751 1 20070923 A 2750 6557421 TORQUE TUBE BOEING 737 7373H4 1384600 NM T/E FLAP WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED A1 CHECK, FOUND RIGHT WING INBOARD T/E FLAP DRIVE TORQUE TUBE WORN. REMOVED AND REPLACED TORQUE TUBE P ER MM. 2 L 7 2 4F RT A16WE 2007092800158 20070928 00158 NM 2007 9 28 2007UALA03777 1 20070919 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EEL LIGHT INOP AT SEAT 7 LEFT AFT LIGHT ASSY. 10-16-07 REPLACED LAMP ASSY. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092800160 20070928 00160 2007 9 28 2007UALA03779 4 20070918 A 2565 RELEASE CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT OVERWING OBSTRUCTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 518UA 24871 RIGHT OVERWING MANUAL BACKUP EMERGENCY RELEASE CABLE IS FROZEN. 10-19-07 ON TROUBLESHOOTING FOUND DEBRIS AROUND CA BLE HINDERING ANY MOVEMENT OF CABLE. CLEANED DEBRIS FROM BACKUP CABLE TO FREE CABLE TRAVEL MOVEMENT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092800167 20070928 00167 SO 2007 9 28 LR7A07092 1 20070917 A 5310 3620116R RIB LKHEED 382 382G 526414U SO FS 132 RBL 55 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 646 4590 DURING SCHEDULED B-2 CHECK, PER JOBCARD HB5303, FOUND COCKPIT RIGHT SIDE RIB CRACKED AT FS 132 WL 204 TO 216 RBL 55. RI B REPLACED IAW SMP583 CHAPTER 51-60 & 51-70. 2 H 7 4 4T A1SO 2007092800173 20070928 00173 2007 9 28 YENA200782 4 20070919 A 2370 VIDEO DISPLAY AIRBUS 320 A320232 3930326 EU ROW 7 ODOR A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 547JB 1849 FLIGHT ATTENDANT REPORTED ELECTRICAL ODOR IN CABIN NEAR ROW 7. ODOR DISSIPATED AFTER APPROXIMATELY 30 MINUTES. COMPLIE D WITH TSM 24-00-00-810-823. NO DEFECTS NOTED. PERFORMED INSPECTION OF LTV SYSTEM PER TSM 23-39-00-810-801. RAN SYSTE M FOR 2 HOURS WITH NO INDICATION OF ANY ODOR. REMOVED AND REPLACED VDU'S AND XEB'S IN ROW 7 AS PRECAUTIONARY PER TSM 2 3-39-00-810-801. OPERATION NORMAL PER AMM 23-39-00. 2 L 7 2 4F RT A28NM 2007092800188 20070928 00188 WP 2007 9 28 ABXA070321 1 20070907 A 5320 4924659501 FITTING DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 CRACKED FITTING AT P-DOME DOOR JAMB - LOWER. REMOVED AND REPLACED FITTING IAW DC9 SRM. 2 L 7 2 4F A6WE 2007092800190 20070928 00190 WP 2007 9 28 ABXA070314 1 20070905 A 5347 S49255848M12000 SEAT TRACK DOUG DC9 DC933F 302207A WP BS 190-214 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 SEAT TRACK CORRODED INSIDE TOP OF DOUBLE TRACK AT FS 214 - 190, RIGHT BUTT LINE 22. REPAIRED SEAT TRACK IAW DC9 SSRM K0 5406. 2 L 7 2 4F A6WE 2007092800192 20070928 00192 WP 2007 9 28 ABXA070316 1 20070905 A 5320 D0489835 CUSP WEB DOUG DC9 DC933F 302207A WP BS 945-965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 LEFT CUSP CRACKED BETWEEN FS 945 - 965. REMOVED AND REPLACED SECTION OF CUSP IAW DC9 SSRM DWG K07259 AND DC9 SRM 51-30- 2. 2 L 7 2 4F A6WE 2007092800204 20070928 00204 NM 2007 9 28 2007UALA03796 1 20070919 A 3250 STEERING SYS BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU NLG WHEEL OUT OF RIG A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 934UA 26662 NOSE WHEEL PULLING SEVERELY TO THE LEFT. NOSE STEERING SYSTEM OUT OF RIG.ADJUSTED NOSE STEERING RIG. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092800216 20070928 00216 NM 2007 9 28 UPS07M50730 1 20070816 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORZ STAB CTR SECTION BARREL NUT BORE RT NR 5 FOUND WITH CORROSION. CORR AT BARREL NUT BORE RMVD SRM 51-21-01 VII R38. BOTTOM RMN BLEND OUT 0.04 0" BORE REAM TO 0.988" DIA RMN BLEND OUT 0.0025" DEEP. EXCEEDED LIMITS. B ARREL NUT BORE, BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED SRM 51-21-01 VII R38. SLEEVE BUSHING FAB & INSTALLED PER EO MD11-5510-19. 409-L, FIG 5. REPAIR C/O IS ACCEPTABLE PER EN 1523-07. 2 L 7 3 4F RT A22WE 2007092800217 20070928 00217 NM 2007 9 28 UPS07M50731 1 20070810 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZ STAB CONSTANT SECTION BARREL NUT BORE RT NR 13 FOUND WITH CORROSION. CORR AT BARREL NUT BORE RM VD. BOTTOM BORE THRU, BORE REAM TO 0.988" DIA, RMN BLEND OUT 0.035" DEEP, EXCEEDED LIMITS. BARREL NUT BORE, BLEND VOID RAD US SMOOTHEN & PROTECTED SRM 51-21-01 VII R38. BUCKET BUSHING FAB & PROTECTED. BUCKET BUSHING INSTALLED PER EO MD1 1-5510-19409-L, FIG 5. REPAIR C/O A AT BARREL NUT BORE NR 13 RT IS ACCEPTABLE PER EN 1516-07. 2 L 7 3 4F RT A22WE 2007100100026 20071001 00026 EU 2007 10 1 USAA920070857 1 20070918 A 5320 D53480043202 SILL AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 644AW 317 SAL - MAJOR REPAIR - C-4 CHECK - NR 5976233, CORROSION ON THE R2 DOOR CUTOUT LOWER SILL, BS 2786 / FR 66 - BS 2884 / FR 68. REPAIRED THE R2 DOOR CUTOUT LOWER SILL, BS 2786 / FR 66 - BS 2884 / FR 68 IAW A320 SRM 53-41-14. 2 L 7 2 4F RT A28NM 2007100100035 20071001 00035 NM 2007 10 1 KCSA071416 1 20070926 A 5313 STRINGER BOEING 747 7472B4B 138481B NM BS 2360 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STR 49R END FITTING CORRODED FWD OF BS 2360. 2 L 7 4 4F RT A20WE 2007100100039 20071001 00039 EA 2007 10 1 TRAX200701381 1 20070922 A 5230 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 914EV 7752 ASD AFT FRAME DRAG ANGLE IS CRACKED AT THE MOTOR PULLEY BRACKET. 2 L 7 2 4F RT A21EA 2007100100049 20071001 00049 NM 2007 10 1 USAA920070841 1 20070917 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916UW 22192 PIT - MAJOR REPAIR - C-4 CHECK, CRACKED FLOOR SUPPORT INTERCOSTAL, BS 1520 - BS 1540, BL 0, WL 208.1. REPLACED FLOOR SU PPORT INTERCOSTAL, BS 1520 - BS 1540, BL 0, WL 208.1 IAW B757-200 SRM 53-60-61. 2 L 7 2 4F RT A2NM 2007100100052 20071001 00052 NM 2007 10 1 USAA920070844 1 20070915 A 5320 ANGLE BOEING 757 757225 1384959 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916UW 22192 PIT - MAJOR REPAIR - C-4 CHECK, CORROSION ON ANGLE, BS 1620 - BS 1640, BL 0. REPAIRED ANGLE, BS 1620 - BS 1640, BL 0 I AW B757-200 SRM 53-00-051 REPAIR 4. 2 L 7 2 4F RT A2NM 2007100100054 20071001 00054 NM 2007 10 1 MASA200700540 1 20070831 A 2120 UNKNOWN DHAV DHC8 DHC8202 2809007 NM CABIN SMOKE A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 991HA 431 INTERMITTENT SMOKE WARNING LIGHT CAME ON IN FLIGHT. MX FOUND SMOKE IN THE CABIN WHEN RUNNING IT UP. MX PERFORMED BLEED CHECKS, SMOKE WARNING SYSTEM OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007100100057 20071001 00057 EA 2007 10 1 HNAA0700173 1 20070921 A 3320 2LA00772341 PSU DHAV DHC8 DHC8311 1386006 EA CABIN HOT A HNAA A UNSCHED LANDING M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 327EN 261 BURNING ODOR AT AFT CABIN, NOTICED BY CREW MEMBERS & AFT F/A CONTROL PANEL APPEARS TO BE HOT TO TOUCH. INSPECTED F/A PA NEL NO DEFECT NOTED CREW GROUND RAN AIRCRAFT WITH BLEEDS ON, NO ABNORMAL ODOR NOTED. DEACTIVATED PSU AT 8DF DUE TO INTE RMIT CHIM ACTIVATION IAW SPECIAL PROCEDURES 23.3. REMOVED AND REPLACED PSU, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007100100060 20071001 00060 EA 2007 10 1 TRAX200701366 1 20070917 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 881AS 7496 MAIN PAX DOOR OUTER HANDLE CRACKED. 2 L 7 2 4F RT A21EA 2007100100063 20071001 00063 2007 10 1 RAIA00709019 4 20070915 A 3418 0861DT5 SENSOR EMB 145 EMB145LR 3260212 SO AOA INOPERATIVE A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 823HK 12532 8965 145475 FLT NR 7960 - IAD - SPS 1 INOP / SPS ADVANCED ON EICAS ON TAKEOFF ROLL. MAINTENANCE REPLACED ANGLE OF ATTACK SENSOR TES T GOOD. 2 L 7 2 4T RT T00011AT 2007100100066 20071001 00066 EU 2007 10 1 07FDEA04320 1 20070927 A 5315 A53978476202 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 FOUND CORROSION ON CROSSBEAM FRAME 62 RT OUTSIDE, AFT CARGO COMPARTMENT. REPLACEMENT OF CROSSBEAM IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100067 20071001 00067 EU 2007 10 1 07FDEA04321 1 20070927 A 5315 A53974322244 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 CORROSION ON CROSSBEAM AT FRAME 62 RT, AFT CARGO COMPARTMENT. REPLACEMENT OF THE CORRODED RT HALF-BEAM IAW SRM 51-72-10 AND SPLICE IAW SRM 53-10-15/FIG 207/SEC F-F. 2 L 7 2 4F RT A35EU 2007100100068 20071001 00068 EU 2007 10 1 07FDEA04322 1 20070927 A 5315 A53973599208 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 CORROSION ON CROSSBEAM AT FRAME 60 LT, AFT CARGO COMPARTMENT. REPAIR PERFORMED REPLACEMENT OF LT HALF-BEAM IAW SRM 51-7 2-10 AND BEAM SPLICE IAW SRM 53-10-15/FIG 207/SEC "E-E". 2 L 7 2 4F RT A35EU 2007100100076 20071001 00076 EU 2007 10 1 07FDEA04278 1 20070925 A 5320 A25573811202 ANGLE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 DAMAGED ANGLE SHEET BETWEEN FRAME 60-61, STGR 28 RT, CARGO DOOR AREA. REPLACEMENT OF ANGLE SHEET IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100077 20071001 00077 EU 2007 10 1 07FDEA04279 1 20070925 A 5320 A25573812202 ANGLE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 DAMAGED ANGLE SHEET BETWEEN FRAME 62-63, STGR 28 RT, CARGO DOOR AREA. REPLACEMENT OF ANGLE SHEET IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100092 20071001 00092 EU 2007 10 1 07FDEA04193 1 20070924 A 5330 A53773485 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 THREE CORROSION SPOTS ON INNER SKIN PANEL BETWEEN FRAME 18-19 AND BETWEEN STRG 49-51 LHS. REPAIR PERFORMED BY LOCAL CUT OUT AF SKIN PANEL BETWEEN STRG 49-50 AND SMOOTH REWORK OF REMAINING CORRODED AREAS, HFEC-, ROTOTEST INSPECTION AND INST ALLING EXTERNAL SKIN DOUBLER IAW EA 6-5312-92140 AND RAS/AS/135/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100100101 20071001 00101 EU 2007 10 1 07FDEA04201 1 20070924 A 5754 SKIN AIRBUS 300 A300B4622 3930401 EU ZONE 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND DENT AT SLAT NR 1 LT ON LOWER TRAILING EDGE SKIN NEAR RIB 23 REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR AND N DT FOR CRACK FREE IAW EA 6-5742-70345 AND RAS/FOK/197/2003 ISS A. 2 L 7 2 4F RT A35EU 2007100100105 20071001 00105 EU 2007 10 1 07FDEA04205 1 20070924 A 5330 A53986301200 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 803FD 378 EXISTING INTERNAL SKIN FLUSH DOUBLER REPAIR BETWEEN FRAME 83-84, STRG 38 RT- 40 RT, NOT CONFORM TO SRM 53-10-12/FIG 227 . DOUBLER THICKNESS OF ONLY 1,8MM. INSTALLED FLUSH REPAIR IS ACCEPTABLE AS PERMANENT REPAIR, REPLACEMENT OF RIVETS LN9 198-4000 ON EACH SIDE OF THE STRINGER FOOT TO SKIN BY HI-LOKS (HL18-6) ACC TO SRM 53-19-14/FIG 201, IAW EA 6-5318-92146 AND RAS/DAHAM/4019725/2005 ISSUE B. 2 L 7 2 4F RT A35EU 2007100100141 20071001 00141 EU 2007 10 1 07FDEA04241 1 20070924 A 5313 A537709780220 STRINGER AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND CORROSION AT STRINGER SEGMENT P 44 RT, C 26 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100200032 20071002 00032 EU 2007 10 2 COEA0704821 1 20070817 A 5753 S5751204920200 PIN AEROSP ATR72 ATR72212 8680945 EU LT FLAP GUIDE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FE 253 FOUND LEVEL 2 CORROSION IN HEAVY CHECK. LT WING IB FLAP CAM GUIDES CORRODED. REPLACED WITH NEW GUIDE PINS. WO NR 7224 4, NR 601003. (K) 2 H 7 2 4T RT A53EU 2007100200040 20071002 00040 NM 2007 10 2 MWEA070223 1 20070919 A 7830 7150922505 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 905ME 55169 RIGHT THRUST REVERSER, UPPER DEFLECTOR DOOR ZEE FRAME IS CRACKED IN RADIUS ON INBOARD END AT STATION 26 AT ATTACH POINT WITH OUTER SKIN. REMOVED DAMAGE, FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F TR A6WE 2007100200056 20071002 00056 EA 2007 10 2 TRAX200701370 1 20070917 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT WEAK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 937EV 8042 F/O'S YELLOW FLASHLIGHT ON C/B PANEL NR 2 BATTERY IS WEAK / UNSERVICEABLE. 2 L 7 2 4F RT A21EA 2007100200081 20071002 00081 NM 2007 10 2 SWAA074729 1 20070920 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007100200089 20071002 00089 SO 2007 10 2 ENE2007F00000 2 20070824 A 8530 SA52006A20P CYLINDER CESSNA 206 U206F 2073333 CE CONT O520 IO520F 17032 SO ENGINE CRACKED E ENEA O OTHER O OTHER NR NOT REPORTED 1 AL 03 7138Q 847 U20603074 818805R BOTH CYLINDER HAVE VISIBLE CRACKS ORIGINATING AT THE EXHAUST VALVE SEAT. (K) 1 H 7 1 3O 3 O A4CE E5CE 2007100200103 20071002 00103 NM 2007 10 2 ASAA0772059 1 20070919 A 3350 D71701100 BATTERY PACK BOEING 737 737790 13844CN NM CABIN FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 648AS 30662 BATTERY PACKS AT FWD AND AFT EXIT DOORS FAILED MTX TEST. REMOVED AND REPLACED BATTERY PACKS. 2 L 7 2 4F RT A16WE 2007100200134 20071002 00134 WP 2007 10 2 ABXA070301 1 20070904 A 5312 591013013 BULKHEAD DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 960AX 47762 AFT PRESSURE BULKHEAD CUTOUT UPPER RIGHT CORNER HAD APPROXIMATELY 1.20 INCH LONG CRACK IN DOUBLER WITH NO PREVIOUS REPAI R CONFIG INSTALLED. NOTE: UPPER LEFT CORNER PREVIOUS J060088-1 CONFIG REPAIRED DOOR CORNERS IAW DC9 SRM. 2 L 7 2 4F A6WE 2007100200135 20071002 00135 NM 2007 10 2 CALA0700527 1 20070921 A 5330 6573746 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70330 23460 INSPECTION FOUND A 1 INCH CRACK IN LEFT FUSELAGE SKIN AT STA 727E, S22L. THE SKIN WAS REPAIRED IAW SRM 53-00-01, FIGURE 201. 2 L 7 2 4F RT A16WE 2007100200145 20071002 00145 WP 2007 10 2 UPS07850706 1 20070911 A 5320 CUSP WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 CABIN STA 1040-1060 LBL 65 CUSP MEMBRANE WEB IS CRACKED AT FWD LIGHTNING HOLE. REPAIRED CUSP MEMBRAN E AT STA 1040-1060 LBL 65 IAW UPS EO DC8-5330- 2159-B. 2 L 7 4 4F RT 4A25 2007100200153 20071002 00153 NM 2007 10 2 UPS07M50713 1 20070803 A 5313 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C CTR CARGO COMPT AT STATION 5-120 LONGERON 44 LEFT FOUND SUSPECTED CRACKED ON DOUBLER. HFEC INSP C/OUT FOUND CRACK APPROX 1 INCH AS MARKED. CRACKED LONGERON SPLICE RMV'D AT CTR CARGO COMPT STA 5-120 LONG 44 LT. LONGERON SPLICE MACHINE FROM 1D1104-7150-T61511 EXTRUSION PER DOUGLAS DWG A5A7116. FPI C/OUT ON FAB SPLICE FOUND NO CRACK. FAB L ONGERON SPLICE HOLES PICKED UP, REPROTECTED, PAINTED & INSTALLED. 2 L 7 3 4F RT A22WE 2007100200165 20071002 00165 NM 2007 10 2 SWAA074763 1 20070923 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007100200168 20071002 00168 NM 2007 10 2 SWAA074769 1 20070923 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007100200171 20071002 00171 NM 2007 10 2 SWAA074748 1 20070923 A 2750 6557421 TORQUE TUBE BOEING 737 7373H4 1384600 NM T/E FLAP WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED A1 CHECK, FOUND LT WING INBOARD T/E FLAP DRIVE TORQUE TUBE WORN. REMOVED AND REPLACED TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007100200172 20071002 00172 NM 2007 10 2 SWAA074762 1 20070923 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007100200173 20071002 00173 NM 2007 10 2 SWAA074760 1 20070923 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 22R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007100200176 20071002 00176 WP 2007 10 2 WRLA2007092 1 20070923 A 5411 SPAR DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE NR 3 PYLON CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 303WL 46917 DURING C-5 CHECK, FOUND CRACK FROM NR 3 PYLON LOWER SPAR LT SIDE BESIDE FAN AIR DUCT FEED THROUGH. REF NR 64879. 10-12 -07 REPAIRED PER DC10 SRM VOL.1 54-20-00. 2 L 7 3 4F 4 F RT A22WE E23EA 2007100200178 20071002 00178 WP 2007 10 2 WRLA2007091 1 20070923 A 5245 SKIN DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE A/C BAY DOOR CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 303WL 46917 DURING C-5 CHECK, FOUND RIGHT AIR CONDITION COMPARTMENT DOOR SKIN PLATE AND INBOARD INTERCOSTAL CRACKED. REF NR 64867. 10-12-07 REPAIR PER DC10 SRM 52-00-01 FIG.4 VOL.1 AND SRM 52-42-01 FIG.1 VOL.3 REV.91. 2 L 7 3 4F 4 F RT A22WE E23EA 2007100200179 20071002 00179 2007 10 2 BB07076 4 20070925 A 2565 D30654122 SLIDE BOEING 757 7572B7 1384964 NM L1 DOOR LOW PRESSURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 936UW 4477 4477 27244 MCO - MAINTENANCE REPORTED THE L1 DOOR ESCAPE SLIDE BELOW LIMITS. MAINTENANCE REMOVED AND REPLACED THE L1 DOOR ESCAPE S LIDE. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2007100200180 20071002 00180 NM 2007 10 2 KCSA071398 1 20070925 A 5311 FRAME BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FUSELAGE FRAME WEB CRACKED AT BS 1265, STR 27L. 2 L 7 4 4F RT A20WE 2007100200182 20071002 00182 NM 2007 10 2 KCSA071401 1 20070925 A 5315 FLOORBEAM BOEING 747 7472B4B 138481B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 UPPER DECK FLOORBEAM DAMAGED AT BS 740, LBL 71. 2 L 7 4 4F RT A20WE 2007100200183 20071002 00183 NM 2007 10 2 KCSA071402 1 20070925 A 5340 STRINGER CLIP BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STRINGER CLIP CRACKED AT BS 440, STR 11L. 2 L 7 4 4F RT A20WE 2007100200184 20071002 00184 NM 2007 10 2 MASA200700453 1 20070725 A 2150 78279018 ACM DHAV DHC8 DHC8202 2809007 NM A/C BAY MALFUNCTIONED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 445YV 5360 445 ASH 7072 DEN. "RTG" DUE TO SMOKE IN COCKPIT. MX REPLACED ACM AND HEAT EXCHANGER. 2 H 7 2 4T RT A13NM 2007100200188 20071002 00188 NM 2007 10 2 MASA200700558 1 20070906 A 2435 23088008 STARTER GEN DHAV DHC8 DHC8202 2809007 NM NR 1 ENGINE MALFUNCTIONED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 987HA 6716 425 ASH FLT 2860 FLG-PHX. DECLARED EMERGENCY FOR NR 1 ENGINE FIRE ON ENGINE SHUT DOWN. WHEN THE CREW WAS SHUTTING THE ENGI NE DOWN THE CAPTAIN NOTICED SMOKE AND SPARKS COMING FROM THE NR 1 ENGINE. MX INSPECTED ENGINE AND FOUND NO EVIDENCE OF A FIRE, BUT FOUND THE DC STARTER GENERATOR IS BAD. THE DC STARTER GENERATOR IS WHAT CAUSED THE SMOKE AND SPARKS. MX IS CHANGING THE NR 1 DC STARTER GENERATOR. 2 H 7 2 4T RT A13NM 2007100200191 20071002 00191 NM 2007 10 2 KCSA071403 1 20070925 A 3350 LIGHT BOEING 747 747221F 1384868 NM COCKPIT INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 748CK 21744 EMERGENCY EXIT LIGHT ABOVE F/O'S SEAT INOP. 2 L 7 4 4F A20WE 2007100200194 20071002 00194 NM 2007 10 2 SWAA074786 1 20070924 A 5311 6546569 BELTFRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 1006, STR 27L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007100200195 20071002 00195 NM 2007 10 2 SWAA074789 1 20070924 A 5534 6547450 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND VERTICAL STABILIZER RT AND LT FITTING CORRODED. REPAIRED FITTING PER EA. 2 L 7 2 4F RT A16WE 2007100200196 20071002 00196 NM 2007 10 2 SWAA074794 1 20070924 A 5514 6551524 FITTING BOEING 737 7373H4 1384600 NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED 10Y CHECK, FOUND LT AND RT HORIZONTAL STABILIZER FITTING CLEVIS LUG FACES CORRODED. REPAIRED FITTING P ER BOEING SB. 2 L 7 2 4F RT A16WE 2007100200197 20071002 00197 NM 2007 10 2 SWAA074777 1 20070924 A 2560 655681911 DOOR BOEING 737 7373H4 1384600 NM COCKPIT OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 F/O'S ESCAPE ROPE DOOR DOES NOT OPEN. ADJUSTED DOOR PER MM. 2 L 7 2 4F RT A16WE 2007100200200 20071002 00200 NM 2007 10 2 SWAA074785 1 20070924 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED OTS CHECK, FOUND STRINGER 26R CORRODED AT BS 1006. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007100200202 20071002 00202 NM 2007 10 2 SWAA074783 1 20070924 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 771SA 27879 DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 7 ABC. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007100200203 20071002 00203 NM 2007 10 2 SWAA074782 1 20070924 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 771SA 27879 DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 1 ABC. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007100200205 20071002 00205 NM 2007 10 2 CALA0700538 1 20070925 A 5314 65621259 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND O/B SPLICE CORRODED ON RIGHT KEEL BEAM FORWARD OF STA 727, RBL 7, IN AFT BAG BIN. THE SPLICE WAS REMOV ED AND A NEW SPLICE ANGLE WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007100200206 20071002 00206 WP 2007 10 2 WRLA2007094 1 20070923 A 5720 VERTICAL SUPPORT DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE RT WING CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 303WL 46917 DURING C-5 CHECK, RT WING FIXED TRAILING EDGE 1 EACH VERTICAL SUPPORT CRACKED AT STA XORS 164-192. N/R 66448. 10-12-07 REPAIRED ACCORDING TO DWG ARC0295. 2 L 7 3 4F 4 F RT A22WE E23EA 2007100200207 20071002 00207 WP 2007 10 2 ABXA070322 1 20070920 A 5610 WINDOW DOUG DC9 DC933F 302207A WP COCKPIT OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED CAPTAIN'S CLEARVIEW WINDOW IAW DC9 MM 56-10-03-5. 2 L 7 2 4F A6WE 2007100200209 20071002 00209 NM 2007 10 2 ZZDA2007271 1 20070925 A 2710 655228611 BEARING BOEING 737 7377BD 1384511 NM CENTERING UNIT WORN A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 37 311AT 33930 DURING TAXI OUT ON THE FLIGHT CONTROL CHECKOUT AILERON CONTROL WHEEL IS BINDING AND WILL NOT RETURN TO NEUTRAL. FOUND W ORN BEARING IN ARM ASSY OF AILERON FEEL CENTERING UNIT. REMOVED AND REPLACED ARM ASSY REF B 737 AMM 27-11, PERFORMED AI LERON FEEL AND CTR UNIT ADJ/TEST, OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2007100200211 20071002 00211 NM 2007 10 2 PIDA07043 1 20070920 A 7830 THRUST REVERSER BOEING 737 737228 13844AG NM LT ENGINE DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 251TR 23792 DURING MAINTENANCE VISIT, NOTED DAMAGE TO LEFT ENGINE I/B THRUST REVERSER SKIN AND SUPPORT FRAME. REPAIRED PER PACE AIR LINES REPAIR PROCEDURE REPORT, EA 78-190. 2 L 7 2 4F RT A16WE 2007100200212 20071002 00212 WP 2007 10 2 WRLA2007101 1 20070926 A 2620 RING DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE EXTINGUISH SYS MISSING A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 303WL 46917 DURING C-CHECK FOUND NR 3 ENGINE FIRE EXTINGUISHING LINE JOINT RING MISSING. REF N/R 67308. 10-12-07 INSTALLED JOIN T RING REF DC10 AMM 26-21-04 REV.81. LEAK CHECKED REF DC10 AMM 26-21-04-201 REV.81. 2 L 7 3 4F 4 F RT A22WE E23EA 2007100200213 20071002 00213 NM 2007 10 2 KCSA071419 1 20070926 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 BS 560 LBL 65 WL 308 SEAT TRACK HAS CORROSION. 2 L 7 4 4F RT A20WE 2007100200214 20071002 00214 NM 2007 10 2 KCSA071420 1 20070926 A 5720 WEB BOEING 747 7472B4B 138481B NM RT WING GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 RIGHT WING I/B AILERON O/B HINGE SUPPORT WEB GOUGED AT WS 807. 2 L 7 4 4F RT A20WE 2007100200215 20071002 00215 NM 2007 10 2 KCSA071421 1 20070926 A 5320 INTERCOSTAL BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA 1265 INTERCOSTAL WEB AT UPPER BOLT HOLE HAS .25 INCH CRACK INDICATION STR 27L. 2 L 7 4 4F RT A20WE 2007100200217 20071002 00217 NM 2007 10 2 KCSA0701423 1 20070926 A 5313 FITTING BOEING 747 7472B4B 138481B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA 1240 STR 26L FWD STRINGER FITTING DAMAGED. 2 L 7 4 4F RT A20WE 2007100200219 20071002 00219 NM 2007 10 2 HNAA0700178 1 20070924 A 3260 DSC1822 RELAY DHAV DHC8 DHC8102 2809003 NM LANDING GEAR FAILED A HNAA O OTHER N FALSE WARNING AP APPROACH 1 EA 07 810EX 308 AFTER GEAR EXTENSION GEAR DOOR AMBER LIGHT REMAINED ON FOR APPROX 20 TO 30 SECONDS AN WENT OUT. HAPPENED EARLIER THAT D AY. CREW CONFIRMED DOORS OPEN, FERRY TO SBY TO SWAP WITH SPARE. REMOVED AND REPLACED RELAY P/N DSC182-2, OPS CHECK GOO D. 2 H 7 2 4T RT A13NM 2007100200221 20071002 00221 EA 2007 10 2 COMA0770052 1 20070923 A 2782 ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA L/E SLAT TRIPPED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 378CA 10097 FLIGHT 5172 - SLAT FAIL MESSAGE RECEIVED ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND LEFT NR 2 SLA T ACTUATOR TRIPPED. RESET ACTUATOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007100200222 20071002 00222 EA 2007 10 2 COMA0760576 1 20070918 A 2751 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 783CA 21005 7315 FLIGHT 5366 - FLAP FAIL MESSAGE RECEIVED AFTER LANDING. REPLACED LEFT BPSU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007100200223 20071002 00223 EA 2007 10 2 COMA0760577 1 20070918 A 2750 860D10018 ECU CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 523CA 10513 7821 FLIGHT 5561 - RECEIVED FLAP FAIL MESSAGE ON APPROACH. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED FECU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007100200224 20071002 00224 EA 2007 10 2 COMA0760578 1 20070919 A 2170 P1096 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA A/C BAY DIRTY A COMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 926CA 7027 FLIGHT 5506 - SMOKE IN COCKPIT AND CABIN NOTED WHEN PACKS TRANSFERRED TO APU. DECLARED EMERGENCY. EVACUATED PASSENGERS ON TAXIWAY. FOUND RIGHT COALESCER BAG WET WITH OIL. REPLACED BAG. FOUND OIL LEVEL SERVICEABLE ON BOTH ENGINES AND AP U. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007100200225 20071002 00225 EA 2007 10 2 COMA0760579 1 20070920 A 2751 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 783CA 11936 7315 FLIGHT 5199 - RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED EO 27-046AD AND REPLA CED LEFT BPSU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007100200226 20071002 00226 EA 2007 10 2 COMA0760580 1 20070920 A 2797 WIRE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT LOOSE A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 786CA 7333 FLIGHT 5671- AT 40 KTS RECEIVED STAB TRIM CAUTION MESSAGE. ABORTED TAKEOFF AND RETURNED TO THE GATE. RESOLDERED LOOSE WIRE ON CAPTAIN'S PITCH DISCONNECT SWITCH. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007100200227 20071002 00227 EA 2007 10 2 COMA0760581 1 20070923 A 7931 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT UNKNOWN A COMA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 01 958CA 7111 FLIGHT 5330 - ON TAKEOFF NOTED THAT NR 1 ENGINE OIL PRESSURE READ ZERO. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. RESET CIRCUIT BREAKER 1M1. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007100200228 20071002 00228 EA 2007 10 2 COMA0760582 1 20070923 A 2751 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 785CA 15790 7326 FLIGHT 5699 - RECEIVED FLAP CAUTION MESSAGE. LANDED WITHOUT INCIDENT. REPLACED LEFT BPSU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007100200229 20071002 00229 EA 2007 10 2 COMA0760583 1 20070923 A 3234 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 819CA 13298 7415 FLIGHT 5452 - RECEIVED NOSE GEAR DISAGREE ON EXTENSION. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED NLG SELE CTOR VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007100200231 20071002 00231 NM 2007 10 2 BB07077 1 20070927 A 3350 LIGHT BOEING 767 767201 1385125 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 246AY 23898 BCN - WHILE ACCOMPLISHING DAILY CHECK MAINTENANCE FOUND 03EA EMERGENCY ESCAPE PATH LIGHTING FILAMENTS EXTINGUISHED AT 1F G/ 2FG/ 10FG LOCATIONS. MAINTENANCE REPLACED EMERGENCY ESCAPE PATH LIGHTING MODULE FILAMENTS. 2 L 7 2 4F RT A1NM 2007100200232 20071002 00232 EA 2007 10 2 TRAX200701384 1 20070923 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 880AS 7606 SERVICE DOOR IS VERY HARD TO OPEN AND CLOSE, F/A IS UNABLE TO OPEN SERVICE DOOR. 2 L 7 2 4F RT A21EA 2007100200234 20071002 00234 EA 2007 10 2 TRAX200701386 1 20070923 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 878AS 7590 EXIT EMERGINCY LIGHT FOR MAIN PASS DOOR INOP. 2 L 7 2 4F RT A21EA 2007100200235 20071002 00235 NM 2007 10 2 CALA0700539 1 20070922 A 5330 143N31511 SKIN BOEING 757 75733N 1384931 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 57864 32588 LIGHTNING STRIKE DAMAGE WAS DISCOVERED ON THE FUSELAGE SKIN JUST FORWARD OF THE TEAR STRAP AT BS 580 BETWEEN STRINGER 7L AND 8L WHILE AIRCRAFT WAS IN A 4C CHECK AT MCO. THE DAMAGE WAS REPAIRED IAW ECRA 5331-01349. 2 L 7 2 4F RT A2NM 2007100200236 20071002 00236 NM 2007 10 2 SWAA074815 1 20070926 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED HC1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007100200237 20071002 00237 NM 2007 10 2 SWAA074814 1 20070926 A 3350 20131A BATTERY PACK BOEING 737 7373K2 13844BA NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED SPV CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007100200239 20071002 00239 NM 2007 10 2 SWAA074817 1 20070926 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 472WN 33831 DURING SCHEDULED HC1 CHECK, FOUND EEPLS LENS CRACKED AT ROW 3 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007100200242 20071002 00242 2007 10 2 SWAA074828 4 20070926 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 782SA 29808 DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007100200243 20071002 00243 NM 2007 10 2 SWAA074829 1 20070926 A 2730 6545187 TORQUE TUBE BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, LEFT ELEVATOR OUTPUT TORQUE TUBE FAILED FREE PLAY CHECK. REMOVED AND REPLACED TORQUE TUBE P ER MM. 2 L 7 2 4F RT A16WE 2007100200244 20071002 00244 NM 2007 10 2 SWAA074824 1 20070926 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 494, STR 26R. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2007100200245 20071002 00245 NM 2007 10 2 SWAA074818 1 20070926 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 471, STR 17R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007100200246 20071002 00246 NM 2007 10 2 SWAA074832 1 20070926 A 5311 6546549 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007100200248 20071002 00248 NM 2007 10 2 SWAA074821 1 20070926 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007100200251 20071002 00251 NM 2007 10 2 SWAA074830 1 20070926 A 5315 6935366 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 539, RBL 25. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2007100200252 20071002 00252 NM 2007 10 2 SWAA074833 1 20070926 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER 28L CRACKED AT BS 374. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007100200253 20071002 00253 2007 10 2 SWAA074822 4 20070926 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007100200254 20071002 00254 NM 2007 10 2 SWAA074827 1 20070926 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 774SW 27882 DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT LIGHT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007100200255 20071002 00255 NM 2007 10 2 SWAA074825 1 20070926 A 5524 DAS1026B1502 BEARING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED 10Y CHECK, LEFT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED HORN BEARING PER MM. 2 L 7 2 4F RT A16WE 2007100200256 20071002 00256 NM 2007 10 2 SWAA074826 1 20070926 A 2560 PH22300L GLOWSTRIP BOEING 737 7373Q8 1384670 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 EEPLS PHOTOLUMINESCENT STRIP LOOSE BETWEEN ROW 5 ABC AND ROW 8 ABC. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007100200257 20071002 00257 NM 2007 10 2 SWAA074823 1 20070926 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 607SW 27927 DURING SCHEDULED BRDG CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 9 DEF. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007100200259 20071002 00259 NM 2007 10 2 KCSA071426 1 20070927 A 5412 BULKHEAD BOEING 747 747246F 1384850 NM NR 4 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 NR 4 PYLON STA 221.9 BULKHEAD WEB WHERE HYD LINE GOES THROUGH IS CRACKED .5 INCH. 2 L 7 4 4F RT A20WE 2007100300021 20071003 00021 CE 2007 10 3 SX42007F00000 1 20070827 A 2140 CONTROLLER RAYTHN 390 390 7150030 CE WILINT FJ44 FJ442A GL BLEED HEAT MALFUNCTIONED E SX4A O OTHER O OTHER NR NOT REPORTED 1 WP 07 6150Y RB150 FAILURE OF BLEED HEAT TEMP CONTROL SYSTEM LT AND RT. BOTH SIDE ENUNCIATED OVERHEAT. SELECTED BLEEDS OFF, RETURNED TO D EPARTURE. LANDING UNEVENTFUL. (K) 1 L 7 2 3F 4 F RT A00010WI E3GL 2007100300027 20071003 00027 NE 2007 10 3 QXEA200701419 2 20070915 A 7320 4120T00P37 FADEC CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE NR 2 ENGINE MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 617QX 13146 10131 NR 2 ENGINE WILL NOT START. RETURNED TO THE GATE. MAINTENANCE REPLACED THE FADEC. OPERATIONAL CHECKS GOOD. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007100300028 20071003 00028 SO 2007 10 3 SIMA200727404 1 20070928 A 3240 0132AFU1 SENSOR EMB 135 EMB135KL 3260302 SO NR 3 BRAKE MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 805AE 145489 IN CLIMB, RIGHT INBOARD BRAKE OVERHEAT EICAS MSG CON ON. TEMP CAME DOWN THEN TEMP WENT BACK UP TO TOP OF GAUGE THEN WEN T BLANK THEN GAUGES NORMAL IN GREEN. RETURNED TO SJC. AFT LANDED BRAKE TEMP OVERHEAT EICAS MESSAGE APPEARED AGAIN. TE MP GAUGE TO MAX ON TAXI TO GATE GAUGE WENT TO FULL HOT TO NORM BACK TO HOT. LANDING VSI AT 300 FPM AND 40,500 LBS. NO MTX REQ FOR OVERWEIGHT LANDING. REMOVED AND REPLACED RIGHT HAND NR 3 BRAKE TEMP SENSOR IAW EMB AMM 32-47-01 OPERATION AL CHECK GOOD AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT T00011AT 2007100300029 20071003 00029 NE 2007 10 3 UPS07650667 2 20070916 A 7200 ENGINE BOEING 767 76734AF 1385212 NM GE CF6 CF680C2B7 NE NR 1 BIRD INGESTION A IPXA O OTHER C F.O.D. AP APPROACH 1 SO 01 314UP 27742 INSPECTION TYPE: ETOP FOD - BIRD STRIKE NR 1 ENGINE. EMERGENCY DECLARED. ON SHORT FINAL CREW REPORTED BIRD INGESTION IN NR 1 ENGINE. ENGINE VIBRATION REACHED 3.8 AND WAS REDUCED TO IDLE. A/C IS OOS. FOUND DAMAGE BLADES 24,25,26,27 BE YOND REPAIR. INSTALLED BLD INGT POS 7-178310 & INT IN POS 26, INST NEW 177208IN POS 6, INST NEW 178246 IN POS 7, INST NE W 177486 IN POS 27, ALL AS PER AMM 72-31-02-4. 2 L 7 2 4F 4 F RT A1NM E13NE 2007100300031 20071003 00031 EA 2007 10 3 QXEA200701488 1 20070924 A 3250 4480000501 ECU CNDAIR CL600 CL6002C10 1390015 EA NLG STEERING FAILED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 609QX 9526 10031 TUL - RETURN TO THE GATE FOR THE NOSE WHEEL STEERING CAUTION LIGHT, MAINTENANCE RESET FAILED. FERRIED THE AIRCRAFT TO P DX WHERE THE ECU AND STEERING MANIFOLD WERE REPLACED. OPERATIONAL CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007100300032 20071003 00032 NM 2007 10 3 QXEA200701489 1 20070930 A 6123 AUTOFEATHER SYS BOMBDR DHC8 DHC8402 1390042 NM PROPELLER MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 403QX 4037 SEA - ON FLIGHT 2484, RETURNED TO GATE. AUTOFEATHER SELECT DID NOT ILLUMINATE ON ED. SWITCH LIGHT SELECT ILLUMINATED. MAINTENANCE INTERROGATED CDS FOR AUTOFEATHER FAULTS AND FOUND 494A AND 494B ON BOTH NR 1 AND 2 PEC'S. CLEARED FAULTS B Y COMPLYING WITH OPERATIONAL TEST OF THE PROP AUTOFEATHER AND UP TRIM SYSTEM. AIRCRAFT RETURNED TO SERVICE. NO PARTS R EPLACED. 2 H 7 2 4T RT A13NM 2007100300033 20071003 00033 NM 2007 10 3 QXEA200701490 1 20070928 A 3010 4100S00503 VALVE BOMBDR DHC8 DHC8402 1390042 NM DEICE SYSTEM INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 1862 1862 4050 EUG - DE-ICE PRESSURE CAUTION LIGHT ILLUMINATED. CHECKLIST WAS RAN, CAUTION LIGHT EXTINGUISHED. RAN BOOTS IN MANUAL RI GHT INBOARD BOOT ON TAIL NOT ILLUMINATING LIGHT TESTS GOOD AND DEICE PRESSURE GOOD. MAINTENANCE REPLACED DDV NR 5. OPE RATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007100300034 20071003 00034 NM 2007 10 3 QXEA200701491 1 20070929 A 2910 4213402 POWER UNIT BOMBDR DHC8 DHC8402 1390042 NM HYD SYSTEM INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 413QX 12799 12799 4060 GEG - ON FLIGHT 2353, RETURNED TO GATE, STANDBY HYDRAULIC PRESSURE INDICATES ZERO PRESSURE. MAINTENANCE REMOVED AND REP LACED STANDBY POWER UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007100300035 20071003 00035 NM 2007 10 3 QXEA200701492 1 20071001 A 2760 3958001005 VALVE BOMBDR DHC8 DHC8402 1390042 NM SPOILERS INOPERATIVE A QXEA O OTHER J WARNING INDICATION LD LANDING 1 NM 09 412QX 14984 14984 4059 SEA - ON FLIGHT 2297, MASTER CAUTION ROLL SPOILER INBOARD GROUND CAUTION ILLUMINATED ON LANDING, ROLL DID NOT RESET WITH CHECKLIST. MAINTENANCE REMOVED AND REPLACED INBOARD LIFT DUMP VALVE. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SER VICE. 2 H 7 2 4T RT A13NM 2007100300036 20071003 00036 NM 2007 10 3 HALA0700414 1 20070926 A 3150 WARNING LIGHT BOEING 767 767332 1382001 NM ILLUMINATED A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, BTB NO FUEL TOTAL INDICATION. FUEL QTY BITE NUISANCE MSG. NO FAULTS NOTED. OK TO CONTINUE PE R BOEING SERVICE LETTER 767-SL-31-032. 2 L 7 2 4F RT A1NM 2007100300037 20071003 00037 NM 2007 10 3 HALA0700416 1 20070915 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 1076-1400 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 LEVEL 1 CORROSION ON SEAT TRACK RBL 88.5 NUMEROUS AREAS BETWEEN STA 1076 AND 1400. REPLACED SEAT TRACK. 2 L 7 2 4F RT A1NM 2007100300038 20071003 00038 NM 2007 10 3 HALA0700417 1 20070927 A 5720 FAIRING BOEING 767 76733A 1385209 NM RT WING CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 CRACK ON RT WING TRAILING EDGE UPPER FIXED FAIRING SUPPORT BEAMS AT WS 1030, WS 1100, AND WS 1178 ABOVE AND FWD OF OUTER AILERON. REPAIRED BY REPLACEMENT WITH REF TO 767-300 SRM 51-40-02 AND BOEING DWG 113T1913, P/N 113T1913-24 AND 113T913 -26. 2 L 7 2 4F RT A1NM 2007100300039 20071003 00039 NM 2007 10 3 HALA0700418 1 20070927 A 5315 FLOORBEAM BOEING 767 76733A 1385209 NM BS 246 CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 CRACK ON FLOORBEAM AT BS 246 ON VERTICAL STIFFENER AT LBL 40 BELOW MID CHORD. REPAIRED IAW 767-300 SRM 53-10-51 FIG 206 REPAIR 2. 2 L 7 2 4F RT A1NM 2007100300040 20071003 00040 NM 2007 10 3 HALA0700415 1 20070926 A 4940 5198588 STARTER BOEING 767 76733A 1385209 NM APU FAILED A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM, APU FAILED TO START, FAULT LGT ILLUM AND EICAS MSG APU FAULT DISPLAYED, ADDITIONAL START ATTEM PTS UNSUCCESSFUL. ACCOMP FIM 49-11-00, APU ECU BITE HAD A/C START CIRCUIT MSG, REPLACED APU STARTER PER AMM 49-41-01 AN D START CIRCUIT RELAY K197. OPS AND LEAK CHK GOOD. RELAY REMOVED AND REPLACED PER FIM 49-11-00, SECURED APU DOORS, FAU LT MSG CLEARED, OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007100300041 20071003 00041 NE 2007 10 3 QXEA200701443 2 20070919 A 7530 ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE NR 2 ENGINE LEAKING A QXEA O OTHER K FLUID LOSS NR NOT REPORTED 1 NM 09 606QX 10023 PDX - CREW REPORTS FUEL DRIPPING FROM THE NR 2 ENGINE COWLING. MAINTENANCE REPLACED THE SLAVE COMPRESSOR VG ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007100300042 20071003 00042 EA 2007 10 3 QXEA200701417 1 20070913 A 3260 496501 SWITCH CNDAIR CL600 CL6002C10 1390015 EA MLG MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 617QX 10686 10130 DEN - JUST PRIOR TO TAKING THE RUNWAY FOR TAKEOFF, RECEIVED A RIGHT GEAR FAULT MESSAGE. MAINTENANCE REPLACED THE RIGHT PRESSURE SWITCH RESTRICTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007100300043 20071003 00043 SO 2007 10 3 SIMA200727401 1 20070927 A 3244 31641 TIRE EMB 135 EMB135KL 3260302 SO MLG DEFLATED A SIMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 803AE 145483 AFTER LANDING, DURING TAXI IT TOOK MORE POWER THAN NORMAL TO TAXI. A BRAKE OVERHEAT INDICATION WAS OBSERVED ON EICAS. NR 3 TIRE WAS FOUND TO BE FLAT. REMOVED AND REPLACED NR 3 MLG WHEEL AND TIRE ASSY IAW WORK CARD NR 32-700-11 2. REMOVE D AND REPLACED NR 3 MLG BRAKE ASSY IAW WORK CARD NR 32-600-14 3. REMOVED AND REPLACED NR 4 MLG WHEEL AND TIRE ASSY IAW WORKCARD NR 32-700-11. NR 3 BRAKE PN-21707 SN-0100 NR 4 MLG TIRE PN-31641 SN-1872. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007100300044 20071003 00044 EA 2007 10 3 SIMA200727402 1 20070929 A 5720 FAIRING CNDAIR CL600 CL6002C10 1390015 EA TE FLAP LOOSE A SIMA O OTHER E VIBRATION/BUFFET DE DESCENT 1 SW 21 500AE 10025 NOISE FROM UNDER FLOOR AT ROWS 11 - 13/VIBE HEARD IN COCKPIT AND FELT IN YOKE. WHILE PERFORMING VIBRATION INSPECTION WC 05-005 FOUND LEFT AND RIGHT FLAP STAB FAIRINGS LOOSE. RESECURED LEFT AND RIGHT FLAP STAB FAIRINGS IAW CRJ AMM 53-82-82 . C/W VIBRATION WORK CARD 05-005. FCF SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007100300045 20071003 00045 SO 2007 10 3 SIMA200727403 1 20070928 A 3350 20131A POWER SUPPLY EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHT INOPERATIVE A SIMA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 856AE 145748 AFT HALF OF CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 4 BATTERY POWER SUPPLY IAW EMB-140 AMM 33-50-04. OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007100300046 20071003 00046 SO 2007 10 3 SIMA200727405 1 20070925 A 2613 0132AFU2 SENSOR EMB 145 EMB145LR 3260212 SO BRAKE TEMP INOPERATIVE A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 616AE 145092 ON TAKEOFF, CREW OBSERVED "BRAKE OVERHEAT" MESSAGE ON EICAS WITH THE NUMBER 2 BRAKE TEMP INDICATION INOP. CREW ABORT TA KEOFF AND RETURN TO THE GATE. C/A ISSUED MEL 32-03. MTX REMOVED AND REPLACED NR 2 BRAKE TEMP SENSOR IAW EMB 145 AMM 32- 47-01. OP CK GOOD MEL 090962-C. RESTORED AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007100300047 20071003 00047 SO 2007 10 3 SIMA200727406 1 20070928 A 3350 LIGHT EMB 135 EMB135KL 3260302 SO CABIN INOPERATIVE A SIMA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 856AE 145748 HALF OF CABIN EMERGENCY LIGHTS INOP DISC, AWAITING LOG PAGE FOR ACTUAL DISC. 2 L 7 2 4F RT T00011AT 2007042300005 20070423 00005 EA 2007 4 23 VNAA0703022 1 20070330 A 4930 FUEL SYS CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE APU LEAKING A VNAA F ACTIVATE FIRE EXT. K B A FLUID LOSS SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE IN INSP/MAINT 1 GL 05 237PS 7906 MAINTENANCE REPORTED SMELLING FUMES WHILE INSIDE THE COCKPIT AFTER TROUBLESHOOTING THE APU AND THE APU RUNNING. MAINTEN ANCE INVESTIGATED AND FOUND THE APU ON FIRE. FIRE WAS EXTINGUISHED USING THE APU FIRE BOTTLE. MAINTENANCE INSPECTED AN D FOUND A FUEL LEAK IN THE APU COMPARTMENT. THE APU WAS INSPECTED AND DEFERRED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007042300006 20070423 00006 NM 2007 4 23 AALA20070606 1 20070405 A 3350 0201720003 LIGHT BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 181AN 29591 ORD - EMERGENCY LIGHT AT FLOOR AT SEAT 17D MISSING COVER AND BULB. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FLOOR AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007042300007 20070423 00007 NM 2007 4 23 AALA20070607 1 20070405 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 662AA 25296 MIA - EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A2NM 2007042300013 20070423 00013 NM 2007 4 23 AALA20070605 1 20070404 A 3010 ANTI-ICE VALVE BOEING 767 767323 1385205 NM RT WING MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 389AA 27449 MIA INFLIGHT - DURING CLIMB, RECEIVED RIGHT WING ANTI-ICE EICAS MESSAGE WITH ASSOCIATED VALVE LIGHT. TURNED ON WING ANT I-ICE AND VALVE LIGHT AND EICAS MESSAGE WENT OUT. AFTER APPROXIMATELY TWO MINUTES LEFT VALVE EICAS MESSAGE ILLUMINATED AND LEFT BLEED AND LEFT PACK INOPERATIVE. LANDED MIA WITHOUT INCIDENT. REPLACED RIGHT WING ANTI-ICE VALVE. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007042300016 20070423 00016 NM 2007 4 23 AALA20070610 1 20070405 A 3350 LENS BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 198AA 32392 DFW - EMERGENCY LIGHT AT SEAT 33D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 33D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007042300020 20070423 00020 NM 2007 4 23 AALA20070583 1 20070330 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 604AA 27055 DFW - EMERGENCY LIGHT AT SEAT 29D INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 29D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2007042300022 20070423 00022 NM 2007 4 23 AALA20070577 1 20070330 A 2560 SIGN BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 662AA 25296 MIA - EMERGENCY EXIT SIGN ABOVE LEFT NUMBER FOUR DOOR MISSING. REPLACED EMERGENCY EXIT SIGN ABOVE LEFT NUMBER FOUR DOOR . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007042300024 20070423 00024 NM 2007 4 23 AALA20070572 1 20070329 A 7711 TRANSMITTER BOEING 757 757223 1384957 NM EPR MALFUNCTIONED A AALA O OTHER O OTHER DE DESCENT 1 SW 21 657AM 24615 SEA INFLIGHT T1661/29MAR - EMERGENCY DECLARED ON DESCENT INTO SEA DUE TO LEFT ENGINE PRESSURE RATIO FLUX. UNABLE TO CON TROL ENGINE THRUST. LANDED SEA WITHOUT INCIDENT. REPLACED LEFT ENGINE PRESSURE RATIO TRANSMITTER. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007042300027 20070423 00027 NM 2007 4 23 AALA20070587 1 20070401 A 2421 IDG BOEING 757 757223 1384957 NM LT ENGINE MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 654A 24612 JFK INFLIGHT T1567/01APR - DURING CLIMB, LEFT ENGINE GENERATOR DRIVE LIGHT ILLUMINATED BUT GENERATOR NEVER WENT OFF LINE . APU WAS ON PLACARD. EMERGENCY DECLARED. LANDED JFK OVERWEIGHT WITHOUT INCIDENT. REPLACED INTEGRATED DRIVE GENERATO R FOR LEFT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007042300032 20070423 00032 NM 2007 4 23 AALA20070592 1 20070401 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 656AA 24614 MIA - EMERGENCY LIGHT AT SEAT 28D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A2NM 2007042300040 20070423 00040 NM 2007 4 23 AALA20070616 1 20070408 A 3350 BPS73 BATTERY PACK BOEING 767 767223 1385123 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 322AA 22323 LAX - EMERGENCY LIGHT AT SEAT 31AB INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT 31AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007042300042 20070423 00042 NM 2007 4 23 AALA20070617 1 20070409 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 628AA 24586 MIA - EMERGENCY LIGHTS FROM SEAT ROWS 17 TO 25 INOPERATIVE. CHARGED BATTERY PACKS FOR EMERGENCY LIGHTS FROM SEAT ROWS 1 7 TO 25. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007042300046 20070423 00046 NM 2007 4 23 AALA20070626 1 20070411 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 776AN 29582 DFW - EMERGENCY LIGHT AT FIRST CLASS GALLEY RIGHT CORNER AT FLOOR INOPERATIVE. REPLACED EMERGENCY LIGHT AT FIRST CLASS GALLEY RIGHT CORNER AT FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007042300051 20070423 00051 NM 2007 4 23 AALA20070596 1 20070402 A 2613 OVERHEAT LOOP BOEING 737 737823 13844BZ NM OVERHEAT DETECT FAULTY A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 931AN 30079 MIA INFLIGHT - DURING CLIMB, LEFT WING BODY OVERHEAT LIGHT ILLUMINATED. ISOLATED LEFT SIDE BUT LIGHT ILLUMINATED AGAIN . RETURNED TO MIA AND LANDED WITHOUT INCIDENT. FOUND FAULTY LOOP M268. REPLACED OVERHEAT LOOP M268. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042300053 20070423 00053 NM 2007 4 23 AALA20070598 1 20070402 A 3697 TERMINAL BOEING 767 767323 1385205 NM REGULATOR VALVE BROKEN A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 383AN 26995 LIM INFLIGHT T912/02APR SCL TO MIA - CREW REPORTED A LEFT ENGINE BLEED DUCT LEAK INDICATION. LANDED LIM WITHOUT INCIDE NT. FOUND BROKEN TERMINAL AT LEFT PRESSURE REGULATOR VALVE AT POINT ONE. REPLACED TERMINAL. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A1NM 2007042300060 20070423 00060 NM 2007 4 23 AWXA200700495 1 20070409 A 5320 69353654 ATTACH ANGLE BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - CABIN FLOOR WEB ATTACH ANGLE CRACKED, BS 380 - BS 400, BL 0, WL 208. REPLACED CABIN FLOOR WEB ATTACH ANGLE, BS 38 0 - BS 400, BL 0, WL 208 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007042300065 20070423 00065 NM 2007 4 23 AWXA200700483 1 20070412 A 5210 69698541 WEB BOEING 737 7373G7 1384595 NM R1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 MIA - R1 DOOR AFT LOWER CORNER WEB, CRACKED, BS 344, S13R, WL 209.80. REPAIRED R1 DOOR AFT LOWER CORNER WEB, CRACKED, BS 344, S13R, WL 209.80 IAW B737-300 SRM 51-70-13. 2 L 7 2 4F RT A16WE 2007042300076 20070423 00076 NM 2007 4 23 DL76G070328 1 20070415 A 2730 2827001011 ACTUATOR BOEING 767 7673P6 1385105 NM PWA 4060 PW4060 52119 NE LT ELEVATOR LEAKING A DALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 27 155DL 25269 724639 FLT 128/15 NOTIFIED MTC AT APPROX 2300E THAT RT SYS HYD WAS DOWN TO .43 AND FALLING. HAD CREW TURN OFF RT HYD AND FLUID LOSS STOPPED. CREW DECIDED TO DIVERT TO BOS. AFTER BOS MTC INSPECTED AIRCRAFT FOUND THE LEFT ELEVATOR-RT SYS PCA LEAK ING HYD FLUID. REMOVED AND REPLACED LT ELEVATOR RT HYD SYS CTR POSITION PCA. OPS CHK AND LEAK CHK OK. ALL PER AMM. A LL RII REQUIREMENTS MET QC4021. 2 L 7 2 4F 4 F RT A1NM E24NE 2007042300080 20070423 00080 NM 2007 4 23 EIA2007053 1 20070309 A 5312 PRESSURE PANEL BOEING 747 747212B 1384886 NM NLG WW CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 485EV 20712 NOSE WHEEL WELL WEB CRACKED BETWEEN STA 265-280 LT SIDE AT WL 160. REMOVED DAMAGE, NDT'D AREA, FABRICATED AND INSTALLED REPAIR PER B747 SRM 53-10-04 FIGURE 116 PAGES 708-711. 2 L 7 4 4F A20WE 2007042300086 20070423 00086 NM 2007 4 23 EIA2007059 1 20070321 A 3350 51356B37 LIGHT BOEING 747 747132 1384882 NM PWA JT9 JT9D* NE CABIN INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481EV 19896 EMERGENCY EXIT LIGHT FOUND INOP DURING MAINTENANCE. REPAIRED PER MM 33-51-07, OPS CKD GOOD PER 33-51-00. 2 L 7 4 4F 4 F A20WE E20EA 2007042300088 20070423 00088 NM 2007 4 23 EIA2007031 1 20070223 A 2611 SMOKE DETECTOR BOEING 747 747273C 1384896 NM CARGO BAY MALFUNCTIONED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 471EV 20651 MAIN CARGO SMOKE DETECTOR 1A FAILED TEST. DEFFERED PER MEL 26-11. UNABLE TO DUPLICATE, SYSTEM OPS CHK GOOD PER MM 31-2 0-00. 2 L 7 4 4F A20WE 2007042300089 20070423 00089 NM 2007 4 23 EIAA2007032 1 20070303 A 3240 4308DA4 METERING VALVE BOEING 747 747273C 1384896 NM BRAKE SYS DEFECTIVE A EIAA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 NM 09 470EV 20653 WHEN APPLYING PARKING BRAKE, PRESSURE DROPS FROM 3000 TO 1000 ON APPROX 50 SEC, T/S IN PROGRESS WITH SHUTTLE VALVE AND B REAK MODULE. REMOVED AND REPLACED PARKING BRAKE VALVE, INTERCONNECT VALVE, LEFT AND RIGHT METERING VALVES. SYSTEM LEAK AND OPS CHK NORMAL PER MM32-41-00. NORMAL OPERATION OF SYSTEM VERIFIED ON TAXI CHECK. 2 L 7 4 4F A20WE 2007042300090 20070423 00090 NM 2007 4 23 EIA2007041 1 20070222 A 5711 SPAR BOEING 747 747SR46 1384816 NM RT WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 RIGHT WING FRONT SPAR LOWER CHORD AT FSSO 1341 HAS CORROSION ON FORWARD SIDE OF THE VERTICAL FLANGE. REMOVED CORROSION, NDT'D AREA, FABBED AND INSTALLED REPAIRS AT FORWARD SIDE VERTICAL FLANGE FSSO 1261-1331 AND 1341 PER ECRA 477-57-118-2. 2 L 7 4 4F RT A20WE 2007042300094 20070423 00094 NM 2007 4 23 EIA2007045 1 20070220 A 5330 SKIN BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 RIGHT UPPER FUSELAGE FLAT SIDE SKIN CRACKED AT STATION 370 STRINGER 8R. REMOVED DAMAGE, NDT'D AREA, FABBED AND INSTALLE D REPAIR PER ECRA 477-53-115-2. 2 L 7 4 4F RT A20WE 2007042300098 20070423 00098 NM 2007 4 23 EIA2007049 1 20070220 A 5313 STRINGER BOEING 747 747SR46 1384816 NM FUSELAGE GOUGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 RIGHT FUSELAGE STATION 370 STRINGER 8R GOUGED ON UPPER FLANGE. REMOVED AND REPLACED STRINGER PER B747 SRM 53-10-03 FIGU RE 3 DETAIL IV ALTERNATIVE II 9-10H. 2 L 7 4 4F RT A20WE 2007042300099 20070423 00099 NM 2007 4 23 EIA2007050 1 20070208 A 5730 SKIN BOEING 747 747SR46 1384816 NM RT WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 RIGHT WING LEADING EDGE SKIN CORRODED ON UPPER SURFACE AT FFSO 1405. REMOVED CORROSION, NDT'D AREA, FABBED AND IN STALLED REPAIR PER B747 57-30-03 PAGE 9-13. 2 L 7 4 4F RT A20WE 2007042300100 20070423 00100 NM 2007 4 23 EIA2007051 1 20070305 A 3350 900835A BATTERY PACK BOEING 747 747212B 1384886 NM CABIN DISCHARGED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486EV 20888 UPPER DECK SERVICE DOOR EMERGENCY LIGHT INOP. REPLACE BATTERY PACK, OPS CHECK GOOD PER MM 34-44-01. 2 L 7 4 4F A20WE 2007042300103 20070423 00103 SO 2007 4 23 SIMA200710606 1 20070413 A 2130 FITTING EMB 145 EMB145LR 3260212 SO CABIN PRESSURE UNKNOWN A SIMA A I UNSCHED LANDING CABIN DEPRESSURIZATION O OTHER CL CLIMB 1 SW 21 900AE 14500885 AIRCRAFT WOULD NOT PRESSURIZE IN BOTH AUTO OR MANUAL. REMOVED OUTFLOW VALVES HOLD OPEN CLIPS AND PERFORMED OPERATIONAL TEST OF PRESSURIZATION CONTROL SYSTEM IN BOTH MODES WITH NO DEFECTS. 2 L 7 2 4T RT T00011AT 2007042300105 20070423 00105 EA 2007 4 23 SIMA200710608 1 20070413 A 3610 GG670800025 SHUTOFF VALVE CNDAIR CL600 CL6002C10 1390015 EA LT ENGINE FAILED A SIMA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 521AE 5838 10142 LEFT COWL ANTI-ICE DUCT WARNING ILLUMINATED, ENGINE SHUTDOWN. EMERGENCY DECLARED, DIVERTED TO BNA. REMOVED AND REPLACE D PRESSURE SHUTOFF VALVE IAW CRJ AMM 36-12-05 WITH NO DEFECTS NOTED. REMOVED AND REPLACED LEAK TRANSDUCER IAW CRJ AMM 3 0-22-03 WITH NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007042300114 20070423 00114 SO 2007 4 23 SIMA200710703 1 20070408 A 5315 14521721009 FLOORBEAM EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 800AE 13129 4800 145425 GALLEY FLOOR DIGITAL FOUND CORRODED. PERFORMED CUTOUT OF CORRODED AREA. REPLACED CORRODED AREA IAW EMB SRM 53-21-10, F IGURE 201. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300117 20070423 00117 SO 2007 4 23 SIMA200710707 1 20070413 A 5320 13500436001 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AE 15775 4800 145275 LEFT OMEGA BEAM AT CROSSMEMBER BETWEEN FRAMES 33 AND 34 CORRODED. PERFORMED CUTOUT, FABRICATED AND INSTALLED DOUBLER IA W EMB SRM 53-00-10, FIGURE 202. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300123 20070423 00123 SO 2007 4 23 SIMA200710705 1 20070410 A 5320 14522178005 SILL EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 800AE 13129 4800 145425 SERVICE DOOR SILL FOUND CORRODED. BLENDED AND TREATED AREA AND INSTALLED REPAIR DOUBLER BLEND AREA IAW EMB SRM 53-21-02 . RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300124 20070423 00124 SO 2007 4 23 SIMA200710725 1 20070413 A 5347 13500438001 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AE 15775 4800 145275 RIGHT INBOARD SEAT TRACK BETWEEN FRAME 24 TO 32 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURN ED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300125 20070423 00125 SO 2007 4 23 SIMA200710713 1 20070413 A 5320 14521721009 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AE 15775 4800 145275 FOWARD DIGITAL CORRODED AT FRAME 15. REPAIRED FORWARD DIGITAL IAW EMB IC2009-145/02225. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300130 20070423 00130 SO 2007 4 23 SIMA200710716 1 20070413 A 5347 13500439001 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AE 15775 4800 145275 LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAME 23 TO 32. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNE D AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300131 20070423 00131 SO 2007 4 23 SIMA200710717 1 20070413 A 5347 145320605011 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AE 15775 4800 145275 RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETU RNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300139 20070423 00139 SO 2007 4 23 SIMA200709904 1 20070405 A 3240 15851 PRESSURE SWITCH EMB 135 EMB135KL 3260302 SO PARKING BRAKE FAILED A SIMA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 SW 21 805AE 200 145489 ABORTED TAKEOFF, RECEIVED NO TAKEOFF CONFIGURATION WARNING ON EICAS, FLAPS AT 9 DEGREES, SPOILER CLOSED, TRIM AT 7 DEGRE ES AND TL AT 75 PERCENT. REMOVED AND REPLACED EMERGENCY PARKING BRAKE PRESSURE SWITCH IAW EMB AMM 32-44-07, PERFORMED C ONFIGURATION OPERATIONAL CHECK IAW AMM 31-51-00 WITH NO DEFECTS. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300140 20070423 00140 EA 2007 4 23 SIMA200709905 1 20070406 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 500AE 6647 730 10025 EMERGENCY LIGHTS INOPERATIVE AT ROW 1 AND 11, REAR EMERGENCY EXIT AND LEFT LOWER WINDOW EXIT SIGNS INOPERATIVE. REMOVED AND REPLACED NUMBER 3 BATTERY PACK IAW CRJ AMM 33-51-17 AND REPLACED CEILING FLOOD LIGHT BULB IAW AMM 33-51-09. OPERAT IONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007042300142 20070423 00142 EA 2007 4 23 TRAX200700500 1 20070407 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 STA 280 FWD AND AFT FLOOR SUPPORT ANGLES CORRODED AT BL 0. REMOVED FWD FLOOR SUPPORT ANGLE REF CRJ200SRM 51-42-06, AFT FLOOR SUPPORT ANGLE WILL BE REPAIRED ON N/R-00090 W/O 55779. PSP19749 10APR07. INSTALLED NEW FWD FLOOR SUPPORT ANGLE P ER CRJ 200 SRM 51-42-06. SUPPLEMENTAL - SDR CLOSED 04/16/07. 2 L 7 2 4F RT A21EA 2007042300144 20070423 00144 EA 2007 4 23 TRAX200700523 1 20070412 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 835AS 7258 RIGHT OBLIQUE ANGLE CRACKED AFT 621 BULKHEAD. 2 L 7 2 4F RT A21EA 2007042300145 20070423 00145 EA 2007 4 23 TRAX200700524 1 20070412 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 835AS 7258 RIGHT I/B INTERCOSTAL LOCATED AT FS 484 AND RBL 27, IS CRACKED. 2 L 7 2 4F RT A21EA 2007042300148 20070423 00148 EA 2007 4 23 TRAX200700529 1 20070416 A 5320 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 659CA 10153 FS 280.00 CROSSBEAM CORRODED & CRACKED ON UPPER FLANGE. [SUP 05-03-07] REPAIRED IAW ALL SRM`S. 2 L 7 2 4F RT A21EA 2007042300149 20070423 00149 EA 2007 4 23 TRAX200700530 1 20070416 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 659CA 10153 FS 280.00 FWD CENTER FLOOR SUPPORT ANGLE CORRODED. [5-1-07] REMOVED 280 FWD CENTER FLOOR SUPPORT ANGLE. LOCATED HOLES AND NUTPLATES ON NEW SERVICEABLE FWD CENTER FLOOR SUPPORT ANGLE IAW CRJ SRM 51-41-11. OK TO INSTALL FWD CENTER FLOOR SUP PORT ANGLE. INSTALLED SERVICEABLE FWD CENTER FLOOR SUPPORT ANGLE AT FS 280.00 CROSSBEAM IAW CRJ SRM 51-42-06 & CRJ SRM 5 1-42-06 & CRJ SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007042300150 20070423 00150 EA 2007 4 23 TRAX200700531 1 20070416 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 659CA 10153 LEFT LOWER FS 280.00 WEB HAS CORROSION. [5-1-07] BLENDED OUT MINOR SURFACE CORROSION ON LT LOWER FS 280 WEB IAW CRJ 70 0 SRM 53-11-10. APPROX .003 MATERIAL REMOVED IN WORST AREAS IAW CRJ 700 SRM 51-25-06. TOPCOATED REPAIRED AREA IAW CRJ S RM 51-25-16. 2 L 7 2 4F RT A21EA 2007042300153 20070423 00153 EA 2007 4 23 TRAX200700535 1 20070416 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 879AS 7600 RIGHT O/W EXTERIOR EMERGENCY AFT LIGHT INOP. 2 L 7 2 4F RT A21EA 2007042300155 20070423 00155 EA 2007 4 23 TRAX200700515 1 20070411 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 LEFT SIDE FS 625 CLIP CRACKED (MARKED). INSTALLED NEW LEFT SIDE 625 CLIP PER CRJ200 SRM 51-42-21. SUPPLEMENTAL - SDR C LOSED 04/16/07. 2 L 7 2 4F RT A21EA 2007042300158 20070423 00158 EA 2007 4 23 TRAX200700518 1 20070412 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 751EV 10163 RIGHT EMERGENCY EXIT LOWER EXIT LIGHT HAS SEVERAL INOP BULBS. 2 L 7 2 4F RT A21EA 2007042300159 20070423 00159 EA 2007 4 23 TRAX200700509 1 20070410 A 5320 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 CARGO DOOR TRACK CROSSBEAM AFT LOWER SUPPORT BRACKET CRACKED (MARKED). REMOVED AND REPLACED CARGO DOOR TRACK CROSSBEAM AFT LOWER SUPPORT BRACKET PER CRJ 200 SRM 51-42-20. SUPPLEMENTAL - SDR CLOSED 04/16/07. 2 L 7 2 4F RT A21EA 2007042300160 20070423 00160 EA 2007 4 23 TRAX200700491 1 20070408 A 5532 SKIN CNDAIR CL600 CL6002B19 1900309 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 VERTICAL L/E UPPER CORNER CRACKED ON RIGHT SIDE. CUT AWAY DAMAGED AREA (C/W STEPS 1AND 2) IAW REO 601R-55-32-165 CB7015 474. SUPPLEMENTAL - SDR CLOSED 04/16/07. 2 L 7 2 4F RT A21EA 2007042300166 20070423 00166 EA 2007 4 23 TRAX200700521 1 20070410 A 2720 RUDDER CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 846AS 7328 RIGHT RUDDER 80 PERCENT UNCOMMANDED. EMERGENCY DECLARED. FLTS 4177, 4913, 4888, 4913 CX. 2 L 7 2 4F RT A21EA 2007042300168 20070423 00168 EA 2007 4 23 TRAX200700482 1 20070407 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 MINOR SURFACE CORROSION RT SIDE FLOOR SILL RBL 36 STA 349 (MARKED). REMOVED SURFACE CORROSION IAW CRJ SRM 51-21-06. 04 /08/2007. SUPPLEMENTAL - SDR CLOSED 04/16/07. 2 L 7 2 4F RT A21EA 2007042300169 20070423 00169 EA 2007 4 23 TRAX200700484 1 20070407 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 STA 280 BULKHEAD WEB CRACKED AT RBL 9. BEGAN REMOVING FASTENERS THROUGH LT AND RT STA 280 WEB AND RELATED STRUCTURE AS PER CRJ 200 SRM 51-42-00 AND REO 601R-53-11-926. EWB 702040900. CONTINUED REMOVAL OF ASSOCIATED PARTS. MADE CUT AND REMOVED CRACKED / CORRODED CENTER SECTION OF WEB AT LBL 7 THRU RBL 7. REMOVED IAW REO 601R-53-11-926. PERFORMED ED DY CURRENT INSPECTION OF CUT LINES PER REO 601R-53-11-926 IAW CRJ 200 NDTM PART 1, 51-20-06. NO DEFECTS NOTED. STARTE D TRIMMING AND LOCATED EXISTING HOLES IN -1 AND -2 DOUBLER, TRIMMED -3 FILLER AND LOCATED EXISTING HOLES. TRIMMED -5 AF T FLOORS SUPPORT ANGLE TO SIZE IAW CRJ 200 SRM 601R-53-11-926 MS 7022223. FABRICATED -13, -18 SHIM FROM 2024 T3 .050" B 2 L 7 2 4F RT A21EA 2007042300175 20070423 00175 NM 2007 4 23 CALA0700175 1 20070413 A 5320 STRUCTURE BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24202 30429 NUT PLATE HOLE CORRODED AT STA 986, RBL 23. REPAIRED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 2007042300183 20070423 00183 EA 2007 4 23 COMA0760304 1 20070408 A 5532 6002113444 PANEL CNDAIR CL600 CL6002B19 1900309 EA VERTICAL STAB WARPED A COMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 595SW 7292 YAW MOTION NOTED DURING CLIMB, AUTOPILOT ON AND OFF. RETURNED TO CMH. FOUND THE RIGHT LOWER VISOR PANEL BOWED OUT, REP LACED THE VISOR PANEL. 2 L 7 2 4F RT A21EA 2007042300184 20070423 00184 EA 2007 4 23 COMA0760328 1 20070418 A 5320 POST CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 7013 CRACK ON INBOARD FLANGE OF LBL 36 POST AT FS 409+128 AS SEEN FROM AVIONICS BAY. COMPLIED WITH REO-53-41-056. 2 L 7 2 4F RT A21EA 2007042300188 20070423 00188 EA 2007 4 23 COMA0760323 1 20070416 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 783CA 7315 FLAPS FAIL MSG AT 30 DEGREES AT FINAL, GO AROUND INITIATED, FLT LANDED SAFELY. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007042300189 20070423 00189 EA 2007 4 23 COMA0760309 1 20070410 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 815CA 7397 FLAPS FAILED A ZERO DEGREES DURING APPROACH. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007042300191 20070423 00191 EA 2007 4 23 COMA0760324 1 20070417 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA K NONE O OTHER DE DESCENT 1 SO 01 818CA 17735 7408 RIGHT WINDSHIELD CRACKED ON DESCENT. LANDED WITHOUT INCIDENT. REPLACED THE RIGHT WINDSHIELD. 2 L 7 2 4F RT A21EA 2007042300196 20070423 00196 EA 2007 4 23 COMA0760306 1 20070408 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 7013 INTERCOSTAL CRACKED AT FS 484 RBL 27. REPLACED INTERCOSTAL PER SRM 51-42-20. 2 L 7 2 4F RT A21EA 2007042300197 20070423 00197 EA 2007 4 23 COMA0760307 1 20070408 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 7013 INTERCOSTAL CRACKED AT FS 484 LBL 27. REPLACED INTERCOSTAL PER SRM 51-42-20. 2 L 7 2 4F RT A21EA 2007042400007 20070424 00007 EA 2007 4 24 SWIA200718138 1 20070313 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 865AS 7507 PAX DOOR AFT WEB IS CRACKED IN THE RADIUS OF STEP NR 2 DISCOVERED AT C-CHECK. INSTALLED REPAIR DOUBLER ON PAX DOOR AFT SIDE PANEL STEP NR 2 PER CRJ200 REO 601R-52-11-1207. 2 L 7 2 4F RT A21EA 2007042400015 20070424 00015 NM 2007 4 24 ASAA0741581 1 20070420 A 5315 65C339501 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 CORROSION ON FLOORBEAM. REPAIRED CORRODED FLOORBEAM IAW EA 5310 02713. 2 L 7 2 4F RT A16WE 2007042400021 20070424 00021 EU 2007 4 24 07FDEA01522 1 20070418 A 5343 ATTACH FITTING AIRBUS 310 A310324 3930206 EU LT MLG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 801FD 539 LT MLG RIB 5 FWD LUG, CORROSION FOUND IN LUG FACES AND BORE THE MLG LT. REPAIRED AS PER REPAIR INSTRUCTION R57249121. WORK COVERED BY RAS/BAC/1004683/2007 ISSUE A. 2 L 7 2 4F RT A35EU 2007042400022 20070424 00022 EU 2007 4 24 07FDEA01523 1 20070418 A 5343 ATTACH FITTING AIRBUS 310 A310324 3930206 EU CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 801FD 539 RT MLG RIB 5 FWD LUG, CORROSION FOUND IN LUG FACES AND BORE THE MLG RT. REPAIRED AS PER REPAIR INSTRUCTION R57249121. WORK COVERED BY RAS REF: RAS/BAC/1004683/2007 ISSUE A. 2 L 7 2 4F RT A35EU 2007042400026 20070424 00026 WP 2007 4 24 IXXA07SMN096S 1 20070208 A 5730 SKIN DOUG DC8 DC862 3021970 WP ZONE 500 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE SLOT VANE UPPER SKIN HAD NON STANDARD REPAIR AT S TATION XS 520.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS O R CORROSION FOUND. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLI ED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS FROM STATION XS 520.000 IAW FAA FORM 8110-3, NUMBER 07042 DATED 0 2-07-07, SEMAN DRAWING NUMBER ED-4453, DATED 02-02-07, EO SEMAN NUMBER 2007197 DATED 02-07-07, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, FORM SEMAN 242-2, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-20D, AND DC8 SR 2 L 7 4 4F 4A25 2007042400037 20070424 00037 EA 2007 4 24 SWIA200718108 1 20070316 A 7930 TRACK CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW RIGHT THRUST REVERSER INBOARD UPPER TRACK CRACKED AT FORWARD STOP ATTACHMENT HOLE, DISCOVERED AT C-CHECK. REPLACED RIGH T THRUST REVERSER INBOARD UPPER TRACK P/N 228-50809-801 PER CRJ200 AMM 78-34-11-000-801. 2 L 7 2 4F RT A21EA 2007042400041 20070424 00041 EA 2007 4 24 SWIA200718112 1 20070225 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 PAX DOOR INTERIOR INTERCOSTAL ABOVE ACCESS PANEL 832DL IS CORRODED BEYOND REPAIRABLE LIMITS, DISCOVERED AT C-CHECK. INS TALLED NEW INTERCOSTAL ABOVE ACCESS PANEL 832DL, P/N 600-31902-1. 2 L 7 2 4F RT A21EA 2007042400047 20070424 00047 EA 2007 4 24 COMA0760311 1 20070410 A 2840 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA FUEL SYSTEM MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 01 969CA 7141 ON TAKEOFF RIGHT SIDE FUEL QTY AND TOTAL FUEL QTY IND AMBER, AUTO CROSS FLOW INHIBIT STATUS MSG. FLIGHT RETURNED TO ACY AND LANDED SAFELY. DEFERRED EICAS FUEL QUANTITY READOUTS (LEFT RIGHT AND TOTAL) PER MEL 28-41-01-2. 2 L 7 2 4F RT A21EA 2007042400048 20070424 00048 EU 2007 4 24 07FDEA01438 1 20070411 A 5310 DOOR FRAME AIRBUS 310 A310 EU FUSELAGE WORN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 801FD 539 FWD CARGO COMPARTMENT DOOR FWD FRAME WORN ON FRAME 20 STR 42 REPAIRED PER FEDEX EA 6-5330-106703. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS " MAJOR " 2 L 7 2 4F RT A35EU 2007042400049 20070424 00049 EA 2007 4 24 COMA0760302 1 20070405 A 3260 J-BOX CNDAIR CL600 CL6002B19 1900309 EA E&E BAY LOOSE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 797CA 7344 GEAR DISAGREE ON T/O, A/C RETURNED BACK TO CVG AND LANDED SAFELY. INSPECTED AND FOUND JB11 LOOSE IN IT'S RACK, RESECURE D JB11. 2 L 7 2 4F RT A21EA 2007042400051 20070424 00051 EU 2007 4 24 07FDEA01439 1 20070411 A 5310 DOOR FRAME AIRBUS 310 A310 EU FUSELAGE WORN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 801FD 539 FWD CARGO COMPARTMENT DOOR AFT FRAME FOUND WORN AT FRAME 25 REPAIRED PER FEDEX EA 6-5330-106703. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS " MAJOR. 2 L 7 2 4F RT A35EU 2007042400052 20070424 00052 EA 2007 4 24 COMA0760322 1 20070416 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 709CA 7238 FLAPS FAIL CAUTION MSG. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G ) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007042400053 20070424 00053 EA 2007 4 24 COMA0760319 1 20070415 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 526CA 7824 FLAPS FAIL CAUTION MSG. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G ) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007042400055 20070424 00055 EU 2007 4 24 07FDEA01440 1 20070411 A 5730 SKIN AIRBUS 310 A310 EU LT WING CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 801FD 539 LT WING OUTER SKIN SURFACE WITH CORROSION ON T/E AREA 591 RIB 27 REPAIRED PER FEDEX EA 6-5710-106708. REPAIR EVALUAT ED PER GMM 6-2-100 AND CLASSIFIED AS " MAJOR. 2 L 7 2 4F RT A35EU 2007042400058 20070424 00058 EA 2007 4 24 COMA0760326 1 20070418 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA CABIN DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 32349 7013 DURING HMV7 INSP FOUND CORROSION ON LOWER SIDE OF INNER CABIN DOOR SKIN AT ACCESS 832EL. REPLACED INNER SKIN PER SRM 51 -42-06, 51-42-20, 51-45-00, 52-10-31. 2 L 7 2 4F RT A21EA 2007042400060 20070424 00060 2007 4 24 HNAA0700071 4 20070416 A 3452 071127622 CONTROL HEAD DHAV DHC8 DHC8102 2809003 NM NR 2 TRANSPONDER CONTAMINATED A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 906HA 57250 70 9 NR 2 TRANSPONDER SMOKED THEN MADE POPPING NOISE THEN FAIL TO OPERATE, SUSPECT WATER IN NR 2 TRANSPONDER. REMOVED NR 2 T RANSPONDER CONTROLLER C/P. REMOVED AND REPLACED NR 2 TRANSPONDER R/T, CONTROL HEAD, OPS CHECK GOOD IAW 34-52-00. CORR CHECK GOOD IAW W/C 34-53-01F. EXCESSIVE WATER FOUND IN COCKPIT COMING FROM DITCHING HATCH AND F/O'S SIDE PANEL. INSPEC TED DITCH HATCH AND SEALED F/O'S SIDE WINDOW IAW SP&P 56.1.1, PRESSURIZED A/C, NO LEAKS NOTED AT THIS TIME. 2 H 7 2 4T RT A13NM 2007042400061 20070424 00061 NM 2007 4 24 07FDEA01527 1 20070418 A 5712 RIB BOEING 727 727233 138408A NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 223FE 20935 COMPLY WITH EA 7-5710-102033 WINGS (AD 90-06-09 AND AD 94-07-08) MAIN FRAME - RIB REPAIR EO 7-5710-7-2308 PART 2. COMPLI ED WITH EA 7-5710-102033 (AD90-06-09 AND AD 94-07-08) RIB REPAIR EO 7-5710-7-2308 PART 2. 2 L 7 3 4F RT A3WE 2007042400062 20070424 00062 NM 2007 4 24 HNAA0700067 1 20070415 A 2150 7827906 ACM DHAV DHC8 DHC8102 2809003 NM A/C BAY MALFUNCTIONED A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 805EX 40879 1144 228 STRONG ODOR OF PLASTIC WITH BOTH BLEEDS SELECTED ON. REMOVED AND REPLACED HEAT EXCHANGER P/N 778683-2, S/N OFF 840241, S/N ON 960411 IAW 21-50-05. REMOVED AND REPLACED ACM IAW W/C 21-50-03R. OPS AND LEAK CHECKS GOOD. 16APR07 - APU MAKES LOUD NOISE. MEL AUXILIARY POWER UNIT. 2 H 7 2 4T RT A13NM 2007042400071 20070424 00071 EA 2007 4 24 HNAA0700068 1 20070329 A 5730 85712112 PLATE DHAV DHC8 DHC8311 1386006 EA RT WING CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 337EN 31265 284 CORROSION FOUND ON BOTH LADDER PLATES AND ACCESS PANEL 523AT AND 623AT. CORROSION, ON LADDER PLATES AND PANELS 523AT AN D 623AT. REMOVED AND PROTECTED IAW RD 8-57-0469, RD 8-57-0455 AND RD8-57-3617. HFEC CHECK, NO CRACKS FOUND. MAINTENAN CE PROGRAM TO BE AMENDED IAW RD8-57-3617. 2 H 7 2 4T RT A13NM 2007042400074 20070424 00074 NM 2007 4 24 KCSA071154 1 20070418 A 5311 FRAME BOEING 747 747236B 1384804 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 LEFT WHEEL WELL BS 1335 FRAME I/B FLANGE REINFORCEMENT ANGLE CORRODED AT LBL 123, WL 173. 2 L 7 4 4F A20WE 2007042400076 20070424 00076 NM 2007 4 24 KCSA071152 1 20070417 A 5311 FRAME BOEING 747 747236B 1384804 NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 FRAME 260 IN FWD PIT DENTED AT STR 30L. 2 L 7 4 4F A20WE 2007042400077 20070424 00077 NM 2007 4 24 KCSA071149 1 20070416 A 5415 BRACE BOEING 747 747132 1384882 NM NR 4 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 709CK 20247 NR 4 PYLON DIAGONAL BRACE CHAFED OUT OF LIMITS AT LOWER ATTACH POINT. 2 L 7 4 4F A20WE 2007042400078 20070424 00078 NM 2007 4 24 KCSA071150 1 20070416 A 5415 BRACE BOEING 747 747132 1384882 NM NR 1 PYLON GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 709CK 20247 NR 1 PYLON DIAGONAL BRACE HAS TWO GOUGES AT FWD ATTACH POINT. 2 L 7 4 4F A20WE 2007042400080 20070424 00080 NM 2007 4 24 KCSA071156 1 20070418 A 5311 FRAME BOEING 747 747236B 1384804 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STA 500 STR 47L AFT SIDE OF FRAME HAS DAMAGED WEB. 2 L 7 4 4F A20WE 2007042400081 20070424 00081 NM 2007 4 24 KCSA071157 1 20070418 A 5311 FRAME BOEING 747 747236B 1384804 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 SEAT TRACK SUPPORT FRAME HAS .75 INCH CRACK AT STA 570 RBL 25 WL 116. 2 L 7 4 4F A20WE 2007042400086 20070424 00086 WP 2007 4 24 MWEA070095 1 20070413 A 2560 3753213153 LANYARD DOUG DC9 DC982 3022082 WP GIRT BAR BROKEN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 810ME 48072 AFT GALLEY GIRT BAR CABLE BROKEN. REMOVED AND REPLACED AFT GALLEY GIRT LANYARD. 2 L 7 2 4F A6WE 2007042400090 20070424 00090 2007 4 24 QXEA200700617 4 20070414 A 3416 ALTIMETER CNDAIR CL600 CL6002C10 1390015 EA COCKPIT UNKNOWN A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 619QX 10246 PDX- CLIMBING THROUGH 5000 FEET RECEIVED A GLD UNSAFE CAUTION MESSAGE AND FO'S RADIO ALTIMETER WAS SHOWING ZERO FEET WIT H A BARBER POLE. C/W CHECKLIST AND ALL RETURNED TO NORMAL. MAINTENANCE C/W RADIO ALTIMETER OPERATIONAL CHECK AND GROUN D SPOILERS OPERATIONAL CHECKS WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007042400091 20070424 00091 EA 2007 4 24 QXEA200700643 1 20070416 A 2760 PCU CNDAIR CL600 CL6002C10 1390015 EA SPOILERS FAILED A QXEA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 09 616QX 10128 DEN - RECEIVED A INBOARD FLIGHT SPOILERS AND INBOARD SPOILERONS CAUTION MESSAGE WHEN FLIGHT SPOILERS WERE DEPLOYED IN FL IGHT. ON LANDING AFTER TOUCHDOWN, THE RIGHT INBOARD SPOILER DEPLOYED BUT THE LEFT DID NOT. MAINTENANCE INTERROGATED TH E MDC AND FOUND A L IB MFS PCU FAILED PCU JAM MESSAGE. CLEARED BY SERVICE LETTER CRJ-700-SL-27-052D. NO OTHER FAULTS N OTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007042400092 20070424 00092 EA 2007 4 24 QXEA200700646 1 20070419 A 2610 FIRE WARNING CNDAIR CL600 CL6002C10 1390015 EA NONE A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 604QX 10019 PDX - FIRE SYSTEM FAULT CAUTION MESSAGE RECEIVED EN ROUTE. RAN CHECKLIST AND NO FURTHER MESSAGES APPEARED. MAINTENANCE FOUND THE "FIRE DET A" CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER AND COMPLIED WITH OPERATIONAL CHECK. CHECKS GOOD . AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007042400093 20070424 00093 NM 2007 4 24 QXEA200700641 1 20070417 A 6120 AUTOFEATHER SYS DHAV DHC8 DHC8202 2809007 NM NONE A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 09 355PH 500 SEA FLIGHT NR 2110 ON TAKEOFF, AUTOFEATHER SWITCH LIGHT DAR. TAKEOFF ABORTED AT 60KTS. MAINTENANCE PERFORMED AUTOFEATH ER SYSTEM AND POWER UPTRIM TEST IAW -8200 ENGINE RIG MANUAL 6-8, PAGE 3-65, STEPS B1-13. NO PARTS REPLACED. OPERATIONA L CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007042400094 20070424 00094 WP 2007 4 24 070101 1 20070416 A 3350 400 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 875GA 53468 DURING A ROUTINE OVERNIGHT SERVICE CHECK MAINTENANCE INSPECTION LAS VEGAS MAINTENANCE REPORTED THAT THE AFT EMERGENCY EX IT SIGNS/LIGHTS ABOVE THE DOORS WOULD NOT TEST. LAS VEGAS FURTHER REPORT THE REMOVAL AND REPLACEMENT OF THE BS-105 EMER GENCY LIGHTS POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLA NE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007042400095 20070424 00095 WP 2007 4 24 070102 1 20070416 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 879GA 53486 DURING A ROUTINE OVERNIGHT SERVICE CHECK MAINTENANCE INSPECTION LAS VEGAS MAINTENANCE REPORTED THAT THE CEILING MOUNTED EMERGENCY LIGHTS WOULD NOT TEST. THEY FURTHER REPORT THE REMOVAL AND REPLACEMENT OF BATTERY PACK(S). A SATISFACTORY OP ERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007042400096 20070424 00096 NM 2007 4 24 07FDEA01521 1 20070417 A 3297 WIRE BOEING 727 727233 138408A NM NLG DAMAGED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 223FE 20935 FERRY FLIGHT AFTER RAISING GEAR HANDLE UP HAD UNSAFE NOSE GEAR RED LIGHT. CYCLED GEAR IAW QRH UNSAFE NOSE GEAR LIGHT RE ILLUMINATED. ALL DOORS INDICATED SAFE. CONTINUED FLIGHT WITH GEAR HANDLE UP. TROUBLESHOT SYSTEM IAW WDM 32-64-01 FOUN D BAD SPLICE IN WIRE W1386-018- 20. REMOVED AND REPLACED SPLICE IAW SWPM 20-10-12, PERFORMED EXT AND RETRACTION IAW 32- 33-000-5. OP'S CHECKS GOOD. 2 L 7 3 4F RT A3WE 2007042400097 20070424 00097 NM 2007 4 24 PIDA07018 1 20070413 A 3350 BATTERY PACK BOEING 757 757236 1384971 NM CABIN DISCHARGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 757BJ 22176 EMERGENCY LIGHTS IN VICINITY OF THE L2 DOOR ARE INOP. REPLACED BATTERY PACK AND OPS CHECKED OK. 2 L 7 2 4F RT A2NM 2007042400098 20070424 00098 SO 2007 4 24 RAIA00704045 1 20070415 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 850HK 145003 FLT NR 8059 - RIC - RUBBER BURNING ODOR REPORTED FROM PAX IN ROW 18. MAINTENANCE PERFORMED INSP OF ALL EMERGENCY LIGHTS & BLEED DUCTS, RAN APU, ENGINES AND PACKS NO DEFECTS OR SMELLS NOTED AT THIS TIME. 2 L 7 2 4T RT T00011AT 2007042400099 20070424 00099 EA 2007 4 24 TRAX200700513 1 20070411 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 349 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 FS 349 FRAME HAS CORROSION DAMAGE IN MAIN AVIONICS BAY CORROSION WAS REMOVED UNDER THE TWO CLIPS ON FS 349 IAW CRJ 200 S RM 51-21-06. 2 L 7 2 4F RT A21EA 2007042400101 20070424 00101 EA 2007 4 24 TRAX200700514 1 20070411 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 333 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 FS 333 FRAME HAS CORROSION DAMAGE IN MAIN AVIONICS BAY REMOVED FASTNERS ,BLENDED FS 333 FRAME IAW CRJ 200 SRM 51-21-06. 2 L 7 2 4F RT A21EA 2007042400102 20070424 00102 SO 2007 4 24 RAIA00704047 1 20070416 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 833HK 145240 PRE FLT NR 8018 - STL - EMERGENCY LIGHT INOP AT RIGHT ROW SIDE WALL POSITION. MAINTENANCE RESECURED CONNECTORS, OPS CHE CK GOOD. 2 L 7 2 4T RT T00011AT 2007042400105 20070424 00105 WP 2007 4 24 IXXA07SMN128S 1 20070223 A 5730 SKIN DOUG DC8 DC862F 3021972 WP RT WING MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C-CHECK INSPECTION, FOUND RT WING OUTBOARD SECTION LEADING EDGE HAS A NONE STANDARD REPAIR DOUBLER AT STA TION XFS 710. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROS ION FOUND AFTER NDT INSPECTION. FABRICATED REPAIR DOUBLER CLEANED,TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEA LANT TO FAYING SURFACES. INSTALLED REPAIR PARTS. IAW FAA FORM 8110-3 NUMBER 07110 DATED 03-14-07, SEMAN DRAWING NUMBER ED-4454 DATE 02-19-07, E.O SEMAN NUMBER 2007198 DATE 03-14-07, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 NDT SPM PART 06-10- 01-001, SEMAN 242-2, DC8 SRM 51-1-8B, . DC8 SRM 51-1-11, DC8 SRM 51-1-20D, AND DC8 SRM 51-3-1 2 L 7 4 4F 4A25 2007042400106 20070424 00106 SO 2007 4 24 RAIA00704038 1 20070413 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 830HK 145313 POST FLT NR 5542 - STL - CABIN EMERGENCY LIGHT INOP. MAINTENANCE RESEATED CONNECTOR PERFORMED CHECK OF LIGHTS CHECK GOO D. 2 L 7 2 4T RT T00011AT 2007042400109 20070424 00109 SO 2007 4 24 RAIA00704040 1 20070414 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 850HK 145003 PRE FLT 7901 - ORD - EXTERIOR EMERGENCY LIGHT AT SERVICE DOOR INOP. MAINTENANCE DEFERRED PER MEL. 2 L 7 2 4T RT T00011AT 2007042400115 20070424 00115 2007 4 24 SWAA071835 4 20070412 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007042400123 20070424 00123 NM 2007 4 24 SWAA071931 1 20070419 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 705SW 27839 EEPLS COVER MISSING AT ROW 10 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007042400125 20070424 00125 NM 2007 4 24 SWAA071945 1 20070419 A 3350 471N5212 CAP BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 482WN 29852 DURING SCHEDULED MV2 CHECK, FOUND LT FWD CABIN EEPLS END CAP BROKEN. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 2007042400128 20070424 00128 NM 2007 4 24 SWAA071937 1 20070419 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007042400137 20070424 00137 NM 2007 4 24 SWAA071886 1 20070417 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 729SW 27861 DURING SCHEDULED MV1 CHECK, FOUND EEPLS COVER MISSING AT ROW 19 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007042400138 20070424 00138 NM 2007 4 24 SWAA071885 1 20070417 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 440LV 29835 EEPLS COVER LOOSE AT ROW 4 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007042400141 20070424 00141 NM 2007 4 24 SWAA071874 1 20070416 A 5330 6545765 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007042400149 20070424 00149 NM 2007 4 24 SWAA071878 1 20070417 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007042400154 20070424 00154 NM 2007 4 24 SWAA071867 1 20070414 A 5310 6546812 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 880, LBL 65, WL 208. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2007042400155 20070424 00155 NM 2007 4 24 SWAA071888 1 20070417 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007042400156 20070424 00156 NM 2007 4 24 SWAA071866 1 20070414 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007042400160 20070424 00160 2007 4 24 SWAA071880 4 20070417 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007042400170 20070424 00170 NM 2007 4 24 SWAA071845 1 20070412 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 912, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007042400173 20070424 00173 NM 2007 4 24 SWAA071840 1 20070412 A 5230 6547952524 SKIN BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT AFT LOWER CORNER. REMOVED AND REPLACED AFT CARGO DOOR P ER MM. 2 L 7 2 4F RT A16WE 2007042400175 20070424 00175 NM 2007 4 24 SWAA071956 1 20070419 A 5311 6546541 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 3R. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2007042400176 20070424 00176 NM 2007 4 24 SWAA071955 1 20070419 A 5311 6546541 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 3L. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2007042400180 20070424 00180 NM 2007 4 24 SWAA071952 1 20070419 A 5315 6546812 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 55. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2007042400183 20070424 00183 NM 2007 4 24 SWAA071941 1 20070419 A 5311 65C22909 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007042400194 20070424 00194 NM 2007 4 24 2007UALA01184 1 20070416 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED WITH SERVICEABLE BATTERY PACK. OP CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007042400195 20070424 00195 EU 2007 4 24 2007UALA01200 1 20070417 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 480UA 1555 CABIN EMERGENCY LIGHTS CHECK FAILS -EPSU EMERGENCY BATTERY RIGHT. [SUP 4-24-07] EPSU BATTERY REPLACED AT 12WL AND EMER GENCY LIGHTS TEST OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007042400203 20070424 00203 NM 2007 4 24 2007UALA01208 1 20070416 A 2910 HYDRAULIC SYSTEM BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CENTER SYS MALFUNCTIONED A UALA O OTHER K FLUID LOSS CR CRUISE 1 WP 29 674UA 29242 CREW REPORTS LOSS OF CENTER SYSTEM HYDRAULICS. [SUP 05-04-07] FOUND LEAK IN RIGHT WHEEL WELL. RT CENTER AC MOTOR P UMP LEAKING AT OUTPUT PRESSURE LINE. REPLACED PACKING AND UNION. NO LEAKS NOTED. A/C OK FOR SERVICE. SUSPECT VIBRATIO N LOOSENED PRESS LINE CONNECTION & CAUSED LEAK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007042400207 20070424 00207 NM 2007 4 24 2007UALA01213 1 20070417 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 MAIN CABIN TEE CAP AT STA 324 IS CORRODED. [06-14-07] MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF T-C AP, MOST OUTBOARD 14 IN. RBL. FABRICATED PER UA ENGINEERING SPECIFICATIONS AND INSTALLED NEW REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007042400211 20070424 00211 2007 4 24 SIMA200710614 4 20070415 A 3425 HG2011AC03 AHRS EMB 135 EMB135KL 3260302 SO COCKPIT FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 840AE 9947 5 145656 AUTOPILOT LOST WITH STALL PROTECTION SYSTEM ADVANCED MESSAGE - DIVERTED TO BNA. REMOVED AND REPLACED NUMBER 1 AHRS COMP UTER AND FAN IAW CRJ AMM, OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE 2 L 7 2 4F RT T00011AT 2007042400216 20070424 00216 NM 2007 4 24 2007UALA01220 1 20070419 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 SKIN DENTED AT BS STA 747R FROM 8 INCHES FWD TO 9 INCHES AFT. DENT IS BETWEEN STRINGER 19R AND 20R. DENT IS ON A SKIN LAP SEAM, 1EA RIVET HEAD IS PULLED WITHIN DENT. [SUP 05-16-07] MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF S TRINGER. MFG'D & INSTALLED STRINGER REPAIR PIECES. REMOVED DAMAGED SECTION OF UPPER SKIN. MFG'D & INSTALLED DOUBLERS & F ILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007042400227 20070424 00227 NM 2007 4 24 2007UALA01190 1 20070416 A 3350 CHARGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 OVERWING EMERGENCY LIGHT 2 TOP LIGHT INOP. REPLACED BATTERY CHARGER ASSY. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007042400234 20070424 00234 NM 2007 4 24 2007UALA01191 1 20070416 A 3350 5851836 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY CEILING LIGHT ABOVE ROW 61 RT. REPLACED LIGHT ASSY AND CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007042400235 20070424 00235 NM 2007 4 24 2007UALA01192 1 20070415 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 506UA 24627 EEL LIGHT BAR IN FRONT OF THE K-LAV IS INOPERATIVE. [SUP 4-24-07] REPLACED EEL LIGHT AND OPS CHECK GOOD PER MM 33-51-9 6 ON NON ROUTINE Z2494N. 2 L 7 2 4F 4 F RT A2NM E17NE 2007042400237 20070424 00237 NM 2007 4 24 2007UALA01194 1 20070415 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 506UA 24627 CABIN EEL LIGHT STRIPS INOP IN FIRST CLASS, IN FRONT OF MID LAV ECONOMY SECTION. [SUP 4-24-07] REPLACED EEL FEEDER PER MM 33-51-11 AND OPS CHECK GOOD PER MM 33-51-00 ON NON ROUTINE Z2497N. 2 L 7 2 4F 4 F RT A2NM E17NE 2007042400239 20070424 00239 NE 2007 4 24 2007UALA01196 2 20070416 A 7200 ENGINE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 1 SHUTDOWN A UALA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 WP 29 107UA 26900 727685 FLIGHT DIVERTED DUE NR 1 ENGINE SHUTDOWN. [06-14-07] TWO BOLTS THAT RETAIN THE OIL PUMP IDLER BEARING (MB-18) OU TER RACE, IN THE MAIN GEARBOX (MGB), HAD BACKED OUT. ONE (1) OF THESE GOT PAST THE MGB SUMP SCREEN, AND INTO THE ROTATI NG GEAR MESH OF THE MAIN OIL PUMP. THIS CAUSED PUMP SEIZURE AND FAILURE OF THE OIL PUMP DRIVE SHAFT AT ITS DESIGNED SHE AR POINT. THIS WAS A FIRST RUN MGB. IN THE INTERIM UA IS ADDING LOCK LIQUID TO THESE BOLTS, AND IS INSPECTING MGB BE ARINGS MB-16, MB-17, AND MB-18 WHENEVER MGB CARBON SEALS ARE REPLACED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007042400258 20070424 00258 NM 2007 4 24 USAA070279 1 20070412 A 5534 ANGLE BOEING 737 737401 1384701 NM VERTICAL STAB WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 RIGHT SKATE ANGLE WORN AT BS 1006, RT SIDE OF VERTICAL STAB SKATE ANGLE. FABRICATED REPLACEMENT ANGLE PER SRM 51-40-02, DEFECT SIZE: 2 X 1 INCH. 2 L 7 2 4F RT A16WE 2007042400260 20070424 00260 NM 2007 4 24 USAA070278 1 20070412 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 STA 727D + 12 INCHES, S23R HAS CRACK. INSTALLED DOUBLER/TRIPLER & SHEAR TIES PER TR 53-60-03A, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007042300010 20070423 00010 NM 2007 4 23 AALA20070601 1 20070404 A 3350 GUARD BOEING BOEING 767 767323 1385205 NM COCKPIT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 342AN DO0127 33081 JFK - EMERGENCY LIGHT SWITCH GUARD IN COCKPIT BROKEN. REPLACED EMERGENCY LIGHT CONTROL PANEL IN COCKPIT OVERHEAD FOR BR OKEN EMERGENCY LIGHT SWITCH GUARD IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007042300012 20070423 00012 NM 2007 4 23 AALA20070603 1 20070404 A 3350 CONTACT BOEING 757 757223 1384957 NM CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 634AA 24592 MIA - EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. CLEANED CONTACTS FOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007042300023 20070423 00023 WP 2007 4 23 AALA20070586 1 20070401 A 2910 HYDRAULIC LINE DOUG DC9 DC983 3022083 WP HYDRAULIC SYS CRACKED A AALA O OTHER J WARNING INDICATION DE DESCENT 1 SW 21 975TW 53625 DFW INFLIGHT T842/01APR INBOUND TO DFW LOST RIGHT HYDRAULIC QUANTITY AND PRESSURE. DECLARED EMERGENCY AND LANDED WITH MAIN LANDING GEAR DOORS DOWN WITHOUT INCIDENT. FOUND CRACKED HYDRAULIC LINE AT RUDDER HYDRAULIC SHUTOFF VALVE RIGHT HY DRAULIC SYSTEM. REPLACED HYDRAULIC LINE AND REPLACED RIGHT CASE DRAIN FILTER, AND RIGHT PRESSURE FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007042300028 20070423 00028 EU 2007 4 23 AALA20070588 1 20070401 A 2730 359002001201 COMPUTER AIRBUS 300 A300B4605R 3930308 EU E&E BAY MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 59081 639 MIA INFLIGHT T1190/01APR MBJ TO JFK - FLIGHT HAD DUAL RUDDER FAULT INDICATION. EMERGENCY DECLARED AND AIRCRAFT LANDED MIA WITHOUT INCIDENT. AIRCRAFT WAS OVERWEIGHT FOR LANDING. REPLACED NUMBER ONE AND TWO FEEL LIMITATION COMPUTER. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007042300030 20070423 00030 EU 2007 4 23 AALA20070590 1 20070401 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70079 619 MIA - EMERGENCY PATH LIGHT AT SEAT 29G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 29G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007042300031 20070423 00031 NM 2007 4 23 AALA20070591 1 20070401 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 388AA 27448 MIA - EMERGENCY LIGHT AT SEAT 38B INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 38B. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A1NM 2007042300037 20070423 00037 WP 2007 4 23 AALA20070613 1 20070406 A 3222 VALVE DOUG DC9 DC982 3022082 WP NLG FAULTY A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 416AA 49327 YYC - NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO YYC AND LANDED WITHOUT INCIDENT. SERVICED NOSE GEAR STRUT WITH NITROGEN AND REPLACED VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007042300047 20070423 00047 WP 2007 4 23 AALA20070622 1 20070410 A 3350 BUMPER BLOCK DOUG DC9 DC982 3022082 WP CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 214AA 49162 LGA - OVERHEAD EMERGENCY EXIT LIGHT AT SEAT ROW 20 HAS MISSING BUMPER. REPLACED BUMPER FOR OVERHEAD EMERGENCY EXIT LIGH T AT SEAT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007042300050 20070423 00050 NM 2007 4 23 AALA20070594 1 20070402 A 2530 OVEN BOEING 757 757223 1384957 NM GALLEY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 604AA 27055 JFK INFLIGHT - NUMBER ONE OVEN IN FIRST CLASS SMOKING WHILE IN USE. OVEN WAS TURNED OFF AND SMALL PATCH CONTINUE TO GLO W AT LEFT SIDE OF HEATING ELEMENT. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. CLEANED BURNED DEBRIS AND GREASE ON HE ATING ELEMENT FOR NUMBER ONE OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007042300062 20070423 00062 NM 2007 4 23 AWXA200700480 1 20070310 A 5210 6545871502 SKIN BOEING 737 7373G7 1384595 NM L1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - CRACKED L1 DOOR INNER SKIN, BS 347.30, S12L - S14L, NEAR STOP PIN CUTOUTS NR 5, NR 6 AND NR 7. REPAIRED L1 DOOR I NNER SKIN, BS 347.30, S12L - S14L, NEAR STOP PIN CUTOUTS NR 5, NR 6 AND NR 7 IAW ER 03-5200-07097-ES1. 2 L 7 2 4F RT A16WE 2007042300067 20070423 00067 NM 2007 4 23 AWXA200700485 1 20070312 A 5320 6517684642 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 MCN - CRACKED INTERCOSTAL WEB, BS 294.5, S7L. REPLACED INTERCOSTAL WEB, BS 294.5, S7L IAW AWA ER 03-5312-07093-SS4. 2 L 7 2 4F RT A16WE 2007042300077 20070423 00077 NM 2007 4 23 DL76G070329 1 20070416 A 2761 271002215 ACTUATOR BOEING 767 767332 1382001 NM SPOILER FAILED A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 1608 30573 SPOILER EICAS STATUS MSG FOUND NR 11 SPOILER ACT INOP. REPLACED BY NEW ON ACC MM 27-61-02-424-023. ALL TESTS ACC AMM 2 7-61-00 501 C/OU OK. INSPECTION PERFORMED. 2 L 7 2 4F RT A1NM 2007042300078 20070423 00078 NM 2007 4 23 DLM88070295 1 20070405 A 5330 5936434129 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 945DL 49818 LT FUSELAGE SKIN FS 260 BETWEEN LONGERONS 29L AND 30 CORROSION. ISSUED ER/A 460861-14 WHICH DOCUMENTED SKIN REPAIR. TC AS INTERNAL DOUBLER WAS EXTENDED AND AN EXTERNAL REPAIR DOUBLER WAS ADDED. ER/A REFERS TO AMX REPAIR DWG AMR0953595 WHI CH ACCOMPLISHED THE REPAIR. REPETITIVE INSPECTIONS INITIATED AT 8000 HR INTERVALS. 2 L 7 2 4F RT A6WE 2007042300079 20070423 00079 NM 2007 4 23 DLM88070318 1 20070412 A 3350 41B004AD07G3 BATTERY DOUG MD88 MD88 3023688 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 920DL 49644 724655 FWD O/WING EXITS INT EXIT SIGNS LIGHTS INOP. REPLACED BATTERIES IN CHARGER PACK. 2 L 7 2 4F 4 F RT A6WE E24NE 2007042300081 20070423 00081 NM 2007 4 23 EIA2007054 1 20070309 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 485EV 20712 FUSELAGE SKIN CRACKED AT BS 340 BETWEEN STRINGERS 6L-7L. REMOVED DAMAGE, NDT'D AREA, FABRICATED AND INSTALLED REPAIR PE R B747 SRM 53-30-03 PAGES 77-78D. 2 L 7 4 4F A20WE 2007042300087 20070423 00087 NM 2007 4 23 EIA2007060 1 20070313 A 2611 21562A SMOKE DETECTOR BOEING 747 747273C 1384896 NM CABIN NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 470EV 20653 NR 6 LOWER DECK SMOKE DETECTOR WILL NOT TEST. REPLACED DETECTOR WHEN RELAMPING DID NOT HELP. TESTED GOOD PER MM 26-16- 00. 2 L 7 4 4F A20WE 2007042300096 20070423 00096 NM 2007 4 23 EIA2007047 1 20070222 A 5730 SKIN BOEING 747 747SR46 1384816 NM RT WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 RIGHT WING LOWER SKIN CORRODED ON UPPER SURFACE AT FSSO 1290 AT OUTBOARD JACKPAD. REMOVED CORROSION, NDT AREA, FABBED A ND INSTALLED REPAIR PER ECRA 477-57-114-2 2 L 7 4 4F RT A20WE 2007042300097 20070423 00097 NM 2007 4 23 EIA2007048 1 20070220 A 5711 SPAR BOEING 747 747SR46 1384816 NM RT WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 CORROSION ON FRONT SPAR WEB UNDER RIGHT WING JACK PAD FITTING AT WING STATION 1290. REMOVED CORROSION, NDT'D AREA, FABB ED AND INSTALLED REPAIR PER ECRA 477-57-113-2. 2 L 7 4 4F RT A20WE 2007042300102 20070423 00102 EU 2007 4 23 SIMA200710602 1 20070410 A 3020 ANTI-ICE SYSTEM SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING UK UNKNOWN 1 SW 21 904AE 340B314 RIGHT INTAKE LIGHT ON IN-FLIGHT, RETURNED TO DFW. TROUBLESHOT SYSTEM WITH NO DEFECTS NOTED, RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007042300110 20070423 00110 SO 2007 4 23 SIMA200710601 1 20070410 A 3350 LIGHT EMB 135 EMB135LR 3260305 SO CABIN MALFUNCTIONED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 737MW 145396 EMERGENCY LIGHT STRIPS AT ROW 3 THROUGH ROW 5 ARE INOPERATIVE. PERFORMED OPERATIONAL TEST IAW EMB AMM 33-50-00 WITH NO DEFECTS NOTED, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300121 20070423 00121 SO 2007 4 23 SIMA200710706 1 20070410 A 5320 14521413605 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 800AE 13129 4800 145425 CENTER OMEGA BEAM CORRODED AT FRAME 25. PERFORMED CUTOUT OF CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SR M 53-00-10. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300136 20070423 00136 SO 2007 4 23 SIMA200710720 1 20070413 A 5347 14530659005 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AE 15775 4800 145275 LEFT INBOARD SEAT TRACK BETWEEN FRAME 32 AND 46 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRA FT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300143 20070423 00143 EA 2007 4 23 TRAX200700520 1 20070413 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 755EV 10185 F/O`S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007042300162 20070423 00162 EA 2007 4 23 TRAX200700493 1 20070408 A 5312 FLOOR SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 CORROSION ON RIGHT PRESSURE FLOOR FROM FS 460 TO FS 513. [SUP 4-23-07] COMPLIED WITH ALL FAA APPROVED DATA. 2 L 7 2 4F RT A21EA 2007042300173 20070423 00173 NM 2007 4 23 CALA0700185 1 20070419 A 5730 114N2106 SKIN BOEING 757 757224 1384958 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17133 29282 RT WING LEADING EDGE SKIN CRACKED AT RIB STA 471, BEHIND NR 8 SLAT AT I/B DRIVE TRACK. REPAIRED IAW ECRA 5731-1303 AND SRM 51-70-07. 2 L 7 2 4F RT A2NM 2007042300178 20070423 00178 NM 2007 4 23 CALA0700178 1 20070416 A 5320 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19357 23841 CRACKED ANGLE FOR INTERCOSTAL STRINGER 16L AT STA 344. REPAIRED IAW SRM 53-10-04. 2 L 7 2 4F RT A16WE 2007042300180 20070423 00180 NM 2007 4 23 CALA0700180 1 20070417 A 5315 141T5108 FLOORBEAM BOEING 767 767424ER 1385270 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76065 29460 FLOOR SUPPORT CORRODED AT BS 325 LBL 53-55. REPAIRED IAW SRM 53-00-51 FIG 201, REPAIR 1. 2 L 7 2 4F RT A1NM 2007042300182 20070423 00182 EA 2007 4 23 COMA0760303 1 20070406 A 3241 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 1900309 EA ANTI-SKID SYS TRIPPED A COMA K NONE O OTHER AP APPROACH 1 SO 01 991CA 7216 CIRCUIT BREAKER 2G3 ANTI-SKID TRIPPED DURING APPROACH. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. RESET CIRCUI T BREAKER, PERFORMED BITE CHECK PER AMM 32-44-06, NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007042300185 20070423 00185 EA 2007 4 23 COMA0760329 1 20070418 A 5320 POST CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 7013 CRACK ON INBOARD FLANGE OF RBL 27 POST AT FS 409+128 AS SEEN FROM AVIONCS BAY. COMPLIED WITH REO-53-41-056. 2 L 7 2 4F RT A21EA 2007042300194 20070423 00194 EA 2007 4 23 COMA0760313 1 20070411 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 592SW 7279 AFTER LANDING DURING FLAP RETRACTION RECEIVED A FLAP FAIL MESSAGE AT 27 DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTI ON MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLA P CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007042300195 20070423 00195 EA 2007 4 23 COMA0760305 1 20070408 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 7013 CRACK PROPAGATING FROM PARKING BRAKE CABLE HOLE IN FWD HYD COMPARTMENT FS 202.75, BL 23.71. COMPLIED WITH REO-53-11-563 . 2 L 7 2 4F RT A21EA 2007042400013 20070424 00013 NM 2007 4 24 ASAA0741580 1 20070418 A 2697 321893 TERMINAL BOEING 737 737490 1384715 NM OVERHEAT LOOP CORRODED A ASAA D RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 NM 02 705AS 29318 FAULT LIGHT ILLUMINATED DURING OVERHEAT FIRE TEST. ENGINE NR 1 OVERHEAT LIGHT FAILED TO ILLUMINATE DURING TEST. A-LOOP FAILED. CHANGED ALL A I TERMINAL LUGS ON FAN AND FIREWALL OVERHEAT LOOPS. 2 L 7 2 4F RT A16WE 2007042400016 20070424 00016 EA 2007 4 24 SWIA200718145 1 20070313 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 865AS 7507 PAX DOOR AFT WEB CRACKED AT TOP OF MIDDLE STEP, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLES AND DOUBLER TO AFT PAX D OOR WEB PER CRJ200 REO 601R 52-11-702 REV 'A' STEP 8-12. 2 L 7 2 4F RT A21EA 2007042400030 20070424 00030 EA 2007 4 24 SWIA200718148 1 20070313 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 865AS 7507 STA 280 FORWARD FLOOR SUPPORT ANGLE SHOWS EVIDENCE OF CORROSION, DISCOVERED AT C-CHECK. REPLACED FLOOR SUPPORT ANGLE AN D INBOARD AND OUTBOARD ENDS OF ANGLE P/N 600-34017-21 IAW CRJ200 SRM CH 51-42-06 PG 11 PARA 9. 2 L 7 2 4F RT A21EA 2007042400033 20070424 00033 EA 2007 4 24 SWIA200718104 1 20070316 A 5240 BRACKET CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 ROLLER BRACKET ON AFT SIDE OF SERVICE DOOR HAS CORRODED HARDWARE, DISCOVERED ON C-CHECK. REPLACED HARDWARE ON SERVICE D OOR ROLLER BRACKET IAW CRJ200 AMM 20-21-00-910-801. 2 L 7 2 4F RT A21EA 2007042400039 20070424 00039 EA 2007 4 24 SWIA200718109 1 20070316 A 7830 TRACK CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 RIGHT THRUST REVERSER INBOARD LOWER TRACK CRACKED AT STOP ATTACHMENT HOLE, DISCOVERED AT C-CHECK. REPLACED RIGHT THRUST REVERSER INBD LOWER TRACK P/N 228-50809-801 PER CRJ200 AMM 78-34-11-000-801. 2 L 7 2 4F RT A21EA 2007042400057 20070424 00057 EA 2007 4 24 COMA0760320 1 20070415 A 2613 LOOP CNDAIR CL600 CL6002B19 1900309 EA OUT OF ADJUST A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 914CA 7012 DURING CLIMBOUT RECEIVED AN ANTI-ICE DUCT WARNING, PERFORMED QRH, MSG CLEARED, FLT DIVERTED TO IND. ADJUSTED LOOP AND P ERFORMED AN OPERATIONAL CHECK. NO DISCREPANCIES NOTED. 2 L 7 2 4F RT A21EA 2007042400087 20070424 00087 EA 2007 4 24 SWIA200718152 1 20070416 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 915SW 7615 THE EXTERIOR FORWARD AND MIDDLE EMERGENCY EXIT LIGHTS ON THE RIGHT SIDE ARE INOP. RELAMPED THE FORWARD AND MIDDLE RIGHT SIDE EMERGENCY LIGHTS IAW AMM 33-25-00. 2 L 7 2 4F RT A21EA 2007042400088 20070424 00088 2007 4 24 SWIA200718153 4 20070418 A 3417 ADC CNDAIR CL600 CL6002B19 1900309 EA NR 1 MALFUNCTIONED A SWIA O OTHER O OTHER DE DESCENT 1 NM 07 439SW 7578 EFIS COMP WITH MACH TRIM CAUTION MESSAGE ON DESCENT ALONG WITH ASSOCIATED FLAGS. REPLACED NR 1 ADC IAW MM 34-13-01. PU RGED MAIN PITOT STATIC SYSTEM IAW MM 34-11-00. 2 L 7 2 4F RT A21EA 2007042400089 20070424 00089 NM 2007 4 24 QXEA200700642 1 20070418 A 6120 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM NR 1 PROP UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 422QX 4150 LAX FLIGHT NR 2304: AFTER ENGINE START, NR 1 PROP WOULD NOT COME OUT OF FEATHER. AIRCRAFT RETURNED TO BLOCK. MAINTENAN CE C/W STAR OF THE NR 1 ENGINE, UNFEATHERED AND FEATHERED NR 1 PROP 4 TIMES. TIME TO UNFEATHER WAS IN LIMITS EACH TIME. REFERENCE AMM TASK 61-20-00-501-502. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007042400107 20070424 00107 SO 2007 4 24 RAIA00704037 1 20070413 A 7697 2306140 WIRE HARNESS EMB 145 EMB145LR 3260212 SO NR 2 ENGINE FAULTY A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 841HK 145382 PRE FLT 8010 - STL - ENGINE 2 NO DISPATCH. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE INTERNAL YELLOW B-HARNESS, NO F AULTS AT THIS TIME. 2 L 7 2 4T RT T00011AT 2007042400111 20070424 00111 SO 2007 4 24 RAIA00704043 1 20070415 A 3020 ANTI-ICE VALVE EMB 145 EMB145 3260210 SO NR 1 ENGINE MALFUNCTIONED A RAIA O OTHER O OTHER TO TAKEOFF 1 CE 03 802HK 145066 FLT NR 3570 - PIT - E1 ANTI-ICE FAIL ON TAKEOFF. MAINTENANCE SECURED VALVE OPEN AND DEFERRED PER MEL. 2 L 7 2 4F RT T00011AT 2007042400112 20070424 00112 SO 2007 4 24 RAIA00704041 1 20070414 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 830HK 145313 POST FLT NR 5578 - STL - EMERGENCY LIGHT GALLEY WALL EXIT LOCATOR INTERMITTENT. MAINTENANCE RESEATED CONNECTOR TO LIGHT ASSY, SYSTEM CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007042400113 20070424 00113 NM 2007 4 24 SWAA071944 1 20070419 A 5311 6546532 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007042400118 20070424 00118 NM 2007 4 24 SWAA071847 1 20070413 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 EEPLS PHOTOLUMIESCENT STRIP MISSING AT ROW 15 ABC. INSTALLED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007042400133 20070424 00133 NM 2007 4 24 SWAA071943 1 20070419 A 5311 6546525 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007042400143 20070424 00143 NM 2007 4 24 SWAA071869 1 20070415 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 363, STR 8L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007042400148 20070424 00148 NM 2007 4 24 SWAA071876 1 20070416 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007042400168 20070424 00168 NM 2007 4 24 SWAA071838 1 20070412 A 5330 6545765 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 513D, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007042400169 20070424 00169 NM 2007 4 24 SWAA071844 1 20070412 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 422, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007042400171 20070424 00171 NM 2007 4 24 SWAA071846 1 20070412 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 19R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007042400179 20070424 00179 NM 2007 4 24 SWAA071940 1 20070419 A 5311 6546593 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007042400186 20070424 00186 NM 2007 4 24 SWAA071939 1 20070419 A 5523 65C2638427A TAB BOEING 737 7373H4 1384600 NM LT ELEVATOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED BRDG CHECK, FOUND LT ELEVATOR TAB CRACKED AT PUSH ROD FITTING INBOARD LUG. REMOVED AND REPLACED TAB PE R MM. 2 L 7 2 4F RT A16WE 2007042400191 20070424 00191 NM 2007 4 24 SWAA071851 1 20070413 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007042400205 20070424 00205 NM 2007 4 24 2007UALA01211 1 20070417 A 5330 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 906UA 25006 SKIN DAMAGED BETWEEN BS 887 & BS 928 & FROM BUT NOT INCLUDING STRINGERS 20R AND 23R. [SUP 05-16-07] REPAIRED PER SRM 53-00-01. 2 L 7 2 4F 4 F RT A16WE E21EU 2007042400213 20070424 00213 EU 2007 4 24 2007UALA01218 1 20070418 A 2622 CARTRIDGE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FIRE BOTTLE DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 427UA 512 AFT WATER FIRE BOTTLE CO-2 CARTRIDGE FOUND EMPTY BUT BOTTLE FULL OF WATER. [06-22-07] REPLACED FIRE EXTINGUISHER ASSEM BLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007042400230 20070424 00230 NM 2007 4 24 F3LA200700062 1 20070416 A 2612 PPA110200 FIRE DETECTOR AIRBUS A319 A319111 3930336 NM CARGO BAY NO TEST A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 906FR 1684 DURING C4/S1 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT DETECTORS (2) FAILED TEST. REPLACED AFT CARGO COMPARTMENT FIRE DETECTORS (5WH AND 6WH). PERFORMED OPS TEST OF CARGO SMOKE DETECTORS IAW A319 AMM 26-16-15-000-001. 2 L 7 2 4F RT A28NM 2007042400231 20070424 00231 NM 2007 4 24 F3LA200700056 1 20070416 A 3350 LAMP AIRBUS A319 A319111 3930336 NM EMERGENCY LIGHT INOPERATIVE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 1684 DURING C4/S1 CHECK, INSPECTION REPORTED BULBS INOP IN ROW 4 AND 6 ABC SEAT FLOOR PATH LIGHTING. RELAMPED ROW 4 AND 6 AB C SEAT FLOOR PATH LIGHTS. OPS CHECK NORMAL IAW A319 AMM 33-51-00-710-007. 2 L 7 2 4F RT A28NM 2007042400232 20070424 00232 NE 2007 4 24 DHLA200700023 2 20070404 A 7230 COMPRESSOR BOEING 727 727223 1384074 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE STALLED A DHLA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 05 754DH 22008 DEPARTING RNWY 22R AT ILN, NR 2 ENG COMPRESSOR STALL OCCURRED AT AN EPR OF 2.05. WIND WERE 290DEG AT 14 GUSTING TO 26 (7 0DEG X-WIND) IAS -0, OAT - 13DEG, PA - 1077 A/C GW 178.8. FOR INFORMATION ONLY. INSPECTED INLET AND EXHAUST OF NR 2 EN G PER AOM CHPT 1.8 PG 5 AND IAW M/M CHPT 71-00-00. NO DAMAGE NOTED. A/C IS OK TO RETURN TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2007042400233 20070424 00233 NM 2007 4 24 F3LA200700080 1 20070417 A 3397 WIRE HARNESS AIRBUS A319 A319111 3930336 NM EMERGENCY LIGHT DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 1684 DURING C4/S1 CHECK, INSPECTION REPORTED SEAT EMERGENCY LIGHT AT ROW 21 INOP. REPINNED WIRE HARNESS ASSY 350WL10 UNDER R OW 21 IAW ASM 33-51-00, SCH 04, P101, SHEET 3. OPS CHECKED GOOD IAW AMM 33-51-00-710-008. 2 L 7 2 4F RT A28NM 2007042400244 20070424 00244 EU 2007 4 24 USAA070270 1 20070412 A 5347 SEAT TRACK AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 174US 1492 CORROSION AT 3 PLACES AT LEFT I/B SEAT TRACK FROM FRAME 47-47.2. CUT OFF DAMAGED SECTION, SPLICED IN NEW SECTION PER SR M 53-41-15 FIG 202; CORROSION TASK JA-220-25502, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A28NM 2007042400268 20070424 00268 NM 2007 4 24 USAA070274 1 20070412 A 5320 FLOOR SUPPORT BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 FLOORBOARD SUPPORT ANGLE CRACKED AT STA 500G + 5 S17R. REMOVED & MADE NEW ANGLE PER SRM 53-30-51, 51-10-02, DEFECT SIZE : .5 INCH. 2 L 7 2 4F RT A16WE 2007042400270 20070424 00270 NM 2007 4 24 USAA070272 1 20070412 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 STA 294.5 - 329 S17R HAS CORROSION. REMOVED & MADE NEW Z-ANGLES PER SRM 51-10-02; CORR TASK C53-107-02; LEVEL 2 DEFEC T SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007042400275 20070424 00275 EA 2007 4 24 VNAA0704008 1 20070415 A 5350 GC21905045 RADOME CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE FUSELAGE DAMAGED A VNAA O OTHER O OTHER DE DESCENT 1 GL 05 720PS 5549 10178 CREW REPORTED A LIGHTNING STRIKE ON DESCENT. MAINTENANCE PERFORMED A VISUAL EN ROUTE AND DETAILED LIGHTNING STRIKE INSP ECTION. AIRCRAFT WAS FERRIED TO DAYTON FOR REPAIR. MAINTENANCE INSPECTED AND REPAIRED ALL DAMAGE. MAINTENANCE ALSO RE PLACED THE RADOME IN ACCORDANCE WITH THE AIRCRAFT MAINTNENACE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007042400286 20070424 00286 NM 2007 4 24 ASAA0741586 1 20070420 A 5754 65C26602301 SLAT BOEING 737 7374Q8 138447Q NM NR 2 DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 HL NR 2 LEADING EDGE SLAT UPPER I/B TRAILING EDGE CORNER DISBONDED. REPAIRED IAW SRM 51-70-10 REPAIR NR 4. 2 L 7 2 4F RT A16WE 2007042400287 20070424 00287 NM 2007 4 24 ASAA0741587 1 20070420 A 5320 65C3184779 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 FLOOR SUPPORT CORRODED. FLOOR SUPPORT REPLACED WITH NEW PART IAW SRM 51-40-02 AND 51-40-05. 2 L 7 2 4F RT A16WE 2007042400297 20070424 00297 NM 2007 4 24 ASAA0741589 1 20070420 A 5320 6641210L11 FITTING BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 INTERCOSTAL SHEAR CLIP CRACKED. SHEAR CLIP REPLACED WITH FABRICATED REPAIR PART AT INTERCOSTAL IAW EA 5310 02714. 2 L 7 2 4F RT A16WE 2007042400302 20070424 00302 NM 2007 4 24 ASAA0741591 1 20070420 A 5730 65C2627078 SKIN BOEING 737 7374Q8 138447Q NM RT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 RIGHT WING O/B LEADING EDGE AT WS 290 FIXED LEADING EDGE SKIN CRACKED. FIXED LEADING EDGE SKIN REPAIRED IAW SRM 51-70-1 7. 2 L 7 2 4F RT A16WE 2007042400303 20070424 00303 NM 2007 4 24 ASAA0741592 1 20070420 A 5320 69774772 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 AFT CABIN CORROSION FOUND ON FLOOR SUPPORT ANGLE. CORRODED FLOOR ANGLE REPLACED WITH FABRICATED REPAIR PART IAW SRM 53- 60-51 FIG 20, 51-40-05 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007042400304 20070424 00304 NM 2007 4 24 ASAA0741593 1 20070420 A 5320 6552878U125 SILL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 L2 DOORWAY LOWER SILL CHORD CORROSION FOUND. REPLACED LWR SILL CHORD WITH NEW PART IAW SRM 51-40-05 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007042400305 20070424 00305 NM 2007 4 24 ASAA0741594 1 20070420 A 5320 6545855U122 SILL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 CORROSION FOUND ON R2 SILL CHORD. CORRODED SILL CHORD REPLACED WITH NEW PART IAW SRM 51-40-05 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007042400307 20070424 00307 NM 2007 4 24 ASAA0741596 1 20070420 A 5313 65458001272 STRINGER BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 STR 11L FOUND CRACKED AT FASTENER HOLES. CRACK REPAIRED IAW EA 5310 02714. 2 L 7 2 4F RT A16WE 2007042400309 20070424 00309 NM 2007 4 24 ASAA0771597 1 20070420 A 5320 146A750319 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 AFT PIT FLOOR SUPPORT CORRODED AT STA 772 REPAIRED IAW EA 5320 01799. 2 L 7 2 4F RT A16WE 2007042400326 20070424 00326 NM 2007 4 24 QXEA200700620 1 20070415 A 3260 401020101 PROXIMITY SENSOR BOMBDR DHC8 DHC8402 1390042 NM MLG MALFUNCTIONED A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 417QX 4086 SEA FLIGHT NR 2392: RT MAIN GREEN DOWN LOCKED LIGHT AND RED UNSAFE LIGHT ILLUMINATED. GEAR APPEARED TO STAY UP AND LOCK ED. ALL OTHER INDICATIONS NORMAL. MAINTENANCE QUERIED PSEU AND FOUND RGDLK1 FAULT. PROX SENSOR OPEN FLIGHT LEG 01. R EMOVED AND REPLACED S13RGDK1 IAW 32-61-06-000-802/400-802. PERFORMED OPS TEST OF LANDING GEAR EXTENSION AND RETRACTION IAW 32-31-00-710-801. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007042400327 20070424 00327 WP 2007 4 24 07FDEA01479 1 20070412 A 3210 ARG7557501 BOLT DOUG DC10 DC1010 3022110 WP ZONE 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 390FE 46624 DURING LT MLG REMOVAL, THE LT MLG FWD TRUNNION BOLT (P/N:ARG7557-501) WAS FOUND TO BE CORRODED. ALSO LT MLG FWD TRUNNIO N BOLT SPACER (P/N:ARG7653-3) SPIRAL GROOVE LUBE HOLES WERE NOT DRILLED OUT TO PROPER SIZE PER DOUGLAS B/P: ARG7653. RE PLACED CORRODED TRUNNION BOLT AND SLEEVE WITH SERVICEABLE PARTS ON SEQ 800, W/C 32T1701-L DURING "C" CHECK, W/O 36243 AT LAX HVMX GEAR CHANGE. REF ITEM NR 3A, SEQ 800 S800, ITEM 4K7-14. 2 L 7 3 4F A22WE 2007042400328 20070424 00328 WP 2007 4 24 07FDEA01480 1 20070412 A 3210 ARG7557501 BOLT DOUG DC10 DC1010 3022110 WP ZONE 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 390FE 46624 DURING RT MLG REMOVAL, THE FWD RT TRUNNION BOLT (P/N: ARG7557-501) WAS FOUND TO BE SEVERELY CORRODED. ALSO, THE RT MLG TRUNNION BOLT INNER SLEEVE (P/N: ARG7653- 3), SPIRAL LUBE HOLES WERE NOT DRILLED OUT TO THE PROPER SIZE PER DOUGLAS B/P : ARG7653 REPLACED CORRODED TRUNNION BOLT AND SLEEVE WITH SERVICEABLE PARTS ON SEQ 801, W/C32T1701-R DURING "C" CHECK, W /O36243 AT LAX HVMX GEAR CHANGE REF ITEM NR 3A, SEQ 801, S801, ITEM 4K7-14. 2 L 7 3 4F A22WE 2007042400329 20070424 00329 EA 2007 4 24 MALA070054 1 20070418 A 2740 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 602XJ 8045 ON DEPARTURE, CLEAN CONFIG A/P ON WING LEVEL CLIMBING SPEED 250 AT 6000 FT STAB TRIM RUNAWAY CLACKER CAME ON, IMMED DISC ONNECTED STAB TRIM WITH DISC BUTTON LT SIDE CONTROL YOKE LEVELED OFF EXCESSIVE FORCE REQ. PULLED C/B 2F5 4A1 RETURNED T O MSP STAB TRIM WAS STOPPED AT 6.0. COMPLETED MM 409 NR 302105 COMPLETED OPS TEST, GROUND MAINT TEST, AND FUNCTIONAL TE ST OF HSTCU SYSTEM OPS CHECK GOOD. DOWNLOADED FDR COMPLETED BOMBARDIER ACTION PLAN NR 1. REPLACED HSTCU REF LOG NR 165 1161 FOR TEST FLIGHT. TEST FLIGHT REQUIRED DUE TO STAB TRIM RUNAWAY REF LOG PAGE 1635157. NTSB REQUESTS TEST OF STAB T RIM INPUTS. PERFORMED STAB TRIM INPUT TEST IAW NTSB TRIM SWITCH TESTED. 2 L 7 2 4F RT A21EA 2007042400330 20070424 00330 NM 2007 4 24 DHL2007782506 1 20070406 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 560 S27R CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 782DH 21998 FOUND STR 27R AT BS 560 IS CORRODED. CUT OUT DAMAGED STRINGER APPROX LENGTH 16" IAW B727 SRM 53-10-3 FIG 1. FABBED NEW STRINGER REPAIR FROM P/N BAC1477075T-6 PO NR 5096200 AND P/N BAC 1496-1317075-T6 PO NR 9004539 APPROX DIM 22" IAW B727 SRM 53-10-3 FIG 1 AN SRM 53-10-2 FIG 9. INSTALLED STRINGER REPAIR AT BS 560 AT 27R IAW B727 SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2007042400331 20070424 00331 WP 2007 4 24 IXXA07SMN098S 1 20070208 A 5340 FITTING DOUG DC8 DC862 3021970 WP ZONE 200 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING FRAME, CRACKED AT STATION 759.000, LONGERON 18 LEFT. REMOVED FASTENERS. PERFORMED STOP HOLE ON CRACK END. PERFORMED NDT INSPECTION. NO CORROSION OR CRACK PROGRESSI ON FOUND. FABRICATED REPAIR ANGLE (HORIZONTAL FLANGE) AND (VERTICAL FLANGE) AND FILLER. PERFORMED HEAT TREATMENT. CLE ANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS FROM STATION 759.000 IAW FAA FORM 8110-3, NUMBER 07058 DATED 02-15-07,SEMAN DRAWING NUMBER ED-4461 DATED 02-13-07,EO SEMAN NUMBER 2007220 DATED 02-15-07, DC8 SRM 51-1 -20D, DC8 SRM 51-3-0, SEMAN DRAWING NUMBER ED-4461, DC8 NDT SPM PART 06-10-01-001, FORM SEMAN 242-2, DC8 SRM 51-1-1 PAGE 2 L 7 4 4F 4A25 2007042400332 20070424 00332 WP 2007 4 24 IXXA07SMN099S 1 20070208 A 5512 SKIN DOUG DC8 DC862 3021970 WP ZONE 300 MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER. LEADING EDGE OUTER SKIN NON STANDARD REPAIR AT STA TION XFS 178.750. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA.. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED,TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 07058 DATED 02-15-07, SEMAN DRAWING NUMBE R ED-4450 DATED 02-14-07 AND EO SMN NUMBER 2007194 DATED 02-15-07, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 NDT SPM PART 06 -10-01-001,FORM SMN 242-2, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-20D, AND DC8 SRM 51-3-1. 2 L 7 4 4F 4A25 2007042500002 20070425 00002 NM 2007 4 25 ASAA0771599 1 20070420 A 5347 143A75019 SUPPORT BOEING 737 737790 13844CN NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 FWD PIT CARGO TIE DOWN IS GOUGED AT STA 495 REPAIRED IAW EA 5320 01821. 2 L 7 2 4F RT A16WE 2007042500006 20070425 00006 NM 2007 4 25 UPS07549648 1 20070328 A 5311 143N1017 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 419UP 23906 INSPECTION TYPE:C DENT IN FWD CARGO FUSELAGE FRAME STA 760,S24R. COMPLIED WITH EA 757-5332-A1632 & UPS EO NO B757-5310- 26600-A. 2 L 7 2 4F RT A2NM 2007042500007 20070425 00007 NM 2007 4 25 UPS07549649 1 20070327 A 5311 146N102848 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 419UP 23906 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1220 BETWEEN S25L TO S26L. COMPLIED WITH EA 757-5362-27-A1628 UP S EO B757-5310-26601-A. 2 L 7 2 4F RT A2NM 2007042500008 20070425 00008 2007 4 25 070104 4 20070417 A 3425 4608000306 AHRS DOUG DC9 DC987 3022087 WP NR 1 MALFUNCTIONED A WX0A O OTHER G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 WP 19 948MA 49778 FLIGHT 802 TOL/PIE - THE FLIGHT CREW REPORTED THAT THE LEFT EFIS SYSTEM DISPLAYED "AHRS BUSS 1". THIS MESSAGE WAS ACCOM PANIED BY LOSS OF LEFT ATTITUDE, LEFT HEADING AND RIGHT RMI COMPASS. CAPTAIN SELECTED EFIS TRANSFER TO 'BOTH ON 2' FOR THE REMAINDER OF THE FLIGHT WHICH RESTORED HIS INSTRUMENTS. ST PETERSBURG MAINTENANCE REPORT THE REMOVAL AND REPLACEMEN T OF THE LEFT ATTITUDE/HEADING REFERENCE UNIT. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 22-01-05. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007042500011 20070425 00011 WP 2007 4 25 UPS07849636 1 20070417 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:N/A BTB - EMERGENCY LIGHTS ILLUMINATED IN THE ARMED POSITION WITH A/C POWER ON. MAINTENANCE WILL REPLAC E THE BATTERY/RELAY PACK ASSY AS A PRECAUTIONARY. ORDERED ON REQ A927417. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER MM 33-00-01-2. 2 L 7 4 4F RT 4A25 2007042500015 20070425 00015 NM 2007 4 25 UPS07549651 1 20070328 A 5311 146N1020 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 419UP 23906 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1850, S26R. COMPLIED WITH EA 757-5362-A1635 & UPS EO B757-5310-2 6623-A. 2 L 7 2 4F RT A2NM 2007042500016 20070425 00016 NM 2007 4 25 DLM88070338 1 20070419 A 5330 5911401211 SKIN DOUG MD88 MD88 3023688 NM FS 218 L29R DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 DURING HMV, THE FUSELAGE SKIN WAS SEVERELY DAMAGED NEAR FS 218 AND LONGERON 29R. A PERMANENT REPAIR WAS ACCOMPLISHED PE R BOEING INSTRUCTIONS, AS CONTAINED IN ERA 460138-14. 2 L 7 2 4F RT A6WE 2007042500019 20070425 00019 NM 2007 4 25 UPS07549653 1 20070328 A 5311 143N102518 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 419UP 23906 INSPECTION TYPE:C DENT IN FWD CARGO FUSELAGE FRAME STA 720 BETWEEN S23R AND S24R. COMPLIED WITH EA 757-5332-27-A1631 & UPS EO B757-5310-26595-A. 2 L 7 2 4F RT A2NM 2007042500023 20070425 00023 NM 2007 4 25 UPS07549658 1 20070331 A 5412 311N3271 BULKHEAD BOEING 757 75724APF 1384969 NM NR 2 PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 419UP 23906 INSPECTION TYPE:C NR 2 PYLON AFT BULKHEAD LOWER CORNER INBOARD & OUTBOARD SIDE CHAFED. COMPLIED WITH EA 757-5453-27-A16 37 & UPS EO B757-26607-A. 2 L 7 2 4F RT A2NM 2007042500024 20070425 00024 NM 2007 4 25 UPS07649646 1 20070403 A 5347 SEAT TRACK BOEING 767 76734AF 1385212 NM FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 323UP 27749 INSPECTION TYPE:C SEAT TRACK FLANGES GOUGED AT BS 632-654+20 RBL 54 WL 200. REMOVED AND REPLACED SEAT TRACK SECTION BS 621-654+55 RBL 54 IAW ER 07 07-1909 AND SRM 53-00-52-2R 9 FIG 201. 2 L 7 2 4F RT A1NM 2007042500027 20070425 00027 WP 2007 4 25 UPS07849672 1 20070420 A 3350 SOCKET DOUG DC8 DC873F 302199F WP CONTROL PANEL INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:N/A EMERGENCY ELECTRIC CONTROL PANEL HAS INOP LIGHT SOCKETS. DEFERRED EMERGENCY ELEC CONTROL PANEL LIGH TS PER MEL 33-1. [SUP 4-25-07] REMOVED AND REPLACED LIGHT PANEL PER DC8 MM 33, SYSTEM CHECKED OK. CLEARED DMI 348799 AND REMOVED PLACARD. 2 L 7 4 4F RT 4A25 2007042500034 20070425 00034 NM 2007 4 25 UPS07549634 1 20070328 A 5311 146N103069 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 419UP 23906 INSPECTION TYPE:C DENTS IN FT CARGO FUSELAGE FRAME STA 1480, BETWEEN S25L AND S26L (2EA). FRAME REPAIR AT STA 1480 BETW EEN S25L & S26L (2EA) ACCOMPLISHED PER EA 757-5362-27-A1636, WITH NO DEVIATIONS AND PER UPS EO B757-5310-26570-A. 2 L 7 2 4F RT A2NM 2007042500037 20070425 00037 WP 2007 4 25 UPS07849626 1 20070402 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 MAIN CARGO FLOORBEAM AT STA 280 RBL 24 CRACKED FROM EXFOLIATION CORROSION. CUT OUT DAMAGED AREA OF F LOORBEAM AT STA 280 RBL 24 IAW SRM 51-2-1 PG 8 FIG 1. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW SRM TR 51-13 0 FIG 1 SHEET 1. 2 L 7 4 4F RT 4A25 2007042500039 20070425 00039 SO 2007 4 25 SIMA200710004 1 20070419 A 3350 20131A POWER SUPPLY EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHTS FAILED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 716AE 10557 5110 145264 EMERGENCY LIGHT WOULD NOT TEST PROPERLY. REMOVED AND REPLACED NUMBER 1 EMERGENCY POWER SUPPLY IAW EMB 33-50-04. OPERAT IONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042500041 20070425 00041 EU 2007 4 25 SIMA200711002 1 20070417 A 3020 DUCT SAAB SF340 340B 7860101 EU INTAKE FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 391AE 442 340B391 RIGHT INTAKE LIGHT ILLUMINATED IN FLIGHT, RETURNED TO LAX. REMOVED AND REPLACED RIGHT LOWER INTAKE DUCT IAW SAAB AMM. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007042500047 20070425 00047 NM 2007 4 25 UPS07449644 1 20070419 A 5755 SKIN BOEING 747 747200 1384847 NM NR 5 SPOILER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:N/A NR 5 FLT SPOILER HAS UPPER SURFACE SKIN PEELING BACK AND DELAMINATED APPROX 25 PERCENT OF SURFACE AR EA. REMOVED AND REPLACED NR 5 FLT SPOILER IAW AMM 27-61-01. OPS CHECKS GOOD. 2 L 7 4 4F RT A20WE 2007042500048 20070425 00048 NM 2007 4 25 UPS07549641 1 20070418 A 5230 143N80272 CAM BOEING 757 75724APF 1384969 NM CARGO DOOR BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 461UP 28265 INSPECTION TYPE:N/A NR 3 MCD FWD LATCH CAM BROKEN. REMOVED AND REPLACED NR 3 MCD LATCH CAM IAW EO B757-5230-2665-A PG 4 ITEM 10 AND REF IPC B757 52-32-52-05 ITEM 190 AND B757 AMM 20-11-00-2. OPERATIONAL CHECK OF MCD NORMAL PER B757 AMM 52 -32-00-5. 2 L 7 2 4F RT A2NM 2007042500050 20070425 00050 WP 2007 4 25 UPS07849639 1 20070330 A 5330 57799133N1 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 AFTER REMOVAL OF C-2 (B-PIT) SCUFF PLATE FOUND CORROSION ON FUSELAGE SKIN. REMOVED CORROSION AND FOU ND SKIN TO BE OUT OF LIMITS IAW SRM 53-2-0 FIG 1F. PROCURED AND INSTALLED REPLACEMENT SKIN FROM STA 450-610 L31L-L31R I AW SRM 51-1-20D, AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007042500051 20070425 00051 NM 2007 4 25 UPS07M49647 1 20070302 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:C AFT CARGO STA 1967 LONGERON R40 FOUND WITH CORROSION AS MARKED. AFT CARGO LONGERON R40 STA 1958-1980 DAMAGED AREA CUT & REMOVED. HFEC INSP CARRIED OUT & NO CRACK EVIDENT. LONGERON & SPLICE FAB. FPI CARRIED ON FAB LONGE RON & SPLICE, FOUND NO CRACK. LONGERON & SPLICE FASTENER HOLE PICK UP. NEW LONGERON & SP SPLICE REPROTECTED. NEW LONG ERON, SPLICE, FRAME & SHEAR CLIP INSTALLED PER SRM 53-10-00 FIG 1&2 VOL I REV 38 & SRM 51-31-01 VOL II REV 38. 2 L 7 3 4F RT A22WE 2007042500054 20070425 00054 NM 2007 4 25 UPS07M49661 1 20070301 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:C CTR CARGO STA 5-113, LONGERON L40 FOUND WITH CORROSION AS MARKED. CTR CARGO STA 5-113 LONG L40 SPLICE & CORROSION LONGERON CUT OFF PER SRM 51-33-01 V2 R38. REP LONG & SPLICE FAB PER SRM 53-10-00 FIG 2 V1 R38. FPI CUT OU T PER DPS 4.707 ON FAB LONG & SPLICE FOUND NO CRACK EVIDENT ALL REPAIR PARTS REPROTECTED PER SRM 51-21-01 V2 R 38. OK T O INSTALL. REPAIR LONG & SPLICE INSTALLED PER SRM 53-10-00 V1 R38. 2 L 7 3 4F RT A22WE 2007042500056 20070425 00056 NM 2007 4 25 UPS07M49662 1 20070212 A 5753 NRC67681 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM FLAP VANE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:C LEFT OUTBOARD FLAP, FLAP VANE SUPPORT FITTINGS FOUND WITH CORROSION AT INTERIOR OF LIGHTENING HOLES AS MARKED. LEFT O/B FLAP VANE REMOVED AS PER AMM 27-50-32 R 55. SEND TO SHOP FOR REPAIR. LEFT O/B FLAP VANE INSTALLED A S PER AMM 27-50-32 R55. OPERATIONAL AND TEST CARRIED OUT AS PER AMM 27-50-00 REV 55. 2 L 7 3 4F RT A22WE 2007042500057 20070425 00057 GL 2007 4 25 SIMA200711006 2 20070415 A 7261 AE3007A13 ENGINE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL NR 2 LEAKING A SIMA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 802AE 14471 6792 145471 CAE311654 OIL ODOR COMING FROM NUMBER 2 ENGINE BLEED SYSTEM, RETURNED TO RDU. REMOVED AND REPLACED NUMBER 2 ENGINE IAW AMERICAN E AGLE WORK CARD 72-000-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007042500059 20070425 00059 SO 2007 4 25 SIMA200711008 1 20070417 A 2760 8005701 PROXIMITY SENSOR EMB 135 EMB135KL 3260302 SO SPOILERS FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 849AE 9665 145716 SPOILER FAIL MESSAGE, SPOILERS SHOWED OPEN WHEN CLOSED. RETURNED TO DFW. REMOVED AND REPLACED LEFT AND RIGHT SPOILER P ROXIMITY SENSORS. 2 L 7 2 4F RT T00011AT 2007042500060 20070425 00060 NM 2007 4 25 UPS07M49667 1 20070421 A 2841 INDICATION SYS DOUG MD11 MD11F 3023600 NM FUEL SYSTEM MALFUNCTIONED A IPXA K NONE O OTHER UK UNKNOWN 1 SO 01 284UP 48541 DIVERSION - ALL FUEL QUANTITIES INDICATORS ROLLED BACK. DEFERRED NR 2 FUEL QUANTITY M348824. [SUP 05-07-07] REPLACED MULTI JUNCTION PROBE PER MM 28-41-40-4. ALSO REPLACED SEM PER MM 28-41-92-4. ACCOMPLISHED FUEL SYSTEM TEST AS REQUIRED, NO FAULTS FOUND. QTY WORKS NORMAL AT THIS TIME. THIS CLEARS M348824. 2 L 7 3 4F RT A22WE 2007042500064 20070425 00064 SO 2007 4 25 SIMA200711011 1 20070417 A 5310 14538111001 RIB EMB 145 EMB145LR 3260212 SO ZONE 200 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 668HH 8008 145785 BIRD STRIKE INSPECTION REVEALED DENT AFT OF FRAME 10 BETWEEN STRINGER 2R AND CENTER LINE ABOVE WINDOW. REMOVED AND REPL ACED RIB AT FRAME 10 ABOVE WINDOW IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007042500065 20070425 00065 NM 2007 4 25 SWAA071863 1 20070414 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED SPV CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS DIM WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED BATTERY PACKS AND BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007042500067 20070425 00067 NM 2007 4 25 SWAA071963 1 20070420 A 5322 69353656 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 13R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007042500069 20070425 00069 NM 2007 4 25 SWAA071856 1 20070413 A 5340 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007042500070 20070425 00070 NM 2007 4 25 SWAA071854 1 20070413 A 5340 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 22R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007042500071 20070425 00071 NM 2007 4 25 SWAA071837 1 20070412 A 5330 65C381921 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504C, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007042500072 20070425 00072 EU 2007 4 25 07FDEA01500 1 20070413 A 5330 NSA66035 SKIN AIRBUS 310 A310324 3930206 EU FUSELAGE CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 810FD 452 DUE TO REMOVAL OF SOME FASTENERS DURING REMOVAL OF CORROSION ON OUTER SKIN AT C80, P5-6 RHS IT WAS IMPOSSIBLE TO REINSTA LL SOME FASTENERS WITHOUT DAMAGING THE AFT PRESSURE BULKHEAD. REPAIR PERFORMED BY INSTALLATION OF FOUR ALTERNATE BOLTS NSA 6603-5, APPROVED BY EA 6-5319-103240 AND RAS/DAHAM/4020934/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007042500073 20070425 00073 NM 2007 4 25 SWAA071843 1 20070412 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 395, STR 14L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007042500074 20070425 00074 NM 2007 4 25 SWAA071842 1 20070412 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 372, STR 14L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007042500075 20070425 00075 NM 2007 4 25 SWAA071857 1 20070415 A 3397 8100022628 CONNECTOR BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 249WN 34951 EEPLS INOP AT ROW 1 ABC. SECURED EEPLS CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2007042500076 20070425 00076 NM 2007 4 25 SWAA071850 1 20070413 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND STRINGER 4R CRACKED AT BS 887. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007042500077 20070425 00077 NM 2007 4 25 SWAA071972 1 20070422 A 3350 100031 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 406WN 27894 FWD CABIN EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2007042500078 20070425 00078 NM 2007 4 25 SWAA071971 1 20070422 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007042500079 20070425 00079 NM 2007 4 25 SWAA071964 1 20070420 A 5311 141A1120 FRAME BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 745SW 29491 DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 296, RBL 54, WL 209. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007042500080 20070425 00080 NM 2007 4 25 QXEA200700621 1 20070415 A 3231 MECHANISM BOMBDR DHC8 DHC8402 1390042 NM MLG DOOR BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 SEA FLIGHT NR 2372: LANDING GEAR EXTENSION DOOR LOCKING MECHANISM BROKEN. DOOR WILL NOT CLOSE. MAINTENANCE REPLACED LA TCHING MECHANISM AS REQUIRED. OPS CHECK GOOD. NO OTHER DEFECTS NOTED. NO OTHER PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007042500083 20070425 00083 EA 2007 4 25 SWIA200718097 1 20070410 A 5610 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 07 706SK 10149 CRACK IN UPPER LEFT CORNER OF LEFT WINDSHIELD. REPLACED PILOT'S WINDSHIELD PER CRJ 200 MM 56-11-01, PN NP139321-13 S/N OFF 04017H3560. 2 L 7 2 4F RT A21EA 2007042500086 20070425 00086 EA 2007 4 25 SWIA200718099 1 20070411 A 3350 LENS CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BROKEN A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 732SK 10194 EMERGENCY LIGHT LENS PLACARD IS MISSING AT GALLEY SERVICE DOOR. REPLACED FLOOD LIGHT ASSEMBLY IAW CRJ MM 33-51-01. 2 L 7 2 4F RT A21EA 2007042500087 20070425 00087 EA 2007 4 25 SWIA200718100 1 20070412 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT MISSING A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 918SW 7645 AFT RED EMERGENCY EXIT SIGN IS MISSING. REPLACED AFT RED EMERGENCY EXIT SIGN IAW AMM 33-51-00. 2 L 7 2 4F RT A21EA 2007042500088 20070425 00088 EA 2007 4 25 SWIA200718101 1 20070415 A 3397 TERMINAL BLOCK CNDAIR CL600 CL6002C10 1390015 EA CHART LIGHT SHORTED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 742SK 10197 CAPTAINS AND FIRST OFFICERS CHART LIGHTS ARE INOP. FOUND CHART HOLDER WIRING TO BE SHORTING TO TERMINAL BLOCK ON LIGHT STRIP DUE TO LOOSE HARDWARE. SECURED LOOSE HARDWARE ON CAPTAINS AND FIRST OFFICERS CHART LIGHTS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007042500089 20070425 00089 2007 4 25 SWAA071959 4 20070420 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 457WN 33856 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007042500090 20070425 00090 NM 2007 4 25 SWAA071960 1 20070420 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, LBL 4. REPAIRED SKIN PER SB AND SRM. 2 L 7 2 4F RT A16WE 2007042500094 20070425 00094 NM 2007 4 25 SWAA071965 1 20070421 A 5311 6545805 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 277, STR 16L. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007042500097 20070425 00097 NM 2007 4 25 SWAA071961 1 20070420 A 5330 6547955 BEAR STRAP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT BS 846, STR 26R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007042500100 20070425 00100 NM 2007 4 25 SWAA071968 1 20070421 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007042500101 20070425 00101 WP 2007 4 25 07FDEA01518 1 20070416 A 5330 SKIN DOUG DC10 DC1010 3022110 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 397FE 46631 DURING MD10-10 ACF MODIFICATION AND REPAIR ASSESSMENT PROG EXISTING REPAIR ON SKIN STA 1039 RT SIDE BETWEEN L 50 TO L 51 . REMOVED EXISTING REPAIR IAW SRM 51-35-01 VOL II . CUT DAMAGED SKIN AND REMOVED CORROSION. PERFORMED CHECK LIMITS AN D TREATED IAW SRM 51-21-01 VOL II. REPAIRED SKIN IAW SRM 53-20-00 FIG 6 SH 3-4. 2 L 7 3 4F A22WE 2007042500102 20070425 00102 NM 2007 4 25 SWAA071883 1 20070416 A 3350 D71701100 BATTERY PACK BOEING 737 7377AD 1384502 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 798SW 28436 DURING SCHEDULED HC1 CHECK, RIGHT OVERWING EMERGENCY EXIT LIGHT FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007042500105 20070425 00105 NM 2007 4 25 SWAA071892 1 20070416 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 761RR 27875 DURING SCHEDULED CV CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007042500107 20070425 00107 EU 2007 4 25 07FDEA01532 1 20070420 A 5554 A55471602200 ATTACH FITTING AIRBUS 300 A300B4605R 3930308 EU ZONE 300 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 FOUND DEFORMATION AT RUDDER ATTACH FITTING UPPER FLANGE (P/N A554-71602-200), SIZE OF DEFORMATION: 5MM BY 5MM, DEPTH 2MM . DEFORMATION AREA IS FREE OF CRACKS AND CORROSION, NO REPAIR ACTION REQUIRED IAW EA 6-5546-106448 AND RAS/DAHAM/402209 1/2007 ISSUE "A". 2 L 7 2 4F RT A35EU 2007042500109 20070425 00109 WP 2007 4 25 IXXA07SMN101S 1 20070208 A 5753 SKIN DOUG DC8 DC862 3021970 WP ZONE 500 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP LOWER SKIN HAS A NON STANDARD REPAIR, AT STATION XW 115. 000. REMOVED PLATING WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN AND REPAIR PARTS. CLEANED, TREATED AND PR IMED AREA AND PLATING. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN AND REPAIR PARTS IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-7-1 FIGURE 1 PAGE 2 ITEM "D", DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 2007042500112 20070425 00112 NM 2007 4 25 SWAA071893 1 20070416 A 3246 BEARING BOEING 737 7377H4 1384404 NM LT MLG FAILED A SWAA K NONE O OTHER TX TAXI/GRND HDL 1 SW 29 765SW AD384 29805 NR 1 TIRE REPORTED FLAT BY ANOTHER AIRCRAFT. INSPECTED LEFT MLG, FOUND AXLE DAMAGE DUE TO NR 1 WHEEL BEARING FAILED. R EMOVED AND REPLACED NR 1 MLG INNER CYLINDER PER MM. 2 L 7 2 4F RT A16WE 2007042500113 20070425 00113 NM 2007 4 25 SWAA071900 1 20070418 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 420WN 29825 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 15 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007042500116 20070425 00116 NM 2007 4 25 SWAA071891 1 20070416 A 3350 471A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 223WN 32492 DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER MISSING AT ROW 13 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007042300132 20070423 00132 SO 2007 4 23 SIMA200710721 1 20070413 A 5321 145224459003 RAMP EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AE 4800 145275 RIGHT FLOOR PANEL RAMP CORRODED FROM FRAME 18R TO 20R. REMOVED AND REPLACED RAMP IAW EMB SRM 51-40-02. RETURNED AIRCRA FT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300133 20070423 00133 SO 2007 4 23 SIMA200710722 1 20070413 A 5347 13500439003 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 718AE 15775 4800 145275 LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAME 23 TO 32. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURN ED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042300170 20070423 00170 NM 2007 4 23 CALA0700182 1 20070417 A 5315 141T5108 FLOORBEAM BOEING 767 767424ER 1385270 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76065 29460 FLOOR SUPPORT CORRODED AT BS 325, LBL 53-55. REPAIRED IAW SRM 53-00-51 FIG 201, REPAIR 1. 2 L 7 2 4F RT A1NM 2007042300172 20070423 00172 NM 2007 4 23 CALA0700184 1 20070418 A 5242 6545830 SKIN BOEING 737 7373T0 1384582 NM E&E BAY DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 SKIN CRACKED AT FWD CORNER OF E&E DOOR RIVET. REPAIRED IAW SRM 52-00-01 FIG 201. 2 L 7 2 4F RT A16WE 2007042300187 20070423 00187 EA 2007 4 23 COMA0760321 1 20070416 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 708CA 7235 FLAPS FAIL CAUTION MSG. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G ) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007042300192 20070423 00192 EA 2007 4 23 COMA0760310 1 20070410 A 2424 GCU CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 01 447CA 7552 ADG DEPLOYED ON WEIGHT OFF GEAR, A/C RETURNED TO ABE AND LANDED SAFELY. REPLACED THE ADG GCU. 2 L 7 2 4F RT A21EA 2007042400010 20070424 00010 EA 2007 4 24 SWIA200718141 1 20070313 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 865AS 7507 RBL9 STATION 280 LOWER FLOOR SUPPORT IS CRACKED AT INBOARD AND OUTBOARD CLIPS, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLE ANGLE FILLER IAW CRJ200 REO 601R-53-11-171 STEP 6 AND 7. INSTALLED CLIPS AND FILLERS AT STATION 280 RBL 9.0 IAW C RJ200 REO 601R-53-11-171, REV D REPAIR SCHEME B. 2 L 7 2 4F RT A21EA 2007042400011 20070424 00011 EA 2007 4 24 SWIA200718142 1 20070313 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 865AS 7507 PAX DOOR FORWARD WEB CRACKED AT HANDRAIL SUPPORT BRACKET, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLES AND DOUBLER ON FORWARD PAX DOOR WEB PER CRJ200 REO 601R-52-11-702 REV A STEP 8 THRU 12. 2 L 7 2 4F RT A21EA 2007042400014 20070424 00014 EA 2007 4 24 SWIA200718144 1 20070313 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 865AS 7507 PAX DOOR AFT WEB CRACKED AT HANDRAIL SUPPORT BRACKET, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLES AND DOUBLER ON AFT PAX DOOR WEB PER CRJ200 REO 601R-52-11-702 REV A STEP 5-12. 2 L 7 2 4F RT A21EA 2007042400019 20070424 00019 EA 2007 4 24 SWIA200718147 1 20070313 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT MLG WW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 865AS 7507 LEFT WHEEL WELL BRAKE TRANSDUCER BRACKET IS CRACKED, DISCOVERED AT C-CHECK. REPLACED CRACKED SUPPORT BRACKET PN 601R 75 2-62-157 IN LEFT WHEEL WELL PER CRJ200 SRM 51-42-06 AND CRJ200 MOD IS601R 5320-0003 REV 'A'. 2 L 7 2 4F RT A21EA 2007042400020 20070424 00020 NM 2007 4 24 QXEA200700640 1 20070418 A 2420 DH103024600CSIIB INVERTER DHAV DHC8 DHC8202 2809007 NM MALFUNCTIONED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 357PH 1436 504 YVR FLIGHT NR 2127 - AUX INVERTER POWER CIRCUIT BREAKER ACCOMPANIED BY ELECTRICAL ODOR IN COCKPIT. MAINTENANCE REPLACED AUX INVERTER IAW AMM. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007042400023 20070424 00023 NM 2007 4 24 07FDEA01524 1 20070418 A 5320 WEB BOEING 727 727233 138408A NM BS 760-780 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 223FE 20935 WEB AT STA 760-780 RBL65-70.5 IS CRACKED STR 17R 3 " CRACK FABRICATED WEB ON TRAVELER T7/671242 AND SRM 51-10-1. INSTAL LED ON NR S00009. 2 L 7 3 4F RT A3WE 2007042400027 20070424 00027 NM 2007 4 24 ASAA0741584 1 20070420 A 5320 65496793 INTERCOSTAL BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 INTERCOSTAL BETWEEN FRAMES CRACKED AT FWD END. REMOVED AND REPLACED CRACKED INTERCOSTAL PER SRM 51-30-01 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007042400035 20070424 00035 EA 2007 4 24 SWIA200718106 1 20070316 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 OUTBOARD CLIP AT FS280 RBL 9 IS CRACKED, DISCOVERED DURING C-CHECK. REPLACED DAMAGED OUTBOARD CLIP P/N 601R311011-57 AT FS280 RBL9 IAW CRJ200 SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007042400036 20070424 00036 NM 2007 4 24 ASAA0741577 1 20070413 A 3350 S283TO143 CHARGER BOEING 737 737490 1384715 NM CABIN MALFUNCTIONED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 796AS 28891 SEVERAL (4 TOTAL) EMERGENCY LIGHTS COME ON MOMENTARILY THEN GO OUT RIGHT AWAY DURING EMERGENCY LIGHTS TEST. REPLACED BA TTERY CHARGER AND BATTERY PACK. 2 L 7 2 4F RT A16WE 2007042400043 20070424 00043 NM 2007 4 24 QXEA200700647 1 20070419 A 2840 UNKNOWN DHAV DHC8 DHC8202 2809007 NM PUMP LIGHT UNKNOWN A QXEA D RETURN TO BLOCK P NO WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 374PH 528 PDX FLIGHT NR 2204 - NR 2 AUX PUMP LIGHT DOES NOT ILLUMINATE AFTER START WITH SWITCH SELECTED ON. LIGHT DOES TEST. MAI NTENANCE GROUND RAN AIRCRAFT, CYCLED BOTH AUX PUMPS ON AND OFF SEVERAL TIMES. BOTH LIGHTS OPS CHECK GOOD. NO PARTS REP LACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007042400046 20070424 00046 EA 2007 4 24 SWIA200718151 1 20070417 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 446SW 7666 FOUND RIGHT SIDE WINDOW IS CRACKED. REPLACED RIGHT SIDE WINDOW IAW AMM 56-12-01, P/N NP139322-001, S/N 02063H9831. 2 L 7 2 4F RT A21EA 2007042400069 20070424 00069 WP 2007 4 24 IXXA07SMN122S 1 20070223 A 5710 SPLICE DOUG DC8 DC862F 3021972 WP ZONE 600 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, NR 4 ALT TANK SPLICES FITTING SHOW CORROSION OUT OF LIMITS AT STA XRS 435 NEAR S60. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-0 PAGE 16. REMOVED CORRODED SPL ICE FITTING IAW DC8 SRM 51-1-20D. FABRICATED SPLICE FITTING IAW ATI REPAIR SPECIFICATION NR 2003-05, DWG DOUGLAS NR 364 0143. PERFORMED HEAT TREATMENT IAW DC8 SRM 51-1-1 PAGES 1, 13, 17. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 08-00 -02 TO 07. CLEANED, TREATED AND PRIMED AREA & SPLICE FITTING. IAW DC8 SRM 51-1-8B. INSTALLED SPLICE FITTING. IAW DC8 SR M 51-1-20D, DC8 SRM 51-3-1. L 2 L 7 4 4F 4A25 2007042400070 20070424 00070 WP 2007 4 24 IXXA07SMN124S 1 20070223 A 5340 46413240501 FITTING DOUG DC8 DC862F 3021972 WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C-CHECK INSPECTION, FOUND MAIN CARGO BATHTUB FITTING CRACKED AT STATION 1530 L34L. REMOVED AND REPLACED BATHTUB FITTING. IAW DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 2007042400073 20070424 00073 NM 2007 4 24 KCSA071153 1 20070418 A 5347 SEAT TRACK BOEING 747 747236B 1384804 NM CARGO BAY CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 FWD PIT SEAT TRACK CRACKED AT BS 765, RBL 25. 2 L 7 4 4F A20WE 2007042400075 20070424 00075 NM 2007 4 24 KCSA071151 1 20070417 A 5330 SKIN BOEING 747 747236B 1384804 NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STA 1000 STR 19L LAP SEAM ON SKIN DENTED. 2 L 7 4 4F A20WE 2007042400100 20070424 00100 SO 2007 4 24 RAIA00704044 1 20070415 A 3020 M932466022M RELAY EMB 145 EMB145 3260210 SO ANTI-ICE SYS FAULTY A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 802HK 145066 FLT NR 3570 - PIT - E1 ANTI-ICE FAIL MESSAGE WITH VALVE SECURED OPEN. MAINTENANCE REPLACED RELAY K0534, SYSTEM OPS CHEC K GOOD. 2 L 7 2 4F RT T00011AT 2007042400103 20070424 00103 SO 2007 4 24 RAIA00704048 1 20070416 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO AIRSTAIRS INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 825HK 145510 PRE FLT NR 5493 - STL - EMERGENCY LIGHT ON HAND RAIL HINGE OF AIRSTAIRS INOP. MAINTENANCE DEFERRED LIGHT PER MEL. 2 L 7 2 4T RT T00011AT 2007042400108 20070424 00108 SO 2007 4 24 RAIA00704039 1 20070413 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN DIRTY A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 833HK 145240 PRE FLT NR 8008 - IAD - LEFTHAND SIDE EXIT EMERGENCY LIGHT OVERWING EXIT MARKER INOP. MAINTENANCE CLEANED CONNECTOR AT INVERTER 4 & 5 SYSTEM, OPERATIONAL NORMAL. 2 L 7 2 4T RT T00011AT 2007042400110 20070424 00110 SO 2007 4 24 RAIA00704042 1 20070414 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 810HK 145231 PRE FLT NR 8065 - ORD - EMERGENCY LIGHT RIGHTHAND OVERWING EXIT MARKER INOP. MAINTENANCE SECURED CONNECTOR ON LIGHT ASS Y. OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007042400116 20070424 00116 NM 2007 4 24 HALA0700171 1 20070415 A 2913 66180 PUMP BOEING 717 717200 1383700 NM LT HYD SYSTEM FLUCTUATES A HALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 480HA 55125 LT HYDRAULIC PUMP FAIL. PRESSURE FLUCTUATED BETWEEN 3000 PSI AND ZERO AT FLIGHT IDLE. TURNED LT ENG DRIVEN PUMP OFF AN D TURNED ON TRANSFER PUMP, PRESSURE AND QTY NORMAL.//R/R LEFT ENG HYD PUMP PER M/M 29-11-01 GRD RUN GOOD CHECKED PLUG P1 -3355 PIN A TO PLUG P1-7824B PIN B3 WIRING CHKD OK, CHECKED S-32 CHECK OK PER 717 FIM 29-10 TASK 801 HHAL5743/580. 2 L 7 2 4F TR A6WE 2007042400119 20070424 00119 WP 2007 4 24 IXXA07SMN127S 1 20070223 A 5730 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND NUMBER 1 STUB WING SKIN LOWER PART HAS A NON STANDARD REPAIR AT STATION XFS 56 2.5. REMOVED EXISTING NON STANDARD REPAIR. PERFORMED STOP HOLE ON CRACK END. FABRICATED EXTERNAL DOUBLER AND INTERNAL DOUBLER. PERFORMED HEAT TREATMENT. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SUR FACES. INSTALLED REPAIR PARTS. IAW DC8 SRM 57-2-1A FIGURE 1 PAGE 3, DC8 SRM 51-1-21, DC8 SRM 51-1-1 PAGES 1,13,17, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-20D, AND DC8 SRM 51-3-1. 2 L 7 4 4F 4A25 2007042400136 20070424 00136 NM 2007 4 24 SWAA071861 1 20070416 A 3610 212A2410 DUCT BOEING 737 7373A4 1384585 NM FUSELAGE CRUSHED A SWAA G O2 MASK DEPLOYED J WARNING INDICATION CL CLIMB 1 SW 29 676SW 23288 AT FL 240, CABIN ALT HORN SOUNDED, ALT CLIMBED TO 15,000 FT AND MASKS DEPLOYED. FOUND AFT PRESSURE BULKHEAD APU PNEUMAT IC DUCT CRUSHED. REMOVED AND REPLACED AFT PRESSURE BULKHEAD APU PNEUMATIC DUCT PER MM. 2 L 7 2 4F RT A16WE 2007042400139 20070424 00139 NM 2007 4 24 SWAA071871 1 20070416 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 238WN 34713 EEPLS LIGHT COVER BROKEN AT ROW 3 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007042400159 20070424 00159 NM 2007 4 24 SWAA071860 1 20070415 A 3234 BACC2C4C00996 CABLE BOEING 737 7373H4 1384600 NM COCKPIT OUT OF RIG A SWAA K NONE J WARNING INDICATION AP APPROACH 1 SW 29 303SW 22943 ON APPROACH TO LAX LOWERED LANDING GEAR, 3 GREEN AND 3 RED INDICATOR LIGHTS ILLUMINATED. EXTENDED LANDING GEAR MANUALLY , GEAR INDICATED SAFE. FOUND GEAR HANDLE CABLE OUT OF RIG. RIGGED GEAR HANDLE CABLE PER MM. 2 L 7 2 4F RT A16WE 2007042400161 20070424 00161 2007 4 24 SWAA071872 4 20070416 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007042400162 20070424 00162 2007 4 24 SWAA071873 4 20070416 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007042400163 20070424 00163 NM 2007 4 24 SWAA071881 1 20070416 A 3350 D71701100 BATTERY BOEING 737 7377AD 1384502 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 798SW 28436 DURING SCHEDULED HC1 CHECK, LEFT FWD CABIN EMERGENCY EXIT LIGHT FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007042400167 20070424 00167 2007 4 24 SWAA071858 4 20070413 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR MALFUNCTIONED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 404WN 27892 DURING SCHEDULED MV2 CHECK, UNSUCCESSFUL DEPLOYMENT OF R1 DOOR EMERGENCY EVAC SLIDE. REMOVED AND REPLACED EVAC SLIDE PE R MM. 2 L 7 2 4F RT A16WE 2007042400177 20070424 00177 NM 2007 4 24 SWAA071953 1 20070419 A 5311 6546541 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 1. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2007042400181 20070424 00181 NM 2007 4 24 SWAA071950 1 20070419 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 9L. REPAIRED FRAME PER EA. 2 L 7 2 4F RT A16WE 2007042400184 20070424 00184 NM 2007 4 24 SWAA071947 1 20070419 A 5311 65C2565510 FRAME BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007042400187 20070424 00187 NM 2007 4 24 SWAA071935 1 20070419 A 5754 65C266011 SLAT BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED C2 CHECK, FOUND LT WING NR 1 L/E SLAT DELAMINATED AT UPPER T/E WEDGE. REMOVED AND REPLACED NR 1 SLAT P ER MM. 2 L 7 2 4F RT A16WE 2007042400188 20070424 00188 NM 2007 4 24 SWAA071936 1 20070419 A 5754 65C2660399 SLAT BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED C2 CHECK, FOUND LT WING NR 3 L/E SLAT DELAMINATED AT UPPER T/E WEDGE. REMOVED AND REPLACED NR 3 SLAT P ER MM. 2 L 7 2 4F RT A16WE 2007042400196 20070424 00196 NM 2007 4 24 2007UALA01201 1 20070417 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 UPPER DECK AFT MOST WALL EEL INOPERATIVE. REPAIRED SHORTED AND ARCING FEEDER WIRE, SPLICED IN NEW SECTION. CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007042400198 20070424 00198 NM 2007 4 24 2007UALA01203 1 20070416 A 3350 SIGN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 506UA 24627 AT THE L3 DOOR THE LOWER EMERGENCY EXIT SIGN IS INOP. [SUP 4-24-07] REPINNED CONNECTOR D6676 IAW WDM 33-51-22. OPS CH ECK GOOD PER MM 33-51-10. 2 L 7 2 4F 4 F RT A2NM E17NE 2007042400224 20070424 00224 NM 2007 4 24 2007UALA01187 1 20070416 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 SEATS 4E & 5A EEL ARE INOPERATIVE. REPLACED WITH NEW EMERGENCY LIGHT. OP CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007042400253 20070424 00253 NM 2007 4 24 USAA070281 1 20070412 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 BS 727D BETWEEN S-8L AND S-9L HAS CRACK. INSTALLED REPAIR ANGLES PER TR 53-10-20E, DEFECT SIZE: .030 INCH (2 EA). 2 L 7 2 4F RT A16WE 2007042400266 20070424 00266 NM 2007 4 24 USAA070276 1 20070412 A 5754 65C26602224 SKIN BOEING 737 737401 1384701 NM L/E SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 NR 5 SLAT WEDGE LOWER SURFACE AT OUTBOARD AUX TRACK. INSTALLED REPAIR DOUBLER PER SRM 51-70-10, REP 4, DEFECT SIZE: 2 X 6 INCHES. 2 L 7 2 4F RT A16WE 2007042400272 20070424 00272 NM 2007 4 24 SB07028 1 20070417 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 440US 24811 DCA - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 24 AND 25 INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007042500012 20070425 00012 NM 2007 4 25 DL757070333 1 20070417 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM FS 590-661 CANNING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 669DN 25142 DURING ACCOMPLISHMENT OF REVISION D OF ER/A 098031-14AD, PERMANENT REPAIR INSTRUCTIONS, SKIN PANEL WAS REPLACED. OLD RE PAIRS HAD OVERSIZED HOLES AND WERE FILLED WITH OVERSIZED FASTENERS PER BOEING INSTRUCTIONS. BOEING PROVIDED 8100 APPROV ING REPAIR. AS SKIN PANEL WAS REPLACED, AD IS NO LONGER AFFECTED. 2 L 7 2 4F RT A2NM 2007042500013 20070425 00013 NM 2007 4 25 DL757070334 1 20070417 A 2120 UNKNOWN BOEING 757 757232 1384965 NM CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 661DN 24972 ELECTRIC ODOR THROUGHOUT FLT VICINITY AFT LAV. RAN ALL ELEC DEVICES THROUGHOUT CABIN. OPENED AFT CEILING PANELS LAV SH ROUDS. LAV WATER HEATERS CKS GOOD CKD. RECIRC FANS. NO ELEC ODOR. SLIGHT MUSTY ODOR AFT LT LAV. DRAINED AND SVC LAV S. NO OTHER DISCREPANCIES FOUND. 2 L 7 2 4F RT A2NM 2007042500026 20070425 00026 WP 2007 4 25 UPS07849666 1 20070421 A 2150 A/C PACK DOUG DC8 DC871F 302199D WP A/C BAY ODOR A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 01 718UP 46018 INSPECTION TYPE:N/A STALE ODOR IN FLIGHT APPEARS TO COME FROM RIGHT PACK. NO SMELL NOTED WHEN LEFT PACK RAN. TRANSFERR ED RIGHT PACK INOP PER MEL 21-38-1. DEFERRAL M348809. PERFORMED ADJ/TEST OF RT PACK W/NO DEFECTS NOTED PER MM 21-55-00 -5. DEFERRAL CLEARED. 2 L 7 4 4F RT 4A25 2007042500028 20070425 00028 NM 2007 4 25 UPS07M49640 1 20070407 A 5754 ARB2850505 RIB DOUG MD11 MD11F 3023600 NM L/E SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 272UP 48571 INSPECTION TYPE:3C LEFT WING FIXED LEADING EDGE I/B SLAT TRACK FITTING BETWEEN NR 7 & 8 SLATS IS CRACKED. REMOVED AND R EPLACED SLAT TRACK FITTING (RIB) BETWEEN NR 7 & 8 SLATS IAW MD-11 SRM 51-35-01. 2 L 7 3 4F RT A22WE 2007042500053 20070425 00053 NM 2007 4 25 UPS07M49660 1 20070228 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:C CTR CARGO LT TUNNEL AREA, STA 5-118 THRU STA 5-73 FOUND CORROSION ON LONGERON L38 AS MARKED. LT LONG L38 STA 5-73 THRU 5-118 SKIN REMOVED FOR ACCESS PER SRM 51-31- 01 VOL II. REPAIR LONG SECTION & REPAIR SPLICE FAB PER D OUGLAS DWG A5A 7046 & SRM 53-10-00 V2 R38. FPI CUT OUT PER DPS4.707 FOUND NO CRACK EVIDENT. REP LONG & SPLICE REPROTEC TED PER SRM 51-21-01 V2 R38. OK TO INSTALL. REP LONG & SPLICE INSTALLED PER SRM 51-31-01 V2 R38. 2 L 7 3 4F RT A22WE 2007042500063 20070425 00063 EU 2007 4 25 SIMA200711010 1 20070417 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 535-560 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 381AE 18154 340B381 LEFT FUSELAGE DAMAGED BETWEEN STATION 535 TO 560 AND STRINGER 1518 TO 1520. CUT OUT DAMAGED SKIN, FABRICATED AND INSTAL LED A DOUBLER IAW SAAB REPAIR STATEMENT 340 SDS 012207, PARA ONE, DATED 04/16/07. 2 L 7 2 4T RT A52EU 2007042500082 20070425 00082 NM 2007 4 25 SWAA071962 1 20070420 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED RON CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007042500108 20070425 00108 WP 2007 4 25 IXXA07SMN097S 1 20070208 A 5754 SKIN DOUG DC8 DC862 3021970 WP ZONE 500 MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE SLOT VANE UPPER SKIN HAD NON STANDARD REPAIR AT S TATION XOLDI 6.225. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION NO CRACKS O R CORROSION FOUND. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLI ED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS FROM STATION XOLDI6.225 IAW FAA FORM 8110-3 NUMBER 07042 DATED 02 -07-07, SEMAN DRAWING NUMBER ED-4452 DATED 02-06-07, EO SEMAN NUMBER 2007196 DATED 02-07-07, DC8 SRM 51-1-21, DC8 SRM 5 1-1-20D, DC8 SRM 51-3-0,DC8 NDT SPM PART 06-10-01-001, FORM SEMAN 242-2, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND DC8 SRM 5 2 L 7 4 4F 4A25 2007042500115 20070425 00115 NM 2007 4 25 SWAA071895 1 20070416 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 440LV 29835 EEPLS COVER LOOSE AT ROW 3 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007042500117 20070425 00117 NM 2007 4 25 SWAA071905 1 20070418 A 5210 507945299 DOOR FRAME BOEING 737 7373H4 1384600 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR LOWER FRAME CRACKED AT LOWER FWD CORNER. REMOVED AND REPLACED L1 DOOR PER MM. 2 L 7 2 4F RT A16WE 2007042500118 20070425 00118 2007 4 25 SWAA071902 4 20070418 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR UNWANTED DEPLOY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 461WN 32465 R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007042500119 20070425 00119 2007 4 25 SWAA071896 4 20070418 A 2565 63551101 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 741SA 29277 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007042500121 20070425 00121 NM 2007 4 25 SWAA071894 1 20070416 A 3230 654482517 UPLOCK ACTUATOR BOEING 737 7373H4 1384600 NM LT MLG FAULTY A SWAA K NONE J WARNING INDICATION CL CLIMB 1 SW 29 607SW 27927 UNSAFE GEAR POSITION INDICATED UPON GEAR RETRACTION. FERRIED TO HOU FOR TROUBLESHOOTING. REMOVED AND REPLACED LT MLG U PLOCK ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2007042500122 20070425 00122 NM 2007 4 25 SWAA071925 1 20070418 A 5330 6545767 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, RBL 3. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007042500124 20070425 00124 NM 2007 4 25 SWAA071915 1 20070418 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 394, RBL 1.625. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007042500127 20070425 00127 NM 2007 4 25 SWAA071897 1 20070418 A 5753 6546434301 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED C3 CHECK, FOUND LEFT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD T/E. REMOVED AND REPLACED AFT FL AP PER MM. 2 L 7 2 4F RT A16WE 2007042500128 20070425 00128 NM 2007 4 25 SWAA071903 1 20070418 A 5755 HINGE BOEING 737 7373H4 1384600 NM NR 4 SPOILER WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW MA5084 26579 LEFT WING NR 4 SPOILER HINGE WORN. REMOVED AND REPLACED NR 4 SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007042500129 20070425 00129 NM 2007 4 25 SWAA071904 1 20070418 A 5311 6546531 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 19L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007042500131 20070425 00131 NM 2007 4 25 SWAA071922 1 20070418 A 5311 6546539 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT LEFT BS 616, WL 202. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007042500132 20070425 00132 NM 2007 4 25 SWAA071913 1 20070418 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 3 O'CLOCK POSITION. REPAIRED WEB PER S RM. 2 L 7 2 4F RT A16WE 2007042500135 20070425 00135 NM 2007 4 25 SWAA071919 1 20070418 A 5315 6546811 FLOORBEAM BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 967, LBL 26 TO RBL 43. REMOVED AND REPLACED UPPE R CHORD PER SRM. 2 L 7 2 4F RT A16WE 2007042500136 20070425 00136 NM 2007 4 25 SWAA071909 1 20070418 A 2560 6547463 FITTING BOEING 737 7373H4 1384600 NM L1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER MM. 2 L 7 2 4F RT A16WE 2007042500137 20070425 00137 NM 2007 4 25 SWAA071906 1 20070418 A 2560 6547463 FITTING BOEING 737 7373H4 1384600 NM R1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER MM. 2 L 7 2 4F RT A16WE 2007042500138 20070425 00138 NM 2007 4 25 SWAA071907 1 20070418 A 2560 6547463 FITTING BOEING 737 7373H4 1384600 NM R1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER MM. 2 L 7 2 4F RT A16WE 2007042500141 20070425 00141 NM 2007 4 25 SWAA071926 1 20070418 A 3397 65C27093 CONNECTOR BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. SECURED LOOSE CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2007042500142 20070425 00142 NM 2007 4 25 SWAA071920 1 20070418 A 5340 65C27314 STRINGER CLIP BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007042500143 20070425 00143 NM 2007 4 25 SWAA071910 1 20070418 A 5340 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007042500145 20070425 00145 NM 2007 4 25 SWAA071928 1 20070418 A 5322 69353656 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 17L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007042500146 20070425 00146 2007 4 25 SWAA071898 4 20070418 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007042500147 20070425 00147 NM 2007 4 25 SWAA071901 1 20070418 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 420WN 29825 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007042500148 20070425 00148 NM 2007 4 25 SWAA071917 1 20070418 A 3350 OL3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 406WN 27894 DURING SCHEDULED SPV CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 5 DEF. REMOVED AND REPLACED LIGHT BULB ER MM. 2 L 7 2 4F RT A16WE 2007042500149 20070425 00149 NM 2007 4 25 AALA20070660 1 20070320 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 958AN 30091 TUL - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500153 20070425 00153 NM 2007 4 25 AALA20070644 1 20070207 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 913AN 29514 TUL - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500154 20070425 00154 NM 2007 4 25 AALA20070645 1 20070207 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 913AN 29514 TUL - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500159 20070425 00159 NM 2007 4 25 AALA20070670 1 20070406 A 3397 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 765AN 32879 AFW - EMERGENCY LIGHT AT SEAT ROW 41C TO G INOPERATIVE. REPLACED EMERGENCY LIGHT SEAT HARNESS CONNECTOR AT SEAT 41C TO G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007042500160 20070425 00160 NM 2007 4 25 AALA20070638 1 20070202 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 973AN 29548 TUL - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500161 20070425 00161 NM 2007 4 25 AALA20070639 1 20070202 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 955AN 29540 TUL - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500162 20070425 00162 NM 2007 4 25 AALA20070640 1 20070202 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 955AN 29540 TUL - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500166 20070425 00166 NM 2007 4 25 USAA070292 1 20070418 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 STA 440 STR 8-9L HAS CRACK. INSTALLED DOUBLER PER TR 53-10-20E, DEFECT SIZE: 0.5 INCH. 2 L 7 2 4F RT A16WE 2007042500167 20070425 00167 EU 2007 4 25 BA07004 1 20070418 A 2913 974800 PUMP AIRBUS 330 A330323 3930335 EU HHYDRAULIC SYS FAILED A USAA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 EA 19 273AY 23978 2024 0337 FLIGHT 1071, PHL-SJU: DURING CRUISE, THE GREEN SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO. FLIGHT RETURNED TO PHL. MAI NTENANCE REPLACED THE GREEN SYSTEM HYDRAULIC PUMPS AND FILTERS. 2 L 7 2 4F RT A46NM 2007042500168 20070425 00168 EU 2007 4 25 SA07026 1 20070417 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU CABIN FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 722US 22998 1097 BDL - THE EMERGENCY LIGHT SYSTEM FAULTED WITH -EXT LOAD AFT L- MESSAGE DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE RE PLACED THE AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007042500170 20070425 00170 NM 2007 4 25 USAA070259 1 20070403 A 5320 143N55202B ANGLE BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 200UU 27809 BS 740-800, WL 208.1, RBL 64.40 HAS CORROSION. REMOVED, FABRICATED & INSTALLED CHORD IAW BOEING DWG 143N5520 & SRM 51-4 0-02, PARA 7(D) FIG 12, DEFECT SIZE: 15 X 1 INCH. 2 L 7 2 4F RT A2NM 2007042500171 20070425 00171 NM 2007 4 25 QXEA200700625 1 20070414 A 3010 4100S00503 VALVE BOMBDR DHC8 DHC8402 1390042 NM DEICE SYSTEM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 418QX 957 4143 SEA FLIGHT NR 2425: DEICE PRESSURE CAUTION LIGHT ON, DEC AND APP RAN CHECKLIST. CAUTION LIGHT WENT OUT AND CAME BACK ON . MAINTENANCE INTERROGATED CDS AND FOUND FAULT 'LOW PRESS 6A'. GVI OF DEICE BOOTS ON VERTICAL AND HORIZONTAL STAB SHOWE D NO DEFECTS. PERFORMED FUNCTIONAL TEST OF THE AIRFRAME PNEUMATIC DEICING SYSTEM PER Q400 AMM TASK 31-11-00-720-801. T HE LOWER VERTICAL STAB AND THE RIGHT OUTBOARD TAIL BOOT DID NOT INFLATE WITH DEICE PRESSURE CAUTION. REMOVED AND REPLAC ED NR 6 DDV IAW Q400 AMM TASK 30-11-16 PG 401-408. FUNCTIONAL TEST OF THE AIRFRAME DEICING SYSTEM GOOD PER Q400 AMM TAS K 30-11-00-720-801. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007042500174 20070425 00174 NM 2007 4 25 DHL2007782501 1 20070414 A 5312 PRESSURE PANEL BOEING 727 727227 1384078 NM BS 740-760 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 782DH 21998 CABIN PRESSURE WEB AT BS 740 TO 760, RT, IS CRACKED AT AFT HOLE. FABRICATED NEW PRESSURE WEB FROM 7075-T6, .040" BY 13. 5" BY 9.5", PO NR 9003110, PER B727 SRM 53-10-2 FIG 3. TREATED, PRIMED, AND INSTALLED PRESS WEB PER B727 SRM 51-10-2 AN D 51-30-2. 2 L 7 3 4F A3WE 2007042500176 20070425 00176 NM 2007 4 25 AALA20070659 1 20070319 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 923AN 29524 TUL - EMERGENCY LIGHT BATTERY PACK IN COACH CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN COAC H CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500177 20070425 00177 NM 2007 4 25 AALA20070661 1 20070320 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 958AN 30091 TUL - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500178 20070425 00178 NM 2007 4 25 SB07030 1 20070418 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 432US 24554 CLT - MAINTENANCE FOUND THE FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PA CK AT POWER SUPPLY M01132. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007042500182 20070425 00182 NM 2007 4 25 AALA20070631 1 20070124 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 AFW - EMERGENCY LIGHT BATTERY PACK AT AFT COACH SEATS M33401 FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY P ACK AT AFT COACH SEATS M33401. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007042500185 20070425 00185 NM 2007 4 25 AALA20070629 1 20070123 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 954AN 30089 TUL - EMERGENCY BATTERY PACK IN CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY BATTERY PACK IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500186 20070425 00186 NM 2007 4 25 AALA20070637 1 20070202 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 973AN 29548 TUL- EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500187 20070425 00187 NM 2007 4 25 AALA20070642 1 20070202 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 955AN 29540 TUL - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500188 20070425 00188 NM 2007 4 25 AALA20070652 1 20070223 A 3350 5283W6032 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 976AN 30099 TUL - EMERGENCY LIGHT BATTERY PACK IN COACH CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN COAC H CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500189 20070425 00189 NM 2007 4 25 AALA20070653 1 20070308 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 975AN 29549 TUL - EMERGENCY LIGHT BATTERY PACK IN COACH CABIN FOR SEAT ROWS 15 TO 21 FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIG HT BATTERY PACK IN COACH FOR SEAT ROWS 15 TO 21 CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500190 20070425 00190 NM 2007 4 25 USAA070317 1 20070423 A 5320 ATTACH ANGLE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 STR 15L WEB AT FRAME 348 HAS CRACK. INSTALLED NEW ANGLE PER SRM 51-10-2, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007042500192 20070425 00192 NM 2007 4 25 QXEA200700622 1 20070413 A 3150 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM CAUTION LIGHT UNKNOWN A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 420QX 4147 GEG FLIGHT NR 2371: CABIN HOT DUCT CAUTION LIGHT ON. DUCT TEMP IN NORMAL RANGE. AIRCRAFT RETURNED TO GATE. MAINTENANC E C/W FIM TASK 21-60-00-810-804. ECS FAULTS CLEARED AND CAUTION LIGHT EXTINGUISHED. CABIN DUCT TEMP NEVER INDICATED AB OVE NORMAL ON TEMP INDICATOR. ORIGINAL FAULT CODE 4101 ECU ANLG CH-1 NEVER REAPPEARED. AFTER OPS CHECK OF ECS TEMP CON TROL SYSTEM. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007042500193 20070425 00193 NM 2007 4 25 QXEA200700623 1 20070415 A 3150 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM CAUTION LIGHT UNKNOWN A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 425QX 4039 SEA FLIGHT NR 2378: NR 2 RUD HYD CAUTION LIGHT ON TAXI. AIRCRAFT RETURNED TO GATE. MAINTENANCE C/W DH8-400-SL-27-007A. PERFORMED C/B RESET PROCEDURES. GROUND RAN ENGINES. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVIC E. 2 H 7 2 4T RT A13NM 2007042500194 20070425 00194 NM 2007 4 25 F3LA200700081 1 20070418 A 3350 321430 BATTERY PACK AIRBUS A319 A319111 3930336 NM EMERGENCY LIGHT FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 906FR 1684 DURING C4/S1 CHECK, INSPECTION REPORTED FWD LEFT AND AFT LEFT EPSU BATTERIES FAILED CAPACITY CHECK. REPLACED EMERGENCY ESCAPE PATH LIGHT BATTERY PACKS, FWD, AFT, MID L AND MID R. OPS CHECKS NORMAL IAW AMM 33-51-38-00-002 AND 33-51-38-400- 002. 2 L 7 2 4F RT A28NM 2007042500196 20070425 00196 WP 2007 4 25 IXXA07SMN095S 1 20070208 A 5551 SEO85500094 FITTING DOUG DC8 DC862 3021970 WP ZONE 300 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LOWER FITTING ANGLE CRACKED AT STATION XFS 60.00 0. REMOVED DAMAGED FITTING ANGLE. CLEANED, TREATED AND PRIMED. INSTALLED NEW FITTING ANGLE IAW DC8 SRM 51-1-21, DC8 S RM 51-1-8B, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, AND DC8 SRM 51-3-1. 2 L 7 4 4F 4A25 2007042500200 20070425 00200 NM 2007 4 25 AALA20070654 1 20070308 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 975AN 29549 TUL - EMERGENCY LIGHT BATTERY PACK AT OVERHEAD PASSENGER ENTRY DOOR FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BA TTERY PACK AT OVERHEAD PASSENGER ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500201 20070425 00201 NM 2007 4 25 AWXA200700504 1 20070415 A 5340 6935352501 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - FOUND CRACKED STRINGER CLIP, BS 907, S3R. REPLACED STRINGER CLIP, BS 907, S3R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007042500202 20070425 00202 EU 2007 4 25 AWXA200700506 1 20070416 A 5315 D53472172203 FLOORBEAM AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 SAL - FOUND CORROSION ON CABIN FLOORBEAM, FR 66 + 7", -Y1292. REPLACED CABIN FLOORBEAM, FR 66 - FR 68, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007042500205 20070425 00205 NM 2007 4 25 AWXA200700509 1 20070410 A 5313 65596644 STRINGER SPLICE BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - FOUND CRACKED STRINGER SPLICE CHANNEL, BS 360, S4L. REPLACED STRINGER SPLICE CHANNEL, BS 360, S4L IAW B737-300 SR M 51-40-02. 2 L 7 2 4F RT A16WE 2007042500207 20070425 00207 NM 2007 4 25 AWXA200700511 1 20070409 A 5340 69414372 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - CRACKED STRINGER CLIP, BS 663, S10R. REPLACED STRINGER CLIP, BS 663, S10R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007042500209 20070425 00209 NM 2007 4 25 USAA070322 1 20070423 A 5320 SUPPORT ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 STA 320-348, LEFT SIDE FWD ENTRY, INBOARD DOOR SILL SUPPORT ANGLE HAS CORROSION. REPLACED WITH NEW PART PER SRM 51-10-0 2, 51-40-02; CORR TASK C53-107-01; LEVEL 2, DEFECT SIZE: 6 INCHES. 2 L 7 2 4F RT A16WE 2007042500210 20070425 00210 NM 2007 4 25 AALA20070671 1 20070406 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 765AN 32879 AFW - SEAT MOUNTED EMERGENCY LIGHTS IN AFT COACH INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 43C FOR SEAT M OUNTED EMERGENCY LIGHTS IN AFT COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007042500211 20070425 00211 NM 2007 4 25 USAA070323 1 20070423 A 2560 ATTACH FITTING BOEING 737 737401 1384701 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 BS 312 AT S17L FWD GIRT BAR ATTACH FITTING OF MED HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PER SRM 51-40-0 7; CORR TASK C53-107-01; LEVEL 2, DEFECT SIZE: .5 X .250 INCH. 2 L 7 2 4F RT A16WE 2007042500213 20070425 00213 NM 2007 4 25 AALA20070672 1 20070406 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 765AN 32879 AFW - EMERGENCY LIGHTS AT FIRST CLASS SEATS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK FOR FIRST CLASS SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007042500214 20070425 00214 NM 2007 4 25 AALA20070677 1 20070411 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 959AN 30828 TUL - EMERGENCY LIGHTS AT SEAT ROW 19ABC INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROW 19ABC. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500215 20070425 00215 NM 2007 4 25 AALA20070632 1 20070125 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 910AN 29512 TUL - EMERGENCY LIGHT BATTERY PACK FOR MID CABIN BETWEEN STATION NUMBERS 700 TO 750 FAILED FUNCTIONAL TEST. REPLACED EM ERGENCY LIGHT BATTERY PACK AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500216 20070425 00216 NM 2007 4 25 AALA20070634 1 20070125 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 910AN 29512 TUL - EMERGENCY LIGHT BATTERY PACK AT AFT GALLEY FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK AT AFT G ALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500217 20070425 00217 NM 2007 4 25 AALA20070648 1 20070208 A 5730 122T4701 SKIN BOEING 767 767323 1385205 NM LT WING WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 386AA 27060 AFW - LEFT WING LOWER SKIN SURFACE AT APPROXIMATELY WING STATION 602 AND JUST AFT OF STRINGER 66 UNDER FAIRING FOR OUTBO ARD FLAP HAS TWO WORN AREAS. AREA OF DISCREPANCY IS 0.7 INCHES BY 1.0 INCHES AND 7 INCH DIAMETER WITH .005 DEPTH. BLEN DED AREA UNTIL SMOOTH AND PERFORM HIGH FREQUENCY EDDY CURRENT INSPECTION FOR CRACKS. ROTO PEENED AREA AND REFINISH WITH ALODINE AND TWO COATS OF BMS 10 79 PRIMER. 2 L 7 2 4F RT A1NM 2007042500219 20070425 00219 NM 2007 4 25 AALA20070662 1 20070320 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 958AN 30091 TUL - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500220 20070425 00220 NM 2007 4 25 AALA20070663 1 20070320 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 958AN 30091 TUL - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500223 20070425 00223 NM 2007 4 25 HALA0700170 1 20070414 A 3040 6240655 CONTROL UNIT BOEING 767 767300 1385204 NM WINDOW HEAT MALFUNCTIONED A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 583HA 67285 67285 25531 ETOPS SIGNIFICANT SYSTEM, R FWD WINDOW EICAS MSG. REMOVED AND REPLACED CONTROL WINDOW HEAT UNIT PER AMM 30-41-01. OPS CK GOOD OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007042500225 20070425 00225 NM 2007 4 25 HALA0700172 1 20070415 A 2913 66180 PUMP BOEING 717 717200 1383700 NM HYD SYSTEM FAILED A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 480HA 6487 6487 55125 BTB - HYD L PUMP FAIL LT ON. REMOVED AND REPLACED LT HYD ENG, DRIVEN PUMP PER AMM 29-11-01. OPS CHECK OK, LEAK CHECK O K. SECURITY CHECK OK. 2 L 7 2 4F TR A6WE 2007042500226 20070425 00226 WP 2007 4 25 070099 1 20070414 A 3350 6011779 BATTERY PACK DOUG DC9 DC987 3022087 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 948MA 49778 DURING A ROUTINE OVERNIGHT SERVICE CHECK MAINTENANCE INSPECTION ST PETERSBURG MAINTENANCE REPORTED THAT BOTH OVERWING EM ERGENCY EXIT HATCH EXIT SIGNS WOULD NOT TEST. THE FURTHER REPORT THE REMOVAL AND REPLACEMENT OF AN EMERGENCY LIGHT POWE R SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED T O SERVICE. 2 L 7 2 4F RT A6WE 2007042500228 20070425 00228 2007 4 25 070098 4 20070414 A 3160 4055900906 SYMBOL GENERATOR DOUG DC9 DC983 3022083 WP NR 2 FAILED A WX0A O OTHER O OTHER CR CRUISE 1 WP 19 868GA 49554 FLIGHT 453 ICT/LAS - THE FLIGHT CREW REPORTED THAT THE FIRST OFFICER'S PFD AND ND FAILED IN FLIGHT, THEY POSITIONED THE EFIS SOURCE SELECTOR TO BOTH ON 1 AND CONTINUED THE FLIGHT. LAS VEGAS MAINTENANCE REPORT THE REMOVAL AND REPLACEMENT OF THE NR 2 SYMBOL GENERATOR. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 34-22-10. THE AIRPLANE HAS RETUR NED TO SERVICE. 2 L 7 2 4F RT A6WE 2007042500229 20070425 00229 NM 2007 4 25 USAA070306 1 20070423 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 531AU 24478 SKIN AT BS 380, BL 0 (E&E EXHAUST DUCT CUTOUT) HAS CRACK. FAB'D & INSTALLED INNER & OUTER DOUBLERS PER TYP REP 53-30-18 A & EA 98624, DEFECT SIZE: .75 INCH. 2 L 7 2 4F RT A16WE 2007042500233 20070425 00233 NM 2007 4 25 USAA070310 1 20070423 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 BS 492 S-24R HAS CRACK. FAB'D & INSTALLED REPAIR PARTS PER SRM 53-00-53, 51-40-02 BOEING DWG 65-20723, DEFECT SIZE: .2 50 INCH. 2 L 7 2 4F RT A16WE 2007042500237 20070425 00237 WP 2007 4 25 07FDEA01503 1 20070413 A 5270 PROXIMITY SENSOR DOUG MD10 MD1010F 3022112 WP CARGO DOOR UNKNOWN A FDEA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 25 362FE 48261 ON DEPARTURE RECEIVED LVL 2 CARGO DOOR FWD "B" ALERT, RAN QRH AND ALERT DISAPPEARED, MEL 52-40-01-05: CARGO DOOR FWD "B " ALERT INOP. VERIFY DOOR IS CLOSED AND LOCKED PRIOR TO BLOCK-OUT. INSPECTED "B" DOOR WARNING SWITCH FOR FWD LWR CARGO DOOR WARNING FOR CONDITION AND SECURITY. NOTED NO FAULTS. REMOVED AND REPLACED THE LOWER FWD CARGO DOOR WARNING "B" ( D1-92) PROXIMITY SENSOR, DOOR WARNING SYSTEM OPS NORMAL. REF MD10-10 AMM 52-70-03-2. 2 L 7 3 4F RT A22WE 2007042500241 20070425 00241 WP 2007 4 25 07FDEA01504 1 20070416 A 5330 SKIN DOUG DC10 DC1010 3022110 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 397FE 46631 DURING MD10-10 ACF MODIFICATION FOUND 3 DENTS ON EXTERNAL SKIN BETWEEN STA 1797 TO 1804 RT SIDE LONGERON 29 TO LONGERON 30, DENT 0.32" BY 2" BY 1" STA 1802 TO 1804, DENT 0.32" BY 1" BY .050" STA 1801, DENT 0.32" 1.80" BY 1" STA 1797 TO 179 9. PERFORMED REPAIR FOR SRM 53-20-00 FIG 6 VOL. I. 2 L 7 3 4F A22WE 2007042500244 20070425 00244 NM 2007 4 25 USAA070324 1 20070423 A 5347 CARGO TRACK BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 STA 727F, LBL 17.2, CARGO TIEDOWN TRACK HAS CORROSION. FABRICATED TRACK SECTION PER SRM 53-00-53 FIG 201; CORR TASK C53 -202-01; LEVEL 2. 2 L 7 2 4F RT A16WE 2007042500245 20070425 00245 NM 2007 4 25 USAA070316 1 20070423 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 STA 294.5 STR 11L HAS CRACK. INSTALLED REPAIR ANGLE PER SRM 51-40-06, 51-40-02, 51-40-05; BOEING DWG 65-14210, DEFECT S IZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007042500249 20070425 00249 NM 2007 4 25 QXEA200700520 1 20070408 A 3260 82400033057 DOWNLOCK SENSOR DHAV DHC8 DHC8202 2809007 NM MLG MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 359PH 514 PDX - ON FLIGHT 2186, DURING TAXI HAD INTERMITTENT GEAR WARNING HORN WITH ASSOCIATED RIGHT MAIN GEAR UNSAFE INDICATION. MAINTENANCE REMOVED AND REPLACED RIGHT HAND MAIN LANDING GEAR DOWNLOCK PROX SENSOR. FUNCTIONAL TEST IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007042500250 20070425 00250 NM 2007 4 25 QXEA200700521 1 20070407 A 6123 9542153653323 SWITCH DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 356PH 502 SEA - ON FLIGHT 2085, AUTO FEATHER SELECT LIGHT INDICATION FAILS TO ILLUMINATE UPON BEING DEPRESSED. MAINTENANCE REMOVE D AND REPLACED THE AUTO FEATHER SWITCH. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007042500252 20070425 00252 WP 2007 4 25 IXXA07SMN120S 1 20070223 A 5313 2753715 LONGERON DOUG DC8 DC862F 3021972 WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT, LONGERON-36 CRACKED AT STATION 1100.000. REMOVED FASTEN ERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED LONGERON SEGMENT. FABRICATED NEW SEGMENT OF LONGERON AND EXTERNAL DOU BLER. INSTALLED NEW REPAIR PARTS IAW FORM 8100-9 DATED 03/15/2007, BOEING MESSAGE NUMBER 1-296019761-5 DATED 03/15/2007 , DC8 SRM 53-2-2 FIGURE 13 TR NUMBER 53-191, DATED 10/15/2003, DC8 SRM 51-1-21, BOEING MESSAGE NUMBER 1-296019761-5 (SKE TCH JCTO4049 FIGURE 1AND 2), SEMAN DRAWING ED-4470, AND DC8 SRM 53-4-1 FIGURE 44B SHEET 1 ITEM "R", DC8 SRM 51-2-0 FIGUR E 50 SHEET 72B. 2 L 7 4 4F 4A25 2007042500254 20070425 00254 NM 2007 4 25 NWAA071345653 1 20070411 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 553NW 26500 DURING A LINE CHECK, THE EMERGENCY EXIT SIGN AT DOOR 3 LEFT FOUND INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY P OWER SUPPLY IAW AMM 33-51-07, OP CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2007042500045 20070425 00045 WP 2007 4 25 UPS07849635 1 20070324 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 REMOVE STEEL DOUBLER FROM C-2 (B-PIT) DOOR JAMB UPPER FWD CORNER AND REPAIR PER DC8 SRM 53-2-0 FIG 20 . REMOVED STEEL DOUBLER FROM B-PIT DOOR JAMB UPPER FWD CORNER IAW SRM 51-01-21A. FABRICATED AND INSTALLED CORRECT TRIP LER, DOUBLER, AND FILLER AT B-PIT UPPER FWD DOOR JAMB CORNER IAW SRM 53-2-0 FIG 20 AND SRM TR 53-186. 2 L 7 4 4F RT 4A25 2007042500046 20070425 00046 NM 2007 4 25 UPS07249643 1 20070420 A 5610 GUIDE ARM BOEING 727 72722C 138400F NM WINDOW OUT OF ADJUST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE:N/A CAPTAIN'S SLIDING WINDOW WILL NOT OPEN. ADJUSTED GUIDE PIN OF CAPTAIN'S SLIDING WINDOW WITH REF TO MM 56-12-11-5. WINDOW OPERATES AND SECURES LOCKED NORMAL. 2 L 7 3 4F A3WE 2007042500049 20070425 00049 NE 2007 4 25 UPS07549642 2 20070419 A 7200 ENGINE BOEING 757 75724APF 1384969 NM PWA 2037 PW2040 NE NR 2 BIRD STRIKE A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 01 413UP 23853 INSPECTION TYPE:N/A ENGINE PNEUMATICS PRODUCING A BURNT SMELL IN COCKPIT. WHEN TAI IS ACTIVATED SMELL GETS STRONGER. O DOR IS UNUSUAL APU PNEUMATICS DOES NOT PRODUCE THE ODOR. FOUND EVIDENCE OF BIRD STRIKE ON NR 2 ENGINE. PERFORMED BIRD STRIKE INSPECTION PER FIM 71-05-00 FIGURE 102. OK TO CONTINUE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007042500052 20070425 00052 NM 2007 4 25 UPS07M49659 1 20070228 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:C CTR CARGO, STA 1540 LONGERON L45 FOUND WITH CORROSION AS MARKED. THE A/M LONGERON L45 STA 1540 AREA O PENED UP FOR REPAIR PER SRM 51-31-0 1 V2 R38. S/BUSHING REMOVED PER EN 1148-07 FOR EXISTING REPAIR ON L45. LONGERON & SPLICE FAB PER SRM 53-10-00 V1 F2 R38. FPI CUT OUT ON FAB LONGERON & SPLICE FOUND NO CRACK EVIDENT. S/BUSHING FAB PER EN1148-07. OK TO INSTALL. REPAIRED S/BUSHING INSTALLED PER EN1148-07, FOUND SATIS. 2 L 7 3 4F RT A22WE 2007042500055 20070425 00055 EA 2007 4 25 SIMA200711001 1 20070419 A 2780 766389M CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA ZONE 600 FAILED A SIMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 21 522AE 7944 1353 10147 FLAPS AND SLATS SELECTED TO ZERO, INDICATION SHOWED ZERO WITH NO BARBER POLE, RETURNED TO DFW. REMOVED AND REPLACED NUM BER 2 SFECU IAW CRJ AMM 27-51-05. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007042500058 20070425 00058 NM 2007 4 25 UPS07M49664 1 20070212 A 5753 NRC67682 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM FLAP VANE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:C RIGHT OUTBOARD FLAP, FLAP VANE SUPPORT FITTINGS FOUND WITH CORROSION AT INTERIOR OF LIGHTENING HOLES A S MARKED. RIGHT O/B FLAP VANE REMOVED AS PER AMM 27-50-32 R.55. SEND TO SHOP FOR REPAIR. RIGHT O/B FLAP INSTALLED PER AMM 27-50-32 R 55. OPERATIONAL CHECK CARRIED OUT AS PER AMM 27-50-00 R 55. 2 L 7 3 4F RT A22WE 2007042500061 20070425 00061 NM 2007 4 25 UPS07M49668 1 20070423 A 5610 SLIDING WINDOW DOUG MD11 MD11F 3023600 NM COCKPIT DEFECTIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 252UP 48768 INSPECTION TYPE:N/A FIRST OFFICER'S SLIDING WINDOW WILL NOT CLOSE. REMOVED TRIM ON F/O'S WINDOW TO FOM. PROVIDED UPPER WINDOW FRAME SHIM PER BOEING DRAWING NO NBA 6046 & RIGGED F/O WINDOW PER AMM 56-12-01-5. WINDOW OPERATION NORMAL FOLLOWI NG TRIM INSTALLATION. 2 L 7 3 4F RT A22WE 2007042500062 20070425 00062 SO 2007 4 25 SIMA200711009 1 20070415 A 5210 14533404401 BRACKET EMB 135 EMB135KL 3260302 SO ZONE 800 CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 808AE 12717 4800 145519 MAIN ENTRANCE DOOR LOCKING HANDLE BRACKET CRACKED. STOP DRILLED, FABRICATED AND INSTALLED DOUBLER IAW EMB IC2007/145-02 59A. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042500066 20070425 00066 EU 2007 4 25 SIMA200711003 1 20070416 A 3240 50125893 BRAKE SAAB SF340 340B 7860101 EU ZONE 700 SMOKE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 263AE 3309 103 340B263 POST FLIGHT REVEALED SMOKE OBSERVED FROM NUMBER 2 WHEEEL ASSEMBLY. REMOVED AND REPLACED NUMBER 2 BRAKE ASSEMBLY AND NUM BER 1 AND 2 TIRES IAW SAAB AMM. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007042500068 20070425 00068 SO 2007 4 25 SIMA200711007 1 20070417 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EXIT SIGN BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 906AE 14500894 FOUND EXIT ROW OVERHEAD SIGN WILL NOT TEST. REPAIRED BROKEN WIRE IAW EMB AWM 20-21-00. OPERATIONAL CHECK GOOD, RETURNE D AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007042500081 20070425 00081 2007 4 25 QXEA200700626 4 20070416 A 3425 42000332501 AHRS BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 403QX 11755 4037 GEG FLIGHT NR 2350, ON CLIMB 17-18000, GOT AUTO PILOT DISCONNECT, ELEVATOR FEEL CAUTION, NR 2 DHG FAIL, NR 2 ATT FAIL, Y D FAIL AND AHARS 2 FAIL MESSAGE ON FMS. MAINTENANCE REMOVED AND REPLACED NR 2 AHRS IAW MTC 6342101. OPS CHECK GOOD. A IRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007042500084 20070425 00084 NM 2007 4 25 SWAA071958 1 20070420 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 229WN 32498 EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007042500085 20070425 00085 SO 2007 4 25 SWIA200718098 1 20070410 A 2710 PULLEY EMB 120 EMB120ER 3260203 SO AILERON CONTROL WORN A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 218SW 120287 AILERON CONTROLS BIND IN CENTERED POSITION. REPLACED OUTBOARD AILERON PULLEYS ON LEFT AND RIGHT WINGS IAW MM 27-00-00. 2 L 7 2 4T RT A31SO 2007042500091 20070425 00091 EA 2007 4 25 SWIA200718102 1 20070413 A 2760 5120011 PCU CNDAIR CL600 CL6002C10 1390015 EA SPOILERS LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 NM 07 613SK 907 907 10038 AFTER GEAR EXTENSION RECEIVED A "HYD 2 LO PRESS" WITH ASSOCIATED LEFT AND RIGHT INBOARD SPOILERONS AND LEFT AND RIGHT IN BOARD FLIGHT SPOILERS AS WELL AS RIGHT THRUST REVERSER CAUTION MESSAGES. ALSO, RECEIVED AN OUTBOARD BRAKES CAUTION MESS AGE ON ROLLOUT. HYDRAULIC RESERVOIR NR 2 QUANTITY SHOWS 5 PERCENT. REPLACED RIGHT, INBOARD, MULTI FUNCTION SPOILER PCU IAW CRJ 700 MM 27-62-01. NO LEAKS NOTED. 2 L 7 2 4F RT A21EA 2007042500092 20070425 00092 NM 2007 4 25 SWAA071966 1 20070421 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING DUCT CUTOUT BS 378.5, LBL 2.8. REPAIRED SKI N PER SWA EA. 2 L 7 2 4F RT A16WE 2007042500093 20070425 00093 WP 2007 4 25 07FDEA01510 1 20070416 A 5330 SKIN DOUG DC10 DC1010 3022110 WP ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 397FE 46631 DURING MD10-10 ACF MODIFICATION AND REPAIR ASSESMENT PROG EXITING REPAIR ON EXTERNAL SKIN STA 603 TO STA 617 RT SIDE BE TWEEN L 43 TO L 45. REMOVED OLD REPAIR (BECAUSE IS NOT COMPLIANCE WITH SRM 53-20-00 FIG 6) AND INSTALLED NEW REPAIR I AW SRM 53-20-00 FIG 6 VOL I. 2 L 7 3 4F A22WE 2007042500095 20070425 00095 NM 2007 4 25 SWAA071970 1 20070421 A 5755 654645170A SPOILER BOEING 737 7375H4 138449D NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SERVICE CHECK, FOUND LEFT WING NR 0 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED NR 0 SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007042500096 20070425 00096 NM 2007 4 25 SWAA071969 1 20070421 A 5322 6546569 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 8L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007042500098 20070425 00098 WP 2007 4 25 07FDEA01512 1 20070416 A 5753 SKIN DOUG DC10 DC1010 3022110 WP ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 397FE 46631 DURING MD10-10 ACF MODIFICATION AND REPAIR ASSESSMENT RT WING INBOARD FLAP UPPER SIDE WITH EXISTING REPAIR STA XIFH 219. 550 REPAIR CARRIED OUT IAW SRM 57-10-00 FIG 85. 2 L 7 3 4F A22WE 2007042500099 20070425 00099 NM 2007 4 25 SWAA071967 1 20070421 A 5330 6550570 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT FWD CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007042500103 20070425 00103 NM 2007 4 25 SWAA071859 1 20070414 A 3233 KSC274009V BEARING BOEING 737 7377H4 1384404 NM NLG ACTUATOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 737JW 27869 DURING SCHEDULED HC1 CHECK, FOUND NLG ACTUATOR UPPER ATTACH POINT BEARING LOOSE. REPAIRED ACTUATOR PER SWA EA. 2 L 7 2 4F RT A16WE 2007042500104 20070425 00104 EU 2007 4 25 07FDEA01531 1 20070420 A 5730 SKIN AIRBUS 310 A310324 3930206 EU WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 ELONGATED HOLES AT PYLON SUPPORT BRACKET AND BOTTOM WING SKIN, LT/RT WING. REPAIR PERFORMED BY OVERSIZING HOLES AND INS TALLING BUSHES IAW EA 6-5720-66169 AND RAS/BAE/1002502/2006. 2 L 7 2 4F RT A35EU 2007042500106 20070425 00106 NM 2007 4 25 SWAA071890 1 20070416 A 3350 1619 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 223WN 32492 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007042500110 20070425 00110 WP 2007 4 25 IXXA07SMN105S 1 20070208 A 5754 VANE DOUG DC8 DC862 3021970 WP ZONE 600 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE SLOT VANE HAS A NON STANDARD REPAIR, BETWEEN STA TION XS 515.720 AND XS 520.168. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR P ARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 07042 DATED 02-07-07, SEMA N DRAWING NUMBER ED-4457 DATED 02-02-07, EO SEMAN NUMBER 2007208 DATED 02-07-07, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, FORM SMN 242-2, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND DC8 SRM 51-3-1. 2 L 7 4 4F 4A25 2007042500111 20070425 00111 NM 2007 4 25 QXEA200700624 1 20070415 A 3150 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 402QX 4032 PDX FLIGHT NR 2196: ENGINE ADPT HEAT NR 1 CAUTION ANNC-ON DURING PUSH OUT OF THE GATE. AIRCRAFT RETURNED TO SERVICE. M AINTENANCE PERFORMED OPS TEST OF THE ENGINE AIR INTAKE ANIT-ICING IAW Q400 AMM TASK 30-21-00-710-801. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007042500114 20070425 00114 NM 2007 4 25 SWAA071899 1 20070418 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 420WN 29825 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007042500120 20070425 00120 NM 2007 4 25 SWAA071916 1 20070418 A 5310 6519603 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 373, RBL 67 TO RBL 69. REMOVED AND REPLACED WEB PER SR M. 2 L 7 2 4F RT A16WE 2007042500125 20070425 00125 NM 2007 4 25 SWAA071923 1 20070418 A 5330 6545768 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 390, RBL 3. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007042500126 20070425 00126 NM 2007 4 25 SWAA071918 1 20070418 A 5753 6546434 SKIN BOEING 737 7373L9 1384470 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND LEFT WING OUTBOARD AFT FLAP DELAMINATED UPPER INBOARD SURFACE. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007042500130 20070425 00130 NM 2007 4 25 SWAA071921 1 20070418 A 5311 6546539 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT RIGHT BS 616, WL 202. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007042500139 20070425 00139 NM 2007 4 25 SWAA071908 1 20070418 A 2560 6547463 FITTING BOEING 737 7373H4 1384600 NM L1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER MM. 2 L 7 2 4F RT A16WE 2007042500140 20070425 00140 NM 2007 4 25 SWAA071927 1 20070418 A 5311 6558280 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 360, STR 27L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007042500144 20070425 00144 NM 2007 4 25 SWAA071911 1 20070418 A 5753 65C30462 FLAP BOEING 737 7373A4 1384585 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED 22Y CHECK, FOUND LEFT WING INBOARD FORE FLAP CRACKED AT LOWER AFT END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007042500151 20070425 00151 NM 2007 4 25 AALA20070655 1 20070309 A 3397 0201875001 WIRE HARNESS BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 975AN 29549 TUL - EMERGENCY LIGHTS AT SEAT ROW 28DEF INOPERATIVE. REPINNED WIRES AT SIDEWALL AND INSTALLED IN CONNECTOR FOR EMERGEN CY LIGHTS AT SEAT ROW 28DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500152 20070425 00152 NM 2007 4 25 AALA20070656 1 20070313 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 914AN 29514 TUL - EMERGENCY LIGHT BATTERY PACK IN AFT CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN AFT CA BIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500155 20070425 00155 NM 2007 4 25 AALA20070646 1 20070207 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 913AN 29514 TUL - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500156 20070425 00156 NM 2007 4 25 AALA20070647 1 20070207 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 913AN 29514 TUL - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500157 20070425 00157 NM 2007 4 25 AALA20070668 1 20070406 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 765AN 32879 AFW - EMERGENCY LIGHT BATTERY PACK FOR LEFT NUMBER THREE DOOR FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK FOR LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007042500158 20070425 00158 NM 2007 4 25 AALA20070669 1 20070406 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 765AN 32879 AFW - EMERGENCY LIGHT BATTERY PACK FOR RIGHT NUMBER TWO DOOR FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY P ACK FOR RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007042500163 20070425 00163 NM 2007 4 25 USAA070301 1 20070418 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 STA 847-927, S2L-S2R CHAFED. INSTALLED DOUBLER/TRIPLER & WEAR STRIPS PER SRM 53-60-01, DEFECT SIZE: 23 INCHES ON LEFT SIDE; 13 INCHES ON RIGHT SIDE, .013 INCH DEEP MAX. 2 L 7 2 4F RT A16WE 2007042500165 20070425 00165 NM 2007 4 25 USAA070291 1 20070418 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 STA 400 STR 8-9L HAS CRACK. INSTALLED DOUBLER PER TR 53-10-20E, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007042500169 20070425 00169 EU 2007 4 25 SA07027 1 20070417 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU CABIN FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 722US 22998 1097 BDL - DURING THE EMERGENCY LIGHTS TEST, RECEIVED -EPSU FWD L- MESSAGE. MAINTENANCE REPLACED THE FORWARD LEFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007042500172 20070425 00172 NM 2007 4 25 SB07032 1 20070419 A 3350 20131ASMI BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 506AU 23381 BOS - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE AFT RIGHT REAR GALLEY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE AFT RIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007042500173 20070425 00173 NM 2007 4 25 AALA20070641 1 20070202 A 3350 D72702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 955AN 29540 TUL - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500175 20070425 00175 NM 2007 4 25 DHL2007782503 1 20070416 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 760 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 782DH 21998 CABIN FLOOR PANEL SUPPORT AT BS 760, BETWEEN LBL 44 AND LBL 66, IS CRACKED AT I/B ENDS. REMOVED FLOOR SUPPORT, FABRICAT ED REPAIR ANGLES FROM 7075-T6, .032" BY 6" BY 2" (2 EA.), PO NR 9004042, PER B727 SRM 51-10-3 AND 51-40-3 FIG 1. TREATE D, PRIMED, AND INSTALLED REPAIR PARTS TO FLOOR SUPPORT PER B727 SRM 51-10-2 AND 51-30-2. REINSTALLED FLOOR SUPPORT PER B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007042500180 20070425 00180 NM 2007 4 25 AALA20070666 1 20070323 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 752AN 30260 AFW - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007042500183 20070425 00183 NM 2007 4 25 AALA20070651 1 20070217 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 779AN 29955 AFW - EMERGENCY LIGHT BATTERY PACK IN CABIN AT AFT LEFT NUMBER TWO DOOR FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGH T BATTERY PACK IN CABIN AT AFT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007042500191 20070425 00191 NM 2007 4 25 USAA070318 1 20070423 A 5320 ATTACH ANGLE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 BS 348 S15L HAS CRACK. REMOVED & REPLACED PART PER SRM 51-10, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007042500197 20070425 00197 NM 2007 4 25 USAA070320 1 20070423 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 INNER CHORD ANGLE AT BOTTOM OF FRAME 616R AT S17R HAS CRACK. REMOVED & INSTALLED DOUBLER PER TR 53-62-01, DEFECT SIZE: .750 INCH. 2 L 7 2 4F RT A16WE 2007042500198 20070425 00198 NM 2007 4 25 USAA070321 1 20070423 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 STA 320-348 LEFT SIDE FWD ENTRY HAS CORROSION. INSTALLED NEW Z-ANGLE PER SRM 51-10-02; 51-40-02; CORR TASK C53-107-01; LEVEL 2, DEFECT SIZE: .5 X .5 INCH. 2 L 7 2 4F RT A16WE 2007042500199 20070425 00199 NM 2007 4 25 QXEA200700619 1 20070416 A 2997 CONTACTOR DHAV DHC8 DHC8202 2809007 NM UNKNOWN A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 374PH 528 PDX FLIGHT NR 2086 AT COMPLETION OF PUSHBACK UNFEATHERED NR 1 PROP COMPLETED AFTER START FLOW TURNING AUX PUMP ON STANDB Y HYD PUMPS ON FLAPS 3. NOTICED NR 2 AUX PUMP INOP BUBLS TEST GOOD. UNFEATHERED NR 2 AND THEN BOTH AUX PUMPS GOOD. FE ATHERED NR 2 AND NR 2 AUX PUMP INOP. FUEL TRANSFER RIGHT TO LEFT INOP AS WELL. ALSO, WITH NR 1 PTOP MAX NR 2 PROP FEAT HER NR 1 STANDBY HYDRAULIC PRESSURE INOP WITH STANDBY SWITCHES ON. MAINTENANCE INSTALLED NEW LEFT BUSS 2421-K1 CONTACTO R. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007042500203 20070425 00203 EU 2007 4 25 AWXA200700507 1 20070414 A 5210 D53112198200 FITTING AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 SAL - CORROSION ON L1 DOOR FITTING, FR 16 - FR 20, +Y1732. REPLACED L1 DOOR FITTING, FR 16 - FR 20, +Y1732 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007042500204 20070425 00204 NM 2007 4 25 AWXA200700508 1 20070408 A 5753 6546431279 SKIN BOEING 737 73733A 1384673 NM ZONE 500 DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - LEFT WING OUTBOARD FOREFLAP LOWER SURFACE DISBONDED, WBL 220 - WBL 226. REPAIRED LEFT WING OUTBOARD FOREFLAP LOW ER SURFACE, WBL 220 - WBL 226 I/A/W B737-300 SRM 51-70-10-2R4 FIGURE 203. 2 L 7 2 4F RT A16WE 2007042500208 20070425 00208 NM 2007 4 25 AWXA200700512 1 20070410 A 5340 69414372 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - FOUND CRACKED STRINGER CLIP, BS 663, S10L. REPLACED STRINGER CLIP, BS 663, S10L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007042500212 20070425 00212 NM 2007 4 25 AALA20070667 1 20070323 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 752AN 30260 AFW - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007042500218 20070425 00218 NM 2007 4 25 AALAF20070649 1 20070217 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 779AN 29955 AFW - EMERGENCY LIGHT BATTERY PACK IN CABIN AT FORWARD RIGHT NUMBER TWO DOOR FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN AT FORWARD RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007042500221 20070425 00221 NM 2007 4 25 AALA20070664 1 20070322 A 3350 1317 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 916AN 29517 TUL - EMERGENCY LIGHT AT FLIGHT DECK INOPERATIVE. RELAMPED EMERGENCY LIGHT AT FLIGHT DECK. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A16WE 2007042500222 20070425 00222 WP 2007 4 25 070100 1 20070415 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 863GA 49911 DURING A ROUTINE OVERNIGHT SERVICE CHECK MAINTENANCE INSPECTION SANFORD MAINTENANCE REPORTED THAT THE OVERHEAD EMERGENCY LIGHTS FROM ROW 31 TO THE AFT LAV DOORS WOULD NOT TEST. THE FURTHER REPORT THE REMOVAL AND INSTALLATION OF AN EMERGENC Y LIGHT POWER SUPPLY BATTERY PACK AT FUSELAGE STATION 1100R. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007042500224 20070425 00224 NM 2007 4 25 USAA070313 1 20070423 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 STUB FRAME WEB AT 294.5 S12L HAS CRACK. INSTALLED NEW FAB'D PART PER SRM 51-10-02, 51-40-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007042500227 20070425 00227 NM 2007 4 25 USAA070315 1 20070423 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 STA 294.5, S16L HAS CRACK. FAB'D NEW WEB PER BOEING DWG 65-17684; SRM 51-30-01, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007042500230 20070425 00230 EU 2007 4 25 USAA070307 1 20070423 A 5315 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 170US 1462 AROUND SCREW HOLE, FRAME 66, Y-1292 HAS CORROSION. CUT OUT DAMAGE, INSTALLED FILLER & REPAIR ANGLES PER SRM 53-41-14,; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A28NM 2007042500231 20070425 00231 EU 2007 4 25 USAA070308 1 20070423 A 5320 D5347208900400 FLOOR SUPPORT AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 176UW 1499 FLOOR SUPPORT -Y1292 AT FRAME 67 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-42-00, 51-44-11, CORR TASK JA-260-53500, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A28NM 2007042500232 20070425 00232 EU 2007 4 25 USAA070309 1 20070423 A 5320 D5347217220500 FLOOR SUPPORT AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 176UW 1499 FLOOR SUPPORT -Y1292 AT FRAME 69 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-42-00, 51-44-11; CORR TASK JA-260-53500, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A28NM 2007042500234 20070425 00234 NM 2007 4 25 USAA070311 1 20070423 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 BS 492, S21R HAS CRACK. FAB'D & INSTALLED REPAIR PARTS PER SRM 53-00-53, 51-40-02, BOEING DWG 65-20723, DEFECT SIZE: 0 .03 INCH. 2 L 7 2 4F RT A16WE 2007042500235 20070425 00235 WP 2007 4 25 IXXA07SMN116S 1 20070223 A 5340 37739062 FITTING DOUG DC8 DC862F 3021972 WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT, CRACKED ON FITTING BETWEEN STATION 798.000 AND LEFT BOT TOM LINE 24". REPLACED CRACKED FITTING N/P IAW SRM 51-1-20D, AND SRM 51-3-1. 2 L 7 4 4F 4A25 2007042500236 20070425 00236 NM 2007 4 25 USAA070312 1 20070423 A 5310 REVEAL BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 FWD SERVICE DOOR SEAL REVEAL AT FWD UPPER CORNER OF DOORWAY HAS CRACK. REMOVED AND REPLACED WITH NEW PART PER SRM 51-10 -02; DWG 65-55878; DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007042500240 20070425 00240 WP 2007 4 25 070106 1 20070421 A 3350 408822101 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 886GA 49931 DURING A ROUTINE OVERNIGHT SERVICE CHECK MAINTENANCE INSPECTION, SANFORD REPORTED THAT AN EMERGENCY LIGHT AT ROW 34 WOUL D NOT TEST. SANFORD FURTHER REPORT THE REMOVAL AND INSTALLATION OF AN EMERGENCY LIGHTS POWER SUPPLY BATTERY PACK FOR TH E AFFECTED ASSEMBLY. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007042500242 20070425 00242 WP 2007 4 25 IXXA07SMN093S 1 20070208 A 5512 SKIN DOUG DC8 DC862 3021970 WP ZONE 300 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, RIGHT HORIZONTAL STABILIZER. UPPER INBOARD LEADING EDGE OUTER SKIN CORRODED, STATIO N XFS 178.750. REMOVED EXISTING NON STANDARD REPAIR, AND REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA . PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS FROM STATION XFS 178.750 IAW FAA FORM 8110-3- NUMBER 07110 DATED 03-14-07, SEMAN DRAWING NUMBER ED-4451 DATED 02-14-07, EO SEMAN NUMBER 2007195 D ATED 03-14-07, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 55-2-0 PAGE 12, SEMAN DRAWING NUMBER 2 L 7 4 4F 4A25 2007042500243 20070425 00243 NM 2007 4 25 USAA070314 1 20070423 A 5310 DOOR FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 FWD SERVICE DOORWAY FRAME AT UPPER FWD STOP FITTING LOWER Q/B CORNER HAS CRACK. REMOVED DAMAGED FRAME & REPLACED WITH N EW PER DWG; 365-55878, SRM 51-10-02, DEFECT SIZE: .250 INCH. 2 L 7 2 4F RT A16WE 2007042500251 20070425 00251 WP 2007 4 25 IXXA07SMN115S 1 20070223 A 5522 PANEL DOUG DC8 DC862F 3021972 WP ELEVATOR CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER ELEVATOR UPPER PANEL CORRODED, BETWEEN STATION XE 65 .158 AND XE 132.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAY ING SURFACES. INSTALLED NEW SKIN. BALANCE ELEVATOR FOUND WITHIN OF TOLERANCE LIMITS, MOMENT:1521.12N-LBS IAW DC8 SRM 5 1-1-8 PAGES 17AND18, DC8 SRM 55-2-0 PAGE 12,DC8 SRM 55-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 55-4-1 FIGURE 1 SHEET 1AND 2 ITEM "E"AND"F,"DC8 SRM 51-1-9 TR NUMBER 51-142 DATED 04-05-06, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 2007042500256 20070425 00256 NM 2007 4 25 NWAA071355521 1 20070414 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 521US 23209 DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHT AT AND AISLE LIGHTS AFT OF DOOR 2 LEFT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK (M733) IAW MM 33-51-07, OPS CHECK NORMAL. 2 L 7 2 4F RT A2NM 2007042500265 20070425 00265 NM 2007 4 25 AMTA200700177 1 20070327 A 3150 WARNING SYSTEM BOEING 757 75723N 1384973 NM RROYCE RB211 RB211* 54555 NE EVAC SLIDE MALFUNCTIONED A AMTA K NONE O OTHER TX TAXI/GRND HDL 1 GL 11 520AT 27976 GIRT BAR ENGAGEMENT LIGHT EXT WITH EVACUATION SLIDE ARMING LEVER IN ARMED POS AT ENTRY DOOR 2L. INSPECTED DOOR SLIDE LI GHT. LIGHT OPS CHECK NORMAL.(K) 2 L 7 2 4F 4 F RT A2NM A12EU 2007042500267 20070425 00267 NE 2007 4 25 ASMF200704012 2 20070417 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LEFT UNKNOWN W ASMF C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 23 583MD 49659 725486 AIRCRAFT REJECTED TAKEOFF DUE TO LT ENGINE DID NOT ACCELERATE. THE PARAMETERS WERE: LT ENGINE WITH EPR 1.40 AND RT ENGIN E WITH EPR 1.86 AND T/O FLX TEMP 50. DURING MAINTENANCE CHECK, THE ACCELERATION CHAMBER AND MOISTURE TRAMP SERVICES WER E PERFORMED IAW MM 73-20-03, ALL CORRECT. DURING OVERNIGHT CHECK, BOTH ENGINES THROTTLE SYSTEMS WERE CHECKED IAW MM 78-1 1-00, ENGINES WERE TRIMMED AND ACCELERATION TEST WAS PERFORMED IAW MM 76-11-00 AND 71-00-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007042500268 20070425 00268 NM 2007 4 25 ASMF200704002 1 20070408 A 3620 1296662 SENSOR BOEING 737 737* NM GE CFM56 CFM56* 13802 NE BLEED AIR SYS FAILED W ASMF C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 23 997AM 7035 30283 AIRCRAFT REJECTED TAKEOFF AT 65 KNOTS DUE TO BLEED TRIP OFF LIGHT TURNED ON, ABNORMAL PROCEDURE QRH 2-4 WAS PERFORMED, R ETURNING TO PLATFORM. AFTER MAINTENANCE INSPECTION, REPORT WAS DEFERRED IAW MEL 36-8. DURING TRANSIT CHECK, 390 DEGREES PNEUMATIC TEMPERATURE SENSOR OF RT ENGINE WAS REPLACED IAW MM 36-12-08, TESTED CORRECT. 2 L 7 2 4F 4 F RT A16WE E2GL 2007042500272 20070425 00272 WP 2007 4 25 ASMF200704011 1 20070413 A 7920 811131 PRESSURE VALVE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE OIL SYSTEM FAILED W ASMF A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 23 754RA 12081 49641 725620 AIRCRAFT RETURNED, DUE TO HIGH OIL PRESSURE (57 PSI) AND TEMPERATURE (157 DEGREES C) INDICATIONS OF RT ENGINE WERE SHOWN . DURING MAINTENANCE CHECK, A BOROSCOPIC INSPECTION WAS PERFORMED AND CHIP DETECTOR WAS CHECKED, ALL CORRECT. AS PRECAUT IONARY ACTION OIL, FILTER AND OIL PRESSURE REGULATOR VALVE WERE REPLACED AND ADJUSTED IAW MM 79-20-03, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007042500275 20070425 00275 SO 2007 4 25 C2XA07RI014 1 20070411 A 3350 110049 CHARGER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13988 145265 DURING ROUTINE MAINTENANCE, MX FOUND LT FWD EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED NR 1 EMERGENCY BATTERY CHARGER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AC WAS APPROVED TO RETURN TO FLIGHT. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007042500277 20070425 00277 SO 2007 4 25 C2XA07IA088 1 20070419 A 3260 8005701 PROXIMITY SENSOR EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL NLG FAULTY A C2XA K NONE N FALSE WARNING CL CLIMB 1 SW 27 16112 145660 FLT 2916, DURING CLIMB THE LANDING FAILED TO RETRACT. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR PROXIMITY S ENSOR, OPERATIONALLY TESTED THE GEAR AND CLEARED THE DISCREPANCY. 2 L 7 2 4F 4 F RT TE6CH 2007042500279 20070425 00279 SO 2007 4 25 C2XA07RI012 1 20070401 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL COCKPIT ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14959 145091 FLT 2335 - CREW REPORTED BURNING SMELL WHEN ANTI-ICE SYSTEM WAS ON IN ICING. MX RAN BOTH ENGINES, WITH ANTI ICE SYSTEM O N AND COULD NOT DUPLICATE THE SMELL. AC WAS APPROVED TO RETURN TO FLIGHT. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007042500283 20070425 00283 CE 2007 4 25 DJFA2007050 1 20070414 A 3340 LIGHT RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP NLG UNSECURE E DJFA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 23 817TA 258552 TRIP NR 1167989, CREW REPORTED BURNING SMELL FROM THE NOSE AREA. MAINTENANCE DISCOVERED TAXI LAMP NOT SECURED TO THE HO USING. LAMP CAUSED RADOME TO OVERHEAT AND INDUCED BURINING ODOR INTO THE CABIN. MAINTENANCE REMOVED AND REPLACED THE R ADOME AND TAXI LIGHTS & INSTALLED NEW SEALS AROUND TAXI LAMPS. 2 L 7 2 4F 4 F RT A3EU E6WE 2007042500285 20070425 00285 WP 2007 4 25 IXXA07SMN117S 1 20070223 A 5340 FITTING DOUG DC8 DC862F 3021972 WP BS 781 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT, CRACKED ON FITTING BETWEEN STATION 781.000 RIGHT BOTTOM LINE 24". REPLACED FITTING IAW SRM 51-1-21, SRM 51-1-20D, AND SRM 51-3-1, EO NUMBER 53-DC8-2235. 2 L 7 4 4F 4A25 2007042500286 20070425 00286 WP 2007 4 25 070090 1 20070407 A 3320 D77311001 BALLAST DOUG DC9 DC983 3022083 WP CABIN LIGHTS ODOR A WX0A O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 19 869GA 53294 FLIGHT 452 LAS/ICT, THE FLIGHT CREW REPORTED THAT A FLIGHT ATTENDANT REPORTED A STRONG ELECTRICAL SMELL IN FLIGHT BETWEE N ROW 10 AND 11 (LEFT). PASSENGER SERVICE PANEL AND OVERHEAD STOWAGE BIN IMMEDIATELY ABOVE FELT WARM. PHASE OF FLIGHT ASSUMED TO BE CRUISE ALTHOUGH NOT SPECIFIED BY FLIGHT CREW. THE FLIGHT CREW ALSO DOES NOT SPECIFY ANY PRECAUTIONARY ACT IONS AS A RESULT OF THE REPORTED ODOR. THE AIRPLANE LANDED WITHOUT FURTHER REPORTED INCIDENT. WICHITA CONTRACT MAINTE NANCE REPORT LOCATING THE SOURCE OF THE ODOR, PULLING CIRCUIT BREAKER SB7 AND DEFERRING THE LEFT LOWER SIDEWALL LIGHTS P ER MEL 33-02 UNDER THE GUIDANCE OF MAINTENANCE CONTROL. THE AIRPLANE RETURNED TO LAS WHERE MAINTENANCE REPORT THE REMOV 2 L 7 2 4F RT A6WE 2007042500287 20070425 00287 WP 2007 4 25 IXXA07SMN119S 1 20070223 A 5340 37739061 FITTING DOUG DC8 DC862F 3021972 WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND IN MAIN CARGO COMPARTMENT A CRACKED ON FITTING AT STATION 781.000 LEFT BOTTOM LINE 24". REPLACED CRACKED FITTING IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D AND DC8 SRM 51-3-1. 2 L 7 4 4F 4A25 2007042500288 20070425 00288 SO 2007 4 25 SWIA200718073 1 20070326 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DAMAGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 297SW 120327 LEFT OVERWING EMERGENCY INTERIOR "EXIT" LIGHT FAILS TO COME ON. REPAIRED WIRE NR 2 ON BACK OF SIGN. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2007042500291 20070425 00291 EA 2007 4 25 SWIA200718076 1 20070329 A 2497 WIRE CNDAIR CL600 CL6002B19 1900309 EA PFD BURNED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 410SW 7066 RECEIVED MULTIPLE CAUTION MESSAGES. THE NR 2 MFD, PFD AND THE RTU WENT DARK. REPLACED BURNED WIRES AND TERMINALS FROM CBP2 TO JB1 IAW WM 20-12-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2007042500292 20070425 00292 EA 2007 4 25 SWIA200718077 1 20070327 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 919SW 7657 CABIN EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2007042500293 20070425 00293 SO 2007 4 25 SWIA200718078 1 20070331 A 3350 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 289YV 120289 EMERGENCY LIGHT ABOVE MAIN CABIN DOOR DOES NOT ILLUMINATE. RELAMPED EMERGENCY LIGHT BULB ABOVE MAIN CABIN DOOR. OPERAT IONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2007042500294 20070425 00294 SO 2007 4 25 SWIA200718079 1 20070403 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DISCONNECTED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 215SW 120281 EXIT SIGN LOCATED IN DOOR OF OVERHEAD BIN AT ROW 9 IS NOT WORKING. REPAIRED WIRING. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2007042500299 20070425 00299 EA 2007 4 25 SWIA200718084 1 20070401 A 2150 GG670950093 ACM CNDAIR CL600 CL6002C10 1390015 EA RIGHT SMOKE A SWIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 728SK 10192 THE FLIGHT ATTENDANT ADVISED THERE IS SMOKE IN THE CABIN. RETURNED TO GATE. REPLACED RIGHT AIR CYCLE MACHINE PER AMM 2 1-51-08, S/N OFF 00853. 2 L 7 2 4F RT A21EA 2007042500300 20070425 00300 WP 2007 4 25 IXXA07SMN094S 1 20070208 A 5512 SKIN DOUG DC8 DC862 3021970 WP ZONE 300 MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER.- LEADING EDGE OUTER SKIN NON STANDARD REPAIR AND C ORROSION AT STATION XFS 178.750. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. REMOVED CORROSION. FOUND OUT OF LIM ITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. FABRICATED NEW SKINS AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PAR TS FROM STATION XFS 178.750. IAW FAA FORM 8110-3, NUMBER 07110 DATED 03-14-07,SEMAN DRAWING NUMBER ED-4451, DATED 02-14- 07,EO SEMAN NUMBER 2007195 DATED 03-14-07, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 55-2-0 PAGE 12, DC8 NDT SPM PART 06-10-0 2 L 7 4 4F 4A25 2007042500301 20070425 00301 WP 2007 4 25 070087 1 20070405 A 2410 CSD DOUG DC9 DC983 3022083 WP RIGHT OVERSERVICED A WX0A H DEACTIVATE SYST/CIRCUITS W M H INADEQUATE Q C OVER TEMP ELECT. POWER LOSS-50 PC CR CRUISE 1 WP 19 865GA 49998 FLIGHT 478 LAS/FAR, THE FLIGHT CREW REPORTED THAT THE RIGHT CSD OIL TEMPERATURE INDICATION WAS READING HIGH AND DISCONNE CTED THE RIGHT CSD. THE FLIGHT CREW DID NOT SPECIFY. FAR CONTRACT MAINTENANCE DEFERRED THE CSD/GENERATOR UNDER THE DIRE CTION OF MAINTENANCE CONTROL PER MEL 24-01. THE AIRPLANE RETURNED TO LAS WHERE MAINTENANCE REPORT THAT THE RIGHT CSD WA S FOUND OVER SERVICED. LAS VEGAS MAINTENANCE FURTHER REPORT THAT THE CSD WAS CORRECTLY SERVICED PER AMM 12-12-01. A SA TISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE MEL REMOVED. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007042500303 20070425 00303 2007 4 25 07FDEA01416 4 20070410 A 2565 LIGHT DOUG DC10 DC1010 3022110 WP L1 DOOR RAFT INOPERATIVE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 L1 DOOR RAFT BOTTLE PRESS TO TEST LIGHT INOP. REMOVED L1 DOOR LWR SLIDE RAFT COVER, REPLACED BATTERIES, L1 DOOR LOW PRE SS BOTTLE LIGHT PRESS TO TEST GOOD. REINSTALLED L1 DOOR LWR SLIDE RAFT COVER IAW FX DC10 MM 25-61-01-2 TIMCO MECH 9782 7,7389. REMOVED L1 DOOR LOWER SLIDE-RAFT COVER. REPLACED BATTERIES, L1 DOOR LOW PRESSURE BOTTLE LIGHT PRESS TO TEST G OOD. REINSTALLED L1 DOOR LOWER SLIDE-RAFT COVER IAW DC10 MM 25-61-01-2. 2 L 7 3 4F A22WE 2007042500305 20070425 00305 EU 2007 4 25 07FDEA01418 1 20070411 A 5315 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 814FD 534 HEAVY CORROSION ON THE TOP CAP BEAM AT C24 LT. TOP CAP BEAM REPAIR PERFORMED IAW SRM 53-10-15 / FIG 207 AND SRM 51-72-1 0. 2 L 7 2 4F RT A35EU 2007042500312 20070425 00312 EU 2007 4 25 07FDEA01426 1 20070411 A 5322 A57112116201 SHEAR TIE AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 814FD 534 CRACK FINDINGS DURING ACCOMPLISHMENT OF EO 6-5310-7-5020, SB A310-53-2124, RHS, C43 RT HOLE H2 CRACK LENGTH 7MM; C45 HOL E H22 CRACK LENGTH 7MM; C46 HOLE H25 CRACK LENGTH 8MM; C46 HOLE 27 CRACK LENGTH 6MM REPAIR PERFORMED BY FRAME FOOT REPLA CEMENT ON C43, C46 BY OVERSIZING HOLE 22, C45 AND BUSHING INSTALLATION IN DOUBLER AND FRAME ON C46, HOLE H25 AND H27 IAW EA 6-5315-103304 AND RAS 045755/022/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007042500313 20070425 00313 WP 2007 4 25 IXXA07SMN109S 1 20070223 A 5340 37544730501 FITTING DOUG DC8 DC862F 3021972 WP BS 440-460 BROKEN B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD BELLY PIT FITTING BROKEN, BETWEEN STATION 440.000 AND STATION 460.000, L-31L. REMOVED DAMAGED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-20D AND DC8 SRM 51-3-1. 2 L 7 4 4F 4A25 2007042500317 20070425 00317 CE 2007 4 25 DXTA200702133 1 20070423 A 3242 BRAKE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LEFT FAULTY E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 639QS 5605139 LT BRAKE EXTREMELY SPONGY ON TAXI IN. [4-27-07] BLED BRAKE SYSTEM IAW CESSNA 560 XL M/M CHAPTER 32-42-00. OPS CHK SATISF ACTORY. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007042500318 20070425 00318 CE 2007 4 25 DXTA200702135 1 20070423 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE COPILOT WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 390QS 5600490 COPILOTS BRAKES BEING WEAK, SOFT OR SPONGY. [SUP 04-27-07] TAXIED ACFT AND FOUND EXCESSIVE TRAVEL ON COPILOT'S LEFT PE DAL. BRAKE SYSTEM BLED, AIR BUBBLES SEEN WHEN LEFT BRAKE BLED. TAXIED ACFT AND BRAKES CHECK GOOD. COPILOT PEDAL REQUIRE EQUAL FORCE FOR STOPPING. OPS & LEAK CHECK GOOD ON BRAKES. 2 L 7 2 4F 4 F RT A22CE E25EA 2007042500320 20070425 00320 CE 2007 4 25 DXTA200702112 1 20070416 A 3246 WHEEL RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP NLG OUT OF ROUND E DXTA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 07 882QS 258482 AFTER GEAR RETRACTION THERE IS A VERY SIGNIFICANT VIBRATION THAT LASTS FOR ABOUT 2 MINUTES, COMING FROM THE NOSE GEAR. T/S WHEEL ASSEMBLY BY REMOVING & BALANCING, FOUND TIMES TO BE OUT OF ROUND FACILITATING REPLACEMENT, RECEIVED OVH WHEEL ASSEMBLIES FROM NETJETS, CHECKED BALANCE OF OVH WHEEL ASSY CHECK GOOD. INSTALLED ASSEM ON NOSE STRUT, TIRES INFLATED T O 100 PSI IAW 800XP CMM 32-44-49 / AMM 32-40-00 / AMM 12-00-00. 2 L 7 2 4F 4 F RT A3EU E6WE 2007042500321 20070425 00321 CE 2007 4 25 DXTA200702107 1 20070415 A 2161 CONTROLLER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TEMP MALFUNCTIONED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 907QS 7500201 CABIN PAC HAS BURNED ODOR COMING INTO CABIN. NO DIVERTION. REMOVED AND REPLACED INOP TEMP CONTROLLER OPS CHECK GOOD IA W CE750 MM 21-61-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007042500323 20070425 00323 NM 2007 4 25 DXTA200702108 1 20070415 A 3620 WARNING SYSTEM GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE COCKPIT UNKNOWN E DXTA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CR CRUISE 1 GL 07 708QS 069 LT ENG BLEED AIR LEAK, RED WARNING MESSAGES ILLUMINATED IN FLT-QUICK REF HANDBOOK PROCEDURES FOLLOWED IAW EH-3 BLEED AIR LEAK CHECKLIST. LT BLEED AIR LEAK REMAINED ON SO LT ENGINE SHUTDOWN IAW CHECKLIST. REMOVED DUCT COMING OFF PRSOU VALVE, REPLACED O-RINGS REMOVED V BOND GASTON LINE COMING OFF ACM, INSTALLED NEW V BAND GASKET ON LINE COMING OFF ACM P/N 2434 6-200A LEAK AND OPS CHECK GOOD REFERENCE G200 M/M 21-11-05. REMOVED CLAMP FOR RIGHT BLEED FIRE LOOP. INSTALLED NEW CLAMP P/N AN742-7 REFERENCE G200 M/M 26-00-00. REMOVED LEFT BLEED AIR CONTROLLER P/N 35009-20 S/N 02025 AND INSTALLED IN APU POSITION. REMOVED APU BLEED AIR CONTROLLER P/N 35009-20 S/N D1870 AND INSTALLED IN THE LT POSITION. 2 L 7 2 4F 4 F RT A53NM E35NE 2007042500325 20070425 00325 CE 2007 4 25 DXTA200702113 1 20070416 A 3260 WARNING LIGHT CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE COCKPIT ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 615QS 5605360 AFTER TAKEOFF RED GEAR UNLOCK LIGHT REMAINED ON. FLEW FOR APPROX 1 HOUR TO GET BELOW MAX LANDING WEIGHT AND IN THAT TIM E THE HYDRAULIC PRESSURE ANNUNCIATOR CAME ON ONE TIME FOR APPROX 1 SECOND. JACKED AIRCRAFT, INSPECTED AND CLEANED UPLO CK SWITCHES IN ALL THREE GEARS AND NO VISUAL DEFECTS WERE NOTED. PERFORMED SEVERAL OPERATIONAL CHECK OF LANDING GEAR FOR PROPER OPERATION AND ALSO NO DEFECTS WERE NOTED. COULDN'T DUPLICATE DISCREPENCY. ALL WORK WAS PERFORMED IAW CE-560XL MM CH. 32-01-00 2 L 7 2 4F 4 F RT A22CE E00059EN 2007042500326 20070425 00326 CE 2007 4 25 DXTA200702114 1 20070417 A 3260 WARNING LIGHT CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE COCKPIT ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 615QS 5605360 AFTER TAKEOFF , THE RED GEAR UNLOCK LIGHT REMAINED ILLUMINATED. JACKED AIRCRAFT, INSPECTED AND CLEANED UPLOCK SWITCHES IN ALL THREE GEARS AND NO VISUAL DEFECTS WERE NOTED. PERFORMED SEVERAL OPERATIONAL CHECK OF LANDING GEAR FOR PROPER OPER ATION AND ALSO NO DEFECTS WERE NOTED. COULDN'T DUPLICATE DISCREPENCY. ALL WORK WAS PERFORMED IAW CE-560XL MM CH. 32-01-0 0 2 L 7 2 4F 4 F RT A22CE E00059EN 2007042500327 20070425 00327 CE 2007 4 25 DXTA200702116 1 20070418 A 3260 WARNING LIGHT CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE COCKPIT ILLUMINATED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 663QS 5605263 AFTER TAKEOFF GOT GEAR UNLOCK LIGHT / HYDRAULIC PRESSURE STEADY LIGHT AFTER GEAR RETRACTION. TROUBLESHOT TO THE NOSE GE AR UPLOCK SWITCH OUT OF RIG. MADE UPLOCK SWITCH ADJUSTMENT. OPS CHECK GOOD. IAW CE560 XL MM CH 32-30-05. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007042500328 20070425 00328 NM 2007 4 25 DXTA200702117 1 20070418 A 2740 WARNING LIGHT AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE COCKPIT ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 07 251QS 202 PITCH FELL CAUTION LIGHT ILLUMINATED DURING TAKEOFF AND STAYED ILLUMINATED FOR APPROXIMATELY 3 MINUTES. REPLACED PITCH VARIABLE BELLCRANK WITH A REPAIRED UNIT IN ACCORDANCE WITH F2000 MM 27-318. OPERATIONAL CHECKS GOOD. 2 K 7 2 4F 4 F RT A50NM E44NE 2007042500329 20070425 00329 CE 2007 4 25 DXTA200702118 1 20070418 A 2720 LIMITER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RUDDER MALFUNCTIONED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 956QS 7500156 (RUDDER LIMIT FAIL A) AMBER CAS MESSAGE IN CRUISE WITH AUTOPILOT ON. FAILED AT 21 PERCENT. REPLACED A & B SYSTEM RUDDE R LIMITERS IAW CESSNA 750 MM 27-23-00. OPERATIONAL CHECKS GOOD IAW CESSNA 750 MM 27-20-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007042500331 20070425 00331 NM 2007 4 25 DXTA200702125 1 20070421 A 3260 WARNING SYSTEM AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE COCKPIT ACTIVATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 259QS 159 AFTER T/O (3) RED LIGHTS NO GREEN ON GEAR, RED HANDLE FLASHING. PUT GEAR DOWN GOT (3) GREEN LIGHTS, NO RED LIGHTS NO FLA SHING HANDLE. [4-27-07] TROUBLESHOT DISCREPANCY TO FAULTY NLG UPLOCK BOX PER CHECK IAW FALCON 2000 MM 32-320. REMOVED AND REPLACED NLG UPLOCK BOX WITH REPAIRED UNIT AND PERFORMED NOSE GEAR UPLOCK CHECK IAW MM 32-214. NO FURTHER DEFECTS NO TED. 2 K 7 2 4F 4 F RT A50NM E44NE 2007042500332 20070425 00332 CE 2007 4 25 DXTA200702127 1 20070421 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MALFUNCTIONED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 383QS 5600483 DURING LANDING ROLL F.O. (COPILOT SIDE) STATED (NO BRAKES), BRAKE PEDALS FELT VERY SPONGY. NORMAL BRAKING PILOT SIDE. NO LEAKS OBSERVED ON POSTFLIGHT. [4-27-07] BLED THE ANTI-SKID BRAKE SYSTEM IAW THE BLEED PROCEDURE IN CE560 MM CH 32-4 2-00. NO FURTHER DEFECTS NOTED. 2 L 7 2 4F 4 F RT A22CE E25EA 2007042500335 20070425 00335 CE 2007 4 25 DXTA200702131 1 20070422 A 3246 BALANCE WEIGHT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG WHEEL MISSING E DXTA C ABORTED TAKEOFF W E INADEQUATE Q C VIBRATION/BUFFET TO TAKEOFF 1 GL 07 966QS 7500166 AT APPROX 85 KTS VIBRATION DEVELOPED ON NOSE GEAR, YD OFF AND FGC FAIL A AND B ILLUMINATED. T/O ABORTED SHIMMY FELT IN N OSE GEAR WHILE DECELERATING THRU 20 KTS GROUND SPEED. [4-27-07] FOUND NO BALANCE WEIGHTS ON NOSE WHEEL ASSEMBLIES. R EMOVED LT & RT ASSEMBLIES. INSTALLED CUSTOMER SUPPLIED OVERHAULED ASSEMBLIES. REPACKED BEARINGS INSPECTED NOSE GEAR & OPS CK STEERING. INSPECTION GOOD. ALL IAW CE750 MM 32-41-01 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007042500338 20070425 00338 CE 2007 4 25 DXTA200702136 1 20070424 A 3260 WARNING LIGHT CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE COCKPIT ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 392QS 5600429 AFTER DEPARTURE, WHEN THE LANDING GEAR HANDLE WAS MOVED TO THE UP POSITION, THE GEAR UNLOCK AND THE HYD PRESS ON LIGHTS REMAINED ILLUMINATED. THE HANDLE WAS RETURNED TO DOWN, (3) GREEN ILLUMINATED, ALL OTHER INDICATIONS WERE NORMAL [SUP 4 -27-07] INSPECTED LANDING GEAR AND PERFORMED SEVERAL LANDING GEAR FUNCTIONAL TESTS I/A/W CE560 MM 32-01-00 WITH NO DEFE CTS NOTED. 2 L 7 2 4F 4 F RT A22CE E25EA 2007042500339 20070425 00339 NM 2007 4 25 DXTA200702137 1 20070424 A 2120 UNKNOWN GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE COCKPIT ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 07 701QS 141 ACRID ELECTRICAL BURNING SMELL EMINATING FROM BEHIND LT PILOT SEAT IN COCKPIT. CHECKED ALL CB'S, NOTHING FOUND (POPPED). [4-27-07] PERFORMED ENG RUN AND APCS RUNS FOR COCKPIT SMELLS, RUNS SATISFACTORY. ACCESSED L/R RELAY PANEL FOUND SATIS FACTORY. ACCESSED FWD EQUIPMENT CLOSET CB CHR105& CHR203 POPPED. RESEAT OPS CK 115AC OUTLET GOOD. .RE-RACK AIRSHOW COMPU TER. OPS CK GOOD. ACCESSED L/H PILOT WINDSHIELD HEAT T/B. AT OVERHEAD FOUND SATISFACTORY. OPS CHECK DOOR MOTOR GOOD. COU LD NOT DUPLICATE BURNING ODOR FOUND AIRCRAFT SATISFACTORY FOR FLIGHT WORK DONE IAW G2000 M/M CH 5-00-00 AND CH 24-00-00. 2 L 7 2 4F 4 F RT A53NM E35NE 2007042500341 20070425 00341 CE 2007 4 25 GLBA20060940 1 20070420 A 2910 1013880167 HYDRAULIC LINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT MLG DEFECTIVE A GLBA O OTHER O OTHER DE DESCENT 1 NM 03 247GL UE247 FLIGHT 5128, ENROUTE, PILOTS REPORTED THAT WHILE INFLIGHT MAIN GEAR EXTENDED AND THE LANDING GEAR RELAY CIRCUIT BREAKER POPPED. CREW MANUALLY EXTENDED GEAR TO ACHIEVE A (3) GREEN CONFIGURATION. MAINTENANCE REMOVED AND REPLACED A FLEXIBLE H YDRAULIC LINE IN THE RT GEAR AREA AND PERFORMED AN OPERATIONAL CHECK IAW MM 32-30-10. OPERATIONAL AND LEAK CHECK GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2007042500342 20070425 00342 2007 4 25 GUUA04140701 4 20070414 A 3160 6229682002 DPU BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE COCKPIT SHORTED A GUUA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 29 46AR UE27 FLIGHT: 6007, DURING APPROACH COPILOTS EADI WENT BLANK THEN STARTED TO SMOKE. REPLACED COPILOTS DPU OPERATIONAL CHECK N ORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007042500344 20070425 00344 CE 2007 4 25 GUUA04200701 1 20070420 A 5524 1016200131BW HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 16540 UE172 AT SCHEDULED INSPECTION DISCOVERED LT ELEVATOR CENTER HINGE BRACKET HAS EXFOLIATION. REPLACED LT ELEVATOR CENTER HINGE BRACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 2007042500345 20070425 00345 CE 2007 4 25 GUUA04130701 1 20070413 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE COCKPIT FUMES A GUUA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 29 81556 UE239 FLIGHT: 9214, DURING APPROACH ELECTRICAL FUMES IN COCKPIT. OPERATIONAL CHECK ALL ELECTRICAL AND ENVIRONMENTAL SYSTEMS N O EVIDENCE OF ELECTRICAL FUMES NOTED. 2 L 7 2 4T 4 T RT A24CE E26NE 2007042500346 20070425 00346 2007 4 25 070091 4 20070408 A 3418 9650449002 COMPUTER DOUG DC9 DC983 3022083 WP STALL WARNING MALFUNCTIONED A WX0A O OTHER J WARNING INDICATION AP APPROACH 1 WP 19 865GA 49998 FLIGHT 453 ICT/LAS - THE FLIGHT CREW REPORTED THAT "AUTOSLAT FAIL" ANNUNCIATOR ILLUMINATED DURING APPROACH TO LAS. WHIL E THE LOGBOOK ENTRY SPECIFIES THAT A QRH PROCEDURE WAS ACCOMPLISHED IT DOES NOT SPECIFY WHETHER A SINGLE STALL SYSTEM WA S IDENTIFIED OR BOTH. LAS VEGAS MAINTENANCE REPORT THE REMOVAL AND REPLACEMENT OF THE NR 1 STALL WARNING COMPUTER. A SA TISFACTORY OPERATIONAL CHECK OF THE STALL WARNING SYSTEM PER AMM 34-19-02 AND OF THE AUTOSLAT SYSTEM PER AMM27-81-00 WAS ACCOMPLISHED. THE AIRPLANE HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007042500347 20070425 00347 EU 2007 4 25 07FDEA01428 1 20070411 A 5730 SKIN AIRBUS 310 A310324 3930206 EU RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 814FD 534 CRACK FINDING ON PYLON REINFORCEMENT PLATE, RIB 8-9, RT WING (HOLE 1, CRACK LENGTH 14MM; HOLE 4 CRACK LENGTH 20MM). R EPAIR PERFORMED BY REAM UP HOLES IAW EA 6-5720-101271 AND RAS/BAE/1003147/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007042500349 20070425 00349 EU 2007 4 25 07FDEA01430 1 20070411 A 5730 SKIN AIRBUS 310 A310324 3930206 EU RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 814FD 534 CORROSION FINDINGS ON BOTTOM SKIN PANEL NR 1 AND NR 2, RT WING, RIB 17-27. REPAIR PERFORMED BY BLEND OUT AND OVERSIZING FASTENER HOLE RIB 28A-29 IAW EA 6-5720-103284 AND RAS/BAE/1003245/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007042500351 20070425 00351 EU 2007 4 25 07FDEA01436 1 20070411 A 5310 DOOR FRAME AIRBUS 310 A310324 3930206 EU FUSELAGE WORN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 801FD 539 FUSELAGE FRAME 20 STRG 37 FWD CARGO COMP´T DOOR FWD FRAME FOUND WORN REPAIRED PER FEDEX EA NR 6-5330-106703. REPAIR EVA LUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR". 2 L 7 2 4F RT A35EU 2007042500353 20070425 00353 2007 4 25 07FDEA01345 4 20070404 A 2565 69599211 BRACKET BOEING 727 727225 1384077 NM ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 MAIN ENTRY DOOR EMERG ESCAPE SLIDE, BACK PAN LWR LATCH HINGED RETAINER, MOUNT BLOCK HAS EXFOLIATION CORROSION. INSTALLE D NEW BRACKET REF SRM 51-30-2 PG 2. 2 L 7 3 4F A3WE 2007042500354 20070425 00354 NM 2007 4 25 07FDEA01346 1 20070404 A 5210 65299946 ARM BOEING 727 727233 138408A NM ZONE 800 FAILED A FDEA O OTHER O OTHER LD LANDING 1 SO 25 220FE NA 20934 FORWARD ENTRY DOOR OPENED UPON TOUCHDOWN. AFTER FURTHER INSP FOUND THE UPPER GUIDE ARM WORN CAUSING THE DOOR OPEN LOCK NOT TO WORK AND DOOR HARD TO CLOSED. REMOVED AND REPLACED THE UPPER GUIDE ARM IAW 727 M/M 52-11-001-5. OPS CHECK GOOD OF THE DOOR OPERATION A/C OK FOR CONT SERVICE. 2 L 7 3 4F RT A3WE 2007042500355 20070425 00355 NM 2007 4 25 07FDEA01347 1 20070404 A 5315 BAC1518391 FLOORBEAM BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 MAIN DECK FLOORBEAM UPPER FLANGE IS CORRODED AT BS 1110, RBL 22, WL 208 CORROSION DAMAGE REPAIRED REFERENCE EA NR 7-5310 -106997. 2 L 7 3 4F A3WE 2007042500356 20070425 00356 EU 2007 4 25 07FDEA01348 1 20070403 A 2133 OUTFLOW VALVE AIRBUS 310 A310222 3930315 EU CABIN PRESS SYS MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 449FE 217 NR 2 AUTO PRESSURIZATION SYSTEM FWD AND AFT VALVES WOULD NOT CLOSE. NR 1 SYSTEM COULD NOT CONTROL AIRCRAFT PRESSURE. ATTEMPTED TO CONTROL PRESSURIZATION MANUALLY. STILL COULD NOT CONTROL PRESSURIZATION WITH THE NR 2 FWD AND AFT VALVES IN THE OPEN POSITION ITEM CLOSED WITH OPS CK OK. REMOVED AND REPLACED FWD AND AFT OUTFLOW VALVES AND SYS 2 CONTROLLER, PRESSURIZED A/C AND CHECKED OPERATION. 2 L 7 2 4F RT A35EU 2007042500358 20070425 00358 EA 2007 4 25 SWIA200718086 1 20070401 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 406SW 7030 CABIN FILLED WITH SMOKE AFTER INITIAL POWER-UP. PERFORMED OPERATIONAL CHECK OF LEFT AND RIGHT PACKS. UNABLE TO DUPLICA TE. 2 L 7 2 4F RT A21EA 2007042500359 20070425 00359 EA 2007 4 25 SWIA200718087 1 20070401 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 926SW 7687 CAPTAINS SIDE WINDOW CRACKED INFLIGHT. REPLACED CAPTAIN'S SIDE WINDOW IAW AMM 56-12-01. 2 L 7 2 4F RT A21EA 2007042500361 20070425 00361 2007 4 25 SWIA200718089 4 20070331 A 2210 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO AUTO PILOT SYS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 562SW 13554 13554 120336 WITH AUTOPILOT ENGAGED, AIRCRAFT PITCHED NOSE UP THEN NOSE DOWN. REPLACED NR 2 AUTOPILOT COMPUTER. 2 L 7 2 4T RT A31SO 2007042600001 20070426 00001 NM 2007 4 26 DU4R2007098 1 20070408 A 5720 106003183 PLATE BOEING 757 757232 1384965 NM RT WING CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND RT WING TANK PLATE 641JB CORRODED. REPAIRED BY REMOVING AND REPLACING WITH P/N 10-60031-83 IAW DELTA JOB CARD OPN 3612. 2 L 7 2 4F RT A2NM 2007042600005 20070426 00005 SO 2007 4 26 C2XA07RI015 1 20070409 A 3231 22250100003 SOLENOID VALVE EMB 145 EMB145XR 3260214 SO NLG INOPERATIVE A C2XA K NONE E VIBRATION/BUFFET CR CRUISE 1 SW 27 12136 11220 11220 145719 FLIGHT 2513 - EWR - CREW REPORTED VIBRATION AND EXCESSIVE NOISE IN FLIGHT AFTER GEAR RETRACTION. EWR MX FOUND NOSE GEAR DOORS NOT TO CLOSE. MX REMOVED AND REPLACED GEAR DOOR SOLENOID VALVE. MX ALSO REMOVED AND REPLACED LANDING GEAR CONTR OL LEVER. MX PERFORMED OPERATIONAL CHECK OF LANDING GEAR SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO FLIGHT. 2 L 7 2 4F RT 2007042600006 20070426 00006 NM 2007 4 26 NWAA071585643 1 20070423 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 543US 26490 DURING OVERNIGHT LINE CHECK, FOUND DOOR 2 RIGHT EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED DOOR 2 RIGHT POWE R SUPPLY, REF FIM NR 33-51-00, FIG NR 103. OPS CHECK NORMAL. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2007042600007 20070426 00007 SO 2007 4 26 C2XA07SH021 1 20070415 A 5312 14526850401 FIREWALL EMB 145 EMB145LR 3260212 SO APU BAY CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13990 145277 SHV - DURING C-CHECK MAINTENANCE APU FIREWALL LOWER SECTION HAS RIVET INDENTATION. MAINTENANCE REPAIRED APU FIREWALL AT FRAME 81 LOWER SECTION IAW EC5310-01359. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007042600008 20070426 00008 SO 2007 4 26 C2XA07SH019 1 20070414 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13990 145277 SHV - DURING C-CHECK MAINTENANCE FOUND CENTER OMEGA BEAM WITH CORROSION AT FRAME 20 AND FRAME 23. MAINTENANCE REPAIRED CENTER OMEGA BEAM AT FRAME 20 TO 23 IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007042600009 20070426 00009 SO 2007 4 26 C2XA07SH022 1 20070415 A 5320 14524796001 FITTING EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13990 145277 SHV - DURING C-CHECK MAINTENANCE FOUND CORROSION ON SHEAR CLIPS AT FRAMES 65 & 68. MAINTENANCE REPAIRED SHEAR CLIPS AT FRAMES 65 & 68 IAW EC 5330-01458. AIRCRAFT APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007042600012 20070426 00012 SO 2007 4 26 C2XA07IA093 1 20070420 A 3397 CONNECTOR EMB 145 EMB145EP 3260221 SO CABIN LOOSE A C2XA K NONE O OTHER UK UNKNOWN 1 SW 27 14943 145040 IAH - FLIGHT 2277, THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN ABOVE THE F/A SEAT WORKED INTERMITTENTLY. MAINTENANCE INSPECTED THE AIRCRAFT AND RESECURED THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRA FT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042600013 20070426 00013 SO 2007 4 26 C2XA07IA091 1 20070418 A 3350 SG9632 LIGHT EMB 145 EMB145XR 3260214 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17138 145727 IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE AISLE PATH LIGHTING WAS INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND RESECURED THE LIGHT STRIP BY THE GALLEY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS A PPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007042600016 20070426 00016 NM 2007 4 26 CALA0700198 1 20070423 A 5320 6517684638 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 NR 12 INTERCOSTAL CRACKED AT STA 294.5 TO 303.9. REPAIRED IAW ECRA 5311-01314. 2 L 7 2 4F RT A16WE 2007042600017 20070426 00017 NM 2007 4 26 CALA0700199 1 20070423 A 5340 69265552 ATTACH ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 STRINGER 16L, STA 348.2 UPPER ATTACH ANGLE CRACKED AT THE DOOR STOP FITTING FASTENER HOLE. REPAIRED IAW ECRA 5311-01314 . 2 L 7 2 4F RT A16WE 2007042500123 20070425 00123 NM 2007 4 25 SWAA071924 1 20070418 A 5330 6545767 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, LBL 1. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007042500133 20070425 00133 NM 2007 4 25 SWAA071912 1 20070418 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 5 O'CLOCK POSITION. REPAIRED WEB PER S RM. 2 L 7 2 4F RT A16WE 2007042500150 20070425 00150 NM 2007 4 25 AALA20070636 1 20070202 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 973AN 29548 TUL - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042500164 20070425 00164 NM 2007 4 25 USAA070290 1 20070418 A 5320 654583471 STRAP BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 BS 312 RBL 45, STABILIZER STRAP HAS CRACK. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 41-10-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007042500179 20070425 00179 NM 2007 4 25 AALA20070650 1 20070217 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 779AN 29955 AFW - EMERGENCY LIGHT BATTERY PACK IN CABIN AT FORWARD LEFT NUMBER TWO DOOR FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN AT FORWARD LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007042500181 20070425 00181 NM 2007 4 25 AALA20070630 1 20070124 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 AFW - EMERGENCY LIGHT BATTERY PACK FOR BUSINESS CLASS SEATS M33098 FAILED FUNCTIONAL TEST. REPLACED BATTERY PACK FOR EM ERGENCY LIGHT AT BUSINESS CLASS SEATS M33098. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007042500184 20070425 00184 NM 2007 4 25 SB07031 1 20070417 A 5610 5893543129 WINDSHIELD BOEING 737 7373B7 1384580 NM COCKPIT CRACKED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 505AU 28454 14494 23380 CLT FLT1047 - EN ROUTE FROM CMH TO CLT, CREW REPORTED VIA ACARS THAT THE CAPTAIN'S WINDSHIELD BEGAN ARCING AND THE OUTER PANE BEGAN CRACKING. CREW SLOWED AIRCRAFT TO 250 KNOTS AND DAMAGE STABILIZED. FLIGHT LANDED AT CLT WITHOUT FURTHER IN CIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S L1 WINDSHIELD PER JOB CARD J356-11-01. OPERATIONAL CHECK NORMAL . 2 L 7 2 4F RT A16WE 2007042500195 20070425 00195 NM 2007 4 25 USAA070319 1 20070423 A 5320 TIE CLIP BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 STA 294.5 FRAME S13L HAS CRACK. REMOVED AND REPLACED TIE CLIP PER SRM 51-20-01; 51-10-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007042500206 20070425 00206 NM 2007 4 25 AWXA200700510 1 20070410 A 5340 693535214 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - FOUND CRACKED STRINGER CLIP, BS 597, S8L. REPLACED STRINGER CLIP, BS 597, S8L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007042500238 20070425 00238 NM 2007 4 25 DHL2007782502 1 20070414 A 5312 PRESSURE PANEL BOEING 727 727227 1384078 NM BS 740-760 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 782DH 21998 CABIN PRESSURE WEB AT BS 740 TO 760, LT, IS CRACKED AT AFT HOLE. FABRICATED NEW PRESSURE WEB FROM 7075-T6, .040" BY 13. 5" BY 9.5", PO NR 9004539, PER B727 SRM 53-10-3 FIG 7 AND 51-20-1. TREATED, PRIMED, AND INSTALLED PRESS WEB PER B727 SR M 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 2007042500239 20070425 00239 NM 2007 4 25 USAA070305 1 20070423 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 531AU 24478 FUSELAGE SKIN BS 727E + 3 INCHES, 1 INCH BELOW S-18L HAS CRACK. FABRICATED & INSTALLED DOUBLER PER SRM 53-00-01, REPAIR 31, DETAIL XI, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007042500253 20070425 00253 WP 2007 4 25 IXXA07SMN121S 1 20070223 A 5313 2753715 LONGERON DOUG DC8 DC862F 3021972 WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT, LONGERON-35 RIGHT CRACKED AT STATION 1100.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED LONGERON SEGMENT. FABRICATED NEW SEGMENT OF LONGERON AND EXTERN AL DOUBLER. INSTALLED NEW REPAIR PARTS NEW FASTENERS IAW FORM 8100-9 DATED 03/15/2007, BOEING MESSAGE NUMBER 1-29601976 1-5 DATED 03/15/2007, DC8 SRM 53-2-2 FIGURE 13 TR NUMBER 53-191 DATED 10/15/2003, DC8 SRM 51-1-21, DC8 SRM 53-2-2 FIGURE 13 TR NUMBER 53-191, BOEING MESSAGE NUMBER 1-296019761-5 (SKETCH JCTO4049 FIGURE 1AND 2), SEMAN DRAWING ED-4470,DC8 SRM 53-4-1 FIGURE 44B SHEET 1 ITEM "R", AND DC8 SRM 51-2-0 FIGURE 50 SHEET 72B. 2 L 7 4 4F 4A25 2007042500261 20070425 00261 EU 2007 4 25 2007F00032 1 20070418 A 3260 82301217 BRACKET ISRAEL 1124 1124 4500102 EU GARRTT TFE731 TFE731* 01518 WP NLG BROKEN E K NONE J WARNING INDICATION AP APPROACH 1 SO 14 890BA 8613 8613 301 NOSE DOWNLOCK SWITCH MOUNTING BRACKET BROKEN: REPLACED BRACKET ASSEMBLY, INSTALLED A NEW UNIT PN: 823012-17. SECURITY, L EAK AND FUNCTION CHECKS PERFORMED WITH NO FAULTS FOUND. MAINTENANCE DONE IAW MM CHAPTERS: 29 AND 32. REF: 8130-3 (1/22/ 98) WO 4105-080112705. AUTH: NR CAAI AE-35. 2 M 7 2 4F 4 F A2SW E6WE 2007042500271 20070425 00271 NM 2007 4 25 ASMF200704014 1 20070422 A 7110 31421003 COWLING BOEING 737 737* NM CFMINT CFM567 CFM567B22 13802 NE LT ENGINE BIRD STRIKE W ASMF K NONE C F.O.D. IN INSP/MAINT 1 SW 23 850AM 10474 33786 892688 DURING TRANSIT CHECK, A BIRD STRIKE WAS DETECTED IN THE LT ENGINE NOSE COWLING. A BIRD STRIKE INSPECTION WAS PERFORMED I AW MM 05-51-48, FOUNDING A DENT OUT OF LIMITS WITH 18 INCHES LENGTH X 8 INCHES WIDTH AND 2 INCHES DEPTH, SO AIRCRAFT WAS SENT TO THE HANGAR. DURING OVERNIGHT CHECK, THE LT ENGINE NOSE COWLING WAS REPLACED IAW MM 71-11-01, TESTED CORRECT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007042500276 20070425 00276 SO 2007 4 25 C2XA07IA089 1 20070417 A 3040 3801D2MODA CONTROLLER EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL COCKPIT FAILED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 13123 9209 145688 FLT 2177 - UPON ARRIVAL TO THE TERMINAL THE CAPTAIN REPORTED A STRONG ELECTRICAL ODOR IN THE CABIN AND COCKPIT. MAINTENA NCE FOUND THE WINDSHIELD HEAT CONTROLLER TO HAVE FAILED CAUSING THE SMOKE SMELL. THE AFFECTED CONTROLLER WAS REPLACED, T HE WINDSHIELD HEATING SYSTEM OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED. 2 L 7 2 4F 4 F RT TE6CH 2007042500282 20070425 00282 WP 2007 4 25 IXXA07SMN118S 1 20070223 A 5340 37739062 FITTING DOUG DC8 DC862F 3021972 WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT, CRACKED ON FITTING BETWEEN STATION 759.000, LEFT BOTTOM LINE 24". REPLACED CRACKED FITTING IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1, AND EO NUMBER 53-DC8-2235. 2 L 7 4 4F 4A25 2007042500284 20070425 00284 WP 2007 4 25 IXXA07SMN126S 1 20070223 A 5310 BEAM DOUG DC8 DC862F 3021972 WP BS 1540 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 45961 DURING ROUTINE C CHECK INSPECTION, MAIN CARGO UPPER FLANGE BEAM WITH CRANK 1" AT STA 1540.000 RBL 39". PERFORMED MAJOR REPAIR IAW SRM 51-2-1 FIG 1 SHEET 8,12 TR NR 51-130 DATE 01/26/04. REMOVED FASTENERS IAW SRM 51-1-21, CUT DAMAGED AREA AND FABRICATED NEW FLANGE SEGMENT (AL 7075-T6 0.125) AND (02EA) REPAIR ANGLES OF (EXTRUSION 7075T6 0.125 P/N S1325214) A ND FILLER AL 7075-T6.IAW SRM 51-2-1 FIG 1, SHEET 8,12, TR NR 51-130 SRM 53-5-2 FIG 3, SHEET 2, ITEM "D" SRM 51-2-0 FIG 5 0, SHEET 61. CLEANED TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW SRM 51-2-1, FIG 1, SHEET 8, 12, AND SRM 51-1-20D, 51-3-1. (TORQUE) 2 L 7 4 4F 4A25 2007042500306 20070425 00306 EU 2007 4 25 07FDEA01419 1 20070411 A 5730 SKIN AIRBUS 310 A310324 3930206 EU RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 814FD 534 CORROSION AROUND THE INBOARD (RIB 13-14) AND OUTBOARD (RIB 27-28) OVERWING REFUELING PORTS OF THE LT AND RT WINGS. REPA IR PERFORMED BY LOCALIZED BLENDING AND SOME SUIT LOCALLY MANUFACTURED PACKERS IAW EA 6-5720-103301 AND RAS/BAE/1002880/2 006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007042500308 20070425 00308 EU 2007 4 25 07FDEA01421 1 20070411 A 5313 A53986217 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 TOOL DAMAGE A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 814FD 534 MISDRILLED HOLE IN STRINGER P54 AT C59. STRINGER REPAIR PERFORMED IAW SRM 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007042500311 20070425 00311 CE 2007 4 25 DJFA2007049 1 20070412 A 5511 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZ STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 792TA RK264 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE RT IB HORIZONTAL STA BILIZER, THE LT AND RT RIBS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMU NIQUE' NR 70. [SUP 05-04-07] BOTH BRACKETS WERE REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007042500334 20070425 00334 CE 2007 4 25 DXTA200702129 1 20070422 A 3246 WHEEL CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG VIBRATES E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 938QS 7500183 NOSE WHEEL VIBRATION ON TAKEOFF ROLL. YAW DAMP DISENGAGED. TAKEOFF ABORTED. [4-27-07] REMOVED AND REPLACED BOTH NOSE W HEEL ASSEMBLIES WITH OVERHAULED NOSE WHEEL ASSEMBLIES. WORK DRIVE IAW CHAP 32-41-01 OF THE CE750 MM. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007042500337 20070425 00337 CE 2007 4 25 DXTA200702094 1 20070408 A 2842 99144272 FLOAT SWITCH CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LT&RT WING INTERMITTENT E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 971QS 7396 7500071 HAD A RED (NO TAKEOFF) AFTER BRAKE RELEASE BELOW 30 KNOTS. REMOVED AND REPLACED BOTH FUEL LOW LEVEL FLOAT SWITCHES IAW MM 28-20-07. OPS CHECKS, LEAK CHECKS GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007042500350 20070425 00350 EU 2007 4 25 07FDEA01434 1 20070411 A 5730 SKIN AIRBUS 310 A310324 3930206 EU LT WING MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 814FD 534 AT LT WING REAR SPAR, FOUR MISDRILLED HOLES WHILE INSTALLING REINFORCING PLATE R573-49237-202, -203 IAW SB A310-57-2081. REPAIR PERFORMED BY OVERSIZING THE HOLES IAW EA 6-5710-103264 AND RAS/BAE/1003170/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007042500352 20070425 00352 NM 2007 4 25 07FDEA01344 1 20070404 A 5740 692288217 BRACKET BOEING 727 727225 1384077 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 NR 6 FLAP TRACK OTBD FAIRING ATTACH BRACKET IS CRACKED REMOVED AND REPLACED NR 6 FLAP TRACK OTBD BRACKET REF SRM 5130-2 PGS 3, 4 AND 5 AND SRM 51-20-031-7 PGS 1, 3 AND 7. 2 L 7 3 4F A3WE 2007042600004 20070426 00004 SO 2007 4 26 C2XA07RI016 1 20070420 A 3610 23073461125 DUCT CLAMP EMB 145 EMB145XR 3260214 SO BLEED AIR SYS DEFECTIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14174 14500876 FLT 2726 - EWR - CREW REPORTED ENGINE NR 1 ITT OVERTEMPERATURE ON CLIMBOUT AT FLIGHT LEVEL 180. CREW PERFORMED AIR RETU RN AND LANDED ACFT UNEVENTFULLY. EWR MX INSPECTED AND FOUND BAD 9TH STAG BLEED DUCT CLAMP. CLAMP WAS REMOVED AND REPLA CED. EWR MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO FLIGHT. 2 L 7 2 4F RT 2007042600010 20070426 00010 SO 2007 4 26 C2XA07SH020 1 20070415 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16987 145261 SHV - DURING C-CHECK MAINTENANCE FOUND CORROSION ON THE I/B SIDE & FLANGE OF THE LEFT OMEGA BEAM AT FRM 20. MAINTENANCE REPAIRED LEFT OMEGA BEAM AT FRM 20 IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007042600011 20070426 00011 SO 2007 4 26 C2XA07IA092 1 20070418 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16151 145758 MCI - DURING MAINTENANCE INSPECTION, THE FORWARD OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS AP PROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007042600018 20070426 00018 NM 2007 4 26 DU4R2007099 1 20070408 A 5730 106003183 PLATE BOEING 757 757232 1384965 NM RT WING CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND RT WING TANK PLATE 641FB CORRODED. REPAIRED BY REMOVING AND REPLACING WITH P/N 10-60031-83 IAW DELTA JOB CARD OPN 3612. 2 L 7 2 4F RT A2NM 2007042600019 20070426 00019 NM 2007 4 26 DU4R2007100 1 20070408 A 5730 106003183 PLATE BOEING 757 757232 1384965 NM RT WING CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND RT WING TANK PLATE 641DB CORRODED. REPAIRED BY REMOVING AND REPLACING WITH P/N 10-60031-83 IAW DELTA JOB CARD OPN 3612. 2 L 7 2 4F RT A2NM 2007042600020 20070426 00020 NM 2007 4 26 DU4R2007101 1 20070408 A 5730 106003183 PLATE BOEING 757 757232 1384965 NM RT WING CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND RT WING TANK PLATE 641AB CORRODED. REPAIRED BY REMOVING AND REPLACING WITH P/N 10-60031-83 IAW DELTA JOB CARD OPN 3612. 2 L 7 2 4F RT A2NM 2007042600021 20070426 00021 NM 2007 4 26 DU4R2007102 1 20070408 A 5730 106003183 PLATE BOEING 757 757232 1384965 NM RT WING CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND RT WING TANK PLATE 641MB CORRODED. REPAIRED BY REMOVING AND REPLACING WITH P/N 10-60031-83 IAW DELTA JOB CARD OPN 3612. 2 L 7 2 4F RT A2NM 2007042600022 20070426 00022 NM 2007 4 26 DU4R2007103 1 20070412 A 5730 106003183 PLATE BOEING 757 757232 1384965 NM RT WING CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND RT WING TANK PLATE 641EB CORRODED. REPAIRED BY REMOVING AND REPLACING WITH P/N 10-60031-83 IAW DELTA JOB CARD OPN 3612. 2 L 7 2 4F RT A2NM 2007042600023 20070426 00023 NM 2007 4 26 DU4R2007104 1 20070412 A 5730 112N61011 PLATE BOEING 757 757232 1384965 NM LT WING CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND LT WING TANK PLATE 541EB CORRODED. REPAIRED BY REMOVING AND REPLACING WITH P/N 112N6101-1 IAW DELTA JOB CARD OPN 3512. 2 L 7 2 4F RT A2NM 2007042600024 20070426 00024 NM 2007 4 26 DU4R2007105 1 20070411 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM BS 324 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND CORROSION AT FWD CABIN FLOORBEAM UPPER SURFACE BS 324 B/O RBL 50. REPAIRED BY REMOVING CORRODED T CAP, FABRICATED AND INSTALLED NEW T CAP 72 BY 3 BY 2 FROM AND10136-2409 EXTRUSION IAW B757 SRM 51-40-05, AND 53-10-08D. 2 L 7 2 4F RT A2NM 2007042600025 20070426 00025 NM 2007 4 26 CALA0700200 1 20070423 A 5320 6916970501 FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 L1 DOOR FUSELAGE OPENING CLIP CRACKED IN RADIUS ON S15L, STA 348. REPAIRED IAW ECRA 5311-01314. 2 L 7 2 4F RT A16WE 2007042600026 20070426 00026 NM 2007 4 26 HALA0700175 1 20070419 A 3610 UNKNOWN BOEING 767 767300 1385204 NM BLEED WARNING UNKNOWN A HALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 13 588HA 33466 ETOPS SIGNIFICANT SYSTEM, ON DESCENT LEFT ENG BLEED LIGHT ILLUMINATED AND L ENG PRV EICAS MSG ILLUMINATED. TURNED OFF L EFT ENG BLEED AIR SWITCH AND LEFT PACK CONTROL SELECTOR. PERFORMED TEST PER FIM 36-10-00 FIG 123. OPS CK'S NORMAL. NO FAULTS. NO MSG'S. 2 L 7 2 4F RT A1NM 2007042600027 20070426 00027 NM 2007 4 26 HALA0700173 1 20070419 A 3610 PNEUMATIC SYSTEM BOEING 767 767300 1385204 NM UNKNOWN A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 592HA 33468 ETOPS SIGNIFICANT SYSTEM, LEFT PNEUMATIC SYSTEM IS NOT BEING PRESSURIZED BY L ENGINE. PERFORMED BITE OF AIR SUPPLY MODU LE NO FAULTS NOTED. OPS CHECK OF L PNEUMATIC SYSTEM OPERATES NORMAL PER FIM 36-10-00 FIG 15 SHEET 1. 2 L 7 2 4F RT A1NM 2007042600028 20070426 00028 NM 2007 4 26 CALA0700187 1 20070420 A 5311 6545801512 FRAME BOEING 737 7373T0 1384582 NM BS 227 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19357 23841 CORROSION INSIDE LWR NOSE COMPARTMENT AFT SIDE OF CUTOUT, STA 227. REPAIRED IAW ECRA 5311-01308. 2 L 7 2 4F RT A16WE 2007042600029 20070426 00029 NM 2007 4 26 CALA0700188 1 20070421 A 5322 697305711 SHEAR TIE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19357 23841 FWD BAG BIN STA 500D, BL 0, CRACKED SHEAR TIE. REPAIRED IAW SRM 51-40-02, AND DRWG 69-73057-11. 2 L 7 2 4F RT A16WE 2007042600030 20070426 00030 NM 2007 4 26 CALA0700189 1 20070421 A 5314 65C385022 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19357 23841 LWR FUSELAGE SKIN BULGING AT STA 540, RBL 4. REPAIRED IAW SRM 51-40-02, AND 53-60-12. 2 L 7 2 4F RT A16WE 2007042600032 20070426 00032 NM 2007 4 26 CALA0700191 1 20070421 A 5311 65465403 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19357 23841 LEFT FRAME CRACKED AT STA 639 ON OUTBOARD CHORD. REPAIRED IAW ECRA 5311-01312. 2 L 7 2 4F RT A16WE 2007042600036 20070426 00036 NM 2007 4 26 CALA0700195 1 20070417 A 5220 SPRING BOEING 767 767424ER 1385270 NM EMERGENCY EXIT OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76065 29460 RIGHT EMERGENCY DOOR INTERNAL HANDLE CANNOT BACK AGAINST DOOR LINING. ADJUSTED TORSION SPRING ON THE TORQUE TUBE IAW AM M 52-22-01. 2 L 7 2 4F RT A1NM 2007042600037 20070426 00037 NM 2007 4 26 CALA0700196 1 20070420 A 2133 9510504 OUTFLOW VALVE BOEING 737 737724 13844BY NM CABIN PRESSURE MALFUNCTIONED A CALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 16709 28779 IN ALT PRESSURIZATION MODE AUTO FAIL LIGHT ILLUMINATED CABIN CLIMBING/DESCENDING ERRATICALLY. PSID IN ORANGE RANGE. RE MOVED AND REPLACED OUTFLOW VALVE IAW TASK 21-31-03-000-801, 21-31-03-400. 2 L 7 2 4F RT A16WE 2007042600038 20070426 00038 NM 2007 4 26 KCSA071159 1 20070418 A 5313 FITTING BOEING 747 747236B 1384804 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STR 40L END FITTING CORRODED FWD OF BS 2360. 2 L 7 4 4F A20WE 2007042600039 20070426 00039 NM 2007 4 26 KCSA071160 1 20070418 A 5313 FITTING BOEING 747 747236B 1384804 NM FUSLEAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STR 50L END FITTING CORRODED FWD OF BS 2360. 2 L 7 4 4F A20WE 2007042600040 20070426 00040 NM 2007 4 26 KCSA071161 1 20070418 A 5313 FITTING BOEING 747 747236B 1384804 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 STR 49R END FITTING CORRODED FWD OF BS 2360. 2 L 7 4 4F A20WE 2007042600041 20070426 00041 NM 2007 4 26 KCSA071163 1 20070422 A 5314 FITTING BOEING 747 747236B 1384804 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 CORROSION ON FITTING ON TOP OF KEEL BEAM AT BS 1480, LBL 9, WL 119. 2 L 7 4 4F A20WE 2007042600042 20070426 00042 NM 2007 4 26 SWAA072005 1 20070423 A 5315 141A5504 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 744SW 29490 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 19 TO RBL 47. REMOVED AND REPLACED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007042600043 20070426 00043 NM 2007 4 26 SWAA072006 1 20070423 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 744SW 29490 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 5. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007042600044 20070426 00044 NM 2007 4 26 SWAA071978 1 20070423 A 3350 1619 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 246LV 32507 DURING SCHEDULED MV3 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007042600045 20070426 00045 NM 2007 4 26 SWAA071980 1 20070423 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007042600047 20070426 00047 NM 2007 4 26 SWAA072001 1 20070423 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 210WN 34162 DURING SCHEDULED MV2 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007042600048 20070426 00048 2007 4 26 SWAA072004 4 20070423 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 768SW 30587 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007042600052 20070426 00052 NM 2007 4 26 SWAA072000 1 20070423 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007042600056 20070426 00056 NM 2007 4 26 SWAA071992 1 20070423 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007042600057 20070426 00057 NM 2007 4 26 SWAA071995 1 20070423 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007042600058 20070426 00058 NM 2007 4 26 SWAA071988 1 20070423 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007042600060 20070426 00060 NM 2007 4 26 SWAA071987 1 20070423 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007042600061 20070426 00061 NM 2007 4 26 SWAA071993 1 20070423 A 5311 6546551 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007042600062 20070426 00062 NM 2007 4 26 SWAA071994 1 20070423 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007042600063 20070426 00063 NM 2007 4 26 SWAA071984 1 20070423 A 5311 6546554 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007042600064 20070426 00064 NM 2007 4 26 SWAA071985 1 20070423 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007042600065 20070426 00065 NM 2007 4 26 SWAA071986 1 20070423 A 5311 6546557 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007042600066 20070426 00066 NM 2007 4 26 SWAA071991 1 20070423 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007042600067 20070426 00067 NM 2007 4 26 SWAA072007 1 20070423 A 5315 6546812 FLOORBEAM BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, LBL 3 TO LB 5. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007042600068 20070426 00068 NM 2007 4 26 SWAA071976 1 20070423 A 5313 6551698 STRINGER SPLICE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER S RM. 2 L 7 2 4F RT A16WE 2007042600069 20070426 00069 NM 2007 4 26 SWAA071990 1 20070423 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007042600072 20070426 00072 NM 2007 4 26 SWAA071973 1 20070423 A 5754 65C26601 SLAT BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED 14Y CHECK, FOUND RIGHT WING NR 5 L/E SLAT DELAMINATED UPPER AFT END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007042600074 20070426 00074 NM 2007 4 26 SWAA071979 1 20070423 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED MV2 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007042600077 20070426 00077 NM 2007 4 26 SWAA071975 1 20070423 A 5552 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED 14Y CHECK, RIGHT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR HORN BEARING PER MM. 2 L 7 2 4F RT A16WE 2007042600080 20070426 00080 NM 2007 4 26 USAA070294 1 20070418 A 5414 ACCESS PANEL BOEING 737 737301 1384611 NM LT PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 590US 23935 LEFT PYLON ACCESS PANEL 5727L ON OUTER SKIN HAS CRACK. INSTALLED DOUBLER PER TR 54-30-07, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007042600083 20070426 00083 NM 2007 4 26 ZZDA070419147 1 20070417 A 3260 893602 PSEU BOEING 717 717200 1383700 NM E&E BAY MALFUNCTIONED A ZZDA O OTHER N FALSE WARNING AP APPROACH 1 SO 15 957AT 55019 ON APPROACH WITH GEAR LOWERED GEAR UNSAFE WITH THREE RED LIGHTS WITH GEAR HANDLE DOWN CHECKLIST GEAR SHOWED SAFE LANDED STRAIGHT AHEAD. JACKED A/C REF B717 AMM 07-11, PERFORMED ADJUSTMENT TEST OF LANDING GEAR INDICATION PER 717 AMM 32-00, NO FAULTS OR DISCREPANCIES NOTED REMOVED AND REPLACED PSEU AS PRECAUTIONARY REF AMM 32-61, DOWNJACKED A/C RTS PASSED. 2 L 7 2 4F TR A6WE 2007042600091 20070426 00091 NM 2007 4 26 HALA0700176 1 20070418 A 2150 A/C PACK BOEING 767 76733A 1385209 NM LEFT UNKNOWN A HALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 13 593HA 33424 ETOPS SIGNIFICANT SYSTEM, L PACK HIGH EICAS AND LT PACK AUTO SHUTDOWN ON FINAL. PERFORMED PTC BITE PROCEDURES PER FIM 2 1-51-00; SYS CHECK OK. LEFT AC PACK OPS CHECK OK, NO ALERTS/MSGS NOTED. OK FOR SVC. 2 L 7 2 4F RT A1NM 2007042600092 20070426 00092 NM 2007 4 26 HALA0700174 1 20070417 A 2150 SWITCH BOEING 767 76733A 1385209 NM RT PACK RESET STUCK A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, RIGHT PACK TEMP, ICAS MSG RIGHT PACK RESET SWITCH IS STUCK IN THE IN (PRESSED) POSITION. RESE T RT PACK RESET SWITCH. CHECK OK. 2 L 7 2 4F RT A1NM 2007042600093 20070426 00093 NM 2007 4 26 NWAA1365501 1 20070417 A 3234 SWITCH BOEING 757 757251 1384970 NM MLG SELECTOR FAILED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 501US 23190 ON CLIMB OUT PASSING FL 250 AT APPROXIMATELY 290 KNOTS, UNCOMMANDED GEAR EXTENSION OCCURRED WITH THE GEAR HANDLE IN THE OFF POSITION. GEAR GREEN (NOSE, LEFT, RIGHT) AND DOORS AND GEAR AMBER LIGHTS ILLUMINATED UNTIL GEAR HANDLE WAS PUT IN DO WN POSITION THEN GEAR LIGHT EXTINGUISHED. CREW RETURNED TO SFO AND ATC DECLARED AN EMERGENCY. AN OVERWEIGHT LANDING WA S MADE AND THE FLIGHT LANDED WITHOUT INCIDENT. AIRCRAFT FERRIED TO SEA FOR MAINTENANCE, FOUND SWITCH S10191 BAD, REPLAC ED SWITCH. REPLACED RELAYS K10369 AND K10370. FOUND ELECTRICAL SHORT ON WIRE W2516-1025-20 AND SHORT IN CONNECTOR D403 700P. REPLACED CONNECTOR. JACKED AIRCRAFT AND SWUNG GEAR, OPS CHECKED NORMAL PER AMM 32-32-00 PAGE 501. AIRCRAFT OK F 2 L 7 2 4F RT A2NM 2007042600096 20070426 00096 EU 2007 4 26 07FDEA01535 1 20070423 A 5313 A53974482202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 CORROSION FOUND ON STRINGER BETWEEN C70-C71, P49 LT. REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007042600097 20070426 00097 EU 2007 4 26 07FDEA01536 1 20070423 A 5313 A53986218 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 FOUND OLD STRINGER REPAIR C60-61, P49, IS NOT PERFORMED IAW SRM. REPAIR RENEWED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007042600099 20070426 00099 EU 2007 4 26 07FDEA01538 1 20070423 A 5330 A53989559386 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 300 CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 809FD 449 CORROSION AT SKIN PANEL (A539-89559-386) AT C92 AND SEVERAL PARTS C91/92 BILGE AREA. REPAIR PERFORMED BY REPLACEMENT IAW SRM 51-72-10 OF FOLLOWING PARTS: T-SECTION A539-89317-208 / -209 / -206, SUPPORT SECTION A539-89330-216, PROFILE A539 -89317-228, ANGLES A539-89317-229 / -224 / -225 / -222 / -223 / -246, ANGLES A539-89579-200 / -201 / -202 / -203, BUTT S TRAP A539-89317-246, STIFFENER A539-89155-214, FLANGE A539-89155-204 / -236, SEALING STRIP A539-87435-200 / -201, WEB PL ATE A539-89317-202. REPAIR OF SKIN PANEL PERFORMED BY BLEND OUT AND FLAP PEENING IAW EA 6-5319-99196 AND RAS/DATLS/0003 123/2006 ISSUE "B". 2 L 7 2 4F RT A35EU 2007042600100 20070426 00100 NM 2007 4 26 07FDEA01539 1 20070423 A 5730 SKIN DOUG MD11 MD11 3023602 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 RIGHT WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT FOUND CRACKED. [SUP 05-09-07] CRACK AT RIGHT HAND WING FIXED LEAD ING EDGE TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57 -10-00 FIGURE 42 VOLUME I TR 57-8. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007042600101 20070426 00101 NM 2007 4 26 07FDEA01540 1 20070423 A 5730 SKIN DOUG MD11 MD11 3023602 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 LEFT WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT FOUND CRACKED. [SUP 05-11-07] CRACK AT LEFT HAND WING FIXED LEADIN G EDGE TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57- 10-00 FIGURE 42 VOLUME I TR 57-8. REPAIR CLASSIFIED AS MAJOR PE R GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007042600103 20070426 00103 NM 2007 4 26 07FDEA01542 1 20070423 A 5713 STRINGER DOUG MD11 MD11 3023602 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 CRACK FOUND AT STRINGER END 11R (XORS 704), APPROX 9.5" LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07 ] CRACK AT STRINGER END 11R (XORS 704), APPROX 9.5" LENGTH ON RIGHT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIG URE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007042600105 20070426 00105 NM 2007 4 26 07FDEA01544 1 20070423 A 5713 STRINGER DOUG MD11 MD11 3023602 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 CRACK FOUND AT STRINGER END 12L (XORS 642), APPROX 4.5" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07] CRACK AT STRINGER END 12L (XORS 642), APPROX 4.5" LENGTH ON LEFT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIGUR E 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007042600106 20070426 00106 NM 2007 4 26 07FDEA01545 1 20070423 A 5713 STRINGER DOUG MD11 MD11 3023602 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 CRACK FOUND AT STRINGER END 13L (XORS 629), APPROX 14" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07 ] CRACK FOUND AT STRINGER END 13L (XORS 629), APPROX 14" LENGTH ON LEFT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIG URE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007042600109 20070426 00109 WP 2007 4 26 07FDEA01549 1 20070423 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP BS 735 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 FLOOR STRUCTURE CORROSION AROUND CLIP NUT ATTACHMENT STA 735 RBL 58-72. REMOVED AND REPLACED SUPPORT AEAO397-503 IN REF ERENCE TO MD/DC SRM 51-35-01 VOL II PG 1. REPAIR CLASSIFIED AS MAJOR. 2 L 7 3 4F A22WE 2007042600110 20070426 00110 WP 2007 4 26 07FDEA01550 1 20070423 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP ZONE 900 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 FS 1219 BL 94 RT FLOORBOARD ATTACH ANGLE CORRODED AROUND FASTENER HOLE. REMOVED AND REPLACED SUPPORT AEA0397-533 IN REF ERENCE TO MD/DC 10 SRM 51-33-01 VOLII PG. 2 L 7 3 4F A22WE 2007042600111 20070426 00111 NM 2007 4 26 07FDEA01551 1 20070423 A 5343 ACA7017501 FITTING DOUG MD11 MD11 3023602 NM BS 595 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 NOSE LANDING GEAR, LEFT TRUNNION FITTING WITH 1.25 INCH CRACKED. [SUP 05-14-07] REPAIRED PER SRM 53-40-00 VOLUME I, FIGURE 23 OPTION 2. COMPLIED WITH FEDEX EA 1-5310-109864. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007042600114 20070426 00114 NM 2007 4 26 DU4R2007106 1 20070422 A 5311 FRAME BOEING 757 757232 1384965 NM BS 1645 S27L CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND CORROSION IN AFT CARGO PIT ON WASTE DRAIN LINE BOX FRAME AFT I/B CORNER BS 1645 S-27L. REPAIRED BY FABRICATING AN D INSTALLING NEW INTERCOSTAL 21 BY 4.5 FROM, STRINGER REPAIR 39 BY 3 FROM BAC1498-204 7075-T62, STRINGER SPLICE 10 BY 3 FROM BAC1498-204 7075-T62, ATTACH ANGLE 5 BY 2 FROM 2024-T3 .063 AND WATER PAN P/N 146N3641-44 IAW BOEING DWG NR 146N364 1 AND DPS 900-2 NR 5, B757 SRM 51-10-02, 51-40-02, 51-20-01, 51-20-05, 53-10-04, 53-00-03, 51-30-01 PG 8, AND 51-40-05. 2 L 7 2 4F RT A2NM 2007042600116 20070426 00116 WP 2007 4 26 NWAA071579604 1 20070420 A 2750 VANE DOUG DC9 DC932 3022066 WP FLAP VANE OBSTRUCTED A NWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 01 604NW 47222 WHEN THE CREW SELECTED 40 DEGREES OF FLAPS DURING APPROACH FOR LANDING, THE AIRCRAFT ROLLED TO THE RIGHT UNCOMMANDED. C REW WAS ABLE TO CORRECT THE ROLL OF THE AIRCRAFT WITH FOUR UNITS OF LEFT WING DOWN AILERON. THE LANDING WAS COMPLETED WITHOUT INCIDENT AND THE AIRCRAFT TAXIED TO THE GATE. MAINTENANCE FOUND THE LT MOVEABLE FLAP VANE STICKING ON THE VANE GUIDE AND LUBRICATED THE VANE GUIDE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007042600117 20070426 00117 NM 2007 4 26 AALA20070673 1 20070406 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 765AN 32879 AFW - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007042600118 20070426 00118 NM 2007 4 26 AALA20070674 1 20070411 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 959AN 30828 TUL - EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042600122 20070426 00122 NM 2007 4 26 AALA20070633 1 20070125 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 910AN 29512 TUL - EMERGENCY LIGHT BATTERY PACK AT FORWARD CABIN OVERHEAD AT STATION 325 FAILED FUNCTIONAL CHECK. REPLACED EMERGENCY LIGHT BATTERY PACK AT FORWARD CABIN OVERHEAD AT STATION 325. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042600123 20070426 00123 NM 2007 4 26 AALA20070643 1 20070202 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 955AN 29540 TUL - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042600124 20070426 00124 NM 2007 4 26 AALA20070657 1 20070314 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 914AN 29514 TUL - EMERGENCY LIGHT BATTERY PACK AT SEAT 18F FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK AT SEAT 18 F. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042600126 20070426 00126 WP 2007 4 26 NWAA071509884 1 20070415 A 5411 FRAME DOUG DC9 DC951 3022051 WP NR 1 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 677MC 47756 DURING ENGINE CHANGE, FOUND CRACKS IN NR 1 PYLON HORIZONTAL WEB FRAME AT XN 39.250. REPAIRED PER EA 98-209044. 2 L 7 2 4F RT A6WE 2007042600127 20070426 00127 NM 2007 4 26 NWAA071526744 1 20070330 A 5315 FLOORBEAM BOEING 747 747212F 1384851 NM BS 380 DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 644NW 24177 DURING "M" CHECK, FOUND SHORT EDGE MARGIN ON UPPER DECK FLOORBEAM REINFORCEMENT STRAPS AT BS 380 RT AND LT. ALSO, FOUND CRACK IN FLOORBEAM CHORD FASTENER HOLE AT BS 380 RBL 74. REPAIRED PER EA 67-208994. 2 L 7 4 4F RT A20WE 2007042600128 20070426 00128 WP 2007 4 26 NWAA071519751 1 20070421 A 5420 WEB DOUG DC9 DC941 302207N WP RT PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 751NW 47115 DURING SCHEDULED ENGINE CHANGE, FOUND CRACK IN LOWER EDGE OF RT PYLON CLOSURE WEB LIGHTENING HOLE AT STA YN 164. REPAIR ED PER EA 97-208937. 2 L 7 2 4F A6WE 2007042600132 20070426 00132 NM 2007 4 26 NWAA071495636 1 20070422 A 5410 SUPPORT BEAM BOEING 757 757251 1384970 NM NR 2 FAN COWL DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 536US 26483 DURING UPPER LINK BEARING REPLACEMENT NR 2 FAN COWL SUPPORT BEAM LOWER WEB WAS DAMAGED. REPAIRED PER EA 56-208439. 2 L 7 2 4F RT A2NM 2007042600133 20070426 00133 NM 2007 4 26 NWAA071566306 1 20070312 A 5322 SHEAR TIE BOEING 747 747451 1384940 NM BS 1160 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 666US 23821 DURING "M" CHECK, FOUND CRACK IN FASTENER HOLE OF TENSION TIE FRAME AT BS 1160 RBL 63. REPAIRED PER EA 63-209219. 2 L 7 4 4F RT A20WE 2007042600134 20070426 00134 NM 2007 4 26 NWAA071476306 1 20070313 A 5311 FRAME BOEING 747 747451 1384940 NM BS 1140 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 666US 23821 DURING "M" CHECK, FOUND CRACK ON FRAME WEB AND FRAME DOUBLER TENSION TIE AT BS 1140 RBL 70. REPAIRED PER EA 63-209214. 2 L 7 4 4F RT A20WE 2007042600135 20070426 00135 NM 2007 4 26 NWAA071456306 1 20070409 A 5311 FRAME BOEING 747 747451 1384940 NM BS 1265 S26L CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 666US 23821 DURING "M" CHECK, FOUND CRACK IN FRAME WEB HOLE AT BS 1265 S26L. ACCOMPLISHED INTERIM REPAIR PER EA 63-208916 SECTION I. REPETITIVE INSPECTIONS TO BE ACCOMPLISHED PER SECT II EVERY 2000 CYCLES. SECTION III PERMANENT REPAIR TO BE ACCOMPLIS HED BASED ON SECTION II INSPECTION FINDINGS. 2 L 7 4 4F RT A20WE 2007042600138 20070426 00138 NM 2007 4 26 NWAA071386306 1 20070313 A 5311 FRAME BOEING 747 747451 1384940 NM BS 500 S10L CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 666US 23821 DURING "M" CHECK, FOUND CRACK IN FRAME FASTENER HOLE AT BS 500 S10L. REPAIRED PER EA 63-209228. 2 L 7 4 4F RT A20WE 2007042600139 20070426 00139 NM 2007 4 26 NWAA071416306 1 20070313 A 5311 FRAME BOEING 747 747451 1384940 NM BS 500 S10R CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 666US 23821 DURING "M" CHECK, FOUND CRACK IN FORWARD FASTENER HOLE AT FRAME TO STRINGER CONNECTION BS 500 S10R. REPAIRED PER EA 63- 209223. 2 L 7 4 4F RT A20WE 2007042600142 20070426 00142 NM 2007 4 26 NWAA071396306 1 20070314 A 5322 SHEAR TIE BOEING 747 747451 1384940 NM BS 1120 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 666US 23821 DURING "M" CHECK, FOUND CRACK IN TENSION TIE CHANNEL AT BS 1120 RBL 71. REPAIRED PER EA 63-209225. 2 L 7 4 4F RT A20WE 2007042600144 20070426 00144 NM 2007 4 26 NWAA071406306 1 20070313 A 5320 INTERCOSTAL BOEING 747 747451 1384940 NM BS 1920-1960 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 666US 23821 DURING "M" CHECK, FOUND CORROSION ON BULK CARGO FLOOR PANEL SUPPORT INTERCOSTAL BS 1920-1960 LBL 55. REPAIRED PER EA 63 -209224. 2 L 7 4 4F RT A20WE 2007042600145 20070426 00145 NM 2007 4 26 NWAA071466306 1 20070310 A 5320 SUPPORT BRACKET BOEING 747 747451 1384940 NM BS 1120 S13R CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 666US 23821 DURING "M" CHECK WHILE PERFORMING SB 747-53A-2507 STAGE 2 INSPECTION, FOUND CRACKS IN SUPPORT BRACKET AND WEB FOR SLOPIN G PANEL AT BS 1120 S13R. REPAIRED PER EA 63-208915. 2 L 7 4 4F RT A20WE 2007042600146 20070426 00146 NE 2007 4 26 HALA0700177 2 20070420 A 7250 DUCT BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE TURBINE COOLING CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 580328 NR 1 ENG TURBINE CASE COOLING DUCT CRACKED 2 PLACES APPROX 10 O'CLOCK POSITION 1" LONG AND .75" LONG. CRACKED LPT TURBI NE CASE COOLING MANIFOLD IN TWO LOCATIONS AT THE WELD JOINT IS ACCEPTABLE AS IS. NEED TO REINSPECT CRACKED MANIFOLD EVE RY 30 CYCLES. MEASURE AND REPORT CRACK LENGTH TO POWERPLANT ENGINEERING. REPLACE THE UPPER LPT COOLING MANIFOLD ON OR BEFORE NEXT A CHECK. 2 L 7 2 4F 4 F RT A1NM E13NE 2007042600148 20070426 00148 EU 2007 4 26 07FDEA01446 1 20070411 A 5730 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 TOOL DAMAGE A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 814FD 534 RT WING REAR SPAR, MISDRILLED HOLE ON BOTTOM SKIN DURING EMBODIMENT OF SB 57-2081. REPAIR WAS PERFORMED BY OVERSIZING T HE HOLE IAW EA 6-5710-103285 AND RAS/BAE/1003241/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007042600149 20070426 00149 EU 2007 4 26 07FDEA01447 1 20070411 A 5311 A53980044233 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 814FD 534 FOUND CRACK IN FRAME SEGMENT C74, P'26 RT. REPAIR PERFORMED BY REPLACEMENT OF AFFECTED FRAME SEGMENT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007042600150 20070426 00150 WP 2007 4 26 07FDEA01448 1 20070411 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1381-1441 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 397FE 46631 DURING INSPECT, FOUND CORROSION ON L30 B/T STA 1381 TO STA 1441 RT SIDE. REPAIRED LONGERON FITTING PER SRM 53-10-00 FIG 1 AND 2 VOL I. 2 L 7 3 4F A22WE 2007042600152 20070426 00152 NM 2007 4 26 F3LA200700079 1 20070330 A 5315 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION AROUND NUTPLATE HOLE AT FR 66 ON FLOORBEAM BETWEEN FR 66 AND FR 64 AT Y1292. REMOVED AND REPLACED FLOORBEAM ASSY IAW A319 SRM 51-42-11. 2 L 7 2 4F RT A28NM 2007042600153 20070426 00153 EA 2007 4 26 SWIA200718115 1 20070225 A 7830 BRACKET CNDAIR CL600 CL6002B19 1900309 EA INLET COWL CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 LEFT ENGINE NOSE INLET COWL FLANGE HAS CRACKED WIRE BRACKET AT 8:00 POSITION, DISCOVERED AT C-CHECK. REPLACED WIRE BRA CKET P/N 228-50020-145 ON LEFT NOSE INLET COWL FLANGE IAW CRJ SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007042600154 20070426 00154 EA 2007 4 26 SWIA200718116 1 20070225 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW CRACKED CLIP ON AFT SIDE OF STA 280 BULKHEAD, DISCOVERED AT C-CHECK INSPECTION. REPLACED CLIP P/N 601R51570-31 IAW CRJ2 00 SRM 51-40-11. 2 L 7 2 4F RT A21EA 2007042600155 20070426 00155 EA 2007 4 26 SWIA200718117 1 20070226 A 5320 THRESHOLD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 866AS 7517 CORROSION EXISTS UNDER PAX DOOR THRESHOLD TOP FOLDING STEP ATTACH INTERCOSTAL, DISCOVERED AT C-CHECK INSPECTION. INSTAL LED NEW INTERCOSTAL AND TOP CAP ANGLE AT PAX DOOR THRESHOLD PER CRJ200 SRM 51-42-06 PG 1-18 AND CRJ200 SRM 51-42-21 PG 1 -9. 2 L 7 2 4F RT A21EA 2007042600156 20070426 00156 EA 2007 4 26 SWIA200718118 1 20070226 A 7120 601370157 YOKE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 866AS 7517 LEFT ENGINE FORWARD MOUNT YOKE UPPER AND LOWER BEARINGS HAVE EVIDENCE OF PITTING CORROSION. LOWER BEARING IS FROZEN, DI SCOVERED AT C-CHECK INSPECTION. REPLACED LEFT ENGINE FORWARD MOUNT YOKE P/N 601-37015-7. 2 L 7 2 4F 4 F RT A21EA E15NE 2007042600158 20070426 00158 EA 2007 4 26 SWIA200718120 1 20070226 A 2510 SEAT BACK CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 866AS 7517 PILOTS SEAT BACK SUPPORTS ARE CRACKED, DISCOVERED AT C-CHECK INSPECTION. INSTALLED NEW SUPPORT P/N1C3076-1AJT AND P/N1 C3076-2AJT PER CRJ200 SRM 51-42-10. 2 L 7 2 4F RT A21EA 2007042600159 20070426 00159 EA 2007 4 26 SWIA200718121 1 20070226 A 2510 SEAT BACK CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 866AS 7517 CO-PILOTS SEAT BACK SUPPORTS CRACKED, DISCOVERED AT C-CHECK INSPECTION. INSTALLED NEW SEAT BACK SUPPORTS P/N1C3076-2AJT AND P/N1C3076-1AJT PER CRJ200 SRM 51-42-10. 2 L 7 2 4F RT A21EA 2007042600160 20070426 00160 EA 2007 4 26 SWIA200718122 1 20070226 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT MLG WW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 866AS 7517 RIGHT WHEEL WELL TRANDUCER BRACKET IS CRACKED, DISCOVERED AT C-CHECK INSPECTION. INSTALLED NEW TRANSDUCER BRACKET P/N 6 01R-75262-157 PER CRJ200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007042600161 20070426 00161 EA 2007 4 26 SWIA200718123 1 20070226 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT MLG WW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 866AS 7517 LEFT WHEEL WELL TRANSDUCER BRACKET IS CRACKED, DISCOVERED AT C-CHECK INSPECTION. INSTALLED NEW TRANSDUCER BRACKET P/N 6 01R-75262-159 PER CRJ200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007042600163 20070426 00163 EA 2007 4 26 SWIA200718125 1 20070226 A 5260 AIRSTAIR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 866AS 7517 PAX DOOR STAIR CASE IS CRACKED AFT OF STEP NR 3, DISCOVERED AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER CRJ200 RE O 601R 52-11-702 REV 'A' ZONE 2 REPAIR. 2 L 7 2 4F RT A21EA 2007042600167 20070426 00167 NM 2007 4 26 AWXA200700502 1 20070410 A 5313 65516989 STRINGER SPLICE BOEING 737 73733A 1384673 NM BS 907 S4L CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - CRACKED STRINGER SPLICE CHANNEL, BS 907, S4L. REPLACED STRINGER SPLICE CHANNEL, BS 907, S4L IAW B737-300 SRM 51-4 0-02. 2 L 7 2 4F RT A16WE 2007042600168 20070426 00168 EA 2007 4 26 QXEA200700558 1 20070330 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 296 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - LIGHTNING STRIKE DAMAGE AT FS 296.00 2.7" DOWN OF STRINGER 16R. REPAIRED IAW REO670-53-21-257 AND SRM 51-42-06 . 2 L 7 2 4F RT A21EA 2007042600169 20070426 00169 EA 2007 4 26 QXEA200700557 1 20070329 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 296 S17R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - LIGHTNING STRIKE DAMAGE AT STRINGER 17R 4.7" FORWARD OF FS 296.00. REPAIRED IAW REO670-53-21-257 AND SRM 51-42 -06. 2 L 7 2 4F RT A21EA 2007042600172 20070426 00172 WP 2007 4 26 IXXA07SMN107S 1 20070223 A 5350 SKIN DOUG DC8 DC862F 3021972 WP TAIL CONE CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND TAIL CONE LOWER SKIN CORRODED STATION XFS 1813.000. REMOVED FASTENERS AS NEEDE D TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED , TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS AND NEW FASTENE RS IAW DC8 SRM 53-2-0 FIGURE 1D SHEET 3 PAGE 2K, DC8 SRM 51-1-21, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 53-2-0 PAGE 2P, DC 8 SRM 53-5-2 FIGURE 2 PAGE 3 ITEM "G", DC8 SRM 51-1-8B, AND DC8 SRM 51-1-11. 2 L 7 4 4F 4A25 2007042600173 20070426 00173 EU 2007 4 26 F3LA200700048 1 20070403 A 2121 VD3810 FAN AIRBUS A318 A318111 3940019 EU CABIN DEFECTIVE A F3LA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 805FR 1660 FLIGHT CREW REPORTED TOXIC ODOR IN CABIN DURING FLIGHT. ODOR MORE PREVALENT IN AFT PASSENGER CABIN AREA. INSPECTED AFT GALLEY AREA AND FOUND AFT CARGO VENT FAN DEFECTIVE. REPLACED FAN PER AMM 21-28-54-000-001. RAN PACKS AND ENGINES FOR SEVERAL MINUTES AND NO UNUSUAL ODORS WERE DETECTED. 2 L 7 2 4F RT 2007042600176 20070426 00176 NM 2007 4 26 DHL2007782504 1 20070405 A 5343 SUPPORT FITTING BOEING 727 727227 1384078 NM NLG TRUNNION CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 782DH 61330 61330 21998 NLG RT TRUNNION SUPPORT FITTING LOWER CAP PRESENTS CORROSION. REMOVED CORROSION AT RT TRUNNION BORE ORG DIA 2.488" FINA L DIA 2.587" MAT LOSS WITHIN LIMITS IAW B727 SRM 53-40-1 FIG 2. CHAMFER BORE HOLE TO .6 BY 45 DEGREES IAW B727 SRM 53-40 -1 FIG 2, PENETRANT INSPECTED MACHINED SURFACES OF TRUNNION FITTING IAW BOEING MM 20-20-02, NO DEFECTS NOTED. FAB NEW BEARING HALVES FROM P/N AL-NI BRONZE .620,PO NR 7177170 IAW B727 SRM 53-40-1 FIG 2. PENETRANT INSPECTED MACHINED SURFAC ES OF NEW HALVES IAW BOEING BSOPM 20-20-02, NO DEFECTS NOTED. CAD PLATED OUTER SURFACES OF BEARING IAW FAS FORM FAS 003 6 REV. 4. INSTALLED NEW HALVES BEARING AT RT TRUNNION IAW B727 SRM 53-40-1 FIG 2. 2 L 7 3 4F A3WE 2007042600177 20070426 00177 EA 2007 4 26 SWIA200718128 1 20070226 A 5210 ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 866AS 7517 PAX DOOR AFT UPPER CORNER HAS CRACKED INTERIOR ANGLE, DISCOVERED AT C-CHECK. INSTALLED INTERIOR ANGLE P/N 601R31-8094-2 AT PAX DOOR UPPER CORNER PER CRJ200 SRM 51-42-06. RII 52-900-1001. 2 L 7 2 4F RT A21EA 2007042600178 20070426 00178 EA 2007 4 26 SWIA200718129 1 20070305 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 448SW 7678 PAX DOOR WEB CRACKED UNDER HANDRAIL SUPPORT BRACKET ON AFT SIDE, DISCOVERED AT C-CHECK INSPECTION. INSTALLED FABRICATED PARTS 601R-52-11-702-7, -9,-17,-19,-15,-16 AND -21 PER REO 601R-52-11-702A. 2 L 7 2 4F RT A21EA 2007042500262 20070425 00262 EU 2007 4 25 2007F00033 1 20070418 A 3260 82301217 BRACKET ISRAEL 1124 1124 4500102 EU GARRTT TFE731 TFE731* 01518 WP NLG BROKEN E K NONE J WARNING INDICATION AP APPROACH 1 SO 14 890BA 8613 8613 301 NOSE DOWNLOCK SWITCH MOUNTING BRACKET BROKEN: REPLACED BRACKET ASSEMBLY, INSTALLED A NEW UNIT PN: 823012-17. SECURITY, L EAK AND FUNCTION CHECKS PERFORMED WITH NO FAULTS FOUND. MAINTENANCE DONE IAW MM CHAPTERS: 29 AND 32. REF: 8130-3 (1/22/ 98) W.O. 4105-080112705. AUTH: NR CAAI AE-35. 2 M 7 2 4F 4 F A2SW E6WE 2007042500264 20070425 00264 NM 2007 4 25 AMTA200700178 1 20070327 A 3150 WARNING SYSTEM BOEING 757 75723N 1384973 NM RROYCE RB211 RB211* 54555 NE EVAC SLIDE MALFUNCTIONED A AMTA K NONE O OTHER TX TAXI/GRND HDL 1 GL 11 520AT 27976 GIRT BAR ENGAGMENT LIGHT EXTN WITH DOOR IN THE ARMED POSITION R-2. INSPECTED DOOR SLIDE LIGHT. LIGHT OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A2NM A12EU 2007042500266 20070425 00266 NM 2007 4 25 AMTA200700188 1 20070411 A 4990 OIL COOLER BOEING 757 75733N 1384931 NM RROYCE RB211 RB211524B4 54555 NE APU UNKNOWN A AMTA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 561TZ 33526 APU AUTO SHUTDOWN. RESTART UNSUCCESSFUL. (K) REMOVED AND REPLACED OIL COOLER. LEAK CHECK GOOD. APU CHECKS GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007042500269 20070425 00269 NM 2007 4 25 ASMF200704010 1 20070413 A 4920 507263812761 APU DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE LEAKING W ASMF K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION IN INSP/MAINT 1 SW 23 162PL 2512 49765 DURING TRANSIT CHECK WAS DETECTED SMOKE AND OIL ODOR IN THE CABIN; ADDITIONALLY, THE SMOKE ALARM OF THE AFT LT LAVATORY WAS ACTIVATED. AIRCRAFT WAS VENTILATED AND SMOKE ALARM WAS DEACTIVATED, AIR CONDITIONING SYSTEM WAS CHECKED, BEING CORRE CT. APU WAS DETECTED LEAKING, SO APU AND WATER SEPARATORS WERE REPLACED IAW MM 49-10-00 AND 21-20-02, TEST CORRECT IAW M M 21-00-00 PAGE 501, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2007042500270 20070425 00270 NM 2007 4 25 ASMD200704013 1 20070419 A 3610 39271012 AUGMENT VALVE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE BLEED AIR SYS FAILED W ASMF G B O2 MASK DEPLOYED EMER. DESCENT J WARNING INDICATION CL CLIMB 1 SW 23 168PL 60661 27185 53174 RT PNEUMATIC SYSTEM FAILED DURING CLIMB, SO RT PNEUMATIC CABIN DEPRESSURIZED AND PASSENGERS OXYGEN MASKS WERE ACTIVATED. CAPTAIN PERFORMED ABNORMAL PROCEDURE DESCENDING AT 25,000 FEET. DURING MAINTENANCE CHECK, THE OXYGEN MASKS AND 25 OXYGE N GENERATORS WERE DETECTED ACTIVATED. AIRCRAFT WAS SENT TO THE HANGAR AND AUGMENTATION VALVE, 25 OXYGEN GENERATORS AND P RESSURE SWITCHES WERE REPLACED IAW MM 36-10-01, 35-22-01 AND 21-31-09; TESTS WERE PERFORMED IAW MM 36-10-00, 21-32-00, 3 5-20-00 AND 21-32-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007042500274 20070425 00274 SO 2007 4 25 C2XA07IA087 1 20070416 A 3350 20131A BATTERY PACK EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14143 2039 145739 FLT 2780 - DURING PREFLIGHT INSPECTION THE CEILING EMERGENCY LIGHT AT THE PASSENGER DOOR DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CL EARED THE DISCREPANCY. 2 L 7 2 4F 4 F RT TE6CH 2007042500278 20070425 00278 SO 2007 4 25 C2XA07IA090 1 20070418 A 3350 110049 POWER SUPPLY EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16151 145758 FLT 2887, DURING SCHEDULED MAINTENANCE THE RT OVERWING EMERGENCY EXIT LIGHT DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY POWER SUPPLY, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY . 2 L 7 2 4F 4 F RT TE6CH 2007042500280 20070425 00280 EU 2007 4 25 F3LA200700047 1 20070402 A 3397 CONNECTOR AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHTS DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 903FR 1560 MAINTENANCE REPORTED EPSU AFT L FAULTED. CLEANED AND INSPECTED PINS ON CONNECTOR TO EPSU AFT L POWER SUPPLY. PERFORMED EMERGENCY LIGHT TEST PER AMM 23-73-00-861-001 AND 33-51-38. OPS TEST GOOD. 2 L 7 2 4F RT A28NM 2007042500281 20070425 00281 SO 2007 4 25 C2XA07RI013 1 20070401 A 4990 OIL SYSTEM EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL APU OVERSERVICED A C2XA K NONE W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 12142 145735 FLT 2287, CREW REPORTED COCKPIT SMELLS OF SMOKE WHEN PACK NR 2 IS SELECTED. MX INSPECTED APU AND FOUND SIGNS OF EXCESSIV E OIL SERVICE. MX CLEANED APU AREA AND PERFORMED OPS CHECK OF PACK NR 2. OPS CHECK GOOD, NO SIGNS OF SMOKE FOUND. 2 L 7 2 4F 4 F RT TE6CH 2007042500289 20070425 00289 EA 2007 4 25 SWIA200718074 1 20070329 A 2910 O-RING CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 07 446SW 7666 AFTER GEAR EXTENSION, HYD PUMP 3A CAUTION MESSAGE. HYDRAULIC SYSTEM 3 EMPTY. REPLACE O-RING ON NR 3A PRESSURE MANIFOLD . OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2007042500290 20070425 00290 EA 2007 4 25 SWIA200718075 1 20070328 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCONNECTED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 448SW 7678 GALLEY OVERHEAD EMERGENCY EXIT LIGHT INOP. SECURED WIRING AT CONNECTION. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2007042500295 20070425 00295 SO 2007 4 25 SWIA200718080 1 20070402 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS MISSING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 299SW 120329 ENTRY WAY EXIT PLACARD IS MISSING. REMOVED REMAINING EXIT SIGN HOUSING AT AND INSTALLED NEW LIGHT ASSEMBLY. OPERATIONA L CHECK GOOD, P/N 10-1301-15. 2 L 7 2 4T RT A31SO 2007042500296 20070425 00296 SO 2007 4 25 SWIA200718081 1 20070403 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 578SW 120346 STRINGER 8 AT RIB 8 IN LEFT INBOARD WING IS CRACKED, DISCOVERED DURING 5A CHECK. REPLACED STRINGER 8 AT RIB 8 IN LEFT I NBOARD WING PER EMB 120 SRM 57-20-03. 2 L 7 2 4T RT A31SO 2007042500297 20070425 00297 EA 2007 4 25 SWIA200718082 1 20070328 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR STUCK A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 954SW 7815 SERVICE DOOR HANDLE WILL NOT OPEN FROM OUTSIDE.CLEANED EXCESSIVE AMOUNT OF GREASE FROM HANDLE IAW MM 52-41-03. OPERATI ONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2007042500298 20070425 00298 SO 2007 4 25 SWIA200718083 1 20070331 A 2597 WIRE EMB 120 EMB120ER 3260203 SO COFFEEMAKER BURNED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 580SW 120348 LEFT HOT JUG IS NOT HEATING. REPLACED BURNED WIRE LEAD AND CONNECTOR. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2007042500302 20070425 00302 NM 2007 4 25 07FDEA01415 1 20070410 A 2497 WIRE DOUG MD11 MD11 3023602 NM BS 1136 BURNED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 592FE 48550 FOUND SEVERAL WIRES AND MOD BLOCKS BURNED AT S3-438 IN CENTER ACCESSORY LT SIDE JUST AFT OF EPC BAY NR 1 AT STA 1136 JUS T BELOW FLOOR PANEL. INSPECTED AND REPAIRED DAMAGED WIRES AND MOD BLOCKS PER EA 1-2821-109931 "FUEL SYSTEM REPAIR/INSPE CT DAMAGED WIRES". PERFORMED OPS CHECKS ON AFFECTED CIRCUITS PER W/D 23-41-03, 26- 23-01, 28-22-05, 32-44-01, 32-48-02 , AND 36-15-01. ALL CHECKS NORMAL. 2 L 7 3 4F RT A22WE 2007042500304 20070425 00304 NM 2007 4 25 07FDEA01417 1 20070410 A 5730 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RIGHT WING, NR 4 LEADING EDGE SLAT O/B TRACK LOWER CUTOUT I/B CORNER FOUND CRACKED. [SUP 04-30-07] REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007042500307 20070425 00307 EU 2007 4 25 07FDEA01420 1 20070411 A 5330 SKIN AIRBUS 310 A310324 3930206 EU ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 814FD 534 AN OLD REPAIR DOUBLER BETWEEN C76-C77, P22-P23 LT WAS NOT CONFORM TO THE INDICATED REFERENCE: SRM 53-10-12/FIG 202. DOU BLER REPAIR HAS BEEN RENEWED IAW SRM 53-10-12/FIG 225, APPROVED BY EA 6-5318-101262. 2 L 7 2 4F RT A35EU 2007042500309 20070425 00309 EU 2007 4 25 07FDEA01422 1 20070411 A 5340 A53973106200 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 814FD 534 FOUND CORROSION ON FITTING C59A, P44-46 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007042500314 20070425 00314 EU 2007 4 25 07FDEA01427 1 20070411 A 5730 A57310000 PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 814FD 534 CORROSION FINDINGS ON CENTER WING BOX LOWER PANEL LT AT C47 IN SEVERAL HOLES (NR 1- NR 21). REPAIR PERFORMED BY BLEND O UT AND REAM UP HOLES IAW EA 6-5710-103305 AND RAS 046071/006/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007042500316 20070425 00316 CE 2007 4 25 DXTA200702124 1 20070420 A 4940 STARTER CESSNA 680 680CE 2076811 CE APU FAILED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 07 380QS 6800089 APU SHUTDOWN AFTER A BURNING ODOR PRESENT IN THE CABIN. APU SYSTEM FAIL FOLLOWED THE SHUTDOWN. [4-27-07] REMOVED AND R EPLACED APU STARTER GENERATOR IAW 680 MM CHPT 49-40-00. LEAK AND OPS CHECK GOOD 2 L 7 2 4F RC T00012WI 2007042500319 20070425 00319 CE 2007 4 25 DXTA200702134 1 20070423 A 3220 LANDING GEAR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG VIBRATION E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 904QS 7500210 SEVERE VIBRATION AT APPROXIMATELY 60 KNOTS DURING TAKE-OFF. YAW DAMPER DISCONNECTED ANF NR1 ADC FAILED. ABORTED TAKEOF F. [SUP 04-27-07] NOTED TIRES WERE BOTH OUT OF ROUND. REMOVED AND REPLACED BOTH NOSE TIRES. YAW DAMP DISCONNECT AND NR 1 ADC FAILURE DUE TO NOSE GEAR VIBRATION. NO FAULTS FOUND. WORK DONE IAW CHAPTER 32-41-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007042500322 20070425 00322 CE 2007 4 25 DXTA200702110 1 20070415 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 393QS 5600393 FO BRAKES VERY SOFT AND SPONGY. F/O BRAKE PEDALS TRAVELS TO THE STOP. CAPTAINS SIDE SOFT AS WELL. BLEED BRAKE PER CITAT ION 560 M/M 32-42-00. OPS AND LEAK CHECK GOOD AT THIS TIME. 2 L 7 2 4F 4 F RT A22CE E25EA 2007042500324 20070425 00324 CE 2007 4 25 DXTA200702111 1 20070416 A 2150 A/C PACK CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL A/C BAY ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 982QS 7500182 STRONG BURN SMELL FROM COCKPIT PACK. PAC TURNED OFF. NO DIVERSION. REMOVED & REPLACED COCKPIT ACM IAW CESSNA 750 MM CH PT 21-51-00. OPS & LEAK CHECKS GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007042500330 20070425 00330 CE 2007 4 25 DXTA200702119 1 20070418 A 2740 WARNING LIGHT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL COCKPIT ILLUMINATED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 942QS 7500024 PITCH FEEL FAIL AMBER CAS MESSAGE ILLUMINATED IN FLIGHT. REMOVED AND REPLACED LINEAR ACTUATOR IAW CE750 MM 27-33-00. OP ERATIONAL CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007042500333 20070425 00333 CE 2007 4 25 DXTA200702128 1 20070421 A 3240 BRAKE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MALFUNCTIONED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 838QS 258338 BRAKES NEED ALMOST FULL PEDAL DEFLECTION FOR MAXIMUM BRAKING. NOT SURE IF MAX BRAKING WAS NEEDED IT WOULD BE AVAILABLE. [4-27-07] BLED ALL 4 BRAKE ASSEMBLIES OPS AND LEAK CHECK GOOD. ALL WORK DONE I/A/W HAWKER 800XP MM CH 32-40-00 2 L 7 2 4F 4 F RT A3EU E6WE 2007042500336 20070425 00336 CE 2007 4 25 DXTA200702115 1 20070418 A 2120 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL COCKPIT ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 904QS 7500210 FUMES IN THE COCKPIT. SOURCE BELIEVED TO BE FROM COCKPIT/CABIN PACS, OCF FLT. ICT-ICT. FOUND RESIDUAL SOAP IN OZONE CO NVERTERS. CLEANED & REINSTALLED OZONE CONVERTERS & COALESCER SOCKS IAW CE750 M.M. 21-71-00. LEAK & OPS CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007042500340 20070425 00340 NM 2007 4 25 F3LA200700065 1 20070328 A 5321 FLOORBOARD AIRBUS A319 A319111 3930336 NM GE CF700 CF7002D2 30010 NE CABIN CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED RUST BUILD-UP IN AFT OB MOUNTING HOLE IN FLOORBOARD, AFT LT LAVATORY. INSTALLED NEW BUSHING AND PACKING IN FLOORBOARD UNDER LAV D AFT OB MOUNT IAW A319 AMM 25-43-41-400-001. 2 L 7 2 4F 4 F RT A28NM E7EA 2007042500343 20070425 00343 CE 2007 4 25 GUUA04170701 1 20070417 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT MLG SLOW A GUUA O OTHER O OTHER AP APPROACH 1 SO 29 81538 UE199 FLIGHT: 9167, DURING APPROACH LANDING GEAR WOULD NOT EXTEND. MANUALLY EXTENDED LANDING GEAR. LANDED WITHOUT INCIDENT. R EPLACED LANDING GEAR POWER PACK MOTOR AND RT LANDING GEAR ACTUATOR. OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007042500348 20070425 00348 EU 2007 4 25 07FDEA01429 1 20070411 A 5730 SKIN AIRBUS 310 A310324 3930206 EU LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 814FD 534 CORROSION FINDINGS ON BOTTOM SKIN PANEL NR 1 AND NR 2, RIB 17-19 AND RIB 21-24. REPAIR PERFORMED BY BLEND OUT CORROSION IAW EA 6-5720-103322 AND RAS/BAE/1003249/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007042500357 20070425 00357 NE 2007 4 25 REXA200700051 2 20070403 A 7261 PLUG CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENGINE OIL MISSING A REXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 8836A 7836 GEE873838 AFTER TAKEOFF FROM SBN, THE AIRCRAFT CLIMBED TO FL290. SHORTLY AFTER REACHING CRUISE ALTITUDE, THE RIGHT ENGINE OIL PRE SSURE WARNING ILLUMINATED FOLLOWED BY A DROP IN OIL PRESSURE ON THE RT OIL PRESSURE GAUGE. THE FLIGHT CREW PERFORMED TH E QRH AND REDUCED POWER ON THE ENGINE. SEEING THAT THE OIL PRESSURE CONTINUED TO DROP, THE CAPTAIN ELECTED TO SHUTDOWN THE ENGINE. AN EMERGENCY WAS DECLARED AND AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WAS MADE AT MSP. MAINTENANCE FO UND THAT THE AIRCRAFT HAD A MEL'D NR 2 ENGINE DRIVEN HYDRAULIC PUMP. FURTHER INVESTIGATION REVEALED THAT THE PUMP HAD N OT BEEN PROPERLY MEL'D AT SBN. OIL LOSS WAS THE RESULT OF A MISSING SPLINE PLUG AND O-RING WHICH ARE PART OF THE MEL KI 2 L 7 2 4F 4 F RT A21EA E15NE 2007042500360 20070425 00360 SO 2007 4 25 SWIA200718088 1 20070329 A 3097 CONNECTOR EMB 120 EMB120ER 3260203 SO WINDSHIELD WIPER OVERHEATED A SWIA O OTHER M OVER TEMP TX TAXI/GRND HDL 1 NM 07 295UX 120295 RIGHT WINDSHIELD WIPER INOP. REPLACED OVERHEATED PINS AT CONTROLLER CONNECTION. 2 L 7 2 4T RT A31SO 2007042500362 20070425 00362 EU 2007 4 25 07FDEA01444 1 20070411 A 5280 STRUT AIRBUS 310 A310324 3930206 EU RT MLG DOOR DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 801FD 539 RT MLG DOOR STRUT W/SKIN SURFACE DAMAGED REPAIRED PER FEDEX EA NR 6-5280-106709 AND SRM 51-77-12. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. 2 L 7 2 4F RT A35EU 2007042600002 20070426 00002 NM 2007 4 26 NWAA071365501 1 20070417 A 3234 SWITCH BOEING 757 757251 1384970 NM MLG SELECTOR FAILED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 501US 23190 ON CLIMB-OUT PASSING FL 250 AT APPROXIMATELY 290 KNOTS, UNCOMMANDED GEAR EXTENSION OCCURRED WITH THE GEAR HANDLE IN THE OFF POSITION. GEAR GREEN (NOSE, LEFT, RIGHT) AND DOORS AND GEAR AMBER LIGHTS ILLUMINATED UNTIL GEAR HANDLE WAS PUT IN D OWN POSITION THEN GEAR LIGHT EXTINGUISHED. CREW RETURNED TO SFO AND ATC DECLARED AN EMERGENCY. AN OVERWEIGHT LANDING W AS MADE AND THE FLIGHT LANDED WITHOUT INCIDENT. AIRCRAFT FERRIED TO SEA FOR MAINTENANCE, FOUND SWITCH S10191 BAD, REPLA CED SWITCH. REPLACED RELAYS K10369 AND K10370. FOUND ELECTRICAL SHORT ON WIRE W2516-1025-20 AND SHORT IN CONNECTOR D4 03700P. REPLACED CONNECTOR. JACKED AIRCRAFT AND SWUNG GEAR, OPS CHECKED NORMAL PER AMM 32-32-00 PAGE 501. AIRCRAFT OK 2 L 7 2 4F RT A2NM 2007042600003 20070426 00003 SO 2007 4 26 C2XA07RI018 1 20070419 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO CARGO BAY INOPERATIVE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 15973 18759 145159 FLIGHT 2882 - EWR - CREW REPORTED NR 2 CARGO SMOKE DETECTOR INOP. EWR MX REMOVED AND REPLACED NR 2 CARGO SMOKE DETECTOR IAW EMB AMM 26-23-00. MX PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007042600014 20070426 00014 SO 2007 4 26 C2XA07RI017 1 20070415 A 2120 BTW126814334 FLEX DUCT EMB 145 EMB145LR 3260212 SO A/C BAY DAMAGED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 15983 145239 FLT 2987 - EWR - FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN COMING FROM FLOOR VENT BETWEEN ROWS 9-11. EWR MX FOUND NR 1 PACK DUCT TO BE OFF RECIRCULATE FAN AND TO BE DAMAGED. MX REMOVED AND REPLACED DUCT IAW EMB 145 MM 21-20-04. MX PER FORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007042600015 20070426 00015 NM 2007 4 26 CALA0700197 1 20070423 A 5340 69165096 ATTACH ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 L1 DOOR STOP FITTING LOWER ATTACH ANGLE CRACKED AT THE DOOR STOP FITTING FASTENER HOLE. REPAIRED IAW ECRA 5311-01314. 2 L 7 2 4F RT A16WE 2007042600033 20070426 00033 NM 2007 4 26 CALA0700192 1 20070421 A 5311 65465403 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19357 23841 LEFT FRAME CRACKED AT STA 639 ON O/B CHORD. REPAIRED IAW ECRA 5311-01312. 2 L 7 2 4F RT A16WE 2007042600034 20070426 00034 NM 2007 4 26 CALA0700193 1 20070421 A 5311 654654043 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19357 23841 FUSELAGE FRAME AND WEB CRACKED AT STA 639 AT STRINGER 17L. REPAIRED IAW ECRA 5311-01311. 2 L 7 2 4F RT A16WE 2007042600035 20070426 00035 NM 2007 4 26 CALA0700194 1 20070421 A 5330 6545769 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19357 23841 FUSELAGE SKIN INSIDE AIR DISTRIBUTION BAY FWD SIDE OF STA 540 STR 28RT KEEL BEAM CORRODED. REPAIRED IAW ECRA 5331-01301 . 2 L 7 2 4F RT A16WE 2007042600046 20070426 00046 NM 2007 4 26 SWAA072002 1 20070423 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 737JW 27869 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 4 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007042600055 20070426 00055 NM 2007 4 26 SWAA071996 1 20070423 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007042600059 20070426 00059 NM 2007 4 26 SWAA071983 1 20070423 A 5311 6546549 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007042600070 20070426 00070 NM 2007 4 26 SWAA071989 1 20070423 A 5311 65C25228 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007042600071 20070426 00071 NM 2007 4 26 SWAA071982 1 20070423 A 5311 65C25230 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007042600073 20070426 00073 NM 2007 4 26 SWAA072008 1 20070423 A 5754 65C26601 SLAT BOEING 737 7373T5 1384608 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 22Y CHECK, FOUND RIGHT WING NR 5 L/E SLAT CRACKED AT INBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007042600075 20070426 00075 NM 2007 4 26 SWAA071977 1 20070423 A 2560 P2070001 FLASHLIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 223WN 32492 DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2007042600076 20070426 00076 NM 2007 4 26 SWAA071997 1 20070423 A 5552 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 613SW 27931 DURING SCHEDULED C4 CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED INPUT ROD BEARING PER MM. 2 L 7 2 4F RT A16WE 2007042600078 20070426 00078 NM 2007 4 26 SWAA071974 1 20070423 A 5552 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED 14Y CHECK, LEFT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR HORN BEARING PER MM. 2 L 7 2 4F RT A16WE 2007042600102 20070426 00102 NM 2007 4 26 07FDEA01541 1 20070423 A 5713 STRINGER DOUG MD11 MD11 3023602 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 CRACK FOUND AT STRINGER END 11L (XORS 704), APPROX 13" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07 ] CRACK AT STRINGER END 11L (XORS 704), APPROX 13" LENGTH ON LEFT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIGUR E 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007042600107 20070426 00107 NM 2007 4 26 07FDEA01546 1 20070423 A 5713 STRINGER DOUG MD11 MD11 3023602 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 CRACK FOUND AT STRINGER END 50L (XORS 152), APPROX 8" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07] CRACK AT STRINGER END 50L (XORS 152), APPROX 8" LENGTH ON LEFT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIGURE 10 V OLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007042600108 20070426 00108 WP 2007 4 26 07FDEA01547 1 20070423 A 5347 SEAT TRACK DOUG DC10 DC1030 3023501 WP BS 1099-1321 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 319FE 47820 MCD SEAT TRACK FROM STA 1099 TO STA 1321 RBL 47 HAS 6 AREAS WITH WORN LUGS. FOUND DURING C CHECK AT MAE, REMOVED AND R EPLACED DAMAGED SEAT TRACK 2 L 7 3 4F A22WE 2007042600112 20070426 00112 WP 2007 4 26 07FDEA01548 1 20070423 A 5730 SKIN DOUG DC10 DC1010 3022110 WP RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 RIGHT WING UPPER SURFACE HAS CORROSION JUST O/B OF TRUNNION DOUBLER. [SUP 05-21-07] REMOVED COROSION FROM WING SKIN,OR IG THICKNESS .495,AMOUNT REMAINING.476,MATERIAL LOSS .019 FOUND TO BE WITHIN LIMITS IAW DC/MD SRM 57-10-00 FIG.61 VOL I,51-20-00 FIG2 VOL III AND EA 8-5710-109149. ALODINED,PRIMED, APPLIED TOPCOAT IAW DC/MD 51-21-01 VOL II. MINOR REPAIR 2 L 7 3 4F A22WE 2007042600113 20070426 00113 NM 2007 4 26 DU4R2007089 1 20070419 A 5330 SKIN BOEING 757 757232 1384965 NM BS 1480-1500 DENTED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND EXTERNAL LOWER FUSELAGE SKIN BUCKLED AT S-26L AND BETWEEN BS 1480 TO 1500. REPAIRED BY CUTTING OUT BUCKLED/DENTED AREA, FABRICATED AND INSTALLED 2 REPAIR DOUBLERS 5 BY 5 FROM 2024-T3 .063 IAW DELTA SRM 53-00-01 FIG 101, 53-00-01 FIG 201, 51-10-02 PG 7 AND 51-40-02. 2 L 7 2 4F RT A2NM 2007042600115 20070426 00115 NM 2007 4 26 DU4R2007107 1 20070422 A 5311 FRAME BOEING 757 757232 1384965 NM BS 1661 S26-28R CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND CORROSION IN AFT CARGO PIT LWR FRAME FWD FACE AT BS 1661 FROM S-26L TO S-28R. REPAIRED BY FABRICATING AND INSTALL ING 3 SHEAR TIES 1.5 BY 4", 4" BY 4", 7.5" BY 3" FROM 7075-T6 .050 AND ONE 4.5" BY 5" FROM 7075-T6 .071 AND REPAIR DOUB LER 20 BY 6 FROM 7075-T6 .063" IAW BOEING DWG 146N1032 AND 140N202, DPS 900-2 NR 5, B757 SRM 53-00-07, 51-10-02, 51-40-0 2, 51-40-02, AND 51-20-01. 2 L 7 2 4F RT A2NM 2007042600119 20070426 00119 NM 2007 4 26 AALA20070675 1 20070411 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 959AN 30828 TUL - EMERGENCY LIGHTS IN FORWARD CABIN CEILING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FORWARD CABI N CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042600121 20070426 00121 NM 2007 4 26 AALA20070665 1 20070322 A 3350 1010427 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 916AN 29517 TUL - EMERGENCY LIGHT AT SEAT 5E HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042600125 20070426 00125 NM 2007 4 26 AALA20070658 1 20070319 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 923AN 29524 TUL - EMERGENCY LIGHT BATTERY PACK IN COACH CABIN FAILED FUNCTIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IN COAC H CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042600129 20070426 00129 NM 2007 4 26 NWAA071536744 1 20070402 A 5311 FRAME BOEING 747 747212F 1384851 NM BS 840 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 644NW 24177 DURING "M" CHECK FOUND CRACKS IN FASTENER HOLE FRAME WEB TENSION TIE AREA AT BS 840 LT AND RT. REPAIRED PER EA 67-20899 2. 2 L 7 4 4F RT A20WE 2007042600130 20070426 00130 NM 2007 4 26 NWAA071546744 1 20070402 A 5311 FRAME BOEING 747 747212F 1384851 NM BS 820 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 644NW 24177 DURING "M" CHECK, FOUND CRACKS IN FRAME FASTENER HOLES AT TENSION TIE AREA BS 820 LT AND RT. REPAIRED PER EA 67-208989. 2 L 7 4 4F RT A20WE 2007042600131 20070426 00131 NM 2007 4 26 NWAA071556744 1 20070404 A 5311 FRAME BOEING 747 747212F 1384851 NM BS 2120 S25-26R CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 644NW 24177 DURING "M" CHECK, FOUND CRACK IN FRAME AT BS 2120 S25R AND S26R. REPAIRED PER EA 67-208996. 2 L 7 4 4F RT A20WE 2007042600136 20070426 00136 NM 2007 4 26 NWAA071486306 1 20070412 A 5320 INTERCOSTAL BOEING 747 747451 1384940 NM BS 340 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 666US 23821 DURING "M" CHECK, FOUND CRACKS IN UPPER CROWN INTERCOSTAL AT BS 340 BL 0. REPAIRED PER EA 63-208913. 2 L 7 4 4F RT A20WE 2007042600137 20070426 00137 NM 2007 4 26 NWAA071376306 1 20070313 A 5311 FRAME BOEING 747 747451 1384940 NM BS 480 S10L CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 666US 23821 DURING "M" CHECK, FOUND CRACK IN FRAME TO STRINGER CONNECTION FASTENER HOLE AT BS 480 S10L. REPAIRED PER EA 63-209229. 2 L 7 4 4F RT A20WE 2007042600141 20070426 00141 NM 2007 4 26 NWAA071436306 1 20070311 A 5322 SHEAR TIE BOEING 747 747451 1384940 NM 1180 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 666US 23821 DURING "M" CHECK, FOUND CRACKS ON UPPER LOBE TENSION TIE FRAME WEB FASTENER HOLES AT BS 1180 LT. REPAIRED PER EA 63-209 218. 2 L 7 4 4F RT A20WE 2007042600143 20070426 00143 NM 2007 4 26 NWAA071446306 1 20070311 A 5322 SHEAR TIE BOEING 747 747451 1384940 NM BS 1180 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 666US 23821 DURING "M" CHECK, FOUND CRACK ON UPPER LOBE TENSION TIE FORWARD CHANNEL AT BS 1180 RT. REPAIRED PER EA 63-209217. 2 L 7 4 4F RT A20WE 2007042600147 20070426 00147 NM 2007 4 26 HALA0700178 1 20070420 A 4910 1796251 VALVE BOEING 717 717200 1383700 NM APU FAILED A HALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 13 479HA 55124 CABIN CREW REPORTS ACIDIC ODOR IN THE CABIN CAUSING HEADACHE AND SORE THROAT. REMOVED AND REPLACED APU START PURGE VALV E PER AMM 49-31-12-(6597). OPS CHECK GOOD, NO ODORS DETECTED. 2 L 7 2 4F TR A6WE 2007042600157 20070426 00157 EA 2007 4 26 SWIA200718119 1 20070226 A 5520 BOLT CNDAIR CL600 CL6002B19 1900309 EA LT ELEVATOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 866AS 7517 LEFT ELEVATOR TRANSMITTER ARM HAS CORRODED BOLT AND NUT, DISCOVERED AT C-CHECK INSPECTION. REPLACED BOLT AND NUT ON LEF T ELEVATOR TRANSMITTER ARM IAW CRJ200 AMM 20-24-00-910-801. 2 L 7 2 4F RT A21EA 2007042600162 20070426 00162 EA 2007 4 26 SWIA200718124 1 20070226 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 625 S14R CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 866AS 7517 FS 625 BULKHEAD STRINGER 14 HAS CRACKED CLIP ON RIGHT AND LEFT SIDE, DISCOVERED AT C-CHECK INSPECTION. REPLACED FS 625 BULKHEAD CLIPS P/N 601-35012-51 AND P/N 601-35012-52 IAW CRJ200 SRM 51-40-11 AND CRJ200 SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007042600164 20070426 00164 EA 2007 4 26 SWIA200718126 1 20070226 A 5260 AIRSTAIR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 866AS 7517 PAX DOOR STAIR CASE IS CRACKED FORWARD OF STEP 5, DISCOVERED AT C-CHECK INSPECTION. REPLACED PAX DOOR REPAIR PARTS PER CRJ200 REO 601R 52-11-702 REV 'A'. 2 L 7 2 4F RT A21EA 2007042600165 20070426 00165 NM 2007 4 26 AWXA200700500 1 20070410 A 5313 65516982 STRINGER SPLICE BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - FOUND CRACKED STRINGER SPLICE CHANNEL, BS 907, S4R. REPLACED STRINGER SPLICE CHANNEL, BS 907, S4R IAW B737-300 SR M 51-40-02. 2 L 7 2 4F RT A16WE 2007042600166 20070426 00166 NM 2007 4 26 AWXA200700501 1 20070408 A 5754 65C26601180SP SKIN BOEING 737 73733A 1384673 NM NR 6 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - RIGHT WING NR 6 SLAT LOWER SURFACE CRACKED IN TWO LOCATIONS, SS 295.40 - SS 297.40 AND SS 386.75 - SS 389.00. REP AIRED RIGHT WING NR 6 SLAT LOWER SURFACE, SS 295.40 - SS 297.40 AND SS 386.75 - SS 389.00 IAW B737-300 SRM 57-43-01-2R6 FIGURE 201. 2 L 7 2 4F RT A16WE 2007042600170 20070426 00170 EA 2007 4 26 QXEA200700556 1 20070401 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 250 S17R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - LIGHTNING STRIKE DAMAGE AT STRINGER 17R 4.7" FORWARD OF FS 250.00. REPAIRED IAW REO670-53-21-257 AND SRM 51-42 -06. 2 L 7 2 4F RT A21EA 2007042600171 20070426 00171 EA 2007 4 26 QXEA200700559 1 20070330 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 296 S16R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - LIGHTNING STRIKE DAMAGE AT FS 296.00 3.7" DOWN OF STRINGER 16R. REPAIRED IAW REO670-53-21-257 AND SRM 51-42-06 . 2 L 7 2 4F RT A21EA 2007042600175 20070426 00175 WP 2007 4 26 IXXA07SMN110S 1 20070223 A 5512 SKIN DOUG DC8 DC862F 3021972 WP HORIZONTAL STAB CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 70003 2979 45961 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LOWER PANEL HAS CORROSION, STATION XE 221.000 AND X E 272.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. APPLIED SEALANT TO FAYING SURFACE S. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-8 PAGES 17 AND 18, DC8 SRM 55-2-0 PAGE 12, DC8 SRM 55-1-0 PAGE 1, DC8 SRM 51 -1-21,DC8 SR 55-3-1 FIGURE 1 SHEET 1 AND 2 ITEM "S"AND "T", DC8 SRM 51-1-9 TR NUMBER 51-142 DATED 04-05-06, DC8 SRM 51-1 8B, AND DC8 SRM 51-1-11. 2 L 7 4 4F 4A25 2007042600183 20070426 00183 EA 2007 4 26 SWIA200718134 1 20070305 A 7830 TRACK CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 448SW 7678 FOUND CRACK AT LOWER CORNER OF RIGHT THRUST REVERSER TRACK COVER PANEL, DISCOVERED AT C-CHECK INSPECTION. INSTALLED NEW PANELON RIGHT THRUST REVERSER IAW CRJ200 AMM 20-21-00-910-801. 2 L 7 2 4F RT A21EA 2007042600184 20070426 00184 EA 2007 4 26 SWIA200718135 1 20070305 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 448SW 7678 PAX DOOR WEB CRACKED UNDER HANDRAIL SUPPORT BRACKET ON FORWARD SIDE, DISCOVERED ON C-CHECK. INSTALLED BRACKET REPAIR P/ N 601R-52-11-702-1, -2, AND -3 PER REO 601R-52-11-702 PG 1-4. 2 L 7 2 4F RT A21EA 2007042600186 20070426 00186 NM 2007 4 26 DU4R2007085 1 20070406 A 5330 SKIN BOEING 757 757232 1384965 NM BS 600 DENTED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 6709 22811 FOUND 2 DENTS AT BS 600 W/L 197. ACCOMPLISHED PERMANENT REPAIR TO BS 600 W/L 197 BY CUTTING OUT DENTED AREA, FABRICATED AND INSTALLED DOUBLER REPAIR 16 BY 10 FROM 2024-T3 .063 B757 SRM 53-00-01 FIG 201. 2 L 7 2 4F RT A2NM 2007042600187 20070426 00187 NM 2007 4 26 DU4R2007086 1 20070410 A 5311 FRAME BOEING 757 757232 1384965 NM BS 1600 CHAFED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 637DL 23760 FOUND BENT AND CHAFED FRAME IN AFT PIT BS 1600 S-25R - S-26R. REPAIRED BY BLENDING, CUTTING OUT DENTED AREA. FABRICATE D AND INSTALLED DOUBLER REPAIR 14-1/2 BY 2 FROM 2024-T3 .063 B757 SRM 53-00-07 FIG 201. 2 L 7 2 4F RT A2NM 2007042600214 20070426 00214 SO 2007 4 26 RAIA00704052 1 20070417 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO RT OVERWING LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 810HK 145231 POST FLT NR 8090 - IAD - EMERGENCY LIGHT AT RIGHT OVERWING EXIT IDENTIFIER INOP. MAINTENANCE ADJUSTED EMERGENCY EXIT LI GHT AT RIGHT SIDE OVERWING EXIT. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007042600215 20070426 00215 SO 2007 4 26 RAIA00704067 1 20070422 A 3350 BATTERY EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS DISCHARGED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 821HK 145068 PRE FLT NR 5527 - STL - EMERGENCY LIGHTS LEFT ON. MAINTENANCE LET BATTERIES CHARGE. OPS CHECKED OK. 2 L 7 2 4F RT T00011AT 2007042600216 20070426 00216 SO 2007 4 26 RAIA00704061 1 20070419 A 3610 SEAL EMB 145 EMB145LR 3260212 SO DUCT BLOWN A RAIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 03 835HK 145670 FLT NR 8034 - IAD - ENGINE 2 BLEED LEAK CLIMING THRU 15000' PASSENGERS IN REAR OF A/C ON RIGHT SIDE REPORTED LOUD BANG F OLLOWED BY WHOOSHING AIR SOUND. MAINTENANCE REPLACED O-RINGS AND RECONNECTED DUCT COUPLING, OPS NORMAL . 2 L 7 2 4T RT T00011AT 2007042600217 20070426 00217 SO 2007 4 26 RAIA00704064 1 20070420 A 3350 317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 819HK 145062 PRE FLT NR 5576 - STL - AFT FLOOD LIGHT INOP. MAINTENANCE RELAMPED FLOOD LIGHT, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007042600218 20070426 00218 SO 2007 4 26 RAIA00704053 1 20070418 A 5210 UNKNOWN EMB 145 EMB145 3260210 SO PAX DOOR UNKNOWN A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 821HK 145068 PRE FLT NR 5488 - IAD- PAX DOOR WILL NOT OPEN AND APPEARS SLIGHTLY OPEN AND JAMMED. MAINTENANCE CYCLED DOOR HANDLE OPE N AND CLOSED MAIN DOOR FROM THE INSIDE AND OUTSIDE. INSPECTED DOOR ACTUATING AND LOCKING MECHANISM. NO FAULTS DETECTED . 2 L 7 2 4F RT T00011AT 2007042600219 20070426 00219 SO 2007 4 26 RAIA00704065 1 20070421 A 2741 UNKNOWN EMB 145 EMB145LR 3260212 SO DUAL PITCH TRIM UNKNOWN A RAIA O OTHER J WARNING INDICATION DE DESCENT 1 CE 03 811HK 145256 FLT NR 5506 - STL - DUAL PITCH TRIM FAIL IN-FLIGHT. MAINTENANCE RESET A/C POWER PERFORMED GROUND OPS CHECK ON MAIN AND BACK-UP PITCH TRIM SYSTEM. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007042600220 20070426 00220 SO 2007 4 26 RAIA00704062 1 20070419 A 3240 42951 CONTROL UNIT EMB 145 EMB145LR 3260212 SO BRAKES MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 837HK 13340 13340 145255 FLT NR 7890-ORD-OUTBOARD BRAKES INOP MESSAGE ON EICAS. MAINTENANCE REPLACED BRAKE CONTROL UNIT CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007042600221 20070426 00221 SO 2007 4 26 RAIA00704068 1 20070422 A 3231 22250100003 SOLENOID EMB 145 EMB145LR 3260212 SO NLG MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 813HK 18390 18390 145044 FLT NR 5533-STL-NOISE FROM NOSE GEAR. MAINTENANCE REMOVED AND REPLACED LANDING GEAR SOLENOID VALVE. LEAK AND OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007042600235 20070426 00235 SO 2007 4 26 SIMA200711403 1 20070420 A 5320 14525480003 SILL EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 810AE 13175 4800 145525 FOUND AFT CARGO DOOR SILL CORRODED. REMOVED AND REPLACED SILL IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042600236 20070426 00236 NM 2007 4 26 USAA070296 1 20070418 A 5240 ANGLE BOEING 737 737401 1384701 NM SERVICE DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 FOUND CORROSION FWD SVC DOOR Z ANGLE, BS 294-330, S17L. REPLACED Z ANGLE PER SRM 51-40-02; CORROSION LEVEL 2; TASK C53- 107-01, DEFECT SIZE: 36" BY 3". 2 L 7 2 4F RT A16WE 2007042600237 20070426 00237 NM 2007 4 26 USAA070297 1 20070418 A 5320 TRACK BOEING 737 737401 1384701 NM BS 727F CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 FOUND CORROSION STA 727F + 7.5 AT LBL 8.10. INSTALLED REPAIR PARTS PER TR 53-10-06B; CORROSION TASK C53-202-01; LEVEL 2 , DEFECT SIZE: 1/2". 2 L 7 2 4F RT A16WE 2007042600238 20070426 00238 NM 2007 4 26 USAA070298 1 20070418 A 5347 65538446 CARGO TRACK BOEING 737 737401 1384701 NM BS 787-797 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 FOUND CARGO FLOOR TIEDOWN AT FLANGE AND NUTPLATE HOLES, 787-797 RBL 13.80. REMOVED BAD TRACK AND INSTALLED NEW PER SM 5 1-10-02; CORROSION TASK C53-202-01, LEVEL 2, DEFECT SIZE: 1/2". 2 L 7 2 4F RT A16WE 2007042600239 20070426 00239 NM 2007 4 26 USAA070289 1 20070418 A 5322 SHEAR TIE BOEING 737 737401 1384701 NM BS 1156 S5-12L CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 FOUND CORROSION STA 1156 S5L TO S12L, ON TIE STRAP. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-20-01; CORRO SION TASK C53-701-01, LEVEL 2 DEFECT SIZE: 1/2". 2 L 7 2 4F RT A16WE 2007042600240 20070426 00240 NM 2007 4 26 USAA070300 1 20070418 A 5340 65B57839Y30 MOUNT BOEING 737 737401 1384701 NM BS 294 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 FOUND CORROSION, BS 294 + 9, LBL 12. REPLACED WITH NEW MOUNT PER SRM 51-10-02; CORR TASK C53-107-02; LEVEL 2, DEFECT SI ZE: 1/2". 2 L 7 2 4F RT A16WE 2007042600241 20070426 00241 NM 2007 4 26 USAA070288 1 20070418 A 5322 SHEAR TIE BOEING 737 737401 1384701 NM BS 1156 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 FOUND CORROSION TIE STRAP AT STA 1156 S5R TO S12R. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-20-01; CORROS ION TASK C53-701-01; LEVEL 2 DEFECT SIZE: 1/2". 2 L 7 2 4F RT A16WE 2007042600242 20070426 00242 NM 2007 4 26 USAA070302 1 20070418 A 5320 STIFFENER BOEING 737 737401 1384701 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 FOUND CRACK VERTICAL STIFFENER, MLG WW, STA 663.15, LBL 6.15. REMOVED DAMAGE, INSTALLED CHANNEL, ANGLE AND STRAP REPAIR PARTS PER TR 57-10-03B DEFECT SIZE: 1.0". 2 L 7 2 4F RT A16WE 2007042600243 20070426 00243 NM 2007 4 26 USAA070303 1 20070418 A 5512 SKIN BOEING 737 7373B7 1384580 NM HORIZONTAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 529AU 24411 FOUND CRACK LEFT STAB LOWER SKIN JUST FWD OF FASTENERS IN REAR SPAR NEAR STAB STA 118. FAB'D AND INSTALLED FILLER AND D OUBLER PER TR 55-10-07, DEFECT SIZE: 1.2". 2 L 7 2 4F RT A16WE 2007042600244 20070426 00244 NM 2007 4 26 USAA070304 1 20070418 A 5311 FRAME BOEING 737 737401 1384701 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 FOUND CRACK STA 440 RT SIDE FRAME 1" BELOW TOP PSU ATTACH POINT. TRIMMED OUT FRAME, INSTALLED REPAIR DOUBLERS AND FILLE RS PER TR 53-10-20E, DEFECT SIZE: 1/4" (2 EA). 2 L 7 2 4F RT A16WE 2007042700003 20070427 00003 CE 2007 4 27 AMWA84156 1 20070423 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER DISCHARGED A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 133YV 22342 186 UE133 BATT CHARGE ANNUN ILLUM IN FLT. NO INCIDENTS, ACFT CONTINUED TO DESTINATION. REMOVED AND REPLACED BATTERY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007042700007 20070427 00007 NM 2007 4 27 QXEA200700673 1 20070417 A 5310 DOOR FRAME DHAV DHC8 DHC8202 2809007 NM EMERGENCY EXIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - RIGHT EMERGENCY EXIT APERTURE, ALL 4 STOPS ON FUSELAGE HAVE FRETTING CORROSION. REPAIRED IAW RD8-53-126. 2 H 7 2 4T RT A13NM 2007042700008 20070427 00008 NM 2007 4 27 QXEA200700666 1 20070413 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM BS 600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - FOUND CORROSION ON THE LOWER "L" BRACKET FOR THE CARGO FLOOR RISER AT STATION 600, 21" LEFT OUTBOARD AROUND THE NUTPLATE. REPAIRED IAW SRM 51-20-11, 51-40-11. 2 H 7 2 4T RT A13NM 2007042700009 20070427 00009 NM 2007 4 27 QXEA200700669 1 20070411 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 531 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - FOUND SUSPECT DENT IN RIGHT SIDE OF FUSELAGE EXTERIOR SKIN AT STATION X531.500, Z120.000. REPAIRED IAW RD8-53- 5384 AND RD8-53-9560. 2 H 7 2 4T RT A13NM 2007042700010 20070427 00010 NM 2007 4 27 QXEA200700668 1 20070414 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAPS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - FOUND LEFT FLAP TRACK NR 4 HAS SPOTS OF CORROSION ON MOST SURFACES, ESPECIALLY IN THE ROLLER TRACK AREA. REPAI RED IAW RD8-57-988. 2 H 7 2 4T RT A13NM 2007042700011 20070427 00011 NM 2007 4 27 QXEA200700671 1 20070413 A 5340 SUPPORT ANGLE DHAV DHC8 DHC8202 2809007 NM LAVATORY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX -LAVATORY COMPARTMENT SUPPORT 90 DEGREE ANGLE INSIDE FUSELAGE HAS AREAS OF CORROSION ALONG TOP AND INSIDE EDGE, BETWEEN FS X199 AND X222 AT Z102. REPAIRED IAW SRM 51-20-11 AND RD8-53-9563. 2 H 7 2 4T RT A13NM 2007042700013 20070427 00013 NM 2007 4 27 QXEA200700667 1 20070414 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAPS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - LEFT FLAP TRACK NR 5 HAS SURFACE CORROSION ON THE UNDERSIDE OF THE TOP OUTBOARD TRACK JUST FORWARD OF THE ROLLE R CONTACT AREA AND ON THE FORWARD PORTION OF THE OUTBOARD SIDE ROLLER TRACK. REPAIRED IAW RD8-57-989. 2 H 7 2 4T RT A13NM 2007042700014 20070427 00014 NM 2007 4 27 QXEA200700674 1 20070411 A 5310 DOOR FRAME DHAV DHC8 DHC8202 2809007 NM EMERGENCY EXIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - RIGHT FORWARD EMERGENCY EXIT HAS 2 CHAFE MARKS AT BOTTOM OF DOOR FRAME 5" OF CENTER ON EACH SIDE. REPAIRED IAW SRM 51-40-11, 51-40-00. 2 H 7 2 4T RT A13NM 2007042700020 20070427 00020 EA 2007 4 27 TRAX200700537 1 20070417 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA BS 640 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 835AS 7258 FOUND RT FS 640 INNER BONDED SKIN DOUBLER CRACKED AT STR 9. COMPLIED WITH EC/TC ASA REO 601R-53-61-506. RII-5001388. 2 L 7 2 4F RT A21EA 2007042700024 20070427 00024 NM 2007 4 27 ASAA0771607 1 20070422 A 5753 113A26721 FLAP TRACK BOEING 737 737790 13844CN NM TE FLAPS WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 LT INBD AFT FLAP OTBD TRACK HAS WORN PLATING REPLACED IAW AMM 27 51 16. 2 L 7 2 4F RT A16WE 2007042700025 20070427 00025 NM 2007 4 27 ASAA0771603 1 20070422 A 5740 113A41002 FITTING BOEING 737 737790 13844CN NM SPOILER ACTUATOR GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 NR 12 SPOILER LOCK GOUGED INTO SPOILER ACTUATOR FITTING. REPLACED IAW AMM 27 62 91. 2 L 7 2 4F RT A16WE 2007042700026 20070427 00026 NM 2007 4 27 ASAA0771610 1 20070422 A 5315 147A56766 FLOORBEAM BOEING 737 737790 13844CN NM BS 950 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 FLOORBEAM AT STA 950 IS CORRODED REPAIRED IAW 51 40 02. 2 L 7 2 4F RT A16WE 2007042700027 20070427 00027 NM 2007 4 27 ASAA0771604 1 20070422 A 5315 147A55068 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 FLOORBEAM AT STA 986.5 IS CORRODED AT FASTENER HOLES REPAIRED IAW EA 5310 02717. 2 L 7 2 4F RT A16WE 2007042700028 20070427 00028 NM 2007 4 27 ASAA0771609 1 20070422 A 5320 147A57104 SUPPORT BOEING 737 737790 13844CN NM BS 990-1016 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 EXTRUSION AT STA 990 IS CORRODED AT FASTENER HOLES REPAIRED IAW SRM 51 40 02. 2 L 7 2 4F RT A16WE 2007042700029 20070427 00029 NM 2007 4 27 QXEA200700655 1 20070410 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 427 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - DENT IN LEFT EXTERIOR FUSELAGE AT STATION 427 AND STRINGER 26L. REPAIRED IAW RD8-53-5384. 2 H 7 2 4T RT A13NM 2007042700030 20070427 00030 NM 2007 4 27 QXEA200700656 1 20070410 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 302 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - DENT IN UPPER FUSELAGE SKIN AT STATION 302.400, 5" RIGHT OF CENTERLINE. REPAIRED IAW RD8-53-5384. 2 H 7 2 4T RT A13NM 2007042700031 20070427 00031 NM 2007 4 27 QXEA200700658 1 20070410 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 599 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - DENT PROTRUDING OUTWARDS IN FUSELAGE SKIN AT STATION 599.0 BETWEEN STRINGER 24R AND 25R. REPAIRED IAW RD8-53-5 384. 2 H 7 2 4T RT A13NM 2007042700032 20070427 00032 NM 2007 4 27 QXEA200700657 1 20070412 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 300 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - DENT IN UPPER FUSELAGE AT STATION 300.00 ON LEFT SIDE ABOVE ICE SHIELD. REPAIRED IAW RD8-53-5384. 2 H 7 2 4T RT A13NM 2007042700033 20070427 00033 NM 2007 4 27 QXEA200700660 1 20070412 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 428-525 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - CABIN SEAT TRACK NR 8 HAS MINOR SCRATCHES AT STATIONS X428, X436 - X456, X467 - X487, X501 - X525. REPAIRED IA W RD8-53-1339 AND SRM 51-40-00, 51-40-11. 2 H 7 2 4T RT A13NM 2007042700034 20070427 00034 NM 2007 4 27 QXEA200700661 1 20070413 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 516 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - FOUND CABIN SEAT TRACK NR 12 HAS CORROSION AT STATION X516. REPAIRED IAW RD8-53-1342. 2 H 7 2 4T RT A13NM 2007042700035 20070427 00035 NM 2007 4 27 QXEA200700659 1 20070412 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 580 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - CABIN SEAT TRACK NR 9 HAS CORROSION AT STATION X580 CENTER FLOORBOARD ATTACH NUTPLATE. REPAIRED IAW RD8-53-784 AND SRM 51-40-00, 51-40-11. 2 H 7 2 4T RT A13NM 2007042700036 20070427 00036 NM 2007 4 27 QXEA200700662 1 20070412 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 543-547 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - FOUND SEAT TRACK NR 6 HAS CORROSION BETWEEN STATION 543 AND 547. REPAIRED IAW RD8-53-4936 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007042700037 20070427 00037 NM 2007 4 27 QXEA200700663 1 20070413 A 5310 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSLEAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - FOUND CORROSION AROUND THE APERTURE FOR PANEL 144HZ. REPAIRED IAW SRM 51-20-11. 2 H 7 2 4T RT A13NM 2007042700038 20070427 00038 NM 2007 4 27 QXEA200700664 1 20070413 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 221 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - FOUND CABIN SEAT TRACK NR 7 HAS CORROSION AT STATION X221. REPAIRED IAW RD8-53-4698 AND SRM 51-40-11, 51-40-00 . 2 H 7 2 4T RT A13NM 2007042700039 20070427 00039 NM 2007 4 27 HNAA0700072 1 20070422 A 3350 AML21GBA2CD HOUSING DHAV DHC8 DHC8102 2809003 NM LIGHT SWITCH UNKNOWN A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 814EX 37521 70 318 ATTENDANT'S EMERGENCY LIGHT SWITCH YELLOW LIGHT DOES NOT COME ON. REMOVED AND REPLACED 3351-52. 2 H 7 2 4T RT A13NM 2007042700040 20070427 00040 WP 2007 4 27 07FDEA01593 1 20070425 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1159-1216 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 BARREL SECTION STA Y=1159 TO Y=1216 LONG 48L TO 47R FOUND CORROSION ON SKIN, SHEAR TIES, LOMGERONS, RIVETS, DRAIN HOLES AND AROUND INLET DUCT REPAIR IAW SRM 53-20-00 FIG 13 VOL1. 2 L 7 3 4F A22WE 2007042700041 20070427 00041 WP 2007 4 27 07FDEA01594 1 20070425 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP BS 1257-1278 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 BARREL SECTION STA Y=1257 TO Y=1278 LONG 47L TO 47R FOUND CORROSION ON SKIN, SHEAR TIES, LONGERONS, RIVETS, DRAIN HOLES AND AROUND INLET DUCT REPAIR IAW SRM 53-20-00 FIG 13. 2 L 7 3 4F RT A22WE 2007042700042 20070427 00042 EA 2007 4 27 TRAX200700536 1 20070417 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 874AS 7551 FA'S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007042700043 20070427 00043 EA 2007 4 27 TRAX200700538 1 20070418 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 709EV 10068 AFT MOST CEILING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007042700044 20070427 00044 EA 2007 4 27 TRAX200700539 1 20070418 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 872AS 7542 CREW REPORTS PAX DOOR HARD TO OPEN. 2 L 7 2 4F RT A21EA 2007042700045 20070427 00045 EA 2007 4 27 TRAX200700540 1 20070418 A 5210 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 659CA 10153 PAX DOOR AFT DRAG ANGLE CRACKED. [5-1-07] CUTOUT DAMAGED SECTION OF PAX DOOR AFT DRAG ANGLE AS REQUIRED. FABRICATED SPL ICE ANGLE, AND SPLICE DOUBLERS. COMPLIED WITH LPI OF PAX DOOR AFT GRAG ANGLE CUTLINES IAW REO 670-52-11-072. NO DEFECT S NOTED. 2 L 7 2 4F RT A21EA 2007042700046 20070427 00046 EA 2007 4 27 TRAX200700541 1 20070418 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 659CA 10153 FLOOR ANGLE AT PAX DOOR ENTRANCE IS CORRODED. REMOVED FLOOR ANGLE AT PAX DOOR ENTRANCE. REPAIRED IAW SRM. 2 L 7 2 4F RT A21EA 2007042700047 20070427 00047 EA 2007 4 27 TRAX200700542 1 20070418 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 785 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 659CA 10153 CORROSION ON LEFT SIDE SEAT RAIL IMMEDIATELY AFT OF EMERGENCY EXIT FS 785. 2 L 7 2 4F RT A21EA 2007042700048 20070427 00048 EA 2007 4 27 TRAX200700543 1 20070418 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 785 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 659CA 10153 FOUND CORROSION ON RT SIDE SEAT RAIL IMMEDIATELY AFT OF EMERGENCY EXIT, FS 785. 2 L 7 2 4F RT A21EA 2007042600031 20070426 00031 NM 2007 4 26 CALA0700190 1 20070421 A 5414 301A31091 PLATE BOEING 737 7373T0 1384582 NM NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19357 23841 NR 1 ENGINE PYLON PANEL OPENING FOR PANEL 5724 CRACKED. REPAIRED IAW ECRA 5431-01034. 2 L 7 2 4F RT A16WE 2007042600049 20070426 00049 NM 2007 4 26 SWAA071981 1 20070423 A 2782 65445517 ACTUATOR BOEING 737 7373H4 1384600 NM L/E SLAT BYPASSING A SWAA K NONE O OTHER AP APPROACH 1 SW 29 632SW 27707 DECLARED EMERGENCY. ON APPROACH L/E SLATS/FLAPS WOULD NOT EXTEND FOR LANDING. EXTENDED FLAPS PER ALTERNATE METHOD. IN SPECTED AND FOUND LEFT INBOARD KRUEGER FLAP ACTUATOR BYPASSING. REMOVED AND REPLACED LEFT INBOARD ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2007042600050 20070426 00050 NM 2007 4 26 SWAA072003 1 20070423 A 5330 6545772 SKIN BOEING 737 7377H4 1384404 NM FUSELAGE CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 745SW 29491 DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE SKIN CHAFED UNDER DORSAL FIN BS 925. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007042600051 20070426 00051 NM 2007 4 26 SWAA071999 1 20070423 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 830, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007042600053 20070426 00053 NM 2007 4 26 SWAA071998 1 20070423 A 5311 6545805 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007042600054 20070426 00054 NM 2007 4 26 SWAA072009 1 20070423 A 5312 6545819 PRESSURE PANEL BOEING 737 7373T5 1384608 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 22Y CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT BS 259, RBL 7.75 TO LBL 7.75. REPAIRED CEILING PANEL PER ACO. 2 L 7 2 4F RT A16WE 2007042600079 20070426 00079 NM 2007 4 26 USAA070293 1 20070418 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 BS 727B S-8R HAS CRACK. REPAIRED PER TR 53-10-20E, DEFECT SIZE: .250 INCH. 2 L 7 2 4F RT A16WE 2007042600094 20070426 00094 WP 2007 4 26 07FDEA01533 1 20070422 A 5753 SKIN DOUG MD10 MD1010F 3022112 WP LT WING TE FLAP GOUGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 68050 47804 LT WING O/B FLAP O/B LOWER SKIN GOUGED ON INTERIOR SIDE. CUT OUT DAMAGE REF; DC/MD10-10 SRM 57-10-00 FIG 85 VOL 1. FAB BED REPAIR DOUBLER. [SUP 04-30-07] REF; DC/MD10 -10 SRM 57-10-00 VOL 1. ALODINED AND PRIMED REF; DC/MD10-10 SRM 51-21 -01 VOL 11. INSTALLED DOUBLER REF; DC/MD10-10 SRM 51-35-01, VOL 11. TOUCH UP PAINT REF; DC/MD10-10 SRM 51-21-02 VOL 11. 2 L 7 3 4F RT A22WE 2007042600095 20070426 00095 WP 2007 4 26 07FDEA01534 1 20070422 A 5753 SKIN DOUG MD10 MD1010F 3022112 WP LT WING TE FLAP GOUGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 68050 47804 LT WING O/B FLAP O/B LOWER SKIN GOUGED ON INTERIOR SIDE. CUT OUT DAMAGED PART REF; DC/MD10-10 SRM 57-10-00 FIG 85 VOL 1 . FABBED DOUBLER REF; DC/MD10-10 SRM 57-10-00 VOL1. ALODINED AND PRIMED REF; DC/MD10-10 SRM 51-21-01 VOL 11. INSTALLE D DOUBLER REF; DC/MD10-10 SRM 51-35-01 VOL 11. TOUCH UP PAINT REF; DC/MD10-10 SRM 51-21-02 VOL11. 2 L 7 3 4F RT A22WE 2007042600098 20070426 00098 EU 2007 4 26 07FDEA01537 1 20070423 A 5730 SKIN AIRBUS 310 A310324 3930206 EU RT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 ELONGATED HOLES ON PYLON SUPPORT BRACKET AND WING BOTTOM SKIN, RIB 8-9 RT. REPAIR PERFORMED BY OVERSIZING AND INSTALLIN G BUSHES IAW DRW R572-49184, APPROVED BY EA 6-5720-99169 AND RAS/BAE/1002502/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007042600104 20070426 00104 NM 2007 4 26 07FDEA01543 1 20070423 A 5713 STRINGER DOUG MD11 MD11 3023602 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 CRACK FOUND AT STRINGER END 10R (XORS 760), APPROX 12.5" LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. [SUP 05-11-0 7] CRACK AT STRINGER END 10R (XORS 760), APPROX 12.5" LENGTH ON RIGHT HAND WING TANK REPAIRED AS PER SRM 57-20-00 F IGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007042600120 20070426 00120 NM 2007 4 26 AALA20070676 1 20070411 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 959AN 30828 TUL - EMERGENCY LIGHTS IN AFT CABIN CEILING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT CABIN CEILIN G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007042600140 20070426 00140 NM 2007 4 26 NWAA071426306 1 20070312 A 5322 SHEAR TIE BOEING 747 747451 1384940 NM BS 1160 DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 666US 23821 DURING "M" CHECK, FOUND TENSION TIE WITH ELONGATED FASTENER HOLE AT BS 1160 LBL 59. REPAIRED PER EA 63-209221. 2 L 7 4 4F RT A20WE 2007042600151 20070426 00151 NM 2007 4 26 F3LA200700078 1 20070411 A 2571 MOUNT AIRBUS A319 A319111 3930336 NM BATTERY RACK CHAFED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED FRETTING ON BATTERY RACK MOUNTS. REPLACED (4) MOUNT FITTINGS AT FR 10 IAW EA NR A9-53R-10649. 2 L 7 2 4F RT A28NM 2007042600179 20070426 00179 EA 2007 4 26 SWIA200718130 1 20070305 A 5230 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 448SW 7678 CARGO DOOR FORWARD TRACK, BOTTOM SUPPORT BRACKET IS CRACKED, DISCOVERED ON C-CHECK INSPECTION. REPLACED CRACKED CARGO D OOR FORWARD TRACK BOTTOM SUPPORT BRACKET PER CRJ200 SRM 51-62-06 PG 11 AND 18. 2 L 7 2 4F RT A21EA 2007042600182 20070426 00182 EA 2007 4 26 SWIA200718133 1 20070305 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 448SW 7678 FS 280 BULKHEAD LBL9 HAS CRACKED CLIP ON OUTBOARD SIDE, DISCOVERED ON C-CHECK INSPECTION. REPLACED CLIP AT STATION 280 LBL9 P/N 601R31113-57 IAW CRJ200 SRM 51-42-20 PGS 23-24. 2 L 7 2 4F RT A21EA 2007042600222 20070426 00222 SO 2007 4 26 RAIA00704054 1 20070418 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 812HK 145373 POST FLT NR 5524 - STL - EMERGENCY LIGHT BULB ON STRIP AISLE FLOOD LIGHT IS INOP. MAINTENANCE RESEATED LIGHT BULB. 2 L 7 2 4T RT T00011AT 2007042600223 20070426 00223 GL 2007 4 26 RAIA00704063 2 20070420 A 7261 4252070 CARBON SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 GENERATOR LEAKING A RAIA B A EMER. DESCENT UNSCHED LANDING K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CE 03 832HK 145771 312510 FLT NR 8012-ORD-ENGINE NR 1 LOW OIL PRESSURE EICAS MESSAGE ENGINE NR 1 QUANITY LOW. MAINTENANCE REMOVED AND REPLACED NR 1 GENERATOR CARBON SEAL. NO LEAKS NOTED AT THIS TIME. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007042600224 20070426 00224 SO 2007 4 26 RAIA00704051 1 20070417 A 5210 DOOR EMB 145 EMB145 3260210 SO PAX DOOR LACK OF LUBE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 809HK 145187 POST FLT NR 5524-STL-PAX DOOR DIFFICULT TO OPEN. MAINTENANCE LUBED DOOR FRAME AND INSPECTED MAIN PAX DOOR . 2 L 7 2 4F RT T00011AT 2007042600225 20070426 00225 EU 2007 4 26 AWXA200700514 1 20070417 A 5210 D5311245600100 FITTING AIRBUS 320 A320231 3930325 EU ZONE 800 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 SAL - R1 DOOR SUPPORT ARM UPPER FITTING BEARING ATTACHMENT HOLE WORN AND BEARING IS MIGRATING. REPLACED R1 DOOR SUPPORT ARM UPPER FITTING IAW A320 AMM 52-11-12. 2 L 7 2 4F RT A28NM 2007042600226 20070426 00226 EU 2007 4 26 AWXA200700515 1 20070411 A 5321 D5357180500300 FLOOR PANEL AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 SAL - FOUND CORROSION ON CABIN FLOOR PANEL 262 FF, FR 66 - FR 68, -Y1292 TO -Y 1732. REPLACED CABIN FLOOR PANEL 262 FF, FR 66 - FR 68, -Y1292 TO -Y 1732 IAW A320 SRM 51-72-11 AND AWA TASK CARD C1C53303. 2 L 7 2 4F RT A28NM 2007042600227 20070426 00227 EU 2007 4 26 AWXA200700516 1 20070411 A 5321 D5367005000200 FLOOR PANEL AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 SAL - FOUND CORROSION ON CABIN FLOOR PANEL 261 FF, FR 66 - FR 68, +Y1292 TO +Y1732. REPLACED CABIN FLOOR PANEL 261 FF, FR 66 - FR 68, +Y1292 TO +Y1732 IAW A320 SRM 51-72-11 AND AWA TASK CARD C1C53303. 2 L 7 2 4F RT A28NM 2007042600228 20070426 00228 EU 2007 4 26 AWXA200700517 1 20070411 A 5321 D5361014900100 FLOOR PANEL AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 SAL - FOUND CORROSION ON CABIN FLOOR PANEL 222 FF, FR 16 - FR 20, -Y1292 TO -Y1732. REPLACED CABIN FLOOR PANEL 222 FF, FR 16 - FR 20, -Y1292 TO -Y1732 IAW A320 SRM 51-72-11 AND AWA TASK CARD C1C53302. 2 L 7 2 4F RT A28NM 2007042600229 20070426 00229 SO 2007 4 26 SIMA200711405 1 20070420 A 5347 14532605015 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 810AE 13175 4800 145525 RIGHT OUTBOARD SEAT TRACK CORRODED AT FRAME 36 TO 46. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHINCAL NOTICE 53-110-R2. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT T00011AT 2007042600230 20070426 00230 SO 2007 4 26 SIMA200711406 1 20070420 A 5347 14232606017 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 810AE 13175 4800 145525 LEFT OUTBOARD SEAT TRACK CORRODED AT FRAME 46 TO 52. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL ORDER 53-110-R2. RETURNED AIRCRAFT TO SERVICE 2 L 7 2 4F RT T00011AT 2007042600231 20070426 00231 GL 2007 4 26 SIMA200711401 2 20070421 A 7200 ENGINE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL NR 1 SHUTDOWN A SIMA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 802AE 145471 CAE311899 NUMBER ONE ENGINE SHUTDOWN UNCOMMANDED ON GROUND, DOWN LOADED FADEC AND CMC DISCREPANCIES LABELS AND FOUND NO FAULT MESS AGES. INSPECTED INLET AND EXHAUST WITH NO DISCREPANCIES NOTED, GROUND RUN NUMBER ONE ENGINE IAW ROLLS ROYCE MM, CHAPTER 72-00-00 WITH NO DISCREPANCIES. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007042600232 20070426 00232 SO 2007 4 26 SIMA200711407 1 20070420 A 5320 14522461011 DOUBLER EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 810AE 13175 4800 145525 RIGHT HAT BEAM DOUBLER CORRODED AT FRAME 22. REMOVED AND REPLACED DOUBLER AT FRAME 22. REMOVED AND REPLACED DOUBLER IA W EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042600233 20070426 00233 GL 2007 4 26 SIMA200711402 2 20070421 A 7200 AE3007A1 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL ZONE 400 VIBRATION A SIMA O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SW 21 639AE 9709 2734 145182 CAE312313 ENGINE TWO ON START VIBRATIONS INCREASED BETWEEN 35 TO 40 PERCENT, N1 REMAIN IN GREEN BAND. REMOVED AND REPLACED NUMBER TWO ENGINE IAW AMERICAN EAGLE WORK CARD. OPERATIONAL AND LEAK CHECK GOOD. RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007042600234 20070426 00234 SO 2007 4 26 SIMA200711404 1 20070420 A 5310 14522460009 GUSSET EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 810AE 13175 4800 145525 FOUND GUSSET AT FRAME 20 CORRODED. REMOVED AND REPLACED GUSSET IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007042700001 20070427 00001 NM 2007 4 27 KCSA071162 1 20070421 A 3350 70031230 LIGHT BOEING 747 747209F 1384800 NM PWA JT9 JT9D7R4G2 52054 NE EMERGENCY EXIT INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 704CK 22299 EMERGENCY EXIT SIGN ABOVE RT UPPER DECK ESCAPE DOOR IS INOP. 2 L 7 4 4F 4 F RT A20WE E3NE 2007042700002 20070427 00002 NM 2007 4 27 C1HA200779001 1 20070417 A 3260 H1010153 SWITCH BOEING 727 727225 1384077 NM MLG MALFUNCTIONED A C1HA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 679MG 22557 AFTER EXTENDING LANDING GEAR THE LT AND RT MAIN GEAR GREEN LTS ILLUMINATED AND THE RED NOSE GEAR LT REMAINED ILLUMINATED WITHOUT A GREEN INDICATION. AFTER 2 TO 3 MINUTES THE NOSE GEAR GREEN LIGHT ILLUMINATED AND THE RED LT EXTINGUISHED. R EPLACED NOSE GEAR LOCK AND POSITION SWITCHES REF 32-61-71. OPS CHECK GOOD, LIGHT OPERATIONS NORMAL. 2 L 7 3 4F A3WE 2007042700006 20070427 00006 NM 2007 4 27 QXEA200700672 1 20070417 A 5310 DOOR FRAME DHAV DHC8 DHC8202 2809007 NM EMERGENCY EXIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - FOUND LEFT EMERGENCY EXIT APERTURE, ALL 4 STOPS ON FUSELAGE HAVE FRETTING CORROSION. REPAIRED IAW RD8-53-126. 2 H 7 2 4T RT A13NM 2007042700017 20070427 00017 EU 2007 4 27 BMAC07002 1 20070423 A 3260 BULB BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110UG 01514 WP MLG INDICATOR WRONG PART A B16A O OTHER W P INADEQUATE Q C NO WARNING INDICATION AP APPROACH 1 SO 35 530PA 732 DURING APPROACH PHASE AT BED UNABLE TO GET GREEN LIGHT ON RT MAIN AND NOSE. SWAPPED BULBS AND FINALLY GOT GREEN LIGHT ON RT MAIN. STILL NO RED OR GREEN LIGHT ON NOSE. PROCEEDED WITH CHECK LIST AND LANDED UNEVENTFULLY. INSTALLED GEAR LOCK PI NS. MAINT FOUND INCORRECT BULB INSTALLED, AND REPLACED ALL 12 BULBS IN THE INDICATOR, OPS CHECKED GOOD. PERFORMED GEAR S WINGS AND OPS CHECKED GOOD. 2 L 7 2 4T 4 T RT A21EU E4WE 2007042700018 20070427 00018 EU 2007 4 27 MALA070056 1 20070425 A 5753 STRUCTURE SAAB SF340 340B 7860101 EU TE FLAPS DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436XJ 340B436 THE RT FLAP, P/N 7257800-574, S/N 1326, IS DAMAGED APPROXIMATELY 4.0" FROM THE AFT EDGE AND 2.6' FROM THE INBOARD END OF THE PART. THE DAMAGE HAS BEEN REPAIRED IAW MESABA EO NR S57060. REF: EAMS WORK ORDER 216293 TASK 6501. 2 L 7 2 4T RT A52EU 2007042700021 20070427 00021 NM 2007 4 27 ASAA0771608 1 20070422 A 5321 141A5810175 FLOORBOARD BOEING 737 737790 13844CN NM LAVATORY DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 FWD LAV FLOOR BOARD DAMAGED AND DISBONDED REPAIRED IAW AMM 25 00 00. 2 L 7 2 4F RT A16WE 2007042700022 20070427 00022 NM 2007 4 27 ASAA0771605 1 20070422 A 5753 113A26721 FLAP TRACK BOEING 737 737790 13844CN NM TE FLAPS WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 RT INBD AFT FLAP TRACK HAS WORN PLATING REPLACED IAW AMM 27 51 16. 2 L 7 2 4F RT A16WE 2007042700023 20070427 00023 NM 2007 4 27 ASAA0771606 1 20070422 A 5753 113A26721 FLAP TRACK BOEING 737 737790 13844CN NM TE FLAPS WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 RT INBD AFT FLAP OTBD TRACK HAS AREA OF WORN PLATING REPLACED FLAP TRACK IAW AMM 27 51 16. 2 L 7 2 4F RT A16WE 2007042700049 20070427 00049 EA 2007 4 27 TRAX200700544 1 20070419 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 903EV 7621 FOUND EMERGENCY LIGHT ON CEILING AT ROW 5 IS INOP. 2 L 7 2 4F RT A21EA 2007042700050 20070427 00050 EA 2007 4 27 TRAX200700545 1 20070417 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS WARNING LIGHT A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 824AS 7203 LEVEL AT 3,000' IN PATTERN AT MDT AT 200 KNOTS, RECEIVED FLAPS FAIL MSG AT 0 DEG, FOLLOWED QRH AND LANDED IN MDT. "FLAP HANDLE WAS NOT MOVED OUT OF 0 DEG OR TOUCHED". EMERGENCY EQUIPMENT ON STANDBY AS A PRECAUTION. 2 L 7 2 4F RT A21EA 2007042700051 20070427 00051 EA 2007 4 27 TRAX200700546 1 20070417 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 824AS 7203 FLAPS FAIL AT ZERO OUT OF 20,000 FT, WITHOUT TOUCHING FLAPS AT ALL. LANDING IN SBN NO PROBLEM, VERY SOFT LANDING. EMER GENCY EQUIPMENT ON STANDBY AS A PRECAUTION. 2 L 7 2 4F RT A21EA 2007042700052 20070427 00052 EU 2007 4 27 MALA070051 1 20070312 A 3610 TUBE SAAB SF340 340B 7860101 EU BLEED AIR SYS LEAKING A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 407XJ 340B407 RIGHT BLEED AIR LEAK CAUTION LIGHT ILLUMINATED. CLOSED BLEED VALVE AND BLEED AIR LEAK CAUTION LIGHT WENT OUT. CND PROB LEM. LEAK CHECK RIGHT BLEED SYSTEM. NO LEAKS FOUND. PER ENGINEERING REQUEST, REPLACED RIGHT BLEED TUBE. OPS AND LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 2007042700053 20070427 00053 EU 2007 4 27 2007UALA01144 1 20070413 A 5100 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE VIBRATION A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 428UA 523 DURING CLIMB-OUT, AIRCRAFT VIBRATION VARYING SPEEDS AND ALTITUDES. CRUISE SMOOTH. [SUP 06-06-07] REPLACED ALL THREE RUDDER ACTUATOR ROD ENDS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007042700054 20070427 00054 EU 2007 4 27 2007UALA01145 1 20070413 A 3260 PROXIMITY SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG CONTAMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 431UA 571 RTFL UNDER AMBER ALERT DUE TO NLG NOT RETRACTING. [SUP 06-06-07] INITIALLY REPLACED THE NR 2 LGCIU, BUT FURTHER TROUBL ESHOOTING FOUND THE NOSE LANDING GEAR PROXIMITY SENSORS TO BE COVERED IN GREASE. CLEANED PROXIMITY SENSORS 12GA, 18GA, 3 0GA AND 31GA. 2 L 7 2 4F 4 F RT A28NM E40NE 2007042700055 20070427 00055 NM 2007 4 27 2007UALA01146 1 20070414 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 960-987 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 AFT CABIN FLOOR STRUCTURE AT DOOR CUT-OUT 2L, INNER CREASE BEAM ANGLE HAS CORROSION IN SPOTS ON UPPER SURFACE AT BS 960- 987 LBL50 40-50 WL 209. [SUP 5-1-07] MAJOR REPAIR: INSTALLED NEW CREASE BEAM ANGLE PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2007042700056 20070427 00056 NM 2007 4 27 2007UALA01147 1 20070414 A 5512 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZONTAL STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 DENT IN RT HORIZONTAL STABILIZER LEADING EDGE APPROX SIX RIVET ROWS FROM FUSELAGE. [SUP 5-10-07] MAJOR REPAIR: INSTALL ED DOUBLER REPAIR PER SRM 55-10-01 PG 201-203 REPAIR NR 2. 2 L 7 2 4F 4 F RT A16WE E2GL 2007042700057 20070427 00057 NM 2007 4 27 2007UALA01148 1 20070414 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 927 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 INNER SURFACE OF FUSELAGE SKIN CRACKED ON EDGE OF BONDED DOUBLER AFT OF STA 927 FRAME BTWN STR 22R AND 23R. [SUP 05-01- 07] MAJOR REPAIR: INSTALLED EXTERNAL SKIN DOUBLER REPAIR PER SRM 53-00-01 REPAIR 31 DETAIL XI. 2 L 7 2 4F 4 F RT A16WE E2GL 2007042700058 20070427 00058 NM 2007 4 27 2007UALA01149 1 20070414 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 278-279 GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 UPPER EXTERNAL FUSELAGE SKIN GOUGED FROM APPARENT JET WAY CONTACT BS 278-279 STR 3L. [SUP 05-01-07] MAJOR REPAIR: INS TALLED EXTERNAL DOULBER-TRIPLER REPAIR PER SRM 53-00-01 REPAIR 31. 2 L 7 2 4F 4 F RT A16WE E2GL 2007042700059 20070427 00059 NM 2007 4 27 2007UALA01150 1 20070414 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 695 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 LEFT WHEEL WELL BS 695 FRAME CHORD ANGLE CRACKED INNER RADIUS AREA. [SUP 05-01-07] MAJOR REPAIR: REPLACED INNER FRAME CHORD PER MM 53-10-98 PG601. 2 L 7 2 4F 4 F RT A16WE E2GL 2007043000002 20070430 00002 NM 2007 4 30 ABXA070126 1 20070405 A 5230 140T26033 BEAM BOEING 767 767281 1385109 NM CARGO DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 794AX 23144 FORWARD LOWER CARGO DOOR BEAM WAS CORRODED AT THE INSULATION BLANKET NUT PLATES. REPAIRED FORWARD LOWER CARGO DOOR BEAM IAW B767 MM. 2 L 7 2 4F RT A1NM 2007043000004 20070430 00004 WP 2007 4 30 ABXA070117 1 20070423 A 5310 99115055 WINDOW FRAME DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 DURING COCKPIT WINDOW MOD, EA 53300036, FOUND FRAME CRACKED. REPAIRED IAW DC9 SRM 53-03, FIGURE 34. 2 L 7 2 4F A6WE 2007043000005 20070430 00005 NE 2007 4 30 KCSA07041 2 20070424 A 7200 FILTER BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE EVC CONTAMINATED A KCSA O OTHER R Y J PARTIAL RPM/PWR LOSS ENGINE STOPPAGE WARNING INDICATION DE DESCENT 1 GL 23 716CK 19753 AT 8000', IDLE THRUST EGT NR 4 AT 874 DEGREES CELSIUS AND N2 AT 43 PERCENT. ALL OTHER INSTRUMENTS NORMAL. ACCOMPLISHED ENGINE STALL IN FLT (ABNORMAL EGT) CHECKLISTS. ATTEMPTED RESTART WITH RAPID RESTART PROCEDURE QRH-69. RESULTED IN DUP LICATE INDICATIONS. ACCOMPLISHED QRH-79, AGAIN. RESTART SECOND ATTEMPT USING QRH-69, SUCCESSFUL. DURING SAME PERIOD, NR 1 ENGINE EXPERIENCED SAME INDICATIONS, PERFORMED QRH-79. DECISION MADE TO NOT ATTEMPT A RESTART. COMPLETED QRH-67. LANDED SAFELY. WINDMILL OIL PRESSURE UP 5 PSI. PERFORMED WINDMILL INSPECTION IAW B747 MM 72-00-00. NO DEFECTS NOTED. PERFORMED LEAK CHECK OF FILTER AND CHIP DETECTORS IAW B747 MM 71-00. NO LEAKS NOTED. PERFORMED FIM PROCEDURES IAW B7 2 L 7 4 4F 4 F A20WE E20EA 2007043000007 20070430 00007 NM 2007 4 30 ABXA070127 1 20070410 A 5312 146T5405056 PRESSURE PANEL BOEING 767 767281 1385109 NM BS 1350 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 794AX 23144 PRESSURE PANEL AT FS 1350, RIGHT BUTT LINE 40 WAS CORRODED. REMOVED, REPLACED AND REINSTALLED PRESSURE PANEL AT FS 1350 , RIGHT BUTT LINE 40. 2 L 7 2 4F RT A1NM 2007043000008 20070430 00008 WP 2007 4 30 ABXA070111 1 20070228 A 5311 99196181 FRAME DOUG DC9 DC931 3022065 WP BS 718 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 949AX 47325 CRACK WITH EXFOLIATION ABOVE RADIUS ON FORWARD SIDE OF FRAME AT STA 718, APPEARED TO BE IN THE WEB AREA. REPLACED FRAME ON EA 53400323-001-2. 2 L 7 2 4F A6WE 2007043000011 20070430 00011 WP 2007 4 30 ABXA070121 1 20070409 A 5521 99184501 SPAR DOUG DC9 DC915F 3022037 WP LT ELEVATOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 785TW 47015 X-RAY INSPECTION ON LEFT ELEVATOR REVEALED CRACKS AT STATIONS: XE 74(.750), XE 191(.600), XE 195(.750), XE 199 (.750), A ND XE 219 (.400). REPAIRED CRACKS AT STATIONS: XE 191, XE 195, XE 199 AND XE 219. NO CRACKS DETECTED AT XE 74. REPAIR ED IAW DC9 SRM 55-02. 2 L 7 2 4F A6WE 2007043000013 20070430 00013 WP 2007 4 30 ABXA070113 1 20070405 A 5310 WINDOW FRAME DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 WHILE COMPLYING WITH EA 53300036-003 COCKPIT WINDOW ENCLOSURE MOD PER AD 2002-21-09 DOUBLER WAS FOUND CRACKED. REPLACED PER EA 53300036-0034 THROUGH 017 AND WO 600265187, S/B DC9 53-290, DWG SR09530268. 2 L 7 2 4F A6WE 2007043000014 20070430 00014 WP 2007 4 30 ABXA070123 1 20070406 A 5312 BULKHEAD DOUG DC9 DC915F 3022037 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 785TW 47015 AFT PRESSURE BULKHEAD DOOR CUTOUT UPPER RIGHT CORNER DOUBLER HAD APPROXIMATELY 1.5" RADIUS CRACK. REPAIRED UPPER RIGHT C ORNER OF AFT PRESSURE BULKHEAD IAW DC9 SRM J060088-543 REPAIR AND DC9 SB 53-137. 2 L 7 2 4F A6WE 2007043000015 20070430 00015 WP 2007 4 30 ABXA070124 1 20070412 A 5312 BULKHEAD DOUG DC9 DC915F 3022037 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 785TW 47015 CRACK OF UNKNOWN LENGTH AND DIRECTION IN DOUBLER UPPER LEFT AFT PRESSURE BULKHEAD DOOR CUTOUT CORNER. STOP DRILLED CRAC K IN -13 DOUBLER, INSTALLED REPAIR IAW DC9 SRM J060088-543 AND DC9 SB 53-137. 2 L 7 2 4F A6WE 2007043000016 20070430 00016 WP 2007 4 30 ABXA070114 1 20070423 A 5340 99578606 BRACKET DOUG DC9 DC941 302207N WP COCKPIT WINDOW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 DURING COCKPIT WINDOW MOD EA 53300036, FOUND BRACKET CRACKED. REMOVED AND REPLACED IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 2007043000019 20070430 00019 NM 2007 4 30 SWAA072024 1 20070424 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007043000024 20070430 00024 NM 2007 4 30 SWAA072042 1 20070424 A 5711 6545321 SPAR BOEING 737 7373T5 1384608 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 22Y CHECK, FOUND RT WING AFT SPAR CASTING CRACKED AT STA 228. REMOVED AND REPLACED AFT SPAR CASTING PE R SRM. 2 L 7 2 4F RT A16WE 2007043000025 20070430 00025 NM 2007 4 30 SWAA072031 1 20070424 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM BS 777 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 777, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007043000028 20070430 00028 NM 2007 4 30 SWAA072012 1 20070424 A 5311 6545808 FRAME BOEING 737 7373H4 1384600 NM BS 295 S11L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 295, STR 11L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007043000029 20070430 00029 NM 2007 4 30 SWAA072027 1 20070424 A 5311 6546529 FRAME BOEING 737 7373L9 1384470 NM BS 440 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007043000033 20070430 00033 NM 2007 4 30 SWAA072036 1 20070424 A 5311 6546555 FRAME BOEING 737 7375H4 138449D NM BS 867 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007043000038 20070430 00038 NM 2007 4 30 DL76L070354 1 20070422 A 4920 380029817 ENGINE BOEING 767 767332 1382001 NM APU FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 183DN 32790 27110 APU HISTORY OF NO START AND NOT ENOUGH AIR FOR MEC. BITE CK OF ECU SHOWS 143 CODE EGT TRIM MODE WILL REQUIRE APU CHANGE . REMOVED AND REPLACED APU. PERFORMED OPS CHECK AND PNEU CHECK, ALL NORMAL. 2 L 7 2 4F RT A1NM 2007043000039 20070430 00039 NM 2007 4 30 DL76G070356 1 20070423 A 3240 26124121A BRAKE BOEING 767 767332 1382001 NM NR 4 LEAKING A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 1613B 32776 AFTER LANDING TOWER REPORTED RT MAIN GEAR EMERGENCY. CREW CAME OUT SPRAYED GEAR. REPORTED LIGHT SMOKE IND NORMAL THE W HOLE TIME. PERFORMED BRAKE FIRE INSP. REPLACED NR 4 BRAKE ASSY AND NR 4 WHEEL ASSY PER MM BRAKE MPN 2612412-1A WHEEL M PN IS 767-300ERM. FOUND BRAKE PISTON BROKEN AND LEAKING. 2 L 7 2 4F RT A1NM 2007043000043 20070430 00043 NM 2007 4 30 DL76L070364 1 20070425 A 3397 WIRE BOEING 767 767332 1382001 NM EMERGENCY LIGHTS LOOSE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 175DN 24803 EMERGENCY LIGHTS IN SEATS 23GH THRU 30GH INOP. TRIED SEVERAL NEW BULBS NO HELP, TRIED NEW BATTERY CHARGER NO HELP RE-IN STALLED ORIG. FOUND WIRE LOOSE AT SEAT 23GH SIDE PANEL LOOSE, RESECURED WIRE, EMERGENCY LIGHTS CK'S NORMAL. 2 L 7 2 4F RT A1NM 2007043000044 20070430 00044 WP 2007 4 30 ABXA070134 1 20070405 A 5320 99234843 STRUCTURE DOUG DC9 DC932 3022066 WP BS 180 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 UPPER CARGO SUBFLOOR CRACKED AT LEFT BUTT LINE 50, FS 180. REPAIRED SUBFLOOR LEFT BUTT LINE 50 AT STA 180 IAW DC9 SRM 5 3-01. 2 L 7 2 4F A6WE 2007043000045 20070430 00045 WP 2007 4 30 ABXA070135 1 20070405 A 5347 S2914913M24000 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 160 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 UPPER CARGO SEAT TRACK CORRODED AT RIGHT BUTT LINE 9, FS 160. REMOVED AND REPLACED SEAT TRACK IAW DC9 SRM 51-10-3 AND 5 1-30-1. 2 L 7 2 4F A6WE 2007043000046 20070430 00046 WP 2007 4 30 ABXA070136 1 20070405 A 5313 3914677501 LONGERON SPLICE DOUG DC9 DC932 3022066 WP BS 794-813 L30 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 FOUND LONGERON 30 SPLICE FS 794 - 813 CRACKED. REMOVED AND REPLACED LONGERON 30 STA 794 - 813 IAW DC9 SRM 53-11-3. 2 L 7 2 4F A6WE 2007043000047 20070430 00047 WP 2007 4 30 ABXA070137 1 20070405 A 5347 S2914913M24000 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 493 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 FOUND SEAT TRACK AT RIGHT BUTT LINE 11 CORRODED ON BOTH SIDES OF SPLICE AT STA 493. REMOVED AND REPLACED SEAT TRACK IAW DC9 SRM 53-05. 2 L 7 2 4F A6WE 2007043000048 20070430 00048 WP 2007 4 30 ABXA070133 1 20070405 A 5320 99234843 STRUCTURE DOUG DC9 DC932 3022066 WP BS 180 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 UPPER CARGO SUBFLOOR CRACKED AT RIGHT BUTT LINE 28, FS 180. REPAIRED SUBFLOOR RIGHT BUTT LINE 28 AT STA 180 IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 2007043000050 20070430 00050 NM 2007 4 30 KCSA071164 1 20070426 A 5315 FLOORBEAM BOEING 747 747236B 1384804 NM BS 1640 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 FLOORBEAM UPPER CHORD IS CORRODED AT STA 1640 RBL49 WL-200. 2 L 7 4 4F A20WE 2007043000051 20070430 00051 SO 2007 4 30 LR7A07017 1 20070421 A 5330 SKIN LKHEED 382 382G 526414U SO FS 902 DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 438 4590 DURING SCHEDULED A CHECK PER JOB CARD HA1200, FOUND FUSELAGE DAMAGED RT SIDE APPROX 4 INCHES LONG 2 INCHES WIDE AT FS 90 2, WL198, RBL 61.62. REPAIRED DAMAGE IAW MEA 382-53-07-036, LOG PAGE 26514 ITEM M1. 2 H 7 4 4T A1SO 2007043000053 20070430 00053 EU 2007 4 30 AWXA200700519 1 20070423 A 5315 D53472172204 FLOORBEAM AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 664AW 1621 SAL - CORROSION ON CABIN FLOORBEAM, FR 66 + 6" TO FR 67 + 17", + Y1162 TO +Y1292. REPLACED CABIN FLOORBEAM, FR 66 - FR 68, +Y1162 TO +Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007043000056 20070430 00056 EU 2007 4 30 AWXA200700522 1 20070423 A 5347 D53472190211 SEAT TRACK AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 664AW 1621 SAL - FOUND CORROSION ON CABIN RAIL SEAT/FLOORBEAM, FR 64 TO FR 66, -Y1292. REPLACED CABIN RAIL SEAT/FLOORBEAM, FR 64 T O FR 66, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007043000058 20070430 00058 NM 2007 4 30 AWXA200700524 1 20070409 A 5320 644795711 SILL BOEING 737 73733A 1384673 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - FOUND CORROSION ON AFT CARGO DOOR CUT OUT LOWER SILL STRAP, BS 790 - BS 847, S25R. REPLACED AFT CARGO DOOR CUT OU T LOWER SILL STRAP, BS 790 - BS 847, S25R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007043000060 20070430 00060 NM 2007 4 30 PIDA07023 1 20070420 A 5340 STRINGER CLIP BOEING 737 7372K5 138448X NM BS 727A CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 DURING MAINTENANCE, FOUND STR 8LT TIE CLIP CRACKED AT BS 727A. REPLACED TIE CLIP PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2007043000061 20070430 00061 NM 2007 4 30 PIDA07024 1 20070420 A 5340 STRINGER CLIP BOEING 737 7372K5 138448X NM BS 747 CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 DURING MAINTENANCE, FOUND STR 7RT TIE CLIP CRACKED AT BS 747. REPLACED TIE CLIP PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2007043000062 20070430 00062 NM 2007 4 30 PIDA07019 1 20070419 A 5540 WEDGE BOEING 737 737228 13844AG NM RUDDER DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 251TR 23792 DURING MAINTENANCE, DISCOVERED A NICK IN THE TRAILING EDGE OF THE RUDDER APPROXIMATELY 86 INCHES FROM THE LOWER END. RE PAIRED DAMAGE PER SRM 51-40-15 REPAIR 11 AND BOEING MESSAGES 1-317406998-1, -7, -8, -9, -10, AND -11 WITH FAA DOA APPROV ED 8100-9 DATED APR 19, 2007. 2 L 7 2 4F RT A16WE 2007043000063 20070430 00063 NM 2007 4 30 PIDA07020 1 20070420 A 5315 FLOORBEAM BOEING 737 7372K5 138448X NM BS 312 CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 DURING MAINTENANCE CHECK, NOTED CORROSION ON UPPER CHORD OF BS 312 FLOORBEAM FROM BL 0 TO LBL 12. REPLACED SECTION OF T EE CAP PER SRM 53-10-9 FIGURE 5. 2 L 7 2 4F RT A16WE 2007043000066 20070430 00066 EU 2007 4 30 07FDEA01552 1 20070424 A 5311 SEE4B FRAME AIRBUS 310 A310 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 CORROSION ON FRAME CONNECTION , C80, P`36 REPAIR PERFORMED BY REPLACEMENT OF CORRODED SECTIONS (A539-87426-212/-211) AND INSTALLING BOLTS NAS 6603-5 INSTEAD OF RIVETS, APPROVED BY EA 6-5319-99170 AND RAS/DAHAM/4020596/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007043000067 20070430 00067 EU 2007 4 30 07FDEA01553 1 20070424 A 5320 A53771456088 PROFILE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 AT FWD CARGO DOOR CUT OUT, C20A SEALING SECTION CORRODED REPAIR PERFORMED BY REPLACE THE PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007043000068 20070430 00068 EU 2007 4 30 07FDEA01554 1 20070424 A 5310 A53611674201 SPLICE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 CORROSION AT SPLICE C19, P46 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007043000069 20070430 00069 EU 2007 4 30 07FDEA01555 1 20070424 A 5315 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 TOP CAP BEAM C33 CORRODED SPLICE REPAIR OF TOP CAP BEAM PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 2007043000072 20070430 00072 WP 2007 4 30 ABXA070103 1 20070316 A 5311 9919619504 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 AFT RIGHT MAIN FRAME HAD CRACK AT FORWARD AND AFT FLANGES, MUST BE REPLACED PER NEA 53400102-002-30. REMOVED AND REPLAC ED RIGHT MAIN FRAME IAW DC9 EA 53400326-001-2. CRACK LENGTHS WERE 1" AND 1 1/4". 2 L 7 2 4F A6WE 2007043000073 20070430 00073 WP 2007 4 30 ABXA070105 1 20070402 A 5315 99234849 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 175 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 FLOORBEAM CRACKED TO LIGHTENING HOLE APPROXIMATELY STA 175, BUTT LINE 0. REPAIRED AREA IAW REA D953-55576MR. 2 L 7 2 4F A6WE 2007043000074 20070430 00074 WP 2007 4 30 ABXA070092 1 20070313 A 5712 9919474501 RIB DOUG DC9 DC932 3022066 WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 LEFT WING XRS 164, RIB FITTING CRACKED. REMOVED AND REPLACED RIB AT LEFT WING XRS 164 IAW DC9 SRM. 2 L 7 2 4F A6WE 2007043000075 20070430 00075 WP 2007 4 30 ABXA070093 1 20070313 A 5312 5917463247 BULKHEAD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 AFT PRESSURE BULKHEAD LEFT UPPER DOOR CORNER HAD 2 CRACKS THAT NEEDED TO BE STOP DRILLED. REMOVED OUTSIDE DOUBLER, STOP DRILLED CRACKS IAW SRO J060088. REINSTALLED DOUBLER IAW SRO J060088 AND DC9 SRM 51-30-5. CRACK LENGTHS WERE 7/8", 3/4 " AND 1". 2 L 7 2 4F A6WE 2007043000076 20070430 00076 WP 2007 4 30 ABXA070094 1 20070315 A 5322 99577397 SHEAR TIE DOUG DC9 DC932 3022066 WP BS 945 S15-16R CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 SHEAR TIE CRACKED AT FS 945, BETWEEN LONGERON 15 RIGHT AND LONGERON 16 RIGHT. REMOVED AND REPLACED SHEAR TIE IAW DC9 SR M 51-30-2, 51-30-5 AND 51-30-1. 2 L 7 2 4F A6WE 2007043000077 20070430 00077 WP 2007 4 30 ABXA070096 1 20070314 A 5311 99196189 FRAME DOUG DC9 DC932 3022066 WP BS 718 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 LOWER POCKETS IN MAIN FRAME IN LEFT WHEEL WELL HAD CORROSION AROUND LOWER VERTICAL ATTACH BOLTS. CLEANED, TREATED CORRO SION AROUND LOWER VERTICAL ATTACH BOLT ON LEFT MAIN FRAME 718 AIW DC9 SRM. 2 L 7 2 4F A6WE 2007043000078 20070430 00078 WP 2007 4 30 ABXA070108 1 20070405 A 5311 99115057 FRAME DOUG DC9 DC941 302207N WP BS 83 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 WHILE COMPLYING WITH EA 53300036-003, COCKPIT WINDOW ENCLOSURE MOD PER AD 2002-21-09, DOUBLER P/N: 991505-7 WAS FOUND CR ACKED, 1.0" AND .875. REPLACED IAW EA 53300036-003 THROUGH 017 AND WO 600265187, S/B DC9 53-290 AND DWG SR09530268. 2 L 7 2 4F A6WE 2007043000082 20070430 00082 NM 2007 4 30 2007UALA01156 1 20070413 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1440 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 AFT PIT STA 1440 AT STR 26L FRAME DENTED, 2 PLACES. [SUP 05-16-07] MAJOR REPAIR ACCOMPLISHED: PERFORMED A FRAME "J" SECTION REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007043000085 20070430 00085 2007 4 30 2007UALA01160 4 20070415 A 2565 STRAP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GIRT BAR MISROUTED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 402UA 439 MED 2R SLIDE ARMING LEVER CAME OUT OF THE ARM POSITION IN FLIGHT (ALSO ECAM SHOWED NOT ARMED). PER SAMC CYCLED ARMING L EVER AND HANDLE WILL NOT ARM AND SLIGHT NOISE IN DOOR AREA. [06-12-07] FOUND GIRT BAR YELLOW STRAP WEDGED IN GIR T BAR MOUNT SLOT. ROUTED STRAP CORRECTLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007043000087 20070430 00087 EU 2007 4 30 2007UALA01163 1 20070414 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 406UA 454 EMERGENCY LIGHT TEST FAILED ON 3SVC CK. FAULTS INT LOADS EMERG L, EXT LOADS EMERG L, AND COMM EMERG L IN VIEW. SUPPLEM ENTAL DATA UPDATE REPLACED POWER SUPPLY AND BATTERY. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007043000089 20070430 00089 EU 2007 4 30 2007UALA01165 1 20070413 A 3350 BR964422 LAMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 464UA 1290 FOUND SEAT 11C EEL LIGHT RED INOPERATIVE. SUPPLEMENTAL DATA UPDATE, REPLACED LAMPS. OPS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007043000091 20070430 00091 EU 2007 4 30 2007UALA01167 1 20070413 A 3397 BR963165 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 446UA 834 CABIN EMERGENCY LIGHTS FAIL 3SVC CK. EPSU COMM FWD LEFT DISPLAYED. SUPPLEMENTAL DATA UPDATE, FOUND WIRE PULLED OUT OF SOCKET ON CONNECTOR AT 10WL PSU ABOVE DOOR 1L, CEILING PANEL REMOVED FOR ACCESS AND CONNECTOR REMOVED. CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007043000092 20070430 00092 NM 2007 4 30 2007UALA01168 1 20070413 A 5241 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 FWD GALLEY DOOR FWD LOWER FRAME IS CRACKED AT 2 FASTENER HOLES. [SUP 05-01-07] MAJOR REPAIR: INSTALLED NEW FRAME SPLIC E SECTION KIT 69-69430-9. REFERENCE SRM 51-40-02 7 DWG 69-69430. 2 L 7 2 4F 4 F RT A16WE E2GL 2007043000094 20070430 00094 NM 2007 4 30 2007UALA01170 1 20070415 A 3350 1619 LAMP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 350UA 24301 RIGHT SIDE OVERWING EMERGENCY LIGHT INOPERATIVE. [SUP 05-01-07] RELAMPED LIGHT. 2 L 7 2 4F 4 F RT A16WE E2GL 2007043000098 20070430 00098 NM 2007 4 30 2007UALA01174 1 20070415 A 3397 794640 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY EEL LIGHT INOPERATIVE AT DOORS 3 MIDLAVS CROSSAISLE. REPAIRED FEEDER CABLE. OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007043000101 20070430 00101 NM 2007 4 30 2007UALA01177 1 20070415 A 3350 80541 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 1J INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY EEL LIGHT INOPERATIVE AT SEAT 1J AFT. SUPPLEMENTAL DATA UPDATE REPLACED LIGHT ASSY. OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007043000102 20070430 00102 NM 2007 4 30 2007UALA01178 1 20070414 A 3520 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OXYGEN MASK FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 506UA 24627 FOUND CABIN EMERGENCY OXYGEN MASK DEPLOY FAILS, OPS CHECK. [06-14-07] REPLACED ALTITUDE PRESSURE SWITCH. 2 L 7 2 4F 4 F RT A2NM E17NE 2007043000110 20070430 00110 WP 2007 4 30 ABXA070131 1 20070403 A 5712 9919330509 RIB DOUG DC9 DC932 3022066 WP LT WING L/E CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 LEFT LEADING EDGE RIB HAD CRACKED DOUBLER 2ND RIB INBOARD OF NR 11 TRACK. REPAIRED RIB IAW REA D957-55597. 2 L 7 2 4F A6WE 2007043000114 20070430 00114 NM 2007 4 30 2007UALA01226 1 20070419 A 5310 BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 680 S13R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 MAIN CABIN, STUB BEAM CRACKED STA 680, 10 INCH ABOVE STR 13R. [SUP 05-04-07] MAJOR REPAIR ACCOMPLISHED: REMOVED WEB. FABRICATED & INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2007043000120 20070430 00120 NM 2007 4 30 2007UALA01232 1 20070419 A 2432 CHARGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BATTERY FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 EICAS WHITE STATUS MSG "MAIN BAT CHGR" DISPLAYED. WILL NOT CLEAR. [06-14-07] REPLACED MAIN BATTERY AND CHARGER PER UA ENGINEERING SPECIFICATIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007043000121 20070430 00121 EU 2007 4 30 2007UALA01233 1 20070419 A 2720 ROD END AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RUDDER WORN A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 492UA 1755 A-C EXPERIENCED VIBRATION 280 KTS FL240. F/A`S VERY CONCERNED IN AFT CABIN. SMOOTHED OUT FL 280 240 KNOTS. [06-22-07 ] RUDDER FREEPLAY CHECK FOUND WORN ROD END ON GREEN SYSTEM SERVO CONTROL ACTUATOR. REPLACED WORN ROD END. 2 L 7 2 4F 4 F RT A28NM E40NE 2007043000126 20070430 00126 NM 2007 4 30 2007UALA01239 1 20070419 A 5754 WEDGE BOEING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 5 SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA A10213 24799 INBD SLAT WEDGE DELAMINATED T/E WEDGE DELAMINATED. T/E WEDGE REPLACED WITH NEW. 2 L 7 2 4F 4 F RT A2NM E17NE 2007043000128 20070430 00128 WP 2007 4 30 ABXA070109 1 20070405 A 5311 99115055 FRAME DOUG DC9 DC941 302207N WP BS 83 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 WHILE COMPLYING WITH EA 53300036-003, COCKPIT WINDOW ENCLOSURE MOD PER AD 2002-21-09, DOUBLER P/N: 991505-5 WAS FOUND CR ACKED .75. REPLACED IAW EA 53300036-003 THROUGH 017 AND WO 600265187, S/B DC9 53-290 AND DWG SR09530268. 2 L 7 2 4F A6WE 2007043000130 20070430 00130 WP 2007 4 30 ABXA070100 1 20070315 A 5340 99122438 ATTACH ANGLE DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 UPPER SURFACE OF PYLON BULKHEAD TO FLOORBEAM ATTACH ANGLE AT STA 965 CORRODED FROM RIGHT BUTT LINE 55, RIGHT BUTT LINE 3 6. FABRICATED AND INSTALLED NEW PYLON BULKHEAD TO FLOORBEAM ATTACH ANGLE IAW DAC DWG 9912243. 2 L 7 2 4F A6WE 2007043000131 20070430 00131 WP 2007 4 30 ABXA070110 1 20070405 A 5310 99115056 WINDOW FRAME DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 WHILE COMPLYING WITH EA 53300036-003, COCKPIT WINDOW ENCLOSURE MOD PER AD 2002-21-09, DOUBLER P/N: 991505-6 WAS FOUND CR ACKED .5. REPLACED IAW EA 53300036-003 THROUGH 017 AND WO 600265187, S/B DC9 53-290 AND DWG SR09530268. 2 L 7 2 4F A6WE 2007043000132 20070430 00132 NM 2007 4 30 NOCA08407 1 20070415 A 3240 PRESSURE SWITCH BOEING 757 75728A 1384976 NM AUTOBRAKE SYS MALFUNCTIONED A NOCA O OTHER J WARNING INDICATION LD LANDING 1 EA 15 756NA 32448 AUTO-BRAKE DISENGAGE ON LANDING CORRECTIVE ACTION REPLACED PRESSURE SWITCHES S282 AND S283 PER MM 32-42-00, OPS CHECK OK . 2 L 7 2 4F RT A2NM 2007043000133 20070430 00133 NM 2007 4 30 SWAA072044 1 20070425 A 3350 100031 SIGN BOEING 737 7375H4 138449D NM EMERGENCY EXIT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 FOUND FWD CABIN EMERGENCY EXIT SIGN COVER BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM. 2 L 7 2 4F RT A16WE 2007043000134 20070430 00134 NM 2007 4 30 SWAA072045 1 20070425 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 771SA 27879 FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007043000135 20070430 00135 NM 2007 4 30 SWAA072062 1 20070425 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 723SW 27855 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP ROW 6 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007043000136 20070430 00136 NM 2007 4 30 SWAA072061 1 20070425 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 425LV 29829 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 3 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007043000138 20070430 00138 NM 2007 4 30 SWAA072058 1 20070425 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM BS 410 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, LBL 1. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007043000142 20070430 00142 NM 2007 4 30 SWAA072057 1 20070425 A 5311 6546526 FRAME BOEING 737 7373G7 1384595 NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007043000144 20070430 00144 NM 2007 4 30 SWAA072056 1 20070425 A 5311 6546593 FRAME BOEING 737 7373G7 1384595 NM BS 500C S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007043000146 20070430 00146 NM 2007 4 30 SWAA072041 1 20070424 A 5754 STRUCTURE BOEING 737 7373T5 1384608 NM RT WING SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007043000147 20070430 00147 NM 2007 4 30 SWAA072019 1 20070424 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 787 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000148 20070430 00148 NM 2007 4 30 SWAA072039 1 20070424 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 520 S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000149 20070430 00149 NM 2007 4 30 SWAA072014 1 20070424 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727A S2L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000151 20070430 00151 NM 2007 4 30 SWAA072016 1 20070424 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727D S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000153 20070430 00153 NM 2007 4 30 SWAA072018 1 20070424 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 887 S6L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000154 20070430 00154 NM 2007 4 30 SWAA072020 1 20070424 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 847 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000155 20070430 00155 NM 2007 4 30 SWAA072021 1 20070424 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 907 S2R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000160 20070430 00160 NM 2007 4 30 SWAA072034 1 20070424 A 5311 65C34356 FRAME BOEING 737 7375H4 138449D NM BS 482A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007043000162 20070430 00162 NM 2007 4 30 QXEA200700676 1 20070413 A 5330 DOUBLER DHAV DHC8 DHC8202 2809007 NM FUSLEAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - LAVATORY EXTERIOR SERVICE PANEL SURROUND DOUBLER ON FUSELAGE IS CHAFED IN 2 PLACES ALONG AFT EDGE BY DOOR APERT URE. REPAIRED IAW RD8-53-3299 AND SRM 51-20-36, 51-20-16. 2 H 7 2 4T RT A13NM 2007043000167 20070430 00167 NM 2007 4 30 QXEA200700680 1 20070414 A 5313 STRINGER DHAV DHC8 DHC8202 2809007 NM BS 201 S31L CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - STRINGER 31L CASTING AT FRAME X201 HAS CORROSION. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007043000168 20070430 00168 NM 2007 4 30 QXEA200700682 1 20070425 A 3230 82454301001 CABLE BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY RELEAS FRAYED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 404QX 4046 GEG FLIGHT NR 2338: LT MAIN LANDING GEAR DOORS WOULDN'T OPEN WITH EMERGENCY RELEASE HANDLE. FOUND LOWER AFT CABLE AT LE VER OFF PULLEY AND FRAYED. MAINTENANCE REMOVED AND REPLACED THE CABLE WITH NEW CABLE FROM STOCK. CHECKS WELL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007043000169 20070430 00169 NM 2007 4 30 QXEA200700683 1 20070425 A 2610 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM FIRE DETECTION WARNING LIGHT A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 419QX 4145 STS FLIGHT NR 2467: 'CHECK FIRE DETECT' MASTER WARNING LIGHT ILLUMINATED AFTER BOTH ENGINE START WITH NO OTHER INDICATIO NS NOTED. MAINTENANCE CYCLED POWER TO THE FIRE DETECT SYSTEM. PERFORMED FIRE DETECT SYSTEM TEST. NO DEFECTS NOTED. N O PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007043000171 20070430 00171 NM 2007 4 30 SWAA072051 1 20070425 A 5315 6547980 CREASE BEAM BOEING 737 7373L9 1384470 NM BS 807-827 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 807 TO BS 827, RBL 70. REMOVED AND REPLACED CREASE BEA M WEB PER SRM. 2 L 7 2 4F RT A16WE 2007042600180 20070426 00180 EA 2007 4 26 SWIA200718131 1 20070305 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 448SW 7678 STATION 280 BULKHEAD RBL 12.0 LOWER FLANGE IS CRACKED, DISCOVERED AT C-CHECK INSPECTION. INSTALLED REPAIR ANGLE -4 CLIP S AND -6 FILLER AT STATION 280 BULKHEAD RBL 12 PER CRJ200 REO 601R53-11-171. 2 L 7 2 4F RT A21EA 2007042600181 20070426 00181 EA 2007 4 26 SWIA200718132 1 20070305 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 448SW 7678 STATION 280 BULKHEAD RBL9 HAS INBOARD AND OUTBOARD CRACKED CLIPS, DISCOVERED ON C-CHECK INSPECTION. REMOVED AND REPLACE D INBOARD AND OUTBOARD CLIP PER CRJ200 REO 601-53-11-177 AND STANDARD REPAIR 601R 53-0057A. 2 L 7 2 4F RT A21EA 2007042600185 20070426 00185 NM 2007 4 26 DU4R2007084 1 20070403 A 5210 SHAFT BOEING 757 757232 1384965 NM L2 DOOR CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND CORROSION ON L-2 DOOR LOWER HINGE ARM SHAFT INTERNAL UPPER NUT RUSTED. REPAIRED BY INSTALLING NEW UPPER AND LOWER BEARINGS. INSTALLED NEW LOWER HINGE ARM P/N 140N2651-49 IAW B757 CCM 52-11-15 AND SOPM 20-50-03. 2 L 7 2 4F RT A2NM 2007042700005 20070427 00005 NM 2007 4 27 QXEA200700665 1 20070407 A 5320 STIFFENER DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - FOUND CORROSION ON THE STIFFENER AT STATION 600 THAT THE CARGO DOOR THRESHOLD ATTACHES TO. REPAIRED IAW SRM 51 -40-11, 51-40-00. 2 H 7 2 4T RT A13NM 2007042700012 20070427 00012 NM 2007 4 27 QXEA200700670 1 20070415 A 5340 GUSSET DHAV DHC8 DHC8202 2809007 NM EMERGENCY EXIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - RIGHT FORWARD EMERGENCY EXIT APERTURE BOTTOM SILL GUSSET/WEB PLATES AND RIVETS HAVE CORROSION BETWEEN FS X209 T O X279 AT STRINGER 24S. REPAIRED IAW SRM 51-40-11, 51-40-00. 2 H 7 2 4T RT A13NM 2007043000022 20070430 00022 NM 2007 4 30 SWAA072022 1 20070424 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007043000023 20070430 00023 2007 4 30 SWAA072011 4 20070424 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 223WN 32492 FOUND R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007043000030 20070430 00030 NM 2007 4 30 SWAA072032 1 20070424 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM BS 440 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007043000031 20070430 00031 NM 2007 4 30 SWAA072028 1 20070424 A 5311 6546532 FRAME BOEING 737 7373L9 1384470 NM BS 480 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007043000032 20070430 00032 NM 2007 4 30 SWAA072035 1 20070424 A 5311 6546534 FRAME BOEING 737 7375H4 138449D NM BS 520 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007043000035 20070430 00035 NM 2007 4 30 SWAA072025 1 20070424 A 5311 6549906 FRAME BOEING 737 7373L9 1384470 NM BS 1112 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 1112, RBL 20, WL 202. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007043000036 20070430 00036 WP 2007 4 30 ABXA070107 1 20070417 A 7931 41800044 TRANSMITTER DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 1 ENGINE DEFECTIVE A ABXA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CL CLIMB 1 GL 23 826AX 1 46061 671391 AT TOP OF CLIMB, NR 1 ENGINE OIL PRESSURE STARTED DROPPING OFF INTO CAUTIONARY RANGE. RAN ABNORMAL CHECK LIST, REDUCED POWER TO IDLE. OIL PRESSURE DROPPED BELOW RED LINE, SECURED ENGINE AND RETURNED FOR LANDING. REPLACED NR 1 ENGINE OIL P RESSURE TRANSMITTER IAW DC8 MM 79-30-33. OPS CHECK GOOD ON ENGINE RUN. 2 L 7 4 4F 4 F 4A25 1E8 2007043000059 20070430 00059 NM 2007 4 30 PIDA07022 1 20070420 A 5340 STRINGER CLIP BOEING 737 7372K5 138448X NM BS 663 S11L CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 DURING MAINTENANCE, FOUND STR 11LT TIE CLIP CRACKED AT BS 663.17. REPLACED TIE CLIP PER SRM 51-30-0. 2 L 7 2 4F RT A16WE 2007043000080 20070430 00080 NM 2007 4 30 2007UALA01154 1 20070416 A 5340 FITTING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSLEAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA 24380 NOSE JACK PAD FITTING SUPPORT STRUCTURE DAMAGED. [SUP 05-16-07] REPLACED DAMAGED JACK PAD STRUCTURE IAW FRR UAL-744-02 61. A/C OK FOR SERVICE. PERMANENT REPAIR SET FOR FOR HEAVY VIST LATER IN 2007. SUSPECT JACK PAD IMPACTED BY GROUND SERV ICE EQUIPMENT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007043000096 20070430 00096 NM 2007 4 30 2007UALA01172 1 20070415 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY EEL LIGHTS ARE INOPERATIVE AT THE LWR WALL ACROSS LAVS 100, 104 AND 110. ALSO AT SEATS 6L THRU 8L. REPLACED BATTERY ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007043000097 20070430 00097 NM 2007 4 30 2007UALA01173 1 20070415 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 FOUND EMERGENCY EXIT LIGHT INOPERATIVE AT DOOR 2L BUSTLE. RELAMPED. OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007043000099 20070430 00099 NM 2007 4 30 2007UALA01175 1 20070415 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY EXIT LIGHT INOPERATIVE AT UPPER DECK CEILING AT ROW 13. RELAMPED, OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007043000105 20070430 00105 NM 2007 4 30 2007UALA01181 1 20070414 A 2120 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN ODOR A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 WP 29 660UA 27115 ON FINAL APPROACH, STRONGER ELECTRICAL ODOR RETURNED THROUGHOUT ACFT ALONG WITH HAZE IN CABIN. [SUP 05-04-07] REPLAC ED LEFT RECIRC FILTER AND LEFT RECIRC FAN. SMELL GONE A & NO HAZE. A/C RETURNED TO SERVICE. SUSPECT WEAR IN RECIRC FAN LED TO SHORT CIRCUIT & CURRENT SURGE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007043000106 20070430 00106 NM 2007 4 30 2007UALA01182 1 20070413 A 2930 INDICATION SYS BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE HYD QTY MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 662UA 27159 RTFL DUE TO RIGHT AND CENTER HYDRAULIC SYSTEMS QUANTITY INDICATION PROBLEMS. [SUP 05-16-07] REPLACED HYD. QTY. MONITOR UNIT PER MM 29-33-01. OP CHECKS NORMALLY. A/C RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007043000108 20070430 00108 2007 4 30 2007UALA01223 4 20070418 A 2565 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 RIGHT EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE BULB WILL NOT TEST. [06-14-07] CONFIRMED BOTTLE PRESSURE SWITCH S104 64 IS READING OPEN BETWEEN PINS A-C DUE TO INSUFFICIENT BOTTLE PRESSURE NOTED AT 2600 PSI. SWITCH IS DESIGNED TO OPEN W HEN BOTTLE PRESS READS BELOW 2780 PSI. REPLACED BOTTLE ASSY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007043000113 20070430 00113 NM 2007 4 30 2007UALA01225 1 20070419 A 5310 BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 680 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 MAIN CABIN STUB BEAM CRACKED STA 680, JUST BELOW 5 INCH STR 11L. [SUP 05-04-07] MAJOR REPAIR ACCOMPLISHED: REMOVED W EB. FABRICATED & INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2007043000116 20070430 00116 NM 2007 4 30 2007UALA01228 1 20070419 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1640 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 RT MAIN CABIN FLOORBEAM, UPPER CHORD HAS CORROSION BEYOND LIMITS, BS 1640, BETWEEN LBL10 TO RBL 87. [SUP 05-04-07] MA JOR REPAIR ACCOMPLISHED: REMOVED DAMAGED CHORD. FABRICATED & INSTALLED NEW CHORD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007043000117 20070430 00117 NM 2007 4 30 2007UALA01229 1 20070419 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L-4 DOOR UPPER DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 L-4 DOOR UPPER GATE CORRODED AND CRACKED. [SUP 05-04-07] REPLACED UPPER GATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007043000118 20070430 00118 EU 2007 4 30 2007UALA01230 1 20070419 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 420UA 489 CREW O2 EMPTY ONLY 50 PSI AT SHUTDOWN. [06-22-07] "PRESS TO TEST" SLIDE SWITCH ON CAPTAIN'S O2 MASK STOWAGE BOX STIC KS, ALLOWING SLOW LEAK THROUGH TEST FUNCTION. REPLACED OXYGEN MASK STOWAGE BOX. 2 L 7 2 4F 4 F RT A28NM E40NE 2007043000124 20070430 00124 NM 2007 4 30 2007UALA01236 1 20070420 A 3350 8100133801 LIGHT BOEING 727 727222 1384073 NM PWA PW4077 PW4077 NE SEAT 14D MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 776UA 26937 AFT EEL LIGHT AT SEAT 14D IS MISSING. REPLACED LIGHT ASSY. OPS CHECKS GOOD. 2 L 7 3 4F 4 F A3WE E46NE 2007043000140 20070430 00140 NM 2007 4 30 SWAA072047 1 20070425 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 730D S19R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730D, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007043000150 20070430 00150 NM 2007 4 30 SWAA072015 1 20070424 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727A S3L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000152 20070430 00152 NM 2007 4 30 SWAA072026 1 20070424 A 5340 65C27314 STRINGER CLIP BOEING 737 7373L9 1384470 NM BS 294 S13L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000157 20070430 00157 NM 2007 4 30 SWAA072037 1 20070424 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 482A S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482A, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000158 20070430 00158 NM 2007 4 30 SWAA072017 1 20070424 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 767 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000174 20070430 00174 NM 2007 4 30 SWAA072055 1 20070425 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM BS 767 S14L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000176 20070430 00176 NM 2007 4 30 SWAA072053 1 20070425 A 5340 65C27314 STRINGER CLIP BOEING 737 7373L9 1384470 NM BS 578 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000177 20070430 00177 NM 2007 4 30 SWAA072043 1 20070425 A 2612 6676 FIRE LOOP BOEING 737 7377H4 1384404 NM NR 1 NACELLE FAULTY A SWAA O OTHER N FALSE WARNING CL CLIMB 1 SW 29 467WN 33830 NR 1 ENGINE FIRE WARNING "A" LOOP LIGHT ILLUMINATED. REMOVED AND REPLACED FIRE LOOP "A" HARNESS PER MM. 2 L 7 2 4F RT A16WE 2007043000179 20070430 00179 NM 2007 4 30 SWAA072085 1 20070426 A 5311 6546539 FRAME BOEING 737 7375H4 138449D NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT LH BS 616, WL 199. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2007043000183 20070430 00183 NM 2007 4 30 SWAA072080 1 20070426 A 5311 65C25230 FRAME BOEING 737 7373L9 1384470 NM BS 727E S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007043000184 20070430 00184 NM 2007 4 30 SWAA072087 1 20070426 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 827 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000185 20070430 00185 NM 2007 4 30 SWAA072069 1 20070426 A 5340 65CC27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727D S6R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000187 20070430 00187 NM 2007 4 30 SWAA072067 1 20070426 A 5340 65CC27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 747 S5L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000188 20070430 00188 NM 2007 4 30 SWAA072066 1 20070426 A 5340 65CC27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727D S6L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000189 20070430 00189 NM 2007 4 30 SWAA072065 1 20070426 A 5340 65CC27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727D S5L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000190 20070430 00190 NM 2007 4 30 SWAA072064 1 20070426 A 5340 65CC27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727C S6L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000191 20070430 00191 2007 4 30 SWAA072078 4 20070426 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 618WN 28034 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007043000192 20070430 00192 NM 2007 4 30 SWAA072088 1 20070426 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 783SW 29809 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007043000193 20070430 00193 NM 2007 4 30 SWAA072074 1 20070426 A 3350 3071BPEGPL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007043000196 20070430 00196 NM 2007 4 30 SWAA072083 1 20070426 A 5311 6516301 FRAME BOEING 737 7373L9 1384470 NM BS 188 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, RBL 33, WL 208. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007043000197 20070430 00197 NM 2007 4 30 SWAA072071 1 20070426 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 740A S14L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740A, STR 14L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007043000198 20070430 00198 NM 2007 4 30 SWAA072076 1 20070426 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 727E S22L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 22L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007043000205 20070430 00205 NM 2007 4 30 NOCA08607 1 20070420 A 2910 LINE BOEING 767 767300 1385204 NM HYD SYSTEM LOOSE A NOCA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 15 769NA 28039 IN FLIGHT EICAS "L HYD QTY" ON WITH ACCOMPANYING DROP IN L HYD QTY ON STATUS PAGE. INSPECTED MIDDLE RUDDER PCU, ELEVATO R DEEL UNIT, RATIO CHANGER, RT YAW DAMP SERVO NO LEAKS NOTED INSPECTED INSIDE VERTICAL FIN FOUND B-NUT FOR LT HYD SYSTEM LINE LOOSE TIGHTENED B-NUT AND PERFORMED LEAK CHECK NO LEAK NOTED CONTD ON 4M. SERVICED LT HYD SYSTEM PER MM 12-12-01 DUE LT HYD SYSTEM LOSS REMOVED AND REPLACED CASE DRAIN, PRESSURE AND RETURN FILTER REMOVED AND REPLACED CASE DRAIN PRESS URE AND RETURN AND ENG PRESSURE FILTER PER MM 29-11-17 LK CK OK. LEFT ENGINE EDP REQUIRES REPLACEMENT DUE LOST QTY OF H YD FLUID REMOVED AND REPLACED NR 1 EDP PER MM 29-11-05 RAN ENGINE. OPS AND LEAK CK OK. 2 L 7 2 4F RT A1NM 2007043000206 20070430 00206 EA 2007 4 30 TRAX200700547 1 20070412 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 835AS 7258 FOUND 2 NTERCOSTAL CLIPS CRACKED LT AFT 621 BULKHEAD BETWEEN FS 621.00 AND 625.00. 2 L 7 2 4F RT A21EA 2007043000207 20070430 00207 EA 2007 4 30 TRAX200700548 1 20070419 A 3250 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING WARNING LIGHT A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 923EV 7826 STEERING INOP MSG AFTER TAKEOFF, COMPLIED WITH QRH, LANDED W/ NWS OFF, HIT A LARGE BUMP ON TAKE OFF INTERSECTING RUNWAYS , EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007043000210 20070430 00210 NE 2007 4 30 MALA070055 2 20070421 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 410XJ 340B410 GEE785669 INFLIGHT LEFT CHIP DETECTOR ANNC PULLED POWER BACK TO FI. ENGINE WAS STABLE FOR 45 SECONDS THEN ITT WENT UP AS TORQUE B OUNCED 20-25 AND THEN THE NG WENT BELOW 20 PERCENT AND SHUT DOWN PER QRD. REMOVED AND REPLACED LT ENGINE PN ON/OFF CT7- 9B S/N ON GE-E785767, SN OFF GE-E785669. 2 L 7 2 4T 4 T RT A52EU E8NE 2007050100001 20070501 00001 EU 2007 5 1 07FDEA01586 1 20070424 A 3230 MECHANISM AIRBUS 310 A310203 3930313 EU MLG DIRTY A FDEA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 25 429FE 364 RAISING GEAR ON T/O NOSE GEAR DOOR LIGHT REMAINED ON. ILLUMINATED ON BOTH SYS AS SPEED INCREASED TO 200 KNOTS, NOISE AN D VIB WAS FELT FROM THE NOSE GEAR. NOISE AND VIB REMAINED UNTIL GEAR WAS LOWERED AGAIN, AND THEN THE LIGHT WENT OUT. FOUND FWD LEFT GEAR DOOR MECHANISMS STICKY AND DRY. CLEANED AND LUBED AND CHECKED RIGGING. OPS CHECKED REF M/M 32-31-0 0-5 AND 32-00-00-5. OPS CHECKED GOOD AND RESTORED A/C TO NORMAL CONFIG AND IS OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2007050100003 20070501 00003 NM 2007 5 1 07FDEA01588 1 20070425 A 5754 SLAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 RIGHT WING, LEADING EDGE SLAT TRACK NR 12 CUT OUT FOUND WITH 1.5 INCH CRACK. [SUP 05-14-07] TRIMMED OUT AND REPAIRED A S PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050100005 20070501 00005 NM 2007 5 1 07FDEA01590 1 20070425 A 5710 STRUCTURE DOUG MD11 MD11F 3023600 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 LEFT WING, TELESCOPIC DUCT CUT-OUT FOUND WITH 0.5 INCH CRACK. [SUP 05-14-07] REPAIRED AS PER SRM 57-10-00 VOLUME I ( T.R.) FIGURE 42. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050100006 20070501 00006 NM 2007 5 1 07FDEA01591 1 20070425 A 5710 STRUCTURE DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 RIGHT WING, TELESCOPIC DUCT CUT-OUT FOUND WITH 0.4375 INCH CRACK. [SUP 05-14-07] REPAIRED AS PER SRM 57-10-00 VOLUME I (T.R.), FIGURE 42. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050100008 20070501 00008 NM 2007 5 1 07FDEA01595 1 20070425 A 5311 ACA71231 FRAME DOUG MD11 MD11F 3023600 NM BS 535 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 LEFT MAINFRAME STA 535 AT 9G NET SUPPORT YOKE AREA FOUND CHAFED. [SUP 05-10-07] REPAIR CARRIED OUT AS PER FEDEX AIRCRA FT ENGINEERING STANDARD REWORK DRAWING NR: SRZ 53-503. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050100009 20070501 00009 NM 2007 5 1 07FDEA01596 1 20070425 A 5753 NRC6762501 VANE DOUG MD11 MD11 3023602 NM ZONE 500 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 RIGHT WING, INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED. [SUP 05-15-07] REMOVED AND REPLACED AS PER AMM 27-50-22 -4. ADJUSTMENT CARRIED OUT AS PER AMM 27-50-22-5. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050100010 20070501 00010 NM 2007 5 1 07FDEA01597 1 20070425 A 5753 NRC6762501 VANE DOUG MD11 MD11 3023602 NM ZONE 500 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 LEFT WING, INBOARD FLAP VANE LOWER SURFACE FOUND WITH EXISTING REPAIR WHICH IS NOT COVERED BY SRM. [SUP 05-16-07] REM OVED AND REPLACED AS PER AMM 27-50-22-04. ADJUSTMENT CARRIED OUT AS PER AMM 27-50-22-05. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050100011 20070501 00011 NM 2007 5 1 07FDEA01598 1 20070426 A 5311 AFA00193 FRAME DOUG MD11 MD11 3023602 NM BS 1721 L12L DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 MAIN DECK CARGO COMPARTMENT, MAIN FRAME STA 1721 AT LONGERON 12L FOUND WITH DENT. [SUP 05-08-07] REPAIRED AS PER SRM 5 3-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050100012 20070501 00012 NM 2007 5 1 07FDEA01599 1 20070426 A 5311 AFA00193 FRAME DOUG MD11 MD11F 3023600 NM BS 1721 L12R DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 MAIN DECK CARGO COMPARTMENT, MAIN FRAME STA 1721 AT LONGERON 12R FOUND WITH DENT. [SUP 05-08-07] REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050100015 20070501 00015 NM 2007 5 1 07FDEA01602 1 20070426 A 5311 AFA00283 FRAME DOUG MD11 MD11F 3023600 NM BS 1681 L12L DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 MAIN DECK CARGO COMPARTMENT, MAIN FRAME STA 1681 AT LONGERON 12L FOUND WITH DENT. [SUP 05-08-07] REPAIRED AS PER SRM 5 3-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050100016 20070501 00016 NM 2007 5 1 07FDEA01603 1 20070426 A 5311 AFA00283 FRAME DOUG MD11 MD11F 3023600 NM BS 1681 L12R DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 MAIN DECK CARGO COMPARTMENT, MAIN FRAME STA 1681 AT LONGERON 12R FOUND WITH DENT. [SUP 05-08-07] REPAIRED AS PER SRM 5 3-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050100019 20070501 00019 EU 2007 5 1 07FDEA01606 1 20070426 A 5754 RIB AIRBUS 310 A310324 3930206 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 SLAT NR 2 LT DENT ON LEADING EDGE OVER RIB 52 REPAIR PERFORMED BY CUT OUT AND FLUSH DOUBLER INSTALLATION IAW SRM 57-43-1 1 FIG 202. 2 L 7 2 4F RT A35EU 2007050100024 20070501 00024 EU 2007 5 1 07FDEA01612 1 20070426 A 5714 STRUCTURE AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 809FD 449 DEVIATIONS DURING EMBODIMENT OF SB A310-57-2047 REV 2, SEVERAL HOLES WERE FOUND WITH DAMAGES: HOLE 63 RT (MISDRILLED PIL OT HOLE), HOLE 35A, 42 RT (TOOLING MARK), HOLE 18LH (TOOLING MARK). REPAIR PERFORMED BY REAM UP THE HOLES IAW EA 6-5710 -99209 AND RAS/044239/010/2006 ISS. A. 2 L 7 2 4F RT A35EU 2007050100025 20070501 00025 EU 2007 5 1 07FDEA01613 1 20070426 A 5313 SEE4A STRINGER AIRBUS 310 A310324 3930206 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 CORROSION ON STRINGER P48 AND 55 LT (A539-86217, A539-86218) AT C59-60 AND P56 LT (A539-74267-202) AT C62-64 STRINGER RE PAIR PERFORMED IAW SRM 53-10-14 FIG 201/201A. 2 L 7 2 4F RT A35EU 2007050100028 20070501 00028 EU 2007 5 1 07FDEA01616 1 20070426 A 5313 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 FOUND CORROSION AT STRINGER P52 LT, C54.3-C55/58 AND P56L, C54.2-55/58 STRINGER REPAIR PERFORMED ON P56 LT, C54.2-55/58 IAW SRM 53-10-14 FIG 201 AND BLEND OUT THE CORROSION AT P53LH, C54.3-55/58 IAW EA 6-5316-99233 AND RAS/DATLS/0003124/200 6 ISS. A. 2 L 7 2 4F RT A35EU 2007050100030 20070501 00030 EU 2007 5 1 07FDEA01618 1 20070426 A 5330 A53980911202 DOUBLER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 CORROSION FOUND ON DOUBLER A539-80911-202, C72-73, P41-43LHS REPAIR PERFORMED BY BLEND OUT AND FLAP PEENING IAW SRM 51-2 9-00, APPROVED BY EA 6-5318-99190 AND RAS/DAHAM/4020661/2006 ISS A. 2 L 7 2 4F RT A35EU 2007050100031 20070501 00031 NM 2007 5 1 07FDEA01619 1 20070426 A 5754 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 FOUND LEFT WING, NR 3 SLAT LEADING EDGE FOUND DENT. [SUP 05-15-07] DENT ON NR 3 SLAT LEADING EDGE AT LEFT HAND WING SM OOTHENED OUT AND FOUND OUT OF LIMIT PER SRM 57-10-00 FIGURE 16 VOLUME I. REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-1 11095, REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050100033 20070501 00033 EU 2007 5 1 07FDEA01621 1 20070426 A 5313 A53974484206 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 FOUND CORROSION AT STRINGER P45 LT, C71-72 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007050100034 20070501 00034 EU 2007 5 1 07FDEA01622 1 20070426 A 5313 A53986212 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 FOUND CORROSION AT STRINGER P54, 55, 56 LT, C70-72, STRINGER REPAIR PERFORMED IAW SRM 53-10-14. 2 L 7 2 4F RT A35EU 2007050100036 20070501 00036 EU 2007 5 1 07FDEA01624 1 20070426 A 5714 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 CORROSION AT CENTER WING BOX TOP SKIN AT TRACK 5-6 LT ON C46.2-47, 5-6 RT ON C47 REPAIR PERFORMED BY BLEND OUT AND OVERS IZING IAW EA 6-5710-99188 AND RAS/43898/038/2006 ISS. A 2 L 7 2 4F RT A35EU 2007050100037 20070501 00037 EU 2007 5 1 07FDEA01625 1 20070426 A 5210 SEEPARA4B CHANNEL AIRBUS 310 A310324 3930206 EU ZONE 800 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 AFT PAX DOOR LOWER DOOR CHANNEL DAMAGED (DEFORMATION) REPAIR PERFORMED BY REPLACEMENT OF PARTS (LOWER CHANNEL P/N A521-7 5271-202, SEGMENT P/N A521-75325-332). 2 L 7 2 4F RT A35EU 2007050100038 20070501 00038 EU 2007 5 1 07FDEA01627 1 20070426 A 5313 A53974484206 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 CORROSION AT STRINGER P48 LT, C71-72 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007050100039 20070501 00039 EU 2007 5 1 07FDEA01628 1 20070426 A 5313 A53974482204 STRINGER SPLICE AIRBUS 310 A310324 3930206 EU ZONE 100 MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 DUE TO INSTALLATION OF A STRINGER CONNECTING SECTION FOUND THAT THE NEW SECTION IS NOT POSSIBLE TO INSTALL. REPAIR PERF ORMED BY FABRICATION OF A LONGER CONNECTING SECTION PER DWR A539-74482, APPROVED BY EA 6-5317-99210 AND RAS/DAHAM/403070 6/2006 ISS A. 2 L 7 2 4F RT A35EU 2007050100042 20070501 00042 WP 2007 5 1 07FDEA01632 1 20070426 A 5311 FRAME DOUG DC10 DC1010 3022110 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 397FE 46631 ACF MODIFICATION AND REPAIR ASSESSMENT AFT FUSE WASTE TANK COMPT STA 1996 LT SIDE TO L. 50 FROM L. 52 REPAIR EXISTING WI TH LIGHT CORROSION. REMOVED EXISTING REPAIR, PERFORMED INSPECTION, CUP ANGLE B/T L46 AND L48 RT SIDE AND B/T L 48 TO L 50 LT SIDE IAW SRM 53-30-00 FIG 5 VOL I. FABRICATED AND INSTALLED NEW CAP ANGLE AND SPLICES IAW SRM 53-30-00 FIG 5 VOL I. 2 L 7 3 4F A22WE 2007050100043 20070501 00043 WP 2007 5 1 07FDEA01633 1 20070426 A 5311 FRAME DOUG DC10 DC1010 3022110 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 397FE 46631 MD 10-10 ACF MODIFICATION AND REPAIR ASSESSMENT AFT FUSE WASTE TANK COMPT STA 1996 RT SIDE TO L 47 FROM L 50 REPAIR EXIS TING WITH LIGHT CORROSION. PERFORMED REPAIR WITH NRC NR 1202. 2 L 7 3 4F A22WE 2007050100045 20070501 00045 NM 2007 5 1 QXEA200700686 1 20070422 A 3010 4100S00503 VALVE BOMBDR DHC8 DHC8402 1390042 NM DEICE SYSTEM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 413QX 1529 1529 4060 SEA FLIGHT NR 2348: ON DESCENT, DEICE PRESSURE CAUTION ILLUMINATED AT REDUCED POWER. CONDUCTED E/A CHECKLIST AND LIGHT RE-ILLUMINATED ON SUBSEQUENT CYCLE. PRESSURE NORMAL BUT HORIZONTAL STAB INBOARD LIGHT (LEFT) DID NOT ILLUMINATE. MAINT ENANCE REMOVED AND REPLACED DDV NR 6 IAW AMM Q400 TASK 30-11-16-000-801 AND TASK 30-11-16-400-801. OPS CHECK GOOD IAW T ASK 30-11-00-720-801. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007050100047 20070501 00047 EA 2007 5 1 QXEA200700653 1 20070421 A 2840 73811812 COMPUTER CNDAIR CL600 CL6002C10 1390015 EA FUEL QTY MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 610QX 1960 10033 SEA - FLIGHT 2544, RETURN TO THE GATE WITH FUEL IMBALANCE. LEFT WING SHOWING 600 LBS HEAVY. CORRECTED ON TAXI. TURNIN G TO RUNWAY RIGHT WING WAS 600 LBS HEAVY THEN RETURNED TO NORMAL. AT ARRIVAL BACK AT GATE RT IMBALANCE RETURNED. MAINT ENANCE REPLACED THE FUEL QUANTITY GAUGING COMPUTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007050100048 20070501 00048 NE 2007 5 1 QXEA200700688 2 20070426 A 7200 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE LT ENGINE MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 605QX 10022 SEA - LEFT ENGINE WOULD NOT START. FUEL FLOW, IGNITION, AND ROTATION ALL NORMAL. NO ITT RISE. RETURNED TO THE GATE. MAINTENANCE PERFORMED 2 STARTS WITH NO PROBLEMS NOTED. NO FAULTS FOUND. RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007050100049 20070501 00049 EA 2007 5 1 QXEA200700615 1 20070412 A 2720 8220845002 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA EICAS ROUTING MALFUNCTIONED A QXEA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 09 290RB 3658 10029 PDX - FLIGHT 2595 - RETURNED TO THE GATE AFTER THE RUDDER TRIM WOULD NOT GET FULL DEFLECTION. WILL NOT GO INTO TAKEOFF RANGE. MAINTENANCE REPLACED THE EICAS ROUTING UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007050100050 20070501 00050 2007 5 1 QXEA200700645 4 20070414 A 3410 8220372436 DADC CNDAIR CL600 CL6002C10 1390015 EA NR 2 MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 610QX 7909 10033 PDX - FLIGHT 2545 (SEA-PDX) - STALL FAIL MESSAGE FOLLOWED BY ADC 2 FAIL. STICK SHAKER OND OVERSPEED WARNING ENDED WHEN FO'S ADC SOURCE CHANGED TO ADC 1. RETURNED TO THE FIELD AND MADE A UNEVENTFUL LANDING, MAINTENANCE REPLACED THE NR 2 DA DC. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007050100051 20070501 00051 EA 2007 5 1 QXEA200700614 1 20070412 A 3020 54011485 VALVE CNDAIR CL600 CL6002C10 1390015 EA ANTI ICE SYSTEM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 608QX 3418 10026 PDX - FLIGHT 2506 - RETURNED TO THE FIELD AFTER A LEFT ENGINE ANTI-ICE CAUTION MESSAGE. UNEVENTFUL LANDING. REPLACED T HE COWL ANTI-ICE VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007050100054 20070501 00054 2007 5 1 AWXA200700513 4 20070420 A 2565 D30664109 SLIDE AIRBUS 320 A320231 3930325 EU L1 DOOR FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 634AW 32253 5650 091 MX REPORTED L-1 SLIDE WILL NOT STAY ARMED. MX REPLACED THE L-1 SLIDE. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007050100056 20070501 00056 EU 2007 5 1 07FDEA01560 1 20070424 A 5320 A53778669210 ACCESS PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 809FD 449 FOUND FOUR NON RECORDED POCKET REPAIRS ON MANHOLE FITTING C23-C24. REPAIR PERFORMED BY REPLACEMENT OF MANHOLE FITTING I AW DRW: R537-06163 ISSUE "B", APPROVED BY EA 6-5310-99203 AND RAS/DABRE/7006670/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007050100057 20070501 00057 NM 2007 5 1 QXEA200700681 1 20070425 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY MISINSTALLED A QXEA O OTHER W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 NM 09 346PH 477 PDX FLIGHT NR 2121 MASTER CAUTION - SMOKE WENT OFF NUMBEROUS TIMES DURING CLIMB (AFTER 10000') CRUISE (16000') AND APPRO ACH. MAINTENANCE INSPECTED BAGGAGE COMPARTMENT SMOKE DETECTORS. FOUND NO COPPER SHIELDING TAPE INSTALLED ON EITHER SMO KE DETECTOR. INSTALLED SHIELDING TAPE. SYSTEM OPERATION CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007050100058 20070501 00058 EU 2007 5 1 07FDEA01561 1 20070424 A 5320 A53778685206 ACCESS PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 FOUND MORE THAN FOUR OLD NON RECORDED POCKET REPAIRS ON MANHOLE FITTING, C38.1-C38.2. THIS IS NOT ALLOWED IAW SRM 53-14 -12 / PG 228. REPAIR PERFORMED BY REPLACEMENT OF MANHOLE FITTING IAW DRW: R537-06164 ISSUE "D", APPROVED BY EA 6-5310-1 01336 AND RAS/DABRE/7006671/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007050100060 20070501 00060 WP 2007 5 1 07FDEA01567 1 20070424 A 5730 SKIN DOUG DC10 DC1010 3022110 WP RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 RT WING T/E LWR SKIN FOUND SEVERE CORROSION ON BEAVER TAIL AT STA XORS 231. REPAIR IAW EA FEDEX 8-5710-108070. 2 L 7 3 4F A22WE 2007050100061 20070501 00061 EU 2007 5 1 07FDEA01568 1 20070424 A 5230 A52370076202 BEAM AIRBUS 310 A310324 3930206 EU ZONE 800 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 FOUND DENT 40 BY 35 BY 1MM AT FWD CARGO COMPARTMENT DOOR, BEAM C22-C22A. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SR M 52-32-00/PB 200. 2 L 7 2 4F RT A35EU 2007050100062 20070501 00062 WP 2007 5 1 07FDEA01569 1 20070424 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1059-1119 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 EXISTING LONGERON SPLICE REPAIR ON FWD CARGO COMPT FROM STA 1079 TO STA 1119 LONGERON 44 RT. INSTALL NEW LONGERON SECTI ON IAW SRM 53-10-00 FIG 1 VOL 1. 2 L 7 3 4F A22WE 2007050100063 20070501 00063 EU 2007 5 1 07FDEA01570 1 20070424 A 5754 STRUCTURE AIRBUS 310 A310324 3930206 EU ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 DENT IN FOLDING NOSE, KRUEGER FLAP RT. REPAIR PERFORMED BY FILLING THE DENT IAW SRM 51-73-10, APPROVED BY EA 6-5745-991 86 AND RAS/SA/040/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007050100065 20070501 00065 WP 2007 5 1 07FDEA01572 1 20070424 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP BS 580 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 NLG WHEEL WEEL LT VERTICAL BULKHEAD CRACK LONG .75" AT STA 580 Z=-47 REPAIR IAW SRM 53-30-00 FIG 6 VOL 1. 2 L 7 3 4F A22WE 2007050100067 20070501 00067 EU 2007 5 1 07FDEA01573 1 20070424 A 5710 TRACK AIRBUS 310 A310324 3930206 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 SEVERAL DAMAGES (IMPACTS) ON L/E TRACK NR 2 RT. REPAIR PERFORMED BY BLEND OUT IAW SRM 51-74-10 AND INSTALLING AN INFILL -PLATE IAW EA 6-5741-101246 AND RAS/BAE/1002809/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007050100070 20070501 00070 WP 2007 5 1 07FDEA01576 1 20070424 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP NLG WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 NLG WHEEL WELL QTY 6 CRACK ON RT VERTICAL BULKHEAD FROM STA 583 TO 592 FROM Z=-40 TO Z=-52 REPAIR IAW 53-30-00 FIG 6 SH2 VOL 1. 2 L 7 3 4F A22WE 2007050100072 20070501 00072 WP 2007 5 1 07FDEA01579 1 20070424 A 5754 WEB DOUG DC10 DC1010 3022110 WP NR 1 SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 RT WING FOUND CRACK QTY 1 ON WEB ON SLAT NR 1 REPAIR IAW SRM 57-00-01 FIG 12 VOL1. 2 L 7 3 4F A22WE 2007050100073 20070501 00073 WP 2007 5 1 07FDEA01580 1 20070424 A 5330 SKIN DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 397FE 46631 MODIFICATION AND REPAIR ASSESTMENT RT WING INBOARD AILERON FRONT SPAR WITH EXISTING REPAIR STA XIA 372 TO 374 REMOVED D OUBLER (EXISTING REPAIR), FOUND CRACKS. REMOVED AILERON RT INBOARD. REPAIRED SKIN DOUBLER. INSTALLED FILLER AND COVER IAW MM 20-50-02. INSTALLED AILERON AND CHECKED IAW MM 27-10-01-4. 2 L 7 3 4F A22WE 2007050100074 20070501 00074 WP 2007 5 1 MWEA070096 1 20070422 A 2910 B-NUT DOUG DC9 DC982 3022082 WP HYD LINE LEAKING A MWEA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 13 808ME 48070 ONE OR BOTH AIR CONDITIONING PACKS PUT OUT A FAINT HOT OIL SMELL, WHEN OPERATED BY THE APU. FOUND HYDRAULIC LEAK IN FRO NT OF APU AIR INLET, TIGHTENED B NUT. 2 L 7 2 4F A6WE 2007050100075 20070501 00075 WP 2007 5 1 07FDEA01585 1 20070424 A 5310 DOOR FRAME DOUG DC10 DC1010 3022110 WP BS 1305 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 397FE 46631 MODIFICATION AND REPAIR ASSESSMENT R3 DOOR ON JAMB STA 1305 SIDE LOWER FOUND WEB WITH EXISTING REPAIR REMOVED EXISTING REPAIR NOT IN COMPLIANCE WITH SRM 53-50-00 FIG 19. 2 L 7 3 4F A22WE 2007050100076 20070501 00076 CE 2007 5 1 BSAASDR0707 1 20070411 A 3297 WIRED14B22 WIRE BEECH 1900 1900D 1154162 CE MLG HANDLE CHAFED A BSAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 05 173YV UE173 WHEN GEAR HANDLE WAS SELECTED DOWN, THE LANDING GEAR INDICATION CD TRIPPED. CREW ABORTED LANDING AND FOLLOWED EMERGENCY PROCEDURES. CREW VERIFIED GEAR WAS DOWN AND LOCKED. A CHAFED WIRE WAS FOUND UNDER THE FLOOR BY THE PCB RACKS, WIRE NR D14B22. WIRE WAS REPAIRED, AND CHAFE PROTECTED. 2 L 7 2 4T RT A24CE 2007050100077 20070501 00077 CE 2007 5 1 DXTA200702160 1 20070428 A 3260 UNKNOWN CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG WARNING LIGHT E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 632QS 5605132 AFTER TAKE OFF THE RED GEAR UNLOCK LIGHT REMAINED ILLUMINATED. CYCLED THE GEAR DOWN, LIGHT EXTINGUISHED. [SUP 05-03-07] FOUND NOSE GEAR NOT SEATING IN UPLOCK. JACKED AIRCRAFT AND PERFORMED NOSE GEAR STRUT SERVICING PROCEDURE IAW CE560XL M M 12-14-00. PERFORMED SEVERAL GEAR SWINGS, AND LANDING GEAR AND GEAR INDICATION OPS CHECK NORMAL. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007050100078 20070501 00078 NE 2007 5 1 DXTA200702157 2 20070428 A 7200 ENGINE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE LEFT POWER LOSS E DXTA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 07 123QS RK486 PCEJA0766 LT ENGINE DID NOT MAKE TAKEOFF POWER (99.2) IT ONLY REACHED (98.0) RT ENGINE PERFORMED NORMALLY. [SUP 05-03-07] REPLA CED LT ENGINE HMU,P/N 790155-10, S/N F64557, WITH O/H'D UNIT P/N 790155-10, S/N F32591 IAW CHAPT73-20-02, CHAPT73-10-02 AND CHAPT73-10-12 OF P&W JT15D-D M, M, UNIT INSTALLED WITH NEW SEAL AND PACKING. 2 H 7 2 4F 4 F RT A16SW E25EA 2007050100080 20070501 00080 CE 2007 5 1 DXTA200702156 1 20070428 A 2750 UNKNOWN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE TE FLAPS MALFUNCTIONED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 309QS 5600509 WHEN FLAP HANDLE IS MOVED OUT OF (ZERO) POSITION, AIRCRAFT WILL ROLL RT. MANUALLY STOPPED THE ROLL AT 30 DEGREE BANK. AU TOPILOT WAS (OFF). [SUP 05-03-07] ADJUSTED RIGHT FLAP ACTUATOR ROD END OUT 1/2 TURN TO MATCH LEFT FLAP. IAW CE560 M/M CH 27-51-00 M/M CH 27-51-00, OPS CHECKED AND TRAVEL CHECKED GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2007050100081 20070501 00081 CE 2007 5 1 DXTA200702132 1 20070422 A 5210 62146292 CONTROL VALVE CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE DOOR SEAL INOPERATIVE E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 820QS 2631 5600650 AFTER FLIGHT, CABIN DOOR WOULD NOT OPEN FROM INSIDE, APPLIED EXCESSIVE FORCE MULTIPLE TIMES OVER 15 MINUTE PERIOD. HAD T O OPEN DOOR FROM OUTSIDE. TOOK A WHILE AND WAS VERY HARD FROM OUTSIDE ALSO. AIR PRESSURE WAS NOT RELEASING. REMOVED AND REPLACED MAIN CABIN DOOR SEAL INFLATION VALVE AND PERFORMED ADJUSTMENT AND TEST IAW MM CHAPT 36-11-02, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00053EN 2007050100082 20070501 00082 CE 2007 5 1 GUUA04210701 1 20070421 A 2697 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FIRE BOTTLE LOOSE A GUUA O OTHER J WARNING INDICATION CR CRUISE 1 SO 29 69547 UE189 FLIGHT 9253- DURING FLIGHT RT DISCHARGE LIGHT ILLUMINATED ON AND OFF. SECURED WIRES ON THE RT FIRE BOTTLE. 2 L 7 2 4T 4 T RT A24CE E26NE 2007050100084 20070501 00084 CE 2007 5 1 DXTA200702161 1 20070429 A 3240 UNKNOWN CESSNA 560 560XL 2076702 CE BRAKE SYSTEM MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 686QS 5605661 DURING START BRAKE LOW PRESS AND ANTI SKID INOP LIGHT CAME ON. IT WENT OUT AS RPM INCREASED, CAME ON AGAIN AS TAXI ST ARTED. BRAKE PRESS REMAINED OK. EMER BRAKE NOT USED. [SUP 05-03-07] REMOVED BRAKE LOW PRESSURE SWITCH AND INSTALLED NEW UNIT IAW CESSNA 560XL M/M CH. 32-44-20. LEAK AND OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A22CE 2007050100086 20070501 00086 EA 2007 5 1 040607 2 20070406 A 7324 FLOW DIVIDER GULSTM 500 500B 0141106 SW LYC O540 IO540E1A5 41532 EA FUEL SYSTEM LEAKING E ZJWA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 05 411ET 1621214 RL245448 THE RT ENGINE EXPERIENCED A LOSS OF POWER AND INDICATED A SIGNIFICANT INCREASE IN FUEL FLOW. THE ENGINE WAS SHUTDOWN AND A THE AIRCRAFT LANDED AT THE NEXT AVAILABLE AIRPORT. MAINTENANCE REVEALED THAT THE RETURN TO TANK LINE FROM THE FUEL FL OW DIVIDER WAS LOOSE AND LEAKING. THIS WOULD CAUSE A MASSIVE INCREASE IN FUEL FLOW. IT WAS A RELATIVELY LOW TIME INSTALL ATION AND POSSIBLY SOME TWIST IN THE LINE CAUSED IT TO BACKOFF. 1 H 7 2 3O 3 O 6A1 1E4 2007050100088 20070501 00088 CE 2007 5 1 DXTA200702162 1 20070429 A 3241 ANTI-SKID SYS CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 341QS 5600341 ANTI-SKID PULSES DURING NORMAL BRAKE USE. RETURNED TO DEPARTURE. [SUP 05-03-07] REMOVED & REPLACED A/S CONTROL BOX IAW CESSNA 560 M/M CHPT 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007050100089 20070501 00089 CE 2007 5 1 DXTA200702163 1 20070427 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 352QS 5600352 BRAKES NOT WORKING WELL AT SPEEDS ABOVE 5 KNOTS. WITH ANTI SKID OFF BRAKES WORK FINE. [SUP 05-16-07] INSPECTED ANTI SK ID WIRING FOUND BAD GROUND FROM P1007 LT WHEEL TRANSNDUCER. CLEANED CORROSION FROM PLUG PL008. PERFORMED ANTISKID SYSTEM OPS CHECK OPS CHECKS GOOD ALL WORK DONE IAW CE-560 M.M. 32-42-00-710. 2 L 7 2 4F 4 F RT A22CE E25EA 2007050100090 20070501 00090 CE 2007 5 1 GUUA04200702 1 20070420 A 5330 SKIN BEECH 1900 1900D 1154162 CE BS 327 CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 82539 UE168 SCHEDULED INSPECTION DISCOVERED BELLY SKIN CORROSION AT FS 327.830 BETWEEN STRINGER 15R THRU 14R. REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW STRUCTURAL REPAIR MANUAL 51-70-06. 2 L 7 2 4T RT A24CE 2007050100094 20070501 00094 CE 2007 5 1 GLBA20060941 1 20070424 A 2731 HINGE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE ELEVATOR TRIM LACK OF LUBE A GLBA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 03 202UX UE202 FLIGHT 5067, PILOT REPORTED THAT THE ELEVATOR TRIM STUCK TWICE DURING FLIGHT AND WAS UNABLE TO ADVANCE TRIM PAST 1/2 NOT CH NOSE DOWN POSITION. MAINTENANCE CLEANED AND LUBED AFFECTED HINGE AREAS, AND AN OPERATIONAL CHECK FLIGHT WAS PERFORMED WHICH WAS FOUND SATISFACTORY. SUBSEQUENT MX CHECK UPON ARRIVAL IN DENVER OF THE ELEVATORS WERE OK. 2 L 7 2 4T 4 T RT A24CE E26NE 2007050100096 20070501 00096 CE 2007 5 1 DXTA200702120 1 20070419 A 3234 99145514 CONTROL HANDLE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 970QS 5424 7500070 LANDING GEAR WILL NOT RETRACT. REPLACED LANDING GEAR CONTROL HANDLE IAW MM CH 32-30-01. LANDING GEAR CHECKS OK. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007050100098 20070501 00098 CE 2007 5 1 DXTA200702122 1 20070420 A 3240 UNKNOWN RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP BRAKE ASSY MALFUNCTIONED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 858QS 258691 BRAKES REQUIRED EXCESSIVE INPUT TO SLOW AIRCRAFT. PEDALS ARE SOFT BOTH SIDES. THOROUGHLY CHECKED NOSE GEAR STEERING ME CHANISM. FOUND NO OBVIOUS PROBLEMS. CONDUCTED TAXI CHECK WITH FLIGHT CREW. TAXI CHECK GOOD. WORK PERFORMED IN REFERENCE TO MM CHAPTER 32-50-00. FOR DETAILS REFER TO FAS WO NR 07-953. 2 L 7 2 4F 4 F RT A3EU E6WE 2007050100099 20070501 00099 WP 2007 5 1 07FDEA01634 1 20070426 A 5230 DOOR DOUG MD10 MD1010F 3022112 WP CARGO DOOR CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 68050 47804 FWD PIT HAS CORROSION IN THE AFT CORNER BETWEEN DOOR SEAL AND BEAM. [SUP 05-30-07] REMOVED CORROSION FROM RAIL AND FO UND MATERIAL LOSS TO WITHIN ALLOWABLE LIMITS IAW DC/MD 10 SRM 53-50-00 VOL I FIG. 15A. ALODINED AND PRIMED REWORK AREA IAW DC/MD 10 SRM 51-21-01, VOL II PG 21 AND24. REMOVED CORROSION FROM FRAME AND WEB AND FOUND MATERIAL LOSS FOR BOTH T O EXCEED ALLOWABLE LIMITS IAW DC/MD 10 SRM 53-00-01 VOL I FIG 1B. REPAIRED FRAME IAW FED EX EA 8-5350- 109161 "FUSEL AGE-FWD LOWER CARGO DOOR JAMB FRAME STA 1002 CORD-REPAIR" REPAIRED WEB IAW DC/MD10 SRM 53-00-01 VOLI FIG 10. 2 L 7 3 4F RT A22WE 2007050100103 20070501 00103 2007 5 1 QXEA200700651 4 20070422 A 3497 MILT7928115 TERMINAL BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA BROKEN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 409QX 4051 PDX FLIGHT NR 2527: CAPTAIN SIDE ALT FAIL MESSAGE AFTER PUSH BACK. AIRCRAFT RETURNED TO GATE. MAINTENANCE REPLACED BROKE N RING TERMINAL AT GROUND STUD GS15 IAW Q400 SDM 34-11-01, SHEET 2 OF 8, PAGE 2. ICP OPS TESTED GOOD IAW MTC 6316103. AI RCRAFT REMAINS CAT III QUALIFIED. PLACARD REFLECTS CAT III. MTX CONTROL HAD BEEN NOTIFIED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2007050100105 20070501 00105 NM 2007 5 1 QXEA200700654 1 20070423 A 2750 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA TE FLAPS MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 422QX 4150 BIL FLIGHT NR 2411: FLAP POWER CAUTION LIGHT. AIRCRAFT RETURNED TO GATE. MAINTENANCE CLEARED FLAP POWER CAUTION NVMAND C/W IAW DH8-400-SL-27-002A. NO FURTHER FAULTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2007050100110 20070501 00110 CE 2007 5 1 DXTA200702154 1 20070427 A 2741 UNKNOWN CESSNA 560 560XL 2076702 CE TRIM SYS MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 600QS 5605664 PILOTS AUTO PILOT TRIM DISCONNECT BUTTON POPPED OUT OF YOKE IN FLIGHT. [SUP 05-03-07] SECURED PILOT A/P TRIM DISCONNEC T SWITCH PER STANDARD PRACTICE. 2 L 7 2 4F RT A22CE 2007050100111 20070501 00111 CE 2007 5 1 DXTA200702155 1 20070427 A 2720 RUDDER PEDAL CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE RUDDER CONTROL DAMAGED E DXTA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 07 624QS 5605302 AFTER ROTATION, THE YAW DAMPER WOULD NOT ENGAGE AND WHEN WE TURNED LT, THE LT RUDDER PEDAL WOULD NOT MOVE. AFTER ENGAG ING AND DISENGAGING THE YAW DAMPER THE RUDDER OPERATED NORMALLY. ON THE GROUND WE COULD FEEL AND HEAR GRINDING SOUND IN THE RUDDER PEDALS WHILE TAXIING. [SUP 05-03-07] REMOVED AND REPLACED THE AUTOPILOT CONTROLLER IAW THE CESSNA 560XL MAIN TENANCE MANUAL 22-11-03. OPS CHECK OF THE AUTOPILOT CONTROLLER GOOD IAW THE HONEYWELL PRIMUS 1000 INTEGRATED AVIONICS S YSTEM TEST AND FAULT ISOLATION MANUAL FOR THE EXCEL. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007050100114 20070501 00114 CE 2007 5 1 DXTA200702143 1 20070426 A 2150 ACM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 931QS 7500064 FOWL ODOR & LIGHT VISIBLE SMOKE IN CABIN COMING FROM ACMS. REMOVED AND REPLACED CABIN AIR CYCLE MACHINE. OPS. AND LEAK C HECKED GOOD. IAW. 750 M/M CH. 21-51-00. OLD P/N: 738384-33. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007050100115 20070501 00115 CE 2007 5 1 DXTA200702146 1 20070426 A 3150 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL WARNING LIGHT E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 951QS 7500151 TAKEOFF ABORTED DUE TO MACH TRIM OFF AND YD DAMP OFF CAS MESSAGE PRIOR TO 80 KTS. [SUP 05-02-07] CONFIRMED SPLIT IN AIR SPEED INDICATION AS WELL AS CONFIRIMED DISCREPANCY CAS MESSAGES. TROUBLESHOT TO A LARGE AMOUNT OF WATER IN PITOT PLUMBIN G. PURGED PLUMBING. OPERATIONAL CHECK AND LEAK CHECKS GOOD. NO SPLIT NOTED POST MAINTENANCE. MAINTENANCE IAW 750 MM CHAP TER 34-11-01 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007050100118 20070501 00118 CE 2007 5 1 DXTA200702138 1 20070424 A 3230 PIVOT CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG LACK OF LUBE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 334QS 5600434 ON DEPARTURE, GEAR SELECTED UP AND GEAR UNSAFE LIGHT REMAINED ILLUMINATED ALONG WITH HYD PRESS LIGHT ON FOR APPROX 1.5 M INS. NOSE WHEEL FINALLY CAME UP LIGHTS WENT OUT, LOUD NOISE FROM NOSE WHEEL AREA HEARD. LUBED LT MLG PIVOT BOLT IAW AC MM CHAPTER 32-10-00. OPS CHECKED LAND GEAR NO DEFECTS SERVICED HYDRAULIC SYSTEM IAW AC MM 12-12-01. 2 L 7 2 4F 4 F RT A22CE E25EA 2007050100119 20070501 00119 CE 2007 5 1 DXTA200702144 1 20070426 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG WEAK E DXTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 341QS 5600341 NO BRAKES ON THE COPILOTS SIDE, BRAKE PEDALS VERY SPONGY. PERFORMED BRAKE BLEED IAW CESSNA 560 MM CH 32-42-00. PERFORME D LEAK CHECK. NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A22CE E25EA 2007050100120 20070501 00120 CE 2007 5 1 DXTA200702145 1 20070426 A 3150 WARNING LIGHT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LT AILERON ILLUMINATED E DXTA O OTHER F FLT CONT AFFECTED LD LANDING 1 GL 07 944QS 7500144 FLIGHT CONTROL PAGE INDICATES LT AILERON LOW AND INDICATES LIMITED TRAVEL. [SUP 05-02-07] TROUBLESHOT & VERIFIED AILERO N TRAVELS TO BE NORMAL - LH AILERON INDICATES NORMALLY. FOUND RH INDICATION OUT OF ALIGN & FOUND FLEXIBLE COUPLING LOOSE AT SENSOR. REMOVED & REPLACED FLEXIBLE COUPLING & ADJUSTED POSITION SENSOR IAW 750 MM CHAPTER 57-60-00. OPS CHECK NORMA L. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007050100122 20070501 00122 NE 2007 5 1 DXTA200702148 2 20070426 A 7200 ENGINE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LEFT MALFUNCTIONED E DXTA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 333QS 5600333 LT ENGINE SHUTS DOWN WHEN THROTTLE IS BROUGHT TO FLIGHT IDLE DURING SPEED BRAKE CHECK. [SUP 05-02-07] ADJUSTED LT ENG FLOW DIVIDER PUSH ROD IAW 560MM 76-11-00 OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2007050100126 20070501 00126 CE 2007 5 1 DXTA200702159 1 20070428 A 2120 UNKNOWN CESSNA 750 750 2076810 CE COCKPIT ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 990QS 7500190 NOXIOUS BURNED OIL ODOR IN COCKPIT DURING GROUND OPS. [SUP 05-03-07] GAINED ACCESS FOR APU FOUND OIL LEAK AT CHIP DET ECTOR PLUG . BURN OIL TRAVELING IN THE CABIN. FIXED AND CLEANED OIL LEAK. OPS CHECKED AND LEAK GOOD. MAINTENANCE PERFOR MED IAW CESSNA CITATION 750-AMM 49-10-00. 2 L 7 2 4J RT T00007WI 2007050100127 20070501 00127 NM 2007 5 1 SWAA072096 1 20070427 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 520 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050100128 20070501 00128 NM 2007 5 1 SWAA072097 1 20070427 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 520 S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050100129 20070501 00129 NM 2007 5 1 SWAA072099 1 20070428 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 685 S3L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050100130 20070501 00130 NM 2007 5 1 SWAA072109 1 20070428 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM BS 827 S14L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050100132 20070501 00132 NM 2007 5 1 SWAA072102 1 20070428 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 727B S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050100134 20070501 00134 NM 2007 5 1 SWAA072089 1 20070427 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED A1 CHECK, FOUND FWD LEFT CABIN BULLNOSE EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007050100135 20070501 00135 NM 2007 5 1 SWAA072090 1 20070427 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 225WN 34333 EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007042600188 20070426 00188 NM 2007 4 26 DU4R2007087 1 20070411 A 5753 113N21081 TORQUE TUBE BOEING 757 757232 1384965 NM TE FLAP CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND CORROSION INSIDE LT I/B T/E FLAP FAIL/SAFE TORQUE TUBE. REPAIRED BY REMOVING AND REPLACING TORQUE TUBE P/N 113N21 08-1 AND 2 FITTINGS I/B AND O/B IAW B757 AMM 27-51-05 AND DELTA EA 06-097981-14 REV A. 2 L 7 2 4F RT A2NM 2007042600189 20070426 00189 NM 2007 4 26 DU4R2007088 1 20070411 A 5753 113N21061 TORQUE TUBE BOEING 757 757232 1384965 NM TE FLAP CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND CORROSION INSIDE RT I/B T/E FLAP FAIL/SAFE TORQUE TUBE. REPAIRED BY REMOVING AND REPLACING TORQUE TUBE ASSY P/N 1 13N2106-1AND I/B AND O/B CARRIAGE HALVES IAW B757 AMM 27-51-05 AND DELTA EA 06-097981-14 REV A . 2 L 7 2 4F RT A2NM 2007042600190 20070426 00190 NM 2007 4 26 DU4R2007090 1 20070412 A 5313 STRINGER BOEING 757 757232 1384965 NM BS 1500-1520 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND CORROSION IN AFT PIT S-29L O/B SIDE FROM BS 1500 TO BS 1520 LT. REPAIRED BY FABRICATING AND INSTALLING REPAIR DOU BLER 8 BY 3 BY FROM 7075-T6 .090 IAW 51-20-01, 53-40-02 AND 53-00-03. 2 L 7 2 4F RT A2NM 2007042600191 20070426 00191 NM 2007 4 26 DU4R2007091 1 20070417 A 5313 STRINGER BOEING 757 757232 1384965 NM BS 1530 S28L CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND CORROSION AFT PIT S-28L AT BS 1530 LT. REPAIRED BY CUTTING OUT CORRODED SECTION, FABRICATED AND INSTALLED REPAIR SPLICE 8.5 BY .090 FROM BAC1498-204 T62 EXTRUSION IAW B757 SRM 53-00-53, 51-20-01 AND 51-40-02. 2 L 7 2 4F RT A2NM 2007042600192 20070426 00192 NM 2007 4 26 DU4R2007092 1 20070414 A 5313 STRINGER BOEING 757 757232 1384965 NM BS 1500-1520 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND CORROSION AFT PIT S-29R AT BS 1500 TO BS 1520 RT. REPAIRED BY CUTTING OUT CORRODED SECTION, FABRICATED AND INSTAL LED REPAIR SPLICE 8.5 BY 3 .090 FROM BAC1498-204 EXTRUSION IAW B757 SRM 53-00-53, 51-20-01 AND 51-40-02. 2 L 7 2 4F RT A2NM 2007042600193 20070426 00193 NM 2007 4 26 DU4R2007093 1 20070416 A 5313 STRINGER BOEING 757 757232 1384965 NM BS 1460 S29L CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND CORROSION AROUND RIVET IN AFT CARGO PIT JUST FWD OF BS 1460 AT S-29L. REPAIRED BY REMOVING AND REPLACING FABRICAT ED STRINGER SPLICE 12 BY 3 FROM 7075-T6 .090 IAW B757 SRM 53-00-02, 51-20-01 AND 53-60-03. 2 L 7 2 4F RT A2NM 2007042600194 20070426 00194 NM 2007 4 26 DU4R2007094 1 20070416 A 5340 69455792930 FITTING BOEING 757 757232 1384965 NM BS 1400-1420 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND CORROSION IN AFT PIT ON LOWER C2 DOOR SILL AREA FITTINGS AT BS 1400 AND 1420 S-27R. REPAIRED BY REMOVING AND REPL ACING 2 FITTINGS P/N 69-45579-29 AND 2 P/N 69-45579-30 IAW B757 SRM 51-40-02 AND 51-20-01. 2 L 7 2 4F RT A2NM 2007042600195 20070426 00195 NM 2007 4 26 DU4R2007095 1 20070419 A 5322 SHEAR TIE BOEING 757 757232 1384965 NM BS 1460 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND CORROSION IN AFT PIT ON SHEAR CLIP AT BS 1460 S-25, 26R. REPAIRED BY REMOVING SHEAR CLIP, FABRICATING AND INSTALL ING SHEAR CLIP 1 BY 1 BY 8 FROM 7075-T6 .050 IAW B757 SRM 53-00-07, 51-20-01, 51-40-02. 2 L 7 2 4F RT A2NM 2007042600196 20070426 00196 NM 2007 4 26 DU4R2007096 1 20070418 A 5322 SHEAR TIE BOEING 757 757232 1384965 NM BS 1280 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND CORROSION IN AFT PIT SHEAR TIE AFT SIDE BS 1280 S-28 - S-29L. REPAIRED BY FABRICATING AND INSTALLING SHEAR TIE 6 BY 2 FROM 7075-T6 .063 IAW B757 SRM 53-00-07, 51-40-2 AND 51-20-01. 2 L 7 2 4F RT A2NM 2007042600197 20070426 00197 NM 2007 4 26 DU4R2007097 1 20070412 A 5322 SHEAR TIE BOEING 757 757232 1384965 NM BS 1260 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 604DL 22811 FOUND CORROSION ON AFT PIT LWR ANGLE AND SHEAR TIE BS 1260 FWD SIDE OF MAIN FRAME BETWEEN S-28R AND S-29R. REPAIRED BY REMOVING CORRODED SHEAR TIE AND INSTALLING NEW SHEAR TIE P/N 140N2006-103 IAW B757 SRM 51-20-01 AND 51-40-02. FABRICATE D AND INSTALLED SHEAR ANGLE 6 BY 22 FROM BAC1505-100962 IAW B757 DRAWING NR 140N2006. 2 L 7 2 4F RT A2NM 2007042600198 20070426 00198 NE 2007 4 26 DHLA200700022 2 20070418 A 7230 COMPRESSOR BOEING 727 727223 1384074 NM PWA JT8 JT8D15A 52051 NE ENGINE STALLED A DHLA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 05 754DH 22008 REJECTED TAKEOFF AT APPROX 20 KNOTS DUE TO AN AUTOPACK TRIP AND AN APPARENT COMPRESSOR STALL. 2 L 7 3 4F 4 F A3WE E2EA 2007042600199 20070426 00199 NM 2007 4 26 QXEA200700598 1 20070411 A 2120 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM CABIN ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 09 420QX 4147 LAX FLIGHT NR 2470: ON DESCENT, FA ADVISED OF ODOR OF FUMES NEAR ROW 18. TURNED NR 2 BLEED OFF, NO CHANGE WITH BLEED NR 1 OFF AND NR 2 ON, ODOR DISSIPATED. MAINTENANCE INSPECTED NR 2 ENGINE AND FOUND NO DISCREPANCIES. RAN NR 1 AND NR 2 E NGINE. CYCLED ON NR 1 BLEED. NO ODOR OR FUMES NOTICED. CYCLED ON NR 2 BLEED WITH NO ODOR OR FUMES NOTICED. CHECKED O IL LEVEL WHICH WAS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007042600200 20070426 00200 2007 4 26 QXEA200700599 3 20070411 A 6197 CONNECTOR BOMBDR DHC8 DHC8402 1390042 NM PEC DIRTY A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 421QX 4149 SEA FLIGHT NR 2418: POWER PLANT MESSAGE AFTER ENGINES STARTED. AIRCRAFT RETURNED TO GATE. MAINTENANCE INTERROGATED CDS . FOUND FAULT CODES 130B ON 32 PROP AND 274 ON NR 1 PROP. CLEARED FAULTS PER Q400 AMM TASK 61-20-36-070-801. CLEANED ALL ELECTRICAL CONNECTORS ON NR 1 AND NR 2 PEC AND PCU. PERFORMED GROUND IDLE ENGINE RUN PER AMM TASK 71-00-00-868-811. POWER PLANT MESSAGE AND FAULT CODES DID NOT REOCCUR. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007042600201 20070426 00201 NM 2007 4 26 QXEA200700600 1 20070411 A 5270 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR WARNING LIGHT A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 414QX 4061 SEA FLIGHT NR 2386: DURING TAXI OUT, FUSELAGE DOOR WARNING LIGHT ILLUMINATED. AFT CARGO DOOR SHOWED OPEN. AIRCRAFT RET URNED TO GATE. MAINTENANCE C/W GVI OF AFT CARGO DOOR WITH NO DEFECTS NOTED. C/W OPERATIONAL TEST OF THE AFT BAGGAGE DO OR IAW TASK 52-31-00-710-801. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007042600202 20070426 00202 EA 2007 4 26 QXEA200700565 1 20070404 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 202 S15R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - LIGHTNING STRIKE DAMAGE ON EDGE OF SKIN AT FS 202.00 STRINGER 15R. REPAIRED IAW REO670-53-21-257. 2 L 7 2 4F RT A21EA 2007042600203 20070426 00203 EA 2007 4 26 QXEA200700566 1 20070331 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 210 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - LIGHTNING STRIKE DAMAGE AT STRINGER 15R 2.5" FORWARD OF FS 210.00. REPAIRED IAW REO670-53-21-257. 2 L 7 2 4F RT A21EA 2007042600204 20070426 00204 EA 2007 4 26 QXEA200700567 1 20070331 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 210 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - LIGHTNING STRIKE DAMAGE AT STRINGER 15R 0.9" FORWARD OF FS 210.00. REPAIRED IAW REO670-53-21-257. 2 L 7 2 4F RT A21EA 2007042600205 20070426 00205 EA 2007 4 26 QXEA200700568 1 20070330 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 310 S16R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - LIGHTNING STRIKE DAMAGE AT STRINGER 16R 5.5" FORWARD OF FS 310.00. REPAIRED IAW REO670-53-21-257 AND SRM 51-21- 06. 2 L 7 2 4F RT A21EA 2007042600206 20070426 00206 EA 2007 4 26 QXEA200700561 1 20070330 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 296 S17R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - LIGHTNING STRIKE DAMAGE AT STRINGER 17R 4.5" AFT OF FS 296.00. REPAIRED IAW REO670-53-21-257 AND SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007042600207 20070426 00207 EA 2007 4 26 QXEA200700562 1 20070330 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 296 S17R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - LIGHTNING STRIKE DAMAGE AT STRINGER 17R 3.5" AFT OF FS 296.00. REPAIRED IAW REO670-53-21-257. AND SRM 51-42-06 . 2 L 7 2 4F RT A21EA 2007042600208 20070426 00208 EA 2007 4 26 QXEA200700564 1 20070330 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 193 S16R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - LIGHTNING STRIKE DAMAGE ON DOOR CUTOUT AT FS 193.00 6" ABOVE STRINGER 16R. REPAIRED IAW REO670-53-21-257 AND S RM 51-42-06. 2 L 7 2 4F RT A21EA 2007042600209 20070426 00209 EA 2007 4 26 QXEA200700560 1 20070330 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 296 S16R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - LIGHTNING STRIKE DAMAGE AT FS 296.00 4.7" DOWN OF STRINGER 16R. REPAIRED IAW REO670-53-21-257 AND SRM 51-42-06 . 2 L 7 2 4F RT A21EA 2007042600210 20070426 00210 EA 2007 4 26 QXEA200700569 1 20070330 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 453 S15R DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 C3 OKC - LIGHTNING STRIKE DAMAGE AT FS 453.00 2.7" DOWN OF STRINGER 15R. REPAIRED IAW REO670-53-21-257. 2 L 7 2 4F RT A21EA 2007042600211 20070426 00211 NM 2007 4 26 DHL2007743506 1 20070406 A 5711 SPAR BOEING 727 727225 1384077 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 DISCOVERED WHILE IN "A" CHECK A/C 743DH AT MCO, THEN FERRIED TO VQQ REF ASTAR NR 078282 AND NR 078290. LT WING AFT FALS E SPAR ANGLE JUST FWD OF NR 7 SPOILER FITTING CRACKED IN ANGLE APPROX 2 1/2" LONG STARTING FROM INBD AND RUNNING BELOW F ASTENERS. CUT OUT DAMAGE ANGLE LT WING FWD NR 7 SPOILER FITTING DIM, 20 1/2" BY 3" IAW SB727-57-158 REV 1 FIG 6. FABRI CATED NEW ANGLE SECTION MAT, USED BAC1514-1437 7075T6 PO NR 9004179 DIM 20 1/2" BY 3". FABRICATED 2 ANGLE REPAIR MAT US ED 7075T6 .071 PO NR 9004201 DIM 15" BY 2.75" AND 12.5" BY 2.75 INCH AND RADIUS FILLER MAT. USED 7075T6 .090 PO NR 90041 71 DIM 11.75" BY 1.5" IAW SB727-57-158 REV 1 FIG 6. REMOVED DOUBLER AS REQ IAW SB727-57-158 REV 1 FIG 6. FABRICATED NE 2 L 7 3 4F A3WE 2007042600212 20070426 00212 NM 2007 4 26 F3LA200700054 1 20070330 A 5315 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM BETWEEN FR 68 AND FR 69 AT Y1292. FLOORBEAM FOUND TO BE OUT OF LIMITS PER A319 ARM 51-00-14, FIG 101. REPLACED FLOORBEAM IAW A319 SRM 51-42-11 AND SRM 51-44-11. 2 L 7 2 4F RT A28NM 2007042600213 20070426 00213 NE 2007 4 26 SA07028 2 20070418 A 7321 8061532 HMU AIRBUS A321 A321211 3930370 EU GE CFM56 CFM56* 13802 NE ZONE 400 LEAKING A USAA O OTHER E K VIBRATION/BUFFET FLUID LOSS DE DESCENT 1 EA 19 179UW 18256 1 1521 575200 DTW FLT 902 EN ROUTE CLT TO DTW, DURING DESCENT, BELOW FL 290, ENGINE 1 BEGAN TO RUMBLE AND VIBRATE. THE AUTOTHROTTLE W AS DISCONNECTED AND THE NUMBER 1 ENGINE WAS BROUGHT BACK IDLE AND THE VIBRATIONS STOPPED. AT 7,000 FEET AND 210 KNOTS, THE AUTOTHROTTLES WERE RE-ENGAGED AND ALL OPERATIONS WERE NORMAL. AFTER LANDING AND ARRIVAL AT THE GATE, THE GROUND CRE W NOTICED A TRAIL OF FUEL THAT FOLLOWED THE NUMBER ENGINE, ENDING IN A PUDDLE UNDERNEATH IT. ALSO, A 1,000 POUND DIFFER ENCE IN FUEL BURN BETWEEN THE LEFT AND RIGHT FUEL TANKS WAS NOTED. MAINTENANCE FOUND THE NUMBER 1 ENGINE HMU LEAKING. THE HMU WAS CHANGED WITH THE ENGINE. THE ENGINE WAS CHANGED DUE TO OTHER PERFORMANCE ISSUES NOT RELATED TO THE FUEL LEA 2 L 7 2 4F 4 F RT A28NM E2GL 2007042600245 20070426 00245 EU 2007 4 26 USAA070282 1 20070418 A 5311 FRAME AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 176UW 1499 FOUND CORROSION FR 66 - Y1732. INSTALLED DOUBLER PER SRM 53-41-14; CORROSION TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1 /2 SQ IN. 2 L 7 2 4F RT A28NM 2007042600246 20070426 00246 EU 2007 4 26 USAA070283 1 20070418 A 5315 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 176UW 1499 FOUND CORROSION FWD OF L4 DOOR SILL AT FRAME 66. CUT OUT DAMAGED AREA AND FABRICATED FILLER PER SRM 53-41-14; CORROSION TASK JA-260-53500; LEVEL 1 DEFECT SIZE: 1/2" DIA. 2 L 7 2 4F RT A28NM 2007042600247 20070426 00247 NM 2007 4 26 USAA070284 1 20070418 A 5310 6545413174 BEAM BOEING 737 737301 1384611 NM BS 614 CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 590US 23935 FOUND BEAM CHAFED UPPER SURFACE OF RT AIR CONDITINING PACK PR BAC AT CHORD BS 614.90. INSTALLED REPAIR STRAP PER EA 986 02A, DEFECT SIZE: .6" BY .5" BY .020" 2 L 7 2 4F RT A16WE 2007042600248 20070426 00248 NM 2007 4 26 USAA070285 1 20070418 A 5310 6545413173 BEAM BOEING 737 737301 1384611 NM BS 548-637 CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 590US 23935 FOUND CHAFED UPPER SURFACE BEAM CHORD IN LEFT A/C PACK BAY AT BS 548.85, 569.70, 637.50. FABRICATED AND INSTALLED REPAI R STRAPS PER EA 98602A, DEFECT SIZE: .6" BY .5" X .010" TO .025". 2 L 7 2 4F RT A16WE 2007042600249 20070426 00249 NM 2007 4 26 USAA070286 1 20070418 A 5330 SKIN BOEING 737 737401 1384701 NM BS 1156 S12R WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 FOUND SKIN WORN STA 1156 S12R LOWER LT AFT HORIZ STAB ATTACH CUT OUT. REMOVED AND FABRICATED NEW PER DWG 65-48240, MSM 10-11, DEFECT SIZE: 1/2" AREA. 2 L 7 2 4F RT A16WE 2007042600250 20070426 00250 NM 2007 4 26 USAA070299 1 20070418 A 5320 65770651 INTERCOSTAL BOEING 737 737401 1384701 NM BS 294 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 FOUND CORROSION BS 294+9 LBL 12, ON INTERCOSTAL. DEFECTIVE PART REPLACED WITH NEW PER SRM 51-10-02; CORROSION TASK C53- 107-02; LEVEL 2, DEFECT SIZE: 1/2". 2 L 7 2 4F RT A16WE 2007042600251 20070426 00251 NM 2007 4 26 USAA200704004 1 20070422 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 450UW 24933 1.5" CRACK FOUND AT L2 DOOR LOWER HINGE CUT OUT. INSTALLED DOUBLER/TRIPLER PER EA 84451. 2 L 7 2 4F RT A16WE 2007042600252 20070426 00252 NM 2007 4 26 USAA070331 1 20070425 A 5347 SEAT TRACK BOEING 737 737401 1384701 NM BS 344-356 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 FOUND SEAT TRACK CORRODED, BETWEEN BS 344-356, LBL 24. REPLACED SEAT TRACK PER SRM 53-00-52 AND EA 98591; CORR TASK C53 -107-02; LEVEL 2, DEFECT SIZE: 12". 2 L 7 2 4F RT A16WE 2007042600253 20070426 00253 NM 2007 4 26 USAA070330 1 20070425 A 5712 RIB BOEING 737 737401 1384701 NM RT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 FOUND CRACKED LOWER CHORD RT WBL 135.5 INSPAR RIB. INSTALLED REPAIR PARTS PER EA 98573, DEFECT SIZE: .05. 2 L 7 2 4F RT A16WE 2007042600254 20070426 00254 NM 2007 4 26 USAA070329 1 20070425 A 5712 RIB BOEING 737 737401 1384701 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 FOUND CRACK, LOWER CHORD OF LT WBL 135.5 INSPAR RIB. REMOVED DAMAGED AREA AND INSTALLED REPAIR PARTS PER EA 98574, DEFE CT SIZE: .05". 2 L 7 2 4F RT A16WE 2007042600255 20070426 00255 NM 2007 4 26 USAA070328 1 20070425 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 360 S14L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 FOUND ANGLE CRACKED, STR 14L, STA 360, AT LOCK FASTENER COMMON TO TIE CLIP JUST FWD OF FRAME 360. FAB'D NEW ANGLE PER S RM 51-10-02 PER SR 51-10-02, DEFECT SIZE: .5". 2 L 7 2 4F RT A16WE 2007042600256 20070426 00256 2007 4 26 USAA070327 4 20070425 A 2565 ATTACH FITTING BOEING 737 737401 1384701 NM AFT GIRT BAR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 FOUND CORROSION AFT GIRT BAR ATTACH FITTING, BS 344, S17L. FAB'D NEW ATTACH FITTING PER DWG 65C16121; CORROSION TASK C5 3-107-01; LEVEL 2, DEFECT SIZE: 1/2". 2 L 7 2 4F RT A16WE 2007042600257 20070426 00257 EU 2007 4 26 USAA070326 1 20070425 A 5315 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 170US 1462 FOUND CORROSION AROUND SCREW HOLE, FRAME 66, Y-1292. CUT OUT DAMAGE, INSTALLED FILLER AND REPAIR ANGLES PER SRM 53-41-1 4, PRINCIPLE 6; CORROSION TASK JA-260-535, DEFECT SIZE: 1". 2 L 7 2 4F RT A28NM 2007042600258 20070426 00258 EU 2007 4 26 USAA070325 1 20070425 A 5315 D5311460202 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSLEAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 170US 1462 FOUND CORROSION FLOORBEAM -Y254 BETWEEN FR 19 AND 20. REMOVED CORROSION AND INSTALLED FILLER AND DOUBLER PER SRM 53-00- 14, FIG 204, CORROSION TASK JA-220-53500, DEFECT SIZE: 1" BY 1". 2 L 7 2 4F RT A28NM 2007042600259 20070426 00259 NM 2007 4 26 USAA200704005 1 20070423 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 727D S24L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 23704 CRACK FOUND AT STA 727D + 18" AND S24L. INSTALLED DOUBLER PER SRM 53-00-01 AND TR 53-60-03A. 2 L 7 2 4F RT A16WE 2007042600260 20070426 00260 NM 2007 4 26 SB07033 1 20070419 A 2133 7207375 OUTFLOW VALVE BOEING 737 737401 1384701 NM CABIN PRESSURE FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 424US 53962 175 23991 PIT FLT1482 EN ROUTE FROM DCA TO IND, CREW REPORTED PRESSURIZATION PROBLEMS. IN AUTO, STANDBY OR MANUAL DC PRESSURIZATI ON MODE, AS CABIN APPROACHES APPROXIMATELY 7.4 PSI, THE CABIN BECOMES UNCONTROLLABLE WITH CLIMB RATE IN EXCESS OF 2,000 FPM WITH PACKS ON HIGH. OPERATIONS DECIDED TO DIVERT AIRCRAFT TO PIT DUE TO AIRCRAFT HISTORY. FLIGHT LANDED IN PIT WIT HOUT FURTHER INCIDENT. MAINTENANCE DUPLICATED PROBLEM AND FOUND LEFT SAFETY RELIEF VALVE OPENING AT AROUND 6.5 TO 7 PSI . REPLACED SAFETY RELIEF VALVE. PRESSURIZED AIRCRAFT AND FOUND RELIEF VALVES TO OPEN AT 8.3 PSI. REFERENCE MM 21-32-2 1. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2007042600261 20070426 00261 NE 2007 4 26 SB07034 2 20070422 A 7200 9325M85G03 ENGINE BOEING 737 737401 1384701 NM GE CFM56 CFM56* 13802 NE LEFT FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 EA 19 422US 48706 6317 23989 725124 BWI FLT1517 DURING CLIMB-OUT FROM DCA, EN ROUTE TO TPA, CREW REPORTED THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMI NATED AND REMAINED ON. CREW DECLARED AN EMERGENCY, SHUT DOWN THE NR 1 ENGINE AND DIVERTED TO BWI. FLIGHT LANDED WITHOU T FURTHER INCIDENT. MAINTENANCE FOUND METAL IN THE NR 1 ENGINE FORWARD CHIP DETECTOR. CHIP ANALYSIS REVEALED M50 BEARI NG MATERIAL. REMOVED AND REPLACED NR 1 ENGINE ASSEMBLY PER JOB CARD JK71-00-01. OPERATIONAL CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2007042600263 20070426 00263 NM 2007 4 26 C36001 1 20070331 A 2432 UNKNOWN BOEING 747 747200F 1384866 NM PWA JT9 JT9D7R4G2 52054 NE UNKNOWN A Q4TA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 01 299JD 24196 P725311 2 HOURS AFTER TAKEOFF ELECTRICAL ODOR IN COCKPIT. OBSERVED MAIN BATTERY VOLTAGE DROPPING THROUGH 22 VOLTS. WITHIN 10 MIN UTES VOLTAGE HAD DROPPED TO 13 VOLTS AND ODOR WAS STRONGER. PULLED MAIN BATTERY CHARGER CIRCUIT BREAKER, VOLTAGE (BATTER Y) STOPPED DROPPING AND ODOR DISSIPATED. 2 L 7 4 4F 4 F RT A20WE E3NE 2007042600264 20070426 00264 CE 2007 4 26 DXTA200702139 1 20070425 A 3260 BULB CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG INDICATOR INOPERATIVE E DXTA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 900QS 7500123 ON FINAL APPROCH NOSE GEAR INDICATOR LIGHT DID NOT ILLUMINATE WHEN GEAR WAS SELECTED. [SUP 05-02-07] CLEANED CONNECTOR OF NOSE GEAR DOWN AND LOCK SWITCH AND REMOVED AND REPLACED 2 BULBS IN NOSE GEAR INDICATOR IAW CE-750 MM CHAP 33-10-01. OPS CHECKED GEAR EXTENTION AND RETRACTION IAW CE-750 MM CHAP 32-30-00. OPS CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007042600265 20070426 00265 CE 2007 4 26 DXTA200702140 1 20070425 A 2750 FLAP SYSTEM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS FAILED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 903QS 7500162 AFTER TAKEOFF (FLAPS FAIL) CAS MESSAGE CAME ON AFTER TRYING TO RETRACT THE FLAPS. FLAPS FAILED AT 15 DEGREES, FLAPS WIL L NOT RESET. [SUP 05-02-07] REMOVED & REPLACED FLAP CONTROLLER & PDU IAW CE750 AMM 27-50-00 AND 27-52-00. OPERATIONAL CHECK GOOD WITH NO FURTHER DEFECTS NOTED IAW CE750 AMM 27-50-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007042600266 20070426 00266 CE 2007 4 26 DXTA200702141 1 20070425 A 3150 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TRIM MESSAGE UNKNOWN E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 975QS 7500175 ON FINAL APPROACH RECEIVED AMBER CAS MESSAGE PRI STAB TRIM FAIL AND MACH TRIM OFF. SECONDARY TRIM OPERATES NORMALLY. [ SUP 05-02-07] PERFORMED SYSTEM OP'S CHECKS. SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME. ALL WORK DONE I.A.W. CE750 M/ M 27-40-00 & 45-45-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007042600268 20070426 00268 EA 2007 4 26 S9BA00307 1 20070409 A 5340 ATTACH FITTING DHAV DHC6 DHC6300 2802606 EA BS 239 CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 888P 37490 125 620 RT FORWARD FRAME 239 AFT WING ATTACHMENT LUG HAS CORROSION. REMOVED AND REPLACED FRAME SUBASSEMBLY, SIDE FUSELAGE STA 2 39.88 1 H 7 2 3T RT A9EA 2007042600269 20070426 00269 EA 2007 4 26 S9BA00407 1 20070412 A 5711 SPAR CAP DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA RT WING CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 888PV 37409 89 620 FOUND CORROSION ON RT WING LOWER MAIN WING SPAR CAP BETWEEN STATION 35.2 AND STATION 74. REPAIRED IAW RD-57-24 AND INST ALLED SKIN PATCH IAW SRM 57-30-00 FROM STA 47 TO STATION 60. 1 H 7 2 3T 4 T RT A9EA E4EA 2007042600270 20070426 00270 EA 2007 4 26 S9BA0607 1 20070421 A 5740 C6W104829 ATTACH FITTING DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA RT WING CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 888PV 37490 89 620 RT WING AFT ATTACH FITTING CORRODED. REMOVED AND REPLACED WING ATTACH FITTING IAW SB 6/295 REV D. 1 H 7 2 3T 4 T RT A9EA E4EA 2007042600271 20070426 00271 SW 2007 4 26 53445041507 1 20070415 A 2810 FUEL CAP BELL 407 407 1182206 SW ALLSN 250C 250C47B GL NOT SEATED E QMLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 408AM 53445 DEPARTED, 30 MILES AWAY ON A HEADING OF 080. (4) MINUTES INTO THE FLIGHT, MED CREW INFORMED ME THERE WAS THE STRONG SMEL L OF JET FUEL IN THE AIRCRAFT. CHECKED THE FUEL AND PRESSURE GAUGES AND COULDN'T SMELL ANY FUMES EITHER. LOOKED FOR A S UITABLE LZ AND WHILE PREPARING TO LAND INFORMED DISPATCH OF SITUATION AND POSITION. ON LONG FINAL, I COULD NOW SMELL THE FUMES AS WELL. LANDED WITHOUT INCIDENT, AND SHUTDOWN. INSPECTED ACFT AND COULDN'T FIND ANY EVIDENCE OF FUEL LEAKS. WAIT ED FOR MECHANIC TO ARRIVE. HE COULDN'T FIND ANY LEAKS EITHER. HOWEVER THE FUEL CAP APPEARED TO NOT SEAT CORRECTLY CAUSIN G FUEL TO SEEP OUT THROUGH THE FILLER PORT. MECHANIC RELEASED ACFT FOR SERVICE AND ORDERED A NEW FUEL CAP. FLEW ACFT BA 1 G 7 1 3U 3 U O H2SW E1GL 2007042600273 20070426 00273 2007 4 26 QXEA200700652 4 20070420 A 3425 42000332501 AHRS BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA NR 2 MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 403QX 87 4037 FLIGHT NR 2359: ELEVATOR FEEL CAUTION LIGHT. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED NR 2 AHRS COMPU TER IAW MTC 6342101. OPS TEST GOOD. AIRCRAFT REMAINS CAT III. PLACARD READS CAT III. MTX CONTROL HAS BEEN NOTIFIED. AI RCRAFT RETURNED TO SERVICE 2 H 7 2 4T 4 T RT A13NM E00062EN 2007042600274 20070426 00274 EU 2007 4 26 BAQA20070010 1 20070323 A 6320 OILPUMP OIL SYSTEM UROCOP AEROSP AS355 AS355F1 8680810 EU MAIN GEAR BOX DEFECTIVE E BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 5797X 6689 1024 M5280 5182 MAIN GEAR BOX OIL PUMP FAILED AD03-21-09-R1, DARK PURPLE COLORED OIL IN SIGHT GLASS. REMOVED AND REPLACED MAIN GEAR BOX CONTAINING OIL PUMP, COMBINER GEAR BOX, EPICYCLIC, AND ROTOR SHAFT ASSEMBLY IAW EMERGENCY ALERT SB 05.00.40 REV 2 DATED DECEMBER 20,2006 1 G 7 2 3U H11EU 2007042600275 20070426 00275 CE 2007 4 26 AMWA84103 1 20070420 A 5240 UNKNOWN BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA PAX DOOR UNKNOWN A AMWA O OTHER N FALSE WARNING NR NOT REPORTED 1 CE 07 127ZV UE127 AFTER TAKEOFF THE CABIN DOOR ANNUN ILLUMINATED. RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENT. OPERATED DOOR N UMEROUS TIMES. OPS CHECKED GOOD. 2 L 7 2 4T 3 T RT A24CE E2NE 2007042600276 20070426 00276 NM 2007 4 26 QXEA200700649 1 20070421 A 2420 CIRCUIT BOARD DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE INVERTER INOPERATIVE A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 348PH 484 SEA FLIGHT NR 2044 ON TAXI OUT AUX INVERTER LIGHT ON (INVERTER INOP). MAINTENANCE REPLACED THE AUX INVERTER CONTROL CIRC UIT BREAKER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007042600278 20070426 00278 CE 2007 4 26 AMWA28025 1 20070413 A 5414 11498007824 SKIN PANEL BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT NACELLE WORN A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 162ZV UE162 RT NACELLE SKIN CAUSED FRICTION WEAR DAMAGE. REPAIRED IAW DESIGNATED ER DRAWING 1900D 162-1 REV 1R AND BSRM 51-40-02 AN D 51-40-03. 2 L 7 2 4T 4 T RT A24CE E26NE 2007042700015 20070427 00015 NE 2007 4 27 07N106HN01 2 20070422 A 7200 ENGINE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE POWER LOSS E QMLA R A AUTOROTATION UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 NM 03 106HN 2818 9362 APPROXIMATELY 22 MINUTES INTO FLT, PILOT EXPERIENCED INDICATIONS OF ENGINE FAILURE, LOW ROTOR RPM AUDIO CAME ON FOLLOWED AT THE SAME TIME WITH AIRCRAFT YAW. PILOT ENTERED AUTOROTATIONAL DESCENT AND LOOKED FOR LANDING AREA UNDER THE NVGS WHI LE MAKING A MAYDAY CALL TO APPROACH CONTROL. FLT MEDIC ALSO MADE MAYDAY CALL TO MEDCOM. AFTER SETTING UP FOR LANDING P ILOT HAD TIME TO LOOK AT ENGINE INDICATIONS BRIEFLY AND DETERMINED THAT PARTIAL POWER CONDITION WAS NOW INDICATED. DUE T O LOW ALTITUDE, 250 FT AGL, PILOT FELT THAT THERE WAS LITTLE TIME TO REGAIN ENGINE CONTROL WITH FUEL CONTROL LEVER. AUTO WAS COMPLETED WITH SKID AND CROSSTUBE DAMAGE. NO INJURIES TO CREW OR PATIENT. AIRCRAFT IS BEING REMOVED FROM FIELD AN 1 G 7 1 3U 3 U H9EU E19EU 2007042700019 20070427 00019 NM 2007 4 27 SB07029 1 20070417 A 3310 695517963 MODULE BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FWD ELEC P9 PNL FAULTY A USAA A UNSCHED LANDING P NO WARNING INDICATION DE DESCENT 1 EA 19 434US 42562 42562 24556 IAD FLT1724, ON DESCENT, CREW REPORTED THERE WAS NO INDICATION OF GEAR EXTENSION (RED OR GREEN LIGHTS) WHEN LANDING GEAR HANDLE WAS PUT IN THE DOWN POSITION. CREW PERFORMED QUICK REFERENCE HANDBOOK PROCEDURES AND EXTENDED THE GEAR MANUALLY. STILL NO LIGHTS. FLIGHT DIVERTED TO IAD FOR LONGER RUNWAYS. AIRCRAFT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCI DENT. AN EMERGENCY WAS DECLARED. MAINTENANCE INSPECTED GEAR INDICATION LIGHTS AND FOUND THEM INOPERATIVE DUE TO MASTER D IM BEING PARTIALLY INOPERATIVE. REMOVED AND REPLACED ANNUNCIATOR AND DIMMING MODULE M469. ALSO, REMOVED AND REPLACED R ELAYS R33, R34, R87, DIODE M208, AND CARDS M560 AND M564 IAW MM 33-13-11, 33-18-18 AND 33-18-17. OPERATIONAL CHECK OF MA 2 L 7 2 4F 4 F RT A16WE E21EU 2007042700060 20070427 00060 NM 2007 4 27 ASAA0771611 1 20070422 A 5320 141A54103 INTERCOSTAL BOEING 737 737790 13844CN NM BS 277-294 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 INTERCOSTAL CRACKED AT STA 277 REPAIRED IAW SRM 51 70 11. 2 L 7 2 4F RT A16WE 2007042700061 20070427 00061 NM 2007 4 27 ASAA0771612 1 20070422 A 5321 141A5810236 FLOORBOARD BOEING 737 737790 13844CN NM BS 294-344 PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 CABIN FLOOR BOARD IS PUNCTURED ON UPPER SURFACE REPAIRED IAW SRM 53 00 50. 2 L 7 2 4F RT A16WE 2007042700062 20070427 00062 NM 2007 4 27 ASAA0771613 1 20070422 A 5320 141A83166 SILL BOEING 737 737790 13844CN NM BS 277-294 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 RI DOOR SILL STRAP IS CORRODED REPAIRED IAW SRM 51 40 2. 2 L 7 2 4F RT A16WE 2007042700063 20070427 00063 NM 2007 4 27 ASAA0771614 1 20070422 A 5321 141A5810237 FLOORBOARD BOEING 737 737790 13844CN NM BS 328-380 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 FLOORBOARD 222CF IS CRACKED AT CORNER AND EDGE REPAIRED IAW 53-00-50. 2 L 7 2 4F RT A16WE 2007042700064 20070427 00064 NM 2007 4 27 ASAA0771615 1 20070422 A 5321 147A5810136 FLOORBOARD BOEING 737 737790 13844CN NM BS 950-986 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 FLOORBOARD AT STA 950 IS CRACKED IN 8 LOCATION REPAIRED IAW SRM 53 00 50. 2 L 7 2 4F RT A16WE 2007042700065 20070427 00065 NM 2007 4 27 ASAA0771616 1 20070422 A 5230 143A61121 SKIN BOEING 737 737790 13844CN NM CARGO DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 AFT CARGO COMPARTMENT DOOR HAD TWO CREASES IN IT REPAIRED IAW 52 30 01360. 2 L 7 2 4F RT A16WE 2007042700066 20070427 00066 NM 2007 4 27 ASAA0771617 1 20070422 A 5315 147A56765 FLOORBEAM BOEING 737 737790 13844CN NM BS 950 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 FLOOR SUPPORT AT STA 950 IS CORRODED ON UPPER FLANGE REPAIRED IAW SRM 51 40 02. 2 L 7 2 4F RT A16WE 2007042700067 20070427 00067 NM 2007 4 27 ASAA0771618 1 20070422 A 5320 147A56601 INTERCOSTAL BOEING 737 737790 13844CN NM BS 947-967 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 INTERCOSTAL AT STA 947 967 IS CORRODED REPAIRED IAW SRM 51 40 02. 2 L 7 2 4F RT A16WE 2007042700068 20070427 00068 NM 2007 4 27 2007UALA01152 1 20070415 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 312-360 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 FWD CABIN FLOOR STRUCTURE CREASE BEAM Z-ANGLE HAS CORROSION ON UPPER SURFACE THROUGHOUT LENGTH BS 312 TO 360 LBL 55-60 W L 208. [SUP 05-01-07] MAJOR REPAIR: INSTALLED NEW CREASE BEAM Z-ANGLE, REFERENCE SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2007043000006 20070430 00006 NM 2007 4 30 ABXA070119 1 20070319 A 5240 BEAM BOEING 767 767281 1385109 NM R1 DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 774AX 22789 LOWER FORWARD CORNER OF THE R1 DOOR HAD A CRACKED BEAM. REPAIRED AREA IAW REA B652-55550-MR. 2 L 7 2 4F RT A1NM 2007043000009 20070430 00009 WP 2007 4 30 ABXA070112 1 20070306 A 5312 99101553 PRESSURE PANEL DOUG DC9 DC931 3022065 WP BS 708 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 949AX 47325 WHEEL WELL PRESSURE PANEL WAS BULGED AND CRACKED AT APPROXIMATELY FS 708, BUTT LINE 0. REPAIRED WHEEL WELL PRESSURE PAN EL APPROXIMATELY FS 708 IAW DC9 REA D953-55487. 2 L 7 2 4F A6WE 2007043000012 20070430 00012 WP 2007 4 30 ABXA070122 1 20070402 A 5752 591005126 TAB DOUG DC9 DC915F 3022037 WP RIGHT AILERON DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 785TW 47015 RIGHT AILERON OUTBOARD TAB DELAMINATED 3 PLACES, 1 UPPER AND 2 LOWER APPROXIMATELY 3 BY 3, 3 BY1 1/2, OUTBOARD TIP REPAI R DISBOND. REMOVED AND REPLACED RIGHT AILERON TRIM TAB IAW DC9 MM 27-10-5. 2 L 7 2 4F A6WE 2007043000018 20070430 00018 WP 2007 4 30 ABXA070125 1 20070410 A 5312 59101303 BULKHEAD DOUG DC9 DC915F 3022037 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 785TW 47015 AFT PRESSURE BULKHEAD SKIN CRACKED AT UPPER LEFT DOOR CUTOUT. REMOVED AND REPLACED SKIN IAW DC9 SRM 51-30-2 AND 51-30-5 . 2 L 7 2 4F A6WE 2007043000020 20070430 00020 NM 2007 4 30 SWAA072010 1 20070424 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007043000021 20070430 00021 NM 2007 4 30 SWAA072023 1 20070424 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007043000027 20070430 00027 NM 2007 4 30 SWAA072013 1 20070424 A 5311 6545808 FRAME BOEING 737 7373H4 1384600 NM BS 295 S12L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 295, STR 12L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007043000034 20070430 00034 NM 2007 4 30 SWAA072029 1 20070424 A 5311 6546557 FRAME BOEING 737 7373G7 1384595 NM BS 887 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007043000040 20070430 00040 NM 2007 4 30 DL738070358 1 20070424 A 3244 B737800M TIRE BOEING 737 737832 13844CF NM NR 1 POSITION FAILED A DALA O OTHER O OTHER LD LANDING 1 SO 27 392DA 30561 ON LANDING TOWER REPORTED SMOKE FROM CAPTAINS SIDE. NO INDICATION INSIDE OF ANY MALFUNCTION. FIRE CREW DISCOVERED NR 1 TIRE BLOWN. REPLACED NR 1 WHEEL ASSY FWD ANTI-SKID TO MCO/PLAC. T/S PER FIM 32-42-00-810. REPLACED PARKING BRAKE SHU TOFF VALVE PER AMM. CHECK OK MCO AND PLACARD REMOVED. 2 L 7 2 4F RT A16WE 2007043000052 20070430 00052 EU 2007 4 30 AWXA200700518 1 20070423 A 5315 D53472188204 FLOORBEAM AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 664AW 1621 SAL - FOUND CORROSION ON CABIN FLOORBEAM, FR 68.6" TO FR 69 + 3", + Y1162. REPLACED CABIN FLOORBEAM, FR 68 - FR 69 + 3" , +Y1162 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007043000055 20070430 00055 EU 2007 4 30 AWXA200700521 1 20070423 A 5315 D53472172205 FLOORBEAM AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 664AW 1621 SAL - FOUND CORROSION ON CABIN FLOORBEAM, FR 66 TO FR 67, - Y1162 TO -Y1292. REPLACED CABIN FLOORBEAM, FR 66 - FR 67, -Y1162 TO -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007043000057 20070430 00057 EU 2007 4 30 AWXA200700523 1 20070421 A 5340 201163207 STAY AIRBUS 320 A320231 3930325 EU ZONE 700 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 SAL - FOUND CORROSION ON RIGHT MAIN LANDING GEAR LOWER SIDE STAY. REPLACED RIGHT MAIN LANDING GEAR LOWER SIDE STAY IAW A320 AMM 32-11-16. 2 L 7 2 4F RT A28NM 2007043000064 20070430 00064 NM 2007 4 30 PIDA07025 1 20070420 A 5340 STRINGER CLIP BOEING 737 7372K5 138448X NM BS 947 CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 DURING MAINTENANCE, FOUND STR 2LT TIE CLIP CRACKED AT BS 947. REPLACED TIE CLIP PER SRM 51-30-0. 2 L 7 2 4F RT A16WE 2007043000065 20070430 00065 NM 2007 4 30 PIDA07021 1 20070421 A 5311 FRAME BOEING 737 7372K5 138448X NM BS 927 DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 DURING INSPECTION, NOTED FIGURE 8 HOLE IN BS 927 FRAME AT STR 6LT. REPAIRED FRAME PER SRM 51-40-02, 51-40-05 AND 51-30- 00 AND REPLACED STRINGER CLIP PER SRM 51-40-02 AND 51-40-03. 2 L 7 2 4F RT A16WE 2007043000070 20070430 00070 EU 2007 4 30 07FDEA01559 1 20070424 A 5753 A57970100011 FLAP AIRBUS 310 A310324 3930206 EU ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 SEVERAL DAMAGES (DENTS, CORRODED CORE) ON RT INBOARD FLAP AT LOWER AND UPPER SURFACE BETWEEN RIB2-9. REPAIR PERFORMED I AW SRM 57-53-12/FIG 208/209, APPROVED BY EA 6-5753-99189 AND RAS/DABRE/7006468/2006 ISSUE "B". 2 L 7 2 4F RT A35EU 2007043000079 20070430 00079 NM 2007 4 30 2007UALA01153 1 20070415 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 960-996 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 AFT CABIN FLOOR STRUCTURE CREASE BEAM HAS CORROSION ON UPPER SURFACE BS 960-996 RBL 46-57 AT 208. [SUP 05-01-07] MAJOR REPAIR: INSTALLED NEW CREASE BEAM. REFERENCE SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2007043000086 20070430 00086 NM 2007 4 30 2007UALA01162 1 20070414 A 3350 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 843UA 1573 PTP PANEL KEPT GETTING EPSU BATTERY EMER L MESSAGE. SUPPLEMENTAL DATA UPDATE RESET EMERGENCY LIGHT BREAKERS. TEST PASS ED ON PTP PANEL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007043000088 20070430 00088 EU 2007 4 30 2007UALA01164 1 20070413 A 3350 LAMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 464UA 1290 CEILING EVACUATION LIGHT AT ROW 14 INOPERATIVE. [SUP 05-16-07] FOUND CONNECTOR NOT INSTALLED ON LIGHT ASSY. SECURED CO NNECTOR. LIGHT CHECK'S GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007043000100 20070430 00100 NM 2007 4 30 2007UALA01176 1 20070415 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY EEL LIGHT INOPERATIVE AT SEAT 5J AFT. RELAMPED. OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007043000107 20070430 00107 NM 2007 4 30 2007UALA01183 1 20070414 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN DETACHED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 786UA 26938 EMERGENCY EXIT PATH LIGHTING STRIP ON LEFT SIDE OF SEAT 1E FELL OFF AGAIN. REPLACED LIGHT ASSY. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007043000122 20070430 00122 NM 2007 4 30 2007UALA01234 1 20070420 A 3397 58781 FEEDER CABLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 202UA 24717 AFT CABIN EEL LIGHTS INOP FROM ROW 15 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT. R EPLACED CABLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007043000129 20070430 00129 WP 2007 4 30 ABXA070099 1 20070315 A 5412 4912539V2 BULKHEAD DOUG DC9 DC932 3022066 WP RT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 RIGHT PYLON BULKHEAD AT STA 965 HAD CRACKED ATTACH FITTING AT RIGHT BUTT LINE 32. REMOVED AND REPLACED FITTING IAW DAC DWG 9912243. 2 L 7 2 4F A6WE 2007043000137 20070430 00137 NM 2007 4 30 SWAA072060 1 20070425 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 425LV 29829 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 13 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007043000139 20070430 00139 NM 2007 4 30 SWAA072046 1 20070425 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 514A S19R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514A, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007043000145 20070430 00145 NM 2007 4 30 SWAA072052 1 20070425 A 5310 6547979 CREASE BEAM BOEING 737 7373L9 1384470 NM BS 787-797 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 787 TO BS 797, RBL 70. REMOVED AND REPLACED CREASE BEA M WEB PER SRM. 2 L 7 2 4F RT A16WE 2007043000156 20070430 00156 NM 2007 4 30 SWAA072038 1 20070424 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 520 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000159 20070430 00159 NM 2007 4 30 SWAA072033 1 20070424 A 5311 65C34355 FRAME BOEING 737 7375H4 138449D NM BS 482 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007043000161 20070430 00161 NM 2007 4 30 SWAA072040 1 20070424 A 5313 BAC1498 STRINGER BOEING 737 7373T5 1384608 NM BS 1006-1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 22Y CHECK, FOUND STRINGER 26R CORRODED BETWEEN BS 1006 AND BS 1016. REMOVED AND REPLACED STRINGER PE R SRM. 2 L 7 2 4F RT A16WE 2007043000163 20070430 00163 NM 2007 4 30 QXEA200700675 1 20070413 A 5330 DOUBLER DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - LAVATORY EXTERIOR SERVICE PANEL SURROUND DOUBLER ON FUSELAGE IS CORRODED ALONG BOTTOM EDGE. REPAIRED IAW RD8-5 3-2103 AND RD8-53-3229 AND SRM 51-30-26. 2 H 7 2 4T RT A13NM 2007043000165 20070430 00165 NM 2007 4 30 QXEA200700678 1 20070414 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSLEAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - FUSELAGE SKIN UNDER THE LOWER ATC ANTENNA IS CORRODED. REPAIRED IAW SRM 51-20-16, 51-20-36, AND DR8-53-7127. 2 H 7 2 4T RT A13NM 2007043000170 20070430 00170 NM 2007 4 30 QXEA200700684 1 20070425 A 2822 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM AUX FUEL PUMP MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 423QX 4153 BOI FLIGHT NR 2423: AFTER ENGINE START, CREW NOTICED FUEL AUX PUMP CIRCUIT BREAKERS POPPED. AIRCRAFT RETURNED TO GATE. MAINTENANCE RESET CIRCUIT BREAKERS PER GMM 5-18-0. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007043000175 20070430 00175 NM 2007 4 30 SWAA072059 1 20070425 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 380 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000178 20070430 00178 NM 2007 4 30 SWAA072086 1 20070426 A 5311 6546539 FRAME BOEING 737 7375H4 138449D NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT RT BS 616, WL 199. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2007043000181 20070430 00181 NM 2007 4 30 SWAA072082 1 20070426 A 5311 6546593 FRAME BOEING 737 7373L9 1384470 NM BS 500A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007043000182 20070430 00182 NM 2007 4 30 SWAA072075 1 20070426 A 5310 6547979 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 747-767 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 747 AND BS 767, LBL 70. REMOVED AND REPLACED CREA SE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2007043000199 20070430 00199 NM 2007 4 30 SWAA072077 1 20070426 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 727D S23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 23L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007043000200 20070430 00200 NM 2007 4 30 SWAA072084 1 20070426 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM BS 788 S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 788, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007043000203 20070430 00203 NM 2007 4 30 SWAA072079 1 20070426 A 5753 6546434302 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD LOWER END. REMOVED AND REPLACE F LAP PER MM. 2 L 7 2 4F RT A16WE 2007043000208 20070430 00208 EA 2007 4 30 TRAX200700549 1 20070420 A 3220 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA NOSE INOPERATIVE A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 980EV 7759 AFTER T/O NOSE GEAR WOULD NOT COME UP AFTER SELECTED IN THE UP POSITION, NOSE WHEEL STEERING INOP ON LANDING, A/C RETURN ED TO MCN AFTER TAKEOFF. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007043000209 20070430 00209 EA 2007 4 30 TRAX200700550 1 20070420 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 859AS 7421 FWD PAX DOOR IS VERY DIFFICULT TO UNLATCH AND OPEN FROM THE OUTSIDE. 2 L 7 2 4F RT A21EA 2007050100013 20070501 00013 NM 2007 5 1 07FDEA01600 1 20070426 A 5311 AFA00203 FRAME DOUG MD11 MD11F 3023600 NM BS 1701 L12L DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 MAIN DECK CARGO COMPARTMENT, MAIN FRAME STA 1701 AT LONGERON 12L FOUND WITH DENT. [SUP 05-08-07] REPAIRED AS PER SRM 5 3-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050100014 20070501 00014 NM 2007 5 1 07FDEA01601 1 20070426 A 5311 AFA00203 FRAME DOUG MD11 MD11F 3023600 NM BS 1701 L12R DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 MAIN DECK CARGO COMPARTMENT, MAIN FRAME STA 1701 AT LONGERON 12R FOUND WITH DENT. [SUP 05-08-07] REPAIRED AS PER SRM 5 3-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050100021 20070501 00021 NM 2007 5 1 07FDEA01608 1 20070426 A 5711 ARB74131 SPAR DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 LEFT WING, REAR SPAR UPPER CAP SURFACE AT ABOUT STA XORS 1046 FOUND WITH CORROSION. [SUP 05-14-07] REPAIRED AS PER FEDEX EA 1-5710-109868, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050100026 20070501 00026 EU 2007 5 1 07FDEA01614 1 20070426 A 5313 A53986217 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 FOUND CORROSION ON STRINGER P44 RT, C54-54.2 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007050100055 20070501 00055 NM 2007 5 1 C1HA200792001 1 20070421 A 2130 SWITCH BOEING 727 727212 138407G NM A/C PACK DEFECTIVE A C1HA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 292AS 21458 AT FL 250 CABIN PRESS STARTED CLIMBING AT 100FT PER MIN PERFORMED COM 2.21.16 UNABLE TO STOP CLIMB. STARTED DESCENT, CA BIN WOULD NOT HOLD PRESSURE UNTIL PASSING 17,000 FT CABIN ALT PEAKED AT 9,000 FT RETURNED TO CUN. REMOVED DEFECTIVE PAC K SWITCH FOR RT PACK AND REPLACED WITH NEW SWITCH. OPS CHECK GOOD, MM 21-50-01. 2 L 7 3 4F A3WE 2007050100059 20070501 00059 WP 2007 5 1 07FDEA01565 1 20070424 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP BS 488-495 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 NLG WHEEL WELL NR 6 CRACKS ON LT VERTICAL BULKHEAD FROM STA 488 TO 495 FROM Z=-60 AT Z=-65, REPAIR IAW SRM 53-40-00 VOL 1. 2 L 7 3 4F A22WE 2007050100071 20070501 00071 EU 2007 5 1 07FDEA01578 1 20070424 A 5314 SEE4A KEELBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 CORROSION IN AIR CONDITIONING COMPARTMENT RT, KEEL BEAM (A538-11587-201, A538-11200-200): P'51, C44-45; P'51, C45-46; ST RINGER (A538-11380-201, A538-11597-200): P'48, C40; P'51, C42. REPAIR PERFORMED BY BLEND OUT IAW SRM 51-74-10 AND INST ALLING OVERSIZE FASTENERS IAW SRM 51-40-30, APPROVED BY EA 6-5315-99214 AND RAS 044433/005/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007050100087 20070501 00087 SO 2007 5 1 N93A19042007 1 20070419 A 5530 1159B2156225 ANGLE GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU BULKHEAD CRACKED E N93A K NONE O OTHER IN INSP/MAINT 1 SO 13 493QS 10063 1293 DURING 5000 LANDING INSPECTION MAINTENANCE FOUND 793 BULKHEAD CAP ANGLE CRACKED. 2 L 7 2 4F 4 F RT A12EA E25NE 2007050100092 20070501 00092 NE 2007 5 1 GUUA04030701 2 20070403 A 7200 3044900 POWERPLANT BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RIGHT FLUCTUATES A GUUA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SO 17 190YV 24074 UE190 PCE114194 FLIGHT: 9171, DURING FLIGHT AT 17,000 FEET, RT ENGINE TORQUE FLUCTATES FROM 3,000 LBS TO 2,500 LBS FOR 3 SECONDS. TORQU E STABLIZED AT 2,700 LBS FOR 10 SECONDS FOLLOWED BY ERRATIC TORQUE READINGS FROM 3,000 LBS TO 1,500 LBS WITH ITT AT 850 DEGREES. PERFORMED MEMORY ITEMS FOR ENGINE FAILURE IN FLIGHT TO SECURE ENGINE. DIVERTED, LANDED WITHOUT INCIDENT. REPL ACED RT ENGINE ASSEMBLY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007050100093 20070501 00093 EU 2007 5 1 YENA2007026 1 20070423 A 2150 10007004 ACM EMB ERJ190 ERJ190100IGW 3260408 EU NR 1 SEIZED A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 267JB 338 19000065 FLT 1251, 1029Z, AIR RETURN, SMOKE IN COCKPIT, PACK NR 1 FAIL. PERFORMED TROUBLESHOOTING IAW FIM 21-51-00-810-833A, FOUN D PACK NR 1 ACM SEIZED. REMOVED AND REPLACED NR 1 ACM IAW AMM 21-51-05, OPS CK GOOD. 2 L 7 2 4F RT A57NM 2007050100104 20070501 00104 GL 2007 5 1 02118 1 20070406 A 7931 12635002 PRESSURE SWITCH CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO HARTZL HCJ3Y PHCJ3YF1 GL OIL PRESSURE FLUCTUATES E J4PA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 13 509SR 293 2180 689969 FP5066B OIL PRESSURE DROPPED TO 20 PSI IN CRUISE FLIGHT, DURING CRUISE OIL GAUGE FLUCTUATED +- 4 PSI, BETWEEN 33-37 OTHER INDICA TIONS NORMAL, REMOVED AND CLEANED OIL PRESSURE SENDING UNIT REINSTALLED AND OPERATIONAL CHECKED GOOD. 1 L 7 1 3O 3 O NT A00009CH E3SO 5 C P36EA 2007050100109 20070501 00109 CE 2007 5 1 DXTA200702153 1 20070427 A 2120 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CABIN SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 931QS 7500064 ON GROUND WITH APU RUNNING, CABIN PAC OFF, CABIN FILLED WITH SMOKE. [SUP 05-03-07] TO FAILED CABIN PAC AIRCYLE MACHINE. WHILE T/S FOUND LP BLEED AIR ISULATION VALVE STICKING. REMOVED AND REPLACED ISOLATION VALVE AND CABIN AIR CYCLE MACHINE . BOTH OPS. CHECKED AND LEAK CHECKED GOOD. IAW. 750 M/M CH. 21-51-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007050100121 20070501 00121 CE 2007 5 1 DXTA200702147 1 20070426 A 3260 INDICATION SYS CESSNA 560 560XL 2076702 CE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 689QS 5605659 GREEN LT GEAR POSITION INDICATOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION ON TAKEOFF. [SUP 05-02-07] INSTALLE D MLG CONTROLLER (REPAIRED) AND INSPECTED ACTUATOR ON LT MAIN GEAR.CYCLED GEAR SEVERAL TIMES,NO FAULTS FOUND.SEE CJI W/O 026717 FOR DETAILS ALL WORK DONE IAW 560XL MM 32-30-01. 2 L 7 2 4F RT A22CE 2007050100124 20070501 00124 CE 2007 5 1 DXTA200702150 1 20070426 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE MLG CHATTERING E DXTA O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 GL 07 810QS 5600625 WHILE TAXING AT SLOW SPEED BRAKE CHATTER ENCOUNTERED BOTH AUDIBLE AND FELT THRU BRAKE PEDALS. UNABLE TO DETERMINE RT OR LT SIDE. [SUP 05-03-07] BLED BRAKE SYSTEM IAW CESSNA 560 MAINT. MAN. CHAP. 32-42, AIR FOUND IN SYS, NO OTHER DEFECTS NOTED. 2 L 7 2 4F 4 F RT A22CE E00053EN 2007050100131 20070501 00131 NM 2007 5 1 SWAA072101 1 20070428 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 616 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050100133 20070501 00133 NM 2007 5 1 SWAA072108 1 20070428 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM BS 344 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050100138 20070501 00138 NM 2007 5 1 SWAA072091 1 20070427 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM BS 370 S17R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 370, STR 17R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007050100141 20070501 00141 NM 2007 5 1 SWAA072092 1 20070427 A 5310 6545979 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 727D-727E CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 727D AND BS 727E, STR 17R. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007050100142 20070501 00142 NM 2007 5 1 SWAA072093 1 20070427 A 5310 6545979 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 767-787 S17R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 767 AND BS 787, STR 17R. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007050100143 20070501 00143 NM 2007 5 1 SWAA072105 1 20070428 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050100144 20070501 00144 NM 2007 5 1 SWAA072100 1 20070428 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 685 S1 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050100145 20070501 00145 NM 2007 5 1 SWAA072095 1 20070427 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 482A S5L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482A, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050100147 20070501 00147 NM 2007 5 1 DU4R2007108 1 20070421 A 5330 SKIN BOEING 757 757232 1384965 NM BS 610-630 S7-8R DAMAGED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 6709 30481 FOUND LIGHTNING STRIKE ON SKIN BETWEEN BS 610 AND 630 AT S-7R AND S-8R. REPAIRED BY CUTTING OUT S-7R FROM BS 610 TO 630 . FABRICATED AND INSTALLED STRINGER REPAIR 9-1/2 BY 3 FROM BAC1498-234 AND 4 SPLICES 9-1/2 BY 1 FROM 7075-T6 .040 IAW B 757 SRM 53-00-01 FIG 201. REPAIR 4 AS DIRECTED BY TIMCO RFTS #60002, DATED 4-9-2007. 2 L 7 2 4F RT A2NM 2007050100149 20070501 00149 EA 2007 5 1 SWIA200718154 1 20070318 A 2510 SEAT BACK CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 447SW 7677 CO-PILOTS SEAT LEFT BACKREST SUPPORT IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED PN 1C3076-1AUT PER CRJ200 SRM 51-42-1 0 PG 1-8. 2 L 7 2 4F RT A21EA 2007043000001 20070430 00001 WP 2007 4 30 ABXA070116 1 20070423 A 5310 99115056 WINDOW FRAME DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 DURING COCKPIT WINDOW MOD, EA 53300036, FOUND FRAME CRACKED. REPAIRED IAW DC9 SRM 53-03, FIGURE 34. 2 L 7 2 4F A6WE 2007043000003 20070430 00003 WP 2007 4 30 ABXA070118 1 20070423 A 5310 99115057 WINDOW FRAME DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 DURING COCKPIT WINDOW MOD, EA 53300036, FOUND FRAME CRACKED. REPAIRED IAW DC9 SRM 53-03, FIGURE 34. 2 L 7 2 4F A6WE 2007043000010 20070430 00010 NM 2007 4 30 ABXA070120 1 20070327 A 5315 451T19034 FLOORBEAM BOEING 767 767281 1385109 NM BS 1402 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 774AX 22789 FLOOR SUPPORT CORRODED AT FS 1402, LEFT BUTT LINE 21. REMOVED, REPAIRED AND REINSTALLED FLOOR SUPPORT IAW B767 51-70-12 AND 51-40-O2. 2 L 7 2 4F RT A1NM 2007043000017 20070430 00017 WP 2007 4 30 ABXA070115 1 20070423 A 5340 99578605 BRACKET DOUG DC9 DC941 302207N WP COCKPIT WINDOW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 DURING COCKPIT WINDOW MOD, FOUND BRACKET CRACKED. REMOVED AND REPLACED IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 2007043000026 20070430 00026 NM 2007 4 30 SWAA072030 1 20070424 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM BS 749 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007043000037 20070430 00037 NM 2007 4 30 WRNA200700022 1 20070417 A 3297 CONNECTOR BOEING 747 747212B 1384886 NM BRAKE VALVE DIRTY A WRNA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 05 526UP 21937 TAKEOFF WARNING HORN CAME ON AT BRAKE RELEASE. TROUBLESHOOT PER FIM 31-26-00 PG 109, FOUND TAKEOFF WARNING CIRCUITS OPE RABLE. DURING TROUBLESHOOTING, FOUND PARKING BRAKE LIGHT NOT ILLUMINATING, CLEANED AND RESEATED PARKING BRAKE VALVE CON NECTOR. PERFORMED AURAL TAKEOFF WARNING SYSTEM OPERATION TEST PER 747 MM 31-26-00 PAGE 502, OPS CHECKED NORMAL. AIRCRA FT RELEASED FOR SERVICE. 2 L 7 4 4F A20WE 2007043000049 20070430 00049 WP 2007 4 30 ABXA070138 1 20070405 A 5347 S2914913M24000 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 718 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 FOUND SEAT TRACK RIGHT BUTT LINE 44 CORRODED AT STA 718. REMOVED AND REPLACED SEAT TRACK STA 570 TO 748 IAW DC9 SRM 51- 30-1. REINSTALLED FLOOR PANELS IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 2007043000054 20070430 00054 EU 2007 4 30 AWXA200700520 1 20070423 A 5315 D53472189200 FLOORBEAM AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 664AW 1621 SAL - CORROSION ON CABIN FLOORBEAM, FR 68 - 6" TO FR 69, - Y1162. REPLACED CABIN FLOORBEAM , FR 68 - FR 69, -Y1162 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007043000071 20070430 00071 WP 2007 4 30 ABXA070102 1 20070315 A 5312 59101303 BULKHEAD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 AFT PRESSURE BULKHEAD LOWER DOOR CORNER HAD A CRACK IN SKIN. THE REPAIR INSTALLED DID NOT MATCH ANY CONFIGURATION OF DW G J060088 IN NUMBER, PLACEMENT AND MATERIAL OF DOUBLERS. REMOVED PREVIOUS REPAIR. NO CRACKS FOUND. REPAIRED LOWER DOO R CORNER IAW SERVICE REWORK DWG J060088-519 CONFIGURATION. 2 L 7 2 4F A6WE 2007043000084 20070430 00084 NM 2007 4 30 2007UALA01158 1 20070413 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1061 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 MAIN CABIN CREASE BEAM WEB HAS CORROSION STA 1061, LBL 7 0. [SUP 05-04-07] MAJOR REPAIR ACCOMPLISHED: REMOVED CO RROSION. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007043000090 20070430 00090 EU 2007 4 30 2007UALA01166 1 20070413 A 3397 BR963165 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 464UA 1290 FOUND SEAT 2B HAS 2 EA EEL LIGHTS INOPERATIVE. SUPPLEMENTAL DATA UPDATE, REPLACED LAMP ASSY NO HELP FOUND FLOOR RUN WIR E PULLED OUT OF CONNECTOR BLOCK AT SEAT MUX AREA REINSTALLED PIN, OPS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007043000093 20070430 00093 NM 2007 4 30 2007UALA01169 1 20070413 A 2620 SQUIB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO 2 BOTTLE NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 398UA 24673 FOUND CARGO 2 BOTTLE ARMED LIGHT WILL NOT TEST. [SUP 05-01-07] FOUND BAD NR 2 BOTTLE SQUIB AND REPLACED THE SAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2007043000095 20070430 00095 NM 2007 4 30 2007UALA01171 1 20070415 A 3350 7945243 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY EEL LIGHTS INOPERATIVE AT UPPER DECK EEL EXIT SIGNS AND UPPER DECK FWD HALF OF SEATS AND WALL. SECURED CONNEC TOR. OPS CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007043000109 20070430 00109 NM 2007 4 30 2007UALA01224 1 20070419 A 5310 BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 680 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 MAIN CABIN STUB BEAM CRACKED STA 680 JUST ABOVE 10 INCH STR 13L. [SUP 05-04-07] MAJOR REPAIR ACCOMPLISHED: REMOVED WE B. FABRICATED & INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2007043000111 20070430 00111 WP 2007 4 30 ABXA070132 1 20070403 A 5753 5912150510 HINGE FITTING DOUG DC9 DC932 3022066 WP RT WING TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 AFT FLAP HINGE FITTING CRACKED AT ACTUATOR ATTACH EAR, STA 164. REMOVED AND REPLACED HINGE FITTING IAW DC9 SRM. 2 L 7 2 4F A6WE 2007043000112 20070430 00112 NM 2007 4 30 PIDA07026 1 20070425 A 5320 FLOOR SUPPORT BOEING 737 7372K5 138448X NM BS 767 CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 DURING INSPECTION, NOTED CORROSION ON LOWER SURFACE OF THE OUTBOARD LONGITUDINAL FLOOR SUPPORT ANGLE IN THE AFT CARGO BI N AT BS 767 +6. REMOVED DAMAGED SECTION OF FLOOR SUPPORT AND REPAIRED PER SRM 53-10-5. 2 L 7 2 4F RT A16WE 2007043000115 20070430 00115 NM 2007 4 30 2007UALA01227 1 20070419 A 5310 BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 680 S11R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 MAIN CABIN, STUB BEAM CRACKED STA 680, 5 INCH BELOW STR 11R. [SUP 05-04-07] MAJOR REPAIR ACCOMPLISHED: REMOVED WEB. FABRICATED & INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2007043000119 20070430 00119 2007 4 30 2007UALA01231 4 20070419 A 2565 SLIDE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE DOOR 1R WRONG PART A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 656UA 25394 DOOR 1R SLIDE IS THE WRONG PART. [SUP 05-18-07] REPLACED DOOR 1R SLIDE ASSY PER AMM 25-66-01 WITH THE CORRECT SLIDE P/ N. NEW SLIDE INSTALLED IS MR25708 (649-9059). 2 L 7 2 4F 4 F RT A1NM E24NE 2007043000125 20070430 00125 NM 2007 4 30 2007UALA01238 1 20070420 A 2780 SLAT SYSTEM BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE WARNING MESSAGE A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 664UA 29236 LE SLAT ASYMMETRY EICAS MSG. [SUP 05-18-07] FOUND SENSOR S304 TARGET BROKEN OFF -S304 WILL NEED ADJUSTMENT AFTER TARGE T ASSEMBLY REPLACED. EICAS MESSAGE CLEARED. A/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007043000127 20070430 00127 WP 2007 4 30 ARWA20070401 1 20070421 A 2910 HOSE DOUG DC10 DC1010 3022110 WP HYD SYSTEM DAMAGED A ARWA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 68041 46900 DEPARTING MNMG, LOST HYDRAULIC PRESSURE AND QUANTITY NR 3 SYSTEM; PERFORMED APPLICABLE CHECKLIST, AND CONTINUED TO MROC. REMOVED AND REPLACED RT MAIN LANDING GEAR TRIM CYLINDER HYDRAULIC HOSE ASSEMBLY IN ACCORDANCE WITH M/M 20-40-02; SERVI CED NR 3 HYDRAULIC SYSTEM IN ACCORDANCE WITH M/M 12-13-02. OPERATIONAL CHECK MAIN HYDRAULIC SYSTEM IN ACCORDANCE WITH M /M 29-00-00 AND 29-02-00, NO LEAK NOTED; RETURN LANDING GEAR HANDLE TO ITS NORMAL OPERATION IN ACCORDANCE WITH M/M 32-30 -00. 2 L 7 3 4F A22WE 2007043000141 20070430 00141 NM 2007 4 30 SWAA072048 1 20070425 A 5753 6546486129 STRUCTURE BOEING 737 7373L9 1384470 NM LT WING FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND LT WING INBOARD MID FLAP CRACKED AT LOWER OUTBOARD END. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007043000143 20070430 00143 NM 2007 4 30 SWAA072050 1 20070425 A 5322 6546569 SHEAR TIE BOEING 737 7373L9 1384470 NM BS 986 S22L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986, STR 22L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007043000164 20070430 00164 NM 2007 4 30 QXEA200700677 1 20070414 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 5 FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - RIGHT WING NR 5 FLAP TRACK INBOARD SIDE LOAD ROLLER TRACK SURFACE HAS SURFACE RUST FORMING. REPAIRED IAW RD8-5 7-989. 2 H 7 2 4T RT A13NM 2007043000166 20070430 00166 NM 2007 4 30 QXEA200700679 1 20070414 A 5320 VERTICAL SUPPORT DHAV DHC8 DHC8202 2809007 NM BS 201 S31L CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 C5 PDX - VERTICAL SUPPORT FOR UPPER FRAME X201 AT STRINGER 31L IS CORRODED ON THE LOWER END. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007043000204 20070430 00204 NM 2007 4 30 NOCA08507 1 20070419 A 7700 44A2562 SWITCH BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E437 54555 NE ALTITUDE MALFUNCTIONED A NOCA O OTHER J WARNING INDICATION CL CLIMB 1 EA 15 754NA 293 LEFT ENGINE SURGE COMPRESSOR STALL AT FL.360 DURING CLB AT 1.38 EPR LEFT ENG SURGE AGAIN BEFORE INITIAL DESCENT AND DURI NG DESCENT TOTAL OF 3 TIMES ALL ENGINE INDICATIONS NORMAL AFTER ENGINE SURGE. ACP INSPECTION OF LEFT ENG INLET, EXHAUST CHIP DETECTORS NO FAULTS OR DEFECTS NOTED. PER FIM 71-06-00 MM 71-00-00-206. ACCOMPLISH BITE OF L EEC PER FIM 73-21-0 0, NO FAULTS NOTED. CONTINUE TROUBLESHOOTING. OPERATIONALLY TESTED THE LT ENGINE ALTITUDE SWITCH PER MM 75-32-07. NO DEFECTS. FOUND 2 BOROSCOPE BLANKING PLUGS FOR IP AND HP TURBINE AT 5 O`CLOCK POSITION LOOSE SECURED AS REQUIRED BY BORO INSPECTOR. REPLACED ALTITUDE SWITCH PER MM 75-32-07 PER ROLLS ROYCE ADVICE. ACP TEST 3 PER MM 71-00-00, NO FAULT FOUN 2 L 7 2 4F 4 F RT A2NM E12EU 2007050100002 20070501 00002 WP 2007 5 1 07FDEA01587 1 20070424 A 5210 ABA85371 HANDLE DOUG MD10 MD1010F 3022112 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 R1 DOOR EMERGENCY HANDLE BACKLOCK DOES NOT HOLD HANDLE ONCE HANDLE IS MOVED TO EMERGENCY POSITION. FOUND OVERRIDE LEV ER BINDING WITH BACKLOCK. REPLACED BUSHING, SEAL AND LEVER IAW MD10-10 MM 52-11-14-2 AXIAL PLAY CK GOOD. PERFORMED PNE UMATIC TEST TO CK BACK LOCK, OPS CK GOOD IAW MD10-10-MM 52-10-01-2. 2 L 7 3 4F RT A22WE 2007050100032 20070501 00032 EU 2007 5 1 07FDEA01620 1 20070426 A 5220 DOOR AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 EMERGENCY EXIT CORROSION AT C42A-43A, P26 LT/RT REPAIR PERFORMED BY BLEND OUT IAW SRM 51-74-00 AND FLAP PEENING IAW SRM 51-29-00, APPROVED BY EA 6-5220-99215 AND RAS/DATLS/0003162/2006 ISS B. 2 L 7 2 4F RT A35EU 2007050100041 20070501 00041 WP 2007 5 1 07FDEA01631 1 20070426 A 5310 BEAM DOUG DC10 DC1010 3022110 WP CARGO DOORWAY CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 68050 47804 FWD PIT HAS CORROSION IN THE FORWARD LOWER CORNER BETWEEN DOOR SEAL AND BEAM. [SUP 05-30-07] REMOVED CORROSION FROM RA IL, VERIFIED BLEND OUT AND REMAINING THICKNESS, PER FEDEX EA 8-5350-109152. 2 L 7 3 4F A22WE 2007050100052 20070501 00052 EA 2007 5 1 QXEA200700644 1 20070417 A 2840 73811813 COMPUTER CNDAIR CL600 CL6002C10 1390015 EA FUEL QTY MALFUNCTIONED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 611QX 12487 10041 LIT - FLIGHT 4328 (LIT-DEN). RETURNED TO THE FIELD FOR FUEL CHANNEL 1/2 AND CROSS FLOW PUMP MESSAGES. FUEL QUANTITY SH OWING DASHES. UNEVENTFUL LANDING, MAINTENANCE REPLACED THE FUEL QUANTITY GAUGING COMPUTER. OPERATIONAL CHECKS GOOD. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007050100053 20070501 00053 WP 2007 5 1 ABXA070128 1 20070413 A 5610 TRACK DOUG DC9 DC941 302207N WP COCKPIT WINDOW MISSING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 FIRST OFFICER'S CLEARVIEW SLIDING WINDOW WOULD NOT OPEN. FOUND CAM FOLLOWER FOR FIRST OFFICER'S WINDOW MISSED TRACK OF UPPER LOCKING BAR. LUBED HINGE ASSEMBLY OF UPPER LOCKING BAR. WINDOW OPS CHECKS GOOD IAW DC9 MM 56-10-3. 2 L 7 2 4F A6WE 2007050100068 20070501 00068 WP 2007 5 1 07FDEA01574 1 20070424 A 5330 SKIN DOUG DC10 DC1010 3022110 WP ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 397FE 46631 MODIFICATION AND REPAIR ASSESSMENT RT WING DROP LEADING EDGE WITH WORN AND MISSING MATERIAL ON EXISTING REPAIR. REMOV ED INNER SKIN AND EXISTING REPAIR IAW SRM 51-31-01 VOL II. REPAIR DOUBLER, INSTALLED IAW SRM 57-10-00 FIG 55 VOL I. R EINSTALLED HINGE, FWD ANGLE INNER SKIN. 2 L 7 3 4F A22WE 2007050100069 20070501 00069 WP 2007 5 1 07FDEA01575 1 20070424 A 5512 SKIN DOUG DC10 DC1010 3022110 WP HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 HORIZONTAL STABILIZER LWR INT SKIN PANELS CONSTANT SECTION CRACKED INFLYABLE LIMIT ACCOMPLISH EA 8-5510-96122. 2 L 7 3 4F A22WE 2007050100083 20070501 00083 GL 2007 5 1 I5HA0758008 2 20070418 A 7200 PROBE CVAC 580 580 2422806 WP ALLSN 501D 501D13 03004 GL PT2 ICED A I5HA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 23 582 7010 475 700112 DURING CLIMBOUT, EN-ROUTE, AT APPROX 15,000 FT MSL, CREW OBSERVED THE RT ENGINE HORSEPOWER DECREASE TO APPROXIMATELY 600 ACCOMPANIED BY A CORRESPONDING DECREASE IN FUEL FLOW AND TIT. NO IMMEDIATE CHANGE IN RPM. CAPTAIN UNABLE TO MAKE ANY CHANGES IN ENGINE HORSEPOWER WITH POWER LEVER MOVEMENT. ENGINE WAS E-HANDLED IAW PROCEDURES IN QRH, ACFT RETURNED & LAN DED UNEVENTFULLY. CREW DID NOT DECLARE AN EMERGENCY. ENGINE INSPECTED FOR FOD. NONE FOUND. ALL FUEL FILTERS INSPECTE D & FOUND CLEAN EXCEPT LOW PRESSURE FILTER WHICH HAD A SMALL AMOUNT OF MATERIAL IN IT. LOW PRESSURE FUEL FILTER REPLACE D. MX CREW PERFORMED A LOW & HIGH POWER ENGINE RUN & COULD NOT DUPLICATE DISCREPANCY. ALL ENGINE PARAMETERS NORMAL. A 2 L 7 2 4T 4 T RT E282 2007050100091 20070501 00091 SO 2007 5 1 GUUA04220701 1 20070422 A 3350 OL3071BPELP BULB EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE EMERGENCY LIGHTS INOPERATIVE A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 29 268AS 120202 EMERGENCY LIGHTING ON CABIN FLOOR STRIP IN THE REAR ON AIRCRAFT NOT WORKING. REPLACED INOPERATIVE LIGHTS IN CABIN FLOOR STRIP. 2 L 7 2 4T 4 T RT A31SO E20NE 2007050100102 20070501 00102 GL 2007 5 1 CHQA200700011 2 20070424 A 7200 AE3007A1P ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 SMOKE A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 296SK 14121 5 145514 CAE311971 FLIGHT 6240, LAVATORY SMOKE DURING TAKEOFF. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE. NO SMOKE DURING OPS CHECK. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007050100106 20070501 00106 CE 2007 5 1 AMWA84156BC 1 20070423 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER DISCHARGED A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 133YV 22342 186 UE133 BATT CHARGE ANNUN ILLUM IN FLT. NO INCIDENTS, ACFT CONTINUED TO DESTINATION. THIS BATTERY CHARGE ILLUMINATION IS CONSI DERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS. REMOVED AND REPLACED BATTERY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007050100107 20070501 00107 CE 2007 5 1 DXTA200702151 1 20070427 A 2720 YAW DAMPER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MALFUNCTIONED E DXTA C ABORTED TAKEOFF J F WARNING INDICATION FLT CONT AFFECTED TO TAKEOFF 1 GL 07 939QS 7500193 EICAS MESSAGES, YAW DAMPER OFF LOWER, YAW DAMPER NOT CENTERED. (MACH TRIM OFF) ILLUMINATED DURING THE TAKEOFF ROLL AFT ER 40 KTS. [SUP 05-03-07] PERFORMED PITOT/STATIC LEAK CHECK AND FOUND NR 2 MADC PITOT FLEX LINE LEAKING. REPAIRED LINE IN ACCORDANCE WITH FAR 91.411 PART 43 APPENDICES E AND F AND CITATION 750 MM CH 34-11-08. PERFORMED LEAK CHECK AND FOUN D TO BE OK. EICAS MESSAGES NO LONGER DISPLAYED AT 40 KTS. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007050100108 20070501 00108 CE 2007 5 1 DXTA200702152 1 20070427 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE RIGHT WEAK E DXTA O OTHER O OTHER LD LANDING 1 GL 07 341QS 5600341 BRAKES ARE SPONGY AND SLOPPY FEELING DURING LANDING. RT SIDE PULSATED INTERMITTENTLY. [SUP 05-03-07] PERFORMED BRAKE & ANTI-SKID BLEEDING PROCEDURE 3 TIMES ON EACH WHEEL TO ENSURE REMOVAL OF ALL AIR FROM SYSTEM. LEAK CHECK GOOD. TAXIED A IRCRAFT FOR 20 MINUTES AT VARIOUS SPEEDS & BRAKE PRESSURES APPLIED WITH NO FAULTS NOTED. ALL WORK DONE IAW CE560 MM CHAP 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007050100113 20070501 00113 CE 2007 5 1 DXTA200702142 1 20070425 A 2120 UNKNOWN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE CABIN ODOR E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 332QS 5600523 SMELL OF FUMES FROM OVERHEAD WEMAC VENTS ESPECIALLY WHEN TEMPERATURE CONTROL IS ADJUSTED TO A WARMER SETTING. [SUP 05-0 2-07] INSPECTED ENGINES FOR INTERNAL OIL LEAKS. INSPECTED NR 1 ENGINE NR 3 BRG OIL TUBES WHILE ACCOMPLISHING ESVI - NO L EAKS NOTED. BORESCOPED NR 2 ENGINE NR 3 BEARING OIL TUBES - NO OIL LEAKS NOTED. ACCOMPLISHED GROUND RUNS - COULD NOT DUP LCATE SMELL. WORK DONE IAW JT15D-5D MM 3040342R20 DATED 5/12/06 2 L 7 2 4F 4 F RT A22CE E25EA 2007050100125 20070501 00125 CE 2007 5 1 DXTA200702126 1 20070421 A 5730 ACCESS PANEL CESSNA 560 560XL 2076702 CE LT WING MISINSTALLED E DXTA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 07 693QS 5605657 IN FLIGHT ABOVE 200 KTS THERE IS A RUMBLING VIBRATION THAT VIBRATES THE WHOLE AIRPLANE. IT CHANGES PITCH OR SEVERITY WI TH INCREASE IN SPEED, 250 KTS IS THE SPEED THAT IT IS MOST PRONOUNCED. FOUND ACCESS PANEL ON LOWER LT STUB WING NR 313A L TO BE OVERLAPPING PANEL NR 313AC AND OIL CANNING. TRIMMED PANEL NR 313AL IAW SRM OK 51-00-03 AND MM CH 53-30-00. INSTA LLED PANEL NR 313AL NO OIL CANNING PRESENT. 2 L 7 2 4F RT A22CE 2007050100150 20070501 00150 EA 2007 5 1 SWIA200718155 1 20070318 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 447SW 7677 RT MAIN GEAR BRAKE TRANSDUCER BRACKET CRACKED, DISCOVERED AT C-CHECK. INSTALLED BRACKET P/N 601R75262-157 IAW CRJ200 SR M 51-42-03. 2 L 7 2 4F RT A21EA 2007050100151 20070501 00151 EA 2007 5 1 SWIA200718156 1 20070318 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MOTOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 447SW 7677 PAX DOOR PULL IN MOTOR BRACKET IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED PN 601R317745-7 PER CRJ200 SRM 51-42-06 PG 11-18 AND 51-42-21 PG 17, 19. 2 L 7 2 4F RT A21EA 2007050100152 20070501 00152 EA 2007 5 1 SWIA200718158 1 20070318 A 5346 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 447SW 7677 RIGHT LOWER ENGINE BEAM WEB AT FORWARD INBOARD ACCESS PANEL CUTOUT IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED REPAIR DOUBLER, SHIM, STRAP AND ANGLE PER CRJ200 REO 601R 53-61-358 REV 'A' APRIL 31 2002. 2 L 7 2 4F RT A21EA 2007050100153 20070501 00153 EA 2007 5 1 SWIA200718159 1 20070403 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 927SW 7693 THIRD OVERHEAD EMERGENCY FLOODLIGHT IS INOP. REPLACED OVERHEAD EMERGENCY LIGHT IAW AMM 33-51-16. 2 L 7 2 4F RT A21EA 2007050100154 20070501 00154 EA 2007 5 1 SWIA200718160 1 20070418 A 3350 SIGN CNDAIR CL600 CL6002C10 1390015 EA CABIN MISSING A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 773SK 10236 FOUND OVERHEAD EMERGENCY EXIT SIGN IS MISSING. INSTALLED COVER PER CRJ MM CH 33-51-00. 2 L 7 2 4F RT A21EA 2007050100157 20070501 00157 SO 2007 5 1 SWIA200718163 1 20070423 A 3350 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 226SW 120296 WHITE EMERGENCY LIGHT AT ROW 7 INOP. RELAMPED WHITE EMERGENCY FLOOR LIGHT AT ROW 7. 2 L 7 2 4T RT A31SO 2007050100159 20070501 00159 EA 2007 5 1 SWIA200718165 1 20070328 A 5340 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 AFT EQUIPMENT BAY FS 625 LBL40 ANGLE CRACKED, DISCOVERED AT C-CHECK. REPLACED ANGLE AT FS 625 LBL 210 NEW PN 601-35012- 51 PO 71471 AS PER CRJ200 SRM REF 51-42-21 PG 1. 2 L 7 2 4F RT A21EA 2007050100160 20070501 00160 EA 2007 5 1 SWIA200718166 1 20070328 A 5720 CLAMP CNDAIR CL600 CL6002B19 1900309 EA CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 LEFT WING PICCOLO TUBE CLAMPS CRACKED INSIDE ACCESS PANELS 530FZ, 530GZ, 530JZ, 530AZ AND 530BZ, DISCOVERED AT C-CHECK. REPLACED CLAMPS INSIDE ACCESS PANELS 530FZ AND 530GZ WITH P/N 601R80004-7, PANEL 530JZ WITH P/N 601R8004-9, AND PANELS 530AZ AND 530BZ WITH P/N 600-800G1-9 PER CRJ200 AMM 30-11-41-000-801. 2 L 7 2 4F RT A21EA 2007050100164 20070501 00164 EA 2007 5 1 SWIA200718170 1 20070328 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 ENGINE SUPPORT BEAM LOWER WEB AT LBL15 AND RBL15 IS CRACKED IN THREE LOCATIONS, DISCOVERED AT C-CHECK. FABRICATED P/N 6 01R53-61-2129-51-6 SHIMS AND SPLICE ANGLES P/N 601R 641-2129-1/-2 PER CRJ200 REO 601R 53-61-2129 STEPS FIG 1/2. INSTALL ED ALL REPAIR PARTS ON LOWER AFT ENG WEB PER CRJ200 REO RE0 601R 53-61-2129 SB601R 53-068. 2 L 7 2 4F RT A21EA 2007050100165 20070501 00165 EA 2007 5 1 SWIA200718171 1 20070328 A 5240 BOLT CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 SERVICE DOOR CUT OUT LOWER DOWN LOCK ROLLER GUIDE BOLTS CORRODED, DISCOVERED AT C-CHECK. REMOVED AND REPLACED 8 BOLTS, 8 WASHERS (P/N AN960JD416), 8 WASHERS (P/N NAS1149CO463R) AND 8 NUTS IAW CRJ200 AMM TASK 20-21-00-944-001. 2 L 7 2 4F RT A21EA 2007050100167 20070501 00167 EU 2007 5 1 AWXA200700525 1 20070423 A 5321 D5367180500500 FLOOR PANEL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 664AW 1621 SAL - CORROSION ON AFT LAV AND GALLEY FLOOR PANEL 262 FF, FR 66 - FR 68. REPLACED AFT LAV AND GALLEY FLOOR PANEL 262 FF , FR 66 - FR 68 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007050100169 20070501 00169 EU 2007 5 1 AWXA200700527 1 20070421 A 5315 D5347219320000 FLOORBEAM AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 664AW 1621 SAL - FOUND CORROSION ON MAIN CABIN FLOORBEAM, FR 66 + 6" TO FR 70, -Y765. REPLACED MAIN CABIN FLOORBEAM, FR 66 + 6" TO FR 70, -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007050100170 20070501 00170 NM 2007 5 1 AWXA200700528 1 20070410 A 5311 654652652 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - FOUND CRACKED FRAME, BS 400, S9R. REPAIRED FRAME, BS 400, S9R IAW B737-300 SRM 53-00-07-2R2, FIGURE 201. 2 L 7 2 4F RT A16WE 2007050100171 20070501 00171 NM 2007 5 1 AWXA200700529 1 20070410 A 5311 654655211 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - FOUND CRACKED FRAME, BS 827, S9L. REPAIRED FRAME, BS 827, S9L IAW B737-300 SRM 53-00-07-2R2, FIGURE 201. 2 L 7 2 4F RT A16WE 2007050200002 20070502 00002 NM 2007 5 2 AWXA200700531 1 20070410 A 5311 654652927 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - CRACKED FRAME, BS 440, S9L. REPAIRED FRAME, BS 440, S9L IAW B737-300 SRM 53-00-07-2R2, FIGURE 201. 2 L 7 2 4F RT A16WE 2007050200003 20070502 00003 NM 2007 5 2 AWXA200700532 1 20070410 A 5311 654653232 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - FOUND CRACKED FRAME, BS 480, S9L. REPAIRED FRAME, BS 480, S9L IAW B737-300 SRM 53-00-07-2R2, FIGURE 201. 2 L 7 2 4F RT A16WE 2007050200007 20070502 00007 SO 2007 5 2 SIMA200712003 1 20070424 A 5101 UNKNOWN EMB 145 EMB145LR 3260212 SO FUSELAGE VIBRATION A SIMA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SW 21 657AE 145744 VIBRATION FELT INFLIGHT BETWEEN ROW 3 AND ROW 7. 2 L 7 2 4T RT T00011AT 2007050200008 20070502 00008 SO 2007 5 2 SIMA200712007 1 20070426 A 2720 UNKNOWN EMB 135 EMB135LR 3260305 SO RUDDER MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 723AE 145288 RUDDERS HARD TO MOVE ON TAKEOFF, YAW DAMPER FAILURE MESSAGE. PERFORMED AUTOPILOT OPERATIONAL CHECK IAW EMB AMM 22-11-00 WITH NO DEFECTS. PERFORMED RUDDER MANUAL AND AUTO SHUTOFF ADJUSTMENT TEST IAW EMB 27-25-00 WITH NO DEFECTS, RETURNED A IRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050200014 20070502 00014 SO 2007 5 2 SIMA200712014 1 20070428 A 2131 22250N030301 CONTROLLER EMB 145 EMB145LR 3260212 SO ZONE 200 FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 645AE 10317 3162 145212 LOST PRESSURIZATION INDICATION, UNABLE TO RE-PRESSURIZE IN MANUAL OR AUTO, RETURNED TO ROW. REMOVED AND REPLACED DIGITA L CONTROLLER IAW EMB AMM 21-31-01. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050200015 20070502 00015 EU 2007 5 2 AWXA200700546 1 20070429 A 5530 D5537123500600 HINGE FITTING AIRBUS 320 A320231 3930325 EU VERTICAL STAB WORN A AWXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 28 626AW 65 CREW REPORTED CLIMBING THROUGH FL 220 AT 340 KTS A/C VIBRATION FELT ON THE HORIZONTAL AXIS. MX REPLACED THE RUDDER HING E ARM FITTINGS: NR 1, NR 2, NR 3, NR 4, NR 5, AND NR 7. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVI CE. 2 L 7 2 4F RT A28NM 2007050200016 20070502 00016 EU 2007 5 2 AWXA200700535 1 20070427 A 5347 D53112827200 DUMMY RAIL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 664AW 1621 SAL - FOUND CORROSION ON MAIN CABIN DUMMY RAIL, FR12 - FR16, +Y503.2. REPLACED MAIN CABIN DUMMY RAIL, FR12 - FR16, +Y50 3.2 IAW A320 SRM 51-42-11. 2 L 7 2 4F RT A28NM 2007050200017 20070502 00017 EU 2007 5 2 AWXA200700536 1 20070427 A 5320 D53475765206 SILL AIRBUS 320 A320232 3930326 EU ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 664AW 1621 SAL - FOUND CORROSION ON BULK CARGO DOOR LOWER SILL, FR 60 - FR 61, -Y625 TO -Y680. REPAIRED BULK CARGO DOOR LOWER SIL L, FR 60 - FR 61, -Y625 TO -Y680 IAW A320 SRM 53-41-49. 2 L 7 2 4F RT A28NM 2007050200019 20070502 00019 NM 2007 5 2 AWXA200700538 1 20070409 A 5755 SKIN BOEING 737 73733A 1384673 NM ZONE 600 DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW MA2538 23627 MCN - RIGHT WING NR 5 SPOILER UPPER AND LOWER SURFACE HAS DISBONDED AREAS, WS 120.25 - WS 132.25. REPAIRED RIGHT WING N R 5 SPOILER UPPER AND LOWER SURFACE, WS 120.25 - WS 132.25 IAW A320 SRM 51-70-10-2R4 FIGURE 202. 2 L 7 2 4F RT A16WE 2007050200020 20070502 00020 NM 2007 5 2 AWXA200700539 1 20070410 A 5311 654652927 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - FOUND CRACKED FUSELAGE FRAME, BS 440, S9R. REPAIRED FUSELAGE FRAME, BS 440, S9R IAW B737-300 SRM 53-00-07-2R2, FI GURE 201. 2 L 7 2 4F RT A16WE 2007050200023 20070502 00023 NM 2007 5 2 AWXA200700542 1 20070410 A 5311 65465548 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - CRACKED FUSELAGE FRAME, BS 847, S9L. REPAIRED FUSELAGE FRAME, BS 847, S9L IAW B737-300 SRM 53-00-07-2R2, FIGURE 2 01. 2 L 7 2 4F RT A16WE 2007050200024 20070502 00024 NM 2007 5 2 AWXA200700543 1 20070410 A 5313 654988630 STRINGER BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - FOUND CRACKED STRINGER, BS 500C - BS 500D, S16R. REPAIRED STRINGER, BS 500C - BS 500D, S16R IAW AWA ER 03-5312-01 094-DD1. 2 L 7 2 4F RT A16WE 2007050200027 20070502 00027 EU 2007 5 2 07FDEA01630 1 20070426 A 5730 A57965171002 FAIRING AIRBUS 310 A310324 3930206 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 A 200 MM CRACK IN INNER FACE NEAR PIVOT POINT AT NR 4 LT MOVEABLE FAIRING BONDING REPAIR PERFORMED IAW EA 6-5720-99195 A ND RAS/FOK/069/2006 ISS A. 2 L 7 2 4F RT A35EU 2007050200044 20070502 00044 EA 2007 5 2 MASA200700023 1 20070110 A 3350 59256 INVERTER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 154SF 7154 ASH 7132 IAD. EMERGENCY LIGHT AT LEFT OVERWING EXIT INOP. MX REPLACED INVERTER. 2 L 7 2 4F RT A21EA 2007050200046 20070502 00046 EA 2007 5 2 MASA200700025 1 20070112 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EXIT SIGN DISCONNECTED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37218 7218 ASH 2765 PHX. EMERGENCY EXIT SIGN NEAR MAIN CABIN DOOR WILL NOT ILLUMINATE. MX RESECURED LOOSE CONNECTOR IN BACK OF SI GN AND LIGHT, OP CHECKED GOOD. 2 L 7 2 4F RT A21EA 2007050200047 20070502 00047 EA 2007 5 2 MASA200700026 1 20070112 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 917FJ 15017 ASH 2936 PHX. FWD SERVICE DOOR LOWER EMERGENCY LIGHT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2007050200048 20070502 00048 NM 2007 5 2 MASA200700027 1 20070113 A 3350 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 455YV 455 ASH 7084 DEN. TWO FWD EMERGENCY ESCAPE PATH LIGHT INOP. MX OPS CHECKED SYSTEM. OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2007050200049 20070502 00049 EA 2007 5 2 MASA200700029 1 20070114 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 930LR 15030 ASH 2688 CLT. SERVICE DOOR EMERGENCY FLOOD LIGHT COVER MISSING. MX REMOVED AND REPLACED BULBS AND LIGHT ASSEMBLY. 2 L 7 2 4F RT A21EA 2007050200050 20070502 00050 EA 2007 5 2 MASA200700169 1 20070328 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77278 7278 ASH 2920 PHX. FLOOR EMERGENCY PATH LIGHTING INOP. REMOVED AND REPLACED STRIP LIGHT. 2 L 7 2 4F RT A21EA 2007050200051 20070502 00051 EA 2007 5 2 MASA200700170 1 20070328 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77278 7278 ASH 2920 PHX. RT OVERWING LOWER EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED EXIT SIGN. 2 L 7 2 4F RT A21EA 2007050200052 20070502 00052 NM 2007 5 2 P5CA0701518 1 20070315 A 5230 STRUCTURE BOEING 747 74747UF 1384812 NM CARGO DOOR CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 496MC 29257 AFT LWR CARGO DOOR LWR FWD CORNER MINOR CHAFING V-SHAPE .125 INCH. INTERIM REPAIR FROM ENGINEERING PER DER-ISSUED FAA 8 110-3. 2 L 7 4 4F RT A20WE 2007050200060 20070502 00060 EA 2007 5 2 MASA200700199 1 20070410 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 905J 15005 ASH 2678 CLT. EMERGENCY LIGHTS TURN ON WHEN SELECTED TO ARMED. MX REMOVED AND REPLACED PCB5 IN JB-11. NO FURTHER DEFE CTS NOTED. 2 L 7 2 4F RT A21EA 2007050200061 20070502 00061 SO 2007 5 2 MASA200700200 1 20070412 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 ASH 7149 GSP. LEFT EMERGENCY EXIT DOOR LIGHT INOPERATIVE. CAPTAIN TURNED THE LIGHTS ON AGAIN AND THEN LIGHT OPS CHECKE D GOOD. 2 L 7 2 4T RT T00011AT 2007050200062 20070502 00062 EA 2007 5 2 MASA200700186 1 20070404 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75984 7489 ASH 7373 PIT. FWD EMERGENCY PATH, AMBER LIGHT STRIP INOP. MX RESECURED WIRING. 2 L 7 2 4F RT A21EA 2007050200063 20070502 00063 EA 2007 5 2 MASA200700187 1 20070405 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 931LR 15031 ASH 2610 SAV. CEILING LEVEL EMERGENCY FLOOD LIGHT INOP. MX RELAMPED FLOOD LIGHT. 2 L 7 2 4F RT A21EA 2007050200064 20070502 00064 EA 2007 5 2 MASA200700202 1 20070413 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 97325 7325 ASH 2825 PHX. FLIGHT DECK EMERGENCY FLASHLIGHT RED INDICATOR LIGHT NOT BLINKING. MX REPLACED FLASHLIGHT. 2 L 7 2 4F RT A21EA 2007050200065 20070502 00065 EA 2007 5 2 MASA200700209 1 20070415 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37218 7218 ASH 2916 COS. AFT LT EXTERNAL OVERWING EMERGENCY LIGHT INOP. MX RELAMPED THE LIGHT. 2 L 7 2 4F RT A21EA 2007050200066 20070502 00066 EA 2007 5 2 MASA200700214 1 20070417 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 909FJ 15009 ASH 2708 PHX. THREE EMERGENCY EXIT LIGHTS HAVE 1 BULB INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2007050200067 20070502 00067 EA 2007 5 2 MASA200700216 1 20070418 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77286 7286 ASH 2923 BFL. LEFT MID EXTERIOR EMERGENCY LIGHT INOP. MX RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2007050200068 20070502 00068 EA 2007 5 2 MASA200700217 1 20070422 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 570ML 7206 ASH 7125 IAD. CREW REPORTED ONE CEILING EMERGENCY FLOOD LIGHT INOP. MX RELAMPED, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007050200069 20070502 00069 EA 2007 5 2 MASA200700219 1 20070422 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37218 7218 ASH 2840 YUM. NR 3 CEILING EMERGENCY FLOOD LIGHT INOP. MX RELAMPED FLOOD LIGHT. 2 L 7 2 4F RT A21EA 2007050200070 20070502 00070 EA 2007 5 2 MASA200700224 1 20070423 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37228 7228 ASH 2925 PHX. LT EMERGENCY LOWER GREEN EXIT SIGN AT OVERWING EXIT WAS REPORTED AS INOP. MX PERFORMED SYSTEM OPERATIONA L CHECKS AND IT OPERATED NORMALLY. MX PERFORMED SYSTEM OPERATIONAL CHECKS AND EXIT SIGN OPERATED NORMALLY. 2 L 7 2 4F RT A21EA 2007050200071 20070502 00071 EA 2007 5 2 MASA200700038 1 20070120 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 909FJ 15009 ASH 2969 PHX. EMERGENCY FLOOD LIGHT INOP - 3RD AFT. MX RELAMPED FLOOD LIGHT. 2 L 7 2 4F RT A21EA 2007050200072 20070502 00072 EA 2007 5 2 MASA200700039 1 20070121 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 47202 7202 ASH 7320 IAD. PILOT REPORTED CEILING LEVEL EMERGENCY FLOOD LIGHTS AT ROW 5 INOP. MX RELAMPED FLOOD LIGHTS. 2 L 7 2 4F RT A21EA 2007050200073 20070502 00073 NM 2007 5 2 MASA200700042 1 20070121 A 3350 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 445YV 445 ASH 2039 DEN. FWD EMERGENCY EXIT LIGHT & SIGN ABOVE LAV INOP. MX REPLACED BATTERY PACK. 2 H 7 2 4T RT A13NM 2007050200074 20070502 00074 EA 2007 5 2 MASA200700046 1 20070122 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN WRONG PART A MASA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SW 07 7305V 7305 ASH 2802 PHX. EMERGENCY FLOOR LIGHTING AT ROW 8 NOT ORANGE IN COLOR. MX INSTALLED CORRECT FLOOR LIGHTING COVER. 2 L 7 2 4F RT A21EA 2007050200075 20070502 00075 EA 2007 5 2 MASA200700050 1 20070124 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT DIRTY A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 17175 7175 ASH 7391 MHT. LT OVERWING EMERGENCY EXIT DOOR CAUTION IN FLIGHT. MX CLEANED AND RESECURED PROX SENSOR, OPS CHECKED GO OD ON PRESSURE CHECK. 2 L 7 2 4F RT A21EA 2007050200077 20070502 00077 EA 2007 5 2 MASA200700167 1 20070328 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCONNECTED A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 17231 7231 ASH 2743 COS. REPORTED ONE FLOOR PATH LIGHT SEGMENT INOP. MX RECONNECTED WIRE. 2 L 7 2 4F RT A21EA 2007050200078 20070502 00078 EA 2007 5 2 MASA200700132 1 20070303 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 77286 7286 ASH 2752 PHX. PILOT REPORTED THE AFT CEILING LEVEL EMERGENCY FLOOD LIGHT INOP. MX RELAMPED THE LIGHT. 2 L 7 2 4F RT A21EA 2007050200079 20070502 00079 EA 2007 5 2 MASA200700140 1 20070307 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 37178 7178 ASH 2984 PHX. PAX DOOR AND SERVICE DOOR FLOOR EMERGENCY FLOOD LIGHTS HAD INOP BULBS. MX RELAMPED THE BULBS AS REQUIRED . 2 L 7 2 4F RT A21EA 2007050200082 20070502 00082 EA 2007 5 2 MASA200700151 1 20070319 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 75995 7361 ASH 7466 ORD. OVERHEAD EMERGENCY FLOOD LIGHT INOP AT ROW 3. RELAMPED OVERHEAD EMERGENCY FLOOD LIGHT. 2 L 7 2 4F RT A21EA 2007050200084 20070502 00084 EA 2007 5 2 MASA200700155 1 20070321 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 649BR 7414 ASH FLT 7193 ORD-ROC. EMERGENCY LIGHTS WILL NOT TURN OFF. MX RESET THE EMERGENCY LIGHTS CIRCUIT BREAKER AND THE SYSTEM OP CHECKED GOOD. 2 L 7 2 4F RT A21EA 2007050200086 20070502 00086 EA 2007 5 2 MASA200700164 1 20070326 A 3350 1317 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 931LR 15031 ASH 2610 SAV. CAPTAIN REPORTED THIRD AFT CEILING EMERGENCY LIGHT INOP. MX RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2007050200087 20070502 00087 EA 2007 5 2 MASA200700166 1 20070327 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77260 7260 ASH 2835 TUS. PILOT REPORTED THAT THE EMERGENCY LIGHT AT FLOOR LEVEL NEXT TO THE SERVICE DOOR WAS INOP. MX FOUND THE W IRE CONNECTING THE LIGHT ASSY WAS DAMAGED. REPAIRED THE WIRE, THE LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2007050200091 20070502 00091 EA 2007 5 2 TRAX200700554 1 20070422 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 974EV 7594 FS 484 AT RBL 36 INTERCOSTAL IS CRACKED AT TOP O/B RIVET. REMOVED CRACKED CLIP AT FS 484 RBL 36 INTERCOSTAL IAW CRJ 200 SRM 51-42-06 (1127/RA334) DUPLICATED CRACKED CLIP USING 2024T3.063 ALUMINUM IAW CRJ SRM 51-24-21. INSTALLED CLIP IAW C RJ SRM 51-42-21. SUPPLEMENTAL - SDR CLOSED 05/01/07. 2 L 7 2 4F RT A21EA 2007050200093 20070502 00093 EA 2007 5 2 TRAX200700556 1 20070422 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE J WARNING INDICATION CR CRUISE 1 SO 27 937EV 8042 FLAPS FAIL AT CRZ FL300 AT ZERO. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007050200094 20070502 00094 EA 2007 5 2 TRAX200700557 1 20070423 A 5320 BEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 750EV 10161 STA 280 BEAM CORRODED OUT OF LIMITS. REMOVED AND REPLACED STA 280 BEAM IAW REO 670-53-11-052. SUPPLEMENTAL - SDR CLOSE D 04/27/07. 2 L 7 2 4F RT A21EA 2007050200098 20070502 00098 EA 2007 5 2 TRAX200700564 1 20070424 A 5320 SILL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 750EV 10161 CORROSION FOUND ON RIGHT 280 FLOOR SILL RBL 45. 2 L 7 2 4F RT A21EA 2007050200099 20070502 00099 EA 2007 5 2 TRAX200700567 1 20070424 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 829AS 7232 CAPTAIN`S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007050200101 20070502 00101 EA 2007 5 2 TRAX200700570 1 20070425 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 856AS 7404 ASD FLOOD LIGHT AND BOTH FWD EXTERIOR EMERGENCY LIGHTS INOP. 2 L 7 2 4F RT A21EA 2007050200103 20070502 00103 EA 2007 5 2 TRAX200700573 1 20070426 A 3250 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA COCKPIT ACTIVATED A ASOA K NONE J WARNING INDICATION CL CLIMB 1 SO 27 761ND 10213 N/W/S INOP MESSAGE DURING FLT. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007050200105 20070502 00105 EA 2007 5 2 MASA200700069 1 20070202 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 37178 7178 ASH 2869 PHX. ALL EMERGENCY EXIT LIGHT ILLUMINATE WITH THE SWITCH IN THE ARM POSITION. MX RESET THE ESS BUSS C/B, AND THE SYSTEM FUNCTIONED NORMALLY. 2 L 7 2 4F RT A21EA 2007050200106 20070502 00106 EA 2007 5 2 MASA200700078 1 20070204 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 27173 7173 ASH 7157 BUF. EMERGENCY FLOOR LIGHTS AFT HALF INOP. MX RESECURED STRIP, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2007050300006 20070503 00006 NM 2007 5 3 SWAA072106 1 20070428 A 3350 OL3071BPEGPL LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED C3 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007050300007 20070503 00007 NM 2007 5 3 MASA200700037 1 20070119 A 3350 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 991HA 431 ASH 2885 PHX. CABIN EMERGENCY LIGHTS FLICKER IN ON POSITION. MX REMOVED AND REPLACED RELAY, OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2007050300012 20070503 00012 EA 2007 5 3 MASA200700087 1 20070210 A 3350 SIGN CNDAIR CL600 CL6002C10 1390015 EA CABIN DETACHED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 510MJ 10101 ASH 7455 ORD. CAPTAIN REPORTED THE EXIT SIGN ON FORWARD BULKHEAD WILL NOT STAY ATTACHED. MX RESECURED SIGN. 2 L 7 2 4F RT A21EA 2007050300013 20070503 00013 EA 2007 5 3 MASA200700089 1 20070210 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 37218 7218 ASH 2816 SBP. RIGHT SIDE EMERGENCY EXIT LIGHT INOP. MAINTENANCE SECURED THE CONNECTOR, OP'S GOOD. 2 L 7 2 4F RT A21EA 2007050300021 20070503 00021 EA 2007 5 3 MASA200700114 1 20070221 A 3350 110049 BATTERY CNDAIR CL600 CL6002D24 1390016 EA CABIN DISCHARGED A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 908FJ 15008 ASH 2699 CLT. SEVERAL EMERGENCY LIGHTS INOP IN CABIN. MX REPLACED THE BATTERY AND CHARGER. 2 L 7 2 4F RT A21EA 2007050300022 20070503 00022 EA 2007 5 3 MASA200700120 1 20070226 A 3350 STRIP CNDAIR CL600 CL6002D24 1390016 EA CABIN LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 921FJ 15021 ASH 2602 CLT. EMERGENCY FLOOR STRIP ROW 16 NOT SECURE. MX SECURED STRIP. 2 L 7 2 4F RT A21EA 2007050300029 20070503 00029 NM 2007 5 3 MASA200700130 1 20070302 A 3260 LIGHT DHAV DHC8 DHC8202 2809007 NM COCKPIT INOPERATIVE A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 455YV 455 ASH 7078 DEN. NOSE GEAR GREEN LIGHT NOT ILLUM ON EXT, ALT EXT NOSE GEAR LIGHT NOT ILLUM. MX RELAMPED, CLEANED PHOTO CE LL SOCKET. 2 H 7 2 4T RT A13NM 2007050300039 20070503 00039 WP 2007 5 3 UPS07849685 1 20070414 A 5320 5894282502 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 T-BOLT BACKUP FITTING CRACKED IN C-PIT TORQUE BOX, STA 1177 L33R UPPER AND LWR FLANGES. REMOVED DAMA GED FITTING AT STA 1177 L33R IAW SRM 51-1-20D. LOCATED DRILLED UP AND INSTALLED FITTING AT STA 1177 L33R IAW SRM 51-3-2 AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 2007050300042 20070503 00042 WP 2007 5 3 070108 1 20070426 A 3260 H1410168906 CONTROL SWITCH DOUG DC9 DC983 3022083 WP NLG INDICATOR MALFUNCTIONED A WX0A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 19 864GA 49912 RED NOSE GEAR LIGHT ILLUMINATED INFLIGHT WITH GEAR HANDLE UP. FLIGHT CREW FOLLOWED QRH AND LIGHT DID NOT EXTINGUISH. A IRCRAFT RETURNED TO LAS AND LIGHT WENT OUT ON DESCENT AND REDUCED AIRSPEED. MAINTENANCE DEPARTMENT REMOVED AND REPLACED CONTROL SWITCH REF AMM 32-21-01 AND PERFORMED OPERATIONAL CHECK OF NOSE GEAR LANDING GEAR REF AMM 32-60-00. OPERATIONA L CHECK NORMAL. AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007050300043 20070503 00043 NE 2007 5 3 QXEA200700687 2 20070426 A 7532 4121T67P02 BLEED VALVE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE NR 2 ENGINE LEAKING A QXEA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 614QX 13620 10049 PDX - FUEL LEAKING FROM NR 2 ENGINE. MAINTENANCE REPLACED THE OBV VALVE IAW 75-31-01-000-801-A01 AND 75-31-01-400-801-A 01. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007050300044 20070503 00044 EU 2007 5 3 F3LA200700094 1 20070424 A 5320 D53480043206 SILL AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 801FR 4759 1939 DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR SILL PLATE HAD CORROSION FWD OF FR66. REPLACED L2 DOOR SILL IAW 51-42-11, FIG 6 AND 7. 2 L 7 2 4F RT 2007043000172 20070430 00172 NM 2007 4 30 SWAA072049 1 20070425 A 5340 65C27314 STRINGER CLIP BOEING 737 7373L9 1384470 NM BS 747 S11L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000180 20070430 00180 NM 2007 4 30 SWAA072081 1 20070426 A 5311 6546551 FRAME BOEING 737 7373L9 1384470 NM BS 807 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007043000186 20070430 00186 NM 2007 4 30 SWAA072068 1 20070426 A 5340 65CC27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 767 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007043000194 20070430 00194 NM 2007 4 30 SWAA072073 1 20070426 A 3350 3071BPEGPL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007043000195 20070430 00195 NM 2007 4 30 SWAA072063 1 20070426 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 225WN 34333 FOUND EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007043000201 20070430 00201 NM 2007 4 30 SWAA072072 1 20070426 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 734A S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 734A, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007043000202 20070430 00202 NM 2007 4 30 SWAA072070 1 20070426 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 934 S20L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007050100004 20070501 00004 NM 2007 5 1 07FDEA01589 1 20070425 A 5754 SLAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 RIGHT WING, LEADING EDGE SLAT TRACK NR 14 CUT-OUT FOUND WITH 0.4375 INCH CRACK. [SUP 05-16-07] CUTOUT CRACKED AREA T RIMMED OUT AND REPAIRED AS PER SRM 57-10-00 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050100007 20070501 00007 NM 2007 5 1 07FDEA01592 1 20070425 A 2130 39854021 SHUTOFF VALVE BOEING 727 727277 138408S NM CABIN PRESSURE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 243FE 21480 DURING CLIMB-OUT CABIN ALTITUDE WAS NOTED AT 7,500' CLIMBING THRU FL220 WITH BOTH PACKS ON AND CARGO HEAT OUTFLOW VALVE CLOSED. SWAPPED BLEEDS WITH NO EFFECT. ATTEMPTED STANDBY MODE AS WELL AS MANUAL MODE WITH NO EFFECT. OUTFLOW VALVE W AS FULLY CLOSED IN DC MODE WITH NO EFFECT. TROUBLESHOOTING PRESS PROBLEM. ON BLOCK IN FOUND ALL DOORS SECURE AND PER C REW DE-BRIEF PACKS APPEARED TO BE OPERATING NORMALLY. FOUND RT PACK VALVE FAILED CLOSED. REMOVED AND REPLACED RT FWD P ACK VALVE IAW MM 21-55-071-0. PRESS OPS CK GOOD PER MM 21-31-000-5. 2 L 7 3 4F RT A3WE 2007050100017 20070501 00017 EU 2007 5 1 07FDEA01604 1 20070426 A 5311 A53879305200 FRAME AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 EXFOLIATION CORROSION AT C49, P14-15 LT REPAIR PERFORMED BY BLEND OUT THE CORROSION IAW. SRM 51-74-10 AND FLAP PEENING I AW. SRM 51-29-00, APPROVED BY EA 6-5315-99194 AND RAS/DATLS/0003112/2006 ISS. A 2 L 7 2 4F RT A35EU 2007050100018 20070501 00018 NM 2007 5 1 07FDEA01605 1 20070426 A 5711 ARB74132 SPAR DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 RIGHT WING, REAR SPAR UPPER CAP AT ABOUT STA XORS 1042 FOUND WITH CORROSION. [SUP 05-14-07] REMOVED AS PER SRM 57-21 -01 VOLUME II. MATERIAL REMOVED =0.043" ORIGINAL THICKNESS =0.136", REMAINING THICKNESS =0.093" AND FOUND EXCEEDED L IMITS AS PER 57- 20-00 VOLUME I FIGURE 16. REPAIR CARRIED OUT AS PER FEDEX EA 15710-109869. 2 L 7 3 4F RT A22WE 2007050100020 20070501 00020 NM 2007 5 1 07FDEA01607 1 20070426 A 5711 ARB74142 SPAR DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 RIGHT WING, REAR SPAR LOWER CAP AT ABOUT STA XORS 1046-1050 FOUND WITH CORROSION. [SUP 05-14-07] REMOVED AS PER SR M 51-21-01 VOLUME II. MATERIAL REMOVED= 0.064", ORIGINAL THICKNESS= 0.108", REMAINING THICKNESS= 0.044", AND EXCEEDED LIMITS AS PER SRM 57-20-00 VOLUME I, FIGURE 16. REPAIR CARRIED OUT ON REWORKED AREA AS PER FEDEX EA 1-5710-109870. R EPAIR CLASSIFIED AS MAJOR PER GMMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050100022 20070501 00022 EU 2007 5 1 07FDEA01609 1 20070426 A 5313 A53811371202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 FOUND CORROSION IN AIR CONDITIONING COMPARTMENT ON KEEL BEAM C45/46, P51 LT, PANEL C40/42, P50- 51 LT, STRINGER P 50 LT , C43-44. REPAIR PERFORMED BY BLEND OUT THE CORROSION ON KEEL BEAM AND PANEL IAW SRM 51-74-10 AND STRINGER REPAIR ON P5 0, C43-44 IAW TD 044433/004/2006 ISS C, APPROVED BY EA 6-5315-99214 AND RAS 044433/005/2006 ISS A. 2 L 7 2 4F RT A35EU 2007050100023 20070501 00023 EU 2007 5 1 07FDEA01610 1 20070426 A 5714 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 CORROSION ON CENTER WING BOX TOP SKIN TRACK 4-5 LT, C 42-47; TRACK 3-4 LT, C46.1-47; TRACK 2-3 RT, C47; TRACK 4-5, C47; TRACK 4 RT, C40 REPAIR PERFORMED BY BLEND OUT CORROSION AND INSTALLING OVERSIZE FASTENER IN ALL AREA AND IN ADDITION INS TALLING A REPAIR DOUBLER BETWEEN TRACK 4-5, C44.1-45 AND 42.2-43.2, APPROVED BY EA 6-5710-99188 AND RAS 043898/038/2006 ISS.A. 2 L 7 2 4F RT A35EU 2007050100027 20070501 00027 EU 2007 5 1 07FDEA01615 1 20070426 A 5340 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 809FD 449 FOUND OLD MISDRILLED HOLES HOLES ON CORNER FITTING C 23, 24, 25 LT. REPAIR PERFORMED BY REPLACEMENT OF PART A537-73644 -204 (2) AND A537-73644-208 IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007050100029 20070501 00029 EU 2007 5 1 07FDEA01617 1 20070426 A 5310 A53980071203 BEAM AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 OLD GROOVES ON LONGITUDINAL BEAM C73A-75A, P26 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007050100035 20070501 00035 EU 2007 5 1 07FDEA01623 1 20070426 A 5313 A53986212 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 CORROSION AT STRINGER P56, C66-70; LT STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007050100044 20070501 00044 NM 2007 5 1 QXEA200700685 1 20070425 A 3150 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM NR 2 BLEED WARNING LIGHT A QXEA O OTHER J WARNING INDICATION TO TAKEOFF 1 NM 09 415QX 4081 SEA FLIGHT NR 2373: NR 2 BLEED HOT CAUTION. PERFORMED CHECKLIST. LIGHT WENT OUT (DURING TAKEOFF). MAINTENANCE INTERRO GATED CDS. NO FAULTS FOUND. C/W OPS TEST OF THE BLEED AIR SYSTEM IAW AMM 30-11-00-710-002. OPS CHECK GOOD. NO OTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT OK FOR CONTINUED SERVICE. 2 H 7 2 4T RT A13NM 2007050100046 20070501 00046 2007 5 1 QXEA200700618 4 20070415 A 3410 8220372436 DADC CNDAIR CL600 CL6002C10 1390015 EA MALFUNCTIONED A QXEA O OTHER P NO WARNING INDICATION CR CRUISE 1 NM 09 615QX 7493 10065 PDX - WHILE IN TURBULENCE FO'S PFD DISPLAY LOST AIRSPEED HEADING AND ALTITUDE INFORMATION. AFTER 20-30 SECONDS DISPLAY BACK TO NORMAL. MAINTENANCE REPLACED THE DADC. OPERATIONAL CHECKS GOOD AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007050100064 20070501 00064 WP 2007 5 1 07FDEA01571 1 20070424 A 5330 SKIN DOUG DC10 DC1010 3022110 WP ZONE 100 DAMAGED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 373FE 46611 LWR NOSE SKIN ACCIDENTAL DAMAGE AT STA 458 X=16 LT TO X=16 RT REPAIR IAW SRM 53-20-00 FIG 6 SH16 VOL1. 2 L 7 3 4F A22WE 2007050100066 20070501 00066 EU 2007 5 1 AWXA200700505 1 20070422 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHT FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 655AW 1075 PHX - EES - MX REPORTED POWER SUPPLY ROW 8A/C RIGHT INOP. MX REPLACED THE POWER SUPPLY AT ROW 8 A/C. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007050100079 20070501 00079 CE 2007 5 1 DXTA200702158 1 20070428 A 4920 APU CESSNA 680 680CE 2076811 CE SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 362QS 6800051 STARTED APU. TURNED BLEED ON AND COCKPIT FILLED WITH A BLUE - GRAY SMOKE, WE COULD NOT SMELL OIL OR ELECTRICAL ODOR. SHU T EVERYTHING DOWN. [SUP 05-03-07] APU OIL LEVEL WAS FOUND OVER SERVICED. CORRECTED SERVICING IAW HONEYWELL MM 49-90-0 0. REMOVED AND REPLACED CONDENSOR SOCK IAW 680 MM 12-19-00. ALL OPS CHECKS AND LEAK CHECKS GOOD. 2 L 7 2 4F RC T00012WI 2007050100097 20070501 00097 CE 2007 5 1 DXTA200702121 1 20070419 A 3240 BRAKE ASSY CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG WORN E DXTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 964QS 7500164 WHILE TAXIING AC PULLS HARD LEFT. PERFORMED GVI OF LT AND RT MAIN BRAKE ASSY'S NO LEAKS OR DEFECTS NOTED. PERFORMED BRA KE WEAR INDICATOR CHECK ON LT AND RT BRAKE ASSY'S LT IB BRAKE ASSY WAS THE SHORTEST AT .2500 INCH REMAINING. PERFORMED TAXI OF AC AT 50-60 KTS WITH NO PULLING NOTED. IAW MM 32-41-00, 32-42-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007050100101 20070501 00101 CE 2007 5 1 041507N318CS1 1 20070415 A 2731 55654509295 ACTUATOR CESSNA 500 550 2076604 CE ELEVATOR TRIM CONTAMINATED E Z5FA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 EA 63 318CS 5501029 DURING DECENT THROUGH 6000 FT MSL, ELEVATOR TRIM FROZE. BOTH MANUAL AND ELECTRIC OPERATION OF TRIM INOPERATIVE. CREW DEC LARED AN EMERGENCY, DIVERTED FROM SCHEDULED DESTINATION. AIRCRAFT LANDED WITHOUT INCIDENT. WATER WAS FOUND IN BOTH MAN UFACTURED LT AND RT TRIM ACTUATORS, PN 5565450-92 AND -95. ON SITE MAINTENANCE LUBRICATED TRIM ACTUATORS EXPELLING WATER AND PERFORMED OPERATIONAL CHECKS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 4F A22CE 2007050100148 20070501 00148 NM 2007 5 1 DU4R2007109 1 20070417 A 5330 SKIN BOEING 757 757232 1384965 NM BS 480 S8-9R DAMAGED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 6709 30481 FOUND LIGHTNING STRIKE AT BS 480 BETWEEN S-8R AND S-9R. REPAIRED BY CUTTING OUT STRIKE AREA 2.45" BY 1.42", HFEC CUTOUT , NO RELEVANT INDICATIONS. FABRICATED AND INSTALLED REPAIR PLATE 10 BY 15 FROM 7075-T6 .050”, FILLER FROM 7075-T6 .040" AND SHIMS FROM 7075-T6 .032" IAW B757 SRM 53-00-01 FIG 201 REPAIR 4 AS DIRECTED BY TIMCO RFTS NR 60004 DATED 4-10-2007. 2 L 7 2 4F RT A2NM 2007050100156 20070501 00156 EA 2007 5 1 SWIA200718162 1 20070420 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 608SK 10252 THE NR 3 OVERHEAD EMERGENCY LIGHT IS INOP. RELAMPED LIGHT IAW MM 33-51-00. 2 L 7 2 4F RT A21EA 2007050100161 20070501 00161 EA 2007 5 1 SWIA200718167 1 20070328 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 FLOOR SUPPORT STRUCTURE AT FS 484 RBL 30 HAS A CRACKED ANGLE, DISCOVERED AT C-CHECK. REPLACED CLIP PN 601R31171-9 PER R EO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2007050100162 20070501 00162 EA 2007 5 1 SWIA200718168 1 20070328 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 FS 280 RBL 9 FLOOR SUPPORT UPPER ANGLE IS CRACKED, DISCOVERED AT C-CHECK. FABRICATED AND INSTALLED REPAIR PART -6, -4 S PLICE ANGLE AND -2 FILLER ANGLE IAW CRJ 200 SRM 51-42-10 AND REO 601R-53-11-137 REV NC. 2 L 7 2 4F RT A21EA 2007050100163 20070501 00163 EA 2007 5 1 SWIA200718169 1 20070328 A 5720 SHROUD CNDAIR CL600 CL6002B19 1900309 EA RIGHT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 RIGHT L/E OUTBOARD SECTION SHROUD CRACKED, DISCOVERED AT C-CHECK. INSTALLED NEW SHROUD PER CRJ200 SRM REF 57-41-29 AND CRJ200 SRM REF 51-25-00 PG 1. 2 L 7 2 4F RT A21EA 2007050200011 20070502 00011 SO 2007 5 2 SIMA200712004 1 20070425 A 7500 23073462125 CLAMP EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LEFT ENGINE MISSING A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 693AE 6155 2322 14500868 CAE312733 RECEIVED ENGINE ONE ATTCS NO MARGAIN AND EXCEEDANCE ON TAKEOFF, LOW SPEED ABORT. INSTALLED NEW V-BAND CLAMP ON LEFT UPP ER COMPRESSOR BLEED LINE IAW ROLLS ROYCE MM 75-31-00. LEAK CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007050200053 20070502 00053 EA 2007 5 2 MASA200700171 1 20070328 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77286 7286 ASH 2765 PHX. ORANGE ESCAPE PATH LIGHTING INOP AT THE SERVICE DOOR. MX REMOVED AND REPLACED THE STRIP, OPS NORMAL. 2 L 7 2 4F RT A21EA 2007050200054 20070502 00054 EA 2007 5 2 MASA200700175 1 20070331 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 930LR 15030 ASH 2601 CLT. TWO CEILING EMERGENCY FLOOD LIGHTS INOP. MX RELAMPED FLOOD LIGHTS. 2 L 7 2 4F RT A21EA 2007050200055 20070502 00055 EA 2007 5 2 MASA200700180 1 20070402 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 650ML 7137 ASH 7429 IAD. PILOT REPORTED EMERGENCY ESCAPE PATH LIGHTS ROWS 2-6 INOP AND LOWER LEFT OVERWING EMERGENCY LIGHT INOP. MX WAS CALLED OUT AND OPS CHECKED THE EMERGENCY LIGHT, OPS CHECK WAS GOOD. NO DEFECT WERE NOTED. 2 L 7 2 4F RT A21EA 2007050200056 20070502 00056 EA 2007 5 2 MASA200700183 1 20070403 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17156 7156 ASH 7321 ORD. EMERGENCY FLOOR PATH LIGHTING INOP AT ROW 10. MX CALLED OUT AND FOUND CONNECTION NOT SECURED PROPERLY. RECONNECTED CONNECTION. 2 L 7 2 4F RT A21EA 2007050200057 20070502 00057 EA 2007 5 2 MASA200700184 1 20070403 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27318 7318 ASH 2737 PHX. PILOT REPORTED THE RIGHT AFT EMERGENCY EXIT LIGHT INOP. MX RELAMPED EMERGENCY EXIT LIGHT. 2 L 7 2 4F RT A21EA 2007050200058 20070502 00058 EA 2007 5 2 MASA200700191 1 20070407 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 932LR 15032 ASH 2757 PHX. THE 2ND EMERGENCY CEILING LIGHT INOP. MX RELAMPED EMERGENCY CEILING LIGHT. 2 L 7 2 4F RT A21EA 2007050200059 20070502 00059 EA 2007 5 2 MASA200700193 1 20070407 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCONNECTED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 97325 7325 ASH 2925 PHX. FWD HALF OF THE EMERGENCY FLOOR LIGHTS INOP. MX RECONNECTED THE LIGHT STRIPS AND OP CHECKS WERE GOOD. 2 L 7 2 4F RT A21EA 2007050200088 20070502 00088 NM 2007 5 2 MASA200700061 1 20070128 A 3350 POWERPACK DHAV DHC8 DHC8202 2809007 NM CABIN FAULTY A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 454YV 454 ASH 7065 DEN. PAX DOOR EMERGENCY ESCAPE LIGHT INOP. MX REPLACED THE POWER PACK. 2 H 7 2 4T RT A13NM 2007050200095 20070502 00095 EA 2007 5 2 TRAX200700560 1 20070423 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 683BR 7692 CAOT FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007050200096 20070502 00096 EA 2007 5 2 TRAX200700561 1 20070423 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 752EV 10166 FWD PAX DOOR OUTER HANDLE BROKEN. 2 L 7 2 4F RT A21EA 2007050200104 20070502 00104 EA 2007 5 2 MASA200700065 1 20070130 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 75991 7422 ASH RON CAE. ALL EMERGENCY LIGHTS INOP. MX REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERY PACKS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007050300011 20070503 00011 EA 2007 5 3 MASA200700084 1 20070208 A 3350 BUTTON CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS POPPED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27172 7172 ASH 7278 IAD. PILOT REPORTED THAT THE EMERGENCY LIGHTS CONTROL BUTTON WAS POPPED. MX RESET THE C/B AND OPS CHECKED EME RGENCY LIGHTS, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007050300018 20070503 00018 EA 2007 5 3 MASA200700112 1 20070221 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXIT SIGN INOPERATIVE A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 649BR 7414 ASH 7262 IAD. MAIN PAX DOOR EMERGENCY EXIT SIGN BULBS BURNED OUT. MX RELAMPED SIGN. 2 L 7 2 4F RT A21EA 2007050300045 20070503 00045 EU 2007 5 3 F3LA200700095 1 20070424 A 5320 D53480043206 SILL AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 801FR 4759 1939 DURING C-3 CHECK, INSPECTION REPORTED CORROSION IN NUTPLATE HOLES ON THE L2 DOOR SILL PLATE AT FR66. REPLACED L2 DOOR S ILL IAW SRM 51-42-11, FIG 6 AND 7. 2 L 7 2 4F RT 2007050300046 20070503 00046 EA 2007 5 3 QXEA200700689 1 20070428 A 2613 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA OVERHEAD DETECT DIRTY A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 613QX 10045 PDX - AFTER REACHING CRUISE ALTITUDE, A MLG BAY OVERHEAT WARNING CAME ON FOLLOWED BY A BAY OVERHEAT CAUTION. THEY WENT OUT, THEN THE MLG BAY CAUTION CAME BACK ON AND STAYED ON. ALL BTMS INDICATIONS GREEN. RAN CHECKLIST AND MLG BAY OVERHE AT WENT OUT AND STAYED OUT. MAINTENANCE FOUND NO FAULTS IN HISTORY. CLEANED AND RESEATED CONNECTORS. OPERATIONAL CHEC KS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007050300047 20070503 00047 EA 2007 5 3 A6WA200740211 1 20070421 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 454AW 7842 RIGHT OBLIQUE ANGLE AT FS 625 IS CRACKED 1 INCH LONG. (M) MAINTENANCE REMOVED AND INSTALLED NEW SERVICEABLE OBLIQUE AN GLE IAW SRM 51-42-06. (K) 2 L 7 2 4F RT A21EA 2007050300048 20070503 00048 EA 2007 5 3 TRAX200700566 1 20070424 A 3250 STEERING SYS CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A ASOA K NONE J WARNING INDICATION CR CRUISE 1 SO 27 839AS 7284 IN FLIGHT NOSE WHEEL STEERING INOP CAUTION MESSAGE. COMPLIED WITH QRH. CAUTION MESSAGE PERSISTED. LANDED WITH NOSE WH EEL STEERING INOP. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007050300050 20070503 00050 SW 2007 5 3 041907 1 20070419 A 5340 ES10119 SPACER GULSTM 500 500B 0141106 SW NLG STEERING ACT BROKEN E ZJWA O OTHER E VIBRATION/BUFFET LD LANDING 1 CE 05 518TM 500B99526 PILOT REPORTED A VIOLENT NOSE SHIMMY ON LANDING. THE LINK STUD ON THE SPACER ASSEMBLY P/N ES10119 HAD BROKEN CAUSING TH E STEERING ACTUATOR TO NO LONGER BE ATTACHED TO THE NOSE COLLAR. 1 H 7 2 3O 6A1 2007050300051 20070503 00051 NM 2007 5 3 UPS07M49673 1 20070205 A 5753 NRC6753503 STOP FITTING DOUG MD11 MD11F 3023600 NM LT WING TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:C LT WING O/B FLAP MID STOP FITTING FOUND WITH CRACK AS MARKED. LHW O/B FLAP I/B AND O/B HINGE ASSY, CA RRIAGE, VANE TRACK AND HINGE FAIRING SUPPORT REMOVED PER CMM 57-52-04 R.57 AND SRM 51-31-01 V.II R.38 SEND OUT FOR REPAI R. LHW OB FLAP IB AND OB HINGE ASSY, VANE TRACK AND HINGE FAIRING SUPPORT INSTALLED PER CMM 57-52-04 R.57 AND SRM 51-31 -01 V.II R. FUNCTIONAL CHK AND RIGGING CARRIED OUT PER AMM 27-50-00 R.55. 2 L 7 3 4F RT A22WE 2007050300052 20070503 00052 NM 2007 5 3 UPS07M49675 1 20070329 A 5320 WEB DOUG MD11 MD11F 3023600 NM BS 1450 CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C RH MLG W/W, FUSELAGE SIDE DOOR CUTOUT AT STA 1450 RBL 105 01 EA WEB ON O/B EDGE FOUND CHAFFED AS MARKE D. CHAFE MARK REMOVED, FOUND EXCEED LIMIT ORIG THK 0.040" MATL REMOVED 0.032" REMAIN THK 0.008" PER SRM 53-00-01 FIG3 V OLIR38. DAMAGED WHEN REMOVED PER SRM51 -35-01VOLIIR38. FAB NEW WEB PER BOEING DWG ANB7180REVAF MATL 7075-0.04 0". HEA T TREAT PER DPS7.00-1 AND HRB82.4 PER DPS1.05-3. HOLES PICKUP AND PROTECTED PER SRM 51-35-01 AND 51-21-01VIIR38. INSTA LL PER SRM 51-35-01 VOL IIR38. 2 L 7 3 4F RT A22WE 2007050300056 20070503 00056 WP 2007 5 3 IXXA070023O 1 20070426 A 3260 STRIKER DOUG DC8 DC873F 302199F WP ZONE 700 OBSTRUCTED A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 602AL 91770 2098 45991 DURING CLIMB-OUT OF KTOL, THE UPLATCH CHECK FAILED LIGHT AND FLICKERED, THEN REMAINED ON. THE CREW ACCOMPLISHED ALL NEC ESSARY PROCEDURES, THE LIGHT REMAINED ILLUMINATED. THE CREW CONTINUED FLIGHT AND FELT A MODERATE BUMP. THE CREW RETURN ED TO KTOL AND LANDED WITH OUT INCIDENT. MAINTENANCE REPLACED MAIN LANDING GEAR DOORS LIGHT SOCKET, AND INSPECTED MAIN LANDING GEAR DOORS AND FOUND LEFT MAIN LANDING GEAR DOOR SWITCH STRIKER CATCHING ON SEAL RETAINER, TRIMMED SWITCH STRIKE R. JACKED AIRCRAFT AND PERFORMED EXTENSION AND RETRACTION SIX TIMES IAW DACO DC8 MAINTENANCE MANUAL 32-30-0. NO OTHER DEFECTS FOUND. MAINTENANCE PERFORMED OPERATIONAL CHECK ON MAIN LANDING GEAR DOOR LIGHT. CHECK WAS GOOD IAW DACO DC8 MA 2 L 7 4 4F RT 4A25 2007050300057 20070503 00057 EU 2007 5 3 F3LA200700096 1 20070424 A 5320 D53480043206 SILL AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 801FR 4759 1939 DURING C-3 CHECK, INSPECTION REPORTED CORROSION IN NUTPLATE HOLE UNDER THE FWD GIRT FITTING ON THE L2 DOOR SILL. REPLAC ED L2 DOOR SILL IAW SRM 51-42-11, FIG 6 AND 7. 2 L 7 2 4F RT 2007050300058 20070503 00058 NM 2007 5 3 CALA0700201 1 20070424 A 5310 507945178 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 L1 DOOR FRAME CRACKED AT NR 6 AFT DOOR STOP. REPAIRED IAW ECRA 5210-01934 2 L 7 2 4F RT A16WE 2007050300059 20070503 00059 NM 2007 5 3 CALA0700202 1 20070424 A 5310 507945178 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSLEAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 L1 DOOR FRAME CRACKED AT NR 7 AFT DOOR STOP. REPAIRED IAW ECRA 5210-01934. 2 L 7 2 4F RT A16WE 2007050300064 20070503 00064 NM 2007 5 3 CALA0700207 1 20070425 A 5311 6546552 FRAME BOEING 737 7373T0 1384582 NM BS 827 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 FOUND CRACKED FRAME AT STA 827 STR9 RT. REPAIRED IAW ECRA 5310-04622. 2 L 7 2 4F RT A16WE 2007050300065 20070503 00065 EU 2007 5 3 F3LA200700097 1 20070424 A 5320 D5347043620800 SPLICE AIRBUS A318 A318111 3940019 EU L2 DOOR SILL CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 801FR 4759 1939 DURING C-3 CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON OTBD UPPER ANGLE AFT ATTACHMENT HOLE UPON REMOVAL OF L2 DOO R SILL SPLICE ANGLES FWD OF FR66. REPLACED L2 DOOR SILL SPLICE ANGLES IAW SRM 51-42-11, FIG 6 AND 7. 2 L 7 2 4F RT 2007050300068 20070503 00068 EA 2007 5 3 TRAX200700551 1 20070419 A 2620 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA EXTINGUISH SYS ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 975EV 7599 CARGO BOTTLE LOW MSG ILLUMINATED ON DEPARTURE. RETURNED TO GPT. EMERGENCY DECLARED. FLT 4546 DEL 200 MINS. CARGO COM PARTMENT FIRE EXTINGUISHING SYSTEM. 2 L 7 2 4F RT A21EA 2007050300069 20070503 00069 NM 2007 5 3 ANCF200700009 1 20070501 A 4940 A703CD CONTACTOR BOEING 767 767383 1385214 NM APU START FAILED W ANCF F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 23 984AN 24357 APU FAILED TO START FAULT LIGHT ILLUM AND EICAS MSG. APU FAULT DISPLAYED, ADDITIONAL START ATTEMPTS UN SUCCESFULL. VIS UALLY SMOKE WAS DETECTED IN THE APU AREA AND APU FIRE EXTINGUISHER SYSTEM WAS USED. IN ACCORDANCE WITH WDM 49-41-11 PAG E 1 THE WIRES W020-032-24 AND W1050-033-24 WERE CHECKED BY CONTINUITY AND ISOLATION. THE APU CRANK CONTACTOR K117 WAS R EPLACED IN ACCORDANCE WITH AMM 49-41-05 PAG 401 AND APU START RELAY K197 WAS REPLACED TOO. IN ACCORDANCE WITH AMM 49-61 -05 PAGE 401 THE ECU WAS REPLACED AND IN ACCORDANCE WITH AMM 24-31-04 PAGE 401 THE APU BATTERY WAS REPLACED. AUXILIARY POWER UNIT WAS REMOVED AND REPLACED IN ACCORDANCE WITH AMM 49-11-01 PAGE 401. TEST SATISFACTORY. FIRE EXTINGUISHER SYST 2 L 7 2 4F RT A1NM 2007050300070 20070503 00070 EU 2007 5 3 F3LA200700087 1 20070421 A 5315 D5347209001000 FLOORBEAM AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 801FR 4759 1939 DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE ON FLOORBEAM Y1292, AFT OF FR66. REPLACED FLOORBEAM AT Y1292 AFT OF FR66 IAW SRM 51-42-11, FIG 6 AND 7. 2 L 7 2 4F RT 2007050300071 20070503 00071 EA 2007 5 3 TRAX200700576 1 20070418 A 5260 STEP CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 659CA 10153 PAX DOOR, TOP STEP, FWD BASE RADIUS CRACKED, (MARKED). 2 L 7 2 4F RT A21EA 2007050300074 20070503 00074 EA 2007 5 3 TRAX200700578 1 20070423 A 5320 INTERCOSTAL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 659CA 10153 INTERCOSTAL AFT OF EXTERNAL POWER RECEPTICAL BOX DAMAGED IN RADIUS. 2 L 7 2 4F RT A21EA 2007050300075 20070503 00075 2007 5 3 DL76S070337 4 20070413 A 2565 101651303 SLIDE BOEING 767 767332 1382001 NM R1 DOOR UNSERVICEABLE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 128DL 24078 UPON REMOVAL OF THE R1 DOOR SLIDE BUSTLE IT WAS DISCOVERED THAT THE DOOR SLIDE HAD BECOME PARTIALLY UNLACED. IT APPEARS THAT ONE OF THE CABLES THAT ACTUATE THE CAM BAR WHICH RELEASES THE TENSION ON THE LACING CORDS WAS SOME HOW RELEASED. THE SLIDE WAS REPLACED ON NRC 50024. 2 L 7 2 4F RT A1NM 2007050300076 20070503 00076 NE 2007 5 3 DL76L070362 2 20070424 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 OIL CONSUMPTION A DALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 27 195DN 59274 28452 724150 RT ENGINE HIGH OIL COMSUMPTION. REPLACED NR 2 ENG PER TRANS 1T149. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050300078 20070503 00078 NM 2007 5 3 DL76L070366 1 20070417 A 5410 PW4060 ACOUSTIC PANEL BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 NACELLE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 183DN 21414 27110 724149 FOUND DURING HMV AT GSO, NR 1 ENG FAN COWL ACOUSTICAL PANEL HAS A CRACK INSIDE OF A DENT AT THE 4 O`CLOCK POSITION JUST FWD OF THE FAN BLADES. REPAIRED BY REMOVING CRACKED AREA AND POTTING AREA IAW B 767 SRM 51-00-01 REPAIR NR 1 ENGINE 201 . 2 L 7 2 4F 4 F RT A1NM E24NE 2007050300079 20070503 00079 NM 2007 5 3 DL76L070367 1 20070417 A 5410 PW40603 ACOUSTIC PANEL BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 NACELLE DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 183DN 62642 27110 724139 NR 2 ENGINE AFT ACOUSTIC PANEL AT APPROX 3:30 POSITION IS DELAMINATED. REPAIRED BY REMOVING DELAM AREA AND POTTING AREA IAW B767 - 300 SRM 54-00-01 REPAIR AND FIG 201. WORKED ON N/R20439 DURING HMV IN GSO. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050300080 20070503 00080 EA 2007 5 3 TRAX200700579 1 20070426 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 974EV 7594 ENGINE SUPPORT BEAM CRACKED ON UPPER WEB AT APPROXX RBL 9.0. [SUP 05-08-07] REPAIRED ENGINE SUPPORT BEAM IAW ASAS T/C EO 600-53-169 AND REO'S 601R-53-61-2152 AND REO 601R-53-61-870. 2 L 7 2 4F RT A21EA 2007050300081 20070503 00081 NM 2007 5 3 DL76L070368 1 20070417 A 5410 TORQUE BOX BOEING 767 767332 1382001 NM NR 2 NACELLE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 183DN 27110 FOUND DURING HMV AT GSO, NR 2 PYLON NACELLE STRUT MID TORQUE BOX UPPER WEB IS CRACKED. REPAIRED IQW B767 SRM 54-53-02 F IG 201 REPAIR 2. 2 L 7 2 4F RT A1NM 2007050300083 20070503 00083 EA 2007 5 3 TRAX200700580 1 20070426 A 5320 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 974EV 7594 CORROSION ALONG FWD RIGHT WALL OF CARGO BAY (MARKED). 2 L 7 2 4F RT A21EA 2007050300087 20070503 00087 EA 2007 5 3 TRAX200700574 1 20070424 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 750EV 10161 RIGHT STA 280 WEB CORRODED OUT OF LIMITS. 2 L 7 2 4F RT A21EA 2007050300088 20070503 00088 NM 2007 5 3 DL76L070374 1 20070417 A 5420 WEB BOEING 767 767332 1382001 NM NR 1 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 183DN 27110 NR 1 PYLON UPPER WEB WHERE WIRE HARNESS RUNS THROUGH, CRACKED 2 PLACES. INSTALLED NEW STIFFENER AND INSTALLED DOUBLERS AND FILLERS PER B767 SRM 54-53-02. ITEM WORKED DURING HMV IN GSO ON N/R CARD 20538. 2 L 7 2 4F RT A1NM 2007050300090 20070503 00090 NM 2007 5 3 DL76L070375 1 20070417 A 5330 SKIN BOEING 767 767332 1382001 NM BS 1461 S27-28L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 183DN 27110 FOUND DURING HMV AT GSO, DENT ON LT LOWER SKIN FS 1461 BETWEEN S27L AND S28L. REPAIRED PER EA 460909-14 REV 1R DATED 3- 30-07. PERMANENT CATAGORY A REPAIR, WORKED ON N/R 24044. 2 L 7 2 4F RT A1NM 2007050300091 20070503 00091 NM 2007 5 3 SWAA072154 1 20070501 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 753, STR 21R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007050300092 20070503 00092 NM 2007 5 3 DL76L070376 1 20070417 A 5315 FLOORBEAM BOEING 767 767332 1382001 NM BS 1483 LBL11-45 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 183DN 27110 FOUND DURING HMV IN GSO, MAIN CABIN FLOORBEAM HAS CORROSION GS 1483 LBL 1 - LBL 45. REPAIRED FLOORBEAM IAW SRM 53-00-51 D FIG 201. WORK ACCOMPLISHED ON N/R 24135. 2 L 7 2 4F RT A1NM 2007050300098 20070503 00098 NM 2007 5 3 DL757070378 1 20070426 A 2120 BACC10JB204C CLAMP BOEING 757 757232 1384965 NM RT A/C PACK BROKEN A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 681DA 26957 AT FL340 WITH SINGLE PACK DISPATCH CABIN CONTINUED TO CLIMB TO 500FPM AND IN AUTO ONE. VALVE DID NOT SHOW FULLY CLOSED, 7 PSID CBN ALT 10000. MANUALLY CLOSED VLV IAW QUICK REF CKLIST, CBN REACHED 13000 FT. DESCENT AND RETURN TO CVG. FOU ND CLAMP BROKEN ON RT PACK OUTPUT DUCT. REPLACED BOTH CLAMPS. PRESSURIZED ACFT. ALL CKS NORMAL. 2 L 7 2 4F RT A2NM 2007050300099 20070503 00099 NM 2007 5 3 SWAA072148 1 20070501 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 22R. R&R SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007050300102 20070503 00102 NM 2007 5 3 SWAA072150 1 20070501 A 5311 6546596 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B. STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050300103 20070503 00103 NM 2007 5 3 SWAA072131 1 20070501 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050300105 20070503 00105 NE 2007 5 3 DL777070381 2 20070428 A 7200 TRENT892 ENGINE BOEING 777 777232 1385232 NM RROYCE RB211 RB211TRENT89 NE NR 2 SURGES A DALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 27 860DA 5022 29951 051156 DURING ROTATION AND CLIMB, NR 2 ENGINE SURGED 4 TO 6 TIMES ENGINE CONTINED TO OPERATE AND SAFETY RETURNED TO NRT. FOUND EGT EXCEEDENCE. 2 L 7 2 4F 4 F RT T00001SE E00050EN 2007050300106 20070503 00106 NM 2007 5 3 SWAA072157 1 20070501 A 5311 6546596 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050300107 20070503 00107 NM 2007 5 3 DL76G070382 1 20070428 A 2530 811150417 COFFEEMAKER BOEING 767 767332 1382001 NM AFT GALLEY ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 172DZ 29691 ACRID ODOR IN CABIN, CBR12 CLOSED RAN ALL CHILLERS OVENS RECIRC FANS GAINED ACCESS TO AFT CHILLERS AND EXHAUST FANS. NO FAULTS FOUND GAINED ACE TO RECIRC FANS NO FAULTS FOUND. FOUND AFT COFFEEMAKER LOC A ELECTRICALLY INOP. REPLACED SAME, OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007050300110 20070503 00110 NE 2007 5 3 DL757070385 2 20070430 A 7200 PW2037RTC ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 MALFUNCTIONED A DALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 27 677DL 56370 716521 25982 716521 RT ENG ROLLED BACK AND THEN SHUTDOWN. NO ABNORMAL INDICATION PRIOR TO THIS EVENT. RT ENG SIMPLY QUIT ON ITS OWN, DUE T O EPCS MSG OF S PDIU AND HISTORY OF R ENG SEC CONT STATUS MSG. REPLACED RT ENG EEC, RT ENG PDIU AND RT ENG PMA STATOR. ALSO, INSPECTED ASSOC ENG WIRING HARNESS. RT ENG NOW CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050300114 20070503 00114 EU 2007 5 3 F3LA200700086 1 20070421 A 3220 D65569EB BUSHING AIRBUS A318 A318111 3940019 EU NLG TORSION LINK CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 801FR 4759 1939 DURING C-3 CHECK, INSPECTION REPORTED NLG UPPER TORSION LINK FROM STRUT CORRODED INSIDE ATTACH LUG. REMOVED CORROSION U NDER BUSHINGS OF NLG UPPER TORSION LINK ATTACH POINT AND REPLACED BUSHINGS IAW EA NR A8-32R-11869. 2 L 7 2 4F RT 2007050300115 20070503 00115 EU 2007 5 3 F3LA200700085 1 20070421 A 5740 BOLT AIRBUS A318 A318111 3940019 EU WINGLET ATTACH CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 801FR 4759 1939 DURING C-3 CHECK, INSPECTION REPORTED WINGLET ATTACH HARDWARE RUSTY. REPLACED WINGLET ATTACH HARDWARE (MILD SURFACE COR ROSION ON BOLT HEADS) ON LT WING IAW AMM 57-31-22-400-001. 2 L 7 2 4F RT 2007050300118 20070503 00118 EU 2007 5 3 F3LA200700091 1 20070427 A 5320 WEB AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 801FR 4759 1939 DURING C-3 CHECK, INSPECTION REPORTED RT SIDE CABIN FLOOR WEB 69 AND 70 HAD VERY LIGHT CORROSION AT NUT PLATES, MOSTLY O N LWR SIDE. REPLACED SHEAR PLATE IAW SRM 51-42-11. 2 L 7 2 4F RT 2007050300122 20070503 00122 NM 2007 5 3 DU4R2007111 1 20070423 A 5330 SKIN BOEING 757 757232 1384965 NM BS 660-680 DAMAGED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 637DL 23760 FOUND 2 LIGHTNING STRIKES BETWEEN BS 660 - BS 680 AND S-4R – S-6R. REPAIRED BY CUTTING OUT .750" CIRCLE AT LIGHTNING ST RIKE AREA. HFEC CUT OUT IAW D6-34N301-6-51-00-19, NO RELEVANT INDICATIONS NOTED. FABRICATED AND INSTALLED REPAIR DOUBL ER 5.5" BY 5.5 FROM 2024-T3 .090 AND SHEAR TIE FROM 7075-T6 .050" IAW B757 SRM 51-40-05, 51-40-06, 51-40-08, 51-40-02 AN D 53-00-01 FIG 201 REPAIR (7). 2 L 7 2 4F RT A2NM 2007050300124 20070503 00124 NM 2007 5 3 DU4R2007113 1 20070424 A 5330 SKIN BOEING 757 757232 1384965 NM BS 510 S28-29R DENTED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 637DL 23760 FOUND FUSELAGE SKIN DENTED AT BS 510 S-28R - S-29R GOUGED. DENT RATIO A/Y = .020 TOO CLOSE TO FRAME. CUT OUT DENT IAW B757 SRM 53-00-01 FIG 201. HFEC CUT OUT IAW B757 NDT PT. 6, 51-00-19, NO RELEVANT INDICATIONS NOTED. FABRICATED AND IN STALLED DOUBLER 6.8" BY 8.6" FROM 2024-T3 .050" IAW B757 SRM 51-20-01 AND 53-00-01 FIG 201. 2 L 7 2 4F RT A2NM 2007050300125 20070503 00125 NM 2007 5 3 SWAA072149 1 20070501 A 5755 6573730 SPOILER BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED MV1 CHECK, FOUND RT WING #3 FLIGHT SPOILER CRACKED AT FWD INBOARD END. REPAIRED SPOILER PER SWA EA. 2 L 7 2 4F RT A16WE 2007050300126 20070503 00126 NM 2007 5 3 DU4R2007114 1 20070419 A 5330 SKIN BOEING 757 757232 1384965 NM BS 440-460 DAMAGED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 637DL 23760 FOUND LIGHTNING STRIKE BETWEEN BS 440 AND BS 460 S-1R. REPAIRED BY CUTTING OUT STRIKE AREA. FABRICATED AND INSTALLED R EPAIR DOUBLER 14.40 BY 7.40 FROM 2024-T3 .063 IAW B757 SRM 53-00-01 FIG 201. 2 L 7 2 4F RT A2NM 2007050300127 20070503 00127 NM 2007 5 3 SWAA072132 1 20070501 A 5311 65C25230 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050300130 20070503 00130 NM 2007 5 3 SWAA072162 1 20070501 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10R. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050300131 20070503 00131 NM 2007 5 3 SWAA072161 1 20070501 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050300136 20070503 00136 WP 2007 5 3 UPS07849671 1 20070414 A 5340 4753360U502 FITTING DOUG DC8 DC873F 302199F WP BS 822 L22L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 822 L22L. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007050300137 20070503 00137 NM 2007 5 3 SWAA072137 1 20070501 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050300138 20070503 00138 WP 2007 5 3 UPS07849680 1 20070114 A 5340 ATTACH FITTING DOUG DC8 DC873F 302199F WP FS 787 L13R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 787 L13R. REMOVED FITTING AT STA 787 L13R IAW SRM 51-1-20D. FABRICATE D AND INSTALLED LONGERON END FITTING AT STA 787 L13R IAW SRM 51-01-21-0, NAD SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007050300139 20070503 00139 WP 2007 5 3 UPS07849681 1 20070415 A 5320 FINGER DOUBLER DOUG DC8 DC873F 302199F WP FS -60 RBL 22 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 SEVERAL AREAS OF CORROSION AND POSSIBLE CRACK IN FINGER DOUBLER COCKPIT SUBFLOOR FS -60, RBL 22. REM OVED CORRODED FINGER DOUBLER AT STA -60 RBL 22 IAW SRM 51-1-21. FABRICATED AND INSTALLED FINGER DOUBLER AT STA -60 RBL2 2 IAW DWG 5612298, AND SRM51-1-21. 2 L 7 4 4F RT 4A25 2007050300140 20070503 00140 NM 2007 5 3 SWAA072138 1 20070501 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8R. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050300141 20070503 00141 WP 2007 5 3 UPS07849683 1 20070415 A 5320 FINGER DOUBLER DOUG DC8 DC873F 302199F WP FS -25 RBL 22 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 CORROSION AND POSSIBLE STRESS CRACK ON FINGER DOUBLER COCKPIT SUB FLOOR FS -25 TO 8 RBL 22. REMOVED FINGER DOUBLER AT STA -25 TO 8 RBL 22 IAW SRM 51-1-21. FABRICATED AND INSTALLED FINGER DOUBLER AT STA -25 TO 8 RBL 22 I AW DWG5612298, AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007050300144 20070503 00144 WP 2007 5 3 NWAA071609606 1 20070425 A 2160 LINE DOUG DC9 DC932 3022066 WP PRESSURE REG DISCONNECTED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 606NW 47225 DURING CLIMB, THE FLIGHT ATTENDANT REPORTED BOTH AFT LAVATORY SMOKE DETECTORS WERE SOUNDING. A MINUTE LATER THE FLIGHT CREW SMELLED FUMES IN THE COCKPIT. NO MENTION OF COM COMPLIANCE BUT CREW DID SAY THE SMELL CLEARED SOMEWHAT AND THEN RE TURNED SLIGHTLY WORSE WHEN THE AIRCRAFT WAS ON SHORT FINAL. THE FLIGHT RETURNED TO A NORMAL SAFE LANDING BACK AT MSP. MAINTENANCE FOUND A SENSE LINE TO THE PRESSURE REGULATOR DISCONNECTED. THE LINE WAS RECONNECTED, ACM WAS FUNCTIONALLY C HECKED, AND THE COALESCER BAGS WERE REPLACED. PACK BURN-OUT PROCEDURES COMPLIED WITH, COALESCER BAGS REPLACED AGAIN, AN D WHEN NO SMOKE OR FUMES WERE GENERATED THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007050300146 20070503 00146 NM 2007 5 3 HALA07001082 1 20070422 A 5330 SKIN BOEING 767 767332 1382001 NM BS 264 S26L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 FOUND FUSELAGE SKIN LEFT BS 264 STRINGER 26 HAS LIGHTNING DAMAGE AT FASTENER. REMOVED DAMAGE FASTENER AND REPAIRED LIGH TNING DAMAGE AT BS 264 STR 26 IAW 767 SRM 53-00-01 FIG 201 AND HAL M105 597053. 2 L 7 2 4F RT A1NM 2007050300147 20070503 00147 NM 2007 5 3 SWAA072144 1 20070501 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 2L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050300148 20070503 00148 NM 2007 5 3 HALA0700194 1 20070422 A 5330 SKIN BOEING 767 767332 1382001 NM BS 274 S26L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 FUSELAGE SKIN LEFT BS 274 STR 26 HAS LIGHTNING DAMAGE. REPAIRED PER HAL M105 597053. 2 L 7 2 4F RT A1NM 2007050300155 20070503 00155 NM 2007 5 3 SWAA072159 1 20070501 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 2L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050300156 20070503 00156 NM 2007 5 3 HALA0700181 1 20070422 A 5330 SKIN BOEING 767 767332 1382001 NM BS 256 S27L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 LIGHTNING STRIKE, BS 256 ABOVE STR 27L DAMAGE. REPAIRED LIGHTNING STRIKE BY REMOVING AND REPLACING FASTENER AT BS 256 S TR 27L PER SRM 53-00-01 FIG 201 SECITON II AND HAL M105 FILE 597053. 2 L 7 2 4F RT A1NM 2007050300158 20070503 00158 NM 2007 5 3 HALA0700195 1 20070422 A 5330 SKIN BOEING 767 767332 1382001 NM BS 254 S24-26L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 FUSELAGE SKIN LT BS 254, BETWEEN STR 24 AND STR 26 HAS LIGHTNING DAMAGE. REPAIRED PER HAL M105 597053. 2 L 7 2 4F RT A1NM 2007050300161 20070503 00161 NM 2007 5 3 HALA0700185 1 20070422 A 5330 SKIN BOEING 767 767332 1382001 NM BS 266 S24-26L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 FUSELAGE SKIN LT BS 266, BETWEEN STR 24 AND STR 26 HAS LIGHTNING DAMAGE AT FASTENER. REMOVED DAMAGE AND REPAIRED IAW 76 7 SRM 53-00-01 FIG 201 AND HAL M105 597053. 2 L 7 2 4F RT A1NM 2007050300162 20070503 00162 NM 2007 5 3 SWAA072139 1 20070501 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 10R. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050300163 20070503 00163 NM 2007 5 3 HALA0700191 1 20070422 A 5330 SKIN BOEING 767 767332 1382001 NM BS 355 S34-35R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 FUSELAGE SKIN RT BS 355 BETWEEN STR 34 AND STR 35 HAS LIGHTNING STRIKE. REPAIRED PER HAL M105 FILE 597053. 2 L 7 2 4F RT A1NM 2007050300164 20070503 00164 NM 2007 5 3 HALA0700198 1 20070422 A 5330 SKIN BOEING 767 767332 1382001 NM BS 184 S30L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 FUSELAGE SKIN LT BS 184, ABOVE STR 30 HAS LIGHTNING DAMAGE. REPAIRED PER HAL M105 NR 597053. 2 L 7 2 4F RT A1NM 2007050300170 20070503 00170 NM 2007 5 3 SWAA072164 1 20070501 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 401WN 29813 DURING SCHEDULED HC2 CHECK, RT OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007050300173 20070503 00173 NM 2007 5 3 HALA0700179 1 20070422 A 5330 SKIN BOEING 767 767332 1382001 NM BS 426 GOUGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 WHILE WORKING CUSTOMER CARD NR 01731, FOUND SKIN GOUGED AT BS 426 STR 33 RT. REPAIRED PER HAL M105 597053. 2 L 7 2 4F RT A1NM 2007050300176 20070503 00176 NM 2007 5 3 HALA0700193 1 20070422 A 5330 SKIN BOEING 767 767332 1382001 NM BS 256 S24-26L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 FUSELAGE SKIN, LT BS 256, BETWEEN STR 24 AND STR 26 HAS LIGHTNING DAMAGE AT FASTENER. REMOVED AND REPLACED FASTENER PER SRM 53-00-01 FIG 201 SECTION II AND HAL M105 FILE NR 597053. 2 L 7 2 4F RT A1NM 2007050300177 20070503 00177 NM 2007 5 3 SWAA072124 1 20070430 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 479WN 33990 DURING SCHEDULED MV3 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. R&R LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007050300178 20070503 00178 NM 2007 5 3 HALA0700189 1 20070422 A 5330 SKIN BOEING 767 767332 1382001 NM BS 284 S34L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 SEVERAL LIGHTNING STRIKES ON EXTERNAL FUSELAGE SKIN BS 284 STR 34L. REPAIRED PER 767 SRM 53-00-01 FIG 201 AND HAL M105 597053. 2 L 7 2 4F RT A1NM 2007050300179 20070503 00179 NM 2007 5 3 HALA0700202 1 20070426 A 5753 SKIN BOEING 767 767332 1382001 NM RT WING TE FLAP DENTED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 591HA 33423 RIGHT WING INBOARD AFT FLAP LOWER SURFACE HAS GRAVEL DAMAGE 27 INCHES INBOARD OF OUTBOARD END 16 INCHES FORWARD OF TRAIL ING EDGE. REPAIRED PER 767 SRM 51-70-01-06 -0. 2 L 7 2 4F RT A1NM 2007050300182 20070503 00182 NM 2007 5 3 SWAA072123 1 20070430 A 3397 471N5212 CONNECTOR BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW ROW 1 ABC. SECURED CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2007050300184 20070503 00184 2007 5 3 CHQA200700012 4 20070430 A 3160 7014300901 DISPLAY EMB 135 EMB135KL 3260302 SO COCKPIT INOPERATIVE A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 382SK 13469 13469 145624 FLIGHT 5303 - AUS-STL - AT FL 370, MESSAGE DISPLAYED TO CHECK PFD. CREW LOOKED TO PFD, RED X DISPLAYED FOLLOWED BY SCRE EN BLANKING. ATTEMPTED TO INCREASE BRIGHTNESS, SCREEN REMAINED BLANK AND CREW NOTED AN ACRID SMELL. NO VISIBLE SMOKE. DIVERTED TO SGF. MAINTENANCE REMOVED AND REPLACED PFD 2 DISPLAY IAW EMB MM 34-22-01. OPS CHECK NORMAL AT THIS TIME. 2 L 7 2 4F RT T00011AT 2007050300187 20070503 00187 NM 2007 5 3 SWAA072122 1 20070430 A 3397 471N5212 CONNECTOR BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 405WN 27893 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 2 ABC. SECURED EEPLS CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2007050300188 20070503 00188 NM 2007 5 3 SWAA072126 1 20070430 A 5743 6537877 FITTING BOEING 737 7373H4 1384600 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED SERVICE CHECK, FOUND RT MLG WALKING BEAM OUTBOARD FWD STAB FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2007050300190 20070503 00190 NM 2007 5 3 SWAA072127 1 20070430 A 5743 6537877 FITTING BOEING 737 7373H4 1384600 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED SERVICE CHECK, FOUND LT MLG WALKING BEAM OUTBOARD AFT STAB FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2007050300195 20070503 00195 NM 2007 5 3 SWAA072110 1 20070430 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 FUSELAGE SKIN CRACKED AT BS 503C, STR 8R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007050300197 20070503 00197 NM 2007 5 3 SWAA072116 1 20070430 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007050300199 20070503 00199 NM 2007 5 3 AALA20070689 1 20070415 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AA 24617 DFW - EMERGENCY LIGHT AT SEAT 17D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007050300201 20070503 00201 NM 2007 5 3 AALA20070691 1 20070415 A 3350 BEZEL BOEING 757 757223 1384957 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AA 24617 DFW - EMERGENCY LIGHT AT SEAT 17D HAS BROKEN BEZEL. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007050300203 20070503 00203 WP 2007 5 3 AALA20070686 1 20070414 A 3350 0201804001 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7518A 49895 MSP - EMERGENCY LIGHT AT SEAT ROW 22 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 22. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007050300204 20070503 00204 WP 2007 5 3 AALA20070684 1 20070414 A 2150 1173T0640 SWITCH DOUG DC9 DC982 3022082 WP AIR CONDITIONING INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7530 49922 ABQ INFLIGHT T1898/14APR - AFTER TAKEOFF, RIGHT PACK WENT TO ZERO. PRESSURIZATION FLOW INDICATION ILLUMINATED AND AIRC RAFT LOST PRESSURE. MASKS DID NOT DROP. RETURNED TO ABQ AND LANDED WITHOUT INCIDENT. LEFT PACK WAS ON PLACARD. AFTER LANDING RIGHT PACK PERFORMED NORMALLY. REPLACED LEFT PACK HEAD EXCHANGER COOLING FAN AND REPLACED RIGHT SECOND SEGMENT CLIMB PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007050300205 20070503 00205 NM 2007 5 3 SWAA072112 1 20070430 A 3350 6556633 LIGHT BOEING 737 7373K2 13844BA NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 LT OVERWING EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007050300206 20070503 00206 NM 2007 5 3 SWAA072118 1 20070430 A 5315 6564804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND FLOOR BEAM WEB CRACKED AT BS 727B, LBL 26. R&R WEB PER SRM. 2 L 7 2 4F RT A16WE 2007050300208 20070503 00208 NM 2007 5 3 SWAA072114 1 20070430 A 2560 P4010021 BATTERY BOEING 737 7373A4 1384585 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 674AA 23252 AFT CABIN EMERGENCY FLASHLIGHT INOP. R&R FLASHLIGHT BATTERIES PER MM. 2 L 7 2 4F RT A16WE 2007050300211 20070503 00211 NM 2007 5 3 SWAA072166 1 20070501 A 5315 141A5502 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 745SW 29491 DURING SCHEDULED 8Y CHECK, FOUND FLOOR BEAM UPPER CHORD CRACKED AT BS 294.5, RBL 52. REPAIRED CHORD PER ER. 2 L 7 2 4F RT A16WE 2007050300213 20070503 00213 NM 2007 5 3 SWAA072169 1 20070501 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 745SW 29491 DURING SCHEDULED 8Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 2 DEF. R&R LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007050300216 20070503 00216 NM 2007 5 3 SWAA072170 1 20070501 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 745SW 29491 DURING SCHEDULED 8Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 3 DEF. R&R LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007050300218 20070503 00218 NM 2007 5 3 SWAA072128 1 20070501 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 458WN 33857 EEPLS COVER MISSING AT ROW 22 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007050300220 20070503 00220 NM 2007 5 3 SWAA072098 1 20070427 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 271LV 29090 DURING SCHEDULED HC1 CHECK, FWD CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007050300221 20070503 00221 NM 2007 5 3 SWAA072153 1 20070501 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 517D, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007050100136 20070501 00136 NM 2007 5 1 SWAA072104 1 20070428 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 247WN 32508 EEPLS COVER MISSING AT ROW 15 DEF. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007050100137 20070501 00137 NM 2007 5 1 SWAA072094 1 20070429 A 5311 6545630 FRAME BOEING 737 7375H4 138449D NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007050100139 20070501 00139 NM 2007 5 1 SWAA072103 1 20070428 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM BS 757 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 FUSELAGE SKIN CRACKED AT BS 757, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007050100140 20070501 00140 NM 2007 5 1 SWAA072107 1 20070428 A 5330 6545857 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007050100146 20070501 00146 NM 2007 5 1 07FDEA01643 1 20070426 A 5754 ARB1669502 SKIN DOUG MD11 MD11 3023602 NM ZONE 500 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 RIGHT WING, LEADING EDGE SLAT NR 3 TRAILING EDGE LOWER SURFACE FOUND WITH GOUGE MARK. [SUP 05-16-07] SURFACE SMOOTHE NED OFF AND REPROTECTED AS PER SRM 51-21-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050100155 20070501 00155 SO 2007 5 1 SWIA200718161 1 20070413 A 3350 SIGN EMB 120 EMB120ER 3260203 SO CABIN BROKEN A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 237SW 120314 FOUND MAIN CABIN DOOR EXIT PLACARD IS BROKEN. INSTALLED SERVICEABLE LENSE. 2 L 7 2 4T RT A31SO 2007050200005 20070502 00005 SO 2007 5 2 SIMA200712001 1 20070423 A 2120 UNKNOWN EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL COCKPIT ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 836AE 145635 STRONG OIL ODOR IN COCKPIT DURING FLIGHT. [SUP 05-08-07] REMOVED AND REPLACED LEFT HAND ENGINE IAW AMERICAN EAGLE WORK CARD 72-000-00. OPERATIONAL AND LEAK CHECKS COMPLIED WITH NO LEAKS - RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007050200013 20070502 00013 SO 2007 5 2 SIMA200712009 1 20070427 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCONNECTED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 616AE 145092 MAIN ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. RECONNECTED DOOR LIGHT IAW EMB AMM 33-50-06. OPERATIONAL CHECK GOOD, RETU RNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050200042 20070502 00042 EA 2007 5 2 MASA200700021 1 20070107 A 2170 7536893 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA CABIN AIR ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 154SF 7154 ASH 7134 IAD. PILOT REPORTED A FUEL ODOR IN COCKPIT, ODOR SEEMED GET STRONGER AS THE PACK TEMPERATURE WAS INCREASED. M X REPLACED FUEL LINE TO APU, REPLACED COALESCER BAGS, RAN PACKS, FUEL ODOR CLEAR. 2 L 7 2 4F RT A21EA 2007050200043 20070502 00043 EA 2007 5 2 MASA200700022 1 20070110 A 3350 601R461051 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 154SF 7154 ASH 7132 IAD. FIRST 5 ROWS OF EMERGENCY FLOOR LIGHTS INOP. MX REPLACED LIGHT STRIP. 2 L 7 2 4F RT A21EA 2007050200080 20070502 00080 EA 2007 5 2 MASA200700142 1 20070308 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 97325 7325 ASH 2843 PHX. EMERGENCY EXIT FLOODLIGHT NEAR PAX DOOR INOP. MX FOUND BROKEN WIRE ON BACK OF SIGN AND REPAIRED WIRE. 2 L 7 2 4F RT A21EA 2007050200085 20070502 00085 EA 2007 5 2 MASA200700163 1 20070326 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA CABIN ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 515MJ 10117 ASH 7493 ORD. STRONG ODOR OF FUEL IN BOTH EXIT ROWS. PERFORMED ENGINE RUNS, NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2007050200089 20070502 00089 EA 2007 5 2 TRAX200700552 1 20070422 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 974EV 7594 FS 484 AT LBL 36 INTERCOSTAL IS CRACKED AT TOP O/B RIVET. REMOVED DAMAGE PORTION OF INTERCOSTAL AT FS 484/LBL 36 PER RE O 601R-53-41-059. FABRICATED REPAIR ANGLE FROM 2024-T3 .063 PO 9345-1 PER REO 601R-53-41-059. FOR LPI REFER TO W/C 410 (BOTH REPAIR ANGLE AND CUTLINE) INSTALLED REPAIR ANGLE IAW REO 601R-53-41-059. SUPPLEMENTAL - SDR CLOSED 05/01/07. 2 L 7 2 4F RT A21EA 2007050200090 20070502 00090 EA 2007 5 2 TRAX200700553 1 20070422 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 974EV 7594 FS 484 AT RBL 27 INTERCOSTAL IS CRACKED IN RADIUS. REMOVED CRACKED CLIP AT FSA 484 RBL 27 INTERCOSTAL IAW CRJ 200 SRM 5 1-42-06 BHS1124 4-25-07. DUPLICATED INTERCOSTAL IAW CRJ SRM 53-41-43 USING PREFORMED ANGLE P/N 56144-3, INSTALLED ANGLE IAW CRJ SRM 51-42-20. SUPPLEMENTAL - SDR CLOSED 05/01/07. 2 L 7 2 4F RT A21EA 2007050300017 20070503 00017 EA 2007 5 3 MASA200700111 1 20070221 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 571ML 7209 ASH 7103 IAD. PILOT REPORTED THE CEILING LEVEL EMERGENCY FLOOD LIGHT AT APPROX ROW 9 INOP. MX RELAMPED FLOOD LIGHT. 2 L 7 2 4F RT A21EA 2007050300020 20070503 00020 EA 2007 5 3 MASA200700113 1 20070221 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN MALFUNCTIONED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 922FJ 15022 ASH 2632 CLT. EMERGENCY LIGHTS TURN ON WHEN SELECTED TO ARMED POSITION. MX RESET SYSTEM AND PERFORMED OPS CHECK. NO F URTHER DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007050300032 20070503 00032 WP 2007 5 3 UPS07849684 1 20070412 A 5720 CHANNEL DOUG DC8 DC873F 302199F WP WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 T-CHANNEL CRACKED UPPER SURFACE AT XRS 204 BETWEEN STRINGERS 60 AND 59. STOPPED DRILLED CRACK AT XRS 204 BETWEEN STRINGERS 59 & 60 IN NR 4 MAIN TANK IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SR M 57-02-00-0, AND SRM 51-01-08. 2 L 7 4 4F RT 4A25 2007050300041 20070503 00041 EA 2007 5 3 TRAX200700559 1 20070423 A 2620 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA EXTINGUISH SYS ACTIVATED A ASOA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 27 720EV 10115 APU SQUIB AND APU BOTTLE LOW MESSAGES. APU FIRE EXTINGUISHING SYSTEM - APU INOPERATIVE. 2 L 7 2 4F RT A21EA 2007050300049 20070503 00049 EU 2007 5 3 F3LA200700084 1 20070427 A 2497 CONTACTOR AIRBUS A318 A318111 3940019 EU DAMAGED A F3LA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 NM 03 803FR 4313 2017 AIR RETURN AT 0130Z FOR MULTIPLE ECAMS ASSOCIATED W/AC ESS BUSS. DEPARTURE OUT OF KDEN, LEVELING AT 35,000 FT, RECEIVED ECAM ENG 1 IGN A AND ENG 2 IGN A, C/B TRIPPED L ELEC BAY, YAW DAMPER 1, RUD TRIM 1, AND TRV LIM 1. CAPTAINS PFD ND FWD DISPLAYS ALL WENT BLANK. AFTER SELECTING AC ESS FEED TO ALTN, RECOVERED ALL DISPLAY FUNCTIONS. STILL HAD REMAINING IN OP SYSTEMS, INCLUDING NO FUEL INDICATIONS ON EWD. RETURNED TO KDEN AND LANDED AIRCRAFT WITHOUT INCIDENT. REPLACED CONT ACTOR 9 BY U1 IAW AMM 24-2255, PB 401. OPS CHECKED GOOD. REPLACED CONTACTOR 3XC IAW AMM 24-25-55, PB 401. OPS CHECKED GOOD. REPLACED RELAY 13XC IAW AMM 20-46-50. OPS CHECKED GOOD. REPLACED C/B 4XC IAW AMM 20-46-10. OPS CHECKED GOOD. 2 L 7 2 4F RT 2007050300060 20070503 00060 NM 2007 5 3 CALA0700203 1 20070423 A 5755 HINGE BOEING 767 767424ER 1385270 NM NR 6 SPOILER CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76065 29460 NR 6 SPOILER INBOARD HINGE CORRODED. REPAIRED IAW SRM 57-51-02. 2 L 7 2 4F RT A1NM 2007050300072 20070503 00072 EA 2007 5 3 TRAX200700577 1 20070418 A 5210 STEP CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 659CA 10153 PAX DOOR TOP STEP AFT BASE RADIUS CRACKED (MARKED). 2 L 7 2 4F RT A21EA 2007050300073 20070503 00073 2007 5 3 NWAA071623205 4 20070426 A 2565 CABLE AIRBUS 320 A320211 3930320 EU SLIDE RESERVOIR BROKEN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 305US 041 LEFT OVERWING EMERGENCY EXIT ESCAPE SLIDE RESERVOIR ACTUATING CABLE FOUND BROKEN. REPLACED LT OVERWING SLIDE RESERVOIR, INSPECTION OK. 2 L 7 2 4F RT A28NM 2007050300082 20070503 00082 NE 2007 5 3 DL757070370 2 20070425 A 7200 726004417 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 OVERTEMP A DALA E ENGINE SHUTDOWN A FLAME/FIRE NR NOT REPORTED 1 SO 27 615DL 22822 728781 DURING TAXI, NR 2 ENG OCCURRED A TAILPIPE MAX EGT REACHED 796 FOR 7 SECONDS. FUEL CTRL JUST PREV REPLACED SUSP BAD, ENG CHG IN PROGRESS. REPLACED NR 2 ENG ON TRANS 6T103. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050300085 20070503 00085 EA 2007 5 3 TRAX200700582 1 20070427 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 738EV 10146 F/O'S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007050300095 20070503 00095 NM 2007 5 3 SWAA072146 1 20070501 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 15L. R&R SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007050300108 20070503 00108 NM 2007 5 3 DL76L070384 1 20070427 A 5414 311T31571 ANGLE BOEING 767 767332 1382001 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 173DN 24800 THE NR 2 PYLON CLOSEOUT ANGLE WAS FOUND WITH A CRACK IN THE OUTBOARD SIDE. THE MIDSPAR FITTINGS ALSO HAD TOOLING DAMAGE . THE DAMAGED ANGLE WAS REPAIRED WITH REPAIR STRAPS. 2 L 7 2 4F RT A1NM 2007050300117 20070503 00117 NM 2007 5 3 QXEA200700691 1 20070501 A 5210 CAM ROLLER BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR LACK OF LUBE A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 408QX 4050 SEA FLIGHT: FLIGHT ATTENDANT REPORTS LEFT REAR PAX DOOR DIFFICULT TO OPEN. MAINTENANCE LUBRICATED LEFT REAR PAX DOOR CA M ROLLERS. OPERATED SEVERAL TIMES. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED T O SERVICE. 2 H 7 2 4T RT A13NM 2007050300123 20070503 00123 NM 2007 5 3 DU4R2007112 1 20070425 A 5330 SKIN BOEING 757 757232 1384965 NM BS 1390 GOUGED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 637DL 23760 FOUND AFT CARGO DOOR EXT SKIN BS 1390 S-26 - S-27R GOUGED. REPAIRED BY FABRICATING AND INSTALLING REPAIR DOUBLER 5-1/2" BY 16-7/8 FROM 2024-T3 .071 IAW B757 SRM 51-20-01, 51-41-00-352-013. 2 L 7 2 4F RT A2NM 2007050300129 20070503 00129 NM 2007 5 3 SWAA072141 1 20070501 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050300132 20070503 00132 NM 2007 5 3 UPS07549669 1 20070407 A 5350 148N3662 TAIL CONE BOEING 757 75724APF 1384969 NM BS 1893 LBL 8 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 419UP 23906 INSPECTION TYPE:C HOLE IN TAILCONE STA 1893 LBL 8. COMPLIED WITH EA NR 757-5381-27-A1656. NO DEVIATIONS AND UPS RAA NR 757-53-20242. 2 L 7 2 4F RT A2NM 2007050300133 20070503 00133 NM 2007 5 3 SWAA072135 1 20070501 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 4L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050300134 20070503 00134 WP 2007 5 3 UPS07849670 1 20070414 A 5340 3755172501 FITTING DOUG DC8 DC873F 302199F WP DOOR FRAME GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 LOWER FWD T-BOLT FITTING GOUGED AT C-PIT DOOR JAM. REMOVED AND REPLACED LWR FWD T-BOLT FITTING IAW S RM 51-3-2. 2 L 7 4 4F RT 4A25 2007050300135 20070503 00135 NM 2007 5 3 SWAA072136 1 20070501 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 3L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050300183 20070503 00183 NM 2007 5 3 XXUA200704038 1 20070407 A 5311 FRAME BOEING 757 7572Q8 1384972 NM BS 209-222 DAMAGED A XXUA K NONE O OTHER IN INSP/MAINT 1 EA 15 926JS 24964 AIRCRAFT DAMAGE BEHIND NOSE RADOME LOWER PART OF AIRCRAFT FRAME (20 BY 2 1/2) LOCATION BS 209-222 AND BL 8L-25R. FABRIC ATED ALL REPAIRS PARTS PER BOEING REPAIR SKETCH SR 1-312155879. INSTALLED ALL REPAIR PARTS WITH SEALANT PER BOEING REPA IR SKETCH R 1-312155879. RESTORED ALL SURFACE FINISH PER MM 51-21-00. PRESSURIZED AIRCRAFT DUE TO DAMAGE AND REPAIR, N O LEAKS NOTED PER MM 21-31-03. 2 L 7 2 4F RT A2NM 2007050300189 20070503 00189 NM 2007 5 3 SWAA072125 1 20070430 A 5743 6537877 FITTING BOEING 737 7373H4 1384600 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED SERVICE CHECK, FOUND LT MLG WALKING BEAM OUTBOARD FWD STAB FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2007050300198 20070503 00198 NM 2007 5 3 AALA20070688 1 20070414 A 2120 CLAMP BOEING 757 757223 1384957 NM VALVE LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 188AN 32382 BOS - INFLIGHT T96/14APR - LEFT ENGINE OVERHEAT INDICATION ILLUMINATED DURING CLIMB. RETURNED TO BOS AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE. FOUND PRECOOLER CLAMPS LOOSE AND EVIDENCE OF AIR LEAKAGE AT PT6 VALVE. REPL ACED PT6 VALVE DUCT AND TIGHTENED PRECOOLER CLAMPS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007050300200 20070503 00200 NM 2007 5 3 AALA20070690 1 20070415 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AA 24617 DFW - EMERGENCY LIGHT AT SEAT 17D HAS MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007050300207 20070503 00207 NM 2007 5 3 SWAA072121 1 20070430 A 5311 65C25229 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 14L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007050300212 20070503 00212 NM 2007 5 3 SWAA072130 1 20070501 A 3230 273A1401 MANIFOLD BOEING 737 7377H4 1384404 NM NLG W/W FAULTY A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 717SA 27851 AIRTURN BACK - NOSE GEAR WOULD NOT RETRACT, CYCLED GEAR LEVER TWICE NO HELP. RED AND GREEN LIGHTS ILLUMINATED. R&R NOS E GEAR HYD LOCKING ACTUATOR MANIFOLD ASSY PER MM. 2 L 7 2 4F RT A16WE 2007050300223 20070503 00223 NM 2007 5 3 USAA070333 1 20070501 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 503UW 23237 STA 835 STR 25R, BLENDED & TREATED PER EA 98621. DEFECT SIZE: 2 INCHES 2 L 7 2 4F RT A16WE 2007050300224 20070503 00224 NM 2007 5 3 AALA20070681 1 20070413 A 3350 CM1317 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 675AN 29425 BOS - EMERGENCY LIGHTS AT LEFT ROW 27 INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT LEFT ROW 27. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A2NM 2007050300225 20070503 00225 NM 2007 5 3 AALA20070682 1 20070413 A 3350 CM1317 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 675AN 29425 BOS - EMERGENCY LIGHTS AT RIGHT ROW 29 INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT RIGHT ROW 29. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007050300226 20070503 00226 NM 2007 5 3 AALA20070683 1 20070413 A 3397 WIRE HARNESS BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 953AN 29539 MIA - EMERGENCY LIGHT AT SEAT 14D INOPERATIVE. RESECURED WIRES AND CONNECTOR FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007050300231 20070503 00231 NM 2007 5 3 ZZDA070427151 1 20070424 A 5270 SWITCH BOEING 737 737 UTILSYS NM CABIN DIRTY A ZZDA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 15 267AT 33919 LEFT OVERWING ANNUNCIATOR LIGHT ON TAKE OFF ROLL. INSPECTED BOTH L WING EXIT OVERWING SWITCHES FOUND AFT SWITCH A BIT S TICKY. CLEANED AND LUBED BOTH SWITCH PLUNGERS ASSY. IAW SOPM 20-41-05 AND AT THE RECOMMENDATIONS OF 737NG-FTD-52-0700. OPS NORMAL AND LOCKED 2 L 7 2 4F RT A16WE 2007050300235 20070503 00235 NM 2007 5 3 ZZDA070426147 1 20070418 A 5311 FRAME BOEING 717 717200 1383700 NM FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 968AT 55029 AFT FUSELAGE COMP AT STA 1178.225 BETWEEN LONG'S 16L AND 17L, CANTED FRAME IS CRACKED. INSTALLED FORMED REPAIR AT CANTE D FRAME ON STA 1178.225 LEFT HAND BETWEEN LONG 16 AND 17 PER SRM 51-20-11 FIG 201. 2 L 7 2 4F TR A6WE 2007050300236 20070503 00236 NM 2007 5 3 ZZDA070426149 1 20070423 A 5311 ANGLE BOEING 717 717200 1383700 NM FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 969AT 55030 AFT ACCESSORY COMPARTMENT FS 1178 CANTED FRAME ANGLE CRACKED NEAR LONGERON 15R. INSTALLED ANGLE FOR REPAIR 1 SIDE OF AN GLE 11 1/2 X 2 1/2 IAW B717 SRM 51-70-11. 2 L 7 2 4F TR A6WE 2007050300237 20070503 00237 NM 2007 5 3 ZZDA070426150 1 20070418 A 5311 FRAME BOEING 717 717200 1383700 NM FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 968AT 55029 AFT FUSELAGE COMPARTMENT AT STA 1178.225 BETWEEN LONG 16 AND 17 RIGHT HAND CANTED FRAME CRACK. 2 L 7 2 4F TR A6WE 2007050300238 20070503 00238 NM 2007 5 3 ZZDA070426156 1 20070426 A 5270 6302612 SWITCH BOEING 737 737 UTILSYS NM OVERWING DOOR ACTIVATED A ZZDA K NONE N FALSE WARNING TO TAKEOFF 1 SO 15 267AT 33919 LT OVERWING ANNUNCIATOR LIGHT ILLUMINATED ON T/O PRESSURIZATION OKAY. REMOVED AND REPLACED AFT SWITCH ON LEFT OVERWING EXIT DOOR. RESET FAULT AND OPS CHECKED GOOD IN REF TO 737 AMM 52-71-22 . 2 L 7 2 4F RT A16WE 2007050300239 20070503 00239 NM 2007 5 3 ZZDA070427157 1 20070427 A 5270 630262 SWITCH BOEING 737 737 UTILSYS NM OVERWING DOOR FAULTY A ZZDA K NONE N FALSE WARNING CR CRUISE 1 SO 15 267AT 33919 LT WING OVERWING DOOR ILLUMINATED. REMOVED AND REPLACED AFT INDICATION SWITCH ON LT OVER WING DOOR IAW BOEING 737 AMM 5 2-71-13. OPS CK GOOD. 2 L 7 2 4F RT A16WE 2007050300242 20070503 00242 2007 5 3 ZZDA070430153 4 20070430 A 2565 D29982225 SLIDE BOEING 717 717200 1383700 NM L1 DOOR UNSERVICEABLE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 942AT 55005 DURING RII INSPECTION THE PINS WERE FOUND PULLED. R&R L1 SLIDE ASSY( FOUND PIN PULLED ) IAW REF MM 25-61-01. 2 L 7 2 4F TR A6WE 2007050300244 20070503 00244 NM 2007 5 3 2007UALA01018 1 20070403 A 2824 125334D1 VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT & LT X-FEED FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 660UA 27115 UNEXPLAINED FUEL TRANSFER PER CREW. SUPPLEMENTAL DATA UPDATE REPLACED BOTH CROSSFEED VALVES AND REPAIRED FUEL LEAK AT B OTTOM OF FWD SPAR BETWEEN RT AND CTR FUEL TANKS. PERFORMED SERVICE TIP TEST AND HAD NO UNWANTED TRANSFER. A/C RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050300245 20070503 00245 NM 2007 5 3 2007UALA01241 1 20070420 A 5330 SKIN BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 CRACK ON AFT LT LOWER FUSELAGE AFT OF WING SCAN LIGHT AFT OF PREVIOUS RPR, CRACK IS ON THE EDGE OF A STRINGER. [SUP 05- 08-07] MAJOR REPAIR ACCOMPLISHED: DAMAGED AREA CUTOUT. MFG'D & INSTALLED DOUBLER, TRIPLER AND FILLER REPAIR. 2 L 7 2 4F RT A16WE 2007050300246 20070503 00246 NM 2007 5 3 2007UALA01242 1 20070420 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 541UA 25253 13C FLOOR STRIP LOOSE. EEL LIGHT INOP AT 13D. REPLACED EEL LAMP AND AND REUSED THE JUMPER AND STRIP, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050300249 20070503 00249 WP 2007 5 3 NWAA071619993 1 20070330 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 1005 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8986E 47402 DURING "H" CHECK, FOUND CRACKS IN FRAME AT APU DOOR CUTOUT BS 1005 RBL 30-LBL 30. REPAIRED PER EA 98-208491. 2 L 7 2 4F A6WE 2007050300250 20070503 00250 EU 2007 5 3 2007UALA01245 1 20070421 A 2150 A/C PACK AIRBUS 320 A320232 3930326 EU NR 2 OVERHEATED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 406UA 454 CREW REPORTED BAD ODOR IN THE CABIN. NR 2 PACK OVERHEATED SO IT WAS SHUT DOWN, THUS DESCENDING TO FL300. CONTINUED TO DESTINATION. REPLACED NR 2 RAM AIR OUTLET ACT. OPS CHECKS GOOD. AND ALSO PACK CONTROLLER AS PRECAUTION. NO REPEATS SIN CE 10/13. 2 L 7 2 4F RT A28NM 2007050300254 20070503 00254 2007 5 3 2007UALA01249 4 20070421 A 2565 SLIDE BOEING 737 737322 1384676 NM L2 DOOR DISLODGED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 SLIDE AT DOOR 2L DISLODGED. [SUP 05-16-07] REMOVED SLIDE PACK AND REPACKED SLIDE. 2 L 7 2 4F RT A16WE 2007050300255 20070503 00255 2007 5 3 2007UALA01250 4 20070421 A 2565 SLIDE BOEING 737 737322 1384676 NM R2 DOOR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 301UA 23642 DOOR 2R SLIDE PACK COMING OUT OF CONTAINER. [SUP 05-16-07] REPLACED SLIDE ASSEMBLY. 2 L 7 2 4F RT A16WE 2007050300256 20070503 00256 NM 2007 5 3 F3LA200700083 1 20070422 A 5410 STRUCTURE AIRBUS A319 A319111 3930336 NM NR 2 NACELLE FAILED A F3LA A UNSCHED LANDING C F.O.D. CL CLIMB 1 NM 03 904FR 1579 NR 2 ENGINE COWLING DEPARTED AIRCRAFT. CAUSE UNKNOWN AT THIS TIME AND IS UNDER INVESTIGATION BY THE FAA. [SUP 05-15- 07] THE NR 2 ENGINE FWD CANTILEVER ASSY SUSTAINED SIGNIFICANT DAMAGE. REMOVED AND REPLACED NR 2 ENGINE CANTILEVER ASSY . PER EA A9-57R-11875. 2 L 7 2 4F RT A28NM 2007050300257 20070503 00257 2007 5 3 2007UALA01251 4 20070421 A 2565 COVER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EVAC SLIDE LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 671UA 30026 DOOR 1R SLIDE PACK COVER APPEARS LOOSE. [SUP 05-18-07] SLIDE REMOVED FROM ACFT. REINSTALLED REPLACEMENT SLIDE. SLIDE B USTLE REINSTALLED. A/C RETURNED TO SERVICE. SLIDE PROBLEM ROOT CAUSE: SUSPECT IMPACT BY CLEANING & FOOD SERVICE EQUIPM ENT LOOSENED PACK COVER. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050300258 20070503 00258 NM 2007 5 3 2007UALA01252 1 20070420 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT & CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 578UA 26694 ELECTRICAL BURNING ODOR IN COCKPIT & CABIN, DISSIPATED QUICKLY, TURNED OFF RIGHT RECIRCULATION FAN. [06-14-07] CONDUCTED TROUBLESHOOTING TO IDENTIFY WHETHER SOURCE OF ODOR COULD BE FWD E&E COMP OR PNEUMATICS. RAN PACKS SEVERAL HRS ALSO RT FAN UNABLE TO DUPLICATE. ROOT CAUSE COULD NOT BE ESTABLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050300259 20070503 00259 NM 2007 5 3 2007UALA01253 1 20070421 A 5270 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR UNSECURE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 576UA 26690 DOOR 4R WILL NOT ARM. [06-14-07] SECURED SLIDE LANYARD: OPS CHK GOOD.AND ARMS NORMAL 2 L 7 2 4F 4 F RT A2NM E17NE 2007050300262 20070503 00262 EU 2007 5 3 2007UALA01256 1 20070421 A 3350 BATTERY AIRBUS 320 A320232 3930326 EU CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 484UA 1609 EMERGENCY LIGHT TEST FAILING EPSU BATTERY EMERGENCY L. RESET OPS CHECKS GOOD. 2 L 7 2 4F RT A28NM 2007050300263 20070503 00263 NM 2007 5 3 2007UALA01257 1 20070422 A 3397 58781 WIRE HARNESS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 501UA 24622 EEL FLOOR LIGHTS INOP FROM SEAT 24 TO 32. REPLACED CABLE ASSY. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050300264 20070503 00264 2007 5 3 2007UALA01258 4 20070420 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR ACTIVATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 RAMP PERSONNEL FOUND DOOR 1L SLIDE OFF DOOR AND ON FLOOR. [06-14-07] REASSEMBLED AND REATTACHED SLIDE TO DOOR 1L PER UA ENGINEERING SPECIFICATIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050300266 20070503 00266 NM 2007 5 3 2007UALA01261 1 20070423 A 7330 WARNING LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FILTER BYPASS ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 311UA 23672 727186 RTFL DUE TO LEFT ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED. [SUP 05-16-07] CAUSE IS UNDETERMINABLE. NO DEFECTS FOUN D. REPLACED FUEL FILTER AS A PRECAUTION. 2 L 7 2 4F 4 F RT A16WE E21EU 2007050300267 20070503 00267 NM 2007 5 3 2007UALA01263 1 20070423 A 5311 ANGLE BOEING 737 737322 1384676 NM RT MLG WW CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 RIGHT HAND WHEEL WELL BS 695 FRAME INNER CHORD ANGLE CRACKED, LOWER INNER RADIUS. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED CRACKED CHORD ANGLE. 2 L 7 2 4F RT A16WE 2007050300269 20070503 00269 NM 2007 5 3 2007UALA01265 1 20070423 A 5347 SEAT TRACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 CABIN SEAT TRACK AT BS 770 AND LBL 54 IS EXFOLIATED. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION & DAMAGED SECTION OF SEAT TRACK. FABRICATED & INSTALLED SEAT TRACK SECTION, SPLICE PLATE & SPLICE CHANNEL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050300270 20070503 00270 SO 2007 5 3 SIMA200712008 1 20070427 A 2150 78210011 PRESSURE SWITCH EMB 135 EMB135KL 3260302 SO NR 1 A/C PACK FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 838AE 17504 11319 145651 PACK ONE OVERLOAD MESSAGE FOLLOWED BY PACK TWO OVERLOAD MESSAGE, EMERGENCY DECLARED. RETURNED TO ACT. PERFORMED FUNCTI ONAL CHECK OF NUMBER ONE PACK WITH NO DEFECTS NOTED. REMOVED AND REPLACED NUMBER TWO PACK OVERPRESSURE SWITCH IAW EMB 2 1-51-06. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050300271 20070503 00271 NM 2007 5 3 2007UALA01266 1 20070423 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 MAIN CABIN STR 15L CRACKED STA 680. [SUP 05-04-07] MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED STRINGER. FABRICATED & INSTALLED NEW CHORD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050300274 20070503 00274 NM 2007 5 3 2007UALA01267 1 20070424 A 5415 LUG BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 PYLON CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 178UA 24385 BORE CORRODED AND SCRATCHED - NR 4 PYLON UNDER WING FITTING BEARING LUG, BOTH SIDES. [SUP 05-16-07] BORE CORRODED AND SCRATCHED - NR 4 PYLON UNDER WING FITTING BEARING LUG, BOTH SIDES. ACCOMPLISHED BORING THE DSB UNDER WING FITTINGS PER C OA 899993040 & SB 747-54A2218. FINAL HOLE DIA AFTER HONE: INBD=2.2446" OUTBTD=2.2448". CORROSION & VIBRATION AGGRAVATE D BY HIGH TEMP CAUSED DUAL SIDE BRACE HOLE SURFACE DETERIORATION. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050300277 20070503 00277 NM 2007 5 3 2007UALA01268 1 20070424 A 5415 LUG BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 PYLON CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 178UA 24385 BORE CORRODED AND SCRATCHED - NR 4 PYLON DUAL SIDE BRACE FITTING BEARING LUG, BOTH SIDES. [SUP 05-16-07] BORE CORRODED AND SCRATCHED - NR 4 PYLON DUAL SIDE BRACE FITTING BEARING LUG, BOTH SIDES. ACCOMPLISHED BORING THE DSB UNDER WING FITT INGS PER COA 899993040 & SB 747-54A2218. FINAL HOLE DIA AFTER HONE: INBD=2.2450" OUTBTD=2.2452". CORROSION & VIBRATION AGGRAVATED BY HIGH TEMP CAUSED DUAL SIDE BRACE HOLE SURFACE DETERIORATION. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050300278 20070503 00278 NM 2007 5 3 DLM88070342 1 20070420 A 5512 5922578515 SKIN DOUG MD88 MD88 3023688 NM HORIZONTAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 903DE 53380 DURING ACCOMPLISHMENT OF EA 09-460214-12 OPN 0101, THE TRIM OUT IN THE HORIZONTAL STAB UPPER INBOARD SKIN PANEL EXTENDED PAST THE BARREL NUT PAD UP. THE TRIM OUT AND SPOTFACE INTO THE PAD UP WAS SUBMITTED TO BOEING FOR APPROVAL, AND WAS AP PROVED AS A TEMPORARY REPAIR PER THE TYPICAL STAB UPPER SKIN INSPECTIONS. THIS WAS DOCUMENTED AND INCLUDED IN ERA 46138 7-14. 2 L 7 2 4F RT A6WE 2007050300281 20070503 00281 NE 2007 5 3 2007UALA01271 2 20070424 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 SURGES A UALA O OTHER O OTHER DE DESCENT 1 WP 29 657UA 27112 727856 NR 2 ENGINE SILENT SURGE. [SUP 05-18-07] REPLACED NR 2 ENG ELECTRONIC ENGINE CONTROL PER AMM 73 -21-04. RT ENG PIMU HA D 'EEC CH-A T29 RNG FAIL' REF SMC 2. REF LOG 1 DURING ENG RUN AFTER REPLACE OF EEC FOUND PIMU FAULT 'EEC CH-A T29 RNG F AIL'. REPLACED NR 2 ENG LEFT 2.9 BLEED VALVE THERMOCOUPLE PER AMM 75-32-06, ENGINE CKS GOOD. A/C RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050300282 20070503 00282 NM 2007 5 3 DL764070343 1 20070421 A 2520 SEAT BOEING 767 767432ER 1385134 NM 6B SMOKE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 841MH 29714 SMOKE FROM SEAT 6B WHILE BEING ADJUSTED. PERFORMED INSPECTION OF ALL ACTUATORS AND CONNECTOR. REACTIVATED, SEAT AND OP ERATED SEVERAL TIMES WHILE SITTING SEAT. NO SMOKE SEEN OR ODOR NOTICED. OPERATION NORMAL MCO/PLAC REMOVED. 2 L 7 2 4F RT A1NM 2007050300283 20070503 00283 2007 5 3 2007UALA01272 4 20070423 A 2565 SLIDE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE L1 DOOR OUT OF LIMITS A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 DOOR 1L SLIDE IS OUT OF LIMITS. [SUP 05-18-07] SLIDE SHOULD READ NO LESS THAN 2975 AT 70 DFG, IT IS CURRENTLY READING 2500. REPLACED SLIDE. A/C RETURNED TO SERVICE. SLIDE PROBLEM ROOT CAUSE: SUSPECT SEAL DETERIORATION AT FILL VALVE PRE SSURE HOSE CONNECTION. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050300284 20070503 00284 2007 5 3 DL76L070344 4 20070421 A 2310 231001831 TRANSCEIVER BOEING 767 767332 1382001 NM LT HF SYSTEM FAILED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 199DN 28456 LEFT HF FAILED IN FLIGHT, UNABLE TO RESET SYSTEM. DUE TO THEATER RESTRICTIONS A/C RETURNED TO ATL FOR REPAIR. REMOVED AND REPLACED LT HF XCVR OPN CKS NML. 2 L 7 2 4F RT A1NM 2007050300288 20070503 00288 NM 2007 5 3 DL76L070350 1 20070422 A 3244 767ERM TIRE BOEING 767 767332 1382001 NM NR 3 FAILED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 1201P 28458 NR 3 MLG TIRE HAS LARGE FLAT SPOT FROM MISSING 12X8 INCH CHUNK OF RUBBER DOWN TO THE CORD. REMOVED AND REPLACED NR 3 ML G WHEEL ASSY PER AMM. PRESS CK GOOD. FLIGHT RTB DUE TO BUMPING NOISE DURING TAXI, FLAT SPOT ON TIRE. 2 L 7 2 4F RT A1NM 2007050300289 20070503 00289 NM 2007 5 3 DL76L070351 1 20070422 A 3244 TIRE BOEING 767 767332 1382001 NM NR 4 FAILED A DALA O OTHER O OTHER LD LANDING 1 SO 27 1201P 28458 UPON LDG, NR 4 TIRE FAILED AND DAMAGED THE NR 4 HUBCAP AND XDCR DRIVE COUPLING. TIRE SKID APPEARS TO HAVE CAUSED THE TI RE FAILURE. IN WORK T/S ANTI-SKID SYS, WILL UPDATE. NR 4 WHEEL TIRE BLOWN. REMOVED AND REPLACED NR 4 WHEEL ASSY WITH A.A. WHEEL ASSY P/N 260811-5. PLY RATING CHECKED ALSO. AOG DESK AND CONFIG DESK NOTIFIED. NIL DAMAGE TO GEAR OR UNDER WIN FROM BLOWN TIRE. REPLACED NR 4 ANTI-SKID CONTROL VALVE PER M/M. LEAK CHECKED REMOVED AND REPLACED NR 4 ANTI-SKID TRANSDUCER PER M/M. 2 L 7 2 4F RT A1NM 2007050300292 20070503 00292 EU 2007 5 3 F3LA200700088 1 20070421 A 5315 D5347217220400 FLOORBEAM AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 801FR 4759 1939 DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE HOLE ON FLOORBEAM Y1292 FWD OF FR68. REPLACED FLOORBEA M AT Y1292 FWD OF FR68 IAW SRM 51-42-11, FIG 6 AND 7. 2 L 7 2 4F RT 2007050300294 20070503 00294 2007 5 3 2007UALA01273 4 20070421 A 2210 AUTOPILOT SYS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 WP 29 198UA 28716 WITH CENTRE AUTO-PILOT IN CMD IN CLEAR AND SMOOTH AIR AIRCRAFT ABRUPTLY PITCHED NOSE DOWN, A-C LOST 30 FEET AND IMMEDIAT ELY HARSHLY PITCHED UP THEN BEGAN TO PORPOISE. [SUP 05-18-07] REPLACED CTR FLIGHT CONTROL COMPUTER. REF SMC3, NEEDS C AT 3. PERFORMED CAT III PER MMM 22-10-00 AND 34-61-00 CMC GRD CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050300296 20070503 00296 EU 2007 5 3 2007UALA01276 1 20070423 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 474UA 1475 EMERGENCY LIGHT TEST FAILS WITH "EPSU INT LOAD" MESSAGE. [SUP 05-16-07] REPLACED EPSU. ALSO REPLACED BATTERY. OPS CHEC KS GOOD. 2 L 7 2 4F RT A28NM 2007050300297 20070503 00297 NM 2007 5 3 2007UALA01277 1 20070423 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM CABIN SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 351UA 24319 EMERGENCY EXIT LIGHTS INOP ON FLOOR FROM ROW 15 TO LAST ROW. REPLACED SHORTED LAMP AT THE LAST SEAT ROW. OPERATES NORM ALLY. 2 L 7 2 4F RT A16WE 2007050300298 20070503 00298 NM 2007 5 3 2007UALA01278 1 20070424 A 3350 1317 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE COCKPIT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHT INOP COCKPIT CEILING. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050300299 20070503 00299 NM 2007 5 3 2007UALA01279 1 20070424 A 3350 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 WALL EEL INOP: UPPER DECK LT WALL ACROSS FROM LAV 124. FOUND INOP LAMP ASSY. REMOVED LAMP, PARTS IN AREA. LAMP ON AOG. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050300300 20070503 00300 NM 2007 5 3 2007UALA01280 1 20070424 A 3350 1317 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EEL INOP: SEAT 32 LEFT. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050300301 20070503 00301 2007 5 3 2007UALA01281 4 20070423 A 2565 CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE FROZEN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 509UA 24763 RT OVERWING SLIDE, MANUAL BACKUP CABLE IS FROZEN. [SUP 06-06-07] REPLACED CABLE, AND THE NON-FUNCTIONAL CABLE HAS BEEN THE ROOT CAUSE OF THE PROBLEM. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050300302 20070503 00302 2007 5 3 2007UALA01282 4 20070423 A 2564 LATCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OVERHEAD RAFT FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 590UA 28708 AFT OVERHEAD RAFT STOWAGE COMPARTMENT WILL NOT OPEN. [SUP 05-16-07] ADJUSTED LATCH. OP CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050300303 20070503 00303 EA 2007 5 3 QXEA200700692 1 20070430 A 2840 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA CROSSFLOW PUMP UNKNOWN A QXEA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 NM 09 615QX 10065 PDX - FLIGHT 2509 RETURN TO THE GATE FOR A XFLOW PUMP CAUTION ILLUMINATED WHEN THE FUEL SYSTEM IS SELECTED TO MANUAL PRI OR TO TAKEOFF. MAINTENANCE WAS UNABLE TO DUPLICATE THE PROBLEM. GROUND RAN BOTH ENGINES AND THE SYSTEM TESTED NORMALLY . NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007050300304 20070503 00304 EU 2007 5 3 F3LA200700090 1 20070421 A 5315 D5347218920400 FLOORBEAM AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 801FR 4759 1939 DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE HOLE ON FLOORBEAM -Y1292, AFT OF FR68. REPLACED FLOORB EAM AT FR68 STATION -Y1292 IAW SRM 51-42-11. 2 L 7 2 4F RT 2007050300306 20070503 00306 NM 2007 5 3 DHL2007788505 1 20070423 A 5730 SKIN BOEING 727 727214 138407R NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 RIGHT WING FIXED L/E NR 5 SLAT, INBD TRACK CUTOUT FOR SLAT TRACK SEAL, AFT INBD RADIUS, .5"-.75" LONG CRACK W/S 383.5. CUTOUT DAMAGED AREA 7" BY 2.25" IAW B727 SRM 57-30-4. FABRICATED NEW DOUBLER 7" BY 5.375 BY .040, 301 1/2 HARD AND FILL ER 7" BY 2.25 BY .040, 301 1/2 HARD IAW B727 SRM 57-30-4. PRIMED PARTS AND INSTALLED DOUBLER REPAIR IAW B727 SRM 51-10- 2 AND 57-30-4. 2 L 7 3 4F A3WE 2007050300307 20070503 00307 NM 2007 5 3 DHL2007788501 1 20070424 A 5753 6521630174 SKIN BOEING 727 727214 138407R NM FOREFLAP GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 RIGHT WING, INBD FOREFLAP, INBD UPPER SURFACE GOUGED, WS 198, RWBL 84. REMOVED DAMAGED AREA APPROX 5" DIA IAW B727 SRM 51-40-20,PAR 7, FIG 3. FABRICATED FILLER 5" DIA AND DOUBLER 8" DIA FROM 2024T6 IAW B727 SRM 51-40-24, FIG 1 AND 57-50-2 FIG 3. CLEANED, PREPPED, ANODIZED, PRIMED AND INSTALLED REPAIR PARTS IAW B727 SRM 51-40-20, PAR 8, 14, 15, 18, 20 AND 22, 51-40-24 FIG 1 AND 57-50-2 FIG 3. 2 L 7 3 4F A3WE 2007050300308 20070503 00308 NM 2007 5 3 UPS07M49678 1 20070319 A 5350 STRUCTURE DOUG MD11 MD11F 3023600 NM TAIL CONE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C FWD TAIL CONE: LT RETRACTABLE DOOR EXTERIOR FIN FOUND DENT AS MARKED NR 6660. DENT AREA FOUND BEYOND LIMIT PER SRM 51-81-01 VOLIR38. DAMAGED AREA TRIMMED PER SRM 52-00-01VOLIR38. HFEC INSP C/OUT PER DAC NDTSPM REV13 06- 10 -01.001. FOUND NO CRACK EVIDENT. REPAIR DOUBLER AND FILLER FAB USING 2024T3- 0.032" PER SRM 52-00-01VOLIR38. TREAT ED PER SRM 51-21-01VOLIIR38. PAINTED PER SRM 51-21-01VOLIIR38. INSTALLED PER SRM51-35-01 VOLIIREV38. 2 L 7 3 4F RT A22WE 2007050300309 20070503 00309 NM 2007 5 3 2007UALA01284 1 20070423 A 3350 D71702001 BATTERY PACK BOEING 777 777222 1385219 NM CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 799UA 26926 C XOME AT PED NR 4 RT AND LT OVERHEAD PANEL EMERG LIGHTS INOP. REPLACED BATTERY PACK ABOVE DOOR 4 RIGHT. OP CHECKED GO OD. 2 L 7 2 4F RT T0001SE 2007050300310 20070503 00310 NM 2007 5 3 UPS07M49688 1 20070223 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM BS 1541 L37R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:C CTR CRGO, RT TUNNEL AREA, STA 5-53 THROUGH STA 1541 LONGERON R37 FOUND WITH CORROSION AT SEVERAL LOCAT IONS AS MARKED. CTR CARGO RT STA 5-53-5-113 SKIN AND LONGERON R37 REMOVED PER SRM51-31-01 V.II R.38. LONGERON REWORKED PER DOUGLAS DWG A5A7022. FPI CARRIED OUT PER DPS 4.707 REV AW FOUND NO CRACK EVIDENT. LONGERON R37 FASTENER HOLES PICK ED UP PER SRM 51-31-01 V.II R.38.CTR CGO RT STA 5-53 TO 5-113 SKIN AND NEW LONGERON R37. INSTALLED PER SRM 51-31-01 V.I I R.38. 2 L 7 3 4F RT A22WE 2007050300312 20070503 00312 NM 2007 5 3 UPS07M49689 1 20070303 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM BS 815 S48 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:C FWD CARGO BILGE AREA LONGERON L48 FOUND WITH CORROSION AS MARKED. FWD CARGO STA 815 LONG L48 REMOVE A ND FOUND OVER LIMITS PER SRM 53-00-01 FIG 3 V.I R.38. HFEC CARRIED OUT PER DAC NDTSPM R.13 PART6 06-10-01.001/011. FOU ND NO CORROSION CRACK. REPAIR ANGLES FAB PER EN1146-07. FPI CARRIED OUT PER DPS 4.707 REV AW AND FOUND NO CRACK EVIDEN T. REP ANGLES AND SHIM AT FWD CARGO STA 815 LONG L48. INSTALLED PER SRM 51-31-01 V.II R.38. 2 L 7 3 4F RT A22WE 2007050300314 20070503 00314 WP 2007 5 3 UPS07849713 1 20070414 A 5340 DC853020002 FITTING DOUG DC8 DC873F 302199F WP FS 759 L22R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 BOOT FITTING CORRODED AT STA 759 L22R. REMOVED CORRODED BOOT FITTING AT STA 759 L22R IAW SRM 51-1-20 D. PROCURED, LOCATED, DRILLED UP, AND INSTALLED BOOT FITTING AT STA 759 L22R IAW SRM 51-1-21, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007050300315 20070503 00315 WP 2007 5 3 UPS07849714 1 20070428 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 FOUND EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY BATTERY PACK PER MM 33-50-02-2. CK'S NORMAL. 2 L 7 4 4F RT 4A25 2007050300316 20070503 00316 WP 2007 5 3 UPS07849717 1 20070427 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 DURING PREFLIGHT WHEN GROUND POWER TO BATTERY, EMERGENCY LIGHTS DID NOT WORK. REPLACED EMERGENCY BATTERY PACK PER MM 33 -50-02-2. CK'S NORMAL. 2 L 7 4 4F RT 4A25 2007050300319 20070503 00319 EU 2007 5 3 2007UALA01287 1 20070424 A 2910 CONTROL UNIT AIRBUS 320 A320232 3930326 EU GREEN HYD SYS MALFUNCTIONED A UALA O OTHER K FLUID LOSS AP APPROACH 1 WP 29 452UA 955 LOST GREEN HYDRAULIC SYSTEM. [06-22-07] FOUND A LEAKING HYDRAULIC TUBE B-NUT ON THE NR 1 ENGINE THRUST REVERSER HYDR AULIC CONTROL UNIT. REPLACED HYDRAULIC TUBING AND B-NUT. ALSO REPLACED THE NR 1 ENGINE DRIVEN PUMP, HIGH PRESSURE FLITER AND CASE DRAIN FILTER AS A PRECAUTION. 2 L 7 2 4F RT A28NM 2007050300321 20070503 00321 NM 2007 5 3 UPS07M49708 1 20070413 A 5320 INTERCOSTAL DOUG MD11 MD11F 3023600 NM BS 1256-1273 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C DOOR 3 CROWN AREA, AT STA 1256 TO STA 1273 LONG 1 RT INTERCOSTAL FACE FOUND CORROSION. CORROSION REMO VED PER SRM 51-21-01 VOL IIR38 ORI THK 0.032" MATL REMOVED 0.023" MATL REMAIN 0.009" FOUND OUT OF LIMIT PER SRM 53-00-01 FIG1AVOLIR38. INTERCOSTAL REMOVED PER SRM 51-35-01VOL IIR38. NEW INTERCOSTAL FAB PER BOEING DWG AEA0202REVK. HEAT TR EATED PER DPS7.00-1 AND HARD VALUE 15T88.5 PER DPS1 05-3. HOLES PICK UP, PROTECTED AND PAINT. INSTALLED PER SRM 51-35- 01 VOLIIR38. 2 L 7 3 4F RT A22WE 2007050300322 20070503 00322 NM 2007 5 3 UPS07M49709 1 20070315 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1931-2007 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C AFT CABIN, LT CURVED SEAT TRACK I/B AND O/B FLANGE UPPER AND LOWER SURFACE FOUND CORROSION BETWEEN STA 1931 - STA 2007 LT 107.5". CORROSION REMOVED PER SRM 51-21-01 VIIR38. ORI THK 0.080" MATL REMOVED 0.040" MATL REMAIN 0.040" OUT OF LIMIT PER SRM 53-70-00 FIG 3 VIR38. AREA TRIM OFF, HFEC INSPECTION C/O PER DACNDTSPMR1306-10-01.001, NO C RACK EVIDENT. NEW SEATTRACK AND SPLICE RWK PER SRM53-70-00 FIG 1 VIR38. HOLES PICKUP AND PROTECTED PER SR 51-35-01 AND 51-21-01 VIIR38. INSTALLED PER SRM 51-31-01 VIIR38 AND 51-33-01VIIR38. 2 L 7 3 4F RT A22WE 2007050300323 20070503 00323 NM 2007 5 3 2007UALA01288 1 20070425 A 5730 SKIN BOEING 777 777222 1385219 NM RT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 799UA 26926 RT WING L/E AFT OF NR 9 SLAT CRACKED OUT FROM RESTORATION SEAL CUTOUTS. [SUP 05-18-07] RT WING L-E AFT OF NR 9 SLAT CR ACKED OUT FROM RESTORATION SEAL CUTOUTS. REPAIRED PER OV WRITE-UP W1682T AND R&R R41952. 2 L 7 2 4F RT T0001SE 2007050300326 20070503 00326 NM 2007 5 3 DHL2007788507 1 20070424 A 5347 BAC15201466 SEAT TRACK BOEING 727 727214 138407R NM BS 868-950C CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 MAIN CARGO DECK, SEAT TRACK LBL 45L, FROM BS 850 TO 950C, SURFACE CORROSION, STA 868 TO 950C REMOVED .009 MATERIAL, ORIG INAL MATERIAL THICKNESS .230, MATERIAL REMAINING .221 WITHIN LIMITS IAW B727 SRM 53-10-1, FIG 3. TREATED AND PRIMED ARE A IAW B727 SRM 51-10-2. STA 852.56 TO 868.65 REMOVED CORROSION AND MATERIAL REMAINING OUT OF LIMITS IAW B727 SRM 53-10- 1, FIG 1. REMOVED FLOATING SEAT TRACK IAW B727 SRM 51-30-2. FABRICATED NEW FLOATING SEAT TRACK FROM BAC 1520-1466-7075 T6, 16" LONG IAW B727 SRM 53-10-1, FIG 7 AND 51-30-5. TREATED PRIMED AND INSTALLED SEAT TRACK IAW B727 SRM 51-10-2, 51- 30-2 AND 53-10-1, FIG 7. 2 L 7 3 4F A3WE 2007050300327 20070503 00327 EU 2007 5 3 AWXA200700534 1 20070428 A 3350 321431 BATTERY PACK AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHT FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 640AW 448 LAS - EEL - LT AFT EPSU BATTERY PACK FAILED TEST. MX REMOVED AND REPLACED BATTERY PACK PER TASK CARD A1C33302. OPERATI ONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007050300329 20070503 00329 EU 2007 5 3 2007UALA01290 1 20070424 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 409UA 462 SEATS 11C & 22C EEL LIGHTS HAVE 1 LAMP INOPERATIVE. [SUP 05-16-07] REPLACED LAMP. OPS GOOD. 2 L 7 2 4F RT A28NM 2007050300330 20070503 00330 NM 2007 5 3 DHL2007788503 1 20070419 A 5755 651734781A HINGE FITTING BOEING 727 727214 138407R NM NR 3 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 LEFT WING UPPER T/E, NR 3 SPOILER PANEL, CENTER OUTBD HINGE FITTING IS CRACKED. STOP DRILLED CRACK .250 DIA AT END OF C RACK IAW B727 SRM 51-10-1, VERIFIED WITH NTD HFEC IAW B727 NDTM PT6-51-00-00, FIG 23, CRACK TERMINATED IN STOP DRILL HOL E. FABRICATED 6' BY 4" DOUBLER FROM 7075T6, .071 IAW B727 SRM 57-30-4 FIG 10. TREATED, PRIMED AND INSTALLED REPAIR PAR T IAW B727 SRM 51-10-2, 51-30-2 AND 57-30-4, FIG 10. 2 L 7 3 4F A3WE 2007050300332 20070503 00332 WP 2007 5 3 ARWA20070402 1 20070425 A 7930 O-RING DOUG DC10 DC1030 3023501 WP NR 1 ENGINE OIL UNKNOWN A ARWA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SO 19 524MD 46999 NR 1 ENGINE PRECAUTIONARY ENGINE SHUTDOWN, LOW OIL PRESSURE INDICATIONS. C-SUMP TUBE AT 6 O'CLOCK POSITION SLEEVE AND O -RING DAMAGED. REPLACE O-RINGS AND SECURED SLEEVE IN ACCORDANCE WITH ARROW M/M 70-00-00. DURING RUN-UP, NO LEAKS FOUND AND OIL PRESSURE NORMAL IN ACCORDANCE WITH M/M 71-06-00. 2 L 7 3 4F A22WE 2007050300333 20070503 00333 NM 2007 5 3 DHL2008788501 1 20070424 A 5753 6521630174 SKIN BOEING 727 727214 138407R NM RT WING FOREFLAP GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 RIGHT WING, INBD FOREFLAP, INBD UPPER SURFACE GOUGED, WS 198, RWBL 84. REMOVED DAMAGED AREA APPROX 5" DIA IAW B727 SRM 51-40-20, PAR 7, FIG 3. FABRICATED FILLER 5" DIA AND DOUBLER 8" DIA FROM 2024T6 IAW B727 SRM 51-40-24, FIG 1 AND 57-50- 2 FIG 3. CLEANED, PREPPED, ANODIZED, PRIMED AND INSTALLED REPAIR PARTS IAW B727 SRM 51-40-20, PAR 8, 14, 15, 18, 20 AND 22, 51-40-24 FIG 1 AND 57-50-2 FIG 3. 2 L 7 3 4F A3WE 2007050300336 20070503 00336 NM 2007 5 3 2007UALA01294 1 20070424 A 2560 RING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 589UA 28707 DOOR 1L MISSING D RING. [06-14-07] FOUND LANYARD MISSING INSTALLED SERVICABLE LANYARD. INSTALLED. ()INSPECTED D OOR 3L AND D-RING IS INSTALLED. REPLACED LANYARD AT DOOR 1L. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050300339 20070503 00339 2007 5 3 DHLA200700024 2 20070427 A 7200 ENGINE BOEING 727 7272Q9 138448M NM NR 2 POWER LOSS A DHLA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 05 740DH 21930 ON TAKEOFF ROLL, BELOW 80 KTS NR 2 ENG N1 INDICATOR DROPPED TO 0 PERCENT. ALL OTHER ENGINE PARAMETERS NORMAL, 146,700LB S.;80 KTS IAS;26C PA-26FT.1. ENTERED ON DMI NR 28913 IAW MEL 77-2 CAT"B" PLACARD INSTALLED + SP-77-2. 2 L 7 3 4F RT A3WE 2007050300340 20070503 00340 NM 2007 5 3 DHL2007782512 1 20070501 A 5330 SKIN BOEING 727 727227 1384078 NM BS 351 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 782DH 21998 LOWER HALF OF FUSELAGE EXTERIOR SURFACE RT, BS 351.0, DENTED BETWEEN STR 24R AND 25R. CUT OUT DAMAGED AREA 3.3" BY 3.5" . FABRICATED, REPAIR DOUBLER FROM 2024-T3, .050" BY 12" BY 12", PO NR 9004174; REPAIR FILLER FROM 2024-T3, .063" BY 14" BY 2", PO NR 9003641, PER B727 SRM 53-30-3 FIG 5. TREATED, PRIMED, AND INSTALLED REPAIR PARTS PER B727 SRM 53-30-3 FIG 5 AND 51-10-2. 2 L 7 3 4F A3WE 2007050300341 20070503 00341 NM 2007 5 3 2007UALA01297 1 20070425 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 AFT CABIN FLOOR STRUCTURE, FLOORBEAM UPPER "T" CAP UPPER SURFACE HAS 2 SPOTS OF CORROSION. BS 1016 RBL 5 TO 14.5 AT WL 208. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION. FABRICATED & INSTALLED FILLER, STRAP & NESTED ANGLE REPAIR ON FWD SIDE OF FLOORBEAM CAP. 2 L 7 2 4F RT A16WE 2007050300342 20070503 00342 EU 2007 5 3 UPS07149686 1 20070424 A 2910 GASKET AIRBUS A300 A300F4622R 3930360 EU HYDRAULIC SYSTEM FAILED A IPXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 160UP 0005 EMERGENCY DECLARED INTO SJU DUE TO GREEN HYDRAULIC SYSTEM FAILURE. A/C LANDED SAFELY AND WAS TOWED TO RAMP. FOUND PRES SURE SW GASKET BROKEN AT GREEN MANIFOLD HP REPLACED AS REQD PER AMM 29-00-00- AND 31-53-03. REMOVED AND REPLACED BOTH G REEN ENGINE DRIVEN PUMPS IAW AMM 29-11-32-04 AND REPLACED BOTH ENGINE CASE ELEMENT FILTERS AS A PRECAUTION. ACCOMPLISHE D LEAK CHECK AND OPS CHECK. 2 L 7 2 4F RT A35EU 2007050300343 20070503 00343 NM 2007 5 3 DHL2007782510 1 20070430 A 5311 65196818 FRAME BOEING 727 727227 1384078 NM BS 320 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 782DH 21998 LARGE AREA OF CORROSION AT BS 320 APPROX, ON FRAME AND LOWER CHORD ANGLE, IN E-BAY FWD CRAWLWAY, RT SIDE BILGE AREA. LO WER NOSE CHORD CORRODED BEYOND LIMITS: REMOVED AND REPLACED LOWER RT NOSE CHORD ASSY PER B727 SRM 51-30-5, 51-30-2, AND 53-10-2 FIG 1. CUT OUT DAMAGED SECTION OF FRAME, 6" BY 6"; FABRICATED FILLER FROM 7075-T0, .050" BY 6" BY 6", PO NR 9 004219 AND HEAT TREATED TO T6 HARDNESS PER FASI ENGINEERING REPORT NR 2-37153-801 REV A. FABRICATED FRAME SPLICE FROM 7 075-T6, .050" BY 11.5" BY 5.5", PO NR 9004843. FABRICATION COMPLETED PER B727 SRM 53-10-2 FIG 1 AND 551-40-3 FIG 1. TR EATED, PRIMED, AND INSTALLED REPAIR PARTS PER B727 SRM 51-10-2 AND 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2007050300346 20070503 00346 NM 2007 5 3 DHL2007782508 1 20070430 A 5754 65162211 SKIN BOEING 727 727227 1384078 NM NR 4 SLAT DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 782DH 21998 NR 4 SLAT DENTED ON L/EDGE, LWS 380. CUT OUT DAMAGE, FABRICATED DOUBLER FROM 2024-T0, .080" BY 9" BY 4" (2 EA), PO NR 5 09622; FABRICATED FILLER FROM 2024-T3, .063" BY 4.75" BY 3.5", PO NR 9003641, PER B727 SRM 57-50-2 FIG 2 AND 57-50-3 FIG 1. HEAT TREATED 2024-T0 MATERIAL TO T4 PER FASI ENG REPORT NR 2-37153-801 REV A. TREATED, PRIMED, AND INSTALLED REPAI R PARTS PER B727 SRM 51-10-2, AND 57-50-3 FIG 1. 2 L 7 3 4F A3WE 2007050300350 20070503 00350 NM 2007 5 3 AWXA200700547 1 20070423 A 5320 143N85235 INTERCOSTAL BOEING 757 7572S7 1384962 NM BS 1240-1440 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 MCN - CRACKED INTERCOSTAL WEB, BS 1420 - BS 1440, S15R. REPLACED INTERCOSTAL WEB, BS 1420 - BS 1440, S15R IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007050300352 20070503 00352 NM 2007 5 3 DHL2007788504 1 20070418 A 5753 652163479 SKIN BOEING 727 727214 138407R NM LT WING TE FLAP DEBONDED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 LEFT INBD AFT FLAP, UPPER SURFACE LWBL 244, UPPER SURFACE CRACKED AND DISBONDED. REMOVED DAMAGED AREA 12.5" BY 15", CLE ANED, PREPPED AREA IAW B727 SRM 51-40-20, PAR 7, FIG 3. FABRICATED DOUBLER 3" BY 15" AND SKIN 12.5" BY 15" FROM 7075T6, .012, PRIMED, APPLIED ADHESIVE FILM IAW B727 SRM 51-40-20, PAR 8, 14, 15 AND 18, 51-40-24, FIG 3, AND 57-50-2 FIG 3. I NSTALLED AND CURED REPAIR AREA IAW B727 SRM 51-40-20, PAR 20 AND 51-40-24, FIG 3. FINISHED REPAIR AREA IAW B727 SRM 51- 40-20, PAR 22. 2 L 7 3 4F A3WE 2007050300353 20070503 00353 NM 2007 5 3 DHL2007788502 1 20070420 A 5313 BAC14981467075 STRINGER BOEING 727 727214 138407R NM BS 700-720 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 FWD LWR CARGO COMPARTMENT BS 700-720, STR 28L CORROSION ON STR. CUTOUT DAMAGED STR APPROX 30.25" LONG IAW B727 SRM 53-1 0-3 FIG 1. FABRICATED REPAIR PARTS, 2 HAT SECTIONS 12" AND 18.25" LONG FROM BAC1498-131-7075T6 AND 2 EACH SPLICES 12.25 AND 12.625" LONG FROM BAC1498-146-7075T6 IAW B727 SRM 53-10-2 FIG 9. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW B7 27 SRM 51-10-2, 53-10-2 FIG 9 AND 51-30-2. 2 L 7 3 4F A3WE 2007050300357 20070503 00357 NM 2007 5 3 UPS07549704 1 20070427 A 5610 WINDOW BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 467UP 25483 CAPTAIN'S SLIDING WINDOW CRANK CAME OFF SHAFT. INSTALLED SERVICEABLE BOLT ASSY REF IPC 52-11-09 AND AMM 56-11-04-4, OPS CHECK NORMAL. 2 L 7 2 4F RT A2NM 2007050300358 20070503 00358 NM 2007 5 3 UPS07549719 1 20070403 A 5311 146N102911 FRAME BOEING 757 75724APF 1384969 NM BS 1460 S26-27R DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 414UP 23854 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1460, BET S26R AND S27R. ACCOMPLISHED ON FINAL EA NR 757-5363-27 -A644 AND UPS NR B757-5310-2663-A. 2 L 7 2 4F RT A2NM 2007050300359 20070503 00359 NM 2007 5 3 UPS07549723 1 20070501 A 2150 A/C PACK BOEING 757 75724APF 1384969 NM LEFT ODOR A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 406UP 23728 LEFT PACK HAS FOUL ODOR. OPERATED LEFT PACK FOR EXTENDED PERIOD OF TIME. NO ODOR NOTED. THIS CLEARS M349455. 2 L 7 2 4F RT A2NM 2007050300363 20070503 00363 2007 5 3 UPS07549740 2 20070502 A 7200 ENGINE BOEING 757 75724APF 1384969 NM LEFT DAMAGED A IPXA E ENGINE SHUTDOWN C J F.O.D. WARNING INDICATION AP APPROACH 1 SO 01 463UP 28267 LEFT ENGINE SHUT DOWN PER QRH. EMERGENCY DECLARED DUE TO LARGE BIRD ST STRIKE ON FIRST OFFICER'S NR 1 WINDOW. EICAS MS GS APPEARED. OIL PRESSURE FOR LEFT ENGINE WAS AT 0 AND THE EGT AT 165. [SUP 05-07-07] R & R LEFT ENGINE PER T/C 5001/ 5002RR AND ALL APPLICABLE MM REFERENCES. CHECKS GOOD. 2 L 7 2 4F RT A2NM 2007050300365 20070503 00365 WP 2007 5 3 UPS07849721 1 20070424 A 5712 RIB DOUG DC8 DC873F 302199F WP LWS 876 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 LT WING OB LE CRACKED AT XFS 876. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2. REPAIR ANGLES IA W SRM 57-02-00, 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2007050300366 20070503 00366 WP 2007 5 3 UPS07849722 1 20070424 A 5712 RIB DOUG DC8 DC873F 302199F WP LWS 804 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 LT WING OB LE RIB CRACKED AT XFS 804. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2 REPAIR ANGLES IAW SRM 57-02-00, 51-01-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2007050300367 20070503 00367 NM 2007 5 3 2007UALA01300 1 20070425 A 5230 DOOR FRAME BOEING 737 737322 1384676 NM AFT CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 AFT CARGO DOOR FWD LOWER FRAME CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED FRAME SECTION. 2 L 7 2 4F RT A16WE 2007050300369 20070503 00369 NM 2007 5 3 2007UALA01302 1 20070425 A 5230 SKIN BOEING 737 737322 1384676 NM AFT CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 AFT CARGO DOOR S-N 020 LINE REPAIR INSTALLED ON EXTERIOR SKIN 18 INCHES FROM LOWER SIDE & 8 INCHES FROM FWD SIDE. MAJOR REPAIR ACCOMPLISHED: REMOVED LINE REPAIR. FABRICATED & INSTALLED FILLER & EXTERNAL DOUBLER REPAIR. 2 L 7 2 4F RT A16WE 2007050300370 20070503 00370 NM 2007 5 3 2007UALA01303 1 20070425 A 5320 INTERCOSTAL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 CABIN UNDER FLOORBOARD #P23, INTERCOSTAL UPPER ANGLE IS CRACKED AT STA 293, RBL 36. MAJOR REPAIR ACCOMPLISHED: REMOVED LINE REPAIR. FABRICATED & INSTALLED FILLER & EXTERNAL DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050300371 20070503 00371 NM 2007 5 3 2007UALA01304 1 20070425 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 LIGHTNING STRIKE AT STA 760, BELOW STR 4L. MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT DAMAGE. INSTALLED FILLER AND DOUBLER . 2 L 7 2 4F 4 F RT A1NM E24NE 2007050100158 20070501 00158 EA 2007 5 1 SWIA200718164 1 20070422 A 5753 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA LT TE FLAP DAMAGED A SWIA O OTHER O OTHER AP APPROACH 1 NM 07 971SW 7947 BIRD STRIKE TO LEFT INBOARD FLAP ON APPROACH INTO YWG. REPLACED LEFT INBOARD FLAP INBOARD LEADING EDGE PER 57-52-01. 2 L 7 2 4F RT A21EA 2007050100166 20070501 00166 EA 2007 5 1 SWIA200718172 1 20070328 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT AILERON PULLE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 LEFT AILERON OUTBOARD PULLEY BRACKET HAS CORRODED HARDWARE, DISCOVERED AT C-CHECK. REPLACED CORRODED HARDWARE ON LEFT A ILERON OUTBOARD PULLEY ATTACHING BRACKET PER CRJ200 SRM 51-41-02 PG 5, 6 AND 7. 2 L 7 2 4F RT A21EA 2007050100168 20070501 00168 EU 2007 5 1 AWXA200700526 1 20070423 A 5321 D5367180500400 FLOOR PANEL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 664AW 1621 SAL - CORROSION ON AFT LAV AND GALLEY FLOOR PANEL 261 FF, FR 66 - FR 68. REPLACED AFT LAV AND GALLEY FLOOR PANEL 261 FF , FR 66 - FR 68 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007050200001 20070502 00001 NM 2007 5 2 AWXA200700530 1 20070410 A 5311 65465588 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - FOUND CRACKED FRAME, BS 907, S9R. REPAIRED FRAME, BS 907, S9R IAW B737-300 SRM 53-00-07-2R2, FIGURE 201. 2 L 7 2 4F RT A16WE 2007050200004 20070502 00004 EU 2007 5 2 AWXA200700533 1 20070411 A 5210 FE174004 DAMPENER AIRBUS 320 A320231 3930325 EU ZONE 800 DEFECTIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 626AW 65 SAL - EES - L1 DOOR ASSIST DAMPENER DOES NOT WORK CORRECTLY WHILE OPENING AND CLOSING THE DOOR. REPLACED AND OPERATIONA L CHECKED THE L1 DOOR ASSIST DAMPENER IAW A320 AMM 52-11-14. 2 L 7 2 4F RT A28NM 2007050200006 20070502 00006 SO 2007 5 2 SIMA200712002 1 20070424 A 3250 STEERING SYS EMB 135 EMB135LR 3260305 SO NLG MALFUNCTIONED A SIMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 736DT 145388 LOST NOSE WHEEL STEERING WITH ELECTRICAL FAULTS DURING APU START UP. [SUP 05-08-07] PERFORMED ELECTRICAL RESET IAW EMB AMM 24-80-00 WITH ALL INDICATIONS NORMAL. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050200009 20070502 00009 SO 2007 5 2 SIMA200712011 1 20070426 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT LOOSE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 647AE 145222 EMERGENCY EXIT LIGHT ABOVE SERVICE DOOR INOPERATIVE. RESECURED LOOSE CONNECTOR ABOVE GALLEY CEILING PANEL IAW EMB AMM 2 0-00-00. OPERATIONAL CHECK GOOD IAW EMB AMM 33-50-11. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050200012 20070502 00012 2007 5 2 SIMA200712006 4 20070424 A 3417 ADC EMB 145 EMB145LR 3260212 SO NR 1 FAILED A SIMA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SW 21 614AE 145086 NUMBER ONE AIR DATA COMPUTER FAILURE, DIVERTED TO LRD. PERFORMED PITOT LEAK CHECK IAW EMB AMM 34-13-00 WITH NO DEFECTS. OPERATIONAL CHECK GOOD IAW EMB AMM 34-15-00. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050200018 20070502 00018 NM 2007 5 2 AWXA200700537 1 20070409 A 5755 SKIN BOEING 737 73733A 1384673 NM ZONE 500 DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW MA6398 23627 MCN - LEFT WING NR 4 GROUND SPOILER HAS AREA OF DISBOND, WS 188.75. REPAIRED LEFT WING NR 4 GROUND SPOILER, WS 188.75 I AW B737-300 SRM 51-70-10-2R4, FIGURE 201. 2 L 7 2 4F RT A16WE 2007050200021 20070502 00021 NM 2007 5 2 AWXA200700540 1 20070425 A 5322 140N2002345 SHEAR TIE BOEING 757 7572S7 1384962 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 MCN - FOUND CRACKED SHEAR TIE, BS 1460, S29L - S30L. REPLACED SHEAR TIE, BS 1460, S29L - S30L IAW B757-200 SRM 51-40-05 AND 51-30-01. 2 L 7 2 4F RT A2NM 2007050200022 20070502 00022 NM 2007 5 2 AWXA200700541 1 20070410 A 5311 65465935 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - CRACKED FUSELAGE FRAME, BS 500A, S9L. REPAIRED FUSELAGE FRAME, BS 500A, S9L IAW B737-300 SRM 53-00-07-2R2, FIGURE 201. 2 L 7 2 4F RT A16WE 2007050200025 20070502 00025 NM 2007 5 2 AWXA200700544 1 20070410 A 5311 654655734 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - FOUND CRACKED FUSELAGE FRAME, BS 887, S9R. REPAIRED FUSELAGE FRAME, BS 887, S9R IAW B737-300 SRM 53-00-07-2R2, FI GURE 201. 2 L 7 2 4F RT A16WE 2007050200026 20070502 00026 NM 2007 5 2 AWXA200700545 1 20070410 A 5311 90526911 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - FOUND CRACKED FUSELAGE FRAME, BS 767, S9R. REPAIRED FUSELAGE FRAME, BS 767, S9R IAW B737-300 SRM 53-00-07-2R2, FI GURE 201. 2 L 7 2 4F RT A16WE 2007050200035 20070502 00035 EA 2007 5 2 MASA200700001 1 20070101 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 651BR 7426 ASH 1003 HNL. RT EXTERIOR FWD EMERGENCY LIGHT INOP. MX REPLACED THE LAMP AND OP CHECK WAS GOOD. 2 L 7 2 4F RT A21EA 2007050200036 20070502 00036 EA 2007 5 2 MASA200700006 1 20070102 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75993 7372 ASH 7130 RDU. CREW REPORTED THE PAX DOOR EXIT LIGHT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2007050200037 20070502 00037 EA 2007 5 2 MASA200700007 1 20070102 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75993 7372 ASH 7185 IAD. FWD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT LED NOT FLASHING AND STRAP BROKEN. MX REMOVED AND REPLACED FLA SHLIGHT ASSY. 2 L 7 2 4F RT A21EA 2007050200038 20070502 00038 EA 2007 5 2 MASA200700008 1 20070103 A 3350 59256 INVERTER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17175 7175 ASH 7212 DSM. AFT HALF OF THE EMERGENCY FLOOR PATH LIGHTING INOP. MX REMOVED AND REPLACED INVERTER. 2 L 7 2 4F RT A21EA 2007050200039 20070502 00039 EA 2007 5 2 MASA200700017 1 20070104 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 939LR 15039 ASH 2644 CLT. CEILING EMERGENCY FLOOD LIGHT ROW 12 INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2007050200040 20070502 00040 EA 2007 5 2 MASA200700018 1 20070106 A 3350 20131A BATTERY CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 913FJ 12161 15013 ASH 2639 CLT. LEFT AND RIGHT LOWER EMERGENCY EXIT ROW SIGNS INOP. MX REMOVED AND REPLACED NR 3 AND NR 4 EMERGENCY LIGH T BATTERIES AND POWER SUPPLIES. 2 L 7 2 4F RT A21EA 2007050200041 20070502 00041 EA 2007 5 2 MASA200700019 1 20070106 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 956LR 15056 ASH 2990 ELP. CABIN CEILING LEVEL EMERGENCY FLOOD LIGHT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2007050200081 20070502 00081 EA 2007 5 2 MASA200700146 1 20070315 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 76996 7357 ASH 7159 IAD. REPORTED ONE CEILING FLOOD LIGHT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2007050200083 20070502 00083 EA 2007 5 2 MASA200700154 1 20070321 A 3350 CHARGER CNDAIR CL600 CL6002B19 1900309 EA CABIN FAULTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 649BR 7414 ASH 7304 ORD. EMERGENCY LIGHTS WILL NOT TURN OFF. MX REMOVED AND REPLACED NR 4 CHARGER, OP CHECK GOOD. 2 L 7 2 4F RT A21EA 2007050200092 20070502 00092 EA 2007 5 2 TRAX200700555 1 20070422 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 930EV 8014 CAPTAIN'S FLASHLIGHT BULB INOP. 2 L 7 2 4F RT A21EA 2007050200097 20070502 00097 EA 2007 5 2 TRAX200700563 1 20070424 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 750EV 10161 LEFT STA 280 WEB CORRODED OUT OF LIMITS. 2 L 7 2 4F RT A21EA 2007050200100 20070502 00100 EA 2007 5 2 TRAX200700568 1 20070424 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 858AS 7417 FLOOR EMERGENCY LIGHTS AFT OF OVERWING EXIT ARE INOP. FLT 4722 DEL 165 MINS. 2 L 7 2 4F RT A21EA 2007050200102 20070502 00102 EA 2007 5 2 TRAX200700571 1 20070425 A 3397 WIRE CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS DAMAGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 748EV 10158 1ST CEILING LEVEL EMERGENCY FLOODLIGHTS OUT. CABIN EMERGENCY LIGHTS - CEILING LEVEL FLOODLIGHTS) [SUP 05-09-07] REPIN NED WIRE AT 1ST CEILING EMERGENCY LIGHT . OPS CKED GOOD 2 L 7 2 4F RT A21EA 2007050300009 20070503 00009 EA 2007 5 3 MASA200700083 1 20070207 A 3350 1317 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 932LR 15032 ASH 2630 CLT. THE 7TH EMERGENCY CEILING FLOOD LIGHT INOP. MX RELAMPED FLOOD LIGHT. 2 L 7 2 4F RT A21EA 2007050300014 20070503 00014 EA 2007 5 3 MASA200700094 1 20070211 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN CONTAMINATED A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 77278 7278 ASH 2923 PHX. ONE FLOOR LEVEL EMERGENCY EXIT LIGHT INOP. MX CLEANED DEBRIS, DRIED MOISTURE ON CANNON PLUG. 2 L 7 2 4F RT A21EA 2007050300015 20070503 00015 EA 2007 5 3 MASA200700103 1 20070216 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 77278 7278 ASH 2748 PHX. EMERGENCY EXIT LIGHT AT SERVICE DOOR INOP. MAINTENANCE RELAMPED THE LIGHT, OPS NORMAL. 2 L 7 2 4F RT A21EA 2007050300016 20070503 00016 EA 2007 5 3 MASA200700105 1 20070219 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 571ML 7209 ASH 7299 ORD. ALL FLOOR LEVEL EXIT LIGHTS INOP. MX REMOVED AND REPLACED THE POWER STRIPS, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007050300024 20070503 00024 EA 2007 5 3 MASA200700121 1 20070226 A 3350 1317 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 938LR 15038 ASH 2660 CLT. CEILING EMERGENCY FLOOD LIGHT INOP. MX RELAMPED FLOOD LIGHT. 2 L 7 2 4F RT A21EA 2007050300027 20070503 00027 EA 2007 5 3 MASA200700128 1 20070228 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 591ML 7388 ASH 7285 PWM. LT FWD OVERWING EXTERIOR EMERGENCY LIGHT INOP. MX RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2007050300053 20070503 00053 NM 2007 5 3 UPS07M49676 1 20070318 A 5410 FAIRING DOUG MD11 MD11F 3023600 NM NR 2 INTAKE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C ENGINE NR 2 AIR INTAKE DUCT FAIRING NR 364DR EXTERIOR FACE FOUND DENTED AS MARKED (14 AREAS). DENT ME ASURED FOUND OUT OF LIMIT PER SRM 51-71-00 VOL IIR38, DEPTH 0.068" WIDTH 1". 06 EA DENTS TRIMMED OUT PER SRM 51-71-00VOL IIR38. HFEC C/OUT PER DAC NDTSPM REV13 06-10-01.001 NO CRACK EVIDENT. REPAIR FILLERS FAB PER SRM 51-71-0016B VOL IIR38 MATL 2024T3-0.016". FAIRING NR 364DR C/OUT BO BONDING OF FILLER AND DOUBLERS TO PNL PER SRM 51-71-00 VOL IIR38. 2 L 7 3 4F RT A22WE 2007050300055 20070503 00055 WP 2007 5 3 070107 1 20070423 A 3350 362624 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 865GA 49998 DURING A SERVICE CHECK MAINTENANCE DEPARTMENT PERSONNEL IN LAS VEGAS REPORTED THAT EMERGENCY FLOOR PATH LIGHTING WAS INO P AND MISSING SEGMENTS. LAS VEGAS MAINTENANCE REPLACED AND SECURED EMERGENCY FLOOR PATH LIGHTING. A SATISFACTORY OPERA TIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007050300062 20070503 00062 NM 2007 5 3 CALA0700205 1 20070425 A 5311 6546551 FRAME BOEING 737 7373T0 1384582 NM BS 807 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 FOUND CRACKED FRAME AT STA 807, STR 9LT. REPAIRED IAW ECRA 5310-04626. 2 L 7 2 4F RT A16WE 2007050300063 20070503 00063 NM 2007 5 3 CALA0700206 1 20070425 A 5311 6546552 FRAME BOEING 737 7373T0 1384582 NM BS 827 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 FOUND CRACKED FRAME AT STA 827 STR 9LT. REPAIRED IAW ECRA 5310-04622. 2 L 7 2 4F RT A16WE 2007050300096 20070503 00096 NM 2007 5 3 NWAA071635655 1 20070425 A 3350 LAMP BOEING 757 757251 1384970 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 555NW 33391 DURING LINE CHECK, FOUND EMERGENCY SLIDE LIGHT AT DOOR 4 LEFT INOPERATIVE. RELAMPED LIGHT, NO HELP. REMOVED AND REPLAC ED AFT LEFT HAND POWER SUPPLY (P/N: BPS7-3). LIGHT OPS CHECKS GOOD. 2 L 7 2 4F RT A2NM 2007050300100 20070503 00100 NM 2007 5 3 DL757070379 1 20070427 A 3260 ROLLER BOEING 757 757232 1384965 NM MLG DOOR SWITCH DAMAGED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 624DL 22914 AFTER TAKEOFF WHEN GEAR WAS RETRACTED DOOR LIGHT REMAINED ON WITH ASSOC EICAS GEAR MESSAGE. RTN TO CVG WITH UNEVENTFUL LANDING. FLT CREW REPORTED FLT ATTENDANT NOTED NOISE AT FWD NOSE OF ACFT. T/S IAW MM AND FOUND NOSE DOORS WOULD NOT CL OSE WITH GRD SW. FOUND ROLLER ON S10362 FLAT SPOTTED. REPLACED SAME. JACKED AND CYCLED NOSE GEAR. OPS CKS GOOD. 2 L 7 2 4F RT A2NM 2007050300101 20070503 00101 NM 2007 5 3 SWAA072133 1 20070501 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050300104 20070503 00104 2007 5 3 DL757070380 4 20070427 A 2330 UNKNOWN BOEING 757 757232 1384965 NM ENTERTAIN SYS ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 608DA 22815 A SLIGHT ELECTRICAL ODOR WAS DETECTED AROUND ROW 39DEF. PAX WERE REMOVED WHILE ODOR WAS THROUGHLY INVESTIGATED, ODOR DI SSIPATED WHEN ENTERTAINMENT SYS SHUTDOWN, THIS OCCURRED DURING FLIGHT 1418 FROM SLC TO EWR.. OPERATED SYSTEM, NO ELECTR ICAL ODOR NOTED. ALL IFE CHKS GOOD 39 DEF. REMOVED MCO AND PLACARDS. 2 L 7 2 4F RT A2NM 2007050300113 20070503 00113 NM 2007 5 3 DL738070387 1 20070105 A 3350 B21506 BATTERY BOEING 737 737832 13844CF NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 395DN 30773 716521 AFT EMERGENCY PATH LIGHT INOP. REPLACED POWER PACK FUSE, OPS CHK OK. 2 L 7 2 4F 4 F RT A16WE E17NE 2007050300119 20070503 00119 NM 2007 5 3 NWAA071595501 1 20070413 A 5414 SKIN PANEL BOEING 757 757251 1384970 NM NR 2 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 501US 23190 DURING "M" CHECK, FOUND CRACK IN 2 PYLON RT SKIN PANEL LIGHTING HOLE AT NAC STA 133. REPAIRED PER EA 55-208817. 2 L 7 2 4F RT A2NM 2007050300120 20070503 00120 EA 2007 5 3 REXA200700052 1 20070421 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA RIGHT SMOKE A REXA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 25 8944B 3675 7944 CREW REPORT SMOKE IN COCKPIT ON CLIMB OUT. QRH FOLLOWED PERFORMED AIR RETURN TO TUL. MAINTENANCE INSPECTED AIRCRAFT AN D DEFERRED RIGHT ACM (AIR CYCLE MACHINE) PER MEL 21-51-01. 2 L 7 2 4F RT A21EA 2007050300121 20070503 00121 NM 2007 5 3 DU4R2007110 1 20070425 A 5330 SKIN BOEING 757 757232 1384965 NM BS 560-580 DAMAGED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 637DL 23760 FOUND 2 LIGHTNING STRIKES BETWEEN BS 560 - BS 580 AND S-2R S-3R. REPAIRED BY CUTTING OUT LIGHTNING STRIKE AREA. HFEC C UT OUT IAW D6-34N301-6-51-00-19, NO RELEVANT INDICATIONS NOTED. FABRICATED AND INSTALLED REPAIR DOUBLER 10-3/8 BY 10-3/ 8 FROM 2024-T3 .063 IAW B757 SRM 53-00-01 FIG 201 PG 201 REPAIR (2). 2 L 7 2 4F RT A2NM 2007050300149 20070503 00149 NM 2007 5 3 SWAA072145 1 20070501 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050300150 20070503 00150 NM 2007 5 3 HALA0700190 1 20070422 A 5330 SKIN BOEING 767 767332 1382001 NM BS 332 S23-24L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 FUSELAGE SKIN BS 322, BETWEEN STR 23L AND STR 24L HAS LIGHTNING STRIKE. LISGHTNING STRIKE OF FUSELAGE SKIN BS 332 BETWE EN STR 23 AND 24 LH WAS REPAIRED PER HAL M105 597053. 2 L 7 2 4F RT A1NM 2007050300152 20070503 00152 NM 2007 5 3 SWAA072160 1 20070501 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 5L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050300153 20070503 00153 NM 2007 5 3 HALA0700201 1 20070426 A 5753 SKIN BOEING 767 767332 1382001 NM RT WING TE FLAP DENTED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 591HA 33423 RIGHT WING INBOARD AFT FLAP LOWER SURFACE HAS GRAVEL DAMAGE 38 INCHES INBOARD OF OUTBOARD FAIRING 15 INCHES FORWARD OF T RAILING EDGE. REPAIRED PER STRM 51-70-01-06-0. 2 L 7 2 4F RT A1NM 2007050300154 20070503 00154 NM 2007 5 3 HALA0700183 1 20070422 A 5330 SKIN BOEING 767 767332 1382001 NM BS 273 S29-30R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 FUSELAGE SKIN RIGHT BS 273, BETWEEN STR 29 AND STR 30 HAS LIGHTNING STRIKE. LIGHTNING STRIKE REPAIRED PER HAL M105 5970 53. 2 L 7 2 4F RT A1NM 2007050300159 20070503 00159 NM 2007 5 3 HALA0700200 1 20070426 A 5753 SKIN BOEING 767 767332 1382001 NM RT WING TE FLAP DENTED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 591HA 33423 RIGHT WING INBOARD AFT FLAP LOWER SURFACE HAS RAVEL DAMAGE INBOARD END TO 74 INCHES OUTBOARD,TRAILING EDGE FORWARD 16 IN CHES. REPAIRED PER 767 SRM 51-70-01-06-0. 2 L 7 2 4F RT A1NM 2007050300169 20070503 00169 NM 2007 5 3 HALA0700187 1 20070422 A 5330 SKIN BOEING 767 767332 1382001 NM BS 266-276 DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 LIGHTNING STRIKES, BS 266 TO BS 276 BETWEEN STR 27L AND 30L. REPAIRED PER HAL M105 597053. 2 L 7 2 4F RT A1NM 2007050300174 20070503 00174 NM 2007 5 3 HALA0700180 1 20070422 A 5330 SKIN BOEING 767 767332 1382001 NM BS 246 S32R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 FUSELAGE SKIN RT BS 246, STR 32 HAS LIGHTNING DAMAGE. REPAIRED DAMAGED FUSELAGE SKIN AT BS 246, STR 32R IAW ER 06-3352 SECTION 11 AND SRM 53-00-01-2R-1 FIG 201 2 L 7 2 4F RT A1NM 2007050300181 20070503 00181 NM 2007 5 3 HALA0700184 1 20070422 A 5330 SKIN BOEING 767 767332 1382001 NM BS 276 S26L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 FUSELAGE SKIN LT BS 276, STR 26 HAS LIGHTNING DAMGE AT FASTENER. REMOVED AND REPLACED FASTENER ON FUSELAGE SKIN AT BS 2 76 STR 26R PER SRM 53-00-01 FIG 201 SECTION II AND HAL M105 597053. 2 L 7 2 4F RT A1NM 2007050300185 20070503 00185 EA 2007 5 3 604ME41507 1 20070415 A 7732 6015091013 SIGNAL COND UNIT CNDAIR CL600 CL6002B16 1900305 EA FAILED E WWQA O OTHER J WARNING INDICATION CL CLIMB 1 WP 07 604ME 5120 5112 SIGNAL CONDITIONER FAILED. 2 L 7 2 4F RT A21EA 2007050300186 20070503 00186 WP 2007 5 3 AALA20070678 1 20070228 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9619V 53566 TUL- EMERGENCY LIGHTS AT CABIN OVERWING EXITS INOPERATIVE. REPLACED BATTERY PACK AT STATION 875 FOR EMERGENCY LIGHTS AT CABIN OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007050300193 20070503 00193 NM 2007 5 3 SWAA072111 1 20070430 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 FUSELAGE SKIN CRACKED AT BS 514C, STR 8R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007050300194 20070503 00194 NM 2007 5 3 SWAA072120 1 20070430 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505C, STR 14L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007050300196 20070503 00196 WP 2007 5 3 AALA20070687 1 20070414 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7518A 49895 MSP - CEILING EMERGENCY LIGHTS AT SEAT ROWS 25 AND 26 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT SEAT ROWS 25 AND 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007050300202 20070503 00202 WP 2007 5 3 AALA20070685 1 20070414 A 3350 OL714BPE BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7518A 49895 MSP - EMERGENCY LIGHT AT SEAT ROW 22 MISSING LAMP. RELAMPED EMERGENCY LIGHT AT SEAT ROW 22. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F A6WE 2007050300209 20070503 00209 NM 2007 5 3 SWAA072119 1 20070430 A 2560 PH22300L GLOWSTRIP BOEING 737 7373A4 1384585 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED SPV CHECK, FOUND EEPLS PHOTO LUMINESCENT STRIP WORN AT ROW 23 ABC. R&R STRIP PER MM. 2 L 7 2 4F RT A16WE 2007050300219 20070503 00219 NM 2007 5 3 SWAA072147 1 20070501 A 5312 6517582 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE BULKHEAD WEB CRACKED AT BS 178, RBL 10.5 TO RBL 12, WL 218. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007050300228 20070503 00228 NM 2007 5 3 AALA20070680 1 20070413 A 3350 CM1317 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 675AN 29425 BOS - EMERGENCY LIGHTS AT LEFT ROW 20 INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT LEFT ROW 20. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A2NM 2007050300229 20070503 00229 EU 2007 5 3 F3LA200700093 1 20070424 A 5320 SILL AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 801FR 4759 1939 DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR SILL THRESHOLD HAD CORROSION AROUND SEVERAL NUTPLATE HOLES. REPLACED L2 D OOR SILL IAW SRM 51-42-11, FIG 6 AND 7. 2 L 7 2 4F RT 2007050300243 20070503 00243 NM 2007 5 3 ZZDA070423155 1 20070423 A 5311 ANGLE BOEING 717 717200 1383700 NM FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 969AT 55030 AFT ACCESSORY COMPARTMENT FS 1178 CANTED FRAME ANGLE CRACKED NEAR LONGERON 15R. INSTALLED ANGLE FOR REPAIR 1 ZIDE OF AN GLE 11 1/2 X 2 1/2 IAW B717 SRM 51-70-11. 2 L 7 2 4F TR A6WE 2007050300248 20070503 00248 NM 2007 5 3 2007UALA01244 1 20070421 A 3250 SENSOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE MLG STEERING MALFUNCTIONED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 816UA 871 NW STEERING FAULT DISPLAYED ON UPPER ECAM SCREEN WHILE ENROUTE. NEEDED TOW TO GATE. ON SUBSEQUENT FLIGHT HAD LOW LEVEL GREEN HYD INDICATION. TOW TO GATE ALSO NEEDED. [06-22-07] FAULT TRACING FOUND A WANDERING SIGNAL VOLTAGE FROM 4GC NOSE WHEEL STEERING FEEDBACK SENSOR. REPLACED FAULTY FEEDBACK SENSOR AND REPLACED 6GC NOSE WHEEL STEERING SERVO AS A PRE CAUTION. 2 L 7 2 4F 4 F RT A28NM E40NE 2007050300252 20070503 00252 NM 2007 5 3 2007UALA01247 1 20070421 A 5310 DOOR FRAME BOEING 737 737522 138449F NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 906UA 25006 FWD CARGO DOOR CUT OUT AFT FRAME IS CRACKED IN TWO PLACES. FIRST CRACK IS ON AFT SIDE OF FRAME IN RADIUS ADJACENT TO IB UPPER CORNER OF LOWER STOP FITTING, SECOND CRACK IS ON FWD SIDE OF FRAME JUST BELOW UPPER CORNER IB CORNER OF LOWER STOP FITTING. [SUP 05-04-07] MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKS. ACCOMPLISHED NESTED ANGLE REPAIR. 2 L 7 2 4F RT A16WE 2007050300265 20070503 00265 NM 2007 5 3 2007UALA01259 1 20070419 A 2720 PCU BOEING 777 777222 1385219 NM RUDDER LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 222UA 30553 ARRIVAL CHECK FOUND RUDDER UPPER POWER CONTROL PACKAGE HYD HEAVY LEAK. [SUP 05-18-07] REPLACED UPPER RUDDER POWER CONT ROL UNIT. REF MM 27-21-11 P401. COMPLETED OPERATIONAL CHK AND LEAK CHECK . BOTH CHECKED OK. 2 L 7 2 4F RT T0001SE 2007050300275 20070503 00275 SO 2007 5 3 SIMA200712013 1 20070428 A 2810 2770138101 FLAPPER VALVE EMB 145 EMB145LR 3260212 SO ZONE 500 FAILED A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 615AE 18765 145087 FUEL LEAKING FROM LEFT WING, RETURNED TO DFW. REMOVED AND REPLACED FUEL FLAPPER VALVE IAW EMB AMM 28-11-04. OPERATIONA L CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050300279 20070503 00279 NM 2007 5 3 2007UALA01269 1 20070424 A 5415 LUG BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 1 PYLON CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 178UA 24385 BORE CORRODED AND SCRATCHED - NR 1 PYLON UNDER WING FITTING BEARING LUG, BOTH SIDES. [SUP 05-16-07] BORE CORRODED AND SCRATCHED - NR 1 PYLON UNDER WING FITTING BEARING LUG, BOTH SIDES. ACCOMPLISHED BORING THE DSB UNDER WING FITTINGS PER C OA 899993040 & SB 747-54A2218. FINAL HOLE DIA AFTER HONE: INBD=2.2446" OUTBTD=2.2447". CORROSION & VIBRATION AGGRAVATED BY HIGH TEMP CAUSED DUAL SIDE BRACE HOLE SURFACE DETERIORATION. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050300290 20070503 00290 NM 2007 5 3 DL76S070352 1 20070420 A 5330 146T35112 SKIN BOEING 767 767332 1382001 NM FS 1269 S31R GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 138DL 25409 THE FUSELAGE SKIN WAS GOUGED FORWARD OF THE C2 DOOR OPENING AT STA 1269, S31R. GOUGE AFTER BLENDING WAS 1 BY 0.8 IN. T HE DAMAGED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED. 2 L 7 2 4F RT A1NM 2007050300291 20070503 00291 NM 2007 5 3 DLM88070353 1 20070315 A 5230 PAN DOUG MD88 MD88 3023688 NM CARGO DOOR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 905DL DL22 49536 SPARE CARGO DOOR. SDR REQUIRED FOR SRM 52-05D FIG 050. CRACK ON INNER PAN UNDER NR 3 STOP ON FORWARD SIDE OF DOOR. IN STALLED DOUBLER PER SRM 52-05 D FIG 50. 2 L 7 2 4F RT A6WE 2007050300313 20070503 00313 NM 2007 5 3 UPS07549712 1 20070403 A 5311 146N103078 FRAME BOEING 757 75724APF 1384969 NM BS 1500 S26R DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 414UP 23854 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1500, 526R. ACCOMPLISHED ON EA 757-5362-27-A1648 AND UPS NR B757 -5310-26691-A. 2 L 7 2 4F RT A2NM 2007050300324 20070503 00324 NM 2007 5 3 UPS07M49710 1 20070315 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1921-2007 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C AFT CABIN, RHS CURVED SEAT TRACK I/B AND O/B FLANGE UPPER AND LOWER SURFACE FOUND CORROSION FROM STA 1 921 - STA 2007. (-107.5"). CORROSION REMOVED PER SRM 51-21-01 VOLIIR38 ORI THK 0.080" MATL REMOVED 0.030" MAT`L REMAIN 0.050" FOUND OUT OF LIMIT PER SRM 53-70-00 FIG3 VOLIR38. SEATTRACK REMOVED PER SRM 51-31-01 VOLIIR38. RWK PER SRM 53-7 0-00 FIG1VOLIIR38. NEW SEATTRACK HOLES PICKUP AND PROTECTED PER SRM51-31-01 AND 51-21-01 VOLIIR38. NEW SEATTRACK INSTA LLED PER SRM 51-31-01 VOLIIR38. 2 L 7 3 4F RT A22WE 2007050300325 20070503 00325 EU 2007 5 3 2007UALA01289 1 20070424 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU EXIT SIGN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 409UA 462 2 RT DOOR UPPER EMERGENCY EXIT SIGN HAS 5 INOP LAMPS. [SUP 05-16-07] REPLACED LAMP. 2 L 7 2 4F RT A28NM 2007050300338 20070503 00338 NM 2007 5 3 2007UALA01296 1 20070426 A 3350 POWER SUPPLY BOEING 737 737322 1384676 NM CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 302UA 23643 RT OVERWING SIDEWALL EMERGENCY LIGHT OUT. BAD INVERTER, SWAPPED WITH LT TO CONFIRM. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A16WE 2007050300345 20070503 00345 NM 2007 5 3 DHL2007782509 1 20070430 A 5311 FRAME BOEING 727 727227 1384078 NM BS 360 S26-27R CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 782DH 21998 FUSELAGE LOWER LOBE, BS 360 FRAME, BETWEEN STR 26R AND 27R, HAS EXFOLIATION CORROSION ON FWD SIDE. CUT OUT DAMAGED AREA 5" BY 1.5", FABRICATED 2 FILLERS FROM 7075-T6, .071" BY 5" BY 1.5", PO NR 9004150; DOUBLER FROM 7075-T6, .071" BY 7" BY 4.5", PO NR 9004150, PER B727 SRM 53-10-2 FIG 1 AND 53-10-4 FIG 14. TREATED, PRIMED, AND INSTALLED REPAIR PARTS PER B7 27 SRM 51-10-2 AND 53-10-4 FIG 14. 2 L 7 3 4F A3WE 2007050300347 20070503 00347 NM 2007 5 3 DHL2007782515 1 20070502 A 5330 SKIN BOEING 727 727227 1384078 NM BS 254 S10L CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 782DH 21998 EXT FUSELAGE BS 254 AT STR 10L HAS EDGE CRACKED TO FASTENER HOLE. CUT OUT DAMAGED SKIN, 1.5" 1", PER B727 SRM 53-30-3 FIG 29. FABRICATED FILLER FROM 2024-T3, .063" BY 1.5" BY 1", PO NR 9004670; AND DOUBLER FROM 2024-T3, .080" BY 14.5" BY 12.75", PO NR 7177117; TREATED, PRIMED, AND INSTALLED REPAIR PARTS PER B727 SRM 51-10-2 AND 53-30-3 FIG 29. CAT "A" R EPAIR. 2 L 7 3 4F A3WE 2007050300348 20070503 00348 NM 2007 5 3 DHL2007788506 1 20070421 A 5753 6521631261 SKIN BOEING 727 727214 138407R NM LT WING FOREFLAP GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 LEFT W/S 464, OUTBD FOREFLAP, INBD L/E AT PREVIOUS REPAIR DOUBLER GOUGED. REMOVED GOUGED DOUBLER IAW B727 SRM 51-30-2. FABRICATED REPAIR DOUBLER 5" BY 6" BY .063 FROM 2024T3 AND FILLER 2.20" BY 1.90" BY .063 FROM 2024T3 IAW B727 SRM 57-50 -4, FIG 4. TREATED AND INSTALLED REPAIR IAW B727 SRM 51-10-2 AND 57-50-4, FIG 4. 2 L 7 3 4F A3WE 2007050300354 20070503 00354 NM 2007 5 3 DHL2007788508 1 20070424 A 5347 BAC1520792 SEAT TRACK BOEING 727 727214 138407R NM BS 690-740 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 MAIN CARGO DECK, SEAT TRACK LBL 45L, AT 750F, SURFACE CORROSION. REMOVED SEAT TRACK BS 690 TO 740 IAW B727 SRM 51-30-2. FABRICATED TWO NEW SEAT TRACKS FROM BAC 1520-792-7178T6511, 7'.8" LONG AND 6'.8" LONG AND TWO ANGLES FROM BAC 1503-100 122-7178T6311, 1'.2" BY 2.5" AND 1'.25" BY 2.50" IAW B727 SRM 53-10-5, FIG 1 AND 53-10-2 FIG 7. TREATED PRIMED AND INST ALLED SEAT TRACK IAW B727 SRM 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 2007050300355 20070503 00355 NM 2007 5 3 UPS07549711 1 20070403 A 5311 146N103071 FRAME BOEING 757 75724APF 1384969 NM BS 1520 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 414UP 23854 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1520. ACCOMPLISHED ON FINAL EA NR 757-5362-27-A1646 AND UPS NR B 757-5310-26672-A. 2 L 7 2 4F RT A2NM 2007050300362 20070503 00362 NM 2007 5 3 2007UALA01299 1 20070425 A 5230 TEE FITTING BOEING 737 737322 1384676 NM AFT CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 AFT CARGO DOOR LOWER "T" CHORD CRACKED AT LOWER AFT CORNER. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED LOWER "T" CH ORD ASSY. 2 L 7 2 4F RT A16WE 2007050300364 20070503 00364 WP 2007 5 3 UPS07849720 1 20070424 A 5712 RIB DOUG DC8 DC873F 302199F WP LWS 798 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 C3 LT WING OB LE RIB CRACKED AT XFS 798. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2. REPAIR ANGLES IAW SRM 57-07- 00, 57-02-00, 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2007050300372 20070503 00372 NM 2007 5 3 2007UALA01305 1 20070425 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 AFT PIT STA 1540 LT AT STR 25L, FRAME IS DENTED ON INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT DAMAGE. INS URANCE CUT & INSTALLED "J" ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050300373 20070503 00373 NM 2007 5 3 2007UALA01306 1 20070425 A 2930 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE HYDRAULIC SYS ACTIVATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 668UA 30024 "C" HYDRAULIC PRIM 1 WARNING. [SUP 05-18-07] CYCLED PUMP CIRCUIT BREAKER. HYD PRESS AND INDICATIONS RESTORED. OPERATED PUMP THROUGH SEVERAL CYCLES AND NO PROBLEMS NOTED. UNABLE TO DUPLICATE WARNING INDICATIONS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050300376 20070503 00376 NM 2007 5 3 2007UALA01309 1 20070425 A 3510 OXYGEN SYSTEM BOEING 737 737322 1384676 NM CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 CREW O2 READING 1400 PSI. [SUP 05-16-07] SERVICED TO FULL. 2 L 7 2 4F RT A16WE 2007050300377 20070503 00377 2007 5 3 2007UALA01310 4 20070424 A 2565 527S0035 GAUGE AIRCRUISERS D31516121 AIRBUS 320 A320232 3930326 EU EVAC SLIDE DAMAGED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 476UA A8841 1508 LOW PRESSURE READING ON GAUGE. LEAK AROUND PRESSURE GAUGE THREADS. REMOVED PRESSURE GAUGE AND FOUND STRIPPED THREADS O N GAUGE AND GAUGE ADAPTOR. REPLACED GAUGE AND ADAPTOR, RECHECKED FOR LEAKS. CHECKS OK. TECHNICIAN LEFT AND NEW TECHNI CIAN HAS BEEN GIVEN TRAINING ON THE PROPER INSERTION AND THREADING OF GAUGE INTO VALVE THREADS. 2 L 7 2 4F RT A28NM 2007050300380 20070503 00380 NM 2007 5 3 2007UALA01313 1 20070426 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 FUSELAGE CUT-OUT AT FWD PIT DOOR AFT FRAME AFT SIDE IS CRACKED IN RADIUS JUST INBOARD OF LWR STOP FITTING UPPER END. [S UP 05-16-07] MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. INSTALLED NESTED ANGLE REPAIR. 2 L 7 2 4F RT A16WE 2007050300381 20070503 00381 NM 2007 5 3 2007UALA01314 1 20070426 A 5330 SKIN BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 BS 380 AT BL 0 LOWER FUSELAGE SKIN CRACKED AT EXHAUST DUCT FOR EQUIPMENT COOLING. CRACKED AT AFT END OF CUT-OUT. [SUP 05-16-07] MAJOR REPAIR: ACCOMPLISHED COA930011. 2 L 7 2 4F RT A16WE 2007050300385 20070503 00385 NM 2007 5 3 2007UALA01318 1 20070426 A 5414 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 NR 2 ENG PYLON PNL CUT OUT CRACKED AT UPR FWD CORNER LOCATED ON I-B PYLON SKIN ACCESS HOLE CUT OUT JUST FWD OF HYD BAY. MAJOR REPAIR ACCOMPLISHED: STOP DRILLED CRACK. FABRICATED & INSTALLED DOUBLER REPAIRS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050300386 20070503 00386 2007 5 3 2007UALA01319 4 20070426 A 2565 CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE DISENGAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 LT AFT MED SLIDE RELEASE CABLE DISENGAGED. [SUP 05-18-07] RE-ENGAGED SLIDE RELEASE CABLE PER MM 25-66-00. READY FOR SE RVICE. SLIDE PROBLEM ROOT CAUSE: SUSPECT CABLE DISENGAGED BY CONTACT WITH CABIN SERVICE EQUIPMENT DURING LOADING/UNLOAD ING. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050300387 20070503 00387 NM 2007 5 3 2007UALA01320 1 20070425 A 3320 LAMP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE LAV LIGHT INOPERATIVE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 670UA 29240 LAVS SYSTEM 2 LIGHTS CB POPPED AGAIN. REPEAT GRIPE. FOUND PROBLEM ISOLATED TO AFT CABIN LAVS. CK'D ALL DR SWITCHES AND HANDICAPPED LIGHT SWITCH. ALL CHECKED GOOD. FOUND "OCCUPIED" SIDE OF LAV OCCUPIED SIGN LIGHT BULBS SHORTED. RELAMPED, C KS GOOD. OK FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050300390 20070503 00390 NM 2007 5 3 ASAA0741621 1 20070502 A 5523 65C257979 SKIN BOEING 737 7374Q8 138447Q NM ELEVATOR TAB DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 776AS 25109 LT ELEV TAB UPPER SURFACE T E IS SPLIT 51" FROM I B END. PREPPED THE TAB UPPER SKIN SURFACE FOR BONDING CUT AND APPLIED REPAIR PLIES IAW SRM 51 70 05 PAPR 3. 2 L 7 2 4F RT A16WE 2007050400002 20070504 00002 NM 2007 5 4 ASAA0741622 1 20070502 A 5753 6546430517 SKIN BOEING 737 7374Q8 138447Q NM T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 776AS 25109 LT IB FOR FLAP DENTED OUT OF LIMITS NEAR CENTER TRACK. REMOVED THE DAMAGED AREA OF LOWER SKIN FABRICATED AND INSTALLED A SKIN FILLER AND REPAIR DOUBLER IAW SRM 51 70 10 PARA 8 11 15 18 AND 20. 2 L 7 2 4F RT A16WE 2007050400004 20070504 00004 EU 2007 5 4 07FDEA01680 1 20070501 A 5315 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU FUSELAGE BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 679FE 793 AFT CARGO PIT, CABIN FLOORBEAM LOWER FLANGE BENT, FR60, STA X3991, BL - Y1750 TO 2050. REPAIRED LOWER FLANGE ON FLOORBE AM FR60, STA X3991, BL - Y1750-2050 IAW FED EX EA 6-5310-109141. 2 L 7 2 4F RT A35EU 2007050400007 20070504 00007 NM 2007 5 4 ASAA0741626 1 20070502 A 5754 65C2679413 SKIN BOEING 737 7374Q8 138447Q NM L/E SLAT CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 776AS 25109 NR 2 SLAT SKIN LWR LIP IS CRACKED AROUND FASTENER HOLES JUST BELOW THE O B AUX TRACK. CUT OUT THE DAMAGED AREA OF SKIN FABRICATED AND INSTALLED A SKIN FILLER AND EXTERNAL SPLICE PLATE IAW SRM 57 40 01 FIG 206 REPAIR 6. 2 L 7 2 4F RT A16WE 2007050400009 20070504 00009 NM 2007 5 4 ASAA0741628 1 20070502 A 5753 SKIN BOEING 737 7374Q8 138447Q NM T/E FLAP PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 776AS 25109 THE IB FORE FLAP IS PUNCTURED NEAR THE CENTER TRACK. REMOVED THE DAMAGED AREA OF LWR SKIN FABRICATED AND INSTALLED A SK IN FILLER AND A REPAIR DOUBLER IAW SRM 51 70 10 PARA 8 11 15 18 AND 20. 2 L 7 2 4F RT A16WE 2007050400010 20070504 00010 WP 2007 5 4 07FDEA01681 1 20070502 A 5314 KEELBEAM DOUG DC10 DC1010 3022110 WP BS 1501 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 LT KEEL BEAM WEB AT STA 1501 Z= -40 APPROX FOUND CRACK ON EXISTING REPAIR. REPAIR WEB IAW SRM 53-00-01 FIG 10 VOL 1. 2 L 7 3 4F A22WE 2007050400012 20070504 00012 NM 2007 5 4 ASAA0741629 1 20070502 A 5322 654655819 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 776AS 25109 SHEAR TIE CRACKED. CUT OUT DAMAGED SECTION OF FRAME (SHEAR TIE) FABRICATED AND INSTALLED A REPAIR SHEAR TIE DOUBLER AND RADIUS FILLERS IAW SRM 53 00 07 FIG 201 REPAIR 5. 2 L 7 2 4F RT A16WE 2007050400014 20070504 00014 EU 2007 5 4 MALA070059 1 20070501 A 5320 SEAT TRACK SAAB SF340 340B 7860101 EU BS 294-300 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 SEAT TRACK AT BL0, IS CORRODED OUT OF LIMITS, ON THE CENTER AISLE FLOORBOARD SUPPORT FLANGE, BETWEEN FS 294 AND 300. TH E DAMAGED AREA HAS BEEN REPAIRED IAW MESABA EO NR S53342 REF: EAMS WORK ORDER 216320 TASK 1519. 2 L 7 2 4T RT A52EU 2007050400015 20070504 00015 WP 2007 5 4 ASAA0781619 1 20070426 A 3350 60030451 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 965AS 53079 NUMEROUS EMERGENCY EXIT LIGHT INOPERATIVE IN TAIL COMPARTMENT AREA. REPLACED BATTERIES. 2 L 7 2 4F RT A6WE 2007050400019 20070504 00019 EU 2007 5 4 07FDEA01647 1 20070427 A 5330 A53778669210 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 MISALIGNED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 809FD 449 DURING MANHOLE FITTING REPLACEMENT AT C23-C24 FOUND TWO PILOT HOLES (P49 RT, P54 LT) NOT IN ACCORDANCE WITH THE OLD HOLE S ON EXTERNAL SKINS REPAIR PERFORMED BY BUSHING REPAIR AT P49RH AND P54 LT AND PLUG THE TWO HOLES WITH FASTENER NAS1097A D5 IAW EA 6-5310-99203 AND RAS7006670/2006 ISS A. 2 L 7 2 4F RT A35EU 2007050400020 20070504 00020 NM 2007 5 4 SWAA072172 1 20070502 A 5512 185A1702 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 723SW 27855 DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138.70. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400021 20070504 00021 NM 2007 5 4 07FDEA01648 1 20070427 A 5230 65571411 DOOR BOEING 727 7272S2F 1384O81 NM ZONE 800 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 210FE 22932 FWD CARGO DOOR AT 6'' FROM AFT EDGE AND 11'' FROM FROM BOTTOM EDGE. REPAIR DID NOT CONFORM TO CURRENT SRM 52-00-3, FOUN D DURING AGING A/C INSPECTION REMOVED EXISTING REPAIR ON LOWER SKIN OF FWD CARGO DOOR 6'' FROM AFT AND 11''FROM BOTTOM EDGE. FABRICATED AND INSTALLED DOUBLER REF SRM 52-00-3 FIG 4. 2 L 7 3 4F A3WE 2007050400025 20070504 00025 WP 2007 5 4 070109 1 20070429 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A WX0A O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 WP 19 862GA 49556 AFT CARGO DOOR FRAME WAS STRUCK BY A BAGGAGE BELT LOADER AT THE LOWER DOOR FRAME SILL APPROXIMATELY 8"(STATION 1203) FRO M THE LEFT SIDE, CAUSING SKIN DAMAGE THE SIZE OF A HALF QUARTER. REPAIR TO THE SKIN AS BEEN ACCOMPLISHED IAW ALLEGIANT AIR ERO NR 5305-001. AIRCRAFT HAS BEEN RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007050400027 20070504 00027 NM 2007 5 4 NWAA071646744 1 20070402 A 5322 TENSION TIE BOEING 747 747212F 1384851 NM BS 800 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 644NW 24177 DURING "M" CHECK FOUND CRACKS IN TENSION TIE FORWARD AND AFT CHANNEL FASTENER HOLES AT BS 800 LT AND RT. REPAIRED PER E A 67-208990. 2 L 7 4 4F RT A20WE 2007050400032 20070504 00032 NM 2007 5 4 NWAA071666744 1 20070402 A 5322 TENSION TIE BOEING 747 747212F 1384851 NM BS 900 DEFORMED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 644NW 24177 DURING "M" CHECK, FOUND TENSION TIE FORWARD CHANNEL DEFORMED AT BS 900 RT. REPAIRED PER EA 67-208991. 2 L 7 4 4F RT A20WE 2007050400034 20070504 00034 NM 2007 5 4 NWAA071696744 1 20070406 A 5414 SKIN BOEING 747 747212F 1384851 NM NR 4 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 644NW 24177 DURING "M" CHECK, FOUND CRACKS IN NR 4 PYLON SKIN AND STIFFENER AT NAC STA 218 AND ACCESS PANEL 483CL CUTOUT. REPAIRED PER EA 67-209238. 2 L 7 4 4F RT A20WE 2007050400035 20070504 00035 NM 2007 5 4 NWAA071726310 1 20070501 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY EXIT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670US 24225 DURING LINE CHECK, TEST EMERGENCY POWER DOOR BATTERY ANNUNCIATOR LIGHT WOULD NOT ILLUMINATE AT RT UPPER DECK DOOR. REMO VED AND REPLACED BATTERY PACK PER AMM 52-23-14. 2 L 7 4 4F RT A20WE 2007050400038 20070504 00038 EA 2007 5 4 SWIA200718174 1 20070322 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 925SW 7682 FLOORBEAM IS CRACKED AT RBL11 AND BOTH INBOARD AND OUTBOARD CLIPS ARE CRACKED, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLE, CLIP, FILLER, ANGLE FILLER, SHIM P/N 601R-53-11-1169-1 AND CLIP P/N 601R31113-58 IAW CRJ200 REO 601R-53-11-171, R EV D AND REO 601R-53-11-1169. 2 L 7 2 4F RT A21EA 2007050400039 20070504 00039 EA 2007 5 4 SWIA200718175 1 20070322 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 925SW 7682 FLOORBEAM IS CRACKED AT LBL11, DISCOVERED AT C-CHECK. INSTALLED FILLER ANGLE AND SPLICE ANGLES IAW CRJ200 REO 601R-53-1 1-138. 2 L 7 2 4F RT A21EA 2007050400040 20070504 00040 EA 2007 5 4 SWIA200718176 1 20070322 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 925SW 7682 PAX DOOR FWD WEB CRACKED AT STEPS 3 AND 4, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLES, SHIM AND DOUBLER PER CRJ200 REO 601R-52-11-702 REV A. 2 L 7 2 4F RT A21EA 2007050400049 20070504 00049 EA 2007 5 4 SWIA200718183 1 20070429 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM FAILED A SWIA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 NM 07 866AS 7517 AFTER LANDING, HYDRAULIC PUMP 2B CAUTION MESSAGE APPEARED, FOLLOWED BY HYD 2 LO PRESS MESSAGE. NR 2 HYDRAULIC QUANTITY SHOWS 0 PERCENT. REPLACED NR 2 AC MOTOR PUMP IAW MM 29-11-03. 2 L 7 2 4F RT A21EA 2007050400050 20070504 00050 NM 2007 5 4 SWAA072194 1 20070502 A 5755 654645170A SPOILER BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED MV1 CHECK, FOUND RT WING NR 3 FLIGHT SPOILER CRACKED AT AFT OUTBOARD END. R&R SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007050400051 20070504 00051 NM 2007 5 4 SWAA072209 1 20070502 A 5311 6546526 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400052 20070504 00052 EA 2007 5 4 SWIA200718184 1 20070427 A 5310 STRIKER CNDAIR CL600 CL6002B19 1900309 EA DOOR SEAL DAMAGED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 403SW 7028 FOUND MAIN CABIN DOOR IS SQUEALING VERY LOUDLY. RETURNED TO SLC. REPAIRED DOOR SEAL STRIKER IAW CRJ REO 601R-53-22-033. 2 L 7 2 4F RT A21EA 2007050400054 20070504 00054 SO 2007 5 4 SWIA200718185 1 20070426 A 3350 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 291SW 120318 ONE WHITE FLOOR PROXIMITY EMERGENCY LIGHT AT ROW 5 WILL NOT TEST. RELAMPED THE WHITE EMERGENCY FLOOR LIGHT. 2 L 7 2 4T RT A31SO 2007050400055 20070504 00055 NM 2007 5 4 SWAA072195 1 20070502 A 5311 6546536 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400056 20070504 00056 EA 2007 5 4 SWIA200718186 1 20070427 A 3520 OXYGEN MASK CNDAIR CL600 CL6002B19 1900309 EA LAVATORY UNWANTED DEPLOY A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 449SW 7699 LAVATORY O2 MASK DEPLOYED AFTER TAKE-OFF. RESTOWED O2 MASK IAW AMM 35-11-15. 2 L 7 2 4F RT A21EA 2007050400057 20070504 00057 NM 2007 5 4 DHL2007782511 1 20070501 A 5310 SHEAR ANGLE BOEING 727 727227 1384078 NM BS 328 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 782DH 21998 E/E BAY FWD CRAWLWAY RT SIDE PRESENTS CRACK AND EXFOLIATION CORROSION AT BS 328.0 SHEAR TIE SUPPORT ANGLE BRACKET BETWEE N STR 26R AND 27R. CUT OUT DAMAGED AREA. FABRICATED NEW SHEAR TIE ATTACH ANGLE AND DOUBLER FROM 7075-T6, .050" BY 4.5" BY 2" (SHEAR TIE) AND .050" BY 6" BY 3" (DOUBLER), PO NR 9004843, PER B727 SRM 53-10-4 FIG 13. TREATED, PRIMED, AND IN STALLED REPAIR PARTS PER B727 SRM 51-10-2 AND 53-10-4 FIG 13. 2 L 7 3 4F A3WE 2007050400059 20070504 00059 EA 2007 5 4 SWIA200718187 1 20070427 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 920SW 7660 TWO OVERHEAD EMERGENCY LIGHTS IN CABIN WILL NOT TEST. RELAMPED BOTH OVERHEAD EMERGENCY EXIT LIGHTS. 2 L 7 2 4F RT A21EA 2007050400060 20070504 00060 EA 2007 5 4 SWIA200718188 1 20070430 A 3350 RELAY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT MALFUNCTIONED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 405SW 7029 EMERGENCY LIGHTS ILLUMINATE IMMEDIATELY WHEN ARMED. REPLACED AC ESSENTIAL BUSS SENSE RELAY KIXD PER CRJ MM 24-51-27. 2 L 7 2 4F RT A21EA 2007050400061 20070504 00061 SO 2007 5 4 SWIA200718189 1 20070430 A 2150 A/C PACK EMB 120 EMB120ER 3260203 SO LEFT ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 578SW 120346 LEFT "PACK FAIL" LIGHT ILLUMINATED IN CRUISE ACCOMPANIED BY STRONG BURNING ODOR. OPERATED LEFT PACK ON GROUND FOR APPRO XIMATELY 30 MINUTES. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4T RT A31SO 2007050400062 20070504 00062 EA 2007 5 4 SWIA200718190 1 20070429 A 3350 COVER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGIHT MISSING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 705SK 10145 FOUND EMERGENCY LIGHT COVER IN GALLEY IS MISSING. REPLACED EMERGENCY FLOOD LIGHT LENSE IAW MM 33-51-11. 2 L 7 2 4F RT A21EA 2007050400063 20070504 00063 NM 2007 5 4 KNNA200700030 1 20070428 A 7830 LEVER BOEING UNKNOWN BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE THRUST REVERSER BINDING A KNNA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 WP 25 326DL 55862 200 UNKNOWN 23098 IN FLIGHT DURING DESCENT INTERMITTENTLY AT FIRST THEN STEADY PROCEDURES WERE FOLLOWED WITH THRUST LEVERS BINDING (RESTRI CTED) ENGINE 1 WAS SHUTDOWN IAW CHECK LIST. EMERGENCY DECLARED. THRUST REVERSER WAS TRANSFER TO DMI LOG TROUBLESHOOTIN G IS IN PROCESS. 2 L 7 2 4F 4 F RT A16WE E2EA 2007050400064 20070504 00064 WP 2007 5 4 UPS07849725 1 20070329 A 5340 FITTING DOUG DC8 DC873F 302199F WP FS 1200 RBL 65 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 C-PIT, AT UPPER CORNER OF CROSS SLIDE DOOR CUTOUT, FITTING HAS 4.5" CRACK STA 1200 RBL 65. REMOVED C RACK FITTING AT STA 1200 RBL 65 C-PIT DOOR CUT OUT IAW SRM 51-1-20D. INSTALLED REPLACEMENT FITTING AT STA 1200 RBL 65 C -PIT DOOR CUT OUT IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007050400067 20070504 00067 WP 2007 5 4 UPS07849729 1 20070414 A 5340 ATTACH FITTING DOUG DC8 DC873F 302199F WP FS 756 L13L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 756 L13L. REMOVED END FITTING AT STA 756 L13L IAW SRM 51-1-20D. LOCAT ED, DRILLED UP AND INSTALLED REPLACEMENT FITTING AT STA 756 L13L IAW SRM 51-3-2, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007050300054 20070503 00054 NM 2007 5 3 UPS07M49677 1 20070319 A 5320 STRUCTURE DOUG MD11 MD11F 3023600 NM TAIL CONE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C FWD TAIL CONE: LT RETRACTABLE DOOR EXTERIOR FIN DENT AS MARKED NR 6669. DENT AREA D/Y=2.5"/0.110"=22. 73 FOUND BEYOND LIMIT PER SRM 51-80-01VOLI IR38. AREA TRIMMED PER SRM 52-00-01 VOLIR38. HFEC INSP C/OUT PER DAC NDTS P M REV13 06-10-01.001 NO CRACK EVIDENT. REPAIR DOUBLER AND FILLER FAB MATL 2024T3-0.032" PER SRM 52-00-01 VOLIR38. TREA TED PER SRM 51-21-01 VOLIIR38. PAINTED PER SRM 51-21-01 VOLIIR38. INSTALL PER SRM 51-35-01VOLII REV38. 2 L 7 3 4F RT A22WE 2007050300061 20070503 00061 NM 2007 5 3 CALA0700204 1 20070425 A 5311 6546558 FRAME BOEING 737 7373T0 1384582 NM BS 907 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 FOUND CRACKED FRAME AT STA 907, STR 9 RT. REPAIRED IAW ECRA 5310-04625 2 L 7 2 4F RT A16WE 2007050300066 20070503 00066 EU 2007 5 3 F3LA200700098 1 20070425 A 5531 D5537003100051 RIB AIRBUS A318 A318111 3940019 EU VERTICAL STAB SCRATCHED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 801FR 4759 1939 DURING C-3 CHECK, INSPECTION REPORTED LE OF VERTICAL STAB FIN HAD DEEP SCRATCH MARKS (TOOL MARKS) BETWEEN PANELS NR 322B L AND 322CL ON ATTACHMENT BRACKET WHERE PANEL 322BL ATTACHES. REPLACED RIB FOR VERT STAB LE BETWEEN PANELS 322BL AND 32 2CL IAW SRM 51-42-11 AND AMM 20-21-11. 2 L 7 2 4F RT 2007050300077 20070503 00077 NM 2007 5 3 DL76L070365 1 20070425 A 3800 288235 COMPRESSOR BOEING 767 767332 1382001 NM WATER SYSTEM BURNED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 178DN 25143 A/C 178 ON FLT 154/25 OUT OF JFK RETURNED TO THE GATE WITH STRONG BURNING RUBBER SMELL AROUND AFT GALLEY. JFK MTC FOUND WATER COMPRESSOR BURNED UP. REPLACED WATER COMPRESSOR OPS CK GOOD REMOVED MCO/PLAC. 2 L 7 2 4F RT A1NM 2007050300084 20070503 00084 EA 2007 5 3 TRAX200700581 1 20070427 A 3350 CHARGER CNDAIR CL600 CL6002B19 1900309 EA CABIN DEFECTIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 TROUBLESHOT EMERGENCY LIGHTS FOUND NR 1 BATTERY MOUNT CHARGER UNIT DEFECTIVE. 2 L 7 2 4F RT A21EA 2007050300086 20070503 00086 NM 2007 5 3 DL757070372 1 20070427 A 5330 148N32161 SKIN BOEING 757 757232 1384965 NM BS 1851-1854 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 637DL 23760 DURING CURRENT HMV, CORROSION WAS FOUND ON THE INTERIOR SKIN PANEL JUST BELOW THE S-25L LAP FROM BODY STATION 1851 TO 18 54 LEFT. THE DAMAGE WAS OUTSIDE OF THE SRM LIMITS. THE DAMAGE WAS TRIMMED OUT AND A BOEING APPROVED REPAIR WAS INSTALL ED PER 460838-14. 2 L 7 2 4F RT A2NM 2007050300089 20070503 00089 EA 2007 5 3 TRAX200700575 1 20070426 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA K NONE J WARNING INDICATION CR CRUISE 1 SO 27 903EV 7621 LEFT WINDSHIELD SHATTERED. EMERGENCY DECLARED. FLTS 4213, 4214 CX. 2 L 7 2 4F RT A21EA 2007050300093 20070503 00093 NM 2007 5 3 DL76L070377 1 20070417 A 5320 FLOOR SUPPORT BOEING 767 767332 1382001 NM FS 933-1087 WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 183DN 27110 FOUND DURING HMV AT GSO, MAIN CABIN RT SIDE AT STA 933-1087 RBL 33 FLOOR SUPPORT T CAP AND LONGITUDINAL SUPPORT HOLE ELO NGATED FASTENER HOLES/ CHAFING AROUND FASTENERS. REMOVED FLOOR SUPPORT FROM STA 999-1087 RBL 33 IAW B767 - 300 SRM 51-4 0-02. FAB`D AND INSTALLED REPAIR STRAPS IAW B767 SRM 53-00-51 FIG 201 REPAIR 4 AND B767 SRM 51-40-01. FAB'D AND INSTAL LED FLOOR SUPPORT AND REPAIR ANGLES IAW B767 SRM 51-70-12 AND 51-40-02. WORKED ON N/R 24143. 2 L 7 2 4F RT A1NM 2007050300094 20070503 00094 NM 2007 5 3 SWAA072152 1 20070501 A 5310 6545834 CREASE BEAM BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 277 AND BS 294.5, LBL 52. R&R CREASE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2007050300097 20070503 00097 NM 2007 5 3 SWAA072134 1 20070501 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050300109 20070503 00109 NM 2007 5 3 SWAA072151 1 20070501 A 5312 6549868 BULKHEAD BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 7L. REPAIRED WEB PER ER. 2 L 7 2 4F RT A16WE 2007050300111 20070503 00111 NM 2007 5 3 SWAA072155 1 20070501 A 5311 6554892 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 320, STR 21L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007050300112 20070503 00112 NM 2007 5 3 DL76G070386 1 20070430 A 3150 M285T025919 CIRCUIT CARD BOEING 767 767332 1382001 NM PWA 2037 PW2037 NE MALFUNCTIONED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 177DZ 29698 716521 AFTER APPLYING T/O, POWER AND BEGINNING TAKEOFF ROLL AT APPROX 10-20 KTS THE PARKING BRAKE TAKEOFF CONFIG WARNING ANNUNC IATED MID A/C FLT ATTENDANT STATED SHE FELT A CYCLING OF BRAKES AND SHUTTERING. LUBED PARKING BRAKE VALVE MECHANISM. R ERACKED TAKEOFF CONFIG CARD M620 PERFORMED T/O CONFIG TEST ALL PASSED. 2 L 7 2 4F 4 F RT A1NM E17NE 2007050300116 20070503 00116 EU 2007 5 3 F3LA200700092 1 20070424 A 5321 D5361060500100 FLOORBOARD AIRBUS A318 A318111 3940019 EU CABIN CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 801FR 4759 1939 DURING C-3 CHECK, INSPECTION REPORTED FLOORBOARD 222FF (R1 ENTRY) CORRODED. REPLACED FLOORBOARD 222FF IAW AMM 53-12-12- 400-001. 2 L 7 2 4F RT 2007050300128 20070503 00128 NM 2007 5 3 UPS07249687 1 20070424 A 2120 DUCT BOEING 727 7271A7C 13840X2 NM AIRSTAIRS BAY BLOWN A IPXA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 935UP 20143 EMERGENCY DECLARED, LWR AFT BODY OVERHEAT WARNING LIGHT ILLUM. ALL EPR INDICATIONS INOP. STDBY HYD OVERHEAT LT ILLUM. CAPT'S RADIO INTERMITTENT CREW WAS ASKED TO DEVIATE DUE TO WEATHER, BUT DECLARED EMERGENCY DUE TO VARIOUS MALFUNCTIONS. FOUND BLOWN DUCT IN AIRSTAIRS COMPARTMENT. 2 L 7 3 4F A3WE 2007050300142 20070503 00142 NM 2007 5 3 SWAA072140 1 20070501 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7R. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050300143 20070503 00143 NM 2007 5 3 SWAA072142 1 20070501 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2R. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050300145 20070503 00145 NM 2007 5 3 SWAA072143 1 20070501 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050300151 20070503 00151 NM 2007 5 3 HALA0700197 1 20070422 A 5330 SKIN BOEING 767 767332 1382001 NM BS 185 S30R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 FUSELAGE SKIN RT BS 185.5 JUST BELOW STR 30 HAS LIGHTNING STRIKE. REPAIRED PER HAL M105 NR 597053. 2 L 7 2 4F RT A1NM 2007050300157 20070503 00157 NM 2007 5 3 HALA0700192 1 20070422 A 5330 SKIN BOEING 767 767332 1382001 NM BS 320 S23-24L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 FUSELAGE SKIN BS 320 BETWEEN STR 23L AND STR 24L HAS LIGHTNING STRIKE. REPAIRED PER HAL M105 597053. 2 L 7 2 4F RT A1NM 2007050300160 20070503 00160 NM 2007 5 3 SWAA072158 1 20070501 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482A, STR 8R. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050300165 20070503 00165 NM 2007 5 3 SWAA072163 1 20070501 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND STRINGER 8R CRACKED AT BS 482A. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007050300166 20070503 00166 NM 2007 5 3 HALA0700199 1 20070424 A 5313 STRINGER BOEING 767 767332 1382001 NM BS 433 S33R CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 FORWARD CARGO BAY HAS CORROSION ON STR 33R AT BS 433 (UNDER LOWER FLANGE) AT STR SPLICE. STRINGER SPLICE AT BS 433 STR 33R FOUND TO BE COMPLETELY CORRODED THROUGH (100% LOSS). SPLICE REMOVED IAW SRM 51-40-02-06-0. NEW SPLICE FABRICATED F ROM HFAB53-SSP-011 (LOT 730642) AND INSTALLED IAW SRM 51-40-02. ALODINE, PRIMER AND PAINT APPLIED PRIOR TO INSTALLATION IAW MM 51-21-04 AND 51-21-10. ALL ACCESSED ROLLER TRAYS INSTALLED IAW MM 25-53-02-404-004. 2 L 7 2 4F RT A1NM 2007050300167 20070503 00167 NM 2007 5 3 HALA0700196 1 20070422 A 5330 SKIN BOEING 767 767332 1382001 NM BS 236-246 DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 FUSELAGE SKIN RT BS 236 TO BS 246 BETWEEN STR 32 AND STR 35 HAS 3 AREAS OF LIGHTNING DAMAGE. REPAIRED PER HAL M105 NR 5 97053. 2 L 7 2 4F RT A1NM 2007050300168 20070503 00168 2007 5 3 SWAA072156 4 20070501 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007050300171 20070503 00171 NM 2007 5 3 HALA0700188 1 20070422 A 5330 SKIN BOEING 767 767332 1382001 NM BS 220 S24-27L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 FUSELAGE SKIN, LT BS 220 BETWEEN STR 24 AND STR 27 HAS LIGHTNING DAMAGE AT FASTENERS. REMOVED DAMAGE AND REPAIRED IAW 7 67 SRM 53-00-01/201 SECT II STEP 3A AND HAL M105 597053. 2 L 7 2 4F RT A1NM 2007050300172 20070503 00172 NM 2007 5 3 SWAA072165 1 20070501 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 401WN 29813 DURING SCHEDULED HC2 CHECK, LT OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007050300180 20070503 00180 NM 2007 5 3 SWAA072115 1 20070430 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 406WN 27894 EEPLS COVER LOOSE AT ROW 3 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007050300191 20070503 00191 NM 2007 5 3 SWAA072113 1 20070430 A 5755 654456115 SPOILER BOEING 737 7373Q8 1384670 NM LT WING FAULTY A SWAA K NONE F FLT CONT AFFECTED AP APPROACH 1 SW 29 662SW 23255 SIGNIFICANT ROLL TO LEFT ON APPROACH WITH FLAPS AT 40. R&R NR 2 SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007050300192 20070503 00192 NM 2007 5 3 SWAA072117 1 20070430 A 5523 6545166 PUSHROD BOEING 737 7373H4 1384600 NM LT ELEVATOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED 14Y CHECK, FOUND LT ELEVATOR TRIM TAB PUSH ROD FWD ROD END CORRODED. R&R TRIM TAB PUSH ROD PER MM. 2 L 7 2 4F RT A16WE 2007050300214 20070503 00214 NM 2007 5 3 SWAA072168 1 20070501 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 745SW 29491 DURING SCHEDULED 8Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 3 ABC. R&R LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007050300215 20070503 00215 NM 2007 5 3 SWAA072167 1 20070501 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 745SW 29491 DURING SCHEDULED 8Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 1 ABC. R&R LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007050300217 20070503 00217 NM 2007 5 3 SWAA072129 1 20070501 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 479WN 33990 DURING SCHEDULED MV1 CHECK, FOUND EEPLS COVER BROKEN AT ROW 11 ABC. R&R COVER PER MM. 2 L 7 2 4F RT A16WE 2007050300260 20070503 00260 EU 2007 5 3 2007UALA01254 1 20070423 A 3350 BR964421 LIGHT AIRBUS 320 A320232 3930326 EU EXIT SIGN MISSING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 433UA 589 BOTH AFT DOOR LWR EMERGENCY EXIT LIGHT HAVE 1EA LAMP INOP. REPLACED MISSING LAMPS FROM EXIT SIGNS. 2 L 7 2 4F RT A28NM 2007050300268 20070503 00268 NM 2007 5 3 2007UALA01264 1 20070423 A 5230 SKIN BOEING 737 737322 1384676 NM CARGO DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 FWD CARGO DOOR HAS A 8" LONG .312" WIDE .062" DEPTH DENT, 3" FWD OF AFT DOOR EDGE AND 20" UP FROM BOTTOM OF DOOR. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR RUNNING FULL LENGTH & TWO THIRDS WIDTH OF DOOR. 2 L 7 2 4F RT A16WE 2007050300276 20070503 00276 NM 2007 5 3 DL76L070340 1 20070420 A 5420 311T31571 ANGLE BOEING 767 767332 1382001 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 182DN 25987 DURING ACCOMPLISHMENT OF INSPECTIONS OF THE NR 2 PYLON MIDSPAR FITTINGS AND CLOSEOUT ANGLE PER OPN 5281AD (01-074944-12) . THE CLOSEOUT ANGLE WAS FOUND CRACKED IN THE TYPICAL LOCATIONS AT THE FASTENERS COMMON TO THE MIDSPAR FITTINGS. THE MI D SPAR FITTINGS WERE INSPECTIONS AND NO INDICAITONS WERE NOTED. THE CLOSEOUT ANGLE WAS REPLACED WITH A NEW PART PER INS TRUCTIONS CONTAINED IN ERA 461325-14AD. 2 L 7 2 4F RT A1NM 2007050300285 20070503 00285 NE 2007 5 3 DL76S070345 2 20070422 A 7200 CF680A2 ENGINE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 1 POWER LOSS A DALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 27 132DN 55811 2298 24981 580322 WHILE IN CLIMB AND AT LEVEL 34K AND THROTTLING BACK TO CRZ POWER THE LEFT ENGINE HAD A LOUD POP WITH LOSS OF THRUST WITH ENGINE AT IDLE THERE WAS NO THROTTLE RESPONSE THEN THE ENGINE WAS SHUT DOWN BY THE PILOT. A/C RETURNED TO ATL AND LAND ED SAFELY. NUMBER ONE ENGINE REPLACED PER TRANS 1T144. 2 L 7 2 4F 4 F RT A1NM E13NE 2007050300287 20070503 00287 NE 2007 5 3 DLM88070348 2 20070422 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 LEAKING A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 992DL 46414 53344 718247 NR 2 ENGINE IFSD DUE TO LOSS OF OIL QTY AND PRESSURE. REPLACED NR 2 ENGINE PER TRANS 9T102. 2 L 7 2 4F 4 F RT A6WE E9NE 2007050300293 20070503 00293 EA 2007 5 3 QXEA200700690 1 20070429 A 4900 100021102 CHARGER CNDAIR CL600 CL6002C10 1390015 EA APU MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 614QX 2050 263 10049 PDX - FLIGHT 2561 - RETURN TO THE GATE FOR A APU BATTERY CHARGER STATUS MESSAGE. MAINTENANCE REPLACED THE BATTERY CHARG ER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007050300295 20070503 00295 NM 2007 5 3 2007UALA01275 1 20070423 A 3350 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 852UA 1671 DURING 3 SVC EMERGENCY LIGHT CHK, AFT POWER SUPPLY BATTERY FAULTED. [SUP 05-16-07] REPLACED BATTERY, TESTED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007050300311 20070503 00311 NE 2007 5 3 2007UALA01285 2 20070420 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 SURGES A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 717551 NR 2 ENG SURGED DURING GROUND RUN FOR BLEED T-S. [SUP 05-18-07] ACCOMPLISHED NR 2 ENGINE VISUAL CHK. REPLACED IDG OIL AND SCAV. OIL FILTER. INSPECTED MAG CHIP DET. PER MM79-21-1 0 601. NR 2 ENGINE REQUIRES BORESCOPE PER TROUBLESHOOTING OF SMC2. BORESCOPED C5,C6,C14,C15, T1&T2 AS REQ IN MM 71-05-00. FOUND ALL OK FOR INTERVAL-1. A/C RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050300320 20070503 00320 NM 2007 5 3 UPS07M49707 1 20070413 A 5320 INTERCOSTAL DOUG MD11 MD11F 3023600 NM BS 1256-1273 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C DOOR 3 CROWN AREA, AT STA 1256 TO STA 1273 LONG 1 LT INTERCOSTAL BOTH FACES FOUND CORROSION. CORROSIO N REMOVED PER SRM 51-21-01 VOLIIR38 ORI THK 0.032", MAT'L REMOVED 0.020", MAT'L REMAINED 0.012" FOUND OUT OF LIMIT PER SRM 53-00-01 FIG1AVOLIR38. INTERCOSTAL REMOVED PER SRM 51-35-01 VOLIIR38. NEW INTERCOASTAL FAB PER BOEING DWG AEA0202R EVK. HEAT TREAT PER DPS7.00-1 AND HARDNESS VALUE 15T88.5 PER DPS1.05-3. INTERCOSTAL INSTALL PER SRM 51-35-01 VOL IIR38 . 2 L 7 3 4F RT A22WE 2007050300328 20070503 00328 NM 2007 5 3 GTIA200700016 1 20070427 A 5210 HOOK AIRBUS A319 A319132 3930340 NM L1 DOOR DIRTY A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 506NK 2490 L1 DOOR WILL NOT LOCK OPEN. REMOVED DOOR STAY MECHANISM , CLEANED DEBRIS FROM MECHANISM, REINSTALLED STAY MECHANISM. 2 L 7 2 4F RT A28NM 2007050300334 20070503 00334 NM 2007 5 3 2007UALA01292 1 20070424 A 3350 58781 FEEDER CABLE BOEING 737 737322 1384676 NM CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 342UA 24246 FIRST 10 ROWS OF COACH EEL LIGHTS ARE INOPERATIVE. REPLACED EEL LIGHT FEEDER CABLE FROM WALL TO STRIP. 2 L 7 2 4F RT A16WE 2007050300337 20070503 00337 NM 2007 5 3 2007UALA01295 1 20070424 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 671UA 30026 SEAT MOUNTED EMERGENCY LIGHT MISSING AT SEAT 41AB. REPLACED MISSING LIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050300351 20070503 00351 NM 2007 5 3 AWXA200700548 1 20070407 A 5330 6545775594 SKIN BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - FOUND CRACKED FUSELAGE SKIN, BS 891, S25R. REPAIRED FUSELAGE SKIN, BS 891, S25R IAW B737-300 SRM 53-00-01-2R31 FI GURE 201. 2 L 7 2 4F RT A16WE 2007050300356 20070503 00356 NM 2007 5 3 2007UALA01298 1 20070425 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 AFT CABIN FLOOR STRUCTURE, UPPER "T" CAP CORRODED ON UPPER SURFACE AT BS 1016 LBL5 TO 39 WL 208. MAJOR REPAIR ACCOMPLIS HED: REMOVED CORROSION. FABRICATED & INSTALLED FILLER, STRAP & NESTED ANGLE REPAIR. 2 L 7 2 4F RT A16WE 2007050300360 20070503 00360 NM 2007 5 3 UPS07549730 1 20070403 A 5330 143N3323 SKIN BOEING 757 75724APF 1384969 NM BS 660 S15L DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 414UP 23854 INSPECTION TYPE:C LEFT EXTERNAL FUSELAGE HAS DENT OVER STRINGER STA 660 STGR 15L. CHK DENT FOUND OUT LIMITS PER SRM 53- 00-01-1A, DETAIL III, DENT OVER STRINGER 2. REMOVED FASTENERS IN AIR GRILL AND SIDEWALL TO DISPLACE FOR ACCESS IAW SRM 51-40-02 3. DISPLACED INSULATION FOR ACCESS IAW AMM 25-55-07-4. REMOVED EXISTING FASTENERS FOR ACCESS IAW AMM 51-40-02 AND SRM 53-00-01 FIG 201 REP 2. 2 L 7 2 4F RT A2NM 2007050300361 20070503 00361 NM 2007 5 3 UPS07549731 1 20070403 A 5330 143N3323 SKIN BOEING 757 75724APF 1384969 NM BS 660 S15L DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 414UP 23854 INSPECTION TYPE:C LEFT EXTERNAL FUSELAGE HAS DENT OVER STRINGER STA 660 STGR 15L. CHK DENT FOUND OUT LIMITS PER SRM 53- 00-01-A, DETAIL III DENT OVER STRINGER. REMOVED FASTENERS IN AIRGRILL AND SIDEWALL TO DISPLACE FOR ACCESS IAW SRM 51-40 -02. DISPLACED INSULATION FOR ACCESS IAW AMM 25-55-07-4. DISPLACED INSULATION FOR ACCESS IAW AMM 25-55-07-4. REMOVED EXISTING FASTENERS IAW SRM 51-40-02 AND SRM 53-00-01 FIG 201. 2 L 7 2 4F RT A2NM 2007050300383 20070503 00383 NM 2007 5 3 2007UALA01316 1 20070426 A 2140 HEATER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE AFT BUNKROOM FAULTY A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 WP 29 180UA 25224 FA REPORT UNUSUAL ODOR IN AFT BUNKROOM. [SUP 05-18-07] CHECKED FOR BURN, FOUND BURNING SMELL COMES BACK WHEN F/A CREW REST HEATER OPERATED. DEACTIVATED HEATER PER MEL 2141A. REPLACED CREW REST HEATER AND OPS CHECK NORMAL. SUSPECT HEATER E LEMENT SHORTING WITH HIGH CURRENT MELTING INSULATION/ PLASTIC IN HEATER UNIT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050400008 20070504 00008 NM 2007 5 4 ASAA0741627 1 20070502 A 5753 65C2755214 SKIN BOEING 737 7374Q8 138447Q NM T\E FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 776AS 25109 THE RT OB MID FLAP IS CHAFED ON AN EXITING LE DOUBLER AT THE IB END. REMOVED THE EXITING REPAIR DOUBLER FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 57 53 01 FIG 201 REPAIR 8. 2 L 7 2 4F RT A16WE 2007050400017 20070504 00017 NM 2007 5 4 07FDEA01645 1 20070426 A 5754 ARB712823 RIB DOUG MD11 MD11F 3023600 NM NR 1 SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 LEFT WING NR 1 SLAT INBOARD RIB ATTACHED TO THE PERFORMANCE FAIRING FOUND WITH ONE (1) INCH CRACK AT THE LOWEST STUD ARE A. [SUP 05-14-07] REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100 . 2 L 7 3 4F RT A22WE 2007050400024 20070504 00024 NM 2007 5 4 SWAA072171 1 20070502 A 3230 273A12011 ACTUATOR BOEING 737 7377H4 1384404 NM NLG FAULTY A SWAA K NONE J WARNING INDICATION CL CLIMB 1 SW 29 717SA 27851 NOSE GEAR WOULD NOT RETRACT. CYCLED GEAR HANDLE NOSE GEAR RETRACTED. R&R NLG LOCK ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2007050400028 20070504 00028 NM 2007 5 4 NWAA071686744 1 20070402 A 5315 FLOORBEAM BOEING 747 747212F 1384851 NM BS 440 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 644NW 24177 DURING "M" CHECK, FOUND CORROSION ON UPPER DECK FLOORBEAM UPPER CHORD BS 440 LBL 76. REPAIRED PER EA 67-209236. 2 L 7 4 4F RT A20WE 2007050400029 20070504 00029 NM 2007 5 4 SWAA072208 1 20070502 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400031 20070504 00031 NM 2007 5 4 NWAA071656744 1 20070401 A 5322 TENSION TIE BOEING 747 747212F 1384851 NM BS 860 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 644NW 24177 DURING "M" CHECK, FOUND CRACKS IN TENSION TIE CHANNEL FASTENER HOLES AT BS 860 LT. REPAIRED PER EA 67-208993. 2 L 7 4 4F RT A20WE 2007050400033 20070504 00033 NM 2007 5 4 NWAA071706744 1 20070406 A 5411 FRAME BOEING 747 747212F 1384851 NM NR 3 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 644NW 24177 DURING "M" CHECK, FOUND CRACKS IN NR 3 PYLON FRAME AND STIFFENER AT NAC STA 210 AND CUT OUT SKIN AT ACCESS PANEL 473 CL. REPAIRED PER EA 67-209239. 2 L 7 4 4F RT A20WE 2007050400036 20070504 00036 WP 2007 5 4 UPS07849724 1 20070430 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS WEAK A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 DURING PDC, FOUND EMERGENCY LIGHTING DIM. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2007050400044 20070504 00044 EA 2007 5 4 SWIA200718180 1 20070322 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 925SW 7682 ENGINE SUPPORT BEAM CRACKED AT RIGHT LOWER WEB ON FORWARD INBOARD CORNER, DISCOVERED AT C-CHECK. INSTALLED ALL REPAIR P ARTS FOR RIGHT LOWER ENGINE SUPPORT BEAM PER REO 601R-53-61-358 REV A. 2 L 7 2 4F RT A21EA 2007050400046 20070504 00046 EA 2007 5 4 SWIA200718181 1 20070427 A 3244 50105711 TIRE CNDAIR CL600 CL6002B19 1900309 EA MLG FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 432SW 7548 RIGHT INBOARD MAIN TIRE BLEW OUT ON TAKEOFF WITH ASSOCIATED RIGHT ANTI-SKID LIGHT AND RIGHT INBOARD BTMS INOP. RETURNED TO SLC. REMOVED AND REPLACED NR 3 AND NR 4 WHEEL ASSEMBLY'S IAW 32-40-00PN 5010571-1 SN ON MAY03-5690 SN OFF MAR03-554 0. 2 L 7 2 4F RT A21EA 2007050400068 20070504 00068 WP 2007 5 4 UPS07849735 1 20070501 A 2150 A/C PACK DOUG DC8 DC871F 302199D WP RIGHT ODOR A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 718UP 46018 FOWL ODOR EMITTING FROM RT PACK. OPERATED THE RT PACK WITH A GROUND CART AND WITH THE NR 3 AND NR 4 ENGINES SEPARATELY PER AMM 21-55-00-5. ENSURED NO FUMES OR ODORS CAME FROM THE RIGHT PACK. COMPLIED WITH H136216, NO FUMES OR ODORS DURIN G RIGHT PACK OPERATION. A/C IS OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2007050400069 20070504 00069 WP 2007 5 4 UPS07849736 1 20070501 A 2560 ESCAPE ROPE DOUG DC8 DC871F 302199D WP EMERGENCY EXIT LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 CAPTAIN'S ESCAPE ROPE UNSECURE AND COVER LOOSE. RESECURED CAPTAIN'S ESCAPE ROPE AND COVER. 2 L 7 4 4F RT 4A25 2007050400070 20070504 00070 WP 2007 5 4 UPS07849737 1 20070424 A 5712 RIB DOUG DC8 DC873F 302199F WP LWS 591 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 LT WING OUTBD L/E RIB CRACKED AT XFS 591. NDT VERIFIED CRACK ENDS AT FASTENER HOLE IAW NDSPM 06-10-0 1-001. FABRICATED AND INSTALLED REPAIR ANGLE AT LT WING OUTBD L/E STA XFS 591 IAW SRM 57-03-03 FIG 6. 2 L 7 4 4F RT 4A25 2007050400071 20070504 00071 WP 2007 5 4 UPS07849738 1 20070424 A 5712 RIB DOUG DC8 DC873F 302199F WP LWS 609 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 LT WING OUTBD L/E RIB CRACKED AT STA XFS 609. NDT VERIFIED CRACK TERMINATES AT FASTNER HOLE IAW NDSP M 06-10-01-001. FABRICATED AND INSTALLED REPAIR ANGLE AT L/WING L/E RIB STA XFS 609 IAW SRM 57-03-03 FIG 6. 2 L 7 4 4F RT 4A25 2007050400075 20070504 00075 NM 2007 5 4 UPS07M49733 1 20070501 A 3350 LIGHT DOUG MD11 MD11F 3023600 NM EMERGENCY EXIT NO TEST A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 258UP 48416 EMERGENCY LIGHTS WILL NOT TEST. RESET CIRCUIT BREAKER AND EMERGENCY LIGHTS OPERATE NORMAL. 2 L 7 3 4F RT A22WE 2007050400077 20070504 00077 NM 2007 5 4 DHL2007782513 1 20070501 A 5740 BRACKET BOEING 727 727227 1384078 NM ACTUATOR ROD EXCESS PLAY A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 782DH 21998 RT INBD AFT FLAP CONTROL CABLE ACTUATOR ROD LOWER MOUNTING BRACKET LOOSE INSIDE FLAP, RWBL 101.0. ACCESS GAINED TO AFFE CT REPAIR; CUT OUT AFT FLAP L/E SECTION, 8.5" BY 14" PER B727 SRM 57-40-4 FIG 17. FABRICATED 2 REPAIR SPLICES FROM 2024 -T3, .050" BY 5.5" BY 14", AND .050" BY 5" BY 14", PO NR 9004042, PER B727 SRM 57-50-4 FIG 11. TREATED, PRIMED, AND INS TALLED REPAIR PARTS PER B727 SRM 51-10-2 AND 57-50-4 FIG 11. 2 L 7 3 4F A3WE 2007050400078 20070504 00078 NM 2007 5 4 SWAA072175 1 20070502 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400080 20070504 00080 NM 2007 5 4 SWAA072202 1 20070502 A 5311 6546553 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400081 20070504 00081 NM 2007 5 4 SWAA072199 1 20070502 A 5311 6546555 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400084 20070504 00084 NM 2007 5 4 SWAA072200 1 20070502 A 5311 6546558 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400085 20070504 00085 NM 2007 5 4 SWAA072176 1 20070502 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400089 20070504 00089 NM 2007 5 4 SWAA072177 1 20070502 A 5311 65C22910 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 13L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400090 20070504 00090 NM 2007 5 4 SWAA072174 1 20070502 A 5311 65C25228 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400095 20070504 00095 NM 2007 5 4 SWAA072179 1 20070502 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050400097 20070504 00097 NM 2007 5 4 SWAA072180 1 20070502 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 16L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050400100 20070504 00100 NM 2007 5 4 SWAA072182 1 20070502 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050400102 20070504 00102 CE 2007 5 4 42807N303CS1 1 20070428 A 3260 S33682 LAMP CESSNA 500 550 2076604 CE PWA 530 PW530A NE INDICATOR INOPERATIVE E Z5FA L A ABORTED APPROACH UNSCHED LANDING P NO WARNING INDICATION AP APPROACH 1 EA 63 303CS 5500814 DURING APPROACH, THE LANDING GEAR WAS SELECTED DOWN. THE USUAL (3) BUMPS WERE HEARD BUT ONLY (2) GREEN LIGHTS ILLUMINATE D. THE RT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. THE LANDING GEAR WAS CYCLED WITH THE SAME RESULTS AND INDICA TION. THE EMERGENCY CHECKLIST WAS USED INCLUDING BLOWING THE GEAR DOWN. AN ANNUCIATOR TEST WAS ACCOMPLISHED AND THE RT MAIN LANDING GEAR GREEN LIGHT WAS INOP. AIRCRAFT DIVERTED, APPROACH WAS NOTIFIED AND AN EMERGENCY DECLARED. THE AIRCRAFT MADE A PASS BY THE TOWER AND ALL (3) LANDING GEAR APPEARED TO BE DOWN. THE AIRCRAFT MADE AN UNEVENTFUL LANDING. MAINTE NANCE TROUBLESHOT PROBLEM AND FOUND THE INDICATION SYSTEM AT FAULT. THE INDICATOR LAMP WAS REPLACED, HYDRAULIC SYSTEM SE 1 L 7 2 4F 4 F A22CE E00053EN 2007050400103 20070504 00103 CE 2007 5 4 DXTA200702164 1 20070430 A 3220 YAW DAMPER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG MALFUNCTIONED E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 901QS 7500102 SEVERE NOSE WHEEL VIBRATION DURING TAKEOFF ROLL. TAKEOFF WAS ABORTED, LOWER YD TURNED ITSELF OFF. REMOVED AND REPLACED BOTH NOSE WHEEL ASSY. DUE TO HIGH VIBRATION. ALL WORK IAW CE750 M.M. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007050400104 20070504 00104 NM 2007 5 4 SWAA072207 1 20070502 A 5330 65C381921 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 366, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400106 20070504 00106 NM 2007 5 4 SWAA072184 1 20070502 A 5523 69633918 BOLT BOEING 737 7373H4 1384600 NM LT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. R&R NR 1 HINGE BUSHING AND BOLT PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400108 20070504 00108 NM 2007 5 4 SWAA072185 1 20070502 A 5523 69633918 BOLT BOEING 737 7373H4 1384600 NM LT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. R&R NR 2 HINGE BUSHING AND BOLT PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400113 20070504 00113 NM 2007 5 4 SWAA072189 1 20070502 A 5523 69633918 BOLT BOEING 737 7373H4 1384600 NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED 10Y CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. R&R NR 3 HINGE BUSHING AND BOLT PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400115 20070504 00115 NM 2007 5 4 SWAA072190 1 20070502 A 5523 69633918 BOLT BOEING 737 7373H4 1384600 NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. R&R NR 1 HINGE BUSHING AND BOLT PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400117 20070504 00117 NM 2007 5 4 SWAA072204 1 20070502 A 5313 BAC1498 STRINGER BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND STRINGER 16R CRACKED AT BS 504C. REPAIRED STRINGER PER ER. 2 L 7 2 4F RT A16WE 2007050400119 20070504 00119 NM 2007 5 4 SWAA072192 1 20070502 A 5523 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM LT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED BRDG CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. R&R NR 1 HINGE BEARING AND BUSHING PER MM. 2 L 7 2 4F RT A16WE 2007050400129 20070504 00129 CE 2007 5 4 DJFA2007052 1 20070427 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 476LX 2596 RK376 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE LT IB HORIZONTAL STA BILIZER, THE LT RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUÉ' NR 70. MAINTENANCE REPLACED THE RIB ASSEMBLY. 2 H 7 2 4F 4 F RT A16SW E25EA 2007050400130 20070504 00130 EU 2007 5 4 AALA20070722 1 20070420 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80084 675 MIA EMERGENCY LIGHT AT SEAT 10G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 10G. SYSTEM GROUND CHECKED NORMAL OPERA TION. (CLOSED) 2 L 7 2 4F RT A35EU 2007050400132 20070504 00132 EU 2007 5 4 AALA20070729 1 20070422 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70073 516 MIA EMERGENCY LIGHT AT SEAT 36C HAS LOOSE WIRE. SECURED WIRE FOR EMERGENCY LIGHT AT SEAT 36C. SYSTEM GROUND CHECKED NO RMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A35EU 2007050400136 20070504 00136 NM 2007 5 4 USAA200705001 1 20070429 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 1" CRACK FOUND AT STA 727D STR 23L ON SKIN. (CLT) INSTALLED DOUBLER PER TR 53-60-03A 2 L 7 2 4F RT A16WE 2007050400147 20070504 00147 CE 2007 5 4 AMWA84318BC 1 20070430 A 2497 661054 BATTERY CABLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER BATTERY CORRODED A AMWA O OTHER J WARNING INDICATION CL CLIMB 1 CE 07 244YV UE244 BATT CHARGE ANNUNCIATOR ILLUMINATED ON DEPARTURE JUST AFTER GEAR RETRACTION. THIS BATTERY CHARGE ANNUNCIATOR LIGHT ILLU M IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTIONS TO THE PILOTS. CLEANED AND RESECURED BATTERY CONNECTIO NS. 2 L 7 2 4T 4 T RT A24CE E26NE 2007050400157 20070504 00157 NM 2007 5 4 USAA070334 1 20070501 A 5313 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 503UW 23237 TWO AREAS, 6" LONG S-27L BETWEEN BS 986.5 & BS 1006. SPLICED IN PORTS OF IDENTICAL PART PER SRM 53-00-03, REPAIR NR 1, FIG 201; CORR TASK C53-202-01. DEFECT SIZE: 6" LONG (2 AREAS) 2 L 7 2 4F RT A16WE 2007050400164 20070504 00164 NM 2007 5 4 USAA070337 1 20070501 A 5320 STIFFENER BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 503UW 23237 RBL 6 STA 663 FWD WALL OF MLG WHEEL WELL JUST ABOVE B SYS HYD PUMP. INSTALLED DOUBLER PER EA 98640. DEFECT SIZE: 2" 2 L 7 2 4F RT A16WE 2007050400169 20070504 00169 NM 2007 5 4 USAA070339 1 20070501 A 5320 FLOOR SUPPORT BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 BETWEEN BL0 TO LBL -24 AT STA 540. REMOVED & REPLACED SUPPORT ANGLE PER SRM 51-10-02. DEFECT SIZE: 1" 2 L 7 2 4F RT A16WE 2007050400174 20070504 00174 NM 2007 5 4 USAA070340 1 20070501 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 STA 480 BETWEEN STR 8 & 9 RT AT ATTACH BRACKET ON FRAME, INBD RIVET. INSTALLED REPAIR ANGLES PER TR 53-10-20E. DEFECT SIZE: 1/4" 2 L 7 2 4F RT A16WE 2007050400177 20070504 00177 NM 2007 5 4 AALA20070727 1 20070421 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 394AN 29431 DFW EMERGENCY PATH LIGHT IN CABIN HAS BROKEN WIRE. REPAIRED WIRE FOR EMERGENCY LIGHT IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A1NM 2007050400178 20070504 00178 WP 2007 5 4 AALA20070718 1 20070420 A 3231 39567851 LINK DOUG DC9 DC982 3022082 WP NLG DOOR BROKEN A AALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 21 430AA 49342 LGA INFLIGHT T707/20APR DURING GEAR RETRACTION FELT HEAVY VIBRATION IN THE NOSE GEAR AREA. RETURNED TO LGA AND LANDED WITHOUT INCIDENT. FOUND LEFT NOSE GEAR DOOR LINK LATCH BROKEN. REPLACED LEFT NOSE GEAR DOOR LINK ASSEMBLY. SYSTEM GRO UND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2007050400182 20070504 00182 NM 2007 5 4 AALA20070716 1 20070419 A 3350 1317 LIGHT BOEING 767 767323 1385205 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 351AA 24032 SFO EXTERIOR EMERGENCY LIGHT AT RIGHT HAND SIDE OVERWING INOPERATIVE. RELAMPED EXTERIOR EMERGENCY LIGHT AT RIGHT HAND SIDE OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A1NM 2007050400184 20070504 00184 NM 2007 5 4 AALA20070715 1 20070418 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 681AA 25338 LAX EMERGENCY LIGHT ASSEMBLY AT SEAT 30D MISSING. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 30D. SYSTEM GROUND CHECKE D NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A2NM 2007050400185 20070504 00185 NM 2007 5 4 AALA20070713 1 20070419 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 380AN 25449 MIA EMERGENCY LIGHTS FROM SEAT ROWS 30B TO 35B INOPERATIVE. RECHARGED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT ROWS 30B TO 35B. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A1NM 2007050400187 20070504 00187 NE 2007 5 4 AALA20070712 2 20070418 A 7230 COMPRESSOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LT ENGINE STALLED A AALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 21 975TW 53625 718445 ORD INFLIGHT T1877/18APR AFTER TAKE OFF LEFT HAND ENGINE COMPRESSOR STALLED. THROTTLE RETARDED AND INDICATIONS NORMAL . RETURNED TO ORD AND LANDED WITHOUT INCIDENT. METAL DEBRIS FOUND IN LEFT HAND ENGINE EXHAUST. REPLACED LEFT HAND ENG INE ON 19 APR 2007 AT ORD. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F RT A6WE E9NE 2007050400191 20070504 00191 NM 2007 5 4 AALA20070719 1 20070419 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 777AN 29585 MIA FLOOR PROXIMITY EMERGENCY LIGHT AT GALLEY NUMBER THREE HAS BROKEN LENS TRIM. REPLACED FLOOR PROXIMITY EMERGENCY LI GHT ASSEMBLY AT GALLEY NUMBER THREE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT T00001SE 2007050400192 20070504 00192 NM 2007 5 4 AALA20070723 1 20070421 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 761AJ 31478 NRT EMERGENCY LIGHT AT SEAT 3D AFT INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 3D AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT T00001SE 2007050400193 20070504 00193 WP 2007 5 4 AALA20070724 1 20070420 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 456AA 49561 SFO EMERGENCY LIGHT AT SEAT 6E INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 6E. SYSTEM GROUND CHECKED NORMAL OPERATI ON. (CLOSED) 2 L 7 2 4F A6WE 2007050400196 20070504 00196 EU 2007 5 4 AALA20070704 1 20070417 A 3350 BR964814 FIXTURE AIRBUS 300 A300B4605R 3930308 EU CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14068 511 JFK EMERGENCY LIGHT AT SEAT 24C HAS MISSING FIXTURE. REPLACED LIGHT FIXTURE FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM G ROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A35EU 2007050400200 20070504 00200 WP 2007 5 4 AALA20070700 1 20070417 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7549A 53031 LGA EMERGENCY LIGHT AT LEFT AND RIGHT HAND AFT OF WING INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AND RIGHT HAND AFT OF WING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2007050400201 20070504 00201 EA 2007 5 4 554304292007 1 20070429 A 2750 FLAP SYSTEM CNDAIR CL604 CL604 1900301 EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED E J7SA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 05 332FX 5543 FLAPS FAILED AT 13 DEGREES ON APPROACH. CREW DECLARED AN EMERGENCY AND PERFORMED AN UNEVENTFULL LANDING. MX DISPATCHED WITH BREAKOUT BOX. AFTER RESET, FLAPS OPERATIONAL CHECKS PERFORMED ON COMPLETE AND ISOLATED SYSTEMS. COULD NOT DUPLICAT E ERROR. NO MX HISTORY OF THIS DISCREPANCY FOUND. AIRCRAFT RELEASED AS CND. 2 L 7 2 4F 4 F RT A21EA E15NE 2007050400202 20070504 00202 WP 2007 5 4 AALA20070701 1 20070417 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7549A 53031 LGA EMERGENCY LIGHT AT FLOOR LEVEL AT FIRST CLASS LAVATORY INOPERATIVE. REPLACED CONNECTOR FOR EMERGENCY LIGHT AT FLOO R LEVEL AT FIRST CLASS LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2007050300222 20070503 00222 NM 2007 5 3 USAA070344 1 20070501 A 5320 MOUNT BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 STA 727D+12 AT RBL 2, ANTENNA MOUNT Z SUPPORT. DRILLED & INSTALLED NEW PART PER SRM 51-10-02. DEFECT SIZE: 1 INCH 2 L 7 2 4F RT A16WE 2007050300227 20070503 00227 NE 2007 5 3 AALA20070679 2 20070413 A 7250 TURBINE BLADES DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LEFT ENGINE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 416AA 49327 717823 STL INFLIGHT T2303/13APR - ORD - DFW DURING CRUISE AT FLIGHT LEVEL 320, CREW HEARD LOUD BANG AND FELT A YAW. INDICATIO NS SHOWED THE LEFT ENGINE SHUTDOWN. LANDED STL WITHOUT INCIDENT. SINGLE ENGINE TIME APPROXIMATELY 15 MINUTES. REPLACE D LEFT ENGINE ON 15 APR 2007 AT STL DUE TO TURBINE BLADE FAILURE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007050300240 20070503 00240 NE 2007 5 3 ZZDA070427154 2 20070427 A 7230 COMPRESSOR RROYCE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE NR 2 ENGNE STALLED A ZZDA A UNSCHED LANDING R E PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CL CLIMB 1 SO 15 954AT 13358 55016 COMPRESSOR STALL NR 2 AFTER T/O. HAD ROLLBACK TO IDLE. FOR VIBRATION FOR 3 TO 5 MIN RAN CHECK LIST- ENGINE CAME BACK WE RETURNED FOR LANDING. NO TGT EXCEEDED. REPLACED NR 2 ENG A/C OK FOR SERVICE 2 L 7 2 4F 4 F TR A6WE E00061EN 2007050300241 20070503 00241 NM 2007 5 3 ZZDA070428152 1 20070428 A 5220 A42006692302 SOLENOID BOEING 737 737 UTILSYS NM OVERWING DOOR MALFUNCTIONED A ZZDA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 15 267AT 33919 LT OVER WING LIGHT ILLUMINATED ON T/O ROLL. REMOVED & REPLACED LT O/W DOOR FLIGHT LOCK SOLENOID IAW AMM 52-22-41. OPS C HECK GOOD. 2 L 7 2 4F RT A16WE 2007050300247 20070503 00247 EU 2007 5 3 F3LA200700089 1 20070421 A 5315 D5347218820400 FLOORBEAM AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 801FR 1939 DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE HOLE ON FLOORBEAM Y1292 AFT OF FR68. REPLACED FLOORBEA M AT Y1292 AFT OF FR68 IAW 51-42-11, FIG 6 AND 7. 2 L 7 2 4F RT 2007050300251 20070503 00251 NE 2007 5 3 2007UALA01246 2 20070421 A 7230 COMPRESSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE STALLED A UALA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 29 454UA 1104 V11015 CREW RECEIVED NR 1 ENG STALL ECAM AT FL380 IN LIGHT CHOP & LIGHT MTN WAVE ACTIVITY. LOUD BANG HEARD BY F/A. [06-14- 07] REPLACED NR 1 ENGINE DUE TO STALL HISTORY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007050300272 20070503 00272 SO 2007 5 3 SIMA200712005 1 20070424 A 2197 524864 INVERTER EMB 145 EMB145LR 3260212 SO RECIRC FAN BURNED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 629AE 17961 145130 STRONG ELECTRICAL ODOR FOR ONE MINUTE AND THEN DISSIPATED. REMOVED AND REPLACED NR 1, NR 2 RECIRCULAR FANS AND NR 1 REC IRCULAR FAN INVERTER IAW EMB AMM. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050300273 20070503 00273 EA 2007 5 3 SIMA200712010 1 20070427 A 2131 GG670980025 CONTROLLER CNDAIR CL600 CL6002C10 1390015 EA CABIN PRESSURE FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 515AE 8965 10121 UNABLE TO PRESSURIZE AIRCRAFT IN MANUAL OR AUTO MODE, NO CAUTION MESSAGES, DIVERTED TO XNA. REMOVED INSULATION FROM SAF ETY VALVE AND REMOVED AND REPLACED NUMBER TWO CABIN PRESSURE CONTROLLER IAW EMB AMM. OPERATIONAL CHECK GOOD, RETURNED A IRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007050300280 20070503 00280 NM 2007 5 3 2007UALA01270 1 20070424 A 5415 LUG BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 1 PYLON CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 178UA 24385 BORE CORRODED AND SCRATCHED - NR 1 PYLON STRUT FITTING BEARING LUG, BOTH SIDES. [SUP 05-16-07] BORE CORRODED AND SCRAT CHED - NR 1 PYLON STRUT FITTING BEARING LUG, BOTH SIDES. ACCOMPLISHED BORING THE DSB UNDER WING FITTINGS PER COA 899993 040 & SB 747-54A2218. FINAL HOLE DIA AFTER HONE: INBD=2.2750" OUTBTD=2.2450". CORROSION & VIBRATION AGGRAVATED BY HIGH TEMP CAUSED DUAL SIDE BRACE HOLE SURFACE DETERIORATION. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050300286 20070503 00286 NM 2007 5 3 DL76G070347 1 20070422 A 3244 767300ERM TIRE BOEING 767 767332 1382001 NM MLG SEPARATED A DALA O OTHER D INFLIGHT SEPARATION LD LANDING 1 SO 27 1608 30573 NR 4 TIRE HAD RECAP COME OFF ON LANDING. REPLACED NR 4 WHEEL ASSY PER MM OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007050300305 20070503 00305 NM 2007 5 3 2007UALA01283 1 20070423 A 3350 D71702001 BATTERY PACK BOEING 777 777222 1385219 NM CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 799UA 26926 M2 GALLEY UNITS BOTH RT AND LT EEL LIGHT STRIPS INOPERATIVE. REPLACED BATTERY PACK IN DOOR OVERHEAD PANEL AT 2 LEFT. O P CHECKED GOOD. 2 L 7 2 4F RT T0001SE 2007050300317 20070503 00317 NM 2007 5 3 2007UALA01286 1 20070421 A 5347 CARGO TRACK BOEING 737 737322 1384676 NM AFT CARGO BAY CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 AFT CARGO PIT FLOOR SUPPORT RT TRACK SECTION (ADJACENT TO DOOR ) HAS CORROSION ON FLOOR FLANGE. MAJOR REPAIR ACCOMPLISH ED: REMOVED EXISTING EXFOLIATION. INSTALLED NEW FLOOR SUPPORT & NUTPLATES. INSTALLED NEW TRACK AND 2 FT OF SPLICE ANGL E. 2 L 7 2 4F RT A16WE 2007050300349 20070503 00349 NM 2007 5 3 DHL2007782514 1 20070502 A 5313 BAC1498147 STRINGER BOEING 727 727227 1384078 NM BS 1183-1158 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 782DH 21998 FOUND STR 28R AT BS 1183 TENSION TIE IS CORRODED. REMOVED CORRODED STRINGER SECTION, 24" LENGTH. FABRICATED NEW STR SE CTION FROM BAC1498-147, PO NR 3345302, 24" BY 5.875" AND STR SPLICE FROM BAC1498-131, PO NR 9003505, 20" LONG, PER B727 SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9. TREATED, PRIMED, AND INSTALLED REPAIR PARTS PER B727 SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2007050300368 20070503 00368 NM 2007 5 3 2007UALA01301 1 20070425 A 5330 SKIN BOEING 737 737322 1384676 NM FUSELAGE SCRATCHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 UPPER FUSELAGE AT BS 269 & STR 3L SKIN HAS DEEP SCRATCHES. MAJOR REPAIR ACCOMPLISHED: BLENDED OUT SCRATCHES. FABRICAT ED & INSTALLED FILLER, DOUBLER & TRIPLER EXTERNAL REPAIR. 2 L 7 2 4F RT A16WE 2007050400006 20070504 00006 NM 2007 5 4 ASAA0741625 1 20070502 A 5330 6552988121 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 776AS 25109 OUTWARD DING IN FUSELAGE SKIN REMOVED SKIN DAMAGE BY DRILLING A 0.1935" HOLE INSTALLED A BACR15BB6 RIVET IAW ASA EA 5330 02205 REV NEW AND AAR EA 112004 REV IR. 2 L 7 2 4F RT A16WE 2007050400011 20070504 00011 WP 2007 5 4 07FDEA01683 1 20070502 A 5512 SKIN DOUG DC10 DC1010 3022110 WP HORIZONTAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 LT HORIZONTAL STAB EXTERNAL SKIN HAS CORROSION ON UPPER SURFACE AT REAR SPAR XE 48.5. ALL WORK ACCOMPLISHED ON FEDEX EA .8-5500-110623-STAB, LT SIDE-UPPER AFT SPAR. 2 L 7 3 4F A22WE 2007050400013 20070504 00013 EU 2007 5 4 MALA070058 1 20070501 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 294-300 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 SEAT TRACK AT LBL 18.3, IS CORRODED OUT OF LIMITS, ON A PREVIOUS REPAIR, BETWEEN FS 294 AND 300. REMOVED AND REPLACED T HE REPAIR IAW MESABA EO#S53342. REF: EAMS WORK ORDER 216320 TASK 1518. 2 L 7 2 4T RT A52EU 2007050400022 20070504 00022 EU 2007 5 4 07FDEA01649 1 20070427 A 5730 SKIN AIRBUS 310 A310203 3930313 EU LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 408FE 257 L-WING TE BOTTOM SKIN AT PANEL 581AB CUTOUT HAS CRACK ON LOWER SKIN RIB 11 WITH APPROX 0.75 IN LONG REF N00166 STOP DRIL LED CRACK, DRILLED UP DOUBLER AND COLDWORKED AND INSTALLED IAW EA 6-5710-107726 AND SB A310-57-2066. 2 L 7 2 4F RT A35EU 2007050400037 20070504 00037 EA 2007 5 4 SWIA200718173 1 20070322 A 2510 SEAT BACK CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 925SW 7682 PILOT SEAT RIGHT BACK SUPPORT CRACKED, DISCOVERED AT C-CHECK, INSTALLED NEW SUPPORT P/N 1C3076-2AJT IAW CMM 25-14-10. 2 L 7 2 4F RT A21EA 2007050400041 20070504 00041 EA 2007 5 4 SWIA200718177 1 20070322 A 5210 ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 925SW 7682 CRACK AT PAX DOOR STRUCTURE ANGLE INSIDE 832AR CUT OUT, DISCOVERED AT C-CHECK. INSTALLED NEW DOUBLER ANGLE P/N 601R-318 094-2 AS PER CRJ200 SRM 51-42-06 PG 5-19 AND CRJ200 SRM 51-42-21 PG 15-19. 2 L 7 2 4F RT A21EA 2007050400047 20070504 00047 NM 2007 5 4 SWAA072193 1 20070502 A 5315 6545812 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND FLOOR BEAM CRACKED AT BS 328, RBL 50. REPAIRED FLOOR BEAM PER SRM. 2 L 7 2 4F RT A16WE 2007050400065 20070504 00065 WP 2007 5 4 UPS07849727 1 20070414 A 5340 ATTACH FITTING DOUG DC8 DC873F 302199F WP FS 901 L19R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 901 L19R. REMOVED CRACKED FITTING AT STA 901 L19R IAW SRM 51-1-20D. L OCATED DRILLED UP, AND INSTALLED REPLACEMENT FITTING AT STA 901 L19R IAW SRM 51-3-2, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007050400073 20070504 00073 2007 5 4 UPS07M49726 4 20070430 A 2565 COVER DOUG MD11 MD11F 3023600 NM LT ESCAPE SLIDE UNSECURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 LEFT SLIDE PACK COVER (EMERG EGRESS NOT SEATED PROPERLY). RESECURED COVER. 2 L 7 3 4F RT A22WE 2007050400087 20070504 00087 NM 2007 5 4 SWAA072203 1 20070502 A 5322 6546569 SHEAR TIE BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. R&R SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007050400093 20070504 00093 NM 2007 5 4 SWAA072178 1 20070502 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 9L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050400099 20070504 00099 NM 2007 5 4 SWAA072183 1 20070502 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 8L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050400101 20070504 00101 NM 2007 5 4 SWAA072181 1 20070502 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 16L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050400110 20070504 00110 NM 2007 5 4 SWAA072186 1 20070502 A 5523 69633918 BOLT BOEING 737 7373H4 1384600 NM LT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. R&R NR 4 HINGE BUSHING AND BOLT PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400111 20070504 00111 NM 2007 5 4 SWAA072187 1 20070502 A 5523 69633918 BOLT BOEING 737 7373H4 1384600 NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. R&R NR 4 HINGE BUSHING AND BOLT PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400121 20070504 00121 NM 2007 5 4 SWAA072191 1 20070502 A 5523 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED BRDG CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. R&R NR 1 HINGE BEARING AND BUSHING PER MM. 2 L 7 2 4F RT A16WE 2007050400159 20070504 00159 NM 2007 5 4 USAA070336 1 20070501 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 503UW 23237 BS 727D, JUST ABOVE S-10L. FAB'D & INSTALLED DOUBLER PER SRM 53-00-01, REP 31. DEFECT SIZE: 3" 2 L 7 2 4F RT A16WE 2007050400166 20070504 00166 EU 2007 5 4 USAA070338 1 20070501 A 5320 SILL AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 170US 1462 LT AFT DOOR SILL AT FWD END FR 66. REPAIRED PER EA 84449 & SRM 53-41-14 PRIN NR 6. DEFECT SIZE: 5/8" DIA. 2 L 7 2 4F RT A28NM 2007050400183 20070504 00183 NM 2007 5 4 AALA20070714 1 20070419 A 3350 LENS BOEING 767 767323 1385205 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 380AN 25449 MIA EMERGENCY LIGHT AT SEAT 13H HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 13H. SYSTEM GROUND CHECKE D NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A1NM 2007050400189 20070504 00189 NM 2007 5 4 AALA20070711 1 20070412 A 2150 ACM BOEING 767 767223 1385123 NM A/C BAY SEIZED A AALA O OTHER E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 21 328AA 22328 JFK INFLIGHT T40/12APR FLIGHT ATTENDANT REPORTED LOUD NOISE UNDER BUSINESS CLASS GALLEY FOLLOWED BY VIBRATION AND SMOK E IN CABIN. LANDED JFK WITHOUT INCIDENT. FOUND LEFT HAND AIR CYCLE MACHINE SEIZED. REPLACED LEFT HAND AIR CYCLE MACHI NE. ALSO REPLACED A PRECAUTION LEFT HAND LOW LIMIT VALVE AND LEFT HAND TEMPERATURE CONTROL VALVE. SYSTEM GROUND CHECKE D NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A1NM 2007050400197 20070504 00197 NM 2007 5 4 AALA20070699 1 20070417 A 3350 LENS BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 183AN 29593 MIA EMERGENCY LIGHT AT FORWARD RIGHT NUMBER ONE DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT FORWARD RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A2NM 2007050400207 20070504 00207 EU 2007 5 4 AALA20070697 1 20070417 A 2910 661616160280 HYDRAULIC LINE AIRBUS 300 A300B4605R 3930308 EU LT PYLON CHAFED A AALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 21 70072 515 SJU INFLIGHT T1845/17APR GREEN HYDRAULIC SYSTEM FLUID LOSS. MANUALLY LOWERED LANDING GEAR. LANDED SJU WITHOUT INCIDEN T. LOST NOSE WHEEL STEERING. FOUND LEFT ENGINE PYLON FLEXIBLE HOSE CHAFED AGAINST PIPE AND LEAKING FLUID THROUGH PIN H OLE. REPLACED HYDRAULIC LINE ON NUMBER ONE ENGINE PYLON AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A35EU 2007050400208 20070504 00208 CE 2007 5 4 DXTA200702166 1 20070501 A 2120 UNKNOWN CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE CABIN SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 606QS 5605338 CABIN FILLED WITH SMOKE WHEN LT ENGINE WAS STARTED (APU WAS ON- ON THE GROUND. [SUP 05-16-07] REMOVED & REPLACED APU I AW 560XL M.M. CHAPTER 49-10-00. OPERATION AND LEAK CHECKS GOOD. REMOVED UNIT HRS. 140.3 CYL. 304. INSTALLED UNIT HOURS 2 424.3 CYCLES 3905. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007050400209 20070504 00209 NM 2007 5 4 AALA20070693 1 20070416 A 3350 SWITCH BOEING 777 777223 1385213 NM CABIN FAULTY A AALA O OTHER O OTHER CR CRUISE 1 SW 21 793AN 30255 LHR INFLIGHT T134/16APR DURING FLIGHT ALL EMERGENCY LIGHTS CAME ON. CYCLED EMERGENCY LIGHT SWITCH SEVERAL TIMES UNTIL LIGHT EXTINGUISHED AND SYSTEM WORKED NORMAL. LANDED LHR WITHOUT INCIDENT. TESTED ALL EMERGENCY LIGHTS. COULD NOT DUPL ICATE FAULT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT T00001SE 2007050400217 20070504 00217 WP 2007 5 4 AALA20070702 1 20070417 A 3350 LENS DOUG DC9 DC982 3022082 WP CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7549A 53031 LGA EMERGENCY LIGHT AT GALLEY HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT GALLEY. SYSTEM GROUND CHECKED NO RMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2007050400218 20070504 00218 NM 2007 5 4 AALA20070705 1 20070417 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 915AN 29516 TUL EMERGENCY LIGHTS AT STATION 727 CENTER IN MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT STATI ON 727 CENTER IN MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A16WE 2007050400219 20070504 00219 NM 2007 5 4 AALA20070706 1 20070417 A 3350 8200037702 LENS BOEING 737 737823 13844BZ NM CABIN CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 915AN 29516 TUL EMERGENCY LIGHT AT STATION 628 LEFT BUTTLINE 60 FOR OVERWING EXIT LOCATOR HAS CRACKED LENS. REPLACED LENS FOR EMER GENCY LIGHT AT STATION 628 LEFT BUTTLINE 60 FOR OVERWING EXIT LOCATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A16WE 2007050400228 20070504 00228 WP 2007 5 4 AALA20070696 1 20070417 A 3231 DOOR DOUG DC9 DC982 3022082 WP NLG OPEN A AALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SW 21 234AA 49181 MEM INFLIGHT T383/17APR DURING GEAR RETRACTION CREW REPORTED EXTREME AIRFRAME VIBRATION. RETURNED TO MEM AND LANDED WI THOUT INCIDENT. WHEN LOWERED GEAR FOR LANDING VIBRATION DIMINISHED. NO UNSAFE GEAR INDICATIONS. UPON INSPECTION IT AP PEARED ONE NOSE GEAR DOOR HAD NOT BEEN CLOSED. INSPECTED NOSE GEAR DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLO SED) 2 L 7 2 4F A6WE 2007050400230 20070504 00230 WP 2007 5 4 AALA20070692 1 20070415 A 3222 SEAL DOUG DC9 DC982 3022082 WP NLG STRUT DAMAGED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 553AA 53083 JFK INFLIGHT T1977/15APR NOSE LANDING GEAR WOULD NOT RETRACT. LANDED JFK WITHOUT INCIDENT. REPLACED NOSE LANDING GEA R STRUT SEALS AND SERVICED NOSE LANDING GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2007050400231 20070504 00231 NM 2007 5 4 AALA20070698 1 20070417 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39356 24037 MIA EMERGENCY LIGHT AT OVERHEAD SEAT 31J INOPERATIVE. CLEANED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT OVERHEAD SEAT 31J. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A1NM 2007050400235 20070504 00235 WP 2007 5 4 ABXA070144 1 20070406 A 5330 591970731 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 1.125" LFEC CRACK INDICATION BETWEEN FASTENERS AT LOWER FORWARD CORNER. FASTENERS ARE AT EDGE OF CUTOUT AND COMMON TO D OOR SEAL DEPRESSOR. REPAIRED AFT LOWER CARGO LOWER FORWARD CORNER IAW DC9 SRM. 2 L 7 2 4F A6WE 2007050400237 20070504 00237 WP 2007 5 4 ABXA070146 1 20070406 A 5320 592457545 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 FLOOR SUPPORT CHANNEL EXFOLIATED IN 3 PLACES - FS 365 TO 380, LONGERON 28 LEFT. REPAIRED AREA IAW DC9 SRM. 2 L 7 2 4F A6WE 2007050400238 20070504 00238 WP 2007 5 4 ABXA070147 1 20070406 A 5420 991550032 ANGLE DOUG DC9 DC932 3022066 WP RT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 ANGLE CRACKED - PYLON AFT SPAR, AFT SIDE, LOWER STRAP, OUTBOARD END - JUST INBOARD OF AFT ENGINE MOUNT. REMOVED AND REP LACED ANGLE IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2007050400239 20070504 00239 WP 2007 5 4 ABXA070140 1 20070405 A 5220 59131951 DOOR FRAME DOUG DC9 DC932 3022066 WP EMERGENCY EXIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 RIGHT FORWARD OVERWING EXIT DOOR HAD CRACKED DOOR OUTER FRAME IN 1 PLACE AT SEAL SUPPORT FITTING. REPAIRED CRACK IAW DC 9 SRM. 2 L 7 2 4F A6WE 2007050400240 20070504 00240 WP 2007 5 4 ABXA070141 1 20070405 A 5220 59131951 DOOR FRAME DOUG DC9 DC932 3022066 WP EMERGENCY EXIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 LEFT AFT OVERWING EXIT DOOR HAD CRACKED DOOR OUTER FRAME IN 3 PLACES AT SEAL SUPPORT FITTINGS. REPAIRED AREA IAW DC9 SR M. 2 L 7 2 4F A6WE 2007050400242 20070504 00242 WP 2007 5 4 ABXA070143 1 20070405 A 5310 5912285509 RETAINER DOUG DC9 DC932 3022066 WP WINDOW FRAME CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 CRACK IN UPPER FORWARD CORNER OF WINDOW RETAINER JUST AFT OF STA 699 FRAME. REPAIRED AREA IAW REA D956-55634-MR. 2 L 7 2 4F A6WE 2007050400243 20070504 00243 WP 2007 5 4 ABXA070148 1 20070410 A 5347 S2914913M24000 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 SEAT TRACK CORRODED LOWER FLANGE AND UNDERSIDE OF TRACK AT STA 560 TO 600 LEFT BUTT LINE 12. REMOVED AND REPLACED SEAT TRACK FS 49 L - 606 LEFT BUTT LINE 1L IAW DC9 SRM 53-05. 2 L 7 2 4F A6WE 2007050400249 20070504 00249 NM 2007 5 4 CALA0700209 1 20070425 A 5311 6546557 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 FOUND CRACKED FRAME AT STA 887 NSTR 9RT. REPAIRED IAW ECRA 5310-04623. 2 L 7 2 4F RT A16WE 2007050400250 20070504 00250 NM 2007 5 4 CALA0700210 1 20070425 A 5311 6546554 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 FOUND CRACKED FRAME AT STA 847 STR 9RT. REPAIRED IAW ECRA 5310-04624. 2 L 7 2 4F RT A16WE 2007050400251 20070504 00251 NM 2007 5 4 CALA0700211 1 20070425 A 3350 D71701100 BATTERY PACK BOEING 737 737824 13844BZ NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12216 28776 EMERGENCY PATH LIGHTS INOP BETWEEN ROWS 15ABC AND 24ABC. REPAIRED IAW AMM 33-51-06. 2 L 7 2 4F RT A16WE 2007050400252 20070504 00252 NM 2007 5 4 CALA0700212 1 20070425 A 5311 6546554 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 FOUND CRACKED FRAME AT STA 847 STR 9LT. REPAIRED IAW ECRA 5310-04624. 2 L 7 2 4F RT A16WE 2007050400255 20070504 00255 NM 2007 5 4 CALA0700214 1 20070425 A 5320 6561777505 CHANNEL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 FOUND CRACK AT STA 360 STR 14 LEFT. REPAIRED IAW ECRA 5311-01314. 2 L 7 2 4F RT A16WE 2007050400256 20070504 00256 NM 2007 5 4 CALA0700224 1 20070502 A 5311 6520722U70 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14358 23943 INSPECTION FOUND A 1/4" CRACK IN THE FORWARD BAGGAGE BIN FORWARD FRAME AT THE FOURTH STOP PAD FROM TOP, STA 440, S13R TO S28R. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007050400257 20070504 00257 NM 2007 5 4 CALA0700225 1 20070502 A 5330 6545777 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17329 23459 INSPECTION FOUND A 1/2" CRACK IN FUSELAGE SKIN AT THE R-2 DOOR LOWER HINGE CUTOUT FWD LOWER CORNER, STA 947.5, S13R TO S 14R. THE CRACKED AREA OF SKIN WAS CUT OUT AND A REPAIR DOUBLER, TRIPLER, AND FILLER WERE INSTALLED IAW SRM 53-60-01. 2 L 7 2 4F RT A16WE 2007050400258 20070504 00258 NM 2007 5 4 CALA0700226 1 20070502 A 5314 65C385021 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14358 23943 INSPECTION FOUND A 2" CRACK IN LT KEEL BEAM AT STA 540, S29L. THE KEEL BEAM WAS REPAIRED IAW SRM 53-60-12, PAGE 206, DE TAIL NR 2. 2 L 7 2 4F RT A16WE 2007050400259 20070504 00259 NM 2007 5 4 CALA0700215 1 20070425 A 5230 6549889 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 LWR FWD CORNER NEAR LIGHTNING HOLE HAS A 1/2 IN CRACK ON INNER SKIN. REPAIRED IAW ECRA 5230-01790. 2 L 7 2 4F RT A16WE 2007050400263 20070504 00263 NM 2007 5 4 CALA0700219 1 20070427 A 5330 6545775594 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 FOUND FUSELAGE SKIN CRACKED 2 INCHES AT STA 727D, 17-23 R. REPAIRED IAW ECRA 5331-01303. 2 L 7 2 4F RT A16WE 2007050400265 20070504 00265 NM 2007 5 4 CALA0700228 1 20070503 A 5330 6545778 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17329 23459 INSPECTION FOUND A 0.65" CRACK IN FUSELAGE SKIN AT THE R-2 DOOR UPPER HINGE CUTOUT UPPER FORWARD CORNER. THE SKIN WAS R EPAIRED IAW SRM 53-60-01. 2 L 7 2 4F RT A16WE 2007050400269 20070504 00269 NM 2007 5 4 CALA0700223 1 20070501 A 5210 6551276U10 STOP FITTING BOEING 737 7373T0 1384582 NM L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14358 23943 INSPECTION FOUND A 1" CRACK IN L-1 DOOR TOP AFT STOP FITTING. THE STOP FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-0 2. 2 L 7 2 4F RT A16WE 2007050400272 20070504 00272 EA 2007 5 4 QXEA200700693 1 20070413 A 5330 SKIN PANEL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 C4 OKC - FOUND PANEL 384LB HAS MINOR CHAFFING. REPAIRED IAW SRM57-52-01, AND 51-21-11. 2 L 7 2 4F RT A21EA 2007050400274 20070504 00274 EA 2007 5 4 QXEA200700696 1 20070418 A 5730 SKIN PANEL CNDAIR CL600 CL6002C10 1390015 EA WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 C4 OKC - FOUND PANEL 632CB INNER SKIN CHAFED. REPAIRED IAW SRM 57-41-01 AND 51-21-11. 2 L 7 2 4F RT A21EA 2007050400275 20070504 00275 EA 2007 5 4 QXEA200700701 1 20070413 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 C4 OKC - LOWER TCAS ANTENNA MOUNTING SKIN HAS LIGHT CORROSION. REPAIRED IAW SRM 51-21-11, 51-21-06. 2 L 7 2 4F RT A21EA 2007050400277 20070504 00277 EA 2007 5 4 QXEA200700698 1 20070417 A 5751 SKIN CNDAIR CL600 CL6002C10 1390015 EA RT AILERON CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 C4 OKC - RIGHT AILERON CHAFED ON TOP LEADING EDGE. REPAIRED IAW SRM 57-61-01, 51-12-00 AND 51-21-11. 2 L 7 2 4F RT A21EA 2007050400281 20070504 00281 WP 2007 5 4 07FDEA01685 1 20070502 A 5320 DOUBLER DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 AFT FUSELAGE WASTE TANK COMPT, FRAME LWR FWD AND AFT CHORDS AT LONGERONS ATTACH FASTENERS HAVE CORROSION BETWEEN L49R A ND L52 AT STA 1997 REMOVED FASTENERS FROM FRAME STA 1997 L49-52 PER MD/DC 10 SRM 51-31-01 VOL 2. REMOVED CORROSION PER MD/DC10 SRM 51-21-01 VOL II ORIG THICKNESS IS .071 PER DOUGLAS DRAWING 34929209 REV C. REMAINING THICKNESS IS .058 AND IS FOUND TO BE WITHIN LIMITS PER MD/DC10 SRM 53-00-01 FIG 1B VOL 1. DOUBLER WAS FOUND TO BE CORRODED AND REQUIRED TO BE FABED PER MD10/DC10 SRM 53-30-00 FIG 5 VOL1. DRILLED UP PER 51-31-01 PAGE 2 VOL II, ALODINED PER MD/DC10 51-21-01 PAGE 31 VOLII PRIMED PER 51-21- 01 PAGE 24 VOLI. INSTALLED PER 51-31-01 VOL II. 2 L 7 3 4F A22WE 2007050400283 20070504 00283 NM 2007 5 4 07FDEA01687 1 20070503 A 5753 SKIN DOUG MD11 MD11 3023602 NM T/E FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 RIGHT WING, OUTBOARD FLAP INBOARD TRAILING EDGE UPPER SURFACE FOUND DELAMINATED 5" BY 7" (LENGTH X WIDTH). REMOVED AN D REPLACED AS PER AMM 20-50-02. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050400284 20070504 00284 NM 2007 5 4 07FDEA01688 1 20070503 A 5753 SKIN DOUG MD11 MD11 3023602 NM T/E FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 RIGHT WING OUTBOARD FLAP CENTER TRAILING EDGE LOWER SURFACE FOUND DELAMINATED 4" BY 4" (LENGTH X WIDTH). [SUP 05-15-0 7] REMOVED AND REPLACED AS PER AMM 20-50-02. 2 L 7 3 4F RT A22WE 2007050400285 20070504 00285 NM 2007 5 4 07FDEA01689 1 20070503 A 5753 FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 LEFT WING OUTBOARD FLAP INBOARD AFT HINGE FORWARD FITTING INBOARD CENTER HOLE FOUND WITH CORROSION DURING ACCOMPLISHMENT OF EO 1-5750-7-5008. ORIGINAL HOLE DIAMETER = 0.580"; FINAL HOLE DIAMETER = 0.657". [SUP 05-14-07] COMPLIED WITH FED EX EA 1-5750-109875, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050400286 20070504 00286 NM 2007 5 4 07FDEA01690 1 20070503 A 5753 FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 LEFT WING OUTBOARD FLAP INBOARD AFT HINGE FORWARD FITTING INBOARD CENTER HOLE FOUND WITH CORROSION DURING ACCOMPLISHMENT OF EO 1-5750-7-5008. ORIGINAL HOLE DIAMETER = 0.580"; FINAL HOLE DIAMETER = 0.656". [SUP 05-14-07] COMPLIED WITH FEDE X EA 1-5750-109875, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050400288 20070504 00288 NM 2007 5 4 07FDEA01692 1 20070503 A 5730 SKIN DOUG MD11 MD11 3023602 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RIGHT WING, LEADING EDGE LOWER SURFACE 619CB PANEL FWD I/B SIDE CORNER FOUND 5/8 INCH CRACK AT XOS 607. [SUP 05-22-07] REPAIR CARRIED OUT AT RIGHT WING - LEADING EDGE LOWER SURFACE 619CB PANEL FWD I/B SIDE CORNER, XOS 607 AS PER SRM 5 7-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050400289 20070504 00289 EU 2007 5 4 07FDEA01651 1 20070427 A 5522 SKIN AIRBUS 310 A310203 3930313 EU LT ELEVATOR DEBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 408FE 257 LT ELEVATOR LOWER SKIN IS DISBONDED AT RIB 13 ,5 IN FROM T/E 7.5 IN LONG. REPAIRED DAMAGED AREA IAW EA 6-5520-110453. 2 L 7 2 4F RT A35EU 2007050400291 20070504 00291 WP 2007 5 4 07FDEA01676 1 20070501 A 5514 ALC750212 FLANGE DOUG DC10 DC1010 3022110 WP HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 RT HORIZONTAL STAB CENTER LE SECTION OB UPPER ATTACH POINT FLANGE CRACKED AT NUTPLATES. REMOVED AND REPLACED RT HORIZON TAL LE SECTIONS CENTER OUTBOARD UPPER "T" CAP CHORD AT XFS 241, IAW DC/MD 10-10 SRM 51-31-01 VOL II AND 51-33-01 VOL II. 2 L 7 3 4F A22WE 2007050800157 20070508 00157 SW 2007 5 8 PNSA070301 1 20070315 A 7712 31024766 SIGNAL COND UNIT SWRNGN SA227 SA227AC 8780603 SW INDICATION SYS BROKEN A PNSA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 AL 03 2719H AC713B AFTER STARTING THE TAKEOFF ROLL, DID NOT GET TORQUE RISE. ABORTED TAKEOFF. POSSIBLY A STUCK GAUGE, SO TRIED IT AGAIN G ETTING THE SAME PROBLEM, ABORTED AND RETURNED TO THE GATE. REMOVED AND REPLACED TORQUE GAUGE AND TORQUE SIGNAL CONDITIO NER. 2 L 7 2 4T RT A8SW 2007050400293 20070504 00293 WP 2007 5 4 07FDEA01679 1 20070501 A 5320 FITTING DOUG MD10 MD1010F 3022112 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 MAIN CARGO DOOR-LOWER JAMB FITTING NR 5 SHOWS CRACK/CORROSION AT LOWER HOLE. 2 L 7 3 4F RT A22WE 2007050400294 20070504 00294 WP 2007 5 4 07FDEA01671 1 20070430 A 5514 ANGLE DOUG MD10 MD1010F 3022112 WP HORIZ STAB CRACKED A FDEA K NONE O OTHER NR NOT REPORTED 1 SO 25 68050 47804 RT HORIZONTAL L/E CENTER I/B SECTION UPPER I/B ATTACHED FLANGE CRACKED MARKED. REMOVED CRACKED RT HORIZ L/E T-CAP SECTI ON AT UPPER I/B STA XFS 166 IAW DC/MD 10 SRM 55-00-01 FIG, 6 VOL 1, AND INSTALLED ANGLE REPAIR PER MD/DC10 SRM 55-00-01 FIG, 6 VOL 1. 2 L 7 3 4F RT A22WE 2007050400295 20070504 00295 EU 2007 5 4 07FDEA01653 1 20070427 A 5330 SKIN AIRBUS 310 A310203 3930313 EU FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 411FE 359 PREVIOUS REPAIR LOCATED ON R/SIDE FUSELAGE SKIN BETWEEN FR 66 TO 67 BETWEEN STR 35TO 38 RT HAS AN EXTERNAL REPAIR DOUBLE R MEASURING 8.8 BY 11.9. REPAIR REVIEWED AND FOUND NOT TO BE IAW A310-200 SRM 53-10-12 FIG 226 SHEET 2. REWORKED REPAI R IAW A310-200 SRM 53-10-12, FIG 226 SHEET 2 REF N00503. 2 L 7 2 4F RT A35EU 2007050400298 20070504 00298 NM 2007 5 4 07FDEA01657 1 20070428 A 5320 AEA06612 LINK DOUG MD11 MD11 3023602 NM CENTER LG WW WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 CENTER LANDING GEAR, WHEEL WELL BRACKET LOCK LINK CHAMPER FOUND WORN. [SUP 05-04-07] REPAIRED AS PER SRM 53-40-00 VOLU ME I, FIGURE 10. REPAIR CALSSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050400299 20070504 00299 NM 2007 5 4 07FDEA01658 1 20070428 A 5720 ANGLE DOUG MD11 MD11 3023602 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 RIGHT WING, LEADING EDGE CAVITY AT ABOUT XOS 774 STRIP ANGLE FOUND WITH APPROX 0.3124 INCH CRACKED. [SUP 05-14-07] RT F IXED LEADING EDGE STRINGER, CRACK REPAIR. REPAIR CLASSIFIED AS MINOR PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050400300 20070504 00300 NM 2007 5 4 07FDEA01659 1 20070428 A 5720 ANGLE DOUG MD11 MD11 3023602 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 RIGHT WING, LEADING EDGE CAVITY AT ABOUT XOS 659 STRIP ANGLE FOUND WITH APPROX 0.5 INCH CRACKED. [SUP 05-14-2007] FIXE D LEADING EDGE STRINGER, CRACK REPAIR. CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050400303 20070504 00303 NM 2007 5 4 07FDEA01662 1 20070430 A 5753 HINGE FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 LEFT WING, OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING OUTBOARD NR 3 BOLT HOLE FOUND CORRODED. [SUP 05-15-07] REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-00-5. COMPLY WITH FEDEX EA 1-57 10-111094. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050400304 20070504 00304 NM 2007 5 4 07FDEA01663 1 20070430 A 5753 STRUT DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 LEFT WING, OUTBOARD FLAP INBOARD HINGE FITTING AFT STRUT (P/N: ARC2126) FWD AND AFT HOLE FOUND CORRODED. [SUP 05-15-0 7] COMPLIED WITH FEDEX E.A. 1-5750-111092. 2 L 7 3 4F RT A22WE 2007050400305 20070504 00305 NM 2007 5 4 07FDEA01664 1 20070430 A 5753 HINGE FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 LEFT WING, OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING INBOARD NR 1 BOLT HOLE FOUND CORRODED. REMOVED & REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT & TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094. 2 L 7 3 4F RT A22WE 2007050400307 20070504 00307 NM 2007 5 4 07FDEA01667 1 20070430 A 5753 HINGE FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 LEFT WING, OUTBOARD FLAP INBOARD HINGE AFT SUPPORT FITTING AFT BOLT HOLE FOUND CORRODED. REMOVED & REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT & TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094. 2 L 7 3 4F RT A22WE 2007050400308 20070504 00308 NM 2007 5 4 07FDEA01668 1 20070430 A 5720 STIFFENER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 LEFT WING LEADING EDGE CAVITY STIFFENER FOUND WITH APPROX 0.25 INCH CRACK AT XOS 667. [SUP 05-15-07] REPAIRED AS PER FEDEX EA 1-5720-109874, WINGS - LEADING EDGE STRINGER - CRACK REPAIR. REPAIR CLASSIFIED AS MINOR PER GMMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050400309 20070504 00309 NM 2007 5 4 07FDEA01669 1 20070430 A 5730 SKIN DOUG MD11 MD11F 3023600 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 LEFT WING, CRACK INDICATIONS (APPROX 0.0156 INCH DEPTH ) REVEALED IN FIVE (5) EACH FASTENER HOLES TOWARDS THE EDGE OF AC CESS CUTOUT LOWER SKIN ACCESS DOOR (BETWEEN XOR=683.4 AND XOR=713.6). REPAIRED AS PER FEDEX EA 1-5710-109878, REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050400310 20070504 00310 NM 2007 5 4 07FDEA01670 1 20070430 A 5730 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 RIGHT WING, CRACK INDICATIONS (APPROX 0.0156 INCH DEPTH) REVEALED IN SIX (6) EACH FASTENER HOLES TOWARDS THE EDGE OF ACC ESS DOOR CUTOUT LOWER SKIN (BETWEEN XOR=683.4 AND XOR=713.6). [SUP 05-14-07] REPAIRED AS PER FEDEX EA 1-5710-109877, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050700002 20070507 00002 CE 2007 5 7 DA62007F00006 1 20070315 A 3246 BEARING BEECH 60 B60 1153605 CE LYC O540 TIO540* 41532 EA LG WHEEL CORRODED E DA6A O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SW 09 171EC P288 DURING ANNUAL INSPECTION, FOUND WHEEL BEARINGS AND RACES TO BE WORN AND CORRODED. ALSO, FOUND THAT THERE WERE (2) DIFFE RENT TYPES OF GREASE USED IN THE WHEEL BEARINGS AND THE MANUAL REF A MIL-G-3545 ONLY, WHICH IS A HIGH TEMP GREASE AND IS RED OR AMBER IN COLOR. THE GREASE FOUND ON THE NOSE WHEEL BEARINGS WAS LT GRAY ALMOST WHITE AND THE MAIN WHEEL BEARING GREASE ON THE LT SIDE APPEARED TO BE CORRECT AND THE RT SIDE WAS BLACK IN COLOR AND HAD A ROUGH FEEL TO IT. MAIN TIRES WERE DOCUMENTED AS REMOVED AND REPLACED. LOG ENTRY DATE 12/20/2006. BEARING AND RACES WILL BE REMOVED AND REPLACED. (K) 1 L 7 2 3O 3 O A12CE E14EA 2007050700011 20070507 00011 EA 2007 5 7 TRAX200700588 1 20070429 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 916EV 7757 OVERWING EXIT ON RIGHT SIDE FWD EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007050700014 20070507 00014 EA 2007 5 7 A6WA200740200 1 20070417 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 GL 31 448AW 7814 FLAPS FAIL IN FLIGHT WHEN FLAPS 8 DEGREES SELECTED, FLAPS FAILED AT 0 DEGREES. VISUALLY INSPECTED EACH OB FLAP NO EVIDE NCE OF TWISTING, SKEWING OR ABNORMAL DEFORMATION NOTED. OB FLAP POSITION INDICATION ARE NOT OUTSIDE GO RANGE. FLAP FAI L MESSAGE NOT ILLUMINATED, FLAPS OPS NORMAL, IAW AWAC SUPP 98-018B. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007050700018 20070507 00018 WP 2007 5 7 AMTA200700200 1 20070422 A 3411 0856CR9 PROBE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE PITOT/STATIC UNSERVICEABLE A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 163AT 13087 13087 1229 CAPT ALTIMETER READ 250 FT LOW AT FL310. VERIFIED BY INS AND ATC GROUND READOUT. REMOVED AND REPLACED CAPT UPPER LT PI TOT STATIC PROBE IAW AMM 34-13-01. PERFORMED PITOT STATIC LEAK CHECK, SYSTEM OPS CHECK GOOD. (K) 2 L 7 3 4F 4 F A23WE E12EU 2007050700019 20070507 00019 EA 2007 5 7 WAI2007F00001 1 20070306 A 2612 24412086 FIRE LOOP CNDAIR CL600 CL6001A11 1900302 EA LYC ALF502 ALF502* 41580 EA LT NACELLE SHORTED E WAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 403WY 8054 1059 FLIGHT CREW REPORTED LT ENGINE FIRE DETECTION FAIL LIGHT CAME ON JUST PRIOR TO ROTATION, THEN FIRE LIGHT CAME ON JUST PR IOR TO ROTATION, THEN FIRE WARNING CAME ON AT 1,500 FT DURING CLIMB. STAYED ON AFTER DISCHARGING BOTH FIRE BOTTLES. RET URNED TO BASE AFTER LANDING, APPEARED TO BE NO FIRE. FOUND LT ENGINE PYLON FIRE LOOP BAD AND LT ENGINE CORE FIRE LOOP BA D. REPLACED IAW MM. PERFORMED FIRE DETECTION SYSTEM OPS CHECK, NO DEFECTS NOTED. (K) 2 L 7 2 4F 4 F RT A21EA E6NE 2007050700021 20070507 00021 CE 2007 5 7 DA62007F00005 1 20070315 A 5610 WINDOW BEECH 60 B60 1153605 CE LYC O540 TIO540* 41532 EA COCKPIT MISINSTALLED E DA6A K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 09 171EC P288 DURING ANNUAL INSPECTION, PILOT AND CO-PILOT SIDE WINDOWS SEALANT WAS FOUND TO BE CRACKED AND FULL OF AIR POCKETS. FOUN D SEALANT TO BE IMPROPERLY APPLIED TO ATTEMPT TO RESEAL WINDOWS. AFTER REMOVAL OF THE SIDE WINDOWS, FOUND WASHERS IN SE ALANT APPARENTLY USED AS SPACERS BETWEEN THE WINDOW AND FRAME, BUT THERE IS NO REFERENCE FOR SPACERS TO BE INSTALLED AT THE WINDOW LOCATIONS IAW MM. SPACERS WILL BE REMOVED AND WINDOWS WILL BE SEALED AND REINSTALLED IAW MM. (K) 1 L 7 2 3O 3 O A12CE E14EA 2007050700022 20070507 00022 EA 2007 5 7 A6WA200740155 1 20070325 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 461AW 7870 FLAPS FAIL CAUTION MESSAGE ON DEPARTURE. INSPECTED FLAPS, NO EVIDENCE OF SKEW FOUND. RESET FLAP SYSTEM IAW AMM SUPPLEM ENT 98-018B. FLAPS OPS CHECK OK. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007050700026 20070507 00026 NM 2007 5 7 AMTA200700190 1 20070412 A 3350 LIGHT BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE CABIN SHORTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 31 514AT 27971 EMERGENCY FLOOR PATH LIGHTING FROM R-3 TO ROW 31 INOPERATIVE. TROUBLESHOT, FOUND LIGHT ASSY AT ROW 30-31 SHORTED. REPL ACED LIGHT ASSY ALL OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007050700027 20070507 00027 NE 2007 5 7 SWD2007F00002 2 20070319 A 7200 GAS GENERATOR AIRTRC AT802 AT802A 0390308 SW PWA PT6 PT6A67A 52043 NE FLANGE ERODED H SWDG O OTHER O OTHER NR NOT REPORTED 1 SW 11 805D 1800 902A0156 PCERD0077 AS THE HEAD BOLTS WERE BEING REMOVED FOR HSI. ONE NUT DETACHED FROM THE BOLT SHANK WITH THE THREAD INSIDE THE NUT. CLO SE INSPECTION OF THE ADJACENT BOLT REVEALED SEVERE EROSION (NOT CORROSION OR STRETCH DAMAGE) TO THE BOLT SHANK. IT WAS FURTHER NOTED AND PHOTOGRAPHED BY THE MFG REP THAT THE EXHAUST DUCT FLANGE AND GAS GENERATOR FLANGE IN THE BROKEN BOLT A REA HAD MATERIAL LOSS THAT WAS ALLOWING P3 AIR LOSS THAT MAYBE ATTRIBUTED TO THE HIGHER THAN NORMAL OIL TEMP INDICATION ON THE GROUND.. THE AIR LEAK IS VENTING ONTO THE SCAVENGE OIL TUBE COUPLING. MFG REP SAYS THAT THIS IS AN ISOLATED CAS E AND IS NOT A SAFETY OF FLIGHT ISSUE AS THAT THERE ARE MANY MORE BOLTS THAT HOLD C-FLANGE TOGETHER. (K) 1 L 7 1 3T 4 T NC A19SW E26NE 2007050700030 20070507 00030 EU 2007 5 7 WAI2007F00000 1 20070305 A 2133 1032788 OUTFLOW VALVE ISRAEL 1124 1124A 4500103 EU GARRTT TFE731 TFE731* 01518 WP CABIN PRESSURE LEAKING E WAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 325LW 5961 334 AIRCRAFT PRESSURIZATION INTERMITTENT. PRESSURIZATION WILL WORK WITH NO DEFECTS ON ONE FLIGHT; THE VERY NEXT FLIGHT, SYS TEM WOULD NOT WORK AT ALL. CLEANED OUTFLOW AND SAFETY VALVES; STILL INTERMITTENT. INSTALLED NEW SAFETY AND OUTFLOW SOL ENOID VALVES (A AND B), INSTALLED OVERHAULED SAFETY VALVE, AND RIGGED LEFT MLG GROUND CONTACT SWITCH IAW MM. PERFORMED SEVERAL FUNCTIONAL CHECK FLIGHT, NO DEFECTS NOTED. (K) 2 M 7 2 4F 4 F A2SW E6WE 2007050700031 20070507 00031 NE 2007 5 7 FSE2007F00000 2 20070223 A 7261 AS3209222 O-RING CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE OIL CAP LEAKING A FSEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 65 716SX 4018 5600281 (REF NR N716SX-07-1) FL 300, CREW NOTED DECREASE IN LT ENGINE OIL PRESSURE. ENGINE WAS SHUTDOWN IAW EMERGENCY PROCEDUR ES. AIRCRAFT CONTINUED TO SERVICE FACILITY. MAINTENANCE DETERMINED THAT OIL FILLER CAP WAS LEAKING AT HIGH POWER SETTI NGS DUE TO DAMAGED OR DEFECTIVE O-RING. IAW MM, NO ADDITIONAL INSPECTION WERE REQUIRED. O-RING WAS REPLACED AND FILLER CAP WAS ADJUSTED IAW MM. ENGINE SERVICED WITH OIL AND RETURNED TO SERVICE. (K) 2 L 7 2 4F 4 F RT A22CE E25EA 2007050700032 20070507 00032 NE 2007 5 7 TRAX200700606 2 20070502 A 7320 DRAIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENGINE LEAKING A ASOA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 870AS 7530 STRONG FUEL SMELL IN FLT DECK ON DESCENT AND AT GATE LT ENG WAS LEAKING FUEL FROM DRAIN. FLT 4532 CX. 2 L 7 2 4F 4 F RT A21EA E15NE 2007050700034 20070507 00034 NM 2007 5 7 AMTA200700197 1 20070418 A 2560 BATTERY BOEING 737 73783N 13844HI NM FLASHLIGHT INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 310TZ 28243 FLASHLIGHT IN AFT GALLEY INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IN AFT GALLEY REF 25-64-00. OPS CHECK GO OD. (K) 2 L 7 2 4F RT A16WE 2007050700035 20070507 00035 EA 2007 5 7 TRAX200700591 1 20070430 A 3350 BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 760EV 10212 LEFT OVERWING EMERGENCY EXIT, LOWER EMERGENCY EXIT SIGN IS INOP. FOUND NR 3 BATTERY PACK VOLTS LOW. REMOVED AND REPLAC ED EMERGENCY LIGHT BATTERY PACK IAW CRJ 200 AMM 33-00. OPS CHECK GOOD. {SDR - CLOSED} 2 L 7 2 4F RT A21EA 2007050700036 20070507 00036 CE 2007 5 7 HYT2007F00000 1 20070401 A 5730 262207431 SKIN CESSNA 208 208B 2073701 CE PWA PT6 PT6* 52043 EA WING LE DAMAGED E HYTA O OTHER O OTHER NR NOT REPORTED 1 AL 01 900WA 208B0659 SMOKING RIVETS IN LEADING EDGE SKIN UPPER SEAM. EVERY COUNTERSUNK HOLE FROM WS 35 TO WS 141 WAS FRETTING AGAINST THE RI VET HEAD. SAME CONDITION TO SAME EXTENT ON BOTH WINGS. IT APPEARS THE SKIN WAS COUNTERSUNK TOO DEEPLY. SAME CONDITION TO LESSER EXTENT FOUND ON OTHER AC IN THE FLEET. MFG ADDRESSES THIS ISSUE IN THE SRM WITH (2) TYPES OF REPAIR DEPENDIN G ON SEVERITY OF DAMAGE. (K) 1 H 7 1 3T 3 T A37CE E2NE 2007050700037 20070507 00037 CE 2007 5 7 DA62007F00002 1 20070220 A 2750 3536415159 MOTOR BEECH 60 B60 1153605 CE LYC O540 TIO540* 41532 EA TE FLAPS DAMAGED E DA6A O OTHER O OTHER NR NOT REPORTED 1 SW 09 171EC 3373 P288 FLAPS FAILED IN DOWN POSITION ON LANDING. DURING TROUBLESHOOTING AND INSPECTION FOUND FLAP MOTOR AND WIRING TO BE SUBME RGED IN WATER APPROXIMATELY 1.5 INCHES TO 2 INCHES DEEP. AFTER WATER WAS CLEANED UP AND MOTOR WAS ALLOWED TO DRY FLAPS FUNCTIONED PROPERLY. FLAP MOTOR WILL BE REPLACED OR OVERHAULED, AC BELLY WILL BE COMPLETELY DRIVED OUT, AND ANY POSSIBL E AREAS WHERE LEAKS COULD OCCUR WILL BE INSPECTED AND CORRECTED AS NEEDED. (K) 1 L 7 2 3O 3 O A12CE E14EA 2007050700041 20070507 00041 NM 2007 5 7 AMTA200700109 1 20070223 A 2130 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN PRESSURE MALFUNCTIONED A AMTA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 11 403TZ 24664 UNABLE TO MAINTAIN 10,000 FT CABIN AT FL 250, DESCENDED TO 11,000, CABIN ALT 9500. PERFORMED RT ENGINE SINGLE PACK OPER ATOR CONFIDENCE CHECK IAW MM. AC MAINTAINED PRESSURE IAW CHECK. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2007050700043 20070507 00043 EA 2007 5 7 TRAX200700597 1 20070501 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN DETACHED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 EMERGENCY LIGHT AT TOP OF ENTRY DOOR NEED TO BE REATTACHED. FLT 4568 DEL 69 MINS. 2 L 7 2 4F RT A21EA 2007050700045 20070507 00045 CE 2007 5 7 DA62007F00007 1 20070221 A 5210 604730085601 DOOR BEECH 60 B60 1153605 CE LYC O540 TIO540* 41532 EA MAIN PAX CORRODED E DA6A K NONE O OTHER IN INSP/MAINT 1 SW 09 171EC P288 DURING ANNUAL INSP FOUND CORROSION IN THE CABIN ENTRY DOOR IN 3 LOCATIONS. FIRST LOCATION WAS AT THE MIDDLE LOCKING PIN GUIDE ANGLE PIECE. THE SECOND LOCATION IS AT THE LOWER LOCKING PIN GUIDE ANGLE PIECE AND THE THIRD LOCATION IS ON A FR AME AT THE LOWER FWD CORNER WHERE HINGE SPROCKET ATTACHES. AREAS OF CORROSION WILL BE REPAIRED BY REMOVAL AND REPLACEME NT OF ANGLES AND FRAME. (K) 1 L 7 2 3O 3 O A12CE E14EA 2007050700046 20070507 00046 2007 5 7 A6Y2007F00001 4 20070304 A 2300 COOLING FAN BEECH 58 58 1152740 CE CONT O550 IO550* SO RADIO SYSTEM OUT OF POSITION E A6YA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 09 8257H TH1650 APPROXIMATELY 20 MINUTES INTO THE FLIGHT PILOT SUSPECTED AN ELECTRICAL BURNING ODOR. HE NOTICED SOME SMOKE COMING FROM UNDER INSTRUMENT PANEL. AT THAT TIME HE COMPLETED THE MEMORY ITEMS FOR (ELECTRICAL SMOKE OR FIRE). AFTER 1 TO 2 MINUTE S SMOKE AND ODOR DISSIPATED. AFTER REGAINING RADIO COMMUNICATIONS WITH CENTER, PILOT DECLARED AN EMERGENCY AND ASKED FO R VECTORS TO NEAREST AIRPORT. PILOT ACCEPTED VECTORS TO K3BS. FLIGHT LANDED UNEVENTFULLY. RADIO COOLING FAN FOUND RUB BING BETWEEN FAN AND HOUSING. REPOSITIONED FAN INSPECTED SIMILAR COOLING FANS ACROSS FLEET. (K) 1 L 7 2 3O 3 O 3A16 E3SO 2007050700047 20070507 00047 SO 2007 5 7 BUE2007F00002 1 20070208 A 7800 NAS620548 BOLT GULSTM G1159 G1159A 3970109 SO RROYCE SPEY SPEY55515P 54521 EU EJECTOR ASSY SHEARED E BUEA K NONE O OTHER IN INSP/MAINT 1 GL 23 416WM 040 487 ( REF NR: 287N416WM) DURING INSPECTION FOUND THE RT EJECTOR OB BEARING FITTING UPPER BOLT SHEARED, LOWER BOLT BENT/BEGIN NING TO SHEAR, IB BEARING FITTING UPPER AND LOWER BOLTS BENT/BEGINNING TO SHEAR, AND THE IB AND OB TRANSLATOR LINKS BENT . REPLACED BOTH TRANSLATOR LINKS, ALL IB/OB UPPER AND LOWER BEARING FITTING BOLTS AND THE OB BEARING FITTING ASSEMBLY ( PRECAUTIONARY). (K) 2 L 7 2 4F 4 F A12EA E2EU 2007050700049 20070507 00049 NM 2007 5 7 AMTA200700187 1 20070408 A 7400 UNKNOWN BOEING 737 73783N 13844HI NM EEC WARNING MESSAGE A AMTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 11 314TZ 30640 DURING CLIMBOUT, BOTH ENG EEC`S ILLUM. ALT MODE SELECTED HELD ALT IAW PROC. REFORMED FIM PROCEDURE 73-05-00-810-811. NO FAULTS FOUND OK FOR SERVICE. (K) 2 L 7 2 4F RT A16WE 2007050700050 20070507 00050 2007 5 7 AMTA200700186 4 20070409 A 2397 9640453011 COUPLER BOEING 757 75733N 1384931 NM RROYCE RB211 RB211* 54555 NE HF RADIO DAMAGED A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 561TZ 33526 LT HF TRANSMISSION AND RECEPTION WEAK AND INTERMITTENT. REMOVED AND REPLACED LEFT HF COUPLER IAW MM 23-11-01-4, OPS CHE CKS GOOD AT THIS TIME, TRANS AND RECEPTION LOUD AND CLEAR. (K) 2 L 7 2 4F 4 F RT A2NM A12EU 2007050700056 20070507 00056 NM 2007 5 7 DLM88070395 1 20070502 A 5312 991556173 ANGLE DOUG MD88 MD88 3023688 NM PRESSURE BLKHEAD CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 AFT BULKHEAD INTERNAL ANGLE BETWEEN L28L AND L28R CORRODED. PART REPLACED. 2 L 7 2 4F RT A6WE 2007050700057 20070507 00057 NM 2007 5 7 AWXA200700549 1 20070422 A 5320 6545834552 INTERCOSTAL BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - CRACKED CABIN FLOOR INTERCOSTSAL STIFFENER, BS 328, RBL 32, WL 208. REPLACED CABIN FLOOR INTERCOSTSAL STIFFENER, BS 328, RBL 32, WL 208 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007050300374 20070503 00374 2007 5 3 2007UALA01307 4 20070425 A 2565 SLIDE BOEING 737 737322 1384676 NM L2 DOOR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 AFT ENTRY DOOR (2L) SLIDE PRESSURE INDICATOR MIGRATING AWAY FROM WINDOW VIEW. [SUP 05-16-07] REPLACED SLIDE ASSEMBLY. 2 L 7 2 4F RT A16WE 2007050300378 20070503 00378 NM 2007 5 3 2007UALA01311 1 20070424 A 7710 STALL WARNING AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 825UA 980 V10189 STALL DISPLAYED ON UPPER ECAM SCREEN DURING POWER DECELERATION. ENGINE NOT SHUTDOWN - ENG 1. CREW COMMENTS: LEVEL AT 3 7000 DURING POWER REDUCTION DUE TO LIGHT TURBULENCE- MODERATE CHOP. ENG INDICATIONS NORMAL. [06-14-07] FOUND LOOS E LINE AND FITTING AT SOLENOID 4020KS1A. REPLACED SOLENOID AND PERFORMED FUNCTION TEST. 2 L 7 2 4F 4 F RT A28NM E40NE 2007050300379 20070503 00379 NM 2007 5 3 2007UALA01312 1 20070426 A 8010 SWITCH BOEING 737 737522 138449F NM NR 1 START POPPED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 919UA 25386 CREW REPORTS NR 1 START SWITCH MADE LOUD POPPING NOISE WITH SPARKS. [SUP 05-16-07] INCORRECT INSTALLATION. THE WIRING FROM THE SWITCH WAS PINCHED BETWEEN THE SWITCH AND THE PANEL, RATHER THAN PROPERLY ROUTED BEHIND THE SWITCH. REPLACED S TART SWITCH, DAMAGED WIRES, AND DAMAGED INSULATION. 2 L 7 2 4F RT A16WE 2007050300388 20070503 00388 NE 2007 5 3 2007UALA01321 2 20070427 A 7532 BLEED VALVE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 835UA 1426 RTFL DUE TO A PRESSURIZATION PROBLEM. [06-22-07] REPLACED NR 2 BLEED AIR REGULATOR VALVE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007050300389 20070503 00389 WP 2007 5 3 ASAA0781620 1 20070427 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP COCKPIT DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 947AS 53020 COCKPIT OVERHEAD EMERGENCY LIGHTS DID NOT ILLUMINATE DURING TEST. REPLACED BATTERY PACKS. 2 L 7 2 4F RT A6WE 2007050400001 20070504 00001 WP 2007 5 4 07FDEA01673 1 20070430 A 5511 ALC0705123 RIB DOUG MD10 MD1010F 3022112 WP HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 RT HORIZONTAL STABILIZER I/B L/E SECTION NOSE O/B RIB FLANGE CRACKED XFS108, AND ATTACHED CLIP HAS SHEARED FASTENER. IN STALLED REPAIR ANGLE AND STOP DRILLED CRACK IN RT HORIZONTAL STABILIZER IN/B L/E SECTION FORMER RIB AT XFS 108 AND INSTA LLED NEW FASTENERS IAW DC/MD10 SRM 53-00-01 FIG 8, SHIT 1, PG 26B. VOL 1. 2 L 7 3 4F RT A22WE 2007050400003 20070504 00003 NM 2007 5 4 07FDEA01674 1 20070429 A 7603 BACC2A3A07670EE THROTTLE CABLE BOEING 727 727233 138408A NM ZONE 400 SHEARED A FDEA O OTHER S AFFECT SYSTEMS CR CRUISE 1 SO 25 267FE 21673 NR 1 THROTTLE BINDS 2/3 THROUGH TRAVEL. FOUND NR 1 THROTTLE CABLE BROKEN IN BELLY. LOOSE CABLE COILED IN AVIONICS BAY . FOUND THROTTLE CABLE (T1B) BROKEN AT STA 673, REMOVED FWD AND AFT CARGO CEILING PANELS FOR ACCESS TO CABLE RUN "K" FR OM STA 450 TO 980. FOUND BREAK DUE TO CABLE RUBBING ON TOPSIDE OF CARGO COMPT CEILING LIGHT FIXTURE AND WIRING {L783} P ER WDM 33-36-01. INSTALLED NR 1 THROTTLE CABLE AND RIGGED PER B727-200 AMM 76-11-000-5. NEEDS CLOSE UP AND TEST PER STEP 5D. PERFORMED TEST ENG CONTROL SYSTEM PER 727-200 MM 76-11-000-5 5D. OK TO CLOSE. LIGHT FIXTURE REMOVED AND REPL ACED CORRECTLY AND RE-WIRED PER SWPM. 2 L 7 3 4F RT A3WE 2007050400005 20070504 00005 NM 2007 5 4 ASAA0741623 1 20070502 A 5753 6546430510 DOUBLER BOEING 737 7374Q8 138447Q NM T/E FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 776AS 25109 RT IB FORE FLAP CHAFED ON AN EXITING REPAIR DOUBLER ON THE UPPER SIDE. REMOVED THE EXITING REPAIR DOUBLER AND FILLER FAB RICATED AND INSTALLED A REPLACEMENT DOUBLER AND FILLER IAW SRM 51 70 10 PARA 7 8 11 15 18 AND 20. 2 L 7 2 4F RT A16WE 2007050400016 20070504 00016 NM 2007 5 4 07FDEA01644 1 20070426 A 5754 ARB712824 RIB DOUG MD11 MD11F 3023600 NM NR 1 SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 RIGHT WING, NR 1 SLAT INBOARD RIB FOUND WITH 0.05 INCH CRACKED. [SUP 05-14-07] RIB REMOVED & REPLACED ON RT WING, NR 1 SLAT INBOARD AS PER SRM 51-35-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050400023 20070504 00023 EU 2007 5 4 07FDEA01650 1 20070427 A 5320 STRUCTURE AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 408FE 257 AFT CARGO COMPT BILGE AREA BETWEEN FR 60-61 HAS CORROSION AROUND 18 EA RIVET BUCKTAILS ON S56R. REMOVED CORROSION IAW A 310-200 SRM 51-74-10 CHECKED LIMITS IAW A310-200 SRM 53-10-00. FOUND STRG TO BE OUT OF LIMITS. REPAIRED STR IAW A310-2 00 SRM 53-10-14. 2 L 7 2 4F RT A35EU 2007050400026 20070504 00026 NM 2007 5 4 SWAA072206 1 20070502 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 435, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007050400030 20070504 00030 NM 2007 5 4 NWAA071676744 1 20070402 A 5322 TENSION TIE BOEING 747 747212F 1384851 NM BS 880 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 644NW 24177 DURING "M" CHECK, FOUND CRACKS IN TENSION TIE CHANNEL FASTENER HOLES AT BS 880 LT AND RT. REPAIRED PER EA 67-208995. 2 L 7 4 4F RT A20WE 2007050400042 20070504 00042 EA 2007 5 4 SWIA200718178 1 20070322 A 5210 MOUNT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MOTOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 925SW 7682 CRACK AT PAX DOOR ASSIST MOTOR MOUNT STRUCTURE AFT RADIUS, DISCOVERED AT C-CHECK. INSTALLED NEW STIFFENER P/N 601R 3177 45-7 P/O 27867 PER CRJ200 SRM 51-42-06 PG 4 AND 18. 2 L 7 2 4F RT A21EA 2007050400043 20070504 00043 EA 2007 5 4 SWIA200718179 1 20070322 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 925SW 7682 FLOORBEAM IS CRACKED AT LBL11 DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLE AND FILLER AT LBL9 PER CRJ200 REO 601R 53-1 1-171 REV 'D' AND CLIPS AND FILLER AT LBL9 PER REO 601R 53-11-171 REV 'D'. 2 L 7 2 4F RT A21EA 2007050400045 20070504 00045 NM 2007 5 4 SWAA072211 1 20070502 A 5310 6545807 DOOR FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED MV4 CHECK, FOUND R1 DOOR FWD STUB FRAME CRACKED AT BS 294.5, STR 12R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400048 20070504 00048 EA 2007 5 4 SWIA200718182 1 20070427 A 2760 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILERS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED LD LANDING 1 NM 07 427SW 7497 AIRCRAFT ROLLED UNCOMMANDED TO THE LEFT ON SHORT FINAL AND LANDING FLARE WITH NO CROSSWINDS. REPLACED NR 2 SECU. OPERA TIONAL CHECK AND BITE TEST GOOD, PN: 49-164-06, S/N OFF: 01501. 2 L 7 2 4F RT A21EA 2007050400053 20070504 00053 NM 2007 5 4 SWAA072210 1 20070502 A 5311 6546532 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400058 20070504 00058 EU 2007 5 4 NWAA071713247 1 20070501 A 3350 BATTERY PACK AIRBUS 320 A320212 3930322 EU EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 347NW 408 RT EMERGENCY POWER SUPPLY UNIT BATTERY PACK READS ZERO VOLTS. REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY PACK, OP CHE CKS GOOD. 2 L 7 2 4F RT A28NM 2007050400066 20070504 00066 WP 2007 5 4 UPS07849728 1 20070414 A 5340 ATTACH FITTING DOUG DC8 DC873F 302199F WP FS 697 L18L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 697 L18L. REMOVED CRACKED END FITTING AT STA 697 L18L IAW SRM 51-1-20D . LOCATED, DRILLED UP, AND INSTALLED END FITTING AT STA 697 L18L IAW SRM 51-3-1, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007050400072 20070504 00072 WP 2007 5 4 UPS07849739 1 20070424 A 5340 ATTACH ANGLE DOUG DC8 DC873F 302199F WP FS 1766 L16L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD TO L16L ATTACH ANGLE CRACKED AT STA 1766. REMOVED ATTACH ANGLE AT STA 1766 L16 L IAW SRM 51-1-21. FABRICATED AND INSTALLED INTERCOSTAL CLIP AT STA 1766 L16L IAW DWG NR 5773844, AND SRM'S 51-1-20D, 5 1-3-2. 2 L 7 4 4F RT 4A25 2007050400076 20070504 00076 NM 2007 5 4 SWAA072197 1 20070502 A 5311 6546549 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400079 20070504 00079 NM 2007 5 4 SWAA072198 1 20070502 A 5311 6546552 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400088 20070504 00088 NM 2007 5 4 SWAA072173 1 20070502 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400096 20070504 00096 NE 2007 5 4 DCG2007F00000 2 20070323 A 7250 0292208230 MANIFOLD SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE GAS GENERATOR COKED E DCGA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 711JH 6791 806 3397 9740 BEFORE THE FIRST FLIGHT OF THE DAY THE PILOT COULD NOT START ENGINE. INSPECTED ENGINE ASSY AND FOUND THE GAS GENERATOR LOCKED UP DUE TO COKING FROM THE FUEL INJECTION MANIFOLD. REMOVE THE ENGINE ASSY AND ASSIST TECH IN REPLACING THE FUEL INJECTION MANIFOLD. (K) 1 G 7 1 3U 3 U H9EU E19EU 2007050400116 20070504 00116 NM 2007 5 4 SWAA072188 1 20070502 A 5523 69633918 BOLT BOEING 737 7373H4 1384600 NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. R&R NR 2 HINGE BUSHING AND BOLT PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400142 20070504 00142 NM 2007 5 4 USAA200705003 1 20070501 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 511AU 23594 FOUND 2.25" CRACK AT STA 727D AT STR 23L. (CLT) INSTALLED DOUBLER PER TR 53-60-03A. 2 L 7 2 4F RT A16WE 2007050400158 20070504 00158 NM 2007 5 4 USAA070335 1 20070501 A 5720 STIFFENER BOEING 737 737301 1384611 NM CENTER WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 503UW 23237 LBL 6 AT STA 663.75 AT CENTER WING SPAR, FWD WALL OF MLG WHEELWELL ABOVE A. INSTALLED DOUBLER PER TR 57-10-03 REV B. D EFECT SIZE: 1" 2 L 7 2 4F RT A16WE 2007050400175 20070504 00175 NE 2007 5 4 AALA20070725 2 20070421 A 7230 BLADE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LT ENGINE DAMAGED A AALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 21 598AA 53288 728191 EWR INFLIGHT T1179/21APR DURING CLIMB LEFT ENGINE COMPRESSOR STALLED AT 600 FEET ABOVE GROUND LEVEL. POSSIBLE BIRD STR IKE. RETURNED TO EWR AND LANDED WITHOUT INCIDENT. ENGINE SHUT DOWN FOR TAXI. REPLACED NUMBER ONE ENGINE ON 20 APR 2007 AT EWR DUE TO BLADE DAMAGE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F RT A6WE E9NE 2007050400176 20070504 00176 NM 2007 5 4 AALA20070726 1 20070421 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 391AA 27451 MIA EMERGENCY LIGHTS AT RIGHT HAND SIDE FROM ROW 10H TO BULKHEAD IN COACH INOPERATIVE. REPLACED BATTERY PACK FOR EMERG ENCY LIGHTS AT RIGHT HAND SIDE FROM ROW 10H TO BULKHEAD IN COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A1NM 2007050400179 20070504 00179 NE 2007 5 4 AALA20070720 2 20070420 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LEFT OIL CONSUMPTION A AALA O OTHER J WARNING INDICATION DE DESCENT 1 SW 21 7546A 53028 717387 DFW INFLIGHT T569/20APR IN DESCENT WITH THROTTLES AT IDLE LEFT OIL PRESSURE LOW LIGHT ILLUMINATED ALONG WITH OIL PRESSU RE OF ZERO. SHUT DOWN LEFT ENGINE. LANDED DFW WITHOUT INCIDENT. SINGLE ENGINE TIME 15 TO 20 MINUTES. REPLACED NUMBER ONE ENGINE ON 23 APR 2007 AT DFW DUE TO OIL PRESSURE LOSS, OUT OF LIMITS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOS ED) 2 L 7 2 4F 4 F A6WE E9NE 2007050400180 20070504 00180 EU 2007 5 4 AALA20070721 1 20070420 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80084 675 MIA EMERGENCY LIGHT AT SEAT 18G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 18G. SYSTEM GROUND CHECKED NORMAL OPERA TION. (CLOSED) 2 L 7 2 4F RT A35EU 2007050400181 20070504 00181 WP 2007 5 4 AALA20070717 1 20070419 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG MALFUNCTIONED A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 427AA 49339 ORD INFLIGHT T1130/19APR NOSE GEAR DID NOT EXTEND DURING FIRST ATTEMPT. NOSE GEAR RED LIGHT ILLUMINATED. NOSE GEAR IN DICATOR PIN SHOWED UNSAFE GEAR. TOWER CONFIRMED NO NOSE LANDING GEAR. ON GO AROUND THE LANDING GEAR CAME DOWN AND LOCK ED. LANDED ORD WITHOUT INCIDENT. REMOVED AND INSPECTED STRUT PISTON FOR DAMAGE AND SERVICED STRUT. SYSTEM GROUND CHEC KED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2007050400195 20070504 00195 NM 2007 5 4 AALA20070728 1 20070421 A 3350 1010427 LENS BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 664AA 25298 TPA EMERGENCY LIGHT AT SEAT 5E OVERHEAD MISSING LENS. REPLACED LENS FOR OVERHEAD EMERGENCY LIGHT AT SEAT 5E. SYSTEM G ROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A2NM 2007050400226 20070504 00226 EU 2007 5 4 AALA20070703 1 20070417 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14068 511 JFK SEAT MOUNTED EMERGENCY LIGHTS AT RIGHT HAND FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGE NCY LIGHTS AT RIGHT HAND FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A35EU 2007050400232 20070504 00232 WP 2007 5 4 AALA20070695 1 20070417 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 567AM 53293 BOS EMERGENCY LIGHTS AT LEFT AND RIGHT HAND OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT L EFT AND RIGHT HAND OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A6WE 2007050400234 20070504 00234 WP 2007 5 4 07FDEA01672 1 20070430 A 5347 ACA7400501 SEAT TRACK DOUG MD10 MD1010F 3022112 WP GE CF6 CF66D 30020 GL BS 625-775 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 MAIN CABIN SEAT TRACK BENT SEVERAL AREAS BETWEEN STA. 625 AND STA. 775, BL107.5. REMOVED BENT AREAS IAW EA NR 8-5310-110 60411, (FUSELAGE MAINFRAME-SEAT TRACK BETWEEN STA. 635-765/X=107.25. TRIMMED SEAT TRACK LOBES), ALODINED AND PRIMED IA W SRM 51-21-01 PG.1 VOL 11. 2 L 7 3 4F 4 F RT A22WE E23EA 2007050400241 20070504 00241 WP 2007 5 4 ABXA070142 1 20070405 A 5511 5918000523 SPAR CAP DOUG DC9 DC932 3022066 WP HORIZ STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 LEFT HORIZONTAL STABILIZER LOWER SPAR OUTBOARD END CRACKED JUST ABOVE DRAINS, TRAVELS INBOARD UNDER HINGE. REPAIRED LEF T HORIZONTAL STABILIZER LOWER SPAR CAP IAW DC9 SRM 55-02. 2 L 7 2 4F A6WE 2007050400245 20070504 00245 WP 2007 5 4 ABXA070149 1 20070430 A 7931 31801040 TRANSMITTER DOUG DC8 DC863F 302198F WP NR 2 ENGINE DEFECTIVE A ABXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 23 826AX 9 46061 DURING CRUISE NR 2 ENGINE OIL PRESSURE WENT TO OFF SCALE LOW MOMENTARILY AND RECOVERED. FIFTEEN MINUTES LATER, AGAIN OF F SCALE LOW AND STAYED. SECURED NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE PRESSURE TRANSMITTER IAW DC8 MM 70-32-01 -2. RAN ENGINE, NO LEAKS. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2007050400246 20070504 00246 WP 2007 5 4 ABXA070150 1 20070430 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 959AX 47761 EMERGENCY LIGHTS INOPERATIVE ON PREDEPARTURE CHECK. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00 -8. 2 L 7 2 4F A6WE 2007050400248 20070504 00248 CE 2007 5 4 DXTA200702165 1 20070501 A 3260 SWITCH CESSNA 680 680CE 2076811 CE NLG DOOR OUT OF ADJUST E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 368QS 6800073 FRONT NOSE DOOR L AMBER CAUTION MESSAGE ILLUMINATED AFTER TAKE OFF AND ACCELERATING MESSAGE ILLUMINATED. LIGHT EXTINGUIS HED WHEN LANDING GEAR EXTENDED. ADJUSTED LEFT NOSE ACCESS DOOR SWITCH PER CE 680 M/M 52-70-00. OPS CKS GOOD. 2 L 7 2 4F RC T00012WI 2007050400253 20070504 00253 2007 5 4 DXTA200702168 4 20070501 A 3160 DISPLAY CESSNA 500 560CESSNA 2076750 CE NR 2 INOPERATIVE E DXTA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 GL 07 392QS 5600429 DURING TAKEOFF, RMU NR 2 & THE NR 2 PFD BOTH WENT BLANK. AFTER A COUPLE SECONDS THE PFD WENT TO A RED X AND THEN ABOUT 1 0 SECONDS LATER A NORMAL DISPLAY CAME BACK ON. THE RMU TOOK ABOUT ONE MINUTE TO COME BACK ON & HAVE A NORMAL DISPLAY. FO UND NR 2 PFD INCORRECTLY RACKED. REMOVED AND RE-RACK NR 2 PFD IAW CESSNA 560 M.M. CH 34-23-02. REMOVED NR 2 RMU CHECKED CONNECTOR FOR SECURITY REINSTALLED IAW CESSNA 560 M.M. CH 23-13-00. BOTH SYSTEMS OPERATED NORMALLY 2 L 7 2 4F RT A22CE 2007050400254 20070504 00254 NM 2007 5 4 CALA0700213 1 20070425 A 5347 6545410199 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 LEFT OB SEAT TRACK FLOOR SPT CRACKED AT STA 727B. REPAIRED IAW ECRA 5311-01316. 2 L 7 2 4F RT A16WE 2007050400260 20070504 00260 NM 2007 5 4 CALA0700216 1 20070425 A 3350 BR964411 LIGHT BOEING 737 7373T0 1384582 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 76355 23593 FOUND EMERGENCY LIGHT ON SEAT 12C INOP. REPAIRED IAW AMM 33-51-81. 2 L 7 2 4F RT A16WE 2007050400271 20070504 00271 EA 2007 5 4 QXEA200700694 1 20070413 A 5330 SKIN PANEL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 C4 OKC - PANEL 684GB HAS MINOR CHAFFING. REPAIRED IAW SRM 57-52-01 AND 51-21-11. 2 L 7 2 4F RT A21EA 2007050400276 20070504 00276 EA 2007 5 4 QXEA200700697 1 20070417 A 5730 SKIN CNDAIR CL600 CL6002C10 1390015 EA WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 C4 OKC - FOUND PANEL 632CB OUTER SKIN DAMAGED TWO PLACES. REPAIRED IAW SRM 57-41-01 AND 57-42-32. 2 L 7 2 4F RT A21EA 2007050400287 20070504 00287 NM 2007 5 4 07FDEA01691 1 20070503 A 5350 HINGE FITTING DOUG MD11 MD11 3023602 NM TAIL CONE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 TAIL CONE COMPARTMENT, LT HINGE FITTING FOUND CRACKED, VIEWED FROM AFT ACCESSORY COMPARTMENT. [SUP 05-14-07] REMOVED & REPLACED AS PER DAC DWG AJC7346 AND SRM 51-31-01 VOL.II. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050700009 20070507 00009 EA 2007 5 7 TRAX200700586 1 20070429 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 877AS 7579 LEFT EXTERNAL AFT O/W EMERGENCY LIGHT INOP 2 L 7 2 4F RT A21EA 2007050700013 20070507 00013 EA 2007 5 7 TRAX200700590 1 20070424 A 5720 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 974EV 7594 RANRC 356. POSSIBLE CRACK FOUND AT AFT FASTENER HOLE FOR LT DRAIN NEXT TO BOOST PUMP IN CANISTER. [07-23-07] REPAIRED IAW ALL SRM AND EO`S. 2 L 7 2 4F RT A21EA 2007050700025 20070507 00025 EA 2007 5 7 A6WA200740187 1 20070405 A 3040 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE WINDSHIELD HEAT WARNING LIGHT A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 410AW 7490 LT WINDSHIELD HEAT MESSAGE ILLUMINATED IN FLIGHT. COMPLIED WITH QRH. [07-31-07] COMPLIED WITH CONNECTION OF SPARE TEM P SENSORS IAW AMM 30-41-06. OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007050700029 20070507 00029 CE 2007 5 7 K5L2007F00000 1 20070306 A 5610 10138402522 WINDSHIELD BEECH 200 A200 1152921 CE PWA PT6 PT6A41 52043 EA COPILOTS FAILED E K5LA O OTHER O OTHER NR NOT REPORTED 1 EA 05 636B 3190 BC61 WHEN IN CRUISE FLIGHT AT FL210 AND -42 DEGREES C, THE INNER PANE ON THE CO-PILOTS WINDSHIELD SHATTERED. NO PIECES BROKE LOOSE AND NORMAL DESCENT AND SAFE LANDING WERE MADE AT KLEB. THERE WAS NO LOSS OF CABIN PRESSURE. LAST INSPECTION WAS 3 MONTH AND 100 HOURS PRIOR TO THE INCIDENT. (K) 1 L 7 2 4T 4 T A24CE E4EA 2007050700033 20070507 00033 CE 2007 5 7 DA62007F00004 1 20070104 A 2730 CONTROL CABLE BEECH 60 B60 1153605 CE LYC O540 TIO540* 41532 EA LT ELEVATOR CORRODED E DA6A K NONE O OTHER IN INSP/MAINT 1 SW 09 171EC P288 DURING ANNUAL INSP, FOUND SEVERAL CONTROL CABLES THAT WERE CORRODED DUE TO BEING SUBMERGED IN WATER AND THAT WERE EXPOSE D TO THE EVAPORATION OF THE WATER THAT HAD COLLECTED IN THE BELLY OF THE AC. CONTROL CABLES WILL BE REMOVED AND REPLACE D, WATER DRIED UP AND ANY POSSIBLE AREAS THAT MAY BE A LEAK WILL BE INSPECTED AND CORRECTED AS NEEDED. ALSO FOUND CONTR OL CABLE PULLEYS SEIZED; LT ELEVATOR PULLEYS AFT OF AFT SPAR, AILERON PULLEYS FWD OF FWD SPAR, AND ELEVATOR PULLEYS IN T AIL CONE. THESE PULLEYS WILL BE REMOVED AND REPLACED. (K) 1 L 7 2 3O 3 O A12CE E14EA 2007050700038 20070507 00038 EA 2007 5 7 TRAX200700594 1 20070501 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 752EV 10166 LT AFT MOST EXTERNAL EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007050700052 20070507 00052 EA 2007 5 7 TRAX200700599 1 20070502 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 820AS 7188 BONDED SKIN DOUBLER CRACKED IN AFT EQUIP BAY, LT SIDE STR 9, FS 640. [07-23-07] REPAIRED IAW EO 601R-53-61-506. 2 L 7 2 4F RT A21EA 2007050700055 20070507 00055 NM 2007 5 7 DLM88070391 1 20070501 A 3350 41B004AD07G3 BATTERY DOUG MD88 MD88 3023688 NM EMERGENCY LIGHT WEAK A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 969DL 53172 FOUND OVERWING EMERGENCY EXIT IDENTIFIER LIGHTS INOP. REPLACED BATTERIES. EMERGENCY LIGHTS CHECK GOOD. 2 L 7 2 4F RT A6WE 2007050700059 20070507 00059 NM 2007 5 7 AWXA200700550 1 20070418 A 5320 654797321 SHEAR WEB BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - CRACKED CABIN FLOOR SHEAR WEB, BS 616 - BS 639, RBL 65, WL 208. REPLACED CABIN FLOOR SHEAR WEB, BS 616 - BS 639, RBL 65, WL 208 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007050700060 20070507 00060 NM 2007 5 7 AWXA200700551 1 20070418 A 5313 65516981 STRINGER SPLICE BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - CRACKED STRINGER SPLICE CHANNEL, BS 907, S5L. REPLACED STRINGER SPLICE CHANNEL, BS 907, S5L IAW B737-300 SRM 51-4 0-02. 2 L 7 2 4F RT A16WE 2007050700061 20070507 00061 NM 2007 5 7 AWXA200700552 1 20070418 A 5313 65516989 STRINGER SPLICE BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - CRACKED STRINGER SPLICE CHANNEL, BS 907, S4L. REPLACED STRINGER SPLICE CHANNEL, BS 907, S4L IAW B737-300 SRM 51-4 0-02. 2 L 7 2 4F RT A16WE 2007050700062 20070507 00062 EA 2007 5 7 TRAX200700601 1 20070502 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 884AS 7513 RANRC 349. RT FS 484 INTERCOSTAL IS CRACKED ON O/B SIDE. [SUP 05-08-07] REPAIRED CRACKED INTERCOSTAL ON O/B SIDE OF RT FS 484 IAW BOMBARDIER REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2007050700063 20070507 00063 NM 2007 5 7 AWXA200700553 1 20070424 A 5340 69414372 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - FOUND CRACKED STRINGER ATTACH CLIP, BS 663, S10R. REPLACED STRINGER ATTACH CLIP, BS 663, S10R IAW B737-300 SRM 51 -40-02. 2 L 7 2 4F RT A16WE 2007050700068 20070507 00068 NM 2007 5 7 AWXA200700558 1 20070502 A 3397 CONNECTOR BOEING 737 73733A 1384673 NM ZONE 200 BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 166AW 23627 MCN - EEL - FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT WILL NOT ILLUMINATE. REPLACED FORWARD FLIGHT ATTENDANT EMERGE NCY FLASHLIGHT POWER UNIT DUE TO A BROKEN CONNECTOR. 2 L 7 2 4F RT A16WE 2007050700071 20070507 00071 NM 2007 5 7 DU4R2007117 1 20070407 A 5315 BAC1518338 FLOORBEAM BOEING 757 757232 1384965 NM BS 337 S17L CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 637DL 23760 FOUND CORROSION ON FLOORBEAM UPPER TEE CAP AT BS 377 AND LBL 19. REPAIRED BY CUTTING OUT CORRODED AREA, FABRICATED AND INSTALLED REPAIR TEE CAP 13 BY 2 BY 2 BY 2-1/2 FROM BAC1505-100617, REPAIR L-ANGLE 11 BY ½ BY 2 FROM BAC 1490-6199 7075 -T6 .063 AND 13 BY 2 BY ½ FROM 7075-T6 .050 AND REPAIR STRAP 11 BY ½ FROM 7075-T6 .090 AND 13 BY ½ BY FROM 7075-T6 .063 IAW B757 SRM 51-20-01 AND 53-00-51D. 2 L 7 2 4F RT A2NM 2007050700072 20070507 00072 NM 2007 5 7 DU4R2007118 1 20070421 A 5310 146N56003 CREASE BEAM BOEING 757 757232 1384965 NM BS 1180-1200 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 637DL 23760 FOUND CORRODED CREASE BEAM ANGLE AT BS 1180 TO BS 1200 LT. REPAIRED BY REMOVING CREASE BEAM, FABRICATED, HEAT TREATED A ND INSTALLED REPAIR BEAM 2 BY 2 BY 22 FROM 60-11925 EXTRUSION P/N T827537-1 BOEING DWG.146N5600 IAW B737 SRM 51-40-02, 5 1-40-05 AND 51-20-01. 2 L 7 2 4F RT A2NM 2007050700073 20070507 00073 EA 2007 5 7 TRAX200700602 1 20070502 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 884AS 7513 RANRC 352. FS 280 RT O/B ANGLE CRACKED AT RBL 9. [SUP 05-11-07] REMOVED FS 280 R/H O/B ANGLE AND FABRICATED NEW ANGLE FROM 2024 T-3 .050", PO 8398-1, IAW REO 601R-53-11-137. 2 L 7 2 4F RT A21EA 2007050700104 20070507 00104 NM 2007 5 7 SWAA072212 1 20070503 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 AFT CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007050700120 20070507 00120 NM 2007 5 7 SWAA072232 1 20070503 A 5320 6545401 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED SPV CHECK, FOUND RIGHT W/W VERTICAL STIFFENER CRACKED AT BS 663, RBL 6.15. REPAIRED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2007050700123 20070507 00123 NM 2007 5 7 SWAA072217 1 20070503 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 384, STR 15L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007050700124 20070507 00124 NM 2007 5 7 SWAA072214 1 20070503 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 900, STR 22R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007050700126 20070507 00126 NM 2007 5 7 SWAA072215 1 20070503 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 865, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007050700127 20070507 00127 NM 2007 5 7 SWAA072216 1 20070503 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 924, STR 23R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007050700131 20070507 00131 NM 2007 5 7 SWAA072234 1 20070503 A 5311 6546554 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050700134 20070507 00134 NM 2007 5 7 SWAA072230 1 20070503 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 639, STR 16R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007050700135 20070507 00135 NM 2007 5 7 SWAA072229 1 20070503 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED C2 CHECK, FOUND RIGHT WING NR 6 L/E SLAT CRACKED AT OUTBOARD T/E. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007050700139 20070507 00139 NM 2007 5 7 SWAA072233 1 20070503 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED C1 CHECK, FOUND RIGHT WING NR 6 L/E SLAT CRACKED AT INBOARD L/E. REPAIRED SLAT PER SWA EA. 2 L 7 2 4F RT A16WE 2007050700141 20070507 00141 NM 2007 5 7 SWAA072228 1 20070503 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050700144 20070507 00144 NM 2007 5 7 SWAA072223 1 20070503 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050700145 20070507 00145 NM 2007 5 7 SWAA072219 1 20070503 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050700146 20070507 00146 NM 2007 5 7 SWAA072220 1 20070503 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050700150 20070507 00150 NM 2007 5 7 SWAA072224 1 20070503 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050700154 20070507 00154 NM 2007 5 7 SWAA072239 1 20070503 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050700155 20070507 00155 NM 2007 5 7 SWAA072240 1 20070503 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050700157 20070507 00157 NM 2007 5 7 SWAA072226 1 20070503 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050700159 20070507 00159 NM 2007 5 7 SWAA072242 1 20070503 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND STRINGER 6L CRACKED AT BS 727B. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007050700161 20070507 00161 NM 2007 5 7 SWAA072213 1 20070503 A 3350 PH22300L STRIP BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 1 ABC. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007050700162 20070507 00162 NM 2007 5 7 UPS07549703 1 20070427 A 3610 BLEED VALVE BOEING 757 75724APF 1384969 NM BLEED AIR SYS MALFUNCTIONED A IPXA K NONE J WARNING INDICATION CL CLIMB 1 SO 01 471UP 28842 INSPECTION TYPE:N/A AT APPROX 0100Z CLIMBING OUT OF ABOUT FL340 TO A FILED ALTITUDE OF FL390, THE F/O WAS FLYING & THE A UTOPILOT ENGAGED. CABIN ALTITUDE ALERT ILLUM, ALONG W/AUDIO WARNING. ATC WAS ADVISED THAT THERE WAS A PRESSURIZATION P ROBLEM & WOULD HAVE TO DESCEND. PERFORMED ECS BITE PER 36-11-00-5. RAN ENGINES (CREW) BLEEDS OPERATE NORMAL PER AMM 36 -11-00-5. GROUND OPS CHECK OK. PERFORMED PRESSURIZATION CONTROL BITE TEST PER AMM 21-31-00-5. GROUND OPS CHECKS OK. 2 L 7 2 4F RT A2NM 2007050700166 20070507 00166 WP 2007 5 7 UPS07849741 1 20070426 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 LEFT WING CENTER RIB CRACKED AT XFS 409. STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER IAW S RM 57-02-00 51-1-21, AND 51-1-20D. 2 L 7 4 4F RT 4A25 2007050700168 20070507 00168 WP 2007 5 7 UPS07849744 1 20070407 A 5320 97537891 CUSP WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2, 6 INCH CRACK ON CUSP AT FS 1220 RIGHT SIDE FLOORBEAM FITTING L21R. REPAIRED CUSP AT STA 1133 - 1248 L21R IAW SAA EA008-5330-01-A0815, UPS RAA DC8-53-20622, SRM TR 53-180, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007050700169 20070507 00169 WP 2007 5 7 UPS07849745 1 20070410 A 5532 564779637 SKIN DOUG DC8 DC873F 302199F WP VERTICAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 EVIDENCE OF CORROSION UNDER VERT STAB SKIN, RIGHT SIDE LARGE AREA OF PILLOWED SKIN WITH SEVERAL FAILE D RIVETS. EXTERIOR ZR252-296 ALONG REAR SPAR. REMOVED AND REPLACED RIGHT VERT STAB SKIN IAW SRM 51-1-21, 51-1-20D, AND 51-3-0. 2 L 7 4 4F RT 4A25 2007050700170 20070507 00170 WP 2007 5 7 UPS07849747 1 20070504 A 2150 A/C PACK DOUG DC8 DC871F 302199D WP A/C BAY OVERHEATED A IPXA D RETURN TO BLOCK M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 700UP 45900 NR 3 ENG RUNNING DURING PUSHBACK, ELEC BUSS FAILURE. SMOKE IN FLIGHT DECK WHILE BEING TOWED BACK IN. SDR FILED OPEN, NR 2 PACK OVERHEAT WAS DETERMINED TO BE THE CAUSE OF SMOKE. [SUP 05-07-07] NR 2 PACK WAS FOUND TO BE CAUSE OF SMOKE IN C/P. R&R NR 3 ENG GEN CONT PANEL PER MM 24-20-00. RAN NR 3 ENGINE MANY TIMES WITH LOAD APPLIED. OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2007050700172 20070507 00172 EU 2007 5 7 USAA070359 1 20070504 A 5712 RIB AIRBUS 330 A330323 3930335 EU RT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 271AY 323 RT WING RIB 6 AT AFT APERTURE REFUEL PIPE ATTACHMENT FASTENERS. TEMPORARY REPAIR PER EA 98639. DEFECT SIZE: LESS THAN 1" 2 L 7 2 4F RT A46NM 2007050700173 20070507 00173 NM 2007 5 7 USAA070358 1 20070504 A 5754 65C26608101 SLAT BOEING 737 7374B7 1384702 NM L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 441US 24812 LOWER L/E WBL 279.25 IN LINE WITH O/B AUX TRACK. FAB'D & INSTALLED FILLER & DOUBLER PER SRM 57-43-01. DEFECT SIZE: .25 " 2 L 7 2 4F RT A16WE 2007050400074 20070504 00074 NM 2007 5 4 SWAA072196 1 20070502 A 5311 6546548 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400082 20070504 00082 NM 2007 5 4 SWAA072201 1 20070502 A 5311 6546557 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050400091 20070504 00091 NM 2007 5 4 SWAA072205 1 20070502 A 5340 65C27314 STRINGER CLIP BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 20L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050400098 20070504 00098 CE 2007 5 4 07060 1 20070426 A 3251 380580150011 HOUSING RKWELL NA265 NA26565 7630107 CE GARRTT TFE731 TFE7313R1D 01518 WP STEERING ACTUATO CRACKED E DGCA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 03 570R 46575 NOSE LANDING GEAR STEERING ACTUATOR HOUSING DEVELOPED A CRACK AND LEAKED HYDRAULIC FLUID ON THE RAMP. 2 L 7 2 4J 4 F A2WE E6WE 2007050400128 20070504 00128 NM 2007 5 4 AALA20070708 1 20070417 A 3350 8200037702 LENS BOEING 737 737823 13844BZ NM CABIN CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 915AN 29516 TUL EMERGENCY LIGHT AT STATION 590 RIGHT BUTTLINE 60 FOR OVERWING EXIT LOCATOR HAS CRACKED LENS. REPLACED LENS FOR EMER GENCY LIGHT AT STATION 590 RIGHT BUTTLINE 60 FOR OVERWING EXIT LOCATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED ) 2 L 7 2 4F RT A16WE 2007050400139 20070504 00139 NM 2007 5 4 USAA200705002 1 20070429 A 5512 SKIN BOEING 737 7374B7 1384702 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 2" CRACK FOUND AT RT HORIZ STAB LOWER SKIN CENTER OF 3" PANEL. (CLT) INSTALLED TEMPORARY DOUBLER PER TR 55-10-07 REV B. 2 L 7 2 4F RT A16WE 2007050400156 20070504 00156 CE 2007 5 4 DJFA2007048A 1 20070412 A 5320 67130519 WEB CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG WW CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 704LX 8043 7500091 DURING A SCHEDULED INSPECTION, MAINTENANCE DISCOVERED MULTIPLE CRACKS IN THE NOSE WHEEL WELL AREA. THE UPPER CENTER WEB WAS CRACKED. THE WEB CRACK WAS ABOUT .6 INCHES LONG. MX REMOVED AND REPLACED CENTER WEB SUPPORT IAW DRAWING NR 67180 0, REPLACED 6717711-41-5 LINES ASSYS AND SWAPPED ALL CRT LINES AND TUBES FOR WEB REPLACEMENT IAW MM CH 20-10-03. REFERE NCE SDR'S DJFA2007048 AND 048B FOR ADDITIONAL DATA. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007050400160 20070504 00160 CE 2007 5 4 DJFA2007048B 1 20070412 A 5312 671305183 DOUBLER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG WW CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 704LX 8043 7500091 DURING A SHCEDULED INSPECTION, MAINTENANCE DISCOVERED MULTIPLE CRACKS IN THE NOSE WHEEL WELL AREA. THE LT TOP DOUBLER W AS FOUND CRACKED. THE CRACK ON THE DOUBLER WAS .8 INCHES LONG. MX REMOVED AND REPLACED THE DOUBLER IAW DRAWING NR 671 800, REPLACED 6717711-41-5 LINES ASSYS AND SWAPPED ALL CRT LINES AND TUBES FOR WEB REPLACEMENT IAW MM CH 20-10-03. REF ERENCE SDR'S DJFA2007048 AND 048A FOR ADDITIONAL DATA. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007050400194 20070504 00194 WP 2007 5 4 AALA20070730 1 20070422 A 3231 DOOR DOUG DC9 DC982 3022082 WP NLG OPEN A AALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 21 480AA 49655 MEM INFLIGHT T1725/22APR DURING CLIMB CREW REPORTED NOSE GEAR VIBRATIONS AND GEAR DOOR LIGHT ILLUMINATED. RETURNED TO MEM AND LANDED WITHOUT INCIDENT. FOUND NOSE GEAR DOOR OPEN. CLOSED DOOR AND FOUND ALL INDICATIONS NORMAL. SYSTEM GRO UND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2007050400210 20070504 00210 CE 2007 5 4 DXTA200702167 1 20070501 A 3220 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG FAILED E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 904QS 7500210 SEVERE VIBRATION AT APPROXIMATELY 60 KNOTS DURING TAKEOFF. YAW DAMPER DISCONNECTED AND NR 1 ADC FAILED. ABORTED TAKE OFF IAW ETA PROCEDURE. FOUND NLG SQUAT SWITCH OUT OF ADJUST. ADJUSTED SWITCH AS REQUIRED IAW 750 MM 32-60-00. SERVICED N LG STRUT IAW 750 MM 12-10-38. RETORQUED NLG TORQUE LINK BOLTS IAW 750 MM 32-20-00. ADJUSTED NLG CASTER IAW 750 MM 32-30 -03. REPLACED NLG ACT ELASTOMERS IAW 750 SB 32-43. RETORQUED NLG TRUNNION MOUNT BOLTS IAW 750 MM 32-20-00. REMOVED AND R EPLACED L/R NLG WHEEL ASSY IAW 750 MM 32-41-00. PERFORMED GEAR SWING IAW 750 MM 32-20-01. ALL OPS CHECK GOOD. TAXI CHECK GOOD. C/W DAMPER LINEAR ACT TEST IAW 750 MM 27-24-00. C/W NR 1 MADC OPS CHECK IAW 750 MM 34-11-08. ALL OPS CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007050400216 20070504 00216 NM 2007 5 4 AALA20070707 1 20070417 A 3350 8200037702 LENS BOEING 737 737823 13844BZ NM CABIN CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 915AN 29516 TUL EMERGENCY LIGHT AT STATION 628 RIGHT BUTTLINE 60 FOR OVERWING EXIT LOCATOR HAS LENS CRACKED. REPLACED LENS FOR EME RGENCY LIGHT AT STATION 628 RIGHT BUTTLINE 60 FOR OVERWING EXIT LOCATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSE D) 2 L 7 2 4F RT A16WE 2007050400220 20070504 00220 WP 2007 5 4 AALA20070694 1 20070416 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 271AA 49293 ORD INFLIGHT T1872/16APR UNABLE TO RETRACT NOSE GEAR. RED LIGHT ILLUMINATED WITH GEAR HANDLE IN UP POSITION ACCOMPANIE D BY AIR NOSE. NOSE LANDING HEAR PIN WAS FLUSH. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED AND SERVICED NO SE LANDING GEAR STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2007050400244 20070504 00244 WP 2007 5 4 ABXA070139 1 20070405 A 5347 S4925848M36000 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 SEAT TRACK SECTION BUTT LINE 0, STA 570 - 785 CORRODED AT STA 785 - 765, 737, 710 - 699, 680 - 670 AND 636 - 617. REMOVE D AND REPLACED SEAT TRACK STA 160 - 784 IAW DC9 SRM 51-30-1 AND 51-10-4. 2 L 7 2 4F A6WE 2007050400262 20070504 00262 NM 2007 5 4 CALA0700218 1 20070426 A 5311 6546547251 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 FOUND CRACKED FRAME AT STA 727, S 14L. REPAIRED IAW ECRA 5311-01317. 2 L 7 2 4F RT A16WE 2007050400266 20070504 00266 NM 2007 5 4 CALA0700220 1 20070429 A 3350 D71701100 CHARGER BOEING 767 767424ER 1385270 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 66057 29452 THE EMERGENCY LIGHTS AT ROWS 18-21DEF WERE FOUND INOPERATIVE. THE BATTERY AND CHARGER WERE REPLACED IAW MM 33-51-07, PA GE 201. 2 L 7 2 4F RT A1NM 2007050400270 20070504 00270 SO 2007 5 4 C2XA07TY023 1 20070502 A 5514 14524978001 HOUSING EMB 145 EMB145LR 3260212 SO HORIZ STAB DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13903 145479 TYS C-CHECK- DISCREPANCY- RT HORIZONTAL STAB. HINGE POINT HAS MIGRATED BUSHING AT IT'S FLANGE. REMOVED BUSHINGS REWORK ED HOUSING TO 1ST OVERSIZE OF 1.664" AND INSTALLED NEW BUSHINGS IAW EMB 135/145 SRM 55-10-02. 2 L 7 2 4T RT T00011AT 2007050400279 20070504 00279 EA 2007 5 4 QXEA200700699 1 20070415 A 5754 SKIN CNDAIR CL600 CL6002C10 1390015 EA L/E SLAT SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 C4 OKC - RIGHT SLAT NR 3 SCRATCHED ON LEADING EDGE. REPAIRED IAW SRM 51-12-00 AND 51-21-11, 57-42-01. 2 L 7 2 4F RT A21EA 2007050400280 20070504 00280 NM 2007 5 4 07FDEA01684 1 20070502 A 5720 652165835 BRACKET BOEING 727 7272S2F 1384O81 NM RT WING CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 RT WING'S LOWER TRAILING EDGE PANELS OUTBD STRUT MOUNT BRACKET IS CRACKED BY NR 7 TRANSMISSION REMOVED AND REPLACED RT W ING LOWER EDGE PANEL MOUNT BRACKET SRM 51-30-2 PG 1. 2 L 7 3 4F A3WE 2007050400282 20070504 00282 NM 2007 5 4 07FDEA01686 1 20070503 A 5311 ACA71231 FRAME DOUG MD11 MD11 3023602 NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 FOUND LEFT MAIN FRAME STA 535 AT 9G NET SUPPORT YOKE AREA FOUND CHAFFED AT LONGERON 23L. [SUP 05-10-07] REPAIR CARRIED OUT AS PER FEDEX AIRCRAFT ENGINEERING STANDARD REWORK DRAWING NR: SRZ 53-503. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2 -100. 2 L 7 3 4F RT A22WE 2007050400290 20070504 00290 EU 2007 5 4 07FDEA01652 1 20070427 A 5322 SHEAR TIE AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 408FE 257 A/C BAY AT RT SIDE OF KEEL BEAM AND ON TOP VERTICAL FLANGE OF FR 46 , 1 SHEAR TIE BRACKET HAS CRACK .51 LONG. REMOVED A ND REPLACED SHEAR TIE IAW A310-200 SRM 51-72-10 AND EA 6-5320-110446. 2 L 7 2 4F RT A35EU 2007050400292 20070504 00292 NM 2007 5 4 07FDEA01677 1 20070501 A 5321 6567245187 FLOORBOARD BOEING 727 7272S2F 1384O81 NM CARGO BAY PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 AFT LOWER CARGO PIT 1ST OR FWD FLOORBOARD HAS MANY PUNCTURES FABRICATED NEW PANEL REF 51-30-5. ALODINED AND PRIMED BOTT OM SIDE OF PANEL REF MM 51-20-021-7 AND MM 51-20-031-7. 2 L 7 3 4F A3WE 2007050400301 20070504 00301 NE 2007 5 4 07FDEA01660 2 20070429 A 7200 ENGINE AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE NR 2 BIRD INGESTION A FDEA C E ABORTED TAKEOFF ENGINE SHUTDOWN C R E F.O.D. PARTIAL RPM/PWR LOSS VIBRATION/BUFFET TO TAKEOFF 1 SO 25 667FE 771 HIGH SPEED REJECT CLE 24L AT 135 KTS. A SEAGULL WENT IN THE NR 2 ENG FOLLOWED BY A HEAVY VIBRATION. NR 2 ENG INDICATI ONS APPEARED NORMAL AFTER STOPPING THE AIRCRAFT. [SUP 05-04-07] REPLACED 5 EA. 1ST. STG. FAN BLADES PER MM 72-21-00 -4-05. SPINNER STILL TO BE INSTALLED. RAN NR 2 ENG AS PER A300 JRH PERFORMED VIBRATION SURVEY. ENGINE PARAMETERS CHE CKS OK DURING 40 AND 83 PERCENT POWER ASSURANCE. DURING 40 PERCENT PARAMETERS INDICATE D VIB (N1) .2 AND VIB (N2) .6. THE PARAMETERS DURING 83 PERCENT INDICATED VIB (N1) .8 AND VIB (N2) .4. ENGINE REMAINS IN LIMITS AS PER VIBRATION SURVEY. OPS CHECKS OK, OK FOR SERVICE. 2 L 7 2 4F 4 F RT A35EU E13NE 2007050400302 20070504 00302 NM 2007 5 4 07FDEA01661 1 20070430 A 5753 HINGE FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 LEFT WING, OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING INBOARD NR 2 BOLT HOLE FOUND CORRODED. REMOVED & REPLACED AS PE R AMM 27-50-30-4. ADJUSTMENT & TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094. 2 L 7 3 4F RT A22WE 2007050700001 20070507 00001 GL 2007 5 7 BUW2007F00000 1 20070401 A 2150 WHEEL CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO EVAPORATOR DISINTEGRATED E BUWA O OTHER O OTHER NR NOT REPORTED 1 EA 07 927SE 285 2238 EVAPORATOR BLOWER WHEEL DISINTEGRATED IN HOUSING. (K) 1 L 7 1 3O 3 O NT A00009CH E3SO 2007050700004 20070507 00004 CE 2007 5 7 VOX2007F00000 1 20070404 A 5414 COWLING MTSBSI MU2 MU2B36 5780412 CE GARRTT TPE331 TPE3316252B 01514 WP HARTZL HCB3T HCB3TN5 GL RIGHT NACELLE DAMAGED E VOXA O OTHER O OTHER NR NOT REPORTED 1 NM 03 740PB 657 UPPER RT COWLING CAME OPEN IN FLIGHT. RECOMMEND INSTALLING 2 SCREWS AT LEADING EDGE OF COWLING TO PREVENT THIS HAPPENIN G. (K) 1 H 7 2 3T 4 T RT A10SW E2WE 6 C P15EA 2007050700010 20070507 00010 EU 2007 5 7 TRAX200700587 1 20070429 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN INTERMITTENT A ASOA K NONE O OTHER NR NOT REPORTED 1 SO 27 641AS 387 EMERG LIGHTS COMING ON DURING FLIGHT INTERMITTENT WHEN LEFT IN ARMED POSITION. 2 H 7 2 4T RT 2007050700015 20070507 00015 EA 2007 5 7 TRAX200700583 1 20070428 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 683BR 7692 EMERGENCY LIGHTING AT APPROX ROW 9 TO ROW 12 INOP. NOTE NEW LIGHTING IS IN GALLEY AREA AND NEEDS TO BE REINSTALLED FORM ROW 9 TO ROW 14. 2 L 7 2 4F RT A21EA 2007050700024 20070507 00024 2007 5 7 GAIA0703OP 4 20070222 A 3457 8144002241J RECEIVER BOEING 727 727214 138407R NM PWA JT8 JT8D7B 52053 NE GPS SHORTED A GAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 07 750US 21512 DURING APPROACH TO LANDING, THE FLIGHT CREW REPORTED SMOKE IN THE COCKPIT. AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL LANDING WAS MAD. INSPECTION REVEALED THAT THE GPS RECEIVER HAD SHORTED OUT. REMOVED AND REPLACED THE GPS RECEIVER. OP S CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 3 4F 4 F A3WE E2EA 2007050700028 20070507 00028 CE 2007 5 7 GNL2007F00000 1 20070401 A 2697 M624266R128125N CONNECTOR BEECH 200 B200 1152922 CE LT ENG FIRE CORRODED A GNLA O OTHER O OTHER NR NOT REPORTED 1 SW 01 200VU 3534 BB1393 AC WAS FLYING THROUGH IMC WEATHER, WITH A LARGE ACCUMULATION OF MOISTURE, WHEN THE PILOT NOTICED A LT ENGINE FIRE LIGHT. ALL THE OTHER SYSTEMS WERE MONITORED AND THE ENGINE FIRE LIGHT WAS DETERMINED TO BE FALSE. THE AC WAS LANDED WITHOUT EVENT. UPON INSPECTION OF THE FIRE DETECT SYSTEM, A SMALL AMOUNT OF MOISTURE AND CORROSION WAS FOUND ON THE CONNECTOR P LUG CONNECTING THE FIRE SYSTEM TO THE ENGINE FIRE WALL. THE MOISTURE AND CORROSION WERE REMOVED AND THE SYSTEM OPERATIO NALLY TESTED GOOD. (K) 1 L 7 2 4T A24CE 2007050700044 20070507 00044 CE 2007 5 7 BTA2007F00000 1 20070405 A 2612 UNKNOWN CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP FIRE DETECTION MALFUNCTIONED E BTAA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 23 86VP 6500089 RT ENGINE FIRE LIGHT CAME ON DURING CLIMBOUT, RETARDED THROTTLE LIGHT WENT OUT, ADVANCED THROTTLE LIGHT CAME BACK ON AND LANDED. PERFORMED LEAK CHECKS WITH COWLING OPEN, RAN AT FULL POWER FOR 10 MINUTES, COULD NOT DUPLICATE PROBLEM. FLEW AIRCRAFT BACK TO HOME BASE FOR FURTHER TROUBLESHOOTING. PROBLEM DID NOT REPEAT ON RETURN FLIGHT. CAUSE UNKNOWN AT THIS TIME. WHEN IDENTIFIED, A FOLLOW UP REPORT WILL BE SUBMITTED. (K) 2 L 7 2 4F 4 F A9NM E6WE 2007050700048 20070507 00048 NM 2007 5 7 AMTA200700185 1 20070408 A 3397 WIRE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211* 54555 NE EMERGENCY LIGHT DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 522AT 29330 EMERGENCY FLOOR TRACK LIGHTING 3 DEF THRU 10 DEF INOPERATIVE. INSPECTED FLOOR TRACK WIRING FOUND WIRES DISCONNECTED RES ECURED TRACK COVERS, OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM A12EU 2007050700053 20070507 00053 NM 2007 5 7 DL76L070389 1 20070430 A 5414 311T31571 FITTING BOEING 767 767332 1382001 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 180DN 25985 THE NR 2 PYLON CLOSE OUT ANGLE WAS FOUND CRACKED AND THE MIDSPAR FITTING WAS DAMAGED DURING ANGLE REMOVAL. THE CRACKED ANGLE WAS REPLACED AND THE MIDSPAR FITTING WAS REPLACED PER S/B 767-54-0080. 2 L 7 2 4F RT A1NM 2007050700054 20070507 00054 NM 2007 5 7 DL76L070390 1 20070501 A 2131 211002835 CONTROLLER BOEING 767 767332 1382001 NM CABIN PRESSURE MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 190DN 28447 ON CLIMB-OUT HAD EQUIP COOLINNG O/HEAT LIGHT. AFTER SELECTING O/RIDE LIGHT EXTINGUISHED. SHORTLY AFTER HAD CABIN ALT A UTO 1 AND AUTO2 EICAS MSG WITH RISING CABIN ALTITUDE. SELECTED MANUAL AND REGAINED CONTROL OVER CABIN PRESS. CABIN ALT AUTO 2 CLEARED AND SELECTED BUT CABIN ALT CLIMBED AGAIN. BACK TO MANUAL AND RETURN TO ATL. REPLACED K 1008 RELAY GROU ND CK NML REPLACED HEATEXCHANGER. SHUTOFF VALVE BITE CHECK ON LT CONTROLLER, REMOVED AND REPLACED CONTROLLER CKS GOOD. 2 L 7 2 4F RT A1NM 2007050700058 20070507 00058 EA 2007 5 7 TRAX200700600 1 20070502 A 5753 ANGLE CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 ETNRTC 500-13, AT WS 178 OUTB'D FLAP ANGLE ON THE FLAP AFT SIDE ANGLE CRACKED. [SUP 05-15-07] AFTER FURTHER INVESTIGAT ION HOLE WAS FOUND TO BE DOUBLE HOLED THRERFORE WAS RWORKED TO INSTALL OVERSIZE FASTENER IAW SRM 51 42 20 , 51 42 06. 2 L 7 2 4F RT A21EA 2007050700066 20070507 00066 NM 2007 5 7 AWXA200700556 1 20070418 A 5340 693535214 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - FOUND CRACKED STRINGER ATTACH CLIP, BS 727A, S10R. REPLACED STRINGER ATTACH CLIP, BS 727A, S10R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007050700067 20070507 00067 NM 2007 5 7 AWXA200700557 1 20070425 A 5340 693535214 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - FOUND CRACKED STRINGER ATTACH CLIP, BS 639, S2L. REPLACED STRINGER ATTACH CLIP, BS 639, S2L IAW B737-300 SRM 51-4 0-02. 2 L 7 2 4F RT A16WE 2007050700069 20070507 00069 NM 2007 5 7 DU4R2007115 1 20070427 A 5313 STRINGER BOEING 757 757232 1384965 NM BS 1850 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 637DL 23760 FOUND CORRODED STRINGER 25L AT BS 1850 (EMPENNAGE INTERNAL). REPAIRED BY REMOVING SHEAR TIE AND SECTION OF STRINGER. F ABRICATED AND INSTALLED STRINGER 25.0 FROM BAC 1498-132 AND SPLICE 10.0 FROM BAC1498-144 IAW B757 SRM 53-00-03 FIG 201, 51-20-01 AND 51-40-02. 2 L 7 2 4F RT A2NM 2007050700089 20070507 00089 EA 2007 5 7 TRAX200700605 1 20070502 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 ANGLE AND CLIP CRACK AT FS 484 LBL 27 AND LBL 36. [SUP 05-15-07] CUTOUT AT CRACKED ANGLE AND CLIP AT FS 484 LBL 27 AND LBL 36 WAS PERFORMED IAW REO 601R-53-41-059. HFEC PERFORMED BY HEATHAIR W/O 36306 IAW REO 601R-53-41-059. NO CRACKS F OUND. AMO 46-90 CRACKED ANGLE AND CLIP AT FS 484 LBL 27 AND 36 WERE REPAIRED IAW REO 601R-53-41-059 2 L 7 2 4F RT A21EA 2007050700100 20070507 00100 EA 2007 5 7 TRAX200700593 1 20070430 A 3250 ECU CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING OUT OF RIG A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 839AS 7284 DURING CRUISE RECEIVED NOSEWHEEL STEERING INOP MSG ON EICAS FOLLOWED QRH BUT MSG DID NOT GO OUT WHEN NLG STEERING SWITCH RETURNED TO ARMED POS TURNED NLG STEERING BACK OFF AS PER QRH AND COORDINATED WITH MX AND FLT CONTROL TO RTB {A/C RETU RNED TO ATL AFTER T/O} (EMERGENCY DECLARED} RERIGGED NOSE WHEEL STEERING ECU IAW CRJ 200 AMM 32-51-00 AND CRJ 200 AMM 3 2-51-20 OPS CHK GOOD. {SDR -CLOSED} 2 L 7 2 4F RT A21EA 2007050700103 20070507 00103 2007 5 7 C2XA07RI020 4 20070417 A 3418 0861DT5MOD2 VANE EMB 145 EMB145EP 3260221 SO NR 1 AOA BROKEN A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14947 10573 145054 FLIGHT 1219 - EWR - JUST AFTER WHEELS UP ON THE TAKEOFF, CREW REPORTED THE FOLLOWING MESSAGES DISPLAYED ON EICAS: SPSI-2 INOP, STICK PUSHER FAIL, SPS ADVANCED. CREW FOLLOWED THE QRC PROCEDURES AND AIR RETURNED. UPON REACHING GATE, IT WAS DISCOVERED THAT AOA VANE NR 1 WAS SNAPPED. EWR MX REMOVED AND REPLACED NR 1 AOA VANE, IAW EMB 145 27-36-01. MX PERFORM ED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050700122 20070507 00122 NM 2007 5 7 SWAA072235 1 20070503 A 5330 6545767 SKIN BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, LBL 2. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007050700153 20070507 00153 NM 2007 5 7 SWAA072238 1 20070503 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050700156 20070507 00156 NM 2007 5 7 SWAA072241 1 20070503 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050700171 20070507 00171 2007 5 7 UPS07849749 4 20070503 A 2565 SLIDE DOUG DC8 DC873F 302199F WP COCKPIT MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:N/A ESCAPE SLIDE NOT IN DOOR. INSTALLED ESCAPE SLIDE ON DOOR IAW MM 25-60-01-2. 2 L 7 4 4F RT 4A25 2007050700177 20070507 00177 NM 2007 5 7 USAA070355 1 20070504 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 441US 24812 STA 727E + 2", S-24L. REPAIR DOUBLER INSTALLED PER SRM 53-00-01, REPAIR 31. DEFECT SIZE: 1.5" 2 L 7 2 4F RT A16WE 2007050700188 20070507 00188 CE 2007 5 7 DJFA2007051 1 20070426 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 712TA 7313 RK186 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE LEFT INBOARD HORIZON TAL STABILIZER, THE LT RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN BEECHJET CO MMUNIQUE' NR 70. [SUP 05-21-07] MAINTENANCE REPLACED THE RIB. 2 H 7 2 4F 4 F RT A16SW E25EA 2007050700189 20070507 00189 CE 2007 5 7 DJFA2007048 1 20070412 A 5311 713051112 FRAME CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL FUSELAGE CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 704LX 8043 7500091 DURING A SHCEDULED INSPECTION, MAINTENANCE DISCOVERED MULTIPLE CRACKS IN THE NOSE WHEEL WELL AREA. THE CRACK ON THE UPP ER FRAME WAS ABOUT .3 INCH. MX REMOVED AND REPLACED THE FRAME IAW DRAWING NR 671800, REPLACED 6717711-41-5 LINES ASSYS AND SWAPPED ALL CRT LINES AND TUBES FOR WEB REPLACEMENT IAW MM CH 20-10-03. REFERENCE SDR'S DJFA2007048A AND 048B FOR A DDITIONAL INFORMATION. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007050700191 20070507 00191 EU 2007 5 7 07FDEA01556 1 20070424 A 5311 A53973031246 FRAME AIRBUS 310 A310324 3930206 EU ZONE 200 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 4 PLUGGED HOLES IN FRAME SEGMENT REPAIR PERFORMED BY REPLACEMENT OF FRAME SEGMENT C71 LT BETWEEN P4-5 AND P18-22 IAW SR M 51-72-10. 2 L 7 2 4F RT A35EU 2007050700201 20070507 00201 EA 2007 5 7 COMA0760333 1 20070425 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 739CA 21347 7273 DURING FS 559 INSPECTION FOUND CRACK AT SEMI-PRESSURE BULKHEAD, FS 559, RBL 18, WL 59.10. STOP DRILLED CRACK AND INSTAL LED DOUBLER PER CRJ REO 601R-53-41-353. 2 L 7 2 4F RT A21EA 2007050700203 20070507 00203 SO 2007 5 7 C2XA07RI019 1 20070426 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13908 145465 RIC - MX - DURING ROUTINE MAINTENANCE, RIC MX FOUND EMERGENCY EXIT SIGN INOPERATIVE. MX REMOVED AND REPLACED BATTERY IN VERTER. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050700205 20070507 00205 SO 2007 5 7 C2XA07IA098 1 20070421 A 3350 2013BR BATTERY PACK EMB 145 EMB145XR 3260214 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17169 8722 8722 14500844 IAH - DURING MAINTENANCE INSPECTION, THE LEFT HAND MIDDLE EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS AP PROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007050700206 20070507 00206 EA 2007 5 7 COMA0760332 1 20070419 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 918CA 32968 7018 DURING FS 559 INSPECTION FOUND 2 EA CRACKS AT SEMI-PRESSURE BULKHEAD, FS 559, RBL 9-18. REMOVED DAMAGE AND INSTALLED DO UBLER PER COMAIR SR10-5341-0001. 2 L 7 2 4F RT A21EA 2007050700208 20070507 00208 SO 2007 5 7 C2XA07IA095 1 20070424 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A C2XA C ABORTED TAKEOFF J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 13949 145057 IAH - FLIGHT 2824, THE CREW REPORTED A 115VAC OFF BUSS INDICATION WITH A BURNING SMELL IN THE COCKPIT. MAINTENANCE INSP ECTED THE AIRCRAFT AND COULD NOT DUPLICATE ANY DISCREPANCY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050700210 20070507 00210 SO 2007 5 7 C2XA07SH025 1 20070504 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145EP 3260221 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14940 145033 SHV - DURING C-CHECK LEFT OMEGA BEAM HAS CORROSION ON FR 20. MX REPAIRED LEFT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 53-00 -10. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 2007050700211 20070507 00211 SO 2007 5 7 C2XA07SH26 1 20070504 A 5522 14537534002 SKIN EMB 145 EMB145LR 3260212 SO RT ELEVATOR DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14902 145496 SHV - DURING C-CHECK LIGHTNING STRIKE ON RIGHT ELEVATOR UPPER O/B TRAILING EDGE SURFACE. MX REPAIRED DAMAGE ON RIGHT EL EVATOR UPPER O/B TRAILING EDGE SURFACE IAW EC 5330-01692. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050700213 20070507 00213 SO 2007 5 7 C2XA07RI023 1 20070423 A 2750 WARNING SYSTEM EMB 145 EMB145XR 3260214 SO FLAP SYSTEM ACTIVATED A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 27 12195 14500943 FLT 17 - ONT - CREW ABORTED TAKEOFF DUE TO FLAP FAIL INDICATION. ONT MX PERFORMED FLAP SYSTEM RESET. MX PERFORMED OPER ATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007050700215 20070507 00215 SO 2007 5 7 C2XA07CL041 1 20070501 A 3232 21180100009 ACTUATOR EMB 145 EMB145EP 3260221 SO NLG DEFECTIVE A C2XA K NONE J WARNING INDICATION DE DESCENT 1 SW 27 13929 145009 CLE FLIGHT 2349 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE WHEN THE GEAR WAS EXTENDED. MAINTENANCE INSPEC TED AND FOUND THE RIGHT NOSE GEAR DOOR WAS SLOW TO OPEN. THE NOSE GEAR DOOR ACTUATOR WAS REPLACED AND OPERATIONAL CHECK S WERE GOOD. 2 L 7 2 4F RT T00011AT 2007050700216 20070507 00216 SO 2007 5 7 C2XA07RI24 1 20070417 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO LAVATORY DEFECTIVE A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 11193 4130 4130 14500938 FLT 54 - ONT - CREW REPORTED LAV SMOKE INDICATION ON EICAS. ONT MX REMOVED AND REPLACED LAV SMOKE DETECTOR IAW EMB 145 AMM 26-14-01. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007050700219 20070507 00219 EA 2007 5 7 COMA0770025 1 20070420 A 3250 481051 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA NLG FAILED A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 655CA 10134 FLIGHT 4996 - NWS FAILED DURING TAKEOFF ROLL. ABORTED TAKEOFF. REMOVED AND REPLACED STEERING MANIFOLD PRESSURE SWITCH. 2 L 7 2 4F RT A21EA 2007050700222 20070507 00222 SO 2007 5 7 C2XA07CL040 1 20070425 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 13123 145688 CLE FLIGHT 2895 - THE CREW REPORTED A STRONG FUEL SMELL ON CLIMBOUT. THE CREW SWITCHED FROM APU BLEED TO ENGINE BLEED A ND FUMES WENT AWAY. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE APU BLEED SYSTEM AND NO FUEL ODOR WAS NOTICED. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT 2007050700223 20070507 00223 EA 2007 5 7 COMA0770026 1 20070425 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA CABIN DISCHARGED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 374CA 12328 10090 FLIGHT 5451 - EMERGENCY LIGHT INOP RIGHT SIDE OVER WING EXIT. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY PACK. 2 L 7 2 4F RT A21EA 2007050700224 20070507 00224 EA 2007 5 7 COMA0760338 1 20070425 A 2740 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 927CA 7031 FLIGHT 5657 - ON TAKEOFF AFTER FLAP RETRACTION STAB TRIM AND MACH TRIM CAUTION MESSAGE DISPLAYED AND WOULD NOT RESET IN FLIGHT. AIRCRAFT RETURNED BACK TO BOS AND LANDED SAFELY. PERFORMED SYSTEM RESET, SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2007050700227 20070507 00227 EA 2007 5 7 COMA0760336 1 20070423 A 3210 17064103 FITTING MESSIER CNDAIR CL600 CL6002B19 1900309 EA LT MLG CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 10804 DCL05394 7044 THE LEFT MAIN LANDING GEAR FITTING FAILED ULTRASONIC INSPECTION. REPLACED MAIN LANDING GEAR FITTING. 2 L 7 2 4F RT A21EA 2007050700228 20070507 00228 EA 2007 5 7 COMA0760337 1 20070424 A 2760 SPOILER CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE N FALSE WARNING CR CRUISE 1 SO 01 926CA 7027 FLIGHT 5159 - DURING FLIGHT, FLIGHT SPOILER AND SPOILERON CAUTION MESSAGES APPEARED. PERFORMED RESET OF SPOILER SYSTEM, SYSTEM OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007050700229 20070507 00229 EA 2007 5 7 BUW2007F00001 2 20070401 A 7310 RETURN LINE CESSNA 182 182T 2072703 CE LYC O540 IO540AB1A5 EA FUEL SYSTEM LOOSE E BUWA K NONE O OTHER IN INSP/MAINT 1 EA 07 875CP 18281871 DURING THE INSPECTION FOR SB 07-71-01 THE FUEL RETURN LINE AT THE FIREWALL BULKHEAD FITTING WAS FOUND LOOSE. (K) 1 H 7 1 3O 3 O NT 3A13 1E4 2007050700230 20070507 00230 SO 2007 5 7 C2XA07IA100 1 20070428 A 3320 BR90002 BALLAST EMB 145 EMB145EP 3260221 SO CABIN BURNED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16927 145006 HRL - FLIGHT 2002, DURING PREFLIGHT INSPECTION THE CREW REPORTED A POSSIBLE BURNING SMELL IN THE GALLEY WHEN THE AIRCRAF T WAS POWERED UP. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE CABIN LIGHT BALLAST A SEAT 1A TO BE BURNT. THE BALL AST WAS DISCONNECTED AND THE CABIN LIGHT PLACED ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRA FT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED BALLAST, OPERATIONALLY CHECKED THE LIGHTING SYSTEM WITH NO DEFECTS NOTED, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050700232 20070507 00232 SO 2007 5 7 RAIA00704070 1 20070423 A 3397 GROUND WIRE EMB 145 EMB145 3260210 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 809HK 145187 PRE FLT NR 5517 - STL - EMERGENCY LIGHT FLOOR PROXIMITY LIGHTS INOP. MAINTENANCE FOUND GROUND WIRE LOOSE, SECURED GROUN D WIRE AND LIGHT STRIP OPS NORMAL. 2 L 7 2 4F RT T00011AT 2007050700233 20070507 00233 SO 2007 5 7 RAIA00704073 1 20070425 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 819HK 145062 POST FLT NR 5568 - STL - EMERGENCY LIGHT AFT CEILING EXIT LOCATOR IS OUT. MAINTENANCE REMOVED AND REPLACED EMERGENCY LI GHT INVERTER OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007050700234 20070507 00234 SO 2007 5 7 RAIA00704072 1 20070424 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 831HK 145232 PRE FLT NR 7884 - ORD - EMERGENCY LIGHT OUT ABOVE 3A. MAINTENANCE RELAMPED, OPS CHECK GOOD ON GROUND. 2 L 7 2 4T RT T00011AT 2007050700235 20070507 00235 2007 5 7 RAIA00704071 4 20070423 A 3140 7013348949 DAU EMB 145 EMB145LR 3260212 SO NR 1 MALFUNCTIONED A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 814HK 5642 5642 145046 FLT NR 5527 - STL - AT FL290, 115VAC BUSS OFF LINE, BLEED 1 LOW TEMP, BATT 2 OVERTEMP, LOW O2 WARNING, DASHED LINES APPE ARED ON OXY PRESSURE / TEMP. MAINTENANCE REMOVED AND REPLACED NR 1 DAU CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007050700236 20070507 00236 SO 2007 5 7 RAIA00704069 1 20070423 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 840HK 145341 POST FLT NR 7968 - ORD - EMERGENCY LIGHT LEFTHAND OVERWING EXIT MARKER. MAINTENANCE RESECURED LIGHT ASSY. OPS CHECK GO OD. 2 L 7 2 4T RT T00011AT 2007050700237 20070507 00237 EU 2007 5 7 07FDEA01563 1 20070424 A 5313 A53974203 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 FOUND THE FOLLOWING STRINGER CORRODED: P52, C67-70; P49, C67-69; P48, C67-70; P46, C65-68 AND P53, C66-68. CLIP C67, P56-57 IS ALSO CORRODED. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 / FIG 201 AND REPLACEMENT OF CLIP (A539-74223-214) IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007050700238 20070507 00238 EU 2007 5 7 07FDEA01566 1 20070424 A 5313 SEE4B STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 THE FOLLOWING CONNECTING SECTION WERE HEAVY CORRODED: P46, P48, P49, P50, P51, P53, P55, P56 AND P57 AT C65; AND STRINGE R P47 AND P48 AT C65-66. REPAIR PERFORMED BY REPLACEMENT OF ALL CONNECTION SECTIONS IAW SRM 51-72-10 (P/N: A539-74232-2 00, A539-74228-200, A539-74229-200, A539-73303-200, A539-73925-200) AND STRINGER REPAIR IAW SRM 53-10-14/ FIG 201 (A539- 86212). 2 L 7 2 4F RT A35EU 2007050700242 20070507 00242 WP 2007 5 7 MWEA070099 1 20070502 A 4950 7936913577 B-NUT DOUG DC9 DC982 3022082 WP APU LOOSE A MWEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 13 808ME 48070 WITH BOTH ENGINES OFF APU ON, WITH AIR SELECTED ON WITH RIGHT PACK, CABIN GOT A OIL SMELL & HAZE. TIGHTENED B-NUT ON PR ESSURE LINE, LEAK CHECKED GOOD. 2 L 7 2 4F A6WE 2007050700244 20070507 00244 NM 2007 5 7 MWEA070098 1 20070425 A 5220 247629 SWITCH BOEING 717 717200 1383700 NM TAILCONE INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 910ME 55174 INTERNAL TAIL CONE RELEASE LIGHT SWITCH DID NOT ACTUATE AFTER TAIL CONE WAS RELEASED FOR TEST FUNCTION. REMOVED AND REP LACED INTERNAL TAIL CONE LOCKING SWITCH. 2 L 7 2 4F TR A6WE 2007050700245 20070507 00245 EU 2007 5 7 YENA2007031 1 20070501 A 3234 215TS07Y00 CONTROL LEVER AIRBUS 320 A320232 3930326 EU COCKPIT FAULTY A YENA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 15 644JB 2540 2880 FLT 937, ORD-LGB, ON TAKEOFF SELECTED GEAR HANDLE UP, WOULD NOT MOVE. LEFT GEAR DOWN. RETURNED TO ORD. REMOVED AND RE PLACED LANDING GEAR CONTROL LEVER IAW 32-31-11-04. SYSTEM OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 2007050700246 20070507 00246 EA 2007 5 7 COMA0760346 1 20070429 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 720SW 7297 FLIGHT 5338 - FLAPS FAIL MESSAGE AT 30 DEGREES ON APPROACH, AIRCRAFT LANDED SAFELY. COMPLIED WITH AD 2006-12-21 FLAP CA UTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007050700247 20070507 00247 EA 2007 5 7 COMA0760341 1 20070427 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 806CA 7359 RIGHT WING FUEL PANEL 640BB MATING MATERIAL SURFACE ON WING IS CHAFED. REWORKED AREA IAW REO 601R-57-21-030 REV F. 2 L 7 2 4F RT A21EA 2007050700248 20070507 00248 EA 2007 5 7 COMA0760342 1 20070427 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 806CA 7359 RIGHT 718 FRAME IS CRACKED AT FS 718.00 BETWEEN STRINGERS 10 AND 12 EO 53-027, FUSELAGE-STRUCTURAL REPAIR NEEDS COMPLIED WITH ON W/O 252555. REPAIRED RIGHT SIDE FRAME AT FS 718 PER REO 601R-53-61-193 PART C OF SB 601R-53-055A IAW EO 53-027 . 2 L 7 2 4F RT A21EA 2007050700250 20070507 00250 EA 2007 5 7 COMA0760343 1 20070427 A 2810 HOUSING CNDAIR CL600 CL6002B19 1900309 EA WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 806CA 7359 LEFT AND RIGHT COLLECTOR TANK DRAIN VALVE HOUSING FWD AND AFT SCREW HOLES IN WING HAVE ELONGATED HOLES REF NR 00021, 000 22, 00023, 00024 ON MAJ REPAIR W/O 252555. REWORKED AREA IAW EA 10-5721-01684. 2 L 7 2 4F RT A21EA 2007050700251 20070507 00251 EA 2007 5 7 COMA0760344 1 20070428 A 7931 1153P0012 PRESSURE SWITCH CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 960CA 7117 FLIGHT 5637 - RIGHT ENGINE OIL PRESSURE WARNING DURING CLIMBOUT, AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOV ED AND REPLACED RIGHT ENGINE OIL PRESSURE SWITCH. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007050700252 20070507 00252 EA 2007 5 7 COMA0760345 1 20070428 A 7931 APTE142F10001 TRANSDUCER CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE FAULTY A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 987CA 4355 7199 FLIGHT 5354 - ABORTED TAKEOFF AT 80 KTS DUE TO LEFT ENGINE HIGH OIL PRESSURE. UNABLE TO DUPLICATE HIGH OIL PRESSURE, RE MOVED AND REPLACED ENGINE OIL PRESSURE TRANSDUCER. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007050700253 20070507 00253 EA 2007 5 7 COMA0760347 1 20070430 A 3260 M835362028M RELAY CNDAIR CL600 CL6002B19 1900309 EA WOW FAILED A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 629BR 7251 FLIGHT 5405 - NR 2 ENGINE THROTTLE BINDING ON TAKEOFF, ABORTED TAKEOFF. REMOVED AND REPLACED RIGHT WOW RELAY (2K2KE). 2 L 7 2 4F RT A21EA 2007050700255 20070507 00255 NM 2007 5 7 HNAA0700074 1 20070429 A 2910 82920010263 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM NR 2 BURST A HNAA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 07 907HA 56232 5472 011 AFTER GEAR RETRACTION, LOSS OF NR 2 HYD FLUID IN FLIGHT WITH NR 2 ISO VALVE CAUTION LIGHT AND F/A REPORTING FLUID ENTERI NG CABIN AREA NEAR ROW 5 & 6 DF THRU PSU'S. FOUND UP HYD LINE BURST IN CABIN, CAPPED BOTH PRESSURE AND RETURN LINES, LE AK CHECK GOOD. AIRCRAFT FERRIED TO SBY FOR INSPECTION, CLEANING AND LINE REPLACEMENT. 2 H 7 2 4T RT A13NM 2007050700256 20070507 00256 NM 2007 5 7 HNAA0700075 1 20070428 A 3260 82400033039 PROXIMITY SWITCH DHAV DHC8 DHC8102 2809003 NM NLG FAULTY A HNAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 07 827EX 30664 8679 DCL44795 390 RED UNSAFE LIGHT FOR NOSE GEAR ILLUMINATED INFLIGHT ASSOCIATED WITH CLUNKING NOISE FROM NOSE GEAR. INSPECTED BEAM AND N OSE DECK FOR CRACKS, NONE FOUND. CHECKED PSEU FOR FAULTS (CODE 10 APPEARED), REMOVED AND REPLACED NOSE GEAR DRAG STAY P ROXY SWITCH, ADJUSTED GAP, SWUNG GEAR SEVERAL TIMES, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007050700258 20070507 00258 NM 2007 5 7 PIDA07030 1 20070501 A 5230 65C8073525 STRUCTURE BOEING 737 7372K5 138448X NM CARGO DOOR CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 DURING MAINTENANCE, NOTED FORWARD AND AFT CORNERS OF THE AFT CARGO DOOR LOWER -T- CORD ARE CRACKED. REPLACED -T- CORD I N ACCORDANCE WITH DRAWING 65C80735 AND SRM 51-30-1. 2 L 7 2 4F RT A16WE 2007050700259 20070507 00259 NM 2007 5 7 PIDA07029 1 20070426 A 5315 FLOORBEAM BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 DURING MAINTENANCE, NOTED CORROSION ON UPPER CORD OF BS 294 FLOORBEAM FROM BL 0 TO LBL 12. REPLACED SECTION OF FLOORBEA M -T- CAP FROM LBL 12 TO THE RIGHT SERVICE DOOR PER SRM 53-10-9 FIGURE 5. 2 L 7 2 4F RT A16WE 2007050700260 20070507 00260 NM 2007 5 7 PIDA07028 1 20070430 A 5340 STRINGER CLIP BOEING 737 7372K5 138448X NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 DURING MAINTENANCE, NOTED STRINGER 18LT TIE CLIP CRACKED AT BS 277. REPLACED TIE CLIP PER SRM 51-30-02 AND DRAWING 65-7 3744. 2 L 7 2 4F RT A16WE 2007050700262 20070507 00262 NM 2007 5 7 R61A20070008 1 20070424 A 2781 1702288A SENSOR EMB ERJ170 ERJ170100SU 3260403 NM L/E SLAT FAULTY A R61A O OTHER N FALSE WARNING AP APPROACH 1 GL 11 823MD 4251 17000044 PILOT REPORTED SLAT FAIL MESSAGE ON EICAS DURING APPROACH, DECLARED EMERGENCY FOLLOWED QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO A/C. TROUBLESHOT AND REMOVED AND REPLACED RIGHT HAND OUTBOURD SKEW SENSOR AND HARNESS. OPERATIONAL CHECK GOOD AND RETURNED A/C TO SERVICE. 2 L 7 2 4F RT A56NM 2007050700263 20070507 00263 SO 2007 5 7 RAIA00705001 1 20070501 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 819HK 145062 POST FLT NR 5596 - STL - EMERGENCY LIGHT MAIN DOOR EXIT MARKER LIGHT DIM. MAINTENANCE RESEATED QUICK DISCONNECT CONNECT ORS ON MAIN DOOR EMERGENCY LIGHTS, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007050700264 20070507 00264 SO 2007 5 7 RAIA00704075 1 20070427 A 3610 BLEED AIR SYS EMB 145 EMB145LR 3260212 SO NR 1 ENGINE LEAKING A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 816HK 145055 FLT NR 5574 - PIT - NR 1 ENGINE BLEED LEAK IN FLIGHT. MAINTENANCE PLACED ON DEFERRAL PER MEL. 2 L 7 2 4T RT T00011AT 2007050700265 20070507 00265 SO 2007 5 7 RAIA00704074 1 20070427 A 3350 100865 BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 814HK 145046 PRE FLT NR 5535 - STL - GALLEY WALL EXIT LOCATOR AND FWD CEILING EXIT LOCATOR EMERGENCY LIGHTS OUT. MAINTENANCE REMOVED AND REPLACED BATTERY NR 1, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007050700267 20070507 00267 SO 2007 5 7 RAIA00704078 1 20070429 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 818HK 145059 PRE FLT NR 5576 - STL - COCKPIT FLOOD LIGHT EMERGENCY LIGHT IS INOP. MAINTENANCE REMOVED AND REPLACED NR 1 EMERGENCY LI GHT BATTERY POWER SUPPLY, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007050700268 20070507 00268 SO 2007 5 7 RAIA00704077 1 20070428 A 3620 M835362024M RELAY EMB 145 EMB145LR 3260212 SO BLEED AIR SYS FAILED A RAIA K NONE O OTHER TX TAXI/GRND HDL 1 CE 03 844HK 14500838 FLT NR 7982 - ALB - BLEED 2 LO TEMP EICAS MESSAGE DOES NOT APPEAR DURING TEST. MAINTENANCE REMOVED AND REPLACED BLEED T EST RELAY, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007050700271 20070507 00271 EU 2007 5 7 YENA2007029 1 20070430 A 2121 20092455101 FAN AIRBUS 320 A320232 3930326 EU E&E BAY FROZEN A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 615JB 2461 FLT 477, BOS-OAK, AT APPROX 0145Z, DIVERTED TO ORD, AFT AVIONICS RACK SMOKE INDICATION IN FLIGHT. FOUND AFT RACK VENT F AN FAIL LIGHT ILLUMINATED AND VENT FAN FROZEN UP. REPLACED AFT VENT FAN SYSTEM. OPERATED FOR TWO HOURS WITH NO DEFECTS NOTED, SYSTEM OPS CHECK GOOD PER AMM 23-39-00. 2 L 7 2 4F RT A28NM 2007050700275 20070507 00275 NM 2007 5 7 NOCA08907 1 20070430 A 5312 BULKHEAD BOEING 757 75728A 1384976 NM FUSELAGE CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 750NA 26277 LEVEL 1 CORROSION CENTER WEB STA 1102 AT HYD BULKHEAD FITTING LEFT MLG WHEEL WELL. REMOVED CORROSION AND BLENDED AREA A S PER SRM 53-40-12, REPAIRED PER ESO 90309. 2 L 7 2 4F RT A2NM 2007050700276 20070507 00276 NM 2007 5 7 NOCA09007 1 20070430 A 5312 BULKHEAD BOEING 757 75728A 1384976 NM FUSELAGE CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 750NA 26277 LEVEL 1 CORROSION CENTER WEB STA 1100 AT HYD BULKHEAD FITTING RIGHT MLG WHEEL WELL. REMOVED CORROSION AND BLENDED AREA AS PER ESO 90309. 2 L 7 2 4F RT A2NM 2007050700278 20070507 00278 NM 2007 5 7 NOCA09207 1 20070430 A 5320 TRANS PANEL BOEING 757 75728A 1384976 NM FUSELAGE CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 750NA 26277 LIGHT SCATTERED CORROSION TRANSITION PANEL STA 1220-1280 RIGHT SIDE. REMOVED CORROSION, TREATED, PRIMED AND PAINTED AS PER SRM 51-10-01 AND 52-20-01. 2 L 7 2 4F RT A2NM 2007050700281 20070507 00281 NM 2007 5 7 NOCA09607 1 20070430 A 5320 TRANS PANEL BOEING 757 75728A 1384976 NM FUSELAGE CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 750NA 26277 LIGHT SCATTERED CORROSION TRANSITION PANEL STA 1420-1530 LEFT SIDE. REMOVED CORROSION, TREATED PRIMED AND PAINTED AS PE R SRM 51-10-01 AND 51-20-01. 2 L 7 2 4F RT A2NM 2007050700283 20070507 00283 NM 2007 5 7 NOCA09807 1 20070504 A 3260 857801 SWITCH BOEING 767 767306 1385148 NM RIGHT MALFUNCTIONED A NOCA K NONE N FALSE WARNING LD LANDING 1 EA 15 768NA 29898 LANDING GEAR DOORS EICAS ILLUMINATED AFTER LANDING GEAR SELECTED DOWN. PERFORMED BITE ON PSEU PER FIM 32-09-03 AND 32-3 0-00, REPLACED S264 RIGHT LATCH SWITCH NR 2 SYS PER MM 32-61-02, OPS CHECK OK. 2 L 7 2 4F RT A1NM 2007050700286 20070507 00286 NM 2007 5 7 USAA070332 1 20070501 A 5310 STOP FITTING BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 503UW 23237 AFT FRAME OF FWD CARGO DOOR SURROUND AT BS 492 S-24R LOWER DOOR STOP CRACKED. INSTALLED DOUBLER PER EA 98633, DEFECT SI ZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007050800002 20070508 00002 NM 2007 5 8 SB07036 1 20070503 A 5610 58935842 WINDOW BOEING 737 7374B7 1384702 NM COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 456UW 15377 15377 25020 MCO FLT 1908 - EN ROUTE FROM PBI TO DCA, THE FIRST OFFICER'S NR 5 EYEBROW WINDOW SHATTERED. CAPTAIN ELECTED TO DIVERT T O MCO. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICER'S NR 5 EYEBROW WINDOW PER MM 56-11-31. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2007050800003 20070508 00003 NM 2007 5 8 USAA070354 1 20070501 A 5320 TIE CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 STA 807 STR 4, STRINGER TIE CLIP CRACKED. REPLACED TIE CLIP PER SRM 51-10-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007050800004 20070508 00004 NM 2007 5 8 USAA070345 1 20070501 A 5320 SUPPORT BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 STA 727D + 12 INCHES AT RBL 2, ANTENNA BRACKET SUPPORT MOUNT CRACKED. DRILLED & INSTALLED NEW PART PER SRM 51-10-02, DE FECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007050800005 20070508 00005 NM 2007 5 8 USAA070346 1 20070501 A 5320 FLOOR SUPPORT BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 BETWEEN BL 0 TO RBL 24 AT STA 540 FLOOR SUPPORT ANGLE CRACKED. REMOVED & REPLACED SUPPORT ANGLE PER SRM 51-10-02, DEFEC T SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007050800006 20070508 00006 NM 2007 5 8 USAA070347 1 20070501 A 5512 SKIN BOEING 737 7374B7 1384702 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 BOTTOM SIDE OF RT HORIZ STAB SKIN SPAR STA 133.70 CRACKED. INSTALLED DOUBLER PER TR 55-10-07, REV B, DEFECT SIZE: 1 IN CH. 2 L 7 2 4F RT A16WE 2007050800008 20070508 00008 NM 2007 5 8 USAA070349 1 20070501 A 5320 TIE CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 BS 500C S-3R, TIE CLIP, STRINGER CRACKED. REMOVED TIE CLIP & INSTALLED NEW PER SRM 51-10-02, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007050800009 20070508 00009 NM 2007 5 8 USAA070350 1 20070501 A 5320 TIE CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 BS 706, S-11L, TIE CLIP, STRINGER CRACKED. REMOVED TIE CLIP & INSTALLED NEW PER SRM 51-10-02, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007050800012 20070508 00012 NM 2007 5 8 F3LA200700103 1 20070423 A 5754 SKIN AIRBUS A319 A319111 3930336 NM NR 1 SLAT DENTED A F3LA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 NM 03 904FR SA2589 1579 DURING TAKEOFF, NR 2 ENGINE FAN COWL DEPARTED AIRCRAFT HITTING NR 1 SLAT. SLAT HAD SEVERE DENT DAMAGE TO LEADING EDGE O F STRUCTURE. REPLACED NR 1 SLAT IAW AMM 27-84-63-400-002, REFERENCE SDR F3LA200700083. 2 L 7 2 4F RT A28NM 2007050800013 20070508 00013 NM 2007 5 8 F3LA200700104 1 20070423 A 5512 SKIN AIRBUS A319 A319111 3930336 NM HORIZONTAL STAB PUNCTURED A F3LA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 NM 03 904FR AR1607 1579 DURING TAKEOFF, NR 2 ENGINE FAN COWL DEPARTED AIRCRAFT HITTING OTBD HORIZONTAL STABILIZER LEADING EDGE. PUNCTURE WAS FO UND ABOUT MID SPAN OF LEADING EDGE. REPLACED RT OTBD HORIZONTAL STAB L/E IAW AMM 55-12-11-400-001, REFERENCE SDR F3LA20 0700083. 2 L 7 2 4F RT A28NM 2007050800014 20070508 00014 WP 2007 5 8 07FDEA01694 1 20070503 A 5347 S492914727700 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 1501 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 FOUND MAIN DECK SEAT TRACK CRACKED STA 1501 RBL8. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED SEAT TRACK SPLICE PLATE AND SPLICE HAT IAW DC/MD 10 SRM 51-21-01 VOL I, PAGE 1-30. FOR FINAL INSTALLATION OF SEAT TRACK SEE N/R N00567. 2 L 7 3 4F A22WE 2007050800015 20070508 00015 WP 2007 5 8 07FDEA01695 1 20070503 A 5347 492914713500 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 1581 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 FOUND MAIN DECK SEAT TRACK CRACKED STA 1581 RBL8. REMOVED AND REPLACED SEAT TRACK SECTION IAW STA 1501-1581 IAW DC/MD 1 0 SRM 53-70- 00 VOL I AND 51-31-01 VOL.II PAGE 1-30. SEE N/R NOO567-SDR NR 07-1694. 2 L 7 3 4F A22WE 2007050800017 20070508 00017 NM 2007 5 8 07FDEA01697 1 20070504 A 5330 6554575 SKIN BOEING 727 7272S2F 1384O81 NM ZONE 100 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 AGING A/C INSPECTION FOUND EXISTING FLUSH REPAIR BETWEEN STA 720D-720E AT STR 19R ON LAP SPLICE. REPAIR HAD ADDITIONAL WEAR ON THE FILLER. REMOVED WORN FILLER, FABRICATED FILLER AND INSTALLED. REF SRM 53-30-3 FIG 14. 2 L 7 3 4F A3WE 2007050400211 20070504 00211 WP 2007 5 4 DXTA200702169 2 20070501 A 7300 UNKNOWN RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP FUEL SYSTEM MALFUNCTIONED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 811QS 258614 P107719 ENG NR 1 FUEL AND FUEL LOOK UP LIGHT CAME ON DURING T/O ROLL. T/O ABORTED AT APPROX 60 KTS, LIGHT WENT OUT WITH THROTTLE S REDUCTION. REPLACED BOTH FUEL FILTERS P/N 897830-1. RAN BOTH ENGINES. OPS & LEAK CHECK GOOD. NO DEFECTS NOTED IAW H80 0XP MM CHP 73-22-01. REF FAS 07-1085. 2 L 7 2 4F 4 F RT A3EU E6WE 2007050400222 20070504 00222 NM 2007 5 4 AALA20070709 1 20070417 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 915AN 29516 TUL EMERGENCY LIGHT AT STATION 609 IN MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT STATION 609 I N MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A16WE 2007050400224 20070504 00224 NM 2007 5 4 AALA20070710 1 20070417 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 915AN 29516 TUL EMERGENCY LIGHT AT STATION 322 IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT STATION 3 22 IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A16WE 2007050400236 20070504 00236 WP 2007 5 4 ABXA070145 1 20070406 A 5313 5920319504 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 LONGERON 30 CRACKED ON BOTH SIDES - FS 439 TO 446. REMOVED AND REPLACED LONGERON 30, STA 439 TO 446 IAW DC9 SRM. 2 L 7 2 4F A6WE 2007050400247 20070504 00247 NM 2007 5 4 CALA0700208 1 20070425 A 5311 6546557 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 FOUND CRACKED FRAME AT STA 887, STR 9LT. REPAIRED IAW ECRA 5310-04623. 2 L 7 2 4F RT A16WE 2007050400261 20070504 00261 NM 2007 5 4 CALA0700217 1 20070425 A 3397 BR963180 WIRE HARNESS BOEING 737 7373T0 1384582 NM CABIN UNKNOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 76355 23593 FOUND EMERGENCY LIGHT ON SEAT 21C INOP. REPAIRED IAW AMM 33-51-81. 2 L 7 2 4F RT A16WE 2007050400264 20070504 00264 NM 2007 5 4 CALA0700227 1 20070503 A 5311 6546593 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17329 23459 INSPECTION FOUND FORWARD CARGO COMPARTMENT FRAME CORRODED AT STA 500 BETWEEN STRINGER 26L AND 27L. A SHEAR TIE AND FILL ER WERE INSTALLED IAW SRM 53-00-07. 2 L 7 2 4F RT A16WE 2007050400267 20070504 00267 NM 2007 5 4 CALA0700221 1 20070422 A 5330 6545774 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17328 23458 INSPECTION FOUND A 2.125" CRACK IN LT FUSELAGE SKIN AT STA 727E, S24L, AFT OF EMERGENCY LIGHT. REPAIRED IAW SRM 53-00-0 1, REPAIR 31. 2 L 7 2 4F RT A16WE 2007050400268 20070504 00268 NM 2007 5 4 CALA0700222 1 20070430 A 5310 147A812634 DOOR FRAME BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 35204 30576 INSPECTION FOUND THE R-2 LOWER DOOR SILL AFT FRAME CHORD CORRODED AT STA 992.8, S17R, RBL 45. REPAIRED IAW ECRA 5311-01 315. 2 L 7 2 4F RT A16WE 2007050400273 20070504 00273 EA 2007 5 4 QXEA200700695 1 20070414 A 5330 SKIN PANEL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 C4 OKC - PANEL 684HT HAS MINOR CHAFING. REPAIRED IAW SRM 57-52-01 AND 51-21-11. 2 L 7 2 4F RT A21EA 2007050400278 20070504 00278 EA 2007 5 4 QXEA200700702 1 20070413 A 5310 DOOR FRAME CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 C4 OKC - AVIONICS BAY DOOR CUTOUT HAS MINOR CORROSION ON INNER SKIN. REPAIRED IAW SRM 51-21-06, 53-21-01. 2 L 7 2 4F RT A21EA 2007050400297 20070504 00297 NM 2007 5 4 07FDEA01656 1 20070427 A 5330 6554583 SKIN BOEING 727 7272S2F 1384O81 NM FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 210FE 22932 FOUND EXISTING EXTERNAL REPAIR APPROX STA 1050 AT STR 20L. DID NOT CONFORM TO CURRENT SRM 53-30-3 ON AGING A/C INSPECTI ON. REMOVED EXTERNAL REPAIR, FABRICATED STRUCTURAL FILLER AND REPAIR DOUBLER AND INSTALLED REF SRM 53-30-3 FIG 5, PAGES 20-23 2 L 7 3 4F A3WE 2007050400306 20070504 00306 NM 2007 5 4 07FDEA01666 1 20070430 A 5753 HINGE FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 LEFT WING, OUTBOARD FLAP INBOARD HINGE AFT SUPPORT FITTING FORWARD BOLT HOLE FOUND CORRODED. REMOVED & REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT & TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094. 2 L 7 3 4F RT A22WE 2007050700007 20070507 00007 CE 2007 5 7 BUW2007F00002 1 20070401 A 5415 FITTING CESSNA 182 182T 2072703 CE LYC O540 IO540* 41532 EA FUEL LINE LOOSE E BUWA O OTHER O OTHER NR NOT REPORTED 1 EA 07 199CA 18281548 DURING THE INSPECTION FOR SB 07-71-01 THE FUEL RETURN LINE AT THE FIREWALL BULKHEAD FITTING WAS FOUND LOOSE. (K) 1 H 7 1 3O 3 O NT 3A13 1E4 2007050700012 20070507 00012 EA 2007 5 7 TRAX200700589 1 20070429 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 980EV 7759 CAPT'S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007050700020 20070507 00020 EA 2007 5 7 TRAX200700584 1 20070428 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 752EV 10166 FWD FA FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007050700039 20070507 00039 EA 2007 5 7 TRAX200700595 1 20070501 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 884AS 7513 RANRC 298. RT OBLIQUE ANGLE CRACKED IN AEB. [SUP 05-11-07] REMOVED AND REPLACED RT OBLIQUE ANGLE, P/N 601-35012-52, IA W BOMBARDIER CRJ 200 SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007050700042 20070507 00042 EA 2007 5 7 TRAX200700596 1 20070501 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 884AS 7513 RANRC 319. ESCAPE CREW HATCH HAS WORN PLACARD (EMERGENCY EXIT). [SUP 05-08-07] REMOVED AND REPLACED ESCAPE CREW EMERGE NCY PLACARD WITH NEW SERVICEABLE PLACARD P/N S1859 IAW CRJ 200 AMM 11-20-00. 2 L 7 2 4F RT A21EA 2007050700070 20070507 00070 NM 2007 5 7 DU4R2007116 1 20070427 A 5330 148N32161 SKIN BOEING 757 757232 1384965 NM BS 1851-1854 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 637DL 23760 FOUND CORRODED SKIN AT BS 1845 BS 1850 LBL 24 (EMPENNAGE INTERNAL). REPAIRED BY TRIMMING OUT CORRODED AREA, HFEC INSPEC TED NO CRACKING NOTED. FABRICATING AND INSTALLING PERMANENT REPAIR DOUBLER 9.5 BY 10.0 FROM 7075-T6 .063 AND FILLER FRO M 7075-T6 .071 CLAD IAW DELTA ERA 460838-14 REV ORIGINAL DATED 4-26-07, B757 SRM 53-00-01 FIGURE 101, DETAIL II, 51-40-0 8, FAA FORM 8100-9. 2 L 7 2 4F RT A2NM 2007050700074 20070507 00074 NM 2007 5 7 DU4R2007119 1 20070421 A 5343 S113N1031 TRUNNION BOEING 757 757232 1384965 NM BS 1180 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 637DL 23760 FOUND CORRODED RT MLG AFT TRUNNION BEARING AND HOUSING. REPAIRED BY REMOVING AND REPLACING TRUNNION BEARING AND HOUSING WITH P/N NR S113N103-05 S/N K05639 IAW B757 MM 57-54-07. 2 L 7 2 4F RT A2NM 2007050700075 20070507 00075 EA 2007 5 7 TRAX200700603 1 20070502 A 5320 FLANGE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 884AS 7513 FS 280 UPPER AFT FLANGE IS CRACKED ON RT SIDE O/B OF RBL 9. [SUP 05-11-07] REPAIRED FS 280 UPPER AFT FLANGE R/H O/B OF RBL 9 PER: REO 601R-53-11-136. COMPLIED WITH EO 600-53-0091. 2 L 7 2 4F RT A21EA 2007050700088 20070507 00088 EA 2007 5 7 TRAX200700604 1 20070502 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 CORROSION ON FLOOR ANGLE LT AND RT BTWN FS 409.0 + 128 TO FS 559.00. [SUP 05-15-07] ON FLOOR ANGLE L/H AND R/H. COR ROSION REMOVED AS PER SRM 51-21-06. CORROSION PREVENTION AS PER SRM 51-21-11 AND PAINT AS PER SRM 51-21-11. MATERIAL T HICKNESS .080, MATERIAL REMOVED .002, WITHIN LIMITS PER SRM 53-41-45 FIGURE 101. 2 L 7 2 4F RT A21EA 2007050700148 20070507 00148 NM 2007 5 7 SWAA072218 1 20070503 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050700152 20070507 00152 NM 2007 5 7 SWAA072227 1 20070503 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050700165 20070507 00165 NM 2007 5 7 UPS07549746 1 20070403 A 5311 146N102885 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 414UP 23854 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1320, BETWEEN S25L AND S26L. TRIMMED OUT DAMAGED AREA 1.55"W X 1 .10"L IAW EA 757-5362-27-A1643 STEP 1. HFEC INSPECTED AREA PER NTM 51-00-00 PT6. NO CRACK INDICATION NOTED. TRIMMED O UT .040" AROUND CUT FINAL DIMENSION 1.6"W X 1.10"L. FABBED REPAIR ANGLE IAW MAE TRAVELER T7/674692 MAT'L 7075-0 080C BA TCH 481491, HEAT TREAT TO T6 LOT 20587. 2 L 7 2 4F RT A2NM 2007050700167 20070507 00167 WP 2007 5 7 UPS07849742 1 20070426 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 LEFT WING CENTER L/E UPPER RIB CRACKED AT XFS 484. STOP DRILLED CRACK IAW SRM 57-02-00. FABRICATED AND INSTALLED 2 DOUBLERS IAW SRM 57-02-00, 51-1-21, AND 51-1-20D. 2 L 7 4 4F RT 4A25 2007050700174 20070507 00174 NM 2007 5 7 USAA070357 1 20070504 A 5753 6546434301MC WEDGE BOEING 737 7374B7 1384702 NM T/E FLAP DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 441US 24812 LT I/B TE FLAP WEDGE. REMOVED DAMAGE & INSTALLED REPAIR DOUBLER PER EA 98647. DEFECT SIZE: 3" DIA. 2 L 7 2 4F RT A16WE 2007050700198 20070507 00198 EA 2007 5 7 COMA0760335 1 20070422 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 931CA 31147 7037 BULKHEAD WEB CRACKED AT FS 559 BETWEEN RBL 9 AND RBL 18. INCORPORATED A PERMANENT REPAIR PER EA 10-5341-01667. 2 L 7 2 4F RT A21EA 2007050700202 20070507 00202 EA 2007 5 7 COMA0760334 1 20070421 A 3230 46193 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 659BR 7509 FLIGHT 4984 - ON APPROACH RECEIVED GEAR DISAGREE WARNING MESSAGE. RAN QRH. LANDED CVG WITHOUT INCIDENT. REPLACED NLG PRIORITY VALVE. PROBLEM PERSISTED. REPLACED MLG PRIORITY VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007050700212 20070507 00212 SO 2007 5 7 C2XA07SH024 1 20070504 A 5534 14540881003 BUSHING EMB 145 EMB145EP 3260221 SO VERTICAL STAB WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13936 145025 SHV - DURING C-CHECK RIGHT SPHERICAL BEARING FITTING ON VERTICAL STAB HINGE POINT IS WORN BEYOND TOLERANCE. MX REPAIRED RIGHT SPHERICAL BEARING FITTING ON VERTICAL STAB HINGE POINT BY REAMING TO 2ND REWORK AND INSTALLING OVERSIZE BUSHING I AW EMB 145 SRM 55-30-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050700225 20070507 00225 EA 2007 5 7 COMA0760339 1 20070427 A 3234 601R751461 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 804CA 17366 7352 FLIGHT 5475 - GEAR DISAGREE, NOSE DOOR INDICATED INTRANSIT, AIRCRAFT RETURNED BACK TO BOS AND LANDED SAFELY. REMOVED AN D REPLACED NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2007050700249 20070507 00249 EA 2007 5 7 COMA0760340 1 20070427 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 806CA 7359 LEFT WING FUEL PANEL 540BB MATING SURFACE ON WING IS CHAFED. REWORKED AREA IAW REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2007050700261 20070507 00261 NM 2007 5 7 PIDA07027 1 20070427 A 5315 FLOORBEAM BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 DURING MAINTENANCE, NOTED CORROSION ON THE UPPER CORD OF THE BS 344 FLOORBEAM FROM LBL 50 TO RBL 16. INSTALLED REPLACEM ENT SECTION OF -T- CAP PER SRM 53-10-09. 2 L 7 2 4F RT A16WE 2007050700269 20070507 00269 EU 2007 5 7 YENA2007027 1 20070424 A 5210 SEAL EMB ERJ190 ERJ190100IGW 3260408 EU PAX DOOR DIRTY A YENA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 15 206JB 19000025 FLT 1242, TPA TO BOS, RETURNED TO TPA AFTER HEARING LOUD WIND NOISE FROM 1R DOOR AND VIBRATION. PRESSURIZATION NOTES: CABIN ALT 7300 FT, RATE OF CLIMB 700-800 FPM, AP 4 PSI, AT FL190. CLEANED DOOR SEAL & PERFORMED PRESSURIZATION CHECK IA W AMM 21-31-00-720-802A. NO AIR LEAK NOTED AT R-1 DOOR. FOUND GALLEY DRAIN VALVE HANDLE NOT FULLY CLOSED. MINOR LEAK NOTED AND CORRECTED. A/C OK FOR CONTINUED SERVICE. 2 L 7 2 4F RT A57NM 2007050700274 20070507 00274 NM 2007 5 7 NOCA08807 1 20070430 A 5312 BULKHEAD BOEING 757 75728A 1384976 NM FUSELAGE CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 750NA 26277 CORROSION - CENTER WEB STA 1100 AT HYD BULKHEAD FITTING LEFT MLG WHEEL WELL. REMOVED CORROSION AND BLENDED AREA PER SRM 53-40-12, REPAIRED PER ESO 90309. 2 L 7 2 4F RT A2NM 2007050700284 20070507 00284 NM 2007 5 7 NOCA09907 1 20070503 A 3350 BPS73 CHARGER BOEING 767 767306 1385148 NM CABIN INOPERATIVE A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 768NA 29898 RIGHT HAND FIRST CLASS EMERGENCY FLOOR LIGHTS DIM THEN EXTINGUISH. REPLACED FWD BATTERY CHARGER, OPS CHECK OK. 2 L 7 2 4F RT A1NM 2007050800001 20070508 00001 NM 2007 5 8 USAA070343 1 20070501 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 STUB FRAME ATTACH POINT BS 616 & LBL 64 CRACKED. INSTALLED REPAIR ANGLE PER TYP REP 53-62-05, DEFECT SIZE: .250 INCH. 2 L 7 2 4F RT A16WE 2007050800019 20070508 00019 EU 2007 5 8 F3LA200700100 1 20070421 A 5320 D53480043207 SILL AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 801FR 4759 1939 DURING C-3 CHECK, INSPECTION REPORTED R2 DOOR SILL PLATE CORRODED FWD OF FR66. REPLACED R2 DOOR SILL IAW SRM 51-42-11. 2 L 7 2 4F RT 2007050800020 20070508 00020 NM 2007 5 8 DHL2007788509 1 20070418 A 5753 652163229 SKIN BOEING 727 727214 138407R NM LT WING TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 LEFT INBD MID FLAP LWBL 85-100, LOWER T/E CHORD CRACKED THREE PLACES ON CUTOUTS. CUTOUT DAMAGE AREA 46.625" BY 2" IAW B 727 SRM 51-40-3, FIG 1. FABRICATED NEW ANGLE FROM BAC1503-100046-7075T6, 46.625" BY 2" AND TWO EACH SPLICES FROM BAC 15 03-100046-7075T6, 7.375" BY 2" IAW B727 SRM 51-40-3, FIG 1 AND 57-50-2, FIG 5. TREATED PRIMED AND INSTALLED PARTS IAW B 727 SRM 51-10-2, 51-30-2 AND 57-50-2, FIG 5. 2 L 7 3 4F A3WE 2007050800021 20070508 00021 NM 2007 5 8 QXEA200700713 1 20070429 A 5246 85414708101 ACCESS DOOR BOMBDR DHC8 DHC8402 1390042 NM NR 1 HYD BAY UNLATCHED A QXEA O OTHER O OTHER CL CLIMB 1 NM 09 410QX 4053 PDX FLIGHT NR 2351: MECHANIC RIDING IN BACK REPORTED THE NR 1 HYD ACCESS DOOR CAME UNLATCHED AND THEN SEPARATED FROM TH E AIRCRAFT. MAINTENANCE REPLACED THE NR 1 HYD ACCESS DOOR BY INSTALLING + RIVETS. CHECKS GOOD. AIRCRAFT RETURNED TO S ERVICE. 2 H 7 2 4T RT A13NM 2007050800022 20070508 00022 NM 2007 5 8 QXEA200700714 1 20070502 A 5230 DITCHING DAM BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 400QX 4030 SEA FLIGHT 2438: ON PUSHBACK, DITCHING DAM ON MCD FELL. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND RESET DITCHING DAM ON MCD. CHECKS OK. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007050800023 20070508 00023 NM 2007 5 8 QXEA200700716 1 20070503 A 5210 DITCHING DAM BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 400QX 4030 PDX FLIGHT NR 2262: MAIN CABIN DOOR DITCHING DAM FELL OFF. AIRCRAFT RETURNED TO GATE. MAINTENANCE RESET THE DITCHING D AM WITH NO OTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007050800025 20070508 00025 EA 2007 5 8 QXEA200700711 1 20070416 A 5730 SKIN CNDAIR CL600 CL6002C10 1390015 EA LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 C4 OKC - LEFT WING FIXED LEADING EDGE CHAFED AFT OF THE MATING POINT OF SLAT NR 1 AND NR 2. REPAIRED IAW SRM 51-12-00, 57-41-01, 51-21-11. 2 L 7 2 4F RT A21EA 2007050800026 20070508 00026 EA 2007 5 8 QXEA200700709 1 20070414 A 5754 SKIN CNDAIR CL600 CL6002C10 1390015 EA NR 2 SLAT DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 C4 OKC - LEFT SLAT NR 2 LEADING EDGE IS SCRATCHED. REPAIRED IAW SRM 57-42-01, 51-10-06, 51-21-06. 2 L 7 2 4F RT A21EA 2007050800027 20070508 00027 EA 2007 5 8 QXEA200700710 1 20070414 A 5754 SKIN CNDAIR CL600 CL6002C10 1390015 EA NR 1 SLAT DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 C4 OKC - LEFT SLAT NR 1 LEADING EDGE IS SCRATCHED. REPAIRED IAW SRM 57-42-01, 51-21-11, 51-10-00. 2 L 7 2 4F RT A21EA 2007050800028 20070508 00028 EA 2007 5 8 QXEA200700707 1 20070417 A 5330 PANEL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 C4 OKC - FOUND PANEL 584JB HAS LIGHT CHAFING. REPAIRED IAW SRM 57-52-01. 2 L 7 2 4F RT A21EA 2007050800029 20070508 00029 EA 2007 5 8 QXEA200700708 1 20070116 A 5730 PANEL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 C4 OKC - FOUND PANEL 584AB CHAFED AT CUTOUT. REPAIRED IAW 51-12-00, 57-51-01. 2 L 7 2 4F RT A21EA 2007050800032 20070508 00032 NM 2007 5 8 USAA070353 1 20070501 A 5320 TIE CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 STR 15R AT BS 270, STRINGER TIE CLIP CRACKED. REPLACED TIE CLIP PER SRM 51-10-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007050800033 20070508 00033 NM 2007 5 8 F3LA200700102 1 20070423 A 5754 D5746027700100 SKIN AIRBUS A319 A319111 3930336 NM NR 2 SLAT DENTED A F3LA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 NM 03 904FR SA2579 1579 DURING TAKEOFF, NR 2 ENGINE FAN COWL DEPARTED AIRCRAFT HITTING NR 2 SLAT. SLAT HAD SEVERE DENT AND GOUGE TO LEADING EDG E OF STRUCTURE. REPLACED NR 2 SLAT IAW AMM 27-84-64-400-002, REFERENCE SDR F3LA200700083. 2 L 7 2 4F RT A28NM 2007050800034 20070508 00034 NM 2007 5 8 USAA070342 1 20070501 A 5320 TIE CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 STA 827 S4R CRACKED. REMOVED & REPLACED TIE CLIP PER SRM 51-10-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007050800035 20070508 00035 2007 5 8 SB07035 4 20070428 A 3441 HG1050AD04 IRU BOEING 737 7374B7 1384702 NM E&E BAY FAILED A USAA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 EA 19 458UW 50166 50166 25022 MCO FLT 1672 - CLIMBING THROUGH 3,000 FEET OUT OF MCO, EN ROUTE TO BWI, CREW REPORTED BOTH ADI'S AND HSI'S FAILED. FLIG HT RETURNED TO FIELD AT MCO AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND RE PLACED THE NR 2 IRU. PERFORMED SATISFACTORY FUNCTIONAL CHECK PER MM. COULD NOT VERIFY PROBLEM WITH NR 1 IRU. FUNCTION AL CHECK OF LEFT IRU SYSTEM GOOD. REMOVED AND REPLACED RIGHT DAA PER MM 34-28-41. OPERATIONAL TEST GOOD. 2 L 7 2 4F RT A16WE 2007050800037 20070508 00037 NM 2007 5 8 USAA070287 1 20070418 A 5514 6548240511 TIE BOEING 737 737401 1384701 NM HORIZ STAB WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 LEFT HORIZONTAL STA 0 AT REAR SPAR HAS WEAR. REMOVED AND REPLACED BOW TIE PER SRM 51-01-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007050800038 20070508 00038 WP 2007 5 8 DHL2007806516 1 20070328 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP BS 1560-1580 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 FUS AFT ACCY COMPT INTERNAL DOUBLER CORRODED (STA 1560.000 - 1580.000, L-22R). REMOVED CORROSION FROM INTERNAL DOUBLER (STA 1540.000 - 1580.000) IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED INTERNAL DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED INTERNAL DOUBLER (AL7075T6 0.025") IAW SRM 53-4-1 FIG 17A. CLEANED, TREATED AND PRIMED INTERNAL DOUBLER AND AREA IAW SRM 51-1-8B. INSTALLED INTERNAL DOUBLER IAW SRM 51-1-21, SRM 51-1-20D, SRM 51- 3-1 (TORQUE) (STA 1510.000 - 1580.000) 2 L 7 4 4F RT 4A25 2007050800041 20070508 00041 WP 2007 5 8 DHL2007806600 1 20070416 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 55 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT FLOORBEAM CORRODED STA 55.000 RBL 54 (FLOORBEAM SEGMENT) MAJOR REPAIR. REMOVED CORROSION IAW SRM 51-1- 8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FLOORBEAM IAW SRM 51-1-20D. FABRICATED NEW FLO OR (EXTRUSION P/N S2772345) IAW SRM 53-3-1 FIG 6. CLEANED, TREATED AND PRIMED AREA AND NEW FLOORBEAM IAW SRM 51-1-8B. INSTALLED NEW FLOORBEAM IAW SRM 51-1-20D, SRM 51-3-1 PG 2A (TORQUE). THIS MAJOR REPAIR WAS PERFORMED IAW SRM 53-1-0 PG 1, SRM 53-3-1 FIG 6. 2 L 7 4 4F RT 4A25 2007050800042 20070508 00042 NM 2007 5 8 BB07035 1 20070429 A 5330 149T76172 ACCESS PANEL BOEING 767 7672B7 1385107 NM FUSELAGE DEPARTED A USAA K NONE D INFLIGHT SEPARATION CR CRUISE 1 EA 19 256AY 26847 FLIGHT 1012, PHL-STT: DURING FLIGHT, RIGHT ADP ACCESS PANEL LIBERATED FROM FUSELAGE WITH RESULTING SECONDARY FUSELAGE D AMAGE. MAINTENANCE REPLACED PANEL 195NL AND ACCOMPLISHED FUSELAGE REPAIRS FOR SECONDARY DAMAGE. 2 L 7 2 4F RT A1NM 2007050800045 20070508 00045 NM 2007 5 8 2007UALA01376 1 20070501 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 CABIN DOOR 2 RIGHT CUTOUT FOR UPPER HINGE HAS 0.25 INCH CRACK. [SUP 06-06-07] INSTALLED A DOUBLER REPAIR ON THE AFFEC TED AREA WITH BOEING APPROVED UA ENGINEERING SPECIFICATION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050800046 20070508 00046 NM 2007 5 8 2007UALA01378 1 20070502 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 EMERGENCY CEILING LIGHT ROW 44R & ROW 13 INOP. RELAMPED EMERGENCY CEILING LIGHT, OP CHECKS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050800047 20070508 00047 NM 2007 5 8 2007UALA01379 1 20070501 A 3350 58673 INVERTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 509UA 24763 F-C EMERGENCY ESCAPE PATH LIGHTING INOP. REPLACED POWER INVERTER. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050800048 20070508 00048 EU 2007 5 8 2007UALA01380 1 20070502 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 433UA 589 L2 DOOR SILL HAS CORROSION AT AFT SIDE NEAR FRAME 68. MAJOR REPAIR ACCOMPLISHED: INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007050800050 20070508 00050 NM 2007 5 8 2007UALA01382 1 20070503 A 5420 FITTING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 PYLON CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 104UA 26902 LIGHT CORROSION - BOTH DIAGONAL SIDE BRACE WING FITTING LUG BORE AT NR 4 PYLON. [SUP 05-29-07] ACCOMPLISHED BORING THE DUAL SIDE BRACE WING FITTING LUG BOTH HOLES PER COA 899993040 & SB 747-54A2218. FINAL HOLE DIA: INBD=2.2449, OUTBD=2.27 50. A/C OK FOR RETURN TO SERVICE. GALVANIC REACTION & VIBRATION AGGRAVATED BY HIGH TEMP CAUSED DUAL SIDE BRACE HOLE SU RFACE DETERIORATION. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050800051 20070508 00051 NM 2007 5 8 2007UALA01383 1 20070502 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 RIGHT MAIN CABIN FLOOR STRUCTURE, EVIDENCE OF CORROSION BETWEEN FLOOR WEB AND SUPPORT ANGLE, BS 1681, RBL 34. MAJOR REP AIR ACCOMPLISHED: REMOVED ENTIRE LENGTH OF DAMAGED FLOORBEAM T-CAP. FABRICATED & INSTALLED REPLACEMENT CHORD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050800052 20070508 00052 NM 2007 5 8 2007UALA01384 1 20070503 A 2621 BOTTLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 & NR 2 NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 372UA 24637 ON PREFLT, THE CARGO FIRE EXT BOTTLE 1 AND 2 ARMED LIGHTS DON`T COME ON WHEN PANEL TESTED OR WHEN CARGO PIT ARMED SW IS PLACED IN FWD OR AFT CARGO POSITIONS. REPLACED 1 AND 2 CARGO BOTTLES, DIVERTER VALVE, FILTERS AND METERING VALVE.REF. 2 L 7 2 4F 4 F RT A16WE E21EU 2007050800053 20070508 00053 NM 2007 5 8 2007UALA01385 1 20070503 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY EEL LIGHT INOPERATIVE AT SEAT 5A AFT EEL LIGHT. [SUP 05-08-07] RELAMPED. OPS CHECKED GOOD. [SUP 05-16-07] RELAMPED. OPS CHECKED GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050800054 20070508 00054 NM 2007 5 8 2007UALA01386 1 20070503 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY LIGHT INOP AT DOOR 2L AFT SILL LIGHT. [SUP 05-08-07] RELAMPED. OPS CHECKED GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050800056 20070508 00056 NM 2007 5 8 2007UALA01388 1 20070502 A 2530 CHILLER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DIRTY A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 654UA 25392 SMOKE ODOR REPORTED IN BUSINESS CLASS GALLEY CHILLER AREA. [SUP 05-29-07] REPLACED AIR CHILLER AS PER AMM 25-33-04. CLEANED DIRTY VENTS. CHECKED OKAY FOR SERVICE. SUSPECT CHILLER MOTOR OVERHEATED AS VENT BECAME RESTRICTED BY DEBRIS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050800058 20070508 00058 EU 2007 5 8 2007UALA01390 1 20070502 A 2560 GIRT BAR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE AFT LT DOOR DIRTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 409UA 462 AFT LEFT DOOR WILL NOT ARM. [06-26-07] CLEANED DEBRIS FROM GIRT BAR AREA. 2 L 7 2 4F 4 F RT A28NM E40NE 2007050800059 20070508 00059 NM 2007 5 8 2007UALA01391 1 20070501 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 337UA 24241 FWD CARGO DOOR CUTOUT AFT FRAME WEB HAS TWO EACH CRACKS AT LWR DOOR STOP FITTING FASTENER HOLES. MAJOR REPAIR ACCOMPLIS HED: REMOVED DAMAGE. FABRICATED & INSTALLED EXTERNAL NESTED ANGLE REPAIRS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007050800060 20070508 00060 NM 2007 5 8 2007UALA01341 1 20070428 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 503UA 24624 FUSELAGE DAMAGE TO AFT CARGO PIT DOOR THRESHOLD AND SURROUNDING STRUCTURE. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SKIN. MFG & INSTALLED FILLER AND DOUBLER REPAIR. INSTALLED NEW CENTER THRESHOLD PLATE AND NEW FWD CORNER PLATE. SEALE D ALL EDGES. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050800062 20070508 00062 NM 2007 5 8 2007UALA01344 1 20070428 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 FWD PIT, LEFT SIDE STA 660 BETWEEN STR 25 AND 26L, MAIN FRAME HAS DENT INTO RADIUS UPPER BEND. MAJOR REPAIR ACCOMPLISHE D: TRIMMED OUT DAMAGE. COLD WORKED HOLES & INSTALLED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050800063 20070508 00063 NM 2007 5 8 2007UALA01345 1 20070428 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 FWD PIT, LEFT SIDE, STA 580 BETWEEN STR 24L AND 25L, MAIN FRAME IS DENTED 3 PLACES, WITH ONE INTO FRAME UPPER RADIUS BEN D. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGE. COLD WORK HOLES & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050800064 20070508 00064 NM 2007 5 8 2007UALA01348 1 20070429 A 5210 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 R-2 DOOR FRAME IS CRACKED AT UPPER HINGE CUTOUT, .25 INCH LONG, FOUND AT THE 7 O'CLOCK POSITION. MAJOR REPAIR ACCOMPLIS HED: CUT OUT DAMAGED AREA. FABRICATED & INSTALLED A CRES DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050800065 20070508 00065 NE 2007 5 8 2007UALA01358 2 20070430 A 7200 PILOT VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 502UA 24623 726533 RTFL DUE TO SMOKE IN COCKPIT. [SUP 06-06-07] FOLLOWED SOP AND SHUTDOWN UTILITY BUSSES, ODOR AND SMOKE DISSIPATED SLIGH TLY. INSPECTION OF NR 1 ENG FOUND EVIDENCE OF OIL COMING OUT OF 2.8 COMPRESSOR BLEEDS AT 6 O'CLOCK & OUT OF 8TH STG BLE ED PNEUMATIC DUCTS. ALSO FOUND METAL DEBRIS IN 8TH STG CHECK VALVE. REPLACED PILOT VALVE AND HIGH STAGE VALVE. REPLAC ED NR 1 ENGINE. THE EXACT CAUSE OF THIS IRREGULARITY COULD NOT BE ESTABLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050800069 20070508 00069 NM 2007 5 8 2007UALA01362 1 20070428 A 3350 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 811UA 847 EMERGENCY LIGHT TEST FAILED. FAULTED EPSU BATTERY LEFT. [SUP 05-08-07] REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATT ERY. TEST OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007050800070 20070508 00070 NM 2007 5 8 2007UALA01364 1 20070430 A 2822 PUMP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE LEFT FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 664UA 29236 LEFT AFT FUEL BOOST PUMP FAILED IN FLIGHT. [SUP 05-24-07] LEFT AFT FUEL BOOST PUMP INOP. REPLACED PUMP PER MM 28-22 - 03 . OP CHECKED OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050800071 20070508 00071 NM 2007 5 8 2007UALA01365 1 20070430 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 FUSELAGE SKIN CRACKED AT STA 516-518 AT CHEM MILLED STEP .5 INCH BELOW STR 12L. MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT DAMAGE & NDT FOR CRACK CONTAINMENT. FABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007050800072 20070508 00072 NM 2007 5 8 2007UALA01366 1 20070430 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 FWD ENTRY DOOR (1L) LOWER HINGE CUTOUT HAS 1 EACH FASTENER HOLE CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE FRO M HOLE & BEAR STRAP. NDT FOR CRACK CONTAINMENT. FABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR AT CUTOUT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007050800073 20070508 00073 NM 2007 5 8 2007UALA01367 1 20070430 A 5210 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 NR 2 LEFT DOOR FWD FRAME CUTOUT FOR UPPER HINGE CRACKED. [SUP 06-06-07] INSTALLED A DOUBLER REPAIR ON THE AFFECTED ARE A WITH BOEING APPROVED UA ENGINEERING SPECIFICATION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050800075 20070508 00075 WP 2007 5 8 DHL2007806571 1 20070415 A 5340 37799782 FITTING DOUG DC8 DC873F 302199F WP BS 702 L18L CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 FOUND MAIN CARGO COMPT FITTING CRACKED 1.500" STA 702.875 L-18L. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TR EATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-120D, SRM 51-3-1 PG 2A (TORQUE). REFER TO JC EC-00246-001 (WO 470) FOR FITTING FABRICATION. 2 L 7 4 4F RT 4A25 2007050800082 20070508 00082 WP 2007 5 8 DHL2007806577 1 20070417 A 5315 975400288 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1220 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 ITEM REF. NR. 049960: AFT CARGO COMPT FLOORBEAM SUPPORT FITTING CORRODED, STA 1220.000 RBL 50". REMOVED CORROSION IAW S RM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FITTING IAW SRM 51-1-20D. FABRICATED N EW FITTING (AL7075"0" 0.125") IAW DWG# 9754002. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTIN G IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE) REFER TO JC EC-00263-001 (WO 470) FOR FITTING FABRICATION. 2 L 7 4 4F RT 4A25 2007050800086 20070508 00086 WP 2007 5 8 DHL2007806518 1 20070404 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT WING WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 RT INBD FLAP UPPER SKIN WORN STA XW 105.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOVED DAMAG ED PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED PLATING (AL2024T3 0.040") IAW SRM 57-7-1 FIG 1 ITEM D, SRM 51-1 -14 PG 1. CLEANED, TREATED AND PRIMED AREA AND NEW PLATING INNER FACE IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFA CE IAW SRM 51-1-11. INSTALLED NEW PLATING IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007050800094 20070508 00094 WP 2007 5 8 DHL2007806566 1 20070410 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 920 S6-7R DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT FRAME HAS A MISDRILLED HOLE STA 920.000 L-6R TO L-7R. PERFORMED MAJOR REPAIR IAW FAA FORM8110-3 DATED 04-04-07, JC EC-00283-001, REPAIR ORDER NR 2-50701-801 DATED 04-04-07 (ED-4499). PERFORMED NDT INSPECTION IAW DC8 NDT S PM PART 06-10-01-001. NO CRACK OR CORROSION FOUND. CLEANED AND REFINISHED DAMAGED AREA IAW REPAIR ORDER NR 2-50701-801 , SRM 53-2-0 FIG 1F SHEET 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007050800095 20070508 00095 WP 2007 5 8 DHL2007806596 1 20070418 A 5200 DOUBLER DOUG DC8 DC873F 302199F WP ACCESS DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 RT WING ACCESS DOOR NR 505E INTERNAL DOUBLER CRACKED 0.250" STA XRS 128.000 S-5 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 04-18-07, BOEING MESSAGE NR 1-306853011-4 DATED 04-17-07, NR 1-306853011-2 DATED 03-27-07. RE MOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTION IAW BOEING MSG NR 1-306853011-2, NR 1-306853011-4, SEMAN DWG NR ED-4481-1, SRM 57-2-1 FIG 36. PERFORMED NDT INSP IAW BOEING NDT SPM PART 08-00-02 TO 07. FABRICATED INTE RNAL REPAIR DOUBLER (AL7075T6 0.063") EXTERNAL DOUBLER (AL7075T6 0.160") AND FILLER (7075T6511 0.360") IAW BOEING MESSAG E NR 1-306853011-2, 1-306853011-4, SEMAN DWG NR ED-4481-1. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51 2 L 7 4 4F RT 4A25 2007050800098 20070508 00098 WP 2007 5 8 DHL2007806582 1 20070416 A 5410 INLET DOUG DC8 DC873F 302199F WP RT NACELLE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 NR 3 ENG LT/RT NACELLE INLET COWL WORN STA YN 157.000 AT 12 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2, 3. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN (AL202 4T3 0.080") AND SPLICE (STEEL 17-7PH 0.050") IAW DC8 70 SRM 71-5-2 FIG 2 SHEET 1, 2, 3. HEAT TREATED SPLICE FROM 17-7PH CRESS TO 17-7PH CRESS (H1050) IAW SRM 51-1-16. CLEANED, TREATED AND PRIMED AREA AND SKIN IAW SRM 51-1-8B. APPLIED SEA LANT TO FAYING SURFACE IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW SRM 71-5-2 FIG 2 SHEET 1, 2, 3, SRM 51-1-21A. 2 L 7 4 4F RT 4A25 2007050800099 20070508 00099 WP 2007 5 8 DHL2007806575 1 20070415 A 5340 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT FITTING CRACKED 1.500" STA 5.000 RBL 46". REMOVED CRACKED FITTING IAW SRM 51-1-120D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050800100 20070508 00100 WP 2007 5 8 DHL2007806593 1 20070417 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP BS 865 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 RT MLG INBD DOOR JAMB FLANGE WORN STA 865 RBL 45 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-09 -07, ENGINEERING VARIATION AUTHORIZATION NR D852-00001 REV IR DATED 03-14-07. REMOVED FASTENERS IAW SRM 51-1-21. CUT O UT DAMAGED SECTION AND FABRICATED "Z" ANGLE (7075"0" 0.063") AND (2EA) SPLICES (AL7075"0" 0.071") IAW ASTAR DWG ES-D8520 0001-001-D, DOUGLAS DWG 5616307. HEAT TREATED "A" ANGLE AND SPLICE FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-17. PE RFORMED NDT INSP IAW DPS 4.707-1. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW ASTAR DWG NR ES D85200001-001-D, SRM 51-1-21. REFER TO JC 8-32-00-003 FOR OPS CHECK. 2 L 7 4 4F RT 4A25 2007050800101 20070508 00101 WP 2007 5 8 DHL2007806594 1 20070418 A 5230 DOOR DOUG DC8 DC873F 302199F WP BS 1400-1420 MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 806DH 89284 46002 REPAIR ON FWD LWR CORNER OF "D" CARGO DOOR (STA 1400.000 - 1420.000 L-31R TO L-35R) IS NOT IN ACCORDANCE WITH DWG NR SR0 8530019 (SHOWS CORROSION TOO) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW DOUGLAS DWG NR 5779936. REMOVED NON STANDARD RE PAIR IAW SRM 51-1-21, SRM 51-1-20D. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2 P. REMOVED CORRODED SKIN PANEL IAW SRM 51-1-21, SRM 51-1-20D. CLEANED TREATED AND PRIMED AREA AND NEW SKIN PANEL IAW S RM 51-1-8B. INSTALLED NEW SKIN PANEL (P/N 5615371-71N1) (2014T6 0.071" AL) IAW DOUGLAS DWG NR 5779936, SRM 53-4-1 FIG 1 7A ITEM "B", SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE) SRM 51-1-11. REPAIR ON "D" CARGO DOOR IAW DWG NR SR08530019 2 L 7 4 4F RT 4A25 2007050800102 20070508 00102 WP 2007 5 8 DHL2007806586 1 20070417 A 5711 FRAME DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 RT WING INBD L/E FORMER WITH CRACKS 1" AND 1.500" (MAJOR REPAIR) STA XCW 69.000. PERFORMED MAJOR REPAIR IAW SRM 57-3-3 FIG 1. REMOVED CRACKED FORMER IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED FORMER (AL7075"0" 0.090") IAW SRM 57-3-3 FI G 1, SRM 51-1-4. HEAT TREATED FORMER FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED ARE A AND FORMER IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-12. INSTALLED NEW FORMER IAW SRM 51-1-20 D, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007050800110 20070508 00110 WP 2007 5 8 DHL2007806515 1 20070328 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 1580 L11L CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT INTERCOSTAL SUPPORT ANGLE CRACKED 1" STA 1580.000 L-11L. REMOVED CRACKED INTERCOSTAL SUPPORT ANGLE IAW SRM 51-1-21. FABRICATED ANGLE (AL 7075T6 0.040") IAW SRM 53-2-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND ANGLE IAW SRM 51-1-8B. INSTALLED ANGLE IAW SRM 51-1-21 2 L 7 4 4F RT 4A25 2007050800115 20070508 00115 WP 2007 5 8 DHL2007806558 1 20070410 A 5340 3750025503 FITTING DOUG DC8 DC873F 302199F WP BS 781 L18R CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT FITTING CRACK 1" STA 781.500 L-18R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PR IMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 PG 2A (TORQUE). REFER TO JC EC-00253-001 (WO 470) FOR FITTING FABRICATION. 2 L 7 4 4F RT 4A25 2007050800118 20070508 00118 WP 2007 5 8 DHL2007806507 1 20070328 A 5340 3758496U2 FITTING DOUG DC8 DC873F 302199F WP BS 1140-1120 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 AFT CARGO COMPT BILGE FITTING CRACKED STA 1140.000 - 1120.000 L-35R. REMOVED AND REPLACED CRACKED FITTING IN AFT CARGO COMPT BILGE (STA 1140.000 - 1120.000, L-35R) IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050800124 20070508 00124 WP 2007 5 8 07FDEA01678 1 20070501 A 5710 STRUCTURE DOUG MD10 MD1010F 3022112 WP FUSLEAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 390FE 46624 DURING LAX "C" CHECK VISIT W.O 36243; RH OB FLAP - IB FWD HINGE ASSEMBLY 3 STRUCTURAL CRACKS WERE DISCOVERED. ARB2431- 2 (OB SIDE OF ASSEMBLY )1.25" CRACK FROM 1ST TO 2ND FASTENER. 1.25" CRACK FROM 5TH TO 6TH FASTENER. NON-ROTINE N0 1103 ARB2431-502 (IB SIDE OF ASSEMBLY) 1.00" CRACK FROM 10TH TOWARD 11TH FASTENER. EA 8-5710-105699 WAS CREATED. BO EING HAS DETERMINED THAT THE CRACK (S) CONDITION IS STRUCTURALLY ACCEPTABLE FOR CONTINUED SERVICE. E.A. 8-5710-105699 REQUIRES AN INSPECTION AT EACH "B" CHECK UNTIL THE HINGE SUPPORTS ARE REPLACED AT NO LATER THAN THE NEXT "C" CHECK O R 24 MONTHS. THE HINGE SUPPORT FITTINGS WILL BE REPLACED WITH IMPROVED PARTS. 2 L 7 3 4F RT A22WE 2007050800140 20070508 00140 EU 2007 5 8 PNSA070302 1 20070318 A 2697 WIRE SAAB SF340 340B 7860101 EU RT ENGINE LOOSE A PNSA E D ENGINE SHUTDOWN RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 AL 03 675PA 340B206 RIGHT ENGINE TAILPIPE HOT WARNING LIGHT CAME ON DURING TAXI. ENGINE WAS SHUT DOWN AND MAINTENANCE WAS CALLED. MX FOUND WIRES LOOSE ON AFT INBOARD HEAT DETECTOR AND SEALANT WAS IN PLACE. LAST INSPECTION OF HEAT DETECTORS WAS PERFORMED 868 HOUR PREVIOUSLY. WEATHER CONDITIONS AT ANC WAS CLEAR AND CALM, TEMPERATURE 5 DEGREES F AT 6:30 LOCAL. 2 L 7 2 4T RT A52EU 2007050800141 20070508 00141 EU 2007 5 8 CPCP2007009 1 20070302 A 5347 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 545AT 545 RIGHT I/B SEAT TRACK CORRODED. SEAT TRACK REPLACED IAW SRM 51-25-03. 2 H 7 2 4T RT A53EU 2007050800142 20070508 00142 EU 2007 5 8 CPCP20070007 1 20070302 A 5320 STRUCTURE AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 545AT 545 RIGHT Z-FLOOR CORRODED. RIGHT Z-FLOOR REPLACED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007050800143 20070508 00143 EU 2007 5 8 CPCP20070008 1 20070302 A 5320 THRESHOLD AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 545AT 545 PAX DOOR THRESHOLD CORRODED. PAX DOOR THRESHOLD REPLACED AS PER SRM 51-25-01 AND 51-25-03. 2 H 7 2 4T RT A53EU 2007050800144 20070508 00144 EU 2007 5 8 CPCP20070002 1 20070323 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 420AT 0420 CORROSION FOUND ON FLOORBEAM ON FRAME 40. 2 H 7 2 4T RT A53EU 2007050800145 20070508 00145 EU 2007 5 8 CPCP20070010 1 20070304 A 5320 STRUCTURE AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 545AT 545 CORROSION FOUND ON RIGHT INNER CHORD. RIGHT INNER CHORD BETWEEN FRAME 16 - 18 REPAIRED IAW SRM 53-31-50 FIG 402. 2 H 7 2 4T RT A53EU 2007050800146 20070508 00146 EU 2007 5 8 CPCP20070006 1 20070302 A 5347 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 545AT 545 RIGHT O/B SEAT TRACK CORRODED. RIGHT O/B SEAT TRACK REPLACED AS PER SRM 51-75-04. 2 H 7 2 4T RT A53EU 2007050800147 20070508 00147 NM 2007 5 8 SWAA072275 1 20070505 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050800148 20070508 00148 NM 2007 5 8 SWAA072254 1 20070504 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007050800149 20070508 00149 NM 2007 5 8 SWAA072273 1 20070505 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050800150 20070508 00150 NM 2007 5 8 SWAA072282 1 20070505 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050800151 20070508 00151 NM 2007 5 8 SWAA072267 1 20070505 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050800152 20070508 00152 NM 2007 5 8 SWAA072274 1 20070505 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050800153 20070508 00153 NM 2007 5 8 SWAA072261 1 20070505 A 3350 8100137801 LENS BOEING 737 7377H4 1384404 NM EXTERIOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 714CB 27848 DURING SCHEDULED MV2 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT EXTERIOR LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007050800154 20070508 00154 2007 5 8 SWAA072244 4 20070504 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007050800155 20070508 00155 2007 5 8 SWAA072259 4 20070504 A 2565 D31354 SLIDE BOEING 737 7373T5 1384608 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 696SW 23064 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007050800156 20070508 00156 NM 2007 5 8 SWAA072257 1 20070504 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 756SA 27872 DURING SCHEDULED HC1 CHECK, LEFT FWD CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY P ACK PER MM. 2 L 7 2 4F RT A16WE 2007050800158 20070508 00158 EU 2007 5 8 CPCP20070004 1 20070302 A 5347 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 545AT 545 LEFT I/B SEAT TRACK CORRODED. LEFT I/B SEAT TRACK BETWEEN FRAME 13 TO 23 REPLACED IAW SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007050800159 20070508 00159 EU 2007 5 8 CPCP20070005 1 20070302 A 5347 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 545AT 545 RIGHT I/B SEAT TRACK CORRODED. RIGHT I/B SEAT TRACK REPLACED AS PER SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007050800160 20070508 00160 EU 2007 5 8 CPCP20070003 1 20070302 A 5347 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 545AT 545 LEFT O/B SEAT TRACK CORRODED. SEAT TRACK REPLACED IAW SRM 57-25-04. 2 H 7 2 4T RT A53EU 2007050800161 20070508 00161 NM 2007 5 8 WRNA200700023 1 20070323 A 5753 65B01901208 FLAP BOEING 747 747230B 1384889 NM RT WING DELAMINATED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 508MC 21644 DURING B-CHECK, RIGHT INBOARD FORE FLAP WAS FOUND WITH DAMAGE, A 42 INCH LONG X 19 INCH WIDE PREVIOUS REPAIR, 45 INCHS F ROM OUTBOARD END, DEPARTED FORE FLAP WITH 40% MATERIAL LOSS. ACCOMPLISHED REPAIR PER 747 SRM 51-40-12. 2 L 7 4 4F A20WE 2007050800165 20070508 00165 NM 2007 5 8 2007UALA01327 1 20070429 A 3520 OXYGEN MASK BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE COCKPIT DAMAGED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 669UA 30025 FLIGHT DIVERTED DUE TO FIRST OFFICER'S OXYGEN MASK PROBLEM. [SUP 05-24-07] FIRST-OFFICER'S O2 MASK BROKEN. MOVABLE RE D SQUEEZE TAB BROKEN OFF AT BASE REPLACED FIRST-OFFICER'S O2 MASK . SUSPECT ROUGH HANDLING BY FLIGHT CREW. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050800166 20070508 00166 WP 2007 5 8 DHL2007806535 1 20070409 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 55 L21R CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 FOUND MAIN CARGO COMPT FITTING CORRODED STA 55.000 L-21R. REMOVED CORROSION FROM FITTING IAW SRM 51-1-8 PG 17-18. FOUN D OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-0, SRM 51-3-1 PG 2A (TORQUE). 2 L 7 4 4F RT 4A25 2007050800168 20070508 00168 WP 2007 5 8 DHL2007806562 1 20070331 A 5340 3779498508 FITTING DOUG DC8 DC873F 302199F WP BS 902 L19R CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT FWD FITTING CRACKED 1" STA 902.125 L-19R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED A ND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 PG 2A (TORQUE). REFER TO JC EC-0251 -001 (WO 470) FOR FITTING FABRICATION. 2 L 7 4 4F RT 4A25 2007050800170 20070508 00170 WP 2007 5 8 DHL2007806537 1 20070405 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP BS 280-300 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 FOUND UPPER CARGO COMPT NR 2 TRACK LUG WORN (STA 280.000 - 300.000). REMOVED WORN SEGMENT OF TRACK NR 2 AND EXISTING SP LICES IAW SRM 53-2-3, SRM 51-3-0, SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA AND EXISTING SPLICES IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND REINSTALLED SPLICES IAW SRM 53-2-3 PG 49-50, SRM 51-1-21, SRM 51-3-0, SRM 51-3-1 PG 3 (T ORQUE). 2 L 7 4 4F RT 4A25 2007050800171 20070508 00171 WP 2007 5 8 DHL2007806544 1 20070405 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 980 DAMAGED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT FRAME HAS A MISDRILLED HOLE STA 980.000 L-12L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110 -3 DATED 03-30-07, REPAIR ORDER NR 2-50561-801 DATED 03-29-07 (ED4502). PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 0 6-10-01-001. NO CRACK OR CORROSION FOUND. ENCLOSED SMN FORM 242-2. PLUGGED MISDRILLED HOLE WITH RIVET (MS20470D) IAW SRM 53-2-0 FIG 1F SHEET 2, SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. REFER TO JC EC-00267-001 FOR REPAIR. 2 L 7 4 4F RT 4A25 2007050800173 20070508 00173 WP 2007 5 8 DHL2007806568 1 20070410 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 742 DAMAGED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT FRAME HAS A MISDRILLED HOLE AT STA 742.250 L-20R TO L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW F AA FORM 8110-3 DATED 04-04-07, JC EC-00283-001, REPAIR ORDER NR 2-50701-801 DATED 04-04-07 (ED-4497). PERFORMED NDT INS PECTION IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK OR CORROSION FOUND. CLEANED AND REFINISHED DAMAGED AREA IAW REPAIR ORDER NR 2-50701-801, SRM 53-2-0 FIG 1F SHEET 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007050800174 20070508 00174 WP 2007 5 8 DHL2007806552 1 20070411 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 1240 L35R CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 AFT CARGO COMPT BILGE FITTING CRACKED STA 1240.000 L-35R. REMOVED AND REPLACED CRACKED FITTING AT AFT CARGO COMPT BILGE STA 1240.000 L-35R IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050800178 20070508 00178 WP 2007 5 8 DHL2007806531 1 20070404 A 5730 DOUBLER DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 RT WING ACCESS DOOR NR 505F INTERNAL DOUBLER HAS TWO CRACKS OF 0.500" AND 0.250" STA XRS 18.000 S-5 (MAJOR REPAIR). PER FORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 36. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW SRM 57-2-1 FIG 36. PERFORMED NDT INSPECTION IAW SRM 57-2-1 FIG 36 PG 133-134. NO CRACK OR CORROSION FOUND AFTER CUT OUT. ENCLOSE D SMN FORM 242-4. FABRICATED EXT REPAIR DOUBLER (AL7075T6 0.160") INTERNAL DOUBLER (AL7075T6 0.063") AND FILLER (AL2024 T3 511 0.375") IAW SRM 57-2-1 FIG 36. APPLIED POLYURETHANE TOP YELLOW COATING TO FILLER IAW SRM 51-1-12 PG 7-12. CLEAN ED, TREATED AND PRIMED AREA AND INTERNAL/EXTERNAL DOUBLER IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 5 2 L 7 4 4F RT 4A25 2007050800180 20070508 00180 WP 2007 5 8 DHL2007806533 1 20070409 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT INTERNAL DOUBLER CORRODED (STA 8.000 - 25.000 L-21R). REMOVED CORROSION FROM INTERNAL DOUBLER IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED INTERNAL DOUBLER IAW SRM 53-1-0 PG 1,SRM 51-1-21. FABRICATED NEW INTERNAL DOUBLER (AL7075T6 0.025") IAW SRM 53-3-3 PG 3 FIG 1. CLEANED, TREATED AND PRIMED AREA AND INTER NAL DOUBLER IAW SRM 51-1-8B. INSTALLED NEW INTERNAL DOUBLER IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007050800181 20070508 00181 WP 2007 5 8 DHL2007806534 1 20070409 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 35 L21R CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT FITTING CORRODED STA 35.000 L-21R. REMOVED CORROSION FROM FITTING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51 -1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-0, SRM 51-3-1 PG 2A (TORQUE). 2 L 7 4 4F RT 4A25 2007050700064 20070507 00064 NM 2007 5 7 AWXA200700554 1 20070422 A 5340 6935350503 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23627 MCN - FOUND CRACKED STRINGER ATTACH CLIP, BS 500D, S12L. REPLACED STRINGER ATTACH CLIP, BS 500D, S12L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007050700065 20070507 00065 NM 2007 5 7 AWXA200700555 1 20070418 A 5340 69353521 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - FOUND CRACKED STRINGER ATTACH CLIP, BS 747, S14R. REPLACED STRINGER ATTACH CLIP, BS 747, S14R IAW B737-300 SRM 51 -40-02. 2 L 7 2 4F RT A16WE 2007050700092 20070507 00092 EA 2007 5 7 TRAX200700592 1 20070430 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 860AS 7433 AFT EMERGENCY FLOOR TRACK LIGHTING IS INOP. PERFORMED OPS TEST OF THE EMERGENCY FLOOR TRACK LIGHTING SYSTEM IAW CRJ200 AMM 33-50. OPS TEST GOOD. COULD NOT DUPLICATE PROBLEM. {SDR - CLOSED} 2 L 7 2 4F RT A21EA 2007050700128 20070507 00128 NM 2007 5 7 SWAA072236 1 20070503 A 5322 6546529 SHEAR TIE BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, RBL 7 TO LBL 7. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007050700132 20070507 00132 NM 2007 5 7 SWAA072237 1 20070503 A 5313 6551698 STRINGER SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER S RM. 2 L 7 2 4F RT A16WE 2007050700147 20070507 00147 NM 2007 5 7 SWAA072221 1 20070503 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050700149 20070507 00149 NM 2007 5 7 SWAA072222 1 20070503 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050700151 20070507 00151 NM 2007 5 7 SWAA072225 1 20070503 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050700158 20070507 00158 NM 2007 5 7 SWAA072231 1 20070503 A 5320 69620146 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED SERVICE CHECK, FOUND RIGHT W/W VERTICAL STIFFENER CRACKED AT BS 663.75, RBL 6.15. REPAIRED STIFFENER P ER SWA EA. 2 L 7 2 4F RT A16WE 2007050700160 20070507 00160 NM 2007 5 7 SWAA072243 1 20070503 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 270WN 29089 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007050700164 20070507 00164 NM 2007 5 7 UPS07549743 1 20070408 A 5412 311N3271 BULKHEAD BOEING 757 75724APF 1384969 NM NR 2 PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 414UP 23854 INSPECTION TYPE:C NR 2 PYLON AFT BULKHEAD LOWER SECTION LT & RT SIDES CHAFED. BULKHEAD MILL & NDT WERE DONE REF TRAV T7 /675147. ORIGINAL THICKNESS .200 REMOVED .040 REMAINING .160 X 1.25W X 2.1L ON I/B SIDE. O/B SIDE ORIGINAL THICKNESS . 200 REMOVED .080 REMAINING .120 X 1.25W X 2.1L PER PRELIMINARY 1 EA 757-5453-27-A1658 2. SHOT PEEN REWORK AREAS IAW SOP M 20-10-03 PER EA 757-5453-27-A1658 PRELIM 1 ACCOMPLISHED. 2 L 7 2 4F RT A2NM 2007050700175 20070507 00175 NM 2007 5 7 USAA070356 1 20070504 A 5230 6546921225XE SKIN BOEING 737 7374B7 1384702 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 441US 24812 UPPER AFT CORNER OF DOOR HANDLE CUTOUT. REMOVED DAMAGE, INSTALLED FABRICATED REPAIR PARTS PER TR 52-10-01A. DEFECT SIZ E: 1/4" CRACK 2 L 7 2 4F RT A16WE 2007050700195 20070507 00195 SO 2007 5 7 C2XA07IA099 1 20070428 A 3350 20131A BATTERY PACK EMB 145 EMB145EP 3260221 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15926 11521 788 145005 IAH - FLIGHT 2264, DURING PREFLIGHT INSPECTION, THE CREW REPORTED SOME OF THE AISLE PATH LIGHTING TO BE INOPERATIVE. MA INTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHE CKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050700207 20070507 00207 SO 2007 5 7 C2XA07IA094 1 20070423 A 2425 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO ELECTRICAL SYS MALFUNCTIONED A C2XA B A EMER. DESCENT UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 12922 145338 ICT - FLIGHT 2725, THE CREW REPORTED AN ELEC EMERGENCY ABNORMAL MESSAGE ON EICAS DURING CLIMB. THE CREW PERFORMED AN EM ERGENCY DESCENT, AND LANDED AT ICT WITHOUT INCIDENT. THE CREW RESET THE AIRCRAFT POWER AND VERIFIED NORMAL OPERATIONS, MX VERIFIED THAT LANDING WAS LESS THAN 6 FOS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050700214 20070507 00214 SO 2007 5 7 C2XA07TY022 1 20070427 A 5320 14004724005 STRUCTURE EMB 145 EMB145LR 3260212 SO FUSELAGE MISDRILLED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13553 145585 TYS - DISCREPANCY- MISSDRILLED HOLES ON RIGHT SIDE OF CARGO BETWEEN FRAME 62 AND 62A. INSTALLED REINFORCEMENT AT FRAME 62 AND 62A BETWEEN 11R AND 12R IAW EMB 145 EC5310-01407. 2 L 7 2 4T RT T00011AT 2007050700218 20070507 00218 SO 2007 5 7 C2XA07RI022 1 20070418 A 3230 22250100003 SOLENOID VALVE EMB 145 EMB145LR 3260212 SO LANDING GEAR DEFECTIVE A C2XA K NONE O OTHER CR CRUISE 1 SW 27 13970 14681 3588 145146 FLT 2745 - EWR - CREW REPORTED AT FL 350, SMOOTH AIR QUICK OPEN AND CLOSING SOUNDS COMING FROM NOSE WHEEL DOORS WERE AUD IBLE FROM COCKPIT AND FRONT CABIN. SOUND OCCURRED ABOUT SIX TIMES. EWR MX REMOVED AND REPLACED SOLENOID VALVE. MX PER FORMED LEAK CHECK AND OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050700221 20070507 00221 SO 2007 5 7 C2XA07RI021 1 20070430 A 2611 WARNING SYSTEM EMB 135 EMB135ER 3260203 SO SMOKE WARNING MALFUNCTIONED A C2XA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 27 27512 145274 FLT 2979 - BDL - CREW REPORTED LAV SMOKE IND ON EICAS WITH NO SMOKE. CREW RESET SYSTEM AND MESSAGE WAS CLEARED. 2 L 7 2 4F RT T00011AT 2007050700231 20070507 00231 NM 2007 5 7 AMTA200700175 1 20070327 A 2612 644501 PRINTED CKT BOAR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211* 54555 NE FIRE DETECTION FAULTY A AMTA K NONE N FALSE WARNING CR CRUISE 1 GL 11 519AT 27975 EICAS STATUS MSG RT ENG OH LP2 DISPLAYED. REMOVED AND REPLACED FIRE DETECTION PRINTED CIRCUIT CARD M684 IAW FIM 26-11-0 0 AND AMM 26-10-01-4, PERFORMED FIRE/OVHT TEST, NO FAULTS NOTED. (K) 2 L 7 2 4F 4 F RT A2NM A12EU 2007050700239 20070507 00239 WP 2007 5 7 07FDEA01693 1 20070503 A 5347 S492914713500 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 MAIN DECK LEFT SIDE SEAT TRACK SCALLOP WORN AT STA1385 LBL 27. FABRICATED, ALODINED, PRIMED AND INSTALLED SEAT TRACK SE CTION IN REF TO DC10 SRM 53-70-01 VOL 1,51-21-01 VOL.II AND 51-31-01 VOL II. 2 L 7 3 4F A22WE 2007050700243 20070507 00243 NM 2007 5 7 MWEA070097 1 20070426 A 5330 5940766505 SKIN BOEING 717 717200 1383700 NM FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 917ME 55179 FUSELAGE DENT AT STATION 237 BETWEEN LONGERON 18 LEFT & 19 LEFT. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2007050700254 20070507 00254 EA 2007 5 7 COMA0760331 1 20070416 A 5312 FLOOR SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 931CA 7037 DURING A HMV7 INSPECTION, THE PRESSURE FLOOR SKIN AT FS 460 BETWEEN LBL 9 AND RBL 9 WAS FOUND TO BE CRACKED IN 3 PLACES. PERFORMED REPAIR PER REO 601R-53-41-10. 2 L 7 2 4F RT A21EA 2007050700266 20070507 00266 SO 2007 5 7 RAIA00704076 1 20070427 A 3350 SG9632 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 849HK 145002 POST FLT NR 8053 - STL - FLOOR PROXIMITY LIGHT EMERGENCY LIGHTS OUT. MAINTENANCE INSTALLED EMERGENCY PATH STRIP. OPS C HECK GOOD. 2 L 7 2 4T RT T00011AT 2007050700270 20070507 00270 EU 2007 5 7 YENA2007028 1 20070424 A 5240 DEFLECTOR EMB ERJ190 ERJ190100IGW 3260408 EU R1 DOOR CANNING A YENA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 15 206JB 19000025 FLT 1242, TPA TO BOS, RETURNED TO TPA (2ND OCCURRENCE), AFTER HEARING DOOR NOISE AND CABIN PRESSURE PROBLEM, HAPPEN THRU 10K WHEN WING A1 CYCLES AT 16K LEVEL CABIN ALT STILL CONTINUED TO CLIMB WAS THRU 7400 BEFORE STARTING BACK DOWN. FOUND R-1 DOOR DEFLECTOR WORN AND OIL-CANNING. TRIMMED SEAL, ACCOMPLISHED CPCS BITE CHECK, NO FAULTS, PERFORMED FUSELAGE LEA K RATE CHECK AND FOUND TO BE WITHIN LIMITS PER AMM 21-31-00. PERFORMED VISUAL INSP OF UPPER-LOWER FUSELAGE SKIN, NO DEF ECTS NOTED. CHECKED PACKS ACM'S AND HEAT EXCHANGERS FOR LEAKS, NONE FOUND. NO EICAS MSG PRESENT. A/C OK FOR SERVICE. 2 L 7 2 4F RT A57NM 2007050700272 20070507 00272 2007 5 7 YENA2007030 4 20070430 A 2330 ENTERTAIN SYS AIRBUS 320 A320232 3930326 EU CABIN ODOR A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 593JB 2280 FLT 428, AT APPROX 0:45Z PBI TO BOS DIVERTED TO MCO, SMELL OF SMOKE REPORTED IN FWD LAV/ FWD GALLEY AREA. ACCOMPL TSM T ASK 24-00-00-810-823 ELEC BURNING SMELL OR FUMES IN CABIN. NO SMELL OF SMOKE NOTED. LVTV ACCOMP TSM TAS 23-39-000-810- 801 ELEC ODORS OR FUMES IN CABIN DUE TO LIVE TV SYS ROWS 1-3 A-F. NO DEFECTS NOTED. CHECKED WIRING IN PANELS 2000VU IN FWD GALLEY AND 80 VU IN E&E. NO DEFECTS NOTED. 2 L 7 2 4F RT A28NM 2007050700273 20070507 00273 NM 2007 5 7 NOCA08707 1 20070425 A 5753 SKIN BOEING 757 75728A 1384976 NM T/E FLAP CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 755NA 30043 LEVEL 1 CORROSION ON I/B FWD FLAP UPPER SKIN 18 - 36 INCHES I/B END 15 INCHES FROM T/E. REMOVED AND BLENDED OUT CORROSI ON PER 57-53-01, ALODINED AND PRIMERED AND PAINTED PER SRM 51-20-01. 2 L 7 2 4F RT A2NM 2007050700282 20070507 00282 NM 2007 5 7 NOCA09707 1 20070430 A 5320 TRANS PANEL BOEING 757 75728A 1384976 NM FUSELAGE CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 750NA 26277 LIGHT SCATTERED CORROSION TRANSITION PANEL STA 1530-1640 LEFT SIDE. REMOVED CORROSION, TREATED, PRIMED AND PAINTED AS P ER SRM 51-10-01 AND 51-20-01. 2 L 7 2 4F RT A2NM 2007050700285 20070507 00285 2007 5 7 NOCA09507 4 20070430 A 2565 D30654122 SLIDE BOEING 757 75728A 1384976 NM L1 DOOR ACTIVATED A NOCA O OTHER O OTHER UK UNKNOWN 1 EA 15 756NA 32448 L1 SLIDE INOP, FOUND L1 DOOR 1/4 OPENED. THE EVAC SLIDE HALF OUT OF CONTAINER CASE WITH THE GIRT BAR STILL ATTACHED TO THE DOOR FRAME. THE EVACUATION SLIDE HANDLE WAS IN THE ARMED POSITION AND THE DOOR ASSIST BOTTLE HAD FIRED. REMOVED AN D REPLACED L-1 DOOR SLIDE AND DOOR ASSIST BOTTLE REF EO 757-25-199 AND PL 756-25-01, OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2007050800010 20070508 00010 2007 5 8 QXEA200700715 4 20070503 A 2210 7003974730 COMPUTER DHAV DHC8 DHC8202 2809007 NM FLT GUIDANCE INOPERATIVE A QXEA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 09 356PH 4785 4785 502 PDX - ON FLIGHT 2211, ON CLIMB-OUT FO WAS HAND FLYING THE AIRCRAFT WHEN THE AUTOPILOT ENGAGED AND TURNED TO THE RIGHT. THE FO HIT THE DISENGAGE BUTTON ON THE YOKE AND THE AUTOPILOT DISENGAGED AND FLEW NORMALLY. AFTER THAT, THE FO WAS STAR TING A SHALLOW RIGHT TURN WHEN THE AUTOPILOT ENGAGED AND TRIED TO TURN FURTHER TO THE RIGHT. MAINTENANCE REMOVED AND RE PLACED THE FLIGHT GUIDANCE COMPUTER AND FGCP. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007050800011 20070508 00011 EA 2007 5 8 QXEA200700700 1 20070415 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 C4 OKC - FUSELAGE HAS SMALL SCRATCHES WHERE ANTENNA WAS REMOVED. REPAIRED IAW SRM 51-12-00 AND 51-20-08, 51-21-11. 2 L 7 2 4F RT A21EA 2007050800016 20070508 00016 NM 2007 5 8 USAA070351 1 20070501 A 5320 TIE CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 BS 663, S-10L, TIE CLIP, STRINGER CRACKED. REMOVED TIE CLIP & INSTALLED NEW PER SRM 51-10-02, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007050800024 20070508 00024 EA 2007 5 8 QXEA200700706 1 20070414 A 5330 PANEL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 C4 OKC - FOUND PANEL 584ET HAS MINOR CHAFING. REPAIRED IAW SRM 51-21-00, 51-12-00, AND 51-21-11. 2 L 7 2 4F RT A21EA 2007050800030 20070508 00030 EU 2007 5 8 F3LA200700101 1 20070427 A 5321 D53471124200 SHEAR PLATE AIRBUS A318 A318111 3940019 EU CABIN FLOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 801FR 4759 1939 DURING C-3 CHECK, INSPECTION REPORTED LT SIDE OF CABIN FLOOR WEB 69 AND 70 HAD VERY LIGHT CORROSION AT NUT PLATES, MOSTL Y ON LWR SIDE. REPLACED SHEAR PLATE IAW SRM 51-42-11. 2 L 7 2 4F RT 2007050800031 20070508 00031 NM 2007 5 8 USAA070352 1 20070501 A 5320 TIE CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 BS 747, S-4R, TIE CLIP CRACKED. REMOVED TIE CLIP & INSTALLED NEW PER SRM 51-10-02, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007050800044 20070508 00044 NM 2007 5 8 2007UALA01374 1 20070430 A 3350 60243 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 520UA 24890 EEL STRIP IN FRONT OF FWD AFT LAV INOPERATIVE. [SUP 05-08-07] REPLACED EEL STRIP. OPS CHK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050800049 20070508 00049 NM 2007 5 8 2007UALA01381 1 20070503 A 5420 FITTING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 PYLON CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 104UA 26902 LIGHT CORROSION - RIGHT DIAGONAL SIDE BRACE STRUT FITTING LUG BORE AT NR 4 PYLON. [SUP 05-29-07] ACCOMPLISHED BORING O F THE STRUT DUAL SIDE BRACE FTG LUG OUTBD HOLE PER COA 899993040 AND SB 747-54A2218 FIG 8. FINAL HOLE SIZE = 2.2450". A/ C OK FOR SERVICE. GALVANIC REACTION & VIBRATION AGGRAVATED BY HIGH TEMP CAUSED DUAL SIDE BRACE HOLE SURFACE DETERIORATI ON. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050800074 20070508 00074 WP 2007 5 8 DHL2007806564 1 20070410 A 5340 3750025504 FITTING DOUG DC8 DC873F 302199F WP BS 781 L18L CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT FITTING 1 INCH CRACK STA 781.500 L-18L. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AN D PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 PG 2A (TORQUE). REFER TO JC EC-00255 -001 (WO 470) FOR FITTING FABRICATION. 2 L 7 4 4F RT 4A25 2007050800076 20070508 00076 NM 2007 5 8 2007UALA01368 1 20070430 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 LOWER FUSELAGE SKIN DENTED AT BS 480 AT STR 22R. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED AREA. FABRICATED & INSTA LLED FILLER & INTERNAL DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050800077 20070508 00077 EU 2007 5 8 2007UALA01369 1 20070430 A 8011 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE SPARKS A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 483UA 1586 CREW REPORTS, DURING ENG 1 START NO N2 ROTATION WITH GOOD START VALVE OPEN INDICATION. RAMP REPORTED SPARKS FROM STARTE R AREA. [06-26-07] REPLACED THE STARTER AND START VALVE. PRESENCE OF SPARKS INDICATES PROBABLE INTERNAL BEARING FAILURE RESULTING IN TURBINE CONTACT WITH HOUSING. 2 L 7 2 4F 4 F RT A28NM E40NE 2007050800078 20070508 00078 NM 2007 5 8 2007UALA01370 1 20070430 A 3350 5880758781362624 LIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 942UA 26679 EEL LIGHTS INOP FROM ROW 8 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT. REPLACED EEL STRIP IN FRONT OF GALLEY CART STOWAGE. REPLACED CABLE FROM ROW 15 AFT TO GALLEY EEL STRIP. REPLACED EEL STRIPS AT ROW S 9 & 12. 2 L 7 2 4F 4 F RT A16WE E21EU 2007050800079 20070508 00079 WP 2007 5 8 DHL2007806554 1 20070408 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 RT CTR L/E OTBD SLOT HOLES ELONGATED, STA XOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-05-07, ENGINEERING VARIATION AUTHORIZATION NR D852-00003 DATED 03-18-07 REV IR. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED FILLER (AL7075T6 0.063") AND REPAIR DOUBLER (AL7075T6 0.071") IAW DWG ASTAR ESD85 200003-001-D. PERFORMED NDT INSPECTION IAW DACO DPS 4.707-1. CLEANED, TREATED AND PRIMED AREA, FILLER AND INNER FACE O F REPAIR DOUBLER IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW ASTA DWG NR ESD85200003-001-D, SRM 51-1-11, SRM 51-1-21, S RM 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050800081 20070508 00081 NM 2007 5 8 2007UALA01371 1 20070501 A 3350 SIGN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INTERMITTENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26877 UPPER DECK DOORS EXIT SIGNS INTERMITTENTLY FLASHING. OPS CHECKED EMERGENCY LIGHT SYSTEM. CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050800083 20070508 00083 WP 2007 5 8 DHL2007806504 1 20070325 A 5315 ANGLE DOUG DC8 DC873F 302199F WP BS 50 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 FWD ACCY COMPT SUB-FLOORBEAM ANGLE CORRODED STA 50.000 LBL 30". REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT O F LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED SUPPORT ANGLE IAW SRM 51-1-21. FABRICATED NEW SUPPORT ANGLE (AL2024T3 0.050") IAW SRM 53-2-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND SUPPORT ANGLE IAW SRM 51-1-8B. INSTALLED SUPPORT ANG LE IAW SRM 51-1-21, SRM 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050800084 20070508 00084 NM 2007 5 8 2007UALA01372 1 20070430 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 509UA 24763 R-1 EXTERIOR EMERGENCY LIGHT IS INOP. [SUP 05-16-07] RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050800085 20070508 00085 NM 2007 5 8 SWAA072262 1 20070505 A 5311 6546551 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050800087 20070508 00087 NM 2007 5 8 SWAA072263 1 20070505 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050800088 20070508 00088 NM 2007 5 8 SWAA072264 1 20070505 A 5311 6546557 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 14L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050800089 20070508 00089 NM 2007 5 8 SWAA072271 1 20070505 A 5311 6546593 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050800091 20070508 00091 WP 2007 5 8 DHL2007806590 1 20070419 A 5340 37540252 FITTING DOUG DC8 DC873F 302199F WP BS 1220 S26R CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 AFT CARGO COMPT FITTING 3 INCH CRACKED STA 1220.000 L-26R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). REFER TO JC EC-00247-001 FOR FITTING FABRICATION (WO 470). 2 L 7 4 4F RT 4A25 2007050800092 20070508 00092 NM 2007 5 8 SWAA072268 1 20070505 A 5310 6546958 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 470, RBL 65. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007050800093 20070508 00093 NM 2007 5 8 SWAA072270 1 20070505 A 5310 6546958 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 415 AND BS 430, RBL 65. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007050800096 20070508 00096 WP 2007 5 8 DHL2007806532 1 20070404 A 5730 DOUBLER DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 LT WING ACCESS DOOR NR 505F INTERNAL DOUBLER CRACKED 0.250" STA XRS 21.000 S-5 TO S-6 (MAJOR REPAIR). PERFORMED MAJOR R EPAIR IAW SRM 57-2-1 FIG 36. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW SRM 57-2-1 FIG. 36. PERFORM ED NDT INSPECTION IAW SRM 57-2-1 FIG 36 PG 133-134. NO CRACK OR CORROSION FOUND AFTER CUT OUT. ENCLOSED SMN FORM 242-4 . FABRICATED EXTERNAL REPAIR DOUBLER (AL7075T6 0.160") INTERNAL DOUBLER (AL7075T6 0.063") AND FILLER (AL2024T3 511 0.37 5") IAW SRM 57-2-1 FIG 36. APPLIED POLYURETHANE TOP YELLOW COATING TO FILLER IAW SRM 51-1-12 PG 7-12. CLEANED, TREATED AND PRIMED AREA AND INTERNAL/EXTERNAL REPAIR DOUBLER IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1- 2 L 7 4 4F RT 4A25 2007050800097 20070508 00097 WP 2007 5 8 DHL2007806591 1 20070420 A 5720 ANGLE DOUG DC8 DC873F 302199F WP TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 RT INBD FLAP LWR "T" ANGLE CRACKED 1 1/2" STA XW 91.000. REMOVED CRACKED "T" ANGLE IAW SRM 51-1-21. FABRICATED NEW "T' ANGLE (EXTRUSION S2701008) IAW SRM 57-7-1 PG 4. CLEANED, TREATED AND PRIMED AREA AND "T" ANGLE IAW SRM 51-1-8B. INSTA LLED "T" ANGLE IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007050800105 20070508 00105 WP 2007 5 8 DHL2007806557 1 20070412 A 5755 56551651 SKIN DOUG DC8 DC873F 302199F WP NR 1 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 NR 1 LT SPOILER PANEL LWR SKIN DELAMINATED. REMOVED AND REPLACED NR 1 LT SPOILER PANEL IAW MM 27-61-1 PG 201-206. REFE R TO NR 075764 FOR OPS CHECK. 2 L 7 4 4F RT 4A25 2007050800107 20070508 00107 WP 2007 5 8 DHL2007806514 1 20070405 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 320 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 FWD CARGO COMPT FITTING CRACKED 0.500", STA 320.000 L-26L TO L-27L. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050800182 20070508 00182 WP 2007 5 8 DHL2007806522 1 20070404 A 5740 FITTING DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 RT WING FWD FITTING CRACKED 1" STA XW 74.000 S-51, REF NR 3 MAIN TANK ACCESS DOOR NR 505F) MAJOR REPAIR. PERFORMED MAJO R REPAIR IAW SRM 57-1-0 PG 1. REMOVED DAMAGED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D. CLEANED AND APPLIED POLYURETH ANE YELLOW COATING IAW SRM 51-1-12 PG 7-12. INSTALLED NEW FITTING IAW SRM 51-1-23, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050800184 20070508 00184 WP 2007 5 8 DHL2007806523 1 20070402 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP BS 520-540 MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 806DH 89864 46002 REPAIR ON FWD UPPER JAMB CORNER OF "B" CARGO DOOR IS NOT IN ACCORDANCE WITH DWG SR08530019 (STA 520.000 - 540.000 L-25R TO L-27R) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW AD2005-18-07, S/B DC8 53-078, DOUGLAS DWG NR SR08530019, 5750776. R EMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001 . NO CRACK OR CORROSION FOUND. ENCLOSED SMN FORM 242-2. FABRICATED FILLER (AL7075T6 0.080") REPAIR DOUBLER (AL7075T6 0.090") AND REPAIR TRIPLER (AL7075T6 0.125") IAW DOUGLAS DWG #SR08530019. CLEANED, TREATED AND PRIMED AREA AND REPAIR P ARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW DOUGLAS DWG SR085 2 L 7 4 4F RT 4A25 2007050800186 20070508 00186 WP 2007 5 8 DHL2007806580 1 20070415 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 RT WING UPPER EXT SKIN CRACKED 0.250" STA XRS 74.000 S-11 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 10 SHEET 1, PG 59-60. CUT OUT DAMAGED SECTION AND FABRICATED DOUBLER (AL7075T6 0.125") AND FILLER PLUG (AL7075T6 0.280") I AW SRM 57-2-1 FIG 10 SHEET 1 PG 59-60. TAPERED REPAIR DOUBLER FROM 0.125" TO 0.080" IAW SRM 57-2-1 FIG 10 SHEET 1 PG 59 -60, SRM 51-10-0 FIG 1 SHEET 20. PERFORMED NDT INSPECTION AFTER CUT OUT. NO CRACK OR CORROSION FOUND. ENCLOSED SMN FO RM 242-2. APPLIED POLYURETHANE TOP YELLOW COATING TO FILLER PLUG IAW SRM 51-1-12. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER INNER FACE IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-11. INSTALLED REPAIR PARTS 2 L 7 4 4F RT 4A25 2007050800205 20070508 00205 NM 2007 5 8 DLM88070431 1 20070219 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 939DL 49812 FUSELAGE LOWER SKIN REPAIR AT STA 731 BETWEEN LONGERONS 30 AND 29R - SKIN CORRODED. REPAIRED PER DRAWING AMR0953584 R01 DATED 090209 AND ERA 459485-14. 2 L 7 2 4F RT A6WE 2007050800206 20070508 00206 NM 2007 5 8 DLM88070432 1 20070219 A 5310 DOOR FRAME DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 939DL 49812 CARGO DOOR JAMB REPAIR - PITTING CORROSION ON BOTTOM OF AFT CARGO COMP DOOR JAMB BETWEEN STA 1115 AND 1212. REPAIRED PR SRM 53-05D, FIG 63. 2 L 7 2 4F RT A6WE 2007050800207 20070508 00207 NM 2007 5 8 DLM88070433 1 20070219 A 5311 9912246115 FRAME DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 939DL 49812 FUSELAGE FRAME TEE REPLACEMENT - CORROSION ON FRAME STA 1380 LOWER SECTION BETWEEN LONGERONS 24L AND 24R. DAMAGED FRAME TEE SECTION REPLACED WITH NEW P/N 9912246-115. 2 L 7 2 4F RT A6WE 2007050800208 20070508 00208 NM 2007 5 8 DLM88070434 1 20070118 A 5310 DOOR FRAME DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 941DL 49814 SUPERFICIAL CORROSION O AFT PASS DOOR JAMB - CORROSION ON LOWER HORIZ SECTION OF AFT PAX DOOR JAMB FWD SURFACE NEAR STA 1338. CORROSION REMOVED, PERMANENT REPAIR INSTALLED PER SRM 53-05D FIG 34. 2 L 7 2 4F RT A6WE 2007050800209 20070508 00209 NM 2007 5 8 DLM88070435 1 20070118 A 5310 DOOR FRAME DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 941DL 49814 EXFOLIATION CORROSION ON DOOR JAMB AFT CARGO COMPARTMENT - LOWER SECTION. CORROSION REMOVED AND PERMANENT REPAIR INSTAL LED PER SRM 53-05D FIG 63. 2 L 7 2 4F RT A6WE 2007050800210 20070508 00210 NM 2007 5 8 DLM88070436 1 20070118 A 5330 5936434129 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 941DL 49814 FUSELAGE SKIN REPAIR AT STA 250, LONGERON 30 - DENT WITH CREASE. PERMANENT REPAIR INSTALLED PER AMX DRAWING AMR0953571 AND ERA 383116-14. 2 L 7 2 4F RT A6WE 2007050800211 20070508 00211 NM 2007 5 8 DLM88070437 1 20070118 A 5523 5910413 TAB DOUG MD88 MD88 3023688 NM ELEVATOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 941DL 49814 DELAMINATION ON LT HORIZ STAB ELEVATOR CONTROL TAB AT STA XET=80.750TO XET=66.625. PERMANENT REPAIR INSTALLED PER AMX REPAIR DRAWING AMR0955070 AND ERA 458461-14. 2 L 7 2 4F RT A6WE 2007050800215 20070508 00215 NM 2007 5 8 AMTA200700205 1 20070429 A 3030 0851FJ1 PROBE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE PITOT UNSERVICEABLE A AMTA K NONE J WARNING INDICATION IN INSP/MAINT 1 GL 11 514AT 27971 CAPT PITOT LIGHT REMAINED ILLUMINATED AFTER ENGINE START. REMOVED AND REPLACED CAPTAINS PITOT PROBE IAW MM 34-11-01. P ERFORMED ADJ AND TEST IAW 34-11-01. PERFORMED PITOT LEAK CHECK NO LEAKS NOTED. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007050800221 20070508 00221 WP 2007 5 8 DHL2007806601 1 20070417 A 5280 CHANNEL DOUG DC8 DC873F 302199F WP BS 980 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 RT MLG INBD DOOR FLANGE ZEE CHANNEL AFT PART WORN STA 980.000 RBL 45" (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FO RM 8110-3 DATED 04-09-07, ENGINEERING VARIATION AUTHORIZATION NR D85200005 REV IR DATED 03-27-07. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT SECTION IAW ASTAR DWG NR D85200005-001-D. FABRICATION REPAIR FILLER (AL7075T6 0.063") AND REPAIR DOUBLER (STEEL 301 1/2H 0.040") IAW ASTAR DWG NR D852-00005-001-D, DAC DWG NR 5616307. PERFORMED NDT INSP IAW DACO DPS 4.707-1. CLEANED, TREATED AND PRIMED AREA AND FILLER IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1 -11. INSTALLED REPAIR PARTS IAW ASTAR DWG NR D852-00005-001-D, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050800223 20070508 00223 NM 2007 5 8 DLM88070449 1 20070328 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE MISREPAIRED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 943DL 49816 FUSELAGE SKIN REPAIR AT STA 1322 BETWEEN LONGERONS 25R TO 26R - NONAPPROVED PERMANENT REPAIR. PERMANENT REPAIR PERFORME D IAW AM REPAIR DRAWING NR AMR0953591 REV01 AND ERA 460142-14. 2 L 7 2 4F RT A6WE 2007050800224 20070508 00224 NM 2007 5 8 DLM88070450 1 20070328 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 943DL 49816 FUSELAGE SKIN REPAIR AT STA 1437 BETWEEN LONGERONS 1L-4L - SKIN CRACKED. PERMANENT REPAIR INSTALLED IAW AM REPAIR DRAWI NG NR AMR0953592 R01 AND ERA 460141-14. 2 L 7 2 4F RT A6WE 2007050800225 20070508 00225 NM 2007 5 8 DLM88070451 1 20070329 A 5534 BUSHING DOUG MD88 MD88 3023688 NM VERTICAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 943DL 49816 CORROSION ON BUSHINGS OF VERTICAL STAB PIVOT POINT OUTBOARD AND INBOARD SIDE. NEW BUSHINGS FABRICATED AND INSTALLED PER SRM 55-02D PARA 24A (A), (B) AND (C). 2 L 7 2 4F RT A6WE 2007050800226 20070508 00226 NM 2007 5 8 DLM88070452 1 20070329 A 5312 SR0953000133 TEE FITTING DOUG MD88 MD88 3023688 NM FUSELAGE WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 943DL 49816 AFT PRESSURE BULKHEAD TEE LOWER PORTION REPAIR AT STA 1338, LONGERON 28L-28R - WEAR. A PORTION OF THE LOWER PART OF BUL KHEAD TEE WAS SECTIONED AND NEW SECTION INSTALLED PER EA 09-086680-12 REV E. 2 L 7 2 4F RT A6WE 2007050800227 20070508 00227 NM 2007 5 8 DLM88070453 1 20070328 A 5310 DOOR FRAME DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 943DL 49816 STRUCTURAL REPAIR AT THE FWD CARGO DOOR JAMB - EXFOLIATION CORROSION. CORROSION REMOVED, PERMANENT REPAIR INSTALLED PER SRM 53-05D, FIG 804D. 2 L 7 2 4F RT A6WE 2007050800228 20070508 00228 NM 2007 5 8 DLM88070454 1 20070328 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 943DL 49816 FUSELAGE SKIN REPAIR AT ST 1437 BETWEEN LONGERONS 3R-4R - SKIN CRACKED. PERMANENT REPAIR INSTALLED PER SRM 53-04D, FIG 27. 2 L 7 2 4F RT A6WE 2007050800229 20070508 00229 NM 2007 5 8 DLM88070455 1 20070329 A 5311 9912246115 FRAME DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 943DL 49816 CORROSION ON FRAME AT STA 1380 BETWEEN LONGERON 28R-28L. CORROSION REMOVED AND NEW FRAME INSTALLED PER SRM 51-10-23 AND 51-10-30. 2 L 7 2 4F RT A6WE 2007050800230 20070508 00230 NM 2007 5 8 DLM88070456 1 20070417 A 5330 5911401179 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 945DL 49818 REPAIR ON FUSELAGE SKIN BETWEEN STA 180-207 AND LONGERONS 19-22L - TEMPORARY REPAIR. TEMPORARY REPAIR REMOVED AND PERMA NENT REPAIR INSTALLED PER SRM 53-05D, FIG 57A. 2 L 7 2 4F RT A6WE 2007050800247 20070508 00247 NM 2007 5 8 DLM88070464 1 20070414 A 5330 59114073 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 945DL 49818 CRACK ON FUSELAGE SKIN AT THE STA 175 ON RT UPPER FWD CORNER. DAMAGE REMOVED AND PERMANENT REPAIR INSTALLED PER SRM 53- 05D, FIG 112, SH 3. 2 L 7 2 4F RT A6WE 2007050900003 20070509 00003 WP 2007 5 9 DHL2007806589 1 20070419 A 5340 37540252 FITTING DOUG DC8 DC873F 302199F WP BS 340 S26R CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 FOUND FWD CARGO COMPT FITTING 3" CRACK STA 340.000 L-26R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED A ND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE) REFER TO JC EC-00247-001 (W O 470) FOR FITTING FABRICATION. 2 L 7 4 4F RT 4A25 2007050900004 20070509 00004 WP 2007 5 9 DHL2007806553 1 20070410 A 5340 4758514501 FITTING DOUG DC8 DC873F 302199F WP BS 1140 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 AFT CARGO COMPT BILGE FITTING CRACKED STA 1140.000 L-33R TO L-32R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). REFER TO JC EC-0 0259-001 (WO 470) FOR FITTING FABRICATION. 2 L 7 4 4F RT 4A25 2007050900005 20070509 00005 WP 2007 5 9 DHL2007806556 1 20070409 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 879 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 LT MLG WW L-24 FRAME FITTING CORRODED STA 879.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 8 SHEET 1, 3, 6. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 FIG 1F SHEET 3. REMOVED CORRODED FRAME FITTING IAW SRM 51-1-20D. FABRICATED (4EA) SPLICES, (4EA) SHIMS BOTH FROM AL7075T7351, (1EA) DOUBLER FROM AL7075T 651 0.125") (2EA) SHIMS FROM AL7075T651 0.071" IAW SRM 53-2-0 FIG 8 SHEET 1, 3, 6. HEAT TREATED DOUBLER AND SHIM FROM A L7075T651 TO 7075T6 IAW SRM 51-1-1 PG 13, 17. CUT OUT NEW FRAME FITTING IAW SRM 53-2-0 FIG 8 SHEET 1. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 53-2-0 FIG 8 SHEET 1, 3, 6, SRM 51-1- 2 L 7 4 4F RT 4A25 2007050900007 20070509 00007 WP 2007 5 9 DHL2007806546 1 20070408 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 RT OTBD FLAP UPPER SKIN WORN STA XF 226.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-30-07, ASTAR DRAWING NR D857R1020 DATED 03-28-07. REMOVED EXISTING DAMAGED REPAIR SEGMENT AND INTERNAL SPLICE IAW SRM 51-1-21. FABRICATED NEW REPAIR PLATING SEGMENT 9AL2024T3 0.071") AND INTERNAL SPLICE (AL2024T3 0.080") IAW ASTAR DWG NR D857R10 20. CLEANED, TREATED AND PRIMED AREA AND INTERNAL SPLICE AND INNER FACE OF NEW REPAIR SEGMENT IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW SRM 51-1-21, SRM 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050900013 20070509 00013 WP 2007 5 9 DHL2007806506 1 20070329 A 5720 ANGLE DOUG DC8 DC873F 302199F WP BS 125-169 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 FOUND RT OUTBD FLAP T/E ANGLE CRACKED (STA XF 125.000 - 169.000). REMOVED CRACKED ANGLE IAW SRM 51-1-21. FABRICATED NE W ANGLE (AL2024 "0" 0.050") IAW SRM 57-7-1 FIG 3. PERFORMED HEAT TREATMENT FROM 2024 "0" TO 2024T4 IAW SRM 51-1-1 PG 1- 13-17. CLEANED, TREATED AND PRIMED AREA AND ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-21, SRM 51-1-21A. 2 L 7 4 4F RT 4A25 2007050900012 20070509 00012 NM 2007 5 9 EIA2007063 1 20070403 A 2120 UNKNOWN BOEING 747 747212B 1384886 NM COCKPIT ODOR A EIAA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NM 09 486EV 20888 STRONG ELECTRICAL SMELL NOTED ON SHORT FINAL NO SMOKE NOTED ALL CB CHECKED CLOSED ELECTRICAL SYSTEM VOLTS AND FREQ LOADS NORMAL. ALL SYSTEMS TROUBLESHOT NO DEFECTS NOTED NOW OR ON NEXT FLIGHT. 2 L 7 4 4F A20WE 2007050900014 20070509 00014 WP 2007 5 9 DHL2007806508 1 20070402 A 5730 5611014503 SKIN DOUG DC8 DC873F 302199F WP LT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 FOUND LT WING T/E LWR PANEL SKIN DELAMINATED (STA XF 219.000 - 339.000). REMOVED AND REPLACED LT WING T/E LWR PANEL (ST A XF 219.000 - 339.000) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050900015 20070509 00015 WP 2007 5 9 DHL2007806517 1 20070403 A 5755 56551652 SKIN DOUG DC8 DC873F 302199F WP NR 1 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 NR 1 RT SPOILER PANEL EXTERNAL SKIN DELAMINATED. REMOVED AND REPLACED NR 1 RT SPOILER PANEL IAW MM 27-61-1 PG 201-206. REFER TO NR 075764 FOR OPS CHECK. 2 L 7 4 4F RT 4A25 2007050900017 20070509 00017 WP 2007 5 9 DHL2007806567 1 20070409 A 5320 CUSP WEB DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT UPPER CUSP CORRODED (STA 35.000 - 60.000, L-21R) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW BOEING MSG N R 1-307875056-2 DATED 03-28-07. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED CUSP IAW SRM 53-1-0 PG 1, SRM 51-1-21. FABRICATED NEW CUSP: UPPER ANGLE (P/N 5615180-59) AND LWR ANGLE (P/N 5615180-61) BOTH FROM 2024"0" 0.063" IAW BOEING MESSAGE NR 1-307875056-2 DOUGLAS DWG NR 5615180, SRM 53-3-3 FIG 5. PERFORMED HEAT TREATMENT FROM 2024"0" TO 2024T4 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED AREA AND REPAI R PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW BOEING MESSAGE 2 L 7 4 4F RT 4A25 2007050900018 20070509 00018 WP 2007 5 9 DHL2007806603 1 20070405 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1680 DAMAGED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT FRAME HAS A MISDRILLED HOLE STA 1680.000 L-21L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 81 10-3 DATED 03-30-07. REPAIR ORDER NR 2-50561-801 DATED 03-29-07 (ED-4504). PERFORMED NDT INSPECTION IAW DC8 NDT SPM PA RT 06-10-01-001. NO CRACK OR CORROSION FOUND. ENCLOSED SMN FORM 242-2. PLUGGED MISDRILLED HOLE WITH RIVET (MS20470D) IAW SRM 53-2-0 FIG 1F, SHEET 2 SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007050900020 20070509 00020 WP 2007 5 9 DHL2007806513 1 20070402 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 1140-1160 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 AFT CARGO COMPT BILGE FITTING CRACKED (STA 1140.000 - 1160.000 L-35R). REMOVED AND REPLACED CRACKED FITTING AT AFT CARG O COMPT BILGE (STA 1140.000 - 1160.000 L-35R) IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050900023 20070509 00023 WP 2007 5 9 DHL2007806525 1 20070404 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 600 DAMAGED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT FLOORBEAM HAS A MISDRILLED HOLE, STA 600.000 RBL 38" (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 51 -2-1 FIG 1, TR NR 51-130 DATED 01-26-04. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION IAW SRM 51-2-1 FIG 1, TR NR 51-130 SHEET 7. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK OR CORROSION FOUND AFTER CUT OUT. FABRICATED REPAIR ANGLE (AL7075T6 511 0.125") AND FILLER (AL7075T6 0.125") IAW SRM 51-2-1 FIG 1 SHEET 7-9-12. CLEANED, TREATED AN D PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR P ARTS IAW SRM 51-2-1 FIG 1 SHEET 7-9-12, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050900024 20070509 00024 WP 2007 5 9 DHL2007806526 1 20070330 A 5730 56488941 PANEL DOUG DC8 DC873F 302199F WP LT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 LT WING T/E UPPER PANEL EXTERNAL SKIN DELAMINATED (STA XA 507.000 - 566.000). REMOVED DELAMINATED T/E UPPER PANEL (STA XA 507.000 - 566.000) IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW T/E PANEL IAW SR M 51-3-0, SRM 51-3-1 PG 2A. 2 L 7 4 4F RT 4A25 2007050900026 20070509 00026 WP 2007 5 9 DHL2007806529 1 20070403 A 5711 FRAME DOUG DC8 DC873F 302199F WP RT WING BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 FOUND RT WING CTR L/E INTERIOR FORMER BROKEN STA XFS 510.222. REMOVED FASTENERS IAW SRM 51-1-20D. FABRICATED ANGLE DOU BLER (AL7075-0 0.063") IAW SRM 57-2-0 PG 9-10, SRM 57-3-3 FIG 4. HEAT TREATED ANGLE DOUBLER FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED ANGLE DOUBLER AND AREA IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050900030 20070509 00030 NM 2007 5 9 EIA2007065 1 20070401 A 5711 SPAR BOEING 747 747132 1384882 NM RT WING CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 RT WING FORWARD SPAR I/B LOWER CHORD CRACKED AT FSSO 1446 ON VERTICAL AND HORIZONTAL FLANGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 479-57-218-2 REV A. 2 L 7 4 4F A20WE 2007050900032 20070509 00032 WP 2007 5 9 DHL2007806539 1 20070408 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1580 DEFORMED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT FRAME DEFORMED STA 1580.000 L-21L. PERFORMED MAJOR REPAIR IAW SRM 53-4-1 FIG 51. REMOVED DAMAGED FRAM E SEGMENT IAW SRM 53-1-0 PG 1, SRM 51-1-20D. FABRICATED NEW FRAME SEGMENT P/N 2645791 (7075"0" 0.071") IAW SRM 53-4-1 F IG 51 SHEET 21 ITEM "A", SRM 51-2-0 FIG 52, SRM 53-2-0 FIG 2 SHEET 1, SRM 53-2-0 FIG 2 SHEET 8, TR NR 53-110 DATED 11-10 -00. FABRICATED (2EA) SPLICE ANGLES (7075"0" 0.071") IAW SRM 53-2-0 FIG 2 SHEET 5, TR NR 53-125 DATED 08-31-01, SRM 53-2 -0 FIG 2 SHEET 7, TR NR 53-110 DATED 11-10-00. HEAT TREATED FRAME SEGMENT AND (2EA) SPLICE ANGLES FROM 7075"0" TO 7075T 6 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAY 2 L 7 4 4F RT 4A25 2007050900034 20070509 00034 WP 2007 5 9 DHL2007806587 1 20070416 A 7160 NOSE COWL DOUG DC8 DC873F 302199F WP NR 2 ENGINE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 NR 2 ENG RT NOSE COWL UPPER PORTION WORN (STA YN 147.534 - 163.000, AT 12 O'CLOCK POS) MAJOR REPAIR. PERFORMED MAJOR RE PAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2, 3. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED SK IN (AL2024T3 0.080") AND SPLICE (STEEL 17-7PH 0.050") IAW DC8 70 SRM 71-5-2 FIG 2 SHEET 1 ,2 3. HEAT TREATED SPLICE FRO M 17-7PH CRES TO 17-7PH CRES (H1050) IAW SRM 51-1-6. CLEANED, TREATED AND PRIMED AREA AND SKIN IAW SRM 51-1-8B. APPLIE D SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW SRM 71-5-2 FIG 2 SHEET 1, 2, 3, SRM 51-1-21A. 2 L 7 4 4F RT 4A25 2007050900035 20070509 00035 WP 2007 5 9 DHL2007806547 1 20070410 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT FITTING CORRODED STA 100.000 L-21R. REMOVED CORROSION FROM FITTING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INS TALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-0 (TORQUE). 2 L 7 4 4F RT 4A25 2007050900037 20070509 00037 WP 2007 5 9 DHL2007806549 1 20070409 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 1220 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 "C" CARGO DOOR JAMB FITTING 0.500" CRACK STA 1220.000 L-34R - L-35R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CUT OUT NEW FITTING AND FABRICATED REPAIR ANGLE (AL7075T6 511 0.125") IAW SRM 53-2-0 FIG 2D. CLEANED, TREATED AND PRIMED AREA AND REPAIR ANGLE IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR ANGLE AND FITTI NG IAW SRM 53-2-0 FIG 2D, SRM 51-1-120D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050900041 20070509 00041 WP 2007 5 9 DHL2007806505 1 20070405 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 1180 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 STRUCTURE UNDER NR 3 CROSS SLIDE CARGO DOOR HAS A CRACKED FITTING STA 1180.000 L-28L. REMOVED AND REPLACED CRACKED FITT ING AT STA 1180.000 L-28L, STRUCTURE UNDER NR 3 CROSS SLIDE CARGO DOOR IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050900044 20070509 00044 WP 2007 5 9 DHL2007806584 1 20070416 A 5410 DOOR DOUG DC8 DC873F 302199F WP NR 4 NACELLE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 NR 4 ENG LT/RT NACELLE INLET COWL WORN, STA YN 157.000 AT 12 O'CLOCK POS (EXTERIOR) MAJOR REPAIR. PERFORMED MAJOR REPAI R IAW SRM 71-5-2 FIG 2 SHEET 1, 2, 3. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW S KIN (AL2024T3 0.080") AND SPLICE (STEEL 17-7 PH 0.050") IAW DC8 70 SRM 71-5-2 FIG 2 SHEET 1, 2, 3. HEAT TREATED SPLICE FROM 17.7PH CRES TO 17.7PH CRES (H1050) IAW SRM 51-1-16. CLEANED, TREATED AND PRIMED AREA AND SKIN IAW SRM 51-1-8B. AP PLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW SRM 71-5-2 FIG 2 SHEET 1, 2, 3, SRM 51-1-2 1. 2 L 7 4 4F RT 4A25 2007050900047 20070509 00047 WP 2007 5 9 DHL2007806573 1 20070416 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 LT WING CTR L/E LWR SKIN HAS ELONGATED HOLES STA XFS 526.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-05-07, ENGINEERING VARIATION AUTHORIZATION NR D857-00004 DATED 03-27-07 REV IR. FABRICATED REPAIR DOUBLER (AL 7075T6 0.071") IAW ASTAR DWG NR ES D85700004-001-D. PERFORMED NDT INSPECTION IAW DACO DPS 4.707-1. NO CRACK OR CORROSI ON FOUND. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR DOUBLER IAW ASTAR DWG NR ES-D8570004-001-D, SRM 51-1-21, SRM 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050900048 20070509 00048 WP 2007 5 9 DHL2007806592 1 20070419 A 5340 47794962 FITTING DOUG DC8 DC873F 302199F WP BS 902 L18R CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT FITTING 1" CRACK STA 902.125 L-18R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PR IMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE) REFER TO JC EC-00276-001 (WO 470 ) FOR FITTING FABRICATION. 2 L 7 4 4F RT 4A25 2007050900049 20070509 00049 WP 2007 5 9 DHL2007806545 1 20070405 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 960 L20-21L DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT FRAME HAS A MISDRILLED HOLE STA 960.000 L-20L TO L-21L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-30-07, REPAIR ORDER NR 2-50561-801 DATED 03-29-07 (ED-4500). PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK OR CORROSION FOUND. ENCLOSED SMN FORM 242-2. PLUGGED MISDRILLED HOLE WITH RIVET (MS20 470D) IAW SRM 53-2-0 FIG 1F SHEET 2, SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. REFER TO JC EC-002 67-001 FOR REPAIR. 2 L 7 4 4F RT 4A25 2007050900052 20070509 00052 NM 2007 5 9 F3LA200700110 1 20070423 A 5730 SKIN AIRBUS A319 A319111 3930336 NM WING GOUGED A F3LA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 NM 03 904FR 1579 DURING TAKEOFF, NR 2 ENGINE FAN COWL DEPARTED AIRCRAFT HITTING INBD UNDER WING AREA. SEVERAL GOUGES AND SCRATCHES WERE FOUND BETWEEN RIBS 4 AND 6 AND STRINGERS 2 THRU 7. 2 L 7 2 4F RT A28NM 2007050900053 20070509 00053 NM 2007 5 9 F3LA200700105 1 20070423 A 5522 SKIN AIRBUS A319 A319111 3930336 NM ELEVATOR DELAMINATED A F3LA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 NM 03 904FR CG5172 1579 DURING TAKEOFF, NR 2 ENGINE FAN COWL DEPARTED AIRCRAFT HITTING ELEVATOR ABOUT MID-SPAN. OUTER SKIN WAS DELAMINATED AND SHOWED LOSS OF INNER CORE MATERIAL. ALSO, THE END OF A COWL HOLD OPEN ROD WAS IMBEDDED IN THE ELEVATOR. [SUP 05-10-07] REPLACED RT ELEVATOR IAW AMM 27-34-41-000-001. 2 L 7 2 4F RT A28NM 2007050900055 20070509 00055 NM 2007 5 9 MZZA0700007 1 20070417 A 5542 SKIN BOEING 737 737824 13844BZ NM RUDDER CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 35236 28801 INSPECTION FOUND UPPER RUDDER T/E CORRODED AT LOWER STATIC WICK ALONG BASE PLATE LOWER FORWARD EDGE, RUD STA 278-283. TH E RUDDER WAS REPAIRED IAW ECRA 5540-01234 AND ECRA 5540-01232. A RUDDER BALANCE PROCEDURE WAS PERFORMED IAW SRM 51-60-0 7. 2 L 7 2 4F RT A16WE 2007050900058 20070509 00058 EU 2007 5 9 F3LA200700108 1 20070504 A 3520 OXYGEN MASK AIRBUS A318 A318111 3940019 EU CABIN NO TEST A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 801FR 1939 WHILE PERFORMING MASK DROP TEST, ROWS 15 AND AFT ON BOTH SIDES, 7, 8, AND 9 RT SIDE, R2 DOOR AND C LAV DID NOT DROP COMP LETELY. RESET MASKS AND PERFORMED TEST AGAIN IAW AMM 35-23-00-710-001. OPS CHECKED GOOD. 2 L 7 2 4F RT 2007050900071 20070509 00071 NM 2007 5 9 EIA2007087 1 20070401 A 5314 KEELBEAM BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 WEB CRACKED NEAR RIVET HOLE AT STA 1002 KEEL BEAM LT SIDE SECOND ROW OF RIVETS. KEEL BEAM WEB REPAIRED PER SRM 53-10-09 FIG 4. 2 L 7 4 4F A20WE 2007050900072 20070509 00072 NM 2007 5 9 EIA2007074 1 20070413 A 2697 2156646 CONNECTOR BOEING 747 747273C 1384896 NM SMOKE DETECTOR DIRTY A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 471EV 20651 MAIN DECK SMOKE DETECTOR 2B WILL NOT TEST, ITEM DEFERRED PER MEL 26-11. CLEAN AND RESET CANNON PLUG. OPS CHECK NORMAL PER MM 26-14-00, DEFERRAL CLEARED. 2 L 7 4 4F A20WE 2007050900079 20070509 00079 NM 2007 5 9 EIA2007084 1 20070407 A 5313 STRINGER BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 FOUND STRINGER CORRODED AT CENTER ELECTRONIC COMPARTMENT CUTOUT AREA BS760-780 STRINGER 47L. DAMAGED SECTION OF STRINGE R CUT AND REMOVED. REPAIR SPLICE SECTION FABRICATED PER SRM 53-10-03 FIG 1. REPAIR PARTS INSTALLED PER SRM 51-30-02 & 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007050900080 20070509 00080 NM 2007 5 9 EIA2007085 1 20070331 A 5322 SHEAR TIE BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 FOUND FRAME SHEAR TIE AT BS 180 BETWEEN STRINGER 34L AND 35L CRACKED. SHEAR TIE REMOVED AND FABRICATED PER SRM 53-10-04 AND INSTALLED PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007050900082 20070509 00082 NM 2007 5 9 EIA2007090 1 20070331 A 5322 SHEAR TIE BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 FOUND FRAME SHEAR TIE AT BODY STATION 220 BETWEEN STRINGER 30L AND 29L CRACKED. SHEAR TIE REMOVED AND FABRICATED PER SR M 53-10-04 INSTALLED PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007050900083 20070509 00083 NM 2007 5 9 EIA2007092 1 20070407 A 5313 STRINGER BOEING 747 747212B 1384886 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 FOUND STRINGER 24A BODY STATION 140-190 WITH OVERSIZE HOLES. REMOVED STRINGER AND FABRICATED AND INSTALLED PER B747 SRM 53-10-03. 2 L 7 4 4F A20WE 2007050900088 20070509 00088 NM 2007 5 9 EIA2007070 1 20070407 A 3350 900835A BATTERY PACK BOEING 747 747121 1384871 NM CABIN DISCHARGED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480EV 6587 20348 UPPER DECK EMERGENCY EXIT SIGN LIGHT AT CREW DOOR INOP. REQUIRES CHARGER AND BATTERY. REPLACED BATTERY CHARGER AND BAT TERY PACK IN UPPER DECK EMERGENCY EXIT SIGN IAW 33-51-07 OPS CKD OL PER 33-51-07. 2 L 7 4 4F A20WE 2007050900090 20070509 00090 NM 2007 5 9 EIA2007075 1 20070317 A 5744 65B1047213 ATTACH FITTING BOEING 747 747212B 1384886 NM WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 NUMBER 4 FLAP TRACK FWD FITTING MATING SURFACE OF BEARING FOUND WITH PITTING CORROSION. BEARING REMOVED AS PER SB 747-5 7-2325 FIG 30. FITTING HOLE FOUND PITTED AND BORING ACCOMPLISHED PER SB 747-57-2325 STEP 7. CARRIED OUT FPI NIL CRACKS FOUND. CHAMFER CARRIED OUT PER SB 747-57-2325 STEP 15 & 16. FOUND SATISFACTORY. FABRICATED BUSHING PER SB 747-57-226 2 FIG 13 CADMIUM PLATED BUSHING AND INSTALLED. 2 L 7 4 4F A20WE 2007050900091 20070509 00091 NM 2007 5 9 EIA2007062 1 20070401 A 2612 FIRE LOOP BOEING 747 747200 1384847 NM FIRE DETECTION MALFUNCTIONED A EIAA K NONE N FALSE WARNING CL CLIMB 1 NM 09 471EV 20651 AFTER TO FROM CYQX DURING CLIMB OUT APU FIRE DETECTION SYSTEM INDICATED A FALSE FIRE WARNING FOR 1 SECOND FOLLOWED BY "B " LOOP REMAINING ILLUMINATED. AFTER APPROX 1 HR "B" LOOP EXTINGUISHED. BOTH LOOPS TESTED NORMAL AFTER FALSE FIRE WARNI NG. 2 L 7 4 4F RT A20WE 2007050900092 20070509 00092 NM 2007 5 9 EIA2007079 1 20070405 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482EV 20713 FOUND DOOR 5R CEILING EMERGENCY LIGHT INOPERATIVE. DOOR 5R CEILING EMERGENCY ASSY AND BATTERY ASSY REPLACED AND CHECKED SATISFACTORY PER B747 MM 33-51-00. 2 L 7 4 4F A20WE 2007050900093 20070509 00093 NM 2007 5 9 EIA2007076 1 20070322 A 5347 65B112421 SEAT TRACK BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 SEAT TRACK FOUND CORRODED AT LBL11 STA 470. SEAT TRACK REMOVED AS PER B747 SRM 51-30-02. SEAT TRACK TRIMMED AND PRIMER APPLIED AS PER B747 SOPM 20-41-02. SEAT TRACK INSTALLED PER B747 SRM 53-10-05 FIG 4. 2 L 7 4 4F A20WE 2007050900096 20070509 00096 SO 2007 5 9 SIMA200712704 1 20070505 A 2510 12315660401 HOLDER EMB 135 EMB135KL 3260302 SO FLIGHT DECK BURNED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 815AE 12775 145545 CAPTAIN CHART HOLDER SMOKING ON POWER UP, SMOKE STOPPED AFTER HOLDER LIGHTS TURNED OFF. REMOVED AND REPLACED CHART HOLD ER IAW EMB AMM 25-12-11. FUNCTIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050700179 20070507 00179 NM 2007 5 7 USAA070341 1 20070501 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 STA 500C BETWEEN STR 8 & 9, RT AT ATTACH BRACKET AT INBD RIVET HOLE. INSTALLED REPAIR ANGLES PER TR 53-10-20E. DEFECT SIZE: 1/4" 2 L 7 2 4F RT A16WE 2007050700204 20070507 00204 SO 2007 5 7 C2XA07IA097 1 20070426 A 3350 74441 LIGHT EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16147 145749 IAH - FLIGHT 2071, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THE EMERGENCY EXIT LIGHT ABOVE THE F/A HEADREST TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSY, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AI RCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007050700209 20070507 00209 SO 2007 5 7 C2XA07IA096 1 20070424 A 4920 M4504113A APU EMB 145 EMB145LR 3260212 SO APU BAY LEAKING A C2XA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16999 8277 8277 145307 JAN - FLIGHT 2395, THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN WITH THE APU RUNNING. CONTRACT MAINTENANCE INSPECTE D THE AIRCRAFT, AND PLACED THE APU ON MEL 49-00-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT R ETURNED TO IAH ON 04/27/07 WHERE MAINTENANCE REMOVED AND REPLACED THE APU, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVE D THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050700217 20070507 00217 SO 2007 5 7 C2XA07SH023 1 20070429 A 5310 14525480003 BEAM EMB 145 EMB145LR 3260212 SO CARGO BAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14902 145496 SHV DURING C-CHECK CARGO DOOR CUTOUT LOWER BEAM AT FR 65-68 HAS CORROSION. MX REMOVED AND REPLACED CARGO DOOR CUT OUT L OWER BEAM AT FR 65-68 IAW 145 SRM 51-40-02 AND CPM 51-21-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050700220 20070507 00220 SO 2007 5 7 C2XA07TY024 1 20070507 A 3397 M3902931229 CONNECTOR EMB 145 EMB145XR 3260214 SO CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11109 145657 TYS DURING A 3A SERVICE/ROUTINE CHECK, THE RIGHT FWD CABIN BULKHEAD EXIT SIGN WAS FOUND INOP. MAINTENANCE FOUND A BAD C ONNECTOR. MAINTENANCE REPLACED THE CONNECTOR AND OPS CHECK WERE GOOD IAW EMB 145 SPWM. AIRCRAFT RELEASED BACK TO SERVI CE. 2 L 7 2 4F RT 2007050700226 20070507 00226 CE 2007 5 7 DA62007F00000 1 20070321 A 5220 60430053601 ESCAPE HATCH BEECH 60 B60 1153605 CE LYC O540 TIO540* 41532 EA CHAFED E DA6A K NONE O OTHER IN INSP/MAINT 1 SW 09 171EC P288 DURING ANNUAL INSPECTION FOUND HINGED COVER FOR EMERGENCY EXIT RELEASE HANDLE WAS SAFETIED CLOSED WITH .020 INCH STAINLE SS STEEL WIRE NOT COOPER BREAKAWAY WIRE OF (.040 INCH - .012 INCH). HAD TO CUT WIRE WITH WIRE CUTTING PLIERS IN ORDER T O BE ALLOWED ACCESS TO THE RELEASE HANDLE TO ACTUATE IT IN ORDER TO REMOVE THE ESCAPE HATCH. ESCAPE HATCH WOULD NOT MOV E FREELY IN AND OUT OF THE ESCAPE HATCH HOLE. THE FIRST ITEM NOTED FOR THIS WAS THE WELD BEAD ON SUPPORT STRIKER AT FWD LWR CORNER AND AN EXCESSIVE AMOUNT OF MATERIAL FROM THE WELD BEAD CAUSING IT TO BIND BETWEEN THE HATCH AND AIRFRAME. T HE EXCESS MATERIAL WILL BE BLENDED AND ABRASIONS DRESSED. THE NEXT ITEM FOUND WAS THE WIRING TO THE PAX COMM. CONTROL 1 L 7 2 3O 3 O A12CE E14EA 2007050700257 20070507 00257 NM 2007 5 7 PIDA07031 1 20070430 A 5313 STRINGER BOEING 737 7372K5 138448X NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 DURING MAINTENANCE, NOTED CRACK AT THE END OF STR 16RT AT BS 500B+2. REPAIRED PER SB 737-53-1145. 2 L 7 2 4F RT A16WE 2007050700277 20070507 00277 NM 2007 5 7 NOCA09107 1 20070430 A 5312 BULKHEAD BOEING 757 75728A 1384976 NM FUSELAGE CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 750NA 26277 LEVEL 1 CORROSION CENTER WEB STA 1102 HYD BULKHEAD FITTING RIGHT MLG WHEEL WELL. REMOVED AND BLENDED AREA AS PER ESO 90 309. 2 L 7 2 4F RT A2NM 2007050700279 20070507 00279 NM 2007 5 7 NOCA09307 1 20070430 A 5320 TRANS PANEL BOEING 757 75728A 1384976 NM FUSELAGE CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 750NA 26277 LIGHT SCATTERED CORROSION TRANSITION PANEL STA 1440-1530 RIGHT SIDE. REMOVED CORROSION, TREATED, PRIMED AND PAINTED AS PER SRM 51-10-10 AND 52-20-01. 2 L 7 2 4F RT A2NM 2007050700280 20070507 00280 NM 2007 5 7 NOCA09407 1 20070430 A 5320 TRANS PANEL BOEING 757 75728A 1384976 NM FUSELAGE CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 750NA 26277 LIGHT SCATTERED CORROSION TRANSITION PANEL STA 1530 1640 RIGHT SIDE. REMOVED CORROSION, TREATED, PRIMED AND PAINTED AS PER SRM 51-10-01 AND 51-20-01. 2 L 7 2 4F RT A2NM 2007050800007 20070508 00007 NM 2007 5 8 USAA070348 1 20070501 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 STA 967 RBL 17 HAS CORROSION. FAB'D BEAM CAP & SUPPORT ANGLES, STRAPS PER SRM 53-00-51 FIG 201; CORR TASK C53-107-01; L EVEL 2, DEFECT SIZE: 42.5 INCHES. 2 L 7 2 4F RT A16WE 2007050800036 20070508 00036 NM 2007 5 8 USAA070295 1 20070418 A 5514 6548240512 TIE BOEING 737 737401 1384701 NM HORIZ STAB WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 RIGHT HORIZONTAL STA 0 AT REAR SPAR HAS WEAR. REMOVED AND REPLACED BOW TIE PER SRM 51-01-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007050800039 20070508 00039 WP 2007 5 8 DHL2007806538 1 20070408 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1580 DEFORMED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT FRAME DEFORMED STA 1580.000 L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-4-1 FIG 51. REMOV ED DAMAGED FRAME SEGMENT IAW SRM 53-1-0 PG 1, SRM 51-1-20D. FABRICATED NEW FRAME SEGMENT P/N 2645791 (7075"0" 0.071") I AW SRM 53-4-1 FIG 51 SHEET 21 ITEM "A", SRM 51-2-0 FIG 52, SRM 53-2-0 FIG 2 SHEET 1, SHEET 8, TR NR 53-110 DATED 11-10-0 0. FABRICATED (2EA) SPLICE ANGLES (7075"0" 0.071") IAW SRM 53-2-0 FIG 2 SHEET 5, TR NR 53-125 DATED 08-31-01 FIG 2 SHEE T 7, TR NR 53-110 DATED 11-10-00. HEAT TREATED FRAME SEGMENT AND (2EA) SPLICE ANGLES FROM 7075"0" TO 7075T6 IAW SRM 51- 1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES 2 L 7 4 4F RT 4A25 2007050800040 20070508 00040 WP 2007 5 8 DHL2007806599 1 20070420 A 5280 CHANNEL DOUG DC8 DC873F 302199F WP BS 865 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 LT MLG LT DOOR ZEE CHANNEL EDGE WORN (MAJOR REPAIR) STA 865.000 RBL 45. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE D 03-30-07, ENGINEERING VARIATION AUTHORIZATION NR D852-00002 DATED 03-17-07 REV IR. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED NEW "Z" ANGLE (AL7075"0" 0.063") (2EA) SPLICES (AL7075"0" 0.071") AND STRAP (30 1 1/2H 0.040") IAW ASTAR DWG NR D85200002-001-D, DOUGLAS DWG 5616307. HEAT TREATED "Z" ANGLE AND SPLICE FROM 7175"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-17. PERFORMED NDT INSPECTION IAW DPS 4.707-1. CLEANED, TREATED AND PRIMED AREA AND REPA IR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW ASTAR DWG NR D85200002-001-D, SRM 51-1-21. FOR OPS CHECK REFER TO 2 L 7 4 4F RT 4A25 2007050800057 20070508 00057 EU 2007 5 8 2007UALA01389 1 20070502 A 2121 BEARING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FAN FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 442UA 780 BLOWER FAN INOPERATIVE. UPON ARRIVAL TO AIRCRAFT FOUND C/B`S AD10 AND AE02 OPEN AND ELECTRICAL ODOR ON FLIGHT DECK. [0 6-26-07] REPLACED BLOWER FAN. SUSPECT FAILED BEARINGS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007050800061 20070508 00061 NM 2007 5 8 2007UALA01343 1 20070428 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 DOOR 2L HAS HALF INCH CRACK AT UPPER HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA. INSTALLED CRES DO UBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050800090 20070508 00090 WP 2007 5 8 DHL2007806519 1 20070402 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP BS 1160-1180 MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 806DH 89284 46002 REPAIR ON FWD UPPER JAMB CORNER OF "C" CARGO DOOR (STA 1160.000 - 1180.000, L-21R TO L-23R) IS NOT IN ACCORDANCE WITH DW G NR SR08530019 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD2005-18-07, S/B DC8 53-078, DOUGLAS DWG NR SR08530019, 575 0776. REMOVED NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-0 1-001. NO CRACK OR CORROSION FOUND. ENCLOSED SMN FORM 242-2. FABRICATED REPAIR DOUBLER (AL7075T6 0.090") AND REPAIR T RIPLER (AL7075T6 0.125") IAW DOUGLAS DWG NR SR08530019. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1- 8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW DOUGLAS DWG NR SR08530019, SRM 51-1 2 L 7 4 4F RT 4A25 2007050800108 20070508 00108 NM 2007 5 8 SWAA072269 1 20070505 A 5310 6546958 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 390, RBL 65. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007050800109 20070508 00109 NM 2007 5 8 SWAA072272 1 20070505 A 5311 65C22908 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050800111 20070508 00111 NM 2007 5 8 SWAA072265 1 20070505 A 5311 65C22910 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 14R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050800112 20070508 00112 WP 2007 5 8 DHL2007806597 1 20070408 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT WING TE FLAP WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 RT OTBD FLAP UPPER SKIN WORN STA XF 226.000 (MAJOR REPAIR.). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-30-07, ASTAR DWG NR D857R1020 DATED 03-28-07. REMOVED EXISTING DAMAGED REPAIR SEGMENT AND INTERNAL SPLICE IAW SRM 51-1-21. F ABRICATED NEW REPAIR PLATING SEGMENT (AL2024T3 0.071") AND INTERNAL SPLICE (AL2024T3 0.080") IAW ASTAR DWG NR D857R1020. CLEANED, TREATED AND PRIMED AREA, INTERNAL SPLICE AND INNER FACE OF NEW REPAIR SEGMENT IAW SRM 51-1-8B. APPLIED SEALA NT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW SRM 51-1-21, SRM 51-3-0, SRM 51-3-1 (TORQUE) AND JC E C-00265-001. 2 L 7 4 4F RT 4A25 2007050800113 20070508 00113 NM 2007 5 8 SWAA072253 1 20070504 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050800114 20070508 00114 NM 2007 5 8 SWAA072280 1 20070505 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050800116 20070508 00116 NM 2007 5 8 SWAA072279 1 20070505 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050800117 20070508 00117 NM 2007 5 8 SWAA072278 1 20070505 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050800119 20070508 00119 NM 2007 5 8 SWAA072277 1 20070505 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050800120 20070508 00120 NM 2007 5 8 SWAA072276 1 20070505 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007050800121 20070508 00121 NM 2007 5 8 SWAA072258 1 20070505 A 3350 10107451 SIGN BOEING 737 7373K2 13844BA NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007050800122 20070508 00122 NM 2007 5 8 SWAA072256 1 20070504 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 728SW 27860 DURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 120. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007050800123 20070508 00123 NM 2007 5 8 SWAA072252 1 20070504 A 5610 58935577 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED A1 CHECK, FOUND FLIGHT DECK L2 WINDOW ARCHING AND CRACKED. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2007050800125 20070508 00125 2007 5 8 SWAA072247 4 20070504 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 209WN 32484 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007050800126 20070508 00126 2007 5 8 SWAA072260 4 20070505 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 242WN 32505 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007050800127 20070508 00127 NM 2007 5 8 SWAA072245 1 20070504 A 2782 654485113 ACTUATOR BOEING 737 7373T0 1384582 NM NR 4 SPOILER DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 LEFT WING NR 4 SPOILER OUTBOARD ACTUATOR MOUNT LOBE SHEARED. REMOVED AND REPLACED SPOILER ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2007050800128 20070508 00128 NM 2007 5 8 SWAA072248 1 20070504 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 507, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007050800129 20070508 00129 NM 2007 5 8 SWAA072281 1 20070505 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 783, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007050800130 20070508 00130 NM 2007 5 8 SWAA072246 1 20070504 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 FUSELAGE SKIN CRACKED AT BS 787, STR 19R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007050800131 20070508 00131 NM 2007 5 8 SWAA072255 1 20070504 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007050800132 20070508 00132 NM 2007 5 8 SWAA072250 1 20070504 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 923, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007050800133 20070508 00133 NM 2007 5 8 SWAA072249 1 20070504 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007050800134 20070508 00134 NM 2007 5 8 SWAA072251 1 20070504 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007050800135 20070508 00135 NM 2007 5 8 SWAA072266 1 20070505 A 5311 6546549 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 14R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007050800136 20070508 00136 CE 2007 5 8 BSAASDR0708 1 20070424 A 2197 P563 PIN BEECH 1900 1900D 1154162 CE ENVIRON SYS NOT SEATED A BSAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 05 3199Q UE213 CREW REPORTED THE LEFT ENVIRO FAIL CAME ON AT 1000 FT AGL, SYSTEM WAS RECYCLED PER THE CHECKLIST, AND CAME ON AGAIN AT 5 000 FT AGL. CREW RETURNED TO STATION. THE RIGHT ENVIRONMENTAL SYSTEM WAS PREVIOUSLY DEFERRED. LEFT SIDE OF OVERPRESSU RE SWITCH CONNECTOR HAD A PIN IN THE CONNECTOR THAT WAS FOUND UNSEATED. RESEATED PIN. RIGHT SIDE DEFERRAL WAS CLEARED BY CLEANING & RESEATING CONNECTOR P563 TO THE OVERPRESSURE SWITCH. GROUND RUN OPERATIONAL & FUNCTION CHECK WERE GOOD. AN OPERATIONAL CHECK FLIGHT WAS COMPLETED, BOTH SYSTEMS OPS CHECK NORMALLY. 2 L 7 2 4T RT A24CE 2007050800137 20070508 00137 CE 2007 5 8 BSAASDR0709 1 20070427 A 2134 1143840391 PRESSURE SWITCH BEECH 1900 1900D 1154162 CE A/C SYSTEM SHORTED A BSAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 05 3199Q UE213 DURING CLIMB, BOTH ENVIR FAIL LIGHTS CAME ON, CREW RETURNED TO STATION WITH NO FURTHER INCIDENT. LEFT SYSTEM WAS INITIA LLY REPAIRED BY REPLACING PRECOOLER THRU VALVE & BYPASS VALVE. AFTER EXTENSIVE TROUBLESHOOTING, THE RIGHT SYSTEM WAS RE PAIRED BY REPLACING SHORTED PRESSURE SWITCH. THIS SWITCH WAS INTERMITTENTLY & PARTIALLY INTERNALLY SHORTED BETWEEN 4 OF THE PINS TO EACH OTHER AND TO THE CASE. THIS INTERMITTENT FAULT IS SUSPECTED TO BE ROOT CAUSE OF THIS INCIDENT. 2 L 7 2 4T RT A24CE 2007050800138 20070508 00138 EU 2007 5 8 CPCP20070001 1 20070321 A 5320 STIFFENER AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 420AT 420 CORROSSION FOUND ON FR 1 STIFFENER. 2 H 7 2 4T RT A53EU 2007050800162 20070508 00162 NM 2007 5 8 2007UALA01323 1 20070427 A 5330 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 838UA 1477 RIGHT FUSELAGE SKIN IS GOUGED AT FRAME 64 BETWEEN STR 23R & 24R, REPAIR WILL BE IN CRITICAL SKIN AREA AT BUTT SPLICE. M AJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007050800163 20070508 00163 NM 2007 5 8 2007UALA01324 1 20070427 A 3350 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 846UA 1600 CIDS TEST FAILS EPSU BATTERY AFT L. RESET 13WL, TEST PASSED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007050800164 20070508 00164 NM 2007 5 8 2007UALA01326 1 20070429 A 2497 CONNECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 1 PYLON ARCED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 848UA 1647 NR 1 ENG PYLON, GENERATOR FEEDER CABLE, J-SIDE AT FIREWALL DISCONNECT HAS ONE PIN DAMAGED DUE TO ARCING. [06-26-07] RE PLACED CABLE CONNECTOR ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007050800195 20070508 00195 NM 2007 5 8 DLM88070425 1 20070204 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 938DL 49811 FUSELAGE SKIN REPAIR AT STA 222 BETWEEN LONGERONS 15L AND 17L - SKIN DENTED. INSTALLED PERMANENT REPAIR PER SRM 53-04D, FIG 12B. 2 L 7 2 4F RT A6WE 2007050800196 20070508 00196 NM 2007 5 8 DLM88070426 1 20070402 A 5330 FASTENER DOUG MD88 MD88 3023688 NM FUSELAGE LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 938DL 49811 FUSELAGE SKIN REPAIR BETWEEN STA 560-588 AND LONGERONS 22-26R - LOOSE FASTENERS ON PREVIOUS REPAIRS. SKIN REPAIRED PER DRAWING AMR0953589 AND APPROVED BY ERA 460134-14. 2 L 7 2 4F RT A6WE 2007050800198 20070508 00198 NM 2007 5 8 DLM88070427 1 20070205 A 5753 SKIN DOUG MD88 MD88 3023688 NM T/E FLAP VANE DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 938DL 49811 OUTBOARD FLAP INBD GUIDE VANE REPAIR - DELAMINATION ON LEFT OUTBOARD FLAP INBOARD GUIDE VANE LEADING EDGE. PERMANENT RE PAIR INSTALLED SRM 37-03D, PARA 8A, FIG 9A. 2 L 7 2 4F RT A6WE 2007050800200 20070508 00200 NM 2007 5 8 DLM88070428 1 20070205 A 5310 DOOR FRAME DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 938DL 49811 FWD SERVICE DOOR JAMB REPAIR - CRACK AT FWD UPPER CORNER OF FWD SERVICE DOOR JAMB STA 173. PERMANENT REPAIR INSTALLED P ER SRM 53-05D FIGURE 112. 2 L 7 2 4F RT A6WE 2007050800202 20070508 00202 NM 2007 5 8 DLM88070429 1 20070219 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 939DL 49812 DENT IN FUSELAGE SKIN STA 1183 BETWEEN 29L AND 30. PERMANENT REPAIR WAS ACCOMPLISHED PER SRM 53-04D, FIG 12B. 2 L 7 2 4F RT A6WE 2007050800231 20070508 00231 NM 2007 5 8 DLM88070457 1 20070417 A 3211 5935812509 FITTING DOUG MD88 MD88 3023688 NM LT MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 945DL 49818 LT MAIN LANDING GEAR SUPPORT FITTING, EXFOLIATION CORROSION ON INNER BORE OF BUSHING. CORROSION REMOVED, PERMANENT REPA IR PERFORMED FOLLOWING INSTRUCTIONS AND RECOMMENDATIONS CONTAINED IN THE BCAG SR09570087 AND BCAG SR-ID 1-301794190. 2 L 7 2 4F RT A6WE 2007050800232 20070508 00232 NM 2007 5 8 DLM88070458 1 20070417 A 5311 9912246115 FRAME DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 945DL 49818 EXFOLIATION CORROSION ON LOWER SECTION OF FRAME STA 1380. DAMAGED TEE REMOVED AND NEW SECTION INSTALLED PER DOUGLAS DRA WING 9912246. 2 L 7 2 4F RT A6WE 2007050800233 20070508 00233 NM 2007 5 8 DLM88070459 1 20070416 A 5312 SR0953000133 TEE FITTING DOUG MD88 MD88 3023688 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 945DL 49818 TOOLING MARKS ON LOWER T-CAP CHORD OF AFT PRESSURE BULKHEAD AT STA 1338 BETWEEN LONGERONS 28L-28R. SKIN P/N 5911429-151 TRIMMED FOR ACCESS. CHORD P/N SR09530001-33 SPLICED PER EA 09-086680-12 REV E, OPN 0603. SKIN REPAIRED PER SRM 53-03 F IG 37. 2 L 7 2 4F RT A6WE 2007050800235 20070508 00235 NM 2007 5 8 DLM88070461 1 20070416 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 945DL 49818 CRACKS ON FUSELAGE SKIN BETWEEN LONGERONS 2R AND 3R AT STA 1437. PERMANENT REPAIR INSTALLED IAW SRM 53-04 FIG 27. 2 L 7 2 4F RT A6WE 2007050800236 20070508 00236 NM 2007 5 8 DLM88070462 1 20070416 A 5311 9911859121 FRAME DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 945DL 49818 REPAIR OF CRACKS IN STA 1446 UPPER CANTED FRAME. FRAME OUTER CAP P/N 9911859-121 REMOVED. NEW CAP INSTALLED PER SRM 53 -03D FIG 30. 2 L 7 2 4F RT A6WE 2007050800242 20070508 00242 NM 2007 5 8 DLM88070463 1 20070414 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 945DL 49818 CORROSION AT FUSELAGE SKIN STA 260 BETWEEN LONGERONS 30 AND 29L. CORROSION REMOVED AND PERMANENT REPAIR INSTALLED IAW R EPAIR DRAWING AMR0953595 R2 DATED 03APR07 AND ERA 460861-14. 2 L 7 2 4F RT A6WE 2007050800254 20070508 00254 NE 2007 5 8 DLM88070467 2 20070504 A 7250 TURBINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE FAILED A DALA A UNSCHED LANDING R Y PARTIAL RPM/PWR LOSS ENGINE STOPPAGE CL CLIMB 1 SO 27 998DL 36117 53370 726918 ON CLIMBOUT THROUGH 7000 FT LEFT ENG HAD A LOUD BANG, STALL EGT CLIMBED THROUGH 770 DEGREES. OIL PRESSURE INDICATED ZER O ENGINE STOPPED RUNNING- CREW COMPLETED ENGINE SEVERE DAMAGE SHUTDOWN CHECKLIST. AFTER ARRIVAL OIL QTY APPEARED NORMAL , MTC CONFIRMED REAR TURBINE FAILURE AND BLADES IN TAILPIPE. RMVD/REPL FIRE BOTTLE PER AMM-NDS CK OUT209056. REPLACED ENGINE PER TRANSMITTAL 9T102235979. COMPLETED CK-OUT OF FIR BOTTLE PER AMM. 2 L 7 2 4F 4 F RT A6WE E9NE 2007050800255 20070508 00255 NM 2007 5 8 DLM88070468 1 20070413 A 5753 SKIN DOUG MD88 MD88 3023688 NM T/E FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 945DL 49818 LT INBOARD FLAP LOWER SKIN REPAIR BETWEEN STA XW=47 AND XIFO=64.7248 - TEMPORARY REPAIR INSTALLED. TEMPORARY REPAIR REM OVED, DAMAGED SKIN TRIMMED OUT AND NEW SECTION WAS SPLICED PER AM REPAIR DWG AMR0957194 R01 DATED 14MAR07 AND ERA 460139 -14. 2 L 7 2 4F RT A6WE 2007050800256 20070508 00256 NM 2007 5 8 DL76S070469 1 20070421 A 5315 BAC1509100682 FLOORBEAM BOEING 767 767332 1382001 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 128DL 24078 FWD CARGO COMPT FLOORBEAM CHORD CORRODED AT STA 456 RBL 44 AND REPAIRED PER 53-00-07 FIG 201 ON NR 52071 2 L 7 2 4F RT A1NM 2007050800257 20070508 00257 NM 2007 5 8 DL76S070470 1 20070421 A 5315 BAC1509100682 FLOORBEAM BOEING 767 767332 1382001 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 128DL 24078 FWD CARGO COMPT FLOORBEAM CHORD FOUND CORROSION AT STA 434 RBL44 AND WAS REPAIRED ON SRM 53-00-07 FIG 201 REPAIR SCHEME ON NR 520726. 2 L 7 2 4F RT A1NM 2007050800258 20070508 00258 NM 2007 5 8 DL76S070471 1 20070418 A 5315 HXB149953FT FLOORBEAM BOEING 767 767332 1382001 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 128DL 24078 CABIN BS RBL 15 TO 40 FLOOR BEAM FOUND CORRODED, REPAIRED ON NR 51179 PER 53-00-01 FIG 101. 2 L 7 2 4F RT A1NM 2007050800259 20070508 00259 NM 2007 5 8 DL76S070472 1 20070419 A 5320 AND101342009 FLOOR SUPPORT BOEING 767 767332 1382001 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 128DL 24078 CABIN BS 996 TO 999 LBL 33 FLOOR SUPPORT LWR FACE FOUND CRACKED - REPAIRED PER SRM 53-00-51 REPAIR 3 2 L 7 2 4F RT A1NM 2007050900001 20070509 00001 2007 5 9 DL76L070480 4 20070507 A 3413 0665000110 INDICATOR BOEING 767 767332 1382001 NM COCKPIT FAILED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 1200K 28457 CAPT VSI INDICATOR FAILED ON TAXI OUT ELECTRICAL FUMES WERE PRESENT PULL CB SMELL DISSIPATED. REPLACED C/B C586 AND REP LACED CAPT VSI PER AMM OPS NML. NO FUMES PRESENT. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS 2 L 7 2 4F RT A1NM 2007050900008 20070509 00008 WP 2007 5 9 DHL2007806501 1 20070320 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP BS 1670-1705 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 UPPER CARGO COMPT NR 3 TRACK LUG WORN (STA 1670.000 - 1705.000). CUT OUT NR 3 TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 4 9-50 FIG 14. FABRICATED SPLICES (AL7075T6 0.100"/ 0.125"/ 0.160") IAW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND SPLICES IAW SRM 51-3-0, SRM 53-2-3 PG 49-50 FIG 14, SRM 5 1-3-1 PG 2A (TORQUE). 2 L 7 4 4F RT 4A25 2007050900011 20070509 00011 NM 2007 5 9 EIA2007072 1 20070408 A 3350 S1356B37 BATTERY PACK BOEING 747 747273C 1384896 NM CABIN DISCHARGED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 471EV 20651 UPPER DECK EMERGENCY DOME LITE INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK AND OPS CKD PER B747 AMM 33-51-00. 2 L 7 4 4F A20WE 2007050900029 20070509 00029 WP 2007 5 9 DHL2007806511 1 20070330 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP BS 228 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 FOUND UPPER CARGO COMPT NR 7 TRACK LUG WORN STA 228.000. CUT OUT WORN SECTION OF TRACK NR 7 IAW SRM 53-2-3 PG 17-19. C LEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG AND CHANNEL IAW SRM 53-2-3 PG 17-19, SRM 51-3 -0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050900036 20070509 00036 WP 2007 5 9 DHL2007806548 1 20070412 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 759 CRACKED A DHLA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT FITTING CRACKED 1" STA 759.000 L-13R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050900038 20070509 00038 NM 2007 5 9 EIA2007066 1 20070331 A 5730 SKIN BOEING 747 747132 1384882 NM RT WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 RT WING AT HOLES 1467 AT LOWER CHORD CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER ECRA 479-57-217-2 . 2 L 7 4 4F A20WE 2007050900039 20070509 00039 WP 2007 5 9 DHL2007806560 1 20070410 A 5340 37798742 FITTING DOUG DC8 DC873F 302199F WP BS 834 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 FOUND MAIN CARGO COMPT FITTING CRACKED 0.500" STA 834.500 L-13R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TR EATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 PG 2A (TORQUE). REFER TO JC EC-00271-001 (WO 470) FOR FITTING FABRICATION. 2 L 7 4 4F RT 4A25 2007050900043 20070509 00043 WP 2007 5 9 DHL2007806583 1 20070416 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1320 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 AFT CARGO COMPT FRAME CORRODED, STA 1320.000 L-24L TO L-25L. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2. REMOVED FAST ENERS IAW SRM 51-1-20D. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT CORRODED FRAME SEGMENT IAW SRM 53-2-0 FIG 2 SHEET 2. FABRICATED NEW FRAME SEGMENT (P/N 52537716) IAW SRM 53-4-1 FIG 51 S HEET 15 ITEM A, SRM 53-2-0 FIG 2 SHEET 1, SRM 51-2-0 FIG 50. FABRICATED ANGLE AND SPLICE BOTH FROM 7075"0" 0.080" IAW S RM 53-2-0 FIG 2 SHEET 7-8, TR NR 53-110 DATED NOV 10-2000. HEAT TREATED ANGLE AND SPLICE FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFA 2 L 7 4 4F RT 4A25 2007050900046 20070509 00046 WP 2007 5 9 DHL2007806551 1 20070410 A 5551 FITTING DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 LT HORIZ STAB LWR FITTING CRACKED, STA XFS 60.000. REMOVED CRACKED FITTING IAW SRM 51-1-21, SRM 51-1-20D. CLEANED, TRE ATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 2 L 7 4 4F RT 4A25 2007050900056 20070509 00056 EU 2007 5 9 F3LA200700106 1 20070425 A 5321 D5367180500500 FLOOR PANEL AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 801FR 4759 1939 DURING C-3 CHECK, INSPECTION REPORTED FLOOR PANEL 262FF AT R-2 DOOR CORRODED ON BOTTOM OF PANEL. REPLACED FLOORBOARD 26 2FF IAW AMM 53-42-12-400-001. 2 L 7 2 4F RT 2007050900060 20070509 00060 NM 2007 5 9 TSAA0753019 1 20070502 A 5311 657374142 FRAME BOEING 737 737230 1384401 NM BS188 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 821AL 23155 DURING INSPECTION OF THE BS 178 WEB, CRACKS WERE DISCOVERED ON THE BS 188 FRAME AT WL 207 ON BOTH LEFT AND RIGHT SIDES. LEFT SIDE CRACK IS APPROX 1.75 INCHES LONG. RIGHT SIDE CRACK IS APPROX. 2 INCHES LONG. [SUP 05-10-07] INTERIM REPAIR PERFORMED PER ECO 3650 PART I. CRACKS WERE STOP DRILLED AT BS 188 WL 207 LEFT AND RIGHT SIDES. RE-INSPECTION PER ECO 3 650 PART II IS REQUIRED EVERY TWO WEEKS FOR 150 DAYS OR WHEN AIRCRAFT IS FERRIED TO FINAL DESTINATION. PERMANENT REPAIR REQUIRED PER ECO 3650 PART III IF AIRCRAFT IS TO BE USED AFTER FINAL FERRY FLIGHT OR 09/08/2007. 8110-3 RECEIVED ON 05 /03/2007 2 L 7 2 4F RT A16WE 2007050900068 20070509 00068 NM 2007 5 9 EIA2007086 1 20070407 A 5313 STRINGER BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 STRINGER FOUND CORRODED AT STA 800 STRINGER 45L. DAMAGED SECTION OF STRINGER CUT AND REMOVED FABRICATED SPLICE SECTION PER SRM 53-10-03 REPAIR PARTS INSTALLED PER SRM 51-30-02/SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007050900075 20070509 00075 NM 2007 5 9 EIA2007083 1 20070407 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 EVIDENCE OF CORROSION FOUND AT STA 810, WL 91 BETWEEN S45R AND S46R. CORROSION REMOVED AS PER SRM 51-10-01 FOUND OUT OF LIMITS PER SRM 53-30-01. CARRIED OUT REPAIRS PER N482EV-07-003(BOEING 1-307245973) 2 L 7 4 4F A20WE 2007050900081 20070509 00081 NM 2007 5 9 EIA2007088 1 20070413 A 5720 65B159424 SUPPORT BEAM BOEING 747 747212B 1384886 NM RT WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 RT WING INBOARD LEADING EDGE SUPPORT BEAM FOUND WITH EXFOLIATION CORROSION. REMOVED SUPPORT BEAM HFEC INSPECTION CARRIE D OUT ON CUT OUT AREA. NIL CRACKS NOTED. REPAIR CARRIED OUT PER N482EV-07-0004/SRM 51-40-04. 2 L 7 4 4F A20WE 2007050900085 20070509 00085 NM 2007 5 9 EIA2007061 1 20070328 A 2611 30284R9B SMOKE DETECTOR BOEING 747 747200B NM NR 5 NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486EV 20888 NR 5 A LOOP SMOKE DETECTOR WILL NOT TEST. REPLACED SMOKE DETECTOR PER 26-14-01, TEST OK. 1 L 7 4 4F RT A20WE 2007050900087 20070509 00087 NM 2007 5 9 EIA2007091 1 20070331 A 5322 SHEAR TIE BOEING 747 747212B 1384886 NM FUSELAGE OUT OF LIMITS A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 FOUND FRAME SHEAR TIE AT BODY STATION 200-220 BETWEEN STRINGER 35L & 34L WITH TOO LARGE A GAP TO NEW SKIN REPLACEMENT. FABRICATED SHEAR TIE PER B747 SRM 53-10-04 INSTALLED PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007050900089 20070509 00089 NM 2007 5 9 EIA2007077 1 20070327 A 5347 SEAT TRACK BOEING 747 747212B 1384886 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 STA 543 SEAT TRACK DAMAGED AT RBL 11. SEAT TRACK REMOVED AND SENT TO WORKSHOP FOR CROWN AND FLANGE TRIMMING. PRIMER AP PLIED. SEAT TRACK INSTALLED AS PER B747 SRM 51-30-02, SRM 53-10-05 FIG 4. 2 L 7 4 4F A20WE 2007050900097 20070509 00097 EA 2007 5 9 SIMA200712702 1 20070505 A 5350 RADOME CNDAIR CL600 CL6002C10 1390015 EA NOSE ERODED A SIMA O OTHER E VIBRATION/BUFFET DE DESCENT 1 SW 21 515AE 10121 CONTINUOUS NOISE FROM FRONT OF AIRCRAFT NOSE, VIBRATION NOTED, POST FLIGHT INSPECTION REVEALED RADOME EROSION TAPE DELAM INATED. REMOVED AND REPLACED EROSION TAPE IAW AMERICAN EAGLE PROCEDURES. PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DEF ECTS NOTED. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007050900100 20070509 00100 GL 2007 5 9 SIMA200712302 2 20070501 A 7261 ENGINE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL ZONE 400 LEAKING A SIMA O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 21 837AE 14753 4741 145647 CAE311416 "SUP" LAVATORY SMOKE DETECTOR GOING OFF ON TAKEOFF, VISIBLE SMOKE IN CABIN - RETURNED TO DFW. REMOVED AND REPLACED NUMB ER 2 ENGINE IAW AMERICAN EAGLE WORK CARD 72-000-00. ALL OPERATIONAL AND LEAK CHECKS COMPLIED WITH NO DEFECTS NOTED, RET URNED AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007050900103 20070509 00103 NM 2007 5 9 TSAA0753020 1 20070503 A 5330 6545775 SKIN PANEL BOEING 737 737230 1384401 NM BS 887 S23-24R CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 821AL 23155 WHILE PERFORMING INSPECTIONS TO COMPLY WITH AD 2005-13 A CRACK APPROX 2" LONG WAS DISCOVERED AT BS887 +3 BETWEEN STR 23R AND STR 24R. [SUP 05-22-07] CRACK APPROX 2 LONG WAS REPAIRED AT BS 887 + 3 BETWEEN STR 23R AND STR 24R IAW SRM 53-30- 3 PROCEDURE VII. CUTOUT INSPECTED IAW NDT MANUAL PT. 6 51-00-00 FIG 23. FINAL REPAIR SIZE APPROX. 12 X 10. 2 L 7 2 4F RT A16WE 2007050900104 20070509 00104 NM 2007 5 9 TSAA0753021 1 20070503 A 5330 6552988 SKIN PANEL BOEING 737 737230 1384401 NM BS 947 S21-22L CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 821AL 23155 WHILE PERFORMING INSPECTIONS TO COMPLY WITH AD 2005-13-30 A CRACK APPROX 3" LONG, LOCATED AT BS947 +15 BETWEEN STR 21L A ND STR 22L WAS DISCOVERED. [SUP 05-22-07] CRACK APPROX 3 LONG, LOCATED AT BS 947 + 15 BETWEEN STR 21L AND STR 22L WAS REPAIRED IAW SRM 53-30-3 PROCEDURE VII. CUTOUT INSPECTED IAW NDT MANUAL PT. 6 51-00-00 FIG 23. FINAL REPAIR SIZE APPR OX. 26 X 23. 2 L 7 2 4F RT A16WE 2007050900108 20070509 00108 SO 2007 5 9 SIMA200712820 1 20070501 A 5310 14522183011 PROFILE EMB 145 EMB145LR 3260212 SO ZONE 200 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 933JN 4893 14500918 FOUND SERVICE DOOR SURROUND PROFILE AT STRINGER 15R WAS DAMAGED. REMOVED AND REPLACED PROFILE IAW EMB SRM 51-20-03 AND 51-40-02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050900109 20070509 00109 SO 2007 5 9 SIMA200712822 1 20070416 A 5310 14522183009 PROFILE EMB 145 EMB145LR 3260212 SO ZONE 200 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 933JN 4893 14500918 SERVICE DOOR SURROUND PROFILE AT STRINGER 11R WAS DAMAGED. REMOVED AND REPLACED PROFILE IAW EMB SRM 51-20-03 AND 51-40- 02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050900110 20070509 00110 SO 2007 5 9 SIMA200712807 1 20070501 A 5310 14000450001 GUSSET EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 810AE 13175 4800 145525 LEFT GUSSET CORRODED BETWEEN FRAME 59 AND FRAME 61. REMOVED AND REPLACED GUSSET IAW EMB SRM 51-40-02 AND EMB IC2007-145 /02567. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050900111 20070509 00111 SO 2007 5 9 SIMA200712809 1 20070501 A 5347 13500439005 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 810AE 13175 4800 145525 FOUND LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAME 19 TO FRAME 24. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01 -06. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050900112 20070509 00112 SO 2007 5 9 SIMA200712810 1 20070501 A 5347 14000486009 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 810AE 13175 4800 145525 FOUND RIGHT INBOARD SEAT TRACK CORRODED BETWEEN FRAME 24 TO FRAME 28. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01 -06. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050900113 20070509 00113 SO 2007 5 9 SIMA200712816 1 20070501 A 5315 13500437003 FLOORBEAM EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 810AE 13175 4800 145525 RIGHT OMEGAS BEAM INBOARD SIDE FOUND CORRODED BETWEEN FRAME 31 AND FRAME 33. REMOVED AND REPLACED OMEGA BEAM IAW EMB SR M 51-40-02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050900114 20070509 00114 SO 2007 5 9 SIMA200712818 1 20070417 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 939AE 4842 14500923 CARGO DOOR SILL FOUND CORRODED. REMOVED AND REPLACED SILL IAW EMB EMB SRM 51-40-02. RETURNED AIRRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050900115 20070509 00115 2007 5 9 SIMA200712803 2 20070507 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO RIGHT OVERTEMP A SIMA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 671AE 145793 AT TAKEOFF POWER RIGHT ENGINE HIGH ITT, RIGHT ENGINE PARAMETERS HIGH, RETURNED TO ORD. 2 L 7 2 4T RT T00011AT 2007050900118 20070509 00118 SO 2007 5 9 SIMA200712814 1 20070501 A 5320 14521721009 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 810AE 13175 4800 145525 FOWARD DIGITAL CORRODED BELOW FLIGHT DECK THRESHOLD. REMOVED DAMAGED AREA AND SPLICED IN NEW FORWARD THRESHOLD IAW EMB SRM, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050900119 20070509 00119 SO 2007 5 9 SIMA200712821 1 20070416 A 5310 14522183009 PROFILE EMB 145 EMB145LR 3260212 SO ZONE 200 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 933JN 4893 14500918 SERVICE DOOR SURROUND PROFILE AT STRINGER 13R WAS DAMAGED. REMOVED AND REPLACED PROFILE IAW EMB SRM 51-20-03 AND 51-40- 02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050900121 20070509 00121 SO 2007 5 9 SIMA200712808 1 20070501 A 5347 14532606015 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 810AE 13175 4800 145525 LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAME 36 TO FRAME 46. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050900124 20070509 00124 SO 2007 5 9 SIMA200712812 1 20070501 A 5347 14000486003 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 810AE 13175 4800 145525 RIGHT INBOARD SEAT TRACK CORRODED BETWEEN FRAME 28 TO FRAME 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050900125 20070509 00125 SO 2007 5 9 SIMA200712813 1 20070501 A 5315 14000231011 FLOORBEAM EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 810AE 13175 4800 145525 FLOOR SUPPORT CORRODED AT FRAME 25 AROUND FASTENERS. REMOVED AND REPLACED FLOOR SUPPORT IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050900126 20070509 00126 SO 2007 5 9 SIMA200712823 1 20070416 A 5310 14500183009 PROFILE EMB 145 EMB145LR 3260212 SO ZONE 200 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 933JN 4893 14500918 SERVICE DOOR SURROUND PROFILE AT STRINGER 9R FORWARD AND AFT WAS DAMAGED. REMOVED AND REPLACED PROFILE IAW EMB SRM 51-2 0-03 AND 51-40-02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050900127 20070509 00127 EA 2007 5 9 SIMA200712824 1 20070427 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 280-295 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 501BG 10017 FOUND FUSELAGE DENT BETWEEN FS 280 TO FS 295 AND STRINGER 23R AND 24R. PERFORMED PERMANENT REPAIR IAW AMERICAN EAGLE EN GINEERING TECHNICAL NOTICE CR-53MR-121. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007050900128 20070509 00128 EA 2007 5 9 SIMA200712825 1 20070418 A 5315 CC670341757 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 501BG 11449 4174 10017 STA 280 FLOORBEAM CORRODED ALONG TOP FLANGE. SPLICED IN NEW STA 280 FLOOR BEAM AND EXTENTION MOUNTS IAW AMERICAN EAGLE ENGINEERING ORDER CR-53MR-119. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007050900130 20070509 00130 EU 2007 5 9 2007UALA01329 1 20070428 A 3350 321431 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 422UA 503 EEL LIGHT TEST FAIL: -BATTERY FWD LT. REPLACED EEL LIGHT BATTERY AT DOOR 1L. TESTS NORMALLY NOW. 2 L 7 2 4F 4 F RT A28NM E40NE 2007050900132 20070509 00132 2007 5 9 2007UALA01331 4 20070429 A 2565 SLIDE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU L2 DOOR UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 903UA 25003 THE 2L SLIDE OFF MOUNTING. [SUP 05-16-07] REINSTALLED SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007050900134 20070509 00134 NM 2007 5 9 2007UALA01333 1 20070429 A 5312 PRESSURE PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RT MLG WW WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 RIGHT WHEEL WELL ABOVE SPOILER MIXER RATIO CHANGER PRESSURE DECK SKIN WORN IN 2 AREAS. [SUP 05-16-07] MAJOR REPAIR ACC OMPLISHED: BLENDED OUT DAMAGE. FABRICATED & INSTALLED A FILLER & TRIPLER REPAIR TO PRESSURE DECK SKIN UPPER SURFACE INC ORPORATING EXISTING DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007050900135 20070509 00135 SO 2007 5 9 SIMA200712826 1 20070425 A 5320 14522178005 SILL EMB 135 EMB135KL 3260302 SO ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 814AE 19063 145541 SERVICE DOOR CENTER SILL CORRODED BETWEEN FRAME 20 AND FRAME 22. REMOVED AND REPLACED SILL IAW EMB SRM 51-40-02. RETUR NED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050900136 20070509 00136 SO 2007 5 9 SIMA200712401 1 20070501 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 906AE 5762 14500894 EMERGENCY LIGHT INOPERATIVE AT EXIT ROW, FERRIED TO ORD. REMOVED AND REPLACED INVERTER IAW EMB AMM 33-50-11. OPERATION AL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050900137 20070509 00137 NM 2007 5 9 2007UALA01334 1 20070429 A 5342 FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 VERTICAL STAB FUSELAGE FITTING AT BS 1088 RIGHT AFT PRIMARY FITTING FORWARD FACE CORRODED. [SUP 05-16-07] MAJOR REPAIR : REMOVED CORROSION AND SPOT FACED FORWARD FACE OF AFT RIGHT HAND SIDE PRIMARY FITTING. 2 L 7 2 4F 4 F RT A16WE E21EU 2007050900138 20070509 00138 NM 2007 5 9 2007UALA01335 1 20070429 A 5313 STRINGER SPLICE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 CABIN INTERIOR AT BS 348 AND STRINGER S-15L SPLICE CHANNEL LOWER FLANGE CRACKED. [SUP 05-16-07] MAJOR REPAIR ACCOMPLIS HED: REMOVED & REPLACED CRACKED SPLICE CHANNEL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007050900143 20070509 00143 NM 2007 5 9 2007UALA01340 1 20070428 A 5350 TAIL CONE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 TAIL CONE 18 INCH PUNCTURE AT STA 1898. [SUP 05-16-07] MAJOR REPAIR ACCOMPLISHED: MANUFACTURED & INSTALLED STRUCTURAL FILLERS AND DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050900145 20070509 00145 NM 2007 5 9 2007UALA01346 1 20070428 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 EEL LIGHT BAR BROKEN STA 740. REPLACED LIGHT BAR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050900146 20070509 00146 NM 2007 5 9 2007UALA01347 1 20070428 A 3397 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 509UA 24763 EEL BASE WIRE AT STA 1600 DAMAGED. REPLACED DAMAGED WIRE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050900149 20070509 00149 NM 2007 5 9 2007UALA01350 1 20070427 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 STA 246 FLOORBEAM LBL 11 AFT SIDE MID CHORD CRACKED AT LWR RADIUS NEAR FASTENER. MAJOR REPAIR ACCOMPLISHED: CUT OUT CH ORD DAMAGE FROM LBL 59 TO RBL 49. FABRICATED & INSTALLED REPAIR ANGLE, STRAPS & MID CHORD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050900151 20070509 00151 NM 2007 5 9 C1HA200795015 1 20070504 A 5315 FLOORBEAM BOEING 727 727290 138408W NM BS 1110 CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 FOUND FLOORBEAM CORRODED AT STA 1110 LBL 25-45. REPAIRED FLOORBEAM STA 1110 FROM RBL 20 TO LBL 65 IAW B727 SRM 53-10-8 FIG 3. 2 L 7 3 4F A3WE 2007050900152 20070509 00152 NM 2007 5 9 C1HA200795030 1 20070504 A 5313 14981587075T6 STRINGER BOEING 727 727290 138408W NM BS 470 S26R CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 FOUND CORROSION STR 26R STA 470. FABRICATED AND INSTALLED REPAIR PARTS FOR STRINGER 26R BS 450 - 490 IAW B727 SRM 53-10 -3 FIG 1. 2 L 7 3 4F A3WE 2007050900153 20070509 00153 NM 2007 5 9 C1HA200795028 1 20070504 A 5313 STRINGER BOEING 727 727290 138408W NM BS 410 S28L CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 FOUND CORROSION STR 28L AT STA 410. REPAIRED STRINGER AT BS 410 28L IAW B727 SRM 53-10-2 AND 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2007050900154 20070509 00154 NM 2007 5 9 C1HA200795007 1 20070504 A 5347 1520792 SEAT TRACK BOEING 727 727290 138408W NM BS 1130 CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 FOUND CORROSION ON SEAT TRACK AT AFT CUTOUT AND MOUNT POINT STA 1130 LBL 25. REPLACED SEAT TRACK AT BS 1110-1130 LBL 25 , P/N BAC1520-792 IAW B727 SRM 53-10-5 FIG 7. 2 L 7 3 4F A3WE 2007050900155 20070509 00155 NM 2007 5 9 C1HA200795017 1 20070504 A 5347 1520792 SEAT TRACK BOEING 727 727290 138408W NM BS 880-950 CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 FOUND MAIN CABIN STA 880 TO 950 LBL 24 SEAT TRACK HAS CORROSION ON TOP SURFACE. FABRICATED AND INSTALLED NEW SEAT TRACK P/N BAC1520-792 (91") IAW B727 SRM 53-10-5 FIG 1. 2 L 7 3 4F A3WE 2007050900156 20070509 00156 NM 2007 5 9 C1HA200795029 1 20070504 A 5311 1505100360 FRAME BOEING 727 727290 138408W NM BS 351 S28R CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 FOUND CORROSION STA 351.2 FRAME AT 28R. REMOVED EXISTING TEE CHORD FRAME, FABRICATED AND INSTALLED NEW TEE CHORD IAW B7 27 SRM 53-10-2 FIG 1. 2 L 7 3 4F A3WE 2007050900159 20070509 00159 NM 2007 5 9 C1HA200795009 1 20070504 A 5347 1520792 SEAT TRACK BOEING 727 727290 138408W NM BS 380-460 CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 FOUND CORROSION ON SEAT TRACK BS 380 - 460 RBL 45. REPLACED SEAT TRACK AT BS 380 TO 460 RBL 45 IAW B727 SRM 53-10-2 AND 53-10-5 FIG 7. 2 L 7 3 4F A3WE 2007050900160 20070509 00160 NM 2007 5 9 C1HA200795023 1 20070504 A 5320 SHEAR WEB BOEING 727 727290 138408W NM BS 1166 CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 AFT CABIN LT SHEAR WEB BS 1166 LBL 35 HAS HEAVY PITTED CORROSION. REPAIRED AFT CABIN LT SHEAR WEB AT BS 1166 LBL 35 IAW B727 SRM 53-10-2 AND 51-40-2. 2 L 7 3 4F A3WE 2007050900163 20070509 00163 NM 2007 5 9 C1HA200795024 1 20070504 A 5315 FLOORBEAM BOEING 727 727290 138408W NM BS 1130 CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 BS 1130 FLOORBEAM AT LOWER FORWARD FLANGE HAS CORROSION (RBL-10). FOUND CORROSION OUT LIMITS, CUT OUT DAMAGE, FABRICATE D AND INSTALLED FILLERS, ANGLE, RADIUS FILLER AND STRAP REPAIRS TREATED AND PRIMED IAW B727 SRM 51-10-2, 53-10-1, 53-10- 8 AND 51-30-2 FIG 1. 2 L 7 3 4F A3WE 2007050900164 20070509 00164 WP 2007 5 9 N865F1134011 1 20070326 A 5300 UNKNOWN DOUG DC8 DC863F 302198F WP COCKPIT CORRODED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 46088 FOUND COCKPIT SUBFLOOR WITH CORROSION AT STA.-67.00 L21L CPCP455L 0552. 2 L 7 4 4F 4A25 2007050800018 20070508 00018 NM 2007 5 8 07FDEA01698 1 20070504 A 5330 6554575 SKIN BOEING 727 7272S2F 1384O81 NM BS 720D S19L WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 AGING A/C INSPECTION FOUND EXISTING FLUSH REPAIR BETWEEN STA 720D-720E AT STR 19L, ON LAP SPLICE. REPAIR HAS ADDITIONAL WEAR ON THE FILLER. REMOVED WORN FILLER, FABRICATED FILLER AND INSTALLED REF SRM 53-30-3 FIG 14. 2 L 7 3 4F A3WE 2007050800068 20070508 00068 NM 2007 5 8 2007UALA01361 1 20070428 A 5210 HANDLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L2 DOOR OUT OF POSITION A UALA K NONE W INADEQUATE Q C CR CRUISE 1 WP 29 309UA 23670 DOOR 2L OUTSIDE DOOR HANDLE CAME OUT OF STOWED POSITION DURING FLIGHT. [SUP 05-16-07] CAUSE UNKNOWN. ALL CHECKS WERE N ORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007050800080 20070508 00080 WP 2007 5 8 DHL2007806576 1 20070411 A 5522 SKIN DOUG DC8 DC873F 302199F WP RT ELEVATOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 RT ELEVATOR UPPER SKIN DEFLECTED (STA XE 22.875 - 228.031) MAJOR REPAIR (DAMAGED). PERFORMED MAJOR REPAIR IAW SRM 55-4- 1 FIG 1 (SHEET 1-2). REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK OR CORROSION FOUND. ENCLOSED SMN FORM 242-2. FABRICATED PANEL PLATING: SKIN AND F INGER DOUBLER BOTH FROM (AL2024T3 0.016") IAW SRM 55-4-1 FIG 1 SHEET 1-2 ITEM "E""F". BONDED BOTH PARTS WITH HYSOL IAW SRM 51-1-9A, TR NR 51-141 DATED 04-03-06. CLEANED, TREATED AND PRIMED AREA AND PANEL PLATING INNER FACE IAW SRM 51-1-8B . APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-11. INSTALLED PANEL PLATING (STA XE 132.000 TO XE 246.000) IAW SRM 51 2 L 7 4 4F RT 4A25 2007050800103 20070508 00103 WP 2007 5 8 DHL2007806572 1 20070412 A 5280 56489322 HINGE DOUG DC8 DC873F 302199F WP RT MLG DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 RT MLG OUTBD DOOR HINGE CRACKED. REMOVED AND REPLACED RT MLG OUTBD DOOR IAW MM 31-12-1 PG 405. REFER TO JC 8-32-00-003 FOR OPS CHECK. 2 L 7 4 4F RT 4A25 2007050800104 20070508 00104 WP 2007 5 8 DHL2007806595 1 20070418 A 5730 DOUBLER DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 LT WING ACCESS DOOR NR 505F INTERNAL DOUBLER CRACKED 0.250" STA XRS 135.000 X-5 TO S-6 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 04-18-07, BOEING MESSAGE NR 1-306853011 DATED 04-18-07, NR 1-306853011-2 DATED 03-27-07 . REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW BOEING MSG NR 1-306853011-2 , NR 1-306853011-4, SEMAN DWG NR ED-4482-1, SRM 57-2-1 FIG 36. PERFORMED NDT INSP IAW BOEING NDT SPM PART 08-00-02 TO 0 7. FABRICATED INTERNAL REPAIR DOUBLER (AL7075T6 0.063") EXTERNAL DOUBLER (AL7075T6 0.160") AND FILLER (AL7075T6511 0.36 0") IAW BOEING MESSAGE NR 1-306853011-2, NR 1-306853011-4, SEMAN DWG ED-4482-1. CLEANED, TREATED AND PRIMED AREA AND RE 2 L 7 4 4F RT 4A25 2007050800217 20070508 00217 WP 2007 5 8 DHL2007806581 1 20070416 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1420 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT FRAME FITTING HAS A MISDRILLED HOLE STA 1420.000 L-20R TO L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED DAMAGED FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-11. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 (TO RQUE). 2 L 7 4 4F RT 4A25 2007050800260 20070508 00260 NE 2007 5 8 DL777070473 2 20070428 A 7230 BLADES BOEING 777 777232 1385232 NM RROYCE RB211 RB211TRENT89 NE NR 2 ENGINE DAMAGED A DALA A UNSCHED LANDING A FLAME/FIRE TO TAKEOFF 1 SO 27 860DA 28777 29951 51156 ON TAKE OFF OUT OF NRT THE RIGHT EXPERIENCED 4 TO 6 STALLS WITH FLAMES FROM TAILPIPE. A/C RTB TO NRT. ENGINE WAS NOT S HUTDOWN. FURTHER INSPECTION REVEALED METAL ON THE MCD AND IN THE TAILPIPE. MAX TGT OF 946 AND 940 FOR 8 SECONDS. PER AMM ENGINE CHANGE REQUIRED. PERFORMED BORO INSP PER AMM. FOUND SEVERAL BLADES BENT/DAMAGED HPC BORO PLUG HP5S. PERFOR MED POWERPLANT AFTER SURGE INSP PER AMM. REPLACED NR 2 E PER TRANS 11T003. ETOPS CATEGORY 'C': UNCOMMANDED PWR CHANG ES, SURGES, OR STALLS 2 L 7 2 4F 4 F RT T00001SE E00050EN 2007050800261 20070508 00261 NM 2007 5 8 DL76G070475 1 20070505 A 3610 80217010 VALVE BOEING 767 767332 1382001 NM RIGHT UNSERVICEABLE A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 1604R 30180 RIGHT PRV MESSAGE ON TAKEOFF ROLL. RIGHT PRV FOUND AT FAULT - R/R SAME. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTA L TO ETOPS 2 L 7 2 4F RT A1NM 2007050900002 20070509 00002 WP 2007 5 9 DHL2007806585 1 20070416 A 7160 NOSE COWL DOUG DC8 DC873F 302199F WP NR 1 ENGINE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 NR 1 ENGINE NOSE COWLING RT UPPER PART WORN AT 12 O'CLOCK POS STA YN 163.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2, 3. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED SKIN (AL20 24T3 0.080") AND SPLICE (STEEL 17-7PH 0.050") IAW DC870 SRM 71-5-2 FIG 2 SHEET 1, 2, 3. HEAT TREATED SPLICE FROM 17-7PH CRESS TO 17-7 PH CRESS (H1050) IAW SRM 51-1-6. CLEANED, TREATED AND PRIMED AREA AND SKIN IAW SRM 51-1-8B. APPLIED SEA LANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW SRM 71-5-2 FIG 2 SHEET 1, 2, 3, SRM 51-1-21A. 2 L 7 4 4F RT 4A25 2007050900009 20070509 00009 WP 2007 5 9 DHL2007806536 1 20070409 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 25 L21R CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 FOUND MAIN CARGO COMPT FITTING CORRODED STA 25.000 L-21R. REMOVED CORROSION FROM FITTING IAW SRM 51-1-8 PG 17-18. FOUN D OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-0, SRM 51-3-1 PG 2A (TORQUE). 2 L 7 4 4F RT 4A25 2007050900010 20070509 00010 NM 2007 5 9 EIA2007095 1 20070422 A 2611 BULB AUTRONICS BOEING 747 747273C 1384896 NM SMOKE DETECTOR INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 471EV 20651 NR 2 MAIN DECK SMOKE DETECTOR INOP. RELAMPED NR 2 SMOKE DETECTOR. OPS CHECKED GOOD IAW B747 MM 26-14-00. 2 L 7 4 4F A20WE 2007050900016 20070509 00016 WP 2007 5 9 DHL2007806530 1 20070402 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 280 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 NR 1 CARGO DOOR JAMB FITTING CORRODED, STA 280.000 L-31R. REMOVED CORROSION FROM FITTING AT NR 1 CARGO DOOR JAMB IAW SR M 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FITTING IAW SRM 51-1-20D. CLEANED, TREA TED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050900021 20070509 00021 NM 2007 5 9 EIA2007069 1 20070407 A 2782 DRIVE ASSY BOEING 747 747230B 1384889 NM L/E SLAT MALFUNCTIONED A EIAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 09 478EV 23286 NR 1 LT LEADING EDGE DRIVE FAILED TO RETRACT PNEU OR ELEC AFTER T/O FROM JFK AIRCRAFT RETURNED TO JFK. AWAITING CORRECT IVE ACTION 2 L 7 4 4F A20WE 2007050900027 20070509 00027 WP 2007 5 9 DHL2007806510 1 20070327 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP BS 1588 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 UPPER CARGO COMPT NR 2 TRACK LUG WORN STA 1588.000. REMOVED WORN TRACK SEGMENT AND SPLICES IAW SRM 51-3-0. CLEANED, TR EATED AND PRIMED AREA AND NEW TRACK SEGMENT AND SPLICES IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND REINSTALLED SP LICES IAW SRM 53-2-3 PG 50 FIG 14, SRM 51-3-1 PG 2A (TORQUE). 2 L 7 4 4F RT 4A25 2007050900028 20070509 00028 NM 2007 5 9 EIA2007068 1 20070322 A 5415 ATTACH ANGLE BOEING 747 747132 1384882 NM NR 3 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 NR 3 PYLON STA 270 BULKHEAD AFT SIDE I/B AND AFT O/B OF FRONT SPAR CHORD ASSY HAS SKIN TO BULKHEAD ATTACH ANGLES CRACKED . REPAIRED NR 3 PYLON STA 270 BULKHEAD AFT SIDE I/B AND O/B SIDE SKIN TO BULKHEAD ATTACH ANGLES PER B747 SRM 54-120-03 FIG 19, 51-20-01 FIG 1 PAGE 13, 51-10-02 PAGES 6-8 AND 51-30-02 PAGES 8-9. 2 L 7 4 4F A20WE 2007050900031 20070509 00031 NM 2007 5 9 EIA2007067 1 20070401 A 5711 SPAR BOEING 747 747132 1384882 NM RT WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 RT WING FWD SPAR O/B LOWER CHORD CORRODED FROM 1467-1475. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER ECRA 4 79-57-218-2 REV A. 2 L 7 4 4F A20WE 2007050900045 20070509 00045 WP 2007 5 9 DHL2007806550 1 20070410 A 5514 STIFFENER DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 LT HORIZ STAB STIFFENER CRACKED 1" STA XFS 47.500. REMOVED CRACKED STIFFENER IAW SRM 51-1-21. CLEANED, TREATED AND PRI MED AREA IAW SRM 51-1-8B. INSTALLED NEW STIFFENER IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007050900084 20070509 00084 NM 2007 5 9 EIA2007093 1 20070331 A 5313 STRINGER BOEING 747 747212B 1384886 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 FOUND STRINGER 28AL BETWEEN BODY STATION 180-200 WITH OVERSIZED HOLES. REMOVED STRINGER 28AL FROM BODY STATION 180-200. FABRICATED PER B747 SRM 53-10-03 FIG 3. 2 L 7 4 4F A20WE 2007050900086 20070509 00086 NM 2007 5 9 EIA2007096 1 20070422 A 2611 2156646 SMOKE DETECTOR BOEING 747 747273C 1384896 NM NR 1 FAILED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 471EV 20651 NR 1A MAIN DECK SMOKE DETECTOR INOP. REMOVED AND REPLACED 1A SMOKE DETECTOR ON MAIN DECK OPS CKED GOOD PED B747 MM 26-1 4-02. 2 L 7 4 4F A20WE 2007050900094 20070509 00094 NM 2007 5 9 EIA2007082 1 20070322 A 5347 SEAT TRACK BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 SEAT TRACK FOUND CORRODED AT LBL 11 STA 470. SEAT TRACK REMOVED AS PER SRM 51-30-01. SEAT TRACK TRIMMED AND PRIMER APP LIED PER SOPM 20-41-01. SEAT TRACK INSTALLED PER SRM 53-10-05 FIGURE 4. 2 L 7 4 4F A20WE 2007050900095 20070509 00095 SO 2007 5 9 SIMA200712703 1 20070505 A 2612 3601133500 FIRE DETECTOR EMB 145 EMB145LR 3260212 SO LEFT ENGINE FAILED A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 631AE 8273 7049 145139 ENGINE ONE FIRE DETECT FAIL CAUTION MESSAGE ON TAKEOFF. REMOVED AND REPLACED NUMBER ONE ENGINE FIRE DETECTOR IAW EMB AM M 26-11-01 AND ENGINE PYLON FIRE DETECTOR IAW EMB 26-11-02. OPERATIONAL CHECKS GOOD ON BOTH COMPONENTS, RETURNED AIRCRAF T TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050900101 20070509 00101 SO 2007 5 9 SIMA200713201 1 20070430 A 2720 12009421249 CONTROL ROD EMB 145 EMB145LR 3260212 SO RUDDER EXCESS PLAY A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AE 17809 145148 PERFORMING AN A CHECK FOUND UPPER RUDDER CONTROL ROD HAD PLAY BETWEEN THE ROD END AND ROD TUBE. REMOVED AND REPLACED UP PER RUDDER CONTROL FOR PLAY AND LOWER CONTROL ROD AS PRECAUTIONARY, FDR DOWNLOADED. COMPONENTS AND FDR DATA RELEASED TO OEM FOR ANALYSIS. PERFORMED OPERATIONAL CHECKS WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050900107 20070509 00107 SO 2007 5 9 SIMA200712819 1 20070416 A 5310 14522183011 PROFILE EMB 145 EMB145LR 3260212 SO ZONE 200 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 933JN 4893 14500918 SERVICE DOOR SURROUND PROFILE AT STRINGER 7R WAS DAMAGED. REMOVED AND REPLACED PROFILE IAW EMB SRM 51-20-03, 51-40-02 A ND 51-40-02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050900117 20070509 00117 SO 2007 5 9 SIMA200712811 1 20070501 A 5347 13500439007 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 810AE 13175 4800 145525 LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAME 19 TO FRAME 23. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. R ETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050900120 20070509 00120 SO 2007 5 9 SIMA200712806 1 20070501 A 5310 14526437001 GUSSET EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 810AE 13175 4800 145525 FOUND RIGHT GUSSET CORRODED BETWEEN FRAME 59 AND FRAME 61. REMOVED AND REPLACED GUSSET IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050900123 20070509 00123 EA 2007 5 9 SIMA200712801 1 20070507 A 3397 WIRE CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 501BG 10017 RIGHT OVERWING LOWER EMERGENCY LIGHT INOPERATIVE. REPAIRED BROKEN WIRE ON CONNECTOR P350 WIRE NUMBER THREE IAW EMB WM 3 3-50-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007050900131 20070509 00131 2007 5 9 2007UALA01330 4 20070427 A 2565 SLIDE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU L2 DOOR UNKNOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 918UA 25385 STRINGS HANGING OUT OF DOOR 2L ESCAPE SLIDE. [SUP 05-16-07] REPLACED SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007050900140 20070509 00140 NM 2007 5 9 2007UALA01337 1 20070429 A 5320 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 LEFT UPPER FUSELAGE FWD ENTRY DOOR UPPER HINGE CUTOUT HAS 3 EA EXISTING FASTENER HOLES CRACKED. [SUP 05-16-07] MAJOR REPAIR ACCOMPLISHED: ENLARGED HOLES & SPOT FACE TO REMOVE DAMAGE. FABRICATED & INSTALLED EXTERNAL FILLER & DOUBLER REP AIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007050900147 20070509 00147 NM 2007 5 9 2007UALA01349 1 20070429 A 3397 CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 644UA 25094 EMERGENCY FLOOR LIGHTING STRIP NEAR 1B COMING UP. POSITIONED CABLE IN THE CORRECT PLACE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050900148 20070509 00148 NM 2007 5 9 C1HA200795018 1 20070504 A 5313 STRINGER BOEING 727 727290 138408W NM BS 720B S15L CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 FOUND STRINGER 15L CRACKED AT BS 720B. REPAIRED STRINGER 15L AT BS 720B IAW B727 SRM 53-10-3 FIG 5. 2 L 7 3 4F A3WE 2007050900165 20070509 00165 WP 2007 5 9 N865F1480010 1 20070430 A 5321 PANEL DOUG DC8 DC863F 302198F WP COCKPIT CORRODED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 78924 46088 COCKPIT SUBFLOOR PRESSURE PANEL EXISTING REPAIR WITH CORROSION STA -17.00 LBL 50". 2 L 7 4 4F 4A25 2007050900166 20070509 00166 WP 2007 5 9 N865F1479009 1 20070430 A 5313 STRINGER DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 78924 46088 COCKPIT SUB FLOOR STRINGER DOUBLER WITH CORROSION AT STA -117.00 CPCP 455R 0552. 2 L 7 4 4F 4A25 2007050900168 20070509 00168 NM 2007 5 9 C1HA200795022 1 20070504 A 5347 15201466 SEAT TRACK BOEING 727 727290 138408W NM BS 740-760 CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 FOUND CABIN SEAT TRACK AT BS 740-760 LBL 24 IS CORRODED BEYOND LIMITS. REPLACED MAIN CABIN SEAT TRACK AT BS 740-760 LBL 24 IAW B727 SRM 53-10-2 AND 53-10-5. 2 L 7 3 4F A3WE 2007050900170 20070509 00170 NM 2007 5 9 C1HA200795032 1 20070504 A 5313 14981427075T6 STRINGER BOEING 727 727290 138408W NM BS 475 S27L CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 FOUND CORROSION IN E/E BAY AT BS 475 STR 27L. REPAIRED STR 27L AT BS 475 IAW B727 SRM 53-10-2 FIG 9 AND 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2007050900172 20070509 00172 NM 2007 5 9 C1HA200795016 1 20070504 A 5347 1520792 SEAT TRACK BOEING 727 727290 138408W NM BS 1010-1130 CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 FOUND SEAT TRACK CORRODED IN SEVERAL MARKED AREAS STA 999-1110 LBL 25. REMOVED AND REPLACED SEAT TRACK ON STA 1010-1130 LBL 25 IAW B727 SRM 51-30-2 AND 53-10-5 FIG 7. 2 L 7 3 4F A3WE 2007050900173 20070509 00173 SO 2007 5 9 SIMA200712827 1 20070425 A 5315 14521700007 FLOORBEAM EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 814AE 13063 4800 145541 LEFT OMEGA BEAM INBOARD SIDE CORRODED AT FRAME 20 CROSSBEAM. REMOVED DAMAGE AND INSTALLED DOUBLER IAW EMB SRM 53-00-01, FIGURE 201. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050900174 20070509 00174 NM 2007 5 9 2007UALA01352 1 20070427 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 AFT CARGO PIT FRAME UPPER CHORD CORRODED AROUND FASTENER HOLES STA 1197, LBL 42 TO RBL 42. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION. FABRICATED & INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 2007052500084 20070525 00084 NE 2007 5 25 2007UALA01354 2 20070429 A 7200 PW4060 ENGINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 SURGES A UALA C ABORTED TAKEOFF E A VIBRATION/BUFFET FLAME/FIRE TO TAKEOFF 1 WP 29 661UA 65645 27158 717654 GROUP 3 SURGE ON TAKE OFF 1.33 EPR. PASSENGER COMFIRMED FLAMES FROM RT SIDE OF ACFT. ENGINE RECOVERED NO OTHER LIMITS EX CEEDED AND RESPONSE OK. SUPPLEMENTAL DATA UPDATE REPLACED #2 ENGINE. #2 ENG-RUN UP ENGINE PER AMM71-00-56-201 ACCT OF ENG REPLACEMENT. -#2 ENG OP CHKD GOOD ON ENG RUN, NO FAULTS, NO LKS. POST REMOV AL BORESCOPE OF REMOVED ENGINE SHOWS NORMAL TURBINE DETERIORATION.REMOVED ENGINE APPEARS TO HAVE CLASSIC GROUP THREE SUR GE CHARACTERISTICS: I.E. HIGH PRESS COMPRESSOR CONTACTS AIRSEALS & OPENS CLEARANCES. COMPRESSED AIR SLIPS-BACK & CAUSES BACK PRESSURE WITH RESULTING STALL. KNOWN DETERIORATION PATTERN. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050900178 20070509 00178 NM 2007 5 9 2007UALA01357 1 20070429 A 2121 FAN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 799UA 26926 F/A'S REPORTED SLIGHT SMOKE OR ELECTRICAL ODOR IN CABIN ORIGINATING FROM BUSINESS CLASS. REPLACED RIGHT HAND RECIRCULA TION FAN PER MM 21-25-07, ALL OPS GOOD,TEST PASS PER MAT OF RECIRC FAN SYS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007050900179 20070509 00179 EU 2007 5 9 2007UALA01363 1 20070430 A 2720 SERVO AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RUDDER PEDAL VIBRATION A UALA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 490UA 1728 VIBRATION AT 300KT APPEARS TO GO AWAY WITH RIGHT RUDDER INPUT STOPS AT 275 WITH NO SAMC TEXT: CREW REPORTING VIBRATION WHILE CLIMBING AT SPEEDS ABOVE 275 WITH NOTICEABLE VIBRATIONS FELT IN SEAT AND RUDDER PEDALS THAT WOULD BE CORRECTED WIT H RIGHT RUDDER INPUTS. VIBRATION STOPS AT SPEED BELOW 275. [06-26-07] YELLOW SYS RUDDER SERVO ACT FOUND WITH EXCEESIV E ROD END PLAY. REPLACED YELLOW SYSTEM RUDDER SERVO ACTUATOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007050900181 20070509 00181 NM 2007 5 9 2007UALA01393 1 20070503 A 2913 PUMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE MALFUNCTIONED A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 563UA 26665 LANDED UNDER AMBER ALERT DUE TO LOSS OF LEFT ENGINE HYDRAULIC PUMP. [SUP 06-01-07] LT HYD SYSTEM FAILED. REPLACED NR 1 ENGINE DRIVEN HYD PUMP. ALSO REPLACED LT EDP PRESSURE AND CASE DRAIN FILTER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050900183 20070509 00183 NM 2007 5 9 2007UALA01395 1 20070503 A 3150 WARNING SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 520UA 24890 RECEIVED FLAPS DISAGREE INDICATION ON APPROACH. [SUP 06-06-07] FLAPS FAILED TO MOVE. TRAILING EDGE LIGHT ILLUMINATED. EICAS MESSAGE 'TE FLAP DISAGREE' DISPLAYED. FLAPS OPERATE NORMALLY ON ALTERNATE SYSTEM. CONDUCTED OPERATION CHECKS OF THE FLAP AND LEADING EDGE SYSTEM, COULD NOT DUPLICATE PROBLEM AND CAUSE OF DISCREPANCY NOT ESTABLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050900185 20070509 00185 NM 2007 5 9 2007UALA01397 1 20070503 A 5523 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU ELEVEVATOR TAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 330UA 24191 LEFT ELEV TAB UPPER SKIN CRACKED AT HINGE NR 2 APPROX FIVE EIGHTH'S OF AN INCH IN LENGTH. REPLACED LEFT ELEVATOR TAB. 2 L 7 2 4F 4 F RT A16WE E21EU 2007050900192 20070509 00192 NM 2007 5 9 2007UALA01399 1 20070503 A 2721 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RUDDER TRIM MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 WP 29 565UA 26669 RUDDER TRIM FAILED TO TRIM IN LEFT DIRECTION. [SUP 06-06-07] DURING DESCENT STARTED TO WORK ERRATICALLY IN ONE DIRECTI ON. BY THE TIME IT ARRIVED AT GATE, IT OPERATED NORMALLY. REPLACED RUDDER TRIM ACTUATOR. ACCOMPLISHED INSPECTION OF RUDDER TRIM ACTUATOR INSTALLATION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050900194 20070509 00194 NM 2007 5 9 2007UALA01401 1 20070503 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE BURNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 337UA 24241 LOWER LIP OF EXTERNAL POWER CONNECTOR DOOR FRAME HAS A HALF INCH BURN-OFF ON METAL FRAME. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED INTERNAL DOUBLER & ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007050900195 20070509 00195 NM 2007 5 9 2007UALA01402 1 20070503 A 5320 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FSUELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 337UA 24241 FORWARD CARGO DOOR GAP BETWEEN FORWARD CARGO DOOR AND THRESHOLD HAS A 1 INCH SCRIBE 0085" DEEP. MAJOR REPAIR ACCOMPLISH ED: REPAIRED BLENDED SCRIBE AREA & INSTALLED REPAIRED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007050900197 20070509 00197 NM 2007 5 9 2007UALA01404 1 20070504 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EEL 46 ABC INOPERATIVE. RELAMPED EEL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050900199 20070509 00199 NM 2007 5 9 2007UALA01406 1 20070504 A 3350 9F19948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EEL 4J FWD & 35 ABC ARE INOPERATIVE. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050900200 20070509 00200 NM 2007 5 9 2007UALA01407 1 20070504 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 CEILING EMERGENCY LIGHT INOPERATIVE AT ROW 8 LEFT. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050900201 20070509 00201 NM 2007 5 9 2007UALA01408 1 20070503 A 2730 PULLEY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ELEVATOR CONTROL CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 CABIN CROWN AREA, 2 EACH ELEVATOR CONTROL CABLE PULLEYS ARE CRACKED AT STA 340 BETWEEN STR 2L AND STR 3L. [SUP 06-06-07 ] REMOVED AND REPLACED PULLEYS AT STA 340 AND VERIFIED CABLE TENSION. ACCOMPLISHED FUNCTIONAL CHECK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050900203 20070509 00203 NM 2007 5 9 2007UALA01411 1 20070502 A 2530 MOTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2 CART LIFT OVERHEATED A UALA K NONE M OVER TEMP IN INSP/MAINT 1 WP 29 182UA 25279 CART LIFT MOTOR NR 2 OVERHEATED AFTER CATERING SERVICE LOADED 8 FOOD CARTS. [SUP 06-01-07] REPLACED CART LIFT ACTUATOR MOTOR ASSY PER MM25-38-02. OP CHECKED GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050900205 20070509 00205 NM 2007 5 9 KCSA07042 1 20070504 A 2120 UNKNOWN BOEING 747 7472B4B 138481B NM CABIN ODOR A KCSA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 713CK 21099 NR 1 PACK RUMBLING AND BURNING SMELL FROM DUCT, TEMPS NORMAL. 2 L 7 4 4F RT A20WE 2007050900206 20070509 00206 EU 2007 5 9 200705071 1 20070503 A 2822 PUMP EMB ERJ170 ERJ170100SE 3260406 EU FUEL SYSTEM MALFUNCTIONED A UHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 866RW 17000129 FLIGHT 6451 MEM TO ATL ON THE TAKEOFF ROLL AS POWER WAS APPLIED, CREW RECEIVED A BLUE CREW AWARENESS EICAS MESSAGE, FUEL 2 FEED FAULT. THE TAKEOFF WAS ABORTED AT ABOUT 10 KNOTS. MAINTENANCE ADVISED THE CREW TO CYCLE A/C PUMP 2. CREW COMP LIED. SYSTEM OPS CHECK NORMAL. NO OTHER MAINTENANCE REQUIRED. 2 L 7 2 4F RT A56NM 2007050900207 20070509 00207 EU 2007 5 9 200705072 1 20070503 A 2913 5116402 PUMP EMB ERJ170 ERJ170100SE 3260406 EU NR 2 ENGINE LEAKING A UHLA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 GL 11 651RW 17000072 FLIGHT 7511 IAD TO DFW ABOUT 25 MINUTES INTO THE FLIGHT THE CREW RECEIVED -HYD 2 LO QTY- EICAS MESSAGE. HYDRAULIC FLUID AT 20%, DECREASING TO BELOW 10%. CREW DIVERTED TO CMH. ABOUT 30 MILES FROM CMH, CREW RECEIVED -HYD 2 LO PRESS-, EICAS MESSAGE. THE FLUID QUANTITY DECREASED TO 0% AND THE PRESSURE WAS 0. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INC IDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP. 2 L 7 2 4F RT A56NM 2007050900209 20070509 00209 WP 2007 5 9 ARWA20070502 1 20070503 A 3244 TIRE DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE NR 5 FAILED A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET TO TAKEOFF 1 SO 19 450ML 47831 517829 POST FLIGHT FOUND NR 5 TIRE SHREDDED AND DAMAGE TO AIRCRAFT AND NR 1 ENGINE. [SUP 06-01-07] REMOVED AND REPLACED NR 6 MAIN WHEEL ASSEMBLY IN ACCORDANCE WITH DC-10 M/M 32-41-01. 2 L 7 3 4F 4 F RT A22WE E23EA 2007050900210 20070509 00210 2007 5 9 C2XA07RI025 4 20070501 A 2297 WIRE EMB 145 EMB145XR 3260214 SO COCKPIT BROKEN A C2XA K NONE J WARNING INDICATION AP APPROACH 1 SW 27 13124 145689 FLT 2556 EWR - CREW REPORTED FD WENT INTO GO-AROUND MODE BY ITSELF ON APPROACH. EWR MX FOUND BROKEN WIRES AT THRUST LEV ER GO-AROUND MICRO SWITCH. MX REPAIRED WIRES AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007050900212 20070509 00212 SO 2007 5 9 C2XA07IA110 1 20070504 A 3350 2013BR BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11551 6286 1660 145411 IAH - DURING MAINTENANCE INSPECTION THE FORWARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED THE NUMBER ONE EMERGENCY LIGHT BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050900213 20070509 00213 GL 2007 5 9 C2XA07IA107 2 20070506 A 7321 23078837 FADEC EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL MALFUNCTIONED A C2XA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 27 17138 1864 1864 145727 CAE312345 IAH - FLIGHT 2326, THE CREW REPORTED THAT THE AIRCRAFT WOULD NOT COME OUT OF TAKEOFF MODE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE THE FADEC 2A, OPERATIONALLY CHECKED WITH NO DEF ECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT TE6CH 2007050900216 20070509 00216 SO 2007 5 9 C2XA07IA106 1 20070504 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 36915 5954 2592 145421 IAH - FLIGHT 2942, DURING PREFLIGHT INSPECTION THAT SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE CHARGED THE AFFECTED EMERGENCY LIGHT BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050900221 20070509 00221 SO 2007 5 9 C2XA07ON002 1 20070508 A 5270 INDICATION SYS EMB 145 EMB145XR 3260214 SO CARGO DOOR MALFUNCTIONED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 14162 0808 FL 22 - ONT TO TUL - AIR RETURN DUE TO BAGGAGE DOOR OPEN ON EICAS. CREW RETURNED TO ONT. MX INSPECTED BAGGAGE DOOR AND FOUND NO EVIDENCE OF BAGGAGE DOOR BEING OPEN IN FLIGHT. MX FOUND AN INDICATION PROBLEM. A/C WAS RELEASE IAW MEL 52-70 -00/2 CAT-C CONTROL 121022. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2007050900222 20070509 00222 SO 2007 5 9 C2XA07CL043 1 20070508 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16961 145103 CLE FLIGHT 2473 THE CREW REPORTED THE ASILE PATH EMERGENCY LIGHTS BETWEEN THE EXIT ROWS WERE INOPERATIVE. MAINTENANCE P ERFORMED OPERATIONAL CHECKS OF THE EMERGENCY LIGHTS AND OPERATIONAL CHECKS WERE GOOD. NO DEFECTS NOTED. THE AIRCRAFT W AS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007050900224 20070509 00224 NM 2007 5 9 SWAA072286 1 20070507 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 LEFT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007050900226 20070509 00226 NM 2007 5 9 SWAA072285 1 20070507 A 2731 6545166 CONTROL ROD BOEING 737 7373G7 1384595 NM ELEVATOR TAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, FOUND RIGHT ELEVATOR TAB CONTROL ROD CRACKED AT DRAIN HOLE. REMOVED AND REPLACED CONTROL RO D PER MM. 2 L 7 2 4F RT A16WE 2007050900227 20070509 00227 NM 2007 5 9 SWAA072299 1 20070507 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 770, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007050900230 20070509 00230 NM 2007 5 9 SWAA072305 1 20070507 A 5330 655298871 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 957, STR 17L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007050900232 20070509 00232 NM 2007 5 9 SWAA072295 1 20070507 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM L2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007050900234 20070509 00234 NM 2007 5 9 SWAA072293 1 20070507 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM L1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2007050900236 20070509 00236 NM 2007 5 9 SWAA072289 1 20070507 A 5754 65C26602312A WEDGE BOEING 737 7373H4 1384600 NM L/E SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED C4 CHECK, FOUND RIGHT NR 5 L/E SLAT UPPER T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PE R MM. 2 L 7 2 4F RT A16WE 2007050900237 20070509 00237 NM 2007 5 9 SWAA072288 1 20070507 A 5754 65C26603202A WEDGE BOEING 737 7373H4 1384600 NM L/E SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED C4 CHECK, FOUND RIGHT NR 4 L/E SLAT UPPER T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PE R MM. 2 L 7 2 4F RT A16WE 2007050900238 20070509 00238 NM 2007 5 9 SWAA072283 1 20070507 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 3 DEF. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007051000001 20070510 00001 NM 2007 5 10 ASAA0741630 1 20070507 A 5320 65C334952 WEB BOEING 737 7374Q8 138447Q NM FUSELAGE PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 AFT CABIN FLOOR WEB PUNCTURED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 51-70-13 FIG 1. 2 L 7 2 4F RT A16WE 2007051000002 20070510 00002 NM 2007 5 10 ASAA0771631 1 20070507 A 5320 146A75021 ANGLE BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 AFT CARGO PIT AT BS 787 LEFT ZEE ANGLE IS CORRODED. REPAIRED IAW SRM 53-60-53 FIG 2. 2 L 7 2 4F RT A16WE 2007051000005 20070510 00005 EA 2007 5 10 TRAX200700620 1 20070504 A 5220 HANDLE CNDAIR CL600 CL6002C10 1390015 EA ESCAPE HATCH CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 706EV 10054 CREW EMERGENCY ESCAPE HATCH OUTER HANDLE CORRODED. 2 L 7 2 4F RT A21EA 2007051000006 20070510 00006 EU 2007 5 10 TRAX200700621 1 20070504 A 5260 STEP AEROSP ATR72 ATR72 EU PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 TOP STEP ON PAX DOOR BROKEN. 2 H 7 2 4T RT 2007051000007 20070510 00007 EA 2007 5 10 TRAX200700607 1 20070423 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 974EV 7594 PAX DOOR TOP STEP CRACKED ON AFT AND FWD SIDE. 2 L 7 2 4F RT A21EA 2007051000009 20070510 00009 EA 2007 5 10 TRAX200700609 1 20070503 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 CORROSION ON FLOORBEAM BETWEEN FS 559.00 +112 TO 621 AND LBL 9. [SUP 05-15-07] CORROSION ON FLOOR BEAM BTWN FS 559.00 +112 TO 621 AND LBL 9 REMOVED AS PER SRM 51-21-06. ALODINED AND PRIMED AS PER SRM 51-21-11. PAINTED AS PER SRM 51-21-1 1. 2 L 7 2 4F RT A21EA 2007051000011 20070510 00011 EA 2007 5 10 TRAX200700611 1 20070503 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 CORROSION ON FLOORBEAM BETWEEN FS 559.00 + TO 621.00 AND LBL 2. [SUP 05-17-07] REMOVED CORROSION AND FOUND OUT OF LIM ITS IAW REO 601R-53-00-005. FLOORBEAM FABRICATED AS PER SRM 51-24-36. FABRICATE FLOORBEAM INSTALLED AS PER SRM 51-42-2 0. 2 L 7 2 4F RT A21EA 2007051000012 20070510 00012 EA 2007 5 10 TRAX200700612 1 20070503 A 5320 SPLICE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 CORROSION ON FLOOR SUPPORT STRUCTURE CAP SPLICE AT FS 559.00 +112 AND 589.00 FROM LBL 45 TO RBL 45. REMOVED CORROSION A S PER SRM 51-21-06. ALODINED, PRIMED AND PAINTED AS PER SRM 51-21-11. MATERIAL THICKNESS .063", MATERIAL REMOVED .005". WITHIN LIMITS PER SRM 53-00-00 FIG. 1. 2 L 7 2 4F RT A21EA 2007051000018 20070510 00018 EA 2007 5 10 TRAX200700617 1 20070504 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR PEELING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 706EV 10054 ASD EXIT PLACARD PEELING. REMOVED AND REPLACED ASD EXIT PLACARD IAW CRJ 700 AMM 11-30-02. 2 L 7 2 4F RT A21EA 2007051000024 20070510 00024 NM 2007 5 10 CALA0700232 1 20070504 A 5320 69265552 FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14358 23943 INSPECTION FOUND A .5 INCH CRACK IN ANGLE CLIP AT STA 351.20, S16L. REPAIRED IAW ECRA 5311-01320. 2 L 7 2 4F RT A16WE 2007051000027 20070510 00027 NM 2007 5 10 CALA0700235 1 20070505 A 5330 6545800 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17329 23459 INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT THE AFT LOWER CORNER OF THE R-1 DOOR CUTOUT, STA 328, S18R. REPAIR ED IAW SRM 53-10-01. A DIP WAS ISSUED TO INSPECT THE REPAIR WITHIN 60,000 FLIGHT HOURS AFTER REPAIR ACCOMPLISHMENT. 2 L 7 2 4F RT A16WE 2007051000029 20070510 00029 NM 2007 5 10 CALA0700237 1 20070425 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 INSPECTION FOUND TWO SMALL CRACKS ON THE OUTBOARD FLANGE OF THE LBL 45 LONGITUDINAL FLOORBEAM JUST FORWARD OF STA 727B. REPAIRED IAW ECRA 5311-01316. 2 L 7 2 4F RT A16WE 2007051000032 20070510 00032 NM 2007 5 10 SWAA072297 1 20070507 A 5524 REP4HE8 BEARING BOEING 737 7373G7 1384595 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, LEFT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BEARING AND BUSHING PER MM. 2 L 7 2 4F RT A16WE 2007051000033 20070510 00033 NM 2007 5 10 SWAA072298 1 20070507 A 5524 REP4HE8 BEARING BOEING 737 7373G7 1384595 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, RIGHT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BEARING AND BUSHING PER MM. 2 L 7 2 4F RT A16WE 2007051000034 20070510 00034 NM 2007 5 10 SWAA072291 1 20070507 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED BRDG CHECK, FOUND RIGHT FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2007051000035 20070510 00035 NM 2007 5 10 SWAA072290 1 20070507 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED BRDG CHECK, FOUND LEFT FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2007051000036 20070510 00036 NM 2007 5 10 SWAA072301 1 20070507 A 2560 PH22300L GLOWSTRIP BOEING 737 7375H4 138449D NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED MV2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN BETWEEN ROW 4 DEF AND ROW 6 DEF. REMOVED AND REPLAC ED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007051000037 20070510 00037 NM 2007 5 10 SB07037 1 20070507 A 2170 V1211 COALESCER BAG BOEING 737 737301 1384611 NM A/C BAY DIRTY A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 EA 19 588US 23933 BWI FLT 1853 - ON TAKEOFF FROM PHL, EN ROUTE TO BWI, CREW REPORTED A NAUSEATING SMELL IN THE COCKPIT FROM THE AIR CONDIT IONING SYSTEM. SMELL REMAINED DURING FLIGHT AND LANDING. MAINTENANCE OPERATED EACH PACK FOR 30 MINUTES AND DETECTED A STALE ODOR FROM THE AIR VENTS IN THE COCKPIT. REMOVED AND REPLACED LEFT AND RIGHT COALESCER BAGS PER MM 21-51-41. GROU ND OPERATED PACKS OFF APU. NO ODORS NOTED. 2 L 7 2 4F RT A16WE 2007051000040 20070510 00040 NM 2007 5 10 USAA070364 1 20070508 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 RBL 49 FS 947-967 HAS CORROSION. REMOVED & REPLACED INTERCOSTAL PER SRM 53-60-51; CORR TASK C53-107-02; LEVEL 2, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007051000044 20070510 00044 NM 2007 5 10 USAA070360 1 20070508 A 5313 STRINGER BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 STA 639 AT STR 4R HAS CRACK. REMOVED & REPLACED PER SRM 51-20-00, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007051000045 20070510 00045 NM 2007 5 10 BB07036 1 20070505 A 2432 425402M0D1 CHARGER BOEING 767 767201 1385125 NM MAIN BATTERY FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 249AU 63342 477 23901 FLIGHT 740, PHL-MAD: DURING CRUISE, CREW RECEIVED A MAIN BATTERY CHARGER FAULT MESSAGE. FLIGHT RETURNED TO PHL. MAINT ENANCE REPLACED THE BATTERY CHARGER. NO FURTHER FAULTS. 2 L 7 2 4F RT A1NM 2007051000048 20070510 00048 2007 5 10 UPS07649774 4 20070508 A 2310 HF COMM BOEING 767 76734AF 1385212 NM COCKPIT INOPERATIVE A IPXA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SO 01 307UP 27760 INSPECTION TYPE:ETOP TAT = 29498 TAC = 9308 DIVERSION - RECEPTION AND TRANSMISSION ON BOTH HF INOP. ACCOMPLISHED RADIO OPERATIONAL CHECK ON BOTH HF'S PER MM23-11-00-5. OPS CHECK OK. 2 L 7 2 4F RT A1NM 2007051000049 20070510 00049 WP 2007 5 10 UPS07849761 1 20070414 A 5313 SAA3779658502 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 855 L10R. REMOVED AND REPLACED LONGERON END FITTING IAW SRM 51-1 -20D, 51-1-21, AND 51-3-0. 2 L 7 4 4F RT 4A25 2007051000050 20070510 00050 WP 2007 5 10 UPS07849763 1 20070417 A 5711 SAA3644046501 BRACKET DOUG DC8 DC873F 302199F WP WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 LOWER FRONT SPAR CAP BRACKET IS CRACKED IN 2 PLACES BETWEEN XRS 463-428 NR 1 ALT. REMOVED, FABRICATE D AND INSTALLED BRACKET IN NR 1 ALT TANK IAW SRM 51-01-20D, 51-03-02, AND DWG 76335150001. 2 L 7 4 4F RT 4A25 2007051000051 20070510 00051 WP 2007 5 10 UPS07849765 1 20070412 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 L1 DOOR CUTOUT HAS RIVET WITH NO ED AT LWR HINGE CUTOUT. REMOVED, FABRICATED, AND INSTALLED L1 DOOR JAMB FRAME IAW SRM 51-1-21, 0D, 51-03-02,51-1-8,51-01-14, AND 51-3-0. 2 L 7 4 4F RT 4A25 2007051000052 20070510 00052 WP 2007 5 10 UPS07849772 1 20070508 A 3350 5708458 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. EMERGENCY EXIT BATTERY PACK REPLACED AND TESTED IAW AMM 30-50-01-2. OP S CHECK GOOD. 2 L 7 4 4F RT 4A25 2007051000053 20070510 00053 WP 2007 5 10 UPS07849775 1 20070504 A 3350 LIGHT DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:N/A TWO EMERGENCY LIGHTS AT MAIN CREW ENTRY DOOR INOP. RELAMPED INOP EMERGENCY LIGHTS PER MM 33-01-00. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2007051000054 20070510 00054 WP 2007 5 10 UPS07849776 1 20070508 A 7100 ENGINE DOUG DC8 DC871F 302199D WP CFMINT CFM56 CFM562AFR 13802 EU NR 3 FLAMED OUT A IPXA B EMER. DESCENT X ENGINE FLAMEOUT CR CRUISE 1 SO 01 701UP 45938 692422 INSPECTION TYPE:AS-E AT FLIGHT LEVEL 360 NR 3 ENGINE FLAMED OUT. RAN FLAME OUT CHECKLIST & RESTART IN FLIGHT CHECKLIST WHILE DESCENDING TO FLIGHT LEVEL 240 RESTART SUCCESSFUL OPERATED NORMALLY REMAINDER OF FLIGHT. PERFORMED ENGINE FLAME-O UT T/S REF MM 71-00-00-1 FIG 139. NO SIGNIFICANT FINDINGS. PERFORMED HI POWER RUN W/BOOST & FEED PUMP OFF. EDP OPERAT ES NORMALLY. OK FOR SERVICE. 2 L 7 4 4F 4 F RT 4A25 E21EU 2007051000055 20070510 00055 NM 2007 5 10 UPS07M49768 1 20070404 A 5744 HINGE DOUG MD11 MD11F 3023600 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C RIGHT WING O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT FOUND CORRODED. CORROSION REMOVED FOUND EXC EED LIMIT CMM57-44-08PG602-607R57. FPI C/O DACNDTSP RACK EVIDENT. RWK AREA ETCH INSP SATIS BSOPM20-11-01R57. FLAP PEEN ING C/O BSOPM20-11-01R57. CAD PL BSOPM20-10-01R57. BUSHINGS FAB CMM57-44-0 8R57. HEAT TREAT DPS5.00-2 HRC 41.7 DPS1.0 5-5. MPI C/O NO CRACK. CAD P L BSOPM20-10-01R57. BUSHING & SHIM INSTL PER CMM57-44-08. 2 L 7 3 4F RT A22WE 2007051000056 20070510 00056 NM 2007 5 10 UPS07M49769 1 20070319 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C MID CABIN-SEAT TRACK CROWN CORROSION AT SEVERAL LOC AS MARKED FROM STA 745 TO STA 1129 RBL 8.5. CORR ON S/TRACK CROWN STA 879 RBL 8.5" RMV SRM 51-21-01VIIR38 ORI THK 0 .145" MATL RMV 0.025" MATL RMD 0.070" OUT OF LIMIT SR M 53-70-00 FIG 3VIR 38. S/TRACK TRIM OFF SRM 53-70-00 FIG 1 VIR38. HFEC INSP C/O DACNDTSPMR13 06-10-01.001 NO CRACK. S/TRACK & SPLICE RWK SRM 53-70-00 FIG 1 VIR38. PAINT RWK AREA SRM 51-21-01VIIR38. INSTL S/TR SRM 51-31-01 & 51-33-01VI IR38. 2 L 7 3 4F RT A22WE 2007051000057 20070510 00057 NM 2007 5 10 UPS07M49770 1 20070319 A 5350 SUPPORT ANGLE DOUG MD11 MD11F 3023600 NM TAIL CONE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C TAIL CONE ACCESS PANEL SUPPORT ANGLE RIGHT DENTED. SUPPORT DENTED AREA SMOOTHED & MEASURED D/Y 0.75"X 0.040"=18.75 BEYOND LIMIT SRM 51-80-01VIIR38. SUPPORT ANGLE FAB BOEING DWG AKC7546. HEAT TREAT PER DPS 7.00-1 & HARDNE SS VALUE HRB 58.5 PER DPS 1.05-3. HOLES TRANSFERRED SRM 51-35-01VIIR38. NEW SUPPORT TREAT & PAINT SRM 51-21-01VIIR38. INSTL PER SRM 51-35-01VIIR38. 2 L 7 3 4F RT A22WE 2007051000058 20070510 00058 EU 2007 5 10 UPS07149760 1 20070506 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 152UP 0835 INSPECTION TYPE:N/A CTR GLARESHIELD EMERGENCY LIGHT 91LE INOP. RELAMPED CTR GLARESHIELD LIGHT 91LE. OPS CHECK GOOD PER 33-12-00-09. 2 L 7 2 4F RT A35EU 2007051000059 20070510 00059 SO 2007 5 10 C2XA07RI028 1 20070506 A 2611 FDS765A2 SMOKE DETECTOR EMB 135 EMB135ER 3260203 SO LAVATORY DEFECTIVE A C2XA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SW 27 27512 7846 5847 145274 FLT 2214 - EWR - CREW REPORTED GATE RETURN FOR A SECOND TIME DUE TO LAV SMOKE FALSE ALARM. FIRST TIME SYSTEM WAS RESET. EWR MX REMOVED AND REPLACED LAV SMOKE DETECTOR IAW EMB 135 AMM 26-14-01. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007051000060 20070510 00060 GL 2007 5 10 C2XA07RI026 2 20070504 A 7200 UNKNOWN EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL NR 1 ENGINE SMOKE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 12142 145735 CAE312328 FLT 2496 - EWR - CREW REPORTED ENGINE NR 1 SMOKE COMING OUT FROM THE EXHAUST AND CONTINUING FOR 15 MINUTES AFTER SHUT DO WN ON TAXI IN. EWR MX PERFORMED OPERATIONAL CHECK OF NR 1 ENGINE (HIGH POWER RUN) AND COULD NOT DUPLICATE THE PROBLEM. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F 4 F RT TE6CH 2007051000061 20070510 00061 NM 2007 5 10 UPS07549752 1 20070403 A 5311 146N103072 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 414UP 23854 INSPECTION TYPE:C DENTS IN AFT CARGO FUSELAGE FRAME 1540, BETWEEN S25R-S26R (2EA). ACCOMPLISHED ON FINAL EA 757-5362-27 -A1645 AND UPS B757-5310-26662. 2 L 7 2 4F RT A2NM 2007051000062 20070510 00062 NM 2007 5 10 UPS07549753 1 20070403 A 5311 143N102489 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 414UP 23854 INSPECTION TYPE:C DENT IN FORWARD CARGO FUSELAGE FRAME STA 720, S24L. REMOVED DAMAGED AREA L 1.200X W 1.160 PER EA 757- 5362-27-A1652. NDT ON REWORK AREA IAW NTM 51-00-00 PTG NO CRACKS NOTED. PERFORM. 040" INSURANCE CUT L 1.32" X 1.200 PE R EA 757-5362-27-A1652. FABRICATED REPAIR ANGLE 071" THICK, 7075-O CLAD, BATCH 53268, TR/T2/673463. ACCOMPLISHED ON FI NAL EA 757-5362-27-A1652 AND UPS B757-5310-26673 2 L 7 2 4F RT A2NM 2007051000063 20070510 00063 NM 2007 5 10 UPS07549754 1 20070403 A 5311 146N103069 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 414UP 23854 INSPECTION TYPE:C DENTS IN AFT CARGO FUSELAGE FRAME STA 1480, BETWEEN S25L AND 26L (2EA). ACCOMPLISHED ON FINAL EA 757- 5362-27-A1644 AND UPS ENG B757-5310-26669-A. 2 L 7 2 4F RT A2NM 2007051000064 20070510 00064 NM 2007 5 10 UPS07549755 1 20070403 A 5311 146N103097 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 414UP 23854 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1560, S26L. ACCOMPLISHED ON FINAL EA 757-5362-27-A1647 AND UPS 7 57-5310-26668-A. 2 L 7 2 4F RT A2NM 2007051000065 20070510 00065 NM 2007 5 10 UPS07549756 1 20070403 A 5311 143N10242 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 414UP 23854 INSPECTION TYPE:C DENTS IN FORWARD CARGO FUSELAGE FRAME STA 820, BETWEEN S22R AND S24R (2EA). REMOVED DAMAGE 2 PLACES U PPER L=1.0" W=1.160" LOWER 1.400 W=1.160 IAW EA757-5362-27-A1651. NDT ON REWORK AREA IAW NTM 51-00-00 PT.6 NO CRACKS NO TED. ENLARGED THE TRIM OUT BY .04" ON 2 PLACES UPPER L=1.04" W=1.2 PER EA 757-5362-27-A1651 STEP 3. ACCOMPLISHED ON FI NAL EA 757- 5332-27-A1651 AND UPS B757-5310-26677-A. 2 L 7 2 4F RT A2NM 2007051000066 20070510 00066 NM 2007 5 10 UPS07549757 1 20070403 A 5311 146N102886 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 414UP 23854 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1340, BETWEEN S25L AND S26L. TRIMMED OUT DAMAGE AREA 1.56"W X 0. 96"L IAW EA 757-5362-27-A1650. PRELIMINARY 1 STEP 1. HFEC AREA PER NTM 51-00-00 PT6. NO CRACK INDICATIONS NOTED. TRI MMED OUT .040" AROUND UCT FINAL DIMENSION 1.6"W X 1.00"L. REMOVED 2EA STRINGER CLIPS, 1 EA SPLICE IAW EA 757-5362-27-A 1650. ACCOMPLISHED ON FINAL EA757-5362-27-A1650 AND UPS B757-5310-2667. 2 L 7 2 4F RT A2NM 2007051000067 20070510 00067 NM 2007 5 10 UPS07649759 1 20070503 A 3350 SWITCH BOEING 767 76734AF 1385212 NM COCKPIT DEFECTIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 330UP D00118 27756 INSPECTION TYPE:N/A THE EMERGENCY EXIT LIGHT SWITCH DOES NOT RETURN TO THE ARMED POSITION WHEN THE SWITCH CAP IS CLOSED. REMOVED AND REPLACED EMERGENCY LIGHT PANEL ASSY IAW AMM 33-50-00. OPS CHECKS OK. 2 L 7 2 4F RT A1NM 2007051000111 20070510 00111 NM 2007 5 10 SWAA072337 1 20070508 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007051000112 20070510 00112 NM 2007 5 10 SWAA072338 1 20070508 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007051000113 20070510 00113 NM 2007 5 10 SWAA072327 1 20070508 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007051000114 20070510 00114 NM 2007 5 10 SWAA072348 1 20070508 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 416WN 32453 DURING SCHEDULED SPV CHECK, FOUND LEFT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007051000115 20070510 00115 NM 2007 5 10 SWAA072324 1 20070508 A 5313 BAC1498 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, FOUND STRINGER 26R CORRODED AT BS 540. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007051000116 20070510 00116 NM 2007 5 10 USAA070368 1 20070509 A 5210 507945178 SKIN BOEING 737 737401 1384701 NM DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 FWD & AFT OK NR 5 STOP PIN ACCESS HOLE ON AFT SIDE OF TORQUE BOX HAS CRACK. INSTALLED EXTERNAL DOUBLER PER TYP REP 52-1 0-16, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007051000117 20070510 00117 NM 2007 5 10 USAA070367 1 20070509 A 5753 65C263101A WEDGE BOEING 737 7374B7 1384702 NM T/E FLAP WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 441US 24812 WEAR MARKS LEFT INBOAD MID FLAP TRAILING EDGE WEDGE, UNDERSIDE 34 INCHES FROM I/B END. INSTALLED BONDED REPAIR DOUBLER PER EA 98647, DEFECT SIZE: 6 INCHES. 2 L 7 2 4F RT A16WE 2007051000119 20070510 00119 EA 2007 5 10 TRAX200700625 1 20070505 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 CORROSION ON FLOOR SUPPORT STRUCTURE CAP SPLICE AT FS 559.00 + 80 FROM LBL 45 TO RBL 45. CORROSION ON FLOOR SUPPORT STR UCTURE CAP PLICE AT FS 559.00 +80 FROM LBL 45 TO RBL 45. REMOVED AS PER SRM 51-21-06 AND BLENDED AREA. TREATED AS PER SRM (51-21-11)(51-25-06). PAINT APPLED AS PER SRM 51-25-01. MATERIAL THICKNESS .100, MATERIAL REMOVED .005, WITHIN LIM ITS AS PER SRM 53-00-00 (FIG 101) 2 L 7 2 4F RT A21EA 2007051000120 20070510 00120 EA 2007 5 10 TRAX200700626 1 20070505 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 RIGHT SILL CORRODED BETWEEN FS 559.00 + 80 TO 559.0 +112. 2 L 7 2 4F RT A21EA 2007051000121 20070510 00121 EA 2007 5 10 TRAX200700627 1 20070505 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 CORROSION ON FLOORBEAM BETWEEN FS 559.00 + 80 TO FS 559.00 + 112 RBL 9. [SUP 05-22-07] CORROSION ON FLOOR BEAM BTWN FS 559.00+80 TO FS559.00+112 RBL 9 REMOVED IAW SRM 51-21-06. FOUND BEYOND LIMITS IAW SRM 53-51-43 FIG. 101. REPAIR PREFOR MED IAW SRM 53-00-43 REPAIR NR 1. 2 L 7 2 4F RT A21EA 2007050800237 20070508 00237 WP 2007 5 8 DHL2007806555 1 20070408 A 5730 SKIN DOUG DC8 DC873F 302199F WP RWS 526 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 RT WING CTR L/E LOWER SKIN HOLES ELONGATED STA XFS 526.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 D ATED 04-06-07, ENGINEERING VARIATION AUTHORIZATION NR D857-00006 REV IR DATED 03-28-07. REMOVED FASTENERS IAW SRM 51-1- 21. FABRICATED REPAIR DOUBLER (AL7075T6 0.071") IAW ASTAR DWG NR ESD85700006-001-D. PERFORMED NDT INSPECTION IAW DACO DPS 4.707-1. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF REPAIR DOUBLER IAW SRM 51-1-8B. APPLIED SEALANT TO FAY ING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR DOUBLER IAW ASTAR DWG NR ESD85700006-001-D, SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007050800238 20070508 00238 WP 2007 5 8 DHL2007806559 1 20070410 A 5340 47516431 FITTING DOUG DC8 DC873F 302199F WP BS 742 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT FITTING CRACKED 0.500" STA 742.250 L-13R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 PG 2A (TORQUE). REFER TO JC EA-002 52-001 (WO 470) FOR FITTING FABRICATION. 2 L 7 4 4F RT 4A25 2007050800239 20070508 00239 WP 2007 5 8 DHL2007806561 1 20070410 A 5340 37798741 FITTING DOUG DC8 DC873F 302199F WP BS 834 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 FOUND MAIN CARGO COMPT FITTING 0.500" CRACKED STA 834.500 L-18R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TR EATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 PG 2A (TORQUE) REFER TO JC EC -00245-001 (WO 470) FOR FITTING FABRICATION. 2 L 7 4 4F RT 4A25 2007050800240 20070508 00240 WP 2007 5 8 DHL2007806602 1 20070417 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1490-1520 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 AFT CARGO COMPT L-24R CRACKED 1" (STA 1490.000 - 1520.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DAT ED 04-17-07, BOEING MESSAGE3 1-299391776-2 DATED 03-14-07 AND NR 1-316315027-2 DATED 04-17-07. REMOVED FASTENERS IAW SR M 51-1-21. CUT OUT DAMAGED LONGERON SEGMENT IAW SRM 53-2-2 FIG 4A. FABRICATED NEW LONGERON SEGMENT (EXTRUSION P/N S259 7424) IAW BOEING MESSAGE NR 1-299391776-2 AND SPLICE (EXTRUSION P/N S2641454) IAW BOEING MESSAGE NR 1-316315027-2, SRM 5 3-2-2 FIG 10 SHEET 1-3, TR NR 56-153 DATED 12-10-02, SRM 53-2-2 FIG 10 SHEET 4 TR NR 53-193 DATED 03-15-04, SRM 51-2-0 F IG 50. NDT INSPECTED SPLICE IAW SRM 53-2-2 FIG 10 NOTE 22, DC8 NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIME 2 L 7 4 4F RT 4A25 2007050800241 20070508 00241 WP 2007 5 8 DHL2007806527 1 20070404 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 902 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT AFT FITTING CRACK 1" STA 902 125 L-19R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AN D PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 PG 2A. 2 L 7 4 4F RT 4A25 2007050800243 20070508 00243 WP 2007 5 8 DHL2007806569 1 20070412 A 5340 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 STRUCTURE UNDER "A" CROSS-SLIDE CARGO DOOR, FITTING CRACKED 0.500" STA 320.000 L-27L. REMOVED CRACKED FITTING IAW SRM 5 1-1-20D. CUT OUT NEW FITTING AND FABRICATED REPAIR ANGLE (7075T6511 0.125") IAW SRM 53-2-0 FIG 2D. CLEANED, TREATED AN D PRIMED AREA AND REPAIR ANGLE IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-11. INSTALLED REPAIR AN GLE AND FITTING IAW SRM 53-2-0 FIG 2D, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050800244 20070508 00244 WP 2007 5 8 DHL2007806570 1 20070415 A 5340 27799782 FITTING DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 FOUND MAIN CARGO COMPT FITTING CRACKED 0.750" STA 759.000 L-18R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TR EATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 PG 2A (TORQUE). REFER TO JC EC-00246-001 (WO 470) FOR FITTING FABRICATION. 2 L 7 4 4F RT 4A25 2007050800245 20070508 00245 WP 2007 5 8 DHL2007806579 1 20070417 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 1040 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT FRAME FITTING HAS A MISDRILLED HOLE STA 1040.000 L-20L TO L-21L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED DAMAGED FITTING IAW SRM 53-1-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLI ED SEALANT TO FAYING SURFACE IAW SRM 51-1-11. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050800246 20070508 00246 WP 2007 5 8 DHL2007806540 1 20070410 A 5720 ANGLE DOUG DC8 DC873F 302199F WP LWS 527 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 NR 1 STUB WING FORMER ANGLE CRACKED STA XS 527.000. REMOVED CRACKED ANGLE IAW SRM 51-1-21. FABRICATED NEW ANGLE (7075" 0" 0.080") IAW DOUGLAS DWG NR 9753297. HEAT TREATED ANGLE FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-17. CLEANED, T REATED AND PRIMED AREA AND NEW ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007050800248 20070508 00248 WP 2007 5 8 DHL2007806500 1 20070315 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1550-1560 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 UPPER CARGO COMPT FLOOR PANEL UPPER SKIN CORRODED (STA 1550.000 - 1560.000) RBL 51" - 54". REMOVED CORROSION FRONT FLOO R PANEL UPPER SKIN (STA 1550.000 - 1560.000) IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OU T FLOOR PANEL DAMAGED SEGMENT AND FABRICATED FILLER (ALCLAD 7075T6 0.071") AND DOUBLER (ALCLAD 7075T6 0.080") IAW SRM 53 -2-3 PG 39-40. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLER IAW SRM 53-2-3 PG 39-40, SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007050800249 20070508 00249 WP 2007 5 8 DHL2007806541 1 20070409 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 1220 L35-36R CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 "C" CARGO DOOR JAMB FITTING CORRODED STA 1220.000 L-35R TO L-36. REMOVED CORROSION FROM "C" CARGO DOOR JAMB FITTING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FITTING IAW SRM 51-1-20D. CUT OUT NE W FITTING AND FABRICATED REPAIR ANGLE (AL7075T6 511 0.125") IAW SRM 53-2-0 FIG 2D. CLEANED, TREATED AND PRIMED AREA AND REPAIR ANGLE IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-11. INSTALLED REPAIR ANGLE AND FITTING I AW SRM 53-2-0 FIG 2D, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050800250 20070508 00250 WP 2007 5 8 DHL2007806598 1 20070419 A 5740 48888592 FITTING DOUG DC8 DC873F 302199F WP RWS 25 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 NR 4 MAIN TANK FITTING CRACKED STA XRS -255.000 S-51. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND P RIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). FOR FITTING FABRICATION SEE J C EC-00293-001 (WO 470). 2 L 7 4 4F RT 4A25 2007050800251 20070508 00251 WP 2007 5 8 DHL2007806578 1 20070417 A 5320 56434332 ANGLE DOUG DC8 DC873F 302199F WP BS 857 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 RT MLG W/W REAR SPAR WEB ANGLE CORRODED AT STA 857.125 RBL 45". REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT O F LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED ANGLE IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8 B. INSTALLED NEW ANGLE IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE) REFER TO JC EC-00261-001, DWG NR 5643433 FOR ANGLE FABRICA TION. 2 L 7 4 4F RT 4A25 2007050800252 20070508 00252 NM 2007 5 8 DLM88070465 1 20070413 A 5310 DOOR FRAME DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 945DL 49818 CARGO DOOR JAMB BEAM REPAIR - CORROSION ON BOTTOM OF AFT CARGO COMPARTMENT DOOR JAMB BEAM BETWEEN STA 1175 AND 1195. CO RROSION REMOVED AND PERMANENT REPAIR INSTALLED PER SRM 53-05, FIG 63. 2 L 7 2 4F RT A6WE 2007050800253 20070508 00253 NM 2007 5 8 DLM88070466 1 20070413 A 5524 5919752505 BALANCE WEIGHT DOUG MD88 MD88 3023688 NM LT ELEVATOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 945DL 49818 EXFOLIATION CORROSION ON BALANCE TIP OF LEFT ELEVATOR INBOARD FACE. PERMANENT REPAIR ACCOMPLISHED BY REPLACING THE BALA NCE TIP FOLLOWING INSTRUCTIONS AND RECOMMENDATIONS CONTAINED IN DWG 5910412. 2 L 7 2 4F RT A6WE 2007050900006 20070509 00006 WP 2007 5 9 DHL2007806542 1 20070409 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP BS 1665 L25-26L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 AFT ACCY COMPT INTERNAL DOUBLER CORRODED, STA 1665.000 L-25L TO L-26L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FO RM 8110-3 DATED 04-05-07, DWG NR AD08-53-101 REV IR DATED 03-30-07. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND O UT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT DAMAGED SECTION AND FABRICATED EXTERNAL REPAIR DOUBLER (AL7075T6 0.063") AND SHIM (AL7075T6 0.032") IAW DWG AD08-53-101. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTAL LED REPAIR PARTS IAW DWG NR AD08-53-101, SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007050900019 20070509 00019 WP 2007 5 9 DHL2007806512 1 20070402 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 717 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT BELOW CABIN FLOOR FITTING CRACKED STA 717.750 RBL 22". REMOVED AND REPLACED CRACKED FITTING IN MAIN CA RGO COMPT STA 717.750 RBL 22" IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050900022 20070509 00022 WP 2007 5 9 DHL2007806520 1 20070402 A 5542 SKIN DOUG DC8 DC873F 302199F WP RUDDER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 LT RUDDER EXT SKIN DENTED AT STA ZR 188.781 AND CRACKED 1" AT STA ZR 198.844 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PANEL PLATING (PLATI NG AND BONDED DOUBLER, BOTH FROM AL 2024T3 0.016") IAW SRM 55-6-1 FIG 1 PG 2 ITEM 1. BONDED BOTH PARTS WITH HYSOL IAW S RM 51-1-9. CLEANED, TREATED AND PRIMED AREA AND NEW PANEL PLATING IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE I AW SRM 51-1-11. INSTALLED NEW PANEL PLATING IAW SRM 51-1-21. REFER TO NR 075840 FOR BALANCING. 2 L 7 4 4F RT 4A25 2007050900025 20070509 00025 NM 2007 5 9 EIA2007071 1 20070408 A 3350 S1356B37 LIGHT BOEING 747 747273C 1384896 NM CABIN INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 471EV 20651 UPPER DECK LEFT HAND SIDE ABOVE EMERGENCY EXIT CEILING LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER AMM 32-51-00 OPS CKD GOOD. 2 L 7 4 4F A20WE 2007050900033 20070509 00033 NM 2007 5 9 EIA2007064 1 20070321 A 5210 SKIN BOEING 747 747132 1384882 NM R1 DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 R1 DOOR OUTER SKIN CRACKED AT AFT LOWER CORNER. CUTOUT DAMAGED AREA, FABBED AND INSTALLED DOUBLER AND FILLER PER B747 S RM 52-00-03 FIG 4 PAGES 5-6C AND 51-30-02 PAGES 8-9. 2 L 7 4 4F A20WE 2007050900040 20070509 00040 WP 2007 5 9 DHL2007806588 1 20070417 A 5522 SKIN DOUG DC8 DC873F 302199F WP RT ELEVATOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 RT ELEVATOR LWR SKIN DEFLECTED (STA XE 222.875 - 228.031) DAMAGED (MAJOR REPAIR) DAMAGED BY SEMAN (SEE ACCIDENT REPORT). PERFORMED MAJOR REPAIR IAW SRM 55-4-1 FIG 1 SHEET 1, 2 PG 2, 3. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SR M 51-1-21. FABRICATED NEW PANEL PLATING: SKIN AND FINGER DOUBLER BOTH FROM AL2024T3 0.016" IAW SRM 55-4-1 FIG 1 SHEET 1 , 2 PG 2, 3 ITEM "E" "F". BONDED BOTH PARTS IAW SRM 51-1-9 TR NR 51-142 DATED 04-05-06, SRM 51-1-9A, TR NR 51-141 DATED 04-03-06. CLEANED, TREATED AND PRIMED AREA AND NEW PANEL PLATING IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED NEW PANEL PLATING IAW SRM 51-1-21, SRM 51-3-0 (TORQUE) BETWEEN STA XE 132.000 AND 246.000. 2 L 7 4 4F RT 4A25 2007050900042 20070509 00042 WP 2007 5 9 DHL2007806524 1 20070402 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 717 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT BELOW CABIN FLOOR FITTING CRACKED STA 717.750 RBL 22". REMOVED AND REPLACED CRACKED FITTING IN MAIN CA RGO COMPT STA 717.750 RBL 22" IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007050900050 20070509 00050 WP 2007 5 9 DHL2007806563 1 20070410 A 5340 47504221 FITTING DOUG DC8 DC873F 302199F WP BS 857 L19R CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 MAIN CARGO COMPT FITTING CRACKED 0.500", STA 857.125 L-19R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 PG 2A (TORQUE). REFER TO JC EC-00 260.001 (WO 470) FOR FITTING FABRICATION. 2 L 7 4 4F RT 4A25 2007050900051 20070509 00051 NM 2007 5 9 EIA2007089 1 20070413 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE DEBONDED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 FOUND FUSELAGE SKIN FWD OF STA 2460 BETWEEN 17L AND 18L DISBONDED APPROX 2"X". REPAIR CARRIED OUT PER N482EV-07-0006(SR M53-30-04 FIG 3)APPROVED PER BOEING MESSAGE 1-310403476-4. 2 L 7 4 4F A20WE 2007050900054 20070509 00054 NM 2007 5 9 TSAA0729017 1 20070426 A 2917 3141602 REGULATOR BOEING 737 737236 1384476 NM HYD SYSTEM UNKNOWN A TSAA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 WP 13 828AL 12456 23051 FLT 107 HNL-LIH - LOUD FLUTTER HEARD ON ROTATION. CONTINUED TO 2000 FT. RETURNED FOR LANDING. AIRCRAFT TAXIED TO GATE AT HNL WITHOUT FURTHER INCIDENT. VISUALLY INSPECTED AIRCRAFT, WING TO BODY FAIRINGS, AND FLIGHT CONTROLS. NO DEFECTS NOTED. REMOVED AND REPLACED HYDRAULIC HEAD PRESSURE REGULATOR. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007050900057 20070509 00057 EU 2007 5 9 F3LA200700107 1 20070425 A 5315 D5347207500100 FLOORBEAM AIRBUS A318 A318111 3940019 EU FUSELAGE DAMAGED A F3LA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 03 801FR 4759 1939 DURING C-3 CHECK, INSPECTION REPORTED FWD SPLICE OF R2 DOOR SILL HAD TWO DOUBLE DRILLED HOLES, ONE COMPLETELY THROUGH TH E FWD FLOORBEAM. REPLACED DAMAGED FLOORBEAM IAW SRM 51-42-11. 2 L 7 2 4F RT 2007050900059 20070509 00059 NM 2007 5 9 EIA2007081 1 20070316 A 5711 SPAR BOEING 747 747212B 1384886 NM LT WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 CORROSION FOUND AT TOP CHORD ASSY AT LT WING IN FRONT OF SPOILER NR 5 & NR 6. BEAM ASSY UPPER "T" CHORD REMOVED FROM WB L 285-WBL345. FABRICATED AS PER SRM 51-40-04 FIG 3. REPAIR CARRIED OUT PER B747 SRM 51-40-04 FIG 3. 2 L 7 4 4F A20WE 2007050900061 20070509 00061 NM 2007 5 9 ASMF200705003 1 20070504 A 2910 LINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE HYD SYSTEM LEAKING W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 169PL 53175 DURING TRANSIT CHECK, A LOW HYDRAULIC LEVEL WAS DETECTED IN THE LT SYSTEM WITH AN INDICATION OF 6 QUARTERS. DURING MAINT ENANCE INSPECTION, THE LEAK WAS CONFIRMED IN THE LT MAIN WHEEL WELL, SO AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERN IGHT CHECK, HYDRAULIC LINE AND TEE WERE REPLACED IAW MM 20-10-13, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007050900073 20070509 00073 NM 2007 5 9 EIA20070073 1 20070405 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 NOSE GEAR WELL STA 340, LEFT WL 150 FOUND BASE AND HOLES DAMAGED 1/2" BY 1/2" BEYOND SRM 53-10-01 PAGE 3 FIG 1 LIMIT. C HORD FABRICATED BY WORKSHOP INSTALLED PER BOEING 747 SRM 51-30-02. 2 L 7 4 4F A20WE 2007050900106 20070509 00106 SO 2007 5 9 SIMA200712815 1 20070501 A 5315 13500437001 FLOORBEAM EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 810AE 13175 4800 145525 RIGHT OMEGA BEAM INBOARD SIDE CORRODED BETWEEN FRAME 24 AND FRAME 25. REMOVED AND REPLACED OMEGA BEAM IAW EMB SRM 51-40 -02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050900116 20070509 00116 SO 2007 5 9 SIMA200712805 1 20070501 A 5315 13500428401 FLOORBEAM EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 810AE 13175 4800 145525 LEFT OMEGA BEAM CORRODED AT FRAME 20 CROSSMEMBER, REPLACED PREVIOUS DOUBLERS IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050900129 20070509 00129 NM 2007 5 9 2007UALA01325 1 20070427 A 3397 CONNECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 847UA 1627 DOOR 1L FAILS EMERGENCY LIGHT TEST ON CIDS READS EPSU BATT EMERG L. CLEANED CONNECTOR AND RESET BATTERY PACK POWER SUPP LY AT LEFT OVERWING EXIT RETESTED EMERGENCY LIGHTS REF NR 3 SERVICE, TEST OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007050900139 20070509 00139 NM 2007 5 9 2007UALA01336 1 20070429 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 EXTERNAL FUSELAGE SKIN HAS A 4 INCH CRACK 13 INCHES AFT OF BS 927 JUST ABOVE STR 24L. [SUP 05-16-07] MAJOR REPAIR ACCO MPLISHED: CUT OUT DAMAGED AREA. FABRICATED & INSTALLED A EXTERNAL DOUBLER, TRIPLER, FILLER & STRAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007050900150 20070509 00150 NM 2007 5 9 2007UALA01351 1 20070427 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 STA 246 FLOORBEAM UPPER WEB CRACKED OUT OF LWR FASTENER AT LBL 21. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED D OUBLER REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050900161 20070509 00161 NM 2007 5 9 C1HA200795005 1 20070504 A 5720 PLENUM BOEING 727 727290 138408W NM WING CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 A/C RAM AIR PLENUM HAS SURFACE CORROSION ON NR 2 TANK LWR SKIN ABOVE LT PRIMARY HEAT EXCHANGER. BLENDED OUT CORROSION D AMAGE, MAT LOSS .050, ORIGINAL THK .225. FLUORESCENT DYE PENETRANT AREA, NO DEFECTS NOTED. TREATED AND PRIMED AREA IAW B727 SRM 51-10-2. RESTORED FINISH IAW B727 MM 51-20-151. 2 L 7 3 4F A3WE 2007050900167 20070509 00167 NM 2007 5 9 C1HA200795019 1 20070504 A 5313 STRINGER BOEING 727 727290 138408W NM BS 720C S15L CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 FOUND STR 15L CRACKED AT BS 720C. REPAIR STR 15L AT BS 720C IAW B727 SRM 53-10-3 FIG 5. 2 L 7 3 4F A3WE 2007050900176 20070509 00176 NM 2007 5 9 2007UALA01355 1 20070428 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 EEL STRIP ON SEAT 2E LOOSE. SECURED STRIP ON SEAT. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007050900182 20070509 00182 NM 2007 5 9 2007UALA01394 1 20070503 A 2197 CONNECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FAN DAMAGED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 831UA 1291 FLIGHT DIVERTED DUE TO THUNDERSTORMS. SMOKE IN COCKPIT. [06-26-07] FOUND BACKSHELL BROKEN ON BLOWER-FAN. BACKSHELL TE MPORARILY SECURED. REPLACED CONNECTOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007050900208 20070509 00208 SO 2007 5 9 CHQA200700013 1 20070501 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN & COCKPIT SMOKE A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 11 288SK 145461 FLIGHT 8288 - IAH-BRO - ON TAKEOFF THROUGH 2000 FEET THE FLIGHT CREW NOTICED AN UNUSUAL ODOR. LEVELED OFF AND IMMEDIATE LY RAN MEMORY ITEMS PER SMOKE IN CABIN. THE F/A CONFIRMED THE ODOR AND BY THE TIME QRH WAS RAN FOR SMOKE IN COCKPIT THE F/A CALLED UP AND REPORTED ODOR WAS GOING AWAY. F/A DID CHECK OF THE CABIN, REPORTING BACK THAT EVERYTHING IN THE BACK WAS NORMAL. AT THIS TIME THE FLIGHT CREW DECIDED TO CONTINUE CLIMB UP TO 15,000 FT. MASKS CAME OFF AND EVERYTHING WAS FUNCTIONING PERFECTLY NORMAL. ELECTED TO CONTINUE TO BRO BASED ON PAST EXPERIENCE OF UNUSUAL ODORS FROM AC PACKS BEFOR E THAT TURNED OUT TO BE NOTHING. TWENTY-FIVE MINUTES LATER IN FLIGHT AT FL260, EXPERIENCED A DISTINCT BURNING SMELL SHO 2 L 7 2 4T RT T00011AT 2007050900215 20070509 00215 SO 2007 5 9 C2XA07IA105 1 20070501 A 3222 1170C000002 STRUT EMB 145 EMB145LR 3260212 SO NLG LOW A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 13988 14681 14681 145265 IAH - FLIGHT 2887, THE CREW REPORTED A LANDING GEAR AIR GROUND FAILURE MESSAGE ON TAKEOFF. THE AIRCRAFT LANDED AT IAH W ITHOUT INCIDENT WHERE MAINTENANCE SERVICED THE NOSE LANDING GEAR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAF T WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007050900217 20070509 00217 SO 2007 5 9 C2XA07IA103 1 20070503 A 3350 78241 INVERTER EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15926 145005 IAH - DURING MAINTENANCE INSPECTION, THE NUMBER TWO AND THREE EMERGENCY EXIT FLOOR STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED , AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050900218 20070509 00218 SO 2007 5 9 C2XA07IA104 1 20070501 A 3397 744412 CONNECTOR EMB 145 EMB145XR 3260214 SO CABIN DISCONNECTED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14105 145649 IAH - FLIGHT 2110, DURING PREFLIGHT INSPECTION AN EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURE D THE CONNECTOR ON THE SIGN, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007050900220 20070509 00220 SO 2007 5 9 C2XA07IA108 1 20070505 A 3350 LIGHT EMB 145 EMB145XR 3260214 SO CABIN MALFUNCTIONED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 24103 145645 IAH - FLIGHT 2682, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENA NCE RESET THE EMERGENCY LIGHT SYSTEM, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007050900225 20070509 00225 NM 2007 5 9 SWAA072302 1 20070507 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 727SW 27859 DURING SCHEDULED 8Y CHECK, FOUND LEFT HORIZONTAL STAB LOWER SKIN CRACKED 12 INCHES FROM AFT SPAR, 27 INCHES FROM INBOARD EDGE. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007050900239 20070509 00239 NM 2007 5 9 SWAA072287 1 20070507 A 3397 8100022602 CONNECTOR BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 405WN 27893 EEPLS INOP AT ROW 1 ABC. SECURED LOOSE CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2007051000015 20070510 00015 EA 2007 5 10 TRAX200700615 1 20070504 A 5260 STEP CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 706EV 10054 SUSPECT CRACK ON ASD UNDER TOP STEP AFT SIDE (MARKED). [SUP 05-11-07] REMOVED AND REPLACED PANEL PER CRJ 700 SRM 51-42 -13. 2 L 7 2 4F RT A21EA 2007051000017 20070510 00017 EA 2007 5 10 TRAX200700618 1 20070504 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 706EV 10054 ASD OUTER HANDLE CRACKED. [SUP 05-14-07] REMOVED AND REPLACED HANDLE IAW CRJ 700 AMM 52-11-03. OPS CK GOOD IAW CRJ 70 0 MM 52-11-03 MS 23531. 2 L 7 2 4F RT A21EA 2007051000019 20070510 00019 EA 2007 5 10 TRAX200700623 1 20070504 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 SERVICE DOOR WON'T OPEN. 2 L 7 2 4F RT A21EA 2007051000022 20070510 00022 NM 2007 5 10 CALA0700230 1 20070504 A 5330 654576987 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17329 23459 INSPECTION FOUND FUSELAGE SKIN BENEATH NR 1 DME ANTENNA CORRODED AT STA 460, S29L. THE CORRODED SECTION OF SKIN WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW ECRA 5331-01305. A DIP WAS ISSUED TO REINSPECT THE REPAIR AT 60,000 FLIGHT CYCLES THEN EVERY 30,000 FLIGHT CYCLES THEREAFTER. 2 L 7 2 4F RT A16WE 2007051000026 20070510 00026 NM 2007 5 10 CALA0700234 1 20070504 A 5330 65558721 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17329 23459 INSPECTION FOUND A 1 INCH CRACK IN INNER SKIN FORWARD OF R-2 DOOR BETWEEN UPPER AND LOWER HINGES AT STA 950. THE INNER SKIN WAS REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007051000030 20070510 00030 NM 2007 5 10 SWAA072303 1 20070507 A 2560 PH22300L GLOWSTRIP BOEING 737 7373T5 1384608 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED BRDG CHECK, FOUND RIGHT MID CABIN EELS PHOTOLUMINESCENT STRIP WORN. REMOVED AND REPLACED EEPLS STRIP P ER MM. 2 L 7 2 4F RT A16WE 2007051000031 20070510 00031 NM 2007 5 10 SWAA072304 1 20070507 A 2560 PH22300L GLOWSTRIP BOEING 737 7373T5 1384608 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED BRDG CHECK, FOUND RIGHT AFT CABIN EELS PHOTOLUMINESCENT STRIP WORN. REMOVED AND REPLACED EEPLS STRIP P ER MM. 2 L 7 2 4F RT A16WE 2007051000039 20070510 00039 NM 2007 5 10 USAA070365 1 20070508 A 5322 SHEAR TIE BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 511AU 23594 ON SHEAR TIE, BS 986.5, BETWEEN S-26R & S-27L HAS CORROSION. REMOVED & REPLACED SHEAR TIE, & PORTION OF S-26R FOR ACCES S PER SRM 53-00-03; CORR LEVEL 2, DEFECT SIZE: 3" X 2". 2 L 7 2 4F RT A16WE 2007051000042 20070510 00042 NM 2007 5 10 USAA070362 1 20070508 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 BS 450, BL-0 HAS CRACK. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER SRM 53-30-19A, EA 98652, DEFECT SIZE: .0625. 2 L 7 2 4F RT A16WE 2007051000047 20070510 00047 NM 2007 5 10 UPS07549764 1 20070403 A 5311 146N103078 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 414UP 23854 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1500, S26R. ACCOMPLISHED ON EA 757-5362-27-A1648 AND UPS B757-53 10-26691-A. 2 L 7 2 4F RT A2NM 2007051000070 20070510 00070 WP 2007 5 10 UPS07849751 1 20070501 A 5330 9754944501 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:C2 INSPECTION FOUND PREVIOUS LWR CORNER REPAIR AT STA 1220 THE CUTOUT WAS TO CLOSE TO EDGE AND EXTENDS D OUBLER BEYOND NORMAL LENGTH. REMOVED AND REPLACED RIVETS WITH HI-LOKS AT C-3 DOOR LWR AFT CORNER IAW SAA EA 008-5330-01 -A0809 REV-A, UPS EO DC8-5330-26611-B, SRO 8530019, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007051000110 20070510 00110 NM 2007 5 10 SWAA072336 1 20070508 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007051000122 20070510 00122 EA 2007 5 10 TRAX200700628 1 20070505 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 CORROSION ON FLOORBEAM BETWEEN FS 559.00 + 80 TO FS 559.00 + 112 RBL 27. [SUP 05-15-07] CORROSION ON FLOOR BEAM BTWN F S 559.00 + 80 TO FS 559.00 +112 RBL 27 REMOVED AS PER 51-21-06. ALODINED, PRIMED AND PAINTED AS PER SRM 51-21-11. 2 L 7 2 4F RT A21EA 2007051000123 20070510 00123 EA 2007 5 10 TRAX200700629 1 20070505 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 ANGLE FS 280 LBL 9 TO RBL 9 CORRODED. [SUP 05-15-07] OUT OF LIMITS IAW SRM 53-11-15.ANGLE AT FS 280 LBL 9 TO RBL 9. R EMOVED AS PER SRM 51-42-06. INSTALLED ANGLE AT F/S 280 BL9 TO BR9 IAW SRM 51-42-21 ALSO SRM 51-42-13. 2 L 7 2 4F RT A21EA 2007051000127 20070510 00127 SO 2007 5 10 C2XA07IA111 1 20070503 A 3350 110049 CHARGER EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15926 145005 IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED SEVERAL EMERGENCY LIGHTS TO BE OUT. MAINTENANCE REMOVED AND REPLACE D THE NUMBER TWO EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007051000128 20070510 00128 SO 2007 5 10 C2XA07SH027 1 20070510 A 5320 FLOOR SUPPORT EMB 145 EMB145EP 3260221 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13936 145025 SHV - DURING C-CHECK LEFT OMEGA BEAM HAS CORROSION AT FR 20. MX REPAIRED CORRODED AREA AT FR 20 LEFT OMEGA BEAM IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 2007051000131 20070510 00131 SO 2007 5 10 C2XA07RI027 1 20070505 A 2697 CONNECTOR EMB 145 EMB145XR 3260214 SO FIRE DETECTION LOOSE A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 14116 145672 FLT 2868 - EWR - CREW REPORTED, -E2 FIRE DET FAIL-. ENGINE INDICATION NORMAL, MESSAGE APPEARED ABOVE FL 320 /OAT - 58 C . EWR MX FOUND CONNECTOR LOOSE (P0915). MX RESECURED PLUG AND PERFORMED OPERATIONAL CHECK OF THE SYSTEM IAW EMB 145 AM M 26-10-00. OPERATIONAL CHECK SUCCESSFULLY ACCOMPLISHED. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007051000132 20070510 00132 NM 2007 5 10 KPVA20074 1 20070508 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8103 1386005 NM CARGO BAY FAULTY A KPVA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 809WP 032 (PIREP) CLIMBING OUT AT 6000 FT FROM HNL THE SMOKE WARNING LIGHT KEPT COMING ON INTEMITTANTLY AND STAYED ON. (MX) REMOV ED AND REPLACED NR 2 BAGGAGE SMOKE DETECTOR AND PERFORMED OPS CHECK IAW DHC-8 MM 26-12-00 PG 201. 2 H 7 2 4T RT A13NM 2007051000133 20070510 00133 NM 2007 5 10 KPVA20073 1 20070502 A 3150 WARNING SYSTEM DHAV DHC8 DHC8103 1386005 NM COCKPIT MALFUNCTIONED A KPVA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 13 979HA 373 (PIREP) WHILE ADVANCING POWER LEVERS FOR TAKEOFF, CONFIGURATION HORN SOUNDED. AIRCRAFT EXITED THE RUNWAY AND RECYCLED A LL SWITCHES FOR TAKEOFF. RECYCLING THE SWITCHES REMEDIED THE PROBLEM, TAXIED BACK FOR TAKEOFF AND COMPLETED THE FLIGHT WITHOUT INCIDENT. 2 H 7 2 4T RT A13NM 2007051000134 20070510 00134 SO 2007 5 10 RAIA00705009 1 20070505 A 3297 WIRE HARNESS EMB 145 EMB145LR 3260212 SO NLG STEERING DEFECTIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 840HK 145341 FLT NR 8011 - ORD - NOSE WHEEL STEERING FAIL -MAKING GRINDING NOISE- STEERING MESSAGE INOP. MAINTENANCE REMOVED AND REP LACED FEEDBACK POTENTIOMETER 7 DEG PROX SWITCH HARNESS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007051000135 20070510 00135 SO 2007 5 10 RAIA00705011 1 20070506 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 830HK 145313 POST FLT NR 5452 - STL - EMERGENCY LIGHT IN GALLEY INOP. MAINTENANCE RESECURED CONNECTOR ON EMERGENCY LIGHT IN GALLEY. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007051000136 20070510 00136 SO 2007 5 10 RAIA00705002 1 20070502 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 839HK 14500829 POST FLT NR 7900 - ORD - EMERGENCY FLOOR LIGHT STRIP AT 1A IS LOOSE. MAINTENANCE SECURED EMERGENCY LIGHT STRIP. OPERAT IONAL CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007051000137 20070510 00137 SO 2007 5 10 RAIA00705005 1 20070503 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 840HK 145341 POST FLT NR 7953 - RIC - EMERGENCY LIGHT AT LEFTHAND OVERWING EXIT MARKER INOP. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT POWER SUPPLY. 2 L 7 2 4T RT T00011AT 2007051000138 20070510 00138 SO 2007 5 10 RAIA00705003 1 20070502 A 2421 GENERATOR EMB 145 EMB145LR 3260212 SO NR 1 ENGINE INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 834HK 145269 FLT NR 8020 - STL - NR 1 ENGINE DRIVEN GENERATOR WILL NOT PRODUCE VOLTS/AMPS. MAINTENANCE DEFERRED ENGINE 1 GENERATOR P ER MEL. 2 L 7 2 4T RT T00011AT 2007051000139 20070510 00139 2007 5 10 RAIA00705004 4 20070502 A 3425 HG2010AC02 AHRS EMB 145 EMB145 3260210 SO NR 2 MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 807HK 19688 145119 FLT NR 3566 - RIC - F/O'S ATT/HEADING FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED THE NR 2 AHRS, OPS CHECK GOOD AT T HIS TIME. 2 L 7 2 4F RT T00011AT 2007051000140 20070510 00140 SO 2007 5 10 RAIA00705006 1 20070503 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN OUT OF ADJUST A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 840HK 145341 PRE FLT NR 7965 - IAD - EMERGENCY LIGHT LEFT SIDE EXIT ROW LIGHT AT 12A OUT. MAINTENANCE ADJUSTED LIGHT, OPS CHECK GOOD . 2 L 7 2 4T RT T00011AT 2007051000141 20070510 00141 SO 2007 5 10 RAIA00705007 1 20070504 A 2913 MPEV30086 PUMP EMB 145 EMB145LR 3260212 SO NR 1 FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 832HK 5850 145771 FLT NR 7901 - IAD - ELECTRIC HYDRAULIC PUMP NR 1 FAIL AFTER PUSHBACK. MAINTENANCE REMOVED AND REPLACED NR 1 ELECTRICAL H YDRAULIC PUMP, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007051000142 20070510 00142 SO 2007 5 10 RAIA00705010 1 20070505 A 3411 DRAIN EMB 145 EMB145LR 3260212 SO PITOT/STATIC SYS CONTAMINATED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 847HK 14500857 FLT NR 7902 - IAD - F/O'S ALTITUDE INFORMATION (ALTIMETER & ALT SELECT) WENT MISSING ON T/O ROLL. MAINTENANCE DRAIN WAT ER OUT OF F/O PITOT DRAIN. RESET BOTH ADCS. OPS CHECK NORMAL 2 L 7 2 4T RT T00011AT 2007051000143 20070510 00143 SO 2007 5 10 RAIA007012 1 20070507 A 3240 39807 CONTROL VALVE EMB 145 EMB145 3260210 SO BRAKE SYS MALFUNCTIONED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 809HK 145187 FLT NR 5565 - STL - LEFT INBOARD BRAKE DRAGGING DURING TAXI. MAINTENANCE REMOVED AND REPLACED BRAKE CONTROL VALVE AND T HE NR 2 BRAKE. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007051000144 20070510 00144 SO 2007 5 10 RAIA00705013 1 20070507 A 3030 M835366022M RELAY EMB 145 EMB145ER 3260211 SO PITOT HEAT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 808HK 145157 FTL NR 5458 - STL - PITOT 3 HEAT FAIL. MAINTENANCE REMOVED AND REPLACED RELAY K0278AT POSITION B16 AND RESET POWER TO A LL. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007051000145 20070510 00145 2007 5 10 RAIA00705017 4 20070508 A 3425 AHRS EMB 145 EMB145 3260210 SO NR 1 FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 804HK 145082 FLT NR 3564 - PIT - ATTITUDE AND HEADING REFERENCE SYSTEM NR 1 FAIL. MAINTENANCE REMOVED AND REINSTALLED SAME UNIT. SY STEM OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007051000146 20070510 00146 SO 2007 5 10 RAIA00705018 1 20070508 A 3350 78241 POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 840HK 145341 POST FLT NR 7896 - IAD - EMERGENCY EXIT LEFTHAND OVERWING EXIT IDENTIFIER INOP. MAINTENANCE REPLACED POWER SUPPLY. 2 L 7 2 4T RT T00011AT 2007051000147 20070510 00147 SO 2007 5 10 RAIA00705014 1 20070507 A 3240 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO PARKING BRAKE FAULTY A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 835HK 145670 FLT NR 7914 - MLI - TAKEOFF CONFIGURE WARNING. MAINTENANCE CLEANED EMERGENCY PARKING BRAKE PRESSURE SWITCH AND PRESSURI ZED SYSTEM. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007051000148 20070510 00148 SO 2007 5 10 RAIA00705016 1 20070508 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 813HK 145044 POST FLT NR 5568 - STL - EMERGENCY LIGHT FWD FLOOR PROXIMITY LIGHTS INOP. MAINTENANCE RESECURED CONNECTOR, SYSTEM CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007051000149 20070510 00149 2007 5 10 RAIA00705008 4 20070504 A 3418 0861DT5 SENSOR EMB 145 EMB145ER 3260211 SO STALL WARNING MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 808HK 17927 145157 FLT NR 5462 - STL - NR 2 AOA HEAT INOP MESSAGE ON TAXI-OUT. MAINTENANCE REMOVED AND REPLACED THE NR 2 AOA SENSOR. SYST EM CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007051000150 20070510 00150 EA 2007 5 10 SWIA200718202 1 20070424 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING DAMAGED A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 438SW 7574 RIGHT INBOARD WING LEADING EDGE IS DENTED FROM A BIRD STRIKE. REMOVED AND REPLACED LEADING EDGE SKIN AND THREE DAMAGED RIBS IAW CRJ SRM 51-40-11, 51-42-06 AND 51-42-13. 2 L 7 2 4F RT A21EA 2007051000151 20070510 00151 EA 2007 5 10 SWIA200718203 1 20070506 A 2916 73031 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYS FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 916SW 13000 13000 7634 AFTER TAKEOFF RECEIVED HYD 3 LO PRESS MESSAGE ALONG WITH A GEAR DISAGREE. SYSTEM 3 SHOWED 200 PSI WITH 100% QUANTITY. RETURNED TO FIELD. REPLACED HYDRAULIC RESERVOIR NR 3 IAW AMM 29-12-30. 2 L 7 2 4F RT A21EA 2007051100013 20070511 00013 NM 2007 5 11 DL76S070476 1 20070419 A 5320 BAC15062066 FLOOR SUPPORT BOEING 767 767332 1382001 NM CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 128DL 24078 CABIN BS 998 TO 999 RBL FLOOR SUPPORT LWR FACE FOUND CRACKED. REPAIRED PER 53-00-51 FIG 201 ON NR 515601. 2 L 7 2 4F RT A1NM 2007051100020 20070511 00020 NE 2007 5 11 SA07025 2 20070411 A 7200 ENGINE AIRBUS A321 A321211 3930370 EU CFMINT CFM56 CFM565B3P 13006 NE NR 1 MALFUNCTIONED A USAA A UNSCHED LANDING R A B PARTIAL RPM/PWR LOSS FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 189UW 1425 779509 TPA FLT 1945 EN ROUTE CLT TO RSW. OVER THE VICINITY OF GNV, THE NUMBER ONE ENGINE N1 SPEED DROPPED TO 50 PERCENT. A PA SSENGER REPORTED TO HAVE SEEN FIRE AND SMOKE COME FROM THE NUMBER ONE ENGINE. THE FLIGHT DIVERTED TO TPA, AND DURING DE SCENT, REGAINED POWER IN THE NUMBER ONE ENGINE. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. 2 L 7 2 4F 4 F RT A28NM E37NE 2007051100022 20070511 00022 NM 2007 5 11 ZZDA070506158 1 20070506 A 5320 PAN BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933AT 55071 AFT CARGO COMPARTMENT LOWER DOOR JAMB EXTERNAL SURFACE CORROSION IN SEVERAL SPOTS. INSTALLED AFT CARGO DOOR JAMB PAN CO RROSION SPLICES REPAIR AS PER B717 SRM 53-20-15 MAT USED 7075-0 .040 SPLICE 5 X 4.75 LONG. 2 L 7 2 4F TR A6WE 2007051100027 20070511 00027 NM 2007 5 11 DL764070373 1 20070426 A 3350 336701252 POWER SUPPLY BOEING 767 767432ER 1385134 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 841MH 29714 INTERIOR CEILING EMERGENCY LIGHT ABOVE SEAT GROUP 1AB INOP. FOUND LOOSE GRD WIRE, RECONNECTED. LIGHT STILL INOP. FOUN D PWR SUPPLY BAD. REPLACED PWR SUPPLY, OP CHECK GOOD. MCO/PLAC REMOVE. 2 L 7 2 4F RT A1NM 2007051100030 20070511 00030 NM 2007 5 11 DLM88070396 1 20070501 A 2720 4616065BN CONTROL QUADRANT DOUG MD88 MD88 3023688 NM RUDDER PEDAL BROKEN A DALA K NONE G MULTIPLE FAILURE TX TAXI/GRND HDL 1 SO 27 936DL 49723 CAPTAINS RUDDER PEDALS WON`T ADJUST. FOUND RUDDER PEDAL ADJUSTMENT QUADRANT ASSY BROKEN. ALSO FOUND RUDDER PEDAL ADJUS TMENT CABLE BROKEN. REMOVED AND INSTALLED NEW QUADRANT AND NEW RUDDER PEDAL CABLE. ADJ CABLE. ADJUSTED AND OPERATED C ABLE AND QUADRANT. ALL CHECKS NORMAL. NO RII REQ. QUADRANT P/N 4616065BN. 2 L 7 2 4F RT A6WE 2007051100036 20070511 00036 2007 5 11 SWIA200718196 4 20070501 A 3442 RADAR CNDAIR CL600 CL6002B19 1900309 EA WEATHER RADAR FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 936SW 7726 RADAR FAILED AFTER TAKEOFF. RETURNED TO DEN. REMOVED AND REPLACED WEATHER RADAR. REF CRJ 200 MM CHPT 34-41-01 & 34-41 -00. 2 L 7 2 4F RT A21EA 2007051100037 20070511 00037 EA 2007 5 11 SWIA200718197 1 20070430 A 3244 TIRE CNDAIR CL600 CL6002C10 1390015 EA LT MLG BLOWN A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 756SK 10221 LEFT OUTER MAIN TIRE BLEW OUT. DUE TO NR 1 TIRE FLAT UPON ARRIVAL. REMOVED AND REPLACED NR 1 AND NR 2 MAIN WHEEL ASSEM BLY IAW CRJ MM 32-41-01. P/N 5013641 (NR1) SN/OFF NOV04-1445 (NR2) SN/OFF DEC06-1437. 2 L 7 2 4F RT A21EA 2007051100038 20070511 00038 SO 2007 5 11 SWIA200718198 1 20070501 A 3350 SIGN EMB 120 EMB120ER 3260203 SO CABIN BROKEN A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 294SW 120321 EXIT ROW SIGN AT ROW 6 IS BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 6. 2 L 7 2 4T RT A31SO 2007051100040 20070511 00040 SO 2007 5 11 SWIA200718200 1 20070502 A 5610 NP1513112 WINDSHIELD EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 569SW 1767 1767 120344 FIRST OFFICERS WINDSHIELD DAMAGED FROM JET BLAST. REPLACED FIRST OFFICERS WINDSHIELD IAW EMB MM 56-10-01. 2 L 7 2 4T RT A31SO 2007051100041 20070511 00041 NM 2007 5 11 ZZDA070508160 1 20070508 A 5320 PAN BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933AT 55071 FWD CARGO COMP LOWER DOOR JAMB HAS CORROSION IN SEVERAL SPOTS. INSTALLED FWD CARGO DOOR LOWER JAMB PAN CORROSION SPLICE REPAIR PER B717 SRM 53-20-15 FIG 201. MAT USED 2024-D .050 SIZE 5 X 4.75 INCHES. 2 L 7 2 4F TR A6WE 2007051100048 20070511 00048 EA 2007 5 11 VNAA0704009 1 20070416 A 2740 9960013 SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PITCH TRIM FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 244PS 7201 7912 CREW REPORTED A STAB TRIM AND MACH TRIM CAUTION MESSAGE ON TAKEOFF ROLL. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PITCH TRIM DISCONNECT SWITCH IN ACCORDANCE WITH THE AIRCRAFT MAI NTENANCE MANUAL 27-41-30-000(400)-801. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007051100057 20070511 00057 EA 2007 5 11 VNAA0704011 1 20070419 A 3411 0856KV9 PROBE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE PITOT/STATIC SYS DAMAGED A VNAA O OTHER O OTHER DE DESCENT 1 GL 05 712PS 5943 10168 CREW REPORTED A LIGHTNING STRIKE ON DESCENT. MAINTENANCE PERFORMED AN ENROUTE AND A DETAILED LIGHTNING STRIKE INSPECTIO N. AIRCRAFT WAS FERRIED TO DAYTON FOR REPAIR. MAINTENANCE INSPECTED AND REPAIRED ALL DAMAGE. MAINTENANCE ALSO REMOVED AND REPLACED THE LEFT HAND PITOT STATIC PROBE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 34-11-01-000/400-801. OPS AND LEAK CHECKS GOOD AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007051100062 20070511 00062 EA 2007 5 11 VNAA0704012 1 20070419 A 5350 GC21905045 RADOME CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE FUSELAGE DAMAGED A VNAA O OTHER O OTHER DE DESCENT 1 GL 05 723PS 5943 10181 CREW REPORTED A LIGHTNING STRIKE TO THE AIRCRAFT NOSE ON DESCENT. MAINTENANCE PERFORMED A DETAILED LIGHTNING STRIKE INS PECTION. AIRCRAFT WAS FERRIED TO DAYTON FOR REPAIR. MAINTENANCE INSPECTED AND REPAIRED ALL DAMAGE. MAINTENANCE ALSO R EMOVED AND REPLACED THE RADOME IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 53-81-80-400-801-A01. AIRCRAFT WAS RE LEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007051100064 20070511 00064 EU 2007 5 11 PNSA070501 1 20070509 A 7722 RELAY SAAB SF340 SF340A 7850100 EU RT ITT CONTAMINATED A PNSA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 AL 03 109XJ 340A109 AT APPROX 60 KTS IAS DUE TO LOSS OF RT ENGINE ITT INDICATION LOSS. FOUND OIL ON RELAY 68KF, CLEANED DID GROUND RUNS, OP CHECK OK. 2 L 7 2 4T RT A52EU 2007051100067 20070511 00067 EA 2007 5 11 PNSA070401 2 20070413 A 7313 LW18265 FUEL NOZZLE PIPER PA32 PA32301 7103207 SO LYC O540 IO540K1G5 41532 EA ENGINE MALFUNCTIONED E PNSA A UNSCHED LANDING E VIBRATION/BUFFET TO TAKEOFF 1 AL 03 4327P 328406002 L2529048E ON TAKEOFF ENGINE BEGIN RUNNING ROUGH LANDED AND CALLED MX. REMOVED AND REPLACED FUEL NOZZLES. 1 L 7 1 3O 3 O A3SO 1E4 2007051100076 20070511 00076 EA 2007 5 11 VNAA0704015 1 20070424 A 2750 ECU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE T/E FLAP MALFUNCTIONED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 250PS 7929 CREW REPORTED AFTER TAKEOFF A FLAPS FAIL MESSAGE AT 8 DEGREES. CREW ELECTED TO RETURN TO MEM AND LANDED WITHOUT INCIDEN T. MAINTENANCE INSPECTED AND RESET THE FECU. MAINTENANCE ALSO CYCLED THE FLAPS PER THE SERVICE LETTER 00-001. OPERATI ONAL CHECKS GOOD AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007051100077 20070511 00077 NM 2007 5 11 SWAA072362 1 20070509 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 229WN 32498 DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007051100079 20070511 00079 NM 2007 5 11 SWAA072356 1 20070509 A 5753 654643099 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED HC2 CHECK, FOUND LEFT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2007051100080 20070511 00080 NM 2007 5 11 SWAA072361 1 20070509 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 9L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007051100085 20070511 00085 NM 2007 5 11 SWAA072358 1 20070509 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007051100086 20070511 00086 NM 2007 5 11 SWAA072353 1 20070509 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 493WN 32477 DURING SCHEDULED MV2 CHECK, FOUND RIGHT LOWER AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIG HT BULB PER MM. 2 L 7 2 4F RT A16WE 2007051100087 20070511 00087 2007 5 11 SWAA072357 4 20070509 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007051100088 20070511 00088 2007 5 11 SWAA072355 4 20070509 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007050900098 20070509 00098 EA 2007 5 9 SIMA200712701 1 20070505 A 5230 DOOR CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY UNSECURE A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 506AE 10056 COULD NOT CONTROL PRESSURIZATION IN EITHER OR MANUAL MODES. PROPERLY STOWED CARGO DOOR, PERFORMED OPERATIONAL CHECK IAW CRJ AMM 52-31-00 WITH NO DEFECTS, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007050900099 20070509 00099 NM 2007 5 9 EIA2007078 1 20070407 A 5313 STRINGER BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 FOUND STRINGER CORRODED AT CEC CUTOUT AREA BS 760-780 STR 47L. DAMAGED SECTION OF STRINGER CUT AND REMOVED. FABRICATED PER SAMPLE. REPAIR SECTION FABRICATED PER SRM 53-10-03 FIG 1. REPAIR PARTS INSTALLATION CARRIED OUT PER B747 SRM 51-3 0-02, SRM 53-10-03 FIG1. 2 L 7 4 4F A20WE 2007050900102 20070509 00102 NM 2007 5 9 EIA2007080 1 20070407 A 5313 STRINGER BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 FOUND STRINGER 47L BETWEEN BS 740 TO BS 780 CORRODED. DAMAGED SECTION OF STRINGER CUT AND REMOVED. SPLICE SECTION FABR ICATED PER SRM 53-10-03 REPAIR PARTS INSTALLATION CARRIED OUT PER B747 SRM 51-30-02 & 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007050900105 20070509 00105 SO 2007 5 9 SIMA200712804 1 20070501 A 5315 13500428401 FLOORBEAM EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 810AE * 4800 145525 LEFT OMEGA FOUND CORRODED AT FRAME 24 AND FRAME 25. REPAIRED OMEGA BEAM IAW EMB SRM 53-00-10, FIGURE 202. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050900122 20070509 00122 SO 2007 5 9 SIMA200712817 1 20070501 A 5310 14522461011 SUPPORT BEAM EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 810AE 13175 4800 145525 RIGHT HAT BEAM DOUBLER CORRODED AT FRAME 20. REMOVED DAMAGED AREA AND INSTALLED NEW DOUBLER IAW EMB SRM 51-40-02. RETU RNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050900133 20070509 00133 NM 2007 5 9 2007UALA01332 1 20070429 A 5532 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU VERTICAL STAB DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 FIN STA 145, BETWEEN FWD AND AFT SPAR HAS DAMAGE. [SUP 05-16-07] MAJOR REPAIR ACCOMPLISHED: REMOVED EXISTING REPAIRS & DAMAGED SKIN SECTION. FABRICATED & INSTALLED EXTERNAL SKIN SPLICE REPAIR PLATES AT UPPER & LOWER ENDS OF NEW SKIN PANE L SECTION. DOUBLER INSTALLED ON RT FIN STA 154. 2 L 7 2 4F 4 F RT A16WE E21EU 2007050900141 20070509 00141 NM 2007 5 9 2007UALA01338 1 20070429 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 BS 294 SHEAR TIE CRACKED AT STRINGER 11L. [SUP 05-16-07] MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKED SHEAR TIE. FABRI CATED & INSTALLED NEW SHEAR TIE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007050900144 20070509 00144 NM 2007 5 9 2007UALA01342 1 20070428 A 5210 INDICATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR STICKS A UALA O OTHER L NO TEST IN INSP/MAINT 1 WP 29 506UA 24627 CREW REPORTS DOOR 4L WILL NOT ARM AT DEPARTURE. [SUP 06-06-07] DOOR FOUND TO ARM AND DISARM NORMAL. LUBE INDICATOR A RM POP OUT WAS STICKING AND APPEARED TO HAVE CAUSED THE PROBLEM WITH ARMING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050900157 20070509 00157 NM 2007 5 9 C1HA200795025 1 20070504 A 5313 69436951 STRINGER BOEING 727 727290 138408W NM BS 740 S27L CORRODED A C1HA O OTHER O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 FOUND CORROSION AT STA 740. CUT OUT DAMAGED AREA FROM STR 27L AT STA 740, FAB`D STR REPAIR AND SPLICE. TREATED AND PRI MED. REMOVED AND REPLACED DAMAGED FITTING AT LT STA 740 AT STR 27L. INSTALLED ALL PARTS IAW B727 SRM 53-10-3 FIG 1 AND 51-30-2. 2 L 7 3 4F A3WE 2007050900158 20070509 00158 NM 2007 5 9 C1HA200795002 1 20070504 A 5330 SKIN BOEING 727 727290 138408W NM BS 303 CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 EXT FUSE BS 303 AT L-1 DOOR LOWER HINGE HAS REPAIR DOUBLER CRACKED IN FWD CUTOUT. REMOVED EXISTING REPAIR DOUBLER, HFEC INSP AND FOUND SKIN AND INNER DOUBLER CRACKED, CRACK APPROX 2 1/4" LONG. CUTOUT DAMAGED AREA IAW B727 SRM 51-10-1. RE PAIRED AREA IAW CA EO-727-5331-19 AND BOEING SKETCH NR 1-316284639-3. 2 L 7 3 4F A3WE 2007050900162 20070509 00162 NM 2007 5 9 C1HA200795027 1 20070504 A 5313 1498142707075T STRINGER BOEING 727 727290 138408W NM BS 420 S28R CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 FOUND CORROSION ON FRAME STA 420 BL 0 TO STR 28R. REMOVED DAMAGED SECTION OF STRINGER, FABRICATED AND INSTALLED NEW SEC TION FROM BS 400-420 STR 28R IAW B727 SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2007050900169 20070509 00169 NM 2007 5 9 C1HA200795031 1 20070504 A 5313 STRINGER SPLICE BOEING 727 727290 138408W NM BS 475 S26L CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 FOUND CORROSION IN E/E BAY AT BS 475 STR 26L. REMOVED EXISTING MANUFACTURE SPLICE, FABRICATED AND INSTALLED NEW SPLICE IAW B727 SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2007050900171 20070509 00171 NM 2007 5 9 C1HA200795033 1 20070504 A 5313 14581327075T6 STRINGER SPLICE BOEING 727 727290 138408W NM BS 540 S26R CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 FOUND FWD CARGO COMPARTMENT AT BS 540 STR 26R HAS HEAVY CORROSION AT SPLICE. REMOVED AND REPLACED FWD CARGO BS 540 STR 26R SPLICE ANGLE IAW B727 SRM 53-10-2 AND 53-40-3. 2 L 7 3 4F A3WE 2007050900184 20070509 00184 NM 2007 5 9 2007UALA01396 1 20070503 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 AFT PIT FLOOR PNL SUPPORT STR AT LBL 3 HAS CORROSION IN STA 1330 AREA. [SUP 06-06-07] FABRICATED REPAIR REPAIR VII. OR IGINAL MATERIAL 0.063, REMAINING AFTER CLEAN UP 0.044. INSTALLED REPAIR PER UA ENGINEERING SPECIFICATIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050900193 20070509 00193 NM 2007 5 9 2007UALA01400 1 20070503 A 3397 BR963165 CABLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN CUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 839UA 1507 FOUND EMERGENCY EXIT ROW LIGHT INOP AT SEAT 6. REPLACED CABLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007050900211 20070509 00211 SO 2007 5 9 C2XA07CL042 1 20070505 A 2621 346000731 FIRE BOTTLE EMB 145 EMB145XR 3260214 SO CARGO BAY INTERMITTENT A C2XA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 SW 27 11155 145782 CLE FLIGHT 2409 THE CREW REPORTED A BAG SMOKE DETECT INDICATION ON THE ECIAS, ALSO A BAG FIRE BOTTLE FAIL MESSAGE. THE AIRCRAFT DIVERTED TO CLEVELAND AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE BAG FIRE BOTTLES. O PERATIONAL CHECKS WERE GOOD. P/N 33700027-1, S/N 52206D1. 2 L 7 2 4F RT 2007050900214 20070509 00214 SO 2007 5 9 C2XA07IA102 1 20070502 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145EP 3260221 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15926 145005 IAH - DURING MAINTENANCE INSPECTION SEVERAL EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN T O SERVICE. 2 L 7 2 4F RT T00011AT 2007050900223 20070509 00223 NM 2007 5 9 SWAA072284 1 20070507 A 3350 10107451 SIGN BOEING 737 7377H4 1384404 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 455WN 32462 R2 DOOR EMERGENCY EXIT SIGN FELL OFF. INSTALLED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007050900231 20070509 00231 NM 2007 5 9 SWAA072306 1 20070507 A 5330 655298871 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 975, STR 20L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007050900235 20070509 00235 NM 2007 5 9 SWAA072292 1 20070507 A 5754 65C26602 WEDGE BOEING 737 7373H4 1384600 NM L/E SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND LEFT WING NR 2 LEADING EDGE SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM. 2 L 7 2 4F RT A16WE 2007051000004 20070510 00004 EU 2007 5 10 TRAX200700622 1 20070504 A 5260 STEP AEROSP ATR72 ATR72 EU AIRSTAIR DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 TOP STEP OF AIRSTAIR DOOR IS BROKEN. 2 H 7 2 4T RT 2007051000008 20070510 00008 EA 2007 5 10 TRAX200700608 1 20070502 A 5320 FLANGE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 884AS 7513 FS 280 UPPER AFT FLANGE IS CRACKED ON LEFT SIDE O/B OF LBL 9. [SUP 05-11-07] REPAIRED F.S. 280 UPPER AFT FLANGE LT O/B OF LBL 9 PER: REO 601R-53-11-136. 2 L 7 2 4F RT A21EA 2007051000013 20070510 00013 EA 2007 5 10 TRAX200700613 1 20070503 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 CLIP ON RIGHT AFT FACE BULKHEAD INTERCOSTAL CRACKED FS 621.00. [SUP 05-17-07] REMOVED AND REPLACED IAW REO 601R-53-61- 100, AND ASA EO 600-53-174C. 2 L 7 2 4F RT A21EA 2007051000014 20070510 00014 EA 2007 5 10 TRAX200700614 1 20070504 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 861AS 7445 ASD BOTTOM STEP CRACKED. 2 L 7 2 4F RT A21EA 2007051000016 20070510 00016 EA 2007 5 10 TRAX200700616 1 20070504 A 5260 STEP CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 706EV 10054 SUSPECT CRACK ON ASD UNDER TOP STEP FWD SIDE (MARKED). [SUP 05-11-07] REMOVED AND REPLACED PANEL PER CRJ 700 SRM 51-42 -13. 2 L 7 2 4F RT A21EA 2007051000020 20070510 00020 EA 2007 5 10 TRAX200700624 1 20070504 A 3250 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA NLG STEERING MALFUNCTIONED A ASOA K NONE N FALSE WARNING CL CLIMB 1 SO 27 744EV 10157 NWS CAUTION AFTER TAKEOFF. RAN QRH TURNED OFF. RESET ON THE GROUND AND OPERATION NORMAL. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007051000023 20070510 00023 NM 2007 5 10 CALA0700231 1 20070504 A 5320 69265553 FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14358 23943 INSPECTION FOUND A .5 INCH CRACK IN ANGLE CLIP AT BS 348.20, S16L. REPAIRED IAW ERCA 5311-01320. 2 L 7 2 4F RT A16WE 2007051000025 20070510 00025 NM 2007 5 10 CALA0700233 1 20070504 A 5320 69165096 FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14358 23943 INSPECTION FOUND A .5 INCH CRACK IN ANGLE CLIP AT BS 348.20, S16L. REPAIRED IAW ECRA 5311-01320. 2 L 7 2 4F RT A16WE 2007051000028 20070510 00028 NM 2007 5 10 CALA0700236 1 20070506 A 5330 141A372212 SKIN BOEING 737 737924 13848A1 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 38403 30120 INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT EXTERNAL POWER DOOR LOWER HINGE AREA, STA 235.8 - 243.7, S20R. AN I NTERIM REPAIR WAS PERFORMED IAW ECRA 5330-03672. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR PER ECRA 5330-03672, PA RT 3 WITHIN 12 MONTHS. 2 L 7 2 4F RT A16WE 2007051000038 20070510 00038 NM 2007 5 10 USAA070366 1 20070508 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 511AU 23594 FLOORBEAM T-CAP AT BS 986.5, BL 0.0-BL 5 HAS CORROSION. FAB'D & INSTALLED FILLERS, ANGLES, STRAPS PER EA 98654, CORR LE VEL 2, DEFECT SIZE: 4 AREAS; 2 = 1" X .75" X .010" TO .025", AND 2 = 1" X 2" X .060". 2 L 7 2 4F RT A16WE 2007051000041 20070510 00041 NM 2007 5 10 USAA070363 1 20070508 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 BL 0 FS 927-947, L-ANGLE CRACKED. REMOVED ANGLE & FAB'D NEW PER SRM 51-10-02, 51-20-01, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007051000043 20070510 00043 NM 2007 5 10 USAA070361 1 20070508 A 5313 STRINGER BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 STA 616 STR 4R CRACKED. REMOVED & REPLACED PER SRM 51-20-00, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007051000068 20070510 00068 WP 2007 5 10 UPS07849748 1 20070426 A 5730 DOUBLER DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 CRACK ON INTERNAL DOUBLER ON RIGHT WING CENTER LEADING EDGE UPPER SURFACE I/B EDGE OF SLOT DOOR. REM OVED INTERNAL DOUBLER ON RIGHT WING CENTER LEADING EDGE IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR DOUBLER ON RIG HT WING LEADING EDGE IAW DWG 5718963-236, AND SRM 51-3-2. 2 L 7 4 4F RT 4A25 2007051000069 20070510 00069 WP 2007 5 10 UPS07849750 1 20070425 A 5311 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 MAIN CABIN, CORROSION ON BELTFRAME END FITTING, STA 220 L21R. REMOVED AND REPLACED BELTFRAME FITTING AT STA 220 L21R IAW SRM 51-1-20D, AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 2007060500098 20070605 00098 NM 2007 6 5 WRLA2007066 1 20070506 A 2741 ASM7337507 DRIVE ASSY DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE TRIM SYS SHEARED A WRLA J A DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 11 271WA 48518 AIR RETURN. AFTER TAKEOFF CAPTAIN AND FIRST OFFICER FOUND LONGITUDINAL TRIM HANDLE WOULD NOT TRIM THE HORIZONTAL STAB. STAB REMAINED AT 7.6 UNITS OF TRIM. AUTOPILOT LEFT AND RIGHT DID NOT AFFECT TRIM POSITION. DURING PRESENT AND MODERAT E PITCH CHANGE FELT IN THE YOKE. HOWEVER STAB REMAINED AT 7.6 UNITS. DUMPED FUEL AND RETURNED TO LIPA WHEN ON THE GROU ND TESTED THE LONG TRIM HANDLES, HYD SYS PRESSURE DEFLECTION WAS NOTED BUT NO STAB MOVEMENT. [SUP 05-30-07] FOUND DIF FERENTIAL DRIVE UNIT SHEARED. REMOVED AND REPLACED CHAIN DIFFERENTIAL FUSE DRIVE UNIT PER AMM 27-44-04. CHAINS AND ACTUA TORS WEAR FOUND TO BE WITHIN SERVICABLE LIMITS. PERFORMED GENERAL VISUAL INSPECTION OF HORIZONTAL STAB RANGE OF MOVEMENT 2 L 7 3 4F 4 F RT A22WE E24NE 2007051000118 20070510 00118 NM 2007 5 10 WRLA2007067 1 20070508 A 5210 NBA62624 SKIN DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE PAX DOOR DEFORMED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 274WA 48633 DURING PERFORMING 4C CHECK OF DATUM A/C, EGAT FOUND A DEFORMATION ON RIGHT FORWARD PASSENGER DOOR SKIN AFT UPPER CORNER. TRIM OUT DAMAGED AREA AND INSTALL FILLER AND EXTERNAL DOUBLER PER SRM 52-10-00 FIGURE 10. 2 L 7 3 4F 4 F RT A22WE E24NE 2007051000152 20070510 00152 EA 2007 5 10 SWIA200718204 1 20070505 A 5320 SEAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A SWIA K NONE O OTHER TX TAXI/GRND HDL 1 NM 07 957SW 7829 PAX DOOR AFT STRIKER SEAL IS SEVERELY DAMAGED. FOUND TO BE A MAJOR REPAIR. REPAIRED PAX DOOR AFT STRIKER SEAL IAW BOMB ARDIER REO 601R-53-22-033 TYPE III. 2 L 7 2 4F RT A21EA 2007051000153 20070510 00153 2007 5 10 SWIA200718205 4 20070506 A 2211 6229815904 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT SYS MALFUNCTIONED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 986SW 7967 WHILE CRUISING AT 32,000 FEET WITH AUTOPILOT ENGAGED, STAB TRIM AND MACH TRIM MESSAGES APPEARED. NEITHER STAB OR MACH T RIM WOULD RE-ENGAGE. AUTOPILOT WORKED NORMALLY. REPLACED THE NR 2 FCC CARD PER MM 22-12-14. P/N: 622-9815-904, S/N ON : 10JXC, S/N OFF: 1L3NM. 2 L 7 2 4F RT A21EA 2007051000154 20070510 00154 EA 2007 5 10 SWIA200718206 1 20070430 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 963SW 7865 CAPTAIN'S WINDSHIELD SHATTERED INFLIGHT IN CRUISE. REPLACED CAPTAIN'S WINDSHIELD PER AMM 56-11-01. P/N OFF: 601433033 -17, S/N OFF: 03171H6862. 2 L 7 2 4F RT A21EA 2007051000155 20070510 00155 EA 2007 5 10 SWIA200718207 1 20070507 A 3620 LOOP CNDAIR CL600 CL6002C10 1390015 EA BLEED AIR SYS MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 728SK 10192 CLIMBING THROUGH FL230, RECEIVED A -L BLEED DUCT- WARNING MESSAGE. RETURNED TO CVG. REPLACED LOOP MT 139 IAW 36-21-01. P/N: GG670-80107-1. 2 L 7 2 4F RT A21EA 2007051000156 20070510 00156 NM 2007 5 10 SCNA07006 1 20070510 A 3350 LIGHT BOEING 737 7378Q8 13844BX NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 805SY 30032 THE LEFT AFT OVERWING DOOR AFT WINDOW EMERGENCY EXIT LIGHT WAS FOUND INOP. MAINTENANCE REPLACED THE BULB IN THE EMERGEN CY EXIT LIGHT. 2 L 7 2 4F RT A16WE 2007051000157 20070510 00157 EA 2007 5 10 TRAX200700630 1 20070505 A 3250 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA NLG STEERING ACTIVATED A ASOA K NONE J WARNING INDICATION CR CRUISE 1 SO 27 744EV 10157 STEER INOP CAUTION MSG DISPLAYED. C/W QRH. REPEAT WRITE UP. FLT 4737 CX. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007051000158 20070510 00158 EA 2007 5 10 SWIA200718201 1 20070502 A 4930 B-NUT CNDAIR CL600 CL6002B19 1900309 EA APU FUEL SYSTEM LEAKING A SWIA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 459SW 7782 AFTER TAKEOFF FROM SLC, THE CABIN SMELLED OF FUEL AFTER THE APU WAS SHUTDOWN. FOUND APU FUEL SOLENOID TO BE LEAKING AT THE B-NUT CONNECTION. TIGHTENED B-NUT ON APU FUEL SOLENOID. NO LEAKS NOTED. 2 L 7 2 4F RT A21EA 2007051000159 20070510 00159 SO 2007 5 10 SWIA200718191 1 20070502 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 586SW 120354 EMERGENCY EXIT LIGHTING WILL NOT ILLUMINATE. REPLACED FORWARD EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-02. 2 L 7 2 4T RT A31SO 2007051000160 20070510 00160 EA 2007 5 10 SWIA200718192 1 20070501 A 3520 OXYGEN MASK CNDAIR CL600 CL6002C10 1390015 EA LAVATORY UNWANTED DEPLOY A SWIA G O2 MASK DEPLOYED O OTHER CR CRUISE 1 NM 07 368CA 10075 THE O2 MASKS IN FORWARD LAV DEPLOYED IN FLIGHT. RESTOWED LAV O2 MASKS. 2 L 7 2 4F RT A21EA 2007051000161 20070510 00161 SO 2007 5 10 SWIA200718193 1 20070426 A 3397 CONNECTOR EMB 120 EMB120ER 3260203 SO CABIN DISCONNECTED A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 579SW 120347 FORWARD FLOOR EMERGENCY LIGHTS ARE INOP. RECONNECTED FORWARD EMERGENCY LIGHT STRIP CONNECTOR. 2 L 7 2 4T RT A31SO 2007051100035 20070511 00035 EA 2007 5 11 SWIA200718195 1 20070503 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 925SW 7682 EMERGENCY LIGHT POD INOP. RELAMPED EMERGENCY LIGHT IAW MM CHAPTER 33-50-00. 2 L 7 2 4F RT A21EA 2007051100081 20070511 00081 NM 2007 5 11 SWAA072360 1 20070509 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 8L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007051100083 20070511 00083 NM 2007 5 11 SWAA072363 1 20070509 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007051100084 20070511 00084 NM 2007 5 11 SWAA072359 1 20070509 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007051100090 20070511 00090 NE 2007 5 11 YENA2007032 2 20070508 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 SURGES A YENA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 15 561JB 1927 V11398 ENG NR 1 STALL ON CLIMB. ONE SURGE. EXAMINED THE INLET, EXHAUST AND BLEED VALVES FOR FOREIGN MATERIAL AND EVIDENCE OF INTERNAL ENGINE DAMAGE IAW AMM TASK 71-00-00-810-808. NO DEFECTS NOTED. PERFORMED BOROSCOPE INSPECTION OF HPC STAGES E NG 1, 3, 6 AND 12 IAW 72-00-00-06. NO DEFECTS NOTED. ENG NR 1 OK FOR CONTINUED SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007051100092 20070511 00092 2007 5 11 ZZDA070509161 4 20070509 A 2565 FITTING BOEING 717 717200 1383700 NM EVAC SLIDE MISSING A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924AT 2453 55080 L1 DOOR SLIDE PACK MISSING A CLIP. REMOVED AND REPLACED L1 DOOR SLIDE ASSY REF AM/M 25-61. 2 L 7 2 4F TR A6WE 2007051100093 20070511 00093 NM 2007 5 11 R61A20070010 1 20070504 A 2780 1700064E CONTROLLER EMB ERJ170 ERJ170100SU 3260403 NM E&E BAY FAILED A R61A O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 823MD 6453 976 17000044 CREW REPORTED SLATS FAIL MESSAGE ON APPROACH. SLATS FAILED AT 3 DEGREES, DECLARED AN EMERGENCY AND FOLLOWED QRH PROCEDU RES LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO AIRCRAFT AND TROUBLESHOT. REMOVED AND REPLACED SF-ACE CONTR OLLER, SYSTEM OPERATIONAL CHECK GOOD AND A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A56NM 2007051100094 20070511 00094 NM 2007 5 11 AWXA200700568 1 20070504 A 3397 BMS13311122 WIRE BOEING 737 7373G7 1384595 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 309AW 24711 SNA - EEL - EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE FROM SEAT ROW 12 ABC THRU 18 ABC. REPAIRED BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 18 ABC AND PERFORMED OPERATIONAL CHECK IAW B737-300 AMM 33-51-02. 2 L 7 2 4F RT A16WE 2007051100095 20070511 00095 EU 2007 5 11 AWXA200700569 1 20070505 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 648AW 770 LAS - EEL - FORWARD EMERGENCY LIGHT BATTERY FAILED EMERGENCY LIGHT TEST. REPLACED AND OPERATIONAL CHECKED FORWARD EMERG ENCY LIGHT BATTERY IAW AWA TASK CARD A1C33302. 2 L 7 2 4F RT A28NM 2007051100096 20070511 00096 EU 2007 5 11 AWXA200700570 1 20070507 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU CABIN FAILED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 PHX - EEL - LEFT EMERGENCY EXIT LIGHT FAILS TEST. REPLACED AND OPERATIONAL CHECKED THE LEFT EMERGENCY LIGHT POWER SUPPL Y BATTERY IAW AWA TASK CARD A1C33302. 2 L 7 2 4F RT A28NM 2007051100102 20070511 00102 EU 2007 5 11 AWXA200700575 1 20070506 A 5347 D53472190202 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 665AW 1644 SAL - MAJOR REPAIR - BC-4 CHECK - CORROSION ON CABIN RAIL SEAT, FR 64 TO FR 66 + 6, +Y765. REPLACED CABIN RAIL SEAT, FR 64 TO FR 66 + 6, +Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007051100103 20070511 00103 EU 2007 5 11 AWXA200700576 1 20070504 A 5347 D53472190210 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 665AW 1644 SAL - MAJOR REPAIR - BC-4 CHECK - CORROSION ON CABIN RAIL SEAT, FR 64 TO FR 66 + 6, +Y1292. REPLACED CABIN RAIL SEAT, F R 64 TO FR 66 + 6, +Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007051100105 20070511 00105 EU 2007 5 11 AWXA200700577 1 20070508 A 5320 D53475765206 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 665AW 1644 SAL - MAJOR REPAIR - BC-4 CHECK - CORROSION ON BULK CARGO COMPARTMENT DOOR CUTOUT LOWER SILL, FR 61 + 9 AND FR 61 + 19. REPAIRED BULK CARGO COMPARTMENT DOOR CUTOUT LOWER SILL, FR 61 + 9 AND FR 61 + 19 IAW A320 SRM 53-41-49, FIGURE 203. 2 L 7 2 4F RT A28NM 2007051100106 20070511 00106 EU 2007 5 11 AWXA200700578 1 20070509 A 5321 D5367180500300 FLOORBOARD AIRBUS 320 A320231 3930325 EU CABIN DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 625AW 064 PHX - MAJOR REPAIR - R2 DOOR ENTRYWAY FLOORBOARD 262 FF DELAMINATED, FR 66 - FR 68, -Y1292 TO -Y1732. REPLACED R2 DOOR ENTRYWAY FLOORBOARD 262 FF DELAMINATED, FR 66 - FR 68, -Y1292 TO -Y1732 IAW AWA TASK CARD R1C25306. 2 L 7 2 4F RT A28NM 2007051100108 20070511 00108 EA 2007 5 11 TRAX200700631 1 20070506 A 3620 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA BLEED AIR SYS ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 710EV 10071 RIGHT BLEED DUCT WARNING. A/C RETURNED TO ATL AFTER T/O. RELATED TO DEFECT 306811-2. EMERGENCY DECLARED. FLT 4331, 4 899 CX. 2 L 7 2 4F RT A21EA 2007051100110 20070511 00110 EA 2007 5 11 TRAX200700633 1 20070506 A 2560 MEGAPHONE CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 659CA 10153 AFT MEGA PHONE INOP. 2 L 7 2 4F RT A21EA 2007051100111 20070511 00111 NM 2007 5 11 AWXA200700560 1 20070505 A 5320 6545402279 STIFFENER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 PHX - MAJOR REPAIR - RIGHT HAND MAIN LANDING GEAR WHEEL WELL FORWARD BULKHEAD VERTICAL STIFFENER CRACKED, BS 663.75, RB L 6.15, WL 170. REPAIRED RIGHT HAND MAIN LANDING GEAR WHEEL WELL FORWARD BULKHEAD VERTICAL STIFFENER, BS 663.75, RBL 6. 15, WL 170 IAW AWA ER 03-5712-06054-BA1. 2 L 7 2 4F RT A16WE 2007051100112 20070511 00112 NM 2007 5 11 AWXA200700561 1 20070504 A 5523 65C2638425 ATTACH FITTING BOEING 737 7373G7 1384595 NM ELEVATOR TAB CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 PHX - MAJOR REPAIR - LEFT HAND ELEVATOR TAB PUSH ROD ATTACH FITTING LUG CRACKED, ELEVATOR STATION 32 TO ELEVATOR STATION 39.22. REPLACED LEFT HAND ELEVATOR TAB IAW AWA TASK CARD R6C27007. 2 L 7 2 4F RT A16WE 2007051100115 20070511 00115 NM 2007 5 11 AWXA200700564 1 20070427 A 5330 654577572 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - C-20 CHECK - CRACKED FUSELAGE SKIN, BS 727E, S21R. REPAIRED FUSELAGE SKIN, BS 727E, S21R IAW B737- 300 SRM 53-00-01-2R31, FIGURE 201. 2 L 7 2 4F RT A16WE 2007051100116 20070511 00116 NM 2007 5 11 AWXA200700565 1 20070416 A 5330 654577472 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - C-20 CHECK - CRACKED FUSELAGE SKIN, BS 930, S24L. REPAIRED FUSELAGE FUSELAGE SKIN, BS 930, S24L IA W B737-300 SRM 53-00-01-2R30, FIGURE 201. 2 L 7 2 4F RT A16WE 2007051100117 20070511 00117 NM 2007 5 11 AWXA200700566 1 20070407 A 5320 65479733 SHEAR WEB BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - MAJOR REPAIR - C-20 CHECK - CRACKED CABIN SHEAR WEB, BS 63 - BS 640, RBL 65, WL 208. REPLACED CABIN SHEAR WEB, BS 63 - BS 640, RBL 65, WL 208 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007051100119 20070511 00119 NM 2007 5 11 AWXA200700581 1 20070422 A 3350 P4010021 BATTERY BOEING 757 7572S7 1384962 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 904AW 23566 MCN - EEL - C-11 CHECK - RIGHT HAND MID AFT FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT BATTERY IS DISCHARGED. REPLACED AND OPERATIONAL CHECKED RIGHT HAND MID AFT FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT POWER UNIT. 2 L 7 2 4F RT A2NM 2007051100120 20070511 00120 EU 2007 5 11 AWXA200700582 1 20070506 A 5315 D53472189204 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 665AW 1644 SAL - MAJOR REPAIR - BC-4 CHECK - CORROSION ON CABIN FLOORBEAM, FR 68 + 6 TO FR 69 + 4, -Y1162. REPLACED CABIN FLOORBEA M, FR 68 + 6 TO FR 69 + 4, -Y1162 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007051100125 20070511 00125 NM 2007 5 11 PIDA07032 1 20070508 A 5230 SKIN BOEING 737 7372K5 138448X NM CARGO DOOR CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 DURING MAINTENANCE, NOTED A CRACK IN THE AFT UPPER CORNER OF THE AFT CARGO DOOR SKIN AT THE HANDLE ACCESS CUTOUT. REPLA CED DOOR SKIN PER DWG 65-47952 AND SRM 51-30-02 AND 51-30-02 DUE TO PROXIMITY TO AN EXISTING REPAIR AND OTHER MULTIPLE D ENTS AND SCRATCHES. 2 L 7 2 4F RT A16WE 2007051100159 20070511 00159 WP 2007 5 11 07FDEA01703 1 20070504 A 5230 FITTING DOUG DC10 DC1010 3022110 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 MAIN CARGO DOOR LOWER SILL NR 7 SPOOL LATCH BACKUP FITTING IS CRACKED. [SUP 05-21-07] REMOVED AND REPLACED NR 7 SPOOL LATCH BACKUP FITTING IAW DC/MD10 SRM 51-33-01 PG1 VOL II AND EA 8-5230-110682, DAC DRAWING AFA 2132 REV B. MINOR REP AIR 2 L 7 3 4F A22WE 2007051100160 20070511 00160 NM 2007 5 11 CALA0700238 1 20070509 A 5315 6545812 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, RBL 32-34. A REPAIR STRAP WAS INSTALLED IAW SRM 53-00-51, FIGURE 201. 2 L 7 2 4F RT A16WE 2007051100162 20070511 00162 SO 2007 5 11 C2XA07CL044 1 20070509 A 3231 22270100001 SOLENOID VALVE EMB 145 EMB145LR 3260212 SO NLG LEAKING A C2XA K NONE O OTHER LD LANDING 1 SW 27 14902 145496 CLE FLIGHT 3094 THE CREW REPORTED A LOUD CONTINOUS BANGING SOUND FROM NOSE GEAR AFTER LANDING. MAINTENANCE INSPECTED AN D REPLACED THE LANDING GEAR SOLENOID VALVE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007051100163 20070511 00163 NM 2007 5 11 MWEA070100 1 20070506 A 5730 SKIN PANEL BOEING 717 717200 1383700 NM LT WING LOOSE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 908ME 55172 REPORTED FUEL SEEPAGE FROM THE LEFT WING. RESECURED INBOARD FUEL TANK PANEL. 2 L 7 2 4F TR A6WE 2007051100165 20070511 00165 WP 2007 5 11 070111 1 20070509 A 7920 B-NUT DOUG DC9 DC982 3022082 WP LT ENGINE LOOSE A WX0A C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 WP 19 886GA 49931 DURING TAKEOFF ROLL THE LEFT ENGINE OIL PRESSURE LOW LIGHT CAME ON, OIL PRESSURE INDICATOR READING WAS 19 PSI AT 80 KNOT S. ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE DEPARTMENT PERSONNEL DISCOVERED A LOOSE B-NUT AT THE LOW OIL PRES SURE SWITCH AND ABOUT ONE QUART OF OIL IN THE COWL. THE B-NUT WAS TIGHTENED AND THE OIL QUANITY WAS CHECKED AND OIL ADD ED AS REQUIRED. LEAK AND OPS CHECK GOOD, THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007051100166 20070511 00166 NM 2007 5 11 MWEA070106 1 20070511 A 7830 7150923REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 917ME 55179 LEFT THRUST REVERSER BOTTOM DEFLECTOR DOOR HAS A CRACKED ZEE FRAME, OUTBOARD SIDE AT STATION 35.669. INSTALLED ZEE FRAM E. 2 L 7 2 4F TR A6WE 2007051100167 20070511 00167 NM 2007 5 11 MWEA070107 1 20070511 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 917ME 55179 LEFT THRUST REVERSER, BOTTOM DEFLECTOR DOOR HAS A CRACKED ZEE FRAME, OUTBOARD SIDE AT STATION 26.666. INSTALLED ZEE FRA ME. 2 L 7 2 4F TR A6WE 2007051100172 20070511 00172 NM 2007 5 11 C1HA200795004 1 20070504 A 5320 SUPPORT ANGLE BOEING 727 727290 138408W NM FUSELAGE CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 LEFT VENTRAL STAIRWELL LT TORQUE BOX SUPPORT ANGLE IS CRACKED AT STA 1253 BELOW BAZOOKA TUBES. FABRICATED AND INSTALLED REPAIR DOUBLER AT BS 1253 LEFT TORQUE BOX SUPPORT ANGLE MATERIAL USE 7075-T6 .050, DIM 8 X 3, IAW B727 SRM 51-40-3 FIG 1 & 53-10-2 FIG 6. 2 L 7 3 4F A3WE 2007051100173 20070511 00173 NM 2007 5 11 CIHA200795010 1 20070504 A 5347 BAC1520792 SEAT TRACK BOEING 727 727290 138408W NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 CORROSION ON SEAT TRACK BS 344 - 380 RBL 45. REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 53-10-2 AND 53-10-5 FIG 7. 2 L 7 3 4F A3WE 2007051100177 20070511 00177 NM 2007 5 11 C1HA200795006 1 20070504 A 5311 FRAME BOEING 727 727290 138408W NM FUSELAGE CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 COCKPIT FRAME AT STA 277 AND STR 16RT IS CRACKED APPROX 1 INCH LONG, VERIFED BY HFEC (BEHIND FE CONSOLE). REPAIRED COCK PIT FRAME AT STA 277, STR 16RT IAW B727 SRM 53-10-2 AND 51-40-2. 2 L 7 3 4F A3WE 2007051100181 20070511 00181 NM 2007 5 11 C1HA200795011 1 20070504 A 5320 150910030 SUPPORT BOEING 727 727290 138408W NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 SURFACE CORROSION ON MAIN CABIN FWD LAV AFT WALL SUPPORT BS 344 RBL 15 - RBL 65. REPLACED LAV SUPPORT BS 344 RBL 15 TO 65 IAW B727 SRM 53-10-2. 2 L 7 3 4F A3WE 2007051100187 20070511 00187 NM 2007 5 11 C1HA200795012 1 20070504 A 5320 145028317075T6 ANGLE BOEING 727 727290 138408W NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 FOUND CORROSION ON WEB ANGLE IN SEVERAL MARKED AREAS BETWEEN STA 1148-1165 RBL 60. REPLACED ANGLE BETWEEN STA 1148 TO 1 165 RBL 60 IAW B727 SRM 53-10-2 AND 51-40-3. 2 L 7 3 4F A3WE 2007051100190 20070511 00190 NM 2007 5 11 C1HA200795014 1 20070504 A 5320 BRACKET BOEING 727 727290 138408W NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 FOUND CORROSION EMANATING FROM BENEATH ANGLE BRACKET O/B OF AFT LAV FITTINGS AT STA 1165 RBL 45. REPLACED BRACKET ANGLE IAW B727 SRM 51-40-3 AND 53-10-2 AND REPAIRED SHEAR WEB IAW B727 SRM 53-10-2 AND 51-40-2. 2 L 7 3 4F A3WE 2007051100192 20070511 00192 NM 2007 5 11 C1HA200795003 1 20070504 A 5330 SKIN BOEING 727 727290 138408W NM FUSELAGE CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 FOUND FUSE BS 1098 RBL 1 HAS 1/2" CRACK IN FASTENER HOLE. CUT OUT CRACKED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B727 SB 727-53A0204 REV 3 FIG 2 AND AD 94-05-04-06.2 2 L 7 3 4F A3WE 2007051100199 20070511 00199 WP 2007 5 11 NWAA071779988 1 20070510 A 5711 SPAR CAP DOUG DC9 DC931 3022065 WP RT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8944E 47167 DURING H-CHECK FOUND CRACK IN RIGHT WING AFT UPPER SPAR CAP AT STA XCWS 58.5. REPAIRED PER EA 99-208494. 2 L 7 2 4F A6WE 2007051100201 20070511 00201 EU 2007 5 11 NWAA071743226 1 20070505 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 326US 17727 1344 282 LEFT FORWARD EMERGENCY LIGHT POWER SUPPLY INOP. REPLACED LEFT FORWARD EMERGENCY LIGHT POWER SUPPLY, CHECKS OK. 2 L 7 2 4F RT A28NM 2007051100205 20070511 00205 NM 2007 5 11 NWAA071755638 1 20070504 A 2422 INVERTER BOEING 757 757251 1384970 NM STANDBY BURNED A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 538US 26485 EICAS STATUS MESSAGE -STBY INVERTER-, ALONG WITH SLIGHT SMELL OF BURNING ELECTRICS THRU OUT CABIN AND COCKPIT. MAINTENA NCE: PERFORMED TSM PROCEDURE 24-37-00, FOUND OLD STANDBY INVERTER BURNT; REPLACED STATIC (STANDBY) INVERTER. AIRCRAFT OK FOR SERVICES. 2 L 7 2 4F RT A2NM 2007051100206 20070511 00206 NM 2007 5 11 QXEA200700730 1 20070425 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - RIGHT HAND INBOARD SEAT TRACK NR 11 HAS PITTING CORROSION STATION 10.5 TO 102.5, AROUND FORWARD CARGO PIT MOUNT S. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007051100207 20070511 00207 NM 2007 5 11 QXEA200700733 1 20070425 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - RIGHT HAND INBOARD SEAT TRACK NR 13 HAS DAMAGE ON TRACK AT STATION 450.0. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007051100208 20070511 00208 NM 2007 5 11 QXEA200700734 1 20070425 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - RIGHT HAND INBOARD SEAT TRACK NR 13 HAS CORROSION PITTING AT STATION 510 TO 550. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007051100209 20070511 00209 EU 2007 5 11 TRBA2007009 1 20070319 A 3350 LIGHT AEROSP ATR72 ATR72212A 8680902 EU PWA PW120 PW127 NE CABIN OUT OF POSITION A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 541AT 541 PERFORMING POST FLIGHT CREW NOTED STAIR EMERGENCY LIGHT INOPERATIVE. REPOSITIONED CENTER ENTRANCE LIGHT BULB IAW JIC 33 -20-00. TESTED SATISFACTORY. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007051100211 20070511 00211 NM 2007 5 11 07FDEA01705 1 20070504 A 5220 6396002 STOP FITTING BOEING 727 727200 138407E NM DOOR FRAME CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 MAIN DECK RT AFT OVER WING DOOR CUTOUT HAS 1 EA STOP PAD CRACKED AT FWD UPP POS BS 825 REMOVED AND REPLACED STOP PAD REF . 52-20-002-8 PG.1 2 L 7 3 4F RT A3WE 2007051100212 20070511 00212 WP 2007 5 11 07FDEA01706 1 20070504 A 5347 ADA765619 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 CABIN FLOOR SEAT TRACK GOUGED BETWEEN STA-1019 AND STA 1039 LBL 50. REMOVED AND REPLACED MAIN CABIN FLOOR SEAT TRACK A T LBL 50 FROM STA 1006 TO STA 1046 IAW DC/MD 10 SRM 53-70-00 FIG 1 VOL 1. 2 L 7 3 4F A22WE 2007051100213 20070511 00213 WP 2007 5 11 07FDEA01707 1 20070504 A 5347 4929150 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 MAIN CABIN SEAT TRACK WORN STA 635 BL 8.5. REMOVED AND REPLACED SEAT TRACK REF DC/MD 10 SRM 51-10-01 VOL III PG 85 53-7 0-00 VOL I FIG 1, 51-31-01 VOL II PG 4 , 51-33-01 VOL II PG 4. 2 L 7 3 4F A22WE 2007051100215 20070511 00215 WP 2007 5 11 07FDEA01751 1 20070510 A 5347 492914713500 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 MAIN DECK LT SIDE SEAT TRACK HAS CORROSION AT STA 1204 LBL 27. BLENDED AREA AND FOUND OUT OF LIMITS IAW DC10 SRM 53-70- 00 FIG 5 VOL I. REMOVED SEAT TRACK FROM STA 1049/1129 LBL 27 IAW DC10 SRM 53-70-00 FIG I VOL III, MAT ID FOR SEAT TRACK 4929147 IAW DC10 SRM 53-42-01 VOL III PAGE 7. FABRICATED DRILLED AND COUNTERSUNK SEAT TRACK AND SPLICES HAT AND PLATE IAW SRM 53-70-00 FIG 5 VOL I. ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL II PAGES 1-2. INSTALLED SEAT TRACK AND SPL ICES REPAIR IAW DC10 SRM 51-31-01 VOL II PAGE 2 CLASSIFIED AS MAJOR. 2 L 7 3 4F A22WE 2007051400002 20070514 00002 NM 2007 5 14 QXEA200700735 1 20070425 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - LEFT HAND INBOARD SEAT TRACK NR 5 HAS PITTING CORROSION AT STATION 60 TO 80. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007051400003 20070514 00003 NM 2007 5 14 QXEA200700737 1 20070425 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - LEFT HAND INBOARD SEAT TRACK NR 7 HAS PITTING CORROSION AT STATION 228.0 TO 280.07. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007050900175 20070509 00175 NM 2007 5 9 2007UALA01353 1 20070427 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 MAIN CABIN FLOORBEAM INTERCOSTAL UPPER ANGLE CRACKED AT STA 337, LBL 41. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKED AN GLE. FABRICATED & INSTALLED NEW ANGLE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050900177 20070509 00177 NM 2007 5 9 2007UALA01356 1 20070429 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 AFT EMERGENCY LIGHT ON SEAT 2F IS BROKEN. REPLACED LIGHT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007050900180 20070509 00180 2007 5 9 2007UALA01392 4 20070502 A 2565 BOTTLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EVAC SLIDE LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 174UA GS1370 24381 LOW BOTTLE PRESSURE. [SUP 05-16-07] SMALL PIN HOLE LEAK AROUND FILLER VALVE AND BAD O-RING. REPLACED O-RING AND FITTING CHARGE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050900196 20070509 00196 NM 2007 5 9 2007UALA01403 1 20070503 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY EXIT PATH LIGHTING FLASHES ON AND OFF ROW 54 AND AFT ON LEFT SIDE. REPLACED BATTERY ASSY, OP CHECKS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050900198 20070509 00198 NM 2007 5 9 2007UALA01405 1 20070504 A 3397 794640 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EEL 5E AFT, DOOR 5R TRAN AISLE & 44 HJK ARE INOPERATIVE. SECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050900204 20070509 00204 NE 2007 5 9 ARWA20070501 2 20070503 A 7230 BLADES DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE NR 1 COMPRESSOR DAMAGED A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET TO TAKEOFF 1 SO 19 450ML 47831 517829 JUST PRIOR TO ROTATION, DURING TAKEOFF ROLL, A/C SUDDENDLY BEGAN TO VIBRATE, AND DURING INITIAL CLIMB VIBRATION WAS DETE RMINED TO BE COMING FROM NR 1 ENGINE. ENGINE WAS SHUTDOWN. [SUP 06-01-07] PERFORMED FULL BOROSCOPE INSPECTION AND FOU ND COMPRESSOR SECTION BLADES TIP WITH SOME DENT WITH IN LIMITS IAW CF6-50 M/M 72-00-00. REMOVED AND REPLACED STG 1 FAN B LADES IAW DC-10-30 MM 72-21-00 AND R & R SPINNER IAW DC-10-30 M/M 72-21-00. ACCOMPLISHED VIBRATION CHECK AND FOUND NORMA L IAW DC-10-30 MM 72-00-00. MPA RUN CHECK NORMAL IAW DC-10-30 M/M 71-00-00. 2 L 7 3 4F 4 F RT A22WE E23EA 2007050900219 20070509 00219 SO 2007 5 9 C2XA07IA101 1 20070426 A 3350 110049 POWER SUPPLY EMB 145 EMB145XR 3260214 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27190 14500934 IAH - DURING MAINTENANCE INSPECTION THE GALLEY EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPR OVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007050900228 20070509 00228 NM 2007 5 9 SWAA072296 1 20070507 A 5311 6546560 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 947, STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007050900229 20070509 00229 NM 2007 5 9 SWAA072300 1 20070507 A 5330 6552988 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 972, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007050900233 20070509 00233 NM 2007 5 9 SWAA072294 1 20070507 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM L1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2007051000003 20070510 00003 EA 2007 5 10 TRAX200700619 1 20070504 A 2560 GLOWSTRIP CNDAIR CL600 CL6002C10 1390015 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 706EV 10054 EMERGENCY FLOOR PHOTOLUMINESCENT STRIPS BROKEN THROUGHOUT CABIN. [SUP 05-11-07] REMOVED AND REPLACED EMERGENCY FLOOR P HOTOILLUMINESCENT STRIPS THROUGHOUT CABIN IAW CRJ700 AMM 33-51-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007051000010 20070510 00010 EA 2007 5 10 TRAX200700610 1 20070503 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 SEAT RAIL CORRODED AT FS 559.00 + 80 AND RBL 27. [SUP 05-15-07] CORROSION ON SEAT RAIL AT F.S 559.00 +112 RBL 27 REMOV ED AS PER SRM 51-21-06. MATERIAL THICKNESS .100, MATERIAL REMOVED .032. OUT OF LIMITS AS PER SRM 53-61-49 FIG 101. N EW SEAT RAIL INSTALLED AT F/S 559.00 +112 RBL 27 AS PER SRM 51-42-02. 2 L 7 2 4F RT A21EA 2007051000021 20070510 00021 2007 5 10 CALA0700229 4 20070506 A 2565 63931134 SLIDE BOEING 757 757324 1384930 NM R1 DOOR LOW PRESSURE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 57857 10108 32816 INSPECTION FOUND THE R-1 DOOR SLIDE HAD LOW PRESSURE. THE SLIDE WAS REMOVED AND REPLACED IAW MM 25-66-01. 2 L 7 2 4F RT A2NM 2007051000046 20070510 00046 NM 2007 5 10 UPS07449766 1 20070507 A 5312 PRESSURE PANEL BOEING 747 747121 1384871 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:C ULTRASONIC INSP FOUND CRACK INDICATION AT BS 333 TO BS 334 BL 0 LEFT SIDE 1 INCH APPROX IN - LENGTH (C RACK LENGTH 0.68"). A REPAIR DOUBLER ADDED ON NOSE WHEEL WELL TOP PANEL UPPER SURFACE AT BTN BS 320 - BS 340 BL 0 IAW S RM 53-10-04 FIG 119 AS PER HX RS R53-18-35794 AND UPS EO B747-5310-26793. 2 L 7 4 4F A20WE 2007051000071 20070510 00071 NM 2007 5 10 UPS07M49663 1 20070205 A 5753 NRC6753504 STOP FITTING DOUG MD11 MD11F 3023600 NM T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:C RIGHT WING O/B FLAP MID STOP FITTING FOUND WITH CRACK AS MARKED. RIGHT WING O/B FLAP I/B & O/B HINGE ASSY, SIDE CARRIAGE & FLAP VANE TRACK REMOVED AS PER CMM 57-52-04 R.57. SEND OUT FOR REPAIR. RIGHT WING O/B FLAP VANE TRACK, SIDE CARRIAGE & I/B & O/B HINGE ASSY INSTALLED AS PER CMM 57-52-04 R.57. I/B & O/B HINGE FAIRING SUPPORTS INSTAL LED AS PER SRM 51-31-01 V.II R.38. ADJUSTMENT & TEST CARRIED OUT PER AMM 27-50-00 R.55. 2 L 7 3 4F RT A22WE 2007051000072 20070510 00072 NM 2007 5 10 SWAA072308 1 20070508 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 726SW 27858 DURING SCHEDULED MV2 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007051000073 20070510 00073 NM 2007 5 10 SWAA072340 1 20070508 A 3350 3071BPEGPL LIGHT BOEING 737 737317 138447P NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007051000074 20070510 00074 NM 2007 5 10 SWAA072347 1 20070508 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 214WN 32486 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 11 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007051000075 20070510 00075 NM 2007 5 10 SWAA072307 1 20070508 A 5610 5893543139 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT CRACKED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 29 650SW 27720 AT CRUISE FLIGHT DECK L1 WINDOW ARCHED AND CRACKED. REMOVED AND REPLACED L1 WINDOW PER MM. 2 L 7 2 4F RT A16WE 2007051000076 20070510 00076 2007 5 10 SWAA072349 4 20070508 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 773SA 27881 DURING SCHEDULED MV3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007051000077 20070510 00077 NM 2007 5 10 SWAA072350 1 20070508 A 5320 6545834 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED BRDG CHECK, FOUND FLIGHT DECK FLOOR WEB CRACKED AT FWD OUTBOARD LAPTOP MOUNT LOCATION. REPAIRED FLOOR WEB PER MM. 2 L 7 2 4F RT A16WE 2007051000078 20070510 00078 NM 2007 5 10 SWAA072318 1 20070508 A 5315 6545834 FLOORBEAM BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 294, LBL 13 TO RBL 12. REMOVED AND REPLACED FLOO RBEAM CHORD PER SRM. 2 L 7 2 4F RT A16WE 2007051000079 20070510 00079 NM 2007 5 10 SWAA072341 1 20070508 A 5311 6546525 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007051000080 20070510 00080 NM 2007 5 10 SWAA072339 1 20070508 A 5311 6546525 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007051000081 20070510 00081 NM 2007 5 10 SWAA072342 1 20070508 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007051000082 20070510 00082 NM 2007 5 10 SWAA072329 1 20070508 A 5322 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 10L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007051000083 20070510 00083 NM 2007 5 10 SWAA072343 1 20070508 A 5311 6546532 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007051000084 20070510 00084 NM 2007 5 10 SWAA072345 1 20070508 A 5322 6546536 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 616, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007051000085 20070510 00085 NM 2007 5 10 SWAA072346 1 20070508 A 5322 6546536 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 639, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007051000086 20070510 00086 NM 2007 5 10 SWAA072315 1 20070508 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007051000087 20070510 00087 NM 2007 5 10 SWAA072316 1 20070508 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 27R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007051000088 20070510 00088 NM 2007 5 10 SWAA072310 1 20070508 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 13L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007051000089 20070510 00089 NM 2007 5 10 SWAA072344 1 20070508 A 5311 6546550 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007051000090 20070510 00090 NM 2007 5 10 SWAA072322 1 20070508 A 5313 6546569 STRINGER SPLICE BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER S RM. 2 L 7 2 4F RT A16WE 2007051000091 20070510 00091 NM 2007 5 10 SWAA072321 1 20070508 A 5313 6546569 STRINGER SPLICE BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED ANAD REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007051000092 20070510 00092 NM 2007 5 10 SWAA072309 1 20070508 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007051000093 20070510 00093 NM 2007 5 10 SWAA072319 1 20070508 A 5311 6558280 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007051000094 20070510 00094 NM 2007 5 10 SWAA072311 1 20070508 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 13R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007051000095 20070510 00095 NM 2007 5 10 SWAA072326 1 20070508 A 5311 6558280 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007051000096 20070510 00096 NM 2007 5 10 SWAA072325 1 20070508 A 5311 65C25229 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007051000097 20070510 00097 NM 2007 5 10 SWAA072320 1 20070508 A 5311 65C25230 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007051000098 20070510 00098 NM 2007 5 10 SWAA072323 1 20070508 A 5754 65C266011 SLAT BOEING 737 7373L9 1384470 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND LEFT WING NR 1 L/E SLAT CRACKED AT LOWER INBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007051000099 20070510 00099 NM 2007 5 10 SWAA072317 1 20070508 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007051000100 20070510 00100 NM 2007 5 10 SWAA072314 1 20070508 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007051000101 20070510 00101 NM 2007 5 10 SWAA072312 1 20070508 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007051000102 20070510 00102 NM 2007 5 10 SWAA072313 1 20070508 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007051000103 20070510 00103 NM 2007 5 10 SWAA072328 1 20070508 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007051000104 20070510 00104 NM 2007 5 10 SWAA072330 1 20070508 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007051000105 20070510 00105 NM 2007 5 10 SWAA072331 1 20070508 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007051000106 20070510 00106 NM 2007 5 10 SWAA072332 1 20070508 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007051000107 20070510 00107 NM 2007 5 10 SWAA072333 1 20070508 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007051000108 20070510 00108 NM 2007 5 10 SWAA072334 1 20070508 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007051000109 20070510 00109 NM 2007 5 10 SWAA072335 1 20070508 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007051000124 20070510 00124 SO 2007 5 10 C2XA07IA115 1 20070504 A 2697 M8372375R1212N CONNECTOR EMB 145 EMB145XR 3260214 SO SMOKE DETECTION LOOSE A C2XA O OTHER N FALSE WARNING DE DESCENT 1 SW 27 11155 145782 AUS - FLIGHT 2793, THE CREW REPORTED A BAGGAGE SMOKE/FIRE WARNING LIGHT ILLUMINATED DURING DESCENT. THE AIRCRAFT LANDE D AT AUS WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND RESECURED A LOOSE CONNECTOR ON THE NUMBER TWO BAG GAGE SMOKE DETECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007051000125 20070510 00125 SO 2007 5 10 C2XA07IA114 1 20070416 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13949 7681 410 145057 BNA - DURING MAINTENANCE INSPECTION THE NUMBER TWO EMERGENCY LIGHT BATTERY WAS FOUND TO BE NOT HOLDING A CHARGE. MAINTE NANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007051000126 20070510 00126 SO 2007 5 10 C2XA07IA112 1 20070503 A 3350 78241 INVERTER EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15926 145005 IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE NUMBER TWO AND NUMBER THREE AISLE PATH LIGHT STRIPS TO BE INOPER ATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECT S, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007051100015 20070511 00015 NM 2007 5 11 DL76S070477 1 20070419 A 5315 HXB149953FT FLOORBEAM BOEING 767 767332 1382001 NM CABIN CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 128DL 24078 CABIN BS 325, 20 TO 25 FLOORBEAM UPPER SURFACE FOUND CORRODED REPAIRED ON NR 51553. 2 L 7 2 4F RT A1NM 2007051100017 20070511 00017 NM 2007 5 11 DL76S070482 1 20070419 A 5347 SEAT TRACK BOEING 767 767332 1382001 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 128DL 24078 CABIN BS 998 TO 999 RBL SEAT TRACK LWR FACE FOUND CRACKED. REPAIRED ON NR 515558. 2 L 7 2 4F RT A1NM 2007051100024 20070511 00024 NM 2007 5 11 ZZDA070507159 1 20070507 A 5320 FITTING BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933AT 55071 VHF ANTENNA MOUNT FITTING CORRODED BETWEEN STA 906 AND 927 AT 6 O'CLOCK. REMOVED AND REPLACED VHF ANTENNA MOUNT FITTING PER B717 SRM 51-41-02. 2 L 7 2 4F TR A6WE 2007051100039 20070511 00039 EA 2007 5 11 SWIA200718199 1 20070502 A 5610 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 770SK 10243 RIGHT SIDE WINDOW SHATTERED. REPLACED RIGHT SIDE WINDOW IAW CRJ 700 MM 56-12-01. P/N OFF 601R33033-24, S/N OFF 05238H9 811. 2 L 7 2 4F RT A21EA 2007051100053 20070511 00053 2007 5 11 VNAA0704010 4 20070419 A 3418 C16258AA SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STALL WARNING DAMAGED A VNAA O OTHER O OTHER CL CLIMB 1 GL 05 242JS 7358 7911 CREW REPORTED A LIGHTNING STRIKE ON CLIMBOUT. MAINTENANCE PERFORMED AN ENROUTE AND A DETAILED LIGHTNING STRIKE INSPECTI ON. AIRCRAFT WAS FERRIED TO DAYTON FOR REPAIR. MAINTENANCE INSPECTED AND REPAIRED ALL DAMAGE. MAINTENANCE ALSO REMOVE D AND REPLACED THE RIGHT HAND ANGLE OF ATTACK IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 27-35-05-000/400-801. OPS CHECKS GOOD AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007051100063 20070511 00063 2007 5 11 PNSA070402 4 20070415 A 3445 TRANSCEIVER SAAB SF340 340B 7860101 EU TCAS MALFUNCTIONED A PNSA O OTHER O OTHER CL CLIMB 1 AL 03 675PA 340B206 DURING CLIMBOUT TCAS INDICATE AN RA WITH NO TRAFFIC THEN ALERTED MULTIPLE TA'S WITH MULTIPLE RA'S TCAS DEFERRED OVER THE PHONE. REMOVED AND REPLACED RADAR TRANCEIVER OP'S CHECK OK. 2 L 7 2 4T RT A52EU 2007051100089 20070511 00089 2007 5 11 SWAA072351 4 20070505 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 605SW 27956 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007051100099 20070511 00099 NM 2007 5 11 AWXA200700573 1 20070410 A 5340 693535214 STRINGER CLIP BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - MAJOR REPAIR - C-20 CHECK - CRACKED STRINGER CLIP, BS 616, S2R. REPLACED STRINGER CLIP, BS 616, S2R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007051100100 20070511 00100 NM 2007 5 11 AWXA200700574 1 20070410 A 5753 654783813 SKIN BOEING 737 73733A 1384673 NM RT MIDFLAP CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - MAJOR REPAIR - C-20 CHECK - RIGHT WING INBOARD MIDFLAP LEADING EDGE CRACKED, WBL 163 AT CUTOUT FOR EXHAUST GATE UP PER LINKAGE. REPAIRED RIGHT WING INBOARD MIDFLAP LEADING EDGE CRACKED, WBL 163 AT CUTOUT FOR EXHAUST GATE UPPER LINKAGE IAW B737-300 SRM 57-53-01-2R2, FIGURE 201. 2 L 7 2 4F RT A16WE 2007051100122 20070511 00122 EU 2007 5 11 AWXA200700584 1 20070505 A 5315 D53472172204 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 665AW 1644 SAL - MAJOR REPAIR - BC-4 CHECK - CORROSION ON CABIN FLOORBEAM, FR 66 + 6 TO FR 67 + 16, +Y1162 TO +Y1292. REPLACED C ABIN FLOORBEAM, FR 66 + 6 TO FR 67 + 16, +Y1162 TO +Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007051100123 20070511 00123 EU 2007 5 11 AWXA200700585 1 20070503 A 5315 D5347218820400 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 665AW 1644 SAL - MAJOR REPAIR - BC-4 CHECK - CORROSION ON CABIN FLOORBEAM, FR 68 + 6 TO FR 69 + 4, +Y1162. REPLACED CABIN FLOORBE AM, FR 68 + 6 TO FR 69 + 4, +Y1162 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007051100124 20070511 00124 NM 2007 5 11 AWXA200700586 1 20070407 A 5743 65C365451 FITTING BOEING 737 73733A 1384673 NM LT WING CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - MAJOR REPAIR - C-20 CHECK - LEFT WING MAIN LANDING GEAR SUPPORT BEAM FITTING CRACKED, RSS 224. REPLACED LEFT WING MAIN LANDING GEAR SUPPORT BEAM FITTING, RSS 224 IAW AWA ER 03-5722-07128-SS1. 2 L 7 2 4F RT A16WE 2007051100156 20070511 00156 WP 2007 5 11 07FDEA01700 1 20070504 A 5230 FITTING DOUG DC10 DC1010 3022110 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 MAIN CARGO DOOR-LOWER SILL- NR 2 SPOOL LATCH-BACKUP FITTING- IS CRACKED. [SUP 05-18-07] REMOVED AND REPLACED NR 2 SPOOL LATCH BACKUP FITTING IAW DC/MD10 SRM 51-33-01. VOLII PAGE1 AND EA 8-5230-110682[FUSELAGE-MAIN CARGO DOOR LOWER JAMB FITTING INSPECTION AND DOOR RIG. MINOR REPAIR 2 L 7 3 4F A22WE 2007051100157 20070511 00157 WP 2007 5 11 07FDEA01701 1 20070504 A 5230 FITTING DOUG DC10 DC1010 3022110 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 MAIN CARGO DOOR-LOWER SILL-33 SPOOL LATCH-BACKUP FITTING IS CRACKED. [SUP 05-18-07] REMOVED AND REPAIRED NR 3 SPOOL B ACKUP FITTING IAW DC/MD10 SRM 51-33-01 AND EA 8-5230-110682. MINOR REPAIR 2 L 7 3 4F A22WE 2007051100158 20070511 00158 WP 2007 5 11 07FDEA01702 1 20070504 A 5230 FITTING DOUG DC10 DC1010 3022110 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 MAIN CARGO DOOR LOWER SILL NR 6 SPOOL LATCH BACKUP FITTING IS CRACKED. [SUP 05-18-07] REMOVED AND REPLACED NR 6 SPOOL LATCH BACKUP FITTING IAW DC/MD10 SRM 51-33- 01,PAGE 1 VOLII AND EA 8-5230-110682. MINOR REPAIR. 2 L 7 3 4F A22WE 2007051100161 20070511 00161 NM 2007 5 11 NWAA071763137 1 20070508 A 3350 32145410 EPSU AIRBUS A319 A319114 3930350 NM CABIN MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 337NB 20223 6920 1685 PERFORMED EMERGENCY ESCAPE LIGHT POWER SUPPLY TEST ON FWD L UNIT, FAULT ILLUMINATED. REPLACED FWD L EPSU, CHECKS OK. 2 L 7 2 4F RT A28NM 2007051100170 20070511 00170 NM 2007 5 11 C1HA200795021 1 20070504 A 5320 ANGLE BOEING 727 727290 138408W NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 ANGLE CORRODED RIGHT CUSP ANGLE TO FRAME SPLICE ATTACHED AFT SIDE OF STA 740 RIB AT FLOOR LEVEL STA 740-743 RBL 61. COR ROSION FOUND OUT OF LIMITS. REPLACED ANGLE IAW B727 SRM 53-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 2007051100193 20070511 00193 NM 2007 5 11 C1HA200795020 1 20070504 A 5313 STRINGER BOEING 727 727290 138408W NM FUSELAGE CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 FOUND STRINGER 15R CRACKED AT BS 720B. REPAIRED STR 15R AT BS 720B IAW B727 SRM 53-10-3 FIG 5. 2 L 7 3 4F A3WE 2007051100210 20070511 00210 NM 2007 5 11 07FDEA01704 1 20070504 A 5220 6396002 STOP FITTING BOEING 727 727200 138407E NM DOR FRAME CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 MAIN DECK RT RWD OVER WING DOOR CUTOUT HAS 4 EA CRACKED STOP PADS AT THE FOLLOWING POS: FWD UPP, AFT UPP, AFT MID, LWR B S 760-783. REMOVED AND REPLACED STOP PADS (4 EA) REF MM 52-20-002-8 PG1. 2 L 7 3 4F RT A3WE 2007051100214 20070511 00214 WP 2007 5 11 07FDEA01750 1 20070510 A 5347 493215412000 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 MAIN DECK LT SIDE SEAT TRACK HAS CORROSION AT STA 935 LBL 27. WORK ACCOMPLISHED IN CONJUNCTION WITH NON ROUTINE. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW DC10-MD10 SRM 53-70-00 VOL I FIG 5 FROM STA 905 TO STA 1005. CLASSIFIED AS MAJOR, R EPLACED SEAT TRACK AT LBL 27 STA 905 TO STA 1005 DC10/MD10 SRM 51-31-01 VOL II ALL SIGN OFFS ACCOMPLISHED ON NON ROUTINE DUE TO ANOTHER WRITE UP IN SAME TRACK. 2 L 7 3 4F A22WE 2007051400010 20070514 00010 NM 2007 5 14 QXEA200700731 1 20070425 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - RIGHT HAND INBOARD SEAT TRACK NR 12 HAS PITTING CORROSION STATION 102.5 TO 228.0. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007051400012 20070514 00012 NM 2007 5 14 QXEA200700732 1 20070425 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - RIGHT HAND INBOARD SEAT TRACK NR 13 HAS CORROSION PITTING AT STATION 228 TO 240. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007051400014 20070514 00014 NM 2007 5 14 QXEA200700728 1 20070425 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 19 HAS CORROSION IN CHANNEL AT FS X371 AND X388. REPAIRED IAW RD8/4-53-884 A ND SRM 51-40-10, 51-42-15, 51-42-05 AND 51-42-45. 2 H 7 2 4T RT A13NM 2007051400022 20070514 00022 NM 2007 5 14 07FDEA01711 1 20070507 A 5711 SPAR CAP BOEING 727 727225 1384077 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 465FE 21289 RT WING UPPER SURFACE AT SPOILER PANEL NR 11 AREA SPAR CAP HAS CRACK AROUND 3RD HINGE FITTING. NDT NOTED NO CRACKED PER NTM 51-00-00 PT6 (AFTER STOP DRILL). STOP DRILLED 0.025" HOLE AT THE END OF CRACKED IAW SRM 57-30-4 FIG10 SHEET 1/3. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER RT WING UPPER SURFACE AT SPOILER PANEL 11 AREA SPAR CAP IA W SRM 57-30-4 FIG 10 SHEET 1 AND 3, CLEANED LOWER AREA OF PANEL NR 11 SPOILER SPAR CAP IAW MM 12-40-000-2, PAGE 1 TO PAG E 14. MINOR REPAIR WING STA 464. 2 L 7 3 4F A3WE 2007051400023 20070514 00023 NM 2007 5 14 07FDEA01712 1 20070507 A 5420 BRACKET BOEING 727 727225 1384077 NM ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 465FE 21289 NR 3 PYLON HOLE "P" BRACKET CRACKED FWD OUTBD SEEN INSIDE PYLON AS PER STEP4. 2 ON W/C 7-5410-7-3304. REMOVED AND REPL ACED ANGLE( 69-16917-2) IAW SRM 51-30-2 AND 51-10-4. NDT CHECKED "P" HOLE FOR CRACK AND NO CRACK NOTED IAW NTM 51-00-11 . 2 L 7 3 4F A3WE 2007051400026 20070514 00026 NM 2007 5 14 07FDEA01734 1 20070510 A 5320 WEB DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 FOUND UPPER CARGO DOOR CUTOUT, LOWER SILL'S WEB CORRODED AT STA 660. [SUP 05-22-07] REPAIR CARRIED OUT AT UPPER CARGO DOOR CUTOUT, LOWER SILL'S WEB, STA 660 AS PER FEDEX EA 1-5310-111100. 2 L 7 3 4F RT A22WE 2007051400028 20070514 00028 WP 2007 5 14 07FDEA01736 1 20070510 A 5347 AGA38555 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 AFT LOWER CARGO, CORROSION AT TIEDOWN SEAT TRACK SURFACE AND AT NUT PLATES HOLES UPPER AND LOWER SURFACES, FS 1790-167 L BL 21". REMOVED DAMAGE SEAT TRACK SECTIONS AND FABRICATED NEW SECTIONS AND SPLICES IAW MD/DC 10 SRM 53-70-00 FIG 1 VOL I. ALODINED AND PRIMED IAW MD/DC 10 SRM 51-21-01-VOL II. INSTALLED IAW MD/DC 10 SRM 53-70-00 FIG1 VOL I, AND 51-31-01 VOL II. THIS IS A MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2007051400029 20070514 00029 EU 2007 5 14 07FDEA01737 1 20070510 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 410FE 356 FWD CARGO COMP MDCC FLOORBEAM C33 HAS A CRACK BETWEEN SEAT TRACKS 4L AND 5L, CRACK LENGTH .125. REMOVED CRACK FROM FLO ORBEAM PER SRM 53-10-15; FABBED 2 REPAIR ANGLES PER SRM 50-40-21; ALODINED, PRIMED, TOPCOATED PER SRM 51-75-10; INSTALLE D REPAIR PARTS PER SRM 53-10-15 FIG 20, SH 2A. 2 L 7 2 4F RT A35EU 2007051400030 20070514 00030 EU 2007 5 14 07FDEA01738 1 20070510 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 6 AREAS OF CORROSION EXIST AT MDCC SEAT TRACK NR 1 BETWEEN FRAMES 61 THRU 71/72 EACH AREA MEASURES 1.25 SQ INCHES. REMO VED CORROSION ON SEAT TRACK IAW A310-200 SRM 51-74-10 3 AREAS FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-16 PB 101 . ALODINED, PRIMED, AND TOPCOATED, 3 AREAS IAW A310-200 SRM 51-21-10 AND 51-75-10. REPLACED TRACK SECTION FOUND TO BE OUT OF LIMITS IAW A310-200 SRM SUP 53-10-16 FIG 202. 2 L 7 2 4F RT A35EU 2007052400089 20070524 00089 NM 2007 5 24 SWAA072559 1 20070521 A 5753 6546435 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER SURFACE. REPAIRED FLAP P ER SRM. 2 L 7 2 4F RT A16WE 2007051400031 20070514 00031 WP 2007 5 14 07FDEA01740 1 20070510 A 5711 SPAR CAP DOUG DC10 DC1010 3022110 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 LEFT WING UPPER SPAR CAP HAS CORROSION MIGRATING UNDER SKIN PLATE AT XORS 645-671. [SUP 05-16-07] REMOVED CORROSION F OUND TO BE WITHIN LIMITS IAW FEDEX E.A 8-5710-109150 STEP 3 (LT WING CORROSION BETWEEN XORS=412-800- REPAIR). ALODIN ED AND PRIMED IAW DC10 SRM 51-21-01 VOL II. MINOR REPAIR. 2 L 7 3 4F A22WE 2007051400032 20070514 00032 WP 2007 5 14 07FDEA01718 1 20070508 A 5347 S4929150 SEAT TRACK DOUG DC10 DC1010F 3022111 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 MAIN DECK SEAT TRACK HAS GOUGE AND WORN AT STA 1016 LBL 8. REMOVED, FABRICATED, INSTALLED SEAT TRACK SECTION IAW DC/MD1 0 SRM 53-70-00 VOL I FIG 5 SHT 5, 53-70-00 VOL I FIG 1 PAGE 3-6A. MAJOR REPAIR. 2 L 7 3 4F A22WE 2007051400033 20070514 00033 WP 2007 5 14 07FDEA01719 1 20070508 A 5312 TEE FITTING DOUG DC10 DC1010F 3022111 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 AFT PRESSURE BULKHEAD TEE FITTING CORRODED AT STA 2007 BL 0. REMOVED DAMAGE AND REPAIRED TEE FITTING IAW MD/DC10 SRM 53 -40-00 VOL I FIG 16 PAGE 93. 2 L 7 3 4F A22WE 2007051400034 20070514 00034 NM 2007 5 14 QXEA200700772 1 20070428 A 5260 TRACK BOMBDR DHC8 DHC8402 1390042 NM AFT STAIRS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - INBOARD SUPPORT FLANGE ATTACHED TO AFT ENTRY FOLDING STAIR INBOARD TRACK IS CORRODED ON UPPER SURFACE. REPAIRE D IAW SRM 51-25-10, 51-21-00, 51-21-10, 51-14-00. 2 H 7 2 4T RT A13NM 2007051400035 20070514 00035 NM 2007 5 14 QXEA200700766 1 20070429 A 5311 FRAME BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - STRUCTURE FRAME CASTELLATION IS CORRODED AT STATION X7.0, Y4.0L, Z94.0, BELOW MAIN CABIN DOOR LAY SHAFT. REPAI RED IAW SRM 51-21-00, 51-21-10, 51-25-05. 2 H 7 2 4T RT A13NM 2007051400036 20070514 00036 NM 2007 5 14 QXEA200700768 1 20070425 A 5320 SUPPORT BRACKET BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - UPPER AFT SUPPORT BRACKET IS CRACKED LOCATED X747.602 RIGHT HAND SIDEWALL AND STRINGER 20R. REPAIRED IAW SRM 5 1-20-10, 51-25-10, AND 51-42-00. 2 H 7 2 4T RT A13NM 2007051400039 20070514 00039 NM 2007 5 14 07FDEA01722 1 20070509 A 5755 651734781 SKIN BOEING 727 7272S2F 1384O81 NM NR 4 SPOILER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 FOUND UPPER WING CUTOUT FOR NR 4 SPOILER HINGE HAS TWO SMALL CRACKS, LOCATION OF HINGE IS SECOND HINGE INBOARD END OF SP OILER. STOPPED DRILLED ENDS OF CRACK AND INSTALLED DOUBLER REF SRM 57-30-4/ FIGURE NR 10 PAGES 27-31. 2 L 7 3 4F A3WE 2007051400040 20070514 00040 NM 2007 5 14 07FDEA01723 1 20070509 A 5530 69708044 WEB BOEING 727 7272S2F 1384O81 NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 VERTICAL STAB ELEVATOR FEEL CONTROL UNIT PLATFORM ASSY FWD LT VERTICAL WEB CRACKED ON INTERNAL SIDE AT THE 2 MOST FWD LW R FASTENERS. REPLACED LT VERTICAL WEB ON VERT STAB ELEVATOR FEEL CONTROL UNIT PLATFORM. REF SRM 51-30-2 PG 1-12. 2 L 7 3 4F A3WE 2007051400041 20070514 00041 WP 2007 5 14 07FDEA01724 1 20070509 A 5730 SKIN DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 397FE 46631 MD 10-10 ACF MODIFICATION AND REPAIR ASSESTMENT RT WING LEADING EDGE STA XORS 506 LOWER SIDE CLOSE TO PANEL FUEL PANEL, SKIN WITH CRACK OF ABOUT 2 INCH REMOVED ACCESS DOOR, REPAIRED FIXED L.E IAW SRM 57-10-00 FIG 68 SHEETS 2 AND 3. INST ALLED ACCESS DOOR. PERFORMED CHECK AMM 27-30-06-06. 2 L 7 3 4F A22WE 2007051400044 20070514 00044 WP 2007 5 14 07FDEA01728 1 20070509 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 397FE 46631 ACF MODIFICATION AND REPAIR ASSESSMENT\AFT CARGO COMPT TUNNEL SIDE RT: STA 1801-1821 NICK ON THE LONGERON 27 PERFORMED B LEND-OUT AND CHECK LIMITS IAW SRM 53-00-01 FIG 1 B. INSTALLED ANGLE AND EXISTING STRAP IAW SRM 53-00-01 FIG 7 AND SRM 5 1-33-01 VOL. II. PROTECTED IAW SRM 51-21-01 VOL II. 2 L 7 3 4F A22WE 2007051400045 20070514 00045 WP 2007 5 14 07FDEA01729 1 20070509 A 5322 SHEAR TIE DOUG DC10 DC1010 3022110 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 397FE 46631 MD 10-10 ACF MODIFICATION AND REPAIR ASSESSMENT AFT CARGO COMPARTMENT: MISSING MATERIAL AND CORROSION ON SHEAR CLIP STA 1956 B/T L 48 TO L 50 LT SIDE REMOVED CLIPS ATTACHING FOR ACCESS: REMOVED INTERCOSTAL AND RIVETS, CUT OUT SHEAR CLIP DAM AGED, CLEANED EXCESS OF SEALANT, TREATED AREA. REPAIRED SHEAR CLIP AND REINSTALLED ALL PARTS REMOVED FOR ACCESS AND PAI NTED WITH HIGH IMPACT PAINT. 2 L 7 3 4F A22WE 2007051400049 20070514 00049 NM 2007 5 14 QXEA200700764 1 20070425 A 5320 THRESHOLD BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - FORWARD CARGO DOOR AT BOTTOM THRESHOLD ON FUSELAGE IS CORRODED AT X17.850. REPAIRED IAW SRM 51-14-00, 51-21-00 , 53-20-25. 2 H 7 2 4T RT A13NM 2007051400050 20070514 00050 NM 2007 5 14 QXEA200700765 1 20070425 A 5312 PRESSURE BLKHD BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - NOSE LANDING GEAR LOWER FORWARD PRESSURE BULKHEAD IS CHAFED AT X111.000. REPAIRED IAW RD8/4-53-1224. 2 H 7 2 4T RT A13NM 2007051400052 20070514 00052 EU 2007 5 14 200705111 1 20070507 A 2751 59128437 SENSOR EMB ERJ170 ERJ170100SE 3260406 EU LEFT DEFECTIVE A UHLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 11 856RW 17000078 FLIGHT 6472 DFW TO JFK AFTER DEPARTING DFW IN CRUISE FLIGHT THE CREW RECEIVED AN AMBER FLAP FAILURE EICAS WARNING. DIVE RT TO IND AND DECLARED AN EMERGENCY. MAINTENANCE REMOVED AND REPLACED THE LEFT O/B T4 SKEW SENSOR. 2 L 7 2 4F RT A56NM 2007051400053 20070514 00053 SO 2007 5 14 C2XA07RI030 1 20070507 A 3350 SIGN EMB 145 EMB145LR 3260212 SO CABIN LOOSE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 13992 145284 FLT 2964 - EWR - CREW REPORTED EMERGENCY LIGHT SIGN ABOVE ROW 12 INOPERATIVE. EWER MX RESECURED EXIT SIGN AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007051400055 20070514 00055 WP 2007 5 14 07FDEA01741 1 20070510 A 5711 SPAR CAP DOUG DC10 DC1010 3022110 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 LEFT WING REAR SPAR CAP HAS CORROSION MIGRATING UNDER WING SKIN AT ST XORS 600-606. [SUP 05-16-07] REMOVED CORROSION I AW DC10 SRM 51-21-01 VOLII ,ORIG THICKNESS .300 REMAINING .290 FOUND TO BE WITHIN LIMITS IAW 57-20-00 VOLII.REMOVED A ND REPLACED FASTENERS,ALODINED AND PRIMED IAW DC10 SRM 51-33-01 VOL II,51-21-01. MINOR REPAIR. 2 L 7 3 4F A22WE 2007051400056 20070514 00056 WP 2007 5 14 07FDEA01742 1 20070510 A 5711 SPAR CAP DOUG DC10 DC1010 3022110 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 LEFT WING UPPER REAR SPAR CAP HAS CORROSION ON AFT UPPER SURFACE AT XORS 480-490. [SUP 05-16-07] REMOVED CORROSION FOU ND TO BE WITHIN LIMITS IAW FEDEX E.A. 8-57-109150 STEP 2 (LT WING CORROSION BETWEEN XORS=480-800)ALODINED AND PRIMED DC1 0 SRM 51-21-01 VOL II. MINOR REPAIR. 2 L 7 3 4F A22WE 2007051400057 20070514 00057 WP 2007 5 14 07FDEA01743 1 20070510 A 5311 FRAME DOUG DC10 DC1010 3022110 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 AFT CARGO COMPARTMENT AT STA 1942 FROM L51L TO L51R FRAME HAS CORROSION. REMOVED AND REPLACED STIFFENERS IAW DC/MD10 SR M 51-31-01 AND 51-33-01. AFTER CORROSION REMOVAL. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC/MD10 SRM 53-30-00 FIG 8 VOL I. 2 L 7 3 4F A22WE 2007051400058 20070514 00058 WP 2007 5 14 07FDEA01744 1 20070510 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 MAIN DECK SEAT TRACK SCALLOP WORN STA 1356 RBL47 REMOVED, FABRICATED AND INSTALLED SEAT TRACK SPLICE PLATE AND HAT SECTI ON IAW DC/MD10 SRM 51-33-01 VOL II PAGE 1-30 AND 53-70-00 VOL I PAGE 3-6. 2 L 7 3 4F A22WE 2007051400060 20070514 00060 WP 2007 5 14 07FDEA01746 1 20070510 A 5347 493215412000 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 FOUND CORROSION ON SEAT TRACK FROM STA 695 TO 735 LBL28. REMOVED, FABRICATED, AND INSTALLED SEAT TRACK SECTION IAW DC/M D10 SRM 53-70-00 VOL I FIG 1 SHT 1 AND 53-70-00 VOL1 FIG 5 SHT 2 AND 51-21-01 VOL II. 2 L 7 3 4F A22WE 2007051400061 20070514 00061 WP 2007 5 14 07FDEA01747 1 20070510 A 5347 WDA70047 SEAT TRACK DOUG DC10 DC1010F 3022111 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 FOUND MAIN DECK SEAT TRACK SCALLOP WORN STA 1777 RBL 27. REMOVED, FABRICATED, AND INSTALLED SEAT TRACK SECTION DC/MD10 SRM 53-42-01 VOL III FIG 5 AND 53-70-00 VOL I FIG 1 SHT 1 AND 51-21-01 VOL II PAGE 21, 25. 2 L 7 3 4F A22WE 2007051400062 20070514 00062 WP 2007 5 14 07FDEA01748 1 20070510 A 5347 S49915012000 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 FOUND MAIN DECK LEFT SIDE SEAT TRACK SCALLOP WORN AT STA 1265 LBL 8. REMOVED, FABRICATED, AND INSTALLED SEAT TRACK SECT ION IAW DC/MD10 SRM 53-70-00 VOL I FIG 5 SHT 1 AND 53-42-01 VOL III PAGE 5. 2 L 7 3 4F A22WE 2007051400065 20070514 00065 WP 2007 5 14 07FDEA01753 1 20070510 A 5347 4929150 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 1248-1351 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 MAIN DECK SEAT TRACK SCALLOP WORN STA 1300 RBL 27 BLENDED AND FOUND TO BE OUT OF LIMITS PER MD10/DC10 SRM 53-70-00 VOL I PG 21. REMOVED SEAT TRACK SECTION RBL 27 STA 1248 TO STA 1351 PER MD10/DC10 SRM 53-70-00 VOL I PG 21. SEAT TRACK MA TERIAL IS 4929150 PER MD/DC10 SRM 53-42-01 PG 13 FIG 5 VOL III. SCALLOPED SEAT TRACK PER DC10 SRM 53-70-00 VOL I MATERI AL ID FOR SPLICE HAT 4932154-1200 PO NR 570758-3 AND SPLICE PLATE 7075-T6 .050" PO NR 57122.5 PER MD 10 DC10 SRM 53-70-0 0 FIG I VOL I. FABRICATED SEAT TRACK, SPLICE PLATE AND SPLICE HAT PER MD10/DC10 SRM 53-70-00 VOL I. ALODINED AND PRIME D SEAT TRACK, SPLICE PLATE SPLICE HAT PER MD/DC10 SRM 51-21-01 PG 1 VOL I. 2 L 7 3 4F A22WE 2007051400067 20070514 00067 2007 5 14 UPS07149777 4 20070508 A 2565 SLIDE AIRBUS A300 A300F4622R 3930360 EU CARGO DOOR UNWANTED DEPLOY A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 143UP 0826 INSPECTION TYPE:N/A SLIDE DEPLOYED WHEN CLOSING MAIN CARGO DOOR PRIOR TO BLOCKOUT. INSTALLED NEW SLIDE IAW M/M 25-61-21 -04. SERVICED FWD DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IAW M/M 52-10-14-03. THIS CLEARS M-350038. 2 L 7 2 4F RT A35EU 2007051400068 20070514 00068 NM 2007 5 14 UPS07549783 1 20070511 A 2120 UNKNOWN BOEING 757 75724APF 1384969 NM COCKPIT SMOKE A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 01 464UP 28268 DECLARED AN EMERGENCY DUE TO CREW REPORTING SMOKE IN THE COCKPIT. [SUP 05-14-07] ACCOMPLISHED AMM 05-51-14-2 HIGH ENER GY STOP INSP. FOUND NO FAULTS ON TIRES CONDITION AND BRAKE OPERATION. REF LOG PAGE 587368 ITEM 3. OPERATED APU & ENGINES FOR EVIDENCE OF OIL IN BLEED SYST. NO FAULTS FOUND.RAN L&R PACKS NO EVIDENCE OF SMOKE SMELL.INSP WINDOW HEAT TERM NO EV IDENCE OF SHORTS.INSP CARGO COMPTS & E&E OK FOR SERVICE. SUSPECT SMOKE FROM FLORIDA GROUND FIRES 2 L 7 2 4F RT A2NM 2007051400069 20070514 00069 EA 2007 5 14 TRAX200700634 1 20070503 A 5320 PLATE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 FLOOR LANDING GEAR PLATE CORROSION BETWEEN FS 559.00 +112 TP 612.00 LBL 45.00 AROUND NUT PLATE HOLES. 2 L 7 2 4F RT A21EA 2007051400070 20070514 00070 EA 2007 5 14 TRAX200700635 1 20070503 A 5320 PLATE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 CORROSION ON 3 PLATES BETWEEN FS 574.00 TO 621.00 AND 3 SEALS MISSING. [SUP 05-15-07] CORROSION REMOVED ON 3 PLATES B ETWEEN FS 574.00 TO 621.00 IAW SRM 51-21-06. ALODINE APPLIED IAW SRM 51-21-11. FINISH AREA IAW SRM 51-21-16. GASKETS (3) INSTALLED ON 3 PLATES BETWEEN FS 574.00 TO 621.OO IAW SRM 51-41-04. MATERIAL THICKNESS .063, MATERIAL REMOVED .003, WITHIN LIMITS PER SRM 53-00-00. 2 L 7 2 4F RT A21EA 2007051400072 20070514 00072 EA 2007 5 14 TRAX200700637 1 20070507 A 5610 WINDSCREEN CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA K NONE O OTHER CR CRUISE 1 SO 27 906EV 7642 PILOT SIDE FRONT WINDSCREEN CRACKED DURING FLIGHT AT 12,000 FT MSL. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007051400074 20070514 00074 EA 2007 5 14 COMA0770027 1 20070504 A 5244 DOOR CNDAIR CL600 CL6002C10 1390015 EA COMM DOOR OPEN A COMA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 641CA 10122 FLIGHT 5192 - COMM HATCH ON NOSE LEFT OPEN. RETURNED TO AIRPORT, FOUND NO DAMAGE, RESECURED DOOR, NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007051400076 20070514 00076 EA 2007 5 14 COMA0760354 1 20070501 A 3297 17300233 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING FAULTY A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 420CA 7451 FLIGHT 5293 - NWS INOP ON SHORT FINAL, WOULD NOT RESET. REMOVED AND REPLACED NLG STEERING HARNESS. 2 L 7 2 4F RT A21EA 2007051400087 20070514 00087 NM 2007 5 14 HNAA0700077 1 20070421 A 2997 M8372395R1005N WIRE DHAV DHC8 DHC8102 2809003 NM HYDRAULIC SYS CHAFED A HNAA O OTHER N FALSE WARNING CL CLIMB 1 EA 07 838HA 35366 35366 220 NR 2 HYDRAULIC ISO VALVE CAUTION LIGHT ILLUMINATED ON CLIMBOUT. HYDRAULIC PRESSURE AND QUANTITY NORMAL. UPON GEAR EXTE NSION, OUTBOARD ROLL SPOILER HYDRAULIC CAUTION LIGHT ILLUMINATED. AIRCRAFT LANDING DECLARED AN EMERGENCY, AIRCRAFT LAND ED SAFELY. INSPECTED AIRCRAFT FOR LEAKS, NONE FOUND. CHECKED NR 2 QUANTITY LEVEL AT 4.5, INSPECTED ISOLATION SWITCH AN D NO DEFECTS NOTED. OPS CHECKED NR 2 ISO IAW WORK CARD 29-20-10 OPS CHECK GOOD. PERFORMED EVALUATION FLIGHT, EVALUATIO N FLIGHT SATISFACTORY. ON 25 APRIL THE ENGINE DRIVEN HYDRAULIC PUMP CAUTION LIGHT CAME ON IN FLIGHT, CAUTION LIGHT MEL' D. 27 APRIL 2007 FOUND WIRES CHAFING. REPLACED CONNECTOR ON HYDRAULIC SYSTEM PRESSURE TRANSMITTER AND SPU LOW PRESSURE 2 H 7 2 4T RT A13NM 2007051000129 20070510 00129 SO 2007 5 10 C2XA07RI029 1 20070506 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN SMOKE A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 14950 145061 FLT 2438 - ORF - CREW REPORTED SMOKE IN CABIN. PACK NR 1 SYSTEM WAS MELED. MX IAH PERFORMED OPERATIONAL CHECK OF PACK SYSTEMS 1 AND 2 AND COULD NOT DUPLICATE THE PROBLEM. OPERATIONAL AND FUNCTIONAL CHECKS WERE PERFORMED SUCCESSFULLY. AC FT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007051000130 20070510 00130 SO 2007 5 10 C2XA07IA113 1 20070428 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13914 145430 MCI - DURING MAINTENANCE INSPECTION THE AFT OVERWING EMERGENCY EXIT LOCATOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007051100004 20070511 00004 NM 2007 5 11 ASMF200705004 1 20070506 A 2910 LINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE HYD SYSTEM LEAKING W ASMF D RETURN TO BLOCK K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 23 169PL 53175 AIRCRAFT RETURNED TO PLATFORM DUE TO SMOKE ODOR IN PASSENGERS CABIN. A HYDRAULIC LEAK WAS DETECTED IN THE APU INLET DUCT . THE HYDRAULIC LEAK WAS REPAIRED AND WATER SEPARATORS WERE REPLACED IAW MM 21-20-02, TESTED CORRECT. DURING BOARDING, T HE HYDRAULIC ODOR WAS PRESENT AGAIN AND FLIGHT WAS CANCELLED. DURING OVERNIGHT CHECK, THE AFT ACCESSORIES COMPARTMENT WA S CHECKED DETECTING A HYDRAULIC LEAK IN THE RETURN LINE OF THE LT HYDRAULIC SYSTEM. HYDRAULIC RETURN LINE WAS REPLACED I AW MM 20-10-03 TESTED CORRECT. DURING OVERNIGHT CHECK, A NEW HYDRAULIC LEAK WAS DETECTED IN THE STEERING HYDRAULIC LINE. THE STEERING HYDRAULIC LINE, APU AND TEMPERATURE CONTROL VALVE WERE REPLACED IAW MM 20-10-03, 49-00-01 AND 21-20-03, TE 2 L 7 2 4F 4 F RT A6WE E9NE 2007051100074 20070511 00074 EA 2007 5 11 VNAA0704014 1 20070418 A 2150 32156222 REGULATOR VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT A/C PACK FAILED A VNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 05 241PS 6708 7909 CREW REPORTED THE LEFT PACK BLOWING SMOKE ON FLIGHT DECK. MAINTENANCE INSPECTED AND DEFERRED THE LEFT HAND AIR CONDITIO NING PACK PER MEL 21-51-01. MAINTENANCE REMOVED AND REPLACED THE PRESSURE REGULATING VALVE IN ACCORDANCE WITH THE AIRCR AFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007051100078 20070511 00078 NM 2007 5 11 SWAA072354 1 20070509 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER AFT CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007051100082 20070511 00082 NM 2007 5 11 SWAA072352 1 20070509 A 3350 65C27093 LIGHT BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007051100097 20070511 00097 EU 2007 5 11 AWXA200700571 1 20070507 A 3397 D9299200900200 GROUND WIRE AIRBUS 320 A320231 3930325 EU CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 629AW 076 PHX - EEL - SEAT ROW 11R EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. RECONNECTED GROUND WIRE ON BACK OF THE EMERGENCY ESCA PE PATH LIGHT HOUSING AT SEAT ROW 11R AND OPERATIONAL CHECKED IAW A320 AMM 33-51-00. 2 L 7 2 4F RT A28NM 2007051100098 20070511 00098 NM 2007 5 11 AWXA200700572 1 20070419 A 5313 65457679 STRINGER BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - C-20 CHECK - CRACKED STRINGER, BS 500C, S16R. REPAIRED STRINGER, BS 500C, S16R IAW AWA ER 03-5312- 01094-DD1. 2 L 7 2 4F RT A16WE 2007051100107 20070511 00107 EU 2007 5 11 AWXA200700579 1 20070509 A 5321 D5367161500000 FLOORBOARD AIRBUS 320 A320231 3930325 EU CABIN DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 625AW 064 PHX - MAJOR REPAIR - CABIN FLOORBOARD 241EF IN CENTER AISLE IS DELAMINATED AT SEAT ROW 12. REPLACED CABIN FLOORBOARD 24 1EF IN CENTER AISLE AT SEAT ROW 12 IAW AWA TASK CARD R1C25306. 2 L 7 2 4F RT A28NM 2007051100109 20070511 00109 EA 2007 5 11 TRAX200700632 1 20070506 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 901EV 7616 LEFT EMERGENCY EXIT LIGHT FWD OF PAX DOOR IS INOP. 2 L 7 2 4F RT A21EA 2007051100113 20070511 00113 NM 2007 5 11 AWXA200700562 1 20070410 A 5311 90526913 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - MAJOR REPAIR - C-20 CHECK - CRACKED FUSELAGE FRAME, BS 727C, S9R. REPAIRED FUSELAGE FRAME, BS 727C, S9R IAW B737- 300 SRM 53-00-07-2R2, FIGURE 201. 2 L 7 2 4F RT A16WE 2007051100114 20070511 00114 NM 2007 5 11 AWXA200700563 1 20070410 A 5311 90526913 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - MAJOR REPAIR - C-20 CHECK - CRACKED FUSELAGE FRAME, BS 727E, S9L. REPAIRED FUSELAGE FRAME, BS 727E, S9L IAW B737- 300 SRM 53-00-07-2R2, FIGURE 201. 2 L 7 2 4F RT A16WE 2007051100121 20070511 00121 EU 2007 5 11 AWXA200700583 1 20070506 A 5315 D53472172205 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 665AW 1644 SAL - MAJOR REPAIR - BC-4 CHECK - CORROSION ON CABIN FLOORBEAM, FR 66 + 6 TO FR 67 + 16, -Y1292. REPLACED CABIN FLOORBE AM, FR 66 + 6 TO FR 67 + 16, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007051100168 20070511 00168 NM 2007 5 11 MWEA070108 1 20070511 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 917ME 55179 RIGHT THRUST REVERSER, UPPER DEFLECTOR DOOR HAS A CRACK ON END OF ZEE FRAME, INBOARD SIDE AT STATION 26.666. INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007051100169 20070511 00169 NM 2007 5 11 NWAA071735649 1 20070505 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 549US 26496 DURING LINE CHECK FOUND DOOR L1 EMERGENCY EXTERIOR LIGHT INOPERABLE. RELAMPED, NO HELP. INSTALLED EMERGENCY BATTERY PA CK AND POWER SUPPLY PER AMM 33-51-07. OPS CHECK NORMAL. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2007051100171 20070511 00171 NM 2007 5 11 C1HA200795001 1 20070504 A 5720 ANGLE BOEING 727 727290 138408W NM RT WING CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 RIGHT WING L/E STA 130.7 INTERNAL ANGLE AT FRONT SPAR LWR CRACKED. FABRICATED AND INSTALLED REPAIR PART IAW B727 M/M 57 -20-21 PG 801 AND SEALED AS REQUIRED IAW B727 M/M 51-30-11. 2 L 7 3 4F A3WE 2007051100176 20070511 00176 NM 2007 5 11 C1HA200795008 1 20070504 A 5347 15207927178T65 SEAT TRACK BOEING 727 727290 138408W NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 CORROSION ON SEAT TRACK BS 420-480 RBL 55. REPLACED SEAT TRACK FROM BS 420 TO 480 RBL 55 IAW B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 7. 2 L 7 3 4F A3WE 2007051100182 20070511 00182 NM 2007 5 11 CIHA200759026 1 20070504 A 5320 SUPPORT ANGLE BOEING 727 727290 138408W NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 295AS 22147 STRINGER 26L TO FRAME SUPPORT ANGLE CORRODED BS 950F. REMOVED SUPPORT ANGLE, FABRICATED AND INSTALLED NEW SUPPORT ANGLE IAW B727 SRM 51-10-3 FIG 2 & 51-30-2 FIG 1. 2 L 7 3 4F A3WE 2007051100197 20070511 00197 EA 2007 5 11 QXEA200700773 2 20070508 A 7261 OIL SYSTEM BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA NR 2 ENGINE OVERSERVICED A QXEA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NM 09 404QX 4046 SEA FLIGHT 2380: ON FINAL APPROACH WHEN POWER WAS REDUCED TO FLIGHT IDLE, A SMELL OF OIL OF EXHAUST WAS COMING FROM AIR VENTS IN COCKPIT AND CABIN. AIRCRAFT WAS FERRIED TO PDX. MAINTENANCE C/W COMPRESSOR AND TURBINE WASH OF THE NR 2 ENGIN E IAW Q400 AMM TASK 72-00-00-160-805. RAN ENGINES THROUGHOUT ALL POWER RANGES WITH BLEEDS SELECTED ON AND OFF. NO SMEL L NOTED. PRIOR TO ENGINE WASH, NR 2 ENGINE WAS OVER SERVICED WITH APPROX 2 QUARTS OF ENGINE OIL. NO FURTHER DEFECTS NO TED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2007051100216 20070511 00216 WP 2007 5 11 07FDEA01708 1 20070506 A 5347 AEA73257 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 CABIN FLOOR SEAT TRACK GOUGED AT STA 1161 TO STA 1171 LBL 48. REMOVED AND REPLACED CABIN SEAT TRACK FROM STA 1129 TO S TA 1189, LBL 48 IAW DC/MD10 SRM 53-70-00 FIG 1, VOL 1. 2 L 7 3 4F A22WE 2007051100217 20070511 00217 WP 2007 5 11 07FDEA01709 1 20070506 A 5347 ACA73991 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 CABIN FLOOR SEAT TRACK LUG BROKEN OUT AT STA 635 LBL47. REMOVED AND REPLACED CABIN FLOOR SEAT TRACK SECTION FROM STA 62 2 TO STA 746 LBL47 IAW DC/MD10 SRM 53-70-00 FIG 5 , VOL 1. 2 L 7 3 4F A22WE 2007051400020 20070514 00020 NM 2007 5 14 QXEA200700769 1 20070427 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - NR 10 SEAT TRACK HAS CORROSION ON FLANGE AT AFT SPLICE. REPAIRED IAW SRM 51-40-15, RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007051400025 20070514 00025 NM 2007 5 14 07FDEA01733 1 20070509 A 2450 ELECTRICAL SYS BOEING 727 727233 138408A NM E-1 CONTAMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 282FE 22349 AT ROTATION, ESSENTIAL POWER FAIL LIGHT CAME ON MOMENTARILY THEN WENT OUT WITH NR 1 GENERATOR FAIL. UNABLE TO BRING NR 1 BUSSSM20ACD200A2 ON LINE. LOST THE FOLLOWING: CAPT'S INST LIGHTS, PITCH TRIM, ASYM FLAPS, NR 1 EPR WITH PACKS TRIPP ED, NR 1 OIL TEMP WENT -40 DEGREES, SYS A-HYD WENT DOWN TO 2000 PSI, ENG FAIL LIGHTS CAME ON. CAME BACK AND LANDED UNEV ENTFULLY. WATER INTRUSION FOUND ON E-1 ELECTRICAL SHELF FROM RAIN. AREA DRIED AND GCU CHANGED PRECAUTIONARY. REMOVED AND REPLACED NR 1 GCU AND VOLTAGE REGULATOR IAW B727-200MM 20-10-011. RAN ALL 3 ENGINES IAW 727 JRH CH5. ALL BUS TIES CLOSE. 2 L 7 3 4F RT A3WE 2007051400027 20070514 00027 NM 2007 5 14 07FDEA01735 1 20070510 A 5230 SKIN BOEING 727 7272S2F 1384O81 NM CARGO DOOR MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 210FE 22932 FOUND ON AGING A/C INSP AFT LOWER CARGO DOOR SKIN REPAIR ON AFT LWR CORNER DID NOT CONFORM TO CURRENT SRM 52-00-3 FIG 3. REMOVED EXISTING DOUBLER INSTALLED NEW EXTERNAL DOUBLER REPAIR REF SRM. 52-00-3 FIG 3. 2 L 7 3 4F A3WE 2007051400042 20070514 00042 NM 2007 5 14 07FDEA01726 1 20070509 A 5314 65C337511 KEELBEAM BOEING 727 7272S2F 1384O81 NM BS 950A S29L CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 AFT PIT BILGE KEEL BEAM OB FLANGE IS CORRODED BS 950A 2, STR 29L, WL139. ACCOMPLISHED REPAIR OF KEEL BEAM CHORD OB FLG BD 950A 2, STR 29, REF FED EX EO NR 7-5310-7-2356 CARD 6 PG 2 FIG 3 NOTE 1. 2 L 7 3 4F A3WE 2007051400046 20070514 00046 WP 2007 5 14 07FDEA01730 1 20070509 A 5512 SKIN DOUG DC10 DC1010 3022110 WP ZONE 300 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 397FE 46631 ACF MODIFICATION AND REPAIR ASSESSMENT HORIZONTAL STABILIZER LT SIDE DENTS, NICKS, DEFORMATION RIB AND SKIN AND 10 EA R IVETS LOOSE ON LOWER SKIN B/T STA 48.500 TO STA XE 67.225 AND STA XE 88.625 TO STA XE 100.455. REMOVED DETACHABLE ELE VATOR , REMOVED LWR INB SKIN PANEL. PERFORMED INSPECTION ON RIBS AND LATCHING POINT. REPLACED INBD LWR SKIN PANEL, PER FORMED EA2 REPAIRS ON OUTBOARD LOWER PANEL. INSTALLED DETACHABLE ELEVATOR , APPLIED SEALANT ON L EDGE PANEL. 2 L 7 3 4F A22WE 2007051400066 20070514 00066 SO 2007 5 14 C2XA07RI031 1 20070507 A 2560 7287580501 GLOWSTRIP EMB 145 EMB145XR 3260214 SO CABIN MISSING A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 11106 145650 FLT 2761 - EWR - CREW REPORTED FLUORESCENT STRIP IN GALLEY AREA MISSING. EWR MX INSTALLED EMERGENCY LIGHT STRIP AND PER FORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007051400071 20070514 00071 EA 2007 5 14 TRAX200700636 1 20070504 A 5534 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 706EV 10054 SUSPECT CRACK AT BASE OF VERTICAL STAB LT SIDE (MARKED). WORK COMPLETED IN ACCORDANCE WITH ALL CRJ 700 SRMS. 2 L 7 2 4F RT A21EA 2007051400077 20070514 00077 NM 2007 5 14 ASMF20070505 1 20070510 A 2120 39271012 VALVE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE LEFT FAILED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 158PL 32703 32703 49761 DURING TRANSIT CHECK CAPTAIN REPORTED PRESSURIZATION FAILURE, AT 25000 FEET FLOW AND CABIN ALT LIGHTS TURNED ON. DURING MAINTENANCE CHECK AUTOMATIC CABIN PRESSURE CONTROL SYSTEMS WERE INOPERATIVE. SYSTEMS WERE DEFERRED IAW MEL 21-24 AND AIR CRAFT WAS DISPATCHED. MAINTENANCE REPLACE BOTH AUGMENTATION VALVES AND PNEUMATIC PILOT PRESSURE REGULATOR IAW MM 36-10- 01 AND 36-10-02, BUT DURING TEST IT WAS DETECTED LOW FLOW IN LT SIDE. THE LT AUGMENTATION VALVE WAS REPLACED AGAIN IAW M M 36-10-01, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007051400080 20070514 00080 EA 2007 5 14 COMA0760356 1 20070502 A 3234 7455025 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A COMA K NONE O OTHER CL CLIMB 1 SO 01 912CA 11346 7011 FLIGHT 5402 - SELECTED GEAR UP AND GEAR DID NOT RETRACT. CYCLED GEAR HANDLE DOWN THEN BACK UP, CLEARED MESSAGES AND RAI SED GEAR. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE ASSEMBLY. 2 L 7 2 4F RT A21EA 2007051400085 20070514 00085 EA 2007 5 14 HNAA0700078 1 20070422 A 5210 NAS11046 BOLT DHAV DHAV DHC8 DHC8311 1386006 EA PAX DOOR MISSING A HNAA O OTHER O OTHER UK UNKNOWN 1 EA 07 328EN 26616 281 UNABLE TO OPEN THE PAX DOOR FROM THE INSIDE. FERRYING AIRCRAFT TO CLT FOR REPAIRS. REPLACED MISSING BOLT AND WASHER TH AT SUPPORTS OUTER SKIN RIGHT SIDE AT BOTTOM STEP, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007051400089 20070514 00089 NE 2007 5 14 HNAA0700076 2 20070420 A 7261 310450001 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 MALFUNCTIONED A HNAA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 805EX 37864 2351 228 120911 WITH NR 2 ENGINE RUNNING, SELECTED BLEED AIR CAUSED MIST OR SMOKE IN CABIN. FERRIED AIRCRAFT TO MDT, MDT INSPECTED AIRC RAFT FOUND NR 2 ENGINE HAD OIL IN BLEEDS. REMOVED AND REPLACED ENGINE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007051400091 20070514 00091 NM 2007 5 14 HNAA0700079 1 20070416 A 2910 8290009153 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM NLG LEAKING A HNAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 EA 07 982HA 33414 33414 380 WHILE CLIMBING THROUGH 17,000 FEET ABOUT 40 MILES EAST OF PIT, THE NUMBER 2 HYDRAULIC SYSTEM DROPPED TO 1/2 QUART. RETU RNED TO PIT, DECLARED AN EMERGENCY. FLIGHT LANDED AND TAXIED TO GATE WITHOUT FURTHER INCIDENT. INSPECTED AND FOUND LEA K AT THE STEERING ACTUATOR. INSTALLED A TEMPFLEX LINE, RAN AIRCRAFT OPERATED STEERING SYSTEM OPS AND LEAK CHECK GOOD. 2 H 7 2 4T RT A13NM 2007051400092 20070514 00092 EA 2007 5 14 HNAA0700081 1 20070512 A 3350 OL6839BPEGPL LIGHT DHAV DHC8 DHC8311 1386006 EA CABIN INOPERATIVE A HNAA K NONE L NO TEST UK UNKNOWN 1 EA 07 336EN 33780 33780 336 THIRD EMERGENCY CENTER FLOOR BULB FROM THE FRONT BURNT OUT. REPLACED BULB, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007051400093 20070514 00093 NM 2007 5 14 UPS07649785 1 20070511 A 5753 FLAP BOEING 767 76734AF 1385212 NM T/E FLAP DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 313UP 27764 DAMAGE TO RIGHT O/B FLAP. DENTS AND DELAMINATION BEYOND SRM LIMIT. [SUP 05-14-07] ACCOMPLISHED STEPS 1 THRU 5A AND ST EP 5B ON DENT 2 ONLY PER EO B767-5750-25812-A, PARAGRAPH 6A. ACCOMPLISHED INTERIM REPAIRS TO REMAINING AREAS PER EO B767 -5750-26812A. REPEAT INSPECTIONS EVERY 7 DAYS. PERM REPAIR/PART REPLACEMENT IN 90 DAYS. 2 L 7 2 4F RT A1NM 2007051400095 20070514 00095 NM 2007 5 14 UPS07M49778 1 20070319 A 5350 SKIN DOUG MD11 MD11F 3023600 NM TAIL CONE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C FWD TAIL CONE RIGHT RETRACTABLE DOOR INTERIOR FWD SECT REAR OF SAFETY BARRIER STOWAGE ANGLE SKIN CHAFE D AS MARKED. CHAFED AREA REMOVED FOUND EXCEED LIMIT MATL THK 0.020" THK REMAIN 0.000" THK REMOVED 0.020" AREA 2" X 1" P ER SRM 53-00-01VIR38. DAMAGE AREA TRIM SRM 52-00-01VIR38. HFEC INSP C/O DAC NDTSPM R13 06-10-01.001. NO CRACK FOUND. DOUBLER REPAIR & FILLER FAB USE 2024T3-0.063". DOUBLER, FILLER TREATED, PAINTED SRM 51-21-01VIIR38. BOTH INSTL SRM 52 -00-01VIR38. 2 L 7 3 4F RT A22WE 2007051400098 20070514 00098 NM 2007 5 14 MWEA070101 1 20070510 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 922ME 55184 RIGHT THRUST REVERSER UPPER DEFLECTOR DOOR ZEE FRAME 26.666 HAS A CRACK IN THE RADIUS ON THE INBOARD END. INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007051400099 20070514 00099 NM 2007 5 14 MWEA070102 1 20070510 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 922ME 55184 RIGHT THRUST REVERSER LOWER DEFLECTOR DOOR ZEE FRAME STATION 26.666 HAS A CRACK ON THE INBOARD END. INSTALLED ZEE FRAME . 2 L 7 2 4F TR A6WE 2007051400104 20070514 00104 NM 2007 5 14 MWEA070104 1 20070510 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 922ME 55184 LEFT THRUST REVERSER LOWER DEFLECTOR DOOR ZEE FRAME STATION 26.666 HAS A CRACK ON THE INBOARD END. INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007051400106 20070514 00106 NM 2007 5 14 MWEA070105 1 20070510 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 922ME 55184 LEFT THRUST REVERSER LOWER DEFLECTOR DOOR ZEE FRAME STATION 26.666 HAS A CRACK ON THE OUTBOARD END. INSTALLED ZEE FRAME . 2 L 7 2 4F TR A6WE 2007051400108 20070514 00108 NM 2007 5 14 MWEA070109 1 20070509 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 916ME 55178 LEFT LOWER THRUST REVERSER FRAME LOCATED AT STATION 26.666 HAS A CRACK ON THE INBOARD END. INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007051400111 20070514 00111 NM 2007 5 14 MWEA070111 1 20070509 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 916ME 55178 APPROXIMATELY .25 INCH CRACK IN END OF ZEE FRAME INSIDE LEFT THRUST REVERSER UPPER BUCKET, INBOARD SIDE AT STATION 26.66 6. INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007051400113 20070514 00113 NM 2007 5 14 SWAA072384 1 20070510 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 463WN 32467 DURING SCHEDULED MV3 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007051400123 20070514 00123 NM 2007 5 14 SWAA072366 1 20070510 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 455, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007051400134 20070514 00134 NM 2007 5 14 SWAA072376 1 20070510 A 5311 6558280 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 13R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007051400137 20070514 00137 NM 2007 5 14 SWAA072377 1 20070510 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007051400138 20070514 00138 NM 2007 5 14 SWAA072378 1 20070510 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007051400140 20070514 00140 NM 2007 5 14 SWAA072379 1 20070510 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007051400141 20070514 00141 NM 2007 5 14 SWAA072375 1 20070510 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007051400142 20070514 00142 2007 5 14 SWAA072364 4 20070509 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007051400143 20070514 00143 NM 2007 5 14 SWAA072382 1 20070510 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 421LV 32452 DURING SCHEDULED HC2 CHECK, LEFT OVERWING EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PA CK PER MM. 2 L 7 2 4F RT A16WE 2007051400144 20070514 00144 NM 2007 5 14 SWAA072383 1 20070510 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 421LV 32452 DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PA CK PER MM. 2 L 7 2 4F RT A16WE 2007051400146 20070514 00146 NM 2007 5 14 USAA200705U06 1 20070510 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 A 1 INCH CRACK FOUND AT STA 727D, STR 23R. INSTALLED DOUBLER & TRIPLER PER TR 53-60-03A, SRM 53-00-01 FIG 201, REPAIR 3 1. 2 L 7 2 4F RT A16WE 2007051400148 20070514 00148 NM 2007 5 14 USAA200705U05 1 20070511 A 5340 STRINGER CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 A 1 INCH CRACK FOUND AT STA 344, STR 15, TIE CLIP. REMOVED & REPLACED STRINGER CLIP PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007051400149 20070514 00149 EA 2007 5 14 COMA0760363 1 20070506 A 7830 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 956CA 7105 FLIGHT 5280 - LEFT T/R UNLOCK MESSAGE DURING POWER-UP. TROUBLESHOT LEFT T/R SYSTEM AND PERFORMED OPS CHECKS, NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007051400150 20070514 00150 EA 2007 5 14 COMA0760364 1 20070507 A 2750 7805013 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 914CA 18833 7012 FLIGHT 5458 - AFTER LANDING, FLAPS SELECTED TO 20, FAILED AT 26 LT AND 28 RT. PERFORMED EO 27-046AD. REPLACED FLAP CON TROL HANDLE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007051400151 20070514 00151 EA 2007 5 14 COMA0760360 1 20070504 A 3260 622EN1436 SWITCH CNDAIR CL600 CL6002B19 1900309 EA NLG DOOR FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 912CA 7011 FLIGHT 5107 - AFTER TAKEOFF RECEIVED GEAR WARNING, GEAR DISAGREE AND NOSE DOOR WARNING, EXTINGUISHED ON LEVEL-OFF. PERF ORMED FUNCTIONAL CHECK OF LANDING GEAR EXTENSION/RETRACTION SYSTEM. REPLACED NOSE DOOR SWITCH. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007051400154 20070514 00154 EA 2007 5 14 COMA0760367 1 20070509 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR ACTIVATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 934CA 7042 FLIGHT 4953 - RECEIVED PAX DOOR LATCH CAUTION ON TAKEOFF. ABORTED TAKEOFF. RETURNED TO GATE. DEFERRED IAW MEL 52-70-0 1-1. 2 L 7 2 4F RT A21EA 2007051400155 20070514 00155 EA 2007 5 14 COMA0760358 1 20070502 A 2613 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA OVERHEAT WARNING ACTIVATED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 779CA 7306 FLIGHT 5482 - CARGO OVERHEAT MESSAGE IN FLIGHT, AIRCRAFT DIVERTED TO JAN AND LANDED SAFELY. PERFORMED OPS CHECK OF CARG O FANS, ALL CHECKS GOOD PER AMM 21-55-00. 2 L 7 2 4F RT A21EA 2007051400156 20070514 00156 EA 2007 5 14 COMA0760368 1 20070506 A 2750 860D10018ABCD CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAULTY A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 916CA 27651 7014 FLIGHT 5468 - AFTER LANDING SELECTED FLAPS TO 20 DEGREES, FAILED AT 27 DEGREES. REPLACED FECU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007051400165 20070514 00165 EA 2007 5 14 COMA0760357 1 20070502 A 3350 364911 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN LOW A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 995CA 7229 FLIGHT 5047 - CREW REPORTS FIRST EMERGENCY FLOOR LIGHT DIM. REMOVED AND REPLACED LAMP-FLEX SOLID FOR FORWARD MOST EMERG ENCY FLOOR TRACK LIGHTING. 2 L 7 2 4F RT A21EA 2007051400167 20070514 00167 EA 2007 5 14 TRAX200700646 1 20070509 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 874AS 7551 EMERGENCY CEILING LIGHT ABOVE ROW 4 INOP. 2 L 7 2 4F RT A21EA 2007051400169 20070514 00169 EA 2007 5 14 COMA0760362 1 20070504 A 2150 RESTRICTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA LT PACK DEFECTIVE A COMA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 01 597SW 7293 FLIGHT 5542 - RECEIVED CABIN ALT CAUTION. CABIN PRESS RISING SLOWLY BUT STEADILY THROUGH 8000 FT. PERFORMED QRH, EMERG ENCY DESCENT TO 10000. CABIN PRESS STABILIZED. REPLACED LEFT PACK WATER SEPARATOR RESTRICTOR. 2 L 7 2 4F RT A21EA 2007051400174 20070514 00174 EA 2007 5 14 COMA0760369 1 20070514 A 5312 88308 POST CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 929CA 7035 DURING HMV7 INSPECTION FOUND BULKHEAD POST LOWER END CRACKED, FS 559, RBL 9. REMOVED DAMAGE AND INSTALLED DOUBLER PER B OMBARDIER REO 601R-53-41-057. 2 L 7 2 4F RT A21EA 2007051400175 20070514 00175 EA 2007 5 14 TRAX200700638 1 20070507 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GALLEY SMOKE A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 878AS 7590 FLT ATTENDANT SMELLED SMOKE IN GALLEY AREA IN FLT DECLARED EMERGENCY. 2 L 7 2 4F RT A21EA 2007051400177 20070514 00177 EA 2007 5 14 TRAX200700640 1 20070508 A 5320 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 FS 280 CROSSBEAM HAS CORROSION ON UPPER FLANGE. [SUP 05-24-07] REMOVED CROSSBEAM FROM FS 280. BEGAN LOCATING RT CROSSB EAM SPLICE PN CC670-34175-7 IAW REO670-53-11-047. LOCATED LT AND RT SECTION AND GABLE FLOORBEAM FS 280 PN CC670-34175-7 , IAW BOMBARDIER REO 670-53-11-047. OK TO INSTALL LT SERVICEABLE FLOORBEAM SECTION. OK TO INSTALL RT SERVICEABLE FLOORB EAM SECTION. STARTED INSTALLING LT BS 280 CROSSBEAM IAW REO 670-53-11-047. INSTALLED ALL REQUIRED FASTENERS. LT & RT BS 280 CROSSBEAM SECTION IAW REO 670-53-11-047. OK TO PRIME, LOCATED AND DRILLED NUTPLATE HOLES FOR FLOORBOARDS IAW SRM 51-40-11. INSTALLED NUTPLATES NAS1870-3-3 PO 10001 IAW SRM 51-42-15. 2 L 7 2 4F RT A21EA 2007051400179 20070514 00179 EA 2007 5 14 TRAX200700644 1 20070509 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 FS 280.00 FWD CENTER FLOOR SUPPORT ANGLE CORRODED. [SUP 05-25-07] REMOVED CENTER FLOOR SUPPORT ANGLE FROM FS 280. LOCA TED SERVICEABLE FS 280. FWD CENTER FLOOR SUPPORT ANGLE PN CC670-33292-13S/ OK TO INSTALL SERVICEABLE ANGLE. INSTALLED S ERVICEABLE FLOOR SUPPORT ANGLE IAW CRJ 700 SRM 51-42-06 AND CRJ SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007051400180 20070514 00180 EA 2007 5 14 TRAX200700645 1 20070509 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 724EV 10138 FWD EXT EMERGENCY LIGHTS AND INTERNAL PAX DOOR AND SERVICE DOOR EMERGENCY EXIT LIGHTS INOP. 2 L 7 2 4F RT A21EA 2007051400181 20070514 00181 NE 2007 5 14 ZES2007F00000 2 20070421 A 7320 324476813 FUEL CONTROL BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE RT ENGINE INOPERATIVE E ZESA O OTHER R PARTIAL RPM/PWR LOSS AP APPROACH 1 EA 03 6WU 40 BB1668 ON APPROACH, RT ENGINE LOST POWER AND WAS UNRESPONSIVE TO THROTTLE MOVEMENT. FUEL CONTROL WAS REPLACED AND AIRCRAFT RE TURNED TO SERVICE. (K) 1 L 7 2 4T 4 T A24CE E4EA 2007051400185 20070514 00185 WP 2007 5 14 07FDEA01754 1 20070510 A 5347 S4929147 SEAT TRACK DOUG DC10 DC1010F 3022111 WP BS 908-1005 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 MAIN DECK LT SIDE SEAT TRACK HAS GOUGE AT STA 943 LBL 27 REMOVED CORROSION IN REF TO DC10/MD10 SRM 51-21-01 VOL II, FOUN D TO BE OUT OF LIMITS IAW DC10/MD10 SRM 53-70-00 VOL 1 FIG 5. REMOVED SEAT TRACK AND SPLICE IAW DC10/ MD 10 SRM 51-31 -01 VOL II PG 1 MAT ID FOR SEAT TRACK S4929147, PO NR 571386.1 MAT ID FOR SPLICE IS 4932154, MAT ID FOR PLATE IS .050" 7 075-T6. SCALLOPED SEAT TRACK IAW DC10/MD 10 SRM 53-70-00 VOL I. FABRICATED SPLICE AND SPLICE PLATE IAW DC10/MD 10 SRM 53-70-00 VOL I PGS 3-6A. FABRICATED SEAT TRACK IAW DC10/MD10 SRM 53- 70-00 VOL I PG 22. ALODINED AND PRIMED SEAT TRACK AND SPLICE AND SPLICE PLATE IN REF TO DC10/ MD10 SRM 51-21-01 VOL II PGS 24 AND 21. 2 L 7 3 4F A22WE 2007051400186 20070514 00186 WP 2007 5 14 07FDEA01755 1 20070510 A 5347 S49321541200 SEAT TRACK DOUG DC10 DC1010F 3022111 WP BS 705-745 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 CABIN SEAT TRACK HOLE AREAS AT LBL 76 FS 675-735 HAVE CORROSION REMOVED CORROSION IAW DC10-SRM VOL II 51-21-01 PG 28 ORI G THICKNESS .080 REMOVED .039 FOUND TO BE OUT OF LIMITS IAW DC10 SRM VOL I 53-70-00 FIG 5. REMOVED AND REPLACED SEAT TR ACK IAW DC10 SRM 53-70-00 VOL I FIG 1 SHT 2. 2 L 7 3 4F A22WE 2007051400187 20070514 00187 WP 2007 5 14 07FDEA01756 1 20070510 A 5347 S4929405 SEAT TRACK DOUG DC10 DC1010F 3022111 WP BS 1551-1671 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 MAIN DECK SEAT TRACK SCALLOP WORN STA 1621 RBL 47 REMOVED FLOOR BOARDS FROM STA 1561-1741. BROKEN SCALLOP FOUND TO BE O UT OF LIMITS IAW DC10 SRM 53-70-00 VOL I FIG 5. REMOVED SEAT TRACK FROM STA 1551-1671 RBL 47 IN REF WITH DC10 SRM 53- 70-00, VOL I FIG 1. FABRICATED SEAT TRACK AND SPLICE PLATE IAW DC10 SRM 53-70-00 VOL I. ALODINED AND PRIMED IAW 51-21- 01 SRM DC-10 PG 1-30 VOL II. INSTALLED SEAT TRACK AND SPLICE IAW DC10 SRM 51-35-01 PG 1 VOL II. INSTALLED FLOORBOARD I AW AMM 53-21-08-2 DC10-10 PG 1-4 (FIG 201 SHEET 1). INSTALLED RBL 47 SEAT TRACK AT STA 1551-1676 INSTALLED FLOOR BOAR D AT STA 1561-1741. 2 L 7 3 4F A22WE 2007051400189 20070514 00189 WP 2007 5 14 07FDEA01714 1 20070507 A 5347 SEAT TRACK DOUG DC10 DC1010F 3022111 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 MAIN DECK LEFT SIDE SEAT TRACK WORN AT STA 1119 LBL 47. REMOVED,FABRICATED, INSTALLED SEAT SECTION IAW DC/MD10 SRM 53-7 0-00 VOL I PAGE FIG1 SHEET 1 AND 51-21-01 VOL II PAGE 21, 25. 2 L 7 3 4F A22WE 2007051400190 20070514 00190 WP 2007 5 14 07FDEA01715 1 20070507 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 MAIN DECK LEFT SIDE SEAT TRACK WORN AT STA 1089 LBL 47. REMOVED, FABRICATED, INSTALLED SEAT TRACK SECTION IAW DC/MD10 S RM 53-70-00 VOL I FIG 5 SHT 1 AND 2,51-21-01 VOL II PAGE 21 AND 25. 2 L 7 3 4F A22WE 2007051400193 20070514 00193 NM 2007 5 14 DL757070446 1 20070504 A 5415 112N7003 FITTING BOEING 757 757232 1384965 NM NR 1 PYLON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 627DL 22917 DURING ACCOMPLISHMENT OF EA 06-070332-03AD, SIP MOD, HOLE NR 51 AS IDENTIFIED IN THE EA REQUIRED OVERSIZING BEYOND THE E A MAX. THE EA ALLOWS OVERSIZING TO 1ST OVER, AND THE HOLE REQUIRED OVERSIZING TO 2ND OVER. BOEING PROVIDED AMOC 8100 A PPROVAL OF THE OVERSIZE HOLE CONDITION AS DETAILED IN 461451-14AD 2 L 7 2 4F RT A2NM 2007051400195 20070514 00195 NM 2007 5 14 DL764070481 1 20070507 A 7797 609200018F WIRE HARNESS BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 2 ENGINE UNSERVICEABLE A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 830MH GDBBJ41R 29701 706261 RT ENG EGT KEPT SURGING INTO RED EVEN WITH THROTTLE RETARDED. INSP RT THERMOCOUPLE LEAD ALL LEADS CONNECTORS SECURE. F OUND SEVERAL CORRODED/BURNED PINS ON THERMOCOUPLE JBOX. REPLACED JBOX NEEDS FURTHER TROUBLESHOOTING/CHECKOUT. FOUND UP PER EGT HARNESS TO HAVE INTERMITTENT OPEN REPLACED UPPER EGT HARNESS OPS CK ENG PER M/M RAN ENG TO 93 PERCENT N1 EGT WIT HIN LIMITS NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A1NM E23EA 2007051400197 20070514 00197 EU 2007 5 14 TRBA2007008 1 20070317 A 3397 WIRE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE CABIN DAMAGED A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 434AT CREW NOTICED EMERGENCY EXIT LIGHT AT BOTTOM OF SERVICE DOOR INOPERATIVE. REPAIRED WIRE AND TESTED EMERGENCY LIGHT IAW M M 33-55-00. FOUND WORKING PROPERLY. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007051400198 20070514 00198 NE 2007 5 14 TRBA2007010 2 20070320 A 7324 263701 FLOW DIVIDER AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE RT ENGINE LEAKING A TRBA O OTHER R X PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT CL CLIMB 1 SO 29 447AM 6 447 WHILE IN CLIMB, NR 2 ENGINE TQ DROPS SLOWLY UP TO 25 PERCENT AND LOST POWER UNTIL THE ENGINE FLAMED OUT BY ITSELF. REPL ACED FUEL FLOW DIVIDER IAW MM 72-01-40 AND FUEL NOZZLES 8,9,10,11 AND 12 TRANSFER TUBES AND SEALS IAW 72-01-40. PERFORM ED ENGINE RUN UP NO LEAKS FOUND AND WORKING PROPERLY. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007051400203 20070514 00203 2007 5 14 AMTA200700212 4 20070430 A 3160 1741010301 CDU BOEING 737 73783N 13844HI NM COCKPIT MALFUNCTIONED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 318TZ 28247 CAPTAIN`S CDU DISPLAY BLANK. REMOVED AND REPLACED CAPTAINS CDU REF 34-61-01. OPS CHECK GOOD. (K) 2 L 7 2 4F RT A16WE 2007051400204 20070514 00204 NM 2007 5 14 AMTA200700203 1 20070426 A 3350 LIGHT BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE CABIN DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 522AT 29330 FLOOR PATH LIGHTING INOPERATIVE FROM ROW 1-4. RECONNECTED LIGHT ASSY. AT ROW 4. OPS CK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007051400205 20070514 00205 NM 2007 5 14 AMTA200700213 1 20070430 A 4940 28B5457 STARTER GEN BOEING 737 73783N 13844HI NM APU MALFUNCTIONED A AMTA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 318TZ 15304 1582 28247 APU WILL NOT START. REPLACED STARTER GENERATOR. OPS CHECK NORMAL. (K) 2 L 7 2 4F RT A16WE 2007051400214 20070514 00214 NM 2007 5 14 AMTA200700204 1 20070426 A 3020 7646B000 ANTI-ICE VALVE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE FAULTY A AMTA K NONE J WARNING INDICATION CR CRUISE 1 GL 11 552TZ 4220 88 32586 EICAS MSG R ENG ANTI-ICE DISPLAYED AND ENG ANTI-ICE VALVE LIGHT REMAINED ILLUM W/SW. ON R ENG ANTI-ICE CB WAS TRIPPED. RESET CB W/SW OFF. EICAS MSG AND VALVE LIGHT EXTINGUISHED. R ENG A/I WORKED NORMAL ON REPLACED ENGINE ANTI-ICE VALVE R AN ENGINE ANTI-ICE VALVE RAN ENGINE AND ACCOMPLISHED ANTI-ICE ADJUSTMENT/TEST REF MM 30-21-00-5, OPS AND LEAK CHECK GOOD . (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007051400216 20070514 00216 NM 2007 5 14 AMTA200700211 1 20070430 A 4940 28B5457 STARTER GEN BOEING 737 73783N 13844HI NM APU INOPERATIVE A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 318TZ 15304 1582 28247 APU GEN INOPERATIVE. REMOVED AND REPLACED APU GEN OPS CHECK GOOD IAW 49-41-21-4. (K) 2 L 7 2 4F RT A16WE 2007051400217 20070514 00217 EU 2007 5 14 TRBA2007003 1 20070125 A 3350 3011210 LIGHT AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE PAX ENTRY INOPERATIVE A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 288AM 288 DURING PRE-FLIGHT, CAPTAIN FOUND THE STAIR EMERGENCY LIGHT INOPERATIVE. REPLACED AND TESTED ENTRY STAIR EMERGENCY LIGHT ASSY IAW MM 33-51-00, FOUND SYSTEM WORKING PROPERLY. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007051400218 20070514 00218 EU 2007 5 14 TRBA2007015 1 20070329 A 3397 WIRE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE CABIN DAMAGED A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 308AE 309 WHILE PERFORMING POST FLIGHT, CREW NOTICED MAIN CABIN DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED WIRE AT MAIN CABI N EMERGENCY EXIT LIGHT ASSY IAW 33-22-17. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007051400221 20070514 00221 SO 2007 5 14 N382007F00001 1 20070413 A 2761 1159SCH30511 ACTUATOR GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU LT SPOILER LEAKING E N38A K NONE K FLUID LOSS IN INSP/MAINT 1 EA 05 970SJ 11823 1146 ON AIRCRAFT POST FLIGHT INSPECTION, FOUND GROUND SPOILER ACTUATOR SEEPING HYDRAULIC FLUID. CLEANED AFFECTED AREA, GROUN D RUN AIRCRAFT TO ACTUATE SPOILERS, AND FOUND ACTUATOR SEEPING BETWEEN VALVE BODY AND ACTUATOR HOUSING. REMOVED AND REP LACED ACTUATOR. LEAK CHECKED, OK. (K) 2 L 7 2 4F 4 F RT A12EA E25NE 2007051400222 20070514 00222 CE 2007 5 14 S2G2007F00000 1 20070414 A 5751 122005317 HINGE BRACKET CESSNA 206 U206F 2073333 CE CONT O520 IO520* 17032 SO LT AILERON CRACKED E S2GA K NONE O OTHER IN INSP/MAINT 1 NM 07 1372V U20602588 FOUND SEVERAL CRACKS IN BOTH LT AILERON HINGE BRACKETS IN RADIUS OF THE LOWER EARS. THIS WAS FOUND DURING AN ANNUAL INS PECTION. (K) 1 H 7 1 3O 3 O A4CE E5CE 2007051400226 20070514 00226 NM 2007 5 14 AMTA200700196 1 20070415 A 3020 7646B000 ANTI-ICE VALVE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE MALFUNCTIONED A AMTA K NONE O OTHER TX TAXI/GRND HDL 1 GL 11 552TZ 12969 12969 32586 RT ENG ANTI-ICE VALVE SLOW TO OPEN. VALVE OPENED WHEN SWITCH RECYCLED. REPLACED RT ENGINE INLET THERMAL ANTI-ICE VALVE IAW MM 30-21-03. OPS CHECK NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007051400227 20070514 00227 NM 2007 5 14 AMTA200700198 1 20070422 A 4970 WARNING SYSTEM BOEING 737 73783N 13844HI NM APU MALFUNCTIONED A AMTA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 318TZ 28247 APU FAULT LT ILLUMINATED ON START. PERFORMED APU BITE CK, FOUND MSG 49-41011, PERFORMED BITE CK IAW FIM 49-40-00-810, F IM 49-60-00-810, NO CURRENT FAULT FOUND. (K) 2 L 7 2 4F RT A16WE 2007051400228 20070514 00228 EU 2007 5 14 TRBA2007016 1 20070402 A 3350 5211309111B LIGHT AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE CABIN INOPERATIVE A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 414WF 414 WHILE PERFORMING PS-2 CHECK MECH FOUND RT GALLEY EMERGENCY LIGHT INOPERATIVE. REPLACED RT GALLEY EMERGENCY LIGHT IAW MM 33-50-00. (K) 2 H 7 2 4T 4 T RT E20NE 2007051400229 20070514 00229 EU 2007 5 14 TRBA2007017 1 20070402 A 3350 OL6836BDE LIGHT AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE CABIN LOW A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 431AT WHILE PERFORMING PRE-FLIGHT CREW NOTICED LOWER EMERGENCY LIGHT AT SERVICE DOOR DIM. REPLACED SERVICE EMERGENCY EXIT SIG N LIGHT BULB IAW MM 33-50-00. (K) 2 H 7 2 4T 4 T RT E20NE 2007051400230 20070514 00230 CE 2007 5 14 S2G2007F00001 1 20070414 A 5751 122005217 HINGE BRACKET CESSNA 206 U206F 2073333 CE CONT O520 IO520* 17032 SO LT AILERON CRACKED E S2GA K NONE O OTHER IN INSP/MAINT 1 NM 07 1372V U20602588 FOUND SEVERAL CRACKS IN BOTH LT AILERON HINGE BRACKETS IN RADIUS OF THE LOWER EARS. THIS WAS FOUND DURING AN ANNUAL INS PECTION. (K) 1 H 7 1 3O 3 O A4CE E5CE 2007051400231 20070514 00231 EU 2007 5 14 TRBA2007006 1 20070215 A 3320 E038711 LIGHT AEROSP ATR72 ATR72212A 8680902 EU PWA PW120 PW127 NE CABIN BURNED OUT A TRBA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 29 536AT 3962 536 WHILE IN TAXI, NR2 F/A REPORTED ELECTRICAL SMOKE SMELL. AC RETURNED TO STTFOR CHECK. REPLACED FLUORESCENT LIGHT BULB A ND FOUND IT WORKING PROPERLY IAW MM 33-21-23. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007051400232 20070514 00232 EU 2007 5 14 TRBA2007012 1 20070325 A 3350 FUSE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE BATTERY PACK BLOWN A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 348AE 349 CREW NOTICED LOWER EXIT LIGHT AT SERVICE DOOR INOPERATIVE. REPLACED FUSE AT POWER SUPPLY FIN 62WL AND BULB AT LOWER ASS Y FOR EMERGENCY LIGHT AT SERVICE DOOR IAW JIC 33-50-00, OPS CHECKS GOOD. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007051400235 20070514 00235 SW 2007 5 14 BAQA200700012 1 20070420 A 2820 130100 PUMP BOLKMS 117 BK117C2 5626002 SW TMECA ARRIEL ARRIEL1 60030 NE FUEL SYSTEM MALFUNCTIONED E BAQA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 03 766ME 156 9066 NR 1 ENGINE PRIME PUMP CIRCUIT BREAKER POPS. REMOVED AND REPLACED NR 1 ENGINE PRIME PUMP. SYSTEM OPERATIONAL CHECKS GO OD. 1 G 7 2 3U 3 U H13EU E19EU 2007051500001 20070515 00001 WP 2007 5 15 07FDEA01758 1 20070510 A 3210 LANDING GEAR DOUG MD10 MD1010F 3022112 WP MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION LD LANDING 1 SO 25 383FE 46616 WHEN GEAR INITIALLY LOWERED FOR LANDING, ALL INDICATIONS REMAINED RED. RECYCLED GEAR AND AFTER A DELAY ALL INDICTIONS R EAD GREEN. DURING CREW DEBRIEF, CREW STATED WHEN GEAR INITIALLY LOWERED THERE WAS NO PHYSICAL IND VIBRATION OR FEELING THAT THE GEAR WAS EVEN LOWERING UNTIL RECYCLED AND THEN AFTER SOME DELAY COULD FEEL THE GEAR ACTUALLY LOWERING AND AFTE R MORE DELAY GOT THREE GREENS. TROUBLE SHOT PER FIM 32-30 UP TO STEP 5. VERIFIED RIGGING FROM GEAR HANDLE TO SELECTOR VALVE. ALL CHECKS NORMAL REF MD10-10MM 32-31-01-5. REMOVED AND REPLACED EMERGENCY LANDING GEAR CONTROL MICROSWITCH S1 -392 PER MD10 MM 32-32-01-2. OPS CHECK NORMAL PER MM 32-30-00-5. 2 L 7 3 4F RT A22WE 2007051500002 20070515 00002 EU 2007 5 15 07FDEA01761 1 20070511 A 3040 WIRE AIRBUS 310 A310203 3930313 EU WINDOW HEAT SHORTED A FDEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 25 415FE 349 CAPT WINDOW HEAT SIDE SLIDING WINDOW WIRING SHORTED OUT AND MOMENTARY CAUGHT FIRE PULLED ASSOCIATED CB H86. ACCOMPLISH ED EA 6-3040-111404, DISCONNECT, CAP AND STOW OF FIVE EACH WIRES AT TERMINAL STRIP 195VT. MEL PROCEDURES STILL NEED TO BE ACCOMPLISHED. RELEASED FOR SERVICE PER MEL/CDL: 30-42-01-01-A. REPAIRED WIRING ON LT NR 2 SLIDING WINDOW PER E.A. 6-3040-111404. REPLACED COILED CORD PER SMP. OPS CHECKS GOOD; WINDOW HEAT, CAPT'S MAP AND CONSOLE LIGHTS. REF. WRI'S 3 0-40/9471, 33-10/9469, 33-10/9470. 2 L 7 2 4F RT A35EU 2007051500005 20070515 00005 NM 2007 5 15 DLM88070492 1 20070504 A 5511 59361151 SPAR DOUG MD88 MD88 3023688 NM HORIZONTAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DL 49541 TOOLING DAMAGE WAS FOUND IN TWO HOLES IN THE OUTER SECTION OF THE HORIZONTAL STABILIZER REAR SPAR AND RIB. THE HOLES WE RE OVERSIZED. 2 L 7 2 4F RT A6WE 2007051500010 20070515 00010 NM 2007 5 15 DL76P070497 1 20070507 A 5247 7321380706 ACTUATOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE APU DOOR INOPERATIVE A DALA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 143DA 15662 25991 P2307 3 APU START ATTEMPTS AT 39000/ 35000/ AND 23000 NO RPMS A APU DOOR STATUS MSG DISPLAYED APU INOP. FOUND APU DOOR ACTUAT OR C/B POPPED. RESET C/B APU STARTED NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007051500016 20070515 00016 NM 2007 5 15 DL76L070388 1 20070501 A 2934 291702127 TRANSMITTER BOEING 767 767332 1382001 NM HYD QTY UNKNOWN A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 178DN 25143 RTB - ON TAXI LEFT HYD QTY WENT TO 0 THEN, LATER RETURNED TO .84. REPLACED LEFT HYD QTY TRANSMITTER PER M/M 29 WTY CKS NML. LEAK OP CKS GOOD REMOVED MCO AND PLACARD. 2 L 7 2 4F RT A1NM 2007051500017 20070515 00017 NM 2007 5 15 DL764070394 1 20070503 A 2997 WIRE BOEING 767 767432ER 1385134 NM HYD QTY INDICATO DISCONNECTED A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 841MH 29714 AIRCRAFT 1817 FLT 11 03 MAY - DURING TAXI HAD LEFT HYD QTY FLUCTUATING. HAD TO RTB TO APPLY MEL. REMOVED PIN AT D2704- B3 RETERMINATED WIRE. RECONNECTED PTU SIGNAL WIRE IN P37 PNL TB274 DIODE R397C PER MEL LT HYD QTY CKS NML. REMOVED MCO AND PLAC. 2 L 7 2 4F RT A1NM 2007051100091 20070511 00091 NM 2007 5 11 R61A20070007 1 20070424 A 2781 1702288A SENSOR EMB ERJ170 ERJ170100SU 3260403 NM L/E SLAT FAULTY A R61A O OTHER N FALSE WARNING AP APPROACH 1 GL 11 823MD 4251 17000044 PILOT REPORTED SLAT FAIL MESSAGE ON EICAS DURING APPROACH, DECLARED EMERGENCY FOLLOWED QRH AND LANDED WITH OUT INCIDENT. MAINTENANCE WAS DISPATCHED TO A/C. TROUBLESHOT AND REMOVED AND REPLACED RIGHT HAND OUTBOURD SKEW SENSOR AND HARNESS. OPERATIONAL CHECK GOOD AND RETURNED A/C TO SERVICE. 2 L 7 2 4F RT A56NM 2007051100104 20070511 00104 EU 2007 5 11 AWXA200700567 1 20070502 A 5347 D53371110008 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 665AW 1644 SAL - MAJOR REPAIR - BC-4 CHECK - CORROSION ON CABIN SEAT TRACK,+Y765, FR 45 + 5 - FR 46 + 14. REPLACED CABIN SEAT TRAC K,+Y765, FR 41 - FR 47 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007051100118 20070511 00118 NM 2007 5 11 AWXA200700580 1 20070509 A 3397 D9299200900200 WIRE AIRBUS A319 A319132 3930340 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 802AW 924 PHX - EEL - EMERGENCY ESCAPE PATH AISLE LIGHT AT SEAT ROW 12 HAS A BROKEN WIRE. REPAIRED AND OPERATIONAL CHECKED EMERGE NCY ESCAPE PATH AISLE LIGHT AT SEAT ROW 12 IAW AIRBUS ESPM 20-48-14 AND A319 AMM 33-50-00. 2 L 7 2 4F RT A28NM 2007051100164 20070511 00164 WP 2007 5 11 070110 1 20070503 A 3260 DOWNLOCK SENSOR DOUG DC9 DC983 3022083 WP NLG OUT OF ADJUST A WX0A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 19 866GA 49910 NLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF. QRH COMPLIED WITH BY FLIGHT CREW. NLG RED UNSAFE REMAINED ILL UMINATED. AIRCRAFT RETURNED TO THE FIELD (LAS). NO EMERGENCY DECLARED, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DEPARTMENT INSPECTED AND ADJUSTED THE NLG DOWNLOCK SENSOR IAW AMM 32-60-65. PERFORMED GEAR SWING, OPS CHECK GOOD IAW AM M 32-60-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007051400008 20070514 00008 NM 2007 5 14 QXEA200700736 1 20070427 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - LEFT HAND INBOARD SEAT TRACK NR 6 HAS PITTING CORROSION AT STATION 105.5 TO 228.0. REPAIRED IAW RD8/4-53-884 A ND RD8/4-53-1895. 2 H 7 2 4T RT A13NM 2007051400009 20070514 00009 NM 2007 5 14 QXEA200700729 1 20070425 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - RIGHT HAND INBOARD SEAT TRACK NR 10 HAS PITTING CORROSION STATION 39.5 TO 10.5. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007051400019 20070514 00019 NM 2007 5 14 QXEA200700763 1 20070501 A 5711 SPAR BOMBDR DHC8 DHC8402 1390042 NM RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - RIGHT HAND WING INBOARD LOWER SPAR FLANGE CHAFED OUTBOARD EDGE. REPAIRED IAW SRM 51-21-00 AND RD8/4-57-796. 2 H 7 2 4T RT A13NM 2007051400038 20070514 00038 NM 2007 5 14 07FDEA01721 1 20070509 A 5320 69708043 WEB BOEING 727 7272S2F 1384O81 NM ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 VERTICAL STAB ELEVATOR FEEL CONTROL UNIT PLATFORM ASSY FWD RT VERTICAL WEB CRACKED ON INTERNAL SIDE AT THE TWO MOST FWD LWR FASTENERS. REMOVED RT VERTICAL WEB, PICKED UP HOLES IN NEW WEB, INSTALLED RIVETS AND HILOCKS IN NEW WEB, REF SRM 51-30-2. 2 L 7 3 4F A3WE 2007051400059 20070514 00059 WP 2007 5 14 07FDEA01745 1 20070510 A 5347 492914713500 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 FOUND CORROSION ON SEAT TRACK AT STA 605 LBL 28. REMOVED, FABRICATED AND INSTALLED SEAT TRACK SECTION IAW DC/MD10 SRM 5 3-70-00 VOL I FIG 1 SHT 1 AND 53-70-00 VOL I FIG 5, SHT 2 AND 51-21-01 VOL II PAGE 21. 2 L 7 3 4F A22WE 2007051400064 20070514 00064 WP 2007 5 14 07FDEA01752 1 20070510 A 5347 492914713500 SEAT TRACK DOUG DC10 DC1010F 3022111 WP BS 1129 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 MAIN DECK LT SIDE SEAT TRACK IS CRACKED AT STA 1220 LBL 27 REMOVED SEAT TRACK FROM STA 1129 /1229 LBL 27 IAW DC10-SRM 51 -31-01 VOL II MAT ID FOR SEAT TRACK 4929147 IAW DC10 SRM 53-42-01 VOL III PAGE 7 MATERIAL ID FOR SPLICE HAT AND SPLICE P LATE 4932154 AND 7075 T6 .050 IAW DC10 SRM 53-70-00 PAGE 5 VOL I. FABRICATED, DRILLED AND COUNTERSUNK NEW SEAT TRACK SE CTION AND SPLICED REPAIR IAW DC10-SRM 53-70-00 FIG 5 VOL I. ALODINED AND PRIMED IAW DC-10 SRM 51-21-01 PAGE 1. INSTA LLED SEAT TRACK AND SPLICES REPAIR IAW DC10 SRM 51-31-01 VOL II PAGE 1. 2 L 7 3 4F A22WE 2007051400075 20070514 00075 EA 2007 5 14 COMA0760353 1 20070501 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 966CA 27177 7132 DURING FS 559 INSPECTION FOUND CRACK AT SEMI-PRESSURE BULKHEAD, FS 559, RBL 18. STOP DRILLED CRACK AND INSTALLED DOUBLE R PER CRJ REO 601R-53-41-353. 2 L 7 2 4F RT A21EA 2007051400102 20070514 00102 NM 2007 5 14 MWEA070103 1 20070510 A 7830 7150923REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 922ME 55184 RIGHT THRUST REVERSER DEFLECTOR DOOR ZEE FRAME STATION 35.669 HAS A CRACK ON THE INBOARD END. INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007051400120 20070514 00120 NM 2007 5 14 SWAA072381 1 20070510 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 482B, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007051400145 20070514 00145 NM 2007 5 14 SWAA072368 1 20070510 A 3350 MS157721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007051400147 20070514 00147 NM 2007 5 14 USAA200705U04 1 20070508 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 515AU 23701 APPROX 15.5 INCH CRACK IN FUSELAGE RUNS LONGITUDINAL, LOCATED BETWEEN STA 482 & 500, BETWEEN STR 28L & 28R. INSTALLED D OUBLER REPAIR & INSTALLED NEW ANTENNA SUPPORT KIT PER EA 84528. 2 L 7 2 4F RT A16WE 2007051400199 20070514 00199 EU 2007 5 14 TRBA2007011 1 20070322 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU PWA PW120 PW127 NE CABIN DISCHARGED A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 529AM 529 ON POST FLIGHT CREW REPORTED EMERGENCY LIGHT BY SERVICE DOOR INOPERATIVE. REPLACED BATTERY PACK AT POWER SUPPLY 61WL IA W JIC 33-51-21, OPT CHECK GOOD IAW JIC 33-50-00. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007051400219 20070514 00219 NE 2007 5 14 TRBA2007013 2 20070323 A 7200 ENGINE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE RIGHT MALFUNCTIONED A TRBA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 29 260AE 263 SHORTLY AFTER TAKEOFF, RT ENGINE. AC DECLARED EMERGENCY AND RETURNED TO DEPARTURE, NO FIRE INDICATION NOTED. REMOVED A ND REPLACED RT ENGINE IAW MM 055006-CS20000-00R1. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007051400233 20070514 00233 NE 2007 5 14 TRBA2007002 2 20070118 A 7200 PW127 ENGINE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE NR 2 FAILED A TRBA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 29 410AT 19651 2687 410 WHILE IN CLIMB AT 15,000 FT, LOST NR 2 ENGINE NP, TQ, ITT AND OIL PRESSURE. ENGINE WAS SHUT DOWN BY FLIGHT CREW IAW CHE CKLIST. REMOVED AND REPLACED RT ENGINE IAW MTX WORK CARD ENGINE REMOVED AND REPLACED NR 055006-CS-20000-001R1. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007051400234 20070514 00234 NE 2007 5 14 TRBA2007004 2 20070206 A 7200 ENGINE AEROSP ATR72 ATR72212A 8680902 EU PWA PW120 PW127 NE NR 2 MALFUNCTIONED A TRBA O OTHER R Y PARTIAL RPM/PWR LOSS ENGINE STOPPAGE NR NOT REPORTED 1 SO 29 548AT 548 AT 16,000 FTS NR2 ENGINE ROLLED BACK TO 0 TQ AND FEATHERED WHILE ENROUTE. WHILE PERFORMEING MEMORY ITEMS THE NR 2 POWER LEVER WAS BROUGHT BACK TO FLT IDLE AND THE ENGINE RESTARTED ON ITS OWN. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007051500003 20070515 00003 NM 2007 5 15 DL738070489 1 20070503 A 5312 141A74131 BULKHEAD BOEING 737 737832 13844CF NM FS 227 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3757D 30813 THE NLG WHEEL WELL FORWARD BULKHEAD SUSTAINED DAMAGE FROM BLOWN TIRE. THE DAMAGED WEB AND BEAM WERE CUT AWAY AND A REPA IR DOUBLER AND ANGLE WERE INSTALLED. 2 L 7 2 4F RT A16WE 2007051500007 20070515 00007 NM 2007 5 15 DLM88070494 1 20070508 A 2910 HYDRAULIC SYSTEM DOUG MD88 MD88 3023688 NM OVERSERVICED A DALA O OTHER W J INADEQUATE Q C WARNING INDICATION AP APPROACH 1 SO 27 919DL 49584 DESCENDING THROUGH 1900 GOT LT HYD PRESS LOW MESSAGE ON OAP. PRESS INDICATED ZERO QTY 19. TURNED OFF ENG PUMP. OM GND PRESSURE VARIED BETWEEN ZERO AND 3000 WITH NO PUMPS ON QTY VARIED BETWEEN 11-19. INSPECTED AIRCRAFT NO LEAKS FOUND. F OUND HYD SYSTEM OVERSERVICED BLEED SYSTEM OF AIR AND FLUID TO NORMAL.OPERATED FLIGHT CONTROL WITH HYD ALL CK'S NML. HYD QTY AND PRESSURE CK'D GOOD. NO HISTORY AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A6WE 2007051500008 20070515 00008 NM 2007 5 15 DL777070495 1 20070508 A 3244 TIRE BOEING 777 777232 1385232 NM NLG DAMAGED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 867DA 29743 LEFT NOSE TIRE SIDE WALL DAMAGE ON PUSH BACK. REPLACED LT NOSE WHEEL ASSY PER MM. 2 L 7 2 4F RT T00001SE 2007051500012 20070515 00012 NM 2007 5 15 DLM88070499 1 20070509 A 3213 592060213 STRUT DOUG MD88 MD88 3023688 NM NLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 NLG SHOCK STRUT CYLINDER CORROSION CLEANED UP PER CMM, BUT CADMIUM PLATING OMITTED ON A TIME-LIMITED BASIS. 2 L 7 2 4F RT A6WE 2007051500014 20070515 00014 NM 2007 5 15 DL76L070501 1 20070426 A 5411 311T311020 SPAR BOEING 767 767332 1382001 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 180DN 25985 THE NR 2 PYLON UPPER SPAR WEB WAS FOUND CRACKED AT THE FUEL LINE PASS THROUGH. THE CRACKED WEB WAS CUT OUT AND A REPAIR DOULBER WAS INSTALLED. 2 L 7 2 4F RT A1NM 2007051500022 20070515 00022 2007 5 15 DL76L070484 4 20070507 A 2210 15366007 ACTUATOR BOEING 767 767332 1382001 NM YAW DAMPER LEAKING A DALA O OTHER K FLUID LOSS CR CRUISE 1 SO 27 174DN 24802 CENTER HYD LOW LEAK TRACED TO LT YAW DAMPER SERVO ACTUATOR P/N REQUIRED 1536600-7, LEAY SERVO S/N 1979. A/C DISP IAW ME L 22-21-01 CAT C. C HYD SYSTEM SERVICED TO FULL WITH 6 GALLONS. REMOVED AND REPLACED LEFT YAW DAMPER SERVO PER AMM 21- 21-02 MANF PN 1540500-9. LEAK CHK AND SERVO TEST GOOD. PER TOPP 40-30-05 ITEM NOT RII MCO AND PLACARD REMOVED. 2 L 7 2 4F RT A1NM 2007051500024 20070515 00024 NM 2007 5 15 DLM88070486 1 20070504 A 5330 5936434129 SKIN DOUG MD88 MD88 3023688 NM BS 560-588 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 DURING HMV AT GDL, LIGHTNING STRIKES WERE REPAIRED AT THREE LOCATIONS IN THE FUSELAGE SKIN, P/N 5936434-129 BETWEEN STA 560 AND 588, S-26L AND S-27L. REPAIRED PER AMR0953606R02, ER/A 461310-14. 2 L 7 2 4F RT A6WE 2007051500026 20070515 00026 2007 5 15 DL76L070503 2 20070510 A 7532 79275516 CONTROLLER BOEING 767 767332 1382001 NM ENGINE BLEED MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 182DN 930470 25987 AFTER ENG START L BLEED OFF MSG W/NO ENG A/I AVAILABLE. RETURNED TO GATE. SWAPPED L HPSOV/LPRV NO HELP. REPLACED PRV C ONTROLLER. REACTIVATED L HPSOV. RAN ENGINE. BLEED SYSTEM OPERATES NORMALLY. 2 L 7 2 4F RT A1NM 2007051500027 20070515 00027 NM 2007 5 15 DL76S070504 1 20070509 A 3350 20121 CHARGER BOEING 767 767332 1382001 NM EMERGENCY LIGHTS MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 124DE 23438 EMERGENCY LIGHT EXIT SIGN INOP AT L1 AND R1 DOOR. INSTALLED NEW BATTERY AND CHARGER TRA, FOUND TRAY AND BATTERY PACK AS SY MISSING AT L1 POSITION. 2 L 7 2 4F RT A1NM 2007051500028 20070515 00028 NM 2007 5 15 DL738070505 1 20070508 A 5312 148A22811 BULKHEAD BOEING 737 737832 13844CF NM BS 1016 LBL 20 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 387DA 30374 THE AFT PRESSURE BULKHEAD WEB SUSTAINED TOOLING DAMAGE. THE DAMAGED SECTION OF WEB WAS CUT OUT AND A DOUBLER WAS INSTAL LED. 2 L 7 2 4F RT A16WE 2007051500029 20070515 00029 NM 2007 5 15 DL738070506 1 20070410 A 5530 175A16017 BEAM BOEING 737 737832 13844CF NM VERTICAL STAB DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 373DA 29621 THE VERTICAL STABILIZER LT TRAILING EDGE BEAM HAS TWO HOLES MISDRILLED. THE DAMAGED HOLES WERE OVERSIZED. 2 L 7 2 4F RT A16WE 2007051500031 20070515 00031 NM 2007 5 15 DLM88070508 1 20070510 A 5753 VANE DOUG MD88 MD88 3023688 NM LT TE FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 EROSION AND DELAMINATION ON LOWER SURFACE, DENTS ON UPPER SURFACE OF LT INNER FLAP O/B VANE. AEROMEXICO PERFORMED PERMA NENT REPAIR FOR THE DAMAGED SKIN PORTION IAW MD-80 SRM 57-03 FIG 9A (DELTA AIRLINES SRM CHAPTER 57-03D FIG 9A) 2 L 7 2 4F RT A6WE 2007051500032 20070515 00032 NM 2007 5 15 DLM88070509 1 20070510 A 5753 VANE DOUG MD88 MD88 3023688 NM RT WING TE FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 DELAMINATION AT LOWER SURFACE ON RT WING INBOARD FLAP VANE BETWEEN STATIONXCW=79.00 AND XCW=104.500. AMX PERFORMED PERM ANENT REPAIR PER SRM 57-03 FIG 9A. 2 L 7 2 4F RT A6WE 2007051500042 20070515 00042 NM 2007 5 15 UPS07549796 1 20070511 A 5350 RADOME BOEING 757 75724APF 1384969 NM FUSELAGE FAILED A IPXA O OTHER O OTHER CL CLIMB 1 SO 01 452UP 25473 PILOT REPORT - DURING CLIMB HEARD SINGLE THUMP ON LOWER RIGHT SIDE OF NOSE OF A/C. RADOME SUSTAINED STRUCTURAL FAILURE. [SUP 05-18-07] R & R NOSE RADOME IAW AMM 53-12-01-4 AND PERFORMED WEATHER RADAR TEST. ALL CHECKS NORMAL. 2 L 7 2 4F RT A2NM 2007051500044 20070515 00044 WP 2007 5 15 UPS07849781 1 20070420 A 5330 SKIN DOUG DC8 DC873F 302199F WP FS 1400 L27R MISREPAIRED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 REMOVE STEEL DOUBLER FROM THE C-4 (D-PIT) UPPER FWD CORNER AND REPAIR PER SRM 53-2-0 FIG 21. REMOVED AND REPLACED DOUBLER AT C-4 (D-PIT) UPPER FWD CORNER IAW SRM 53-02-00 FIG 21, AND SRM TR 53-140, & 53-188, THIS REPAIR REQUIRES AN MPI WITH INITIAL INSPECTION AT 14000 LANDINGS, & REPETITIVE INSP AT EVERY 4400 LANDINGS IAW TR 53-188. 2 L 7 4 4F RT 4A25 2007051500045 20070515 00045 WP 2007 5 15 UPS07849782 1 20070426 A 5330 SKIN DOUG DC8 DC873F 302199F WP FS 1690 L32L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 FS 1690 L32L HAS A 1 INCH CRACK AND EXISTING REPAIR DOUBLER AT L30L SRM REPAIR WILL NOT BE INCOMPLIAN CE WITH EO DC8-5330-20248. CUT OUT DAMAGED AREA AT STA 1690 L32L IAW SRM 53-2-0. FABRICATED AND INSTALLED REPAIR DOUBL ER, FINGER DOUBLERS, AND FILLERS AT STA 1690 L30L -L34R IAW UPS EO DC8-5330-20248, AND SRM 53-02-01 FIG 7. 2 L 7 4 4F RT 4A25 2007051500047 20070515 00047 WP 2007 5 15 UPS07849788 1 20070424 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP FS 1766 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 AFT PRESS BULKHEAD CRACKED AT STA 1766 L10L, LBL 25 AND LBL 35. CUT OUT DAMAGED AREA AT STA 1766 LBL 25 AND LBL 35 IAW SRM 53-2-5 FIG 14A. FABRICATED AND INSTALLED REPAIR FILLERS, AND DOUBLERS AT STA 1766 LBL 25 AND LBL 35 IAW SRM 53-2-5 FIG 14, AND TR 53-194. THIS REPAIR REQUIRES DAMAGE TOLERENCE INSP WITH INITIAL AT 4,000 LANDINGS & R EPETITVE INSP AT EVERY 4000 LANDINGS THERE AFTER PER TR 53-194. 2 L 7 4 4F RT 4A25 2007051500051 20070515 00051 SO 2007 5 15 C2A07SH028 1 20070513 A 5320 14521713605 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17984 145246 SHV - DURING C-CHECK CORROSION ON CENTER OMEGA BEAM FROM FR 20 TO 23. MX REMOVED AND REPLACED CENTER OMEGA BEAM FROM FR 18-23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007051500054 20070515 00054 NM 2007 5 15 MWEA070114 1 20070511 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 917ME 55179 RIGHT THRUST REVERSER, UPPER DEFLECTOR DOOR HAS A CRACK ON END OF ZEE FRAME, INBOARD SIDE AT STATION 26.666. INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007051500055 20070515 00055 NM 2007 5 15 ASAA0741381 1 20070111 A 5753 SKIN BOEING 737 7374Q8 138447Q NM FORE FLAP MISREPAIRED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 02 774AS 25107 RIGHT I/B FORE FLAP HAS 2 REPAIRS WITHIN ONE INCH OF EACH OTHER. EDGE DISTANCE IS TOO SHORT PER SRM. REMOVED PREVIOUS REPAIRS, PREPPED AREA FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 51-70-10 REPAIR 1. 2 L 7 2 4F RT A16WE 2007051500056 20070515 00056 EA 2007 5 15 COMAO760371 1 20070514 A 5315 60034017351 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FS 295 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 929CA 7035 DURING HMV7 INSPECTION FOUND FLOOR SUPPORT CHANNEL CRACKED AT LEFT CORNER FS 295, LBL 10. INSTALLED NEW P/N 600-34017-3 51 CHANNEL IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007051500057 20070515 00057 WP 2007 5 15 UPS07849791 1 20070411 A 5711 55978341 SPAR CAP DOUG DC8 DC873F 302199F WP WING TANK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 CRACK ON LWR CENTER SPAR CAP FLANGE NEAR XRS 172 NR 2 MAIN TANK. REPAIRED WING CENTER LWR CAP AND WE B AT STA XRS 168 NR 2 MAIN TANK IAW SAA EA 008-5710-01-A0808, UPS EO DC8-5710-26734-A, SRO8570015, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007051500058 20070515 00058 NM 2007 5 15 UPS07M49674 1 20070311 A 5753 HINGE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:C RIGHT WING O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT PIN ATTACHMENT HOLE SPOT FACE FOUND CORRODED. RIG HT WING AFT O/B FLAP I/B HINGE PIVOT I/B BORE BUSHING & SPOTFACE CORROSION REMOVED & FOUND EXCESS LIMIT AS PER CMM 57-52 -04 PG 621-22 REV.57. FPI CARRIED OUT IAW DAC NDT 8PM R.13 PART 8 REWORKED AREA & FOUND NO CRACK & CORROSION EVIDENT. MPI CARRIED OUT PER DPS4.704 REV. AN ON FAB BUSHING NO CRACK EVIDENT. BUSHING INSTALLED AS PER EN 1208-07. 2 L 7 3 4F RT A22WE 2007051500059 20070515 00059 NM 2007 5 15 UPS07M49767 1 20070319 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 745-1129 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C MID CABIN - SEAT TRACK CROWN CORROSION AT STA 745 - 1129 LBL 8.5 AT SEVERAL LOC AS MARKED. CORROSION ON SEAT TRACK REMOVED PER SRM 51-21-01VIIR38 ORI THK 0.145" MATL REMOVED 0. 030" MATL REMAIN 0.115" EXCEED LIMIT PER SRM 53-70-00 FIG 3 VIR38. SEAT TRACK TRIM OFF PER SRM 53-70-00 FIG 1VIR38. HFEC C/O PER DACNDTSPMR13PT06.10.01 .001 NO CR ACK EVIDENT. NEW SEAT TRACK & SPLICE RWK PER SRM 53-70-00 FIG 1VIR 38. PROTECTED PER SRM 51-21-01VIIR38. INSTALLED PE R SRM 51-31-01 VIIR38. 2 L 7 3 4F RT A22WE 2007051500061 20070515 00061 NM 2007 5 15 UPS07M49793 1 20070319 A 5350 FRAME DOUG MD11 MD11F 3023600 NM TAIL CONE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C TAIL CONE ACCESS CUTOUT AFT FRAME DAMAGED AS MARKED. DAMAGED AREA ON BEAM, CHANNEL REMOVE. FOUND BEY OND LIMIT. MAT'L THK 0.04 0"X0.063" THK REMAIN 0.027"X0.040" THK REMOVED 0.013"X0.023" SRM 53-00-01VIR R38. DAMAGED BE AM, CHANNEL REMOVED SRM 51-31-01 VIIREV38. NEW BEAM, CHANNEL FAB USE 2024-0-0.040" & 2024-0-0.063" BOEING DWG AKC7528/7 546. ITEMS HEAT TREAT DPS 7.00-1, HARD HRB 61.8 DPS 1.05-3. ITEMS TREATED SRM 51-21. 2 L 7 3 4F RT A22WE 2007051500067 20070515 00067 NM 2007 5 15 DLM88070519 1 20070508 A 5210 SKIN DOUG MD88 MD88 3023688 NM L1 DOOR GOUGED A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 906DL 49537 FOUND ON ARRIVAL DAMAGE 2 FT AFT 1L DOOR AT FLOOR LEVEL A 5 INCH BY 1 INCH GOUGE. REPAIRED PER SRM 53-04D PAGE 33 ITEM B CLASS 1 REPAIR. WHILE DOWN FOR REPAIR ALSO WORKED MSU C/N C05037125 ACTL 3102 FOR PREVIOUS DAMAGE INCORP, ORATING A F OUR CORNER DOUBLER REPAIR PER SRM 53-04D PAGE 33 ITEM B CLASS 1 REPAIR. REF ITEM 011 OF LOGSHEET G774302. 2 L 7 2 4F RT A6WE 2007051500068 20070515 00068 NM 2007 5 15 DL764070520 1 20070511 A 2120 UNKNOWN BOEING 767 767432ER 1385134 NM CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 845MH 29719 PASSENGER NOTICED A FAINT ELECTRICAL ODOR SEAT 4C ON APPROACH. INSPECTED SEAT 4C AREA OPERATED SEAT LIGHTS GASPER. NO ELECTRICAL ODOR NOTICED. NO FAULTS FOUND. 2 L 7 2 4F RT A1NM 2007051500072 20070515 00072 NM 2007 5 15 DLM88070524 1 20070509 A 3213 592060213 STRUT DOUG MD88 MD88 3023688 NM NLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 PITTING CORROSION ON NOSE GEAR SHOCK STRUT. TIME LIMITED REPAIR INSTALLED PER ERA461314-14. PERMENANT REPAIR TO BE AC COMPLISHED 500 FLIGHT CYCLES FROM MAY 7,2007 OR NO LATER THAN JULY 4 2007. 2 L 7 2 4F RT A6WE 2007051500075 20070515 00075 NM 2007 5 15 DLM88070527 1 20070509 A 5523 5910414501 TAB DOUG MD88 MD88 3023688 NM LT ELEVATOR DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 SEVERAL DENTS AT TRAILING EDGE OF THE LT ELEVATOR GEARED TA, P/N 5910414-501 IN THE VICINTY AREA OG STATION XET = 119.75 . PERMENANT REPAIR WAS PERFORMED IAW SRM 55-04 PARA 3 FIG 2. APPLYING PROCEDURES EST IN SRM 51-70-2. 2 L 7 2 4F RT A6WE 2007051500076 20070515 00076 NM 2007 5 15 DLM88070528 1 20070510 A 5523 5910413507 TAB DOUG MD88 MD88 3023688 NM LT ELEVATOR DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 SEVERAL DENTS AT TRAILING EDGE OF THE LT ELEVATOR CONTROL TAB P/N 5910413-513 IN THE VINCINTY AREA OF STA. XET =80.75. PERMANENT REPAIR WAS ACCOMPLISHED IAW SRM 55-04 PARA 3 FIG 2 APPLYING PROCEDURES EST IN SRM 51-70-2. 2 L 7 2 4F RT A6WE 2007051500085 20070515 00085 NM 2007 5 15 DL76G070537 1 20070115 A 5330 SKIN BOEING 767 767332 1382001 NM BS 1274 S31-32R GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1608 30573 EXT FUSELAGE STA 1274 STR 31R TO STR 32R SKIN GOUGED. REPAIRED PER ERA 459461-14 TIME LIMITED REPAIR. 2 L 7 2 4F RT A1NM 2007051500086 20070515 00086 NM 2007 5 15 DL76G070538 1 20070115 A 5330 SKIN BOEING 767 767332 1382001 NM BS 618-628 S23R SCRATCHED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1608 30573 EXT FUSELAGE SKIN SCRATCHED BS 618-628 S23R. REPAIRED PER ERA 459504-14. 2 L 7 2 4F RT A1NM 2007051500088 20070515 00088 NM 2007 5 15 DL76G070540 1 20070115 A 5330 SKIN BOEING 767 767332 1382001 NM BS 1373 S28-29R GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1608 30573 EXT FUSELAGE RS AFT OF AFT PIT DOOR CUTOUT LWR SKIN SECTION STA 1373 BETWEEN STR 29R AND STR 28R SKIN HAS PREVIOUS GOUGE , ALSO HAS GAP UNDER FASTENER. REPAIRED PER SRM 53-00-01 FIG 201 REPAIR 14. 2 L 7 2 4F RT A1NM 2007051500093 20070515 00093 NM 2007 5 15 DLM88070547 1 20070510 A 5320 MEMBRANE DOUG MD88 MD88 3023688 NM BS 1485 L6R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 CRACKED MEMBRANE AND REPAIR DOUBLER ON FUSELAGE INNER STRUCTURE AT STA Y=1485 CANT LONG 6 RT. PERMENANT REPAIR INSTALLE D PER SRM 53-01 (AMX200602028). 2 L 7 2 4F RT A6WE 2007051500096 20070515 00096 NM 2007 5 15 DLM88070550 1 20070510 A 5753 VANE DOUG MD88 MD88 3023688 NM LT TE FLAP DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 EROSION AND DELAMINATION ON LOWER SURFACE DENTS ON UPPER SURFACE OF LT INNER FLAP OUTBD VANE. DOUBLER, FILLER REPAIR BO NDING WAS DONE IAW SRM 51-70-2D PARA H. REPAIRED IAW SRM 57-03D PARA 8A FIG 9A. 2 L 7 2 4F RT A6WE 2007051500097 20070515 00097 NM 2007 5 15 DLM88070551 1 20070510 A 5753 VANE DOUG MD88 MD88 3023688 NM RH TE FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 INADEQUATE REPAIR AND DELAMINATION ON RT INNER FLAP INNER VANE. FILLER, DOUBLER REPAIR WERE FABRICATED IAW SRM 57-03D P AR 8A FIG 9A ( SHEET 1 AND 2 ) RT INNER FLAP INNER VANE WAS REPAIRED IAW SRM 57-03 PAR 8A FIG 9A SHEET 1 AND 2 (AMX 2002 02768). 2 L 7 2 4F RT A6WE 2007051500098 20070515 00098 NM 2007 5 15 AALA20070734 1 20070423 A 3350 0201922001 SOCKET BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 658AA 24616 JFK - RED EMERGENCY SEAT PATH LIGHT AT SEAT 17D INOPERATIVE. FOUND WIRE BROKEN AT SOCKET. REPLACED SOCKET ASSEMBLY FOR RED EMERGENCY SEAT PATH LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007051500099 20070515 00099 NM 2007 5 15 AALA20070731 1 20070423 A 3350 P4010021000 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 945AN 30085 LGA - EMERGENCY FLASHLIGHT AT FORWARD JUMPSEAT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY FLASHLIGHT AT FORWARD J UMPSEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007051500100 20070515 00100 NM 2007 5 15 AALA20070732 1 20070423 A 3350 P4010021000 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 945AN 30085 LGA - EMERGENCY FLASHLIGHT AT AFT LEFT INBOARD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY FLASHLIGHT AT AFT LEFT INBOARD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007051500102 20070515 00102 WP 2007 5 15 AALA20070737 1 20070423 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7543A 53025 LGA - EMERGENCY CEILING LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY CEILING LIGHTS AT FOR WARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051500103 20070515 00103 NM 2007 5 15 AALA20070746 1 20070424 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 175AN 32394 SFO - EMERGENCY LIGHTS FROM SEAT ROWS 16DEF TO 25DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT ROWS 16DEF TO 25DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007051500104 20070515 00104 NM 2007 5 15 AALA20070750 1 20070425 A 3350 CM767 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 964AN 30093 LAX - LEFT NUMBER ONE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007051500105 20070515 00105 NM 2007 5 15 AALA20070751 1 20070426 A 2910 HOSE BOEING 757 757223 1384957 NM HYD SYSTEM FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 663AM 25297 JFK INFLIGHT T1853/26APR LGA TO MIA LANDED JFK DUE TO LOSS OF LEFT HYDRAULIC SYSTEM FAILED. PERFORMED MANUAL GEAR AND FLAP PROCEDURES. LANDED JFK OVERWEIGHT WITHOUT INCIDENT. FOUND HYDRAULIC LINE TO LEFT GEAR UNLOCK ACTUATOR FAILED. RE PLACED HOSE ASSEMBLY FOR LEFT GEAR UNLOCK ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007051500106 20070515 00106 NM 2007 5 15 UPS07M49795 1 20070409 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 859-899 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C MID CABIN - CORROSION ON SEAT TRACK CROWN & FLANGE AT STA 859 - 899 X= -8.0. SEAT TRACK PARTS REMOVED PER SRM 51-31-01 VOL 2 REV 38. CORRODED SEAT TRACK TRIMMED OFF PER SRM 53-70-00 FIG 1 VOL 1 REV 38. HFEC INSP CUTOUT & FOUND NO CRACK. CORRODED SEAT TRACK REPAIRED, SPLICE HAT, SPLICE HAT PLATE FAB PER SRM 53-70-00 VOL 1 FIG 1 REV 38. TRACK & FAB PARTS INSTALLED PER SRM 51-31-01 VOL 2 REV 38. 2 L 7 3 4F RT A22WE 2007051500107 20070515 00107 NM 2007 5 15 USAA070380 1 20070514 A 5753 65C263203 SKIN BOEING 737 7374B7 1384702 NM LT WING TE FLAP CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 LEFT OUTBOARD MID FLAP L/E SKIN AT INBOARD FORE FLAP OPENING HAS CRACK. INSTALLED SPLICE PLATE & FILLER PER SRM 57-53-0 1 REP 7, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007051500109 20070515 00109 NM 2007 5 15 USAA070382 1 20070514 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM BS 344 LBL 40 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 STA 344 LBL 40 HAS CORROSION. INSTALLED NEW T-CAP SECTION PER SRM 53-10-01; CORR TASK C53-107-02; LEVEL 2, DEFECT SIZE: 1 X 1 INCH. 2 L 7 2 4F RT A16WE 2007051500111 20070515 00111 NM 2007 5 15 USAA070384 1 20070514 A 5322 SHEAR TIE BOEING 737 7374B7 1384702 NM BS 360 S14-15L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 BETWEEN STR 14L & 15L AT STA 360 HAS CRACK. REPLACED SHEAR TIE PER SRM 51-10-02, BOEING DWG 65-58-280, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007051500112 20070515 00112 NM 2007 5 15 USAA070385 1 20070514 A 5313 STRINGER BOEING 737 7374B7 1384702 NM BS 360 S14L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 STR 14L STA 360 IS CRACKED. REPLACED STRINGER PER SRM 51-10-02, BOEING DWG 65-17685, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007051500113 20070515 00113 NM 2007 5 15 CALA0700239 1 20070512 A 5320 149N722269 STRUCTURE BOEING 757 757324 1384930 NM LT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 75854 32813 INSPECTION FOUND A 1 INCH CRACK IN LEFT WHEEL WELL CHORD LOCATED O/B AND AFT OF DOOR OPENING. THE CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007051500114 20070515 00114 NM 2007 5 15 CALA0700240 1 20070513 A 5320 149N722270 STRUCTURE BOEING 757 757324 1384930 NM RT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 75854 32813 INSPECTION FOUND A 1 INCH CRACK IN RIGHT WHEEL WELL CHORD LOCATED O/B AND AFT OF DOOR OPENING. THE CHORD WAS REMOVED AN D REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007051500115 20070515 00115 NM 2007 5 15 CALA0700241 1 20070513 A 5315 BAC1518399 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, RBL 43-54. THE CORRODED SECTION OF FLOORBEAM WAS REPLACED IAW SRM 51- 40-02. 2 L 7 2 4F RT A16WE 2007051500116 20070515 00116 NM 2007 5 15 CALA0700242 1 20070513 A 5315 BAC1518399 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND FLOORBEAM CORRODED AT FLOORBOARD MOUNT HOLES, STA 967, S17L TO S17R. REPAIRED FLOORBEAM IAW SRM 53-00- 51, FIGURE 201, PAGE 201. 2 L 7 2 4F RT A16WE 2007051500117 20070515 00117 2007 5 15 AALA20070736 4 20070423 A 2565 62772215 SLIDE BOEING 777 777223 1385213 NM L2 DOOR INOPERATIVE A AALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 21 758AN 32637 GRU - LEFT NUMBER TWO DOOR ESCAPE SLIDE DETACHED FROM THE DOOR AND FELL DOWN TO THE TRUCK STAIR. SLIDE HANDLE NOT DISAR MED WHEN THE DOOR WAS OPEN. REPLACED LEFT NUMBER TWO DOOR ESCAPE SLIDE AND DOOR ASSIST BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007051500118 20070515 00118 WP 2007 5 15 AALA20070735 1 20070423 A 2730 SERVO DOUG DC9 DC983 3022083 WP YAW DAMPER INOPERATIVE A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 948TW 49575 DFW INFLIGHT T2265/23APR ORD TO PVR - AT FLIGHT LEVEL 320 BOTH AUTOPILOTS AND YAW DAMPER INOPERATIVE. LANDED DFW WITHOU T INCIDENT. REPLACED ELEVATOR SERVO. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007051500121 20070515 00121 WP 2007 5 15 AALA20070748 1 20070425 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9622A 53593 DEN - EMERGENCY LIGHT IN COCKPIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN COCKPIT AT LOCATION 5 23. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007051500122 20070515 00122 NM 2007 5 15 AALA20070740 1 20070424 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 DFW - OVERHEAD EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. RELAMPED OVERHEAD EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007051500124 20070515 00124 NM 2007 5 15 AALA20070752 1 20070426 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 792AN 30253 MIA - EMERGENCY AISLE LIGHT AT SEAT 27B INOPERATIVE. RELAMPED EMERGENCY AISLE LIGHT AT SEAT 27B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007051500125 20070515 00125 NM 2007 5 15 AALA20070753 1 20070426 A 3397 CONTACT BOEING 767 767323 1385205 NM EMERGENCY LIGHT DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 358AA 24039 SFO - LEFT NUMBER TWO DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. CLEANED LEFT NUMBER TWO DOOR EMERGENCY LIGHT ASSEMBLY CONTACT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007051500126 20070515 00126 NM 2007 5 15 AALA20070749 1 20070425 A 3350 0201804001 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 955AN 29540 LGA - EMERGENCY LIGHT AT SEAT 10D HAS CRACKED LENS INOPERATIVE. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007051500127 20070515 00127 NM 2007 5 15 AALA20070756 1 20070426 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 941AN 29534 MIA - EMERGENCY LIGHTS AT SEAT 18D INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OP ERATION. 2 L 7 2 4F RT A16WE 2007051500128 20070515 00128 NM 2007 5 15 AALA20070757 1 20070426 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 946AN 30600 MIA - LEFT NUMBER FOUR DOOR EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007051500129 20070515 00129 NM 2007 5 15 AALA20070759 1 20070426 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 603AA 27054 MIA - LEFT DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED LEFT DOOR EXTERIOR EMERGENCY LIGHT. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007051500130 20070515 00130 NM 2007 5 15 AALA20070762 1 20070427 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 762AN 31479 MIA - EMERGENCY LIGHT AT SEAT 22G MISSING LENS INOPERATIVE. REPLACED LENS FOR EMERGENCY LIGHTS AT SEAT 22G. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007051500133 20070515 00133 NM 2007 5 15 AALA20070769 1 20070428 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 758AN 32637 DFW - EMERGENCY LIGHTS AT SEAT 34C MISSING LENS INOPERATIVE. REPLACED LENS FOR EMERGENCY LIGHTS AT SEAT 34C. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007051500134 20070515 00134 WP 2007 5 15 AALA20070770 1 20070428 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7544A 53026 LGA - EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD CABIN. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051500135 20070515 00135 NM 2007 5 15 AALA20070755 1 20070426 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 941AN 29534 MIA - EMERGENCY LIGHTS AT SEAT 15D INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OP ERATION. 2 L 7 2 4F RT A16WE 2007051500138 20070515 00138 NM 2007 5 15 AALA20070763 1 20070427 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 762AN 31479 MIA - EMERGENCY LIGHT AT SEAT 22G MISSING LAMPS. RELAMPED EMERGENCY LIGHTS AT SEAT 22G. SYSTEM GROUND CHECKED NORMAL O PERATION. 2 L 7 2 4F RT T00001SE 2007051500139 20070515 00139 NM 2007 5 15 AALA20070765 1 20070427 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 798AN 30797 MIA - EMERGENCY LIGHTS AT SEAT 23C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHTS AT SEAT 23C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007051500141 20070515 00141 NM 2007 5 15 AALA20070758 1 20070426 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 670AA 25335 DFW - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROW 11D INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 11D. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007051500142 20070515 00142 WP 2007 5 15 AALA20070771 1 20070428 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7544A 53026 LGA - OVERHEAD EMERGENCY LIGHT AT FORWARD LAVATORY INOPERATIVE. REPLACED BATTERY PACK B5 23 FOR EMERGENCY LIGHT AT FORW ARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051500143 20070515 00143 WP 2007 5 15 AALA20070772 1 20070428 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7544A 53026 LGA - EMERGENCY AISLE LIGHT AT SEAT 8D INOPERATIVE. RELAMPED EMERGENCY AISLE LIGHT AT SEAT 8D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F A6WE 2007051500144 20070515 00144 NM 2007 5 15 AALA20070764 1 20070427 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 798AN 30797 MIA - EMERGENCY LIGHTS AT SEAT 23C INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT SEAT 23C. SYSTEM GROUND CHECKED NORMAL OP ERATION. 2 L 7 2 4F RT T00001SE 2007051500146 20070515 00146 WP 2007 5 15 AALA20070773 1 20070428 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7544A 53026 LGA - EMERGENCY FLASHLIGHT AT AFT ENTRY DOOR HAS BROKEN BAND. REPLACED BAND FOR EMERGENCY FLASHLIGHT AT AFT ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051500147 20070515 00147 EU 2007 5 15 AALA20070775 1 20070428 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70054 461 MIA - EMERGENCY LIGHTS AT SEAT 10G INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT SEAT 10G. SYSTEM GROUND CHECKED NORMAL OP ERATION. 2 L 7 2 4F RT A35EU 2007051500148 20070515 00148 WP 2007 5 15 AALA20070778 1 20070428 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 501AA 49738 DFW - EMERGENCY LIGHTS AT OVERHEAD TAIL CONE INOPERATIVE. REPLACED BATTERY PACK B5 27 FOR OVERHEAD EMERGENCY LIGHTS AT TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051500150 20070515 00150 NM 2007 5 15 AALA20070790 1 20070430 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 637AM 24595 MIA - EMERGENCY LIGHT AT SEAT 12D INOPERATIVE. RECONNECTED CONNECTOR ASSEMBLY AT SIDEWALL FOR EMERGENCY LIGHT AT SEAT 1 2D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007051500152 20070515 00152 NM 2007 5 15 AALA20070782 1 20070429 A 3350 8039001 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9414W 53189 LGA - EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 23 FOR EMERGENCY LIGHTS AT FORWARD CAB IN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2007051500153 20070515 00153 WP 2007 5 15 AALA20070783 1 20070429 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 417AA 49328 ATL - EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051500155 20070515 00155 NM 2007 5 15 AALA20070786 1 20070430 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 795AN 30257 MIA - EMERGENCY LIGHT AT FORWARD GALLEY COMPARTMENT HAS BROKEN WIRES AND CRACKED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FORWARD GALLEY COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007051500156 20070515 00156 EA 2007 5 15 A6WA207740179 1 20070401 A 5340 SUPPORT FITTING CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR ASSIST CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 457AW 7854 PAX - DOOR ASSIST MOTOR SUPPORT FITTING (PN 601R317745-7) CRACKED APPROX .2 INCH LONG. MAINTENANCE TRIMMED OUT CRACKED IAW BSC EO 601R-52-11427. (M) 2 L 7 2 4F RT A21EA 2007051500162 20070515 00162 NM 2007 5 15 USAA070386 1 20070514 A 5313 STRINGER BOEING 737 7374B7 1384702 NM BS 360 S15L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 STR 15L AT STA 360 HAS CRACK. INSTALLED NEW STRINGER PER SRM 51-10-02 & BOEING DWG G5-17685, DEFECT SIZE: .75 INCH. 2 L 7 2 4F RT A16WE 2007051500163 20070515 00163 NM 2007 5 15 USAA070387 1 20070514 A 5330 SKIN BOEING 737 7374B7 1384702 NM BS 727F S24R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 STA 727F AND S-24R HAS CRACK. INSTALLED DOUBLER PER SRM 53-00-01, DEFECT SIZE: 1.5 INCH. 2 L 7 2 4F RT A16WE 2007051500166 20070515 00166 EA 2007 5 15 A6WA200740164 1 20070316 A 2611 PU90421R3 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LAVATORY MALFUNCTIONED A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 440AW 9482 7766 SMOKE TOILET CASS MESSAGE AFTER TAKEOFF WITH LAV SMOKE ALARM ACTIVATED RAN QRH, MESSAGE EXTINGUISHED ALARM OFF F/A REPPO RTED NO INDICATION OF SMOKE OR FIRE ON INSPECTION. RAN ENGINE WITH APU AIR SWITCH OVER TO BLEED AIR AND NO SMOKE CAUTIO N MESSAGE WITH EITHER APU OR ENGINE SUPPLYING PACKS NO EXTERNAL ENGINE OIL LEAKS NOTED. SUSPECT FAULTY LAV SMOKE DETECT ION SYSTEM. REMOVED AND REPLACED SMOKE DETECTOR UNIT, OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007051500169 20070515 00169 2007 5 15 DATA200700001 4 20070405 A 2312 39100024 AUDIO PANEL STBROS SD3 SD330 8100602 EU NR 1 VHF INTERMITTENT E DATA O OTHER O OTHER NR NOT REPORTED 1 GL 13 330AC SH3007 NUMBER 2 VHF RADIO INOP. NUMBER 1 VHF RADIO INTERMITTENT. CLEANED F/O AUDIO SELECT PANEL CONNECTORS. 2 H 7 2 4T A41EU 2007051500171 20070515 00171 NM 2007 5 15 USAA070370 1 20070514 A 5340 STRINGER CLIP BOEING 737 7374B7 1384702 NM BS 294 S13L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 STA 294.5 S13L CRACK ON TIE CLIP. REMOVED & MADE NEW CLIP, TREATED, PRIMED & INSTALLED PER SRM 51-20-01, BOEING DWG 65- 1633, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007051500172 20070515 00172 NM 2007 5 15 USAA070371 1 20070514 A 5320 INTERCOSTAL BOEING 737 7374B7 1384702 NM BS 328-344 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 INTERCOSTAL STA 328-344, LBL 44 HAS CRACK. REMOVED & INSTALLED NEW INTERCOSTAL PER SRM 51-10-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007051500175 20070515 00175 NM 2007 5 15 USAA070374 1 20070514 A 5322 SHEAR TIE BOEING 737 7374B7 1384702 NM BS 277 S9-10L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 RADIUS BS 277 BETWEEN S9L & S10L FRAME SHEAR TIE HAS CRACK. REMOVED & REPLACED SHEAR TIE PER SRM 51-70-11, DEFECT SIZE: 1.5 INCH. 2 L 7 2 4F RT A16WE 2007051500176 20070515 00176 NM 2007 5 15 USAA070375 1 20070514 A 5311 FRAME BOEING 737 7374B7 1384702 NM BS 277 S10L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 BS 277 FRAME WEB AT TIE CLIP S10L INBOARD ATTACH FASTENER HAS CRACK. INSTALLED FABRICATED REPAIR CHANNEL PER SRM 53-00- 07, DEFECT SIZE: 1.25 INCH. 2 L 7 2 4F RT A16WE 2007051500177 20070515 00177 NM 2007 5 15 USAA070376 1 20070514 A 5414 SKIN BOEING 737 7374B7 1384702 NM PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 FWD UPPER CORNER OF ACCESS PANEL 5724L OPENING, PYLON SKIN HAS CRACK. INSTALLED REPAIR DOUBLER PER TR 54-50-07, DEFECT SIZE: .125 INCH. 2 L 7 2 4F RT A16WE 2007051500178 20070515 00178 NM 2007 5 15 USAA070369 1 20070514 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM BS 178 CANNING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 OIL CANNING & MATERIAL LOSS AT 178 BULKHEAD. INSTALLED REPAIR DOUBLER PER EA 98632, DEFECT SIZE: 3 INCHES DIA. 2 L 7 2 4F RT A16WE 2007051500179 20070515 00179 NM 2007 5 15 USAA070378 1 20070514 A 5320 ANGLE BOEING 737 7374B7 1384702 NM BS 294 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 STA 294 AT FWD SERVICE DOOR HAS CRACK. DRILLED & INSTALLED NEW PART PER SRM 51-10-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007051500180 20070515 00180 EU 2007 5 15 USAA070388 1 20070514 A 5315 D5311281820401 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 179UW 1521 FLOORBEAM Y254 HAS CORROSION. REMOVED & REPLACED BEAM PER SRM 51-72-11; CORR TASK JA-220-53500, LEVEL 1, DEFECT SIZE: 2.5 X 3.5 INCHES. 2 L 7 2 4F RT A28NM 2007051500182 20070515 00182 NE 2007 5 15 HNAA0700084 2 20070509 A 7321 ECU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 MALFUNCTIONED A HNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 07 826EX 389 121230 NR 1 ENGINE TORQUE FLUX = OR - 10 PERCENT IN FLIGHT ALONG WITH ASSOCIATED NH, ITT, AND FUEL FLOW. RETURNED TO MDT. REP LACED NR 1 ECU OPS CHECK GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2007051500184 20070515 00184 SO 2007 5 15 EAVA200701117 2 20070503 A 8500 ENGINE CESSNA 414 414A 2075907 CE CONT O520 TSIO520* 17040 SO MCAULY 3AF32C 3AF32C* GL RIGHT VIBRATION E EAVA E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 GL 09 416RA 414A0486 208086J 901380 AT CRUISE ENGINE DEVELOPED VIBRATION. REQUESTED DESCENT AND TURN TO NEAREST SUITABLE FIELD. REDUCED ENGINE POWER TO ID LE ON DOWNWIND, FELT A JOLT AND SAW RIGHT ENGINE ACCESS PANEL PUSH OUT. FEATHERED AND SECURED RIGHT ENGINE AND LANDED. 1 L 7 2 3O 3 O A7CE E8CE 5 C P22EA 2007051500185 20070515 00185 NM 2007 5 15 P5CA0701521 1 20070403 A 2420 766088A IDG BOEING 747 74746NF 13848BT NM NR 2 FAILED A P5CA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 15 454PA 30812 ELEC BUSS ISLN 4, NO LAND 3, ENG 2&3 REV, ELEC GEN 2, NR 1 CDU INTERMITTENT. REPLACED NR 2 IDG PER MM 24-11-01 AND REPL ACED NR 2 GCU PER MM 24-23-01. OPS CHECK NORMAL. IT IS BELIEVED THAT NR 2 GEN WAS CAUSING ALL OTHER INDICATIONS TO FLU CTUATE. GCU P/N 746011L; S/N 1952. IDG P/N AND S/N INCLUDED ABOVE. 2 L 7 4 4F RT A20WE 2007051400021 20070514 00021 NM 2007 5 14 07FDEA01710 1 20070506 A 5711 SPAR CAP DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RIGHT WING, TRAILING EDGE REAR SPAR UPPER CAP FOUND CORROSION AT XORS 1042. [SUP 05-22-07] REPAIRED AS PER FEDEX EA 1- 5710-111099. 2 L 7 3 4F RT A22WE 2007051400024 20070514 00024 WP 2007 5 14 07FDEA01713 1 20070507 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 MAIN DECK SEAT TRACK SCALLOP WORN STA 1490 RBL 47. REMOVED, FABRICATED, INSTALLED SEAT TRACK SECTION IAW DC/MD10 SRM 53 -70-00 VOL I PAGE 22 AND 53-42-01 VOL III, MAJOR REPAIR. 2 L 7 3 4F A22WE 2007051400037 20070514 00037 NM 2007 5 14 07FDEA01720 1 20070508 A 5312 6518745 PRESSURE PANEL BOEING 727 7272S2F 1384O81 NM BS 931-932 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 LT W/W PRESSURE DECK LOWER SURFACE HAS SURFACE CORROSION AT WL 208, BS 931- 932, LBL 5"-7". REPAIRED LT W/W PRESSURE D ECK LOWER SURFACE AT WL 208, BS 931-932, LBL 5"-7" IAW SRM 51-10-6 PAGE 12 AND IAW SRM 51-10-2 2 L 7 3 4F A3WE 2007051400043 20070514 00043 WP 2007 5 14 07FDEA01727 1 20070509 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 397FE 46631 ACF MODIFICATION AND REPAIR ASSESSMENT LT MLG WHEEL WELL: AT STA 1510, AT X = 30 FOUND LONG WITH CRACK THE 1 INCH ACCOM PLISHED CRACK STOP DRILL 1/4 '' DIA AND REPAIRED LONGERON IAW SRM 53-00-01 FIG 9 VOL I. 2 L 7 3 4F A22WE 2007051400047 20070514 00047 NM 2007 5 14 QXEA200700770 1 20070502 A 2760 SPOILER BOMBDR DHC8 DHC8402 1390042 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - LEFT HAND OUTBOARD SPOILER, OUTBOARD END IS CHAFED WHERE CONTACTS OUTBOARD FLAP. REPAIRED IAW RD8/4-57-795. 2 H 7 2 4T RT A13NM 2007051400048 20070514 00048 NM 2007 5 14 QXEA200700771 1 20070502 A 5311 FRAME BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - FUSELAGE FRAMES IS GOUGED AT STATION X722.102, LEFT HAND SIDE CABIN, INBOARD FLANGE TOP SURFACE AT CABIN FLOOR LEVEL. REPAIRED IAW SRM 53-40-15 AND RD8/4-53-1904. 2 H 7 2 4T RT A13NM 2007051400051 20070514 00051 NM 2007 5 14 QXEA200700753 1 20070424 A 5320 ANGLE BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - CORROSION AT END OF ANGLE ATTACHED TO INTERCOSTAL, INBOARD OF LAY SHAFT AT STATION X19.4. REPAIRED IAW SRM 51- 21-00, 51-40-15. 2 H 7 2 4T RT A13NM 2007051400054 20070514 00054 EU 2007 5 14 07FDEA01732 1 20070509 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 6 AREAS OF CORROSION EXIST AT MDCC SEAT TRACK L-2 BETWEEN FRAMES 63 AND 64 THRU FRAME 70, DEFECTED AREA MEASURES 10 SQ I NCHES DUE TO AREA OF CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED SEAT TRACK BY SPLICING IN NEW TRACK SECTION IAW A310 -200 SRM 53-10-16. 2 L 7 2 4F RT A35EU 2007051400063 20070514 00063 WP 2007 5 14 07FDEA01749 1 20070510 A 5347 492915012000 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 MAIN DECK LEFT SIDE SEAT TRACK SCALLOP WORN AT STA 1139 LBL8. REMOVED, FABRICATED AND INSTALLED SEAT TRACK SECTION IAW DC/MD10 SRM 53-70-00 VOL I FIG1 SHT 1, 53-70-00 VOL 1 FIG 5 SHT 1 AND 51-21-01 VOL II PAGE 21, 25. 2 L 7 3 4F A22WE 2007051400073 20070514 00073 EA 2007 5 14 COMA0760352 1 20070501 A 3234 555406 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 929CA 27657 7035 FLIGHT 9461- GEAR DISAGREE WARNING AND NOSE DOOR OPEN MESSAGE WHEN GEAR SELECTED DOWN. REMOVED AND REPLACED NLG SELECTO R VALVE. 2 L 7 2 4F RT A21EA 2007051400078 20070514 00078 EA 2007 5 14 COMA0760355 1 20070501 A 3250 STEERING SYS CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA K NONE N FALSE WARNING CR CRUISE 1 SO 01 420CA 7451 FLIGHT 5620 - NWS INOP CAUTION MESSAGE IN FLIGHT, WOULD NOT RESET. RESET SYS AND PERFORMED OPS CHECK OF NWS SYS WITH NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007051400094 20070514 00094 WP 2007 5 14 UPS07849784 1 20070511 A 3260 DOWNLOCK SWITCH DOUG DC8 DC873F 302199F WP LT MLG INOPERATIVE A IPXA K NONE N FALSE WARNING AP APPROACH 1 SO 01 811UP 46089 INSPECTION TYPE:N/A EMERGENCY DECLARED - LEFT MAIN GEAR LIGHTS DID NOT ILLUMINATE GREEN. REPLACED BULBS WITH KNOWN BULB S THAT WORKED BUT STILL COULD NOT GET GREEN LIGHTS TO ILLUMINATE. WITH THE FLAPS AT 35 DEG THE LANDING GEAR WARNING HOR N DID NOT SOUND. T/S AND FOUND FAULTY DOWN SWITCH ASSY PER DC8 MM 32-60-00-1. REMOVED AND REPLACED FAULTY SWITCH. A/C READY FOR SERVICE. 2 L 7 4 4F RT 4A25 2007051400109 20070514 00109 NM 2007 5 14 MWEA070110 1 20070509 A 7830 7150923REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 916ME 55178 CRACK BEGINNING TO FORM IN LEFT THRUST REVERSER BOTTOM BUCKET, OUTBOARD SIDE, IN ZEE FRAME RADIUS STATION 35.699. INSTA LLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007051400114 20070514 00114 NM 2007 5 14 SWAA072367 1 20070510 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED C4 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007051400116 20070514 00116 NM 2007 5 14 SWAA072369 1 20070510 A 5315 6545410 FLOORBEAM BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 744A, RBL 25. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007051400122 20070514 00122 NM 2007 5 14 SWAA072372 1 20070510 A 5330 6545766 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504D, STR 14L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007051400125 20070514 00125 NM 2007 5 14 SWAA072365 1 20070510 A 5311 6545805 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 277, BL 0, WL 182.1. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007051400129 20070514 00129 NM 2007 5 14 SWAA072374 1 20070510 A 5311 6546529 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440 ,STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007051400152 20070514 00152 EA 2007 5 14 COMA0760365 1 20070507 A 2750 860D10018ABCD CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAULTY A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 914CA 8793 7012 FLIGHT 5458 - AFTER LANDING, FLAPS SELECTED TO 20, FAILED AT 26 LT AND 28 RT. PERFORMED EO 27-046AD. REPLACED FECU. N O FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007051400153 20070514 00153 EA 2007 5 14 COMA0760366 1 20070508 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 929CA 31723 7035 TWO CRACKS VERIFIED WITH EDDY CURRENT ON SEMI-PRESSURE BULKHEAD AT FS 559 BETWEEN RBL 9 AND RBL 18. REPAIRED SEMI-PRESS URE BULKHEAD AT FS 559 AS PER REO 601R-53-41-353. 2 L 7 2 4F RT A21EA 2007051400176 20070514 00176 EA 2007 5 14 TRAX200700639 1 20070508 A 5210 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 PAX DOOR AFT DRAG ANGLE CRACKED (MARKED). [SUP 05-17-07] CUTOUT DAMAGED SECTION OF PAX DOOR AFT DRAG ANGLE IAW REO 670- 52-11-072. DC699 5-14-07. 2 L 7 2 4F RT A21EA 2007051400184 20070514 00184 EU 2007 5 14 TRBA2007007 1 20070306 A 3350 7012210 LIGHT AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE CABIN INOPERATIVE A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 322AC 320 PERFORMING POST FLIGHT CREW NOTED LT FWD EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED FWD FLOOD LIGHT BULB IAW JIC 33-50 -00. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007051400188 20070514 00188 EU 2007 5 14 07FDEA01757 1 20070510 A 5200 ACCESS PANEL AIRBUS 300 A300F4605R 3930327 EU DAMAGED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 669FE 774 ON TAKEOFF WHEN LANDING GEAR WAS RETRACTED THE LEFT MAIN GEAR DOOR AMBER LIGHT STAYED ILLUMINATED ON BOTH THE OVERHEAD AND FORWARD PANEL. DROPPED LEFT GEAR DOOR AND DISCOVERED INNER ACCESS PANEL TO LEFT PACK LAYING ON GEAR DOOR. (SMASHED ) UNABLE TO REINSTALL ACCESS PANEL. DOOR OPENS AND CLOSES NORMALLY, INSPECTED LEFT MAIN GEAR DOOR AND LEFT GEAR FOR DA MAGE, NONE FOUND. PERFORMED DUMMIE RETRACT. [SUP 05-14-07] INSTALLED SERVICEABLE PER SMP. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2007051400194 20070514 00194 NM 2007 5 14 DL76L070478 1 20070506 A 2131 CONTROLLER BOEING 767 767332 1382001 NM CABIN PRESSURE MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 179DN 25144 CABIN AUTO INOP LIGHT ILLUMINATED ON TAXI OUT. T/S PER FIM. PERFORMED CABIN PRESSURE CONTROLLER BITE FOR SYS 1 AND 2. VERIFIED NO FAULTS ON BOTH CONTROLLERS. RESET ALL CHKS GOOD. NO LIGHT AND EICAS MSG. 2 L 7 2 4F RT A1NM 2007051400201 20070514 00201 NM 2007 5 14 AMTA200700202 1 20070424 A 2150 3964801 CONTROL VALVE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LT PACK UNSERVICEABLE A AMTA K NONE J WARNING INDICATION CR CRUISE 1 GL 11 517AT 27973 EICAS MSG L PACK OFF WITH SWITCH IN AUTO POSITION. PACK OFF LIGHT REMAINS ON WITH SWITCH MOVED TO STBY N, C OR W. REMO VED AND REPLACED FLOW CONTROL AND SHUTOFF VALVE IAW MM 21-51-01-2. OPS NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007051400206 20070514 00206 NM 2007 5 14 AMTA200700215 1 20070503 A 4990 FILTER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE APU OIL SYS DIRTY A AMTA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 522AT 29330 APU FAILED TO START, APU FAULT MESSAGE - ECU SHOWS LOP SHUTDOWN. FOUND DELTA P ON OIL PRESS FILTER POPPED REPLACED FILT ER. RESET DELTA P, RAN APU NO FAULTS NOTED. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007051400207 20070514 00207 NE 2007 5 14 TRBA2007014 2 20070330 A 7324 263701 FLOW DIVIDER AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE RT ENGINE DEFECTIVE A TRBA O OTHER X ENGINE FLAMEOUT AP APPROACH 1 SO 29 447AM 447 ON APPROACH RT ENGINE FLAME OUT, LANDED SUCCESSFULLY. REPLACED RT ENGINE FUEL NOZZLE KIT, AND FUEL FLOW DIVIDER IAW MM 71-01-40. PERFORMED ENGINE RUN-UP AND FOUND SATISFACTORY. (K) 2 H 7 2 4T 4 T RT E20NE 2007051400209 20070514 00209 CE 2007 5 14 AXS2007F00001 1 20070403 A 2612 61423179275 FIRE DETECTOR BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL LT ENGINE SHORTED E AXSA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 65 192WA U152 DURING CLIMB OUT, THE LT ENGINE FIRE WARNING LIGHT CAME ON. THE PILOT DECLARED AND EMERGENCY, RETURNED TO BASE, LANDED WITHOUT INCIDENT. THE PILOT DID NOT SEE FLAMES OR SMOKE COMING FROM THE ENGINE AND DID NOT HAVE ANY OTHER INDICATIONS OF AN ENGINE FIRE, THEREFORE HE DID NOT SHUT THE ENGINE DOWN INFLIGHT. MAINTENANCE INSPECTED THE ENGINE FOR SIGNS OF FI RE AND NONE WERE FOUND. TROUBLESHOOTING OF THE LT FIRE DETECTION SYSTEM REVELED A BAD FIRE DETECTOR AT THE 12 O`CLOCK P OSITION ON THE LT ENGINE. WHEN THE WIRES WERE MOVED GOING INTO THE DETECTOR THE WARNING LIGHT WOULD ILLUMINATE. MAINTE NANCE REPLACE THE FIRE DETECTOR, OPERATION CHECKED, OK, AND THE AC WAS RETURNED TO SERVICE. (K) 1 L 7 2 3T 4 T A14CE E4EA 6 C P15EA 2007051400211 20070514 00211 NE 2007 5 14 TRB2007F00001 2 20070330 A 7313 FUEL NOZZLE AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE RT ENGINE DEFECTIVE A TRBA O OTHER X ENGINE FLAMEOUT AP APPROACH 1 SO 29 447AM 447 ON APPROACH RT ENGINE FLAMED OUT. LANDED SUCCESSFULLY. REPLACED RT ENGINE FUEL NOZZLE KIT, AND FUEL FLOW DIVIDER IAW M M 71-01-40. PERFORMED ENGINE RUN-UP AND FOUND SATISFACTORY. (K) 2 H 7 2 4T 4 T RT E20NE 2007051400213 20070514 00213 NM 2007 5 14 AMTA200700189 1 20070411 A 3350 D7171100 BATTERY PACK BOEING 737 73783N 13844HI NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 310TZ 28243 L1 ENTRY DOOR AREA EGRESS LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK IAW MM 35-51-06-2. OPS CHECKS GOOD. OK FOR S ERVICE. (K) 2 L 7 2 4F RT A16WE 2007051400225 20070514 00225 NM 2007 5 14 AMTA200700208 1 20070429 A 3620 41SG2651 TRANSDUCER BOEING 737 73783N 13844HI NM BLEED AIR SYS MALFUNCTIONED A AMTA K NONE N FALSE WARNING TO TAKEOFF 1 GL 11 319TZ 30643 LT DUCT PRESSURE INCREASED WITH APPLICATION OF T/O POWER AND THEN IMMEDIATELY DROPPED TO ZERO. NO MASTER CAUTION OR WAR NING LIGHTS. REMOVED AND REPLACED LT PRESSURE TRANSDUCER REF 36-21-01-4. OPS CHECK NORMAL. (K) 2 L 7 2 4F RT A16WE 2007051500009 20070515 00009 NM 2007 5 15 DLM88070496 1 20070508 A 3297 G237D20BL WIRE DOUG MD88 MD88 3023688 NM NLG BROKEN A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 966DL 53115 ON DEPARTURE FROM MCO, RED NLG UNSAFE LIGHT REMAINED ILLUM WITH HANDLE UP NOSE GEAR IND PIN WAS FLUSH NO VIBES FELT PER CL LANDING HANDLE MOVED TO EXT POSITION NOSE GEAR REMAIN RED NLG IND PIN IND GEAR WAS DOWN AND LOCKED. BIT CHK OF PSEU IND FAULT CODE 457 NLG SENSOR DOWNLOCK WIRING FOUND AND REPAIR BROKEN SENSOR WIRE PSEU BITE CKS NML NLG SWUNG AND NOW CK S NORMAL. 2 L 7 2 4F RT A6WE 2007051500013 20070515 00013 NM 2007 5 15 DL76P070500 1 20070425 A 5315 7075T6 FLOORBEAM BOEING 767 767332 1382001 NM BS 287 RBL18 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1402A 25989 FWD GALLEY FLOOR SUPPORT TOP SURFACE CORRODED STA 287 RBL18. REPAIRED PER SRM 53-00-51D REF NR 67268820001 STA 287 FLOO RBEAM. 2 L 7 2 4F RT A1NM 2007051500015 20070515 00015 NM 2007 5 15 DL76G070502 1 20070510 A 2520 ACTUATOR BOEING 767 767332 1382001 NM SEAT FOOTREST ODOR A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 176DZ 29697 ELECTRICAL SMELL WHEN OPERATING SEAT 4F. REPLACED LEGREST AND FOOTREST ACT ALSO INSPECTED HARNESS FOR CHAFING NONE FOUN D ADJ SEAT BACK ACT CKS OK MCO/PLAC REMOVED. 2 L 7 2 4F RT A1NM 2007051500020 20070515 00020 NE 2007 5 15 DL76L070479 2 20070507 A 7261 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 LEAKING A DALA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 27 187DN 51136 27582 101004 DUE NUMBER 2 ENG EXCESSIVE HIGH OIL CONSUMPTION, PERFORMED EXT INSPECTION. NO OIL LEAK NOTED AFTER ENG RUN UP. AIRCRAF T POSITIONED FERRY TO ATL ON FLT 9903 DUE TO EXISTING PROBLEM WITH THE NR 3 BEARING LEAK INTO THE TAILPIPE. LEAK HAS PR OGRESSED PAST OIL CONSUMPTION LIMIT AND WILL REQUIRE ENG CHANGE. NR 2 E/C C/W PER TRANS 1T149. 2 L 7 2 4F 4 F RT A1NM E24NE 2007051500025 20070515 00025 NM 2007 5 15 DLM88070487 1 20070507 A 7120 59357112 MOUNT DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE RT ENGINE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 101004 RT PYLON FRONT SPAR ENGINE MOUNT FITTING LOWER HOLE HAD CORROSION IN THE BORE AND SURROUNDING FORWARD FACE. REPAIRED PE R ER/A 461312-14. 2 L 7 2 4F 4 F RT A6WE E9NE 2007051500035 20070515 00035 NM 2007 5 15 DLM88070512 1 20070510 A 5330 5920323249 SKIN DOUG MD88 MD88 3023688 NM FUSLEAGE WRINKLED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 WRINKLES IN FUSELAGE SKIN STA Y294.00 TO Y=351.00 AND BETWEEN LONGERONS 24 AND 26 RT. DAMAGED SKIN WAS REPLACED USING A PERMANENT REPAIR IAW SRM 53-04 FIG 12C. 2 L 7 2 4F RT A6WE 2007051500050 20070515 00050 EA 2007 5 15 COMA0760370 1 20070514 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 640 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 929CA 7035 DURING HMV7 INSPECTION FOUND REAR PRESSURE BULKHEAD CRACKED AROUND LINTEL FITTING. REMOVE DAMAGE AND INSTALLED DOUBLER PER BOMBARDIER REO 601R-53-61-2168 AND REO 301R-53-61-1230. 2 L 7 2 4F RT A21EA 2007051500060 20070515 00060 NM 2007 5 15 UPS07M49792 1 20070511 A 5321 FLOOR PANEL DOUG MD11 MD11F 3023600 NM MAIN CARGO DECK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP 48575 INSPECTION TYPE:N/A AFT CARGO FLOOR PANEL DAMAGED. REPAIRED IAW SRM 53-60-00. 2 L 7 3 4F RT A22WE 2007051500064 20070515 00064 NM 2007 5 15 DL76L070515 1 20070331 A 5415 311T31521 FITTING BOEING 767 767332 1382001 NM NR 1 NACELLE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 191DN 28448 THE NR 1 PYLON MID SPAR ATTACH FITTING WAS DAMAGED BY AND ELECTRICAL SHORT. THE DAMAGED AREA OF THE FITTING WAS BLENDED AWAY, NO REINFORCEMENT NECESSARY. 2 L 7 2 4F RT A1NM 2007051500065 20070515 00065 NM 2007 5 15 DL76S070516 1 20070316 A 5314 145T87609 KEELBEAM BOEING 767 767332 1382001 NM FS 1042 WL 157 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 132DN 24981 THE KEEL BEAM AT FS 1402, WL 157 WAS FOUND WITH A VERTICAL CRACK JUST FORWARD OF THE STA 1043 STIFFENER. THE CRACKED AR EA WAS CUT OUT AND A DOUBLER WAS INSTALLED. 2 L 7 2 4F RT A1NM 2007051500066 20070515 00066 NM 2007 5 15 DL738070517 1 20070316 A 5330 147A311011 SKIN BOEING 737 737832 13844CF NM FS 1013 PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3767 30821 THE FUSELAGE SKIN, STRINGERS, AND FRAMES WERE DAMAGED FROM GROUND DAMAGE. THE DAMAGED SKIN, STRINGERS, AND FRAMES WERE CUT OUT AND DOUBLERS AND REPAIR ANGELS WERE INSTALLED. 2 L 7 2 4F RT A16WE 2007051500070 20070515 00070 NM 2007 5 15 DLM88070522 1 20070510 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 560-588 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 LIGHTNING STRIKES DAMAGE AT THREE LOCATIONS ON AIRPLANE SKIN, BETWEEN STA Y=560 AND STA Y=588 AND BETWEEN LONGERONS 26 A ND 27 LT. PERMANENT REPAIR INSTALLED IAW AERO MEXICO DRAWING NO#AMR0953606 R02. DOCUMENTED IN DELTA ERA 461310-14. 2 L 7 2 4F RT A6WE 2007051500074 20070515 00074 NM 2007 5 15 DL76G070526 1 20070512 A 2841 300710404 PROCESSOR BOEING 767 767332 1382001 NM FUEL QTY FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1609 30574 DURING FUELING RT FUEL QTY DISPLAY IN FLIGHT COMPARTMENT INOP. RESET C/B QTY 1 AND 2 ALSO READ OUT FUEL QTY PROCESSOR F AULTS INDICATED AL COMPENSATORS AFTER CLEARED MEMORY RERACKED PROCESSOR NO HELP IND BLANK. REPLACED F/Q PROCESSOR BORRO WED FROM KLM AND OPS CK OK. 2 L 7 2 4F RT A1NM 2007051500095 20070515 00095 NM 2007 5 15 DLM88070549 1 20070510 A 5320 3031346002 FITTING DOUG MD88 MD88 3023688 NM BS 218 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 FOUND CRACK ON FWD JACK POINT FITTING. NEW JACK POINT FITTING WAS INSTALLED IAW DWG 9951888 (AMX 200301685). 2 L 7 2 4F RT A6WE 2007051500101 20070515 00101 NM 2007 5 15 AALA20070733 1 20070423 A 3350 P4010021000 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 945AN 30085 LGA - EMERGENCY FLASHLIGHT AT AFT RIGHT INBOARD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY FLASHLIGHT AT AFT RIGH T INBOARD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007051500108 20070515 00108 NM 2007 5 15 USAA070381 1 20070514 A 5320 SUPPORT ANGLE BOEING 737 7374B7 1384702 NM BS 312-344 S17L CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 STA 312-344 S-17L, ENTRY DOOR SILL SUPPORT ANGLE HAS CORROSION. REMOVED ANGLE, DRILLED NEW & INSTALLED PER SRM 51-10-02 , 51-20-01; CORR TASK C53-100-02, LEVEL 2, DEFECT SIZE: 10 INCHES. 2 L 7 2 4F RT A16WE 2007051500132 20070515 00132 EU 2007 5 15 AALA20070768 1 20070428 A 5210 ACCUMULATOR AIRBUS 300 A300B4605R 3930308 EU L1 DOOR LOW PRESSURE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14077 612 MIA - LEFT NUMBER ONE DOOR EMERGENCY NITROGEN BOTTLE DAMPER ACCUMULATOR POUNDS PER SQUARE INCH IS BELOW LIMIT. SERVICED LEFT NUMBER ONE DOOR EMERGENCY NITROGEN BOTTLE DAMPER ACCUMULATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007051500157 20070515 00157 2007 5 15 R61A20070009 4 20070425 A 3140 70244401903 POWER SUPPLY EMB ERJ170 ERJ170100SU 3260403 NM NR 1 MAU INOPERATIVE A R61A O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 818MD 17000039 CREW REPORTED WHILE SETTING UP FOR APPROACH HAD MAU 1B FAIL ALONG WITH A SPOILER FAULT. CREW DECLARED AN EMERGENCY FOLL OWED QRH PROCEDURES LANDED WITHOUT INCIDENCE. MAINTENANCE WAS DISPATCHED TO A/C TROUBLESHOT AND FOUND MAU 1 POWER SUPPL Y INOPERATIVE. REMOVED AND REPLACED MAU 1 POWER SUPPLY, OPERATIONAL CHECK GOOD. A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A56NM 2007051500159 20070515 00159 CE 2007 5 15 G41A2007001 1 20070430 A 2130 UNKNOWN LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP CABIN PRESS SYS MALFUNCTIONED E G41A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 01 43MF 284 FLYING AT 450 FROM MMUN TO ABQ THE CABIN ALTITUDE STARTED CLIMBING AND COULD NOT BE STOPPED, THE CREW STARTED A DESCENT TO 270 AND LANDED IN ELP. A FUNCTIONAL TEST OF THE PRESSURIZATION SYSTEM AND A CABIN LEAK RATE CHECK WERE COMPLETED. T HE PROBLEM COULD NOT BE DUPLICATED ON THE GROUND. 2 L 7 2 4F 4 F A10CE E6WE 2007051500160 20070515 00160 EU 2007 5 15 DATA200700003 1 20070412 A 3213 201116301 AXLE STBROS SD3 SD360 8100606 EU RT MLG SEPARATED E DATA O OTHER O OTHER LD LANDING 1 GL 13 136LR SH3752 AFTER NORMAL LANDING, THE RIGHT MAIN WHEEL SEPARATED FROM THE AIRCRAFT ON TAXI. AFTER MAINTENANCE INSPECTION IT WAS DET ERMINED THE AXLE SEPARATED FROM THE MAIN GEAR BEAM ASSEMBLY. ANOTHER SERVICEABLE LANDING GEAR BEAM WILL BE INSTALLED AL ONG WITH OTHER REQUIRED PARTS THAT WERE INDIRECTLY DAMAGED BY THE INCIDENT. AIRCRAFT WILL BE MAINTENANCE FERRIED TO MKE FOR FURTHER EVALUATION. 2 H 7 2 4T A41EU 2007051500164 20070515 00164 NM 2007 5 15 USAA070377 1 20070514 A 5330 SKIN BOEING 737 7374B7 1384702 NM BS 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 STA 400 RADIO ALT AFT SATELLITE HOLE RBL 1 HAS CRACK. INSTALLED REPAIR DOUBLER PER TYP REP 53-30-10A, DEFECT SIZE: .20 0 INCH. 2 L 7 2 4F RT A16WE 2007051500174 20070515 00174 NM 2007 5 15 USAA070373 1 20070514 A 5753 65C263203 SKIN BOEING 737 7374B7 1384702 NM LT MID TE FLAP CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 INBOARD LEADING EDGE OF LEFT OUTBOARD MIDFLAP CHAFED. INSTALLED DOUBLER PER SRM 53-01, DEFECT SIZE: 1 X 2 INCH. 2 L 7 2 4F RT A16WE 2007051600001 20070516 00001 NM 2007 5 16 UIEA200700152 1 20070406 A 5311 FRAME BOEING 747 747243B 1384830 NM BS 740 S6R CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 UPPER DECK STATION 740 STRINGER 6R FRAME CUTOUT CRACKED. REPAIRED STRINGER CUTOUT PER SRM 53-10-04 FIG 54. 2 L 7 4 4F A20WE 2007051600002 20070516 00002 NM 2007 5 16 UIEA200700153 1 20070405 A 5311 FRAME BOEING 747 747243B 1384830 NM BS 1960 S13R DEFORMED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 MAIN DECK STATION 1960 STRINGER 13R FRAME INNER FLANGE FOUND DEFORMED. REPAIRED PER SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 2007051600003 20070516 00003 NM 2007 5 16 UIEA200700181 1 20070410 A 5311 FRAME BOEING 747 747243B 1384830 NM BS 200 S14L CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 LT S14 AREA FRAME CRACKED. CRACKED FRAME WEB REPAIRED AS PER SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 2007051600004 20070516 00004 NM 2007 5 16 UIEA200700156 1 20070405 A 5340 65B125821 BRACKET BOEING 747 747243B 1384830 NM BS 1416 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 AFTER REMOVAL OF PAX DECK SPLICE FITTING AT STATION 1416 LBL 2 IN THE BLG WHEEL WELL IS FOUND CRACKED. REPLACED FITTING PER SRM 51-10-01 PAGE 9. 2 L 7 4 4F A20WE 2007051600005 20070516 00005 NM 2007 5 16 UIEA200700159 1 20070403 A 5320 SUPPORT BOEING 747 747243B 1384830 NM BS 1110 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 AIR-CONDITIONING BAY FAIRING SUPPORT FOUND CORRODED AS MARKED AT STA 1110 LBL 12 (191EL FAIRING ATTACH AREA). REMOVED C ORROSION AND REPAIRED PER SRM 53-50-04 FIG 2. 2 L 7 4 4F A20WE 2007051600007 20070516 00007 NM 2007 5 16 UIEA200700164 1 20070404 A 5310 DOOR FRAME BOEING 747 747243B 1384830 NM BS 488 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 RT NR 1 MED NR 9 DOOR STOP FTG AREA FOUND CRACK AT BS 488 FRAME WEB TOOLING HOLE APPROX 1/16" AND 1/8" LONG. RT NR 1 ME D NR 9 DOORS STOP FTG AREA CRACK WEB REPAIRED AS PER SRM 53-10-04 FIG 121. 2 L 7 4 4F A20WE 2007051600008 20070516 00008 NM 2007 5 16 UIEA200700165 1 20070404 A 5510 HINGE FITTING BOEING 747 747243B 1384830 NM BS 2598 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 EMP LT HORIZ STAB C/S STAB HINGE NR 28 HOLE FOUND CRACK AT HINGE FTG 11 O/C POSITION APPROX 1/8" LONG. REPAIRED AS PER BOEING MSG 1-305519321-7. 2 L 7 4 4F A20WE 2007051600009 20070516 00009 NM 2007 5 16 UIEA200700158 1 20070403 A 5415 ATTACH ANGLE BOEING 747 747243B 1384830 NM NR 2 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 NR 2 PYLON CAP SKIN OUTBOARD LOWER ATTACH ANGLE FOUND CRACKED AS MARKED. REPAIRED AS PER SRM 54-11-02 FIG 7. 2 L 7 4 4F A20WE 2007051600012 20070516 00012 2007 5 16 UIEA200700205 4 20070416 A 3140 WARNING HORN BOEING 747 747271C 1384869 NM FALSE ACTIVATION A UIEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 15 537MC 22403 TAKEOFF WARNING HORN SOUNDED WITH ALL THROTTLES AT N-1 APPROX 104.9 JUST PRIOR TO 80 KNOTS. (RTO). TAKEOFF AURAL WARN T EST CARRIED OUT AS PER MM 31-26-00, NO FAULTS FOUND. AURAL WARN UNIT ELECT CONNECTION INSPECTED AND CHECKED OK. FLAPS, SPEED BRAKE AND STAB TRIM SYSTEM ALL EXERCISED. 2 L 7 4 4F A20WE 2007051600016 20070516 00016 NM 2007 5 16 UIEA200700169 1 20070411 A 5511 SPAR BOEING 747 747243B 1384830 NM HORIZONTAL STAB CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 EMP LT HORIZ STAB HINGE FTG AREA FOUND NR 25 HOLE CRACK AT REAR SPAR UPPER CHORD APPROX 3/16" RUNNING O/B LOWER DIRECTIO N. REPAIRED AS PER BOEING MSG 1-305519321-7. 2 L 7 4 4F A20WE 2007051600017 20070516 00017 NM 2007 5 16 UIEA200700208 1 20070425 A 5280 DOOR BOEING 747 74747UF 1384812 NM MLG DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 412MC 30559 RT WING LANDING GEAR DOOR ELEPHANT EAR FAIRING IS DAMAGED ON THE LOWER SURFACE AS MARKED. REPAIRED IAW XEO- 52-042307. 2 L 7 4 4F RT A20WE 2007051600018 20070516 00018 NM 2007 5 16 UIEA200700160 1 20070406 A 5320 SUPPORT BOEING 747 747243B 1384830 NM BS 1050 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 FX - AIR COND BAY FAIRING SUPPORT FOUND CORRODED AT BS 1050 LBL 12, LBL 28 (191AL FRG ATTACH AREA). OUT OF LIMIT FAIRIN G SUPPORT LWR CHORD LWR FLANGE REPAIRED AS PER SRM 53-50-06 FIG 2. 2 L 7 4 4F A20WE 2007051600020 20070516 00020 NM 2007 5 16 AALA20070739 1 20070424 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 DFW - EMERGENCY LIGHT AT SEAT 20C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT T00001SE 2007051600022 20070516 00022 NM 2007 5 16 AALA20070743 1 20070424 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 DFW - EMERGENCY LIGHT AT SEAT 26C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT T00001SE 2007051600023 20070516 00023 NM 2007 5 16 SWAA072398 1 20070511 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 757LV 29850 DURING SCHEDULED HC1 CHECK, FOUND RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 128, 24 INCHES AFT OF FRONT SPAR. REP AIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007051600024 20070516 00024 NM 2007 5 16 SWAA072386 1 20070511 A 2560 232A4104 STRAP BOEING 737 7377H4 1384404 NM EMERGENCY ESCAPE WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 204WN 29855 DURING SCHEDULED MV3 CHECK, FOUND CAPTAIN'S EMERGENCY ESCAPE STRAP WORN. REMOVED AND REPLACE STRAP PER MM. 2 L 7 2 4F RT A16WE 2007051600025 20070516 00025 2007 5 16 SWAA072388 4 20070511 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 718SW 27852 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007051600029 20070516 00029 NM 2007 5 16 SWAA072389 1 20070511 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 908 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 908, STR 4L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007051600030 20070516 00030 NM 2007 5 16 SWAA072392 1 20070511 A 5753 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 1633 22944 DURING SCHEDULED HC1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED INBOARD END. REMOVED AND REPLACED FLAP PE R MM. 2 L 7 2 4F RT A16WE 2007051600031 20070516 00031 NM 2007 5 16 SWAA072395 1 20070511 A 5230 6547952 SKIN BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT DOOR HANDLE CUTOUT UPPER AFT CORNER. REPAIRED DOOR SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007051600032 20070516 00032 NM 2007 5 16 SWAA072396 1 20070511 A 5311 65C22908 FRAME BOEING 737 7373G7 1384595 NM BS 500B S20L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007051600033 20070516 00033 NM 2007 5 16 SWAA072397 1 20070511 A 5311 65C22910 FRAME BOEING 737 7373G7 1384595 NM BS 500D S20L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 20L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007051600034 20070516 00034 NM 2007 5 16 SWAA072393 1 20070511 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM BS 500C S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007051600036 20070516 00036 NE 2007 5 16 TQ0A20070004 2 20070511 A 8530 CYLINDER DHAV DHC2 DHC2* 2800108 EA PWA R985 R985* 52008 NE HAMSTD 23D 23D40 NE NUMBER 4 FAILED E TQ0A A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 AL 05 930TG 7611 759 1041 11715 D8561 NR 4 CYLINDER FAILURE AND SEPARATION FROM ENGINE CASE. ROUGH ENGINE LANDING AT TAQUAN AIR. 1 H 7 1 3R 3 R A806 5E1 6 C P719 2007051600037 20070516 00037 NM 2007 5 16 UIEA200700168 1 20070411 A 5330 BEAR STRAP BOEING 747 747243B 1384830 NM BS 1315 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 M/DECK LT MED NR 3 CUT-OUT AFT UPPER CORNER SMALL STEEL DOUBLER 1 HOLE CRACK AT BEAR STRAP APPROX 0.030" LONG (AFTER COR NER REMOVED). CRACKED HOLE REPAIRED AS PER BOEING MSG 1-309886570-4, WORK DETAILS REF N.R C51491. 2 L 7 4 4F A20WE 2007051600038 20070516 00038 NM 2007 5 16 UIEA200700172 1 20070409 A 5313 STRINGER BOEING 747 747243B 1384830 NM ZONE 100 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 FX - STRINGER FOUND CORROSION CRACKED AT STA2260-S-51L. CORROSION CRACKED STRINGER, REPAIRED AS PER SRM 53-10-02. 2 L 7 4 4F A20WE 2007051600039 20070516 00039 NM 2007 5 16 UIEA200700179 1 20070404 A 5311 FRAME BOEING 747 747243B 1384830 NM BS 200 S13-14L CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 LT BS 200 FRAME IS FOUND CRACKED AT 11EA FASTENER HOLES BETWEEN S13L AND S14L. CRACKED FRAME WEB REPAIRED AS PER SRM 51 -40-03 FIG 1. 2 L 7 4 4F A20WE 2007051600040 20070516 00040 NM 2007 5 16 UIEA200700162 1 20070403 A 5320 WEB BOEING 747 747243B 1384830 NM BS 360-380 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 M/D STA 360-380 S26R FLOOR WEB CRACK AT SKIN ATT AREA. CRACKED FLOOR WEB REPAIRED AS PER SRM 51-40-03 FIG 3. 2 L 7 4 4F A20WE 2007051600042 20070516 00042 NM 2007 5 16 UIEA200700167 1 20070411 A 5330 BEAR STRAP BOEING 747 747243B 1384830 NM BS 1315-1319 DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 M/DECK R3 DOOR AFT UPPER CORNER AREA BEAR STRAP DELAMINATED. DELAMINATED BEAR STRAP CORROSION REMOVED, OUT OF LIMIT, RE PAIRED AS PER BOEING MSG 1-30886570-4. 2 L 7 4 4F A20WE 2007051600044 20070516 00044 CE 2007 5 16 UIEA200700171 1 20070406 A 5330 SKIN CESSNA 185 A185E 2072818 CE BS 800 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 561MC 1851012 M/DECK L2 DOOR FWD CUT-OUT REVEAL CRACK AT LWR AREA. CRACK REMOVED AND REPAIRED AS PER SRM 53-10-04 FIG 84. 1 H 7 1 3O 3A24 2007051600045 20070516 00045 NM 2007 5 16 UIEA200700203 1 20070330 A 5753 SKIN BOEING 747 747230B 1384889 NM GE CF6 CF650* 30018 NE TE FLAP DELAMINATED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 512MC 21220 RT WING O/B MID FLAP UPPER SURFACE LEADING EDGE AT WING STA 1000.00 TO WING STA 995.00 IS DELAMINATED 2.5IN WIDE 4.5IN L ONG. REPAIRED RT WING O/B MID FLAP UPPER SURFACE DELAMINATION IAW SRM 51-10-01 EO4757A353. 2 L 7 4 4F 4 F A20WE E23EA 2007051600046 20070516 00046 NM 2007 5 16 UIEA200700174 1 20070409 A 5320 SUPPORT BOEING 747 747243B 1384830 NM BS 880 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 FAIRING SUPPORT FRAME AT STA 880 LWR SIDE LBL 2 AND RBL 2 FOUND CORRODED. OUT OF LIMIT LWR CHORD REPAIRED AS PER SRM 53 -50-04. 2 L 7 4 4F A20WE 2007051600049 20070516 00049 NM 2007 5 16 UIEA200700210 1 20070425 A 5751 STRUCTURE BOEING 747 74747UF 1384812 NM RT AILERON DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 412MC 30559 RIGHT INBOARD AILERON OUTBOARD AFT CORNER DAMAGED TO PREVIOUS REPAIR APPROX 3.0" BY 4.0". REPAIRED IAW XEO- 57-042307-1 2 L 7 4 4F RT A20WE 2007051600051 20070516 00051 NM 2007 5 16 UIEA200700209 1 20070425 A 5753 PANEL BOEING 747 74747UF 1384812 NM TE FLAP DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 412MC 30559 LT O/B AFT FLAP HAS UPPER ALUMINUM HONEYCOMB PANEL DENTS. REPAIRED IAW XEO- 57-042307-3. 2 L 7 4 4F RT A20WE 2007051600055 20070516 00055 NM 2007 5 16 UIEA200700211 1 20070425 A 5753 STRUCTURE BOEING 747 74747UF 1384812 NM TE FLAP DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 412MC 30559 RIGHT OUTBOARD AFT FLAP HAS A NICK IN THE TRAILING EDGE AS MARKED 0.25" BY 0.25". REPAIRED IAW XEO- 57-042307-2. 2 L 7 4 4F RT A20WE 2007051600057 20070516 00057 NM 2007 5 16 UIEA200700177 1 20070404 A 5322 SHEAR TIE BOEING 747 747243B 1384830 NM BS 860 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 RT BS 860 TENSION TIE AREA HOLE NR 6 FOUND CRACKED AT AFT CHANNEL APPROX 0.060" IN LENGTH RUNNING UPWARD. RT BS 860 TEN SION TIE CRACKED AFT CHANNEL, REPAIRED AS PER BOEING MSG 1-306486452-2. 2 L 7 4 4F A20WE 2007051600059 20070516 00059 NM 2007 5 16 UIEA200700180 1 20070412 A 5311 FRAME BOEING 747 747243B 1384830 NM BS 1740 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 M/D BS 1740 S-13R-S14R FRAME FOUND CRACKED AND DEFORMED. M/D BS 1740 S13R-S14R DAMAGE FRAME REPAIRED FROM S11R TO S15R/ 16R AS PER BOEING MSG 1-309862807-8. 2 L 7 4 4F A20WE 2007051600060 20070516 00060 NM 2007 5 16 UIEA200700182 1 20070402 A 5340 FITTING BOEING 747 747243B 1384830 NM BS 840 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 M/D RT BS 840 FRAME TO TENSION TIE CONNECTION FOUND NR 8 HOLE CRACK AT TENSION TIE AFT CHANNEL. CRACKED AFT CHANNEL REP AIRED AS PER BOEING MSG 1-303978264-2. 2 L 7 4 4F A20WE 2007051600062 20070516 00062 EA 2007 5 16 TRAX200700649 1 20070511 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 859AS 7421 FLAP FAIL AT 30. EMERGENCY EQUIPMENT ON STANDBY AS A PRECAUTION. FLT 4670 CX. 2 L 7 2 4F RT A21EA 2007051600066 20070516 00066 EA 2007 5 16 TRAX200700654 1 20070509 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 RIGHT LOWER FS 280 WEB HAS CORROSION. [SUP 05-22-07] RESOLVED ON W/O: 58937 TASKCARD: N/R-00073. 2 L 7 2 4F RT A21EA 2007051600068 20070516 00068 EA 2007 5 16 TRAX200700656 1 20070510 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR TORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 PAX DOOR -TO OPEN- PLACARD TORN. [SUP 05-22-07] REMOVED AND REPLACED WITH NEW SERVICEABLE ONE PN S7247-1 IAW CRJ 700 A MM 11-30-02 AJONES 1017 5-14-07. 2 L 7 2 4F RT A21EA 2007051600070 20070516 00070 NM 2007 5 16 KPVA20075 1 20070511 A 3230 69210 SEQUENCE VALVE DHAV DHC8 DHC8103 1386005 NM NLG INOPERATIVE A KPVA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 WP 13 809WP 032 (PIREP) NOSE GEAR WOULD NOT EXTEND USING NORMAL HYDRAULIC SYSTEM. GEAR EXTENSION USING ALTERNATE SYSTEM. (MX) REMOVED AND REPLACED RELAYS 3261-K11 AND 6231-K7 IAW DHC-8 WD 32-30-00 PG 1 SHEET 4. DID NOT SOLVE PROBLEM. (MX) REMOVED AND R EPLACED NOSE GEAR DOOR MECHANICAL SEQUENCE VALVE IAW DHC-8 MM 32-20-31 PAR 1 PG 201-202. OPS CHECK AND LEAK CHECK GOOD. PERFORM EXTENSION AND RETRACTION OPERATIONAL TEST OF LANDGING GEAR IAW DHC-8 MM 32-30-00 PAR 2 PG 203-206. NO DEFECTS NOTED. NOTE; POST MAINTENANCE CHECK FLIGHT (PMCF) GOOD. 2 H 7 2 4T RT A13NM 2007051600071 20070516 00071 NE 2007 5 16 ABXA070151 2 20070509 A 7261 STRAINER DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE LT ENGINE OIL CONTAMINATED A ABXA E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 GL 23 924AX 47403 665570 LEFT OIL STRAINER CLOG LIGHT CAME ON IN FLIGHT. FOLLOWED ABNORMAL PROCEDURE AND SHUT DOWN ENGINE. ENGINE WINDMILLED FO R 18 MINUTES WITH 12 PSI OIL PRESSURE OBSERVED. REMOVED AND INSPECTED MAIN OIL FILTER. FOUND SMALL PARTICAL METAL CONT AMINATES WITH SOME CARBON. FLUSHED OIL SYSTEM AND REPLACED MAIN OIL FILTER. GROUND RAN NR 1 ENGINE AND REINSPECTED MAI N OIL FILTER, NO CONTAMINATES FOUND. INSPECTED OIL RESTRICTOR FITTING AND FOUND COKE CLOGGING NR 40 RESTRICTOR. SUSPEC T THIS AS THE SOURCE OF CLOG LIGHT. CLEANED RESTRICTOR AND PUT ENGINE ON 200 HOUR WATCH PER P&W MM 72-00-00-810-004. 2 L 7 2 4F 4 F A6WE E2EA 2007051600072 20070516 00072 NE 2007 5 16 ABXA070152 2 20070510 A 7261 OIL SYSTEM DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE NR 1 ENGINE LOW PRESSURE A ABXA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 23 924AX 54136 47403 665570 LEFT ENGINE OIL STRAINER CLOGGING LIGHT FOLLOWED BY LOW OIL PRESSURE LIGHT. OIL PRESSURE WAS 22 PSI. SHUT DOWN LEFT EN GINE. REPLACED LEFT ENGINE IAW JC 9090010. GROUND OPS CHECK GOOD. 2 L 7 2 4F 4 F A6WE E2EA 2007051600074 20070516 00074 SO 2007 5 16 C2XA07RI032 1 20070514 A 2612 14535259405 MODULE EMB 145 EMB145LR 3260212 SO FIRE DETECTION INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12564 11591 5600 145618 FLT 2346 - EWR - CREW REPORTED BAG FIRE EXT LIGHT WILL NOT ILLUMINATE DURING TEST. EWR MX REMOVED AND REPLACED BAG FIRE EXT MODULE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007051600075 20070516 00075 SO 2007 5 16 C2XA07SH029 1 20070513 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145EP 3260221 SO CARGO BAY INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15932 145015 SHV - DURING ROUTINE MAINTENANCE THE BAGGAGE COMPARTMENT SMOKE DETECTOR FAILED THE OPERATIONAL TEST. MAINTENANCE REMOVE D AND REPLACED THE DETECTOR IAW EMB 145 AMM 26-11-01. THE ENSUING OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVE D FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007051600077 20070516 00077 SO 2007 5 16 C2XA07IA117 1 20070511 A 2611 FAU75A14 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY INOPERATIVE A C2XA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 27 16999 145307 IAH - FLIGHT 3083, THE CREW REPORTED THAT THE LAV SMOKE DETECTOR KEPT GOING OFF. THE AIRCRAFT LANDED AT IAH WITHOUT INC IDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LAV SMOKE DETECTOR PANEL, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007051600080 20070516 00080 NM 2007 5 16 UIEA200700213 1 20070427 A 5730 PANEL BOEING 747 747271C 1384869 NM LT WING DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 LT WING LEADING EDGE HAS A 6.5 INCH LONG BY 3.0 INCH WIDE DENT AT ILES 207.0. PERMANENT REPAIR WAS ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18 SHEETS 1 THRU 5 AND B747-200 51-40-12. ALSO, REFERENCE ATLAS AIR EO NR 4757A357. 2 L 7 4 4F A20WE 2007051600083 20070516 00083 NM 2007 5 16 UIEA200700192 1 20070405 A 5311 FRAME BOEING 747 747243B 1384830 NM BS 270 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 M/D STA270 S-R13A AREA FRAME CRACK. CRACKED FRAME WEB REPAIRED AS PER BOEING MSG 1-307196918-1-2. 2 L 7 4 4F A20WE 2007051600084 20070516 00084 NM 2007 5 16 UIEA200700148 1 20070408 A 5330 SKIN BOEING 747 7472D7B 1384803 NM BS 2650-2658 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 FUSELAGE SKIN HAS 12" CRACK FROM STA 2650 TO 2658 ON RIGHT SIDE OF AIRCRAFT BETWEEN STRINGERS 11R AND 13R. FOUND CRACKE D IN A SEMI-CIRCULAR SHAPE. REPAIRED PER SRM 53-30-03 FIG 1 DETAIL L AND XEO 53-04-06-07. (TIME LIMITED REPAIR) 2 L 7 4 4F RT A20WE 2007051600088 20070516 00088 NM 2007 5 16 UIEA200700188 1 20070403 A 5320 WEB BOEING 747 747243B 1384830 NM BS 340-360 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 M/D STA 340-360 S-26R FLR WEB CRACK AT SKIN ATT AREA. CRACKED FLOOR WEB REPAIRED AS PER SRM 51-40-03 FIG 3. 2 L 7 4 4F A20WE 2007051600090 20070516 00090 NM 2007 5 16 UIEA200700193 1 20070406 A 5313 STRINGER BOEING 747 747243B 1384830 NM BS 1283 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 CABIN FLR SUPPORT BS 1283 RBL 117 CORROSION. OUT OF LIMIT, SUPPORT REPAIRED AS PER BOEING 1-310385513-2. 2 L 7 4 4F A20WE 2007051600091 20070516 00091 NM 2007 5 16 UIEA200700218 1 20070502 A 5313 STRINGER BOEING 747 7472D7B 1384803 NM BS 460-480 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 BS 460-480 STRINGER 28R FOUND SEVERAL HOLES ELONGATED. BS 460-480 STRINGER 28R REPLACED AS PER SRM 51-10-01 PAGE 9 AND AS PER SRM 51-30-02. 2 L 7 4 4F RT A20WE 2007051600092 20070516 00092 NM 2007 5 16 UIEA200700161 1 20070404 A 5347 SEAT TRACK BOEING 747 747243B 1384830 NM BS 1440-1480 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 CABIN TIE DOWN TRACK FLANGE CORRODED AT BS 1440-1480 RBL33. CORROSION SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 25. 2 L 7 4 4F A20WE 2007051600095 20070516 00095 NM 2007 5 16 UIEA200700198 1 20070404 A 5311 FRAME BOEING 747 747243B 1384830 NM BS 200 S13-14L CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 M/D LT BS 200 FRAME INNER CHORD IS FOUND CRACKED AT 1 FASTENER HOLE BETWEEN S13L AND S14L. CRACKED INNER CHORD REPAIRED AS PER SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 2007051600097 20070516 00097 NM 2007 5 16 UIEA200700196 1 20070406 A 5311 FRAME BOEING 747 747243B 1384830 NM ZONE 200 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 RT BS 900 TENSION TIE AREA NR 5 HOLE FOUND CRACK AT FRAME WEB THRU THICKNESS RUNNING I/B AND NR 10 HOLE FOUND CRACK AT F RAME WEB APPROX 0.060" IN LENGTH RUNNING DOWNWARD. CRACKED FRAME WEB REPAIRED AS PER BOEING MSG 1-306586780-2. 2 L 7 4 4F A20WE 2007051600100 20070516 00100 NM 2007 5 16 UIEA200700200 1 20070411 A 5350 KEELBEAM BOEING 747 747243B 1384830 NM ZONE 100 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 KEEL BEAM PNL NR 191KK EXTERNAL AND INTERIOR SURFACE CORROSION REVEALED. KEEL BEAM PANEL NR 191KK OUT OF LIMIT HINGE AR EA REPAIRED AS PER SRM 51-40-03 FIG 1 AND SKIN REPAIRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2007051600101 20070516 00101 NM 2007 5 16 UIEA200700202 1 20070409 A 5314 KEELBEAM BOEING 747 747243B 1384830 NM ZONE 100 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 KEEL BEAM PNL NR 191JJ INTERIOR SURFACE CORROSION REVEALED AT SEVERAL LOCATIONS. KEEL BEAM PANEL NR 191JJ INTERIOR SUPP ORT REPLACED AS PER SRM 51-10-01 PP AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007051600113 20070516 00113 EU 2007 5 16 200705151 1 20070511 A 3250 STEERING SYS EMB ERJ170 ERJ170100SE 3260406 EU NLG FAILED A UHLA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 11 643RW 17000060 FLIGHT 7057 IAD TO MIA LANDING IN MIA THE CREW RECEIVED A STEER FAIL INDICATION WITH GEAR EXTENSION. DECLARED A PRECAUT IONARY EMERGENCY, AND LANDED THE AIRPLANE WITHOUT INCIDENT. RESET MAU 2 CB, FAULT CLEARED. STEERING OPS CHECK GOOD. 2 L 7 2 4F RT A56NM 2007051600114 20070516 00114 SO 2007 5 16 RAIA00705024 1 20070512 A 3350 307 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 837HK 145255 PRE FLT NR 7920 - ORD - EMERGENCY LIGHT AISLE FLOOD LIGHT INOP. MAINTENANCE RELAMPED OVERHEAD CEILING EMERGENCY FLOOD L IGHT CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007051600118 20070516 00118 NM 2007 5 16 MWEA070117 1 20070514 A 5230 5910157109 PAN BOEING 717 717200 1383700 NM CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 916ME 55178 INNER CARGO DOOR PAN IS CRACKED, FORWARD. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2007051600119 20070516 00119 NM 2007 5 16 MWEA070115 1 20070514 A 2530 8203120000C OVEN BOEING 717 717200 1383700 NM GALLEY SMOKE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 906ME 55170 FLIGHT ATTENDANT REPORTED SMOKE BILLOWING FROM MIDDLE GALLEY OVEN. FOUND BURNT FOOD IN OVEN. 2 L 7 2 4F TR A6WE 2007051600121 20070516 00121 SO 2007 5 16 SWIA200718208 1 20070507 A 2750 12064207615 CONTROL LEVER EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 284YV 8964 8964 120284 AFTER TAKEOFF, A FLAP DISAGREEMENT APPEARED. THE OUTBOARD FLAPS DID NOT RETRACT AND THE DISAGREEMENT REMAINED. RETURNE D TO LAX, CLEANED CONNECTORS ON OUTBOARD FLAP ACTUATORS. REPLACED FLAP CONTROL HANDLE IAW 27-50-00. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007051600122 20070516 00122 EA 2007 5 16 SWIA200718209 1 20070508 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 367CA 10069 EMERGENCY CEILING POD LIGHT INOP. REPLACED LAMP IN EMERGENCY CEILING POD LIGHT, PN: 1317. 2 L 7 2 4F RT A21EA 2007051600123 20070516 00123 EA 2007 5 16 SWIA200718210 1 20070509 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA LEFT ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 927SW 7693 FUEL ODOR FROM LEFT PACK WHILE ON THE GROUND AS WELL AS INFLIGHT. INSPECTED LEFT ACM OIL LEVEL AND FOUND TO BE OVER SER VICED. REMOVED EXCESS OIL AND CHECKED COMPRESSOR INLET AND DISCHARGE LINES FOR DISCREPANCIES BUT FOUND NOTHING. PACK F UNCTIONS NORMALLY. 2 L 7 2 4F RT A21EA 2007051600124 20070516 00124 EA 2007 5 16 SWIA200718211 1 20070315 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 706SK 10149 STATION 280 FLOOR SUPPORT BEAM CRACKED, DISCOVERED AT C-CHECK. REPLACED STATION 280 FLOORBEAM AND FLOORBEAM SUPPORT IAW REO 670-53-11-047 AND SB670BA-53-026 AND SRM 51-42-06-001-001-A01 AND REPLACED BRACKETS AT STATION 280 LBL 9.0 AND RBL 9.0 IAW SB670BA-53-026. 2 L 7 2 4F RT A21EA 2007051600127 20070516 00127 EA 2007 5 16 SWIA200718214 1 20070315 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 706SK 10149 PAX DOOR AFT WEB CRACKED AT SECOND STEP, DISCOVERED AT C-CHECK. REPLACED REPAIR ANGLES AND INTERNAL REPAIR DOUBLER PER REO 670-52-11-104. 2 L 7 2 4F RT A21EA 2007051600128 20070516 00128 EA 2007 5 16 SWIA200718215 1 20070315 A 5210 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 706SK 10149 PAX DOOR AFT DRAG ANGLE CRACKED NEAR DOOR ASSIST MOTOR CABLE PULLEY, DISCOVERED AT C-CHECK. REPLACED PARTS FOR PAX DOOR AFT DRAG ANGLE IAW REO 670-52-11-072. 2 L 7 2 4F RT A21EA 2007051400096 20070514 00096 NM 2007 5 14 UPS07M49779 1 20070402 A 5753 SKIN DOUG MD11 MD11F 3023600 NM T/E FLAP DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C LEFT WING I/B FLAP UPPER SKIN, FWD OF I/B SEGMENT, FOUND WITH SEVERAL DENTS AS MARKED DENT MARK M EASURE DEP 0.015", LEN 0.90" WID 0.80", WITHIN LIMIT PER SRM 51-80-01VIIR38. HFEC INSP C/O DAC NDTSPM R13 06-10-01.001 FOUND CRACK APPX 0.5".DENT AREA TRIM OUT SRM 57-10-00VI FIG 34R38. HFEC INSP ON TRIM AREA, NO CRACK EVIDENT. NEW DOUBL ER FAB SRM 57-10-00 FIG 34VIR38 . REPROTECT & PAINT PER SRM 51-21-01VIIR38, INSTL SRM 51-35-01VIIR38. 2 L 7 3 4F RT A22WE 2007051400097 20070514 00097 NM 2007 5 14 UPS07M49780 1 20070319 A 5350 FRAME DOUG MD11 MD11F 3023600 NM TAIL CONE SCRATCHED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C TAIL CONE RIGHT ABOVE FLOOR PANEL FRAME SCRATCH AS MARKED. SCRATCH MARK REMOVED, FOUND BEYOND LIMIT. MATL THK 0.040" THK REMN 0.07", THK REMV 0.013" PER SRM 53-00-01VIR38. DAMAGED SUPPORT REMOVED PER SRM 51-35-01VIIR38. NEW SUPPORT FAB USE 2024-0-0.032" PER BOEING DRW AKC7543. SUPPORT HEAT TREATED DPS 7.00-1 & HARDNESS 15782.3 DPS1.05- 3 SUPPORT TREATED/PAINTED SRM 51-21-01VIIR38, INSTL SRM 51-31-01VIIR38. 2 L 7 3 4F RT A22WE 2007051400118 20070514 00118 NM 2007 5 14 SWAA072373 1 20070510 A 5330 6545766 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 374, STR 26L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007051400127 20070514 00127 NM 2007 5 14 SWAA072370 1 20070510 A 5322 6546529 SHEAR TIE BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, BETWEEN RBL 8 AND RBL 13. REMOVED AND REPLACED SHEAR TI E PER SRM. 2 L 7 2 4F RT A16WE 2007051400130 20070514 00130 NM 2007 5 14 SWAA072380 1 20070510 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 8L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007051400132 20070514 00132 NM 2007 5 14 SWAA072371 1 20070510 A 5313 6551698 STRINGER SPLICE BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 27R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007051400135 20070514 00135 NM 2007 5 14 SWAA072385 1 20070510 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 24R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007051400166 20070514 00166 EA 2007 5 14 COMA0760359 1 20070503 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 965CA 7131 DURING FS 559 INSPECTION FOUND SEMI-BULKHEAD CRACKED AT RBL 18. STOP DRILLED CRACK AND INSTALLED DOUBLER IAW REO 601R-5 3-41-353. 2 L 7 2 4F RT A21EA 2007051400168 20070514 00168 EA 2007 5 14 COMA0760361 1 20070504 A 2150 DRAIN LINE CNDAIR CL600 CL6002B19 1900309 EA LT PACK DEFECTIVE A COMA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 01 597SW 7329 FLIGHT 5542 - RECEIVED CABIN ALT CAUTION. CABIN PRESS RISING SLOWLY BUT STEADILY THROUGH 8000 FT. PERFORMED QRH, EMERG ENCY DESCENT TO 10000. CABIN PRESS STABILIZED. REPLACED LEFT PACK WATER SEPARATOR DRAIN LINE. 2 L 7 2 4F RT A21EA 2007051400172 20070514 00172 EA 2007 5 14 TRAX200700647 1 20070510 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 858AS 7417 FLOOR PROXIMITY LIGHTING INOP ROW 10-14. FLT 4129 DEL 40 MINS. ELECTROLUMINESCENT FLOOR PROXIMITY EMERGENCY ESCAPE PAT H MARKING SYSTEM. 2 L 7 2 4F RT A21EA 2007051400178 20070514 00178 EA 2007 5 14 TRAX200700642 1 20070508 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 850AS 7355 EMERGENCY FLOOR TRACK LIGHTING BROKEN. 2 L 7 2 4F RT A21EA 2007051400191 20070514 00191 NM 2007 5 14 07FDEA01716 1 20070507 A 5311 BAC15171062 FRAME BOEING 727 7272S2F 1384O81 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 MAIN DECK BODY FRAME IB CHORD IS CRACKED AT BS 930, STR 13R-14R. REPAIRED 2 FRAME BS 930 PER SRM 53-10-4 FIG 1. 2 L 7 3 4F A3WE 2007051400192 20070514 00192 NM 2007 5 14 07FDEA01717 1 20070507 A 5347 AEA732523 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 FOUND UPPER CARGO COMPARTMENT, SEAT TRACK AT LBL 8.5 CORRODED AT STA 1299. [SUP 05-21-07] REPAIR CARRIED OUT AS PER SR M 53-70-00 FIG. 1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007051400223 20070514 00223 SO 2007 5 14 F7H2007F00000 1 20070326 A 3233 350302 O-RING PIPER PA23 PA23250 7102308 SO LYC O540 TIO540* 41532 EA LT MLG ACTUATOR WORN H F7HS O OTHER O OTHER CL CLIMB 1 WP 13 31PD 8626 277654016 PILOT REPORTED LT MAIN GEAR WOULD NOT RETRACT AFTER TAKEOFF. PROBABLE CAUSE WAS WORN O-RINGS IN LT MAIN GEAR ACTUATING CYLINDER ASSEMBLY. (K) 1 L 7 2 3O 3 O 1A10 E14EA 2007051500004 20070515 00004 NM 2007 5 15 DLM88070491 1 20070503 A 5511 5918000523 SPAR DOUG MD88 MD88 3023688 NM HORIZONTAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DL 49541 THE LT OUTER SECTION REAR SPAR OF THE HORIZONTAL STABILIZER WAS FOUND CORRODED IN THE LOWER CAP BARREL NUT HOLE. THE DA MAGED HOLE WAS OVERSIZED. 2 L 7 2 4F RT A6WE 2007051500006 20070515 00006 NM 2007 5 15 DL738070493 1 20070504 A 5330 143A325032 SKIN BOEING 737 737832 13844CF NM FS 500F DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3747D 29665 THE FUSELAGE WAS STRUCK BY A TRUCK TEARING A LARGE HOLE IN THE SKIN AND BREAKING A FRAME AND STRINGERS. THE DAMAGED SKI N, STRINGER, AND FRAME WERE CUT OUT AND REPAIR DOUBLERS AND ANGLES WERE INSTALLED. 2 L 7 2 4F RT A16WE 2007051500011 20070515 00011 NM 2007 5 15 DL76P070498 1 20070508 A 5247 7321380706 ACTUATOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE APU DOOR ACTIVATED A DALA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 143DA 15662 25991 P2307 THREE HOURS INTO FLIGHT, JUST PRIOR TO DESCENT. ATTEMPTED 3 APU START ATTEMPTS AT FL330. THE MAJORITY OF THE FLIGHT WA S FLOWN AT FL390. NONE OF THE ATTEMPTS WERE SUCCESSFUL WITH AN APU DOOR STATUS MSG ON EICAS ABOUT A MINUTE INTO EACH ATTEMPT. NO STATUS MSG ON GROUND. FWD TO MCO/PLACARD PER MEL 49-15-01A. APU INOP. INLET DOOR SECURED CLOSED. REMOVED AND REPLACED APU DOOR ACTUATOR PER M/M. BATTERY AND CHARGER, OPS CK NML. 2 L 7 2 4F 4 F RT A1NM E24NE 2007051500021 20070515 00021 2007 5 15 DL76L070483 4 20070507 A 3410 066500011001 INDICATOR BOEING 767 767332 1382001 NM VSI INOPERATIVE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 1200K 28457 101004 CAPT VSI INOP ON TAXI-OUT APPROX 20 MIN INTO TAXI. REPLACED CAPTS VSI PER AMM. OPS CHK NML. PART ROBBED FROM A/C 173. MPN 066-50001-1001 S/N 10139 CAPT POS. AC RTB TWICE FOR SAME PROBLEM. FIRST IND REMOVED AND REPLACED WITH PREV SHOPH IST. 2ND IND SAME THING BUT DIFFERENT SHOP HIST. C/B WAS ALSO REMOVED AND REPLACED ON 1ST RTB DUE TO ELEC FUME REPORTE D. CONNECTOR AND WIRING WERE CHECKED PRIOR TO 3RD IND. REPLACED C/B C586 AND REPLACED CAPT IVSI PER AMM. OPS CHK NML, NO FUMES PRESENT. 2 L 7 2 4F RT A1NM 2007051500023 20070515 00023 NM 2007 5 15 DL76S070485 1 20070422 A 5315 BAC15063123 FLOORBEAM BOEING 767 767332 1382001 NM BS 654 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 128DL 24078 FWD CARGO COMPT FLOORBEAM CHORD FOUND AT STATION 654+110 LBL 20 AND REPAIRED ON NR 52120 SRM 53-00-07 FIGURE 201, REPAIR 4. 2 L 7 2 4F RT A1NM 2007051500034 20070515 00034 NM 2007 5 15 DLM88070511 1 20070510 A 5330 5920323249 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 DENT AND EXISTING PERMANENT REPAIR WERE REPORTED ON FUSELAGE SKIN P/N 5920323-249, BETWEEN Y= 332.00 AND Y=351.00 AND BE TWEEN LONGERONS 19 RT AND 20 RT. AMX INSTALLED PERMANENT REPAIR PER SRM 53-04 FIG 12 C. 2 L 7 2 4F RT A6WE 2007051500039 20070515 00039 NM 2007 5 15 HNAA0700083 1 20070507 A 3320 404910 SOCKET DHAV DHC8 DHC8102 2809003 NM CABIN LIGHTS BURNED A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 846EX 34887 2548 326 ELECTRICAL ODOR NOTICED AT ROW 3 RIGHT HAND SIDE. PERFORMED HIDDEN DAMAGE INSPECTION, REPLACED LIGHT SOCKET AT 3 AC, OP S CHECK GOOD. 2 H 7 2 4T RT A13NM 2007051500046 20070515 00046 WP 2007 5 15 UPS07849786 1 20070424 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP FS 1766 L10R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 AFT PRESS BULKHEAD CRACKED 2 AREAS AT STA 1766 L10R, RBL 25 AND RBL 35. CUT OUT DAMAGED AREA AT ST 1 766 L10R, RBL 25 AND RBL 35 IAW SRM 53-02-05 FIG 14A. FABRICATED & INSTALLED REPAIR DOUBLERS, & FILLERS AT STA 1766 L10 R IAW SRM 53-02-05 FIG 14 AND TR 53-194. THIS REPAIR REQUIRES DAMAGE TOLERANCE INSP WITH INITIAL AT 4,000 CYCLES AND RE PEAT INSP AT EVERY 4,000 CYCLES THERE AFTER IAW TR 53-194. 2 L 7 4 4F RT 4A25 2007051500048 20070515 00048 WP 2007 5 15 UPS07849789 1 20070502 A 5311 FRAME DOUG DC8 DC873F 302199F WP FS 240 L31R GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 A-PIT, BELT FRAME GOUGED AT STA 240 L31R. TRIMMED OUT DAMAGED AREA AT STA 240 L31R IAW E0 DC8-5310-1 1728-B, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EO DC8-5310-11728-B. 2 L 7 4 4F RT 4A25 2007051500052 20070515 00052 NM 2007 5 15 MWEA070112 1 20070511 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 917ME 55179 LEFT THRUST REVERSER, BOTTOM DEFLECTOR DOOR HAD A CRACKED ZEE FRAME AT OUTBOARD SIDE AT STATION 26.666. INSTALLED ZEE F RAME. 2 L 7 2 4F TR A6WE 2007051500053 20070515 00053 NM 2007 5 15 MWEA070113 1 20070511 A 7830 7150923REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 917ME 55179 LEFT THRUST REVERSER, BOTTOM DEFLECTOR DOOR HAS A CRACKED ZEE FRAME OUTBOARD SIDE AT STATION 35.669. INSTALLED ZEE FRAM E. 2 L 7 2 4F TR A6WE 2007051500077 20070515 00077 NM 2007 5 15 DL757070529 1 20070512 A 2120 UNKNOWN BOEING 757 757232 1384965 NM CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 642DL 23996 DURING DESCENT, F/A ADVISED US OF A HOT PLASTIC ODOR TOWARD THE MIDCABIN AREA, SMELL DISSIPATED AFTER APPROX 4 MIN. CHE CKED LIGHTS IN CABIN AND PERFORMED CABIN WALK THROUGH. NO ABNORMAL ODORS NOTED. OPERATED PNEUMATICS. ALL CHECK NORMAL WITH NO ABNORMAL ODORS NOTED. OK FOR CONTINUED SERVICE. 2 L 7 2 4F RT A2NM 2007051500078 20070515 00078 NM 2007 5 15 DLM88070530 1 20070510 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 332-351 S20R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 DUE AT HMV, 3 SRM 53-04D DENT IN FUSELAGE BETWEEN SAT 332 AND351 STRINGER 19-20 RT PERMENANT REPAIR. REPAIRED PER SRM 5 3-04D FIG 12C. 2 L 7 2 4F RT A6WE 2007051500080 20070515 00080 NM 2007 5 15 DL76G070532 1 20070115 A 5330 SKIN BOEING 767 767332 1382001 NM FS 1350 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1608 30573 EXT FUSELAGE RS AFT OF AFT PIT DOOR CUTOUT LWR SKIN SECTION STA 1350 STR 31R TO STR 27R SKIN HAS AREAS OF GOUGING. COMP LIED WITH INSTRUCTIONS OF ERA 459507-14 TIME LIMITED REPAIR. 2 L 7 2 4F RT A1NM 2007051500081 20070515 00081 NM 2007 5 15 DL76G070533 1 20070115 A 5330 SKIN BOEING 767 767332 1382001 NM BS 1362 S31-32R DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1608 30573 EXT FUSELAGE STA 1362 BETWEEN STR 31R AND32R HAS STATIC DISCHARGE. REPAIRED PER ERA 459550-14. 2 L 7 2 4F RT A1NM 2007051500082 20070515 00082 NM 2007 5 15 DL76G070534 1 20070115 A 5330 SKIN BOEING 767 767332 1382001 NM BS 1406 S20R GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1608 30573 EXT FUSELAGE UPPER AFT CORNER OF DOOR CUTOUT SKIN GOUGED STA 1406 AND STR 20R. REPAIRED PER ERA 459506-14 TIME LIMITED REPAIR. 2 L 7 2 4F RT A1NM 2007051500083 20070515 00083 NM 2007 5 15 DL76G070535 1 20070115 A 5330 SKIN BOEING 767 767332 1382001 NM BS 1774 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1608 30573 EXT FUSELAGE FWD UPPER CORNER OF AFT PIT COOR CUTOUT STA 1774 SKIN GOUGED. REPAIRED PER ERA 459462-14 TIME LIMITED REPA IR. 2 L 7 2 4F RT A1NM 2007051500110 20070515 00110 NM 2007 5 15 USAA070383 1 20070514 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM BS 947 RBL 4 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 STA 947 RBL 4 HAS CORROSION. INSTALLED TEE CAP REPAIR PER EA 98634 & TYP REP 53-60-02; LEVEL 2; CORR TASK C53-107-01. 2 L 7 2 4F RT A16WE 2007051500120 20070515 00120 NM 2007 5 15 AALA20070747 1 20070424 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 643AA 24601 MIA - EMERGENCY LIGHT AT SEAT 3E INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 3E. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007051500140 20070515 00140 WP 2007 5 15 AALA20070766 1 20070427 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 492AA 49730 LGA - EMERGENCY LIGHTS AT TAIL CONE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT TAIL CONE. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051500145 20070515 00145 WP 2007 5 15 AALA20070767 1 20070427 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 492AA 49730 LGA - EMERGENCY LIGHTS AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051500149 20070515 00149 NM 2007 5 15 AALA20070789 1 20070430 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 378AN 25447 SFO - EMERGENCY LIGHT AT SEAT 22B HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22B. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007051500158 20070515 00158 EA 2007 5 15 A6WA200740159 1 20070327 A 5311 S614413 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS 617 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 416AW 7603 FOUND FRAME CLIP AT FS 617 AT LBL 9 IS CRACKED .25 INCH CRACK IN RADIUS. MAINTENANCE REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007051500161 20070515 00161 SO 2007 5 15 L0FR200700001 1 20070402 A 3246 3006041 WHEEL EMB 120 EMB120 3260201 SO MLG SHEARED B EVAB K NONE O OTHER IN INSP/MAINT 1 AL 03 DRIVE KEY SCREWS SHEARED AND SEVERAL BACKED OUT. KEY LUGS SEVERELY DAMAGED. 2 L 7 2 4T RT A31SO 2007051500168 20070515 00168 SO 2007 5 15 NOB2007F00000 1 20070309 A 3220 9652200 SPRING PIPER PA34 PA34200T 7103406 SO CONT O360 TSIO360E 17025 SO NLG OBSTRUCTED E NOBA A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 EA 63 38858 347770350 NLG WOULD NOT EXTEND WHILE ON APPROACH. AC RETURNED & THROUGH G-LOAD MANUEVERS, MANAGED TO GET NLG TO EXTEND PRIOR TO L ANDING. PROBLEM WAS DETERMINED TO BE INTERFERENCE BETWEEN NLG CENTERING SPRING ROD END ATTACHMENT CLEVIS BOLT HEAD AND REAR TORQUE TUBE FOR NLG DOOR ACTUATING MECHANISM. ORIGINAL NOSE GEAR CENTERING SPRING REMOVED AS AN ASSY, COMPLETE WI TH ATTACHING ROD END. A SERVICEABLE ASSY WAS INSTALLED EQUIVALENT TO LATEST AVAILABLE ASSY FROM THE MFG, PN 9652200. UPON GEAR RETRACTION THE CENTERING SPRING FORWARD ATTACHING CLEVIS BOLT INTERFERED WITH THE REAR TORQUE TUBE OF THE NOSE GEAR DOOR ACTUATING MECHANISM AND PREVENTED THE NOSE GEAR FROM EXTENDING UPON COMMAND AND THOUGH ACTIVATION OF THE EMER 1 L 7 2 3O 3 O A7SO E9CE 2007051500170 20070515 00170 NM 2007 5 15 USAA070379 1 20070514 A 5312 PRESSURE PANEL BOEING 737 7374B7 1384702 NM BS 664 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 BEADED PRESSURE DECK AT BS 664 LBL 32 HAS CRACK. INSTALLED DOUBLER PER TR 53-60-04 FIG 1, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007051500173 20070515 00173 NM 2007 5 15 USAA070372 1 20070514 A 5313 STRINGER SPLICE BOEING 737 7374B7 1384702 NM BS 360 S15L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 STRINGER SPLICE AT STA 360 STR 15L HAS CRACK. REPLACED STRINGER SPLICE PER SRM 51-10-02 & 51-40-02, DEFECT SIZE: .5 IN CH. 2 L 7 2 4F RT A16WE 2007051500187 20070515 00187 NM 2007 5 15 HNAA0700085 1 20070504 A 2120 UNKNOWN DHAV DHC8 DHC8102 2809003 NM CLOSET ODOR A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 810EX 308 BURNING ODOR COMING FROM WARDROBE CLOSET. UNABLE TO LOCATE THE CAUSE OF ODOR, TURNED INVERTER OFF ONE AT A TIME NO CHAN GE INSP DC CONTACTOR BOX, NO ODOR FROM CONTACTOR BOX. RAN NR 1 ENGINE AT A TIME NO ODOR NOTED. RAN BOTH ENGINES AND OD OR CAME BACK WITH BLEEDS ON OR OFF OR RECIRCULATION FAN ON OR OFF. PULLED TRU CIRCUIT BREAKERS ONE AT A TIME. REMOVED WARDROBE DOOR, AVIONICS PANELS BY OBSERVERS SEAT VISUAL INSP OF RELAYS/WIRES & ALL INTERIOR & EXTERIOR LIGHTING. RAN A/ C FOR 35 MINUTES WITH BLEEDS ON & OFF. NO DEFECTS OR ODORS NOTED. INSTALLED WARDROBE DOOR & AVIONICS PANELS AS REQUIR ED. ALSO RAN ALL AC SYSTEMS INCLUDING W/S HEAT. AFTER 10 DAYS NO FUTHER BURNING ODORS NOTED. 2 H 7 2 4T RT A13NM 2007051600010 20070516 00010 NM 2007 5 16 UIEA200700154 1 20070405 A 5311 FRAME BOEING 747 747243B 1384830 NM BS 2000 S13R DEFORMED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 MAIN DECK STATION 2000 STRINGER 13R FRAME INNER FLANGE FOUND DEFORMED. REPAIRED FLANGE PER SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 2007051600013 20070516 00013 NM 2007 5 16 UIEA200700206 1 20070420 A 2910 60B0025435 HOSE BOEING 747 747243B 1384830 NM NR 1 ADP BURST A UIEA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 15 517MC 23300 NR 1 ENGINE HAD VISIBLE SMOKE COMING FROM THE TAIL PIPE JUST PRIOR TO BLOCK IN. ALL INDICATIONS IN FLIGHT DECK WERE NOR MAL. FOUND NR 1 ADP PRESS LINE BURST. REMOVED AND REPLACED THE LINE CLEANED RESIDUAL FLUID FROM THE COWLING AND SERVIC ED THE HYD FLUID. OPS AND LEAK CHECKED OKAY PER 29-11-40 AND 29-11-08. 2 L 7 4 4F A20WE 2007051600014 20070516 00014 NM 2007 5 16 UIEA200700163 1 20070404 A 5310 VERTICAL BEAM BOEING 747 747243B 1384830 NM BS 280 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 NWW RT VERTICAL BEAM WEB AT BS 280 WL 170-180 LOWER STAND OFF HOLE FOUND CRACK APPROX 1/8" LONG. CRACK WEB REPAIRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2007051600015 20070516 00015 NM 2007 5 16 UIEA200700166 1 20070411 A 5330 BEAR STRAP BOEING 747 747243B 1384830 NM BS 1315-1319 DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 M/DECK L3 DOOR AFT UPPER CORNER AREA DELAMINATED BEAR STRAP. OUT OF LIMIT DELAMINATION BEAR STRAP REPAIRED AS PER BOEIN G MSG 1-309886570-4. 2 L 7 4 4F A20WE 2007051600026 20070516 00026 2007 5 16 SWAA072387 4 20070511 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 710SW 27844 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007051600047 20070516 00047 NM 2007 5 16 UIEA200700175 1 20070411 A 5310 PANEL BOEING 747 747243B 1384830 NM BS 1160-1200 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 KEEL BEAM PANEL NR 191KK CRACKED AT RT FWD HINGE CUT-OUT AS MARK. CRACKED HINGE CUT-OUT SKIN REPAIRED AS PER SRM 51-40- 02. 2 L 7 4 4F A20WE 2007051600052 20070516 00052 2007 5 16 UIEA200700204 4 20070415 A 3441 463001183003 INU BOEING 747 7472D7B 1384803 NM NR 1 INOPERATIVE A UIEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 527MC 22471 INFLIGHT, 7MINS AFTER T/O, NR 1 INS WENT TO WRN WITH NO DISPLAYS. NR 1 ATT FLAG AND NR 1 HDG FLAG APPEARED AND A/T WENT INOP. SWAPPED NR-1 INS NAV UNIT WING NR-3 INS NAV UNIT. TESTED NR-1 INS NAV UNIT PER AMM 34-41-03. CHECKED GOOD NO A CTION CODES. 2 L 7 4 4F RT A20WE 2007051600054 20070516 00054 NM 2007 5 16 UIEA200700176 1 20070406 A 5310 PLATE BOEING 747 747243B 1384830 NM BS 940 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 M/DECK BS940 RT TENSION TIE STEEL PLATE FASTENER HOLE 2 FOUND SHORT EDGE MARGIN AT UPPER ROW MOST O/B. REPAIRED AS PER BOEING MSG 1-303983211-1-2, FIG 3. 2 L 7 4 4F A20WE 2007051600063 20070516 00063 EA 2007 5 16 TRAX200700651 1 20070505 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA PAX DOORWAY CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 CORROSION FOUND AT SEVERAL PLACES ON PASSENGER DOOR LOWER SILL. 2 L 7 2 4F RT A21EA 2007051600064 20070516 00064 EA 2007 5 16 TRAX200700652 1 20070508 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 LOWER STEP OF PAX DOOR STAIRCASE IS CORRODED. 2 L 7 2 4F RT A21EA 2007051600085 20070516 00085 NM 2007 5 16 UIEA200700195 1 20070404 A 5322 SHEAR TIE BOEING 747 747243B 1384830 NM ZONE 200 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 RT BS 860 TENSION TIE AREA HOLE NR 5 FOUND CRACKED AT FWD CHANNEL APPROX 0.030" ON LENGTH RUNNING UPWARD. CRACKED TENSI ON TIE FWD CHANNEL REPAIRED AS PER BOEING MSG 1-306484452-2. 2 L 7 4 4F A20WE 2007051600086 20070516 00086 NM 2007 5 16 UIEA200700201 1 20070412 A 3232 2670296 ACTUATOR VALVE BOEING 747 747271C 1384869 NM MLG DOOR FAILED A UIEA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 EA 15 537MC 22403 DIVERSION TO JFK, AFTER T/O THE GEAR WAS RETRACTED RED GEAR LIGHT REMAINED ON APPROX 3 SECS LATER THE NOSE GEAR DOOR CAM E OPEN AND THEN CLOSED. DOOR CYCLED 3 TIME WITH GEAR HANDLE IN THE UP POSITION. REMOVED AND REPLACED NOSE GEAR DOOR OP ERATED SEQUENCE VALVE IAW MM 32-34-07. REMOVED AND REPLACED NOSE GEAR DOOR ACTUATOR IAW MM 32-34-14. DOOR CHECKED NORM AL IN PRIMARY AND ALTERNATE. 2 L 7 4 4F A20WE 2007051600094 20070516 00094 NM 2007 5 16 UIEA200700151 1 20070410 A 5510 7075000501N SUPPORT CHANNEL BOEING 747 747243B 1384830 NM HORIZONTAL STAB CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 LT STAB 344QBL PANEL AFT SUPPORT AREA FOUND CRACKED. REPLACED SUPPORT CHANNEL PER BOEING MESSAGE 1-307217093-2. 2 L 7 4 4F A20WE 2007051600098 20070516 00098 NM 2007 5 16 UIEA200700197 1 20070405 A 5511 RIB BOEING 747 747243B 1384830 NM HORIZONTAL STAB CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 EMP LT STAB T/E RIB AT STAB BL421.5 WEB FOUND CRACKED. CRACKED WEB REPAIRED AS PER SRM 55-10-06 FIG 4. 2 L 7 4 4F A20WE 2007051600099 20070516 00099 NM 2007 5 16 UIEA200700199 1 20070411 A 5314 KEELBEAM BOEING 747 747243B 1384830 NM BS 1040-1100 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 KEEL BEAM PNL NR 191HH EXTERNAL AND INTERIOR SURFACE CORROSION REVEALED. KEEL BEAM PANEL NR 191HH HINGE ATTACHMENT AREA OUT OF LIMIT, REPAIRED AS PER SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 2007051600102 20070516 00102 NM 2007 5 16 UIEA200700194 1 20070406 A 5411 SPAR BOEING 747 747243B 1384830 NM LT NACELLE DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 NR 4 ENG LT LOWER SPAR CHORDS (SIDE COWL HINGE AREA) AFT AREA FOUND DAMAGED. DAMAGED WEB REPAIRED AS PER BOEING MSG 1-3 08420578-2. 2 L 7 4 4F A20WE 2007051600105 20070516 00105 NM 2007 5 16 UIEA200700150 1 20070410 A 5320 144U00313 PANEL BOEING 747 7472D7B 1384803 NM BS 1241-1250 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 MAIN DECK STATION 1241 TO 1250 LBL 75 TO 97 CLOSEOUT PANEL NEAR TRIM AIR DUCT FOUND CRACKED. MAIN DECK STATION 1241 TO 1250 LBL CLOSEOUT PANEL REPLACED AS PER SB 747-53-2329 PART 4. 2 L 7 4 4F RT A20WE 2007051600111 20070516 00111 EU 2007 5 16 0511070132 1 20070511 A 6320 BEARING CAGE UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE M/R GEARBOX FAILED E E3MA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 03 533ME 0132 THE -CHIP LIGHT- WARNING WAS ILLUMINATED ON THE CAD. FOUND BROKEN BEARING CAGE MATERIAL LAYING IN THE BASE OF THE MAIN GEAR BOX. MATERIAL APPEARED TO COME FROM THE OIL COOLER BLOWER QUILL BEARING. 1 G 7 2 3U 3 U H88EU E34NE 2007051600115 20070516 00115 SO 2007 5 16 RAIA00705025 1 20070512 A 3240 SHUTOFF VALVE EMB 145 EMB145LR 3260212 SO BRAKE ASSY DIRTY A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 817HK 145058 FLT NR 5558 - ATL - LEFT HAND INBOARD BRAKE FAIL ON TAKEOFF. MAINTENANCE CLEANED CONNECTOR ON BRAKE SHUTOFF VALVES AND OPS CHECK OF MAIN BRAKE SYSTEM AND ALL OPS INDICATIONS NORMAL. 2 L 7 2 4T RT T00011AT 2007051600116 20070516 00116 SO 2007 5 16 RAIA00705028 1 20070514 A 3260 8005701 SENSOR EMB 145 EMB145EP 3260221 SO WOW MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 827HK 7664 145021 FLT NR 5537 - STL - DOWNLOCK RELEASE WILL NOT MOVE TO RETRACT LANDING GEAR FOLLOWING TAKEOFF. MAINTENANCE INSPECTED AND CLEANED ALL 4 WEIGHT ON WHEEL PROXIMITY SENSOR, REMOVED AND REPLACED A BAD PROXIMITY SENSOR ON LEFTHAND MAIN GEAR PERFO RMED GEAR SWING, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007051600117 20070516 00117 SO 2007 5 16 RAIA00705026 1 20070514 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 812HK 145373 POST FLT NR 5537 - STL - EMERGENCY LIGHT FLOOR PROXIMITY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED NR 2 EMERGENCY LI GHT INVERTER, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007051600125 20070516 00125 EA 2007 5 16 SWIA200718212 1 20070315 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 706SK 10149 FOUND COCKPIT FLOOR SUPPORT IS CRACKED AT FS 280, DISCOVERED AT C-CHECK. REPLACED COCKPIT FLOOR SUPPORT ANGLE P/N CC670 -33292-9 IAW CRJ700 SRM 51-42-21-001-001-A01. 2 L 7 2 4F RT A21EA 2007051600129 20070516 00129 NM 2007 5 16 UIEA200700215 1 20070430 A 2121 FAN BOEING 747 74747UF 1384812 NM E/E BAY ODOR A UIEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 496MC 29257 ELECTRICAL ODOR IN THE COCKPIT. T/S FOUND E/E COOLING SUPPLY FAN FAILED CAUSING ODOR. DEACTIVATED E/E COOLING SUPPLY F AN IAW DDPG 21-28-06 AS PER MAINTENANCE ACTION PERFORMED. 2 L 7 4 4F RT A20WE 2007051600130 20070516 00130 NM 2007 5 16 UIEA200700149 1 20070410 A 5510 7075000501N CHANNEL BOEING 747 747243B 1384830 NM RT STAB CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 RT STAB ACCESS PANEL 344 QBR OUTBOARD AFT CORNER PANEL SUPPORT FOUND CRACKED. REPLACED OUTBOARD AFT CORNER SUPPORT CHAN NEL PER BOEING MESSAGE 1-307272180-2. 2 L 7 4 4F A20WE 2007051600132 20070516 00132 NM 2007 5 16 UIEA200700214 1 20070427 A 5730 PANEL BOEING 747 747271C 1384869 NM RT WING DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 RT WING UPPER L/E PANEL AT WS 440.0 HAS AN AREA OF 24.0 INCH LONG BY 12.0 INCH WIDE OF DELAMINATION. PERMANENT REPAIR W AS ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18 SHEETS 1 THRU 5 AND 747-200 SRM 51-40-12. ALSO, REFERENCE ATLAS AIR EO NR 4757A358. 2 L 7 4 4F A20WE 2007051600178 20070516 00178 EA 2007 5 16 SWIA200718216 1 20070405 A 5743 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BRAKE ASSY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 979SW 7954 BRAKE TRANSDUCER BRACKET CRACKED IN LEFT GEAR WHEEL WELL, DISCOVERED AT C-CHECK. REPLACED BRACKET PER CRJ200 SRM 51-42- 06 PAGE 11. 2 L 7 2 4F RT A21EA 2007051600180 20070516 00180 EA 2007 5 16 SWIA200718218 1 20070405 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 979SW 7954 STATION 621 BULKHEAD RIGHT CORNER FLOORBOARD SUPPORT ANGLE IS CRACKED, DISCOVERED AT C-CHECK. REPAIRED FLOOR SUPPORT AN GLE FS621 RT IAW CRJ200 REO 601R-53-61-117 REV C. 2 L 7 2 4F RT A21EA 2007051600181 20070516 00181 EA 2007 5 16 SWIA200718219 1 20070405 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 979SW 7954 FS 280 FLOOR SUPPORT BEAM HAS CRACKED UPPER SUPPORT ANGLE AT LBL9/RBL9 AND ALL FOUR CLIPS ARE CRACKED, DISCOVERED AT C-C HECK. REPLACED FILLER ANGLE, SPLICE ANGLES AND CLIPS AT STA280 LBL9/RBL9. 2 L 7 2 4F RT A21EA 2007051600184 20070516 00184 EA 2007 5 16 SWIA200718222 1 20070405 A 5210 ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 979SW AFT PAX DOOR ANGLE FITTING IS CRACKED, DISCOVERED AT C-CHECK. REPLACED AFT ANCHOR FITTING PER CRJ200 AMM 52-11-17 PAGES 427-430. 2 L 7 2 4F RT A21EA 2007051600190 20070516 00190 WP 2007 5 16 AALA20070817 1 20070507 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 486AA 49679 LGA - EMERGENCY LIGHTS AT AFT TAIL CONE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT TAIL CONE. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051700002 20070517 00002 NM 2007 5 17 AALA20070809 1 20070505 A 3397 WIRE HARNESS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 372AA 25199 MIA - EMERGENCY LIGHT AT SEAT 29B INOPERATIVE. SECURED WIRE HARNESS TO LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 29B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007051700004 20070517 00004 WP 2007 5 17 AALA20070811 1 20070505 A 3350 GUARD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 DFW - EMERGENCY LIGHT AT SEAT 21D MISSING GUARD. REPLACED GUARD FOR EMERGENCY LIGHT AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051700012 20070517 00012 NM 2007 5 17 AALA20070795 1 20070502 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 MIA - EMERGENCY LIGHT EXIT IDENTIFIER AT FORWARD RIGHT NUMBER THREE DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT EXIT IDE NTIFIER AT FORWARD RIGHT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007051700013 20070517 00013 EU 2007 5 17 AALA20070796 1 20070502 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 59081 639 MIA - EMERGENCY LIGHT AT SEAT 9G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 9G. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F RT A35EU 2007051700015 20070517 00015 EU 2007 5 17 AALA20070799 1 20070503 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 33069 512 MIA - EMERGENCY LIGHT AT SEAT 16G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 16G. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A35EU 2007051700018 20070517 00018 NM 2007 5 17 AALA20070797 1 20070502 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 DFW - EMERGENCY AISLE LIGHT IN RIGHT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK AT RIGHT NUMBER ONE DOOR FOR EMERGENCY AISLE LIGHT AT RIGHT HAND FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007051700019 20070517 00019 NM 2007 5 17 AALA20070802 1 20070504 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 920AN 29521 MIA - EMERGENCY EXIT LIGHT AT LEFT NUMBER TWO DOOR LOOSE. REATTACHED EMERGENCY EXIT LIGHT AT LEFT NUMBER TWO DOOR. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007051700021 20070517 00021 WP 2007 5 17 AALA20070804 1 20070504 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 33414 49325 LGA - SEAT MOUNTED EMERGENCY LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AB5 3 FOR SEAT MOUNTED EMERGENCY LI GHTS AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051700024 20070517 00024 SO 2007 5 17 SWIA200718226 1 20070509 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY EXIT BROKEN A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 290SW 120317 LOWER EMERGENCY EXIT SIGN AT ROW 6BC IS BROKEN. REPLACED LIGHT ASSEMBLY AT ROW 6BC. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007051700025 20070517 00025 EA 2007 5 17 SWIA200718227 1 20070512 A 3397 CIRCUIT BOARD CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT MALFUNCTIONED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 613SK 10038 EMERGENCY LIGHTS ILLUMINATE WHEN IN THE "ARMED" POSITION. REPLACED CIRCUIT BOARD IN JB11 IAW 24-06-11. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007051700026 20070517 00026 EA 2007 5 17 SWIA200718228 1 20070509 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA LEFT FAILED A SWIA O OTHER M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 918SW 15466 8624 7645 LEFT PACK BRIEFLY HAS AN ODOR OF SMOKE, MADE A LOUD NOISE AND THEN OVERTEMPED. REPLACED LEFT AIR CYCLE MACHINE IAW AMM 21-51-10-401. 2 L 7 2 4F RT A21EA 2007051700027 20070517 00027 EA 2007 5 17 SWIA200718229 1 20070507 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 910SW 7566 LEFT AND RIGHT OVERWING EMERGENCY LIGHTS ARE INOP. RELAMPED LEFT AND RIGHT EMERGENCY LIGHTS AS REQUIRED IAW MM 33-5121. 2 L 7 2 4F RT A21EA 2007051700028 20070517 00028 EA 2007 5 17 SWIA200718230 1 20070512 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 603SK 10248 EMERGENCY FLOOD LIGHT AT ROW 15 IS INOP. RELAMPED EMERGENCY LIGHT AT ROW 15 IAW MM 33-51-01. 2 L 7 2 4F RT A21EA 2007051700029 20070517 00029 SO 2007 5 17 SWIA200718231 1 20070514 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 289YV 120289 AT THE GATE WITH PACKS RUNNING OFF OF APU BLEED, THE PACK SMELLED HOT AND THE LAV SMOKE DETECTOR WAS SET OFF. RAN PACKS ON GROUND WITH APU BLEED AND ENGINE BLEED. NO SMOKE OR ODOR WAS NOTICED IN CABIN. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007051700030 20070517 00030 NM 2007 5 17 AALA20070744 1 20070424 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 354AA 24035 MIA - EMERGENCY LIGHT AT SEAT 41B INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 41B. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A1NM 2007051700032 20070517 00032 WP 2007 5 17 AALA20070779 1 20070428 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 501AA 49738 DFW - EMERGENCY LIGHTS AT OVERHEAD SEAT ROW 25 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT SEAT ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051700033 20070517 00033 NM 2007 5 17 AALA20070776 1 20070428 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 389AA 27449 MIA - EMERGENCY LIGHTS AT SEAT ROW 2HJ HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHTS AT SEAT ROW 2HJ. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007051700034 20070517 00034 WP 2007 5 17 AALA20070774 1 20070428 A 1100 PLACARD DOUG DC9 DC982 3022082 WP CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7544A 53026 LGA - EMERGENCY EXIT ROW RECLINE PLACARD MISSING. REPLACED RECLINE PLACARD FOR EMERGENCY EXIT ROW. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051700037 20070517 00037 EU 2007 5 17 AALA20070787 1 20070430 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 41063 506 JFK - EMERGENCY LIGHTS AT FIRST CLASS RIGHT SEAT MOUNTED INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIR ST CLASS RIGHT SEAT MOUNTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007051700039 20070517 00039 NM 2007 5 17 AWXA200700593 1 20070512 A 3350 20121 CHARGER BOEING 757 7572G7 1384963 NM EMERGENCY LIGHTS INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 910AW 24523 PHX - EEL - SEAT ROWS 1 THRU 20 EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REPLACED AFT EMERGENCY LIGHT BATTERY CHARGER IAW B757-200 AMM 33-51. 2 L 7 2 4F RT A2NM 2007051700040 20070517 00040 NM 2007 5 17 AWXA200700622 1 20070428 A 5313 6545775523 STRINGER BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - FOUND CRACKED STRINGER, BS 793, S23R. REPAIRED STRINGER, BS 793, S23R IAW B737-300 SRM 53-00-03-2R1, FIGURE 201. 2 L 7 2 4F RT A16WE 2007051700041 20070517 00041 EU 2007 5 17 AWXA200700623 1 20070514 A 3350 321454 POWER SUPPLY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 642AW 42470 497 584 PHX - EEL - EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 1, 2 AND 5 ARE INOPERATIVE. REPLACED AND OPERATIONAL CHECKED EMER GENCY ESCAPE PATH LIGHT POWER SUPPLY IAW A320 AMM 33-51-38. 2 L 7 2 4F RT A28NM 2007051700042 20070517 00042 NM 2007 5 17 AWXA200700624 1 20070513 A 2730 162300103 COMPUTER BOEING 737 7373G7 1384595 NM ELEVATOR FEEL MALFUNCTIONED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 156AW 20382 6307 23778 LAS - ATO - 85-95 KT REJECTED TAKEOFF AT 28C ON RUNWAY 25R DUE TO A FLIGHT CONTROL MASTER CAUTION WARNING INDICATION. MAINTENANCE PERFORMED STEPS 15 THRU E-2 AS OUTLINED IN THE B737-300 AMM 27-31-00-5 AND TESTED THE DIFFERENTIAL PRESSURE SWITCH WITH NO FAULTS OR DISCREPANCIES NOTED. AS A PRECAUTIONARY MEASURE THE ELEVATOR FEEL COMPUTER WAS REPLACED IAW AW A TASK CARD R6C27010. A SUPPLEMENT WILL BE SUBMITTED AND PART CONDITION WILL BE UPDATED UPON RECEIVING THE COMPONENT TE AR DOWN REPORT FROM THE VENDOR PERFORMING THE REPAIR ON THE ELEVATOR FEEL COMPUTER. 2 L 7 2 4F RT A16WE 2007051700043 20070517 00043 NM 2007 5 17 AWXA200700625 1 20070513 A 5753 SKIN BOEING 757 757225 1384959 NM TE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 000046 22209 MCN - RIGHT WING INBOARD FLAP TRAILING EDGE IS DELAMINATED, MAIN FLAP STATION 120, MAIN FLAP STATION 124. REPAIRED IAW B757-200 SRM 51-70-04. 2 L 7 2 4F RT A2NM 2007051700045 20070517 00045 EU 2007 5 17 AWXA200700627 1 20070514 A 5320 D53480043203 SILL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 665AW 1644 SAL - CORROSION ON R2 DOOR CUT OUT LOWER SILL, FR 66, -Y1732. REPAIRED R2 DOOR CUT OUT LOWER SILL, FR 65 - FR 66, -Y173 2 IAW A320 SRM 5341-14. 2 L 7 2 4F RT A28NM 2007051700046 20070517 00046 EU 2007 5 17 AWXA200700628 1 20070503 A 5321 D5367180500400 FLOOR PANEL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 665AW 1644 SAL - CORROSION ON CABIN FLOORBOARD 261FF, FR 66 - FR 68, +Y1292 TO +Y1732. REPLACED CABIN FLOOR BOARD 261FF, FR 66 - F R 68, +Y1292 TO +Y1732 IAW AWA TASK CARD C1C53303. 2 L 7 2 4F RT A28NM 2007051700047 20070517 00047 EU 2007 5 17 AWXA200700629 1 20070503 A 5321 D5367180500500 FLOOR PANEL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 665AW 1644 SAL - CORROSION ON CABIN FLOOR BOARD 262FF, FR 66 - FR 68, -Y1292 TO -Y1732. REPLACED CABIN FLOOR BOARD 262FF, FR 66 - FR 68, -Y1292 TO -Y1732 IAW AWA TASK CARD C1C53303. 2 L 7 2 4F RT A28NM 2007051700048 20070517 00048 NM 2007 5 17 2007UALA01471 1 20070511 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY EXIT CEILING LIGHT AT UPPER DECK ROW 12 & ENTRY LIGHT AT DOOR 2R ARE INOPERATIVE. [SUP 06-01-07] RELAMPED NO RMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007051700049 20070517 00049 NM 2007 5 17 2007UALA01472 1 20070511 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 5E AFT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY EEL LIGHT INOPERATIVE AT SEAT 5E AFT ASSY. [SUP 06-01-07] SECURED LT ASSY OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007051700051 20070517 00051 NM 2007 5 17 2007UALA01474 1 20070511 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY EXIT SIGN INOP AT AFT CREW REST AREA. [SUP 06-06-07] RELAMPED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007051700059 20070517 00059 EA 2007 5 17 VNAA0705001 1 20070510 A 5100 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE UNKNOWN A VNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 05 254PS 7935 CREW REPORTED THE PLANE SUDDENLY JUMPED ON TAKEOFF ROLL AT 20-30 KTS. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WIT HOUT INCIDENT. MAINTENANCE PERFORMED AN INSPECTION OF THE MAIN LANDING GEAR AND FOUND NO DEFECTS. MAINTENANCE ALSO PER FORMED A TAXI CHECK WITH THE CREW AND FOUND NO DEFECTS IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 32-10-00-210-8 01. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007051700061 20070517 00061 2007 5 17 2007UALA00683 4 20070306 A 2565 BOTTLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE ESCAPE SLIDE LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 826UA A7632 989 LOW BOTTLE PRESSURE. *S/D* GAUGE LEAKING AT TEFLON TAPE. REMOVED GAUGE & INSTALLED NEW TEFLON TAPE. RETESTED & CHECK S OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007051500019 20070515 00019 NE 2007 5 15 DL764070440 2 20070503 A 7200 ENGINE BOEING 767 767432ER 1385134 NM GE CF6 CF680 30025 NE NR 1 FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 834MH 14819 29707 704952 NR 1 ENG FAILED HPC BORO OP 5039. REPLACED NR 1 ENG PER TRANS 14T103. 2 L 7 2 4F 4 F RT A1NM E13NE 2007051500030 20070515 00030 NM 2007 5 15 DL757070507 1 20070405 A 5330 143N31313 SKIN BOEING 757 757232 1384965 NM FS 452-488 S1-2R DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 664DN 25012 THE FUSELAGE SKIN HAS TWO LIGHTNING STRIKES AT FS 452 TO FS 488, S2R TO S1. THE DAMAGED AREA OF SKIN WAS CUT OUT AND A DOULBER WAS INSTALLED. 2 L 7 2 4F RT A2NM 2007051500033 20070515 00033 NM 2007 5 15 DLM88070510 1 20070510 A 5320 PAN DOUG MD88 MD88 3023688 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 CORROSION FOUND ON FWD CARGO COMP DOOR JAMB PAN BETWEEN STA Y=370.00 AND STA Y=427.00. AMX PERFORMED PERMANENT REPAIR P ER SRM 53-05 FIG 804 VIEW C-C AND D. 2 L 7 2 4F RT A6WE 2007051500040 20070515 00040 NM 2007 5 15 HNAA0700082 1 20070513 A 3350 CONTROLLER DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS FAULTY A HNAA O OTHER O OTHER CR CRUISE 1 EA 07 327EX 39194 39194 217 EMERGENCY LIGHTS FLICKERED ON SEVERAL TIMES DURING FLIGHT. REPLACED THE EMERGENCY LIGHT CONTROLLER. 2 H 7 2 4T RT A13NM 2007051500041 20070515 00041 NM 2007 5 15 UPS07449798 1 20070514 A 5730 PANEL BOEING 747 747123 1384873 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 LEFT WING LOWER T/E PANEL HAS 5 FT CRACK. A/C IS OOS. [SUP 05-21-07] REMOVED PANEL FROM A/C. SENT TO SHEETMETAL SHOP . PANEL REINSTALLED IAW EO B747-5720-6416E. 2 L 7 4 4F A20WE 2007051500043 20070515 00043 NM 2007 5 15 UPS07649797 1 20070514 A 3350 LIGHT BOEING 767 76734AF 1385212 NM FWD ENTRY DOOR BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 305UP 27243 FWD ENTRY DOOR INTERIOR EMERGENCY LIGHT INOP. [SUP 5-16-07] MOUNT WILL NOT ALLOW LENS TO BE SECURED. LOWE LAMP BAR SWI VEL IS BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSY PER B767 WDM 33-51-11. OPS CHECK GOOD PER B767 MM 33-51-01-2. 2 L 7 2 4F RT A1NM 2007051500049 20070515 00049 WP 2007 5 15 UPS07849790 1 20070411 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FS 855 LBL 65 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 CENTER SECTION EXTERIOR L-ANGLE CRACKED THRU STOP DRILLED HOLE AT STA 855 LBL 65. REMOVED CRACKED L-ANGLE AT STA 855 LBL 65 IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPAIR FILLER, AND ANGLE DOUBLER AT STA 855 LBL 6 5 IAW SRM 53-02-00 FIG 1B. 2 L 7 4 4F RT 4A25 2007051500062 20070515 00062 NM 2007 5 15 UPS07M49794 1 20070409 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 859-891 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C MID CABIN - CORROSION ON SEAT TRACK CROWN AT STA 859 & STA 891 X=8.0. REMOVED SEAT TRACK PER SRM 51-3 1-01 VOL 2 REV 28. CORRODED SEAT TRACK TRIMMED OFF PER SRM 53-70-00 FIG 1 VOL 1 REV 38. HFEC INSP CUTOUT & FOUND NO CR ACK. CORRODED SEAT TRACK REPAIRED, SPLICE HAT, HAT PLATE FAB PER SRM 53-70-00 VOL 1 FIG 1 REV 38. SEAT TRACK ATTACHED PARTS REINSTALLED PER SRM 51-31-01 VOL 2 REV 38. 2 L 7 3 4F RT A22WE 2007051500063 20070515 00063 NM 2007 5 15 DLM88070513 1 20070510 A 5415 59357112 FITTING DOUG MD88 MD88 3023688 NM RT NACELLE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 CORROSION FOUND ON THE BORE AND SURROUNDING AREA OF THE EXISTING LOWER HOLE (FRONT FACE) OF THE RT PYLON FRONT SPAR ENGI NE MOUNT FITTING, P/N 5935711-2 SATATION 1307.00. TIME LIMITED REPAIR PERFORMED IAW ERA 461312-12REV O. AFFECTED HOLE OF FITTING P/N 5935711-2 WAS ENLARGED AND A BUSHING WAS INSTALLED PER SRM 54-04 FIG 12. 2 L 7 2 4F RT A6WE 2007051500069 20070515 00069 NM 2007 5 15 DL764070521 1 20070511 A 2410 766300G GCU BOEING 767 767432ER 1385134 NM ENGINE FAULTED A DALA D RETURN TO BLOCK G J MULTIPLE FAILURE WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 845MH 29719 FIELD TRIP ON ENGINE START. NO ENGINE DRIVEN GENERATOR CA/BPCU FAULTED BOTH GCU/S. REMOVED AND REPLACED BOTH ENG GCU'S AND REPLACED BPCU. CHECKS GOOD. 2 L 7 2 4F RT A1NM 2007051500071 20070515 00071 NM 2007 5 15 DLM88070523 1 20070509 A 5753 SKIN DOUG MD88 MD88 3023688 NM LT WING TE FLAP DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 DENTS ON LOWER SKIN OF LT INNER FLAP STA XW-49. REPAIRED PER ERA 461313-14 REV O. 2 L 7 2 4F RT A6WE 2007051500073 20070515 00073 NM 2007 5 15 DLM88070525 1 20070509 A 5320 INTERCOSTAL DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 CRACK INTERCOSTAL SAT Y=218 BETWEEN LONGERON 30 AND 29RH. AMX PERFORMED PERMENANT REPAIR PER ERA 460138-14. 2 L 7 2 4F RT A6WE 2007051500079 20070515 00079 NM 2007 5 15 DL76G070531 1 20070115 A 3397 WIRE BOEING 767 767332 1382001 NM BS 1219 BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1608 30573 BROKEN EMERG EQUIPMENT LIGHTING WIRE RIGHT SIDE STA 1219 ROW 30. REPAIRED FEEDER IAW BSWPM 20-10-13. TESTED ON OPN 684 3. 2 L 7 2 4F RT A1NM 2007051500084 20070515 00084 NM 2007 5 15 DL76G070536 1 20070115 A 5330 SKIN BOEING 767 767332 1382001 NM BS 1274 S27-28R GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1608 30573 EXT FUSELAGE FWD SIDE OF AFT PIT DOOR CUTOUT STA 1274 BETWEEN STR 27R AND 28R SKIN GOUGED. REPAIRED PER ERA 459461-14. 2 L 7 2 4F RT A1NM 2007051500087 20070515 00087 NM 2007 5 15 DL76G070539 1 20070115 A 5330 SKIN BOEING 767 767332 1382001 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1608 30573 FUSELAGE SKIN ON FWD AND AFT SIDE OF BULK CARGO DOOR SCRATCHED AND GOUGED. REPAIRED PER ERA 459505-14. 2 L 7 2 4F RT A1NM 2007051500094 20070515 00094 NM 2007 5 15 DLM88070548 1 20070510 A 5320 INTERCOSTAL DOUG MD88 MD88 3023688 NM BS 1322-1338 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 FAA FINDING EXFOLIATION CORROSION ON INTERCOSTAL AND LONGERON 22 LT STA Y=1322 AND STA Y=1338 (TASK CARD 57-53300). INT ERCOSTAL FAB PER DWG 5911423 (AMX200302178). LONGERON CLEANED AND REINSPECTED, NO CORROSION FOUND (AMX 200201264). INT ERCOSTAL REINSTALLED PER SRM 51-30-2 AND DWG 5911423. 2 L 7 2 4F RT A6WE 2007051500119 20070515 00119 NM 2007 5 15 AALA20070745 1 20070424 A 2560 STRAP BOEING 767 767323 1385205 NM FLASHLIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 354AA 24035 MIA - EMERGENCY FLASHLIGHT STRAP BROKEN AT FLIGHT ATTENDANT SEAT MID GALLEY LEFT FORWARD POSITION INOPERATIVE. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT FLIGHT ATTENDANT SEAT MID GALLEY LEFT FORWARD POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007051500123 20070515 00123 NM 2007 5 15 AALA20070742 1 20070424 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 DFW - EMERGENCY LIGHT AT SEAT 25C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT T00001SE 2007051500131 20070515 00131 NM 2007 5 15 AALA20070754 1 20070426 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 345AN 33084 SFO - EXTERIOR EMERGENCY LIGHT AT AFT DOOR INOPERATIVE. RELAMPED EXTERIOR EMERGENCY LIGHT AT AFT DOOR. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007051500136 20070515 00136 NM 2007 5 15 AALA20070760 1 20070427 A 3350 BATTERY BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 393AN 29430 MIA - EMERGENCY FLASHLIGHT AT 17B INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT SEAT 17B. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007051500137 20070515 00137 NM 2007 5 15 AALA20070761 1 20070427 A 3350 BATTERY BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 393AN 29430 DFW - EMERGENCY FLASHLIGHT AT SEAT 17H INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT SEAT 17H. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007051500151 20070515 00151 NM 2007 5 15 AALA20070781 1 20070429 A 3350 0L1098BPEGPL BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 641AA 24599 LGA - EMERGENCY EGRESS LIGHT AT SEAT ROW 5 FORWARD INOPERATIVE. RELAMPED EMERGENCY EGRESS LIGHT AT SEAT ROW 5 FORWARD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007051500154 20070515 00154 WP 2007 5 15 AALA20070785 1 20070430 A 3350 0202226001 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 583AA 53160 MSP - EMERGENCY AISLE LIGHT AT SEAT 15D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY AISLE LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051500165 20070515 00165 GL 2007 5 15 DATA200700004 3 20070424 A 6110 B3339 BOLT HARTZL STBROS SD3 SD330 8100602 EU HARTZL HCB5M HCB5MP3 GL PROPELLER LOOSE E DATA K NONE O OTHER IN INSP/MAINT 1 GL 13 334AC 3283 EVA2102 SH3029 EVA2102 DURING INSPECTION OF AD 2006-22-12 TWO PROPELLER BOLTS WERE FOUND LOOSE. REPLACED PROPELLER BOLTS AND PROPELLER ASSEMBL Y. 2 H 7 2 4T A41EU 6 C P44GL 2007051500167 20070515 00167 EA 2007 5 15 A6WA200740210 1 20070409 A 5753 SKIN CNDAIR CL600 CL6002B19 1900309 EA TE FLAP DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 457AW 7854 BIRD STRIKE ON SHORT FINAL DENT FOUND ON LOWER LEFT INBOARD FLAP SKIN. MAINTENANCE PERFORMED A MAJOR REPAIR TO LT INBOA RD FLAP LOWER SKIN BY INSTALLING A 10 INCH BY 9.25 INCH EXTERNAL REPAIR DOUBLER IAW BSC EO 601R-57-11408B. (M) 2 L 7 2 4F RT A21EA 2007051500181 20070515 00181 NM 2007 5 15 HNAA0700087 1 20070512 A 3350 6104789 BATTERY DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS DISCHARGED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 805EX 4631 251 228 EMERGENCY LIGHTS FOR SIDE WALL AT 1F AND OVERHEAD GALLEY ARE OUT. REPLACED TOP AND BOTTOM EMERGENCY LIGHT BATTERIES IN COAT CLOSET, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007051600006 20070516 00006 NM 2007 5 16 UIEA200700157 1 20070403 A 5320 HXC108663 SUPPORT BOEING 747 747243B 1384830 NM BS 1241 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 LEFT FUSE TO WING LOWER PANEL 191KL FAIRING SUPPORT FRAME AT STA 1241 FOUND CRACKED. FAIRING SUPPORT FRAME REPAIRED IAW SRM 51-40-03. 2 L 7 4 4F A20WE 2007051600019 20070516 00019 NM 2007 5 16 AALA20070738 1 20070424 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 DFW - EMERGENCY LIGHT AT SEAT 9C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 9C. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F RT T00001SE 2007051600021 20070516 00021 NM 2007 5 16 AALA20070741 1 20070424 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 791AN 30254 DFW - EMERGENCY LIGHT AT SEAT 22C HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007051600035 20070516 00035 NM 2007 5 16 SWAA072390 1 20070511 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM BS 906 S4-7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 906, BETWEEN STR 4R AND STR 7R. REPAIRED SKIN PER SWA EA . 2 L 7 2 4F RT A16WE 2007051600043 20070516 00043 NM 2007 5 16 UIEA200700173 1 20070409 A 5320 SUPPORT BOEING 747 747243B 1384830 NM BS 1160 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 FX - AIR COND BAY FAIRING SUPPORT FOUND CORRODED AT BS 1160, LBL58-LBL68. CORROSION OUT OF LIMIT, FAIRING SUPPORT CHORD REPLACED AS PER SRM 51-10-01 PP AND INSTALL AS PER SRM 81-30-02. 2 L 7 4 4F A20WE 2007051600050 20070516 00050 NM 2007 5 16 UIEA200700207 1 20070425 A 5321 FLOOR PANEL BOEING 747 74747UF 1384812 NM BS 2100 PUNCTURED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 412MC 30559 DURING A-4 CHECK IN SYD, BULK CARGO FLOOR WAS FOUND PUNCTURED AT TWO PLACES, SIZE 1"BY 1" AND .5" BY .5" WHEN FLOOR WAS REMOVED. REPAIRED IAW XEO- 53-042407. 2 L 7 4 4F RT A20WE 2007051600053 20070516 00053 NM 2007 5 16 UIEA200700147 1 20070404 A 2121 4100149A FAN BOEING 747 74747UF 1384812 NM GE CF6 CF680C2* GL E/E BAY FAILED A UIEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 15 409MC 30558 UPON ENTERING THE FLIGHT DECK A STRONG ELECTRICAL OR FIRE ODOR WAS EVIDENT. STATUS MESSAGE "EE CLNG SUP FAN" DISPLAYED. FOUND THE EQUIPMENT COOLING SUPPLY FAN FAILED. DEACTIVATED THE FAN IAW DDPG 21-58-6 AND PLACED THE FAN ON DMI M07-050 . 2 L 7 4 4F 4 F RT A20WE E23EA 2007051600065 20070516 00065 EA 2007 5 16 TRAX200700653 1 20070509 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 LEFT LOWER FS 280 WEB HAS CORROSION. [SUP 05-22-07] REMOVED FASTENERS ON LT FS 280 BULKHEAD SKIN LOWER TO FOM REMOVAL OF LT LOWER FS 280 WEB. REMOVED LT LOWER FS 280 WEB IAW REO 670-53-11-052. OK TO INSTALL LT WEB STARTED INSTALLING FASTE NERS IN LT WEB. FINISHED INSTALLING FASTENERS IN LT WEB IAW BOMBARDIER REO 670-53-11-052. OK TO PRIME. 2 L 7 2 4F RT A21EA 2007051600073 20070516 00073 SO 2007 5 16 C2XA07CL045 1 20070514 A 7810 23075866 EXHAUST MIXER EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL NR 1 ENGINE FAILED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14116 10279 145672 312389 CLE FLIGHT 2541 UPON ARRIVING IN CLE FROM AUS THE NR 1 ENGINE EXHAUST MIXER ASSEMBLY WAS FOUND TO BE MISSING LARGE PIECE S. THE EXHAUST CONE WAS DAMAGED AND THE NR 1 THRUST REVERSR WAS ALSO DAMAGED. THE NR 1 ENGINE WAS REPLACED ALONG WITH THE NR 1 THRUST REVERSER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT TE6CH 2007051600076 20070516 00076 SO 2007 5 16 C2XA07IA116 1 20070512 A 3260 355022002 ELECTRONIC UNIT EMB 145 EMB145XR 3260214 SO MLG INOPERATIVE A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 16112 12549 12549 145660 MFE - FLIGHT 2082, THE CREW REPORTED THAT ON TAKEOFF OUT OF MFE, WITH THE GEAR UP AND LOCKED RECEIVED CONTINUOUS LANDING GEAR AURAL WARNINGS. THE AIRCRAFT RETURNED TO MFE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, AND RELEAS ED THE AIRCRAFT ON MEL 34-41-00 CAT A CTL NUMBER 121205, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCR AFT RETURNED TO IAH ON 05/14/07 WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONICS UNIT (LGEU), OPERATI ONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007051600078 20070516 00078 CE 2007 5 16 BSYA200700008 1 20070415 A 3260 1EN18 DOWNLOCK SWITCH LEAR 35 35LEAR 5170600 CE RT MLG INTERMITTENT E BSYA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 4358N 35065 AIRCRAFT EN ROUTE FROM ORL TO CLT, PILOT SELECTED GEAR DOWN NOTHING HAPPENED, CYCLED BREAKERS, NO HELP. BLEW GEAR DOWN WITH EMERGENCY AIR AND LANDED NO PROBLEMS. MAINTENANCE AT CLT JACKED AIRCRAFT AND SWUNG THE GEAR MANY TIMES WITH NO PRO BLEMS, DID HAVE PROBLEMS COMING INTO LCK THE NEXT NIGHT THEN GEAR FINALLY CAME DOWN. FOUND RIGHT GEAR DOWN AND LOCK SWI TCH INTERMITTENT. REMOVED AND REPLACED SWITCH, OPS CHECKS GOOD. 2 L 7 2 4F A10CE 2007051600087 20070516 00087 NM 2007 5 16 UIEA200700217 1 20070502 A 5313 STRINGER BOEING 747 7472D7B 1384803 NM BS 460-480 S28L CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 BS 460-480 STRINGER 28L FOUND SEVERAL HOLES ELONGATED. FOUND BS 460-480 STRINGER 28L REPLACED AS PER SRM 51-10-01 PAGE 9 AND AS PER SRM 51-30-02. 2 L 7 4 4F RT A20WE 2007051600096 20070516 00096 NM 2007 5 16 UIEA200700187 1 20070405 A 5712 RIB BOEING 747 747243B 1384830 NM ZONE 200 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 RHW NR 23 VC FLAP I/B ARM ROTARY ATT RIB AT OLES 1278 I/B FACE FOUND CRACKED AT "D" HOLE FWD STIFFENER AREA. CRACKED RI B "D" HOLE REPAIRED AS PER BOEING MSG 1-308409234-2. 2 L 7 4 4F A20WE 2007051600104 20070516 00104 NM 2007 5 16 UIEA200700190 1 20070405 A 5322 SHEAR TIE BOEING 747 747243B 1384830 NM ZONE 200 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 RT BS 940 TENSION TIE AREA HOLE NR 16 FOUND CRACKED AT AFT CHANNEL APPROX 0.060" RUNNING INBOARD LWR. CRACKED AFT CHANN EL REPAIRED AS PER BOEING MSG 1-303983211-2-2-4. 2 L 7 4 4F A20WE 2007051600107 20070516 00107 SO 2007 5 16 RAIA00705019 1 20070509 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 833HK 881 145240 PRE FLT NR 7900 - MKE - ALL EMERGENCY LIGHTS ARE INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY. 2 L 7 2 4T RT T00011AT 2007051600110 20070516 00110 SO 2007 5 16 RAIA00705022 1 20070511 A 3040 HEATER EMB 145 EMB145LR 3260212 SO WINDSHEILD HEAT ODOR A RAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CE 03 825HK 5689 145510 FLT NR 5576 - STL - STRONG ODOR IN COCKPIT WHEN WINDSHIELD HEAT NR 2 IS SELECTED ON. MAINTENANCE REMOVED AND REPLACED C OCKPIT WINDSHIELD, OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT T00011AT 2007051600120 20070516 00120 SO 2007 5 16 RAIA00705027 1 20070514 A 3350 317 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 812HK 145373 POST FLT NR 5574 - STL - EMERGENCY LIGHT AISLE FLOOD LIGHT BURNED OUT. MAINTENANCE REBULBED, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007051600126 20070516 00126 EA 2007 5 16 SWIA200718213 1 20070315 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 706SK 10149 PAX DOOR FORWARD WEB CRACKED AT SECOND STEP, DISCOVERED AT C-CHECK. REPLACED REPAIR ANGLES AND EXTERNAL DOUBLER PER REO 670-52-11-104. 2 L 7 2 4F RT A21EA 2007051600179 20070516 00179 EA 2007 5 16 SWIA200718217 1 20070405 A 5743 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BRAKE ASSY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 979SW 7954 BRAKE TRANSDUCER BRACKET CRACKED IN RIGHT GEAR WHEEL WELL, DISCOVERED AT C-CHECK. REPLACED BRACKET PER CRJ SRM 51-42-06 PAGE 11. 2 L 7 2 4F RT A21EA 2007051600182 20070516 00182 EA 2007 5 16 SWIA200718220 1 20070405 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 979SW PAX DOOR AFT WEB IS CRACKED BY HANDRAIL DOWN STOP, DISCOVERED AT C-CHECK. REPLACED REPAIR PARTS ON AFT SIDE OF PAX DOOR PER REO 601R 52-11-702 REV 'A'. 2 L 7 2 4F RT A21EA 2007051700006 20070517 00006 WP 2007 5 17 AALA20070813 1 20070505 A 3350 GUARD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 DFW - EMERGENCY LIGHT AT SEAT 21D MISSING GUARD. REPLACED GUARD FOR EMERGENCY LIGHT AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051700010 20070517 00010 NM 2007 5 17 AALA20070792 1 20070429 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 373AA 25200 SFO - EXTERIOR EMERGENCY LIGHT AFT OF RIGHT FLAP INOPERATIVE. RELAMPED EXTERIOR EMERGENCY LIGHT AFT OF RIGHT FLAP. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007051700023 20070517 00023 EA 2007 5 17 SWIA200718225 1 20070511 A 2910 LINE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 NM 07 457SW 7773 RECEIVED A HYD 1 HIGH TEMP CAUTION MESSAGE ON CLIMB-OUT. HYDRAULIC NR 1 SYSTEM QUANTITY INDICATORS WENT TO YELLOW DASHE D LINES WITH NO FLUID. FOUND NR 1 EDP RETURN LINE CHAFED THROUGH. FOUND CRACK IN NR 1 EDP PRESSURE LINE. REPLACED LIN ES. 2 L 7 2 4F RT A21EA 2007051700035 20070517 00035 WP 2007 5 17 AALA20070777 1 20070428 A 3350 SIGN DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 501AA 49738 DFW - EMERGENCY EXIT LIGHT SIGN AT AFT CABIN DOOR DAMAGED. REPLACED EMERGENCY EXIT LIGHT SIGN AT AFT CABIN DOOR. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051700036 20070517 00036 NM 2007 5 17 AALA20070780 1 20070429 A 3350 CM767 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 641AA 24599 LGA - RIGHT NUMBER TWO DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED RIGHT NUMBER TWO DOOR EXTERIOR EMERGENCY LIG HT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007051700038 20070517 00038 NM 2007 5 17 AALA20070788 1 20070430 A 3350 PBS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 605AA 27056 BOS - EMERGENCY LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007051700050 20070517 00050 NM 2007 5 17 2007UALA01473 1 20070511 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY EEL LIGHT INOP ACROSS DOOR 4R LOWER WALL. [SUP 06-01-07] REPLACED FEEDER CABLE OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007051700052 20070517 00052 NM 2007 5 17 2007UALA01475 1 20070511 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY EXIT SIGN INOPERATIVE ABOVE DOOR 5L & JUST AFT OF ROW 61L. [SUP 06-06-07] REPLACED BATTERY PACK . OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007051700058 20070517 00058 NM 2007 5 17 2007UALA01481 1 20070511 A 5730 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT WING CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 RIGHT UPPER WING SKIN HAS NUMEROUS AREAS OF EXFOLIATION CORROSION FROM FRONT SPAR TO AFT SPAR C-T FUSELAGE. [SUP 06-06- 07] RT WING UPPER SURFACE AT FILLET FAIRING MATING SURFACES BETWEEN FRONT SPAR TO REAR SPAR HAS NUMEROUS AREAS BLENDED E XCEEDING SRM. WORK ACCOMPLISHED PER UA ENGINEERING EVALUATION AND RECOMMENDED REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007051700067 20070517 00067 NM 2007 5 17 2007UALA01412 1 20070505 A 5410 LINK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 PYLON CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 104UA 26902 CORROSION - DIAGONAL SIDE BRACE LINK OF NR 4 PYLON INBOARD AFT (ECCENTRIC BUSHING AROUND AREA). [SUP 06-01-07] REPLACE D DSB LINK OF PYLON NR 4 INBOARD AFT AT DSB. A/C RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007051700068 20070517 00068 NM 2007 5 17 2007UALA01413 1 20070505 A 2120 UNKNOWN BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN SMOKE A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 668UA 30024 RTFL DUE TO SMOKE IN CABIN. [SUP 06-01-07] INSPECTED PACK DUCTS & EXCHANGERS, NOTHING FOUND. INSP AND TESTED SMOKE AL ARMS ALL OK. CHECK OPS OF PACKS WITH APU AND ENGINES, INCLUDING HIGH-POWER, NO ODOR OR SMOKE NOTED, REF MM21-00-21. ON 0 7MAY2007, CLEANED OVEN NR R13 ON AMIS ITEM 4652006. SUSPECT DIRTY OVEN WAS SOURCE OF ODOR & SMOKE ON 05MAY2007. 2 L 7 2 4F 4 F RT A1NM E24NE 2007051700070 20070517 00070 EU 2007 5 17 2007UALA01415 1 20070505 A 5347 SEAT TRACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 433UA 589 CABIN OUTBOARD RIGHT SEAT TRACK HAS GOUGED LUG FWD ON FRAME 47. MAJOR REPAIR ACCOMPLISHED: REPLACED FLOORBEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007051700071 20070517 00071 NM 2007 5 17 2007UALA01416 1 20070506 A 5320 PLATE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 642 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 FWD PIT, FWD CARGO DOOR CUTOUT, LOWER MAIN SILL AREA, STA 642, UPPER BEAM CHORD PLATE HAS CRACK INDICATIONS, RBL 60. [SUP 06-01-07] VERIFIED CRACK INDICATIONS PER HFEC INSPECTION. FOUND SILL CRACKED APPROX. 4.5 INCHES LONG. REMOVED LOWE R DOOR SILL AND REPLACED WITH PN 451T1604-4 AND INSTALLED PER SRM 51-40-2. A/C OK FOR SERVICE. SUSPECT MULTIPLE IMPACTS FROM CARGO & LOADING EQUIP CAUSED INITIAL CRACK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007051700072 20070517 00072 NM 2007 5 17 2007UALA01417 1 20070506 A 5310 DOOR FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CARGO DOORWAY PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 AFT PIT DOOR CUTOUT FRAME AFT SIDE JUST UNDER THE APU BATTERY DOOR FRAME WEB PUNCTURED. MAJOR REPAIR ACCOMPLISHED: CUT OUT FRAME WEB DAMAGE. FABRICATED & INSTALLED DOUBLER, SHIMS & FILLER REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 2007051700075 20070517 00075 NM 2007 5 17 2007UALA01420 1 20070504 A 3350 60243 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 315UA 23947 EMERGENCY LIGHT AT RIGHT AFT GALLEY DOOR IS OUT. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007051700076 20070517 00076 NM 2007 5 17 2007UALA01421 1 20070505 A 3350 1619 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 318UA 23950 EMERGENCY LIGHT AT RIGHT LOWER AFT FUSELAGE IS OUT. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007051700081 20070517 00081 NM 2007 5 17 2007UALA01426 1 20070505 A 2597 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE BOTTLE DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 580UA 26698 LEFT OFF WING SLIDE BOTTLE SQUIB, TEST LIGHT ON P-61 PNL STAYS ON. CLEANED CONNECTOR AND OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007051700082 20070517 00082 NM 2007 5 17 2007UALA01427 1 20070505 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 505UA 24626 EXTERIOR EMERGENCY EXIT LIGHT AT DOOR 1 LEFT IS INOP. [SUP 06-06-07] RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007051700083 20070517 00083 NM 2007 5 17 2007UALA01428 1 20070504 A 2400 CIRCUIT BREAKER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SIGNAL FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 647UA 25284 THE EVAC SIGNAL CIRCUIT BREAKER ON THE P6- 1 (F2) POPS WHEN THE EMERGENCY EVAC SWITCH IS HIT. [SUP 06-01-07] REPLACED EMER. EVAC MODULE AT AFT RT PANEL 22. OP CHECKS NORMALLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007051700086 20070517 00086 NM 2007 5 17 2007UALA01431 1 20070506 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SEAT 6HJ FWD & F INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 676UA 30028 SEAT 6HJ FWD & FWD GALLEY EMERGENCY CROSSAISLE EEL LIGHT ARE INOPERATIVE. REPLACED EEL LIGHT ASSEMBLY. OPS CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007051700087 20070517 00087 NM 2007 5 17 AWXA200700587 1 20070510 A 3350 30043233 LIGHT BOEING 737 7373G7 1384595 NM ZONE 200 INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 156AW 23778 PHX - EEL - R1 DOOR EXTERIOR ESCAPE SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED AND OPERATIONAL CHECKED R1 DOOR EXTERIO R ESCAPE SLIDE EMERGENCY LIGHT ASSEMBLY IAW B737-300 AMM 33-51-02. 2 L 7 2 4F RT A16WE 2007051700089 20070517 00089 EU 2007 5 17 AWXA200700589 1 20070510 A 3297 D231200001 WIRE HARNESS AIRBUS 320 A320231 3930325 EU ZONE 700 FAULTY A AWXA O OTHER J WARNING INDICATION DE DESCENT 1 WP 28 621AW 053 LAS - EMERGENCY LANDING - ON DESCENT, BSCU 2 FAILED WITH BSCU 1 ON MEL. RESET PROCEDURES USED PER QRH, NO RECOVERY. FL IGHT CREW DECLARED EMERGENCY AND LANDED AIRCRAFT WITHOUT INCIDENT. AIRCRAFT WAS TOWED TO THE GATE AND MAINTENANCE REMOV ED AND REPLACED THE NOSE LANDING GEAR UPPER 1M AND 2M ELECTRICAL HARNESS. IN ADDITION, BSCU PART NR C202163382D32, SN 0 1574 WAS CHANGED AS A PRECAUTIONARY MEASURE. A SUPPLEMENT WILL BE ACCOMPLISHED UPON RECEIPT OF THE BSCU COMPONENT TEARD OWN REPORT FROM THE VENDOR. 2 L 7 2 4F RT A28NM 2007051700090 20070517 00090 NM 2007 5 17 AWXA200700590 1 20070510 A 5321 D5367180500400 FLOOR PANEL AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 832AW 1643 SAL - CORROSION ON CABIN FLOOR PANEL 261FF. REPLACED CABIN FLOOR PANEL 261FF IAW AWA TASK CARD C1D25318. 2 L 7 2 4F RT A28NM 2007051700091 20070517 00091 EU 2007 5 17 AWXA200700591 1 20070510 A 5755 D5755103920000 HINGE PIN AIRBUS 320 A320232 3930326 EU ZONE 500 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 665AW 1644 SAL - CORROSION ON LEFT WING SPOILER NR 3 CENTER HINGE PIN, WS 7792 - WS 8268. REPLACED LEFT WING SPOILER NR 3 CENTER H INGE PIN, WS 7792 - WS 8268 IAW AWA TASK CARD C3L57322. 2 L 7 2 4F RT A28NM 2007051700093 20070517 00093 EU 2007 5 17 AWXA200700630 1 20070421 A 3397 E0261CF20 WIRE AIRBUS 320 A320231 3930325 EU ZONE 200 DETERIORATED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 626AW 65 SAL - EEL - C-06 CHECK - FORWARD LEFT PARTITION EMERGENCY LIGHT CABLE INSULATION DAMAGED. REPAIRED AND OPERATIONAL CHEC KED FORWARD LEFT PARTITION EMERGENCY LIGHT CABLE IAW AIRBUS ESPM 20-53-21 AND A320 AMM 33-51-00. THIS ITEM WAS PREVIOUS LY SUBMITTED AS CONTROL NR AWXA200700399 ON 04/27/2007 BUT WAS REJECTED DUE TO A DUPLICATION IN THE CONTROL NR WHICH WAS PREVIOUSLY UTILIZED BY 154AW. 2 L 7 2 4F RT A28NM 2007051700095 20070517 00095 NM 2007 5 17 AWXA200700595 1 20070510 A 5321 D5367180500500 FLOOR PANEL AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 832AW 1643 SAL - MAJOR REPAIR - FOUND CORROSION ON CABIN FLOOR PANEL 262 FF. REPLACED CABIN FLOOR PANEL 262 FF IAW AWA TASK CARD C 1D25318. 2 L 7 2 4F RT A28NM 2007051700096 20070517 00096 NM 2007 5 17 AWXA200700596 1 20070510 A 5321 D5361060500100 FLOOR PANEL AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 832AW 1643 SAL - MAJOR REPAIR - FOUND CORROSION ON CABIN FLOOR PANEL 222 FF. REPLACED CABIN FLOOR PANEL 222 FF IAW AWA TASK CARD C 1D25306. 2 L 7 2 4F RT A28NM 2007051700098 20070517 00098 NM 2007 5 17 AWXA200700598 1 20070509 A 5322 D5347112420100 SHEAR TIE AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 832AW 1643 SAL - MAJOR REPAIR - CORROSION ON CABIN SHEAR PLATE, FR 69 - FR 70, -Y1732. REPLACED CABIN SHEAR PLATE, FR 69 - FR 70, -Y1732 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007051700101 20070517 00101 NM 2007 5 17 2007UALA01432 1 20070506 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 676UA 30028 SEAT 10HJ EEL LIGHT & AFT GALLEY RIGHT SIDE CROSSAISLE EEL LIGHT ARE INOPERATIVE. RECONNECTED AND SECURED EEL LIGHT CON NECTOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2007051700102 20070517 00102 NM 2007 5 17 2007UALA01433 1 20070506 A 3397 WIRE HARNESS BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 676UA 30028 SEAT 40HJ EEL LIGHT INOPERATIVE. REPLACED SEAT WIRE HARNESS, OPS CHECK OK. [SUP 06-01-07] REPLACED SEAT WIRE HARNESS , OPS CK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007051700104 20070517 00104 NM 2007 5 17 2007UALA01435 1 20070505 A 7500 LINE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE BLEED SYSTEM RUPTURED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 821UA 944 V11050 FLIGHT DIVERTED WITH AN ENGINE BLEED PROBLEM. REPLACED PRSOV AND HIGH STAGE VALVE. REPLACED BLEED AIR PRESSURE REG SOL ENOID. [06-26-07] FOUND A RUPTURED SENSE LINE BETWEEN THE PRV AND PRV CONTROL SOLENOID. REPLACED SENSE LINE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007051700105 20070517 00105 NE 2007 5 17 2007UALA01436 2 20070507 A 7230 BLADES AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE FAILED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 29 428UA 523 V10292 RTFL WITH NR 1 ENGINE SHUT DOWN. LOUD BAND HEARD ON CLIMBOUT. REPLACED NR 1 ENGINE. [06-26-07] ENGINE INGESTED COWL ING ACOUSTIC PANELS DURING CLIMBOUT CAUSING DAMAGE TO A STAGE 3 COMPRESSOR BLADE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007051700106 20070517 00106 NM 2007 5 17 2007UALA01437 1 20070507 A 2150 A/C PACK BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LEFT UNKNOWN A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 211UA 30217 LEFT AIR COND PACK PROB CAUSED DIVERSION. [SUP 06-01-07] REPLACED RT HAND FLOW CONTROL VALVE PER MM21-51-02. FAULT C LEARED AND OP CHECKED GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007051700107 20070517 00107 NM 2007 5 17 2007UALA01439 1 20070507 A 3350 1010428 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 592UA 28143 EMERGENCY AISLE LIGHTS INOP & LOOSE IN MOUNTING AT ROWS 13 & 32. [SUP 06-06-07] REPLACED THE HOUSINGS AND TESTED SATIS FACTORILY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007051700110 20070517 00110 NM 2007 5 17 2007UALA01442 1 20070507 A 5310 STRUCTURE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE BS 360 S2L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 793UA 26946 STA 360.0 STR 2L IS DAMAGED. [SUP 06-01-07] MAJOR REPAIR ACCOMPLISHED DUE TO LIGHTNING STRIKE DAMAGE ON UPPER FUSE STA 360 STR 2L. REPAIR ACCOMPLISHED AND INSPECTED. A/C OK FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007051700112 20070517 00112 NE 2007 5 17 2007UALA01446 2 20070508 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 MAKING METAL A UALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 553UA 25277 726598 DIVERTED DUE TO RIGHT ENGINE OIL FILTER PRESSURE INDICATOR. AMBER ALERT DECLARED. NR 2 ENG MAIN OIL FILTER HAS LARGE Q TY OF FERROUS FLAKES. [SUP 06-06-07] ALSO CHECKED NR 123 AND NR 5 BEARING C-D'S AND FOUND EXCESSIVE MATERIAL. FILTER AND C'D'S REINSTALLED. REPLACED ENGINE. ATTRIBUTED THE PROBLEM TO FAILED BEARINGS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007051700113 20070517 00113 EU 2007 5 17 2007UALA01447 1 20070508 A 2910 SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYD SYSTEM MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 437UA 655 FLIGHT DIVERTED DUE TO YELLOW HYD RESERVOIR LOW LEVEL. REPLACED LOW LEVEL SWITCH. 2 L 7 2 4F 4 F RT A28NM E40NE 2007051700114 20070517 00114 EU 2007 5 17 2007UALA01449 1 20070508 A 3350 321431 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT FAULTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 460UA 1248 EMERGENCY LIGHT TEST FAILED DURING 3SVC. EPSU BATTERY AFT L IS FAULTED. REPLACED EPSU BATTERY FOR 13WL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007051700134 20070517 00134 EU 2007 5 17 UPS07149804 1 20070514 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU COCKPIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 135UP 0818 EMERGENCY LIGHT OPS CHECK FAIL AS-E CHECK 19. CYCLE CB E-28 EMERGENCY LIGHT - EXIT LIGHT OPS CHECK INTERIOR EMERGENCY L IGHT IAW MM 33-51-00-05. OPS CHECK OK. 2 L 7 2 4F RT A35EU 2007051700136 20070517 00136 NM 2007 5 17 UPS07449805 1 20070513 A 3350 LAMP BOEING 747 747121 1384871 NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 EMERGENCY LIGHT CONTROL SWITCH INDICATOR 1/2 INOP. RELAMPED EMERGENCY, OPS CHECK GOOD. 2 L 7 4 4F A20WE 2007051700137 20070517 00137 NM 2007 5 17 2007UALA01451 1 20070509 A 5310 DOOR FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 921UA 25388 FWD CARGO PIT DOOR CUTOUT AFT FRAME IS CRACKED AT THE LOWER STOP FITTING. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACE D CRACKED FRAME. 2 L 7 2 4F 4 F RT A16WE E21EU 2007051700139 20070517 00139 NM 2007 5 17 2007UALA01454 1 20070509 A 5200 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 MED 2R FRAME IS DAMAGED. [SUP 06-06-07] HFEC INSP FOUND CRACK AT FWD FRAME UPPER HINGE CUT OUT. INSTALLED A DOUBLER REPAIR PER UA APPROVED SPECIFICATION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007051700142 20070517 00142 NM 2007 5 17 2007UALA01458 1 20070509 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 EMERGENCY LIGHT ROW 58 CEILING LIGHT RIGHT INOPERATIVE. [SUP 06-01-07] RELAMPED CEILING LIGHT. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007051700145 20070517 00145 EU 2007 5 17 2007UALA01461 1 20070510 A 2150 A/C PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 421UA 500 RTFL DUE TO NR 2 PACK FAILURE & NR 1 PACK'S CURRENT DEFERRAL. AFTER ATB, ON GROUND TESTING INDICATING NORMAL SINGLE PA CK OPS-PERFORMED PACK TEMP CONTROL TEST- OK, REPLACED TURBINE BYPASS VALVE - ALL OPS TESTS ARE NORMAL- NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007051700146 20070517 00146 NM 2007 5 17 2007UALA01462 1 20070510 A 2910 MODULE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE HYD INTERFACE MALFUNCTIONED A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 783UA 26950 RIGHT HYDRAULIC SYSTEM INOP. QTY SHOWS ZERO. [SUP 06-06-07] REPLACED HYDRAULIC INTERFACE MODULE (HYDIM) (R) CARD. AC TIVE DC HARD FAULT. AFTER REPLACEMENT, INDICATIONS RETURNED TO NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007051700147 20070517 00147 NM 2007 5 17 2007UALA01463 1 20070510 A 2420 IDG BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE APU FAILED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 209UA 30215 CREW REPORTS RIGHT GENERATOR FAILURE. APU BEING USED & APU INLET DOOR OPEN. APU AUTO SHUTDOWN AT 16500 FT 310K & AGAIN AT 14500 FT 250K IDLE POWER. [SUP 06-06-07] NR 2 ENGINE IDG WAS REPLACED, BUT CAUSE OF W-U WAS APU AUTO SHUTDOWN. AF TER TROUBLESHOOTING, APU DIFFERENTIAL PRESSURE SENSOR WAS CLEANED AND RESECURRED. FOLLOW-UP VERIFICATION FLIGHT CONFIRM ED APU OP AT ALTITUDE. PLANE RETURNED TO ETOPS SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007051700148 20070517 00148 EU 2007 5 17 2007UALA01465 1 20070510 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 474UA 1475 CORROSION IN AFT PIT LEFT SIDE AT STRINGER 43L, FRAME 57. MAJOR REPAIR ACCOMPLISHED: INSTALLED SPLICE REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007051700152 20070517 00152 NM 2007 5 17 2007UALA01469 1 20070510 A 3397 LEAD BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 306UA 23667 EEL LIGHTS INOP AFT SECTION LAST 20 FT TO AFT GALLEY. [SUP 06-06-07] REPLACED LEAD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007051700154 20070517 00154 NM 2007 5 17 AWXA200700602 1 20070508 A 5320 D53472190204 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 832AW 1643 SAL - CORROSION ON CABIN FLOORBEAM, FR 66, +Y1292. REPLACED CABIN FLOORBEAM, FR 64 - FR 66, +Y1292 IAW A319 SRM 51-72 -11. 2 L 7 2 4F RT A28NM 2007051700155 20070517 00155 NM 2007 5 17 AWXA200700603 1 20070508 A 5320 D5347217220400 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 832AW 1643 SAL - CORROSION ON CABIN FLOORBEAM, FR 66 + 7", +Y1192. REPLACED CABIN FLOOR BEAM, FR 66 - FR 68, +Y1192 TO +Y1292 IA W A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007051700156 20070517 00156 NM 2007 5 17 AWXA200700604 1 20070507 A 5320 D53472193200 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 832AW 1643 SAL - CORROSION ON CABIN FLOOR BEAM, FR 66 + 14", -Y765. REPLACED CABIN FLOORBEAM, FR 66 - FR 70, -Y765 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007051700158 20070517 00158 NM 2007 5 17 AWXA200700606 1 20070506 A 5320 D53112610200 PLATE AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 832AW 1643 SAL - FOUND CORROSION ON CABIN PLATE, FR 16, -Y1379.5. REPLACED CABIN PLATE, FR 16, -Y1379.5 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007051700159 20070517 00159 NM 2007 5 17 AWXA200700616 1 20070511 A 5310 652072354 DOOR FRAME BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - MAJOR REPAIR - FORWARD CARGO COMPARTMENT DOOR CUT OUT AFT FRAME CRACKED, BS 492.50 S24R AT THE LOWER STOP FITTING . REPAIRED FORWARD CARGO COMPARTMENT DOOR CUT OUT AFT FRAME, BS 492.50 S24R AT THE LOWER STOP FITTING IAW AWA ER 03-533 2-07122-ES1. 2 L 7 2 4F RT A16WE 2007051800004 20070518 00004 NM 2007 5 18 QXEA200700755 1 20070428 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - LOWER SURFACE OF MAIN CABIN DOOR HAS CORROSION IN SEVRAL PLACES. REPAIRED IAW SRM 51-21-00, 51-42-05 AND RD8/4 -53-1892. 2 H 7 2 4T RT A13NM 2007051800005 20070518 00005 NM 2007 5 18 QXEA200700757 1 20070502 A 5414 SKIN BOMBDR DHC8 DHC8402 1390042 NM LT NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - JOBOLTS HAVE WORKED THRU TOP SKIN PANEL AND BUTT STRAP, STATION XN210, LEFT NACELLE. REPAIRED IAW RD8/4-54-154 , AND SRM 51-40-07, 51-42-05. 2 H 7 2 4T RT A13NM 2007051800006 20070518 00006 NM 2007 5 18 QXEA200700759 1 20070426 A 5310 DOOR FRAME BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - THERE IS A SMALL GOUGE ON THE AFT BAG DOOR SURROUND FRAME ABOVE NR 5 STOP FITTING. REPAIRED IAW SRM 51-26-10, 51-14-00, 53-40-15. 2 H 7 2 4T RT A13NM 2007051800007 20070518 00007 NM 2007 5 18 QXEA200700760 1 20070426 A 5310 DOOR FRAME BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - THERE IS A GOUGE ON THE AFT BAG DOOR SURROUND FRAME ABOVE THE LOWER GUIDE ROLLER PLATE. REPAIRED IAW SRM 51-26 -10, 53-40-15. 2 H 7 2 4T RT A13NM 2007051800008 20070518 00008 NM 2007 5 18 QXEA200700761 1 20070426 A 5310 DOOR FRAME BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX -THERE ARE NUMEROUS NICKS AND GOUGES AROUND STOP FITTINGS AND GUIDE ROLLER PLATES ON THE FORWARD BAG SURROUND FRA ME. REPAIRED IAW SRM 51-26-10, 51-14-00, 53-0-15. 2 H 7 2 4T RT A13NM 2007051800014 20070518 00014 NM 2007 5 18 QXEA200700724 1 20070507 A 3150 WARNING LIGHT DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 1 ENGINE FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 365PH 526 PDX FLIGHT NR 2184, NR 1 ENGINE MANUAL CAUTION LIGHT ILLUMINATED ON TAXI OUT. RESET BETA LOCKOUT CIRCUIT BREAKER. CAUT ION LIGHT DID NOT RETURN. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007051800017 20070518 00017 NM 2007 5 18 AALA20070826 1 20070509 A 3350 0201804002 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 688AA 25730 LAX - EMERGENCY LIGHT AT SEAT 9D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A2NM 2007051800018 20070518 00018 NM 2007 5 18 AALA20070819 1 20070508 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 657AM 24615 SFO - EMERGENCY LIGHT AT SEAT 28D INOPERATIVE. RECONNECTED SIDEWALL CONNECTOR FOR EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007051800019 20070518 00019 NM 2007 5 18 AALA20070820 1 20070508 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 382AN 25451 SFO - EMERGENCY EXIT LIGHT AT RIGHT HAND FORWARD SERVICE DOOR INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT RIGHT FORWA RD SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007051800021 20070518 00021 NM 2007 5 18 AALA20070822 1 20070508 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 636AM 24594 MIA - EMERGENCY LIGHT AT SEAT 28D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A2NM 2007051800022 20070518 00022 EU 2007 5 18 AALA20070839 1 20070511 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70074 517 MIA - EMERGENCY LIGHT AT SEAT 28G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 28G. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A35EU 2007051800024 20070518 00024 EU 2007 5 18 AALA20070840 1 20070511 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70074 517 MIA - EMERGENCY LIGHT AT LEFT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007051600027 20070516 00027 NM 2007 5 16 SWAA072391 1 20070511 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM BS 386 S19R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 386, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007051600028 20070516 00028 NM 2007 5 16 SWAA072394 1 20070511 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 942 S23R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007051600041 20070516 00041 NM 2007 5 16 UIEA200700170 1 20070409 A 5320 PANEL BOEING 747 747243B 1384830 NM BS 1240-1250 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 M/DECK BS 1241-1250 LBL 75-97 CLOSE-OUT PANEL NEAR TRIM AIR DUCT FOUND CRACK. TRIM AIR DUCT CLOSE-OUT PANEL. REPLACED AS PER SRM 53-23-29 PART IV. 2 L 7 4 4F A20WE 2007051600048 20070516 00048 NM 2007 5 16 UIEA200700216 1 20070504 A 5310 PANEL BOEING 747 7472D7B 1384803 NM BS 260-280 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 CRACK INDICATION ON RT SIDE PANEL BETWEEN STA 260 AND 280 AT WL 150. CRACK LOCATION IS STA 272 WL 150, BELOW RIVET RUNN ING AFT 15 MM IN LENGTH. REPAIRED CARRIED OUT IAW SRM 53-10-04 FIG 116. 2 L 7 4 4F RT A20WE 2007051600056 20070516 00056 NM 2007 5 16 UIEA200700212 1 20070425 A 5755 RIB BOEING 747 74747UF 1384812 NM NR 8 SPOILER CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 412MC 30559 RT FIXED T/E PANEL SUPPORT RIB OUTBOARD OF NR 8 SPOILER. HAS 1 CRACK IN RIB WEB APPROX 2" IN LENGTH. REPAIRED IAW XEO- 57-042307-5. 2 L 7 4 4F RT A20WE 2007051600058 20070516 00058 NM 2007 5 16 UIEA200700178 1 20070406 A 5311 DOUBLER BOEING 747 747243B 1384830 NM BS 900 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 RT BS 900 TENSION TIE AREA HOLE NR 5 FOUND CRACKED AT FRAME DOUBLER, INSULATION BLANKET HOLE FOUND CRACKED AT FRAME DOUB LER BETWEEN S-8R TO S-9R AND S-10R TO S-10AR. FRAME DOUBLER REPAIRED AS PER BOEING MSG 1-306586780-2. 2 L 7 4 4F A20WE 2007051600061 20070516 00061 EA 2007 5 16 TRAX200700648 1 20070511 A 2910 HYDRAULIC SYSTEM CNDAIR CL600 CL6002B19 1900309 EA NR 2 SYSTEM LOW PRESSURE A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 844AS 7317 JAN - DCA DIVERTED INTO ROA HYD SYSTEM NR 2 HIGH TEMP CAUTION MSG AND THEN LOST PRESSURE. CAPT SHUT THE ENGINE DOWN, QT Y AT 15 PERCENT AFTER LANDING. EN ROUTE TO DCA A/C DIVERTED TO ROA DUE TO MTC. EMERGENCY DECLARED. FLT 4459 CX AND ON 5/12/07 FLT 4623 CX. 2 L 7 2 4F RT A21EA 2007051600067 20070516 00067 EA 2007 5 16 TRAX200700655 1 20070510 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR TORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 PAX DOOR EXIT PLACARD TORN. [SUP 05-17-07] REMOVED AND REPLACED PAX DOOR "EXIT" PLACARD WITH NEW SERVICEABLE ONE IAW C RJ AMM 11-30-02. 2 L 7 2 4F RT A21EA 2007051600069 20070516 00069 EA 2007 5 16 TRAX200700657 1 20070510 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 PAX DOOR OUTER HANDLE CRACKED. [SUP 05-24-07] REMOVED CRACKED OUTER PAX DOOR HANDLE, IAW CRJ 700 AMM 52-11-03. REMOVED SERVICEABLE PAX DOOR HANDLE FLAP, P/N 601R317045-1 FROM UNSERVICEABLE OUTER PAX DOOR HANDLE, IAW CRJ 700 SRM 51-42-06. OKAY TO INSTALL HANDLE. INSTALLED SERVICEABLE PAX DOOR HANDLE, P/N 601R31763-1, IAW CRJ 700 AMM 52-11-03. PAX DOOR HAN DLE FLAP REQUIRES HINGE REPLACEMENT FOR INSTALLATION. LOCATED AND COUNTERSUNK HOLES ON PAX DOOR HANDLE FLAP HINGE, P/N 601R317046-3, IAW CRJ SRM 51-40-11. INSTALLED FLAP WITH SERVICEABLE SPRING, P/N 601R317044-3, IAW CRJ SRM 51-42-06. REQ UIRES OPS CHECK. OPS CHECK GOOD, IAW CRJ AMM 52-11-03. 2 L 7 2 4F RT A21EA 2007051600079 20070516 00079 NM 2007 5 16 UIEA200700186 1 20070406 A 5310 PLATE BOEING 747 747243B 1384830 NM ZONE 200 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 M/D BS 940 LT TENSION TIE STEEL PLATE FASTENER HOLE 1 FOUND SHORT EDGE MARGIN. M/D BS 940 LT TENSION TIE STEEL PLATE RE PAIRED AS PER BOEING MSG 1-30-3983211-2-1 AND 4 FIG 3. 2 L 7 4 4F A20WE 2007051600081 20070516 00081 NM 2007 5 16 UIEA200700183 1 20070402 A 5340 ATTACH FITTING BOEING 747 747243B 1384830 NM BS 840 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 M/D LT BS 840 FRAME TO TENSION TIE CONNECTION FOUND NR 4 HOLE CRACK AT TENSION TIE FWD CHANNEL. CRACK FWD CHANNEL REPAI RED AS PER BOEING MSG 1-303978264-2. 2 L 7 4 4F A20WE 2007051600082 20070516 00082 NM 2007 5 16 UIEA200700184 1 20070402 A 5340 ATTACH FITTING BOEING 747 747243B 1384830 NM BS 840 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 M/D LT BS 840 FRAME TO TENSION TIE CONNECTION FOUND NR 5 HOLE CRACK AT TENSION TIE AFT CHANNEL. M/D LT BS 840 FRAME TO TENSION TIE CONNECTION TENSION TIE AFT CRACKED CHANNEL REPAIRED AS PER BOEING MSG 1-303978264-2. 2 L 7 4 4F A20WE 2007051600089 20070516 00089 NM 2007 5 16 UIEA200700189 1 20070406 A 5311 FRAME BOEING 747 747243B 1384830 NM ZONE 200 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 M/D STA 360 S-23R FRAME STRINGER CUT-OUT CRACK. CRACKED FRAME REPAIRED AS PER BOEING MSG 1-307825515-2-1. 2 L 7 4 4F A20WE 2007051600093 20070516 00093 NM 2007 5 16 UIEA200700185 1 20070402 A 5340 ATTACH FITTING BOEING 747 747243B 1384830 NM BS 880 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 M/D RT BS 880 FRAME TO TENSION TIE CONNECTION FOUND NR 6 HOLE CRACK AT TENSION TIE FWD CHANNEL. CRACKED AFT CHANNEL REP AIRED AS PER BOEING MSG 1-303986330-2. 2 L 7 4 4F A20WE 2007051600103 20070516 00103 NM 2007 5 16 UIEA200700219 1 20070511 A 5751 SKIN BOEING 747 74747UF 1384812 NM RT AILERON DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 409MC 30558 FOUND ON WALK AROUND RT OUTBD LOCATION LOWER SURFACE HAS TWO LOCATIONS WITH PREVIOUS REPAIRS NOT PAINTED. REPAIRED PER XEO 57-050807-2. 2 L 7 4 4F RT A20WE 2007051600108 20070516 00108 SO 2007 5 16 RAIA00705020 1 20070510 A 3350 RPS1B BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 818HK 145059 POST FLT NR 5505 - STL - EMERGENCY LIGHT AISLE FLOOD LIGHT IS OUT. MAINTENANCE REMOVED AND REPLACED NR 1 BATTERY POWER SUPPLY, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007051600109 20070516 00109 SO 2007 5 16 RAIA00705021 1 20070510 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 830HK 145313 POST FLT NR 5492 - STL - EMERGENCY LIGHT SERVICE DOOR EXIT MARKER IS OUT. MAINTENANCE REMOVED AND REPLACED NR 2 EMERGEN CY LIGHT INVERTER, SYSTEM CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007051600112 20070516 00112 2007 5 16 MWEA070116 4 20070511 A 2565 BOTTLE DOUG DC9 DC981 3022081 WP ESCAPE SLIDE LOW PRESSURE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 804ME 48030 TAIL CONE EVACUATION SLIDE BOTTLE PRESSURE GAUGE NOT IN THE GREEN BAND. REMOVED AND REPLACED TAIL CONE SLIDE ASSEMBLY. 2 L 7 2 4F A6WE 2007051600131 20070516 00131 NM 2007 5 16 UIEA200700191 1 20070406 A 5311 FRAME BOEING 747 747243B 1384830 NM ZONE 200 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 BS 360 LT S24A STRINGER CUT-OUT CRACKED. CRACKED FRAME WEB REPAIRED AS PER BOEING MSG 1-307193755-1-2. 2 L 7 4 4F A20WE 2007051600185 20070516 00185 SO 2007 5 16 SWIA200718223 1 20070505 A 2420 SHUNT EMB 120 EMB120ER 3260203 SO APU GENERATOR OVERHEATED A SWIA O OTHER M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 293SW 120320 FIRST OFFICERS RELAY PANEL IS TOO HOT TO TOUCH, ALONG WITH A BURNING ODOR ON FLIGHT DECK. FOUND APU GENERATOR SHUNT/REL AY TO BE OVERHEATING. FOUND BOTH TERMINALS ON RELAY TO BE LOOSE. SECURED TERMINALS. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007051600188 20070516 00188 WP 2007 5 16 AALA20070815 1 20070506 A 3350 OL1098BPEGPL BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 453AA 49558 MSP - EMERGENCY LIGHT AT SEAT 8D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 8D. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F A6WE 2007051600189 20070516 00189 NM 2007 5 16 AALA20070816 1 20070506 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 677AN 29427 ORD - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007051600191 20070516 00191 NM 2007 5 16 AALA20070818 1 20070507 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 650AA 24608 MIA - EMERGENCY EXIT LIGHT AT SEAT 4C INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT SEAT 4C. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A2NM 2007051600192 20070516 00192 NM 2007 5 16 AALA20070807 1 20070505 A 2913 887673 PUMP BOEING 757 757223 1384957 NM HYD SYSTEM LEAKING A AALA A UNSCHED LANDING K FLUID LOSS AP APPROACH 1 SW 21 694AN 26974 JFK INFLIGHT T1298/05MAY - LEFT HYDRAULIC SYSTEM LOST IN FLIGHT. LANDED JFK WITHOUT INCIDENT. REPLACED RIGHT MAIN LAND ING GEAR DOWNLOCK ACTUATOR LINE AND REPLACED LEFT ENGINE DRIVEN HYDRAULIC PUMP, CASE AND RETURN FILTER. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007051700001 20070517 00001 NM 2007 5 17 AALA20070808 1 20070505 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 JFK - SEAT MOUNTED EMERGENCY LIGHTS IN BUSINESS CLASS INOPERATIVE. REPLACED BATTERY PACK AT RIGHT NUMBER TWO DOOR FOR S EAT MOUNTED EMERGENCY LIGHTS IN BUSINESS CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007051700003 20070517 00003 WP 2007 5 17 AALA20070810 1 20070505 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 DFW - EMERGENCY LIGHT AT SEAT 21D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F A6WE 2007051700005 20070517 00005 WP 2007 5 17 AALA20070812 1 20070505 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 DFW - EMERGENCY LIGHT AT SEAT 27D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 27D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F A6WE 2007051700016 20070517 00016 WP 2007 5 17 AALA20070800 1 20070503 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 455AA 49560 LGA - EMERGENCY FLASHLIGHT STRAPS BROKEN AT AFT ENTRY DOOR. REPLACED EMERGENCY FLASHLIGHT STRAPS AT AFT ENTRY DOOR. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051700017 20070517 00017 WP 2007 5 17 AALA20070801 1 20070503 A 2560 STRAP DOUG DC9 DC982 3022082 WP CABIN MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 455AA 49560 LGA - EMERGENCY FLASHLIGHT STRAP MISSING AT LEFT NUMBER TWO DOOR. REPLACED EMERGENCY FLASHLIGHT STRAP AT LEFT NUMBER TW O DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051700022 20070517 00022 WP 2007 5 17 AALA20070805 1 20070504 A 3350 SOCKET DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 33414 49325 LGA - FOUND EMERGENCY LIGHT AT SEAT 14D INOPERATIVE. REPLACED LIGHT SOCKET ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 14D. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051700053 20070517 00053 NM 2007 5 17 2007UALA01476 1 20070511 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY EXIT CEILING ENTRY LIGHT INOP AT DOOR 5L. [SUP 06-06-07] REPLACED BATTERY PACK . OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007051700055 20070517 00055 NM 2007 5 17 2007UALA01478 1 20070511 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY EXIT LIGHT VERY DIM AT DOOR 1L BUSTLE. [SUP 06-06-07] RECHARGED BATTERY PACK OPS NORMAL 2 L 7 4 4F 4 F RT A20WE E24NE 2007051700069 20070517 00069 NM 2007 5 17 2007UALA01414 1 20070505 A 2897 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BOOST PUMP LOOSE A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 545UA 25323 RTFL DUE TO LEFT AFT FUEL BOOST PUMP INOPERATIVE. [SUP 06-06-07] LEFT AFT FUEL PUMP ANNUNCIATED EICAS & LOW PRESS ON I N SWITCH. FOUND NR 1 ENG DRIVEN HYD PUMP CONNECTOR LOOSE. SECURED NR 1 ENGINE EDP DEPRESSURIZATION SOLENOID AS REQUIRE D. 2 L 7 2 4F 4 F RT A2NM E17NE 2007051700077 20070517 00077 NM 2007 5 17 2007UALA01422 1 20070505 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY EXIT LIGHT INOP AT FLIGHT DECK CEILING & ROW 17AB CEILING. RELAMPED EMERGENCY EXIT LIGHT. OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007051700080 20070517 00080 NM 2007 5 17 2007UALA01425 1 20070505 A 3350 20131 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 558UA 26654 EMERGENCY SLIDE LIGHT ON EXTERIOR OF AFT CARGO DOOR, EMERGENCY AISLE LIGHT IN STOW BIN BULLNOSE AT LEFT ROW 26 & EMERGEN CY OVERHEAD EXIT SIGN AT ROW 15-16 ARE INOPERATIVE. REPLACED BATTERY PACK FOR POWER SUPPLIES. 2 L 7 2 4F 4 F RT A2NM E17NE 2007051700084 20070517 00084 NM 2007 5 17 2007UALA01429 1 20070504 A 3520 HOSE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE O2 MASKS KINKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 MAIN CABIN O2 MASK HOSES KINKED SEAT ROWS 2 CENTER, 1 EA 2 RT 1 EA 35 RT 1 EA 35 CENTER, 2 EA 1 EA AT 18C AND R, 29C AND R, AND 17C AND R. REPLACED MASKS WITH KINKED HOSES PER MM35-21-04. CLOSED PSU'S PER MM35-21-04. A/C READY FOR SERVICE . SUSPECT KINKING CAUSED BY IMPROPER PACKING. 2 L 7 2 4F 4 F RT A1NM E24NE 2007051700088 20070517 00088 NM 2007 5 17 AWXA200700588 1 20070509 A 2560 P4010021 CONNECTOR BOEING 737 73733A 1384673 NM FLASHLIGHT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 166AW 23627 MCN - EEL - FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT IS INOPERATIVE. REPLACED AND OPERATIONAL CHECKED THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT POWER UNIT DUE TO A BROKEN CONNECTOR. 2 L 7 2 4F RT A16WE 2007051700103 20070517 00103 NM 2007 5 17 2007UALA01434 1 20070506 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 676UA 30028 EEL LIGHT FRONT OF LAV AT RIGHT SIDE AFT GALLEY INOPERATIVE. REPAIRED WIRING, OPS CHECK OK. [SUP 06-01-07] REPAIRED W IRING, OPS CHECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007051700140 20070517 00140 NM 2007 5 17 2007UALA01455 1 20070509 A 5330 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE BS 219-201 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 793UA 26946 LIGHTNING STRIKE DAMAGE ABOVE COCKPIT AT STA 219 LBL 9.5 AND STA 201 LBL 8. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBL ER REPAIR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007051700153 20070517 00153 NM 2007 5 17 AWXA200700601 1 20070508 A 5320 D53112782202 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 832AW 1643 SAL - MAJOR REPAIR - CORROSION ON CABIN FLOOR SUPPORT, FR 12 - FR 24, -Y765. REPLACED CABIN FLOOR SUPPORT, FR 12 - FR 24, -Y765 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007051700166 20070517 00166 NM 2007 5 17 AWXA200700610 1 20070428 A 5340 69432451 FITTING BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - AFT CARGO COMPARTMENT DOOR CUT OUT SILL WEB INTERCOSTAL FITTING (STOP BLOCK) CRACKED, BS 809, S25R . REPLACED AFT CARGO COMPARTMENT DOOR CUT OUT SILL WEB INTERCOSTAL FITTING (STOP BLOCK), BS 809, S25R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007051800002 20070518 00002 EU 2007 5 18 DHLA200700026 1 20070516 A 2611 CG7GF SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A DHLA O OTHER N FALSE WARNING CR CRUISE 1 GL 05 366DH 249 UPON DESCENT RECEIVED SEVERAL FLT DECK SMOKE WARNINGS WITH SMOKE LIGHT ON MWP WITH SSC, NO SMOKE OR FUMES NOTED IN COCKP IT. REMOVED AND REPLACED FLT DECK SMOKE DETECTOR. AS PER A300 MM 26-14-11. PERFORMED SYSTEMS TEST AS PER A300 MM 26-1 4-00. OPS CK GOOD. 2 L 7 2 4F RT A35EU 2007051800009 20070518 00009 NM 2007 5 18 QXEA200700762 1 20070501 A 5711 SPAR BOMBDR DHC8 DHC8402 1390042 NM RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - RIGHT WING INBOARD LOWER SPAR FLANGE CHAFED INBOARD EDGE. REPAIRED IAW SRM 51-21-00 AND RD8/4-57-796. 2 H 7 2 4T RT A13NM 2007051800023 20070518 00023 WP 2007 5 18 AALA20070833 1 20070510 A 3350 PORTABLE LIGHT DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 464AA 49594 DFW - PORTABLE EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT AT FORWARD CABIN. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051800028 20070518 00028 2007 5 18 QXEA200700778 4 20070511 A 3442 MI5853512 INDICATOR DHAV DHC8 DHC8202 2809007 NM WX RADAR MALFUNCTIONED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 350PH 3091 488 IDA FLIGHT NR 2165, AFTER TURNING ON ALL ELECTRONICS IN THE FLIGHT DECK THERE WAS A SLIGHT ELECTRICAL ODOR AFTER ONE MIN UTE IT WAS VERY STRONG AND REACHED BACK TO ROW THREE. THERE WAS NO SMOKE THAT WE NOTICED BUT SOMETHING WAS BURNING. RE PLACED WEATHER RADAR INDICATOR PER D-8 MM 34-41-05-000-801. INSPECTED ATTACHING AND SURROUNDING WIRE BUNDLES FOR HIDDEN DAMAGE, NONE FOUND. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007051800029 20070518 00029 WP 2007 5 18 AALA20070854 1 20070513 A 3350 PORTABLE LIGHT DOUG DC9 DC982 3022082 WP CABIN UNSECURE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 262AA 49290 DFW - PORTABLE EMERGENCY LIGHT IN CABIN NOT SECURED. SECURED PORTABLE EMERGENCY LIGHT IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051800030 20070518 00030 WP 2007 5 18 AALA20070855 1 20070513 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 262AA 49290 DFW - EMERGENCY LIGHTS AT SEAT ROWS 13 TO 16 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 13 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051800031 20070518 00031 WP 2007 5 18 AALA20070856 1 20070513 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 262AA 49290 DFW - EMERGENCY LIGHT AT SEAT ROW 13 INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT ROWS 13. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F A6WE 2007051800032 20070518 00032 WP 2007 5 18 AALA20070857 1 20070513 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 262AA 49290 DFW - EMERGENCY LIGHT AT SEAT ROW 14 INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT ROWS 14. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F A6WE 2007051800033 20070518 00033 NM 2007 5 18 AALA20070841 1 20070512 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 938AN 29533 MIA - EMERGENCY LIGHT AT SEAT 10D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A16WE 2007051800035 20070518 00035 WP 2007 5 18 AALA20070843 1 20070513 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 403A 49314 LGA - EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD CABIN. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051800036 20070518 00036 WP 2007 5 18 AALA20070844 1 20070513 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 403A 49314 LGA - EMERGENCY LIGHTS AT TAIL CONE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT TAIL CONE. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051800037 20070518 00037 WP 2007 5 18 AALA20070845 1 20070514 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 438AA 49456 SFO - EMERGENCY EXIT LIGHTS AT RIGHT AND LEFT AFT ESCAPE DOOR INOPERATIVE. REPLACED BATTERY PACK AT ROW 21 FOR EMERGENCY EXIT LIGHTS AT RIGHT AND LEFT AFT ESCAPE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007051800038 20070518 00038 WP 2007 5 18 AALA20070846 1 20070514 A 3350 LENS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 438AA 49456 SFO - EMERGENCY PATH LIGHT AT AFT STAIRWELL FORWARD SIDE HAS CRACKED LENS. REPLACED LENS FOR EMERGENCY PATH LIGHT AT AF T STAIRWELL FORWARD SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007051800039 20070518 00039 WP 2007 5 18 AALA20070858 1 20070513 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 262AA 49290 DFW - EMERGENCY LIGHT AT SEAT ROW 15 INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT ROWS 15. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F A6WE 2007051800040 20070518 00040 WP 2007 5 18 AALA20070847 1 20070514 A 3350 BULB DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 438AA 49456 SFO - CEILING EMERGENCY LIGHT AT SEAT ROW 3 INOPERATIVE. RELAMPED CEILING EMERGENCY LIGHT AT SEAT ROW 3. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007051800041 20070518 00041 WP 2007 5 18 AALA20070859 1 20070513 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 262AA 49290 DFW - EMERGENCY LIGHT AT SEAT ROW 16 INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT ROWS 16. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F A6WE 2007051800043 20070518 00043 NM 2007 5 18 751003 1 20070430 A 5753 FITTING BOEING 747 747228F 1384895 NM FORE FLAP SHEARED A Q2SA O OTHER O OTHER AP APPROACH 1 EA 63 751SA 000599 22678 LOUD THUMP HEARD WHEN MOVING FLAPS FROM 10 TO 20 DEGREES. INSPECTED AIRCRAFT AND FOUND RT INBD TRAILING EDGE FORE-FLAP FITTING SHEARED AND OTHER COMPONENTS IN THE AREA DAMAGED. REMOVED AND REPLACED FORE-FLAP, 2 EACH RIBS, RT INBD AILERON AND PERFORMED A FLAP SKEW INSPECTION IAW AMM 05-51-43. 2 L 7 4 4F A20WE 2007051800044 20070518 00044 NM 2007 5 18 AALA20070849 1 20070513 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 787AL 30010 DFW - EMERGENCY LIGHT AT RIGHT AFT GALLEY PARTITION MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RIGHT AFT GALLEY PARTITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007051800046 20070518 00046 WP 2007 5 18 AALA20070850 1 20070513 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 262AA 49290 DFW - EMERGENCY LIGHT AT SEAT ROW 11 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 11. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051800047 20070518 00047 WP 2007 5 18 AALA20070851 1 20070513 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 262AA 49290 DFW - EMERGENCY LIGHT AT SEAT ROW 11 INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT ROW 11. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F A6WE 2007051800050 20070518 00050 NM 2007 5 18 AALA20070823 1 20070508 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 636AM 24594 MIA - EMERGENCY LIGHT AT SEAT 30D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 30D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007051800051 20070518 00051 WP 2007 5 18 IXXA07SMN151S 1 20070421 A 5340 3640887U FITTING DOUG DC8 DC871F 302199D WP ZONE 100 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, IN MAIN CARGO COMPARTMENT, FOUND CORROSION ON FITTING ABOVE MAIN LANDING GEAR WHEEL W ELL CEILING BETWEEN STATION 960.000 - 980.000 RIGHT BOTTOM LINE 40". REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING, IAW DC8 SRM 51-3-1,DC8 SRM 51-1-8, DC8 SRM 53-2-0 PAGE 2P, DC8 SRM 51-1-20D, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007051800052 20070518 00052 NM 2007 5 18 DHL2007788510 1 20070504 A 5313 BAC14934127075 STRINGER BOEING 727 727214 138407R NM BS 510 S27R CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 EXFOLIATION ON STRINGER 27R STA 510. CUT OUT DAMAGED AREA OF STR 27R 7 INCHES IN LENGTH IAW B727 SRM 53-10-3, FIG 1. F ABRICATED STRINGER FILLER FROM 7075T6, 7" BY.040", CHORD FROM BAC 1493-412-7075T6, 15 INCHES LONG TWO EACH, ANGLE FROM BAC 1498-140-7075T6, 13.25" LONG IAW B727 SRM 53-10-3, FIG 1 AND 51-20-1. TREATED PRIMED AND INSTALLED REPAIR IAW B727 SRM 51-10-2 AND 53-10-3, FIG 1. 2 L 7 3 4F A3WE 2007051800054 20070518 00054 WP 2007 5 18 IXXA07SMN148S 1 20070421 A 5313 S1616757 LONGERON DOUG DC8 DC871F 302199D WP BS 1766-1794 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE TAIL SECTION LONGERON 17 RIGHT HAND, WITH A CRACK AT STATION 1766.000 TO STATION 1794.000. REMOVED CRACKED LONGERON. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW LONGERON IAW DC8 SRM 5 3-5-1 PAGE 22 FIGURE 7 SHEET 1 ITEM "B", DC8 SRM 53-1-0 PAGE 1, DC8 SRM 51-1-20D, DC8 SRM 51-1-8B, DC8 SRM 51-2-0 PAGE 3 9 FIGURE 50 SHEET 37, DC8 SRM 51-1-21, AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007051800055 20070518 00055 WP 2007 5 18 IXXA07SMN149S 1 20070421 A 5313 S1616757 LONGERON DOUG DC8 DC871F 302199D WP BS 1766-1794 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE TAIL SECTION LONGERON 17 LEFT HAND, WITH A CRACK AT STATION 1766.000 TO STATION 1794.000. REMOVED CRACKED LONGERON. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW LONGERON IAW DC8 SRM 5 3-5-1 PAGE 22 FIGURE 7 SHEET 1 ITEM "B", DC8 SRM 53-1-0 PAGE 1, DC8 SRM 51-1-20D, DC8 SRM 51-1-8B, DC8 SRM 51-2-0 PAGE 3 9 FIGURE 50 SHEET 37, DC8 SRM 51-1-21, AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007051800059 20070518 00059 WP 2007 5 18 IXXA070025O 1 20070515 A 2913 57155A PUMP DOUG DC8 DC862F 3021972 WP HYDRAULIC SYS LEAKING A IXXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 11 71CX 70203 200 45961 DURING CLIMB-OUT FROM KTOL, THE CREW NOTICED HYDRAULIC QUANTITY DECREASING. THE CREW RETURNED TO KTOL AND LANDED WITHOU T INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THAT THE RUDDER HYDRAULIC PUMP WAS DEFECTIVE. MAINTENANCE REM OVED AND REPLACED THE RUDDER HYDRAULIC PUMP, AND RESERVICED HYDRAULIC SYSTEM. MAINTENANCE PERFORMED OPERATIONAL AND LEA K CHECK. OPERATIONAL CHECK WAS GOOD AND NO LEAKS DETECTED IAW MAINTENANCE MANUAL 27-24-2. AIRCRAFT RETURNED TO SERVICE . 2 L 7 4 4F 4A25 2007051800060 20070518 00060 WP 2007 5 18 IXXA070026O 1 20070515 A 2910 LINE DOUG DC8 DC862F 3021972 WP HYD SYSTEM LEAKING A IXXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 11 71CX 70204 201 45961 DURING CLIMB-OUT FROM KTOL, THE CREW NOTICED HYDRAULIC QUANITY STARTED DROPPING RAPIDLY TOWARD EMPTY. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND PRESSURE FLEX LINE LEAKING AT NUMBER TWO ENGINE DRIVEN HYDRAULIC PUMP. MAINTENANCE TIGHTEND THE FLEX LINE, RESERVICED HYDRAULIC SYSTEM, OPERATIONAL AND LEA K CHECK WAS GOOD, IAW DACO DC8 MAINTENANCE MANUAL 29-10-12 AND ATI ERH 70.01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2007051800063 20070518 00063 EU 2007 5 18 AALA20070827 1 20070509 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 90070 513 MIA - EMERGENCY LIGHTS AT SEAT ROWS 19C TO 28C INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROWS 19C TO 28C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007051800066 20070518 00066 NM 2007 5 18 AALA20070836 1 20070511 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 MIA LGA - EMERGENCY EXIT IDENTIFIER LIGHT AT AFT SIDE OF RIGHT NUMBER TWO DOOR INOPERATIVE. RELAMPED EMERGENCY EXIT IDE NTIFIER LIGHT AT AFT SIDE OF RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007051800067 20070518 00067 NM 2007 5 18 AALA20070837 1 20070512 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 781AN 29586 LHR LGA - EMERGENCY LIGHT AT FIRST CLASS COAT CLOSET BROKEN. SECURED RIGHT LOWER EMERGENCY LIGHT LENS INTO FRAME MOUNT AT FIRST CLASS COAT CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007051800069 20070518 00069 2007 5 18 AALA20070824 4 20070509 A 2330 MONITOR BOEING 757 757223 1384957 NM CABIN SHORTED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 602AN 27053 SXM INFLIGHT T1738/09MAY - AFTER TAKEOFF FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. RETURNED TO SXM AND LANDED WITHOUT I NCIDENT. FOUND NUMBER FIVE MONITOR WITH SHORT THAT CAUSED MONITOR TO SMOKE WHEN POWERED ON. REPLACED MONITORS NUMBER T HREE AND FIVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007051800070 20070518 00070 WP 2007 5 18 AALA20070830 1 20070510 A 2822 PUMP DOUG DC9 DC982 3022082 WP FUEL BOOST INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 443AA 49469 ORD INFLIGHT T2337/10MAY - AFT CENTER BOOST PUMP CIRCUIT BREAKER POPPED. CAPTAIN UNABLE TO GET FUEL FROM CENTER TANK. RETURNED TO ORD DUE TO PASSENGER CUSTOMER SERVICE AND MAINTENANCE AVAILABILITY. LANDED WITHOUT INCIDENT. REPLACED AFT CENTER FUEL BOOST PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051800071 20070518 00071 WP 2007 5 18 AALA20070831 1 20070510 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 559AA 53089 LGA - EMERGENCY LIGHT AT FLIGHT DECK OVERHEAD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FLIGHT DECK OVE RHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051800072 20070518 00072 WP 2007 5 18 AALA20070832 1 20070510 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 559AA 53089 LGA - EMERGENCY ESCAPE PATH LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY ESCAPE PATH LIGHTS AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051800075 20070518 00075 NM 2007 5 18 AALA20070825 1 20070509 A 3350 0202226001 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 688AA 25730 LAX - EMERGENCY LIGHT AT SEAT 9D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007051800076 20070518 00076 EU 2007 5 18 DHLA200700027 1 20070516 A 2170 COALESCER BAG AIRBUS 300 A300B4203 3930306 EU CABIN AIR DIRTY A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 05 362DH 084 WHILE IN FLIGHT AN OILY FOUL ODOR WAS OBSERVED ON THE FLIGHT DECK. TURNED OFF PACK NR 2, ODOR WENT AWAY. DURING PREFLI GHT PACK NR 2 WAS RUN FROM THE APU BLEED, NO ODOR WAS OBSERVED. FOUND NR 2 PACK COALESCER BAG EXTREMELY DIRTY. REMOVED AND REPLACED COALESCER BAG IAW A300 M/M CH 21-51-16. OPERATED NR 2 PACK, NO SMELL NOTED 1 20D10-3. 2 L 7 2 4F RT A35EU 2007051800077 20070518 00077 NM 2007 5 18 QXEA200700725 1 20070504 A 3097 BUSS BAR BOMBDR DHC8 DHC8402 1390042 NM PROPELLER DAMAGED A QXEA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 NM 09 405QX 12617 4047 LAX FLIGHT NR 2310: WHEN PROP DEICE WAS SELECTED ON, BOTH AC GENERATORS WENT OFF LINE. AS PER CHECKLIST, RESET BOTH AC GENERATORS. MAINTENACE INSPECTED AND REMOVED AND REPLACED PROP BUS BAR ASSEMBLY IAW AMM TASKS 61-10-06-000-804 AND 61-1 0-06-400-804. OPS CHECK GOOD. NO DEFECTS NOTED. GENERATORS STAYED ON LINE WHEN PROP DEICE WAS SELECTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007051800078 20070518 00078 NM 2007 5 18 QXEA200700738 1 20070425 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 480 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - LEFT INBOARD SEAT TRACK NR 7 HAS DEEP PITTING CORROSION AT STATION 480.0. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007051800079 20070518 00079 NM 2007 5 18 QXEA200700741 1 20070425 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 570-592 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - RIGHT OUTBOARD SEAT TRACK NR 20 HAS CORROSION IN CHANNEL FROM FS X570 TO X592. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007051800080 20070518 00080 NM 2007 5 18 QXEA200700739 1 20070425 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 570-644 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - LEFT OUTBOARD SEAT TRACK NR 3 HAS CORROSION IN CHANNEL AND ON TOP SURFACE BETWEEN STATION 570.0 AND 644.5. REP AIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007051800081 20070518 00081 NM 2007 5 18 QXEA200700740 1 20070425 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 665-668 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - LEFT OUTBOARD SEAT TRACK NR 3 HAS CORROSION IN CHANNEL AND ON TOP SURFACE BETWEEN STATION 665.0 AND 668.0. REP AIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007052100001 20070521 00001 WP 2007 5 21 IXXA07SMN144S 1 20070421 A 5210 HOOK DOUG DC8 DC871F 302199D WP PAX DOOR CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND EXTERIOR FUSELAGE AT NOSE SECTION FORWARD PAX DOOR HOLD OPEN HOOK, WAS CRACKED AT STATION 15.000 LONGERON 16 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM THE REPAIR. REMOVED DAMAGED AREA. PERFORM ED INSPECTION NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED EXTERNAL AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACE. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW FA A FORM 8110-3 NUMBER 07187 DATED 05-03-07, AND SEMAN DRAWING NUMBER ED-4522 DATED 04-20-07, DC8 SRM 51-1-21, 51-3-0, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, 51-3-0, 51-1-20D, AND 51-3-1. 2 L 7 4 4F RT 4A25 2007052100003 20070521 00003 NM 2007 5 21 07FDEA01781 1 20070514 A 5712 RIB BOEING 727 727233 138408A NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 221FE 20932 RT WINGS, RIB AT BL 70-5 FASTENER INSP DURING "B" CHECK CRACK INDICATION WITNESSED BETWEEN BOTH HOLES AND BEYOND. HOLES SHOWN ON FIGURE 1 OF EO 7-5710-7-2308 PT1R. REPAIRED IAW EO 7-5710-7-2308 PT1 AND PT2 AND EA 7-5710-102035 REF WRI 57- 10/0313. 2 L 7 3 4F RT A3WE 2007052100006 20070521 00006 EU 2007 5 21 07FDEA01785 1 20070515 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSLEAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 401FE 191 2 AREAS OF CORROSION EXIST AT MDCC SEAT TRACK L-4 FRAME 37 DEFECTED AREA MEASURES 2 SQ INCHES. REMOVED CORROSION IAW A3 10 SRM51-74-10 OUT OF LIMITS IAW A310 SRM53-10-16. REPLACED SEAT TRACK IAW A310 SRM51-72-10. 2 L 7 2 4F RT A35EU 2007052100007 20070521 00007 EU 2007 5 21 07FDEA01786 1 20070515 A 5340 ATTACH ANGLE AIRBUS 310 A310203 3930313 EU FUSLEAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 401FE 191 BULK CARGO COMPARTMENT FRAME 67 3 ATTACHED ANGLES HAS HEAVY CORROSION NOTED UPON REMOVAL FROM BEAM AT FRAME 67 ON N005 07 VERIFIED MAT ID AS DAN331-3.1534T3511-01 PO NR 05-061648 IAW A310 SRM53-17-15. FABRICATED 3 ANGLES IAW A310 SRM 51-4 0-44 AND 51-72-10. TREATED 3 ANGLES IAW A310 SRM 51-21-10. PRIMED 3 ANGLES IAW A310 SRM51-75-10. INSTALLED 3 ANGLES I AW A310 SRM 51-40-21. REPRODUCED IAW A310 SRM 51-75-10. 2 L 7 2 4F RT A35EU 2007052100010 20070521 00010 WP 2007 5 21 IXXA07SMN147S 1 20070421 A 5522 SKIN DOUG DC8 DC871F 302199D WP LT ELEVATOR DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR. UPPER SKIN DENT WITH CRACK AT STATION XE 156.468 AND STATION XE 161.375. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND INTERNAL REPAIR PARTS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PART AN D NEW FASTENERS. PERFORMED BALANCED FOUND WITHIN MOMENT 1443.36 IN LBS IAW DC8 SRM 55-2-1 FIGURE 8 TR NUMBER 55-1 DATED 11-03-00, DC8 SRM 51-1-21, DC8 SRM 55-2-1 FIGURE 8 TR NUMBER 55-1 SHEET 1 AND 2, DC8 SRM 51-1-9 TR NUMBER 51-142 DATED 04-05-06, DC8 SRM 51-1-9A TR NUMBER 51-141 DATED 04-03-06, DC8 SRM 51-1-8B, AND DC8 SRM 51-4-4 PAGES 1 AND 2. 2 L 7 4 4F RT 4A25 2007052100011 20070521 00011 WP 2007 5 21 IXXA07SMN145S 1 20070421 A 5340 4610355 FITTING DOUG DC8 DC871F 302199D WP ZONE 100 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND BATH TUB FITTING CORRODED, BETWEEN STATION 70.000 AND STATION 80.000 LONGERON 35 RIGHT. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. CLEANED TREATED AND PRIMED AREA. INSTALL ED NEW FITTING IAW DC8 SRM 51-1-8 PAGES 17 AND 18, DC8 SRM 53-2-0 PAGES 2P, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 5 1-1-8B, AND 51-3-1. 2 L 7 4 4F RT 4A25 2007052100013 20070521 00013 NM 2007 5 21 07FDEA01764 1 20070511 A 5753 6521630188 SKIN BOEING 727 7272S2F 1384O81 NM ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 RT FOREFLAP I/B END LOWER SURFACE AND EDGE ARE DELAMINATED REPAIRED DELAMINATION ON I/B END LOWER SURFACE OF FOREFLAP RE F SRM51-40-20. TAP TEST GOOD, PRIMED AND PAINTED REPAIR AREA REF M/M 51-40-20-151-7 COOK TICKET ATTACHED. 2 L 7 3 4F A3WE 2007052100014 20070521 00014 NM 2007 5 21 07FDEA01765 1 20070512 A 5755 65413331 RIB BOEING 727 7272S2F 1384O81 NM NR 7 SPOILER GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 NR 7 SPOILER INBOARD DOWN STOP BRACKET HAS LOOSE LOWER BOLT AND BRACKET IS GOUGED AT ATTACH BOLT BLENDED DAMAGED AREA, N DT FOR MATERIAL LOSS. ORIGINAL THICKNESS.215", MATERIAL REMAINING IS .081 REF SRM 57-20-1 FIG 2. FOUND TO BE OUT OF LI MITS, REF SRM 57-20-1 FIG 2. REMOVED AND REPLACED DOWN STOP BRACKET REF SRM 51-30-2 PG 2. 2 L 7 3 4F A3WE 2007052100015 20070521 00015 NM 2007 5 21 07FDEA01766 1 20070512 A 5712 RIB BOEING 727 727233 138408A NM RT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 221FE 54766 20932 COMPLY WITH E.A. 7-5710-110741-WING (AD 90-06-09:94- 87-08;98-11-03) RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS. COMPL IED WITH EA 7-5710-110741 WING (AD90-06-09-94-0 7-08, 98-11-03) RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS. COMPLIED W ITH EA 5710-110741 WING AD 90-06-09, 94-07-08,98-11-03 RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS. 2 L 7 3 4F RT A3WE 2007052100016 20070521 00016 WP 2007 5 21 07FDEA01767 1 20070513 A 3230 CYLINDER DOUG DC10 DC1030 3023501 WP MLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 317FE 46835 DURING LAX "B" CHECK VISIT WO 36669; FOUND CENTER GEAR RETRACT CYLINDER CRACKED AT ROD END. [SUP 05-30-07] REMOVED AND REPLACED CENTER GEAR RETRACT CYLINDER PER MM 32-38-01-2. INSTALLED NEW CLG ROD END CLEVIS ON RETRACT ACTUATOR PER MM 3 2-38-01-2. 2 L 7 3 4F A22WE 2007052100018 20070521 00018 NM 2007 5 21 DHL2007788519 1 20070417 A 5410 NOSE COWL BOEING 727 727214 138407R NM NR 1 NACELLE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 NR 1 ENG NOSE COWL 7:30 POS AFT EDGE SKIN IS WORN AND CRACKED. CUTOUT DAMAGED AREA (3.50" BY .90"). FABRICATED REPAIR DOUBLER 2024T3 .050 PO 9004690 (11.25" BY 3.50") AND FILLER 2024T3 .040 PO NR 9004779 (3.50" BY .90") IAW B727 SRM 54-30 -3 FIG 8. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 54-30-3 FIG 8 AND 54-10-2 FIG 1. 2 L 7 3 4F A3WE 2007052100022 20070521 00022 NM 2007 5 21 QXEA200700790 1 20070509 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 331 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - CORROSION IN CENTER CHANNEL OF LEFT OUTBOARD SEAT TRACK NR 2 AT STATION 331.0. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007052100024 20070521 00024 NM 2007 5 21 QXEA200700797 1 20070509 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - FO'S OUTBOARD SEAT TRACK HAS GROVES FROM ROLLER CONTACT AT ALL POSITINS WHERE THE SEAT HAS BEEN LATCHED. REPAI RED IAW SRM 53-10-49. 2 H 7 2 4T RT A13NM 2007052100027 20070521 00027 NM 2007 5 21 QXEA200700789 1 20070509 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 165 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - CORROSION ON INBOARD FLANGE OF LEFT CENTER SEAT TRACK NR 6 AT STATION 165.0. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007052100028 20070521 00028 NM 2007 5 21 QXEA200700791 1 20070509 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 388 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - CORROSION IN CENTER CHANNEL OF LEFT SEAT TRACK NR 2 AT STATION 388.0. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007052100029 20070521 00029 NM 2007 5 21 QXEA200700792 1 20070508 A 5410 DIAPHRAGM BOMBDR DHC8 DHC8402 1390042 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - RIGHT NACELLE DIAPHRAGM CRACKED. REPAIRED IAW SRM 51-40-15, 51-42-05, 51-21-10,51-40-35. 2 H 7 2 4T RT A13NM 2007052100030 20070521 00030 NM 2007 5 21 QXEA200700793 1 20070509 A 5310 THRESHOLD BOMBDR DHC8 DHC8402 1390042 NM PAX DOORWAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - MAIN CABIN DOOR THRESHOLD ENTRY FLOOR FLANGE IS CORRODED ON THE TOP AND BOTTOM SURFACES. REPAIRED IAW SRM 51-2 1-00, 51-40-07, AND RD8/4-53-1660. 2 H 7 2 4T RT A13NM 2007052100033 20070521 00033 NM 2007 5 21 QXEA200700726 1 20070506 A 7720 8209601 SENSOR BOMBDR DHC8 DHC8402 1390042 NM COMPRESSOR MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 423QX 4153 PDX FLIGHT NR 2541: CABIN PACK HOT LIGHT ILLUMINATED WITH APU BLEED ON. PACK HOT LIGHT EXTINGUISHES WITH PACK SELECTED OFF. AIRCRAFT RETURNED TO GATE. MAINTENANCE, AS PRECAUTIONARY MEASURE, REMOVED AND REPLACED RT COMPRESSOR OUTLET TEMP SENSOR IAW Q400 AMM TASK 21-51-91-000-801 AND 21-51-91-400. RAN APU FOR 10 MINUTES. SELECTED APU BLEED ON. CHECKED CD S FOR FAULTS. NO FAULTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007052100036 20070521 00036 EU 2007 5 21 07FDEA01779 1 20070512 A 7897 CONNECTOR AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF6* 30020 GL THRUST REVERSER LOOSE A FDEA A UNSCHED LANDING W N INADEQUATE Q C FALSE WARNING CL CLIMB 1 SO 25 655FE 742 705279 NR 2 ENGINE THRUST REVERSER DEACTIVATED DUE TO MEL OF NR 2 ENGINE HP VALVE (MEL 36-11-03). MEM MX FAILED TO SECURE ALL CONNECTORS PER MEL 78-30-01-A. MX SECURED ALL C/P'S PER MEL AND FLT CONTINUED. 2 L 7 2 4F 4 F RT A35EU E23EA 2007052100037 20070521 00037 WP 2007 5 21 IXXA07SMN158S 1 20070421 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1260 L34R CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT FRAME WITH A CRACK AT STATION 1260.000 LONGERON 34 RIGHT TO LONGERON 35 LEFT. REMOVED CRACKED FITTING. FABRICATED FRAME FITTING, SPLICES, AND DOUBLER. PERFORMED HEAT TREATMEN T. PERFORMED NDT INSPECTION NO CRACK OR CORROSION FOUND. TRIMMED OUT NEW FRAME FITTING TO FACILITATE INSTALLATION. CL EANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0 FIGURE 8 SHEET 2, 5, 6, AND 8, DC8 SRM 51-1-8 PAGES 17 AND18, DC8 SRM 53-2-0 PAGE 2P, DC8 SRM 53-2-0 FIGURE 8 SHEET 2 AND 6, DC8 SRM 51-1-20D, ATI R EPAIR SPECIFICATION NUMBER 2003-05, DOUGLAS DRAWING NUMBER 3646956,DC8 SRM 51-1-1 PAGES 1, 13 AND 17, NDT SPM PART 08-00 2 L 7 4 4F RT 4A25 2007052100038 20070521 00038 NM 2007 5 21 DHL2007788517 1 20070509 A 5753 SKIN BOEING 727 727214 138407R NM RT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 RT IB AFT FLAP IS CRACKED 3 PLACES. CUT OUT 3 CRACKED AREAS ON RT IB AFT FLAP UPPER SKIN (1) 1.2" DIA. (2) 1" DIA (3) 1 .8" DIA. CUTOUT 2 DELAMINATED AREAS ON LOWER SKIN (1) 8" BY 8" (2) 8 1/2" BY 23". FABRICATED UPPER DOUBLERS (1) 4.2" D IA (2) 4" DIA. (3) 4.8" DIA. FABRICATED LOWER FILLER (1) 8" BY 8" (2) 8 1/2" BY 23" AND DOUBLER (1) 11" BY 11" (2) 10 1 /2" BY 26" FROM 7075T6 PO# 9003142. CLEANED, PREPPED, PRIMED, BONDED, CLEANED, TREATED, PRIMED, AND SEALED EDGES IAW B7 27 SRM 57-50-2 FIG 3, 51-40-22 FIG 3, AND 51-10-24 FIG 1. 2 L 7 3 4F A3WE 2007052100039 20070521 00039 NM 2007 5 21 DHL2007788518 1 20070417 A 5410 SKIN BOEING 727 727214 138407R NM NR 1 NOSE COWL DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 NR 1 ENG NOSE COWL 9:00 POSITION AFT EDGE SKIN IS BROKEN OUT. CUTOUT DAMAGED AREA (3.50" BY .90"). FABRICATED REPAIR D OUBLER 2024T3 .050 PO NR 9004690 (8.25" BY 2.65") AND FILLER 2024T3 .040 PO NR 9004779 (3.50" BY .90") IAW B727 SRM 54-3 0-3 FIG 8. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 54-30-3 FIG 8 AND 54-10- 2 FIG 1. 2 L 7 3 4F A3WE 2007052100042 20070521 00042 NM 2007 5 21 AWXA200700611 1 20070417 A 5755 654645165A SKIN BOEING 737 73733A 1384673 NM ZONE 600 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - RIGHT WING NR 6 SPOILER UPPER SURFACE CRACKED, WS 318. REPAIRED RIGHT WING NR 6 SPOILER UPPER SURFACE, WS 318 IAW B737-300 SRM 51-70-10-2R4, FIGURE 201. 2 L 7 2 4F RT A16WE 2007052100043 20070521 00043 NM 2007 5 21 AWXA200700612 1 20070417 A 5755 654645168SP SKIN BOEING 737 73733A 1384673 NM ZONE 500 DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - LEFT WING NR 3 SPOILER UPPER SURFACE DEBONDED, WS 290.070 - WS 295.370. REPAIRED LEFT WING NR 3 SPOILER UPPER SUR FACE, WS 290.070 - WS 295.370 IAW B737-300 SRM 51-70-10-2R4, FIGURE 202. 2 L 7 2 4F RT A16WE 2007052100047 20070521 00047 NM 2007 5 21 AWXA200700617 1 20070410 A 5711 6545324 SPAR BOEING 737 73733A 1384673 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - MAJOR REPAIR - LEFT WING REAR SPAR UPPER CHORD CRACKED, RSS 221. REPAIRED LEFT WING REAR SPAR UPPER CHORD, RSS 22 1 IAW AWA ER 03-5722-07128-SS1. 2 L 7 2 4F RT A16WE 2007052100048 20070521 00048 NM 2007 5 21 AWXA200700618 1 20070410 A 5753 65C263201 SPAR BOEING 737 73733A 1384673 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - LEFT WING MID FLAP REAR SPAR UPPER CHORD CRACKED, WBL 202 - WBL 205. REPAIRED LEFT WING MID FLAP REAR SPAR UPPER CHORD, WBL 202 - WBL 205 IAW AWA ER 03-5754-07131-ES1. 2 L 7 2 4F RT A16WE 2007052100049 20070521 00049 NM 2007 5 21 AWXA200700619 1 20070411 A 5311 6546541 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - FOUND CRACKED FRAME, BS 663.75, S2R. REPAIRED FRAME, BS 663.75, S2R IAW AWA ER 03-5332-07128-SS2. 2 L 7 2 4F RT A16WE 2007052100050 20070521 00050 NM 2007 5 21 AWXA200700620 1 20070411 A 5330 654576913 SKIN BOEING 737 73733A 1384673 NM ZONE 100 BULGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - FUSELAGE SKIN INNER TRIPLER BULGING AND HAS MOISTURE UNDERNEATH IT, BS 360 - BS 380, S26L - S27R. REPLACED FUSELA GE SKIN INNER TRIPLER BS 360 - BS 380, S26L - S27R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007052100052 20070521 00052 NE 2007 5 21 HALA0700205 2 20070510 A 7200 UNKNOWN BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE LT ENGINE UNKNOWN A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 480HA 55125 BTB: ENG L SYS FAIL LIGHT CAME ON DURING START. INTERMITTANT FAULT START CIRCUIT (FUEL SW CIRCUIT) ERASED FAULT. PERFO RMED EEC 1 RTS TEST PASSED. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007052100053 20070521 00053 NM 2007 5 21 HALA0700207 1 20070510 A 3350 LIGHT BOEING 767 767300 1385204 NM CABIN INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 580HA 28140 FC RT SIDE AISLE FLOOR AND CROSSOVER AISLE FLOOR LTS INOP EMERGENCY LIGHTS. REPLACED POWER STRIPS FOR AISLE FLOOR LT 90 1, ALL OP NML. 2 L 7 2 4F RT A1NM 2007052100054 20070521 00054 NM 2007 5 21 HALA0700208 1 20070511 A 2410 RELAY BOEING 767 76733A 1385209 NM IDG MALFUNCTIONED A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, R IDG VALVE STATUS MSG. TROUBLESHOT SYSTEM PER FIM 24-20-00 FIG 101 BLOCK 1, ALL TESTS CHECK GOOD. REPLACED K1032 RELAY, OPS CHECKS NORMAL. 2 L 7 2 4F RT A1NM 2007052100055 20070521 00055 NM 2007 5 21 HALA0700209 1 20070513 A 2140 FILTER BOEING 767 767300 1385204 NM TEMP SENSOR DIRTY A HALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, AIRCRAFT EXTREMELY HOT AT FULL COLD SETTING FOR PACKS WHILE ON GROUND DUCT PRESSURE IS 30 PSI SUSPECT PACKS AT OR PLUMBING SYSTEM GOOD AIRBORNE. T/S PER FIM 21-60-00, FOUND CABIN ZONE TEMP SENSOR FILTERS DIRTY CLE ANED SAME, NO FAULTS ON ZONE TEMP CONTROLLER SYSTEM. OPS NORMAL 2 L 7 2 4F RT A1NM 2007052100056 20070521 00056 NM 2007 5 21 AWXA200700621 1 20070407 A 5311 654580761 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - FOUND CRACKED R1 DOOR CUTOUT FWD STUB FRAME, BS 312, S16R. REPLACED R1 DOOR CUTOUT FWD STUB FRAME, BS 312, S16R I AW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007052100057 20070521 00057 NM 2007 5 21 QXEA200700747 1 20070425 A 5340 BRACKET BOMBDR DHC8 DHC8402 1390042 NM BS 728 S20R CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - AFT CARGO COMPARTMENT ON RIGHT SIDE BRACKET CRACKED AT STATION 728 AND STRINGER 20. REPAIRED IAW SRM 51-42-05 AND 51-42-00 AND EA6-53-813. 2 H 7 2 4T RT A13NM 2007052100058 20070521 00058 NM 2007 5 21 QXEA200700746 1 20070426 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - PERMANENT REPAIR FOR DENTS IN SKIN PANEL 85313525. REPAIRED IAW RD8/4-53-1797 AND RD8/4-53-1815. 2 H 7 2 4T RT A13NM 2007052100060 20070521 00060 NM 2007 5 21 QXEA200700752 1 20070426 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - RIGHT OUTBOARD SEAT TRACK NR 17 HAS CORROSION IN CHANNEL AND ON TOP OF TRACK FROM FS X32 TO X73. REPAIRED IAW RD8/4-53-884 AND SRM 51-42-05, 51-40-15. 2 H 7 2 4T RT A13NM 2007052100061 20070521 00061 NM 2007 5 21 QXEA200700743 1 20070425 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 649-669 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - RIGHT OUTBOARD SEAT TRACK NR 20 HAS CORROSION IN CHANNEL FROM FS X649 TO X669. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007052100062 20070521 00062 NM 2007 5 21 QXEA200700744 1 20070424 A 5330 PANEL BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - LAV SERVICE PANEL APERTURE IS CHAFED AFT CENTER AREA. REPAIRED IAW RD8/4-53-347 AND SRM 51-14-00. 2 H 7 2 4T RT A13NM 2007052100064 20070521 00064 NM 2007 5 21 QXEA200700748 1 20070424 A 5320 FLOOR SUPPORT BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - AFT CARGO COMPARTMENT FLOOR STRUCTURE AROUND FASTENER HOLES HAS CORROSION AT ACCESS 144JZ. REPAIRED IAW SRM 51 -21-00, 51-21-10, 51-25-10, AND 51-14-00. 2 H 7 2 4T RT A13NM 2007052100067 20070521 00067 NM 2007 5 21 HALA0700203 1 20070508 A 2420 GCU BOEING 767 767332 1382001 NM LEFT MALFUNCTIONED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 594HA 23275 ATB-EICAS MSG, LT GEN OFF DISPLAYED LT GEN OFF LIGHT ILLUMINATED. GENERATOR SWITCH RESET DID NOT CORRECT CONDITION. AC COMPLISHED BIT IAW 24-20-00 BPCU FAULTED IDG OUT BULB WIRING AND DP TRIP/MAIN BUSS OVERLAP ZONE. REMOVED AND REPLACED L EFT GCU. IDG OUT MSG CLEARED BUT CONDITION SAME. REPLACED BPCU AND TIE BREAKER C902, NO HELP. REINSTALLED ORIGINAL UN IT AND TIE BREAKER. REMOVED AND REPLACED LT IDG IAW DL AMM 24-11-01 AND CONNECTOR D414. OPS CK NML. 2 L 7 2 4F RT A1NM 2007052100068 20070521 00068 NM 2007 5 21 DHL2007788515 1 20070429 A 5310 DOOR FRAME BOEING 727 727214 138407R NM CARGO DOORWAY CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 C2 DOOR CUTOUT AFT FRAME INNER CHORD IS CHORDED WITH EXFOLIATION BETWEEN STR 25R-26R. CUTOUT DAMAGED AREA IAW AD39-53-1 01 IR. FABRICATED NEW STRAP, FILLER, AND TWO ANGLES IAW DWG AD39-53-101IR. TREATED AND PRIMED ALL REPAIR PARTS AND ARE A IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW DWG AD39-53-101IR. 2 L 7 3 4F A3WE 2007052100070 20070521 00070 NM 2007 5 21 AWXA200700632 1 20070504 A 5311 654795946 FRAME BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - MAJOR REPAIR - AFT CARGO COMPARTMENT DOOR CUT OUT FORWARD FRAME CRACKED, BS 794, S22R - S26R. REPAIRED AFT CARGO COMPARTMENT DOOR CUT OUT FORWARD FRAME CRACKED, BS 794, S22R - S26R IAW AWA ER 03-5361-07130-ES2. 2 L 7 2 4F RT A16WE 2007052100071 20070521 00071 NM 2007 5 21 DHL2007788521 1 20070417 A 5512 PANEL BOEING 727 727214 138407R NM HORIZONTAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 VERTICAL LE PANEL NR 9502 LOWER INTERIOR PANEL BENT AND CRACKED. REMOVED PREVIOUS REPAIR ON PANEL NR 9502 IAW B727 SRM 51-30-2. FABRICATED REPAIR DOUBLER 7075T6 .025 (16.5" BY 8.5") PO NR 9004219 IAW B727 SRM 55-30-2 FIG 2 AND 51-40-2 FIG 1. TREATED AND PRIMED PART IAW B727 SRM 51-10-2. INSTALLED IAW B727 SRM 51-30-2 AND 51-40-2. 2 L 7 3 4F A3WE 2007052100076 20070521 00076 NM 2007 5 21 UPS07649799 1 20070514 A 7930 OIL SYSTEM BOEING 767 76734AF 1385212 NM NR 1 ENGINE LOW PRESSURE A IPXA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 01 322UP 27748 INSPECTION TYPE:ETOP DIVERSION - TAT 27,083, TAC 8418, TET 28,050 , TEC 8775 TSESV1 186:36 IFSD NR 1 ENGINE LOST OIL PR ESSURE BELOW RED LINE LIMIT. ACCOMPLISHED ENG FAILURE/SHUTDOWN. DIVERTED TO KIX. SECURED LOOSE B-NUT AT OIL PUMP DISC HARGE LINE. PERFORMED NO OIL PRESSURE INSPECTION PER MM 77-00-00-6, NO METAL FOUND. SERVICED ENGINE OIL & ENGINE RUN, ALL PARAMETERS NORMAL. A/C OK TO CONTINUE. 2 L 7 2 4F RT A1NM 2007052100077 20070521 00077 NM 2007 5 21 UPS07649802 1 20070513 A 3350 8200008704 SIGN BOEING 767 76734AF 1385212 NM EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 305UP 27243 INSPECTION TYPE:PS DURING PERIODIC SERVICE CHECK, FOUND EMERGENCY LIGHT L312 AT INOP. DETERMINED WIRES CRIMPED BETWEEN STRUCTURE AND LIGHT ASSY. LIGHT ASSY WAS ALSO UNSERVICEABLE. SHORTED PWR WIRE BLEW LOAD FUSE IN BATTERY PACK/CHARGER. REPLACED BATTERY PACK/CHARGER AND L312 LIGHT ASSY. REPAIR DAMAGED WIRING TO LIGHT. EMERGENCY LIGHT CHECKED NORMAL AFT ER CORRECTIVE ACTION. 2 L 7 2 4F RT A1NM 2007052100079 20070521 00079 WP 2007 5 21 UPS07849803 1 20070420 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 HFEC & VISUAL INSPECTION DETECTED A CRACK ON THE C-4 (D-PIT) UPPER FWD DOOR JAMB CORNER. CRACK RUNS FROM FASTENER HOLE TO EDGE OF CUTOUT. REMOVED EXISTING DOUBLER. CUT OUT DAMAGE. FABRICATED AND INSTALLED DOUBLER, TRI PLER AND FILLER. REAMED DISCREPANT FASTENER HOLES IAW SRM 53 53-02-0 FIG 21 AND SAA EA 008-5330-01-A0827. 2 L 7 4 4F RT 4A25 2007052100081 20070521 00081 WP 2007 5 21 UPS07849808 1 20070423 A 5330 SKIN DOUG DC8 DC873F 302199F WP FS 310 L2R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 FUSELAGE EXTERIOR SKIN CORRODED AT FS 310 L2R. CUT OUT DAMAGED AREA AT STA 310 L2R IAW SRM 53-02-01 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER, FINGER DOUBLER, AND FILLER AT STA 310 L2R IAW SRM 53-02-01 FIG 7. 2 L 7 4 4F RT 4A25 2007052100082 20070521 00082 WP 2007 5 21 UPS07849809 1 20070421 A 5330 SKIN DOUG DC8 DC873F 302199F WP FS 520 L31R GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 FUSELAGE EXTERIOR EXISTING REPAIR DOUBLER HAS DEEP GOUGE AND FASTENER HEADS MISSING AT STA 520 L31R. REMOVED DAMAGED DOUBLER AND CUT OUT AREA AT STA 520 L31R IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLERS AT STA 520 L31R IAW SAA EA 008-5330-01-A0847, UPS RAA DC8-53-20626, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007051600183 20070516 00183 EA 2007 5 16 SWIA200718221 1 20070405 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 979SW 7954 PAX DOOR FORWARD WEB IS CRACKED UNDER HANDRAIL DOWNSTOP BRACKET, DISCOVERED AT C-CHECK. REPLACED PARTS ON FORWARD WEB O F PAX DOOR PER CRJ200 REO 601R-52-11-702 (REV A). 2 L 7 2 4F RT A21EA 2007051600186 20070516 00186 EA 2007 5 16 SWIA200718224 1 20070511 A 3520 OXYGEN MASK CNDAIR CL600 CL6002C10 1390015 EA LAVATORY UNWANTED DEPLOY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 340CA 10062 FORWARD LAV 02 MASK WAS FOUND DEPLOYED. RESTOWED 02 MASKS IN FORWARD LAV. 2 L 7 2 4F RT A21EA 2007051600187 20070516 00187 NM 2007 5 16 AALA20070806 1 20070504 A 3610 HEAT EXCHANGER BOEING 767 767323 1385205 NM LEFT CRACKED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 383AN 26995 DFW INFLIGHT T963/04MAY - AT CRUISE LEFT BLEED DUCT OVERHEAT INDICATIONS. RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. RESEATED DUCT LEAK CONTROL CARD AND REPLACED CRACKED LEFT HEAT EXCHANGER. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A1NM 2007051700007 20070517 00007 WP 2007 5 17 AALA20070814 1 20070505 A 3397 WIRE HARNESS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7512A 49806 DFW - EMERGENCY LIGHT AT OVERHEAD STATION 1400 HAS QUICK DISCONNECT DISCONNECTED. RECONNECTED QUICK DISCONNECT FOR EMER GENCY LIGHT AT OVERHEAD STATION 1400. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051700008 20070517 00008 NM 2007 5 17 AALA20070791 1 20070501 A 2421 STATOR BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE ALTERNATOR INOPERATIVE A AALA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 21 703TW 27620 727207 GEG INFLIGHT T1092/01MAY - LEFT ENGINE AUTO FLAMEOUT DURING CLIMB. RESTART UNSUCCESSFUL. LANDED GEG WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE ELECTRIC ENGINE CONTROL ALTERNATOR STATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007051700009 20070517 00009 WP 2007 5 17 AALA20070793 1 20070501 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 484AA 49677 SFO - EMERGENCY FLOOR LIGHT AT RIGHT SIDE OF CABIN INOPERATIVE. RELAMPED EMERGENCY FLOOR LIGHT AT RIGHT SIDE OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051700011 20070517 00011 2007 5 17 AALA20070794 2 20070502 A 7310 FILTER BOEING 767 767323 1385205 NM RT ENGINE INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 344AN 33083 MIA INFLIGHT T1647/2MAY - RIGHT ENGINE FUEL FILTER CLOG LIGHT ILLUMINATED DURING CLIMB. RETURNED TO MIA AND LANDED WITH OUT INCIDENT. REPLACED RIGHT ENGINE FUEL FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007051700014 20070517 00014 NM 2007 5 17 AALA20070798 1 20070503 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7375A 25202 SFO- EMERGENCY LIGHT AT MID GALLEY RIGHT SIDEWALL MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT MID GALLEY RIGHT S IDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007051700020 20070517 00020 2007 5 17 AALA20070803 4 20070404 A 2565 SLIDE DOUG DC9 DC982 3022082 WP GALLEY DOOR LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 MEX - EMERGENCY SLIDE AT AFT GALLEY DOOR LOOSE. REPOSITIONED EMERGENCY SLIDE AT AFT GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051700031 20070517 00031 NM 2007 5 17 AALA20070784 1 20070429 A 2560 STRAP BOEING 767 767323 1385205 NM FLASHLIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 392AN 29429 MIA - EMERGENCY FLASHLIGHT BREAK STRAP SEAL AT RIGHT BUSINESS CLASS GALLEY BROKEN. REPLACED STRAP FOR EMERGENCY FLASHLI GHT BREAK STRAP SEAL AT RIGHT BUSINESS CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007051700044 20070517 00044 NM 2007 5 17 AWXA200700626 1 20070511 A 3510 38001606 HOSE BOEING 757 7572S7 1384962 NM CREW O2 SYSTEM RUPTURED A AWXA A UNSCHED LANDING O OTHER DE DESCENT 1 WP 28 902AW 23322 LAX - DIV - FLIGHT NR 432 DIVERTED TO LAX DUE TO CREW O2 SYSTEM DEPLETED. FLIGHT CREW DECLARED AN EMERGENCY DUE TO THE INABILITY TO MAINTAIN RVSM ALTITUDE BUT AFTER THE AIRCRAFT WAS OUT OF THE RVSM THE CAPTAIN DEEMED THE SITUATION A NON-EM ERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT AND MAINTENANCE REPLACED A RUPTURED O2 LINE BELOW THE O2 MASK STORAGE BO X IAW AWA TASK CARD R1B35601. 2 L 7 2 4F RT A2NM 2007051700054 20070517 00054 NM 2007 5 17 2007UALA01477 1 20070511 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY EXIT SILL LIGHTS BOTH FWD AND AFT INOPERATIVE AT DOOR 5L. [SUP 06-06-07] REPLACED BATTERY PACK . OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007051700056 20070517 00056 NM 2007 5 17 2007UALA01479 1 20070511 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 OVERWING EXTERIOR EMERGENCY EXIT LIGHTS INOP, RIGHT SIDE 2 AFT LIGHT ASSEMBLIES. [SUP 06-06-07] REPLACED BATTERY PACK. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007051700057 20070517 00057 NM 2007 5 17 2007UALA01480 1 20070511 A 5730 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT WING CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 LEFT UPPER WING SKIN CORRODED AT MID SPAR C-T FUSELAGE. [SUP 06-06-07] PERFORMED DETAILED VISUAL INSPECTION OF THE LT FWD TRUNNION FUSE PINS FOR LOOSE FUSE PINS AND CORROSION ON ADJACENT STRUCTURE. WORK ACCOMPLISHED PER UA ENGINEERING EV ALUATION AND RECOMMENDED REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007051700062 20070517 00062 2007 5 17 2007UALA01123 4 20070410 A 2565 C179363 DISK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE BOTTLE RUPTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 LOW BOTTLE PRESSURE. *S/D* RUPTURE DISK FAILURE. CAUSE UNKNOWN. REPLACED RUPTURE DISK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007051700079 20070517 00079 NM 2007 5 17 2007UALA01424 1 20070505 A 3350 9F19948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 51R INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 51 RIGHT. REPLACED LIGHT ASSY, OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007051700092 20070517 00092 NM 2007 5 17 AWXA200700592 1 20070506 A 5315 D53472190211 FLOORBEAM AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 832AW 1643 SAL - CORROSION ON CABIN FLOORBEAM, FR 65 + 22", -Y1292. REPLACED CABIN FLOORBEAM, FR 64 - FR 66, -Y1292 IAW A319 SRM 5 1-72-11. 2 L 7 2 4F RT A28NM 2007051700097 20070517 00097 NM 2007 5 17 AWXA200700597 1 20070509 A 5347 D531114142000 SEAT TRACK AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 832AW 1643 SAL - MAJOR REPAIR - CORROSION ON CABIN SEAT TRACK, FR 21, -Y189. REPLACED CABIN SEAT TRACK, FR 21, -Y189 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007051700099 20070517 00099 NM 2007 5 17 AWXA200700599 1 20070509 A 5322 D53471124200 SHEAR PLATE AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 832AW 1643 SAL - MAJOR REPAIR - CORROSION ON CABIN SHEAR PLATE, FR 69 - FR 70, +Y1732. REPLACED CABIN SHEAR PLATE, FR 69 - FR 70, +Y1732 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007051700111 20070517 00111 NM 2007 5 17 2007UALA01443 1 20070507 A 5330 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE BS 247 S1L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 793UA 26946 UPPER FUSELAGE SKIN AT STA 247 STR 1L LBL 4 IS DAMAGED. MAJOR REPAIR ACCOMPLISHED: INSTALLED TRIPLER REPAIR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007051700144 20070517 00144 NM 2007 5 17 2007UALA01460 1 20070509 A 3350 3071BPEGPL LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 776UA 26937 SEATS 18C, 19C, 19G, 22G, 32G & 39G EEL LIGHTS ARE INOPERATIVE. RELAMPED EEL LIGHTS. OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007051700149 20070517 00149 2007 5 17 2007UALA01466 4 20070510 A 2565 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 577UA 26693 EMERGENCY ESCAPE LIGHT REMAINED EXTINGUISHED DURING SLIDE SQUIB TEST 2 ON SIDE 5 (05=L, 06=R). [SUP 06-06-07] FOUND LEFT OVERWING EVAC SLIDE BOTTLE PRESS LOW. ACCOMPLISHED A ONE TIME RECHARGE. SQUIB TEST OK. CYLINDER REPLACED AT FIRST M AINT STATION WHERE PARTS WERE AVAILABLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007051700157 20070517 00157 NM 2007 5 17 AWXA200700605 1 20070507 A 3350 30043211 LIGHT BOEING 737 73733A 1384673 NM ZONE 200 INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 166AW 23627 MCN - EEL - C-20 CHECK - L2 DOOR SLIDE LIGHT IS INOPERATIVE. REPLACED AND OPERATIONAL CHECKED THE L2 DOOR SLIDE LIGHT A SSEMBLY IAW B737-300 AMM 33-51-02. 2 L 7 2 4F RT A16WE 2007051700167 20070517 00167 EU 2007 5 17 07FDEA01760 1 20070511 A 3097 WIRE AIRBUS 310 A310203 3930313 EU WINDOW HEAT SHORTED A FDEA H DEACTIVATE SYST/CIRCUITS A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 415FE 349 CAPT WINDOW HEAT SIDE SLIDING WINDOW WIRING SHORTED OUT AND MOMENTARY CAUGHT FIRE PULLED ASSOCIATED CB H86. WIRING CAPP ED AND STOWED AND ASSOCIATED ITEMS, SLIDING WINDOW HEAT, SEVERAL LIGHTS ON THE CAPT'S SIDE PLACED ON MEL. 2 L 7 2 4F RT A35EU 2007051800003 20070518 00003 NM 2007 5 18 QXEA200700754 1 20070428 A 5320 THRESHOLD BOMBDR DHC8 DHC8402 1390042 NM FUSLEAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - UPPER SURFACE OF MAIN CABIN DOOR THRESHOLD HAS CORROSION IN SEVERAL PLACES. REPAIRED IAW SRM 51-21-00, 51-42-0 5. 2 H 7 2 4T RT A13NM 2007051800010 20070518 00010 NM 2007 5 18 QXEA200700758 1 20070429 A 5415 FITTING BOMBDR DHC8 DHC8402 1390042 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - LEFT NACELLE OUTBOARD SHOULDER FITTING IS CRACKED LOCATED AT UPPER OUTBOARD SECTION OF NACELLE FORMER XN210.0. REPAIRED IAW RD8/4-54-154 AND SRM 51-42-05. 2 H 7 2 4T RT A13NM 2007051800011 20070518 00011 NM 2007 5 18 QXEA200700756 1 20070429 A 5410 DIAPHRAGM BOMBDR DHC8 DHC8402 1390042 NM LT NACELLE BENT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - LEFT NACELLE OUTBOARD DIAPHRAGM WEB PLATE IS BENT AND HAS SOME BLOWN OUT HOLES. REPAIRED IAW SRM 54-30-10, 51- 21-00, 51-42-05. 2 H 7 2 4T RT A13NM 2007051800015 20070518 00015 NM 2007 5 18 QXEA200700723 1 20070507 A 2140 7786971 VALVE DHAV DHC8 DHC8202 2809007 NM TEMP TRIM MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 345PH 11031 476 SEA FLIGHT NR 2044, UPON BRINGING NR 2 ENGINE OUT OF FEATHER AFTER START, PILOTS AND FA DETECTED A BURNING ODOR. ODOR DI SIPATED AFTER 5 MINUTES. FOLLOWING THAT WE WERE UNABLE TO CONTROL THE CABIN TEMPERATURE IN AUTO OR MANUAL MODE. ATTEMP TED LATCHED TRIM/PACK VALVES CHECKLIST WITH NO SUCCESS. MAINTENANCE REPLACED TEMPERTURE TRIM VALVE IAW -8 MMM 21-60-11, PAGE 401-405. ALSO REPLACED AIR CYCLE MACHINE IAW -8 AMM 21-50-11, PAGES 41-404. FUNCTIONAL CHECK OF THE TEMP CONTRO L SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007051800027 20070518 00027 EA 2007 5 18 A6WA200740209 1 20070324 A 5310 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 416AW 7603 CARGO DOOR SUPPORT BEAM LOWER ANGLE THAT ATTACHES TO REAR PRESSURE BULKHEAD IS CRACKED .4 INCH IN LENGTH. MAINTENANCE R EMOVED AND REPLACED CARGO DOOR SUPPORT BEAM LOWER ANGLE IAW CRJ 200 SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007051800062 20070518 00062 2007 5 18 IXXA070028O 4 20070424 A 2300 G2200ATI AUDIO PANEL DOUG DC8 DC862F 3021972 WP COCKPIT DEFECTIVE A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 11 71CX 70211 199 45961 DURING FLIGHT FROM RJTY THE CREW SMELLED SMOKE, THE FIRST OFFICER'S AUDIO CIRCUIT BREAKER OPENED THE SMELL OF SMOKE STOP PED. THE CREW LANDED IN WSAP WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FIRST OFFICER'S AUDIO SELECT PANEL IAW DACO DC8 MAINTENANCE MANUAL 23-50-1. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2007051800064 20070518 00064 WP 2007 5 18 AALA20070834 1 20070510 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 464AA 49594 DFW - OVERHEAD EMERGENCY LIGHTS AT SEAT ROWS 13 TO 14 INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD SEAT ROW 13 FOR OV ERHEAD EMERGENCY LIGHTS AT SEAT ROWS 13 TO 14. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051800082 20070518 00082 NM 2007 5 18 QXEA200700742 1 20070425 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 599-626 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - RIGHT OUTBOARD SEAT TRACK NR 20 HAS CORROSION IN CHANNEL AND ON TOP FROM FS X599 TO X626. REPAIRED IAW RD8/4-5 3-884. 2 H 7 2 4T RT A13NM 2007052100005 20070521 00005 EU 2007 5 21 07FDEA01784 1 20070515 A 5310 CROSSBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 401FE 191 AFT CARGO COMPARTMENT RT SIDE FRAME 58 CROSSBEAM COMMON TO FLOOR PANELS 152CF, 152DF HAVE 2 EACH AREAS OF CORROSION TOTA L 10 SQUARE INCHES REWORKED CORROSION IAW A310 SRM 51-74-10 REMOVED AND REPLACED CROSS BEAM AND SPLICE IAW A310 SRM 51-4 0-21, 51-23-00, 51-75-10, 53-10-15, AND DWG 53974268. 2 L 7 2 4F RT A35EU 2007052100012 20070521 00012 EU 2007 5 21 07FDEA01763 1 20070511 A 2750 4907905 COMPUTER AIRBUS 310 A310222 3930315 EU TE FLAPS FAILED A FDEA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 25 455FE 331 FLAPS STUCK AT 20 DEG/20 DEG DURING EMERG CHKLIST. FIRST STUCK AT 20DEG/15DEG WITH BOTH SYS 1 AND SYS 2 LIGHT ON. CHCK D FAULT CODE ON SFCC FOUND HIGH SPEED PRESS SWITCH ON NR 1 SFCC AND MAIN CONTROL VALVE ON NR 2 SFCC. CHECKED WIRE INTEG RITY AND PHYSICAL CONDITION OF PRESS SWITCH AND MAIN CONTROL VALVE, NO DEFECT NOTED. FURTHER VISUAL INSPECTION FOUND RT TORQUE LIMITER POP-OUT AND NO ENOUGH LUBRICATION ON FLAP SCREW JACK. PROPERLY LUBRICATED AND SERVICED GEAR BOXES PER MM27-50-00-3 AND REPLACED BOTH SFCC FOR PRECATIONARY PER MM27-51-18. RAN ENGINE PER A310-JRH AND PERFORMED FLAPS OPERA TIONAL CHK SEVERAL TIMES, SATISFACTORY AND NO FAULT FOUND. 2 L 7 2 4F RT A35EU 2007052100017 20070521 00017 WP 2007 5 21 IXXA07SMN136S 1 20070421 A 5343 FITTING DOUG DC8 DC871F 302199D WP ZONE 700 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT MAIN LANDING GEAR WHEEL WELL JOINT FITTING WITH CORROSION AT STATION 940. 000 LONGERON 24 RIGHT. REMOVED CORROSION. FOUNDED OUT OF LIMITS REMOVED CORRODED FITTING. FABRICATED FRAME FITTING, S PLICES AND DOUBLER. PERFORMED HEAT TREATMENT PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. TRIMMED OUT NEW F RAME FITTING TO FACILITATE INSTALLATION. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0 FIGURE 8 SHEET 2, 5, 6, AND8, DC8 SRM 51-1-8 PAGES 17 AND 18, DC8 SRM 53-2-0 PAGE 2P, DC8 SRM 51-1-20D,D C8 SRM 51-1-1 PAGES 1, 13, AND 17,NDT SPM PART 08-00-02 TO 07,DC-8 SRM 53-2-0 FIGURE 8 SHEET 2 AND 6, DC-8 SRM 51-1-8B, 2 L 7 4 4F RT 4A25 2007052100023 20070521 00023 NM 2007 5 21 QXEA200700786 1 20070509 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - SURFACE CORROSION ON CENTER RIGHT SEAT TRACK NR 10 AT STATION .5.0. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007052100044 20070521 00044 NM 2007 5 21 AWXA200700613 1 20070418 A 5340 65C2702165 ATTACH ANGLE BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - FOUND CRACKED ATTACH ANGLE, BS 663, S9L. REPLACED ATTACH ANGLE, BS 663, S9L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007052100045 20070521 00045 NM 2007 5 21 AWXA200700614 1 20070422 A 5311 654580761 FRAME BOEING 737 73733A 1384673 NM BS 291 S16R CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - CRACKED R1 DOOR CUT OUT FWD STUB FRAME, BS 291, S16R. REPLACED R1 DOOR CUT OUT FWD STUB FRAME, BS 291, S16R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007052100059 20070521 00059 NM 2007 5 21 QXEA200700751 1 20070424 A 5320 ANGLE BOMBDR DHC8 DHC8402 1390042 NM BS 782 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - CORROSION AROUND SCREW HOLE AT AFT CARGO COMPARTMENT DIVIDING WALL LOWER ANGLE STATION X782 ABOUT 12" OUTBOARD OF SEAT TRACK NR 9. REPAIRED IAW SRM 51-21-00, 51-21-10, 51-25-10. 2 H 7 2 4T RT A13NM 2007052100063 20070521 00063 NM 2007 5 21 QXEA200700745 1 20070429 A 5311 FRAME BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - CRACKED RIVET HOLE ON FRAME AT X69.4 ABOVE STRINGER 19P. REPAIRED IAW RD8/4-53-017 AND SRM 51-25-05. 2 H 7 2 4T RT A13NM 2007052100069 20070521 00069 NM 2007 5 21 AWXA200700631 1 20070505 A 5311 6546561509 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - R2 DOOR CUT OUT FORWARD UPPER STUB FRAME CRACKED, BS 957, S12R. REPLACED R2 DOOR CUT OUT FORWARD UPPER STUB FRAME , BS 957, S12R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007052100073 20070521 00073 NM 2007 5 21 DHL2007788512 1 20070429 A 5753 6521630187 SKIN BOEING 727 727214 138407R NM LT WING TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 LEFT WING, INBD FORE FLAP LOWER SURFACE DELAMINATED AT LWBL 125. CUT OUT DELAMINATED AREA 8.4" BY 9.4" CLEANED AND PREP PED AREA TO BOND IAW B727 SRM 51-40-20, PAR 7, FIG 3 AND 51-40-24, FIG 1. FABRICATED DOUBLER 10" BY 12.4" AND FILLER 8. 4" BY 9.4" FROM .016, 2024T3, ANODIZED, PRIMED AND APPLIED ADHESIVE FILM IAW B727 SRM 51-40-20, PAR 8, 14, 15, 18 AND 51 -40-24, FIG 1 AND 57-50-2, FIG 3. INSTALLED, CURED AND FINISHED REPAIR IAW B727 SRM 51-40-20 AND 51-40-24, FIG 1. 2 L 7 3 4F A3WE 2007052100074 20070521 00074 NM 2007 5 21 DHL2007788513 1 20070423 A 5754 651622188 SKIN BOEING 727 727214 138407R NM RT WING NR5 SLAT DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 RIGHT WING, LWS 383.5, L/E SLAT AERO FENCE, LOWER AFT COMPOSITE SURFACE AREA IS CRACKED, LAYERS ARE SPLITTING. SANDED, CLEANED AND PREPPED 9" BY 5" DAMAGED AREA IAW B727 SRM 51-40-9, PAR 4, FIG 1. FABRICATED, IMPREGNATED (7781-50) FIBERGL ASS AND 50A RESIN. INSTALLED FIBERGLASS PLIES AND CURED IAW B727 SRM 51-40-9, PAR 4, FIG 1. 2 L 7 3 4F A3WE 2007052100078 20070521 00078 WP 2007 5 21 UPS07849800 1 20070513 A 3350 BATTERY DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS NO TEST A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:N/A EMERGENCY LIGHTS WON'T TEST. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT PER MM 33-50-01-2. 2 L 7 4 4F RT 4A25 2007052100080 20070521 00080 WP 2007 5 21 UPS07849806 1 20070424 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FS 869 L24L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 L24L 12 INCHES AFT OF BARREL NUT STA 869 CRACKED: VIEWED FROM TOP OF WING. STOP DRILLED CRACKED L24 L AT STA 869 IAW SRM 53-2-2 VIEW G. STOP DRILLS TERMINATE CRACKS PER HFEC NDTS 06-10-01.001. FABRICATED AND INSTALLED -3, -5 DOUBLERS, -7, -9 REPAIR ANGLES, AND FILLERS AT STA 869 L24L IAW SRM 53-2-2 FIG 5, AND SRM TR 53-123 GEN NOTE 4. 2 L 7 4 4F RT 4A25 2007052100085 20070521 00085 EA 2007 5 21 TRAX200700663 1 20070513 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 RIGHT FUSELAGE AFT EXT EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007052100086 20070521 00086 EA 2007 5 21 TRAX200700664 1 20070513 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 859AS 7421 PAX DOOR WOULD NOT OPEN WITH OUTER HANDLE. 2 L 7 2 4F RT A21EA 2007052100089 20070521 00089 EA 2007 5 21 TRAX200700667 1 20070513 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 844AS 7317 SERVICE DOOR DOES NOT CLOSE. 2 L 7 2 4F RT A21EA 2007052100090 20070521 00090 EA 2007 5 21 TRAX200700668 1 20070513 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 681BR 7680 F/A REPORTS PAX DOOR HARD TO OPEN FROM THE INSIDE. 2 L 7 2 4F RT A21EA 2007052100091 20070521 00091 NM 2007 5 21 ASAA0741633 1 20070514 A 5315 65C3394116 FLOORBEAM BOEING 737 7374Q8 138447Q NM BS 312 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 FLOORBEAM CORRODED UPPER CHORD. REMOVED CORRODED SECTION OF UPPER CHORD FABRICATED AND INSTALLED REPLACEMENT CHORD ANGL ES AND SHIMS IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2007052100092 20070521 00092 NM 2007 5 21 ASAA0741634 1 20070514 A 5320 6552878122 WEB BOEING 737 7374Q8 138447Q NM BS 950-986 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 FLOOR WEB BELOW L2 DOOR CRACKED (UNDER MOPSILL). REMOVED DAMAGED WEB, FABRICATED AND INSTALLED REPLACEMENT WEB IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 2007052100093 20070521 00093 CE 2007 5 21 DXTA200702201 1 20070517 A 2170 COALESCER BAG CESSNA 750 750 2076810 CE CABIN AIR ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 990QS 7500190 SMOKEY ODOR IN CABIN, NO VISIBLE SMOKE. [SUP 05-22-07] REMOVED BOTH COALESCERS COCKPIT IS CLEAN. CABIN HAS OIL INSIDE SEPERATOR AND SOCK IS SATURATED WITH OIL. CLEANED SEPERATOR AND REPLACED SOCK. REMOVED AND REPLACED CABIN ACM. RAN ACM A ND LEAK CHECKS GOOD. OPS CHECKS GOOD. ALL WORK IAW HAMILTON SUNDSTRAND MM 21-50-03. 2 L 7 2 4J RT T00007WI 2007052100095 20070521 00095 CE 2007 5 21 DXTA200702183 1 20070510 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE MLG MALFUNCTIONED E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 354QS 5600356 F/O'S BRAKES ARE SPONGY DURING NORMAL OPERATIONS. PERFORMED BRAKE BLEED PROCEDURE TO LEFT & RIGHT BRAKES. BRAKES OPS C HECK GOOD IAW CESSNA 560 MM 32-42-00. 2 L 7 2 4F RT A22CE 2007052100098 20070521 00098 CE 2007 5 21 DXTA200702186 1 20070510 A 3244 315381 TIRE CESSNA 750 750 2076810 CE NLG OUT OF ROUND E DXTA C ABORTED TAKEOFF E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 GL 07 935QS 619 7500135 AT 70 KNOTS ON TAKEOFF ROLL NOSEWHEEL SHIMMY OCCURRED RAPIDLY AND VIOLENTLY KNOCKING YAW DAMPER OFF LINE. FOUND BOTH NO SE TIRES OUT OF ROUND. REPLACED BOTH NOSE WHEEL ASSY. ALL WORK DONE IAW CE-750 CH 32-41-01. 2 L 7 2 4J RT T00007WI 2007052100099 20070521 00099 EA 2007 5 21 COMA0770028 1 20070515 A 5330 SKIN PANEL CNDAIR CL600 CL6002C10 1390015 EA BS 394-453 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 397CA 10102 FUSELAGE SKIN CRACKING DISCOVERED WITH EDDY CURRENT AT FS 394.0, 421.0, 437.0 AND 453.0 AT STRINGER 16L. REPAIRED AREAS IAW REO 670-53-21-276. 2 L 7 2 4F RT A21EA 2007052100100 20070521 00100 NM 2007 5 21 CALA0700243 1 20070326 A 5330 SKIN BOEING 757 757324 1384930 NM BS 1180 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 75858 32817 INSPECTION FOUND A LIGHTNING STRIKE AT EDGE OF FUSELAGE RIVET, STA 1180+80 BETWEEN STRINGERS 1&2R. AN INTERIM REPAIR WA S PERFORMED IAW ECRA 5330-0356 AND A DIP WAS ISSUED TO CONTACT STRUCTURES ENGINEERING AFTER 10 BUT NO LATER THAN 11 MONT HS FOR PERMANENT REPAIR. 2 L 7 2 4F RT A2NM 2007052100102 20070521 00102 NM 2007 5 21 CALA0700245 1 20070504 A 5311 146A128214 FRAME BOEING 737 737724 13844BY NM BS 867 S25L CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17719 28938 INSPECTION FOUND FRAME CORRODED AT STA 867, S25L. THE FRAME WAS REPAIRED IAW SRM 51-70-11. 2 L 7 2 4F RT A16WE 2007052100103 20070521 00103 NM 2007 5 21 CALA0700246 1 20070515 A 5320 6552878U124 ANGLE BOEING 737 7373T0 1384582 NM BS 907-1006 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND Z-ANGLE AT L-2 DOOR, STA 907-1006, LBL 50 CORRODED. THE Z-ANGLE WAS REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007052100105 20070521 00105 NM 2007 5 21 CALA0700248 1 20070515 A 5320 65C807351 ANGLE BOEING 737 7373T0 1384582 NM BS 947-1000 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND Z-ANGLE AT R-2 DOOR ENTRYWAY, STA 947.5-1000, S17R, CORRODED. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007052100106 20070521 00106 NM 2007 5 21 CALA0700249 1 20070430 A 5311 FRAME BOEING 737 737824 13844BZ NM BS 992 S17R CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 35204 30576 INSPECTION FOUND AFT FRAME CHORD AT R-2 DOOR LOWER SILL, STA 992, S17R, LBL 0 TO RBL 64 CORRODED. THE FRAME WAS REPAIRE D IAW ECRA 5311-01315. 2 L 7 2 4F RT A16WE 2007052100107 20070521 00107 NM 2007 5 21 CALA0700250 1 20070507 A 5710 UNK VAPOR BARRIER BOEING 737 737824 13844BZ NM LT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76503 33461 INSPECTION FOUND THE LEFT WHEEL WELL FORWARD BULKHEAD (WING CENTER SECTION AFT SPAR VAPOR BARRIER) CRACKED. THREE CRACK S WERE FOUND MEASURING 7 INCHES, 19.5 INCHES, AND 4 INCHES. THE VAPOR BARRIER WAS REMOVED AND REPLACED IAW ECRA 5710-02 116. 2 L 7 2 4F RT A16WE 2007052100108 20070521 00108 NM 2007 5 21 CALA0700251 1 20070507 A 5712 UNK BULKHEAD BOEING 737 737824 13844BZ NM RT MLG W/W CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76503 33461 INSPECTION FOUND THE RIGHT WHEEL WELL FORWARD BULKHEAD (WING CENTER SECTION AFT SPAR VAPOR BARRIER) CRACKED. THERE WERE TWO CRACKS MEASURING 12.75 INCHES AND 8 INCHES. THE VAPOR BARRIER WAS REMOVED AND REPLACED IAW ECRA 5710-02116. 2 L 7 2 4F RT A16WE 2007052100109 20070521 00109 CE 2007 5 21 DXTA200702182 1 20070509 A 3260 S31762 SQUAT SWITCH CESSNA 560 560XL 2076702 CE MLG INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 672QS 602 5605663 AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT HANDLE LOCKED IN DOWN POSITION. REMOVED AND REPLACED LEFT SQUAT SWITCH WIT H NEW. OPS CHECK GOOD. REF CESSNA 560XL MM 32-61-00. 2 L 7 2 4F RT A22CE 2007052100110 20070521 00110 NM 2007 5 21 ASAA0741635 1 20070516 A 5752 654645523C TAB BOEING 737 7374Q8 138447Q NM AILERON DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 LEFT AILERON TAB IS DELAMINATED AT T/E. REMOVED AND REPLACED LEFT AILERION TAB IAW AMM 27-11-21 PG 401. 2 L 7 2 4F RT A16WE 2007052100112 20070521 00112 NM 2007 5 21 ASAA0741637 1 20070516 A 5320 6545855122 SILL BOEING 737 7374Q8 138447Q NM BS 915-1006 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 AR AFT MOPSILL CORRODED (INNER CHORD). REMOVED CORRODED SILL, REPLACED SILL WITH NEW PART IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007052100113 20070521 00113 NM 2007 5 21 ASAA0741639 1 20070516 A 5320 654587574 SILL BOEING 737 7374Q8 138447Q NM CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 R1 DOOR SILL (INNER CHORD) IS CORRODED. REMOVED CORRODED SILL, REPLACED WITH NEW PART IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007052100116 20070521 00116 WP 2007 5 21 UPS07849820 1 20070428 A 5522 SKIN DOUG DC8 DC873F 302199F WP LT ELEVATOR CANNING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 L/ELEVATOR UPPER SKIN ON INBD SIDE HAS DINGS AND SKIN HAS OIL CANNING. CUT OUT DAMAGED SKIN ON L/ELE VATOR AT STA XE 57.5 IAW SRM 55-02-01-0, FABRICATED, BONDED FINGER DOUBLER, AND INSTALLED REPLACEMENT SKIN ON L/ELEVATOR AT STA XE 57.5 IAW DWG 5654970, AND SRM 55-2-1 FIG 11. 2 L 7 4 4F RT 4A25 2007052100117 20070521 00117 WP 2007 5 21 UPS07849821 1 20070510 A 5340 4641324U501 FITTING DOUG DC8 DC873F 302199F WP FS 1690 L34R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 END FITTING CRACKED AT STA 1690 L34R, 2.5 INCHES AT BARREL NUT HOLE. REMOVED CRACKED END FITTING AT STA 1690 L34R IAW SRM 51-01-20D. LOCATED, DRILLED UP, AND INSTALLED END FITTING AT STA 1690 L34R IAW SRM 51-03-02, AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 2007052100118 20070521 00118 WP 2007 5 21 UPS07849822 1 20070427 A 5312 PRESSURE PANEL DOUG DC8 DC873F 302199F WP FS 863 MISREPAIRED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 VISUAL INSP OF PRESSURE WEB AT STA 863 RBL 42-48, FOUND DOUBLER TO BE TAPERED ON ENDS, WITH NO TAPERE D SHIMS INSTALLED, REF: EO DC8- 5310-22195-B. INSTALLED CORRECT REPAIR AT STA 863 RBL 42-48 IAW SAA EA 008-5310- 01-A08 41, UPS EO DC8-5310-22195-C, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007052100119 20070521 00119 WP 2007 5 21 UPS07849823 1 20070425 A 5330 56493284 SKIN DOUG DC8 DC873F 302199F WP FS 1746 L26-30R MISREPAIRED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 L28R AT FS 1746 HAS 2 EA EXISTING REPAIR DOUBLERS UPPER AND LWR OF L28R, NOT IN COMPLIANCE WITH EO DC 8-5330-20248 NOR DWG SRO8530032. REPAIRED FUSELAGE TAIL SECTION SKINS AT STA 1746, L28R - L30R IAW SAA EA 008-5330-01-A 0854, UPS EO DC8-5330-26800-A, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007052100122 20070521 00122 NM 2007 5 21 UPS07M49813 1 20070328 A 5310 DOOR FRAME DOUG MD11 MD11F 3023600 NM BS 1926 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C AFT CARGO DOOR FWD AND AFT JAMBS HAS SCALLOPED IN SEVERAL AREA. REMOVED HEAT DUCT ON AFT CARGO STA 19 26 PER AMM20-50-02 REV 50. FWD & AFT JAMB FASTENERS REMOVED PER SRM 51-31-01 VOL 2 REV 38. HFEC INSP CUT OUT FOUND NO CRACK. REPAIR DOUBLERS FAB, FASTENER HOLES PICKUP, REWORKED, REPROTECTED & INSTALLED PER SRM 53-50-00 FIG 16 VOL1 REV 3 8. AFT CARGO HEAT DUCT STA 1926 REINSTALLED PER AMM20-50-02 REV 50. 2 L 7 3 4F RT A22WE 2007052100124 20070521 00124 NM 2007 5 21 UPS07M49815 1 20070412 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1264-1391 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C CABIN - CORROSION ON SEAT TRACK CROWN AT STA 1351 X=-75.0. SEAT TRACK CORROSION REMOVED FOUND EXCEEDE D LIMITS PER SRM 53-70-00 FIG 3 REV 38 VOL 1. SEAT TRACK ATTACHED PARTS STA 1264-1391 X=-75 REMOVED PER SRM 51-31-01 VO L 2 REV 38. CORRODED SEAT TRACK REPAIRED, SPLICE HAT & PLATE FAB PER SRM 53-70-01 VOL 1 FIG 1 REV 38. FAB PARTS & SEAT TRACK INSTALLED PER SRM 51-31-01 VOL 2 REV 38. 2 L 7 3 4F RT A22WE 2007052100127 20070521 00127 NM 2007 5 21 P5CA0701522 1 20070510 A 2913 60B0025610 PUMP BOEING 747 74746NF 13848BT NM NR 2 ENGINE LEAKING A P5CA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 EA 15 451PA 30809 HYDR ENG NR 2 ON EICAS DISPLAY. FOUND EDP LEAKING AND SHAFT SHEARED. REMOVED AND REPLACED EDP AND INSTALLED COVER PLAT E P/N G29003-1 PER AMM 29-11-05 P 201. DEFERRED PER MEL 29-1-1-C. LEAKS CHECK OK. 2 L 7 4 4F RT A20WE 2007052100128 20070521 00128 EA 2007 5 21 TRAX200700658 1 20070512 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 978EV 7723 REMOVED EMERGENCY LIGHT ASSY FROM PAX DOOR ENTRY ASSY BR9279-232 FOR ACFT 832. 2 L 7 2 4F RT A21EA 2007052100129 20070521 00129 EA 2007 5 21 TRAX200700659 1 20070512 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA ILLUMINATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 908EV 7654 ANTI ICE DUCT WARNING AND SYNOPTIC PAGE IS SHOWING RT FUSELAGE RED FLOW BAR. EN ROUTE TO MDT A/C DIVERTED TO TYS DUE TO MTC. EMERGENCY DECLARED. FLT 4291 DEL 25 MINS. 2 L 7 2 4F RT A21EA 2007052100131 20070521 00131 EA 2007 5 21 TRAX200700661 1 20070512 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN TORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 832AS 7243 EMERGENCY LIGHT BY STAIR DOOR IS TORN. 2 L 7 2 4F RT A21EA 2007052100132 20070521 00132 EA 2007 5 21 TRAX200700662 1 20070512 A 5260 DOOR CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 834AS 7254 ASD HARD TO CLOSE. FLT 4574 DEL 25 MINS. 2 L 7 2 4F RT A21EA 2007052100134 20070521 00134 EA 2007 5 21 COMA0760372 1 20070516 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FS 559 LBL 9 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 956CA 7105 DURING 559 INSPECTION FOUND .5 INCH CRACK AT LOWER OUTBOARD SIDE OF LBL VERTICAL STIFFENER. REMOVED DAMAGE AND INSTALLE D DOUBLER PER BOMBARDIER REO 601R-53-41-057. 2 L 7 2 4F RT A21EA 2007052100135 20070521 00135 NM 2007 5 21 WRLA2007068 1 20070515 A 5730 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE LT WING DAMAGED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 273WA 48519 FLT 8129/LEJ/ATL 05/15/2007. ON POST FLIGHT INSPECTION WORLD AIRWAYS MAINTENANCE FOUND LEFT WING REFUEL PANEL DAMAGED A ND PINCHED BY NR 4 LEADING EDGE SLAT. REMOVED LEFT WING FUELING PANEL DOOR, TRIMMED OUT DAMAGE, INSPECTED PER DELTA AIR LINES ERA 461879-14, NO ADDITIONAL DAMAGE. INSTALLED SERVICEABLE FUEL DOOR IAW MM 57-40-01 AND SRM 51-31-01, ITEM WORK ED ON DELTA NR CARD 001. REMOVED AND INSTALLED NR 4 LEADING EDGE SLAT LEFT WING PER MM 27-80-30. REPAIRED LEFT WING L/ E SKIN AT STATIONS XOS 618, XOS 627 AND XOS 635 PER WORLD AIRWAYS ERA 07-57-036 AND DELTA AIR LINES ERA 461879-14. 2 L 7 3 4F 4 F RT A22WE E24NE 2007052100142 20070521 00142 NM 2007 5 21 ASAA0741642 1 20070515 A 5210 AN202KP23B BEARING BOEING 737 7374Q8 138447Q NM R1 DOOR ERODED A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 760AS 25098 CATERING REPORTED THE L1 DOOR INOPERABLE. FERRIED TO SEA, REMOVED AND REPLACED R1 DOOR PER AMM. 2 L 7 2 4F RT A16WE 2007052100144 20070521 00144 CE 2007 5 21 BSAASDR0712 1 20070512 A 3234 SWITCH BEECH 1900 1900D 1154162 CE MLG HANDLE INOPERATIVE A BSAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 05 139ZV UE139 DURING APPROACH WHEN CREW SELECTED GEAR DOWN THE LANDING GEAR RELAY CONTROL CB TRIPPED WHEN THE GEAR WAS HALFWAY DOWN. CREW ABORTED THE APPROACH AND MANUALLY EXTENDED THE GEAR. CREW LANDED WITH NO FURTHER INCIDENT. ALL WIRING & COMPONENT S IN THE LANDING GEAR CONTROL CIRCUIT BREAKER WAS INSPECTED, ALL 3 GEAR, ACTUATORS, SHUTTTLE VALVE, LEADING EDGE WIRING, NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR OCF, CREW NOTED THE PROBLEM COULD BE REPEATED WHILE IN 15 DEGREE LEFT BANK , FOUND BAD SWITCH & LOOSE SPRING IN LANDING GEAR CONTROL HANDLE. REPLACED LANDING GEAR HANDLE ASSEMBLY, SYSTEM OPS CHE CK GOOD. 2 L 7 2 4T RT A24CE 2007052100148 20070521 00148 EU 2007 5 21 YENA2007034 1 20070514 A 3234 CONTROL HANDLE AIRBUS 320 A320232 3930326 EU MLG DAMAGED A YENA O OTHER O OTHER CL CLIMB 1 EA 15 644JB 2880 FLT 61, AFTER TAKEOFF SYR TO JFK, GEAR FAILED TO RETRACT. GEAR HANDLE WOULD NOT MOVE. GEAR HANDLE PANEL DISPLACED OUT APPRROX .5 INCH. ACCOMPLISHED TSM 32-31-00-30-885. LANDING GEAR RETRACTION/EXTENSION DONE 4 TIMES. NO FAULT NOTED. N O FAULT FOUND ON PFR FAULT REPORT. FOUND L/G CONTROL LEVER UNIT DISPLACED. INSPECTED CONNECTOR & REINSTALLED L/G CONT LEVER UNIT. OPS CHECK NORMAL PER 32-31-71-00-001. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2007052100149 20070521 00149 CE 2007 5 21 BSAASDR0711 1 20070511 A 3230 LANDING GEAR BEECH 1900 1900D 1154162 CE MAINS FAILED A BSAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 05 139ZV UE139 DURING APPROACH, WHEN CREW SELECTED GEAR DOWN, THE LANDING GEAR CONTROL RELAY CIRCUIT BREAKER TRIPPED HALFWAY THROUGH TH E GEAR EXTENSION. CREW ABORTED LANDING, PERFORMED MANUAL EXTENSION AND LANDED WITH NO FURTHER INCIDENT. THE GEAR CB WA S RESET, AND THE GEAR WAS CYCLED MULTIPLE TIMES WITH NO FAILURE. GEAR CONTROL PCB AND WIRING WERE INSPECTED, AND NO DEF ECT FOUND. PERFORMED MUTLIPLE GEAR SWINGS WITH NO FAILURE. 2 L 7 2 4T RT A24CE 2007052100150 20070521 00150 WP 2007 5 21 IXXA07SMN140S 1 20070421 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1581 L26R MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, IMPROPER REPAIR LOCATED AT STATION 1581 LONGERON 23 RIGHT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN, EXTERNAL DOUBLER, AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACE. INSTALLED REP AIR PARTS IAW DC8 SRM 51-1-21, 51-1-20D,SEMAN DRAWING NUMBER ED-4521,DC8 NDT SPM PART 06-10-01.001,DC8 SRM 51-1-8B,DC8 S RM 51-1-11, AND 51-3-1. 2 L 7 4 4F RT 4A25 2007052100151 20070521 00151 WP 2007 5 21 IXXA07SMN141S 1 20070421 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR LOCATED AT STATION 1.600 LONGERON 28 RIGHT. REMOVED EXISTING R EPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN, EXTERNAL DO UBLER, INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACE. INSTALL ED REPAIR PARTS IAW DC8 SRM 51-1-21, 51-1-20D, SEMAN DRAWING NUMBER ED-4520, DC8 NDT SPM PART 06-10-01.001, DC8 SRM 51-1 -8B, DC8 SRM 51-1-11, AND 51-3-1. 2 L 7 4 4F RT 4A25 2007052100152 20070521 00152 EU 2007 5 21 YNTA200728101 1 20070514 A 5753 YOKE BRAERO DH125 HS125700A 4230170 EU TE FLAPS CORRODED E YNTA L ABORTED APPROACH O OTHER AP APPROACH 1 SW 05 281BT NA0281 ON APPROACH THE FLAP SYSTEM FAILED TO EXTEND PAST 15 DEGREES AND THEN BECAME STUCK AT 15 DEGREES. TRIED TO SET FLAPS TO 25 DEGREES AND FLAPS DID NOT MOVE, RESET FOR 15 DEGREES AND THEN UP TO 0 DEGREES WITH NO MOVEMENT. RESELECTED FLAPS TO 1 5-DEGREE POSITION. LANDED UNEVENTFULLY. AIRCRAFT FLAP SYSTEM HAD BEEN WORKED ON 05/09/2007 WHERE THE FOLLOWING PARTS WER E REPLACED LT FLAP TRUNNION YOKE P/N 25CW733A, BOLT, HEX P/N A102-9D, WASHER P/N SP126D, NUT P/N A103DS AN OPERATIONAL C HECK WAS ACCOMPLISHED AND A TEST FLIGHT CONDUCTED ON 05/10/2007 FOUND FLAP SYSTEM TO BE OPERATIONALLY SATISFACTORY IN BO TH INSTANCES. CORRECTIVE ACTION TAKEN= FOUND FLAP CONTROL UNIT INPUT LEVER ROD END CORRODED. REMOVED FLAP INPUT LEVER RO 2 L 7 2 4F A3EU 2007052100153 20070521 00153 WP 2007 5 21 IXXA07SMN139S 1 20070421 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 445 L27R MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION 445, LONGERON 27.5 RIGHT. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, EXTERNAL DOUBLER AND INTERNAL DOUBLER, CLEANED TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACE. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-1 FIGURE 7 SHEET 1 AND 3, DC8 SRM 51-1-21 AND 51-1-2 0D,DC8 SRM 53-4-1 FIGURE 1 ITEM "B" AND DC8 SRM 51-9-0 FIGURE 68A, DC8 SRM 51-1-8B, AND DC8 SRM 51-1-11. 2 L 7 4 4F RT 4A25 2007052100154 20070521 00154 WP 2007 5 21 IXXA07SMN146S 1 20070421 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 500 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP CRACKED ON UPPER PART EXTERNAL COATING AT STATION XW 10 4.00. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PAR TS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 57-7-1 PAGE 2 FIGURE 1, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21,DC8 SRM 57-7-1 PAGE 2 FIGURE 1 ITEM "D’, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND DC8 SRM 51-3-0, DC8 S RM 51-3-1. 2 L 7 4 4F RT 4A25 2007052100155 20070521 00155 EU 2007 5 21 YENA2007033 1 20070517 A 2780 1702286A SENSOR EMB ERJ190 ERJ190100IGW 3260408 EU SLAT SYSTEM FAULTY A YENA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 15 236JB 2448 19000035 FLT 1046, WHILE RETRACTING FLAPS OUT OF BNA, RECEIVED -SLAT LO RATE- MESSAGE. WHEN EXTENDING FLAPS IN JFK, RECEIVED -SL AT FAIL- MESSAGE. TSI PREVIOUSLY ASSIGNED FOR TROUBLESHOOTING OF SLAT FAIL MESSAGE. PERFORMED TROUBLESHOOTING REF TSI N236 101011. REMOVED & REPLACED SLAT 3 & 4 SKEW SENSOR AS PER AMM 27-83-01 AND REMOVED AND REPLACED SLAT HARNESS W511, N512 AS PER AMM 27-83-07. PERFORMED OPS CHECK. OPS CHECK SATISFACTORY. 2 L 7 2 4F RT A57NM 2007052200001 20070522 00001 NM 2007 5 22 NWAA071873136 1 20070514 A 3350 BATTERY PACK AIRBUS A319 A319114 3930350 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 336NB 1683 EPSU AFT LEFT BATTERY FAULT (CABIN EMERGENCY LIGHTING). REPLACED BATTERY IN AFT LEFT EPSU, CHECKS GOOD. 2 L 7 2 4F RT A28NM 2007052200002 20070522 00002 EA 2007 5 22 SIMA200713504 1 20070509 A 8012 3291393 START VALVE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE RT ENGINE FAILED A SIMA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SW 21 503AE 1655 8 10021 GE965284 NOP STARTER CUTOUT CAUTION MESSAGE IN FLIGHT, FOLLOWED SHUTDOWN PROCEDURES OER AOM. RETURNED TO ORD. REMOVED AND REPLA CED ENGINE TWO START VALVE IAW CRJ AMM. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007052200003 20070522 00003 SO 2007 5 22 SIMA200713501 1 20070509 A 5610 SEAL EMB 145 EMB145LR 3260212 SO COCKPIT WINDOW LOOSE A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 928AE 14500911 HEARD NOISE FROM CAPTAIN'S DV WINDOW AND SEAL COMING OFF WINDOW ON CLIMBOUT, RETURNED TO JAN. REPAIRED CAPTAIN'S DV WIN DOW SEAL IAW EMB AMM. PRESSURE CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007052200004 20070522 00004 EA 2007 5 22 SIMA200713506 1 20070513 A 5610 601R3303319 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SIMA O OTHER O OTHER CR CRUISE 1 SW 21 520DC 10140 10140 HEARD A POP IN FLIGHT, POST FLIGHT INSPECTION REVEALED CAPTAIN'S SIDE WINDOW INNER PANE HAD CRACKED IN SEVERAL AREAS. R EMOVED AND REPLACED CAPTAIN'S LEFT SIDE WINDOW IAW CRJ AMM 56-12-01. PRESSURIZATION CHECKED WITH NO DEFECTS NOTED, RETU RNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007052200005 20070522 00005 EA 2007 5 22 SIMA200713502 1 20070509 A 3010 GG43640067 DETECTOR CNDAIR CL600 CL6002C10 1390015 EA RIGHT FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 513AE 5432 646 10114 INTERMITTENT ICE CAUTION IN FLIGHT THROUGHOUT IN VMC CONDITION. DIVERTED TO XNA. REMOVED AND REPLACED RIGHT ICE DETECT OR IAW EMB AMM. OPERATIONAL CHECK GOOD, RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007052200007 20070522 00007 GL 2007 5 22 SIMA200713505 2 20070513 A 7200 ENGINE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL NR 1 ODOR A SIMA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 847AE 5511 2368 145707 CAE312728 CREW NOTICED ODOR AND SMOKE IN COCKPIT ON TAKEOFF ROLL. REMOVED AND REPLACED NUMBER ONE ENGINE IAW AMERICAN EAGLE WORK CARD 72-00-00. LEAK AND OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007052200009 20070522 00009 EU 2007 5 22 NWAA071853268 1 20070512 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320212 3930322 EU EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 368NW 0996 ON PREFLIGHT, CREW FOUND SEVERAL CABIN EMERGENCY LIGHTS INOP. REPLACED EPSU, CHECKS OK. 2 L 7 2 4F RT A28NM 2007052200010 20070522 00010 2007 5 22 NWAA071863251 4 20070513 A 2210 B397BAM0515 COMPUTER AIRBUS 320 A320212 3930322 EU NR 1 MALFUNCTIONED A NWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 01 351NW 4095 766 IN CRUISE AT FL300, HAD HARD RUDDER KICK (NOTED AS 5-7 DEGREE HEADING DEFLECTION), THEN SMELLED BURNING ELECTRICAL ODOR. FAC 1 FAULT ILLUMINATED. DID NOT RESET FAC. DIVERTED TO LAS. YAW DAMPER 1, RUDDER TRIM 1, RUDDER TRAVEL LIMITER 1, ON ECAM. AIRCRAFT LANDED UNEVENTFULLY. 2 L 7 2 4F RT A28NM 2007052200011 20070522 00011 EU 2007 5 22 07FDEA01788 1 20070515 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 401FE 191 2 CORROSION EXIST AT MDCC SEAT TRACK L-4 BETWEEN FRAMES 2/32 AND FRAME 33 DEFECTED AREA MEASURE 1.5 SQ INCHES. REMOVED CORROSION IAW A310 SRM 51-74-10 MATERIAL LOSS IN LIMITS IAW A310 SRM 53-10-16, SEAT TRACK REMOVED AND REPLACED IAW A310 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007052200013 20070522 00013 2007 5 22 07FDEA01790 4 20070515 A 3418 861CAE1 SENSOR AIRBUS 310 A310203 3930313 EU AOA FAILED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 426FE 245 RTO AT 100KTS , NAV ADC 1 FAILURE WITH ASSOCIATED WARNINGS. SWAPPED 1 ANGLE OF ATTACK AND NR 3 ANGLE OF ATTACK, PER AMM 34-11-19-4. PERFORMED ALPHA PROBE TEST AND AFS/ LAND TEST NO FAULT OR FAILURES. PER TSM 22-00-00. R/I FROM FACT SWA P COMPONENT POSITIONS FROM POSITION 3 TO POSITION 1 SWAPPED NR 1 AND NR 3 AOA SENSORS. PLACED NR 3 AOA ON MEL. REF WRI 34-18-8810. 2 L 7 2 4F RT A35EU 2007052200015 20070522 00015 EU 2007 5 22 07FDEA01792 1 20070515 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 401FE 191 A 1/2" CRACK EXISTS AT FRAME 38 FLOORBEAM FWD FACE BETWEEN SEAT TRACK 4L AND 5L (VISIBLE FROM FWD CARGO OVERHEAD). REPA IRED CROSS BEAM AT FRAME 38 BETWEEN SEAT TRACK 4L AND 5L IAW A310 SRM 53-10-15 FIG 201 SHEET 6A. 2 L 7 2 4F RT A35EU 2007052200016 20070522 00016 EU 2007 5 22 07FDEA01793 1 20070515 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 401FE 191 PREVIOUS REPAIR LOCATED ON MAIN CABIN FLOORBEAM FRAME 55/58 BETWEEN SEAT TRACK 4 AND 5 RT, AFT UPPER FLANGE HAS 1 REPAIR ANGLE MEASURING 12.6" BY 2.6", ALSO THERE IS A REPAIR FILLER ON THE TOP SURFACE OF FLOORBEAM UNDER THE CLS ADAPTER MEAS URING 14.3" BY 1" PREVIOUSLY INSTALLED REPAIR FOUND NOT TO BE IAW SRM OR REPAIR DWG. REMOVED EXISTING REPAIR AND CLS AD APTER, REPLACED THE CLS ADAPTER WITH A NEW PART AND REPAIRED THE FLOORBEAM PER FEDEX EA6-5310-110461 AND REPAIR DWG R532 70150. 2 L 7 2 4F RT A35EU 2007052200017 20070522 00017 EU 2007 5 22 07FDEA01794 1 20070515 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 401FE 191 PREVIOUS REPAIR LOCATED ON AFT CARGO FLOORBEAM FRAME 63 JUST OUTBOARD OF LT AND RT NR 1 ROLLER TRACKS WITH 1 REPAIR SECT ION MEASURING 31" LONG AND 4 EACH REPAIR ANGLES PREVIOUS REPAIR FOUND NOT TO BE IAW A310 SRM 53-10-15 FIG 207. REMOVED EXISTING FASTENERS AND INSTALLED CORRECT FASTENERS PER A310 SRM 51-40-21 A310 SRM 53-10-15 FIG 20. 2 L 7 2 4F RT A35EU 2007052200018 20070522 00018 EU 2007 5 22 07FDEA01795 1 20070515 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 401FE 191 PREVIOUS REPAIR LOCATED ON MAIN CABIN FLOORBEAM FRAME 60 BETWEEN SEAT TRACK 3 AND 4 LT, FWD AND AFT SIDES HAVE 2 EACH RE PAIR ANGLES AND 2 EACH REPAIR STRAPS. THE FLOORBEAM HAS A NEW SECTION REPLACED ON THE LEFT SIDE PREVIOUSLY INSTALLED RE PAIR FOUND NOT TO BE IAW A310 SRM SUPPLEMENT 53-10-15 FIG 201 SHEET 10. REMOVED 16EA 3/16 LOCK FASTENERS REAMED HOLES T O .250 AND INSTALLED 16 EACH HL10VF8 LOCK FASTENERS REPAIR IS IAW A310 SRM SUPPLEMENT 53-10-15 FIG 201 SHEET 10. 2 L 7 2 4F RT A35EU 2007052200020 20070522 00020 EU 2007 5 22 07FDEA01797 1 20070515 A 5330 SKIN AIRBUS 310 A310203 3930313 EU FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 401FE 191 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED AT LEFT SIDE FUSELAGE SKIN ABOVE LAP SEAM BETWEEN FRAMES 38 TO 38.1 AND BETWEEN STRINGERS 41 TO 43 LT MEASURES 6.9" BY 6.9" PREVIOUS INSTALLED REPAIR FOUND NOT TO BE IAW A310 SRM 53-10-12 FIG 225. R EMOVED REPAIR. REPAIRED IAW A310 SRM 53-10-12 FIG 225, COMPLIED WITH FEDEX EA6-5100-110473. 2 L 7 2 4F RT A35EU 2007052200022 20070522 00022 2007 5 22 HALA0700018 4 20070110 A 2320 ACARS BOEING 767 767300 1385204 NM FAILED A HALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, ACARS FAILED TO RECORD OUT-TAXI-OFF TIMES. PERFORMED ACARS MU BITE PER FIM 23-22-00. SYSTEM TESTS OK. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007052200023 20070522 00023 NM 2007 5 22 HALA0700019 1 20070108 A 4940 RELAY BOEING 767 767300 1385204 NM APU STARTER SHORTED A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 590HA 33467 ETOPS SIGNIFICANT SYSTEM, REPEAT WRITE UP APU FAULT EICAS MESSAGE AFTER ATTEMPTED START AFTER LANDING OIL QTY READ FULL ONLY GOT TO 30 PERCENT THEN SHUT DOWN AUTOMATICALLY. OIL QTY READ .25, AT GATE READ .75. STARTED APU START NORMAL OPER ATED AIR PACKS ELECTRICS ALL NORMAL OIL QTY STAYS FULL. APU CHECKED FOR OIL LEAKS, NONE NOTED 1/2 PINT OIL ADDED TO TOP OFF REF FIM 49 11 OO FIG 106 A. REPLACED K 197 APU START RELAY DUE TO HISTORY. 2 L 7 2 4F RT A1NM 2007052200025 20070522 00025 EU 2007 5 22 07FDEA01798 1 20070515 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 3 AREAS OF CORROSION EXIST AT MDCC SEAT TRACK NR 1 DEFECTED AREA MEASURES 7.5 SQ IN FROM FRAMES 76 THRU 79. REMOVED CO RROSION 3 AREAS A, B, C, IAW A310/200 SRM51-74-10 MEASURED MATERIAL LOSS .075 AT AREA A FR-76 MATERIAL LOSS .009 AT AREA B FR77-78 MATERIAL LOSS .003 AERA C FR79 AND CHECKED ALLOWABLE LIMITS IAW A310/200 SRM53-10-16 FIG 101 AREA A AT FR76. FOUND TO BE OUT OF LIMITS AND AREAS B AND C FR 77-78-79 FOUND TO BE WITHIN LIMITS IAW A310/200 SRM 53-10-16 FIG 101. R ESTORED SURFACE PROTECTION TO AREA B/C IAW A310/200 SRM 51-23-10 AND SRM51-75-10, REPAIRED AREA A IAW A310 SRM53-10-16. 2 L 7 2 4F RT A35EU 2007052200027 20070522 00027 EU 2007 5 22 07FDEA01800 1 20070515 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 FWD CARGO COMP MDCC FLOORBEAM C23 HAS A CRACK BETWEEN SEAT TRACKS 2R AND 3R, CRACK LENGTH .125. FAB`D 2 REPAIR ANGLES P ER A310/200 SRM SUPPLEMENT 53-10-15 ALODINED; PRIMED, TOP COATED PER SRM51-75-10; INSTALLED 2 REPAIR ANGLES PER SRM SUPP LEMENT 53-10-15. 2 L 7 2 4F RT A35EU 2007052200028 20070522 00028 EU 2007 5 22 07FDEA01801 1 20070515 A 5531 RIB AIRBUS 310 A310203 3930313 EU VERTICAL STAB DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 VERTICAL STAB RT SIDE AT INTERSECTION OF ACCESS PANELS 323AL AND 323BR APPROX 2.5 INCHES FROM VERTICAL LOWER RIB EDGE 2 EACH WEAR MARKS APPROX .200 IN DIAMETER AND .050 DEEP BLENDED CHAF MARKS IAW A310 SRM 51-73-10 CHECKED LIMITS IAW A310 S RM 55-30-00 (OUT OF LIMITS). CUT OUT DAMAGE IAW A310 SRM 55-31-12 PB201 VERIFIED MATERIAL ID IAW A310 SRM 55-31-12. FA BRICATED DOUBLER IAW A310 SRM 55-31-12. ALODINED DOUBLER IAW A310 SRM 55-31-*12 PRIMED DOUBLER IAW A310 SRM 55-31-12. INSTALLED DOUBLER IAW A310 SRM 55-31-12, HEAT TREATED RIVETS IAW A310 SRM 51-25-00 TOP COATED TO MATCH IAW A310 SRM 51-7 5-10. 2 L 7 2 4F RT A35EU 2007052200029 20070522 00029 EU 2007 5 22 07FDEA01802 1 20070515 A 5531 RIB AIRBUS 310 A310203 3930313 EU VERTICAL STAB DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 VERTICAL STAB RT SIDE AT INTERSECTION OF ACCESS PANELS 323AL AND 323BR APPROX 2.5 INCHES FROM VERTICAL LOWER RIB EDGE 2 EACH WEAR MARKS APPROX .200 IN DIAMETER AND .050 DEEP BLENDED CHAF MARKS IAW A310 SRM 51-73-10 CHECKED LIMITS IA W A310 SRM 55-30-00 (OUT OF LIMITS). CUT OUT DAMAGE IAW A310 SRM 55-31-12 PB201 VERIFIED MATERIAL ID IAW A310 SRM 55-31-12. F ABRICATED DOUBLER IAW A310 SRM 55-31-12. ALODINED DOUBLER IAW A310 SRM 55-31-*12 PRIMED DOUBLER IAW A310 SRM 55-31-12. INSTALLED DOUBLER IAW A310 SRM 55-31-12. HEAT TREATED RIVETS IAW A310 SRM 51-25-00. TOPCOATED TO MATCH IAW A310 SRM 5 1-75-10. 2 L 7 2 4F RT A35EU 2007052200032 20070522 00032 EU 2007 5 22 07FDEA01805 1 20070515 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 AFT CARGO PIT/CABIN FLOORBEAM 54.2 CRACKED RLL 2.5 FEET APPROX TOTAL CRACKED LENGTH .25 REPAIRED FLOORBEAM 54.2 PER FEDE X EA6-5310-110456 AND AIRBUS REPAIR DRAWING R53706311. 2 L 7 2 4F RT A35EU 2007052200034 20070522 00034 EU 2007 5 22 07FDEA01807 1 20070515 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 FWD CARGO COMP FLOORBEAM C38 HAS A CRACK BETWEEN SEAT TRACKS 4L AND 5L REMOVED FLOOR PNL 231VF TO BETWEEN FR 37-40 TO F OM REPAIR PER A310/200 SRM 51-40-12 REWORKED THE MILLED MERTRIAL STIFFENER TO REMOVE CRACK PER A310/200 SRM SUPPLEMENT 5 3-10-15 FIG 201 NDT PER NTM51-10-08 SHOWS NO CRACK INDICATION AFTER REWORK, ALODINE PRIMED AND TOPCOATED MATING SURFACE AND 2 EACH ANGLES PER A310/200 SRM 51-21-10 AND SRM 51-75-10. INSTALLED 2 EACH ANGLES PER A310/200 SRM 53-10-15 AND SRM 51-40-21. TOPCOATED REPAIR AREA PER A310/200 SRM 51-75-10. INSTALLED FLOOR PNL 231VF PER A310/200 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007052200035 20070522 00035 NM 2007 5 22 NWAA071886305 1 20070516 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 665US 23820 DURING OVERNIGHT LINE CHECK, EMERGENCY LIGHTS AT ROWS 1 TO 4 RIGHT SIDE WERE INOP. MAINTENANCE REMOVED AND REPLACED POW ER SUPPLY. OPERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007052200038 20070522 00038 NM 2007 5 22 HALA0700213 1 20070516 A 2150 SENSOR BOEING 767 767300 1385204 NM PACK TEMP UNKNOWN A HALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, CABIN TEMPS ON THE GRN PRIOR TO DEPARTURE VERY HOT BOTH PACKS ON ALL TROM VALVES CLOSED PACK O UT L NO READING, R- -2, DUCT PRESS L 32, R 32, PACK FLOW L 0,R 0, RAM AIR DOOR L 0.0, R 0.02, CABIN TEMPS F80, M82, A82. PERFORMED BITE OF ZONE TEMP CONTROLLER PER FIM 21-60-00 AND BITE OF BOTH PACK CONTROLLERS PER FIM 21-51-00 NO FAULTS N OTED HEATED A/C TO 80 THEN COOLED TO 68 IN 10 MIN REMOVED AND REPLACED L PACK TEMP SENSOR PER AMM 21-51-08, OPS CK GOOD. 2 L 7 2 4F RT A1NM 2007052200041 20070522 00041 NM 2007 5 22 HALA0700210 1 20070518 A 4940 4502425C ECU BOEING 767 76733A 1385209 NM APU MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, APU WOULD NOT START AFTER 2 ATTEMPTS. REMOVED AND REPLACED ECU AND RESEATED CONNECTOR AT APU COMPARTMENT. OPS CHECK GOOD, WORK DONE IAW AMM 49-61-05. 2 L 7 2 4F RT A1NM 2007052200042 20070522 00042 NM 2007 5 22 HALA0700212 1 20070515 A 2150 A/C PACK BOEING 767 767300 1385204 NM MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, AIRCRAFT EXTREMELY HOT AT FULL COLD SETTING WHILE ON GROUND DUCT PRESSURE 30 PSI PACKS SYSTEM NORMAL OPERATION AIRBORNE, REPEAT WRITE UP SEE NR 54 PAGE 192680. RAN BOTH LEFT AND RIGHT PACKS , RAN TEMPS FROM COLD T O HOT ALL ZONES CHECK OK, CHECKED ZONE TEMP SENSOR FILTERS THEY WERE ALL CLEAN. T/S FIM REF 21-60-00. NO EICAS MSG'S F OUND SYSTEM OPS CKS NORMAL. 2 L 7 2 4F RT A1NM 2007052200043 20070522 00043 SO 2007 5 22 SIMA200714002 1 20070513 A 3350 66367 LIGHT EMB 135 EMB135KL 3260302 SO CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 839AE 11414 145653 ROWS 3 THROUGH 6 EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED FLOOR PROXIMITY STRIP AT ROW 5 AND 6 IAW EMB AMM 33 -50-12. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052200044 20070522 00044 EU 2007 5 22 SIMA200714037 1 20070507 A 5315 7253621504 FLOORBEAM SAAB SF340 340B 7860101 EU ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 218AE 22611 5000 340B218 GALLEY FLOOR SUPPORT ANGLE CORRODED AT FS 225. CUTOUT CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW SAAB REPAIR STATEMENT 340SDS012273. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007052200045 20070522 00045 SO 2007 5 22 SIMA200714003 1 20070513 A 3350 66903 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 668HH 8211 145785 FORWARD EMERGENCY LIGHT STRIP INOPERATIVE. REMOVED AND REPLACED LIGHT STRIP IAW EMB AMM 33-50-12. OPERATIONAL CHECK GO OD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007052200048 20070522 00048 NM 2007 5 22 NWAA071816716 1 20070511 A 2612 CIRCUIT CARD BOEING 747 747251F 1384898 NM FIRE DETECTION MALFUNCTIONED A NWAA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 01 616US 21120 DURING CRUISE, PILOT HAD A MOMENTARY "CARGO FIRE " INDICATION, LIGHTS AND FIRE BELL. FLIGHT CONTINUED ON AND LANDING WA S UNEVENTFUL. MAINTENANCE TESTED BOTH LOWER AND MAIN DECK CARGO FIRE WARNING PER AMM 26-14-00, AND REPLACED A8 FIRE WAR NING AND DETECTOR CARD AS A PRECAUTIONARY PER AMM 26-10-00. OPERATIONAL CHECKED GOOD AND A/C OK FOR RETURN TO SERVICE. 2 L 7 4 4F A20WE 2007051700064 20070517 00064 NM 2007 5 17 2007UALA01159 1 20070414 A 5754 STRUCTURE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 13 SLAT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 226UA 20001 30226 NUMBER 13 SLAT APPEARS DAMAGED. REPLACED NR 13 SLAT REF: MM 27-81-15. OP CHECKS GOOD. NO MESSAGES. A/C RETURNED TO S ERVICE. SUSPECT SLAT DAMAGED BY FOD DURING TAKEOFF OR LANDING. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007051700066 20070517 00066 NM 2007 5 17 2007UALA01470 1 20070510 A 3397 58791 FEEDER CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 331UA 24192 EEL LIGHTS INOP ON FLOOR FROM ROW 15 AFT. *S/D* REPLACED POWER FEEDER CABLE IN FLOOR TRACK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007051700074 20070517 00074 2007 5 17 2007UALA01419 4 20070506 A 2565 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 524UA 24977 NUMBER 1 SQUIB TEST FAILURE FOR LEFT EMERGENCY ESCAPE SLIDE. CLEANED AND RELAMPED BULB. [SUP 06-06-07] CLEANED AND RE LAMPED BULB. ACCOMPLISHED SQUIB TEST SEVERAL TIMES ON P61 PANEL. TESTED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007051700085 20070517 00085 NM 2007 5 17 2007UALA01430 1 20070504 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 EEL LIGHT BAR AT THE AFT GALLEY AREA IS BROKEN. REPLACED LIGHT BAR. OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007051700094 20070517 00094 NM 2007 5 17 AWXA200700594 1 20070511 A 5311 6520722501 FRAME BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - FORWARD CARGO COMPARTMENT DOOR CUT OUT FORWARD FRAME CRACKED, BS 440, S24R AT LOWER STOP FITTING. REPAIRED FORWAR D CARGO COMPARTMENT DOOR CUT OUT FORWARD FRAME, BS 440, S24R AT LOWER STOP FITTING IAW AWA ER 03-5332-07128-SS4. 2 L 7 2 4F RT A16WE 2007051700100 20070517 00100 NM 2007 5 17 AWXA200700600 1 20070508 A 5320 D53111412200 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 832AW 1643 SAL - MAJOR REPAIR - CORROSION ON CABIN FLOOR SUPPORT, FR 12 - FR 24, -Y254. REPLACED CABIN FLOOR SUPPORT, FR 12 - FR 24, -Y254 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007051700108 20070517 00108 NM 2007 5 17 2007UALA01440 1 20070507 A 5310 STRUCTURE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE BS 256 LBL 10 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 793UA 26946 STA 256 LBL 10 IS DAMAGED. [SUP 06-01-07] MAJOR REPAIR ACCOMPLISHED DUE TO LIGHTNING STRIKE DAMAGE ON UPPER FUSE BS 25 6 LBL 10. REPAIR ACCOMPLISHED AND INSPECTED. A/C OK FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007051700135 20070517 00135 EU 2007 5 17 UPS07149824 1 20070516 A 2150 A/C PACK AIRBUS A300 A300F4622R 3930360 EU ODOR A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 150UP 0833 DURING ADVANCE OF THRUST FOR TAKEOFF, A STRONG BURNING ODOR ENTERED THE AIR SYSTEM. THE ODOR WAS PERSISTENT UNTIL THRUS T REDUCTION. UPON DESCENT AND LANDING THE SMELL CAME BACK STRONGER. PERFORMED ENGINE RUN AND OPERATED BOTH PACKS. NO DEFECTS NOTED. 2 L 7 2 4F RT A35EU 2007051700141 20070517 00141 2007 5 17 2007UALA01457 4 20070509 A 2565 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 DOOR 1L SLIDE PACK APPEARS TO BE LOOSE. REPLACED SLIDE ASSY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007051700143 20070517 00143 NM 2007 5 17 2007UALA01459 1 20070509 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 EMERGENCY LIGHT ROW 43 ABC INOPERATIVE. [SUP 06-01-07] RELAMPED ROW 43AGC.OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007051700150 20070517 00150 2007 5 17 2007UALA01467 4 20070508 A 2565 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE 3R DOOR STIFF A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 576UA 26690 DOOR 3R DOOR ARM DISARM SWITCH VERY STIFF AND DIFFICULT TO USE. [SUP 06-06-07] REMOVED SLIDE LUBED MECHANISM TO ALLEVI ATE THE STIFFNESS CONDITION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007051700151 20070517 00151 NM 2007 5 17 2007UALA01468 1 20070510 A 3350 32145410 BATTERY PACK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 855UA 1737 EMERGENCY LIGHTS EPSU BATTERY EMERGENCY LEFT MESSAGE. REPLACED BATTERY PACK. GROUND CHECKS OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007051700163 20070517 00163 NM 2007 5 17 AWXA200700607 1 20070506 A 5320 D53472189202 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 832AW 1643 SAL - MAJOR REPAIR - CORROSION ON CABIN FLOORBEAM, FR 68 + 1.5", -Y1192. REPLACED CABIN FLOORBEAM, FR 68 - FR 69, -Y1 192 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007051700164 20070517 00164 NM 2007 5 17 AWXA200700608 1 20070407 A 5311 6546540 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - MAJOR REPAIR - CRACKED FRAME, BS 639, S16R. REPAIRED FRAME, BS 639, S16R IAW AWA ER 03-5362-07122-SS4. 2 L 7 2 4F RT A16WE 2007051700165 20070517 00165 NM 2007 5 17 AWXA200700609 1 20070423 A 5313 143N3110145 STRINGER BOEING 757 7572S7 1384962 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 MCN - MAJOR REPAIR - FOUND CRACKED STRINGER, BS 645, S16L. REPAIRED STRINGER BS 624 - BS 645, S16L IAW B757-200 SRM 53- 00-03-2R1, FIGURE 201. 2 L 7 2 4F RT A2NM 2007051800001 20070518 00001 NM 2007 5 18 DHL2007788516 1 20070501 A 5751 SKIN BOEING 727 727214 138407R NM LT AILERON DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 LT OB AILERON TAB HAS AREA OF DELAMINATION AT OB END UPPER SURFACE. CUTOUT DELAMINATED AREA ON LT OB AILERON TAB UPPER OB END APPROX 1" BY 3 1/2". FABRICATED FILLER APPROX 1" BY 3 1/2" AND DOUBLER APPROX 2 1/2" BY 5" FROM 2024T3 PO NR 900 3621. CLEANED, PREPARED, PRIMED, BONDED, CLEANED, TREATED, PRIMED, AND SEALED EDGES IAW B727 SRM 57-50-2 FIG 8 AND 51-4 0-20. TAB WEIGHT BEFORE REPAIR 3.62 LBS, TAB WEIGHT AFTER REPAIR 3.63 LBS WITHIN LIMITS IAW B727 SRM 51-80 FIG 12. 2 L 7 3 4F A3WE 2007051800012 20070518 00012 NM 2007 5 18 DHL2007788514 1 20070424 A 5753 SKIN BOEING 727 727214 138407R NM LT WING TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT BN593 21958 LEFT WING, INBD FORE FLAP, LOWER SURFACE NEAR TRACK FITTING, LWBL 90, AREA DELAMINATED. CUT OUT DELAMINATED AREA 13" BY 15.5" FABRICATED FILLER, 13" BY 15.5" AND DOUBLER, TWO EACH, 3" BY 15.5" FROM .016, 2024T3. ANODIZED, PRIMED AND APPLI ED ADHESIVE FILM IAW B727 SRM 51-40-20, PAR 8, 14, 15, 18 AND 57-50-2, FIG 3. COMPLETED BONDING, CLEANED, TREATED AND S EALED IAW B727 SRM 51-40-20 AND 51-40-24, FIG 1. 2 L 7 3 4F A3WE 2007051800013 20070518 00013 NM 2007 5 18 DHLA200700025 1 20070511 A 3350 BATTERY BOEING 727 727227 1384078 NM EMERGENCY LIGHT INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 GL 05 784DH 22001 EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY EXIT BATTERIES IAW B-MM 33-50-71, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2007051800016 20070518 00016 NM 2007 5 18 QXEA200700776 1 20070509 A 6123 RELAY DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 355PH 500 SEA FLIGHT NR 2019 ON TAKEOFF, AUTOFEATHER FAILED TO ARM. REPLACED NR 1 POWER LEVER LIMIT SWITCH 6121-S7, ADJUSTED SWIT CH. REPLACED RELAY 6121-K15. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007051800020 20070518 00020 NM 2007 5 18 AALA20070821 1 20070508 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 382AN 25451 SFO - EMERGENCY EXIT LIGHT AT LEFT FORWARD SERVICE DOOR INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT LEFT FORWARD SERV ICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007051800025 20070518 00025 WP 2007 5 18 IXXA07SMN157S 1 20070421 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 500 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE LOWER SKIN HAD A NON STANDARD REPAIR AT STATION XFS 426.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA PERFORMED NDT INSPECTION. NO CRACK OR CORROSI ON AFTER NDT TEST. FABRICATED NEW SKIN AND INTERNAL DOUBLER . CLEANED, TREATED AND PRIMED AREA AND NEW REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACE. INSTALLED REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 07187 DATED 05-03-07, SEMAN DRAWIN G NUMBER ED-4529 DATED 04-20-07, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001,DC8 SRM 51-1-8B, DC8 SRM 51-1-11, 51-1-20D, AND 51-3-1. 2 L 7 4 4F RT 4A25 2007051800026 20070518 00026 WP 2007 5 18 IXXA07SMN152S 1 20070421 A 5340 3640887U FITTING DOUG DC8 DC871F 302199D WP ZONE 100 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT HAD CORROSION ON FITTING ABOVE MAIN LANDING GEAR WHEEL W ELL CEILING BETWEEN STATION 960.000 - 980.000 LEFT BOTTOM LINE 40”. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED C ORRODED FITTING. CLEANED TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-8 PAGE 17 AND 18, DC8 SRM 53- 2-0 PAGE 2P DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-1-8B, AND 51-3-1. 2 L 7 4 4F RT 4A25 2007051800034 20070518 00034 NM 2007 5 18 AALA20070842 1 20070512 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 938AN 29533 MIA - EMERGENCY LIGHT AT SEAT 10D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007051800042 20070518 00042 NM 2007 5 18 AALA20070848 1 20070513 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 787AL 30010 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 24G MISSING LENS. REPLACED LENS FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 24G . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007051800045 20070518 00045 NM 2007 5 18 QXEA200700774 1 20070508 A 3020 D3899924WD97SN CONNECTOR BOMBDR DHC8 DHC8402 1390042 NM ENGINE HEAT DAMAGED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 423QX 4153 SEA - ON FLIGHT 2332, ENGINE ADAPTER HEAT 2 CAUTION LIGHT ILLUMINATED AFTER PUSHBACK. MAINTENANCE REMOVED AND REPLACED C ONNECTOR. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007051800048 20070518 00048 WP 2007 5 18 AALA20070852 1 20070513 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 262AA 49290 DFW - EMERGENCY LIGHT AT SEAT ROW 16 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 16. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007051800057 20070518 00057 NM 2007 5 18 HALA0700026 1 20070116 A 2410 7988502 VALVE BOEING 767 767300 1385204 NM IDG MALFUNCTIONED A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 585HA 24257 BTB - ETOPS SIGNIFICANT SYSTEM, LEFT IDG VALVE LIGHT ON AFTER ENG START. OK TO CONTINUE PER C 75-21-1-3. REPLACED IDG VALVE/HEAT EXCHANGER PER AMM 24-11-12, OPS NORMAL CLEARED MIC SHEET. 2 L 7 2 4F RT A1NM 2007051800061 20070518 00061 2007 5 18 IXXA070027O 4 20070420 A 2340 G515BA2 SPEAKER DOUG DC8 DC862F 3021972 WP COCKPIT DEFECTIVE A IXXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 11 71CX 70211 199 45961 DURING TAXI OUT AT WSAP, THE CREW SMELLED SMOKE, THEN THE FIRST OFFICER'S AUDIO CIRCUIT BREAKER OPEN, THE FIRST OFFICER' S OVER HEAD SPEAKER WAS HOT TO TOUCH, THE CREW RETURNED TO BLOCK WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FIR ST OFFICER'S OVERHEAD SPEAKER, IAW DACO MAINTENANCE MANUAL 23-00. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE . 2 L 7 4 4F 4A25 2007051800065 20070518 00065 NM 2007 5 18 AALA20070835 1 20070511 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 346AN 33085 MIA - EMERGENCY LIGHT AT CEILING LEFT SIDE FIRST CLASS INOPERATIVE. RELAMPED EMERGENCY LIGHT AT CEILING LEFT SIDE FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007051800068 20070518 00068 EU 2007 5 18 AALA20070838 1 20070511 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70074 517 MIA - EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A35EU 2007052100004 20070521 00004 NM 2007 5 21 07FDEA01782 1 20070514 A 5712 RIB BOEING 727 727233 138408A NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 221FE 20932 COMPLY WITH EA 7-5710-102035 WINGS (AD 90-06-09 AND (94-07-08) MAIN FRAME -RIB REPAIR EO 7-5710-7-2308. COMPLIED WITH EA 7-5710-102035 WINGS (AD 90-06-09 AND AD 94-07-08)MAIN FRAME-RIB UPPER CHORD REPAIR EO 7-5710-7-2308 PART 2. 2 L 7 3 4F RT A3WE 2007052100008 20070521 00008 EU 2007 5 21 07FDEA01787 1 20070515 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 401FE 191 MDCC HAS 2 AREAS OF CORROSION ON SEAT TRACK L-4 FRAME 34 AFFECTED AREA MEASURES 2 SQ INCHES. REMOVED CORROSION IAW A3 10 SRM 51-74-10 OUT OF LIMITS IAW A310 SRM53-10-16. REMOVED AND REPLACED SEAT TRACK L-4 IAW A310 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007052100020 20070521 00020 NM 2007 5 21 QXEA200700794 1 20070509 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - CAPTAINS OUTBOARD SEAT TRACK HAS GROVES WORN FROM ROLLER CONTACT AT ALL POSITIONS WHERE THE SEAT HAS BEEN LATCH ED. REPAIRED IAW SRM 53-10-49. 2 H 7 2 4T RT A13NM 2007052100026 20070521 00026 NM 2007 5 21 QXEA200700788 1 20070509 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 165 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - CORROSION ON INBOARD FLANGE OF RIGHT SEAT TRACK NR 12 AT STATION 165.0. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007052100031 20070521 00031 NM 2007 5 21 QXEA200700727 1 20070504 A 3020 4100S02802 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM INTAKE HEAT DAMAGED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 423QX 4153 RNO FLIGHT NR 2444: ENG ADAPT HEAT 2 CAUTION LIGHT. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED NR 2 E NGINE AIR INTAKE WIRE HARNESS FROM WHERE THE HARNESS CONNECTS TO THE INTAKE LIP HEATER TO THE FIREWALL CONNECTOR PLUG 98 11-2601. C/W OPS CHECK OF THE ENGINE AIR INTAKE ANTI-ICING SYSTEM PER Q400 AMM 30-21-00-710-801. OPS CHECK GOOD. NO D EFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007052100032 20070521 00032 NM 2007 5 21 DHL2007788511 1 20070503 A 5753 6521630187 SKIN BOEING 727 727214 138407R NM LT FORE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 LEFT WING INBD FORE FLAP, LWBL 74 UPPER SURFACE DELAMINATED AT EXISTING REPAIR. REMOVED DELAMINATED AREA 2.5" BY 7" CLE ANED AND PREPPED AREA TO BOND IAW B727 SRM 51-40-20, PAR 7, FIG 3. FABRICATED DOUBLER 10" BY 5.7" AND FILLER 2.5" BY 7" FROM .016, 2024T3, ANODIZED, PRIMED AND APPLIED ADHESIVE FILM IAW B727 SRM 51-40-20, PAR 8,14,15,18 AND 51-40-24, FIG 1 AND 57-50-2, FIG 3. INSTALLED, CURED AND FINISHED REPAIR IAW B727 SRM 51-40-20, PAR 20 AND 22, 51-40-24, FIG 1. 2 L 7 3 4F A3WE 2007052100034 20070521 00034 NM 2007 5 21 07FDEA01776 1 20070514 A 5711 ARB74132 SPAR DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 RIGHT WING, REAR SPAR UPPER CAP AT ABOUT STA XORS 1044 FOUND WITH CORROSION REFER TO SNRM NO.: N00247 (SDR TRACKING NO .: 07-1605). COMPLIED WITH FEDEX EA NR 1-5710-109869, WINGS, RIGHT REAR SPAR UPPER CAP CORROSION COMMON TO STATIONS XO RS = 1039 THROUGH XORS = 1047 REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007052100035 20070521 00035 NM 2007 5 21 07FDEA01777 1 20070514 A 5753 SR115700267001 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 LT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CRACKED. LT WING OUTBD FLAP ASSY REMOVED AND REPLACED AS PER MD11 CMM 57-52-04. LT OUTBD FLAP ADJUSTMENT CARRIED OUT AS PER AMM 27-50-00-830-805, FOUND SATIS. 2 L 7 3 4F RT A22WE 2007052100066 20070521 00066 NM 2007 5 21 QXEA200700750 1 20070501 A 5410 DIAPHRAGM BOMBDR DHC8 DHC8402 1390042 NM LT NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - LEFT NACELLE DIAPHRAGM REPAIR IS MISSING FASTENERS AND SMOKING LOCATED ABOVE OUTBOARD FLAP. REPAIRED IAW RD8/4 -54-155 AND SRM 51-42-05. 2 H 7 2 4T RT A13NM 2007052100072 20070521 00072 NM 2007 5 21 DHL2007788522 1 20070424 A 5347 CARGO TRACK BOEING 727 727214 138407R NM BS 790-840 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 MAIN CARGO DECK SEAT TRACK BBL 24L FROM BS 790 - 840 SHOWS CORROSION. FOUND SEAT TRACK CORRODED OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 3. REMOVED SEAT TRACK SECTION AT MAIN CARGO DECK STA 759.45L - 852.45L BBL24L IAW B727 SRM 51-30-2. FA BRICATED NEW SEAT TRACK MAT USED PO NR 7191218 P/N BAC1520-841-7178-T6 DIM 96" LONG IAW B727 SRM 53-10-5 FIG 2 AND 51-30 -5. OK TO TREAT AND PRIME AREA AND PART. TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. OK TO INSTALL SEAT TR ACK. INSTALLED NEW SEAT TRACK IAW B727 SRM 51-30-2 AND 53-10-5 FIG 2. 2 L 7 3 4F A3WE 2007052100083 20070521 00083 NM 2007 5 21 USAA200705U07 1 20070513 A 5340 ATTACH FITTING BOEING 737 7374B7 1384702 NM BS 294 S11L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 A .25 INCH CRACK FOUND AT STA 294.5 S11L. MANUFACTURED & INSTALLED NEW ATTACH CLIP PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007052100094 20070521 00094 NM 2007 5 21 ASAA0741641 1 20070510 A 5512 657378211 SKIN BOEING 737 7374Q8 138447Q NM LT LE STABLIZER DAMAGED A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 773AS 25106 DAMAGE TO LEFT LEADING EDGE HORIZ STAB. REMOVED L/E AND ACCOPMLISHED REPAIR IAW SRM 55-10-01 REPAIR 3. 2 L 7 2 4F RT A16WE 2007052100096 20070521 00096 NM 2007 5 21 DXTA200702184 1 20070510 A 3260 PROXIMITY SWITCH GULSTM 200 200 4500308 NM MLG OUT OF RIG E DXTA O OTHER N FALSE WARNING DE DESCENT 1 GL 07 718QS 136 RIGHT MAIN LANDING GEAR RED INDICATION IN FLIGHT WITH GEAR NOT SELECTED DOWN. INDICATION APPEARED SLOWING BELOW 300 KTS . T/S PROBLEM NOTED RIGHT GEAR DOOR BOX SWITCH TO BE OUT OF RIG. ADJUSTED DOOR PROX SWITCH & PERFORMED OPS CHECK, WITH NO DEFECTS NOTED. 2 L 7 2 4F RT A53NM 2007052100104 20070521 00104 NM 2007 5 21 CALA0700247 1 20070423 A 5320 6517684638 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 294-303 S12L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 INSPECTION FOUND A 1 INCH CRACK IN NR 12 INTERCOSTAL AT STA 294.5-303.9, S12L. A NEW INTERCOSTAL WAS INSTALLED IAW ECRA 5311-01314. 2 L 7 2 4F RT A16WE 2007052100123 20070521 00123 NM 2007 5 21 UPS07M49814 1 20070409 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1831-2007 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C AFT CABIN CORROSION ON SEAT TRACK CROWN & FLANGE AT STA 1966 X=-107. RIGHT NR 4 PASSENGER DOOR SILL R EMOVED. REMOVED SEAT TRACK & ATTACH PARTS STA 1831-2007 RBL 107 PER SRM 51-31-01 VOL 2 REV 38. CORRODED SEAT TRACK TRI MMED OFF. HFEC INSP CUT OUT - NO CRACKS. CORRODED SEAT TRACK REPAIR SPLICE HAT, SPLICE HAT PLATE FAB PER SRM 53-70-00 VOL 1 FIG 7 REV 38. TRACK & FAB PARTS INSTALLED PER SRM 51-31-01 VOL 2 REV 38. 2 L 7 3 4F RT A22WE 2007052100139 20070521 00139 NM 2007 5 21 ZZDA070511162 1 20070511 A 2120 UNKNOWN BOEING 717 717200 1383700 NM ODOR A ZZDA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 15 997AT 55141 ON SHORT FINAL APPROACH ELECTRICAL FIRE ODOR DETECTED, RADAR TURNED OFF, PREDICTIVE WIND SHEAR FAIL ALERT BECAME DISPLAY ED AFTER LANDING BAD POWER TRANSFER BREAK OCCURRED WHEN RIGHT ENGINE SHUTDOWN AFTER THREE MINUTES COOL DOWN PERIOD. PER FORMED WX TEST IAW 717 AMM 34-41-00 NO CURRENT DEFECTS NOTED. INSPECTED WX RT AND ANTENNA, NO ODORS DETECTED IN COMPART MENT, OPERATED PARTS, NO ODOR DETECTED. 2 L 7 2 4F TR A6WE 2007052100145 20070521 00145 EU 2007 5 21 YENA2007035 1 20070516 A 2780 SLAT SYSTEM EMB ERJ190 ERJ190100IGW 3260408 EU LE SLATS FAILED A YENA B EMER. DESCENT J WARNING INDICATION AP APPROACH 1 EA 15 236JB 19000035 FLT 1048, BNA TO JFK, SLAT FAIL. FAULT CODE 27511013EACE PRESENT. PERFORMED FIM TASK 27-81-00-810-805-. CLEARED SF-AC E INHIBITS AS PER AMM 45-45-00. PERFORMED OPS CHECK OF SLAT SYS IAW AMM 27-83-00. ALL FUNCTIONS NORMAL. NO FAULTS ON EICAS. 2 L 7 2 4F RT A57NM 2007052200006 20070522 00006 EU 2007 5 22 SIMA200713503 1 20070509 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS FAILED A SIMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 21 317AE 27867 450 340B317 EMERGENCY ESCAPE FLOOR PROXIMITY PATH LIGHTS INOPERATIVE AT ROW 4 AND ROW 6. REMOVED AND REPLACED EMERGENCY POWER SUPPL Y 22LN AND 23LN IAW SAAB AMM 33-50-10. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007052200049 20070522 00049 WP 2007 5 22 NWAA071809996 1 20070511 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8932E 47141 DURING "H" CHECK, FOUND CRACK IN SKIN AT UPPER CORNER OF 1L DOOR JAMB JUST FORWARD OF A PREVIOUS REPAIR. REPAIRED PER E A 99-208486. 2 L 7 2 4F A6WE 2007052200050 20070522 00050 NM 2007 5 22 NWAA071826314 1 20070511 A 2530 CONTROLLER BOEING 747 747451 1384940 NM OVEN STUCK A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 01 674US 30269 DURING FLIGHT, GALLEY 2-C OVEN 2-45 WAS VERY HOT, AND SMELLED OF BURNING WIRES. PULLED CIRCUIT BREAKERS. FLIGHT CONTIN UED ON AND LANDING WAS UNEVENTFUL. MAINTENANCE FOUND BUTTON STUCK ON OVEN CONTROLLER. REMOVED AND REPLACED OVEN CONTR OLLER. OPERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007052200051 20070522 00051 NM 2007 5 22 NWAA071835514 1 20070512 A 3397 CONNECTOR BOEING 757 757251 1384970 NM EMERGENCY LIGHTS LOOSE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 514US 23202 DURING LINE CHECK, FOUND EMERGENCY FLOOR LIGHTS AT ROWS 23 TO 32 INOPERATIVE. RESET ELECTRICAL PLUG ON POWER SUPPLY. AI RCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2007052200052 20070522 00052 SO 2007 5 22 SIMA200714007 1 20070518 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LAVATORY SMOKE A SIMA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 628AE 5598 3011 145124 CAE312725 RECEIVED LAVATORY SMOKE WARNING ON CLIMB, EMERGENCY DECLARED. RETURNED TO DFW. REMOVED AND REPLACED NUMBER TWO ENGINE IAW AMERICAN EAGLE WORK CARD 72-00-00. OPERATIONAL AND LEAK CHECKS PERFORMED WITH NO DEFECTS, AIRCRAFT RETURNED TO SERV ICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007052200053 20070522 00053 SO 2007 5 22 SIMA200714005 1 20070514 A 2731 3622001015 ACTUATOR EMB 145 EMB145LR 3260212 SO ZONE 300 FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 690AE 6584 14500858 PITCH TRIM INOP MESSAGE AT 37,000 FEET, BACKUP SYSTEM WORKED NORMAL. REMOVED AND REPLACED HORIZONTAL STABLIZER ACTUATOR IAW EMB AMM 27-40-02. OPERATIONAL CHECK GOOD, PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS NOTED. RETURNED AIRCR AFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007052200054 20070522 00054 SO 2007 5 22 SIMA200714010 1 20070520 A 2760 149002 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO ZONE 700 FAILED A SIMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 21 697AB 6662 14500875 SPOILER FAIL CAUTION MESSAGE AND SPOILER OPEN INDICATION ON CLIMB-OUT THROUGH 10,000 FEET. REMOVED AND REPLACED RIGHT W ING OUTBOARD PROXIMITY SENSOR IAW EMB AMM 27-63-04. OPERATIONAL CHECKED GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007052200055 20070522 00055 SO 2007 5 22 SIMA200714008 1 20070518 A 2120 UNKNOWN EMB 135 EMB135LR 3260305 SO COCKPIT ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 707EB 145195 CREW NOTICED BURNING ODOR ON IN THE FLIGHT DECK AFTER LANDING, FLIGHT ATTENDANT NOTICE ODOR IN FRONT PORTION OF CABIN. PERFORMED ENGINE RUNS WITH PACKS ON WITH NO DEFECTS. INSPECTED ELECTRICAL SYSTEMS AND COMPONENTS FINDING NO DEFECTS. R ETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052200057 20070522 00057 EU 2007 5 22 SIMA200714014 1 20070501 A 5311 7253813485 FRAME SAAB SF340 340B 7860101 EU ZONE 200 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 219AE 22769 5000 340B219 FOUND FRAME AT FUSELAGE FRAME 677.0 DENTED. REMOVED AND REPLACED FRAME IAW SAAB SRM 51-40-21, 51-40-40 AND 51-20-50. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007052200060 20070522 00060 EU 2007 5 22 SIMA200714015 1 20070501 A 5311 7253813117 FRAME SAAB SF340 340B 7860101 EU ZONE 200 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 219AE 22769 5000 340B219 FRAME 668.0 FOUND DENTED. REMOVED AND RELACED FRAME IAW SAAB SRM 51-40-21, 51-40-40 AN D51-20-50. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007052200062 20070522 00062 EU 2007 5 22 SIMA200714017 1 20070508 A 5311 7253813485 FRAME SAAB SF340 340B 7860101 EU ZONE 200 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 218AE 22611 5000 340B218 FOUND FUSELAGE FRAME AT FS 677 DAMAGED. REMOVED AND REPLACED DAMAGED FRAME IAW SAAB SRM 51-40-21 AND 51-40-40. AIRCARF T RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007052200064 20070522 00064 EU 2007 5 22 SIMA200714016 1 20070505 A 5311 72537040782 FRAME SAAB SF340 340B 7860101 EU ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 218AE 22611 5000 340B218 PREVIOUS REPAIR ON FRAME 258 FOUND TO BE CORRODED. REMOVED PREVIOUS REPAIR. FABRICATED AND INSTALLED NEW REPAIR PARTS IAW SAAB SRM 53-70-30. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007052200065 20070522 00065 SO 2007 5 22 SIMA200714020 1 20070513 A 5320 13500469403 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 719AE 15875 4800 145276 FLOOR PANEL RISER AT FRAME 22 CORRODED. REMOVED AND REPLACED RISER IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052200066 20070522 00066 SO 2007 5 22 SIMA200714027 1 20070513 A 5347 14530658005 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 719AE 15875 4800 145276 RIGHT SEAT TRACK CORRODED BETWEEN FRAMES 36 AND 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN E AGLE ENGINEERING TECHNICAL NOTICE EM-53-110R2. RETURNED AIRCRAFT TO SERVICE 2 L 7 2 4F RT T00011AT 2007052200068 20070522 00068 SO 2007 5 22 SIMA200714023 1 20070513 A 5340 14524131011 ATTACH BRACKET EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 719AE 15875 4800 145276 PASSENGER DOOR THRESHOLD BRACKETS CORRODED BETWEEN FRAME 17 AND 18. REMOVED AND REPLACED BRACKETS IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052200071 20070522 00071 SO 2007 5 22 SIMA200714022 1 20070513 A 5320 14521721009 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 719AE 15875 4800 145276 FOWARD DIGITAL CORRODED BETWEEN FRAMES 15 AND 18. REPAIRED DIGITAL IAW EMB IC 2007-15/03083. AIRCRAFT RETURNED TO SERV ICE. 2 L 7 2 4F RT T00011AT 2007052200072 20070522 00072 SO 2007 5 22 SIMA200714024 1 20070513 A 5347 13500439001 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 719AE 15875 4800 145276 LEFT SEAT TRACK CORRODED BETWEEN FRAMES 23 AND 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRC RAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052200074 20070522 00074 EU 2007 5 22 SIMA200714030 1 20070509 A 5315 7253721471 FLOORBEAM SAAB SF340 340B 7860101 EU ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 218AE 22769 5000 340B218 GALLEY FLOOR SUPPORT ANGLE AT FS272 CORRODED. CUTOUT CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW SAAB SRM 53-7 0-30. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007052200075 20070522 00075 SO 2007 5 22 SIMA200714032 1 20070516 A 5313 14529152007 STRINGER SPLICE EMB 135 EMB135KL 3260302 SO ZONE 100 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 854AE 9759 4800 145743 STRINGER 19L SPLICE SECTION BETWEEN FRAMES 23 AND 24 DAMAGED. REMOVED DAMAGE AND INSTALLED NEW SPLICE IAW EMB IC2007-14 5/0329A. AIRCARFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052200079 20070522 00079 SO 2007 5 22 SIMA200714031 1 20070514 A 5315 14521413605 FLOORBEAM EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 942LL 4931 14500930 FOUND CORROSION AROUND A NUT PLATE ON THE RIGHT OMEGA BEAM. REMOVED CORROSION, PERFORMED NDT WITH NO REJECTABLE INDICAT IONS. FABRICATED AND INSTALLED A DOUBLER IAW EMB SRM 53-21-10 AND 53-40-02. AIRCARFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007052200080 20070522 00080 SO 2007 5 22 SIMA200714033 1 20070516 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 942LL 4931 14500930 LEFT OMEGA BEAM CORRODED AT FRAME 20. CUTOUT CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10, FIG URE 201, SHEET 1. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007052200082 20070522 00082 EU 2007 5 22 SIMA200714036 1 20070507 A 5320 7253621504 ANGLE SAAB SF340 340B 7860101 EU ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 218AE 22611 5000 340B218 PREVIOUS GALLEY ANGLE REPAIR AT FS225 CORRODED. REMOVED PREVIOUS REPAIR. FABRICATED AND INSTALLED REPAIR PARTS IAW SAA B SRM 51-40-21. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007052200084 20070522 00084 NM 2007 5 22 DL764070565 1 20070517 A 5322 SHEAR TIE BOEING 767 767432ER 1385134 NM BS 1219, BL 0 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 828MH 29699 CORROSION ON AFT CARGO PIT SHEAR TIE AT STA 1219, BL 0. FOUND CORROSION OUT OF LIMITS PER SRM. REMOVED AND REPLACED SH EAR TIE IAW SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007052200085 20070522 00085 NM 2007 5 22 DL764070566 1 20070517 A 5330 SKIN BOEING 767 767432ER 1385134 NM BS 1395 S2L DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 828MH 29699 LIGHTNING STRIKE DAMAGE ON FUSELAGE CROWN SKIN BUTT JOINT AT STA 1395, STR 2L. REPAIRED PER ERA 461548-14 REV ORIG. 2 L 7 2 4F RT A1NM 2007052200086 20070522 00086 NM 2007 5 22 DL764070567 1 20070516 A 5246 5006149A PANEL BOEING 767 767432ER 1385134 NM LT WING MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 844MH 29717 L AUX FUEL PUMP ACCESS PANEL NOTED MISSING ON ARRIVAL. INSTALLED NEW ACCESS PANEL. MCO AND PLACARD REMOVED. 2 L 7 2 4F RT A1NM 2007052200087 20070522 00087 NM 2007 5 22 DL76S070569 1 20070517 A 5330 148T2130 SKIN BOEING 767 767332 1382001 NM FS 1725 S7R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 128DL 24078 DURING INSPECTION OF THE FS 17.25 SKIN AND CHORD STRAP AREA AT S-7R PER 01-451043-03AD, CRACKS WERE FOUND. THE EA PROVI DED A CRACK REPAIR PER 767 SRM 53-80-01 REPAIR 5, HOWEVER THE CRACK EXTENDED OUTSIDE OF THE TYPICAL AREA. DUE TO THIS, BOEING WAS CONTACTED AND PROVIDED AMOC 8100 APPROVAL OF A MODIFIED SRM REPAIR PER ERA 461617-14AD. 2 L 7 2 4F RT A1NM 2007052200089 20070522 00089 NM 2007 5 22 DL764070571 1 20070518 A 2611 SMOKE DETECTOR BOEING 767 767432ER 1385134 NM MALFUNCTIONED A DALA O OTHER N FALSE WARNING CR CRUISE 1 SO 27 837MH 29710 BOTH SMOKE DETECTORS AT 4R ALARMED NO APPARENT SMOKE OR FIRE. PERFORMED TEST ON SMOKE DETECTORS ALL INDICATIONS NORMAL. INSPECTED BOTH 4R LAVS NO EVIDENCE OF FIRE OR OVERHEAT HEAT DETECTOR DECALS CHK GOOD. NO TROUBLE FOUND, NO HISTORY OK FOR SVC. 2 L 7 2 4F RT A1NM 2007052200090 20070522 00090 NM 2007 5 22 DL76G070572 1 20070519 A 5330 143T32114 SKIN BOEING 767 767332 1382001 NM FS 577 S28L PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 16065 30199 SKIN STRUCK BY GRND EQUIP AT FS 577 BELOW S28L AND CABIN PRESSURE STATIC PORT. DAMAGE CUT OUT AND REPAIR DOUBLER INSTAL LED. 2 L 7 2 4F RT A1NM 2007052200093 20070522 00093 NM 2007 5 22 DL76S070577 1 20070521 A 5343 FRAME BOEING 767 767332 1382001 NM MLG ATTACH CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 128DL 24078 DURING HMV INSPECTION FOUND RT MLG SUPPORT BEAM SIDE FRAME LUG FWD FLANGE AND BORE SURFACE HAD PITTING CORROSION. FLANG E AND BORE SURFACE CORROSION REMOVED PER SRM 53-50-90. 2 L 7 2 4F RT A1NM 2007052200098 20070522 00098 NM 2007 5 22 DL76G070554 1 20070216 A 5740 113T11673 FITTING BOEING 767 7673P6 1385105 NM TE FLAPS CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 155DL 25269 CORROSION WAS FOUND IN THE ATTACH HOLES OF THE LT AND RT INBOARD FLAP SUPPORT BEAMS. THE HOLES WERE OVERSIZED TO REMOVE THE CORROSION AND BUSHED. 2 L 7 2 4F RT A1NM 2007052200102 20070522 00102 NM 2007 5 22 DLM88070558 1 20070225 A 5512 5922578515 SKIN DOUG MD88 MD88 3023688 NM HORIZONTAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 994DL 53346 RT HORIZONTAL STABILIZER SKIN WAS FOUND CRACKED IN UPPER SKIN, 0.75 IN. LONG. THE CRACK WAS CUT OUT OF THE SKIN AND A N EW SKIN WILL BE INSTALLED WITHIN 2000 FLIGHT HOURS. 2 L 7 2 4F RT A6WE 2007052200103 20070522 00103 NM 2007 5 22 DLM90070559 1 20070228 A 5512 5922578521 SKIN DOUG MD90 MD9030 3023690 NM HORIZONTAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 THE RT UPPER SKIN PANEL ON THE HORIZONTAL STABILIZER WAS FOUND CRACKED. THE CRACKED SKIN WAS CUT OUT AND A NEW SKIN PAN EL WILL BE INSTALLED WITHIN 2000 FLIGHT HOURS. 2 L 7 2 4F RT A6WE 2007052200105 20070522 00105 NM 2007 5 22 DL757070561 1 20070513 A 5330 146N3700111 SKIN BOEING 757 757232 1384965 NM FS 1705 S20L PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 A SERVICE TRUCK STRUCK THE FUSELAGE PUNCTURING THE SKIN AT FS 1705, S20L. THE DAMAGED SKIN WAS CUT OUT AND A REPAIR DOU BLER WAS INSTALLED. 2 L 7 2 4F RT A2NM 2007052200107 20070522 00107 NM 2007 5 22 HALA0700102 1 20070314 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 481HA 55126 ON CLIMB-OUT ITO, LIGHTNING STRIKE RT UPPER AREA ABOVE COCKPIT. ACCOMPLISHED TASK CARD HAL M584-717 EXAMINE FOR LIGHTNI NG STRIKE, OK FOR SERVICE. 2 L 7 2 4F TR A6WE 2007052200108 20070522 00108 NM 2007 5 22 SWAA072528 1 20070520 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052200109 20070522 00109 NM 2007 5 22 SWAA072526 1 20070520 A 5310 6546817 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 312-344 S17L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM CHORD CORRODED BETWEEN BS 312 AND BS 344, STR 17L. REPAIRED CHORD PER SRM . 2 L 7 2 4F RT A16WE 2007052200110 20070522 00110 NM 2007 5 22 SWAA072517 1 20070520 A 5754 65C26601 SKIN BOEING 737 7373H4 1384600 NM RT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING NR 5 L/E SLAT INBOARD T/E DELAMINATED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007052200111 20070522 00111 NM 2007 5 22 SWAA072508 1 20070518 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727C S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007052200113 20070522 00113 NM 2007 5 22 SWAA072534 1 20070520 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 520 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052200114 20070522 00114 NM 2007 5 22 SWAA072535 1 20070520 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 597 S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052200115 20070522 00115 NM 2007 5 22 SWAA072536 1 20070520 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 616 S5L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052200116 20070522 00116 NM 2007 5 22 SWAA072537 1 20070520 A 5313 BAC1498 STRINGER BOEING 737 7373Q8 1384670 NM BS 727C S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER 8R CRACKED AT BS 727C. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007052200117 20070522 00117 NM 2007 5 22 SWAA072530 1 20070520 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 773 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 728SW 27860 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 773, BETWEEN LBL 12.5 AND RBL 8.1. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007052200120 20070522 00120 2007 5 22 SWAA072516 4 20070520 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVA C SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052200125 20070522 00125 SO 2007 5 22 C2XA07IA118 1 20070516 A 3350 20131A BATTERY PACK EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14168 13878 770 14500840 IAH - DURING MAINTENANCE INSPECTION THE LT AND RT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE A IRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007052200126 20070522 00126 NM 2007 5 22 SWAA072527 1 20070520 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052200128 20070522 00128 NM 2007 5 22 SWAA072434 1 20070517 A 3350 10107451 SIGN BOEING 737 737301 1384611 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED PM CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007052200129 20070522 00129 NM 2007 5 22 SWAA072447 1 20070517 A 3350 1619 LAMP BOEING 737 737317 138447P NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER M M. 2 L 7 2 4F RT A16WE 2007052200130 20070522 00130 NM 2007 5 22 SWAA072442 1 20070517 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 712SW 27846 DURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 138.7. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007052200132 20070522 00132 NM 2007 5 22 SWAA072432 1 20070517 A 3350 20131 BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED A2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007052200133 20070522 00133 NM 2007 5 22 SWAA072448 1 20070517 A 3350 20131 BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED HC1 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007052200134 20070522 00134 NM 2007 5 22 SWAA072430 1 20070517 A 3350 311500 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 729SW 27861 DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 19 DEF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007052200135 20070522 00135 NM 2007 5 22 SWAA072415 1 20070517 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 456WN 32463 EEPLS COVER LOOSE AT ROW 5 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007052200136 20070522 00136 NM 2007 5 22 SWAA072420 1 20070516 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 487WN 33854 EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007052200137 20070522 00137 NM 2007 5 22 SWAA072422 1 20070517 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 202WN 33999 DURING SCHEDULED MV3 CHECK, FOUND EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007052200138 20070522 00138 2007 5 22 SWAA072411 4 20070514 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 466WN 30677 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052200143 20070522 00143 NM 2007 5 22 SWAA072446 1 20070517 A 5330 6545765 SKIN BOEING 737 7375H4 138449D NM BS 747 S17L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 17L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007052200147 20070522 00147 NM 2007 5 22 SWAA072425 1 20070516 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 967 S25L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 967, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007052200149 20070522 00149 NM 2007 5 22 SWAA072401 1 20070513 A 5330 6545800 SKIN BOEING 737 7375H4 138449D NM BS 259 S23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007052200150 20070522 00150 NM 2007 5 22 SWAA072402 1 20070513 A 5330 6545800 SKIN BOEING 737 7375H4 138449D NM BS 259 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007052200151 20070522 00151 NM 2007 5 22 SWAA072406 1 20070513 A 5312 6545819 PRESSURE PANEL BOEING 737 7373T5 1384608 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED MV1 CHECK, FOUND NLG W/W PRESSURE PANEL WEB CRACKED AT RIGHT BS 246, WL 170. REPAIRED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2007052200153 20070522 00153 NM 2007 5 22 SWAA072418 1 20070515 A 5340 6546543 SUPPORT FITTING BOEING 737 7373H4 1384600 NM BS 685 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SERVICE CHECK, FOUND RIGHT BS 685 MLG SUPPORT FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2007052200154 20070522 00154 NM 2007 5 22 SWAA072421 1 20070515 A 5330 6546765 SKIN BOEING 737 7375H4 138449D NM BS 747 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007052200156 20070522 00156 NM 2007 5 22 SWAA072419 1 20070515 A 5743 655223537 FITTING BOEING 737 7373H4 1384600 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SERVICE CHECK, FOUND LEFT WING AFT MLG STABILIZER FITTING CORRODED. REMOVED AND REPLACED STABILIZER FI TTING PER MM. 2 L 7 2 4F RT A16WE 2007052200157 20070522 00157 NM 2007 5 22 SWAA072427 1 20070515 A 3350 6556633 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 428WN 29844 DURING SCHEDULED MV3 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007052200158 20070522 00158 2007 5 22 SWAA072416 4 20070517 A 2565 65C16820 HOOK BOEING 737 7377H4 1384404 NM R1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 223WN 32492 R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2007052200160 20070522 00160 NM 2007 5 22 SWAA072409 1 20070516 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 636WN 27709 R1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007052200161 20070522 00161 NM 2007 5 22 SWAA072453 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 767 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052200163 20070522 00163 NM 2007 5 22 SWAA072454 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500D S2R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052200173 20070522 00173 NM 2007 5 22 AWXA200700650 1 20070417 A 5330 654576656 SKIN BOEING 737 73733A 1384673 NM BS 489 S14R CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - FOUND CRACKED FUSELAGE SKIN, BS 489, S14R. REPAIRED FUSELAGE SKIN, BS 489, S14R IAW B737-300 SRM 5 3-00-01-2R30, FIGURE 201. 2 L 7 2 4F RT A16WE 2007052200174 20070522 00174 NM 2007 5 22 AWXA200700651 1 20070417 A 5330 654576656 SKIN BOEING 737 73733A 1384673 NM BS 491 S14R CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - C-20 CHECK, CRACKED FUSELAGE SKIN, BS 491, S14R. REPAIRED FUSELAGE SKIN, BS 491, S14R IAW B737-300 SRM 53-00-01-2R30, FIGURE 201. 2 L 7 2 4F RT A16WE 2007052200176 20070522 00176 EU 2007 5 22 AWXA200700636 1 20070503 A 5321 D5361060500100 FLOOR PANEL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 665AW 1644 SAL - MAJOR REPAIR - CORROSION ON CABIN FLOOR BOARD 222 FF, FR 16 - FR 20, -Y1292 TO -Y1732. REPLACED CABIN FLOOR BOARD 222 FF, FR 16 - FR 20, -Y1292 TO -Y1732 IAW AWA TASK CARD C1C53302. 2 L 7 2 4F RT A28NM 2007052200178 20070522 00178 NM 2007 5 22 AWXA200700638 1 20070510 A 5340 69353521 STRINGER CLIP BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - FOUND CRACKED STRINGER CLIP, BS 727E, S22L. REPLACED STRINGER CLIP, BS 727E, S22L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007052200179 20070522 00179 NM 2007 5 22 AWXA200700639 1 20070420 A 5313 65457679 STRINGER BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - CRACKED STRINGER, BS 500C, S16L. REPAIRED STRINGER, BS 500C, S16L IAW AWA ER 03-5312-01094 . 2 L 7 2 4F RT A16WE 2007052300003 20070523 00003 NM 2007 5 23 2007UALA01534 1 20070517 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 510UA 24780 RIGHT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300005 20070523 00005 NM 2007 5 23 2007UALA01536 1 20070517 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 510UA 24780 EXTERIOR EMERGENCY LIGHTS INOP AT DOORS L1, L2, AND 3L. [SUP 06-06-07] REPLACED BATTERY AND RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300007 20070523 00007 2007 5 23 2007UALA01538 4 20070517 A 2565 LINE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EVAC SLIDE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 805UA 783 NR 1 MED SLIDE MOORING LINE WORN THRU 80 PERCENT. [06-26-07] REPLACED NR 1 SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052300008 20070523 00008 NM 2007 5 23 2007UALA01540 1 20070516 A 3260 WARNING LIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT ILLUMINATED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 927UA 26649 CREW COMMENTS: UPON RAISING GEAR AFTER TAKEOFF, LEFT AND RIGHT RED GEAR LIGHTS STAYED ON & RIGHT GREEN GEAR. CREW HAD CYCLED GEAR AFTER INDICATION POST TO, ALL GEAR LIGHTS WERE GREEN AFTER. MTC PERFORMED SEVERAL TESTS ONCE IN HANGAR IN CLUDING MANUAL EXTENTION AND SEVERAL GEAR CYCLES- NO DEFECTS COULD BE DUPLICATED. THIS CONDITION HAS NOT RETURNED TO TH E A/C SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007052300009 20070523 00009 NM 2007 5 23 2007UALA01541 1 20070517 A 3250 ROD END BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU NLG WORN A UALA O OTHER E VIBRATION/BUFFET LD LANDING 1 WP 29 941UA 26676 NOSE WHEEL VIBRATES DURING LANDING AND TAXI. [06-14-07] FOUND PLAY IN STEERING ACTUATOR CONNECTING RODS ATTACH POINT BUSHINGS. REPLACED LEFT AND RIGHT NLG STEERING ACTUATOR ROD ENDS, ATTACHING BOLTS AND BUSHINGS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007052300010 20070523 00010 NM 2007 5 23 2007UALA01542 1 20070517 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DIRTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 596UA 28749 DOOR 2L WILL NOT ARM. [06-14-07] REMOVED DEBRIS FROM GIRT BAR AREA, SECURED COSMETIC SEAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300011 20070523 00011 NM 2007 5 23 2007UALA01543 1 20070518 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT SMOKE A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 585UA 26709 SMOKE AND FUMES IN THE COCKPIT. [06-14-07] ON PREFLT CHECK WHEN FLT CREWS TURNED ON WINDOW HEAT, ACRID ODOR NOTICE D. FOUND 1L WINDOW POWER TERMINAL BURNED & ASSOCIATED TERMINAL CAP MELTED. NOTICED CAPT'S FLOOD LIGHTS WERE INOP, WHEN FLOOD LIGHT RHEOSTAT TURNED TO FULL BRIGHT, ODOR REAPPEARED. ISOLATED FAULT DOWN TO CAPTAINS & CENTER PANEL FLOODLIGHT CONTROL UNIT, WHICH IS LOCATED BEHIND PANEL NEAR RUDDER. RESET LIGHT BREAKERS, LIGHT WORKED NORMAL & NO SIGN OF SMOKE O R ODOR WITH C.BREAKER FOR CAPTS NR 1 FRONT WINDOW HEAT OPEN AND DEFFERED. REPLACED WINDOW AND WINDOW HEAT CONTROLLER, P RECAUTIONARY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300012 20070523 00012 NM 2007 5 23 2007UALA01544 1 20070516 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 AFT CARGO STA 1420 LEFT SIDE FRAME HAS A DENT STR 27L. [06-14-07] MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE SKIN AN D INSTALLED REPAIR ANGLE PER UA ENGINEERING SPECIFICATIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300013 20070523 00013 NM 2007 5 23 2007UALA01545 1 20070516 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 FWD CARGO STA 600 LEFT SIDE FRAME DENTED STR 24L. [06-14-07] MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE SKIN, REPLACED PRODUCTION SLICE AND REPAIRED DAMAGED AREA PER UA ENGINEERING SPECIFICATIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007051800049 20070518 00049 WP 2007 5 18 AALA20070853 1 20070513 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 262AA 49290 DFW - EMERGENCY LIGHT AT SEAT ROW 16 INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT ROW 16. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F A6WE 2007051800056 20070518 00056 NM 2007 5 18 QXEA200700777 1 20070501 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - SEAT TRACK JUST INBOARD AND AFT OF ACCESS 144JZ HAS CORROSION. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007051800058 20070518 00058 2007 5 18 HALA0700023 4 20070112 A 3460 4052500923 FMC BOEING 767 767300 1385204 NM LEFT UNKNOWN A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 585HA 24257 BTB - CAPT L FMC QUIT AFTER ENG START. RETURNED TO GATE WHEN APU GEN TRANSFERRED L FMD START AGAIN. RAN BOTH ENGS. CO ULD NOT DUPLICATE PROBLEM. AS PRECAUTION RERACKED L FMC. GND OPS CHK OK PER AMM 34-61-01. PERFORMED TASK 30, NO FAULT S NOTED. A/C OK TO REMAIN IN LAND 3. 2 L 7 2 4F RT A1NM 2007051800073 20070518 00073 NM 2007 5 18 AALA20070828 1 20070510 A 2530 251000308 OVEN BOEING 757 757223 1384957 NM GALLEY INOPERATIVE A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 192AN 32386 MAN T95/10MAY - AFT GALLEY NUMBER ONE OVEN CIRCUIT BREAKER POPPED PRECEDED BY ELECTRICAL FUMES AND SMOKE ALARM. CIRCUIT BREAKER TRIPPED AND COLLARED. AIRCRAFT DISPATCHED TO BOS IN ACCORDANCE WITH PDL 25 99M. REPLACED AFT GALLEY NUMBER ON E OVEN IN BOS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007051800074 20070518 00074 NM 2007 5 18 AALA20070829 1 20070510 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 384AA 26996 DFW - BATTERY PACK AT M739 FOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT M739 FOR EMERGENCY LIGHTS. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007052100009 20070521 00009 WP 2007 5 21 IXXA07SMN150S 1 20070421 A 5311 FRAME DOUG DC8 DC871F 302199D WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FRAME FLANGE WITH A CRACK AT STATION 1580.000 LONGERON 2 1LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED FRAME SEGMENT. FABRICATED NEW FRAME SEGMENT. P ERFORMED HEAT TREATMENT TO FRAME SEGMENT AND ANGLES. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALAN T TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0 FIGURE 2 SHEETS 4 AND 6, DC8 SRM 51-1-21, DC8 SRM 53-4- 1 FIGURE 51 SHEET 21 ITEM A, DC8 SRM 53-2-0 FIGURE 2 SHEET 1, DC8 SRM 53-2-0 FIGURE 2 SHEETS 7 AND 8, T/R NUMBER 53-110 DATED 11-10-00,DC8 SRM 51-1-1 PAGES 1, 13, 17,DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-20D, AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007052100019 20070521 00019 NM 2007 5 21 QXEA200700796 1 20070509 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - FO'S INBOARD SEAT TRACK HAS GROVES FROM ROLLER CONTACT AT ALL POSITIONS WHERE THE SEAT HAS BEEN LATCHED. REPAI RED IAW SRM 53-10-49. 2 H 7 2 4T RT A13NM 2007052100021 20070521 00021 NM 2007 5 21 QXEA200700795 1 20070509 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - CAPTAINS INBOARD SEAT TRACK HAS GROVES WORN FROM ROLLER CONTACT AT ALL POSITIONS WHERE THE SEAT HAS BEEN LATCHE D. REPAIRED IAW SRM 53-10-49. 2 H 7 2 4T RT A13NM 2007052100025 20070521 00025 NM 2007 5 21 QXEA200700787 1 20070509 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - SURFACE CORROSION ON CENTER RIGHT SEAT TRACK NR 10 AT STATION 1.5. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007052100040 20070521 00040 NM 2007 5 21 EIA2007094 1 20070313 A 5322 SHEAR TIE BOEING 747 747212B 1384886 NM BS 240 MISINSTALLED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 482EV 20713 FOUND FRAME SHEAR TIE AT BODY STATION 240 BETWEEN STRINGER 34A AND 36 WITH TOO BIG A GAP AFTER SKIN REPLACEMENT. SHEAR TIE REMOVED AND FABRICATED PER B747 SRM 53-10-04, INSTALLED PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007052100041 20070521 00041 NM 2007 5 21 EIA2007097 1 20070506 A 2120 UNKNOWN BOEING 747 747131 1384881 NM COCKPIT SMOKE A EIAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 479E 19898 AFTER APPROX 10 MIN FLT, CREW DETECTED SMOKE IN THE COCKPIT, WHICH CAUSED THE LAV SMOKE ALARM TO SOUND. BATHROOM SMOKE ALARM SOUNDED, F/O INVESTIGATED AND FOUND HEAVY LIQUID MIST IN UPPER AND MAIN DECK AREA. MIST HAD NO ODOR. AIRCRAFT IN SPECTED, ELECTRICAL SYSTEM, ACM AND ENGINE RUNS PERFORMED, NO DEFECT NOTED DURING INSPECTION, AIRCRAFT HAS FLOWN WITHOUT ANY OCCURRENCE AFTER INSPECTION CONDUCTED. 2 L 7 4 4F A20WE 2007052100046 20070521 00046 NM 2007 5 21 AWXA200700615 1 20070509 A 5310 5007945249 DOOR FRAME BOEING 737 73733A 1384673 NM ZONE 800 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - CRACKED L1 DOOR FRAME AFT SIDE, BS 347, S13L - S14L, AT NR 5, 6, 7 FROM TOP STOP PIN CUTOUTS. REPAIRED L1 DOOR FR AME AFT SIDE, BS 347, S13L - S14L IAW AWA ER 03-5210-07128-SS3. 2 L 7 2 4F RT A16WE 2007052100051 20070521 00051 NM 2007 5 21 HALA0700204 1 20070509 A 4900 UNKNOWN BOEING 767 767300 1385204 NM APU UNKNOWN A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 588HA 33466 ETOPS SIGNIFICANT SYSTEM, APU AUTO SHUT DOWN AS PACKS WERE TURN OFF FOR ENG START. PERFORMED FIM 49-11-00 FIG 103 APU B ITE, NO FAULTS NOTED. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007052100088 20070521 00088 EA 2007 5 21 TRAX200700666 1 20070513 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT NO TEST A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 836AS 7263 LEFT OVERWING EMERGENCY EXIT DOOR FAILED FUNCTIONAL TEST. REFER TO TASK 000-52-830-104. [07-23-07] REPAIRED IAW; AMM 12-20-52, AND AMM 52-21-00. 2 L 7 2 4F RT A21EA 2007052100097 20070521 00097 CE 2007 5 21 DXTA200702185 1 20070510 A 2910 D45C24 PRESSURE SWITCH CESSNA 560 560XL 2076702 CE HYD SYSTEM INOPERATIVE E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 658QS 514 5605665 AFTER FLAPS WERE SELECTED UP, HYD PRESS ANNUNCIATOR REMAINED ILLUMINATED. AFTER 40 SECONDS -STAB MISCOMP- ANNUNCIATOR A LSO ILLUMINATED WITH FLASHING MASTER CAUTION. RAN AIRCRAFT ON EITHER & BOTH ENGINES CYCLED FLAPS FOUND STABS OPERATION WITHIN TIME LIMITS. (22 SECONDS FULL TRAVEL). CONNECTED GROUND HYDRAULIC UNIT. FOUND OPERATION STILL WITHIN LIMITS. (NO CHANGE) SUSPECT AIRSPEED SWITCH. (TAH32256). C/W AIRSPEED SWITCH CHECK, RESISTANCE BETWEEN PIN A AND B NOT TO BE I NFINITE. REMOVED & REPLACED AIR SPEED SWITCH IAW 560 XL MM 27-40-00. C/W LEAK TEST IAW 560 XL MM 34-11-08, MM 604. PO SITION HORIZONTAL STAB IAW 560XL MM 27-40-00. SYSTEM OPS TEST OKAY. 2 L 7 2 4F RT A22CE 2007052100121 20070521 00121 NM 2007 5 21 UPS07M49810 1 20070318 A 5315 FLOORBEAM DOUG MD11 MD11F 3023600 NM BS 1841 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C CENTER CARGO, STA 1841 BETWEEN RBL 4 & 22, FLOORBEAM WEB FWD FACE ATTACHED MID CHORD, CORROSION FOUND AT SEVERAL SPOTS. CORROSION ON FLOORBEAM WEB FACE MID CHORD REMOVED SRM 51-21-01VOL II R38. ORI THK 0.080" MATL REMOVE D 0.060" (RBL 4"-10") MATL REMAINING 0.020" FOUND OUT OF LIMIT SRM 53-00-01 FIG 3 VOL I R38. NEW CHORD FAB BOEING DWG A CA7170RT USE MATL S2932021-7075T6511. CORRODED CHORD REMOVED & NEW CHORD INSTALLED AT STA 1841 FROM RBL 42" TO LBL 42" PER SRM 51-31-01 VOL II R39. 2 L 7 3 4F RT A22WE 2007052100133 20070521 00133 EA 2007 5 21 COMA0760373 1 20070516 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FS 559 RBL 18 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 956CA 7105 DURING 559 INSPECTION FOUND .5 INCH CRACK AT BASE OF VERTICAL STIFFENER, FS 559, RBL 18. REMOVED DAMAGE AND INSTALLED D OUBLER PER REO 601R-53-41-067. 2 L 7 2 4F RT A21EA 2007052100136 20070521 00136 NM 2007 5 21 UPS07M49818 1 20070414 A 5320 A5A707110 INTERCOSTAL DOUG MD11 MD11F 3023600 NM BS 5-53-5-73 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C CABIN - INTERCOSTAL FOUND CRACKED AT L7 RIGHT STA 5-53 TO 5-73. EXISTING INTERCOSTAL & ATTACHED PARTS AT L7 RIGHT STA 5-53 TO 5-73 REMOVED PER SRM 51-31-01 VOL 2 REV 38. INTERCOSTAL P/N:A5A7071-10, FAB PER BOEING DWG A5A 7071. INTERCOSTAL HEAT TREATED & ALODINED PER SRM 51-21-01 VOL 2 REV 38. FASTENER HOLES PICKUP ON FAB INTERCOSTAL. FA B INTERCOSTAL & ATTACHED PARTS INSTALLED PER SRM 51-31-01 VOL 2 REV 38. 2 L 7 3 4F RT A22WE 2007052100138 20070521 00138 EA 2007 5 21 COMA0760374 1 20070516 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FS 559, RBL9 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 956CA 7105 DURING 559 INSPECTION FOUND 2 INCH CRACK ON INBOARD SIDE AND .5 INCH CRACK AT OUTBOARD SIDE OF VERTICAL STIFFENER, RBL 9 , FS 559. REMOVED DAMAGE AND INSTALLED DOUBLERS PER REO 601R-53-41-520. 2 L 7 2 4F RT A21EA 2007052100140 20070521 00140 NM 2007 5 21 ZZDA070513163 1 20070513 A 5311 FRAME BOEING 717 717200 1383700 NM BS 1178 L16-18L CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 937AT 55091 CRACK ON CANTED FRAME STA 1178.225 BETWEEN LONGERON 16 LT AND 18 LT. INSTALLED ANGLE REPAIR 16 X 2 INCHES MAT USED 7075 .0 0.80. HEAT TREATMENT TO 7075T6 GENERAL PROCESS SPECIFICATION 98 PMS 247.PS 01 AS PER SRM 51-70-11. 2 L 7 2 4F TR A6WE 2007052100143 20070521 00143 NM 2007 5 21 CALA0700252 1 20070516 A 5311 652072284 FRAME BOEING 737 737524 1384721 NM BS 400 S17-28R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 58606 27319 INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR CUTOUT FORWARD FRAME AT LOWER STOP PAD, STA 400, S17R TO S28R. A NEW FRAME WAS INSTALLED IAW SRM 51-10-02 AND 51-40-00. 2 L 7 2 4F RT A16WE 2007052200118 20070522 00118 2007 5 22 SWAA072515 4 20070520 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED MV3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052300017 20070523 00017 EU 2007 5 23 2007UALA01549 1 20070519 A 5320 ANGLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 412UA 465 RIGHT WHEEL WELL LOWER FUSELAGE BELLY FAIRING SUPPORT ANGLE 5 IN RBL IS CRACKED AT FRAME 40. MAJOR REPAIR ACCOMPLISHED: REPLACED ANGLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052300023 20070523 00023 NM 2007 5 23 2007UALA01555 1 20070520 A 2530 OVEN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE GALLEY ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 813UA 858 CREWS REPORTS ELECTRICAL BURNING ODOR IN CABIN. [06-26-07] PERFORMED MULTIPLE OPERATIONAL CHECKS AT VARIOUS STATIONS W ITH NO FURTHER BURNING ODOR. OVEN WAS REPLACED 2 DAYS PRIOR, SO SUSPECT THAT ODOR WAS FROM DIRT OR DEBRIS BURNING OFF TH AT WAS GATHERED WHILE UNIT WAS IN STORAGE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052300025 20070523 00025 2007 5 23 2007UALA01557 4 20070520 A 2565 COVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EVAC SLIDE UNSECURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 456UA 1128 CREW REPORT: 2 RT DOOR HANDLE COVER SEPARATED FROM A-C. [06-26-07] RESECURED SLIDE COVER. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052300027 20070523 00027 NM 2007 5 23 2007UALA01562 1 20070520 A 3350 58783362624 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 309UA 23670 EEL LIGHTS INOP AFT OF ROW 18. REPLACED CABLE & TWO LAMPS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007052300028 20070523 00028 NM 2007 5 23 2007UALA01563 1 20070520 A 3350 1619 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 328UA 24148 LEFT & RIGHT OVERWING EMERGENCY LIGHTS ARE INOP. RELAMPED EMERGENCY LIGHT, OP CHECKS OKAY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007052300029 20070523 00029 NM 2007 5 23 2007UALA01564 1 20070519 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY CEILING LIGHT ABOVE ROW 34 RIGHT INOP. RELAMPED EMERGENCY LIGHT, OK CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052300034 20070523 00034 NM 2007 5 23 2007UALA01569 1 20070520 A 3397 794640 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EEL AT DOOR 5L XAISLE INOP. SECURED LAMP CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052300041 20070523 00041 NM 2007 5 23 2007UALA01576 1 20070520 A 2121 FAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN MALFUNCTIONED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 521UA 24891 ACRID SMOKEY SMELL IN CABIN AND RIGHT RECIRC FAN WENT INOP AS WELL. RIGHT RECIRC TURNED OFF AND SMELL DISSIPATED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300043 20070523 00043 NM 2007 5 23 2007UALA01578 1 20070518 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 584UA 26706 DOOR 1R WILL NOT ARM. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300044 20070523 00044 NM 2007 5 23 2007UALA01579 1 20070518 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 585UA 26709 EMERGENCY EXIT SLIDE LIGHT INOP AT DOOR 4R. [SUP 06-06-07] RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300045 20070523 00045 EU 2007 5 23 2007UALA00637 1 20070302 A 5270 E00800208C CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FWD CARGO DOOR LOOSE A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 405UA 45414 452 CREW REPORTS FWD CARGO DOOR ECAM ON CLIMB. FOUND A LOOSE CONNECTOR ON DOOR SWITCH. RESECURED, INDICATES OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052300046 20070523 00046 NM 2007 5 23 2007UALA01240 1 20070420 A 2420 2B751A TRANSFORMER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN SHORTED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 662UA 27159 ELECTRICAL POWER PROBS CAUSED RTFL. REPLACED CURRENT TRANSFORMER T9000. REF WDM25-31-12, WDM25-31-13, WDM33-31-13 & WD M33-27-12. RELUGGED WIRE (32-16) AT C9010 W12 DUE TO HEAT DAMAGE. PERFORMED LOAD TEST AND LOAD SHED TEST OPS CHECKS NO RMAL REF GNMM02-0-21-001. APPLIED POWER TO GALLEY AND TESTED ALL FUNCTIONS. ALL FUNCTIONS TESTED NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007052300051 20070523 00051 EU 2007 5 23 2007UALA01485 1 20070511 A 3520 LANYARD AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN IMPROPER PART A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 454UA 1104 CABIN SEAT 7ABC OXYGEN MASKS HAVE WRONG PARTS. GENERATOR IS MISSING FOAM AT FWD END AND LANYARDS ARE THE WRONG TYPE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052300057 20070523 00057 NM 2007 5 23 2007UALA01491 1 20070511 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 303UA 23644 EEL LIGHTING INOPERATIVE IN AFT CABIN & GALLEY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007052300058 20070523 00058 NM 2007 5 23 SWAA072475 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300059 20070523 00059 NM 2007 5 23 SWAA072496 1 20070517 A 3350 101073 LENS BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007052300060 20070523 00060 NM 2007 5 23 SWAA072503 1 20070517 A 5753 6546435 FLAP BOEING 737 7375H4 138449D NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND LEFT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007052300067 20070523 00067 NM 2007 5 23 SWAA072494 1 20070517 A 5322 6546569 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 987, STR 23R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007052300068 20070523 00068 NM 2007 5 23 SWAA072486 1 20070517 A 5322 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 908, STR 24L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007052300069 20070523 00069 NM 2007 5 23 SWAA072504 1 20070517 A 5754 65C26601 SLAT BOEING 737 7375H4 138449D NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING NR 5 L/E SLAT UPPER INBOARD T/E DELAMINATED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007052300071 20070523 00071 NM 2007 5 23 SWAA072473 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727F, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007052300072 20070523 00072 NM 2007 5 23 SWAA072476 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300073 20070523 00073 NM 2007 5 23 SWAA072474 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300074 20070523 00074 NM 2007 5 23 SWAA072477 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300077 20070523 00077 NM 2007 5 23 SWAA072470 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300079 20070523 00079 NM 2007 5 23 SWAA072468 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300080 20070523 00080 NM 2007 5 23 SWAA072485 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300084 20070523 00084 NM 2007 5 23 SWAA072480 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007052300086 20070523 00086 NM 2007 5 23 SWAA072482 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007052300087 20070523 00087 NM 2007 5 23 SWAA072465 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300088 20070523 00088 NM 2007 5 23 SWAA072484 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300089 20070523 00089 NM 2007 5 23 SWAA072487 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300091 20070523 00091 NM 2007 5 23 SWAA072489 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300093 20070523 00093 NM 2007 5 23 SWAA072491 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300094 20070523 00094 NM 2007 5 23 SWAA072492 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300100 20070523 00100 NM 2007 5 23 SWAA072532 1 20070520 A 5315 140A0346 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 728SW 27860 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 345, RBL 1. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007052300101 20070523 00101 NM 2007 5 23 SWAA072531 1 20070520 A 5315 140A0346 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 728SW 27860 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 343, RBL 1. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007052300102 20070523 00102 NM 2007 5 23 SWAA072512 1 20070519 A 3350 20131A BATTERY PACK BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED SERVICE CHECK, FOUND RIGHT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007052300103 20070523 00103 NM 2007 5 23 SWAA072509 1 20070519 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 776WN 30591 EEPLS COVER LOOSE AT ROW 5 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007052300104 20070523 00104 NM 2007 5 23 SWAA072514 1 20070520 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 247WN 32508 EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007052300106 20070523 00106 NM 2007 5 23 SWAA072523 1 20070520 A 5315 6545410 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED BETWEEN BS 657 AND BS 669, LBL 24.5. REPAIRED FLOORBE AM PER EA. 2 L 7 2 4F RT A16WE 2007052300109 20070523 00109 NM 2007 5 23 SWAA072518 1 20070520 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 890, STR 25R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007052300110 20070523 00110 NM 2007 5 23 SWAA072519 1 20070520 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 870, STR 25R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007052300113 20070523 00113 NM 2007 5 23 SWAA072513 1 20070519 A 5311 6546526 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052300115 20070523 00115 NM 2007 5 23 SWAA072450 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300116 20070523 00116 NM 2007 5 23 SWAA072456 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300118 20070523 00118 NM 2007 5 23 SWAA072464 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300121 20070523 00121 NM 2007 5 23 SWAA072461 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300122 20070523 00122 NM 2007 5 23 SWAA072462 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300127 20070523 00127 NM 2007 5 23 SWAA072408 1 20070516 A 3397 AMCO2RAO3W CONNECTOR BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 207WN 34012 EMERGENCY EXIT LIGHT INOP AT ROW 11C. FOUND LOOSE CONNECTOR, SECURED LOOSE CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2007052300128 20070523 00128 NM 2007 5 23 SWAA072424 1 20070516 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED SERVICE CHECK, FOUND STRINGER 27R CORRODED AT BS 964. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007052300131 20070523 00131 2007 5 23 SWAA072413 4 20070517 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052300132 20070523 00132 2007 5 23 SWAA072403 4 20070513 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052300133 20070523 00133 2007 5 23 SWAA072426 4 20070517 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 635SW 27708 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052300134 20070523 00134 NM 2007 5 23 SWAA072443 1 20070517 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 712SW 27846 DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007052300135 20070523 00135 NM 2007 5 23 SWAA072440 1 20070517 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 438WN 29833 DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2007052300136 20070523 00136 NM 2007 5 23 SWAA072439 1 20070517 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 438WN 29833 DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED ND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007052300137 20070523 00137 NM 2007 5 23 SWAA072437 1 20070517 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 438WN 29833 DURING SCHEDULED HC2 CHECK, LEFT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK P ER MM. 2 L 7 2 4F RT A16WE 2007052300141 20070523 00141 NM 2007 5 23 SWAA072400 1 20070512 A 3350 MS155721 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007052300142 20070523 00142 NM 2007 5 23 SWAA072414 1 20070517 A 2560 PH22300L GLOWSTRIP BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 EEPLS PHOTOLUMINESCENT STRIP MISSING AT ROW 3 DEF. INSTALLED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007052300143 20070523 00143 NM 2007 5 23 ASAA0791649 1 20070517 A 5321 453A161079 FLOOR PANEL BOEING 737 737990 NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 FWD CARGO PIT FLOOR PANEL NR 3 IS CORRODED. REPAIRED IAW SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007052300145 20070523 00145 NM 2007 5 23 ASAA0791651 1 20070517 A 5321 453A161083 FLOOR PANEL BOEING 737 737990 NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 FWD CARGO PIT FLOOR PANEL NR 5 CORRODED. REPAIRED IAW SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007052300150 20070523 00150 NM 2007 5 23 ASAA0791659 1 20070517 A 5347 146A750614 SPLICE BOEING 737 737990 NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO PIT TIE DOWN SPLICE CORRODED. REPAIRED IAW SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007052300163 20070523 00163 NM 2007 5 23 ASAA0791672 1 20070517 A 5321 453A261037 FLOOR PANEL BOEING 737 737990 NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO FLOOR PANEL CORRODED. REPAIRED IAW SRM 51-40-02. 2 L 7 4 4F RT A16WE 2007052300164 20070523 00164 NM 2007 5 23 ASAA0791673 1 20070517 A 5321 453A261057 FLOOR PANEL BOEING 737 737990 NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO FLOOR PANEL CORRODED. REPAIRED IAW SRM 51-40-02. 2 L 7 4 4F RT A16WE 2007052300169 20070523 00169 NM 2007 5 23 ASAA0791678 1 20070517 A 5320 143A750214 INTERCOSTAL BOEING 737 737990 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 FWD CARGO PIT INTERCOSTAL CRACKED. REPAIRED IAW SRM 53-30-53 FIG 2. 2 L 7 4 4F RT A16WE 2007052300170 20070523 00170 NM 2007 5 23 2007UALA01492 1 20070513 A 3397 CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 304UA 23665 AFT 15 FEET OF EEL TRACK LIGHTS ARE OUT ON LEFT SIDE OF FLOOR. [SUP 06-06-07] REPLACED FEEDER CABLE ON FLOOR AND EEL STRIP ON FLOOR IN GALLEY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007052300172 20070523 00172 NM 2007 5 23 2007UALA01494 1 20070512 A 3260 HORN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU WARNING SYSTEM FAULTY A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 309UA 23670 LANDING GEAR WARNING HORN CANNOT BE SILENCED WITH BUTTON. [06-14-07] REPLACED AURAL WARNING UNIT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007052300178 20070523 00178 NM 2007 5 23 2007UALA01501 1 20070512 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 508UA 24744 EEL LIGHT MISSING SEAT 16C. [SUP 06-06-07] REPLACED LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300184 20070523 00184 NM 2007 5 23 ASAA0791684 1 20070517 A 5320 149A810989 BEAM BOEING 737 737990 NM FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO PIT VERTICAL BEAM CHAFED. REPAIRED IAW SRM 51-40-02. 2 L 7 4 4F RT A16WE 2007052300185 20070523 00185 NM 2007 5 23 ASAA0791685 1 20070517 A 5347 14647150119 CARGO TRACK BOEING 737 737990 NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO PIT TIE DOWN TRACK CORRODED. REPAIRED IAW SRM 53-00-53. 2 L 7 4 4F RT A16WE 2007052300190 20070523 00190 NM 2007 5 23 2007UALA01503 1 20070514 A 5310 DOOR FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 925UA 26646 FWD CARGO DOOR CUTOUT FRAME, AFT FRAME IS CRACKED IN TWO PLACES AT LOWER BOTTOM STOP FITTING ONE CRACK IS IN RADIOUS ON AFT SIDE OF FRAME AND THE OTHER ON FWD SIDE OF FRAME, BOTH CRACKS ARE LOCATED AT I/B UPPER CORNER OF STOP FITTING VERIFI ED BY HFEC. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED FWD CARGO DOOR CUTOUT AFT FRAME. 2 L 7 2 4F 4 F RT A16WE E21EU 2007052300193 20070523 00193 EU 2007 5 23 2007UALA01506 1 20070512 A 2697 RELAY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SMOKE WARNING INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 446UA 834 ON CARGO SMOKE TEST AGENT 2 DISCHARGE LIGHT DOES NOT ILLUMINATE. [06-29-07] FAULT TRACED TO A FAULTY RELAY. REPLACED 17WX DISCHARGE 2 LIGHT RELAY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052300195 20070523 00195 NM 2007 5 23 2007UALA01509 1 20070513 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 29 581UA 26701 VERBAL FROM CREW - SMOKEY, BURNING, CHEMICAL ODOR IN FIRST CLASS CABIN. SMELL WAS NOTICED BY SEVERAL PASSENGERS AND FLT ATTENDANTS. ODOR WAS NOTICED ON TAKEOFF AND LANDING. [SUP 06-06-07] RAN LT AND RT ENGINES BLEEDS ON & OFF, PACKS ON EACH PNEUMATIC SYSTEM ISOLATED, PACKS OPERATED OFF APU, RECIRC FAN ON AND OFF, NO ODORS DETECTED. CAUSE OF ODOR COULD N OT BE DETERMINED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300199 20070523 00199 NM 2007 5 23 2007UALA01514 1 20070515 A 5310 DOOR FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 925UA 26646 FWD CARGO DOOR CUTOUT FWD FRAME IS CRACKED AT O/B LOWER CORNER OF LOWER STOP FITTING. MAJOR REPAIR: REMOVED DAMAGE. F ABRICATED AND INSTALLED EXTERNAL NESTED ANGLES AND FILLER REPAIR. REFERENCE MM 53-30-75. 2 L 7 2 4F 4 F RT A16WE E21EU 2007052300201 20070523 00201 NM 2007 5 23 2007UALA01516 1 20070515 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 AFT CARGO STA 1440 LEFT SIDE FRAME HAS DENT STR 25L. [SUP 06-06-07] MAJOR REPAIR ACCOMPLISHED. SPLICED IN DOUBLER RE PAIR, THIS IS A TIME LIMITED REPAIR FOR 12 MONTHS FROM 08 MAY07 UNLESS A NEW FAA 8100-9 IS ISSUED PRIOR TO THAT TIME IN COMPLIANCE WITH 14 CFR 25.571. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300202 20070523 00202 NM 2007 5 23 2007UALA01517 1 20070516 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BS 2080 S35R CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 195UA 26899 EXTERNAL FUSELAGE SKIN CORRODED AT RIGHT WASTE VENT OUTLET APPROX BS 2080 STR 35R. [SUP 06-01-07] MAJOR REPAIR ACCOMP LISHED: CUTOUT CORROSION. INSTALLED EXTERNAL DOUBLER/TRIPLER REPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052300203 20070523 00203 NM 2007 5 23 2007UALA01518 1 20070516 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 AFT CARGO COMPARTMENT BS 727B AT STR 20L STRINGER CLIP IS CRACKED. MAJOR REPAIR: REMOVED AND REPLACED STRINGER CLIP. REFERENCE SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2007052300204 20070523 00204 NM 2007 5 23 2007UALA01519 1 20070516 A 2421 GENERATOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LEFT DISCONNECTED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 799UA 26926 LEFT GENERATOR DISCONNECTED DUE TO LOW OIL PRESSURE. FLIGHT DIVERTED. [06-14-07] REMOVED AND REPLACED LEFT IDG. ACC OMPLISHED SERVICE AND LEAK CHECK. ACCOMPLISHED 5 MIN IDLE RUN AND FOUND NO LEAKS. OK FOR SERVICE. SUSPECT SEAL LEAKAGE PROBLEM. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007052300207 20070523 00207 NM 2007 5 23 SWAA072569 1 20070521 A 5320 6545401 STIFFENER BOEING 737 7373G7 1384595 NM RT MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED SPV CHECK, FOUND RIGHT MLG W/W VERTICAL STIFFENER CRACKED AT BS 663, RBL 6.15. REMOVED AND REPLACED ST IFFENER PER ACO. 2 L 7 2 4F RT A16WE 2007052400001 20070524 00001 NM 2007 5 24 SWAA072541 1 20070521 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 735E AND BS 747, STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007052400002 20070524 00002 EU 2007 5 24 DHLA200700028 1 20070517 A 2150 A/C PACK AIRBUS 300 A300B4203 3930306 EU NR 2 ODOR A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 05 362DH 084 STRONG ODOR WAS OBSERVED ON FLIGHT DECK AFTER TURNING OFF PACK NR 2 ODOR WENT AWAY. DEFFERED NR 2 PACK IAW MEL 21-51-01 CAT C ASSIGNED CONTROL NR 29073 PLACARDS INSTALLED. 2 L 7 2 4F RT A35EU 2007052400005 20070524 00005 EU 2007 5 24 CPCP20070023 1 20070418 A 5210 SUPPORT AEROSP ATR72 ATR72212 8680945 EU PAX DOOR CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 308AE 308 LT AFT PASSENGER DOOR THREAD SUPPORT 5 IS CORRODED. NEW THREAD SUPPORT 5 INSTALLED IAW SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007052400006 20070524 00006 NM 2007 5 24 DHLA200700029 1 20070519 A 2170 COALESCER BAG BOEING 727 727227 1384078 NM ODOR A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 05 784DH 22001 CHEMICAL/BURNING ODOR COMING FROM PACKS WHEN SUPPLIED BY ENGINE AIR MORE EVIDENT AT HIGH POWER SETTINGS. REMOVED AND RE PLACED LEFT AND RT PACK WATER SEPARATOR COALESCER IAW M/M 21-55-51 P/N 22D10 RAN ALL ENGINES IAW JRH 5.2, NO ODORS OR DE FECTS NOTED. 2 L 7 3 4F A3WE 2007052400008 20070524 00008 NM 2007 5 24 ASAA0741655 1 20070520 A 5753 65C3570329 SKIN BOEING 737 7374Q8 138447Q NM T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 LEFT WING O/B FORE FLAP LOWER SURFACE HAS MULTIPLE DENTS. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007052400009 20070524 00009 NM 2007 5 24 ASAA0741652 1 20070520 A 5320 654587573 WEB BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 WEB BELOW R1 DOOR CUTOUT IS CORRODED ON LOWER SURFACE. REMOVED CORRODED WEB, FABRICATED AND INSTALLED NEW WEB IAW SRM 5 1-40-02. 2 L 7 2 4F RT A16WE 2007052400010 20070524 00010 EU 2007 5 24 CPCP20070025 1 20070418 A 5310 STRUCTURE AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 308AE 308 LT GUTTER CORRODED BETWEEN FRAME 36 AND 39. NEW LT GUTTER BETWEEN FRAME 36 AND 39, INSTALLED IAW SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007052400011 20070524 00011 EU 2007 5 24 CPCP20070022 1 20070418 A 5210 SUPPORT AEROSP ATR72 ATR72212 8680945 EU PAX DOOR CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 308AE 308 LT AFT PASSENGER DOOR THREAD SUPPORT 1(BOTTOM) IS CORRODED. NEW THREAD SUPPORT 1 (BOTTOM), INSTALLED IAW SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007052400014 20070524 00014 EU 2007 5 24 CPCP20070016 1 20070323 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 420AT 420 CORROSION FOUND ON LT I/B SEAT TRACK AT FRAME 36. TRACK LT I/B AT FRAME 36 REPAIRED IAW SRM 53-00-00 FIG 434. 2 H 7 2 4T RT A53EU 2007052400015 20070524 00015 NM 2007 5 24 DHL2007788526 1 20070518 A 5410 NOSE COWL BOEING 727 727214 138407R NM NR 1 NACELLE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 WHILE IN C CHECK AT FLIGHT STAR, NR 1 ENG NOSE COWLING 9:00 POS AFT END COWLING FAYING SURFACE IS WORN AWAY AND KNIFE ED GED. CUT OUT DAMAGED AREA ON NR 1 ENGINE NOSE COWLING AFT END 9:00 POSITION IAW B727 SRM 54-10-03 FIG3. CUTOUT AREA 5" BY 75", FABRICATED DOUBLER FILLER AND STRAP ON NR 1 ENG NOSE COWLING AFT END 9:00 POS IAW B727 SRM 51-20-01 AND B727 SR M 54-10-03 FIG 3. DOUBLER AND FILLER AND STRAP MATERIAL 7075-T6-.063 PO NR 9004042 DOUBLER DIM 10" BY .75" BY 1" FILLER DIM 4.98" BY 1" STRAP DIM 8" BY .75" IAW B727 SRM 54-10-03 FIG 3 SHT 2. TREATED AND PRIMED NR 1 ENG NOSE COWLING DOUBL ER AND FILLER AND STRAP IAW B727 SRM 51-10-2. INSTALLED FABRICATED DOUBLER, FILLER, STRAP ON NR 1 ENG COWLING AFT END 9 2 L 7 3 4F A3WE 2007052400016 20070524 00016 SO 2007 5 24 CHQA200700016 1 20070515 A 2120 UNKNOWN EMB 135 EMB135KL 3260302 SO COCKPIT ODOR A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 11 373SK 145543 FLIGHT 5334 - STL-BNA - ON SHORT FINAL, SMOKE AND BURNING/ELECTRICAL ODOR IN COCKPIT AND CABIN. APU WAS OFF, PACKS ON, ANTI-ICE OFF, ENGINES AT 60 PERCENT N1. OPERATED COCKPIT AND CABIN RECIRCULATION FANS IAW EMB MM 21-24-01. BOTH TEST N ORMAL. RAN APU, BOTH ENGINES, BOTH PACKS, BOTH RECIRCULATION FANS; COULD NOT DUPLICATE SMOKE ODOR. 2 L 7 2 4F RT T00011AT 2007052400019 20070524 00019 NM 2007 5 24 ASAA0791644 1 20070517 A 5320 143A812210 WEB BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 FWD CARGO DOORWAY LWR WEB FOUND CORRODED. REPAIRED IAW SRM 51-40-02. 2 L 7 4 4F RT A16WE 2007052400020 20070524 00020 NM 2007 5 24 07FDEA01819 1 20070515 A 5753 65192502 FLAP TRACK BOEING 727 7272S2F 1384O81 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 LEFT WING TE OB FLAP OB TRACK IS CORRODED AT AFT ATTACH POINT. TRACK ASSEMBLY REPLACED ON FED EX W/C 27X5707-01 REF MM 27-51-031-4. 2 L 7 3 4F A3WE 2007052400026 20070524 00026 NM 2007 5 24 QXEA200700802 1 20070511 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 780 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - PITTING AT LEFT CENTER SEAT TRACK NR 9 AT STATION 780.0. REPAIRED IAW SRM 51-42-05, 51-21-10, 51-42-05, AND 51 -40-15. 2 H 7 2 4T RT A13NM 2007052400027 20070524 00027 NM 2007 5 24 ASAA0791647 1 20070517 A 5321 453A161013 FLOOR PANEL BOEING 737 737990 NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 FWD CARGO FLOOR PANEL NR 1 CORRODED. REPAIRED IAW SRM 51-40. 2 L 7 4 4F RT A16WE 2007052400030 20070524 00030 NM 2007 5 24 QXEA200700801 1 20070512 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 416 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - CORROSION IN CENTER CHANNEL OF CENTER SEAT TRACK NR 7 AT STATION 416.0. REPAIRED IAW RD8/4-53-884 AND RD8/4-53 -1913. 2 H 7 2 4T RT A13NM 2007052400031 20070524 00031 NM 2007 5 24 QXEA200700803 1 20070516 A 5410 DIAPHRAGM BOMBDR DHC8 DHC8402 1390042 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - LEFT NACELLE DIAPHRAGM CRACKED. REPAIRED IAW SRM 51-42-00. 2 H 7 2 4T RT A13NM 2007052400032 20070524 00032 EA 2007 5 24 TRAX200700679 1 20070516 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 882AS 7503 LEFT FS 640 FUSELAGE SKIN BONDED DOUBLER IS CRACKED JUST AFT OF THE BOX BEAM. [07-23-07] COMPLIED WITH REO 601R-53-6 1-506 REPAIRED BONDED DOUBLER REFER TO EC/TC EO REO 601R-53-61-506. 2 L 7 2 4F RT A21EA 2007052400033 20070524 00033 NM 2007 5 24 QXEA200700805 1 20070512 A 5310 DOOR FRAME BOMBDR DHC8 DHC8402 1390042 NM BS 696 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - AFT SERVICE DOOR FRAME IS CHAFED BY A FLOOR BOARD AT STATION X696. REPAIRED IAW RD8/4-53-1914. 2 H 7 2 4T RT A13NM 2007052400040 20070524 00040 EA 2007 5 24 TRAX200700670 1 20070514 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 974EV 7594 1ST AND 2ND FROM FRONT CEILING EMERGENCY LIGHTS INOP. 2 L 7 2 4F RT A21EA 2007052400042 20070524 00042 EA 2007 5 24 TRAX200700672 1 20070515 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 836AS 7263 CREW ESCAPE HATCH 3 EXTERIOR PLACARDS WORN. THE RED ARROW FOR DIRECTIONS, OPEN & EMERGENCY EXIT, PUSH TO RELEASE AND TU RN TO OPEN PLACARDS. [07-23-07] REMOVED AND REPLACED THREE (3) LISTED EXTERIOR PLACARDS ON CREW ESCAPE HATCH IAW CRJ 200 AMM 11-20-00. 2 L 7 2 4F RT A21EA 2007052400043 20070524 00043 NM 2007 5 24 QXEA200700807 1 20070512 A 5511 SPAR BOMBDR DHC8 DHC8402 1390042 NM HORIZONTAL STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - THERE ARE LOOSE RIVETS ON THE LEFT HORIZONTAL STAB FORWARD LOWER SPAR FLANGE AT YH 0 TO YH 24. REPAIRED IAW SR M 51-42-45. 2 H 7 2 4T RT A13NM 2007052400044 20070524 00044 NM 2007 5 24 QXEA200700808 1 20070511 A 5511 SPAR BOMBDR DHC8 DHC8402 1390042 NM HORIZONTAL STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - THERE ARE LOOSE RIVETS ON THE LEFT HORIZONTAL STAB FORWARD UPPER SPAR FLANGE AT UH 0 TO YH 24. REPAIRED IAW SR M 51-42-45. 2 H 7 2 4T RT A13NM 2007052400045 20070524 00045 NM 2007 5 24 QXEA200700814 1 20070512 A 5753 SKIN BOMBDR DHC8 DHC8402 1390042 NM RT WING TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - RIGHT WING OUTBOARD FLAP UPPER SURFACE HAS A CHAFE IN SKIN FROM WING TRAILING EDGE SEAL LOCATED AT YW 211 TO YW 264. REPAIRED IAW SRM 51-21-10, 51-25-10, 57-52-30. 2 H 7 2 4T RT A13NM 2007052400046 20070524 00046 EA 2007 5 24 TRAX200700673 1 20070515 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 836AS 7263 CRACK FOUND AT FS 484 AT RBL 27 OUTBOARD ON INTERCOSTAL. REMOVED CRACKED ANGLE AT FS 484 AT RBL 27 O/B INTERCOSTAL IAW REO 601R-53-41-059. INSTALLED NEWLY MANUFACTURED CLIP. (.063, 2024-T3, PO 9345-1) IAW REO 601R-53-41-059. SUPPLEMENTA L - SDR CLOSED 05/22/07. 2 L 7 2 4F RT A21EA 2007052400047 20070524 00047 NM 2007 5 24 UIEA200700221 1 20070507 A 5415 ATTACH ANGLE BOEING 747 7472D7B 1384803 NM NR 1 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 NR 1 PYLON AFT MOUNT BULKHEAD FITTING CAP SKIN ATTACH ANGLE BOTH SIDES FOUND CRACKED. THE CHORD CRACKED FLANGES WERE RE MOVED BY TRIMMING PER SRM 51-10-01. THE EDGES AND FASTENER HOLE WERE NDT INSPECTED. FILLERS AND REPAIR ANGLES WERE INS TALLED ON FORWARD AND AFT SIDES OF THE LEFT AND RIGHT CHORDS PER BOEING DOCUMENT 1-320850399-1. 2 L 7 4 4F RT A20WE 2007052400048 20070524 00048 NM 2007 5 24 UIEA200700222 1 20070507 A 5415 ATTACH ANGLE BOEING 747 7472D7B 1384803 NM NR 3 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 NR 3 PYLON AFT MOUNT BULKHEAD FITTING CAP SKIN ATTACH ANGLE BOTH SIDES FOUND CRACKED. THE CHORD CRACKED FLANGES WERE RE MOVED BY TRIMMING PER SRM 51-10-01. THE EDGES AND FASTENER HOLES WERE NDT INSPECTED. FILLERS AND REPAIR ANGLES WERE IN STALLED ON FORWARD AND AFT SIDES OF THE LEFT AND RIGHT CHORDS PER BOEING DOCUMENT 1-320831752-4. 2 L 7 4 4F RT A20WE 2007052400049 20070524 00049 NM 2007 5 24 UIEA200700223 1 20070507 A 5415 ATTACH ANGLE BOEING 747 7472D7B 1384803 NM NR 4 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 NR 4 PYLON AFT MOUNT BULKHEAD FITTING CAP SKIN ATTACH ANGLE BOTH SIDES FOUND CRACKED. THE CHORD CRACKED FLANGES WERE RE MOVED BY TRIMMING PER SRM 51-10-01. THE EDGES AND FASTENER HOLES WERE NDT INSPECTED. FILLERS AND REPAIR ANGLES WERE IN STALLED ON FORWARD AND AFT SIDES OF THE LEFT AND RIGHT CHORDS PER BOEING DOCUMENT 1-321346972-4. 2 L 7 4 4F RT A20WE 2007052400050 20070524 00050 EU 2007 5 24 07FDEA01809 1 20070515 A 5330 A53778736 SKIN AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 CORROSION BEHIND DME ANTENNA C30-31 BOTTOM CENTERLINE REPAIR PERFORMED BY BLEND OUT, APPROVED BY EA 6-5313-106471 AND RA S/DABRE/7007755/2007 ISS. B 2 L 7 2 4F RT A35EU 2007052400051 20070524 00051 EA 2007 5 24 TRAX200700683 1 20070517 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 836AS 7263 SEAT TRACK ON FLOOR UNDER OVERHEAD BIN 1 AB SHOWS SIGNS OF CORROSION TO FWD SECTION OF TRACK. [SUP 05-24-07] REMOVED A ND REPLACED SEAT TRACK P/N 601R-31032-15 IAW CRJ 200 AMM 53-01-11. 2 L 7 2 4F RT A21EA 2007052400053 20070524 00053 NM 2007 5 24 QXEA200700831 1 20070520 A 2750 FLAP SYSTEM BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 NM 09 415QX 4081 SEA FLIGHT NR 2072: ON APPROACH, FLAP POWER CAUTION LIGHT ILLUMINATED. FLAPS STUCK AT 10 DEGREES. AIRCRAFT RETURNED TO FIELD. MAINTENANCE USED FIM 27-50-00-810-802 FOR TROUBLE SHOOTING. VERIFIED NO FAULTS IN CDS. PERFORMED OPS TEST OF FLAP SYSTEM IAW Q400 AMM 27-50-00-710-801. NO DEFECTS NOTED. NOTE FLAP POWER CAUTION CLEARED DURING RESET OF CDS AMM 4 5-00-27-743-801. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007052100087 20070521 00087 EA 2007 5 21 TRAX200700665 1 20070513 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT NO TEST A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 836AS 7263 RIGHT OVERWING EMERGENCY EXIT DOOR FAILED FUNCTIONAL TEST. REFER TO TASK 000-52-830-104. REPAIRED IAW; AMM 12-20-52, A ND AMM 52-21-00. 2 L 7 2 4F RT A21EA 2007052100101 20070521 00101 NM 2007 5 21 CALA0700244 1 20070504 A 5330 146A7402 DOUBLER BOEING 737 737724 13844BY NM BS 787-847 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17719 28938 INSPECTION FOUND THE AFT LAV SERVICE PANEL (INNER DOUBLER) CORRODED AT STA 787-847, S25L TO S26L. THE DOUBLER WAS REMOV ED AND REPLACED IAW SRM 51-10-02, PAGE 8, FIGURE 1. 2 L 7 2 4F RT A16WE 2007052100111 20070521 00111 NM 2007 5 21 ASAA0741636 1 20070516 A 5320 6552878125 SILL BOEING 737 7374Q8 138447Q NM BS 915-1006 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 LEFT AFT MOP SILL CORRODED (INNER CHORD). REMOVED CORRODED SILL, REPLACED SILL WITH NEW PART IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007052100120 20070521 00120 NM 2007 5 21 UPS07M49692 1 20070323 A 5230 GUARD DOUG MD11 MD11F 3023600 NM CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C LWR AFT CARGO DOOR VENT DOOR PROTECTION GUARD LWR SURFACE FOUND MINOR SURFACE CORROSION. CORROSION RE MOVED PER SRM 51-21-01VOL II R38 ORI THK 0.063" MATL REMOVED 0.040" MATL REMAIN 0.023" FOUND OUT OF LIMIT PER SRM 52-00- 01 FIG 1 A VOL I R38. NEW ANGLE FAB PER BOEING DWG AGA7494 USING MATL 2024-O-0.063". HEAT TREATED PER DPS7.00-1 & HARD VALUE HRB65-5 PER DPS1.05-3. PICK UP HOLES & PROTECTED PER SRM 51-31-01 & 51-21-01 VOL II R38. INSTALLED PER SRM 51-3 5-01 VOL II R38. 2 L 7 3 4F RT A22WE 2007052100125 20070521 00125 NM 2007 5 21 UPS07M49816 1 20070414 A 5320 AFA776121 INTERCOSTAL DOUG MD11 MD11F 3023600 NM BS 1661-1681 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C CABIN - INTERCOSTAL FOUND CRACKED AT L7 RIGHT STA 1661 - 1681. EXISTING INTERCOSTAL & ATTACH PARTS L7 RIGHT STA 1661-1681 REMOVED PER SRM 51-31-01 VOL 2 REV 38. INTERCOSTAL P/N:AFA7761-21 FAB PER BOEING DWG AFA7761 REV D . INTERCOSTAL HEAT TREATED, ALODINED PER SRM 51-21-01 VOL 2 REV 38. FASTENER HOLES PICKUP ON FAB INTERCOSTAL & PAINTED . FAB INTERCOSTAL & ATTACHED PARTS INSTALLED PER SRM 51-35-01 VOL 2 REV 38. 2 L 7 3 4F RT A22WE 2007052100126 20070521 00126 NM 2007 5 21 UPS07M49817 1 20070414 A 5320 AFA77619 INTERCOSTAL DOUG MD11 MD11F 3023600 NM BS 1541-1561 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C CABIN - INTERCOSTAL FOUND CRACKED AT L7 RIGHT STA 1541 - 1561. EXISTING INTERCOSTAL & ATTACHED PARTS STA 1541-1561 L7 LEFT REMOVED PER SRM 51-31-01 VOL 2 REV 38. INTERCOSTAL P/N AFA7761-9 FAB PER BOEING DWG AFA7761 REV D . INTERCOSTAL HEAT TREAT & ALODINED PER SRM 51-21-01 VOL 2 REV 38. FASTENER HOLES PICKUP ON FAB INTERCOSTAL. FAB INTE RCOSTAL & ATTACHED PARTS INSTALLED PER SRM 51-31-01 VOL 2 REV 38. 2 L 7 3 4F RT A22WE 2007052100130 20070521 00130 EA 2007 5 21 TRAX200700660 1 20070512 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 847AS 7335 CAPT'S FLASHLIGHT DEAD. 2 L 7 2 4F RT A21EA 2007052100137 20070521 00137 NM 2007 5 21 UPS07M49819 1 20070504 A 5340 ABA712125ABA71 ATTACH ANGLE DOUG MD11 MD11F 3023600 NM BS 383-401 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C COCKPIT - STA 383 - 401 APPROX LBL 4 WEB P/N: ABA7121-25 & ABA7121-39 CLIP ANGLE FOUND CRACKED. ATTAC H CRACK INTERCOSTAL FASTENERS & INNER SUPPORT PARTS REMOVED PER SRM 51-31-01 VOL 2 REV 38. NEW INTERCOSTAL P/N:ABA7121- 25 & CLIP ABA7121- 39 FAB PER DWG ABA7121. INTERCOSTAL & CLIP HEAT TREATED PER DPS7.00-1 NEW INTERCOSTAL & CLIP FASTENE R HOLES PICKUP & REPROTECTED. FAB IN INTERCOSTAL & CLIP INSTALLED PER SRM 51-31-01 VOL 2 REV 38. 2 L 7 3 4F RT A22WE 2007052200026 20070522 00026 EU 2007 5 22 07FDEA01799 1 20070515 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 DUMMY TRACK IN FWD PIT FR 38.2 TO FR 40 TH NR 5 WORN .040 REMOVED AND REPLACED 2 FLOOR BOARDS IAW A310/200 AMM53-10-25-4 . REMOVED AND REINSTALLED 1 DUMMY TRACK SECTION AND ATTACHING PARTS IAW A310 SRM 51-40-21. REPAIRED HOLE IN DUMMY SEAT TRACK IAW A310/200 SRM53-15-16. 2 L 7 2 4F RT A35EU 2007052200056 20070522 00056 EU 2007 5 22 SIMA200714011 1 20070502 A 5347 7253742409 SEAT TRACK SAAB SF340 340B 7860101 EU ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 218AE 22611 5000 340B218 FOUND SEAT TRACK 36R TO BE CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SAAB SRM 53-70-60. RETURNED AIRCRAFT TO SERVI CE. 2 L 7 2 4T RT A52EU 2007052200058 20070522 00058 EU 2007 5 22 SIMA200714012 1 20070505 A 5311 7253740782 FRAME SAAB SF340 340B 7860101 EU ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 218AE 22611 5000 340B218 PREVIOUS REPAIR ON FRAME 258.0 FOUND CORRODED. REMOVED PREVIOUS REPAIR, FABRICATED AND INSTALLED REPAIR PARTS IAW SAAB SRM 53-70-30. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007052200059 20070522 00059 EU 2007 5 22 SIMA200714013 1 20070503 A 5315 7253740782 FLOORBEAM SAAB SF340 340B 7860101 EU ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 219AE 22769 5000 340B219 FLOORBEAM AT FRAME 258.0 CORRODED. CUTOUT CORROSION, FABRICATED AND INSTALLED NEW REPAIR PARTS IAW SAAB SRM 53-70-30. RETURNED AIRCARFT TO SERVICE 2 L 7 2 4T RT A52EU 2007052200061 20070522 00061 SO 2007 5 22 SIMA200714019 1 20070513 A 5320 13500437001 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 719AE 15875 4800 145276 RIGHT OMEGA BEAM CORRODED BETWEEN FRAMES 24 TO 25. REPAIRED OMEGA BEAM IAW EMB SRM 53-00-10. AIRCRAFT RETURNED TO SERV ICE 2 L 7 2 4F RT T00011AT 2007052200067 20070522 00067 SO 2007 5 22 SIMA200714021 1 20070513 A 5320 14522178005 SILL EMB 135 EMB135LR 3260305 SO ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 719AE 15875 4800 145276 SERVICE DOOR SILL CORRODED BETWEEN FRAMES 19 AND 22. REPAIRED DOOR SILL IAW EMB IC 2007-145/03094. RETURNED AIRCRAFT T O SERVICE. 2 L 7 2 4F RT T00011AT 2007052200076 20070522 00076 SO 2007 5 22 SIMA200714035 1 20070512 A 5311 14523152401 FRAME EMB 145 EMB145LR 3260212 SO ZONE 100 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 942LL 4931 14500930 MISDRILLED RIVET HOLE AT FRAME 52 AND STRINGER LH10. INSTALLED OVERSIZE FASTENERS IAW EMB IC2007-145/03228, PARAGRAPH 3 . 2 L 7 2 4T RT T00011AT 2007052200078 20070522 00078 EA 2007 5 22 SIMA200714029 1 20070505 A 5310 AV67021186001 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 522AE 7696 3878 10147 LEFT LOWER FORWARD FUSELAGE DRAG ANGLE AT RIGHT SPAR 67.5 DATUM HAD A 0.6 INCH CRACKED. PERFORMED REPAIR IAW AMERICAN EAGLE ENGINEERING ORDER CR-55MR-026. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007052200092 20070522 00092 NE 2007 5 22 DL76G070576 2 20070519 A 7320 CPU BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 1 EEC FAILED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 1604R LMDD8245 30180 704736 RTB - ON TAXI, LT EEC CONTROL MSG, EEC CH A CB POPPED. REMOVED AND REPLACED LT EEC, OPS CK OK. 2 L 7 2 4F 4 F RT A1NM E13NE 2007052200095 20070522 00095 2007 5 22 DL76S070400 4 20070417 A 2565 101651303 SLIDE BOEING 767 767332 1382001 NM PAX DOOR UNSERVICEABLE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 128DL 24078 RT FWD DOOR SLIDE RELEASE CABLE FOUND DETACHED DURING DOOR INSPECTION, THE R-1 DOOR SLIDE HAS BEEN REPLACED, S/N OFF PA0 828. 2 L 7 2 4F RT A1NM 2007052200096 20070522 00096 NM 2007 5 22 DL777070546 1 20070512 A 3246 328040006 WHEEL BOEING 777 777232 1385232 NM NR 8 MISSING A DALA O OTHER O OTHER NR NOT REPORTED 1 SO 27 863DA 29735 NR 8 WHEEL ASSY MISSING ON ARRIVAL ATL. NOTIFIED BY TLV A WHEEL HUBCAP FOUND ON RUNWAY. C/W BURST TIRE INSPECTION ON LOG ITEM 030 INSTALLED TIRE ASS PER M/M. INSTALLED NEW NR BRAKE AND SLEEVE IAW 32-45-07. INSTALLED TRANSDUCER PER AMM 32-42-05, ALL CHECKS GOOD. REMOVED AND REPLACED CENTER AXLE RT MLG PER MM 32-11-26-400-802 AND 32-11-26-000-802. 2 L 7 2 4F RT T00001SE 2007052200119 20070522 00119 2007 5 22 SWAA072511 4 20070519 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052200123 20070522 00123 NM 2007 5 22 SWAA072505 1 20070518 A 3397 W145005920 WIRE BOEING 737 7373G7 1384595 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 L1 DOOR EMERGENCY EXIT LIGHT INOP. FOUND GROUND WIRE BROKEN. REPAIRED GROUND WIRE PER MM. 2 L 7 2 4F RT A16WE 2007052200124 20070522 00124 GL 2007 5 22 C2XA07ON003 2 20070516 A 7200 AE3007A1E ENGINE EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL NR 1 ODOR A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 11192 4297 4297 936 CAE312748 WHILE CLIMBING THROUGH 10,000 FT, CABIN CREW REPORTED A VERY STRONG ACRID ODOR FROM MAIN CABIN DOOR BACK THROUGH SEAT 4A . CONTRACT MX REMOVED PANELS, INSPECTED LIGHTS BALLAST AND BULBS CONTACTS FROM PASSENGER SEAT 1A THRU 4A, ALSO REMOVED CD PLAYER AND INSPECTED WIRING. A/C WAS RELEASE ON A FERRY FLIGHT FROM SMF TO ONT. MX REMOVED AND REPLACED NR 1 ENG I AW TASKCARD 6271001 ALL LEAKS AND OPERATIONAL CHECKS SUCCESSFULLY. THE A/C WAS APPROVED TO RETURN FOR SERVICE. [07-27- 07] MX REMOVED AND REPLACED NR 1 ENG IAW TASKCARD 6271001. ALL LEAK AND OPERATIONAL CHECKS SUCCESFULLY.THE A/C WAS APPR OVED TO RETURN FOR SERVICE. 2 L 7 2 4F 4 F RT TE6CH 2007052200140 20070522 00140 2007 5 22 SWAA072404 4 20070513 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052200141 20070522 00141 2007 5 22 SWAA072441 4 20070517 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 712SW 27846 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052200145 20070522 00145 NM 2007 5 22 SWAA072429 1 20070515 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM BS 751 S23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 751, STR 23L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007052200148 20070522 00148 NM 2007 5 22 SWAA072435 1 20070517 A 5330 6545800 SKIN BOEING 737 7373A4 1384585 NM BS 267 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 267, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007052200155 20070522 00155 NM 2007 5 22 SWAA072445 1 20070517 A 5330 6550570 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT FWD END. REPAIRED SKIN PER SWA EA . 2 L 7 2 4F RT A16WE 2007052200159 20070522 00159 NM 2007 5 22 SWAA072433 1 20070517 A 5522 65C25753 SKIN BOEING 737 7373H4 1384600 NM RT ELEVATOR DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED HC1 CHECK, FOUND RIGHT ELEVATOR LOWER SKIN DISBONDED AT INBOARD T/E STA 24.90. REPAIRED SKIN PER SWA E A. 2 L 7 2 4F RT A16WE 2007052200162 20070522 00162 NM 2007 5 22 SWAA072463 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052200164 20070522 00164 NM 2007 5 22 SWAA072455 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500D S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052200165 20070522 00165 NM 2007 5 22 AWXA200700634 1 20070418 A 5730 114N407837 SKIN BOEING 757 7572S7 1384962 NM RT WING CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 MCN - C-11 CHECK - RIGHT WING NR 9 SLAT COVE PANEL CRACKED, WS 639.1. REPLACED RIGHT WING NR 9 SLAT COVE PANEL, WS 639. 1 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007052200168 20070522 00168 2007 5 22 AWXA200700645 4 20070516 A 2565 D31516317 SLIDE AIRBUS A319 A319132 3930340 NM R1 DOOR DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 832AW 34754 2618 1643 SAL - EES - BC-4 CHECK - THE R1 DOOR EMERGENCY ESCAPE SLIDE WAS FOUND TO BE EXPANDED/PARTIALLY INFLATED DURING A VISUAL INSPECTION OF THE SLIDE. THE R1 DOOR EMERGENCY ESCAPE SLIDE WAS REPLACED IAW AWA TASK CARD R1C25311. 2 L 7 2 4F RT A28NM 2007052200170 20070522 00170 NM 2007 5 22 AWXA200700647 1 20070418 A 5330 655298875 SKIN BOEING 737 73733A 1384673 NM BS 951 S10L CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - C-20 CHECK - CRACKED FUSELAGE SKIN, BS 951, S10L AT THE L2 DOOR UPPER HINGE CUT OUT. REPAIRED FUSE LAGE SKIN, BS 951, S10L AT THE L2 DOOR UPPER HINGE CUT OUT IAW B737-300 SRM 53-60-01-2R5, FIGURE 201. 2 L 7 2 4F RT A16WE 2007052200171 20070522 00171 NM 2007 5 22 AWXA200700648 1 20070511 A 5330 654576660 SKIN BOEING 737 73733A 1384673 NM BS 500D S14R CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - C-20 CHECK - CRACKED FUSELAGE SKIN, BS 500D, S14R. REPAIRED FUSELAGE SKIN, BS 500D, S14R IAW B737- 300 SRM 53-00-01-2R30, FIGURE 201. 2 L 7 2 4F RT A16WE 2007052200180 20070522 00180 NM 2007 5 22 AWXA200700640 1 20070418 A 3350 BR963512007 WIRE HARNESS BOEING 757 7572S7 1384962 NM ZONE 200 BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 MCN - EEL - C-11 CHECK - SEAT MOUNTED FLOOR PROXIMITY EMERGENCY WIRING HARNESS BROKEN IN SEVERAL PLACES. REPAIRED SEAT MOUNTED FLOOR PROXIMITY EMERGENCY WIRING HARNESS IAW B757-200 AMM 33-59-00. 2 L 7 2 4F RT A2NM 2007052300006 20070523 00006 NM 2007 5 23 2007UALA01537 1 20070517 A 4900 ACTUATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE APU SYSTEM DAMAGED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 APU DOOR C/B POPPING. [06-14-07] FOUND DAMAGED WIRES & REPAIRED SAME: PROBLEM PERSISTS. REPLACED APU INLET DOOR ACT UATOR PER MM 49-15-06-0401. OPS CKS GOOD. SUSPECT INTERNAL SHORT IN DOOR ACTUATOR DUE TO DIRT & VIBRATION. 2 L 7 2 4F 4 F RT A1NM E24NE 2007052300015 20070523 00015 NM 2007 5 23 2007UALA01547 1 20070518 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 FLT CREWS REPORTED INTERIOR EMERGENCY LIGHTS ON RIGHT SIDE TURNS ON INTERMITTENTLY IN FLIGHT, THE LIGHTS ARE FROM ROWS 1 9-27 ON THE RIGHT SIDE. [SUP 06-06-07] REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007052300016 20070523 00016 EU 2007 5 23 2007UALA01548 1 20070519 A 5314 ANGLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 412UA 465 LEFT WHEEL WELL LOWER FUSELAGE BELLY FAIRING SUPPORT ANGLE 5 IN LBL IS CRACKED AT FRAME 46. MAJOR REPAIR ACCOMPLISHED: REPLACED KEEL BEAM ANGLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052300019 20070523 00019 NM 2007 5 23 2007UALA01551 1 20070519 A 5310 DOOR FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 922UA 26642 FWD CARGO DOOR CUTOUT, AFT FRAME CRACKED IN TWO PLACES AT INBOARD UPPER CORNER OF LOWER STOP FITTING. ONE CRACK IS ON A FT SIDE OF FRAME IN RADIUS AND THE OTHER ON FWD SIDE OF FRAME. MAJOR REPAIR ACCOMPLISHED: INSTALLED FILLER AND ANGLE R EPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007052300024 20070523 00024 NM 2007 5 23 2007UALA01556 1 20070520 A 5712 STIFFENER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU MLG WW CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 303UA 23644 WHEEL WELL FWD BULKHEAD HAS CRACKED STIFFENER JUST FWD OF AILERON BELLCRANK SHAFT. MAJOR REPAIR: MAJOR REPAIR ACCOMPLI SHED. REPAIRED PER MM57-12-96, REPAIR NUMBER 3. 2 L 7 2 4F 4 F RT A16WE E21EU 2007052300032 20070523 00032 NM 2007 5 23 2007UALA01567 1 20070519 A 3350 80541 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY LIGHT NEAR DOOR 5 RIGHT ALONG MIDDLE BOTTOM LAV WALL INOP. REPLACED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052300033 20070523 00033 NM 2007 5 23 2007UALA01568 1 20070520 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 DOORS 4L & 5L EMERGENCY SLIDE LIGHTS ARE INOP. [SUP 06-06-07] REPLACED LT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052300036 20070523 00036 NM 2007 5 23 2007UALA01571 1 20070521 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY LIGHT AT DOOR 4R SLIDE ALUM INOP. [SUP 06-06-07] RELAMPED SLIDE EMERGENCY LIGHT. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052300037 20070523 00037 NM 2007 5 23 2007UALA01572 1 20070521 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 OVERWING EMERGENCY LIGHT INOP RIGHT 2ND ASSY FROM AFT. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052300061 20070523 00061 NM 2007 5 23 SWAA072497 1 20070517 A 5311 6546526 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052300075 20070523 00075 NM 2007 5 23 SWAA072472 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300095 20070523 00095 NM 2007 5 23 SWAA072493 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300096 20070523 00096 NM 2007 5 23 SWAA072495 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300123 20070523 00123 NM 2007 5 23 SWAA072457 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300126 20070523 00126 NM 2007 5 23 SWAA072399 1 20070512 A 5330 65C381921 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 FUSELAGE SKIN CRACKED AT BS 374, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007052300146 20070523 00146 NM 2007 5 23 ASAA0791653 1 20070517 A 5320 146A940139 FLOOR SUPPORT BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO FLOOR SUPORT -T- CORRODED. REPAIRED IAW SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007052300147 20070523 00147 NM 2007 5 23 ASAA0791656 1 20070517 A 5320 146A790343 FLOOR SUPPORT BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO PIT FLOOR SUPPORT CHANNEL CORRODED. REPAIRED IAW SRM EA5270 02720. 2 L 7 4 4F RT A16WE 2007052300149 20070523 00149 NM 2007 5 23 ASAA0791658 1 20070517 A 5320 146A94014 FLOOR SUPPORT BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO PIT FLOOR SUPPORT -T- CORRODED. REPAIRED IAW SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007052300154 20070523 00154 NM 2007 5 23 ASAA0791663 1 20070517 A 5320 146A750611 SPLICE BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO PIT FLOOR CHANNEL SPLICE CORRODED. 2 L 7 4 4F RT A16WE 2007052300155 20070523 00155 NM 2007 5 23 ASAA0791664 1 20070517 A 5320 SPLICE BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO PIT FLOOR CHANNEL SPLICE CORRODED. REPAIRED IAW SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007052300160 20070523 00160 NM 2007 5 23 ASAA0791669 1 20070517 A 5320 146A750219 CHANNEL BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO Z-CHANNEL CORRODED. REPAIRED IAW SRM 51-40-02. 2 L 7 4 4F RT A16WE 2007052300181 20070523 00181 NM 2007 5 23 ASAA0791681 1 20070517 A 5347 146A750119 CARGO TRACK BOEING 737 737990 NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO PIT TIE DOWN TRACK CORRODED. REPAIRED IAW SRM 53-00-53. 2 L 7 4 4F RT A16WE 2007052300189 20070523 00189 WP 2007 5 23 ASAA0781643 1 20070511 A 5240 SKIN DOUG DC9 DC983 3022083 WP LAV SERVICE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 SMALL GOUGE FOUND AT 2 O'CLOCK POSITION ON LAVATORY AFTER SERVICE DOOR. REMOVED DAMAGED AREA. INSTALLED DOUBLER AND FI LLER PER EA 5330 02208. 2 L 7 2 4F RT A6WE 2007052400013 20070524 00013 EU 2007 5 24 CPCP20070018 1 20070323 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 420AT 420 CORROSION FOUND ON RT SEAT TRACK BETWEEN FRAME 36 AND 39. RT SEAT TRACK BETWEEN FRAME 36 AND 39 REPLACED AS PER SRM 51- 25-04. 2 H 7 2 4T RT A53EU 2007052400054 20070524 00054 EU 2007 5 24 07FDEA01810 1 20070515 A 5313 A53974202 STRINGER AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 STRINGER CORROSION P53 AND P55 AT C65-66 REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007052400056 20070524 00056 EA 2007 5 24 5072007 2 20070501 A 8530 CYLINDER GULSTM 500 500B 0141106 SW LYC O540 IO540E1A5 41532 EA NR 2 BROKEN E ZJWA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 05 690RR 500B116988 RL412148 THE HOLD DOWN STUDS ON NR 2 CYLINDER BROKE CAUSING ON OIL LEAK TO LOSS OIL PRESSURE. 1 H 7 2 3O 3 O 6A1 1E4 2007052400058 20070524 00058 EA 2007 5 24 TRAX200700687 1 20070517 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 836AS 7263 RIGHT 640 SKIN BONDED BUTT STRAP DOUBLER IS CRACKED. [07-23-07] COMPLIED WITH EC/TC REO 601R-53-61-506. 2 L 7 2 4F RT A21EA 2007052400060 20070524 00060 WP 2007 5 24 IXXA07SMN153S 1 20070421 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1699 L27L MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT AFT FUSELAGE SKIN PANEL AND SKIN SPLICES OF LONGERON 27 LEFT AT STATION 1699. REMOVED EXISTING EXTERNAL REPAIR DOUBLER. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABR ICATED NEW SKIN, EXTERNAL DOUBLER, AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEAL ANT TO FAYING SURFACES. DEACTIVATED UAL DRAIN FOR CUSTOMER REQUEST. INSTALLED REPAIR PARTS IAW FAA FORM 8100-9 DATED 04- 23-07, MESSAGE BOEING NUMBER 1-317422975-5 DATED 04-23-07, AIRWORTHINESS DIRECTIVE 2007-02-02, SERVICE BULLETIN DACO DC8 -53A80, DOUGLAS DRAWING SR08530032, SEMAN DRAWING NUMBER ED-4519 DATED 04-17-07, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 2 L 7 4 4F RT 4A25 2007052400062 20070524 00062 EA 2007 5 24 TRAX200700677 1 20070515 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 981EV 7768 FLOOR EMERGENCY LIGHTS FROM ROW 1CD TO ROW 6CD INOP. 2 L 7 2 4F RT A21EA 2007052400063 20070524 00063 NM 2007 5 24 UPS07549827 1 20070515 A 3350 GUARD BOEING 757 75724APF 1384969 NM EMERGENCY LIGHT LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 454UP 25475 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT SWITCH STAYS IN ON POSITION. FOUND EMERGENCY EXIT LIGHT SWITCH GUARD LOOSE AND RESECURED AS REQUIRED. OPS TEST EMERGENCY EXIT LIGHT SYSTEM SATISFACTORY PER AMM 33-51-00-5. 2 L 7 2 4F RT A2NM 2007052400064 20070524 00064 NM 2007 5 24 SWAA072555 1 20070521 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 27L CRACKED AT BS 1036. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007052400071 20070524 00071 EU 2007 5 24 UPS07149829 1 20070518 A 5210 FITTING AIRBUS A300 A300F4622R 3930360 EU DOOR DIRTY A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 148UP 0831 INSPECTION TYPE:N/A ESCAPE SLIDE WILL NOT ARM. REMOVED DEBRIS FROM FWD FLOOR FITTING CONSISTING OF SAFETY WIRE SCRAPS A ND SHOP RAG STRINGS. OPS CHECK PER 52-10-30-05F. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2007052400076 20070524 00076 NM 2007 5 24 UPS07549838 1 20070507 A 5711 FITTING BOEING 757 75724APF 1384969 NM LT WING SPAR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 401UP 23723 INSPECTION TYPE:SPV LEFT FWD TRUNNION BEARING LWR I/B ATTACH POINT, WHERE LWR I/B FUSE PIN IS, SPAR FITTING I/B FACE HAS CORROSION AROUND BUSHING HOLE. REPAIRED PER GOODRICH ER REPAIR O7-2294. 2 L 7 2 4F RT A2NM 2007052400080 20070524 00080 WP 2007 5 24 UPS07849835 1 20070429 A 5313 57577781 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 L33R SPLICE BETWEEN STA 1640-1660 CRACKED. REMOVED AND REPLACED LONGERON SECTION FROM STA 1640-1660 L33R IAW SRM 51-01-20D, 51-1-21, AND 51-3-2. 2 L 7 4 4F RT 4A25 2007052400082 20070524 00082 WP 2007 5 24 IXXA07SMN156S 1 20070421 A 5330 SKIN DOUG DC8 DC871F 302199D WP ZONE 100 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT AFT FUSELAGE SKIN PANEL AND SKIN SPLICES OF LONGERON 28RIGHT AT STATION 1690. REMOVED EXISTING EXTERNAL REPAIR DOUBLER. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. F ABRICATED NEW SKIN, EXTERNAL DOUBLER, AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. DEACTIVATED UAL DRAIN FOR CUSTOMER REQUEST. INSTALLED REPAIR PARTS IAW FAA FORM 8100-9 DA TED 04-23-07, MESSAGE BOEING NUMBER 1-317422975-5 DATED 04-23-07, AIRWORTHINESS DIRECTIVE 2007-02-02, SERVICE BULLETIN D ACO DC8-53A80, DOUGLAS DRAWING SR08530032, SEMAN DRAWING NUMBER ED-4519 DATED 04-17-07, DC8 SRM 51-1-21, DC8 SRM 51-1-20 2 L 7 4 4F RT 4A25 2007052400085 20070524 00085 NM 2007 5 24 UPS07549834 1 20070518 A 3340 SWITCH BOEING 757 75724APF 1384969 NM COCKPIT BURNED A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 433UP 25464 INSPECTION TYPE:N/A STRONG SMELL OF BURNING RUBBER WHEN EXTENDING THE LANDING GEAR. FOUND TERMINAL NR 3 ON LEFT RUNWAY TURNOFF LIGHT SWITCH & TERMINAL END ON WIRE W2066-0412-20 BURNED. REPLACED SWITCH AND TERMINAL END W/REF TO CMM 33-11-7 1. C/W ADJ/TEST TO AMM 33-42-00-5, SATISFACTORY. 2 L 7 2 4F RT A2NM 2007052400093 20070524 00093 NM 2007 5 24 SWAA072570 1 20070521 A 5311 6546529 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 24R. REPAIRED FRAME PER ACO. 2 L 7 2 4F RT A16WE 2007052400095 20070524 00095 NM 2007 5 24 SWAA072556 1 20070521 A 5311 6546534 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052400097 20070524 00097 NM 2007 5 24 SWAA072567 1 20070521 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052400102 20070524 00102 NM 2007 5 24 SWAA072552 1 20070521 A 5311 6546596 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052400103 20070524 00103 NM 2007 5 24 SWAA072560 1 20070521 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052400104 20070524 00104 NM 2007 5 24 SWAA072551 1 20070521 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052400105 20070524 00105 WP 2007 5 24 07FDEA01820 1 20070515 A 5730 SKIN DOUG DC10 DC1010 3022110 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 RIGHT WING T/EDGE UPPER SURFACE CLOSE-OUT PANEL IS BULGED AT SEVERAL LOCATIONS, BETWEEN NR 2 AND NR 5 SPOILER AREA. 2 L 7 3 4F A22WE 2007052400108 20070524 00108 NM 2007 5 24 SWAA072550 1 20070521 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007052400114 20070524 00114 NM 2007 5 24 SWAA072549 1 20070521 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007052400116 20070524 00116 NM 2007 5 24 SWAA072553 1 20070521 A 5311 65C343551 BELTFRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 482, STR 20L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052400128 20070524 00128 NM 2007 5 24 SWAA072572 1 20070521 A 3350 MS155721 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007052400141 20070524 00141 EU 2007 5 24 TRBA200725 1 20070519 A 3350 7012210 BULB AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHT INOPERATIVE A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 541AT 541 PAX DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND INSTALLED LIGHT BULB IAW MM NR 33-51-25. OPERATIONAL CHECK OK. 2 H 7 2 4T RT A53EU 2007052400142 20070524 00142 NM 2007 5 24 AALA20070877 1 20070518 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 675AN 29425 JFK - EMERGENCY LIGHT AFT OF LEFT NUMBER THREE DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AFT OF LEFT NUMBER THREE DOOR . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007052400143 20070524 00143 NM 2007 5 24 UIEA200700224 1 20070516 A 5312 PRESSURE PANEL BOEING 747 7472D7B 1384803 NM BS 294 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 LEFT NWW SIDE PANEL BS 294 WL 140 CRACKED AT WEB. THE CRACK WAS REPAIRED BY TRIMMING DAMAGED AREA AND INSTALLING TWO RE PAIR DOUBLERS USING .050 2024T3 AS PER BOEING MESSAGE 1-321296136-2. 2 L 7 4 4F RT A20WE 2007052400144 20070524 00144 NM 2007 5 24 UIEA200700226 1 20070511 A 5320 TENSION TIE BOEING 747 7472D7B 1384803 NM BS 880 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 BS 880R FRAME TO TENSION TIE CONNECTION FOUND CRACK AT FRAME. REPAIRED BY TRIMMING OF DAMAGED TENSION TIE CHANNELS AND SPLICING IN A NEW CHANNEL SIMILAR TO SRM 53-10-11 FIGURE 1 AS PER BOEING MESSAGE 1-317931893-3. 2 L 7 4 4F RT A20WE 2007052400145 20070524 00145 NM 2007 5 24 UIEA200700225 1 20070517 A 5320 TENSION TIE BOEING 747 7472D7B 1384803 NM BS 840 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 BS 840L FRAME TO TENSION TIE CONNECTION FOUND HOLES 4, 15 AND 19 CRACKED AT FORWARD CHANNEL. REPAIRED TENSION TIES BY T RIMMING OF THE DAMAGED TENSION TIR CHANNELS AND SPLICING IN NEW CHANNELS SIMILAR TO SRM 53-10-11 FIGURE 1 AS PER BOEING MESSAGE 1-317931689-31-1. 2 L 7 4 4F RT A20WE 2007052400146 20070524 00146 NM 2007 5 24 UIEA200700227 1 20070516 A 5510 HINGE FITTING BOEING 747 7472D7B 1384803 NM RT STAB CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 RIGHT STABILIZER C/S HINGE AREA HOLE 14 AND 29 CRACKED. LEFT STABILIZER C/S HINGE ARE HOLES 5, 7 AND 27 CRACKED. HINGE FITTING REPAIRED PER SB 747-55A2050 R1 AND BOEING MESAGE 1-319880689-1. 2 L 7 4 4F RT A20WE 2007052400147 20070524 00147 NM 2007 5 24 UIEA200700228 1 20070514 A 5312 BULKHEAD BOEING 747 7472D7B 1384803 NM BS 2598 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 BS 2598 BULKHEAD AT STABILIZER HINGE SUPPORT FITTING ONE HOLE IS CRACKED. CRACK IN THE AFT INNER CHORD REPAIRED BY TRIM MING OUT DAMAGED MATERIAL AND INSTALLING A FILLER AND A REPAIR STRAP AS PER BOEING MESSAGE 1-320247988-6. 2 L 7 4 4F RT A20WE 2007052400148 20070524 00148 NM 2007 5 24 UIEA200700229 1 20070507 A 5415 ATTACH ANGLE BOEING 747 7472D7B 1384803 NM NR 1 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 NR 1 PYLON AFT MOUNT BULKHEAD FITTING CAP SKIN ATTACH ANGLE STATION 286 BOTH SIDES CRACKED. THE CHORDS CRACKED FLANGES WERE REMOVED BY TRIMMING PER SRM 51-10-01. ALL FASTENERS HOLES WERE NDT INSPECTED. REPAIR FILLERS AND ANGLES WERE INST ALLED ON FORWARD AND AFT SIDES OF THE LEFT AND RIGHT SIDE CHORDS AS PER BOEING MESSAGE 1-320850399-4. 2 L 7 4 4F RT A20WE 2007052400149 20070524 00149 NM 2007 5 24 UIEA200700230 1 20070520 A 5330 SKIN BOEING 747 7472D7B 1384803 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 NR 3R DOOR CUTOUT AFT LOWER CORNER SKIN AND BEARSTRAP CRACKED. REPAIRED BY TRIMMING OUT CORROSION AND CRACKS ON THE SKI N AND BEARSTRAP AND INSTALLING THREE STEEL DOUBLERS AS PER BOEING MESSAGE 1-321361058-2. 2 L 7 4 4F RT A20WE 2007052400150 20070524 00150 NM 2007 5 24 UIEA200700231 1 20070520 A 2612 FIRE WARNING BOEING 747 747341 13848AM NM APU FALSE ACTIVATION A UIEA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 EA 15 355MC 23395 APU FIRE LIGHT AND BELL IN FLIGHT. COMPLIED WITH FHB SECTION 3. INSPECTED APU NIL FAULTS FOUND. REMOVED AND REPLACED FIRE BOTTLE AND SQUIB ASSY PER AMM 26-22-01 SQUIB TEST OKAY. 2 L 7 4 4F RT A20WE 2007052400151 20070524 00151 EU 2007 5 24 AWXA200700635 1 20070516 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHT FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 653AW 29808 29799 1003 ORD - EEL - DURING OVERNIGHT CHECK, EMERG LIGHT "PUSH BUTTON" TEST FAILED. FWD EPSU FAULTS "UNIT FAULT". MX REPLACED T HE EPSU POWER SUPPLY AND BATTERY PACK. 2 L 7 2 4F RT A28NM 2007052400152 20070524 00152 NM 2007 5 24 AALA20070883 1 20070518 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 917AN 29518 MIA - EMERGENCY LIGHT AT SEAT 22A INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT 22A. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007052400153 20070524 00153 NM 2007 5 24 SWAA072540 1 20070521 A 3350 OL3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED HC1 CHECK, FOUND FWD LEFT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007052400154 20070524 00154 NM 2007 5 24 AALA20070878 1 20070517 A 3397 0201875003 WIRE HARNESS BOEING 757 757223 1384957 NM EMERGENCY LIGHT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 663AM 25297 DFW - EMERGENCY LIGHT AT SEAT 36D INOPERATIVE. REPLACED HARNESS FOR EMERGENCY LIGHT AT SEAT 36D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007052400155 20070524 00155 NM 2007 5 24 AALA20070880 1 20070518 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 750AN 30259 MIA - EMERGENCY LIGHT AT SEAT 40G HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 40G. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007052400156 20070524 00156 NM 2007 5 24 AALA20070884 1 20070518 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 917AN 29518 MIA - EMERGENCY LIGHT AT AFT CABIN LEFT SIDE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT CABIN LEFT S IDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007052400157 20070524 00157 WP 2007 5 24 AALA20070885 1 20070518 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 77421 49333 BOS - EMERGENCY EXIT SIGN LIGHT AT UPPER FORWARD OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN LI GHT AT UPPER FORWARD OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007052400158 20070524 00158 EU 2007 5 24 AALA20070864 1 20070515 A 3350 LENS AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 8067A 510 MIA - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007052400159 20070524 00159 NM 2007 5 24 AALA20070865 1 20070516 A 3350 MODULE BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 386AA 27060 MIA - EMERGENCY LIGHTS AT SEAT ROWS 32H TO 35H INOPERATIVE. RESET MODULE FOR EMERGENCY LIGHTS AT SEAT ROWS 32H TO 35H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007052400160 20070524 00160 NE 2007 5 24 AALA20070873 2 20070517 A 7230 COMPRESSOR BOEING 757 757223 1384957 NM RROYCE RB211 RB211535* NE RIGHT ENGINE STALLED A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 612AA 24488 31111 DFW INFLIGHT T688/17MAY - RIGHT ENGINE VIBRATION AND COMPRESSOR STALL DURING CLIMB. ENGINE GAS TEMPERATURE PEAK 1018. ENGINE SHUT DOWN BY CREW IN FLIGHT. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT LANDING INSP ECTION. REPLACED RIGHT ENGINE ON 18 MAY AT DFW. 2 L 7 2 4F 4 F RT A2NM E12EU 2007052400161 20070524 00161 WP 2007 5 24 AALA20070866 1 20070516 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 472AA 49647 LGA - UPPER EMERGENCY FLASHLIGHT AT FORWARD ENTRY HAS MISSING STRAP. REPLACED STRAP FOR UPPER EMERGENCY FLASHLIGHT AT F ORWARD ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007052400162 20070524 00162 NM 2007 5 24 AALA20070860 1 20070514 A 3350 LIGHT BOEING 757 7572Q8 1384972 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 706TW 28165 DFW - EMERGENCY EGRESS LIGHTS FROM SEAT ROW 17D TO AFT LAVATORY INOPERATIVE. REPLACED FLOOR PATH EMERGENCY LIGHTS GROUN D POWER STRIP FROM SEAT ROW 17D TO AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007052400163 20070524 00163 EU 2007 5 24 AALA20070875 1 20070517 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14061 471 MIA - EMERGENCY LIGHT AT SEAT ROWS 7G TO 18G INOPERATIVE. REPLACED BATTERY PACK AT NUMBER TWO DOOR FOR EMERGENCY LIGHT AT SEAT 7G TO 18G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007052400164 20070524 00164 EU 2007 5 24 AALA20070863 1 20070515 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70054 461 MIA - EMERGENCY LIGHTS AT SEAT 19G TO 28G INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT 19G TO 28G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007052400165 20070524 00165 NE 2007 5 24 MALA070061 2 20070508 A 7532 BLEED VALVE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE MALFUNCTIONED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 414XJ 340B414 GEE785734 RIGHT BLEED CLOSED LIGHT ILLUMINATED. RESET AND IT ILLUMINATED AGAIN. FOLLOWED BY TEMP UNCONTROLLABLE. CREW SHUTDOWN RIGHT ENGINE. REPLACED RT ENGINE PRSOV AND REPLACED RT RHEOSTAT ON AIRCONDITIONING PANEL. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2007052400166 20070524 00166 NM 2007 5 24 KNNA200700028 1 20070426 A 5330 SKIN BOEING 737 7372Q8 138448K NM PWA JT8 JT8D217 52053 NE BS 480-500 CANNING A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 413JG 23148 FWD CARGO PIT OIL CAN EFFECT ON SKIN BETWEEN STR 22R AND STR-21R. ALSO BETWEEN STA 480R AND STA 500R ACO NR 075363, PRO VIDE INSTRUCTIONS ON REPAIR OF SKIN AT BS 480-500, STR 21R-22R SRM BOEING 53-30-3. 2 L 7 2 4F 4 F RT A16WE E9NE 2007052400167 20070524 00167 NM 2007 5 24 KNNA200700027 1 20070503 A 5330 2024T3 SKIN BOEING 737 7372Q8 138448K NM PWA JT8 JT8D17 52049 NE BS 420 DENTED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 413JG 23148 DENT ON FUSELAGE SKIN BETWEEN STR 26R TO STR 25R AT BS 420 R, ACO NR 075366, PROVIDE INSTRUCTIONS ON REPAIR OF SKIN AT BS 420 R STR-25R-26R, SRM 53-30-3. 2 L 7 2 4F 4 F RT A16WE E2EA 2007052400169 20070524 00169 2007 5 24 QXEA200700824 4 20070518 A 3440 CONNECTOR BOMBDR DHC8 DHC8402 1390042 NM RF ANTENNA LOOSE A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 427QX 4156 SEA FLIGHT NR 2466: WX FAIL DISPLAYED ON BOTH MFD'S. E/A CHECKLIST DID NOT RECTIFY. MAINTENANCE INSPECTED AND FOUND LO OSE PLUG TO RF ANTENNA. SECURED PLUG AND OPS CHECK WEATHER RADAR SYSTEM PER Q400 AMM TASK 34-41-00-710-802. OPS CHECK IS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007052400170 20070524 00170 NM 2007 5 24 QXEA200700825 1 20070520 A 5230 HANDLE BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR UNSECURE A QXEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 NM 09 422QX 4150 EUG FLIGHT NR 2421: AFTER TAKEOFF, BAGGAGE DOOR/FUSELAGE WARNING ILLUMINATED. UPON INSPECTION FOUND HANDLE TO BE POPPED OUT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE C/W TASK AMM 05-48-13-210-801. DOOR OPERATES NORMALLY PER AMM TASK 52-3 1-00-710-801. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007052400172 20070524 00172 NM 2007 5 24 2007UALA01524 1 20070517 A 3350 32145410 BATTERY PACK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 855UA 1737 CIDS TEST -EPSU BATTERY EMER R- ATA 33-51- 38. REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052400175 20070524 00175 EU 2007 5 24 2007UALA01528 1 20070517 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DETACHED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 483UA 1586 SEAT 1C EEL LIGHT INOP. FOUND 2 WIRES DETACHED UNDER SEAT RAIL. [SUP 06-06-07] REPAIRED EEL LIGHT WIRES UNDER SEAT 1C . 2 L 7 2 4F 4 F RT A28NM E40NE 2007052400176 20070524 00176 NM 2007 5 24 2007UALA01529 1 20070518 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY LIGHT INOP AT UPPER DECK CEILING ROW 13 & FWD GALLEY CEILING. REPLACED LAMPS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052400179 20070524 00179 EU 2007 5 24 SA07029 1 20070516 A 2160 963A000002 VALVE AIRBUS A321 A321211 3930370 EU A/C BAY MALFUNCTIONED A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 192UW 24306 8253 1496 LGA FLT 938, EN ROUTE CLT TO LGA. AFTER TAKEOFF, A -HOT AIR- ODOR WAS NOTICED IN BOTH THE CABIN AND COCKPIT. THE APU WAS OFF AT THE TIME. WHEN THE LEFT AIR PACK WAS TURNED OFF, THE ODOR BECAME WORSE. THE PACKS WERE RECONFIGURED AND THE FLIGHT CONTINUED TO LGA. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE TRIM AIR VALVES ON MEL, AND R ELEASED THE AIRCRAFT FOR SERVICE. MAINTENANCE REPLACED THE AFT TRIM AIR VALVE. LEAK CHECKS OK. 2 L 7 2 4F RT A28NM 2007052400180 20070524 00180 EU 2007 5 24 SA07030 1 20070518 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 747UW 19892 1301 TPA - THE EMERGENCY LIGHT AT SEAT 18A WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. OPE RATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007052400182 20070524 00182 NM 2007 5 24 USAA070400 1 20070522 A 5512 SKIN BOEING 737 7374B7 1384702 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 455UW 24997 STA 110.5 - 113 AT TRAILING EDGE LOWER SKIN HAS CRACK. REPAIRED PER TYPICAL 55-10-07, SRM 55-10-01 FIG 201 REP 4, DEFEC T SIZE: 2.5 INCHES. 2 L 7 2 4F RT A16WE 2007052400183 20070524 00183 NM 2007 5 24 USAA070399 1 20070521 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 940UW 27805 RBL 14-17 STA 1660 CABIN FLOORBEAM FASTENER HOLES CORRODED. INSTALLED FAB'D NUT PLATE STRIP ANGLE PER TYP REP 53-15-02, 51-40-02, CORR TASK C53-251-03; LEVEL 1, DEFECT SIZE: 3"L X .800"W X .025"D. 2 L 7 2 4F RT A2NM 2007052400185 20070524 00185 NM 2007 5 24 USAA070397 1 20070521 A 5523 65C2638416 SKIN BOEING 737 7374B7 1384702 NM ELEVATOR TAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 444US 24862 RIGHT TAB NR 3 ATTACH POINT, TAB SKIN AT MAST FITTING CRACKED. REMOVED DAMAGE & INSTALLED REPAIR DOUBLER PER TR 55-20-0 3, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007052400186 20070524 00186 NM 2007 5 24 USAA070396 1 20070521 A 5312 PRESSURE PANEL BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 456UW 25020 BEADED PRESS DECK BS 665, LBL 20, WL 200 HAS CRACK. INSTALLED SKIN REPAIR PER TR 53-60-04, DEFECT SIZE: .75 INCH. 2 L 7 2 4F RT A16WE 2007052400187 20070524 00187 NM 2007 5 24 USAA070395 1 20070521 A 5310 DOOR FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 BS 440 & S-24R HAS CRACK. INSTALLED DOUBLERS PER EA 98676, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007052400188 20070524 00188 NM 2007 5 24 USAA070394 1 20070521 A 5310 DOOR FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 BS 492.4 & S-24R HAS CRACK. INSTALLED DOUBLERS PER EA 98675, DEFECT SIZE: .75 INCH. 2 L 7 2 4F RT A16WE 2007052400189 20070524 00189 NM 2007 5 24 USAA070393 1 20070521 A 5320 6517684638 INTERCOSTAL BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 BS 294.5, S-12L HAS CRACK. REMOVED & REPLACED DAMAGED PART PER SRM 51-10-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007052400191 20070524 00191 NM 2007 5 24 USAA070391 1 20070521 A 5320 FITTING BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 STA 360, S14L HAS CRACK. INSTALLED NEW CLIP/MFG PART PER DRAWING 65-17684-638, SRM 51-10-02, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007052400197 20070524 00197 NM 2007 5 24 DHL2007788527 1 20070414 A 5310 TORQUE BOX BOEING 727 727214 138407R NM BS 1223 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 WHILE IN "C" CHECK, AFT STAIRWELL RT TORQUE BOX HAS CRACK AT INBD WEB LIGHTENING HOLE STA 1223. STOP DRILLED CRACK IAW B727 SRM 51-10-1, FABRICATED REPAIR DOUBLER 7075T6 .025 PO NR 9004219 6.6" BY 3.75" IAW B727 SRM 53-10-2 FIG 6. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 2007052400198 20070524 00198 NM 2007 5 24 07FDEA01822 1 20070515 A 5530 651748456 STIFFENER BOEING 727 7272S2F 1384O81 NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 ANGLE CRACKED ON THE VERTICAL STAB LEADING EDGE WEB LOCATED ON THE UPPER RIGHT ON THE AFT SIDE OF WEB AND THE UPPER STAB BULKHEAD REMOVED AND REPLACED STIFFENER ANGLE ON VERTICAL STAB. REFERENCE SRM 51-30-02, PG 3. 2 L 7 3 4F A3WE 2007052400199 20070524 00199 WP 2007 5 24 07FDEA01824 1 20070516 A 5522 ALC7301506 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 DURING DENT EVALUATION ON RT OUTBOARD ELEVATOR UPPER SKIN HFEC INSPECTION REVEALED A 1" CRACK. CUT OUT DAMAGED SKIN, FA BRICATED REPAIR DOUBLER AND FILLER AND INSTALLED REF. DC/MD10 55-00-01 FIG 3, VOL I. ALODINED AND PRIMERED PER REF DC /MD 10 SRM 51-21-01 VOL II. RECALCULATED WEIGHT AND BALANCE PER REF DC/MD 10 SRM 55-20-00 VOL II. RECORDED NEW BALANCE CONDITION ON BALANCE TAG. THIS WAS A MINOR REPAIR. 2 L 7 3 4F RT A22WE 2007052400200 20070524 00200 WP 2007 5 24 07FDEA01825 1 20070516 A 5522 ALC7386506 SKIN DOUG DOUG MD10 MD1010F 3022112 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 46942 47804 RT INBOARD ELEVATOR UPPER SKIN IS CRACKED ON EDGE. CUT OUT DAMAGED SKIN, FABRICATED REPAIR DOUBLER AND FILLER, AND INST ALLED REF. DC/MD 10 SRM 55-00-01 FIG 3 VOL I AND 51-31-01 VOL II. ALODINED AND PRIMERED PER REF MD/DC 10 SRM 51-21-01 VOL II. THIS IS A MINOR REPAIR. 2 L 7 3 4F RT A22WE 2007052400201 20070524 00201 NE 2007 5 24 P5CA0701523 2 20070517 A 7320 AC9227F1790 FILTER BOEING 747 747243B 1384830 NM GE CF6 CF650* 30018 NE FUEL CLOGGED A P5CA C ABORTED TAKEOFF X J ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 EA 15 516MC 22507 517825 ON TAKEOFF, NR 2 ENGINE FLAMED OUT. ENGINE HAD SUCCESSFUL RESTART. INLET AND EXHAUST FEELING AND COMPRESSOR CHECKED SA TIS NR 2 FUEL TANK WAS SUMPED THEN REPLACED NR 2 ENGINE FUEL FILTER. NO FURTHER PROBLEMS. 2 L 7 4 4F 4 F A20WE E23EA 2007052400202 20070524 00202 EU 2007 5 24 MALA070063 1 20070519 A 3350 SWITCH SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A MALA O OTHER O OTHER CR CRUISE 1 GL 15 435XJ 340B435 EMERGENCY LIGHTS CB L8 POPPED OUT IN FLIGHT. REMOVED AND REPLACED 29LN, EMERGENCY LIGHT SWITCH ON FLIGHT ATTENDANT PANE L IAW SF340 MM 20-20. EMERGENCY LIGHTS ALL CHECK GOOD IAW MM 33-50. 2 L 7 2 4T RT A52EU 2007052400203 20070524 00203 SO 2007 5 24 CHQA200700018 1 20070520 A 2611 SWITCH EMB 145 EMB145LR 3260212 SO FIRE WARNING MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 11 298SK 145508 FLIGHT 3005 - PHL-GSO - AT FL270, RECEIVED FIRE BELL AND A RED "BAGG SMOKE" EICAS MESSAGE. RAN QRH, FIRED THE BAGGAGE FI RE EXTINGUISHING BOTTLES. MESSAGE REMAINED. DECLARED AN EMERGENCY, DIVERTED TO RIC. MAINTENANCE REMOVED AND REPLACED TEST SWITCH, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007052400204 20070524 00204 EU 2007 5 24 MALA070064 1 20070518 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 298 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 445XJ 340B445 SEAT TRACK AT BL 0.0 AND STA 298 IS CORRODED OUT OF ALLOWABLE LIMITS. INSTALLED REPAIR DOUBLER IAW MESABA EO S53342. R EFERENCE EAMS WORK ORDER 216422 TASK 1511. 2 L 7 2 4T RT A52EU 2007052400205 20070524 00205 EU 2007 5 24 MALA070065 1 20070518 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 298 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 445XJ 340B445 SEAT TRACK AT LBL 18.3 AND STA 298 IS CORRODED OUT OF ALLOWABLE LIMITS. INSTALLED REPAIR DOUBLER IAW MESABA EO S53342. REFERENCE EAMS WORK ORDER 216422 TASK 1509. 2 L 7 2 4T RT A52EU 2007052400206 20070524 00206 EU 2007 5 24 MALA070066 1 20070518 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU BS 231 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 445XJ 340B445 FOUND FLOOR FLANGE AT STA 231 BI 0.0 IS CORRODED OUT OF LIMITS. REPAIRED IAW MESABA EO S53102 REFERENCE EAMS WORK ORDER 216422 TASK 1526. 2 L 7 2 4T RT A52EU 2007052400207 20070524 00207 NM 2007 5 24 HALA0700215 1 20070518 A 4940 5198588 STARTER BOEING 737 73733A 1384673 NM APU INOPERATIVE A HALA O OTHER O OTHER CR CRUISE 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, VERIFICATION FLIGHT FOR APU COMPLETE, APU OPERATES ABNORMALLY. DID NOT START. FAULT LIGHT ON . REMOVED AND REPLACED APU STARTER PER AMM 49-41-01-004-001 APU OPS CHECK NORMAL AT THIS TIME. 2 L 7 2 4F RT A16WE 2008030400015 20080304 00015 NM 2008 3 4 DHL2007748033 1 20071102 A 5310 WINDOW FRAME BOEING 727 727225 1384077 NM BS 950F-970 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 RIGHT WINDOW FRAME PLUG AT STATION 950F TO 970 HAS CORROSION. REMOVED WINDOW PANE AND PLUG AT BS 950F TO 970 RIGHT IAW M/M 53-20-00 FIGURE 1 AND AEI DRAWING NR AE727-1-105 REV B. REMOVED CORROSION FROM WINDOW FRAME, FOUND OUT OF LIMITS I AW SRM 51-10-6, 56-20-1 FIGURE 1 AND 56-20-2 FIGURE 1. CLEANED WINDOW PLUG IAW BSOPM 20-30-03, NO CORROSION NOTED IAW S RM 51-10-6 PARA 3. FABRICATED DOUBLE FRAME REPAIR IAW SRM 53-20-3 FIG 1. TREATED AND PRIMED PARTS AND AREA IAW SRM 51- 10-2. INSTALLED REPAIR WASHERS AND DOUBLER FRAME REPAIR AND WINDOW PLUG PANEL AT STATION 950F TO 970 RT IAW SRM 53-20-3 FIGURE 1 AND 51-30-2, MM 53-20-00 FIGURE 1, LEAK CHECK GOOD IAW MM 21-30-00. 2 L 7 3 4F A3WE 2008030400018 20080304 00018 NM 2008 3 4 DHL2007793015 1 20071204 A 5322 SHEAR TIE BOEING 727 727247 138408F NM BS 344 S12R CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 FRAME AT BS 344 CHAFING AT 9G BARRIER SHEAR TIE STRINGER 12R. REMOVED AND REPLACED ATTACH ANGLE (SHEAR TIE) AT STRINGER 3R P/N 2942-3 PO NR 734151 IAW DRAWING NR 2936 REV B AND MM CHAPTER 25 PAGE 20 REV G MARCH 28, 2005 ON 9G BARRIER. 2 L 7 3 4F A3WE 2008030400020 20080304 00020 NM 2008 3 4 DHL2007748034 1 20071102 A 5310 WINDOW FRAME BOEING 727 727225 1384077 NM BS 950F-970 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 LT WINDOW FRAME PLUG AT STATION 950F TO 970 HAS CORROSION. REMOVED WINDOW PANE AND PLUG IAW MM 53-20-00 AND DRAWING NR AE727-1-105. CLEANED WINDOW PLUG PANE FOR EVALUATION NO CORROSION NOTED IAW S0PM 20-30-3. REMOVED CORROSION ON WINDOW FRAME. CORROSION FOUND OUT OF LIMITS IAW M/M 53-20-01 AND SRM 51-10-6. FABRICATED DOUBLER REPAIR IAW SRM 53-20-3 FIGUR E 1. TREATED AND PRIMED PARTS AND FRAME IAW SRM 51-10-2. INSTALLED REPAIR WASHERS, DOUBLER AND WINDOW PLUG IAW SRM 53- 20-3 FIGURE 1, 51-30-2 AND MM 53-20-00 FIGURE 1. LEAK CHECK GOOD IAW MM 21-30-0. 2 L 7 3 4F A3WE 2008030400023 20080304 00023 NM 2008 3 4 DHL2007793020 1 20071208 A 5313 STRINGER BOEING 727 727247 138408F NM BS 1130 S27L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 STRINGER SPLICE CORRODED ON STRINGER 27L AT STATION 1130 IN CHANNEL AND AFT OUTBOARD FLANGE EXFOLIATED. CUT OUT DAMAGE IAW SRM 53-10-23 FIGURE 1. FABRICATED REPAIR IAW SRM 53-10-3 FIGURE 1. TREATED AND PRIMED PART AND AREA IAW SRM 51-10- 2. INSTALLED STRINGER REPAIR PARTS IAW SRM 53-10-3 FIGURE 1. 2 L 7 3 4F A3WE 2008030400025 20080304 00025 NM 2008 3 4 DHL2007793024 1 20071201 A 5311 FRAME BOEING 727 727247 138408F NM BS 1110 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 AFT CARGO COMPARTMENT FRAME AT STATION 1110 UPPER FLANGE IS DENTED BETWEEN STRINGER 27R AND 26R. CUT OUT DAMAGE AREA AT AFT CARGO COMPARTMENT FS 1110 UPPER FLANGE IAW SRM 51-40-3 FIGURE 1. FABRICATED REPAIR IAW SRM 51-40-3 FIGURE 1 AND 53 -10-2 FIGURE 5. HEAT TREATED PART IAW NR FAS0115 REV 11. TREATED AND PRIMED PART IAW SRM 51-10-2. INSTALLED REPAIR AT FS 1110 BETWEEN STRINGER 27R TO 26R IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008030400029 20080304 00029 NM 2008 3 4 DHL2007793031 1 20071205 A 5315 FLOORBEAM BOEING 727 727247 138408F NM BS 276 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 EXFOLIATED CORROSION ON FLOORBEAM BS 276 RBL 14. CUT OUT CORRODED SECTION OF FLOORBEAM IAW SRM 51-40-4 FIGURE 1. FAB RICATED FILLER, 1 ANGLE AND FILLER FOR VERTICAL STIFFENER IAW SRM 51-40-4. TREATED AND PRIMED PARTS IAW SRM 51-10-2. I NSTALLED REPAIR PARTS AND WEB STIFFENER IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008030400067 20080304 00067 NM 2008 3 4 2007UALA03911 1 20070926 A 5343 TRUNNION BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NLG GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 NLG TRUNNION IS CREAKING AND GROANING. AFTER FURTHER ANALYSIS, IT HAS BEEN DETERMINED THIS IS NOT AN SDR REPORTABLE EVE NT. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030400088 20080304 00088 NM 2008 3 4 DHL2007742065 1 20071120 A 5322 SHEAR TIE BOEING 727 727225 1384077 NM BS 1148 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 CORROSION AFT PIT ON SHEAR TIE BS 1148 ABOVE STRINGER 26R. REMOVED CORROSION IAW SRM 51-10-6, FOUND OUT OF LIMITS IAW SRM 53-10-1 FIGURE 1 AND 53-10-2 FIGURE 5. REMOVED SHEAR TIE IAW SRM 51-30-2. FABRICATED NEW SHEAR TIE IAW SRM 53-10-2 FIGURE 5 AND 51-30-5. TREATED AND PRIMED SHEAR TIE IAW SRM 51-10-2 AND INSTALLED NEW SHEAR TIE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008030400113 20080304 00113 NM 2008 3 4 DHL2007742061 1 20071209 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 600 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 SPLICE PLATE (FLOORBEAM) AT LBL 65 BS 600 HAS CRACK FROM SLOT RADIUS. REMOVED CRACK FLOORBEAM SPLICE PLATE IAW B-727 SR M 51-30-2 AND AEI DRAWING NR AE727-3-A004. FABRICATED NEW SPLICE PLATE FROM 2024-T3 0.125" PO NR 9005802 APPROXIMATE DI MENSION 10.9375" BY 6.75" BY 6.125" BY 4.8125" IAW AEI DRAWING NR AE727-1-042 REV E AND JC EC00670-001. INSTALLED NEW F LOORBEAM SPLICE PLATE AT BS 600 LBL65 IAW AEI DRAWING AE727-1-042 REV E AND B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008030400117 20080304 00117 NM 2008 3 4 DHL2007742057 1 20071213 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 990-970 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 SURFACE CORROSION, AFT PIT BETWEEN BS 990 TO BS 970 STRINGER 29L. REMOVED CORROSION AFT PIT BETWEEN BS 990 TO BS 970 ST RINGER 29L IAW B-727 SRM 51-10-6. FOUND CORROSION OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1 AND 53-10-2 FIGURE 5. F ABRICATED REPAIR PARTS IAW ED NR EDAE59-3 REV A. TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED REPAIR IAW B-727 SRM 51-30-2 AND ED NR EDAE59-3 REV A. REPAIR PARTS, FILLER FROM 7075-T6, 0.032" BY 24" BY 1" PO NR 9005482, DOUBLER FRO M 7075-0 0.050" BY 22" BY 7.5" PO NR 722966 AND TRIPLER FROM 7075-T6 0.050" BY 22: BY 1.25" PO NR 9004940. 2 L 7 3 4F A3WE 2008030400143 20080304 00143 NM 2008 3 4 DHL2007742059 1 20071120 A 5311 FRAME BOEING 727 727225 1384077 NM BS 303.9 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 FUSELAGE STATION 303.9 FRAME WEB IS CRACKED AT STRINGER 15 WEB CUT OUT AND STRINGER 16 WEB CUT OUT AND CRACK INDICATION AT INBOARD CHORD WEB CUT OUT VERIFIED BY NDT. REMOVED CRACKED PARTS IAW B-727 SRM 51-30-2 AND SB727-53A-0153 REV 7. LO CATED AND DRILLED NEW PARTS IAW B-727 SRM 51-30-5 AND 51-30-2. TREATED AND PRIMED PARTS IAW B-727 SRM 51-10-2. INSTALL ED NEW PART AT FUSELAGE STATION 303.9 FRAME STRINGERS 15L AND 16L IAW B-727 SRM 51-30-2 AND SB727-53A-0153 REV 7. 2 L 7 3 4F A3WE 2008030500003 20080305 00003 NM 2008 3 5 QXEA200801936 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 400-410 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - SEAT TRACK NR 1 HAS SCRATCHES ON TOP BETWEEN STATION 400 AND 410. REPAIR IAW RD8-52-1342 AND -8 200 ND TM PART 6 51-00-01 AND -8 200 SRM 51-20-16, 51-20-66. 2 H 7 2 4T RT A13NM 2008030500004 20080305 00004 NM 2008 3 5 QXEA200801952 1 20071204 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 312 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - FRAME AT STATION X312, 8 INCHES FROM CENTER LINE IS CRACKED AT TOP FLANGE. REMOVED DAMAGED FRAME SECTI ON, INSTALLED FRAME SPLICE IAW RD8-53-9913 AND D8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008030500005 20080305 00005 NM 2008 3 5 QXEA200801953 1 20071204 A 5320 FITTING DHAV DHC8 DHC8202 2809007 NM BS 202 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - AFT TENSION FITTING FOR STRINGER 31S AT FRAME X202.75 IS CORRODED. REMOVED CORRODED TENSION FITTING AN D INSTALLED NEW FITTING FROM STOCK IAW D8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008030500007 20080305 00007 NM 2008 3 5 QXEA200801926 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 436-445 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - RIGHT OUTBOARD SEAT TRACK NR 11 HAS CORROSION AND SCRATCHES AT STATION X436 TO X445. REPAIRED IAW -8 200 RD8-53-1342 AND -8 200 NDTM PART 6 51-00-01 AND -8 200 SRM 51-20-16, 51-20-66. 2 H 7 2 4T RT A13NM 2008030500008 20080305 00008 NM 2008 3 5 QXEA200801888 1 20071204 A 5315 FLOORBEAM DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - OBLONG DRILL HOLE IN FLOORBOARD BEAM FS X2, Y9.25 RT, AT NR 7 SEAT TRACK INTERSECTION. REMOVED FLOORBE AM, INSTALLED NEW FLOORBEAM FROM STOCK IAW D8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008030500010 20080305 00010 EA 2008 3 5 QXEA200802058 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 813 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT SIDE RAIL SEAT TRACK WORN AND LOWER LIP GOUGED AT APPROXIMATELY STATION 813.70. BLENDED TO REMOVE GOUGE ON TRACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030500011 20080305 00011 EA 2008 3 5 QXEA200802062 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 517 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT SIDE RAIL SEAT TRACK HAS CORROSION AT APPROXIMATELY STATION 517.00. REMOVED LOCALIZED CORROSION BY BLENDING SEAT TRACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED ARE AS. 2 L 7 2 4F RT A21EA 2008030500013 20080305 00013 EA 2008 3 5 QXEA200801986 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 645-648 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT CENTER SEAT TRACK HAS CORROSION AT STATION 645 TO 648. BLENDED OUT CORROSION FROM SEAT TRACK, IN SPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030500014 20080305 00014 EA 2008 3 5 QXEA200801987 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 663-665 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT CENTER SEAT TRACK HAS CORROSION AT STATION 663 TO 665.5. BLENDED OUT CORROSION FROM SEAT TRACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030500015 20080305 00015 EA 2008 3 5 QXEA200801994 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 662-665 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT CENTER SEAT TRACK HAS CORROSION AT STATION 662 TO 665. BLENDED OUT CORROSION FROM SEAT TRACK, INS PECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030500029 20080305 00029 NM 2008 3 5 QXEA200801865 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 545 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - RIGHT OUTBOARD SEAT TRACK NR 9 HAS CORROSION AT STATION X545. REPAIRED IAW RD 8-53-784, INSPECTED NO C RACKS NOTED IAW NDTM 51-00-01. 2 H 7 2 4T RT A13NM 2008030500030 20080305 00030 NM 2008 3 5 QXEA200801943 1 20071204 A 5710 STRUCTURE DHAV DHC8 DHC8202 2809007 NM RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - RIGHT WING INBOARD LEADING EDGE UPPER FLANGE HAS MILD FRETTING CORROSION AROUND SCREW HOLES APPROXIMATE LY STATION YW48. REPAIRED IAW RD8-57-1513 AND DASH 8 200 SRM 51-20-36. 2 H 7 2 4T RT A13NM 2008030500031 20080305 00031 NM 2008 3 5 QXEA200801925 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 307 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - SEAT TRACK NR 1 HAS SCRATCHES IN TOP AT STATION 307. REPAIRED IAW RD8-53-1342, -8 200 NDTM PART 6 51-0 0-01 AND -8 200 SRM 51-20-16, 51-20-66. 2 H 7 2 4T RT A13NM 2008030500042 20080305 00042 NM 2008 3 5 QXEA200801937 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 484-488 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - SEAT TRACK NR 2 HAS SCRATCHES ON TOP BETWEEN STATION 484 AND 488. REPAIRED IAW RD8-53-1342 AND -8 200 NDTM PART 6 51-00-01 AND -8 200 SRM 51-20-16, 51-20-66. 2 H 7 2 4T RT A13NM 2008030500044 20080305 00044 NM 2008 3 5 QXEA200801929 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 332-333 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - SEAT TRACK NR 1 HAS CORROSION ON TOP BETWEEN STATION 332-333. REPAIRED IAW RD8-53-1342, -8 200 NDTM PAR T6 51-00-01 AND -8 200 SRM 51-20-16, 51-20-66. 2 H 7 2 4T RT A13NM 2008030500045 20080305 00045 NM 2008 3 5 QXEA200801930 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 467 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - RIGHT OUTBOARD SEAT TRACK NR 11 HAS CORROSION AND SCRATCHES AT STATION X467. REPAIRED IAW RD8-53-1342, RD8-53-4847 AND -8 200 NDTM PART6 51-00-01 AND -8 200 SRM 51-20-16, 51-20-66. 2 H 7 2 4T RT A13NM 2008030500046 20080305 00046 NM 2008 3 5 QXEA200801933 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 349-364 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - SEAT TRACK NR 1 HAS SCRATCHES ON TOP BETWEEN STATION 349 AND 364. REPAIRED IAW RD8-53-1342 AND -8 200 NDTM PART6 51-00-01 AND -8 200 SRM 51-20-16, 51-20-66. 2 H 7 2 4T RT A13NM 2008030500062 20080305 00062 EA 2008 3 5 QXEA200801985 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 631-635 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT CENTER SEAT TRACK HAS CORROSION AT STATION 631 TO 635. BLENDED OUT CORROSION FROM SEAT TRACK, IN SPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030500063 20080305 00063 EA 2008 3 5 QXEA200801990 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 553-555 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT SEAT TRACK HAS CORROSION AT STATION 553 TO 555. BLENDED OUT CORROSION FROM SEAT TRACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030500105 20080305 00105 EA 2008 3 5 QXEA200802063 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 645-648 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT HAND SIDE SEAT TRACK HAS CORROSION AT STATION 645.5 TO 648. BLENDED TO REMOVE CORROSION, INSPECTE D, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030500108 20080305 00108 EA 2008 3 5 QXEA200802006 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 570 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT CENTER SEAT TRACK HAS CORROSION AT STATION 570. BLENDED OUT CORROSION FROM SEAT TRACK, INSPECTED , REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030500110 20080305 00110 EA 2008 3 5 QXEA200802003 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 507 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT SEAT TRACK HAS CORROSION AT STATION 507. BLENDED OUT CORROSION FROM SEAT TRACK, INSPECTED, REMAI NED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030500111 20080305 00111 EA 2008 3 5 QXEA200802004 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 532 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT HAND SEAT TRACK HAS CORROSION AT STATION 532.00. BLENDED TO REMOVE CORROSION FROM TRACK, INSPEC TED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030500150 20080305 00150 NM 2008 3 5 QXEA200801891 1 20071204 A 5313 STRINGER DHAV DHC8 DHC8202 2809007 NM BS 488 S24R CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - POSSIBLE CORROSION ON STRINGER 24R STATION X488 THROUGH X547/Z100 DIRECTLY BELOW DATO GRILL. REPAIRED REF -8 200 SRM 51-20-11, 53-00-16, 51-20-16, 51-20-36. 2 H 7 2 4T RT A13NM 2008030500151 20080305 00151 NM 2008 3 5 QXEA200801940 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 513-520 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - SEAT TRACK NR 5 HAS SCRATCHES ON TOP BETWEEN STATION 513 AND 520. REPAIRED IAW RD8-53-1339 AND -8 200 NDTM PART 6 51-00-01 AND -8 200 SRM 51-20-16, 51-20-66. 2 H 7 2 4T RT A13NM 2008030500152 20080305 00152 NM 2008 3 5 QXEA200801941 1 20071204 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - LEFT FLAP NR 2 TRACK LOWER RAMP HAS 2 DIVOTS. REPAIRED IAW RD8-57-986 AND --8 200 NDTM PART 6 51-00-01 AND 1-82-7A PT 1, 51-00-04. 2 H 7 2 4T RT A13NM 2008030500153 20080305 00153 NM 2008 3 5 QXEA200801938 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 445-455 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - SEAT TRACK NR 5 HAS SCRATCHES ON TOP BETWEEN STATION 445 AND 455. REPAIRED IAW RD8-53-1339 AND -8 200 NDTM PART 6 51-00-01 AND -8 200 SRM 51-20-16, 51-20-66. 2 H 7 2 4T RT A13NM 2008030500156 20080305 00156 NM 2008 3 5 QXEA200801951 1 20071204 A 5340 ATTACH FITTING DHAV DHC8 DHC8202 2809007 NM FLOOR SUPPORT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - AFTER CLEANING BILGE AREA, MAINTENANCE SUSPECTS CORROSION ON STRINGER 31R FLOOR SUPPORT ATTACH FITTING. REPAIRED PER DASH 8 200 CPM CHAPTER 4, SRM 51-20-11 51-20-16, 51-20-36, 51-40-11 AND -8 200 NDTM PART 6 51-00-01, PART 1 51-00-04. 2 H 7 2 4T RT A13NM 2008030500166 20080305 00166 NM 2008 3 5 QXEA200801934 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 488 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - RIGHT OUTBOARD SEAT TRACK NR 11 HAS CORROSION AT STATION X488. REPAIRED IAW RD8-53-1342, DHC-8-200 SRM 51-00-01, 51-20-16 AND 51-20-66. 2 H 7 2 4T RT A13NM 2008030600052 20080306 00052 NM 2008 3 6 UPS08M51695 1 20071207 A 5330 DOUBLER DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C CENTER CARGO AT STATION 1538 LONGERON 44LT FOUND SUSPECTED CRACK ON SPLICE DOUBLER. HFEC INSP C/O PER DAC NDT SPM R13,06-10-01.001 & CRACK FOUND IN 2 AREA, FWD & AFT AS MARKED APPROX 2" IN LENGTH. CRACK SPLICE REMOVED PE R SRM 51-33-01 V.II R35. NEW SPLICE FAB PER DWG A5A7114.FPI C/O PER DPS4.707 REV AW ON NEW SPLICE FOUND NO CRACK EVIDEN T. NEW FAB SPLICE PER SRM 51-3 3-01 V.II R35. 2 L 7 3 4F RT A22WE 2008030600083 20080306 00083 NM 2008 3 6 UPS08M51706 1 20071221 A 5512 PANEL DOUG MD11 MD11 3023602 NM HORIZ STAB DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C EMPENNAGE, LT HORIZONTAL STABILIZER FRONT SPAR, TOP OF ACCESS PANEL 331A Z CUTOUT AREA, UPPER SURFACE MOUNTING HOLES FOR L/E PANEL 331BT, FOUND WITH 11 EA ELONGATED MOUNTING HOLES AS MARKED. GANG CHANNEL ASSY REMOVED FOR ACCESS PER SRM 51-35-01 V.II R35. QTY 11EA ELONGATED HOLES REAMED PER EN 1010-08. HFEC OPEN HOLE INSP C/O PER DAC NDTS PM R13 06-10-01.003 ON REWORKED AREA & FOUND NO CRACK EVIDENT. REPAIRED BORE PROTECTED & BUSHING INSTALLED PER EN 1010- 08. THIS REPAIR IS TIME LIMITED FOR 24 MONTHS PENDING A DAMAGE TOLERANCE ANALYSIS. 2 L 7 3 4F RT A22WE 2007052200008 20070522 00008 NM 2007 5 22 NWAA071845516 1 20070512 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM EMERGENCY LIGHTS WEAK A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 516US 23204 DURING LINE CHECK, FOUND AFT SECTION EMERGENCY FLOOR PROXIMITY LIGHTS DIM WHEN TESTED. REMOVED AND REPLACED POWER SUPPL Y AT DOOR 3R. OPS CHECKS NORMAL PER AMM 33-51-11. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2007052200014 20070522 00014 EU 2007 5 22 07FDEA01791 1 20070515 A 5311 FRAME AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 401FE 191 BULK CARGO COMPARTMENT RT FRAME 67 PANEL LAND COMMON TO FLOOR PANEL 162HF HAS 1 AREA OF CORROSION. TOTAL 4 SQUARE INCHE S REMOVED CORROSION FROM UPPER FLANGE IAW A310 SRM 51-74-10 UPON REMOVAL OF CORROSION FOUND ADDITIONAL CORROSION BEYOND REPAIR BETWEEN MATING SURFACES ON LWR FLANGE REMOVED OLD BEAM AND REPLACED WITH NEW ONE P/N A5397422320051 IAW A310 AR M51-40-21. REPROTECTED AREA IAW A310 SRM 51-75-10. 2 L 7 2 4F RT A35EU 2007052200019 20070522 00019 EU 2007 5 22 07FDEA01796 1 20070515 A 2750 FLAP SYSTEM AIRBUS 310 A310203 3930313 EU TE FLAPS MALFUNCTIONED A FDEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 25 425FE 264 FLAP FAULT BOTH LIGHT SY1/SY2 WHEN FLAPS SET TO 15-15. RECYCLED FLAPS AND WORKED OK, BUT A BIT SLOW. NEED SAFETY WIRE ON FLAP OVERRIDE SWITCH. SYSTEM NR 1 AND NR 2 FAULTS CLEARED AT THIS TIME. MTP SHOWED NR 2 SFCC FAULT. PERFORMED BIT E TEST OF SFCC THAT SHOWED 'JAM'. RESET SFCC. CYCLED FLAPS SEVERAL TIMES THROUGH FULL RANGE WITH NO FAULTS NOTED, USIN G ENGINES. FLAPS OPS CHECK NORMAL PER A310 AMM 27-50-00. INSPECTED FLAPS, NO DEFECTS NOTED. SAFETY FLAP OVERRIDE SWI TCH. 2 L 7 2 4F RT A35EU 2007052200031 20070522 00031 EU 2007 5 22 07FDEA01804 1 20070515 A 5310 WINDOW FRAME AIRBUS 310 A310203 3930313 EU COCKPIT CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 1ST OFFICER SLIDING WINDOW ASSY FRAME HAS CHAFED AREA FWD END 2 PLACES COMPLIED WITH FEDEX EA6-5610-110455 PART 1. 2 L 7 2 4F RT A35EU 2007052200037 20070522 00037 NM 2007 5 22 NWAA071806314 1 20070510 A 2530 OVEN BOEING 747 747451 1384940 NM GALLEY CONTAMINATED A NWAA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 01 674US 30269 DURING FLIGHT, SMOKE FROM OVEN NR 2 IN GALLEY NR 2. FOUND RICE BURNED INSIDE OF OVEN. PULLED CIRCUIT BREAKERS. REQUIR ED THE USE OF A HALON FIRE EXTINGUISHER. FLIGHT CONTINUED ON AND LANDING WAS UNEVENTFUL. MAINTENANCE REMOVED AND REPLA CED OVEN, AND HALON FIRE EXTINGUISHER. OPERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007052200063 20070522 00063 EU 2007 5 22 SIMA200714018 1 20070508 A 5311 7253813007 FRAME SAAB SF340 340B 7860101 EU ZONE 200 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 218AE 22611 5000 340B218 FUSELAGE FRAME AT FS 658 DAMAGED. REMOVED AND REPLACED DAMAGED FRAME IAW SAAB SRM 51-40-21 AND 51-40-40. RETURNED AIRC RAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007052200073 20070522 00073 SO 2007 5 22 SIMA200714028 1 20070513 A 5347 13500439007 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 719AE 15875 4800 145276 LEFT SEAT TRACK CORRODED BETWEEN FRAMES 18 AND 23. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EA GLE ENGINEERING TECHNICAL NOTICE EM-53-110R2. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052200091 20070522 00091 NM 2007 5 22 DLM88070573 1 20070519 A 2910 294703417 MODULE DOUG MD88 MD88 3023688 NM HYD SYSTEM UNSERVICEABLE A DALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 911DL 49542 AFTER TAKEOFF PASSING THRU 8000 FT TURNED OFF RT ELEC PUMP AND AUX PUMP, LT HYD PRESS DROPPED TO ZERO AND QTY TO 1. C/W QRH CKLIST AND TURNED OFF LT ENG PUMP APPROX 2 MINS LATER. FOUND POP OUT IND HOUSING IN LT SYS PRESS MODULE OFF OF MOD U REPLACED FILTER HOUSING PER AMM. SEE ITEM 13 FOR PUMP AND FILTER CHECK. NDS LEAK CK 624270. LEAK CK GOOD. PERFO RMED HY SYS CK AND RESERVICE FOLLOWING IN-FLIGHT FLUID LOSS PER AMM. REMOVED AND REPLACED NR 1 HYD EDP PER AMM 278549. REPLACED PRE RETURN AND CASE DRAIN FILTERS 278549. LEAK CK GOOD. 2 L 7 2 4F RT A6WE 2007052200097 20070522 00097 NM 2007 5 22 DLM88070553 1 20070414 A 5512 5922578515 SKIN DOUG MD88 MD88 3023688 NM HORIZONTAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 977DL 53258 THE RT HORIZONTAL STABILIZER UPPER INBD SKIN PANEL FOUND CRACKED - 1.25 IN LONG. THE CRACK WAS CUT OUT OF THE SKIN AND INSPECTED. THE PANEL WILL BE REPLACED AT WITHIN 2000 FLIGHT HOURS. 2 L 7 2 4F RT A6WE 2007052200104 20070522 00104 NM 2007 5 22 DL757070560 1 20070226 A 5312 146N88358201 BULKHEAD BOEING 757 757232 1384965 NM FS 1720 S25L-25R GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 603DL 22810 THE AFT FUSELAGE PRESSURE BULKHEAD WAS DAMAGED DURING A TAIL STRIKE. THE BULKHEAD CHORDS WERE CUT OUT AND A NEW SECTION WAS FABRICATED AND SPLICED IN. REF ER/A'S 460538-14 AND 460643-14 FOR SAME DAMAGE. 2 L 7 2 4F RT A2NM 2007052200106 20070522 00106 NM 2007 5 22 DL76L070562 1 20070515 A 3350 20121 CHARGER BOEING 767 767332 1382001 NM EMERGENCY LIGHTS INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 178DN 25143 EMERGENCY LIGHTS FIRST CLASS INOP. REPLACED FUSES AND CHARGER 9008. OPS CK GOOD. 2 L 7 2 4F RT A1NM 2007052400012 20070524 00012 EU 2007 5 24 CPCP20070017 1 20070323 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 420AT 420 CORROSION FOUND ON LT SEAT TRACK BETWEEN FRAME 36 AND 39. LT SEAT TRACK BETWEEN FRAME 36 AND 39, REPLACED AS PER SRM 51 -25-04. 2 H 7 2 4T RT A53EU 2007052400017 20070524 00017 WP 2007 5 24 07FDEA01816 1 20070515 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP FUSELAGE UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 385FE 46619 RT PRIMARY STATIC PORT HAS SKIN MISMATCH GREATER THAN .006 IN 3 EA AREAS OF THE CONTROLLED AREA. MISMATCH MEASUREMENTS WERE .013, .020, .023 REPAIRED AREA IAW SRM 53-20-00 VOL 1 FIGURE 9. ATTENTION RECORDS REPAIR IS A CATEGORY B REPAIR WH ICH REQUIRES REPETITIVE INSPECTION AS FOLLOWS DAMAGE CAT B, TOLERANCE INSPECTION REQUIREMENT, INITIAL 34,00, REPETITIVE 23,000 REPLACEMENT N/A. 2 L 7 3 4F RT A22WE 2007052400022 20070524 00022 NM 2007 5 24 QXEA200700799 1 20070516 A 2730 7G773 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007 NM RUDDER MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 356PH 2929 502 YVR FLIGHT NR 2035 - DURING NR 2 PROP TRANSITION FROM START/FEATHER TO 1200, RUD FULL PRESS CAUTION LIGHT INTERMITTENTLY ILLUMINATED SOMETIMES STAYING ON FOR A COUPLE OF MINUTES, SOMETIMES JUST A FEW SECONDS. REMOVED PANEL 322HR. CLED AIR FROM NR 2 RUDDER PCU. REPLACED NR 2 RUDDER FULL PRESSURE CAUTION SWITCH. OPERATIOINAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007052400024 20070524 00024 NM 2007 5 24 ASAA0791646 1 20070517 A 5320 143A7501168 SUPPORT BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 FWD CARGO PIT CORROSION ON RIGHT SUPPORT-Z. REPAIRED IAW SRM 53-40. 2 L 7 4 4F RT A16WE 2007052400039 20070524 00039 EA 2007 5 24 TRAX200700690 1 20070519 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 843AS 7310 EMERGENCY EXIT SIGN AT ROW 8 WILL NOT ILLUMINATE. 2 L 7 2 4F RT A21EA 2007052400041 20070524 00041 EA 2007 5 24 TRAX200700671 1 20070515 A 5210 BRACKET CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 919EV 7780 DURING CRJ101 INSP INSIDE ASD ACCESS PANEL 832AR, FOUND UPPER FWD ASD FRAME BRACKET CRACKED. 2 L 7 2 4F RT A21EA 2007052400057 20070524 00057 EA 2007 5 24 TRAX200700686 1 20070517 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 836AS 7263 LEFT 640 SKIN BONDED BUTT STRAP DOUBLERS CRACKED. [07-23-07] COMPLIED WITH EC/TC REO 601R-53-61-506. 2 L 7 2 4F RT A21EA 2007052400067 20070524 00067 NM 2007 5 24 SWAA072545 1 20070521 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 437WN 29832 DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007052400069 20070524 00069 NM 2007 5 24 SWAA072543 1 20070521 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 437WN 29832 DURING SCHEDULED HC2 CHECK, LEFT FWD EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2007052400074 20070524 00074 EU 2007 5 24 UPS07149844 1 20070523 A 4920 APU AIRBUS A300 A300F4622R 3930360 EU APU BAY SHUTDOWN A IPXA K NONE O OTHER NR NOT REPORTED 1 SO 01 131UP 0815 CREW DECLARED EMERGENCY INTO SJU AFTER APU AUTO SHUT DOWN AND NR 1 GENERATOR WAS PREVIOUSLY DEFERRED ON M350956. [SUP 0 5-25-07] ACCOMPLISHED OPS CHECK IAW A300 MM 49-10-00-05. OPS CHECK NORMAL AT THIS TIME. R & R NR 1 GENERATOR CONTROL UN IT IAW A300 MM 24-22-12-04. THIS CLEARS M340946 2 L 7 2 4F RT A35EU 2007052400075 20070524 00075 NM 2007 5 24 UPS07549837 1 20070507 A 5711 FITTING BOEING 757 75724APF 1384969 NM LT WING SPAR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 401UP 23723 INSPECTION TYPE:SPV LEFT FWD TRUNNION BEARING LWR OUTBOARD ATTACH POINT, WHERE LWR OUTBOARD FUSE PIN IS, SPAR FITTING OU TBOARD FACE HAS CORROSION AROUND BUSHING HOLE. REPAIRED PER GOODRICH ER REPAIR 07-2294. 2 L 7 2 4F RT A2NM 2007052400106 20070524 00106 NM 2007 5 24 SWAA072547 1 20070521 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 2007052400117 20070524 00117 NM 2007 5 24 SWAA072542 1 20070521 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 225WN 34333 DURING SCHEDULED MV2 CHECK, FOUND RIGHT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BUL B PER MM. 2 L 7 2 4F RT A16WE 2007052400177 20070524 00177 NM 2007 5 24 2007UALA01530 1 20070518 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EEL LIGHT AT UPPER DECK LWR WALL ACROSS LAVS. [SUP 06-06-07] SECURED CONNECTOR. OPS. CKS. NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052400178 20070524 00178 NM 2007 5 24 2007UALA01531 1 20070518 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EEL LIGHT INOPERATIVE AT SEAT 48 HJK. REPLACED LIGHT ASSY, OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052400190 20070524 00190 NM 2007 5 24 USAA070392 1 20070521 A 5320 CHANNEL BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 STA 360, S15L HAS CRACK. INSTALLED NEW CLIP/MFG PART PER SRM 51-10-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007052400192 20070524 00192 NM 2007 5 24 USAA070390 1 20070521 A 5320 INTERCOSTAL BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 STA 294.5, S12L HAS CRACK. INTERCOSTAL AND CLIP REPLACED PER BOEING DWG 65-17684-638, SRM 51-10-02, DEFECT SIZE: .25 I NCH. 2 L 7 2 4F RT A16WE 2007052400211 20070524 00211 NM 2007 5 24 USAA070413 1 20070523 A 5340 MOUNT BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 STA 947, LBL 25, INBOARD AFT LAV MOUNT HAS CORROSION. REMOVED & REPLACED NEW PART PER IPC 53-42-00: CORR TASK C53-107- 02; LEVEL 2, DEFECT SIZE: 3 INCHES. 2 L 7 2 4F RT A16WE 2007052400212 20070524 00212 NM 2007 5 24 USAA070412 1 20070523 A 5320 TIE CLIP BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 STA 597 S3R HAS CRACK. REMOVED & REPLACED PER SRM 51-20-01, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007052400213 20070524 00213 NM 2007 5 24 USAA070411 1 20070523 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 STA 947-967, LBL 49 HAS CORROSION. INSTALLED NEW PART PER 54C33367 IPC 53-42-00-92; CORR TASK C53-107-02; LEVEL 2, DEFE CT SIZE: 20 INCHES. 2 L 7 2 4F RT A16WE 2007052400217 20070524 00217 NM 2007 5 24 USAA070407 1 20070523 A 5754 65C26602264 SLAT BOEING 737 737401 1384701 NM WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 OUTBOARD OF INBOARD EDGE NR 5 L/E SLAT DELAMINATED. FABRICATED CORE & DOUBLER PER SRM 51-70-10, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007052400218 20070524 00218 NM 2007 5 24 USAA070406 1 20070523 A 5315 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 FWD SIDE OF BS 312 FLOORBEAM, LBL 27, WL 207, STIFFENING ANGLE CRACKED. INSTALLED NEW ANGLE PER SRM 51-10-02, DEFECT SI ZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007052400219 20070524 00219 NM 2007 5 24 USAA070405 1 20070523 A 5313 STRINGER BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 STA 500C/R AT STR 10R HAS CRACK. INSTALLED REPAIR CHANNEL & SPACERS PER SRM 53-00-03, DEFECT SIZE: .3125 INCH. 2 L 7 2 4F RT A16WE 2007052400220 20070524 00220 NM 2007 5 24 USAA070404 1 20070523 A 5320 TIE CLIP BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 BS 706 S-4L HAS CRACK. REPLACED CLIP PER SRM 51-10-02, DEFECT SIZE: .125 INCH. 2 L 7 2 4F RT A16WE 2007052400225 20070524 00225 NM 2007 5 24 USAA070402 1 20070523 A 5320 TIE CLIP BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 STA 277, S-11R, STRINGER TIE CLIP HAS CRACK. INSTALLED NEW CLIP PER SRM 51-10-02, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007052400227 20070524 00227 WP 2007 5 24 ABXA070153 1 20070420 A 5330 591143331 SKIN DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 905AX 47147 FUSELAGE SKIN CRACKED 2 PLACES FS 1087 LONGERON 3 - LONGERON 4 RIGHT. REPAIRED FUSELAGE SKIN AT STA 1095, LONGERON 3 - 4 RIGHT IAW DC9 SRM 53-04. 2 L 7 2 4F A6WE 2007052400229 20070524 00229 WP 2007 5 24 ABXA070156 1 20070425 A 5210 591412161 PAN DOUG DC9 DC932 3022066 WP MAIN ENTRY DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 985AX 47522 MAIN ENTRY DOOR FRAME CRACKED AT FORWARD LOWER CORNER JUST FORWARD OF LOWER HINGE POINT. REMOVED AND REPLACED DOOR PAN SEGMENT IAW DC9 SRM. 2 L 7 2 4F A6WE 2007052400232 20070524 00232 CE 2007 5 24 RU3A0702 1 20070516 A 6120 PROPELLER BEECH 300 300BEECH 1152930 CE OUT OF ADJUST E RU3A O OTHER J WARNING INDICATION LD LANDING 1 SW 15 71 FF6 RT PROP PITCH LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT YAWED RIGHT. POWER INCREASED TO MAINTAIN CONTROL. WHEN RETURNED T O IDLE FOR LANDING IT WAS OK. TROUBLESHOT AND NO FAULT FOUND. DURING FLARE FOR LANDING, RT PROP APPEARED TO GO INTO GR OUND RANGE, NO PROP PITCH LIGHT NOTED. AFTER LANDING, CONDUCTED GND IDLE LOW PITCH CHECK PER CFM, NO ANOMALY NOTED. AD JUSTED BETA RODS AND SET FLIGHT IDLE TORQUE. ALL CHECKS NORMAL. 2 L 7 2 4T A24CE 2007052400233 20070524 00233 EU 2007 5 24 CPCP20070015 1 20070323 A 5320 FLOOR SUPPORT AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 420AT 420 CORROSION FOUND ON LT "Z" FLOOR SUPPORT BETWEEN FRAME 39 AND 40. LEFT "Z" FLOOR REPLACED IAW SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007052400234 20070524 00234 WP 2007 5 24 ABXA070161 1 20070516 A 5311 99115057 FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 FOUND CRACKED FRAME DURING WINDOW FRAME MOD EA 53300036, REF AD 2002-21-09. REMOVED AND REPLACED FRAME IAW DC9 SRM 51-3 0-02. 2 L 7 2 4F A6WE 2007052400235 20070524 00235 EU 2007 5 24 CPCP20070014 1 20070323 A 5311 FRAME AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 420AT 420 CORROSION FOUND ON FRAME 38 BETWEEN STG 21L AND 21R. FRAME 38 21L AND 21R REPAIRED IAW SRM 53-01-40 FIG 414. 2 H 7 2 4T RT A53EU 2007052400236 20070524 00236 WP 2007 5 24 ABXA070162 1 20070516 A 5320 99578607 ANGLE DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 FOUND ANGLE CRACKED DURING WINDOW FRAME MOD EA 53300036, REF AD 2002-21-09. REMOVED AND REPLACED IAW DC9 SRM 51-30-02. 2 L 7 2 4F A6WE 2007052400237 20070524 00237 WP 2007 5 24 ABXA070163 1 20070516 A 5320 99578605 BRACKET DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 FOUND BRACKET CRACKED DURING WINDOW FRAME MOD EA 53300036, REF AD 2002-21-09. REMOVED AND REPLACED BRACKET IAW DC9 SRM 51-30-02. 2 L 7 2 4F A6WE 2007052400238 20070524 00238 EU 2007 5 24 CPCP20070013 1 20070323 A 5320 THRESHOLD AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 420AT 420 CORROSION FOUND ON RT THRESHOLD GUTTER. RT THRESHOLD GUTTER REPLACED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007052400239 20070524 00239 EU 2007 5 24 CPCP20070019 1 20070323 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 420AT 420 CORROSION FOUND ON LT SEAT TRACK BETWEEN 39 AND 41. LT SEAT TRACK BETWEEN FRAME 39 AND 41 REPLACED AS PER SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007052400240 20070524 00240 EU 2007 5 24 CPCP20070011 1 20070323 A 5311 FRAME AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 420AT 420 CORROSION FOUND ON FRAME BEAM 40. FLOORBEAM 40 REPAIRED IAW SRM 53-00-00 FIG 435 SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007052400241 20070524 00241 EU 2007 5 24 CPCP20070012 1 20070323 A 5320 FLOOR SUPPORT AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 420AT 420 CORROSION FOUND ON RT "Z" FLOOR SUPPORT. RT "Z" FLOOR SUPPORT REPLACED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007052400242 20070524 00242 EU 2007 5 24 CPCP20070021 1 20070324 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 420AT 420 FLOORBEAM FRAME 39 FOUND CORRODED NEAR SERVICE DOOR THRESHOLD. FLOOR BEAM REPLACEMENT C/OUT ON NRWC 174954. 2 H 7 2 4T RT A53EU 2007052400243 20070524 00243 EU 2007 5 24 CPCP20070027 1 20070418 A 5320 SUPPORT AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 308AE 308 RT THRESHOLD SUPPORT AND LOWER SURFACE BETWEEN FRME 36 TO 39 CORRODED. RT THRESHOLD BETWEEN FRAME 36 TO 39 REPLACED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007052400244 20070524 00244 EU 2007 5 24 CPCP20070028 1 20070418 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 308AE 308 FLOORBEAM 36 CORRODED ON UPPER AND LOWER SURFACE. NEW FLOORBEAM 36 INSTALLED IAW SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007052400245 20070524 00245 EU 2007 5 24 CPCP20070029 1 20070418 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 308AE 308 FLOORBEAM 39 UPPER AND LOWER SURFACE CORRODED. FLOORBEAM 39 REPLACED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007052400246 20070524 00246 EU 2007 5 24 CPCP20070020 1 20070324 A 5313 STRINGER AEROSP ATR72 ATR72212 8680945 EU FUSLEAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 420AT 420 FOUND CORROSION FOUND ON RT STG 21. STG 21 RT AT FRAME 24 AND 25 REPAIRED IAW SRM 53-00-00 FIG 428. 2 H 7 2 4T RT A53EU 2007052400247 20070524 00247 EU 2007 5 24 CPCP20070026 1 20070418 A 5320 FLOOR SUPPORT AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 308AE 308 LT "Z" FLOOR UPPER AND LOWER SURFACE BETWEEN FRAME 39 AND 40 CORRODED. LEFT "Z" FLOOR SUPPORT BETWEEN FRAME 39-40 REPLA CED AS PER SRM 51-25-02. 2 H 7 2 4T RT A53EU 2007052400248 20070524 00248 EU 2007 5 24 CPCP20070024 1 20070418 A 5320 THRESHOLD AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 308AE 308 LT THRESHOLD CORRODED BETWEEN FRAME 36 AND 39. NEW LT THRESHOLD BETWEEN FRAME 36 AND 39 INSTALLED IAW SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007052400249 20070524 00249 NM 2007 5 24 DHL2007785001 1 20070519 A 5753 SKIN BOEING 727 727214 138407R NM TE FLAP CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 WHILE IN "A" CHECK, RT INBD TE FLAP PREVIOUS REPAIR HAS CHAFFING ON LE OF FOREFLAP. REMOVED PREVIOUS REPAIR IAW B727 SR M 51-30-2. FABRICATED NEW DOUBLER FROM 2024T3 .063 PO NR 9005138 DIM 5 1/4" BY 4 1/4' IAW B727 SRM 57-50-04 FIG 1 AND 5 7-50-2 FIG 3. TREATED AND PRIMED DOUBLER IAW B727 SRM 51-10-2 AND INSTALLED NEW REPAIR DOUBLER AT RT IB TE FOREFLAP (AT WBL 243) IAW B727 SRM 57-50-4 FIG 1 AND 51-30-2. 2 L 7 3 4F A3WE 2007052400250 20070524 00250 NM 2007 5 24 DHL2007788528 1 20070510 A 5753 SKIN BOEING 727 727214 138407R NM TE FLAPS DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 WHILE IN "C" CHECK, 3 DENTS ON R/W I/B AFT FLAP UPPER SURFACE 31", 55", AND 82" FROM I/B END. EVALUATED 3 DENTS AT 31" A=1.5, Y=.032, A/Y=46.37. 55" A=1.5", Y=.038, A/Y=39.47. 82" A=1.8, Y=.028, A/Y=64.28. AREA FOUND WITHIN LIMITS IAW B72 7 SRM 53-10-1 FIG 1. C/W HFEC ON 3 DENTS IAW B727 NDTM PT6 51-00-00 FIG 23. ALL 3 DENTS INDICATE CRACKS. CUTOUT 3 CRA CKED AREAS ON RT IB AFT FLAP UPPER SKIN (1) 1.2" DIA (2) 1" DIA (3) 1.8" DIA CUTOUT 2 DELAMINATED AREAS ON LOWER SKIN (1 ) 8" BY 8" (2) 8" BY 23". FABRICATED UPPER DOUBLERS (1) 4.2" DIA (2) 4" (3) 4.8" DIA. FABRICATED LWR FILLER (1) 8" BY 8" (2) 8 1/2" BY 23" AND DOUBLER 11" BY 11" (20 10 1/2" BY 26" FROM 7075T6 .016 PO NR 9003142. BONDED, CLEANED, TREATED 2 L 7 3 4F A3WE 2007052400251 20070524 00251 SO 2007 5 24 CHQA200700014 1 20070510 A 2913 PV303211MODA PUMP EMB 145 EMB145LR 3260212 SO HYD SYSTEM INOPERATIVE A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 271SK 12230 1214 145305 FLIGHT 7816 - YYA-IAD - DURING TAKEOFF, RECEIVED "HYD 1 LOW QTY". DURING CLIMB, RECEIVED "E1 HYD PUMP FAIL". RAN QRH AND SHUT OFF ELECTRIC HYDRAULIC PUMP 1, GEAR DOORS OPENED DUE TO LACK OF PRESSURE. DECLARED AN EMERGENCY DUE TO NO FLUID IN THE ENGINE DRIVEN PUMP. TRIED TO NORMALLY EXTEND THE GEAR, BUT IT DID NOT LOWER. FOLLOWED QRH FOR ABNORMAL EXTENSION OF GEAR, DIVERTED TO BUF WITH NO INCIDENT. "E1 HYD PUMP FAIL" CLEARED FROM EICAS. MAINTENANCE REMOVED AND REPLACED THE ENG INE DRIVEN PUMP. 2 L 7 2 4T RT T00011AT 2007052400252 20070524 00252 SO 2007 5 24 CHQA200700015 1 20070513 A 2824 2810051104 VALVE EMB 145 EMB145LR 3260212 SO FUEL SYSTEM LEAKING A CHQA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 11 571RP 8144 8144 14500827 FLIGHT 6428 - CMH-MCO - AFTER TAKEOFF CLIMBING THROUGH 3500 FEET, FLIGHT ATTENDANT CALLED SAYING THERE WAS FUEL POURING OUT OF THE RIGHT WING. BY LOOKING AT THE FUEL QUANTITY GAUGES, THERE WAS A 100 POUND DIFFERENCE. RETURNED TO FIELD. M AINTENANCE REMOVED AND REPLACED THE RIGHT WING VENT VALVE. 2 L 7 2 4T RT T00011AT 2007052400253 20070524 00253 NM 2007 5 24 07FDEA01778 1 20070512 A 3150 WARNING HORN BOEING 727 727227 1384078 NM FALSE ACTIVATION A FDEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 493FE 21531 REJECTED TAKEOFF AT 75 KTS, ACFT WEIGHT 130,000 DUE TO UNSCHEDULED AIRSPEED/MACH AURAL WARNING SYSTEM MEL 12MAY07 03:27, BFM R ACN RELEASED FOR SERVICE PER MEL/CDL: 34-04-03 CATEGORY: B EXPIRATION: 15MAY07. MEM R PERFORMED MACH AURAL WARN TEST IAW 727-200 M/M 34-14-002-5 AND NO FAULTS FOUND, UNABLE TO DUPLICATE REPORTED DISCREPANCY. REMOVED AND REPLACED B OTH CAPT'S AND F/O'S MACH AIRSPEED INDICATORS IAW 727-200 M/M 34-12-021-4. 2 L 7 3 4F A3WE 2007052400254 20070524 00254 2007 5 24 QXEA200700828 2 20070519 A 7320 8193007008 FADEC BOMBDR DHC8 DHC8402 1390042 NM ENGINE MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 415QX 1474 4081 SJC FLIGHT NR 2406: POWER PLANT MESSAGE ON ED DURING PUSHBACK AND TAXI. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND INSTALLED SERVICEABLE FADEC IAW Q400 AMM TASK 73-21-01-000-801 AND 73-21-01-400-801. OPS CHECK GOOD. AIRCRAFT RET URNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007052400255 20070524 00255 NM 2007 5 24 QXEA200700829 1 20070520 A 2120 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM CABIN ODOR A QXEA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 422QX 4150 LAX FLIGHT NR 2307: CREW REPORTS 'HOT ELECTRICAL SMELL' IN AFT GALLEY AFTER PUSHBACK. AIRCRAFT RETURNED TO GATE. MAINT ENANCE INSPECTED BOTH HOT WATER JUGS FOR ANY SIGNS OF HEAT DAMAGE OR SMELLS WITH AND WITHOUT RUNNING. REMOVED AFT GALLE Y CENTER OVERHEAD PANEL FOR INSPECTION. REINSTALLED PANEL. INSPECTED RECIRC FAN AND PACK AREA FOR EXCESSIVE HEAT OR SM ELLS. INSPECTED ALL OVERHEAD AND SIDEWALL LIGHT BALLASTS AND PSU PANELS. NO HEAT DAMAGE, SMELLS OR OTHER DEFECTS NOTED . INSPECTED AFT CARGO PIT AND LIGHTING. REMOVED FWD LT TRASH CART. GROUND RAN BLEEDS OF APU, 31 AND 32 ENGINE IN VARI OUS SETTINGS SEPARATELY AND TOGETHER FOR 3 SEPARATE 30 MINUTE SESSIONS. ALSO CYCLING RECIRC FAN ON AND OFF. INITIALLY 2 H 7 2 4T RT A13NM 2007052400256 20070524 00256 WP 2007 5 24 AALA20070892 1 20070519 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 561AA 53091 LGA - SEAT TRACK EGRESS EMERGENCY LIGHT AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR SEAT TRACK EGRESS EMERG ENCY LIGHT AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007052400257 20070524 00257 WP 2007 5 24 AALA20070904 1 20070521 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 580AA 53157 LGA - EMERGENCY EXIT LIGHT AT FORWARD RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT AT FORWARD RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007052400258 20070524 00258 WP 2007 5 24 AALA20070914 1 20070522 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 77421 49333 LGA - EMERGENCY LIGHT AT OVERHEAD SEATS 20DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD SEATS 20DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007052400259 20070524 00259 NM 2007 5 24 AALA20070912 1 20070517 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 924AN 29525 TUL - EMERGENCY LIGHT BATTERY PACK AT M1675 INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK AT M1675. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007052400260 20070524 00260 NM 2007 5 24 AALA20070909 1 20070522 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 394AN 29431 DFW - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 24B INOPERATIVE. RELAMPED SEAT MOUNTED EMERGENCY LIGHT AT SEAT 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007052400261 20070524 00261 NM 2007 5 24 AALA20070913 1 20070517 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 924AN 29525 TUL - EMERGENCY LIGHT BATTERY PACK AT M1676 INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK AT M1676. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007052400262 20070524 00262 NM 2007 5 24 AALA20070908 1 20070522 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 394AN 29431 DFW - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 24A INOPERATIVE. RELAMPED SEAT MOUNTED EMERGENCY LIGHT AT SEAT 24A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007052400263 20070524 00263 NM 2007 5 24 AALA20070910 1 20070507 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 964AN 30093 TUL - EMERGENCY LIGHT BATTERY PACK AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORW ARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007052400264 20070524 00264 WP 2007 5 24 ABXA070164 1 20070516 A 5320 99578606 BRACKET DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 FOUND CRACKED BRACKET DURING WINDOW FRAME MOD 9957860-6, REF AD 2002-21-09. REMOVED AND REPLACED BRACKET IAW DC9 SRM 51 -30-2. 2 L 7 2 4F A6WE 2007052400267 20070524 00267 WP 2007 5 24 ABXA070160 1 20070516 A 5311 99115056 FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 FOUND FRAME CRACKED DURING WINDOW FRAME MOD EA 53300036, REF AD 2002-21-09. REPAIRED FRAME IAW DC9 SRM 53-03 FIG 34. 2 L 7 2 4F A6WE 2007052400268 20070524 00268 EU 2007 5 24 WRNA200700024 1 20070502 A 3230 A5281104820100 UPLOCK AIRBUS 300 A300B4203 3930306 EU NLG WORN A WRNA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 SO 05 504TA 216 NOSE GEAR DOOR UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF ALONG WITH SEVERE VIBRATION FROM NOSE GEAR AREA. FOUND RIGHT NOSE LANDING GEAR DOOR UP-LOCK ROLLER ASSEMBLY BRACKET LOOSE. REPLACED RIGHT HAND FORWARD SERRATED PLATE P/N A5281106120100 AND AFT SERRATED PLATE P/N A5281106120000 AND AFT UP-LOCK ROLLER FITTING P/N A5281104820100, ACCOMPLISHED RIG AND OPS C HECK, IAW A300 MM 32-22-11. CHECKED GOOD, A/C RELEASED FOR SERVICE. 2 L 7 2 4F RT A35EU 2007052400269 20070524 00269 NM 2007 5 24 CALA0700253 1 20070518 A 5311 BAC15141087 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND A 1 INCH CRACK IN LEFT MAIN FRAME AT STA 616, S17L, BELOW MAIN DECK FLOOR. THE FRAME WAS REPAIRED IAW ECRA 5311-01158. 2 L 7 2 4F RT A16WE 2007052400271 20070524 00271 NM 2007 5 24 CALA0700255 1 20070522 A 5311 6545810 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND FRAME CORRODED AT STA 312, S28L. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-40-02 AND 53-00-07. 2 L 7 2 4F RT A16WE 2007052400272 20070524 00272 EA 2007 5 24 COMA0770029 1 20070510 A 2150 GG670950095 ACM CNDAIR CL600 CL6002C10 1390015 EA A/C BAY SEIZED A COMA D RETURN TO BLOCK J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 669CA 10596 10176 FLIGHT 5282 - RECEIVED RIGHT PACK FAIL MESSAGE AND SMOKE IN CABIN. SMOKE DISSIPATED AFTER PACK WAS DESELECTED. RETURNE D TO GATE. REPLACED RIGHT ACM. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007052400278 20070524 00278 SO 2007 5 24 RAIA00705035 1 20070518 A 3350 RPS1B BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 833HK 145240 PRE FLT NR 7922 - DAY - EMERGENCY LIGHT FLOOR PROXIMITY AND AFT CEILING EXIT LOCATOR BOTH OVERWING EXIT IDENTIFIER ARE I NOP. MAINTENANCE REMOVED AND REPLACED NR 3 BATTERY PACK SYSTEM, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007052400280 20070524 00280 SO 2007 5 24 RAIA00705037 1 20070519 A 2611 SMOKE WARNING EMB 145 EMB145LR 3260212 SO CARGO BAY MALFUNCTIONED A RAIA F A ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 846HK 14500855 FLT NR 7920 - STL - BAG SMOKE LIGHT ILLUMINATED, PUSHED BAG FIRE BOTTLE BUTTON. MAINTENANCE INSPECTED AND FOUND NO EVID ENCE OF FIRE. REMOVED AND REPLACED FIRE BOTTLES, OPS CHECK SMOKE DETECTION SYSTEM, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007052400281 20070524 00281 SO 2007 5 24 RAIA00705038 1 20070519 A 3350 317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 842HK 14500830 PRE FLT NR 7911 - ORD - EMERGENCY LIGHT IN CEILING AFT AISLE FLOOD LIGHT IS OUT. MAINTENANCE RELAMPED EMERGENCY LIGHT, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007052400284 20070524 00284 EU 2007 5 24 200705213 1 20070520 A 3234 9037B000104 CONTROL HANDLE EMB ERJ170 ERJ170100SE 3260406 EU COCKPIT DEFECTIVE A UHLA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 11 646RW 32 17000066 FLIGHT 7722 ORD TO GRR GEAR DID NOT RETRACT UPON TAKEOFF, RETURN TO ORD, NORMAL LANDING. MAINTENANCE REMOVED AND REPLAC ED THE LANDING GEAR CONTROL HANDLE. 2 L 7 2 4F RT A56NM 2007052400286 20070524 00286 EU 2007 5 24 WRNA200700025 1 20070512 A 5540 A55470010002D RUDDER AIRBUS 300 A300B4203 3930306 EU DELAMINATED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 501TR 53 DURING WALK AROUND POSSIBLE DELAMINATION NOTED ON TRAILING EDGE OF RUDDER. RUDDER REMOVED, REPAIRED IAW SRM 55-41-11 PG 148-149, SRM 51-21-00 PG 15, 21, 22 SRM 51-40-00 PG 731-733 FIG 709, SRM 55-41-11 PG 148, 149 SRM 51-42-20 AND PCS PROCE SS PROCEDURES PCS-PS0001, SRM 51-41-50. PRIMED AND PAINTED IAW SRM 51-40-12. RUDDER RETURNED SERVICEABLE TO BE RE-INST ALLED ON AIRCRAFT. 2 L 7 2 4F RT A35EU 2007052400287 20070524 00287 NM 2007 5 24 KCSA071165 1 20070521 A 5412 BULKHEAD BOEING 747 747212B 1384886 NM NR 1 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 NR 1 PYLON HAS APPROX 2.5 INCHES CRACK ON CLOSURE BULKHEAD WEB AT NAC STA 180 BETWEEN WL 138 AND WL 152. 2 L 7 4 4F A20WE 2007052400288 20070524 00288 NE 2007 5 24 COMA0760375 2 20070508 A 7261 6087T04P06 SCAVENGE PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENGINE FAILED A COMA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 416CA 20512 7450 FLIGHT 5679 - EN ROUTE CVG-PVD RECEIVED A LOW LEFT ENGINE OIL PRESSURE WARNING, CREW DECLARED AN EMERGENCY, PERFORMED IF SD OF THE LEFT ENGINE AND DIVERTED TO PIT. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT ENGINE LUBRICATION/SCAVEN GE PUMP. 2 L 7 2 4F 4 F RT A21EA E15NE 2007052400289 20070524 00289 SO 2007 5 24 RAIA00705029 1 20070515 A 3350 LIGHT EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 827HK 145021 PRE FLT NR 5470 - STL - EMERGENCY LIGHT MAIN DOOR FLOOD LIGHT IS INOP. MAINTENANCE REMOVED AND REPLACED BULB, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007052400290 20070524 00290 SO 2007 5 24 RAIA0070530 1 20070515 A 5270 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 831HK 145232 FLT NR 8036 - SYR - BAG DOOR CAPTION WILL NOT EXTINGUISH. MAINTENANCE DEFERRED PER MEL. 2 L 7 2 4T RT T00011AT 2007052400291 20070524 00291 NM 2007 5 24 CALA0700257 1 20070522 A 5311 6545810 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND FRAME CORRODED AT STA 312, RBL 2, S27R-28R. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED I AW SRM 53-00-07, FIGURE 201, REPAIR 1. 2 L 7 2 4F RT A16WE 2007052400294 20070524 00294 EA 2007 5 24 COMA0760377 1 20070513 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 929CA 31723 7035 CRACK AT RIGHT SIDE FS 574.00 BETWEEN STRINGERS 6 AND 7. REPLACED SPLICE ANGLE IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007052400295 20070524 00295 EA 2007 5 24 COMA0760378 1 20070515 A 3350 59257 INVERTER CNDAIR CL600 CL6002B19 1900309 EA CABIN FAULTY A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 914CA 7012 FLIGHT 5302 - CABIN FLOOR EMERGENCY LIGHTING INOPERATIVE BETWEEN SEATS 1 AND 5. REPLACED INVERTER AT BATTERY PACK NR 3. 2 L 7 2 4F RT A21EA 2007052400296 20070524 00296 SO 2007 5 24 200714311 1 20070522 A 5347 13500439003 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 24 AND 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM. RETURNED AIRC RAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052400297 20070524 00297 SO 2007 5 24 200714307 1 20070522 A 5320 14524131009 BRACKET EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 DURING MBV INSPECTION, FOUND FORWARD CABIN FLOOR U SHAPE BRACKET AT FRAME 17 AND STRINGER 16 LEFT SIDE CORRODED. REMOVE D AND REPLACED BRACKET IAW EMB SRM. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052400299 20070524 00299 SO 2007 5 24 200714319 1 20070522 A 5347 14530659005 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 LEFT INBOARD SEAT TRACK BETWEEN FRAMES 36 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM AND ETN 53-110R2 . RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052400302 20070524 00302 SO 2007 5 24 200714313 1 20070522 A 5347 14532606017 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAME 47 AND 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM AND ETN EM 53-11 0R2. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052400304 20070524 00304 SO 2007 5 24 200714321 1 20070522 A 5347 14530658007 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM. RETURNED AIRC RAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052400305 20070524 00305 SO 2007 5 24 200714320 1 20070522 A 5347 13500412003 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 LEFT INBOARD SEAT TRACK BETWEEN FRAMES 53 AND 55 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM AND ETN EM-53-11 0R2. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052500003 20070525 00003 SO 2007 5 25 200714324 1 20070522 A 5347 14530658005 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 36 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM. RETURNED AIRC RAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052500004 20070525 00004 SO 2007 5 25 200714305 1 20070522 A 5315 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 FOUND FLOORBEAM AT FRAME 22 CORRODED. REMOVED AND REPLACED FLOORBEAM IAW EMB SRM. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052500005 20070525 00005 SO 2007 5 25 200714310 1 20070522 A 5347 14532606015 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 FOUND LEFT OUTBOARD SEAT TRACK BETWEEN FRAMES 36 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM. RETURNE D AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052500006 20070525 00006 SO 2007 5 25 200714316 1 20070522 A 5347 14532605015 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 RIGHT OUTBOARD SEAT TRACK BETWEEN FRAMES 36 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM. RETURNED AIR CRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052500008 20070525 00008 SO 2007 5 25 200714325 1 20070522 A 5347 14530659007 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 LEFT INBOARD SEAT TRACK BETWEEN FRAMES 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM. RETURNED AIRCR AFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052500009 20070525 00009 SO 2007 5 25 200714309 1 20070522 A 5347 14532605017 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 RIGHT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAME 47 AND 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM AND ETN EM 53-1 10R2. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052500011 20070525 00011 SO 2007 5 25 200714308 1 20070522 A 5347 13500439007 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 FOUND LEFT INBOARD SEAT TRACK BETWEEN FRAMES 17 AND 23 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052500014 20070525 00014 EA 2007 5 25 200714303 1 20070506 A 5320 67053110522 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 522AE 7696 3878 10147 WEB AT STATION 280 LEFT AND RIGHT SIDE AT FLOORBEAM MATING AREA CORRODED. REMOVED AND REPLACED WEB IAW AEA EO CR 53MR 1 23. 2 L 7 2 4F RT A21EA 2007052500015 20070525 00015 SO 2007 5 25 200714301 1 20070520 A 5320 14525422001 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 935AE 14500920 LEFT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 60 AND 61 CORRODED. C/A - REPLACED FLOOR SUPPORT IN ACCORDANCE WITH EMB SRM. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007052500016 20070525 00016 EA 2007 5 25 QXEA200700720 1 20070506 A 2840 73811813 COMPUTER CNDAIR CL600 CL6002C10 1390015 EA FUEL QTY INOPERATIVE A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 611QX 10026 938 10041 PDX - FLIGHT 2512. RECEIVED A FUEL CHANNEL 1/2 CAUTION MESSAGE. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LAN DING. MAINTENANCE FOUND WATER ON THE FUEL QUANTITY GAUGING COMPUTER AND TRAY. REPLACED FQGC AND CLEANED AREA OF WATER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007052500017 20070525 00017 EA 2007 5 25 QXEA200700780 1 20070510 A 2910 TY215215A ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA THRUST REVERSER BROKEN A QXEA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 NM 09 603QX 14988 10011 PDX - UPON LANDING HYDRAULIC SYSTEM NR 1 LOST PRESSURE. ENGINE PUMP RAN 10 MINUTES AFTER PRESSURE LOSS, AND ELECTRIC PU MP RAN 5 MINUTES. MAINTENANCE FOUND THE NR 1 FEEDBACK ACTUATOR ON THE THRUST REVERSER LEAKING AT THE LOWER DRIVESHAFT A TTACH POINT DUE TO BROKEN ATTACH HARDWARE. REPLACED THE ACTUATOR. OPERATIONAL CHECKS GOOD AIRCRAFT RETURNED TO SERVICE . 2 L 7 2 4F RT A21EA 2007052500018 20070525 00018 EA 2007 5 25 QXEA200700717 1 20070503 A 2612 FIRE WARNING CNDAIR CL600 CL6002C10 1390015 EA FALSE ACTIVATION A QXEA K NONE N FALSE WARNING IN INSP/MAINT 1 NM 09 612QX 10042 SEA - FIRE SYSTEM FAULT MESSAGE DISPLAYED INTERMITTENT. MAINTENANCE PERFORMED CONTINUITY CHECK OF SYSTEM. ALL CHECKS G OOD. AIRCRAFT RETURNED TO SERVICE WITH NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007052500019 20070525 00019 EA 2007 5 25 QXEA200700718 1 20070503 A 4900 WE38007703 APU CNDAIR CL600 CL6002C10 1390015 EA ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 290RB 3867 10029 PDX - CABIN HAS A "DIRTY SOCK" ODOR. MAINTENANCE REPLACED THE APU IAW AMM 49-10-00-000-801-A01. OPERATIONAL CHECKS GOO D. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007052500020 20070525 00020 EA 2007 5 25 QXEA200700783 1 20070510 A 2150 GG43620053 SENSOR CNDAIR CL600 CL6002C10 1390015 EA NR 2 A/C PACK MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 618QX 10205 FAT- FLIGHT 2534, RECEIVED A RIGHT PACK FAULT STATUS MESSAGE. MAINTENANCE COULD NOT DUPLICATE. ON 5/13, SAME MESSAGE R ECEIVED AND MAINTENANCE REPLACED THE NR 2 PACK DISCHARGE TEMP SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4F RT A21EA 2007052500021 20070525 00021 2007 5 25 QXEA200700826 4 20070521 A 3442 071015190101 TRANSCEIVER BOMBDR DHC8 DHC8402 1390042 NM WX RADAR SYS MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 404QX 676 247 4046 SEA FLIGHT NR 2019: WX FAIL IN CRUISE. CYCLED OFF PER MTX. MFD SHOWED MESSAGE IN ALL POSITIONS. AIRCRAFT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED THE WEATHER RADAR TRANSCEIVER PER Q400 AMM 34-41-01, PG 401-406. OPS CHECK GOO D. NO WX FAIL MESSAGE SHOWN. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007052500022 20070525 00022 NM 2007 5 25 QXEA200700830 1 20070515 A 7921 D2887355C VALVE BOMBDR DHC8 DHC8402 1390042 NM OIL COOLER MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 413QX 4060 MFR FLIGHT: NR 1 OIL TEMP, 119 DEGREES IN CRUISE AT FL250. BYPASS DOOR CLOSED IAW EMERGENCY CHECK LIST. NO CHANGE. IN FO CRUISE TQ 65 PERCENT OAT - 27. NR 1 OIL PRESSURE 69. MAINTENANCE PERFORMED SPECIAL INSPECTION FOR ELEVATED OIL TEMP PER Q400 MM 05-53-00-210-814 FOR LEVEL B OIL TEMP AND REPLACED OIL COOLER BYPASS VALVE PER Q400 MM 79-21-06-400-801. A LL POST MTX TESTS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007052500024 20070525 00024 EA 2007 5 25 SWIA200718233 1 20070516 A 3350 AD20131A POWER SUPPLY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT FAILED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 455SW 6353 6353 7760 THIRD AND FOURTH OVERHEAD EMERGENCY FLOOD LIGHT IS INOP. REPLACED NR 3 ELBP WITH A SERVICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007052500026 20070525 00026 EU 2007 5 25 AALA20070930 1 20070520 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 50051 459 MIA - EMERGENCY LIGHT AT SEAT 11G INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 11G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007052500028 20070525 00028 NM 2007 5 25 AALA20070935 1 20070524 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 779AN 29955 MIA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 26C HAS MISSING LENS. REPLACED LENS FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007052500029 20070525 00029 NM 2007 5 25 AALA20070936 1 20070524 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 779AN 29955 MIA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 26C INOPERATIVE. RELAMPED SEAT MOUNTED EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007052500030 20070525 00030 NM 2007 5 25 AALA20070934 1 20070524 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 779AN 29955 MIA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 22C HAS MISSING LENS. REPLACED LENS FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007052500032 20070525 00032 NM 2007 5 25 AALA20070933 1 20070524 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 779AN 29955 MIA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. RELAMPED SEAT MOUNTED EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007052500033 20070525 00033 NM 2007 5 25 AALA20070921 1 20070417 A 3350 8200037702 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 915AN 29516 TUL - EMERGENCY LIGHT AT RIGHT OVERWING EXIT STATION 628 HAS CRACKED LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RIGHT O VERWING EXIT STATION 628. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007052500035 20070525 00035 NM 2007 5 25 AALA20070922 1 20070417 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 915AN 29516 TUL - EMERGENCY LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007052500038 20070525 00038 NM 2007 5 25 AALA20070923 1 20070419 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 961AN 30092 TUL - EMERGENCY LIGHTS AT MID CABIN STATION 565 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID CABIN ST ATION 565. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007052500040 20070525 00040 NM 2007 5 25 AALA20070925 1 20070430 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 963AN 29543 TUL - EMERGENCY LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK AT M1676 FOR EMERGENCY LIGHTS AT MID CABIN. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007052500041 20070525 00041 NM 2007 5 25 AALA20070918 1 20070417 A 3350 8200037702 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 915AN 29516 TUL - EMERGENCY LIGHT AT OVERWING EXIT STATION 590 HAS CRACKED LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERWING EXIT STATION 590. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007052500042 20070525 00042 NM 2007 5 25 AALA20070917 1 20070417 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 915AN 29516 TUL - EMERGENCY LIGHTS IN MID CABIN INOPERATIVE. REPLACED BATTERY PACK M1694 FOR EMERGENCY LIGHTS IN MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007052500043 20070525 00043 EU 2007 5 25 AALA20070931 1 20070520 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 50051 459 MIA - EMERGENCY LIGHT AT SEAT 18G INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 18G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007052500045 20070525 00045 EA 2007 5 25 QXEA200700781 1 20070508 A 3150 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA UNKNOWN A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 601QX 10009 DEN - FLIGHT 4183, RIGHT BLEED MASTER CAUTION ON CLIMB-OUT. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING . MAINTENANCE FOUND NO POSTED MESSAGE IN MDC. PERFORMED FIM TASK 30-22-01-810-810-A01. NO DEFECTS NOTED. PERFORMED O PS CHECK OF PRSOV WITH NO DEFECTS. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007052500046 20070525 00046 EA 2007 5 25 200714201 1 20070520 A 3320 F18T5WW BULB CNDAIR CL600 CL6002C10 1390015 EA CABIN LIGHT BROKEN A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 21 515AE 10121 FLIGHT ATTENDANT NOTICED RUBBER BURNING SMELL FROM AROUND ROW 17. REMOVED AND REPLACED BROKEN CEILING LIGHT BULB IAW CR J AMM. OPS CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007052500048 20070525 00048 2007 5 25 QXEA200700823 4 20070520 A 3442 071015190101 TRANSCEIVER BOMBDR DHC8 DHC8402 1390042 NM WX RADAR SYS MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 427QX 121 4 4156 BZN FLIGHT NR 2381: WX FAIL MESSAGE ON MFD 1. RAN CHECKLIST. RECEIVED TEST PATTERN BUT NO RETURNS WITH WX FAIL MESSAGE AGAIN. MAINTENANCE REMOVED AND REPLACED WX RADAR TRANSCEIVER. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007052500054 20070525 00054 EA 2007 5 25 QXEA200700818 1 20070509 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT DISCHARGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 616QX 10573 2774 10128 OKC - MID CABIN EMERGENCY EXIT SIGN LIGHTS ARE INOP. REPLACED BATTERY PACK EPSU IAW CRJ-700 33-51-17-000-801-A01. OPER ATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007052500057 20070525 00057 WP 2007 5 25 AALA20070893 1 20070520 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 298AA 49310 LGA - EMERGENCY LIGHT AT OVERHEAD COCKPIT INOPERATIVE. REPLACED BATTERY PACK AT FORWARD CABIN FOR EMERGENCY LIGHT AT OV ERHEAD COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007052500059 20070525 00059 EU 2007 5 25 AALA20070901 1 20070520 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 50051 459 MIA- EMERGENCY LIGHT AT SEAT 18G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 18G. SYSTEM GROUND CHECKED NORMAL OPERA TION. 2 L 7 2 4F RT A35EU 2007052500061 20070525 00061 WP 2007 5 25 AALA20070915 1 20070522 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 77421 49333 LGA - EMERGENCY LIGHT AT OVERWING FORWARD POSITION INOPERATIVE. REPLACED BATTERY PACK IN OVERHEAD BIN FOR EMERGENCY LIG HT AT OVERWING FORWARD POSITION. 2 L 7 2 4F A6WE 2007052500063 20070525 00063 NM 2007 5 25 DHL2007785002 1 20070519 A 5310 WEB BOEING 727 727214 138407R NM BS 1303 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 WHILE IN "A" CHECK, CRACK ON AFT AIRSTAIR AREA TORQUE BOX WEB AT LIGHTENING HOLE BS 1303. STOP DRILLED CRACK IAW B727 SRM 51-10-1 PARA 10. FAB REPAIR DOUBLER FROM 7075T6 .040 PO NR 9004940 APPROX DIM 4" BY 2" IAW B727 SRM 51-40-2 FIG 1 A ND 53-10-2 FIG 6. INSTALLED REPAIR DOUBLER AT AFT AIRSTAIR TORQUE BOX WEB BS1303 IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007052500065 20070525 00065 WP 2007 5 25 AALA20070905 1 20070521 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 496AA 49734 LGA - EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT B523 FOR EMERGENCY LIGHTS IN FORWARD CABI N. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007052500066 20070525 00066 NM 2007 5 25 AALA20070911 1 20070507 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 964AN 30093 TUL - EMERGENCY LIGHTS AT RIGHT SEAT ROWS 15 TO 21 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT SEA T ROWS 15 TO 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007052500067 20070525 00067 NM 2007 5 25 AALA20070895 1 20070520 A 2750 PIN BOEING 757 757223 1384957 NM TE FLAP DAMAGED A AALA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SW 21 677AN 29427 JFK INFLIGHT T1298/20MAY MIA TO LGA - TRAILING EDGE FLAP DISAGREE INDICATION ILLUMINATED ON APPROACH. LANDING MADE WITH FLAPS AT 20. DECLARED EMERGENCY AND LANDED JFK WITHOUT INCIDENT DUE TO HIGHER LANDING SPEED. FOUND LEFT INBOARD FLAP INBOARD TRANSMISSION OVER TORQUE PIN POPPED. RESET PIN AND SERVICED TRANSMISSION. SYSTEM GROUND CHECKED NORMAL OPERATI ON. 2 L 7 2 4F RT A2NM 2007052500070 20070525 00070 WP 2007 5 25 AALA20070894 1 20070520 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 979TW 53629 LAX - EMERGENCY LIGHTS AT AFT EXIT SIGNS LEFT AND RIGHT OVERWING DOORS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT EXIT SIGNS LEFT AND RIGHT OVERWING DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007052200012 20070522 00012 EU 2007 5 22 07FDEA01789 1 20070515 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 401FE 191 2 AREAS CORROSION EXIST AT MDCC SEAT TRACK L-4 BETWEEN FRAMES 2/32 AND FRAME 33, DEFECTED AREA MEASURE 1.5 SQ INCHES. R EMOVED CORROSION IAW A310 SRM 51-74-10 MATERIAL LOSS IN LIMITS IAW A310 SRM 53-10-1. SEAT TRACK REMOVED AND REPLACED IA W A310 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007052200021 20070522 00021 SO 2007 5 22 SIMA200713801 1 20070513 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN ODOR A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 662EH 7305 2199 145777 CAE312735 ON TAKEOFF, LAVATORY SMOKE LIGHT ILLUMINATED WITH STRONG ODOR IN CABIN, RETURNED TO CMI. REMOVED AND REPLACED NUMBER 2 ENGINE IAW AMERICAN EAGLE WORK CARD. PERFORMED OPERATIONAL AND LEAK CHECKS WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007052200024 20070522 00024 NM 2007 5 22 HALA0700020 1 20070106 A 4990 O-RING BOEING 767 767300 1385204 NM APU OIL CAP CUT A HALA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 13 590HA 33467 ETOPS SIGNIFICANT SYSTEM, APU HAD AUTO SHUTDOWN. FAULT LIGHT ILLUMINATED. EICAS MESSAGE APU FAULT DISPLAYED (NOTE: OIL .5 NOW .75 EGT WAS 770 DEGS). OK FOR SERVICE PER FIM 49-11-00 FIM SERVICED APU OIL AND REPLACED APU CAP O-RING, NO LEA KS NOTED. 2 L 7 2 4F RT A1NM 2007052200030 20070522 00030 EU 2007 5 22 07FDEA01803 1 20070515 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 AFT CARGO PIT/CABIN FLOORBEAM 61 CRACKED AT APPROX 6 FEET RLL TOTAL CRACK LENGTH .30 APPROX COMPLIED WITH FEDEX EA6-53 10-11460. 2 L 7 2 4F RT A35EU 2007052200033 20070522 00033 EU 2007 5 22 07FDEA01806 1 20070515 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 6 AREAS OF CORROSION EXIST AT MDCC SEAT TRACK L-3 BETWEEN FRAMES 74 THRU 79 EACH DEFECTED AREA MEASURE 1.5 SQ INCHES COR ROSION REMOVED IAW A310/200 SRM 51-74-10 ONE SPOT FOUND OUT OF LIMITS IAW A310/200 SRM 53-10-16 DAMAGED AREA TRIMMED OUT IAW SRM 53-10-16. REPLACED PARTS, FABED IAW SRM 53-10-16, NEW PARTS ALODINED IAW A310/200 SRM 51-21-10 PARTS, PROTECTE D IAW A310/200 SRM53-10-16 SEAT TRACK CUT AND SPLICED AT FR 77 10" -80/82. 2 L 7 2 4F RT A35EU 2007052200036 20070522 00036 NM 2007 5 22 NWAA071786716 1 20070510 A 2612 FIRE LOOP BOEING 747 747251F 1384898 NM B SYSTEM NO TEST A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 616US 21120 DURING FLIGHT, PILOT HAD A MOMENTARY "FIRE DETECTION" LIGHT ON FORWARD PANEL WITH MOMENTARY AURAL WARNING. ACCOMPLISHED COM PROCEDURE AND FOUND "B" LOOP FAILED TEST. FLIGHT CONTINUED ON AND LANDING WAS UNEVENTFUL. MAINTENANCE INTERCHANGE D FIRE DETECTOR CARDS PER FIM. OPERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F A20WE 2007052200039 20070522 00039 NM 2007 5 22 HALA0700211 1 20070518 A 3350 LIGHT BOEING 767 76733A 1385209 NM CABIN INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 583HA 25531 FLOOR PATH FROM SEAT 16 THRU 20 EMERGENCY, LIGHTS INOP, LEFT SIDE. REMOVED AND REPLACED EMERGENCY LIGHTS. FLOOR PATH F ROM SEAT 16 THRU 20 PER 33-51-3. OPS CHECK NORMAL, OK FOR SERVICE, LEFT SIDE. 2 L 7 2 4F RT A1NM 2007052200040 20070522 00040 NE 2007 5 22 HALA0700214 2 20070516 A 7200 ENGINE BOEING 767 767300 1385204 NM PWA 4060 PW4060 52119 NE RIGHT SMOKE A HALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM, ON TAKEOFF (HNL) TOWER REPORTED SMOKE FROM RIGHT ENG. ENG INDICATIONS NORMAL CONTINUED TO LAX PER MAINT CONTROL. RAN ENGINE FOR 5 MINUTES NO LEAKS NOTED. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007052200046 20070522 00046 EU 2007 5 22 SIMA200714004 1 20070514 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 313AE 14537 340B313 ALL EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED ALL FIVE EMERGENCY LIGHT POWER SUPPLIES IAW SAAB AMM 33-50-10. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007052200047 20070522 00047 EU 2007 5 22 SIMA200714006 1 20070514 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 902AE 25087 639 340B269 AFT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AT ROW 9BC IAW SAAB AMM 33-50-10. OPERAT IONAL CHECKED GOOD, RETURN AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007052200069 20070522 00069 SO 2007 5 22 SIMA200714025 1 20070513 A 5347 145030659005 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 719AE 15875 4800 145276 LEFT SEAT TRACK CORRODED BETWEEN FRAMES 36 AND 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURNED AIRC RAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052200070 20070522 00070 SO 2007 5 22 SIMA200714026 1 20070513 A 5347 14530658007 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 719AE 15875 4800 145276 RIGHT SEAT TRACK CORRODED BETWEEN FRAMES 47 AND 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN E AGLE ENGINEERING TECHNICAL NOTICE EM-53-110R2. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052200077 20070522 00077 SO 2007 5 22 SIMA200714001 1 20070513 A 2741 3621001013 COMPUTER EMB 145 EMB145LR 3260212 SO ZONE 300 FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 690AE 6581 14500858 PITCH TRIM MAIN INOP WARNING MESSAGE, RETURNED TO DFW. REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT IAW EMB AMM 27-40-01. OPERATIONAL CHECKED GOOD, PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS. RETURNED AIRCRAFT TO SERVIC E. 2 L 7 2 4T RT T00011AT 2007052200081 20070522 00081 SO 2007 5 22 SIMA200714034 1 20070508 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 942LL 4931 14500930 SERVICE DOOR CENTER SILL CORRODED. REMOVED CORROSION, PERFORMED NDT WITH NO REJECTABLE DEFECTS NOTED. FABRICATED AND I NSTALLED DOUBLER IAW EMB SRM 53-21-02. 2 L 7 2 4T RT T00011AT 2007052200083 20070522 00083 NM 2007 5 22 DL76L070563 1 20070516 A 5415 311T31571 ANGLE BOEING 767 767332 1382001 NM NR 1 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 179DN 25144 THE NR 1 ENGINE PYLON CLOSEOUT ANGLE WAS FOUND CRACKED. THE CLOSEOUT ANGLE WAS REMOVED AND REPLACED. 2 L 7 2 4F RT A1NM 2007052200088 20070522 00088 NM 2007 5 22 DL757070570 1 20070518 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM FS 434 S17L DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 602DL 22809 DURING CURRENT HMV, A DENT WAS FOUND ON THE EXTERIOR SKIN PANEL P/N 143N3320-3 JUST ABOVE S-17L AT FS 443. THE SUBJECT DAMAGE WAS OUTSIDE OF THE ALLOWABLE DAMAGE LIMITS OF THE SRM. THE DAMAGE WAS TRIMMED OUT AND AN EXTERNAL REPAIR DOUBLER INSTALLED PER ER/A 460840-14, WHICH WAS BOEING APPROVED. 2 L 7 2 4F RT A2NM 2007052200094 20070522 00094 NM 2007 5 22 DL76S070578 1 20070521 A 5312 BAC15051011192 BULKHEAD BOEING 767 767332 1382001 NM BS 1725 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 128DL 24078 BULKHEAD OUTER CORD STRAP FOUND CRACKED AT STRINGER-7R BS 1725 (AREA APPROX 1"). REPAIRED PER ERA 461617-14AD. REQUIRE S REPETITIVE INSPECTION AT 37,500 CYCLES. 2 L 7 2 4F RT A1NM 2007052200099 20070522 00099 NM 2007 5 22 DL757070555 1 20070112 A 5311 146N88358201 FRAME BOEING 757 757232 1384965 NM FS 1720 S25L-25R GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 604DL 22811 REPLACEMENT FUSELAGE CHORD SECTIONS WERE FABRICATED TO REPLACE DAMAGED FRAME SECTIONS. REPLACEMENT PARTS WERE MADE AND INSTALLED. 2 L 7 2 4F RT A2NM 2007052200100 20070522 00100 NM 2007 5 22 DL757070556 1 20070131 A 5313 148N32223 STRINGER BOEING 757 757232 1384965 NM FS 1720 S29L GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 FUSELAGE STR 29L REQUIRES REPLACEMENT DUE TO TAIL STRIKE DAMAGE. REPLACEMENT STRINGER WAS FABRICATED AND DAMAGED STRING ER WAS REPLACED. 2 L 7 2 4F RT A2NM 2007052200101 20070522 00101 NM 2007 5 22 DL757070557 1 20070205 A 5312 146N88358201 BULKHEAD BOEING 757 757232 1384965 NM FS 1720 S25L-25R GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 THE AFT PRESSURE BULKHEAD WAS DAMAGED FROM A TAIL STRIKE. THE DAMAGED SECTION OF BULKHEAD CHORD WAS CUT AWAY AND A NEW SECTION WAS FABRICATED AND INSTALLED. 2 L 7 2 4F RT A2NM 2007052200112 20070522 00112 NM 2007 5 22 SWAA072529 1 20070520 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 787 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052500072 20070525 00072 WP 2007 5 25 AALA20070906 1 20070521 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 496AA 49734 LGA - EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AB51 FOR EMERGENCY LIGHTS AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007052500075 20070525 00075 NM 2007 5 25 AALA20070886 1 20070519 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 388AA 27448 MIA - EMERGENCY LIGHT AT OVERHEAD COCKPIT DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT OVERHEAD COCKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007052500080 20070525 00080 NM 2007 5 25 AALA20070889 1 20070519 A 2910 HOSE BOEING 757 757223 1384957 NM HYD SYSTEM LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 21 621AM 24579 ORD INFLIGHT T681/19MAY - ON FIRST APPROACH AUTO SPEEDBRAKE INDICATION WHEN SPOILERS ARMED. RESET NO HELP. WHEN LANDIN G GEAR EXTENDED RIGHT MAIN LANDING GEAR UNSAFE INDICATION. INITIATED GO AROUND AND LOWERED LANDING GEAR MANUALLY. LAND ED ORD WITHOUT INCIDENT. FOUND HYDRAULIC LEAK IN GEAR AREA. AIRCRAFT TAKEN OUT OF SERVICE FOR REPAIR. REPLACED HYDRAU LIC LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007052500085 20070525 00085 NE 2007 5 25 RU3A0703001 2 20070518 A 7320 3032125 LINE BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60A 52043 NE ENGINE BROKEN E RU3A B E A EMER. DESCENT ENGINE SHUTDOWN UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 SW 15 66 8965 4967 FF1 PCE95333 APPROXIMATELY 2 TO 2 1/2 MINUTES AFTER TAKEOFF, NOTICED THE LEFT TORQUE GAUGE GOES TO APPROX 10 PERCENT OR LESS, FOLLOWE D BY THE LEFT NO FUEL TRANSFER LIGHT ILLUMINATING, FOLLOWED BY THE AIRCRAFT YAWING TO THE LEFT AND THEN THE OTHER ENGINE GAUGES REFLECTING THE LEFT ENGINE FAILED. NO FIRE LIGHT WAS ILLUMINATED. UNEVENTFUL SINGLE ENGINE LANDING ACCOMPLISHE D. REPLACED THE LEFT ENGINE PY LINE GOING TO THE PROP GOVERNOR WITH SERVICEABLE ASSEMBLY P/N 3032125. GROUND RUN OPS C HECKED GOOD. 2 L 7 2 4T 4 T A24CE E4EA 2007052500086 20070525 00086 NE 2007 5 25 HALA0700216 2 20070518 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE LEFT OVERHEATED A HALA O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 WP 13 596HA 23276 ETOPS SIGNIFICANT SYSEM, LT ENG EGT WENT TO RED RANGE (942 DEG) EEC WAS ON. DURING TAKEOFF ROLL, EGT WAS W/IN LIMITS. DURING CLIMB, WE NOTICED THE MAX INDICATOR SHOWED THAT IT HAD REACHED 942 DEG. IT MUST HAVE BEEN A MOMENTARY JUMP, BECA USE WE DIDN’T SEE IT. ACCOMPLISHED FIM71-05-00 FIG 109 ENG HAD AN EGT EXCEEDANCE. THE EEC WAS ON. ACCOMPLISHED VISUAL INSP OF ENG PER AMM 71-00-00-862-002-600 STEP G(6)3. NO DEFECTS NOTED. NOTE:EICAS EXCEEDANCE PAGE SHOWED EGT 942 DEG F OR 16 SEC MOC AND POWERPLANT ENGINEER NOTIFIED. ENG OK FOR CONTINUED SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007052500087 20070525 00087 2007 5 25 HALA0700220 4 20070521 A 3400 HG1050AE10 IRU BOEING 767 76733A 1385209 NM UNKNOWN A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 593HA 33423 ETOPS SIGNIFICANT SYSTEM, C IRS FAULT LIGHT ON EICAS AND IRS PANEL. REPLACED C IRU. OPS CHECK OK PER MM 34-21-01. PER FORMED MCDP TEST NR 30 PASSED. A/C LMP STATUS REMAINS IN "LAND 3". 2 L 7 2 4F RT A1NM 2007052500088 20070525 00088 NM 2007 5 25 HALA0700221 1 20070522 A 2840 UNKNOWN BOEING 767 767332 1382001 NM FUEL INDICATION UNKNOWN A HALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 13 598HA 23278 ETOPS SIGNIFICANT SYSTEM, FUEL CONFIG LIGHT CAME ON IN DESCENT 3000 NR LATERAL IMBALANCE BETWEEN LEFT AND RIGHT WING TAN KS. ALL OTHER INDICATIONS NORMAL. NO EVIDENCE OF LEAK. STICKED LEFT AND RIGHT TANK FUEL QUANTITY, LT 30.6 9748 INDICA TING 9700. RIGHT 25.6 7015 INDICATING 7600 SYSTEM OK PER FIM 28-41-00 FIG 107 SHEET 1. 2 L 7 2 4F RT A1NM 2007052500089 20070525 00089 WP 2007 5 25 NWAA071919955 1 20070520 A 3240 BRAKE ASSY DOUG DC9 DC931 3022065 WP MLG LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 01 922RW 47182 ON A VERY SHORT FINAL APPROACH FOR LANDING ,THE CREW NOTICED THAT ALL OF THE FLUID FROM THE RIGHT HYDRAULIC SYSTEM HAD D EPLETED. THE AIRCRAFT COMPLETED A NORMAL SAFE TOUCHDOWN AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE FOUND THE NR 3 BRAKE ASSEMBLY LEAKING AND REPLACED IT. ALSO FOUND THE RUDDER HYDRAULIC POWER SHUTOFF VALVE LEAKING AND REPLAC ED IT. ALL APPLICABLE PUMPS AND FILTERS WERE REPLACED, HYDRAULIC SYSTEM SERVICED TO FULL, LEAK CHECKED, AND FUNCTIONALL Y CHECKED. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007052500090 20070525 00090 SO 2007 5 25 SWIA200718234 1 20070512 A 2750 FLAP SYSTEM EMB 120 EMB120ER 3260203 SO TE FLAPS OUT OF ADJUST A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 284YV 120284 FLAPS WOULD NOT RETRACT PROPERLY ON TAKEOFF. OUTBOARD PAIR REMAINED 2 LIGHT BARS DOWN WITH FLAP DISAGREEMENT INDICATION , RETURNED TO LAX. REPLACED LEFT WING TRAILING EDGE FAIRING ADJACENT TO OUTBOARD FLAP. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007052500091 20070525 00091 EA 2007 5 25 SWIA200718235 1 20070512 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 455SW 7760 AFT PORTION OF CENTER OVERHEAD EXIT LIGHT IS INOP. REPLACED BULB IN EXIT SIGN, OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007052500092 20070525 00092 EA 2007 5 25 SWIA200718236 1 20070515 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 964SW 7868 FRONT SECTION OF EMERGENCY FLOOR LIGHTING IS INOP. INSTALLED SERVICEABLE POWER STRIP FOR FORWARD EMERGENCY FLOOR LIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007052500093 20070525 00093 EA 2007 5 25 SWIA200718237 1 20070513 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA LEFT SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 907SW 16458 9662 7511 LEFT PACK TEMPERATURE IS HOT. NOT CONTROLLABLE IN AUTO OR MANUAL MODES. SMOKE CAME THROUGH COCKPIT VENTS UNTIL LEFT PAC K WAS TURNED OFF. REPLACED LEFT ACM AND LEFT PRSOV. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2007052500095 20070525 00095 EA 2007 5 25 SWIA200718239 1 20070515 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS BURNED OUT A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 611SK 10035 TWO AFT EMERGENCY LIGHTS IN CEILING ARE INOP. RELAMPED OVERHEAD POD LIGHTS IN CEILING. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007052500096 20070525 00096 EA 2007 5 25 SWIA200718240 1 20070516 A 3350 LENS CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT MISSING A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 910SW 7566 EMERGENCY LIGHTS MISSING FROM EXIT LIGHT POD. NEED NEW LENS COVERS. REPLACED WHITE AND RED LENSES AND LAMPS ON OVERHEA D EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD IAW AMM 33-81-00. 2 L 7 2 4F RT A21EA 2007052500097 20070525 00097 EA 2007 5 25 SWIA200718241 1 20070512 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 970SW 7881 FIRST EMERGENCY CEILING FLOOD LIGHT IS INOP. REPLACED BULB ON FIRST CEILING EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2007052500098 20070525 00098 EA 2007 5 25 SWIA200718242 1 20070512 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 983SW 7961 CREW REPORTS THAT CABIN FILLED WITH SMOKE AFTER APU START UP AND PACKS SELECTED ON. OPERATED PACKS AND APU THROUGH SEVE RAL CYCLES FOR 15 MINUTES. COULD NOT DUPLICATE DISCREPANCY. BOTH PACKS AND APU WITHIN NORMAL OPERATING TEMPERATURE. 2 L 7 2 4F RT A21EA 2007052500099 20070525 00099 EA 2007 5 25 SWIA200718243 1 20070514 A 5210 SEAL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 917SW 7641 CABIN DOOR AFT STRIKER SEAL HAS DAMAGE THAT IS OUT OF LIMITS. REPAIRED AFT STRIKER SEAL PER REO 601R53-22-033 TYPE 3 RE PAIR, M-337, COMPLETED. 2 L 7 2 4F RT A21EA 2007052500100 20070525 00100 NM 2007 5 25 HALA0700222 1 20070523 A 2613 261121168 DETECTOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE MALFUNCTIONED A HALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, L ENG OH LP 2 ON AFTER LANDING. REMOVED AND REPLACED LEFT OH DETECTOR LP 2 PER FIM 26-11-00. OPS CHECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007052500101 20070525 00101 EA 2007 5 25 SWIA200718245 1 20070523 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMREGENCY LIGHT INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 453SW 7743 TWO EMERGENCY LIGHTS IN THE CEILING AND AFT SECTION OF EMERGENCY FLOOR LEVEL LIGHTING IS INOP. REPLACED AFT EMERGENCY B ATTERY PACK. REF AMM 33-50-00. 2 L 7 2 4F RT A21EA 2007052500103 20070525 00103 EA 2007 5 25 SWIA200718247 1 20070519 A 2760 PCU CNDAIR CL600 CL6002D24 1390016 EA SPOILER LEAKING A SWIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 07 805SK 1783 1783 15069 DURING CLIMB, RECEIVED A HYD EDP 1A MESSAGE. RETURNED TO FIELD. REPLACED RIGHT OUTBOARD SPOILER PCU IAW MM 27-63-01. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2007052500104 20070525 00104 SO 2007 5 25 SWIA200718248 1 20070519 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 234SW 120308 FORWARD SECTION OF EMERGENCY FLOOR LIGHTING IS INOP. REPLACED FORWARD ELBP IAW 33-50-02 EMB MM. 2 L 7 2 4T RT A31SO 2007052500105 20070525 00105 2007 5 25 SWIA200718249 4 20070521 A 3417 0856KV9 PITOT SYSTEM CNDAIR CL600 CL6002B19 1900309 EA FALSE INDICATION A SWIA O OTHER N FALSE WARNING DE DESCENT 1 NM 07 408SW 7238 7238 7055 EFIS COMP MON CAUTION MESSAGE ON DESCENT. CAPTAIN SIDE AIRSPEED IS INACCURATE. FOUND "DETECTABLE CURL' ON LEFT PITOT T UBE OPENING. REPLACED LEFT PITOT TUBE. REPLACED ADC NR 1, P/N: 822-0372-445 S/N ON: G77F S/N OFF: 12V9P 2 L 7 2 4F RT A21EA 2007052500106 20070525 00106 EA 2007 5 25 SWIA200718250 1 20070521 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 772SK 10235 GALLEY EMERGENCY EXIT LIGHT BULB IS INOP AND COVER IS MISSING. REPLACED LIGHT BULB AND COVER. 2 L 7 2 4F RT A21EA 2007052500107 20070525 00107 EA 2007 5 25 SWIA200718251 1 20070521 A 5610 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 340CA 10062 LEFT WINDSHIELD CRACKED ON CLIMB-OUT, RETURNED TO SLC. LEFT WINDSHIELD WAS REPLACED IAW MM 56-11-01, P/N OFF: NP-139321 -003 S/N OFF: 02085H2662. 2 L 7 2 4F RT A21EA 2007052500108 20070525 00108 EA 2007 5 25 SWIA200718252 1 20070521 A 2710 BUSHING CNDAIR CL600 CL6002B19 1900309 EA LT AILERON NOISY A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 905SW 7437 SIGNIFICANT SQUEAKING NOISE FROM LEFT AILERON IN BOTH DIRECTIONS. REPLACED LEFT AILERON HINGE BUSHINGS AND HARDWARE IAW MM 27-14-15. 2 L 7 2 4F RT A21EA 2007052900001 20070529 00001 SO 2007 5 29 C2XA07TY025 1 20070522 A 3350 BA50933901 BATTERY EMB 135 EMB135ER 3260203 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27506 206 LEFT & RIGHT OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGER IAW EMB 135 MM 3 3-50-04. OPS CHECK GOOD AIRCRAFT RELEASED FROM A CHECK AND RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052900002 20070529 00002 NM 2007 5 29 2007UALA01328 1 20070429 A 3230 2670169M6 VALVE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE MLG FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 179UA 25158 NO RETRACT LANDING GEAR & RTFL DUE TO CAUTION/STATUS MESSAGE. EXPERIENCED A RECURRENCE OF THIS CONDITION ON 2ND FLIGHT OUT. *S/D* ACP TROUBLESHOOTING PER FIM 32-31-00 FOUND ACTUATOR DIMENSIONS OUT. REPLACED RIGHT BODY GEAR TILT ACTUATOR PER MM 32-13-15. STILL HAVE PROBLEM. REPLACED RIGHT BODY GEAR TILT BYPASS VALVE PER MM 32-13-16 AND FUSE PER MM 32-13 -24. READY FOR TEST FLIGHT ON 05MAY07 0700L DEPARTURE. REPLACED FUSE AND VALVE ASSY, CLEARED CH4616. SEVERAL GEAR SWI NGS ACCOMP. A/C OK FOR RETURN TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007070300022 20070703 00022 EU 2007 7 3 2007UALA01558 1 20070520 A 5532 TAPE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE VERTICAL STAB PEELING A UALA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 476UA 832 1508 STRONG VIBRATION IN AFT GALLEY REPORTED BY FLT ATTENDANTS. STRONG ENOUGH TO VIBRATE ITEMS OFF COUNTER. SUPPLEMENTAL DAT A UPDATE PERFORMED RUDDER FREEPLAY CHECK AND FOUND WITHIN LIMITS. FOUND EROSION PROTECTOVE TAPE PEELING FROM LEADING EDG E OF VERTICAL STABILIZER. REPAIRED TAPE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052900003 20070529 00003 NM 2007 5 29 2007UALA01559 1 20070520 A 2721 ACTUATOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE RUDDER OUT OF ADJUST A UALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 WP 29 804UA 759 WITH RUDDER SHOWING 0 DEG TRIM IN COCKPIT ACTUAL RUDDER POS IS 1 INCH RIGHT OF INDEX ON TAIL CONE. [06-26-07] REPLACE D AND ADJUSTED RUDDER TRIM ACTUATOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052900004 20070529 00004 EU 2007 5 29 2007UALA01560 1 20070520 A 5101 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE UNKNOWN VIBRATION A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 443UA 820 AIRFRAME VIBRATIONS BEGIN IN CLIMB FL185 AND FADES OUT APPROX FL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052900006 20070529 00006 NM 2007 5 29 2007UALA01581 1 20070519 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SEAT 3H MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 672UA 30027 SEAT EEL STRIP LIGHT AT 3H MISSING. [SUP 06-06-07] REPLACED EEL STRIP LIGHT ON SEAT 3H. 2 L 7 2 4F 4 F RT A1NM E24NE 2007052900009 20070529 00009 NM 2007 5 29 2007UALA01583 1 20070521 A 2120 UNKNOWN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT ODOR A UALA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 29 771UA 26932 777100 CREW REPORTS ON TAKE OFF TOWER REPORTED SMOKE FROM ENG 1, NO ABNORMAL ENG PARAMETER OR EICAS MSG, IT WAS A FULL POWER TA KE OFF DUE TO EPR MODE BEING INOP. VISUAL INSP OF ENG AREA DURING FLIGHT WAS NORMAL, NO ODOR IN COCKPIT OR CABIN (CONFI RMED BY CREW). [06-14-07] ALL ENGINE SYSTEMS CHECKED NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007052900020 20070529 00020 EU 2007 5 29 2007UALA01596 1 20070522 A 5101 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE UNKNOWN VIBRATION A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 481UA 1559 VIBRATION FELT DURING CLIMB IN MID-AFT CABIN AREA. AFTER LEVEL-OFF VIBRATION STOPPED. VIBRATION WAS FELT IN CLIMB AND DESCENT AND IT WAS A SIDE TO SIDE MOTION THAT GOT MORE PRONOUNCED WITH INCREASE IN SPEED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052900025 20070529 00025 NM 2007 5 29 2007UALA01605 1 20070522 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 CROSSAISLE 5 LEFT EMERGENCY LIGHT INOPERATIVE. [SUP 06-06-07] REPLACED LIGHT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052900026 20070529 00026 NM 2007 5 29 2007UALA01606 1 20070522 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 DOOR 5 LEFT CROSSAISLE EMERGENCY LIGHT LAMP INOP. [SUP 06-06-07] RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052900028 20070529 00028 NM 2007 5 29 2007UALA01608 1 20070522 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 STAIRS EMERGENCY LIGHTS INOPERATIVE. [SUP 06-06-07] FOUND DISCONNECTED. RECONNECTED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052900029 20070529 00029 NM 2007 5 29 2007UALA01609 1 20070522 A 2620 SQUIB BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EXTINGUISHER NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 FIRE EXTINGUISHER SQUIB TEST INOPERATIVE. [06-15-07] LIGHT CIRCUIT FAILS. REPLACED LIGHT PANEL. FOUND SQUIB O P-TEST SATISFACTORILY PER MM26-21-00. A/C OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052900030 20070529 00030 NM 2007 5 29 2007UALA01610 1 20070521 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE STAIRWAY LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 182UA 25279 EEL LIGHT STAIRWAY RIGHT SIDE UD LOOSE. [SUP 06-06-07] SECURED EEL. LIGHTS CK OK . 2 L 7 4 4F 4 F RT A20WE E24NE 2007052900032 20070529 00032 NM 2007 5 29 2007UALA01613 1 20070523 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY OVERWNG LIGHT RIGHT SIDE 2ND ASSY FROM AFT FWD BULB INOPERATIVE. [SUP 06-06-07] RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052900039 20070529 00039 NM 2007 5 29 2007UALA01620 1 20070523 A 5754 BEARING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 8 SLAT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 NR 8 SLAT I/B AUX TRACK BEARING & ATTACH BOLT FOUND BROKEN. LAYING IN WING L/E CAVITY 2 MORE BROKEN BOLTS & BEARINGS FO UND IN SAME CAVITY. [06-20-07] INSTALLED NR 8 IB AUX TRACK BOLT AND BEARING. CHECKED AND ADJUSTED SLAT. ATTRIBUTED F AILURE TO A FAILED BEARING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052900041 20070529 00041 NM 2007 5 29 2007UALA01622 1 20070523 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1640 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 AFT GALLEY AREA STA 1640, BL 0 TO RBL 54 AREA, FLOORBEAM TEE CAP UPPER SURFACE HAS SURFACE CORROSION AT FASTENER HOLES. [SUP 06-01-07] MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION. REMOVED DAMAGED SECTION OF T-CAP. FABRICATED & INSTALLED NEW TEE CAP SECTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052900042 20070529 00042 NM 2007 5 29 2007UALA01623 1 20070523 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1022 S17R CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 STR 17R CREASE BEAM WEB AT BS 1022 HAS SURFACE CORROSION ON UPPER SURFACE. [SUP 06-01-07] MAJOR REPAIR ACCOMPLISHED: R EMOVED CORROSION. REMOVED WEB. FABRICATED & INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052900043 20070529 00043 NM 2007 5 29 2007UALA01624 1 20070523 A 2597 WIRE HARNESS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR SLIDE FRAYED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 DOOR 4L ESCAPE SLIDE LATCH HARNESS FRAYED INTO STITCHING. [06-20-07] REPLACED DOOR 4L SLIDE LATCH HARNESS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052900047 20070529 00047 NM 2007 5 29 2007UALA01628 1 20070524 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY LIGHT INOPERATIVE AT RIGHT OVERWING FWD MOST ASSY FWD BULB. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052900048 20070529 00048 NM 2007 5 29 2007UALA01629 1 20070521 A 2560 CIRCUIT BREAKER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE K4 AT THE P 310 FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 214UA 30220 EVACUATION TEST BUTTON ACTIVATES THE EVAC WARNING SYSTEM. [06-15-07] PULLED EVAC SIGNAL CB K4 AT THE P 310 PANEL IN THE EE COMPARTMENT PULLED PER CREW REQUEST. RESET CIRCUIT BREAKER AND ACCOMPLISHED SYSTEM TEST PER MMOV 25-63-02, SYS TEM CHECKS NORMALLY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007052900050 20070529 00050 SO 2007 5 29 C2XA07IA120 1 20070518 A 3240 BRAKE ASSY EMB 145 EMB145LR 3260212 SO MLG MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 17984 145246 IAH - FLIGHT 2528, THE CREW REPORTED A -BRK OUTBD- MESSAGE ON EICAS ON FINAL APPROACH, AND THAT THE OUTBOARD BRAKES DID NOT WORK ON ROLLOUT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE BRAKES WITH NO DEFECTS NOTED, AND TH E AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007052900052 20070529 00052 EA 2007 5 29 COMA0760381 1 20070518 A 2750 860D10018ABCD CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 931CA 8200 7037 FLIGHT 4939 - RECEIVED FLAP FAIL MESSAGE AFTER LANDING. REPLACED FECU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007052900054 20070529 00054 EA 2007 5 29 COMA0760379 1 20070516 A 5270 840534 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 1900309 EA CABIN DOOR FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 597SW 7293 FLIGHT 5454 - DURING CLIMBOUT OF CVG RECEIVED A CABIN DOOR HANDLE MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO TH E FIELD. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE CABIN DOOR PROXIMITY SWITCH, PS2MB. 2 L 7 2 4F RT A21EA 2007052900058 20070529 00058 SO 2007 5 29 C2XA07CL046 1 20070522 A 2612 3601133500230 FIRE DETECTOR EMB 135 EMB135ER 3260203 SO NR NACELLE FAULTY A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 14505 145192 CLE FLIGHT 2238, THE CREW REPORTED A ENGINE 1 FIRE DETECT FAIL MESSAGE ON THE EICAS IN FLIGHT. MAINTENANCE INSPECTED AN D REPLACED THE E1 FIRE/OVERHEAT DETECTOR. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2007052900059 20070529 00059 NM 2007 5 29 PIDA07033 1 20070519 A 5315 FLOORBEAM BOEING 737 7372K5 138448X NM BS 967 CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 DURING MAINTENANCE, NOTED CORROSION ON UPPER FLANGE OF BS 967.5 FLOORBEAM. REPLACED DAMAGED SECTION OF FLOORBEAM PER EA 53-122. 2 L 7 2 4F RT A16WE 2007052900060 20070529 00060 NM 2007 5 29 PIDA07034 1 20070521 A 5315 FLOORBEAM BOEING 737 7372K5 138448X NM BS 947 CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 DURING MAINTENANCE, NOTED CORROSION ON UPPER FLANGE OF BS 947.5 FLOORBEAM. REPLACED DAMAGED SECTION OF FLOORBEAM PER EA 53-120. 2 L 7 2 4F RT A16WE 2007052900062 20070529 00062 EA 2007 5 29 COMA0760385 1 20070520 A 2916 73031 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA NR 3 HYD SYS LEAKING A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 956CA 9916 7105 FLIGHT 5661- RECEIVED GEAR DISAGREE MESSAGE. ABORTED APPROACH, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. FOUND N R 3 HYDRAULIC RESERVOIR LEAK DECAY RATE OUT OF LIMITS. REPLACED RESERVOIR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007052900063 20070529 00063 EA 2007 5 29 COMA0760384 1 20070518 A 5610 NP13932110 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA O OTHER O OTHER DE DESCENT 1 SO 01 971CA 11164 7145 FLIGHT 5194 - F/O WINDSHIELD CRACKED. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED F/O WINDSHIELD. 2 L 7 2 4F RT A21EA 2007052900065 20070529 00065 SO 2007 5 29 C2XA07RI033 1 20070522 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14173 14500872 IAD - DURING ROUTINE MAINTENANCE, MX FOUND RIGHT OVERWING EMERGENCY LIGHT EXIT INOP. MX PROCEED WITH TROUBLESHOOTING AN D FOUND INVERTER INOP. MX REMOVED AND REPLACED INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVE D TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007052900066 20070529 00066 EA 2007 5 29 COMA0760386 1 20070520 A 2913 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM MALFUNCTIONED A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 965CA 7131 FLIGHT 5389 - HYD PUMP 1B CIRCUIT BREAKER POPPED WHILE STARTING NR 1 ENGINE. RETURNED TO GATE. RESET BREAKER, PERFORME D OPS CHECK, NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007052900067 20070529 00067 EA 2007 5 29 COMA0760387 1 20070521 A 3040 16591 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA WINDSHIELD HEAT FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 916CA 19962 7014 FLIGHT 5381 - DURING CLIMBOUT OF CVG RECEIVED A RIGHT WINDSHIELD HEAT CAUTION ON MESSAGE, FLIGHT RETURNED TO THE FIELD. REPLACED THE WINDSHIELD TEMPERATURE CONTROLLER. 2 L 7 2 4F RT A21EA 2007052900068 20070529 00068 NM 2007 5 29 SWAA072609 1 20070522 A 3350 101073 COVER BOEING 737 7375H4 138449D NM EMERGENCY LIGHTS CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT COVER CRACKED. REMOVED AND REPLACED LIGHT COVER PER M M. 2 L 7 2 4F RT A16WE 2007052900069 20070529 00069 NM 2007 5 29 SWAA072622 1 20070522 A 5315 147A55067 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 728SW 27860 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 27.50. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007052900070 20070529 00070 NM 2007 5 29 SWAA072611 1 20070522 A 2750 256A3700 TORQUE TUBE BOEING 737 7377H4 1384404 NM TE FLAP DRIVE BENT A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 256WN 32514 DURING SCHEDULED HC1 CHECK, FOUND LEFT WING INBOARD FLAP DRIVE TORQUE TUBE BENT AT LEFT SIDE. REMOVED AND REPLACED TORQ UE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007052900074 20070529 00074 2007 5 29 SWAA072580 4 20070522 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 771SA 27879 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052900076 20070529 00076 NM 2007 5 29 SWAA072602 1 20070522 A 5311 6516301 FRAME BOEING 737 7373L9 1384470 NM BS 188 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 188, LBL 33, WL 208. REMOVED AND REPLACED CHORD PE R SRM. 2 L 7 2 4F RT A16WE 2007052900078 20070529 00078 NM 2007 5 29 SWAA072581 1 20070522 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 782 S20L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 782, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007052900079 20070529 00079 NM 2007 5 29 SWAA072582 1 20070522 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 800 S19L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007052900081 20070529 00081 NM 2007 5 29 SWAA072598 1 20070522 A 5315 6545833 FLOORBEAM BOEING 737 7373L9 1384470 NM BS 270 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND ZEE CHORD CORRODED AT BS 270, BETWEEN LBL 11 AND RBL 11, WL 208. REMOVED AND REPLACED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2007052900082 20070529 00082 NM 2007 5 29 SWAA072601 1 20070522 A 5315 6545834 FLOORBEAM BOEING 737 7373L9 1384470 NM BS 312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 312, RBL 1. REPAIRED WEB PER ER. 2 L 7 2 4F RT A16WE 2007052900083 20070529 00083 NM 2007 5 29 SWAA072606 1 20070522 A 5753 SKIN BOEING 737 7373Y0 1384671 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED MV1 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLA P PER MM. 2 L 7 2 4F RT A16WE 2007052900086 20070529 00086 NM 2007 5 29 SWAA072591 1 20070522 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 727B S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052900087 20070529 00087 NM 2007 5 29 SWAA072590 1 20070522 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052900088 20070529 00088 NM 2007 5 29 SWAA072603 1 20070522 A 5322 6546529 SHEAR TIE BOEING 737 7373L9 1384470 NM BS 343 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 343, LBL 12, WL 156. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007052900089 20070529 00089 NM 2007 5 29 SWAA072619 1 20070522 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 500B S13L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500B, STR 13L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007052900092 20070529 00092 NM 2007 5 29 SWAA072621 1 20070522 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM BS 727B S13L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 13L. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2007052900094 20070529 00094 NM 2007 5 29 SWAA072593 1 20070522 A 5311 6550568 FRAME BOEING 737 7373H4 1384600 NM BS 994 S13R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 994.5, STR 16R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007052900095 20070529 00095 NM 2007 5 29 SWAA072595 1 20070522 A 5551 6551524 FITTING BOEING 737 7373L9 1384470 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND LEFT AND RIGHT HORIZONTAL STAB FITTING CLEVIS LUG FACES CORRODED. REPAIRED FITTING PE R SRM. 2 L 7 2 4F RT A16WE 2007052900100 20070529 00100 2007 5 29 SWAA072597 4 20070522 A 2565 6557463 GIRT BAR BOEING 737 7373L9 1384470 NM L1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007052900101 20070529 00101 NM 2007 5 29 SWAA072604 1 20070522 A 5311 65C25228 FRAME BOEING 737 7373L9 1384470 NM BS 727C S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727C, STR 8R. REPAIRED FRAME SECTION PER SWA EA. 2 L 7 2 4F RT A16WE 2007052900105 20070529 00105 NM 2007 5 29 SWAA072615 1 20070522 A 5313 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 400 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052900106 20070529 00106 NM 2007 5 29 SWAA072614 1 20070522 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 639 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052900107 20070529 00107 NM 2007 5 29 SWAA072613 1 20070522 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 727B S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007052900108 20070529 00108 NM 2007 5 29 SWAA072612 1 20070522 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 727A S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007052900109 20070529 00109 NM 2007 5 29 SWAA072586 1 20070522 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 907 S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052900110 20070529 00110 NM 2007 5 29 SWAA072587 1 20070522 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 616 S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052900111 20070529 00111 NM 2007 5 29 SWAA072588 1 20070522 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 616 S5L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052900112 20070529 00112 NM 2007 5 29 SWAA072589 1 20070522 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 360 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052900113 20070529 00113 NM 2007 5 29 SWAA072605 1 20070522 A 5340 65C27314 STRINGER CLIP BOEING 737 7373L9 1384470 NM BS 520 S12R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 12R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052900114 20070529 00114 2007 5 29 SWAA072610 4 20070522 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052900115 20070529 00115 2007 5 29 SWAA072584 4 20070522 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052900119 20070529 00119 WP 2007 5 29 MWEA070119 1 20070519 A 2560 989803136291 BATTERY DOUG DC9 DC981 3022081 WP EMERGENCY LIGHTS FAILED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 AED FAILED SELF TEST LOW BATTERY. REMOVED AND REPLACED BATTERY. 2 L 7 2 4F A6WE 2007052900121 20070529 00121 NM 2007 5 29 ASAA0741690 1 20070522 A 5754 SKIN BOEING 737 7374Q8 138447Q NM NR 3 SLAT DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 NR 3 SLAT INBOARD TRAILING EDGE HAS COMPOSITE LAYERS SHOWING. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007052900124 20070529 00124 NM 2007 5 29 ASAA0741693 1 20070523 A 5311 65C312403 FRAME BOEING 737 737490 1384715 NM BS 794 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 706AS 28894 AFT CARGO PIT FRAME DOUBLER FOUND CORRODED. FRAME REPLACED WITH NEW PART IAW SRM 51-40-05. 2 L 7 2 4F RT A16WE 2007052900126 20070529 00126 NM 2007 5 29 SWAA072651 1 20070524 A 3350 20131 BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007052900128 20070529 00128 NM 2007 5 29 SWAA072642 1 20070523 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 796SW 27889 DURING SCHEDULED MV2 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007052900129 20070529 00129 NM 2007 5 29 SWAA072646 1 20070524 A 3350 311500 LENS BOEING 737 7373TO 138447G NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED RON CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 8 DEF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007052900130 20070529 00130 NM 2007 5 29 SWAA072663 1 20070524 A 3350 311500 LENS BOEING 737 7373L9 1384470 NM EMERGENCY LIGHTS CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007052900133 20070529 00133 2007 5 29 SWAA072647 4 20070521 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 231WN 32499 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052900134 20070529 00134 2007 5 29 SWAA072649 4 20070524 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 744SW 29490 DURING SCHEDULED RON CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052900140 20070529 00140 NM 2007 5 29 SWAA072645 1 20070523 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 822 S25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 822, STR 25R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007052900141 20070529 00141 NM 2007 5 29 SWAA072644 1 20070523 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 733 S21R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733, STR 21R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007052900142 20070529 00142 NM 2007 5 29 SWAA072637 1 20070523 A 5753 SKIN BOEING 737 7373H4 1384600 NM LT TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED C4 CHECK, FOUND LEFT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2007052900143 20070529 00143 NM 2007 5 29 SWAA072632 1 20070523 A 5753 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED HC2 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2007052900147 20070529 00147 NM 2007 5 29 SWAA072660 1 20070524 A 5322 6546546 SHEAR TIE BOEING 737 7373Q8 1384670 NM BS 867 S20L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 867, STR 20L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007052900149 20070529 00149 NM 2007 5 29 SWAA072665 1 20070524 A 5311 6546558 FRAME BOEING 737 7375H4 138449D NM BS 907 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052900150 20070529 00150 NM 2007 5 29 SWAA072657 1 20070524 A 5315 6546812 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 1006 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 1006, RBL 50. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007052900153 20070529 00153 NM 2007 5 29 SWAA072654 1 20070524 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007052900156 20070529 00156 NM 2007 5 29 SWAA072656 1 20070524 A 3397 65C27093 CONNECTOR BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. FOUND LOOSE CONNECTOR, SECURED CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2007052900159 20070529 00159 NM 2007 5 29 SWAA072635 1 20070523 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500C S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052900161 20070529 00161 NM 2007 5 29 SWAA072648 1 20070524 A 2130 7207376 VALVE BOEING 737 7377H4 1384404 NM CABIN PRESSURE INOPERATIVE A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 708SW 27842 AIR TURNBACK, AIRCRAFT DID NOT PRESSURIZE IN AUTO OR ALTERNATE MODE. REMOVED AND REPLACED NEGATIVE PRESSURE VALVE PER M M. 2 L 7 2 4F RT A16WE 2007052900163 20070529 00163 NM 2007 5 29 SWAA072631 1 20070523 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 337 S23R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED HC2 CHECK, FOUND STRINGER 23R CRACKED AT BS 337. REPAIRED STRINGER PER SWA EA. 2 L 7 2 4F RT A16WE 2007052900167 20070529 00167 2007 5 29 SWAA072641 4 20070523 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052900171 20070529 00171 NM 2007 5 29 SWAA072667 1 20070524 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 728SW 27860 DURING SCHEDULED 8Y CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007052900173 20070529 00173 NM 2007 5 29 SWAA072627 1 20070523 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 15 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007052900175 20070529 00175 NM 2007 5 29 ASAA0741696 1 20070523 A 5755 656719517 FITTING BOEING 737 7374Q8 138447Q NM NR 4 SPOILER CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 NR 4 SPOILER INBOARD ACTUATOR MOUNT FITTING HAS FRETTING CORROSION. REMOVED FITTING, INSTALLED NEW FITTING IAW SRM 51-4 0-02. 2 L 7 2 4F RT A16WE 2007052900176 20070529 00176 NM 2007 5 29 ASAA0741697 1 20070523 A 5347 CARGO TRACK BOEING 737 7374Q8 138447Q NM BS 470-512 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 CARGO TIE DOWN IS GOUGED. REMOVED DAMAGED SECTION OF TRACK, FABRICATED AND INSTALLED REPLACEMENT TRACK IAW ASA EA 5310 02722. 2 L 7 2 4F RT A16WE 2007100200043 20071002 00043 NM 2007 10 2 MWEA070224 1 20070920 A 7830 7150922REV6 CHANNEL BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 912ME 55175 UPPER OUTBOARD ZEE CHANNEL AT STATION 26 IS CRACKED ON RIGHT THRUST REVERSER. REMOVED DAMAGE, FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F TR A6WE 2007100200047 20071002 00047 NM 2007 10 2 F3LA200700243 1 20070915 A 5730 FASTENER AIRBUS A319 A319111 3930336 NM LT WING DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 INSPECTION REPORTED LIGHTNING DAMAGE TO LEFT WING UPPER SURFACE AT FASTENER RIB 17, 12 INCHES FWD OF AFT SPAR. REMOVED DAMAGED FASTENER, BLENDED DAMAGED AREA, PERFORMED REQUIRED NDT PROCESS AND INSTALLED NEW FASTENER IAW EA A9-57R-12145. 2 L 7 2 4F RT A28NM 2007100200048 20071002 00048 NM 2007 10 2 F3LA200700244 1 20070915 A 5730 FASTENER AIRBUS A319 A319111 3930336 NM LT WING DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 INSPECTION REPORTED LIGHTNING DAMAGE TO LEFT WING UPPER SURFACE AT FASTENER RIB 17, JUST FWD OF NR 4 SPOILER. REMOVED D AMAGED FASTENER, PERFORMED REQUIRED NDT PROCESS, AND INSTALLED NEW FASTENER IAW EA A9-57R-12145. 2 L 7 2 4F RT A28NM 2007100200049 20071002 00049 EU 2007 10 2 COEA0703742 2 20070828 A 7261 O-RING FOKKER F27 F27MK600 4990706 EU RROYCE AVON AVON532R 54517 EU TRANSFER TUBE LEAKING A COEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 13 742FE 10349 AIR TURN BACK, FLT NR 7777. AFTER TAKE-OFF CREW OBSERVED LOW OIL PRESSURE ON THE RT ENGINE. AIRCRAFT RETURNED TO DEPAR TURE. LANDING WAS MADE WITH BOTH ENGINES RUNNING. FOUND OIL TRANSFER TUBE LEAKING ON THE RT SIDE OF THE ENGINE (BEHIND FEATHERING PUMP). REMOVED AND REINSTALLED FEATHERING PUMP FOR ACCESS IAW RR MM 61-2. REMOVED OIL TRANSFER TUBES, REIN STALLED WITH NEW O-RINGS IAW RR MM 72-8. NO LEAKAGE NOTED AFTER GROUND RUNS, OIL PRESSURE GOOD, PROP CHECKS GOOD. SERV ICED OIL IAW RR MM 72-8. (K) 2 H 7 2 4T 4 J A817 E307 2007100200055 20071002 00055 EA 2007 10 2 TRAX200701369 1 20070917 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 861AS 7445 GEAR DISAGREE MSG ON TAKEOFF - NOSE GEAR REMAINED OUT. FOLLOWED QRH. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARE D. 2 L 7 2 4F RT A21EA 2007100200066 20071002 00066 EU 2007 10 2 TRAX200701379 1 20070920 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN INTERMITTENT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 TWO MIN LIGHT COMES ON INTERMITTENT. 2 H 7 2 4T RT 2007100200076 20071002 00076 NM 2007 10 2 SWAA074722 1 20070918 A 5610 571762 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT ARCED A SWAA K NONE O OTHER CR CRUISE 1 SW 29 338SW 23960 AT FL 350 FLIGHT DECK L1 WINDOW ARCING. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2007100200080 20071002 00080 NM 2007 10 2 SWAA074720 1 20070920 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 14L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007100200083 20071002 00083 NM 2007 10 2 SWAA074739 1 20070920 A 5753 6546435335 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED C4 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT LOWER SURFACE. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2007100200096 20071002 00096 NM 2007 10 2 SWAA074736 1 20070920 A 3350 65C34691 LIGHT BOEING 737 737317 138447P NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 5 DEF. REPAIRED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007100200102 20071002 00102 NM 2007 10 2 SWAA074733 1 20070920 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTLUMINESCENT STRIP LOOSE BETWEEN ROW 7 ABC AND ROW 9 ABC. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007100200114 20071002 00114 2007 10 2 RAIA00709022 4 20070917 A 3140 7013348940 DAU EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 824HK 16023 4835 145498 FLT NR 5490 - IAD - AFTER TAKEOFF, GOING THRU 15,000 FT, ALL PRESSURE INDICATIONS WENT TO DASHES. MAINTENANCE REMOVED A ND REPLACED DAU NR 2, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007100200124 20071002 00124 SO 2007 10 2 RAIA00709017 1 20070915 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 829HK 145281 POST FLT NR 7981 - IAD - RIGHT OVERWING EXIT LIGHT INOP. MAINTENANCE DEFERRED WING EXIT LIGHT PER MEL. 2 L 7 2 4T RT T00011AT 2007100200133 20071002 00133 WP 2007 10 2 ABXA070307 1 20070810 A 5320 991555047 INTERCOSTAL DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 907AX 47203 AFT LOWER CARGO INTERCOSTAL WAS CORRODED AT THE NUT PLATES AND ON THE UPPER SURFACE BETWEEN STA 980 AND 996 AT LONGERON 28 LEFT. REMOVED AND REPLACED INTERCOSTAL IAW DC9 SRM. 2 L 7 2 4F A6WE 2007100200136 20071002 00136 NM 2007 10 2 CALA0700528 1 20070922 A 5313 BAC1498158 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND STRINGER 22L CORRODED AT STA 1013. THE STRINGER WAS REPAIRED IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 2007100200148 20071002 00148 WP 2007 10 2 UPS07850709 1 20070822 A 5534 STIFFENER DOUG DC8 DC873F 302199F WP VERTICAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 FITTING CRACKED AT TOP OF VERTICAL STAB SPAR, BETWEEN LT AND RT SPAR CAPS. REPAIRED STIFFENER ON VER TICAL STAB SPAR IAW DWG 4651109 AND SRM 51-1-20 D. 2 L 7 4 4F RT 4A25 2007100200155 20071002 00155 NM 2007 10 2 UPS07M50715 1 20070718 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C CENTER CARGO PIT ON L48 FOUND CORROSION STA 1531.0 AS MARKED. CORR LONGERON CUTOFF PER SRM 53-10-00 V I R38. HFEC INSP C/O PER DAC NDTSP M R13 PART06-10-01-001, NO CRACK FOUND. REPAIR LONGERON & SPLICE FAB SRM 53-10-00 V I R38 & EN1501-07. LONGERON & SPLICE REPROTECTED & PRIMER TOUCHED UP AS PER SRM 51-21-01 V3 R38. REPAIR LONGERON PARTS INSTALLED PER SRM 51-31-01 VII R38 & ATTACH AREA PARTS INSTALLED PER SRM 51-31-01VII R38. 2 L 7 3 4F RT A22WE 2007100200177 20071002 00177 WP 2007 10 2 WRLA2007093 1 20070923 A 5330 SKIN DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE FUSELAGE UNKNOWN A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 303WL 46917 DURING C-5 CHECK, CUSTOMER REQUEST FOUND UNIDENTIFIED SKIN DOUBLER ON RIGHT HAND SIDE NOSE AT STA 453 LONGERON 41. NR 6 6431. 10-12-07 EC-INSP REF. NDT SPM PART G REV.13 RESULTS OK. REINSTALLED ORIGINAL DOUBLER CLASS 1 REPAIR REF SRM VOL .1 53-20-00 REV.91 2 L 7 3 4F 4 F RT A22WE E23EA 2007100200181 20071002 00181 NM 2007 10 2 KCSA071399 1 20070925 A 5210 FRAME BOEING 747 7472B4B 138481B NM R5 DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 NR 5 RIGHT MAIN ENTRY DOOR LOWER FWD CORNER VERTICAL CHORD HAS A 1 INCH CRACK. 2 L 7 4 4F RT A20WE 2007100200185 20071002 00185 NM 2007 10 2 MASA200700494 1 20070809 A 3230 11300105 UPLOCK ACTUATOR DHAV DHC8 DHC8202 2809007 NM MLG MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 446YV 25667 446 ASH 7081 DRO. PILOT WROTE, THE LANDING GEAR WOULD NOT EXTEND, HAD TO MANUALLY EXTEND. FERRIED A/C TO GJT WHERE MX REPL ACED BOTH MAIN GEAR UPLOCK ACTUATORS. 2 H 7 2 4T RT A13NM 2007100200186 20071002 00186 NM 2007 10 2 MASA200700530 1 20070829 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM NR 1 INTERMITTENT A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 991HA 8637 431 ASH 2907 GJT. SMOKE DETECTOR WARNING LIGHT INTERMITTENT IN FLIGHT. MX CHANGED THE NUMBER 1 DETECTOR. 2 H 7 2 4T RT A13NM 2007100200190 20071002 00190 NE 2007 10 2 MASA200700560 2 20070907 A 7320 VALVE DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE NR 1 ENGINE ACTIVATED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 437YV 437 TM123319 ASH FLT 2849 PHX. AFTER ENGINE START FLIGHT DECK FOGS UP WITH AN ODOR. MX REMOVED AND REPLACED NR 1 ENGINE P2.5 SWITCH ING VALVE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007100200201 20071002 00201 NM 2007 10 2 SWAA074792 1 20070924 A 2560 P4010021 BATTERY BOEING 737 7375H4 138449D NM FLASHLIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2007100200250 20071002 00250 NM 2007 10 2 SWAA074820 1 20070926 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007100300009 20071003 00009 SO 2007 10 3 2007F00054 1 20070911 A 5210 6304500 SPRING PIPER PA34 PA34200T 7103406 SO CONT O360 TSIO360* 17025 SO PAX DOOR DISCONNECTED I A UNSCHED LANDING O OTHER CL CLIMB 1 GL 25 464WA 347870189 TENSION SPRING ON UPPER CABIN DOOR LATCH BECAME DISCONNECTED. CAUSED THE UPPER DOOR LATCH NOT TO LATCH/SEAL, ALLOWED RA IN TO ENTER. 1 L 7 2 3O 3 O A7SO E9CE 2007100300024 20071003 00024 SW 2007 10 3 EGI2007F00000 1 20070707 A 6320 412040004127 TRANSMISSION BELL 412 412EP 1182205 SW PWA PT6T PT6T3 52045 EA MAIN ROTOR MAKING METAL E EGIA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 09 416EV 76 36424 DURING LOCAL TRAINING TRANSMISSION CHIP LIGHT CAME ON. AC WAS LANDED WITHOUT FURTHER INCIDENT. INVESTIGATION REVEALED NONFERROUS METAL FLAKES ON THE DEBRIS MONITOR. THE OIL WAS DRAINED THROUGH A STRAINER AND NO METAL WAS FOUND IN STRAINE R. THE EXTERNAL FILTER WAS CUT OPEN, NO METAL WAS FOUND IN THE FILTER. THE EXTERNAL FILTER WAS REPLACED. THE SUMP SCR EEN WAS REMOVED AND NO METAL FOUND. THE TRANSMISSION WAS FLUSHED WITH (3) QUARTS OF OIL AND SUMP SCREEN REINSTALLED. S ERVICED TRANSMISSION. THE AIRCRAFT WAS GROUND RUN FOR 45 MINUTES AT A HIGHER TORQUE SETTING (LIGHT ON SKIDS). CHECK OF CHIP DETECTOR AND DEBRIS MONITOR FOLLOWING GROUND RUN FOUND NO CHIPS OR FLAKES OF METAL. AC WROTE UP FOR DAILY INSPECT 1 G 7 2 4U 4 U H4SW E22EA 2007100400001 20071004 00001 SO 2007 10 4 SIMA200726903 1 20070924 A 3297 355022002 WIRE HARNESS EMB 135 EMB135KL 3260302 SO MLG PROX SWITCH DAMAGED A SIMA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 SW 21 807AE 145506 LANDING GEAR FAILED TO RETRACT LOCKED IN DOWN POSITION (HANDLE). CREW ELECTED TO RETURN TO SJC. AIRCRAFT LANDED AND RE TURNED SAFELY TO THE GATE. REMOVED AND REPLACED NOSE PROX SWITCH HARNESS AND LANDING GEAR ELECTRONIC CONTROL. 2 L 7 2 4F RT T00011AT 2007100400002 20071004 00002 SO 2007 10 4 SIMA200726902 1 20070925 A 3150 WARNING LIGHT EMB 145 EMB145LR 3260212 SO MLG ILLUMINATED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 616AE 145092 BRAKE OVERHEAT MESSAGE ON EICAS WITH THE NUMBER 2 BRAKE TEMP INDICATION INOP. CREW ELECTED TO ABORT TAKEOFF AND RETURN TO THE GATE. ISSUED MEL 32-03. 2 L 7 2 4T RT T00011AT 2007100400010 20071004 00010 NM 2007 10 4 AALA20071821 1 20070919 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 938AN 29533 TUL - EMERGENCY LIGHTS IN AREA OF STATION 750 MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AREA OF STATION 750 MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007100400018 20071004 00018 NM 2007 10 4 DLM90071252 1 20070918 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 769-788 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 CSP WEB CORRODED OOL AT STA 769 - 788 LT SIDE. REPAIRED IAW ERA 3981911-14MA REV ORIG AND SRM 53-00-011 VOL III. 2 L 7 2 4F RT A6WE 2007100400021 20071004 00021 NM 2007 10 4 DLM90071255 1 20070918 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 588-626 L24 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 FOUND CABIN SEAT TRACK CORRODED AT STA 612. REPAIRED SEAT TRACK IAW MD90 SRM 53-40-01 VOL I. 2 L 7 2 4F RT A6WE 2007100400023 20071004 00023 NM 2007 10 4 DLM90071257 1 20070924 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 522 - 541 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 RT CUSP WEB CORRODED STA 522-541. CUSP WEB REPLACED ON W/O 1002987 2400 0227. DL 63329 2 L 7 2 4F RT A6WE 2007100400026 20071004 00026 EA 2007 10 4 SWIA200718702 1 20070918 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 926SW 7687 FLT 6543 - RIGHT SIDE FLOOR EMERGENCY LIGHT STRIP IS OUT OF SERVICE. REPLACED FLOOR ILLUMINATION STRIP WITH A SERVICEAB LE UNIT. 2 L 7 2 4F RT A21EA 2007100400032 20071004 00032 EA 2007 10 4 SWIA200718708 1 20070919 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 07 934SW 7722 FLT 6593 - DURING DESCENT, DETECTED AN ELECTRIC BURNING ODOR. THE ODOR LASTED FOR 10 SECONDS WITH NO SMOKE SEEN. INSPE CTED CABIN AND COCKPIT FOR BURN INDICATIONS. NO DISCREPANCIES NOTED. COULD NOT DUPLICATE. 2 L 7 2 4F RT A21EA 2007100400033 20071004 00033 EA 2007 10 4 SWIA200718709 1 20070917 A 3350 SIGN CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT MISSING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 770SK 10243 FLT 6408 - EXIT SIGN MISSING AT FLOOR OF GALLEY BULKHEAD BY THE SERVICE DOOR. INSTALLED SERVICEABLE LENS ON FLOOR EMERG ENCY EXIT FLOODLIGHT. OPS TEST GOOD. 2 L 7 2 4F RT A21EA 2007100400040 20071004 00040 EA 2007 10 4 A6WA200740492 1 20070831 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 424AW 7656 PASSENGER DOOR TOP STEP EDGE MEMBER CRACKED. SUP - MAINTENANCE REPAIRED IAW REO NR 601R-52-11-279. (M) 2 L 7 2 4F RT A21EA 2007100400071 20071004 00071 NM 2007 10 4 AALA20071807 1 20070925 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 794AN 30256 JFK - EMERGENCY LIGHT AT SEAT ROW 20C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 20C. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007100400077 20071004 00077 WP 2007 10 4 AALA20071815 1 20070926 A 3350 0202226001 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 465A 49595 LAX - EMERGENCY LIGHT AT SEAT 10D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007100400078 20071004 00078 EU 2007 10 4 AALA20071816 1 20070927 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 91050 423 LGA - EMERGENCY LIGHT AT STATION 243 INOPERATIVE. REPLACED BATTERY PACK AND MODULE FOR EMERGENCY LIGHT AT STATION 243. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007100400089 20071004 00089 EA 2007 10 4 A6WA200740511 1 20070915 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 425AW 7663 RT KIDNEY PANEL CUTOUT AT FWD FUSELAGE HAS ONE ELONGATED HOLE. MAINTENANCE REPAIRED IAW REO 601R-53-11-162. (M) 2 L 7 2 4F RT A21EA 2007100400090 20071004 00090 EA 2007 10 4 A6WA200740536 1 20070901 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 202 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 424AW 7656 FORWARD PRESSURE BULKHEAD AT FS 202.75 LOWER LT CORNER SKIN IS CRACKED AROUND BULKHEAD FITTING FOR RT INBOARD BRAKE LINE . MAINTENANCE CUT AWAY DAMAGED SECTION OF WEB AND INSTALLED REPAIR DOUBLE IAW BSC EO 601R-53-12837. (M) 2 L 7 2 4F RT A21EA 2007100400093 20071004 00093 EU 2007 10 4 07FDEA04153 1 20070921 A 5210 A52175270202 STRUT AIRBUS 310 A310324 3930206 EU ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORROSION ON U-STRUT AT UPPER EDGE OF AFT PAX DOOR LT, BETWEEN FRAME 73A-75A. REPLACEMENT OF STRUT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100400102 20071004 00102 EU 2007 10 4 07FDEA04258 1 20070924 A 5730 A57247017001 SKIN AIRBUS 300 A300B4605R 3930308 EU ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORROSION AND DELAMINATION FOUND AT RT WING TE PANEL ASSY TO PREVIOUS REPAIRS REPAIR PERFORMED BY DAMAGE REMOVAL, BONDIN G REPAIR AND INSTALLING OF NEW ANGLES AND DOUBLERS IAW EA 6-5720-112455 AND RAS/BAE/1003755/2006 ISS A. 2 L 7 2 4F RT A35EU 2007100400116 20071004 00116 EA 2007 10 4 A6WA200740459 1 20070811 A 2701 YOKE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT LOOSE A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 465AW 7893 UNUSUAL NOISE HEARD WHEN FIRST OFFICER YOKE TURNED. MORE NOTICEABLE WHEN TURNED RIGHT. ALSO NOTED THROUGH FLOOR ON CAP TAINS SIDE. RETORQUED FIRST OFFICERS YOKE REF SB CRJ-SL-27-045 REV A AND M 27-11-01. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007100400118 20071004 00118 EU 2007 10 4 07FDEA04172 1 20070921 A 5311 A53973405206 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 HEAVY CORROSION ON CONNECTING SEGMENT FRAME 70, STRG 44 RT. REPLACEMENT OF CONN SEGMENT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100400122 20071004 00122 EU 2007 10 4 07FDEA04176 1 20070921 A 5320 A53986743206 WEB AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 DAMAGED WEB PLATE AT STRG 36 RT, BETWEEN FRAME 86-87. REPLACEMENT OF WEB IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100400128 20071004 00128 EU 2007 10 4 TRBA2007082 1 20070925 A 3350 30130003013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHTS FAILED A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 540AM 540 EMERGENCY LIGHTS LAST 4 FLASH ON AND OFF. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK AT LOCATION 62WL AND 73WL IAW AMM JIC 33-91-21 RAI 10000-007. 2 H 7 2 4T RT A53EU 2007100400131 20071004 00131 EU 2007 10 4 07FDEA04290 1 20070926 A 5330 A53812189 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 FOUND HEAVY CORROSION ON SKIN PANEL BETWEEN FRAME 39-40, STGR 28-33 LT AND TWO OVALIZED HOLES ON FITTING (SEE DRW. A535- 10563) AT FRAME 39, STGR 28. REPAIR PERFORMED BY BLEND OUT CORROSION IAW TD 942.038560/011/2005 ISSUE A AND TD 942.0385 60/047/2005 ISSUE A OVAL HOLES REPAIRED BY OVERSIZING AND BUSHING IAW TD 038560/017/2005 ISSUE B. CONTAINING ALL IN EA 6-5314-82934, APPROVED BY RAS/AS/0153/2005 ISSUE A AND OVERSIZED HOLES WITH RAS/AS/0154/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100400137 20071004 00137 EU 2007 10 4 07FDEA04296 1 20070926 A 5230 A52370100204 LONGERON AIRBUS 300 A300B4622R 3930312 EU CARGO DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 FOUND DAMAGED LONGERON BETWEEN DOOR ATTACH FITTING FRAME 22A-23, BEAM NR 1 OF FWD CARGO COMPARTMENT DOOR. REPLACEMENT O F LONGERON IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100400138 20071004 00138 EU 2007 10 4 07FDEA04354 1 20070928 A 5730 A57260046204 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 OLD DOUBLER REPAIR AT RT WING-LET TO STATIC DISCHARGER NO. V, FINAL REPAIR IS NECESSARY. AFTER REMOVAL OF DOUBLER FOUND ADDITIONAL CORROSION AND A MISDRILLED HOLE ON THE SKIN OF INBOARD PANEL OF RT FENCE. REPAIR PERFORMED BY SKIN CUTOUT A ND INSTALLING FABRICATED REPAIR DOUBLER AND FILLER IAW EA 6-5730-82863 AND RAS/FOK/080/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100400139 20071004 00139 EU 2007 10 4 07FDEA04355 1 20070928 A 5330 A53612607200 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 MISINSTALLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 806FD 458 FOUND OLD EXTERNAL DOUBLER REPAIR ON FUSELAGE SKIN BETWEEN FRAME 11-12, STGR 25-26 LT IAW RAS 031880/026/2004 ISSUE A TH IS REPAIR WAS ONLY AUTHORIZED FOR ONE FERRY FLIGHT TO DRESDEN BECAUSE OF SOME DEVIATIONS AGAINST SRM 53-12-12/FIG 202. REPAIR PERFORMED BY INSTALLATION OF NEW DOUBLER IAW EA 6-5312-82857 AND RAS 031880/039/2004 ISSUE A. 2 L 7 2 4F RT A35EU 2007100400140 20071004 00140 EU 2007 10 4 07FDEA04356 1 20070928 A 5720 A57244004200 PLATE AIRBUS 310 A310324 3930206 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND CRACKED REINFORCING PLATE ON SLAT TRACK NR 6, FWD OF FRONT SPAR, UPPER SKIN, LT WING. REPLACEMENT OF REINFORCING PLATE ON TRACK 6 LT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100400141 20071004 00141 EU 2007 10 4 07FDEA04357 1 20070928 A 5720 A57244005200 PLATE AIRBUS 310 A310324 3930206 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND CRACKED REINFORCING PLATE ON SLAT TRACK NR 7, FWD OF FRONT SPAR, UPPER SKIN, LT WING. REPLACEMENT OF REINFORCING PLATE ON TRACK 7 LT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100400143 20071004 00143 EU 2007 10 4 07FDEA04359 1 20070928 A 5730 A57243205200 SKIN AIRBUS 310 A310324 3930206 EU ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND CHAFING MARKS BETWEEN SLAT TRACK 5 AND SLAT TRACK 6, LEADING EDGE SKIN, LT WING. REPLACEMENT OF CHAFED NOSE SKIN IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100400144 20071004 00144 EU 2007 10 4 07FDEA04360 1 20070928 A 5730 A57243204202 SKIN AIRBUS 310 A310324 3930206 EU ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND CHAFING MARKS BETWEEN JACK 3 AND SLAT TRACK 5, LEADING EDGE SKIN, LT WING. NOSE SKIN REPAIR PERFORMED SRM 57-41 -12/FIG 203, 204. 2 L 7 2 4F RT A35EU 2007100400146 20071004 00146 EU 2007 10 4 07FDEA04362 1 20070928 A 5330 A57246241201 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND ON OLD NOSE SKIN REPAIR IAW SRM 57-41-12/FIG 203, 204, CHAFING MARKS BETWEEN SLAT TRACK 1 AND SLAT TRACK 2, LEAD ING EDGE SKIN, RT WING. NOSE SKIN REPAIR RENEWED, NEW REPAIR SKIN IAW SRM 57-41-12/FIG 203, 204. 2 L 7 2 4F RT A35EU 2007100400147 20071004 00147 2007 10 4 A6WA200740483 4 20070823 A 3460 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA FLT CONTROL MALFUNCTIONED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 31 402AW 7281 RUDDER FLUTTER IN FLIGHT AT 290 KNOTS, CAUSING LIGHT AIRFRAME VIBRATION, FLUTTER REDUCED WITH REDUCED AIRSPEED TO 250 KN OTS, FLUTTER REDUCED WITH RUDDER PEDAL PRESSURE. REMOVED AND REPLACED FLIGHT CONTROL COMPUTER (FCC) NR 2 IAW MM 22-12-1 4, OPS CHECK OK. (M) 2 L 7 2 4F RT A21EA 2007100400148 20071004 00148 EA 2007 10 4 SWIA200718712 1 20070924 A 3350 INVERTER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 938SW 7741 FLT 6445 - EMERGENCY LIGHTING ALONG FLOOR STRIP IS INOP. REPLACED NR 2 EMERGENCY LIGHT INVERTER IAW 33-51-07. OPS CHEC K GOOD. 2 L 7 2 4F RT A21EA 2007100400149 20071004 00149 SO 2007 10 4 SWIA200718713 1 20070802 A 2730 CONTROL CABLE EMB 120 EMB120ER 3260203 SO LT ELEVATOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 213SW 120277 FOUND AT C-CHECK, LEFT ELEVATOR INBOARD MIDDLE CABLE IS CORRODED. REPLACED THE LEFT INBOARD CABLE IAW MM 27-00-01. 2 L 7 2 4T RT A31SO 2007100400151 20071004 00151 EA 2007 10 4 SWIA200718715 1 20070720 A 5320 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA CARGO DOORWAY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 507CA 7796 FOUND AT C-CHECK, FORWARD LOWER CARGO DOOR SURROUND CHANNEL IS CRACKED. REPLACED CHANNEL AT CARGO DOOR SURROUND BOTTOM PER CRJ2100 SRM 51-42-06 PG 14-18. 2 L 7 2 4F RT A21EA 2007100400154 20071004 00154 NM 2007 10 4 GTIA200700020 1 20070919 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 514NK 2679 FLOORBEAM AT -Y765 FR 66 CORRODED. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2007100400155 20071004 00155 NM 2007 10 4 GTIA200700021 1 20070919 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 514NK 2679 FLOORBEAM AT Y765 AND FR 66 CORRODED. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2007100400157 20071004 00157 EU 2007 10 4 07FDEA04363 1 20070928 A 5730 A57243204203 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND ON OLD NOSE SKIN REPAIR IAW SRM 57-41-12/FIG 204, CHAFING MARKS BETWEEN JACK 3 AND SLAT TRACK 5, LEADING EDGE SK IN, RT WING. NEW REPAIR SKIN INSERT INSTALLED IAW SRM 57-41-12/FIG 203, 204. 2 L 7 2 4F RT A35EU 2007100400159 20071004 00159 EU 2007 10 4 07FDEA04184 1 20070921 A 5310 A53988424203 CROSSBEAM AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORROSION ON CROSS STRUT AT FRAME 84, STRG 15 RT FRONT SIDE. REPLACEMENT OF CROSS STRUT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100400161 20071004 00161 EU 2007 10 4 07FDEA04186 1 20070921 A 5542 A55470131006 PANEL AIRBUS 310 A310324 3930206 EU ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 TWO CRACKS AT LEADING EDGE ACCESS PANEL NR 2 OF RUDDER INNER SKIN, HONEYCOMP CORE AND OUTER SKIN CRACKED AT ACCESS HOLE EDGES, MAX CRACK LENGTH = 75MM. REPAIR PERFORMED BY WET-LAY-UP REPAIR AS PER TD/K4/S1/19611/2005/A, APPROVED BY EA 6-55 42-82890 AND RAS/DAHAM/4019611/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100400164 20071004 00164 NM 2007 10 4 TSAA0753052 1 20070920 A 5330 65458001000 SKIN BOEING 737 737282C 13844AU NM BS 306 S18R CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 826AL 23051 WHILE ACCOMPLISHING VISUAL INSPECTION DURING SERVICE CHECK, A CRACK WAS DISCOVERED AT BS 306 AT STR 18. MAINTENANCE ALO NG WITH ENGINEERING IS RESEARCHING THE REPAIR. ECO 3673 REPAIRED CRACKED. 8100-9 WAS RECEIVED FROM BOEING. AIRCRAFT W AS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007100400165 20071004 00165 EU 2007 10 4 07FDEA04365 1 20070928 A 5730 A57243206201 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND CHAFING MARKS BETWEEN SLAT TRACK 6 AND JACK 4, LEADING EDGE SKIN, RT WING. REPAIR PERFORMED BY INSTALLATION OF NE W SKIN INSERT IAW SRM 57-41-12/FIG 203, 204. 2 L 7 2 4F RT A35EU 2007100400166 20071004 00166 NM 2007 10 4 07FDEA03951 1 20070918 A 5740 ARC7490501 TEE FITTING DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 AFTER BUSHING REMOVAL, RIGHT WING INBOARD FLAP VANE INBOARD TEE FITTING BORE FOUND CORRODED. RIGHT WING INBOARD FLAP VANE INBOARD TEE FITTING REMOVED AND REPLACED AS PER AMM 27-50-22-4. 2 L 7 3 4F RT A22WE 2007100400168 20071004 00168 NM 2007 10 4 HALA0700412 1 20070925 A 4900 APU BOEING 767 76733A 1385209 NM MALFUNCTIONED A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM, APU FAULT HUNG 20 PERCENT. PERFORMED APU ECU BITE PER FIM 49-11-00 FIG 103. NO FAULTS NOTED. ACCOMP NORMAL START AT GATE. APU RUNS NORMALLY PER 49-11-00 IN THE AMM. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007100400169 20071004 00169 NM 2007 10 4 HALA0700411 1 20070925 A 4920 211734220 ECU BOEING 767 767332 1382001 NM APU FAILED A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 598HA 23278 ETOPS SIGNIFICANT SYSTEM, FAULT LIGHT ILLUM AND EICAS MSG APU FAULT DISPLAYED SECOND ATTEMPT INDICATES HUNG START. ACCO MPLISHED APU ECU BITE. NO FAULTS NOTED. REMOVED AND REPLACED APU ECU PER AMM 49-61-05. STARTED APU SEVERAL TIMES ON G ROUND. APU ECU NO FAULTS NOTED APU OIL GOOD. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007100400171 20071004 00171 SO 2007 10 4 SIMA200727306 1 20070924 A 5315 14521413605 FLOORBEAM EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 817AE * 5000 145554 DURING A MBV INSPECTION, THE CENTER BEAM AT FRAME 20 WAS FOUND TO BE CORRODED ON THE LT SIDE. REMOVED OLD DOUBLER AND R EPLACED WITH A NEW DOUBLER IAW EMB 145 SRM 53-21-10 STEPS 1-6. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT T00011AT 2007100400172 20071004 00172 SO 2007 10 4 SIMA200727305 1 20070924 A 5315 14521413605 FLOORBEAM EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 817AE 12829 5000 145554 DURING A MBV INSPECTION, THE CENTER BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED OLD DOUBLER AND REPLACED WITH A NEW DOUBLER IAW EMB 145 SRM 53-21-10 STEPS 1-6. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007100400173 20071004 00173 SO 2007 10 4 SIMA200727307 1 20070926 A 5320 14521413605 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 817AE * 5000 145554 DURING A MBV INSPECTION A PREVIOUS REPAIR BETWEEN FRAMES 24 AND 25 ON THE CENTER OMEGA BEAM WAS FOUND CORRODED. REMOVED EXISITING REPAIR AND REPLACE WITH NEW IAW EMB SRM 53-00-10, 51-40-02, AND 53-22-10. RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007100400174 20071004 00174 EU 2007 10 4 SIMA200727302 1 20070914 A 5311 7253813117 FRAME SAAB SF340 340B 7860101 EU BENT A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 211NE 22399 340B211 DURING A HMBV INSPECTION, THE RIGHT FUSELAGE FRAME AT STATION 668.0 WAS FOUND BENT. INSTALLED NEW FRAME P/N 7253813-117 IAW SAAB SRM CHAPTER 51-40-21. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007100400175 20071004 00175 EU 2007 10 4 SIMA200727301 1 20070927 A 5311 7253813499 FRAME SAAB SF340 340B 7860101 EU BS 658 BENT A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 211NE 22399 5000 340B211 DURING A HMBV INSPECTION, THE RIGHT FUSELAGE FRAME AT STATION 658.5 WAS FOUND BENT ABOVE FLOOR LEVEL. INSTALLED DOUBLER IAW SAAB REPAIR STATEMENT 340 SDS 013159 DATED SEPT 27, 07. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007100400176 20071004 00176 EU 2007 10 4 SIMA200727303 1 20070926 A 5347 7253799381 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 211NE 22399 5000 340B211 DURING A HMBV INSPECTION, THE SEAT TRACK AT BUTT LINE 0 WAS FOUND CORRODED AT FUSELAGE STA 297. SPLICED IN A NEW TRACT USING PN 7253799-381. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007100400177 20071004 00177 2007 10 4 QXEA200701493 4 20070928 A 3452 6229614113 CONTROL HEAD DHAV DHC8 DHC8202 2809007 NM ATC MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 365PH 11776 50 526 SEA FLIGHT NR 2132 ATC TRANSPONDERS 1 AND 2 REPORT INOP. TRANSPONDERS RE-CYCLED MANY TIMES WITH TCAS ON AND OFF, STILL NO TRANSPONDER SIGNAL REPORTED FROM ATC. "TCAS FAIL" MESSAGE ALSO DISPLAYED IN BOTH IVSI'S. REPLACED TCAS CONTROL HEAD AND PERFORMED OPERATIONAL TEST. TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007100400178 20071004 00178 NM 2007 10 4 QXEA200701495 1 20071001 A 2420 31708001A GENERATOR DHAV DHC8 DHC8202 2809007 NM NR 2 MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 367PH 17307 5587 511 SEA FLIGHT NR 2194 - WHILE CLIMBING THROUGH 16000 FEET, NR 2 AC GENERATOR CAUTION LIGHT ILLUMINATED. AFTER RESETTING AC GENERATOR 2 LIGHT ILLUMINATED AGAIN NOTICED A BRIEF SOUND LIKE A SLIGHT ENGINE SURGE A FEW MINUTES PRIOR. HOWEVER, ALL ENGINE INDICATIONS WERE NORMAL AND STABLE. ALL DEICE EQUIPMENT WAS ON AND WORKING NORMALLY. REPLACED NR 2 AC GENERATO R. FUNCTIONAL TEST OF AC GENERATION SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007100400179 20071004 00179 NM 2007 10 4 QXEA200701499 1 20070930 A 3150 WARNING LIGHT DHAV DHC8 DHC8202 2809007 NM BETA SYS FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 367PH 511 SEA FLIGHT NR 2164 - UPON STARTING THE BETA LOCKOUT TEST RECEIVED BOTH NR 1 MANUAL AND NR 2 MANUAL CAUTION LIGHTS. MAIN TENANCE RESET BETA LOCKOUT SYSTEM AND COMPLIED WITH BETA LOCKOUT OPERATIONAL CHECK IAW -8 200 AMM 76-10-16. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007100400180 20071004 00180 NM 2007 10 4 QXEA200701494 1 20070930 A 3240 21599 BRAKE ASSY DHAV DHC8 DHC8202 2809007 NM MLG VIBRATES A QXEA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 NM 09 367PH 511 SEA FLIGHT NR 2064, UPON TAXI OUT, AIRCRAFT BEGAN TO SHAKE, WHEN APPLYING BRAKES SHAKING GOT WORSE. REPLACED ALL 4 BRAK ES IAW T/C 93424201. TOK AIRCRAFT OUT FR TAXI, NO VIBRATION NOTICED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERV ICE. 2 H 7 2 4T RT A13NM 2007100400181 20071004 00181 NM 2007 10 4 QXEA200701504 1 20070925 A 2420 31708001A GENERATOR DHAV DHC8 DHC8202 2809007 NM NR 1 MALFUNCTIONED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 354PH 2883 498 YVR FLIGHT NR 2450, NR 1 AC GENERATOR CAUTION LIGHT WOULD NOT RESET PER CHECKLIST. FERRIED TO PDX. REPLACED NR 1 AC GE NERATOR IAW 24-21-00-400-801. ALSO, REPLACED TRANSFORMERS, BOTH GCU'S AND RELAYS 2421-K1 AND K2. OPERATIONAL CHECK GOO D. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007100400182 20071004 00182 NM 2007 10 4 QXEA200701505 1 20071001 A 2840 WARNING LIGHT DHAV DHC8 DHC8202 2809007 NM FUEL MALFUNCTIONED A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 369PH 513 MFR FLIGHT NR 2106 - TANK 2 AUX PUMP INDICATOR LIGHT FAILS TO ILLUMINATE WHEN SWITCH SELECTED, FUEL AUX CONT CIRCUIT BRE AKER POPPED. MAINTENANCE RESET CIRCUIT BREAKER IAW GMM 5-18-0. OPERATIONAL TEST GOOD. NO PARTS REPLACED. AIRCRAFT RE TURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007100400183 20071004 00183 EA 2007 10 4 SWIA200718718 1 20070720 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 507CA 7796 CARGO COMPARTMENT CRACKS AT STA 621 ON FLOOR SUPPORT STRUCTURE, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 SRM 51-42-06 PAGE 11 AND 51-42-21 PAGE 17. 2 L 7 2 4F RT A21EA 2007100400184 20071004 00184 EA 2007 10 4 A6WA200740460 1 20070815 A 2730 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA PITCH FEEL MALFUNCTIONED A A6WA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 31 447AW 7812 DURING TAKEOFF/LANDING, ELEVATOR REQUIRES GREATER THAN NORMAL FORCE TO MOVE AFT, NO BINDING FELT. REMOVED AND REPLACED FIRST OFFICERS PITCH FEEL LINEAR ACTUATOR IAW AMM 27-31-23. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007100400185 20071004 00185 EA 2007 10 4 SWIA200718719 1 20070720 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 507CA 7796 STA 621 FLOOR SUPPORT STRUCTURE IS CRACKED ON RIGHT SIDE, FOUND AT C-CHECK. INSTALLED REPAIR PARTS TO FS 621 RIGHT FLOO R SUPPORT PER CRJ200 SRM 51-42-06 PAGE 11 AND 51-42-21 PAGE 17. 2 L 7 2 4F RT A21EA 2007100400186 20071004 00186 EA 2007 10 4 SWIA200718720 1 20070720 A 5210 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 507CA 7796 PAX DOOR AFT SIDE OF DOOR SUPPORT STRUCTURE ANGLE IS CRACKED IN THE CORNER, FOUND AT C-CHECK. INSTALLED REPAIR PARTS ON AFT SIDE OF PAX DOOR PER REO:601R-52-11-513 REV A. 2 L 7 2 4F RT A21EA 2007100400187 20071004 00187 EA 2007 10 4 SWIA200718721 1 20070720 A 5210 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 507CA 7796 INTERCOSTAL IS CRACKED AT INSIDE RADIUS ON PAX DOOR AFT SIDE, FOUND AT C-CHECK. REPLACED INTERCOSTAL IAW CRJ200 SRM 51- 42-06 PG 1-20 51-42-21 PG 1-18 51-42-13 PG 1-7. 2 L 7 2 4F RT A21EA 2007100400188 20071004 00188 EA 2007 10 4 A6WA200740484 1 20070829 A 2740 SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM FAULTED A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 469AW 7917 IN FLIGHT STAB CHANNEL 1 DISENGAGED, ABLE TO REENGAGE NO PROBLEM DURING APPROACH BOTH STAB TRIM AND MACH TRIM FAILED, UN ABLE TO REENGAGE. AIRCRAFT CONFIGURATION WAS AUTOPILOT OFF, FLAPS 20 AND TRIM 3.8 COMPLIED WITH QRH AND LANDED. FIRST O FFICERS STAB TRIM DISCONNECT SWITCH FOUND AT FAULT. REMOVED AND REPLACED PER AMM 27-41-30-400-802. (M) 2 L 7 2 4F RT A21EA 2007100400189 20071004 00189 EA 2007 10 4 A6WA200740509 1 20070907 A 5340 601R3111358 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 425AW 7663 FOUND FS 280 LBL 9 INBOARD CLIP CRACKED. SUP - MAINTENANCE REPLACED CLIP IAW SRM 51-42-06 AND 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007100400190 20071004 00190 EA 2007 10 4 A6WA200740506 1 20070907 A 5340 601R530057A ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 425AW 7663 FOUND FS 280 RBL 9 OUTBOARD CLIP CRACKED. SUP - MAINTENANCE REPLACED CLIP IAW SRM 51-42-06 AND BSC SRM 601R-53-0057A. ( M) 2 L 7 2 4F RT A21EA 2007100400193 20071004 00193 EU 2007 10 4 07FDEA04297 1 20070926 A 5720 A57111092202 FITTING AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CRACK FINDINGS AT RT CENTER WING C 47 VERTICAL FLANGE ANGLE FITTING HOLE NR H (A=55MM,B=30MM) AND NR N (A=32MM,B=31MM) A ND NR 39 WITH BUSH REPAIR AND INCORRECT FASTENER INSTALLED. REPAIR PERFORMED BY OVERSIZING HOLE NR H, N UNTIL CRACK REM OVAL AND INSTALLING CORRECT FASTENER NSA 5351-8 AT HOLE NR 39 IAW EA 6-5710-112497 AND RAS/053592/015/2007 ISS A. 2 L 7 2 4F RT A35EU 2007100400194 20071004 00194 EU 2007 10 4 07FDEA04298 1 20070926 A 5720 A57111092203 FITTING AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CRACK FINDINGS AT LT CENTER WING C 47 VERTICAL FLANGE ANGLE FITTING HOLE NR H (A=33MM,B=31MM) AND NR I (A=12MM,B=10MM) R EPAIR PERFORMED BY OVERSIZING HOLE NR H, I UNTIL CRACK AND CUT THE EXTERNAL FITTING REMOVAL IAW EA 6-5710-112497 AND RAS /053592/015/2007. 2 L 7 2 4F RT A35EU 2007100400195 20071004 00195 EU 2007 10 4 07FDEA04299 1 20070926 A 5753 A57960000002 SKIN AIRBUS 300 A300B4605R 3930308 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 FOUND AT LT INNER FLAP LOWER SKIN CRACKED (4MM) AND HOLES DAMAGED REPAIR PERFORMED BY REMOVAL OF CRACKS AND OVERSIZING T HE DAMAGED HOLES IAW EA 6-5752-112505 AND RAS/FOK/024/2007 ISS A. 2 L 7 2 4F RT A35EU 2007100400198 20071004 00198 EU 2007 10 4 07FDEA04302 1 20070926 A 5313 A53778096200 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 FOUND DEBONDED STRINGER 42 BETWEEN FRAME 28-30 LT. REPAIR PERFORMED BY CUTTING STRINGER BETWEEN FRAME 30-31, REMOVING A ND CHECKING THEM IF DAMAGED. INSTALLING AGAIN IAW SRM 53-10-14/FIG 201, 202. 2 L 7 2 4F RT A35EU 2007100400199 20071004 00199 EU 2007 10 4 07FDEA04303 1 20070926 A 5720 A57271993202 ANGLE AIRBUS 300 A300B4622R 3930312 EU ZONE 500 NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 FOUND OLD REPAIR AT CLOSING RIB TO TRACK NR 1 LT WING (LHT GLB S868048 AND REPORT 34624), PERMANENT REPAIR HAVE TO BE PE RFORMED AT NEXT D-CHECK. REPAIR PERFORMED BY INSTALLING NEW ORIGINAL PARTS IAW DWG A572-42993, A572-42285 AND SRM 51-72 -10. 2 L 7 2 4F RT A35EU 2007100400200 20071004 00200 EU 2007 10 4 07FDEA04304 1 20070926 A 5720 A57242282004 PLATE AIRBUS 300 A300B4622R 3930312 EU ZONE 500 NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 FOUND OLD REPAIR AT CLOSING RIB TO TRACK NR 1 LT WING (LHT GLB S868048 AND REPORT 34624), PERMANENT REPAIR HAVE TO BE PE RFORMED AT NEXT D-CHECK. REPAIR PERFORMED BY INSTALLING NEW ORIGINAL PARTS IAW DWG A572-42993, A572-42285 AND SRM 51-72 -10. 2 L 7 2 4F RT A35EU 2007100400202 20071004 00202 EU 2007 10 4 07FDEA04306 1 20070926 A 5730 A57240087 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 500 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 FOUND OLD REPAIR ON BOTTOM SKIN FLANGE SUPPORT STRAP AFT FROM REAR SPAR, INBOARD OF RIB NR 9, LT WING CRACK (20MM) IN SU PPORT FLANGE. REPAIR PERFORMED BY MOD SB A300-57-6064 (FINAL REPAIR). 2 L 7 2 4F RT A35EU 2007100500002 20071005 00002 EU 2007 10 5 07FDEA04394 1 20071001 A 5313 A53811360 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 ISS A. 2 L 7 2 4F RT A35EU 2007100500003 20071005 00003 EU 2007 10 5 07FDEA04395 1 20071001 A 5313 A53811373 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 ISS A. 2 L 7 2 4F RT A35EU 2007100500004 20071005 00004 EU 2007 10 5 07FDEA04396 1 20071001 A 5313 A53778058202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND MISDRILLED HOLES AT STRINGER 41 LT, C33-34 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007100500005 20071005 00005 EU 2007 10 5 07FDEA04397 1 20071001 A 5315 A53978254202 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND OLD MISDRILLED HOLE AT CROSSBEAM C 64 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100500007 20071005 00007 EU 2007 10 5 07FDEA04399 1 20071001 A 5340 A53974321000 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND CORROSION AT FITTING C 63, P44-46 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100500008 20071005 00008 EU 2007 10 5 07FDEA04400 1 20071001 A 5340 A53980141200 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FITTING AT P 48, C78 LT CRACKED (ABOUT 8MM). REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100500014 20071005 00014 EU 2007 10 5 07FDEA04406 1 20071001 A 5415 A54611754501 FITTING AIRBUS 310 A310324 3930206 EU ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND CHAFING MARKS AT PYLON TO WING FITTING RIB 18, PYLON NR 2 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10 . 2 L 7 2 4F RT A35EU 2007100500015 20071005 00015 EU 2007 10 5 07FDEA04407 1 20071001 A 5330 A53778050 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND DURING P TO F CONVERSION A CUT (10MM) AT SKIN PANEL C 35, P 35 LT REPAIR PERFORMED BY CUT OUT THE SKIN AND INSTALL ING A FLUSH REPAIR WITH NEW STRAP AND COUPLING IAW EA 6-5314-82877 AND RAS/DABRE/7005190/2005 ISS A. 2 L 7 2 4F RT A35EU 2007100500016 20071005 00016 EU 2007 10 5 07FDEA04408 1 20071001 A 5330 A53981255205 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND SKIN DENT AT C72, P26-27 RT ON SKIN PANEL NR 1 REPAIR PERFORMED BY CUT OUT THE SKIN AND INSTALLING A EXTERNAL DOUB LER AND FILLER IAW DRAWING R539-70630, APPROVED BY EA 6-5318-81127 AND RAS/DAHAM/4019001/2005 ISS A. 2 L 7 2 4F RT A35EU 2007100500019 20071005 00019 EU 2007 10 5 07FDEA04411 1 20071001 A 5330 A53610263202 PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND OLD DENT AT C 8 IN 9 O'CLOCK POSITION. DOUBLER REPAIR PERFORMED IAW SRM 53-11-12 FIG 201. 2 L 7 2 4F RT A35EU 2007100500021 20071005 00021 EU 2007 10 5 07FDEA04412 1 20071001 A 5313 A53974267 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION AT STRINGER P56 C 68-70 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007100500023 20071005 00023 EU 2007 10 5 07FDEA04416 1 20071001 A 5313 A53974267203 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION AT STRINGER P56 RT BETWEEN C 55/58-59. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007100500025 20071005 00025 EU 2007 10 5 07FDEA04421 1 20071001 A 5313 A53974202480 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION AT STRINGER P54LH BETWEEN C55/58-65 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007100500026 20071005 00026 EU 2007 10 5 07FDEA04422 1 20071001 A 5313 A53974267202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION AT STRINGER P56LH BETWEEN C55/58-65 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007100500028 20071005 00028 EU 2007 10 5 07FDEA04424 1 20071001 A 5313 A53974203210 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION AT STRINGER P47LT, C72 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007100500029 20071005 00029 WP 2007 10 5 07FDEA04425 1 20071001 A 5753 ARC19592 SKIN DOUG DC10 DC1030 3023501 WP ZONE 600 LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 DURING INSPECTION ON RT WING OUTBD FLAP LWR SKIN FOUND 50 LOOSE FASTENERS. 2 L 7 3 4F A22WE 2007100500030 20071005 00030 EU 2007 10 5 07FDEA04426 1 20071001 A 5315 A537773651212 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION AT UPPER FLANGE OF TOP CAP BEAM C33 SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 2007100500031 20071005 00031 EU 2007 10 5 07FDEA04427 1 20071001 A 5313 A53980852 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION AT STRINGER P 54 AND P56, LT, BETWEEN C 70-72 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007100500032 20071005 00032 EU 2007 10 5 07FDEA04428 1 20071001 A 5313 A53980852202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION AT STRINGER P 56LH, BETWEEN C 76-77. REPAIR PERFORMED BY BLEND OUT CORROSION AND FLAP PEENING IAW EA 6- 5318-81118 AND RAS/DATLS/0002357/2005 ISS A. 2 L 7 2 4F RT A35EU 2007100500033 20071005 00033 WP 2007 10 5 07FDEA04429 1 20071001 A 5753 ARC19591 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 500 LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 DURING INSPECTION ON LT WING OUTBD FLAP LWR SKIN FOUND 100 LOOSE FASTENERS. 2 L 7 3 4F RT A22WE 2007100500037 20071005 00037 NM 2007 10 5 DHLA200700050 1 20071003 A 2782 FITTING BOEING 727 7272B7 138407L NM SHUTTLE VALVE FAILED A DHLA O OTHER K FLUID LOSS CL CLIMB 1 GL 05 762AT 22162 UPON FLAP RETRACTION FROM FLAPS 2 TO 0, SYSTEM A HYD QTY WENT TO 0. FOUND FITTING BLOWN OUT ON NR 7 SLAT SHUTTLE VALVE. REPLACED NR 7 SLAT ACTUATOR SHUTTLE VALVE PER M/M 27-81-71. SERVICED HYDRAULICS TO FULL PER 12-12-0. OPS CHECKS NORM AL. 2 L 7 3 4F A3WE 2007100500038 20071005 00038 EU 2007 10 5 DHLA200700049 1 20070929 A 3230 DAMPENER AIRBUS 300 A300B4203 3930306 EU MLG PITCH FEEL FAILED A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 367DH 265 ON T/O, LDG GEAR HANDLE WILL NOT RETRACT. RAN FULL PROCEDURE UNABLE TO RAISE LDG GEAR. FOUND LEFT MAIN LANDING GEAR PI TCH FEEL DAMPENER FAILED. REMOVED AND REPLACED LEFT MLG PITCH DAMPENER PER AMM 32-11-15, OP CHECKS GOOD. 2 L 7 2 4F RT A35EU 2007100500040 20071005 00040 EU 2007 10 5 07FDEA04434 1 20071001 A 7120 A54611155500 MOUNT AIRBUS 310 A310222 3930315 EU ENGINE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 NR 2 PYLON TO ENGINE FORWARD INBD MOUNT PLATE HOLE GALLED INSIDE, FORWARD MOUNT. BLENDED AREA IAW A310-200 SRM 54-51-81 . HOLE SIZE IS .842 WITHIN LIMITS IAW A310-200 SRM 54-51-81. CADIMUM PLATED IAW A310-200 SRM 51-21-10. ADHESION TEST PASSED IAW FEDEX A310-200 SRM 51-21-10. 2 L 7 2 4F RT A35EU 2007100500041 20071005 00041 EA 2007 10 5 A6WA200740532 1 20070823 A 5320 6002113444 PANEL CNDAIR CL600 CL6002B19 1900309 EA CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 467AW 7900 RT LOWER VISOR PANEL 326BR, P/N 600-21134-44, CRACKED APPROX 4.5 INCH LONG AT FORWARD END OF PANEL. MAINTENANCE REPLACE D DAMAGED PANEL WITH A SERVICEABLE REPAIRED PANEL P/N 600-31134-44. (M) 2 L 7 2 4F RT A21EA 2007100500042 20071005 00042 WP 2007 10 5 NACA20070018 1 20070920 A 3230 AN4DD10 BOLT DOUG DC6 DC6A 3021706 WP MLG UPLOCK SHEARED A NACA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 6174C 26 44075 LANDING GEAR UNSAFE CONDITION IN NEUTRAL. FOUND RIGHT UPLATCH SHEAR BOLT SHEARED. REPLACED BOLT AND PERFORMED GEAR SWI NG PER NAC PURDUE MB6-0-1. OPS CHECKED GOOD. 2 L 7 4 4R 6A3 2007100500045 20071005 00045 EA 2007 10 5 A6WA200740488 1 20070826 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 467AW 7900 FOUND FORWARD WEB CRACKED IN RADIUS .400 INCH LONG AT STEP 832CT ON PAX DOOR. S/D - MAINTENANCE REPLACED IAW BOMBARDIER REO 601R-52-11-702. (M) 2 L 7 2 4F RT A21EA 2007100500046 20071005 00046 EA 2007 10 5 A6WA200740455 1 20070812 A 5310 601R35050109 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 464AW 7890 FOUND CARGO DOOR TRACK SUPPORT BEAM ANGLE AT FS 621 IS CRACKED AT BOTTOM ANGLE. MAINTENANCE REPLACED ANGLE IAW CRJ 200 SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007100500050 20071005 00050 2007 10 5 WGEA200700008 4 20071001 A 2397 231062081003 COAX ECLIPS EA500 ECLIPSEEA500 3350000 SW NR 1 COMM DEFECTIVE E WGEA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 135DJ 43 000036 NR 1 COMM WOULD NOT TRANSMIT OR RECEIVE DURING FLIGHT. HAPPENED DURING CLIMB FROM FL 090 TO 110. FOUND BAD COMM NR 1 C OAX CABLE. REMOVED AND REPLACED COMM NR 1 COAX CABLE IAW EA500 AMM 23-10-00. PERFORMED VOICE COMMUNICATION ADJUSTMENT TEST IAW EA500 AMM 23-10-00. CHECKED GOOD. RESECURED AND PERFORMED ADJUSTMENT TEST OF LEFT PFD IAW EA500 AMM 31-10-00. OPS CHECK GOOD. VERIFIED TRANSPONDER NR 1 AND NR 2 COMPLY WITH FAR 91.413 APPENDIX F. PERFORMED ALTITUDE CORRELATION TEST PER PARAGRAPH C OF FAR PART 43 APPENDIX E. NO DATA CORRESPONDENCE ERRORS FOUND FOR TRANSPONDERS NR 1 AND NR 2. 1 L 7 2 4J RT A00002AC 2007100500052 20071005 00052 EU 2007 10 5 07FDEA04367 1 20070928 A 5754 A57843203203 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND SCRATCHES ON NOSE SKIN OF SLAT NR 2 RT WING, RIB 24-27. NOSE SKIN REPAIR PERFORMED IAW SRM 57-43-11/FIG 202/SHEET 11. REFER TO NON ROUTINE DR0399, AT RIB 27 OTHER ASNA0081A FASTENERS ARE INSTALLED ACC TO DRW A578-44242/SHEET 16, IAW AI-STATEMENT 942-037611/005/2005. 2 L 7 2 4F RT A35EU 2007100500054 20071005 00054 EU 2007 10 5 07FDEA04369 1 20070928 A 5320 A53986733 PLATE AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 DAMAGED WEB PLATES BETWEEN FRAME 86-87, STGR 39 LT AND RT. REPLACEMENT OF WEB PLATES LT AND RT IAW SRM 51-72-10 2 L 7 2 4F RT A35EU 2007100500058 20071005 00058 EU 2007 10 5 07FDEA04437 1 20071002 A 5330 SKIN AIRBUS 310 A310222 3930315 EU FUSELAGE CANNING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 LOWER AFT EXTERNAL FUSELAGE SKIN AT FRAME 79, STR 36R-37R HAS BULGE AND OIL CANS. 10-19-07 MAJOR REPAIR, REMOVED D AMAGE AREA, FABBED DOUBLER, ALODINED AND PRIMED, INSTALLED DOUBLER AND WASHERS, APPLIED CPC IAW A310-200 SRM 53-10-12 FIG 225, 51-40-50 FIG 3, 51-21-10 PAGE 62, 53-10-12 PAGE 357, 51-71-10, 51-23-20. 2 L 7 2 4F RT A35EU 2007100500059 20071005 00059 EU 2007 10 5 07FDEA04373 1 20070928 A 5712 A579601320000 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 DURING SCHEDULED B CHECK, LT INBOARD FLAP RIB 25, P/N A 5796011320000 WAS FOUND TO CRACKED IN TWO PLACES, A 1.5 INCH CR ACK WAS FOUND IN THE FWD UPPER RADIUS AND A 1.5 INCH CRACK WAS FOUND IN THE AFT UPPER RADIUS AND FLANGE, REF: N00029. REMOVED AND REPLACED DAMAGED RIB REF: A300 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007100500060 20071005 00060 EU 2007 10 5 07FDEA04438 1 20071002 A 5743 A572240391206 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND AT LT MLG FWD PINTLE PICK-UP FITTING TOOL MARKS AND BORE AND FASTENER HOLE CORROSION. REPAIR PERFORMED BY REPLACE MENT OF FWD PICK UP FITTING IAW DRAWING R572-40266. REPLACEMENT OF TENSION FITTING AND REWORK OF CORROSION IN FASTENER HOLE AND FREEZE BUSH INSTALLATION IAW EA 6-5751-112441 AND RAS/BAE/1005058/2007 ISS A. 2 L 7 2 4F RT A35EU 2007100500061 20071005 00061 EU 2007 10 5 07FDEA04439 1 20071002 A 5320 A57130050204 ANGLE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION AT PICK UP ANGLE C40-41LT REPAIR PERFORMED BY REPLACEMENT OF PICK UP ANGLE AND SPLICING WITH EXTERNAL RE PAIR ANGLE AND INTERNAL STRAP IAW EA 6-5315-106521 AND RAS 052466/027/2007 ISS A. 2 L 7 2 4F RT A35EU 2007100500062 20071005 00062 EU 2007 10 5 07FDEA04440 1 20071002 A 5320 INTERCOSTAL AIRBUS 310 A310222 3930315 EU BS 904 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 E/COMPARTMENT, INTERCOSTAL CRACKED AT COCKPIT FLOORBEAM, FRAME 7, STA 904, BL30L,-Y 760 IN WORK. 10-18-07 REMOVED INTERCOSTAL CRACKED IAW A310 SRM 51-40-21. INTERCOSTAL CRACKED REQUIRES TO REPLACE IAW A310 SRM 51-72-01 MAT ID NEW WEB. 050 2024T3 IAW A310 SRM 51-31-00 PG 19/20 TABLE 3 SHEET 1. MAT EQUIVALANCE CHART ORG MAT IS CLAD 2024-742 REF A310 SRM 5 3-11-15. FORMED WEB REF A310 SRM 53-11-15 AND AEROSPATIALE DWG 107270, LOCATED AND DRILLED IAW A310 SRM 51-40-44. ALOD INED IAW A310 SRM 51-21-10. PRIMED AND PAINTED BOTH IAW A310 SRM 51-23-10. MARKED PN IAW A310 SRM 53-11-15. INSTALLED IA W A310 SRM 51-40-21. MAJOR REPAIR 2 L 7 2 4F RT A35EU 2007100500065 20071005 00065 EU 2007 10 5 07FDEA04443 1 20071002 A 5720 A57110922203 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND AT C47 INTERNAL CENTER WING RT VERTICAL FLANGE FITTING HOLE NR A, NR E, NR F, NR G, NR P, NR Q AND NR S WITH CORRO SION. REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL CORROSION REMOVAL IAW EA 6-5710-106533 AND RAS 052780/019/2007 ISS A. 2 L 7 2 4F RT A35EU 2007100500066 20071005 00066 EU 2007 10 5 07FDEA04444 1 20071002 A 5720 A57111092202 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND AT C47 INTERNAL CENTER WING RT VERTICAL FLANGE FITTING HOLE NR U, NR I AND NR H WITH CORROSION. REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL CORROSION REMOVAL IAW EA 6-5710-106533 AND RAS 052780/019/2007 ISS A. 2 L 7 2 4F RT A35EU 2007100200174 20071002 00174 WP 2007 10 2 WRLA2007096 1 20070923 A 5320 WEB DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 303WL 46917 DURING C-5 CHECK, CENTER CARGO AFT VERTICAL WALL AT STA 1841, THERE IS A DOUBLER REPAIR INSTALLED WITH BLIND RIVETS AND WITHOUT CRACK BLEND OUT. NR 67342. FAA FINDING. 10-12-07 PERFORM FINAL REPAIR PER SRM VOL.1 53-00-01 P.14. 2 L 7 3 4F 4 F RT A22WE E23EA 2007100200193 20071002 00193 EA 2007 10 2 TRAX200701380 1 20070921 A 2560 MEGAPHONE CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 748EV 10158 PORTABLE MEGAPHONE WILL NOT WORK. 2 L 7 2 4F RT A21EA 2007100200198 20071002 00198 NM 2007 10 2 SWAA074773 1 20070924 A 2761 6935981 ROD END BOEING 737 7373H4 1384600 NM SPOILER ACTUATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED C2 CHECK, FOUND RT WING NR 5 GROUND SPOILER OUTBOARD ACTUATOR ROD END BROKEN. REMOVED AND REPLACED ROD END PER MM. 2 L 7 2 4F RT A16WE 2007100200204 20071002 00204 NM 2007 10 2 CALA0700537 1 20070925 A 5330 6545775 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A .75 INCH CRACK WITH CREASE IN SKIN AT STA 900 BETWEEN S23R AND S24R. THE DAMAGED AREA OF SKIN WAS RE MOVED AND DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-00-01, FIGURE 201. 2 L 7 2 4F RT A16WE 2007100200208 20071002 00208 WP 2007 10 2 ABXA070323 1 20070924 A 3350 60030451 POWER SUPPLY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 976AX 604 47596 EMERGENCY EXIT LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW DC9 MM 33-53-02-4. 2 L 7 2 4F A6WE 2007100200210 20071002 00210 NM 2007 10 2 ZZDA2007272 1 20070915 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 936AT 55058 WHILE DOWN JACKING A/C AFT JACK FAILED AND DAMAGED A/C. INSTALLED FILLER, DOUBLER, AND TRIPLER. INSTALLED HL18PB6 HI-L OKS WET WITH PR1422 B1/2. INSTALLED CR3223-5 BLIND FASTENERS FOR AFT TWO FASTENER ROWS COMMON TO THE APB TEE CAP REAR T ANG. MAINTAINED 4-6D FASTENER SPACING AND 2D MIN EDGE DISTANCE. 2 L 7 2 4F TR A6WE 2007100200230 20071002 00230 EA 2007 10 2 COMA0760584 1 20070924 A 3234 750005000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 587SW 29589 7062 FLIGHT 5037 - ON CLIMBOUT FROM BTV NOSE GEAR FAILED TO RETRACT, FOLLOWED BY NOSE GEAR DISAGREE. A/C RETURNED BACK TO BT V AND LANDED SAFELY. REMOVED AND REPLACED MLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2007100200240 20071002 00240 NM 2007 10 2 SWAA074816 1 20070926 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 472WN 33831 DURING SCHEDULED HC1 CHECK, FOUND EEPLS LENS CRACKED AT ROW 2 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007100300001 20071003 00001 EA 2007 10 3 NW6A0070901 1 20070917 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE EMERGENCY LIGHTS INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 157GJ 10230 EMERGENCY LIGHTS BY SERVICE DOOR INOPERATIVE. REPLACED BULB OPS OK. 2 L 7 2 4F 4 F RT A21EA E15NE 2007100300002 20071003 00002 EA 2007 10 3 NW6A0070902 1 20070919 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE EMERGENCY LIGHT INOPERATIVE A N6WA K NONE L NO TEST IN INSP/MAINT 1 CE 03 165GJ 10257 RT EXTERIOR EMERGENCY LIGHT INOP OVERWING EMERGENCY EXIT. REPLACE BULB, OPS OK. 2 L 7 2 4F 4 F RT A21EA E15NE 2007100300003 20071003 00003 SO 2007 10 3 XGN2007F00026 2 20070905 A 8530 TISN712ACA CYLINDER BEECH 36 36BEECH 1151602 CE CONT O520 IO520BA 17032 SO ENGINE CRACKED E XGNA O OTHER O OTHER NR NOT REPORTED 1 SW 05 1194A 581 E159 807201R CRACKED BEHIND INJECTOR BETWEEN 1ST AND 3RD FIN. (K) 1 L 7 1 3O 3 O 3A15 E5CE 2007100400004 20071004 00004 EA 2007 10 4 SIMA200726905 1 20070912 A 5320 67053110521 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 508AE 11463 10072 DURING 3C CHECK INSPECTION REVEALED RIGHT WEB AT STA 280 CORRODED IN SEVERAL LOCATIONS. SPLICED IN NEW WEB AT STA 280 I AW AEA EO CR-53MR-135. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007100400006 20071004 00006 NM 2007 10 4 AALA20071818 1 20070928 A 3350 B21506 FUSE BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 796AN 30796 JFK - EMERGENCY EXIT LIGHT AT OVERHEAD RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED FUSE AT BATTERY PACK FOR EMERGENCY E XIT LIGHT AT OVERHEAD RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007100400007 20071004 00007 WP 2007 10 4 AALA20071817 1 20070927 A 1100 PLACARD DOUG DC9 DC982 3022082 WP CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 451AA 49477 LGA - EMERGENCY EXIT LIGHT AT OVERHEAD BIN LEFT SEAT ROW 20 MISSING BRAILLE BUMPER. REPLACED BRAILLE BUMPER FOR EMERGEN CY EXIT LIGHT AT OVERHEAD BIN LEFT SEAT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007100400008 20071004 00008 NM 2007 10 4 AALA20071819 1 20070928 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 EMERGENCY LIGHT AT RIGHT NUMBER ONE AND LEFT NUMBER TWO DOOR CIRCUIT BREAKER KEEPS POPPING. REPLACED BATTERY PACK AT RI GHT NUMBER ONE DOOR FOR EMERGENCY EXIT LIGHT AT RIGHT NUMBER ONE AND LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007100400009 20071004 00009 NM 2007 10 4 AALA20071820 1 20070919 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 938AN 29533 TUL - EMERGENCY LIGHTS IN AREA OF STATION 500 AFT OF PARTITION INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AREA OF STATION 500 AFT OF PARTITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007100400011 20071004 00011 NM 2007 10 4 AALA20071822 1 20070923 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 938AN 29533 TUL - EMERGENCY LIGHTS IN AREA OF STATION 511 RIGHT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS I N AREA OF STATION 511 RIGHT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007100400022 20071004 00022 NM 2007 10 4 DLM90071256 1 20070924 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 558 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 RT CUSP WEB CORRODED STA 558. REPLACED CUSP WEB ON WORK ORDER 1002987 2400 0227, DL 63329. 2 L 7 2 4F RT A6WE 2007100400027 20071004 00027 EA 2007 10 4 SWIA200718703 1 20070917 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCONNECTED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 938SW 7741 FLT 5967 - THE EMERGENCY FLOOR LIGHTING BETWEEN ROWS 2 AND 5 DOES NOT WORK. ALSO, THE EMERGENCY EXIT SIGN BELOW THE LEF T WING EMERGENCY EXIT DOES NOT WORK. SECURED PLUG AT LIGHT STRIP. OPS CHECK GOOD FOR ALL LIGHTS IAW AMM 33-25-00. 2 L 7 2 4F RT A21EA 2007100400034 20071004 00034 EA 2007 10 4 SWIA200718710 1 20070918 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 770SK 10243 FLT 6027 - EMERGENCY LIGHTS BY PAX DOOR ARE INOP. REPLACED THE PAX DOOR FLOOR LEVEL EMERGENCY LIGHT ASSY IAW MM 33-51-1 1. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2007100400037 20071004 00037 2007 10 4 AALA20071823 4 20070928 A 2320 570111 CONTROL PANEL BOEING 777 777223 1385213 NM AUDIO INOPERATIVE A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 796AN 30796 LHR INFLIGHT T141/28SEP - CREW LOST RADIO TRANSMISSION. EICAS INDICATION ILLUMINATED. RETURNED TO LHR AND LANDED WITHO UT INCIDENT. REPLACED CAPTAINS AUDIO CONTROL PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007100400045 20071004 00045 EA 2007 10 4 QXEA200701496 1 20071001 A 2150 A/C PACK CNDAIR CL600 CL6002C10 1390015 EA RIGHT WARNING MESSAGE A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 603QX 10011 GEG - FLIGHT 2517, RECEIVED A RIGHT PACK CAUTION ON TAXI. RETURNED TO THE GATE. MAINTENANCE PLACED THE SYSTEM ON MEL 2 1-51-1B. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007100400048 20071004 00048 NM 2007 10 4 DL76G071261 1 20070925 A 5315 AND101331002 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 654 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 156DL 25354 FLOORBEAM CORRODED. REMOVED AND REPLACED FLOORBEAM UPPER CHORD PER SRM 53-00-51. 2 L 7 2 4F RT A1NM 2007100400073 20071004 00073 2007 10 4 AALA20071809 4 20070925 A 2565 100504205 SLIDE DOUG DC9 DC982 3022082 WP GALLEY DOOR LOW PRESSURE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 TPA - FORWARD GALLEY DOOR SLIDE PRESSURE OUT OF RANGE. REPLACED FORWARD GALLEY DOOR SLIDE. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F A6WE 2007100400074 20071004 00074 NM 2007 10 4 AALA20071810 1 20070925 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AM 24579 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 2E HAS BROKEN SHROUD. REPLACED SHROUD FOR SEAT MOUNTED EMERGENCY LIGHT A T SEAT ROW 2E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007100400075 20071004 00075 WP 2007 10 4 AALA20071813 1 20070926 A 3350 0201804001 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 465A 49595 LAX - EMERGENCY LIGHT AT SEAT 10D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F A6WE 2007100400081 20071004 00081 EA 2007 10 4 A6WA200740494 1 20070903 A 5312 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA BULKHEAD CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 422AW 7341 THE STIFFENER POST AT RBL 18 ON THE FORWARD FACE OF THE 409 PLUS 128 BULKHEAD IS CRACKED ON THE OUTBOARD SIDE IN THE RAD IUS BY THE LOWER RIVET. SUP - MAINTENANCE REPAIRED STIFFENER POST AT RBL 18 ON FWD FACE OF 409 PLUS 128 BULKHEAD BY TR IMMING OF DAMAGE, FABRICATED REPAIR AND INSTALLED IAW BOMBARDIER REO 601R-53-41-056 REV E. (M) 2 L 7 2 4F RT A21EA 2007100400087 20071004 00087 EA 2007 10 4 A6WA200740535 1 20070827 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 424AW 7656 RT LOWER WING PLANK ACCESS HOLE 650AB HAS MINOR PITTING CORROSION IN NON-CRITICAL AREA OUTBOARD SIDE OF CUTOUT ON LANDIN G. CORROSION AREA IS APPROX 2.5 INCHES IN LENGTH AND .2 INCHES WIDE CORROSION PITTING IS APPROX .004 INCH BY .006 INCH BY .008 INCH DEEP. MAINTENANCE PERFORMED A MAJOR REPAIR BY BLENDING MINOR PITTING CORROSION AFT RT LOWER WING PLANK ACC ESS HOLE 650AB, WS 163, HOLE NR 9 IAW BOMBARDIER REO 601R-57-21-030 REV F. (M) 2 L 7 2 4F RT A21EA 2007100400088 20071004 00088 NM 2007 10 4 P5CA0701534 1 20070925 A 5347 SEAT TRACK BOEING 747 74746NF 13848BT NM BS 1450 BROKEN A P5CA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 15 454PA 30812 MAIN DECK CENTER GUIDE LEFT SEAT TRACK AT STATION 1450 LBL 12 HAS 9 INCHES OF VERTICAL LIP BROKEN. DEFERRED 15 CYCLES A S PER MA A45300-08:00 FAA 8110-3. 2 L 7 4 4F RT A20WE 2007100400092 20071004 00092 EU 2007 10 4 07FDEA04152 1 20070921 A 5730 A57243207203 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FOUND CHAFING MARKS ON LEADING EDGE SKIN BETWEEN SLAT TRACK 7-8 OF RT WING. NOSE SKIN REPAIR PERFORMED IAW SRM 57-41-12 /FIG 203, 204. 2 L 7 2 4F RT A35EU 2007100400097 20071004 00097 EU 2007 10 4 07FDEA04157 1 20070921 A 5320 A53778329 PLATE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORRODED SHEAR PLATE BETWEEN FRAME 36-37 LT, STRG 44. REPLACEMENT OF SHEAR PLATE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100400109 20071004 00109 WP 2007 10 4 07FDEA04165 1 20070921 A 5321 ABA72039 FLOOR PANEL DOUG DC10 DC1010F 3022111 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 PERFORMED INSPECTION AFTER REMOVAL FLOOR PANEL IN COCKPIT WITH OAN JC SP10530208-2JR, FOUND CRACK ON MEMBRANE. REPAIR ED WEB IAW SRM 53-00-01 VOL I FIG 10. 2 L 7 3 4F A22WE 2007100400112 20071004 00112 EU 2007 10 4 07FDEA04168 1 20070921 A 5311 A53772100 FRAME AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 CORROSION ON FRAME 19 LOWER FLANGE BETWEEN STRINGER 52-53 LT. REPAIR PERFORMED BY CUT OUT FRAME FLANGE AND INSTALLING F ABRICATED REPAIR ANGLE ON FRAME IAW TD 038083/004/2005 ISSUE A AND EA 6-5312-82892. 2 L 7 2 4F RT A35EU 2007100400114 20071004 00114 EU 2007 10 4 07FDEA04170 1 20070921 A 5320 A53811601200 WEB AIRBUS 310 A310324 3930206 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 IN AUGUST 1198: SEVERAL SPOTS OF CORROSION HAD BEEN FOUND ON VERTICAL WEB (SEGMENT) OF PRESSURE BULKHEAD AT FRAME 39, Y= 0. REPAIRS HAD BEEN PARTIALLY PERFORMED IN ACCORDANCE WITH TD 582.0939/98 ISSUE A IN JULY 2005: NEW CORROSION FINDINGS HAVE BEEN REPORTED, HOLE D WAS ALSO REPORTED NOT REPAIRED IAW TD 582.0939/98 ISS A. REPAIR PERFORMED IAW TD 582.0939/9 8 ISSUE A AT HOLE D AND IAW TD 942.001478/023/1998 ISSUE B AT HOLE B, APPROVED BY EA 6-5315-82897 AND RAS/AS/0130/2005 I SSUE A. 2 L 7 2 4F RT A35EU 2007100400117 20071004 00117 EU 2007 10 4 07FDEA04171 1 20070921 A 5330 A53811414200 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CHAFING MARK FOUND ON LOWER INNER SKIN BETWEEN FRAME 46-47 AND STRG 44-45. REPAIR PERFORMED BY SMOOTHLY REWORK, DVI-HFE C-ROTOTEST INSPECTION AND INSTALLATION OF R1 OVERSIZED FASTENERS IF NECESSARY IAW EA 6-5315-82917 AND RAS 038213/011/200 5 ISSUE A. 2 L 7 2 4F RT A35EU 2007100400124 20071004 00124 EU 2007 10 4 07FDEA04179 1 20070921 A 5210 A52111409200 FITTING AIRBUS 310 A310324 3930206 EU ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORROSION ON FITTING AT FWD PAX DOOR LT. REPLACEMENT OF FITTING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100400125 20071004 00125 EU 2007 10 4 07FDEA04180 1 20070921 A 5210 A52111141200 FITTING AIRBUS 310 A310324 3930206 EU ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORROSION ON FITTING AT FWD PAX DOOR LT. REPLACEMENT OF FITTING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100400153 20071004 00153 NM 2007 10 4 GTIA200700019 1 20070919 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 514NK 2679 FLOORBEAM AT Y765 BETWEEN FR 67 AND FR 69 HAS CORROSION. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2007100400156 20071004 00156 NM 2007 10 4 GTIA200700022 1 20070919 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 514NK 2679 FLOORBEAM AT R-2 DOOR ENTRANCE BETWEEN FR67 AND FR68 (-Y1292) CORRODED. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2007100400167 20071004 00167 NM 2007 10 4 07FDEA03952 1 20070918 A 5740 ARC7490501 TEE FITTING DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 AFTER BUSHING REMOVAL, RIGHT WING INBOARD FLAP VANE OUTBOARD TEE FITTING BORE FOUND CORRODED. RIGHT WING INBOARD FLAP VANE OUTBOARD TEE FITTING REMOVED AND REPLACED AS PER AMM 27-50-22-4. 2 L 7 3 4F RT A22WE 2007100400170 20071004 00170 EU 2007 10 4 SIMA200727304 1 20070926 A 5310 WINDOW FRAME SAAB SF340 340B 7860101 EU BS 583-608 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 211NE 22399 5000 340B211 DURING A HMBV INSPECTION CORROSION WAS DISCOVERED AROUND THE RT PAX WINDOW BETWEEN FUSELAGE STA 583 AND 608. BLENDED DA MAGE IAW SAAB REPAIR STATION 340 SDS 013060 PARA 1 DATED SEPT 18,2007. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007100400191 20071004 00191 EA 2007 10 4 A6WA200740540 1 20070905 A 5340 601R75262159 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 425AW 7663 BRAKE TRANSDUCER BRACKET IN LT MLG WHEEL WELL IS CRACKED. MAINTENANCE REMOVED AND INSTALLED SERVICEABLE BRACKET P/N 601 R75262-159 IAW CRJ 200 SRM 51-41-04, AND 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007100400192 20071004 00192 EA 2007 10 4 A6WA200740537 1 20070911 A 5753 SKIN CNDAIR CL600 CL6002B19 1900309 EA TE FLAP DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 422AW 7341 LT INBOARD FLAP HAS DENT MEASURING 1.5 INCHES LONG BY 2.5 INCHES WIDE AND .030 INCHES DEEP LOCATED 24 INCHES FROM INBOAR D END OF FLAP AND 6 INCHES FROM TRAILING EDGE, LOWER SKIN. MAINTENANCE CUT AWAY DAMAGED SECTION OF SKIN AND INSTALLED A NON-FLUSH REPAIR DOUBLER IAW CRJ SRM 57-52-00, REPAIR NR 3. (M) 2 L 7 2 4F RT A21EA 2007100400197 20071004 00197 EU 2007 10 4 07FDEA04301 1 20070926 A 5313 A53777942 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 FOUND DEBONDED STRINGER 39 BETWEEN FRAME 28-30 LT AND STGR 41 BETWEEN FRAME 29-30 LT. REPAIR PERFORMED BY CUTTING BOTH STRINGER BETWEEN FRAME 30-31, REMOVING AND CHECKING THEM IF DAMAGED. INSTALLING AGAIN IAW SRM 53-10-14/FIG 201, 202. 2 L 7 2 4F RT A35EU 2007100500001 20071005 00001 EU 2007 10 5 07FDEA04393 1 20071001 A 5313 A53811405 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 ISS A. 2 L 7 2 4F RT A35EU 2007100500006 20071005 00006 EU 2007 10 5 07FDEA04398 1 20071001 A 5711 A57150802203 SPAR AIRBUS 310 A310324 3930206 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 SHOULDERED BOLTS FOUND DURING EMBODIMENT OF SB A310-57-2079 AT HOLE NR 21 AND NR 14 RT REAR SPAR AREA OF SPOILER NR 3 RT REPAIR PERFORMED BY REPLACEMENT OF BUSH IAW EA 6-5720-82852 AND RAS /BAE/1000689/2005 ISS A. 2 L 7 2 4F RT A35EU 2007100500012 20071005 00012 EU 2007 10 5 07FDEA04404 1 20071001 A 5542 A55471575000 SKIN AIRBUS 310 A310324 3930206 EU ZONE 300 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND AT RUDDER TRAILING EDGE LOWER CORNER DELAMINTION NEAR RIB 0 REPAIR PERFORMED IAW SRM 55-41-12 FIG 208A. 2 L 7 2 4F RT A35EU 2007100500018 20071005 00018 EU 2007 10 5 07FDEA04410 1 20071001 A 5330 A53978149200 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND DENT AT SKIN C63-65, P41-42 LT (AREA 1) AND P45-46 LT (AREA 2) DOUBLER REPAIR PERFORMED IN AREA 1 IAW SRM 53-10-12 FIG 228 AND LET THE DENT IN AREA 2 AS IT IS IAW EA 6-5317-81131 AND RAS/DATLS/0002418/2005 ISS A. 2 L 7 2 4F RT A35EU 2007100500020 20071005 00020 EU 2007 10 5 NWAA073283274 1 20070928 A 5230 SKIN AIRBUS 320 A320212 3930322 EU CARGO DOOR PUNCTURED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 374NW 50771 31868 1641 DURING "H" CHECK, FOUND PUNCTURE IN FORWARD CARGO DOOR INNER SKIN. REPAIRED PER EA 32-210218 SECTION I SECTION II OF E A 32-210218 TO BE ACCOMPLISHED WITHIN 180 DAYS. 2 L 7 2 4F RT A28NM 2007100500034 20071005 00034 WP 2007 10 5 07FDEA04430 1 20071001 A 5753 ARC19491 SKIN DOUG DC10 DC1030 3023501 WP ZONE 500 LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 DURING INSPECTION ON LT WING OUTBD FLAP UPPER SKIN FOUND 200 LOOSE FASTENERS. 2 L 7 3 4F A22WE 2007100500036 20071005 00036 EU 2007 10 5 07FDEA04432 1 20071001 A 5330 A536712608200 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND DENT DAMAGE AT SERVICE BOX PANEL C10-13 BUSH REPAIR PERFORMED IAW SRM 53-10-12 FIG 221. 2 L 7 2 4F RT A35EU 2007100500051 20071005 00051 NM 2007 10 5 07FDEA04366 1 20070928 A 5315 6516338283 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 MAIN DECK FLOORBEAM AT STA 720A LBL62 WL 208 T-CAP CORRODED OUT OF LIMITS. REMOVED CORRODED AREA, INSTALLED T-ANGLE AND SPLICE PLATE REPAIR IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007100500057 20071005 00057 EU 2007 10 5 07FDEA04436 1 20071002 A 5730 A57340086208 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION ON LT WING BOTTOM SKIN AT RIB 7-8, CENTER SPAR STRINGER 13 REPAIR PERFORMED BY BLEND OUT THE CORROSION I AW EA 6-5720-112460 AND RAS/BAE/1005212/2007 ISS A. 2 L 7 2 4F RT A35EU 2007100500063 20071005 00063 EU 2007 10 5 07FDEA04441 1 20071002 A 5720 A57111092202 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND AT C47 INTERNAL CENTER WING LT VERTICAL FLANGE HOLE NR I AND NR U WITH CORROSION. REPAIR PERFORMED BY BLEND OUT U NTIL CORROSION REMOVAL AND CUT EXTERNAL FITTING AT HOLE NR I IAW SB 57-6049 IAW EA 6-5710-106533 AND RAS 052780/019/2007 ISS A. 2 L 7 2 4F RT A35EU 2007100500067 20071005 00067 EU 2007 10 5 07FDEA04445 1 20071002 A 5330 A53772016 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND OLD FLUSH REPAIR AT C20-21, P 35-37 LT NOT COMPATIBLE WITH P TO F CONVERSION. REPAIR RENEWED IAW RAS/DABRE/700464 5/2004 ISS A. 2 L 7 2 4F RT A35EU 2007100500068 20071005 00068 NM 2007 10 5 NACA20070019 1 20070923 A 2761 65449617 ACTUATOR BOEING 737 737232 1384475 NM SPOILERS FRACTURED A NACA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 AL 03 321DL 727 23093 "A" SYSTEM HYDRAULIC FAILURE ON GROUND. REMOVED AND REPLACED NR 8 SPOILER ACTUATOR DUE TO HOUSING FAILURE. LEAK CHECK, FUNCTIONAL CHECK AND SPOILER TO FLAP CLEARANCE CHECKED GOOD. REF: B737MM 27-62-101. 2 L 7 2 4F RT A16WE 2007100500069 20071005 00069 EU 2007 10 5 07FDEA04447 1 20071002 A 5542 SKIN AIRBUS 310 A310324 3930206 EU RUDDER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 DELAMINATION FOUND AT RUDDER SIDE PANEL IN THE AREA OF ATTACH FITTINGS REPAIR PERFORMED IAW SRM 55-41-12 FIG 216. 2 L 7 2 4F RT A35EU 2007100500070 20071005 00070 EU 2007 10 5 07FDEA04448 1 20071002 A 5753 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 DAMAGED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 805FD 456 RT INNER FLAP WITH SEVERAL DAMAGES, LIMITED TO 5 FLIGHTS IAW RAS/DABRE/7002673/2003. REPAIR PERFORMED IN WORKSHOP AND R ELEASED IAW FAA FORM 8130-3 NR 05/1145. 2 L 7 2 4F RT A35EU 2007100500071 20071005 00071 EU 2007 10 5 07FDEA04449 1 20071002 A 5730 A57350143 SKIN AIRBUS 310 A310324 3930206 EU ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND ON LT WING ON PYLON NR 1 ELONGATED HOLE AT WING TO PYLON BOTTOM SKIN ON AREA OF HYDRAULIC LINES. REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW DRAWING R572-49184, APPROVED BY EA 6-5720-81128 AND RAS/BAE/100457/2005 ISS A. 2 L 7 2 4F RT A35EU 2007100500072 20071005 00072 EU 2007 10 5 07FDEA04450 1 20071002 A 5730 A57350143 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND ON RT WING ON PYLON NR 2 ELONGATED HOLE AT WING TO PYLON BOTTOM SKIN ON AREA OF HYDRAULIC LINES. REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW DRAWING R572-49184, APPROVED BY EA 6-5720-81128 AND RAS/BAE/100457/2005 ISS A. 2 L 7 2 4F RT A35EU 2007100500073 20071005 00073 EU 2007 10 5 07FDEA04452 1 20071002 A 5753 RIB AIRBUS 310 A310324 3930206 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND OLD REPAIRS ON INBOARD FLAP RIB 21 (POCKET REPAIRS) NOT CONFORM TO SRM REPAIR PERFORMED BY REPLACEMENT OF END RIB 21 IAW SRM 57-2055. 2 L 7 2 4F RT A35EU 2007100500074 20071005 00074 EU 2007 10 5 07FDEA04453 1 20071002 A 5730 A57310051 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION AT CENTER TANK TOP SKIN C 44-48, TRACK 3-5, LT/RT REPAIR PERFORMED BY REMOVAL OF CORROSION AND INSTALLIN G OF TWO DOUBLERS IAW DRAWING R573-10011 AT BEAM 4 AND 6, C 44-2 AND C 44 LT/RT IAW EA 6-5710-81129 AND RAS/AS/0036/2005 ISS A. 2 L 7 2 4F RT A35EU 2007100500075 20071005 00075 EU 2007 10 5 07FDEA04454 1 20071002 A 5347 A53611640200 SEAT TRACK AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND SEAT TRACK C 15A-19, Y-953 CORRODED REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100500076 20071005 00076 EU 2007 10 5 07FDEA04262 1 20070925 A 5311 A53811606200 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 CORROSION ON TEE SEGMENT FRAME 39 LOWER FLANGE BETWEEN STRINGER 52-53 LT. REPAIR PERFORMED BY CUTTING OUT THE DAMAGE PA RT AND REPLACE THE TEE SEGMENT, SPLICED WITH AN ANGLE AND A SPLICE IAW EA 6-5314-82906 AND RAS 038386/005/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100500077 20071005 00077 EU 2007 10 5 07FDEA04263 1 20070925 A 5315 A53773651212 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 HEAVY CORROSION ON CROSSBEAM, FRAME 38.2 RT TO LT, Y-805 TO 805. CROSSBEAM SPLICE REPAIR PERFORMED IAW SRM 53-10-15/FIG 207. 2 L 7 2 4F RT A35EU 2007100500080 20071005 00080 EU 2007 10 5 07FDEA04268 1 20070925 A 5754 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 FOUND OLD DAMAGE (DENTS AND BULGES) ON LEADING EDGE SKIN BETWEEN RIB 15-16 OF SLAT NR 2 LT. REPAIR PERFORMED BY CUT OUT SKIN AND INSTALLING EXTERNAL PATCH REPAIR IAW TD FOK/158/2005 ISSUE A, APPROVED BY EA 6-5743-92143 AND RAS/FOK/158/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100500082 20071005 00082 NM 2007 10 5 07FDEA04270 1 20070925 A 5340 69441049 STRINGER CLIP BOEING 727 727227 1384078 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 AFT PIT STA 1130 LBL 21 WL 140, STRINGER CLIP UNDER "Z" ANGLE HAS LIGHT CORROSION. REMOVED STRINGER CLIP. FABRICATED A ND HEAT TREATED NEW CLIP TO 7075 T6. TREATED, PRIMED, PICKED UP HOLES, AND INSTALLED NEW CLIP. REF: SRM 51-30-2, PG 1-1 2/51-10-1, PG 12/51-10-2, PG 1 BOEING DWG 69-44104-9. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007100500083 20071005 00083 EU 2007 10 5 2007UALA03828 1 20070923 A 2611 SMOKE DETECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 444UA 824 SDAC NR 1 ECAM MESSAGE FOUND DURING PRE DEPARTURE CHECK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007100500086 20071005 00086 NM 2007 10 5 2007UALA03830 1 20070921 A 5320 WEB BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU BS 794-847 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 929UA 26652 AFT PIT INNER THRESHOLD SUPPORT WEB CORRODED AT BS 794-847 STR 25R AT WL 150 APPROX. REPAIRED THRESHOLD SUPPORT WEB. 2 L 7 2 4F 4 F RT A16WE E21EU 2007100500087 20071005 00087 NM 2007 10 5 2007UALA03831 1 20070921 A 5320 STRAP BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU BS 780-800 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 929UA 26652 AFT CARGO PIT STRAP AT BS 780-800 AT STRINGER 16R IS DAMAGED. FABRICATED AND INSTALLED REPLACEMENT STRAP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007100500092 20071005 00092 NM 2007 10 5 2007UALA03836 1 20070922 A 5340 BRACKET BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU GIRT BAR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 FWD CABIN ENTRY DOOR GIRT BAR FITTING BRACKETS CORRODED AT STA 312-344 LBL 55-58 WL 208. CLEANED CORROSION. 2 L 7 2 4F 4 F RT A16WE E21EU 2007100500094 20071005 00094 NM 2007 10 5 2007UALA03949 1 20070927 A 3350 362624 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 334UA 24229 EMERGENCY EXIT LIGHT AT SEAT ROW 17 DEF INOP. REPLACED LAMP. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007100500099 20071005 00099 NM 2007 10 5 2007UALA03954 1 20070927 A 3350 SIGN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE G4A GALLEY EXIT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 518UA 24871 THE G4A GALLEY EXIT LIGHT SIGN CRACKED. 10-23-07 REPLACED EXIT SIGN LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007100500100 20071005 00100 NM 2007 10 5 2007UALA03955 1 20070927 A 2560 FLASHLIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 MID CABIN, RIGHT OUTBOARD FLIGHT SEAT HAS INOP EMERGENCY FLASHLIGHT. 10-23-07 REPLACED EMERGENCY FLASHLIGHT BATTER Y PACK IN RIGHT OUTBOARD FLIGHT ATTENDANT SEAT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007100500101 20071005 00101 NM 2007 10 5 2007UALA03956 1 20070927 A 3350 78941 LAMP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHT MISSING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 676UA 30028 EEL STRIP LIGHT ON SIDE OF SEAT 6H MISSING. 10-23-07 REPLACED EEL STRIP, OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007100500102 20071005 00102 NM 2007 10 5 2007UALA03957 1 20070927 A 2612 CIRCUIT CARD BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE APU FIRE FAULTY A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 795UA 26927 APU FIRE CARD MESSAGE DISPLAYED. 10-23-07 REPLACED CARDS A9 & A12. MESSAGE CLEARED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007100500103 20071005 00103 EU 2007 10 5 2007UALA03958 1 20070927 A 3510 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW OXYGEN LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 410UA 463 THE CREW O2 NEEDS SERVICE. CREW REPORTED CREW O2 READS -TOO FULL- MECH SERVICED O2 SYSTEM TO CORRECT PRESSURE. FIVE DA YS LATER - CREW REPORTS O2 -TOO LOW- SERVICED O2 SYSTEM TO 1820 PSI. NO REPEATS SINCE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007100500108 20071005 00108 NM 2007 10 5 2007UALA03963 1 20071001 A 5753 STRUCTURE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE TE FLAP DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 175UA 24382 RIGHT OUTBOARD AFT FLAP HAS 3 INCH DIA HOLE, BOTTOM AT APPROX 4 FT OUT FROM INBOARDD EDGE AND 7 INCHES UP FROM T/E. REP AIRED IAW SRM 51-70-02. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007100500111 20071005 00111 NM 2007 10 5 2007UALA03967 1 20071001 A 5100 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU UNKNOWN A UALA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 382UA 24657 FAILED MANUAL REVERSION. NOSE PITCHED UP. REQUIRED 3 TURNS NOSE DOWN TRIM. 2 L 7 2 4F 4 F RT A16WE E21EU 2007100500112 20071005 00112 NM 2007 10 5 2007UALA03968 1 20070928 A 5230 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 FWD CARGO DOOR S/N 1791 FRAME CRACKED AT LWR FITTING. MAJOR REPAIR ACCOMPLISHED: REPLACED FRAME WITH P/N 65-91700-866. 2 L 7 2 4F 4 F RT A16WE E21EU 2007100500113 20071005 00113 NM 2007 10 5 2007UALA03969 1 20070928 A 5320 ANGLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 848UA 1647 FWD PIT RE-ENFORCING ANGLE ON STR 42R FROM FR28 TO FR31. MAJOR REPAIR ACCOMPLISHED: REPLACED -L- ANGLE DOUBLER. 2 L 7 2 4F 4 F RT A28NM E40NE 2007100500117 20071005 00117 EU 2007 10 5 UPS07150796 1 20070920 A 5311 FRAME AIRBUS A300 A300F4622R 3930360 EU BS 2400 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 149UP 0832 INSPECTION TYPE:2C TRANSFERRED FROM DMI I318640-DENT 2" X 11" X .0625" DEEP AT STA 2400 FRA 38R. CUT OUT DAMAGE, FABRIC ATED REPAIR DOUBLER AND FILLER, AND INSTALLED IAW A300 SRM 53-10-12 FIG 210. 2 L 7 2 4F RT A35EU 2007100500121 20071005 00121 WP 2007 10 5 UPS07850793 1 20071001 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:N/A ON PRE DEPARTURE CHECK FOUND EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK. REF DC8 AMM 24-00-00. 2 L 7 4 4F RT 4A25 2007100500122 20071005 00122 NM 2007 10 5 UPS07M50788 1 20071001 A 2612 2240153507 FIRE LOOP DOUG MD11 MD11F 3023600 NM GE CF6 CF650C2 30018 NE NR 3 NACELLE SHORTED A IPXA F ACTIVATE FIRE EXT. N FALSE WARNING LD LANDING 1 SO 01 260UP 48418 702327 INSPECTION TYPE:N/A AFTER LANDING RECEIVED LVL 3 ENG 3 FIRE DET ALERT. FOLLOWED PROCEDURE W/FIRE AGENT DISCHARGED. REM OVED AND REPLACED NR 3 ENG UPPER FIRE DETECTOR LOOP ASSY PER MM 26-11-03-4. REMOVED AND REPLACED FDCU PER MM 26-11-02-4 . P/N ON/OFF 8038-02-03. S/N OFF 297 FOR FDCU. 2 L 7 3 4F 4 F RT A22WE E23EA 2007100500123 20071005 00123 NM 2007 10 5 UPS07M50789 1 20070718 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM BS 1597-1605 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C CENTER CARGO PIT ON R48 FOUND CORROSION STA 1597 - 1605. LONGERON R48 CORR AREA STA 1611 TRIM OFF PER EN1491-07. HFEC INSP C/O ON TRIM OFF AREA, NO CRACK EVIDENT. REPAIR LONGERON & SPLICE FAB PER EN1491- 07. FPI C/O ON FAB PARTS, NO CRACK EVIDENT. REPAIR PARTS FASTENER HOLES PICKED-UP, REWORKED & REPROTECTED. REPAIR SKIN & PARTS PAINT ED. REPAIR LONGERON PARTS INSTALLED PER EN1491-07 & SRM 51-31-01 VII R38. 2 L 7 3 4F RT A22WE 2007100500126 20071005 00126 NM 2007 10 5 UPS07M50792 1 20070810 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT BORE LT 22 FOUND WITH CORROSION. CORR AT BARREL NUT BORE REMVD PER SRM 51-21-01 VII R38. BOTTOM SURFACE BORE THRU, BORE REAM TO 1.067" DIA, REMN BLEND OUT 0.140" DEEP, EXCEEDED LIMITS. BARREL NUT BORE REAM FURTHER TO 1.105" DIA PER EN1515-07. BARREL NUT BORE & BLEND OUT PERIPHERY RADIUS, SMOOT HED, PROTECTED. BUCKET BUSHING FAB, PROTECTED & INSTALLED. REPAIR C/O IS ACCEPTABLE PER EN1515-07. 2 L 7 3 4F RT A22WE 2007100500128 20071005 00128 NM 2007 10 5 2007UALA03839 1 20070923 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 492 S24R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 FWD PIT DOOR CUTOUT AFT FRAME AT BS 492.5 AND STRINGER 24R END FITTING DAMAGED. UPPER EDGE CRACKED. REMOVED DAMAGE. FA BRICATED AND INSTALLED REPLACEMENT STRINGER END FITTING. 2 L 7 2 4F 4 F RT A16WE E21EU 2007100500129 20071005 00129 NM 2007 10 5 2007UALA03840 1 20070923 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 616 S17L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 FUSELAGE OVERWING FRAME STA 616 STR 17L HAS CRACK RUNNING FROM BOTTOM TIP UP THRU 2 FASTENER HOLES. REMOVED DAMAGE. FAB RICATED AND INSTALLED NESTED ANGLE AND FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007100500134 20071005 00134 NM 2007 10 5 2007UALA03845 1 20070922 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 DOOR 3L EMERGENCY FWD SILL LIGHT INOP. 10-19-07 RELAMPED. OP CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007100500136 20071005 00136 NM 2007 10 5 2007UALA03847 1 20070922 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EEL ADJACENT TO LAV 100 SIDEWALL & UD LAV ARE INOP. 10-19-07 FOUND EEL LAMP DISCONNECTED. RECONNECTED. OP CHECKS NORMALLY. SUSPECT CONNECTOR SNAGED ON CABIN SERVICE EQUIPMENT AND BECAME DISCONNECTED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007100500143 20071005 00143 NM 2007 10 5 UPS07M50750 1 20070724 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA C ABORTED TAKEOFF O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT BORE RT NR 11 FOUND WITH CORROSION. CORR AT BARREL NUT BO RE REMOVED PER SRM 51-21-01 VII R38. BORE BOTTOM REMN BLEND OUT DEPTH 0.020" DEEP. BORE REAMED TO 0.988" DIA & REMN BL END OUT DEPTH 0.030" DEEP, EXCEEDS LIMITS. BARREL NUT BORE BLEND OUT VOIDS, BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTE D. SLEEVE BUSHING FAB, PROTECTED & INSTLALL. REPAIR C/O AT BARREL NUT BORE NR 11 RT ACCEPTABLE PER EN 1467-07. 2 L 7 3 4F RT A22WE 2007100500144 20071005 00144 NM 2007 10 5 UPS07M50751 1 20070729 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZONTAL CONSTANT SECTION BARREL NUT BORE RT NR 1 FOUND WITH CORROSION. CORR AT BARREL NUT BORE REM OVED PER SRM 51-21-01 VII R38. BORE BOTTOM SURFACE CLEANED. BORE REAMED TO 1.549" DIA, REMN BLEND OUT 0.100" DEEP EXCE ED LIMITS. BARREL NUT BORE REAMED FURTHER TO 1.594" DIA. BARREL NUT BORE, BLEND OUT VOIDS & BOTTOM PER. RADIUS SMOOTH EN & PROTECTED. SLEEVE BUSHING FAB, PROTECTED & INSTALL. REPAIR C/O IS ACCEPTABLE PER EN 1480-07. 2 L 7 3 4F RT A22WE 2007100500145 20071005 00145 NM 2007 10 5 UPS07M50752 1 20070729 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT HOLE LT NR 36 FOUND WITH CORROSION. CORR AT BARREL NUT BO RE REMOVED PER SRM 51-21-01 VII R38. BORE BOTTOM REMN BLEND OUT 0.280" DEEP. BORE REAMED TO 2.538" DIA, REMN BLEND OUT 0.100 " DEEP, EXCEEDS LIMITS. BARREL NUT BORE, BLEND OUT VOIDS, BOTTOM PERIPHERY SMOOTHEN & PROTECTED. SLEEVE BUSHING FAB, PROTECTED & INSTALL. REPAIR DOUBLER, TAPER FILLERS FAB & INSTALL. REPAIR IS ACCEPTABLE PER EN 1472-07. 2 L 7 3 4F RT A22WE 2007100500146 20071005 00146 NM 2007 10 5 UPS07M50753 1 20070801 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT BORE LEFT NR 5 FOUND WITH CORROSION. CORROSION AT BARREL NUT BORE REMVD PER SRM 51-21-01 VII R38. BOTTOM REMN BLEND OUT 0.025" DEEP. BORE REAMED TO 0.988" DIA, REMN BLEND OUT 0.015" DEEP, EXCEEDS LIMITS. BARREL NUT BORE, BLEND OUT VOIDS, BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. SLEEVE B USHING FAB, PROTECTED & INSTALLED. REPAIR C/O AT BARREL NUT BORE 05 LEFT ACCEPTABLE PER EN 1496-07. 2 L 7 3 4F RT A22WE 2007100500147 20071005 00147 NM 2007 10 5 UPS07M50754 1 20070801 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT BORE RIGHT NR 32 FOUND WITH CORROSION. CORROSION AT BARRE L NUT BORE REMOVED PER SRM 51-21-01 VII R38. BOTTOM BORED THRU, BORE REAMED TO 1.178" DIA. REMN BLEND OUT 0.020" DEEP, EXCEEDS LIMITS. BARREL NUT BORE, BLEND OUT VOIDS SMOOTHEN & PROTECTED. BUCKET BUSHING FABBED, PROTECTED & INSTALLED. REPAIR C/O AT BARREL NUT BORE NR 32 RIGHT IS ACCEPTABLE PER EN 1489-07. 2 L 7 3 4F RT A22WE 2007100500150 20071005 00150 NE 2007 10 5 2007UALA03974 2 20070929 A 7230 STATOR VANE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COMPRESSOR LACK OF LUBE A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 823UA 952 V11298 ABORTED TAKEOFF DUE TO NR 2 ENGINE COMPRESSOR STALL. *S/D* ACP POWER ASSURANCE, ACCEL AND DECEL CHECKS, ACCOMPLISHED P OWER ASSURANCE RUNS, ALL PARAMETERS NORMAL, ACCEL 6 SECONDS, DECEL 3 SECONDS, ALL NORMAL NO MESSAGES. ACCOMPLISHED CHEC K INSP OF VSV, LUBRICATION OF HP COMPRESSOR VSV RAN ENG ALL PARAMETERS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007100500151 20071005 00151 NM 2007 10 5 2007UALA03976 1 20070929 A 5230 ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 AFT CARGO DOOR S/N 1607 LOWER DOOR STOP FITTING BEAM, OUTBOARD TEE ANGLE IS CRACKED IN RADIUS AT MOST FORWARD END. MAJO R REPAIR ACCOMPLISHED: REMOVED & REPLACED LWR -T- CHORD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007100500153 20071005 00153 NM 2007 10 5 2007UALA03978 1 20071001 A 4900 BATTERY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 781UA 26945 APU BATTERY FAILURE. 10-26-07 REPLACED APU BATTERY & APU BATTERY CHARGER, SYSTEM OP CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007100500154 20071005 00154 EU 2007 10 5 2007UALA03979 1 20070929 A 2697 RAI2800M0706 CIRCUIT BREAKER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SMOKE DETECTOR FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 430UA 568 CARGO SMOKE TEST FAILED - ONLY WENT THRU CYCLE ONCE. *S/D* T18 SDCU CH2 SYSTEM FAIL. RESET T18 SDCU CH2 MODULE AND C6 SDCU CH1. TEST NORMAL AFTER. 2 L 7 2 4F 4 F RT A28NM E40NE 2007100500157 20071005 00157 NM 2007 10 5 2007UALA03982 1 20070929 A 7160 LINER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR1 ENG FAN CASE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 817UA 873 FOUND HOLE INSIDE NR 1 ENGINE COWL ON WALK AROUND, UNDER ENG BLADE, APPROX 2 INCHES LONG AND 1 INCH WIDE. HOLE IS AT 6 O'CLOCK POS. MEASURES APPROX .75 INCH DIA. *S/D* REPAIRED NR 1 ENG FAN CASE ATTRITION LINER, CURED FOR 3 HOURS WITH H EAT LAMP. 2 L 7 2 4F 4 F RT A28NM E40NE 2007100500158 20071005 00158 NM 2007 10 5 2007UALA03850 1 20070922 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EEL INOP AT LAV 104 SIDEWALL AND SIDEWALL XAISLE BETWEEN DOORS 2L AND 2R. 10-19-07 EEL LIGHTS IN ALL POSITIONS COM E ON AFTER REPLACEMENT OF BATTERY-POWER SUPPLY. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007100500159 20071005 00159 NM 2007 10 5 2007UALA03851 1 20070922 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 DOOR 2L SIDEWALL EXIT SIGN INOP. 10-19-07 EXIT SIGN COMES ON AFTER REPLACEMENT OF BATTERY UNIT. OP CHECKS NORMAL LY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007100500160 20071005 00160 NM 2007 10 5 2007UALA03852 1 20070922 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EEL AT DOOR 1L SIDEWALL INOP. 10-19-07 RELAMPED. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007100500162 20071005 00162 NM 2007 10 5 2007UALA03854 1 20070921 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 503UA 24624 LEFT OVERWING EMERGENCY LIGHT IS INOP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007100500167 20071005 00167 NM 2007 10 5 2007UALA03859 1 20070922 A 2710 AILERON BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE STICKS A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 665UA 29237 AILERON STICKS WHILE INFLIGHT AND HESITATES WHEN CHECKED ON GROUND AFTER LAG. 10-19-07 REPLACED LEFT LATERAL CONTR OL ACTUATOR TORQUE TUBE REF MM 27-11-16. AILERON OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007100500169 20071005 00169 NM 2007 10 5 SB07083 1 20070926 A 3350 20131ASMI BATTERY PACK BOEING 737 7373B7 1384580 NM EMERGENCY LIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 515AU 23701 BFM - MAINTENANCE REPORTED THE EMERGENCY EXIT SIGNS AT THE LEFT-HAND AND RIGHT-HAND FORWARD DOORS INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE BATTERY PACK PER MM 33-51-51. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007100500170 20071005 00170 NM 2007 10 5 SB07084 1 20070928 A 3397 LIGHT BOEING 737 7373B7 1384580 NM CABIN NONE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 526AU 23861 DFW - MAINTENANCE REPORTED THE FLOOR EMERGENCY ESCAPE PATH LIGHTING AT SEAT ROWS 9 AND 11, LEFT-HAND SIDE, INOPERATIVE. MAINTENANCE FOUND THAT THIS IS A NORMAL SITUATION. THESE LIGHTS ARE NOT OPERATIONAL PER MM 33-51-12-0, SECTION 3, PARAGR APH A, SENTENCE 4. 2 L 7 2 4F RT A16WE 2007100500171 20071005 00171 EU 2007 10 5 YENA2007084 1 20070928 A 3150 WARNING MESSAGE THALES AIRBUS 320 A320232 3930326 EU NR 2 ELAC ILLUMINATED A YENA O OTHER J WARNING INDICATION CR CRUISE 1 EA 15 521JB 11141 35 VB014267 1452 DURING CRUISE AT 370 AT .77 MACH AIRCRAFT ABRUPTLY PITCH DOWN THEN RETURNED TO LEVEL FLIGHT. FOLLOWED BY F/CTRL ELAC 2 PITCH FAULT. COMPLETED ECAM, NO FURTHER ACTION NEEDED. REMOVED AND REPLACED ELAC NR 2 IAW AMM 27-93-34-04, OPS CHECK G OOD. 2 L 7 2 4F RT A28NM 2007100500172 20071005 00172 NM 2007 10 5 UPS07550759 1 20070908 A 5511 182N20018 SPAR BOEING 757 75724APF 1384969 NM HORIZONTAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 403UP 23725 INSPECTION TYPE:C FWD SPAR WEB I/B OF RIB 9 FS STA 208 CRACKED. REPAIRED PER UPS EO 757-55-20032 AND GOODRICH EA 07-339 6. 2 L 7 2 4F RT A2NM 2007100500174 20071005 00174 NM 2007 10 5 UPS07650779 1 20070920 A 5340 STRINGER CLIP BOEING 767 76734AF 1385212 NM BS 654 S7L BENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 328UP 27754 INSPECTION TYPE:C1 BENT STRINGER CLIP. REMOVED, FABRICATED, AND INSTALLED PER SRM 51-40-02 AND DRAWING 143T1126. 2 L 7 2 4F RT A1NM 2007100500176 20071005 00176 WP 2007 10 5 UPS07850760 1 20070920 A 5320 FITTING DOUG DC8 DC873F 302199F WP FS 1180 L17R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 FITTING CRACKED AT STA 1180 L17R FWD SIDE. REMOVED, FABRICATED AND INSTALLED REPAIR END FITTING AT S TA 1180 L17R IAW DWG 4750419, AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 2007100500177 20071005 00177 WP 2007 10 5 UPS07850761 1 20070920 A 5320 FITTING DOUG DC8 DC873F 302199F WP FS 1200 L17R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 FITTING CRACKED AT STA 1200 L17R AFT SIDE. REMOVED, FABRICATED, AND INSTALLED REPAIR FITTING AT STA 1200 L17R IAW DWG 4750419, AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 2007100500178 20071005 00178 WP 2007 10 5 UPS07850762 1 20070920 A 5310 FITTING DOUG DC8 DC873F 302199F WP FS 1260 L19R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 FITTING CRACKED AT STA 1260 L19R FWD SIDE. REMOVED, FABRICATED AND INSTALLED REPAIR FITTING AT STA 1 260 L19R IAW DWG 4750419, AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 2007100500179 20071005 00179 EA 2007 10 5 TRAX200701389 1 20070924 A 5340 FITTING CNDAIR CL600 CL6002B19 1900309 EA FLOORBEAM CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 855AS 7395 FITTING OF PRESSURE FLOORBEAM AT FS AND RBL 9 CRACK. 10-9-07 FITTING OF PRESSURE FLOORBEAM AT FS 461 RBL 9 REPLACED I AW SRM 51-42-21 2 L 7 2 4F RT A21EA 2007100500182 20071005 00182 EU 2007 10 5 2007UALA03985 1 20070930 A 3397 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EPSU DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 448UA 842 EPSU INT LOAD EMER L. *S/D* DIRTY CONNECTOR AT 13A POWER SUPPLY. CLEANED POWER SUPPLY CONNECTOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007100500183 20071005 00183 NM 2007 10 5 2007UALA03986 1 20070930 A 2497 TERMINAL BLOCK BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU ELECTRICAL BURNED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 925UA 26646 BURNING ELECTRICAL ODOR IN CABIN. REPLACED TERMINAL BLOCK AND TERMINALS. REPLACED RELAY R350. 2 L 7 2 4F 4 F RT A16WE E21EU 2007100500184 20071005 00184 NM 2007 10 5 2007UALA03987 1 20070930 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 967 STR 2L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 STRINGER ATTACH CLIP CRACKED AT BS 967 STR 2L. MAJOR REPAIR ACCOMPLISHED: REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007100500188 20071005 00188 NM 2007 10 5 2007UALA03991 1 20070929 A 2612 FIRE LOOP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 585UA 26709 STATUS MSG R ENG FIRE LOOP 2. 2 L 7 2 4F 4 F RT A2NM E17NE 2007100500195 20071005 00195 NM 2007 10 5 SWAA074846 1 20070927 A 5330 6545765 SKIN BOEING 737 7373Q8 1384670 NM BS 513 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 513, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007100500196 20071005 00196 NM 2007 10 5 SWAA074835 1 20070927 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM BS 386 S17R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 386, STR 17R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007100500197 20071005 00197 NM 2007 10 5 SWAA074845 1 20070927 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM BS 750 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007100500198 20071005 00198 NM 2007 10 5 SWAA074836 1 20070927 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 978 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 978, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007100500200 20071005 00200 NM 2007 10 5 SWAA074852 1 20070927 A 5210 6545871 FRAME BOEING 737 7377H4 1384404 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 753SW 29848 DURING SCHEDULED 8Y CHECK, FOUND R1 DOOR FWD LOWER STUB FRAME CRACKED AT STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007100900001 20071009 00001 NM 2007 10 9 F3LA200700254 1 20070923 A 5320 D5391550320001 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT FASTENER HOLES UNDER FLOOR SUPPORT FROM STR 38L TO STR 38R C ORRODED. REMOVED AND REPLACED SUPPORT PLATE IAW SRMS 51-42-11 AND 51-72-11. 2 L 7 2 4F RT A28NM 2007100900002 20071009 00002 NM 2007 10 9 F3LA200700252 1 20070925 A 5320 D5347112320300 SUPPORT ANGLE AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED SHEAR PLATE SUPPORT AT -Y1292 BETWEEN FR69 TO FR70 CORRODED. REMOVED AND REPLACED SHEAR PLATE SUPPORT IAW AIRBUS DRAWINGS D53474180 AND D53471123, AND SRM 51-42-11, PARA 6B AND 7B. 2 L 7 2 4F RT A28NM 2007100900003 20071009 00003 NM 2007 10 9 F3LA200700253 1 20070923 A 5320 D53916354200 PLATE AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED LT FWD CARGO COMPARTMENT UNDER FLOOR TRANSITION PANEL SUPPORT HAD CORRODED FASTENE R HOLE FROM FR 25 TO FR 30. REMOVED AND REPLACED SUPPORT PLATE IAW SRM 51-42-11, PAGE 7-9, SEC A-C. 2 L 7 2 4F RT A28NM 2007100900004 20071009 00004 NM 2007 10 9 C1HA200786001 1 20071001 A 5315 FLOORBEAM BOEING 727 7272S7 138407Z NM BS 1110 CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 686CA 22021 BS 1110 FLOORBEAM CORROSION LBL 45 - RBL 45 TOP SURFACE UPPER CHORD. REPAIR BS 1110 FLOORBEAM IAW B727 SRM 53-10-8 FIG 3. 2 L 7 3 4F A3WE 2007100900006 20071009 00006 NM 2007 10 9 C1HA200786003 1 20071001 A 5315 FLOORBEAM BOEING 727 7272S7 138407Z NM BS 344 CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 686CA 22021 NUMEROUS AREAS OF CORROSION ON FLOOR BEAM AT BS 344 LBL 25 - RBL 6. CUT OUT DAMAGED AREA. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW B727 SRM 53-10-8 FIG 9. 2 L 7 3 4F A3WE 2007100900007 20071009 00007 NM 2007 10 9 C1HA200786004 1 20071001 A 5347 1509100612 SEAT TRACK BOEING 727 7272S7 138407Z NM BS 1033 CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 686CA 22021 CORROSION ON TRACK ANGLE AT BS 1033 LBL 54.5. REMOVED EXISTING PART, FABRICATED NEW PART; TREATED AND PRIMED AND INSTAL LED NEW PART IAW B727 SRM 51-30-2 FIG 1 AND 13. 2 L 7 3 4F A3WE 2007100400017 20071004 00017 NM 2007 10 4 DLM90071251 1 20070918 A 5347 SR095300853 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 1260-1364 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 29537 53388 CABIN SEAT TRACK CORRODED BEYOND LIMITS AT LBL24 STA 1260 - 1364. REPLACED SEAT TRACK SECTION IAW MD90 SRM VII 51-30-01 VOL 1. 2 L 7 2 4F RT A6WE 2007100400036 20071004 00036 WP 2007 10 4 AALA20071828 1 20070928 A 1100 83700331 PLACARD DOUG DC9 DC982 3022082 WP SLIDE TORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 413AA 49324 LGA - AFT EMERGENCY EXIT SLIDE HAD TORN DECAL. REPLACED DECAL FOR AFT EMERGENCY EXIT SLIDE. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F A6WE 2007100400039 20071004 00039 NE 2007 10 4 AALA20071827 2 20070928 A 7200 ENGINE BOEING 767 767323 1385205 NM GE CF6 CF680C2B6 30025 NE RIGHT VIBRATION A AALA A UNSCHED LANDING E N VIBRATION/BUFFET FALSE WARNING CL CLIMB 1 SW 21 373AA 25200 690374 LAX INFLIGHT T297/28SEP - CREW REPORTED NUMBER TWO ENGINE N2 VIBRATION INDICATING 3.7 ON CLIMB. NUMBER TWO ENGINE FIRE LOOP ONE ILLUMINATED FIVE TO TEN MINUTES THEN EXTINGUISHED. LANDED LAX WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE ON 30 SEP 2007 AT LAX DUE TO HIGH N2 VIBRATION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A1NM E13NE 2007100400046 20071004 00046 NM 2007 10 4 DLM90071259 1 20070924 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 541 L18R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 CORROSION AT STA 544 AT LONGERON 18R ON LWR SIDE OF WEB. CUSP WEB REPLACED ON W/O 1002987-2400-0227, DL63329. 2 L 7 2 4F RT A6WE 2007100400047 20071004 00047 NM 2007 10 4 DL76G071260 1 20070925 A 5315 AND101331002 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 654 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 156DL 25354 FLOORBEAM FOUND CORRODED. REMOVED AND REPLACED FLOORBEAM UPPER CHORD PER SRM 53-51D. 2 L 7 2 4F RT A1NM 2007100400051 20071004 00051 NM 2007 10 4 DLM90071264 1 20070925 A 2497 WIRE DOUG MD90 MD9030 3023690 NM FWD RELAY PANEL BURNED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 903DA 53383 A/C RETURNED TO GATE, FLT ATTENDANTS REPORTED STRONG ELECTRICAL ODOR IN F/C AREA. FOUND APU RELAY B9-607 WITH HEAT DAMA GE. SPLICED 12 INCHES NEW WIRE-RETERMINATED TERMINALS A2-B2-C2. REPLACED APU RELAY, BASE AND ELECTRICAL BUS TIE. ALL OPS NORMAL. 2 L 7 2 4F RT A6WE 2007100400056 20071004 00056 NM 2007 10 4 QXEA200701501 1 20071001 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 403QX 4037 SEA - ON FLIGHT 2395, DEICE PRESSURE ILLUMINATED IN FLIGHT. RAN CHECKLIST NR 1 OUTERMOST BOOT FAILS TO ILLUMINATE. MAI NTENANCE COMPLIED WITH FUNCTIONAL TEST OF THE A/F PNEUMATIC DEICE SYSTEM THRU 20 CYCLES. OPERATIONAL CHECK GOOD. AIRCR AFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007100400065 20071004 00065 NM 2007 10 4 DLM90071269 1 20070925 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 503 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 SEAT TRACK AT LBL54 STA 503 IS CORRODED OUT OF LIMITS. REPAIRED IAW SRM 53-40-01 VOL 1 FIG 6. 2 L 7 2 4F RT A6WE 2007100400066 20071004 00066 NM 2007 10 4 DLM90071270 1 20070926 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 1360 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 AFT CABIN LBL 44 SEAT TRACK I/B FLANGE IS EXFOLIATED AT FS 1360. REPAIRED SEAT TRACK LBL 44 IAW MD-90 SRM 53-40-FIG 6 O N N/R 63297 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007100400067 20071004 00067 NM 2007 10 4 DL76L071271 1 20070927 A 2750 285T004953 FCU BOEING 767 767332 1382001 NM TE FLAPS MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 176DN 25061 STATUS MSG, FLAP/SLAT ELECTRIC DISPLAYED. REMOVED AND REPLACED FSEU PER MM. BITE CHK OK. RAN FLAPS ALL OK. POWER TRA NSFERRED, ALL OK. 2 L 7 2 4F RT A1NM 2007100400070 20071004 00070 WP 2007 10 4 AALA20071806 1 20070925 A 3222 SCHRADER VALVE DOUG DC9 DC982 3022082 WP NLG STRUT INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7544A 53026 DFW INFLIGHT T744/25SEP - NOSE GEAR WOULD NOT RETRACT. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED SCHRADER VALVE AND ACCOMPLISHED NOSE GEAR STRUT SERVICING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007100400084 20071004 00084 EA 2007 10 4 A6WA200740497 1 20070904 A 5320 600332833 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 425AW 7663 EXTERNAL POWER RECEPTACLE SUPPORT BRACKET, P/N 600-33283-33, IS CRACKED AT RECEPTACLE FORWARD OUTBOARD ATTACH MEDT BOLT HOLE. CRACK IS APPROX .5 INCHES LONG. SUP - MAINTENANCE REMOVED AND INSTALLED SERVICEABLE SUPPORT BRACKET P/N 600-3328 3-33 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007100400095 20071004 00095 EU 2007 10 4 07FDEA04155 1 20070921 A 5320 A53778338 PLATE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORRODED SHEAR PLATES AT FOLLOWING AREAS: BETWEEN FRAME 32-33 RT, 33-34 RT, 32- 33 LT AND 33-34 LT. REPLACEMENT OF SHEA R PLATES IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100400101 20071004 00101 EU 2007 10 4 07FDEA04257 1 20070924 A 5522 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 300 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 RT ELEVATOR FRONT SPAR, UPPER AND LOWER SKIN DELAMINATED AND GLASS FIBER PLY DEBONDED. REPAIR PERFORMED BY INSTALLING H I-LOKS IN DELAMINATED SKIN NEAR LIGHTNING HOLE, FILLING EDGES WITH RESIN, BOND GLASS FIBER WITH RESIN, LEAVE DELAMINATIO N AT UPPER AND LOWER SKIN AS IS, FILLING EDGES AND COUNTERSINK AREA OF PUSHED FASTENERS WITH RESIN IAW TD-FX-A-DAOR-1485 /2005 ISSUE A, EA 6-5521-92142 AND RAS/CASA/4331/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100400103 20071004 00103 EU 2007 10 4 07FDEA04259 1 20070924 A 5313 A53612214200 LONGERON AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 HEAVY CORROSION ON LONGERON BETWEEN FRAME 11-14, Y 730, FLOOR STRUCTURE SECTION 12. REPLACEMENT OF LONGERON IAW SRM 5 1-72-10. 2 L 7 2 4F RT A35EU 2007100400126 20071004 00126 EU 2007 10 4 07FDEA04181 1 20070921 A 5310 A53980022209 FAILSAFE AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FOUND MISDRILLED FASTENER HOLES AT FRAME-FAIL-SAFE-RING, FUSELAGE SKIN BETWEEN FRAME 73-76, STRG 26-27 RHS. REPAIR PERF ORMED BY OVERSIZING HOLES AND INSTALLATION HL13VF8 (DAN8-8) FASTENERS IAW EA 6-5318-82891 AND RAS/DAHAM/4019615/2005 ISS UE A. 2 L 7 2 4F RT A35EU 2007100400130 20071004 00130 EU 2007 10 4 07FDEA04353 1 20070928 A 5753 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 EXISTING EXTERNAL REPAIR DOUBLER ON NOSE SKIN OF OUTBOARD RT FLAP, RIB 10.5 (PANAM EA X3157J518). PERMANENT REPAIR WA S CARRIED OUT ON 25-APR-1994 BY REPLACING THE INSTALLED DOUBLER WITH A 1,8MM THICK ONE AND THE EXISTING FASTENERS WI TH BLIND RIVETS CR3552-P6 TO ELIMINATE KNIFE EDGES. FOUND NO RAS FOR THIS REPAIR. REPLACEMENT OF NOSE-RIB 10.5. REPAI R PATCH RENEWED AND RE-INSTALLED WITH CR3552- P6 FASTENERS IAW RAS/DABRE/7005095/2005 FOR TRACKING HAS BEEN WRITTEN EA 6 -5753-82850. 2 L 7 2 4F RT A35EU 2007100400132 20071004 00132 EU 2007 10 4 07FDEA04291 1 20070926 A 5330 A53810189 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 FOUND HEAVY CORROSION ON SKIN PANEL BETWEEN FRAME 39-40, STGR 28-33 RT. REPAIR PERFORMED BY BLEND OUT CORROSION IAW TD 942.038560/011/2005 ISSUE A AND TD 942.038560/047/2005 ISSUE A. CONTAINING ALL IN EA 6-5314-82934, APPROVED BY RAS/AS/0 153/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100400134 20071004 00134 EU 2007 10 4 07FDEA04293 1 20070926 A 5311 A53970890 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 GOUGES ON INNER FLANGE OF FRAME 55, STGR 15 LT AND RT, AFT OF EMERGENCY EXIT DOOR TORSION BOX, CAUSED BY INCORRECT EQUIP MENT FASTENER INSTALLATION. REPAIR PERFORMED BY SMOOTH BLEND OUT, COVERED BY EA 6-5316-92163, APPROVED BY RAS/DATLS/000 2690/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100400162 20071004 00162 EU 2007 10 4 07FDEA04187 1 20070921 A 5740 A57150234201 FITTING AIRBUS 310 A310324 3930206 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 AREAS OF IMPACT DAMAGE FOUND ON THE AFT FACE OF THE OUTBOARD LUG ON THE RT WING PYLON MOUNTING (ATTACH FITTING), RIB 8-9 . REPAIR PERFORMED BY BLENDING DAMAGE TO REMOVE ALL SHARP EDGES, HFEC INSPECTION AND INSTALLING NEW SELF-LUBRICATING BE ARING IAW EA 6-5720-82880 AND RAS/BAE/1000883/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100400163 20071004 00163 EU 2007 10 4 07FDEA04364 1 20070928 A 5730 A57243205201 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND ON OLD NOSE SKIN REPAIR IAW SRM 57-41-12/FIG 203, 204, CHAFING MARKS BETWEEN SLAT TRACK 5 AND SLAT TRACK 6, LEAD ING EDGE SKIN, RT WING. NEW REPAIR SKIN INSERT INSTALLED IAW SRM 57-41-12/FIG 203, 204. 2 L 7 2 4F RT A35EU 2007100400201 20071004 00201 NM 2007 10 4 07FDEA04305 1 20070926 A 5311 65C158121 FRAME BOEING 727 727227 1384078 NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 NR 2 ENG INLET DUCT HOUSING, FRAME IS CRACKED, LOCATED AT BS 1233 AND LT SIDE OF VERTICAL STAB FWD SPAR FWD AND AFT SIDE OF FRAME CRACKED REMOVED DAMAGE BY CUTTING FRAME AND FRAME ANGLE. FABRICATED REPLACEMENT SECTION OF FRAME AND FRAME ANGLE, FRAME REPAIR ANGLE, FRAME ANGLE REPAIRS AND FILLERS AND INSTALLED ABOVE PARTS. REF BOEING DOCUMENT NR 65C 15812 AND SRM 51-40-3/ FIGURE NR 1/PAGES 1-6. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007100500011 20071005 00011 EU 2007 10 5 07FDEA04403 1 20071001 A 5340 A53973609202 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND MISDRILLED HOLES IN CORNER FITTING C59, P 44 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100500022 20071005 00022 EU 2007 10 5 07FDEA04414 1 20071001 A 5313 A53974203230 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION AT STRINGER P57 C 66. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007100500039 20071005 00039 EU 2007 10 5 07FDEA04433 1 20071001 A 7120 A54611155500 MOUNT AIRBUS 310 A310322 3930334 EU ENGINE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 NR 2 PYLON TO ENGINE FWD MOUNT PLATE, AFT INBD HOLE GOUGED. BLENDED AREA IAW A310-200 SRM 54-51-81. HOLE SIZE IS .842 WITHIN LIMITS IAW A310-200 SRM 54-51-81. CADMIUM PLATED IAW A310-200 SRM 51-21-10. ADHESION TEST PASSED IAW FEDEX A310 -200 SRM 51-21-10. 2 L 7 2 4F RT A35EU 2007100500043 20071005 00043 EA 2007 10 5 A6WA200740530 1 20070824 A 5753 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT TE FLAP DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 467AW 7900 LEFT INBOARD FLAP LOWER SKIN DENTED APPROX 2 INCHES DIAMETER BY .083 INCH DEEP, 1.5 INCH FROM TRAILING EDGE OF FLAP, 1 I NCH FROM INBOARD EDGE OF FLAP, FLAP P/N 601R14002-1, S/N SB/RJ/937. MAINTENANCE REPAIRED FLAP LOWER SKIN USING EXTERNAL DOUBLER IAW CRJ 200 SRM 57-52-00 REPAIR NR 3. (M) 2 L 7 2 4F RT A21EA 2007100500048 20071005 00048 EA 2007 10 5 A6WA200740529 1 20070818 A 5320 6013501252 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FS 625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 467AW 7900 RIGHT OBLIQUE ANGLE IS CRACKED .75 INCH IN RADIUS AT FS 625, WL 100. MAINTENANCE REMOVED AND INSTALLED SERVICEABLE INTE RCOSTAL, P/N 601-35012-52 IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007100500053 20071005 00053 EU 2007 10 5 07FDEA04368 1 20070928 A 5320 A53610607207 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 CORROSION ON UPPER RUN OUT FITTING BETWEEN FRAME 16A-17, STRG 44 RT, AFTER REWORK NO REMAINING THICKNESS WAS EXISTED. REPLACEMENT OF UPPER RUN OUT FITTING IAW. REPAIR DRW R536-10440 ISSUE C. 2 L 7 2 4F RT A35EU 2007100500064 20071005 00064 EU 2007 10 5 07FDEA04442 1 20071002 A 5720 A57111092202 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND AT C47 INTERNAL CENTER WING LT VERTICAL FLANGE HOLE NR G, NR S AND NR T WITH CORROSION. REPAIR PERFORMED BY OVERS IZING THE HOLES UNTIL CORROSION REMOVAL IAW EA 6-5710-106533 AND RAS 052780/019/2007 ISS A. 2 L 7 2 4F RT A35EU 2007100500078 20071005 00078 EU 2007 10 5 07FDEA04264 1 20070925 A 5320 A53778338 PLATE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 CRACKED SHEARPLATES BETWEEN FRAME 38-38.1, STRG 44 RT AND BETWEEN FRAME 38.1- 38.2, STRG 44 LT, FWD CARGO COMPARTMENT. REPAIR PERFORMED BY REPLACEMENT OF BOTH SHEAR PLATES IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100500081 20071005 00081 NM 2007 10 5 07FDEA04269 1 20070925 A 5410 691447614 ANGLE BOEING 727 727227 1384078 NM NR 2 INLET CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 NR 2 ENG INLET DUCT HOUSING FRAME-TO-LEADING EDGE OF VERTICAL STAB ATTACH CLIP ON RT SIDE IS CRACKED LOCATED AT STA 1233 REMOVED CRACKED ATTACH CLIP, FABRICATED NEW CLIP AND INSTALLED. REF BOEING DOCUMENT NR 69-14476/ID NR 0001/ITEM NR 14/ FRAME 1 OF 2 AND SRM 51-30-2. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007100500084 20071005 00084 2007 10 5 2007UALA03948 4 20070927 A 3442 TRANSCEIVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE WX RADAR SYS FAILED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 472UA 1435 PREDICTIVE WINDSHEAR FAILED AGAIN. COULD NOT DUPLICATE ON GROUND, TESTED WINDSHEAR/AFS AND RAN CAT III TEST, ALL GOOD. REPLACED THE WEATHER RADAR TR AS PRECUATIONARY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007100500091 20071005 00091 NM 2007 10 5 2007UALA03835 1 20070922 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 FWD GALLEY DOOR AFT FRAME CRACKED AT OUTBOARD LWR HOLE FOR LOWER STOP FITTING. STOP DRILLED CRACK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007100500115 20071005 00115 EU 2007 10 5 2007UALA03971 1 20070928 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 414UA 472 CREW 02 SYSTEM NEEDS SERVICING. *S/D* SERVICED CREW O2 SYSTEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007100500118 20071005 00118 EU 2007 10 5 UPS07150797 1 20070920 A 5330 SKIN AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 149UP 0832 INSPECTION TYPE:2C LEFT LOWER HALF FR10 EXTERIOR FUSELAGE AT STR 31 IS DENTED. PERFORMED HFEC TO THE DAMAGED SKIN REF A IRBUS NTM 51-10-08 AND PERFORMED DETAILED VISUAL INSPECTION OF THE INTERNAL STRUCTURE TO ENSURE NO CRACKS REF AIRBUS NTM 51-70-00 IAW SAA EA 300-5330-01-A1135 AND UPS EO A300-5330-27788-A 2 L 7 2 4F RT A35EU 2007100500142 20071005 00142 NM 2007 10 5 UPS07M50749 1 20070719 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA C ABORTED TAKEOFF O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT BORE LT NR 27 FOUND WITH CORROSION. CORR REPAIR BUCKET BU SHING REMOVED & BARREL NUT BORE SURFACE CLEANED. REMN BLEND OUT 0.020" DEEP, EXCEEDS EO LIMITS PER EO MD11-5510-19409-L . BORE SIZE 1.180" DIA. BARREL NUT BORE, BLEND OUT PERIPHERY SMOOTHEN & PROTECTED. BUCKET BUSHING FAB & PROTECTED. BU CKET BUSHING INSTALL. REPAIR C/O AT BARREL NUT BORE NR 27 LT, ACCEPTABLE PER EN 1456-07. 2 L 7 3 4F RT A22WE 2007100500148 20071005 00148 EA 2007 10 5 TRAX200701387 1 20070924 A 5210 BRACKET CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 BRACKET AFT OF ASD BOTTOM STEP IS CRACKED. 2 L 7 2 4F RT A21EA 2007100500155 20071005 00155 EU 2007 10 5 2007UALA03980 1 20070929 A 3150 WARNING LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ILLUMINATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 480UA 1555 ELEVATOR SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. *S/D* MOMENTARY TURBULENCE. REPLACED SEC 2 A AS PRECATIONARY - C OULD NOT DUPLICATE FAULT ON GROUND. 2 L 7 2 4F 4 F RT A28NM E40NE 2007100500161 20071005 00161 NM 2007 10 5 2007UALA03853 1 20070923 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INTERMITTENT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 SEATS 20 THRU 24AB EEL LIGHTS CYCLE ON AND OFF. 10-19-07 RESET SYSTEM. EEL OPERATES NORMALLY. UNABLE TO FIND FA ULT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007100500163 20071005 00163 NM 2007 10 5 2007UALA03855 1 20070921 A 3234 HANDLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MLG STUCK A UALA O OTHER O OTHER LD LANDING 1 WP 29 503UA 24624 GEAR HANDLE WOULD NOT RAISE AFTER TOUCH & GO LANDING. WHEN SPOILER HANDLE WAS LOWERED ON LANDING ROLL THE AIRCRAFT ROLL ED RIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007100500164 20071005 00164 2007 10 5 2007UALA03856 4 20070921 A 2565 STRAP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR SLIDE OUT OF POSITION A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 580UA 26698 DOOR 1L SLIDE-RAFT STRAP WITH 'D' RING IS NOT VISIBLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007100500168 20071005 00168 NE 2007 10 5 2007UALA03860 2 20070921 A 7261 OIL SYSTEM BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 1 ENGINE OVERTEMP A UALA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 WP 29 220UA 30223 222097 NR 1 ENGINE HIGH OIL TEMPERATURE. 10-19-07 REPLACED SERVO FUEL HEAT EXCHANGER. ACCOMPLISHED PACK BURN AND FIM 71 -08 TASK 821 AFTER REPLACEMENT. NO ODOR IN CABIN. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007100500180 20071005 00180 NM 2007 10 5 2007UALA03983 1 20070929 A 5340 ATTACH FITTING AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE DOOR SLIDE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 850UA 1653 FWD LEFT MED SLIDE FWD LOWER ATTACH FITTING BROKE. REPLACED FWD LEFT SLIDE ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007100500186 20071005 00186 2007 10 5 2007UALA03989 4 20071001 A 2565 PROXIMITY SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR SLIDE FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 553UA 25277 DOOR 4L THE SLIDE ARM LIGHT WON'T COME ON. 2 L 7 2 4F 4 F RT A2NM E17NE 2007100500187 20071005 00187 NM 2007 10 5 2007UALA03990 1 20070929 A 3510 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FIRST OFFICER'S BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 584UA 26706 FIRST OFFICER'S O2 MASK BROKEN. 2 L 7 2 4F 4 F RT A2NM E17NE 2007100500189 20071005 00189 SO 2007 10 5 C2XA07RI086 1 20070925 A 3232 355022002MOD2 ELECTRONIC UNIT EMB 145 EMB145LR 3260212 SO MLG DOOR UNRELIABLE A C2XA O OTHER O OTHER AP APPROACH 1 SW 27 29917 15465 15465 145414 FLT 2296 - EWR - CREW REPORTED THAT NOSE GEAR DOORS OPENED UN-COMMANDED AT 3000 FT AND 210 KNOTS. EWR MX REMOVED AND RE PLACED LGEU IAW EMB145 AMM 32-32-01 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVIC E. 2 L 7 2 4T RT T00011AT 2007100900009 20071009 00009 EU 2007 10 9 07FDEA04271 1 20070925 A 5753 A57960306 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 LT AND RT CENTER FLAP CHAFING DAMAGE AT TOP SKIN AT RIB 15 AND 23 AFT OF T/E SKIN SPLICE. REPAIR PERFORMED BY SMOOTHLY BLEND THE DAMAGED AREAS WITHOUT INCREASING DEPTH IAW TD FOK/153/2005 ISSUE A, APPROVED BY EA 6-5753-92137 AND RAS/FOK/15 3/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100900010 20071009 00010 EU 2007 10 9 07FDEA04272 1 20070925 A 5753 A57960656 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 LT OUTER FLAP CHAFING DAMAGE AT TOP SKIN AT RIB 4 AND 15A AFT OF T/E SKIN SPLICE. REPAIR PERFORMED BY SMOOTHLY BLEND THE DAMAGED AREAS WITHOUT INCREASING DEPTH IAW TD FOK/154/2005 ISSUE A, APPROVED BY EA 6-5753-92138 AND RAS/FOK/154/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100900013 20071009 00013 NM 2007 10 9 NWAA073305810 1 20070928 A 3350 BATTERY BOEING 757 757351 1384991 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 590NW 32990 DURING OVERNIGHT CHECK, BATTERY TEST FOUND 4 BATTERIES NOT RUNNING LONGER THAN TEN MINUTES. MAINTENANCE REMOVED AND REP LACED 4 EMERGENCY BATTERIES. OPERATIONAL CHECK GOOD AND AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007100900015 20071009 00015 EU 2007 10 9 07FDEA04455 1 20071002 A 5340 A53610687236 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND FITTING AT C13-13A, P26 LT CORRODED REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100900016 20071009 00016 NM 2007 10 9 07FDEA04307 1 20070926 A 5720 6521655270 SUPPORT ANGLE BOEING 727 727227 1384078 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 RT WING ROOT UPPER TE COMPOSITE PANEL INBD SUPPORT ANGLES (2EA ) ARE CRACKED, WBL 70. REMOVED CRACKED ANGLES, REF SRM 5 1-30-2, DRILLED NEW ANGLES TO FIT, REF 51-10-1. INSTALL, REF 51-030-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2007100900017 20071009 00017 EU 2007 10 9 07FDEA04308 1 20070926 A 5750 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 OLD REPAIR ON RT OUTER FLAP TRAILING EDGE AT INBD SIDE, LOWER SKIN AND END RIB IN BAD CONDITION WITH SEVERAL DAMAGES. R EPAIR PERFORMED BY REPLACEMENT OF UPPER SKIN PANEL, RESTORING CONDITION OF TD FOK/010/2005 ISSUE A AND REPLACEMENT OF RI VETS IN LOWER SKIN PANEL IAW EA 6-5754-92167 AND RAS/FOK/010/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100900019 20071009 00019 EU 2007 10 9 07FDEA04310 1 20070926 A 5320 A53981113201 PLATE AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 CRACKED SHEAR PLATE BETWEEN FRAME 79-80, STGR 26 RT. REPLACEMENT OF SHEAR PLATE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100900020 20071009 00020 EU 2007 10 9 07FDEA04311 1 20070926 A 5320 A53973131200 PLATE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 DAMAGED SHEAR PLATE BETWEEN FRAME 69-70, STGR 40 RT. REPLACEMENT OF SHEAR PLATE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100900021 20071009 00021 EU 2007 10 9 07FDEA04312 1 20070926 A 5310 A53978378202 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 FOUND LOCK FASTENER HOLE WITH DIAMETER 6,26MM ON FRAME 54.2, BETWEEN STGR 34-35 LTS, IT'S IN THE PTOF AREA AND IN COLLIS ION WITH FRAME FOOT. REPAIR PERFORMED BY INSTALLING BUSHING RE0001-202 PER DRW RE0003-004 WITH NECESSARY LOCK FASTENER IAW ENG-STATEMENT. 2 L 7 2 4F RT A35EU 2007100900022 20071009 00022 EU 2007 10 9 07FDEA04313 1 20070926 A 5310 A53810967201 DIAPHRAGM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 FOUND TWO DENTS ON DIAPHRAGM BETWEEN TRACK 4-5 LT, FRAME 52-54. REPAIR PERFORMED BY SMOOTHLY REWORK AT DENT ONE, THE OT HER ONE IS REPAIRED BY DRILLING OUT THE SCRATCH (DIA 4MM) AND INSTALLING AN ALUMINUM RIVET IAW EA 6-5314-82929 AND RAS /AS/0166/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100900024 20071009 00024 WP 2007 10 9 07FDEA04315 1 20070926 A 5311 AFA00293 FRAME DOUG DC10 DC1010 3022110 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 DURING MODIFICATION MD10 ACF, FOUND CRACK 4,5" LONG ON THE FRAME AT STA 1761 TO NEXT STRG 13 LT SIDE. REPAIRED FOR SRM 53-30-00 FIG 5 VOL I. 2 L 7 3 4F A22WE 2007100900025 20071009 00025 WP 2007 10 9 07FDEA04316 1 20070926 A 5311 FRAME DOUG DC10 DC1010 3022110 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 DURING MODIFICATION MD10 ACF, FOUND ON FRAME AT STA 1741 TO NEXT STR 11 RT SIDE CRACK 4,5" LONG REPAIRED FOR SRM 53-30-0 0 FIG 5 VOL I. 2 L 7 3 4F A22WE 2007100900026 20071009 00026 NM 2007 10 9 QXEA200701486 1 20070926 A 3150 UNKNOWN DHAV DHC8 DHC8202 2809007 NM UNKNOWN A QXEA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 NM 09 349PH 486 PDX FLIGHT NR 2156 - MULTIPLE NO AIII WARNINGS ON CAT III APPROACH. PERFORMED INDEX COMPENSATION ADJUSTMENT FOR NR 1 A ND NR 2 FLUX VALVES, PERFORMED OPERATIONAL TEST IAW -8 200 TC 9340021, ALL CHECKS GOOD. PERFORMED OPERATIONAL TEST OF H GS RETURN TO SERVICE CAT III, ALL CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007100900031 20071009 00031 EU 2007 10 9 F3LA200700251 1 20070930 A 3350 AD321430 EPSU AIRBUS A318 A318111 3940019 EU EMERGENCY LIGHTS FAULTED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 805FR 1660 DURING A-CHECK, INSPECTION REPORTED EPSU (13WL) BATTERY FAULT. REPLACED EPSU BATTERY (13WL) IAW AMM 33-51-38-PB 401. O PS CHECKED GOOD. 2 L 7 2 4F RT 2007100900032 20071009 00032 WP 2007 10 9 07FDEA04317 1 20070926 A 5311 ABA72213 FRAME DOUG DC10 DC1010 3022110 WP BS 421 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 366FE 46602 DURING MODIFICATION MD10 ACF, FOUND IN AVIONIC COMPT, INTERNAL, STA 421 RT SIDE AT X=-77 ABOUT FRAME WITH CRACK 4,5" LO NG REPAIRED FOR SRM 53-30-00 FIG 5 VOL I. 2 L 7 3 4F A22WE 2007100900033 20071009 00033 NM 2007 10 9 07FDEA04374 1 20070929 A 5720 SUPPORT BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 596FE 48554 LEFT WING FIXED LEADING EDGE, XORS 542 (OUTBOARD OF ACCESS PANEL 518FB), LOWER LONGITUDINAL SUPPORT BRACKET FOUND CRAC KED. 10-16-07 CRACKED SUPPORT BRACKET AT LT WING FIXED LEADING EDGE XOS 542 (OUTBOARD OF ACCESS PANEL 518FB) LOWE R AREA REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007100900034 20071009 00034 EU 2007 10 9 07FDEA04318 1 20070824 A 5730 A5726000000151 SKIN AIRBUS 310 A310222 3930315 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 RT WING FRONT SPAR WITH CORROSION BETWEEN STA 482/RIB 8 AND STA 935/RIB 15. RT WING UPPER SKIN REPAIRED IAW FEDEX EA 6 -5710-113179. 2 L 7 2 4F RT A35EU 2007100900036 20071009 00036 EU 2007 10 9 07FDEA04116 1 20070920 A 5310 A52271028201 DOOR FRAME AIRBUS 310 A310203 3930313 EU ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT RT EMERGENCY EXIT DOOR FRAME SEGMENT 3.1. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100900037 20071009 00037 EU 2007 10 9 07FDEA04117 1 20070920 A 5320 A53973085208 SILL AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORROSION ON THE UPPER FLANGE AFT CARGO DOOR SILL BEAM BETWEEN FRAME 59-59A RT, OUT OF LIMIT. REPAIR PERFORMED BY BLEND OUT AND FLAP PEENING IAW EA 6-5317-82872 AND RAS/DATLS/0002588/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100900039 20071009 00039 EU 2007 10 9 07FDEA04119 1 20070920 A 5330 A53773676200 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 CORROSION ON SKIN INNER COUPLING PLATE AT C19, P53-54 REPAIR PERFORMED BY BLEND OUT UNTIL CORROSION REMOVAL IAW REA 6-53 13-70343 AND RAS/DABRE/700324/2003 ISS A. 2 L 7 2 4F RT A35EU 2007100900042 20071009 00042 NM 2007 10 9 07FDEA04376 1 20070929 A 5754 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 596FE 48554 LEFT WING INBOARD FLAP, INBOARD SEGMENT UPPER SKIN FOUND DENT MARKS. 10-9-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS MINOR PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007100900044 20071009 00044 NM 2007 10 9 07FDEA04378 1 20070929 A 5730 ACCESS PANEL DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 596FE 48554 RIGHT WING LEADING EDGE ACCESS PANEL 618GB INBOARD SUPPORT FOUND CRACKED. 10-16-07 RIGHT HAND WING LEADING EDGE AC CESS PANEL 618GB CRACKED INBOARD SUPPORT STIFFENER REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007100900046 20071009 00046 NM 2007 10 9 07FDEA04380 1 20070929 A 5310 6556992553 DOOR FRAME BOEING 727 727227 1384078 NM ZONE 800 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 CABIN AFT LT SERVICE DOOR, FWD FRAME HAS 2 WORN AREAS, CAUSED BY A DRILL BIT AND SCREW TOO LONG. LOCATED JUST INBD OF F WD UPPER TORQUE TUBE LATCH CRANK, AREA MARKED. INSTALLED NEW FRAME REF, SRM 51-30-2 PG 2. INSTALLED NEW SEAL REF MM 52 -12-011-4 PG 1. REINSTALLED AND ADJUSTED DOOR REF MM 52 14-000-4 PG1. OPS CHECKED GOOD, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007100900050 20071009 00050 NM 2007 10 9 AALA20071799 1 20070920 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 937AN 30082 TUL - EMERGENCY LIGHTS IN MID COACH CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN MID COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007100900052 20071009 00052 NM 2007 10 9 AALA0071801 1 20070920 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 937AN 30082 TUL - EMERGENCY LIGHTS IN FORWARD COACH CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FORWARD COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007100900054 20071009 00054 NM 2007 10 9 AALA20071803 1 20070921 A 3350 3149725 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 361AA 24042 ORD - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR HAD BROKEN LENS. REPLACED LENS FOR EXTERIOR EMERGENCY LIGHT AT L EFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007100900057 20071009 00057 EU 2007 10 9 07FDEA04122 1 20070920 A 5320 A53970875 SHIM AIRBUS 300 A300B4622 3930401 EU ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND SCRUB MARKS AT TORSIONS BOX EMERGENCY EXIT ON LT/RT CROSS SHIMS C56-57A, P15A-16. REPAIR PERFORMED BY REWORK TO S MOOTH CONTOUR IAW EA 6-5316-70333 AND RAS/DATLS/0001412/2003 ISS A. 2 L 7 2 4F RT A35EU 2007100900058 20071009 00058 EU 2007 10 9 07FDEA04123 1 20070920 A 5320 A53611676200 SPLICE AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND CORROSION OUT OF LIMIT AT SPLICE C19, P 50 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100900060 20071009 00060 EU 2007 10 9 07FDEA04125 1 20070920 A 5310 A53611673201 SPLICE AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND CORROSION OUT OF LIMIT AT SPLICE C19, P 54 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100900063 20071009 00063 EU 2007 10 9 07FDEA04329 1 20070927 A 5311 A53989300248 DOUBLER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 FOUND CORRODED DOUBLER AT FRAME 92, STGR 23 AD. REPLACEMENT OF DOUBLER IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100900064 20071009 00064 EU 2007 10 9 07FDEA04382 1 20070930 A 5320 A539733142000 SPLICE AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 AFT CARGO PIT AT FR 58 S-45L IS CORRODED REMOVED AND REPLACED CONNECTOR SPLICE P/N A5397331420000, IN AFT PIT AT FR 58 S TRINGER 45L, IAW A310 SRM 51-40-44, 51-40-21 AND TOP COATED IAW A310 SRM 51-23-10. 2 L 7 2 4F RT A35EU 2007100900065 20071009 00065 EU 2007 10 9 07FDEA04130 1 20070920 A 5230 A52370090208 SKIN AIRBUS 310 A310203 3930313 EU CARGO DOOR CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND OLD INTERNAL DOUBLER REPAIR AT FWD CARGO DOOR SKIN WITH ADDITIONAL DENTS AND SCRATCHES. REPAIR RENEWED BY EXTER NAL DOUBLER IAW SRM 52-30-00 FIG 203, APPROVED BY EA 6-5230-73905. 2 L 7 2 4F RT A35EU 2007100900066 20071009 00066 EU 2007 10 9 07FDEA04131 1 20070920 A 5313 A53980651207 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORROSION ON STRINGER 51 RT BETWEEN FRAME 76-77. STRINGER REPAIR PERFORMED IAW FREIGHTER A300-600 SRM 53-10-14/FIG 206, APPROVED BY EA 6-5318-82875 AND RAS/DAHAM/4019558/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100900067 20071009 00067 EU 2007 10 9 07FDEA04132 1 20070920 A 5313 A53974203 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORROSION ON STRINGER 53 LT BETWEEN FRAME 70-71 AND STRINGER 56 LT BELOW FRAME 70. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007100900070 20071009 00070 NM 2007 10 9 07FDEA04385 1 20071001 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 596FE 48554 CABIN, LBL 8 STA 1885 SEAT TRACK FOUND CORRODED. 10-12-07 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007100900073 20071009 00073 EU 2007 10 9 07FDEA04388 1 20071001 A 5320 A53974355200 FLANGE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND CORRODED FLANGE AT C61-62, P 56 RT-56 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100900076 20071009 00076 EU 2007 10 9 07FDEA04391 1 20071001 A 5313 A53811373 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSIO N IAW EA 6-5315-82855 AND RAS/AS/0095/2005 ISS A. 2 L 7 2 4F RT A35EU 2007100900078 20071009 00078 EU 2007 10 9 07FDEA04330 1 20070927 A 5320 A53989512210 ANGLE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 FOUND CORRODED ANGLE BETWEEN FRAME 92-93, STGR 14-15 LT. REPLACEMENT OF ANGLE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100900082 20071009 00082 EU 2007 10 9 07FDEA04334 1 20070927 A 5754 A53510007206 DOUBLER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 CORROSION ON KRUEGER FLAP DOUBLER AT FRAME 38, STGR 28-33 LT. REPAIR PERFORMED BY BLEND OUT CORROSION, NDT INSPECTION F OR CRACK FREE CONDITION IAW EA 6-5314-92161 AND RAS/DATLS/0002692/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100900084 20071009 00084 EU 2007 10 9 07FDEA04336 1 20070927 A 5330 A53985240 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 FOUND CORROSION ON TOP SKIN PANEL SECTION 19, BETWEEN FRAME 77-78, NEAR STGR 2-3 LT. REPAIR PERFORMED BY BLEND OUT CORR OSION AND FLAP PEENING IAW EA 6-5319-92171 AND RAS/DATLS/0002704/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100900085 20071009 00085 WP 2007 10 9 07FDEA04337 1 20070927 A 5712 ARB1297501 RIB DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 RT WING L/E INT STRUCTURE FOUND CRACK ON UPPER RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I. 2 L 7 3 4F A22WE 2007100900087 20071009 00087 WP 2007 10 9 07FDEA04339 1 20070927 A 5712 ARB1299501 RIB DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 RT WING L/E INT STRUCTURE FOUND CRACK ON UPPER RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I. 2 L 7 3 4F A22WE 2007100900089 20071009 00089 NM 2007 10 9 NWAA073333131 1 20070930 A 5754 SKIN AIRBUS A319 A319114 3930350 NM RT WING SLAT DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 331NB 1567 DURING LINE CHECK, FOUND DAMAGE TO NR 3 RT WING LEADING EDGE SLAT AND FUEL ACCESS PANEL. REPAIRED PER EA 31-210463. 2 L 7 2 4F RT A28NM 2007100900090 20071009 00090 EA 2007 10 9 CHQA20070048 1 20070928 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE OUT OF RIG A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 639BR 7313 GEE872739 CAE TO IAH - AFTER ROTATION OF THE AIRCRAFT, AND THE CALL OF POSITIVE RATE, LANDING GEAR RETRACTION WAS INITIATED. AS T HE GEAR BEGAN STOWING, RECEIVED A TRIPLE CHIME AND GEAR DISAGREE MESSAGE, ACCOMPANIED BY REPEATED BANGING OF THE MAIN GE AR. ADVISED TOWER OF THE EMERGENCY AND LEVELED OFF AT 2500 FT AND CONSULTED QRH EMERGENCY CHECKLIST. IT WAS NOTICED TH AT THE NOSE GEAR WAS INDICATING UP WHILE THE MAINS WERE INDICATING A YELLOW BARBER POLE. THE CHECK LIST CALLED FOR PULL ING THE EMERGENCY GEAR EXTENSION HANDLE. PULLING THE HANDLE GAVE THE INDICATION OF THREE GREEN AND THE BANGING STOPPED. AFTER COMPLETING THE EMERGENCY CHECKLIST, RAN ALL NORMAL CHECKLISTS AND INITIATED A FLY-BY OF THE TOWER TO VISUALLY IN 2 L 7 2 4F 4 F RT A21EA E15NE 2007100900092 20071009 00092 GL 2007 10 9 CHQA20070050 2 20070915 A 7261 23073567 CARBON SEAL EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL NR 2 ENGINE LEAKING A CHQA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 11 375SK 145569 CAE312346 STL TO MSP - AFTER TAKEOFF AT AROUND 1700FT, THE LAV SMOKE ALARM WENT OFF. THE FLIGHT ATTENDANT CONFIRMED THAT THE LAV SMOKE DETECTOR WAS GOING OFF. THERE WAS NO VISIBLE SMOKE BUT A SOOTY SMELL WAS PRESENT. AT THAT TIME AN EMERGENCY WAS DECLARED, ALL CHECK LISTS WERE ACCOMPLISHED, AND THE AIRCRAFT WAS RETURNED TO FIELD. UPON LANDING FIRE DEPARTMENT PERS ONNEL INSPECTED FOR FIRE DAMAGE AND FOUND NONE. MAINTENANCE RAN THE ENGINES AND COULD SMELL SMOKE WHEN THE NR 2 BLEED W AS SELECTED. WHEN THE NR 2 ENINGE WAS VISUALLY INSPECTED, THE "0" CARBON SEAL WAS FOUND TO BE LEAKING. THE "0" CARBON SEAL WAS REPLACED ON THE NR 2 ENGINE, AND THE ENGINE WAS OPS CHECKED AND LEAK CHECKED GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007100900095 20071009 00095 WP 2007 10 9 07FDEA04340 1 20070927 A 5712 ARB1291521 RIB DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 RT WING L/E INT STRUCTURE FOUND CRACK ON UPPER RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I. 2 L 7 3 4F A22WE 2007100900097 20071009 00097 EU 2007 10 9 07FDEA04342 1 20070927 A 5347 A5327923920000 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 670FE 777 MCD SEAT TRACK FROM FR 73 TO FR 65 BL 0 HAS SIX AREAS WITH CORROSION. REMOVED AND REPLACED SEAT TRACK FROM FR 65 TO FR 78 IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007100900098 20071009 00098 EU 2007 10 9 07FDEA04343 1 20070927 A 5753 SKIN AIRBUS 310 A310324 3930206 EU RT TE FLAP FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND OLD REPAIR ON CLOSING RIB 21, INNER FLAP RT FINAL REPAIR ON FLAP BY REPLACEMENT OF END RIB 21 IAW SB A310-57-2055/ PARA 2 F. 2 L 7 2 4F RT A35EU 2007100900100 20071009 00100 EU 2007 10 9 07FDEA04345 1 20070927 A 5542 SKIN AIRBUS 310 A310324 3930206 EU ZONE 300 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND DELAMINATIONS ON RUDDER SIDE PANEL IN AREA OF HINGE ATTACHMENTS AT ALL GFRP-FITTINGS LT AND RT: BR1, BR2, BR4 LOWE R, BR4 CENTER, BR4 UPPER, BR5, BR6 AND BR7. DELAMINATION REPAIR OF GFRP FITTING CONNECTION AT ALL HINGE FITTINGS PERFOR MED IAW SRM 55-41-12/FIG 216. 2 L 7 2 4F RT A35EU 2007100900105 20071009 00105 EU 2007 10 9 07FDEA04350 1 20070927 A 5330 A53611658200 SKIN AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 CORROSION ON FAIL/SAFE RING PAX DOOR NR 1 LT FUSELAGE SKIN PANEL AT FRAME 16A, AFT UPPER CORNER. REPAIR PERFORMED BY BL ENDING CORROSION AND HFEC INSPECTION IN THE AREA IAW EA 6-5312-82849 AND RAS/036735/006/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100900107 20071009 00107 EU 2007 10 9 YENA2007090 1 20071005 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU CABIN ODOR A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 15 605JB 2368 FLT 312, OAK-IAD, APPROX 1200Z, BURNING ELECTRICAL ODOR FROM OVERHEAD EYEBALL VENT AISLE 25, SECURED CABIN FAN AND PLACE D PACKS TO HIGH, ODOR DISSIPATED. ODOR CAME BACK ON DESCENT. COMPLIED WITH TSM 23-39-00-810-801. COULD NOT DUPLICATE WRITE UP. COMPLIED WITH TSM 24-00-00-810-823. COULD NOT ISOLATE THE ELECTRICAL ODOR. OPERATED SYSTEM FOR TWO HOURS WI TH NO INDICATIONS OF ANY ODOR. REMOVED AND REPLACED ALL VDU'S & SEB'S PRECAUTIONARY IN ROW 25ABCDEF. 2 L 7 2 4F RT A28NM 2007100900108 20071009 00108 EA 2007 10 9 TRAX200701448 1 20071001 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 838AS 7276 AAR - CREW ESCAPE HATCH PLACARDS MISSING (X 4). 2 L 7 2 4F RT A21EA 2007100900110 20071009 00110 EU 2007 10 9 TRAX200701450 1 20071001 A 5730 SKIN AEROSP ATR72 ATR72 EU LT WING CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 LEFT WING FLANGE OF ACCESS 521DT CORRODED. 10-11-07 LT WING FLANGE, 521 DT AREA, CORROSION REMOVED IAW SRM 57-14-12 F IG 401 FLANGE WITHIN LIMITS (MATERIAL REMAINING 0.762") IAW SRM 57-14-12 FIG 302 HFEC PERFORMED IAW NTM. NO CRACK S FOUND, REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IAW SRM 57 -14-12 FIG 401. MATERIAL THICKNESS: 0.782 MATERIAL REMOVED: 0.030 WITHIN LIMITS AS PER SRM: 57-14-12 FIG 301. 2 H 7 2 4T RT 2007100900111 20071009 00111 EA 2007 10 9 TRAX200701451 1 20071001 A 5310 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA PAX DOORWAY CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 876AS 7576 ANGLE ON PAX DOOR FRAME UNDER PANEL 832AR IS CRACKED. 10-11-07 REMOVED UNSERVICEABLE PAX DOOR FRAME ANGLE. LOCATED N EW SERVICEABLE DOUBLER IAW CRJ SRM 51-42-06, 51-42-13 AND 51-42-21. OK TO INSTALL. INSTALLED NEW SERVICEABLE DOUBLER P/N 601R318094-2 P.O. 951101 USING HARDWARE, LOCK FASTENERS P/N HST110AG6-4, NUTS P/N KFN587-3 P.O. 950817, RIVETS CR3213-5 -2, 1 SOLID RIVET MS20470AD5-5 IAW CRJ 200 SRM 51-42-06, 51-42-13 AND 51-42-21. REASEMBLED AFT LEVER AND TORQUE (REF FOR M 409A) IAW CRJ 200 AMM 51-11-21. 2 L 7 2 4F RT A21EA 2007100900112 20071009 00112 EU 2007 10 9 TRAX200701452 1 20071001 A 5730 SKIN AEROSP ATR72 ATR72 EU WING CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 FLANGE (ON WING) OF FWD PANEL 622CT CORRODED. 10-11-07 RT WING FLANGE, 622 CT AREA, CORROSION REMOVED IAW SRM 57-14- 12 FIG 401. FLANGE WITHIN LIMITS (MATERIAL REMAINING 0.746") IAW SRM 57-14-12 FIG 301, HFEC PERFORMED IAW NTM, NO CRAC KS FOUND. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IAW SRM 57 -14-12 FIG 401. MATERIAL THICKNESS: 0.782 MATERIAL REMOVED: 0.036 WITHIN LIMITS AS PER SRM: 57-14-12 FIG 301. 2 H 7 2 4T RT 2007100900113 20071009 00113 EU 2007 10 9 TRAX200701453 1 20071001 A 5714 INTERCOSTAL AEROSP ATR72 ATR72 EU WING BOX CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 WING BOX FR 23, JUNCTION WITH INTERCOSTAL, ANGLE CRACKED. 2 H 7 2 4T RT 2007100900114 20071009 00114 EA 2007 10 9 TRAX200701454 1 20071001 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 855AS 7395 FLOORBEAM CRACK AT FS 280.00 RBL 9.5. 10-11-07 FLOORBEAM REPLACED IAW REO 601R-53-11-171 REV D. 2 L 7 2 4F RT A21EA 2007100900115 20071009 00115 EA 2007 10 9 TRAX200701455 1 20071001 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 855AS 7395 SUSPECTED CRACK ON VERTICAL SKIN OF PAX DOOR STEP 832 AT. 10-11-07 HFEC PERFORMED, CRACK CONFIRMED AND MARILED ON TH E PART. CRACK ON VERTICAL SKIN OF PAX DOOR STEP 832 AT REPAIRED IAW SRM 51-12-00 FIG 7. 2 L 7 2 4F RT A21EA 2007100900117 20071009 00117 NM 2007 10 9 KCSA071446 1 20071007 A 5330 SKIN BOEING 747 7472B4B 138481B NM BS 1890-1910 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 C-2 CARGO DOOR SKIN CORRODED BETWEEN BS 1890 AND 1910, STR 40R. 2 L 7 4 4F RT A20WE 2007100900118 20071009 00118 NM 2007 10 9 KCSA071447 1 20071007 A 5330 SKIN BOEING 747 7472B4B 138481B NM BS 680 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FUSELAGE SKIN DAMAGED AT BS 680, STR 33R. 2 L 7 4 4F RT A20WE 2007100900120 20071009 00120 NM 2007 10 9 KCSA071449 1 20071007 A 5420 STIFFENER BOEING 747 7472B4B 138481B NM NR 3 PYLON WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 NR 3 PYLON LOWER SPAR I/B STIFFENER WORN AT PNEUMATIC. DUCT ANTI-ROTATION CLIP BETWEEN NAC STA 180 AND 219. 2 L 7 4 4F RT A20WE 2007100900124 20071009 00124 EA 2007 10 9 TRAX200701462 1 20071002 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 349 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 855AS 7395 ANGLE 601R38983-13 AT FS 349.0 RBL 36 CORRODED OUT OF LIMITS. FABRICATION OF A NEW ANGLE REQUIRED. 2 L 7 2 4F RT A21EA 2007100900128 20071009 00128 EA 2007 10 9 TRAX200701467 1 20071003 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 680BR 7679 ASD AFT DRAG ANGLE CRACKED. 2 L 7 2 4F RT A21EA 2007100900129 20071009 00129 EA 2007 10 9 TRAX200701468 1 20071003 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 680BR 7679 ASD CRACKED UNDER TOP STEP AFT AREA. 2 L 7 2 4F RT A21EA 2007100900132 20071009 00132 EU 2007 10 9 TRAX200701471 1 20071004 A 3150 WARNING LIGHT AEROSP ATR72 ATR72 EU ILLUMINATED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 643AS 413 FLAP UNLOCK LIGHT CAME ON DURING APPROACH. EMERGENCY DECLARED. 2 H 7 2 4T RT 2007100900133 20071009 00133 NM 2007 10 9 SWAA074847 1 20070927 A 5753 6546435 SKIN BOEING 737 7377H4 1384404 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 704SW 27838 DURING SCHEDULED HC2 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007100900134 20071009 00134 NM 2007 10 9 SWAA074851 1 20070927 A 5322 6546546 SHEAR TIE BOEING 737 7373A4 1384585 NM BS 867 S13L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 867, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007100900135 20071009 00135 NM 2007 10 9 SWAA074844 1 20070927 A 5511 6547500 STRAP BOEING 737 7373H4 1384600 NM SPAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED 10Y CHECK, FOUND LEFT HORIZONTAL STABILIZER UPPER AFT SPAR UPPER STRAP CORRODED. REPAIRED STRAP PER SR M. 2 L 7 2 4F RT A16WE 2007100900136 20071009 00136 NM 2007 10 9 KCSA071451 1 20071008 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1640 WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 SEAT TRACK SECTION WORN AT STA 1640 LBL 42. 2 L 7 4 4F RT A20WE 2007100900137 20071009 00137 NM 2007 10 9 KCSA071452 1 20071008 A 5312 BULKHEAD BOEING 747 7472B4B 138481B NM BS 2460 CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 APU PNEUMATIC DUCT SUPPORT CLAMP IS CHAFING ON STA 2460 BULKHEAD INNER CHORD AT LBL 44. 2 L 7 4 4F RT A20WE 2007100900138 20071009 00138 NM 2007 10 9 KCSA071453 1 20071008 A 5315 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 1800 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA 1800 RBL 46 AFT PIT FLOORBEAM LOWER FWD FLANGE CORRODED. 2 L 7 4 4F RT A20WE 2007100900140 20071009 00140 EA 2007 10 9 TRAX200701420 1 20070926 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA CABIN UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 876AS 7576 AAR - EMERGENCY PLACARD ON CREW ESCAPE HATCH NEEDS REPLACING. 2 L 7 2 4F RT A21EA 2007100900141 20071009 00141 EA 2007 10 9 TRAX200701421 1 20070926 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 876AS 7576 AAR - THE PAX DOOR FWD ANCHOR FITTING IS CRACKED. 10-11-07 UPON FURTHER INVESTIGATION FOUND PAX DOOR FWD ANCHOR FITT ING STOP PLATE COVER TO BE CRACKED AND FOUND PAX DOOR FWD ANCHOR FITTING TO BE SERVICEABLE. REMOVED UNSERVICEABLE STOP FITTING. INSTALLED NEW SERVICEABLE STOP FITTING P/N 601R38075-4 P.O. 950840 IAW CRJ 200 AMM 52-11-17. 2 L 7 2 4F RT A21EA 2007100900142 20071009 00142 EU 2007 10 9 TRAX200701422 1 20070927 A 5312 PRESSURE PANEL AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 CORROSION FOUND ON FWD PRESSURE WEB, LBL 10 TOP AREA. 10-9-07 CORROSION REMOVED IAW SRM 51-21-42 WEB OUT OF LIMITS IAW SRM 53-11-00 FIG 301. REPAIR CARRIED OUT IAW SRM 53-11-10 FIG 403 FABRICATION COVER ON W/C 2000-9 MATERIAL THI CKNESS: 0.053 MATERIAL REMOVED: 0.018 OUT OF LIMITS AS PER SRM: 53-11-00 FIG 301. 2 H 7 2 4T RT 2007100900143 20071009 00143 EU 2007 10 9 TRAX200701423 1 20070927 A 5310 DOOR FRAME AEROSP ATR72 ATR72 EU BS 7141 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 CARGO DOOR FRAME AT STA 7141 CRACKED. 10-16-07 HFEC PERFORMED AND CRACK CONFIRMED. CARGO DOOR FRAME REPAIRED WITH DOUBLE IAW SRAS DO/TS-4166/07. REPAIRED INTERCOSTAL ON CARGO DOOR PER EC EO 72-52-0107. 2 H 7 2 4T RT 2007100900145 20071009 00145 NM 2007 10 9 2007UALA03992 1 20070928 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT OF MID GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 646UA 25283 EEL LIGHTS AT RIGHT OF MID GALLEY & AT ROW 5AB ARE INOP. 10-26-07 REPAIRED EEL POWER STRIP. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007100900147 20071009 00147 NM 2007 10 9 SWAA074840 1 20070927 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 277 S12R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 12R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007100900148 20071009 00148 NM 2007 10 9 SWAA074850 1 20070927 A 5753 65C30462 SKIN BOEING 737 7373A4 1384585 NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING OUTBOARD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007100900152 20071009 00152 NM 2007 10 9 SWAA074843 1 20070927 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND MID CABIN EEPLS PHOTOLUMINESCENT STRIP LOOSE. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007100900153 20071009 00153 WP 2007 10 9 MWEA070229 1 20070929 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP ROW 8 - 31 INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 809ME 48071 CABIN CEILING EMERGENCY LIGHTS FROM ROW 8 TO 31 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 2007100900154 20071009 00154 EU 2007 10 9 YENA2007085 1 20071002 A 3350 321431 BATTERY PACK AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHT FAILED A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 566JB 18029 2042 FWD LEFT EPSU BATTERY FAILED ON EMERGENCY POWER TEST. REMOVED AND REPLACED FWD LEFT EPSU BATTERY PACK IAW AMM 33-51-00, OPS CHECK OK. 2 L 7 2 4F RT A28NM 2007100900155 20071009 00155 NM 2007 10 9 2007UALA03993 1 20070928 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT AFT LAV INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 EEL LIGHT BARS AT THE RIGHT AFT LAV & IN FRONT OF THE VCC CABINET ARE INOPERATIVE. 10-26-07 REPAIRED EEL LIGHT BAR PER MM 33-51-10 AND OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007100900157 20071009 00157 NM 2007 10 9 2007UALA03995 1 20070930 A 2497 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT GENERATOR LOOSE A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 660UA 27115 EICAS MSG L GEN DRIVE DISPLAYED. GEN DRIVE LIGHT ILLUM. GEN DRIVE DISCONNECTED. FOUND TERMINAL CONNECTOR LOOSE, CLEAN ED, SECURED AND OPS CK NOW OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007100900158 20071009 00158 NM 2007 10 9 2007UALA03996 1 20070928 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SEAT 1E INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 661UA 27158 EEL STRIP LIGHTS OUT AT SEAT 1E. 10-26-07 REPAIRED EEL STRIP. OP CHECKS NORMALLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007100900161 20071009 00161 NM 2007 10 9 SWAA074917 1 20071002 A 5315 141A5504 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 753SW 29848 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 51. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007100900163 20071009 00163 NM 2007 10 9 SWAA074912 1 20071002 A 5311 6545805 FRAME BOEING 737 7373H4 1384600 NM BS 277 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007100900164 20071009 00164 NM 2007 10 9 SWAA074913 1 20071002 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM BS 440 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007100900167 20071009 00167 NM 2007 10 9 SWAA074915 1 20071002 A 5311 6546552 FRAME BOEING 737 7375H4 138449D NM BS 827 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007100900169 20071009 00169 NM 2007 10 9 SWAA074901 1 20071002 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 344 S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007100400142 20071004 00142 EU 2007 10 4 07FDEA04358 1 20070928 A 5720 A57244005201 PLATE AIRBUS 310 A310324 3930206 EU ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND CRACKED REINFORCING PLATE ON SLAT TRACK NR 7, FWD OF FRONT SPAR, UPPER SKIN, RT WING. REPLACEMENT OF REINFORCING PLATE ON TRACK 7 RT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100400145 20071004 00145 NM 2007 10 4 07FDEA04361 1 20070928 A 5311 65163389 FRAME BOEING 727 727233 138408A NM BS 950 S26L CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 263FE 21625 AFT CARGO STA 950 S-26L HAS A CRACK AND CORROSION ON FRAME STA 950 REMOVED CORROSION IAW SRM 51-10-6, AREA WITHIN LIMITS IAW EA 7-5310-110790, HFEC ACCOMPLISHED, NO DEFECTS NOTED. 2 L 7 3 4F RT A3WE 2007100400150 20071004 00150 SO 2007 10 4 SWIA200718714 1 20070802 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 213SW 120277 FOUND C-CHECK, LEFT SIDEWALL SEAT TRACK HAS CORROSION ON FORWARD SECTION. REPLACED THE LEFT FORWARD SIDEWALL SEAT TRACK SECTION IAW EMB120 AMM 53-01-05. 2 L 7 2 4T RT A31SO 2007100400152 20071004 00152 EA 2007 10 4 SWIA200718716 1 20070720 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 507CA 7796 FOUND AT C-CHECK, STA280 BULKHEAD OUTBOARD LBL9 AND RBL9 CLIP IS CRACKED. INSTALLED LBL9 AND RBL9 OUTBOARD CLIP PER CRJ 200 SRM 51-42-21 PG 11. 2 L 7 2 4F RT A21EA 2007100400158 20071004 00158 EU 2007 10 4 07FDEA04183 1 20070921 A 5310 A53988724205 CROSSBEAM AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FOUND CORROSION ON CROSS STRUT AT FRAME 87, STRG 15 RT AFT SIDE. REPLACEMENT OF CROSS STRUT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100400160 20071004 00160 EU 2007 10 4 07FDEA04185 1 20070921 A 5320 A53610607204 SUPPORT FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CRACKED SUPPORT FITTING BETWEEN FRAME 16A-17, STRG 44 RHS. REPLACEMENT OF FITTING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100400196 20071004 00196 EU 2007 10 4 07FDEA04300 1 20070926 A 5330 A53974526 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 OLD EXTERNAL DOUBLER REPAIR ON FUSELAGE SKIN AT FRAME 67, STGR 51-54 RT, DOUBLER THICKNESS NOT CONFORM TO SRM. DOUBLE R REPAIR RENEWED IAW SRM 53-10-12/FIG 225/SH 2. 2 L 7 2 4F RT A35EU 2007100500009 20071005 00009 EU 2007 10 5 07FDEA04401 1 20071001 A 5313 A53974203574 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND CORROSION AT STRINGER P52 LT, C70-71. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007100500010 20071005 00010 EU 2007 10 5 07FDEA04402 1 20071001 A 5330 A53974481210 DOUBLER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND CORROSION AT DOUBLER C71-72, P 47-48 LT REPAIR PERFORMED BYREWORK OF CORROSION, NDT FOR CRACK FREE AND FLAP PEENIN G IAW EA 6-5317-82856 AND RAS/DATLS/0002522/2005 ISS B. 2 L 7 2 4F RT A35EU 2007100500013 20071005 00013 EU 2007 10 5 07FDEA04405 1 20071001 A 5330 A53772527200 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND NICK ON SKIN PANEL NR 3 C 18-19, P 33 RT REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5313-82859 AND R AS/DABRE/7005143/2005 ISS A. 2 L 7 2 4F RT A35EU 2007100500017 20071005 00017 EU 2007 10 5 07FDEA04409 1 20071001 A 5312 A53811802200 BULKHEAD AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND OLD REPAIR (MISDRILLED HOLE) AT FRAME 54 BULKHEAD LT WEB, WAS ACCEPTED FOR ONLY ONE FERRY FLIGHT. REPAIR RENEWED BY REMOVING THE EXISTING DOUBLER, CUT OUT ON WEB FOOT AND INSTALLING DOUBLER AND REPAIR ANGLE IAW EA 6-5315-81126 AND RA S/AS/0248/2004 ISS B. 2 L 7 2 4F RT A35EU 2007100500024 20071005 00024 EU 2007 10 5 07FDEA04418 1 20071001 A 5313 A53974203226 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION AT STRINGER P55LH BETWEEN C 55/58-61 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007100500027 20071005 00027 WP 2007 10 5 07FDEA04423 1 20071001 A 5230 ADA37741 ANGLE DOUG DC10 DC1010 3022110 WP BS 899 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 LOWER CTR CARGO DOOR CRACK ON FWD LWR CORNER. REPAIRED AREA IAW SRM 52-10-00 FIG 17 VOL I. 2 L 7 3 4F A22WE 2007100500035 20071005 00035 EU 2007 10 5 07FDEA04431 1 20071001 A 5330 A53981600246 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND DENT AT C77-78, P 27-28 LT FLUSH DOUBLER REPAIR PERFORMED IAW SRM 53-10-12 FIG 227 AND STRINGER REPAIR PERFORMED I AW SRM 53-10-14. 2 L 7 2 4F RT A35EU 2007100500044 20071005 00044 EA 2007 10 5 A6WA200740531 1 20070823 A 5310 60135050109 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 467AW 7900 CARGO DOOR SUPPORT BEAM LOWER ANGLE, P/N 601R35050-109, CRACKED IN RADIUS APPROX 1.2 INCHES LONG. MAINTENANCE REMOVED A ND REPLACED BRACKET (ANGLE) P/N 601R-35050-109 IAW CRJ 200 SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007100500047 20071005 00047 EA 2007 10 5 A6WA200740528 1 20070818 A 5320 6013501250 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FS 625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 467AW 7900 LEFT OBLIQUE ANGLE IS CRACKED .75 INCH IN RADIUS AT FS 625, WL 100. MAINTENANCE REMOVED AND REPLACED INSTALLED SERVICEA BLE ANGLE P/N 601-35012-51 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007100500049 20071005 00049 2007 10 5 WGEA200700007 4 20070925 A 2300 70000078102 DISPLAY ECLIPS EA500 ECLIPSEEA500 3350000 SW COCKPIT MALFUNCTIONED E WGEA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 EA 27 135DJ 42 000036 INTERMITTENT COM 1 TRANSMIT PROBLEM ON CLIMB OUT. ON COM 2 DISPLAY ON L PFD, R PFD/COM. WORKED NORMALLY UNTIL LEVEL AT CRUISE. THEN UNABLE TO TR/RX ON COM 1 ON EITHER SIDE. COM 2 FUNCTIONED NORMALLY, BUT THEN STUCK ON 121.8 (LAST FREQ I N ACTIVE). ACTIVE (WINDOW) AND UNABLE TO SWAP FREQUENCY OR CHANGE STBY MORE THAN 1 MBZ 5 MINUTES LATER L PFD COM1/COM2 BUTTON CONTROLLED COM1/COM 2SELECTION ON R PFD. MINUTES LATER L PFD NAV FUNCTIONS FAILED INCLUDING NAV1,NAV2 WORKED BUT WAS UNCHANGEABLE IN FREQUENCY FIELDS. LANDING WHITE ADVISORY CAS "AVIONICS DATA BUSS FAIL". REMOVED AND REPLACED LEFT P FD WITH A REPAIRED UNIT IAW EA500 AMM 31-10-16. PERFORMED OPERATIONAL CHECKS OF LEFT PFD IAW EA500 AMM 31-00-00, NO DEF 1 L 7 2 4J RT A00002AC 2007100500055 20071005 00055 EU 2007 10 5 07FDEA04370 1 20070928 A 5320 A53986751206 PLATE AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 DAMAGED WEB PLATES BETWEEN FRAME 86-87, STGR. 33 LT REPLACEMENT OF WEB PLATE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100500056 20071005 00056 EU 2007 10 5 07FDEA04435 1 20071002 A 5730 A57340086 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION ON RT WING BOTTOM SKIN RIB 1-2 IN FRONT OF FRONT SPAR NEAR TRACK NR 1 REPAIR PERFORMED BY REWORK OF CORR OSION IAW EA 6-5720-112461 AND RAS/BAE/1005290/2007 ISS A. 2 L 7 2 4F RT A35EU 2007100500079 20071005 00079 EU 2007 10 5 07FDEA04265 1 20070925 A 5320 A53778342212 PLATE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 CRACKED SHEAR PLATES BETWEEN FRAME 38-38.1, STRG 44 LT, FWD CARGO COMPARTMENT. REPAIR PERFORMED BY REPLACEMENT OF SHE AR PLATE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100500088 20071005 00088 NM 2007 10 5 2007UALA03832 1 20070922 A 5310 DOOR FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 929UA 26652 AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT LOWER OUTBOARD CORNER OF LOWER STOP. REMOVED & REPLACED AFT PIT DOOR CUTOUT FWD FRAME. 2 L 7 2 4F 4 F RT A16WE E21EU 2007100500093 20071005 00093 NM 2007 10 5 2007UALA03837 1 20070922 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 847-867 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 RIGHT CABIN AREA RIGHT CREASE BEAM INTERCOSTAL UPPER SURFACE CORRODED AT BS 847-867 STRINGER 17R. REPLACED CORRODED CR EASE BEAM. 2 L 7 2 4F 4 F RT A16WE E21EU 2007100500098 20071005 00098 NM 2007 10 5 2007UALA03953 1 20070928 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 527UA 24995 NR 1 RIGHT MAIN ENTRY DOOR EMERGENCY EXIT LIGHT INOP. SERVICE DIFFICULTY IS ATTRIBUTED TO A FUSED LAMP. RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007100500109 20071005 00109 NM 2007 10 5 2007UALA03964 1 20071001 A 5753 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE TE FLAP DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 175UA 24382 LEFT MID FLAP DELAM AND DAMAGE. LEADING EDGE INBOARD, EXTENDING OUT APPROX 5 INCHES. SUSPECT MOISTURE CONTAMINATION. R EPLACED THE LT OUTBOARD FLAP PER MM-27-51-04. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007100500120 20071005 00120 NM 2007 10 5 UPS07450805 1 20071001 A 3350 LAMP BOEING 747 747123F NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:N/A EMERGENCY LIGHT INOP L1 DOOR FWD. RELAMPED EMERGENCY LIGHT, OPS CHECK GOOD 747 MM 33-51-00. 2 L 7 4 4F A20WE 2007100500124 20071005 00124 NM 2007 10 5 UPS07M50790 1 20070801 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT BORE RT NR 10 FOUND WITH CORROSION. CORR AT BARREL NUT BO RE REMVD PER SRM 51-21-01 VII R38. BOTTOM SURFACE CLEANED. BORE REAM TO 0.988" DIA REMN BLEND OUT 0.060" DEEP, EXCEED LIMITS. BARREL NUT BORE, BLEND OUT VOIDS, BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. SLEEVE BUSHING FAB, PROTECTED INSTALLED. REPAIR C/O AT BARREL NUT BORE NR 10 RT IS ACCEPTABLE PER EN1495-07. 2 L 7 3 4F RT A22WE 2007100500125 20071005 00125 NM 2007 10 5 UPS07M50791 1 20070806 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT BORE LEFT NR 19 FOUND WITH CORROSION. CORR AT BARREL NUT BORE REMOVED. BOTTOM BORED THRU BORE REAM TO 1.067" DIA REMN BLEND OUT 0.020" DEEP, EXCEEDED LIMITS. BARREL NUT BORE, BLEND OUT VOID, SMOOTHEN & PROTECTED PER SRM 51-21-01VII R38. BUCKET BUSHING FAB, PROTECTED & INSTALLED. REPAIR C/O AT BARREL NUT BORE NR 19 LEFT IS ACCEPTABLE PER EN1493-07. 2 L 7 3 4F RT A22WE 2007100500127 20071005 00127 NM 2007 10 5 2007UALA03838 1 20070923 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 616 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 FUSELAGE FRAME AT BS 616, 7 INCHES BELOW STRINGER 17R INNER CHORD HAS CRACK RUNNING FROM TIP THROUGH 2 FASTENER HOLES. REMOVED DAMAGE. FABRICATED AND INSTALLED NESTED ANGLE AND FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007100500130 20071005 00130 NM 2007 10 5 2007UALA03841 1 20070923 A 2530 OVEN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE GALLEY ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 118UA 28811 OVEN B43 OMITS ELECTRICAL BURNING ODOR. 10-19-07 REPLACED GALLEY FOOD CART CONTROLLER "PIG TAIL". OP CHECKS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2007100500149 20071005 00149 NM 2007 10 5 2007UALA03973 1 20070928 A 2751 TRANSMITTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TE FLAP OUT OF LIMITS A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 597UA 28750 RIGHT FLAP POSITION TRANSMITTER ACCURACY OUT OF RANGE CAUSING FLAP-SLAT ELEC STATUS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007100500152 20071005 00152 NM 2007 10 5 2007UALA03977 1 20070929 A 5230 6547952U355 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 AFT CARGO DOOR S/N 1604 LWR AFT FRAME CRACKED AT RIVET HOLE ABOVE LWR STOP FITTING. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED LWR AFT FRAME. 2 L 7 2 4F 4 F RT A16WE E21EU 2007100500156 20071005 00156 EU 2007 10 5 2007UALA03981 1 20070928 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 480UA 1555 CREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. *S/D* OXYGEN PRESSURE AT 1430 ON EICAS, APPROX 1550 AT BO TTLE, SERVICED TO FULL ON BOTTLE (1750) EICAS READS 1610. 2 L 7 2 4F 4 F RT A28NM E40NE 2007100500173 20071005 00173 NM 2007 10 5 UPS07650778 1 20070920 A 5340 140T2101403 STRINGER CLIP BOEING 767 76734AF 1385212 NM BS 654 S6L BENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 328UP 27754 INSPECTION TYPE:C1 BENT STRINGER CLIP. REMOVED, FABRICATED, INSTALLED PER SRM 51-40-02 AND DRAWING 143T1126. 2 L 7 2 4F RT A1NM 2007100500175 20071005 00175 NM 2007 10 5 UPS07650781 1 20070920 A 5340 STRINGER CLIP BOEING 767 76734AF 1385212 NM BS 654 S8L BENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 328UP 27754 INSPECTION TYPE:C1 BENT STRINGER CLIP. REMOVED, FABRICATED, INSTALLED PER SRM 51-40-02 AND DRAWING 143T1126. 2 L 7 2 4F RT A1NM 2007100500190 20071005 00190 EA 2007 10 5 TRAX200701391 1 20070924 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA BS 559-621 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 855AS 7395 MANY SEAT RAILS AND BAGGAGE RAILS CORRODED BETWEEN FS 559+80 TO 621.00. 10-9-07 REPLACED CORRODED RAILS AND BAGGAGE RAILS BTWN FS 559 80 TO FS 621.00 AS PER SRM 51-42-02 2 L 7 2 4F RT A21EA 2007100500192 20071005 00192 NM 2007 10 5 SWAA074849 1 20070927 A 3310 LIGHT BOEING 737 7373H4 1384600 NM COCKPIT SHORTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 FLIGHT DECK RIGHT OVERHEAD LIGHT SHORTED OUT. 2 L 7 2 4F RT A16WE 2007100500193 20071005 00193 NM 2007 10 5 SWAA074834 1 20070927 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 236WN 34631 L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007100500194 20071005 00194 NM 2007 10 5 SWAA074848 1 20070927 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 776WN 30591 DURING SCHEDULED HC2 CHECK, FOUND EEPLS INOP AT ROW 5 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007100900011 20071009 00011 NM 2007 10 9 NWAA073315523 1 20070928 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 523US 23617 DURING OVERNIGHT LINE CHECK FOUND IN AFT PASSENGER COMPARTMENT 2 LEFT OVERHEAD BULL NOSE LIGHTS INOPERATIVE. ALSO, FOUN D CENTER OVERHEAD EXIT SIGN, L4 DOOR EXIT SIGN AND L4 DOOR EMERGENCY SLIDE LIGHTS INOP. MAINTENANCE REMOVED AND REPLACE D BATTERY PACKS. OPERATIONAL CHECKED GOOD AND AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007100900014 20071009 00014 NM 2007 10 9 NWAA073325531 1 20070930 A 2161 6259346 CONTROLLER BOEING 757 757251 1384970 NM A/C PACK TEMP MALFUNCTIONED A NWAA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 GL 01 531US 56334 11752 23846 DURING CLIMB-OUT FROM DTW, CABIN AND FLIGHT DECK BECAME VERY HOT. COM PROCEDURE TO ALLEVIATE HEAT COMING FROM PACK WAS INEFFECTIVE. EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO DTW FOR A UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REP LACED 2 TEMP SENSORS, STANDBY PACK TEMP CONTROLLER AND ZONE TEMP CONTROLLER. 2 L 7 2 4F RT A2NM 2007100900023 20071009 00023 EU 2007 10 9 07FDEA04314 1 20070926 A 5313 A53974527224 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 CORROSION ON STRINGER 56 LT, NEAR TO FRAME 59 OUT OF LIMIT REMAINING THICKNESS IS 3,8MM (NOMINAL 4,5MM). REPAIR PERFORM ED BY BLEND OUT TO DEPTH NO GREATER THAN REPORTED, ROTOTEST INSPECTION IN VOID FASTENER HOLES WITH NIL FINDINGS AND NEW FASTENER INSTALLATION IAW EA 6-5317-92145 AND RAS/DATLS/0002670/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100900028 20071009 00028 EU 2007 10 9 07FDEA04457 1 20071002 A 5320 A53974355200 FLANGE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND FLANGE C61-62, AD CORRODED REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100900030 20071009 00030 EU 2007 10 9 TRBA2007081 1 20070925 A 3320 37172 BALLAST AEROSP ATR72 ATR72212A 8680902 EU CABIN LIGHTS FAILED A TRBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 29 545AT 545 FLIGHT ATTENDANT ADVISED OF ELECTRICAL BURNING ODOR ON TAKEOFF. REPLACED BURNED CEILING LIGHT BALLAST CONVERTER PER JIC 32-21-21 ON SEAT 9/10CD. PERFORMED ENGINE RUN-UP AND FOUND AC ACW AND DC ELECTRICAL SYSTEM WORKING PROPERLY, NO BURNIN G ODOR NOTICED PER MM 24-50-00. 2 H 7 2 4T RT A53EU 2007100900035 20071009 00035 EU 2007 10 9 MALA070121 1 20070927 A 3020 CONTROL MODULE SAAB SF340 340B 7860101 EU DE ICE SYS ODOR A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 453XJ 340B453 BURNING ODOR IN COCKPIT, FORWARD CABIN FOLLOWED BY "RT INTAKE" LIGHT CYCLING ON AND OFF, 20 SECOND INTERVALS. LEFT ICIN G CONDITIONS, ENGINE ANTI-ICE SWITCHED OFF, ODOR DISSIPATED. REMOVED AND REPLACED RT DEICE CONTROL MODULE IAW AMM 30-21 -03. REMOVED AND REPLACED LOWER INLET DUCT IAW JOB CARD 7160-301 OPS CHECK GOOD REF 409 NR 302019 FOR DETAILS. 2 L 7 2 4T RT A52EU 2007100900038 20071009 00038 EU 2007 10 9 07FDEA04118 1 20070920 A 5553 A53470625 ATTACH FITTING AIRBUS 310 A310324 3930206 EU ZONE 300 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 DEEP GOUGE ON LT MIDDLE VERTICAL STABILIZER TO FUSELAGE ATTACH FITTING, OUTBOARD SIDE AFT AREA. REPAIR PERFORMED BY SMO OTH BLEND OUT AND NDT INSPECTION FOR CRACK FREE CONDITION IAW EA 6-5319-82881 AND RAS/DAHAM/4019574/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100900041 20071009 00041 NM 2007 10 9 07FDEA04375 1 20070929 A 5720 ANGLE DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 596FE 48554 LT WING FIXED LEADING EDGE, XOS 602, LOWER ANGLE FOUND CRACKED. 10-9-07 REMOVED ANGLE AS PER SRM 51-33-01 VOLUME II AND FABRICATED NEW ANGLE DOUBLER AS PER DRAWING ARB 2933. INSTALLED NEW ANGLE DOUBLER AT LT WING FIXED LEADING E DGE , XOS 602, LOWER AREA AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007100900048 20071009 00048 NM 2007 10 9 AALA20071798 1 20070920 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 937AN 30082 TUL - EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT STATION 500 FOR EMERGENCY LIGHTS IN FORWA RD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007100900079 20071009 00079 EU 2007 10 9 07FDEA04331 1 20070927 A 5320 A53989317 ANGLE AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 FOUND CORRODED ANGLES AT FRAME 92 BETWEEN STGR 9 LT TO 9 RT. REPLACEMENT OF ANGLES IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100900103 20071009 00103 EU 2007 10 9 07FDEA04348 1 20070927 A 5330 A53610633 SKIN AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 CORROSION ON FAIL/SAFE RING PAX DOOR NR 1 FUSELAGE SKIN PANEL AT FRAME 14, STGR 25 RT, AROUND THREE FASTENERS. REPAIR P ERFORMED BY BLENDING CORROSION, HFEC INSPECTION IN THE AREA, ROTOTEST OF HOLES FOR NIL CRACK FINDINGS WITH OVERSIZING HO LES FOR TRANSITION FIT IAW EA 6-5312-82936 AND RAS/AS/069/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100900104 20071009 00104 EU 2007 10 9 07FDEA04349 1 20070927 A 5330 A53610633227 SKIN AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 CORROSION ON FAIL/SAFE RING PAX DOOR NR 1 LT FUSELAGE SKIN PANEL AT FRAME 14, FWD UPPER CORNER. REPAIR PERFORMED BY BLE NDING CORROSION AND HFEC INSPECTION IN THE AREA IAW EA 6-5312-82849 AND RAS/036735/006/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100900125 20071009 00125 EU 2007 10 9 TRAX200701463 1 20071002 A 5753 BRACKET AEROSP ATR72 ATR72 EU LT I/B FLAP BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 LT I/B FLAP, O/B FLAP ARM (3) OMEGA BRACKETS BROKEN. 2 H 7 2 4T RT 2007100900126 20071009 00126 EU 2007 10 9 TRAX200701464 1 20071002 A 5210 INTERCOSTAL AEROSP ATR72 ATR72 EU PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 AFT INTERCOSTAL OF ROLLER STOP, PAX DOOR CRACKED. 10-9-07 ROLLER STOP OF PAX DOOR RAI FOM IAW AMM 20-21-12. AFT INT ERCOSTAL OF ROLLER STOP REPLACED AS PER SRM 51-25-01 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW S.P. 663 AND FAR 4 3, APPENDIX A. REPAIR ACCOMPLISHED IAW SRM 51-25-01. 2 H 7 2 4T RT 2007100900139 20071009 00139 EA 2007 10 9 TRAX200701419 1 20070926 A 5310 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 876AS 7576 AT FS 484, LBL 36 THE O/B PREVIOUS REPAIR CLIP IS CRACKED. 10-9-07 REMOVED CRACKED REAPAIR CLIP FROM FS 484 LBL36 I AW SRM 51-42-21. DUPLICATED REPAIR CLIP FROM 0.063 202473 PO 950261 IAW SRM 51-24-16. LOCATED HOLES IN SERVICEABLE CLIP IAW SRM 51-40-11. 13367. OK TO ALODINE AND PRIME. ALODINED, PRIMED AND TOPCOATED IAW SRM 51-25-16. 13362. INSTALLED NEW DUPLICATED ANGLE AT FS 484 LBL 36 PER SRM 51-42-21 ADN 51-23-00. 13256. OK TO TOUCHUP FINISH. APPLIED FINISH PER SRM 51- 25-16. 13256. 9-28-07. 2 L 7 2 4F RT A21EA 2007100900149 20071009 00149 2007 10 9 SWAA074839 4 20070927 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007100900150 20071009 00150 NM 2007 10 9 SWAA074837 1 20070927 A 3350 MS155721 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007100900160 20071009 00160 NM 2007 10 9 SWAA074911 1 20071002 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 632SW 27707 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007100900168 20071009 00168 NM 2007 10 9 SWAA074909 1 20071002 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 520 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007100900171 20071009 00171 NM 2007 10 9 SWAA074904 1 20071002 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 440 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007100900172 20071009 00172 WP 2007 10 9 MWEA070233 1 20071002 A 5320 5910142U11 WEB DOUG DC9 DC981 3022081 WP BS 408-427 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 814ME 48010 FORWARD CARGO DOOR LOWER CUTOUT BETWEEN FUSELAGE STATION 408 AND 427 FLOOR WEB HAS SURFACE CORROSION. REMOVED CORROSION AND REMOVED AND REPLACED WEB. 2 L 7 2 4F A6WE 2007100900173 20071009 00173 NM 2007 10 9 MWEA070234 1 20071004 A 7830 CHANNEL BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 910ME 55174 RIGHT THRUST REVERSER UPPER BUCKET AFT ZEE CHANNEL IS CRACKED ON INBOARD SIDE AT STATION 36. CUT OUT DAMAGE AND FABRICA TED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2007100900174 20071009 00174 EU 2007 10 9 2007UALA03827 1 20070921 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 413UA 470 THREE SERVICE CABIN EMERGENCY LIGHT TEST FAILED, MESSAGE INT LOADS EMER L. 2 L 7 2 4F 4 F RT A28NM E40NE 2007100900175 20071009 00175 EA 2007 10 9 TRAX200701395 1 20070924 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 926EV 7843 ASD LOWER STEP BROKEN. 2 L 7 2 4F RT A21EA 2007100900176 20071009 00176 EA 2007 10 9 TRAX200701396 1 20070924 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 976EV 7601 EXIT SIGN CAGE ASSEMBLY IN CABIN BROKEN. 2 L 7 2 4F RT A21EA 2007100900178 20071009 00178 EA 2007 10 9 TRAX200701398 1 20070925 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 876AS 7576 PAX DOOR EXTERNAL HANDLE CRACKED. 10-11-07 REMOVED UNSERVICEABLE EXTERNAL PAX DOOR HANDLE AND INSTALLED SERVICEABLE EXTERNAL PAX DOOR HANDLE ASSY IAW CRJ 200 AMM 52-11-03. 2 L 7 2 4F RT A21EA 2007100900181 20071009 00181 EA 2007 10 9 TRAX200701401 1 20070925 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 859AS 7421 FLAPS FAIL AT 20, TOWER DECLARED EMERGENCY. 2 L 7 2 4F RT A21EA 2007100900182 20071009 00182 EA 2007 10 9 TRAX200701402 1 20070925 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA MAIN PAX STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 FLT ATTENDANT REPORTS FORWARD PASSENGER DOOR REQUIRED EXCESSIVE FORCE TO OPEN. DOOR HUNG UP ABOUT HALF WAY DOWN. 2 L 7 2 4F RT A21EA 2007100900183 20071009 00183 NM 2007 10 9 SWAA074905 1 20071002 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 887 S25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007100900184 20071009 00184 NM 2007 10 9 SWAA074906 1 20071002 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 767 S22L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007100900186 20071009 00186 NM 2007 10 9 SWAA074907 1 20071002 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007100900187 20071009 00187 2007 10 9 SWAA074902 4 20071002 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007100900188 20071009 00188 2007 10 9 SWAA074910 4 20071002 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007100900189 20071009 00189 EA 2007 10 9 TRAX200701403 1 20070926 A 7830 TRACK CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 838AS 7276 RIGHT THRUST REVERSER LOWER O/B TRACK IS CRACKED. 10-9-07 REMOVED UNSERVICEABLE RT THRUST REVERSER LOWER O/B TRACK IAW CRJ AMM 78-34-11. PICKED UP NUTPLATES ON SERVICEABLE TRACK IAW CRJ SRM 51-42-06. REAMED AFT MOUNT BUSHING ON TRACK I AW CRJ AMM 20-26-00. INSTALLED SERVICEABLE TRACK P/N 228-50809-803 IAW CRJ AMM 78-34-11. PERFORMED OPS CHECK OF RT THRU ST REVERSER IAW CRJ AMM 71-00-00. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007100900190 20071009 00190 EU 2007 10 9 USAA920070870 1 20070927 A 2913 PUMP AIRBUS 320 A320232 3930326 EU NR 1 ENGINE LEAKING A USAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 EA 19 619AW 527 CREW REPORTED GREEN HYDRAULIC SYSTEM DRAINED DOWN CAUSING AN AMBER INDICATION WHEN GEAR WAS EXTENDED. CREW DECLARED AN EMERGENCY. THE LANDING WAS UNEVENTFUL. MX REPLACED THE NR 1 ENGINE HYDRAULIC PUMP. OPERATIONAL / LEAK CHECK WAS GOOD. OPEN 2 L 7 2 4F RT A28NM 2007100900191 20071009 00191 NM 2007 10 9 KCSA071435 1 20071001 A 5311 FRAME BOEING 747 7472B4B 138481B NM BS 440 S10-11L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 OUTER FLANGE OF FRAME AT SKIN ATTACHMENT AT STA-440 BETWEEN STR-10L AND STR-11L IS CRACKED .5 INCHES. 2 L 7 4 4F RT A20WE 2007100900192 20071009 00192 NM 2007 10 9 KCSA071436 1 20071001 A 5311 FRAME BOEING 747 7472B4B 138481B NM BS 440 S11-12L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 OUTER FLANGE OF FRAME AT SKIN ATTACHMENT AT STA-440 BEWTEEN STR-11L AND STR-12L IS CRACKED .75 INCH. 2 L 7 4 4F RT A20WE 2007100900193 20071009 00193 EU 2007 10 9 TRAX200701406 1 20070926 A 5310 DOOR FRAME AEROSP ATR72 ATR72 EU BS 6695 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 CARGO DOOR FRAME AT STA 6695.5 CRACKED. 10-16-07 HFEC PERFORMED BY HEATHAIR W/O 37536 CRACK CONFIRMED CARGO DOOR F RAME STA 6695.5 REPAIRED WITH DOUBLER IAW SRAS DO/TS-4166/07. REPAIRED INSTERCOSTAL ON CARGO DOOR PER EC EO 72-52-0107. 2 H 7 2 4T RT 2007100900194 20071009 00194 EA 2007 10 9 TRAX200701407 1 20070926 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 364 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 855AS 7395 CORROSION FOUND ON FRAME 364.00 AROUND RIVET OF INTERCOSTAL SKIN BETWEEN STR 26 RT & STR 27 RT. 10-9-07 CORROSION RE MOVED ON FRAME 364 AROUND RIVET OF INTERCOSTAL & SKIN BTW STR 26 & 27 RT IAW SRM 51-21-06 RIVETS REPLACED IAW SRM 51-4 2-06 MATERIAL THICKNESS: 0.050. MATERIAL REMOVED: 0.001 WITHIN LIMITS AS PER SRM: 53-00-00 2 L 7 2 4F RT A21EA 2007100900195 20071009 00195 EA 2007 10 9 TRAX200701408 1 20070926 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 349 S23LR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 855AS 7395 ETNRC - FS 349.00, BETWEEN STR 23R - 23L, LOWER FRAME SEGMENT IS CORRODED. 10-11-07 CORROSION REMOVED AT FS 349.00 B TW STR 23R - 23L IAW SRM 51-21-06 RIVETS REPLACED & IAW SRM 51-42-06 MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.00 2 WITHIN LIMITS AS PER SRM: 53-00-00. 2 L 7 2 4F RT A21EA 2007100900198 20071009 00198 EA 2007 10 9 TRAX200701412 1 20070926 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 PAX DOOR WILL NOT OPEN. 2 L 7 2 4F RT A21EA 2007100900200 20071009 00200 NM 2007 10 9 USAA920070863 1 20070928 A 5330 6936693 SKIN BOEING 737 7373Y0 1384671 NM BS 700 S27LR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 PHX - MAJOR REPAIR - NR 4313819, CRACKED FUSELAGE SKIN, BS 700, S27L - S27R. REPAIRED FUSELAGE SKIN, BS 700, S27L - S27 R IAW B737-300 SRM 53-60-12-2R2. 2 L 7 2 4F RT A16WE 2007100900201 20071009 00201 NM 2007 10 9 USAA920070864 1 20070930 A 5330 6545774 SKIN BOEING 737 7373B7 1384580 NM BS 727E S18L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 530AU 24412 PIT - MAJOR REPAIR - NR 4231314, CRACKED FUSELAGE SKIN, BS 727E, S18L. REPAIRED FUSELAGE SKIN, BS 727E, S18L IAW B737-3 00 SRM 53-00-01 FIGURE 201. 2 L 7 2 4F RT A16WE 2007100900205 20071009 00205 SO 2007 10 9 C2XA07CL084 1 20070927 A 5297 W1717001024 WIRE EMB 145 EMB145LR 3260212 SO DOOR INDICATOR BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14993 145289 THE CREW REPORTED THE MAIN CABIN DOOR WOULD NOT INDICATE LATCH CLOSED. MAINTENANCE INSPECTED AND REPAIRED WIRE W717-001 0-24. MAIN CABIN DOOR WARNING OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007100900208 20071009 00208 NM 2007 10 9 USAA920070869 1 20070928 A 5320 6552842 FLOOR SUPPORT BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6505166, CRACKED FLOOR SUPPORT CHANNEL, BS 537, BL 0 - RBL 25, WL 208.1. REPLACED FLOOR SUPPORT CHANNEL, BS 537, BL 0 - RBL 25, WL 208.1 IAW B737-300 AMM 20-50-11. 2 L 7 2 4F RT A16WE 2007100900210 20071009 00210 EU 2007 10 9 USAA920070872 1 20070928 A 5320 D5348804320200 SILL AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 631AW 077 MCN - MAJOR REPAIR - C-06 CHECK - NR 6504497, CORROSION ON THE L2 DOOR CUTOUT LOWER SILL FITTING, BS 3158 - BS 3257, S23 L. REPAIRED THE L2 DOOR CUTOUT LOWER SILL FITTING, BS 3158 - BS 3257, S23L IAW A320 SRM 53-41-14. 2 L 7 2 4F RT A28NM 2007100900212 20071009 00212 EA 2007 10 9 TRAX200701457 1 20071001 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STICKING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 PAX DOOR DIFFICULT TO OPEN FROM INSIDE. 2 L 7 2 4F RT A21EA 2007100900213 20071009 00213 EA 2007 10 9 TRAX200701418 1 20070927 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 717EV 10088 CAPTAIN`S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007101000005 20071010 00005 NM 2007 10 10 USAA920070908 1 20071004 A 5320 65C326772 SHEAR WEB BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6505192, CRACKED CABIN FLOOR SHEAR WEB, BS 986, LBL 45, WL 208. REPLACED CABIN FLO OR SHEAR WEB, BS 986, LBL 45, WL 208 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007101000010 20071010 00010 EA 2007 10 10 TRAX200701460 1 20071002 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 908EV 7654 SECOND FROM FRONT CEILING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007101000011 20071010 00011 EA 2007 10 10 TRAX200701416 1 20070927 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 870AS 7530 PAX ENTRY DOOR WOULD NOT CLOSE. 2 L 7 2 4F RT A21EA 2007101000013 20071010 00013 NM 2007 10 10 BB07080 1 20071006 A 3350 CONTROL PANEL BOEING 757 7572S7 1384962 NM EMERGENCY LIGHTS FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 902AW 23322 MAINTENANCE FOUND THAT EMERGENCY LIGHTS WILL NOT ARM. REPLACED THE FLIGHT DECK OVERHEAD EMERGENCY LIGHT PANEL. NO FURT HER FAULTS. 2 L 7 2 4F RT A2NM 2007101000014 20071010 00014 EU 2007 10 10 YENA2007083 1 20070927 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU CABIN ODOR A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 565JB 2031 AN INSIDIOUS ELECTRICAL ODOR FROM CAPT'S SIDE OF FLT DECK THROUGHOUT FLIGHT. THE ODOR WAS NOT CONSTANT BUT CYCLIC AND W OULD BE ERRATIC. NOT ABLE TO ISOLATE TO A SPECIFIC SOURCE, DEFINITELY NOTICEABLE. TALKED TO FLIGHT CREW. UNABLE TO ID ENTIFY ODOR. NO CIRCUIT BREAKER TRIPPED. NO ECAM WARNING. NO ODOR DETECTED. OK FOR SERVICE IAW TSM 24-00-00-810-823. TURNED ON ALL LIGHTS AND WINDOW HEAT ON FULL POWER, NOTHING ABNORMAL. ALSO TURNED LTV SCREENS FULL ON, CHECK OK. ALSO PERFORMED TSM 23-39-00-810-801 FOR LTV. ALL NORMAL. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2007101000015 20071010 00015 SO 2007 10 10 C2XA07ON024 1 20070925 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS FAULTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12175 145878 FLT MX - ONT - SERVICE & ROUTINE CHECK - DURING PRELIMINARY INSPECTION EXIT SIGN AT SEAT ROW 3A WAS FOUND INOP. MX PERS ONNEL REMOVED AND INSTALLED NR 3 INVERTER IAW EMB 145 AMM 33-50-00. OPERATIONALLY CHECKED GOOD AND AIRCRAFT WAS RELEASE D TO RETURN FOR SERVICE IN AIRWORTHY CONDITIONS. 2 L 7 2 4F RT 2007101000019 20071010 00019 NM 2007 10 10 HNAA0700187 1 20070810 A 3230 83231029103 UPLOCK HOOK DHAV DHC8 DHC8102 2809003 NM MLG WORN A HNAA C ABORTED TAKEOFF J WARNING INDICATION CL CLIMB 1 EA 07 839EX 226 AFTER GEAR RETRACTION LEFT GEAR DOOR REMAINED IN YELLOW. CYCLED GEAR PER PROCEDURE THEN THE LEFT GEAR WOULD NOT COME DO WN AT ALL. USED ALTERNATE EXTENSION, GOT ALL GREEN LIGHTS. CIRCLED AND RETURNED TO HPN. NO EMERGENCY WAS DECLARED BUT CAPTAIN DID REQUEST CFR TRUCKS. FOUND LEFT GEAR ACTUATOR UPLOCK HOOK WORN. REPLACED BUSHING, RIGGED ACTUATOR AND PROX SWITCH IAW -8 MM 32-10-21, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007101000020 20071010 00020 EA 2007 10 10 TRAX200701436 1 20070928 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 855AS 7395 ETNRC - FOUND CORROSION ON CROSSBEAM AT 281 JLE POSITION (CARGO) FLOOR ATTACHMENT HOLE. 10-11-07 CORROSION ON CROSS B EAM REMOVED IAW SRM 51-21-06, ALODINE APPLIED IAW SRM 51-21-11, PRIMER APPLIED IAW SRM 51-25-06 AND WHITE TOPCOUT APPLIE D IAW SRM 51-25-16 MATERIAL THICKNESS: 0.120 MATERIAL REMOVED: 0.003 WITHIN LIMITS AS PER SRM: 53-00-00 FIG 1. 2 L 7 2 4F RT A21EA 2007101000022 20071010 00022 NM 2007 10 10 USAA920070883 1 20070926 A 5320 141N8631 PAN BOEING 757 757225 1384959 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916UW 22192 PIT - MAJOR REPAIR - C-4 CHECK, CORROSION ON THE FORWARD LAVATORY SERVICING DOOR CUTOUT PRESSURE PAN, BS 418 - BS 428, S 27L - S29L. REPLACED THE FORWARD LAVATORY SERVICING DOOR CUTOUT PRESSURE PAN, BS 418 - BS 428, S27L - S29L IAW B757 DRA WING 141N8631. 2 L 7 2 4F RT A2NM 2007101000023 20071010 00023 EU 2007 10 10 USAA920070884 1 20070928 A 5330 D53480023201 SKIN AIRBUS 320 A320231 3930325 EU ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 644AW 317 SAL - MAJOR REPAIR - NR 5979790 - CORROSION ON EXTERNAL FUSELAGE SKIN BETWEEN BS 3310 / FR 69 TO BS 3366 / FR 70 AND S31 R TO S32R. REPAIRED FUSELAGE SKIN BETWEEN BS 3310 / FR 69 TO BS 3366 / FR 70 AND S31R TO S32R IAW A320 SRM 53-41-11, PA GE 239-244, FIG 205. 2 L 7 2 4F RT A28NM 2007101000027 20071010 00027 NM 2007 10 10 BB07079 1 20071003 A 2910 UNKNOWN BOEING 767 7672B7 1385107 NM HYD SYSTEM LEAKING A USAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 251AY 24764 FLIGHT 715, VCE-PHL: CREW REPORTED LOSS OF CENTER HYDRAULIC SYSTEM PRESSURE INBOUND TO PHL. FLIGHT LANDED NORMALLY. M AINTENANCE REPLACED THE YAW DAMPER SERVO, LT CENTER ELEVATOR PCA, AND LT GEAR DOWNLOCK ACTUATOR. 2 L 7 2 4F RT A1NM 2007101000028 20071010 00028 NM 2007 10 10 KCSA071454 1 20071008 A 5412 BULKHEAD BOEING 747 747SR46 1384816 NM NR 3 NACELLE WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 NR 3 PYLON ENG PRESSURE LINE AT NAC STA 221.9 WORN INTO BULKHEAD. 2 L 7 4 4F RT A20WE 2007101000029 20071010 00029 NM 2007 10 10 KCSA071455 1 20071008 A 5412 BULKHEAD BOEING 747 747SR46 1384816 NM NR 4 NACELLE WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 NR 4 PYLON HYD LINE B-NUT WORN INTO NAC STA 221.9 BULKHEAD. 2 L 7 4 4F RT A20WE 2007101000030 20071010 00030 EU 2007 10 10 TRAX200701438 1 20070927 A 3210 TRUSS AEROSP ATR72 ATR72 EU RT MLG CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 ETNRC - RIGHT MLG TRUSS CRACKED AT FR 26. 10-16-07 HFEC PERFORMED W/O 37536 END OF CRACKS MARKED ON MLG TRUSS. C UTOUT IN RT MLG TRUSS CARRIED OUT IAW DWG 15S535R0199 HFEC PERFORMED AROUND CUT-OUT W/O 37536 NO CRACKS FOUND. REPAIR PERFORMED PER SRM 51-24-04. REPAIRED CRACKS IN RT MLG TRUSS SHEAR MEMBER PER TC EO 72-53-0253 AND SRI DO/TS 4126-07-929 . 2 H 7 2 4T RT 2007101000031 20071010 00031 2007 10 10 ZZDA2007276 4 20071001 A 2565 D29982225 SLIDE BOEING 717 717200 1383700 NM L1 DOOR UNSERVICEABLE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 960AT 55022 L1 DOOR LANYARD SLIDE PIN OUT. REMOVED AND REPLACED L1 SLIDE REF M/M 26-61. 2 L 7 2 4F TR A6WE 2007101000032 20071010 00032 NM 2007 10 10 KCSA071440 1 20071004 A 5315 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 560 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FORWARD BILGE FLOORBEAM IS DAMAGED ON THE FORWARD SIDE OF UPPER CHORD AT STA 560, RBL 20. 2 L 7 4 4F RT A20WE 2007101000033 20071010 00033 NM 2007 10 10 KCSA071437 1 20071004 A 5412 BULKHEAD BOEING 747 747249F 1384849 NM NR 4 NACELLE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 NR 4 PYLON NAC STA 179 VERTICAL BULKHEAD HAS SHEARED FASTENER AND CRACKED (1 INCH) IN WEB. 2 L 7 4 4F A20WE 2007101000034 20071010 00034 NM 2007 10 10 MWEA070230 1 20071002 A 5522 SKIN DOUG MD88 MD88 3023688 NM LT ELEVATOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 822ME 49759 LEFT ELEVATOR AT STATION XHS 45 HAS A LIGHTNING STRIKE AT TOP TRAILING EDGE. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 2007101000035 20071010 00035 EU 2007 10 10 USAA920070897 1 20070927 A 5554 D5537131800200 HINGE FITTING AIRBUS 320 A320231 3930325 EU ZONE 300 WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 644AW 317 SAL - MAJOR REPAIR - C-04 CHECK - NR 5975509, RUDDER HINGE FITTING NR 3 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STA 2279 / RIB 5. REPLACED RUDDER HINGE FITTING 3, VERTICAL STABILIZER STA 2279 RIB 5 IAW A320 AMM 55-36-41. 2 L 7 2 4F RT A28NM 2007101000036 20071010 00036 EU 2007 10 10 USAA920070898 1 20070924 A 5554 D5537131800200 HINGE FITTING AIRBUS 320 A320231 3930325 EU ZONE 300 WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 644AW 317 SAL - MAJOR REPAIR - C-04 CHECK - NR 5975507, RUDDER HINGE FITTING NR 4 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STA 2632 RIB 6. REPLACED RUDDER HINGE FITTING NR 4, VERTICAL STABILIZER STA 2632 RIB 6 IAW A320 AMM 55-36-41. 2 L 7 2 4F RT A28NM 2007101000037 20071010 00037 NM 2007 10 10 KCSA071441 1 20071004 A 5411 FRAME BOEING 747 7472B4B 138481B NM NR 2 NACELLE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 NR 2 PYLON INBOARD REAR ENGINE MOUNT BULKHEAD FRAME IS CORRODED AROUND A FASTENER AT NAC STA 221.90. 2 L 7 4 4F RT A20WE 2007101000038 20071010 00038 NM 2007 10 10 CALA0700540 1 20070927 A 5330 507945 SKIN BOEING 737 7373T0 1384582 NM BS 312 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A .5 INCH CRACK IN INTERIOR SKIN AT 4TH DOOR STOP FROM BOTTOM OF L-1 DOOR, STA 312, S13L. THE DOOR SKI N WAS REPAIRED IAW ECRA 5210-01954. 2 L 7 2 4F RT A16WE 2007101000039 20071010 00039 NM 2007 10 10 CALA0700542 1 20070927 A 5210 507945 PAN BOEING 737 7373T0 1384582 NM L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A .75 INCH CRACK IN L-1 DOOR PAN ON AFT SIDE AT 5TH DOOR STOP FROM BOTTOM. THE DOOR PAN WAS REPAIRED I AW ECRA 5210-01954. 2 L 7 2 4F RT A16WE 2007101000040 20071010 00040 NM 2007 10 10 CALA0700543 1 20070927 A 5730 65C26271 SKIN BOEING 737 7373T0 1384582 NM RT WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70330 23460 INSPECTION FOUND A .75 INCH CRACK IN RIGHT WING LEADING EDGE SKIN AT NR 5 SLAT ACTUATOR. THE SKIN WAS REPAIRED IAW SRM 57-41-01, PAGE 202, FIGURE 201. 2 L 7 2 4F RT A16WE 2007101000041 20071010 00041 SO 2007 10 10 RAIA00709039 1 20070928 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INTERMITTENT A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 840HK 145341 POST FLT NR 7976 - RIC - EMERGENCY LIGHTS AT GALLEY AND EXIT ROW FACING AFT ILLUMINATE INTERMITTENTLY. MAINTENANCE REMO VED AND REPLACED LEFT INVERTER AND CLEANED LIGHT SOCKET. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007101000042 20071010 00042 SO 2007 10 10 RAIA00709031 1 20070923 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A RAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 03 825HK 145510 POST FLT NR 5522 - STL - PAX DOOR DIFFICULT TO OPEN. MAINTENANCE LUBRICATED MAIN DOOR ROLLERS AND CLEANED ACTUATING CAM S. NO FURTHER FAULTS NOTED. 2 L 7 2 4T RT T00011AT 2007101000044 20071010 00044 SO 2007 10 10 RAIA00709041 1 20070930 A 3244 315501 TIRE EMB 145 EMB145 3260210 SO MLG BLEW OUT A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 803HK 145077 FLT NR 3506 - BDL - ABORTED T/O AND BLEW NR 1 MAIN WHEEL ASSY. MAINTENANCE REMOVED AND REPLACED NR 1 MAIN LANDING GEAR TIRE/WHEEL ASSY. CHECKS GOOD. 2 L 7 2 4F RT T00011AT 2007101000045 20071010 00045 SO 2007 10 10 RAIA00709040 1 20070928 A 3297 CONNECTOR EMB 145 EMB145 3260210 SO PROX SENSOR DIRTY A RAIA O OTHER N FALSE WARNING LD LANDING 1 CE 03 820HK 145064 FLT NR 5568 - STL - LANDING GEAR AIR/GROUND FAIL MESSSAGE. MAINTENANCE CLEANED PROX SWITCH CONNECTOR. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007101000046 20071010 00046 SO 2007 10 10 RAIA00709030 1 20070922 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 812HK 145373 PRE FLT NR 5557 - STL - EMERGENCY LIGHT FLOOR PROXIMITY LIGHTS IS OUT. MAINTENANCE RE-SOLDERED WIRE, OPS CHECK OF EMERG ENCY LIGHTING OK. 2 L 7 2 4T RT T00011AT 2007101000048 20071010 00048 WP 2007 10 10 ABXA070324 1 20070928 A 3246 95608595 WHEEL DOUG DC9 DC941 302207N WP NR 4 MLG SEPARATED A ABXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 962AX 83 47768 AIRCRAFT BLOCKED IN WITH NR 4 MAIN TIRE FLAT. FOUND NR 4 WHEEL RIM SEPARATED. REPLACED NR 4 MAIN WHEEL ASSEMBLY, NR 4 BRAKE AND THE RIGHT MAIN LANDING GEAR PISTON AND AXLE ASSEMBLY IAW DC9 MM CHAPTER 32. 2 L 7 2 4F A6WE 2007101000049 20071010 00049 WP 2007 10 10 MWEA070228 1 20070927 A 5230 59101415 PAN DOUG DC9 DC981 3022081 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 814ME 48010 MID CARGO OUTER PAN IS CRACKED AT STOP BEAM NR 1 FORWARD END UNDER RADIUS BLOCK. REMOVED AND REPLACED PAN. 2 L 7 2 4F A6WE 2007101000050 20071010 00050 NM 2007 10 10 USAA920070853 1 20070925 A 5310 6555074 GUSSET BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 PHX - MAJOR REPAIR - NR 4163756, PILOTS NR 1 WINDOW FRAME GUSSET CRACKED, BS 196.5 - BS 203.8, S9L - S10L. REPAIRED PIL OTS NR 1 WINDOW FRAME GUSSET, BS 196.5 - BS 203.8, S9L - S10L IAW B737-300 SRM 53-10-01-2R REPAIR 10, FIGURE 201. 2 L 7 2 4F RT A16WE 2007101000053 20071010 00053 NM 2007 10 10 USAA920070861 1 20070926 A 5315 BAC1505100880 FLOORBEAM BOEING 757 757225 1384959 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916UW 22192 PIT - MAJOR REPAIR - C-4 CHECK, CORROSION ON FLOORBEAM T-CAP, BS 365.25. REPAIRED FLOORBEAM T-CAP, BS 365.25 IAW USAIRW AYS TYPICAL REPAIR 53-15-01. 2 L 7 2 4F RT A2NM 2007101000054 20071010 00054 EU 2007 10 10 USAA920070862 1 20070913 A 5320 D5398004303 SILL AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 644AW 317 SAL - MAJOR REPAIR - C-04 CHECK - NR 5975814, CORROSION ON THE R2 DOOR CUT OUT LOWER SILL, BS 2786 / FR 66. REPAIRED TH E R2 DOOR CUTOUT LOWER SILL, BS 2786 / FR 66 IAW A320 SRM 53-41-14. 2 L 7 2 4F RT A28NM 2007101000058 20071010 00058 SO 2007 10 10 RAIA00709037 1 20070927 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DIRTY A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 833HK 145240 PRE FLT NR 7947 - ORD - EMERGENCY LIGHT LEFTHAND OVERWING EXIT IDENTIFIER IS INOP. MAINTENANCE CLEANED CONNECTOR. OPS CHECKS GOOD ON GROUND. 2 L 7 2 4T RT T00011AT 2007101000061 20071010 00061 SO 2007 10 10 RAIA00709036 1 20070926 A 3350 BULB EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT BURNED OUT A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 808HK 145157 PRE FLT NR 3567 - RIC - EMERGENCY LIGHT NR 1 MAIN DOOR EXTERIOR FLOODLIGHT INOP. MAINTENANCE REMOVED AND REPLACED LIGHT BULB. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007101000062 20071010 00062 NM 2007 10 10 CALA0700555 1 20071002 A 5340 651768464 STRINGER CLIP BOEING 737 7373T0 1384582 NM BS 294.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR CUTOUT FORWARD SIDE STA 294.5 AT STRINGER 10L ANGLE CLIP. THE CLIP WAS REM OVED AND REPLACED IAW ECRA 5311-01361. 2 L 7 2 4F RT A16WE 2007101000064 20071010 00064 NM 2007 10 10 CALA0700557 1 20071002 A 5320 6517684 WEB BOEING 737 7373T0 1384582 NM BS 303.9 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR CUTOUT FORWARD SIDE STA 303.9 AT STRINGER 16L WEB. THE WEB WAS REMOVED AND REPLACED IAW ECRA 5311-01362. 2 L 7 2 4F RT A16WE 2007101000065 20071010 00065 NM 2007 10 10 CALA0700558 1 20071002 A 5320 6517684 WEB BOEING 737 7373T0 1384582 NM BS 294.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR CUTOUT FORWARD SIDE STA 294.5 AT STRINGER 16L WEB. THE WEB WAS REMOVED AND REPLACED IAW ECRA 5311-01362. 2 L 7 2 4F RT A16WE 2007101000066 20071010 00066 NM 2007 10 10 CALA0700559 1 20071002 A 5320 6517684 WEB BOEING 737 7373T0 1384582 NM BS 294.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR CUTOUT FORWARD SIDE STA 294.5 AT STRINGER 15L WEB. THE WEB WAS REMOVED AND REPLACED IAW ECRA 5311-01362. 2 L 7 2 4F RT A16WE 2007101000067 20071010 00067 NM 2007 10 10 CALA0700560 1 20071002 A 5340 66142081 STRINGER CLIP BOEING 737 7373T0 1384582 NM BS 294.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR CUTOUT FORWARD SIDE STA 294.5 AT STRINGER 11L FORWARD SUPPORT CLIP. THE CL IP WAS REMOVED AND REPLACED IAW ECRA 5311-01362. 2 L 7 2 4F RT A16WE 2007101000068 20071010 00068 NM 2007 10 10 CALA0700561 1 20071002 A 5320 6517684 WEB BOEING 737 7373T0 1384582 NM BS 294.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR CUTOUT FORWARD SIDE STA 294.5 AND STRINGER 12L WEB. THE WEB WAS REMOVED AN D REPLACED IAW ECRA 5311-01362. 2 L 7 2 4F RT A16WE 2007101000069 20071010 00069 NM 2007 10 10 CALA0700562 1 20071003 A 5322 69730575 SHEAR TIE BOEING 737 7373T0 1384582 NM BS 500D CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14325 23455 INSPECTION FOUND A .5 INCH CRACK IN LEFT FRAME SHEAR TIE AT STA 500D BETWEEN STRINGERS 10L AND 11L. THE SHEAR TIE WAS R EMOVED AND A NEW SHEAR TIE WAS INSTALLED IAW BOEING DRAWING 69-73057 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007101000070 20071010 00070 SO 2007 10 10 C2XA07RI083 1 20070924 A 3397 WIRE EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHT BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14925 145004 EWR - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY LIGHT PATH STRIP NOT WORKING. MX FOUND STRIP WIRE BROKEN. MX REPA IRED THE WIRING AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007101000072 20071010 00072 NM 2007 10 10 SWAA074866 1 20070930 A 5310 6545819 PANEL BOEING 737 7373T0 1384582 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED HC2 CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT BS 259, LBL 7.75. REPAIRED CEILING PANEL PER ACO. 2 L 7 2 4F RT A16WE 2007101000077 20071010 00077 NM 2007 10 10 SWAA074879 1 20071001 A 5311 6546548 FRAME BOEING 737 7375H4 138449D NM BS 747 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007101000080 20071010 00080 NM 2007 10 10 USAA920070875 1 20071002 A 5340 141N83219 STRINGER CLIP BOEING 757 7572S7 1384962 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 903AW 23323 MCN - MAJOR REPAIR - C-12 CHECK - NR 5976925, CRACKED CLIP ANGLE, BS 350, S8L. REPLACED CLIP ANGLE, BS 350, S8L IAW B75 7-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007101000081 20071010 00081 NM 2007 10 10 USAA920070876 1 20071002 A 5340 141N83219 STRINGER CLIP BOEING 757 7572S7 1384962 NM ZONE 200 - FUSEL CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 903AW 23323 MCN - MAJOR REPAIR - C-12 CHECK - NR 5976926, CRACKED CLIP ANGLE, BS 365.25, S8L. REPLACED CLIP ANGLE, BS 365.25, S8L I AW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007101000086 20071010 00086 NM 2007 10 10 USAA920070881 1 20071002 A 5320 ANGLE BOEING 737 7373B7 1384580 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT - MAJOR REPAIR - FPBH INSPECTION, CRACKED ANGLE, BS 360, S14L - S15L. REPLACED ANGLE, BS 360, S14L - S15L IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007100500089 20071005 00089 NM 2007 10 5 2007UALA03833 1 20070922 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 FWD GALLEY DOOR S/N 1247 AFT FRAME IS CRACKED AT 4TH STOP FITTING. FABRICATED & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007100500095 20071005 00095 NM 2007 10 5 2007UALA03950 1 20070927 A 3350 SIGN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU DOOR 1L EXIT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 334UA 24229 CABIN DOOR 1L EXIT MARKER DOES NOT ILLUMINATE. REPAIRED WIRE W132-074-20 AT DISCONNECT SPLICE LOCATED AT SERVICE ACCESS S PANEL AFT OF COCKPIT DOOR. OP'S CHK'D GOOD PER BASE JIC I2117. 2 L 7 2 4F 4 F RT A16WE E21EU 2007100500096 20071005 00096 NM 2007 10 5 2007UALA03951 1 20070927 A 2750 BACR13CF2A RELAY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE TE FLAPS FAULTED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 196UA 28715 LOST PRIMARY FLAPS ON ALT MODE. 10-23-07 REPLACED RELAYS R7515 & R7513 IN PANEL P54 AS PER SSM 27-51-02 & 03 AND P ER FIM TASK 27-51 883-8 84.RAN FLAPS ON GROUND-NO FAULTS-OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007100500097 20071005 00097 NM 2007 10 5 2007UALA03952 1 20070927 A 3520 OXYGEN BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE PSU READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 501UA 24622 THE O2 BOTTLE AT SEAT 15A IS LOW. 2 L 7 2 4F 4 F RT A2NM E17NE 2007100500104 20071005 00104 NM 2007 10 5 2007UALA03959 1 20070929 A 2751 WARNING MESSAGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TE FLAPS ILLUMINATED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 582UA 26702 FLIGHT DIVERTED DUE TO FLAP DISAGREE STATUS MESSAGE. LANDED UNDER AMBER ALERT AND TAXIED TO GATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007100500105 20071005 00105 NM 2007 10 5 2007UALA03960 1 20070928 A 3231 SELECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE MLG DOOR MALFUNCTIONED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 807UA 798 GEAR DID NOT EXTEND, USED GRAVITY EXTENSION AND LOST NOSE STEERING, TOWED TO GATE. 10-19-07 FOUND AFT MLG DOOR SE LECTOR VALVE INOPERATIVE. REPLACED AFT MLG DOOR SELECTOR VALVE 41GA AND 37GA. DOORS OPEN AND CLOSE NORMALLY. NO RE PEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007100500107 20071005 00107 NE 2007 10 5 2007UALA03962 2 20071002 A 7200 EEC BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 ENGINE UNKNOWN A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 780UA 26944 777043 RTFL DUE TO NR 1 ENG ELECTRONIC ENGINE CONTROL ISSUES. 10-26-07 TROUBLESHOOTING ISOLATED PROBLEM TO P2 MANIFOLD (PRE SSURE INPUT) P2 MANIFOLD IS BLOCKED OR LEAKING. HAD ELECTRONIC ENGINE CONTROL MSG ON L ENG, CH B. CHECKED CONNECTIONS O N P2 MANIFOLD AND LINES, FOUND SECURE. FOUND PIN HOLE LEAK ON BRAIDED P2 SENSE WHICH ATTACHES TO EEC. REPLACED LINE. ACC OMPLISHED EEC TEST ON MAT AND ACCEPTED ENGINE. ACCOMP ENGINE RUN. A/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007100500110 20071005 00110 NM 2007 10 5 2007UALA03965 1 20071001 A 2780 SLAT SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LE SLATS MALFUNCTIONED A UALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 29 379UA 24654 ON TAXI OUT LEADING EDGE SLATS WENT FROM RETRACT TO FULL EXTEND AND BACK WHEN COMMANDED TO 5 DEG. REPLACED NR 2 DSWC. 2 L 7 2 4F 4 F RT A16WE E21EU 2007100500119 20071005 00119 NM 2007 10 5 UPS07450804 1 20071001 A 3350 LIGHT BOEING 747 747123F NM CABIN INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:N/A EMERGENCY LIGHT INOP MCD CEILING FWD OF CREW ENTRY STAIRS. OPERATION CHECKS NORMAL 747 MM 33-51-00. 2 L 7 4 4F A20WE 2007100500131 20071005 00131 NM 2007 10 5 2007UALA03842 1 20070922 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY LIGHTS ON THE STAIRS TO THE UPPER DECK AND AROUND BLINK ON AND OFF. 10-19-07 SECURED EEL STRIP ON STAIRS TO UPPER DECK. OP CHECKED GOOD FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007100500132 20071005 00132 NM 2007 10 5 2007UALA03843 1 20070923 A 3350 CHARGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 RIGHT OVERWING AFT TWO EMERGENCY LIGHT ASSY IS INOP. 10-19-07 REPLACED BATTERY CHARGER UNIT. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007100500133 20071005 00133 NM 2007 10 5 2007UALA03844 1 20070922 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EEL AT 35 HJK, 33 ABC, 4E AFT & AT 43 ABC ARE INOPERATIVE. 10-19-07 RELAMPED ALL SEAT POSITION EEL. OP CHECKS GOO D FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007100500135 20071005 00135 NM 2007 10 5 2007UALA03846 1 20070922 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EEL INOP AT 5E AFT. 10-19-07 SECURED LAMP CONNECTOR. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007100500137 20071005 00137 NM 2007 10 5 2007UALA03848 1 20070922 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EEL INOP ROWS 12-14 & 18. 10-19-07 FOUND CABLE DISCONNECTED. RECONNECTED. OP CHECKS NORMALLY. SUSPECT CABLE DISCO NNECTED FOR CLEANING/ MTCE AND NOT RECONNECTED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007100500139 20071005 00139 NM 2007 10 5 UPS07M50746 1 20070716 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZONTAL STAB RIGHT NR 36 BARREL NUT BORE FOUND CORRODED. CORR AT BARREL NUT BORE REMOVED PER SRM 5 1-21-01 VII R38. BORE BOTTOM REMN BLEND OUT 0.160" DEEP & BORE REAMED TO 2.572" DIA, BOTTOM MACHINED DOWN 0.070" DEEP. BARREL NUT BORE, BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS, SMOOTHEN & PROTECTED. SLEEVE BUSHING FAB, PROTECTED & INST ALLED. FAB & INSTALLED REPAIR DOUBLER & TAPER FILLERS. REPAIR C/O ACCEPTABLE PER EN1445-07. 2 L 7 3 4F RT A22WE 2007100500140 20071005 00140 NM 2007 10 5 UPS07M50747 1 20070718 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT BORE LT 15 FOUND WITH CORROSION. CORR AT BARREL NUT BORE REMOVED PER SRM 51-21-01 VII R38. BORE BOTTOM SURFACE REMN BLEND OUT DEPTH 0.050" DEEP. BORE REAMED TO 1.067" DIA, REM N BLEND OUT DEPTH 0.040" DEEP, EXCEEDED LIMITS. BARREL NUT BORE, BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHEN & P ROTECTED. SLEEVE BUSHING FAB, PROTECTED & INSTALLED. REPAIR C/O ACCEPTABLE PER EN 1447-07. 2 L 7 3 4F RT A22WE 2007100500141 20071005 00141 NM 2007 10 5 UPS07M50748 1 20070717 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT BORE RT NR 9 FOUND WITH CORROSION. CORR AT BARREL NUT BOR E REMOVED PER SRM 51-21-01 VII R38. BORE BOTTOM REMN BLEND OUT 0.025" DEEP. BORE REAMED TO 0.988" DIA. REMN BLEND OUT 0.050" DEEP, EXCEEDED LIMITS. BARREL NUT BORE, BLEND OUT VOID & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. SLEEVE BUSHING FAB, PROTECTED & INSTALL. REPAIR C/O AT BARREL NUT BORE NR 9 RT ACCEPTABLE PER EN 1443-07. 2 L 7 3 4F RT A22WE 2007100500165 20071005 00165 NM 2007 10 5 2007UALA03857 1 20070922 A 2750 FLAP SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TE FLAPS MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 583UA 26705 CREW REPORT: T/E FLAP DISAGREE GOING FLAPS 20 TO 25. 2 L 7 2 4F 4 F RT A2NM E17NE 2007100500185 20071005 00185 NM 2007 10 5 2007UALA03988 1 20070929 A 2612 CONTROL PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FIRE CONTROL FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 337UA 24241 DISCHARGE LIGHT, NR 1 ENGINE, LT BOTTLE, DOES NOT ILLUMINATE WITH MASTER DIM TEST. REPLACED ENGINE AND APU FIRE CONTROL PANEL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007100500191 20071005 00191 EA 2007 10 5 TRAX200701390 1 20070924 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 409-559 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 855AS 7395 ETNRC - FLOOR ANGLE CORRODED LT AND RT BETWEEN FS 409 + 128 TO FS 559. 2 L 7 2 4F RT A21EA 2007100500199 20071005 00199 NM 2007 10 5 SWAA074838 1 20070927 A 5312 6545819 WEB BOEING 737 7373H4 1384600 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED MV1 CHECK, FOUND NLG W/W RIGHT ACCESS PANEL CUTOUT WEB CRACKED AT BS 247. REPAIRED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2007100900005 20071009 00005 NM 2007 10 9 C1HA200786002 1 20071001 A 5315 FLOORBEAM BOEING 727 7272S7 138407Z NM BS 1030 CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 686CA 22021 BS 1030 FLOORBEAM CORROSION LBL 25 - RBL 25 TOP SURFACE UPPER CHORD. REMOVED AND REPLACED PREVIOUS UPPER "T" CHORD REPA IR IAW B727 SRM 53-10-8 FIG 3. 2 L 7 3 4F A3WE 2007100900012 20071009 00012 NM 2007 10 9 NWAA073295810 1 20070923 A 2597 CONNECTOR BOEING 757 757351 1384991 NM OVEN CROSSED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 01 590NW 32990 DURING FLIGHT HAD UNUSUAL SMOKE LIKE ODOR REPORTED IN MOST OF THE CABIN. MAINTENANCE FOUND CONNECTORS WERE CROSS MATED AND NR 15 MALE PIN ON THE OVEN SIDE WAS BURNT. REMOVED AND REPLACED OVEN AND OPERATIONAL CHECKED GOOD. AIRCRAFT HAS RE TURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007100900018 20071009 00018 EU 2007 10 9 07FDEA04309 1 20070926 A 5313 A53610567224 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 CORROSION ON STRINGER 44 LT, BETWEEN FRAME 16A-17. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-12-14/FIG 201. 2 L 7 2 4F RT A35EU 2007100900027 20071009 00027 EU 2007 10 9 07FDEA04456 1 20071002 A 5340 A53610607 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION AT RUN OUT FITTING P44 LT/RT, C17 REPAIR PERFORMED BY REPLACEMENT OF PART IAW DRAWING R536-10440. 2 L 7 2 4F RT A35EU 2007100900029 20071009 00029 EU 2007 10 9 07FDEA04458 1 20071002 A 5313 A53973306200 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION AT STRINGER SEGMENT C 72, 45 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100900040 20071009 00040 EU 2007 10 9 07FDEA04120 1 20070920 A 5311 A53973898 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 HEAVY CORROSION ON MILLED FRAME 59A BETWEEN STRG 40-42 RT. REPAIR PERFORMED BY CUT OUT DAMAGED PORTION AND PARTIAL REPL ACEMENT OF FRAME IAW DRW R539-70138 ISSUE F, APPROVED BY EA 6-5317-82873 AND RAS/DAHAM/4019557/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100900047 20071009 00047 GL 2007 10 9 07FDEA04381 2 20070929 A 7200 CF66D ENGINE DOUG MD10 MD1010F 3022112 WP GE CF6 CF66D 30020 GL NR 1 DAMAGED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 25 386FE 59298 5730 46620 451250 CLIMBING THROUGH FL190 AIRCRAFT SHUDDERED TWICE WITH SLIGHT YAW TO LEFT. LOOKED DOWN AND "ENG 1 EXCEEDENCE" ALERT AND R ED BOXED ENG 1 EGT "951". PULLED ENG 1 TO IDLE AND RAN ENG FIRE SEVERE DAMAGE CHECKLIST. SHUTDOWN NR 1, PULLED NR 1 FI RE HANDLE AND RTBED TO KJAX. BORESCOPED NR 1 ENG COMPRESSOR, HAS 3RD STAGE TIP CLANG (B1-3 PORT ). REQUIRES ENG CHANGE PER 72-00-00-6. REMOVED AND REPLACED NR 1 ENGINE, REF MD-10 WORK CARD 71T0101-1. OK FOR SERVICE. 2 L 7 3 4F 4 F RT A22WE E23EA 2007100900049 20071009 00049 NM 2007 10 9 AALA20071804 1 20070924 A 2910 S271T0054 O-RING BOEING 757 757223 1384957 NM HYD SYSTEM LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 190AA 32384 LAX INFLIGHT T162/24SEP - LEFT HYDRAULIC QUANTITY EICAS MESSAGE WITH RESERVOIR ANNUNCIATION. GEAR AND FLAPS LOWERED NOR MALLY. QUANTITY STABILIZED AT 0.27. LANDED LAX WITHOUT INCIDENT. FOUND DELTA P LEAKING ON LEFT PYLON. REPLACED O-RIN G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007100900055 20071009 00055 NM 2007 10 9 DU4R2007167 1 20070913 A 5410 FITTING BOEING 757 757232 1384965 NM NR 1 PYLON WORN B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 642DL 23996 FOUND DEEPLY WORN CORNER FITTING OF NR 1 PYLON LT AFT LOWER CORNER AT AFT ENGINE MOUNTS. REPAIRED BY BLENDING, HFEC NO RELEVANT INDICATIONS, FABRICATING AND INSTALLING REPAIR GUSSET 4.34" BY 2.88" BY 1.2" FROM 7050-T7451 IAW DELTA EA NR 46 3490-14AD DATED 9/12/07 APPROVED BY FAA FORM 8100-9. 2 L 7 2 4F RT A2NM 2007100900056 20071009 00056 EU 2007 10 9 07FDEA04121 1 20070920 A 5311 A53973557 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORROSION ON MILLED FRAME 63A BETWEEN STRG 32-35 AND STRG 39-41 RT. REPAIR PERFORMED BY SMOOTH BLEND OUT, HFEC INSPECTI ON FOR NIL FINDINGS AND FLAP PEENING IAW EA 6-5317-82874 AND RAS/DAHAM/4019554/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100900059 20071009 00059 EU 2007 10 9 07FDEA04124 1 20070920 A 5330 A53981540 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 OLD DOUBLER REPAIR BETWEEN FRAME 72-73, STRG 29-32 LT IS NOT CONFORM TO SRM 53-10-12/FIG 225/SH 2, DOUBLER THICKNESS IS 1,6MM INSTEAD OF 1,8MM. REPAIR PERFORMED BY INSTALLING NEW SKIN DOUBLER IAW SRM 53-10-12/FIG 228/SH 2. 2 L 7 2 4F RT A35EU 2007100900061 20071009 00061 EU 2007 10 9 07FDEA04126 1 20070920 A 5313 A53981540220 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 803FD 378 DURING CHANGING OLD DOUBLER REPAIR BETWEEN FRAME 72-73, STRG 29-32 LT FOUND LESS EGDE MARGING IN STRINGER 32 LT. STRING ER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007100900062 20071009 00062 EU 2007 10 9 07FDEA04128 1 20070920 A 5330 A53773487 SKIN AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FUSELAGE SKIN AT LAP JOINT P 51, C 19-20 INTERNAL CORRODED REPAIR PERFORMED BY CUT OUT THE LAP JOINT AND INSTALL EXTERNA L DOUBLER IAW DRAWING R537-06279, APPROVED BY RAS/DABRE/7003251/2003 ISS A. 2 L 7 2 4F RT A35EU 2007100900074 20071009 00074 EU 2007 10 9 07FDEA04389 1 20071001 A 5315 A53974219220 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND CROSSBEAM C 63 CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100900077 20071009 00077 EA 2007 10 9 A6WA200740539 1 20070906 A 5230 601R3505025 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 425AW 7663 CARGO DOOR FORWARD TRACK BOTTOM CHANNEL, P/N 601R35050-25 IS CRACKED. MAINTENANCE REMOVED AND INSTALLED SERVICEABLE CHA NNEL P/N 601R35050-25 IAW CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007100900081 20071009 00081 EU 2007 10 9 07FDEA04333 1 20070927 A 5310 A53989431212 BUTT JOINT AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 CORROSION ON BUTT-JOINT BETWEEN FRAME 101-102, STGR 23 RT. REPLACEMENT OF L-SEGMENT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100900086 20071009 00086 WP 2007 10 9 07FDEA04338 1 20070927 A 5712 ARB1161507 RIB DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 RT WING L/E INT STRUCTURE FOUND CRACK ON UPPER RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I. 2 L 7 3 4F A22WE 2007100900093 20071009 00093 EA 2007 10 9 CHQA20070051 1 20071001 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE MALFUNCTIONED A CHQA O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 465SM 7612 GEE873561 CRP TO IAH - ON FINAL APPROACH INTO IAH SELECTED GEAR DOWN AND RECEIVED A GEAR DISAGREE WARNING MESSAGE. CREW CYCLED GE AR A SECOND TIME AND RECEIVED A 3 GREEN AND LOCKED INDICATION. TOWER WAS ASKED TO VERIFY THAT ALL THREE GEAR WERE DOWN AND LOCKED, AND TOWER CONFIRMED THAT THERE WERE THREE DOWN AND LOCKED. CREW WENT THOUGH APPROPRIATE QRH CHECKLISTS AND PREPARED TO LAND. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LANDING GEAR AND PERFORMED SEVERAL GEAR SWIN GS WITHOUT BEING ABLE TO REPRODUCE THE FAULT, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007100900099 20071009 00099 EU 2007 10 9 07FDEA04344 1 20070927 A 5753 A57970100015 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 FAILED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 806FD 458 FOUND OLD DOUBLER REPAIR ON LOWER PANEL, CENTER BOX OF INBOARD FLAP RT, RIB 9-11, NOT IAW SRM 57-52-12/FIG 205, DOUBLER EDGES, LENGTH OF DOUBLER SHEET NOT ALLOWED. REPAIR RENEWED AS PER SRM 57-52-12/FIG 205, RIB 9. REPAIRED AS PER SRM 51- 40-51/FIG 202, ALL IAW EA 6-5752-82935 AND RAS/DABRE/7005009/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100900101 20071009 00101 EU 2007 10 9 07FDEA04346 1 20070927 A 5730 A57350004 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 ELONGATED HYDRAULIC FITTING HOLE NR 1 ON RT WING LOWER SKIN, PYLON SUPPORT BRACKET, RIB 8. REPAIR OF HOLE NR 1 PERFORME D BY OVERSIZING AND BUSHING IAW EA 6-5720-82851 AND RAS/BAE/1000639/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100900106 20071009 00106 NM 2007 10 9 07FDEA04351 1 20070927 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 MAIN CARGO DECK, STA 560 RBL 1-24, WL 208, FLOORBEAM TOP SURFACE HAS CORROSION. REMOVED AND REPLACED FLOORBEAM TEE CAP AND ANGLES IAW SR 27-53-034. 2 L 7 3 4F RT A3WE 2007100900109 20071009 00109 EU 2007 10 9 TRAX200701449 1 20071001 A 5730 SKIN AEROSP ATR72 ATR72 EU LT WING CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 LEFT WING FLANGE OF ACCESS 522CT CORRODED. 10-11-07 LT WING FLANGE 522 CT AREA, CORROSION REMOVED IAW SRM 57-14-12 FI G 401. FLANGE WITHING LIMITS (MATERIAL REMAINING), 0748 IAW SRM 57-14-12. HFEC PERFORMED BY HEATHAIR AMO 46-90 W/O 375 36 IAW NTM NO CRACKS FOUND. 2 H 7 2 4T RT 2007100900119 20071009 00119 NM 2007 10 9 KCSA071448 1 20071007 A 5420 STIFFENER BOEING 747 7472B4B 138481B NM NR 3 PYLON WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 NR 3 PYLON LOWER SPAR O/B STIFFENER WORN AT PNEUMATIC. DUCT ANTI-ROTATION CLIP BETWEEN NAC STA 180 AND 219. 2 L 7 4 4F RT A20WE 2007100900122 20071009 00122 NM 2007 10 9 KCSA071444 1 20071007 A 5320 WEB BOEING 747 747SR46 1384816 NM BS 1660-1680 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 AFT PIT BILGE TORQUE BOX UPPER WEB DAMAGED AT PREVIOUS REPAIR BETWEEN BS 1660 AND 1680, BL 0. 2 L 7 4 4F RT A20WE 2007100900130 20071009 00130 EA 2007 10 9 TRAX200701469 1 20071003 A 5210 STEP CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 719EV 10099 PAX DOOR BOTTOM STEP CRACKED AND LOOSE AT ROD END ATTACH POINT. 2 L 7 2 4F RT A21EA 2007100900131 20071009 00131 EA 2007 10 9 TRAX200701470 1 20071003 A 3150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA ILLUMINATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 878AS 7590 GEAR DISAGREE AND NOSE DOOR OPEN. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007100900146 20071009 00146 NM 2007 10 9 SWAA074841 1 20070927 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 328 S20L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007100900156 20071009 00156 NM 2007 10 9 2007UALA03994 1 20070930 A 3397 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 C-ZONE FLOOR PROXIMITY LIGHTS INOP ON LEFT SIDE. 10-26-07 REMOVED AND REPLACED BATTERY PACK PER MM 33-51-07 , ALSO FOUND LIGHT BAR FEEDER BROKEN IN BETWEEN LH AFT LAVS, REPAIRED PER GN-MM 2-0-15-005 AND OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007100900162 20071009 00162 NM 2007 10 9 SWAA074900 1 20071002 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 247WN 32508 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 3 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007100900165 20071009 00165 NM 2007 10 9 SWAA074916 1 20071002 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 605SW 27956 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 907, LBL 3. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007100900166 20071009 00166 NM 2007 10 9 SWAA074914 1 20071002 A 5311 6546550 FRAME BOEING 737 7375H4 138449D NM BS 787 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007100900179 20071009 00179 EA 2007 10 9 TRAX200701399 1 20070925 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA BS 349-409 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 855AS 7395 ETNRC - LEFT AND RIGHT SEAT TRACKS CORRODED BETWEEN FS 349 TO FS 409 AT LBL 9 AND RBL 9. 10-16-07 REPLACED CORRODE D SEAT RAILS AS PER SRM 51-41-02. 2 L 7 2 4F RT A21EA 2007100900180 20071009 00180 EA 2007 10 9 TRAX200701400 1 20070925 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 909EV 7658 EMERGENCY EXIT SIGN OVER THE AISLE IS BROKEN. 2 L 7 2 4F RT A21EA 2007100900199 20071009 00199 EA 2007 10 9 TRAX200701413 1 20070927 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 755EV 10185 CEILING EMERGENCY LIGHT THIRD FROM FRONT INOP. 2 L 7 2 4F RT A21EA 2007100900202 20071009 00202 NM 2007 10 9 USAA920070865 1 20070927 A 5320 6545819U45 GUSSET BOEING 737 7373B7 1384580 NM BS 259 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 23380 CLT - MAJOR REPAIR - NR 7718326, CRACKED NOSE LANDING GEAR ACTUATOR UPPER ATTACH BRACKET GUSSET, BS 259.5, WL 190. REPL ACED NOSE LANDING GEAR ACTUATOR UPPER ATTACH BRACKET GUSSET, BS 259.5, WL 190 IAW 737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007100900203 20071009 00203 NM 2007 10 9 SB07081 1 20070924 A 3233 65446103 ACTUATOR BOEING 737 7373B7 1384580 NM NLG FAULTY A USAA O OTHER O OTHER AP APPROACH 1 EA 19 505AU 88053 17 23380 NAS - FLT 1833 ON APPROACH TO NAS FROM PHL, CREW STATED THE NOSE LANDING GEAR DID NOT EXTEND ON GEAR EXTENSION. NO GEA R INDICATION WAS RECEIVED, JUST THE LACK OF NOISE/VIBRATION FROM THE GEAR NOT EXTENDING. CREW VERIFIED NOSE LANDING GEA R WAS NOT EXTENDED VIA THE VIEW PORT. PER QRH, MANUAL GEAR EXTENSION PROCEDURE WAS ACCOMPLISHED. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR EXTENSION AND RETRACTION ACTUATOR PER MM 32-33-11. OPERATIONAL CHECK AND LEAK CHECK GOOD. SWUNG GEAR. GEAR SWIN G CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2007101000004 20071010 00004 EU 2007 10 10 USAA920070907 1 20070925 A 5411 D54630731200 SPAR AIRBUS 320 A320231 3930325 EU ZONE 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 636AW 098 MAJOR REPAIR - C-04 CHECK - NR 5989697, RIGHT PYLON OUTBOARD SPAR CRACKED, RIB 6. REPAIRED RIGHT PYLON OUTBOARD SPAR, R IB 6 IAW A320 SRM 54-52-12 FIGURE 203. 2 L 7 2 4F RT A28NM 2007101000087 20071010 00087 EA 2007 10 10 S9BA200700017 1 20070924 A 2197 M835369026M RELAY DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA A/C PACK BURNED A S9BA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 29 573SA 573 SMOKE ODOR IN CABIN. FOUND A/C RELAY BURNED UP. DEFERRED AIR CONDITIONING IAW MEL 21-1 WILL PROVIDE SUPPLEMENTAL INFORMA TION WHEN GENERATED. REMOVED AND REPLACED RELAY M83536/9-026M. NO SN THIS ACTION CLEARED DMI 8743 ACTT 19842.6 ACTC 43 532 1 H 7 2 3T 4 T RT A9EA E4EA 2007101000088 20071010 00088 EA 2007 10 10 S9BA200700020 1 20071009 A 5730 SKIN DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA RT WING CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 888PV 620 "OPEN" RT WING BOTTOM SKIN CORRODED OB OF NACELLE AT STATION 147. 1 H 7 2 3T 4 T RT A9EA E4EA 2007101000089 20071010 00089 EA 2007 10 10 S9BA200700019 1 20071009 A 5730 SKIN DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA LT WING CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 888PV 620 "OPEN" LT WING IB PLANK DOUBLER (STATION 30) CORRODED AT LEADING EDGE. 1 H 7 2 3T 4 T RT A9EA E4EA 2007101000090 20071010 00090 EA 2007 10 10 S9BA200700015 1 20070917 A 5511 SPAR DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA HORIZONTAL STAB CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 19820 125 573 CORROSION FOUND ON FORWARD SPAR OF HORIZONTAL STABILIZER AT SEA FIN MOUNT. (STATION 92)REMOVED AND REPLACED HORIZONTAL STABILIZER. 1 H 7 2 3T 4 T RT A9EA E4EA 2007101000093 20071010 00093 NE 2007 10 10 HEER117344 1 20070913 A 5313 9220202103151 STRINGER SKRSKY S92 S92A NE GE CT7TS CT78A 30136 NE BS 292 CRACKED D HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 592PH 2484 920027 J-STRINGER FOUND CRACKED ACROSS FWD 5 FASTENERS IN RT CABIN OVERHEAD AT STATION 292, BL 10.5. FIRST FASTENER ON STRINGE R ATTACHES TO HAT SECTION SUPPORT FOR TRANSFER MODULE ON ROOF. REMOVED STRINGER, CONTACTED TECH REP FOR MATERIAL SPECS AND PN. ALSO DID NDT ON ROOF. CRS GRANTED PERMISSION TO LOCALLY FABRICATE. STRINGER FOUND NOT TO BE DEBURRED AT ALL F ASTENER HOLES. 2 G 7 2 4U 4 U R00024BO E8NE 2007101000094 20071010 00094 WP 2007 10 10 P3MB0709001 1 20070901 A 5730 SKIN DOUG DC9 DC915 3022036 WP PWA JT8 JT8D7 52053 NE LT WING DENTED I P3MB K NONE O OTHER IN INSP/MAINT 1 SO 29 305PA 45740 DURING POST FLIGHT INSPECTION, FOUND BIRD STRIKE DAMAGE ON LT WING LEADING EDGE, DAMAGE WAS A DENT APROX 8 INCHES LONG, 4 INCHES WIDE AND 1 INCH DEEP, WITH A TEAR IN THE FORM OF A "T" 5 INCHES VERTICAL BY 4 INCHES HORIZONTAL, SECTION OF LEA DING EDGE WAS REMOVED AND SENT FOR REPAIR. REPAIRS WERE MADE SRM 57-06. UNIT REINSTALLED ON AIRCRAFT. 2 L 7 2 4F 4 F A6WE E2EA 2007101000095 20071010 00095 NM 2007 10 10 PIDR07005 1 20070911 A 5330 SKIN BOEING 737 737300 1384610 NM BS 460 CORRODED D PIDR K NONE O OTHER IN INSP/MAINT 1 SO 05 XAUGL 22958 DURING MAINTENANCE CHECK, NOTED CORROSION IN FUSELAGE SKIN AT DME ANTENNA AT BS 460. REPAIRED IAW EA 53-257. 2 L 7 2 4F RT A16WE 2007101000096 20071010 00096 NM 2007 10 10 PIDR07004 1 20070913 A 5330 SKIN BOEING 737 737300 1384610 NM BS 846-861 GOUGED D PIDR K NONE O OTHER IN INSP/MAINT 1 SO 05 XAUGL 22958 DURING MAINTENANCE CHECK, NOTED GOUGE IN FUSELAGE SKIN AT STRINGER 21RT BETWEEN BS 846 AND BS 861. REPAIRED IAW SRM 53- 00-01, FIG 201, REPAIR 32. 2 L 7 2 4F RT A16WE 2007101000099 20071010 00099 NE 2007 10 10 HEEA117386 1 20070918 A 2913 9265015811101 PUMP SKRSKY S92 S92A NE GE CT7TS CT78A 30136 NE HYD SYSTEM FAILED D HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 992PH 114 920055 ENROUTE, NR 2 HYDRAULIC GAUGE DECREASE TO ZERO RED RANGE. NO HYDRAULIC LIGHT ILLUMINATED. CONTINUED AND GAUGE DECREASE D TO ZERO AT IDLE. MAINTENANCE FOUND THE NR 2 HYDRAULIC PUMP HAD FAILED. REPLACED PUMP. 2 G 7 2 4U 4 U R00024BO E8NE 2007101000100 20071010 00100 CE 2007 10 10 DJFA2007108 1 20070909 A 2120 UNKNOWN BEECH MU300 400A 1155402 CE CABIN ODOR E DJFA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 465LX RK454 DURING FLIGHT CREW NOTED A BURNING ODOR FROM THE COPILOTS AIR VENT. AIRCRAFT LANDED SAFELY AT ITS DESTINATION. MAINTEN ANCE COULD NOT DUPLICATE THE DISCREPANCY. NO BURNING ODOR WAS NOTED. 2 H 7 2 4F RT A16SW 2007101000106 20071010 00106 CE 2007 10 10 GUUA09220701 1 20070922 A 3260 H111541 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG INOPERATIVE A GUUA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 29 87554 UE227 AFTER TAKEOFF LANDING GEAR UNSAFE LIGHTS ILLUMINATED WITH LANDING GEAR IN THE UP POSITION. REPLACED LANDING GEAR UPLOCK SWITCH. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101000108 20071010 00108 CE 2007 10 10 GUUA09220703 1 20070922 A 5220 DOOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE EMERGENCY EXIT OUT OF ADJUST A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 69547 UE189 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT AFT EMERGENCY HATCH INNER HANDLE HARD TO OPEN. ADJUSTED RT AFT EMERG ENCY HATCH HANDLE. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101000110 20071010 00110 CE 2007 10 10 GLBA20061006 1 20070924 A 5311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 177 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 210GL UE210 FUSELAGE FRAME CRACKED APPROXIMATELY .8 INCH IN LENGTH AT FS 177 AT STRINGER 9AR. CRACKED AT STRINGER CUTOUT ON FRAME. R EPAIRED FUSELAGE FRAME CRACK AT STRINGER RELIEF HOL AT F.S. 177 STRINGER 9AR. REPAIR APPROXIMATELY 4.4 INCH BY 2.5 INCH .080 2024 T-3. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101000111 20071010 00111 CE 2007 10 10 GUUA09170701 1 20070917 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE PWA 118 PW118 NE LT MLG MALFUNCTIONED A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 29 190YV 17407 UE190 DURING APPROACH "H" OF THE LT "H" LANDING GEAR POSITION INDICATING LIGHTS ONLY ILLUMINATED ON THE THIRD CYCLING OF THE L ANDING GEAR. REPLACED LT MAIN LANDING GEAR ACTUATOR OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E20NE 2007101000113 20071010 00113 EU 2007 10 10 SA07062 1 20070926 A 7932 3957985114 INTERFACE UNIT AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE ZONE 400 INACCURATE A USAA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 19 741UW 21251 1269 575133 BOS - FLT 1266 EN ROUTE BOS TO BDA. DURING CLIMB, AROUND 17,000 FEET, CREW RECEIVED AN ECAM WARNING FOR OIL QUANTITY ON THE NUMBER ONE ENGINE. AFTERWARDS, THE ENGINE OIL AND IDG OIL TEMPERATURES BEGAN TO RISE. THE CREW DECLARED AN EMERGE NCY, AND SHUT DOWN THE NUMBER ONE ENGINE AS REQUIRED BY PROCEDURE. THE FLIGHT RETURNED TO BOS AND LANDED WITHOUT FURTHE R INCIDENT. SINGLE ENGINE TIME WAS 15 MINUTES. MAINTENANCE INSPECTED ENGINE CHIP DETECTORS, AND CHECKED FUEL ODOR IN A N OIL SAMPLE. NO FAULTS WERE FOUND. REPLACED THE ENGINE INTERFACE UNIT AND PERFORMED AN ENGINE RUN. THE ENGINE OIL TE MPERATURES WERE WITHIN LIMITS. 2 L 7 2 4F 4 F RT A28NM E37NE 2007101000114 20071010 00114 EA 2007 10 10 QXEA200701440 1 20070918 A 3297 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE NR 2 BRAKE UNKNOWN A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 617QX 10130 BRAKE OVERHEAT WARNING ON TAKEOFF, RT BRAKE TEMP WENT TO 13-14 ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO THE GATE. MAI NTENANCE DISCONNECTED AND RECONNECTED CONNECTOR PLUG TO THE NR 2 BRAKE. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007101000119 20071010 00119 CE 2007 10 10 DXTA200702498 1 20070925 A 2750 602751 DOWNLOCK SWITCH CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 916QS 7243 7500116 AFTER TAKEOFF, FLAPS RETRACT AND INDICATE UP, BUT SPEED TAPE REMAINS RED IF AIRCRAFT ACCELERATES OVER 210 KTS. T/S FOUND RT MLG DOWN AND LOCK SWITCH BAD. REMOVED AND REPLACED SWITCH. OPS CHECKED SATISFACTORY IAW MM CH 32-30-04. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007101000120 20071010 00120 2007 10 10 DXTA200702499 4 20070925 A 3460 COMPUTER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE FLT GUIDANCE MALFUNCTIONED E DXTA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 399QS 5600510 ON TAKEOFF, JUST AS WE REACHED 40 KIAS, RT PFD BLANKED OUT, AFTER 0 SECONDS A RED X APPEARED, APPX 10 SECONDS AFTER THAT ATT IND AND RMI REAPPEARED BUT NO ADC INFO. SELECTING ADC REV DID NOT RESTORE DATA. ABORTED T/O. RESEATED THE CO-PILOT S FLIGHT GUIDANCE COMPUTER AND PFD. PERFORMED SEVERAL OPERATIONAL TESTS ON THE GROUND AND DURING TAXI. TESTS CHECK GO OD. WORK DONE IAW MM, CH 34-00-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007101000123 20071010 00123 2007 10 10 DXTA200702504 4 20070927 A 3160 DISPLAY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE RIGHT INOPERATIVE E DXTA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 399QS 5600510 AT 60 KNOTS, RT PFD WENT BLANK. DURING ABORTED TAKEOFF RT PFD FLICKERED 2 TIMES WITH A RED X DISPLAYED. AFTER RED X DIS PLAYED PFD WENT BLANK TO NORMAL. UNABLE TO DUPLICATE DISCREPANCY. TROUBLESHOT SYSTEM. FOUND GROUND CONNECTOR CCS20 LOOSE . TIGHTENED GROUND CONNECTOR, OPERATIONAL TEST CHECKS GOOD. MAINTENANCE DONE IAW MFG WIRING DIAGRAM NR 9612674 2 L 7 2 4F 4 F RT A22CE E25EA 2007101000127 20071010 00127 NM 2007 10 10 UPS07550755 1 20070927 A 5610 WINDSHIELD BOEING 757 75724APF 1384969 NM COCKPIT FAILED A IPXA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 402UP 23724 INSPECTION TYPE:N/A DIVERSION - R1 WINDSHIELD ARCED & SHATTERED IN FLIGHT. REPLACED R1 WINDOW PER MM 56-11-01-4. 2 L 7 2 4F RT A2NM 2007101000131 20071010 00131 NM 2007 10 10 UPS07M50742 1 20070814 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1921 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C CABIN - RIGHT STA 1921 Y=-107.25 SEAT TRACK FOUND CORROSION AS MARKED. CABIN RIGHT STA 1921 X=-107.25 CORROSION ON SEAT TRACK REMOVED FOUND EXCEEDS LIMITS. RIGHT NR 4 DOOR SILL PLATE REMOVED. CORRODED SEAT TRACK TRIMMED OFF & AREA REPROTECTED. NEW SEAT TRACK REWORKED, FASTENER HOLES P/U & REPROTECTED. HFEC INSP CUTOUT ON TRIMMED OFF AR EA, FOUND NO CRACK SEAT TRACK SPLICE HAT, SPLICE PLATE FAB, HOLES PICK UP, PROTECT. 2 L 7 3 4F RT A22WE 2007101000134 20071010 00134 NM 2007 10 10 UPS07M50745 1 20070718 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT BORE LEFT NR 21 FOUND WITH CORROSION. CORROSION AT BARREL NUT BORE REMOVED PER SRM 51-21-01 VII R38. BORE BOTTOM SURFACE CLEANED. BORE REAMED TO 1.067" DIA & FOUND REMN BLEND OUT 0.037" DEEP, EXCEEDS LIMITS. BARREL NUT BORE, BLEND OUT VOID & BOTTOM PERIPHERY RADIUS SMOOTHEN, PROTECTED. SLEEVE BUSHING FAB, PROTECTED & INSTALLED. REPAIR C/O AT BARREL NUT BORE NR 21 LEFT ACCEPTABLE PER EN 1449-07. 2 L 7 3 4F RT A22WE 2007101000135 20071010 00135 SO 2007 10 10 C2XA07SH073 1 20070921 A 5751 14573900411 SHROUD EMB 145 EMB145EP 3260221 SO RT AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14947 145054 SHV - DURING C-CHECK MAINTENANCE FOUND RT LOWER AILERON SHROUD WITH CORRODED BONDING PLATES. MAINTENANCE REPAIRED RT LO WER AILERON SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007101000138 20071010 00138 SO 2007 10 10 C2XA07SH076 1 20070921 A 5751 14574000405 SHROUD EMB 145 EMB145EP 3260221 SO LT AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14947 145054 SHV - DURING C-CHECK MAINTENANCE FOUND LT LOWER AILERON SHROUD WITH CORRODED BONDING PLATES. MAINTENANCE REPAIRED LT AI LERON LOWER SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007101000139 20071010 00139 SO 2007 10 10 C2XA07SH077 1 20070921 A 5320 14521700001 FLOOR SUPPORT EMB 145 EMB145EP 3260221 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14947 145054 SHV - DURING C-CHECK MAINTENANCE FOUND RT OMEGA BEAM WITH CORROSION BETWEEN FRAMES 18 & 19. MAINTENANCE REPAIRED RT OME GA BEAM AT FRAME 18 IAW EMB 145 EC 5510-01381. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007101000141 20071010 00141 SO 2007 10 10 C2XA07SH079 1 20070921 A 5310 14540326404 PANEL EMB 145 EMB145LR 3260212 SO FUSELAGE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16546 145562 SHV - DURING C-CHECK MAINTENANCE FOUND PANEL 191 FR WITH COMPOSITE DAMAGE AND TORN EROSION TAPE. MAINTENANCE REPAIRED P NL 191 FR IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007101000142 20071010 00142 SO 2007 10 10 C2XA07SH080 1 20070921 A 5330 14540326403 PANEL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16546 145562 SHV - DURING C-CHECK MAINTENANCE FOUND PANEL 191EL WITH BONDING PLATES CORRODED. MAINTENANCE REPAIRED PANEL 191EL IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007101000143 20071010 00143 SO 2007 10 10 C2XA07RI087 1 20070927 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO CARGO BAY MALFUNCTIONED A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 27 34110 12567 84 145658 FLT 2507 - MEM - CREW REPORTED BAG SMOKE ON EICAS IN FLIGHT AND ON GROUND. NEITHER SMOKE NOR FIRE OBSERVED. EWR MX REM OVED AND REPLACED AFT BAG SMOKE DETECTOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO S ERVICE. 2 L 7 2 4F RT 2007101000147 20071010 00147 NM 2007 10 10 KCSA071430 1 20070928 A 5412 BULKHEAD BOEING 747 7472B4B 138481B NM NR 1 NACELLE WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 NR 1 PYLON FWD ENGINE MOUNT BULKHEAD STA 128.95 CHORD HAS DEEP WEAR AT O/B SIDE. 2 L 7 4 4F RT A20WE 2007101000148 20071010 00148 NM 2007 10 10 KCSA071431 1 20070928 A 5210 STRUCTURE BOEING 747 7472B4B 138481B NM R1 DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 R1 DOOR FWD LOWER CORNER HAS 2 INCH CRACK IN HORIZONTAL CHORD. 2 L 7 4 4F RT A20WE 2007101000149 20071010 00149 NM 2007 10 10 ANCF200700021 1 20070924 A 2400 ELECTRICAL SYS DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE MULTIPLE FAIL W ANCF C ABORTED TAKEOFF H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 SO 23 632CT 49632 DURING TAKEOFF ROLL, HAD AN ELECTRICAL FAILURE: TAKEOFF WAS ABBORTED AT 90 KNOTS. THE FLIGHT GUIDANCE STATUS AND MAINT PNL C/B G 25 WAS TRIPPED. THE AC BUSS PHASE B C/B WAS ALSO TRIPPED. ART WAS ACCURATED. IAW AMM 24-20-00/201 GCU`S WER E CHECKED AND RESET AND IAW WDM 24-23-00 CIRCUIT WAS CHECKED AND CB`S RESET. FAULT NOT DUPLICATE.ALSO IAW AMM 72-00-00 I NLET AND EXHAUST ENGINES WERE INSPECTED. ENGINES ARE NORMAL.. 2 L 7 2 4F 4 F RT E9NE 2007101000150 20071010 00150 NM 2007 10 10 2007UALA 1 20070920 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ROW 7-13 INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 EEL LIGHTS INOP ROWS 7-13. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101000151 20071010 00151 EU 2007 10 10 2007UALA03579 1 20070904 A 2700 341203300 ROD END AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ELE SERVO CONTRL WORN A UALA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 WP 29 421UA 500 MODERATE AIRFRAME VIBRATION DURING CLIMB 320KT - 14000 STOPPED AT 300. *S/D* ELEVATOR SERVO CONTROL ROD END (LT) OUT O F RIG. REPLACED BOTH ELEVATOR SERVO ROD ENDS AND PERFORMED ELEV FREEPLAY CHECK. ALL NORMAL, NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101000162 20071010 00162 EA 2007 10 10 TRAX200701404 1 20070926 A 5740 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 838AS 7276 LT WING L/E 530JL I/B ATTACH ANGLE IS CRACKED IN UPPER AND LOWER RADIUS. REMOVED LT L/E WING ATTACH ANGLE THAT WAS CR ACKED, AND LOCATED NEW SERVICEABLE P/N 600-12045-11 AND INSTALLED, IAW CRJ SRM 51-40-11. 2 L 7 2 4F RT A21EA 2007101000163 20071010 00163 EA 2007 10 10 TRAX200701405 1 20070926 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 838AS 7276 EMERGENCY EXIT AND CLOSED PLACARD ON SERVICE DOOR UNLEDGIBLE. REMOVED UNLEDGIBLE ""CLOSED"" PLACARD AND REPLACED WITH SERVICEABLE PN S1874, IAW CRJ 200 AMM 11-20-00. JC13349. EMERGENCY EXIT PLACARD ON SERVICE DOOR WITH SERVICEABLE PLACA RD PN S1880 IAW CRJ MM 11-20-00. 2 L 7 2 4F RT A21EA 2007101000164 20071010 00164 EA 2007 10 10 TRAX200701409 1 20070926 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 876AS 7576 THE I/B CLIP AT FS 280, RBL 9 IS CRACKED. REMOVED CRACKED I/B CLIP AT FS 280 RBL 9 DUPLICATED PART IAW SRM 53-21-43. L OCATED HOLES ON SERVICEABLE I/B CLIP IAW CRJ 200 SRM 51-40-11. OK TO ALODINE AND PRIME. ALODINED PRIMED AND TOPCOATED IAW CRJ 200 SRM 51-25-00. OK TO INSTALL. INSTALLED SERVICEABLE I/B CLIP AT FS 280 RBL 9 IAW CRJ 200 SRM 51-42-20. 2 L 7 2 4F RT A21EA 2007101000166 20071010 00166 SO 2007 10 10 N93A29092007 1 20070929 A 3250 STEERING SYS GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU NLG MALFUNCTIONED E N93A O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 13 411QS 1311 NOSE STEERING PULLS TO RIGHT WHEN HANDWHEEL IS CENTERED. (OPEN) 2 L 7 2 4F 4 F RT A12EA E25NE 2007101000167 20071010 00167 WP 2007 10 10 UPS07850784 1 20070928 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1690 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 CORROSION FOUND ON OUTER FUSELAGE SKIN AT L28 LT AND FUSELAGE STATION 1690. AREA TOTALS APPROX 10 SQ INCHES. REPAIRED EXTERNAL SKIN CRACKS AT STA 1690, 1718, 1746, L28L IAW SRO 8530032. 2 L 7 4 4F RT 4A25 2007101000168 20071010 00168 WP 2007 10 10 UPS07850785 1 20070928 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1746 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 CORROSION FOUND ON OUTER SKIN AT L28 LT AND FX STATION 1746. AREA TOTALS APPROX 1 SQ INCH. SKIN APPEARS TO BE SEPARATE D AND CRACKED AT 1 EACH FASTENER. REPAIRED EXTERNAL SKIN CRACKS AT STATION 17-1721 L28L IAW SRO 8530032. 2 L 7 4 4F RT 4A25 2007101000216 20071010 00216 NE 2007 10 10 HALA0700420 2 20071001 A 7261 SEAL BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE FUEL HEATER LEAKING A HALA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM, EXCESSIVE OIL DRIPPING FROM NR 1 ENG. ACCOMPLISHED HI PWR RUN PER AMM 79-00-00-206-015-G00. FOUND ACCUMULATION OF OIL ON RT INBD COWLING (NR 1 ENG) GAUZE WRAP FROM OIL IN PORT OF FUEL SERVO HEATER FOUND WET ALONG WITH OIL ACCUMULATOR AROUND FUEL PUMP AREA. REMOVED AND REPLACED FUEL SERVO HEATER OIL IN SEAL, ACCOMPLISHED HI PWR RU N LEAK CHECK GOOD. COWLING CLOSED AND SECURED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101000226 20071010 00226 EU 2007 10 10 07FDEA04467 1 20071002 A 5313 A53974258202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION AT STRINGER SEGMENT P 56, C55/58 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007101000227 20071010 00227 EU 2007 10 10 07FDEA04468 1 20071002 A 5320 FLOOR SUPPORT AIRBUS 310 A310222 3930315 EU CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 FOUND BULK CARGO PIT BETWEEN FR 65 AND 66 AT LBL 50 FLOOR ATTACH IS CORRODED. 10-22-07 FOUND FLOOR SUPPORT TO BE C RACKED AND CORRODED OUT OF LIMITS IAW A310 SRM 53-10-00 TABLE 102; REMOVED AND REPLACED SUPPORT IAW A310 SRM 51-40-21, 51-40- 44, 53-17-15 FIG 9 ITEM 35. 2 L 7 2 4F RT A35EU 2007101000228 20071010 00228 EU 2007 10 10 07FDEA04469 1 20071002 A 5311 FRAME AIRBUS 310 A310222 3930315 EU AFTPIT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 FOUND AFT CARGO PIT AT FRAME 54.1 S-52L CORRODED. 10-29-07 REMOVED CORROSION AT STRINGER 52L FRAME 54.1 IAW A310 S RM 51-74-10, FOUND OUT OF LIMITS IAW A310 SRM 53-10-14, REMOVED STRINGER IAW A310 SRM 53-10-14, FABBRICATED NEW SRTINGER REPAIR AND 2 COUPLINGS IAW 51-10-14, ALODINED AND PRIMED REPAIR PARTS IAW A310 SRM 51-21-10 AND 51-23-10, INSTALLED STR INGER SPLICE AND COUPLINGS IAW FEDEX A310 SRM 53-10-14. 2 L 7 2 4F RT A35EU 2007101000229 20071010 00229 EU 2007 10 10 07FDEA04470 1 20071002 A 5311 FRAME AIRBUS 310 A310222 3930315 EU CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 FOUND AFT CARGO PIT AT FRAME 61 AT S-54L IS CORRODED. 10-11-07 NO GENERAL OR SPECFIC ALLOWABLE DAMAGE FOR STRINGER IAW A310 SRM 53-17-14, REMOVED STRINGER SECTION AND COUPLINGS AND FABBED NEW STRINGER SECTION AND 2 COUPLINGS IAW A3 10 SRM 53-10-14 PG 203/204, ALODINED , PRIMED AND PAINTED REPAIR PARTS IAW A310 SRM 51-21-10 AND 51-23-10. INSTALLED REPAIR PARTS IAW A310 SRM 31-10-14 PG 203/204. 2 L 7 2 4F RT A35EU 2007101000230 20071010 00230 EU 2007 10 10 07FDEA04472 1 20071002 A 5320 FLOOR SUPPORT AIRBUS 310 A310222 3930315 EU CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 FOUND BULK CARGO PIT AT FRAME 63 TO FRAME 64 AT LBL5 FLOOR BOARD SUPPORT ANGLE IS CORRODED. 10-16-07 REMOVED CORRO SION IAW A310 SRM 51-74-10, CHECKED LIMITS IAW A310 SRM 53-17-15, ORG. THICKNESS .074, REMAINING MATERIAL IS.058, FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-10-00, REMOVED FLOOR SUPPORTIAW A310 51-40-21, RECEIVED NEW FLOOR SUPPORT P/N A53474 27920200, LOCATED AND DRILLED NEW FLOOR SUPPORT IAW A310 SRM 51-40-44, INSTALLED IAW A310 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007101000231 20071010 00231 EU 2007 10 10 07FDEA04473 1 20071002 A 5313 STRINGER AIRBUS 310 A310222 3930315 EU AFT PIT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 FOUND AFT CARGO PIT BETWEEN FRAME 62 AND FRAME 63 S-56L CORRODED. 10-15-07 REMOVED CORROSION IAW A310 SRM 51-74-10 , HIGH FREQ FOR ANY CRACKS OR REMAINING CORROSION PER A310 NTM 51-10-08, FABBED REPAIR PARTS AND INSTALLED IAW A310 SRM 53-10-14 PG 204A/204B FIG201A, ALODINED, PRIMED, AND PAINTED IAW A310 SRM 51-21-10,51-23-10 AND A310 AMM 51-25-10. 2 L 7 2 4F RT A35EU 2007101000232 20071010 00232 EU 2007 10 10 07FDEA04474 1 20071002 A 5315 FLOORBEAM AIRBUS 310 A310222 3930315 EU CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 FOUND T CAP OF FLOORBEAM 66 IS CORRODED FROM RBL 47R TO LBL 47L. 10-18-07 REMOVED T CAP IAW A310 SRM 51-40-21, TEE CAP OUT OF LIMITS IAW A310 SRM 53-10-15, RECEIVED NEW FLOORBEAM AND TWO ANGLES, INSTALLED IAW 51-40-21 2 L 7 2 4F RT A35EU 2007101000233 20071010 00233 EU 2007 10 10 07FDEA04475 1 20071002 A 5320 FLOOR SUPPORT AIRBUS 310 A310322 3930334 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 FOUND BETWEEN FRAME 67 AND FRAME 64 RBL44 FLOOR SUPPORT STRUCTURE IS CORRODED. 10-22-07 REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-10-00; REMOVED AND REPLACED SUPPORT STRAP IAW A310 SRM 53-17-14 ITEM 1 FIG 9, AND 51-4 0-44 AND 51-40-21. 2 L 7 2 4F RT A35EU 2007101000241 20071010 00241 NM 2007 10 10 DLM90071274 1 20070928 A 5321 FLOOR SKIN DOUG MD90 MD9030 3023690 NM FS 150 RBL 54 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 FLOOR WEB CORRODED AT STATION 150 NAD RBL 54. REPAIRED WEB IAW MD-90 SRM 51-11-01 FIG 2 ON N/R 63278 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007101000242 20071010 00242 NM 2007 10 10 DLM90071275 1 20070927 A 5320 DRAIN DOUG MD90 MD9030 3023690 NM FS 296 L30 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 FWD CARGO COMPARTMENT FS 295 L30 DRAIN ATTACHMENT HOLES LARGER THAN ALLOWABLE LIMITS. REPAIRED DAMAGED AREA AT FS 295 L 30 IAW MD-90 FIG 12B SHEET 7ON N/R 63399 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007101000243 20071010 00243 NM 2007 10 10 DL76L071277 1 20070929 A 5414 311T345044 SKIN BOEING 767 767332 1382001 NM NR 2 NACELLE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 183DN 27110 CRACK AT FACTORY CUTOUT ON INBOARD SKIN OF NR 2 PYLON. CRACK WAS STOP DRILLED AND DOUBLERS INSTALLED. 2 L 7 2 4F RT A1NM 2007101000244 20071010 00244 NM 2007 10 10 DL76G071279 1 20071001 A 5315 BAC15063123 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 1197 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 156DL 25354 AFT COMPARTMENT STATION 1197 AT LBL 22 CARGO LOWER FLOORBEAM TOP SURFACE CORRODED. REPAIRED PER 53-00-07 REPAIR 4 FIGUR E 201 ON NON ROUTINE AMW512514. 2 L 7 2 4F RT A1NM 2007101000245 20071010 00245 NM 2007 10 10 DL76G071280 1 20071001 A 5315 BAC15063123 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 1197 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 156DL 25354 AFT COMPARTMENT STATION 1197+44 LBL 43 FLOORBEAM CORRODED TOP SIDE. REPAIRED PER 53-00-07 REPAIR 4 FIGURE 201 ON NON RO UTINE AMW516960. 2 L 7 2 4F RT A1NM 2007101100002 20071011 00002 2007 10 11 AMTA200700443 4 20070919 A 3460 4052506955 COMPUTER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE FLT MANAGE UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 517AT 27973 EICAS MSG L FMC FAIL DISPLAYED. (L) FMC BAD, REMOVED AND REPLACED LT FLIGHT MANAGEMENT COMPUTER IAW MM 34-61-01-4, OPS CHECK`S NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007101100003 20071011 00003 NM 2007 10 11 AMTA200700444 1 20070919 A 4900 APU BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE APU BAY AUTO SHUTDOWN A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 518AT 27974 APU AUTO SHUTDOWN WHILE AT GATE. INTEROGATED ECU, NO FAULTS FOUND FOR CURRENT OR PREVIOUS SHUTDOWNS, STARTED APU NORMAL START. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007101100006 20071011 00006 NM 2007 10 11 AMTA200700445 1 20070922 A 5330 SKIN BOEING 737 73783N 13844HI NM BS 797 DENTED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 310TZ 28243 RT LOWER FUSE HAS AN APPROX 14 INCH GOUGE THAT ENDS IN AN APPROX 3 INCH X 50 DENT, STA 797 BETWEEN STR 24R AND 27R JUST BELOW CARGO DOOR. REPAIRED IAW SAA EA 737-5361-09-A1102 24 MONTH TIME LIMITED REPAIR AND TRACKED BY ATA ERA 737-53R-615 8. TREATED PRIMED AND PAINTED REPAIR IAW SRM 51-20-01. (M) 2 L 7 2 4F RT A16WE 2007101100007 20071011 00007 NM 2007 10 11 AMTA200700456 1 20070922 A 5320 SUPPORT ANGLE BOEING 737 73783N 13844HI NM THRESHOLD CRACKED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 310TZ 28243 UPON REMOVAL OF AFT CARGO THRESHOLD WEB AT APPROX STA 810 FOUND SUPPORT ANGLE CRACKED. REMOVED SUPPORT ANGLE SRM 51-40- 02 FAB NEW ANGLE ON TRAVELER 7773560001 LOCATED NEW ANGLE IAW SRM 51-40-01 INSTALLED SUPPORT ANGLE SRM 51-40-02. (K) 2 L 7 2 4F RT A16WE 2007101100008 20071011 00008 NM 2007 10 11 AMTA200700457 1 20070922 A 5320 FLOOR SUPPORT BOEING 737 73783N 13844HI NM BS 787-847 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 310TZ 28243 AFT CARGO FLOOR SUPPORT HAS CORROSION FROM 787 TO 847 RBL 16.5. REMOVED CORROSION SRM 51-10-02 AND FOUND OUT OF LIMITS IAW SRM 53-00-53-1A2. FABRICATED FLOOR SUPPORT TRACK IAW EA 737-5300-09-A1104 AND INSTALLED IAW SRM 53-00-53-2R3 ITEM 4 B 1 AND 2. TREATED AND PRIMED REPAIR IAW SRM 51-20-01. (M) 2 L 7 2 4F RT A16WE 2007101100010 20071011 00010 NM 2007 10 11 DLM90071282 1 20070927 A 5210 STRUCTURE DOUG MD90 MD9030 3023690 NM L1 DOOR BENT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 L-1 DOOR LOWER LIP IS BENT IN 2 PLACES. REPAIRED LOWER LIP IAW MD-90 SRM VOL 2 51-30-01 AND 52-10-01 FIG 2 VOL 1 ON N/R 62422 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007101100013 20071011 00013 2007 10 11 DL76L071288 4 20071002 A 2210 285T0015117 MODULE BOEING 767 767332 1382001 NM FAULTED A DALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SO 27 174DN 24802 DIV DUE AUTOPILOTS WILL NOT ENGAGE-RUDDER RATIO AND AILERON LOCKOUT EICAS MSGS AND LIGHTS ILLUMINATED ON OVERHEAD PNL. MSG CAME ON A 250 KTS GOT STAB TRIM LIGHT FOR 5 SEC MSG DID NOT GO AWAY WHEN WE SLOWED DOWN OR RECONFIGURED /C. FOUND B OTH SAMS FAULTED RESET BOTH REPLACED LT SAM AS PRECAUTIONARY AP NOW EGAGE OK. TEST 30 AND TEST 40 CARRIED OUT OK. LAST FLT FAULTS SAM INFC WITH FCC-L-C-R, NO RUDDER RATIO FAULT BALLS. 2 L 7 2 4F RT A1NM 2007101100017 20071011 00017 NM 2007 10 11 AALA20071842 1 20071002 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 661AA 25295 MIA - EMERGENCY LIGHTS AT SEAT ROWS 17 TO 26 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 17 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007101100020 20071011 00020 NM 2007 10 11 AALA20071834 1 20070929 A 3350 LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 327AA 22327 JFK - EMERGENCY LIGHT AT SEAT ROW 3HJ INOPERATIVE. REPAIRED EMERGENCY LIGHT AT SEAT ROW 3HJ. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A1NM 2007101100022 20071011 00022 NM 2007 10 11 AALA20071841 1 20071001 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 758AN 32637 DFW - EMERGENCY LIGHT AT SEAT 22C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007101100024 20071011 00024 NM 2007 10 11 AALA20071838 1 20071002 A 3397 CIRCUIT BREAKER DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS TRIPPED A AALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 9414W 53189 LGA FLIGHT T1060/02OCT - AUXILIARY POWER UNIT AND EXTERNAL POWER FAILED AFTER PARKING. PASSENGERS REPORTED EMERGENCY L IGHTS IN CABIN INOPERATIVE. FLIGHT ATTENDANTS REPORTED EXIT LIGHTS ON. RESET CIRCUIT BREAKER FOR EMERGENCY LIGHTS IN C ABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2007101100026 20071011 00026 NM 2007 10 11 AALA20071833 1 20070929 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 932AN 29530 MIA - EMERGENCY LIGHT AT FORWARD RIGHT AFT OF FLIGHT ATTENDANT SEAT BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FORWARD RIGHT AFT OF FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007101100029 20071011 00029 NM 2007 10 11 AALA20071831 1 20070929 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 674AN 29424 MIA - EMERGENCY LIGHT AT SEAT 5E INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007101100031 20071011 00031 EU 2007 10 11 07FDEA04372 1 20070928 A 5712 A5796011320100 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 DURING SCHEDULED B CHECK, RT INBOARD FLAP RIB 25, P/N A5796011320100 WAS FOUND TO HAVE A 3 INCH CRACK IN THE FWD UPPER R ADIUS, REF: N00030. REMOVED AND REPLACED DAMAGED RIB REF: A300 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007101100032 20071011 00032 EU 2007 10 11 07FDEA04478 1 20071002 A 5100 UNKNOWN AIRBUS 310 A310203 3930313 EU MULTIPLE FAIL A FDEA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 SO 25 430FE 1935 1935 394 AFTER TAKEOFF CLIMBING OUT OF 3000' ECAM ALERTED AVIONICS SMOKE. NO SNIFFER FAN SMOKE OBSERVED, ECAM CLEANED THE WARNING , AND A FEW SECONDS LATER. ADVISED AGAIN AVIONICS SMOKE. THIS SECOND ECAM ALERT PROMPTED EMERGENCY RETURN AND LANDED S AFELY 26L CYVR. INSPECTED AVIONIC BAY FOR PRESENCE OF FIRE OR BURNED COMPONENTS, NO FAULT FOUND. REMOVED AND REPLACED BOTH COALESCER BAGS. REMOVED AND REPLACED SMOKE DETECTOR POSITION 11WA, 12WA, 13WA. 2 L 7 2 4F RT A35EU 2007101100033 20071011 00033 NM 2007 10 11 07FDEA04479 1 20071003 A 5753 SKIN DOUG MD11 MD11F 3023600 NM LT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 596FE 48554 LEFT WING INBOARD FLAP INBOARD SEGMENT UPPER SURFACE FOUND DENT. 10-12-07 REPAIR CARRIED OUT AT LEFT HAND WING INBO ARD FLAP INBOARD SEGMENT UPPER SURFACE AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100. 2 L 7 3 4F RT A22WE 2007101100039 20071011 00039 EU 2007 10 11 121 1 20071003 A 5320 INTERCOSTAL AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 LEFT INTERCOSTAL BETWEEN FRAMES 36 AND FRAME 38 CORROSION AROUND ANCHOR NUTS. OUT OF LIMITS PER SRM 63-61-00 FIG 301, M ATERIAL THICKNESS .080, MATERIAL REMOVED .025. SEE WC NR 2000-24 FOR FABRICATION. REPLACED LEFT INTERCOSTAL BETWEEN FRA MES 36 AND 38 PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007101100044 20071011 00044 NM 2007 10 11 GTIA200700023 1 20070904 A 3350 321430 BATTERY PACK AIRBUS A321 A321231 3940032 NM EMERGENCY LIGHTS FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 584NK 5805 1408 DURING SIMULATED LOSS OF 28VDC CHECK, THE EXIT LIGHTS OVER L1 AND R1 DOORS DO NOT ILLUMINATE. REPLACED BATTERY PACK ON EPSU 10WL. 2 L 7 2 4F RT A28NM 2007101100045 20071011 00045 EU 2007 10 11 07FDEA04471 1 20071002 A 5311 A5397422024000 FRAME AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 BULK CARGO PIT T CAP AT FRAME 64 BL0 TO LBL15 IS CORRODED NO ALLOWABLE REWORK FOR T-CAP SPECIFIED IAW A310 SRM 53-10-15, REMOVED AND REPLACED T-CAP IAW A310 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007101100046 20071011 00046 WP 2007 10 11 07FDEA04482 1 20071003 A 2497 FEEDER CABLE DOUG MD10 MD1010F 3022112 WP ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 565FE 46996 FOUND FWD CARGO POWER FEEDER CABLES CHAFED THROUGH BETWEEN 875-950. TEMP SPLICED IN NEW FEEDER CABLE, PERMANENT FIX TO FOLLOW. REPLACED DAMAGED FEEDER CABLE FROM EXT PWR CONNECTION AT STA 635 TO 1099 ELECT CONTROL PANEL LT PANEL, OPS CHE CK GOOD PER AMM 20-30-01, AMM 20-30-07. NEED TO STRING TIE FEEDER CABLE FOR EXT PWR STA 635 TO 1099. STRING TIED FEEDER CABLE FROM STA 635 TO STA 1099 AMM 20-30-07. NEED TO INSTALL SPIRAL WRAP ON FEEDER CABLES IN SUMP AREA STA 635 TO 1099. INSTALLD SPIRAL WRAP IAW EO 8-2450-7-5000-4 PER SEQ 953. 2 L 7 3 4F RT A22WE 2007101100048 20071011 00048 EU 2007 10 11 07FDEA04485 1 20071004 A 5313 A53974228200 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION AT STRINGER SEGMENT C 65, P 54 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007101100049 20071011 00049 EU 2007 10 11 07FDEA04488 1 20071004 A 5330 A53974203490 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION AT WEDGE C 70, P56-57 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100900008 20071009 00008 NM 2007 10 9 C1HA200786005 1 20071001 A 5315 1506860 FLOORBEAM BOEING 727 7272S7 138407Z NM BS 1035 CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 686CA 22021 CORROSION ON FLOORBEAM AT BS 1035 LBL 24-45. REMOVED EXISTING PART, FABRICATED NEW PART; TREATED AND PRIMED AND INSTALL ED NEW PART IAW B727 SRM 51-30-2 FIG 1 AND 3. 2 L 7 3 4F A3WE 2007100900043 20071009 00043 NM 2007 10 9 07FDEA04377 1 20070929 A 5754 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 596FE 48554 LEFT WING INBOARD FLAP, INBOARD SEGMENT LOWER SKIN FOUND DENT MARKS. 10-9-07 DENTED AREA MEASURED, DIAMETER = 2" AND DEPTH = 0.058" FOUND ACCEPTABLE AS PER SRM 57-10-00 FIGURE 17 VOLUME I. HFEC INSPECTION CARRIED PER DAC SPM REV13, 0 6-10-01.001 AND NO CRACK FOUND ON DENT AREA. REPAIR CLASSIFIED AS MINOR PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007100900045 20071009 00045 NM 2007 10 9 07FDEA04379 1 20070929 A 5730 DOUBLER DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 596FE 48554 RIGHT WING FIXED LEADING EDGE LOWER ANGLE DOUBLER AT XOS 546 FOUND CRACKED. 10-16-07 RT WING FIXED LEADING EDGE LO WER ANGLE CRACKED DOUBLER AT XOS 546 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007100900051 20071009 00051 NM 2007 10 9 AALA20071800 1 20070920 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 937AN 30082 TUL - EMERGENCY LIGHTS IN AFT COACH CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007100900053 20071009 00053 NM 2007 10 9 AALA20071802 1 20070924 A 3350 0201984002 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 383AN 26995 JFK - EMERGENCY LIGHT AT MID GALLEY RIGHT MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT MID GALLEY RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007100900068 20071009 00068 NM 2007 10 9 07FDEA04383 1 20071001 A 5311 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 596FE 48554 MAIN DECK CARGO COMPARTMENT AT STA 1761 STRINGER 12L AREA FRAME FOUND CHAFED. 10-9-07 CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CAT B REPAIR, INITIAL INSPECTION IS REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECT IONS AT EVERY 9,500 CYCLES. THIS REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007100900069 20071009 00069 NM 2007 10 9 07FDEA04384 1 20071001 A 5311 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 596FE 48554 MAIN DECK COMPARTMENT AT STA 1701 STRINGER 12R AREA FRAME EDGE FOUND CHAFED. 10-9-07 CARRIED OUT REPAIR AS PER SRM 5 3-30-00 FIGURE 1 VOLUME I. DUE TO CAT B REPAIR, INITIAL INSPECTION IS REQUIRED AT 14,500 CYCLES AND REPETITIVE INSPECTIO NS REQUIRED AT EVERY 9,500 CYCLES. THIS REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007100900071 20071009 00071 EU 2007 10 9 07FDEA04386 1 20071001 A 5414 A54611752 PANEL AIRBUS 310 A310324 3930206 EU NR 2 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND CRACK (ABOUT 6MM) AT PYLON NR 2 RIB 8 OUTBOARD SIDE WALL DOUBLER REPAIR PERFORMED IAW SRM 54-51-31 FIG 201. 2 L 7 2 4F RT A35EU 2007100900072 20071009 00072 EU 2007 10 9 07FDEA04387 1 20071001 A 5313 A53974202222 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND CORRODED STRINGER P 21 LT, BETWEEN 55/58-60 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007100900075 20071009 00075 EU 2007 10 9 07FDEA04390 1 20071001 A 5313 A53973717201 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND CORRODED STRINGER SEGMENT P 57 AT C 72 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100900080 20071009 00080 EU 2007 10 9 07FDEA04332 1 20070927 A 5320 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 CORROSION ON L-SEGMENT AT FRAME 101, STGR 14 LT TO 14 RT. REPLACEMENT OF L-SEGMENT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100900083 20071009 00083 EU 2007 10 9 07FDEA04335 1 20070927 A 5210 A52111338204 BEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 CORROSION FOUND ON LT FWD PAX DOOR, BEAM NR 1. REPAIR PERFORMED BY BLEND OUT CORROSION, NDT INSPECTION FOR CRACK FREE C ONDITION IAW EA 6-5211-92172 AND RAS/AS/215/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100900088 20071009 00088 2007 10 9 WGEA200700009 4 20071002 A 3414 1008555 ADC ECLIPS EA500 ECLIPSEEA500 3350000 SW ZONE 200 OUT OF TOLERANCE E WGEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 119DJ 114 000022 AIRSPEED DISAGREE CAUTION DURING TAKEOFF ROLL. LEFT PFD INDICATED 55 KTS, RIGHT PFD INDICATED 65KTS. PERFORMED PITOT AN D STATIC VERIFICATION TEST IAW EA500 AMM 34-10-00. FAILED AT 6000 FEET AND 71 KNOTS. REMOVED AND INSTALLED A NEW NR 2 AIR DATA COMPUTER IAW EA500 AMM 34-10-16. PERFORMED FLIGHT ENVIRONMENT DATA ADJUSTMENT AND TEST IAW EA500 AMM 34-10-00. OPS CHECK GOOD. 1 L 7 2 4J RT A00002AC 2007100900091 20071009 00091 EA 2007 10 9 CHQA20070049 1 20070909 A 3250 601R86100171 SERVO CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NLG STEERING MALFUNCTIONED A CHQA O OTHER J WARNING INDICATION LD LANDING 1 GL 11 483CA 688 7689 GEE873434 TUL TO IAH - RECEIVED STEERING INOP MSG IN FLIGHT AND THE QRH INSTRUCTIONS WERE TO LAND WITH STEERING SWITCHED OFF. DEC LARED EMERGENCY AS A PRECAUTION. LANDING WAS UNEVENTFUL AND A TUG WAS REQUESTED TO TOW THE AIRCRAFT BACK TO THE GATE. MAINTENANCE TROUBLESHOT THE STEERING PROBLEM TO THE ELECTRO HYDRAULIC STEERING SERVO. MAINTENANCE REPLACED THE STEERING SERVO AND THE STEERING SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2007100900094 20071009 00094 EU 2007 10 9 07FDEA04392 1 20071001 A 5313 A53811376200 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 FOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSIO N IAW EA 6-5315-82855 AND RAS/AS/0095/2005 ISS A. 2 L 7 2 4F RT A35EU 2007100900096 20071009 00096 NM 2007 10 9 07FDEA04341 1 20070927 A 5347 A53279239202 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 MCD SEAT TRACK FROM FR 78TO 73 BL 0 HAS 5 AREAS OF CORROSION. REMOVED AND REPLACED SEAT TRACK FROM FR 65-78 IAW SRM 51- 40-21 AND SRM 53-10-10. 2 L 7 3 4F RT A22WE 2007100900116 20071009 00116 NM 2007 10 9 KCSA071445 1 20071007 A 5310 STOP FITTING BOEING 747 747SR46 1384816 NM BS 1265 S22L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 DOOR STOP BACKUP FITTING CRACKED AT BS 1265, STR 22L. 2 L 7 4 4F RT A20WE 2007100900121 20071009 00121 NM 2007 10 9 KCSA071450 1 20071007 A 5420 STIFFENER BOEING 747 7472B4B 138481B NM NR 3 PYLON WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 NR 3 PYLON LOWER SPAR I/B STIFFENER WORN AT PNEUMATIC. DUCT ANTI-ROTATION CLIP BETWEEN NAC STA 180 AND 219. 2 L 7 4 4F RT A20WE 2007100900123 20071009 00123 EA 2007 10 9 TRAX200701461 1 20071002 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 349 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 855AS 7395 CROSS FLOORBEAM CORRODED AT FS 349, RBL 36, ATTACHED TO SERVICE DOOR. 10-11-07 ALODINE APPLIED IAW SRM 51-21-11 AND PRIMER DONE IAW SRM 51-25-06. PAINTED IAW SRM 51-25-16, MATERIAL THICKNESS: 0.080 MATERIAL REMOVED: 0.006, WITHIN L IMITS AS PER SRM: 53-00-00 FIG 101. 2 L 7 2 4F RT A21EA 2007100900127 20071009 00127 EA 2007 10 9 TRAX200701465 1 20071002 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 349 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 855AS 7395 FLOORBEAM ANGLE ON AFT SIDE OF CROSSBEAM FS 349.00 RBL 36 IS CORRODED. 10-16-07 CORROSION ON FLOOR SUPPORT ANGLE O N AFT SIDE OF CROSS BEAM FS 349.00 RBL 36 REMOVED IAW SRM 51-21-06, ANGLE REMOVED IAW SRM 51-42-06. REFER TO W/C 2000 -32 FOR FABRICATION OF FLOOR SUPPORT ANGLE AT FS 349.00 RBL 36 FABRICATED PART FLOOR SUPPORT AT FS 349.00 RBL 36.00 INST ALLED IAW SRM 51-42-06. MATERIAL THICKNESS 0.063. MATERIAL REMOVED 0.020. BEYOND SRM LIMITS 53-00-00 FIG 101. 2 L 7 2 4F RT A21EA 2007100900144 20071009 00144 EA 2007 10 9 TRAX200701424 1 20070927 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 333 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 855AS 7395 LOWER FRAME SEGMENT BETWEEN STR 23R-23L, FS 333.00 IS CORRODED. 10-9-07 CORROSION REMOVED AT LOWER FRAME SEGMENT 333 .00 BETWEEN S23R-23L IAW SRM 51-21-06. RIVETS REPLACED IAW SRM 51-42-06. MATERIAL THICKNESS: 0.050 MATERIAL REMOVE D: 0.001 WITHIN LIMITS AS PER SRM: 53-00-00. 2 L 7 2 4F RT A21EA 2007100900151 20071009 00151 2007 10 9 SWAA074842 4 20070927 A 2565 GIRT BAR BOEING 737 7375H4 138449D NM R1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK MISSING FASTENER. INSTALLED MISSING FASTENER PER MM. 2 L 7 2 4F RT A16WE 2007100900185 20071009 00185 NM 2007 10 9 SWAA074908 1 20071002 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 727 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007100900196 20071009 00196 EA 2007 10 9 TRAX200701410 1 20070926 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 920EV 7810 ROW 6 THRU 8 EMERGENCY LIGHTING INOP. 2 L 7 2 4F RT A21EA 2007100900204 20071009 00204 NM 2007 10 9 USAA920070866 1 20070925 A 5313 STRINGER SPLICE BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - MAJOR REPAIR - FPBH INSPECTION - NR 6006809, CRACKED STRINGER SPLICE, BS 348, S15L. REPLACED STRINGER SPLICE, BS 348, S15L IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007101000024 20071010 00024 NM 2007 10 10 ZZDA2007273 1 20070927 A 2497 286A1062007 WIRE HARNESS BOEING 737 73776N 13844CH NM NR 1 GENERATOR ARCED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 273AT 32662 ON ROUTINE INSPECTION FOUND NR 1 GENERATOR FEEDER CABLE ARCED, FAN COWL CENTER FITTING HAS BURN MARKS FROM ARCING. REMO VED AND REPLACED GENERATOR HARNESS ASSY. 2 L 7 2 4F RT A16WE 2007101000047 20071010 00047 SO 2007 10 10 C2XA07ON023 1 20070926 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT SMOKE A C2XA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 14171 145859 FLT 7743 - LAS TO LAX - FLIGHT CREW ABORTED TAKEOFF DUE TO SMOKE IN COCKPIT. THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT, MX PERSONNEL PERFORMED ENG RUNS WITH FLIGHT CREW; OPERATIONALLY CHECKED PACKS AND AIR BLEED SYSTEMS WITH NO DE FECTS OR ODORS WERE DETECTED AND THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2007101000052 20071010 00052 NM 2007 10 10 USAA920070860 1 20070925 A 5320 651768465 INTERCOSTAL BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6505178, CRACKED INTERCOSTAL BS 303.9, S10L. REPLACED INTERCOSTAL, BS 303.9, S10L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007101000057 20071010 00057 SO 2007 10 10 RAIA00709035 1 20070926 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DIRTY A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 833HK 145240 POST FLT NR 7903 - MKE - GALLEY WALL EXIT LOCATOR LIGHT INOP. MAINTENANCE REMOVED GALLEY WALL EMERGENCY LIGHT CLEANED C ONNECTOR REINSTALLED, OPS CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2007101000060 20071010 00060 SO 2007 10 10 RAIA00709034 1 20070926 A 7830 WARNING MESSAGE EMB 145 EMB145LR 3260212 SO THRUST REVERSER ILLUMINATED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 815HK 145048 FLT NR 5484 - STL - THRUST REVERSER NR 2 DISAGREE MESSAGE ON TAKEOFF ROLL AT ABOUT 60-65 KTS. TAKEOFF ROLL ABORTED. MA INTENANCE DEFERRED TR NR 2 PER MEL. 2 L 7 2 4T RT T00011AT 2007101000071 20071010 00071 WP 2007 10 10 MWEA070231 1 20071001 A 5230 ANGLE DOUG DC9 DC981 3022081 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 814ME 48010 AFT CARGO DOOR LOWER INNER ANGLE AFT OF FORWARD STOP FITTING APPEARS TO HAVE A CRACK EXTENDING PAST STOP DRILL HOLE. FA BRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2007101000073 20071010 00073 NM 2007 10 10 SWAA074865 1 20070930 A 5312 6545819 PRESSURE PANEL BOEING 737 7373T0 1384582 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED HC2 CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT BS 259, RBL 7.75. REPAIRED CEILING PANEL PER ACO. 2 L 7 2 4F RT A16WE 2007101000092 20071010 00092 EA 2007 10 10 S9BA200700018 1 20071001 A 5343 C6FSM123427 ATTACH BRACKET DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA NLG CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 251SA 524 NOSE LANDING GEAR LOWER MOUNTING FITTING CORRODED. 1 H 7 2 3T 4 T RT A9EA E4EA 2007101000101 20071010 00101 NE 2007 10 10 HEER117431 1 20070918 A 8000 9230604805107 FLEX COUPLING SKRSKY S92 S92A NE GE CT7TS CT78A 30136 NE STARTER LEAKING B HEER O OTHER O OTHER NR NOT REPORTED 1 SW 03 392PH 2296 920015 AFTER ENGINE CHANGE COULD NOT CROSS START THE OPPOSITE ENGINE. FOUND THE FLEX COUPLING LEAKING AIR EXCESSIVELY. REMOVE D AND REPLACED CROSS START FLEX COUPLING AND CROSS START WORKED PROPERLY. 2 G 7 2 4U 4 U R00024BO E8NE 2007101000112 20071010 00112 NM 2007 10 10 HNAA0700180 1 20070715 A 2150 782729018 ACM DHAV DHC8 DHC8102 2809003 NM LEAKING A HNAA B EMER. DESCENT J WARNING INDICATION NR NOT REPORTED 1 EA 07 812EX 17301 171 312 SMOKE WARNING LIGHT ILLUMINATED IN FLT ON APPROACH TO LANCASTER (LNS) GOING ON AND OFF INTERMITTENTLY, WITH ASSC MASTER WARNING LIGHT. INSP BAG BAY NO FIRE OR SMOKE DETECTED. REMOVED AND REPLACED FWD AND AFT SMOKE DET'S AS REQ. MECH FOU ND ACM LEAKING OIL. BAG BAY SMOKE DET'S REMOVED AND REPLACED. FERRIED TO MDT. REMOVED AND REPLACED ACM, OPS CHECK GOO D. 2 H 7 2 4T RT A13NM 2007101000133 20071010 00133 NM 2007 10 10 UPS07M50744 1 20070718 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT BORE LEFT NR 18 FOUND WITH CORROSION. CORROSION AT BARREL NUT BORE REMOVED PER SRM 51-21-01 VII R38. BORE THRU BOTTOM 0.0 60". BORE REAMED TO 1.067" DIA & REMN BLEND OUT 0.020 " DEEP FOUND EXCEED LIMITS. BARREL NUT BORE, BLEND OUT VOIDS, PERIPHERY RADIUS SMOOTHEN & PROTECTED PER SRM 51-21-01 VI I R38. REPAIR BUSHING FAB, PROTECTED & INSTALLED. REPAIR C/O AT BARREL NUT BORE NR 18 LEFT ACCEPTABLE PER EN 1448-07. 2 L 7 3 4F RT A22WE 2007101000136 20071010 00136 SO 2007 10 10 C2XA07SH074 1 20070921 A 5751 14574000405 SHROUD EMB 145 EMB145EP 3260221 SO RT AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14947 145054 SHV - DURING C-CHECK MAINTENANCE FOUND RT UPPER AILERON SHROUD WITH CORRODED BONDING PLATES. MAINTENANCE REPAIRED RT UP PER AILERON SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007101000144 20071010 00144 NM 2007 10 10 ASMF200709008 1 20070923 A 3222 STRUT DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NLG LEAKING W ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 158PL 49761 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AFTER TAKEOFF, THE NOSE LANDING GEAR RED LIGHT STAYED ON. MAINTENANCE PERSONN EL PERFORMED THE NOSE GEAR STRUT SERVICE IAW MM 32-21-02 AND THE EXTENSION AND RETRACTION TEST IAW MM 32-30-00, ALL CORR ECT. AS A PRECAUTIONARY ACTION, THE NOSE LANDING GEAR STRUT SEALS WERE REPLACED IAW MM 32-21-02, AS WELL AS EXTENSION/R ETRACTION OPERATIONAL TEST WAS PERFORMED IAW MM 32-31-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007101000153 20071010 00153 EU 2007 10 10 2007UALA03592 1 20070905 A 4900 2550013 MODULE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE APU FAILED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 436UA 638 EMERGENCY SHUTDOWN DISPLAYED ON UPPER ECAM SCREEN - APU. CREW COMMENTS: APU WAS SHUT DOWN 20 MINUTES AGO WHILE ON GROU ND. WHILE AIRBORNE GOT ECAM. *S/D* EIM MODULE FAILURE. REPLACED EIM 8061KM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101000198 20071010 00198 SO 2007 10 10 SIMA200727501 1 20071001 A 2910 HYDRAULIC SYSTEM EMB 145 EMB145LR 3260212 SO MULTIPLE FAIL A SIMA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 SW 21 614AE 145086 IMMEDIATELY AFTER T/O WHEN GEAR LEVER HANDLE PLACED IN "UP" POSITION RECEIVED A MASTER WARNING EICAS MSG "LG LEVER DISAG REE". THE NOSE WHEEL SHOWED UP AND WHITE THE MAINS SHOWED DOWN AND RED. THE HYD FLUID INDICATED ZERO WITH NO PRESS ON THE LT HYD SYSTEM. CREW ALSO HAD ASSOCIATED EICAS MESSAGES "HYD SYS 1 FAIL" HYD SYS 1 INOP" HYD 1 LOW QTY" E1 HYD PUMP FAIL. CREW DECLARED AN EMERGENCY, CREW WAS ABLE TO GET THE LANDING GEAR DOWN AND LOCKED. AFTER A FLYBY CREW LANDED UNE VENTFULLY. 2 L 7 2 4T RT T00011AT 2007101000199 20071010 00199 SO 2007 10 10 SIMA200727502 1 20071002 A 5330 12041320063 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 625AE 19171 145115 DURING MAINTENANCE, FOUND RIGHT FRAME 4 BENT AND SKIN CRACKED. REPAIRED BY REPLACING FRAME AND SKIN IAW EMB SRM 51-40-0 2. A/C WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007101000200 20071010 00200 WP 2007 10 10 IXXA070049O 1 20071002 A 2612 898475 FIRE LOOP DOUG DC8 DC871F 302199D WP NR 4 NACELLE DEFECTIVE A IXXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 11 828BX 86928 444 45993 DURING CLIMB-OUT FROM KTOL, THE CREW NOTICED NUMBER 4 FIRE WARNING LIGHT WAS INTERMITTENT. THE CREW RETURNED TO KTOL WI THOUT INCIDENT. MAINTENANCE INSPECTED NUMBER FOUR FIRE WARNING SYSTEM AND REPLACED LEFT AFT FIRE LOOP, OPERATIONAL CHEC K WAS GOOD IAW DC8 MAINTENANCE MANUAL 26-10-1. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2007101000201 20071010 00201 NM 2007 10 10 DU4R2007168 1 20070913 A 5311 FRAME BOEING 757 757232 1384965 NM ZONE 400 CRACKED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 642DL 23996 FOUND DENT/CRACK ON FRAME BS 1560 BETWEEN S-24L AND S-23L IN AFT PIT. REPAIRED BY CUTTING OUT DENT/CRACK SECTION OF FRA ME, HFEC NO RELEVANT INDICATION. FABRICATED AND INSTALLED FRAME REPAIR 13.5" BY 3" FROM 7075-T6 .063 IAW B757 SRM 51-40 -02, 51-20-01. 2 L 7 2 4F RT A2NM 2007101000202 20071010 00202 NM 2007 10 10 DU4R2007169 1 20070911 A 5414 SKIN BOEING 757 757232 1384965 NM NR 2 NACELLE DAMAGED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 642DL 23996 PERMANENT REPAIR TO NR 2 PYLON FWD SKIN REQUIRED. ACCOMPLISHED PERMANENT REPAIR IAW DELTA EA 06-074338-03 REV B DATED 0 1-30-2003 IAW DELTA ERA 362852-14 REV E DATED 9/5/07 APPROVED PER FAA FORM 8110-3 SIGNED BY DER NR SO-831 DATED 29 SEP 1 997. 2 L 7 2 4F RT A2NM 2007101000203 20071010 00203 NM 2007 10 10 DU4R2007174 1 20070922 A 5311 FRAME BOEING 757 757232 1384965 NM BS 1240 GOUGED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 642DL 23996 FOUND GOUGE IN RT AFT CARGO BS 1240 AND S-23R. REPAIRED BY BLENDING, HFEC IAW D634N301-6-51-00-19, NO CRACK INDICATIONS . FABRICATED AND INSTALLED REPAIR DOUBLER 12 BY 4 FROM 7075-T6 .080 IAW B757 SRM 53-00-53 FIG 101 AND FIG 201, AND 51-40 -02. 2 L 7 2 4F RT A2NM 2007101000204 20071010 00204 NM 2007 10 10 DU4R2007170 1 20070905 A 5414 SKIN BOEING 757 757232 1384965 NM NR 1 NACELLE DAMAGED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 642DL 23996 FOUND TEMPORARY REPAIR NR 1 PYLON I/B SKIN. ACCOMPLISHED PERMANENT REPAIR TO NR 1 PYLON I/B SKIN IAW DELTA EA 06-074338 -03 REV B DATED 01/30/2003 IAW DELTA ERA 093016-14 REV A AND B757 SRM 51-00-00D PG 1 APPROVED PER 14 CFR 121.379(B). 2 L 7 2 4F RT A2NM 2007101000205 20071010 00205 NM 2007 10 10 DU4R2007172 1 20070905 A 5414 SKIN BOEING 757 757232 1384965 NM ZONE 400 DAMAGED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 642DL 23996 TEMPORARY REPAIR TO NR 1 PYLON O/B SKIN. ACCOMPLISHED PERMANENT REPAIR TO NR 1 PYLON O/B SKIN REPAIR IAW DELTA EA 06-07 4338-03 REV B DATED 01/30/2003 IAW DELTA ERA 454258-14 REV ORIG APPROVED PER 14 CFR 121.379(B). 2 L 7 2 4F RT A2NM 2007101000206 20071010 00206 NM 2007 10 10 DU4R2007173 1 20070913 A 5414 SKIN BOEING 757 757232 1384965 NM ZONE 400 DAMAGED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 642DL 23996 FOUND CHAFED NR 2 PYLON AFT WEB FITTING CHAFED AT BOTTOM LT CORNER. REPAIRED BY FABRICATING AND INSTALLED REPAIR HFEC N O RELEVANT INDICATIONS, FABRICATING AND INSTALLING REPAIR GUSSET 4.34" BY 2.88" BY 1.2" FROM 7050-T7451 IAW DELTA ERA 46 3490-14AD DATED 9-12-07 REV ORIG AND B757 SRM 54-51-02 FIG 101 APPROVED BY FAA FORM 8100-9. 2 L 7 2 4F RT A2NM 2007101000218 20071010 00218 EU 2007 10 10 07FDEA04459 1 20071002 A 5313 A53973717200 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION AT STRINGER SEGMENT C 72, P 48 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007101000219 20071010 00219 EU 2007 10 10 07FDEA04460 1 20071002 A 5753 SKIN AIRBUS 310 A310324 3930206 EU TE FLAP MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 805FD 456 FOUND OLD POCKET REPAIRS AT RIB 21 INBOARD FLAP LT NOT CONFORM TO SRM. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SB 5 7-2055. 2 L 7 2 4F RT A35EU 2007101000220 20071010 00220 EU 2007 10 10 07FDEA04461 1 20071002 A 5313 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION AT STRINGER SEGMENT P 56 LT, C 80 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007101100021 20071011 00021 WP 2007 10 11 AALA20071840 1 20071002 A 3222 STRUT DOUG DC9 DC983 3022083 WP NLG DAMAGED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 978TW 53628 YUL INFLIGHT T761/02OCT - UNABLE TO RETRACT NOSE GEAR. RECEIVED RED LIGHT INDICATION. LANDED YUL WITHOUT INCIDENT. AI RCRAFT OUT OF SERVICE FOR REPAIR. 10-16-07 FOUND NOSE GEAR PISTON DAMAGE. REPLACED NOSE GEAR STRUT ASSEMBLY. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007101100030 20071011 00030 NM 2007 10 11 AALA20071832 1 20070929 A 3350 3020421 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 674AN 29424 MIA - EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR BROKEN. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007101100037 20071011 00037 WP 2007 10 11 070159 1 20070920 A 3350 408822101 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 887GA 49932 IT HAS BEEN REPORTED BY THE FLIGHT CREW THE EMERGENCY EVACUATION LIGHTING SYSTEM HAS BEEN FOUND TO BE DEFECTIVE. MAINTE NANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS, AN OPE RATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED T O SERVICE. 2 L 7 2 4F A6WE 2007101100038 20071011 00038 WP 2007 10 11 070160 1 20070921 A 3350 408822101 BATTERY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 893GA 53051 IT HAS BEEN REPORTED BY THE FLIGHT CREW THE EMERGENCY EVACUATION LIGHTING SYSTEM HAS BEEN FOUND TO BE DEFECTIVE. MAINTE NANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPE RATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007101100040 20071011 00040 SO 2007 10 11 SIMA200727701 1 20071001 A 2910 14570242401 HOSE EMB 145 EMB145LR 3260212 SO HYD SYSTEM DAMAGED A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 614AE 145086 IMMEDIATELY AFTER TAKEOFF WHEN GEAR LEVER HANDLE PLACED IN "UP" POSITION RECEIVED EICAS MESSAGES "LG LEVER DISAGREE "HYD SYS 1 FAIL" HYD SYS 1 INOP" HYD 1 LOW QTY" E1 HYD PUMP FAIL. DECLARED AN EMERGENCY AFTER A FLYBY CREW LANDED UNEVENTFU LLY. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR ACTUATOR UP HYDRALIC HOSE P/N 145-70242-401. REPLACED NR 1 EMDP P/N MPEV30086 S/N MS684677. REPLACED E1 HYD PUMP P/N 971808 MOD D S/N MX611193. REPLACED 3 HYD FILTERS P/N 31829-3. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007101100050 20071011 00050 2007 10 11 AALA20071844 4 20071003 A 2565 SLIDE BOEING 757 757223 1384957 NM R4 DOOR PARTIAL INFLATE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 607AM 27058 MIA - RIGHT NR 4 DOOR SLIDE INADVERTENTLY UNSUCCESSFULLY DEPLOYED WHEN OPENED FROM THE INSIDE. SLIDE FELL OUT OF COVER BUT DID NOT INFLATE AND DOOR BOTTLE DISCHARGED. REPLACED RIGHT NUMBER FOUR DOOR SLIDE AND ASSIST BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007101100052 20071011 00052 NM 2007 10 11 AALA20071846 1 20071003 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 347AN 33086 MIA - EXTERIOR EMERGENCY LIGHT AT RIGHT INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY EXIT LIGHT AT RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007101100053 20071011 00053 NM 2007 10 11 AALA20071847 1 20071003 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 397AN 29604 MIA - EMERGENCY LIGHT AT RIGHT FIRST CLASS MISSING LENS. REPLACED LENS FOR EMERGENCY EXIT LIGHT AT RIGHT FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007101100055 20071011 00055 NE 2007 10 11 QXEA200701509 2 20071004 A 7200 ENGINE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 2 MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 347PH 480 PDX FLIGHT NR 2187 - BRINGING NR 2 ENGINE OUT OF FEATHER DURING SINGLE ENGINE TAXI, NP PAUSED AND WHEN ENGINE UNFEATHERE D NR 2 ENGINE MANUAL CAUTION LIGHT ILLUMINATED. MAINTENANCE CYCLED BETA LOCK OUT CIRCUIT BREAKER. OPERATIONAL CHECK GO OD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007101100056 20071011 00056 NM 2007 10 11 QXEA200701510 1 20071004 A 3097 CIRCUIT BREAKER DHAV DHC8 DHC8202 2809007 NM PITOT HEAT TRIPPED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 366PH 510 PDX FLIGHT NR 21568 - ON TAXI NOTICED A PITOT HEAT 2 CAUTION LIGHT, CHECKED CIRCUIT BREAKER AND NOTICED IT POPPED ON PAN EL 2. TAXIED BACK TO GATE. MAINTENANCE RESET CIRCUIT BREAKER. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RET URNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007101100059 20071011 00059 EA 2007 10 11 SWIA200718730 1 20070924 A 2740 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA MACH TRIM MALFUNCTIONED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 943SW 7762 FLT 6550 - STAB AND MACH TRIM WOULD NOT RE-ENGAGE. STAB REMAINED AT 6.2 NOSE UP. REPLACED STAB/MACH TRIM CONTROL PANEL PER AMM 27-41-15 AND RERACKED HSTCU. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007101100060 20071011 00060 EA 2007 10 11 SWIA200718731 1 20070925 A 5240 ROLLER CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR LACK OF LUBE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 947SW 7786 FLT 3824 - SERVICE DOOR IS HARD TO OPEN FROM THE OUTSIDE. LUBED SERVICE DOOR ROLLERS. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2007101100062 20071011 00062 EA 2007 10 11 SWIA200718733 1 20070921 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A SWIA O OTHER O OTHER AP APPROACH 1 NM 07 464SW 7827 FLT 3944 - BIRD STRIKE ON SHORT FINAL. REPLACED THE DAMAGED SKIN AND STIFFENERS BELOW LEFT WINDSHIELD IAW CRJ SRM 51-23 -00, 51-40-11, 51-42-06. 2 L 7 2 4F RT A21EA 2007101100065 20071011 00065 SO 2007 10 11 SWIA200718736 1 20070927 A 5210 HANDLE EMB 120 EMB120ER 3260203 SO PAX DOOR OUT OF ADJUST A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 581SW 120349 FLT 3693 - MAIN CABIN DOOR HANDLE DOES NOT OPEN OR CLOSE EASILY. ADJUSTED TOP/AFT STOP HARDWARE AS REQUIRED IAW 52-10-0 0. 2 L 7 2 4T RT A31SO 2007101100066 20071011 00066 SO 2007 10 11 SWIA200718737 1 20070926 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY EXIT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 560SW 120334 FLT 5504 - FORWARD FLOOR LEVEL EMERGENCY EXIT SIGN IS BROKEN. INSTALLED SERVICEABLE EMERGENCY EXIT LENS. 2 L 7 2 4T RT A31SO 2007101100067 20071011 00067 EA 2007 10 11 SWIA200718738 1 20070927 A 7830 1267588 DRIVE UNIT CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 986SW 11064 11064 7967 FLT 5925 - RIGHT THRUST REVERSER UNLOCKED MESSAGE APPEARED. RETURNED TO FIELD. REPLACED RIGHT ENGINE THRUST REVERSER P DU WITH SERVICEABLE UNIT IAW CRJ 200 AMM 78-32-03. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007101100068 20071011 00068 EA 2007 10 11 SWIA200718739 1 20070924 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 946SW 7776 FLT 1902 - FOUND FORWARD FLOOR EMERGENCY LIGHTING STRIP IS INOP. REPLACED FORWARD FLOOR LIGHT STRIP IAW AMM 33-50-00. 2 L 7 2 4F RT A21EA 2007101100069 20071011 00069 EA 2007 10 11 SWIA200718740 1 20071002 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 466SW 7856 FLT 3767 - RT WINDSHIELD SHATTERED IN CRUISE. REPLACED WINDSHIELD IAW MM 56-11-01, P/N: NP-137321-6 S/N OFF: 03155H569 0. 2 L 7 2 4F RT A21EA 2007101100071 20071011 00071 SO 2007 10 11 SWIA200718742 1 20070905 A 5523 SKIN EMB 120 EMB120ER 3260203 SO ELEVATOR TAB CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 284YV 120284 LEFT ELEVATOR TRIM TAB HAS CORROSION IN BETWEEN SKIN, FOUND AT C-CHECK. REPLACED LEFT ELEVATOR TRIM TAB IAW EMB 120 MM 27-32-01. 2 L 7 2 4T RT A31SO 2007101100074 20071011 00074 2007 10 11 HALA0700425 4 20071001 A 3417 ADC BOEING 767 76733A 1385209 NM MALFUNCTIONED A HALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 581HA 28141 ETOPS SIGNIFICANT SYSTEM, DUE TO AIR DATA MALFUNCTION ON F/O'S SIDE BOTH RUDDER RATIO AND AILERON LOCKOUT EICAS MESSAGES APPEARED AND STAYED ON. T/S PER FIM 34-12-00 FIG 109, NO FAULTS ON LEFT OR RIGHT ADC'S. SYSTEM NORMAL PER FIM MCDP TE ST OF LAST FLIGHT AND NR 30 NO FAULT. 2 L 7 2 4F RT A1NM 2007101100077 20071011 00077 EA 2007 10 11 QXEA200701511 1 20071002 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002C10 1390015 EA DOOR MALFUNCTIONED A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 605QX 10022 BOI - FLIGHT 4276 - DURING PUSHBACK RECEIVED A PROX SYSTEM FAULT 1 STATUS MESSAGE. RETURNED TO THE GATE. MAINTENANCE F OUND NO CURRENT FAULTS IN MDC. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007101100078 20071011 00078 EU 2007 10 11 1217 1 20071003 A 3300 3011180 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU EMERGENCY LIGHTS DEFECTIVE A HYIA K NONE L NO TEST IN INSP/MAINT 1 NE 01 14834 193 EMERGENCY LIGHTING BATTERY PACK UNIT FOUND DEFECTIVE DURING CAP CHECK. BATTERY PACK UNIT REMOVED AND REPLACED PER CMM 33 -51-21. 2 H 7 2 4T RT A53EU 2007101100081 20071011 00081 EU 2007 10 11 HYIA1215 1 20071003 A 3350 3011180 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU EMERGENCY LIGHTS DEFECTIVE A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 EMERGENCY LIGHTING BATTERY PCK UNIT FOUND DEFECTIVE DURING CAP CHECK. BATTERY PACK UNIT REMOVED AND REPLACED PER CMM 33 -51-21. 2 H 7 2 4T RT A53EU 2007101100082 20071011 00082 EU 2007 10 11 HYIA1216 1 20071003 A 3350 3011180 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU EMERGENCY LIGHTS DEFECTIVE A HYIA K NONE L NO TEST IN INSP/MAINT 1 NE 01 14834 193 EMERGENCY LIGHTING BATTERY PACK UNIT FOUND DEFECTIVE DURING CAP CHECK. BATTERY PACK UNIT REMOVED AND REPLACED PER CMM 3 3-51-21. 2 H 7 2 4T RT A53EU 2007101100086 20071011 00086 NM 2007 10 11 NWAA073356307 1 20071003 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY EXIT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 667US 24222 DURING LINE CHECK, FOUND UPPER DECK RT EMERGENCY DOOR BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK PER AMM 52-23-14. OPS CHECKS GOOD. 2 L 7 4 4F RT A20WE 2007101100087 20071011 00087 EU 2007 10 11 07FDEA04492 1 20071005 A 5754 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND AT RT NR 1 SLAT SEVERAL CHAFING MARKS ON LOWER OUTBOARD SKIN PANEL. REPAIR PERFORMED BY CUT OUT THE SKIN AND INST ALLING AN EXTERNAL DOUBLER IAW EA 6-5742-112470 AND RAS/FOK/174/2007 ISS A. 2 L 7 2 4F RT A35EU 2007101100088 20071011 00088 EU 2007 10 11 07FDEA04493 1 20071005 A 5730 A57340088 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION AT LT WING BOTTOM SKIN BETWEEN 8-10 AND 18-19 FWD OF FRONT SPAR REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTECTING IAW EA 6-5720-112535 AND RAS/BAE/1005212/2007. 2 L 7 2 4F RT A35EU 2007101100090 20071011 00090 EU 2007 10 11 07FDEA04495 1 20071005 A 5730 A57140983 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION AT LT WING BOTTOM SKIN BETWEEN 8-9 FWD OF FRONT SPAR REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTE CTING IAW EA 6-5720-112535 AND RAS/BAE/1005212/2007. 2 L 7 2 4F RT A35EU 2007101100091 20071011 00091 NM 2007 10 11 07FDEA04496 1 20071005 A 5754 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 LEFT WING, NR 3 LEADING EDGE SLAT TELESCOPING DUCT CUTOUT OUTBOARD CORNER FOUND CRACK. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-115224, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007101100092 20071011 00092 NM 2007 10 11 07FDEA04497 1 20071005 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 FOUND NOSE LANDING GEAR TRUNNION FITTING SUSPECT WITH CRACK. 10-24-07 REPAIR CARRIED OUT AS PER SRM 53-40-00 FIGUR E 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. REPETITIVELY INSPECT FOR CRACK GROWTH AT NOT TO EXCEED 1 ,500 LANDING INTERVALS AS PER SRM 53-40-00 FIGURE 23 VOLUME I. 2 L 7 3 4F RT A22WE 2007101100093 20071011 00093 NM 2007 10 11 07FDEA04498 1 20071005 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 NOSE LANDING GEAR MOUNTING LEFT TRUNNION FITTING FOUND WITH CRACK. 10-24-07 REPAIR CARRIED OUT AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. REPETITIVELY INSPECT FOR CRACK GROWTH AT NOT TO EXC EED 1,500 LANDING INTERVALS AS PER SRM 53- 40-00 FIGURE 23 VOLUME I. 2 L 7 3 4F RT A22WE 2007101100094 20071011 00094 EU 2007 10 11 07FDEA04500 1 20071005 A 5720 A57246668 PLATE AIRBUS 300 A300B4622R 3930312 EU ZONE 500 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND DELAMINATION ON LT WING INNER SHROUD BOX DEFLECTOR PLATE AROUND ROLLER SUPPORT REPAIR PERFORMED BY BONDING REPAIR IAW EA 6-5755-112536 AND RAS//BAE/1005280/2007 ISS A. 2 L 7 2 4F RT A35EU 2007101100096 20071011 00096 EU 2007 10 11 07FDEA04502 1 20071005 A 5730 A57340087 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION AT RT WING BOTTOM SKIN IN THE AREA OF RIB 5 REPAIR PERFORMED BY BLEND OUT CORROSION, FLAP PEENING AND IN STALLATION OF NEW FASTENER IAW EA 6-5720-112520 AND RAS/BAE/1005222/2007 ISS A. 2 L 7 2 4F RT A35EU 2007101100097 20071011 00097 EU 2007 10 11 07FDEA04503 1 20071005 A 5730 A57340087 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION AT RT WING BOTTOM SKIN IN THE AREA OF RIB 5. REPAIR PERFORMED BY BLEND OUT CORROSION, FLAP PEENING AND INSTALLATION OF NEW FASTENER IAW EA 6-5720-112520 AND RAS/BAE/1005222/2007 ISS A. 2 L 7 2 4F RT A35EU 2007101100098 20071011 00098 WP 2007 10 11 07FDEA04504 1 20071005 A 5313 AGA3086 LONGERON DOUG DC10 DC1010F 3022111 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 CTR CARGO COMPT BILGE, CORROSION WITH EXFOLIATION ON SPLICE AND LONGERON. REPAIRED AREA IAW SRM 53-10-00 VOL I FIG 5. 2 L 7 3 4F A22WE 2007101100100 20071011 00100 EA 2007 10 11 QXEA200701513 1 20071004 A 4930 D97C00614 ACTUATOR VALVE CNDAIR CL600 CL6002C10 1390015 EA APU INOPERATIVE A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 604QX 15409 10019 BUR - FLIGHT 2552, RECEIVED "APU SOV FAIL" CAUTION MESSAGE AFTER APU WAS SHUTDOWN. AFTER RUNNING ABNORMAL SHUTDOWN CHEC KLIST, THE APU STARTED UP AND RAN OK. RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED APU FUEL FEED SHUT OFF VALVE ACTUATOR. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007101100102 20071011 00102 NM 2007 10 11 AALA20071849 1 20071004 A 3397 WIRE HARNESS BOEING 737 737823 13844BZ NM EMEGENCY LGIHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 972AN 30097 LGA - EMERGENCY LIGHT AT SEAT ROW 10DEF INOPERATIVE. RESECURED HARNESS FOR EMERGENCY LIGHT AT SEAT ROW 10DEF. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007101100104 20071011 00104 NM 2007 10 11 AALA20071851 1 20071004 A 3350 SHROUD BOEING 737 737823 13844BZ NM EMEGENCY LGIHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 972AN 30097 LGA - EMERGENCY LIGHT AT SEAT ROW 15DEF MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 15DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007101100107 20071011 00107 NM 2007 10 11 AALA20071854 1 20071004 A 3350 BULB BOEING 767 767323 1385205 NM EMEGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AA 25201 MIA - EMERGENCY LIGHT AT SEAT ROW 31H OVERHEAD INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 31H OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007101100109 20071011 00109 NM 2007 10 11 QXEA200701514 1 20070925 A 3230 8CC314F8Y1 FILTER BOMBDR DHC8 DHC8402 1390042 NM SELECTOR VALVE UNKNOWN A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 410QX 4053 PDX FLIGHT: RIGHT MAIN LANDING GEAR TOOK AN UNUSUALLY LONG TIME TO RETRACT AFTER TAKEOFF. RIGHT MAIN RETRACTED APPROX 1 0-15 SECONDS AFTER REST OF GEAR RETRACTED NORMALLY. MAINTENANCE REPLACED THE SECONDARY MLG SELECTOR VALVE PRESSURE FILT ER. PERFORMED RT MLG RETRACTION ACTUATOR CHECK AND ADJUSTMENT. PERFORMED FUNCTIONAL TEST OF LANDING GEAR PRIMARY EXTEN SION AND RETRACTION IAW Q400 AMM TASK 32-31-00-720-801 AND ALTERNATE EXTENSION SYSTEM IAW TASK 32-34-00-710-801. FUNCTI ONAL TESTS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007101100113 20071011 00113 NM 2007 10 11 F3LA200700258 1 20070923 A 5320 D5361019720140 THRESHOLD AIRBUS A319 A319111 3930336 NM R1 DOORWAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED R1 DOOR THRESHOLD STRIP CORRODED ON LOWER SURFACE. REMOVED AND REPLACED R1 THRESH OLD STRIP IAW AMM 53-12-991-003. 2 L 7 2 4F RT A28NM 2007101100114 20071011 00114 CE 2007 10 11 N2615G 1 20071001 A 2140 520010723 LINE CESSNA 402 402C 207590R CE HEATER FRACTURED E HYIA H DEACTIVATE SYST/CIRCUITS K A FLUID LOSS FLAME/FIRE TX TAXI/GRND HDL 1 NE 01 2615G 006 402C0101 DURING TAXI, PILOT TURNED ON CABIN HEATER. WHEN NO HEAT APPEARED PRESENT, PILOT TURNED OFF HEATER. AT THIS POINT A SMA LL FIRE IGNITED IN THE HEATER BAY. PILOT SECURED THE AIRCRAFT AND EXITED THE AIRCRAFT. THE FIRE WAS EXTINGUISHED WITH MINIMAL DAMAGE TO THE AIRCRAFT. MAINTENANCE LATER FOUND THE HEATER FUEL SUPPLY LINE FRACTURED. 1 L 7 2 3O A7CE 2007101100117 20071011 00117 WP 2007 10 11 070164 1 20070828 A 5230 SKIN DOUG DC9 DC982 3022082 WP CARGO DOOR GOUGED A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 894GA 49660 AFT CARGO DOOR HAS A GOUGE BELOW DOOR HANDLE. ORIGINAL SKIN THICKNESS .050". REMOVED .011", OUT OF LIMITS PER SRM 53- 04 FIG 38. AREA MEASURES 2.7" BY 1.7" BY .011". FABRICATED INTERNAL REPAIR DOUBLER 2024 T3, .032". CARGO DOOR OK FO R CONTINUED SERVICE. 2 L 7 2 4F A6WE 2007101100119 20071011 00119 WP 2007 10 11 070163 1 20070820 A 5230 SKIN DOUG DC9 DC982 3022082 WP CARGO DOOR GOUGED A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 894GA 49660 AFT CARGO PIT DOOR HAS GOUGE ON 3RD STRINGER FROM BOTTOM OF DOOR. ORIGINAL SKIN THICKNESS .050". REMOVED .015" OUT OF LIMITS PER SRM 53-04 FIG 38. AREA MEASURES 2" BY 1" BY .015. FABRICATED INTERNAL REPAIR DOUBLER 2024 T3 .032". DOOR S KIN OK FOR CONTINUED SERVICE. 2 L 7 2 4F A6WE 2007101100122 20071011 00122 NM 2007 10 11 F3LA200700261 1 20070927 A 5755 LUG AIRBUS A319 A319111 3930336 NM NR 4 SPOILER GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED GOUGES ON LT WING NR 4 SPOILER ANTI-ROTATION LUG SURFACE. MACHINED ANTI-ROTATION FLAT, PERFORMED HFEC, AND BONDED REINFORCING PLATE IAW EA A9-57R-12171. 2 L 7 2 4F RT A28NM 2007101100124 20071011 00124 WP 2007 10 11 IXXA070051O 1 20071005 A 2612 FIRE LOOP DOUG DC8 DC871F 302199D WP NR 4 NACELLE FALSE ACTIVATION A IXXA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 11 828BX 86931 447 45993 DURING CRUISE FROM KTOL TO KMCI, NR 4 ENGINE WAS SHUT DOWN FOR A SHORT CIRCUIT LIGHT ON WITH NO FIRE LIGHT OR ALARM BELL DURING TEST. THE CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED NUMBER 4 FIRE LOOPS, NO DEFECTS NOTED. OPERATIO NAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2007101100125 20071011 00125 EU 2007 10 11 SIMA200728101 1 20071005 A 2720 NAS428KN320 BOLT SAAB SF340 340B 7860101 EU DAMPENER UNKNOWN A SIMA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SW 21 253AE 340B253 WITH OR WITHOUT A/P, A/C EXPERIENCES LEFT TO RIGHT LATERAL VIBRATIONS AT HIGHER SPEEDS (NOT TURBULENCE) OVER-200 KTS. N O RELATIONSHIP TO POWER LEVER SETTINGS. COMPLIED WITH INFLIGHT VIBRATION INSPECTION IAW AE WC NR 05-02133 PART 1. DURI NG INSPECTION FOUND RUDDER DAMPENER LT SIDE BOLT BROKEN AND DAMPENER OUT OF ADJUSTMENT (LEVER). REMOVED AND REPLACED DA MPENER LEFT BOLT AND ADJUSTED DAMPENER IN REFERENCE TO SAAB MM 27-22-35. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007101100129 20071011 00129 SO 2007 10 11 SIMA200728106 1 20071007 A 5240 DOOR EMB 135 EMB135KL 3260302 SO EXTERNAL POWER OPEN A SIMA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 21 804AE 145487 NOTED A HIGH FREQUENCY SOUND AND VIBRATION AFTER TAKEOFF AND NOTED AS AIRSPEED SLOWED DOWN SOUND WENT AWAY. PERFORMED I NSPECTION ON AIRCRAFT FOUND 6PV DOOR OPEN NO EXTERNAL DAMAGE TO THE SKIN WAS FOUND AT THIS TIME RE-SECURED THE DOOR AS R EQUIRED AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007101100130 20071011 00130 SO 2007 10 11 SIMA200728105 1 20071006 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 627AE 145121 EMERGENCY LIGHTS AFT OF ROW 13 DOES NOT WORK, THEY COME ON INITIALLY THEN GO DARK. REMOVED AND REPLACED EMERGENCY BATTE RY IAW 33-50-04-000-801-A AND 33-50-04-400-801-A. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007101100134 20071011 00134 SO 2007 10 11 SIMA200727702 1 20071003 A 3233 23093700501 ACTUATOR EMB 145 EMB145LR 3260212 SO RT MLG MALFUNCTIONED A SIMA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 624AE 145111 UPON LANDING, GEAR EXTENSION AT MEM RIGHT MAIN LANDING GEAR DID NOT INITIALLY COME DOWN. AIRCRAFT NATURALLY YAWED THEN GEAR CAME DOWN APPROX 5 SECONDS. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR ACTUATOR. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007101100137 20071011 00137 NM 2007 10 11 F3LA200700265 1 20070922 A 5320 D5347112420000 SHEAR PLATE AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED SHEARED RIVETS IN SHEAR PLATE BETWEEN FR 69 AND FR 70 AT Y1162. FOUND SHEAR PLATE TO BE OUT OF LIMITS IAW SRM 53-00-14. REMOVED SHEAR PLATE IAW SRM 51-72-11. INSTALLED NEW SHEAR PLATE TO SUPPORT ASSY BETWEEN FR 69 AND FR 70 IAW SRM 51-42-11, PARA 6 AND 14. 2 L 7 2 4F RT A28NM 2007101100139 20071011 00139 NM 2007 10 11 F3LA200700267 1 20071002 A 5410 D5463083700100 FAIRING AIRBUS A319 A319111 3930336 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED APPROX A 2 1/2 INCH CRACK ALONG BOTTOM SECTION OF LT ENGINE INBD PYLON PANEL (ABOV E PANEL NR 473AR). REMOVED LATERAL FAIRING ASSY FROM LT ENG I/B SIDE IAW A319 MM 54-57-22-010-050. TRANSFERRED FASTENE R HOLES AND NUT PLATES TO NEW FAIRING ASSY IAW SRM 51-72-11. INSTALLED REPLACEMENT LT ENG PYLON LATERAL FAIRING IAW AMM 54-51-21-400-001. 2 L 7 2 4F RT A28NM 2007101100140 20071011 00140 NM 2007 10 11 F3LA200700268 1 20070930 A 3397 CONNECTOR AIRBUS A319 A319111 3930336 NM EMERGENCY LIGHTS BROKEN A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED EMERGENCY EXIT LIGHTS CONNECTOR 7260VC8 BROKEN. REMOVED AND REPLACED ELECTRICAL C ONNECTOR 7260VC8 IN AFT CABIN EMERGENCY PATH FLOOR LIGHTING SYSTEM IAW AMM 33-51-08 P004, FIG 2. COMPLIED WITH OPERATIO NAL TEST OF THE EMERGENCY LIGHTING IN THE CABIN BY THE EMERGENCY EXIT LT SWITCH. NO DEFECTS NOTED. PERFORMED THE OPERA TIONAL TEST OF THE EMERGENCY LIGHTING IN THE CABIN BY THE "EMERGENCY EXIT LT" SWITCH IAW 33-51-00-710-008. NO DEFECTS N OTED. 2 L 7 2 4F RT A28NM 2007101100141 20071011 00141 NM 2007 10 11 F3LA200700269 1 20070920 A 3350 321430321431 EPSU AIRBUS A319 A319111 3930336 NM EMERGENCY LIGHTS FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 922FR 2012 DURING C-3 CHECK, INSPECTION REPORTED A/C FAILED EMERGENCY LIGHTS BATTERY CAPACITY TEST. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY PACKS 10WL, 13WL, 11WL, AND 12WL IAW AMM 33-51-38-000-002 AND AMM 33-51-38-400-002. PERFORMED OP ERATIONAL TEST OF EPSU'S IAW 33-51-38-400-002. TESTED GOOD. 2 L 7 2 4F RT A28NM 2007101100144 20071011 00144 NM 2007 10 11 AALA20071856 1 20071004 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 344AN 33083 MIA - EMERGENCY LIGHT AT OVERHEAD SEAT 32G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 32G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007101100146 20071011 00146 NM 2007 10 11 AALA20071861 1 20070921 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 AFW - EMERGENCY LIGHT BATTERY PACK AT RIGHT NUMBER TWO DOOR M33098 INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK A T RIGHT NUMBER TWO DOOR M33098. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007101100150 20071011 00150 NM 2007 10 11 AALA20071860 1 20071005 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 JFK - EMERGENCY EXIT SIGN LIGHT AT LEFT NUMBER THREE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN LI GHT AT LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007101100151 20071011 00151 NM 2007 10 11 AALA20071857 1 20071004 A 7830 THRUST REVERSER BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE DAMAGED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 647AM 24605 31010 SJU INFLIGHT T1937/04OCT - CREW HEARD LOUD BOOM FROM RT ENGINE CLIMBING THROUGH FLIGHT LEVEL 320. ENGINE GAS TEMPERATUR E WENT TO AMBER AT 615 DEGREES. N1 WAS AMBER. THROTTLE REDUCED TO IDLE AND ALL PARAMETERS NORMAL AT IDLE. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. FOUND RIGHT ENGINE THRUST REVERSER DAMAGE. FLIGHT FERRIED TO DFW FOR ENGINE CHANGE. AIRCRAFT OUT OF SERVICE FOR EVALUATION AND REPAIR. 10-16-07 REPLACED NR 2 ENGINE ON 06 OCT 2007 AT SJU. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2007101100152 20071011 00152 WP 2007 10 11 AALA20071870 1 20071005 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN MISINSTALLED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 578AA 53155 DFW - EMERGENCY SEAT MOUNTED LIGHTS AT SEAT ROWS 28DEF AND 29DEF OUT OF CONFIGURATION. CORRECTED CONFIGURATION FOR EMER GENCY SEAT MOUNTED LIGHTS AT SEAT ROWS 28DEF AND 29DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007101100153 20071011 00153 WP 2007 10 11 AALA20071871 1 20071005 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 578AA 53155 DFW - EMERGENCY SEAT MOUNTED LIGHT AT SEAT 23D BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY SEAT MOUNTED LIGHT AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007101100156 20071011 00156 NM 2007 10 11 AALA20071865 1 20070921 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 AFW - EMERGENCY LIGHT BATTERY PACK AT RIGHT NUMBER FOUR DOOR M33409 INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK AT RIGHT NUMBER FOUR DOOR M33409. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007101100157 20071011 00157 WP 2007 10 11 AALA20071868 1 20071005 A 2560 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN CRACKED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7525A 49917 LGA - EMERGENCY FLASHLIGHT AT LEFT EMERGENCY DOOR HAS CRACKED CASE. REPLACED EMERGENCY FLASHLIGHT AT LEFT EMERGENCY DOO R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007101100158 20071011 00158 NM 2007 10 11 AALA20071869 1 20071005 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 976AN 30099 LGA - EMERGENCY LIGHT AT AFT LEFT GALLEY DOOR AFT LOWER EXIT SIGN HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT AFT LEFT GALLEY DOOR AFT LOWER EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007101100159 20071011 00159 WP 2007 10 11 AALA20071872 1 20071005 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 578AA 53155 DFW - EMERGENCY LIGHT AT SEAT 10D HAD BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007101100160 20071011 00160 WP 2007 10 11 AALA20071873 1 20071005 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 578AA 53155 DFW - EMERGENCY LIGHT AT SEAT 15D HAD BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007101100162 20071011 00162 WP 2007 10 11 AALA20071875 1 20071005 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 578AA 53155 DFW - EMERGENCY LIGHT AT SEAT 24D HAD BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 24D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007101100164 20071011 00164 NM 2007 10 11 AALA20071867 1 20071003 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 775AN 29584 DFW - EMERGENCY SEAT MOUNTED LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY SEAT MOUNTED LIGHTS IN CA BIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007101100165 20071011 00165 NM 2007 10 11 F3LA200700270 1 20070922 A 5320 SILL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON L2 DOOR SILL AT FR 66 NUT PLATE HOLE. REPAIRED L2 DOOR SILL IAW EA N R A9-53R-12173. 2 L 7 2 4F RT A28NM 2007101100166 20071011 00166 NM 2007 10 11 F3LA200700271 1 20071002 A 5315 D5347217220200 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT Y1292 TO Y1162 JUST AFT OF FR 66 TO JUST FWD OF FR 68. REMOVED AND REPLACED FLOORBEAM IAW 51-42-11 AND DRAWING D53472780. 2 L 7 2 4F RT A28NM 2007101100167 20071011 00167 NM 2007 10 11 F3LA200700272 1 20071002 A 5320 D5347209001000 SEAT TRACK AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON SEAT TRACK AT FR66, Y1291. REMOVED AND REPLACED SEAT TRACK IAW SRM 5 1-42-11. 2 L 7 2 4F RT A28NM 2007101100168 20071011 00168 NM 2007 10 11 F3LA200700273 1 20071002 A 5220 RELEASE CABLE AIRBUS A319 A319111 3930336 NM EMERGENCY EXIT OUT OF ADJUST A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED RT EMERGENCY EXIT HATCH SLIDE RELEASE CABLE NEEDS ADJUSTMENT. ADJUSTED RT EMERGEN CY EXIT HATCH SLIDE RELEASE. OPS TEST GOOD. RE-ATTACHED SLIDE RELEASE CABLE AND SAFTIED AS REQUIRED IAW 25-62-43-400-0 001. 2 L 7 2 4F RT A28NM 2007101100169 20071011 00169 NM 2007 10 11 F3LA200700274 1 20071002 A 5320 WEB AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED RIVETS SHEARED IN WEB JUST AFT OF L2 DOOR BETWEEN FR 68 AND FR 69. REMOVED AND RE PLACED WEB AND FASTENERS IAW DRAWING D18D53480019 AND SRM 51-42-11. 2 L 7 2 4F RT A28NM 2007101100170 20071011 00170 NM 2007 10 11 F3LA200700275 1 20071002 A 5320 D5347112420000 SHEAR PLATE AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON SHEAR PLATE BETWEEN FR 69 AND FR 70 AT -Y1162. REMOVED AND REPLACED SHEAR PLATE IAW DWG D5347418 AND D53471123. 2 L 7 2 4F RT A28NM 2007101100171 20071011 00171 NM 2007 10 11 F3LA200700276 1 20070925 A 5320 STRUCTURE AIRBUS A319 A319111 3930336 NM SILL CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR SILL FWD GIRT BAR FITTING ATTACHMENT HOLE LOCATION AFT INBD CORRODED. REP AIRED DAMAGE IAW EA A9-53R-12160. 2 L 7 2 4F RT A28NM 2007101100172 20071011 00172 NM 2007 10 11 HALA07431 1 20070617 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM FUSELAGE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 LEVEL 1 CORROSION AT SEAT TRACK RBL 59 AT STA. 69, AREA REWORKED AND FOUND WITHIN LIMITS PER SRM 53-00-52. REWORKED ARE A ALODINED AND PAINTED. 2 L 7 2 4F RT A1NM 2007101100173 20071011 00173 NM 2007 10 11 HALA0700434 1 20070917 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 1136 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 LEVEL 1 CORROSION ON SEAT TRACK SECTION 46 LBL, STATION 1136. AREA REWORKED AND FOUND TO BE WITHIN LIMITS, PER SRM 53-0 0-52. REWORKED AREA ALODINED AND PAINTED. 2 L 7 2 4F RT A1NM 2007101100174 20071011 00174 NM 2007 10 11 HALA0700440 1 20070917 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 LEVEL 1 CORROSION ON SEAT TRACK SECTION 46 AT LBL 75 STATION 1197+126. AREA REWORKED AND FOUND TO BE WITHIN LIMITS PER SRM 53-00-52. REWORKED AREA ALODINED AND PAINTED. 2 L 7 2 4F RT A1NM 2007101100177 20071011 00177 EA 2007 10 11 A6WA200740523 1 20070919 A 5347 CARGO TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 FOUND CARGO DOOR FORWARD TRACK LOWER AT CHANNEL CRACKED. 10-24-07 MAINTENANCE REPLACED C-CHANNEL IAW CRJ SRM 51-42-06 . (M) 2 L 7 2 4F RT A21EA 2007101100180 20071011 00180 EA 2007 10 11 A6WA200740526 1 20070921 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 FOUND FS 280 RBL 9 OUTBOARD ATTACH CLIP IS CRACKED. 10-24-07 MAINTENANCE REMOVED AND REPLACED LCIP P/N 601R31113-58 IAW CRJ SRM 51-42-06, 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007101100182 20071011 00182 EA 2007 10 11 A6WA200740514 1 20070919 A 5740 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA LT ELEVATOR DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 468AW 7916 LT ELEVATOR NR 1 HYD SYSTEM PCU ATTACHMENT FITTING ASSY ON ELEVATOR, P/N 601R24056-45, HAS SHEARED LOCK FASTENER AT BOTT OM OF LINE. 10-25-07 MAINTENANCE REPLACED LOCK FASTENER IAW SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007101100185 20071011 00185 EA 2007 10 11 A6WA200740515 1 20070919 A 5740 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA LT ELEVATOR DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 468AW 7916 LT ELEVATOR NR 2 HYD SYSTEM PCU ATTACHMENT FITTING ASSY ON ELEVATOR, P/N 601R24056-443, HAS SHEARED LOCK FASTENER AFT BO TTOM OF LINK. IAW SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007101100186 20071011 00186 NM 2007 10 11 AMTA200700462 1 20070921 A 2120 DUCT BOEING 737 73783N 13844HI NM A/C PACK MISSING A AMTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 11 318TZ 28247 LT PACK ILLUMINATED DURING CLIMB PACK RESET BUT ILLUMINATED AGAIN TEMP WAS ABOUT 185. FOUND DISCHARGE DUCT TO ACM MISSI NG COUPLING, SECURED DUCT AND INSTALLED NEW COUPLING, LEAK CHECK GOOD, OPERATED PACK, TEMP 60 DEGREES NORMAL, PERFORMED BITE IAW FIM 21-62-00-810-801, NO FAULTS. (K) 2 L 7 2 4F RT A16WE 2007101100189 20071011 00189 EA 2007 10 11 A6WA200740516 1 20070919 A 5410 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA RT ELEVATOR DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 468AW 7916 RIGHT ELEVATOR NR 3 HYD SYSTEM PCU ATTACHMENT FITTING ASSY ON ELEVATOR, P/N 601R24056-41, HAS SHEARED LOCK FASTENER AT B OTTOM OF LINK. 10-25-07 MAINTENANCE REPLACED LOCK FASTENER IAW SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007101100191 20071011 00191 NM 2007 10 11 AMTA200700473 1 20070930 A 5751 90004212 SENSOR BOEING 737 73783N 13844HI NM NR 3 FLAP UNSERVICEABLE A AMTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 310TZ 28243 ON CLIMBOUT OF LGA FLAPS FAILED TO RETRACT SHOWING ASYMETRIC CONDITION L 71/4 DEGREES R5 DEGREES. REMOVED AND REPLACED NR3 FLAP SKEW SENSOR IAW 27-59-01-2 OF MM OPS CHECK AND RIG CHECK GOOD. (K) 2 L 7 2 4F RT A16WE 2007052200121 20070522 00121 NM 2007 5 22 SWAA072522 1 20070520 A 3350 MS155721 LAMP BOEING 737 7373T5 1384608 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007052200122 20070522 00122 NM 2007 5 22 SWAA072521 1 20070520 A 3350 MS155721 LAMP BOEING 737 7373T5 1384608 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007052200127 20070522 00127 SO 2007 5 22 C2XA07IA119 1 20070517 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO CABIN ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 13132 145708 IAH - FLT 2765, DURING PREFLIGHT INSPECTION THE CREW REPORTED A FUEL ODOR IN THE CABIN. MAINTENANCE INSPECTED THE AIRCR AFT, RAN ENGINES AND PACKS AND COULD NOT DUPLICATE THE DISCREPANCY, SO THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007052200131 20070522 00131 NM 2007 5 22 SWAA072417 1 20070517 A 3260 189983 SENSOR BOEING 737 7373A4 1384585 NM RT MLG FAULTY A SWAA O OTHER J WARNING INDICATION CL CLIMB 1 SW 29 680AA 23505 AFTER GEAR RETRACTION WITH GEAR HANDLE IN OFF POSITION, RIGHT MLG RED LIGHT ILLUMINATED. CYCLED GEAR LIGHT EXTINGUISHED . REMOVED AND REPLACED RIGHT MLG UPLOCK SENSOR PER MM. 2 L 7 2 4F RT A16WE 2007052200139 20070522 00139 2007 5 22 SWAA072412 4 20070514 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 466WN 30677 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052200142 20070522 00142 NM 2007 5 22 SWAA072410 1 20070514 A 2797 6544784 WIRE BOEING 737 737317 138447P NM NR 5 SLAT BROKEN A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 661SW 23173 AIR TURNBACK, ON FLAP RETRACTION RIGHT WING NR 5 L/E SLAT WOULD NOT RETRACT. CYCLED FLAPS PER QRH, NO HELP. FOUND BROK EN WIRE AT NR 5 L/E SLAT ACTUATOR, REPAIRED WIRE PER MM. 2 L 7 2 4F RT A16WE 2007052200144 20070522 00144 NM 2007 5 22 SWAA072444 1 20070517 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 444 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 444, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007052200146 20070522 00146 NM 2007 5 22 SWAA072428 1 20070515 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM BS 763 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 763, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007052200152 20070522 00152 NM 2007 5 22 SWAA072407 1 20070513 A 5312 6545819 PRESSURE PANEL BOEING 737 7373T5 1384608 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED MV1 CHECK, FOUND NLG W/W PRESSURE PANEL WEB CRACKED AT RIGHT BS 239, WL 170. REPAIRED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2007052200166 20070522 00166 2007 5 22 AWXA200700643 4 20070516 A 2565 D31576317 SLIDE AIRBUS A319 A319132 3930340 NM L1 DOOR DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 832AW 28255 10445 1643 SAL - EES - BC-4 CHECK - THE L1 DOOR EMERGENCY ESCAPE SLIDE WAS FOUND TO BE EXPANDED/PARTIALLY INFLATED DURING A VISUAL INSPECTION OF THE SLIDE. THE L1 DOOR EMERGENCY ESCAPE SLIDE WAS REPLACED IAW AWA TASK CARD R1C25311. 2 L 7 2 4F RT A28NM 2007052200167 20070522 00167 2007 5 22 AWXA200700644 4 20070516 A 2565 D31517317 SLIDE AIRBUS A319 A319132 3930340 NM R2 DOOR DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 832AW 13717 5971 1643 SAL - EES - BC-4 CHECK - THE R2 DOOR EMERGENCY ESCAPE SLIDE WAS FOUND TO BE EXPANDED/PARTIALLY INFLATED DURING A VISUA L INSPECTION OF THE SLIDE. THE R2 DOOR EMERGENCY ESCAPE SLIDE WAS REPLACED IAW AWA TASK CARD R1C25311. 2 L 7 2 4F RT A28NM 2007052200169 20070522 00169 NM 2007 5 22 AWXA200700646 1 20070418 A 5330 654576655 SKIN BOEING 737 73733A 1384673 NM BS 381 S14L CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - C-20 CHECK - FOUND CRACKED FUSELAGE SKIN, BS 381, S14L. REPAIRED FUSELAGE SKIN, BS 381, S14L IAW B 737-300 SRM 53-00-01-2R30, FIGURE 201. 2 L 7 2 4F RT A16WE 2007052200172 20070522 00172 NM 2007 5 22 AWXA200700649 1 20070417 A 5330 654576656 SKIN BOEING 737 73733A 1384673 NM BS 501 S14R CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - C-20 CHECK - CRACKED FUSELAGE SKIN, BS 501, S14R. REPAIRED FUSELAGE SKIN, BS 501, S14R IAW B737-30 0 SRM 53-00-01-2R30, FIGURE 201. 2 L 7 2 4F RT A16WE 2007052200175 20070522 00175 NM 2007 5 22 AWXA200700633 1 20070516 A 5330 6545767 SKIN BOEING 737 73733A 1384673 NM BS 373 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 PHX - MAJOR REPAIR - FUSELAGE SKIN CRACKED, BS 373.2, S14L - S15L, AFT AND BELOW L-1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY. REPAIRED FUSELAGE SKIN CRACKED, BS 373.2, S14L - S15L, AFT AND BELOW L-1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY IAW AWA ER 03-5331-07136-SS2 . 2 L 7 2 4F RT A16WE 2007052200177 20070522 00177 NM 2007 5 22 AWXA200700637 1 20070423 A 5311 6558280511 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - CRACKED FUSELAGE FRAME FOOT, BS 360, S14R, WL 228. REPLACED FUSELAGE FRAME FOOT, BS 360, S14R, WL 228 IAW B737-300 SRM 53-00-07-2R7, FIGURE 201. 2 L 7 2 4F RT A16WE 2007052200181 20070522 00181 WP 2007 5 22 07FDEA01814 1 20070515 A 5311 FRAME DOUG DC10 DC1010F 3022111 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 LT AIR CONDITION COMPT SEVERE CORROSION WITH EXFOLIATION ON FRAME AT STA 495 X=28, REPAIR IAW SRM 53-00-01 FIG 8 VOL 1. 2 L 7 3 4F A22WE 2007052300002 20070523 00002 NM 2007 5 23 2007UALA01533 1 20070518 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EEL LIGHTS INOP AT SEAT 1J FWD AND AFT LIGHT ASSY'S. [SUP 06-06-07] SECURED CONNECTOR. OPS. CKS. NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052300004 20070523 00004 NM 2007 5 23 2007UALA01535 1 20070517 A 3350 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 510UA 24780 EMERGENCY EXIT SIGN L26 INOP. [SUP 06-06-07] REPLACED LIGHT SWITCH. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300021 20070523 00021 2007 5 23 2007UALA01553 4 20070519 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 DOOR 2R SLIDE PRESSURE OUT OF LIMITS. [06-14-07] THERE WAS A SMALL LEAK AT THE SHAFT O-RING. REPLACED NR 2 RT SLID E. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300022 20070523 00022 NM 2007 5 23 2007UALA01554 1 20070519 A 3213 CYLINDER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT MLG CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 RIGHT MLG OUTER CYLINDER JUST ABOVE INNER THREADS FOR GLAND NUT IS HEAVILY CORRODED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300030 20070523 00030 NM 2007 5 23 2007UALA01565 1 20070519 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY LIGHT ROW 40 RIGHT INOP. [SUP 06-06-07] RESECURED CONNECTOR. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052300031 20070523 00031 NM 2007 5 23 2007UALA01566 1 20070519 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY LIGHT ROW 38 LEFT INOP. RELAMPED EMERGENCY LIGHT. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052300035 20070523 00035 NM 2007 5 23 2007UALA01570 1 20070520 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EEL 2J & 3A AFT ARE INOPERATIVE. RELAMPED EEL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052300047 20070523 00047 NM 2007 5 23 2007UALA01274 1 20070423 A 3260 856917 PSEU BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RT BODY MLG FAULTY A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 179UA 25158 THE -GEAR TILT- MSG DISPLAYED AFTER TAKEOFF. FLIGHT CREW DID NOT ATTEMPT TO RETRACT GEAR PER IRREG PROC 14.40.6. RETUR NED TO HKG. CMC DOWNLINK SHOWS RIGHT BODY GEAR TRUCK TILT FAULTING BOTH PRIMARY & ALTERNATE PROX SWITCH. PROX SWITCH E LECTRONIC UNIT REPLACED PER MM 32-09-03. AFTER INSTALLATION, FOUND SATISFACTORY. NO MSG DISPLAYED. A/C RETURNED TO SE RVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052300048 20070523 00048 2007 5 23 2007UALA01482 4 20070510 A 2565 CYLINDER AIRCRUISERS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 1126 25397 PRESSURE IN CYLINDER NOT IN LIMITS. NO LEAK WAS FOUND. REPLACED WITH ANOTHER BOTTLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300049 20070523 00049 EU 2007 5 23 2007UALA01483 1 20070511 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 415UA 475 DURING 3 SVC, CABIN EMERGENCY LIGHT TEST DID NOT PASS. [SUP 06-06-07] REPAIRED BROKEN WIRE AT DOOR HINGE.TESTED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052300050 20070523 00050 EU 2007 5 23 2007UALA01484 1 20070511 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 433UA 589 STRINGER 43 LEFT HAS CORROSION FRAME 57 AND 58. MAJOR REPAIR ACCOMPLISHED: INSTALLED ANGLE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052300052 20070523 00052 EU 2007 5 23 2007UALA01486 1 20070511 A 5314 ANGLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 411UA 464 LOWER KEEL BEAM FRAME 47 FAIRING ATTACH ANGLE LEFT SIDE IS CRACKED. MAJOR REPAIR ACCOMPLISHED: REPLACED ANGLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052300053 20070523 00053 EU 2007 5 23 2007UALA01487 1 20070511 A 5314 ANGLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 411UA 464 LOWER KEEL BEAM FAIRING SUPPORT ANGLE RIGHT SIDE AT FRAME 46 IS CRACKED. MAJOR REPAIR ACCOMPLISHED: REPLACED ANGLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052300056 20070523 00056 NM 2007 5 23 2007UALA01490 1 20070512 A 2697 WIRE HARNESS BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FIRE WARNING DAMAGED A UALA A F UNSCHED LANDING ACTIVATE FIRE EXT. J WARNING INDICATION CL CLIMB 1 WP 29 932UA 26658 RTFL UNDER AMBER ALERT DUE TO APU FIRE LIGHT. FOUND BAD CONNECTOR ON OVERHEAT LOOP HARNESS. REPLACED HARNESS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007052300062 20070523 00062 NM 2007 5 23 SWAA072498 1 20070517 A 5311 6546548 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052300063 20070523 00063 NM 2007 5 23 SWAA072502 1 20070517 A 5311 6546550 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052300064 20070523 00064 NM 2007 5 23 SWAA072499 1 20070517 A 5311 6546552 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052300065 20070523 00065 NM 2007 5 23 SWAA072501 1 20070517 A 5311 6546555 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052300066 20070523 00066 NM 2007 5 23 SWAA072500 1 20070517 A 5311 6546555 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052300076 20070523 00076 NM 2007 5 23 SWAA072471 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007052300078 20070523 00078 NM 2007 5 23 SWAA072478 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007052300082 20070523 00082 NM 2007 5 23 SWAA072469 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300083 20070523 00083 NM 2007 5 23 SWAA072479 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007052300085 20070523 00085 NM 2007 5 23 SWAA072481 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007052300090 20070523 00090 NM 2007 5 23 SWAA072488 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300097 20070523 00097 NM 2007 5 23 SWAA072483 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300098 20070523 00098 NM 2007 5 23 SWAA072510 1 20070519 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007052300105 20070523 00105 NM 2007 5 23 SWAA072525 1 20070520 A 5753 6545321 ATTACH FITTING BOEING 737 7373H4 1384600 NM T/E FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED BRDG CHECK, FOUND LEFT WING NR 1 FLAP TRACK AFT ATTACH FITTING CORRODED. REMOVED AND REPLACED AFT FITT ING PER SRM AND BOEING DRAWING. 2 L 7 2 4F RT A16WE 2007052300107 20070523 00107 NM 2007 5 23 SWAA072524 1 20070520 A 5315 6545410 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 662, RBL 24.5. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2007052300108 20070523 00108 NM 2007 5 23 SWAA072506 1 20070518 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 444, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007052300111 20070523 00111 NM 2007 5 23 SWAA072520 1 20070520 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007052300112 20070523 00112 NM 2007 5 23 SWAA072507 1 20070518 A 5753 6546434 FLAP BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP CRACKED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007052300114 20070523 00114 NM 2007 5 23 SWAA072451 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300119 20070523 00119 NM 2007 5 23 SWAA072460 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300120 20070523 00120 NM 2007 5 23 SWAA072458 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300124 20070523 00124 NM 2007 5 23 SWAA072449 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300148 20070523 00148 NM 2007 5 23 ASAA0791657 1 20070517 A 5320 146A94014 FLOOR SUPPORT BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO PIT FLOOR SUPPORT -T- CORRODED. REPAIRED IAW SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007052300152 20070523 00152 NM 2007 5 23 ASAA0791661 1 20070517 A 5320 146A750351 CHANNEL BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO FLOOR CHANNEL AT BS 767+5 CORRODED. REPAIRED IAW SRM EA 5310 02720. 2 L 7 4 4F RT A16WE 2007052300153 20070523 00153 NM 2007 5 23 ASAA0791662 1 20070517 A 5320 146A750611 SPLICE BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 317AS 30856 AFT CARGO CHANNEL SPLICE CORRODED. REPAIRED IAW SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007052300156 20070523 00156 NM 2007 5 23 ASAA0791665 1 20070517 A 5320 146A750611 SPLICE BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO PIT CHANNNEL SPLICE CORRODED. REPAIRED IAW SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007052300157 20070523 00157 NM 2007 5 23 ASAA0791666 1 20070517 A 5347 146A750613 SPLICE BOEING 737 737990 NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO TIE DOWN SPLICE CORRODED. REPAIRED IAW SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007052300158 20070523 00158 NM 2007 5 23 ASAA0791667 1 20070517 A 5320 146A812712 INTERCOSTAL BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO FLOOR SUPPORT INTERCOSTAL CORRODED. 2 L 7 4 4F RT A16WE 2007052300159 20070523 00159 NM 2007 5 23 ASAA0791668 1 20070517 A 5320 146A750222 CHANNEL BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO Z-CHANNEL CORRODED. REPAIRED IAW SRM 53-00-53 FIG 201. 2 L 7 4 4F RT A16WE 2007052300162 20070523 00162 NM 2007 5 23 ASAA0791671 1 20070517 A 5320 146A750223 ANGLE BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO Z-ANGLE CORRODED. REPAIRED IAW SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007052300165 20070523 00165 NM 2007 5 23 ASAA0791674 1 20070517 A 5321 453A261067 FLOOR PANEL BOEING 737 737990 NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO FLOOR PANEL CORRODED. REPAIRED IAW SRM 51-40-02. 2 L 7 4 4F RT A16WE 2007052300166 20070523 00166 NM 2007 5 23 ASAA0791675 1 20070517 A 5321 453A26109 FLOOR PANEL BOEING 737 737990 NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO FLOOR PANEL CORRODED. REPAIRED IAW SRM 51-40-02. 2 L 7 4 4F RT A16WE 2007052300167 20070523 00167 NM 2007 5 23 ASAA0791676 1 20070517 A 5321 453A261019 FLOOR PANEL BOEING 737 737990 NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO FLOOR PANEL CORRODED. REPAIRED IAW SRM 51-40-02. 2 L 7 4 4F RT A16WE 2007052300168 20070523 00168 NM 2007 5 23 ASAA0791677 1 20070517 A 5320 146A750344 FLOOR SUPPORT BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO FLOOR SUPPORT CHANNEL CORRODED. REPAIRED IAW SRM 5310 02720. 2 L 7 4 4F RT A16WE 2007052300171 20070523 00171 2007 5 23 2007UALA01493 4 20070511 A 2565 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU R2 DOOR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 307UA 23668 2R DOOR SLIDE COMING OUT OF SLIDE PACK. [06-14-07] REPLACED SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007052300174 20070523 00174 NM 2007 5 23 2007UALA01496 1 20070514 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 119UA 28812 EVAC PATH LIGHT BROKEN AND HANGING IN AISLE BY CORD AT 1J. SECURED LIGHT TO SEAT. OPS CHECKS OK PER MM. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052300175 20070523 00175 NE 2007 5 23 2007UALA01497 2 20070512 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 29 570UA 26678 726521 ODOR OF OIL IN COCKPIT AFTER TAKEOFF. ODOR DISSIPATED AFTER SEVERAL MINUTES. [SUP 06-06-07] ACCOMPLISHED TROUBLE SHOO TING, REPLACED RECIRCULATION FILTERS (LT,RT). RAN ENGINES AND APU WITH PACKS ON, FOUND WHAT APPEARED TO BE OIL RESIDUE ALONG INNER DIAMATER OF NR 3 BEARING COMPARTMENT HUB AREA. OIL ODOR IN COCKPIT ON TAKE OFF. ODOR CAME DURING APPLICATI ON OF T.O. PWR UP TO ABOUT 5,000 AGL. SUSPECT NR 1 ENGINE CAUSE OF SMELL . BOROSCOPE NR 3 BRG COMPARTMENT FOR ANY EVIDEN CE OF OIL. NR 1 ENGINE 4 FAN BLADES HAVE NICKS BLADES HAVE NUMBERS 28,17,18, 26. BLENDED BLADES PER UA SPECS. REPLACE D NR 1 ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300176 20070523 00176 NM 2007 5 23 2007UALA01499 1 20070512 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 551UA 25399 DOOR R1 EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. [SUP 06-06-07] REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300177 20070523 00177 NM 2007 5 23 2007UALA01500 1 20070512 A 3397 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 508UA 24744 SEAT EEL LIGHTS OUT FROM 9AB - 11AB. [SUP 06-06-07] RESEATED CONNECTOR FROM INVERTER TO SEAT LIGHTS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300179 20070523 00179 NM 2007 5 23 ASAA0791679 1 20070521 A 5320 146A812710 INTERCOSTAL BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO PIT FLOOR SUPPORT INTERCOSTAL CORRODED. REPAIRED IAW SRM 51-30-01. 2 L 7 4 4F RT A16WE 2007052300180 20070523 00180 NM 2007 5 23 ASAA0791680 1 20070517 A 5347 146A750130 CARGO TRACK BOEING 737 737990 NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO PIT TIE DOWN TRACK CORRODED. REPAIRED IAW SRM 53-00-53. 2 L 7 4 4F RT A16WE 2007052300182 20070523 00182 NM 2007 5 23 ASAA0791682 1 20070517 A 5347 143A7501105 CARGO TRACK BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 FWD CARGO PIT CORROSION ON RIGHT CARGO TRACK. REPAIRED IAW SRM 53-00-53. 2 L 7 4 4F RT A16WE 2007052300183 20070523 00183 NM 2007 5 23 ASAA0791683 1 20070517 A 5320 146A81214 STRAP BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO DOORWAY FLOOR STRAP CORRODED. REPAIRED IAW SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007052300187 20070523 00187 NM 2007 5 23 ASAA0791687 1 20070517 A 5320 146A8125 WEB BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO PIT DOORWAY LOWER WEB CORRODED. REPAIRED IAW SRM EA 5320 01805. 2 L 7 4 4F RT A16WE 2007052300188 20070523 00188 NM 2007 5 23 ASAA0791688 1 20070517 A 5320 146A74022 PAN BOEING 737 737990 NM LAV SERVICE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT LAV SVC PORT LINER PAN CORRODED. REPAIRED IAW SRM 51-40-02. 2 L 7 4 4F RT A16WE 2007052300191 20070523 00191 NM 2007 5 23 2007UALA01504 1 20070514 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 536UA 25156 EEL STRIP IN FRONT OF FWD AFT LAV INOPERATIVE. REPLACED EEL STRIP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300196 20070523 00196 NM 2007 5 23 2007UALA01510 1 20070513 A 5210 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L3 DOOR LOW PRESSURE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 553UA 25277 DOOR 3L OPEN ASSIST PRESSURE IS IN RED ZONE. [SUP 06-06-07] REPLACED BOTTLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300198 20070523 00198 2007 5 23 2007UALA01513 4 20070516 A 2565 D2340117 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 LOW BOTTLE PRESSURE. [SUP 06-06-07] NO LEAK FOUND, WATER TESTED FOR 15 MIN. TOPPED OFF BOTTLE PRESSURE AND LET SIT FO R 24 HOURS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300200 20070523 00200 NM 2007 5 23 2007UALA01515 1 20070515 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 LEFT FUSELAGE SKIN HAS 5 DENTS FROM STA 600 - 660, BETWEEN STR 17L AND 18L. [SUP 06-06-07] MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SKIN AND INSTALLED A DOUBLER REPAIR. THIS IS A TEMP REPAIR, LIMITED TO 12 MONTHS FROM 8MAY07, AND A N EW FAA 8100-9 MUST BE ISSUED PRIOR TO THAT TIME, IN COMPLIANCE TO 14 CFR 25.571. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300206 20070523 00206 NM 2007 5 23 SWAA072538 1 20070521 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 776WN 30591 EEPLS END CAP LOOSE AT ROW 3 DEF. SECURED END CAP PER MM. 2 L 7 2 4F RT A16WE 2007052900181 20070529 00181 EU 2007 5 29 PNSA070504 1 20070517 A 5610 7256100501 WINDSHIELD SAAB SF340 340B 7860101 EU COCKPIT CRACKED A PNSA O OTHER O OTHER DE DESCENT 1 AL 03 675PA 1189 340B206 PRIOR TO DESCENT CAPTAIN`S FRONT WINDSHIELD CRACKED. REMOVED AND REPLACED CAPTAIN'S WINDOW. 2 L 7 2 4T RT A52EU 2007052900182 20070529 00182 SO 2007 5 29 LR7A07018 1 20070516 A 2820 24C117 CHECK VALVE LKHEED 382 382G 526414U SO FUEL SYSTEM LEAKING A LR7A E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 AL 03 404LC 25 4763 FLIGHT CREW REPORTED VISUAL FLUID LEAK BEHIND NR 3 ENGINE ON CLIMBOUT FROM TIN. PERFORMED PRECAUTIONARY SHUT DOWN ON EN GINE NR 3 IAW WITH PROCEDURES AND DIVERTED TO ANC FOR MAINTENANCE. FOUND FUEL LEAKAGE INTO PREVIOUSLY DE-ACTIVATED AUXI LARY TANK BLADDER DURING REFUELING, DUE TO DEFECTIVE CHECK VALVE. REPLACED CHECK VALVE, LOG PAGE 26636 GMM133 ITEM M14. REPLACED RIGHT AUXILARY FUEL TANK BLADDERS, LOG PAGE 26636 ITEM 1. 2 H 7 4 4T A1SO 2007052900184 20070529 00184 CE 2007 5 29 BSAASDR0713 1 20070515 A 2697 70522 WIRE HARNESS BEECH 1900 1900D 1154162 CE LT FIRE LOOP GROUNDED A BSAA O OTHER N FALSE WARNING DE DESCENT 1 NM 05 132YV UE132 DURING DESCENT MASTER CAUTION AND LEFT FIRE WALL FUEL VALVE LIGHT FLICKERED. CREW LANDED WITHOUT INCIDENT. AFTER LANDI NG LEFT FIRE LOOP WOULD NOT TEST. FOUND FIRE LOOP GROUNDING AT THE FIREWALL WIRE HARNESS FEED THRU. WIRE HARNESS FEED THRU WAS ADJUSTED TO PREVENT THE FIRE LOOP FROM GROUNDING, OPERATIONAL CHECKS PERFORMED WITH NO OTHER DEFECTS NOTED. 2 L 7 2 4T RT A24CE 2007052900187 20070529 00187 EA 2007 5 29 TRAX200700703 1 20070521 A 5321 PRESSURE PANEL CNDAIR CL600 CL6002B19 1900309 EA BS 460 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 851AS 7360 PRESSURE FLOOR SKIN CORRODED AT FS 460 BETWEEN LBL 27.00 AND LBL 36.00 (MARKED). 2 L 7 2 4F RT A21EA 2007052900189 20070529 00189 EA 2007 5 29 TRAX200700705 1 20070521 A 3350 POWER SUPPLY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 843AS 7310 NR 3 POWER PACK FOR EMERGENCY LIGHTS INOP. 2 L 7 2 4F RT A21EA 2007052900190 20070529 00190 EU 2007 5 29 TRAX200700706 1 20070521 A 7930 OIL SYSTEM AEROSP ATR72 ATR72 EU NR 1 ENGINE LOW PRESSURE A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 640AS 405 ENG NR 1 LOW OIL PRESSURE IN FLIGHT. COMPLIED WITH QRH RETURNED TO ATL. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECL ARED. 2 H 7 2 4T RT 2007053000004 20070530 00004 NM 2007 5 30 AMTA200700217 1 20070503 A 2810 FUEL SYS BOEING 737 73783N 13844HI NM CONTAMINATED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 317TZ 28246 SHORTLY AFTER TAKEOFF, NR 1 FUEL TANK GAUGE DECREASED TO 6,800 NR WITH IMBALANCE INDICATION. OVER SEVERAL MIN, TO 7,200 NR, AFTER LANDING, NR 1 READ 5,800 NR AND NR 2 INDICATED 7,500 NR. IMBALANCE INDICATION READ OUT. FUEL DID NOT FIND A NY EVIDENCE OF DAMAGE TO THE TANK UNITS OR WIRING HARNESS, FOUND EVIDENCE OF MICROBIAL GROWTH AND EXCESS AMOUNT OF WATER CLEANED TANKS IAW 28-10-00-100. (K) 2 L 7 2 4F RT A16WE 2007053000107 20070530 00107 EA 2007 5 30 SWIA200718253 1 20070402 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 720 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 STRUCTURE AT FS 720 UNDER RT PACK IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED NEW SUPPORT ANGLE P/N 601R95159-25 AND C LIP P/N 601R95159-37 UNDER RIGHT PACK PER CRJ200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007053000108 20070530 00108 EA 2007 5 30 SWIA200718255 1 20070402 A 5315 ATTACH BRACKET CNDAIR CL600 CL6002B19 1900309 EA FLOORBEAM CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 CABIN FLOORBEAM CLIP CRACKED AT FS484 RBL27, DISCOVERED AT C-CHECK. INSTALLED NEW CLIP AT CABIN FLOORBEAM FS 484 RBL 27 PER REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2007053000109 20070530 00109 EA 2007 5 30 SWIA200718256 1 20070402 A 5210 BRACKET CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 PASSENGER DOOR HAS CRACKED BRACKET UNDER THE CLOSING PLATE, DISCOVERED AT C-CHECK. INSTALLED NEW SUPPORT BRACKET PER CR J200 SRM 51-41-02 PG 5. 2 L 7 2 4F RT A21EA 2007053000110 20070530 00110 EA 2007 5 30 SWIA200718257 1 20070402 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 THE FORWARD WEB ON THE PAX DOOR IS CRACKED IN THE RADIUS BETWEEN THE SECOND AND THIRD STEPS, DISCOVERED AT C-CHECK. INS TALLED REPAIR PARTS 601R-52-11-1223 -2,-3,-4 AT PAX DOOR FORWARD WEB PER REO 601R-52-11-1223 SHTS 1-3. 2 L 7 2 4F RT A21EA 2007053000111 20070530 00111 EA 2007 5 30 SWIA200718258 1 20070520 A 3350 RELAY CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 727SK 10191 EMERGENCY LIGHTS ARE FLASHING ON AND OFF IN THE ARMED POSITION. REPLACED RELAY K135. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007053000112 20070530 00112 EA 2007 5 30 SWIA200718259 1 20070522 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 954SW 7815 ONE OVERHEAD EMERGENCY LIGHT POD IS INOP. REPLACED BULB AT OVERHEAD CABIN EMERGENCY LIGHT IAW 33-51-16. 2 L 7 2 4F RT A21EA 2007053000113 20070530 00113 SO 2007 5 30 SWIA200718260 1 20070515 A 3350 BATTERY EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT UNKNOWN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 220SW 11421 4873 120288 EMERGENCY LIGHTS CIRCUIT BREAKER POPS WITH THE SWITCH IN THE OFF POSITION. REPLACED THE FORWARD EMERGENCY LIGHT BATTERY . SYSTEM TESTS GOOD. 2 L 7 2 4T RT A31SO 2007053000114 20070530 00114 EU 2007 5 30 AWXA200700657 1 20070526 A 5321 D5367180500200 FLOOR PANEL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 603AW 661 SAL - CORROSION ON CABIN FLOORBOARD 261FF, FR 66 - FR 68, +Y1292 TO +Y1732. REPLACED CABIN FLOORBOARD 261FF, FR 66 - FR 68, +Y1292 TO +Y1732 IAW AWA TASK CARD C1D25318. 2 L 7 2 4F RT A28NM 2007053000115 20070530 00115 EU 2007 5 30 AWXA200700658 1 20070526 A 5315 D53472284008 FLOORBEAM AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 603AW 661 SAL - CORROSION ON CABIN FLOORBEAM, -Y465, FR 66 + 4". REPLACED CABIN FLOOR BEAM, -Y465, FR65 - FR 67 IAW A320 SRM 51-7 2-11. 2 L 7 2 4F RT A28NM 2007053000116 20070530 00116 EU 2007 5 30 AWXA200700659 1 20070525 A 5315 D53112818200 FLOORBEAM AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 603AW 661 SAL - CORROSION ON CABIN FLOOR SUPPORT, +Y254, FR 16. REPAIRED CABIN FLOOR SUPPORT, +Y254, FR 16 IAW A320 SRM 53-11-14, FIGURE 203. 2 L 7 2 4F RT A28NM 2007053000117 20070530 00117 EU 2007 5 30 AWXA200700660 1 20070525 A 5347 D53472190203 SEAT TRACK AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 603AW 661 SAL - CORROSION ON CABIN SEAT RAIL, -Y765, FR 66 + 4". REPLACED CABIN SEAT RAIL, -Y765, FR 64 - FR 66 IAW A320 SRM 51-7 2-11. 2 L 7 2 4F RT A28NM 2007053000118 20070530 00118 WP 2007 5 30 07FDEA01813 1 20070515 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 397FE 46631 MODIFICATION AND REPAIR ASSESSMENT ON 13 APRIL 2007, DURING PNEUMATIC TESTS WITH AIR, AT 9:30 A.M. THE PRESSURIZED AIR FLEXIBLE HOSE COLLAPSED CAUSING THE END CONNECTING TO THE HANGAR UNDERFLOOR MANIFOLD TO HIT THE LOWER FUSELAGE JUST FWD OF C.A.C. THE IMPACT BETWEEN THE SDR DELETE BECAUSE FOR REPAIR ASSESSMENT NOT REQUIRED. REMOVED FASTENERS, PERFORMED STRIP PAINT, PENETRANT INSPECTION AND VISUAL INSPECTION. REMOVED RADIO ALTIMETER, PERFORMED CUT LONG 52. REPAIRED LONG 52 AND SKIN IAW SRM 53-10-00 FIG 1-2 AND SRM 53-20-00 FIG 6. INSTALLED RADIO ALTIMETER ANTENNA , AND FUNCTIONAL TEST IAW MM 34-42-03-4 AND DWG SP 10240167 AND MM 34-42-00-5. 2 L 7 3 4F RT A22WE 2007053000119 20070530 00119 NM 2007 5 30 DU4R2007121 1 20070517 A 5313 STRINGER BOEING 757 757232 1384965 NM BS 750 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 602DL 22809 FOUND CORROSION ON STRINGER AND SKIN AT BS 750 S-23R. REPAIRED BY CUTTING OUT SECTION OF STRINGER. FABRICATED AND INST ALLED STRINGER REPAIR 14 BY 3.5 FROM BAC1498-204 IAW B757 SRM 51-20-01 AND 53-00-03 FIG 201. 2 L 7 2 4F RT A2NM 2007053000120 20070530 00120 EU 2007 5 30 AWXA200700661 1 20070525 A 5347 D53472190204 SEAT TRACK AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 603AW 661 SAL - CORROSION ON CABIN SEAT RAIL, +Y1292, FR 66. REPLACED CABIN SEAT RAIL,+Y1292, FR 64 - FR 66 IAW A320 SRM 51-72-11 . 2 L 7 2 4F RT A28NM 2007053000121 20070530 00121 SO 2007 5 30 200714502 1 20070524 A 7331 23052613 SENSOR EMB 135 EMB135LR 3260305 SO FUEL SYSTEM DEFECTIVE A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 725AE 4445 3287 145312 FUEL FLOW INDICATOR READS 0. LOW SPEED ABORTED TAKEOFF. REMOVED AND REPLACED ENGINE 2 FUEL FLOW SENSOR. OPERATIONAL AN D LEAK CHECKS GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007053000122 20070530 00122 SO 2007 5 30 2007 1 20070521 A 3320 BR00022 BALLAST EMB 145 EMB145LR 3260212 SO CABIN LIGHTS DEFECTIVE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 619AE 145101 FLIGHT ATTENDANT REPORTED A ELECTRICAL ODOR IN FRONT OF CABIN. REMOVED AND REPLACED GALLEY CEILING LIGHT BALLAST IAW EM B MM. OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007053000123 20070530 00123 EU 2007 5 30 AWXA200700662 1 20070525 A 5320 D5347217200 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 603AW 661 SAL - FOUND CORROSION ON CABIN FLOOR SUPPORT, +Y1192, FR 66 + 4" TO FR 67 + 15". REPLACED CABIN FLOOR SUPPORT,+Y1192, F R 66 + 4" TO FR 67 + 15" IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007053000124 20070530 00124 EU 2007 5 30 AWXA200700663 1 20070525 A 5320 D53571550226 ANGLE AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 603AW 661 SAL - CORROSION ON SUPPORT ANGLE, FR 71 S27R - S32R. REPLACED SUPPORT ANGLE, FR 71 S27R - S32R IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007053000125 20070530 00125 NM 2007 5 30 AWXA200700664 1 20070524 A 5320 D53480019216 SHEAR PLATE AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 804AW 1043 SAL - CORROSION ON SHEAR PLATE (TRAY), +Y1175, FR.68 - FR 69. REPLACED SHEAR PLATE (TRAY), +Y1175, FR.68 - FR 69 IAW A3 19 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007053000126 20070530 00126 EU 2007 5 30 AWXA200700665 1 20070524 A 5320 D53472098000 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 603AW 661 SAL - CORROSION ON CABIN FLOOR SUPPORT, + Y919, FR 65 TO FR 67. REPLACED CABIN FLOOR SUPPORT, + Y919, FR 65 TO FR 67 IA W A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007052300020 20070523 00020 EU 2007 5 23 2007UALA01552 1 20070519 A 2897 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUEL INDICATOR DAMAGED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 421UA 500 RIGHT INBOARD AND OUTBOARD FUEL QTY IND 2 AMBER DASHES ON FUEL PAGE. UNRELIABLE DATA. [06-26-07] FAULT TRACING FOUN D FAULTY FUEL BOOST PUMP FUSE CONNECTOR. REPLACED 4044VCA FUSE CONNECTOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052300026 20070523 00026 NM 2007 5 23 2007UALA01561 1 20070519 A 3350 LIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 936UA 26667 EEL STRIP COMING LOOSE AT ROW 6 LEFT SIDE. [SUP 06-06-07] RESECURED EEL STRIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007052300038 20070523 00038 NM 2007 5 23 2007UALA01573 1 20070521 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EEL 3J FWD & AFT INOPERATIVE. RELAMPED EEL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052300039 20070523 00039 NM 2007 5 23 2007UALA01574 1 20070521 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EEL ADJACENT TO LAV 104 INOPERATIVE. [SUP 06-06-07] SECURED CONNECTOR AT LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052300040 20070523 00040 NM 2007 5 23 2007UALA01575 1 20070521 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 EMERGENCY EXIT FLOOR LIGHTING COMING UP AT FIRST CLASS CLOSET. [SUP 06-06-07] SECURED LIGHT STRIP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300055 20070523 00055 NM 2007 5 23 2007UALA01489 1 20070513 A 3350 1619 LIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 925UA 26646 EXTERIOR FUSELAGE LEFT SIDE JUST AFT OF OVERWING EXIT DOOR, EMERGENCY EXIT LIGHT BURNED OUT. RELAMPED EMERGENCY EXIT LI GHT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007052300070 20070523 00070 NM 2007 5 23 SWAA072467 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300081 20070523 00081 NM 2007 5 23 SWAA072466 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300092 20070523 00092 NM 2007 5 23 SWAA072490 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300117 20070523 00117 NM 2007 5 23 SWAA072452 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300125 20070523 00125 NM 2007 5 23 SWAA072459 1 20070517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052300129 20070523 00129 NM 2007 5 23 SWAA072423 1 20070516 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED SERVICE CHECK, FOUND STRINGER 26L CORRODED AT BS 968. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007052300130 20070523 00130 2007 5 23 SWAA072436 4 20070517 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052300138 20070523 00138 NM 2007 5 23 SWAA072431 1 20070517 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 734SA 27866 DURING SCHEDULED MV2 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007052300139 20070523 00139 NM 2007 5 23 SWAA072438 1 20070517 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 438WN 29833 DURING SCHEDULED HC2 CHECK, MID CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM . 2 L 7 2 4F RT A16WE 2007052300140 20070523 00140 NM 2007 5 23 SWAA072405 1 20070513 A 3350 MS155721 LIGHT BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007052300144 20070523 00144 NM 2007 5 23 ASAA0791650 1 20070517 A 5321 453A161081 FLOOR PANEL BOEING 737 737990 NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 FWD CARGO PIT FLOOR PANEL NR 4 CORRODED. REPAIRED IAW SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007052300151 20070523 00151 NM 2007 5 23 ASAA0791660 1 20070517 A 5320 146A7506 SPLICE BOEING 737 737990 NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO PIT FLOOR CHANNEL SPLICE CORRODED. REPAIRED IAW SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007052300161 20070523 00161 NM 2007 5 23 ASAA0791670 1 20070517 A 5320 146A750218 CHANNEL BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO CHANNEL CORRODED. REPAIRED IAW SRM 53-00-53. 2 L 7 4 4F RT A16WE 2007052300186 20070523 00186 NM 2007 5 23 ASAA0791686 1 20070517 A 5320 149A81090114 ATTACH ANGLE BOEING 737 737990 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AFT CARGO FLOOR ATTACH ANGLE CRACKED. REPAIRED IAW SRM 51-40-02. 2 L 7 4 4F RT A16WE 2007052300192 20070523 00192 NM 2007 5 23 2007UALA01505 1 20070514 A 3350 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 536UA 25156 EMERGENCY LIGHTS INOP AT THE FOLLOWING LOCATIONS: AISLE EXIT SIGN ON CEILING PANEL AT ROW 13, EXIT SIGN OVER RIGHT OVER WING HATCHES, EXIT SIGN AT LWR FWD CORNER OF RT FWD OW HATCH, EXIT SIGN AT LWR FWD CORNER OF LT AFT OW HATCH, & RT AFT O VERWING SLIDE LIGHT ON EXTERIOR OF ACFT. REPLACED BATTERY PACK FOR POWER SUPPLY M10568. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300194 20070523 00194 2007 5 23 2007UALA01508 4 20070513 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR MISROUTED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 590UA 28708 THE 2L WILL NOT ARM. [SUP 06-06-07] REROUTED LANYARD CHORD AND THAT APPEARED TO FIX THE PROBLEM. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300197 20070523 00197 NM 2007 5 23 2007UALA01512 1 20070515 A 3830 LAVATORY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 182UA 25279 FLIGHT DIVERTED DUE TO ALL LAVATORIES GOING INOP. HISSING SOUND NOTED BELOW 1R. TRIED TROUBLESHOOTING TO NO AVAIL. [S UP 06-06-07] EXISTING SERVICE BULLETIN 747-38-2109 DIRECTS TO REPLACE RELAY R8432 (LEVEL SENSING TRANSFER RELAY). THIS RELAY IS IDENTIFIED AS THE SINGLE POINT FAILURE WHICH CAUSES ALL 4 WASTE TANK CONTROLLERS TO LOSE PWR. REPLACED RELAY. A/C RETURNED TO SERVICE WITH NO REPEAT OF PROBLEM. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052300205 20070523 00205 NM 2007 5 23 2007UALA01520 1 20070515 A 2822 PUMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUEL SYSTEM FAILED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 545UA 25323 RETURNED TO THE FIELD AFTER THE LOSS OF THE MAIN FUEL PUMP. [SUP 06-06-07] LEFT AFT BOOST PUMP IS REPAIRED TO CONFIRM FIX. AIRCRAFT REMAINED NON-ETOPS UNTIL A POSITIVE FIX OF FUEL PUMP WAS DETERMINED. REPLACED ENGINE FUEL FEED BOOST PU MP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052400003 20070524 00003 EU 2007 5 24 MALA070062 1 20070514 A 3020 HEATER SAAB SF340 340B 7860101 EU RT INTAKE MELTED A MALA O OTHER M B J OVER TEMP SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 GL 15 454XJ 340B454 THE RIGHT ENGINE INTAKE HAS MELTED ON THE LOWER PART. THIS IS THE RUBBER PORTION OF THE HEATER MAT. CREW NOTED ON POST FLIGHT THAT THEY FOUND THE RIGHT INTAKE DUCT BURNED THROUGH. CREW HAD NOTED THEY SMELLED AN ODD BURNING SMELL WHILE ON APPROACH. REMOVED AND REPLACED FORWARD INLET DUCT PN ON/OFF NH24668-169 SN OFF L169282 SN ON L291273. REMOVED AND REPL ACED DEICE CONTROL MODULE PN ON/OFF 44730-501 SN ON A00601 SN OFF A00221 IAW SF 340 AMM 71-60-05 AND IAW ACT MM 30-21-03 . ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2007052400004 20070524 00004 WP 2007 5 24 IXXA07SMN137S 1 20070421 A 5313 LONGERON DOUG DC8 DC871F 302199D WP ZONE 100 MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR INSTALLED AT A-PIT BASKET DOOR, RIGHT AFT JAMB CORNER AT STATIO N 327 LONGERON 30 RIGHT. REMOVED EXISTING REPAIR. FABRICATED DOUBLER, TRIPLER. CLEANED, TREATED AND PRIMED AREA AND RE PAIR PARTS. APPLIED SEALANT TO FAYING SURFACE. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D, DC8 SRM 53-2-0 FIGURE 19 T /R NUMBER 53-136 AND 53-186, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, 51-1-21, AND AD 2005-18-07, DACO SERVICE BULLETIN DC8-53- 078 AND DOUGLAS DRAWING SR08530019 AND 5750776. 2 L 7 4 4F RT 4A25 2007052400007 20070524 00007 NM 2007 5 24 ASAA0741654 1 20070520 A 5523 65C2638428 TAB BOEING 737 7374Q8 138447Q NM ELEVATOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 RIGHT ELEVATOR TAB NR 3 HINGE CUTOUT IS CRACKED. PREPPED DAMAGED AREA, FABRICATED AND BONDED REPAIR IAW SRM 51-70-17 RE PAIR 7. 2 L 7 2 4F RT A16WE 2007052400018 20070524 00018 NM 2007 5 24 07FDEA01817 1 20070515 A 5755 HINGE BOEING 727 7272S2F 1384O81 NM NR 4 SPOILER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 UPPER WING CUT OUT FOR NR 4 SPOILER HINGE HAS TWO SMALL CRACKS, LOCATION OF HINGE IS SECOND HINGE INBOARD FROM OUTBOARD END OF SPOILER STOPPED DRILLED ENDS OF CRACKS AND INSTALLED DOUBLER. REF SRM 57-30-4, FIGURE NR 10, PAGES 27-31. 2 L 7 3 4F A3WE 2007052400021 20070524 00021 NM 2007 5 24 07FDEA01783 1 20070514 A 5753 ARC43632 WEDGE DOUG MD11 MD11 3023602 NM ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 RIGHT WING OUTBOARD FLAP INBOARD WEDGE TRAILING EDGE UPPER SURFACE FOUND DELAMINATED RIGHT WING OUTBOARD FLAP INBOARD WEDGE REMOVED AND REPLACED AS PER AMM 20-50-02, P/N ON: ARC4363-2, S/N ON: 177679-9. 2 L 7 3 4F RT A22WE 2007052400023 20070524 00023 NM 2007 5 24 ASAA0791645 1 20070517 A 5320 1427501165 CHANNEL BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 FWD CARGO PIT CORROSION ON LEFT SUPPORT ZEE. REPAIRED IAW SRM 53-00-53. 2 L 7 4 4F RT A16WE 2007052400025 20070524 00025 NM 2007 5 24 QXEA200700800 1 20070511 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM BS 292-309 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - THERE ARE SIX UNDOCUMENTED DENTS IN AN AREA ALREADY POPULATED WITH DENTS IN THE RIGHT FUSELAGE SKIN JUST AFT OD THE ICE SHIELD FROM STATION X292 TO X309 BETWEEN STRINGER 17S TO 20S. REPAIRED IAW RD8/4-53-0666, RD8/4-53-1905 AND SR M 51-21-10, 51-25-10. 2 H 7 2 4T RT A13NM 2007052400037 20070524 00037 EA 2007 5 24 TRAX200700688 1 20070519 A 5320 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 870AS 7530 LEFT 640 BONDED DOUBLER IS CRACKED. 2 L 7 2 4F RT A21EA 2007052400038 20070524 00038 EA 2007 5 24 TRAX200700689 1 20070519 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 855AS 7395 AFT PRESSURE BULKHEAD HAS CRACK INDICATION AT LBL 27.5 AND APPROX WL 132. 2 L 7 2 4F RT A21EA 2007052400052 20070524 00052 EA 2007 5 24 TRAX200700684 1 20070517 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 836AS 7263 SEAT TRACK ON FLOOR UNDER OVERHEAD BIN 11CD SHOWS SIGNS OF CORROSION. [07-23-07] REPAIRED IAW; 53-21-49, 51-12-00, AND 51-21-06. 2 L 7 2 4F RT A21EA 2007052400055 20070524 00055 EA 2007 5 24 TRAX200700685 1 20070517 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 836AS 7263 CRACK FOUND ON CLIP AT FS 484 LBL 9. 2 L 7 2 4F RT A21EA 2007052400066 20070524 00066 NM 2007 5 24 SWAA072546 1 20070521 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 437WN 29832 DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PA CK PER MM. 2 L 7 2 4F RT A16WE 2007052400070 20070524 00070 NM 2007 5 24 SWAA072571 1 20070521 A 3350 MS155721 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007052400072 20070524 00072 WP 2007 5 24 UPS07849826 1 20070411 A 5730 57583823 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C1 LEFT WING UPPER REAR SPAR SKIN CRACKED 5 INCHES AT STA XCW 69. REPAIRED LEFT WING UPPER AFT SPAR AT STA XCW 69.5 IAW SAA EA 008- 5710-01-A0835, UPS EO DC8-5730-26787-A, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007052400073 20070524 00073 WP 2007 5 24 UPS07849828 1 20070423 A 5330 57738635 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 FUSELAGE EXTERIOR SKIN GOUGED AT STA 140 L22L. REPAIRED FUSELAGE SKIN AT STA 140 L22L IAW SAA EA 008 -5330-01-A0849 UPS EO DC8-5330-26786-A, DOUGLAS DWG SRO8530027. 2 L 7 4 4F RT 4A25 2007052400086 20070524 00086 WP 2007 5 24 UPS07849831 1 20070423 A 5542 56550779 SKIN DOUG DC8 DC873F 302199F WP RUDDER CANNING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 LEFT RUDDER SKIN OIL CANNING AT STA ZR 185. REPAIRED LEFT RUDDER SKIN AT STA ZR 185 IAW SAA EA 008-2 720-01-A0856 DAC DWG 5655077 REV-S, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007052400087 20070524 00087 NM 2007 5 24 UPS07M49833 1 20070411 A 5330 SKIN DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C RIGHT HOR STAB - UNDER FAIRING 347DF AREA, SEVERAL AREAS OF CORROSION FOUND ON SKIN NEAR LWR FASTENER HOLES AT STA 2130 TO 2164. CORR ON SKIN REMOVED EXCEEDS LIMIT MATL THK 0.125", THK REMOVED 0.055" THK REMAINING 0.070 S RM 53-00-01 VI R38. DAMAGED SKIN TRIM SRM 53-20-00 FIG 12 VI R38. HFEC INSP C/ODAC NDTSPM R13 06-10-01.001 ON TRIM OFF AREA, NO CRACK EVIDENT. REPAIR DOUBLER & FILLER FAB USING MATL 7075-T6-0.100" & 0.063" SRM 53-20-00 VI R38 FIG 12. RE PAIR PARTS INSTALLED PER SRM 53-20-00 VI FIG 12 R39. 2 L 7 3 4F RT A22WE 2007052400091 20070524 00091 NM 2007 5 24 SWAA072562 1 20070521 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R AND 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052400094 20070524 00094 NM 2007 5 24 SWAA072565 1 20070521 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052400096 20070524 00096 NM 2007 5 24 SWAA072568 1 20070521 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052400174 20070524 00174 NM 2007 5 24 2007UALA01527 1 20070517 A 3250 MODULE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NLG STEERING MALFUNCTIONED A UALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 824UA 965 NW STEERING FAULT DISPLAYED ON UPPER ECAM SCREEN. WHEEL. [06-26-07] GROUND SCAN OF NR 1 BSCU INDICATED FAULTY STE ERING SERVO CONTROL MODULE. REPLACED 6GC STEERING SERVO CONTROL MODULE. ALSO REPLACED BSCU AS A PRECAUTION. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052400216 20070524 00216 NM 2007 5 24 USAA070408 1 20070523 A 5320 ATTACH ANGLE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 S16L JUST AFT OF BS 348.20 OUTSIDE LOWER STOP FITTING ATTACH ANGLE HAS CRACK. INSTALLED NEW ANGLE PER SRM 51-10-02, DEF ECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007052400221 20070524 00221 SO 2007 5 24 CHQA200700017 1 20070517 A 5610 163500109 WINDSHIELD EMB 145 EMB145MP 3260216 SO COCKPIT DELAMINATED A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 11 976RP 15945 15945 145322 FLIGHT 3079 - LGA-IND - ELECTRICAL SMELL REPORTED WHEN WINDOW HEAT SELECTED ON DURING DESCENT. MAINTENANCE FOUND WINDSHI ELD 1 WITH SLIGHT DELAMINATION AND DEFORMED AREA WHERE HEATING ELEMENT CONNECTS TO TERMINAL BLOCK. REMOVED AND REPLACED WINDSHIELD 1. 2 L 7 2 4F RT T00011AT 2007052400222 20070524 00222 NM 2007 5 24 DHL2007788525 1 20070517 A 5753 SKIN BOEING 727 727214 138407R NM TE FLAP GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 59731 21958 WHILE AT C CHECK AT FLIGHTSTAR, RT I/B FORE FLAP I/B UPPER SURFACE GOUGED. REMOVED DAMAGED AREA 5" DIA CLEANED AND PREP PED REPAIR AREA, FABRICATED FILLER 5" AND DOUBLER 8" FROM .016" 2024-T3 PO NR 9003189 ALODINED, PRIMED AND APPLIED ADHES IVE FILM IAW B727 SRM 51-40-20,51-40-24 FIG1 AND 57-50-2 FIG 3. CURED REPAIR AREA FINISHED AREA IAW B727 SRM 51-40-20 P AR 22. 2 L 7 3 4F A3WE 2007052400223 20070524 00223 NM 2007 5 24 USAA070403 1 20070523 A 5313 STRINGER SPLICE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 STRINGER SPLICE AT STA 907 STR 4R HAS CRACK. REPLACED WITH NEW STRINGER SPLICE PER SRM 52-10-02, 53-40-02, DEFECT SIZE: 0.5 INCH. 2 L 7 2 4F RT A16WE 2007052400224 20070524 00224 NM 2007 5 24 AWXA200700641 1 20070514 A 3350 21007 SWITCH BOEING 757 7572S7 1384962 NM EMERGENCY LIGHTS INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 904AW 23566 MCN - EEL - C-11 CHECK - EMERGENCY EXIT LIGHTS TEST SWITCH LOCATED AT LEFT AFT EMERGENCY EXIT DOOR IS INOPERATIVE. DOES NOT ACTUATE EXIT LIGHT OVER DOOR. REPLACED EMERGENCY EXIT LIGHTS TEST SWITCH PANEL IAW B757-200 AMM 33-51-01. 2 L 7 2 4F RT A2NM 2007052400226 20070524 00226 NM 2007 5 24 AWXA200700642 1 20070506 A 5320 D53472172205 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 832AW 1643 SAL - MAJOR REPAIR - BC-4 CHECK - CORROSION ON CABIN FLOORBEAM, FR 67 +4", -Y1192 TO -Y1292. REPLACED CABIN FLOORBEAM, FR 66 - FR 68, -Y1192 TO -Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007052400230 20070524 00230 WP 2007 5 24 ABXA070157 1 20070425 A 5210 995575043 STRAP DOUG DC9 DC932 3022066 WP MAIN ENTRY DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 985AX 47522 MAIN ENTRY DOOR INTERIOR FRAME STRAP CRACKED JUST AFT OF DOOR UPPER HINGE POINT AT APPROXIMATELY STA 170. REMOVED AND R EPLACED FRAME STRAP IAW DC9 SRM 51-30-2, 51-30-5, AND 51-30-1. 2 L 7 2 4F A6WE 2007052400231 20070524 00231 WP 2007 5 24 ABXA070159 1 20070426 A 5320 99579113 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 985AX 47522 DAMAGE TO INTERCOSTAL AT STA 351 TO 370 LONGERON 30. REMOVED AND REPLACED INTERCOSTAL IAW DC9 SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 2007052400265 20070524 00265 WP 2007 5 24 ABXA070154 1 20070423 A 5312 5910163255 BULKHEAD DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 905AX 47147 AFT PRESSURE BULKHEAD SKIN CRACKED AT 4:00 POSITION ADJACANT TO DOOR PIN ALIGNMENT RECEPTACLE. REPAIRED CRACK IN SKIN I AW DWG 5934886-502 AND REA D953-55733. 2 L 7 2 4F A6WE 2007052400266 20070524 00266 WP 2007 5 24 ABXA070158 1 20070516 A 5311 99115055 FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 FOUND CRACKED FRAME DURING WINDOW FRAME MOD EA 53300036, REF AD 2002-21-09. INSTALLED REPAIR IAW DC9 SRM 53-03 FIG 34. 2 L 7 2 4F A6WE 2007052400270 20070524 00270 NM 2007 5 24 CALA0700254 1 20070521 A 5313 6545800122 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND STRINGER 28R CORRODED AT STA 325. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-20-01 AND 51-70-13. 2 L 7 2 4F RT A16WE 2007052400274 20070524 00274 SO 2007 5 24 RAIA00705031 1 20070516 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 814HK 145046 PRE FLT NR - STL - EMERGENCY LIGHTS COCKPIT FLOOD LIGHT AND AISLE FLOOD LIGHT ARE INOP. MAINTENANCE REMOVED AND REPLACE D POWER SUPPLY UNIT, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007052400275 20070524 00275 SO 2007 5 24 RAIA00705032 1 20070516 A 3230 23092900001 UPLOCK EMB 145 EMB145 3260210 SO LT MLG MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 821HK 21007 145068 FLT NR 5473 - STL - LANDING GEAR LEVER DISAGREE WARNING AFTER TAKEOFF, LEFT MAIN WAS NOT RETRACTING. MAINTENANCE REMOVE D AND REPLACED LEFTHAND UP-LOCK BOX, LEAK AND OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007052400282 20070524 00282 SO 2007 5 24 RAIA00705039 1 20070520 A 2797 CONNECTOR EMB 145 EMB145LR 3260212 SO SPOILER SYS DIRTY A RAIA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CE 03 833HK 145240 FLT NR 8000 - IAD - SPOILER FAIL & INTERMITTENT UNCOMMANDED SPOILER DEPLOYMENT DURING TAXI. MAINTENANCE CLEANED CONNECT OR ON SPOILERS AND WHEEL SPEED TRANSDUCER, ALL CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007052400283 20070524 00283 EU 2007 5 24 200705212 1 20070519 A 3240 389075011 CONTROL VALVE EMB ERJ170 ERJ170100SE 3260406 EU EMERGENCY BRAKE FAILED A UHLA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 640RW 6507 17000058 FLIGHT 7568 ORD-RSW DIVERTED TO ATL DUE TO EMERGENCY BRAKE LIGHT ON IN COCKPIT. A/C LANDED WITH VISIBLE SMOKE COMING FR OM LANDING GEAR BUT NO FURTHER INCIDENT DURING ROLL OUT. TWO TIRES BLOWN ON LANDING. MAINTENANCE REMOVED AND REPLACED EMERGENCY BRAKE CONTROL VALVE. ALL MAIN TIRES WERE REPLACED. 2 L 7 2 4F RT A56NM 2007052400293 20070524 00293 EA 2007 5 24 COMA0760376 1 20070513 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 929CA 31723 7035 FLIGHT 5320 - CRACK ON RBL 9.0 O/B RADIUS OF VERTICAL STIFFENER AT FS 559.00. REPAIRED CRACK ON RBL 9.0 O/B RADIUS OF V ERTICAL STIFFENER IAW REO 601R-53-41-057. 2 L 7 2 4F RT A21EA 2007052400300 20070524 00300 SO 2007 5 24 200714322 1 20070522 A 5320 14521725001 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 FORWARD CABIN FLOOR SILL LEFT SIDE CORRODED. REMOVED AND REPLACED LEFT FORWARD CABIN SILL IAW EMB SRM. RETURNED AIRCRA FT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052400303 20070524 00303 SO 2007 5 24 200714314 1 20070522 A 5347 13500439005 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 LEFT OUTBOARD SEAT TRACK BETWEEN FRAMES 17 AND 23 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM. RETURNED AIRC RAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052500010 20070525 00010 SO 2007 5 25 200714317 1 20070522 A 5347 13500412001 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 RIGHT AFT INBOARD SEAT TRACK BETWEEN FRAMES 53 AND 57 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM AND ETN EM- 53-110R2. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052500027 20070525 00027 NM 2007 5 25 AALA20070919 1 20070417 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 915AN 29516 TUL - EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD CABIN. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007052500031 20070525 00031 NM 2007 5 25 AALA20070932 1 20070524 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 624AA 24582 MIA - EMERGENCY LIGHTS AT SEAT ROWS 16 TO 25 INOPERATIVE. REPLACED BATTERY PACK AND MODULE FOR EMERGENCY LIGHTS AT SEAT ROWS 16 TO 25. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007052500034 20070525 00034 WP 2007 5 25 AALA20070929 1 20070523 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70504 49798 LGA - EMERGENCY LIGHTS AT FIRST CLASS. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F A6WE 2007052500037 20070525 00037 NM 2007 5 25 AALA20070927 1 20070523 A 3350 0202226001 SHROUD BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 944AN 29535 LGA - EMERGENCY LIGHT AT SEAT 13D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007052500039 20070525 00039 NM 2007 5 25 AALA20070924 1 20070430 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 963AN 29543 TUL - EMERGENCY LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK M1673, STATION 952 FOR EMERGENCY LIGHTS AT AFT C ABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007052500052 20070525 00052 EA 2007 5 25 QXEA200700782 1 20070511 A 2760 5120011 PCU CNDAIR CL600 CL6002C10 1390015 EA SPOILERS MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 615QX 5734 10065 PSP - FLIGHT 2580, DURING FLIGHT CONTROL CHECK THE MASTER CAUTION CAME ON FOR THE OUTBOARD SPOILERS (SPOILERONS AND FLIG HT SPOILERS). RETURNED TO THE GATE. MAINTENANCE REPLACED THE PCU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERV ICE. 2 L 7 2 4F RT A21EA 2007052500056 20070525 00056 EA 2007 5 25 QXEA200700779 1 20070509 A 2612 22802675 ELEMENT CNDAIR CL600 CL6002C10 1390015 EA B FIRE LOOP MALFUNCTIONED A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 612QX 10042 PDX - FIRE SYSTEM FAULT MESSAGE DISPLAYED. MAINTENANCE FOUND THE UPPER DETECT LOOP B TO BE AT FAULT. REPLACED DETECTIO N LOOP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007052500060 20070525 00060 NM 2007 5 25 AALA20070902 1 20070521 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 JFK - SEAT MOUNTED EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGH T AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007052500064 20070525 00064 EU 2007 5 25 F3LA200700112 1 20070515 A 5315 D5347218820400 FLOORBEAM AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 802FR 4993 1991 DURING C-3 CHECK, INSPECTION REPORTED AFT LT LONGITUDINAL BEAM Y1292 HAD SURFACE CORROSION IN FASTENER HOLES AND ON TOP SURFACE. REPLACED CORRODED FLOORBEAMS (P/N D5347217220400 AND D5347218820400) AND COUPLING JUST FWD OF FR67 THRU FR 69 IAW A318 SRM 53-41-14, 51-44-21 AND 51-42-11. 2 L 7 2 4F RT 2007052500068 20070525 00068 WP 2007 5 25 AALA20070897 1 20070220 A 3350 0202226001 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7549A 53031 MSP - EMERGENCY AISLE LIGHT AT SEAT 17D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY AISLE LIGHT AT SEAT 17D. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007052500069 20070525 00069 WP 2007 5 25 AALA20070898 1 20070520 A 3350 OL1098BPEGPL BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7549A 53031 MSP - EMERGENCY AISLE LIGHT AT SEAT 17D HAS BROKEN BULB. RELAMPED EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F A6WE 2007052500071 20070525 00071 WP 2007 5 25 AALA20070896 1 20070520 A 3350 0201804001 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7549A 53031 MSP - EMERGENCY AISLE LIGHT AT SEAT 17D HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007052500076 20070525 00076 NM 2007 5 25 F3LA200700111 1 20070512 A 3230 664700500A4D CONTROL UNIT AIRBUS A319 A319111 3930336 NM MLG INOPERATIVE A F3LA O OTHER J WARNING INDICATION CR CRUISE 1 NM 03 946FR 2763 FLIGHT CREW REPORTED LGCIU 1 FAULT, HAD AMBER X INDICATIONS ON ECAM WHEEL PAGE WHERE THE GREEN TRIANGLE IS NORMALLY LOCA TED. THIS OCCURRED AT THE RT TRIANGLE LOCATION FOR ALL GEARS. FLIGHT CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INC IDENT. COMPLIED WITH TSM 32-31-00-810-809. REPLACED LGCIU 1 IAW AMM 32-31-71, PB 401. OPS CHECKED GOOD. 2 L 7 2 4F RT A28NM 2007052500077 20070525 00077 EU 2007 5 25 AALA20070899 1 20070520 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 50051 459 MIA - EMERGENCY LIGHT AT SEAT 31G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 31G. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A35EU 2007052500078 20070525 00078 NM 2007 5 25 AALA20070907 1 20070521 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 381AN 25450 SFO - EMERGENCY LIGHTS AT SEAT ROW 22H INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT ROW 22H. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A1NM 2007052500079 20070525 00079 NM 2007 5 25 AALA20070891 1 20070519 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 641AA 24599 SFO - SEAT MOUNTED EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK M10789 FOR SEAT MOUNTED EMERGENCY LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007052500083 20070525 00083 NM 2007 5 25 QXEA200700820 1 20070519 A 2930 54271158010 INDICATOR DHAV DHC8 DHC8202 2809007 NM HYD SYSTEM MALFUNCTIONED A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 374PH 3885 528 SEA FLIGHT NR 2026, NR 1 STANDBY HYDRAULIC FLUCTUATING BETWEEN 1 AND 2 THOUSAND PSI. BOTH NR 1 AND NR 2 STANDBY HYDRAUL IC INDICATIONS REMAINED AT 3000 PSI AFTER TURNING SWITCHES OFF. REPLACED DUAL HYDRAULIC PRESSURE INDICATOR FOR STANDBY PUMPS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007052900005 20070529 00005 NM 2007 5 29 2007UALA01580 1 20070518 A 3397 59191 JUMPER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 585UA 26709 FLOOR MOUNTED ESCAPE PATH LIGHTING INOP FROM ROW 9 TO 13. RECONNECTED JUMPER CABLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052900007 20070529 00007 NM 2007 5 29 2007UALA01582 1 20070518 A 3350 LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 769UA 26921 EXTERIOR EMERGENCY LIGHT AT DOOR 2R IS OUT. [SUP 06-06-07] RELAMPED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007052900010 20070529 00010 NE 2007 5 29 2007UALA01584 2 20070521 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LEFT UNKNOWN A UALA A UNSCHED LANDING C F.O.D. CL CLIMB 1 WP 29 455UA 1105 V10316 CREW REPORT: BIRD STRIKE LEFT ENGINE. EPR ROLLED BACK HALFWAY AND CAME BACK NORMAL. BIRD REMAINS IN ENGINE. [07-24-0 7] BIRDSTRIKE AFTER TAKE-OFF RESULTED IN RTF. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052900012 20070529 00012 NM 2007 5 29 2007UALA01587 1 20070519 A 5330 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSLEAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 845UA 1585 FUSELAGE SKIN HAS 6 INCH LONG GOUGE AT FRAME 28 BETWEEN STRINGER 39L & 40L. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052900016 20070529 00016 NM 2007 5 29 2007UALA01592 1 20070521 A 5321 PRESSURE PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 664 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 PRESSURE DECK CRACKED AT STA 664, LBL 30 WL 204 JUST OUTBOARD OF AILERON TOWER SHAFT INPUT. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007052900018 20070529 00018 2007 5 29 2007UALA01594 4 20070521 A 2565 GAUGE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE L2 DOOR SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 664UA 29236 DOOR 2L SLIDE-RAFT BOTTLE PRESSURE IS REPORTED TO BE AT BOTTOM OF GREEN BAND. [06-15-07] THE GAUGE WAS LEAKING OUT OF THE CENTER SHAFT. REMOVED & REPLACED GAUGE. PERFORMED SECURITY CHECK PER MM & AIRCRAFT OK FOR SERVICE. SLIDE PROBLE M ROOT CAUSE WAS WEAR ON SHAFT & SEAL OF GAUGE CENTER SHAFT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007052900024 20070529 00024 NM 2007 5 29 2007UALA01604 1 20070522 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 SEAT 39 HJK EMERGENCY LIGHT LAMP INOPERATIVE. [SUP 06-06-07] RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052900027 20070529 00027 NM 2007 5 29 2007UALA01607 1 20070522 A 3350 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 RIGHT 2 AFT OVERWING EMERGENCY LIGHTS FUSE INOP. [SUP 06-06-07] REPLACED FUSE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052900031 20070529 00031 NM 2007 5 29 2007UALA01611 1 20070523 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EEL LAMP 3J AFT INOPERATIVE. [SUP 06-06-07] RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052900033 20070529 00033 NM 2007 5 29 2007UALA01614 1 20070523 A 3350 20131A BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 566UA 26670 THE FOLLOWING EMERGENCY LIGHTS ARE INOP: SLIDE LIGHT DOOR 2L, EXTERIOR AFT OF WING RIGHT SIDE, EEL LIGHTS ROWS 23-30, E XIT SIGN ROW 29, AISLE LIGHTS ROWS 19, 21 & 23. AFT HATCH HANDLE LIGHT AT ROW 16. REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052900040 20070529 00040 NM 2007 5 29 2007UALA01621 1 20070523 A 2730 PULLEY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ELEVATOR CONTROL CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 CRACKED PULLEY, ELEV CONTROL CABLE ROUTING AT STA 343, FWD CABIN, LEFT UPPER. [06-20-07] INSTALLED NEW PULLEY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052900044 20070529 00044 2007 5 29 2007UALA01625 4 20070523 A 3425 RELAY BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EFIS MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 930UA 26655 RTFL DUE TO ALL 4 EFIS SCREENS BLINKING. REMOVED AND CLEANED EFIS FILTER, FANS AND CHECK VALVES . DISCONNECTED DUCTS TO FORWARD OF FLOW SENSOR TO CHECK FOR OBSTRUCTIONS, ALL OK. REPLACED CONTROL RELAY R401, OPERATES NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007052900056 20070529 00056 SO 2007 5 29 C2XA07SH030 1 20070523 A 5310 14525480003 DOOR FRAME EMB 145 EMB145LR 3260212 SO CARGO DOORWAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13988 145265 SHV - DURING C-CHECK CARGO DOOR CUTOUT LOWER FRAME HAS CORROSION. MX REMOVED AND REPLACED LOWER FRAME OF CARGO DOOR IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007052900061 20070529 00061 NM 2007 5 29 PIDA07035 1 20070519 A 5315 FLOORBEAM BOEING 737 7372K5 138448X NM BS 986 CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 DURING MAINTENANCE, NOTED CORROSION ON UPPER FLANGE OF BS 986.5 FLOORBEAM. REPLACED DAMAGED SECTION OF FLOORBEAM PER EA 53-115. 2 L 7 2 4F RT A16WE 2007052900071 20070529 00071 NM 2007 5 29 SWAA072577 1 20070522 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 249WN 34951 EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007052900072 20070529 00072 NM 2007 5 29 SWAA072574 1 20070522 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 633SW 27936 BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 6 DEF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007052900073 20070529 00073 NM 2007 5 29 SWAA072578 1 20070522 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 484WN 33841 EEPLS COVER MISSING AT ROW 2 DEF. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007052900077 20070529 00077 NM 2007 5 29 SWAA072594 1 20070522 A 2730 6545166 PUSHROD BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, LEFT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR PUSHROD PER MM. 2 L 7 2 4F RT A16WE 2007052900084 20070529 00084 NM 2007 5 29 SWAA072583 1 20070522 A 5755 HINGE FITTING BOEING 737 7373H4 1384600 NM NR 4 SPOILER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C1 CHECK, FOUND LEFT WING NR 4 GROUND SPOILER OUTBOARD HINGE FITTING BROKEN. REMOVED AND REPLACED SPOI LER PER MM. 2 L 7 2 4F RT A16WE 2007052900085 20070529 00085 NM 2007 5 29 SWAA072592 1 20070522 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 867 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052900090 20070529 00090 NM 2007 5 29 SWAA072607 1 20070522 A 5311 6546540 FRAME BOEING 737 7373Q8 1384670 NM BS 639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT LEFT BS 639, WL 208. REMOVED AND REPLACED CHORD PER S RM. 2 L 7 2 4F RT A16WE 2007052900096 20070529 00096 NM 2007 5 29 SWAA072599 1 20070522 A 5313 6551698 STRINGER SPLICE BOEING 737 7373L9 1384470 NM BS 360 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007052900116 20070529 00116 NM 2007 5 29 SWAA072579 1 20070522 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 734SA 27866 DURING SCHEDULED MV2 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007052900117 20070529 00117 NM 2007 5 29 SWAA072575 1 20070522 A 3350 MS155721 LAMP BOEING 737 7375H4 138449D NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007052900125 20070529 00125 NM 2007 5 29 SWAA072624 1 20070523 A 3350 20121 CHARGER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 RIGHT AFT CABIN EMERGENCY EXIT LIGHT STAYS WITH NO POWER. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007052900137 20070529 00137 EU 2007 5 29 YENA2007037 1 20070520 A 2750 FLAP SYSTEM EMB ERJ190 ERJ190100IGW 3260408 EU TE FLAPS MALFUNCTIONED A YENA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 15 236JB 19000035 FLT 908, ORD-JFK FLAP FAIL ON APPROACH. REF FIM 27-51-00-810-802. ACCOMPLISHED ACE NR 1 & 2. RESET CYCLED FLAPS SEVER AL TIMES. NO DEFECTS NOTED ACTIVE FAULT CODE 2-81-00-810-805-A00. 2 L 7 2 4F RT A57NM 2007052900139 20070529 00139 NM 2007 5 29 MWEA070118 1 20070519 A 2530 253001275 OVEN BOEING 717 717200 1383700 NM GALLEY SMOKE A MWEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 13 917ME 55179 OVEN ON AIRCRAFT LEFT, SMOKES WHEN TURNED ON. CLEANED OVEN. 2 L 7 2 4F TR A6WE 2007052900145 20070529 00145 NM 2007 5 29 SWAA072664 1 20070524 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052900148 20070529 00148 NM 2007 5 29 SWAA072666 1 20070524 A 5340 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 767 S27L-R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27L AND STR 27R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007052900155 20070529 00155 NM 2007 5 29 ASAA0741640 1 20070517 A 5313 65C3674539 STRINGER BOEING 737 7374Q8 138447Q NM BS 310-328 CRACKED A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 756AS 25097 AIR START UNIT CONTACTED RIGHT SIDE OF AIRCRAFT BELOW DOOR R1. REPAIRED PER EA 5330 02206. NOTE ADDITIONAL P/N 65C3674 5 23. 2 L 7 2 4F RT A16WE 2007052900157 20070529 00157 NM 2007 5 29 SWAA072668 1 20070524 A 5340 65C27314 STRINGER CLIP BOEING 737 7377H4 1384404 NM BS 420 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 728SW 27860 DURING SCHEDULED 8Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052900160 20070529 00160 NM 2007 5 29 SWAA072634 1 20070523 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500B S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052900178 20070529 00178 NM 2007 5 29 ASAA0741694 1 20070523 A 5350 693575019 STRINGER CLIP BOEING 737 737490 1384715 NM BS 787 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 706AS 28894 AFT CARGO PIT CLIP CORRODED. REPLACED WITH MADE REPAIR PART IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007052900179 20070529 00179 NM 2007 5 29 ASAA0741695 1 20070523 A 5753 65C35703 SKIN BOEING 737 737490 1384715 NM RWS 245 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 706AS 28894 RIGHT WING O/B FORE FLAP DENTED ON UPPER SURFACE. DENT REPAIRED IAW SRM 51-70-10 REPAIR 4. 2 L 7 2 4F RT A16WE 2007052900193 20070529 00193 EA 2007 5 29 TRAX200700710 1 20070522 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 333 S27 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 851AS 7360 FRAME AT FS 333 AT STGR 27 CORRODED. WORK COMPLETED IN ACCORDANCE WITH CRJ 200 SRM 51-21-06, CRJ 200 NDTM 51-20-04. CRJ 200 SRM CRJ 200 51-00-00 APPLIED CIC IAW CRJ 200 SRM 51-21-11. 2 L 7 2 4F RT A21EA 2007053000014 20070530 00014 NM 2007 5 30 TAMF20070002O 1 20070517 A 7997 CONNECTOR BOEING 767 767200 1385120 NM GE CF6 CF680C GL OIL TEMP DAMAGED W TAMF E C ENGINE SHUTDOWN ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 23 770QT 23802 690164 R ENG OIL TEMP HIGH DURING TAKEOFF ROLL. ENGINE WAS SHUTDOWN AND T/O REJECTED. FRM 7902XB02. FIM 31-41-00 WAS PERFORMED AND R ENG OIL TEMP CONNECTOR, D11062 PIN NR 3 WAS FOUND LOOSE. PIN WAS REPLACED IAW WDM 79-34-11 WITH SATISFACTORY RESU LT, NO EICAS MESSAGES DISPLAYED. BRAKE TEMP WAS INSPECTED AND IT WAS FOUND BELOW 4. NO MAINTENANCE ACTIONS WERE REQUIR ED FOR TAKEOFF REJECTION IAW AMM 05-51-14 PAGE 201.THE AIRPLANE RETURNED TO NORMAL OPERATIONS. 2 L 7 2 4F 4 F RT A1NM E23EA 2007052400028 20070524 00028 NM 2007 5 24 QXEA200700804 1 20070513 A 5310 DOOR FRAME BOMBDR DHC8 DHC8402 1390042 NM MAIN PAX CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - FORWARD MAIN CABIN DOOR FRAME IS CHAFED BY A FLOOR PANEL AT STATION X1.0. REPAIRED IAW SRM 51-14-00 AND RD8/4- 53-1912. 2 H 7 2 4T RT A13NM 2007052400029 20070524 00029 NM 2007 5 24 ASAA0791648 1 20070521 A 5321 453A161015 FLOOR PANEL BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 FWD CARGO FLOOR PANEL NR 2 CORRODED. 2 L 7 4 4F RT A16WE 2007052400034 20070524 00034 NM 2007 5 24 QXEA200700806 1 20070513 A 5753 FLAP TRACK BOMBDR DHC8 DHC8402 1390042 NM RWS 281 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - RIGHT WING FLAP TRACK NR 4 AT YW 281.019 HAS TUNGSTEN CARBIDE COATING MISSING INBOARD SURFACE 23" AFT OF REAR S PAR. REPAIRED IAW RD8/4-57-792. 2 H 7 2 4T RT A13NM 2007052400035 20070524 00035 EA 2007 5 24 TRAX200700681 1 20070517 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 843AS 7310 EMERGENCY EXIT SIGN IN CENTER CABIN ROOF, FACING FWD, INOP. 2 L 7 2 4F RT A21EA 2007052400036 20070524 00036 EA 2007 5 24 TRAX200700682 1 20070518 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 860AS 7433 AFT FLOOR LEVEL EMERGENCY LIGHTS INOP. 2 L 7 2 4F RT A21EA 2007052400059 20070524 00059 EA 2007 5 24 TRAX200700675 1 20070515 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 836AS 7263 INTERCOSTAL CRACKED AT FS 484, LBL 27 OUTBOARD. 2 L 7 2 4F RT A21EA 2007052400061 20070524 00061 EA 2007 5 24 TRAX200700676 1 20070515 A 5210 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 919EV 7780 PAX DOOR CRACKED INSIDE ACCESS PANEL 832AR (UPPER FWD FRAME SUPPORT DOUBLER P/N:601R318094-2). OK FOR 600 FLIGHT HRS WITH A RE-INSPECTION AT EVERY 200 FLT HRS TO ENSURE CRACK LENGTH DOES NOT INCREASE. REFERENCE REO: 601R-52-11-1247. 10-18-07 REMOVED AND REPLACED UPPER FWD FRAME SUPPORT DOUBLER IAW CRJ SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007052400068 20070524 00068 NM 2007 5 24 SWAA072544 1 20070521 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 437WN 29832 DURING SCHEDULED HC2 CHECK, MID CABIN EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007052400079 20070524 00079 NM 2007 5 24 UPS07549841 1 20070427 A 5311 146N102847 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 404UP 23726 INSPECTION TYPE:C DENTS IN AFT CARGO FUSELAGE FRAME STA 1280 BETWEEN S25L AND S26L (2EA). UPPER DENT REPAIR AT STA 1280 , WAS ACCOMPLISHED PER FINAL EA 757-5362-27-A1665 AND UPS EO B757-5310-26833-A WITH NO DEVIATIONS. THE LOWER DENT AT ST A 1280, WAS REPAIRED PER FINAL EA 757-5362-27- A1665 AND UPS EO B757-5310-26833-A WITH NO DEVIATIONS. 2 L 7 2 4F RT A2NM 2007052400081 20070524 00081 WP 2007 5 24 UPS07849836 1 20070514 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C2 FLOORBEAM STA 1300 RBL 12 HAS EXFOLIATION CORROSION BETWEEN FLOORBEAM AND FLOORBOARD. REMOVED CORROS ION, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER. IAW SRM 51-1-8, 53-7-3 FIG 10, 51-2-1 FIG 1 SHT 7, TR 51-130 NOTE 19. 2 L 7 4 4F RT 4A25 2007052400083 20070524 00083 2007 5 24 UPS07M49843 4 20070522 A 2211 4059001908 COMPUTER DOUG MD11 MD11F 3023600 NM AUTOPILOT SYS FAILED A IPXA K NONE I FLT. ATTITUDE INST. CL CLIMB 1 SO 01 278UP 48577 INSPECTION TYPE:N/A ATB - FLAP INDICATOR RIGHT SIDE SHOWED FLAPS 14/X WITH FLAP HANDLE UP CYCLED FLAPS TWICE IN FLIGHT. LSAS FAILED MOMENTARILY AFTER AUTO PILOT DISCONNECT. T/S PER AMM 22-00-00 & 27-54-00 FOUND NR 1 FCC FAIL, REPLACED NR 1 FCC & CFDS FCC, AFS R-T-S TESTED NO FAILURE SHOWS AS PER MM 22-01-10, SYSTEM OK FOR SVC. 2 L 7 3 4F RT A22WE 2007052400084 20070524 00084 NM 2007 5 24 UPS07M49845 1 20070521 A 3350 BATTERY PACK DOUG MD11 MD11F 3023600 NM COCKPIT DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP 48576 INSPECTION TYPE:N/A LEVEL 1 ALERT EMERGENCY LIGHT BATTERY 1 LOW ALERT ON PREFLIGHT. PERFORMED R-T-S MSC PER FIM 33-51-0 0-1. OPS NORMAL. 2 L 7 3 4F RT A22WE 2007052400092 20070524 00092 NM 2007 5 24 SWAA072554 1 20070521 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052400098 20070524 00098 NM 2007 5 24 SWAA072563 1 20070521 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052400107 20070524 00107 NM 2007 5 24 SWAA072548 1 20070521 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052400109 20070524 00109 EU 2007 5 24 07FDEA01812 1 20070515 A 5315 A53773651212 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 TOP CAP BEAM C38.2 CORRODED REPAIR PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 2007052400110 20070524 00110 EU 2007 5 24 F3LA200700109 1 20070515 A 5310 SHEAR PLATE AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 802FR 4993 1991 DURING C-3 CHECK, INSPECTION REPORTED AFT RT SHEAR PLATE HAD SMALL AMOUNT OF CORROSION BETWEEN FR 69 AND FR 70. REPLACE D AFT RT SHEAR PLATE IAW SRM 51-42-11 AND 51-72-11. 2 L 7 2 4F RT 2007052400111 20070524 00111 EU 2007 5 24 TRBA200724 1 20070515 A 3350 3011210 LIGHT AEROSP ATR72 ATR72212 8680945 EU CABIN FAILED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 348AE 349 MAIN PAX DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AS PER JIC #33-51-24. OPERATI ONAL CHECK GOOD. 2 H 7 2 4T RT A53EU 2007052400112 20070524 00112 EU 2007 5 24 TRBA2007023 1 20070515 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT FAILED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 407AT 407 EMERGENCY PAX DOOR STAIR LIGHT INOPERATIVE. REPLACED BATTERY PACK AS PER JIC NR 33-51-21. OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A53EU 2007052400113 20070524 00113 WP 2007 5 24 IXXA07SMN135S 1 20070421 A 5330 SKIN DOUG DC8 DC871F 302199D WP ZONE 100 MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT AFT FUSELAGE SKIN PANEL AND SKIN SPLICES OF LONGERON 28 LEFT AT STATION 1690. REMOVED EXISTING EXTERNAL REPAIR DOUBLER. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. F ABRICATED NEW SKIN, EXTERNAL DOUBLER, AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW FAA FORM 8100-9 DATED 04-23-07, MESSAGE BOEING NUMBER 1-3174229 75-5 DATED 04-23-07, AIRWORTHINESS DIRECTIVE 2007-02-02, SERVICE BULLETIN DACO DC8-53A80, DOUGLAS DRAWING SR08530032, SE MAN DRAWING NUMBER ED-4519 DATED 04-17-07, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51- 2 L 7 4 4F RT 4A25 2007052400115 20070524 00115 NM 2007 5 24 TSAA0777025 1 20070516 A 7711 LG4C14 TRANSDUCER BOEING 737 737210C 1384459 NM NR 2 ENGINE FAILED A TSAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 13 834AL 20917 NON-ETOPS CARGO FLIGHT 909 HNL-LIH. ON TAKEOFF ROLL, CREW NOTED THE NR 2 EPR WAS LOW. CREW ABORTED TAKEOFF AT 60 KTS A ND RETURNED TO THE FREIGHT RAMP WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 EPR TRANSDUCER PER MM 77-10 AND OPERATION CHECK NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A16WE 2007052400118 20070524 00118 NM 2007 5 24 QXEA200700809 1 20070511 A 5540 LINK BOMBDR DHC8 DHC8402 1390042 NM RUDDER CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - TRAILING RUDDER UPPER LINK MOUNTING ARM IS CHAFED IN TWO PLACES. REPAIRED IAW RD8/4-55-334. 2 H 7 2 4T RT A13NM 2007052400119 20070524 00119 WP 2007 5 24 IXXA070029S 1 20070421 A 5330 SKIN DOUG DC8 DC871F 302199D WP ZONE 100 MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT AFT FUSELAGE SKIN PANEL AND SKIN SPLICES OF LONGERON 28 RIGH T AT STATION 1690. REMOVED EXISTING EXTERNAL REPAIR DOUBLER. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN, EXTERNAL DOUBLER, AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIE D SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW FAA FORM 8100-9 DATED 04-23-07, MESSAGE BOEING NUMBER 1-3174229 75-5 DATED 04-23-07, AIRWORTHINESS DIRECTIVE 2007-02-02, SERVICE BULLETIN DACO DC8-53A80, DOUGLAS DRAWING SR08530032, SE MAN DRAWING NUMBER ED-4519 DATED 04-17-07, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51- 2 L 7 4 4F RT 4A25 2007052400120 20070524 00120 NM 2007 5 24 QXEA200700810 1 20070511 A 5540 STRUCTURE BOMBDR DHC8 DHC8402 1390042 NM RUDDER CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - FORE RUDDER UPPER ACTUATOR ATTACH POINT IS CHAFED. REPAIRED IAW RD8/4-55-333. 2 H 7 2 4T RT A13NM 2007052400121 20070524 00121 NM 2007 5 24 QXEA200700812 1 20070511 A 5530 HINGE BRACKET BOMBDR DHC8 DHC8402 1390042 NM VERTICAL STAB CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - UPPER HINGE BRACKET ON VERTICAL STAB HAS A CHAFED AREA WHERE FORE RUDDER ATTACHES. REPAIRED IAW RD8-4-55-331/3 . 2 H 7 2 4T RT A13NM 2007052400122 20070524 00122 NM 2007 5 24 QXEA200700811 1 20070512 A 5530 HINGE BRACKET BOMBDR DHC8 DHC8402 1390042 NM VERTICAL STAB CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - LOWER HINGE BRACKET ON VERTICAL STAB HAS A CHAFED AREA WHERE THE FORE RUDDER LINK ATTACHES. REPAIRED IAW RD8/4 -55-335 AND SRM 51-14-01, 51-26-10. 2 H 7 2 4T RT A13NM 2007052400123 20070524 00123 NM 2007 5 24 QXEA200700813 1 20070510 A 5311 FRAME BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - EXTRUDED FRAME MEMBER CONNECTED TO MAIN CABIN DOOR THRESHOLD AT STATION X24.8 HAS CORROSION AROUND BOLT HOLE TO P. REPAIRED IAW SRM 51-42-05, 51-25-10,A ND 51-20-10. 2 H 7 2 4T RT A13NM 2007052400124 20070524 00124 NM 2007 5 24 QXEA200700815 1 20070513 A 5511 SPAR BOMBDR DHC8 DHC8402 1390042 NM HORIZONTAL STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - HORIZONTAL STAB LEADING EDGE SPAR WEB HAS 11 LOOSE CHERRY RIVETS AT STATION LEFT HAND YH 15, CENTER OF WEB. RE PAIRED IAW 51-42-45. 2 H 7 2 4T RT A13NM 2007052400125 20070524 00125 NM 2007 5 24 QXEA200700816 1 20070515 A 5511 SPAR BOMBDR DHC8 DHC8402 1390042 NM HORIZONTAL STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - HORIZONTAL STAB LEADING EDGE SPAR WEB HAS 9 LOOSE CHERRY RIVETS AT STATION RIGHT UH 15, CENTER WEB. REPAIRED I AW SRM 51-42-45. 2 H 7 2 4T RT A13NM 2007052400126 20070524 00126 NM 2007 5 24 SWAA072573 1 20070521 A 3350 MS155721 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007052400127 20070524 00127 NM 2007 5 24 AALA20070869 1 20070516 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 795AN 30257 DFW - CEILING EMERGENCY LIGHT AT SEAT 39C HAS MISSING LENS. REPLACED LENS FOR CEILING EMERGENCY LIGHT AT SEAT 39C. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007052400129 20070524 00129 WP 2007 5 24 AALA20070871 1 20070517 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 455AA 49560 BOS - EMERGENCY LIGHT AT SEAT 28D MISSING RED LENS. REPLACED RED LENS FOR EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007052400130 20070524 00130 EU 2007 5 24 AALA20070876 1 20070517 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14061 471 MIA - EMERGENCY LIGHTS AT SEAT ROWS 19G TO 28G INOPERATIVE. REPLACED BATTERY PACK AT NUMBER THREE DOOR FOR EMERGENCY LI GHTS AT SEAT ROWS 19G TO 28G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007052400131 20070524 00131 WP 2007 5 24 AALA20070882 1 20070518 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 598AA 53288 LAX - EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5103 FOR EMERGENCY LIGHTS IN AFT CABIN. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007052400132 20070524 00132 EU 2007 5 24 AALA20070874 1 20070517 A 3260 SENSOR AIRBUS 300 A300B4605R 3930308 EU NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 77080 626 MIA INFLIGHT T937/17MAY - DURING CLIMB CREW WAS UNABLE TO RETRACT LANDING GEAR WITH POSITION DETECTOR SYSTEM NUMBER TWO , HAD OTHER SYSTEM FAILURES. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR SENSOR. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007052400133 20070524 00133 EU 2007 5 24 AALA20070861 1 20070515 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70079 619 MIA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 12G INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 12G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007052400134 20070524 00134 EU 2007 5 24 AALA20070862 1 20070515 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70054 461 MIA - EMERGENCY LIGHT AT SEAT 13G INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 13G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007052400135 20070524 00135 NM 2007 5 24 AALA20070879 1 20070518 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 MIA - EMERGENCY LIGHT AT SEAT 40G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 40G. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT T00001SE 2007052400136 20070524 00136 NM 2007 5 24 AALA20070881 1 20070518 A 2400 B4301 CONTROL UNIT BOEING 767 767323 1385205 NM EE BAY INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 353AA 24034 SJU INFLIGHT T1416/18MAY - DURING CLIMB, CREW REPORTED LOSS OF LEFT AC BUSS AND LEFT GENERATOR. RETURNED TO SJU AND LAN DED WITHOUT INCIDENT. REPLACED LEFT BUSS TIE BREAKER AND GENERATOR CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATIO N. 2 L 7 2 4F RT A1NM 2007052400137 20070524 00137 NM 2007 5 24 AALA20070867 1 20070516 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971AN 29547 LAX - EMERGENCY LIGHT AT SEAT 17D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A16WE 2007052400138 20070524 00138 NM 2007 5 24 AALA20070868 1 20070516 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971AN 29547 LAX - EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A16WE 2007052400139 20070524 00139 NM 2007 5 24 AALA20070870 1 20070516 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 795AN 30257 LAX - EMERGENCY LIGHT AT SEAT 31G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 31G. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT T00001SE 2007052400140 20070524 00140 WP 2007 5 24 AALA20070872 1 20070517 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 455AA 49560 LAX - EMERGENCY LIGHT AT SEAT 28D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007060800134 20070608 00134 WP 2007 6 8 WRLA2007071 1 20070523 A 5310 DOOR FRAME DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE OVERWING DOOR CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 14075 46922 DURING B-CHECK INSPECTION, RIGHT HAND OVERWING DOOR R-3, AFT LOWER CORNER (AT FLOOR LEVEL) STA 1305 EVIDENCE OF CORROSIO N UNDER DOOR SILL PLATE. [08-07-07] SILL PLATE SUPPORT CHANNEL FOUND CORRODED BEYOND LIMITS. REMOVED CHANNEL, FABRICA TED NEW SUPPORT CHANNEL FROM 7075-T651, AND INSTALLED IN ACCORDANCE WITH DC-10 SRM VOL.2 51-31-01. 2 L 7 3 4F 4 F A22WE E23EA 2007052400173 20070524 00173 EU 2007 5 24 2007UALA01526 1 20070517 A 5330 BUTT JOINT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 417UA 483 REINSTALLED DOUBLER REPAIR AFTER AFT SKIN REPLACEMENT. DOUBLER LOCATED AT FR 70 BUTT JOINT STR 34. MAJOR REPAIR ACCOMP LISHED: INSTALLED NEW DOUBLER AT BUTT JOINT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052400193 20070524 00193 EU 2007 5 24 USAA070389 1 20070521 A 5347 D5347219320000 SEAT TRACK AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 179UW 1521 FRAME 23, RIGHT OUTBOARD SEAT TRACK -Y760 HAS CORROSION. SPLICED IN NEW SECTION IAW SRM 53-00-15 FIG 201, DEFECT SIZE: 1 INCH DIA. 2 L 7 2 4F RT A28NM 2007052400195 20070524 00195 NM 2007 5 24 QXEA200700827 1 20070519 A 2760 WARNING MESSAGE BOMBDR DHC8 DHC8402 1390042 NM SPOILERS FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 425QX 4039 SEA FLIGHT NR 2275: SPOILER OUTBOARD CAUTION, ROLL SPOILER INBOARD AND OUTBOARD HYD CAUTION LIGHTS ON AFTER START. AIRC RAFT RETURNED TO GATE. MAINTENANCE FOUND ROLL SPOILER SENSOR TRIPPED. RESET ROLL SPOILER CABLE SENSOR IAW Q400 AMM TAS K 27-61-00-710-805 STEP 6 THRU END. CAUTION LIGHTS DID EXTINGUISH AND DID NOT RETURN. PERFORMED OPS TEST OF ROLL SPOIL ER SYSTEM IAW Q400 AMM TASK 27-61-00-710-801. OPS CHECK GOOD WITH NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRA FT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007052400196 20070524 00196 EU 2007 5 24 CPCP20070030 1 20070425 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 448AM 448 RIGHT SEAT TRACK BETWEEN FRAME 36-39 CORRODED. REPLACED RIGHT SEAT TRACK AS PER SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007052400210 20070524 00210 NM 2007 5 24 USAA070401 1 20070523 A 5320 ATTACH ANGLE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 JUST BELOW S13L AFT SIDE OF BS 360, TOP END OF SKIN TO FRAME ATTACH ANGLE HAS CRACK. INSTALLED NEW ANGLE PER SRM 51-10- 02, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007052400215 20070524 00215 NM 2007 5 24 USAA070409 1 20070523 A 5312 PRESSURE PANEL BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 BS 664 LBL 32, BEADED PRESSURE DECK HAS CRACK. INSTALLED REPAIR DOUBLER PER TR 53-60-04, DEFECT SIZE: .75 INCH. 2 L 7 2 4F RT A16WE 2007052400228 20070524 00228 WP 2007 5 24 ABXA070155 1 20070423 A 5320 991015113 CUSP WEB DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 905AX 47147 CUSP WEB CRACKED AT STA 598 TO 617 AT BUTT LINE 58 LEFT. REPAIRED AREA OF WEB IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 2007052400276 20070524 00276 SO 2007 5 24 RAIA00705033 1 20070516 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 818HK 145059 PRE FLT NR 5502 - STL - AFT FLOOR PROXIMITY LIGHT IS INOP. MAINTENANCE RECONNECTED LOOSE WIRES, SYSTEM CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007052400279 20070524 00279 SO 2007 5 24 RAIA00705036 1 20070518 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN DAMAGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 819HK 145062 PRE FLT NR 5497 - STL - FLOOR STRIP EMERGENCY LIGHT FLOOR PROXIMITY LIGHT IS INOP. MAINTENANCE REPAIRED WIRES AT STRIP LIGHT, SYSTEM CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007052400285 20070524 00285 EU 2007 5 24 200700025 1 20070512 A 5540 A55470010002D RUDDER AIRBUS 300 A300B4203 3930306 EU DELAMINATED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 501TR 53 DURING WALK AROUND POSSIBLE DELAMINATION NOTED ON TRAILING EDGE OF RUDDER. RUDDER REMOVED, REPAIRED IAW SRM 55-41-11 PG 148-149, SRM 51-21-00 PG 15, 21, 22 SRM 51-40-00 PG 731-733 FIG 709, SRM 55-41-11 PG 148, 149 SRM 51-42-20 AND PCS PROC ESS PROCEDURES PCS-PS0001, SRM 51-41-50. PRIMED AND PAINTED IAW SRM 51-40-12. RUDDER RETURNED SERVICEABLE TO BE RE-INS TALLED ON AIRCRAFT. 2 L 7 2 4F RT A35EU 2007052400292 20070524 00292 NM 2007 5 24 CALA0700258 1 20070508 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AROUND L-2 DOOR LOWER HINGE CUTOUT. THE SKIN WAS REPAIRED IAW SRM 53 -60-01. 2 L 7 2 4F RT A16WE 2007052400298 20070524 00298 SO 2007 5 24 200714315 1 20070522 A 5347 13500439011 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 24 AND 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM AND ETN 53-110R2 . 2 L 7 2 4F RT T00011AT 2007052400301 20070524 00301 SO 2007 5 24 200714312 1 20070522 A 5347 13500438001 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 24 AND 36 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM. RETURNED AIRC RAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052500001 20070525 00001 EA 2007 5 25 QXEA200700833 1 20070523 A 5297 WIRE HARNESS CNDAIR CL600 CL6002C10 1390015 EA CARGO DOOR MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 616QX 10128 DEN - FLIGHT 4277, RECEIVED A PROXI FAULT SYSTEM 2 MESSAGE FOR THE FORWARD CARGO DOOR. RETURNED TO THE GATE, AND MAINTE NANCE PLACED THE SYSTEM ON MEL 52-70-4A. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007052500007 20070525 00007 SO 2007 5 25 200714318 1 20070522 A 5347 13500438003 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 RIGHT OUTBOARD SEAT TRACK BETWEEN FRAMES 24 AND 36 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM. RETURNED AIR CRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052500012 20070525 00012 SO 2007 5 25 200714302 1 20070520 A 5315 14521700001 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 935AE 14500920 LEFT OMEGA BEAM CORRODED ON INBOARD SIDE OF FRAME 20. REPAIRED DAMAGE IAW EMB SRM. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007052500013 20070525 00013 EA 2007 5 25 200714304 1 20070506 A 5315 CC670341757 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 522AE 7696 3878 10147 AT STATION 280 FLOORBEAM FOUND CORROSION ALONG TOP FLANGE FROM BL 24L TO BL 42R. SPLICED IN FRAME 280 AND EXTENSION MOU NTS IAW AEA EO CR 53MR 119. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007052500023 20070525 00023 SO 2007 5 25 SWIA200718232 1 20070513 A 2422 PC2511C INVERTER EMB 120 EMB120ER 3260203 SO NR 1 STATIC MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 584SW 13632 13632 120352 BOTH CAPTAIN AND FIRST OFFICER RECEIVED YELLOW HEADING FLAGS. THEN RED HEADING FLAG. BOTH EHSI'S WERE BETWEEN 50-70 DE GREES OFF OF COMPASS. RETURNED TO SLC, REPLACED NR 1 STATIC INVERTER IAW MM 24-20-01. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007052500025 20070525 00025 NM 2007 5 25 AALA20070920 1 20070417 A 3350 8200037702 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 915AN 29516 TUL - EMERGENCY LIGHT AT LEFT OVERWING EXIT STATION 628 HAS CRACKED LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LEFT OVE RWING EXIT STATION 628. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007052500049 20070525 00049 NM 2007 5 25 QXEA200700832 1 20070523 A 2420 31708001A GENERATOR DHAV DHC8 DHC8202 2809007 NM AC SYSTEM MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 364PH 307 524 SEA FLIGHT NR 2104, AFTER PUSHBACK AC GENERATOR CAUTION LIGHT ILLUMINATED. RAN CHECKLIST. STILL LOAD 0 BUT SHOWED OUTP UT ON PANEL OF 113 VOLTS. REPLACED NR 2 AC VARIABLE FREQUENCY GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007052500050 20070525 00050 EA 2007 5 25 QXEA200700721 1 20070504 A 4910 21195844 ECU CNDAIR CL600 CL6002C10 1390015 EA MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 603QX 13136 10011 YEG - FLIGHT 2515 - AFTER ENGINE START AND PUSHBACK APU DOOR DISPLAYS 4 AMBER DASHES AND ECU FAIL MESSAGE RECEIVED. RET URNED TO THE GATE. MAINTENANCE REPLACED THE ECU AS A PRECAUTION. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007052500051 20070525 00051 EA 2007 5 25 QXEA200700784 1 20070512 A 3150 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA UNKNOWN A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 600QX 10005 OAK - INTERMITTENT FIDEEX FIRE FAULT MESSAGE. MAINTENANCE PLACED ON MEL. MEL CLEARED BY PERFORMING A OPERATIONAL CHECK WITH NO FAULTS FOUND. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007052500053 20070525 00053 NM 2007 5 25 QXEA200700817 1 20070516 A 5210 85217907102 PIN BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR BINDING A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 416QX 4083 PDX FLIGHT NR 2454: FA ADVISES THAT LEFT REAR DOOR HARD TO OPEN AND CLOSE. MAINTENANCE REMOVED AND REPLACED EXTERNAL ME CHANISM GUIDE PINS WHICH WERE BINDING. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007052500055 20070525 00055 EA 2007 5 25 QXEA200700719 1 20070505 A 3310 LIGHT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT SPARKS A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 601QX 10009 TUL- WHILE DEPLAINING THE PASSENGERS, THE FIRST OFFICERS MAP LIGHT STARTED TO ARC AND SPARK FROM THE BACK OF THE UNIT. T HEN FOR APPROX 30 SECONDS IT SMOKED. AFTER THAT, NOTHING ELSE HAPPENED. MAINTENANCE FOUND THE BULB NOT MAKING CONTACT WI TH THE CONTACTOR, ADJUSTED THE CONTACTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007052500058 20070525 00058 EU 2007 5 25 AALA20070900 1 20070520 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 50051 459 MIA - EMERGENCY LIGHT AT SEAT 11G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 11G. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A35EU 2007052500062 20070525 00062 GL 2007 5 25 AALA20070903 2 20070521 A 7320 285T00967 EEC BOEING 767 767323 1385205 NM GE CF6 CF680C2* GL ENGINE INOPERATIVE A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 359AA 24040 690371 LAX INFLIGHT T161/21MAY - ON SHORT FINAL WITH AUTO THROTTLES OFF BOTH ENGINES WERE AT 40 PERCENT N1 THEN RIGHT ENGINE WE NT BACK TO 32 PERCENT N1. LANDED LAX WITHOUT INCIDENT. REPLACED THE M644 ELECTRONIC ENGINE CONTROL CARD. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A1NM E23EA 2007052500074 20070525 00074 NM 2007 5 25 AALA20070888 1 20070519 A 7330 SWITCH BOEING 767 767323 1385205 NM RT ENGINE INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 343AN 33082 ORD INFLIGHT T54/19MAY - DURING CLIMB RIGHT ENGINE FUEL FILTER CLOG INDICATION. NO DECREASE IN AIRCRAFT OR ENGINE PERFO RMANCE. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE FUEL FILTER AND RIGHT ENGINE FUEL FILTER DI FFERENTIAL PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007052500082 20070525 00082 NM 2007 5 25 AALA20070887 1 20070519 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 387AM 27184 MIA - EMERGENCY EXIT SIGN LIGHT AT RIGHT OVERWING DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY EXIT SIGN LIGHT AT RIG HT OVERWING DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007052500109 20070525 00109 EA 2007 5 25 SWIA200718244 1 20070512 A 5410 DOOR CNDAIR CL600 CL6002B19 1900309 EA RT NACELLE DETACHED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 944SW 7764 UPON LANDING, INFORMED BY RAMP THAT THE UPPER RIGHT ENGINE COWLING WAS MISSING. ON POST FLIGHT, FOUND DAMAGE TO THE RIG HT HORIZONTAL STABILIZER LEADING EDGE. REPLACED RIGHT HORIZONTAL LEADING EDGE ASSEMBLY. REPLACED UPPER FAN COWL CAMLOC K RECEPTACLE AND INSTALLED SERVICABLE ENGINE COWL ON RIGHT ENGINE. 2 L 7 2 4F RT A21EA 2007052500110 20070525 00110 EU 2007 5 25 F3LA200700117 1 20070521 A 5321 D5361060500100 FLOOR PANEL AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 802FR 4993 1991 DURING C-3 CHECK, INSPECTION REPORTED FLOOR PANEL 221FF CORRODED. REPLACED FLOOR PANEL 221FF IAW AMM 53-12-12-400-001. 2 L 7 2 4F RT 2007052500111 20070525 00111 EU 2007 5 25 F3LA200700114 1 20070516 A 5321 D5367180500400 FLOOR PANEL AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 802FR 4993 1991 DURING C-3 CHECK, INSPECTION REPORTED FLOOR PANEL 261FF CORRODED. REPLACED PANEL 261FF IAW AMM 53-42-12, PB 401. 2 L 7 2 4F RT 2007052500112 20070525 00112 EU 2007 5 25 F3LA200700115 1 20070516 A 5321 D5367180500500 FLOOR PANEL AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 802FR 4993 1991 DURING C-3 CHECK, INSPECTION REPORTED FLOOR PANEL 262FF CORRODED. REPLACED PANEL 262FF IAW 53-42-12, PB 401. 2 L 7 2 4F RT 2007052500114 20070525 00114 EU 2007 5 25 NWAA071923301 1 20070519 A 3350 POWER SUPPLY AIRBUS 330 A330323 3930335 EU EMERGENCY LIGHTS NO TEST A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 801NW 0524 DOOR 2L EPSU EMERGENCY POWER SUPPLY FAILED IT OPERATIONAL TEST, REMOVED AND REPLACED POWER PACK AND CHECKED GOOD. 2 L 7 2 4F RT A46NM 2007052500115 20070525 00115 EU 2007 5 25 NWAA071933301 1 20070519 A 3350 POWER SUPPLY AIRBUS 330 A330323 3930335 EU EMERGENCY LIGHT NO TEST A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 801NW 0524 CREW REST EPSU EMERGENCY POWER SUPPLY FAILED IT OPERATIONAL TEST, REMOVED AND REPLACED POWER PACK AND CHECKED GOOD. 2 L 7 2 4F RT A46NM 2007052500116 20070525 00116 2007 5 25 F3LA200700119 4 20070523 A 2565 GIRT BAR AIRBUS A318 A318111 3940019 EU L2 DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 802FR 4993 1991 DURING C-3 CHECK, INSPECTION REPORTED L2 FWD GIRT BAR FITTING AND HARDWARE CORRODED. REPLACED GIRT BAR BLANKING PLATE I AW 52-13-31-400-007. 2 L 7 2 4F RT 2007052500117 20070525 00117 EU 2007 5 25 F3LA200700113 1 20070515 A 5320 SHEAR PLATE AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 802FR 4993 1991 DURING C-3 CHECK, INSPECTION REPORTED AFT LT SHEAR PLATE CORRODED BETWEEN FR 69 AND FR70. REPLACED AFT LT SHEAR PLATE IAW SRM 51-42-11. 2 L 7 2 4F RT 2007052500118 20070525 00118 SO 2007 5 25 FFKA118 2 20070517 A 8520 643627 CRANKSHAFT PIPER PA34 PA34200T 7103406 SO CONT O360 TSIO360EB 17025 SO HARTZL HCC2Y BHCC2YF2 GL NR 1 ENGINE CRACKED B FFKA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 05 6935C 1286 1286 347870167 826972R AN7458B PILOT REPORTED AN OIL LEAK COMING FROM THE LEFT (NR 1) ENGINE AFTER FINISHING THEIR FLIGHT FOR THE DAY. MAINTENANCE INV ESTIGATED THE OIL LEAK AND FOUND THE CRANKSHAFT CRACKED AROUND THE CIRCUMFERENCE OF THE PROPELLER FLANGE. WHEN MAINTENA NCE STARTED TO REMOVE THE PROPELLER THEY FOUND AN O-RING IN-BETWEEN THE PROPELLER HUB AND THE CRANKSHAFT FLANGE, WHICH W AS NOT SUPPOSED TO BE THERE. THIS MAY OR MAY NOT HAVE CONTRIBUTED TO THE FAILURE. 1 L 7 2 3O 3 O A7SO E9CE 5 C P920 2007052500119 20070525 00119 NM 2007 5 25 QXEA200700836 1 20070509 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 331-547 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - CORROSION IN CENTER CHANNEL AND UPPER FLANGE OF RIGHT OUTBOARD SEAT TRACK NR 19 FROM STATION 331.0 TO 547.0. REPAIRED IAW RD8/4-53-884, AND SRM 51-40-10, 51-42-15, 51-42-15. 2 H 7 2 4T RT A13NM 2007052500120 20070525 00120 NM 2007 5 25 QXEA200700840 1 20070510 A 5330 DOUBLER BOMBDR DHC8 DHC8402 1390042 NM SERVICE PORT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - CORROSION DAMAGE ON THE LAVATORY SERVICE PORT INTERNAL DOUBLER AT STRINGER 27S. REPAIRED IAW RD8/4-53-347. 2 H 7 2 4T RT A13NM 2007052500121 20070525 00121 NM 2007 5 25 QXEA200700841 1 20070515 A 5210 HANDLE BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - MAIN CABIN DOOR EXTERIOR HANDLE RUBBER BUMPER STOP MOUNT BOLT HOLE IN FUSELAGE IS OVERSIZED AND OVALED. REPAIR ED IAW RD8/4-52-342. 2 H 7 2 4T RT A13NM 2007052500122 20070525 00122 NM 2007 5 25 QXEA200700837 1 20070517 A 5753 FITTING BOMBDR DHC8 DHC8402 1390042 NM TE FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - LEFT OUTBOARD FLAP FORWARD INBOARD AND OUTBOARD MOUNT FITTINGS TO NR 4 CARRIAGE, HAVE FLAT SPOTS WORN ON ENDS. REPAIRED IAW RD8/4-57-228. 2 H 7 2 4T RT A13NM 2007052500123 20070525 00123 NM 2007 5 25 QXEA200700835 1 20070510 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSEAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - PITTING CORROSION ON LEFT CENTER SEAT TRACK UPPER FLANGE FROM STATION 30.0 TO 56.0. REPAIRED IAW RD8/4-53-884, AND SRM 51-42-05, 51-25-90, 51-42-00, 51-40-15. 2 H 7 2 4T RT A13NM 2007052500124 20070525 00124 NM 2007 5 25 QXEA200700839 1 20070509 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM BS 566 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - THERE IS A DENT ON THE LEFT SIDE OF FUSELAGE AFT OF SKIN JOINT X566.025 BETWEEN STRINGERS 12 AND 13. REPAIRED IAW SRM 53-00-00, RD8/4-53-666. 2 H 7 2 4T RT A13NM 2007053000095 20070530 00095 WP 2007 5 30 07FDEA01826 1 20070516 A 5230 SPOOL DOUG DC10 DC1010F 3022111 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 NR 1 MAIN CARGO DOOR LATCH SPOOL BOLT HOLES HAVE CORROSION. REAMED ALL 4 BOLT HOLES NR 2 LATCH SPOOL BOLT HOLES IAW DC1 0 SRM 53-50-00 FIG 17 VOLI TO .460. NO FURTHER EVIDENCE OF CORROSION REMAINS. 2 L 7 3 4F A22WE 2007053000096 20070530 00096 NM 2007 5 30 07FDEA01827 1 20070517 A 5320 6916970501 INTERCOSTAL BOEING 727 7272S2F 1384O81 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 MAIN DECK BODY FRAME INTERCOSTAL ASSY CLIP IS CRACKED BS 351, STR 15L REMOVED AND REPLACED CLIP. REF SRM 51-30-2 PG 1-3 AND 5-7. 2 L 7 3 4F A3WE 2007053000097 20070530 00097 NM 2007 5 30 07FDEA01828 1 20070517 A 5311 651593920 FRAME BOEING 727 7272S2F 1384O81 NM BS 720 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 FWD PIT FRAME, STA 720 DENTED BETWEEN STRINGER 23-24R REMOVED DAMAGE SECTION OF FRAME REF SRM 53-10-4 FIG 1. FABRICATED REPAIR PARTS REF SRM 53-10-4 FIG 1. DRILLED REPAIR PARTS REF 51-10-4, AND INSTALLED NEW REPAIR PARTS REF SRM 53-10-4 FIG 1. 2 L 7 3 4F A3WE 2007053000098 20070530 00098 WP 2007 5 30 070113 1 20070502 A 3350 408822101 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT NO TEST A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 887GA 49932 DURING A ROUTINE OVERNIGHT SERVICE CHECK, INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENC Y EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BA TTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007053000099 20070530 00099 WP 2007 5 30 070114 1 20070503 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS NO TEST A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 862GA 49556 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007053000100 20070530 00100 WP 2007 5 30 070115 1 20070503 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS NO TEST A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 869GA 53294 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007053000101 20070530 00101 WP 2007 5 30 070118 1 20070516 A 3350 BULB DOUG DC9 DC987 3022087 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 948MA 49778 DURING A ROUTINE OVERNIGHT SERVICE CHECK, INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENC Y EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL RELAMPED THE EMERGENCY LIGHT ASSEMBLY AS REQUIRED. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007053000102 20070530 00102 WP 2007 5 30 070112 1 20070502 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS NO TEST A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 862GA 49556 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007053000103 20070530 00103 WP 2007 5 30 070116 1 20070507 A 3350 BULB DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 865GA 49998 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL RELAMPED THE EMERGENCY LIGHT ASSEMBLY AS REQUIRED. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007053000104 20070530 00104 WP 2007 5 30 070117 1 20070508 A 3397 WIRE DOUG DC9 DC987 3022087 WP EMERGENCY LIGHT DAMAGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 948MA 49778 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REPAIRED A DAMAGED WIRE IN THE EMERGENCY LIGHT ASSEMB LY AS REQUIRED. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVI CE. 2 L 7 2 4F RT A6WE 2007053000105 20070530 00105 NM 2007 5 30 DU4R2007120 1 20070523 A 5330 SKIN BOEING 757 757232 1384965 NM BS 310 DAMAGED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 640DL 23994 FOUND LIGHTNING STRIKE AT BS 310 BETWEEN S-2R AND S-3R. REPAIRED BY CUTTING OUT STRIKE AREA, HFEC INSPECTED IAW B757 NT M PT6 51-00-01, 51-00-19 NO RELEVANT INDICATIONS NOTED. FABRICATED AND INSTALLED REPAIR DOUBLER 8.0 BY 7.75 FROM 2024-T 3 .071 IAW B757 SRM 53-00-01 FIG 201. 2 L 7 2 4F RT A2NM 2007053000106 20070530 00106 NM 2007 5 30 07FDEA01818 1 20070515 A 2910 LINE BOEING 727 727233 138408A NM HYD SYSTEM FAILED A FDEA O OTHER K FLUID LOSS LD LANDING 1 SO 25 273FE 22038 AFTER TOUCHDOWN AMD SPOILER DEPLOYMENT, EXPERIENCED LOSS OF "A" HYDRAULIC SYSTEM QUANTITY AND PRESSURE. FOUND BLOWN FLE X LINE ON LT ELEVATOR PCU. PART IS IN STOCK AT SAV. REMOVED AND REPLACED I/B FLEX LINE PER MM27-30-081-4. SERVICED "A " HYD SYS TO FULL PER MM 12-12-000-2. REMOVED AND REPLACED NR 1 AND NR 2 CASE DRAIN FILTERS PER MM 29-11-041-2. REMOVE D AND REPLACED "A" SYSTEM PRESSURE FILTERS PER MM 29-11-062-3. RAN NR 1 AND NR 2 ENGINES. NO METAL FOUND IN FILTERS. ALL SYSTEMS OPS AND LEAK CHECK GOOD. 2 L 7 3 4F RT A3WE 2007053000127 20070530 00127 EU 2007 5 30 AWXA200700666 1 20070524 A 5320 D53472189202 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 - FUSEL CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 603AW 661 SAL - CORROSION ON CABIN FLOOR SUPPORT, -Y1162, FR 67 + 17". REPLACED CABIN FLOOR SUPPORT, -Y1162, FR 67 TO FR 69 IAW A 320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007053000128 20070530 00128 EU 2007 5 30 AWXA200700667 1 20070523 A 5347 D53472190205 SEAT TRACK AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 603AW 661 SAL - CORROSION ON CABIN SEAT RAIL, -Y1292, FR 66. REPLACED CABIN SEAT RAIL, -Y1292, FR 64 - FR 66 IAW A320 SRM 51-72- 11. 2 L 7 2 4F RT A28NM 2007053000129 20070530 00129 NM 2007 5 30 AWXA200700668 1 20070523 A 5320 D53471124200 SHEAR PLATE AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 804AW 1043 SAL - CORROSION ON SHEAR PLATE, +Y1175, FR.69 - FR 70. REPLACED SHEAR PLATE, +Y1175, FR.69 - FR 70 IAW A319 SRM 51-72-1 1. 2 L 7 2 4F RT A28NM 2007053000130 20070530 00130 NM 2007 5 30 AWXA200700669 1 20070523 A 5320 D53472172204 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 804AW 1043 SAL - CORROSION ON CABIN FLOOR SUPPORT, +Y1292, FR 67 - FR 68. REPLACED CABIN FLOOR SUPPORT,+Y1292, FR.67 - FR 68 IAW A 319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007053000131 20070530 00131 NM 2007 5 30 AWXA200700670 1 20070523 A 5320 D53472188204 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 804AW 1043 SAL - MAJOR REPAIR - CORROSION ON CABIN FLOOR SUPPORT, +Y1292, FR 68 - FR 70. REPLACED CABIN FLOOR SUPPORT ,+Y1292, FR 68 - FR 70 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007053000132 20070530 00132 NM 2007 5 30 AWXA200700671 1 20070522 A 5320 D53471124201 SHEAR PLATE AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 804AW 1043 SAL - MAJOR REPAIR - CORROSION ON SHEAR PLATE, -Y1175, FR 69 - FR 70. REPLACED SHEAR PLATE, -Y1175, FR 69 - FR 70 IAW A 319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007053000133 20070530 00133 EU 2007 5 30 AWXA200700672 1 20070524 A 5320 D53472172203 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 603AW 661 SAL - CORROSION ON CABIN FLOOR SUPPORT, -Y1192, FR 66 + 4" TO FR 67 + 15". REPLACED CABIN FLOOR SUPPORT, -Y1192, FR 66 + 4" TO FR 67 + 15" IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007053000134 20070530 00134 EU 2007 5 30 AWXA200700673 1 20070524 A 5320 D5347218820200 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 603AW 661 SAL - CORROSION ON CABIN FLOOR SUPPORT, +Y1162, FR 68. REPLACED CABIN FLOOR SUPPORT, +Y1162, FR 68 - 5" TO FR 69 - 2" I AW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007053000135 20070530 00135 EU 2007 5 30 AWXA200700674 1 20070522 A 5320 D5347219220000 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 603AW 661 SAL - CORROSION ON CABIN FLOOR SUPPORT, +Y765, FR 67 + 16". REPLACED CABIN FLOOR SUPPORT, +Y765, FR 66 + 5" TO FR 70 IA W A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007053000165 20070530 00165 NM 2007 5 30 QXEA200700822 1 20070521 A 6100 UNKNOWN DHAV DHC8 DHC8202 2809007 NM NR 1 PROP TORQUE UNKNOWN A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 347PH 480 SEA FLIGHT NR 2053, DURING NORMAL SINGLE ENGINE TAXI WITH NR 1 PROP FEATHERED POWER LEVERS SET BETWEEN DISC AND FLIGHT I DLE. UPON MOVING NR 1 CONDITION LEVER FROM START/FEATHER TO MAX, NR 1 TORQUE INCREASED RAPIDLY TO 30 PERCENT TORQUE. E NGINE STABILIZED AFTER UNFEATHERING WITH NORMAL SHUTDOWN. MAINTENANCE COMPLIED WITH PCU HEALTH HECK NO DEFECTS NOTED. SET POWER LEVER AND CONDITION LEVER AS PER DISCREPANCY COULD NO DUPLICATE THE PROBLEM. NO PARTS REPLACED. AIRCRAFT RET URNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007053000166 20070530 00166 NM 2007 5 30 QXEA200700821 1 20070519 A 2420 31708001A GENERATOR DHAV DHC8 DHC8202 2809007 NM NR 1 AC MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 NM 09 353PH 517 496 PDX FLIGHT NR 2149 - DURING TAKEOFF, NR 1 AC GENERATOR CAUTION ILLUMINATED AFTER CYCLING NR 1 AC GENERATOR PER CHECK LIS T NR 1 STALL WARNING CAUTION ILLUMINATED THEN WENT OUT. THEN NR 1 AC GENERATOR CAUTION ILLUMINATED AGAIN. MAINTENANCE REPLACED THE NR 1 AC GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007053000167 20070530 00167 NM 2007 5 30 QXEA200700819 1 20070519 A 3397 CONNECTOR DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHTS MALFUNCTIONED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 359PH 514 PDX - EMERGENCY TRACK LIGHTING (AT FORWARD RIGHT EMERGENCY HATCH/DOOR) FORWARD RED LIGHT STRIP INOP. FOUND PINS P3 AND 2 SWAPPED. RE-PINNED CONNECTOR. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007053000168 20070530 00168 EU 2007 5 30 F3LA200700116 1 20070519 A 5347 D5311278220200 SEAT TRACK AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 802FR 4993 1991 DURING C-3 CHECK, INSPECTION REPORTED SURFACE CORROSION ON CABIN FLOOR FR20 AT -Y765 (RT I/B SEAT TRACK). REPLACED SEAT TRACK IAW SRM 51-42-11 AND 51-72-11. 2 L 7 2 4F RT 2007053000169 20070530 00169 WP 2007 5 30 IXXA07SMN138S 1 20070421 A 5313 LONGERON DOUG DC8 DC871F 302199D WP ZONE 100 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR INSTALLED AT A-PIT BASKET DOOR, RIGHT FORWARD JAMB CORNER AT ST ATION 293 LONGERON 30 RIGHT. REMOVED EXISTING REPAIR. FABRICATED REPAIR DOUBLER, TRIPLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACE. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D, DC8 SRM 53-2-0 FIGURE 19 T/R NUMBER 53-136 AND 53-186, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-21, AND DC8 51-3-1,AD 2005-18-07 , DACO SERVICE BULLETIN DC8-53-078, AND DOUGLAS DRAWING SR08530019 AND 5750776. 2 L 7 4 4F RT 4A25 2007053000200 20070530 00200 NM 2007 5 30 SB07039 1 20070524 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM EMERGENCY LIGHTS FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 450UW 24933 BWI - DURING WEEKLY CHECK, MAINTENANCE DISCOVERED THE EMERGENCY EXIT LIGHTS FROM SEAT ROWS 12 THRU 19 INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007053000201 20070530 00201 EA 2007 5 30 COMA0760399 1 20070526 A 2916 73031 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 804CA 13545 7352 FLIGHT 5555 - GEAR DISAGREE MESSAGE, MAIN GEAR UP NOSE GEAR STILL HAS MARKS AND NOSE GEAR SOUNDED DOWN. AIRCRAFT RETURN ED TO GSO AND LANDED SAFELY. REMOVED AND REPLACED SYSTEM NR 3 HYDRAULIC RESERVOIR. 2 L 7 2 4F RT A21EA 2007053000202 20070530 00202 EA 2007 5 30 COMA0760397 1 20070526 A 3230 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA MLG FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 804CA 11924 7352 FLIGHT 5555 - GEAR DISAGREE MESSAGE, MAIN GEAR UP NOSE GEAR STILL HAS MARKS AND NOSE GEAR SOUNDED DOWN. AIRCRAFT RETURN ED TO GSO AND LANDED SAFELY. REMOVED AND REPLACED 3B ACMP. 2 L 7 2 4F RT A21EA 2007052400065 20070524 00065 2007 5 24 SWAA072539 4 20070521 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052400077 20070524 00077 NM 2007 5 24 UPS07549839 1 20070427 A 5311 146N103069 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 404UP 23726 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1480, S26L. REPAIR ACCOMPLISHED PER FINAL EA 757-5362-27-A1667 A ND UPS ENG FILE N NUMBER:757-53-20245 WITH NO DEVIATIONS. 2 L 7 2 4F RT A2NM 2007052400078 20070524 00078 NM 2007 5 24 UPS07549840 1 20070427 A 5311 146N102889 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 404UP 23726 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1400, BETWEEN S25L AND S26L. REPAIR AT FRAME STA 1400, BETWEEN S 25L AND S26L HAS BEEN ACCOMPLISHED PER FINAL EA 757-5362-27-A1664 AND UPS EO B757-5310-26834-A WITH NO DEVIATIONS. 2 L 7 2 4F RT A2NM 2007052400088 20070524 00088 NM 2007 5 24 SWAA072558 1 20070521 A 5753 6546435 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND LEFT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER SURFACE. REPAIRED FLAP PE R SRM. 2 L 7 2 4F RT A16WE 2007052400090 20070524 00090 NM 2007 5 24 SWAA072561 1 20070521 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052400099 20070524 00099 NM 2007 5 24 SWAA072566 1 20070521 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052400100 20070524 00100 NM 2007 5 24 SWAA072564 1 20070521 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R AND 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052400101 20070524 00101 NM 2007 5 24 SWAA072557 1 20070521 A 5312 6546568 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 3 O'CLOCK POSITION. REPAIRED WEB PER S RM. 2 L 7 2 4F RT A16WE 2007052400171 20070524 00171 NM 2007 5 24 2007UALA01522 1 20070515 A 2120 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LAVATORY SHORTED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 508UA 24744 DIVERTED TO DEN UNDER AMBER ALERT DUE ELECTRICAL ODOR IN FORWARD LAVATORY. [06-20-07] FOUND LAV DOOR LOCK-LIGHTING SWI TCH SHORTED & BURNED. LAV POWER CIRCUIT BREAKER POPPED. REPLACED DOOR SWITCH. ALL FUNCTIONS AND SMELLS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052400181 20070524 00181 NM 2007 5 24 BB07037 1 20070521 A 3242 214572 BRAKE BOEING 757 7572B7 1384964 NM NR 7 CRACKED A USAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 EA 19 201UU 6622 27810 FLIGHT 0728, PHL-GLA: AFTER TAKEOFF, HYDRAULIC QUANTITY STARTED DROPPING ON BOTH LEFT AND RIGHT SYSTEMS. RETURNED TO P HL. MAINTENANCE FOUND THE NUMBER 7 BRAKE HOUSING CRACKED. REPLACED BRAKE. 2 L 7 2 4F RT A2NM 2007052400184 20070524 00184 NM 2007 5 24 USAA070398 1 20070521 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 940UW 27805 STA 345, LBL 0 - LBL 20, CABIN FLOORBEAM CORRODED. BLENDED AREA & INSTALLED DOUBLERS PER TYP REP 53-15-02, 51-20-01, CO RR TASK C53-221-03; LEVEL 1, DEFECT SIZE: 1"L X 1"W X .013"D. 2 L 7 2 4F RT A2NM 2007052400214 20070524 00214 NM 2007 5 24 USAA070410 1 20070523 A 5320 BRACKET BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 STA 380 STR 20L HAS CRACK. REMOVED & REPLACED PRIMARY STRUCTURE PER SRM 51-10-02, BOEING MPN 69-45145-1, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007052400273 20070524 00273 NM 2007 5 24 CALA0700256 1 20070521 A 2497 WIRE HARNESS BOEING 737 737524 1384721 NM NR 1 ENGINE BURNED A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 14660 28921 THE LEFT SIDE CABIN LIGHTS QUIT WORKING ACCOMPANIED BY AN ELECTRICAL SMELL SHORTLY AFTER TAKEOFF FROM EWR. THE STAB TRI M QUIT WORKING A SHORT TIME LATER. THE AIRCRAFT WAS RETURNED TO EWR. THE NR 1 BUS OFF LIGHT ILLUMINATED ON FINAL. MAI NTENANCE FOUND THE NR 1 TRANSFORMER RECTIFIER CIRCUIT BREAKER POPPED. THE NR 1 ENGINE GENERATOR FEEDER CABLES WERE BURN T AND THE CONNECTOR AND RECEPTACLE WERE SHORTED AT THE FIREWALL. THE NR 1 ENGINE GENERATOR FEEDER HARNESS WAS REMOVED A ND REPLACED AND CONNECTORS D410 AND D3024 WERE ALSO REMOVED AND REPLACED IAW SWP 20-30-11 AND 20-61-19. AN OPERATIONAL CHECK OF THE NR 1 ENGINE GENERATOR WAS PERFORMED IAW MM 24-21-00, PAGE 509, ITEM N AND NO FAULTS WERE FOUND. 2 L 7 2 4F RT A16WE 2007052400277 20070524 00277 2007 5 24 RAIA00705034 4 20070517 A 3140 DAU EMB 145 EMB145LR 3260212 SO NR 1 MALFUNCTIONED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 811HK 145256 FLT NR 5526 - ATL - DAU NR 1 FAIL ON TAKEOFF. MAINTENANCE RE-RACKED DAU NR 1, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007052400306 20070524 00306 SO 2007 5 24 200714323 1 20070522 A 5347 13500412005 SEAT TRACK EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 LEFT OUTBOARD SEAT TRACK BETWEEN FRAMES 53 AND 55 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM. RETURNED AIRC RAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052500002 20070525 00002 SO 2007 5 25 200714306 1 20070522 A 5320 14522459003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 145224 FOUND FORWARD CABIN FLOOR SUPPORT AT FRAME 20 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW EMB SRM. RETURNED AIRCR AFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007052500036 20070525 00036 NM 2007 5 25 AALA20070926 1 20070430 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 963AN 29543 TUL - EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT M1674 STATION 322 FOR EMERGENCY LIGHT FOR WARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007052500044 20070525 00044 WP 2007 5 25 AALA20070928 1 20070523 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70504 49798 LGA - EMERGENCY LIGHTS AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007052500047 20070525 00047 SO 2007 5 25 200714202 1 20070521 A 3320 BR00022 BALLAST EMB 145 EMB145LR 3260212 SO CABIN LIGHT BLOWN A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 619AE 145101 FLIGHT ATTENDANT REPORTED ELECTRICAL SMELL IN FRONT OF CABIN. REMOVED AND REPLACED GALLEY AREA CEILING LIGHT BALLAST IA W EMB AMM. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007052500073 20070525 00073 WP 2007 5 25 AALA20070916 1 20070522 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 469AA 49599 SFO - EMERGENCY EXIT SIGN LIGHT AT FORWARD OVERWING EXIT DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIG N LIGHT AT FORWARD OVERWING EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007052500081 20070525 00081 NM 2007 5 25 AALA20070890 1 20070519 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39365 24046 MIA - EMERGENCY LIGHT AT SEAT 13H INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 13H. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007053000203 20070530 00203 EA 2007 5 30 COMA0760398 1 20070526 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 804CA 18922 7352 FLIGHT 5555 - GEAR DISAGREE MESSAGE, MAIN GEAR UP NOSE GEAR STILL HAS MARKS AND NOSE GEAR SOUNDED DOWN. AIRCRAFT RETURN ED TO GSO AND LANDED SAFELY. REMOVED AND REPLACED NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2007053000205 20070530 00205 EA 2007 5 30 COMA0760402 1 20070528 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNSECURE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 805CA 7354 FLIGHT 5078 - PAX DOOR OUTER HANDLE CAUTION AFTER TAKEOFF. AIRCRAFT RETURNED BACK TO JAX AND LANDED SAFELY. PAX DOOR O UTER HANDLE VERIFIED NOT STOWED BY GROUND CREW. INSPECTED PAX DOOR OUTER HANDLE AND PERFORMED OPS CHECKS, NO DEFECTS NO TED. 2 L 7 2 4F RT A21EA 2007053000206 20070530 00206 NM 2007 5 30 SB07038 1 20070524 A 3350 1012721 LIGHT BOEING 737 7373B7 1384580 NM SEAT 18C INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 533AU 24515 DCA - MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHTING AT SEAT 18C INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH E LIGHT ASSEMBLY BASE AT SEAT 18C PER MM 33-51-12. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007053100002 20070531 00002 WP 2007 5 31 UPS07849858 1 20070525 A 5250 DOOR DOUG DC8 DC873F 302199F WP COCKPIT OUT OF ADJUST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:N/A COCKPIT DOOR EXTREMELY HARD TO OPEN AFTER CLOSING. ADJUSTED DOOR FOR EASIER OPENING. OPS CHECK GOO D. 2 L 7 4 4F RT 4A25 2007053100005 20070531 00005 2007 5 31 UPS07849861 4 20070526 A 2565 SLIDE DOUG DC8 DC873F 302199F WP PAX DOOR UNSECURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 THE FWD ENTRY EMERGENCY EXIT SLIDE IS SLIPPING OUT OF THE RETAINING COMPARTMENT. REPACKED FWD ENTRY EMERGENCY ESCAPE SL IDE IAW MM 25-60-01-2. 2 L 7 4 4F RT 4A25 2007053100006 20070531 00006 2007 5 31 UPS07849863 4 20070525 A 2565 GAUGE DOUG DC8 DC873F 302199F WP SLIDE BOTTLE OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:N/A ENTRY DOOR SLIDE PRESSURE GAUGE NOT VISIBLE. REPOSITIONED SLIDE SO PRESSURE GAUGE CAN BE READ. 2 L 7 4 4F RT 4A25 2007053100007 20070531 00007 SO 2007 5 31 C2XA07IA124 1 20070526 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14105 145649 IAH - FLIGHT 2739, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN ON THE SERVICE DOOR WAS I NOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEF ECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007053100008 20070531 00008 NM 2007 5 31 UPS07M49856 1 20070321 A 5310 PANEL DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C AFT FUSELAGE COMPARTMENT, ADJACENT STA 2011 AT UPPER TORQUE BOX RT ACCESS DOOR CUTOUT EDGE, PLANE PANE L FOUND CRACKED. CRACKED AREA TRIMMED PER EN1223-07. HFEC INSP C/O DAC NDTSPM R13 06-10 -01.001 ON TRIM AREA, FOUND NO CRACK EVIDENT. FILLER FAB PER EN1223-07. DOUBLER & SHIM FAB SRM 53-40-00 FIG 23 VI R38. SHIM, FILLER TREATED SRM 51- 21-01 VII R38. NEW BRACE FAB PER BOEING DWG AJC7110RA. FPI C/O ON BRACE, NO CRACK EVIDENT. DOUBLER/SHIM/FILLER & BRAC E INSTALLED SRM 51-31-01 VII R39. 2 L 7 3 4F RT A22WE 2007053100009 20070531 00009 SO 2007 5 31 C2XA07IA125 1 20070527 A 3350 3025103 LIGHT EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 31131 145705 IAH - DURING MAINTENANCE INSPECTION THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE AFFECTED LIGHT ASSY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. 2 L 7 2 4F RT 2007053100014 20070531 00014 NM 2007 5 31 ASAA0741716 1 20070530 A 5330 65C329541 SKIN BOEING 737 7374Q8 138447Q NM BS 793-818 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 DENT IN FUSELAGE SKIN. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR FILLERS DOUBLERS AND TRIPLER IAW ASA EA 5330 02211. 2 L 7 2 4F RT A16WE 2007053100020 20070531 00020 WP 2007 5 31 ASAA0781722 1 20070530 A 5320 993053811 CUSP WEB DOUG DC9 DC983 3022083 WP BS 541-560 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 PASSENGER CABIN FLOOR CUSP WEB IS CORRODED. REMOVED THE CORRODED CUSP WEB LOCATED DRILLED AND INSTALLED A REPLACEMENT C USP WEB IAW SRM 51-10-4 PG 1 AND 4 FIG 3 AND DAC DWG 9930538. 2 L 7 2 4F RT A6WE 2007053100024 20070531 00024 NM 2007 5 31 ZZDA070523165 1 20070523 A 5310 DOOR FRAME BOEING 717 717200 1383700 NM CARGO DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 953AT 55015 CORROSION AT FWD CARGO COMPARTMENT LOWER JAMB. INSTALLED NEW LOWER JAMB PAN BETWEEN STA 370-00 AND 427.00 PER B717 SRM 53-20-15 FIG 201. 2 L 7 2 4F TR A6WE 2007053100026 20070531 00026 NM 2007 5 31 CALA0700267 1 20070526 A 5310 6520723U66 DOOR FRAME BOEING 737 7373T0 1384582 NM BS 480-500 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND A .75 INCH CRACK IN FORWARD CARGO DOOR CUTOUT AFT FRAME AT LOWER DOOR STOP FITTING, STA 480-500, S16R T O S28R. THE FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW SRM 51-40-02, PARAGRAPHS 4 AND 7. 2 L 7 2 4F RT A16WE 2007053100030 20070531 00030 NM 2007 5 31 CALA0700271 1 20070527 A 5315 6546811 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12313 23364 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1016, RBL 20. A REPAIR STRAP WAS INSTALLED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 2007053100031 20070531 00031 NM 2007 5 31 CALA0700272 1 20070527 A 5330 6545774 SKIN BOEING 737 7373T0 1384582 NM BS 727D-727E CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14325 23455 INSPECTION FOUND A 1.5 INCH CRACK IN RT FUSELAGE SKIN AT STA 727D-727E, S22R-24R, AT AFT EMERGENCY LIGHT. THE SKIN WAS REPAIRED IAW ECRA 5330-03682. 2 L 7 2 4F RT A16WE 2007053100036 20070531 00036 NM 2007 5 31 2007UALA01633 1 20070524 A 2432 CHARGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MAIN BATTERY FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 550UA 25398 MAIN BATTERY CHARGER STATUS MESSAGE DISPLAYED. [06-20-07] REPLACED A FAULTY BATTERY CHARGER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007053100038 20070531 00038 NM 2007 5 31 2007UALA01635 1 20070525 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHT ROW 1A INOP. FEEDER CABLE FAULTY. [SUP 06-06-07] REPLACED CABLE FROM POWER FEED TO EMERGENCY LIGHT. OP CHECKS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007053100041 20070531 00041 NM 2007 5 31 2007UALA01638 1 20070525 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 DOOR 4R EMERGENCY EVAC PANEL "EVAC" BUTTON LIGHT INOP. REPLACED LAMP. OP CHECKED OK RE F MM 25-63-01. ACPD ON. 2 L 7 4 4F 4 F RT A20WE E24NE 2007053100043 20070531 00043 2007 5 31 2007UALA01640 4 20070524 A 2565 CYLINDER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT OFFWING SLIDE OUT OF TOLERANCE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 LEFT OFFWING SLIDE INFLATION CYLINDER EXCEEDS LIFE LIMIT. [06-20-07] REPLACED LT OFF WING SLIDE CYLINDER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007053100044 20070531 00044 NM 2007 5 31 ASAA0741699 1 20070527 A 5311 654655242 FRAME BOEING 737 7374Q8 138447Q NM BS 827 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 FRAME SKIN ATTACHMENT ANGLE IS CRACKED AT ATTACHMENT HOLE. REMOVED DAMAGED SECTION OF FRAME FABRICATED AND INSTALLED RE PAIR SHEAR TIE FILLER AND ANGLE IAW SRM 53-00-07 REPAIR 3. 2 L 7 2 4F RT A16WE 2007053100047 20070531 00047 NM 2007 5 31 ASAA0741702 1 20070529 A 5753 SKIN BOEING 737 7374Q8 138447Q NM TE FLAP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 1856 28199 LEFT WING O/B TRAILING EDGE FLAP IS DELAMINATED AT I/B AFT CORNER. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAI R FILLER AND DOUBLER IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007053100051 20070531 00051 NM 2007 5 31 ASAA0741707 1 20070526 A 5730 65C262002 SKIN BOEING 737 737490 1384715 NM RT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 706AS 28894 RIGHT WING FIXED L/E SKIN AT NR 5 SLAT ACTUATOR CURTAIN CUTOUT CRACKED. RIGHT WING FIXED L/E SKIN AT NR 5 SLAT ACTUATOR CURTAIN CUTOUT REPAIRED SERVICEABLE IAW SRM 51-70-17. 2 L 7 2 4F RT A16WE 2007053100055 20070531 00055 2007 5 31 2007UALA01641 4 20070524 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT OFFWING LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 RIGHT OFFWING ESCAPE SLIDE DOOR LOOSE ON AFT END WHEN CLOSED AND LATCHED. [06-20-07] SHIMMED EMERGENCY ESCAPE SLIDE DO OR TO FIT TIGHT. CHECKED FIT AND FAIR WITH FUSE AND FOUND OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007053100056 20070531 00056 EA 2007 5 31 COMA0760395 1 20070524 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FS 559 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 964CA 27296 7129 DURING FS 559 INSPECTION FOUND CRACKS AT BASE OF VERTICAL BOX STIFFENER, FS 559, LBL 0 INBOARD AND OUTBOARD SIDE. CUT O UT DAMAGE AND INSTALLED DOUBLERS IAW REO 601R-53-41-057. 2 L 7 2 4F RT A21EA 2007053100057 20070531 00057 EA 2007 5 31 COMA0760396 1 20070524 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FS 559 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 964CA 27296 7129 DURING FS 559 INSPECTION FOUND CRACKS AT LOWER END OF VERTICAL BOX STIFFENER, FS 559 RBL 9 INBOARD AND OUTBOARD SIDE. C UT OUT DAMAGE AND INSTALLED DOUBLERS IAW CRJ REO 601R-53-41-057. 2 L 7 2 4F RT A21EA 2007053100058 20070531 00058 NM 2007 5 31 2007UALA01642 1 20070524 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 EEL LIGHT BAR AT THE LEFT MID LAV (S LAV) IS INOP. [SUP 06-06-07] REPAIRED BROKEN WIRE. OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007053100059 20070531 00059 NM 2007 5 31 2007UALA01643 1 20070524 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 660UA 27115 AFT GALLEY SMALL EEL LIGHT BAR IS INOP. [SUP 06-06-07] REPAIRED WIRING NEAR AFT GALLEY. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007053100062 20070531 00062 2007 5 31 2007UALA01646 4 20070524 A 3197 CONNECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EICAS DIRTY A UALA O OTHER O OTHER CR CRUISE 1 WP 29 674UA 29242 UPPER EICAS SCREEN BLANKED AGAIN, JUST AFTER LEVEL OFF. COCKPIT TEMP WARM WITH FULL COLD SEL. [06-20-07] TROUBLESH OOTING INCLUDED CHECKING AIRFLOW AND COOLING AIR PATH. REMOVED & REINSTALLED EICAS DISPLAYS. OP CHECKED OK & A/C OK FOR SERVICE. SUSPECT DIRTY CONNECTORS OR IMPROPER SEATING OF DISPLAY PANELS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007053100065 20070531 00065 SO 2007 5 31 C2XA07RI035 1 20070529 A 2530 500064001 COFFEEMAKER EMB 145 EMB145LR 3260212 SO GALLEY ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13997 145298 FLT 2465 - EWR - CREW REPORTED BURNING ODOR FROM COFFEEMAKER WHEN POWER DOWN. EWR MX PERFORMED VISUAL INSPECTION OF BOT H COFFEEMAKERS AND NO FAULTS WERE FOUND. ACFT WAS APPROVED TO RETURN TO SERVICE. COFFEEMAKER NR 1 P/N 500-0640-01 S/N 03-1-32803 TT:9809, TC:7818, TSI:3584. COFFEEMAKER NR 2 P/N 500-0640-01 S/N 02-2-30703 TT:10797, TC:7108, TSI:5143. 2 L 7 2 4T RT T00011AT 2007053100066 20070531 00066 2007 5 31 SB07040 4 20070518 A 2565 D31591479 SLIDE BOEING 737 7373B7 1384580 NM ZONE 200 NO TEST A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 527AU 53177 4442 23862 PHL - THE FORWARD RIGHT HAND SERVICE DOOR EMERGENCY ESCAPE SLIDE FAILED THE ANNUAL OPERATIONAL TEST WHEN IT TWISTED DURI NG DEPLOYMENT. MAINTENANCE REPLACED THE SLIDE. INSPECTED OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2007053100069 20070531 00069 SO 2007 5 31 RAIA00705042 1 20070522 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO CARGO BAY INTERMITTENT A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 846HK 6544 14500855 FLT NR 8020 - STL - BAG SMOKE EICAS. MAINTENANCE REMOVED AND REPLACED BOTH DETECTORS, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007053100070 20070531 00070 SO 2007 5 31 RAIA00705043 1 20070522 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 810HK 145231 POST FLT NR 8087 - IAD - RIGHTHAND OVERWING EXIT IDENTIFIER LIGHT INOP. MAINTENANCE RESEATED CONNECTOR ON EMERGENCY LIG HT, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007053100071 20070531 00071 SO 2007 5 31 RAIA00705044 1 20070522 A 2800 UNKNOWN EMB 145 EMB145LR 3260212 SO FUEL QTY UNKNOWN A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 823HK 145475 FLT NR 7975 - RIC - NR 1 FUEL QUANTITY DROPPED TO ZERO IN FLIGHT. MAINTENANCE DEFERRED PER MEL. 2 L 7 2 4T RT T00011AT 2007053100075 20070531 00075 NM 2007 5 31 USAA070416 1 20070525 A 5320 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM BS 305-345 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 940UW 27805 CABIN FLOOR SUPPORT LBL 0, STA 345.0-395 HAS CORROSION. BLENDED AT STA 374 BL 0, REMOVED & REPLACED FLOOR SUPPORT AT ST A 324-395 AT BL 0 PER SRM 53-00-51, DEFECT SIZE: 4.5"L X 2"W X .016"D. 2 L 7 2 4F RT A2NM 2007053100076 20070531 00076 EU 2007 5 31 USAA070415 1 20070525 A 5310 D5347112420000 SHEAR PLATE AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 178US 1519 LEFT SHEAR TIE PLATE FRAMES 69 - 70 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL. CORR TASK JA-260-53500; LEV EL 1, DEFECT SIZE: 5 X 17 INCHES. 2 L 7 2 4F RT A28NM 2007053100079 20070531 00079 EA 2007 5 31 TRAX200700700 1 20070521 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 851AS 7360 LEFT EMERGENCY EXIT HAS CORROSION, BOTTOM INTERNAL AROUND NUT PLATES FOR ALIGNMENT FITTINGS. 2 L 7 2 4F RT A21EA 2007053100083 20070531 00083 EA 2007 5 31 TRAX200700716 1 20070523 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 976EV 7601 PAX DOOR FWD ANCHOR FITTING CRACKED. [07-23-07] REPAIRED IAW; AMM 52-11-17, AND AMM 52-11-17. 2 L 7 2 4F RT A21EA 2007053100085 20070531 00085 EA 2007 5 31 TRAX200700717 1 20070523 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 976EV 7601 PAX DOOR AFT ANCHOR FITTING CRACKED. [07-23-07] REPAIRED IAW; AMM 52-11-17, AMM 25-21-01, AND AMM 25-26-02, 2 L 7 2 4F RT A21EA 2007053100090 20070531 00090 NM 2007 5 31 USAA200705U10 1 20070524 A 5330 SKIN BOEING 737 7374B7 1384702 NM BS 737E S24L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 451UW 24934 A 1 INCH LONG CRACK IN FUSELAGE SKIN AT BS 737E PLUS 3 INCHES, S-24L. FILLER AND DOUBLER INSTALLED PER SRM 53-00-01 FIG 201. 2 L 7 2 4F RT A16WE 2007053100093 20070531 00093 NM 2007 5 31 HNAA0700091 1 20070521 A 3350 BATTERY PACK GRIMES DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS DISCHARGED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 981HA 378 EMERGENCY LIGHTS BATTERY PACK ARE DEAD. SWITCH LEFT IN THE ON POSTION. SENT FERRY PERMIT TO PIT (JETCARE) GOING TO FER RY TO MDT FOR REPAIRS. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERIES AND POWER SUPPLIES OPS CHECK GOOD IAW -8 MM 33-5 5-00 MORE TO FOLLOW. 2 H 7 2 4T RT A13NM 2007053100095 20070531 00095 EA 2007 5 31 HNAA700089 1 20070520 A 5280 85310188104 HINGE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NLG DOOR BROKEN A HNAA O OTHER O OTHER LD LANDING 1 EA 07 336EN 336 AFTER LANDING IT WAS FOUND THAT THE AFT NOSE GEAR DOOR HINGE HAD BROKEN AND THE DOOR HAD RUBBED ON ONE OF THE NOSE TIRES . 2 H 7 2 4T 4 T RT A13NM E20NE 2007053100097 20070531 00097 EA 2007 5 31 COMA0760401 1 20070527 A 2131 21197688 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA CABIN PRESSURE FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 963CA 26549 7127 FLIGHT 5048 - DURING CLIMBOUT, CABIN RATE FLUX +-2400 FT. SWITCH PRESS CONT WITH NO CHANGE, AIRCRAFT RETURNED BACK TO S GF AND LANDED SAFELY. REMOVED AND REPLACED CONTROLLER, CABIN PRESSURE. 2 L 7 2 4F RT A21EA 2007053100099 20070531 00099 NM 2007 5 31 UPS07549850 1 20070506 A 5412 311N3271 BULKHEAD BOEING 757 75724APF 1384969 NM NR 1 PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 404UP 23726 INSPECTION TYPE:C NR 1 PYLON AFT BULKHEAD LT SIDE LOWER AREA CHAFED. BULKHEAD MILL AND NDT WERE DONE REF TRAVT7/679866. START .201 REMOVED .062 REMAINING .139 X 1.25W X 2.1L. SHOT PEENED REWORKED AREA PER SOPM 20-10-03. FINISHED REWORKED AREA PER SOPM 20-43-03 AND PRELIMINARY 2 EA 757-5453-27-A167. GUSSET WERE FABED REF TRAV T7/680704, FILLER WAS FABED R EF TRAV T7/680702. 2 L 7 2 4F RT A2NM 2007053100100 20070531 00100 NM 2007 5 31 UPS07549851 1 20070509 A 5412 311N3271 BULKHEAD BOEING 757 75724APF 1384969 NM NR 2 PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 404UP 23726 INSPECTION TYPE:C NR 2 PYLON AFT BULKHEAD RIGHT LOWER, OUTER SURFACE CHAFED. BULKHEAD MILL AND NDT WERE DONE REF TRAV T 7/679867. START .200 REMOVED .041 REMAINING .159X 1.25W X2.1L. SHOT PEENED REWORKED AREA PER SOPM 20-10-03, FINISHED R EWORKED AREA PER SOPOM 20-43-03 AND PRELIMINARY 2 EA 757-5453-27-A1670. GUSSETS WERE FABED REF TRAV T7/680705, FILLER W AS FABED REF TRAV T7/680703. 2 L 7 2 4F RT A2NM 2007053100102 20070531 00102 NM 2007 5 31 UPS07M49846 1 20070429 A 5230 SKIN DOUG MD11 MD11F 3023600 NM AFT CARGO DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP 48745 INSPECTION TYPE:4C TRANSFERRED FROM DMI D333800 LP 801902 ITEM 2: INTERIM REPAIR FUSLAGE SKIN DAMAGE AT THE BULK CARGO DOOR PERMANENT NO LATER THAN 4-30-07. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW MD-11 SRM 53-50-00 FIG 16 SH EET 9. 2 L 7 3 4F RT A22WE 2007053100103 20070531 00103 NM 2007 5 31 UPS07M49847 1 20070430 A 5753 ARB2850506 FITTING DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP 48745 INSPECTION TYPE:4C LEFT I/B SLAT FITTING BETWEEN NR 7 & 8 SLAT IS CRACKED. REMOVED AND REPLACED FITTING IAW MD-11 SRM 5 1-33-01 AND 51-35-01. 2 L 7 3 4F RT A22WE 2007053100106 20070531 00106 EA 2007 5 31 TRAX200700691 1 20070520 A 5220 SHAFT CNDAIR CL600 CL6002B19 1900309 EA DOOR HANDLE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 851AS 7360 CREW ESCAPE HATCH OUTER HANDLE SHAFT SHOWS SIGNS OF CORROSION. 2 L 7 2 4F RT A21EA 2007053100111 20070531 00111 EA 2007 5 31 TRAX200700697 1 20070520 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 878AS 7590 RIGHT EMERGENCY EXTERIOR AFT OVERWING LIGHT INOP. 2 L 7 2 4F RT A21EA 2007053100112 20070531 00112 NM 2007 5 31 CALA0700259 1 20070523 A 3350 D71702030 CHARGER BOEING 737 737800* NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 73278 31596 THE EMERGENCY AISLE PATH LIGHTING WAS FOUND INOPERATIVE FROM ROW 15-24. THE BATTERY PACK AND CHARGER WERE REPLACED IAW MM 33-51-06. 2 L 7 2 4F RT A16WE 2007053100113 20070531 00113 NM 2007 5 31 CALA0700260 1 20070524 A 3350 BR9279106 SIGN BOEING 737 7373T0 1384582 NM EMERGENCY EXIT INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14325 23455 THE RIGHT OVERWING ESCAPE DOOR EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. THE EXIT SIGN WAS REMOVED AND REPLACED IAW RE FERENCE TO SWP 20-13-12 AND BRUCE WDM 33-50-00. 2 L 7 2 4F RT A16WE 2007053100114 20070531 00114 EA 2007 5 31 TRAX200700698 1 20070520 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 681BR 7680 CAPTAIN`S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007053100115 20070531 00115 EA 2007 5 31 TRAX200700699 1 20070520 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS NO TEST A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 843AS 7310 OVERHEAD EMERGENCY EXIT SIGN DID NOT ILLUMINATE DURING TEST. 2 L 7 2 4F RT A21EA 2007053100118 20070531 00118 NM 2007 5 31 DHL2007740501 1 20070518 A 5322 SHEAR TIE BOEING 727 7272Q9 138448M NM BS 680 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 WHILE IN "C" CHECK, MAIN CABIN, LT BS 680 WL 210 FRAME PRESENTS CRACK (AT SHEAR TIE). CUTOUT DAMAGED AREA, FABRICATED FILLER FROM 7075T6 .040 PO NR 9004940 DIM 2 1/8 BY 1 AND DOUBLER FROM 7075T6 .050 PO NR 9004843 DIM 5 7/8 BY 3 1/4 IAW B 727 SRM 51-40-3 FIG 1 AND 53-10-4 FIG 11. TREATED AND PRIMED AREA AND PARTS IAW B727 SRM 51-10-2 AND INSTALLED FILLER A ND DOUBLER IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007053100120 20070531 00120 WP 2007 5 31 07FDEA01829 1 20070517 A 5311 LATCH DOUG DC10 DC1010 3022110 WP CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 NR 4 MAIN CARGO DOOR LATCH SPOOL BOLT HOLES HAVE CORROSION. REAMED ALL 4 BOLT HOLES AT NR 4 LATCH SPOOL LOCATION TO .46 0 IAW DC10 SRM 53-50-00 FIG 17 VOLI. NO FURTHER EVIDENCE OF CORROSION REMAINS. 2 L 7 3 4F A22WE 2007053100121 20070531 00121 WP 2007 5 31 07FDEA01830 1 20070517 A 5230 LATCH DOUG DC10 DC1010 3022110 WP CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 NR 5 MAIN CARGO DOOR LATCH SPOOL BOLT HOLES HAVE CORROSION. REAMED HOLES TO .520 WITH NO FURTHER EVIDENCE OF CORROSION. REPAIRED IN REF TODC/MD10 SRM 53-50-00 VOLI PAGE 81. 2 L 7 3 4F A22WE 2007053100124 20070531 00124 WP 2007 5 31 07FDEA01833 1 20070517 A 5520 17451EEL BUSHING BOEING DOUG MD10 MD1010F 3022112 WP RT ELEVATOR LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 RT O/B ELEVATOR I/B DAMPNER HINGE FITTING HAT BUSHINGS ARE LOOSE. REMOVED AND REPLACED RT O/B ELEVATOR I/B DAMPNER HING E FITTING HAT BUSHINGS IAW CMM 55-21-01 AND FEDEX EA 8-5520-109163. ORIGINAL ATTACHED TO FEDEX N/R N00836. 2 L 7 3 4F RT A22WE 2007053100126 20070531 00126 WP 2007 5 31 07FDEA01835 1 20070517 A 5520 174190KSI BUSHING BOEING DOUG MD10 MD1010F 3022112 WP LT ELEVATOR LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 LEFT OUTBD ELEVATOR THIRD HINGE FROM INBD SIDE HAT BUSHINGS LOOSE IN FITTING BORE FOR OUTBOARD DAMPNER. REMOVED AND RE PLACED LT O/B ELEVATOR THIRD HINGE FROM I/B SIDE HAT BUSHINGS IAW CMM 55-21-01 AND FEDEX 8-5520-10913-63. ORIGINAL ATTA CHED TO FEDEX N/R N00836. 2 L 7 3 4F RT A22WE 2007053100127 20070531 00127 NM 2007 5 31 DHL2007740503 1 20070524 A 5310 TORQUE BOX BOEING 727 7272Q9 138448M NM BS 294 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 WHILE IN "C" CHECK, NLG WW STA 294 RT LOWER TORQUE BOX WEB IS CRACKED. TRIMMED OUT CRACKED PORTION IAW B727 SRM 51-10-1 . FABRICATED REPAIR DOUBLER FROM 2024T3 .063 PO NR 9005089 DIM 7 1/2 BY 8 1/4 IAW B727 SRM 53-10-2 FIG 2 AND 51-40-2 FI G 1. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007053100130 20070531 00130 NM 2007 5 31 07FDEA01843 1 20070518 A 5230 65242604 TEE FITTING BOEING 727 7272S2F 1384O81 NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 MAIN UPPER CARGO DOOR S/N 9, TEE SUPPORT FITTING CRACKED AT LATCH HOOK 3RD FWD FROM AFT EDGE BY TORQUE TUBE BEARING FITT ING. REMOVED AND REPLACED DAMAGED T- FITTING WITH NEW TEE CLIP FX797 IAE SRM 51-30-2. 2 L 7 3 4F A3WE 2007053100135 20070531 00135 WP 2007 5 31 07FDEA01821 1 20070515 A 5711 SPAR CAP DOUG DC10 DC1010 3022110 WP RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 RIGHT WING HAS CORROSION ON AFT UPPER SPAR CAP AT XORS=718 TO XORS=733 ENTERED IN ERROR, SEE SDR NR 07-1838 N/R N00804 FOR CORRECTIVE ACTION. 2 L 7 3 4F A22WE 2007053100143 20070531 00143 EU 2007 5 31 07FDEA01923 1 20070521 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 PREVIOUS REPAIR LOCATED ON MAIN CABIN FLOORBEAM FRAME 36 BETWEEN SEAT TRACKS 2 AND 3 RT FWD SIDE UPPER FLANGE HAS 1 REPA IR ANGLE MEASURING 8.6" BY 2.4" AND TWO .250 STOP DRILLED HOLES, THE INBOARD STOP DRILL HOLE HAS A CRACK CONTINUING PAST THE DRILL STOP (0.5 INCH CRACK) PREVIOUSLY INSTALLED REPAIR FOUND NOT TO BE IAW FEDEX EA 6-5321-45448. REMOVED EXISTIN G PREVIOUS REPAIR AND REPAIRED PER FEDEX EA6-5310-110483. REMOVED AND REINSTALLED FLOOR PANEL 232XH IAW A310/200 AMM SU PPLEMENT 53-10-23. 2 L 7 2 4F RT A35EU 2007053100145 20070531 00145 EU 2007 5 31 07FDEA01925 1 20070522 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 AFT CARGO PIT/CABIN FLOORBEAM 58 CRACKED JUST BELOW PREVIOUSLY REPAIR RBL6 FEET APPROX TOTAL CRACK LENGTH 1.0 INCH PREVI OUSLY INSTALLED REPAIR NO IAW A310 SRM 53-10-15 FIG 206. REMOVED EXISTING, REPAIR AND REPAIRED IAW FEDEX EA6-5310-11048 2. 2 L 7 2 4F RT A35EU 2007053100146 20070531 00146 EU 2007 5 31 07FDEA01926 1 20070522 A 5330 SKIN AIRBUS 310 A310203 3930313 EU FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 401FE 191 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED AT LEFT SIDE FUSELAGE SKIN BELOW LAP SEAM BETWEEN FRAMES 35/36 AND BETWEEN STRI NGERS 43/45 LT MEASURES 7.2" BY 7.6" PREVIOUSLY INSTALLED REPAIR NOT FOUND TO BE IAW A310 SRM 53-10-12 FIG 205. REMOVED AND REINSTALLED SIDE WALL PANEL 131MW AND FLOOR PANEL 131RF PER A310/200 AMM 25-54-10-2, 53-10-29-4. REMOVED EXISTING REPAIR AND REPAIRED SKIN PER FEDEX EA6-5310-110471. 2 L 7 2 4F RT A35EU 2007053100148 20070531 00148 NM 2007 5 31 07FDEA01928 1 20070522 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 MAIN DECK CARGO COMPARTMENT, SEAT TRACK STA 765 X= 8.5 FOUND BROKEN. [SUP 06-08-07] REPAIR CARRIED OUT AS PER SRM 53- 70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007053100152 20070531 00152 NM 2007 5 31 07FDEA01932 1 20070522 A 5320 65C260382 CHANNEL BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 AT LWR CARGO BAY, BS 1137-1140, RBL 61-62, WL 208, FLOOR SUPPORT CHANNEL I/B FLANGE LOWER SURFACE IS CORRODED. REMOVED SEAT TRACK REF SRM 51-30-02. REMOVED SIDEWALL PANEL, REMOVED SEAT TRACK SUPPORT CHANNEL. FABRICATED NEW PARTS, TREATED , PRIMED AND PAINTED. INSTALLED NEW PARTS REF SRM 51-30-02. 2 L 7 3 4F A3WE 2007053100154 20070531 00154 WP 2007 5 31 07FDEA01934 1 20070522 A 5313 ACA3796501 LONGERON DOUG DC10 DC1010 3022110 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 LT AIR CONDITIONING COMPT SEVERE CORROSION WITH EXFOLIATION ON LONGERON. REPLACED SECTION OF LONGERON P/N ACA3796-501 I AW SRM 53-10-00 VOL 1 FIG 6. 2 L 7 3 4F A22WE 2007053100156 20070531 00156 WP 2007 5 31 07FDEA01936 1 20070522 A 5710 STRUCTURE DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 RT WING STATION CHORD VERTICAL LEG CRACKED. CRACK TRIMMED OUT FOR RELIEF AND REPAIRED ANGLE INSTALLED IAW SRM 57-20-00 FIG 27 SHT 3 VOL 1. 2 L 7 3 4F A22WE 2007053100157 20070531 00157 WP 2007 5 31 07FDEA01943 1 20070522 A 5320 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 COMPLY WITH FEDEX EA NR 8-5230-110663 "FUSELAGE-MAIN CARGO DOOR - LOWER JAMB FITTING INSPECTION AND DOOR RIG". COMPLIED WITH FEDEX EA NR 8-5230-110663 "FUSELAGE- MAIN CARGO DOOR, LOWER JAMB FITTING INSPECTED AND RIGGED." 2 L 7 3 4F RT A22WE 2007053100160 20070531 00160 NM 2007 5 31 07FDEA01847 1 20070518 A 5753 6521630324 SKIN BOEING 727 727233 138408A NM ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FOUND REPAIR LOCATED AT RT O/B FOREFLAP LWR SURFACE I/B END ON AGING A/C INSP. EXISTING REPAIR DID NOT CONFORM TO CURRE NT SRM 51-40-20. REPAIRED RT O/B FOREFLAP AREA REF SRM 51-40-20 PARA 14-20, 21, 22. 2 L 7 3 4F RT A3WE 2007053100161 20070531 00161 NM 2007 5 31 07FDEA01848 1 20070519 A 5511 65229906 SPAR BOEING 727 7272S2F 1384O81 NM RT STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 RT STAB AFT SPAR 3RD BALANCE BAY FROM O/B END, HINGE PANEL FWD ATTACH BRACKET CRACKED AT I/B END REPLACED CHANNEL AND WE B REF SRM 51-30-3 PG 5. 2 L 7 3 4F A3WE 2007053100163 20070531 00163 NM 2007 5 31 07FDEA01850 1 20070519 A 5755 6521658Y29 ATTACH ANGLE BOEING 727 7272S2F 1384O81 NM NR 3 SPOILER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 LT WING, LWR TE PANEL BELOW NR 3 SPOILER PANEL, INBD SET OF ATTACH ANGLES FOR PANEL SUPPORT ROD OTBD ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE REFERENCING SRM 51-30-2. 2 L 7 3 4F A3WE 2007053100164 20070531 00164 NM 2007 5 31 07FDEA01851 1 20070519 A 5753 651920612 FLAP TRACK BOEING 727 7272S2F 1384O81 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 RT WING TOP SIDE OF I/B FLAP O/B FLAP TRACK AT MOUNT HOLE IS CORRODED RT I/B FLAP TRACK (NR 6) REPLACED. NEW TRACK INST ALLED ON W/C 27X5708-03. 2 L 7 3 4F A3WE 2007053100165 20070531 00165 NM 2007 5 31 07FDEA01852 1 20070519 A 5720 6521658U31 SUPPORT ANGLE BOEING 727 7272S2F 1384O81 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 RT WING OB TE LWR SURFACE PANEL SUPPORT ANGLE CRACKED, 4" FWD OF TE, BELOW OB HINGE OF NR 12 SPOILER REPLACED PANEL SUPP ORT ANGLE REF SRM 51-30-02 PAGE 19. 2 L 7 3 4F A3WE 2007053100167 20070531 00167 NM 2007 5 31 07FDEA01854 1 20070519 A 5512 652065838 PANEL BOEING 727 7272S2F 1384O81 NM ZONE 300 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 RT LOWER I/B PNL NR 9214 IS DAMAGED ON HORIZ STAB. REPAIRED RT HORIZONTAL STAB PANEL NR 9214 REF SRM 55-20-3 FIG 1 AND SRM 55-10-2 PG 1, FIG 1, SHT 1. 2 L 7 3 4F A3WE 2007053100170 20070531 00170 2007 5 31 07FDEA01857 4 20070518 A 3454 751780010005 TRANSPONDER DOUG MD10 MD1010F 3022112 WP NR 2 FAILED A FDEA O OTHER O OTHER CR CRUISE 1 SO 25 569FE 47828 IN CRUISE FLIGHT FL 340 TOWER REPORTED US 400' LOW THEN 600' HIGH WITHIN 3 SECONDS ON XPDR NR 1. SWITCHED TO TRANSPONDE R NR 2, CENTER REPORTED US AS STABLE AT FL 340. REMOVED AND REPLACED NR 1 TRANSPONDER PER EO REF 8-3454-7-5001 AND MM R EF 34-54-00-5. 2 L 7 3 4F RT A22WE 2007053100172 20070531 00172 WP 2007 5 31 07FDEA01949 1 20070523 A 5522 SKIN DOUG DC10 DC1010 3022110 WP LT ELEVATOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 LT INBOARD ELEVATOR FOUND DEEP DENT AND NICK 5.250" BY 2.25" DEEP .080" ON UPPER SKIN. REPAIRED SKIN IAW SRM 55-10-00 V OL 1 FIG 8. 2 L 7 3 4F A22WE 2007053100173 20070531 00173 WP 2007 5 31 07FDEA01950 1 20070523 A 5300 MEMBRANE DOUG DC10 DC1010F 3022111 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 COCKPIT CORROSION CON EXFOLIATION ON MEMBRANE, AND 1 CRACK. 2 L 7 3 4F A22WE 2007053100176 20070531 00176 WP 2007 5 31 07FDEA01953 1 20070523 A 5347 S4929149 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 FS 1184 RBL 107.50 NR 10 SEAT TRACK CORRODED AROUND FASTENER HOLES (LOWER SIDE). REMOVED, FABRICATED AND INSTALLED SEAT TRACK SPLICE IAW DC10 SRM VOLUME I 53-70-00 FIG 1. 2 L 7 3 4F A22WE 2007053100180 20070531 00180 NM 2007 5 31 07FDEA01862 1 20070521 A 5713 ARB2932 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT WING, LEADING EDGE CAVITY STRINGER AT XOS 667 FOUND WITH 0.375 INCH CRACK. [SUP 06-08-07] COMPLIED WITH FEDEX EA 1-5710-111105, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM CHAPTER 6-2-100. 2 L 7 3 4F RT A22WE 2007053100182 20070531 00182 EU 2007 5 31 07FDEA01865 1 20070521 A 5410 FAIRING AIRBUS 310 A310203 3930313 EU NR 1 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 NR 1 PYLON TO NACELLE FILLET FAIRING IS CRACKED LENGTH 2.5 IN LT SIDE STA 683/RIB6. INSTALLED NEW FILLET FAIRING IAW SR M 51-40-21. 2 L 7 2 4F RT A35EU 2007053100183 20070531 00183 EU 2007 5 31 07FDEA01866 1 20070521 A 5730 PANEL AIRBUS 310 A310203 3930313 EU LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 LEFT WING LEADING EDGE LOWER SURFACE ACCESS PANEL 524 EB LAND AREA HAS CRACK LENGTH 1.300 IN WS 1403. FABRICATED DOUBLE RS FROM 6061-T6 .063 AND 6061-T6 .071C IAW SRM 57-41-12, SRM 51-71-30, SRM 51-71-40. LOCATED AND DRILLED IAW SRM 51-40- 44. INSTALLED DOUBLERS IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007053100186 20070531 00186 WP 2007 5 31 07FDEA01562 1 20070424 A 5312 AEA016180 BULKHEAD DOUG MD10 MD1010F 3022112 WP ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 LT MLG WHEEL WELL INT STRUCTURE AT STA 1505 X=31 Z=-42 ON VERTICAL BULKEAD FOUND NR 2 CRACK AFTER STOP DRILL OF OLD REP AIR REPAIR IAW SRM53-00-01 FOG 10 VOL 1. 2 L 7 3 4F RT A22WE 2007053100189 20070531 00189 EU 2007 5 31 07FDEA01864 1 20070521 A 5522 SKIN AIRBUS 310 A310203 3930313 EU LT ELEVATOR DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 LT ELEVATOR L/E 3" FROM I/B EDGE HAS DELAMINATED. REMOVED AND INSTALLED LT ELEVATOR I/B TIP IAW MM 55-24-11-4. REPAIRE D TIP IAW SRM 55-24-11. 2 L 7 2 4F RT A35EU 2007060100001 20070601 00001 NM 2007 6 1 DL76S070601 1 20070525 A 2750 271780123 MODULE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE TE FLAPS FAULTED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 134DL 0235 25123 724143 UPON FLAP RETRACTION AFTER T/O FLAP HANDLE UP IND STUCK AT FLAPS 01. FLAP SLAT ELEC STATUS MSG AFTER APPROX 20 MIN . I ND WENT TO FLAPS UP STATUS MSG GONE. PROBLEM REOCCURRED UPON FLAP RETRACT AFTER LANDING. REPLACED RT M840 MODULE, NO F AULTS PER FIM 27-51-00. 2 L 7 2 4F 4 F RT A1NM E24NE 2007060100010 20070601 00010 NM 2007 6 1 DLM88070610 1 20070527 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 1136-1174 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 EXFOLATION CORROSION ON CUSP WEB BETWEEN STA Y=1136 AND STA Y=1174 TASK CARD 58-53313. REPAIRED DOUBLER IAW SRM 53-05D FIG 835D. 2 L 7 2 4F RT A6WE 2007060100013 20070601 00013 NM 2007 6 1 DLM88070613 1 20070526 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 1221-1231 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 EXFOLIATION CORROSION ON RIGHT CUSP WEB BETWEEN STA Y=1221 AND Y=1231 (TASK CARD 58-53313). REPAIRED PER ERA 398191-14M A REV A. 2 L 7 2 4F RT A6WE 2007060100014 20070601 00014 NM 2007 6 1 DLM88070614 1 20070525 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 589 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 EXFOLIATION CORROSION ON RIGHT CUSP WEB AT SAT Y=589 (TASK CARD 58-53313). REPAIRED PER ERA 398191-14MA REV A. 2 L 7 2 4F RT A6WE 2007060100015 20070601 00015 NM 2007 6 1 DLM88070615 1 20070527 A 5311 FRAME DOUG MD88 MD88 3023688 NM BS 1446 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 REPAIR 3 CRACKS ON CANTED FRAME OUTER CAP. LEFT SIDE 2 CRACKS OF 1/2" LONG AND 1.125" LONG AT L-4L AND ONE 1/2" CRACK A T L-3L. INSTALLED NEW FRAME IAW SRM 53-03D FIG 30. 2 L 7 2 4F RT A6WE 2007060100016 20070601 00016 NM 2007 6 1 DLM88070616 1 20070524 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 542 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CORROSION ON LEFT CUSP WEB AT STA Y=542 (TASK CARD 58-53313). REPAIRED PER ERA 398191-14MA REV A. 2 L 7 2 4F RT A6WE 2007060100017 20070601 00017 NM 2007 6 1 DLM88070617 1 20070523 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 864-886 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CORROSION ON LEFT CUSP WEB BETWEEN STA Y=864 AND Y=886 (TASK CARD 58-53313). REPAIRED PER ERA 398191-14MA REV A. NRC T0 056688 2 L 7 2 4F RT A6WE 2007060100018 20070601 00018 NM 2007 6 1 DL76L070619 1 20070528 A 3240 26124121A BRAKE BOEING 767 767332 1382001 NM NR 7 WORN A DALA O OTHER O OTHER LD LANDING 1 SO 27 198DN 28455 NR 7 BRAKE GETS CONSIDERABLY MORE HOT THAN OTHERS. REMOVED AND REPLACED BRAKE ASSY. FOUND CARBON BRAKE STATORS DETERIO RATED. 2 L 7 2 4F RT A1NM 2007060100019 20070601 00019 NM 2007 6 1 DLM88070620 1 20070527 A 5280 593058311 SKIN DOUG MD88 MD88 3023688 NM LT MLG DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 LT MAIN LANDING GEAR DOOR INNER AND OUTER SKINS CRACKED. CRACKS STOP DRILLED AND REPAIR DOUBLERS WERE INSTALLED. 2 L 7 2 4F RT A6WE 2007060100021 20070601 00021 WP 2007 6 1 07FDEA01958 1 20070524 A 5754 SKIN DOUG DC10 DC1010F 3022111 WP NR 2 SLAT DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RT WING LWR SURFACE FOUND DEEP NICKS ON INT SKIN OF SLAT NR 2. TRIMMED OUT DAMAGED PORTION INT SKIN. INSTALLED FILLER AND REPAIRED DOUBLER IAW SRM 57-00-01 FIG 4 SHT 2 VOL 1. 2 L 7 3 4F A22WE 2007060100023 20070601 00023 NM 2007 6 1 DLM88070622 1 20070529 A 2410 696233B CSD DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE INOPERATIVE A DALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 27 967DL 53116 725532 ON T/O OUT OF MIA, RT ENGINE CSD OIL TEMP HIGH AND RT GENERATOR FAILED, STARTED APU AND COVERED RT BUSS AND THEN GOT APU GEN FAILED 3 MINUTES LATER. FOUND RT CSD OVER SERVICED AND METAL ON CSD CHIP DETECTOR. REMOVED AND REPLACED NR 2 CSD /GEN/AND CSD OIL COOLER AND FLUSHED COOLER LINES. R/R AND CHECKED GOOD PER MM. ALSO, REMOVED AND REPLACED CSD DRIVE SE AL. 2 L 7 2 4F 4 F RT A6WE E9NE 2007060100027 20070601 00027 NM 2007 6 1 DLM88070627 1 20070528 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 1319 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 TEMPORARY REPAIR INSTALLED ON FUSELUGE SKIN AT STA 1319 BETWEEN LONGERONS 22 AND 23 RIGHT. INSTALLED PERM REPAIR PER SR M 53-04D ON N/R T0056053,HMV/GDL. 2 L 7 2 4F RT A6WE 2007060100028 20070601 00028 NM 2007 6 1 DL76P070628 1 20070525 A 5330 143T35217 SKIN BOEING 767 767332 1382001 NM BS 620-654 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1402A 25989 DURING HMV, SEVERAL DENTS, SCRATCHES AND GOUGES WERE FOUND AND REPAIRED FROM STA 620 TO 654, S-26R TO S-33R. 2 L 7 2 4F RT A1NM 2007060100029 20070601 00029 NM 2007 6 1 DL76P070629 1 20070527 A 5330 143T35313 SKIN BOEING 767 767332 1382001 NM BS 1351-1395 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1402A 25989 DURING HMV, SEVERAL DENTS AND GOUGES WERE FOUND AND REPAIRED BETWEEN STA 1351 AND 1395, S-26R TO S-33R. 2 L 7 2 4F RT A1NM 2007060100030 20070601 00030 NM 2007 6 1 DL76L070630 1 20070525 A 5340 148T90442 FITTING BOEING 767 767332 1382001 NM BS 1809 S12R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 178DN 25143 FATIGUE CRACK IN TENSION FITTING COMMON TO 1809.5 CHORD REPLACEMENT. OVERSIZED HOLE, COLD WORKED, INSTALLED OVERSIZED F ASTENER. 2 L 7 2 4F RT A1NM 2007060100031 20070601 00031 NM 2007 6 1 DLM90070355 1 20070423 A 5510 5912481531 FITTING DOUG MD90 MD9030 3023690 NM HORIZONTAL STAB CUT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 905DA 53385 HORIZ STAB TORQUE BOX AFT END CUT BY ELEVATOR CABLE FOUND OFF CABLE RUN PULLEY. REPLACED FITTING IAW BOEING DRAWING 594 0483 AND MD90 SRM 51-10-05. 2 L 7 2 4F RT A6WE 2007060100032 20070601 00032 NM 2007 6 1 DL76G070575 1 20070520 A 2120 VALVE BOEING 767 767332 1382001 NM E/E BAY MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 1609 30574 RTB DUE EQUIPMENT COOLING OVERBOARD VALVE LIGHT ILLUMINATED DID NO GO OUT IN STANDBY. NO DISPATCH ALLOWED BY FCP. LOCK ED VALVE CLOSED AND RELEASED PER MEL. RE-ACTIVATED SYSTEM AND PUT BACK IN AUTO SYSTEM, OPS NML. NO HISTORY. MCO AND P LAC REM. 2 L 7 2 4F RT A1NM 2007060100033 20070601 00033 NM 2007 6 1 DL76S070589 1 20070522 A 2913 290001976 PUMP BOEING 767 767332 1382001 NM RT ENGINE LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 130DL 24080 RT HYD EICAS MSG RT HYDS DROPPED TO .016 THEN R HYD PUMP MSG CAME ON. OPENED UP RT ENG. FOUND RT ENG HYD PUMP LEAKING. SUSPECT ENG HYD PUMP FAILURE. PULLED RT T HANDLE. FOUND EDP CASE SEAM LEAKING. NO METAL IN CASE DRAIN OR PRESSURE F ILTERS. FILTERS REPLACED. REPLACED EDP. ON LEAK CK FOUND PRESSURE HOSE LEAKING. REPLACED PRESSURE HOSE. LEAK CK GOO D. COWLS CLOSED HYDS SERVICED. 2 L 7 2 4F RT A1NM 2007060100034 20070601 00034 NM 2007 6 1 DLM88070590 1 20070524 A 5523 5930497501 TAB DOUG MD88 MD88 3023688 NM LT ELEVATOR DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 DURING CURRENT HMV, TWO DELAMINATED AREAS WERE FOUND ON LHS ELEVATOR ANTI FLOAT TAB BETWEEN 202 AND 216.5. AREA WAS REP AIRED PER BOEING INSTRUCTIONS AS CONTAINED IN 461319-14. 2 L 7 2 4F RT A6WE 2007060100035 20070601 00035 NM 2007 6 1 DL76P070592 1 20070523 A 5551 182T13004 FITTING BOEING 767 767332 1382001 NM HORIZONTAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1402A 25989 DURING HMV, THE RT HORIZ STAB PIVOT FITTING BEARING WAS FOUND ROTATED. UPON REMOVAL, THE FITTING BORE WAS FOUND CORRODE D. FITTING WAS REPAIRED PER BOEING S/B 767-55-0008. 2 L 7 2 4F RT A1NM 2007060100036 20070601 00036 NM 2007 6 1 DLM88070593 1 20070524 A 5753 99359426 SKIN DOUG MD88 MD88 3023688 NM RT TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 THE RHS INBOARD FLAP REMOVALBE PANEL LOWER SKIN REQUIRED A SKIN SPLICE PER 461910-14. 2 L 7 2 4F RT A6WE 2007060100041 20070601 00041 NM 2007 6 1 DLM88070599 1 20070525 A 5280 5930583293 DOOR DOUG MD88 MD88 3023688 NM MLG DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 THE LT MLG DOOR HAD A DAMAGED REPAIR. THE OLD REPAIR WAS REPAIRED WITH A STOP DRILLED AND DOUBLERS ON THE INNER AND OUT ER SKIN. 2 L 7 2 4F RT A6WE 2007060100045 20070601 00045 NM 2007 6 1 DL757070633 1 20070530 A 3240 326002025 BRAKE BOEING 757 757232 1384965 NM NR 5 SEIZED A DALA O OTHER M OVER TEMP TX TAXI/GRND HDL 1 SO 27 699DL 29970 AFTER LANDING NR 5 BRAKE SHOWED 5. AFTER BLOCKED FUSE PLUG BLOWN AND TIRE DEFLATED. ON LANDING AUTO BRAKES WERE SET AT 1 AND USED VERY LIGHTLY. FOUND ASSY SEIZED. REMOVED AND REPLACED NR 5 MAIN BRAKE ASSY LEAK CK OK. REINSTALLED WHEEL ASSY PER M/M. 2 L 7 2 4F RT A2NM 2007060100050 20070601 00050 EA 2007 6 1 SWIA200718269 1 20070501 A 5522 SKIN CNDAIR CL600 CL6002C10 1390015 EA LT ELEVATOR DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 668CA 10162 LEFT ELEVATOR WAS STRUCK BY LIGHTNING ON TRAILING EDGE BETWEEN 9TH AND 10TH RIB, DISCOVERED AT C-CHECK. INSTALLED REPAI R PARTS PER REO 670-55-21-038. 2 L 7 2 4F RT A21EA 2007060100054 20070601 00054 EA 2007 6 1 SWIA200718273 1 20070501 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 668CA 10162 COCKPIT FLOORBEAM AT FS 280 CORRODED, DISCOVERED AT C-CHECK. INSTALLED NEW COCKPIT FLOOR SUPPORT ANGLE P/N:CC670-33292- 13 IAW CRJ700 SRM TASK 51-42-06-001-001-A01. 2 L 7 2 4F RT A21EA 2007060100055 20070601 00055 EA 2007 6 1 SWIA200718274 1 20070501 A 5210 STEP CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 668CA 10162 PAX DOOR UPPER MID STEP IS CRACKED ON FORWARD SIDE, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLES AND DOUBLER PER CRJ7 00 REO 670-52-11-104 AND SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007060100056 20070601 00056 EA 2007 6 1 SWIA200718275 1 20070501 A 5210 STEP CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 668CA 10162 PAX DOOR UPPER MID STEP IS CRACKED ON AFT SIDE, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLES AND DOUBLER PER CRJ700 R EO 670-52-11-104 AND SRM 51-12-06. 2 L 7 2 4F RT A21EA 2007060100058 20070601 00058 EA 2007 6 1 SWIA200718278 1 20070408 A 5310 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 576 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 924SW 7681 FOUND CRACK UNDER CARGO DOOR FRAME AT FS576 AND 474LBL, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS PER REO 601R 53-6 4-1741. 2 L 7 2 4F RT A21EA 2007052900008 20070529 00008 SO 2007 5 29 C2XA07CL047 1 20070522 A 3260 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO MLG MALFUNCTIONED A C2XA O OTHER N FALSE WARNING CL CLIMB 1 SW 27 13989 145271 CLE FLIGHT 2863, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE JUST AFTER ROTATION FOLLOWED BY ENG REV DISAGR EE. ENG REV DISAGREE WENT AWAY AFTER LANDING GEAR WAS EXTENDED. THE AIR/GROUND FAIL MESSAGE WENT AWAY AFTER NOSE WHEEL TOUCHED THE GROUND ON LANDING. MAINTENANCE INSPECTED AND COULD NOT DUPLICATE PROBLEM. FOR PERCAUTIONARY PURPOSES THE NOSE LANDING GEAR WOW PROX SWITCH WAS REPLACED ALONG WITH HARNESS. THE NOSE GEAR WAS SERVICED AND THE AIRCRAFT WAS TEST FLOWN WITH NO DEFECTS. 2 L 7 2 4T RT T00011AT 2007052900011 20070529 00011 NM 2007 5 29 2007UALA01586 1 20070519 A 5310 FRAME AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSLEAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 845UA 1585 ACFT HAS DENTS AT FRAMES 26 & 27 BETWEEN STR 37 AND 42 LT. THERE IS ALSO A SCRATCH APPROX .010 DEEP AT FRAME 28 APPROX 10 INCHES LONG BETWEEN STR 39 AND 42 LT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052900013 20070529 00013 NM 2007 5 29 2007UALA01589 1 20070519 A 5320 SUPPORT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BS 460 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 177UA 24384 FWD CARGO PIT, FWD BULKHEAD PARTITION AND E&E RACK SUPPORT STRUCTURE DAMAGED AT STA 460 CARGO FLOOR LEVEL BETWEEN LBL 5. 5 & LBL 45.5. DAMAGE TO SKIN AND INTERNAL STRUCTURE. [SUP 06-01-07] MAJOR REPAIR ACCOMPLISHED: REMOVED FWD BULKHEAD LOWER SKIN. MFG'D AND INSTALLED NEW SKIN IN FWD CARGO FWD WALL LOWER CLOSEOUT SKIN. REMOVED E&E RACK LOWER WEB SUPPORT. REPAIRED WEB SUPPORT & INSTALLED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052900014 20070529 00014 NM 2007 5 29 2007UALA01590 1 20070519 A 5315 FLOORBEAM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BS 480 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 177UA 24384 FWD CARGO PIT, FLOOR STRUCTURE FRAMES AT STA 480 LBL 45.5 AND STA 480 LBL 24.75 ARE BENT AND HAVE PULLED FASTENERS AFT O F STA 480 WEB. [SUP 06-01-07] MAJOR REPAIR ACCOMPLISHED: REMOVED CLIPS AT BOTH WEBS. MFG'D NEW CLIPS AND WEBS AND BEGA N DRILLING AT BOTH LOCATIONS. INSTALLED MFG'D CLIPS AND WEBS WHILE REPAIRING RAILS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052900015 20070529 00015 2007 5 29 2007UALA01591 4 20070522 A 2565 D30654122U1 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR SLIDE READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 LOW BOTTLE PRESSURE. WATER TESTED FOR 10 MINUTES AND NO LEAK WAS FOUND. REPLACED WITH A STOCK BOTTLE AND TOPPED OFF OL D BOTTLE AND PUT BACK IN STOCK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052900017 20070529 00017 NM 2007 5 29 2007UALA01593 1 20070521 A 2620 BOTTLE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CARGO BAY INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 921UA 25388 CARGO DETECT 2ND BOTTLE ARMED LIGHT INOPERATIVE. REPLACED FIRE BOTTLE AND SQUIB- ALL TESTED NORMALLY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007052900019 20070529 00019 NM 2007 5 29 2007UALA01595 1 20070519 A 5101 UNKNOWN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE UNKNOWN VIBRATION A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 849UA 1649 VERY LIGHT LATERAL AIRFRAME VIBRATION IN CLMB AND CRUISE. GOES AWAY WITH AILERON INPUT. SAMC TEXT: FLT CREW REPORTED NO VIBRATION IN DESCENT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052900021 20070529 00021 2007 5 29 2007UALA01601 4 20070522 A 2565 SLIDE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 937UA 26668 DOOR 1L SLIDE PACK APPEARS TO BE HANGING OUT TOO MUCH. [SUP 05-29-07] REMOVED AND READJUSTED SLIDE PACK. REINSTALLED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007052900022 20070529 00022 NM 2007 5 29 2007UALA01602 1 20070522 A 3350 LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 772UA 26930 EXTERIOR EMERGENCY EXIT LIGHTS ADJACENT TO DOORS 3 LEFT AND 2 RIGHT ARE INOPERATIVE. [SUP 06-06-07] RELAMPED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007052900034 20070529 00034 NM 2007 5 29 2007UALA01615 1 20070322 A 3397 58791 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS SEVERED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 87UA 26713 ALL FIRST CLASS EGRESS STRIP INOPERATIVE. FOUND MAIN POWER FEED SEVERED AT ROW 2AB, REPLACED POWER FEED CABLE. OP CHEC KS OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052900035 20070529 00035 NM 2007 5 29 2007UALA01616 1 20070522 A 2800 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUEL TANK UNKNOWN A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 564UA 26666 DURING FLIGHT CENTER FUEL TANK QTY ROSE FROM 0 TO 1300 AND RIGHT WING DOWN 2K LESS THAN LEFT WING. [06-20-07] AT DISPA TCH TIME, FUELER COULD NOT OPEN RIGHT WING FILL VALVE FOUND RT WING FUEL FILL VALVE STUCK IN THE OPEN POSITION. REPLA CED VALVE AND OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052900036 20070529 00036 NE 2007 5 29 2007UALA01617 2 20070523 A 7261 OIL SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 ENGINE UNKNOWN A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 845UA 1585 V10043 RTFL DUE TO NR 2 ENGINE OIL QUANTITY LOSS INDICATION. [06-22-07] THE TWO OIL QUANTITY TRANSMITTERS REPLACED WERE NO FAULT FOUND. THE MOST LIKELY CAUSE OF THIS EVENT IS RELATED TO A POOR HARNESS CONNECTION AND OVER OIL OVER SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052900037 20070529 00037 EU 2007 5 29 2007UALA01618 1 20070523 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 440UA 702 CORROSION ON DOOR L2 DOOR SILL AT FRAME 68. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052900038 20070529 00038 NM 2007 5 29 2007UALA01619 1 20070523 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FORWARD CARGO DOOR CUTOUT AFT FRAME WEB CRACKED AT LOWER DOOR STOP AT LOWER OUTBOARD CORNER AND IN RADIUS ABOVE LOWER DO OR STOP ON AFT SIDE. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKS & INSTALLED DOUBLER/FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007052900046 20070529 00046 NM 2007 5 29 2007UALA01627 1 20070524 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EEL INOP AT SEAT 4F FWD SECTION. CONNECTOR LOOSE. [SUP 06-06-07] FOUND LOOSE CONTACT, SECURED, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007052900051 20070529 00051 EA 2007 5 29 COMA0760383 1 20070518 A 2751 601R93031 TRANSMITTER CNDAIR CL600 CL6002B19 1900309 EA LT WING TE FLAPS FAULTY A COMA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 931CA 26382 7037 FLIGHT 4939 - RECEIVED FLAP FAIL MESSAGE AFTER LANDING. REPLACED LEFT FLAP POSITION TRANSMITTER. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007052900053 20070529 00053 EA 2007 5 29 COMA0760382 1 20070518 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 931CA 443 7037 FLIGHT 4939 - RECEIVED FLAP FAIL MESSAGE AFTER LANDING. REPLACED PDU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007052900055 20070529 00055 EA 2007 5 29 COMA0760380 1 20070518 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 931CA 13995 7037 FLIGHT 4939 - RECEIVED FLAP FAIL MESSAGE AFTER LANDING. REPLACED LEFT BPSU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007052900057 20070529 00057 SO 2007 5 29 C2XA07SH031 1 20070523 A 5315 14521713605 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13988 145265 SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 20. MX REMOVED AND REPLACED CENTER OMEGA BEAM AT FR 20 IAW E MB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007052900064 20070529 00064 SO 2007 5 29 C2XA07RI034 1 20070519 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 27 16981 145208 FLT - 2319 - EWR - CREW REPORTED BURNING ODOR IN COCKPIT FOR ABOUT 5 SECONDS. NO SMOKE OR MESSAGES NOTICED. EWR MX RAN ENGINES AND PACKS, INSPECTED COCKPIT FOR ODOR AND SMOKE BUT NO SMOKE OR ODOR WAS NOTICED. ALL OPERATIONAL TESTS WERE P ERFORMED SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007052900075 20070529 00075 2007 5 29 SWAA072576 4 20070522 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 241WN 32504 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052900080 20070529 00080 2007 5 29 COMA0760388 4 20070521 A 3418 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 735CA 7267 FLIGHT 5360 - DURING TAKEOFF ROLL RECEIVED A STALL WARNING MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORMED RESET OF THE STALL PROTECTION SYSTEM. 2 L 7 2 4F RT A21EA 2007052900091 20070529 00091 NM 2007 5 29 SWAA072620 1 20070522 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 767 S27L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 767, STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007052900093 20070529 00093 NM 2007 5 29 SWAA072608 1 20070522 A 5310 6549889 DOOR FRAME BOEING 737 7375H4 138449D NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND FWD CARGO DOOR AFT FRAME LOWER STOP FITTING LOWER CHORD CRACKED. REMOVED AND REPLACE D CHORD PER SRM. 2 L 7 2 4F RT A16WE 2007052900097 20070529 00097 NM 2007 5 29 SWAA072600 1 20070522 A 5313 6551698 STRINGER SPLICE BOEING 737 7373L9 1384470 NM BS 355 S28R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 355, STR 28R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007052900098 20070529 00098 NM 2007 5 29 SWAA072618 1 20070522 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM BS 908 S24L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 24L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007052900099 20070529 00099 2007 5 29 SWAA072596 4 20070522 A 2565 6557463 GIRT BAR BOEING 737 7373L9 1384470 NM L1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007052900102 20070529 00102 NM 2007 5 29 SWAA072585 1 20070522 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 907 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052900103 20070529 00103 NM 2007 5 29 SWAA072617 1 20070522 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 380 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052900104 20070529 00104 NM 2007 5 29 SWAA072616 1 20070522 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 360 S5L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052900118 20070529 00118 EU 2007 5 29 YENA2007038 1 20070522 A 2510 80555154501 PRINTER AIRBUS 320 A320232 3930326 EU COCKPIT ODOR A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 15 635JB 4732 2725 FLT 145, BUF-JFK, ELECTRICAL ODOR EMANATING FROM RMP2, ACP2, ATC AREA. FOUND EVIDENCE OF BURNING IN PRINTER PAPER. REM OVED & REPLACED PRINTER PER MM 31-35-22, OPS CHECK NORMAL. ALSO CHECKED RMP'S 1 & 2, ACP'S 1 & 2, ATC AREA, NO EVIDENCE OF BURNING IN THIS AREAS. PERFORMED TSM 24-00-00, OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2007052900120 20070529 00120 NM 2007 5 29 ASAA0741689 1 20070522 A 5315 FLOORBEAM BOEING 737 7374Q8 138447Q NM BS 328 CORRODED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 784AS 28199 FLOORBEAM UPPER CHORD IS CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR STRAP AND TAPERED SHIMS IAW ASA E A 5310 02721. 2 L 7 2 4F RT A16WE 2007052900122 20070529 00122 NM 2007 5 29 ASAA0741691 1 20070522 A 5754 SKIN BOEING 737 7374Q8 138447Q NM NR 4 SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 NR 4 SLAT IS CHAFED AT INBOARD CORNER. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-70- 10. 2 L 7 2 4F RT A16WE 2007052900123 20070529 00123 NM 2007 5 29 ASAA0741692 1 20070522 A 5320 6546579531 STIFFENER BOEING 737 7374Q8 138447Q NM BS 1125 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 APU AIR INLET TORQUE BOX OPENING AFT VERTICAL STIFFENER CORRODED AT FASTENER HOLES. REMOVED CORRODED STIFFENER, FABRICA TED AND INSTALLED STIFFENER IAW SRM 51-30-01 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007052900127 20070529 00127 NM 2007 5 29 SWAA072652 1 20070524 A 3350 20131 BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007052900131 20070529 00131 NM 2007 5 29 SWAA072625 1 20070523 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 205WN 34010 EEPLS COVER MISSING AT ROW 11 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007052900132 20070529 00132 2007 5 29 SWAA072626 4 20070523 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 774SW 27882 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052900135 20070529 00135 2007 5 29 SWAA072650 4 20070524 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 774SW 27882 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052900136 20070529 00136 NM 2007 5 29 SWAA072655 1 20070524 A 5320 6545401 STIFFENER BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED BRDG CHECK, FOUND RIGHT W/W VERTICAL STIFFENER CRACKED AT BS 663.75, RBL 6.15. REPAIRED STIFFENER PER ACO. 2 L 7 2 4F RT A16WE 2007052900138 20070529 00138 EU 2007 5 29 YENA2007036 1 20070520 A 2780 1702286A SENSOR EMB ERJ190 ERJ190100IGW 3260408 EU LT OB SLAT FAILED A YENA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 15 236JB 2486 29 19000035 FLT 907, JFK-ORD, SLAT LO RATE MESSAGE ON EICAS, FIRST APPEARED AFTER TAKEOFF ON FLAP RETRACTION. SLAT FAIL MESSAGE DUR ING FLAP EXTENSION. SLAT FAILED BETWEEN LEVER POSITION TO 0 AND 1. PERFORMED SYSTEM TEST IAW FIM TASK 27-53-00-810-803 A & IAW FIM TASK 27-53-00-804A, SYSTEM OPS CHECKS GOOD, NO DEFECTS NOTED. TSI N236TO1018 TROUBLESHOOTING OF SLAT FAIL A SSIGNED. COMPLIED WITH TSI 236TO1018, REMOVED & REPLACED SLAT SKEW SENSOR LEFT REF AMM 27-83-01, OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A57NM 2007052900144 20070529 00144 NM 2007 5 29 SWAA072643 1 20070523 A 5755 MOUNT BOEING 737 7373H4 1384600 NM NR 5 SPOILER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED SERVICE CHECK, FOUND RIGHT WING NR 5 SPOILER OUTBOARD MOUNT ASSY BROKEN. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007052900146 20070529 00146 NM 2007 5 29 SWAA072662 1 20070524 A 5311 6546543 FRAME BOEING 737 7373L9 1384470 NM BS 706 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007052900151 20070529 00151 NM 2007 5 29 SWAA072659 1 20070524 A 5512 65C25727 SKIN BOEING 737 7373A4 1384585 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED C4 CHECK, FOUND RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 92.70. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007052900152 20070529 00152 NM 2007 5 29 SWAA072661 1 20070524 A 5754 65C26601 SKIN BOEING 737 7375H4 138449D NM NR 2 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED BRDG CHECK, FOUND LEFT WING NR 2 LEADING EDGE SLAT TRAILING EDGE DELAMINATED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007052900154 20070529 00154 NM 2007 5 29 SWAA072629 1 20070523 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007052900158 20070529 00158 NM 2007 5 29 SWAA072636 1 20070523 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500B S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007052900162 20070529 00162 NM 2007 5 29 SWAA072630 1 20070523 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 365 S26R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED HC2 CHECK, FOUND STRINGER 26R CRACKED AT BS 365. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007052900164 20070529 00164 2007 5 29 SWAA072640 4 20070523 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052900165 20070529 00165 2007 5 29 SWAA072628 4 20070523 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052900166 20070529 00166 2007 5 29 SWAA072639 4 20070523 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052900168 20070529 00168 2007 5 29 SWAA072623 4 20070523 A 2565 D31354 SLIDE BOEING 737 737301 1384611 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052900169 20070529 00169 2007 5 29 SWAA072653 4 20070524 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052900170 20070529 00170 2007 5 29 SWAA072638 4 20070523 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007052900172 20070529 00172 NM 2007 5 29 SWAA072633 1 20070523 A 3350 MS155721 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007052900174 20070529 00174 NM 2007 5 29 SWAA072658 1 20070524 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 4 ABC. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007052900177 20070529 00177 NM 2007 5 29 ASAA0741698 1 20070523 A 5311 65C25229100 FRAME BOEING 737 7374Q8 138447Q NM BS 727E CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 FRAME IS CORRODED. REMOVED CORRODED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR SECTION OF FRAME IAW SRM 53-00-07 REPAIR 3. 2 L 7 2 4F RT A16WE 2007052900186 20070529 00186 NM 2007 5 29 KCSA071166 1 20070527 A 5315 FLOORBEAM BOEING 747 747221F 1384868 NM BS 1170 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 CORROSION ON MAIN DECK FLOORBOARD ATTACHMENT BEAM AT BS 1170, LBL-11 TO RBL-11. 2 L 7 4 4F A20WE 2007052900191 20070529 00191 EA 2007 5 29 TRAX200700707 1 20070522 A 5321 PRESSURE PANEL CNDAIR CL600 CL6002B19 1900309 EA BS 526 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 851AS 7360 RT PRESSURE FLOOR HAS CORROSION AT FS 526 FLOOR TO SIDEWALL ATTACH. MARKED BLENDED OUT LIGHT SURFACE CORROSION IAW CRJ 200 SRM 51-21-06. DB 20877. COMPLIED WITH EC/TC REO 601R-53-41-523. 2 L 7 2 4F RT A21EA 2007052900192 20070529 00192 EA 2007 5 29 TRAX200700708 1 20070522 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 851AS 7360 ASD SILL FLOOR SUPPORT ANGLE CORRORED IN SEVERAL PLACES (MARKED). 2 L 7 2 4F RT A21EA 2007060500092 20070605 00092 EA 2007 6 5 TRAX200700709 1 20070522 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 349 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 851AS 7360 FRAME AT FS349 AT STGR 27 CORRODED. REMOVED FRAME AT BS 349, BLENDED CORROSION FROM UNDERSIDE OF FRAME FOUND TO BE O UT OF LIMITS PER SRM, REMOVED INTERCOSTAL AT RT BS 349 AFT TO DOOR FRAME AND REMOVED LT VERT. FRAME AT ELEC. JUCTION B OX. INSTALLED NEW FRAME PER SRM 51-40-11. 2 L 7 2 4F RT A21EA 2007052900194 20070529 00194 EA 2007 5 29 TRAX200700711 1 20070522 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 364 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 851AS 7360 FRAME AT FS 364 AT STGR 27 CORRODED. WORK COMPLETED IN ACCORDANCE WITH CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-21-06, CRJ 200 NDTM 51-20-04, CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-00-00 & IAW CRJ 200 SRM 51-21-11. 2 L 7 2 4F RT A21EA 2007052900195 20070529 00195 EA 2007 5 29 TRAX200700712 1 20070522 A 5310 BEAM CNDAIR CL600 CL6002B19 1900309 EA BS 349 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 851AS 7360 TRANSVERSE BEAM CORRODED AT FS 349 AND RBL 45. 2 L 7 2 4F RT A21EA 2007053000003 20070530 00003 SW 2007 5 30 2007F00034 1 20070509 A 6230 222101497109 LEVER BELL BELL 222 222U 1182140 SW LYC LTS101 LTS101750A1 41560 NE SWASHPLATE LOOSE E O OTHER O OTHER NR NOT REPORTED 1 WP 25 222UT 4236 1785 EA140 47559 ON COLLECTIVE LEVER P/N 222-010-497-109FM, PIN P/N 222-010-456-005 SPUN INSIDE BORE OF COLLECTIVE LEVER PRODUCING A BLAC K GREASE TRAIL ON SWASHPLATE AND LEVER ASSY. PIN IS THERMAL FIT AND PRESSED INTO COLLECTIVE LEVER. THE PIN BORE OF COLLE CTIVE LEVER IS WORN BEYOND ANY SERVICEABLE LIMITS AND UNAIRWORTHY. CAUSE OF FAILURE IS UNKNOWN AT THIS TIME. THERE WERE NO ADVERSE EFFECTS TO FLIGHT AND WAS DISCOVERED DURING A MAJOR INSPECTION PROCESS. 1 G 7 2 3U 3 U H9SW E5NE 2007053000008 20070530 00008 NM 2007 5 30 ASMF20070506 1 20070514 A 4930 388250017 FUEL CONTROL BOEING 757 757200 1384950 NM PWA 2037 PW2037 NE APU FAILED W ASMF O OTHER J WARNING INDICATION CL CLIMB 1 SW 23 703AM 16922 16922 27203 AIRCRAFT AIR TURN BACK, APU FAILED DURING CLIMB AND RT GENERATOR WAS INOPERATIVE. AIRCRAFT LANDED WITH 84367 KG AND MAX IMUM LANDING WEIGHT IS 85811 KG IAW DISPATCH MANUAL 5-3-1/2 NOT REQUIRING OVERWEIGHT LANDING INSPECTION. MAINTENANCE PE RSONNEL REPLACED RT INTEGRATED DRIVE GENERATOR (IDG) IAW MM 24-11-01 AND APU FCU AND SURGE VALVE IAW MM 49-31-01 AND 49- 53-01 RESPECTIVELY, TESTED CORRECT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007053000009 20070530 00009 NM 2007 5 30 ANCF200700010 1 20070501 A 5270 SWITCH DOUG MD80 MD83 3023681 NM PWA JT8 JT8D* NE CARGO DOOR MALFUNCTIONED W ANCF O OTHER N FALSE WARNING LD LANDING 1 SO 23 583AN 53183 MID CARGO DOOR OPEN ANNUNCIATION HAD BEEN ON IN FLIGHT. (EMERGENCY LANDING WAS PERFORMED) IAW AMM 52-31-00 PAG 601 PERF ORMED CHECK MID CARGO DOOR SWITCH. NORMAL OPERATION. 2 L 7 2 4F 4 F RT E2EA 2007053000018 20070530 00018 NM 2007 5 30 ASMF200705001 1 20070501 A 2910 7936907529 LINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE HYD SYSTEM LOOSE W ASMF D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 169PL 53175 AIRCRAFT RETURNED TO PLATFORM, THE LT HYDRAULIC HIGH TEMP LIGHT TURNED ON AND DURING TAXI, THE HYDRAULIC QUANTITY VARIAT ION 17 - 7 QUARTERS. DURING MAINTENANCE CHECK, THE LT HYDRAULIC SYSTEM QUANTITY WAS CHECKED AND DETECTED WITH LOW LEVEL. THE LT HYDRAULIC RESERVOIR WAS RECHARGED IAW MM 12-13-01AND DURING HYDRAULIC LEAK TEST WAS DETECTED MODULES LINE LOOSE. THE MODULES LINE WAS TIGHTEN, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007053000019 20070530 00019 NM 2007 5 30 ASMF200705002 1 20070503 A 2410 696233B CSD DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE RIGHT FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 158PL 76767 1867 49761 AIRCRAFT RETURNED TO PLATFORM, RT GENERATOR OUT OF LINE AFTER ENGINES START. DURING MAINTENANCE CHECK, THE RT GCU WAS RE SEATED, BUT THE FAILURE CONTINUED. THE REPORT WAS DEFERRED IAW MEL 24-1-1 CAT B. DURING OVERNIGHT CHECK, THE RT CSD, GEN ERATOR AND HEAT EXCHANGER WERE REPLACED IAW MM 24-10-01, 24-20-01 AND 24-10-03, RESPECTIVELY, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007053000091 20070530 00091 EA 2007 5 30 200714802 1 20070526 A 3241 6007302 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA ANTI SKID SYS FAILED A SIMA O OTHER O OTHER LD LANDING 1 SW 21 510AE 10173 10173 10105 ANTI-SKID INOP ON LANDING. REMOVED ANTI-SKID CONTROL UNIT. OPERATIONAL CHECKS GOOD IAW CRJ AMM. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007053000092 20070530 00092 EU 2007 5 30 200714801 1 20070525 A 2600 UNKNOWN SAAB SF340 340B 7860101 EU TAIL PIPE WARNIN UNKNOWN A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 904AE 340B314 DURING TAKEOFF, GOT RIGHT ENGINE TAIL PIPE HOT WARNING LIGHT. RETURNED TO GATE. INSPECTED RIGHT ENGINE TAIL PIPE FIRE DETECTORS AND CONNECTIONS NO DEFECTS FOUND IAW SAAB AMM. PERFORMED ENGINE RUNS AND OPERATIONAL CHECKS OF FIRE DETECTION SYSTEM IAW SAAB AMM. NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007053000093 20070530 00093 SO 2007 5 30 200714803 1 20070524 A 4930 4504205E FADEC EMB 145 EMB145LR 3260212 SO APU FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 699AE 1731 583 14500883 APU IN OPERATION TO COMPLY WITH MEL 24-5. APU FAILED DURING CLIMB-OUT. REPLACED APU FADEC. OPERATIONAL CHECKS GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007053000094 20070530 00094 NM 2007 5 30 07FDEA01665 1 20070430 A 5754 ARC40081 HINGE FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 LT WING OUTBD FLAP INBD HINGE SUPPORT FITTING OUTBD AND 1 BOLT HOLE FOUND CORROSION. LT WING OUTBD FLAP REMOVED AND R EPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-1110 94 - WINGS, LT WING OUTBD FLAP CONVERSION FROM SR11570026-7001 TO D10-57-010-505SR HAS BEEN COMPLIED WITH. REFER TO SNR M N00732 FOR FURTHER WORK DETAILS. 2 L 7 3 4F RT A22WE 2007053000136 20070530 00136 NM 2007 5 30 AWXA200700656 1 20070522 A 3350 1012721 LAMP BOEING 737 7373G7 1384595 NM EMERGENCY LIGHTS SHORTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 157AW 23779 PHX - EEL - EMERGENCY EXIT LIGHTS ARE INOPERATIVE AT SEAT ROWS 8, 12, 13, 14, 15, 16 AND 17. REPLACED AND OPERATIONAL C HECKED LAMP ASSEMBLY AT SEAT ROW 13 IAW AWA TASK CARD A1C33008. 2 L 7 2 4F RT A16WE 2007053000137 20070530 00137 2007 5 30 DLM90070579 4 20070521 A 2565 LANYARD DOUG MD90 MD9030 3023690 NM AFT STAIR SLIDE OUT OF ADJUST A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 WHEN TAILCONE INADVERTENTLY DEPLOYED SLIDE DID NOT DEPLOY. FOUND THAT ONE OF THE FLOOR MOUNTED ATTACH POINTS FOR THE LA NYARD WAS INCORRECTLY ADJUSTED. ADJUSTED ATTACH POINT AS REQUIRED. 2 L 7 2 4F RT A6WE 2007053000138 20070530 00138 NM 2007 5 30 DL76P070580 1 20070426 A 5330 146T3261 SKIN BOEING 767 767332 1382001 NM BS 1197 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1402A 25989 DURING HMV2 AT BFM, FOUND LT LOWER EXTERNAL FUSELAGE AT STA 1197+ 22 STR 37L DENTED. OUT OF LIMITS PER SRM 53-00-01. R EPAIRED PER SRM 53-00-01 REPAIR 12. 2 L 7 2 4F RT A1NM 2007053000139 20070530 00139 NM 2007 5 30 DL76G070583 1 20070521 A 2730 162000105 COMPUTER BOEING 767 767332 1382001 NM ELEVATOR FEEL MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 171DZ 29690 ELEV FEEL EICAS MSG ON TAXI OUT. REMOVED AND REPLACED ELEVATOR FEEL COMPUTER PER AMM. LEAK CHKS GOOD. OPS CHK GOOD PE R AMM. PART INSTALLED IS AMERICAN AIRLINES PART S/N 403 P/N 162000-105. 2 L 7 2 4F RT A1NM 2007053000140 20070530 00140 2007 5 30 DL764070584 4 20070521 A 3417 10615 TRANSFORMER BOEING 767 767432ER 1385134 NM ADC INTERMITTENT A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 836MH 29709 RIGHT AIR DATA COMPUTER INTERMITTENT, CYCLES ON/OFF EVERY 20 SECONDS, EICAS MESSAGE RT AIR DATA. TROUBLE SHOT PER FIMM 34-26-00 CKD PIN 6 ON LT CTR AND RT ADIRUS. REPLACED TRANSFORMER T140, PERFORMED OPS CK ON RT ADIRU. ALL CKS NORMAL 2 L 7 2 4F RT A1NM 2007053000141 20070530 00141 NM 2007 5 30 DL76P070585 1 20070424 A 5315 BAC15063123 FLOORBEAM BOEING 767 767332 1382001 NM STA 740 LBL29-46 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1402A 25989 DURING HMV2 AT MAE, FOUND FWD CARGO COMPARTMENT BILGE AREA STA 740 LBL 29-46 FLOOR PANEL SUPPORT ANGLE CORRODED. REPAIR ED PER SRM 53-00-07 REPAIR 4. 2 L 7 2 4F RT A1NM 2007053000142 20070530 00142 NM 2007 5 30 DL764070587 1 20070422 A 3350 LIGHT BOEING 767 767432ER 1385134 NM CABIN CONTAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 828MH 29699 R2 DOOR EXTERIOR EMERGENCY LIGHT HAS WATER BEHIND LENSE. CLEANED AND REPAIRED INTERNAL LIGHT ASSY PER CMM 33-51-26. EM ERGENCY LIGHT CHECKS GOOD PER DELTA B767 AMM 33-51-06. 2 L 7 2 4F RT A1NM 2007053000143 20070530 00143 NM 2007 5 30 DL76G070588 1 20070522 A 2131 211738813 CONTROLLER BOEING 767 767332 1382001 NM CABIN PRESSURE MALFUNCTIONED A DALA D RETURN TO BLOCK G MULTIPLE FAILURE TX TAXI/GRND HDL 1 SO 27 1607B 30388 CABIN ALT AUTO 1 AND AUTO 2 INOP. FOUND CONTROLLER FAULT. NO RESET. REPLACED NR 2 CABIN PRESS CONTROLLER. BITE CHECK GOOD. 2 L 7 2 4F RT A1NM 2007053000144 20070530 00144 EU 2007 5 30 AWXA200700675 1 20070522 A 5320 D53480020437 SHEAR PLATE AIRBUS 320 A320232 3930326 EU ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 603AW 661 SAL - CRACK ON SHEAR SHEET, FR 68 TO FR 69, -Y1732. REPLACED SHEAR SHEET, FR 68 TO FR 69, -Y1732 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007053000145 20070530 00145 EU 2007 5 30 AWXA200700676 1 20070523 A 5320 D53480043202 SILL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 603AW 661 SAL - CORROSION ON L2 DOOR CUT OUT LOWER SILL, FR 68 + 16", +Y1732. REPAIRED L2 DOOR CUT OUT LOWER SILL, FR 68 + 16", + Y1732 IAW A320 SRM 53-41-14. 2 L 7 2 4F RT A28NM 2007053000146 20070530 00146 NM 2007 5 30 AWXA200700677 1 20070521 A 5210 D5311245600100 FITTING AIRBUS A319 A319132 3930340 NM ZONE 800 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 804AW 1043 SAL - R1 DOOR UPPER SUPPORT ARM FITTING WORN CAUSING BEARING TO MIGRATE OUT OF THE FITTING. REPLACED R1 DOOR UPPER SUPP ORT ARM FITTING IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007053000147 20070530 00147 EU 2007 5 30 AWXA200700678 1 20070520 A 5320 D53471124200 SHEAR PLATE AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 603AW 661 SAL - CORROSION ON CABIN SHEAR PLATE , +Y1732, FR 69 - FR 70. REPLACED CABIN SHEAR PLATE , +Y1732, FR 69 - FR 70 IAW A3 20 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007053000170 20070530 00170 WP 2007 5 30 IXXA07SMN143S 1 20070421 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND EXTERNAL FUSELAGE NOSE SECTION RIGHT AFT PRIMARY HEAT INTERCHANGER AFT LOWER CO RNER DOUBLER CRACKED AT STATION -12 LONGERON 27 RIGHT. REMOVED EXISTING REPAIR. FABRICATED REPAIR DOUBLER. CLEANED TR EATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACE. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D , DC8 MM 53-30-09 PAGES 201, 202, 206 AND 209, DC8 SRM 51-1-8B, DC8 SRM 51-1-11,DC8 SRM 51-1-20D, AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007053000171 20070530 00171 NM 2007 5 30 TSAA0753024 1 20070514 A 5512 65505781 SPAR BOEING 737 737230 1384401 NM HORIZONTAL STAB CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 823AL 23154 FOUND CORROSION HAS BEEN IDENTIFIED ON THE LEFT HORIZONTAL STABILIZER AT LOCATION STAB STA 230.7. [SUP 06-01-07] THE H ORIZONTAL STABILIZER WAS REMOVED AND REPLACED IN ACCORDANCE WITH AMM 27-41-11. THE AIRCRAFT WAS RETURNED TO SERVICE ON M AY 31, 2007. 2 L 7 2 4F RT A16WE 2007053000172 20070530 00172 NM 2007 5 30 TSAA0753023 1 20070514 A 5330 654581948 SKIN BOEING 737 737230 1384401 NM BS 243 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 823AL 23154 CRACK HAS BEEN DISCOVERED ON WALK-AROUND IN NOSE WHEEL WELL APPROXIMATELY BS 243, INBOARD AND AFT OF LEFT UPPER PRESSURE PANEL. [SUP 06-01-07] ECO 3194 R2 WAS ACCOMPLISHED AS A PERMANENT REPAIR. AIRCRAFT WAS RETURNED TO SERVICE ON MAY 31 , 2007 2 L 7 2 4F RT A16WE 2007053000173 20070530 00173 NM 2007 5 30 TSAA0780022 1 20070513 A 8000 GP043102 SWITCH BOEING 737 73776N 13844CH NM STARTER MALFUNCTIONED A TSAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 740AL 28640 FLIGHT 473 OAK-OGG, AFTER PUSH-BACK WHEN THE NR 1 ENGINE START SWITCH WAS PLACED IN THE GROUND POSITION, THE SWITCH DID NOT LOCK IN POSITION. THE CREW DECIDED TO RETURN TO THE GATE. MAINTENANCE PERFORMED FIM TASK 80-07-00 AND STARTED ENGI NE WITH NO FAULTS FOUND. START SWITCH OPERATED NORMALLY. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007053000174 20070530 00174 WP 2007 5 30 IXXA07SMN142S 1 20070421 A 5330 SKIN DOUG DC8 DC871F 302199D WP ZONE 200 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR LOCATED AT FS 1725 LONGERON 16.5 RIGHT. REMOVED EXISTING REPAI R. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS . APPLIED SEALANT TO FAYING SURFACE. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-1 FIGURE 7 SHEET 1, 3 AND 5, DC8 SRM 51-1 -20D, DC8 SRM 53-2-1 FIGURE 7 SHEET 1, 3 AND 5, DC8 SRM 53-5-1 FIGURE 1 ITEM "D", DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007053000175 20070530 00175 EU 2007 5 30 MALA070060 1 20070503 A 2720 SWITCH SAAB SF340 340B 7860101 EU YAW TRIM FAILED A MALA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 15 433XJ 340B433 YAW TRIM DEFLECTED FULL RIGHT ON TAKEOFF. CREW INITIATED A LOW ENERGY ABORT. VERIFIED STICKING TRIM SWITCH. REPLACED SWITCH IAW SAAB AMM CH 27-22-05, REF 409 CARD NR 301910 FOR DETAILS. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2007053000176 20070530 00176 EA 2007 5 30 TRAX200700719 1 20070524 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 976EV 7601 CARGO COMPARTMENT NET SUPPORT HAS CRACKED ANGLE AT FS 621.00. [07-24-07] REMOVED CARGO COMPARTMENT NET SUPPORT ANGLE AT FS 621.00 IAW CRJ 200 SRM 51-42-13. DUPLICATED FROM 2024-T3, .050 IAW CRJ 200 SRM 53-61-23. OK TO ALODINE, PRIME, AN D PAINT. ALODINED, PRIMED, AND PAINTED IAW CRJ SRM 51-25-16. OK TO INSTALL. INSTALLED ANGLE IAW CRJ SRM 51-42-21. REQUIR ES LEAK CHECK. LEAK CHECK GOOD IAW CRJ AMM 21-30-00. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2007053000177 20070530 00177 EA 2007 5 30 TRAX200700713 1 20070522 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 875AS 7559 SERVICE DOOR WON'T CLOSE PROPERLY. 2 L 7 2 4F RT A21EA 2007053000178 20070530 00178 NM 2007 5 30 CALA0700261 1 20070525 A 3350 ADD71701100 BATTERY PACK BOEING 737 737824 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 26210 28770 THE FIRST CLASS EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-06 . 2 L 7 2 4F RT A16WE 2007053000179 20070530 00179 NM 2007 5 30 CALA0700262 1 20070524 A 5322 6545806 SHEAR TIE BOEING 737 7373T0 1384582 NM BS 275 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND RIGHT NLG WW CHORD SHEAR TIE CORRODED AT STA 275, S25R-S26R. A SHEAR TIE FILLER REPAIR WAS INSTALLED I AW SRM 53-00-07. 2 L 7 2 4F RT A16WE 2007053000180 20070530 00180 NM 2007 5 30 CALA0700263 1 20070524 A 5330 148W4305 SKIN BOEING 777 777224 1385225 NM BS 2344-2370 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 78009 29479 INSPECTION FOUND SKIN CORRODED AT BS 2344-2370, S38R-S43R (TAIL COMPARTMENT AREA). THE SKIN WAS REPAIRED IAW SRM 53-00- 01, REPAIR 7, FIGURE 202. 2 L 7 2 4F RT T00001SE 2007053000181 20070530 00181 NM 2007 5 30 CALA0700264 1 20070524 A 5330 148W4912 SKIN BOEING 777 777224 1385225 NM BS 2272 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 78009 29479 INSPECTION FOUND A .5 INCH CRACK IN RIGHT LOWER SEAL FAIRING SKIN AT BS 2272, S26R. THE SKIN WAS REPAIRED IAW SRM 53-80 -70, REPAIR 1, FIGURE 204. 2 L 7 2 4F RT T00001SE 2007053000182 20070530 00182 NM 2007 5 30 CALA0700265 1 20070525 A 5322 6545806 SHEAR TIE BOEING 737 7373T0 1384582 NM BS 285 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND RIGHT NLG WW SHEAR TIE CORRODED AT STA 285. A REPAIR WAS INSTALLED IAW SRM 53-00-07. 2 L 7 2 4F RT A16WE 2007053000183 20070530 00183 NM 2007 5 30 UPS07449812 1 20070513 A 5510 SPAR BOEING 747 747123 1384873 NM DAMAGED BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:C RIGHT HORIZONTAL STABILIZER UPPER REAR SPAR AND SPLICE PLATE INSP BROKEN BOLTS INDICATION REVEALED ON BOLT 6 & 29. RIGHT HORIZONTAL STAB UPPER REAR SPAR AND SPLICE PLATE BROKEN BOLTS 6 & 29 POSITION REPLACED (BOLTS P/N ON :BACB30US6K17 & BACB30US7K20) WITH NON-MAGNETIC TYPE BOLTS PER B747-5510-16378-G APP 'D'. 2 L 7 4 4F A20WE 2007053000184 20070530 00184 NM 2007 5 30 UPS07649857 1 20070528 A 2560 INERTIA REEL BOEING 767 76734AF 1385212 NM COCKPIT BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 316UP 27744 INSPECTION TYPE:ETOP TIE DOWN INERTIA REEL NEXT TO 1ST OBSERVERS SEAT BROKEN. REMOVED AND REPLACED INERTIA REEL IN COCK PIT, REF B767 MM 25-10. 2 L 7 2 4F RT A1NM 2007053000185 20070530 00185 WP 2007 5 30 UPS07849854 1 20070513 A 5320 STIFFENER DOUG DC8 DC873F 302199F WP FS 857 RBL 60 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C2 STIFFENER IN RT WHEEL WELL STA 857 HAS EXFOLIATION CORROSION. REMOVED STIFFENER AT STA 857 RT WHEEL WELL IAW SRM 51-1-21. FABRICATE AND INSTALLED STIFFENER AT STA 857 RT WHEEL WELL IAW DWG 5613917-19 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007053000186 20070530 00186 WP 2007 5 30 UPS07849855 1 20070520 A 5330 5615374187 SKIN DOUG DC8 DC873F 302199F WP FS 1640 L33R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C3 EXFOLIATED CORROSION UNDER L33R AT STA 1620. REPAIRED SKIN AND FINGER DOUBLER AT STA 1620 L33R IAW S AA EA 008- 5330-00-A0885, UPS RAA DC8-53-20632, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007053000187 20070530 00187 NM 2007 5 30 ABXA070170 1 20070429 A 5340 D067205 FITTING BOEING 767 767205 1385121 NM CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 23058 FORWARD LOWER CARGO DOOR JAMB AFT SILL MOUNTED BASE FITTING WAS CRACKED. REMOVED AND REPLACED FORWARD LOWER CARGO DOOR JAMB AFT SILL MOUNTED BASE SIDE GUIDE RAIL IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007053000188 20070530 00188 WP 2007 5 30 ABXA070166 1 20070510 A 5320 5956034523 FLOOR SUPPORT DOUG DC9 DC941 302207N WP BS 1056-1072 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 951AX 47616 LEFT FLOOR TRACK END FITTING/CLIP CRACKED AND ATTACHING INTERCOSTAL WAS CORRODED UNDER NUT PLATES, STA 1056 - 1072, LONG ERON 27 - 28 LEFT. REMOVED AND REPLACED INTERCOSTAL IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 2007053000189 20070530 00189 WP 2007 5 30 ABXA070167 1 20070510 A 5320 99579123 INTERCOSTAL DOUG DC9 DC941 302207N WP BS 427-446 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 951AX 47616 FRAME BETWEEN STA 427 AND 446 CRACKED AT APPROXIMATELY 435. REMOVED AND REPLACED INTERCOSTAL IAW DC9 SRM. 2 L 7 2 4F A6WE 2007053000190 20070530 00190 NM 2007 5 30 ABXA070168 1 20070424 A 5230 140T26033 BEAM BOEING 767 767205 1385121 NM AFT CARGO DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 23058 HORIZONTAL BEAM ON AFT CARGO DOOR HAD CORROSION AROUND 1 NUT PLATE JUST AFT OF CENTER OF BEAM. REPAIRED AFT LOWER CARGO DOOR BEAM CORROSION IAW B767 SRM 51-70-12. 2 L 7 2 4F RT A1NM 2007053000191 20070530 00191 NM 2007 5 30 ABXA070172 1 20070504 A 5320 96FS6677068AX INTERCOSTAL BOEING 767 767205 1385121 NM BS 368 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 23058 LEVEL I CORROSION ON SUBFLOOR STRUCTURES AT FLOORBEAM BS 368 AND 9G ATTACH POINT CUTOUTS. REMOVED AND REPLACED FITTING IAW B767 SRM 51-10-02. 2 L 7 2 4F RT A1NM 2007053000192 20070530 00192 NM 2007 5 30 ABXA070171 1 20070429 A 5310 D067205AX FITTING BOEING 767 767205 1385121 NM CARGO DOORWAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 23058 AFT LOWER CARGO DOOR JAMB FORWARD SILL MOUNTED BASE FITTING CRACKED. REMOVED AND REPLACED FITTING IAW B767 SRM 51-40-02 . 2 L 7 2 4F RT A1NM 2007053000193 20070530 00193 NM 2007 5 30 ABXA070173 1 20070507 A 5410 313T3380227 DOUBLER BOEING 767 767205 1385121 NM NR 2 NACELLE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 23058 NR 2 PYLON INTERIOR DOUBLER CRACKED AT AFT LOWER EDGE OF OUTBOARD STRUT DOOR. REMOVED AND REPLACED DOUBLER IAW B767 SRM . 2 L 7 2 4F RT A1NM 2007053000194 20070530 00194 WP 2007 5 30 ABXA070165 1 20070508 A 5320 595591158 ANGLE DOUG DC9 DC941 302207N WP FUSLEAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 951AX 47616 THE TEE ANGLE CRACKED, FORWARD DOOR JAMB, INBOARD MOUNT. REMOVED AND REPLACED TEE ANGLE IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2007053000195 20070530 00195 NM 2007 5 30 ABXA070169 1 20070426 A 5410 313T336075 STRUT BOEING 767 767205 1385121 NM NR 2 NACELLE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 23058 INTERIOR STRUCTURE CRACKED STRUT TRAILING EDGE ASSEMBLY 447DB. REMOVED AND REPLACED CRACKED STRUCTURE IAW B767 SRM. 2 L 7 2 4F RT A1NM 2007053000196 20070530 00196 EA 2007 5 30 COMA0760391 1 20070522 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FS 559 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 940CA 30857 7048 DURING FS 559 INSPECTION FOUND CRACK AT LOWER END OF VERTICAL STIFFENER, FS 559, RBL 27, INBOARD SIDE. CUT OUT DAMAGE A ND INSTALLED DOUBLER IAW CRJ REO 601R-53-41-283. 2 L 7 2 4F RT A21EA 2007053000197 20070530 00197 EA 2007 5 30 COMA0760400 1 20070526 A 3150 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 816CA 7398 FLIGHT 5013 - ANTI-ICE DUCT WARNING MESSAGE IN FLIGHT, SYNOPTIC PAGE INDICATED LEFT FUSELAGE DUCT. AIRCRAFT DIVERTED TO AVP AND LANDED SAFELY. PERFORMED OPS CHECK OF BLEED LEAK DETECTION AND WARNING SYSTEM, NO DEFECTS NOTED. GROUND RAN A IRCRAFT, ALL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007053000198 20070530 00198 EA 2007 5 30 COMA0760392 1 20070522 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FS 559 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 940CA 30857 7048 DURING FS 559 INSPECTION FOUND CRACK AT SEMI-PRESSURE BULKHEAD, FS 559, RBL 9, WL 54.1. STOP DRILLED CRACK AND INSTALLE D TEMPORARY DOUBLER PER CRJ REO 601R-53-41-353. 2 L 7 2 4F RT A21EA 2007053000199 20070530 00199 EA 2007 5 30 COMA0760394 1 20070523 A 3260 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA MLG FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 804CA 12441 7352 FLIGHT 5417 - AFTER TAKEOFF RECEIVED GEAR DISAGREE WARNING, AND SHORTLY AFTER, HYDRAULIC OVERTEMP SYSTEM 3 CAUTION. DEC LARED EMERGENCY AND LANDED WITHOUT INCIDENT. TROUBLESHOT PROBLEM TO PSEU. REPLACED PSEU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007053100001 20070531 00001 EU 2007 5 31 UPS07149862 1 20070525 A 3350 CM82400 BULB AIRBUS A300 A300F4622R 3930360 EU EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 125UP 0809 FWD ENTRY DOOR EXIT SIGN MODULE LOWER 2 BULBS ARE INOP. BULBS REPLACED. OP TEST PERFORMED IAW 33-51-13-04. TEST OK. 2 L 7 2 4F RT A35EU 2007053100011 20070531 00011 SO 2007 5 31 C2XA07IA121 1 20070523 A 3320 7287503507 LIGHT EMB 135 EMB135LR 3260305 SO CABIN BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 27 11526 145410 IAH - FLIGHT 2008, THE CREW REPORTED AN ELECTRICAL BURNING ODOR IN THE COCKPIT ON DESCENT, AN EMEREGENCY WAS DECLARED, A ND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE SIDEWAL L LIGHT AT SEAT 7A. OPERATIONAL CHECKS WERE PERFORMED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN T O SERVICE. 2 L 7 2 4F RT T00011AT 2007053100015 20070531 00015 NM 2007 5 31 ASAA0741717 1 20070530 A 5330 65C329541 SKIN BOEING 737 7374Q8 138447Q NM BS 820-832 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 FUSELAGE SKIN SCRATCHED AND DENTED. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW ASA EA 5330 02212. 2 L 7 2 4F RT A16WE 2007053100017 20070531 00017 WP 2007 5 31 ASAA0781719 1 20070530 A 5320 993634139 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP BS 160-218 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 PASSENGER CABIN FLOOR SUPPORT IS CORRODED. FABRICATED AND INSTALLED A REPLACEMENT FLOOR SUPPORT IAW SRM 51-10-4 PG 1 AN D 51-30-1 PARA 1 AND PARA 11. 2 L 7 2 4F RT A6WE 2007053100022 20070531 00022 WP 2007 5 31 ASAA0781724 1 20070530 A 5321 9936640501 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 886-927 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 CABIN FLOOR PANEL DELAMINATED. FABRICATED REPLACEMENT FLOOR PANEL IAW SRM 53-05 PG 122B FIGURES 50 AND 50A AND DCA DWG 9936640. 2 L 7 2 4F RT A6WE 2007053100023 20070531 00023 NM 2007 5 31 ZZDA070523164 1 20070523 A 5310 DOOR FRAME BOEING 717 717200 1383700 NM CARGO DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 953AT 55015 CORROSION ON AFT CARGO COMPARTMENT LOWER JAMB AREA. CUT OUT DAMAGED SECTION OF LOWER JAMB AREA, AND INSTALLED NEW SECTI ON P/N J060228-9 WITH 2EA SPLICES, INSTALLED ON FWD AND AFT SECTION, MATERIAL USED .040 T075-0, HEAT TREATED TO T-6 AND INSTALLED IAW B 717 SRM 53-20-15 FIG 201. 2 L 7 2 4F TR A6WE 2007052900183 20070529 00183 CE 2007 5 29 BSAASDR0710 1 20070430 A 2130 12938000113 BYPASS VALVE BEECH 1900 1900D 1154162 CE MALFUNCTIONED A BSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 05 165YV UE165 INITIAL REPORT - DURING CLIMB, THE RIGHT ENVIR FAIL LIGHT CAME ON, CREW RETURNED TO STATION WITH NO FURTHER INCIDENT. INITIALLY DEFERRED PER MEL 21-4. THE PRECOOLER BYPASS VALVE AND THE PRESSURE REGULATOR VALVE WERE REMOVED AND REPLACED. SYSTEM OPERATIONALLY CHECKED GOOD. 2 L 7 2 4T RT A24CE 2007052900185 20070529 00185 CE 2007 5 29 BSAASDR0714 1 20070516 A 2612 24412886 FIRE LOOP BEECH 1900 1900D 1154162 CE RT NACELLE FALSE INDICATION A BSAA O OTHER N FALSE WARNING DE DESCENT 1 NM 05 171ZV UE171 RIGHT FIRE LOOP ANNUNCIATOR ILLUMINATED WHEN VECTORED TO FINAL (DESCENT) INTO BOSTON. CREW LANDED WITHOUT INCIDENT. TH E RIGHT FORWARD ENGINE FIRE LOOP WAS REMOVED AND REPLACED, AND AN OPERATIONAL CHECK ON THE SYSTEM WAS PERFORMED. 2 L 7 2 4T RT A24CE 2007052900188 20070529 00188 EA 2007 5 29 TRAX200700704 1 20070521 A 1100 SIGN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 EXIT ARROW AT PAX DOOR ENTRANCE WORN. 2 L 7 2 4F RT A21EA 2007053000148 20070530 00148 EU 2007 5 30 AWXA200700679 1 20070520 A 5320 D53480020436 SHEAR PLATE AIRBUS 320 A320232 3930326 EU ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 603AW 661 SAL - MAJOR REPAIR - CRACKED CABIN SHEAR SHEET (TRAY), FR 68, +Y1314. REPLACED CABIN SHEAR SHEET (TRAY), FR 68, +Y1314 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007053000149 20070530 00149 NM 2007 5 30 AWXA200700652 1 20070521 A 3397 BMS13311122 WIRE BOEING 757 7572G7 1384963 NM CABIN LIGHTS BURNED A AWXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 28 909AW 24522 PHX - SMOKE - 7763452 - WHILE TROUBLE SHOOTING FORWARD LAV AND THRESHOLD LIGHTING ISSUES, MX DISCOVERED ARCED WIRING AT ROW 4 OVERHEAD AREA NEXT TO THE NR 2 VIDEO MONITOR. MX COMPLIED WITH ER 19-2335-07142-KK1 FOR ARCED WIRING. SYSTEM OPE RATIONAL CHECKS WERE GOOD PER AMM 33-25-00, 33-26-00, 33-24-00, 38-32-00, 38-13-51-4, 33-51-00-5 AND T/C A1B23604. THE A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007053000150 20070530 00150 WP 2007 5 30 AALA20070939 1 20070524 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7550 53032 ORD - EMERGENCY LIGHT ANNUNCIATOR RIGHT LAMP INOPERATIVE. RELAMPED EMERGENCY LIGHT ANNUNCIATOR RIGHT HAND LAMP. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007053000151 20070530 00151 WP 2007 5 30 AALA20070938 1 20070524 A 3350 P4010051111 MODULE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 573AA 53092 LGA - EMERGENCY AISLE PATH LIGHT AT AFT SERVICE DOOR INOPERATIVE. REPLACED BATTERY MODULE FOR EMERGENCY AISLE PATH LIGH T AT AFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007053000152 20070530 00152 NM 2007 5 30 QXEA200700834 1 20070510 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - SURFACE AND PITTING CORROSION ON FLANGES AND UPPER LIP AND INNER CHANNEL OF RIGHT CENTER SEAT TRACK NR 11 FROM STATION 12.0 TO 70.0. REPAIRED IAW SRM 51-40-07, 51-42-05, 51-40-10, AND RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007053000153 20070530 00153 NM 2007 5 30 QXEA200700838 1 20070511 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 780 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 C4 PDX - PITTING AT RIGHT CENTER SEAT TRACK NR 16 AT STATION 780. REPAIRED IAW RD8/4-53-884, AND SRM 51-40-07, 51-21-10 . 2 H 7 2 4T RT A13NM 2007053000154 20070530 00154 NM 2007 5 30 AALA20070941 1 20070525 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 761AJ 31478 LHR - EMERGENCY LIGHT AT FIRST CLASS CLOSET FLOOR HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT FIRST CLASS CLO SET FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007053000155 20070530 00155 NM 2007 5 30 AALA20070940 1 20070524 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 957AN 29541 MIA - EMERGENCY LIGHT AT SEAT 13D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007053000156 20070530 00156 NE 2007 5 30 AALA20070937 2 20070524 A 7230 BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE COMPRESSOR FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 298AA 49310 718577 ORD INFLIGHT T366/24MAY - RETURNED ORD DUE TO CREW REPORTING LOUD BANG DURING CLIMB AND RIGHT ENGINE GAS TEMPERATURE OV ER 800C. LANDED ORD WITHOUT INCIDENT. SINGLE ENGINE TIME 13 MINUTES. REPLACED NUMBER TWO ENGINE ON 24 MAY AT ORD DUE TO COMPRESSOR BLADE FAILURE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007053000157 20070530 00157 WP 2007 5 30 07FDEA01769 1 20070514 A 5320 ANGLE DOUG DC10 DC1010F 3022111 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 AFT CARGO COMPT BILGE ON CAP ANGLES FOUND LIGHT SURFACE CORROSION. REPAIRED IAW SRM 53-30-00 VOL 1 FIG 9. 2 L 7 3 4F A22WE 2007053000158 20070530 00158 WP 2007 5 30 07FDEA01771 1 20070514 A 5310 DOOR FRAME DOUG DC10 DC1010 3022110 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 MAIN CABIN CRACK LONG .25" ON WEB. REPAIRED JAMB WEB IAW SRM 53-50-00 VOL 1 FIG 19 SHT 2. 2 L 7 3 4F A22WE 2007053000159 20070530 00159 WP 2007 5 30 07FDEA01773 1 20070514 A 5730 SKIN DOUG DC10 DC1010 3022110 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 LT WING LOWER EXT SKIN L/E SLAT TRACK NR 10 FOUND CRACK .50" LONG CUT OUT CRACK AREA AND INSTALLED FILLER AND DOUBLER RE PAIR IAW SRM 57-10-00 FIG 68 VOL 1. 2 L 7 3 4F A22WE 2007053000160 20070530 00160 WP 2007 5 30 07FDEA01775 1 20070514 A 5320 CHANNEL DOUG DC10 DC1010 3022110 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 FWD CARGO COMPT LIGHT CORROSION ON CHANNEL. REPAIR CHANNEL IAW SRM 53-70-00 FIG 4, SHT 1 VOL 1 PAGE 17. 2 L 7 3 4F A22WE 2007053000161 20070530 00161 NM 2007 5 30 NWAA071906731 1 20070506 A 5320 VERTICAL BEAM BOEING 747 747251B 1384892 NM BS 300 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 631US 23111 DURING "L" CHECK WHILE ACCOMPLISHING VERTICAL BEAM INSPECTIONS PER BOEING SB 747-53A2293 FIGURE 4, CRACKS WERE FOUND COM MON TO BS 300 AND BS 320 LT AND RT VERTICAL BEAM WEBS. ALSO, CRACKS WERE FOUND COMMON TO THE BS 280 RT VERTICAL BEAM WE B. REPAIRED PER EA 67-209467. 2 L 7 4 4F A20WE 2007053000162 20070530 00162 NM 2007 5 30 AWXA200700653 1 20070418 A 5330 146N353112 SKIN BOEING 757 7572S7 1384962 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 MCN - MAJOR REPAIR - CRACKED FUSELAGE SKIN, BS 1459, S26L - S27R. REPAIRED FUSELAGE SKIN, BS 1459, S26L - S27R IAW AWA ER 19-5361-07142-SS2. 2 L 7 2 4F RT A2NM 2007053000163 20070530 00163 NM 2007 5 30 AWXA200700654 1 20070419 A 5330 146N3560 SKIN BOEING 757 7572S7 1384962 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 MCN - MAJOR REPAIR - CORROSION BULGE ON FUSELAGE SKIN, BS 1380, S29R. REPAIRED FUSELAGE SKIN, BS 1380, S29R IAW AWA ER 19-5361-07141-SS2. 2 L 7 2 4F RT A2NM 2007053000164 20070530 00164 NM 2007 5 30 AWXA200700655 1 20070418 A 5330 654576659 SKIN BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - FOUND CRACKED FUSELAGE SKIN, BS 500 + 11" AND BS 500B + 1", S14L. REPAIRED FUSELAGE SKIN, BS 500 + 11" AND BS 500B + 1", S14L IAW B737-300 SRM 53-00-01-2R30, FIGURE 201. 2 L 7 2 4F RT A16WE 2007053100010 20070531 00010 SO 2007 5 31 C2XA07IA123 1 20070527 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS DIRTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 34110 145658 IAH - FLIGHT 2089, THE CREW REPORTED THE MID CABIN CEILING EXIT LIGHT TO BE INOP. MAINTENANCE CLEANED THE CONNECTOR ON THE NUMBER FOUR EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. 2 L 7 2 4F RT 2007053100025 20070531 00025 NM 2007 5 31 CALA0700266 1 20070523 A 5330 6545776 SKIN BOEING 737 7373T0 1384582 NM BS 727 S22-23L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76354 23592 INSPECTION FOUND A 1.5 INCH CRACK IN LEFT FUSELAGE SKIN AT STA 727, S22L-23L, AT APPROXIMATELY EIGHT INCHES AFT AND ABOV E EMERGENCY LIGHT. REPAIRED IAW ECRA 5330-03681. 2 L 7 2 4F RT A16WE 2007053100027 20070531 00027 NM 2007 5 31 CALA0700268 1 20070526 A 5313 148W4506 LONGERON BOEING 777 777224 1385225 NM BS 2272 L26R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 78009 29479 INSPECTION FOUND A .5 INCH CRACK IN AFT LOWER LONGERON STRAP AT RIGHT LOWER SEAL FAIRING AREA, STA 2272, S26R. REPAIRED IAW ECRA 5310-04631. 2 L 7 2 4F RT T00001SE 2007053100028 20070531 00028 NM 2007 5 31 CALA0700269 1 20070527 A 5311 6545801512 FRAME BOEING 737 7373T0 1384582 NM BS 227 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND LOWER O/B CHORD CORRODED AT STA 227, RBL 0 TO LBL 3. REPAIRED IAW ECRA 5311-01324 ITEM 1-16, PAGE 1-3. 2 L 7 2 4F RT A16WE 2007053100029 20070531 00029 NM 2007 5 31 CALA0700270 1 20070527 A 5315 6546811 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12313 23364 INSPECTION FOUND FLOORBEAM AT STA 1016 CORRODED AROUND UPPER AND LOWER HOLES FROM LBL 20 TO O/B END. A REPAIR STRAP WAS INSTALLED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 2007053100033 20070531 00033 SO 2007 5 31 C2XA07IA126 1 20070528 A 2120 UNKNOWN EMB 135 EMB135LR 3260305 SO CABIN ODOR A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 14514 145303 SLP - FLIGHT 2148, THE CREW REPORTED A BURNING ODOR AT THE COFFEEMAKERS. THE AIRCRAFT RETURNED TO SLP WHERE THE COFFEEM AKERS WERE PLACED ON MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH ON FLIGHT 2148 WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND COULD NOT DUPLICATE THE DISCREPANCY. THE MEL WAS CLEARED, AND THE AIRCRAF T APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007053100034 20070531 00034 NM 2007 5 31 2007UALA01631 1 20070525 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHTS AT ROWS 2A AFT & 61CB ARE INOP. [SUP 06-06-07] RELAMPED EMERGENCY LIGHT. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007053100035 20070531 00035 NE 2007 5 31 2007UALA01632 2 20070524 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 2 STALLED A UALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 WP 29 219UA 30551 222130 CREW REPORTED A SURGE - STALL IN CRUISE (STEADY STATE) NR 2 ENG, "AUDIBLE" TO FLT AND CABIN CREW. [07-17-07] ENGINE REPLACED. TEARDOWN SHOWED HEAVY HPC BLADE AIRFOIL DAMAGE FROM THE 6TH STAGE AFT. 1/8TH STAGE BLADE AIRFOIL WAS BROKEN OFF 1/2-INCH ABOVE THE PLATFORM. THE DAMAGE RESULTED FROM THE LIBERATION OF 4 VARIABLE STATOR VANE INNER TRUNNION 'BUTT ONS'. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007053100039 20070531 00039 NM 2007 5 31 2007UALA01636 1 20070525 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY CEILING LIGHT FWD OF LAV 104 INOP. REPLACE LAMP. [SUP 06-06-07] RELAMPED EMERGENCY LIGHT. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007053100045 20070531 00045 NM 2007 5 31 ASAA0741700 1 20070527 A 5322 69432774 SHEAR TIE BOEING 737 7374Q8 138447Q NM BS 807 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 SHEAR TIE IS CRACKED. REMOVED DAMAGED SECTION OF FRAME SHEAR TIE, FABRICATED AND INSTALLED REPAIR SHEAR TIE FILLER AND ANGLE IAW SRM 53-00-07 REPAIR 3. 2 L 7 2 4F RT A16WE 2007053100046 20070531 00046 NM 2007 5 31 ASAA0741701 1 20070527 A 5755 FITTING BOEING 737 7374Q8 138447Q NM SPOILER GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 NR 9 FLIGHT SPOILER FITTING IS GOUGED AT ACTUATOR ATTACH POINT. REMOVED AND REPLACED SPOILER ASSY IAW AMM 27-62-71. 2 L 7 2 4F RT A16WE 2007053100048 20070531 00048 NM 2007 5 31 ASAA0741703 1 20070529 A 5755 ATTACH FITTING BOEING 737 7374Q8 138447Q NM NR 4 SPOILER CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 NR 4 GROUND SPOILER O/B ACTUATOR ATTACH FITTING IS BROKEN IN TWO PIECES. NR 4 GROUND SPOILER REMOVED AND REPLACED IAW A MM 27-62-12. 2 L 7 2 4F RT A16WE 2007053100049 20070531 00049 NM 2007 5 31 ASAA0741704 1 20070526 A 5411 697462911 SHEAR TIE BOEING 737 737490 1384715 NM NR 2 NACELLE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 706AS 28894 NR 2 ENGINE PYLON RIGHT SIDE END PANEL SUPPORT BRACKET IS CRACKED. BRACKET REPLACED WITH NEW PART. 2 L 7 2 4F RT A16WE 2007053100050 20070531 00050 NM 2007 5 31 ASAA0741705 1 20070526 A 5230 65566552 WEB BOEING 737 737490 1384715 NM CARGO DOOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 706AS 28894 AFT CARGO DOOR SURROUNDING WEB FOUND CORRODED. AFT CARGO DOOR SURROUNDING WEB REPLACED WITH FABRICATED REPAIR PART IAW SRM 51-30-01 AND 51-40-05. 2 L 7 2 4F RT A16WE 2007053100052 20070531 00052 NM 2007 5 31 ASAA0741708 1 20070526 A 5340 694465711 SUPPORT BRACKET BOEING 737 737490 1384715 NM BS 664 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 706AS 28894 SYSTEM B-HYDRAULIC LINE SUPPORT BRACKET ON RIGHT MLG WW FWD BULKHEAD IS CRACKED. BRACKET REPAIRED IAW SRM 51-31-01. 2 L 7 2 4F RT A16WE 2007053100053 20070531 00053 NM 2007 5 31 ASAA0741709 1 20070526 A 5320 654795732 INTERCOSTAL BOEING 737 737490 1384715 NM BS 767-787 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 706AS 28894 AFT CARGO FLOOR INTERCOSTAL IS CORRODED. CORRODED FLOOR INTERCOSTAL REPLACED WITH FABRICATED REPAIR PART IAW SRM 53-30- 01 AND 53-60-15 FIG 11. 2 L 7 2 4F RT A16WE 2007053100054 20070531 00054 NM 2007 5 31 ASAA0741710 1 20070526 A 5320 654795733 WEB BOEING 737 737490 1384715 NM BS 787-794 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 706AS 28894 AFT CARGO PIT INTERCOSTAL FOUND CORRODED. REPLACED INTERCOSTAL WITH FABRICATED REPAIR PART IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007053100061 20070531 00061 NM 2007 5 31 2007UALA01645 1 20070525 A 2500 SWITCH BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE MODE SELECTOR FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 791UA 26933 CABIN MED 3RT FAILED EPAS BATTERY OPERATIONAL TEST. [06-20-07] REPLACED MODE SELECTOR SWITCH AND OPS CHECK PER MM 52-1 1-28, AND COA208701. TEST OK. A/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007053100063 20070531 00063 EA 2007 5 31 COMA0760389 1 20070520 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 592SW 7279 FLIGHT 5067 - FLAP FAIL AT GATE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PAR AGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2007053100064 20070531 00064 NE 2007 5 31 COMA0670390 2 20070521 A 7200 CF343A1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE RIGHT OVERTEMP A COMA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 01 965CA 28926 7131 807051 FLIGHT 4988 - DURING TAKEOFF ROLL THE RIGHT ENGINE ITT INDICATED 905C, ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLAC ED THE RIGHT ENGINE ASSEMBLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2007053100068 20070531 00068 SO 2007 5 31 RAIA00705041 1 20070521 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 819HK 145062 PRE FLT NR 5575 - STL - EMERGENCY EXIT LIGHT MAIN DOOR EXIT MARKER INOP. MAINTENANCE RESECURED ELECTRICAL CONNECTION TO EMERGENCY LIGHT, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007053100072 20070531 00072 SO 2007 5 31 RAIA00705045 1 20070523 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NLG DOOR INOPERATIVE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 849HK 9040 145002 FLT NR 7894 - STL - AFTER TAKEOFF GEAR CAME UP NORMAL BUT NOSE GEAR DOORS STAYED OPEN. MAINTENANCE REMOVED AND REPLACED PROXIMITY SWITCH ON NOSE UPLOCK. PERFORMED OPS CHECK, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007053100073 20070531 00073 SO 2007 5 31 C2XA07CL048 1 20070525 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO LANDING GEAR OUT OF ADJUST A C2XA B EMER. DESCENT N FALSE WARNING AP APPROACH 1 SW 27 14904 145477 CLE FLIGHT 3004 THE CREW REPORTED ON APPROACH WHEN EXTENDING THE LANDING GEAR A LANDING GEAR AIR/GROUND FAIL MESSAGE CAM E ON THE EICAS. MAINTENANCE INSPECTED AND ADJUSTED THE LEFT AND RIGHT MAIN GEAR PROXIMITY SWITCH 2. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007053100077 20070531 00077 EU 2007 5 31 USAA070414 1 20070525 A 5315 D5311281820401 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 178US 1519 EXFOLIATION AT FR 16 ON TOP OF FLOORBEAM Y254. FLOORBEAM REMOVED & REPLACED PER SRM 51-72-11; CORR TASK JA-220-53500; LEVEL 1, DEFECT SIZE: 1 X 2 INCHES. 2 L 7 2 4F RT A28NM 2007053100080 20070531 00080 EA 2007 5 31 TRAX200700701 1 20070521 A 5740 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 836AS 7263 RIGHT WING MIDDLE LEADING EDGE I/B ATTACH ANGLE CRACKED. 2 L 7 2 4F RT A21EA 2007053100081 20070531 00081 EA 2007 5 31 TRAX200700702 1 20070521 A 5720 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 836AS 7263 LEFT WING I/B LEADING EDGE O/B BRACKET CRACKED. 2 L 7 2 4F RT A21EA 2007053100082 20070531 00082 EA 2007 5 31 TRAX200700721 1 20070524 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 976EV 7601 RIGHT FS 484 STRINGER CLIP CRACKED AT BL 27.00 (MARKED). 2 L 7 2 4F RT A21EA 2007053100084 20070531 00084 EA 2007 5 31 TRAX200700722 1 20070524 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 976EV 7601 LEFT FS 484 ATTACH FITTING CRACKED AND BL 27.00 (MARKED). [07-23-07] REMOVED DAMAGED CLIP FROM LT FS 484 BL 27.00. DUPLICATED CLIP USING SERVICEABLE ANGLE IAW CRJ SRM 51-24-16. OK TO ALODINE, PRIME, AND PAINT. OK TO INSTALL. ALODINED, PRIMED, AND PAINTED IAW 51-25-16. INSTALLED IAW CRJ SRM 51-42-20. 2 L 7 2 4F RT A21EA 2007053100088 20070531 00088 EA 2007 5 31 TRAX200700724 1 20070525 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA BS 559 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 850AS 7355 EXTERIOR FUSELAGE SKIN AT FS 559.00 + 112, RBL 2.00 IS CORRODED. [SUP 05-31-07] REPAIRED IAW SRM 53-00-31 FIG 103 AND SRM 51-21-06. 2 L 7 2 4F RT A21EA 2007053100089 20070531 00089 EA 2007 5 31 TRAX200700725 1 20070525 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 850AS 7355 CRACK SUSPECT AT FS 484 RBL 27 AND RBL 36 UNDER FLOOR INTERCOSTAL. [SUP 05-31-07] REPAIRED IAW REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2007053100092 20070531 00092 EU 2007 5 31 USAA200705U12 1 20070524 A 5310 BEAM AIRBUS A321 A321211 3930370 EU FUSLEAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 178US 1519 A 1.125 X 2 INCH CORROSION FOUND AT RIGHT AFT SILL BEAM. REPAIRED PER SRM 53-41-14. CORROSION TASK JA-260-53500, CORR LEVEL 1. 2 L 7 2 4F RT A28NM 2007053100094 20070531 00094 SO 2007 5 31 C2XA07CL049 1 20070529 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO CARGO BAY INTERMITTENT A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 27 12900 145511 CLE FLIGHT 2401 THE CREW REPORTED A BAGGAGE SMOKE DETECTOR WARNING IN FLIGHT. THE WARNING CAME ON TWICE IN FLIGHT AND W AS VISUALLY INSPECTED BY THE FIRST OFFICER AND FLIGHT ATTENDANT WITH NO INDICATION OF A FIRE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 BAG SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007053100096 20070531 00096 EU 2007 5 31 SA07031 1 20070524 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHTS FAULTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 754UW 15343 864 1328 TPA - RECEIVED MID-CABIN, RIGHT HAND EPSU FAULT DURING THE EMERGENCY LIGHTS OPERATIONAL TEST. MAINTENANCE REPLACED THE MID-CABIN, RIGHT SIDE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. 2 L 7 2 4F RT A28NM 2007053100098 20070531 00098 NM 2007 5 31 UPS07249849 1 20070523 A 3350 BATTERY PACK BOEING 727 72722C 138400F NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT OVER CABIN ENTRY DOOR INOP. REMOVED AND REPLACED BATTERIES IN EMERGENCY EXIT L IGHT IAW B727 MM 33-50-67-2. OPS CHECKS NORMAL. 2 L 7 3 4F A3WE 2007053100101 20070531 00101 WP 2007 5 31 UPS07849853 1 20070524 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY AND RELAY UNIT PER AMM 33-50-01-2. OPS CHECK O K. 2 L 7 4 4F RT 4A25 2007053100104 20070531 00104 NM 2007 5 31 UPS07M49852 1 20070524 A 2432 BATTERY DOUG MD11 MD11F 3023600 NM MASTER DISCHARGED A IPXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 257UP 48451 DIVERTED - BATTERY LOW ALERT. REMOVED AND REPLACED MAIN BATTERIES PER AMM 24-34-02-4 & BATTERY CHARGER PER AMM 24-34-03 -4. OPERATION TEST SATISFACTORY. PERFORMED EMERGENCY POWER SYSTEM TEST PER AMM 24-34-00-5. NO DISCREPANCY FOUND. A/C RETURNED TO SERVICE. 2 L 7 3 4F RT A22WE 2007053100107 20070531 00107 EA 2007 5 31 TRAX200700693 1 20070520 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA BS 409 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 851AS 7360 LEFT SIDE PASSENGER SEAT SIDE RAILS CORRODED AND GOUGED AS MARKED AFT OF FS 409+128. BLENDED SIDE WALL SEAT RAIL P/N 60 1R38312-21 AT FS 409+130 TO DIMENSIONS OF 1" X 3" X .017 DEEP AND AT FS 409+147 TO DIMENSIONS OF 1" X 1" X .007 DEEP. B LENDED SIDEWALL SEAT RAIL P/N 601R38312-115 AT FS 460 TO DIMENSIONS OF 1" X 1" X .004 AND AT FS 494 TO DIMENSIONS OF 1" X 1" X .013. BLENDED SIDEWALL SEAT RAIL P/N 601R38312-25 AT FS 547 TO DIMENSIONS OF 1" X 3" X .007 DEEP AND AT FS 559+3 9 TO DIMENSIONS OF 1" X 2" X .006 DEEP AS PER CRJ 200 SRM 51-12-00. RECEIVED DAMAGE LIMITS FROM BOMBARDIER, LIMITS OF C RJ200 SRM 53-21-49 FIG 101. ALL SIDE SEAT RAIL BLEND OUTS LEFT SIDE AFT OF 409+128 ARE WITHIN LIMITS OF CRJ200 SRM 53-2 2 L 7 2 4F RT A21EA 2007053100108 20070531 00108 EA 2007 5 31 TRAX200700694 1 20070520 A 5347 SEAT TRACK CNDAIR CL600 CL6002B16 1900305 EA BS 409 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 851AS 7360 RIGHT SIDE PASSENGER SEAT SIDE RAILS CORRODED AND GOUGED AS MARKED FWD OF FS 409+128. BLENDED SIDE WALL SEAT TRACK P/N 601R38312-29 AT FS 409+86 TO DIMENSION OF 1" X 1" X .004 DEEP AS PER CRJ200 SRM 51-12-00. RECEIVED DAMAGE LIMITS FROM B OMBARDIER, LIMITS OF CRJ200 SRM 53-21-49 FIG 101. ALL SIDE SEAT RAIL BLEND OUTS RIGHT SIDE FWD OF 409+128 ARE WITHIN LI MITS OF CRJ200 SRM 53-21-49 FIG 101. C/W A044 FINISH ON BLENDED AREAS ON RIGHT SIDE SEAT RAILS IAW CRJ200 SRM 51-21-16. SUPPLEMENTAL - SDR CLOSED 05/25/07. 2 L 7 2 4F RT A21EA 2007053100109 20070531 00109 EA 2007 5 31 TRAX200700695 1 20070520 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA BS 409 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 851AS 7360 RIGHT SIDE PASSENGER SEAT SIDE RAILS CORRODED AND GOUGED AS MARKED AFT OF FS 409+128. BLENDED SIDEWALL SEAT RAIL P/N 60 1R38312-115 AT STA 449.85 TO DIMENSIONS OF 1" X 1" X .007 DEEP AND AT STA 495.98 TO DIMENSIONS OF 1" X 1" X .008 DEEP. BLENDED SIDEWALL SEAT RAIL P/N 601R38312-25 AT STA 559 + 10 TO DIMENSIONS OF 1" X 12" X .008 AND AT STA 559+36 TO DIMENS IONS OF 1" X 1" X .004 DEEP AS PER CRJ 200 SRM 51-12-00. RECEIVED DAMAGE LIMITS FROM BOMBARDIER, LIMITS OF CRJ200 SRM 5 3-21-49 FIG 101. ALL SIDE SEAT RAIL BLEND OUTS RIGHT SIDE AFT OF 409+128 ARE WITHIN LIMITS OF CRJ200 SRM 53-21-49 FIG 1 01. C/W A044 FINISH ON BLENDED AREAS ON RIGHT SIDE SEAT RAILS IAW CRJ200 SRM 51-21-16. SUPPLEMENTAL - SDR CLOSED 05/25 2 L 7 2 4F RT A21EA 2007053100116 20070531 00116 NM 2007 5 31 DHL2007740500 1 20070522 A 5322 SHEAR TIE BOEING 727 7272Q9 138448M NM BS 480 S16-17L CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 WHILE IN "C" CHECK, FRAME STA 480, SHEAR TIE AT FRAME IS CRACKED BETWEEN STR 16L AND STR 17L. REMOVED FASTENERS AND CRA CKED ANGLE AT STA 480 BETWEEN STR 16L AND 17L IAW B727 SRM 51-30-2. FABRICATED ANGLE FROM 7075T6 .040 PO NR 9004940 APP ROX DIM. 6" BY 2" IAW B727 SRM 51-40-3 FIG 1 AND 51-20-1 FIG 7. PRIMED ANGLE IAW B727 SRM 51-10-2. INSTALLED ANGLE AT STA 480 BETWEEN STR 16L AND 17L IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007053100117 20070531 00117 NM 2007 5 31 DHL2007740502 1 20070517 A 5754 SKIN BOEING 727 7272Q9 138448M NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 WHILE IN "C" CHECK, RT WING LE CRACKED AT NR 5 SLAT OB HOOK CUTOUT. STOP DRILLED CRACK IAW B727 SRM 57-30-4 FIG 9 AND 5 1-10-1. FABRICATED REPAIR PLATE FROM 301 1/2HD .025 PO NR 9005090 DIM 7 1/4 BY 5 1/8, FILLER FROM 301 1/2HD .032 PO NR 614973 AND BACKING STRAP FROM 2024T3 .063 PO NR 9005089 DIM 7 1/4 BY 2 3/8 IAW B727 SRM 57-30-4 FIG 9. CUT EXISTING FIL LER STRIP DIM 7 1/4 BY 2 1/8 IAW B727 SRM 57-30-4 FIG 9. TREATED AND PRIMED AREA AND PARTS IAW B727 SRM 51-10-2 AND INS TALLED REPAIR PARTS AT R/WING LE SLAT NR 5 OB HOOK SEAL CUTOUT IAW B727 SRM 51-30-2 AND 57-30-4 FIG 9. 2 L 7 3 4F RT A3WE 2007053100122 20070531 00122 WP 2007 5 31 07FDEA01831 1 20070517 A 3210 836462012 NUT DOUG DC10 DC1030 3023501 WP ZONE 700 INOPERATIVE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 317FE 46835 CENTER GEAR RT PILLOW BLOCK :FWD BOLT BACKED OFF APPROX 1/2 INCH. AFT BOLT LOOSE AND CAN BE ROTATE BY HAND. UPON DISASS EMBLY FOUND PILLOW BLOCK NUTS DO NOT SELF LOCK. REMOVED LT TRUNNION PILLOW BLOCK AND PERFORMED HFEC AND FPI INSPECTION OF HOLE BORE AND BLOCK ASSY PER NDTSPM, TP-MDC-93K0393. NO DEFECTS WERE NOTED. FABRICATED AND INSTALLED FIVE (5). REP AIR BUSHINGS PER CMM 32-15-01. PERFORMED A BREAK AWAY TORQUE CHECK ON THE FOUR (4) PILLOW BLOCK BOLT NUTS PER NASM25027 3.8.2.2.2 TABLE III PRIOR TO RE-INSTALLATION OF TRUNNION PILLOW BLOCK. RE-INSTALLED LT TRUNNION PILLOW BLOCK AND CENTE R LG ASSY PER WC 32T7701. 2 L 7 3 4F A22WE 2007053100123 20070531 00123 WP 2007 5 31 07FDEA01832 1 20070517 A 5520 17451EEL BUSHING BOEING DOUG MD10 MD1010F 3022112 WP RT ELEVATOR LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 RT O/B ELEVATOR O/B DAMPER HINGE FITTING HAT BUSHINGS ARE LOOSE. REMOVED AND REPLACED RT O/B ELEVATOR O/B ELEVATOR O/B DAMPNER HINGE FITTING HAT BUSHINGS IAW CMM 55-21-01 AND FEDEX EA 8-5520-109163. TITLE; LT AND RT ELEVATOR HINGE FITT ING OVERSIZE HOLE-REPAIR. ORIGINAL ATTACHED TO FEDEX N/R N00836. 2 L 7 3 4F RT A22WE 2007053100125 20070531 00125 WP 2007 5 31 07FDEA01834 1 20070517 A 2720 174190KSI BUSHING BOEING DOUG MD10 MD1010F 3022112 WP RT ELEVATOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 RT O/B ELEVATOR I/B ACTUATOR MOUNT FITTING (ON ELEVATOR) CORRODED ON I/B SIDE. REMOVED CORROSION/DAMAGE IAW DAC CMM 55- 21-01. REMOVED, FABRICATED AND INSTALLED BUSHINGS IAW DAC CMM 55-21-01 AND FEDEX 8-5520-109163. TITLE; " STABILIZER- L T AND RT ELEVATOR HINGE OVERSIZE HOLE-REPAIR". 2 L 7 3 4F RT A22WE 2007053100128 20070531 00128 NM 2007 5 31 07FDEA01840 1 20070517 A 5330 BAC1520841 SEAT TRACK BOEING 727 727225 1384077 NM BS 848-870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 465FE 21289 MAIN CABIN SEAT TRACK CORRODED UPPER SURFACE FROM FSTA 848 - 870, LBL 45 BLENDED SEAT TRACK AT 848 - FS870 LBL 45 FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-30-1 (FIG 1); ORDERED NEW SEAT TRACK PART NR BAC1520-841 BATCH NR 3370-1 AND LOCATED AND DRILLED HOLES IAW SRM 51-30-1. TREATED AND PRIMED SEAT TRACK IAW SRM 51-10-2. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2007053100129 20070531 00129 NM 2007 5 31 07FDEA01841 1 20070517 A 5320 FXSRM51101N0 WEB BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 465FE 21289 AFT CARGO STA 970 S-28R WEB HAS CORROSION. REMOVED CORROSION ON WEB AT STA 970 STR 28R CORROSION FOUND OUT OF LIMITS IA W SRM 51-10-6, FABED NEW WEB ON MAE TR T7/679785. INSTALLED THE NEW WEB IAW SRM 51-30-2. INSTALLED STIFFENERS THAT WER E REMOVED PREVIOUSLY FOR ACCESS IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2007053100131 20070531 00131 NM 2007 5 31 07FDEA01844 1 20070518 A 5740 69719803 BRACKET BOEING 727 7272S2F 1384O81 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 LT WING TRAILING EDGE SMALL U SHAPE BRACKET FOR SUPPORT OF OUTBD TRACK FAIRING, IS CRACKED AT THE SERRATIONS INBD FLANGE REMOVED CLIP REF SRM 51-30-02 FIG.7 PG.32 INSTALLED NEW CLIP REF. SRM 51-30-02 PG 2 2 L 7 3 4F A3WE 2007053100132 20070531 00132 NM 2007 5 31 07FDEA01845 1 20070518 A 5310 6559948502 SEAL DEPRESSOR BOEING 727 7272S2F 1384O81 NM CARGO DOOR FRAME GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 FUSE LWR LOBE AFT CARGO DR FRAME INTERIOR SURFACE IS GOUGED AT LOWER AFT CORNER, BS 989, STR 26R. REMOVED AND INSTALL ED NEW LOWER AFT CORNER, OF AFT CARGO PIT DOOR REF SRM 51-30-2 PG 1-12 (SEAL DEPRESSOR). 2 L 7 3 4F A3WE 2007053100134 20070531 00134 EU 2007 5 31 07FDEA01506 1 20070416 A 5754 A5517874000100 SKIN AIRBUS 310 A310324 3930206 EU RT WING DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 801FD 539 THS-FRACTION 341BB AT L/E OF RT THS W/UPPER SKIN SURFACE W/DENT REPAIRED PER SRM 55-12-12 FIG 203. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR". 2 L 7 2 4F RT A35EU 2007053100136 20070531 00136 WP 2007 5 31 07FDEA01823 1 20070516 A 5730 SKIN DOUG DC10 DC1010 3022110 WP RT WING TE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 RIGHT WING TRAILING EDGE UPPER SURFACE CLOSE OUT PANEL IS BULGED AT SEVERAL LOCATIONS BETWEEN NR 2 AND NR 5 SPOILER AREA . REMOVED CORROSION IAW DC/MD10 SRM 51-21-01 VOLII AND FEDEX EA 8-5710-109151 WINGS, RT WING SPAR CORROSION BETWEEN STA XORS 480-733-REPAIR, ALODINED AND PRIMED IAW DC/MD10 SRM 51-21-01 VOLII. 2 L 7 3 4F A22WE 2007053100137 20070531 00137 NM 2007 5 31 07FDEA01836 1 20070517 A 5310 6518915182 FRAME BOEING 727 7272S2F 1384O81 NM TORQUE BOX CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 FUSELAGE LOWER LOBE NH NOSE TUNNEL TORQUE BOX INTERIOR HORIZ WEB IB CHORD IS CORRODED/EXFOILATION, BS 295-301, LBL 15, WL168 BLENDED AND REMOVED CORROSION .018 MATERIAL LOSS, WITHIN LIMITS, APPLIED ALODINE AND PRIMER REF SRM 51-10-1 AND SR M 51-10-2, SRM 53-10-1 PG 1. 2 L 7 3 4F A3WE 2007053100141 20070531 00141 NM 2007 5 31 07FDEA01921 1 20070521 A 5740 FITTING DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT WING LOWER WINGLET AFT FITTING FWD AND AFT HOLES FOUND CORRODED. [SUP 05-29-07] CORRODED FWD AND AFT HOLES AT LEF T HAND WING LOWER WINGLET ATTACHED AFT FITTING REPAIRED AS PER FEDEX EA 1-5730-111107. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007053100142 20070531 00142 EU 2007 5 31 07FDEA01922 1 20070521 A 5320 STIFFENER AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 FLOORBEAM 36, LT BETWEEN SEAT TRACKS NR 2 LT NR 3 LT - FWD SIDE OF FLOORBEAM, VERTICAL STIFFENER AT UPPER END HAS A .500 INCH HORIZONTAL CRACK. REMOVED FLOOR BOARD (2EA) IAW A310/200 SRM 51-40-21. FABRICATED REPAIR ANGLES AND REPAIRED FLO ORBEAM 36 IAW A310/200 SRM 53-10-15. INSTALLED FLOORBOARDS IAW A310/200 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007053100144 20070531 00144 EU 2007 5 31 07FDEA01924 1 20070521 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 A 1.5 SQ INCH AREA OF CORROSION EXIST AT MDCC SEAT TRACK L-5 FRAME 34 FAVED 1 SEAT TRACK AND 4 REPAIR ANGLES PER SRM 53- 10-16, ALODINED PRIMED TOP COATED PER SRM 51-75-10. INSTALLED SEAT TRACK AND 4 REPAIR ANGLES IAW SRM 53-10-16. 2 L 7 2 4F RT A35EU 2007053100147 20070531 00147 EU 2007 5 31 07FDEA01927 1 20070522 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 A 2.0 SQ INCH AREA OF CORROSION EXIST AT MDCC SEAT TRACK L-6 FRAME 34, 1 SEAT TRACK AND 4 REPAIR ANGLES IAW A310 SRM 53- 10-16. ALODINED PRIMED AND TOP COATED IAW SRM 51-75-10. INSTALLED SEAT TRACK AND 4 REPAIR ANGLES IAW A310 SRM 53-10-16 . 2 L 7 2 4F RT A35EU 2007053100149 20070531 00149 NM 2007 5 31 07FDEA01929 1 20070522 A 5720 652678929 SUPPORT ANGLE BOEING 727 7272S2F 1384O81 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 LT WING T/E ANGLE SUPPORT FOR JACKSCREW MOST OUTBD FAIRING IS CRACKED FROM FASTENER HOLE (INBD ANGLE). REPLACED WITH NE W DOUBLER REF 51-30-5 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2007053100150 20070531 00150 NM 2007 5 31 07FDEA01930 1 20070522 A 5720 69262804 DEFLECTOR BOEING 727 7272S2F 1384O81 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 PNL RACK RT WING TO BODY RT WING TO BODY PLN UPPER SURFACE HAS A CRACKED BRACKET. PAINTED AND INSTALLED NEW PARTS, RE F SRM 51-30-023 PG 1. 2 L 7 3 4F A3WE 2007053100151 20070531 00151 NM 2007 5 31 07FDEA01931 1 20070522 A 5320 656725148 SUPPORT ANGLE BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 AFT PIT, STA 1166, WL 200, RBL 48, AFT WALL SUPPORT ANGLE, IS CORRODED UPPER AFT CORNER. BLENDED CORROSION AND FOUND AN GLE TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW ANGLE, REF SRM 51-30-2 PG 1-4, AND BOEING DWG NR 65-67251. 2 L 7 3 4F A3WE 2007053100153 20070531 00153 NM 2007 5 31 07FDEA01933 1 20070522 A 5730 6516285 SKIN BOEING 727 7272S2F 1384O81 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 RT WING, UPPER WING SKIN CRACKS AT NR 12 I/B HINGE CUT OUT. STOP DRILLED CRACK, NDT VERIFIED CRACK TERMINATION, FABRICA TED AND INSTALLED REPAIR DOUBLER REF SRM 57-30-4. 2 L 7 3 4F A3WE 2007053100158 20070531 00158 WP 2007 5 31 07FDEA01846 1 20070518 A 5711 ARB128846 FRAME DOUG MD10 MD1010F 3022112 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 RIGHT WING LEADING EDGE FORMER CRACKED AT XOS625.5 STOP DRILLED CRACK AND INSTALLED REPAIR CLIP PER MD/DC 10-10 SRM 57-2 0-00 FIG 1 VOL I . FUEL CONTROL PANEL WAS REMOVED. REINSTALLED AND OPS CHECKED TO FACILITATE REPAIR IN REF TO MD10-10 MM 28-00-00-5. OPS CHECK GOOD. 2 L 7 3 4F RT A22WE 2007053100162 20070531 00162 NM 2007 5 31 07FDEA01849 1 20070519 A 5311 65163431 FRAME BOEING 727 7272S2F 1384O81 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 AFT CARGO PIT RT SIDE STA 1050 STR 25R FRAME IS DENTED DETERMINED DENT TO BE OUT OF LIMITS, PER SRM 53-10-01. FABRICATE D REPAIR PARTS, TREATED AND PRIMED AND INSTALLED REF SRM 51-40-3 FIG 1, SRM 51-30-02. 2 L 7 3 4F A3WE 2007053100168 20070531 00168 NM 2007 5 31 07FDEA01855 1 20070519 A 5311 65163471 FRAME BOEING 727 7272S2F 1384O81 NM BS 1130 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 AFT PIT STA 1130, LBL 25, STR. 26, FRAME IS DENTED CUT OUT DAMAGE, FABRICATED REPAIR ANGLE FROM 7075-0 .063 AND HEAT TRE ATED TO 7075-T-6 INSTALLED REPAIR ANGLE REF SRM 51-40-03. 2 L 7 3 4F A3WE 2007053100171 20070531 00171 WP 2007 5 31 07FDEA01947 1 20070523 A 5312 AEA05012 BULKHEAD DOUG DC10 DC1010 3022110 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 RT MLG W/W FOUND 2 CRACKS ON VERTICAL BULKHEAD DOUBLER. TRIMMED AREA, FAB AND INSTALLED WEB, SPLICE, FILLER IAW SRM 53- 00-01 VOL 1. 2 L 7 3 4F A22WE 2007053100174 20070531 00174 WP 2007 5 31 07FDEA01951 1 20070523 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 AFT FUSE COMPT FOUND 1 CRACK ON HORIZONTAL WEB AFT SIDE VERTICAL BULKHEAD. REPAIRED IAW SRM 53-00-01 VOL 1 FIG 10. 2 L 7 3 4F A22WE 2007053100175 20070531 00175 WP 2007 5 31 07FDEA01952 1 20070523 A 5330 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 LT FUSELAGE EXTERNAL SKIN CHAFED JUST FORWARD OF MAIN CARGO DOOR CUT-OUT UPPER AREA. AREA IS CHAFED BY TAB ATTACHMENT T O UPPER DOOR CORNER. BLENDED AREA FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-00-01 FIG 1A VOL I, 53-32-01 FIG 2 VOL III AND EA 8-5330-109167-FUSELAGE SKIN CHAFED AT STA 620 ABOVE 12LREPAIR. ORIGINAL THICKNESS .068, MATERIAL REMOVED .022, R EMAINIG THICKNESS .046. 2 L 7 3 4F A22WE 2007053100178 20070531 00178 NM 2007 5 31 07FDEA01860 1 20070520 A 5730 ARB2886503 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT WING TELESCOPIC DUCT CUT-OUT FOUND WITH 0.3125 INCH CRACKED. [SUP 06-08-07] REPAIRED AS PER SRM 57-10-00 VOLUME I , FIGURE 43. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007053100181 20070531 00181 EU 2007 5 31 07FDEA01863 1 20070521 A 5420 BRACKET AIRBUS 310 A310203 3930313 EU NR 1 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 PYLON NR 1 AT AFT T/E LOWER SECTION LOWER FAIRING INNER "A" FRAME SUPPORT BRACKET HAS A CRACK (APPROX 3" LONG) VISIBLE T HRU OPEN ACCESS NR 474DR AND BETWEEN RIB 20-21 THRU LIGHTENING HOLE. REMOVED AND REPLACED WEB IAW SRM 51-40-21. LOCATE D AND DRILLED IAW SRM 51-40- 44, FABBED WEB ON MAE TRAVELER NR T7/678060. 2 L 7 2 4F RT A35EU 2007053100184 20070531 00184 EU 2007 5 31 07FDEA01954 1 20070523 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 MDCC SEAT TRACK R3 FRAME 33- FR 45 7EA AREAS CORROSION 10 SQ IN. REMOVED CORROSION (7EACH AREAS) IAW A310-200 SRM 51-74 -10. FAB`D 1 SEATTRACK FROM FRAME 36- 38.2; FAB`D 2 REPAIR ANGLES IAW A310-200 SRM 53-10-16; ALODINED, PRIMED, TOP CO ATED PER A310-200 SRM 51-75-10. 2 L 7 2 4F RT A35EU 2007053100188 20070531 00188 WP 2007 5 31 07FDEA01945 1 20070522 A 5320 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 MAIN CARGO DOOR NR 6 LATCH SPOOL AND FITTING IS CORRODED. REMOVED NR 6 SPOOL IAW DC/MD10 FEDEX EA NR 8-5230-110663 STEP S 5A AND B. CLEANED,TREATED AND PRIMED IAW FEDEX DC/MD10 SRM 51-21-01 VOL 11. INSTALLED NR 6 SPOOL AND FITTING IAW FED EX EA NR 8-5230-110663. INSTALLED MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING AND RIGGED DOOR IAW FEDEX EA NR 8-5230-1 10663. 2 L 7 3 4F RT A22WE 2007060100002 20070601 00002 NM 2007 6 1 DL76L070602 1 20070526 A 2131 CONTROLLER BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE CABIN PRESSURE MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 179DN 25144 724143 CABIN ALT AUTO 1 AND 2 INOP. PERFORMED BITE TO BOTH CABIN PX CONTROLLERS AS PER FIM 21-31-00 FIG 103. FOUND SATIS FOR FURTHER SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007060100005 20070601 00005 NM 2007 6 1 DL757070605 1 20070527 A 2120 149N716119 DOOR BOEING 757 757232 1384965 NM RAM AIR ACT MISSING A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 699DL 29970 ON DEPARTURE FROM SEA, AFTER CLIMBING THROUGH FL270 MULTIPLE CREW MEMBERS CONTACTED THE FLT DECK WITH EXCESSIVE NOISE AN D VIBRATION VICENITY OF 2L TO WING AREA. FOUND LT RAM AIR DOOR ACCESS PANEL MISSING. ROBBED DOOR FROM A/C 6717. 2 L 7 2 4F RT A2NM 2007060100008 20070601 00008 NM 2007 6 1 DL757070608 1 20070528 A 2120 214N211118 DUCT BOEING 757 757232 1384965 NM CABIN SPLIT A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 676DL 25981 ON CLIMB-OUT, THE OVERHEAD DISTRIBUTION DUCT AT ROW 33/34 AREA LET GO. THE RUPTURE CAUSED THE CEILING PANEL TO BE BLOWN OFF INTO THE CABIN. THE A/C RETURNED TO SJU. 2 L 7 2 4F RT A2NM 2007060100009 20070601 00009 NM 2007 6 1 DL764070609 1 20070528 A 5210 SEAL BOEING 767 767432ER 1385134 NM L4 DOOR LOOSE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 831MH 29702 RTB - DOOR SEAL LOOSE 4L DOOR. CKD PRESS SEAL DOOR 4L OK, REPOSITIONED COVER DOOR SEAL 4L. 2 L 7 2 4F RT A1NM 2007060100011 20070601 00011 NM 2007 6 1 DLM88070611 1 20070527 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 1474 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 TRANS FROM OMI/CMI C/N C02247494 DUE AT HMV SRM 53-04D FIG 12B PERM REPAIR TO 2EA CRACKS IN EMPENNAGE AT STA 1474 12 INC HES LT OF AIRSTAIR CUTOUT. PERM REPAIR ACCOMPLISHED PER SRM 53-04D FIG 12B. 2 L 7 2 4F RT A6WE 2007060100022 20070601 00022 NM 2007 6 1 DLM88070621 1 20070527 A 5720 VANE DOUG MD88 MD88 3023688 NM RT WING DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 DENT ON MID GUIDE VANE OF RIGHT OUTBD FLAP. MID GUIDE VANE WAS REPAIRED IAW SRM 57-03D PARA 8 FIG 9A ON N/R T0056900. 2 L 7 2 4F RT A6WE 2007060100024 20070601 00024 NM 2007 6 1 DLM88070624 1 20070527 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 1309 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACK ON FUSELAGE SKIN AT STA 1309 BETWEEN LONGERONS 6 AND 7 LT. PERMANENT REPAIR INSTALLED PER SRM 53-04D FIG 32, ON N /R TOO56614-HMV-3/GDL. 2 L 7 2 4F RT A6WE 2007060100025 20070601 00025 NM 2007 6 1 DLM88070625 1 20070527 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 1437 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACK ON FUSELAGE SKIN AT STA Y=1437 BETWEEN LONGERONS 4 AND 5 LT. INSTALLED PERM REPAIR IAW 53-04D FIG 27 ON N/R TOO57 038, HMV/GDL. 2 L 7 2 4F RT A6WE 2007060100026 20070601 00026 NM 2007 6 1 DLM88070626 1 20070528 A 5730 SKIN DOUG MD88 MD88 3023688 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACK ON LT WING FIXED TRAILING EDGE UPPER SKIN. PERM REPAIR INSTALLED PER SRM 57-03D FIG 802D ON N/R T0056674, HMV/GDL . 2 L 7 2 4F RT A6WE 2007060100037 20070601 00037 NM 2007 6 1 DL738070594 1 20070524 A 3244 325040031 TIRE BOEING 737 737832 13844CF NM NR 1 MLG WHEEL FAILED A DALA O OTHER O OTHER LD LANDING 1 SO 27 392DA 30561 NR 1 MAIN TIRE BLEW ON LANDING. REPLACED NR 1 MLG WHEEL ASSY IAW AMM. 2 L 7 2 4F RT A16WE 2007060100040 20070601 00040 NM 2007 6 1 DL764070598 1 20070524 A 5270 PSEU BOEING 767 767432ER 1385134 NM LOWER UNKNOWN A DALA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 27 828MH 29699 LT EMERGENY DOOR AND LT AFT ENTRY DOOR EICAS MESSAGE, BIT PSEU PER FIM AND FOUND CARD 007 FAULT-ERASED PER FIM AND PERFO RMED VERIFY-FAULT DID NOT RETURN-DOOR INDICATIONS CHECK OK. 2 L 7 2 4F RT A1NM 2007060100042 20070601 00042 NE 2007 6 1 DL76L070600 2 20070525 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 SURGES A DALA O OTHER O OTHER DE DESCENT 1 SO 27 180DN 45744 724143 25985 724143 AT TOD, CREW REPORTED BUMP NOISE AT APPROX SAME TIME MCC RECEIVED SURGE REPORT FOR THE LEFT ENG. ENG PARAMETERS WERE AL L NORMAL. BOTH ENGS UPON ARRIVAL AT THE GATE. EICAS SHOWED LEFT ENG SURGE DET. T/S PER FIM 71-05-00 FIG 103B. BORO I NSP AND ENG RUN NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007060100043 20070601 00043 NM 2007 6 1 DL757070631 1 20070526 A 5330 SKIN BOEING 757 757232 1384965 NM BS 683 S4L DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 610DL 22817 LIGHTNING DAMAGE IN FUSELAGE SKIN S-4L LAP SPLICE. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F RT A2NM 2007060100044 20070601 00044 NM 2007 6 1 DLM88070632 1 20070530 A 2530 OVEN DOUG MD88 MD88 3023688 NM GALLEY CONTAMINATED A DALA C ABORTED TAKEOFF W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 946DL 49819 PNS-ATL FLT 467 SHORTLY AFTER T/O, A HOT OVEN/BURNING SMELL FLT 1238 BY CP AND CABIN CREW. IT DISSIPATED W/IN FEW MINUT ES. FLT 1238 ATL-SRQ HAPPEN 2ND TIME ODOR WAS STRONGER AND LASTED LONGER. SUSPECTED POSSIBLE BIRD INGESTION. FLT 930 SRQ-ATL, STRONG ELECTRICAL SMELL ON DESCENT. F/A'S SAID SMELLED LIKE SULFUR OR MATCH ODOR VERY STRONG IN COCKPIT. MTC IS IN PROGRESS DNTC. INSPECTED APU INLET AND BOTH ENGINE INTAKES NO TROUBLE FOUND RAN PACKS USING APU AND ENGINES NO SM ELL OBSERVED REPLACED AND RT COALESCER BAGS REMOVED BURNT DEBRIS FROM F/C OVEN. 2 L 7 2 4F RT A6WE 2007060100046 20070601 00046 NM 2007 6 1 DL757070634 1 20070530 A 3350 BATTERY BOEING 757 757232 1384965 NM FLASHLIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 684DA 27104 EMERGENCY FLASHLIGHT AT R4 DOOR INOP. REPLACED BATTERY. 2 L 7 2 4F RT A2NM 2007060100051 20070601 00051 EA 2007 6 1 SWIA200718270 1 20070501 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 668CA 10162 FS 280 FLOORBEAM CRACKED AT RIGHT AND LEFT BUTTLINE 9, DISCOVERED AT C-CHECK. INSTALLED CROSS BEAM SPLICE AT FS 280 PER REO 670-53-11-047. INSTALLED INTERCOSTALS PER CRJ700 SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007060100052 20070601 00052 EA 2007 6 1 SWIA200718271 1 20070501 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 668CA 10162 LEFT WEB AT FS 280 BULKHEAD IS CORRODED, DISCOVERED AT C-CHECK. INSTALLED REPLACEMENT WEB IAW CRJ700 SRM TASK 51-42-06- 001-001-A01 AND 51-42-21-001-001-A01. 2 L 7 2 4F RT A21EA 2007060100053 20070601 00053 EA 2007 6 1 SWIA200718272 1 20070501 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 668CA 10162 RIGHT WEB AT STA 280 BULKHEAD IS CORRODED, DISCOVERED AT C-CHECK. INSTALLED REPLACEMENT WEB IAW CRJ700 SRM TASK 51-42-0 6-001-001-A01 AND 51-42-21-001-001-A01. 2 L 7 2 4F RT A21EA 2007060100057 20070601 00057 EA 2007 6 1 SWIA200718276 1 20070408 A 5743 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT WING WW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 924SW 7681 LEFT WHEEL WELL BRAKE TRANSDUCER BRACKET IS CRACKED, DISCOVERED AT C-CHECK. REPLACED LEFT TRANSDUCER BRACKET PER SRM 51 -42-06 PGS 1-18, P/N: 601R75262-159. 2 L 7 2 4F RT A21EA 2007060100059 20070601 00059 EA 2007 6 1 SWIA200718279 1 20070408 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 924SW FS 280 FLOORBEAM UPPER ANGLE IS CRACKED AT RBL9, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS AND CLIPS IAW CRJ200 REO 601R-53-11-137 STEP 7 & 8. 2 L 7 2 4F RT A21EA 2007060100062 20070601 00062 WP 2007 6 1 07FDEA01966 1 20070525 A 5322 SHEAR TIE DOUG DC10 DC1010 3022110 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 AFT FUSE ATTIC ZONE FOUND 1 CRACK ON SHEAR TIE UPPER VERTICAL BULKHEAD LT SIDE. REPAIRED IAW SRM 53-30-00 FIG 2B VOL 1. 2 L 7 3 4F A22WE 2007060100063 20070601 00063 NM 2007 6 1 NWAA070975513 1 20070526 A 2120 FILTER BOEING 757 757251 1384970 NM EQUIP COOLING DIRTY A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 513US 23201 DURING CLIMB-OUT LAS HAD A BURNING ODOR IN COCKPIT. TURNED UTILITY BUSS SWITCHES OFF. ODOR KEPT GETTING WORSE. TURNED LEFT PACK OFF, SAW SMOKE COMING FROM F/O'S GASPER. TURNED EQUIPMENT COOLING FAN TO ALTERNATE. DIVERTED TO DENVER. MAI NTENANCE: TROUBLE/SHOOTING SYSTEM IAW MM 21-00-01. INSPECTED AIR CONDITIONING SYSTEM, FOUND RECIRCULATION AIR FILTER AN D EQUIPMENT COOLING FILTER VERY DIRTY. REPLACED BOTH FILTERS IAW MM 21-25-02. RAN PACKS FOR SEVERAL HOURS, NO ODOR NOT ED. A/C OK TO CONTINUE SERVICE. 2 L 7 2 4F RT A2NM 2007060100066 20070601 00066 NM 2007 6 1 NWAA071965520 1 20070525 A 3397 WIRE BOEING 757 757251 1384970 NM EMERGENCY LIGHT CUT A NWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 01 520US 23208 FIRST CLASS EMERGENCY FLOOR PROXIMITY LIGHTS WILL NOT TEST. FOUND FLOOR PROXIMITY LIGHT WIRES CUT AND SEAT TRACK COVER INSTALLED INCORRECTLY AT SEATS 2 C/D. REPAIRED WIRES PER SWPM 20-15-26, OPS CHECKS GOOD. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2007060100068 20070601 00068 NM 2007 6 1 NWAA071985503 1 20070528 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM EMERGENCY LIGHTS MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 503US 23192 EMERGENCY FLOOR PROXIMITY LIGHTS IN AFT CABIN ON FLOOR ARE DIM. REMOVED AND REPLACED POWER SUPPLY (WITH BATTERY). LIGH T CHECKS NORMAL. 2 L 7 2 4F RT A2NM 2007060100069 20070601 00069 WP 2007 6 1 07FDEA01963 1 20070524 A 5512 SKIN DOUG DC10 DC1010 3022110 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 LT DETACHABLE UPPER SKIN FOUND 1 CRACK AND 10 RIVETS LOOSE RIVETS. REPAIRED SKIN IAW SRM 55-10-00 VOL 1 FIG 8 AND REPLA CED FASTENERS IAW SRM 51-35-02 VOL 2 PAR 12-10. 2 L 7 3 4F A22WE 2007060100071 20070601 00071 EU 2007 6 1 NWAA072063304 1 20070530 A 3350 POWER SUPPLY AIRBUS 330 A330323 3930335 EU EMERGENCY LIGHTS FAULTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 804NW 0549 THE (EPSU) EMERGENCY POWER SUPPLY UNIT FOR THE (LDMCR) LOWER DECK MOBILE CREW REST FAULTED DURING TEST. REMOVED AND REP LACED THE EPSU 32-3300-4-0074 AND CHECKED OK. 2 L 7 2 4F RT A46NM 2007060100072 20070601 00072 EU 2007 6 1 TRBA2007027 1 20070521 A 2120 41125A01 FLAPPER VALVE AEROSP ATR72 ATR72212A 8680902 EU GROUND AIR BROKEN A TRBA B EMER. DESCENT O OTHER CR CRUISE 1 SO 29 538AT 538 LOUD POP NOISE AT 15,000 FT FOLLOWED BY RAPID DECOMPRESSION. DESCENT MADE TO BELOW 10,000 FT, UNABLE TO PRESSURIZE FOR REMAINDER OF FLIGHT. REPLACED AIR GROUND CONNECTION FLAPPER VALVE AS PER MM 21-22-27. PERFORMED MANUAL PRESS CONTROLLE R SYSTEM OPT AS PER JIC 21-31-00. 2 H 7 2 4T RT A53EU 2007060100073 20070601 00073 WP 2007 6 1 07FDEA01968 1 20070525 A 5320 WEB DOUG DC10 DC1010 3022110 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 COCKPIT CRACK .25" LONG ON MEMBRANE. REPAIRED WEB IAW SRM 53-00-01 VOL 1 FIG 4 SHT 2. 2 L 7 3 4F A22WE 2007060100074 20070601 00074 WP 2007 6 1 07FDEA01969 1 20070525 A 5320 WEB DOUG DC10 DC1010 3022110 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 COCKPIT CORROSION WITH EXFOLIATION ON MEMBRANE AND 1 CRACK. 2 L 7 3 4F A22WE 2007060100075 20070601 00075 WP 2007 6 1 07FDEA01971 1 20070525 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 CTR CARGO COMPT BILGE ON CAP ANGLE FOUND MODERATE CORROSION WITH EXFOLIATION. REPAIRED CAP IAW SRM 53-30-00 VOL 1 FIG 8 . 2 L 7 3 4F A22WE 2007060100076 20070601 00076 WP 2007 6 1 07FDEA01972 1 20070525 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 CLG WHEEL WELL AREA CRACKS ON VERTICAL BULKHEAD. REPAIRED AREA IAW SRM 53-00-01 VOL 1 FIG 10 SHT 4. 2 L 7 3 4F A22WE 2007060100078 20070601 00078 WP 2007 6 1 07FDEA01974 1 20070525 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 NLG W/W FOUND 6 CRACKS ON RT SIDE VERTICAL BULKHEAD. REPAIRED BULKHEAD IAW SRM 53-40-00 FIG 34 VOL 1. 2 L 7 3 4F A22WE 2007060100079 20070601 00079 WP 2007 6 1 07FDEA01975 1 20070525 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 NLG W/W FOUND 1 CRACK .50" LONG ON RT SIDE VERTICAL BULKHEAD. REPAIRED AREA IAW SRM 53-30-00 FIG 6 SHEET 4 VOL 1. 2 L 7 3 4F A22WE 2007060100080 20070601 00080 WP 2007 6 1 07FDEA01976 1 20070525 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 CLG WHEEL WEEL AREA CRACK ON VERTICAL BULKHEAD. REPAIRED AREA IAW SRM 53-00-01 FIG 10 SHT 3 VOL 1. 2 L 7 3 4F A22WE 2007060100081 20070601 00081 EU 2007 6 1 TRBA200728 1 20070529 A 2612 51216052 FIRE LOOP AEROSP ATR72 ATR72212 8680945 EU NR 2 NACELLE FALSE INDICATION A TRBA O OTHER N FALSE WARNING AP APPROACH 1 SO 29 355AT 355 AT 200 FT ON APPROACH TO STT, NR 2 ENGINE GAVE FIRE WARNING INDICATION; EXTINGUISHED BY ITSELF ON LANDING. PERFORMED DV I AND ADJUSTMENT OF FIRE DETECTION LOOPS AS PER MM NR 26-12-61. AT THIS TIME FOUND TURBINE AMBIENT DRAIN CLOGGED. CLEA NED AS PER PWC NR 72-01-40. PERFORMED GROUND RUN-UP. OPS CHECK OK. 2 H 7 2 4T RT A53EU 2007060100085 20070601 00085 NM 2007 6 1 NWAA071996739 1 20070517 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 2000 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 639US 23887 DURING "M" CHECK, FOUND CRACK IN FRAME AT BS 2000 FROM S11R TO S12R. REPAIRED PER EA 67-209715. 2 L 7 4 4F A20WE 2007060100086 20070601 00086 NM 2007 6 1 NWAA072016739 1 20070508 A 5322 TENSION TIE BOEING 747 747251F 1384898 NM BS 840 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 639US 23887 DURING "M" CHECK, FOUND CRACK IN BS 840 TENSION TIE FRAME WEB NR 1 FASTENER HOLE. REPAIRED PER EA 67-209247. 2 L 7 4 4F A20WE 2007060100087 20070601 00087 NM 2007 6 1 NWAA072006739 1 20070514 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 420 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 639US 23887 DURING "M" CHECK, FOUND CRACKS IN FRAME WEB BS 420 AT S15R AND S17R. REPAIRED PER EA 67-29250 SECT I AND II SECTION III TO BE ACCOMPLISHED TO COINCIDE WITH INSPECTIONS PER SB 747-53A2265 UNTIL COMPLETION OF SECTION 41 MOD. 2 L 7 4 4F A20WE 2007060100090 20070601 00090 SO 2007 6 1 SWIA200718261 1 20070518 A 2121 AE1711AA0 COOLING FAN EMB 120 EMB120ER 3260203 SO CABIN SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 297SW 15921 15921 120327 SMOKE IN CABIN AFTER LANDING. REPLACED LEFT GROUND COOLING FAN IAW MM 21-51-03. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007060100091 20070601 00091 EA 2007 6 1 SWIA200718262 1 20070530 A 2913 6619003 PUMP CNDAIR CL600 CL6002D24 1390016 EA HYD SYSTEM LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 NM 07 807SK 15082 ON LANDING RECEIVED AN EDP 1 CAUTION MSG. FOUND LEAK IN THRUST REVERSER ACTUATION SYSTEM. REPLACED LEFT ENGINE EDP IAW 29-11-01. ALSO, REPLACED INBOARD PRESSURE LINE. OPS AND LEAK CHECK GOOD. OPS CHECK GOOD ON THRUST REVERSER, P/N AE71 1152-04. 2 L 7 2 4F RT A21EA 2007060100096 20070601 00096 NM 2007 6 1 C1HA200796009 1 20070529 A 5322 52427629 TENSION TIE BOEING 727 7272J4 1384006 NM BS 1186 S22L CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 696CA 22574 AFT CARGO AT BS 1186 TENSION TIE FITTING AT STR 22L IS CORRODED. REMOVED DAMAGED FITTING AND INSTALLED NEW TENSION TIE FITTING PN 65-24276-26, IAW B727 SRM 51-30-2 FIG 15. 2 L 7 3 4F RT A3WE 2007060100097 20070601 00097 NM 2007 6 1 C1HA200796010 1 20070529 A 5313 14981437075T6 STRINGER BOEING 727 7272J4 1384006 NM BS 312 S21R CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 696CA 22574 CORROSION STA 312 ON STRINGER 21R. CUT OUT DAMAGED AREA OF STR 21R AND REPAIRED STRINGER 21R IAW B727 SRM 53-10-3 FIG 1 . 2 L 7 3 4F RT A3WE 2007060100098 20070601 00098 NM 2007 6 1 C1HA200796005 1 20070529 A 5313 14981477075T6 STRINGER BOEING 727 7272J4 1384006 NM BS 740 S27R CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 696CA 23378 CORROSION STRINGER 27R AT STA 740. REPAIRED STRINGER 27R AT STA 740 IAW B727 SRM 53-10-3 FIG 7. 2 L 7 3 4F RT A3WE 2007060100099 20070601 00099 NM 2007 6 1 C1HA200796011 1 20070529 A 5311 FRAME BOEING 727 7272J4 1384006 NM BS 312 CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 696CA 22574 CORROSION STA 312 AT DOGHOUSE, RT. REPAIRED FRAME AS REQUIRED IAW B727 SRM 53-10-4 FIG 14. 2 L 7 3 4F RT A3WE 2007053000207 20070530 00207 NM 2007 5 30 USAA200705U09 1 20070523 A 5311 FRAME BOEING 737 737401 1384701 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 A 1 INCH LONG CRACK FOUND AT BS 440, S-24R. CLT - REPAIR: REMOVED DAMAGE, FABRICATED & INSTALLED FILLER & REPAIR ANGLE S PER EA 98691. 2 L 7 2 4F RT A16WE 2007053000208 20070530 00208 NM 2007 5 30 2007UALA01398 1 20070503 A 2810 10065500002 SENSOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RT FUEL TANK FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 664UA 29236 FUEL IMBALANCE 2600LBS AFTER 5 HOURS FLT. PROCESSOR FAULT HISTORY INDICATES RT MAIN DENSITOMETER MAY NEED TO BE REPLACE D. RT WING DENSITOMETER WAS REPLACED ON PTT 9832010. FLOAT REPLACED ON PTT 9832014 ON 05MAY2007. REMOVED AND INSTALLE D NEW RIGHT MAIN FUEL TANK DENSITOMETER. OLD S/N 5410, NEW S/N 1822. BITE CK GOOD. SUSPECT CALIBRATION DRIFT CAUSED FA ULTY SENSOR INPUT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007053000209 20070530 00209 NM 2007 5 30 2007UALA01410 1 20070504 A 3244 6F16112518 TIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LT MLG SEPARATED A UALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 29 180UA 25224 WORSENING VIB & FUEL OVERBURN CAUSED FLT TO DIVERT. *S/D* VIBRATION CAUSED BY SUSPECTED BLOWN TIRE(S) DEPARTING OUT OF SYD. LEFT REAR TIRE BLOWN ON LEFT BODY GEAR. WING TO BODY FAIRING PANEL 193CL DAMAGED BY THROWN TREAD. REPLACED BOTH NR 3 & 4 TIRES. REINSTALLED BODY FAIRING PANEL WITH INTERIM REPAIR ACCOMPLISHED. BODY PANEL DAMAGE NOTED AS CAUSE OF VIBRATION ON LEFT SIDE. PANEL DAMAGE CAUSED ADD'L DRAG RESULTING IN HIGHER FUEL BURN. 2 L 7 4 4F 4 F RT A20WE E24NE 2007053100003 20070531 00003 2007 5 31 UPS07849859 4 20070526 A 2565 SLIDE DOUG DC8 DC871F 302199D WP FWD ENTRY DOOR UNSECURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:N/A THE FWD ENTRY DOOR EMERGENCY SLIDE IS SLIPPING OUT OF ITS CONTAINER. FWD ENTRY DOOR SLIDE RESECURED IAW DC8 AMM 25-60-01-2. 2 L 7 4 4F RT 4A25 2007053100004 20070531 00004 2007 5 31 UPS07849860 4 20070525 A 2565 SLIDE DOUG DC8 DC873F 302199F WP DISLODGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 SLIDE FELL OUT OF CONTAINER WHEN OPENING EXIT DOOR. REINSTALLED SLIDE IAW MM 25-60-01-2. 2 L 7 4 4F RT 4A25 2007053100012 20070531 00012 SO 2007 5 31 C2XA07IA122 1 20070523 A 5100 8151138 COUPLING EMB 135 EMB135LR 3260305 SO DUAL TORQUE LOOSE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 27 28529 145512 IAH - FLIGHT 2479, THE CREW REPORTED A STRONG ELECTRICAL BURNING ODOR IN THE COCKPIT AND FWD CABIN ON LANDING. MAINTENA NCE INSPECTED THE AIRCRAFT AND PLACED THE NR 1 PACK ON MEL 21-60-05/1 CAT C, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON FLIGHT 2466, THE AIRCRAFT RETURNED TO IAH WHERE MAINTENANCE RESECURED A LOOSE COUPLING ON THE NR 1 DUAL TO RQUE MOTOR VALVE, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE RVICE. 2 L 7 2 4F RT T00011AT 2007053100013 20070531 00013 NM 2007 5 31 USAA200705U13 1 20070528 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 56951 23595 ONE CRACK APPROX 16 INCHES LONG AT STA 500 BL 0 AT LOWER FWD VHF ANTENNA. [SUP 06-07-07] INSTALLED EXTERNAL DOUBLER 1 1" X 31" PER EA 84619. 2 L 7 2 4F RT A16WE 2007053100016 20070531 00016 WP 2007 5 31 ASAA0781718 1 20070530 A 5320 593096125 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP BS 1098-1212 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 PASSENGER CABIN FLOOR SUPPORT IS CORRODED. FABRICATED AND INSTALLED A REPLACEMENT FLOOR SUPPORT IAW SRM 51-10-4 PG 1 AN D 51-30-1 PG 4. 2 L 7 2 4F RT A6WE 2007053100018 20070531 00018 WP 2007 5 31 ASAA0781720 1 20070530 A 5320 99365495 CUSP WEB DOUG DC9 DC983 3022083 WP BS 160-200 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 PASSENGER CABIN FLOOR RT CUSP WEB IS CRACKED. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4 932106. 2 L 7 2 4F RT A6WE 2007053100021 20070531 00021 WP 2007 5 31 ASAA0781723 1 20070530 A 5320 993053813 CUSP WEB DOUG DC9 DC983 3022083 WP BS 389-503 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 PASSENGER CABIN CUSP WEB IS CORRODED. REMOVED CORRODED WEB LOCATED DRILLED AND INSTALLED A REPLACEMENT WEB IAW SRM 51-3 0-2. 2 L 7 2 4F RT A6WE 2007053100037 20070531 00037 NM 2007 5 31 2007UALA01634 1 20070523 A 5347 CARGO TRACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BS 1850 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 181UA 25278 AFT CARGO PIT STA 1850 2ND CARGO TRACK FROM ENTRANCE HAS 10 INCH CRACK AT PALLET LOCKDOWN AREA. [SUP 05-29-07] MAJOR R EPAIR ACCOMPLISHED: INSTALLED NEW TRACK SECTION FROM AFT END TO EXISTING SPLICE SECTION IN AFT PIT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007053100040 20070531 00040 NM 2007 5 31 2007UALA01637 1 20070525 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 DOORWAY 2L UPPER SILL, AFT EMERGENCY EXIT LIGHT INOP. REPLACED LAMP. OP CHECKED OK RE F MM 33-51-05. ACPD ON. 2 L 7 4 4F 4 F RT A20WE E24NE 2007053100042 20070531 00042 NM 2007 5 31 2007UALA01639 1 20070525 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 RIGHT OVERWING EMERGENCY EXIT LIGHT INOP, 2ND FROM FWD POSITION. LAMP INOPERATIVE. [SUP 06-06-07] RELAMPED, OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007053100067 20070531 00067 2007 5 31 RAIA00705040 2 20070521 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO NR 2 INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 811HK 145256 FLT NR 5535 - STL - NR 2 ENGINE WILL NOT START. MAINTENANCE DEFERRED APU PER MEL. 2 L 7 2 4T RT T00011AT 2007053100074 20070531 00074 NE 2007 5 31 HNAA0700090 2 20070521 A 7324 311851201B FLOW DIVIDER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE NR 2 ENGINE MALFUNCTIONED A HNAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 07 827EX 12 12 390 121185 NR 2 ENGINE POWER LOSS MOMENTARILY OF 30 TO 40 PERCENT TQ HAPPENED 3 TIMES ON CLIMBOUT. AIRCRAFT RETURNED TO FIELD AFTE R TAKEOFF. LGA MAINTENANCE INSPECTED THE ENGINE CONDITION PANEL. CREW REPORTED THAT ENGINE PARAMETERS ALSO DROPPED WIT H TORQUE AND CREW FELT ENGINE SLOW DOWN. RETURNED TO FIELD 5 TO 7 SECONDS. LGA MAINTENANCE INSPECTED LOW PRESSURE FUEL FILTER NO DEBRIS FOUND. LGA MAINTENANCE REMOVED AND REPLACED FUEL FLOW DIVIDER OPS AND LEAK CHECK GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2007053100078 20070531 00078 NM 2007 5 31 HNAA0700092 1 20070508 A 5313 85320056103 STRINGER DHAV DHC8 DHC8102 2809003 NM BS 291 S31R CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 938HA 47703 152 CORRODED RIGHT UNDERFLOOR. CORROSION ON STRINGER 31 AFT OF STATION 291. AT STRINGER 31 FRAME X291 PREVIOUS REPAIR REPL ACED AS PER SRM 53-20-21. 2 H 7 2 4T RT A13NM 2007053100087 20070531 00087 EA 2007 5 31 TRAX200700718 1 20070523 A 5210 BRACKET CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 684BR 7708 PAX DOOR AFT CABLE COUNTER BALANCE ANCHOR BRACKET CRACKED. 2 L 7 2 4F RT A21EA 2007053100091 20070531 00091 NM 2007 5 31 USAA200705U11 1 20070525 A 5330 SKIN BOEING 737 7374B7 1384702 NM BS 727 S23L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 451UW 24934 A 3 INCH CRACK FOUND JUST FWD OF STA 727GLH JUST ABOVE STR 23L. INSTALLED FILLER & DOUBLER PER SRM 53-00-01 FIG 201. 2 L 7 2 4F RT A16WE 2007053100105 20070531 00105 NM 2007 5 31 USAA200705U08 1 20070524 A 5330 SKIN BOEING 737 7374B7 1384702 NM BS 750 S23L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 451UW 24934 A 3 INCH CRACK FOUND AT STR 23L AT STA 750L. REPAIR: FILLER & DOUBLER INSTALLED PER SRM 53-00-01 FIG 201. 2 L 7 2 4F RT A16WE 2007053100110 20070531 00110 EA 2007 5 31 TRAX200700696 1 20070520 A 2560 BATTERY CNDAIR CL600 CL6002B19 1900309 EA FLASHLIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 686BR 7715 F/O`S FLASHLIGHT BATTERIES INOP. 2 L 7 2 4F RT A21EA 2007053100133 20070531 00133 NM 2007 5 31 DHL2007783500 1 20070525 A 3200 UNKNOWN BOEING 727 727227 1384078 NM MLG UNKNOWN A DHLA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 783DH 21999 DURING INBOUND TEST FLIGHT FOR C-CHECK MANUAL GEAR EXTENSION, UNABLE TO EXTEND RIGHT MAIN GEAR. PERFORMED SPECIAL PROCE DURES, RIGHT MAIN DOOR DAMAGE NOTED ON LANDING. AIRCRAFT WAS JACKED IN HANGER AND TRIED TO DUPLICATE PROBLEM. UNABLE T O DUPLICATE PROBLEM. THIS AREA WILL BE LOOKED AT IN FURTHER DETAIL DURING C CHECK. AIRCRAFT INDUCTED INTO C CHECK THIS DATE. 2 L 7 3 4F A3WE 2007053100138 20070531 00138 NM 2007 5 31 07FDEA01837 1 20070517 A 5753 65192497 FLAP TRACK BOEING 727 7272S2F 1384O81 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 LT WING TE IB FLAP OB TRACK IS CORRODED AT FWD END AND SPOILER SPPT ATTACH POINT LT WING INBD T/E FLAP OUTBD (NR3) FLAP TRACK REPLACED ON FED EX W/C 27X5705-03. 2 L 7 3 4F A3WE 2007053100139 20070531 00139 WP 2007 5 31 07FDEA01838 1 20070517 A 5711 SPAR CAP DOUG DC10 DC1010F 3022111 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 RT WING HAS CORROSION ON AFT UPPER SPAR CAP STA.XORS 718 TO733. REMOVED CORROSION IAW DC/MD SRM 51-21-01 VOLII AND FEDE X EA 8-5710-109151, WINGS, RT WING SPAR CORROSION BETWEEN STA XORS 480-733. REPAIR, ALODINED AND PRIMED IAW DC10 SRM 51 -21-01 VOLII. 2 L 7 3 4F A22WE 2007053100140 20070531 00140 WP 2007 5 31 07FDEA01839 1 20070517 A 5347 AGA385517 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 IN THE AFT PIT, THE SEAT TRACKS AT ABOUT BS 1787 TO BS 1981, RBL 20R AND LBL 20L BS 1841 LBL 59L HAVE DEBRIS, LIGHT CORR OSION AND MINOR SCRATCHES. REMOVED, FABRICATED, AND INSTALLED TRACKS IAW DC/MD10 SRM 53-70-00 VOL I FIG 1 SHT 1- 4, AND DAC DRAWING AGA 3855 REV.N. 2 L 7 3 4F A22WE 2007053100155 20070531 00155 WP 2007 5 31 07FDEA01935 1 20070522 A 5320 ADA00556 RETAINER DOUG DC10 DC1010 3022110 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 FWD CARGO CUTOUT DOOR 2 CRACKS ON RETAINER SEAL AND DEEP WEAR ON EXISTING REPAIR SKIN. SKIN REPAIRED IAW SRM 53-20-00 F IG 6 AND 53-50-00 FIG 26 VOL 1. SEAL RETAINER REPLACED IAW SRM 51-30-00 VOL 2. 2 L 7 3 4F A22WE 2007053100159 20070531 00159 NM 2007 5 31 07FDEA01946 1 20070522 A 5313 ASA7112527 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 AFTER BLANKET REMOVAL FOR WINDOW FRAME INSPECTION, MAIN DECK CARGO COMPARTMENT, RIGHT LONGERON 24R SPLICE STA 5-123 FO UND CRACKED. MAIN DECK CARGO COMPARTMENT - RIGHT HAND LONGERON 24R CRACKED SPLICE STA 5- 123 REMOVED AS PER SRM 51-3 1-01 VOLUME II. NEW SPLICE FABRICATED AS PER DOUGLAS DRAWING NO.: A5A7112 AND INSTALLED AS PER SRM 51-31-01 VOLUME I I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007053100166 20070531 00166 NM 2007 5 31 07FDEA01853 1 20070519 A 5753 65192497 FLAP TRACK BOEING 727 7272S2F 1384O81 NM ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 LT WING TE IB FLAP OB TRACK UPP OB FLG WEAR STEP HAS GOUGES/ HIGH METAL 5" - 32" FROM AFT END. LT WING INBD T/E FLAP OU TBD (NR 3) FLAP TRACK REPLACED ON W/C 27X5705-03. 2 L 7 3 4F A3WE 2007053100169 20070531 00169 EU 2007 5 31 07FDEA01856 1 20070519 A 5330 SKIN AIRBUS 310 A310203 3930313 EU FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 LOWER EXTERNAL FUSELAGE SKIN HAS CREASE BETWEEN FR 66 TO FR 67 AND STGR 52R TO STGR 54R APPROX 6 IN CREASE ON FUSELAGE S KIN FOUND TO BE OUT OF LIMIT IAW SRM 53-10-12 FIG 110. REMOVED DAMAGED AREA IAW SRM 53-10-12, FABBED DOUBLER REPAIR MAT ERIAL/2024-T3 .100C BATCH NR 251819 IAW SRM 53-10-12 FIG 226, 224 SRM 53-17-12 FIG 3 SHEET 8. INSTALLED DOUBLER REPAIR IAW SRM 53-10-12 FIG 226. 2 L 7 2 4F RT A35EU 2007053100177 20070531 00177 NM 2007 5 31 07FDEA01859 1 20070520 A 5343 ACA7017501 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 NOSE LANDING GEAR LEFT TRUNNION FITTING FOUND WITH CRACKED. [SUP 06-08-07] NOSE LANDING GEAR LEFT HAND TRUNNION FITTIN G CARRIED OUT REPAIR AS PER SRM 53-40- 00 VOLUME I, FIGURE 23 AND FEDEX E.A.1-5310-111106, REPAIR CLASSIFIED AS MAJO R PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007053100179 20070531 00179 NM 2007 5 31 07FDEA01861 1 20070520 A 5730 ARB2886504 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RIGHT WING LEADING EDGE WING ANTI-ICE TELESCOPIC DUCT CUT-OUT STA XOS 464 AND STA 469 FOUND CRACKED. [SUP 06-08-07] REPAIRED AS PER SRM 57-10-00 VOLUME I, FIGURE 43. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007053100185 20070531 00185 NM 2007 5 31 07FDEA01955 1 20070523 A 5347 4CA7399501 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 AFTER CEILING REMOVAL, 1 CRACK FOUND ON SEAT TRACK LOWER SURFACE AT STA 750 LBL 44. [SUP 06-08-07] REPAIR CARRIED OUT AS PER 53- 70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007053100187 20070531 00187 EU 2007 5 31 07FDEA01507 1 20070416 A 5512 A5517874000100 SKIN AIRBUS 310 A310324 3930206 EU ZONE 300 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 801FD 539 THS - FRACTION 341BB AT L/E OF RT THS W/UPPER SKIN SURFACE W/DENT REPAIRED PER SRM 55-12-12 FIG 203. REPAIR EVALUATED P ER GMM 6-2-100 AND CLASSIFIED AS "MAJOR". 2 L 7 2 4F RT A35EU 2007060100003 20070601 00003 NM 2007 6 1 DL76L070603 1 20070526 A 3610 SHUTOFF VALVE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE RT ENGINE INOPERATIVE A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 186DN 27962 724143 RT ENG PRSOV DID NOT OPEN AFTER PUSHBACK. FOUND C/P LOOSE ON THE PRSOV. SECURED SAME. OPN OF PRSOV NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007060100004 20070601 00004 NE 2007 6 1 DL76L070604 2 20070526 A 7230 COMPRESSOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 180DN 45744 25985 724143 SET UP TO PERFORM BORO INSP OF THE LEFT ENG HPC 5TH-15TH STAGES PER AMM 7200-00-206-344-NOO. THIS DUE TO ENG TREND ALER T AND PREV SURGE REPORT. FOUND DAMAGE TO THE 7TH STAGE HPC AND AFT. REPLACED LT ENG. 2 L 7 2 4F 4 F RT A1NM E24NE 2007060100006 20070601 00006 NM 2007 6 1 DL757070606 1 20070527 A 5330 143N34714 SKIN BOEING 757 757232 1384965 NM FS 495 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 REPAIR OF DENT AND GOUGE AT FS 495 AND STRINGER 28R. DAMAGE CUTOUT AND DOUBLER INSTALLED. 2 L 7 2 4F RT A2NM 2007060100007 20070601 00007 NM 2007 6 1 DL76L070607 1 20070527 A 2410 IDG BOEING 767 767332 1382001 NM NR 1 ENG MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 1201P 28458 DURING TAXI ON SINGLE ENGINE THE LEFT GEN TRIPPED OFFLINE. A SINGLE RESET WAS ATTEMPTED PER QRH. GEN TRIPPED AGAIN AFT ER 20 SECONDS. APU WAS STARTED AND CARRIED THE LOAD NORMALLY. LEFT ENG EEC C1 STATUS MESSAGE ALSO DISPLAYED. TRIED G CU NO HELP. DELTA P POPPED. REMOVED NR 1 ENGINE IDG PER M/M. INSTALLED NR 1 IDG PER M/M. RAN NR 1 ENGINE. CHANGED N R 1 IDG FILTER. NO DEBRIS FOUND. LEAK CHECK GOOD. OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 2007060100012 20070601 00012 NM 2007 6 1 DLM88070612 1 20070527 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 737 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 EXFOLIATION CORROSION ON RT CUSP WEB AT STA Y=737 ON UPPER AND LOWER SURFACE. DOUBLER REPAIRED AND INSTALLED PER ERA 39 8191-14MA REV A. 2 L 7 2 4F RT A6WE 2007060100020 20070601 00020 EU 2007 6 1 07FDEA01957 1 20070524 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 AVIONICS COMPARTMENT FR 16A- FR17, OUTBOARD SIDE STR 44 LT 4 SQ IN CORROSION REMOVED 9 FASTENERS FOR FOM PER A310-200 SR M 51-40-21. REMOVED CORROSION PER A310-200 SRM 51-74-10. MATERIAL BEFORE .063 AFTER .041 LOSS OF .021 FOUND TO BE OUT OF LIMITS PER A310-SRM 53-10-00. COMPLIED WITH EA 6-5310-110480. REINSTALLED FASTENERS PER A310 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007060100038 20070601 00038 NM 2007 6 1 DL76L070595 1 20070524 A 4950 97980612 VALVE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE APU UNSERVICEABLE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 175DN 34380 24803 P1073 A/C RTN TO STAND LOW AIR PRESS FROM APU ENG WOULD NOT START APU AIR SUPPLY INOP MCO/PLACARD, INSTALLED PER MEL 49-11-01C . FOUND SURGE BLEED VLV STUCK IN OPEN POSITION CHANGED SAME, OP NOW NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007060100039 20070601 00039 NM 2007 6 1 DLM88070596 1 20070523 A 5753 VANE DOUG MD88 MD88 3023688 NM TE FLAPS DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 INAPPROPRIATE REPAIR AND DELAMINATION WERE REPAIRED TO A LT WING OUTBD FLAP CENTER FIXED GUIDE VANE, NEAR THE INBD END. REPAIR INCLUDED A 16" WIDE SKIN SPLICE, AND A SECOND 11" WIDE DOUBLER. THE REPAIR IS PERMANENT. 2 L 7 2 4F RT A6WE 2007060100049 20070601 00049 EA 2007 6 1 SWIA200718268 1 20070527 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 960SW 7853 CAPTAINS SIDE WINDOW IS CRACKED. REPLACED LEFT SIDE WINDOW IAW AMM 56-12-01, P/N OFF: NP139322-001, S/N OFF: 03161H608 3. 2 L 7 2 4F RT A21EA 2007060100065 20070601 00065 EU 2007 6 1 NWAA071953236 1 20070524 A 3350 POWER SUPPLY AIRBUS 320 A320212 3930322 EU EMERGENCY LIGHTS NO TEST A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 336NW 355 LEFT FORWARD EMERGENCY LIGHT POWER SUPPLY INTERNAL TEST FAILS (LIGHT HANGS UP). REPLACED LEFT FORWARD EMERGENCY LIGHT P OWER SUPPLY CHARGER UNIT, TESTS OK. 2 L 7 2 4F RT A28NM 2007060100070 20070601 00070 WP 2007 6 1 IXXA07SMN155S 1 20070421 A 5720 S2769796 FITTING DOUG DC8 DC871F 302199D WP ZONE 500 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD SLOT VANE FITTING WITH CORROSION AT STATION XILD 0.7095. REM OVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. FABRICATED NEW FITTING. CLEANED, TREATED AND PRIMED A REA AND FITTING. APPLIED SEALANT TO FAYING SURFACE. INSTALLED NEW FITTING IAW DC8 SRM 57-3-1 FIGURE 8 PAGE 15, DC8 SRM 51-1-8, PAGES 17-18, DC8 SRM 57-2-0, PAGE 16, DC8 SRM 57-1-0, PAGE 1, AND DC8 SRM 51-1-21, DC8 SRM 57-3-1, FIGURE 8 PA GE 15 ITEM D, DC8 SRM 51-2-0 PAGE 75 FIGURE 50, AND SHEET 73, DC8 SRM 51-1-8B, AND DC8 SRM 51-1-11. 2 L 7 4 4F RT 4A25 2007060100083 20070601 00083 WP 2007 6 1 IXXA07SMN154S 1 20070421 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP ZONE 200 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FLOORBEAM WEB CORRODED AT STATION 960.000 RT BOTTOM LINE 40". REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR, REMOVED CORROSION. FOUND OUT OF LIMIT. FABRICATE REPAIR ANGLES O F EXTRUSION. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACE. INSTALLED REPAIR P ARTS IAW DC8 SRM 51-2-1 FIGURE 1 SHEET 1, 2, 3 AND 12 T/R 51-130 DATED 01-26-04, SRM 51-1-20D, DC8 SRM 51-1-8 PAGE 17-18 , DC8 SRM 53-2-0 PAGE 2P, DC8 SRM 53-7-1 FIGURE 13 ITEM R, DC8 SRM 51-2-0 FIGURE 50 SHEET 76, DC8 SRM 51-1-8B, DC8 SRM 5 1-1-11, AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007060100094 20070601 00094 NM 2007 6 1 C1HA200796004 1 20070529 A 5260 651751737 SUPPORT BRACKET BOEING 727 7272J4 1384006 NM AIRSTAIR CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 696CA 22574 AFT AIRSTAIR AREA STA 1263 RT ANGLE SUPPORT BRACKET IS CRACK APPROX 1/2 INCH LONG INSIDE LIGHTNING HOLE. REMOVED CRACKE D SUPPORT ANGLE ON AFT AIRSTAIR STA 1263 RT AND REPLACED WITH NEW IAW B727 SRM 51-30-5 FIG 1 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007060100100 20070601 00100 NM 2007 6 1 C1HA200796003 1 20070529 A 5320 65258152 PAN BOEING 727 7272J4 1384006 NM LAVATORY SERVICE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 696CA 22574 AFT LAV SERVICE PAN AT RT BS 1170 IS DAMAGED AND CORRODED BEYOND LIMITS. DRILLED NEW PAN PN 65-25815-2 AND INSTALLED PA N IAW B727 MM 51-30-*2 FIG 1 AND 15. LEAKED CHECK OK PER B727 MM 38-32-11. 2 L 7 3 4F RT A3WE 2007060100101 20070601 00101 NM 2007 6 1 C1HA200796001 1 20070529 A 5740 658251715 ATTACH FITTING BOEING 727 7272J4 1384006 NM LT WING CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 696CA 22574 LEFT WING NR 2 FLAP TRACK FWD ATTACH FITTING CORRODED AT LUG FACE. REMOVED L/W NR 2 FLAP TRACK FWD ATTACH FITTING AND M ACHINED FITTING CORRODED FACE PER SOPM 20-10-02. TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED IAW B727 SRM 51- 30-2 FIG 15. 2 L 7 3 4F RT A3WE 2007060100102 20070601 00102 NM 2007 6 1 C1HA200796002 1 20070529 A 5730 SKIN BOEING 727 7272J4 1384006 NM LT WING CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 696CA 22574 LT LOWER WING SURFACE APPROX BS 800 IN RAM AIR AREA IS CORRODED (PLENUM). BLENDED OUT DAMAGED AREA AND REPAIRED IAW EO- 727-5710-04 REV IR. 2 L 7 3 4F RT A3WE 2007060100103 20070601 00103 NM 2007 6 1 C1HA200796006 1 20070529 A 5313 652427624 STRINGER BOEING 727 7272J4 1384006 NM BS 1183 S26L CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 696CA 22574 CORROSION STRINGER 26L TENSION FITTING AT 1183. REMOVED AND REPLACED BS 1183 STR 26L TENSION FITTING PN 65-24276-24 PO NR 720764 IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007060100105 20070601 00105 EA 2007 6 1 SWIA200718265 1 20070528 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 955SW 7817 FIRST OFFICERS SIDE WINDOW IS CRACKED. REPLACED FIRST OFFICERS SIDE WINDOW IAW AMM 56-12-01.P/N OFF: NP-139322-001 S/N OFF: 03083H9458 2 L 7 2 4F RT A21EA 2007060100106 20070601 00106 2007 6 1 AMTA200700237 4 20070516 A 2565 SLIDE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE R4 DOOR NO TEST A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 701TZ 46583 R4 DOOR SLIDE FAILED TO DEPLOY ON TEST (AUTO AND MANUAL). REINSTALLED SLIDE SN 004456 FOR EVACUATION TEST IAW MM 25-61- 01. (K) REPLACED SLIDE IAW MM 25-61-01. (K) 2 L 7 3 4F 4 F A22WE E23EA 2007060100109 20070601 00109 NM 2007 6 1 C7WA200700001 1 20070429 A 5230 CONTROLLER BOEING 727 7272Q6 138407V NM PWA JT8 JT8D17R 52049 NE CARGO DOOR SMOKE A C7WA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 29 1279E 21971 ON CLIMBOUT FROM SJU FLIGHT ENGINEER SMELLED SMOKE AND TRIED TO ID SOURCE. ACCOMPLISHED AOM PROCEDURE AND REMOVED POWER FROM CARGO DOOR CONTROL. SMOKE STOPPED AND RETURNED FOR INSPECTION. [06-21-07] INSPECTION OF CARGO DOOR CONTROL AR EA REVEALED THE HYDRAULIC PUMP CONNECTOR PLUG CONNECTED TO THE CONTROL BOX WAS SHORTED AND THE CONTACTS BURNED. REMOVED AND REPLACED CONNECTORS PN MS3102R24-10P AND MS3106F24-10S. OPS CHECK GOOD IAW AEI MAINTENANCE MANUAL. (K) 2 L 7 3 4F 4 F RT A3WE E2EA 2007060100110 20070601 00110 NM 2007 6 1 AMTA200700233 1 20070505 A 3040 HEATER BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT WINDOW INOPERATIVE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 560TZ 33525 RT FWD WINDOW HEAT INOPERATIVE LIGHT ILLUMINATES INTERMITTENTLY AFTER LANDING. COULD NOT DUPLICATE WINDOW HEAT INOPERAT IVE ON GROUND, NO EICAS MSG APPEARED, PERFORMED WINDOW HEAT BITE IAW FIM 30-41-00, RECYCLE POWER SEVERAL TIMES, OPS NOR MAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007060100111 20070601 00111 NM 2007 6 1 AMTA200700227 1 20070504 A 5510 FAILSAFE BOEING 737 73783N 13844HI NM BS 1147 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 304TZ 30675 RT HORIZ STAB FAIL SAFE PIN PITTED 180A1612-2. REPLACED PIN WITH 180A1612-4, AMM 27-41-11-4. (K) TORQUE WRENCH ID NR 01-187T CAL DUE 08-21-07. (M) 2 L 7 2 4F RT A16WE 2007060400001 20070604 00001 SW 2007 6 4 AC2A114524 1 20070314 A 2997 CONNECTOR AGUSTA AB139 AB139 0260110 SW PWA PT6 PT6* 52043 EA BYPASS SWITCH DIRTY B AC2A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 07 139JP 31039 WHILE IN FLIGHT, NR 2 SERVO CAS LIGHT ILLUMINATED. ON HYDRAULIC SYSTEM SYNOPTIC PAGE, THE NR 2 FWD, RT, LT AND T/R SERVO S ALL INDICATED JAMS. EMERGENCY CHECK LIST WAS FOLLOWED AND AIRCRAFT RETURNED TO BASE. CLEANED ELECTRICAL CONNECTOR ON S ERVO BYPASS SWITCHES, INSPECTED HYDRAULIC SYSTEM COMPONENTS AND GROUND RUN. AIRCRAFT RETURNED TO SERVICE. 2 G 7 2 4U 3 T R00002RD E2NE 2007060400061 20070604 00061 WP 2007 6 4 ASAA0781734 1 20070529 A 5321 993653715 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 CABIN FLOOR PANEL HAS CORRODED INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53 05 PARA 11 AND DAC DWG S4932106 . 2 L 7 2 4F RT A6WE 2007060400062 20070604 00062 WP 2007 6 4 ASAA0781735 1 20070529 A 5321 99365881 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 200-256 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 CABIN FLOOR PANEL IS DELAMINATED. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007060400063 20070604 00063 WP 2007 6 4 ASAA0781736 1 20070529 A 5321 99365533 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 200-256 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 CABIN FLOOR PANEL HAS DAMAGED INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007060400064 20070604 00064 NM 2007 6 4 ASAA0741711 1 20070526 A 5280 65C2817829 DOOR BOEING 737 737490 1384715 NM MLG CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 706AS 28894 RIGHT MLG INNER DOOR LOWER T/E CRACKED. REPAIRED GEAR DOOR IAW SRM 53-80-02 REPAIR 2 DETAIL 2. 2 L 7 2 4F RT A16WE 2007060400065 20070604 00065 WP 2007 6 4 ASAA0781712 1 20070529 A 5330 595305077 SKIN DOUG DC9 DC983 3022083 WP BS 259-264 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 FUSELAGE SKIN IS DENTED AFT OF THE FWD LAVATORY SERVICE PANEL WITHIN 1 INCH OF LONGERON 20L. COLD WORKED SKIN, FABRICAT ED DOUBLER ,TREATED, PRIMED AND INSTALLED IAW SRM 51-10-3 PARA 23 AND 30. 2 L 7 2 4F RT A6WE 2007060400066 20070604 00066 WP 2007 6 4 ASAA0781713 1 20070529 A 5320 993053812 CUSP WEB DOUG DC9 DC983 3022083 WP BS 541-560 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 PASSENGER CABIN FLOOR CUSP WEB CORRODED. REMOVED CORROSION MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AN D REPLACED CUSP WEB IAW SRM 51-30-2 AND 51-30-1. 2 L 7 2 4F RT A6WE 2007060400067 20070604 00067 WP 2007 6 4 ASAA0781714 1 20070529 A 5320 99305389 CUSP WEB DOUG DC9 DC983 3022083 WP BS 598-712 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 PASSENGER CABIN FLOOR CUSP WEB CORRODED. REMOVED CORRODED CUSP WEB, LOCATED DRILLED AND INSTALLED A REPLACEMENT CUSP WE B IAW SRM 51-10-4 AND 51-30-2. 2 L 7 2 4F RT A6WE 2007060400068 20070604 00068 WP 2007 6 4 ASAA0781715 1 20070529 A 5330 5920323249 SKIN DOUG DC9 DC983 3022083 WP BS 508-512 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 FUSELAGE SKIN IS DENTED. INSTALLED REPAIR DOUBLER AT RIGHT EXT FUSELAGE. COLD FORMED SKIN BACK TO ORIGINAL BLUEPRINT C ONTOUR AND HFEC PRIOR TO DOUBLER INSTALLATION. ALL PER SRM 53-04 PG 218H. 2 L 7 2 4F RT A6WE 2007060400069 20070604 00069 WP 2007 6 4 ASAA0781725 1 20070530 A 5321 99365813 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 1078-1116 DETERIORATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 CABIN FLOOR PANEL IS BROKEN AT AN INSERT. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S49321 06. 2 L 7 2 4F RT A6WE 2007060400070 20070604 00070 WP 2007 6 4 ASAA0781726 1 20070530 A 5321 99365843 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 1117-1174 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 CABIN FLOOR PANEL IS DELAMINATED. FABRICATED A REPLACEMENT PANEL IAW SRM 53-05 PARA 44 AND DCA DWG S4932106. 2 L 7 2 4F RT A6WE 2007060400071 20070604 00071 WP 2007 6 4 ASAA0781727 1 20070530 A 5321 993664740 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 1116-1174 DETERIORATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 CABIN FLOOR PANEL HAS NUMEROUS DAMAGED INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007060400072 20070604 00072 WP 2007 6 4 ASAA0781728 1 20070530 A 5321 995252313 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 180-200 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 CABIN FLOOR PANEL HAS TEN DAMAGED INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932 106. 2 L 7 2 4F RT A6WE 2007060400073 20070604 00073 WP 2007 6 4 ASAA0781729 1 20070530 A 5321 99366923 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 1079-1155 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 CABIN FLOOR PANEL IS DELAMINATED. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007060400104 20070604 00104 WP 2007 6 4 AALA20070949 1 20070526 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 575AM 53152 DFW - OVERHEAD EMERGENCY LIGHTS FROM SEAT ROWS 13 TO 17 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT S FROM SEAT ROWS 13 TO 17. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007060400105 20070604 00105 WP 2007 6 4 AALA20070945 1 20070525 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 405A 49316 LGA - EMERGENCY LIGHTS AT EXTERIOR AFT OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT EXTERIOR AFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007060400106 20070604 00106 WP 2007 6 4 07FDEA01994 1 20070529 A 5312 NCA604463 BULKHEAD DOUG DC10 DC1010 3022110 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 FWD CARGO COMPT BILGE AREA FOUND 1 CRACK ON TEE CAP OF BLKHD. REPAIRED IAW EA NR 8-5310-96124. 2 L 7 3 4F A22WE 2007060400107 20070604 00107 WP 2007 6 4 07FDEA01995 1 20070529 A 5347 AEA7325525 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 1199 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 MAIN CABIN DEEP WEAR ON SEAT TRACK. REPAIRED SECTION OF SEAT TRACK IAW SRM 53-70-00 PAGE 4 VOL 1. 2 L 7 3 4F A22WE 2007060400108 20070604 00108 EU 2007 6 4 07FDEA01996 1 20070529 A 5340 A53978209 FITTING AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 CORROSION ON AFT CARGO DOOR LOCK FITTING REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007060400109 20070604 00109 EU 2007 6 4 07FDEA01997 1 20070529 A 5340 A53978209 FITTING AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 CORROSION ON AFT CARGO DOOR LOCK FITTING REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007060400110 20070604 00110 WP 2007 6 4 07FDEA01998 1 20070529 A 5512 ALC72061 SKIN PANEL DOUG DC10 DC1010 3022110 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 DURING INSP OF HORIZ STAB CONSTANT SECTION SKIN PANEL, FOUND THREE LOWER INTERIOR SKIN PNLS WITH CRACK, P/N 7205-1, P/ N 7204-1, P/N 7206-1. SEE ATTACHED SHEET FOR ALL REF (INSPECTION FINDING FORM). REPAIRED IAW EA NR 8-5510-96121. 2 L 7 3 4F A22WE 2007060400111 20070604 00111 WP 2007 6 4 07FDEA01999 1 20070529 A 5510 SE105500173 BALANCE WEIGHT DOUG DC10 DC1010 3022110 WP ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 RT OUTB ELEVATOR BALANCE WEIGHT WITH PAINT REMOVED AND LIGHT CORROSION. REPLACED BALANCE WEIGHT IAW CMM 55-21-01. 2 L 7 3 4F A22WE 2007060400112 20070604 00112 EU 2007 6 4 07FDEA02000 1 20070529 A 5311 A53973897 FRAME AIRBUS 300 A300B4605R 3930308 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 FOUND 5 TOO LARGE HOLES AT JACKING POINT C 59, P26-27 RHS REPAIR PERFORMED BY HI-LOK HL110VF8 IN PLACE HL110VF6 IAW EA 6 -5317-106466 AND RAS/DAHAM/4022180/2007 ISS. B 2 L 7 2 4F RT A35EU 2007060400113 20070604 00113 WP 2007 6 4 07FDEA02001 1 20070529 A 5712 ARB07431 RIB DOUG DC10 DC1010 3022110 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 RT WING LOWER RIB CHORD HAS 2 CRACKED LUGS CRACKS EXTEND ABOVE HORIZONTAL FLANGE OF CHORD. REPAIRED IAW SRM 57-20-00 FI G 21 SHT 1 VOL 1. 2 L 7 3 4F A22WE 2007060400114 20070604 00114 EU 2007 6 4 07FDEA02002 1 20070529 A 5321 A57110204 PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 MARKS, DENT, CRACKS AND NICKS AT C47-53, BETWEEN TRACK 5 LT AND 5 RT. REPAIR PERFORMED BY DOUBLER REPAIR AT INTERNAL WE B C47, DRESS OUT SKIN ON DIAPHRAGM , BLEND OUT DAMAGED AREAS IAW EA 6-5315-106463 AND RAS/051804/007/2007 8ISS. A 2 L 7 2 4F RT A35EU 2007060400115 20070604 00115 EU 2007 6 4 07FDEA02003 1 20070529 A 5313 A53980669 STRINGER AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 CORROSION ON STRINGER 56, C76-77 LHS CORROSION BLEND OUT REPAIR PERFORMED IAW EA 6-5318-106463 AND RAS/DAHAM/4022176/200 7 ISS.A 2 L 7 2 4F RT A35EU 2007060400116 20070604 00116 EU 2007 6 4 07FDEA02004 1 20070529 A 5311 A53980042 FRAME AIRBUS 300 A300B4605R 3930308 EU ZONE 100 DAMAGED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 731FD 709 GROOVE AND MISDRILLED SPOT AT C73, P 30-31 RT. REPAIR PERFORMED BY REWORK OF EXISTING GROOVE PER SRM 51-73-10 AND INST ALL RIVET LN9198-3200 IN DRILLED HOLE, APPROVED BY EA 6-5218-106451 AND RAS/DAHAM/4022141/2007 ISS. A 2 L 7 2 4F RT A35EU 2007060400117 20070604 00117 EU 2007 6 4 07FDEA02008 1 20070529 A 5320 A53610996200 STIFFENER AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 CRACK ON LT C12A STIFFENER FITTING, CRACK LENGTH 4MM. REPAIR PERFORMED BY INCORPORATION OF SB A300-53-6137, APPROVED BY EO 6-5340-7-5003. 2 L 7 2 4F RT A35EU 2007060400118 20070604 00118 EU 2007 6 4 07FDEA02009 1 20070529 A 2720 A2727024500200 CLAMP AIRBUS AIRBUS 310 A310203 3930313 EU RUDDER DUPLEX DELAMINATED A FDEA D RETURN TO BLOCK A S FLAME/FIRE AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 25 410FE 356 RUDDER CHECK ON FLIGHT CONTROL TEST UNSAT, RUDDER TRAVEL RESTRICTED ON ECAM, RUDDER PEDALS STUCK IN HALF DOWN POSITION, BOTH LEFT AND RIGHT SIDE, WOULD NOT RETURN TO CENTER POSITION FOUND DUPLEX ROD LWR SEPARATION CLAMP (P/N A2727024500200) RUBBER DISBONDED ALLOWING CLAMP TO FALL INTO LWR RUDDER QUADRANT. REMOVED AND REPLACED CLAMP IAW A310-200 AMM 27-21-17 -4 01. 2 L 7 2 4F RT A35EU 2007060400119 20070604 00119 EA 2007 6 4 QXEA200700856 1 20070518 A 7830 SUPPORT ANGLE CNDAIR CL600 CL6002C10 1390015 EA THRUST REVERSER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 C4 OKC - NR 1 ENGINE LOWER TRANS COWL SUPPORT ANGLE BEHIND 2ND FROM END LATCH IS CRACKED. REPAIRED IAW REO670-78-800, A ND SRM 51-42-13. 2 L 7 2 4F RT A21EA 2007060400120 20070604 00120 EA 2007 6 4 QXEA200700860 1 20070430 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 C4 OKC - LOWER FUSELAGE SKIN HAS MINOR CORROSION AT LOWER TCAS ANTENNA MOUNT. REPAIRED IAW SRM 51-21-06, 53-21-01. 2 L 7 2 4F RT A21EA 2007060400121 20070604 00121 EA 2007 6 4 QXEA200700861 1 20070511 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 C4 OKC - LOWER ADF ANTENNA MOUNTING SKIN HAS LIGHT CORROSION. REPAIRED IAW SRM 51-21-06, AND 53-00-01. 2 L 7 2 4F RT A21EA 2007060400122 20070604 00122 EA 2007 6 4 QXEA200700858 1 20070508 A 5730 PANEL CNDAIR CL600 CL6002C10 1390015 EA WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 C4 OKC - PANEL 584ET CHAFED AT LEADING EDGE. REPAIRED IAW SRM 53-00-01, 51-12-00, AND 53-00-01. 2 L 7 2 4F RT A21EA 2007060400123 20070604 00123 EA 2007 6 4 QXEA200700859 1 20070504 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 485-565 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 C4 OKC - PASSENGER CABIN LEFT SIDE SEAT RAIL FROM FS 485.00 LEFT TO FS 565.00 LEFT HAS NUMEROUS AREAS OF CORROSION AND S CRATCHES. REPAIRED IAW SRM 51-21-06 AND 51-21-11. 2 L 7 2 4F RT A21EA 2007060400124 20070604 00124 EA 2007 6 4 QXEA200700857 1 20070518 A 5410 SUPPORT ANGLE CNDAIR CL600 CL6002C10 1390015 EA NR 2 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 C4 OKC - 2 ENGINE TRANS COWL SUPPORT ANGLE BEHIND 2ND FROM END LATCH IS CRACKED. REPAIRED IAW REO670-78-800, AND SRM 51 -42-13. 2 L 7 2 4F RT A21EA 2007060400125 20070604 00125 EA 2007 6 4 QXEA200700855 1 20070512 A 5410 SUPPORT ANGLE CNDAIR CL600 CL6002C10 1390015 EA NR 1 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 C4 OKC - NR 1 ENGINE UPPER TRANS COWL SUPPORT ANGLE BEHIND 2ND FROM LATCH IS CRACKED. REPAIRED IAW REO670-78-33-800, AN D SRM 51-42-13, 51-42-21. 2 L 7 2 4F RT A21EA 2007060100060 20070601 00060 EA 2007 6 1 SWIA200718281 1 20070408 A 3350 LENS CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 924SW 7681 CABIN FLOOR TRACK EMERGENCY LIGHT LENSE IS CRACKED IN SEVERAL PLACES, DISCOVERED AT C-CHECK. REPLACED CABIN FLOOR TRACK TOP LENSE COVER PER CRJ200 AMM 33-51-01. 2 L 7 2 4F RT A21EA 2007060100067 20070601 00067 WP 2007 6 1 IXXA070030O 1 20070519 A 3297 WIRE DOUG DC8 DC873F 302199F WP ZONE 700 BROKEN A IXXA O OTHER J WARNING INDICATION LD LANDING 1 SW 11 603AL 98004 3197 46003 DURING APPROACH FOR LANDING, THE CREW NOTICE THE RIGHT LANDING GEAR DOWN LIGHT DID NOT ILLUMINATE WHEN GEAR LEVER WAS SE LECTED IN THE DOWN POSITION FOR LANDING. THE CREW ACCOMPLISH ALL NECCESSARY PROCEDURES, AND LANDED IN KLAX WITHOUT INCI DENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A BROKEN WIRE AT TERMINAL STRIP S3-188 30X. MAINTENANCE REPAIRED TH E BROKEN WIRE, AND PERFORMED OPERATIONAL CHECK WAS GOOD, IAW DACO MAINTENANCE MANUAL 20-50-1. AIRCRAFT RETURNED TO SERV ICE. 2 L 7 4 4F RT 4A25 2007060100077 20070601 00077 WP 2007 6 1 07FDEA01973 1 20070525 A 5347 WSP04147 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 MAIN CABIN ON SEAT TRACK FOUND 1 SEVERE CORROSION WITH EXFOLIATION AND 6 ELONGATED HOLES, DISCREPANCY FOUND DURING ACF M ODIFICATION. REPAIRED IAW SRM 53-70-00 FIG 1 VOL 1. 2 L 7 3 4F A22WE 2007060100089 20070601 00089 NM 2007 6 1 NWAA072043132 1 20070523 A 5340 ATTACH FITTING AIRBUS A319 A319114 3930350 NM FUSLEAGE DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 332NB 1570 DURING "H" CHECK MAINTENANCE DAMAGED LAVATORY D ATTACH FITTING. REPAIRED PER EA 31-208441. 2 L 7 2 4F RT A28NM 2007060100092 20070601 00092 SO 2007 6 1 SWIA200718263 1 20070522 A 2121 AE1711AA0 COOLING FAN EMB 120 EMB120ER 3260203 SO CABIN SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 289YV 10731 6755 120289 SMOKE ODOR AND FIRE DETECTOR WENT OFF ON TAXI OUT. REPLACED GROUND COOLING FAN WITH SERVICEABLE UNIT. OPS CHECK GOOD I AW EMB 120 MM 21-51-03. 2 L 7 2 4T RT A31SO 2007060100093 20070601 00093 2007 6 1 SWIA200718264 4 20070520 A 2340 509612 HANDSET EMB 120 EMB120ER 3260203 SO SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 292UX 14979 14979 120292 ON TAXI OUT, FLIGHT ATTENDANTS HANDSET STARTED SMOKING. REPLACED FLIGHT ATTENDANTS HANDSET. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007060400126 20070604 00126 NM 2007 6 4 QXEA200700842 1 20070523 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM ILLUMINATED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 414QX 4061 PDX FLIGHT NR 2359: PUSHER SYSTEM FAIL CAUTION LIGHT ILLUMINATED AFTER ENGINE START. C/W CHECKLIST. AIRCRAFT RETURNED TO GATE. MAINTENANCE CYCLED POWER TO SPM 1 AND 2. POWER UP SELF TEST NORMAL. CAUTION LIGHT OUT. STALL SYSTEM 1 AND 2 TEST NORMAL AT THIS TIME. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007060400127 20070604 00127 NM 2007 6 4 QXEA200700864 1 20070529 A 3150 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 411QX 4055 SEA FLIGHT NR 2392: AFTER START UP, PROP DEICE CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE INTE RROGATED CDS. NO PROP DEICE FAULTS NOTED. CLEARED NR 1 AND 32 PROP DEICE NVM. PERFROMED FUNCTIONAL TEST OF THE PROP I CING SYSTEM IAW Q400 AMM 30-61-00, PAGES 501-502. FUNCTIONAL TEST GOOD. PROP DEICE CAUTION LIGHT DID NOT ILLUMINATE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007060400128 20070604 00128 NM 2007 6 4 QXEA200700866 1 20070529 A 3150 WARNING MESSAGE BOMBDR DHC8 DHC8402 1390042 NM ILLUMINATED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 412QX 4059 LAX FLIGHT NR 2470: POWER PLANT MESSAGE AFTER ENGINE START. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE FOUND FAULT CODE 1 30A ON NR 1 PROP. PERFORMED PEC FAULT CLEAR PROCEDURE IAW Q400 AMM TASK 61-20-36-070-801. OPS TEST OF AUTOFEATHER AND UPTRIM SYSTEM GOOD. POWER PLANT MESSAGE REMAINED OUT. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007060400129 20070604 00129 NM 2007 6 4 07FDEA01919 1 20070521 A 5311 AFA002719 FRAME DOUG MD11 MD11 3023602 NM BS 1661 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 MAIN DECK CARGO COMPARTMENT, LEFT MAIN FRAME STA 1661 EXISTING REPAIR DOUBLER AT LONGERON 12L FOUND DAMAGED. MAIN DEC K CARGO COMPARTMENT, LEFT FUSELAGE MAIN FRAME STA 1661 DAMAGED EXISTING REPAIR DOUBLER AT LONGERON 12L REMOVED AND REPLA CED. REPAIR CARRIED OUT AS PER SRM 53-30 -00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. DAMAGE T OLERANCE INITIAL INSPECTION TO BE CARRIED OUT ON THE NEXT 14,500 CYCLES AND SUBSEQUENT REPEAT INSPECTION TO BE CARRIED OUT EVERY 9,500 CYCLES THEREAFTER AS PER SRM 53-30-00 VOLUME I, FIGURE 1. 2 L 7 3 4F RT A22WE 2007060400130 20070604 00130 NM 2007 6 4 QXEA200700862 1 20070529 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM ILLUMINATED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 401QX 4031 FCA FLIGHT NR 2348: PITCH TRIM CAUTION ILLUMINATED DURING LANDING, THEN EXTINGUISHED APPROXIMATELY 10 SECONDS LATER. PI TCH TRIM CAUTION ILLUMINATED AGAIN PRIOR TO SHUT-DOWN AND REMAINED ILLUMINATED. MAINTENANCE CLEARED THE CAUTION IAW Q40 0 FIM TASK 27-30-00-810-803. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007060400131 20070604 00131 NM 2007 6 4 07FDEA01920 1 20070521 A 5311 AFA002719 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 MAIN DECK CARGO COMPARTMENT, RIGHT MAIN FRAME STA 1661 EXISTING REPAIR DOUBLER AT LONGERON 12R FOUND DAMAGED. MAIN DE CK CARGO COMPARTMENT, RIGHT FUSELAGE MAIN FRAME AT STA 1661. DAMAGED EXISTING REPAIR DOUBLER AT LONGERON 12R REMOVED AN D REPLACED. REPAIR CARRIED OUT AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. DA MAGE TOLERANCE INITIAL INSPECTION TO BE CARRIED OUT ON THE NEXT 14,500 CYCLES AND SUBSEQUENT REPEAT INSPECTION TO BE CAR RIED OUT EVERY 9,500 CYCLES THEREAFTER AS PER SRM 53-30-00 VOLUME I, FIGURE 1. 2 L 7 3 4F RT A22WE 2007060400132 20070604 00132 WP 2007 6 4 07FDEA01937 1 20070522 A 5310 AFA7132 FITTING DOUG MD10 MD1010F 3022112 WP DOOR FRAME CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 MAIN CARGO DOOR LOWER JAMB FITTING NR 3 SHOWS CORROSION AT FORWARD LOWER HOLE. REPAIRED NR 3 LOWER JAMB AND REPLACED S UPPORT FITTING IAW FEDEX EA 8-5230-110663 REV A "FUSELAGE-MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING INSPECTION AND DOOR RIG." 2 L 7 3 4F RT A22WE 2007060400133 20070604 00133 EA 2007 6 4 QXEA200700843 1 20070524 A 3610 GG67080025 SHUTOFF VALVE CNDAIR CL600 CL6002C10 1390015 EA LT BLEED SYS MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 618QX 5745 99 10205 PDX - DURING CLIMB, THE LEFT ENGINE BLEED CAUTION MESSAGE ILLUMINATED. FOLLOWING THE CHECKLIST THE MESSAGE DISAPPEARED. MAINTENANCE REPLACED THE LEFT PRESSURE REGULATOR SHUTOFF VALVE (PRSOV). OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED T O SERVICE. 2 L 7 2 4F RT A21EA 2007060400134 20070604 00134 NM 2007 6 4 QXEA200700863 1 20070527 A 2920 9669963 PRESSURE SWITCH BOMBDR DHC8 DHC8402 1390042 NM HYD SYSTEM MALFUNCTIONED A QXEA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 402QX 15377 15377 4032 SEA FLIGHT NR 2332: DURING HYD NR 3 ISO VALVE TEST, 33 PRESSURE FLUCTUATES AND DROPS WHILE WORKING ELEVATOR. PRESSURE F ALLS TO ZERO. MAINTENANCE REMOVED AND INSTALLED A SERVICEABLE NR 3 HYD SYSTEM PRESSURE SWITCH IAW Q400 AMM 29-12-31-000 -801 AND 29-12-31-400-801. PERFORMED OPS TEST OF NR 3 HYDRAULIC SYSTEM IAW Q400 AMM 29-12-01-710-801. OPS TEST GOOD. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007060400135 20070604 00135 NM 2007 6 4 QXEA200700867 1 20070528 A 3150 WARNING MESSAGE BOMBDR DHC8 DHC8402 1390042 NM ILLUMINATED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 427QX 4156 SEA TO MSO FLIGHT 2340: POWER PLANT MESSAGE CAME ON AND REMAINED ILLUMINATED FOR REMAINDER OF FLIGHT. FLIGHT WAS DIVERTE D TO GEG. MAINTENANCE FOUND FAULT CODE 158B IN CDS. CLEARED FAULT IAW FIM TASK 61-20-04-810-812. FAULT DID NOT REOCCU R. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007060400136 20070604 00136 NM 2007 6 4 TSAA0752027 1 20070523 A 3150 WARNING LIGHT BOEING 737 73776N 13844CH NM ILLUMINATED A TSAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 746AL 29905 NON-ETOPS FLIGHT 482 SNA-RNO - AFTER TAKEOFF, THE CREW NOTED THE AFT CARGO DOOR OPEN INDICATION ILLUMINATED. CREW RETUR NED TO SNA WITHOUT FURTHER INCIDENT. MAINTENANCE DEFERRED THE AFT CARGO DOOR INDICATION PER MEL 52-3-1 AND VERIFIED THE DOOR WAS CLOSED AND LOCKED FOR FLIGHT. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007060400137 20070604 00137 EA 2007 6 4 QXEA200700847 1 20070513 A 5240 SKIN CNDAIR CL600 CL6002C10 1390015 EA R1 DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 C4 OKC - RIGHT FORWARD SERVICE DOOR, R1, AFT LOWER CORNER OUTER SKIN HAS SMALL GOUGE. REPAIRED IAW SRM 52-41-00, 51-12- 00, AND 52-41-01. 2 L 7 2 4F RT A21EA 2007060400138 20070604 00138 NM 2007 6 4 QXEA200700865 1 20070529 A 6120 697072004 GOVERNOR BOMBDR DHC8 DHC8402 1390042 NM OVERSPEED MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 422QX 593 593 4150 PDX FLIGHT NR 2335: NR 1 ENGINE WILL NOT COME OUT OF START AND FEATHER MODE FOLLOWING ENGINE START. NOTICED THAT ON PRE VIOUS START, NR 1 ENGINE WAS SLOWER THAN NORMAL TO ACCELERATE FROM FEATHER TO FLIGHT IDLE, APPROX 5-10 SECONDS. AIRCRAF T RETURNED TO BLOCK. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE OVERSPEED GOVERNOR IAW Q400 AMM TASK 61-20-26-000-801 AND 61-20-26-400-801. OPS CHECK AND LEAK CHECK GOOD. C/W PROPELLER TIME TO UNFEATHER CHECK IAW Q400 AMM TASK 61-20-0 0-720-801. OPS CHECK GOOD. FEATHERED AND UNFEATHERED NR 1 PROP NUMEROUS TIMES MANUALLY AND WITH ENGINE RUNNING. NO FU RTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007060400139 20070604 00139 WP 2007 6 4 07FDEA01938 1 20070522 A 5310 AFA7132 FITTING DOUG MD10 MD1010F 3022112 WP DOOR FRAME CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 MAIN CARGO DOOR-LOWER JAMB FITTING NR 3 SHOWS CORROSION AT AFT LOWER HOLE. REPAIRED NR 3 LOWER JAMB WEB IAW FEDEX EA 8 -5230-110663 REV. A. " FUSELAGE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING INSPECTION AND DOOR RIIG." FITTING(LOWER S UPPORT) REPLACED ON JOB CARD N00788. 2 L 7 3 4F RT A22WE 2007060400140 20070604 00140 WP 2007 6 4 07FDEA01939 1 20070522 A 5310 AFA7132 FITTING DOUG MD10 MD1010F 3022112 WP DOOR FRAME CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 MAIN CARGO DOOR-LOWER JAMB FITTING NR 1 SHOWS CORROSION AT LOWER FORWARD HOLE. REPAIRED LOWER JAMB AND REPLACED SUPPORT FITTING NR 1 IAW FEDEX EA 8-5230-110663. "FUSELAGE- MAIN CARGO DOOR - LOWER JAMB FITTING INSPECTION AND DOOR RIG." 2 L 7 3 4F RT A22WE 2007060400141 20070604 00141 WP 2007 6 4 07FDEA01940 1 20070522 A 5310 AFA7132 FITTING DOUG MD10 MD1010F 3022112 WP DOOR FRAME CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 MAIN CARGO DOOR LOWER JAMB FITTING NR 2 SHOWS CORROSION AT LOWER FORWARD HOLE. REPAIRED LOWER JAMB AND REPLACED SUPPOR T FITTING NR 2 IAW FEDEX EA. 8-5230-110663 REV A. " FUSELAGE- MAIN CARGO DOOR-LOWER JAMB SUPPORT FITTING INSPECTION AND DOOR RIG." LOWER SUPPORT FITTING REPLACED ON JOB CARD N00788. 2 L 7 3 4F RT A22WE 2007060400142 20070604 00142 WP 2007 6 4 MWEA070121 1 20070525 A 3320 0398010 BALLAST DOUG DC9 DC982 3022082 WP ROW 21 INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 809ME 48071 FLIGHT ATTENDANT REPORTED STRANGE SMELL & LIGHT HAZE. REMOVED AND REPLACED BALLEST AT ROW 21. 2 L 7 2 4F A6WE 2007060400143 20070604 00143 EA 2007 6 4 TRAX200700715 1 20070523 A 5720 ANGLE CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 976EV 7601 RT WING MIDDLE LEADING EDGE, I/B ATTACH ANGLE IS CRACKED. REMOVED RT WING MIDDLE LEADING EDGE I/B CRACKED ATTACH ANGL E. INSTALLED NEW SERVICEABLE ATTACH ANGLE, P/N 600-12025-8, RT WING MIDDLE LEADING EDGE I/B, IAW SRM 51-40-11. W/C 1102 . 2 L 7 2 4F RT A21EA 2007060500001 20070605 00001 WP 2007 6 5 ASAA0781730 1 20070530 A 5321 99366483 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 CABIN FLOOR PANEL HAS EDGE DAMAGE. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-03 PG 122B AND DCA DWG S4932106. 2 L 7 2 4F RT A6WE 2007060500002 20070605 00002 WP 2007 6 5 ASAA0781731 1 20070530 A 5321 CHANNEL DOUG DC9 DC983 3022083 WP FLOOR PANEL DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 CABIN FLOOR PANEL HAS A DAMAGED HAT CHANNEL. LOCATED AND DRILLED A REPLACEMENT HAT CHANNEL IAW SRM 51-10-4, 51-30-2 AND DAC DWG 9957918. 2 L 7 2 4F RT A6WE 2007060500005 20070605 00005 WP 2007 6 5 ASAA0781732 1 20070530 A 5330 591140659 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 FUSELAGE SKIN DENTED A PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR. CUT OUT DAMAGED AREA OF SKIN. FABRICATED AND INSTALL ED A SKIN FILLER INTERNAL REPAIR DOUBLERS, REPAIR STRAPS AND FINGER DOUBLERS IAW SRM 53-04 FIG 12C. 2 L 7 2 4F RT A6WE 2007060500006 20070605 00006 WP 2007 6 5 ASAA0781733 1 20070530 A 5320 992366719 WEB DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 DOUBLE DRILLED HOLES ON WEB UNDER FWD CABIN FLOORBOARD SUPPORT ANGLE. CUT OUT DAMAGED AREA OF WEB, FABRICATED AND INSTA LLED A REPAIR FILLER AND DOUBLER IAW SRM 51-70-4 FIG 2. 2 L 7 2 4F RT A6WE 2007060500008 20070605 00008 WP 2007 6 5 ASAA0781737 1 20070529 A 5321 99517883 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN DETERIORATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 CABIN FLOOR PANEL HAS FIBER DAMAGE TO THE UPPER SURFACE. FABRICATED A REPLACEMENT PANEL IAW SRM 53-05 PARA 44 AND DAC D WG S4932106. 2 L 7 2 4F RT A6WE 2007060500009 20070605 00009 WP 2007 6 5 ASAA0781738 1 20070529 A 5321 INSERT DOUG DC9 DC983 3022083 WP FLOOR PANEL CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 CABIN FLOOR PANEL HAS NUMEROUS CORRODED INSERTS. FABRICATED A REPLACEMENT PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932 106. 2 L 7 2 4F RT A6WE 2007060500010 20070605 00010 WP 2007 6 5 ASAA0781739 1 20070529 A 5321 INSERT DOUG DC9 DC983 3022083 WP FLOOR PANEL CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 CABIN FLOOR PANEL HAS NUMEROUS CORRODED INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007060500011 20070605 00011 WP 2007 6 5 ASAA0781740 1 20070529 A 5321 99365465 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 CABIN FLOOR PANEL IS DELAMINATED. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007060500013 20070605 00013 WP 2007 6 5 ASAA0781742 1 20070529 A 5321 INSERT DOUG DC9 DC983 3022083 WP FLOOR PANEL CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 CABIN FLOOR PANEL HAS NUMEROUS CORRODED INSERTS. FABRICATED A REPLACEMENT PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932 106. 2 L 7 2 4F RT A6WE 2007060500014 20070605 00014 WP 2007 6 5 ASAA0781743 1 20070529 A 5321 INSERT DOUG DC9 DC983 3022083 WP FLOOR PANEL CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 CABIN FLOOR PANEL HAS NUMERIOUS INSERTS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S493210 6. 2 L 7 2 4F RT A6WE 2007060500019 20070605 00019 NM 2007 6 5 SWAA072758 1 20070531 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007060500023 20070605 00023 NM 2007 6 5 SWAA072769 1 20070531 A 5711 6545416 SPAR BOEING 737 7373L9 1384470 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND RIGHT WING REAR SPAR UPPER CHORD CRACKED AT STA 224.14. REPAIRED CHORD PER ER. 2 L 7 2 4F RT A16WE 2007060500025 20070605 00025 NM 2007 6 5 SWAA072767 1 20070531 A 5711 6545416 SPAR BOEING 737 7373L9 1384470 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND LEFT WING REAR SPAR UPPER CHORD CRACKED AT STA 274.14. REPAIRED CHORD PER ER. 2 L 7 2 4F RT A16WE 2007060500026 20070605 00026 NM 2007 6 5 SWAA072765 1 20070531 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500028 20070605 00028 NM 2007 6 5 SWAA072764 1 20070531 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500029 20070605 00029 NM 2007 6 5 SWAA072773 1 20070531 A 5330 6545800 SKIN BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER FWD CORNER BS 310. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007060500030 20070605 00030 NM 2007 6 5 SWAA072770 1 20070531 A 5310 6545829505 DOOR FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND E&E DOOR CUTOUT RIGHT FWD CORNER CORRODED AT BS 328, RBL 15.47. REPAIRED INNER CHORD PER SRM. 2 L 7 2 4F RT A16WE 2007060500032 20070605 00032 NM 2007 6 5 SWAA072757 1 20070531 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 727E, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007060500034 20070605 00034 NM 2007 6 5 SWAA072760 1 20070531 A 5315 6546811 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 730SW 27862 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BETWEEN RBL 43 AND LBL 43. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2007060500035 20070605 00035 NM 2007 6 5 SWAA072756 1 20070531 A 5314 6562125 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SPV CHECK, FOUND KEEL BEAM CORRODED AT RIGHT BS 737. REMOVED AND REPLACED KEEL BEAM PER ER. 2 L 7 2 4F RT A16WE 2007060500036 20070605 00036 NM 2007 6 5 SWAA072761 1 20070531 A 5210 656222572 FITTING BOEING 737 7377H4 1384404 NM R1 DOOR DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 726SW 27858 R1 DOOR STUCK CLOSED. FOUND LOWER AFT CAM FITTING DAMAGED. REMOVED AND REPLACED CAM ROLLER FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500039 20070605 00039 NM 2007 6 5 SWAA072745 1 20070530 A 5315 146A94014 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 730SW 27862 DURING SCHEDULED 8Y CHECK, FOUND AFT CARGO BAY FLOORBEAM CORRODED BETWEEN BS 793 AND BS 847, RBL 14. REMOVED AND REPLAC ED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500041 20070605 00041 2007 6 5 SWAA072726 4 20070529 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 237WN 34632 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007060500042 20070605 00042 NM 2007 6 5 SWAA072743 1 20070530 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 446, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007060500043 20070605 00043 NM 2007 6 5 SWAA072747 1 20070530 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007060500044 20070605 00044 NM 2007 6 5 SWAA072748 1 20070530 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 951, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007060500045 20070605 00045 NM 2007 6 5 SWAA072753 1 20070530 A 5311 6545808 BELTFRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 294, STR 11L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500046 20070605 00046 NM 2007 6 5 SWAA072752 1 20070530 A 5311 6545808 BELTFRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 294, STR 12L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500047 20070605 00047 NM 2007 6 5 SWAA072751 1 20070530 A 5311 6545808 BELTFRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 294, STR 13L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500048 20070605 00048 NM 2007 6 5 SWAA072754 1 20070530 A 5315 6545833 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 294, LBL 36 TO RBL 53. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500049 20070605 00049 NM 2007 6 5 SWAA072730 1 20070529 A 5753 6546434 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SPV CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007060500051 20070605 00051 NM 2007 6 5 SWAA072692 1 20070528 A 5315 147A55067 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 728SW 27860 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 27.50. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500056 20070605 00056 NM 2007 6 5 SWAA072672 1 20070525 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 472WN 33831 DURING SCHEDULED MV3 CHECK, FOUND EEPLS COVER CRACKED AT ROW 12 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007060500057 20070605 00057 2007 6 5 SWAA072674 4 20070526 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 456WN 32463 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007060500059 20070605 00059 NM 2007 6 5 SWAA072678 1 20070526 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007060500060 20070605 00060 NM 2007 6 5 SWAA072707 1 20070528 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 20R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007060500061 20070605 00061 NM 2007 6 5 SWAA072677 1 20070526 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 14L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500062 20070605 00062 NM 2007 6 5 SWAA072676 1 20070526 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 413, STR 26L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007060500063 20070605 00063 NM 2007 6 5 SWAA072683 1 20070526 A 5330 6545777 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR UPPER HINGE SKIN CUTOUT CRACKED AT UPPER CORNER. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500064 20070605 00064 NM 2007 6 5 SWAA072699 1 20070528 A 5311 6545808241 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294, STR 13L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500065 20070605 00065 NM 2007 6 5 SWAA072722 1 20070529 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500066 20070605 00066 NM 2007 6 5 SWAA072697 1 20070528 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 9L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007060500068 20070605 00068 NM 2007 6 5 SWAA072698 1 20070528 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007060500069 20070605 00069 EA 2007 6 5 TRAX200700692 1 20070520 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA BS 409 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 851AS 7360 LT SIDE PASSENGER SEAT SIDE RAILS CORRODED AND GOUGED AS MARKED FWD OF FS 409+128. BLENDED SIDEWALL SEAT RAIL PN 601R3 8312-31 AT FS 385 TO DEMINSIONS OF 1"X1"X.007 DEEP. BLENDED SIDEWALL SEAT RAIL PN 601R38312-29 AT STA 409+22 TO DEMINSI ONS OF 1"X1"X .007 DEEP, AT FS 409+51 TO DEMINSIONS OF 1"X3"X.006 AND AT 409+64 TO DEMINSIONS OF 1"X6"X.034" AS PER CRJ 200 SRM 51-12-00. ALL SIDE SEAT RAIL BLEND OUTS LT SIDE FWD OF 409+128 ARE WITHIN LIMITS OF CRJ200 SRM 53-21-49 FIG 10 1 EXCEPT TO BLEND OUT TO SEAT RAIL PN 601R38312-29 AT FS 409+64. REPAIRED LT. SIDE SEAT RAIL AT 409+64 IAW BOMBARDIER R EO 601R-53-00-055 . 2 L 7 2 4F RT A21EA 2007060500070 20070605 00070 NM 2007 6 5 SWAA072716 1 20070529 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500072 20070605 00072 NM 2007 6 5 SWAA072717 1 20070529 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500074 20070605 00074 NM 2007 6 5 SWAA072703 1 20070528 A 5311 6546534 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500075 20070605 00075 NM 2007 6 5 SWAA072723 1 20070529 A 5311 6546537 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 580, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500078 20070605 00078 NM 2007 6 5 SWAA072720 1 20070529 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500080 20070605 00080 NM 2007 6 5 SWAA072715 1 20070529 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500081 20070605 00081 NM 2007 6 5 SWAA072718 1 20070529 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500082 20070605 00082 NM 2007 6 5 SWAA072713 1 20070529 A 5311 6546595 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500084 20070605 00084 NM 2007 6 5 SWAA072710 1 20070529 A 5551 6551524 FITTING BOEING 737 7373H4 1384600 NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND HORIZONTAL STAB FITTING CLEVIS LUG FACES CORRODED. REPAIRED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007060500087 20070605 00087 NM 2007 6 5 SWAA072719 1 20070529 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500088 20070605 00088 NM 2007 6 5 SWAA072688 1 20070527 A 5753 6573731 FLAP BOEING 737 7373H4 1384600 NM LT WING DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND LEFT WING INBOARD MID FLAP DISBONDED AT INBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007060500090 20070605 00090 NM 2007 6 5 SWAA072714 1 20070529 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500091 20070605 00091 NM 2007 6 5 SWAA072693 1 20070528 A 3397 WIRE BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. FOUND BROKEN WIRE ON CONNECTOR, REPAIRED WIRE PER MM. 2 L 7 2 4F RT A16WE 2007060500093 20070605 00093 NM 2007 6 5 SWAA072694 1 20070528 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007060500094 20070605 00094 NM 2007 6 5 SWAA072708 1 20070528 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 19R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007060500095 20070605 00095 NM 2007 6 5 SWAA072701 1 20070528 A 5311 65C34356 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 20L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500096 20070605 00096 NM 2007 6 5 SWAA072671 1 20070525 A 5330 65C381921 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515D, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500097 20070605 00097 NM 2007 6 5 SWAA072709 1 20070528 A 3350 767 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007060500100 20070605 00100 EU 2007 6 5 F3LA200700121 1 20070520 A 5320 D5361019720140 THRESHOLD AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 802FR 4993 1991 DURING C-3 CHECK, INSPECTION REPORTED FLOORBOARD THRESHOLD STRIP 222FF CORRODED AROUND FASTENER HOLES. REPLACED FLOORBO ARD THRESHOLD STRIP IAW AMM 53-12-12-400-001. 2 L 7 2 4F RT 2007060500101 20070605 00101 EU 2007 6 5 AWXA200700686 1 20070526 A 5320 D534711282001 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 603AW 661 SAL - CORROSION ON CABIN FLOOR SUPPORT, FR 69 - FR 70, -Y1762.5. REPLACED CABIN FLOOR SUPPORT, FR 69 - FR 70, -Y1762.5 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007060500102 20070605 00102 EU 2007 6 5 AWXA200700687 1 20070520 A 5320 D53471124201 SHEAR PLATE AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 603AW 661 SAL - CORROSION ON CABIN FLOOR SHEAR PLATE, FR 69 - FR 70, -Y1762.5. REPLACED CABIN FLOOR SHEAR PLATE, FR 69 - FR 70, -Y1762.5 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007060500103 20070605 00103 EU 2007 6 5 AWXA200700688 1 20070520 A 5315 D5347228408 FLOORBEAM AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 603AW 661 SAL - CORROSION ON CABIN FLOORBEAM, FR 66 + 4", -Y254 TO -Y465. REPLACED CABIN FLOORBEAM, FR 64 - FR 67,-Y254 TO -Y465 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007060500104 20070605 00104 EA 2007 6 5 REXA200700053 1 20070503 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A REXA K NONE L NO TEST IN INSP/MAINT 1 SO 25 8944B 7944 EMERG FLOOR PATH LIGHTS ROW 4 AND 7 INOP, INCLUDING ORANGE STRIP, CLEARED BY OPERATIONAL CHECK. 2 L 7 2 4F RT A21EA 2007060500105 20070605 00105 EA 2007 6 5 REXA200700054 1 20070514 A 3350 K601R402151 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A REXA K NONE L NO TEST IN INSP/MAINT 1 SO 25 8736A 7736 EMERGENCY FLOOR PATH LIGHTING STRIP FROM ROW 2 THROUGH 5 INOP. UNIT WAS OPS CHECKED AND FOUND TO BE OPERATIONAL PER THE AMM. 2 L 7 2 4F RT A21EA 2007060500106 20070605 00106 NM 2007 6 5 07FDEA02032 1 20070531 A 2720 CONTROL VALVE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 527FE 48601 AFTER 1 HR 30 MINUTES FLIGHT, A/C RETURN BACK TO STN DUE TO NR 3 HYD QTY LOW. FOUND HYD QTY 3 RESERVOIR DEPLETED TO 1.0 AND FOUND EXCESSIVE LEAK FROM THE NR 1 HORIZONTAL STABILIZER CONTROL VALVE UNION. REQUIRES UNION O- RINGS, EDP PUMP AN D FILTER MODULE. REMOVED AND INSTALLED BOTH ENGINE DRIVEN HYD PUMP ON NR 3 ENGINE AS PER AMM 29-11-20-4. REMOVED AND I NSTALLED ALL THE FOUR HYD OIL FILTERS AS PER AMM 29-12-41-400. REPLACED HORIZONTAL PRIMER Y CONTROL VALVE UNION O-RING. REFILLED NR 3 HYD SYSTEM AS REQUIRED. RAN NR 3 ENGINE AS PER JRH. CYCLED HORIZONTAL STAB FEW TIMES. NO LEAK FOUND ON THE STAB CONTROL VALVE UNION. NR 3 SYSTEM HYD QTY REMAINED SAME. ENGINE RUN BY 245371. 2 L 7 3 4F RT A22WE 2007060500107 20070605 00107 NM 2007 6 5 07FDEA02034 1 20070531 A 5754 SKIN DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LEFT WING, NR 1 LEADING EDGE SLAT I/B EDGE FOUND CRACK NEAR ALIGNMENT PIN HOLE. REPAIR CARRIED OUT PER FEDEX EA 1-5710 -109891. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007060500108 20070605 00108 NM 2007 6 5 07FDEA02035 1 20070531 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 UPPER CARGO COMPARTMENT, SEAT TRACK RBL 75 CORRODED AT STA 1301 TO STA 1361. [06-18-07] REPAIR CARRIED OUT AT UPP ER CARGO COMPARTMENT, SEAT TRACK RBL 75, STA 1267 TO STA 1391 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIF IED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007060500109 20070605 00109 NM 2007 6 5 07FDEA02036 1 20070531 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RIGHT WING, O/B FLAP O/B HINGE AFT FAIRING AFT STRUT FWD BOLT HOLE FOUND CORROSION. [06-18-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-109897. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007060500110 20070605 00110 NM 2007 6 5 07FDEA02037 1 20070531 A 5711 SPAR CAP DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RIGHT WING, TRAILING EDGE REAR SPAR LOWER CAP FOUND CORROSION AT XORS 1067. [06-19-07] 2 L 7 3 4F RT A22WE 2007060500111 20070605 00111 NM 2007 6 5 07FDEA02038 1 20070531 A 5711 SPAR CAP DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RIGHT WING, TRAILING EDGE REAR SPAR LOWER CAP FOUND CORROSION AT XORS 1054. [06-18-07] REPAIR CARRIED OUT AS PER F EDEX EA 1-5710-109898. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007060500134 20070605 00134 NM 2007 6 5 AALA20070957 1 20070527 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 347AN 33086 SFO - EXTERIOR EMERGENCY LIGHT ON LEFT SIDE AFT OF FLAP INOPERATIVE. RELAMPED L642 EXTERIOR EMERGENCY LIGHT ON LEFT SID E AFT OF FLAP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007060500135 20070605 00135 NM 2007 6 5 AALA20070959 1 20070528 A 3350 BRACKET BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISCONNECTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 693AA 26973 TPA - EAT MOUNTED EMERGENCY LIGHT AT ROW 31 BRACKET DISCONNECTED. REPLACED BRACKET FOR SEAT MOUNTED EMERGENCY LIGHT AT ROW 31. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007060500136 20070605 00136 NM 2007 6 5 AALA20070958 1 20070527 A 3350 BULB BOEING 757 757231 1384950 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 727TW 30340 DFW - EMERGENCY LIGHT AT RIGHT AFT DOOR INOPERATIVE. SECURED LIGHT BULB FOR EMERGENCY LIGHT AT RIGHT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007060500137 20070605 00137 EU 2007 6 5 AALA20070961 1 20070528 A 3231 CYLINDER AIRBUS 300 A300B4605R 3930308 EU MLG DOOR FROZEN A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 11060 470 MIA INFLIGHT T639/28MAY - REPEATER RETURNED TO MIA DUE TO BOTH NOSE LANDING GEAR DOOR INDICATORS ILLUMINATED. LANDED MI A WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE. FOUND DOOR ACTUATOR CYLINDER EYEBOLT END FROZEN. REPLACED DOOR ACT UATOR CYLINDER AS REQ PER 32-31-16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007060500138 20070605 00138 WP 2007 6 5 AALA20070962 1 20070528 A 2150 A/C PACK DOUG DC9 DC982 3022082 WP DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 585AA 53248 ORD INFLIGHT T730/28MAY - RETURNED TO ORD DUE TO SMOKE AND FUMES FROM AN UNKNOWN SOURCE. SMELLED OF BURNING RUBBER. LA NDED ORD WITHOUT INCIDENT. AIRCRAFT OUT OF SERVICE FOR EVALUATION. ACCOMPLISHED PACK BURN OUT PER WORKCARD 21 92 12. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007060500139 20070605 00139 NM 2007 6 5 AALA20070964 1 20070528 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 351AA 24032 JFK - EXTERIOR EMERGENCY LIGHT AT AFT RIGHT SIDE OF AIRCRAFT INOPERATIVE. RELAMPED EXTERIOR EMERGENCY LIGHT AT AFT RIGH T SIDE OF AIRCRAFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007060500140 20070605 00140 WP 2007 6 5 AALA20070965 1 20070528 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 468AA 49598 LGA - EMERGENCY LIGHT AT FIRST CLASS SECTION INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FIRST CLASS SECT ION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007060500141 20070605 00141 NM 2007 6 5 07FDEA01980 1 20070525 A 5330 SKIN BOEING 727 727225 1384077 NM BS 1111-1127 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 465FE 21289 EXTERNAL REPAIR ON FUSELAGE SKIN STA 1111-1127 AND STR 21R-23R DOES NOT COMPLY PER SRM. REMOVED OLD REPAIR IAW SRM 51-3 0-2. FABBED NEW DOUBLER IAW SRM 53-30-3 FIG 1 FROM MAT.2024T3 0.05, TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED NEW DOUBLER IAW SRM 53-30-3. 2 L 7 3 4F A3WE 2007060500142 20070605 00142 NE 2007 6 5 HALA0700229 2 20070528 A 7200 ENGINE BOEING 767 767300 1385204 NM PWA 4060 PW4060 52119 NE LEFT MALFUNCTIONED A HALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 581HA 28141 ETOPS SIGNIFICANT SYSTEM, LT ENG EPR AND N1 CONSTANTLY OSCILLATES BETWEEN 1.37/1.39 EARLIER 1.27/1.29 N1 BETWEEN 89.3/89 .6 EARLIER 86.6/86.9 LEFT EGT, N2 AND F/F STEADY ALL RT ENG INDICATIONS STEADY. SAME WITH LT OR RT EICAS COMPUTERS. RA N ENG AND FOUND TO BE WITHIN LIMITS PER MOC AND POWERPLANT ENGINEER, OK TO CONTINUE SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007060500143 20070605 00143 NE 2007 6 5 HALA0700230 2 20070527 A 7297 CONNECTOR BOEING 767 767300 1385204 NM PWA 4060 PW4060 52119 NE ENGINE DIRTY A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM, RT ENG PIMU "MSG RT ENG EEC C2" MSG. PERFORMED CORRECTIVE ACTION FIM 71-PIMU PER PIMU MSG 353 -19. CLEANED AND RETORQUED CONNECTORS. REPAIR CONFIRMATION CKS GOOD. RAN ENG NO MSG. 2 L 7 2 4F 4 F RT A1NM E24NE 2007060500144 20070605 00144 NM 2007 6 5 HALA0700228 1 20070529 A 3040 6240664 CONTROL UNIT BOEING 767 767300 1385204 NM WINDOW HEAT FAULTED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 598HA 23278 ETOPS SIGNIFICANT SYSTEM, LEFT FWD WINDOW HEAT INOP. BIT ON LEFT FWD WINDOW HEAT CONTROL UNIT FAULTED CONTROL UNIT. RE PLACED LEFT FWD WINDOW HEAT CONTROL UNIT PER AMM 30-41-01. 2 L 7 2 4F RT A1NM 2007060500145 20070605 00145 NM 2007 6 5 HALA0700227 1 20070529 A 3397 CONNECTOR BOEING 767 767300 1385204 NM EMERGENCY LIGHTS LOOSE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 590HA 33467 EMERGENCY PATHWAY FLOOR LIGHTING OUT BETWEEN ROWS 24 - 39.SECURED LOOSE CONNECTION AND REPLACED DEFECTIVE LUMINESCENT LI GHT STRIP. 2 L 7 2 4F RT A1NM 2007060500146 20070605 00146 NM 2007 6 5 HALA0700231 1 20070529 A 3150 UNKNOWN BOEING 767 76733A 1385209 NM UNKNOWN A HALA F ACTIVATE FIRE EXT. J WARNING INDICATION CR CRUISE 1 WP 13 589HA 23278 ETOPS SIGNIFICANT SYSTEM, TOTAL FUEL DIFFERS FORM CAPT AND F/O FMC(S) CALCULATED FUEL QTY. FUEL QTY ERROR PAGE 2/2 ALER T MSG DISPLAYED. FUEL FLOW WAS NORMAL TOTAL FUEL 24.8 FMC CALCULATED FUEL 22.3. NO EVIDENCE OF FUEL LEAK. PERFORMED T /S PER FIM 34-61-00 FIG 106 AND 106A STATUS PAGE SHOWS NO SENSOR FAULT, BITE FQP NO FAULT FUEL QTY SHOWS SAME AS FMC FUE L. NO DISCREPANCY SYS OK FOR SERVICE PER AMM AND FIM 34-61-00. 2 L 7 2 4F RT A1NM 2007060500147 20070605 00147 NM 2007 6 5 AALA20070966 1 20070528 A 3350 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 666A 25300 MIA - EMERGENCY LIGHT AT SEAT 15D INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007060500148 20070605 00148 NM 2007 6 5 AALA20070967 1 20070528 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 666A 25300 MIA - EMERGENCY LIGHT AT SEAT 36D INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 36D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007060500149 20070605 00149 WP 2007 6 5 AALA20070969 1 20070528 A 3397 CONTACT DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 561AA 53091 SFO - OVERHEAD EMERGENCY LIGHTS FROM SEAT ROWS 7 TO 15 INOPERATIVE. CLEANED BATTERY CONTACTS FOR EMERGENCY LIGHTS FROM SEAT ROWS 7 TO 15. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007060500150 20070605 00150 NM 2007 6 5 AALA20070970 1 20070528 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 907AN 29509 DFW - EMERGENCY LIGHT AT FORWARD GALLEY WALL HAS BROKEN BASE. REPLACED LIGHT BASE FOR EMERGENCY LIGHT AT FORWARD GALLEY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007060500151 20070605 00151 NM 2007 6 5 HALA0700234 1 20070531 A 2711 CONTROL SYSTEM BOEING 767 76733A 1385209 NM AILERON TRIM MALFUNCTIONED A HALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 WP 13 587HA 33421 ETOPS SIGNIFICANT SYSTEM, AILERON TRIM UNITS TO THE LEFT DURING TAKEOFF,CLIMB AND APPROACH. OK DURING CRUSE SEGMENT. P ERFORMED OPERATIONAL TEST AILERON AND AILERON TRIM, TRIM CONTROL SYSTEM PER AMM 27-11-00-715-002. OPERATION NORMAL. 2 L 7 2 4F RT A1NM 2007060500152 20070605 00152 NM 2007 6 5 HALA0700232 1 20070529 A 2150 32896961 CONTROL VALVE BOEING 767 767300 1385204 NM A/C PACK MALFUNCTIONED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, LEFT A/C PACK INEFFECTIVE IN COOLING AIRCRAFT. REMOVED AND REPLACED LOW LIMIT CONTROL VALVE I AW AMM 21-51-11 LEFT PACK COOLING SYSTEM OPS CHK NML. 2101877 3541 1009 LT 2 L 7 2 4F RT A1NM 2007060500153 20070605 00153 NM 2007 6 5 HALA0700235 1 20070529 A 5730 SKIN BOEING 717 717200 1383700 NM RWS 432 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 484HA 55129 MODERATE CORROSION ON SURFACE SKIN AROUND FUELING CAP AT APPROX STATION 432 BETWEEN STRINGERS NR 2 AND NR 3, 1 3/4" BY 3 /4" BY .029" DEEP. CLEANED AND TREATED CORROSION PER SRM 51-10-9. PRIMED AND PAINTED. 2 L 7 2 4F TR A6WE 2007060500154 20070605 00154 NM 2007 6 5 HALA0700237 1 20070529 A 5730 FAIRING BOEING 717 717200 1383700 NM RT WING CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 484HA 55129 CRACK ON RT WING INBOARD TRACK FAIRING (ELEPHANT EAR). REPAIRED PER HAL 105, FILE NR B10195. FABRICATED AND INSTALLED DOUBLER WITH PR1440, CORROSION PROTECT. PRIMED AND PAINTED. 2 L 7 2 4F TR A6WE 2007060500155 20070605 00155 NM 2007 6 5 HALA0700238 1 20070529 A 5730 FAIRING BOEING 717 717200 1383700 NM LT WING CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 484HA 55129 CRACK ON LT WING FLAP INBOARD TRACK FAIRING (ELEPHANT EAR). REPAIRED PER HAL M 105, FILE B10195. FABRICATED AND INSTAL LED DOUBLER. INSTALLED WITH PR1440. PRIMED AND PAINTED. 2 L 7 2 4F TR A6WE 2007060500156 20070605 00156 NM 2007 6 5 HALA0700239 1 20070529 A 5310 DOOR FRAME BOEING 717 717200 1383700 NM FUSELAGE CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 484HA 55129 FOUND 3/16" CRACK ON FWD DOOR JAMB FRAME, TOP EDGE, RT WHEELWELL. BLENDED OUT CRACK PER HAL M105 FILE NR 484083. PRIME D AND PAINTED. 2 L 7 2 4F TR A6WE 2007060500157 20070605 00157 NM 2007 6 5 HALA0700236 1 20070529 A 5730 SKIN BOEING 717 717200 1383700 NM RWS 432 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 484HA 55129 MODERATE CORROSION ON SURFACE SKIN AROUND FUELING CAP AT APPROX STATION 432, JUST FWD OF STRINGER NR 2 13/8" BY 2" BY .0 30"DEEP. CLEANED, TREATED CORROSION PER SRM 51-10-9. REPAIRED PER M105 FILE NR 484084. PRIMED AND PAINTED. 2 L 7 2 4F TR A6WE 2007060500159 20070605 00159 EU 2007 6 5 07FDEA02010 1 20070529 A 2432 F11QY3714 TRU AIRBUS 310 A310324 3930206 EU NR 2 SMOKE A FDEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 25 815FD 1744 1744 638 WHEN POWERING UP NOTICED SMOKE WAS COMING FROM THE AVIONICS DEPT, SHUT DOWN A/C. CHECKED OUT THE AREA, THE SMOKE WAS GO NE. POWERED UP THE A/C AGAIN ECAM SHOWED T/R UNIT 2 INOP. INSPECTED THE AREA AGAIN, FOUND NO EVIDENCE OF SMOKE OR DAMA GE WIRING. REMOVED AND REPLACED NR 1, NR 2 T/R AND ESS TRU PER M/M 24-32-11-4 OPS CK GOOD. OFF MFG F11QY3714 POS TR2, SRL 1863R, TAG 2B2564, ON MFG F11QY3714, SRL 2.299R, TAG 53A793 R/I OFF MFG F11QY3714 POS TR1, SRL 8062-091, TAG 03A6 66, ON MFG F11QY3714 SRL 1074, TAG 148A13R/I 29MAY07 15:32. R/I OFF MFG F11QY3714, POS ETR SRL 8004-160, TAG 47887A, ON MFG F11QY3714 SRL 1.970R, TAG B86825. 2 L 7 2 4F RT A35EU 2007060500160 20070605 00160 NM 2007 6 5 07FDEA02011 1 20070529 A 5330 SKIN DOUG MD11 MD11 3023602 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 576FE 48501 FORWARD CARGO AFT LOWER CUTOUT SKIN FOUND DENT. [06-12-07] DENT AT FORWARD CARGO AFT LOWER DOOR CUTOUT SKIN TRIMME D OUT AND CARRIED OUT REPAIR AS PER SRM 53-50-00 FIGURE 17 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007060500161 20070605 00161 NM 2007 6 5 07FDEA02012 1 20070529 A 5330 SKIN DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 576FE 48501 APU - FUSELAGE SKIN EXTERIOR AT APU EXHAUST DOOR LOWER SIDE HINGE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5330 -109892. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007060500162 20070605 00162 NM 2007 6 5 07FDEA02013 1 20070529 A 5330 SKIN DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 576FE 48501 MAIN DECK L3 DOOR CUTOUT FORWARD LOWER CORNER FOUND CORRODED. MAIN DECK L3 DOOR CUTOUT FORWARD LOWER CORNER CARRIED OUT REPAIR AS PER SRM 53-50-00 FIGURE 18 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007060500163 20070605 00163 NM 2007 6 5 07FDEA02014 1 20070529 A 5710 SUPPORT DOUG MD11 MD11 3023602 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 576FE 48501 LEFT WING FIXED LEADING EDGE CAVITY INTERIOR UPPER FACE, XORS 562, SUPPORT STRIP FOUND CRACKED. REPAIR CARRIED OUT AS P ER FEDEX E.A. 1-5710-111112. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007060500164 20070605 00164 NM 2007 6 5 07FDEA02015 1 20070530 A 5711 SPAR DOUG MD11 MD11F 3023600 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 576FE 48501 LEFT WING REAR SPAR, BETWEEN OUTBOARD ISLAND MOUNTING BRACKET NR 1 AND NR 2 FROM OUTBOARD, LOWER FACE FOUND CORRODED. R EPAIRED AS PER FEDEX E.A. 1-5710-111113. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007060500165 20070605 00165 NM 2007 6 5 07FDEA02016 1 20070530 A 5330 65155782 SKIN BOEING 727 7272S2F 1384O81 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 LOWER FUSELAGE VHF NR 2 ANTENNA, SKIN ON FWD LIP DAMAGED, AND BASE PNL FOR ANTENNA IS CRACKED SRM 51-30-2. REMOVED VHF ANTENNA PANEL, REPLACED HAT CHANNEL AND INSTALLED PANEL SRM 51-30-2. 2 L 7 3 4F A3WE 2007060500166 20070605 00166 NM 2007 6 5 AWXA200700680 1 20070529 A 5330 6545765 SKIN BOEING 737 7373G7 1384595 NM BS 460 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 PHX - FUSELAGE SKIN CRACKED JUST ABOVE S10L, BS 460. REPAIRED FUSELAGE SKIN JUST ABOVE S10L, BS 460 IAW B737-300 SRM 53 -00-01-2R-31 DETAIL XIX. 2 L 7 2 4F RT A16WE 2007060500184 20070605 00184 NM 2007 6 5 QXEA200700869 1 20070531 A 3010 TRANSMITTER DHAV DHC8 DHC8202 2809007 NM DEICE SYSTEM MALFUNCTIONED A QXEA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 NM 09 366PH 510 SEA FLIGHT NR 2076, AFTER START AND UNFEATHER BOTH ENGINES NR 2 DEICE PRESSURE INDICATES 8 PSI AFTER SELECTING TO ISO RE AD 0. REPLACED NR 2 DEICE PRESSURE TRANSMITTER. AIRFRAME DEICE TESTS GOOD IAW DHC-8-200 MM 30-10-00. AIRCRAFT RETURNE D TO SERVICE. 2 H 7 2 4T RT A13NM 2007060500197 20070605 00197 NM 2007 6 5 HALA0700240 1 20070602 A 2612 644501 CIRCUIT CARD BOEING 767 767332 1382001 NM FIRE DETECTION DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 EICAS STATUS MSG: ENG FIRE LP 1 DISPLAYED. BIT CHECKED PER FIM 26-11-00. REPLACED LEFT ENG LOOP 1 FIRE DETECTION CARD. FUNCTIONAL CHECKED OK PER A MM 26-10-01. 2 L 7 2 4F RT A1NM 2007060100064 20070601 00064 WP 2007 6 1 NWAA071949987 1 20070524 A 2910 LINE DOUG DC9 DC932 3022066 WP HYD SYSTEM LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 987US 47458 AS THE AIRCRAFT CLIMBED AFTER DEPARTING DFW, THE CREW NOTICED THE LOSS OF FLUID QUANTITY AND PRESSURE FROM THE RIGHT HYD RAULIC SYSTEM. COM PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT CONTINUED TO SCHEDULED DESTINATION. AFTER LANDING UN EVENTFULLY THE LANDING GEAR WAS PINNED AND THE AIRCRAFT WAS TOWED TO THE GATE. MAINTENANCE FOUND FLUID LEAKING FROM A L INE COMING OUT OF THE AUXILIARY PUMP. ELECTRICAL WIRES HAD CHAFED BOTH THE WIRES AND THE LINE TO FAILURE. THE WIRE HAR NESS, THE AUX PUMP, THE ENGINE PUMP, AND FILTERS WERE ALL REPLACED. LEAK CHECK WAS GOOD AND THE AIRCRAFT HAS RETURNED T O SERVICE. 2 L 7 2 4F A6WE 2007060100082 20070601 00082 EU 2007 6 1 TRBA2007026 1 20070521 A 2910 MS21902D6 LINE AEROSP ATR72 ATR72212 8680945 EU HYD SYSTEM BROKEN A TRBA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 29 288AM 288 GREEN HYDRAULIC SYSTEM LO LEVEL INDICATION. REPLACED UNION ON LINE FROM BRAKE DUAL VALVE LINE TO BLUE ACCUMULATOR, OPS CHECK GOOD. 2 H 7 2 4T RT A53EU 2007060100084 20070601 00084 NM 2007 6 1 NWAA072036739 1 20070511 A 5322 TENSION TIE BOEING 747 747251F 1384898 NM BS 860 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 639US 23887 DURING "M" CHECK, FOUND CRACKS IN BS 860 TENSION TIE RT CHANNEL NR 5 AND NR 15 FASTENER HOLES AND ONE FASTENER HOLE OF T HE WEB DOUBLER. REPAIRED PER EA 67-209242 SECT I SECTION II INSPECTION TO BE ACCOMPLISHED AT 3000 CYCLE INTERVALS. 2 L 7 4 4F A20WE 2007060100088 20070601 00088 NM 2007 6 1 NWAA072026739 1 20070515 A 5322 TENSION TIE BOEING 747 747251F 1384898 NM BS 820 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 639US 23887 DURING "M" CHECK, FOUND CRACKS IN BS 820 TENSION TIE FRAME WEB FASTENER HOLES RH NR 4, NR 10 AND LT NR 4, NR 9,NR 10, NR 11 AND NR 13. ALSO, FOUND ONE FASTENER HOLE CRACKED ON FAILSAFE CHORD ON S10A. REPAIRED PER EA 209243 SECT I AND SECT II SECTION III AND IV REQUIRE INSPECTIONS AT 3000 CYCLE INTERVALS. 2 L 7 4 4F A20WE 2007060100095 20070601 00095 NM 2007 6 1 C1HA200796008 1 20070529 A 5313 14981317075T6 STRINGER BOEING 727 7272J4 1384006 NM BS 1183 S22L CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 696CA 22574 AFT CARGO STR 22L AT BS 1183 IS CORRODED. CUT OUT DAMAGED SECTION OF STRINGER 22L AND REPAIRED IAW B727 SRM 53-10-3 FIG 1. 2 L 7 3 4F RT A3WE 2007060100108 20070601 00108 EA 2007 6 1 A6WA200740219 1 20070425 A 3220 WHEEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NLG VIBRATION A A6WA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 31 429AW 7711 HIGH SPEED ABORTED TAKE-OFF DUE TO NOSEWHEEL VIBRATION. SPEED WAS 135 KNOTS, BRAKE TEMPS WERE 7-7-7-7. COMPLIED WITH RE JECTED TAKEOFF INSPECTION IAW AMM 05-51-27-210-801. NO DAMAGE NOTED. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007060500012 20070605 00012 WP 2007 6 5 ASAA0781741 1 20070529 A 5321 99365445 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 CABIN FLOOR PANEL IS DELAMINATED. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PARA 44 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007060500016 20070605 00016 WP 2007 6 5 ASAA0781744 1 20070529 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 AFT CARGO DOOR EXTERIOR SKIN IS DENTED 22 INCHES FROM THE AFT EDGE 14 INCHES FROM THE TOP EDGE. CUT OUT DAMAGED AREA OF SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER AND 2 EACH FINGER DOUBLERS IAW SRM 53-04. 2 L 7 2 4F RT A6WE 2007060500022 20070605 00022 NM 2007 6 5 SWAA072771 1 20070531 A 5730 6545407 SKIN BOEING 737 7373L9 1384470 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND LEFT WING UPPER SKIN CORRODED AT BETWEEN STA 119 AND STA 126, FWD SPAR. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007060500024 20070605 00024 NM 2007 6 5 SWAA072768 1 20070531 A 5711 6545416 SPAR BOEING 737 7373L9 1384470 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND RIGHT WING REAR SPAR UPPER CHORD CRACKED AT STR 2, STA 114. REPAIRED CHORD PER ER. 2 L 7 2 4F RT A16WE 2007060500027 20070605 00027 NM 2007 6 5 SWAA072763 1 20070531 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 782, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007060500031 20070605 00031 NM 2007 6 5 SWAA072766 1 20070531 A 5315 6545834 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 294, BL 0. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500037 20070605 00037 NM 2007 6 5 SWAA072755 1 20070531 A 2560 PH22300L GLOWSTRIP BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 EEPLS PHOTOLUMINESCENT STRIP LOOSE BETWEEN ROW 10 DEF AND ROW 12 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007060500038 20070605 00038 NM 2007 6 5 SWAA072740 1 20070530 A 3350 101331 LENS BOEING 737 7373TO 138447G NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 LEFT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007060500052 20070605 00052 NM 2007 6 5 SWAA072686 1 20070526 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 730SW 27862 DURING SCHEDULED 8Y CHECK, FOUND RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 120. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007060500055 20070605 00055 NM 2007 6 5 SWAA072685 1 20070526 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 202WN 33999 DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER MISSING AT ROW 3 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007060500058 20070605 00058 NM 2007 6 5 SWAA072690 1 20070527 A 2910 654482516 HYDRAULIC LINE BOEING 737 7373A4 1384585 NM RT MLG CHAFED A SWAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 29 676SW 23288 AIRTURN BACK / DECLARED EMERGENCY. THE -A- SYSTEM HYDRAULIC FLUID LOSS ON DEPARTURE FROM PHL. FOUND RIGHT MLG DOWNLOCK ACTUATOR LINE CHAFED. REMOVED AND REPLACED LINE PER MM. 2 L 7 2 4F RT A16WE 2007060500073 20070605 00073 NM 2007 6 5 SWAA072704 1 20070528 A 5311 6546534 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500076 20070605 00076 NM 2007 6 5 SWAA072702 1 20070528 A 5311 6546548 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500077 20070605 00077 NM 2007 6 5 SWAA072681 1 20070526 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500167 20070605 00167 NM 2007 6 5 HALA0700224 1 20070517 A 5280 DOOR BOEING 767 767300 1385204 NM RT MLG PUNCTURED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 592HA 33468 PUNCTURE ON THE INNER SURFACE OF THE MLG DOOR, 52"FROM THE AFT EDGE AND 11" FROM THE LWR EDGE. REPAIRED RT MLG DOOR INN ER SURFACE IAW SRM 52.80.02 AND SRM 51-70.03.0G-0. 2 L 7 2 4F RT A1NM 2007060500168 20070605 00168 NM 2007 6 5 HALA0700223 1 20070516 A 5753 STRUCTURE BOEING 767 767300 1385204 NM LT WING TE FLAP DENTED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 592HA 33468 DENT IN LEFT WING INBOARD AFT FLAP, 6" INBOARD OF THE NUMBER 3 FLAP FAIRING. DENT IS OUT OF LIMITS PER SRM 51-70-10. R EPAIRED LT WING I/B AFT FLAP, USING METAL TO METAL HOT BOND METHOD IAW SRM 57-53-01, AND SRM 51-70-2R. 2 L 7 2 4F RT A1NM 2007060500169 20070605 00169 EU 2007 6 5 07FDEA02017 1 20070530 A 5730 FAIRING AIRBUS 310 A310203 3930313 EU LT WING DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 LEFT NR 3 FLAP TRACK MOVABLE FAIRING HAS TWO AREAS OF DELAMINATED. REMOVED DAMAGE AND BONDED REPAIR PLIES PER SRM 57-20 -35 AND PAINTED PER SRM 51-75-10. 2 L 7 2 4F RT A35EU 2007060500170 20070605 00170 NM 2007 6 5 AWXA200700690 1 20070531 A 5311 90526911 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - FOUND CRACKED FRAME, BS 767, S9L. REPAIRED FRAME, BS 767, S9L IAW AWA ER 03-5311-07143-ES1. 2 L 7 2 4F RT A16WE 2007060500171 20070605 00171 NM 2007 6 5 AWXA200700691 1 20070418 A 5311 90526911 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - FOUND CRACKED FRAME, BS 807, S9L. REPAIRED FRAME, BS 807, S9L IAW AWA ER 03-5311-07143-ES1. 2 L 7 2 4F RT A16WE 2007060500172 20070605 00172 NM 2007 6 5 AWXA200700692 1 20070418 A 5311 654655211 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - FOUND CRACKED FRAME, BS 827, S9L. REPAIRED FRAME, BS 827, S9L IAW AWA ER 03-5311-07143-ES1. 2 L 7 2 4F RT A16WE 2007060500173 20070605 00173 NM 2007 6 5 AWXA200700693 1 20070418 A 5311 65465588 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - FOUND CRACKED FRAME, BS 907, S9L. REPAIRED FRAME, BS 907, S9L IAW AWA ER 03-5311-07143-ES1. 2 L 7 2 4F RT A16WE 2007060500174 20070605 00174 NM 2007 6 5 AWXA200700694 1 20070418 A 5330 654576653 SKIN PANEL BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - FOUND CRACKED FUSELAGE SKIN, BS 500D + 1", S14L AT FASTENER HOLE. REPAIRED FUSELAGE SKIN, BS 500D + 1", S14L IAW B737-300 SRM 53-00-01-2R-30, FIGURE 201. 2 L 7 2 4F RT A16WE 2007060500175 20070605 00175 EU 2007 6 5 07FDEA02018 1 20070530 A 7830 BRACKET AIRBUS 310 A310203 3930313 EU THRUST REVERSER GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 EXHAUST NR 1 ENGINE LT T/R, FWD LATCH MOUNT BRACKET GOUGED. COMPLIED WITH EA NR 6-7830-110747 EXHAUST NR 1 ENGINE LT TR -FWD LATCH MOUNT BRACKET GOUGED. COMPLIED WITH EA NR 6-7830-110747 EXHAUST NR 1 ENGINE LT TR, FWD LATCH MOUNT BRACKET GOUGED. 2 L 7 2 4F RT A35EU 2007060500176 20070605 00176 EU 2007 6 5 07FDEA02019 1 20070530 A 7830 BRACKET AIRBUS 310 A310203 3930313 EU THRUST REVERSER GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 NR 2 ENGINE LT T/R FWD LATCH MOUNT BRACKET GOUGED. COMPLIED WITH EA NR 6-7830-110748 EXHAUST, NR 2 ENGINE LT TR FWD LAT CH MOUNT BRACKET GOUGED. COMPLIED WITH EA NR 6-7830-110747 EXHAUST, NR 1 ENGINE LT TR-FWD LATCH MOUNT BRACKET GOUGED. 2 L 7 2 4F RT A35EU 2007060500177 20070605 00177 EU 2007 6 5 07FDEA02020 1 20070530 A 5280 DOOR AIRBUS 310 A310203 3930313 EU RT MLG DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 RT GEAR DOOR EXTERIOR SURFACE HAS AN AREA OF DELAMINATION APPROX 6" IN DIAMETER IN THE CENTER OF THE COMPOSITE FAIRING, AREA MARKED. REMOVED DAMAGE SKIN IAW SRM 51-77-10. CLEANED AND PREPPED DAMAGE AREA IAW SRM 51- 70-10 MIXED RESIN, FAB BED REPAIR PLIES, MIXED BONDING RESIN AND BONDED PLIES IAW SRM 51-7710. APPLIED PRIMER IAW SRM 51-77-10 AND PAINTED REP AIR AREA IAW SRM 51-75-10. 2 L 7 2 4F RT A35EU 2007060500178 20070605 00178 EU 2007 6 5 07FDEA02021 1 20070530 A 5410 STIFFENER AIRBUS 310 A310203 3930313 EU NR 1 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 ENG NR 1 AFT LOWER PYLON INNER COMPARTMENT AT FLOOR AREA,RIB NR 14 "C"-CHANNEL SUPPORT HAS A CRACK VISIBLE THRU OPEN ACC ESS NR 473 AL. REMOVED AND REPLACED STIFFENER IAW SRM 51-40-21 AND 51-40-00. 2 L 7 2 4F RT A35EU 2007060500179 20070605 00179 NM 2007 6 5 07FDEA02022 1 20070530 A 5320 69142991 INTERCOSTAL BOEING 727 7272S2F 1384O81 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 LT AFT WING BODY FILLET B HYD SYS SVC BAY FRG FRAME INTERCOSTAL IS CRACKED AT NR 1 EMDP PRESSURE HOSE BHD FITTING CUTOUT OB HYD RESERVOIR BS 950A 5, STR 23L. REMOVED DAMAGED INTERCOSTAL REF SRM 51-30-2 MFG NEW INTERCOSTAL REF DWG 69-14299, AND INSTALLED NEW INTERCOSTAL REF SRM 51-30-2 2 L 7 3 4F A3WE 2007060500180 20070605 00180 NM 2007 6 5 07FDEA02023 1 20070530 A 5311 656725061 FRAME BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 AFT PIT, AFT BULKHEAD SUPPORT FRAME IS CORRODED AT FASTENER RECEPTACLE BS 1166, LBL 19-RBL 36, WL 179 REMOVED CORROSION, FOUND 3 AREAS TO BE OUT OF LIMITS, IAW SRM 53-10-1. REMOVED DAMAGED AREA, FABRICATED REPAIR PART OUT OF 7075-T6 .063. FABRICATED FILLERS AND TREATED AND PRIMED, IAW SRM 51-40-4, INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2007060500181 20070605 00181 NM 2007 6 5 07FDEA02024 1 20070530 A 5752 652172642 TAB BOEING 727 7272S2F 1384O81 NM ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 RIGHT WING OTBD AILERON TAB HAS A 37" LONG AREA OF DELAM FROM OTBD EDGE. REMOVED AND REPLACED R/W OTBD AILERON TAB REF M/M 27-10-041-4. PERFORMED ADJ/TEST REF MM 27-10-000-5, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2007060500182 20070605 00182 WP 2007 6 5 07FDEA01941 1 20070522 A 5310 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP DOOR FRAME CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 MAIN CARGO DOOR-LOWER JAMB FITTING NR 5 SHOWS CORROSION AT LOWER FORWARD HOLE. REPAIRED NR 5 LOWER JAMB AND REPLACED SUPPORT FITTING IAW FEDEX EA 8-5230-110663 REV A " FUSELAGE-MAIN CARGO DOOR-LOWER JAMB SUPPORT FITTING INSPECTION AND DOOR RIG". 2 L 7 3 4F RT A22WE 2007060500183 20070605 00183 NM 2007 6 5 TSAA0752026 1 20070521 A 5270 WARNING LIGHT BOEING 737 73776N 13844CH NM CARGO DOOR FALSE ACTIVATION A TSAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 13 746AL 29905 ETOPS FLIGHT 481 SNA-HNL - DURING TAKEOFF RUN, CREW NOTED THE AFT CARGO DOOR OPEN INDICATION LIGHT ON. CREW ABORTED TAK EOFF AT APPROXIMATELY 90 KNOTS AIR SPEED. CREW RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED TH E AFT CARGO DOOR AND VERIFIED THE DOOR WAS CLOSED FOR FLIGHT. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007060500198 20070605 00198 NM 2007 6 5 2007UALA00795 1 20070318 A 2497 WIRE HARNESS AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE IDG BURNED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 842UA 19759 1569 FLIGHT DIVERTED DUE TO NUMEROUS ELECTRICAL FAULT ECAM MESSAGES. *S/D* FAULT TRACED BACK TO IDG POWER SUPPLY WIRING HAR NESS. FOUND PIN-B AND 400VC1 CONNECTOR BURNT. REPLACED IDG WIRING HARNESS IN ENGINE AND PYLON AS WELL AS FEEDER CABLES . ALSO REPLACED IDG AND GENERATOR CONTROL UNIT AS A PRECAUTIONARY MEASURE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007060500199 20070605 00199 NE 2007 6 5 2007UALA00798 2 20070315 A 7532 BLEED VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE DIRTY A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 448UA 32720 32720 842 V10099 ENG 2 COMPRESSOR VANE IMPENDING ENG STALL. WARNING CAME ON-OFF 3 TIMES DURING DESCENT. *S/D* REPLACED LPC BLEED MASTE R ACTUATOR. FOUND HEAVY FUEL LACQUERING ON PRESSURE DROP REGULATOR DURING OVERHAUL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007060500200 20070605 00200 NM 2007 6 5 2007UALA00850 1 20070321 A 5270 WARNING MESSAGE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CARGO DOOR FALSE ACTIVATION A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 827UA 1022 RTFL DUE TO FWD CARGO DOOR ECAM MESSAGE. *S/D* PERFORMED VISUAL CHECK OF FWD CARGO DOOR AND PROXIMITY SENSOR AND DID N OT FIND ANY DEFECTS. CAUSE UNKNOWN AT THIS TIME. 2 L 7 2 4F 4 F RT A28NM E40NE 2007060500201 20070605 00201 EU 2007 6 5 2007UALA01009 1 20070402 A 2910 BHC106004 PRIORITY VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE PTU MANIFOLD LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 424UA 437 506 LOSS OF YELLOW QTY & PRESSURE. DECISION MADE TO DIVERT FLIGHT UNDER AMBER ALERT. *S/D* FOUND PRIORITY VALVE WITH HYDR AULIC FLUID STREAMING OUT. REPLACED PRIORITY VALVE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007060500202 20070605 00202 NM 2007 6 5 2007UALA01456 1 20070510 A 2121 6067071 FAN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CARGO BAY FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 647UA 25284 RTFL DUE TO 'BULK CARGO VENT STATUS MESSAGE'. *S/D* BULK CARGO FAN STATUS MESSAGE, MSG GONE WITH BULK HEAT SWITCH IN N ORM. ANIMALS REMOVED FROM AFFECTED COMPARTMENT. REPLACED BULK CARGO PIT VENT FAN. A/C COMPARTMENT NOW SERVICEABLE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007060500204 20070605 00204 NE 2007 6 5 2007UALA01648 2 20070526 A 7200 ENGINE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 FAILED A UALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 WP 29 193UA 26890 727697 RTFL UNDER AMBER ALERT DUE TO NR 4 ENGINE FAILURE. [07-17-07] ENGINE REPLACED AT SFO FOLLOWING 3-ENGINE FERRY. TEARDO WN FOUND A FAILED STAGE-1 HP TURBINE INNER AIRSEAL. MODE CAUSED BY FLUTTER OF THE AIRSEAL. RESULTANT DAMAGE TO THE HP & LP TURBINES WAS SEVERE. ADDITIONALLY, THE HP COMPRESSOR BLADE TIPS WERE HEAVILY WORN DUE TO THE RESULTANT ROTOR UNBA LANCE. THE FAILURE MODE IS STILL UNDER INVESTIGATION BY PWA. INSTALLED A NEW BRUSH SEAL, AND RING DAMPER, AT EVERY H P TURBINE RE-BUILD. 2 L 7 4 4F 4 F RT A20WE E24NE 2007060500205 20070605 00205 NM 2007 6 5 2007UALA01649 1 20070526 A 2150 ACM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN PRESSURE INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 513UA 24810 FLIGHT DIVERTED AFTER THE CABIN WOULD NOT PRESSURIZE. [08-07-07] FOUND ACM NOT RUNNING. ACCOMPLISHED SERVICE TIP AND OP CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500206 20070605 00206 NM 2007 6 5 2007UALA01650 1 20070526 A 2910 HYDRAULIC SYSTEM BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU UNKNOWN A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 925UA 26646 FLIGHT DIVERTED UNDER AMBER ALERT DUE TO LOW -A- SYSTEM HYDRAULIC PRESSURE PROBLEM. ON SUBSEQUENT FLIGHTS ON GEAR RETRA CTION GOT MASTER CAUTION SIX PACK HYDRAULIC LIGHT WITH BOTH A-SYSTEM LOW PRESSURE LIGHTS ON. SYSTEM-A PRESSURE 3000+ AN D QTY 84% AFTER GEAR RETRACTION. 2 L 7 2 4F 4 F RT A16WE E21EU 2007060500207 20070605 00207 EU 2007 6 5 2007UALA01651 1 20070527 A 2150 A/C PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE OVERHEATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 417UA 483 RTFL DUE TO PACK OVERHEAT PROBLEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007060500208 20070605 00208 NM 2007 6 5 2007UALA01652 1 20070525 A 3350 BR964421 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN OUT OF POSITION A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 819UA 893 EMERGENCY EXIT PATH LIGHT HANGING DOWN FWD SIDE OF FC COAT CLOSET. REPLACED LIGHT ASSY. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007060500209 20070605 00209 NM 2007 6 5 2007UALA01653 1 20070525 A 3250 CONTROLLER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NLG STEERING MALFUNCTIONED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 832UA 1321 NW STEER FAULT DISPLAYED ON UPPER ECAM SCREEN. [06-26-07] TROUBLESHOT SYSTEM AND FOUND FAULT ON STEERING ELECTRO HYD RAULIC MODULE. REPLACED NOSE WHEEL STEERING SERVO CONTROL 6GC. 2 L 7 2 4F 4 F RT A28NM E40NE 2007060500210 20070605 00210 NM 2007 6 5 2007UALA01654 1 20070526 A 5320 PLATE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE DOOR 2R SILL CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 839UA 1507 DOOR 2R SILL PLATE HAS CORROSION JUST FWD OF FRAME 68 AT RBL 58. MAJOR REPAIR ACCOMPLISHED: INSTALLED ANGLE DOUBLER RE PAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007060500211 20070605 00211 NM 2007 6 5 2007UALA01655 1 20070528 A 5330 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 841UA 1545 DAMAGE AT AFT FUSELAGE BETWEEN RIB FR62 & FR63 ON BELLY. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SKIN AT STRINGERS 42L, 43L & 43R. NO STRINGERS DAMAGE NOTED. INSTALLED DOUBLER/TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007060500212 20070605 00212 2007 6 5 2007UALA01656 4 20070527 A 2565 BOTTLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE DOOR 1L SLIDE READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 845UA 1585 DOOR ASSIST BOTTLE PRESSURE AT DOOR 1L READS ZERO. 2 L 7 2 4F 4 F RT A28NM E40NE 2007060500217 20070605 00217 NM 2007 6 5 SWAA072687 1 20070526 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 730SW 27862 DURING SCHEDULED 8Y CHECK, FOUND AFT CARGO BAY FLOORBEAM CORRODED AT BS 773, LBL 17. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500219 20070605 00219 2007 6 5 SWAA072691 4 20070528 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007060500220 20070605 00220 2007 6 5 SWAA072684 4 20070526 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007060500221 20070605 00221 2007 6 5 SWAA072670 4 20070525 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED SERVICE CHECK, L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLAC ED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007060500222 20070605 00222 2007 6 5 SWAA072669 4 20070525 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007060500224 20070605 00224 NM 2007 6 5 SWAA072679 1 20070526 A 3350 OL3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SPV CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007060500226 20070605 00226 NM 2007 6 5 SWAA072739 1 20070528 A 5310 6546818 CREASE BEAM BOEING 737 7373L9 1384470 NM FUSELAGE TORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB TORN BETWEEN BS 986 AND BS 1019, RBL 40 AND RBL 45. REMOVED AND REPLA CED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007060500228 20070605 00228 NM 2007 6 5 SWAA072737 1 20070528 A 2560 6557463 FITTING BOEING 737 7373L9 1384470 NM L2 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2007060500229 20070605 00229 NM 2007 6 5 SWAA072736 1 20070528 A 2560 6557463 FITTING BOEING 737 7373L9 1384470 NM R2 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2007060500231 20070605 00231 NM 2007 6 5 SWAA072738 1 20070528 A 2560 6557463 FITTING BOEING 737 7373L9 1384470 NM L2 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2007060500232 20070605 00232 NM 2007 6 5 SWAA072741 1 20070530 A 5753 6573731 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND LEFT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007060500233 20070605 00233 NM 2007 6 5 SWAA072733 1 20070529 A 3350 6574550 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR EMERGENCY EXIT SLIDE LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007060500237 20070605 00237 NM 2007 6 5 SWAA072746 1 20070530 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 730SW 27862 DURING SCHEDULED 8Y CHECK, FOUND AFT CARGO BAY FLOORBEAM CORRODED AT BS 773, BETWEEN LBL 12 AND RBL 12. REMOVED AND REP LACED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500238 20070605 00238 2007 6 5 SWAA072725 4 20070529 A 2565 D31354 SLIDE BOEING 737 737301 1384611 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007060500240 20070605 00240 EU 2007 6 5 2007UALA01657 1 20070526 A 5522 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT ELEVATOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 420UA 489 THERMOGRAPHIC INSPECTION OF THE LEFT ELEVATOR UPPER SKIN AN INDICATION OF POSSIBLE LIGHTNING STRIKE DAMAGE WAS NOTED AT 25.25 INCHES FROM I/B EDGE AND 18.5 INCHES FROM AFT EDGE OF ELEVATOR. [06-26-07] UPPER SKIN WAS CUT OUT IN AREA OF IND ICATION FOR EVALUATION OF HONEYCOMB MATERIAL. NO DAMAGE TO HONEYCOMB MATERIAL WAS NOTED. SKIN WAS REPAIRED PER UA ENGINE ERING SPECIFICATIONS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007060500241 20070605 00241 EU 2007 6 5 2007UALA01658 1 20070525 A 5310 DOOR FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 440UA 702 CORROSION AT R2 DOOR SILL FRAME 68 AND AT FWD END OF R2 DOOR SILL FR 66. MAJOR REPAIR ACCOMPLISHED: INSTALLED 2EA DOUB LER REPAIRS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007060500242 20070605 00242 EU 2007 6 5 2007UALA01659 1 20070528 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 489UA 1702 EMERGENCY EXIT LIGHTS ON W-SWITCH IN ARM. RESET CIDS AND ACCOMPLISHED EMERGENCY LIGHTING SYSTEM TEST. TEST PASS, EMERG ENCY LIGHTS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007060500246 20070605 00246 NM 2007 6 5 2007UALA01663 1 20070526 A 5230 ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 AFT CARGO DOOR S/N 1571 OUTBOARD ANGLE COMMON TO EXTERNAL SKIN HAS A SMALL PIECE MISSING PUNCHED AT RADIOUS LOCATED AT A PPROXIMATELY 8 INCHES FROM FORWARD EDGE AND 16.5 INCHES FROM TOP EDGE ARE MARKED. MAJOR REPAIR ACCOMPLISHED: REPLACED T-ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007060500247 20070605 00247 NM 2007 6 5 2007UALA01664 1 20070526 A 5230 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 AFT CARGO DOOR S/N 1771 INNER SKIN AND DOUBLER WAS ROUTED OUT TO THE VERY EDGE OUT FASTENERS HEAD AT APPROXIMATELY 9 INC HES FROM TOP AND 9.5 INCHES FROM FORWARD EDGE. MAJOR REPAIR ACCOMPLISHED: REPLACED L-ANGLE & INSTALLED A DOUBLER ON TH E INNER SKIN. 2 L 7 2 4F 4 F RT A16WE E21EU 2007060500248 20070605 00248 2007 6 5 2007UALA01665 4 20070527 A 2565 COVER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EVAC SLIDE DEBONDED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 DOOR 1L PLASTIC CLEAR COVER OVER THE ESCAPE SLIDE PRESS GAUGE IS DISBONDED. [07-03-07] REPLACED SLIDE ASSEMBLY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007060500250 20070605 00250 NM 2007 6 5 2007UALA01667 1 20070526 A 3350 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN MALFUNCTIONED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 105UA 26473 MAIN CABIN EMERGENCY LIGHTS CYCLE ON AND OFF INTERMITTENTLY. TESTED EMERGENCY LIGHTS SEVERAL TIMES, OPS CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007060500254 20070605 00254 2007 6 5 2007UALA01672 4 20070525 A 2565 PIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE PULLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 DOOR L2 SLIDE, PIN IS PULLED OUT OF STITCHING. [06-20-07] REPLACED A FAILED SLIDE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500256 20070605 00256 NM 2007 6 5 2007UALA01674 1 20070527 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 AFT PIT, LEFT SIDE, STA 1400, STR 25L AREA, MAIN FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: REMOVED EXISTING REPAIR FR OM FRAME INBOARD FLANGE AT STR 27L. FABRICATED & INSTALLED A NESTED J-ANGLE REPAIR WHICH IS NESTED INSIDE THE EXISTING CHORD BETWEEN STR 25L AND 27L. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500258 20070605 00258 NM 2007 6 5 2007UALA01676 1 20070528 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 AFT PIT RIGHT SIDE, STA 1560 AT STR 25R, MAIN FRAME DENTED (RIB). MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE AND FABRIC ATED A J-ANGLE REPAIR PIECE AND INSTALLED NESTED INSIDE FRAME INBOARD FLANGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500260 20070605 00260 NM 2007 6 5 2007UALA01678 1 20070528 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 FWD PIT, LEFT SIDE, STA 680, BETWEEN STR 23 - 24L, MAIN FRAME HAS DENT (RIB). MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAG E AND FABRICATED A J-REPAIR ANGLE AND INSTALLED TO NEST INSIDE THE FRAME INBOARD FLANGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500262 20070605 00262 NM 2007 6 5 2007UALA01680 1 20070528 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 FWD PIT LEFT SIDE, STA 580, STR 24L - 25L MAIN FRAME BENT (RIB). MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE AND EXISTIN G PRODUCTION SPLICE AND FABRICATED A REPAIR ANGLE AND INSTALLED. ALSO FABRICATED & INSTALLED 1 EA -80 STRINGER CLIP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500263 20070605 00263 2007 6 5 2007UALA01681 4 20070526 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 DOOR SLIDE 1L FELL OUT ON TO AIR STAIR DUE TO NOT BEING DISARMED. [06-20-07] REMOVED AND REPLACED DOOR 1 LT SLIDE AND EMERGENCY POWER RESERVOIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500266 20070605 00266 NM 2007 6 5 2007UALA01684 1 20070525 A 5330 RIVET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 TWO RIVETS DAMAGED BY LIGHTNING STRIKE STA 630 WL 160 ON LEFT SIDE OF FUSELAGE. REMOVED 2 EA BLIND FASTENERS, STEPPED U P HOLES AS REQUIRED. HFEC REVEALED NO CRACKS. INSTALLED 2EA SOLIDS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500267 20070605 00267 NM 2007 6 5 2007UALA01685 1 20070525 A 5330 RIVET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 RIVET DAMAGED BY LIGHTNING STRIKE STA 720 WL 160 ON LEFT SIDE OF FUSELAGE. REMOVED 1EA BLIND FASTENER, STEPPED UP HOLES AS REQUIRED, HFEC REVEALED NO CRACKS. INSTALLED SOLID FASTENER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500268 20070605 00268 NM 2007 6 5 2007UALA01686 1 20070525 A 2560 FLASHLIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 655UA 25393 EMERGENCY FLASHLIGHT INOPERATIVE. LOCATION FLIGHT ATTENDANT SEAT 260 MID CABIN. [07-10-07] REPLACED EMERGENCY FLASH LIGHT ASSY. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007060500269 20070605 00269 2007 6 5 2007UALA01687 4 20070526 A 2565 SLIDE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT OVERWING DEFECTIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 RIGHT OVERWING SLIDE TRIGGER HITTING ON AFT SUPPORT WHEN CLOSING DOOR. [07-10-07] REPLACED SLIDE BECAUSE RT OVERWING S LIDE FABRIC BINDING AT UPPER AFT AREA WHEN CLOSING SLIDE DOOR. ROOT CAUSE IS SUSPECTED SLIDE CAME PARTIALLY UNPACKED TH ROUGH MULTIPLE DOOR OPERATIONS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007060500275 20070605 00275 NM 2007 6 5 2007UALA01694 1 20070527 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 CEILING EMERGENCY LIGHT AT RIGHT ROW 48 INOPERATIVE. RELAMPED CEILING LIGHT. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007060500276 20070605 00276 NM 2007 6 5 2007UALA01695 1 20070527 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY LIGHTS FWD GALLEY FRONT AND SIDE BOTTOM LIGHT, BOTTOM OF CLOSET BESIDE DOOR 1L, BOTTOM FRONT OF CLOSET NEAR DO OR 1, LAV 110 BOTTOM WALL SIDE & BACK, ROWS 6 TO 8AB, AFT OF DOOR 2 LEFT SIDEWALL & BOTTOM OF CLOSET AFT OF ROW 8 LEFT A RE INOPERATIVE. REPLACED BATTERY. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007060500277 20070605 00277 NM 2007 6 5 2007UALA01696 1 20070527 A 3397 794640 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 FLOOR EMERGENCY LIGHTS SEAT 32HJK TO 34HJK INOP. REPLACED FEEDER CABLE. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007060500278 20070605 00278 NM 2007 6 5 2007UALA01697 1 20070527 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 LEFT OVERWING EXT LAMP 2ND FROM BOTTOM (ONE BULB) & RIGHT OVERWING EMERGENCY LIGHTS LWR BOTTOM (BOTH BULBS) ARE INOP. R ELAMPED EMERGENCY LIGHTS. OPS CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007060500279 20070605 00279 NM 2007 6 5 2007UALA01698 1 20070527 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EXIT SIGN FWD OF DOOR 5 RIGHT LWR CEILING INOP. FOUND WIRES AT LAMP LOOSE. TIGHTENED SAME. OPS CHECKED GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2007060500281 20070605 00281 NM 2007 6 5 2007UALA01700 1 20070526 A 3350 9F19948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EMERGENCY EEL LIGHTS ARE INOP AT SEAT 3A AFT, DOOR 5L LWR WALL CROSSAISLE & DOOR 4L LWR WALL AISLE. REPLACED LIGHT ASSY , OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007060500284 20070605 00284 NM 2007 6 5 2007UALA01703 1 20070528 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRUSHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 FWD PIT- LEFT SIDE, STA 600 BETWEEN STR 22- 25L MAIN FRAME CRUSHED (RIB). MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED & INSTALLED A J-ANGLE REPAIR NESTED INSIDE THE FRAME INBOARD FLANGE. FABRICATED & INSTALLED 2 EA -80 STRINGE R CLIPS. FABRICATED & INSTALLED ONE -6 SHEAR TIE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500285 20070605 00285 NM 2007 6 5 2007UALA01704 1 20070528 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 AFT PIT, LEFT SIDE STA 1420 BETWEEN STR 24- 25L, MAIN FRAME DENTED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE & EXISTI NG PRODUCTION SPLICE. FABRICATED & INSTALLED A NEW PRODUCTION SPLICE ANGLE. FABRICATED & INSTALLED 2 EA -15 STRINGER C LIPS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500286 20070605 00286 NM 2007 6 5 2007UALA01705 1 20070528 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 AFT PIT, LEFT SIDE STA 1440, STR 25L AREA, MAIN FRAME DENTED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE ON FRAME INBOA RD FLANGE BETWEEN STR 23L - 23L & 25L, REMOVED EXISTING PRODUCTION SPLICE. FABRICATED & INSTALLED A NEW PRODUCTION SPLI CE ANGLE. FABRICATED & INSTALLED 3EA -15 STRINGER CLIPS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500291 20070605 00291 NM 2007 6 5 2007UALA01710 1 20070527 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 571UA 26681 BOTH FWD & AFT LEFT WING EXTERIOR OVERWING AND ROW 2CD BULLNOSE EXIT EMERGENCY LIGHTS ARE INOPERATIVE. RELAMPED EMERGEN CY LIGHTS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500294 20070605 00294 NM 2007 6 5 2007UALA01713 1 20070528 A 3397 58781 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 512UA 24809 AFT C-ZONE & FWD A-ZONE EEL FEEDERS ARE DAMAGED. REPAIRED EEL FEEDER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500295 20070605 00295 NM 2007 6 5 2007UALA01714 1 20070526 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 CABIN: EEL FLOOR TRACK LIGHTS MISSING 2 FT SECTION AT ROW 1 E-F, RIGHT SIDE. INSTALLED LIGHT STRIP AT SEAT 1 E-F. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007060500299 20070605 00299 EU 2007 6 5 2007UALA01720 1 20070526 A 2597 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EVAC SLIDE IND DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 417UA 483 CIDS DISPLAY LEFT EMERGENCY SLIDE BOTTLE LOW PRESSURE. [06-26-07] FOUND OPEN WIRE DEU-B (300RH4) PIN 36 TO PLUG 7555 VC-A PIN A. BOTH CONNECTORS VERIFIED OK. SUSPECT LOST CONNECTION AT TERMINAL BLOCK 7225VT OR 7223VT. RESEATED PINS 3CD AT TERMINAL BLOCK 7223VT JUST FWD OF WALLBOX 50MK3. 2 L 7 2 4F 4 F RT A28NM E40NE 2007060500302 20070605 00302 NM 2007 6 5 2007UALA01723 1 20070529 A 2613 OVERHEAT SYS BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RT WING ACTIVATED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 308UA 23669 FLIGHT DIVERTED DUE TO RIGHT WING BODY OVERHEAT INDICATION. [06-22-07] FOUND FAULTY OVERHEAT DETECTOR ELEMENTS. REP LACED DETECTOR ELEMENTS M271 AND M356. 2 L 7 2 4F 4 F RT A16WE E21EU 2007060500305 20070605 00305 NM 2007 6 5 ASAA0791752 1 20070531 A 5320 143A7501165 SILL BOEING 737 737990 NM FWD CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 FWD CARGO PIT LT DUST SILL CORRODED REPAIRED IAW SRM 53 00 53 2 L 7 4 4F RT A16WE 2007060600006 20070606 00006 EA 2007 6 6 A6WA200740193 1 20070413 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 454AW 7842 FOUND PASSENGER DOOR FORWRAD ANCHOR FITTING IS CRACKED. [SUP 06-11-07] REMOVED AND REPLACED FORWARD ANCHOR FITTING IAW CRJ AMM 52-11-17-400-804, P/N 601R380742-3. (M) 2 L 7 2 4F RT A21EA 2007060600008 20070606 00008 EA 2007 6 6 A6WA200740124 1 20070312 A 5320 6013501251 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 413AW 7585 AFT EQUIPMENT COMPARTMENT FS 621 TO 625 OBLIQUE ANGLE ON LEFT SIDE CRACKED 1.5 INCH LONG. MAINTENANCE REMOVED CRACKED A NGLE AND INSTALLED NEW ANGLE P/N 601-35012-51 IAW CRJ SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007060600012 20070606 00012 EA 2007 6 6 A6WA200740110 1 20070307 A 5320 S6144A14 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 413AW 7585 LT FS 484 INTERCOSTAL PREVIOUS REPAIR ANGLE AT LBL 36 CRACKED APPROXIMATELY .1 INCH LONG. MAINTENANCE INSTALLED NEWLY F ABRICATED ANGLE IAW BSC STANDARD REPAIR 601R53-0030A AND BOMBARDIER REO 601R-53-41-059A REV A. (M) 2 L 7 2 4F RT A21EA 2007060600013 20070606 00013 SO 2007 6 6 CHQA200700019 1 20070524 A 2121 INTAKE EMB 135 EMB135LR 3260305 SO RECIRC FAN OBSTRUCTED A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 841RP 145737 FLIGHT 6305 - CVG-HTS - ACRID SMOKY SMELL DETECTED IN CABIN AND COCKPIT ABOUT 1 MINUTE AFTER TAKEOFF. RETURNED TO FIELD . PERFORMED VISUAL INSPECTION OF BOTH RT AND LT PACK BAYS AND DUCTS, NO DEFECTS NOTED. REMOVED FLOOR BOARD TO GAIN ACC ESS TO RECIRC FAN AREA. FOUND DUST AND DEBRIS BLOCKING RECIRC FAN INTAKE SCREEN. REMOVED DUST AND DEBRIS AND PERFORMED OPS CHECK IAW EMB MM 21-24-01. PERFORMED OPS CHECK USING APU AND ENGINE AT MAX TAKEOFF IAW ERJ MM 49-10-00 AND 71-00-0 0. NO SMOKE OR SMELL NOTED. 2 L 7 2 4F RT T00011AT 2007060600014 20070606 00014 EA 2007 6 6 A6WA200740201 1 20070313 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 417AW 7610 CARGO DOOR SILL PLATE HAS MINOR SURFACE CORROSION IN AREA OF NUTPLATES FROM FS 574 TO 621. (M) REPAIRED CARGO DOOR SILL PLATE IAW SRM 51-21-01 AND 51-25-01. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007060600019 20070606 00019 EA 2007 6 6 A6WA200740192 1 20070413 A 2910 BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 454AW 7842 RIGHT MLG BAY Z BRACKET FORWARD OF HYDRAULIC TRANSDUCER IS CRACKED. (M) MAINTENANCE REMOVED AND REPLACED BRACKET PN 60 1R75262-155 IAW SRM 51-42-06. (K) 2 L 7 2 4F RT A21EA 2007060600020 20070606 00020 EA 2007 6 6 A6WA200740127 1 20070309 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 413AW 7585 LEFT WING OUTBOARD FUEL PANEL 550BB FOUND CORROSION AROUND WING PLANK APPROX .005 INCH DEEP IN NON-CRITICAL AREA. MAINT ENANCE REPAIRED CORROSION BY BLENDING IAW BOMBARDIER REO 601R-57-030 REV F. (M) 2 L 7 2 4F RT A21EA 2007060600023 20070606 00023 EA 2007 6 6 A6WA200740194 1 20070413 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 454AW 7842 FOUND PASSENGER DOOR AFT ANCHOR FITTING IS CRACKED. [SUP 06-11-07] REMOVED FITTING IAW CRJ AMM 52-11-17-000-804 AND IN STALLED NEW FITTING P/N 601R380741-3 IAW CRJ AMM 52-11-17-400-804. (M) 2 L 7 2 4F RT A21EA 2007060600024 20070606 00024 EA 2007 6 6 CHQA200700020 1 20070531 A 2741 SWITCH CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB DIRTY A CHQA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 11 471SM 7613 FLIGHT 3332 - PVD-CLE - ON CLIMB-OUT AROUND 2000 AGL, FO WAS HAND FLYING, RECEIVED STAB TRIM AND MACH TRIM FAIL MESSAGES . TRIM WOULD NOT RE-ENGAGE. TRIM FAILED AT 5.8 UNITS. DECLARED AN EMERGENCY AND PROCEEDED IMMEDIATELY BACK TO PVD FOR OV ERWEIGHT LANDING. MAINTENANCE CLEANED SWITCHES, RESET HSCU AND MACH TRIM. OPERATION FLIGHT WAS GOOD. 2 L 7 2 4F RT A21EA 2007060600027 20070606 00027 EA 2007 6 6 A6WA200740190 1 20070413 A 2571 RIB CNDAIR CL600 CL6002B19 1900309 EA BATTERY BOX CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 454AW 7842 FOUND RIGHT BATTERY RIB IS CRACKED. (M) MAINTENANCE REPAIRED RT BATTERY RIB IAW EO 601R-57-51-046. (K) 2 L 7 2 4F RT A21EA 2007060100104 20070601 00104 NM 2007 6 1 C1HA200796007 1 20070529 A 5313 652427624 STRINGER BOEING 727 7272J4 1384006 NM BS 1183 S26L CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 696CA 22574 CORROSION STRINGER 26R TENSION FITTING AT 1183. REMOVED AND REPLACED BS 1183 STR 26L TENSION FITTING PN 65-24276-24 IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007060400074 20070604 00074 NM 2007 6 4 QXEA200700870 1 20070601 A 5100 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 405QX 4047 SEA FLIGHT NR 2496: CHECK PFD 1 ILLUMINATED. 3 SECONDS LATER, CHECK ED ILLUMINATED. RAN PFD 1 CHECKLIST. CAUTION DID NOT GO AWAY. RAN SECOND CHECKLIST, ED MESSAGE WENT AWAY. MAINTENANCE REINITIALIZED PFD'S AND ED. ALL FAULTS WENT AWAY AND DID NOT REAPPEAR. PERFORMED OPS CHECK OF PFD 1 IAW MTC 6316104. OPS CHECK GOOD. PERFORMED OPS CHECK OF ED IAW AM M TASK 31-61-01-710-803. OPS CHECK GOOD. AIRCRAFT REMAINS CAT 3 AND FLIGHT DECK PLACARD REFLECTS SAME. MTS CONTROL WA S NOTIFIED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007060400075 20070604 00075 2007 6 4 QXEA200700871 4 20070531 A 3100 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN A QXEA O OTHER J WARNING INDICATION LD LANDING 1 NM 09 418QX 4143 SEA FLIGHT NR 2274: NR 2 DC GEN CAUTION LIGHT ILLUMINATED AFTER TOUCHDOWN. THE CHECKLIST WAS ACCOMPLISHED AND THE CAUTIO N LIGHT EXTINGUISHED. MAINTENANCE C/W FIM TASK 24-30-00-810-813. INTERROGATED EPCU FOR RELATED FAULT CODES. NONE FOUN D. PERFORMED OPS CHECK OF MAIN 28 V DC GENERATION SYSTEM IAW AMM 24-31-00-710-802. OPS CHECK NORMAL. ALSO PERFORMED V ISUAL INSPECTION OF NR 2 DC GENERATOR INSTALLATION. NO FAULTS NOTE. NO PARTS REPLACED AND AIRCRAFT WAS RETURNED TO SER VICE. 2 H 7 2 4T RT A13NM 2007060400076 20070604 00076 NM 2007 6 4 TSAA0726029 1 20070531 A 2612 899929 FIRE DETECTOR BOEING 737 7372Y5 1384554 NM PWA JT8 JT8D9A 52048 NE NR 1 NACELLE FAILED A TSAA E ENGINE SHUTDOWN N FALSE WARNING TX TAXI/GRND HDL 1 WP 13 810AL 24031 P687772B FLIGHT 93 HNL-LIH - AFTER STARTING THE NR 1 ENGINE, THE CREW NOTED THE NR 1 ENGINE FIRE INDICATION LIGHT ILLUMINATED. C REW FOLLOWED THE QRH PROCEDURES: SHUT DOWN NR 1 ENGINE AND DISCHARGED BOTH ENGINE FIRE EXTINGUISHER BOTTLES. AIRCRAFT W AS TOWED BACK TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THAT THERE HAD NOT BEEN AN ENGINE FIRE. MAINTENA NCE REMOVED AND REPLACED THE NR 1 ENGINE LOWER FIRE DETECTION LOOP, AND BOTH ENGINE FIRE EXTINGUISHER BOTTLES. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4U 4 F RT A16WE E2EA 2007060400077 20070604 00077 NM 2007 6 4 QXEA200700845 1 20070528 A 7930 2379003001 REGULATOR DHAV DHC8 DHC8202 2809007 NM FUEL SYSTEM MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 347PH 15609 380 480 PDX FLIGHT NR 2139 ON TAKEOFF AT 1000' AGL WHEN FLAPS SELECTED UP, RECEIVED MASTER CAUTION "RUD PRESS" AND "RUD FULL PRE SS". UPON SELECTING FLAPS DOWN DURING LANDING PHASE BOTH CAUTION LIGHTS WENT OUT. AIRCRAFT DID NO LAND ABOVE MAX LANDI NG WEIGHT. WITH NR 1 AND NR 2 HYDRAULIC SYSTEMS PRESSURIZED SIMULATED AIRSPEEDS GREATER THAN 140 KTS CAUSE RUD FULL PRE SS AND RUD PRESS CAUTION LIGHTS TO ILLUMINATED. WITH AIRSPEED A 0 WHEN NR 2 RUD PUSH TO OFF SWITCH SELECTED ONLY NR 2 R UD HYD CAUTION LIGHT ILLUMINATES. REPLACED RUDDER FUEL PRESSURE REGULATOR IAW DHC=8-200 MM TASKS 27-20-38-000-801 AND 2 7-20-38-400-801. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007060400078 20070604 00078 WP 2007 6 4 07FDEA01981 1 20070525 A 5311 ADA02334 FRAME DOUG MD10 MD1010F 3022112 WP BS 1002 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 FORWARD LOWER CARGO, DOOR TORQUE BOX FORWARD FRAME CORRODED. REMOVED CORROSION FROM FRAME AND WEB AND FOUND MATERIAL LO SS FOR BOTH TO EXCEED ALLOWABLE LIMITS IAW MD/DC 10 SRM53-00-01 VOL I FIG 1B. REPAIRED FRAME IAW FED EX EA NR 8-5350-10 9161 "FUSELAGE-FWD LOWER CARGO DOOR JAMB FRAME STA 1002 CORD-REPAIR". REPAIRED WEB IAW MD/DC10 SRM 53-00-01 VOL I FIG 1 0. 2 L 7 3 4F RT A22WE 2007060400079 20070604 00079 WP 2007 6 4 07FDEA01982 1 20070525 A 5315 ADA02333 FLOORBEAM DOUG MD10 MD1010F 3022112 WP BS 895 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 FORWARD LOWER CARGO, DOOR TORQUE BOX FORWARD FRAME CORRODED. REMOVED CORROSION FROM FRAME AND SUPPORT BRACKET AND FOUND BOTH TO EXCEED ALLOWABLE LIMITS IAW MD/DC 10 SRM 53-00-01 VOL I FIG 1B. REPAIRED FRAME IAW FED EX EA NR 8-5350-109160 "FUSELAGE FWD LOWER CARGO DOOR JAMB FRAME STA 895 CORD REPAIR". FABRICATED AND INSTALLED NEW SUPPORT BRACKET IAW DAC DW G ADA0233 REV L AND DC/MD10 SRM 51-33-01 VOL II PG 1. 2 L 7 3 4F RT A22WE 2007060400080 20070604 00080 WP 2007 6 4 07FDEA01983 1 20070525 A 5511 ALC70832 SPAR DOUG MD10 MD1010F 3022112 WP HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 RT HORIZONTAL STABILIZER OUTBOARD LEADING BOTTOM ATTACH ANGLE CRACKED. REPAIRED IAW FEDEX EA NR 8-5510-109166 "STABILIZE RS, RT STAB LOWER LEADING EDGE, SPAR CRACK REPAIR". 2 L 7 3 4F RT A22WE 2007060400081 20070604 00081 NM 2007 6 4 07FDEA01984 1 20070526 A 5313 STRINGER BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 465FE 21289 FWD CARGO A/C DISTRIBUTION BAY LT FLOOR STR-26L BADLY CORRODED APPROXIMATELY FS-720F-740. JUST O/B OF DUCT. REMOVED CO RRODED SECTION OF STRINGER AT STA 720C TO 740 AND SPLICED IN A NEW SECTION OF STRINGER ON 26L IAW 727 SRM-53-10-3 FIG 1, STRINGER ORIG P/N#65-56236-18. 2 L 7 3 4F A3WE 2007060400082 20070604 00082 NM 2007 6 4 07FDEA01985 1 20070526 A 5313 STRINGER BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 465FE 21289 FWD CARGO A/C DISTRIBUTION BAY LT FLOOR STR-26L BADLY CORRODED APPROXIMATELY FS- 720F-740. JUST O/B OF DUCT. REMOVED CORRODED SECTION OF STRINGER AT STA 720C TO 740 AND SPLICED IN A NEW SECTION OF STRINGER ON 26L IAW 727 SRM-53-10-3 FIG 1, STRINGER ORIG P/N NR 65-56236-18. 2 L 7 3 4F A3WE 2007060400083 20070604 00083 NM 2007 6 4 07FDEA01986 1 20070526 A 3220 ROD BOEING 727 727225 1384077 NM NLG UNKNOWN A FDEA O OTHER J WARNING INDICATION LD LANDING 1 SO 25 462FE 22550 AFTER TAKE OFF FROM MEM, GEAR WAS RET AND THE FWD RED GEAR DOORS LT REMAINED ILLUM WITH ASSOC NOSE GEAR DOOR LT ILLUM ON S/O'S PANEL. C/W QRH, RECYCLED GEAR AND IND REMAINED. CONT'D FLT WITH APPROPRIATE RESTRICTIONS. UPON LDG IN ICT WITH NORM TOUCHDOWN, THE NOSE GEAR BEGAN TO SHAKE VIOLENTLY AT ABOUT 120KTS. NOSE WHEEL STEERING WAS NOT AVAIL. STOPPED A/ C ON THE RWY AND HAD NOSE GEAR PINNED AND TOWED IN. REMOVED AND REPLACED NOSE GEAR PISTON POS ROD, APEX PIN PER M/M. R EMOVED AND REPLACED RT AFT NOSE GEAR DOOR PER M/M. REMOVED AND REPLACED LOWER NOSE GEAR TORSION LINK PER M/M. REMOVED A ND REPLACED NOSE GEAR POS SW PER M/M AND OP'S CK'D PER MM. OP'S CK GOOD. PERF'D NOSE GEAR EXT/RET PER M/M AND CK'D NOS 2 L 7 3 4F A3WE 2007060400084 20070604 00084 EU 2007 6 4 07FDEA01987 1 20070526 A 2910 LINE AIRBUS 310 A310203 3930313 EU HYD SYSTEM LEAKING A FDEA O OTHER K FLUID LOSS LD LANDING 1 SO 25 405FE 237 ON LANDING WITH MEDIUM AUTOBRAKES, LOST ALL GRN SYS HYD QTY GREEN HYD PUMPS WERE SHUT DOWN WITHIN 30 SECONDS. LARGE HYD LEAK SEEN ON RT LANDING GEAR. INVESTIGATING ORIGIN OF LEAK. LOCATED HYD LINE ON RT MLG AT TOP OF GEAR P/N A3241014500 000 RUPTURED. REMOVED LINE AND CAPPED. RAN GRN SYS HYD WITH ELEC AND ENG PUMPS AFTER SERVICING GREEN HYD SYS. NO FURT HER LEAKS DETECTED. AWAITING NEW HYD LINE TO EFFECT REPAIR. ALSO, INSPECTED ENG PUMP DELTA P'S NONE WERE POPPED. REMO VED AND REPLACED RUPTURED HYD LINE AS REQUIRED, LEAK CHK GOOD ON GROUND AT THIS STATION, REF A310 MM 20-23-1 2-0, 29-00-00-4 AND SMP. 2 L 7 2 4F RT A35EU 2007060400085 20070604 00085 NM 2007 6 4 07FDEA01988 1 20070526 A 5340 651631744 ATTACH FITTING BOEING 727 727200 138407E NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 MAIN DECK BODY FRAME INTERCOSTAL ASSY CLIP IS CRACKED BS 351 FWD, STR 15L. REMOVED WEB, REMOVED CLIP, DRILLED AND INSTA LLED NEW CLIP, REINSTALLED WEB REF SRM 51-30-2 FIG. 2 L 7 3 4F RT A3WE 2007060400086 20070604 00086 NM 2007 6 4 07FDEA01989 1 20070526 A 5340 6916970501 ATTACH FITTING BOEING 727 7272S2F 1384O81 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 MAIN DECK BODY FRAME INTERCOSTAL ASSY CLIP IS CRACKED BS 348 AFT, STR 15L. REMOVED PANEL FWD OF STR 15L, STA 348, REMOV ED DOOR STOP, REF SRM 51-30-2 FIG 1. REMOVED DAMAGE CLIP, NEW CLIP INSTALLED ON N/R N00991 WIP NR 4, DOOR STOP. REINST ALLED ON N/R N00991 WIP, NR 4. 2 L 7 3 4F A3WE 2007060400087 20070604 00087 NM 2007 6 4 07FDEA01990 1 20070527 A 5710 UNKNOWN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 576FE 48501 LEFT WING FIXED LEADING EDGE TELESCOPING DUCT CUTOUT FOUND CRACKED. [06-12-07] REPAIR CARRIED OUT AT LEFT HAND WING FIXED LEADING EDGE TELESCOPING DUCT CUTOUT AREA AS PER SRM 57-10-00 FIGURE 43 VOLUME I AND FEDEX E.A. 1-5730-109887 . REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007060400088 20070604 00088 NM 2007 6 4 07FDEA01991 1 20070528 A 5753 HINGE FITTING DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RIGHT WING, O/B FLAP I/B HINGE FITTING FOUND CRACK AT STA XOF 556. [06-18-07] RIGHT WING - O/B FLAP ASSEMBLY REMOVE D AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATIONAL TEST CARRIED OUT AS PER AMM 27-50-00-5, FOUND SATIS . 2 L 7 3 4F RT A22WE 2007060400089 20070604 00089 NM 2007 6 4 07FDEA01992 1 20070529 A 5313 STRINGER DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 CTR CARGO: UNDER FLOOR STA 1821, RT X=56 FOUND STRINGER JOINT END CRACKED. [06-19-07] REPAIR CARRIED OUT AT CTR CARGO: UNDER FLOOR STA 1821, STRINGER S43R JOINT END AS PER SRM 51-33-01 VOLUME II. 2 L 7 3 4F RT A22WE 2007060400090 20070604 00090 WP 2007 6 4 07FDEA01993 1 20070529 A 5312 AFA01613 BULKHEAD DOUG DC10 DC1010 3022110 WP BS 1491 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 CLG W/W SPACE 2 EA CRACKS ON LT VERTICAL BULKHEAD. REPAIRED IAW SRM 53-00-01 FIG 10 VOL 1. 2 L 7 3 4F A22WE 2007060400091 20070604 00091 EA 2007 6 4 QXEA200700846 1 20070525 A 2410 766277B IDG CNDAIR CL600 CL6002C10 1390015 EA MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 607QX 9766 10024 BUR - FLIGHT 2508 - IDG NR 2 STATUS MESSAGE. RETURNED TO THE GATE. MAINTENANCE PLACED THE IDG ON MEL AND ADDITIONAL FU EL WAS ADDED TO THE AIRCRAFT. THE IDG WAS REPLACED MEL CLOSED. RETURN TO SERVICE. 2 L 7 2 4F RT A21EA 2007060400092 20070604 00092 EA 2007 6 4 QXEA200700872 1 20070531 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002C10 1390015 EA ILLUMINATED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 606QX 10023 SEA - FIRE SYSTEM FAULT MESSAGE. PLACED THE SYSTEM ON MEL 26-00-1. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007060400093 20070604 00093 NE 2007 6 4 TSAA0772028 2 20070524 A 7230 COMPRESSOR WHEEL BOEING 737 737282C 13844AU NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAILED A TSAA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 13 826AL 68833 23051 665322 NON-ETOPS CARGO FLIGHT 956 HNL-ITO - DURING CLIMB AT 24500 FEET, CREW HEARD WHAT SOUNDED LIKE A COMPRESSOR STALL FROM TH E NR 1 ENGINE. CREW REDUCED POWER SETTINGS AND ALL ENGINE PARAMETERS WERE NORMAL. CREW LANDED IN ITO WITHOUT FURTHER I NCIDENT. MAINTENANCE FOUND DAMAGE TO THE C2 DISK AND NUMEROUS STATOR VANES. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE PER ALOHA MAINTENANCE FORMS M-211, M-212, M-213 AND M-215. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2007060400094 20070604 00094 NM 2007 6 4 AALA20070943 1 20070526 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 761AJ 31478 NRT - EMERGENCY LIGHT AT FIRST CLASS CLOSET LOWER LEFT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FIRS T CLASS CLOSET LOWER LEFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007060400095 20070604 00095 WP 2007 6 4 AALA20070944 1 20070525 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 405A 49316 LGA - EMERGENCY LIGHT AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 33 FOR EMERGENCY LIGHT AT FORWARD CABIN . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007060400096 20070604 00096 NM 2007 6 4 AALA20070947 1 20070526 A 3350 0201720001 LIGHT BOEING 737 737823 13844BZ NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 925AN 29526 TPA - MAINTENANCE ENTRY AISLE PATH EMERGENCY LIGHT AT SEAT ROW 16D MISSING. REPLACED LIGHT ASSEMBLY FOR AISLE PATH EMER GENCY LIGHT AT SEAT ROW 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007060400097 20070604 00097 WP 2007 6 4 AALA20070950 1 20070526 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 575AM 53152 DFW - OVERHEAD EMERGENCY LIGHTS AT SEAT ROW 26 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT SEAT ROW 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007060400098 20070604 00098 NM 2007 6 4 AALA20070951 1 20070526 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 975AN 29545 MIA - EMERGENCY LIGHT IN CABIN HAS BROKEN LENS ATTACHMENT. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT IN CABIN. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007060400099 20070604 00099 EU 2007 6 4 AALA20070953 1 20070527 A 3260 BDM3003 PROXIMITY SENSOR AIRBUS 300 A300B4605R 3930308 EU MLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 77080 626 MIA INFLIGHT T2217/27 - AFTER TAKEOFF GEAR WOULD NOT RETRACT. HANDLE WOULD NOT GO INTO THE UP POSITION FROM NEUTRAL. R ETURNED TO MIA AND LANDED WITHOUT INCIDENT. FOUND SENSOR 9GA BOGIE BEAN PROXIMITY DETECTOR SYSTEM 1 AT FAULT. REPLACED SENSOR 9GA AND PROXIMITY BOX. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007060400100 20070604 00100 NM 2007 6 4 AALA20070954 1 20070527 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 389AA 27449 SFO - EXTERIOR EMERGENCY LIGHTS ON RIGHT SIDE OF AIRCRAFT INOPERATIVE. REPLACED BATTERY PACK AT M731 FOR EXTERIOR EMERG ENCY LIGHTS ON RIGHT SIDE OF AIRCRAFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007060400101 20070604 00101 NM 2007 6 4 AALA20070942 1 20070525 A 2597 CONNECTOR BOEING 767 767323 1385205 NM ESCAPE SLIDE INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 376AN 25445 JFK - DURING SQUIB TEST LEFT WING SLIDE SQUIB INOPERATIVE. RESEATED CONNECTOR TO BATTERY PACK FOR LEFT WING SLIDE SQUIB . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007060400102 20070604 00102 EU 2007 6 4 AALA20070952 1 20070527 A 3220 RELAY AIRBUS 300 A300B4605R 3930308 EU NOSE GEAR FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 77080 626 MIA INFLIGHT T2217/27MAY MCO TO SJU - DURING CLIMB, AIRCRAFT GETTING INDICATION OF MULTIPULE PROBLEMS. LANDED MIA WITHO UT INCIDENT. REPLACED GEAR RELAYS 996B AND 966B AND PROXIMITY BOX. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007060400103 20070604 00103 NM 2007 6 4 AALA20070948 1 20070526 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 674AN 29424 MIA - EMERGENCY LIGHT AT SEAT ROW 26 INOPERATIVE. REPLACED LEFT BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 26. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007060500003 20070605 00003 2007 6 5 07FDEA02033 4 20070531 A 2200 UNKNOWN AIRBUS 310 A310 EU UNKNOWN A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 449FE 217 SHORTLY AFTER T/O A/C ACTED AS IF THERE WAS GROUND SENSING PROBLEM, MALFUNCTIONS TO INCLUDE; ATS 1, PITCH TRIM 1, AL L THREE PITOT PROBE, CAPT TAT, BOTH PRESS CONTROLERS: GEAR WOULD NOT RETRACT SYS 1, A/P 1&2 INOP. INSTALLED NEW NOSE STRUT SENSOR 55GB PROBE HEAT AND PRESSURIZATION CONTROLLERS CHECK OK. ENGAGED BOTH AP. EACH AP ENGAGES. 2 L 7 2 4F RT A35EU 2007060500004 20070605 00004 NM 2007 6 5 07FDEA02041 1 20070601 A 5347 SEAT TRACK BOEING 727 727200 138407E NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 465FE 21289 CABIN FLOOR SEAT TRACK HAS CORR, FS 460-620, RBL-24". REMOVED CORRODED SEAT TRACK AT RBL 24 , STA 480 TO 620 IAW B727 SR M 53-10-5. FAB NEW SECTION OF SEAT TRACK PO 1142187. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED SEAT TRACK IAW B727 SRM 53-10-5 FIG#1. REMOVED CABLE GUARD AT STA 480- 500. RECEIVED NEW CABLE GUARD ON TRAVELLER T7/680992 LO CATED AND INSTALLED IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007060500007 20070605 00007 NM 2007 6 5 ASAA0741706 1 20070526 A 5320 6547951503 SCUFF PLATE BOEING 737 737490 1384715 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 706AS 28894 AFT CARGO DOOR AFT SCUFF PLATE CRACKED. AFT CARGO PIT AFT SCUFF PLATE REPAIRED IAW ASA EA 5320 01456. 2 L 7 2 4F RT A16WE 2007060500017 20070605 00017 WP 2007 6 5 ASAA0781745 1 20070529 A 5330 595305077 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 EXTERNAL FUSELAGE DENTED AT STA 579 BETWEEN LONG 20L AND 21L. MEASURED DENT AT 4.0 X .015 INCH WITHIN LIMITS PER SRM. REPAIRED IAW SRM 53-04 FIG 38 SHEETS 12 AND 21. COLD FORMED SKIN BACK TO ORIGINAL BLUEPRINT CONTOUR AND ACCOMPLISHED HF EC INSPECTION FABRICATED AND INSTALLED INTERNAL REPAIR DOUBLER. 2 L 7 2 4F RT A6WE 2007060500033 20070605 00033 NM 2007 6 5 SWAA072762 1 20070531 A 5311 6546555 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500040 20070605 00040 NM 2007 6 5 SWAA072728 1 20070529 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 474WN 33861 EEPLS COVER LOOSE AT LEFT OVERWING EXIT. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007060500050 20070605 00050 NM 2007 6 5 SWAA072729 1 20070529 A 5755 654645262A SPOILER BOEING 737 7373H4 1384600 NM LT WING BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED A2 CHECK, FOUND LEFT WING NR 4 GROUND SPOILER OUTBOARD HINGE LUG BROKEN. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007060500053 20070605 00053 GL 2007 6 5 SWAA072689 2 20070526 A 7200 332A1000 ENGINE BOEING 737 7373H4 1384600 NM CFMINT CFM56 CFM563B1US GL NR 1 DAMAGED A SWAA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SW 29 358SW 26595 721468 INFLIGHT SHUTDOWN / AIRTURN BACK / DECLARED EMERGENCY. NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED INTERMITTENTLY D URING CLIMB. PER QRH REDUCED POWER, OIL LIGHT STILL INTERMITTENT, SHUT DOWN ENGINE PER QRH. FOUND FOD AT OIL SCAVENGE FILTER. REMOVED AND REPLACED NR 1 ENGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E2GL 2007060500071 20070605 00071 NM 2007 6 5 SWAA072700 1 20070528 A 5311 6546532 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500079 20070605 00079 NM 2007 6 5 SWAA072724 1 20070529 A 5311 6546551 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500086 20070605 00086 NM 2007 6 5 SWAA072712 1 20070529 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM L1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007060500089 20070605 00089 NM 2007 6 5 SWAA072721 1 20070529 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500112 20070605 00112 EU 2007 6 5 07FDEA01964 1 20070524 A 5522 SKIN AIRBUS 310 A310203 3930313 EU RT ELEVATOR DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 RT ELEV L/E 3" FROM I/B EDGE HAS DELAM. REMOVED RT ELEV I/B TIP IAW MM 55-24-11-4. REPAIRED TIP IAW SRM 55-24-11,RE-IN STALLED TIP IAW MM 55-24-11-4. 2 L 7 2 4F RT A35EU 2007060500113 20070605 00113 NM 2007 6 5 07FDEA02040 1 20070601 A 5330 651753073 SKIN BOEING 727 727233 138408A NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 286FE 22623 ON AGING A/C INSP, FOUND EXISTING REPAIR DID NOT CONFORM TO FED EX STD REWORK DWG SR27-53-024. REMOVED OLD DOUBLER SRM 51-30-2, HFEC VERIFY OF CRACK CONTAINMENT, MANUFACTURED NEW DOUBLER PER DWG SR27-53-024, TREATED AND PRIMED DOUBLER REF MM 51-20-151-7. INSTALLED NEW DOUBLER AND FASTENERS RE SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007060500114 20070605 00114 EU 2007 6 5 07FDEA02042 1 20070601 A 5347 A5327828820300 CARGO TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 662FE 761 MAIN CARGO COMPT AT FR 62, 27" TO 36" RIGHT OF BL, TIEDOWN TRACK WORN. REMOVED AND REPLACED ADAPTER TRACK IAW A300-600 SRM 51-40-21, PARAGRAPH 7. 2 L 7 2 4F RT A35EU 2007060500115 20070605 00115 NM 2007 6 5 AWXA200700689 1 20070418 A 5330 654576653 SKIN BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - CRACKED FUSELAGE SKIN AT FASTENER HOLE, BS 500C + 11", S14L. REPAIRED FUSELAGE SKIN AT FASTENER HOLE, BS 500C + 1 1", S14L IAW B737-300 SRM 53-00-01-2R3, FIGURE 201. 2 L 7 2 4F RT A16WE 2007060500117 20070605 00117 NM 2007 6 5 AALA20070955 1 20070527 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 389AA 27449 SFO - EXTERIOR EMERGENCY LIGHT ON LEFT SIDE POSITION NUMBER THREE INOPERATIVE. RELAMPED L642 EXTERIOR EMERGENCY LIGHT O N LEFT SIDE POSITION NUMBER THREE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007060500185 20070605 00185 NM 2007 6 5 AWXA200700682 1 20070515 A 3233 HOSE AIRBUS A319 A319132 3930340 NM RT MLG LEAKING A AWXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 806AW 1056 LAX - CREW REPORTED LOW GRN HYD PRESS, FOLLOWED BY PTU, LOW LVL. CREW DECLARED AN EMERGENCY DUE TO LOSS OF NOSE WHEEL S TEERING. THE LANDING WAS UNEVENTFUL AND THE A/C WAS TOWED TO THE GATE. MX FOUND THE RIGHT GEAR DOOR ACT HOSE ASSY LEAK ING. MX REPLACED HOSE ASSY, PER 32-12-00 OPS, LEAK CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007060500186 20070605 00186 NM 2007 6 5 AWXA200700683 1 20070524 A 7921 550220011 COOLER AIRBUS A319 A319132 3930340 NM NR 1 ENGINE LEAKING A AWXA O OTHER O OTHER DE DESCENT 1 WP 28 818AW 21337 21337 1375 EWR - CREW REPORTED THE NR 1 ENGINE WILL NOT GO TO IDLE IN FLIGHT, IDLES AT 75 PERCENT N2 WHILE NR 2 IDLES AT 69 PERCENT , FUEL FLOW SPLIT AS WELL. THE CREW DECLARED AN EMERGENCY. THE LANDING WAS UNEVENTFUL. THE A/C TAXIED TO THE GATE. M X REMOVED AND REPLACED FCOC AND FUEL DIVERTER PER AMM 79-21-43. OPERATIONAL/LEAK CHECK WAS GOOD. A/C WAS RETURNED TO S ERVICE. 2 L 7 2 4F RT A28NM 2007060500187 20070605 00187 NM 2007 6 5 AWXA200700684 1 20070516 A 3260 WARNING HORN BOEING 737 7373S3 1384711 NM MLG FALSE ACTIVATION A AWXA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 WP 28 315AW 23734 PHX - CREW REPORTED WITH FLAPS AT 15 THE GEAR WARNING HORN SOUNDED. CREW WENT TO FLAPS AT 10 WARNING HORN QUIT, WENT BA CK TO FLAPS AT 15 THE WARNING HORN SOUNDED AGAIN. CREW DID A GO AROUND AND DECLARED AN EMERGENCY. THE LANDING WAS UNEV ENTFUL. THE A/C TAXIED TO THE GATE. MX PERFORMED LANDING GEAR AURAL WARNING SYSTEM TEST ON EACH GEAR SEPARATELY IAW A1 B31022. OPS CHECK WAS GOOD, NO FAULTS FOUND. 2 L 7 2 4F RT A16WE 2007060500188 20070605 00188 NM 2007 6 5 AWXA200700685 1 20070520 A 2134 1303A000004 VALVE AIRBUS A319 A319132 3930340 NM A/C PACK FAILED A AWXA O OTHER G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 WP 28 812AW 24476 3098 1178 PHL - CREW REPORTED, DURING CLIMB TO F250 PACK 2 TRIPPED. TEMP 32 DEG C ZONE OUTPUT 92 DEG F, PACK FLOW STAYED IN THE L O POSITION. MX REMOVED AND REPLACED NR 2 PACK FLOW CONTROL VALVE PER AMM 21-51-51- 401, OPS/LEAK CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007060500189 20070605 00189 EA 2007 6 5 QXEA200700851 1 20070512 A 5754 SKIN CNDAIR CL600 CL6002C10 1390015 EA NR 3 SLAT DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 C4 OKC - LEFT WING NR 3 SLAT 10.25" FROM OUTBOARD LEADING EDGE HAS ONE DEEP SCRATCH. REPAIRED IAW SRM 51-12-00, 57-42-0 1. 2 L 7 2 4F RT A21EA 2007060500190 20070605 00190 EA 2007 6 5 QXEA200700852 1 20070510 A 5730 SKIN CNDAIR CL600 CL6002C10 1390015 EA WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 C4 OKC - PANEL 671AB GOUGED ON OUTER SURFACE. REPAIRED IAW SRM 57-31-01, 57-32-32. 2 L 7 2 4F RT A21EA 2007060500191 20070605 00191 EA 2007 6 5 QXEA200700853 1 20070512 A 5753 SKIN CNDAIR CL600 CL6002C10 1390015 EA TE FLAP GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 C4 OKC - LEFT WING, INBOARD FLAP, MIDDLE INBOARD VANE SPRING ACTUATOR AREA HAS A GOUGE IN THE SKIN. REPAIRED IAW SRM 51 -12-00, 57-52-01. 2 L 7 2 4F RT A21EA 2007060500192 20070605 00192 EA 2007 6 5 QXEA200700850 1 20070510 A 5753 SKIN CNDAIR CL600 CL6002C10 1390015 EA RT TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 C4 OKC - RIGHT FLAP PANEL 684AB CHAFED. REPAIRED IAW SRM 51-12-00, 51-21-11. 2 L 7 2 4F RT A21EA 2007060500193 20070605 00193 EA 2007 6 5 QXEA200700854 1 20070510 A 5720 SUPPORT CNDAIR CL600 CL6002C10 1390015 EA LT WING WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 C4 OKC - LEFT WING, OUTBOARD FLAP, VANE SUPPORTS ARE WORN TO THE POINT OF RAISED METAL. REPAIRED IAW SRM57-53-02, 51-12 -00. 2 L 7 2 4F RT A21EA 2007060500194 20070605 00194 EA 2007 6 5 QXEA200700848 1 20070509 A 5753 SKIN CNDAIR CL600 CL6002C10 1390015 EA TE FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 C4 OKC - PANEL 684ET HAS WEAR MARK ON LEADING EDGE. REPAIRED IAW SRM 55-00-00, 51-12-00. 2 L 7 2 4F RT A21EA 2007060500195 20070605 00195 EA 2007 6 5 QXEA200700849 1 20070510 A 5753 SUPPORT CNDAIR CL600 CL6002C10 1390015 EA TE FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 C4 OKC - RIGHT WING, OUTBOARD FLAPS, VANE SUPPORTS ARE WORN TO THE POINT OF RAISED METAL. REPAIRED IAW SRM57-53-01, 51- 12-00. 2 L 7 2 4F RT A21EA 2007060500196 20070605 00196 EU 2007 6 5 F3LA200700122 1 20070526 A 3350 32146210 EPSU AIRBUS A318 A318111 3940019 EU EMERGENCY LIGHTS INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 802FR 1991 DURING C-3 CHECK, INSPECTION REPORTED ROW A EMERGENCY EXIT SEAT LIGHTING INOP. REPLACED EPSU IN FWD GALLEY. OPS CHECKE D GOOD IAW AMM 33-51-38-PB 401. 2 L 7 2 4F RT 2007060500218 20070605 00218 2007 6 5 SWAA072680 4 20070526 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED A2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007060500230 20070605 00230 NM 2007 6 5 SWAA072735 1 20070528 A 2560 6557463 FITTING BOEING 737 7373L9 1384470 NM R2 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2007060500239 20070605 00239 NM 2007 6 5 SWAA072727 1 20070529 A 3350 D71702030 CHARGER BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 270WN 29089 DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 11 ABC. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007060500261 20070605 00261 NM 2007 6 5 2007UALA01679 1 20070528 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 AFT PIT, LEFT SIDE, STA 1480 BETWEEN STR 24 - 25L, MAIN FRAME HAS 2 EA DENTS. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAG E AND FABRICATED A J-REPAIR ANGLE AND INSTALLED NESTED INSIDE THE FRAME INBOARD FLANGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500283 20070605 00283 NM 2007 6 5 2007UALA01702 1 20070529 A 7997 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 ENGINE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA 25158 WIRING FOR OIL TEMP SWITCH JUST BELOW STARTER ON NR 4 ENGINE IS CHAFED. [06-20-07] REPLACED CHAFED WIRING FROM OIL TEM PERATURE SWITCH JUST BELOW STARTER ON NR 4 ENGINE. SIGNAL FROM OIL TEMP SYSTEM SHOWED NORMAL READING. A/C OK FOR SERVI CE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007060500289 20070605 00289 NM 2007 6 5 2007UALA01708 1 20070528 A 5411 FITTING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 PYLON DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 NR 1 PYLON AT NAC STA 201, INBOARD MID SPAR FITTING, LOWER TANG, FASTENER HOLE ELONGATED. MAJOR REPAIR ACCOMPLISHED: C LEANED UP DAMAGE. FABRICATED & INSTALLED A FREEZE PLUG. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500292 20070605 00292 NM 2007 6 5 2007UALA01711 1 20070529 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 EMERGENCY STRIP LIGHTING IN FRONT OF 1ST CLASS CABIN LOOSE. RE-SECURED STRIP TO FLOOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060600009 20070606 00009 EA 2007 6 6 A6WA200740107 1 20070307 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 413AW 7585 LEFT FS 484 INTERCOSTAL ANGLE AT LBL 27 CRACKED APPROXIMATELY .1 INCH LONG. MAINTENANCE INSTALLED NEWLY FAB`D ANGLE IAW BSC STANDARD REPAIR 601R. 2 L 7 2 4F RT A21EA 2007060600016 20070606 00016 EA 2007 6 6 A6WA200740207 1 20070418 A 2910 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 417AW 7610 RT HYDRAULIC TRANSDUCER LINE SUPPORT BRACKET, P/N 601R75262-153, CRACKED APPROX .1 INCH LONG IN RT MLG WHEEL WELL CEILIN G. (M) INSTALLED NEW BRACKET IAW SRM 51-42-06. (K) 2 L 7 2 4F RT A21EA 2007060600026 20070606 00026 EA 2007 6 6 A6WA200740205 1 20070418 A 2910 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT MLG BAY CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 417AW 7610 LT HYDRAULIC TRANSDUCER BRACKET, P/N 601R75262-159) CRACKED APPROX .1 INCH LONG IN LT MLG WHEEL WELL CEILING. (M) MAIN TENANCE INSTALLED NEW BRACKET IAW SRM 51-42-06. (K) 2 L 7 2 4F RT A21EA 2007060600039 20070606 00039 SO 2007 6 6 LR7A07019 1 20070216 A 5280 HINGE BRACKET LKHEED 382 382G 526414U SO NLG DOOR CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2613 4590 DURING SCHEDULED C-7 CHECK PER JOB CARD HSP32302, FOUND FWD LT NLG DOOR HINGE BRACKET CRACKED AT FS93, LBL20.5, WL153. REPLACED BRACKET IAW SMP583 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007060600041 20070606 00041 SO 2007 6 6 LR7A07021 1 20070216 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2613 4590 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5324, FOUND RT MWW REAR BULKHEAD WEB CRACKED AT FS 617, RBL 73, WL 185. REPL ACED WEB IAW SMP583 51-60. 2 H 7 4 4T A1SO 2007060600042 20070606 00042 SO 2007 6 6 LR7A07022 1 20070216 A 5312 CAP LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2613 4590 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5315, FOUND RT AFT FUSELAGE BULKHEAD INNER CAP CRACKED AT FS 770, RBL67, WL162 . REPAIRED CAP IAW SMP583 53-50-14. 2 H 7 4 4T A1SO 2007060600043 20070606 00043 SO 2007 6 6 LR7A07023 1 20070216 A 5320 TEE FITTING LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2613 4590 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5313, FOUND LT AFT FUSELAGE BULKHEAD TO LONGERON TEE FITTING CRACKED AT FS 858 , LBL62, WL192. REPLACED FITTING IAW SMP 583 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007060600045 20070606 00045 EA 2007 6 6 A6WA200740119 1 20070308 A 5320 601R3111358 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 413AW 7585 RIGHT FS 280 INBOARD AND OUTBOARD FLOOR SUPPORT ANGLES CRACKED APPROX .1 INCH LONG AT RBL 9.0. MAINTENANCE REMOVED CRAC KED ANGLES AND INSTALLED NEW ANGLES P/N 601R31113-58 IAW CRJ SRM 51-42-06, 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007060600046 20070606 00046 SO 2007 6 6 LR7A07025 1 20070216 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2613 4590 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5324, FOUND RT BOTTOM MWW SKIN CRACKED AND WARPED AT FS 477 - 621, RBL33 - 64 , WL132. REPLACED SKIN IAW SMP 583 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007060600052 20070606 00052 EA 2007 6 6 A6WA200740125 1 20070312 A 5320 6013501257 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 413AW 7585 AFT EQUIPMENT COMPARTMENT FS 621 TO 625 OBLIQUE ANGLE ON RIGHT SIDE CRACKED .5 INCH LONG. MAINTENANCE CRACKED ANGLE AND INSTALLED NEW ANGLE P/N 601-35012-52, IAW CRJ SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007060600054 20070606 00054 EA 2007 6 6 A6WA200740208 1 20070419 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 417AW 7610 FOUND SERVICE DOOR SURROUND STRUCTURE LOWER SILL JOINT BRACKET (P/N 601R38335-1, CORRODED AT FS 318.70 WL 73 STRINGER 18 . (M) REMOVED AND REPLACED BRACKET (PN 601R383355-1) IAW SRM 51-40-11 AND BSC EO 601R53-11628. (K) 2 L 7 2 4F RT A21EA 2007060600056 20070606 00056 NM 2007 6 6 SWAA072778 1 20070601 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007060600057 20070606 00057 NM 2007 6 6 SWAA072777 1 20070601 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007060600058 20070606 00058 NM 2007 6 6 SWAA072779 1 20070601 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM L2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007060600059 20070606 00059 NM 2007 6 6 SWAA072781 1 20070601 A 5314 6562125 KEELBEAM BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND RIGHT KEEL BEAM CRACKED AT BS 540. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2007060600060 20070606 00060 NM 2007 6 6 SWAA072788 1 20070601 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED PAE CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060600061 20070606 00061 NM 2007 6 6 SWAA072804 1 20070602 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007060600062 20070606 00062 NM 2007 6 6 SWAA072798 1 20070602 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007060600064 20070606 00064 NM 2007 6 6 SWAA072800 1 20070602 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007060600071 20070606 00071 NM 2007 6 6 SWAA072782 1 20070601 A 3350 MS157721 LIGHT BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007060600072 20070606 00072 NM 2007 6 6 2007UALA01725 1 20070529 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 UPPER FUSELAGE SKIN UNDER DORSAL FIN HAS MANY WORN AREAS STA 908 TO 860. MAJOR REPAIR ACCOMPLISHED: INSTALLED INTERNAL TEAR STRAP DOUBLERS & EXTERNAL SKIN DOUBLER - TRIPLER REPAIR WITH STAINLESS WEAR STRAPS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007060600074 20070606 00074 NM 2007 6 6 2007UALA01727 1 20070529 A 5230 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CARGO DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 FWD CARGO DOOR DENTED ON AFT EDGE OF FWD CARGO DOOR APPROX DAMAGE TO MEASURE QUARTER INCH IN DEPTH AND HALF INCH IN LENG TH. MAJOR REPAIR ACCOMPLISHED: INSTALLED EXTERNAL DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060600077 20070606 00077 NM 2007 6 6 2007UALA01730 1 20070529 A 3510 OXYGEN SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CREW O2 LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 579UA 26697 CREW O2 PRESSURE APPEARS TO HAVE A SLOW LEAK. STARTED OUT WITH 1640 PSI NOW READS 1600 PSI AFT. [06-20-07] REMOVED BO TTLE AND SVC'D TO 1650PSI. NOTED THAT LEAK WAS EVIDENT AT BOTTLE AFTER CYCLING SHUTOFF VALVE SEVERAL TIMES, NO LEAK NOT ED. REPLACED CREW O2 BOTTLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060600078 20070606 00078 NM 2007 6 6 2007UALA01731 1 20070530 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 NR 2R MED CABIN DOOR UPPER HINGE CUTOUT CRACKED. [06-20-07] MAJOR REPAIR ACCOMPLISHED. REPAIRED 2R MAIN ENTRY CABIN DOOR UPPER HINGE CUT OUT PER UA ENGINEERING SPECIFICATIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060600079 20070606 00079 EU 2007 6 6 2007UALA01732 1 20070530 A 3510 MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 408UA 457 CREW REPORT: FIRST OFFICER`S 02 MASK PUSH TO TEST INOP. OBS MASK OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007060600080 20070606 00080 NM 2007 6 6 2007UALA01733 1 20070529 A 3350 32145410 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 811UA 847 EMERGENCY EXIT LIGHTS ARE ON WITH THE SWITCH OFF AND AN OFF LIGHT ON. REPLACED EPSU BATTERY. PASSED EMERGENCY TEST ON GROUND. 2 L 7 2 4F 4 F RT A28NM E40NE 2007060600081 20070606 00081 NM 2007 6 6 SWAA072817 1 20070604 A 3350 101073 LENS BOEING 737 7373A4 1384585 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007060600085 20070606 00085 NM 2007 6 6 SWAA072823 1 20070604 A 5320 6545401 STIFFENER BOEING 737 7377H4 1384404 NM LT MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 746SW 29798 DURING SCHEDULED 8Y CHECK, FOUND LEFT MLG W/W STIFFENER CRACKED AT BS 663, BETWEEN LBL 6.15 TO LBL 32. REMOVED AND REPL ACED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2007060600087 20070606 00087 2007 6 6 2007UALA01734 4 20070529 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 L-1 DOOR HARD TO ARM AND DISARM. [06-20-07] REMOVED AND REPLACED SLIDE DUE TO SKIRTING MATERIAL INTERFERING WITH GIRT BAR, 2 L 7 2 4F 4 F RT A2NM E17NE 2007060600088 20070606 00088 NM 2007 6 6 2007UALA01735 1 20070529 A 5320 SILL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 502UA 24623 DOOR 3R WOULD NOT ARM. [06-20-07] CLEANED DEBRIS FROM DOOR SILL AREA. ATTRIBUTED THIS DISCREPANCY TO IMPROPER SKIRT ING UNDERNEATH DOOR AND INADEQUATE CLEANING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060600089 20070606 00089 2007 6 6 2007UALA01736 4 20070530 A 2565 BOTTLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EVAC SLIDE LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 807UA 798 CREW REPORT: DOOR 1R SLIDE PRESSURE READS LOW 1200. 2 L 7 2 4F 4 F RT A28NM E40NE 2007060600091 20070606 00091 NM 2007 6 6 2007UALA01738 1 20070530 A 3260 WARNING LIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT ILLUMINATED A UALA O OTHER J WARNING INDICATION TO TAKEOFF 1 WP 29 924UA 26645 ON TAKEOFF GEAR HANDLE TO OFF RIGHT GEAR RED LIGHT ILLUMINATED. [06-22-07] FOUND FAULTY RED LIGHT LOGIC CARD M986. REPLACED LOGIC CARD M986. 2 L 7 2 4F 4 F RT A16WE E21EU 2007060600093 20070606 00093 NM 2007 6 6 2007UALA01740 1 20070530 A 5210 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR INOPERATIVE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 DOOR 2R ARMING LIGHT INOPERATIVE. [06-20-07] REPLACED DOOR 2R PROX SENSOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060600094 20070606 00094 NE 2007 6 6 2007UALA01741 2 20070528 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 572UA 26682 726640 NR 1 ENGINE HIGH OIL CONSUMPTION EXCEEDS LIMIT. [06-20-07] STARTER CARBON SEAL WAS FOUND LEAKING. REPLACED SEAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060600095 20070606 00095 NM 2007 6 6 2007UALA01742 1 20070528 A 2612 FIRE WARNING BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 929UA 26652 NO BELL ON ENG OR CARGO FIRE TEST, NO FIRE WARNING LIGHT EITHER. [07-03-07] FOUND LAMP IN FIRE WARNING LIGHT CUTOUT SW ITCH SHORTING THE ALARM BELL. REPLACED THE LAMP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007060600097 20070606 00097 EA 2007 6 6 TRAX200700745 1 20070529 A 5320 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 RIGHT FS 280 CROSSBEAM HAS CORROSION ON UPPER FLANGE. REPAIRED IAW ALL SRM`S AND REO`S. 2 L 7 2 4F RT A21EA 2007060600098 20070606 00098 EA 2007 6 6 TRAX200700746 1 20070529 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 FS 280 FWD CENTER FLOOR SUPPORT ANGLE CORRODED. REPAIRED IAW ALL SRM`S AND REO`S. 2 L 7 2 4F RT A21EA 2007060600099 20070606 00099 EA 2007 6 6 TRAX200700747 1 20070529 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 LEFT LOWER FS 280 WEB HAS CORROSION. REPAIRED IAW EO670-53-11-052, REO 670-53-11-052, AND CRJ SRM 51-25-16. 2 L 7 2 4F RT A21EA 2007060600100 20070606 00100 EA 2007 6 6 TRAX200700748 1 20070529 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 RIGHT LOWER FS 280 WEB HAS CORROSION. REPAIRED IAW EO670-53-11-052, REO 670-53-11-052, AND CRJ SRM 51-25-16. 2 L 7 2 4F RT A21EA 2007060600101 20070606 00101 EA 2007 6 6 TRAX200700749 1 20070529 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 850AS 7355 CORROSION ON PAX DOORS LOWER SILL BETWEEN FS 310 TO FS 349. 2 L 7 2 4F RT A21EA 2007060600103 20070606 00103 EA 2007 6 6 TRAX200700734 1 20070528 A 5220 DOOR CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 FOUND LEFT OVERWING EMERGENCY EXIT DIFFICULT TO OPEN WHILE PERFORMING FUNCTIONAL TEST OF LEFT OVERWING EMERGENCY EXIT. [SUP 06-07-07] PERFORMED LUBE TASK IAW CRJ 700 AMM 12-20-52-640-802-A01 PERFORMED. OPS CHECK IAW CRJ 700 AMM 52-21-00. NO DEFECTS FOUND AT THIS TIME. 2 L 7 2 4F RT A21EA 2007060600105 20070606 00105 EA 2007 6 6 TRAX200700736 1 20070528 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 730EV 10141 CAPTAIN`S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007060600107 20070606 00107 EA 2007 6 6 TRAX200700738 1 20070529 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 880AS 7606 LEFT WING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007060600108 20070606 00108 EA 2007 6 6 TRAX200700739 1 20070529 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 976EV 7601 LEFT OBLIQUE ANGLE CRACKED. 2 L 7 2 4F RT A21EA 2007060600114 20070606 00114 NM 2007 6 6 SWAA072828 1 20070604 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 758, STR 22L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007060600115 20070606 00115 NM 2007 6 6 SWAA072826 1 20070604 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 812, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007060600116 20070606 00116 NM 2007 6 6 SWAA072813 1 20070603 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007060600118 20070606 00118 NM 2007 6 6 SWAA072815 1 20070604 A 5311 6546527 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060600119 20070606 00119 NM 2007 6 6 SWAA072816 1 20070604 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060600123 20070606 00123 NM 2007 6 6 SWAA072818 1 20070604 A 5314 65621258 KEELBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED C4 CHECK, FOUND KEEL BEAM CORRODED AT BS 533, RBL 6.50. REPAIRED KEEL BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007060600125 20070606 00125 NM 2007 6 6 SWAA072822 1 20070603 A 2913 887477 PUMP BOEING 737 7377H4 1384404 NM HYDRAULIC SYS LEAKING A SWAA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 29 785SW 30602 DECLARED EMERGENCY, AT FL 410 ENGINE DRIVEN HYDRAULIC -B- SYSTEM LIGHT ILLUMINATED, -B- SYSTEM INDICATES ZERO. INSPECTE D HYDRAULIC SYSTEM FOUND -B- SYSTEM ELECTRIC PUMP LEAKING. REMOVED AND REPLACED ELECTRIC PUMP AND CASE DRAIN FILTERS PE R MM. 2 L 7 2 4F RT A16WE 2007060600127 20070606 00127 2007 6 6 SWAA072806 4 20070604 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 607SW 27927 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DOOR WAS NOT DISARMED, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007060600130 20070606 00130 NM 2007 6 6 SWAA072731 1 20070529 A 3350 PH22300L STRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED C3 CHECK, FOUND EEPLS STRIP WORN AT ROW 1 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007060600131 20070606 00131 NM 2007 6 6 SWAA072744 1 20070530 A 5524 REP4HE8 BEARING BOEING 737 7375H4 138449D NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED C4 CHECK, RIGHT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BEARING PER MM. 2 L 7 2 4F RT A16WE 2007060600132 20070606 00132 NM 2007 6 6 SWAA072774 1 20070601 A 3350 101331 LENS BOEING 737 7373G7 1384595 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 RIGHT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007060600135 20070606 00135 NM 2007 6 6 SWAA072786 1 20070601 A 5753 6546430100 FITTING BOEING 737 7373Q8 1384670 NM RT FOREFLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED OTS CHECK, FOUND RIGHT WING INBOARD FORE FLAP CRACKED AT CENTER GUIDE TRACK FITTING. REMOVED AND REPLA CED FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2007060500015 20070605 00015 WP 2007 6 5 NWAA071899936 1 20070518 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE FAILED A NWAA B A EMER. DESCENT UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 01 1799U 47370 THE AIRCRAFT WAS CLIMBING THROUGH FL200 WHEN IT EXPERIENCED A RAPID DECOMPRESSION OF THE CABIN AFTER A LOUD BANG. CREW I NITIATED AN EMERGENCY DESCENT TO 10,000 FT AND COMPLIED WITH COM PROCEDURES. THE CABIN THEN FILLED WITH A BURNING ODOR S O THE CREW DIVERTED TO AN EMERGENCY LANDING AT BUF AND LANDED WITHOUT FURTHER INCIDENT. CFR CONFIRMED NO FIRE OR SMOKE A ND THE AIRCRAFT TAXIED TO THE GATE. MAINTENANCE DISCOVERED A HOLE IN THE FUSELAGE FORWARD OF THE FWD CARGO DOOR. AIRCRAF T WAS FERRIED UN-PRESSURIZED TO MSP WHERE MAINTENANCE REPAIRED THE DAMAGED SKIN AND VERIFIED THAT THERE WAS NO DAMAGE TO ANY LONGERON. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007060500018 20070605 00018 WP 2007 6 5 ASAA0781746 1 20070529 A 5311 9912243241 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 AFT CARGO FRAME AT STA 1307.091 CORRODED. LOCATED AND DRILLED A REPLACEMENT FRAME SECTION AND REPAIR PARTS AND INSTALLE D IAW SRM 53-03 FIG 2A AND SRM 51-30-2. 2 L 7 2 4F RT A6WE 2007060500020 20070605 00020 NM 2007 6 5 SWAA072759 1 20070531 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND MID CABIN OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007060500021 20070605 00021 NM 2007 6 5 SWAA072772 1 20070531 A 5730 6545407 SKIN BOEING 737 7373L9 1384470 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND LEFT WING UPPER SKIN CORRODED AT STA 252, FWD SPAR. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007060500054 20070605 00054 NM 2007 6 5 SWAA072675 1 20070526 A 3350 417A5600 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 747SA 29799 L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007060500067 20070605 00067 NM 2007 6 5 SWAA072696 1 20070528 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 11L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007060500083 20070605 00083 NM 2007 6 5 SWAA072682 1 20070526 A 5230 6547952 SKIN BOEING 737 7375H4 138449D NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR HANDLE CUTOUT SKIN CRACKED AT FWD END. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500085 20070605 00085 NM 2007 6 5 SWAA072711 1 20070529 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM L1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007060500099 20070605 00099 EU 2007 6 5 07FDEA01858 1 20070520 A 5330 SKIN AIRBUS 310 A310 EU FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 LOWER EXTERNAL FUSELAGE SKIN HAS DENT BETWEEN FR 67 TO FR68 STRG 53R TO STRG 54R APPROX 4" REPAIRED IAW SRM 53-10-12 F IG. 225 2 L 7 2 4F RT A35EU 2007060500118 20070605 00118 NM 2007 6 5 07FDEA02005 1 20070525 A 2420 750866D CONTROL UNIT DOUG MD11 MD11 3023602 NM EMERGENCY POWER FAILED A FDEA C ABORTED TAKEOFF J WARNING INDICATION CR CRUISE 1 SO 25 605FE 151 151 48514 AT APPROX 00:00Z GOT A MASTER WARNING LT W/A LEVEL 1 EMERGENCY POWER ON ALERT. COMPLIED W/QRH. SELECTED EMERGENCY POWE R SWITCH TO OFF. GOT LVL 1 L EMERGENCY AC BUSS ALERT. SELECTED EMERGENCY POWER SWITCH BACK TO ARM , STILL HAD EMERGEN CY POWER ON LEVEL ONE ALERT. CONSULTED W/GOC AND MOCC VIA SAT. BATTERY VOLT NOW DOWN TO 24V -51. WHEN VOLT DROPPED TO 22V (AMBER) DEPLOYED ADG IN ELEC BATTERY CHARGED UP TO 32V, ELECTED TO DIVERT SEA. ON NEXT POWER UP, EMERGENCY POWER TEST FAILED. REF WDM 24-61-11, REMOVED AND REPLACED LEFT EMERGENCY CONTROL RELAY (R2-17) PER SMP. REF AMM 24-24-00-5 AND EPCU R-T-S REF AMM 24-08-01-5, ALL TEST PASSED AND CHECKED NORMAL. DID NOT DUPLICATE FAULT, FINAL FIX REMOVED AND 2 L 7 3 4F RT A22WE 2007060500119 20070605 00119 NM 2007 6 5 HALA0700226 1 20070528 A 2150 BULB BOEING 767 767300 1385204 NM A/C PACK MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, BOTH A/C PACKS UNABLE TO COOL CABIN. CABIN TEMP 81DEG WITH NO PAX ON BOARD. REMOVED AND REPL ACED PACK OUTLET BULB PER AMM 21-52-06. GROUND CHECK OK. OK FOR SVC. 2 L 7 2 4F RT A1NM 2007060500120 20070605 00120 NM 2007 6 5 AWXA200700681 1 20070530 A 2560 P2070001214 FLASHLIGHT BOEING 737 7373G7 1384595 NM MAIN CABIN INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 YYC - CREW REPORTED FORWARD EMERGENCY FLASHLIGHT NOT CHARGING (RED LED NOT BLINKING) MX PLACED ON MEL. MX REMOVED AND R EPLACED FLASHLIGHT AND CLEARED MEL. 2 L 7 2 4F RT A16WE 2007060500121 20070605 00121 WP 2007 6 5 07FDEA02025 1 20070530 A 7830 BLOCKER DOOR DOUG MD10 MD1010F 3022112 WP THRUST REVERSER DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 566FE 46989 NR 2 REVERSER WOULD NOT STOW AFTER LANDING. FOUND NR 2 LT REV TRANSLATING COWL MISSING. AFW MX REPORTS AIRCRAFT BLOCKE D IN WITH LT THRUST REVERSER TRANSLATING COWL MISSING. IT APPEARS THERE ARE ALSO BLOCKER DOORS THAT WERE TOWN OFF WITH THE COWL. THIS MOST LIKELY HAPPENED ON LANDING AND TR DEPLOYMENT. THE AIRPORT AUTHORITY FOUND TRANS COWL AND ATTACHING PARTS ON RUNWAY. ALL DEBRIS REMOVED. INITIAL EVALUATION LOOKS LIKE THE AIRCRAFT WILL REQUIRE A TR HALF. REPLACED NR 2 LT THRUST REVERSER. NR 2 THRUST REV, OPS CKS NORMAL. 2 L 7 3 4F RT A22WE 2007060500122 20070605 00122 NM 2007 6 5 07FDEA02026 1 20070531 A 5310 STRUCTURE BOEING 727 7272S2F 1384O81 NM BS 520 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 ON AGING A/C INSPECTION, FOUND EXISTING REPAIR LOCATED AT STA 520, STR 16R-17-R, DID NOT CONFORM TO SRM. REMOVED AND DI SCARDED PREVIOUS ANGLES & INSTALLED NEW REPAIR PARTS, EA I070369 ALL WORK ACCOMPLISHED ON WO 36352/N00878. 2 L 7 3 4F A3WE 2007060500123 20070605 00123 NM 2007 6 5 07FDEA02027 1 20070531 A 5755 SKIN BOEING 727 7272S2F 1384O81 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 RIGHT WING UPPER TE SKIN CRACKED AT NR 12 SPOILER IB CENTER HINGE CUTOUT REMOVED NR 12 SPOILER. REMOVED FASTENERS IN RE PAIR AREA. STOP DRILLED CRACK, NDT VERIFY CRACK TERMINATION. FABRICATED REPAIR PLATE, TREATED AND PRIMED. INSTALLED R EPAIR, APPLIED FILLET SEAL AND PAINTED REPAIR. INSTALLED NR 12 SPOILER, REF SRM 57-30-4. 2 L 7 3 4F A3WE 2007060500124 20070605 00124 EU 2007 6 5 07FDEA02028 1 20070531 A 5730 A57340085 SKIN PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 CORROSION LT WING TOP SKIN PANEL NR 3, RIB 26-27, STRINGER 17A TO REAR SPAR REPAIR PERFORMED BY BLEND OUT AND REMOVAL OF AFFECTED FASTENER IAW EA 6-5730-106449 AND RAS/BAE/1004794/2007 ISS.A 2 L 7 2 4F RT A35EU 2007060500125 20070605 00125 EU 2007 6 5 07FDEA02029 1 20070531 A 5730 A573140086 SKIN AIRBUS 300 A300B4605R 3930308 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 CRACKS AND CORROSION ON RT WING BOTTOM SKIN LOWER SURFACE ON (HOLE 712 CORRODED, HOLE 311 CRACKED A=12MM, B11MM, DRW R57 1-40141 SHEET 14). REPAIR PERFORMED BY REAM UP IAW EA 6-5720-106453 AND RAS/BAE/1004815/2007 ISS.A 2 L 7 2 4F RT A35EU 2007060500127 20070605 00127 EU 2007 6 5 07FDEA02031 1 20070531 A 5347 A5378193720000 TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 662FE 761 MAIN DECK ADAPTER TRACK CORRODED AT APPROX FR 35, STA 2241, -Y890 REMOVED AND REPLACED ADAPTOR IAW A300-600 SRM 51-40-2 1 PARAG 7. 2 L 7 2 4F RT A35EU 2007060500128 20070605 00128 NM 2007 6 5 07FDEA01978 1 20070525 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 720D-720E CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 465FE 21289 FWD CARGO COMPT FS 720D-720E STR-26L HAS CORROSION. CUT OUT DAMAGE IAW SRM 53-30-3 FIG 5. FABBED REPAIR DOUBLERS AND F ILLER IAW SRM 53-30-3 FIG 5. INSTALLED DOUBLER AND FILLER IAW B727 SRM 53-30-3 FIG 5. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007060500129 20070605 00129 NM 2007 6 5 07FDEA01979 1 20070525 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 640 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 465FE 21289 CABIN FLOOR SEAT TRACK HAS CORROSION FS 640 LBL 1". REMOVED CORROSION IAW 727 SRM 51--10-2 FOUND TO BE OUT OF LIMITS AF TER CORROSION REMOVAL IAW SR 53-10-1. FABBED NEW SEAT TRACK IAW SRM 51-30-2 ,TREATED AND PRIMED IAW SRM 51-10-1. REMOV ED AND INSTALLED SEAT TRACK AT BL 0" STA 600 TO 720A IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2007060500130 20070605 00130 EU 2007 6 5 AALA20070960 1 20070528 A 3231 NUT AIRBUS 300 A300B4605R 3930308 EU DOOR ROD END LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 11060 470 MIA INFLIGHT T639/28MAY - RETURNED TO MIA DUE TO BOTH NOSE LANDING GEAR DOOR INDICATORS ILLUMINATED. LANDED WITHOUT INC IDENT. FOUND LEFT LANDING GEAR DOOR ACTUATOR ROD END JAM NUT LOOSE. RESECURED LANDING GEAR DOOR ACTUATOR ROD END JAM N UT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007060500131 20070605 00131 NM 2007 6 5 AALA20070963 1 20070528 A 3350 LENS BOEING 777 777223 1385213 NM EMEGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 797AN 30012 JFK - EMERGENCY LIGHT AT SEAT 20C BROKEN. REPLACED LENS AND LAMP FOR EMERGENCY LIGHT AT SEAT ROW 20C. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007060500132 20070605 00132 EU 2007 6 5 AALA20070968 1 20070528 A 3350 SOCKET AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 8067A 510 MIA - EMERGENCY LIGHT AT SEAT 26C HAS MISSING LENS. REPLACED SOCKET AND LENS FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007060500133 20070605 00133 NM 2007 6 5 AALA20070956 1 20070527 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 347AN 33086 SFO - EXTERIOR EMERGENCY LIGHT ON RIGHT SIDE AFT DOOR INOPERATIVE. RELAMPED L642 EXTERIOR EMERGENCY LIGHT ON RIGHT SIDE AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007060500223 20070605 00223 NM 2007 6 5 SWAA072673 1 20070525 A 3350 D71702030 CHARGER BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 746SW 29798 DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007060500225 20070605 00225 NM 2007 6 5 SWAA072749 1 20070530 A 5311 6546550 BELTFRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500235 20070605 00235 NM 2007 6 5 SWAA072750 1 20070530 A 5311 65C343561 BELTFRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 482A, STR 20R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500236 20070605 00236 NM 2007 6 5 SWAA072732 1 20070529 A 5330 65C35777 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 922, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500243 20070605 00243 EU 2007 6 5 2007UALA01660 1 20070528 A 3397 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 489UA 1702 EMERGENCY ESCAPE PATH LIGHTING INOP AT SEAT 1-ABC. RECONNECTED UNPLUGGED EMERGENCY LIGHT CONNECTOR. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007060500244 20070605 00244 NM 2007 6 5 2007UALA01661 1 20070527 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 23671 FOUND FUSELAGE SKIN HAS 2.5 INCH CRACK AT STA 942 ABOVE STR 24L. [06-22-07] MAJOR REPAIR: REMOVED DAMAGE. ACCOMPLISH ED HFEC INSPECTION. NO DEFECTS. ACOMPLISHED BHEC INSPECTION. NO DEFECTS. FABRICATED AND INSTALLED REPAIR PER EVA 70311 A ND 70311A. 2 L 7 2 4F 4 F RT A16WE E21EU 2007060500249 20070605 00249 NM 2007 6 5 2007UALA01666 1 20070527 A 5512 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZ STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 RIGHT HORIZONTAL STAB REAR SPAR LOWER SKIN APPROX 61 INCHES OUTBOARD OF EMPENNAGE CRACKED. MAJOR REPAIR ACCOMPLISHED: INSTALLED EXTERNAL SKIN DOUBLER & 2EA LWR SKIN REINFORCED ACCESS PLATE REPAIRS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007060500252 20070605 00252 NM 2007 6 5 2007UALA01669 1 20070528 A 5315 FLOORBEAM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 174UA 24381 FWD CARGO COMPT FLOORBEAM UPPER CHORD CRACKED AT BS 780 RBL 70. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE. INSTALLED FILLER & ANGLE REPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007060500255 20070605 00255 NM 2007 6 5 2007UALA01673 1 20070527 A 5210 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 R-2 DOOR, FORWARD FRAME AT UPPER HINGE CUTOUT IS CRACKED. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED A CRES DOU BLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500259 20070605 00259 NM 2007 6 5 2007UALA01677 1 20070528 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 AFT PIT, RIGHT SIDE, STA 1580 AT STR 25R AREA, MAIN FRAME DENTED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE AND FABRIC ATED A J-ANGLE REPAIR PIECE AND INSTALLED NESTED INSIDE FRAME INBOARD FLANGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500271 20070605 00271 NM 2007 6 5 2007UALA01690 1 20070525 A 2530 OVEN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GALLEY SPARKS A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 509UA 24763 FIRST CLASS OVEN NR 107 ELECTRICAL SPARKS FROM BEHIND. TURNED OFF, NO MORE SPARKS. [06-20-07] NO DAMAGE TO AC WIRING NOTED, FOUND GUIDE PIN PUSHED INTO OVEN. REPLACED CONVECTION OVEN, 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500287 20070605 00287 NM 2007 6 5 2007UALA01706 1 20070528 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 AFT PIT, LEFT STA 1580, STR 25L AREA, MAIN FRAME DENTED. MAJOR REPAIR ACCOMPLISHED: REMOVED DENT DAMAGE ON FRAME INBOA RD FLANGE BETWEEN STR 23L - 24L & BETWEEN 26L-27L. REMOVED EXISTING PRODUCTION SPLICE. FABRICATED & INSTALLED A NEW PR ODUCTION SPLICE ANGLE. FABRICATED & INSTALLED 3EA -20 STRINGER CLIPS & 1EA -1 STRINGER CLIP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500288 20070605 00288 NM 2007 6 5 2007UALA01707 1 20070528 A 5720 FITTING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT WING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 INBOARD SIDE LOAD FITTING, INBOARD FWD HOLE DAMAGED RIGHT WING. MAJOR REPAIR ACCOMPLISHED: REAMED HOLE OVERSIZED. COL D WORKED HOLE & FINAL REAMED FOR OVERSIZED FASTENER INSTALLATION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500290 20070605 00290 NM 2007 6 5 2007UALA01709 1 20070526 A 5414 313T3381 PANEL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT PYLON DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 LEFT INBOARD PYLON PANEL IS DELAMINATED & MISSING RIVETS. [07-10-07] REMOVED LEFT INBD PYLON PANEL & CREATED DOUBLER R EPAIR PER SRM. INSTALLED DOUBLER, REINSTALLED PANEL. INSTALLED LEADING EDGE FASTENERS TO COMPLETE INSTALLATION OF PANE L. SUSPECT VIBRATION LED TO RIVETS PULLING THROUGH PANEL & UNBOUND PANEL BEGAN TO DELAMINATE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007060500297 20070605 00297 NM 2007 6 5 2007UALA01717 1 20070526 A 3620 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE BLEED AIR SYS ILLUMINATED A UALA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 WP 29 672UA 30027 727792 ENGINE BLEED LIGHT CAME ON AT TOP OF DESCENT, WITH EICAS BLEED MSG. [07-10-07] CREW SHUT OFF ENG BLEED AIR & ACCOMPLIS HED AIR SUPPLY MODULE BITE TEST. RESET & CHECKED OK. FOLLOWUP TROUBLE SHOOTING FOUND NR 1 ENG ELBOW FTTG LOOSE AT HPS OV. RESECURED ELBOW & VALVE/ SYSTEM CHKS OK. SUSPECT VIBRATION & THERMAL CHANGE CAUSED ELBOW CLAMP TO LOOSEN. 2 L 7 2 4F 4 F RT A1NM E24NE 2007060500298 20070605 00298 NM 2007 6 5 2007UALA01718 1 20070529 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FUSELAGE SCRATCHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 671UA 30026 RIGHT LOWER FUSELAGE SKIN BETWEEN STA 1480 & 1510 HAS SCRATCH, 1 AREA AT STA 1480 IS APPROX 6 INCHES LONG AND DENTED ALO NG THE LAP SEAM. [07-10-07] SKIN WAS REPAIRED PER SRM-53-00-01, REPAIR NR 12. HFEC WAS DONE WITH GOOD RESULTS. A/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007060500301 20070605 00301 2007 6 5 2007UALA01722 4 20070529 A 2565 10540001002 VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EVAC SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 775UA 0649 26947 LOW BOTTLE PRESSURE. THERE WAS A SMALL LEAK IN THE FILLER VALVE. REPLACED WITH NEW FILLER VALVE. REPLACED BOTTLE WITH A STOCK BOTTLE AND REPAIRED THE OLD BOTTLE AND PUT BACK IN STOCK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007060500304 20070605 00304 NM 2007 6 5 ASAA0791751 1 20070531 A 5320 143A7501168 SILL BOEING 737 737990 NM FWD CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 FWD CARGO PIT LT DUST SILL CORRODED REPAIRED IAW 53 00 53 2 L 7 4 4F RT A16WE 2007060600005 20070606 00005 EA 2007 6 6 A6WA200740129 1 20070313 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 413AW 7585 CARGO DOOR SUPPORT BEAM ANGLE THAT ATTACHES TO REAR PRESSURE BULKHEAD IS CRACKED APPROX .5 INCH IN LENGTH. MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE P/N 601R35056-109 IAW CRJ SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007060600007 20070606 00007 EA 2007 6 6 A6WA200740120 1 20070308 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 413AW 7585 LEFT FS 280 INBOARD AND OUTBOARD FLOOR ANGLES CRACKED APPROX .1 INCH LONG AT LBL 9.0. MAINTENANCE REMOVED CRACKED ANGLE S AND INSTALLED NEW ANGLES P/N 601R31113-57 IAW CRJ SRM 51-42-06 AND 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007060600011 20070606 00011 EA 2007 6 6 A6WA200740108 1 20070307 A 5320 6003106819 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 413AW 7585 RIGHT FS 460 FLOOR SUPPORT FITTING P/N 600-31068-19 CRACKED APPROXIMATELY .3 INCH LONG AT OUTBOARD SIDE RBL 9. MAINTENA NCE REMOVED CRACKED FITTING RIGHT FS 460 OUTBOARD SIDE RBL 9. DRILLED UP AND ALODINED NEW FITTING PART NR 600-31068-19. FITTING AND FASTENERS SHOT WET USING PS 870 C-12 SEALANT. (M) 2 L 7 2 4F RT A21EA 2007060600017 20070606 00017 EA 2007 6 6 A6WA200740189 1 20070413 A 2910 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 454AW 7842 LEFT MLG BAY HYDRAULIC TRANSDUCER BRACKET IS CRACKED. (M) [07-17-07] MAINTENANCE REMOVED AND REPLACED BRACKET, P/N 60 1R75262-159, IAW CRJ SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007060600018 20070606 00018 EA 2007 6 6 A6WA200740191 1 20070413 A 2910 BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 454AW 7842 RIGHT MLG BAY HYDRAULIC TRANSDUCER BRACKET CRACKED. (M) MAINTENANCE REMOVED AND REPLACED BRACKET PN 601R75262-157 IAW SRM 51-42-06. (K) 2 L 7 2 4F RT A21EA 2007060600022 20070606 00022 EA 2007 6 6 A6WA200740204 1 20070418 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 417AW 7610 OUTBOARD FLOOR SUPPORT BEAM CLIP AT FS 280, LBL 9.0 IS CRACKED IN RADIUS APPROX .4 INCH LONG. (M) REPAIRED FS 280 CLIP IAW BSC SR 601R530057A. (K) 2 L 7 2 4F RT A21EA 2007060600025 20070606 00025 EA 2007 6 6 A6WA200740202 1 20070418 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 417AW 7610 OUTBOARD FLOOR SUPPORT BEAM CLIP AT FS 280, RBL 9.0 IS CRACKED IN RADIUS APPROX .1 INCH LONG. (M) REPAIRED FS280 CLIP IAW BSC SR 601R530557A. 2 L 7 2 4F RT A21EA 2007060600044 20070606 00044 SO 2007 6 6 LR7A07024 1 20070216 A 5220 SKIN LKHEED 382 382G 526414U SO ESCAPE DOOR CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2613 4590 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5321, FOUND LT AFT AFT ESCAPE HATCH DOOR EXTERIOR SKIN CRACKED AT FS 935, LBL1 2, WL238. REPLACED SKIN IAW SMP583 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007060600048 20070606 00048 SO 2007 6 6 LR7A07026 1 20070216 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2613 4590 DURING SCHEDULED C-7 CHECK PER JOB CARD HSP53300, FOUND NLG PRESSURE SKIN CRACKED AT FS 204, RBL2, WL134. REPAIRED SKI N IAW SMP 583 53-30-17. 2 H 7 4 4T A1SO 2007060600049 20070606 00049 SO 2007 6 6 LR7A07027 1 20070216 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE CHAFED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2613 4590 DURING SCHEDULED C-7 CHECK PER JOB CARD HC2111, FOUND FUSELAGE EXTERIOR SKIN CHAFED AT FS477, RBL80, WL180. REPAIRED S KIN IAW SMP583 51-140-12. 2 H 7 4 4T A1SO 2007060600053 20070606 00053 EA 2007 6 6 A6WA200740126 1 20070309 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 413AW 7585 RIGHT WING OUTBOARD FUEL PANEL 650B FOUND CORROSION AROUND WING PLANK APPROX .005 INCH DEEP IN NON-CRITICAL AREA. MAINT ENANCE REPAIRED CORROSION BY BLENDING IAW BOMBARDIER REO 601R-57-030 REV F. (M) 2 L 7 2 4F RT A21EA 2007060600066 20070606 00066 NM 2007 6 6 SWAA072802 1 20070602 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007060600067 20070606 00067 NM 2007 6 6 SWAA072803 1 20070602 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007060600076 20070606 00076 EU 2007 6 6 2007UALA01729 1 20070529 A 3040 CONTROLLER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE WINDSHIELD MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 469UA 1409 CAPTAIN'S SLIDING WINDOW HOT TO TOUCH AND HAS MANY DELAMINATED BUBBLES. [06-26-07] REPLACED CAPTAIN SLIDING WINDOW. A LSO NR 1 WINDOW HEAT CONTROLLER REPLACED FOR OVERHEATED LT SLIDING WINDOW. ACCOMPLISHED TESTS AFTER WINDOW REPLACEMENT AND NO CLASS 3 MSG WAS PRESENT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007060600096 20070606 00096 EA 2007 6 6 TRAX200700728 1 20070526 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 AFT PRESSURE BULKHEAD WAS FOUND TO BE CRACKED AT LBL 9 AND APPROX WL 100.00 HAS BEEN CONFIRMED CRACK BY ET AND FPI TYPE 1, METHOD C. FOUND DURING COMPLYING WITH AWL 53-61-153. 2 L 7 2 4F RT A21EA 2007060600109 20070606 00109 EA 2007 6 6 TRAX200700740 1 20070529 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 976EV 7601 RIGHT OBLIQUE ANGLE CRACKED. 2 L 7 2 4F RT A21EA 2007060600136 20070606 00136 NM 2007 6 6 SWAA072787 1 20070601 A 5322 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 16R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007060600137 20070606 00137 NM 2007 6 6 SWAA072792 1 20070602 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060600142 20070606 00142 NM 2007 6 6 SWAA072789 1 20070601 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED PAE CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060600143 20070606 00143 NM 2007 6 6 SWAA072794 1 20070602 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060600145 20070606 00145 NM 2007 6 6 SWAA072793 1 20070602 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060600147 20070606 00147 EA 2007 6 6 TRAX200700751 1 20070529 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 835AS 7258 RIGHT EMERGENCY OVERWING MIDDLE EXT LIGHT INOP. 2 L 7 2 4F RT A21EA 2007060600148 20070606 00148 EA 2007 6 6 TRAX200700752 1 20070530 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 850AS 7355 FRAME CORRODED AT FS 364.00 BETWEEN STR 26L TO 26R. 2 L 7 2 4F RT A21EA 2007060600149 20070606 00149 EA 2007 6 6 TRAX200700753 1 20070530 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 850AS 7355 SERVICE DOOR LOWER SILL ANGLE CORRODED AT FS 349.00. SERVICE DOOR LOWER SILL ANGLE REMOVED AND REPLACED AS PER SRM 51-4 2-21, SEALANT APPLIED AS PER SRM 51-23-00, PAINTED AS PER SRM 51-21-11. SUPPLEMENTAL - SDR CLOSED 06/05/07. 2 L 7 2 4F RT A21EA 2007060600151 20070606 00151 EA 2007 6 6 TRAX200700755 1 20070530 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 850AS 7355 CORROSION ON FRAME AT FS 319 BETWEEN STR 25L TO 25R. 2 L 7 2 4F RT A21EA 2007060600154 20070606 00154 EA 2007 6 6 TRAX200700758 1 20070530 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 850AS 7355 FRAME CORRODED AT FS 605 BETWEEN STR 26L AND 27. 2 L 7 2 4F RT A21EA 2007060600155 20070606 00155 SO 2007 6 6 200715201 1 20070529 A 3350 110049 POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 909AE 8038 198 14500899 SEAT 16 A AISLE EMERGENCY LIGHT AND SEAT 19 LEFT OVERWING EMERGENCY LIGHT OUT. REPLACED NUMBER 1 EMERGENCY LIGHT POWER SUPPLY IAW EMB AMM. OPERATIONAL CHECKS GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007060600156 20070606 00156 SO 2007 6 6 200715202 1 20070531 A 5610 NP15131112 WINDSHIELD EMB 135 EMB135LR 3260305 SO COCKPIT CRACKED A SIMA K NONE O OTHER CR CRUISE 1 SW 21 718AE 10365 10365 145275 FIRST OFFICERS FRONT WINDSHIELD OUTER GLASS CRACKED. REPLACED FIRST OFFICERS FRONT WINDSHIELD IAW EMB AMM. OPERATIONAL CHECKS GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007060600157 20070606 00157 EA 2007 6 6 200715003 1 20070527 A 5610 NP13932111 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SIMA A B UNSCHED LANDING EMER. DESCENT O OTHER CR CRUISE 1 SW 21 516AE 9410 10123 PILOT FRONT WINDSHIELD CRACKED. REMOVED AND REPLACED PILOT FRONT WINDSHIELD IAW CRJ MM. OPERATIONAL CHECKS GOOD. RETU RNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007060600160 20070606 00160 EA 2007 6 6 200715002 1 20070527 A 5610 NP1393226 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SIMA O OTHER O OTHER LD LANDING 1 SW 21 517AE 9100 10124 CO PILOT SIDE WINDOW CRACKED. REMOVED AND REPLACED CO PILOT SIDE WINDOW IAW CRJ AMM. OPERATIONAL CHECKS GOOD. RETURNE D AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007060600162 20070606 00162 EA 2007 6 6 SWIA200718283 1 20070417 A 5311 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 927SW 7693 FOUND CRACK IN DOUBLER FRAME ON RIGHT SIDE OF FS 640, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS 601R 36001-4 AND 60 1R 36002-4 PER SB 601R53-061. 2 L 7 2 4F RT A21EA 2007060600167 20070606 00167 EA 2007 6 6 SWIA200718288 1 20070417 A 5210 BRACKET CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 927SW 7693 PAX DOOR HAS CRACKED BRACKET INSIDE ACCESS HOLE (832BR) ON AFT SIDE OF DOOR, DISCOVERED AT C-CHECK. INSTALLED NEW INTER COSTAL P/N 601R-31902-3185 IAW CRJ200 SRM 51-42-06 PG 11. 2 L 7 2 4F RT A21EA 2007060600169 20070606 00169 EA 2007 6 6 SWIA200718290 1 20070416 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 709SK 10159 PAX DOOR OUTER HANDLE IS CRACKED, DISCOVERED AT C-CHECK. REPLACED PAX DOOR OUTER HANDLE PER CRJ700/900 MM TASK 52-11-03 -400-801-A01. 2 L 7 2 4F RT A21EA 2007060600170 20070606 00170 EA 2007 6 6 SWIA200718291 1 20070416 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 709SK 10159 PAX DOOR AFT WEB CRACKED AT MID-STEP, DISCOVERED AT C-CHECK. INSTALLED FABRICATED REPLACEMENT PARTS PER REO 670-52-11-2 58. 2 L 7 2 4F RT A21EA 2007060600172 20070606 00172 EA 2007 6 6 SWIA200718293 1 20070416 A 5210 ROLLER CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 709SK 10159 PASSENGER DOOR LATCH MECHANISM ROLLER IS CORRODED, DISCOVERED AT C-CHECK. REMOVED AND REPLACED ROLLER PER BOMBARDIER CM M 52-12-01. 2 L 7 2 4F RT A21EA 2007060600174 20070606 00174 EA 2007 6 6 SWIA200718295 1 20070601 A 2560 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN UNSECURE A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 941SW 7750 AFT FACING EXIT SIGN ABOVE ROW 8 FELL OFF DURING FLIGHT. RESECURED AFT FACING EXIT SIGN ABOVE ROW 8 IAW AMM 33-10-00. 2 L 7 2 4F RT A21EA 2007060600176 20070606 00176 NM 2007 6 6 DU4R20070123 1 20070529 A 5330 SKIN BOEING 757 757232 1384965 NM FUSELAGE DAMAGED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 602DL 22809 FOUND LIGHTNING STRIKE BS 310 BETWEEN S-8L AND S-9L. REPAIRED BY REMOVING SHEAR TIE, CUT OUT STRIKE AREA, HFEC CUT OUT IAW B757 NTM PT6 51-00-01, 51-00-19 NO RELEVANT INDICATIONS NOTED. TRIMMED OUT AN EXTRA .040” MATERIAL. FABRICATED AND INSTALLED SHEAR TIE 10.0 BY 2.25 FROM 7075-T6 .050 AND SKIN REPAIR 11.5 BY 13.5 FROM 2024-T3 .063 IAW B757 SRM 53-00-01 FIG 201. 2 L 7 2 4F RT A2NM 2007060600178 20070606 00178 SO 2007 6 6 SWIA200718296 1 20070602 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 292UX 2364 2364 120292 FLOOR LEVEL EMERGENCY LIGHTS FORWARD OF ROW 3 INOP. REPLACED FORWARD ELBP WITH SERVICEABLE UNIT. 2 L 7 2 4T RT A31SO 2007060600180 20070606 00180 EA 2007 6 6 SWIA200718298 1 20070530 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 910SW 7566 CABIN CEILING EMERGENCY FLOODLIGHT IS INOP. RELAMPED CABIN CEILING EMERGENCY LIGHTS. 2 L 7 2 4F RT A21EA 2007060600181 20070606 00181 SO 2007 6 6 SWIA200718299 1 20070529 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 295UX 11122 11122 120295 FLOOR LEVEL EMERGENCY LIGHTING IN ROW 9 AND EXIT SIGNS ARE INOP. INSTALLED A SERVICEABLE AFT ELBP. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007060600183 20070606 00183 EA 2007 6 6 SWIA200718301 1 20070531 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 866AS 7517 AFT FLOOR TRACK LIGHTING IS INOP. REPLACED EMERGENCY BATTERY PACK NR 4 IAW AMM 33-51-07. 2 L 7 2 4F RT A21EA 2007060600184 20070606 00184 SO 2007 6 6 SWIA200718302 1 20070531 A 2910 HYDRAULIC LINE EMB 120 EMB120ER 3260203 SO GREEN SYSTEM LEAKING A SWIA O OTHER K FLUID LOSS UK UNKNOWN 1 NM 07 584SW 120352 LOST GREEN SYSTEM HYDRAULIC FLUID. REPLACED BAD SECTION OF HYDRAULIC PRESSURE LINE IN LEFT OUTBOARD NACELLE. SERVICED HYDRAULIC FLUID TO PROPER LEVEL. OPS AND LEAK CHECKS ARE GOOD. 2 L 7 2 4T RT A31SO 2007060600188 20070606 00188 SO 2007 6 6 LR7A07030 1 20070216 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2613 4590 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5313, FOUND RT OUTBOARD BULKHEAD CAP CRACKED AT FS 1012, RBL67, WL270. REPAIR ED BULKHEAD IAW MEA 382-53-07-011. 2 H 7 4 4T A1SO 2007060600190 20070606 00190 EA 2007 6 6 TRAX200700760 1 20070530 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 850AS 7355 RIGHT SILL AS MANY SPOTS OF CORROSION BETWEEN FS 409.00 +128 TO FS 559.00 BL 36 TO BL 47. 2 L 7 2 4F RT A21EA 2007060600191 20070606 00191 EA 2007 6 6 TRAX200700761 1 20070530 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 906EV 7642 LEFT BRACKET CRACKED AT LBL 9 ON AFT SIDE OF BULHEAD 280. 2 L 7 2 4F RT A21EA 2007060600192 20070606 00192 EA 2007 6 6 TRAX200700762 1 20070530 A 5220 HANDLE CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 850AS 7355 CREW ESCAPE HATCH HANDLE CORRODED. 2 L 7 2 4F RT A21EA 2007060600193 20070606 00193 EA 2007 6 6 TRAX200700763 1 20070530 A 2810 FUEL TANK CNDAIR CL600 CL6002B19 1900309 EA LT & RT TANK CONTAMINATED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 850AS 7355 LEFT AND RIGHT FUEL TANK ACCESS PANEL 540AB AND 640AB THERE IS FOD BEHIND THE BAFFLE NEXT TO EJECTOR PUMP. 2 L 7 2 4F RT A21EA 2007060600194 20070606 00194 EA 2007 6 6 TRAX200700764 1 20070530 A 2751 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A ASOA K NONE J WARNING INDICATION CR CRUISE 1 SO 27 841AS 7300 FLAPS FAIL MSG IN FLIGHT FLAPS AT 0 DEG AT FL 300 ORAL WARNING UNIT SOUNDED OVERSPEED IN COCKPIT AND CHIMES IN CABIN. E MERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007060600195 20070606 00195 EA 2007 6 6 TRAX200700765 1 20070531 A 5534 ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 713EV 10081 VERTICAL STABILIZER TO FUSELAGE ANGLE CRACKED ON LEFT T/E. [06-08-07] WORK ACCOMPLISHED ON EC/TC REO 670-55-31-018. 2 L 7 2 4F RT A21EA 2007060600196 20070606 00196 EA 2007 6 6 TRAX200700766 1 20070531 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 713EV 10081 ASD OUTER HANDLE CRACKED. [06-08-07] REMOVED AND REPLACED ASD OUTER HANDLE IAW CRJ 700 MM 52-11-03. 2 L 7 2 4F RT A21EA 2007060600197 20070606 00197 EA 2007 6 6 TRAX200700767 1 20070531 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 RIGHT SIDE FS 640 BONDED SKIN DOUBLER IS CRACKED. [07-24-07] WORK COMPLETED IN ACCORDANCE WITH REO 601R-53-61-506. 2 L 7 2 4F RT A21EA 2007060600199 20070606 00199 EA 2007 6 6 TRAX200700769 1 20070531 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ODOR A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 857AS 7411 FUEL SMELL IN COCKPIT & IN FLIGHT. 2 L 7 2 4F RT A21EA 2007060600201 20070606 00201 EA 2007 6 6 TRAX200700731 1 20070527 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 836AS 7263 PAX DOOR EXTERIOR EMERGENCY LIGHT WILL NOT ILLUMINATE. 2 L 7 2 4F RT A21EA 2007060600203 20070606 00203 EA 2007 6 6 TRAX200700726 1 20070525 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 843AS 7310 SEVERAL EMERGENCY LIGHTS INOP. 2 L 7 2 4F RT A21EA 2007060600204 20070606 00204 NM 2007 6 6 EIA2007111 1 20070424 A 5311 FRAME BOEING 747 747230B 1384889 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 487EV 26286 FRAME WEB CRACKED AT STAND-OFF HOLE STA 300 WL 175 LBL20 IN LT TUNNEL. REPAIRED CRACKED STAND-OFF HOLE AT STA 300 WL 17 5 LBL 20 IN TUNNEL PER B747 SRM 53-10-20 PAGES 90-91 FIGURE 6, 51-20-01 PAGES 11,14-29, 51-30-05 PAGE 5 TABLE 1, 51-10-0 2 PAGES 6-8 ITEM G, SOPM 20-41-02 PAGES 5-9 AND B747 SRM 51-40-02 PAGES 1-3 FIGURE I SHEETS 1-3. 2 L 7 4 4F A20WE 2007060600206 20070606 00206 NM 2007 6 6 EIA2007115 1 20070509 A 5313 STRINGER BOEING 747 747230B 1384889 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 487EV 23286 HEAVY EXFOLIATION CORROSION ON STRINGER 47R AT STATION 790, FORWARD PIT BILGE. REMOVED CORROSION AT STRINGER 47R STATIO N 790, FOUND TO BE OUT OF LIMITS 100 PERCENT MATERIAL LOSS. REMOVED DAMAGE AREA PER B747 SRM 51-30-02 FIGURE 1, NDT CHE CKED NO CRACKS NOTED. REPAIRED PER B747 SRM 53-10-03 FIGURE 1. INSTALLED PER B747 SRM 53-10-03 PAGES 2-3,8-9. 2 L 7 4 4F A20WE 2007060600207 20070606 00207 NM 2007 6 6 EIA2007112 1 20070421 A 5210 STOP FITTING BOEING 747 747230B 1384889 NM PAX DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 487EV 23286 DOOR STOP NR 9 ON LT MAIN ENTRY DOOR CRACK NOTED DURING ACCOMPLISHMENT OF EO, LOCATED AT BS 488 FRAME WEB TOOLING HOLE. REPAIRED MAIN ENTRY DOOR FRAME STA 488 PER SRM B747 53-10-04 FIG 121. 2 L 7 4 4F A20WE 2007060600208 20070606 00208 NM 2007 6 6 EIA2007114 1 20070424 A 5311 FRAME BOEING 747 747230B 1384889 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 487EV 23286 FRAME WEB CRACKED AT STAND OFF HOLE STA 320 W/L 175 LBL 20 IN LT TUNNEL. REPAIRED CRACK AT STAND OFF HOLE AT STA 320 W/ L 175 LBL 20 LT TUNNEL PER B747 53-10-02 PAGE 90 FIGURE 6, 51-20-01 PAGES 11, 14-29, 51-30-05 PAGE 5 TABLE 1, 51-10-02 P AGES 6-8 ITEM G, 51-40-02 FIGURE 1 PAGES 1-3 AND B747 SOPM 20-41-02 PAGES 5-9. 2 L 7 4 4F A20WE 2007060600210 20070606 00210 NM 2007 6 6 EIA2007104 1 20070521 A 5320 TENSION TIE BOEING 747 747230B 1384889 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 487EV 23286 TENSION TIE FRAME BS 940 RT SIDE FUSELAGE CABLE THRU HOLES ENLONGATED AND FASTENER HOLES CRACKED OUT. REMOVED DAMAGE, N DT AREA, FABRICATED AND INSTALLED REPAIR PER ECRA 487-53-048-2. 2 L 7 4 4F A20WE 2007060600211 20070606 00211 NM 2007 6 6 EIA2007106 1 20070520 A 5414 SKIN BOEING 747 747230B 1384889 NM NR 2 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 487EV 23286 UPPER EDGE OF NR 2 PYLON ACCESS PANEL 463AR OPENING IS CRACKED AND WORN. REMOVED DAMAGE, NDT AREA, FABRICATED AND INSTA LLED REPAIR PER ECRA 487-54-043-2. 2 L 7 4 4F A20WE 2007060600213 20070606 00213 NM 2007 6 6 EIA2007121 1 20070604 A 3350 S1356B37 LIGHT BOEING 747 747SR46 1384816 NM CABIN INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477EV 20784 EMERGENCY LIGHT IN THE UPPER DECK STAIR WELL LIGHT ASSY INOP. REMOVE AND REPLACE EMERGENCY LIGHT AT UPPER DECK STAIRWAY PER B747MM 33-51-07. OPS CHECKED GOOD PER B747 MM 33-51-07. 2 L 7 4 4F RT A20WE 2007060600217 20070606 00217 NM 2007 6 6 EIA2007103 1 20070520 A 5414 SKIN BOEING 747 747230B 1384889 NM NR 4 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 487EV 23286 NR 4 PYLON O/B ACCESS PANEL CUTOUT FLANGE CRACKED, PYLON STATION 213.6. REMOVED DAMAGE, NDTD AREA, FABRICATED AND INSTA LLED REPAIR PER ECRA 487-54-046-2. 2 L 7 4 4F A20WE 2007060600218 20070606 00218 NM 2007 6 6 EIA2007105 1 20070521 A 5320 TENSION TIE BOEING 747 747230B 1384889 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 487EV 23286 BS 880 TENSION TIE BEAM RT SIDE COMMON TO FRAME HAS ONE HOLE OUT OF LIMITS PER EO 53-747-1818-06 REV A. REMOVED DAMAGE, NDT AREA, FABRICATED AND INSTALLED REPAIR PER ECRA 487-53-045-2. 2 L 7 4 4F A20WE 2007060600219 20070606 00219 EA 2007 6 6 TRAX200700772 1 20070529 A 5210 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 AFT DRAG ANGLE ON PAX DOOR IS CRACKED. 2 L 7 2 4F RT A21EA 2007060600220 20070606 00220 EA 2007 6 6 TRAX200700774 1 20070601 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 885AS 7521 RIGHT BONDED SKIN DOUBLER CRACKED BETWEEN STRINGER NR 9 AND NR 12 UNDERNEATH 640 DOUBLER. [06-12-07] COMPLED WI TH EC/TC ASA REO 601R-53-61-506 REV C. ON RT SIDE. 2 L 7 2 4F RT A21EA 2007060600221 20070606 00221 EA 2007 6 6 TRAX200700776 1 20070601 A 5313 STRINGER CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 713EV 10081 FS 296 TO FS 310 STRINGER 25R IS CORRODED. [06-08-07] CLEANED FS296 TO FS 310 STRINGER 25R FOUND NO DEFECTS. PER C RJ700 SRM 51-10-00. 2 L 7 2 4F RT A21EA 2007060600223 20070606 00223 EA 2007 6 6 TRAX200700744 1 20070529 A 5320 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 LEFT FS 280 CROSSBEAM HAS CORROSION ON UPPER FLANGE. [SUP 06-07-07] REPAIRED IAW ALL SRM`S AND REO`S. 2 L 7 2 4F RT A21EA 2007060600224 20070606 00224 NM 2007 6 6 KCSA071172 1 20070531 A 5414 ANGLE BOEING 747 747221F 1384868 NM NR 1 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 NR 1 PYLON NAC STA-221 O/B ANGLE CRACKED FWD SIDE OF BULKHEAD. 2 L 7 4 4F A20WE 2007060600225 20070606 00225 NM 2007 6 6 KCSA071173 1 20070531 A 5320 CHANNEL BOEING 747 747221F 1384868 NM FUSELAGE CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 AFT BILGE FUSELAGE FRAME WEB SUPPORT CHANNEL IS CHAFFED AT STA 1680 RBL40. 2 L 7 4 4F A20WE 2007060700002 20070607 00002 WP 2007 6 7 PHA2007F00000 1 20070420 A 6720 369AT5058 SUPPORT HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL T/R PEDALS CRACKED E PHAA O OTHER O OTHER NR NOT REPORTED 1 NM 13 622PB 880318D AFTER A REFUELING STOP ON A PART 91 FLIGHT, THE PILOT PLACED HIS FEET ON THE TAIL ROTOR PEDALS AND FELT THEM MOVE. HIS INSPECTION REVEALED THAT 3 OF THE 4 MOUNT LOCATIONS FOR THE LT TAIL ROTOR PEDAL SUPPORT WERE BROKEN OFF OF THE SUPPORT. THE UPPER LT, LOWER LT, AND UPPER RT MOUNT LUGS SHEARED AT THE MOUNTING LUG. THE RT UPPER MOUNT SHOWED EVIDENCE OF STA INING IN THE CRACK AREA INDICATING THAT IT HAD BEEN PARTIALLY BROKEN FOR AN UNKNOWN PERIOD OF TIME. THIS CRACK WAS NOT VISIBLE DUE TO THE USE OF PROSEAL AS A CORROSION INHIBITER AT THIS LOCATION. (K) 1 G 7 1 3U 3 U H3WE E4CE 2007060700012 20070607 00012 NM 2007 6 7 AMTA200700223 1 20070504 A 5320 FLOOR SUPPORT BOEING 737 73783N 13844HI NM BS 847-864 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 304TZ 30675 AFT PIT B/S 847 THRU 864, RBL 15 CORROSION EXISTS 4 PLACES AS MARKED ON FLOOR ANGLE. REMOVED CORROSION SRM 51-00-53 TRE ATED IAW SRM 51-20-01. (K) 2 L 7 2 4F RT A16WE 2007060700015 20070607 00015 NM 2007 6 7 AMTA200700230 1 20070505 A 5551 PIN BOEING 737 73783N 13844HI NM HORIZONTAL STAB CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 304TZ 30675 LT HORIZ STAB LOWER AFT PIN PITTED, 180A1612-2. REPLACED PIN WITH 180A1612-4, AMM 27-41-11-4. (K) 2 L 7 2 4F RT A16WE 2007060700018 20070607 00018 NM 2007 6 7 AMTA200700229 1 20070505 A 5551 PIN BOEING 737 73783N 13844HI NM HORIZONTAL STAB CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 304TZ 30675 RT HORIZ STAB UPPER AFT ATTACH PIN PITTED, 180A1612-1. REMOVED AND REPLACED WITH 189A1612-3 IAW AMM 27-41-11-4. (K) 2 L 7 2 4F RT A16WE 2007060700019 20070607 00019 NM 2007 6 7 AMTA200700219 1 20070504 A 5320 FLOOR SUPPORT BOEING 737 73783N 13844HI NM BS 872-887 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 304TZ 30675 AFT PIT B/S 872 TO 887, RBL 15 CORROSION EXISTS (2) SPOTS AS MARKED ON FLOOR CHANNEL. (K) 10-26-07 REMOVED CORROSI ON SRM 51-10-02. ORIG .040 SRM 53-30-50 LOSS .002 IS WITHIN LIMITS SRM 53-00-53. DEPTH GAUGE NR 07-802 CAL DUE 08-12-0 7. TREAT AND PRIME SRM 51-20-01. (M) 2 L 7 2 4F RT A16WE 2007060700020 20070607 00020 NM 2007 6 7 AMTA200700226 1 20070504 A 5551 PIN BOEING 737 73783N 13844HI NM HORIZONTAL STAB CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 304TZ 30675 RT LOWER AFT STAB PIN CORRODED PN 180A1612-2. REMOVED AND REPLACES PIN 180A1612-4, AMM 27-41-11-4. (K) 2 L 7 2 4F RT A16WE 2007060700022 20070607 00022 NM 2007 6 7 AMTA200700228 1 20070504 A 5551 PIN BOEING 737 73783N 13844HI NM HORIZONTAL STAB CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 304TZ 30675 LT HORIZ STAB UPPER AFT PIN PITTED (180A1612-1). REPLACED PIN AMM 27-41-11-4 PN 180A1612-3. (K) 2 L 7 2 4F RT A16WE 2007060700023 20070607 00023 NM 2007 6 7 AMTA200700231 1 20070505 A 5347 MOUNT BOEING 737 73783N 13844HI NM LAVATORY CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 304TZ 30675 FWD LAV IB AFT MOUNT CORRODED. REMOVED MOUNT FAB NEW EA 737-2500-09-AO823-1 REINSTALLED SRM 25-46-99, REPAIR 1-1. (K) REMOVED AND REPLACED MOUNT AND BLOCK BRITAX SPM 25-46-99. INSTALLED LAV AMM 25-40-11. (M) 2 L 7 2 4F RT A16WE 2007060700024 20070607 00024 NM 2007 6 7 AMTA200700222 1 20070504 A 5310 CREASE BEAM BOEING 737 73783N 13844HI NM BS 727D-767 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 304TZ 30675 AFT PIT B/S 727D +12 THRU 767, RBL 22 CREASE ANGLE HAS CORROSION, 24 SPOTS AS MARKED. REMOVED CORROSION SRM 51-10-02 OR IG MTL THINK .040, SRM 53-30-53 MTL LOSS .002 TO .003 WITHIN LIMITS IAW SRM 53-00-02 TREATED IAW SRM 51-20-01. (K) 2 L 7 2 4F RT A16WE 2007060700025 20070607 00025 NM 2007 6 7 GAI2007F00000 1 20070427 A 5310 TORQUE BOX BOEING 727 727214 138407R NM PWA JT8 JT8D7B 52053 NE BS 1263 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 750US 21512 DURING INSPECTION IT WAS DISCOVERED THAT THE AFT AIRSTAIRS WOULD NOT TRAVEL TO THE FULLY CLOSED POSITION. FURTHER INSPE CTION FOUND A CRACK IN SECTION 48 LOWER AFT TORQUE BOX BY THE AIRSTAIR ACTUATOR FITTING. THE CRACK WAS REPAIRED IAW SB 727-53-0129. THE AIRSTAIR OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 3 4F 4 F A3WE E2EA 2007060700027 20070607 00027 NM 2007 6 7 AMTA200700232 1 20070505 A 5347 MOUNT BOEING 737 73783N 13844HI NM LAVATORY CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 304TZ 30675 CORROSION ON RT AFT LAV OB FLOOR MOUNT. REMOVED AFT OB BLOCK ATTACHMENT AND 2 FLOOR BLOCKS FAB NEW IAW EA 737-2500-09-A O822-1. INSTALLED IAW SER 25-46-99. REPAIR 1-5. (K) FABRICATED NEW MOUNT AND BLOCKS OF 7075-T73 EA 737-2500-09-A0822 . REMOVED AND REINSTALLED MOUNT AND BLOCKS BRITAX SPM 51-40-02. INSTALLED LAV AMM 25-40-15. (M) 2 L 7 2 4F RT A16WE 2007060700028 20070607 00028 EA 2007 6 7 FFS2007F00000 2 20070427 A 7314 200F5003 PUMP PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA HARTZL HCE3Y HCE3YR2A GL RT ENG FUEL LEAKING E FFSA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 01 3516A 447 317952106 RL139568A DJ8177A DURING A REGULAR SCHEDULED INSPECTION, IT WAS NOTED THAT THE RT ENGINE DRIVEN FUEL PUMP WAS LEAKING. THE PUMP WAS LEAKI NG FROM THE PRESSURE DOME HOUSING GASKETS. (K) 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2007060700029 20070607 00029 CE 2007 6 7 RTE2007F00001 1 20070423 A 5312 BULKHEAD CESSNA 172 172M 2072418 CE LYC O320 O320E2D 41508 EA FUSLEAGE CRACKED A RTEA K NONE O OTHER IN INSP/MAINT 1 NM 01 9379H 17266128 L2972927A DURING ROUTINE SCHEDULED INSPECTION, FOUND FWD PROP BULKHEAD TO BE CRACKED. THIS IS AN ON GOING PROBLEM WITH THESE COMP ONENTS. HAVE SEEN APPROXIMATELY (10) OF THESE BULKHEADS, ALL CRACKED IN THE SAME MANNER. ALL IN THE SAME LOCATION, RI GHT AT THE BEND RADIUS OB OF THE MOUNTING BOLT HOLES, ON DIFFERENT AIRPLANES, ENGINES AND PROPS. BELIEVE THE BEND RADIU S IS TOO SMALL ON THIS PART. ALSO, THE HEAT TREATMENT OR METALURGY MIGHT BE WRONG. (K) 1 H 7 1 3O 3 O NT 3A12 E274 2007060700030 20070607 00030 GL 2007 6 7 BAQ2007F00000 2 20070423 A 7250 23073533 SHIELD AGUSTA A109 A109A2 0260120 EU ALLSN 250C 250C20B 03013 GL 1ST STAGE NOZZLE FAILED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 1PJ 1631 7262 CAE834144 THE AIRCRAFT WAS ON A MAINTENANCE FLIGHT FOR ROUTINE TRACKING AND BALANCING FOLLOWING A MAIN ROTOR BLADE REPLACEMENT. T HE NR 2 ENGINE OIL TEMPERATURE WAS OBSERVED TO BE APPROXIMATELY 15 DEGREES HIGHER THAN THE NR 1 ENGINE OIL TEMPERATURE. ALL OTHER ENGINE PARAMETERS WERE NORMAL. THE NR 2 ENGINE WAS OBSERVED BY ANOTHER AC TO BE EMITTING AN UNUSUAL AMOUNT O F SMOKE. A PRECAUTIONARY LANDING WAS MADE AND THE NR 2 ENGINE WAS SECURED. INSPECTION OF THE NR 2 ENGINE REVEALED A FA ILURE OF THE 1ST STAGE NOZZLE SHIELD DOME ASSY (PN 23073533. THIS IS A KNOWN PROBLEM WHICH MFG HAS ADDRESSED WITH SB CE B-A-1370. THE CEB APPLIES TO EARLIER PN, BUT IS NOT APPLICABLE TO (PN 23073533). THIS FAILURE IS EXACTLY THE ANOMALY W 1 G 7 2 3U 3 U H7EU E4CE 2007060700036 20070607 00036 CE 2007 6 7 A2Y2007F00000 1 20070517 A 3233 98820162 ACTUATOR CESSNA 172 172RG 2072438 CE LYC O360 O360* 41514 EA LT MLG CRACKED E A2YA O OTHER O OTHER NR NOT REPORTED 1 NM 13 6273V 8764 172RG0603 PILOT MADE A NORMAL TAKEOFF AND GEAR RETRACTION. THE TOWER THEN INFORMED THE PILOT THAT THE LT MAIN GEAR LEG WAS NOT FU LLY RETRACTED. HE THEN TRIED TO CYCLE THE GEAR AGAIN WITH THE SAME RESULTS. AFTER CYCLING THE GEAR AGAIN THE GEAR THEN CAME DOWN AND INDICATED LOCKED. INSPECTION FOUND THAT THE ACTUATOR HAD CRACKED AT THE LOWER MOUNTING BOLT HOLE. (K) 1 H 7 1 3O 3 O 3A17 E286 2007060500216 20070605 00216 NM 2007 6 5 SWAA072695 1 20070528 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 7L CRACKED AT BS 295. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007060500227 20070605 00227 NM 2007 6 5 SWAA072734 1 20070528 A 5313 6551698 STRINGER SPLICE BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 7L. REMOVED AND REPLACED STRINGER SPLICE PER S RM. 2 L 7 2 4F RT A16WE 2007060500234 20070605 00234 NM 2007 6 5 SWAA072742 1 20070530 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060500245 20070605 00245 NM 2007 6 5 2007UALA01662 1 20070527 A 3397 CONNECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 342UA 24246 FIRST CLASS SECTION EEL LIGHTS INOPERATIVE. SECURED LOOSE CONNECTIONS. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007060500253 20070605 00253 NM 2007 6 5 2007UALA01670 1 20070528 A 5315 FLOORBEAM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 174UA 24381 FWD CARGO COMPT FLOORBEAM UPPER CHORD CRACKED, BS 560 RBL 30. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED AREA. INSTAL LED FILLER & ANGLE DOUBLER. 2 L 7 4 4F 4 F RT A20WE E24NE 2007060500265 20070605 00265 NM 2007 6 5 2007UALA01683 1 20070525 A 5330 RIVET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 RIVET DAMAGED BY LIGHTNING STRIKE STA 610 WL 160 ON LEFT SIDE OF FUSELAGE. REMOVED BLIND FASTENER, STEPPED UP HOLE AS R EQUIRED. NO CRACKS FOUND, INSTALLED SOLID FASTENER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500270 20070605 00270 NM 2007 6 5 2007UALA01689 1 20070526 A 3350 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 DOOR 1L EMERGENCY LIGHT TEST SWITCH BROKEN. REPLACED SWITCH. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500274 20070605 00274 NM 2007 6 5 2007UALA01693 1 20070527 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY LIGHTS AT ROW 3A AFT & FLOOR RIGHT ROW 2J ARE INOPERATIVE. RELAMPED EMERGENCY LIGHT. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007060500280 20070605 00280 NM 2007 6 5 2007UALA01699 1 20070526 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EMERGENCY EEL LIGHT INOP AT SEAT 2A AFT LIGHT ASSY. SECURED CONNECTOR. OPS CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007060500296 20070605 00296 NM 2007 6 5 2007UALA01716 1 20070527 A 2822 PUMP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FUEL SYSTEM INOPERATIVE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 668UA 30024 RIGHT CTR FUEL PUMP INOP. [07-10-07] REPLACED RIGHT CENTER LOW PRESSURE SWITCH AND RIGHT CENTER OVERRIDE PUMP. LEAK C HECK AND OPS CHECKED PUMP. CHK'S OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007060500300 20070605 00300 EU 2007 6 5 2007UALA01721 1 20070527 A 3250 CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG STEERING FAULTED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 462UA 1272 NW STEERING FAULT DISPLAYED WHEN PUTTING GEAR DOWN. [06-26-07] REPLACED STEERING SEVO CONTROL 6GC AND BSCU STEERING. DETERMINED A FAILED SENSOR 22GA, AFTER RING OUT SENSOR ON RT MAIN TRUCK INITIAL READING WAS 15 OHMS THEN SENSOR READ OPE N. SENSOR MUST READ APPROX 19 OHMS, SENSOR FAILED 2 L 7 2 4F 4 F RT A28NM E40NE 2007060600010 20070606 00010 EA 2007 6 6 A6WA200740109 1 20070307 A 5320 S6144A14 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 413AW 7585 RIGHT FS 484 INTERCOSTAL PREVIOUS REPAIR ANGLE AT RBL 36 CRACKED APPROXIMATELY .1 INCH LONG. MAINTENANCE INSTALLED NEWL Y FABRICATED ANGLE IAW BSC STANDARD REPAIR 601R-53-0030A AND BOMBARDIER REO 601R-53-121-059 REV A. (M) 2 L 7 2 4F RT A21EA 2007060600015 20070606 00015 EA 2007 6 6 A6WA200740203 1 20070418 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 417AW 7610 INBOARD FLOOR SUPPORT BEAM CLIP AT FS 280, LBL 9.0 IS CRACKED IN RADIUS APPROX .2 INCH LONG. (M) REPAIRED FS280 CLIP I AW BSC SR 601R530057A. (K) 2 L 7 2 4F RT A21EA 2007060600021 20070606 00021 EA 2007 6 6 A6WA200740128 1 20070309 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 413AW 7585 RIGHT WING INBOARD FUEL PANEL 640BB FOUND CORROSION AROUND WING PLANK APPROX .005 INCH DEEP IN NON-CRITICAL AREA. MAINT ENANCE REPAIRED CORROSION BY BLENDING IAW BOMBARDIER REO 601R-57-21-030 REV F. (M) 2 L 7 2 4F RT A21EA 2007060600050 20070606 00050 SO 2007 6 6 LR7A07028 1 20070216 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2613 4590 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5321, FOUND LT "ELEPHANT EAR" SKIN CRACKED AT FS847, LBL65, WL180. REPAIRED S KIN IAW SMP583 51-140-12. 2 H 7 4 4T A1SO 2007060600055 20070606 00055 NM 2007 6 6 SWAA072780 1 20070601 A 5315 6546811 FLOORBEAM BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986.5, BETWEEN LBL 43 AND RBL 43. REPAIRED CHORD PER ER. 2 L 7 2 4F RT A16WE 2007060600065 20070606 00065 NM 2007 6 6 SWAA072801 1 20070602 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007060600083 20070606 00083 2007 6 6 SWAA072809 4 20070604 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 469WN 33859 L2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007060600084 20070606 00084 2007 6 6 SWAA072808 4 20070604 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 418WN 29823 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007060600090 20070606 00090 EU 2007 6 6 2007UALA01737 1 20070531 A 3530 OXYGEN BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 493UA 1821 PORTABLE O2 BOTTLE AFT LT LOW. 2 L 7 2 4F 4 F RT A28NM E40NE 2007060600102 20070606 00102 EA 2007 6 6 TRAX200700733 1 20070528 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 870AS 7530 LEFT NR 2 EXTERNAL EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007060600106 20070606 00106 EA 2007 6 6 TRAX200700737 1 20070529 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 719EV 10099 RIGHT AFTMOST EXTERIOR EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007060600110 20070606 00110 EA 2007 6 6 TRAX200700741 1 20070529 A 5240 MECHANISM CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR LACK OF LUBE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 SERVICE DOOR FAILS PULL CHECK FOR FORCE REQUIRED TO OPEN DOOR. FORCE EXCEEDS 35LB MAXIMUM FORCE. LUBRICATED GALLEY SER VICE DOOR IAW CRJ 700 AMM 12-20-52. RECHECK - FUNCTIONAL TEST FOR FORCE REQUIRED. OPS CHECK GOOD, WITHIN LIMITS IAW CR J 700 AMM 52-41-00. SUPPLEMENTAL- SDR CLOSED 06/05/07. 2 L 7 2 4F RT A21EA 2007060600111 20070606 00111 NM 2007 6 6 SWAA072812 1 20070603 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 764, STR 19L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007060600112 20070606 00112 NM 2007 6 6 SWAA072810 1 20070603 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 751, STR 19L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007060600113 20070606 00113 NM 2007 6 6 SWAA072811 1 20070603 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007060600121 20070606 00121 NM 2007 6 6 SWAA072821 1 20070604 A 5511 6547987 RIB BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 14Y CHECK, FOUND LEFT HORIZONTAL STAB RIB CRACKED AT STA 151.75. REMOVED AND REPLACED RIB PER SRM. 2 L 7 2 4F RT A16WE 2007060600128 20070606 00128 2007 6 6 SWAA072807 4 20070604 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007060600133 20070606 00133 2007 6 6 SWAA072775 4 20070601 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 231WN 32499 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007060600134 20070606 00134 NM 2007 6 6 SWAA072785 1 20070601 A 5312 6545819 PRESSURE PANEL BOEING 737 7373A4 1384585 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED HC1 CHECK, FOUND NLG WHEEL WELL WEB CRACKED AT RIGHT BS 259, WL 174. REPAIRED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2007060600139 20070606 00139 NM 2007 6 6 SWAA072790 1 20070601 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED PAE CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060600144 20070606 00144 NM 2007 6 6 SWAA072791 1 20070602 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060600153 20070606 00153 EA 2007 6 6 TRAX200700757 1 20070530 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 850AS 7355 CORROSION ON FRAME AT FS 349 BETWEEN STR 26L TO 26R. 2 L 7 2 4F RT A21EA 2007060600159 20070606 00159 EU 2007 6 6 200715001 1 20070526 A 5220 HANDLE SAAB SF340 340B 7860101 EU EMERGENCY EXIT OUT OF ADJUST A SIMA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 21 219AE 340B219 RIGHT SIDE FORWARD EMERGENCY EXIT DOOR OPENED. ADJUSTED DOOR HANDLE IAW SAAB AMM. OPERATIONAL CHECKS GOOD. RETURNED A IRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007060600163 20070606 00163 EA 2007 6 6 SWIA200718284 1 20070417 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 927SW 7693 PAX DOOR - THE PAX DOOR FORWARD WEB IS CRACKED IN THE RADIUS BETWEEN THE 3RD AND 4TH FIXED STEPS, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS ON FORWARD WEB OF PAX DOOR PER REO 601R-52-11-1235. 2 L 7 2 4F RT A21EA 2007060600164 20070606 00164 EA 2007 6 6 SWIA200718285 1 20070417 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 927SW 7693 PAX DOOR AFT WEB IS CRACKED IN THE RADIUS BETWEEN THE 3RD AND 4TH FIXED STEPS, DISCOVERD AT C-CHECK. INSTALLED ALL REPA IR PARTS ON AFT SIDE OF PAX DOOR PER REO 601R 52-11-702 REV 'A'. 2 L 7 2 4F RT A21EA 2007060600165 20070606 00165 EA 2007 6 6 SWIA200718286 1 20070417 A 5210 BRACKET CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 927SW 7693 PAX DOOR ASSIST MOTOR BRACKET IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED PAX DOOR ASSIST MOTOR BRACKET PER SRM 51-42- 06. 2 L 7 2 4F RT A21EA 2007060600168 20070606 00168 EA 2007 6 6 SWIA200718289 1 20070416 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 709SK 10159 FS 280 SUPPORT BEAM IS CRACKED AT FITTINGS ON LEFT AND RIGHT BUTT LINE 9, DISCOVERED AT C-CHECK. INSTALLED FS 280 BEAM PER REO 670-53-11-047. INSTALLED COCKPIT FLOOR SUPPORT BEAM PN CC670-33292-13 PER CRJ700 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007060600179 20070606 00179 EA 2007 6 6 SWIA200718297 1 20070603 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 929SW 7703 AFT EMERGENCY LIGHT ON CEILING OF CABIN IS INOP. RELAMPED AFT EMERGENCY CEILING LIGHT. 2 L 7 2 4F RT A21EA 2007060600187 20070606 00187 SO 2007 6 6 LR7A07029 1 20070216 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2613 4590 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5321, FOUND RT "ELEPHANT EAR" SKIN CRACKED AT FS 847, RBL65, WL180. REPAIRED SKIN IAW SMP583 51-140-12. 2 H 7 4 4T A1SO 2007060600202 20070606 00202 EA 2007 6 6 TRAX200700732 1 20070527 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 355CA 10067 COCKPIT FLASHLIGHT INOP. FLIGHT ATTENDANT FLASHLIGHTS. 2 L 7 2 4F RT A21EA 2007060600209 20070606 00209 NM 2007 6 6 EIA2007101 1 20070514 A 3350 90083 BATTERY PACK BOEING 747 747273C 1384896 NM CABIN DISCHARGED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 470EV 20653 UPPER DECK EMERGENCY EXIT SIGN LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECKED GOOD PER B747 MM 33-51-00 PAG E 501. 2 L 7 4 4F A20WE 2007060600215 20070606 00215 NM 2007 6 6 EIA2007107 1 20070519 A 5321 FLOOR PANEL BOEING 747 747230B 1384889 NM CABIN CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 487EV 23286 MAIN DECK BS 800 FWD OUTBOARD END OF PANEL 83 HAS CORROSION BETWEEN FLOOR BEAM AND SEAT TRACK. REMOVED CORROSION, NDTD AREA, FABRICATED AND INSTALLED REPAIR PER B747 SRM 53-10-07 FIG 10. 2 L 7 4 4F A20WE 2007060700001 20070607 00001 NM 2007 6 7 AMTA200700234 1 20070512 A 2410 727792M GENERATOR BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE LEFT UNSERVICEABLE A AMTA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 550TZ 12732 52 32584 ON ENG STARTUP (LEFT) GENERATOR DRIVE LIGHT COMES ON. REMOVED AND REPLACED NR 1 IDG IAW M-SHEET M57-24-01 AND AMM 24-11 -01-4. OPS CHECK GOOD NO LEAKS NOTED. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007060700011 20070607 00011 EA 2007 6 7 A6WA200740217 1 20070424 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR LACK OF LUBE A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 406AW 7402 AT ROTATION GOT PAX DOOR CAUTION MESSAGE ILLUMINATED COMPLIED WITH QRH GREEN WITNESS MARKS NOT ALIGNED AT GATE DOOR STIL L WOULD NOT CLOSE PROPERLY. INSPECTED DOOR AND FOUND EXTERNAL HANDLE WOULD NOT STOW WITHOUT USE OF EXCESSIVE FORCE FROM INTERNAL STOW HANDLE. HANDLE STOWS NORMALLY FROM OUTSIDE AIRCRAFT. CAX FLT 3952, 3969, 3596 REF 168980/1. LUBRICATED PAX DOOR LATCH PINS AND OUTER HANDLE. STOWS NORMAL WITH LOCKED GREEN INDICATORS ALIGNED IAW EO E98/023/452. FOR PHASE 4 DOOR. REMOVED FROM MEL. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007060700016 20070607 00016 NM 2007 6 7 AMTA200700235 1 20070513 A 2120 UNKNOWN BOEING 737 73783N 13844HI NM COCKPIT ODOR A AMTA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 11 317TZ 28246 CREW DEBRIEF STRONG ODOR ON DESCENT. ODOR LINGERS IN COCKPIT. CREW STATES PRESSURE PROBLEM AT 22,000 FT WITH RT PACK OP ERATING. (95344) PERFORMED FIM 21-00-00-810-802, FTD-21-05001, MM 21. AC HAS NO FUMES AT THIS TIME. OK FOR SERVICE. (K) 2 L 7 2 4F RT A16WE 2007060700017 20070607 00017 EA 2007 6 7 A6WA200740218 1 20070425 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SPOILERONS ILLUMINATED A A6WA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 435AW 7724 HIGH SPEED ABORTED TAKEOFF DUE TO (SPOILERON) CAUTION MESSAGE. SPEED WAS 110 KNOTS. BRAKE TEMPS WERE 7-8-8-8. FAULT C LEARED USING FIM RESET PROCEDURE IAW AMM 05-51-27-210-801. NO FURTHER INSPECTION REQUIRED FOR REJECTED TAKEOFF. AC OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007060700037 20070607 00037 SO 2007 6 7 VCT2007F00000 1 20070520 A 7933 553673 PROBE PIPER PA34 PA34200T 7103406 SO CONT O360 TSIO360B 17025 SO LT OIL TEMP MALFUNCTIONED E VCTA O OTHER O OTHER NR NOT REPORTED 1 EA 17 19TP 6080 347870383 307599 ERRATIC OIL TEMP GAGE MOVEMENT. (K) 1 L 7 2 3O 3 O A7SO E9CE 2007060700038 20070607 00038 NM 2007 6 7 KCSA071174 1 20070531 A 5311 FRAME BOEING 747 747221F 1384868 NM BS 434 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 STA 434 FRAME CRACKED LBL 49 WL 121 APROX .75 INCH. 2 L 7 4 4F A20WE 2007060700040 20070607 00040 NM 2007 6 7 HNAA0700100 1 20070508 A 5313 CV607X240INEXT STRINGER DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 938HA 152 CORROSION ON STRINGER 31 FWD OF X202. STRINGER 31 FWD OF X202 REPAIRED AS PER RD-8-53-1243. 2 H 7 2 4T RT A13NM 2007060700051 20070607 00051 NM 2007 6 7 DHL2007740515 1 20070606 A 5320 INTERCOSTAL BOEING 727 7272Q9 138448M NM BS 683 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 FWD PIT BS 683 BETWEEN STR'S 27R AND 28R INTERCOSTAL HAS 2 HOLES NEARBY 2 RIVETS. REMOVED INTERCOSTAL IAW 727 SRM 51-30 -2. FABRICATED NEW INTERCOSTAL USING 7075-T6 .032 PO NR 9004940 DIM 18.50" BY 5.50" IAW 727 SRM 53-10-2 FIG 3. ALODINE D AND PRIMED AND REINSTALLED FABRICATED INTERCOSTAL IAW 727 SRM'S 51-10-2 AND 51-20-1 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007060700052 20070607 00052 NM 2007 6 7 NWAA072076311 1 20070531 A 2530 CONTROLLER BOEING 747 747451 1384940 NM OVEN ODOR A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 671US 26477 AFTER TAKEOFF, THE FLIGHT ATTENDANTS CALLED ABOUT A BURNING ODOR FROM GALLEY NR 2. CIRCUIT BREAKERS FOR OVENS 2-45, AND 2-46 WERE PULLED, AND ODOR WAS ELIMINATED. AFTER COOKING BREAKFAST, GALLEY 2A LOST ALL POWER. AS A PRECAUTION THE RED MASTER GALLEY SWITCH WAS TURNED OFF. FLIGHT CONTINUED ON AND LANDING WAS UNEVENTFUL. MAINTENANCE FOUND OVEN 2-45 MOTO R FAN SEIZED AND BURNED. OVEN AND CONTROLLER WERE REMOVED AND REPLACED. OPERATIONAL CHECKED GOOD, AND AIRCRAFT WAS RET URNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007060700054 20070607 00054 NM 2007 6 7 DHL2007740512 1 20070514 A 5344 HINGE BOEING 727 7272Q9 138448M NM BS 650 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 EXT FUSE MCD AFT MOST HINGE SEGMENT BS 650 IS CRACKED ON THE AFT LOBE. REMOVED HINGE SECTION IAW B727-200 AEI MM CHAP 5 2. FAB`D NEW HINGE SECTION FROM MS20001-16-7200 PO NR 9002527 DIM 17" LONG AN 11" LONG IAW B727 MM AEI CHAP 52 TREATED AN PRIMED AREA AN PARTS IAW B727 SRM 51-10-2. INSTALLED NEW HINGE SECTION AT EXT FUSE. MCD AFT BS 650 IAW B727-2000 AE I MM CHAP 52 OPS CHECK GOOD IAW AEI MM CH 52 AN 29. MAJOR REPAIR AND PERMANENT REPAIR. 2 L 7 3 4F RT A3WE 2007060700055 20070607 00055 2007 6 7 QXEA200700873 2 20070601 A 7397 CONNECTOR BOMBDR DHC8 DHC8402 1390042 NM FUEL TEMP SENSOR DIRTY A QXEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 09 407QX 4049 GTF FLIGHT NR 2324: NR 1 FUEL TEMP ERRONEOUSLY SHOWED INDICATIONS FROM NORMAL TO 85 DEG C. FLIGHT WAS DIVERTED TO GEG. MAINTENANCE REMOVED (DISCONNECTED) NR 1 ENG FUEL TEMP SENSOR CONNECTOR AND FOUND IT TO BE DIRTY. CLEANED CONNECTOR AND SENSOR ELECTRICAL CONNECTIONS AND RECONNECTED. PERFORMED TEST OF SENSOR IAW AMM TASK 73-31-09-400-801, STEP 5 FG TESTS GOOD. INDICATED TEMP LOWERED 9 DEG C FROM INITIAL READING AND READING AFTER MTX ACTION. NO OTHER DEFECTS NOTED. NO P ARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007060700056 20070607 00056 NM 2007 6 7 QXEA200700874 1 20070604 A 5610 80260007 WINDSHIELD BOMBDR DHC8 DHC8402 1390042 NM COCKPIT CRACKED A QXEA A D UNSCHED LANDING RETURN TO BLOCK O OTHER CL CLIMB 1 NM 09 425QX 2530 2530 4039 BOI FLIGHT NR 2407: CLIMBING THROUGH 21,000 FEET, CAPTAIN'S WINDSHIELD CRACKED OVER MAJORITY OF AREA. AIRCRAFT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED CAPTAINS WINDSHIELD IAW Q400 AMM 56-10-01, PG 401-415. GROUND OPS CHECK NO RMAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007060700058 20070607 00058 NM 2007 6 7 DHL2007740508 1 20070516 A 5754 HOOK BOEING 727 7272Q9 138448M NM ZONE 500 GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 NR 3 SLAT GOUGED AT O/B SLAT HOOK. ROUTED OUT EDGE WITH MAT LOSS OF 0.192" FOUND OUT OF LIMITS IAW B727 SRM 57-50-1 FIG 1. FAB`D DOUBLER REPAIR FROM 2024-T3 0.125" PO NR 645747 DIM 5" BY 3 1/2" IAW B727 SRM 57-50-3 FIG 10. TREATED AND PR IMED PARTS IAW B727 SRM 51-10-2 AN INSTALLED REPAIR DOUBLER AT NR3 O/B SLAT HOOK IAW B727 SRM 57-50-3 FIG 10, 51-30-2. 2 L 7 3 4F RT A3WE 2007060700059 20070607 00059 2007 6 7 DL76L070635 2 20070531 A 7320 285T0458203 CIRCUIT CARD BOEING 767 767332 1382001 NM ENGINE SPEED MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 188DN 27583 LT ENG SPEED CARD DURING TAXI OUT. RESET C/BS AND RE-SEATED CARD NO HELP. HARD FAULT WITH ENGS SHUTDOWN. PLACED LEFT CARD IN THE RT POSITION AND TESTED NORMAL. RE-POSITIONED CARDS TO ORIGINAL POSITION AND ALL TESTED NORMAL. AIRCRAFT WI LL DEPART ON 60/60 V/F TO DKR. C/BS D15 AND D23 CYCLED DC VOLTAGE MEASURED ALL NORMAL SPEED LEFT RERACKED NO CURE. SPE EDCARD LEFT PLACED IN THE RIGHT POSITION THEN BACK TO ITS ORIGINAL PLACE STS MSG CLEARED GN ENG RUN PERF ALL NORMAL. 2 L 7 2 4F RT A1NM 2007060700060 20070607 00060 NM 2007 6 7 DLM88070637 1 20070527 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 1437 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 FOUND CRACK ON FUSELAGE SKIN AT Y-1427 BETWEEN LONGERON 4 LT AND 5 LT. DAMAGE WAS REPAIRED AS PERMANENT FOLLOWING ALL I NSTRUCTIONS AND RECOMMENDATIONS ON SRM 53-04D FIG 27 ON NR CARD T005703B. 2 L 7 2 4F RT A6WE 2007060700061 20070607 00061 NM 2007 6 7 DLM88070638 1 20070527 A 5347 SEAT TRACK DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 FOUND CORROSION ON SEAT TRACK X = -54 AT STATIONS Y=271, 307, 326, 344, 364, 381, 416, 430, 448, 465, 470, 481, 498, 515 , 531, 547, AND 564. DAMAGE AT STATIONS ABOVE WAS REMOVED IAW SRM 53-05D FIG 4A. 2 L 7 2 4F RT A6WE 2007060700062 20070607 00062 NM 2007 6 7 DL764070639 1 20070601 A 3350 BATTERY PACK BOEING 767 767432ER 1385134 NM EMERGENCY LIGHTS DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 832MH 29704 FOUND ROWS 34-41 RIGHT SIDE EMERGENCY LIGHT INOP. REMOVED AND REPLACD BATTERY PACK AT SEAT ROW 36 FG, OPS NML MFG P/ 71 7-01-100. 2 L 7 2 4F RT A1NM 2007060700065 20070607 00065 NM 2007 6 7 DLM88070642 1 20070527 A 5310 DOOR FRAME DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACK ON DOOR JAMB IN AFT EXTERNAL A/C SERVICE PANEL AT AFT OUTBD CORNER. FABRICATED AND INSTALLED DOUBLER REF SRM. 2 L 7 2 4F RT A6WE 2007060700066 20070607 00066 NM 2007 6 7 DLM88070643 1 20070527 A 5310 DOOR FRAME DOUG MD88 MD88 3023688 NM L MLG DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACK ON LEFT MLG DOOR JAMB AT FWD OUTER SIDE. DOOR JAMB REPLACED IAW DRAWING 5930584 N/R T0056090. 2 L 7 2 4F RT A6WE 2007060700068 20070607 00068 NM 2007 6 7 DHL2007740516 1 20070606 A 5320 INTERCOSTAL BOEING 727 7272Q9 138448M NM ZONE 100 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 FWD PIT BETWEEN STA 680 AND STA 700 INTERCOSTAL AT LT STR 26 IS CRACKED AT TOP EDGE. REMOVED CRACKED INTERCOSTAL IAW SR M 51-30-2 AND FABRICATED A NEW INTERCOSTAL FROM 7075-T6 .050 PO NR 9004940, DIM 10.75" BY 9" IAW 727 SRM 51-20-1 AND 53- 10-2 FIG 3. TREATED AND PRIMED AND REINSTALLED FABRICATED INTERCOSTAL IAW SRM"S 51-10-2 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007060800002 20070608 00002 NM 2007 6 8 QXEA200700885 1 20070524 A 5410 DIAPHRAGM BOMBDR DHC8 DHC8402 1390042 NM NR 1 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 C4 PDX - NR 1 ENGINE NACELLE DIAPHRAGM CRACKED. REPAIRED IAW SRM 51-42-05, 51-40-10. 2 H 7 2 4T RT A13NM 2007060800006 20070608 00006 NM 2007 6 8 QXEA200700888 1 20070522 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 C4 PDX - SEAT TRACK WEB IS CORRODED AROUND SCREW HOLE AT STATION X 1.03 OUTBOARD OF LEFT INBOARD SEAT TRACKS. REPAIRED IAW SRM 51-21-00. 2 H 7 2 4T RT A13NM 2007060800007 20070608 00007 NM 2007 6 8 QXEA200700889 1 20070523 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 C4 PDX - THERE IS CORROSION ON THE RIGHT INBOARD SEAT TRACK INSIDE THE FLANGE AND ON THE FLANGE FROM X2 TO X6.5. REPAIR ED IAW RD8/4-53-884 AND SRM 51-40-10. 2 H 7 2 4T RT A13NM 2007060800012 20070608 00012 NM 2007 6 8 QXEA200700893 1 20070531 A 5311 FRAME BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 C4 PDX - FUSE CIRCUMFERENTIAL FRAME HAS CHAFE DAMAGE AT STATION X1.000 AT Z100.032 UNDER MAIN CABIN DOOR APERTURE LOWER FORWARD CORNER CASTING. REPAIRED IAW SRM 53-20-15 AND RD8/4-53-1928. 2 H 7 2 4T RT A13NM 2007060800016 20070608 00016 NM 2007 6 8 DHL2007740504 1 20070519 A 5754 RIB BOEING 727 7272Q9 138448M NM NR 3 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 LT WING NR 3 SLAT ACTUATOR ROD O/B ATTACH RIB CRACKED. REMOVED NR 3 SLAT ACTUATOR O/B RIB IAW B727 SRM 51-30-2. FABBED NEW RIB MAT. USED 7075 .040 PO NR 9003230 DIM 16" BY 6" BY 6" IAW B727 SRM 51-30-5 AND 57-50-2 FIG 2. HEAT TREATED MAT ERIAL TO T6 CONDITION IAW FAS FORM NR FAS0115 REV 10. TREATED AND PRIMED IAW B727 SRM 51-10-2, INSTALLED IAW B727 SRM 5 1-30-2. 2 L 7 3 4F RT A3WE 2007060800019 20070608 00019 WP 2007 6 8 DHL2007803516 1 20070530 A 5347 CARGO TRACK DOUG DC8 DC873 302199C WP BS 135-270 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 UPPER CARGO COMPT NR 6 TRACK LUGS WORN (STA 135.000 - 270.000). CUT OUT DAMAGED SEGMENT OF TRACK NR 6 AND FABRICATED SP LICES (AL7075T6 0.100"/ 0.125"/ 0.160") IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA AND SPLICES IAW SRM 5 1-1-8B. INSTALLED NEW TRACK SEGMENT P/N SE08530006-3 AND SPLICES IAW SRM 53-2-3 PG 49-50, SRM 51-3-0, SRM 51-3-1 (TORQU E). 2 L 7 4 4F RT 4A25 2007060800021 20070608 00021 WP 2007 6 8 DHL2007803515 1 20070531 A 5730 SKIN DOUG DC8 DC873 302199C WP LT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 LT WING T/E LWR PANEL SKIN DELAMINATED (STA XF 339.000 - 409.000). REMOVED AND REPLACED DELAMINATED LT WING T/E LWR PAN EL IAW SRM 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007060800023 20070608 00023 WP 2007 6 8 DHL2007803502 1 20070523 A 5711 FRAME DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 RT WING OUTBD L/E INNER SECTION LWR FORMER CRACKED 0.500" AT STA 622.250. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATE D TWO ANGLES DOUBLERS (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLES IAW SRM 51- 1-8B. INSTALLED ANGLES IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUED). 2 L 7 4 4F RT 4A25 2007060800024 20070608 00024 WP 2007 6 8 DHL2007803512 1 20070528 A 5320 ANGLE DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 RT MLG W/W ANGLE CRACKED 1" STA 940.000. REMOVED CRACKED ANGLE IAW SRM 51-1-20D. FABRICATED NEW ANGLE (EXTRUSION 26162 79) IAW SRM 53-2-0 PG 1, SRM 51-2-0 FIG 50. CLEANED, TREATED AND PRIMED AREA AND NEW ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007060800025 20070608 00025 WP 2007 6 8 DHL2007803513 1 20070528 A 5320 ANGLE DOUG DC8 DC873 302199C WP LT MLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 LT MLG W/W UPPER ANGLE CRACKED STA XFS 920.000 LBL 44". REMOVED CRACKED ANGLE IAW SRM 51-1-21. FABRICATED NEW ANGLE (A L2024T3 0.050") IAW SRM 53-2-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND NEW ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANGL E IAW SRM 51-1-21 2 L 7 4 4F RT 4A25 2007060800026 20070608 00026 WP 2007 6 8 DHL2007803514 1 20070528 A 5320 ANGLE DOUG DC8 DC873 302199C WP RT MLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 RT MLG W/W ANGLE CRACKED 1" STA 950.000. REMOVED CRACKED ANGLE IAW SRM 51-1-20D. FABRICATED NEW ANGLE (EXTRUSION 26162 79) IAW SRM 53-2-0 PG 1, SRM 51-2-0 FIG 50. CLEANED, TREATED AND PRIMED AREA AND ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-20D, SRM 51-3-1 PG 2. 2 L 7 4 4F RT 4A25 2007060800028 20070608 00028 WP 2007 6 8 DHL2007803509 1 20070525 A 5330 SKIN DOUG DC8 DC873 302199C WP BS 580 S4-5R CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 UPPER FUSELAGE EXT SKIN CRACKED 0.500" APPROX, STA 580.000 L-4R TO L-5R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1, 3. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER (AL7075 T6 0.100") (2EA) INTERNAL FINGER DOUBLERS (AL7075T6 0.050") AND FILLER (AL7075T6 0.090") IAW SRM 53-2-1 FIG 7 SHEET 1-3, SRM 53-4-1 FIG 13 ITEM A, SRM 51-9-0 FIG 68A. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPL IED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW SRM 53-2-1 FIG 7 SHEET 1, 3, SRM 51-1-21, SR M 51-1-20D, SRM 51-3-1 (TORQUE) THIS IS A CLASS 1 TYPE INSPECTION AND NEEDS AN EXTERNAL VISUAL INSPECTION EACH 4.000 FC 2 L 7 4 4F RT 4A25 2007060800031 20070608 00031 NM 2007 6 8 UIEA200700232 1 20070523 A 3230 60B002163 SELECTOR VALVE BOEING 747 7472D7B 1384803 NM MLG LEAKING A UIEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 15 524MC 21784 AIR TURN BACK NR 4 HYDRAULIC SYSTEM LOST JUST ABOVE V1 ON TAKEOFF. SYSTEM WENT TO ZERO PRESSURE AND QUANTITY. EDP WAS PLACED TO SUPPLY OFF. FOUND WING GEAR SELECTOR VALVE IN RT WHEEL WELL LEAKING. REMOVED AND REPLACED VALVE PER 32-31-03 , OPS AND LEAK CHECKED OK. HYD PUMP AND FILTERS REPLACED ALSO SEE LOG PAGE 193806. 2 L 7 4 4F RT A20WE 2007060800032 20070608 00032 NM 2007 6 8 UIEA200700233 1 20070525 A 7830 9105M20G14 SKIN BOEING 747 7472D3B 1384805 NM THRUST REVERSER DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 21252 NR 3 ENGINE RT THRUST REVERSER EXTERIOR SKIN LOWER AREA AT 5 O'CLOCK POSITION HAS 3 EACH DENTS. PERMANENT REPAIR WAS AC COMPLISHED AS PER GE CF6-50 ENGINE MANUAL 78-32-01 REPAIR 3, FIG 1. ALSO, REFERENCE ATLAS AIR EO NR 4778A098. 2 L 7 4 4F RT A20WE 2007060800033 20070608 00033 WP 2007 6 8 DHL2007803518 1 20070527 A 5230 SKIN DOUG DC8 DC873 302199C WP CARGO DOOR MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 803DH 83934 46123 "B" CARGO DOOR SKIN REPAIR RIVETS EDGE DISTANCE NOT IN ACCORDANCE WITH SRM (UPPER PORTION) MAJOR REPAIR. PERFORMED MAJO R REPAIR IAW SRM 52-2-0 FIG 4 SHEET 3. REMOVED EXISTING REPAIR IAW SRM 51-1-21. FABRICATED REPAIR DOUBLER AND FILLER ( AL7075T6 0.063")IAW SRM 52-2-0 FIG 4 SHEET 3, SRM 52-4-1 FIG 3 ITEM "K", SRM 51-9-0 FIG 68A. CLEANED, TREATED AND PRIME D AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IA W SRM 52-2-0 FIG 4 SHEET 3, SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007060800035 20070608 00035 WP 2007 6 8 DHL2007803506 1 20070523 A 5730 DOUBLER DOUG DC8 DC873 302199C WP RT WING SKIN CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 RT WING CTR L/E LWR SKIN INTERNAL DOUBLER CRACKED 0.500" STA XFS 428.000. REMOVED CRACKED INTERNAL DOUBLER IAW SRM 51-1 -21, SRM 51-1-20D. FABRICATED NEW INTERNAL DOUBLER (AL7075T6 0.090") IAW SRM 57-2-0 PG 1 AND CLEANED, TREATED AND PRIME D AREA AND INTERNAL DOUBLER IAW SRM 51-1-8B. INSTALLED INTERNAL DOUBLER IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQ UE). 2 L 7 4 4F RT 4A25 2007060800036 20070608 00036 WP 2007 6 8 DHL2007803500 1 20070523 A 5711 FRAME DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 RT WING OUTBD L/E INNER SECTION LWR FORMER CRACKED 0.500" AT STA XFS 660.000. REMOVED FASTENERS IAW SRM 51-1-21. FABRI CATED ANGLES (2EA) DOUBLERS AL7075T6 0.032" IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. INSTALLED ANGLES DOUBLERS (2EA) IAW SRM 51-1-21, SRM 51-1-20D AND TORQUED IAW SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007060800037 20070608 00037 WP 2007 6 8 DHL2007803503 1 20070523 A 5711 FRAME DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 RT WING OUTBD L/E INNER SECTION LWR FORMER CRACKED 0.500" AT STA XFS 616.250. REMOVED FASTENERS IAW SRM 51-1-21. FABRI CATED 2 ANGLE DOUBLERS AL7075T6 0.032" IAW SRM 57-2-0 PG 9-10. CLEANED,TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW S RM 51-1-8B. INSTALLED 2 ANGLES DOUBLERS IAW SRM 51-1-21, SRM 51-1-20D AND TORQUED IAW SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007060800038 20070608 00038 WP 2007 6 8 DHL2007803501 1 20070523 A 5711 FRAME DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 RT WING OUTBD L/E INNER SECTION LWR FORMER CRACKED 0.500" AT STA XFS 653.750. REMOVED FASTENERS IAW SRM 51-1-21. FABRI CATED 2EA ANGLES DOUBLERS (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLES IAW SRM 51-1-8B. INSTALLED ANGLES DOUBLER IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUED). 2 L 7 4 4F RT 4A25 2007060800039 20070608 00039 NM 2007 6 8 DHL2007740507 1 20070522 A 5210 SKIN BOEING 727 7272Q9 138448M NM ZONE 800 BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 L-2 DOOR LOWER HINGE ARM SKIN IS BROKEN AT FWD END. REMOVED SKIN SECTION IAW B727 SRM 51-30-2. FABBED NEW SKIN FROM 20 24-T3 0.050" PO NR 9005049, DIM 9" BY 1 1/2 " IAW B727 SRM 52-40-1 FIG 4 AND 51-20-1. TREATED AN PRIMED NEW PART IAW B7 27 SRM 51-10-2 AN INSTALLED NEW SKIN SECTION AT L-2 DOOR LOWER HINGE ARM IAW B727 SRM 51-30-2. MAJOR REPAIR. PERMANENT REPAIR. 2 L 7 3 4F RT A3WE 2007060800040 20070608 00040 NM 2007 6 8 DHL2007786503 1 20070328 A 5320 WEB BOEING 727 727214 138407R NM BS 1329 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 756AT 21692 CRACK AT LIGHTENING HOLE, RT LOWER TORQUE BOX STA 1329. STOP DRILLED 0.250" DIAMETER HOLE AT LIGHTENING HOLE RT LOWER T ORQUE BOX STA 1329 IAW B727 SRM 51-40-2. NDT C/W HFEC FOR CRACK STOP VERIFED, IAW B727 NDTM, PT6 51-00-00 FIG 23. FABR ICATED DOUBLER REPAIR AT LIGHTENING HOLE RT LOWER TORQUE BOX STA 1329 MATERIAL USED 7075T6 .040 PO NR 9003110 SIZE 5 3/4 " BY 3 1/2" IAW B727 SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. TREATED ALODINE AND PRIMED PART AND AREA IAW B727 SRM 51-10-2 . INSTALLED DOUBLER REPAIR AT LIGHTENING HOLE STA 1329 IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007060800043 20070608 00043 NM 2007 6 8 NWAA072086729 1 20070531 A 5230 65B179148 PUSHROD BOEING 747 747251F 1384898 NM CARGO DOOR FAILED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 629US 22388 DURING THRU FLIGHT, FOUND DAMAGE TO MAIN DECK CARGO SIDE CARGO DOOR LOWER BEAM WEB AND STIFFENER AT BS 1800. IT WAS DET ERMINED THAT DAMAGE WAS A RESULT OF IMPACT WITH A FAILED DOOR PUSHROD. REPAIR ACCOMPLISHED PER EA 67-209695. 2 L 7 4 4F A20WE 2007060800048 20070608 00048 CE 2007 6 8 DHL2007366001 1 20070530 A 5330 SKIN CESSNA 310 310K 2074228 CE FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 366D 310K0230 LT FUSELAGE BY LAP SEAM BULGE IN SKIN NEAR FRAME 61 AND 62 AND BETWEEN STRINGERS S-44L AND S-45L. 1 L 7 2 3O 3A10 2007060800049 20070608 00049 NM 2007 6 8 DHL2007740514 1 20070606 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 1130 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AFT CARGO BS 1130 BETWEEN STR'S 27R AND 29L, FRAME HAS BARE METAL AND CORROSION. CORROSION REMOVAL OUT OF LIMITS PER B7 27 SRM 53-10-1 FIG 1. REMOVED AND FABRICATED 4 SHEAR TIE ANGLES FROM 7075-T6, .063" BY 6" BY 2.5" ( 4 EACH), PO NR 900 4690. TREATED, PRIMED, AND INSTALLED 4 ANGLES PER B727 SRM 53-10-2 FIG 5, 51-20-1, AND 51-10-2. 2 L 7 3 4F RT A3WE 2007060800050 20070608 00050 WP 2007 6 8 07FDEA01944 1 20070522 A 5230 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP BS 755 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 MAIN CARGO DOOR NR 7 LATCH SPOOL AND FITTING IS CORRODED. REMOVED NR 7 SPOOL IAW FEDEX EA NR 8-5230-110663 REV A. " FU SELAGE-MAIN CARGO DOOR - LOWER JAMB SUPPORT FITTING INSPECTION AND DOOR RIG." CLEANED AND TREATED, PRIMED IAW FEDEX MD 10 SRM 51-21-01 VOL 11. SPOOL AND FITTING INSTALLED NR 7 SPOOL ON EA 8-5230-110663 REV, A. 2 L 7 3 4F RT A22WE 2007060800052 20070608 00052 NM 2007 6 8 DHL2007740517 1 20070606 A 5320 INTERCOSTAL BOEING 727 7272Q9 138448M NM BS 700 S26R DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 BS 700 STR 26R MISDRILLED INTERCOSTAL WEB. REMOVED WEB IAW 727 SRM 51-30-2. FABRICATED NEW WEB USING 2024-T3 .063 PO N R 9004940 DIM 12" BY 8.25" IAW 727 SRM 53-10-2. ALODINED AND PRIMED AND REINSTALLED FABRICATED WEB IAW 727 SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007060800056 20070608 00056 NM 2007 6 8 DHL2007740513 1 20070506 A 5311 FRAME BOEING 727 7272Q9 138448M NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH AFT CARGO BS 1030, BETWEEN STR'S 28R AND 29R, AFT SIDE OF FRAME HAS CORROSION BELOW FAIL SAFE CHORD. CORROSION REMOVAL OUT OF LIMITS PER B727 SRM 53-10-1 FIG 1. CUT OUT SHEAR TIE, FABRICATED NEW SHEAR TIE FROM 7075-T6, .071" BY 6.75" BY 4 ", PO NR 9004940, TREATED, PRIMED, AND INSTALLED SHEAR TIE PER B727 SRM 53-10-4 FIG 12, 51-10-2, AND 53-10-4. 2 L 7 3 4F RT A3WE 2007060800058 20070608 00058 NM 2007 6 8 DLM88070646 1 20070527 A 5712 RIB DOUG MD88 MD88 3023688 NM LT WING BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 BROKEN RIB IN LT FIXED L/E AT STA XFS=218. RIB REMOVED IAW SRM 51-30-2. RIB AND DOUBLER INSTALLED IAW SRM 51-06B FIG 1 7 N/R T0056247. 2 L 7 2 4F RT A6WE 2007060800060 20070608 00060 NM 2007 6 8 DLM88070648 1 20070528 A 5320 SUPPORT DOUG MD88 MD88 3023688 NM BS 788 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACK ON RT SIDE WALL PANEL SUPPORT AT STA Y=788. STIFFENER REMOVED, FABRICATED AND INSTALLED IAW SRM 53-24-0DNR T00563 53. 2 L 7 2 4F RT A6WE 2007060800062 20070608 00062 NM 2007 6 8 DL76L070650 1 20070602 A 3260 SENSOR BOEING 767 767332 1382001 NM MLG INOPERATIVE A DALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 198DN 28455 CREW IS REPORTING MULTIPLE AIR GND PROBLEMS ALONG WITH SEVERAL PROBE HEAT AND FLAP/CONFIG WARNINGS RETURNING TO JFK FOR REPAIRS. JACKED A/C. A/G DISAGREE AND BOTH ICE DETECTOR STATUS MESSAGE DISPLAYED. FOUND SENSOR S268 BAD. REPLACED SE NSOR S268 TEST PER MM. 2 L 7 2 4F RT A1NM 2007060800063 20070608 00063 NM 2007 6 8 DLM88070651 1 20070528 A 5313 LONGERON DOUG MD88 MD88 3023688 NM BS 160 L4L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACK ON LONGERON 4 LT STA Y=160. FABRICATED AND INSTALLED NEW SECTION IAW SRM 53-02 FIG 18. 2 L 7 2 4F RT A6WE 2007060800065 20070608 00065 NM 2007 6 8 DLM88070653 1 20070529 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 1309 L6-7R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACK ON FUSELAGE SKIN AT STA 1309 BETWEEN LONGERONS 6 RT AND 7 RT. DOUBLER REPLACED IAW SRM 53-04D FIG 31 NR T0056620. 2 L 7 2 4F RT A6WE 2007060800066 20070608 00066 NM 2007 6 8 DLM88070654 1 20070529 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 1437 L4-5R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACK ON FUSELAGE SKIN AT STA 1437 BETWEEN LONGERONS 4 RT AND 5 RT. EDDY CURRENT INSPECTION PERFORMED ON SKIN. NO CRAC KS WERE FOUND ACCORDING TO NDT SRM 06-10-01-001 NR T0056624. 2 L 7 2 4F RT A6WE 2007060800067 20070608 00067 NM 2007 6 8 DLM88070656 1 20070529 A 5313 LONGERON DOUG MD88 MD88 3023688 NM BS 208 L11L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACK ON SPLICE AT STA Y=208, LONGERON 11 LT. REPLACED DOUBLER IAW SRM 53-01 FIG 2 NR T0056782. 2 L 7 2 4F RT A6WE 2007060800069 20070608 00069 NM 2007 6 8 DLM88070660 1 20070531 A 5320 WEB DOUG MD88 MD88 3023688 NM BS 1485 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACK ON WEB AT STA Y=1485 CANT AT 10:00 POSITION NRT0057036 WEB REPAIRED IAW SRM 53-01. 2 L 7 2 4F RT A6WE 2007060800071 20070608 00071 NM 2007 6 8 QXEA200700868 1 20070529 A 2430 400SG1680Q2 GENERATOR BOMBDR DHC8 DHC8402 1390042 NM NR 2 DC INOPERATIVE A QXEA D RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 418QX 9575 783 4143 RNO FLIGHT NR 2440: NR 2 DC GENERATOR WILL NOT COME ON LINE. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE REMOVED AND REPLA CED NR 2 DC GEN IAW MTC 6243101. OPS CHECK GOOD. NO DEFECTS OR LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007060800074 20070608 00074 NM 2007 6 8 DLM88070664 1 20070530 A 5280 ANGLE DOUG MD88 MD88 3023688 NM RT MLG DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACK ON ANGLE AT RT MLG DOOR FWD OUTBD. SECTION CHANNEL TRIMMED IAW SRM 52-05D FIG 811D. EDDY CURRENT INSP FOUND NO C RACKS IAW NDT SPM 06-10-01-001. FABRICATED AND INSTALLED REPAIR IAW SRM 52-05D FIG 811D NR T0057071. 2 L 7 2 4F RT A6WE 2007060800076 20070608 00076 NM 2007 6 8 DLM88070666 1 20070530 A 5320 SUPPORT DOUG MD88 MD88 3023688 NM BS 826 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACK ON STANDARD ELECTRONIC LOWER SUPPORT AT STA Y=826 LT SIDE. HFEC PERFORMED IAW NDT SPM 06-10-01-001. NO CRACKS FO UND. SUPPORT REINSTALLED IAW SRM 51-30-2 NR T0056355. 2 L 7 2 4F RT A6WE 2007060800078 20070608 00078 NM 2007 6 8 DLM88070668 1 20070530 A 5340 SUPPORT DOUG MD88 MD88 3023688 NM RT MLG WW CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACK ON RT HYD REFILL FILTER BRACKET IN RT MLG WW. SUPPORT REPLACED IAW EA 09-076074-03 ME02 OPN 0203 NR T0056109. 2 L 7 2 4F RT A6WE 2007060800079 20070608 00079 2007 6 8 DL757070669 4 20070526 A 2565 LANYARD BOEING 757 757232 1384965 NM ESCAPE SLIDE LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 694DA 0812 29726 FOUND LT OVERWING SLIDE PACK PARTIALLY DEPLOYED DURING ROUTINE DEACTIVATION OF EMEGENCY ESCAPE SYSTEM. LANYARD WAS PULL ED FREE FROM SLIDE PACK. C/W OPN 7809 NR 1L ESCAPE DOOR SLIDE REPLACEMENT REF RC 650-651. 2 L 7 2 4F RT A2NM 2007060800081 20070608 00081 NM 2007 6 8 DLM88070671 1 20070531 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 293-299 L21R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CORRODED LOCK FASTENERS ON FUSELAGE SKIN STA 293-299 LONGERON 21 RT. REPLACED HI-LOCKS IAW SRM 51-30-5 NR T0056012. 2 L 7 2 4F RT A6WE 2007060800082 20070608 00082 NM 2007 6 8 DLM88070673 1 20070531 A 5320 FLOOR SUPPORT DOUG MD88 MD88 3023688 NM BS 864 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACK ON FLOOR SUPPORT AT STA Y=864 X=-1. SUPPORT REPLACED IAW SRM 51-30-2 NRT0056134. 2 L 7 2 4F RT A6WE 2007060800083 20070608 00083 NM 2007 6 8 DLM88070674 1 20070529 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 1400-1426 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CORROSION ON FUSELAGE SKIN STA 1400-1426 LONGERON 2 RT. SKIN REPAIRED IAW SRM 51-30-5 NR T0056167. 2 L 7 2 4F RT A6WE 2007060800084 20070608 00084 NM 2007 6 8 DLM88070675 1 20070529 A 5530 ACCESS PANEL DOUG MD88 MD88 3023688 NM VERTICAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CORROSION ON ACCESS 6301A VERTICAL STAB L/E. REPAIRED IAW SRM 51-30-1, NR T0056168. 2 L 7 2 4F RT A6WE 2007060800085 20070608 00085 NM 2007 6 8 DLM88070676 1 20070528 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 870-879 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CORROSION ON DOUBLER REPAIR STA 870-879 LONGERONS 3-5 RT. REPAIRED IAW SRM 51-30-5 NR T0056174. 2 L 7 2 4F RT A6WE 2007060800087 20070608 00087 NM 2007 6 8 DL76L070677 1 20070605 A 2916 RESERVOIR BOEING 767 767332 1382001 NM HYD SYSTEM OVERSERVICED A DALA D RETURN TO BLOCK W K J INADEQUATE Q C FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 188DN 27583 FLUID LEAK FROM WHEEL WELL AREA ON TAXI OUT. FOUND ADP OIL RESERVOIR OVERFILLED WITH SMELL OF HYD FLUID. 2 L 7 2 4F RT A1NM 2007060800088 20070608 00088 NM 2007 6 8 EIA2007117 1 20070509 A 5410 STRAP BOEING 747 747230B 1384889 NM NR 3 NACELLE GOUGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 487EV 23286 NR 3 PYLON LEFT SIDE AFT ACCESS 473CL FED VERTICAL FRAME, HORIZONTAL STRAP AND ANGLE SUPPORT HAS GOUGE. REMOVED GOUGE A ND INSTALLED REPAIR ON NR 3 PYLON LEFT SIDE AFT ACCESS 473CL FWD VERT FRAME HORIZ STRAP AND ANGLE SUPPORT PER B747 SRM 5 4-11-03 FIG 1. 2 L 7 4 4F A20WE 2007060800089 20070608 00089 NM 2007 6 8 QXEA200700877 1 20070604 A 2130 88060B010002 OUTFLOW VALVE BOMBDR DHC8 DHC8402 1390042 NM CABIN PRESSURE MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION TO TAKEOFF 1 NM 09 426QX 4154 RDM FLIGHT NR 2330: FAULT LIGHT ILLUMINATED ON CABIN PRESSURE CONTROLLER. IT ILLUMINATED AFTER TAKEOFF. ABLE TO CONTRO L CABIN PRESSURE IN MANUAL MODE AS PER EMERGENCY CHECKLIST. MAINTENANCE REMOVED AND REPLACED AFT OUTFLOW VALVE. AIRCRA FT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007060800092 20070608 00092 NM 2007 6 8 DLM88070680 1 20070528 A 5310 SPLICE DOUG MD88 MD88 3023688 NM BS 990 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 FOUND CRACK ON UNION SPLICE AT STA Y=990 X=-6. ANGLE REMOVED, FABRICATED AND INSTALLED IAW DWG 5936395 NR T0056307. 2 L 7 2 4F RT A6WE 2007060800093 20070608 00093 NM 2007 6 8 DLM88070681 1 20070528 A 5310 STRUCTURE DOUG MD88 MD88 3023688 NM BS 1174 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CORROSION AT STA 1174 AND LONGERONS 26 LT T0 24 LT. REPAIRED IAW SRM 51-30-3 NR T0056322. 2 L 7 2 4F RT A6WE 2007060800094 20070608 00094 NM 2007 6 8 DLM88070682 1 20070601 A 5310 STRUCTURE DOUG MD88 MD88 3023688 NM BS 1193 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CORROSION AT STA 1193 AND LONGERON 26 LT. REPAIRED IAW SRM 51-30-5 NR T0056323. 2 L 7 2 4F RT A6WE 2007060800095 20070608 00095 NM 2007 6 8 DLM88070683 1 20070601 A 5340 ATTACH FITTING DOUG MD88 MD88 3023688 NM BS 237 BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 BROKEN INTERCOSTAL ATTACH FITTING AT BS 237 BETWEEN LONGERONS 27 LT AND 28 LT. REPLACED INTERCOSTAL CLIP IAW DWG 991555 4 NR T0056349. 2 L 7 2 4F RT A6WE 2007060800097 20070608 00097 NM 2007 6 8 DLM88070685 1 20070601 A 5347 SEAT TRACK DOUG MD88 MD88 3023688 NM BS 220-226. CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CORROSION ON SEAT TRACK X=44 BETWEEN STA Y=220 TO 226. SEAT TRACK SECTION BETWEEN STA 200 TO 303 REPLACED WITH REPAIR S PLICE AT STA 303 IAW SRM 53-05 FIG 4F VIEW A. 2 L 7 2 4F RT A6WE 2007060800098 20070608 00098 NM 2007 6 8 DLM88070686 1 20070602 A 5310 STRUCTURE DOUG MD88 MD88 3023688 NM BS 1287 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CORROSION AT STA Y=1287, LONGERONS 5-4 RT. REPAIRED IAW SRM 51-30-5 NR T0056451. 2 L 7 2 4F RT A6WE 2007060800099 20070608 00099 NM 2007 6 8 DLM88070687 1 20070603 A 5310 STRUCTURE DOUG MD88 MD88 3023688 NM BS 1271 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CORROSION AT STA Y=1271 LONGERONS 9 RT, 5 RT, 3 RT, 2 RT, 4 LT, AND 5 LT. REPAIRED IAW SRM 51-30-5 NR T0056452. 2 L 7 2 4F RT A6WE 2007060800103 20070608 00103 EU 2007 6 8 07FDEA01867 1 20070521 A 5330 A536102652203 SKIN AIRBUS 310 A310222 3930315 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON RT LWR LATERAL PANEL FS 1212-1236, FR 15-15A. REPAIR REQUIRES EVALUATION FOR MAJOR/MIN OR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT TO BE IN ACCORDANCE WITH SRM 53-12-12 FIG 203. REPAIR CONFORMS TO FEDEX ENGINEERING AUTHORIZATION EA 6-5330-106716. 2 L 7 2 4F RT A35EU 2007060800104 20070608 00104 NM 2007 6 8 QXEA200700875 1 20070603 A 3150 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM ELEVATOR PRESS UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 412QX 4059 SEA FLIGHT NR 2332, AFTER CONTROL CHECK, ELEVATOR PRESS CAUTION LIGHT ILLUMINATED. REMAINED ILLUMINATED. NR 3 PUMP/SYS TEM REMAINED PRESSURIZED. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE C/W FIM TASK 29-30-00-810-801 AND AMM TASK 29-12-00- 720-801. FUNCTIONAL TEST OF NR 3 HYD SYSTEM. OPS CHECK GOOD. NO OTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RE TURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007060800105 20070608 00105 NM 2007 6 8 DL76L070691 1 20070604 A 5312 BULKHEAD BOEING 767 767332 1382001 NM FUSELAGE LEAKING A DALA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED AP APPROACH 1 SO 27 175DN 24803 ON APPROACH, HEARD A LOUD BANG FROM THE TAIL AREA WITH VIBRATIONS IN AIRFRAME AND YOKE. REQUIRED A/P DISCONNECT TO CORR ECT AIRCRAFT PITCH. PERFORMED TESTS MCDP 1 8 9 65 68 69, NO INBOUND FAULTS NO TEST FAULTS 481481. PUMPED UP ELEV FEEL COMP BLED ELEV FEEL LINE PER MM 431329. INSP CABLES AND FOUND EVIDENCE OF WATER LEAK ON CABLES IN AREA OF LT P DOME FEE D THRUS. CLEARED CLOGGED FLOOR DRAINS SEE ITEM 8 AND DISASSEMBLED/CLEAN FEED THRU AI SEALS REF SB 767-27AD192. LEAK AN D OPS CK GOOD 930900. 2 L 7 2 4F RT A1NM 2007060800108 20070608 00108 SO 2007 6 8 C2XA07RI036 1 20070524 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY MALFUNCTIONED A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 27 18982 17560 145223 FLT 2754 - EWR - CREW REPORTED LAV SMOKE MSG ON EICAS, NO SMOKE NOTICED. EWR MX RESET LAV SMOKE DETECTOR IAW EMB 145 AM M 26-14-00. MX PERFORMED OPERATIONAL CHECK - NO MSG ON EICAS. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007060800110 20070608 00110 SO 2007 6 8 C2XA07TY026 1 20070606 A 5740 14569009608 BRACKET EMB 145 EMB145LR 3260212 SO RT WING DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12900 145511 TYS - DURING C-CHECK FOUND RIGHT AILERON PCA ATTACH POINT BRACKET WITH AN ELONGATED BUSHING HOLE. THE BRACKET WAS REMOV ED AND REPLACED IAW EC5750-01177. A/C STILL IN C-CHECK. 2 L 7 2 4T RT T00011AT 2007060800113 20070608 00113 NM 2007 6 8 SWAA072831 1 20070605 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007060800116 20070608 00116 NM 2007 6 8 SWAA072850 1 20070605 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 489WN 33855 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007060800119 20070608 00119 NM 2007 6 8 SWAA072857 1 20070605 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 427-447 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BETWEEN BS 427 AND BS 447, LB L 1. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007060800120 20070608 00120 NM 2007 6 8 SWAA072860 1 20070605 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT FWD UPPER CORNER. REPAIRED SKIN P ER ER. 2 L 7 2 4F RT A16WE 2007060800122 20070608 00122 NM 2007 6 8 SWAA072839 1 20070605 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED HC2 CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD CORNER. REMOVED AND REPLACED F LAP PER MM. 2 L 7 2 4F RT A16WE 2007060800123 20070608 00123 NM 2007 6 8 SWAA072843 1 20070605 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060800124 20070608 00124 NM 2007 6 8 SWAA072849 1 20070605 A 5311 6546547 FRAME BOEING 737 7373H4 1384600 NM BS 580 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 580, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060800126 20070608 00126 SO 2007 6 8 RAIA00705050 1 20070526 A 2741 UNKNOWN EMB 145 EMB145EP 3260221 SO PITCH TRIM UNKNOWN A RAIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CE 03 827HK 145021 FLT NR 5505 - JAX - IMMEDIATELY AFTER TAKEOFF UNABLE TO TRIM CONTROL FORCE FOLLOWED BY PITCH TRIM BACKUP & MAIN INOP EIC AS MESSAGE. MAINTENANCE RESET ALL FOUR PITCH TRIM CIRCUIT BREAKERS AND OPERATIONAL TEST OF SYSTEM CHECKS NORMAL. 2 L 7 2 4F RT T00011AT 2007060800127 20070608 00127 SO 2007 6 8 RAIA00705052 1 20070527 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 811HK 145256 PRE FLT NR 5587 - STL - DOOR EMERGENCY LIGHT INOP. MAINTENANCE DEFERRED PER MEL. 2 L 7 2 4T RT T00011AT 2007060800128 20070608 00128 SO 2007 6 8 C2XA07CL050 1 20070531 A 3350 66903 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13949 145057 CLE FLIGHT 2414 - THE CREW REPORTED THE RIGHT AISLE PATH EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE INSPECTED A ND REPLACED THE EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007060600040 20070606 00040 SO 2007 6 6 LR7A07020 1 20070216 A 5280 HINGE BRACKET LKHEED 382 382G 526414U SO NLG DOOR CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2613 4590 DURING SCHEDULED C-7 CHECK PER JOB CARD HSP32302, FOUND FWD RT NLG DOOR HINGE BRACKET CRACKED AT FS 93, RBL20.5, WL153. REPLACED BRACKET IAW SMP583 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007060600047 20070606 00047 SO 2007 6 6 CHQA200700021 1 20070602 A 2910 AE71379016 HYDRAULIC LINE EMB 145 EMB145LR 3260212 SO HYDRAULIC SYS LEAKING A CHQA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 11 292SK 145488 FLIGHT 7780 - BOS-IAD - IN CLIMB-OUT AROUND 14,000 FEET, RECEIVED E1 HYD PUMP FAIL INDICATION AND SYS 1 HYD LOW QTY INDI CATION. NR 1 ENGINE HYDRAULIC PUMP CAME ON, SYSTEM PRESSURE WAS MAINTAINED AT 2900 PSI, ON HYDRAULIC PAGE INDICATION OF QUANTITY WAS AT BOTTOM OF YELLOW RANGE. SHUT OFF NR 1 ELECTRIC HYDRAULIC PUMP, DECLARED EMERGENCY, LANDED WITHOUT INCI DENT. PRESSURE OF 2900 PSI WAS MAINTAINED DURING ROLLOUT. MAINTENANCE FOUND LEAK FROM HYDRAULIC LINE AND REMOVED AND R EPLACED LINE. 2 L 7 2 4T RT T00011AT 2007060600051 20070606 00051 EA 2007 6 6 A6WA200740121 1 20070308 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 413AW 7585 FS 280 AFT FLOOR SUPPORT ANGLE P/N 600-34017 CRACKED APPROX .3 INCH LONG OUTBOARD OF LBL 9.0. MAINTENANCE REPAIRED CRAC KED FLOOR SUPPORT ANGLE P/N 600-34017 BY CUTTING OUT DAMAGE AND INSTALLING REPAIR ANGLE IAW BOMBARDIER REO 601R-53-11-13 8 REV C. (M) 2 L 7 2 4F RT A21EA 2007060600063 20070606 00063 NM 2007 6 6 SWAA072799 1 20070602 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007060600068 20070606 00068 NM 2007 6 6 SWAA072776 1 20070601 A 3350 767 LAMP BOEING 737 7373Y0 1384671 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007060600069 20070606 00069 2007 6 6 SWAA072783 4 20070601 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007060600070 20070606 00070 2007 6 6 SWAA072784 4 20070601 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007060600075 20070606 00075 NM 2007 6 6 2007UALA01728 1 20070530 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 AFT PIT FRAME SHEAR TIE CRACKED BS 727D BETWEEN STR 21L - 22L. MAJOR REPAIR ACCOMPLISHED: INSTALLED SHEAR TIE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007060600082 20070606 00082 NM 2007 6 6 SWAA072805 1 20070603 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 AFT CABIN EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007060600086 20070606 00086 NM 2007 6 6 SWAA072819 1 20070604 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT CONDITIONED AIR CUTOUT FWD LEFT CORNER BS 514. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007060600092 20070606 00092 NM 2007 6 6 2007UALA01739 1 20070529 A 2611 SMOKE DETECTOR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FWD CARGO BAY FAULTY A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 907UA 25007 CREW REPORT: FWD CARGO DETECTION LIGHT -B- ON AND OFF TWICE IN FLIGHT FOR A FEW SECS THEN OFF. REPLACED "B" LOOP SMOKE DETECTORS, 2 L 7 2 4F 4 F RT A16WE E21EU 2007060600104 20070606 00104 EA 2007 6 6 TRAX200700735 1 20070528 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 904EV 7628 FLIGHT ATTENDANT FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007060600117 20070606 00117 NM 2007 6 6 SWAA072820 1 20070604 A 5753 6546435 FLAP BOEING 737 7375H4 138449D NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED SPV CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007060600120 20070606 00120 NM 2007 6 6 SWAA072827 1 20070604 A 5311 65465417 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663.75, STR 1. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060600122 20070606 00122 NM 2007 6 6 SWAA072824 1 20070604 A 5330 655298871 BEAR STRAP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT FWD GALLEY DOOR CUTOUT AFT LOWER CORNER. REPAIRE D SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007060600124 20070606 00124 NM 2007 6 6 SWAA072814 1 20070604 A 5523 69633917 BOLT BOEING 737 7373H4 1384600 NM LT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED C3 CHECK, LEFT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BOLT PER EA. 2 L 7 2 4F RT A16WE 2007060600126 20070606 00126 NM 2007 6 6 SWAA072825 1 20070604 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED 8Y CHECK, FOUND STRINGER 1 CRACKED BETWEEN BS 661 AND BS 667. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007060600129 20070606 00129 NM 2007 6 6 SWAA072829 1 20070604 A 3397 D40042P CONNECTOR BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 730SW 27862 DURING SCHEDULED 8Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. FOUND LOOSE CONNECTOR, SECURED CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2007060600138 20070606 00138 NM 2007 6 6 SWAA072795 1 20070602 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060600146 20070606 00146 EA 2007 6 6 TRAX200700750 1 20070529 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 850AS 7355 CORROSION ON LOWER SILL OF THE SERVICE DOOR. 2 L 7 2 4F RT A21EA 2007060600161 20070606 00161 EA 2007 6 6 SWIA200718282 1 20070417 A 5343 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 927SW 7693 ENGINE SUPPORT BEAM LOWER WEB HAS CRACK ON CORNER OF LEFT ACCESS PANEL CUT OUT, DISCOVERED AT C-CHECK. INSTALLED FABRIC ATED REPAIR PARTS ON LEFT ENGINE BEAM LOWER WEB IAW CRJ200 REO 601R-53-61-358, REV A. 2 L 7 2 4F RT A21EA 2007060600166 20070606 00166 EA 2007 6 6 SWIA200718287 1 20070417 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 927SW 7693 PAX DOOR AFT DRAG ANGLE IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS ON AFT SIDE OF PAX DOOR PER REO 601R- 52-11-513 REV A. 2 L 7 2 4F RT A21EA 2007060600171 20070606 00171 EA 2007 6 6 SWIA200718292 1 20070416 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 709SK 10159 PAX DOOR FORWARD WEB IS CRACKED AT LOWER ATTACH POINT OF MIDDLE STEP, DISCOVERED AT C-CHECK. REPAIRED AREA IAW REO 670- 52-11-104. 2 L 7 2 4F RT A21EA 2007060600173 20070606 00173 EA 2007 6 6 SWIA200718294 1 20070602 A 3230 UPLOCK CNDAIR CL600 CL6002B19 1900309 EA NLG OUT OF ADJUST A SWIA L ABORTED APPROACH J WARNING INDICATION UK UNKNOWN 1 NM 07 958SW 7833 RECEIVED NOSE GEAR DISAGREE MASTER WARNING. GEAR HAD TO BE EXTENDED MANUALLY PER QRH. FOUND NOSE GEAR UPLOCK PIN AT MI NIMUM CLEARANCES. ADJUSTED UPLOCK PIN IAW MM 32-33-05. 2 L 7 2 4F RT A21EA 2007060600175 20070606 00175 NM 2007 6 6 DU4R20070127 1 20070527 A 5330 SKIN BOEING 757 757232 1384965 NM FUSELAGE DENTED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 640DL 23994 FOUND DENTED STRINGER 15L ON EXTERNAL SKIN AT BS 569. REPAIRED BY CUTTING OUT DENT IAW B757 SRM 53-00-01 SECTION OF FRA ME HFEC CUT OUT EDGES HFEC DENT IAW B757 D634N301, PT 6-51-00-19, NO DEFECTS NOTED. FABRICATED AND INSTALLED DOUBLER 10 .5 BY 9.25 FROM 2024-T3 .063”, FILLER FROM 2024-T3 .071" IAW B757 SRM 53-00-01 FIG 201 AND 51-20-02. 2 L 7 2 4F RT A2NM 2007060600177 20070606 00177 NM 2007 6 6 DU4R20070125 1 20070527 A 5311 FRAME BOEING 757 757232 1384965 NM FUSELAGE DENTED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 640DL 23994 FOUND DENT MAIN FRAME UPPER CAP IN FWD PIT BS 720 AT B/L 0. REPAIRED BY FABRICATING AND INSTALLING DOUBLER 5-5/8 BY 1-7 /8 BY 1 FROM 7075-T6 .063 IAW B757 SRM 51-40-05, 51-40-02 AND 51-20-01. 2 L 7 2 4F RT A2NM 2007060600182 20070606 00182 EA 2007 6 6 SWIA200718300 1 20070601 A 5210 LEVER CNDAIR CL600 CL6002C10 1390015 EA CABIN DOOR OUT OF ADJUST A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 367CA 10069 CABIN DOOR IS HARD TO OPEN FROM THE GROUND. ADJUSTED SWIVEL LEVERS, ADJUSTMENT BOLTS AND STOPS IAW 52-11-17. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007060600185 20070606 00185 EA 2007 6 6 SWIA200718303 1 20070531 A 3350 LENS CNDAIR CL600 CL6002C10 1390015 EA CABIN MISSING A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 767SK 10233 EMERGENCY EXIT LIGHT BY GALLEY DOOR IS MISSING THE LENSE COVER. REPLACED EMERGENCY EXIT LIGHT LENSE COVER. 2 L 7 2 4F RT A21EA 2007060600200 20070606 00200 EA 2007 6 6 TRAX200700730 1 20070527 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 821AS 7194 THE 2ND FROM AFT CEILING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007060600212 20070606 00212 NM 2007 6 6 EIA2007108 1 20070518 A 5313 STRINGER BOEING 747 747230B 1384889 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 487EV 23286 HEAVY EXFOLATION CORROSION STRINGER 46L BS 770 TO BS 790. REMOVED CORROSION, NDTD AREA, FABRICATED AND INSTALLED REPAIR PER ECRA 487-53-050-2. 2 L 7 4 4F A20WE 2007060600214 20070606 00214 NM 2007 6 6 EIA2007098 1 20070506 A 2611 2156646 SMOKE DETECTOR BOEING 747 747273C 1384896 NM CARGO BAY NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 471EV 20651 MAIN DECK CARGO SMOKE DETECTOR, ZONE 2, DET "B" WILL NOT TEST. REPLACED SMOKE DETECTOR, OPS CHECKED GOOD PER MM 26-14-0 1. 2 L 7 4 4F A20WE 2007060600222 20070606 00222 EA 2007 6 6 TRAX200700743 1 20070529 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 OUTER PAX DOOR HANDLE IS CRACKED. [07-24-07] REPAIRED IAW AMM 52-11-03, AMM 52-11-02, AND AMM 52-11-03. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2007060700041 20070607 00041 NM 2007 6 7 HNAA0700094 1 20070528 A 3260 841005 PSEU DHAV DHC8 DHC8102 2809003 NM PWA PW121 PW121 52124 NE MLG UNKNOWN A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 809EX 28778 927 302 AFTER GEAR RETRACTION GOT AN AMBER LEFT GEAR DOOR LIGHT FOLLOWED BY A CLUNKING NOISE AND FLASHING GEAR INOP CAUTION LIGH T. ACFT DIVERTED TO ROA AND SWAPPED WITH ACFT 943/HRH. CREW PERFORMED AN ALTERNATE EXTENSION AND LANDED WITHOUT INCIDE NT. MAINTENANCE SWUNG LANDING GEAR SEVERAL TIMES. CND, REMOVED AND REPLACED PSEU AS A PRECAUTION. OPS CHECK GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2007060700047 20070607 00047 SO 2007 6 7 RAIA00705046 1 20070524 A 3260 85390 PROXIMITY SWITCH EMB 145 EMB145 3260210 SO MLG DAMAGED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 805HK 145096 FLT NR 3521 - RIC - LANDING GEAR AIR GROUND FAIL. MAINTENANCE FOUND NOSE LANDING GEAR WEIGHT ON WHEELS SWITCH TO BE DAM AGED. REMOVED AND REPLACED NOSE LANDING GEAR WEIGHT ON WHEEL SWITCH, OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT T00011AT 2007060700057 20070607 00057 NM 2007 6 7 DHL2007740510 1 20070521 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 580 S28LR CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 CORROSION ON FRAME SHEAR TIE BS 580 BETWEEN STR 28R-28L. FOUND CRACK IN SHEAR TIE IAW B727 SRM 51-10-1. FAB`D NEW SHEA R TIE FROM 7075-0 .071" PO NR 9004690. DIM 2 1/4" BY 5" IAW B727 SRM 53-10-4 FIG 15 AN B727 SRM 53-10-2 FIG 3. HEAT TR EAT PART FROM 7075-0 TO 7075T6 IAW FLIGHTSTAR FORM NR FAS 0115 REV 10 TR-02. AREA AN PART TREATED AN PRIMED IAW B727 SR M 51-10-2. REPAIR INSTALLED IAW B727 SRM 53-10-4 FIG 15. MAJOR REPAIR. PERMANENT REPAIR. 2 L 7 3 4F RT A3WE 2007060700064 20070607 00064 NM 2007 6 7 DLM88070641 1 20070527 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 EXFOLIATION CORROSION ON FUSELAGE SKIN AT FWD JACK POINT. REMOVED CORROSION IAW SRM 51-10-3D. SKIN THICKNESS WITHIN LI MITS REF SRM 53-01 FIG 1 N/R CARD T0056045. 2 L 7 2 4F RT A6WE 2007060800001 20070608 00001 NM 2007 6 8 QXEA200700879 1 20070603 A 7500 8209712 SHUTOFF VALVE BOMBDR DHC8 DHC8402 1390042 NM BLEED AIR MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION TO TAKEOFF 1 NM 09 415QX 9664 9664 4081 PDX FLIGHT 2270: DURING TAKE-OFF ROLL, NR 1 BLEED HOT CAUTION LIGHT ILLUMINATED. AS PER CHECKLIST, TURNED OFF NR 1 BLEE D. LIGHT EXTINGUISHED. MAINTENANCE INSPECTED AND FOUND THAT CDS INDICATED L HPSOV FAULTED. REPLACED L HPSOV IAW Q400 AMM TASK 36-11-09-000-801 AND 36-11-09-400-801. GROUND RAN NR 1 ENGINE. FAULT DID NOT REOCCUR. AIRCRAFT RETURNED TO S ERVICE. 2 H 7 2 4T RT A13NM 2007060800004 20070608 00004 NM 2007 6 8 QXEA200700883 1 20070525 A 5753 SKIN BOMBDR DHC8 DHC8402 1390042 NM TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 C4 PDX - THE LEFT INBOARD FLAP UPPER SURFACE HAS CHAFE INTO THE SKIN 6" FROM THE INBOARD END. REPAIRED IAW SRM 57-51-30 , RD8/4-57-807. 2 H 7 2 4T RT A13NM 2007060800005 20070608 00005 NM 2007 6 8 QXEA200700884 1 20070525 A 5753 SKIN BOMBDR DHC8 DHC8402 1390042 NM TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 C4 PDX - THE LEFT OUTBOARD FLAP UPPER SURFACE IS CHAFED ABOUT 2" FROM THE INBOARD END. REPAIRED IAW SRM 57-52-30, RD8/4 -57-809. 2 H 7 2 4T RT A13NM 2007060800017 20070608 00017 NM 2007 6 8 EIA2007116 1 20070510 A 5321 FLOOR PANEL BOEING 747 747230B 1384889 NM BS 358 GOUGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 487EV 23286 MAIN CABIN FLOOR PANEL GOUGED 2 PLACES BS 358 RBL 6. DAMAGED FLOOR PANEL IS WEB OF NOSE WHEEL WELL BOX TOP PANEL. REMO VED GOUGES, AREA OUT OF LIMITS PER B747 SRM 53-10-01 PAGES 2-6. REPAIRED AREA STATION 340 RBL 6 B747 SRM 53-10-04 FIGUR E 119. 2 L 7 4 4F A20WE 2007060800020 20070608 00020 WP 2007 6 8 DHL2007803505 1 20070526 A 5711 FRAME DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 RT WING CTR L/E LWR FORMER CRACKED 0.250" STA XFS 466.615. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED (2EA) DOUBLER (AL7075T6 0.040") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOU BLER IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 PG 1 (TORQUE). 2 L 7 4 4F RT 4A25 2007060800022 20070608 00022 WP 2007 6 8 DHL2007806521 1 20070402 A 5230 SKIN DOUG DC8 DC873 302199C WP CARGO DOOR MISREPAIRED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 89284 46076 REPAIR ON FWD UPPER JAMB CORNER OF "D" CARGO DOOR IS NOT IN ACCORDANCE WITH DWG SR08530019 (STA 1400.000 - 1420.000 L-25 R TO L-27R) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW AD2005-18-07 S/B DC8 53-078, DOUGLAS DWG NR SR08530019, 5750776. REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW DOUGLAS DWG NR SR085300 19. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK OR CORROSION FOUND AFTER CUT OUT. ENCLOSED SMN FOR M 242-2. FABRICATED FILLER (AL7075T6 0.080") REPAIR DOUBLER (AL7075T6 0.090") REPAIR TRIPLER (AL7075T6 0.125") IAW DOUG LAS DWG NR SR08530019. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SU 2 L 7 4 4F RT 4A25 2007060800027 20070608 00027 WP 2007 6 8 DHL2007803510 1 20070523 A 5330 SKIN DOUG DC8 DC873 302199C WP BS 510 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 UPPER FUSELAGE SKIN CRACKED 0.500" STA 510.000 L-5R TO L-6R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1-3. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER (AL 7075T6 0.090") (2EA) INTERNAL FINGER DOUBLER (AL7075T6 0.050") IAW SRM 53-2-1 FIG 7 SHEET 1, 3, SRM 53-4-1 FIG 13 ITEM " A" SRM 51-9-0 FIG 68A. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SU RFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW SRM 53-2-1 FIG 7 SHEET 1, 3, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 ( TORQUE). THIS IS A CLASS 1 TYPE INSPECTION AND NEEDS AN EXTERNAL VISUAL INSPECTION EACH 4.000FC AS PER SRM 53-2-1 FIG 5 2 L 7 4 4F RT 4A25 2007060800029 20070608 00029 WP 2007 6 8 DHL2007803508 1 20070527 A 5711 FRAME DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 RT WING OUTBD L/E INNER SECTION FORMER CRACKED 0.250", STA XFS 635.000. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED (2EA) ANGLE DOUBLERS AL7075T6 0.032" IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SR M 51-1-8B. INSTALLED NEW ANGLE DOUBLERS IAW SRM 51-1-21 AND SRM 51-1-20D. TORQUED IAW SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007060800034 20070608 00034 WP 2007 6 8 DHL2007803504 1 20070523 A 5753 SKIN DOUG DC8 DC873 302199C WP TE FLAP WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 89394 46123 RT OUTBD FLAP UPPER SKIN WORN STA XF 207.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 4, TR NR 57-94 D ATED 10-01-02. REMOVED DAMAGED PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040") IAW SRM 57-7-1 FIG 4, TR NR 57-94 ITEM "C". CLEANED, TREATED AND PRIMED AREA AND NEW PLATING INNER FACE IAW SRM 51-1-8B. A PPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-11. INSTALLED NEW PLATING IAW SRM 51-1-21, SRM 51-3-0, SRM 51-3-1 (TORQUE ). 2 L 7 4 4F RT 4A25 2007060800045 20070608 00045 NM 2007 6 8 DU4R2007128 1 20070531 A 5311 FRAME BOEING 757 757232 1384965 NM BS 1400 S26-27L DENTED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 602DL 22809 FOUND DENT IN UPPER CAP OF AFT PIT MAIN FRAME BS 1400 BETWEEN S-27 AND S-26 LT. REPAIRED BY FABRICATING AND INSTALLING FRAME REPAIR 9 BY 14 FROM 7075-T6 .071 IAW DELTA ERA 380490-14MA REV ORIG, DELTA PROCESS STANDARD 900-5-1 NR 4, B757 SRM 51-40-02, PG 2, 7, AND 8, 51-70-11, AND 51-20-01 PG 1. PLUGGED EXISTING HOLE IAW B757 SRM 51-40-02 AS DIRECTED BY TIM CO RFTS 291041-60024. 2 L 7 2 4F RT A2NM 2007060800051 20070608 00051 NM 2007 6 8 EIA2007110 1 20070504 A 5511 SPAR BOEING 747 747230B 1384889 NM HORIZONTAL STAB DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 487EV 23286 HOLE NR 2 LEFT SIDE HORIZONAL STAB REAR SPAR CHORD IS REAMED TO .405" STILL SHOWS DEFECT AT LIMIT PER SB747-55A2050. RE MOVED AND REPLACED LT HORIZONAL STAB HINGE FITTING PER B747 SRM 51-30-02 PAGES 8/9, 51-30-05 PAGE 5, 51-10-01 AND 51-30- 04 FIG 1. 2 L 7 4 4F A20WE 2007060800053 20070608 00053 NM 2007 6 8 EIA2007120 1 20070604 A 3350 3004185 LIGHT BOEING 747 747SR46 1384816 NM L-5 DOOR BURNED OUT A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477EV 20784 SELF CONTAINED EMERGENCY EXIT LIGHT AT L-5 INOP. REMOVED AND REPLACED SELF CONTAINTED EMERGENCY LIGHT AT L-5 DOOR LOCAT ION PER B747 MM 33-51-06. OPS CKD GOOD PER B747 MM 33-51-06. 2 L 7 4 4F RT A20WE 2007060800055 20070608 00055 NM 2007 6 8 QXEA200700899 1 20070605 A 5241 DOOR BOMBDR DHC8 DHC8402 1390042 NM GALLEY OBSTRUCTED A QXEA O OTHER C F.O.D. TX TAXI/GRND HDL 1 NM 09 405QX 4047 GEG FLIGHT: AFT GALLEY DOOR ON RT SIDE OF AFT GALLEY DIFFICULT TO OPEN. MAINTENANCE REMOVED OBSTRUCTION AS REQUIRED. D OOR OPERATION NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007060800057 20070608 00057 NM 2007 6 8 DLM88070645 1 20070527 A 5280 ANGLE DOUG MD88 MD88 3023688 NM RT MLG DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 FOUND CRACK ON ANGLE AT R MLG DOOR FWD JAMB. NEW ANGLE FABRICATED AND INSTALLED IAW SRM52-05D FIG 811D. 2 L 7 2 4F RT A6WE 2007060800059 20070608 00059 NM 2007 6 8 DLM88070647 1 20070527 A 5320 SUPPORT DOUG MD88 MD88 3023688 NM BS 525 L24L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACK ON LT SIDE WALL PANEL STRUCTURE AT STA Y=525 AND LONG 24LT. SUPPORT REMOVED, FABRICATED AND INSTALLED IAW SRM 53- 24-0D NR T0056350. 2 L 7 2 4F RT A6WE 2007060800061 20070608 00061 NM 2007 6 8 DLM88070649 1 20070528 A 5310 DOOR FRAME DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 GENERAL SURFACE CORROSION ON C1 LOWER DOOR JAMB. CORROSION REMOVED, SURFACE THICKNESS WITHIN LIMITS. TREATED AND PAINT ED IAW SRM 51-10-3D NR T0056370. 2 L 7 2 4F RT A6WE 2007060800077 20070608 00077 NM 2007 6 8 DLM88070667 1 20070530 A 5320 COVER DOUG MD88 MD88 3023688 NM CREW CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACK ON RT COVER NEXT TO CONNECTION JACK HEAD SET BOOM AND MICROPHONE IN CREW CABIN. REPAIRED DAMAGE IAW MM25-00-00-80 1 NR T0056117. 2 L 7 2 4F RT A6WE 2007060800090 20070608 00090 NM 2007 6 8 DLM88070678 1 20070528 A 5310 DOOR FRAME DOUG MD88 MD88 3023688 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CORROSION ON FED UPPER CORNER OF C2 DOOR JAMB. REPAIRED IAW SRM 51-30-2 NR T0056177. 2 L 7 2 4F RT A6WE 2007060800091 20070608 00091 NM 2007 6 8 DLM88070679 1 20070528 A 5310 STRUCTURE DOUG MD88 MD88 3023688 NM BS 997 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CORROSION ON RT WW AFT EDGE STA Y=997, X=-25. REPAIRED IAW DWG 5962021 NR T0056306. 2 L 7 2 4F RT A6WE 2007060800100 20070608 00100 NM 2007 6 8 DLM88070688 1 20070527 A 5310 STRUCTURE DOUG MD88 MD88 3023688 NM BS 256 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CORROSION AT STA Y=256 LONGERON 2 RT. REPAIRED IAW SRM 51-30-5 NR T0056453. 2 L 7 2 4F RT A6WE 2007060800102 20070608 00102 NM 2007 6 8 DLM88070690 1 20070522 A 5743 5935812 ATTACH FITTING DOUG MD88 MD88 3023688 NM MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 WING MLG ATTACH FTGS, SIDE SUPPORT FITTINGS. CORROSION FOUND IN THE HOLE BORE AND COUNTER BORE. CORROSION WAS REMOVED AND NEW BUSHINGS WERE INSTALLED. 2 L 7 2 4F RT A6WE 2007060800106 20070608 00106 NM 2007 6 8 DHL2007740518 1 20070606 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 990 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AFT CARGO BS 990 BETWEEN STRS 27L AND 30 FWD SIDE OF FRAME HAS CORROSION 3 PLACES. REMOVED CORROSION AT FRAME BS 990 BE TWEEN STR 26L AND 28L ORIG. THICKNESS .063 MAT. LOSS .003 REMAINING .060 WITHIN LIMITS IAW 727 SRM 51-10-6 FIG 1 AND 53- 10-2 FIG 5. REMOVED CORROSION AT FRAME 990 BETWEEN STR 28 AND 30L FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 1. CUT OUT D AMAGED AREA APPROX DIM 5"BY 1.5"IAW SRM 53-10-4 FIG 15. FAB FRAME REPAIR FROM P/N 7075-T6 .071 APPROX DIM 9" BY 5" PO N R 9004940 AND FILLER FROM 7075-T6 .063 APPROX DIM 5" BY 1.25" PO NR 9004690 IAW SRM 53-10-4 FIG 12. TREATED, PRIMED AND REINSTALLED FRAME REPAIR IAW SRM 51-10-2, 53-10-4 FIG 12 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007060800107 20070608 00107 SO 2007 6 8 C2XA07RI038 1 20070510 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 34111 145659 FLT 2130 - OMA - CREW REPORTED EMERGENCY EXIT SIGN OVER 12BC SEAT DOOR INOPERATIVE. EWR MX REMOVED AND REPLACED EMERGEN CY LIGHT INVERTER NR 5 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO FLIGHT. 2 L 7 2 4F RT 2007060800109 20070608 00109 SO 2007 6 8 C2XA07RI041 1 20070508 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14905 145476 IAD - DURING SCHEDULED MAINTENANCE, MX FOUND FWD LOWER EMERGENCY LIGHT OUTSIDE THE COCKPIT INOP. MX REMOVED AND REPLACE D LIGHT BULB AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007060800111 20070608 00111 SO 2007 6 8 C2XA07CL051 1 20070531 A 2530 500064001 COFFEEMAKER EMB 145 EMB145LR 3260212 SO GALLEY FAULTY A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13997 10811 145298 CLE FLIGHT 2519 - THE CREW REPORTED A ELECTRICAL BURNING SMELL WHEN THE COFFEE POTS WERE TURNED ON. MAINTENANCE INSPECT ED AND REPLACED THE NR 2 COFFEE POT. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007060800114 20070608 00114 NM 2007 6 8 SWAA072852 1 20070605 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 757LV 29850 DURING SCHEDULED MV1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 4 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007060800115 20070608 00115 NM 2007 6 8 SWAA072851 1 20070605 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 489WN 33855 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007060800130 20070608 00130 SO 2007 6 8 C2XA07RI037 1 20070524 A 3350 7287580505 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16999 145307 FLT 2951 - EWR - CREW REPORTED FLOOR PROXIMITY EMERGENCY LIGHT STRIP INOP. EWR MX REMOVED AND REPLACED LIGHT STRIP AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007060800135 20070608 00135 NM 2007 6 8 SWAA072861 1 20070603 A 3210 LANDING GEAR BOEING 737 7373H4 1384600 NM UNLOCKED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 356SW 25251 DIVERSION / DECLARED EMERGENCY. AFTER TAKEOFF FROM SMF, GEAR HANDLE WOULD NOT MOVE FROM UP TO OFF POSITION. DIVERTED I NTO OAK. FOLLOWED QRH AND MANUALLY LOWERED GEAR. GEAR CONFIRMED DOWN AND LOCKED BY THREE GREEN LIGHTS, VISUAL THROUGH VIEWER, AND TOWER FLY-BY. UPON LANDING, THE NLG RETRACTED. DISCOVERED RIGHT MLG WAS ALSO UNLOCKED. 2 L 7 2 4F RT A16WE 2007060800136 20070608 00136 NM 2007 6 8 SWAA072862 1 20070606 A 2121 215201 FAN BOEING 737 7373Q8 1384670 NM E&E BAY FAULTY A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 29 317WN 24068 AIR TURNBACK, DURING CLIMB F/A REPORTED STRONG ELECTRICAL/CHEMICAL ODOR IN CABIN. REMOVED AND REPLACED GASPER FAN PER M M. 2 L 7 2 4F RT A16WE 2007060800137 20070608 00137 NM 2007 6 8 SWAA072863 1 20070606 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 510 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007060800142 20070608 00142 WP 2007 6 8 WRLA2007070 1 20070523 A 5340 ANB73921 ANGLE DOUG DC10 DC1030 3023501 WP GE CF6 CF645A2 30020 NE BS 1370 CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 14075 46922 CORROSION FOUND DURING B-CHECK IN LEFT W/W AT FS 1370 BETWEEN TANK AFT PANEL CAP STRUCTURE AND SIDE FORGING AT SPLICE AR EA LBL 115, 38 INCHES BWL. [08-07-07] REMOVED AND REPLACED CORRODED ANGLE, P/N ANB7392-1 IN ACCORDANCE WITH DC-10 SRM VOL.2 51-31-01. 2 L 7 3 4F 4 F A22WE E23EA 2007060800143 20070608 00143 NM 2007 6 8 HNAA0700111 1 20070604 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS PINCHED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 816EX 329 TWO PINCHED WIRES UNDER NR 2 EMERGENCY LIGHT BATTERY PACK. REPAIRED TWO PINCHED WIRES AT NR 2 EMERGENCY LIGHT BATTERY P ACK, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007060800144 20070608 00144 SO 2007 6 8 RAIA00706001 1 20070601 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 821HK 145068 PRE FLT NR 5569 - STL - EMERGENCY LIGHT RIGHTHAND OVERWING EXIT MARKER INOP. MAINTENANCE RESEATED CONNECTOR ON EMERGENC Y LIGHT, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007060800145 20070608 00145 SO 2007 6 8 RAIA00706002 1 20070601 A 3350 RPS1B BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 818HK 4278 145059 PRE FLT NR 5481 - STL - AISLE FLOOD LIGHT INOP AT ROW 16. MAINTENANCE REMOVED AND REPLACED BATTERY POWER SUPPLY CHECK G OOD. 2 L 7 2 4T RT T00011AT 2007060800148 20070608 00148 NE 2007 6 8 HNAA0700104 2 20070601 A 7320 311697503 EEC DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE NR 2 ENGINE MALFUNCTIONED A HNAA B EMER. DESCENT F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 EA 07 914HA 53 120233 NR 2 ENGINE MANUAL LIGHT ILLUMINATED & TORQUE DROPPED BY 50 PERCENT. CREW DECLARED EMERGENCY AND LANDED ON RUNWAY 22 WI THOUT INCIDENT. THE CAPTAIN WAVED OFF THE EMERGENCY EQUIPMENT. ALL PASSENGERS WERE FINE. REMOVED AND REPLACED EEC UNI T. OPS CHECK GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2007060800149 20070608 00149 GL 2007 6 8 C2XA07IA128 2 20070529 A 7200 ENGINE EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL NR 1 SHUTDOWN A C2XA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SW 27 11109 11963 3536 145657 CAE312258 AUS - FLIGHT 2081, THE CREW REPORTED AN UNCOMMANDED NR 1 ENGINE SHUTDOWN IN CRUISE. THE AIRCRAFT DIVERTED TO AUS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS , AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. *SDR FILED OPEN AWAITING DETERMINATION OF CAUSE*. 2 L 7 2 4F 4 F RT TE6CH 2007060800151 20070608 00151 NM 2007 6 8 HNAA0700105 1 20070527 A 3350 6013211 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS DISCHARGED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 825EX 51 51 388 FIRST TWO FORWARD FLOOR EMERGENCY LIGHTS INOPERATIVE. DEBOARDED PASSENGERS SO MAINTENANCE COULD WORK THE PROBLEM. REMO VED AND REPLACED NR 400 EMERGENCY LIGHT POWER SUPPLY AND BATTERY, OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2007060800154 20070608 00154 EA 2007 6 8 VNAA0705004 1 20070515 A 3150 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SPOILERONS UNKNOWN A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 259PS 7945 CREW REPORTED A CAS MISCOMP SPOILERON, RIGHT HAND SPOILER AND INBOARD GROUND SPOILER FAULT MESSAGE ON INITIAL TAKEOFF. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CYCLED THE SECU IN ACCORDANCE WITH THE SERVICE LETTER SL-00-001. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007060800155 20070608 00155 EA 2007 6 8 VNAA0705003 1 20070520 A 2150 35002300003 CHECK VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT A/C PACK DAMAGED A VNAA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 GL 05 261PS 6812 7959 CREW REPORTED RECEIVING A RIGHT HAND PACK OVERHEAT (TEMP) CAUTION MESSAGE WHILE SMELLED SMOKE IN THE CABIN DURING TAXI-I N TO THE GATE. MAINTENANCE INSPECTED AND DEFERRED THE RIGHT HAND PACK PER MEL 21-51-01 -C- OPT 1. MAINTENANCE TROUBLES HOT THE RIGHT HAND PACK SYSTEM. MAINTENANCE REMOVED AND REPLACED THE ACM CHECK VALVE IN ACCORDANCE WITH THE AIRCRAFT MA INTENANCE MANUAL 21-52-07-000/400-801. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007060800156 20070608 00156 NM 2007 6 8 KCSA071182 1 20070605 A 5347 SEAT TRACK BOEING 747 747221F 1384868 NM BS 1770-1815 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 MAIN DECK SEAT TRACK IS CORRODED AT LBL 11 FROM STA 1770 TO 1815. 2 L 7 4 4F A20WE 2007060800157 20070608 00157 NM 2007 6 8 KCSA071183 1 20070605 A 5347 SEAT TRACK BOEING 747 747221F 1384868 NM BS 390-402 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 MAIN DECK SEAT TRACK IS CORRODED AT O/B FLANGE RBL 83 FROM STA 390 TO 402. 2 L 7 4 4F A20WE 2007060800158 20070608 00158 NM 2007 6 8 KCSA071184 1 20070605 A 5347 SEAT TRACK BOEING 747 747221F 1384868 NM BS 1152 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 MAIN DECK SEAT TRACK IS CORRODED AT LBL 74 STA 1152. 2 L 7 4 4F A20WE 2007060800161 20070608 00161 NM 2007 6 8 SWAA072845 1 20070605 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM BS 747 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060800165 20070608 00165 NM 2007 6 8 SWAA072840 1 20070605 A 5311 6546595 FRAME BOEING 737 7373H4 1384600 NM BS 727A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060800166 20070608 00166 NM 2007 6 8 SWAA072844 1 20070605 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM BS 727B S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060800169 20070608 00169 NM 2007 6 8 KCSA071185 1 20070606 A 5315 FLOORBEAM BOEING 747 747221F 1384868 NM BS 1920 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 STA 1920 RBL 60 EVIDENCE OF CORROSION ON FUSELAGE DOOR LOCK BEAM WEB. 2 L 7 4 4F A20WE 2007060800171 20070608 00171 WP 2007 6 8 WRLA2007072 1 20070529 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE BS 1461 CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 14075 46922 DURING B-CHECK INSPECTION, CORROSION FOUND ON LOWER END OF LONGERON IN CENTER GEAR W/W RIGHT SIDE AT FS 1461. REMOVED C ORRODED LONGERON FROM CENTER GEAR WHEEL WELL. FABRICATED A REPLACEMENT LONGERON FROM 7075-T6 511 AND INSTALLED IAW DC-1 0 SRM 51-38-01 PG 17. 2 L 7 3 4F 4 F A22WE E23EA 2007060800172 20070608 00172 WP 2007 6 8 WRLA2007073 1 20070527 A 5320 STIFFENER DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE BS 1442 CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 14075 46922 DURING B-CHECK INSPECTION, CORROSION FOUND ON LOWER AFT CORNER OF SUPPORT STRAP IN CENTER W/W RIGHT SIDE ABOVE AFT HINGE ON FWD GEAR DOOR AT FS 1442. REMOVED, FABRICATED, AND INSTALLED TEE STIFFENER IAW DC10 SRM VOL II 51-31-01 & 51-33-01. 2 L 7 3 4F 4 F A22WE E23EA 2007060800175 20070608 00175 NM 2007 6 8 KCSA071167 1 20070530 A 5315 FLOORBEAM BOEING 747 747221F 1384868 NM BS 460 PUNCTURED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 UPPER DECK FLOORBEAM WEB IS PUNCTURED AT STA 460 RBL 46 JUST BELOW UPPER CHORD. 2 L 7 4 4F A20WE 2007060800177 20070608 00177 NM 2007 6 8 KCSA071169 1 20070530 A 5315 FLOORBEAM BOEING 747 747221F 1384868 NM BS 800 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 STA 800 LBL 97.5 FLOORBEAM UPPER CAP FWD FLANGE LOWER SURFACE CORRODED AT FASTENER LOCATION. 2 L 7 4 4F A20WE 2007060800178 20070608 00178 NM 2007 6 8 KCSA071170 1 20070530 A 5320 STIFFENER BOEING 747 747221F 1384868 NM BS 2008 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 BULK CARGO DOOR LONGITUDINAL STIFFENER CORROSION STA 2008. 2 L 7 4 4F A20WE 2007060800179 20070608 00179 NM 2007 6 8 KCSA071171 1 20070530 A 5311 FRAME BOEING 747 747221F 1384868 NM BS 1820 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 AFT BILGE FUSELAGE FRAME UPPER CHORD IS CRACKED AT STA 1820 AT RBL 48 1 INCH. 2 L 7 4 4F A20WE 2007060800181 20070608 00181 SO 2007 6 8 RAIA00705053 1 20070528 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 833HK 145240 POST FLT NR 7961 - IAD - EMERGENCY LIGHT AISLE FLOOD LIGHTS AFT INOP. MAINTENANCE REMOVED AND REPLACED BULBS SYSTEM, OP S CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007060800183 20070608 00183 2007 6 8 RAIA00705055 4 20070529 A 3421 HG2010AC02 AHRS EMB 145 EMB145LR 3260212 SO NR 1 INOPERATIVE A RAIA D RETURN TO BLOCK I FLT. ATTITUDE INST. TX TAXI/GRND HDL 1 CE 03 815HK 14874 145048 FLT NR 5576 - RDU - CAPTAIN`S AHRS FAIL. MAINTENANCE REMOVED AND REPLACED NR 1 AHRS, PERFORMED OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007060800184 20070608 00184 NM 2007 6 8 HNAA0700096 1 20070508 A 5240 85321086059 ACCESS PANEL DHAV DHC8 DHC8102 2809003 NM LAVATORY CORRODED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 938HA 152 HINGE OF LAV SERVICE PANEL, HEAVY CORROSION. CORROSION ON HINGE OF LAV SERVICE PANEL REMOVED AND REPROTECTED IAW SRM 51 -20-11 (0.002") AND LAVATORY SERVICE PANEL REPLACED AND INSTALLED WITH RIVET IAW SRM 51-40-00. 2 H 7 2 4T RT A13NM 2007060800185 20070608 00185 NM 2007 6 8 CALA0700273 1 20070530 A 3397 UNK WIRE BOEING 757 757224 1384958 NM EMERGENCY LIGHT CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14121 27563 THE EMERGENCY SEAT LIGHTS FROM ROW 7-14 WOULD NOT TEST. MAINTENANCE REPAIRED CHAFED WIRES THAT WERE FOUND ON MID HEADER EXIT SIGN IAW SWP 20-10-13. 2 L 7 2 4F RT A2NM 2007060800186 20070608 00186 NM 2007 6 8 CALA0700274 1 20070529 A 2612 285N0028136 CIRCUIT CARD BOEING 757 757324 1384930 NM CARGO FIRE INOPERATIVE A CALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 27 57857 11541 32816 THE FORWARD CARGO FIRE LIGHT ILLUMINATED WITHOUT EICAS MESSAGE OR WARNING BELL WHILE LEVELING OFF AT 33,000 FEET AFTER D EPARTING LAX. BOTH FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT WAS RETURNED TO LAX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE CARGO BIN AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT. THE M10427 AUTO FIRE/OVERHEAT TEST PRIN TED CIRCUIT CARD FOR CARGO FIRE DETECTION WAS REMOVED AND REPLACED. OPERATIONAL CHECKS WERE GOOD. IN ADDITION, BOTH CA RGO FIRE BOTTLES WERE REMOVED AND REPLACED IAW MM 26-23-02-408, ITEM 4 THROUGH G11. 2 L 7 2 4F RT A2NM 2007060800187 20070608 00187 NM 2007 6 8 HNAA0700098 1 20070602 A 3350 2020 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS DISCHARGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 845 344 SEVERAL FLOOR LEVEL EMERGENCY LIGHTS ARE INOP. CALLED PHL LINE MAINT FOR HELP. REMOVED AND REPLACED EMERGENCY BATTERY PACK PS4, OPS CHECK GOOD IAW 33-52-00. 2 H 7 2 4T RT A13NM 2007060800188 20070608 00188 NM 2007 6 8 KCSA071175 1 20070604 A 5711 SPAR BOEING 747 747221F 1384868 NM RT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 RIGHT WING FRONT SPAR LOWER CHORD STRAP CORRODED AT FSSO 1520. 2 L 7 4 4F A20WE 2007060800189 20070608 00189 NE 2007 6 8 AMTA200700195 2 20070417 A 7200 ENGINE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LEFT FAILED A AMTA C ABORTED TAKEOFF Y J ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 GL 11 519AT 27975 31611 LT ENGINE FAILED ON TAKEOFF VOICE RECORDER C/B PULLED (LT ENG LP PUMP) EICAS DISPLAYED. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007060800192 20070608 00192 NM 2007 6 8 KCSA071177 1 20070604 A 5313 STRINGER BOEING 747 747221F 1384868 NM BS 2160-2180 BENT A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 FUSELAGE STR 47L IS BENT BETWEEN BS 2160 AND 2180. 2 L 7 4 4F A20WE 2007060800193 20070608 00193 NM 2007 6 8 KCSA071178 1 20070604 A 5313 STRINGER BOEING 747 747221F 1384868 NM BS 2160-2180 BENT A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 FUSELAGE STR 49L HAS A BENT FLANGE BETWEEN BS 2160 AND 2180. 2 L 7 4 4F A20WE 2007060800194 20070608 00194 NM 2007 6 8 KCSA071179 1 20070604 A 5313 STRINGER BOEING 747 747221F 1384868 NM 2160-2180 BENT A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 FUSELAGE STR 48L HAS A BENT FLANGE BETWEEN BS 2160 AND 2180. 2 L 7 4 4F A20WE 2007061100001 20070611 00001 NM 2007 6 11 USAA070417 1 20070604 A 5330 SKIN BOEING 737 7374B7 1384702 NM BS 847 S27R CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 444US 24862 BS 847, S27R HAS CORROSION. FUSELAGE SKIN BULGING DUE TO CORROSION. REMOVED DAMAGE, INSTALLED REPAIR DOUBLER & ANGLE P ER EA 986778, SRM 53-00-07; CORR TASK C53-100-01, DEFECT SIZE: 4 X 5 INCHES. 2 L 7 2 4F RT A16WE 2007061100002 20070611 00002 NM 2007 6 11 SB07044 1 20070529 A 3350 20131ASMI BATTERY PACK BOEING 737 737401 1384701 NM EMERGENCY LIGHTS DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 CLT - MAINTENANCE FOUND THE FORWARD BATTERY FOR EMERGENCY LIGHTS WOULD NOT HOLD A CHARGE. MAINTENANCE REMOVED AND REPLA CED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007061100003 20070611 00003 NM 2007 6 11 USAA070431 1 20070605 A 5310 6545807U6 DOOR FRAME BOEING 737 737401 1384701 NM BS 296 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 BS 296.5, FWD UPPER CORNER FRAME OF RIGHT FWD SERVICE DOOR CUTOUT AT DOOR STOP FITTING HAS CRACK. REMOVED CRACKED FRAME & INSTALLED NEW PER SRM 51-10-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007061100004 20070611 00004 NM 2007 6 11 USAA070430 1 20070605 A 5512 SKIN BOEING 737 737401 1384701 NM HORIZONTAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 LEFT HORIZONTAL STAB L/E, 6TH SCREW HOLE FROM INBOARD END ON BOTTOM ROW HAS CRACK. REPAIRED BY INSTALLING FREEZE PLUG P ER SRM 55-10-01 & EA 98671, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007061100005 20070611 00005 NM 2007 6 11 USAA070429 1 20070605 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 360 S8L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 BS 360 AT S-8L HAS CRACK. INSTALLED REPLACEMENT ANGLE PER SRM 51-10-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007061100006 20070611 00006 NM 2007 6 11 USAA070428 1 20070605 A 5310 DOOR FRAME BOEING 737 737401 1384701 NM BS 296 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 BS 296.5; FWD UPPER CORNER FRAME OF RIGHT FWD SERVICE DOOR CUTOUT HAS CRACK. DEFECTIVE PART REPLACED WITH IDENTICAL PAR T PER SRM 51-10-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007061100007 20070611 00007 NM 2007 6 11 USAA070427 1 20070605 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 294 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 STA 294 ADJACENT TO S8L, MED STUB BEAM TURN UP ANGLE HAS CRACK. FABRICATED NEW WEB & INSTALLED PER SRM 51-10-02, DEFECT SIZE: 0.5 INCH. 2 L 7 2 4F RT A16WE 2007061100008 20070611 00008 NM 2007 6 11 USAA070426 1 20070605 A 5320 FLOOR SUPPORT BOEING 737 737401 1384701 NM BS 390-394 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 BS 390-394, BL 0, FLOORBOARD SUPPORT ANGLE AT TOP OF WEB AT 2 FASTENER HOLE HAS CRACK. REMOVED CRACKED ANGLE & INSTALLE D NEW PER SRM 51-10-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007061100009 20070611 00009 NM 2007 6 11 USAA070425 1 20070605 A 5720 FLANGE BOEING 737 737401 1384701 NM LWS 135 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 CRACK AT WBL 135.5 AT LEFT WING, LOWER CHORD FLANGE HAS CRACK. INSTALLED DOUBLER PER EA 98655, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007061100010 20070611 00010 NM 2007 6 11 USAA070424 1 20070605 A 5311 FRAME BOEING 737 737401 1384701 NM BS 747 S8-9L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 STA 747 BETWEEN STRINGERS 8 & 9 LEFT HAS CRACK. REMOVED DAMAGED AREA & INSTALLED REPAIR PARTS PER TR 53-10-22A, 53-10-2 0E, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007061100011 20070611 00011 NM 2007 6 11 USAA070423 1 20070605 A 5311 FRAME BOEING 737 737401 1384701 NM BS 727D S8-9 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 STA 727D BETWEEN STRINGERS 8 & 9 ON FRAME HAS CRACK. REMOVED DAMAGED AREA & INSTALLED REPAIR PARTS PER SRM 53-10-20E, S TEP 9, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007061100012 20070611 00012 2007 6 11 SA07034 4 20070606 A 2565 60592101 BOTTLE AIRBUS 320 A320214 3930316 EU ESCAPE SLIDE READS LOW A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 106US 19614 7334 1044 DCA - THE RIGHT HAND OVERWING EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE WAS FOUND LOW DURING INSPECTION. MAINTENANCE ACCOM PLISHED REPLACEMENT OF THE RIGHT HAND OVERWING SLIDE BOTTLE CYLINDER ASSEMBLY. INSPECTED, OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2007061100013 20070611 00013 NM 2007 6 11 USAA070445 1 20070606 A 5311 FRAME BOEING 737 737401 1384701 NM 360 S13L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 STA 360, S13L HAS CRACK. INSTALLED REPAIR ANGLE PER SRM 51-10-02, 51-40-02, DEFECT SIZE: .125 INCH. 2 L 7 2 4F RT A16WE 2007061100014 20070611 00014 NM 2007 6 11 USAA070444 1 20070606 A 5311 FRAME BOEING 737 737401 1384701 NM BS 440 S8-9R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 STA 440R BETWEEN S8R & S9R AC SUPPORT BRACKET ATTACH POINT HAS CRACK. REPAIRED PER T/R 53-10-20E, DEFECT SIZE: .125 IN CH. 2 L 7 2 4F RT A16WE 2007061100015 20070611 00015 NM 2007 6 11 USAA070443 1 20070606 A 5315 65C327558 FLOORBEAM BOEING 737 737401 1384701 NM BS 578 RBL 64 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 STA 578, RBL 64 JUST BELOW CABIN FLOOR LEVEL NEAR S-18R HAS CRACK. REMOVED & REPLACED FLOOR SUPPORT PER SRM 51-10-02, B OEING DWG 6AA5C32755, DEFECT SIZE: 0.5 INCH. 2 L 7 2 4F RT A16WE 2007061100016 20070611 00016 NM 2007 6 11 USAA070442 1 20070606 A 5330 SKIN BOEING 737 737401 1384701 NM BS 880 S1L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 CRACK & DEEP CHAFED AREA FOUND AFT OF CRACK AT BS 880.60, S1L, LT DORSAL. REMOVED DAMAGED AREA & INSTALLED DOUBLER & TR IPLER PER SRM 53-60-01, DEFECT SIZE: 2 INCH CRACK, 12 X 1 INCH CHAFED. 2 L 7 2 4F RT A16WE 2007061100017 20070611 00017 NM 2007 6 11 USAA070441 1 20070606 A 5311 FRAME BOEING 737 737401 1384701 NM BS 867 S8-9R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 BS 867, BETWEEN S-8R AND S-9R HAS CRACKS. CUT OUT CRACKS, INSTALLED REPAIR ANGLES PER TR 53-10-20E, DEFECT SIZE: .5 IN CH. 2 L 7 2 4F RT A16WE 2007061100018 20070611 00018 NM 2007 6 11 USAA070440 1 20070606 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 294 S12L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 MED STUB BEAM TURN DOWN ANGLE, STA 294, ADJACENT TO S12L HAS CRACK. REMOVED DAMAGED PART & INSTALLED NEW PER SRM 51-10- 02, BOEING DWG 65-17684, DEFECT SIZE: 0.5 INCH. 2 L 7 2 4F RT A16WE 2007061100019 20070611 00019 NM 2007 6 11 USAA070439 1 20070606 A 5320 GUSSET BOEING 737 737401 1384701 NM BS 259 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 UPPER RADIUS, STA 259.5, BL 0 HAS CRACK. REMOVED DAMAGED GUSSET & REPLACED WITH NEW PER SRM 53-1-14, FIG 101, DEFECT SI ZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007061100020 20070611 00020 NM 2007 6 11 USAA070438 1 20070606 A 5511 RIB BOEING 737 737401 1384701 NM HORIZONTAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 NR 7 RIB OF LEADING EDGE ON LEFT HORIZONTAL STAB, CRACK & FASTENER PULLED. REMOVED AND REPLACED RIB PER SRM 51-40-00, D EFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007061100021 20070611 00021 NM 2007 6 11 USAA070437 1 20070606 A 5330 SKIN BOEING 737 737401 1384701 NM BS 880 S1L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 CHAFE AREA FWD & AFT OF CRACK, BS 880.60, S1L, LEFT DOSAL FIN SEAT AREA. REMOVED DAMAGED AREA & INSTALLED DOUBLER & TRI PLER, DEFECT SIZE: 2 INCH CRACK AND 12 X 1 INCH CHAFE. 2 L 7 2 4F RT A16WE 2007061100022 20070611 00022 NM 2007 6 11 USAA070436 1 20070606 A 5313 STRINGER BOEING 737 737401 1384701 NM BS 907 S4L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 STA 907, S4L, STRINGER SPLICE HAS CRACK. REMOVED DAMAGED PART, INSTALLED NEW SPLICE PART PER SRM 53-40-02, DEFECT SIZE: .250 INCH. 2 L 7 2 4F RT A16WE 2007061100023 20070611 00023 NM 2007 6 11 USAA070435 1 20070606 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 291-294 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 INNER CHORD ANGLE, RT SIDE BETWEEN STA 291.5 & 294, STR 17 HAS CRACK. REMOVED & REPLACED ANGLE PER SRM 51-10-02, DEFECT SIZE: 2.5 INCH. 2 L 7 2 4F RT A16WE 2007061100024 20070611 00024 NM 2007 6 11 USAA070434 1 20070606 A 5310 DOOR FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 FWD SERVICE DOOR CUTOUT FWD FRAME LOWER STRINGER 17 HAS CRACK. INSTALLED FILLER AND REPAIR ANGLE PER SRM 51-70-11, DEFE CT SIZE: 3 INCHES. 2 L 7 2 4F RT A16WE 2007061100025 20070611 00025 EU 2007 6 11 SA07033 1 20070605 A 3350 321431 BATTERY PACK AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHTS DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 722US 1097 DCA - THE LEFT HAND, MID-CABIN EMERGENCY EXIT LIGHT BATTERY INDICATED A LOW CHARGE. MAINTENANCE REPLACED THE LEFT HAND, MID-CABIN EMERGENCY EXIT LIGHT BATTERY. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007061100026 20070611 00026 NM 2007 6 11 SWAA072706 1 20070528 A 3350 8200036101 LIGHT BOEING 737 73776Q 13845AA NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 550WN 30279 DURING SCHEDULED BRDG CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007061100027 20070611 00027 NM 2007 6 11 SWAA072705 1 20070528 A 3350 8200036101 LIGHT BOEING 737 73776Q 13845AA NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 550WN 30279 DURING SCHEDULED BRDG CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007061100065 20070611 00065 EU 2007 6 11 07FDEA02060 1 20070604 A 5330 A53777053 SKIN AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 TOOLING MARK AT C 33, P22-23 RT REPAIR PERFORMED BY REMOVAL OF TOOLING MARK IAW EA 6-5314-101248 AND RAS/DABRE/7006470/2 006 ISS.A. 2 L 7 2 4F RT A35EU 2007061100066 20070611 00066 EU 2007 6 11 07FDEA02061 1 20070604 A 5730 A57350101 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 RT WING TOP SKIN PANEL NR 2, TRAILING EDGE AREA CORRODED, RIB 26-31 REPAIR PERFORMED BY BLEND OUT IAW EA 6-5720-101256 A ND RAS/BAE/1002866/2006 ISS. A 2 L 7 2 4F RT A35EU 2007061100067 20070611 00067 EU 2007 6 11 07FDEA02062 1 20070604 A 5330 A53998066 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 DENT ON SKIN BETWEEN C74-75, P46-47 LT HFEC INSPECTION PERFORMED, ROTOTEST PERFORMED AROUND 6 FASTENER HOLES IN THIS ARE A, NO FURTHER DAMAGES FOUND. DENT STAY AS IT IS IAW EA 6-5318-101329 AND RAS/DATLS/0003251/2006 ISS. A 2 L 7 2 4F RT A35EU 2007061100068 20070611 00068 EU 2007 6 11 07FDEA02073 1 20070604 A 5310 FRAME AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND FRAME CORRODED. COMPLY WITH EA 6-5310-110742 FUSELAGE MAINFRAME FR 63 RIGHT CORROSION REPAIR COMPLIED WITH EA 6-5 310-110742 FUSELAGE, MAINFRAME, FR 63 RIGHT CORROSION REPAIR AND SPLICE AT STR NR 39. 2 L 7 2 4F RT A35EU 2007061100069 20070611 00069 EU 2007 6 11 07FDEA02074 1 20070604 A 5553 ATTACH FITTING AIRBUS 310 A310203 3930313 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 VERT STAB REAR SPAR RT UPPER MOST HINGE ATTACH FITTING HAS CORROSION. REMOVED HINGE FITTING IAW SRM 51-40-21. LOCATED AND DRILLED NEW FITTING IAW SRM 51-40-44. INSTALLED NEW FITTING IAW SRM 51-40-21. INSTALLED NEW STRINGER CLIPS 1 AND 2 AT RIB25 IAW N/R S00021 AND EA 6-5530-110749. 2 L 7 2 4F RT A35EU 2007061100070 20070611 00070 EU 2007 6 11 07FDEA02075 1 20070604 A 5553 ATTACH FITTING AIRBUS 310 A310203 3930313 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 VERT STAB REAR SPAR RT UPPER MOST HINGE ATTACH FITTING HAS CORROSION. REMOVED HINGE FITTING IAW SRM 51-40-21. LOCATED AND DRILLED NEW FITTING IAW SRM 51-40- 44. INSTALLED NEW FITTING IAW SRM 51-40-21. INSTALLED NEW STRINGER CLIPS 1/2 AT RIB 25 IAW N/R S00021 AND EA 6-5530-110749. 2 L 7 2 4F RT A35EU 2007061100071 20070611 00071 WP 2007 6 11 070120 1 20070517 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 875GA 53468 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENC Y EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BA TTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007060600140 20070606 00140 NM 2007 6 6 SWAA072796 1 20070602 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060600141 20070606 00141 NM 2007 6 6 SWAA072797 1 20070602 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060600150 20070606 00150 EA 2007 6 6 TRAX200700754 1 20070530 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 850AS 7355 CORROSION ON FRAME AT FS 310 BETWEEN STR 26L TO 26R. 2 L 7 2 4F RT A21EA 2007060600152 20070606 00152 EA 2007 6 6 TRAX200700756 1 20070530 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 850AS 7355 CORROSION ON FRAME AT FS 319 BETWEEN STR 26L TO 25R. 2 L 7 2 4F RT A21EA 2007060600158 20070606 00158 SO 2007 6 6 200715004 1 20070529 A 2720 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO RUDDER SYS MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 928AE 14500911 APORTED TAKEOFF RUDDER SYSTEM 1 INOP MESSAGE. PERFORMED OPERATIONAL CHECKS OF THE RUDDER SYSTEM IAW EMB MM. OPERATIONA L CHECKS GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007060600189 20070606 00189 EA 2007 6 6 TRAX200700759 1 20070530 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 850AS 7355 LEFT SILL AS MANY SPOTS OF CORROSION BETWEEN FS 409.00 AND + 128 TO FS 559.00 BL 26 TO BL 47. 2 L 7 2 4F RT A21EA 2007060600198 20070606 00198 EA 2007 6 6 TRAX200700768 1 20070531 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 LEFT SIDE FS 640 BONDED SKIN DOUBLER IS CRACKED. [07-24-07] WORK COMPLETED IN ACCORDANCE WITH REO 601R-53-61-506. 2 L 7 2 4F RT A21EA 2007060600205 20070606 00205 NM 2007 6 6 EIA2007113 1 20070506 A 5512 SKIN BOEING 747 747230B 1384889 NM HORIZ STAB DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 487EV 23286 LEFT HORIZONTAL STABILIZER STATION 210 UPPER SIDE OF THE WEB STIFFENER AT LEFT ACCESS CUT-OUT HAS TOOLING MARKS 2 EA. I NSTALLED REPAIR PLATE, FILLER AND 2 EACH WEB STIFFENERS AT LEFT HORIZONTAL STABILIZER STATION 210 PER B747 SRM 55-10-06 PAGES 8-9 AND 51-30-02 PAGE 8-9. 2 L 7 4 4F A20WE 2007060600216 20070606 00216 NM 2007 6 6 EIA2007109 1 20070504 A 5313 STRINGER BOEING 747 747230B 1384889 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 487EV 23286 FUSELAGE INTERIOR FRAME TO FRAME ANGLE STATION 960 STRINGER 15L HAS MISDRILLED FASTENER HOLES. DAMAGE REMOVED, NDT AREA , FABRICATED AND INSTALLED REPAIR PER ECRA 4887-53-044-2. 2 L 7 4 4F A20WE 2007060700004 20070607 00004 2007 6 7 AMTA200700240 4 20070515 A 2310 9640452012 TRANSCEIVER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE HF SYSTEM UNSERVICEABLE A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 522AT 29330 HF TRANSMISSION AND RECEPTION (INOPERATIVE) AT ALL CREW STATIONS. REPLACED RT HF TRANSCEIVER IAW MM 23-11-03. OPS CHEC K NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007060700005 20070607 00005 2007 6 7 AMTA200700236 4 20070516 A 2565 SLIDE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2B 30018 NE L3 DOOR NO TEST A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 701TZ L-3 DOOR SLIDE FAILED TO DEPLOY ON TEST (AUTO AND MANUAL). REINSTALLED SLIDE SN CC213 FOR EVACUATION TEST IAW AMM-25-61 -01. (K) 2 L 7 3 4F 4 F A22WE E23EA 2007060700010 20070607 00010 NM 2007 6 7 AMTA200700220 1 20070504 A 5310 CREASE BEAM BOEING 737 73783N 13844HI NM BS 727-844 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 304TZ 30675 B/S 727I+8 THRU 844, LBL 22, CORROSION EXISTS AS MARKED 34 SPORTS ON CREASE ANGLE IN AFT PIT. REMOVED 31 NUT PLATES BLE NDED AREA ORIG MTL .040, MTL LOSS .001 TO .003. FOUND WITHIN LIMITS SRM 53-00-53, SRM 53-00-53, DEPTH GAUGE TREATED 51- 20-01. INSTALLED NUT PLATED 51-40-02. (K) 2 L 7 2 4F RT A16WE 2007060700013 20070607 00013 NM 2007 6 7 AMTA200700225 1 20070504 A 5551 PIN BOEING 737 73783N 13844HI NM HORIZONTAL STAB CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 304TZ 30675 LT HORIZ STAB FAIL SAFE PIN PITTED, PN 180A1612-2. REMOVED AND REPLACED PIN (180A1612-4, AMM 27-41-11-4). (K) 2 L 7 2 4F RT A16WE 2007060700039 20070607 00039 WP 2007 6 7 WRLA2007075 1 20070530 A 5320 SUPPORT FITTING DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE CORRODED CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 14075 46922 DURING B-CHECK INSPECTION, CORROSION FOUND ON DIAMETER SUPPORT FITTING TIE BRACE ON LOWER INNER SURFACE IN CENTER LANDIN G GEAR WHEEL WELL RIGHT SIDE FS 1461. REPLACED SPLICE ANGLES AT FS 1461 PER SRM 51-33-01, SRM 53-14-01, SRM 53-00-01, S RM 51-21-01, SRM 51-31-01 AND DPS4 710-3 REV AJ PAGE 5. 2 L 7 3 4F 4 F A22WE E23EA 2007060700042 20070607 00042 NM 2007 6 7 HNAA0700109 1 20070514 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 530 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 937HA 148 STA 530 FROM I/B SEAT RAIL TO O/B SEAT RAIL WEB UNDER FLOOR SHOWS SIGNS OF CORROSION AND FASTENERS CORRODED. REMOVED CO RRODED FASTENERS, REMOVED LIGHT CORROSION, ALODINE AND PRIMED IAW 51-20-11, SRM 51-20-16, REINSTALLED FASTENERS. 2 H 7 2 4T RT A13NM 2007060700045 20070607 00045 EU 2007 6 7 MAC050701 1 20070518 A 7603 POWER LEVER AEROSP ATR42 ATR42300 8680920 EU NR 2 LACK OF LUBE A MTNA O OTHER W INADEQUATE Q C CR CRUISE 1 SO 33 918FX 262 IN CRUISE FLIGHT AT FL220 THE NR 2 POWER LEVER APPEARED TO BE FROZEN AT ITS POWER SETTING. AFTER DESCENT TO 12,000 FT T HE NR 2 POWER LEVER BECAME FREE AND THE POWER COULD THEN BE CHANGED. SERVICE BULLETIN ATR42-76-0009 HAD PREVIOUSLY BEEN ACCOMPLISHED. PANELS WERE REMOVED TO GAIN ACCESS, THE FLEXIBLE CONTROLS WERE LUBED AND THE REMOVED PANELS WERE RESEALE D. OPERATIONAL CHECKS WERE ACCOMPLISHED WITH NO DISCREPANCIES FOUND. THE A/C WAS RETURNED TO SERVICE WITH NO FURTHER D ISCREPANCIES TO THE NR 2 ENGINE CONTROLS. 2 H 7 2 4T RT A53EU 2007060700046 20070607 00046 NM 2007 6 7 HNAA0700106 1 20070602 A 7931 APT761000100D TRANSMITTER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE OIL PRESSURE MALFUNCTIONED A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 838EX 220 121186 NR 1 OIL PRESS READS BETWEEN 75 & 100 PSI IN FLIGHT. CONTACT ROA MAINT THE FLIGHT RETURNED TO THE FIELD IN ROA. NO EME RGENCY WAS DECLARED AND IT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ENG OIL PRESS TRANSMITTER. OPS & LEAK CHECK G OOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2007060700048 20070607 00048 SO 2007 6 7 RAIA00705047 1 20070524 A 3397 WIRE EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 808HK 145157 PRE FLT NR 5587 - STL - EMERGENCY LIGHT FLOOR PROXIMITY LIGHT INOP. MAINTENANCE REPAIRED BROKEN WIRE TO CONNECTOR, OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT T00011AT 2007060700049 20070607 00049 SO 2007 6 7 RAIA00705048 1 20070526 A 5270 WARNING LIGHT EMB 145 EMB145LR 3260212 SO CARGO DOOR FALSE ACTIVATION A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 829HK 145281 FLT NR 9882 - BDL - MAIN BAGGAGE DOOR EICAS MESSAGE REMAINS ON WITH DOOR CLOSED AND LOCK. MAINTENANCE CYCLED DOOR SEVER AL TIMES, VERIFIED CLOSED AND LOCKED DEFERRED PER MEL. 2 L 7 2 4T RT T00011AT 2007060700067 20070607 00067 WP 2007 6 7 NWAA072059750 1 20070430 A 5310 DOUBLER DOUG DC9 DC941 302207N WP FUSELAGE MISMANUFACTURED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 750NW 47114 DURING "H" CHECK WHILE ACCOMPLISHING FORWARD SERVICE DOOR MODIFICATION PER AMI CARD 5310-01296-01B FOUND THAT THE DOUBLE RS COULD NOT PICK UP TWO FASTENERS DUE TO SHORT EDGE DISTANCE. REPAIRED PER EA 97-20945 SECT I, SECTION II TO BE ACCOMP LISHED EVERY 8000 CYCLES. 2 L 7 2 4F A6WE 2007060800003 20070608 00003 NM 2007 6 8 QXEA200700882 1 20070524 A 5410 DIAPHRAGM BOMBDR DHC8 DHC8402 1390042 NM NR 1 NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 C4 PDX - THE NR 1 NACELLE HAS SMOKING FASTENERS ON THE OUTBOARD AFT DIAPHRAGM. REPAIRED IAW RD8/4-54-154, EO 6-54-441, AND SRM 51-42-05. 2 H 7 2 4T RT A13NM 2007060800008 20070608 00008 NM 2007 6 8 QXEA200700890 1 20070523 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 C4 PDX - THERE IS CORROSION ON THE RIGHT INBOARD SEAT TRACK FROM X13.5 TO X49 TRACK 11. REPAIRED IAW RD8/4-53-884, AND SRM 51-42-05. 2 H 7 2 4T RT A13NM 2007060800009 20070608 00009 NM 2007 6 8 QXEA200700891 1 20070526 A 5230 DOOR BOMBDR DHC8 DHC8402 1390042 NM CARGO BAY CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 C4 PDX - FORWARD CARGO DOOR CHAFED ON AFT UPPER TOP OF APERTURE. REPAIRED IAW RD8/4-53-505. 2 H 7 2 4T RT A13NM 2007060800010 20070608 00010 NM 2007 6 8 QXEA200700886 1 20070525 A 5347 CARGO TRACK BOMBDR DHC8 DHC8402 1390042 NM CARGO BAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 C4 PDX - AT X781 Z100 Y9L, THE TRACK HOLD DOWN CLEAT IS CORRODED. REPAIRED IAW RD8/4-53-884, AND SRM 51-40-07, 51-42-05 . 2 H 7 2 4T RT A13NM 2007060800013 20070608 00013 NM 2007 6 8 QXEA200700876 1 20070601 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM AUTO FEATHER FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 420QX 4147 PDX FLIGHT NR 2268: AFTER ENGINE START AND AUTO FEATHER SELECT, NO A/F SELECT ON ED. AIRCRAFT RETURNED TO BLOCK. MAINT ENANCE INTERROGATED CDS. REPORTS A/F SELECT SYSTEM. RESELECTED AUTO FEATHER SYSTEM. AUTO FEATHER PASSED. A/F SELECTE D ON ED SHOWS UP. ALL SYSTEMS NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007060800015 20070608 00015 NM 2007 6 8 DLM88070644 1 20070527 A 5320 ANGLE DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CORROSION ON LEFT TRAPEZOIDAL ANGLE AT FWD UPPER L MLG WW CORNER. NEW ANGLE FABRICATED AND INSTALLED IAW DOUGLAS DRAWIN G 5935852 N/R T0056098. 2 L 7 2 4F RT A6WE 2007060800041 20070608 00041 NM 2007 6 8 DHL2007740509 1 20070523 A 5753 SKIN BOEING 727 7272Q9 138448M NM RT WING TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 RT O/B AFT FLAP WBL 417 HAS DELAMINATION AND SURFACE CORROSION ON AN NEAR T/E. REMOVED DAMAGED AREA APPROX 10" BY 20". CLEANED AN PREPPED AREA TO BE REPAIRED. FAB`D FILLER 10" BY 20" AN 2 DOUBLERS 3" BY 20" FROM .016" 2024-T3 PO NR 90041 74. ANODIZED AN PRIMED AN APPLIED ADHESIVE FILM IAW B727 SRM 51-40-20 PARA 7 FIG 3, 51-40-24 FIG 3 AN 57-50-2 FIG 4. C URED AND FINISHED REPAIR AREA IAW B727 SRM 51-40-20 PARA 20 AN 22 AN 51-40-24 FIG 3. MAJOR REPAIR. PERMANENT REPAIR. 2 L 7 3 4F RT A3WE 2007060800046 20070608 00046 NM 2007 6 8 DU4R20070126 1 20070523 A 5311 FRAME BOEING 757 757232 1384965 NM BS 660 BENT B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 640DL 23994 FOUND BENT MAIN FRAME UPPER SURFACE IN FWD PIT BS 660 AT S-24L. REPAIRED BY CUTTING OUT BENT SECTION OF FRAME. FABRICA TED AND INSTALLED DOUBLER 11-1/2 BY ¼ BY 1 BY 2 FROM 7075-T6 .063 IAW B757 SRM 53-00-07 AND 51-20-01. 2 L 7 2 4F RT A2NM 2007060800054 20070608 00054 NM 2007 6 8 EIA2007122 1 20070604 A 2611 30231A7 SMOKE DETECTOR BOEING 747 747132 1384882 NM CARGO BAY NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481EV 19896 ON PREFLIGHT CHECK, AFT CARGO SMOKE DETECTOR NR 6 NO TEST. REPLACED SMOKE DETECTOR PER B747 MM 26-16-00. 2 L 7 4 4F A20WE 2007060800068 20070608 00068 NM 2007 6 8 DLM88070659 1 20070530 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 984-1003 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 PITTING CORROSION ON LEFT CUSP WEB BETWEEN STA 984 TO 1003. LEFT CUSP WEB BETWEEN STA 984 T0 1003 REPLACED IAW DWG 9930 612 NR T0057018. 2 L 7 2 4F RT A6WE 2007060800073 20070608 00073 NM 2007 6 8 DLM88070663 1 20070530 A 5320 WEB DOUG MD88 MD88 3023688 NM BS 1474-1485 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACKED LT UPPER WEB BETWEEN STA 1474-1485 AT AFT ACCESSORY COMPARTMENT. WEB FABRICATED AND INSTALLED IAW DOUGLAS DRAWI NG 9923630 NR T0057063. 2 L 7 2 4F RT A6WE 2007060800096 20070608 00096 NM 2007 6 8 DLM88070684 1 20070601 A 5320 INTERCOSTAL DOUG MD88 MD88 3023688 NM BS 788 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACK ON INTERCOSTAL OF FLOOR SUPPORT AT STA Y=788 X=0. INTERCOSTAL FABRICATED AND REPLACED IAW SRM 51-70-5 NR T0056354 . 2 L 7 2 4F RT A6WE 2007060800101 20070608 00101 NM 2007 6 8 DLM88070689 1 20070604 A 5300 STRUCTURE DOUG MD88 MD88 3023688 NM BS 275 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CORROSION AT STA Y=275 BETWEEN LONGERONS 3 RT AND 6 LT. REPAIRED IAW SRM 51-30-5 NR T0056455. 2 L 7 2 4F RT A6WE 2007060800112 20070608 00112 NM 2007 6 8 SWAA072833 1 20070605 A 3350 101331 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 432WN 33715 RIGHT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007060800118 20070608 00118 NM 2007 6 8 SWAA072837 1 20070605 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 520 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 9R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007060800125 20070608 00125 2007 6 8 HNAA0700101 4 20070601 A 3443 RADAR DHAV DHC8 DHC8102 2809003 NM FAILED A HNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 07 935HA 142 ON CLIMBOUT FROM SBY THE RADAR FAILED. CREW CYCLED CIRCUIT BREAKER WITH NO FIX. FLIGHT RETURN TO THE FIELD. EMERGENCY WAS NOT DECLARED AND FLIGHT LANDED WITH OUT INCIDENT. CREW IN FLIGHT TURNED OFF INDICATOR AND CYCLED C/B BUT DID NOT T URN INDICATOR BACK ON. PERFORMED RADAR FUNCTION TEST, TESTED NORMALLY A/C DEPARTED AGAIN FOR CLT. 2 H 7 2 4T RT A13NM 2007060800131 20070608 00131 NM 2007 6 8 HNAA0700102 1 20070603 A 7930 APT761000100D TRANSMITTER DHAV DHC8 DHC8102 2809003 NM OIL PRESSURE MALFUNCTIONED A HNAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 07 808EX 299 NR 2 ENGINE OIL PRESSURE GAUGE DROPPED TO 0 PSI, WITH NO WARNING LIGHTS, ALL OTHER ENGINE PARAMETERS NORMAL. REMOVED AN D REPLACED DUAL OIL INDICATOR, REMOVED AND REPLACED NR 2 OIL PRESSURE TRANSMITTER. RAN A/C OPS AND LEAK CHECK GOOD. A/ C OK FOR SERVICE. 2 H 7 2 4T RT A13NM 2007060800132 20070608 00132 EA 2007 6 8 HNAA0700103 1 20070521 A 3350 6013211 BATTERY PACK DHAV DHC8 DHC8311 1386006 EA EMERGENCY LIGHTS DISCHARGED A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 326EN 234 F/A REPORTS EMERGENCY LIGHTS DO NOT WORK. REMOVED AND REPLACED EMERGENCY BATTERY PACKS. 2 H 7 2 4T RT A13NM 2007060800133 20070608 00133 NM 2007 6 8 HNAA0700107 1 20070508 A 5340 85320980105 FITTING DHAV DHC8 DHC8102 2809003 NM BS 291 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 938HA 152 CORROSION ON TOILET SERVICING ACCESS BOX RIGHT UNDER FLOOR. TOILET SERVICING BOX FITTING ON RIGHT UNDER FLOOR REPLACED. 2 H 7 2 4T RT A13NM 2007060800138 20070608 00138 NM 2007 6 8 HNAA0700108 1 20070514 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 510-530 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 937HA 148 LEFT HAND INBOARD SEAT RAIL AT STA 510-530 SHOWS SIGN OF CORROSION AROUND FASTENERS AND SPLICE PLATES. REMOVED FASTENER S, REMOVED LIGHT CORROSION, ALODINE AND PRIMED IAW SRM 51-20-11, SRM 51-20-16. REINSTALLED FASTENERS. 2 H 7 2 4T RT A13NM 2007060800139 20070608 00139 NM 2007 6 8 HNAA0700110 1 20070507 A 5755 BRACKET DHAV DHC8 DHC8102 2809003 NM LT SPOILER CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 936HA 145 LEFT FLIGHT SPOILER DOG BONE HOLE BRACKET CRACKED. TEST WITH HIGH FREQ EDDY CURRENT, NO CRACK FOUND. LEFT INBOARD FLIG HT SPOILER DOG BONE HOLE WEB REPAINTED IAW E08-57-07-3187-SEG 9734. 2 H 7 2 4T RT A13NM 2007060800140 20070608 00140 GL 2007 6 8 C2XA07SH034 2 20070526 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 SHUTDOWN A C2XA B EMER. DESCENT Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SW 27 16571 14099 6501 145633 CAE311739 SHV - DURING CRUISE THE AIRCREW EXPERIENCED AN UNCOMMANDED SHUTDOWN OF THE NR 2 ENGINE ON FLIGHT 3062 FROM TYS TO IAH. AN EMERGENCY WAS DECLARED, DIVERTED TO JAN. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ENGINE IAW EXPRESSJET TASK CA RD 6271001. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS SDR IS BEING FILED OPEN PENDING FINAL DETERMINATION OF ENGINE FAILURE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007060800147 20070608 00147 SO 2007 6 8 C2XA07ON004 1 20070529 A 2824 2770138101 FLAPPER VALVE EMB 145 EMB145LR 3260212 SO FUEL TANK MISSING A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 27 18557 598 FLT 41 - GEG TO GEG - FUEL LEAKING FROM RIGHT WING DURING T/O. MX INSPECTED FUEL TANK AND FOUND MOST OUTBOARD FLAPPER V ALVE MISSING. MX INSTALLED NEW RIGHT WING FLAPPER VALVE AND PERFORMED OPERATIONAL CHECKS SUCCESFULLY. THE A/C WAS APPR OVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007060800164 20070608 00164 NM 2007 6 8 SWAA072847 1 20070605 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, S8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060800174 20070608 00174 NM 2007 6 8 WRLA2007069 1 20070525 A 2121 6054578 FAN DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE CABIN FAILED A WRLA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 801DE 48472 FLIGHT 8011 KBAD/PHIK 05/25/07 - DURING CRUISE FLT350 ELECTRICAL FUMES REPORTED BY CABIN CREW IN A ZONE. COMPLIED WITH VOL 1 PROCEDURES. FUMES DISSIPATED WHEN CAB BUSS SWITCH SELECTED OFF. PAX REPORTED HIGH PITCHED NOISE FROM LEFT REAR W ALL OF -A ZONE- UNKNOWN IF RELATED TO ODOR. ENTERED IN DEFERRED MAINTENANCE LOG DMI M21MA2507-143. RECIRCULATION FAN C ONNECTOR REMOVED AND SECURED. 2 L 7 3 4F 4 F RT A22WE E24NE 2007060800176 20070608 00176 NM 2007 6 8 KCSA071168 1 20070530 A 5347 SEAT TRACK BOEING 747 747221F 1384868 NM BS 390-402 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 SEAT TRACK O/B FLANGE HAS CORROSION FROM STA 390 TO 402 RBL 83. 2 L 7 4 4F A20WE 2007060800180 20070608 00180 SO 2007 6 8 RAIA00705051 1 20070527 A 2731 TAB EMB 145 EMB145 3260210 SO ELEVATOR CRACKED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 807HK 145119 FLT NR 3501 - PIT - STAB TRIM SET AT -4 TO FLY LEVEL. MAINTENANCE FOUND RIGHT SPRING TAB JAMMED ON ATTACHMENT FAIRING A ND FOUND CRACK ON ELEVATOR AT SPRING TAB ROD PASS-THROUGH. REPLACED FAIRING, REPAIRED CRACK PER SRM. 2 L 7 2 4F RT T00011AT 2007061100072 20070611 00072 WP 2007 6 11 070121 1 20070517 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 875GA 53468 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENC Y EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BA TTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007061100073 20070611 00073 WP 2007 6 11 070122 1 20070529 A 3350 408822101 BATTERY PACK DOUG DC9 DC987 3022087 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 945MA 49725 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENC Y EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BA TTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007061100074 20070611 00074 WP 2007 6 11 070123 1 20070524 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 869GA 53294 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENC Y EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BA TTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007061100075 20070611 00075 WP 2007 6 11 070124 1 20070517 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 876GA 53469 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENC Y EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BA TTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007061100076 20070611 00076 WP 2007 6 11 070125 1 20070528 A 3350 408822101 BATTERY PACK DOUG DC9 DC987 3022087 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 945MA 49725 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENC Y EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BA TTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007061100090 20070611 00090 NM 2007 6 11 QXEA200700900 1 20070607 A 2420 11520924 GCU BOMBDR DHC8 DHC8402 1390042 NM NR 2 MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 424QX 1872 1872 4006 SEA FLIGHT NR 2396: NR 2 AC GEN LIGHT ILLUMINATED. AIRCRAFT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED THE A C GENERATOR (PN 28B555-1, S/N 071C0358) IAW Q400 AMM 24-21-01, PAGES 401-410. NO HELP NOTED. REMOVED AND REPLACED AC G ENERATOR GCU IAW Q400 AMM PAGES 401-406. PERFORMED OPS TEST OF THE AC VARIABLE FREQUENCY GENERATION SYSTEM IAW Q400 AMM 24-21-00, PAGES 501-502. OPS CHECK GOOD. REPLACEMENT OF AC GEN WAS IAW MTX TASK CARD NR 6242101. AIRCRAFT WAS RETURN ED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061100091 20070611 00091 EA 2007 6 11 SWIA200718304 1 20070422 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 768SK 10234 PAX DOOR AFT WEB IS CRACKED AT HANDRAIL SUPPORT, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS IN ACCORDANCE WITH CRJ 7 00 REO 601R-52-11-104 REV B. 2 L 7 2 4F RT A21EA 2007061100092 20070611 00092 EA 2007 6 11 SWIA200718305 1 20070422 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 768SK 10234 PAX DOOR FORWARD WEB IS CRACKED AT HANDRAIL SUPPORT, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ 700 REO 67-0 -52-11-104 REV B, REPAIR SCHEME 2 SHEET 6. 2 L 7 2 4F RT A21EA 2007061100093 20070611 00093 EA 2007 6 11 SWIA200718306 1 20070429 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 771SK 10244 PAX DOOR AFT WEB IS CRACKED AT HANDRAIL SUPPORT BRACKET, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS AT PAX DOOR AFT WEB PER REO 670-52-11-104. 2 L 7 2 4F RT A21EA 2007061100094 20070611 00094 EA 2007 6 11 SWIA200718307 1 20070429 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 771SK 10244 PAX DOOR FORWARD WEB IS CRACKED AT HANDRAIL SUPPORT BRACKET, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS PER REO 670- 52-11-104 (B) NOTES 1-10,15. 2 L 7 2 4F RT A21EA 2007061100095 20070611 00095 EA 2007 6 11 SWIA200718308 1 20070605 A 2721 KNOB CNDAIR CL600 CL6002C10 1390015 EA RUDDER TRIM BINDING A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 716SK 10180 RUDDER TRIM RAN AWAY IN FLIGHT. RAN CHECKLIST AND WAS RESET TO NEUTRAL.FOUND RUDDER TRIM KNOB TO BE BINDING ON TRIM PAN EL FACEPLATE. ADJUSTED KNOB TO ACHIEVE CLEARANCE FROM FACEPLATE. 2 L 7 2 4F RT A21EA 2007061100096 20070611 00096 EA 2007 6 11 SWIA200718309 1 20070605 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 943SW 7762 AFT CEILING EMERGENCY LIGHT IS INOP. RELAMPED CEILING EMERGENCY LIGHT AS REQUIRED PER AMM 33-51-16. 2 L 7 2 4F RT A21EA 2007061100097 20070611 00097 EA 2007 6 11 SWIA200718310 1 20070605 A 3397 WIRE CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS DISCONNECTED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 730SK 10193 EXIT SIGN LIGHT AT SEAT 3C INOP. RECONNECTED LOOSE WIRE AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007061100098 20070611 00098 NM 2007 6 11 QXEA200700901 1 20070606 A 5210 HANDLE BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR DIRTY A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 408QX 4050 SEA FLIGHT: FA REPORTS THAT THE LEFT REAR PAX DOOR IS DIFFICULT (TL-2) TO OPEN. MAINTENANCE CLEANED DIRT AND DEBRIS FRO M HANDLE MECHANISM AND APERATURE. LUBED LOCKING MECHANISM. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO S ERVICE. 2 H 7 2 4T RT A13NM 2007061100099 20070611 00099 EA 2007 6 11 SWIA200718311 1 20070605 A 2913 MOTOR CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM DEFECTIVE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 903SW 7425 SELECTED GEAR UP AFTER TAKEOFF AND RECEIVED A GEAR DISAGREE AND A NOSE GEAR DOOR OPEN MESSAGE. RAN QRH AND PROBLEM CORR ECTED ITSELF. RETURNED TO DEN. REMOVED AND REPLACED THE NR 3A AC MOTOR PUMP IAW CRJ 200 MM 29-12-03. OPS CHECK GOOD W ITH NO DEFECTS NOTED, P/N:848847, S/N OFF: MX677647. 2 L 7 2 4F RT A21EA 2007061100100 20070611 00100 SO 2007 6 11 SWIA200718312 1 20070604 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO COCKPIT SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 561SW 120335 UPON ESTABLISHING APU BLEEDS, CABIN AND FLIGHT DECK FILLED WITH SMOKE. RAN BOTH PACKS ON APU BLEED FOR 1.5 HOURS. NO S MOKE NOTED IN CABIN OR COCKPIT. COULD NOT DUPLICATE. SYSTEM CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007061100101 20070611 00101 EA 2007 6 11 SWIA200718313 1 20070605 A 3350 CONTACT CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS DIRTY A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 763SK 10228 OVERHEAD EMERGENCY FLOOD LIGHT BY LAV IS INOP. CLEANED CONTACTS ON EMERGENCY LIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007061100102 20070611 00102 SO 2007 6 11 LR7A07042 1 20070514 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FS 990 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 708 4763 DURING SCHEDULED B-3 CHECK PER JOB CARD HB5302, FOUND AFT BULKHEAD UPPER FUSELAGE TO SIDE BULKHEAD ATTACHMENT GUSSET PLA TE CRACKED AT FS 990, RBL 61, WL 256. REPLACED PLATE IAW SMP583 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007061100103 20070611 00103 SO 2007 6 11 LR7A07043 1 20070514 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FS 968 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 708 4763 DURING SCHEDULED B-3 CHECK PER JOB CARD HB5302, FOUND AFT FUSELAGE UPPER BULKHEAD CRACKED AT FS 968, RBL 18, WL 285. RE PAIRED BULKHEAD IAW SMP583 53-50-06. 2 H 7 4 4T A1SO 2007061200001 20070612 00001 NM 2007 6 12 MWEA070122 1 20070528 A 2530 8203120000C OVEN BOEING 717 717200 1383700 NM GALLEY SMOKE A MWEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 13 916ME 55178 FLIGHT ATTENDANT REPORTED THAT INTENSE SMOKE COMING FROM CENTER OVEN, WHEN TURNED ON. CLEANED FOOD FROM CENTER OVEN HEA TING ELEMENTS. 2 L 7 2 4F TR A6WE 2007061200002 20070612 00002 NM 2007 6 12 MWEA070123 1 20070528 A 2530 8203120000C OVEN BOEING 717 717200 1383700 NM GALLEY SMOKE A MWEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 13 928ME 55194 OVEN NR 2 STARTED TO SMOKE. CLEANED BURNED FOOD DEBRIS FROM BACK OF OVEN & HEATING ELEMENT. 2 L 7 2 4F TR A6WE 2007061200005 20070612 00005 EU 2007 6 12 YNTA200728102 1 20070514 A 5753 CN635MESP56 ROD END BRAERO DH125 HS125700A 4230170 EU FLAP SYSTEM CORRODED E YNTA L ABORTED APPROACH S AFFECT SYSTEMS AP APPROACH 1 SW 05 281BT NA0281 ON APPROACH THE FLAP SYSTEM FAILED TO EXTEND PAST 15 DEGREES AND THEN BECAME STUCK AT 15 DEGREES. TRIED TO SET FLAPS TO 25 DEGREES AND FLAPS DID NOT MOVE, RESET FOR 15 DEGREES AND THEN UP TO 0 DEGREES WITH NO MOVEMENT. RESELECTED FLAPS TO 15-DEGREE POSITION. LANDED UNEVENTFULLY. AIRCRAFT FLAP SYSTEM HAD BEEN WORKED ON 05/09/2007 WHERE THE FOLLOWING PARTS WERE REPLACED LEFT FLAP TRUNNION YOKE P/N 25CW733A, BOLT, HEX P/N A102-9D, WASHER P/N SP126D, NUT P/N A103DS AN OPERATI ONAL CHECK WAS ACCOMPLISHED AND A TEST FLIGHT CONDUCTED ON 05/10/2007. FOUND FLAP SYSTEM TO BE OPERATIONALLY SATISFACTO RY IN BOTH INSTANCES. FOUND FLAP CONTROL UNIT INPUT LEVER ROD END CORRODED. REMOVED FLAP INPUT LEVER ROD END P/N CN6-3 2 L 7 2 4F A3EU 2007061200007 20070612 00007 NM 2007 6 12 MWEA070130 1 20070530 A 2530 8203120000C OVEN BOEING 717 717200 1383700 NM GALLEY SMOKE A MWEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 13 909ME 55173 CENTER OVEN IN GALLEY SMOKES. CLEANED CENTER OVEN. 2 L 7 2 4F TR A6WE 2007061200008 20070612 00008 NM 2007 6 12 MWEA070131 1 20070530 A 2530 8203120000C OVEN BOEING 717 717200 1383700 NM GALLEY SMOKE A MWEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 13 914ME 55177 FLIGHT ATTENDANT NOTED AN OVEN SMOKING EXCESSIVELY. CLEANED OVEN. 2 L 7 2 4F TR A6WE 2007061200009 20070612 00009 NM 2007 6 12 MWEA070126 1 20070529 A 7830 7150922REV2 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 902ME 55166 LEFT THRUST REVERSER, BOTTOM BLOCKER DOOR HAS CRACKS ON OUTBOARD SIDE INSIDE DOOR STRUCTURE AT END OF FRAME RADIUS STATI ON 26.666. FABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007061200010 20070612 00010 NM 2007 6 12 MWEA070127 1 20070529 A 7830 7150923REV2 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 902ME 55166 LEFT THRUST REVERSER BOTTOM BLOCKER DOOR HAS A CRACK ON END OF FRAME RADIUS INSIDE OUTBOARD SIDE OF DOOR STRUCTURE AT ST ATION 35.669. FABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007061200012 20070612 00012 NM 2007 6 12 MWEA070129 1 20070529 A 7830 7150922REV2 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 902ME 55166 LEFT THRUST REVERSER UPPER BLOCKER DOOR HAS A CRACK ON INBOARD END OF FRAME RADIUS INSIDE DOOR STRUCTURE AT STATION 35.6 69. FABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007061200013 20070612 00013 NM 2007 6 12 MWEA070132 1 20070605 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 928ME 55194 LEFT THRUST REVERSER CRACKED AT OUTBOARD END OF FRAME, INSIDE BOTTOM DEFLECTOR DOOR STRUCTURE AT FRAME RADIUS STATION 26 .666. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2007061200014 20070612 00014 NM 2007 6 12 MWEA070133 1 20070605 A 7830 7150923REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 928ME 55194 LEFT THRUST REVERSER CRACKED AT END OF FRAME, OUTBOARD SIDE OF BOTTOM DEFLECTOR DOOR ON FRAME RADIUS STATION 35.669. FA BRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2007061200015 20070612 00015 NM 2007 6 12 MWEA070134 1 20070605 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 928ME 55194 LEFT THRUST REVERSER CRACKED ON INBOARD END OF FRAME INSIDE BOTTOM DEFLECTOR DOOR AT STATION 26.666. FABRICATED AND INS TALLED DOUBLER. 2 L 7 2 4F TR A6WE 2007061200018 20070612 00018 NM 2007 6 12 MWEA070137 1 20070605 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 928ME 55194 RIGHT ENGINE LOWER DEFLECTOR DOOR HAS A CRACK IN THE ZEE FRAME RIGHT END IN THE RADIUS FRAME STATION 26.666. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2007061200019 20070612 00019 NM 2007 6 12 MWEA070138 1 20070605 A 7830 7150923REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 928ME 55194 RIGHT ENGINE THRUST REVERSER DEFLECTOR DOOR HAS A CRACK IN THE ZEE FRAME LEFT END IN THE RADIUS FRAME STATION 36.669. F ABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007061200020 20070612 00020 NE 2007 6 12 05290701 2 20070525 A 7200 791741 LINER BOEING 767 767238 1385114 NM PWA JT9 JT9D7R4E 52054 NE LT ENGINE DEPARTED A L43A C ABORTED TAKEOFF D INFLIGHT SEPARATION TO TAKEOFF 1 EA 27 251MY 18144 3037 23280 716801 DURING TAKEOFF FROM EGSS EN ROUTE TO KIAD MUCH OF THE FAN EXIT OUTER CASE LINER SEGMENT AFT OF THE FAN EXIT GUIDE VANES SEPARATED FROM THE NR 1 ENGINE ESN 716801. THE BRITISH AIRPORT AUTHORITY NOTIFIED MAXJET MAINTENANCE THAT THE DEPARTED LINER HAD BEEN FOUND ON THE RUNWAY AND THAT IT IS POSSIBLY FROM ONE OF MAXJETS AIRCRAFT AS MAXJET WAS THE LAST TO USE TH E RUNWAY. THE NOTIFICATION FROM BAA OCCURED HALFWAY INTO THE 8.0 HR FLIGHT. A P/N ON THE UNIT REVEALED THAT THE PART W AS FROM A JT9 ENGINE AND THAT IT WAS A LINER SEGMENT. MAXJET CONTACTED BOTH MAXJET AIRCRAFT EN ROUTE AND ADVISED BOTH N OT TO USE THRUST REVERSERS ON LANDING AND WERE ASKED IF THERE WERE ANY ABNORMAL INDICATIONS, THE CREWS REPORTED THAT ALL 2 L 7 2 4F 4 F RT A1NM E3NE 2007061200021 20070612 00021 NE 2007 6 12 NOCA10107 2 20070514 A 7532 C8E3812 CONTROL UNIT BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E437 54555 NE LT BLEED VALVE MALFUNCTIONED A NOCA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 750NA 26277 LEFT ENG EXCEEDANCE EGT AND N2 ON TAKEOFF ROLL FOR LESS THAN ONE SECOND. REMOVED AND REPLACED NR 1 ENG BVCU IAW MM 75-3 2-01. IDLE RUN DONE. BVCU BITE CKS OK IAW 71-00-00 & 75-32-00. HIGH POWER RUN ACCOMPLISHED TEST 3. PERFORMED OF 71-0 0-00. ENG CHECKS OK FOR SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2007061200022 20070612 00022 NM 2007 6 12 NOCA10007 1 20070501 A 5210 GUST LOCK BOEING 757 75728A 1384976 NM L2 DOOR BROKEN A NOCA O OTHER O OTHER NR NOT REPORTED 1 EA 15 755NA 30043 L2 DOOR GUST LOCK ASSY BROKEN. INSTALLED GUST LOCK ASSY PER MM 52-11-08. RE-ACCORD ON 5-13-07 L2 DOOR GUST LOCK ASSY B ROKEN. SDR REMAINS OPEN. 2 L 7 2 4F RT A2NM 2007061200023 20070612 00023 NM 2007 6 12 NOCA10207 1 20070518 A 2121 033638 BLOWER BOEING 757 75728A 1384976 NM CABIN MALFUNCTIONED A NOCA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 15 750NA 26277 THE -AFT DET FAN- STATUS MESSAGE ON EICAS. REMOVED AND REPLACED NR 3 AFT BLOWER IAW AMM 26-16-02 AND REMOVED AND REPLAC ED BLOWER NR 3 RELAY K10379 BLOWER RELAY P/N OFF TDH8116-6002, S/N OFF, P/N ON TDH8116-6002, S/N ON 8-11-06-1 IAW WDM 2 6-16-21. OPS CHECKS NORMAL AS PER THE FIM 26-16-00 FIG 104. NO MESSAGE DISPLAYED. A/C OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2007061200024 20070612 00024 NM 2007 6 12 NOCA10307 1 20070524 A 2560 P2070003001 FLASHLIGHT BOEING 757 75728A 1384976 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 754NA 29381 R4 FLIGHT ATTENDANT SEAT LEFT FLASH LIGHT INOP. REMOVED AND REPLACED THE R4 FLASHLIGHT ASSY AND BATTERY P/N P4-01 0021, INSTALLED A NEW SAFETY STRAP. OPS CHECKS OKAY. 2 L 7 2 4F RT A2NM 2007061200026 20070612 00026 NM 2007 6 12 USAA070461 1 20070607 A 5330 SKIN BOEING 737 7374B7 1384702 NM BS 947 S10L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 STA 947.5, S10L AFT ENTRY DOOR UPPER HINGE SKIN CUTOUT HAS CRACK. REMOVED DAMAGE & FABRICATED DOUBLER & INSTALLED, DEFE CT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007061200027 20070612 00027 EU 2007 6 12 USAA070462 1 20070607 A 5311 FRAME AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 180US 1525 FRAME 66 HAS CORROSION. INSTALLED BATH TUB FITTING PER TR 53-41-01, DEFECT SIZE: 1" X 1" X .067". 2 L 7 2 4F RT A28NM 2007061200028 20070612 00028 NM 2007 6 12 USAA070453 1 20070607 A 5320 6531787U5 SUPPORT ANGLE BOEING 737 737401 1384701 NM BS 318-340 S17L CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 BS 318-340, S17L; DOORWAY SILL SUPPORT ANGLE HAS CORROSION. INSTALLED NEW ANGLE PER SRM 51-10-02, 51-30-00; CORR TASK C 53-107-01; LEVEL 2, DEFECT SIZE: .5 X 1 INCH. 2 L 7 2 4F RT A16WE 2007061200029 20070612 00029 WP 2007 6 12 ABXA070175 1 20070529 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP EMERGENCY LIGHTS DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY IAW DC9 AMM 33-53-00-8. 2 L 7 2 4F A6WE 2007061200034 20070612 00034 NM 2007 6 12 USAA070418 1 20070605 A 5320 6561777505 SPLICE BOEING 737 737401 1384701 NM BS 360 S14L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 BS 360, S-14L, CHANNEL SPLICE HAS CRACK. REMOVED DAMAGED CHANNEL SPLICE & INSTALLED NEW SPLICE PER SRM 51-10-02, 51-40- 02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007061200039 20070612 00039 WP 2007 6 12 ABXA070178 1 20070605 A 5310 99115055 WINDOW FRAME DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 WHILE COMPLYING WITH WINDOW FRAME MOD EA53000041, FOUND CRACKED FRAME. REPAIRED AREA IAW DC9 SRM 53-03, FIG 34. 2 L 7 2 4F A6WE 2007061200040 20070612 00040 WP 2007 6 12 ABXA070179 1 20070605 A 5310 99115056 WINDOW FRAME DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 WHILE COMPLYING WITH WINDOW FRAME MOD EA 53000041, FOUND CRACKED FRAME. REPAIRED AREA IAW DC9 SRM 53-03, FIG 34. 2 L 7 2 4F A6WE 2007061200042 20070612 00042 NM 2007 6 12 USAA070466 1 20070608 A 5320 143N54102 SUPPORT BOEING 757 7572B7 1384964 NM BS 680-700 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 BS 680-700, RBL 62.45, GUTTER SUPPORT ASSEMBLY HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-30 -15, 51-10-02; 51-40-02, DEFECT SIZE: 4 X 1 INCH. 2 L 7 2 4F RT A2NM 2007061200044 20070612 00044 NM 2007 6 12 SWAA072842 1 20070605 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061200045 20070612 00045 2007 6 12 SWAA072856 4 20070605 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM R1 DOOR SLIDE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM. 2 L 7 2 4F RT A16WE 2007061200046 20070612 00046 NM 2007 6 12 SWAA072835 1 20070605 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM BS 500B S20R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007061200047 20070612 00047 NM 2007 6 12 SWAA072836 1 20070605 A 5754 65C26602 STRUCTURE BOEING 737 7373H4 1384600 NM NR 2 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED C3 CHECK, FOUND LEFT WING NR 2 L/E SLAT CRACKED AT OUTBOARD TRACK. REPAIRED SLAT PER SWA EA. 2 L 7 2 4F RT A16WE 2007061200049 20070612 00049 2007 6 12 SWAA072830 4 20070605 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007061200051 20070612 00051 EU 2007 6 12 BAQA200700015 1 20070601 A 3320 LT100 DIMMER AEROSP SA365 SA365N1 8680668 EU CABIN LIGHT BURNED OUT E BAQA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 03 93SV 9490 436 6286 IN CRUISE FLIGHT MEDICAL CREW REPORTED A DIMMING OF THE CABIN FLOOD LIGHTING FOLLOWED BY AN "ELECTRICAL BURNING SMELL". 1 G 7 2 3U H10EU 2007061200052 20070612 00052 EU 2007 6 12 BAQA200700016 1 20070530 A 6320 109040003109 GEARBOX AGUSTA A109 A109E 0260119 EU MAIN ROTOR MAKING METAL E BAQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 03 109UP 2213 11061 DURING TAKEOFF, MAIN TRANSMISSION CHIP ILLUMINATED. CYCLED CHIP BURNER ONCE WITH NO SUCCESS. MECHANIC CALLLED. MECHANIC REMOVED AND INSPECTED MAIN GEARBOX AND COUPLING GEARBOX CHIP DETECTORS AND FOUND SMALL FLAKES ON BOTH UPPER AND LOWER C HIP PLUGS. ALL CHIPS WERE WITH IN LIMITS PER AGUSTA A109E M.M. CHIP PLUGS CLEANED AND REINSTALLED. OIL DRAINED AND RESER VICED WITH BP 2380 OIL. REPLACED OIL FILTER. ALL WORK DONE IAW A109E MM CHAPTER 63-00-00 PG 63-5 THRU 63-8 AND CHAPTER 1 2. DURING MAINTENANCE RUN CHIP LIGHT ILLUMINATED. CYCLED CHIP BURNER WITH NO SUCCESS. AIRCRAFT SHUT DOWN WITH OUT INCIDE NT. AIRCRAFT TRANSPORTED TO MANUFACTURER. 1 G 7 2 3U RT H7EU 2007061200056 20070612 00056 NM 2007 6 12 SWAA072888 1 20070607 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SERVICE DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SSWA E A. 2 L 7 2 4F RT A16WE 2007061200057 20070612 00057 NM 2007 6 12 SWAA072918 1 20070607 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SERVICE DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007061200058 20070612 00058 NM 2007 6 12 SWAA072882 1 20070605 A 5753 BRACKET BOEING 737 7375H4 138449D NM FORE FLAP BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW BN786 26567 LEFT WING OUTBOARD FORE FLAP BRACKET BROKEN OFF. REMOVED AND REPLACED FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2007061200059 20070612 00059 NM 2007 6 12 SWAA072866 1 20070607 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061200060 20070612 00060 NM 2007 6 12 SWAA072880 1 20070607 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM BS 482 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 482, STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007061200061 20070612 00061 NM 2007 6 12 SWAA072914 1 20070608 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT RT BS 616, WL 202. REPAIRED FRAME PER TYPICAL REPAIR MANAU L. 2 L 7 2 4F RT A16WE 2007061200063 20070612 00063 EU 2007 6 12 YENA2007044 1 20070602 A 3222 STRUT EMB ERJ190 ERJ190100IGW 3260408 EU NLG UNDERSERVICED A YENA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 EA 15 267JB 19000065 FLT 5102, AIR TURNBACK DUE LDG VOW SYS FAIL CAS, LANDING GEAR FAILED TO RETRACT. SERVICED NOSE LANDING GEAR SHOCK STRUT IAW AMM 32-21-04. PERFORMED OPS CHECK OF LANDING GEAR RETRACTION SYSTEM IAW 32-33-00-05. OPS TEST GOOD. 2 L 7 2 4F RT A57NM 2007061200065 20070612 00065 EU 2007 6 12 YENA2007045 1 20070602 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU CABIN ODOR A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 556JB 1904 AFTER TAKEOFF, APPROX 2100 PM, JFK TO SJC, AIR TURNBACK DUE TO ODOR OF ELECTRICAL BURNING ODOR THROUGHOUT THE CABIN, SOM E ODOR IN THE COCKPIT. PERFORMED TSM 24-00-00-810-823, NO DISCREPANCY NOTED. NO ELECTRICAL ODOR RETURNED UPON AIRCRAFT ARRIVAL. OPERATED PACKS NO ODOR NOTED. COMPLIED WITH TSM 23-39-00-810-801, POWERED UP THE SYS, OPS CHECK OK. ALL GRE EN ON EV IN MAINT CONSOLE, NO ODOR DETECTED, NO FURTHER ACTION REQUIRED. 2 L 7 2 4F RT A28NM 2007061200066 20070612 00066 NM 2007 6 12 SWAA072911 1 20070608 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT RIGHT BS 616, AT LOWER FASTENER ABOVE FUEL TANK. REPAIRED FRAME PER TYPICAL REPAIR MANUAL. 2 L 7 2 4F RT A16WE 2007061200068 20070612 00068 NM 2007 6 12 SWAA072910 1 20070608 A 5311 6546540 FRAME BOEING 737 7373H4 1384600 NM BS 639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT RIGHT BS 639, ATTACH FITTING AT NR 4 SEAT TRACK. REMO VED AND REPLACED STUB FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007061200069 20070612 00069 NM 2007 6 12 SWAA072894 1 20070607 A 5311 6546547 FRAME BOEING 737 7373H4 1384600 NM BS 727 S14R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727, STR 14R. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2007061200071 20070612 00071 NM 2007 6 12 SWAA072887 1 20070607 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061200075 20070612 00075 NM 2007 6 12 SWAA072875 1 20070607 A 5313 6551698 STRINGER SPLICE BOEING 737 7375H4 138449D NM BS 360 S14L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007061200076 20070612 00076 NM 2007 6 12 SWAA072876 1 20070607 A 5313 6551698 STRINGER SPLICE BOEING 737 7375H4 138449D NM BS 360 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007061200077 20070612 00077 NM 2007 6 12 SWAA072890 1 20070607 A 3350 6556633 LIGHT BOEING 737 7373Q8 1384670 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED MV2 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007061200079 20070612 00079 EU 2007 6 12 YENA2007040 1 20070529 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS NO TEST A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 503JB 19175 1123 UPON TEST ROW 10 ABC EMERGENCY LIGHTS DID NOT WORK. REMOVED AND REPLACED POWER SUPPLY (12WL) PER AMM 33-51-38-04. OPS CHECK OK. 2 L 7 2 4F RT A28NM 2007061200080 20070612 00080 NM 2007 6 12 SWAA072886 1 20070607 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM BS 500C S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061200083 20070612 00083 NM 2007 6 12 SWAA072864 1 20070606 A 3350 101114 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 249WN 34951 FWD CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007061200085 20070612 00085 NM 2007 6 12 SWAA072896 1 20070608 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 261WN 32517 EEPLS COVER LOOSE AT ROW 3 DEF. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007061200086 20070612 00086 2007 6 12 SWAA072902 4 20070608 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 764SW 27878 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007061200087 20070612 00087 NM 2007 6 12 SWAA072892 1 20070607 A 5322 65456546 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 787 S28R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007061200088 20070612 00088 NM 2007 6 12 SWAA072889 1 20070607 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 510 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007061200089 20070612 00089 NM 2007 6 12 SWAA072909 1 20070608 A 5315 6545810 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM UPPER TEE CAP CORRODED AT BS 312, BETWEEN LBL 56 AND RBL 56. REMOVED AND R EPLACED FLOORBEAM TEE CAP PER SRM. 2 L 7 2 4F RT A16WE 2007061200090 20070612 00090 EU 2007 6 12 YENA2007048 1 20070605 A 2120 UNKNOWN EMB ERJ190 ERJ190100IGW 3260408 EU CABIN ODOR A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 187JB 19000009 FLIGHT 1093, JFK-CMH, APPROX 1200Z, RETURNED TO JFK, STRONG ODOR OF BURNING PLASTIC REPORTED BY CABIN CREW IMMEDIATELY A FTER TAKEOFF. SEEMED TO BE STRONGEST IN MID-CABIN. SMOKE SEEN FROM BOTH MAINS AFTER LANDING. DEBRIEF CREW ALSO REPORT ED ODOR NOTICED UPON L/G RETRACTION, FOUND ODOR COMING FROM BRAKES 1 TO 4. ALL 4 BRAKES PREVIOUSLY CHANGED DUE CONTAMIN ATION. RINSED MLGS IAW AMM 12-12-10. PERFORMED OPS CK AND INSPECTION OF BRAKES 1, 2, 3, 4. ALL FUNCTIONS NORMAL. NO DEFECTS NOTED. NO EICAS MSGS PRESENT ON GROUND. NO C/B FOUND OUT. OPS CKS OF BRAKES 1, 2, 3, 4 PERFORMED IAW AMM 32-4 0-00. ALSO LTV PERFORMED INSPECTION, NO DEFECTS NOTED. NEXT FLIGHT 1008 JFK/BOS PERFORMED NO ODOR NOTED. 2 L 7 2 4F RT A57NM 2007061200091 20070612 00091 EU 2007 6 12 YENA2007042 1 20070529 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHT NO TEST A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 542JB 20696 1802 EMERGENCY LIGHT BATTERY FAIL TEST ROW 10DEF, (12WL). REMOVED AND REPLACED BATTERY FOR EPSU, FIN NR 12WL PER AMM REF 33- 51-38-04, CHECKS OK. 2 L 7 2 4F RT A28NM 2007061200093 20070612 00093 NM 2007 6 12 BB07039 1 20070602 A 2927 PRESSURE SWITCH BOEING 767 7672B7 1385107 NM HYD SYSTEM MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 253AY 24894 FLIGHT 748, PHL-AMS: FLIGHT DIVERTED TO CLT DUE TO A NUMBER 2 ENGINE DRIVEN PUMP LOW PRESSURE LIGHT. PRESSURE INDICATI ON REMAINED NORMAL. MAINTENANCE REPLACED PRESSURE SWITCH S31. NO FURTHER FAULTS. 2 L 7 2 4F RT A1NM 2007061200094 20070612 00094 NM 2007 6 12 SWAA072853 1 20070605 A 3350 D71701100 BATTERY PACK BOEING 737 7377Q8 1384418 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 799SW 28209 DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007061200097 20070612 00097 NM 2007 6 12 SWAA072855 1 20070605 A 3350 D71701100 BATTERY PACK BOEING 737 7377Q8 1384418 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 799SW 28209 DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PA CK PER MM. 2 L 7 2 4F RT A16WE 2007061200098 20070612 00098 EU 2007 6 12 SA07035 1 20070608 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHTS FAULTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 754UW 23106 108 1328 DCA - THE MID-CABIN, RIGHT HAND EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE MID-CABIN, RIGHT HAND EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007061200101 20070612 00101 NM 2007 6 12 AMTA200700207 1 20070429 A 3610 UNKNOWN BOEING 737 73783N 13844HI NM DUCT PRESSURE UNKNOWN A AMTA O OTHER O OTHER CL CLIMB 1 GL 11 319TZ 30643 ON CLIMB OUT, NOTED NO DUCT PRESSURE ON LT DUCT PRESSURE GAUGE, COULD ONLY RESTORE BY OPENING ISOLATION VALVE. PERFORME D FIM 36-10-00-810-804 AND 805 SYSTEM CHECK NORMAL. (K) 2 L 7 2 4F RT A16WE 2007061200102 20070612 00102 SO 2007 6 12 C2XA07IA131 1 20070605 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NLG INOPERATIVE A C2XA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SW 27 17984 145246 IAH - FLIGHT 2598, THE CREW REPORTED A LOUD NOISE AND VIBRATION IN THE NOSE ARE DURING CRUISE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NLG UPLOCK BOX PROXIMITY SENSOR, OPERATIONALLY CHECKED W ITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061200103 20070612 00103 SO 2007 6 12 C2XA07IA130 1 20070603 A 3397 CONNECTOR EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHTS LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14940 145033 IAH - FLIGHT 2277, DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT AT SEAT 12A WAS INOPER ATIVE. MAINTENANCE RESECURED THE CONNECTOR ON THE AFFECTED LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRA FT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007061200105 20070612 00105 SO 2007 6 12 C2XA07RI043 1 20070601 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BURNED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14952 145067 RIC - DURING SCHEDULE INSPECTION, MX FOUND RIGHT AFT EXTERIOR EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED THE LIGHT B ULB AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061200106 20070612 00106 SO 2007 6 12 C2XA07RI039 1 20070515 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 22971 145149 EWR - DURING SCHEDULE MAINTENANCE, MX FOUND AFT CEILING EMERGENCY ROW EXIT IDENTIFIER INOP. MX REMOVED AND REPLACED FWD CEILING EXIT INVERTER IAW EMB-145 AMM 33-50-11 AND PERFORMED OPERATIONAL SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061200107 20070612 00107 EA 2007 6 12 TRAX200700770 1 20070531 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 885AS 7521 RBL 36 FS 484 ANGLE IS CRACKED. [06-12-07] REMOVED CRACKED ANGLE FROM FS 484 RBL 36 IAW REO 601R-53-41-059 DUPLICA TED NEW ANGLE, PER REO 601R-53-41-059. OK TO LPI. COMPLIED WITH LPI OF MANUFACTURED ANGLE IAW REO 601R-53-41-059 AND N DTM 51-20-08. NO DEFECTS NOTED. INSTALLED NEW ANGLE AND COMPLETED REPAIR IAW REO 601R-53-41-059. LEAK CHECK GOOD IAW CRJ MM 21-31-00. 2 L 7 2 4F RT A21EA 2007061200109 20070612 00109 NM 2007 6 12 CALA0700275 1 20070601 A 5313 BAC1498156 STRINGER BOEING 737 7373T0 1384582 NM BS 967-986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12313 23364 INSPECTION FOUND STRINGER 25L CORRODED AT STA 967-986.5. THE CORRODED SECTION OF STRINGER WAS CUT OUT AND REPAIR PARTS WERE INSTALLED IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 2007060700043 20070607 00043 EU 2007 6 7 TRAX200700727 1 20070525 A 7900 WARNING SYSTEM AEROSP ATR72 ATR72 EU OIL PRESSURE ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 640AS 405 DURING INITIAL CLIMBOUT NR 1 ENG LO OIL PRESS WARNING BOTH LOCAL ALERT & CCAS ACTIVATED. ALERT INTERMITTANT. ALERT ACT IVE FOR APROX 1-2 MIN INITIALLY & OFF 2-3 MIN ALERT ON & OFF 30 SEC - 1 MIN FOR DURATION OF FLIGHT, REPEAT WRITE-UP. A/ C RETURNED TO CHA AFTER T/O. EMERGENCY DECLARED. FLT 4126 CX. 2 H 7 2 4T RT 2007060700050 20070607 00050 SO 2007 6 7 RAIA00705049 1 20070526 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 818HK 145059 POST FLT NR 5488 - STL - EMERGENCY LIGHT LEFTHAND EMERGENCY DOOR FLOOD LIGHT IS OUT. MAINTENANCE REMOVED AND REPLACED B ULB AT 13A PSU PANEL FOUND TO BE GOOD AT THIS TIME. 2 L 7 2 4T RT T00011AT 2007060700053 20070607 00053 NM 2007 6 7 DHL2007740511 1 20070522 A 5330 SKIN BOEING 727 7272Q9 138448M NM FUSELAGE BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 L-2 LOWER HINGE ARM SKIN IS BROKEN AT FWD END. REMOVED SKIN SECTION IAW B727 SRM 51-30-2. FAB`D NEW SKIN FROM 2024-T3 0.050" PO NR 9005049 DIM 9"BY 1 1/2" IAW B727 SRM 52-40-1 FIG 4 ANH 51-20-1. TREATED AND PRIMED NEW PART IAW B727 SRM 5 1-10-2 AND INSTALLED NEW SKIN SECTION AT L-2 DOOR LOWER HINGE ARM IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007060800011 20070608 00011 NM 2007 6 8 QXEA200700887 1 20070524 A 5347 CARGO TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 C4 PDX - AT X781 Z100 Y9R, THE TRACK HOLD DOWN CLEAT IS CORRODED. REPAIRED IAW RD8/4-53-884, SRM 51-40-15 AND 51-42-05. 2 H 7 2 4T RT A13NM 2007060800014 20070608 00014 NM 2007 6 8 QXEA200700878 1 20070603 A 2120 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM GALLEY ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 426QX 4154 PDX: FA REPORTS STRANGE CHEMICAL ODOR IN AFT GALLEY. MAINTENANCE INSPECTED AND DETERMINED ODOR TO BE THAT OF NEW A/C MA NUFACTURER ODOR. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007060800018 20070608 00018 WP 2007 6 8 DHL2007803507 1 20070526 A 5711 FRAME DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 RT WING CTR L/E UPPER FORMER CRACKED, STA XFS 397.750. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. PERFORMED STOP HOLE AND FABRICATED (2EA) DOUBLERS (AL7075T6 0.032" / 0.040") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLERS IAW SRM 51-1-8B. INSTALLED DOUBLERS IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007060800030 20070608 00030 NM 2007 6 8 QXEA200700881 1 20070602 A 3620 8209074 SWITCH BOMBDR DHC8 DHC8402 1390042 NM NR 2 OVER TEMP MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 420QX 761 761 4147 BOI FLIGHT NR 2407: NR 2 BLEED HOT CAUTION LIGHT ILLUMINATED. C/W CHECK LIST AND SELECTED THE NR 2 BLEED SWITCH OFF. M AINTENANCE REMOVED AND REPLACED NR 2 OVER TEMP SWITCH IAW AMM 36-11-16, PG 401-406. GROUND RUN CHECKS GOOD. AIRCRAFT R ETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007060800042 20070608 00042 NM 2007 6 8 DHL2007740520 1 20070604 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 1070 S28-29L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 WHILE IN "C" CHECK, AFT CARGO BS 1070 STR 28L-29L FWD FRAME FLANGE HAS CORROSION. REMOVED CORROSION IAW B727 SRM 51-10- 6. REMOVED FASTENERS TO GAIN ACCESS TO AREA IAW B727 SRM 51-30-2. ORIGINAL MAT .063 IAW B727 SRM 53-10-2 FIG 5, MAT LOS S .008, REMAINING MAT .055. FOUND OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. CUTOUT DAMAGED AREA DIM 5 1/4" BY 4" IAW B7 27 SRM 53-10-4 FIG 11. FABRICATED NEW SHEAR TIE (CONTINUE ON NR 053972) FROM 7075T6 .071 PO NR 9004940 DIM 5 1/4" BY 4" IAW B727 SRM 53-10-4 FIG 11 AND 53-10-2 FIG 5. TREATED AND PRIMED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2 AND I NSTALLED SHEAR TIE REPAIR AT AFT CARGO BS 1070 STR 28L - 29L IAW SRM 53-10-4 FIG 11 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007060800044 20070608 00044 NM 2007 6 8 DHL2007740505 1 20070516 A 5754 RIB BOEING 727 7272Q9 138448M NM NR 3 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 NR 3 SLAT I/B ACTUATOR ROD ATTACH RIB IS CRACKED. REMOVED NR 3 RIB SLAT I/B ACTUATOR ROD CRACKED IAW B727 SRM 51-30--2. INSTALLED NEW RIB P/N 65-17294U13, PO NR 721255 AT SLAT I/B ACTUATOR ROD IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007060800047 20070608 00047 NM 2007 6 8 DHL2007740506 1 20070516 A 5753 SKIN BOEING 727 7272Q9 138448M NM LT WING TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 LT I/B MID FLAP UPPER SURFACE DELAM 36" FROM O/B END. REMOVED DAMAGED AREA APPROX 6 3/4" BY 4" BY 4 1/4" CLEANED AN PRE PPED AREA TO BOND, FABBED FILLER (6 3/4"X 4 1/4") AND FILLER 2 EACH 3" BY 4 1/4" FROM .016 7075-T6 PO NR 9003988, ANODIZ ED, PRIMED AN APPLIED ADHESIVE FILM IAW B727 SRM 51-40-20 PAR 7, FIG 3 AND 57-50-2 FIG 3. INSTALLED REPAIR PARTS, CURED AND FINISHED REPAIR AREA IAW B727 SRM 51-40-20 PAR 20, 22 AND 51-40-24 FIG 3. 2 L 7 3 4F RT A3WE 2007060800064 20070608 00064 NM 2007 6 8 DLM88070652 1 20070529 A 5313 LONGERON DOUG MD88 MD88 3023688 NM STA 160 L25L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACK ON LONGERON 25 LT AT STA 160. INSTALLED NEW SECTION OF LONGERON IAW SRM 53-02 FIG 18. 2 L 7 2 4F RT A6WE 2007060800070 20070608 00070 NM 2007 6 8 DLM88070661 1 20070530 A 5230 STRUCTURE DOUG MD88 MD88 3023688 NM CARGO DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACK IN FWD SECTION OF MID CARGO COMPARTMENT DOOR AREA OF LOCK PINS. CRACK STOP DRILLED. NO CRASKS FOUND PAST STOP DR ILL IAW NDT SPM 06-10-01-001. REPAIR DOUBLER FABRICATED AND INSTALLED IAW SRM 52-05 FIG 26A NR T0057058. 2 L 7 2 4F RT A6WE 2007060800072 20070608 00072 NM 2007 6 8 DLM88070662 1 20070530 A 5320 WEB DOUG MD88 MD88 3023688 NM BS 1474-1485 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACKED UPPER WEB BETWEEN STA 1474 TO 1485 AT AFT ACCESSORY COMPARTMENT. REFABRICATED NEW WEB IAW SRM 53-34-0 FIG 7. WEB INSTALLED IAW SRM 51-30-2 AND SRM 53-34-0 FIG 7 NR T0057062. 2 L 7 2 4F RT A6WE 2007060800075 20070608 00075 NM 2007 6 8 DLM88070665 1 20070530 A 5320 STEP DOUG MD88 MD88 3023688 NM BS 1497-1510 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CRACKS ON RT UTILITY STEP BETWEEN STA 1497 CANTED AND 1510 CANTED. CRACKS STOPPED PER SRM 53-01 FIG 2 SHEET 4. DOUBLER FABRICATED REF SRM 53-01 FIG 2. DOUBLER AND SUPPORT INSTALLED REF SRM 51-30-2 NR T0056531. 2 L 7 2 4F RT A6WE 2007060800080 20070608 00080 NM 2007 6 8 DLM88070670 1 20070530 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 457-476 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 CORRODED LOCK FASTENERS ON FUSELAGE SKIN DOUBLER STA 457-476, LONGERONS 23-25 RT. FASTENERS REPLACED IAW SRM 51-30-5 NR T0056026. 2 L 7 2 4F RT A6WE 2007060800086 20070608 00086 NM 2007 6 8 QXEA200700880 1 20070604 A 3620 SWITCH BOMBDR DHC8 DHC8402 1390042 NM BLEED OVERTEMP MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION TO TAKEOFF 1 NM 09 424QX 1221 1221 4006 PSC FLIGHT: NR 1 BLEED HOT CAUTION LIGHT AFTER TAKEOFF. C/W EA CHECKLIST. MAINTENANCE INTERROGATED CDS AND FOUND FAULT CODE 7001L BLD OVR TMP IN ECS. REPLACED BLEED OVERTEMP SWITCH IN LT NACELLE IAW TASKS 36-11-16-000-801 AND 36-11-16-40 0-801. ACCOMPLISHED TASK 36-11-00-710-802, OPS TEST OF BLEED AIR SYSTEM. TESTED GOOD. NO REOCCURRENCE OF FAULTS. NR 1 BLEED HOT CAUTION LIGHT REMAINED EXTINGUISHED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007060800117 20070608 00117 NM 2007 6 8 SWAA072832 1 20070605 A 3040 CONTROLLER BOEING 737 7375H4 138449D NM COCKPIT ARCED A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 525SW 26567 FLIGHT COMPARTMENT L2 WINDOW ARCING. REMOVED AND REPLACED L2 WINDOW AND WINDOW HEAT CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 2007060800121 20070608 00121 NM 2007 6 8 SWAA072834 1 20070605 A 5330 6545890 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT AFT UPPER CORNER. REPAIRED SKIN P ER ER. 2 L 7 2 4F RT A16WE 2007060800129 20070608 00129 SO 2007 6 8 C2XA07RI044 1 20070605 A 3350 110049 CHARGER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 26545 145558 EWR - DURING SCHEDULED MAINTENANCE, MX FOUND COCKPIT DOOR EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED NR 1 BATTERY CH ARGER IAW EMB 145 AMM 33-50-04 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007060800153 20070608 00153 EA 2007 6 8 VNAA0705005 1 20070518 A 3150 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 GENERATOR UNKNOWN A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 221PS 7889 CREW REPORTED A NR 2 GENERATOR OFF MESSAGE ILLUMINATED DURING TAKEOFF. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WI THOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED AN OPERATIONAL TEST OF THE NR 2 ENGINE GENERATOR IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 24-11-00-861-801. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007060800160 20070608 00160 NM 2007 6 8 SWAA072848 1 20070605 A 5311 6546547 FRAME BOEING 737 7373H4 1384600 NM BS 727 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060800173 20070608 00173 NM 2007 6 8 HNAA0700095 1 20070530 A 3230 IN4004 DIODE DHAV DHC8 DHC8102 2809003 NM MLG ACTIVE A HNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 07 809EX 302 AFTER GEAR RETRACTION RECEIVED AN AMBER LEFT GEAR DOOR LIGHT. CYCLED GEAR RESULTING IN LEFT GEAR DOOR LIGHT ILLUMINATED MOMENTARY, THEN EXTINGUISHED. THEN LANDING GEAR INOP C/L. RETURNED TO FIELD. REMOVED AND REPLACED DIODE 3261-CR3. O PS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007061200110 20070612 00110 NM 2007 6 12 CALA0700276 1 20070601 A 5330 654576987 SKIN BOEING 737 7373T0 1384582 NM BS 480-500B CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND MOUNTING SKIN SURFACE FOR NR 2 COMM ANTENNA CORRODED AT STA 480-500B, S28L TO S28R. THE SKIN WAS REPAI RED IAW ECRA 5331-01316. 2 L 7 2 4F RT A16WE 2007061200111 20070612 00111 NM 2007 6 12 CALA0700277 1 20070601 A 5311 6546555 FRAME BOEING 737 7373T0 1384582 NM BS 867 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT STA 867, S8L-9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04636. 2 L 7 2 4F RT A16WE 2007061200115 20070612 00115 NM 2007 6 12 CALA0700281 1 20070601 A 5311 6546551 FRAME BOEING 737 7373T0 1384582 NM BS 807 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT STA 807 BETWEEN STRINGER 8L AND 9L. THE FRAME WAS REPAIRED IAW E CRA 5310-04636. 2 L 7 2 4F RT A16WE 2007061200116 20070612 00116 NM 2007 6 12 CALA0700282 1 20070601 A 5311 6546557 FRAME BOEING 737 7373T0 1384582 NM BS 887 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT STA 887 BETWEEN STRINGER 8R AND 9R. THE FRAME WAS REPAIRED IAW E CRA 5310-04636. 2 L 7 2 4F RT A16WE 2007061200118 20070612 00118 NM 2007 6 12 CALA0700284 1 20070601 A 5311 6546555 FRAME BOEING 737 7373T0 1384582 NM BS 867 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT STA 867 BETWEEN STRINGER 8R AND 9R. THE FRAME WAS REPAIRED IAW E CRA 5310-04636. 2 L 7 2 4F RT A16WE 2007061200119 20070612 00119 NM 2007 6 12 HNAA0700097 1 20070508 A 5320 85320686101 THRESHOLD DHAV DHC8 DHC8102 2809003 NM CORRODED CORRODED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 938HA 152 PASSENGER DOOR ENTRANCE LOWER STRIP FOUND CORRODED. PASSENGER DOOR ENTRANCE LOWER STRIP THRESHOLD MEMBER REPLACED WITH NEW PART INSTALLED WITH SOLID RIVETS IAW SRM 51-40-00. 2 H 7 2 4T RT A13NM 2007061200120 20070612 00120 EU 2007 6 12 YENA2007039 1 20070529 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS NO TEST A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 503JB 17590 1123 UPON TEST L1 & R1 EMERGENCY LIGHTS DID NOT WORK. REPLACED POWER SUPPLY IAW AMM 33-51-38-04. OPS CHECK NORMAL UPON TEST . 2 L 7 2 4F RT A28NM 2007061200127 20070612 00127 NM 2007 6 12 NOCA10707 1 20070505 A 2560 P4010021 BATTERY BOEING 757 75728A 1384976 NM FLASHLIGHT INOPERATIVE A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 756NA 32448 FLIGHT ATTENDANT FLASHLIGHT AT DOOR 2L INOP. REPLACED FLASHLIGHT BATTERY AS REQ'D, OPS CHECKS NORMAL. 2 L 7 2 4F RT A2NM 2007061200128 20070612 00128 NM 2007 6 12 NOCA10607 1 20070503 A 2611 2156604 DETECTOR BOEING 767 767324 1385203 NM CARGO BAY MALFUNCTIONED A NOCA K NONE N FALSE WARNING IN INSP/MAINT 1 EA 15 767NA 27569 THE FWD CARGO DETECTOR MESSAGE ILLUMINATED ON EICAS DURING TEST. T/S PER FIM 26-16-00 FIG 108. REPLACED FWD CARGO DETE CTOR UNIT, OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 2007061200130 20070612 00130 NM 2007 6 12 CALA0700285 1 20070601 A 5311 6546554 FRAME BOEING 737 7373T0 1384582 NM BS 847 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT STA 847 BETWEEN STRINGER 8R AND 9R. THE FRAME WAS REPAIRED IAW E CRA 5310-04636. 2 L 7 2 4F RT A16WE 2007061200131 20070612 00131 NM 2007 6 12 CALA0700286 1 20070601 A 5311 6546532 FRAME BOEING 737 7373T0 1384582 NM BS 480 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT STA 480 BETWEEN STRINGER 8L AND 9L. THE FRAME WAS REPAIRED IAW E CRA 5310-04636. 2 L 7 2 4F RT A16WE 2007061200132 20070612 00132 NM 2007 6 12 CALA0700287 1 20070601 A 5311 654795978 FRAME BOEING 737 7373T0 1384582 NM BS 947 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND A 5 INCH CRACK IN AFT CARGO DOOR CUTOUT FORWARD FRAME AT LOWER DOOR STOP AREA, STA 947.5, S16R-26R. TH E FRAME WAS REPLACED IAW SRM 51-40-02 AND BOEING DRAWING 65-20723, AND ECRA 5311-01323. 2 L 7 2 4F RT A16WE 2007061200133 20070612 00133 NM 2007 6 12 CALA0700288 1 20070603 A 5314 65C385022 KEELBEAM BOEING 737 7373T0 1384582 NM BS 537 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND RIGHT KEELBEAM CORRODED JUST INSIDE A/C BAY AT STA 537. THE KEELBEAM WAS REPAIRED IAW SRM 53-60-12. 2 L 7 2 4F RT A16WE 2007061200134 20070612 00134 2007 6 12 YENA2007050 4 20070607 A 2330 LSEBUTK1400101 ENTERTAIN SYS AIRBUS 320 A320232 3930326 EU LIVE TV ODOR A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 581JB 978 2141 FLT NR 190, LAS-JFK, BETWEEN 01:00-3:50Z AM, SMELLED SMOKE AT ROW 20, TURNED OFF LTV MASTER AND ODOR DISSIPATED. ACCOMP LISHED TSM 25-39-00-810-801. FOUND XEB AT 19 DEF WITH A STRONG POTENT BURNING ODOR. REMOVED AND REPLACED XEB AT 19DEF PER LTV MM 44-20-17. NO OTHER DISCREPANCIES NOTED. A/C OK FOR CONTINUED SERVICE. 2 L 7 2 4F RT A28NM 2007061200139 20070612 00139 EU 2007 6 12 07FDEA02105 1 20070611 A 5730 A57340088 SKIN PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 OLD REPAIR (BLEND OUT ) ON LT WING BOTTOM SKIN LOWER SURFACE AROUND HOLE 389 IAW DRW R571-40141 SH 17 REPAIR ACCEPTACLE BY AI RAS/BAE/1004818/2007 ISS. A, APPROVED BY EA 6-5720-106454. 2 L 7 2 4F RT A35EU 2007061200140 20070612 00140 NM 2007 6 12 07FDEA02107 1 20070611 A 5311 651768526 FRAME BOEING 727 7272S2F 1384O81 NM BS 348 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 FS 348.2 6 INCHES ABOVE UPPER AFT DOOR STOP HAS A DRILL START ON FUSELAGE FRAME FOUND DURING REMOVAL OF COVER TO WORK DO OR STOP FITTING. INSTALLED FABRICATED REPAIR ANGLE REF SRM 51-40-3 VERIFIED MATERIAL 2024 .080 (O), HEAT TREATED ANGLE, FABRICATED VERIFIED MATERIAL FOR CLIP REF BAC1514-518. HEAT TREATED CLIP FORM TRACKING NR 2007-05-125. INSTALLED CLIP REF SRM 51-10-2 REF W/C, 53101127. 2 L 7 3 4F A3WE 2007061200150 20070612 00150 NM 2007 6 12 AWXA200700711 1 20070529 A 5315 140N250532 FLOORBEAM BOEING 757 757225 1384959 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 MCN - CRACKED CABIN FLOORBEAM WEB CLIP, BS 780 - BS 800, BL0, WL 208.1. REPLACED CABIN FLOORBEAM WEB CLIP, BS 780 - BS 800, BL0, WL 208.1 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007061200151 20070612 00151 2007 6 12 A6WA200740227 4 20070513 A 3425 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AHRS MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 417AW 7610 AFTER TAKEOFF, ROLL AND PITCH INDICATION ON CAPTAINS F/O ATTITUDE INDICATOR CAME ON, FOLLOWED QRH AND RETURNED TO MKE CA PTS PITCH PLUS 7 DEGREES OVER FIRST OFFICER BANK 5-10 DEGREE. REPLACED CAPTAINS AHRS COMPUTER IAW CRJ AM 34-21-01. OPS TEST FOUND SATISFACTORY, FOUND SERVICEABLE. (M) 2 L 7 2 4F RT A21EA 2007061200152 20070612 00152 EA 2007 6 12 A6WA200740228 1 20070510 A 3232 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA NLG DOOR OUT OF RIG A A6WA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 31 407AW 7424 UNUSUAL REPETITIVE NOISE AFTER GEAR RETRACTION. NOISE PERSISTED UNTIL GEAR EXTENSION, REPETITIVE PUMPING. TROUBLESHOOT ING REVEALED R-NOSE DOOR ACTUATOR OUT OF RIG. (M) 2 L 7 2 4F RT A21EA 2007061200157 20070612 00157 EA 2007 6 12 CHQA200700023 1 20070609 A 3222 STRUT CNDAIR CL600 CL6002B19 1900309 EA NLG DISCHARGED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 642BR 7356 FLIGHT 3338 - CLE-PVD - AFTER TAKEOFF, RECEIVED 'GEAR DISAGREE' AND 'STEERING INOP' MASTER CAUTION MESSAGES. AFTER CLIM B-OUT AT 5000 FT, RAN QRH AND DETERMINED THE NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. SELECTED GEAR LEVER TO DOWN POSIT ION. DECLARED AN EMERGENCY WITH ATC. LANDED WITHOUT INCIDENT. MAINTENANCE FERRIED TO SDF. FOUND NOSE STRUT NOT EXTEN DING AND NOT SERVICED WITH NITROGEN. SERVICED STRUT AND PERFORMED GEAR SWINGS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007061200159 20070612 00159 NM 2007 6 12 AWXA200700713 1 20070418 A 5311 65465548 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - CRACKED FRAME, BS 847, S9L. REPAIRED FRAME, BS 847, S9L IAW AWA ER 03-5311-07143-ES1. 2 L 7 2 4F RT A16WE 2007061200160 20070612 00160 NM 2007 6 12 AWXA200700714 1 20070419 A 5330 655298878 SKIN BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - CRACKED FUSELAGE SKIN, BS 960, WL 211. REPAIRED FUSELAGE SKIN, BS 960, WL 211 IAW B737-300 SRM 53-60-01-2R3, FIGU RE 201. 2 L 7 2 4F RT A16WE 2007061200161 20070612 00161 NM 2007 6 12 F3LA200700129 1 20070530 A 5320 D5348015800600 PLATE AIRBUS A319 A319111 3930336 NM CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 920FR 5184 1997 DURING C-3 CHECK, INSPECTION REPORTED BLANKING PLATE FOR GIRT BAR FITTING ON FWD SIDE OF L-2 DOOR CORRODED. REPLACED GI RT BAR BLANKING PLATE IAW AMM 52-12-400-003. 2 L 7 2 4F RT A28NM 2007061200163 20070612 00163 EA 2007 6 12 A6WA200740197 1 20070415 A 5210 ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 454AW 7842 PAX DOOR ANGLE CRACKED APPROX .5 INCH LONG. (M) MAINTENANCE CUT OUT DAMAGED SECTION OF ANGLE AND INSTALLED REPAIR ANGL E AND DOUBLERS IAW REO 601R-52-11-513, REV A. (K) 2 L 7 2 4F RT A21EA 2007061200165 20070612 00165 NM 2007 6 12 AWXA200700707 1 20070604 A 5320 D53471124201 SHEAR PLATE AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 SAL - FOUND CORROSION ON CABIN SHEAR PLATE, FR 69 - FR 70, -Y1162. REPLACED CABIN SHEAR PLATE, FR 69 - FR 70, -Y1162 IA W A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007061200166 20070612 00166 NM 2007 6 12 AWXA200700710 1 20070608 A 5315 D53472189204 FLOORBEAM AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 SAL - CORROSION ON CABIN FLOORBEAM, FR 67 + 18", -Y1162. REPLACED CABIN FLOOR BEAM, FR 68 - FR 69, -Y1162 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007061200168 20070612 00168 EA 2007 6 12 A6WA200740230 1 20070514 A 2840 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA RT FUEL TANK FAULTED A A6WA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 31 446AW 7806 IN FLIGHT RECEIVED FUEL IMBALANCE MESSAGE. RIGHT TANK QUANTITY AND TOTAL FUEL QUANTITY SHOW DASHED LINES. PERFORMED AI R DIVERSION TO ALB. REMOVED AND REPLACED FUEL SYSTEM COMPUTER, IAW AMM 28-41-16. OPS CHECK GOOD. PERFORMED OPS TEST O F TRANSFER SYSTEM, IAW AMM 28-13-00, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007061200170 20070612 00170 NM 2007 6 12 07FDEA02096 1 20070609 A 5320 6580656 WEB BOEING 727 727233 138408A NM ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AGING A/C INSP. FOUND REPAIR LOCATED AT BS 620 FWD LOWER CARGO DOOR AFT FRAME FWD SURFACE UPPER CORNER, HAS ADDITIONAL D AMAGE ON AFT SIDE. REMOVED EXISTING REPAIR REF SRM 51-30-2. BLENDED DAMAGE AREA, ORG. THICKNESS .071, AFTER BLENDING , THICKNESS .064" TO .068". WITHIN LIMITS PER REF SRM 53-10-1 PG 2. MANUFACTURED NEW DOUBLER REF SRM 51-10-2. INSTALL ED DOUBLER AND FASTENERS SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007061200176 20070612 00176 EU 2007 6 12 07FDEA02102 1 20070610 A 5347 R5327049020000 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 662FE 761 MAIN CABIN COMPT BETWEEN FR 65 AND FR 68, 37" RIGHT OF BL SEAT TRACK CORRODED REMOVED CORROSION IAW A300-600 SRM 51-73-1 0, ORIGANAL THICKNESS.136. REMAINING .086. REMOVED .048 FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-16 FIG 102. R EMOVED SEAT TRACK BETWEEN FR 65 AND FR 68 IAW A300-600 SRM 51-40-21MATERIAL ID FOR SEAT TRACK P/N A532740050053 PO NR 57 5719 IAW A300-600 SRM 53-10-16. LOCATED AND DRILLED HOLES IAW A300-600 SRM 51-40-44. PRIMED NEW SEAT TRACK IAW A300-60 0 SRM 51-21-10. PAINTED NEW SEAT TRACK IAW A300-600 SRM 51-23-10. INSTALLED NEW SEAT TRACK IAW A300-600 SRM 53-10-16 F IG 201. 2 L 7 2 4F RT A35EU 2007061200182 20070612 00182 WP 2007 6 12 ARWA20070602 1 20070605 A 2710 BYPASS VALVE DOUG DC8 DC863F 302198F WP BROKEN A ARWA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 441J 45988 AILERON MANUAL REVERSER LIGHT STAYS ON WHILE AILERON IS POWERED AND CONTROL CHECK UNSATISFACTORY. REMOVED AND REPLACED BROKEN BYPASS VALVE TURNBUCKLE AND ADJUSTED AILERON POWER TO MANUAL REVERSION MECHANISM IN ACCORDANCE WITH DC-8 M/M 27-1 1-8; OPERATIONAL CHECK FOUND NORMAL IN ACCORDANCE WITH DC-8 M/M 27-10-0. 2 L 7 4 4F 4A25 2007061200183 20070612 00183 NM 2007 6 12 ARWA20070603 1 20070606 A 7930 VILOC4F VALVE DOUG DC10 DC1040F 3023507 NM NR 3 ENGINE OIL UNKNOWN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 140WE 46920 3 IDLE OIL PRESSURE 23 PSI. REMOVED AND REPLACED NR 3 ENGINE OIL PRESSURE FILTER ADJUSTED OIL PRESSURE RELIEF VALVE IN ACCORDANCE WITH DC-10 M/M 71-00-01. PERFORMED ENGINE RUN OPERATIONAL NORMAL IN ACCORDANCE WITH 71-00-00. 2 L 7 3 4F RT A22WE 2007061200184 20070612 00184 WP 2007 6 12 ARWA20070604 1 20070607 A 3150 UNKNOWN DOUG DC8 DC863F 302198F WP ANTI SKID SYS UNKNOWN A ARWA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 441J 45988 BEFORE TAKEOFF ANTI-SKID INOPERATIVE LIGHT PLUS RAI (F/W) LIGHTS BOTH ILLUMINATED. 2 L 7 4 4F 4A25 2007061200190 20070612 00190 NM 2007 6 12 DL76L070701 1 20070608 A 8011 774860A4 STARTER BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE UNSERVICEABLE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 194DN 28451 724178 AFTER SHUTDOWN FOR 45 MINUTES LEFT ENGINE START VALVE WOULD NOT OPEN. VALVE LIGHT STAYED ILUMINATED. TRIED WITH APU AN D CROSS BLEED. FOUND NR 1 ENG STARTER BAD REPLACED SAME. ALSO, FOUND START VALVE INTERMITTENT. REPLACED SAME, OPS AND LEAK CKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007061200191 20070612 00191 NM 2007 6 12 DL76L070702 1 20070608 A 2530 OVEN BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE GALLEY CONTAMINATED A DALA H DEACTIVATE SYST/CIRCUITS W INADEQUATE Q C CR CRUISE 1 SO 27 185DN 27961 724178 F/A REPORTED UNUSUAL ODOR IN AFT GALLEY AREA LEAD F/A AND RELIEF PILOT BELIVED RELATED TO HEATED DEBRIS CONTENTS OF OVEN OPERATION. SMELL DISAPPEARED WHEN OVEN AND CHILLERS BREAKERS ISOLATED. ALL AFT GALLEY ELECTRICAL COMPONENTS THROUGHLY INSPECTED NIL DEFECT FOUND. C/BS CLOSED AND ALL ELECTRICAL COMPONENT MONITORED IN OPERATION DURING 15 MN, NO PARTICULA R SMELL NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007061200193 20070612 00193 NM 2007 6 12 DL76G070704 1 20070609 A 8011 7755507 STARTER BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 1 ENGINE INOPERATIVE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 173DZ 29692 704738 NR N2 ROTATION NR 1 ENG. REMOVED AND REPLACED NR 1 ENG STARTER AND START VALVE PER M/M OPN NML. 2 L 7 2 4F 4 F RT A1NM E13NE 2007061200194 20070612 00194 NM 2007 6 12 DL757070709 1 20070610 A 2560 P4010021 BATTERY BOEING 757 757232 1384965 NM FLASHLIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 669DN 25142 F/C EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY. 2 L 7 2 4F RT A2NM 2007061200195 20070612 00195 NE 2007 6 12 DL76G070710 2 20070611 A 7200 ENGINE BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6 30025 NE NR 2 UNKNOWN A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 1501P 45452 12047 24983 695373 RTB - RIGHT ENGINE NR 2 ENGINE FUEL CONTROL VALVE LIGHT. NO START VALVE EXCERCISED BY OPERATING FIRE HANDLE. ENGINE GR OUND RUN CARRIED OUT. NIL DEFECTS. 2 L 7 2 4F 4 F RT A1NM E13NE 2007061200197 20070612 00197 EU 2007 6 12 07FDEA01890 1 20070521 A 5754 SKIN AIRBUS 310 A310322 3930334 EU NR 3 SLAT MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON LT WING, L/E OF SLAT 3 WS 1835-1868 RIB 30-31. REPAIR REQUIRES EVALUATION FOR MAJOR/MI NOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 57-44-11 FIG 201, SHEET 2 AND 3. 2 L 7 2 4F RT A35EU 2007061200198 20070612 00198 EU 2007 6 12 07FDEA01915 1 20070521 A 5230 SKIN AIRBUS 310 A310222 3930315 EU CARGO DOOR MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON INNER SKIN OF LOWER AFT CARGO COMP´T DOOR ON FR 60 BETWEEN LONGERON 1-2. REPAIR REQUIR ES EVALUATION FOR MAJOR /MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUAT ED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED IN ACCORDANCE WITH FEDEX ENGINEERING AUT HORIZATION 6-5230-112412. 2 L 7 2 4F RT A35EU 2007061200200 20070612 00200 2007 6 12 HALA0700242 4 20070604 A 3100 4077880908 DISPLAY BOEING 767 767332 1382001 NM COCKPIT INOPERATIVE A HALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 13 597HA 23277 ATB: CAPT'S CDU DISPLAY BLANK, SELECTING ALT FMC SOURCE DID NOT CORRECT FAULT. CDU DISPLAY CAME ON AFTER LANDING. REMO VED AND REPLACED NR 1 MCDU GRD, OPS CK OKAY PER AMM 34-61-02. 2 L 7 2 4F RT A1NM 2007061200202 20070612 00202 NM 2007 6 12 KNNA200700032 1 20070429 A 5330 SKIN BOEING 737 7372Q8 138448K NM PWA JT8 JT8D217 52053 NE BS 777 DAMAGED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 413JG 23148 LOWER LOBE/FUSELAGE SKIN SHOWS SIGNS OF HAVING LOOSE ATTACH RIVETS FROM BSTA-777 BBL-0. FOUND CORROSION AT FASTENER REM OVAL, ACO NR 075380. PROVIDE INSTRUCTIONS ON REPAIR OF SKIN AT BS-777,FROM STR-27L TO STR-27R SRM 53-30-3 FIGURE 5. 2 L 7 2 4F 4 F RT A16WE E9NE 2007061300002 20070613 00002 NM 2007 6 13 QXEA200700903 1 20070607 A 2930 ACCUMULATOR BOMBDR DHC8 DHC8402 1390042 NM HYD SYSTEM LOW A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 419QX 4145 PDX FLIGHT NR 2419, AFTER PUSHBACK, DURING NR 3 ISO VALVE TEST, OBSERVED INTERMITTENT NR 3 HYD CAUTION LIGHT PRESS FLUCT UATION ON NR 3 HYD SYSTEM +- 1800-2600 PSI. AIRCRAFT RETURNED TO GATE. MAINTENANCE, WHILE TROUBLE SHOOTING, FOUND SYST EM 3 AND DCMP BOOT STRAP ACCUMULATORS LOW. SERVICED BOTH ACCUMULATORS IAW SERVICING PLACARDS. ALSO, BLED SYSTEM 3 HYD SYSTEM IAW AMM 29-10-00-870-005. OPS CHECK GOOD IAW AMM 29-12-01-710-801. NO PARTS REPLACED. AIRCRAFT RETURNED TO SER VICE. 2 H 7 2 4T RT A13NM 2007061300003 20070613 00003 NM 2007 6 13 QXEA200700905 1 20070607 A 6123 AUTOFEATHER SYS BOMBDR DHC8 DHC8402 1390042 NM PROPELLER FAULTED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 405QX 4047 PDX FLIGHT NR 2296: ON TAXI, 'AUTO FEATHER SELECT' DID NOT APPEAR ON ED. MAINTENANCE INTERROGATED CDS, FOUND FAULT CODE 64A FOR AUTO FEATHER SELECT BUTTON. C/W AUTO FEATHER SELECT. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061300004 20070613 00004 CE 2007 6 13 GUUA05060702 1 20070506 A 5520 1016200111BW HINGE BRACKET BEECH 1900 1900D 1154162 CE ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 82539 UE168 REPORT: AT SCHEDULED ROUTINE MAINTENANCE LEFT OUTBOARD ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED LEFT OUTBOARD ELEVATOR HINGE BRACKET. 2 L 7 2 4T RT A24CE 2007061300009 20070613 00009 SW 2007 6 13 PNSA070506 1 20070530 A 3250 SWITCH FRCHLD SA227 SA227DC 3377521 SW NLG STEERING UNKNOWN A PNSA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 AL 03 892DC DC892B DURING BEFORE LANDING, CONFIRMED GEAR WAS DOWN, HOWEVER AFTER PRESSING THE NWS BUTTON ON THE POWER LEVER THE NWS FAIL LI GHT BEGAN FLASHING. DECIDED NOT TO LAND 25R BECAUSE OF THE X-WIND, WENT AROUND AND WAS REVECTORED FOR LANDING 14. REMO VED AND REPLACED POWER LEVER SWITCH. 2 L 7 2 4T RT A18SW 2007061300010 20070613 00010 CE 2007 6 13 GUUA05080701 1 20070508 A 3230 571302 MOTOR BEECH 1900 1900D 1154162 CE MLG INOPERATIVE A GUUA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 29 87552 UE216 FLIGHT: 9159 VPS/TPA - DURING APPROACH, LANDING GEAR WOULD NOT COME DOWN WHEN EXTENDED. MANUALLY EXTENDED LANDIND GEAR. REPLACED LANDING GEAR POWER PACK MOTOR. OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY. 2 L 7 2 4T RT A24CE 2007061300011 20070613 00011 CE 2007 6 13 AMWA84511BC 1 20070509 A 2432 CHARGER BEECH 1900 1900D 1154162 CE WARNING LIGHT A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 133YV UE133 BATTERY CHARGER ANNUNCIATOR ILLUMINATED IN FLT. ACFT LANDED WITH NO FURTHER INCIDENT. THIS BATTERY CHARGER ANNUNCIATOR ILLUMINATED WRITEUP IS CONSIDERED A NUISANCE AND A SEVERE DISTRACTION TO THE PILOTS. PARALLELED GENERATORS. 2 L 7 2 4T RT A24CE 2007061300015 20070613 00015 CE 2007 6 13 GUUA05110701 1 20070511 A 3234 1013841377 CONTROL HANDLE BEECH 1900 1900D 1154162 CE MLG FAILED A GUUA O OTHER O OTHER AP APPROACH 1 SO 29 87551 UE206 FLIGHT: 9181 PNS/FLL - DURING APPROACH, NOSE GEAR WOULD NOT EXTEND AND CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER NO SE GEAR EXTENDED BUT CIRCUIT BREAKER POPPED AGAIN. REPLACED LANDING GEAR CONTROL HANDLE. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 2007061300020 20070613 00020 CE 2007 6 13 AMWA06033A 1 20070510 A 5711 1181000136 SPAR CAP BEECH 1900 1900D 1154162 CE WING CORRODED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 142ZV 22220 UE142 BIO - CORROSION RT LOWER SPAR CAP AT WS 124. REPAIRED IAW ENGINEERING AUTHORIZATION REPAIR DWG 1900D142-7 REV 1R. 2 L 7 2 4T RT A24CE 2007061300023 20070613 00023 CE 2007 6 13 DXTA200702189 1 20070513 A 2150 72828433 ACM CESSNA 750 750 2076810 CE AFT SERVICE BAY FROZEN E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 07 908QS 1487 1487 7500108 AFTER LANDING, COCKPIT TEMP INDICATOR ROSE TO 250 DEGREES AND BLACK SMOKE FILLED THE COCKPIT. COCKPIT TEMP WAS UNCONTRO LLABLE THE LAST 30 MINUTES OF THE FLT WITH COCKPIT TEMP AT 150*, REST FLT, LEFT PAC VERY HOT. KPWM TO KSFO. ON GROUND AT KSFO, REPLACED ACM WITH OVERHAULED UNIT. LEAK AND OPERATIONAL CHECK NORMAL IAW CESSNA 750 MM 21-51-00. ACM OVERHAUL ED BY HAMILTON SUNSTRAND. CERT NO SI3R842L. 2 L 7 2 4J RT T00007WI 2007061300027 20070613 00027 NM 2007 6 13 DU4R2007124 1 20070514 A 5313 STRINGER BOEING 757 757232 1384965 NM BS 1681 S29R CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 602DL 22809 FOUND STRINGER 29R AT BS 1681 CORRODED. REPAIRED CORROSION ON STRINGER S-29R AT BS 1681 BY CUTTING OUT AND REMOVING COR RODED SECTION OF STRINGER BS 1670 TO BS 1720 IAW B757 SRM 53-00-53 AND 51-40-02. FABRICATED AND INSTALLED STRINGER SECT ION 50 BY 3 REPAIR FROM BAC1498-144 IAW B757 SRM 51-20-01, 51-40-02 AND 53-00-53. 2 L 7 2 4F RT A2NM 2007061300031 20070613 00031 CE 2007 6 13 DXTA200702170 1 20070502 A 2797 CONNECTOR CESSNA 560 560XL 2076702 CE SPEEDBREAK CORRODED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 681QS 5605181 DURING TAKEOFF ROLL, ABORTED TAKEOFF (BELOW 70KTS) DUE TO ILLUMINATION OF NO TAKEOFF ANNUNCIATOR AND NO TAKEOFF HORN. T ROUBLESHOT SYSTEMS. FOUND EXCESSIVE MOISTURE AND CORROSION IN THE LT SPEEDBRAKE DISCONNECT PLUG PL001. REPLACED PINS, SOCKETS AND PLUG BACKSHELLS WITH NEW IAW CE WDM CH 20-10-04. PERFORMED OPS CK OF "NO TAKEOFF" SYSTEM. OPS CK GOOD. 2 L 7 2 4F RT A22CE 2007061300032 20070613 00032 NM 2007 6 13 DHL2007783502 1 20070604 A 5260 WEB BOEING 727 727227 1384078 NM AFT AIRSTAIRS CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 RT SIDE AIRSTAIRS WEB PANEL CRACKED AT LIGHTING HOLE BS 1243, WL 191, RBL 21. CUT OUT DAMAGED AREA DIM .5 BY .75 IAW B7 27 SRM 51-40-2, FIG 1. FABRICATED NEW DOUBLER REPAIR, MATERIAL USED 7075T6, 040, 4.50 BY 3.50 IAW B727 SRM 51-40-2, FIG 1 AND 53-10-2, FIG 6. TREATED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 51-10-2, 53-30-2 AND 51-40-2, FIG 1. 2 L 7 3 4F A3WE 2007061300034 20070613 00034 CE 2007 6 13 DXTA200702173 1 20070503 A 3241 ANTI-SKID SYS CESSNA 500 560CESSNA 2076750 CE CONTAMINATED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 311QS 5600311 FIRST OFFICER BRAKE PEDALS HAD NO PRESSURE CAPTAIN BRAKE PEDALS SEEMED TO HAVE NORMAL PRESSURE. PERFORMED ANTI-SKID BRA KE BLEED, BRAKE PEDALS CHECKED GOOD AFTER BLEED I/A/W MODEL 560 MM 32-42-00. 2 L 7 2 4F RT A22CE 2007061300035 20070613 00035 NM 2007 6 13 HALA0700244 1 20070606 A 3040 6240665 CONTROLLER BOEING 767 76733A 1385209 NM WINDSHIELD HEAT MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, L FWD WINDOW HEAT INOP "L FWD WINDOW" EICAS MSG DISPLAYED. REPLACED WINDOW HEAT CONTROLLER PE R AMM 30-41-01, OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2007061300036 20070613 00036 NM 2007 6 13 HALA0700246 1 20070606 A 8011 35059347 STARTER BOEING 717 717200 1383700 NM NR 1 ENGINE FAILED A HALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 13 486HA 5157 1335 55131 DURING LEFT ENGINE START ALL PARAMETERS NORMAL WITH EXCEPTION OF SLIGHTLY HIGH TGT. ALL INDICATIONS NORMAL AT IDLE, BUT LINE SERVICE SIGNALED FOR SHUTDOWN DUE TO SMOKE COMING FROM ENGINE EXHAUST. TRIED SUBSEQUENT N2 ROTATION. FOUND NR 1 ENG STARTER FAILED. REPLACED NR 1 ENG STARTER PER AMM 80-11-01. GRD OPS CK OKAY. 2 L 7 2 4F TR A6WE 2007061300037 20070613 00037 NM 2007 6 13 HALA0700245 1 20070606 A 3110 4087440927 DISPLAY BOEING 717 717200 1383700 NM COCKPIT FAILED A HALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 13 478HA 55123 BTB: JUST PRIOR TO TAXI NR 3 DU WENT BLANK FOLLOWED BY ODOR OF ELECTRICAL BURNING. RETURNED TO GATE. DU CAME BACK ON A FTER SHUTTING DOWN ENGINES AND TURNING OFF HYD PUMPS. REPLACED DU NR 3, GRD OPS CK OK PER AMM 31-61-03. 2 L 7 2 4F TR A6WE 2007061300038 20070613 00038 CE 2007 6 13 DXTA200702171 1 20070502 A 5101 UNKNOWN CESSNA 560 560XL 2076702 CE UNKNOWN UNKNOWN E DXTA O OTHER E VIBRATION/BUFFET CR CRUISE 1 GL 07 625QS 5605319 AT FL190 AND 190KIAS, A SUDDEN LOUD, LOW 'THUD' WAS HEARD AND FELT. 3 SECONDS LATER IT WAS HEARD AGAIN. PASSENGER THOU GHT IT CAME FROM BENEATH HIM AT CABIN SEAT POSITION 5/6. NOISE/THUD WAS FELT AND HEARD THROUGH ENTIRE AIRFRAME. PERFOR MED VISUAL INSPECTION OF ENTIRE AIRCRAFT EXERIOR, CHECKED ALL PANELS AND FLIGHT CONTROLS. INSPECTED ENGINES AND PNEUMAT IC DUCTING. NO DEFECTS NOTED. PERFORMED MULTIPLE GEAR SWINGS WITH NO DEFECTS NOTED. A/C IS OK FOR RETURN TO SERVICE. 2 L 7 2 4F RT A22CE 2007061300040 20070613 00040 CE 2007 6 13 GUUA05040702 1 20070504 A 3230 SWITCH BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 29 87552 UE216 FLIGHT: 9197 TLH/TPA - DURING APPROACH, LANDING GEAR DID NOT COME DOWN ON THE FIRST ATTEMPT. REPLACED LANDING GEAR CONT ROL. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 2007061300042 20070613 00042 EU 2007 6 13 SIMA200715001 1 20070526 A 5220 HANDLE SAAB SF340 340B 7860101 EU EMERGENCY EXIT OUT OF ADJUST A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 219AE 340B219 "SUP" RIGHT SIDE FORWARD EMERGENCY EXIT DOOR OPENED IN FLIGHT. ADJUSTED DOOR HANDLE IAW SAAB AMM, OPERATIONAL CHECKS GO OD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007061300043 20070613 00043 SO 2007 6 13 SIMA200715901 1 20070604 A 3350 110049 POWER SUPPLY EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 731BE 11029 3321 145356 FOUND EMERGENCY LIGHTING INOPERATIVE. REMOVED AND REPLACED NUMBER TWO EPSU IAW EMB IAW AMERICAN EAGLE WORK CARD 33-700- 19 AND SECURED LOOSE GROUND STUD GS8506DC IAW EMB AMM 20-13-21. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007061300044 20070613 00044 SO 2007 6 13 SIMA200715904 1 20070606 A 2460 REBCA410A100KB RELAY EMB 145 EMB145LR 3260212 SO FLIGHT DECK FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 661JA 8961 145766 RECEIVED EMERGENCY ARM LIGHT MESSAGE FOLLOWED BY ELECTRICAL ABNORMAL MESSAGE, DIVERTED TO MEM. REMOVED AND REPLACED POW ER DISTRIBUTION BOX AND CONTROL RELAY IAW EMB AMM 24-13-02 WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061300045 20070613 00045 SO 2007 6 13 SIMA200715903 1 20070605 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS SHORTED A SIMA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 668HH 145785 EMERGENCY LIGHT INOPERATIVE AT ROW 1A, 4A AND 7A. REPAIRED SHORT AND BLOWN FUSE AT FLOOD LIGHT IAW EMB AMM. OPERATIONA L CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061300046 20070613 00046 SO 2007 6 13 SIMA200715902 1 20070605 A 2913 971808 PUMP EMB 145 EMB145LR 3260212 SO HYD SYSTEM FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 697AB 6788 14500875 NUMBER ONE ENGINE HYDRAULIC FAIL MESSAGE, RETURNED TO DFW. REMOVED AND REPLACED ENGINE ONE HYDRAULIC PUMP IAW EMB AMM 2 9-10-03. LEAK AND OPERATIONAL CHECK WITH NO DEFECTS NOTED, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061300050 20070613 00050 SO 2007 6 13 SIMA200715802 1 20070603 A 3350 110049 POWER SUPPLY EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHTS FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 823AE 8698 145582 MULTIPLE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 1 POWER SUPPLY IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD, R ETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007061300054 20070613 00054 NM 2007 6 13 DXTA200702176 1 20070504 A 3260 PROXIMITY SWITCH AMD FALC50 FALCON2000 2730170 NM NLG CONTAMINATED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 213QS 113 NOSE GEAR DOOR ANNUNCIATOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. FOUND MOISTURE AND GRIT IN NOSE GEAR UPLO CK PROX SWITCH'S ELECTRICAL CONNECTOR. CLEANED, RECONNECTED AND COMPLETED 3 SUCCESSFUL LANDING GEAR EXTENSION AND RETRA CTIONS WITH NO DISCREPANCIES PER F2000 MM 32-601 AND 32-300. OPS CHECKED GOOD. 2 K 7 2 4F RT A50NM 2007061300055 20070613 00055 NE 2007 6 13 GUUA04180701 2 20070418 A 7200 3044900 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RIGHT SEIZED A GUUA C ABORTED TAKEOFF Y J ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 SO 29 46AR 10803 5008 UE27 114122 FLIGHT: 9265 MHH/PBI - ON STATIC TAKEOFF, AS ADVANCING POWER TO 1,000 LBS OF TORQUE, HEARD LOUD BANG AND RIGHT ENGINE SE IZED OPERATION. ABORTED TAKEOFF. REPLACED RIGHT ENGINE. OPERATIONAL CHECK NORMAL. SUSPECT 2ND STAGE PT BLADE FAILURE . 2 L 7 2 4T 4 T RT A24CE E26NE 2007061300057 20070613 00057 CE 2007 6 13 GUUA04260701 1 20070426 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE MLG LEAKING A GUUA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 29 87552 UE216 FLIGHT:9133 TPA/EYW - DURING APPROACH LANDING GEAR HAD A SLIGHT DELAY WHEN PUT IN THE DOWN POSITION. REPLACED LEFT MAIN LANDING GEAR ACTUATOR. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 2007061300059 20070613 00059 EA 2007 6 13 A6WA20074022 1 20070501 A 2750 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA FLAP WARNING UNKNOWN A A6WA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 31 465AW 7893 FLAPS FAIL CAUTION MESSAGE AND FLAPS FAIL AT 0 DEGREES. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEP S 1.3 AND 1.4, FLAPS RESET. AIRCRAFT RELEASED FOR SERVICE, NO SDU LIGHTS ILLUMINATED AT THIS TIME. (M) 2 L 7 2 4F RT A21EA 2007061300061 20070613 00061 NM 2007 6 13 DHL2007740523 1 20070525 A 5322 SHEAR TIE BOEING 727 7272Q9 138448M NM BS 580 S28L-R CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 WHILE IN "C" CHECK, FWD PIT SKIN UNDER SHEAR TIE AT BS 580 BETWEEN STR 28L AND 28R IS GOUGED AND CORRODED. CUTOUT AREA AT BS 580 BETWEEN STR 28L AND 28R DIM 1"BY 5 1/2" IAW B727 SRM 53-30-3 FIG 1. FABRICATED DOUBLER FROM 2024T3 .100 PO NR 9005138 DIM 14 1/2" BY 12 1/4". FABRICATED FILLER FROM 2024T3 .100 PO NR 9005138 DIM 1" BY 5 1/2" IAW B727 SRM 53-30-3 FIG 1 AND 53-30-2 FIG 2. TREATED AND PRIMED AREA AND PARTS IAW B727 SRM 51-10-2. REPAIR INSTALLED IAW B727 SRM 53-30- 3 FIG 1. 2 L 7 3 4F RT A3WE 2007061300067 20070613 00067 CE 2007 6 13 DXTA200702172 1 20070502 A 3040 99142166 CONTROL UNIT CESSNA 560 560XL 2076702 CE INOPERATIVE E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 650QS 4004 5605150 ON TAKE OFF ROLL, THE RT WINDSHIELD FAULT ANNUNCIATOR ILLUMINATED. REMOVED AND REPLACED POWER CONTROL UNIT ON RT ENG, O PS CHECK GOOD IAW CE 560XL M/M CH 24-20-01. 2 L 7 2 4F RT A22CE 2007061300071 20070613 00071 CE 2007 6 13 DXTA200702192 1 20070514 A 2612 7013348943 DAU CESSNA 750 750 2076810 CE RT ENGINE INOPERATIVE E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 998QS 1069 7500198 3 MINUTES AFTER TAKEOFF, THROTTLES IN CRUISE DETENT, RT ENGINE FIRE CAS MESSAGE CAME ON FOR ABOUT 10 SEC AND THEN CLEARE D. DAU 2 MISCOMPARE ENGINE AMBER CAS MESSAGE CAME ON AT THE SAME TIME. REMOVED AND REPLACED DAU 2 WITH REPAIRED UNIT. OPS CHECK GOOD. WORK DONE IAW 750 MM CHAPTER 31-41-00. 2 L 7 2 4J RT T00007WI 2007061300072 20070613 00072 CE 2007 6 13 DXTA200702193 1 20070514 A 3260 1EN18N119 UPLOCK SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE MLG INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 873QS 3907 258573 ON LANDING GEAR RETRACTION, THE RIGHT RED 'R' GEAR ANNUNCIATOR REMAINED ILLUMINATED. ALL OTHER GEAR INDICATIONS INCLUDI NG THE STANDBY WERE EXTINGUISHED. LANDING GEAR EXTENDED NORMALLY FOR LANDING. TROUBLESHOT AND FOUND INTERMITTENT RT MA IN LANDING GEAR DOOR UPLOCK MICROSWITCH. REPLACED SWITCH KN872 PER THE HAWKER 800XPC MM CHAPTER 32-60-00 AND WIRING DIA GRAM 32-60-10-04 PG 0. OPS CKS GOOD. 2 L 7 2 4F RT A3EU 2007061300073 20070613 00073 WP 2007 6 13 07FDEA01942 1 20070522 A 5340 AFA71321 FITTING DOUG DC10 DC1010F 3022111 WP CARGO DOORWAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 MAIN CARGO DOOR-LOWER JAMB FITTING NR 4 SHOWS CORROSION AT AFT UPPER HOLE. REPAIRED NR 4 LOWER JAMB FITTING AND WEB IAW FEDEX EA 8-5230-110663 REV A. "FUSELAGE-MAIN CARGO DOOR-LOWER JAMB SUPPORT FITTING INSPECTION AND DOOR RIG" LOWER SUPP ORT FITTING REPLACED ON JOB CARD N00788. 2 L 7 3 4F A22WE 2007061300074 20070613 00074 EU 2007 6 13 AWXA200700695 1 20070603 A 3350 321454 POWER SUPPLY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS FAILED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 29393 15865 770 PHX - EL - WHEN THE CREW ARRIVED AT THE A/C THEY NOTICED THE EMERGENCY EXIT LIGHTING WAS ON, SWITCH WAS IN ARMED POSITIO N AND GRN PWR WAS AVAILABLE WITH GRN SERVICE BUS POWERED. MX REPLACED 2 EPSU'S AND BATTERIES. OPERATIONAL CHECK WAS GO OD. 2 L 7 2 4F RT A28NM 2007061300075 20070613 00075 CE 2007 6 13 GUUA04190701 1 20070419 A 3260 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE MLG DIRTY A GUUA O OTHER J WARNING INDICATION CR CRUISE 1 SO 29 87552 UE216 FLIGHT: 9221 TLH/PBI - DURING FLIGHT, LANDING GEAR HANDLE LIGHTS ILLUMINATED. CLEANED BOTH MAIN LANDING GEAR UPLOCK SWI TCHES. COULD NOT DUPLICATE. 2 L 7 2 4T RT A24CE 2007061300077 20070613 00077 CE 2007 6 13 GUUA05040701 1 20070504 A 3210 BOLT BEECH 1900 1900D 1154162 CE BELLCRANK LOOSE A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 29 87551 UE206 FLIGHT: 9184 MIA/GNV - DURING APPROACH WHEN EXTENDING THE LANDING GEAR NOSE GEAR LIGHT DID NOT COME ON THE INTRANSIT LIG HT STAYED ON. RECYCLED THE LANDING GEAR HEARD A LOUD NOISE WHILE GEAR COMING UP. EXTENED LANDING GEAR AGAIN EVERYTHING WAS NORMAL. TIGHTENED NOSE LANDING GEAR BELLCRANK BOLT. LANDING GEAR OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 2007061300079 20070613 00079 EU 2007 6 13 200705311 1 20070525 A 2150 10018582 HEAT EXCHANGER EMB ERJ170 ERJ170100SE 3260406 EU RT A/C PACK CRACKED A UHLA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 11 657RW 5611 17000115 FLIGHT 7628 ORD TO HPN, AFTER TAKEOFF CREW EXPERIENCED VIBRATION IN FLIGHT, DECLARED AN EMERGENCY AND RETURNED TO FIELD. MAINT REPORTS RT PACK RAM AIR INLET LOOSE. ACFT FERRIED TO IND. MAINT REPLACED THE RIGHT HAND DUEL HEAT EXCHANGER. 2 L 7 2 4F RT A56NM 2007061300080 20070613 00080 SO 2007 6 13 LR7A07032 1 20070430 A 5230 SKIN LKHEED 382 382G 526414U SO CARGO DOOR PUNCTURED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2683 4606 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5321, FOUND RAMP DOOR EXTERIOR SKIN PUNCTURED AT RAMP STA6, LBL58. REPAIRED S KIN IAW SMP 583 51-140-12. 2 H 7 4 4T A1SO 2007061300081 20070613 00081 SO 2007 6 13 LR7A07033 1 20070430 A 5230 BULKHEAD LKHEED 382 382G 526414U SO CARGO DOOR CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2683 4606 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5212, FOUND CARGO DOOR REAR BULKHEAD WEB CRACKED IN MULTIPLE PLACES AT FS 1023 , LBL40 - RBL40. REPLACED WEB IAW SMP 583 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007061300088 20070613 00088 SO 2007 6 13 LR7A07040 1 20070430 A 5742 36001619 MOUNT LKHEED 382 382G 526414U SO FS 517 DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2683 4606 DURING SCHEDULED C-8 CHECK PER JOB CARD HSP57131, FOUND NR 2 ENGINE INBD TRUSS MOUNT ATTACH HOLES OVERSIZED AT FS 517, C WS178L, WL280. REPLACED TRUSS MOUNT IAW SMP 583 51-10, 54-30-06, 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007061300094 20070613 00094 NM 2007 6 13 07FDEA02095 1 20070608 A 2721 65727361 TAB BOEING 727 727233 138408A NM RUDDER DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LWR RUDDER TAB LT SIDE HAS SPOT OF SURFACE DAMAGE, 14" UP FROM BOTTOM AND 8" FWD FROM BACK EDGE. REPAIRED DAMAGE TO LOW ER RUDDER TAB LT SIDE REF SRM 51-40-9 PARA 3D. APPLIED CONDUCTIVE COATING REF MM 51-20-051-7. APPLIED PRIMER AND PAIN T REF MM 51-20-151-7. NO RE-BALANCING REQUIRED REF SRM 51-80-0 PG.1A 2 L 7 3 4F RT A3WE 2007061300095 20070613 00095 NE 2007 6 13 F3LA200700123 2 20070531 A 7200 ENGINE AIRBUS A319 A319111 3930336 NM GE CFM56 CFM56* 13802 NE NR 2 MALFUNCTIONED A F3LA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 NM 03 904FR 1579 575253 AIR TURN BACK AT 1710Z, FLIGHT CREW REPORTED NR 2 ENGINE ROLLBACK TO BETWEEN 45 PERCENT AND 55 PERCENT N1 DURING CLIMB-O UT OF 10,000 FT. ENGINE WAS ALSO MAKING VERY LOUD BANGS EVERY 3 SECONDS ACCOMPANIED BY LARGE VIBRATIONS FELT THROUGHOUT THE AIRCRAFT. ALL OTHER ENGINE INDICATIONS WERE WITHIN NORMAL RANGE. FLIGHT CREW DECLARED AN EMERGENCY AND LANDED IN KLAX WITHOUT INCIDENT. AIRCRAFT EXPERIENCED OVERWEIGHT LANDING. THE NR 2 ENGINE IS IN THE PROCESS OF BEING REPLACED. [6-13-07] A BORESCOPE OF THE NO. 2 ENGINE HAS REVEALED THE ROOT CAUSE OF THE DAMAGE TO BE THE SEPARATION OF A STAGE 5 BO OSTER BLADE. 2 L 7 2 4F 4 F RT A28NM E2GL 2007061300097 20070613 00097 CE 2007 6 13 AMWA84489BC 1 20070508 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE MASTER WORN A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 133YV 22533 105 UE133 AT APPROX 2500 AGL, WELL AFTER LANDING GEAR RETRACTION, THE BATT CHG ANNUNCIATOR ILLUM AND REMAINED LIGHTED FOR 15-20 SE C, THEN EXTINGUISHED. ABNORMAL CKLIST PERFORMED, NO FURTHER INCIDENT. THIS BATT CHG ANNUNCIATOR ILLUM WRITEUP IS CONSI DERED A NUISANCE AND A SEVERE DISTRACTION TO THE PILOTS. REMOVED AND REPLACED BATTERY, ENG RUN SHOWS GENS PARALLELED. 2 L 7 2 4T RT A24CE 2007061300099 20070613 00099 SO 2007 6 13 LR7A07046 1 20070607 A 5311 SEGMENT LKHEED 382 382G 526414U SO FS477, RBL35 BROKEN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 722 4698 DURING SCHEDULED B-3 CHECK PER JOB CARD HB5302, FOUND OVERHEAD RING SEGMENT BROKEN AT FS477, RBL35. REPAIRED RING SEGME NT IAW SK382-53-184 R1 REPAIR "B'". 2 H 7 4 4T A1SO 2007061300100 20070613 00100 SO 2007 6 13 LR7A07047 1 20070607 A 5310 WINDOW FRAME LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 722 4698 DURING SCHEDULED B-3 CHECK PER JOB CARD HB5301, FOUND RT CLEAR VISION WINDOW TOP FRAME CRACKED AT WL251. REPAIRED WINDO W FRAME IAW SMP 583 53-30-25. 2 H 7 4 4T A1SO 2007061300105 20070613 00105 CE 2007 6 13 GUUA05170701 1 20070515 A 3210 1018100891 BOLT BEECH 1900 1900D 1154162 CE MLG CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 190YV UE190 AT SCHEDULED INSPECTION DISCOVERED LEFT MAIN LANDING GEAR UPPER DRAG BRACE BOLT TO BE CRACKED IN TWO. CHECKED RIGHT DRA G BRACE UPPER BOLT AND DETERMINED IT ALSO TO BE CRACKED. REPLACED LEFT AND RIGHT DRAG BRACE ASSEMBLIES UPPER BOLTS. 2 L 7 2 4T RT A24CE 2007061300106 20070613 00106 EU 2007 6 13 07FDEA02108 1 20070611 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 662FE 761 MAIN CARGO COMPT BETWEEN FR 59 AND FR 61, 18" RIGHT OF BL LINE SEAT TRACK CORRODED REMOVED CORROSION AND FOUND AREA AP PROXIMATLY 5" AFT OF FR 60 TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-16 FIG 102. ORIGINAL THICKNESS .134 MATERIAL REMO VED IS .056. MATERIAL REMAINING .078. REMOVED SEAT TRACK DAMAGED SECTION IAW A300-600 SRM 51-40-21 PARAGRAPH 7. MATER IAL ID FOR NEW SEAT TRACK A53274005 IAW A300-600 SRM 53-10- 16 FIG 102. DRILLED AND LOCATED HOLES IAW A300-600 SRM 51-4 0-44. PRIMED SEAT TRACK IAW A300-600 SRM 51-21-10. INSTALLED NEW SECTION OF SEAT TRACK IAW A300-600 SRM 53-10-16 FIG 2 01. 2 L 7 2 4F RT A35EU 2007061300107 20070613 00107 SO 2007 6 13 SWIA200718314 1 20070605 A 2150 A/C PACK EMB 120 EMB120ER 3260203 SO RIGHT SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 563SW 120338 RIGHT PACK BLOWS SMOKE IN THE CABIN. RAN RIGHT PACK IN HOT/COLD AND AUTO/MANUAL MODES. NO SMOKE NOTED. 2 L 7 2 4T RT A31SO 2007061300108 20070613 00108 SO 2007 6 13 SWIA200718315 1 20070609 A 2150 A/C PACK EMB 120 EMB120ER 3260203 SO SMOKE A SWIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 567SW 120342 ON TAXI OUT, THE CABIN AND FLIGHT DECK BEGAN TO FILL WITH SMOKE. ASSOCIATED WITH AIR CONDITIONING PACKS. OPERATED BOTH PACKS ON GROUND WITH ENGINE AND APU BLEEDS. FOUND WHEN PACKS SET TO COLD SETTING BOTH PACKS WOULD EMIT SMOKE. TURNED TEMPERATURE SETTING UP AND SMOKE CEASED. 2 L 7 2 4T RT A31SO 2007061300111 20070613 00111 EA 2007 6 13 SWIA200718318 1 20070603 A 5313 STRINGER CNDAIR CL600 CL6002B19 1900309 EA BS 202-220 S24R DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 906SW 7510 STRINGER 24R BETWEEN FS 202 AND FS 220 IS DAMAGED. REPAIRED STRINGER 24R BETWEEN FS 202 AND 220 IAW CRJ 200 SRM 53-00-0 3. 2 L 7 2 4F RT A21EA 2007061300114 20070613 00114 SO 2007 6 13 SWIA200718321 1 20070603 A 5600 WINDSHIELD EMB 120 EMB120ER 3260203 SO CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 582SW 120350 LEFT DIRECT VISION WINDOW IS CRACKED. REPLACED LEFT DIRECT VISION WINDOW IAW 56-11-01. 2 L 7 2 4T RT A31SO 2007061300115 20070613 00115 SO 2007 6 13 SWIA200718322 1 20070610 A 3350 LENS EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS MISSING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 292UX 120292 FORWARD FLOOR TRACK LIGHT IS MISSING RED LENS COVER. REINSTALLED RED LENSE COVER TO FLOOR TRACK LIGHT ASSEMBLY. OPS CH ECK GOOD. 2 L 7 2 4T RT A31SO 2007061300117 20070613 00117 EA 2007 6 13 SWIA200718324 1 20070525 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7089 FOUND FLOORBEAM ANGLE AT FS 280 RBL 9 TO BE CORRODED BEYOND REPAIR, DISCOVERD AT C-CHECK. INSTALLED REPAIR FILLER ANGLE AND SPLICE ANGLES PER CRJ REO 601R-53-11-116. 2 L 7 2 4F RT A21EA 2007061300120 20070613 00120 NM 2007 6 13 AWXA200700716 1 20070523 A 5755 SKIN BOEING 757 757225 1384959 NM SPOILERS DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 MCN - LEFT WING NR 2 SPOILER LOWER SURFACE HAS DISBONDED AREA, WS 56 - WS 567. REPAIRED LEFT WING NR 2 SPOILER LOWER SU RFACE, WS 56 - WS 567 IAW B757-200 SRM 51-70-04. 2 L 7 2 4F RT A2NM 2007061300121 20070613 00121 NM 2007 6 13 AWXA200700717 1 20070528 A 5320 141N516079 FLOOR SUPPORT BOEING 757 757225 1384959 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 MCN - CORROSION ON CABIN FLOOR SUPPORT, BS 324 - BS 345, RBL 60, WL 208.1. REPLACED CABIN FLOOR SUPPORT, BS 324 - BS 34 5, RBL 60, WL 208.1 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007061300148 20070613 00148 EU 2007 6 13 HEEA113681 1 20070120 A 2997 11745033 WIRE HARNESS BOLKMS 117 BK117A1 5626010 EU HYD SYSTEM DAMAGED B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 217AE 7152 PILOT REPORTED NR 2 HYDRAULIC PRESSURE INDICATION FLUCTUATED AND DROPPED TO ZERO AND HYDRAULIC NR 2 LIGHT ILLUMINATED IN TERMITTENTLY. TROUBLESHOT SYSTEM. NO VISUAL ANOMALIES OR EXTERNAL LEAKAGE. CLEANED MAIN HYD. HARNESS, PRESSURE SWITCH AND 2 EACH TRANSDUCER CONNECTOR, APPLIED DC 4 COMPOUND AND REINSTALLED. FUNCTIONAL CHECK OF HYD. SYSTEM TO INCLUDE FL IGHT COMPLIED WITH. FUNCTION CHECK NORMAL, NO DISCREPANICES NOTED. AIRCRAFT RETURNED TO SERVICE. 1 G 7 2 3U H13EU 2007061300150 20070613 00150 EA 2007 6 13 FCPR20070005 2 20070222 A 7320 2541803 DIAPHRAGM PIPER PA31 PA31 7103102 SO LYC O540 TIO540* 41532 EA FCU BINDING B FCPR O OTHER O OTHER NR NOT REPORTED 1 NM 09 539M 100 31834 L1051561A ENGINE RUNS RICH, FOUND SERVO DIAPHRAGM BALL OFF SEAT IN THE CENTER CAUSING EXTREEM RICH CONDITION 1 L 7 2 3O 3 O A20SO E14EA 2007061300152 20070613 00152 SO 2007 6 13 2007F00030 1 20070316 A 3097 9112821 TRANSISTOR GRIMES EMB 145 EMB145 3260210 SO WINDSHIELD WIPER IMPROPER PART B O OTHER O OTHER NR NOT REPORTED 1 GL 05 GRIMES R&O (FQSR015K) REPORTED HIGH FAILURE RATE OF P/N 91-1282-1 TRANSISTOR ASSY. IT WAS DETERMINED BY GRIMES ENGINEER ING THAT THE TRANSITOR CONTAINED IN THE 91-1282-1 ASSY WAS COUNTERFIET. THE INVESTIGATION REVEALED A COUNTERFIET COMPON ENT MOTOROLA MJ10016 DATE CODE 0305 AS THE CUASE OF THE FAILURE. 50 PARTS WERE RECIEVED (BY THE OEM) FROM DR COMPONENTS IN NOV 2006. 32 OF THESE PARTS HAVE BEEN QUARENTINED. 18 PEICES WERE DELIVERED TO FQSR015K. THE R&O (FQSR015K) ACCOU NTED FOR ALL 18 SUSPECT PEICES BUT SOME HAVE ESCAPED INTO THE FIELD. THE WIPER CONTROLLERS WERE RETURNED TO SERVICE PRI OR TO NOTIFICATION OF PROBLEM. ELEVEN 90-0242-5-2'S WERE AFFECTED. AFFECTED SERIAL NUMBERS ARE 0717, 0449, 0667, 0658, 2 L 7 2 4F RT T00011AT 2007061300159 20070613 00159 SO 2007 6 13 N93A28042007 1 20070428 A 3260 1159SCAV4571 DOWNLOCK SWITCH GULSTM G1159 GIV 3980115 SO UNKNOWN E N93A O OTHER J WARNING INDICATION LD LANDING 1 SO 13 490QS 1488 STEER BY WIRE FAIL CASS MESSAGE ON LANDING 2 L 7 2 4F RT A12EA 2007060800141 20070608 00141 NM 2007 6 8 CALA0700289 1 20070602 A 5712 UNK VAPOR BARRIER BOEING 737 737824 13844BZ NM RT WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76504 31604 INSPECTION FOUND FIVE CRACKS IN THE RT WHEEL WELL FORWARD BULKHEAD (WING CENTER SECTION AFT SPAR VAPOR BARRIER). THREE OF THE CRACKS WERE LOCATED AT THE B-SYSTEM RETURN FILTER, ONE AT RBL 45, AND ONE AT RBL 25. THE VAPOR BARRIER WAS REMOV ED AND REPLACED IAW ECRA 5720-02015. A DIP WAS ISSUED FOR A DETAILED REPETITIVE INSPECTION OF BOTH THE RT AND LT VAPOR BARRIERS EVERY 560 CYCLES OR 90 DAYS WHICHEVER COMES FIRST. 2 L 7 2 4F RT A16WE 2007060800146 20070608 00146 EA 2007 6 8 TRAX200700742 1 20070529 A 5720 INTERCOSTAL CNDAIR CL600 CL6002C10 1390015 EA WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 RIGHT I/B SLAT CLOSING PLATE AND INTERCOSTAL CRACKED. LOCATED NEW SERVICEABLE INTERCOASTAL AND INSTALLED WITH SOLID FA STENERS TO SERVICEABLE CLOSING PLATE IAW CRJ 700 SRM 51-42-06. TRIMMED SERVICEABLE CLOSING PLATE TO FIT. OKAY TO PAINT. PRIME AND PAINTED, IAW CRJ SRM 51-25-16. REQUIRES INSTALLATION; CLEARANCE FIT, TO COMPLETE. INSTALLED RT TELESCOPIC DU CT CLOSING PLATE IAW CRJ 700 AMM 27-81-00. CLEARENCE AND FIT CHECK GOOD. 2 L 7 2 4F RT A21EA 2007060800150 20070608 00150 SO 2007 6 8 RAIA00705057 1 20070531 A 3250 12302328403 TILLER EMB 145 EMB145LR 3260212 SO NLG STEERING DEFECTIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 834HK 14966 145269 FLT NR 8010 - STL - NOSE STEERING DISENGAGES WHEN TURNING. MAINTENANCE REMOVED AND REPLACED NOSE WHEEL STEERING HANDLE, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007060800152 20070608 00152 EA 2007 6 8 VNAA0705002 1 20070514 A 3244 707413 TIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NLG FAILED A VNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 05 246PS 27 7920 CREW REPORTED AT AROUND 100 KTS ON TAKEOFF ROLL THAT THE RIGHT NOSE GEAR TIRE SHREDDED AND THE LEFT TIRE WENT FLAT. CRE W ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED BOTH NOSE TIRES IN ACCORD ANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 32-42-01-400-801. MAINTENANCE PERFORMED A STRUCTURAL INSPECTION IN ACCORDANC E WITH THE AIRCRAFT MAINTENANCE MANUAL 05-21-00-220-801. MAINTENANCE ALSO PERFORMED AN INSPECTION CHECK FOR TIRE BURST DAMAGE IN ACCORDANCE WITH THE AIRCRAFT MAINTNENACE MANUAL 05-51-29-210-801. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007060800159 20070608 00159 SO 2007 6 8 C2XA07RI040 1 20070528 A 3241 38793500 SHUTOFF VALVE EMB 145 EMB145LR 3260212 SO BRAKES INOPERATIVE A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 15986 17218 145254 FLT 2616 - EWR - CREW REPORTED INBOARD BRAKE FAIL MESSAGE ON EICAS IN FLIGHT. CREW DECLARED EMERGENCY, BUT ACFT LANDED WITHOUT ANY INCIDENTS. EWR MX REMOVED AND REPLACED INBOARD LEFT BRAKE SHUTOFF VALVE IAW EMB-145 AMM 32-41-05. MX PERFO RMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007060800162 20070608 00162 NM 2007 6 8 SWAA072841 1 20070605 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060800163 20070608 00163 NM 2007 6 8 SWAA072846 1 20070605 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, S8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007060800167 20070608 00167 NM 2007 6 8 SWAA072858 1 20070605 A 5315 6546810 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 967, LBL 27. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007060800168 20070608 00168 NM 2007 6 8 SWAA072859 1 20070605 A 5315 6546810 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 967, RBL 5. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007060800191 20070608 00191 NM 2007 6 8 KCSA071176 1 20070604 A 5347 SEAT TRACK BOEING 747 747221F 1384868 NM BS 1152 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 MAIN DECK SEAT TRACK CORRODED AT BS 1152, LBL 74. 2 L 7 4 4F A20WE 2007061100077 20070611 00077 NM 2007 6 11 QXEA200700894 1 20070529 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 C4 PDX - FUSELAGE SKIN DOUBLER FOR THE VHF 3 ANTENNA IS CORRODED. REPAIRED IAW SRM 51-14-00 AND RD8/4-53-1931. 2 H 7 2 4T RT A13NM 2007061100078 20070611 00078 NM 2007 6 11 QXEA200700896 1 20070529 A 5712 RIB BOMBDR DHC8 DHC8402 1390042 NM RT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 C4 PDX - RIGHT WING COVE RIB UNDER INBOARD SPOILER HAS MISDRILLED RIVET HOLE ON BOTTOM FLANGE AT WS YW 285. REPAIRED IA W RD8/4-57-811 AD SRM 51-42-05. 2 H 7 2 4T RT A13NM 2007061100079 20070611 00079 NM 2007 6 11 07FDEA02081 1 20070607 A 5330 SKIN DOUG MD11 MD11F 3023600 NM BS 1941-2164 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT EXTERIOR SKIN UNDERNEATH BODY FAIRING AREA FOUND CORROSION AT SEVERAL PLACES FROM STA 1941-2164. [06-18-07] REPA IR CARRIED OUT AS PER SRM 53-20-00 FIGURE 13 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007061100080 20070611 00080 NM 2007 6 11 07FDEA02085 1 20070607 A 5330 6554569 SKIN BOEING 727 727233 138408A NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 RT LOWER FUSE STA 380-387 STR 23R, 3 LIGHTNING STRIKES. REMOVED LIGHTNING STRUCK RIVETS, HFEC FOUND CRACKS AROUND RIVET HOLES AND SKIN. REMOVED DAMAGE, SECOND TIME HFEC FOUND NO CRACKS. FAB`D DOUBLER, DRILLED AND INSTALLED, PRIMED AND PA INTED IN REF TO SRM 51-30-2 PG 13-16, SRM 53-30-3 FIG 3, FIG 20. SRM 51-10-2 PG 1. THIS REPAIR WORKED WITH SNRM N00131. 2 L 7 3 4F RT A3WE 2007061100081 20070611 00081 NM 2007 6 11 07FDEA02086 1 20070607 A 5320 PLATE DOUG MD11 MD11F 3023600 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 CENTER CARGO STA 1841 STEP FORWARD WALL FOUND PLATE DAMAGED. [06-18-07] REPAIR CARRIED OUT AS PER SRM 53- 00-01 FIG URE 16 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007061200016 20070612 00016 NM 2007 6 12 MWEA0707135 1 20070605 A 7830 DOOR BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 928ME 55194 LEFT THRUST REVERSER UPPER DEFLECTOR DOOR HAS A CRACK IN OUTBOARD END OF INTERNAL FRAME IN FRAME RADIUS AT STATION 26.66 6. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2007061200025 20070612 00025 NM 2007 6 12 USAA070460 1 20070607 A 5330 SKIN BOEING 737 7374B7 1384702 NM BS 947 S13L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 STA 947.5 & S13L AFT ENTRY DOOR LOWER HINGE SKIN CUTOUT HAS CRACK. FABRICATED DOUBLER & TRIPLER PER TR 53-60-10, EA 987 16, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007061200030 20070612 00030 WP 2007 6 12 ABXA070176 1 20070530 A 3350 60030451 POWER SUPPLY DOUG DC9 DC941 302207N WP EMERGENCY LIGHT DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 9652 47608 DURING PRE-DEPARTURE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW DC9 AMM 33-50 -00. 2 L 7 2 4F A6WE 2007061200032 20070612 00032 NM 2007 6 12 USAA070420 1 20070605 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 291 S12-13R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 STA 291 BETWEEN S12R & S13R, STUB BEAM OUTER ANGLE HAS A CRACK. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51- 10-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007061200035 20070612 00035 NM 2007 6 12 SB07042 1 20070527 A 5610 5893543110 WINDSHIELD BOEING 737 7374B7 1384702 NM COCKPIT CRACKED A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 444US 29744 29744 24862 PBI FLT1733 - EN ROUTE FROM DCA TO PBI, DURING CRUISE, CREW REPORTED THE FIRST OFFICER'S R1 WINDSHIELD BEGAN TO ARC. TH E R1 WINDOW HEAT WAS SELECTED OFF. WITHIN A FEW MINUTES, THE WINDOW STARTED TO CRACK IN MULTIPLE PLACES RESTRICTING VIS IBILITY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICER'S R1 WINDSHIELD PE R MM 56-11-11. ALSO, REMOVED AND REPLACED THE R1 WINDOW HEAT CONTROL UNIT AS PRECAUTIONARY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007061200053 20070612 00053 EU 2007 6 12 BAQA200700013 1 20070505 A 2911 109051270109 ACCUMULATOR AGUSTA A109 A109E 0260119 EU WARNING LIGHT E BAQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 03 911UF 1710 11604 ENROUTE TO SCENE CALL THE EMERGECY HYDRAULIC PRESSURE LIGHT ILLUMINATED. ABORTED THE MISSION AND RETURNED TO BASE. THE OPERATION CONTROL CENTER AND MAINTENANCE WAS NOTIFIED. REPLACED HYDRAULIC ACCUMULATOR GROUP P/N 109-0512-70-109 S/N 823 WITH A SERVICEABLE ACCUMULATOR GROUP SAME P/N NEW S/N 523. OPERATIONAL CHECK COMPLIED WITH, NO DEFECTS NOTED. THIA A/C I S FROM OUR GAINSVILLE, FL PROGRAM. 1 G 7 2 3U RT H7EU 2007061200055 20070612 00055 EU 2007 6 12 YENA2007041 1 20070529 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS NO TEST A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 542JB 20696 1802 EMERGENCY LIGHT POWER SUPPLY UNIT FAILED ON WEEKLY CHECK FOR AFT GALLEY EMERGENCY LIGHTS. REMOVED AND REPLACED POWER SU PPLY UNIT AT POS 13WL PER AMM TASK 33-51-38-04. ALL CHECK NORMAL. 2 L 7 2 4F RT A28NM 2007061200062 20070612 00062 NM 2007 6 12 SWAA072912 1 20070608 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT LT BS 616, AT LOWER FASTENER ABOVE FUEL TANK. REPAIRED FRA ME PER TYPICAL REPAIR MANUAL. 2 L 7 2 4F RT A16WE 2007061200070 20070612 00070 NM 2007 6 12 SWAA072893 1 20070607 A 5311 6546547 FRAME BOEING 737 7373H4 1384600 NM BS 727 S21R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727, STR 21R. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2007061200072 20070612 00072 NM 2007 6 12 SWAA072868 1 20070607 A 5311 6546555 FRAME BOEING 737 7375H4 138449D NM BS 867 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061200073 20070612 00073 NM 2007 6 12 SWAA072869 1 20070607 A 5311 6546558 FRAME BOEING 737 7375H4 138449D NM BS 907 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061200074 20070612 00074 NM 2007 6 12 SWAA072881 1 20070607 A 5322 6546569 SHEAR TIE BOEING 737 7375H4 138449D NM BS 967 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 967 AT JOGGLE ABOVE L2 DOOR. REMOVED AND REPLACED SHEAR TIE P ER SRM. 2 L 7 2 4F RT A16WE 2007061200078 20070612 00078 NM 2007 6 12 SWAA072891 1 20070607 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM BS 500C S20R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007061200084 20070612 00084 NM 2007 6 12 SWAA072917 1 20070607 A 3350 101331 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 785SW 30602 RIGHT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007061200092 20070612 00092 2007 6 12 YENA2007046 4 20070604 A 2330 ENTERTAIN SYS AIRBUS 320 A320232 3930326 EU LIVE TV ODOR A YENA H C DEACTIVATE SYST/CIRCUITS ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 EA 15 554JB 1898 FLT 544, PBI TO EWR, APPROX 1500PM BURNING ODOR IN CABIN NEAR ROW 13 DEF, WHEN LIVE TV SHUT OFF, ODOR IMMEDIATELY WENT A WAY. PERFORMED TSM 23-39-00-810-801, NO FAULTS NOTED. REMOVED AND REPLACED SEB AT SEAT 13DEF AS PRECAUTIONARY. 2 L 7 2 4F RT A28NM 2007061200096 20070612 00096 NM 2007 6 12 SWAA072854 1 20070605 A 3350 D71701100 BATTERY PACK BOEING 737 7377Q8 1384418 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 799SW 28209 DURING SCHEDULED HC2 CHECK, LEFT FWD CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY P ACK PER MM. 2 L 7 2 4F RT A16WE 2007061200099 20070612 00099 NM 2007 6 12 USAA070433 1 20070606 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM BS 301 S13L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 AFT END OF SKIN TO INTERCOSTAL ATTACH ANGLE AT S13, BS 301 HAS CRACK. FABRICATED NEW PART & INSTALLED PER DWG 65-17684, SRM 51-10-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007061200104 20070612 00104 2007 6 12 KCSA07049 2 20070605 A 7200 ENGINE BOEING 747 747123 1384873 NM NR 1 FLAMED OUT A KCSA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 23 717CK 20325 AT FLIGHT LEVEL 370, NR 1 & 4 ENG FLAMEOUT, RAPID RESTARTED ENGINES, NR 1 RELIGHT AT 31.0, NR 4 AT 28.0. BOTH ENGINES S TABILIZED WITH NORMAL PARAMETERS & OPERATED NORMAL FOR REST OF FLIGHT. 2 L 7 4 4F A20WE 2007061200114 20070612 00114 NM 2007 6 12 CALA0700280 1 20070601 A 5311 6546548 FRAME BOEING 737 7373T0 1384582 NM BS 747 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT STA 747 BETWEEN STRINGER 8L AND 9L. THE FRAME WAS REPAIRED IAW E CRA 5310-04636. 2 L 7 2 4F RT A16WE 2007061200117 20070612 00117 NM 2007 6 12 CALA0700283 1 20070601 A 5311 6546552 FRAME BOEING 737 7373T0 1384582 NM BS 827 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT STA 827 BETWEEN STRINGER 8R AND 9R. THE FRAME WAS REPAIRED IAW E CRA 5310-04636. 2 L 7 2 4F RT A16WE 2007061200122 20070612 00122 EU 2007 6 12 YENA2007043 1 20070601 A 3240 39891 CONTROL VALVE EMB ERJ190 ERJ190100IGW 3260408 EU NR 1 FALSE INDICATION A YENA O OTHER J WARNING INDICATION LD LANDING 1 EA 15 178JB 3582 19000004 BRAKE RT & LT FAULT EICAS MESSAGES AT GEAR EXTENSION, TEMPS INDICATE O/B BRAKES FAILED. T/S PER FIM 32-41-00-810-848-A. REMOVED AND REPLACED MAIN BRAKE CONTROL VALVE NR 1 PER AMM 32-41-02/401. ALSO REPLACED MAIN BRAKE SOV 1 PRECAUTIONARY PER AMM 32-41-03. OPS CHECK GOOD, ALSO PERFORMED INFO NOTICE 2006-TO19B, OPS CHECK GOOD, NO LEAKS NOTED. 2 L 7 2 4F RT A57NM 2007061200125 20070612 00125 EA 2007 6 12 VNAA0706001 1 20070603 A 5610 NP13932212 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT FAILED A VNAA B EMER. DESCENT O OTHER CL CLIMB 1 GL 05 209PS 8073 7874 CREW REPORTED ON CLIMBOUT OF HSV THE RIGHT HAND SIDE WINDOW BROKE. CREW ELECTED TO RETURN TO HSV AND LANDED WITHOUT INC IDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND SIDE WINDOW DUE TO INNER PANE SPIDER WEB CRACKS IN ACCORDANCE WI TH THE AIRCRAFT MAINTENANCE MANUAL 56-12-01-400-801. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007061200141 20070612 00141 NM 2007 6 12 F3LA200700125 1 20070530 A 5321 D5367180500400 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CABIN CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 920FR 5184 1997 DURING C-3 CHECK, INSPECTION REPORTED FLOOR PANEL 261FF CORRODED ON LOWER SIDE. REPLACED FLOOR PANEL IAW AMM 53-12-12-0 00-001. 2 L 7 2 4F RT A28NM 2007061200144 20070612 00144 SO 2007 6 12 SIMA200716203 1 20070610 A 3350 LIGHT EMB 135 EMB135KL 3260302 SO MALFUNCTIONED A SIMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 21 807AE 145506 LEFT FLOOR LIGHTS FLICKING WITH EMERGENCY LIGHTS IN ARM POSITION. PERFORMED ADJUSTMENT TEST IAW EMB AMM. OPERATIONAL C HECK GOOD, RETURNED AIRCRAFT SERVICE. 2 L 7 2 4F RT T00011AT 2007061200145 20070612 00145 NM 2007 6 12 AWXA200700708 1 20070603 A 5320 D53480043205 SILL AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 SAL - CORROSION ON R2 DOOR LOWER SILL, FR 67 + 19", -Y1230. REPAIRED R2 DOOR LOWER SILL, FR 67 + 19", -Y1230 IAW A319 SRM 53-41-14. 2 L 7 2 4F RT A28NM 2007061200147 20070612 00147 EA 2007 6 12 A6WA200740196 1 20070415 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 454AW 7842 PAX DOOR AFT SIDE SKIN CRACKED APPROX .2 INCH LONG. (M) MAINTENANCE CUT OUT DAMAGED SKIN AND INSTALLED REPAIR DOUBLER IAW REO 601R-52-11-702, REV A. (K) 2 L 7 2 4F RT A21EA 2007061200148 20070612 00148 EA 2007 6 12 A6WA200740199 1 20070415 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 454AW 7842 LEFT FS 84 INTERCOSTAL CRACKED APPROX .1 INCH LONG AT LBL 36 FLOOR SUPPORT BEAM. (M) MAINTENANCE CUT AWAY DAMAGED FLAN GE AND INSTALLED REPAIR FLANGE IAW REO 601R-53-41-059, REV A AND BSC SR 601R-53-0030A. (K) 2 L 7 2 4F RT A21EA 2007061200154 20070612 00154 EA 2007 6 12 A6WA200740220 1 20070413 A 2600 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE DUCT MALFUNCTIONED A A6WA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 418AW 7618 ANTI-ICE DUCT WARNING ON ED1. LT FUSELAGE SHOWS RED WITH WING ANTI-ICE TURNED OFF. ABORTED TAKEOFF, SPEED AT 70 KNTS. BRAKE TEMPS ARE 03, 03, 04, 05. REMOVED AND REPLACED SENSING ELEMENT A15WK IAW AMM 36-21-04, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007061200156 20070612 00156 SO 2007 6 12 CHQA200700022 1 20070608 A 2120 UNKNOWN EMB 135 EMB135LR 3260305 SO CABIN SMOKE A CHQA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 GL 11 841RP 145737 FLIGHT 6329 - CLE-CVG - ON APPROACH INTO CVG AT APPROXIMATELY 5000 FT, NOTICED A FAINT SMOKE SMELL. LAV SMOKE INDICATION ON EICAS IMMEDIATELY FOLLOWED. FA VERIFIED SMELL BUT NO VISIBLE SMOKE IN LAV OR CABIN. EXECUTED QRH AND WITHIN A COUP LE MINUTES, THE SMELL DISSIPATED AND THE INDICATION WENT AWAY. LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPS CHEC K OF LAV SMOKE SYSTEM IAW MM 26-14-00. OPS CHECK GOOD. PERFORMED GROUND TEST OF PACK SYSTEM WITH BOTH APU AND ENGINE B LEED. COULD NOT DUPLICATE FAULT OR ODOR. 2 L 7 2 4F RT T00011AT 2007061200169 20070612 00169 EA 2007 6 12 A6WA200740229 1 20070514 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA RIGHT UNKNOWN A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 407AW 7424 RIGHT PACK HIGH TEMP CAUTION MESSAGE ON THE GROUND. COMPLIED WITH QRH, HAD SLIGHT ODOR OF SMOKE APPARENT AND SLIGHT HAZ E. (M) [07-31-07] INSPECTED RT PACK, NO DAMAGE NOTED, OIL SERVICE OK. OBSERVED CREW OPERATE LT PACK, NO SIGNS OF SM OKE OR HAZE. (K) 2 L 7 2 4F RT A21EA 2007061200171 20070612 00171 NM 2007 6 12 07FDEA02097 1 20070609 A 5311 69132802 FRAME BOEING 727 7272S2F 1384O81 NM ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 AGING A/C INSP, FOUND FRAME REPAIR AT STA 520, STR 16R-17R, DID NOT CONFORM TO SRM 51-40-3 FIG 1. REMOVED AND DISCARDED PREVIOUS REPAIR ANGLES AND INSTALLED NEW REPAIR PARTS REF. ALL WORK ACCOMPLISHED ON WO#36350/N00878. 2 L 7 3 4F A3WE 2007061200172 20070612 00172 EU 2007 6 12 07FDEA02098 1 20070609 A 5340 A5378193720100 ADAPTER AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 662FE 761 SEAT TRACK ADAPTER AT FR29, -Y953 IS CRACKED. REMOVED AND REPLACED SEAT TRACK ADAPTER ASSY IAW A300-600 SRM 51-40-21 PA R 7. 2 L 7 2 4F RT A35EU 2007061200173 20070612 00173 EU 2007 6 12 07FDEA02099 1 20070609 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 662FE 761 MAIN CARGO COMPT AT FR 66 10" BL 0, SEAT TRACK CORRODED. REMOVED CORROSION IAW A300-600 SRM 51-22-00, PG 12 ORIG THICKN ESS 0.134, MAT LOSS 0.054. REMAINING 0.080, FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-16 FIG 102. REMOVED AND R EPLACED SEAT TRACK SECTION IAW A300-600 SRM 53-10-16 FIG 201. ALODINED IAW A300-600 SRM 51-21-10, PRIMED AND PAINTED IA W A300-600 SRM 51-23-10. 2 L 7 2 4F RT A35EU 2007061200177 20070612 00177 EU 2007 6 12 07FDEA02103 1 20070610 A 5320 R53970189000R SILL AIRBUS 310 A310203 3930313 EU CARGO DOORWAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 AFT CARGO COMPARTMENT AFT LOWER CORNER SILL EXFOLIATED AROUND NR 7 ECCENTRIC DOOR FRAME FITTING REMOVED AND REPLACED DOO R SILL BEAM P/N 539-70189-000 RT IAW 51-32-11-5 AND DWG 17/E53970189 REV A. PERFORMED AFT CARGO DOOR TEST AND ADJUSTME NT TEST STEP 3E ,1 AND 9 IAW AMM 52-32-11-5 CHECK GOOD. WARNING SWITCH OPS CHECKS GOOD IAW AMM 52-71 11-5 CARRY OUT OP ERATIONAL OPS CHECKS GOOD IAW AMM 52-71-11-5. 2 L 7 2 4F RT A35EU 2007061200180 20070612 00180 NM 2007 6 12 ANCF200700011 1 20070529 A 2910 569670 MOTOR BOEING 757 757236 1384971 NM HYD PUMP INOPERATIVE W ANCF A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 23 506NA 24771 FLAPS FAIL TO MOVE, TRAILING EDGE LIGHT ILLUMINATED AND AICES MSG TE FLAPS DISAGREE AND FLAP ISLN VAL DISPLAYED. FLAPS OPERATE NORMAL USING TE ALTN SYSTEM. FLAP LEVEL VIBRATION WAS FELT DURING OPERATION WHEN TAXING OUT. IN ACCORDANCE WIT H FIM 27-51-00 FIG 110 BLOCK 6 AND 26 (FLAP CONTROL), PDU CONTROL VALVE MODULE WAS REPLACED IN ACCORDANCE AMM 27-51-28, NO HELP. IN ACCORDANCE WITH AMM 29-22-04 PAGE 401 WAS REPLACED FLOW LIMITER LH1 AND 2 AND NO HELP. IN ACCORDANCE AMM 2 7-11-08 PAGE 401, THE HYDRAULIC MOTOR PDU WAS REPLACED. TEST ON GROUND SATISFACTORY. 2 L 7 2 4F RT A2NM 2007061200181 20070612 00181 EA 2007 6 12 A6WA200740195 1 20070415 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 454AW 7842 PAX DOOR FORWARD SIDE SKIN CRACKED APPROX .4 INCH LONG. (M) MAINTENANCE CUT OUT DAMAGED SKIN AND INSTALLED REPAIR DOU BLER IAW REO 601R-52-11-702, REV A. (K) 2 L 7 2 4F RT A21EA 2007061200186 20070612 00186 NM 2007 6 12 DL777070672 1 20070605 A 3300 SWITCH BOEING 777 777232 1385232 NM E/E BAY LIGHTS DEFECTIVE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 27 866DA 29738 UNUSUALLY STRONG ODOR NOTED IN MAIN E/E COMPARTMENT. COULD NOT POSITIVELY IDENTIFY NATURE OF ODOR. PERFORMED INSP OF E /E ELECTRICAL COMPONENTS AND WIRING. NO TROUBLE FOUND. ALL C/B-S IN. INSPECT FWD CARGO BIN. ALL OKAY. ODOR DISSIPAT ED AFTER 2 HOURS. MAIN E/E COMPARTMENT LIGHTS NOTED TO GO INTERMITTENTLY DIM THEN BRIGHT. AFTER 2 HOURS LIGHTS INTERMI TTENTLY UNCONTROLLABLE FROM E/E LIGHTS SWITCHES IN BOTH ON OR OFF POSITIONS. FWD TO MCO AND PLAC 33-31-01. C/B PULLED AND COLLARED. REPLACED DEFECTIVE SWITCH. E AND E LIGHTS WORKING NORMAL. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CR ITICAL TO ETOPS. 2 L 7 2 4F RT T00001SE 2007061200199 20070612 00199 NM 2007 6 12 HALA0700241 1 20070604 A 2612 7351 ELEMENT BOEING 767 767332 1382001 NM FIRE DETECTOR UNKNOWN A HALA O OTHER N FALSE WARNING CR CRUISE 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM, EICAS STATUS MSG "L ENG FIRE LP 1" DISPLAYED. REPLACED ELEMENT ASSY TS46 OPER CHK OK PER AMM 26-11-02. 2 L 7 2 4F RT A1NM 2007061300005 20070613 00005 NM 2007 6 13 QXEA200700904 1 20070605 A 2930 9702811 TRANSDUCER BOMBDR DHC8 DHC8402 1390042 NM HYD SYSTEM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 424QX 4006 BOI FLIGHT NR 2302: DURING CLIMB AND CRUISE, NR 2 HYD PRESS FLUCTUATED BETWEEN 3000-2200 QTY GOOD. MAINTENANCE REMOVED AND REPLACED THE NR 2 HYD PRESS TRANSDUCER IAW AMM TASKS 29-30-01-000-801 AND 29-30-01-400-801. LEAK CHECK C/W AND HYD FLUCTUATIONS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061300014 20070613 00014 NM 2007 6 13 DXTA200702187 1 20070511 A 3200 UNKNOWN AMD FALC50 FALCON2000 2730170 NM MLG UNKNOWN E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 275QS 75 BIRD STRIKE ON NOSE GEAR IMPROPER RETRACTION CYCLE EVENTUALLY DID RETRACT. JACKED AIRCRAFT AND INSPECTED NOSE GEAR AREA FOR DAMAGE DUE FROM BIRD STRIKE. NO DAMAGE WAS FOUND. APPLIED POWER TO AIRCRAFT AND CYCLED LANDING GEAR SEVERAL TIMES TO CHECK FOR PROPER OPERATION. GEAR OPS CHECK CHECKED GOOD. PERFORMED A VISUAL INSPECTION AROUND AIRCRAFT STRUCTURE, FLIGHT CONTROLS AND ENGINE INTAKES WITH NO DEFECTS NOTED. WORK DONE IAW DASSAULT FALCON 2000 MM CHAPTER 32-300, 05-102 AND 32-214. 2 K 7 2 4F RT A50NM 2007061300021 20070613 00021 CE 2007 6 13 AMWA06033B 1 20070510 A 5711 1181000131 SPAR CAP BEECH 1900 1900D 1154162 CE ZONE 600 CORRODED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 142ZV 22220 UE142 BIO - CORROSION DAMAGE RT LOWER SPAR CAP AT WS 124. REPAIRED IAW ENGINEERING AUTHORIZATION REPAIR DWG 1900D142-7 REV 1R . 2 L 7 2 4T RT A24CE 2007061300024 20070613 00024 CE 2007 6 13 DXTA200702190 1 20070513 A 3246 WHEEL BEECH MU300 400A 1155402 CE MLG SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 145QS RK421 AFTER LANDING, THE LEFT WHEEL ASSEMBLY WAS SMOKING AND GIVING OFF HEAVY ODOR OF HOT BRAKES OR HOT RUBBER. NO NOTICEABLE CONTROL ISSUES DURING TAXI AFTER LANDING. INSPECTED LT WHEEL AND BRAKE ASSY WITH NO DEFECTS NOTED. PERFORMED TAXI CHE CK WITH NO SMOKE OR ODORS NOTED. OK FOR CONTINUED SERVICE. REF HAWKER 400XP M/M 32-40-00. 2 H 7 2 4F RT A16SW 2007061300041 20070613 00041 CE 2007 6 13 AMWA084391BC 1 20070504 A 2437 23078019 GCU BEECH 1900 1900D 1154162 CE WORN A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 161YV 20125 23 UE161 AFTER TO THE BATTERY CHARGE ANNUN ILLUM. CAPT RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENTS. THIS BC ANNUN IL LUM IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTIONS TO THE PILOTS. PARALLELED GCU`S. 2 L 7 2 4T RT A24CE 2007061300049 20070613 00049 NM 2007 6 13 07FDEA02094 1 20070606 A 2782 651781822 ACTUATOR BOEING 727 727277 138408S NM SLATS INOPERATIVE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 242FE 2534 2534 21178 6 LED FAILED TO RETRACT AFTER TAKEOFF, REMOVED AND REPLACED NR 6 SLAT ACT. 2 L 7 3 4F RT A3WE 2007061300053 20070613 00053 CE 2007 6 13 DXTA200702175 1 20070504 A 2720 991455811 ACTUATOR CESSNA 750 750 2076810 CE RUDDER LIMITER INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 997QS 3770 7500208 RUDDER LIMIT FAIL A , FAILED AT 24 PERCENT. INSTALLED AND OPS CHECKED ACTUATOR IAW 750 M/M 27-30-00. 2 L 7 2 4J RT T00007WI 2007061300056 20070613 00056 CE 2007 6 13 GUUA04230702 1 20070423 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE COCKPIT ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 29 231YV UE231 FLIGHT: 9308 MIA/EYW - DURING APPROACH ODOR IN COCKPIT. PERFORMED ENGINE RUN WITH CAPTAIN CHECK BLEED SYSTEM ALL ELECTR ICAL ON, CHECKED OIL AND BRAKE FLUID NO ODORS AT THIS TIME. 2 L 7 2 4T RT A24CE 2007061300060 20070613 00060 NM 2007 6 13 07FDEA02093 1 20070608 A 5730 APB74411 SKIN DOUG MD11 MD11 3023602 NM BS 1219 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 576FE 48501 TOP OF CENTER TANK RIGHT SIDE FOUND CORROSION AT STA 1219. CORROSION IN TOP OF CENTER TANK RIGHT SIDE AT STA 1219 CARRI ED OUT REPAIR AS PER FEDEX EA NR 1-5710-111114, TITLE: WINGS, CENTER WING FUEL TANK RIGHT SIDE CORROSION REPAIR. REPA IR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007061300062 20070613 00062 NM 2007 6 13 DHL2007740527 1 20070610 A 5720 ANGLE BOEING 727 7272Q9 138448M NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 WHILE AT C CHECK, LWR END OF VERTICLE SUPPORT ANGLE CRACKED ON L/W FIXED IN STA 110. CUT-OUT DAMAGED AREA APPROX DIM 2. 3" BY 1" IAW B272 SRM 51-10-1 FIG 1 AND 51-40-3 FIG 1. FAB ANGLE REPAIR APPROX DIM 9" BY 3" FROM 7075-0 .063 PO NR 9004 779 IAW B727 SRM 51-40-3 FIG 1 AND 57-20-2 FIG 2. FAB FILLER FROM 7075-T6.050 PO NR 9003927 APPROX DIM 2.3 BY 1" IAW B7 27 SRM 51-40-3 FIG 1. INSTALLED REPAIR ANGLE AND FILLER ATL/E WSTA 110 IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2007061300065 20070613 00065 WP 2007 6 13 070119 1 20070528 A 2700 BUTTON DOUG DC9 DC983 3022083 WP FLAP/SLAT SYS STICKING A WX0A A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 19 878GA 53487 DURING CLIMB-OUT FROM LAS, LEADING EDGE SLATS WOULD NOT RETRACT. FLIGHT CREW ELECTED TO RETURN TO LAS FOR A NORMAL LAND ING, NO EMERGENCY PROCEDURE WAS PERFORMED. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED AND FOUND THE FLAP/SLAT LOCK OUT BUTTON STICKY. THE BUTTON WAS CLEANED PER MM 27-50-00. SYSTEM OPERATION PERFORMED NORMAL. AIRCRAFT WAS RETURNED TO SE RVICE. 2 L 7 2 4F RT A6WE 2007061300069 20070613 00069 CE 2007 6 13 DXTA200702194 1 20070514 A 3297 WIRE RAYTHN DH125 HAWKER800XP 7150012 CE LT MLG MISINSTALLED E DXTA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 GL 07 861QS 258361 AFTER TAKEOFF, THE LEFT MAIN GEAR RED LIGHT STAYED ILLUMINATED AFTER GEAR RETRACTION. JACKED A/C AND TROUBLESHOT SYSTEM , FOUND WIRE JK2L WAS LOCATED ON TERMINAL JK3L. CORRECTED MISWIRE AND PERFORMED EXTENSION AND RETRACTION SEVERAL TIMES WITH NO DEFECTS NOTED. ALL WORK PERFORMED IAW HAWKER 800XP MM CHP 32-30-01. 2 L 7 2 4F RT A3EU 2007061300070 20070613 00070 CE 2007 6 13 DXTA200702195 1 20070514 A 3240 UNKNOWN CESSNA 500 560CESSNA 2076750 CE BRAKES UNKNOWN E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 328QS 5600428 ON LANDING ROLLOUT, AT ABOUT 40 KTS, THE BRAKES STOPPED BRAKING. RELEASED THE BRAKES AND REAPPLIED FIRMLY AND THEY RE-E NGAGED. ON POST FLIGHT, FOUND BRAKE FLUID AT AN ACCEPTABLE LEVEL WITH PARKING BRAKE SET AND PRE-CHARGE IN THE MIDDLE OF YELLOW ARC. AFTER PAX DEPLANED, DID HIGH SPEED TAXI WITH A-S SELECTED OFF AND HAD NORMAL BRAKING. READJUSTED CAP DRIV E CLIPS TO .120". REPAIRED SHIELD GROUNDS ON P108/P107, LT TRANSDUCERS. BLED BRAKE ASSY'S. COMPLETED THE ANTI-SKID FU NCTIONAL CHECK SATISFACTORILY. ALL OPS CHECKS ARE GOOD IAW MODEL 560XL MM 32-42-00. 2 L 7 2 4F RT A22CE 2007061300083 20070613 00083 SO 2007 6 13 LR7A07035 1 20070430 A 5742 33035511 FITTING LKHEED 382 382G 526414U SO FS 517 DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2683 4606 DURING SCHEDULED C-8 CHECK PER JOB CARD HSP57131, FOUND NR 2 ENGINE INBD TRUSS MOUNT INBD ATTACH FITTING HOLES OVERSIZED AT FS 517, CWS177L, WL280. REPLACED FITTING IAW SMP583 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007061300084 20070613 00084 SO 2007 6 13 LR7A07036 1 20070430 A 5742 33035501 FITTING LKHEED 382 382G 526414U SO FS 517 DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2683 4606 DURING SCHEDULED C-8 CHECK PER JOB CARD HSP57131, FOUND NR 2 ENGINE INBD TRUSS MOUNT OUTBD ATTACH FITTING HOLES OVERSIZE D AT FS 517, CWS179L, WL280. REPLACED FITTING IAW SMP 583 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007061300092 20070613 00092 NM 2007 6 13 QXEA200700895 1 20070529 A 5753 WEB BOMBDR DHC8 DHC8402 1390042 NM RT WING TE FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 C4 PDX - RIGHT WING FLAP SHROUD WEB HAS DAMAGE ON LIGHTENING HOLE APPEAR TO BE FROM SPOILER ACTUATOR LINK. TOGGLE AT ST ATION YW 317.019. REPAIRED IAW RD8/4-57-158. 2 H 7 2 4T RT A13NM 2007061300145 20070613 00145 NM 2007 6 13 QXEA200700648 1 20070422 A 2131 21178041 CONTROLLER DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE CABIN PRESSURE MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 368PH 2797 512 LMP FLIGHT NR 2011 LEVELING AT 25000 FEET WE GOT A CABIN PRESS WARNING. CABIN ALT 12,000 FEET (FORWARD OUTFLOW WAS NORMA L, BLEEDS WERE ON AND MAX AND THE CABIN DUMP SELECTOR WAS IN AUTO) DECLARED THE EMERGENCY STARTED AND RAN ALL CHECKLISTS TO THEIR COMPLETION IN A 3500 FT DESCENT RATE THE CABIN ALTITUDE DESCENDED TO BELOW 10,000 FEET. LEVELED AT 9500 FEET AND CABIN ALT LEVELED AT AROUND 6000-65000 DIFFERENTIAL WAS AROUND 1.0 - 1.5 DIFF. EVERYTHING APPEARED TO BE NORMAL FOR THE REST OF THE FLIGHT. MAINTENANCE COMPLIED WITH VISUAL INSPECTION OF FORWARD AND AFT OUTFLOW VALVES WITH NO DEFECTS NO TED. REPLACED CABIN PRESSURE CONTROLLER IAW MM TASKS 21-30-069-000-801 AND 21-30-09-400-801. GROUND RAN AIRCRAFT, PRESSU 2 H 7 2 4T 4 T RT A13NM E20NE 2007061300147 20070613 00147 NE 2007 6 13 HEEA113586 1 20070112 A 2612 9231004802103 FIRE DETECTOR SKRSKY S92 S92A NE NR 2 ENGINE MALFUNCTIONED B HEEA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 03 692PH 1353 920028 ENROUTE FROM MC778 TO HBP NR 2 ENGINE FIRE LIGHT CAME ON. REDUCED POWER BELOW 1200 LBS PER HR. FUEL FLOW AND LIGHT WEN T OUT. INCREASED POWER AND LIGHT CAME BACK ON. REVIEWED ENGINE FIRE CHECKLIST AND REDUCED NR 2 ENGINE TO IDLE FOR OEI LANDING AT GRAND ISLE EXXON. ABOUT 10 MINUTES FROM TIME OF EVENT TO LANDING AT 1601. MAINTENANCE REPLACED THE OUTBOAR D AND INBOARD FLAME DETECTORS AND THE OUTBOARD FLAME DETECTOR HARNESS PART NUMBER 92552-04112-041. ALSO INSULATED WIRE TO PIN C WITH HEAT SHRINK AS PER LETTER FROM SIKORSKY. 2 G 7 2 4U R00024BO 2007061300149 20070613 00149 SW 2007 6 13 HEEA114010 1 20070205 A 5630 204030770101 WINDOW BELL 412 412 1182202 SW CREW DOOR CRACKED B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 3893N 33010 PARAMEDIC NOTICED CRACK IN UPPER WINDOW COPILOTS DOOR. WHEN ATTEMPTING TO SECURE THE WINDOW WITH TAPE, WINDOW FELL OUT. MAINTENANCE REPLACED WINDOW. 1 G 7 2 4U H4SW 2007061300165 20070613 00165 WP 2007 6 13 I5HA0758010 1 20070503 A 7810 90632321 EXHAUST PIPE CVAC 580 580 2422806 WP LOOSE A I5HA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 582 475 WHILE EN-ROUTE FROM MIAMI (MIA) TO CANCUN (MUN) THE LEFT HAND ENGINE FIRE WARNING BELL SOUNDED. THE CREW REDUCED POWER ON THE ENGINE AND THE ALARM STOPPED. THE AIRCRAFT RETURNED TO MIA AND LANDED UNEVENTFULLY. THE CREW DID NOT DECLARE AN EMERGENCY. INSPECTION BY MECHANICS REVEALED THE LEFT HAND TAIL PIPE ASSEMBLY HAD COME LOOSE FROM ITS CLAMPS ALLOWING E NGINE EXHAUST TO ESCAPE. THE EXHAUST TAILPIPE, CLAMPS AND STRUCTURE WERE INSPECTED. NO DAMAGE WAS FOUND. MECHANICS RE INSTALLED THE TAILPIPE AND THE ENGINE RUN AT HIGH POWER WITH NO PROBLEMS. THE AIRCRAFT WAS RETURNED TO SERVICE. THIS S ERVICE DIFFICULTY REPORT IS CLOSED. 2 L 7 2 4T RT 2007061300173 20070613 00173 NE 2007 6 13 HEEA114154 1 20070213 A 3230 709001104 CONTROL PANEL SKRSKY S92 S92A NE MLG FAILED B HEEA O OTHER O OTHER AP APPROACH 1 SW 03 892PH 920038 UPON APPROACH TO GC902 DURING BEFORE LANDING CHECK, GEAR WOULD NOT EXTEND. RETURNED TO HUM AND USED EMERGENCY BLOW DOWN . TROUBLESHOOTING REVEALED CONTACTS BETWEEN PINS A AND B OF LANDING GEAR CONTROL PANEL MAINTAINING CONTINUITY WHEN GEAR LEVER IS PLACED IN THE DOWN POSITION. THEREFORE POWER IS CONTINUALLY SUPPLIED TO THE RETRACT SIDE OF THE CONTROL VLAV E. 2 G 7 2 4U R00024BO 2007061300175 20070613 00175 SW 2007 6 13 AC2A114169 1 20070127 A 6200 430310105105 RESTRAINT BELL 430 430 1182150 SW WORN B AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 430CM 49090 WORN DUE TO SHEAR RESTRAINT BEING WORN 1 G 7 2 3U RT H9SW 2007061300176 20070613 00176 SW 2007 6 13 AC2A114171 1 20070127 A 6410 BEARING BELL 430 430 1182150 SW TAIL ROTOR CRACKED B AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 430CM 49090 BEARINGS SCUFFING AND CRACKED 1 G 7 2 3U RT H9SW 2007061300177 20070613 00177 NE 2007 6 13 HEEA114184 1 20070216 A 3231 7625102701101 ROD END SKRSKY S76 S76C 8143008 NE MLG DOOR OUT OF ADJUST B HEEA O OTHER J WARNING INDICATION CL CLIMB 1 SW 03 761P 760588 UNSAFE GEAR RETRACT INDICATION WHEN ATTEMPTING TO RAISE GEAR AFTER TAKEOFF. PERFORMED EMERGENCY PROCEDURE. ADJUSTED DO OR LINK ROD END OUT ONE HALF TURN. OPS CHECK GOOD. 1 G 7 2 3U NC H1NE 2007061300178 20070613 00178 SW 2007 6 13 YTRR114194 1 20070212 A 6200 407010103113 PITCH HORN BELL 407 407 1182206 SW DEBONDED B YTRR K NONE O OTHER IN INSP/MAINT 1 SW 03 407AK 383 53269 DURING INSPECTION FOUND TUNGSTEN CARBIDE COATING ON INNER SURFACE DEBONDED AND CORRODED. 1 G 7 1 3U O H2SW 2007061300179 20070613 00179 SW 2007 6 13 YTRR114195 1 20070212 A 6200 407010103113 PITCH HORN BELL 407 407 1182206 SW CORRODED B YTRR K NONE O OTHER IN INSP/MAINT 1 SW 03 407AK 383 53269 DURING INSPECTION FOUND TUNGSTEN CARBIDE COATING ON INNER SURFACE DEBONDED AND CORRODED. 1 G 7 1 3U O H2SW 2007061300183 20070613 00183 NE 2007 6 13 HEEA114300 1 20070228 A 2435 200SGL144Q1 STARTER GEN SKRSKY S76 S76C 8143008 NE NR 2 FAILED B HEEA O OTHER O OTHER CR CRUISE 1 SW 03 761P 1445 760588 DURING CRUISE FLIGHT IFR, THE NR 2 GENERATOR FAILED. RETURNED TO HOUMA BP. MAINTENANCE REPLACED THE NR 2 STARTER GENER ATOR. 1 G 7 2 3U NC H1NE 2007061300186 20070613 00186 NE 2007 6 13 U0GA114355 1 20070306 A 2612 NONE FIRE WARNING SKRSKY S61 S61N 8142104 NE FALSE INDICATION B U0GA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 03 564EH 61365 NUMBER TWO FIRE LIGHT CAME ON DURING DESCENT, NO VISIABLE SIGNS OF FIRE OR DAMAGE AFTER LANDING. ACTION TAKEN: FOUND 11 :OO TURBINE BLANKING PLATE LEAKING HOT AIR, REMOVED, RESEATED. LEAKCHECKED GOOD ON OPS RUN. 2 G 7 2 4U 1H15 2007061300188 20070613 00188 SW 2007 6 13 O84A114543 1 20070319 A 2435 200SGL124Q STARTER GEN BELL 230 230 1182149 SW NR 1 ENGINE UNSERVICEABLE B O84A O OTHER J WARNING INDICATION CR CRUISE 1 GL 19 880SF 23024 NR 1 GENERATOR FAILED IN CRUSE FLIGHT AND AFTER SHUTDOWN COULD NOT START NR 1 ENGINE DUE TO STARTER WOULD NOT MOTOR. ON E BRUSH WORN BEYOND LIMITS. REPLACED STARTER / GENERATOR. 1 G 7 2 3U NC H9SW 2007061300189 20070613 00189 EU 2007 6 13 PG9A114592 1 20070315 A 6420 350A33318000 TIE ROD UROCOP EC120 EC120B 8680987 EU TAIL ROTOR HUB BROKEN B PG9A K NONE O OTHER IN INSP/MAINT 1 WP 19 132GC 3233 M171 3756 DURING A 100HR INSPECTION, FOUND TWO TT BARS WITH BROKEN LAMINATES. REPLACED WITH NEW. 1 G 7 2 3U NC R0001RD 2007061300191 20070613 00191 EU 2007 6 13 PG9A114594 1 20070315 A 5720 350A33313000 PITCH CONTROL UROCOP EC130 EC130B4 8680989 EU TAIL ROTOR HUB DAMAGED B PG9A K NONE O OTHER IN INSP/MAINT 1 WP 19 132GC 3233 M171 3756 A BROKEN TT BAR LAMINATE DAMAGED THE SPIDER BEYOND LIMITS. INSTALLED SERVICEABLE SPIDER ASSY. 1 G 7 2 3U H9EU 2007061300192 20070613 00192 EU 2007 6 13 HEEA114631 1 20070321 A 7933 MS280341 SENSOR BOLKMS 105 BO105S 5626006 EU NR 2 ENGINE MALFUNCTIONED B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 7170D S840 AFTER SIX MINUTES OF FLIGHT, #2 ENGINE OIL TEMP PEGGED AT MAXIMUM. REDUCED POWER ON #2 TO IDLE. AFTER ONE MINUTE TEMP DROPPED TO HIGH GREEN. LEFT ENGINE RUNNING AT IDLE AND PERFORMED RUNNING LANDING. MAINTENANCE REPLACED THE #2 ENGINE O IL TEMPERATURE BULB. 1 G 7 2 3U H3EU 2007061300194 20070613 00194 SW 2007 6 13 AC2A114642 1 20070321 A 2432 BP9 BATTERY BELL 430 430 1182150 SW MASTER INOPERATIVE B AC2A K NONE O OTHER IN INSP/MAINT 1 SW 31 430CV 49072 INSPECTED BATTERY, BATTERY WOULD NOT ACCEPT CHARGE, BATERY OUTPUT VOLTAGE IS 5 VDC. 1 G 7 2 3U RT H9SW 2007061300196 20070613 00196 SW 2007 6 13 U0GA114871 1 20070402 A 5330 STA8700 SKIN AGUSTA AB139 AB139 0260110 SW BS 8700 CRACKED B U0GA O OTHER O OTHER NR NOT REPORTED 1 SW 03 813DG 31032 CRACK FOUND AT STA. 8700 UPPER LEFT HAND CORNER OF FUSELAGE. COMPLIED WITH BT139-015 PART I REPAIRED BY AGUSTA. 2 G 7 2 4U R00002RD 2007061300201 20070613 00201 SW 2007 6 13 O84A115223 1 20070426 A 6510 222044003107 HANGER ASSY BELL 230 230 1182149 SW TAIL ROTOR DRIVE WORN B O84A C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 19 880SF 4225 23024 FWD TAIL ROTOR HANGER BEARING FAILED. SAFETY STRAP WAS THE ONLY THING HOLDING DRIVESHAFT IN PLACE. PILOT AND CREW NOTI CED A MOMENTARY KNOCKING NOISE AFTER NR 1 ENGINE AT IDLE ONLY. CONTACTED BELL PRODUCT SUPPORT AND REPLACED HANGER BEARI NG ASSY. AFTER INSPECTION. 1 G 7 2 3U NC H9SW 2007061300202 20070613 00202 NE 2007 6 13 HEEA115354 1 20070505 A 2121 85022051 BLOWER SKRSKY S76 S76C 8143008 NE CARGO BAY SMOKE B HEEA O OTHER J WARNING INDICATION CR CRUISE 1 SW 03 766P 760594 DURING IFR CRUISE FLIGHT, AFT BAGGAGE SMOKE CAUTION LIGHT ILLUMINATED. REPLACED BLOWER ASSY. 1 G 7 2 3U NC H1NE 2007061300208 20070613 00208 CE 2007 6 13 050807N334CS1 1 20070508 A 3260 S33682 BULB CESSNA 500 550 2076604 CE MLG INDICATOR BURNED OUT E Z5FA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 63 334CS 5501089 ON APPROACH INTO LAS THE LEFT MAIN LANDING GEAR UNLOCK LIGHT FAILED TO ILLUMINATE UPON GEAR EXTENSION AND INDICATOR LIGH T TEST. THE APPRAOCH WAS ABORTED AND A GO AROUND WAS PERFORMED. THE EMERGENCY GEAR EXTENSION PROCEDURE WAS FOLLOWED AS P ER THE CHECLIST AND AN EMERGENCY LANDING WAS DECLARED INTO LAS. THE AIRCRAFT LANDING WAS UNSEVENTFUL. MAINTENANCE FOUND THE INDICATOR LIGHT BULBS BURNED OUT. THE LIGHT BULBS WERE REPLACED, GEAR SWINGS PERFORMED AND SYSTEM OPS OK. 1 L 7 2 4F A22CE 2007061300209 20070613 00209 EA 2007 6 13 S9BA0507 1 20070506 A 5540 C6TFM102931 HINGE DHAV DHC6 DHC6 2802606 EA ZONE 300 CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 573 RUDDER MID HINGE PLATE AND BEARING ASSY CORRODED 1 H 7 2 3T RT A9EA 2007061300210 20070613 00210 EA 2007 6 13 S9BA0707 1 20070511 A 3246 13A01082001 ATTACH BRACKET DHAV DHC6 DHC6300 2802606 EA ZONE 300 CRACKED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 888PV 620 RIGHT HAND FLOAT FORWARD SPREADER BAR ATTACH FITTING HAS A LONGITUDINAL CRACK (WITH THE GRAIN) ACROSS THE TOP OF THE SPR EADER BAR ATTACHMENT LUG. 1 H 7 2 3T RT A9EA 2007061300230 20070613 00230 CE 2007 6 13 AMWA06033D 1 20070510 A 5414 11498007821 SKIN BEECH 1900 1900D 1154162 CE LT NACLELLE CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 142ZV 22220 UE142 FRICTION CHAFFING OCCURED DURING ENGINE OPERATION RESULTING IN WORN SEGMENTS ON THE LT ENGINE UPPER AFT NACELLE ALONG EN TIRE LENGHT & SHAPE OF NACELLE. REPAIRED IAW ENGINEERING AUTHORIZATION REPAIR DWG 1900D142-1 REV 1R. 2 L 7 2 4T RT A24CE 2007061300235 20070613 00235 NM 2007 6 13 UPS07M49924 1 20070409 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORT STAB BARREL NUT BORE RT NR 09 FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R 38. BO TTOM - REMAIN BLENDOUT DEPTH 0.041" BORE REAMED TO 0.988" DIA REMAIN BLENDOUT 0.026" DEEP EXCEED EO LIMITS. 10X MAG DVI C/O NO CORROSION. BORE REAMED FURTHER TO 1.032" DIA EN1203-07. BORE BLENDOUT & BOTTOM PERI RADIUS, SMOOTHEN & PROTECT SRM 51-21-01 VII R 38. REP AIR SLEEVE BUSHING FAB, PROTECT & INSTALLED EO FIG 5. REPAIR IAW EN1203-07. 2 L 7 3 4F RT A22WE 2007061300236 20070613 00236 EU 2007 6 13 UPS07149880 1 20070605 A 2410 729714E IDG AIRBUS A300 A300F4622R 3930360 EU FLUCTUATES A IPXA O OTHER O OTHER CR CRUISE 1 SO 01 149UP 0832 INSPECTION TYPE:N/A DIVERSION - NR 1 AND 2 IDG HIGH OIL TEMPERATURE AND VOLTS/FREQS FLUCTUATING. *SUPPLEMENTAL SDR* RE PLACED NR 2 IDG. OPS AND LEAK CHECK OK. FOUND AT 1 IDG LOW ON OIL REPLACED THE LEAKING NR 1 IDG FILL SERVICE PORT. OP S AND LEAK CHECK OK. 2 L 7 2 4F RT A35EU 2007061300237 20070613 00237 NM 2007 6 13 ASAA0791754 1 20070531 A 5321 453A261037 FLOOR PANEL BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 FWD CARGO PIT FLOOR PANEL AT STA 727 CORRODED. REPAIRED IAW SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007061300238 20070613 00238 NM 2007 6 13 ASAA0791755 1 20070531 A 5321 453A261057 FLOOR PANEL BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 CORROSION AT AFT CARGO PIT FLOOR PANEL AT STA 727. REPAIRED IAW SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007061300241 20070613 00241 NM 2007 6 13 ASAA0791758 1 20070531 A 5321 453A261067 FLOOR PANEL BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT FLOOR PANEL AT STA 727 CORRODED. REPAIRED IAW 51-40-05. 2 L 7 4 4F RT A16WE 2007061300242 20070613 00242 NM 2007 6 13 ASAA0791759 1 20070531 A 5321 453A151015 FLOOR PANEL BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 FWD CARGO PIT FLOOR PANEL CORRODED. REPAIRED IAW SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007061300243 20070613 00243 NM 2007 6 13 ASAA0791760 1 20070531 A 5321 453A161083 FLOOR PANEL BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 FWD CARGO PIT FLOOR PANEL CORRODED. REPAIRED IAW 51-40-05. 2 L 7 4 4F RT A16WE 2007061300245 20070613 00245 CE 2007 6 13 402037052807 1 20070528 A 7797 30607572 WIRE HARNESS LEAR 45 45LEAR 5170805 CE ALIDSG TPE331 TPE331201A 0517 WP DAMAGED E J7SA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SW 05 611FX 2037 P116646C LEFT ITT IRRATIC DURING FLIGHT. ENGINE WAS SHUTDOWN IN FLIGHT. LEFT ITT IRRATIC DURING FLIGHT. ENGINE WAS SHUTDOWN IN FLIGHT. EMERGENCY DECLARED FOR LANDING. PILOT REPORTED THAT THE LEFT ITT EXCEEDED 1014* TWICE AND THE PILOT PERFORMED AN IN-FLIGHT SHUTDOWN. BOTH N1 INDICATIONS WERE MATCHED. BOTH FF INDICATIONS WERE MATCHED. PILOT FURTHER REPORTED TH AT THE LEFT ITT INDICATION FOLLOWING ENGINE SHUTDOWN WAS 940* AND REMAINED SO UNTIL TOUCHDOWN. MX REVIEWED THE ECTM DOW NLOAD AND THE DEEC SAW THE ITT OUT OF RANGE. RECOMMENDED REPLACING THE ENGINE HARNESS PART NUMBER 3060757-1 OR -2. ENG INE HARNESS REPLACED AND GROUND POWER RUNS PERFORMED. NO FURTHER DEFECTS NOTED. 2 L 7 2 4F 3 T RT T00008WI AEXJ STC 2007061300246 20070613 00246 EA 2007 6 13 COMA0770030 1 20070526 A 5315 CC670341757 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FS 280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 371CA 14236 10082 RIGHT SIDE OF FS 280 FLOORBEAM IS CORRODED. REPAIRED THE FS 280 FLOORBEAM IAW REO 670-53-11-046. 2 L 7 2 4F RT A21EA 2007061300248 20070613 00248 EA 2007 6 13 COMA0760406 1 20070527 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FS 409 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 959CA 27853 7116 CRACK IN LOWER OUTBOARD VERTICAL STIFFENER AT LBL 18 FS 409+128. REPAIRED IAW REO 601R-53-41-056. 2 L 7 2 4F RT A21EA 2007061300251 20070613 00251 EA 2007 6 13 COMA0760405 1 20070527 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FS 559 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 959CA 27853 7116 FOUND CRACK ON LOWER OUTBOARD FLANGE ON SEMI PRESSURE BULKHEAD VERTICAL STIFFENER AT FS 559 RBL 9. REMOVED DAMAGED AREA ON FS 559 RBL 9 VERTICAL STIFFENER AND INSTALLED DOUBLER IAW REO 601R-53-41-057. 2 L 7 2 4F RT A21EA 2007061300252 20070613 00252 NM 2007 6 13 ASAA0791761 1 20070531 A 5320 146A81287 STRAP BOEING 737 737990 NM BS 794 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO STRAP CORRODED AT BS 794.3. REPAIRED IAW SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007061300253 20070613 00253 NM 2007 6 13 ZZDA070606176 1 20070606 A 3350 6011779 BATTERY BOEING 717 717200 1383700 NM EMERGENCY LIGHT OVERHEATED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 891AT 55043 EXTERNAL EMERGENCY LIGHTS ALWAYS ON WHEN SYSTEM OFF. REPLACED BATTERY ASSY B5-125 & OPS GOOD PER AMM 33-51. 2 L 7 2 4F TR A6WE 2007061300256 20070613 00256 NM 2007 6 13 ASAA0791763 1 20070531 A 5321 453A161080 FLOOR PANEL BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 CORROSION ON FWD CARGO FLOOR PANEL AT STA 500A. REPAIRED IAW 51-40-05. 2 L 7 4 4F RT A16WE 2007061300258 20070613 00258 NM 2007 6 13 ASAA0791765 1 20070531 A 5321 453A1610 FLOOR PANEL BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 CORROSION AT FWD CARGO FLOOR PANEL AT STA 500D. REPAIRED IAW SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007061300259 20070613 00259 NM 2007 6 13 ASAA0791766 1 20070531 A 5320 148A750219 SILL BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT DUST SILL CORRODED. REPAIRED IAW SRM 53-00-53. 2 L 7 4 4F RT A16WE 2007061300260 20070613 00260 NM 2007 6 13 ASAA0791767 1 20070531 A 5320 146A750219 SILL BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT DUST SILL CORRODED. REPLACED DUST SILL IAW SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007061300262 20070613 00262 NM 2007 6 13 ASAA0791769 1 20070531 A 5347 146A750115 CARGO TRACK BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 CARGO PIT TIE DOWN TRACK CORRODED. REPAIRED IAW SRM 53-00-53. 2 L 7 4 4F RT A16WE 2007061300263 20070613 00263 NM 2007 6 13 ASAA0791770 1 20070531 A 5347 146A750118 CARGO TRACK BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT PH CARGO TIE DOWN CORRODED. REPAIRED IAW SRM 53-00-53. 2 L 7 4 4F RT A16WE 2007061300264 20070613 00264 NM 2007 6 13 ASAA0791771 1 20070531 A 5753 STRUCTURE BOEING 737 737990 NM TE FLAP DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 LEFT INBOARD TRAILING EDGE FLAP DAMAGE TO THE FLAPS DUE TO SPOILER LOCKS. 2 L 7 4 4F RT A16WE 2007061300265 20070613 00265 NM 2007 6 13 ASAA0791772 1 20070531 A 5753 STRUCTURE BOEING 737 737990 NM TE FLAP DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 RIGHT INBOARD TRAILING EDGE FLAP DAMAGE ON LEADING EDGE DUE TO SPOILER LOCKS. REPAIRED IAW EA 5750 02365. 2 L 7 4 4F RT A16WE 2007061300270 20070613 00270 SW 2007 6 13 HEEA115463 1 20070514 A 3230 222075139111 CONTROL PANEL BELL 430 430 1182150 SW MLG MALFUNCTIONED B HEEA O OTHER J WARNING INDICATION LD LANDING 1 SW 03 430XM 49073 NORMAL OPERATIONS BEFORE LANDING. LANDING GEAR SELECTED DOWN AND NO LANDING GEAR LIGHTS ILLUMINATED. RETURN TO BASE AN D LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LANDING GEAR CONTROL PANEL. 1 G 7 2 3U RT H9SW 2007061300272 20070613 00272 SW 2007 6 13 AC2A115466 1 20070514 A 3210 427036123101 SKID SHOE BELL 427 427 1182207 SW PWC PW207 PW207D NE MLG SEVERED E AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 427CK 56043 MOUNTING EARS ARE RIPPED OUT. 1 G 7 1 3U 3 U R00001RC E42NE 2007061300273 20070613 00273 NM 2007 6 13 2007UALA01322 1 20070428 A 2121 217N1152 COOLING FAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE E/E BAY CLOGGED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 527UA 24995 FLIGHT DIVERTED DUE TO EQUIPMENT COOLING FAULT INDICATION. EQUIPMENT COOLING FAULT ON TAXI, ONCE CHECKLIST C-W AND ALTE RNATE SELECTED EICAS CLEARED. NO CB'S FOUND POPPED ON FLIGHT DECK. COMPLIED WITH MEL CARD. REPLACED COOLING FAN FILTE R. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061300274 20070613 00274 NM 2007 6 13 2007UALA01444 1 20070507 A 3230 CONTROL MODULE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MLG OUT OF RIG A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 543UA 25698 EXECUTED A GO AROUND DUE TO VERBAL TOO LOW/TERRAIN AND LANDING GEAR WARNING MESSAGES. ACCOMPLISHED TROUBLESHOOTING. NO FAULTS FOUND. FOUND GEAR HANDLE BINDING IN DOWN POSITION WHEN PULLING HANDLE OUT OF DETENT. BINDING IS WORSE WITH HYD RAULICS ON. REPLACED LANDING GEAR CONTROL LEVER MODULE, FOUND CABLES THAT RUN FROM CNLT HANDLE TO GEAR CNTL MODULE OUT OF RIG. RIGGED CABLES. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061300276 20070613 00276 NE 2007 6 13 2007UALA01448 2 20070508 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 DAMAGED A UALA A UNSCHED LANDING C F.O.D. CL CLIMB 1 WP 29 597UA 28750 726644 RTFL DUE TO BIRDSTRIKE TO NR 2 ENGINE. NR 2 ENG, WHILE PERFORMING FIM MULTIPLE METAL PIECES FOUND IN THE 10TH STAGE BLE ED DUCT AND IN THE PRE COOLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060800182 20070608 00182 SO 2007 6 8 RAIA00705054 1 20070528 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 830HK 145313 POST FLT NR 5596 - STL - HAND RAIL LIGHT INOP ON STAIRS. MAINTENANCE REPLACED LIGHT BULB FOR EMERGENCY LIGHT ON AIRSTAI RS HANDRAIL SYSTEM, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007060800190 20070608 00190 SO 2007 6 8 C2XA07RI042 1 20070602 A 2910 14523426401 TUBE EMB 145 EMB145LR 3260212 SO HYD SYSTEM CHAFED A C2XA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 16961 145103 FLT 2246 - EWR - CREW REPORTED HYD 1 LOW QTY AND E1 HYD PUMP FAIL ON EICAS. EWR MX FOUND PUMP RETURN TUBE ASSEMBLY CHAF ED / LEAKING IN FUSELAGE AT FR 56. MX REPAIRED THE TUBE ASSY IAW EMB 145 AMM 20-10-03 AND PERFORMED OPERATIONAL CHECK S UCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007060800196 20070608 00196 NM 2007 6 8 KCSA071181 1 20070604 A 5313 STRINGER BOEING 747 747221F 1384868 NM BS 2160-2180 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 FUSELAGE STR 21L DAMAGED BETWEEN BS 2160 AND 2180. 2 L 7 4 4F A20WE 2007061200006 20070612 00006 NM 2007 6 12 NOCA10807 1 20070606 A 3350 767 BULB BOEING 757 75728A 1384976 NM EMERGENCY LIGHTS INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 755NA 30043 EXTERIOR EMERGENCY EXIT LIGHT AT DOOR L4 IS INOP. RELAMPED DOOR L4 EXTERIOR EMERGENCY EXIT LIGHT, OPS CHECKS OKAY. 2 L 7 2 4F RT A2NM 2007061200011 20070612 00011 NM 2007 6 12 MWEA070128 1 20070529 A 7830 7150923REV2 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 902ME 55166 LEFT THRUST REVERSER UPPER BLOCKER DOOR HAS A CRACK IN OUTBOARD END OF DOOR FRAME RADIUS AT STATION 35.669. FABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007061200036 20070612 00036 NE 2007 6 12 TQ0A20070005 2 20070525 A 8560 SUPERCHARGER DHAV DHC2 DHC2* 2800108 EA PWA R985 R9855 52008 NE HARTZL HCB3R HCB3R304 GL ENGINE MAKING METAL E TQ0A E ENGINE SHUTDOWN O OTHER AP APPROACH 1 AL 05 1018A 10589 178 4328 EMA1240 ENGINE LOST SOME POWER ON DESCENT, ONCE THE PLANE LANDED, PILOT REPORTED A METAL TO METAL SOUND. ONCE MAINTENANCE ARRIV ED A LARGE AMOUNT OF OIL WAS SEEN AT THE EXHAUST TAILPIPE. AFTER PULLING THE PROPELLER THROUGH, A HYDRAULIC LOCK OCCURE D AND AT THAT POINT CREW PLACED THE AIRCRAFT ON A BARGE TO RETURN TO TOWN. AT ENGINE REMOVAL A LARGE AMOUNT OF OIL WAS LEAKING THROUGH THE SUPERCHARGER SECTION OF THE ENGINE AND METAL CONTAMINATES WERE DISCOVERED IN THE OIL SCREEN. 1 H 7 1 3R 3 R A806 5E1 5 C P28EA 2007061200038 20070612 00038 WP 2007 6 12 ABXA070177 1 20070605 A 5310 99115057 WINDOW FRAME DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 WHILE COMPLYING WITH WINDOW FRAME MOD EA 53000041, FOUND CRACKED FRAME. REPAIRED AREA IAW DC9 SRM 53-03, FIG 34. 2 L 7 2 4F A6WE 2007061200050 20070612 00050 NE 2007 6 12 BAQA200700014 2 20070509 A 7321 0319858290 FUEL CONTROL AGUSTA A109 A109E 0260119 EU TMECA ARRIUS ARRIUS2K1 NE NR 2 ENGINE FAILED E BAQA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 03 109DU 1456 11503 33012 JUST PRIOR TO BEGINNING APPROACH TO DUKE. #2 ECU MAINTENANCE CAUTION LIGHT ILLUMINATED. AS PIC REDUCED POWER TO BEGIN LA NDING APPROACH, #2 FMU (FUEL CONTROL) FAIL LIGHT ILLUMINATED. #2 ENGINE DROPPED TO 11% TORQUE. PIC TRANSITIONED TO SINGL E ENGINE GO-AROUND PROFILE. ONCE CLIMB WAS ESTABLISHED, PIC SWITCHED #2 ENGINE TO MANUAL CONTROL AND TRIED TO REGAIN CON TOLR OF ENGINE WITH MANUAL TRIM SWITCH. NO ENGINE RESPONSE. PIC DECLARED AN EMERGENCY WITH RDU TOWER AND MADE A SINGLE E NGINE LANDING AT RDU. TURBOMECA FOUND THE FMU STEPPER MOTOR FAILED. THE FMU WAS REPLACED WITH SERVICEABLE FMU P/N 031985 290 S/N 119B.LEAK CHECK C/W ANDD POWER CHECKS. NO DEFECTS NOTED. A/C IS FROM OUR DUKE LIFE FLIGHT PROGRAM IN NORTH CAROL 1 G 7 2 3U 3 U RT H7EU E34NE 2007061200054 20070612 00054 GL 2007 6 12 20070011 2 20070425 A 7250 23073533 TURBINE NOZZLE AGUSTA A109 A109A2 0260120 EU ALLSN 250C 250C20B 03013 GL ENGINE SEPARATED E BAQA B A EMER. DESCENT UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 EA 03 1PJ 3243 240 7262 CAE834144 AFTER TAKEOFF TO PERFORM MAINTENACE M/R TRACK AND BALANCE IT WAS REPORTED TO PILOT, BY ANOTHER AIRCRAFT, THAT HE HAD SMO KE TRAILING HIS AIRCRAFT. EMERGENCY PROCEDURES WERE PEREFORMED AND AIRCRAFT LANDED WITHOUT INCIDENT. THE SMOKE WAS DIS COVERED TO BE ENGINE OIL. COMPANY INVESTIGATION OF TURBINE ASSEMBLY FOUND THE FIRST STAGE NOZZLE SHIELD DOME ASSEMBLY FA ILURE EXPOSING THE #8 ENGINE BEARING TO DIRECT COMBUSTION HEAT. 1 G 7 2 3U 3 U H7EU E4CE 2007061200064 20070612 00064 EU 2007 6 12 YENA2007047 1 20070605 A 2150 10007004 ACM EMB ERJ190 ERJ190100IGW 3260408 EU NR 2 FAILED A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 15 179JB 1763 19000006 FLT 1057, JFK-PIT, APPROX 0230-0300Z BURNING ODOR DURING APPROACH. LIGHT SMOKE REPORTED IN CABIN BY FLIGHT ATTENDANT ON LANDING ROLL METAL SHAVING CAME OUT OF AIR VENTS TOWARD REAR OF AIRCRAFT FOLLOWED BY PACK 2 FAIL EICAS MESSAGE. VERIFI ED PACK NR 2 FAILED. REMOVED AND REPLACED NR 2 ACM IAW AMM 21-51-05. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4F RT A57NM 2007061200067 20070612 00067 NM 2007 6 12 SWAA072915 1 20070608 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT LT BS 616, WL 202. REPAIRED FRAME PER TYPICAL REPAIR MANAU L. 2 L 7 2 4F RT A16WE 2007061200081 20070612 00081 NM 2007 6 12 SWAA072884 1 20070606 A 3244 06066712 TIRE BOEING 737 7373H4 1384600 NM RT MLG SEPARATED A SWAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 29 309SW 22948 NR 4 MAIN TIRE LOST TREAD DURING TAKEOFF. REMOVED AND REPLACED NR 4 MAIN WHEEL AND TIRE ASSY PER MM. REPAIRED MID AND AFT FLAPS AND LANDING GEAR DOOR PER SRM. 2 L 7 2 4F RT A16WE 2007061200112 20070612 00112 NM 2007 6 12 CALA0700278 1 20070602 A 5311 6546557 FRAME BOEING 737 7373T0 1384582 NM BS 887 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT STA 887 BETWEEN STRINGERS 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04636. 2 L 7 2 4F RT A16WE 2007061200113 20070612 00113 NM 2007 6 12 CALA0700279 1 20070601 A 5311 6546552 FRAME BOEING 737 7373T0 1384582 NM BS 827 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT STA 827 BETWEEN STRINGER 8L AND 9L. THE FRAME WAS REPAIRED IAW E CRA 5310-04636. 2 L 7 2 4F RT A16WE 2007061200126 20070612 00126 EU 2007 6 12 YENA2007049 1 20070605 A 2150 BEARING EMB ERJ190 ERJ190100IGW 3260408 EU LT ACM FAILED A YENA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 15 193JB 3724 19000017 FLT 1306, IAD TO JFK, APPROX 1700Z, ODOR (COCKPIT) & SMOKE DETECTED ON INITIAL CLIMB. RETURNED TO FIELD (IAD) PACK 1 FA IL ANNUNCIATED UPON ARRIVAL AT GATE. PERFORMED OPERATIONAL TEST OF COOLING PACKS PER 21-51-60-05. FOUND NR 1 LEFT ACM MAKING GRINDING NOISE AND NR 1 PACK SYSTEM ONLY PRODUCING HOT AIR. SUSPECT AIR BEARING SEIZURE AT ACM. REMOVED AND REP LACED LT NR 1 AIR CYCLE MACHINE AS PER AMM 21-51-05, PERFORMED OPS CHECK. NO ODOR FROM PACKS. OK FOR SERVICE. 2 L 7 2 4F RT A57NM 2007061200129 20070612 00129 NM 2007 6 12 NOCA10507 1 20070531 A 2560 P4010021 BATTERY BOEING 757 75728A 1384976 NM FLASHLIGHT INOPERATIVE A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 756NA 32448 L-2 OUTBOARD EMERGENCY FLASHLIGHT INOP. DEFERRED PER MEL 25-63-4. FLIGHT ATTENDANT MUST HAVE OWN FLASHLIGHT. REMOVED AND REPLACED L-2 OUTBOARD EMERGENCY FLASHLIGHT BATTERY. OPS CHECKS NORMAL. 2 L 7 2 4F RT A2NM 2007061200138 20070612 00138 NM 2007 6 12 DHL2007740524 1 20070525 A 5313 STRINGER BOEING 727 7272Q9 138448M NM BS 950F-970 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 WHILE IN "C" CHECK, AFT CARGO COMPARTMENT, STRINGER 27L BETWEEN STA 950F AND 970 HAS CORROSION AROUND FASTENERS. REMOVE D FASTENERS TO GAIN ACCESS IAW B727 SRM 51-30-2. REMOVED CORROSION IAW B727 SRM 51-10-6, CORROSION FOUND OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. CUTOUT DAMAGED AREA DIM 69 1/8". FABRICATED 2 FILLERS FROM BAC1498-147 .090 PO NR 7178178 DIM 38 1/2" AND 27", 2 SPLICES AND 6 SHIMS IAW B727 SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9. TREATED AND PRIMED PARTS IAW B 727 SRM 51-10-2. INSTALLED REPAIR PARTS AT AFT CARGO COMPT STR 27L BETWEEN BS 950D AND 970 IAW B727 SRM 51 2 L 7 3 4F RT A3WE 2007061200142 20070612 00142 SO 2007 6 12 SIMA200716201 1 20070607 A 2740 3622005015 ACTUATOR EMB 135 EMB135KL 3260302 SO HORIZONTAL STAB FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 842AE 11383 145673 PITCH TRIM INOP MESSAGE ON TAKEOFF, BACKUP SYSTEMS FUNCTIONED NORMAL. REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUAT OR IAW EMB AMM 27-40-02. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007061200146 20070612 00146 NM 2007 6 12 AWXA200700709 1 20070608 A 5315 D53472172205 FLOORBEAM AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 SAL - CORROSION ON CABIN FLOORBEAM, FR 67 + 13", -Y1192. REPLACED CABIN FLOOR BEAM, FR 66 - FR 68, -Y1192 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007061200155 20070612 00155 EA 2007 6 12 A6WA200740224 1 20070511 A 2750 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA FLAP WARNING UNKNOWN A A6WA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 31 465AW 7893 FLAPS FAIL CAUTION MESSAGE INFLIGHT AFTER FLAP 8 TAKEOFF AFTER FLAP RETRACTION ALT, MOVED FLAP HANDLE TO ZERO, FLAPS STA YED AT 8. AIRSPEED 170 KTS OAT 21 DEGREES C. PERFORMED FLAPS FAIL CHECKLIST AND FLAPS 8 LANDING. TOUCHDOWN 164 KTS AT 100/MIN. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4, FLAP SYSTEM RESET OK. AIRCRAFT GOOD FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2007061200158 20070612 00158 NM 2007 6 12 AWXA200700712 1 20070604 A 5315 D534721987200 FLOORBEAM AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 SAL - CORROSION ON CABIN FLOORBEAM, FR 69 + 19", -Y254. REPLACED CABIN FLOOR BEAM, FR 68 - FR 70, -Y254 IAW A319 SRM 51 -72-11. 2 L 7 2 4F RT A28NM 2007061200188 20070612 00188 NM 2007 6 12 DL757070698 1 20070607 A 5420 BRACE BOEING 757 757232 1384965 NM NR 1 PYLON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 640DL 23994 DURING CURRENT HMV, THE NR 1 PYLON DIAGONAL BRACE REQUIRED OVERSIZING BEYOND THE EA LIMITS. AS SUCH, BOEING WAS CONTACT ED FOR APPROVAL TO OVERSIZE BEYOND LIMITS DUE TO AD 2003-18-05, AND THE WORK IS DOCUMENTED IN ERA 461664-14AD. 2 L 7 2 4F RT A2NM 2007061200189 20070612 00189 NE 2007 6 12 DL76G070699 2 20070607 A 7200 ENGINE BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6 30025 NE NR 2 INOPERATIVE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 1501P 45452 12047 695373 24983 695373 R ENGINE WOULD NOT START. R ENG FUEL VLV LIGHT ON PEDESTAL ILLUM. RTB, CYCLED VALVE RAN RT ENG. CHKS GOOD. 2 L 7 2 4F 4 F RT A1NM E13NE 2007061200201 20070612 00201 NM 2007 6 12 HALA0700243 1 20070604 A 2150 22030851 NOZZLE BOEING 767 767300 1385204 NM WATER SPRAY CLOGGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, ON RAMP AT OGG-LEFT PACK OUT TEMP 19DEG/RT PACK OUT-2DEG. TEMP VALVE POSITION R/L 0.00 RAM IN LET DOORS R/L 0.00. PREV ITEMS. UNABLE TO COOL A/C ON GND. FOUND HEAT EXCHANGER WATER SPRAY NOZZLE CLOGGED. REPLACED NOZZLE ASSY PER AMM 21-53-05-004-001. LK AND OPS CK GOOD, LEFT PACK OPS CKS GOOD. 2 L 7 2 4F RT A1NM 2007061300001 20070613 00001 CE 2007 6 13 AMWA84517 1 20070509 A 3230 1293640693 ANNUNCIATOR BEECH 1900 1900D 1154162 CE MLG WORN A AMWA O OTHER O OTHER AP APPROACH 1 CE 07 176YV UE176 UPON DEPART GEAR RETRACTED NORMALLY. NO PROBLEMS UNTIL GEAR EXTENSION. COULD NOT DETERMINE IF GEAR WAS COMPLETELY DOWN . FLEW BY TOWER AND THEY SAID IT APPEARED ONE OF THE GEAR WAS NOT COMPLETELY DOWN. PERFORMED MANUAL EXTENSION, BURNED OFF ADDITIONAL FUEL. DECLARED EMERGENCY AND BRIEFED PASSENGERS. ACFT LANDED WITHOUT FURTHER INCIDENT. REMOVED AND RE PLACED DOWNLOCK ANNUNCIATOR ASSEMBLY. 2 L 7 2 4T RT A24CE 2007061300008 20070613 00008 CE 2007 6 13 GUUA05060701 1 20070506 A 3230 847898 SELECTOR VALVE BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A GUUA O OTHER S AFFECT SYSTEMS AP APPROACH 1 SO 29 87552 UE216 FLIGHT: 9285 FLL/EYW - DURING APPROACH, LANDING GEAR DID NOT EXTEND WHEN SELECTED DOWN. MANUALLY EXTENDED LANDING GEAR. REPLACED SELECTOR VALVE. OPREATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY. 2 L 7 2 4T RT A24CE 2007061300012 20070613 00012 CE 2007 6 13 GUUA05180702 1 20070518 A 5330 SKIN BEECH 1900 1900D 1154162 CE BS 250 CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87551 UE206 AT SCHEDULED INSPECTION DISCOVERED BELLY SKIN CORROSION AT FS 250.00 AT STRINGER 14L. REMOVED DAMAGED SKIN AND INSTALLE D EXTERNAL REINFORCEMENT DOUBLER PER BEECH STRUCTURAL REPAIR MANUAL 51-70-06. 2 L 7 2 4T RT A24CE 2007061300013 20070613 00013 EA 2007 6 13 QXEA200700906 1 20070607 A 3240 BRAKE CNDAIR CL600 CL6002C10 1390015 EA MLG WEAK A QXEA O OTHER O OTHER LD LANDING 1 NM 09 614QX 10049 PDX - ON LANDING IN PDX, THE RIGHT BRAKE WAS VERY WEAK, HAD TO PUSH IT A LOT FURTHER TO GET ANY RESPONSE. MAINTENANCE B LED NR 3 AND NR 4 BRAKES. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007061300016 20070613 00016 CE 2007 6 13 GUUA05130701 1 20070513 A 3260 90422912 ANNUNCIATOR BEECH 1900 1900D 1154162 CE NLG MALFUNCTIONED A GUUA O OTHER N FALSE WARNING AP APPROACH 1 SO 29 16540 UE172 FLIGHT: 9232 TPA/EYW - DURING APPROACH, TWO ATTEMPTS TO GET THE NOSE GEAR DOWN AND LOCKED ON SECOND ATTEMPT IT TOOK TWO MINUTES TO LOCK. REPLACED NOSE GEAR ANNUNCIATOR ASSEMBLY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 2007061300018 20070613 00018 CE 2007 6 13 DXTA200702197 1 20070515 A 3233 99124913 ACTUATOR CESSNA 560 560XL 2076702 CE LT MLG DEFECTIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 696QS 4299 5605296 ON DEPARTURE AFTER RAISING THE GEAR, THE GEAR UNLOCK LIGHT ON AND THE GREEN NOSE GEAR LIGHT ILLUMINATED. RECYCLED THE G EAR AND HAD THE SAME INDICATION. EXTENDED GEAR AND GOT THREE GREEN. LT GEAR DOWN AND LANDED. REMOVED DEFECTIVE NOSE G EAR ACTUATOR AND INSTALLED INSPECTED CUSTOMER SUPPLIED NLG ACTUATOR. OPS CHECK AND LEAK CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. WORK DONE IAW CE-560XL AMM CHAPTER 32-30-03. 2 L 7 2 4F RT A22CE 2007061300019 20070613 00019 CE 2007 6 13 GUUA05040703 1 20070504 A 3297 727722 CIRCUIT BREAKER BEECH 1900 1900D 1154162 CE MLG UNKNOWN A GUUA O OTHER S AFFECT SYSTEMS TO TAKEOFF 1 SO 29 218YV UE218 FLIGHT: 9247 FLL/FLL - AFTER TAKEOFF LANDING, GEAR DID NOT RETRACT. RETURNED TO FLL LANDED WITHOUT INCIDENT. REPLACED THE LANDING GEAR CONTROL CIRCUIT BREAKER. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 2007061300025 20070613 00025 CE 2007 6 13 AMWA84414 1 20070505 A 2750 100384040 MOTOR BEECH 1900 1900D 1154162 CE TE FLAPS LOOSE A AMWA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 07 242YV 5035 2036 UE242 PILOT REPORTED FLAPS INOPERATIVE. SUBSEQUENT INVESTIGATION BY MAINTENANCE PERSONNEL FOUND THAT THE FLAP MOTOR MOUNTING SCREWS (2 EA) HAD COME LOOSE AND BACKED OUT OF THE FLAP GEARBOX ASSEMBLY. FLAP MOTOR, GEARBOX, AND HARDWARE WERE REMOVE D FROM AIRCRAFT AND INSPECTED WITH SATISFACTORY RESULTS FOR CONDITION/TIGHTNESS. FLAP MOTOR/GEARBOX ASSEMBLY WAS REINST ALLED INTO THE AIRCRAFT AND OPERATIONAL CHECKS WERE NORMAL. THERE ARE ONLY 2 MOUNTING SCREWS THAT SECURE THE FLAP MOTOR ONTO THE GEARBOX ASSEMBLY, AND THEY ARE NR 8 FLUSH MOUNTED SCREWS WITH NO MEANS FOR POSITIVE SAFETYING. THE AILERON CR OSS CONNECT CABLE IS DIRECTLY BELOW THIS MOTOR. IF CONDITIONS WERE RIGHT, IT COULD HAVE JAMMED THE AILERONS. WITH THE 2 L 7 2 4T RT A24CE 2007061300026 20070613 00026 NM 2007 6 13 KNNA200700031 1 20070508 A 5322 7075T6 SHEAR TIE BOEING 737 7372Q8 138448K NM PWA JT8 JT8D17 52049 NE BS 787 CORRODED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 413JG 23148 LIGHT SURFACE CORROSION AT SHEAR TIE ON BS 787, LOWER LOBE, BETWEEN STR 27L AND STR 27R, ACO NR 075370 REV 1. PROVIDE I NSTRUCTIONS ON REPAIR AT BS 787, LOWER LOBE, BETWEEN STR 27L AND STR 27R SRM 53-10-4 FIGURE 7. 2 L 7 2 4F 4 F RT A16WE E2EA 2007061300068 20070613 00068 CE 2007 6 13 DXTA200702196 1 20070514 A 5210 SEAL CESSNA 750 750 2076810 CE CABIN DOOR UNKNOWN E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 942QS 7500024 CABIN DOOR SEAL MESSAGE ILLUMINATED 1 HOUR AND 20 MINUTES INTO FLIGHT AT FL430, SHORTLY THERE AFTER IT COMMENCED TO SQUE ALING VERY LOUD. SQUEALING QUIT AROUND FL180 DURING DESCENT. EMERGENCY DECLARED. COULD NOT DUPLICATE "CABIN DOOR SEAL " CAS MESSAGE. PERFORMED FUNCTIONAL AND OPERATIONALLY CHECKS GOOD IAW CE750 M/M 52-10-04. 2 L 7 2 4J RT T00007WI 2007061300078 20070613 00078 NM 2007 6 13 AWXA200700697 1 20070601 A 3233 654482517 ACTUATOR BOEING 737 7373S3 1384711 NM RT MLG FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 313AW 75632 4634 23712 PHX- RETF - CREW REPORTED DURING CLIMB, RAISING THE GEAR CREW RECEIVED A RIGHT GEAR UNSAFE INDICATION CREW DECLARED AN E MERGENCY, BURNED OFF FUEL AND RETURNED TO PHX. THE LANDING WAS UNEVENTFUL. FUP 9809870 WAS ISSUED TO REPLACE CARD M986 . MX REPLACED CARD M986. OPERATIONAL CHECK WAS GOOD. WITH THE LANDING GEAR LEVER IN THE "OFF" POSITION THE RIGHT MAIN LANDING GEAR RED AND GREEN LIGHTS ILLUMINATED. DUE TO HISTORY, ENGINEERING REQUESTED MX REPLACE THE RIGHT MLG UPLOCK A CTUATOR AND THE RIGHT MLG MODULE VALVE ASSEMBLY. MX REPLACED THE COMPONENTS. CREW PERFORMED A FUNCTIONAL CHECK FLIGHT. OPERATIONAL CHECK WAS GOOD. THE A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007061300082 20070613 00082 SO 2007 6 13 LR7A07034 1 20070430 A 5320 34319321 TUBE LKHEED 382 382G 526414U SO FS 814 BENT A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2683 4606 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5313, FOUND RT AFT TUBE STRUT BENT AT FS 814, RBL62, WL165-255. REPLACED TUBE STRUT IAW SMP 583 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007061300086 20070613 00086 SO 2007 6 13 LR7A07038 1 20070430 A 5742 3706561R FITTING LKHEED 382 382G 526414U SO FS 517 DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2683 4606 DURING SCHEDULED C-8 CHECK PER JOB CARD HSP57131, FOUND NR 2 ENGINE OUTBD TRUSS MOUNT OUTBD ATTACH FITTING HOLES OVERSIZ ED AT FS 517, CWS214L, WL280. REPLACED FITTING IAW SMP 583 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007061300087 20070613 00087 SO 2007 6 13 LR7A07039 1 20070430 A 5742 33035502 FITTING LKHEED 382 382G 526414U SO FS 517 SCORED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2683 4606 DURING SCHEDULED C-8 CHECK PER JOB CARD HSP57131, FOUND OUTBD RIB CAP FITTING SCORED AT FS 517, CWS178R, WL280. REPLACE D FITTING IAW SMP 583 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007061300089 20070613 00089 SO 2007 6 13 LR7A07041 1 20070430 A 5330 SKIN LKHEED 382 382G 526414U SO FS 797E DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2683 4606 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5321, FOUND LT FUSELAGE EXTERIOR SKIN DENTED AT FS 797E, LBL62, WL146. REPAIR ED SKIN IAW SMP 583 51-140-12. 2 H 7 4 4T A1SO 2007061300091 20070613 00091 NM 2007 6 13 QXEA200700902 1 20070607 A 3213 4610803 AXLE BOMBDR DHC8 DHC8402 1390042 NM MLG UNKNOWN A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 426QX 310 4154 BOI FLIGHT NR 2320: UPON ARRIVAL AT THE GATE, RAMP PERSONNEL INDICATED SMOKE FROM RIGHT TIRE AREA. MAINTENANCE REMOVED AND REPLACED NR 2 MLG AXLE IAW AMM TASKS 32-11-04-000-801 AND 32-11-04-400-801, STEPS 1-4, A(17). COMPLETED REPLACEMENT OF NR 2 MLG AXLE IAW Q400 AMM TASK 32-11-04-000-801, STEPS 4A (18) THROUGH 5G. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061300151 20070613 00151 CE 2007 6 13 2007F00026 1 20070403 A 3200 LANDING GEAR BEECH 1900 1900D 1154162 CE MALFUNCTIONED H O OTHER G MULTIPLE FAILURE DE DESCENT 1 SW 99 139YV THIS AIRCRAFT HAS HAD MULTIPLE REOCCURRING GEAR MALFUNCTIONS. ON NUMEROUS OCCASIONS THE AIRCRAFT HAS HAD THE LANDING GE AR CIRCUIT BREAKER POP IN-FLIGHT WITCH HAS RESULTED IN A MANUAL PUMPING OF THE LANDING GEAR HYDRAULIC SYSTEM. THE AIRCR AFT HAS BEEN BROUGHT TO THE MAINTENANCE HANGAR FOR THESE ISSUES AND BEEN RETURNED TO SERVICE WITHOUT ANY REPAIR OR RESOL UTION TO THE PROBLEM. THIS IS A SEVER SAFETY ISSUE AND NEEDS TO BE INVESTIGATED BY THE FAA SAFETY BOARD. THE MAINTENAN CE GROUP CONTINUALLY SIGNS OFF THE AIRCRAFT AS "UNABLE TO DUPLICATE". MULTIPLE CREWS HAVE HAD ISSUES WITH THIS AIRCRAFT . FAILURE TO RESOLVE THIS ISSUE WILL EVENTUALLY RESULT IN AN AIRCRAFT ACCIDENT AND MOST LIKELY RESULT IN LOSS OF LIFE. 2 L 7 2 4T RT A24CE 2007061300153 20070613 00153 CE 2007 6 13 2007F00036 1 20070427 A 5210 45A30096 DOOR MTSBSI MU300 MU300 5780602 CE CABIN CRACKED B K NONE O OTHER IN INSP/MAINT 1 CE 09 417KT 14430 A083SA DURING SCHEDULED A, B, & C INSPECTION FOUND CABIN ENTRANCE DOOR CASE ASSEMBLY P/N: 45A30096 CRACKED AT DOOR BUSHING HOLE S. CASE ASSEMBLY IS NONE REPAIRABLE AND REQUIRED REMOVAL AND REPLACEMENT WITH NEW. THE NEW CASE ASSEMBLY CAUSE A INTERFE RENCE FIT WITH THE DOOR HINGE LUGS. RECIEVED A REPAIR DRAWING FROM RDO TO MODIFY DOOOR LUGS TO ALEAVATE INTERFERNCE FIT. 2 H 7 2 4F RT A14SW 2007061300170 20070613 00170 EA 2007 6 13 N6WA0070501 1 20070502 A 3350 6100928 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 163 10255 MX-STL-SERVICE DOOR LOWER EMERG LIGHT INOP. REPLACED BULB ON SERVICE DOOR LIGHT ASSEMBLEY. 2 L 7 2 4F RT A21EA 2007061300240 20070613 00240 NM 2007 6 13 ASAA0791757 1 20070531 A 5321 453A261019 FLOOR PANEL BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 CORROSION ON AFT CARGO PIT FLOOR PANEL. REPAIRED IAW SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007061300254 20070613 00254 NM 2007 6 13 ZZDA070606177 1 20070606 A 3350 8039251 BATTERY BOEING 717 717200 1383700 NM EMERGENCY LIGHT FAILED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 923AT 55051 EMERGENCY LIGHTS ON SEAT ROWS 1, 2, 3 AND 10 INOPERATIVE. REPLACED BATTERY SUPPLY ASSY. 2 L 7 2 4F TR A6WE 2007061300255 20070613 00255 NM 2007 6 13 ASAA0791762 1 20070531 A 5320 142A7501107 FLOOR SUPPORT BOEING 737 737990 NM BS 500 DRILLED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 FWD CARGO FLOOR PANEL SUPPORT AT BS 500 HAS DRILLED HOLES. REPAIRED IAW SRM 53-00-53. 2 L 7 4 4F RT A16WE 2007061300257 20070613 00257 NM 2007 6 13 ASAA0791764 1 20070531 A 5321 453A161014 FLOOR PANEL BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 CORROSION AT FWD CARGO FLOOR PANEL AT STA 395. REPAIRED IAW 51-40-05. 2 L 7 4 4F RT A16WE 2007061300261 20070613 00261 NM 2007 6 13 ASAA0791768 1 20070531 A 5321 146A812712 SHIELD BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 CARGO PIT FLOOR SHIELD AT BS 767 CORRODED. REPAIRED IAW 51-40-02. 2 L 7 4 4F RT A16WE 2007061300268 20070613 00268 GL 2007 6 13 AC2A115393 2 20070505 A 7321 23070613 FUEL CONTROL SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL ENGINE MALFUNCTIONED B AC2A A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 31 7266K 760283 DURING A TRAINING FLIGHT, WE WENT TO 3,500 FEET AND ENTERED AUTOROTATION BY RETARDING BOTH ENGINE LEVERS TO IDLE. AFTER ESTABLISHING A STABILIZED AUTOROTATIONAL GLIDE, I BEGAN THE RECOVERY BY FIRST MOVING THE NR 2 ENGINE LEVER BACK TO FLY . I THEN STARTED MOVING THE NR 1 ENGINE LEVER TO FLY. ABOUT HALF WAY BETWEEN IDLE AND FLY, THE ENGINE QUIT. RATHER TH AN TRY TO RESTART THE ENGINE IN FLIGHT, WE PROCEEDED TO ABBEVILLE AIRPORT AND PERFORMED A SINGLE ENGINE LANDING. AFTER MAINTENANCE CHECKED THE ENGINE, WE STARTED BOTH ENGINES AND CHECKED NR 1 BY MOVING THE ENGINE LEVER DIRECTLY TO “FLY” A S RAPIDLY AS POSSIBLE. EVERYTHING APPEARED NORMAL, BUT WE DECIDED TO REPEAT THE CHECK. WHEN I MOVED THE ENGINE LE 1 G 7 2 3U 3 U H1NE E1GL 2007061300269 20070613 00269 SW 2007 6 13 AC2A115394 1 20070428 A 2497 UNKNOWN WIRE HARNESS BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL DAMAGED B AC2A K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 31 53702 51249 THE MECHANIC WAS PERFORMINGGA DAILY ENGINE WASH. THE AIRCRAFT ENGINE WAS MOTORED AND THE WATER WAS SPRAYED INTO THE ENGI NE. AFTER COAST DOWN THE BATTERY SWITCH WAS TURNED OFF TO LET THE REMAINING WATER DRAIN OUT. WHEN THE BATTERY SWITCHED W AS TURNED OFF THE SYSTEM STAYED ENERGIZED AND THE ENGINE OUT HORN CAME ON. I CYCLED THE SWITCH ATTEMPTING TO TURN OFF T HE BATTERY AND THIS TIME THE ENGINE OUT AND LOW ROTOR HORN SOUNDED. I CYCLED THE SWITCH A THIRD TIME WITH THE SAME RESUL TS. AFTER THE THIRD ATTEMPT TO TURN OFF THE POWER I SMELLED SMOKE, SO I OPENED THE BATTERY DOOR TO DISCONNECT THE BATTE RY AND SAW THE WIRE BUNDLE JUST TO THE RIGHT OF THE BATTERY ARCING. I DISCONNECTED THE BATTERY AND THE ARCING WENT OUT. 1 G 7 1 3U 3 U H2SW E1GL 2007061300271 20070613 00271 NE 2007 6 13 HEEA115464 1 20070430 A 3297 WIRE SKRSKY S76 S76A 8143006 NE MLG CHAFED B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 5435V 760158 ON ARRIVAL AT DC618, EXPERIENCED 3 UNLOCKED INDICATIONS WHEN GEAR WAS LOWERED. ATTEMPTED TO RECYCLE GEAR SEVERAL TIMES AS PER CHECKLIST, TO NO AVAIL. DIVERTED TO BOOTHVILLE, AND LANDED UNEVENTFULLY. THE SHORT CAUSING THE LANDING GEAR POS ITION LIGHT CIRCUIT BREAKER TO POP WAS A CHAFED WIRE IN THE #1 RELAY PANEL FROM PLUG 105 JACK 2 PIN DD TO TERMINAL B2 O F RELAY K28. REPAIRED WIRE AND FUNCTION CHECKED POSITION LIGHT CIRCUIT, FOUND OK. 1 G 7 2 3U H1NE 2007061300277 20070613 00277 NM 2007 6 13 2007UALA01498 1 20070511 A 3820 417N2322 WATER HEATER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LAVATORY FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 571UA 26681 NO H2O PRESSURE TO LAVS OR GALLEYS. 1:10 INTO FLT AFT LAV H2O HEATER. AFT LAV, LAV 'R', LAV IS WHERE ACRID ODOR WAS CO MING FROM. FOUND WATER HEATER OVERTEMP CONDITION TRIPPED CIRCUIT BREAKER INSIDE HEATER. LAV IS WHERE ACRID ODOR WAS CO MING FROM. CB ON PNL P37 WAS COLLARED. ALL OTHER WATERHEATERS HAVE BEEN REACTIVATED. WATER SERVICE PANEL HAD VALVE PA RTIALLY OPEN. RESET CB HEATER AND SYSTEM WAS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061300282 20070613 00282 NM 2007 6 13 QXEA200700911 1 20070608 A 2750 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS UNKNOWN A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 417QX 4086 SEA FLIGHT NR 2299: FLAP POWER CAUTION LIGHT ON AFTER START. PER CHECKLIST, CYCLED L7 CIRCUIT BREAKER. CAUTION LIGHT E XTINGUISHED. MAINTENANCE C/W AIRCRAFT CHECKLIST. CAUTION LIGHT EXTINGUISHED. MTX CONTROL WAS NOTIFIED. NO PARTS REPL ACED AND AIRCRAFT RETURNED TO SERVICE PER MTX CONTROL. 2 H 7 2 4T RT A13NM 2007061300285 20070613 00285 EU 2007 6 13 NWAA072103265 1 20070605 A 3350 BATTERY PACK AIRBUS 320 A320212 3930322 EU EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 365NW 0964 DURING OVERNIGHT LINE CHECK, EPSU INT LOAD EMER RT FAULT. REPLACED RIGHT EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHE CK OK. 2 L 7 2 4F RT A28NM 2007061300286 20070613 00286 NM 2007 6 13 NWAA072096301 1 20070606 A 3350 BATTERY BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 661US 23719 DURING OVERNIGHT LINE CHECK, FOUND TWO AFT RIGHT OVERWING EMERGENCY LIGHTS OUT. MAINTENANCE REMOVED AND REPLACED BATTER Y AND POWER SUPPLY. OPERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007061300288 20070613 00288 NM 2007 6 13 2007UALA01743 1 20070529 A 2722 ACTUATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RUDDER MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 WP 29 398UA 24673 CREW REPORTS RUDDER BINDING, REQUIRED MORE RUDDER PRESSURE TO USE. PEDAL ALSO STICKS AND STUCK ON APPROACH TO IAD. REP LACED RUDDER ACTUATOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061300290 20070613 00290 NM 2007 6 13 2007UALA01745 1 20070531 A 3350 321431 BATTERY PACK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 810UA 843 EMERGENCY EXIT LIGHT SYS TEST FAILED, FAULTED AFT LT BATTERY PACK. BATTERY PACK SYS TEST OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061300293 20070613 00293 NM 2007 6 13 2007UALA01748 1 20070531 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 FWD LT ENTRY DOORWAY UPPER HINGE CUTOUT HAS A FASTENER HOLE WITH A CRACK INDICATION JUST BELOW UPPER HINGE CUTOUT APPROX 7.5" FWD OF FWD DOOR CUTOUT. [06-26-07] MAJOR REPAIR: REMOVED DAMAGE. ACCOMPLISHED DOUBLER AND FILLER REPAIR PER AAR EAI070356 REV IR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061300294 20070613 00294 NM 2007 6 13 2007UALA01749 1 20070531 A 5100 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE NONE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 UPPER FUSELAGE SKIN UNDER DORSAL FIN LT SIDE HAS WORN AREAS FROM BS 908 TO 927. [06-26-07] MAJOR REPAIR: ACCOMPLISHED A FPI INSPECTION NO DEFECTS FOUND AREA TREATED AND PRIMED AND INSTALLED WEAR STRAPS PER AAR EA REV IR EAI070361. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061300295 20070613 00295 NM 2007 6 13 2007UALA01750 1 20070531 A 5330 TEAR STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 UPPER FUSELAGE SKIN UNDER DORSAL FIN RT SIDE HAS WORN AREAS FROM BS 908 TO 967. [06-26-07] MAJOR REPAIR: REMOVED DAMAG E. INSTALLED DOUBLER, TRIPLER AND TEAR STRAP. REFERENCE AAR EA REV IR I070361. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061300296 20070613 00296 NM 2007 6 13 2007UALA01751 1 20070531 A 5230 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO BAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 FWD CARGO DOOR (S-N 1765) AFT FRAME IS CRACKED AT LWR CORNER INNER RADIUS OF OUTBD FLANGE JUST ABOVE LWR STOP FITTING. [06-26-07] MAJOR REPAIR: REMOVED AND REPLACED AFT LOWER FRAME. REFERENCE SRM 51-40-02 AND DRW 65-46921. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061300297 20070613 00297 NM 2007 6 13 2007UALA01752 1 20070531 A 5241 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 FWD GALLEY DOOR, AFT FRAME, THIRD FROM BOTTOM STOP PIN CUTOUT CRACKED. [06-26-07] MAJOR REPAIR: REMOVED CRACK. INSTALL ED REPAIR DOUBLER REF SM 90-52-40-14 JD PG 24 FIG 10 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061300299 20070613 00299 NM 2007 6 13 2007UALA01754 1 20070531 A 5241 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 FWD GALLEY DOOR, AFT FRAME CRACKED LWR END AT OUTBD FASTENER HOLE. [06-26-07] MAJOR REPAIR: REPAIRED PER SRM 52-10-02 PAGE 107 NOTE A. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061300300 20070613 00300 NM 2007 6 13 2007UALA01755 1 20070531 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 LT AFT ENTRY DOOR THRESHOLD INNER CREASE BEAM CHORD ANGLE CORRODED AT BS 963-983 AT WL 208 LBL 53-55. [06-26-07] MAJOR REPAIR: REMOVED CORROSION. REFERENCE PART 4, 51-00-90 AND SRM 53-60-15 FIG 101 PG113. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061300301 20070613 00301 NM 2007 6 13 2007UALA01756 1 20070531 A 5310 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE SCRATCHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 LOWER FUSELAGE BENEATH AFT CARGO PIT DOOR APPROX BS 804 HAS SCRATCHES. [06-26-07] MAJOR REPAIR: REPAIRED LOWER SKIN. I NSTALLED DOUBLER AND FILLER. REFERENCE EA I070390 REV IR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061300303 20070613 00303 NM 2007 6 13 2007UALA01758 1 20070531 A 5313 STRINGER SPLICE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 S15L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 CABIN STRINGER SPLICE STA 360 STR 15L CRACKED, AFT SIDE OF FRAME. [06-26-07] MAJOR REPAIR: FABRICATED AND INSTALLED S TRINGER SPLICE CHANEL PER AAR EA REV IR I070345 AND UA-EVA-70301. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061300304 20070613 00304 NM 2007 6 13 2007UALA01759 1 20070531 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 MAIN CABIN FWD ENTERY DOOR SURROUND STA 294.5 STR 7 LT FWD WEB IS CRACKED. [06-26-07] MAJOR REPAIR: REPLACED STR 7L IN TERCOSTAL WEB PER AAR EA-I070345 AND US EVA-70301. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061300305 20070613 00305 NM 2007 6 13 2007UALA01760 1 20070531 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 S11L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 MAIN CABIN FWD ENTERY DOOR SURROUND AT STA 294.5 STR 11 LT INTERCOSTAL UPPER ATTACH ANGLE IS CRACKED. [06-26-07] MAJOR REPAIR: REPALCED STR 11L INTERCOSTAL ATTACH SHEAR TIE AT BS 294 PER AAR EA-I070345 AND UA EVA-70301. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061300306 20070613 00306 NM 2007 6 13 2007UALA01761 1 20070531 A 5711 SPAR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT WING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 RT WING REAR SPAR FITTING REQUIRES FREEZE PLUG INSTALLATION. [06-26-07] MAJOR REPAIR: FABRICATED AND INSTALLED FREEZE PLUG. REFERENCE AAR EA REV IR I070357. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061300307 20070613 00307 NM 2007 6 13 2007UALA01762 1 20070531 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 727 S13L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 FUSELAGE FRAME CRACKED AT STR CUTOUT, BS 727 STR 13L. [06-26-07] MAJOR REPAIR: INSTALLED NESTED FRAME DOUBLER REPAIR P ER AAR EA-I070344 ON AAR NR12000-2000-0021. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061300309 20070613 00309 NM 2007 6 13 2007UALA01764 1 20070531 A 3340 1317 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NAV LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 LT AND RT AFT NAV INBD LIGHTS ARE INOPERATIVE. RELAMPED. OPS CKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007061300312 20070613 00312 NM 2007 6 13 HALA07000247 1 20070610 A 2720 CONTROL CABLE BOEING 717 717200 1383700 NM RUDDER OUT OF RIG A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 475HA 55121 DURING FLIGHT CONTROL CHECK RUDDER PEDAL TRAVEL IS STIFF. FOUND RUDDER CONTROL CABLE OUT OF RIG. ADJUSTED RUDDER CONTR OL CABLE SYSTEM PER BOEING 717 AMM 27-20-00. PERFORMED OPS CHECK OF RUDDER PEDAL PER AMM 27-20-00. CHECKED OK. INSPEC TED CABLE RUN AFT OF AFT PRESSURE BULKHEAD. 2 L 7 2 4F TR A6WE 2007061300318 20070613 00318 NM 2007 6 13 2007UALA01771 1 20070601 A 3350 LAMP AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 836UA 1460 EMERGENCY ESCAPE PATH LIGHT AT 22ABC INOPERATIVE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061300319 20070613 00319 NM 2007 6 13 2007UALA01772 1 20070601 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 839UA 1507 LT OB SEAT TRACK BETWEEN FRAME 42 AND 47 HAS WORN AREAS BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED: REPLACED FLOORBEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061300320 20070613 00320 NM 2007 6 13 2007UALA01773 1 20070604 A 5347 SEAT TRACK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 839UA 1507 RT IB SEAT TRACK BETWEEN FRAME 42 -47 HAS WORN AREAS BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED: REPLACED FLOORBEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061300323 20070613 00323 EU 2007 6 13 2007UALA01776 1 20070602 A 5311 FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 434UA 592 FWD PIT HAS NUMEROUS CORRODED FASTENERS ON FRAME CLEATS, STRINGERS, STRINGER CLIPS AND SKIN DOUBLERS, FROM FRAME 24 TO F RAME 35 BETWEEN STR 38L AND 38R. REPLACED A TOTAL OF 1290 RIVETS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061300324 20070613 00324 NE 2007 6 13 2007UALA01777 2 20070601 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 OVERSPEED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 448UA 842 V10099 RTFL DUE TO NR 2 ENGINE N2 OVERSPEED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061300328 20070613 00328 NM 2007 6 13 2007UALA01876 1 20070604 A 2810 FUEL CELL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT WING LEAKING A UALA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 29 351UA 24319 FUEL LEAK RT WING, NEAR NR 2 ENG AREA. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061300330 20070613 00330 NM 2007 6 13 2007UALA01878 1 20070606 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EEL INOP: ROW 55 HJK AND ROW 57 HJ. [06-22-07] REPLACED SEAT EEL LAMP,OPS CHECK GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2007061400002 20070614 00002 EU 2007 6 14 TRBA200729 1 20070607 A 3350 E006478A50 SWITCH AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHTS FAILED A TRBA O OTHER O OTHER NR NOT REPORTED 1 SO 29 548AT 548 ALL PAX CABIN EMERGENCY LIGHTS REMAIN ON AT ALL TIMES. RAI 2 MIN, LIGHT SWITCH IAW MM NR 33-12-80. OPT CK OK. 2 H 7 2 4T RT A53EU 2007061400004 20070614 00004 SO 2007 6 14 GUUA05310701 1 20070531 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO CABIN/COCKPIT ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 17 280AS 120231 DURING APU START WITH BOTH ENGINES RUNNING A STRONG ODOR OF JET A ENTERS THE CABIN AND COCKPIT. THIS HAPPENS AT THE END OF THE START SEQUENCE AFTER THE GEN TURNS ON. CHECKED ENGINE AND APU, NO LEAKS NOTED. STARTED APU. OPS CHECK NORMAL. 2 L 7 2 4T RT A31SO 2007061400005 20070614 00005 SO 2007 6 14 GUUA06060701 1 20070606 A 3260 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO MLG DIRTY A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 17 268AS 120202 RED LANDING GEAR SYSTEM, "A" LIGHTS FLICKERED ON AND OFF DURING CRUISE. CLEANED ALL LANDING GEAR PROXIMITY SENSORS. OP ERATIONAL CHECKS SATISFACTORY. 2 L 7 2 4T RT A31SO 2007061400008 20070614 00008 NM 2007 6 14 2007UALA01880 1 20070606 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERG LT INOP, CEILING ROW 12. [06-22-07] RELAMPED,OPS CHECK GOOD RE FMM 33-51-00. 2 L 7 4 4F 4 F RT A20WE E24NE 2007061400010 20070614 00010 NM 2007 6 14 2007UALA01882 1 20070606 A 3350 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 WALL EEL INOP, DOOR 4R AISLE. [06-22-07] REPLACED POWER SUPPLY FOR EEL. OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007061400012 20070614 00012 NM 2007 6 14 2007UALA01781 1 20070602 A 2621 EXTINGUISHER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO BAY DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 BOTH FWD AND AFT PIT FIRE BOTTLES HAVE BEEN DISCHARGED, CONDITION FOUND UPON ARRIVAL. REMOVED AND REPLACED FWD & AFT PI T FIRE BOTTLES. ALSO, REPLACED THE METERING VALVE, DIVERTER AND FILTERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061400015 20070614 00015 2007 6 14 2007UALA01784 4 20070603 A 3442 RADAR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE WX SYSTEM MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 485UA 1617 FLIGHT DIVERTED DUE TO WEATHER RADAR PROBLEM AND INCLEMENT WEATHER. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072600013 20070726 00013 NM 2007 7 26 DHL2007784515 1 20070711 A 5311 FRAME BOEING 727 727227 1384078 NM ZONE 100 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 AFT CARGO COMPARTMENT BS 970, STR 29L-28L HAS FRAME FLANGE CRACKED OUT WITH CORROSION. CUT OUT DAMAGED SHEAR TIE AT BS 970, BETWEEN STR 28L-29L IAW B727 SRM 53-10-4, FIG 13. FABRICATED SHEAR TIE REPAIR MATERIAL USED 7075T6 .071” DIM 6.50 ” BY 7 IAW B727 SRM 53-10-2, FIG 5 AND 53-10-4, FIG 13. TREATED, PRIMED AND INSTALLED SHEAR TIE IAW B727 SRM 51-10-2 AN D 51-30-2. 2 L 7 3 4F A3WE 2007061400017 20070614 00017 NM 2007 6 14 2007UALA01788 1 20070601 A 2160 SHUTOFF VALVE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN TEMP MALFUNCTIONED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 670UA 29240 CABIN TEMPERATURE CONTROL UNACCEPTABLE IN MANUAL. [07-13-07] AFTER EXTENSIVE TROUBLESHOOTING, R & R TRIM AIR PRSOV P ER MM21-61-06, LEAK & OP CHECKED GOOD, BUT PROBLEM REOCCURRED. AFTER MORE TROUBLE-SHOOTING, REPLACED RELAY K629. SYST EM FINALLY WORKED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007061400020 20070614 00020 NM 2007 6 14 2007UALA01791 1 20070602 A 2433 ELECTRICAL SYS BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE DC STANDBY NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 797UA 26924 ELEC STANDBY SYS ELECTRICAL DC-STANDBY POWER SYSTEM FAILED THE SYSTEM SELF-CHECK. [07-06-07] REPLACED BUSS TIE, MAIN BATTERY RELAY. AIRPLANE OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007061400022 20070614 00022 EU 2007 6 14 TRBA200730 1 20070609 A 3222 D63785 STRUT AEROSP ATR72 ATR72212A 8680902 EU NLG SCORED A TRBA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 29 536AT 536 LOTS OF NOISE COMING FROM NOSE WHEEL WHEN TURNING RIGHT. REMOVED AND REPLACED NLG SHOCK ABSORBER AND STRUT IAW JIC NR 3 2-21-00. 2 H 7 2 4T RT A53EU 2007061400023 20070614 00023 2007 6 14 2007UALA01793 4 20070603 A 2565 GIRT BAR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE DOOR 1L OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 SLIDE GIRT HANGING TOO FAR OUT OF SLIDE PACK. [06-26-07] RESECURED GIRT. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061400024 20070614 00024 NM 2007 6 14 2007UALA01885 1 20070608 A 5310 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 610 S16L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 FOUND STA 610 S16L IS DAMAGED. [08-07-07] MAJOR REPAIR ACCOMPLISHED.FABRICATED REPAIR DOUBLERS. NEW REPAIR TO ENCOMPA SS 2 PREVIOUS DOUBLERS IN SAME AREA SHOWING DENT FWD DOOR 2L. BLENDED OUT GOUGES AND EDDY CURRENT TESTED FOR CRACKS, NO CRACKS NOTED. REMOVED KICK PANELS IN F-C AND VISUALLY CHECKED STRICKER FOR CRACKS, NONE NOTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061400025 20070614 00025 EU 2007 6 14 COEA0710903 1 20070109 A 5314 S53574100202 KEELBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A KIMA K NONE O OTHER IN INSP/MAINT 1 NM 13 903FX 179 CORROSION LEVEL 2, DURING HEAVY CHECK, FOUND CORROSION ON BOTTOM SIDE OF KEEL BEAM CHORD FROM AFT EDGE TO 4 INCHES OF AF T EDGE. REMOVED KEEL BEAM CHORD FROM FRAMES 25-27 AND REMOVED CORROSION. FABRICATED AND INSTALLED NEW KEEL BEAM CHORD IAW ATR42 SRM. (M) 2 H 7 2 4T RT A53EU 2007061400026 20070614 00026 NE 2007 6 14 2007UALA01886 2 20070607 A 7250 BLADE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 ENGINE WORN A UALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 WP 29 774UA 40053 11542 26936 777012 RTFL DUE TO NR 1 ENGINE SURGE. ENGINE SURGED IN CRZ APPROX 2-1/2 HRS OUT FROM IAD EN ROUTE MUC. DECISION TO RETURN TO IAD. AFTER LDG, IAD MM FOUND METAL IN TAILPIPE. ENG REPLACED AT IAD. [08-14-07] TEARDOWN REVEALED THAT 4 LP TURBINE TRANSITION DUCTS (PW IPC 72-30-00-002-250, P/N 50M919) HAD EXPERIENCED EXTREME INNER FOOT WEAR. THIS CAUSED A LOSS OF R ADIAL RETENTION AT THE FRONT OF THE DUCT, ALLOWING DUCTS TO DEFLECT INWARDS INTO PRIMARY GASPATH, AND DISTORTING GASPATH FLOW INTO THE LP TURBINE, RESULTING IN SURGE. UA HAS SEEN FOOT WEAR AT TEARDOWN, BUT NEVER TO THIS EXTENT. PARTS HAVE BEEN RETURNED TO MANUFACTURER & MTU FOR FURTHER ANALYSIS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007061400032 20070614 00032 EA 2007 6 14 TRAX200700800 1 20070605 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 907EV 7648 FLAPS FAIL ZERO POSITON IN FLT 30000 FT, EMERGENCY DECLARED, FLT 4338 DEL 37 MINS. [07-06-07] INSPECTED FLAPS, INTERRO GATED FECU & RESET SYSTEM. RESET OK, C/W EO 600-27-0054 A/C OK FOR SERVICE. MOVED TO MCO #044318, PRIORITY 1 REQUIRE C/W OF EO 600-27-0054 WITHIN 72 HRS. C/W EO600-27-0054-01 2 L 7 2 4F RT A21EA 2007061400034 20070614 00034 EA 2007 6 14 TRAX200700802 1 20070607 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 AFT MOST CEILING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007061400037 20070614 00037 EA 2007 6 14 TRAX200700809 1 20070609 A 5210 GATE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 MAIN PASSENGER DOOR STUCK IN CLOSED POSSITION. PRESSURE FLAP WILL OPEN BUT DOOR WILL NOT OPEN FROM INSIDE CABIN OR OUTS IDE CABIN. 2 L 7 2 4F RT A21EA 2007061400039 20070614 00039 EA 2007 6 14 TRAX200700779 1 20070603 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 906EV 7642 CRACK FOUND ON INTERCOSTAL FS 484 RBL 39. 2 L 7 2 4F RT A21EA 2007061400044 20070614 00044 NM 2007 6 14 2007UALA01888 1 20070607 A 2612 FIRE DETECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 1 NACELLE FAULTY A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 839UA 1507 FIRE LOOP A FAULT DISPLAYED ON UPPER ECAM SCREEN - ENG 1. REPLACED NR 1 ENG FIRE DETECTOR UNIT AS PRECAUTION. COULD N OT DUPLICATE FIRE WARNING SIGNAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061400045 20070614 00045 NM 2007 6 14 2007UALA01889 1 20070607 A 3350 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 816UA 871 CABIN EMERGENCY LIGHT TEST FAILED. EPSU 115 VAC EMER L. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061400049 20070614 00049 NM 2007 6 14 2007UALA01893 1 20070607 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN UNKNOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 30024 ALL EMERGENCY EXIT LIGHTS IN CABIN EXCEPT FLOOR PATH LIGHTS ON IN CRUISE MOMENTARILY WITHOUT SWITCH ON. [07-03-07] CO NFERED WITH FLT CREW. LIGHTS CAME ON FOR 30 SEC THEN REMAIN OUT. CYCLE EMERG LIGHTS SWITCH AND CHECKED EMERG LIGHT. OPS CK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007061400050 20070614 00050 NM 2007 6 14 2007UALA01894 1 20070607 A 3350 LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT MISSING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 768UA 26919 FOUND SEAT 1E HAS AFT EMERGENCY LIGHT MISSING. [06-26-07] RELAMPED. TESTED GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007061400051 20070614 00051 NM 2007 6 14 2007UALA01895 1 20070608 A 2432 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 560UA 26660 FLIGHT DIVERTED DUE TO BATTERY MESSAGE. TEMPORARILY LOST ALL F-O FLT INSTRUMENTS. CAME BACK ON AFTER A FEW MINUTES. [ 08-07-07] FO INSTRUMENTS CAME BACK ON AFTER A FEW MINUTES. REPLACED MAIN BATTERY AND BATTERY CHARGER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061400052 20070614 00052 NM 2007 6 14 2007UALA01896 1 20070609 A 3150 UNKNOWN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE WARNING LIGHT A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 831UA 1291 RTFL DUE TO SMOKE ECAM MESSAGE INDICATION. NO DEFECTS IDENTIFIED THROUGH TROUBLESHOOTING. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061400055 20070614 00055 CE 2007 6 14 DXTA200702180 1 20070508 A 3240 BRAKE ASSY RAYTHN DH125 HAWKER800XP 7150012 CE MLG WEAK E DXTA K NONE O OTHER IN INSP/MAINT 1 GL 07 858QS 258691 BRAKES VERY SPONGY AND UNEQUAL. BLED BRAKES IAW HAWKER 800XP MM 32-40-00. TAXIED ACFT AND OPERATED BRAKES. NO DISCREP ANCIES WERE NOTED. 2 L 7 2 4F RT A3EU 2007061400056 20070614 00056 CE 2007 6 14 DXTA200702181 1 20070508 A 3241 HUB CESSNA 500 560CESSNA 2076750 CE ANTI SKID SYS OUT OF LIMITS E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 319QS 5600519 WHILE DECELERATING STRAIGHT AHEAD ON THE RUNWAY, AT APPROX 20 KNOTS, BRAKES RELEASED MOMENTARILY THEM FUNCTIONED NORMALL Y. AIRCRAFT WAS NOT IN A TURN. FOUND ANTI-SKID HUB CLIPS TO BE OUT OF .140" LIMIT. ADJUSTED CLIPS IAW CHAP 32-42-00 O F THE CE-560 MAINT MANUAL. BLED ANTI-SKID BRAKE SYSTEM IAW CHAP 32-42-00 OF THE CE-560 MAINT MANUAL. OPERATIONAL CHECK S SATISFACTORY. 2 L 7 2 4F RT A22CE 2007061400058 20070614 00058 NM 2007 6 14 F3LA200700124 1 20070530 A 5321 D5367180500500 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 920FR 5184 1997 DURING C-3 CHECK, INSPECTION REPORTED FLOOR PANEL 262FF CORRODED ON LOWER SIDE. REPLACED FLOOR PANEL IAW AMM 53-12-12-0 00-001. 2 L 7 2 4F RT A28NM 2007061400060 20070614 00060 EU 2007 6 14 07FDEA01874 1 20070521 A 5330 A53778050 SKIN AIRBUS 310 A310222 3930315 EU ZONE 100 UNKNOWN A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED LT FS 2029-2082 FR 37-38 AND STR 39-42. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETE RMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFOR M TO AN SRM REPAIR. NEW REPAIR WAS ACCOMPLISHED PER SRM 53-10-12 FIG 228 SHEET 1. 2 L 7 2 4F RT A35EU 2007061400061 20070614 00061 EU 2007 6 14 07FDEA01877 1 20070521 A 5330 R53610174 SKIN AIRBUS 310 A310222 3930315 EU ZONE 200 NONE A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED LT FS 1285 FR16A STR20-23. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-12-81 FIG 203. 2 L 7 2 4F RT A35EU 2007061400062 20070614 00062 EU 2007 6 14 07FDEA01883 1 20070521 A 5753 A579713010160 FLAP AIRBUS 310 A310222 3930315 EU ZONE 500 NONE A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON LT LWR WING SURFACE OUTBOARD FLAP WS935-996 RIB15-16. REPAIR REQUIRES EVALUATION FOR M AJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR CONFORMS TO EXISTING FEDEX EN GINEERING AUTHORIZATION EA 6-5750-81815. 2 L 7 2 4F RT A35EU 2007061400068 20070614 00068 NM 2007 6 14 F3LA200700127 1 20070602 A 2150 ABS10405664 SEAL AIRBUS A319 A319111 3930336 NM NR 2 PACK WORN A F3LA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 03 925FR 2103 WHILE PARKED AT GATE, FLIGHT CREW REPORTED BURNED ELECTRIC ODOR IN COCKPIT. PERFORMED TSM TASKS 26-15-00-810-804 AND 26 -17-00-810-804. ODOR FOUND TO BE COMING FROM NR 2 PACK, WHICH HAD WORN SEALS. REPLACED SEALS ON NR 2 PACK IAW AMM 21-5 2-23, PB 401 AND REPLACED ACM GASKET IAW AMM 21-52-21-000-002/400-002. PERFORMED OPS TEST, NO LEAKS OR ODOR NOTED. 2 L 7 2 4F RT A28NM 2007061400069 20070614 00069 NM 2007 6 14 TSAA0732030 1 20070531 A 3244 26123012 TIRE BOEING 737 7377Q8 1384418 NM NR 3 MLG FAILED A TSAA O OTHER O OTHER CL CLIMB 1 WP 13 751AL 30674 ETOPS FLIGHT 442 HNL-OAK, AFTER FLIGHT AQ442 DEPARTED, TOWER RECEIVED A REPORT OF TIRE REMNANTS ON THE RUNWAY. THE FLIG HT CREW REPORTED NO ADVERSE CONDITIONS ON TAKE OFF OR DURING FLIGHT AND CONTINUED TO OAK. THE CREW LANDED IN OAK AND TA XIED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NR 3 MAIN TIRE HAD FAILED AND THE TREAD HAD SEPARATED FROM THE TIRE. MAINTENANCE CONDUCTED THE TIRE TREAD LOSS CONDITIONAL INSPECTION PER AMM 05-51-54-2. MAINTENANCE ALSO F OUND DAMAGE TO THE RIGHT INBOARD TRAILING EDGE FLAP AND TWO UNDER-WING PANELS. MAINTENANCE REPLACED BOTH THE NR 3 AND N R 4 MLG WHEEL ASSEMBLIES, THE TRAILING EDGE FLAP, AND THE TWO DAMAGED WING PANELS. THE AIRCRAFT WAS RETURNED TO SERVICE 2 L 7 2 4F RT A16WE 2007061400073 20070614 00073 NM 2007 6 14 AWXA200700698 1 20070418 A 5311 90526913 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - FOUND CRACKED FRAME, BS 727E, S9R. REPAIRED FRAME, BS 727E, S9R IAW AWA ER 03-5311-07143-ES1. 2 L 7 2 4F RT A16WE 2007061400076 20070614 00076 NM 2007 6 14 DHL2007740519 1 20070606 A 5320 INTERCOSTAL BOEING 727 7272Q9 138448M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AFT CARGO BS 950F-970 AT STR 29L HAS INNER COSTAL FLANGE WITH CORROSION. REMOVED CORRODED ANGLE IAW 727 SRM 51-10-6. F ABRICATED NEW ANGLE FROM 7075-T6 .040 PO NR 9005049 DIM 18.75" BY 2" IAW SRM 53-10-2 FIG 5 AND 51-20-1. TREATED, PRIMED AND REINSTALLED FAB'D ANGLE IAW 727 SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007061400078 20070614 00078 NM 2007 6 14 AWXA200700701 1 20070603 A 5320 D53112198201 FITTING AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 SAL - CORROSION ON L1 DOOR LOWER SILL CENTER FITTING, FR 16 - FR 20, -Y1732. REPLACED L1 DOOR LOWER SILL CENTER FITTING , FR 16 - FR 20, -Y1732 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007061400079 20070614 00079 NM 2007 6 14 AWXA200700702 1 20070528 A 5320 143N51583 STRAP BOEING 757 757225 1384959 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 MCN - CRACKED CABIN FLOOR STABILIZATION STRAP, BS 365.26 - BS 377.7, LBL 25, WL 208.1. REPAIRED CABIN FLOOR STABILIZATI ON STRAP, BS 365.26 - BS 377.7, LBL 25, WL 208.1 IAW B757-200 SRM 53-10-51-2R1. 2 L 7 2 4F RT A2NM 2007061400083 20070614 00083 NM 2007 6 14 AWXA200700706 1 20070423 A 5311 654652545 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - CRACKED FRAME, BS 380, S16L, WL 217. REPAIRED FRAME, BS 380, S16L, WL 217 IAW B737-300 SRM 53-00-0 7-2R7, FIGURE 201. 2 L 7 2 4F RT A16WE 2007060800195 20070608 00195 NM 2007 6 8 KCSA071180 1 20070604 A 5313 STRINGER BOEING 747 747221F 1384868 NM BS 2160-2180 BENT A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 FUSELAGE STR 50L HAS A BENT FLANGE BETWEEN BS 2160 AND 2180. 2 L 7 4 4F A20WE 2007061100028 20070611 00028 NM 2007 6 11 BB07040 1 20070606 A 3397 WIRE BOEING 757 757225 1384959 NM EMERGENCY LIGHTS LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925UW 22205 EMERGENCY LIGHT AT ROW 21DEF FOUND INOPERATIVE. MAINTENANCE FOUND A LOOSE WIRE AT THE LIGHT ASSEMBLY. RESECURED EMERGE NCY LIGHT. NO FURTHER FAULTS. 2 L 7 2 4F RT A2NM 2007061100029 20070611 00029 NM 2007 6 11 USAA070455 1 20070607 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 947-990 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 ZEE ANGLE, RBL 59 FS 947 - 990 AFT UPPER FLANGE. L ANGLE REPAIR INSTALLED PER SRM 51-70-11; CORR TASK C53-107-02; LEVEL 2, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007061100030 20070611 00030 NM 2007 6 11 USAA070447 1 20070607 A 5320 FLOOR SUPPORT BOEING 737 737401 1384701 NM BS 500G-520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 CRACKS, 3 EA, BS 500G - BS 520, BL-0. NEW SUPPORT INSTALLED PER SRM 51-10-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007061100031 20070611 00031 NM 2007 6 11 USAA070448 1 20070607 A 5754 65C26601381A SKIN BOEING 737 737401 1384701 NM NR 1 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 INBOARD END OF NR 1 SLAT T/E DELAMINATED. REMOVED DAMAGED AREA, FABRICATED DOUBLER & INSTALLED PER SRM 51-70-10, DEFECT SIZE: 1 X 3 INCHES. 2 L 7 2 4F RT A16WE 2007061100032 20070611 00032 NM 2007 6 11 USAA070449 1 20070607 A 5754 65C26601284 SKIN BOEING 737 737401 1384701 NM SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 OUTBOARD END UPPER & LOWER T/E DELAMINATED. REMOVED DAMAGED AREA, FABRICATED INTERNAL & EXTERNAL DOUBLERS & INSTALLED. DEFECT SIZE: 9 INCHES. 2 L 7 2 4F RT A16WE 2007061100033 20070611 00033 NM 2007 6 11 USAA070450 1 20070607 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 BS 312, LBL 11 - RBL 49; CABIN FLOORBEAM, UPPER CHORD HAS CORROSION. FAB'D & INSTALLED NEW FLOORBEAM UPPER CHORD SECTIO N & SPLICE ANGLES PER SRM 53-10-51, REP 5, DEFECT SIZE: 1 X 2 INCHES. 2 L 7 2 4F RT A16WE 2007061100034 20070611 00034 NM 2007 6 11 USAA070451 1 20070607 A 5330 SKIN BOEING 737 737401 1384701 NM BS 753 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 STA 753 BL 0 HAS CORROSION. CUT OUT DAMAGE, INSTALLED DOUBLER PER SRM 53-00-01 FIG 201, REP 31; CORR LEVEL 1, DEFECT SI ZE: 2 X 2 INCHES. 2 L 7 2 4F RT A16WE 2007061100035 20070611 00035 NM 2007 6 11 USAA070452 1 20070607 A 5320 6517688U165 SILL BOEING 737 737401 1384701 NM BS 312-354 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 SEVERAL; AREAS, BS 312 - 354, S-17: Z-CHORD ANGLE AT FWD, ENTRY DOOR SILL HAS CORROSION. INSTALLED NEW ANGLE PER SRM 51 -10-02, 51-20-00; CORR TASK C53-107-01, CORR LEVEL 2, DEFECT SIZE: 1 X 1 INCH. 2 L 7 2 4F RT A16WE 2007061100036 20070611 00036 NM 2007 6 11 USAA070446 1 20070607 A 5311 FRAME BOEING 737 737401 1384701 NM BS 480 S8-9L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 THREE EACH RADIATING CRACKS AT STA 480L, BETWEEN S8L & S9L. CUT OUT CRACKED AREA, INSTALLED REPAIR ANGLES PER TR 53-10- 20E, DEFECT SIZE: .080 INCH. 2 L 7 2 4F RT A16WE 2007061100037 20070611 00037 NM 2007 6 11 USAA070454 1 20070607 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 BS 344, LBL 35 - RBL 8, TEE CAP OF FLOORBEAM HAS CORROSION. FABRICATED REPAIR PARTS & INSTALLED PER TR 53-10-01B, SRM 5 3-10-51 REP 6; CORR TASK C53-107-02, DEFECT SIZE: 3 INCHES. 2 L 7 2 4F RT A16WE 2007061100038 20070611 00038 EU 2007 6 11 USAA070463 1 20070607 A 5315 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 180US 1525 FR 66 BATH TUB AREA HAS CORROSION. INSTALLED BATH TUB FITTING PER SRM 53-41-14, DEFECT SIZE: 1" X 1" X .056". 2 L 7 2 4F RT A28NM 2007061100039 20070611 00039 NM 2007 6 11 USAA070456 1 20070607 A 5340 ATTACH ANGLE BOEING 737 737401 1384701 NM BS 322-334 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 Z-SHAPED DOOR SILL ATTACH ANGLE BS 322 - 334, LBL 60 HAS CORROSION. REMOVED & REPLACED ANGLE PER SRM 51-10-02; CORR TAS K C53-107-01; LEVEL 2, DEFECT SIZE: 12 INCHES. 2 L 7 2 4F RT A16WE 2007061100040 20070611 00040 NM 2007 6 11 USAA070457 1 20070607 A 5315 6545834610 FLOORBEAM BOEING 737 737401 1384701 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 BS 328 + 8, RBL 44 - 59 FLOORBOARD SUPPORT HAS CORROSION. NEW SUPPORT INSTALLED PER SRM 51-10-02; CORR TASK C53-107-02; LEVEL 2, DEFECT SIZE: 3 INCHES. 2 L 7 2 4F RT A16WE 2007061100041 20070611 00041 NM 2007 6 11 USAA070458 1 20070607 A 5330 6545788 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 444US 24862 AFT GALLEY DOOR CUTOUT UPPER HINGE SKIN HAS CRACK. ROUTED OUT DAMAGED AREA PER EA 98680, DEFECT SIZE: .50 INCH. 2 L 7 2 4F RT A16WE 2007061100042 20070611 00042 NM 2007 6 11 SB07041 1 20070529 A 3350 20121 CHARGER BOEING 737 7373B7 1384580 NM EMERGENCY LIGHTS INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 533AU 24515 ORF - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEATS 17, 18, 19, AND 20 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONALLY CHECK NORMAL. 2 L 7 2 4F RT A16WE 2007061100043 20070611 00043 NM 2007 6 11 SB07043 1 20070529 A 3397 WIRE HARNESS BOEING 737 737401 1384701 NM EMERGENCY LIGHTS CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 MCO - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY EXIT LIGHTS AT ROWS 24 AND 25, LEFT-HAND SIDE, WERE INOPERATIVE. AIRCRAFT WAS MAINTENANCE FERRIED TO CLT, WHEREAS, MAINTENANCE FOUND THE EMERGENCY LIGHTING WIRE HARNESS CHAFED AND SHORT ED AT SEAT ROW 25. REPAIRED WIRES AND REPLACED BATTERY PACK CHARGER ASSEMBLY AS REQUIRED. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A16WE 2007061100044 20070611 00044 NM 2007 6 11 BB07038 1 20070526 A 3150 WARNING LIGHT BOEING 767 767201 1385125 NM BOOST PUMP UNKNOWN A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 249AU 23901 FLIGHT 743, BCN-PHL: DURING CRUISE, LEFT AFT BOOST PUMP LIGHT ILLUMINATED. DUE TO MINIMUM FUEL REQUIREMENTS FOR PHL, A /C DIVERTED TO BOS FOR EXTRA FUEL. MAINTENANCE RELEASED THE A/C PER MEL 28-2201A. 2 L 7 2 4F RT A1NM 2007061100045 20070611 00045 EU 2007 6 11 SA07032 1 20070529 A 3350 32145510 EPSU AIRBUS A321 A321211 3930370 EU EMERGENCY LIGHT FAULTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 177US 21033 1517 TPA - THE MID-CABIN EMERGENCY LIGHT POWER SUPPLY UNIT FAULTED DURING THE EMERGENCY LIGHTS OPERATIONAL CHECK. MAINTENANC E REPLACED THE MID-CABIN EMERGENCY POWER SUPPLY UNIT. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2007061100046 20070611 00046 NM 2007 6 11 USAA070459 1 20070607 A 5310 6547959 DOOR FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CRACK IN FRAME WEB, FWD CARGO DOOR FWD FRAME AT LOWER DOOR STOP FITTING. INSTALLED REPAIR DOUBLER PER EA 98691, DEFECT SIZE: 1.5 INCH. 2 L 7 2 4F RT A16WE 2007061100047 20070611 00047 NM 2007 6 11 07FDEA02076 1 20070606 A 5752 652173624 TAB BOEING 727 7272S2F 1384O81 NM ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 RIGHT WING INBD AILERON TAB OTBD AFT AREA HAS 1" AREA OF DELAM REMOVED AND REINSTALLED R/W INBD AILERON TAB REF MM 27-10 -011-4 ADJ/CHECK REF MM 27-10-000-5, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2007061100048 20070611 00048 EU 2007 6 11 07FDEA02077 1 20070606 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 662FE 761 MAIN CARGO COMPT BETWEEN F72 AND F73, 33" LEFT OF BL SEAT TRACK CORRODED REMOVED CORROSION REF A300-600 SRM 51-73-10, OR IGINAL MATERIAL THICKNESS OF .134 AND .093 AFTER BLEND. OUT OF LIMITS FOR A TOTAL LOSS OF .041 REF A300-600 SRM 53-10-1 6 FIG 102. REMOVED SEAT TRACK REF A300-600 SRM 51-40-21 PARA 7. FABRICATED NEW SEAT TRACK REF A300-600 SRM 53-10-16 PA RA 6 FIG 201 AND 203. DRILLED NEW SEAT TRACK REF A300-600 SRM 51-40-44 PARA 2. ALODINED AND PRIMED NEW SEAT TRACK REF A300-600 SRM 51-21-10 AND 51-23-10. PAINTED NEW SEAT TRACK REF A300-600 SRM 51-23-10 PARA 1. INSTALLED SEAT TRACK REF A300-600 SRM 53-10-16 PARA 6. 2 L 7 2 4F RT A35EU 2007061100049 20070611 00049 WP 2007 6 11 07FDEA02078 1 20070606 A 3150 FIRE WARNING DOUG DC10 DC1030F 3023504 WP ILLUMINATED A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 304FE 46992 PDIS:304 EN ROUTE FROM KMEM TO TLC AT FL340, RECEIVED LEVEL 3 CRG FIRE LWR FWD. ACCOMPLISHED PHASE ONE AND REFERRED TO THE RED TABS. THE CKLIST DIRECTED US TO LAND AT THE NEAREST SUITABLE AIRPORT, LANDED KCRP. ACN RELEASED FOR SERVICE PE R MEL/CDL: 26-22-01-02-B. FIRE EXT CYLINDER NR 1 INOP. ALL LWR CARGO COMPARTMENTS MUST REMAIN EMPTY." NO EVIDENCE OF S MOKE OR FIRE DMG. REMOVED AND REPLACED NR 1 LOWER CARGO FIRE EXTINGUISHER CONTAINER IN REF TO MD10 AMM 26-22-01-4 AND A MM 26-22-03-4. STILL REQUIRES OPS CHECK PER 26-22-01-4, OP'S NORMAL C/W W/STEP 1 OF MTSI. REMOVED AND REPLACED ALL (4) FWD LWR COMPT FIRE/SMOKE DETECTORS IAW MM10-30 26-14-01-4. OP'S CHECK NORMAL. C/W W/STEP 7 OF MTSI. REMOVED AND REPL 2 L 7 3 4F RT A22WE 2007061100050 20070611 00050 NM 2007 6 11 07FDEA02043 1 20070602 A 5315 65163169 FLOORBEAM BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 CABIN FLOORBEAM HAS CORROSION STA 344 LBL 36" TO 54" REMOVED CORROSION, ORIGINAL MATERIAL .107, REMAINING .086", ROTO PE ENED AREA. TREATED AND PRIMED AREA REF 51-10-02, MM 51-20-151 AND SOPM 20-10-03, AND EA NR 7-5310-111639. 2 L 7 3 4F A3WE 2007061100051 20070611 00051 EU 2007 6 11 07FDEA02044 1 20070602 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 401FE 191 2 HOLES ELONGATED AT FR 54 STRINGER 44 LT HOLE NR 1 =.200 BY .242 AND NR 2 =.249X.286. REPAIRED HOLES IAW EA 6-5330-110 462. 2 L 7 2 4F RT A35EU 2007061100052 20070611 00052 EU 2007 6 11 07FDEA02045 1 20070602 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 401FE 191 1 FASTENER HOLE AT FR 54 AND STRINGER 35L APPEARS TO HAVE A BUSHING THAT HAS FALLEN OUT. REPAIRED HOLE IAW EA 6-5330-11 0462. 2 L 7 2 4F RT A35EU 2007061100053 20070611 00053 EU 2007 6 11 07FDEA02046 1 20070602 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 401FE 191 2 HOLES ELONGATED AT FR 54 STRINGER 36 RT, HOLE NR 1 = .200 BY .220 AND NR 2 =.188 BY .221 REPAIRED HOLES IAW EA 6-5330- 110462. 2 L 7 2 4F RT A35EU 2007061100054 20070611 00054 EU 2007 6 11 07FDEA02047 1 20070602 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 401FE 191 3 HOLES ELONGATED AT FS 54 STRINGER 45 RT NR 1 =.263 BY .289 , NR 2 =.187 BY .201 AND NR 3 =.263 NR .283 REPAIRED HOLES IAW EA 6-5330-110462. 2 L 7 2 4F RT A35EU 2007061100056 20070611 00056 EU 2007 6 11 07FDEA02049 1 20070602 A 5310 STRUCTURE AIRBUS 310 A310203 3930313 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 401FE 191 2 HOLES ELONGATED AT FS 54 STRINGER 36 LT NR 16 =.200 BY .220 AND NR 17 = .188 BY .221. REPAIRED HOLES IAW EA 6-5330-11 0462. 2 L 7 2 4F RT A35EU 2007061100057 20070611 00057 EU 2007 6 11 07FDEA02050 1 20070602 A 5347 A5378193620200 TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 662FE 761 MAIN CABIN, ADAPTER TRACK, FRAME 30, BL Y60, DAMAGED. REMOVED AND RELPACED ADAPTER TRACK IAW A300-600 SRM 51-40-20, PAR AGRAPH 7. 2 L 7 2 4F RT A35EU 2007061100058 20070611 00058 NM 2007 6 11 07FDEA02051 1 20070602 A 5753 6521630222 SKIN BOEING 727 727233 138408A NM ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 RT INBD FOREFLAP T/E IS DELAMINATED 36" FROM INBD END. REPAIRED DELAMINATION REF SRM 51-40-21 PG 1 AND 2, TAP TEST GOOD . 2 L 7 3 4F RT A3WE 2007061100059 20070611 00059 NM 2007 6 11 07FDEA02052 1 20070602 A 5330 SKIN DOUG MD11 MD11F 3023600 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 576FE 48501 CENTER CARGO DOOR AFT CUTOUT LOWER SKIN FOUND MATERIAL ABRASION. [06-12-07] DAMAGED AREA AT CENTER CARGO DOOR AFT CU TOUT LOWER SKIN TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-50-00 FIGURE 17 VOLUME I. REPAIR CLASSIFIED AS MAJO R PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007061100060 20070611 00060 NM 2007 6 11 07FDEA02053 1 20070602 A 5330 SKIN DOUG MD11 MD11F 3023600 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 576FE 48501 CENTER CARGO DOOR AFT CUTOUT LOWER SKIN FOUND MATERIAL ABRASION. [06-12-07] DAMAGED AREA AT CENTER CARGO DOOR AFT C UTOUT LOWER SKIN TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-50-00 FIGURE 17 VOLUME I. REPAIR CLASSIFIED AS MAJ OR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007061100061 20070611 00061 NM 2007 6 11 07FDEA02054 1 20070604 A 5711 SPAR CAP DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RIGHT WING, TRAILING EDGE REAR SPAR UPPER CAP FOUND CORRODED AT XORS 1038. [06-18-07] REPAIR CARRIED OUT AS PER FED EX EA 1-5710-109902. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007061100062 20070611 00062 EU 2007 6 11 07FDEA02055 1 20070604 A 5313 A53986217 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 CORROSION ON STRINGER P30 AND P31, C88-91 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007061100063 20070611 00063 EU 2007 6 11 07FDEA02057 1 20070604 A 5330 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 INNER SKIN DAMAGE (NOTCH, CRACK -10MM) C26/32 P37 LT REPAIR PERFORMED BY SKIN/STRINGER REPAIR IAW EA 6-5314-101316 AND R AS/DABRE/7006560/2006. 2 L 7 2 4F RT A35EU 2007061100064 20070611 00064 EU 2007 6 11 07FDEA02058 1 20070604 A 5321 A53811651200 PRESSURE PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 DENT ON HORIZONTAL PRESSURIZED FLOOR C39/40 Y=450 AND Y=953 LT REPAIR PERFORMED BY INSTALLING A SHIM AND DOUBLER IAW EA 6-5315-99231 AND RAS 044539/005/2006 . 2 L 7 2 4F RT A35EU 2007061100082 20070611 00082 NM 2007 6 11 AWXA200700696 1 20070522 A 3220 D64433 PIN AIRBUS A319 A319132 3930340 NM NLG CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 814AW 1281 DTW - NOSE LANDING GEAR UPPER AND LOWER TORQUE LINK CONNECTING HINGE PIN CRACKED. REPLACED NOSE LANDING GEAR UPPER AND LOWER TORQUE LINK CONNECTING HINGE PIN IAW A320 AMM 32-21-11. 2 L 7 2 4F RT A28NM 2007061100083 20070611 00083 EU 2007 6 11 07FDEA02087 1 20070607 A 5311 SEEPARA4B FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 C44 RT AND C46 RT, FOUND OLD DOUBLER REPAIR ON FRAME DUE TO CRACKING FINDINGS IAW SB 53-6122 REPAIR PERFORMED BY REPLACE MENT OF FRAME C 44 (P/N A538-12310-201) AND 46 (P/N A538-12312-201) IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007061100084 20070611 00084 EU 2007 6 11 07FDEA02088 1 20070607 A 5414 A54611516 PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 CRACK (L<25MM) ON PYLON NR 2, RIB 8, OUTBOARD SIDE DOUBLER REPAIR PERFORMED IAW SB 54-6015 AND DWG R546-10124, APPROVED BY EA 6-5451-103251. 2 L 7 2 4F RT A35EU 2007061100085 20070611 00085 EU 2007 6 11 07FDEA02089 1 20070607 A 5730 57340086 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 600 WORN A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 726FD 575 ELONGATED HOLES ON RT WING-PYLON SUPPORT BRACKET AND BOTTOM SKIN, RIB 8 AREA REPAIR PERFORMED BY OVERSIZING HOLES AND MA NUFACTURING FREEZE PLUGS IAW DWG R571-50532 ISS. A. APPROVED BY EA 6-5720-103269 AND RAS/BAE/1003287/2006 ISS. A 2 L 7 2 4F RT A35EU 2007061100086 20070611 00086 EU 2007 6 11 07FDEA02090 1 20070607 A 5730 A57340086 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 ELONGATED HOLES ON LT WING-PYLON SUPPORT BRACKET AND BOTTOM SKIN REPAIR PERFOMED BY OVERSIZING THE HOLE AND MANUFACTURE A FREEZE PLUG IAW DWG R571- 50532, APPROVED BY EA 6-5720-103269 AND RAS/BAE/1003287/2006 ISS. A 2 L 7 2 4F RT A35EU 2007061100087 20070611 00087 NM 2007 6 11 07FDEA02091 1 20070607 A 5712 RIB BOEING 727 727277 138408S NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 RIGHT RIB CHORD UPPER VERTICAL FLANGE HOLE AT STATION 760.95. LOWER FWD HOLE (B), RELEVANT CRACK INDICATION NOTED AT THE 9 O`CLOCK POSITION LOOKING I/B. MADE TEMPORARY REPAIR PER ENGINEERING AND AIRCRAFT WAS FERRIED TO VENDOR FOR PERMANENT REPAIR. 2 L 7 3 4F RT A3WE 2007061100088 20070611 00088 WP 2007 6 11 07FDEA02092 1 20070607 A 5310 AFA3250 DOOR FRAME DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 EXFOLIATION CORROSION LOCATED AT LOWER AFT CARGO DOOR CUTOUT, FWD LOWER CORNER. CORROSION EXCEEDED SRM LIMITS AFTER REM OVAL, REQUIRED EA TO FLY UNTIL NEXT C CHECK. 2 L 7 3 4F RT A22WE 2007061100089 20070611 00089 NM 2007 6 11 DHL2007740521 1 20070607 A 5340 69436951 FITTING BOEING 727 7272Q9 138448M NM KEELBEAM CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH EXT FUSE BS 740 AT LT KEEL BEAM FITTING HAS CORNER FITTING WITH EXFOLIATED CORROSION. REMOVED DAMAGED FITTING IAW B727 SRM 51-30-2. LOCATED NEW FITTING AND DRILLED PART 69-43695-1 PO NR 721211 IAW B727 SRM 51-30-5 AND 51-10-1 FIG 1. TREA TED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED ANGLE FITTING IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007061200003 20070612 00003 NM 2007 6 12 MWEA070124 1 20070528 A 5248 RETAINING CLIP BOEING 717 717200 1383700 NM TAIL CONE INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 928ME 55194 WHILE PERFORMING THE TAIL CONE RELEASE CHECK THE AFT PRESSURE BULKHEAD DOOR WOULD NOT DEPLOY DROP THE TAIL CONE. ADJUST ED SPRING RETAINING CLIPS TO OBTAIN 30 POUNDS PULL FORCE AS REQUIRED. 2 L 7 2 4F TR A6WE 2007061200004 20070612 00004 NM 2007 6 12 MWEA070125 1 20070529 A 7920 42D1091A SWITCH DOUG MD88 MD88 3023688 NM LEFT ENGINE INOPERATIVE A MWEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 13 701ME 49760 LEFT OIL STRAINER CLOGGING LIGHT CAME ON. REMOVED AND REPLACED OIL PRESSURE DIFFERENTIAL SWITCH. 2 L 7 2 4F RT A6WE 2007061200017 20070612 00017 NM 2007 6 12 MWEA070136 1 20070605 A 7830 7150922REVC DOOR BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 928ME 55194 RIGHT ENGINE THRUST REVERSER UPPER DEFLECTOR DOOR HAS A CRACK IN THE ZEE FRAME RIGHT END IN THE RADIUS FRAME STATION 26. 666. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2007061200031 20070612 00031 NM 2007 6 12 USAA070421 1 20070605 A 5330 SKIN BOEING 737 737401 1384701 NM STA 380-450 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 STA 380-450, BL 0 HAS CRACK. INSTALLED LARGE DOUBLER 102" X 26" PER TR 53-30-19A, EA 98652, DEFECT SIZE: 0.125" TO -0. 350". 2 L 7 2 4F RT A16WE 2007061200033 20070612 00033 NM 2007 6 12 USAA070419 1 20070605 A 5320 ANGLE BOEING 737 737401 1384701 NM S 291 S11-12R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 STA 291 RT BETWEEN S11R & S12R, STUB BEAM OUTER ANGLE HAS A CRACK. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-10-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007061200041 20070612 00041 NE 2007 6 12 MWEA070139 2 20070607 A 7200 JT8D217C ENGINE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217 52053 NE LEFT FAILED A MWEA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 GL 13 814ME 48010 LEFT ENGINE FAILED. REMOVED AND REPLACED LEFT ENGINE. 2 L 7 2 4F 4 F A6WE E9NE 2007061200043 20070612 00043 NM 2007 6 12 USAA070465 1 20070608 A 5320 143N54102 SUPPORT BOEING 757 7572B7 1384964 NM BS 720-740 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 BS 720 - 740 RBL 62.45 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-30-15, 51-10-02, 51-40-02, DEFECT SIZE: 6 X 1 INCH. 2 L 7 2 4F RT A2NM 2007061200048 20070612 00048 2007 6 12 SWAA072838 4 20070605 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007061200082 20070612 00082 NM 2007 6 12 SWAA072901 1 20070608 A 3350 10107451 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 739GB 29275 L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007061200095 20070612 00095 NM 2007 6 12 SB07045 1 20070607 A 3397 WIRE BOEING 737 7373B7 1384580 NM EMERGENCY LGIHTS BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 23704 PIT - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHT AT SEAT 7ABC BROKEN/INOPERATIVE. MAINTENANCE REPAIRED WIRES ON SEAT MOUNTED EMERGENCY LIGHT AT SEAT 7ABC. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007061200100 20070612 00100 NM 2007 6 12 USAA070432 1 20070606 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM BS 301 S10L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 RADIUS OF INTERCOSTAL TO SKIN ATTACH ANGLE JUST ABOVE S10L BS 301 HAS CRACK. FABRICATED NEW WEB & INSTALLED PER DWG 65- 17684, SRM 51-10-02, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007061200108 20070612 00108 EA 2007 6 12 TRAX200700771 1 20070531 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 312-340 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 850AS 7355 CORROSION ON FLOOR SUPPORT BRACKETS AT PAX DOOR ENTRANCE FS 315 FS 340. UNDER FLOOR PANEL 231CLF. 2 L 7 2 4F RT A21EA 2007061200121 20070612 00121 NE 2007 6 12 ABXA070174 2 20070523 A 7200 CF680A2 ENGINE BOEING 767 767232 1385132 NM GE CF680 CF680A2 NE NR 2 DEFECTIVE A ABXA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 GL 23 739AX 4843 22216 580125 RIGHT ENGINE SHUTDOWN IN FLIGHT DUE TO HIGH EGT AND HIGH ENGINE VIBRATION (METAL FOUND IN THE TAILPIPE). REMOVED AND RE PLACED RIGHT ENGINE ON WO 600272604, REF JOB CARD 7010 FOR WORK ACCOMPLISHED IAW B767 MM. 2 L 7 2 4F 4 F RT A1NM E13NE 2007061200143 20070612 00143 SO 2007 6 12 SIMA200716202 1 20070607 A 2120 UNKNOWN EMB 135 EMB135LR 3260305 SO CABIN ODOR A SIMA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 21 712AE 145247 SMOKE APPEARED AFTER SELECTING CRUISE THRUST, EMERGENCY DECLARED. DIVERTED TO JFK. PERFORMED TROUBLESHOOTING IAW ROLLS ROYCE FAULT ISOLATION MANUAL 72-00-00 AND EMB AMM 21-20-00 WITH NO DEFECTS NOTED. PERFORMED 75 PERCENT N2 RUNS WITH AN D WITHOUT PACKS WITH NO DEFECTS NOTED. PERFORMED VISUAL INSPECTION OF PACKS WITH NO DEFECTS NOTED. RETURNED AIRCRAFT T O SERVICE. 2 L 7 2 4F RT T00011AT 2007061200164 20070612 00164 EA 2007 6 12 A6WA200740198 1 20070415 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 454AW 7842 RIGHT FS 484 INTERCOSTAL CRACKED APPROX .1 INCH LONG AT RBL 36 FLOOR SUPPORT BEAM. (M) MAINTENANCE CUT AWAY DAMAGED FL ANGE AND INSTALLED REPAIR FLANGE IAW REO 601R53-41-059, REV A AND BSC SR 601R-53-0030A. (K) 2 L 7 2 4F RT A21EA 2007061200167 20070612 00167 GL 2007 6 12 2350 1 20070531 A 7721 16578001 PROBE CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO HARTZL HCJ3Y PHCJ3YF1 GL NR 2 CHT SHORTED E J4PA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 13 851CD 1493 917741 FP4176B DURING CRUISE FLIGHT, THE NR 2 CHT READS 380*-420*. AIRCRAFT MADE AN UNSCHEDULED LANDING AT KCAE AT APPROXIMATELY 2010 LOCAL. ONE PASSENGER ON BOARD. AIRCRAFT LANDED WITHOUT INCIDENT OR INJURIES. THE NR 2 CHT READ HOTTER THAN THE OTHERS AND SPIKED INTO THE WARNING AREA WHEN THE BOOST PUMP WAS TURNED OFF. THE NR 2 EGT READ NORMAL DURING THE ENTIRE FLIGHT . MECHANIC FOUND THE NR 2 CHT PROBE WIRE TO BE FAULTY (BARE WIRE AT SPRING END OF LEAD). OPERATIONAL CHECKED SATISFACT ORY AFTER REPLACEMENT OF PROBE. AIRCRAFT RETURNED TO KGMU WITH NO FURTHER MALFUNCTIONS. 1 L 7 1 3O 3 O NT A00009CH E3SO 5 C P36EA 2007061200174 20070612 00174 EU 2007 6 12 07FDEA02100 1 20070609 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 662FE 761 MAIN CARGO COMPT AT FR66 10" BL 0, SEAT TRACK CORRODED. REMOVED CORROSION IAW A300-600 SRM 51-22-00, PG 12. ORIG THICK NESS 0.134, MAT LOSS 0.054, REMAINING 0.080, FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-16 FIG 102. REMOVED AND R EPLACED SEAT TRACK SECTION IAW A300-600 SRM 53-10-16 FIG 201. ALODINED IAW A300-600 SRM 51-21-10, PRIMED AND PAINTED IA W A300-600 SRM 51-23-10. 2 L 7 2 4F RT A35EU 2007061200187 20070612 00187 NM 2007 6 12 DLM88070697 1 20070607 A 4990 PRESSURE SWITCH DOUG MD88 MD88 3023688 NM APU OIL SYSTEM LEAKING A DALA D RETURN TO BLOCK K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 937DL 16601 49810 ON PUSHBACK, APU SHUTDOWN AS CABIN FILLED WITH SMOKE. MTC IN PROGRESS ON APU AND DUCT BURNOUT. FND APU LOW OIL PRESSUR E SWITCH LEAKING OIL. REPLACED SAME, NO LEAKS NOTED. WHILE PERFORMING OP 5089 APU AUTO SHUTDOWN FOR LOW OIL PRESSURE. REPLACED ECU AS PRECAUTION REMOVED AND REPLACED APU PER TRANS 9T103, C/W OPN 5089 APU /ENGINE DUC BURNOUT. 2 L 7 2 4F RT A6WE 2007061300017 20070613 00017 NM 2007 6 13 QXEA200700908 1 20070609 A 3250 481505 MANIFOLD BOMBDR DHC8 DHC8402 1390042 NM NLG STEERING MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 415QX 9705 1 4081 SEA FLIGHT NR 2348: AFTER ABOUT 20 SECONDS OF TAXI IN SEA, THE MASTER CAUTION CAME ON ALONG WITH THE NOSE WHEEL STEERING CAUTION LIGHT. FOLLOWED CHECKLIST AND BOTH LIGHTS CAME ON WITHIN ABOUT 2-3 SECONDS. TAXIED BACK TO GATE. MAINTENANCE REMOVED AND REPLACED NOSEWHEEL STEERING MANIFOLD IAW Q400 AMM TASK 32-51-16-000-801 AND 32-51-16-400-801. OPS CHECK GO OD. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061300022 20070613 00022 CE 2007 6 13 DXTA200702188 1 20070512 A 3260 602751 DOWNLOCK SWITCH CESSNA 750 750 2076810 CE LT MLG STICKING E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 967QS 8172 7500067 WHEN ATTEMPTING TO RAISE LANDING GEAR, LEFT MAIN INDICATION REMAINED GREEN (DOWN). ROTARY TEST GOOD. TROUBLESHOT, FOUN D DOWNLOCK SWITCH LT GEAR STICKING. REMOVED AND REPLACED LT GEAR DOWNLOCK SWITCH. RIGGED SWITCH AND SAFTIED. OPS CHEC K GOOD. WORK DONE IAW THE CE750 MM CH 32-30-04 2 L 7 2 4J RT T00007WI 2007061300029 20070613 00029 NM 2007 6 13 C8GA20070005 1 20070530 A 2820 LINE BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE FUEL SYSTEM LEAKING A C8GA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 29 801EA 22432 700741 FLT 2819 FROM DFW TO TOL. DURING DESCENT INTO TOL, THE NR 1 ENGINE WAS UNRESPONSIVE TO THROTTLE MOVEMENT. AS PRECAUTION ARY NR 1 ENGINE WAS SHUTDOWN AND AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION R EVEALED THE FUEL INLET LINE TO THE P&D VALVE WAS LEAKING. REPLACED FUEL LINE SEAL AND RESECURED LINE PERFORMED LEAK AND OPS CHECK. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2007061300030 20070613 00030 CE 2007 6 13 GUUA04290701 1 20070429 A 2910 HYDRAULIC SYSTEM BEECH 1900 1900D 1154162 CE LEAKING A GUUA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 29 82539 UE168 FLIGHT: 9264 MHH/FLL - UPON LANDING, NO RIGHT BRAKE PRESSURE BRAKING INOPERATIVE POST FLIGHT REVEALED HYDRAULIC FLUID LE AK. SECURED RIGHT BRAKES FRONT BLEEDING PORTS. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 2007061300033 20070613 00033 CE 2007 6 13 GUUA05100701 1 20070510 A 3260 UNKNOWN BEECH 1900 1900D 1154162 CE MLG ANNUNCIATOR UNKNOWN A GUUA O OTHER O OTHER CR CRUISE 1 SO 29 16540 UE172 FLIGHT: 9257 EYW/FLL - DURING FLIGHT, LANDING GEAR ANNUNCIATOR CIRCUIT BREAKER POPPED THEN AGAIN WHEN LANDING GEAR EXTEN DED. CHECKED WIRES FOR CHAFING, NO DEFECTS NOTED. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 2007061300048 20070613 00048 CE 2007 6 13 GUUA05180701 1 20070518 A 3297 CONNECTOR BEECH 1900 1900D 1154162 CE MLG LOOSE A GUUA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 87555 UE234 FLIGHT:9167 PBI/TLH - AFTER TAKEOFF LANDING GEAR DID NOT RETRACT. RETURNED TO PBI, SELECTED GEAR DOWN LEFT MAIN GEAR WO ULD NOT GIVE A SAFE DOWN LOCKED INDICATION. MANUALLY EXTENDED LANDING GEAR. LANDED WITHOUT INCIDENT. RESECURED MAIN L ANDING GEAR LEFT AND RIGHT SQUAT SWITCH CONNECTORS. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 2007061300052 20070613 00052 SO 2007 6 13 SIMA200715801 1 20070603 A 2120 UNKNOWN EMB 135 EMB135LR 3260305 SO CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 719AE 145276 OIL ODOR ON FLIGHT DECK AT A=CRUISE ALTITUDE. PERFORMED EMB FIM TASK 21-20-00-810-801, STEP 51 AND RR FIM TASK 72-00-00 -810-814 WITH NO DEFECTS NOTED. PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007061300063 20070613 00063 SO 2007 6 13 LR7A07044 1 20070514 A 5320 BEAM LKHEED 382 382G 526414U SO FS 497 BROKEN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 708 4763 DURING SCHEDULED B-3 CHECK PER JOB CARD HB3200, FOUND LT MWW BOW BEAM INBD CAP BROKEN AT FS 497, LBL63, WL158. REPLACED CAP IAW SMP 583 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007061300064 20070613 00064 NM 2007 6 13 DHL2007740525 1 20070525 A 5313 STRINGER BOEING 727 7272Q9 138448M NM BS 950F-970 S27L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 WHILE IN "C" CHECK, AFT CARGO COMPARTMENT, STRINGER 27L BETWEEN STA 950F AND 970 HAS CORROSION AROUND FASTENERS. REMOVE D FASTENERS TO GAIN ACCESS IAW B727 SRM 51-30-2. REMOVED CORROSION IAW B727 SRM 51-10-6, CORROSION FOUND OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. CUTOUT DAMAGED AREA DIM 69 1/8". FABRICATED 2 FILLERS FROM BAC1498-147 .090 PO NR 7178178 DIM 38 1/2" AND 27", 2 SPLICES FROM BAC1498-131 7075T6 PO NR 9004535 DIM 17 1/2" AND 16", AND 6 SHIMS FROM 7075T6 .071 P O NR 9004779 DIM 17 1/2", 16" (2EA), 15", AND 13" (2EA) IAW B727 SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9. TREATED AND PRIME D PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS AT AFT CARGO COMPT STR 27L BETWEEN BS 950D AND 970 IAW B727 SRM 51 2 L 7 3 4F RT A3WE 2007061300085 20070613 00085 SO 2007 6 13 LR7A07037 1 20070430 A 5742 3706561L FITTING LKHEED 382 382G 526414U SO FS 517 DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2683 4606 DURING SCHEDULED C-8 CHECK PER JOB CARD HSP57131, FOUND NR 2 ENGINE OUTBD TRUSS MOUNT INBD ATTACH FITTING HOLES OVERSIZE D AT FS 517, CWS212L, WL280. REPLACED FITTING IAW SMP 583 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007061300090 20070613 00090 NM 2007 6 13 QXEA200700892 1 20070524 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 C4 PDX - CORROSION ON LOWER SURFACEOF CARGO BAY FLOOR WEB BELOW NR 9 SEAT TRACK OUTBOARD FLANGE BETWEEN X728.102 AND X74 7.602. REPAIRED IAW SRM 51-21-00, 51-14-36, AND 51-25-45. 2 H 7 2 4T RT A13NM 2007061300096 20070613 00096 2007 6 13 A6WA200740226 4 20070512 A 3197 WIRE CNDAIR CL600 CL6002B19 1900309 EA GLARESHIELD SHORTED A A6WA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 31 433AW 7289 CPLT ROLL COMMAND MESSAGE ON ED2 IN FLIGHT. GREEN CPLT ROLL LIGHT ILLUMINATED ON GLARESHIELD. COMPLIED WITH QRH. ROLL DISCONNECT HANDLE PULLED. EMERGENCY LANDING DECLARED. (M) [07-20-07] ISOLATED SHORT TO IB L/E (LT) REPAIRED WIRE CN619A22 AND CN620AZZ IAW WM 20-11-60, OPS CHECK GOOD. REF 16650-3 FOR L/E SEALANT. (K) 2 L 7 2 4F RT A21EA 2007061300098 20070613 00098 SO 2007 6 13 LR7A07045 1 20070607 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FS 497 BROKEN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 722 4698 DURING SCHEDULED B-3 CHECK PER JOB CARD HB5302, FOUND LT FUSELAGE INTERIOR UPPER BULKHEAD BROKEN AT FS 497, LBL 59, WL26 0. REPAIRED BULKHEAD IAW MEA 382-53-07-041. 2 H 7 4 4T A1SO 2007061300101 20070613 00101 CE 2007 6 13 GUUA05300702 1 20070530 A 3297 WIRE BEECH 1900 1900D 1154162 CE MLG CHAFED A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 29 16540 UE172 FLIGHT: 9216 PNS/TPA - DURING APPROACH, WHEN LANDING GEAR SELECTED DOWN GEAR EXTENDED NORMALLY, BUT NO 3 GREEN LIGHTS. FOUND CIRCUIT BREAKER FOR GEAR INDICATION POPPED. RESET CIRCUIT BREAKER GREEN LIGHTS ILLUMINATED. REPAIRED CHAFED WIRE S G25A22, D40A22, D39B22, K11B22, K16A22, K8A22N AT A406 RELAY PANEL ASSEMBLY. LANDING GEAR EXTENSION AND RETRACTION OP ERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 2007061300102 20070613 00102 CE 2007 6 13 GUUA05300701 1 20070530 A 3260 1123640215 RELAY BEECH 1900 1900D 1154162 CE MLG WARNING SHORTED A GUUA O OTHER N FALSE WARNING AP APPROACH 1 SO 29 82539 UE168 FLIGHT: 9151 PNS/TPA DURING APPROACH LANDING GEAR WARNING HORN SILENCE BUTTON CAUSES GEAR WARNING LIGHTS TO EXTINGUISH. REPLACED NUMBER 8 RELAY CARD MODULE. LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 2007061300103 20070613 00103 SO 2007 6 13 GUUA05120701 1 20070512 A 5341 12062387601 ATTACH FITTING EMB 120 EMB120ER 3260203 SO RT WING CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 261AS 120141 AT SCHEDULED INSPECTION DISCOVERED RIGHT WING TO FUSELAGE FITTING UPPER ATTACH AREA CRACKED. REPAIRED RIGHT WING TO FUS ELAGE FITTING IN ACCORDANCE WITH FAA APPROVED DATA CONTAINED IN RBHA CTA DER RCE2001C12-24, REPORT NUMBER IC2007-120/020 3B. 2 L 7 2 4T RT A31SO 2007061300104 20070613 00104 CE 2007 6 13 GUUA05200702 1 20070520 A 3260 SWITCH BEECH 1900 1900D 1154162 CE MLG OUT OF ADJUST A GUUA O OTHER N FALSE WARNING AP APPROACH 1 SO 29 218YV UE218 FLIGHT: 9267 EYW/MIA DURING APPROACH LANDING GEAR HORN AND LIGHT ANNUNCIATED AT ABOUT 75 PERCENT N1 OR ABOUT 500LBS OF T ORQUE. SYSTEM WORKS BUT AT A LOWER VALUE THAN NORMAL. ADJUSTED PEDESTAL SWITCHES OPERATIONAL CHECK NORMAL. TEST FLIGH T SATISFACTORY. 2 L 7 2 4T RT A24CE 2007061300109 20070613 00109 SO 2007 6 13 SWIA200718316 1 20070602 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DISCONNECTED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 576SW 120345 EMERGENCY EXIT SIGN OVER 6A IS INOPERATIVE. REPAIRED BROKEN WIRE BEHIND EMERGENCY LIGHT. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007061300110 20070613 00110 2007 6 13 SWIA200718317 4 20070610 A 3416 1190AM1 ALTIMETER EMB 120 EMB120ER 3260203 SO COCKPIT FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 568SW 8743 8661 120343 ON CLIMB-OUT, CAPTAINS ALTIMETER FAILED ALONG WITH ALTITUDE ALERTER. BOTH DISPLAYS SHOW HEADING FLAGS. ATC ADVISED WE WERE OFF COURSE AND ALTITUDE WAS NOT REPORTING. RETURNED TO FIELD. REPLACED CAPTAINS ALTIMETER WITH SERVICEABLE UNIT. PERFORMED PITOT STATIC LEAK CHECK IAW MM 34-22-00. 2 L 7 2 4T RT A31SO 2007061300112 20070613 00112 EA 2007 6 13 SWIA200718319 1 20070603 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA BS 202-220 DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 906SW 7510 FUSELAGE DAMAGE BETWEEN FS 202.75 AND FS 220.00 AND BETWEEN STRINGERS 23R AND 24R. REPAIRED FUSELAGE BETWEEN FS 202.75 AND FS 220 AND BETWEEN STRINGERS 23R AND 24R IAW REO NR 601R-53-11-1191. 2 L 7 2 4F RT A21EA 2007061300113 20070613 00113 EA 2007 6 13 SWIA200718320 1 20070606 A 3520 OXYGEN MASK CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 437SW 7564 PAX O2 MASKS DEPLOYED AT ROW 10C & D. RESTOWED OXYGEN MASKS AT ROW 10C AND D. 2 L 7 2 4F RT A21EA 2007061300144 20070613 00144 WP 2007 6 13 4531504022007 2 20070402 A 7230 BLADE LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE7312 01518 WP RT ENGINE BENT E J7SA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 SW 05 437FX 315 P116768C RT ENGINE INGESTED A BIRD ON TAKEOFF. FAN BLADE BENT. TAKE-OFF ABORTED. AIRCRAFT DID NOT ROTATE. CREW SAYS BIRD APPEARE D TO BE A SEAGULL. 2 L 7 2 4F 4 F RT T00008WI E6WE 2007061300146 20070613 00146 NE 2007 6 13 HEEA113488 1 20070105 A 5620 7620710009192 WINDOW SKRSKY S76 S76C 8143008 NE PAX CABIN LOOSE B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 746P 760623 DURING CRUISE FLIGHT, 20 MIN. AFTER DEPARTURE, PILOTS HEARD A WINDSPILL LIKE NOISE AND PASSENGERS REPORTED THAT THE RIGH T PAX WINDOW WAS VIBRATING AND THE WEATHER STRIPPING WAS PARTIALLY COMING OFF THE WINDOW FRAME. RETURNED TO MCY AT SLOW SPEED. 1 G 7 2 3U NC H1NE 2007061300182 20070613 00182 NE 2007 6 13 HEEA114254 1 20070226 A 2435 7655009006108 STARTER GEN SKRSKY S76 S76C 8143008 NE NR 1 FAILED B HEEA K NONE O OTHER CR CRUISE 1 SW 03 781P 252 760630 WHILE IN CRUISE NR 1 GENERATOR FAILED. PERFORMED EMERGENCY PROCEDURES AND RETURNED TO MCY. MAINTENANCE FOUND NR 1 STAR TER GEN DRIVESHAFT SHEARED. 1 G 7 2 3U NC H1NE 2007061300185 20070613 00185 SW 2007 6 13 YTRR114335 1 20070302 A 5302 206031403005S ATTACH FITTING BELL 206 206L4 1182110 SW TAIL BOOM CRACKED B YTRR K NONE O OTHER IN INSP/MAINT 1 SW 03 410RL 2808 52310 ON PREFLIGHT PILOT FOUND TAILBOOM MOVEMENT EXCESSIVE. ON INSPECTION FOUND TAILBOOM ATTACH FITTING CRACKED. 1 G 7 1 3U NC H2SW 2007061300190 20070613 00190 EU 2007 6 13 PG9A114593 1 20070315 A 6410 350A33310000 HUB UROCOP EC130 EC130B4 8680989 EU TAIL ROTOR DAMAGED B PG9A K NONE O OTHER IN INSP/MAINT 1 WP 19 132GC 3233 3756 A BROKEN LAMINATE OF A TT BAR HAD RUBBED INTO THE BLADE ROOT. REPLACED BLADE WITH A SERVICEABLE BLADE. 1 G 7 2 3U H9EU 2007061300193 20070613 00193 2007 6 13 HEEA114633 2 20070322 A 7200 23005290 ENGINE SKRSKY S76 S76A 8143006 NE NR 1 OVERTEMP B HEEA O OTHER M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 SW 03 911MJ 8668 760231 ENGINE NR 1 OIL TEMP INDICATION ROSE AND REMAINED ABOVE RED LINE, EMERGENCY PROCEDURE PERFORMED OVER NEXT 5-10 MINUTES, AS ENGINE LEVER WAS RETARDED TO IDLE MOMENTARILY BEFORE SHUTTING DOWN, THE ENGINE NR 1 OIL PRESS LIGHT ILLUMINATED, ENGI NE WAS SHUT DOWN AND AIRCRAFT DIVERTED TO MORGAN CITY PHI. REPLACED ENGINE ASSY - SUSPECT ENGINE OIL PUMP FAILURE. 1 G 7 2 3U H1NE 2007061300197 20070613 00197 EU 2007 6 13 HEEA114929 1 20070407 A 7714 L771M40C1009 INDICATOR UROCOP EC135 EC135P2 5620027 EU TRIPLE TACH INOPERATIVE B HEEA O OTHER J WARNING INDICATION CR CRUISE 1 SW 03 320PH 0430 DURING CRUISE FLIGHT NR 1 AND NR 2 N2 GAUGES WENT TO ZERO. REPLACED TRIPLE TACH INDICATOR. 1 G 7 2 3U H88EU 2007061300200 20070613 00200 NE 2007 6 13 HEEA115124 1 20070422 A 3411 NONE PITOT TUBE SKRSKY S76 S76C 8143008 NE OBSTRUCTED B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 505PH 760505 PITOT BLOCKAGE CAUSING SIGNIFICANT DISCREPANCY IN READINGS BETWEEN ALL INDICATORS. GPS SHOWED GS ERROR IN EXCESS OF 60 KNOTS. LANDING GEAR AUDIO WARNING SOUNDED CONTINUOUSLY EVEN IN CRUISE. MAINTENANCE CLEANED WASP NEST FROM PITOT TUBE. 1 G 7 2 3U NC H1NE 2007061300206 20070613 00206 CE 2007 6 13 050907N307CS1 1 20070509 A 3260 MS25237327 BULB CESSNA 500 550 2076604 CE MLG INDICATOR BURNED OUT E Z5FA A L UNSCHED LANDING ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 63 307CS 5500974 ON APPROACH INTO PVD THE RIGHT MAIN LANDING GEAR LIGHT WOULD NOT ILLUMINATE WHITH GEAR SELECTED IN THE DOWN POSITION. TH E CREW FOLLOWED THE AFM PROCEDURES DECLARED AN EMERGENCY AND DIVERTED TO BED. THE EMERGENCY GEAR EXTEND PROCEDURE WAS PE RFORMED AND THE AIRCRAFT LANDED INTO BED WITHOUT INCIDENT. MAINTENANCE TROUBLE SHOT THE DISCREPANCY TO BAD ANNUCIATOR LI GHT BULBS. THE BULBS WERE REPLACED, GEAR SWINGS PERFORMED, OPERATION CHECKED OK. 1 L 7 2 4F A22CE 2007061300207 20070613 00207 CE 2007 6 13 050807N406CS1 1 20070508 A 2610 UNKNOWN CESSNA 525 525 2076601 CE SMOKE DETECTOR UNKNOWN E Z5FA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 EA 63 406CS 525B0043 ON DESCENT INTO CYYZ THE BAGGAGE SMOKE LIGHT ILLUMINATED. NO VISUAL OR ODOR OF SMOKE WAS DETECTED BY THE FLIGHT CREW. TH E CREW DECLARED AN ENERGENCY AND DIVERTED TO BUF. LANDING WAS UNEVENTFUL. NO SIGNS OF SMOKE OR FIRE INSIDE THE BAGGAGE C OMPARTMENT WAS DETECTED ONCE THE AIRCRAFT WAS ON THE GROUND. MAINTENANCE INSPECTED THE BAGGAGE COMPARTMENT PERFORMED A S YSTEM OPS CHECK AND NO DEFECTS WERE NOTED. 1 L 7 2 4F RT A1WI 2007061300228 20070613 00228 SO 2007 6 13 GLBA20060945 1 20070509 A 5330 SKIN EMB 120 EMB120ER 3260203 SO FUSLEAGE DENTED A GLBA K NONE O OTHER TX TAXI/GRND HDL 1 NM 03 96ZK 120096 MAJOR REPAIR - DENT/GOUGE JUST AFT OF CARGO DOOR CUT OUT. AREA AFFECTED IS APPROXIMATELY 14 INCHES LONG BETWEEN FRAME 45 & 46 FROM F.S.15435 TO F.S. 15790 JUST BELOW CARGO FLOOR. MAINTENANCE REPAIRED AREA AT FRAMES 45 AND 46 FROM F.S.15435 TO F.S. 15790 I.A.W. EMB-120 SRM 53-00. REPAIR DIMENSIONS APPROXIMATELY 19 1/4 INCH X 9 INCH. MATERIAL 2024-T3 .O4O. RI I INSPECTION COMPLIED WITH I.A.W. TASK CARD 8.2.1. 2 L 7 2 4T RT A31SO 2007061300229 20070613 00229 CE 2007 6 13 AMWA06033C 1 20070510 A 5414 11498007822 SKIN BEECH 1900 1900D 1154162 CE RT NACELLE CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 142ZV 22220 UE142 FRICTION CHAFFING OCCURED DURING ENGINE OPERATION RESULTING IN WORN SEGMENTS ON THE RT ENGINE UPPER AFT NACELLE ALONG EN TIRE LENGTH & SHAPE OF NACELLE. REPAIRED IAW ENGINEERING AUTHORIZATION REPAIR DWG 1900D142-1 REV 1R. 2 L 7 2 4T RT A24CE 2007061300233 20070613 00233 2007 6 13 U0GA115388 4 20070506 A 2312 KY19630 RADIO AEROSP AS355 AS355* EU UNKNOWN B U0GA O OTHER O OTHER NR NOT REPORTED 1 SW 03 191EH 2505 HEARD 1 G 7 2 3U H11EU 2007061300234 20070613 00234 NM 2007 6 13 UPS07M49923 1 20070326 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORIZONTAL STAB BARREL NUT BORE NR 2 LEFT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01VII R 3 8. BOTTOM SURF REMAIN BLENDOUT 0.035" DEEP X 0 .150" DIA BORE REAMED TO 1.067" DIA REMAIN BLENDOUT 0.020" DEEP EXCEED E O LIMITS. 10X MAG DVI C/O NO CORROSION. BORE BOTTOM PERI & BLENDOUT PERI RADIUS, SMOOTHED & PROTECTED SRM 51-21-01 VII R 38. REPAIR SLEEVE BUSHING FAB, PROTECTED & INSTALLED EO FIG 5. REPAIR C/O AT BN BORE NR 2 LT IAW EN1174-07. 2 L 7 3 4F RT A22WE 2007061300250 20070613 00250 GL 2007 6 13 BQVA200766071 1 20070605 A 3233 GW31221007 ACTUATOR BOMBDR BD700 BD7001A11 1390022 GL MLG CONTAMINATED E BQVA O OTHER J WARNING INDICATION AP APPROACH 1 EA 01 205EL 56 56 9201 DURING FINAL APPROACH TO TUCSON, AZ (TUS) WHEN THE LANDING GEAR WAS SELECTED DOWN AN UNSAFE INDICATION WAS ILLUMINATED F OR THE LEFT MAIN POSITION. DURING THREE ATTEMPTS THE UNSAFE INDICATION REMAINED AND AFM ABNORMAL PROCEDURES FOR GEAR EX TENSION WERE FOLLOWED; THE UNSAFE INDICATION REMAINED. THE AIRCRAFT MADE A LOW PASS BY THE TOWER TO VERIFY GEAR DOWN, A N EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT; PROCEDING TO MAINTENANCE AT LEARJET. THE LT DRAG STA Y ACTUATOR WAS REPLACED AND THE LANDING GEAR WAS CYCLED 4 TIMES ON JACKS WITH NO DEFECTS; THE AIRCRAFT WAS RETURNED TO S ERVICE. 2 L 7 2 4F RT T00003NY 2007061300278 20070613 00278 NM 2007 6 13 2007UALA01507 1 20070512 A 7920 41816054 TRANSMITTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE OIL SYS MALFUNCTIONED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 552UA 26641 727201 FLUCTUATING OIL PRESSURE ON NR 1 ENGINE. WENT FROM 102 TO 180 SETTLING TO 160 IN CRUISE. FOUND LINE DISCONNECTED AT BO TTOM OF DEOILER. SECURED LINE. RAN ENGINE AT IDLE FOR 5 MIN. NO LEAKS FOUND. REPLACED NR 1 ENGINE OIL SCAVENGE VALVE AND OIL PRESSURE TRANSMITTER FOR PRESS FLUX. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061300279 20070613 00279 NM 2007 6 13 QXEA200700909 1 20070611 A 3060 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM PROP DE ICE SYS UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 424QX 4006 PDX FLIGHT NR 2311: AFTER PUSH BACK AND PRIOR TO TAXING, WHEN THE PROPS WERE TAKEN OUT OF FEATHER, THE PROP DEICE CAUTIO N LIGHT ILLUMINATED. AFTER RETURNING TO THE GATE AND PUTTING THE PROPS TO FEATHER, THE LIGHT WENT OUT. MAINTENANCE FOU ND NO FAULTS NOTED IN CDS. STARTED AIRCRAFT UNDER SAME CONDITIONS AS DESCRIBED ABOVE AND PROP DEICE CAUTION LIGHT DID N OT ILLUMINATE. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061300280 20070613 00280 NM 2007 6 13 2007UALA01523 1 20070516 A 3230 257U000228 MODULE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE MLG FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 179UA 25158 AFTER DEPARTURE, LANDING GEAR WOULD NOT RETRACT. A/C RETURNED TO FIELD, EXPERIENCED A RECURRENCE OF THIS CONDITION ON N EXT FLIGHT OUT. AFTER EXTENSIVE TROUBLE SHOOTING, INCLUDING ON-GRND GEAR CYCLES, ISOLATED PROBLEM TO LANDING GEAR HANDL E MODULE. REPLACED LEVER ACTUATOR LG HANDLE MODULE, LNDG GEAR SYST, OP CHECKED OK REF MM 32-31-01. 2 L 7 4 4F 4 F RT A20WE E24NE 2007061300283 20070613 00283 EA 2007 6 13 A6WA200740139 1 20070320 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 421ZW 7346 FLAPS FAIL AT 20 DEGREES AND FLAPS WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED FECU S/N 895, TSN 10680, CSN 9 539. (M) 2 L 7 2 4F RT A21EA 2007061300284 20070613 00284 2007 6 13 A6WA200740138 2 20070320 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA LEFT MALFUNCTIONED A A6WA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 GL 31 451AW 7832 AT CRUISE FL230, LEFT ENGINE WAS UNRESPONSIVE TO THRUST LEVER MOVEMENT. PERFORMED ENGINE RUNS WITH SPEED CONTROL ON AND OFF WITH NO CHANGE IN ENGINE PARAMETERS, CLEANED LT T2 SENSOR PER AMM 73-21-11. OPS CHECK GOOD PER AMM 71-00-00. REMO VED FROM MEL. (M) 2 L 7 2 4F RT A21EA 2007061300287 20070613 00287 NM 2007 6 13 QXEA200700914 1 20070606 A 3010 4100S00503 VALVE BOMBDR DHC8 DHC8402 1390042 NM DEICE SYS MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 402QX 1219 83 4032 SEA FLIGHT NR 2263: WHEN AIRFRAME ICE PROTECTION WAS SELECTED, THE NR 2 BOOT PAIR ON THE FO'S SIDE DID NOT INFLATE RESUL TING IN A DEICE PRESSURE CAUTION LIGHT. RAN THE CHECKLIST. ALL PRESSURES WERE NORMAL. WHEN DESCENDING INTO WARMER TEM PERATURES, THE SYSTEM STARTED WORKING NORMALLY. MAINTENANCE REMOVED AND INSTALLED SERVICEABLE RT OUTBD DDV IAW Q400 AMM 30-11-16-000-801 AND 30-11-16-400-801. OPS TEST PASSED IAW Q400 AMM 30-11-16-710-801. WITH VALVE REMOVED, PURGED DEIC E LINES TO REMOVE MOISTURE. NO MOISTURE WAS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061300291 20070613 00291 2007 6 13 2007UALA01746 4 20070531 A 2565 D31516121 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE DOOR 1L UNSERVICEABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 481UA 1559 LOW BOTTLE PRESSURE 2 L 7 2 4F 4 F RT A28NM E40NE 2007061300313 20070613 00313 2007 6 13 HALA0700248 4 20070610 A 3460 4077880908 CDU BOEING 767 767300 1385204 NM COCKPIT MALFUNCTIONED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 590HA 4892 4892 33467 ETOPS SIGNIFICANT SYSTEM, TWICE (4 TIMES) F/O FMC DISPLAY WENT BLANK ONLY TO RETURN WITHIN 3 SECONDS WITH NO LOSS OF INF ORMATION. REMOVED AND REPLACED FMCS CDU AS PER M/M 34-61-02-422-036. CDU TEST 34-61-02-712-035. CDU OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 2007061300325 20070613 00325 EU 2007 6 13 2007UALA01778 1 20070601 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT IMPROPER PART A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 460UA 1248 DURING EMERGENCY LIGHT EEL TEST, HALF OF THE SEATS FAILED TO ILLUMINATE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061400011 20070614 00011 NM 2007 6 14 2007UALA01883 1 20070607 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 FOUND SEAT 3J AFT EEL INOP. [06-22-07] REPLACED CONNECTOR, OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007061400013 20070614 00013 2007 6 14 2007UALA01782 4 20070601 A 3460 FMC BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE MALFUNCTIONED A UALA O OTHER O OTHER AP APPROACH 1 WP 29 116UA 26908 DURING COUPLED APPROACH 15 MILES OUT FOUND A-C LINED UP ON 25L NOT 25R AS LOADED. ARRIVAL PAGE WAS BLANK RIGHT FMC THEN LEFT FROZE THEN DUMPED. NO EICAS WARNINGS. LANDED USING RAW DATA. [07-27-07] ACCOMPLISHED TROUBLESHOOTING. IDENT IFIED FLIGHT MANAGEMENT COMPUTER PROBLEM. REPLACED FMC. SYSTEM TESTED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072700007 20070727 00007 EU 2007 7 27 07FDEA02566 1 20070723 A 5310 CROSSBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 CORROSION ON CROSSBEAM AT C67 RT (-Y805 TILL -Y1470, P/N A539-74360-200) AND C56A LT (Y805 TILL Y1470, P/N A539-74268-20 0). AFTER BLENDING, REMAINING THICKNESS WAS OUT OF LIMIT. REPAIR PERFORMED BY INSTALLING SPLICE IAW SRM 53-10-15/FIG 2 07. 2 L 7 2 4F RT A35EU 2007061400019 20070614 00019 NM 2007 6 14 2007UALA01790 1 20070602 A 2420 IDG BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LEFT FAULTED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 211UA 30217 ELEC GEN DRIVE L LEFT IDG FAULT. [07-06-07] REPLACED IDG PER MM 24-11- 01, SUBSEQUENT VERIFICATION FLIGHT CONFIRMED C ORRECTION OF PREVIOUS PROBLEM. AIRPLANE OK FOR ETOPS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007061400031 20070614 00031 EA 2007 6 14 TRAX200700799 1 20070605 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA OPEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 839AS 7284 SERVICE DOOR OPENED WHILE AIRPLANE PARTIALLY PERSSURIZED. SERVICE DOOR WILL NOT CLOSE. 2 L 7 2 4F RT A21EA 2007061400036 20070614 00036 EA 2007 6 14 TRAX200700804 1 20070607 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 CEILING EMERGENCY LIGHT ABOVE LAV DOOR INOP. 2 L 7 2 4F RT A21EA 2007061400042 20070614 00042 EA 2007 6 14 TRAX200700782 1 20070603 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 906EV 7642 AFT PRESSURE BULKHEAD FOUND CRACKED ON LT AT LINTEL FITTING LOCATION SEE ADDITONAL WORK SHEET FOR DETAILS, REO 601R-53-6 11-123. 2 L 7 2 4F RT A21EA 2007061400047 20070614 00047 EU 2007 6 14 2007UALA01891 1 20070607 A 2721 TRIM SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RUDDER MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 WP 29 455UA 1105 A-C UNABLE TO RUDDER TRIM WHILE AUTOPILOT IS ENGAGED. REPLACED RUDDER TRIM ACTUATOR, ACCOMPLISHED RIG CHECKS OF ALL FL IGHT CONTROLS- ALL NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061400075 20070614 00075 NM 2007 6 14 AWXA200700700 1 20070530 A 5340 140N250532 ATTACH FITTING BOEING 757 757225 1384959 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 MCN - FOUND CRACKED CABIN INTERCOSTAL CLIP, BS 440 - BS 460, BL 0, WL 208.1. REPLACED CABIN INTERCOSTAL CLIP, BS 440 - BS 460, BL 0, WL 208.1 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007061400080 20070614 00080 NM 2007 6 14 AWXA200700703 1 20070419 A 5313 6559664 STRINGER SPLICE BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - CRACKED STRINGER SPLICE, BS 360, S4L. REPLACED STRINGER SPLICE, BS 360, S4L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007061400081 20070614 00081 NM 2007 6 14 AWXA200700704 1 20070416 A 5210 50079454 SKIN BOEING 737 73733A 1384673 NM ZONE 800 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - FOUND CRACKED L1 DOOR INNER SKIN, BS 347. REPAIRED L1 DOOR INNER SKIN, BS 347 IAW AWA ER 03-5210-07151-DH1. 2 L 7 2 4F RT A16WE 2007061400085 20070614 00085 SO 2007 6 14 LR7A07049 1 20070607 A 5311 LS5371 FRAME SPLICE LKHEED 382 382G 526414U SO FS 617 WL 285 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 722 4698 DURING SCHEDULED B-3 CHECK PER JOB CARD HB5302, FOUND CABIN OVERHEAD RING SEGMENT SPLICE PLATE CRACKED AT FS 617, WL285, RBL20. REPLACED SPLICE PLATE IAW SMP 583 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007061400086 20070614 00086 SO 2007 6 14 LR7A07050 1 20070607 A 5311 LS5371 FRAME SPLICE LKHEED 382 382G 526414U SO FS 477 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 722 4698 DURING SCHEDULED B-3 CHECK PER JOB CARD HB5302, FOUND CABIN OVERHEAD RING SEGMENT SPLICE PLATE CRACKED AT FS 477, WL285, RBL20. REPLACED SPLICE PLATE IAW SMP 583 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007061400090 20070614 00090 NM 2007 6 14 DHL2007740526 1 20070608 A 5310 STRUCTURE BOEING 727 7272Q9 138448M NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21999 WHILE IN "C" CHECK, REMOVED FASTENERS IAW B727 SRM 51-30-2. CUTOUT DAMAGED AREA APPROX DIM 3 1/4" IAW B727 SRM 53-10-4 FIG 1. FABRICATED FILLER REPAIR MATERIAL USED BAC1498-145 7075T62 PO NR 9004219 DIM 3 1/4" LONG AND BAC1498-131 7075T6 PO NR 9004989 DIM 16" LONG. STRAP 7075T6 .063" PO NR 9005090 DIM 16" BY .625 AND 13" BY .625" IAW B727 SRM 53-10-3 FIG 1. TREATED AND PRIMED REPAIR AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR AT STR 26L BETWEEN STA 1130 TO 1142 IAW B 727 SRM 53-10-3. 2 L 7 3 4F RT A3WE 2007061400092 20070614 00092 EA 2007 6 14 A6WA200740223 1 20070505 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A A6WA O OTHER J WARNING INDICATION CR CRUISE 1 GL 31 418AW 7618 FLAPS FAILED AT 21,000 FEET QRH COMPLIED WITH. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 THR U 1.4 FLAP RESET. A/C RELEASED FOR SERVICE. NO TWISTING OR SKEWING DETECTED. 2 L 7 2 4F RT A21EA 2007061400093 20070614 00093 NM 2007 6 14 QXEA200700910 1 20070611 A 3150 WARNING MESSAGE BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS ILLUMINATED A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 424QX 4006 PDX FLIGHT NR 2311: WHILE SITTING ON THE RAMP, A FLAP POWER CAUTION LIGHT ILLUMINATED. RESET THE L7 FLAP POWER CAUTION CIRCUIT BREAKER PER EM CHECKLIST AND MTX CONTROL. FLAP POWER CAUTION LIGHT RE-ILLUMINATED. MAINTENANCE RESET FLAP NVM. CAUTION LIGHT WENT OUT. NO FURTHER DEFECTS AND NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061400094 20070614 00094 NM 2007 6 14 QXEA200700912 1 20070606 A 3097 697071272 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM PROP DEICE SYS DAMAGED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 405QX 4047 SEA FLIGHT NR 2474: PROP DEICE CAUTION LIGHT ILLUMINATED IN FLIGHT ON NR 1 SIDE. RESET ONE TIME PER EA CHECKLIST. CAUT ION LIGHT ILLUMINATED AGAIN. MAINTENANCE REMOVED AND REPLACED LT PROP NR 5 BLADE PROP DEICE WIRE HARNESS IAW Q400 AMM 6 1-00-06-000-805 AND 61-10-06-400-805. OPS CHECK GOOD IAW Q400 AMM 36-61-00-720-802. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061400095 20070614 00095 NM 2007 6 14 QXEA200700913 1 20070609 A 2920 4213402 POWER UNIT BOMBDR DHC8 DHC8402 1390042 NM STBY HYD SYSTEM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 412QX 12528 12528 4059 BLI FLIGHT NR 2491: AFTER START, SELECTED STBY HYD PRESS ON AND NO STBY PRESSURE WAS INDICATED. RAN MEL 29-30-2 CHECKLI ST AND NO PRESSURE WAS INDICATED ON SYSTEM NR 1 AS PER STEP 3. A/C GEN NR 2 WOULD SHOW A LOAD INCREASE WHEN STBY HYD PR ESS WAS SELECTED ON WITH NO PRESSURE INCREASE. HYD QUANTITY NORMAL AND NO CIRCUIT BREAKERS POPPED. MAINTENANCE REMOVED AND REPLACED SYSTEM NR 1 STANDBY POWER UNIT IAW DHC8/400 AMM 29-11-36-000-801/-400-801. C/W OPERATIONAL CHECK IAW 29-11 -36-710-801. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061400097 20070614 00097 NM 2007 6 14 2007UALA01898 1 20070610 A 3200 UNKNOWN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE MLG UNKNOWN A UALA O OTHER J WARNING INDICATION TO TAKEOFF 1 WP 29 20UAÊ 29166 ANTI-SKID STATUS POSSIBLE BLOWN TIRE ON T/O. NR 5 BRAKE SHOWING A FAULT. [07-27-07] AFTER CONSIDERABLE TROUBLESHOOT ING, IDENTIFIED BAD NR 5 ANTI-SKID TRANSDUCER. REPLACED LEFT BODY GEAR NR 5 ANTI-SKID TRANSDUCER PER MM 32-42-04-401. T ESTED TRANSDUCER PER MM 32-42-04-401. BAD FROM STOCK. ROBBED AIRCRAFT 8127 KNOWN GOOD TRANSDUCER AND REPLACED PER MM32- 42-04 PG401 AND PERFORMED WHEEL SPIN UP TEST.GRD CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007081500253 20070815 00253 NM 2007 8 15 CALA0700415 1 20070809 A 5311 6546560508 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND FRAME CORRODED AT STA 947.5 BETWEEN S21L AND S21R, LBL 10 TO RBL 10. THE FRAME WAS REMOVED AND REPLACE D IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007061400098 20070614 00098 NM 2007 6 14 2007UALA01900 1 20070608 A 3397 WIRE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 815UA 867 FOUND EMERGENCY LIGHTS AT SEATS 18C AND 22C ARE INOP. [07-03-07] REPAIRED WIRING AT 18C AND RELAMPED 22C OPS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007070900133 20070709 00133 NM 2007 7 9 SWAA073168 1 20070625 A 3350 20131A BATTERY BOEING 737 7373A4 1384585 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007061400102 20070614 00102 EU 2007 6 14 2007UALA01905 1 20070608 A 3350 SIGN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 456UA 1128 CABIN MED NR 1LT LWR EMERGENCY EXIT SIGN INOPERATIVE. [07-24-07] REPLACED 90WL1 EXIT MARKER. OP TEST OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061400103 20070614 00103 EU 2007 6 14 2007UALA01906 1 20070609 A 5711 SPAR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE WING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 444UA 824 FOUND UPPER FLANGE ON LT SUB SPAR IS DAMAGED. SPAR REPAIRED PER SRM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061200123 20070612 00123 EA 2007 6 12 VNAA0705007 1 20070527 A 2760 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SPOILERONS UNKNOWN A VNAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 05 218PS 7885 CREW REPORTED AN AMBER SPOILERON CAS MESSAGE ON APPROACH. CREW FOLLOWED THE QRH AND NOTIFIED ATC REQUESTING A GO-AROUND . AFTER THE GO-AROUND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RESET THE SYSTEM IN ACCORDANCE WITH THE SERVICE LETTER SL-00-001. OPERATIONAL CHECKS WERE PERFORMED, MESSAGE DID NOT RE-APPEAR. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007061200135 20070612 00135 SO 2007 6 12 SIMA200715601 1 20070531 A 3350 2013BR BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 614AE 1325 959 145086 CABIN EMERGENCY LIGHT WILL NOT STAY ILLUMINATED. REMOVED AND REPLACED FOUR EMERGENCY POWER PACKS IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061200136 20070612 00136 SO 2007 6 12 SIMA200715602 1 20070601 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 664MS 10973 26 145779 EMERGENCY LIGHT SYSTEM MALFUNCTION. REMOVED AND REPLACED FOUR POWER PACKS IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD , RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061200137 20070612 00137 GL 2007 6 12 SIMA200715603 2 20070601 A 7200 AE30007A1 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL RIGHT LEAKING A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 695AE 5565 2945 14500870 CAE312798 LAVATORY SMOKE WARNING WITH SMOKE IN CABIN AND FLIGHT DECK. REMOVED AND REPLACED NUMBER TWO ENGINE IAW AMERICAN EAGLE W ORKCARD 72-000-00. LEAK AND OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007061200153 20070612 00153 EA 2007 6 12 A6WA200740225 1 20070415 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT HYD SYS CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 465AW 7893 LEFT HYDRAULIC TRANSDUCER BRACKET, P/N 601R75262-159, CRACKED APPROXIMATELY .1 INCH LONG IN LEFT MLG WHEEL WELL CEILING. INSTALLED NEW BRACKET IAW CRJ SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007061200162 20070612 00162 CE 2007 6 12 RU3A0704 1 20070531 A 3233 6081059803 ACTUATOR LEAR 60 60LEAR 5170707 CE MLG LEAKING E RU3A O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SW 15 PROBLEM WITH LEAKING MAIN LANDING GEAR ACTUATORS SINCE 01/01/2005. THERE WERE 7 IN 2005, 8 IN 2006, AND SO FAR IN 2007 THERE HAVE BEEN 4. THE AVERAGE MEAN TIME BETWEEN FAILURES HAS BEEN 375.4. COMPLIANCE WITH THE APPLICABLE SERVICE BULLE TINS HAS NOT CORRECTED THE PROBLEM. 2 L 7 2 4F RT A10CE 2007061200175 20070612 00175 NM 2007 6 12 07FDEA02101 1 20070609 A 5311 BA1512965 FRAME BOEING 727 7272S2F 1384O81 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 210FE 22932 FOUND ON AGING A/C INSP FOUND EXISTING REPAIR AT STA 760 FRAME DOES NOT CONFORM TO SB 727-53-0197. REMOVED AND DISCARDE D EXISTING REPAIR. ACCOMPLISHED HFEC OF DAMAGE. FABRICATED REPAIR PARTS AND INSTALLED, REF FED EX EA 7-5310-113044. 2 L 7 3 4F A3WE 2007061200179 20070612 00179 NM 2007 6 12 DHL2007783501 1 20070604 A 5320 WEB BOEING 727 727227 1384078 NM AFT AIRSTAIRS CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 RT SIDE AIRSTAIRS WEB PANEL CRACKED AT LIGHTING HOLE BS 1233, WL 166, RBL 21. CUT OUT DAMAGED AREA DIM .5 BY .75 IAW B7 27 SRM 51-40-2, FIG 1. FABRICATED NEW DOUBLER REPAIR, MATERIAL USED 7075T6, 040, 3.50” BY 4.75 IAW B727 SRM 51-40-2, FI G 1 AND 53-10-2, FIG 6. TREATED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 51-10-2, 51-40-2, FIG 1 AND 53-30-2. 2 L 7 3 4F A3WE 2007061200185 20070612 00185 NM 2007 6 12 ANCF200700012 1 20070602 A 3210 PIN DOUG MD80 MD83 3023681 NM MLG INSTALLED W ANCF A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 SO 23 632CT 49632 AFTER TAKEOFF LEFT AND RIGHT AND GEAR DOOR OPEN LIGHTS REMAIN ON. ABNORMAL CHECK LIST CARRIED OUT AND RETURNED. LANDIN G EXTEND AND ALL INDICATION WERE NORMAL. NORMAL LANDING CARRIED OUT SKBO. GEAR LOCK PINS WERE FOUND INSTALLED ON BOTH MAIN LANDING GEAR. IAW TASK CARD 0003 AV NUMERAL 1D WERE REMOVED GEAR LOCK PINS. 2 L 7 2 4F RT 2007061200192 20070612 00192 NE 2007 6 12 DLM88070703 2 20070608 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 LEAKING A DALA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 937DL 37709 49810 726824 ATB - SMOKE IN THE CABIN ON TAKEOFF/CLIMB. POWER REDUCED. SMOKE/ODOR DISSIPATED. POWER REAPPLIED, SMOKE/ODOR RETURNED ALONG WITH AFT SMOKE DETECTOR SOUNDING. CROSSFEED VALVES CLOSED. NR 2 ENG REPLACED ON TRANS 9T102. 2 L 7 2 4F 4 F RT A6WE E9NE 2007061200196 20070612 00196 NM 2007 6 12 DU4R2007129 1 20070529 A 5313 STRINGER BOEING 757 757232 1384965 NM BS 1480 S29L CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 602DL 22809 FOUND S-29L CORRODED IN AFT PIT AT BS 1480. REPAIRED CORRODED STRINGER BY REMOVING AND INSTALLING STRINGER P/N 146N3110 -8201 AND SPLICE IAW B757 SRM 53-00-03. 2 L 7 2 4F RT A2NM 2007061200203 20070612 00203 NM 2007 6 12 KNNA200700029 1 20070429 A 5300 SKIN BOEING 737 7372Q8 138448K NM PWA JT8 JT8D17 52049 NE BS 807-827 DAMAGED A KNNA O OTHER O OTHER IN INSP/MAINT 1 WP 25 413JG 23148 LOWER LOBE/FUSELAGE SKIN, SHOWS SIGNS OF HAVING LOOSE ATTACH RIVETS FROM BS 807 TO BS 827 AT BBL-0. FOUND CORROSION AT THE TIME FASTENER REMOVAL. ACO NR 075369 PROVIDE REPAIRS INSTRUCTIONS ON SKIN REPAIR AT BS 807-827 BBL 0, SRM 53-10-4 F IGURE 6. 2 L 7 2 4F 4 F RT A16WE E2EA 2007061300006 20070613 00006 CE 2007 6 13 GUUA05140701 1 20070514 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE CABIN ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 29 87557 UE246 FLIGHT: 9133 JAX/TPA - AFTER TAKEOFF WITH BOTH BLEED AIR VALVES OPEN AND HEAT APPPLIED IN THE MANUAL MODE BURNED ODOR PE RSISTS. ODOR WENT AWAY WHEN BLEED AIR VALVES WERE CLOSED. RAN ENGINES WITH BLEED VALVES OPEN FOR SEVERAL MINUTES COULD NOT DUPLICATE PROBLEM. 2 L 7 2 4T RT A24CE 2007061300007 20070613 00007 CE 2007 6 13 GUUA05200701 1 20070520 A 3297 1003810061 WIRE HARNESS BEECH 1900 1900D 1154162 CE NLG DAMAGED A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 29 16540 UE172 FLIGHT: 9300 FPO/FLL DURING APPROACH, LANDING GEAR DOWN NO NOSE GEAR LIGHT INDICATION. CONTINUED TO FLL LANDED WITHOUT INCIDENT. FOUND BAD WIRE ON NOSE DOWNLOCK HARNESS REPLACED NOSE GEAR DOWNLOCK SWITCH AND HARNESS ASSEMBLY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 2007061300028 20070613 00028 NM 2007 6 13 DU4R2007130 1 20070514 A 5340 ATTACH ANGLE BOEING 757 757232 1384965 NM BS 1680 S28-29R CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 602DL 22809 FOUND CORROSION AFT PIT MAIN FRAME FWD ATTACH ANGLE BS 1680 BETWEEN S-28 - S-29R. REPAIRED CORROSION ON FRAME ATTACH AN GLE BY FABRICATING AND INSTALLING NEW FRAME ATTACH ANGLE FROM 7075-T6 .071" CLAD IAW B757 SRM 51-40-02, 51-70-11 AND 51- 20-01. 2 L 7 2 4F RT A2NM 2007061300039 20070613 00039 CE 2007 6 13 AMWA084392BC 1 20070504 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE MASTER DISCHARGED A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 161YV 19708 440 UE161 AFTER TAKEOFF, THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED. CAPT RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENT. THIS BATTERY CHARGE ANNUNCIATOR LIGHT ILLUM IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTIONS TO THE PILOT S. CLEANED SHUNT AND REMOVED AND REPLACED BATTERY. 2 L 7 2 4T RT A24CE 2007061300058 20070613 00058 NM 2007 6 13 HALA0700225 1 20070201 A 5330 SKIN BOEING 767 767332 1382001 NM BS 287-434 DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 DUE TO MULTIPLE LIGHTNING STRIKES AND BLENDED OUT AREAS IN THE FUSELAGE SKIN AT BS 287-434, STR 37L-37R, SKIN REQUIRES R EPLACEMENT. REPLACED FUSELAGE SKIN AT BS 287-434, STR 37L-37R IAW ER 06-3352 AND HAL M105 NR 597053. 2 L 7 2 4F RT A1NM 2007061300066 20070613 00066 NM 2007 6 13 DHL2007740522 1 20070607 A 5330 SKIN BOEING 727 7272Q9 138448M NM BS 181 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 RT LOWER HALF OF FUSELAGE EXTERIOR SURFACE PRESENTS DENT AT BS 190, BETWEEN STR 24R AND 25R. CUT OUT DAMAGED AREA, 1.75 " BY 1.75" AREA, FABRICATED DOUBLER FROM 2024-T3, .050" BY 11" BY 10.5", PO NR 9005049; FILLER FROM 2024-T3, .063" BY 12 .5" BY 2", PO NR 9004940, PER B727 SRM 53-30-2 FIG 1 AND 53-30-3 FIG 14. ALODINED, PRIMED, AND INSTALLED REPAIR PARTS P ER B727 SRM 51-10-2 AND 53-30-3 FIG 14. THIS IS A CAT "B" REPAIR. 2 L 7 3 4F RT A3WE 2007061300076 20070613 00076 CE 2007 6 13 GUUA05020701 1 20070502 A 3297 114364068 CIRCUIT BOARD BEECH 1900 1900D 1154162 CE MLG FAILED A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 29 87552 UE216 FLIGHT: 9216 PNS/TPA - DURING APPROACH, SECOND LANDING GEAR EXTENSION ATTEMPT GEAR EXTENDED AFTER 20 SECONDS. REPLACE T IME DELAY PC BOARD AND LANDING GEAR RELAY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 2007061300093 20070613 00093 CE 2007 6 13 DXTA200702203 1 20070517 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE MLG WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 361QS 5600361 BOTH CO-PILOTS BRAKES ARE SPONGY, THE PEDALS TRAVEL ABOUT 1/4 WAY DOWN BEFORE THE BRAKES APPLY. PERFORMED BRAKE BLEEDIN G PROCEDURE. OPS CHECK NORMAL AT THIS TIME, WORK PERFORMED IAW CE-560 MM CHAP 32-42-00. 2 L 7 2 4F RT A22CE 2007061300116 20070613 00116 EA 2007 6 13 SWIA200718323 1 20070525 A 5220 CLEVIS PIN CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7089 LEFT EMERGENCY EXIT FORWARD HINGE FITTING CLEVIS PIN IS CORRODED AND FROZEN, DISCOVERED AT C-CHECK. REPLACED PIN IAW CR J200 AMM 52-21-00-820-801. 2 L 7 2 4F RT A21EA 2007061300118 20070613 00118 CE 2007 6 13 GUUA05270701 1 20070527 A 7930 OIL SYSTEM BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NR 2 ENGINE LOW PRESSURE A GUUA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 SO 29 87554 19568 2413 UE227 PCE114432 FLIGHT: 9297 EYW/FLL DURING FINAL INTO FLL, THE NR 2 ENGINE LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED. SECURED THE NR 2 ENGINE. CONTINUED TO FLL LANDED WITHOUT INCIDENT. SERVICED NR 2 ENGINE OIL SYSTEM. REMOVED NR 2 ENGINE STARTER GENERA TOR INSPECTED AREA FOR LEAKS. NO LEAKS NOTED. REINSTALLED STARTER GENERATOR. RAN ENGINE OPERATIONAL CHECK, NORMAL, NO LEAKS NOTED. 2 L 7 2 4T 4 T RT A24CE E26NE 2007061300119 20070613 00119 CE 2007 6 13 GUUA05250701 1 20070525 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE MLG BYPASSING A GUUA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 16540 15653 UE172 FLIGHT: 9173 EYW/FLL AFTER TAKEOFF LANDING GEAR CIRCIUT BREAKER POPPED WHEN LANDING GEAR HANDLE WAS SELECTED TO THE UP P OSITION. RAN ORH RESET CIRCUIT BREAKER. REPLACED THE RIGHT MAIN LANDING GEAR ACTUATOR. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 2007061300156 20070613 00156 NE 2007 6 13 0096538 3 20070427 A 6114 7901012 ACTUATOR DHAV DHC8 DHC8102 2809003 NM HAMSTD 14SF 14SF5 NE CORRODED B EY2R K NONE P NO WARNING INDICATION UK UNKNOWN 1 GL 03 CORROSION, BEYOND SPEC. 2 H 7 2 4T RT A13NM 6 C P7NE 2007061300172 20070613 00172 2007 6 13 B65A114152 4 20070214 A 2200 41800847100 ACTUATOR UROCOP EC135 EC135T1 5620026 EU UNSERVICEABLE B B65A O OTHER J WARNING INDICATION DE DESCENT 1 SW 03 135CR 3128 0164 CAUSING AN ACTUATOR. P DAMP LIGHT AND AN AMBER P ON PFD. CHANGED PART, CK OK 1 G 7 2 3U H88EU 2007061300174 20070613 00174 SW 2007 6 13 AC2A114168 1 20070127 A 6200 430310101107 RESTRAINT BELL 430 430 1182150 SW WORN B AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 430CM 49090 WORN ELASTAMER 1 G 7 2 3U RT H9SW 2007061300180 20070613 00180 2007 6 13 YTRR114196 2 20070210 A 7320 23070606 FUEL CONTROL BELL 206 206B 1181511 SW ENGINE MALFUNCTIONED B YTRR K NONE O OTHER CR CRUISE 1 SW 03 37AJ 1877 UNABLE TO ADJUST ENGINE TEMPERATURES DURING THE START SEQUENCE. 1 G 7 1 3U H2SW 2007061300184 20070613 00184 SW 2007 6 13 YTRR114334 1 20070207 A 5302 206031418005S ATTACH FITTING BELL 206 206B 1181511 SW TAILBOOM CRACKED B YTRR K NONE O OTHER IN INSP/MAINT 1 SW 03 72Z 3537 ON ROUTINE INSPECTION FOUND TAILBOOM VERTICAL FIN ATTACH FITTING CRACKED. 1 G 7 1 3U H2SW 2007061300187 20070613 00187 EU 2007 6 13 U0GA114547 1 20070319 A 2612 TERMINAL BOLKMS 105 BO105CBS 5626008 EU UNKNOWN UNKNOWN B U0GA O OTHER O OTHER NR NOT REPORTED 1 SW 03 291EH S842 IN FLIGHT FROM GIBSON TO HOUMA 1 G 7 2 3U NC H3EU 2007061300195 20070613 00195 SW 2007 6 13 AC2A114643 1 20070323 A 2432 RG222 BATTERY BELL 206 206L3 1182108 SW MASTER DISCHARGED B AC2A O OTHER O OTHER NR NOT REPORTED 1 SW 31 31079 51526 PILOT WORE BATTERY DOWN TRYING TO START AIRCRAFT 1 G 7 1 3U H2SW 2007061300198 20070613 00198 NE 2007 6 13 HEEA114930 1 20070407 A 3230 ROD END SKRSKY S76 S76C 8143008 NE MLG WARNING LIGHT B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 761P 760588 AFTER RAISING GEAR, RED LIGHT REMAINED ILLUMINATED. RETURNED TO HUM FOR LANDING. ADJUSTED EXPLOSIVE LINK ROD END REPLA CED. 1 G 7 2 3U NC H1NE 2007061300199 20070613 00199 SW 2007 6 13 YTRR115095 1 20070418 A 6310 23066678 BEARING CAGE BELL 407 407 1182206 SW GEARBOX BROKEN B YTRR O OTHER O OTHER CR CRUISE 1 SW 03 167RL 53167 ENGINE GEARBOX MAKING METAL. ON INSPECTION FOUND NR 3 BEARING CAGE BROKEN. 1 G 7 1 3U O H2SW 2007061300231 20070613 00231 CE 2007 6 13 AMWA06033E 1 20070510 A 5311 129430031119 FRAME BEECH 1900 1900D 1154162 CE BS 228-378 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 142ZV 22220 UE142 AT MULTIPLE FUSELAGE STATIONS FRICTION CHAFING HAS OCCURED, THE DEPTH OF THE CHAFFING RANGES FROM .019 TO .030. REPAIRE D IAW ENGINEERING AUTHENTICATION REPAIR DRAWING 1900D142-6 REVA 2 L 7 2 4T RT A24CE 2007061300232 20070613 00232 CE 2007 6 13 AMWA06033F 1 20070510 A 5710 1181200445 STIFFENER BEECH 1900 1900D 1154162 CE LWS 124 CORRODED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 142ZV 22220 UE142 BIO CORROSION DAMAGE IN LT MAIN TANK NACELLE. RIB REPAIR WS 124. REPAIRED IAW ENGINEERING AUTHORIZATION REPAIR DWG 1900D 142-3 2 L 7 2 4T RT A24CE 2007061300239 20070613 00239 NM 2007 6 13 ASAA0791756 1 20070531 A 5321 453A26109 FLOOR PANEL BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 CORROSION ON AFT CARGO PIT FLOOR PANEL. REPAIRED IAW SRM 51-40-050. 2 L 7 4 4F RT A16WE 2007061300247 20070613 00247 EA 2007 6 13 COMA0760403 1 20070527 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FS 559 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 959CA 27853 7116 FOUND CRACKS ON INBOARD AND OUTBOARD LOWER FLANGES ON LBL 9 VERTICAL AT FS 559. REPAIRED CRACK AT OUTBOARD LOWER FLANGE ON LBL 9 VERTICAL AT FS 559 IAW REO 601R-53-41-057. 2 L 7 2 4F RT A21EA 2007061300249 20070613 00249 EA 2007 6 13 COMA0760407 1 20070527 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FS 559 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 959CA 27853 7116 FOUND CRACK ON LOWER INBOARD FLANGE OF VERTICAL STIFFENER AT FS 559 LBL 27. COMPLIED WITH REO 601R-53-41-283. 2 L 7 2 4F RT A21EA 2007061300267 20070613 00267 2007 6 13 I5HA0758009 2 20070501 A 7261 6829079 PUMP CVAC 580 580 2422806 WP OIL SYSTEM OUT OF LIMITS A I5HA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 23 588X 52 WHILE EN-ROUTE FROM BORINQUEN (BQN) TO PORT-O-SPAIN (POS) APPROXIMATELY ONE HOUR INTO THE FLIGHT, THE CREW OBSERVED THE RIGHT HAND REDUCTION GEARBOX OIL PRESSURE DECREASE FROM APPROXIMATELY 150 PSI TO APPROXIMATELY 100 PSI. MINIMUM IS 130 PSI. THE CREW ELECTED TO SECURE THE ENGINE USING PROCEDURES IN THE QUICK REFERENCE HANDBOOK (QRH) AND RETURN TO BQN WHE RE THEY LANDED UNEVENTFULLY. THE REDUCTION GEARBOX OIL PUMP AND FILTER ASSEMBLY WAS REMOVED AND REPLACED AND THE AIRCR AFT RETURNED TO SERVICE. THIS SERVICE DIFFICULTY REPORT (SDR) IS CLOSED. 2 L 7 2 4T RT 2007061300275 20070613 00275 NM 2007 6 13 2007UALA01445 1 20070507 A 3350 416N2220 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 534UA 25129 RIGHT EMERGENCY ESCAPE TEST 2 FAILED. ACCOMPLISHED 1 TIME RECHARGE OF SERVICE BOTTLE. BOTTLE REPLACED AT THE FIRST MA INT OPPORTUNITY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061300281 20070613 00281 NM 2007 6 13 2007UALA01612 1 20070523 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EEL 8GH INOPERATIVE. SECURED FEEDER CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007061300292 20070613 00292 EU 2007 6 13 2007UALA01747 1 20070531 A 5730 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE WINGS DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 416UA 479 LEFT AND RIGHT LWR WING SKINS HAD DAMAGED FASTENER HOLES AT MOUNTING FLANGE OF PANELS 540NB, 540PB, AND 640NB, 1EA HOLE AT EACH PANEL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061300308 20070613 00308 NM 2007 6 13 2007UALA01763 1 20070531 A 3350 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 EEL LIGHT IN FRONT OF RT MID LAV IS INOPERATIVE. SPLICED CONNECTOR TO PWR STRIP. 2 L 7 2 4F 4 F RT A1NM E24NE 2007061300311 20070613 00311 NM 2007 6 13 2007UALA01766 1 20070531 A 3350 LAMP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 346UA 24250 OVERWING EMERGENCY EXIT LIGHT INOPERATIVE ON RIGHT SIDE. [06-22-07] RELAMPED OPS CKS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061300315 20070613 00315 NM 2007 6 13 2007UALA01768 1 20070601 A 3350 BATTERY PACK BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHT UNRELIABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 222UA 30553 FOUND 4R DOOR BATTERY PACK SERVICEABLE DATE SMUDGED AND HARD TO READ. [07-06-07] REPLACED EPAS BATTERY PACK ASSY PER M MOV 52-11-20 CONFIG 1 AND CONFIG 2. AIRCRAFT READY FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007061300316 20070613 00316 NM 2007 6 13 2007UALA01769 1 20070601 A 5210 CYLINDER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE DOOR 4R SQUIB UNRELIABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 222UA 30553 FOUND DOOR 4R EPAS DOOR CYLINDER SQUIB TO HAVE NO EXPIRATION DATE. [07-06-07] REPLACED EPAS DOOR ASSIST CYCLINDER SQU IB WITH ONE THAT HAS AN EXPIRATION DATE & AIRPLANE OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007061300317 20070613 00317 NE 2007 6 13 2007UALA01770 2 20070531 A 7200 ENGINE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE VIBRATION A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 934UA 26662 721571 HIGH ENGINE VIBRATION INDICATION, BOTH ENGINES. LEVELS DO NOT CHANGE W-THROTTLE. REPLACED AVM REF MM 77-31- 04 DUE TO NO TEST, RAN BOTH ENGINES AT VARIOUS POWER SETTINGS: NO ABNORMAL INDICATIONS. NO DEFECTS NOTED. CAN NOT CONFIRM CUSTOM ER COMPLAINT. NO FAULT FOUND. UNIT PASSED TEST PROCEDURES IAW COMPONENT MAINTENANCE MANUAL (CMM) 77-30-25,REV 3. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061300329 20070613 00329 NM 2007 6 13 2007UALA01877 1 20070607 A 5270 UNKNOWN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CARGO DOOR WARNING LIGHT A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 827UA 1022 RTFL DUE TO FWD CARGO DOOR ECAM MESSAGE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061400003 20070614 00003 SO 2007 6 14 GUUA06040701 1 20070604 A 3234 12025226501 CONTROL BOX EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A GUUA O OTHER O OTHER CL CLIMB 1 SO 17 261AS 120141 LANDING GEAR HAD TO BE CYCLED THREE TIMES BEFORE IT COMES UP, REPLACED LANDING GEAR CONTROL BOX. 2 L 7 2 4T RT A31SO 2007061400006 20070614 00006 SO 2007 6 14 GUUA06080701 1 20070608 A 3320 1317 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT INOPERATIVE A GUUA K NONE L NO TEST IN INSP/MAINT 1 SO 17 285AS 120265 AT SCHEDULED INSPECTION, DETERMINED EMERGENCY LIGHT ABOVE ROW SIX TO BE INOPERATIVE. REPLACED LAMP. 2 L 7 2 4T RT A31SO 2007061400007 20070614 00007 NM 2007 6 14 2007UALA01879 1 20070606 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY LT INOP:RT OVERWING FWD ASSY. [06-22-07] REPLACED LAMPS OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007061400016 20070614 00016 NM 2007 6 14 2007UALA01786 1 20070601 A 2560 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FLASHLIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 552UA 26641 FOUND EMERGENCY FLASHLIGHT FAULTY. [07-24-07] REPLACED ALL EMERGENCY FLASHLIGHT BATTERIES. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061400035 20070614 00035 EA 2007 6 14 TRAX200700803 1 20070607 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 390CA 10106 CAPT'S FLASHLIGHT IS INOP. 2 L 7 2 4F RT A21EA 2007061400038 20070614 00038 EA 2007 6 14 TRAX200700805 1 20070610 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 FA REPORTS CABIN ENTRANCE DOOR DIFFICULT TO OPEN. 2 L 7 2 4F RT A21EA 2007061400043 20070614 00043 NE 2007 6 14 2007UALA01887 2 20070607 A 7261 DEOILER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 ENGINE LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 839UA 1507 V10967 NR 2 ENGINE HIGH OIL CONSUMPTION EXCEEDS LIMIT. FOUND NR 2 ENG DEOILER OVERBOARD AIR DRIPPING OIL AT A RATE OF 40 DROPS -MIN AT ABOVE IDLE SPEED. REPLACED DEOILER SEAL AND BREATHER TUBE PACKING. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061400053 20070614 00053 CE 2007 6 14 DXTA200702178 1 20070505 A 3240 38771 CONTROL VALVE BEECH MU300 400A 1155402 CE BRAKE SYS INOPERATIVE E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 102QS 1647 RK380 NO BRAKES ON RIGHT SIDE. RIGHT BRAKE PEDAL P/CP GOES TO FLOOR. REMOVED AND REPLACED POWER BRAKE ANTI-SKID CONTROL VALV E IAW HAWKER 400 XP MM 32-40-00. OPS AND LEAK CHECK GOOD. 2 H 7 2 4F RT A16SW 2007061400054 20070614 00054 CE 2007 6 14 DXTA200702179 1 20070505 A 2150 73838433 ACM CESSNA 750 750 2076810 CE AFT SERVICE BAY SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 936QS 799 799 7500036 CABIN PACK SENDING SMOKE INTO THE CABIN. ON GROUND AT KIAH AFTER FLIGHT FROM KPDK, INSTALLED REPAIRED ACM IAW CESSNA 75 0 MM CH 21-51-00. 2 L 7 2 4J RT T00007WI 2007061400063 20070614 00063 EU 2007 6 14 07FDEA01884 1 20070521 A 5200 A57661500 AILERON AIRBUS 310 A310222 3930315 EU ZONE 500 NONE A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON LT LWR WING SURFACE, AILERON WS 482-513 RIB8-9. REPAIR REQUIRES EVALUATION FOR MAJOR/M INOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND TO CONFORM TO S RM 57-61-12 FIG 201, PAGE 204. 2 L 7 2 4F RT A35EU 2007061400064 20070614 00064 EU 2007 6 14 07FDEA01885 1 20070521 A 5200 A57843101 SLAT AIRBUS 310 A310222 3930315 EU ZONE 500 NONE A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON LT WING, L/E OF SLAT 1 WS 139-207 RIB 3-4. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 57-42-11 FIG 202 SHEET 2, PAGE 213. 2 L 7 2 4F RT A35EU 2007061400065 20070614 00065 EU 2007 6 14 07FDEA01906 1 20070521 A 5200 A53974203 STRINGER AIRBUS 310 A310222 3930315 EU ZONE 100 NONE A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON LOWER AFT CARGO COMP´T FR 59-60 STRG 52 RT. REPAIR REQUIRES EVALUATION FOR MAJOR /MINO R DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SR M 53-10-14, FIG 201, PAGE 203/204. 2 L 7 2 4F RT A35EU 2007061400066 20070614 00066 EU 2007 6 14 07FDEA01907 1 20070521 A 5200 A3974202 STRINGER AIRBUS 310 A310222 3930315 EU ZONE 100 NONE A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON LOWER AFT CARGO COMP´T FR 59-61 STRG 54 RT. REPAIR REQUIRES EVALUATION FOR MAJOR /MINO R DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-10-14, FIG 201, PAGE 203/204. 2 L 7 2 4F RT A35EU 2007061400070 20070614 00070 EU 2007 6 14 07FDEA01876 1 20070521 A 5330 A52111307 SKIN AIRBUS 310 A310222 3930315 EU ZONE 800 NONE A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON FWD RT PAX/CREW DOOR AT AFT LOWER CORNER. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR D ETERMINATION AND IF WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 52- 10-00 FIG 203. 2 L 7 2 4F RT A35EU 2007061400071 20070614 00071 EA 2007 6 14 QXEA20070897 1 20070605 A 2611 4462534 DETECTOR CNDAIR CL600 CL6002C10 1390015 EA LAVATORY MALFUNCTIONED A QXEA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 608QX 2783 10026 DEN - FLIGHT 4331 - ON POWER UP OF AIRCRAFT, FIRE DETECTOR IN LAVATORY ALARM IS ON. MAINTENANCE REPLACED THE LAVATORY S MOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007061400074 20070614 00074 NM 2007 6 14 AWXA200700699 1 20070419 A 5210 65458731523 DOOR FRAME BOEING 737 73733A 1384673 NM ZONE 800 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - R1 DOOR AFT FRAME CRACKED AT THE 3RD AND 4TH STOP. REPAIRED R1 DOOR AFT FRAME AT THE 3RD AND 4TH S TOP IAW AWA ER 03-5200-07142-SS3. 2 L 7 2 4F RT A16WE 2007061400082 20070614 00082 NM 2007 6 14 AWXA200700705 1 20070417 A 5210 5007945249 DOOR FRAME BOEING 737 73733A 1384673 NM ZONE 800 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - CRACKED L1 DOOR AFT FRAME, BS 347, S9L - S12L AT THE 4TH, 5TH, 6TH AND 7TH STOP PIN CUT OUTS. REPA IRED L1 DOOR AFT FRAME, BS 347, S9L - S12L AT THE 4TH, 5TH, 6TH AND 7TH STOP PIN CUT OUTS IAW AWA ER 03-5210-07151-DH1. 2 L 7 2 4F RT A16WE 2007061400089 20070614 00089 SO 2007 6 14 LR7A07053 1 20070607 A 5310 BEAM LKHEED 382 382G 526414U SO FS 557 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 722 4698 DURING SCHEDULED B-3 CHECK PER JOB CARD HB3200, FOUND RT UPPER MWW BOW BEAM CRACKED AT FS 557, WL202. REPAIRED BOW BEAM IAW SMP 583 53-40-14. 2 H 7 4 4T A1SO 2007061400101 20070614 00101 EU 2007 6 14 2007UALA01904 1 20070608 A 5101 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE VIBRATION A UALA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 456UA 1128 VIBRATION NOISE ENCOUNTERED IN FLIGHT. REMOVED PANELS AND REPLACED SEALS AND FASTENERS. NO VIBES REPORTED FROM OUTBOU ND CREWS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061400105 20070614 00105 EU 2007 6 14 2007UALA01908 1 20070609 A 5754 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 4 SLAT DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 444UA 824 LT NR 4 LE SLAT, LEFT WING DAMAGED FROM CONTACTING JET BRIDGE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061400106 20070614 00106 EU 2007 6 14 2007UALA01909 1 20070610 A 2622 EXTINGUISHER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LAVATORY READS LOW A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 445UA 826 AFT LAV FIRE EXTINGUSHER IN RED BAND. REPLACED LAV AUTO FIREX. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061400107 20070614 00107 EU 2007 6 14 2007UALA01910 1 20070610 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SEATS 3C & 19C INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 481UA 1559 EMERGENCY AISLE LIGHTS AT SEAT 3C AND 19C ARE INOPERATIVE. [07-03-07] REPLACED EEL LIGHT ASSY, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061400108 20070614 00108 EU 2007 6 14 2007UALA01911 1 20070609 A 3397 CIRCUIT BREAKER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 484UA 1609 FOUND CABIN EMERGENCY LIGHT TEST FAILS. [07-03-07] RESET CIDS, CYCLED EMERGENCY LIGHT BREAKERS. CABIN EMERGENCY LIGHT TEST PASSED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071700203 20070717 00203 EA 2007 7 17 TRAX200700931 1 20070704 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 882AS 7503 F/A REPORTS THAT THE PAX DOOR IS HARD TO CLOSE. MAIN HANDLE WILL NOT STOW ALL THE WAY DOWN. 2 L 7 2 4F RT A21EA 2007061400111 20070614 00111 NM 2007 6 14 2007UALA01915 1 20070607 A 2810 TANK BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUEL SYSTEM LEAKING A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 786UA 26938 FUEL IMBALANCE. EICAS FUEL HAS HISTORY. [07-13-07] TROUBLESHOOTING FUEL IMBALANCE. FOUND LEAK IN LT MAIN TANK, DEFU ELED, SUMPED TANK. FND AFT BOOST PUMP DISCHARGE CHECK VALVE BAD. INSTALLED REPLACEMENT FLAPPER FUEL TANK OVERRIDE VALVE & SYSTEM CHECKED OK DURING VERIFICATION FLIGHT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007061400112 20070614 00112 EU 2007 6 14 2007UALA01916 1 20070608 A 3040 HEATER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT WINDOW INOPERATIVE A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 463UA 1282 LOWER FRONT SIDE OF CAPT SLIDING WINDOW HEAT INOP. WINDOW AREAS COLD AND FOGS UP LIMITING VISIBILITY. REPLACED NR 2 WINDOW 2 L 7 2 4F 4 F RT A28NM E40NE 2007061400113 20070614 00113 NM 2007 6 14 2007UALA01917 1 20070609 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 927 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 FUSELAGE SKIN AFT OF AFT CARGO DOOR IS DAMAGED. FRAME STA 927 BENT, STA 947.5 CRACKED. STRINGERS 22R AND 23R BENT AND SHEAR TIE STA 927 BENT. [07-03-07] ACCOMPLISHED MAJOR REPAIRS OF ALL DAMAGED AREAS. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061400115 20070614 00115 NM 2007 6 14 2007UALA01919 1 20070609 A 5341 TORQUE TUBE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD GALLEY DOOR UNSTABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 FWD GALLEY DOOR CUTOUT TORQUE TUBE HAS MOVEMENT BEYOND 0.003. [07-03-07] REPLACED THE BEARING AND TORQUE TUBE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061400117 20070614 00117 NM 2007 6 14 2007UALA01921 1 20070609 A 5230 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE AFT CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 AFT CARGO DOOR SN 230 INTERIOR SKIN AFT LOWER CUTOUT HAS STOP DRILLED CRACKS. [07-03-07] REMOVED DAMAGE. INSTALLED DOU BLER PER GNMM 1-0-8-067. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061400122 20070614 00122 NM 2007 6 14 2007UALA01926 1 20070608 A 3510 TRANSDUCER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE OXYGEN SYSTEM FLUCTUATES A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 799UA 26926 FLIGHT DIVERTED DUE TO CREW OXYGEN INDICATION. [07-13-07] REPLACED OXYGEN PRESSURE TRANSDUCER. NO ADDITIONAL FLUCTUATI ON NOTED. A/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007061400123 20070614 00123 NM 2007 6 14 AWXA200700718 1 20070527 A 5754 114N407737 SKIN BOEING 757 757225 1384959 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 MCN - LEFT WING NR 3 SLAT COVE SKIN CRACKED, WS 515. REPLACED LEFT WING NR 3 SLAT COVE SKIN, WS 515 IAW B757-200 SRM 5 1-40-02. 2 L 7 2 4F RT A2NM 2007061400125 20070614 00125 2007 6 14 AWXA200700722 4 20070602 A 2565 60592101 SLEEVE AIRBUS A319 A319132 3930340 NM ESCAPE SLIDE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 21437 9950 1049 SAL - EES - RIGHT OVERWING EMERGENCY EXIT SLIDE RESERVOIR CONNECTION SLEEVE CRACKED. REPLACED AND OPERATIONAL CHECKED R IGHT OVERWING EMERGENCY EXIT SLIDE RESERVOIR IAW A319 AMM 25-62-46. 2 L 7 2 4F RT A28NM 2007061400126 20070614 00126 EA 2007 6 14 SWIA200718325 1 20070525 A 5346 BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7089 UPPER ENGINE BEAM ANGLE IS CRACKED AT FS 640 AND STR 10, DISCOVERED AT C-CHECK. REPLACED ANGLE P/N 601-35006-61 PER CRJ 200 SRM 51-42-21 PGS 1-20. 2 L 7 2 4F RT A21EA 2007061400127 20070614 00127 EA 2007 6 14 SWIA200718326 1 20070525 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7089 CRACK FOUND ON SKIN AFT OF RIGHT NOSE GEAR CUT-OUT, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS AS PER REO 601R-53-11 -048. 2 L 7 2 4F RT A21EA 2007061400132 20070614 00132 EA 2007 6 14 SWIA200718331 1 20070525 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7089 CABIN FLOOR SUPPORT STRUCTURE IS CRACKED AT FS 484 AND RBL36, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLE PER REO 601 R-53-41-059 AND CRJ200 SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007061400133 20070614 00133 EA 2007 6 14 SWIA200718332 1 20070525 A 5310 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 338 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7089 CRACK FOUND AT FS 338.00 FRAME MEMBER ON PAX DOOR, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS AT FS 338.00 ON PAX DO OR PER REO 601R-52-11-402 REV G. 2 L 7 2 4F RT A21EA 2007061400134 20070614 00134 EA 2007 6 14 A6WA200740130 1 20070316 A 2750 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS DAMAGED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 31 444ZW 7788 FLAPS FAIL CAUTION, FLAPS CONFIRMED AT ZERO DEGREES, COMPLIED WITH QRH. REMOVED AND REPLACED FLEX DRIVESHAFT NR 1, (PDU TO INBOARD FLAP) AS PER AMM 27-53-10, OPS TEST OF FLAPS GOOD AT THIS TIME. INSPECTED FLEX SHAFT, FOUND NO BARBER PULL. REMOVED MOISTURE AND LUBED REF AMM 27-53-10. (M) 2 L 7 2 4F RT A21EA 2007061400135 20070614 00135 EA 2007 6 14 A6WA200740137 1 20070319 A 2197 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA NR 2 TEMP UNKNOWN A A6WA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 31 464AW 7890 DURING FLIGHT , IDG NR 2 MESSAGE CAME ON AFT 28,000 FT, COMPLIED WITH QRH. AIR DIVERSION TO MDT, PERFORMED EMERGENCY LA NDING. REMOVED AND REPLACED IDG NR 2, NO FIX. REMOVED AND REPLACED IDG NR 2 TEMP BULB, NO FIX. REMOVED AND REPLACED I DG HEAT EXCHANGER, NO FIX. REPLACED ENG IDG NR 2 TEMP CONNECTOR 2P22E2. OPS CHECK GOOD. IDG S/N 1110/3346 TSN 11659 C SN 10169 - IDG OIL COOLER S/N 1207 TSN 7641 CSN 6954. (M) 2 L 7 2 4F RT A21EA 2007061400141 20070614 00141 EA 2007 6 14 QXEA20070907 1 20070606 A 5280 CC670330983 DOOR CNDAIR CL600 CL6002C10 1390015 EA NLG DAMAGED A QXEA O OTHER O OTHER AP APPROACH 1 NM 09 602QX 10010 BIL- ON APPROACH FOR LANDING ON FLIGHT 4317, AS THE GEAR WAS EXTENDED, HEARD A LOUD "POP". GEAR INDICATION FINE, MADE A NORMAL APPROACH AND LANDING. MAINTENANCE FOUND THE MOUNT BRACKET FOR THE AFT NOSE GEAR DOOR TWISTED AND JAMMED AGAINST THE RIGHT NOSE WHEEL. REMOVED THE DOOR AND ATTACHING HARDWARE AND FERRIED THE AIRCRAFT FROM BIL TO PDX FOR REPAIRS. I N PDX, REPLACED THE GEAR DOOR AND ASSOCIATED RODS, BRACKETS, BUSHINGS, AND HARDWARE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007061400149 20070614 00149 SO 2007 6 14 HYIA2611X 2 20070527 A 7200 TSIO520VB ENGINE CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO MCAULY 3AF32C 3AF32C505 GL ZONE 400 FAILED E HYIA E ENGINE SHUTDOWN Y ENGINE STOPPAGE AP APPROACH 1 NE 01 2611X 1825 1825 402C0072 831928R 001123 RIGHT ENGINE FAILURE ON 1/2 MILE FINAL TO RUNWAY 25 AT PVC, CREW FEATHERED ENGINE AND LANDED. LATER INSPECTION ON 5-27- 07 FOUND INTERNAL FAILURE IN THE RIGHT ENGINE. ENGINE REMOVED AND REPLACED ON 5-28-07. A/C RETURNED TO SERVICE AND ENG TO BE SENT TO MANUFACTURE FOR INVESTIGATION. 1 L 7 2 3O 3 O A7CE E8CE 5 C P22EA 2007061400152 20070614 00152 NM 2007 6 14 ZZDA070529166 1 20070529 A 3520 402E30035000 PSU BOEING 717 717200 1383700 NM SEAT 16 DEF MALFUNCTIONED A ZZDA B EMER. DESCENT O OTHER CR CRUISE 1 SO 15 944AT 55007 THE 02 MASKS AT ROWS 16 DEF DID NOT DROP DURING EMERGENCY DESCENT. REMOVED AND REPLACED PSU PER AMM 25-25. OPS CHECK G OOD PER MM 35-22. 2 L 7 2 4F TR A6WE 2007061400153 20070614 00153 NM 2007 6 14 ZZDA070529167 1 20070529 A 3520 402E30035000 PSU BOEING 717 717200 1383700 NM 29 DEF MALFUNCTIONED A ZZDA B EMER. DESCENT O OTHER CR CRUISE 1 SO 15 944AT 55007 THE 02 MASKS AT ROWS 29 DEF DID NOT DROP DURING EMERGENCY DESCENT. REMOVED AND REPLACED PSU PER AMM 25-25. OPS CHECK G OOD PER MM 35-22. 2 L 7 2 4F TR A6WE 2007061400154 20070614 00154 NM 2007 6 14 ZZDA070529168 1 20070529 A 3520 402E3035000 PSU BOEING 717 717200 1383700 NM 30 DEF MALFUNCTIONED A ZZDA B EMER. DESCENT O OTHER CR CRUISE 1 SO 15 944AT 55007 THE 02 MASKS AT ROWS 30 DEF DID NOT DROP DURING EMERGENCY DESCENT. REMOVED AND REPLACED PSU PER AMM 25-25. OPS CHECK G OOD PER MM 35-22. 2 L 7 2 4F TR A6WE 2007061400155 20070614 00155 NM 2007 6 14 ZZDA070529169 1 20070529 A 3520 402E30025001 PSU BOEING 717 717200 1383700 NM SEAT 27 AC MALFUNCTIONED A ZZDA B EMER. DESCENT O OTHER CR CRUISE 1 SO 15 944AT 55007 THE 02 MASKS AT ROWS 27 AC DID NOT DROP DURING EMERGENCY DESCENT. REMOVED AND REPLACED PSU PER AMM 25-25. OPS CHECK GO OD PER MM 35-22. 2 L 7 2 4F TR A6WE 2007061400156 20070614 00156 NM 2007 6 14 ZZDA070529170 1 20070529 A 2130 5971858503 DUCT BOEING 717 717200 1383700 NM CABIN PRESSURE SEPARATED A ZZDA B EMER. DESCENT O OTHER CR CRUISE 1 SO 15 944AT 55007 AT 30,000 FT HEARD LOUD POP. CABIN ALT ALERT ON. DESCENDED TO 10,000 FEET. MASK DEPLOY IN CABIN. INSPECTED AND FOUND LARGE CHECK VALVE ON AIR CONDITION SYSTEM LOCATED AT AFT PRESSURE BULKHEAD WITH DAMAGED FLAPPER VALVE AND SPIDER DUCT S EPARATED. REMOVED AND REPLACED CHECK VALVE AND SPIDER DUCT ASSEMBLY PER AMM 21-22. PERFORMED CABIN PRESSURE CHECK. RE F AMM 21-30, OPS CHECK GOOD. 2 L 7 2 4F TR A6WE 2007061400157 20070614 00157 NM 2007 6 14 ZZDA070529171 1 20070529 A 2130 5912287509 CHECK VALVE BOEING 717 717200 1383700 NM CABIN PRESSURE DAMAGED A ZZDA B EMER. DESCENT O OTHER CR CRUISE 1 SO 15 944AT 55007 AT 30,000 FT HEARD LOUD POP. CABIN ALT ALERT ON. DESCENDED TO 10,000 FEET. MASK DEPLOY IN CABIN. INSPECTED AND FOUND LARGE CHECK VALVE ON AIR CONDITION SYSTEM LOCATED AT AFT PRESSURE BULKHEAD WITH DAMAGED FLAPPER VALVE AND SPIDER DUCT S EPARATED. REMOVED AND REPLACED CHECK VALVE AND SPIDER DUCT ASSEMBLY PER AMM 21-22. PERFORMED CABIN PRESSURE CHECK. RE F AMM 21-30, OPS CHECK GOOD. 2 L 7 2 4F TR A6WE 2007061400158 20070614 00158 2007 6 14 ZZDA070529172 4 20070529 A 2565 D29982225 SLIDE BOEING 717 717200 1383700 NM R-1 DOOR LOW PRESSURE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 983AT 55052 R1 DOOR SLIDE GAUGE IS IN THE RED. REMOVED AND REPLACED R-1 DOOR SLIDE REF B717 AMM 25-61. 2 L 7 2 4F TR A6WE 2007061400159 20070614 00159 EU 2007 6 14 UPS07149864 1 20070530 A 3350 LAMP AIRBUS A300 A300F4622R 3930360 EU EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 174UP 0005 INSPECTION TYPE:N/A EMERGENCY LIGHT IS INOP. RELAMPED EMERGENCY LIGHT, OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2007061400162 20070614 00162 NM 2007 6 14 ASAA0791749 1 20070531 A 5320 STRAP BOEING 737 737990 NM BS 787-794 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT CORROSION ON FLOOR STRAP AT BS 787. REPAIRED IAW SRM 51-40-06. 2 L 7 4 4F RT A16WE 2007061400163 20070614 00163 NM 2007 6 14 ASAA0791750 1 20070531 A 5347 143A7501116 CARGO TRACK BOEING 737 737990 NM BS 460-500 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 FWD CARGO PIT LEFT TIE DOWN TRACK GOUGED. REPAIRED IAW SRM 53-00-53. 2 L 7 4 4F RT A16WE 2007061400164 20070614 00164 EA 2007 6 14 COMA0760404 1 20070527 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FS 559 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 959CA 27853 7116 FOUND CRACK ON LOWER INBOARD SIDE FLANGE OF SEMI PRESSURE BULKHEAD VERTICAL STIFFENER AT FS 559, RBL 9. REMOVED DAMAGED AREA ON FS 559 RBL 9 VERTICAL STIFFENER AND INSTALLED DOUBLER IAW REO 601R-53-41-057. 2 L 7 2 4F RT A21EA 2007061400165 20070614 00165 NM 2007 6 14 UPS07549865 1 20070427 A 5311 146N102885 FRAME BOEING 757 75724APF 1384969 NM BS 1320 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 404UP 23726 INSPECTION TYPE:C DENTS IN AFT CARGO FUSELAGE FRAME STA 1320, BETWEEN S25L AND S26L (2EA). ACCOMPLISHED BOTH UPPER AND LOWER DENT REPAIRS IAW EA757-5362-27- A1666 AND UPS EO B757-5310-26894-A WITH NO DEVIATIONS. 2 L 7 2 4F RT A2NM 2007061400168 20070614 00168 NM 2007 6 14 UPS07549868 1 20070415 A 5532 SKIN BOEING 757 75724APF 1384969 NM VERTICAL STAB DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 404UP 23726 INSPECTION TYPE:C VERTICAL STAB RT SIDE SKIN PANEL P/N 175N2001-4 HAS DELAMINATION IN 2 PLACES, 41.0" X 19.0" OF DELAM 4 .0" FROM TOP OF PNL, 7.0" FROM FWD EDGE. 10.0" X 5.0" OF DELAM 68" FROM TOP, 18" FROM FWD EDGE OF PANEL REF: D348458, P ANEL P/N 175N2001. REMOVED, REPAIRED AND REINSTALLED PER REO ARO22062, B757 SRM 51-40-01 AND MM 51-21-10-7 AND B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007061400170 20070614 00170 NM 2007 6 14 UPS07549874 1 20070512 A 5414 SKIN BOEING 757 75724APF 1384969 NM NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 404UP 23726 INSPECTION TYPE:C NR 1 PYLON LEFT SIDE FWD SKIN HAS STOP DRILLED CRACK & REPAIR DOUBLER. OPEN STOPDRILL HOLE BY 1/32 PE R PRELIMINARY 1 EA 757-5451-27-A1674 STEP 2. NOTE: NO PLUG REQUIRED FOR NEW DOUBLER, NO HOLE EXISTS. ACCOMPLISHED PER FINAL EA 757-5451-27-A1674. 2 L 7 2 4F RT A2NM 2007061400171 20070614 00171 WP 2007 6 14 UPS07849870 1 20070517 A 5313 STRINGER DOUG DC8 DC873F 302199F WP BS 204 S62-63 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C2 CRACK ON FWD STRINGER END FITTING AT XRS 204 FROM STRINGER S-62 - S-63. REMOVED END FITTING AT STA X RS 204 S-62 - S-63 IAW SRM 51-03-02, FABRICATED AND INSTALLED END FITTING AT STA XRS 204 STRINGER S-62 TO STRINGER S-63 IAW DWG 5615767 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007061400172 20070614 00172 WP 2007 6 14 UPS07849875 1 20070522 A 5280 SKIN DOUG DC8 DC873F 302199F WP NLG DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C1 LEFT NLG DOOR SKIN IS CRACKED ON OUTBOARD SIDE. CUT OUT DAMAGED SKIN ON LT NLG DOOR IAW SRM 52-02-03 . FABRICATED AND INSTALLED REPAIR DOUBLER, AND FILLER ON LEFT NLG DOOR IAW SRM 52-02-0 FIG 2, AND 51-1-21. 2 L 7 4 4F RT 4A25 2007061400173 20070614 00173 NM 2007 6 14 UPS07M49869 1 20070423 A 5753 MOUNT DOUG MD11 MD11F 3023600 NM LT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C LEFT WING I/B FLAP I/B ACTUATOR ENCLOSURE, UPPER AFT LARGE ROLLER BEARING MO MOUNTING FOUND CORRODED. I/B & O/B BUSHINGS MOUNT ELONG HOLE EXCEED LIMIT. I/B HOLE MATL REMOVED 0.0 06" O/B HOLE MATL REMOVED 0.015". MAX ALLO W DIA 1.000". FPE C/O DPS4.707 REV AW, NO CORROSION. REWORK HOLES DIA & THK EVAL & FOUND ACCEPTABLE EN1265-0 7. BUSHI NG 2EA FAB EN1265-07. MPI C/O ON FAB BUSHINGS, FOUND NO CRACK. BUSHINGS INSTALLED PER EN1265-07. 2 L 7 3 4F RT A22WE 2007061400177 20070614 00177 NM 2007 6 14 ASAA0791773 1 20070531 A 5330 146A323128 SKIN BOEING 737 737990 NM BS 767-847 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 DENT ON FUSELAGE SKIN AT BS 767. REPAIRED IAW EA 5330 02213. 2 L 7 4 4F RT A16WE 2007061400180 20070614 00180 EA 2007 6 14 COMA0760408 1 20070527 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FS 409 RBL27 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 959CA 27853 7116 CRACK IN LOWER VERTICAL STIFFENER AT FS 409+128 RBL18. REPAIRED BOTTOM VERTICAL BEAM PER REO 601R-53-41-056. 2 L 7 2 4F RT A21EA 2007061400181 20070614 00181 EA 2007 6 14 COMA0760409 1 20070528 A 5320 VERTICAL BEAM CNDAIR CL600 CL6002B19 1900309 EA BS 409 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 959CA 27853 7116 VERTICAL BEAM LBL 27 FS 409+128 INBOARD SIDE CRACKED. REPAIRED PER REO 601R-53-41-056. 2 L 7 2 4F RT A21EA 2007061400182 20070614 00182 EA 2007 6 14 COMA0760410 1 20070528 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FS 559 LBL18 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 959CA 27853 7116 FOUND CRACK ON LOWER INBOARD FLANGE OF VERTICAL STIFFENER AT LBL 18 FS 559.00. REPAIRED PER REO 601R-53-41-067. 2 L 7 2 4F RT A21EA 2007061400183 20070614 00183 EA 2007 6 14 COMA0760411 1 20070528 A 5320 VERTICAL BEAM CNDAIR CL600 CL6002B19 1900309 EA BS 409 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 959CA 27853 7116 VERTICAL BEAM LBL 27 FS 409+128 OUTBOARD LOWER SIDE CRACKED. REPAIRED PER REO 601R-53-41-056. 2 L 7 2 4F RT A21EA 2007061400184 20070614 00184 EA 2007 6 14 COMA0760412 1 20070530 A 2750 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA TE FLAP MALFUNCTIONED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 446CA 7546 FLIGHT 5199 - ON APPROACH FLAP HANDLE WOULD NOT MOVE PAST 20 DEGREES. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REM OVED FLAP HANDLE COVERS AND CLEANED AREA. COMPLIED WITH FUNCTIONAL CHECK. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007061400185 20070614 00185 EA 2007 6 14 COMA0760413 1 20070531 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FS 409 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 914CA 32873 7012 DURING HMV-7 INSPECTION FOUND CRACK AT LOWER END OF VERTICAL STIFFENER, FS 409+128, LBL 36. CUT OUT DAMAGE AND INSTALLE D DOUBLER IAW BOMBARDIER REO 601R-53-41-189. 2 L 7 2 4F RT A21EA 2007061400186 20070614 00186 EA 2007 6 14 COMA0760414 1 20070531 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 202 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 735CA 7267 BULKHEAD SKIN IS CRACKED AT FS 202.75 BL 71, WL 69 WHERE PARKING BRAKE CABLE GOES THROUGH FWD BULKHEAD. CUT OUT DAMAGE AND REPAIRED PER EA 10-5311-01731 AND REO 53-11-563. 2 L 7 2 4F RT A21EA 2007061400187 20070614 00187 EA 2007 6 14 COMA0760415 1 20070531 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 559 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 735CA 7267 BULKHEAD SKIN IS CRACKED AT FS 559.00 RBL 18 WL 59.10 UNDER THE RIGHT AILERON QUADRANT UPPER O/B BOLT REF. CUT OUT DAMA GE AND INSTALLED A PERMANENT REPAIR DOUBLER TO FS 559.00 BULKHEAD PER COMAIR SR10-5341-0001 REV A SECTION 1. 2 L 7 2 4F RT A21EA 2007061400191 20070614 00191 WP 2007 6 14 UPS07849883 1 20070525 A 5320 FITTING DOUG DC8 DC873F 302199F WP FS 834 L18L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C1 FITTING CRACKED AT STA 834 L18L. REMOVED END FITTING AT STA 834 L18L IAW SRM 51-01-20D. FABRICATED AND INSTALLED END FITTING AT STA 834 L18L IAW DWG 3779874, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007061400192 20070614 00192 WP 2007 6 14 UPS07849884 1 20070604 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 EVIDENCE OF CORROSION BETWEEN FUSELAGE SKIN, FINGER DOUBLER AND LONGERON 31R, STARTING AT STA 70 AND EXTENDING APPROX 6 FEET REFERENCE D351779 AND FERRY PERMIT 9033. [06-29-07] REMOVED LWR FWD PANEL IN "A" PIT TO ACCESS AREA PER SRM 51-3-0 & OPENED UP EXTERNAL SKIN FROM STA 70-128.0 L29R-L33R. R/R FINGER DOUBLER PER SRM 51-1-20D & 51-1-21. REMOVED CORR. AT L31R FROM STA 70-90 PER SRM 53-2-0 FIG 1F. TREATED & PRIMED PER SRM 51-1-8. 2 L 7 4 4F RT 4A25 2007061400193 20070614 00193 EA 2007 6 14 COMA0760417 1 20070531 A 2710 SPRING CNDAIR CL600 CL6002B19 1900309 EA AILERONS OUT OF RIG A COMA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 01 709CA 7238 FLIGHT 5503 - LEFT AND RIGHT AILERON MORE STIFF THAN NORMAL. -A- ON PFD WITH AUTO-PILOT ON, IN TURNS. HYD PUMP 1A SQUE ALING. AILERONS FELT NORMAL WHEN DISCONNECTED. FOUND BOTH CENTERING MECHANISMS FORCE TOO HIGH. RIGGED LEFT AND RIGHT AILERON CENTERING MECHANISM SPRING. NO FURTHER DEFECTS. FLIGHT CHECK GOOD. 2 L 7 2 4F RT A21EA 2007061400194 20070614 00194 EA 2007 6 14 COMA0760418 1 20070601 A 2520 PSU CNDAIR CL600 CL6002B19 1900309 EA CABIN DISLODGED A COMA A UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 SO 01 932CA 7038 FLIGHT 5131 - PAX SERVICE UNIT DROPPED FROM CEILING ABOVE ROWS 9-12B. DIVERTED TO JFK, LANDED WITHOUT INCIDENT. REINST ALLED, NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007061400196 20070614 00196 EA 2007 6 14 COMA0760420 1 20070601 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA LEFT UNCONTROLLABLE A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 721CA 7259 FLIGHT 5228 - LEFT A/C PACK UNCONTROLLABLE IN AUTO OR MANUAL. RETURNED TO OMA, LANDED WITHOUT INCIDENT. INSPECTED LEFT PACK AND DUCTS FOR DAMAGE, PERFORMED TEMP CONTROL CHECK. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007061400197 20070614 00197 EA 2007 6 14 COMA0760421 1 20070601 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY NONE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 685BR 7712 FLIGHT 5037 - RECEIVED LAV SMOKE WARNING. RETURNED TO ATL. LANDED WITHOUT INCIDENT. INSPECTED LAV AND PERFORMED OPS C HECK OF LAV SMOKE DETECTOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007061400199 20070614 00199 EA 2007 6 14 COMA0760423 1 20070605 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 914CA 32873 7012 DURING HMV-7 INSPECTION, FOUND CRACK IN RADIUS OF FLOORBEAM UPPER FLANGE. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW BOMB ARDIER REO 601R-53-11-137. 2 L 7 2 4F RT A21EA 2007061400200 20070614 00200 CE 2007 6 14 6019306062007 1 20070606 A 2931 730635 PRESSURE SWITCH LEAR 60 60LEAR 5170707 CE HYD SYSTEM MALFUNCTIONED E J7SA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 05 249FX 193 LEFT HYDRAULIC LIGHT ILLUMINATED IN FLIGHT. RIGHT HYDRAULIC LIGHT ILLUMINATED IN FLIGHT. FLIGHT CREW REPORTED THE HYDR AULIC PRESSURE GAGE INDICATED SYSTEM PRESSURE WITH A DROP IN PRESSURE (DOWN TO APPROX 1300 PSI) UPON GEAR AND FLAP EXTE NTION - PRESSURE RETURNED TO NORMAL PRESSURE WITH GEAR AND FLAPS SET. FSR REQUESTED THE CREW TO RUN ENGINES ONE AT A TI ME AND CHECK SYSTEM PRESSURES. FLIGHT CREW REPORTED BACK THAT LEFT AND RIGHT ENGINES RUN SEPARATELY AND ALL CHECKED NOR MAL. FLIGHT CREW REPORTED BOTH LEFT AND RIGHT HYDRAULIC LIGHTS ILLUMINATED AT 1000 PSI ON ENGINE SHUT DOWN. HYDRAULIC RESEVOIR AT 3/4 FULL ON SITE GLASS AND HYDRAULIC ACCUMULATORS NORMAL. MX TROUBLESHOOTING PROVED A BAD PRESSURE SWITCH. 2 L 7 2 4F RT A10CE 2007061400202 20070614 00202 NM 2007 6 14 UPS07649915 1 20070512 A 5347 SEAT TRACK BOEING 767 76734AF 1385212 NM BS 1439 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 306UP 27759 INSPECTION TYPE:2C SEAT TRACK CORRODED. REPAIRED IAW SRM 53-00-52-2R REPAIR 9. 2 L 7 2 4F RT A1NM 2007061400203 20070614 00203 NM 2007 6 14 UPS07649916 1 20070512 A 5347 SEAT TRACK BOEING 767 76734AF 1385212 NM BS1373-1390 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 306UP 27759 INSPECTION TYPE:2C SEAT TRACK CORRODED. REPAIRED IAW SRM 53-00-52-2R REPAIR 9. 2 L 7 2 4F RT A1NM 2007061300289 20070613 00289 NM 2007 6 13 2007UALA01744 1 20070531 A 2420 GENERATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 596UA 28749 FLIGHT DIVERTED DUE TO LOSS OF NR 2 GENERATOR. [08-07-07] RT GENERATOR DRIVE DISC LIGHT ILLUMINATED WITH EICAS MSG. REPLACED RIGHT GCU. RESET DRIVE DISC AND SERVICED IDG AS PRECAUTIONARY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061300298 20070613 00298 NM 2007 6 13 2007UALA01753 1 20070531 A 5230 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 FWD GALLEY DOOR, FWD FRAME CRACKED AT LWR END AT FASTENER HOLE. [06-26-07] MAJOR REPAIR: REPAIRED BY STOP DRILLING. RE FERENCE SRM 52-10-02 PG 107 NOTE A. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061300310 20070613 00310 NE 2007 6 13 2007UALA01765 2 20070531 A 7314 PUMP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FUEL SYSTEM MALFUNCTIONED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 664UA 29236 724371 HIGH FUEL BURN. REPLACED FUEL PUMP & FUEL FLOW TRANSMITTER PER MM 73-31-01. CONDUCTED VERIFICATION FLIGHT & CREW REP ORTED GOOD PERFORMANCE OF ENGINE & FUEL FLOW INDICATIONS. AIRCRAFT OK FOR ETOPS OPERATION. 2 L 7 2 4F 4 F RT A1NM E24NE 2007061300314 20070613 00314 NM 2007 6 13 2007UALA01767 1 20070531 A 5210 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE PAX DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 FWD ENTERY DOOR CUTOUT HINGE BOX WEB CRACKED AT STR 10L AT BODY STA 294. FABRICATED AND INSTALLED ATTACHED ANGLE REPAIR . 2 L 7 2 4F 4 F RT A16WE E2GL 2007061300321 20070613 00321 EU 2007 6 13 2007UALA01774 1 20070603 A 2612 FIRE LOOP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 NACELLE UNKNOWN A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 472UA 1435 FIRE LOOP B FAULT DISPLAYED ON UPPER ECAM SCREEN, ENG 1. ALMOST THE ENTIRE LOOP B DETECTION CIRCUIT WAS REPLACED (LOOPS , FDU, FIRE HANDLE CONTROL UNIT). LOOP HAD STILL FAULTED UP UNTIL 6/27/07. NO REPEATS SINCE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061300322 20070613 00322 EU 2007 6 13 2007UALA01775 1 20070601 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SEAT 10C NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 473UA 1469 EMERGENCY LIGHT TEST FAILS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061400001 20070614 00001 SO 2007 6 14 GUUA06020702 1 20070602 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO CABIN ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 17 280AS 120231 STRONG ODOR OF JET A WHEN APU FIRST STARTED. INSPECTED APU FOR LEAKS, NO LEAKS NOTED. INSPECTED BLEED CONNECTIONS, ALL ARE SECURE. OPS CHECK NORMAL. NO DEFECTS NOTED. 2 L 7 2 4T RT A31SO 2007073000063 20070730 00063 NM 2007 7 30 C1HA200796012 1 20070722 A 3246 26045611 WHEEL BOEING 727 7272J4 1384006 NM MLG FRACTURED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 696CA 22574 WHILE PERFORMING MX TAXI I/B ANTISKID LIGHT ILLUMINATED A/C TAXIED DIFFICULT STOPPED A/C AND FOUND NR 1, 2, 4 TIRES FLAT NR 3 TIRE MISSING AC REMOVED FROM SERVICE FOR REPAIRS, STATUS REMAINS OPEN. 2 L 7 3 4F RT A3WE 2007061400014 20070614 00014 NM 2007 6 14 2007UALA01783 1 20070602 A 3600 ENGINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RIGHT OVERHEATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 644UA 25094 727587 RTFL DUE TO RIGHT ENGINE BLEED OVERHEAT INDICATION. [07-10-07] REPLACED FAN AIR VALVE AND FAN AIR TEMP SENSOR, PERFO RMED HIGH POWER RUN, PS CK OK . AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007061400018 20070614 00018 NM 2007 6 14 2007UALA01789 1 20070601 A 2800 UNKNOWN BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FUEL SYSTEM LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 675UA 29243 DURING FUELING FUELER REPORTS FUEL LEAKING INTO CENTER TANK. [07-31-07] ACCOMPLISHED PRESSURIZED FUEL VALVES FOR 15 MIN NO LEAKS FOUND. SUSPECT REFUEL DRAIN BACKFLOW (NORMAL CONDITION). NO HISTORY OF OTHER FUEL LEAKS. 24 HOURS LATER, ACCOMPLISHED FUELING AND DEFUELING OF LT AND RT FUEL TNKS PER 767 FOM. NO FUEL LEAK TO CTR TNK WAS FOUND. UNABLE TO DU PLICATE ON GROUND. A/C COMPLETED SEVERAL WEEKS OPERATION WITH NO FURTHER REPORT OF FUEL LEAKING. 2 L 7 2 4F 4 F RT A1NM E24NE 2007061400021 20070614 00021 2007 6 14 2007UALA01792 4 20070602 A 2565 SLIDE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE DOOR 1R UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 DOOR 1R SLIDE PACK IS HANGING DOWN. [07-24-07] REPACKED SLIDE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061400029 20070614 00029 NE 2007 6 14 402502252007 2 20070115 A 7200 TAY6118C ENGINE GULSTM GIVX GIVXG450 3980205 SO RROYCE TAY TAYMK6118 NE NR 1 VIBRATION E N93A A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 13 440QS 820 4025 85051 DURING CLIMBOUT A STRONG SHUDDER WAS FELT THROUGHOUT THE AIRFRAME. 2 L 7 2 4F 4 F RT A12EA A25NE 2007061400030 20070614 00030 EA 2007 6 14 TRAX200700798 1 20070605 A 5210 BOLT CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 718EV 10095 PAX DOOR WILL NOT CLOSE AND LOCK PROPERLY, DOOR APPEARS TO BE OUT OF RIG AFT ASSY HAS CROSS OVER TUBE BOLT MISSING. 2 L 7 2 4F RT A21EA 2007061400033 20070614 00033 EA 2007 6 14 TRAX200700801 1 20070606 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 F/A FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007061400040 20070614 00040 EA 2007 6 14 TRAX200700780 1 20070603 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 906EV 7642 CRACK ON LOWER FLANGE OF FRAME 280.00 RBL 9.00 REO 601R53-11-171 TO BE C/OUT MAJOR, RESOLVED ON W/O: 59833 TASKCARD: N/R -00027. CUTOUT DONE ON LOWER FLANGE OF FRAME 280.00 RBL 9 IAW REO 601R53-11-171 REV D. HFEC PERFORMED ON LOWER FLANGE OF FRAME 280 RBL 285 CUT OUT AND BLEND RADIUS OF ANGLE FILLER. HEATHAIR W/O 36485 AMO NR 46-90. NO CRACKS FOUND. JOB COMPLETE ON LOWER FLANGE OF FRAME 280 RBL 9 IAW REO 601R-53-11-171 REV "D" (SCHEME B). REPAIRED PILOTS BULKHEAD AT FS 2 80.00 RT BL 9.00 IAW EO600-53-90 C/W. 2 L 7 2 4F RT A21EA 2007061400041 20070614 00041 EA 2007 6 14 TRAX200700781 1 20070603 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 906EV 7642 FLOOR ANGLE STRUCTURE CRACK ON RT AT FS 621.00, RESOLVED ON W/O: 59833 TASKCARD: N/R-00036. ON FLOOR STRUCTURE AT FS 62 1 RT SIDE ANGLE REMOVED AS PER SRM 51-42-06. FLOOR ANGLE STRUCTURE AT FS 621 RT SIDE REINSTALLED PER REO 601R-53-61-117 REV C. PRIMER AND PAINT DONE AS PER SRM 51-21-11. 2 L 7 2 4F RT A21EA 2007061400057 20070614 00057 CE 2007 6 14 DXTA200702200 1 20070517 A 3150 UNKNOWN CESSNA 560 560XL 2076702 CE UNKNOWN E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 679QS 5605279 IN CRUISE, AT FL300 "STAB MIS COMP" AND "HYD PRESS" ANNUNCIATORS ILLUMINATED. CONNECTED AIR DATA TEST SET AND PERFORMED FULL "TWO POSITION HORIZONTAL STAB OPERATIONAL CHECK" AND "AIRSPEED SWITCH AND HORIZONTAL STAB OPS CHECK" IAW CH 27-40-0 0 OF THE CE-560XL MM. NO DEFECTS NOTED. DISCONNECTED TEST EQUIPMENT. 2 L 7 2 4F RT A22CE 2007061400059 20070614 00059 EU 2007 6 14 07FDEA01872 1 20070521 A 5330 A53978149 SKIN AIRBUS 310 A310222 3930315 EU ZONE 100 UNKNOWN A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED LT FS 3249-3302 FR 60-61 AND STR43-40. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETER MINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. INFO: ON THE UPPER RIGHT CORNER, ITEM NON ROUTIN E NR 202 SHOULD BE NON ROUTINE NR 207. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-10-12 FIG 228 SHEET2, PAGE401/40 2. 2 L 7 2 4F RT A35EU 2007061400067 20070614 00067 NM 2007 6 14 F3LA200700126 1 20070530 A 5315 D5347217220290 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 920FR 5184 1997 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM Y1292 BETWEEN BS FR66 AND FR68 AROUND ATTACH HOLES/NUT CLIP S, TOP AND BOTTOM. REPLACED FLOORBEAM IAW SRM 51-42-11. 2 L 7 2 4F RT A28NM 2007061400072 20070614 00072 EA 2007 6 14 QXEA20070898 1 20070604 A 2780 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA SLAT NONE A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 605QX 10022 DEN - WHEN FLAPS SELECTED TO 20 DEGREES RECEIVED A SLAT FAIL CAUTION MESSAGE. PER THE CHECKLIST, SELECTED THE PREVIOUS FLAP SETTING AND OPERATION WAS NORMAL. MAINTENANCE INSPECTED AIRCRAFT AND FOUND NO FAULT OR MESSAGES IN THE MDC. CYCLE D SLATS SEVERAL TIMES WITH NO DEFECTS. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007061400077 20070614 00077 WP 2007 6 14 ARWA20070601 1 20070604 A 2133 OUTFLOW VALVE DOUG DC10 DC1010 3022110 WP CABIN PRESSURE LACK OF LUBE A ARWA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 19 68041 46900 WITH ALL 3 PACKS OPERATING, UNABLE TO MAINTAIN CABIN ALTITUDE BELOW 10,000. OUTFLOW VALVE FULL CLOSED (MANUALLY). FOUN D THRUST RECOVERY VALVE LOCKED OPEN; LUBED OUTFLOW VALVE MECHANISM; CHECK MANUALLY OPERATION NORMAL ON GROUND IN ACCORDA NCE WITH DC-10 M/M 21-31-04 AND 21-30-00. TRANSFERED TO DMI NR 20774. 2 L 7 3 4F A22WE 2007061400114 20070614 00114 NM 2007 6 14 2007UALA01918 1 20070608 A 5310 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 727C S23R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 FOUND STA 727C+12 STR 23R HAS .25" HOLES FROM PREVIOUS REPAIR. [07-03-07] REMOVED DAMAGE. FABRICATED AND INSTALLED U A ND J CHANNEL PER SRM 53-00-03 REPAIR I. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061400121 20070614 00121 NM 2007 6 14 2007UALA01925 1 20070608 A 5310 STRUCTURE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FUSELAGE SCRATCHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 665UA 29237 ALT STATIC PORT, RIGHT SIDE FUSELAGE, JUST FWD OF FWD CARGO DOOR HAS 5 IN LONG SCRATCH THRU WHITE CIRCLE, JUST UNDER STA TIC PORT. [08-08-07] DAMAGE DEPTH IS .0021 OK PER 53-00-01 ALSO PER 51-10-03 ITEM F. BURNISHED SCRATCH PER SRM 51-1 0-02. TOUCHED UP WHITE BORDER PAINT AS NEEDED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007061400129 20070614 00129 EA 2007 6 14 SWIA200718328 1 20070525 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7089 CABIN FLOORBEAM STRUCTURE IS CRACKED AT FS 484 AND LBL36, DISCOVERED AT C-CHECK. INSTALLED NEW CLIP AT FS 484 AND LBL36 IAW REO 601R-52-4-059. 2 L 7 2 4F RT A21EA 2007061400137 20070614 00137 EA 2007 6 14 A6WA200740154 1 20070325 A 5410 DOOR CNDAIR CL600 CL6002B19 1900309 EA RT NACELLE OPEN A A6WA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 465AW 7893 PERFORMED AIR RETURN AFTER N1 FAN VIBRATION ON NR 2 ENGINE ASSOCIATED WITH AIRFRAME VIBRATION. VERTICAL DESCENT RATE LE SS THAN 360 FPM AT TOUCHDOWN. LANDING WEIGHT 51,000 LBS. OVERWEIGHT LANDING INSPECTION NOT REQUIRED. RT ENGINE UPPER TRANSLATING COWL OPENED IN FLIGHT. REMOVED AND REINSTALLED ORIGINAL DAMAGED UPPER TRANSLATING COWL IAW CRJ AMM 71-11-0 1 AND REQUIRED REO FROM SHORTS FOR DAMAGE. COMPLIED WITH REQUIRED REO 601R-78-33-3528 REV WC20 FOR TAP TEST. APPLIED P AINT TO SCRATCH. APPLIED YELLOW DOT TO DENT. (M) 2 L 7 2 4F RT A21EA 2007061400147 20070614 00147 SO 2007 6 14 HYIA135 2 20070524 A 7200 TSIO520VB ENGINE CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO NR 1 FAILED E HYIA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 NE 01 6879R 2004 2004 402C0611 831906R DURING CRUISE FLIGHT NR 1 ENGINE VIBRATED THEN LOST POWER, ENGINE WAS SHUT DOWN. LEFT ENG HAD A INTERNAL FAILURE, ENG W AS REMOVED AND REPLACED. AIRCRAFT RETURNED TO SERVICE. FAILED ENG HAS BEEN SENT TO MANUFACTURE FOR TEARDOWN AND INVEST IGATION. 1 L 7 2 3O 3 O A7CE E8CE 2007061400167 20070614 00167 NM 2007 6 14 UPS07549867 1 20070512 A 5330 SRM5300012R7 SKIN BOEING 757 75724APF 1384969 NM BS 1585 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 462UP 28266 INSPECTION TYPE:C LIGHTNING STRIKE AT FUSELAGE EXTERNAL SURFACE APPROX STA 1585 BETWEEN S7R AND S8R. DISPLACED INSULATI ON STA 1580 TO 1600 S7R TO S8R FOR ACCESS IAW AMM25-55-07-4. LIGHTNING STRIKE DAMAGE EXCEEDED THE ALLOWABLE DAMAGE LIMI TS PER SRM 53-00-01. TRIMMED DAMAGE OUT TO 1 INCH IAW SRM 53-00-01. HFEC IAW NTM 51-00-00 PT 6. 2 L 7 2 4F RT A2NM 2007061400169 20070614 00169 NM 2007 6 14 UPS07549871 1 20070507 A 5532 174N110211 SKIN BOEING 757 75724APF 1384969 NM VERTICAL STAB DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 404UP 23726 INSPECTION TYPE:C VERTICAL STAB LEADING EDGE PANEL NR 321CL INNER SURFACE DELAMINATED (PANEL RACK). REMOVED DAMAGE, FAB RICATED REPAIR PARTS FROM 2024-T3.016 BAT 1138598 PO MST0021331, PREPPED SURFACE AREAS & BONDED WITH BMS 5-101 PER FINAL EA 757-5530-27-A1668. 2 L 7 2 4F RT A2NM 2007061400176 20070614 00176 2007 6 14 ZZDA070603175 4 20070603 A 2565 D29982225 CABLE BOEING 717 717200 1383700 NM R1 DOOR SLIDE DISCONNECTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 948AT 55011 R-1 SLIDE CABLE DISCONNECTED, POSSIBLY OUT OF ITS NORMAL CONDITION. REMOVED R-1 DOOR SLIDE AND FOUND PINS PULLED OUT. REPLACED SLIDE AS OUTLINED IN 717 M/M 35-61. 2 L 7 2 4F TR A6WE 2007061400195 20070614 00195 EA 2007 6 14 COMA0760419 1 20070601 A 5610 NP1393222 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA O OTHER O OTHER CR CRUISE 1 SO 01 995CA 23156 7229 FLIGHT 5383 - F/O SIDE WINDOW CRACKED. FOLLOWED QRH, DESCENDED, REDUCED DIFFERENTIAL PRESSURE TO 6.0. REPLACED F/O SID E WINDOW. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007061400201 20070614 00201 NM 2007 6 14 UPS07549892 1 20070512 A 5311 146N102911 FRAME BOEING 757 75724APF 1384969 NM BS 1460 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 462UP 28266 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1460 BETWEEN S25R AND S26R. REPAIRED FRAME PER FINAL EA 757-5360 -27-A1673 AND UPS EO B757-5310-26974-A. 2 L 7 2 4F RT A2NM 2007061400204 20070614 00204 NM 2007 6 14 UPS07649917 1 20070510 A 5330 SKIN BOEING 767 76734AF 1385212 NM BS 687 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 306UP 27759 INSPECTION TYPE:2C CRACKS IN SKIN AT UPPER GPS ANTENNA DOUBLER. REPAIRED IAW EO B767-5330-26944-A, ER 07-2324. CUT OUT DAMAGED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A1NM 2007061400205 20070614 00205 GL 2007 6 14 UPS07849879 2 20070604 A 7200 CFM562 ENGINE DOUG DC8 DC873F 302199F WP GE CFM CFM562 GL NR 4 FLAMED OUT A IPXA E ENGINE SHUTDOWN A FLAME/FIRE CL CLIMB 1 SO 01 880UP 46080 693410 INSPECTION TYPE:N/A ATB - NR 4 ENGINE FLAMEOUT CLIMBING THROUGH 30,000FT. NOTICED FUEL PUMP IN OFF POSITION. RAN ENGIN E FLAMEOUT CHECK LIST AND ENGINE RESTARTED. ALL INDICATIONS NORMAL FOR REMAINDER OF FLIGHT. PERFORMED NEG PRESSURE CHE CK ON NR 4 ENG. FUEL FEEDLINES PRESSURE CHECK GOOD. FUEL STICKED TANKS, ALL READINGS NORMAL IAW MM 28-22-12-2. RESTAR T ENGINE NORMAL. REMOVED NR 4 ENG FUEL FILTER, NO CONTAMINATION. REMOVED AND REPLACED CFE BOOST PUMP NR 4 ENG, OPS CHE CK GOOD IAW 73-10-01-2. REMOVED AND REPLACED NR 4 TANK SELECT VALVE. FOUND 6" X 12" RAG IN FUEL SUPPLY TUBE. REMOVED RAG. ENG RUN NORMAL, ALL CHECKS GOOD IAW 71-00-00-0. 2 L 7 4 4F 4 F RT 4A25 E2GL 2007061400206 20070614 00206 2007 6 14 UPS07849886 4 20070606 A 2565 SLIDE DOUG DC8 DC873F 302199F WP CABIN LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:N/A CABIN ESCAPE SLIDE WILL NOT STOW. INSTALLED RETAINING PIN IN SLIDE PER AMM 25-60-01-2. 2 L 7 4 4F RT 4A25 2007061400208 20070614 00208 WP 2007 6 14 UPS07849889 1 20070515 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FS 520 L27R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C2 HFEC AND VISUAL INSPECTION DETECTED A .125 INCH CRACK ON THE C-2 DOOR LWR FWD DOOR JAMB CORNER. REPA IRED C-2 DOOR LWR FWD DOOR JAMB CORNER IAW SRM 53-02-00-0 FIG 22, AND SRM TR 53-187. 2 L 7 4 4F RT 4A25 2007061400210 20070614 00210 WP 2007 6 14 UPS07849912 1 20070509 A 5330 57723875 SKIN DOUG DC8 DC873F 302199F WP FS 290 L21L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C2 BULGING SKIN ON EXTERIOR OF SKIN AT STA 290 L21L AFT OF MAIN CARGO DOOR. REPAIRED FUSELAGE SKIN AT S TA 290 L21L AFT OF MAIN CARGO DOOR IAW SAA EA 008-5330-01-A0883, UPS EO DC8-5330-26921-A, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007061400211 20070614 00211 NM 2007 6 14 UPS07M49887 1 20070510 A 5330 AJC7060506 SKIN DOUG MD11 MD11F 3023600 NM FS 2160 L33-35R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP 48745 INSPECTION TYPE:4C AFT EXTERIOR FUSELAGE RIGHT SIDE BETWEEN FS 2007-2160 HAS SURFACE CORROSION WHERE UPPER AND LOWER HOR IZONTAL STAB FAIRINGS ATTACHES TO FUSELAGE. REMOVED CORROSION IAW MD-11 SRM 51-21-01, AREA AT FS 2160 L33R-L35R FOUND O UT OF LIMITS. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SAA EA 011-5330-01-A0881. 2 L 7 3 4F RT A22WE 2007061400212 20070614 00212 NM 2007 6 14 UPS07M49890 1 20070606 A 2910 2249426503 FILTER HOUSING DOUG MD11 MD11F 3023600 NM HDY SYSTEM CRACKED A IPXA O OTHER K FLUID LOSS NR NOT REPORTED 1 SO 01 253UP 48439 INSPECTION TYPE:N/A DIVERSION - AIRCRAFT DIVERTED TO KIX DUE TO NR 1 HYDRAULIC LOSS. *SUPPLEMENTAL SDR* FOUND CRACK ON HYD FILTER MODULE. REPLACED NR 1 ENG HYD FILTER MODULE PER MM 29-12-30 AND SERVICED HYD FLUID. LEAK CHECKS OK. 2 L 7 3 4F RT A22WE 2007061400214 20070614 00214 NM 2007 6 14 UPS07M49894 1 20070405 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 33 LT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01VII R38. BOTT OM-REMAIN BLENDOUT 0.070" DEEP BORE REAMED TO 1.178" DIA REMAIN BLENDOUT 0.070" DEEP EXCEED EO LIMITS. 10X MAG DVI C/O NO CORROSION. BN BORE BLENDOUT & BOTTOM PERI RADIUSED, SMOOTHEN & PROTECTED SRM 51-21-01VII R38. REPAIR SLEEVE BUSHING FAB & INSTALED PER EO FIG 5. REPAIR C/O AT BN BORE NR 33LT IS ACCEPTABLE IAW EN1202-07. 2 L 7 3 4F RT A22WE 2007061400216 20070614 00216 NM 2007 6 14 ZZDA070606178 1 20070603 A 3350 8039251 BATTERY PACK BOEING 717 717200 1383700 NM EMERGENCY LIGHT MALFUNCTIONED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 896AT 55048 EMERGENCY EXIT LIGHT ABOVE TAIL CONE ILLUMINATES DURING TAKEOFF. LIGHT IN CEILING ON AIRCRAFT RIGHT (LOCATED IN TAIL CO NE) ALSO ILLUMINATED. BOTH LIGHTS EXTINGUISHED IN FLIGHT AFTER 15 MINUTES. REMOVED AND REPLACED AFT CABIN EMERGENCY LI GHT BATTERY PACK. OPS CHECK GOOD. REF M/M 33-51-00. 2 L 7 2 4F TR A6WE 2007061400217 20070614 00217 CE 2007 6 14 N514NC 1 20070610 A 2497 WIRE CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO NLG WW CHAFED E HYIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NE 01 514NC 402C0514 CREW SMELLED BURNING ODOR IN COCKPIT DURING FLIGHT. MX INSPECTED AND FOUND WIRES IN NLG WHEEL WELL CHAFED. MX REPAIRED WIRING AND RELEASED A/C. 1 L 7 2 3O 3 O A7CE E8CE 2007061400218 20070614 00218 NM 2007 6 14 UPS07649936 1 20070609 A 3240 26124121A BRAKE ASSY BOEING 767 76734AF 1385212 NM MLG FAILED A IPXA E ENGINE SHUTDOWN A FLAME/FIRE TX TAXI/GRND HDL 1 SO 01 320UP 27747 INSPECTION TYPE:ETOP TAXIING INTO EWR RAMP NR 5 BRAKE ASSY INTERNALLY FAILED CAUSING LOW LEVEL HYD FLUID FIRE DUE TO CRA CKED PUCK ASSEMBLY. PERFORMED HIGH ENERGY STOP/HEAT DAMAGE CONDITION INSPECTION IAW MM REF 05-51-14-2, NO FIRE DAMAGE NOTED ON ALL ADJACENT A/C STRUCTURES AND ASSEMBLIES. 2 L 7 2 4F RT A1NM 2007061400220 20070614 00220 CE 2007 6 14 GLBA20060946 1 20070513 A 2435 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA STARTER GEN DAMAGED A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 192GL UE192 ABORTED TAKEOFF, DURING TAKEOFF ROLL PILOTS REPORTED THAT A LT DC GENERATOR ANNUNCIATOR ILLUMINATED. MAINTENANCE REPAIRE D A WIRE AT THE LT STARTER GENERATOR. REFERENCE MFG 1900D 24-00-00. OPERATIONAL CHECK OF THE SYSTEM WAS GOOD. 2 L 7 2 4T 3 T RT A24CE E2NE 2007061400222 20070614 00222 CE 2007 6 14 DXTA200702177 1 20070505 A 3260 9006EN43 PROXIMITY SENSOR RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG INOPERATIVE E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 871QS 797 258763 LT MAIN GEAR AUX ANNUNCIATOR REMAINS ON WITH THE LANDING GEAR RETRACTED. TROUBLESHOT SYSTEM FOUND LT AUX DOWNLOCK SWITC H INOP. REPLACED SWITCH WITH NEW SWITCH OPS CHECK GOOD. ALL WORK IAW MM CH 32-60-00. 2 L 7 2 4F 4 F RT A3EU E6WE 2007061400224 20070614 00224 SW 2007 6 14 AC2A115478 1 20070514 A 2121 ES731861 FAN BELL 427 427 1182207 SW PWC PW207 PW207D NE CABIN AIR DAMAGED E AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 427CK 50 56043 FAN BLADES DISENGAGED FROM THE FAN DRIVE AND DAMAGED THE HUB AND BLADES. 1 G 7 1 3U 3 U R00001RC E42NE 2007061400232 20070614 00232 CE 2007 6 14 DJFA2007056 1 20070519 A 2150 COALESCER BAG CESSNA 750 750 2076810 CE ALLSN AE300 AE3007A GL CABIN AIR DIRTY E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 704LX 7500091 TRIP NR 1182065 CREW REPORTED OILY ODOR COMING FORM THE GASPERS. FLIGHT CONTINUED. MAINTENANCE FOUND THE COALESCER SOC KS DIRTY. BOTH SOCKS WERE CLEANED AND REINSTALLED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007061400233 20070614 00233 WP 2007 6 14 CNMA20070008 1 20070502 A 2740 AJH7337507 DRIVE ASSY DOUG DC10 DC1030 3023501 WP GE CF6 CF650* 30018 NE MALFUNCTIONED A CNMA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED DE DESCENT 1 SW 07 270AX 2422 378 48318 AT 10,000 MSL AIRCRAFT SLOWED TO 250 KTS, AP OUT OF TRIM LIGHT ILLUMINATED GREATER THAN 5 SECONDS. AUTOPILOT DECOUPLED AND AC PITCHED NOSE DOWN EXCESSIVELY. TRIM SWITCHES FROM BOTH CONTROL COLUMNS DID MOVE LONG TRIM HANDLES BUT STAB INDIC ATOR REMAINED FIXED AT ONE DEGREE NOSE UP SETTING. ALTERNATE TRIM SWITCHES ALSO MOVED HANDLES BUT INDICATOR SETTING REM AINED AT ONE. MANUAL MOVEMENT OF LONG TRIM HANDLES ALSO INEFFECTIVE. QRH PROCEDURES FOLLOWED IAW COM. UNEVENTFUL LAND ING AT ATL. FULL UP ELEVATOR CONTROL REQUIRED DURING APPROACH AND FLARE. PERFORMED DRIVE CHAIN TENSION AND CHAIN WEAR IAW AMM 27-44. BOTH CHAINS ARE WITHIN AMM LIMITS. (R CLARK 11350 5-4-07). ACCOMPLISHED JACK SCREW MEASUREMENT CHECK IA 2 L 7 3 4F 4 F A22WE E23EA 2007061400234 20070614 00234 CE 2007 6 14 AMWA84785BC 1 20070520 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MASTER WEAK A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 166YV 24278 633 UE166 DURING FLT, THE BATTERY CHARGE ANNUN ILLUMINATED. ACFT LANDED WITH NO FURTHER INCIDENT. THIS BATTERY CHARGE ANNUN WRIT EUP IS A NUISANCE A SEVERE DISTRACTION TO THE PILOTS. REMOVED AND REPLACED BATTERY. 2 L 7 2 4T 3 T RT A24CE E2NE 2007061400236 20070614 00236 CE 2007 6 14 DJFA2007057 1 20070521 A 5552 HINGE BRACKET CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LT ELEVATOR CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 708LX 7500109 DURING A SCHEDULED INSPECTION, MAINTENANCE DISCOVERED THE LT ELEVATOR HINGE BRACKET CRACKED. THE CRACK WAS .23 INCHES L ONG ON THE OB SIDE. CRACK WAS CONFIRMED THROUGH NDI. MAINTENANCE IS REPALCING THE ELEVATOR HINGE BRACKET. [06-17- 07] MAINTENANCE REPLACED THE ELEVATOR ASSEMBLY. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007061400240 20070614 00240 CE 2007 6 14 052407N412CS 1 20070524 A 3230 LANDING GEAR CESSNA 525 525 2076601 CE WILINT FJ44 FJ44 66000 GL MALFUNCTIONED E Z5FA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 63 412CS 525B0059 ON APPROACH, AFTER GEAR WAS EXTENDED, NO GEAR DOWN INDICATION WAS NOTED ON ANY OF THE (3) ANNUNCIATORS. ABORTED APPROACH INITIATED A GO-AROUND AND RAN THE GEAR CHECKLIST. TOWER ADVISED ALL GEAR APPEARED TO BE DOWN. BLEW GEAR DOWN AND REQUES TED EMERGENCY EQUIPMENT TO BE STANDING BY. ATC DECLARED EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT IN MAI NTENANCE AT THIS TIME. ON SITE MAINTENANCE PERFORMED GEAR RETRACTION TESTS, SERVICE BLOWDOWN BOTTLE, ALL CHECKS GOOD. CR EW PERFORMED OPERATIONAL CHECK FLIGHT WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE 5-26-07. 1 L 7 2 4F 4 F RT A1WI E3GL 2007061400245 20070614 00245 CE 2007 6 14 DXTA200702205 1 20070518 A 3233 67422175 ELASTOMER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG ACTUATOR WORN E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 901QS 7615 7500102 EXCESSIVE NOSEWHEEL VIRBRATION DURING TAKEOFF, TAKE-OFF ABORTED. REPLACED BOTH NOSE TIRES WITH NEW AND REPLACED WORN NOS E GEAR ACTUATOR ELASTOMERS WITH NEW. TIGHTENED NOSE TORQUE LINK HARDWARE. WORKED IAW CHAPTERS 32-41-01 AND 32-30-03 OF T HE 750 MM. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007061400246 20070614 00246 CE 2007 6 14 DXTA200702206 1 20070518 A 2611 SMOKE DETECTOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CARGO BAY DIRTY E DXTA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 902QS 7500002 (BAGGAGE SMOKE) CAS ILLUMINATED IN FLIGHT. SELECTED PWR ON PERFORMED BAGGAGE SMOKE OPS CK IAW MM CH 26-14-00 OPS CHECK G OOD. REMOVED BAGGAGE SMOKE ALARM VENT COVERS FOUND ALARM TO BE EXTREMELY DUSTY CLEANED SMOKE ALARM VENT COVER REINSTALLE D ALARM AND COVER. OPS CHECK GOOD IAW MM CH 26-14-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007061400247 20070614 00247 NM 2007 6 14 DXTA200702209 1 20070521 A 3240 C2203470060700 CONTROL UNIT AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE BRAKE SYSTEM INTERMITTENT E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 284QS 2218 185 WHEN BRAKING THE AIRCRAFT TO A FULL STOP AT LOW TAXI SPEEDS, LT BRAKE RELEASED AS PRESSURE ON THE BRAKE PEDALS IS LESSEN ED TO PREVENT NOSE DIP. IS MOST PRONOUNCED WHEN PARKING OR HOLDING SHORT. REMOVED OLD NR 2 BSCU AND REPLACED WITH REPAIR ED UNIT. OPERATIONAL TEST PASSED IAW CH 32-446 OF THE F-2000 MM. ALL WORK PERFORMED IAW CH'S 45-001, 29-000, 24-000, AN D 29-112 OF THE F-2000 MM. 2 K 7 2 4F 4 F RT A50NM E44NE 2007061400248 20070614 00248 CE 2007 6 14 DXTA200702210 1 20070522 A 3240 BRAKE ASSY RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG WEAK E DXTA O OTHER O OTHER LD LANDING 1 GL 07 880QS 258570 UPON LANDING, CREW STATED THAT (BRAKES FEEL SPONGY). ACCOMPLISHED BLEEDING OF MAIN BRAKE SYSTEM, EMERG BRAKE SYSTEM, AN D MAXARETS, TAXI CHECKED AND BRAKES FOUND NORMAL IAW MM CH 32-40-00. REF HBS-VNY WO 21-04-901 SQK 1.5. 2 L 7 2 4F 4 F RT A3EU E6WE 2007061400249 20070614 00249 CE 2007 6 14 DXTA200702214 1 20070523 A 2710 4006719903 SERVO CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL AILERONS INOPERATIVE E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 944QS 6568 7500144 FL410, AIRCRAFT STARTED LT BANK (YOKE MOVED ABOUT 60 FT TO THE LT) CASS MESSAGE RETRIM LT WING DOWN CAME ON. LIGHT WENT OUT AFTER ABOUT 5 MINS. REPLACED AILERON SERVO IAW MM CH 22-10-01. OP'S CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007061400252 20070614 00252 CE 2007 6 14 DXTA200702218 1 20070527 A 3220 UPLOCK CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG OUT OF TOLERANCE E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 931QS 7500064 DURING CRUISE, HEARD AND FELT BUMPING OF THE PLANE. DURING DESCENT FELT AND HEARD A LOUD BUMP AND HAD A MOMENTARY NOSE G EAR RED UNLOCK LIGHT. PERFORMED GEAR BUMP TROUBLESHOOTING IAW MM 32-30-00. FOUND NOSE GEAR UPLOCK AND LT MAIN UPLOCK O UT OF TOLERANCE, ADJUSTED IAW MM 32-30-00. CHECKED GOOD, NO DEFECTS NOTED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007061400253 20070614 00253 CE 2007 6 14 DXTA200702219 1 20070527 A 3240 BRAKE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LT MLG WEAK E DXTA O OTHER O OTHER LD LANDING 1 GL 07 670QS 5605170 LT BRAKE FADES NEAR END OF ROLLOUT DURING MEDIUM, CONTINUOUS BRAKING. ACCOMPLISHED BRAKE BLEEDING PROCEDURE IAW MM 32-4 2-00. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007061400254 20070614 00254 CE 2007 6 14 DXTA200702232 1 20070601 A 2910 HYDRAULIC SYSTEM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LOW E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 920QS 7500120 IN CRUISE (HYD VOLUME LOW A (CAS) MESSAGE ILLUMINATED HYDRAULIC QUANTITY OF A SYSTEM INDICATED 5 PERCENT. WE FOLLOWED CHECKLIST AND BLEW DOWN LANDING GEAR AND USED EMERGENCY BRAKES AND STEERING UPON LANDING. [06-15-07] REMOVED AND REP LACED NOSE WHEEL STEERING CENTERING HOSE. RESET LANDING GEAR BLOW DOWN SYSTEM AND SERVICED BOTTLE AS REQUIRED. PERFORMED OPERATIONAL CHECK OF NORMAL LANDING GEAR SYSTEM. OPS CHECK GOOD. NO LEAKS NOTED. PERFORMED OPERATIONAL CHECK OF NOSE WH EEL STEERING. OPS CHECK GOOD. NO LEAKS NOTED. ALL WORK DONE IAW CESSNA X MM 32-30-06 AND 32-50-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007061500003 20070615 00003 CE 2007 6 15 DXTA200702221 1 20070528 A 2750 CONTROL HANDLE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS MALFUNCTIONED E DXTA O OTHER F FLT CONT AFFECTED LD LANDING 1 GL 07 945QS 7500029 DURING FINAL APPROACH WHEN FLAPS WERE SELECTED TO 35 DEGREES, FLAPS FAIL BETWEEN FLAPS 15 AND FLAP 35. INTERROGATED FLAP CONTROLLER BITE CODES. CODES 2 AND 6 WERE SET. REMOVED FLAP CONTROL HANDLE AND CLEANED OPTICAL SWITCHES. REINSTALLED FL AP CONTROL HANDLE. FLAP SYS OPS CHECK GOOD MM CHP 27-51-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007061500005 20070615 00005 CE 2007 6 15 DJFA2007059 1 20070530 A 5511 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 718TA RK195 DURING A SCHEDULED INSPECTION, MAINTENANCE DISCOVERED A RIB FLANGE CRACKED ON THE RT SIDE OF THE H-STAB APPROX 7 INCH FR OM THE AFT EDGE ON THE BOTTOM FLANGE. SDR WILL BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION. 2 H 7 2 4F 4 F RT A16SW E25EA 2007061500006 20070615 00006 CE 2007 6 15 DELA200700003 1 20070516 A 2422 66084271 INVERTER LEAR 55 55LEAR 5170702 CE FAILED E DELA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 242RB 132 SECONDARY INVERTER FAILED ON TAXI-OUT. 2 L 7 2 4F A10CE 2007061500008 20070615 00008 NM 2007 6 15 DXTA200702191 1 20070513 A 3297 WIRE GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE MLG BROKEN E DXTA O OTHER N FALSE WARNING DE DESCENT 1 GL 07 718QS 136 RT MLG RED INDICATION IN FLIGHT W/GEAR NOT SELECTED DOWN. IT OCCURRED DESCENDING THROUGH 9000 FT. AT 250 KIAS. ACCOMPANI ED BY RED GEAR SPEED LIMIT INDICATIONS. M2B- FOUND A BROKEN WIRE AND WATER IN THE BACKSHELL OF WHEEL WELL DISCONNECT 44 GJ1. RE-PINNED CONNECTOR AND REPLACED THE BACKSHELL AND PROTECTIVE BOOT IAW STANDARD WIRING PRACTICES AND G200 WDM 32-00 -00. PERFORMED A COMPLETE SYS FUNCTIONAL TEST IAW G200 MM 32-10-11 AND CMP 326001, NO FAULTS FOUND AT THIS TIME. 2 L 7 2 4F 4 F RT A53NM E35NE 2007061500009 20070615 00009 NM 2007 6 15 DXTA200702216 1 20070526 A 3260 84738722 PROXIMITY SENSOR AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE NLG INOPERATIVE E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 213QS 6144 113 RED NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. SELECTED GEAR DOWN AND GEAR EXTENDED NORMALLY. ALL INDICATIONS NORMAL.REMOVED INOP NOSE GEAR UPLOCK DETECTOR AND INSTALLED A NEW UNIT IAW CH 32-600 OF THE MM OPS CHECK GOO D. 2 K 7 2 4F 4 F RT A50NM E44NE 2007061500011 20070615 00011 NM 2007 6 15 DXTA200702220 1 20070528 A 3260 803682 PROXIMITY SENSOR AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE MLG DOOR INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 262QS 5155 162 LANDING GEAR WAS EXTENDED USING ABNORMAL GEAR EXTENSION CHECKLIST BECAUSE, UPON TAKEOFF AT GEAR RETRACTION NEITHER MAIN GEAR CAME UP. REMOVED LT GEAR DOOR PROX SWITCH PN 803682, SN1408 INSTALLED PN 84799031 SN 2047. REMOVED RT GEAR DOOR P ROX SWITCH PN 803682 SN 1401 INSTALLED PN - 803682 SN 1131. REMOVED PCB (417JE) PN F422 SN 5303 INSTALLED PN 12-337-3 9 SN 333. REMOVED RELAY (5OYGM) PN F302-122 NSN INSTALLED PN F302-122 NSN. ALL CHECKS PERFORMED IAW THE MM 32-300 AN D 32-002 WITH NO DEFECTS NOTED AT THIS TIME. 2 K 7 2 4F 4 F RT A50NM E44NE 2007061500014 20070615 00014 CE 2007 6 15 DXTA200702242 1 20070605 A 3297 WIRE HARNESS CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG DAMAGED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 391QS 5600493 UNEVEN BRAKE SURGE DURING LANDING ROLL. IT FEELS AS IF THE BRAKES ARE BEING PUMPED. [06-15-07] INSPECTED RUDDER PEDA L SUPPORTS I/A/W SL560-27-13 W/NO DEFECTS NOTED. INSPECTED ANTI-SKID SYSTEM WIRING & PERFORMED ANTI-SKID WIRING CHECK I AW NJA T/S FORM DATED 11/7/05, REPAIRED TWO BROKEN GROUND TERMINALS ON RT ANTI-SKID WIRE HARNESS. ALL WIRE SYSTEM CHECK S AFTER REPAIR FOUND WITHIN LIMITS. PERFORMED TAXI CHECK OF ANTI-SKID SYSTEM E BRAKE SYSTEM OPS CHECKED GOOD NO BRAKE SU RGING NOTED, MAINTENANCE PERFORMED IAW CE-560 MM CH 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007061500020 20070615 00020 NM 2007 6 15 DXTA200702230 1 20070531 A 3240 TRANSDUCER AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE WHEEL SPEED MALFUNCTIONED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 284QS 185 WHEN BRAKING AT LOW TAXI SPEEDS THE LT BRAKE RELEASES AND THE AIRCRAFT WILL PULL TO THE RT. PERFORMED FUNCTIONAL CHECK O F ANTI-SKID SYSTEM, BOTH CHANNELS AND BOTH SYSTEMS ARE WORKING IAW M/M 32-414 CHECKED WIRING FROM BOTH BSCU'S TO ALL TR ANDUCERS AND SERVO VALVES WITH NO DEFECTS NOTED. CLEARED ALL FAULT SFROM AIRCRAFT COMPUTERS AND EICAS DISPLAYS AND RESE T ALL MINELCOS. REMOVED NR1 AND NR2 WHEEL SPEED TRANSDUCERS AND OPS CHECKED ANTI-SKID SYSTEM GOOD IAW MM 32-414. 2 K 7 2 4F 4 F RT A50NM E44NE 2007061500021 20070615 00021 CE 2007 6 15 DXTA200702231 1 20070531 A 3240 99144683 METERING VALVE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL BRAKES WORN E DXTA O OTHER O OTHER LD LANDING 1 GL 07 975QS 5657 7500175 LT BRAKE PEDALS DO NOT DEPRESS EVENLY PREVENTING SMOOTH APPLICATION OF BRAKES. REPLACED WORN POWER BRAKE METERING VALVE WITH UNIT OVERHAULED, W/O NR C51242, ON MARCH 17, 2007. IAW CHAP. 32-42-00 OF MM. OPERATIONAL CHECKS, LEAK CHECK SAT ISFACTORY. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007061500022 20070615 00022 EA 2007 6 15 ACE060507 2 20070605 A 7314 DIAPHRAGM CRANEXXXXXXX BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA FUEL PUMP RUPTURED E YADA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 AL 03 112AX 1165 B1075 UC45 FUEL DRIPPING FROM NR 1 ENGINE, GANG DRAIN. REPLACED NR 1 LOW PSI FUEL PUMP. DISASSEMBLY OF PUMP REVEALED A RUPTURED D IAPHRAGM, PN RA5326 WITH 1165 TSI. 2 L 7 2 4T 4 T RT A24CE E4EA 2007061500023 20070615 00023 CE 2007 6 15 DXTA200702244 1 20070606 A 3600 CLAMP RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP REAR BAY LEAKING E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 815QS 258705 APPROX 5 MIN AFTER TAKEOFF, REAR BAY OVERHEAT LIGHT CAME ON. [06-15-07] RAN AIRCRAFT AT POWER AND FOUND NR 1 MAV LEAKING AT BOTH CLAMPS. O/B CLAMP WAS LEAKING DIRECTLY ON TEMP SENSOR. REMOVED NR 1 MAV AND REPLACED SEALS WITH NEW P/N 6-646-1 PAR AND 24096-200A AND REINSTALLED MAV. PERFORMED LEAK CHECK WITH NR 1 ENGINE AT POWER. LEAK CHECK SATISFACOTRY . SAFETY WIRED LINES AND CLAMPS AS REQUIRED. WORK DONE IAW HAWKER 800XP MM CH 21-10-25. 2 L 7 2 4F 4 F RT A3EU E6WE 2007061500024 20070615 00024 CE 2007 6 15 DXTA200702246 1 20070606 A 5210 DOOR BEECH MU300 400A 1155402 CE MAIN PAX STUCK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 149QS RK473 MAIN CABIN DOOR WOULD NOT OPEN PRIOR TO DEPLANING AFTER A 1.2 HOUR FLIGHT. PASSENGERS AND CREW DEPLANED THROUGH THE EMER GENCY EXIT ESCAPE HATCH. [06-15-07] INSPECTED CABIN DOOR & FOUND STEP CABLE UPPER BRACKET BENT & ROD END JAMMED BETWEEN CABIN & DOOR. STRAIGHTENED & RE-SECURED CABLE BRACKET. LUBED CABIN DOOR PINS. OPERATIONAL CHECKS OF CABIN DOO R GOOD, NO DEFECTS NOTED. MAINTENANCE PERFORMED IAW BEECHJET 400A MM CH 52-10-00. 2 H 7 2 4F RT A16SW 2007061500026 20070615 00026 CE 2007 6 15 DXTA200702234 1 20070601 A 2740 41011680107 ACTUATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE HORIZONTAL STAB INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 686QS 632 5605661 STAB MISCOMPARE LIGHT ILLUMINATES ON FLAP RETRACTION AFTER T/O. REMOVED HORIZONTAL STAB ACTUATOR AND INSTALLED AN INSPE CTED ACTUATOR. OPS AND LEAK CHECKS GOOD. WORK DONE IAW CHAPTER 27-40-00 OF THE MM. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007061500028 20070615 00028 NM 2007 6 15 NOCA10407 1 20070529 A 3350 BPS73 BATTERY PACK BOEING 767 767304 NM EMERGENCY LIGHTS INOPERATIVE A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 769NA 28039 L2 & R2 EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK AT L2 DOOR PER WDM 33-51-01, ALL OPS OK. 2 L 7 2 4F RT A1NM 2007061500029 20070615 00029 EA 2007 6 15 TRAX200700778 1 20070602 A 5210 LONGERON CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 906EV 7642 FOUND CORROSION ON PASSENGER DOOR LOWER LONGERON. 2 L 7 2 4F RT A21EA 2007061500030 20070615 00030 EA 2007 6 15 TRAX200700783 1 20070603 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA BS 540-616 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 906EV 7642 FOUND CORROSION ON SEAT TRACK IN CARGO FROM FS 540 TO FS 616, SEE ADDITIONAL WORK SHEET. 2 L 7 2 4F RT A21EA 2007061500033 20070615 00033 EA 2007 6 15 TRAX200700787 1 20070604 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 885AS 7521 FOUND FS 280 AT RBL 9 O/B ANGLE IS CRACKED. 2 L 7 2 4F RT A21EA 2007061500036 20070615 00036 EA 2007 6 15 TRAX200700790 1 20070604 A 5320 BRACE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 975EV 7599 ANGLE BRACE IS CRACKED AT FS 280.0 RBL 9.0 ON THE OUTSIDE. 2 L 7 2 4F RT A21EA 2007061500038 20070615 00038 EA 2007 6 15 TRAX200700792 1 20070604 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 340 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 975EV 7599 ASD THRESHOLD, FLOOR PANEL SUPPORT AT FS 340 IS CORRODED. 2 L 7 2 4F RT A21EA 2007061500041 20070615 00041 2007 6 15 TRAX200700797 2 20070605 A 7261 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE FLUCTUATES A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 979EV 7737 AT FL320, RECEIVED LT ENG WARNING MSG, ENG OIL PRESS FLUX BETWEEN 23 - 34 PSI, FOLLOWED QRH, REDUCED ENG POWER TO GROUND IDLE, RELATED TO DEFECT NR 305469-1. EN ROUTE TO GRB, A/C DIVERTED TO ORD DUE TO MTC, EMERGENCY DECLARED, FLT 4404 (X2 ) CX AND ON 06/06/07 FLT 4265 CX. 2 L 7 2 4F RT A21EA 2007061500042 20070615 00042 SO 2007 6 15 FDKA200704171 1 20070425 A 3350 AD20131A POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 829MJ 253 145228 FDM 6206 JFK-MHT (1014 PHX LCL) - EMERGENCY EXIT DOOR LIGHT INOP. MX REMOVED AND REPLACED NR 3 POWER SUPPLY. 2 L 7 2 4T RT T00011AT 2007061500043 20070615 00043 SO 2007 6 15 FDKA200704176 1 20070429 A 3350 BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DISCHARGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 830MJ 145259 FDM 6000 MCO-RDU (0639 PHX LCL) - EMERGENCY LIGHTS LEFT ON CAUSING BATTERY CHARGE TO BE LOW. MX RECHARGED BATTERIES AND OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007061500044 20070615 00044 SO 2007 6 15 FDKA200704178 1 20070429 A 3350 BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DISCHARGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 830MJ 145259 FDM 6146 ATL (1930 PHX LCL) - CAPT CALLED SAYING THAT THE EMERGENCY LIGHT BATTERIES WEREN’T CHARGED FOR 22 HOURS. MX OP S CHECKED THE LIGHTS AND FOUND NO DEFECTS. 2 L 7 2 4T RT T00011AT 2007061500045 20070615 00045 SO 2007 6 15 FDKA200705181 1 20070503 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6010 RDU-FLL (0430 PHX LCL) - CREW REPORTED 1 EMERGENCY FLOOR LIGHT STRIP INOPERATIVE. MX RESET SYSTEM AND SYSTEM O PERATED NORMALLY. 2 L 7 2 4T RT T00011AT 2007061500046 20070615 00046 NM 2007 6 15 FDKA200705183 1 20070504 A 3350 GROUND WIRE DHAV DHC8 DHC8101 2809002 NM EMERGENCY LIGHTS BROKEN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 805LR 039 FDM 6198 JFK-BTV (1247 PHX LCL). ROW 2 OVERHEAD EMERGENCY LIGHT INOP. MX REPAIRED BROKEN GROUND WIRE. 2 H 7 2 4T RT A13NM 2007061500047 20070615 00047 NM 2007 6 15 FDKA200705196 1 20070509 A 3350 10126271 LIGHT DHAV DHC8 DHC8101 2809002 NM CABIN BROKEN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 807LR 070 FDM RON JFK (1330 PHX LCL) - ROW 4 C/D EMERGENCY EXIT LIGHT BROKEN. MX REMOVED AND REPLACED EMERGENCY LIGHT ASSY. 2 H 7 2 4T RT A13NM 2007061500048 20070615 00048 WP 2007 6 15 IXXA070031O 1 20070604 A 3000 CLAMP DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D* 52039 NE ANTI ICE SYS BROKEN A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 799AL 47407 3744 45922 671011 DURING CLIMB FROM KTOL NR 1 ENGINE ANTI-ICE LIGHT ILLUMINATED, OIL PRESSURE LIGHT FLICKERED, EGT DROPED TO 270°C, LOW PR ESSURE PNEUMATIC CONTROL CIRCUIT BREAKER POPPED, ENGINE GENERATOR FAIL LIGHT ILLUMINATED WHILE VOLTS AND FREQUENIES WERE NORMAL. CLIMB POWER WAS SET AT EPR 1.70, AND EGT 560°C. THE ENGINE POWER LEVER WAS RETARDED TO IDLE AND ALL INDICATION S RETURNED TO NORMAL. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE AND FOUN D THE CENTER INTERMEDIATE ANTI-ICING AIR MANIFOLD FORWARD CLAMP BOLT BROKEN. MAINTENANCE REPLACED THE BOLT AND REPAIRED WIRES IN THE PYLON IAW DACO DC8 MM 20-50-1. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4 F 4A25 1E8 2007061500050 20070615 00050 2007 6 15 NWAA072119604 4 20070609 A 2320 36145764501 CONTROL PANEL DOUG DC9 DC932 3022066 WP ACARS SHORTED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 604NW 36250 1392 47222 THE ACARS COMMUNICATIONS AND REPORTING SYSTEMS IN THE COCKPIT FAILED AND CAUSED SMOKE SHORTLY AFTER TAKEOFF. THE ELECTR IC POWER TO THE ACARS UNIT WAS DISABLED AND COM PROCEDURES WERE COMPLIED WITH. THE SMOKE DID STOP AND THE AIRCRAFT RETU RNED TO A SAFE BUT OVERWEIGHT LANDING BACK AT DFW. MAINTENANCE DETERMINED THAT THE ACARS CONTROL PANEL SHORTED OUT BUT DID NOT CAUSE ANY COLLATERAL DAMAGE TO SURROUNDING AREAS. THE CONTROL PANEL WAS REPLACED AND THE SYSTEM CHECKED OUT FIN E. THE AIRCRAFT WAS RETURNED TO OPERATIONAL STATUS. 2 L 7 2 4F A6WE 2007061500051 20070615 00051 EU 2007 6 15 F3LA200700130 1 20070609 A 2910 6425658505 LINE AIRBUS A318 A318111 3940019 EU HYD SYSTEM WORN A F3LA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 03 806FR 91 2218 FLIGHT CREW REPORTED YELLOW HYDRAULIC QUANTITY LOW. FOLLOWED HYD QTY LOW ECAM: PTU-OFF; ENG DRIVEN PUMP-OFF. YELLOW HY DRAULIC PUMP NEVER CAVITATED OR OVERHEATED. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT AND WAS TOWE D TO THE GATE. PERFORMED CHECK OF YELLOW HYD SYS FOR POSSIBLE CAVITATION IAW AMM 29-00-00-280-006, STEP 4A. REPLACED P RESSURE LINE FOR TRANSDUCER IAW AMM 20-23-11-911-001. REPLACED NR 2 ENG CASE DRAIN FILTER IAW AMM 29-13-93-610-041. RE PLACED HP FILTER IAW AMM 29-13-45-610-001. REPLACED LP FILTER IAW AMM 29-13-44, PB 401. NO CONTAMINATION FOUND IN THE FILTERS REPLACED. NO CAVITATION WAS REPORTED IAW 29-00-00-280-006, STEP 4A, STEP 1. CHECKED FOR EXTERNAL LEAKING OF HY 2 L 7 2 4F RT 2007061500054 20070615 00054 WP 2007 6 15 DHL2007803521 1 20070603 A 5730 565122115SP PANEL DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 LT WING LWR PANEL CRACKED 1" STA XW -3.125. REMOVED PANEL IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 5 1-1-8B. INSTALLED NEW PANEL IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). REFER TO JC EC-00359-001 (WO 1028) FOR PANEL FABRIC ATION. 2 L 7 4 4F RT 4A25 2007061500055 20070615 00055 WP 2007 6 15 DHL2007803519 1 20070603 A 5720 565122114 CHANNEL DOUG DC8 DC873 302199C WP RTWING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 RT WING LWR FAIRING ZEE CHANNEL CRACKED 1" STA XW -3.125. REMOVED CRACKED ZEE CHANNEL IAW SRM 51-1-21. CLEANED, TREATE D AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL IAW SRM 51-1-21. REFER TO JC EC-00360-00 (WO 1028) FOR ZEE FA BRICATION. 2 L 7 4 4F RT 4A25 2007061500056 20070615 00056 WP 2007 6 15 DHL2007803530 1 20070603 A 5710 VANE DOUG DC8 DC873 302199C WP LT WING UNKNOWN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 LT OUTBD VANE SLOT HAS AN INTERIM REPAIR AT STA XOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-01-07, DWG NR AD42-57-104 REV IR DATED 05-16-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTION AND FABRICATED EXTERNAL REPAIR DOUBLER (AL7075T6 0.071") INTERNAL DOUBLER (AL7075T6 0.063") AND FILLER (AL7075T6 0.063") IAW DWG NR AD42-57-104. CLEANED, TREATED AND PRIMED AREA, FILLER, INTERNAL DOUBLER AND INNER FACE OF EXT REPAIR DOUBLER IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DWG NR AD42-57-104, SRM 51-1-11, SRM 51-1-21, SR M 51-3-0, SRM 51-1-20D, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007061500057 20070615 00057 WP 2007 6 15 DHL2007803528 1 20070603 A 5712 97532944 RIB DOUG DC8 DC873 302199C WP WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 NR 4 STUB WING RIB CRACKED STA XOLDO 67.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW JC EC-00364-001, DOUGLAS DWG NR 9753297. REMOVED CRACKED RIB IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW RIB (P/N 9753297-4SP) IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE). REFER TO JC EC-00364- 001 (WO 1028) FOR RIB FABRICATION. 2 L 7 4 4F RT 4A25 2007061500059 20070615 00059 WP 2007 6 15 DHL2007803529 1 20070603 A 5710 VANE DOUG DC8 DC873 302199C WP RT WING UNKNOWN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 RT OUTBD VANE SLOT HAS AN INTERIM REPAIR AT STA XOLDO 67 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3- DA TED 06-01-07, DWG NR AD42-57-102 REV IR DATED 05-16-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-0. C UT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER (AL7075T6 0.071") INTERNAL DOUBLER AND FILLER BOTH FROM AL7075T6 0. 063" IAW DWG NR AD42-57-102. CLEANED, TREATED AND PRIMED AREA, FILLER, INTERNAL DOUBLER AND INNER FACE OF REPAIR DOUBLE R IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DWG NR AD42-57-102, SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0, S RM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007061500061 20070615 00061 WP 2007 6 15 DHL2007803525 1 20070601 A 5740 576989130 ATTACH ANGLE DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 RT WING CTR L/E OUTBD VANE SLOT ATTACH ANGLE CRACKED 1/2" STA XOLDI 6.225. REMOVED CRACKED ANGLE IAW SRM 51-1-21. CLEA NED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-21. REFER TO JC EC-00372-001 (WO 1028) FOR ANGLE FABRICATION. 2 L 7 4 4F RT 4A25 2007061500062 20070615 00062 WP 2007 6 15 DHL2007803523 1 20070603 A 5754 VANE DOUG DC8 DC873 302199C WP LT WING UNKNOWN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 LT OUTBD VANE SLOT HAS AN INTERIM REPAIR AT STA XOLDO 67 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DAT ED 06-01-07, DWG NR AD42-57-105, REV IR DATED 05-17-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-0. C UT OUT DAMAGED SECTION AND FABRICATED EXTERNAL REPAIR DOUBLER (AL7075T6 0.071") INTERNAL DOUBLER (AL7075T6 0.063") AND F ILLER (AL7075T6 0.063") IAW DWG NR AD42-57-105. CLEANED, TREATED AND PRIMED AREA, FILLER, INTERNAL DOUBLER AND INNER FA CE OF EXT REPAIR DOUBLER IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DWG NR AD42-57-105, SRM 51-1-11, SRM 51-1-21, SRM 5 1-1-20D, SRM 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007061500063 20070615 00063 WP 2007 6 15 DHL2007803526 1 20070604 A 5730 DOUBLER DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 RT WING CTR L/E UPPER ANGLE DOUBLER CRACKED STA XFS 428.000. REMOVED CRACKED ANGLE DOUBLER IAW SRM 51-1-21, SRM 51-1-20 D. FABRICATED ANGLE DOUBLER (AL7075"0" 0.080") IAW SRM 57-2-0 PG 9-10, SRM 57-3-3. HEAT TREATED ANGLE DOUBLER FROM 707 5"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED, PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED A NGLE DOUBLER IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007061500066 20070615 00066 WP 2007 6 15 070127 1 20070604 A 3350 408822101 BATTERY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 875GA 53468 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007061500068 20070615 00068 SO 2007 6 15 SIMA200716303 1 20070611 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 650AE 8184 1109 145417 EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REMOVED AND REPLACED NUMBER TWO BATTERY PACK AND CHARGER IAW EMB AMM. O PERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061500069 20070615 00069 GL 2007 6 15 SIMA200716301 2 20070609 A 7261 23073567 CARBON SEAL EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL NR 1 ENGINE LEAKING A SIMA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 710TB 4348 145224 CAE312830 STRONG OILY ODOR WITH ENGINE BLEEDS ON. REMOVED AND REPLACED NR 1 CARBON SEAL IAW ROLLS ROYCE MM 72-25-25. LEAK AND OP ERATIONAL CHECKS GOOD, PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007061500072 20070615 00072 EA 2007 6 15 TRAX200700796 1 20070605 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 909EV 7658 CABIN EMERGENCY ESCAPE HATCH EXTERIOR INSTRUCTION PLACARD MISSING, RESOLVED ON W/O: 61271 TASKCARD: N/R-00122. REMOVED AND REPLACED CABIN EMERGENCY ESCAPE HATCH EXTERIOR INSTRUCTION PLACARD WITH NEW SERVICEABLE PLACARD P/N S1859, PO NR ASA 115 IAW CRJ 200 AMM 11-20-01. 2 L 7 2 4F RT A21EA 2007061500074 20070615 00074 EA 2007 6 15 TRAX200700806 1 20070607 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 909EV 7658 FOUND FS 484 LBL 27.0 O/B ANGLE CRACKED. 2 L 7 2 4F RT A21EA 2007061500075 20070615 00075 EA 2007 6 15 TRAX200700807 1 20070607 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 909EV 7658 FOUND FS 484 RBL 36.00 O/B ANGLE CRACKED. 2 L 7 2 4F RT A21EA 2007061500078 20070615 00078 NE 2007 6 15 AWXA200700720 2 20070607 A 7200 V2500A1 ENGINE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 1 FLAMED OUT A AWXA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 WP 28 634AW 49457 7413 091 0031 EWR - PHX - IFSD - CREW REPORTED HEARING A "BANG" FOLLOWED BY THE NR 1 ENGINE SHUTTING DOWN. CREW INITIATED AN IN-FLIGH T RESTART OF THE NR 1 ENGINE, ENGINE STARTED AND UPON APPLICATION OF POWER ANOTHER BANG WAS HEARD FOLLOWED BY THE NR 1 E NGINE SHUTTING DOWN. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO SDF. THE LANDING WAS UNEVENTFUL. THE A/C TAXIED T O THE GATE. MX PERFORMED A BOROSCOPE OF THE NR 1 ENGINE. MX DISCOVERED DAMAGE TO BLADES FROM STAGE 7 THRU STAGE 12. MX REPLACED THE NR 1 ENGINE PER TASK CARD R5M71302. ENGINE POWER RUNS WERE GOOD. THE A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E311NE 2007061500080 20070615 00080 NM 2007 6 15 DU4R2007132 1 20070608 A 5412 BULKHEAD BOEING 757 757232 1384965 NM NR 1 NACELLE CHAFED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 640DL 23994 FOUND CHAFED LOWER OUTBOARD CORNER OF NR 1 PYLON AFT BULKHEAD. REPAIRED BY FABRICATING AND INSTALLING GUSSET 4.34 BY 2. 88 BY 1.2 BY .100 FROM 7050-T7451 AND FILLER FROM 15-5PH.125 IAW DELTA ERA 461663-14AD DATED 6/7/07 REV ORIG APPROVED BY FAA FORM 8100-9, WITH AMOC TO PARAGRAPH (A) OF FAA AD 2003-18-05. 2 L 7 2 4F RT A2NM 2007061500081 20070615 00081 NM 2007 6 15 DU4R2007131 1 20070608 A 5412 BULKHEAD BOEING 757 757232 1384965 NM NR 2 NACELLE CHAFED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 640DL 23994 FOUND CHAFED LOWER OUTBOARD CORNER OF NR 2 PYLON AFT BULKHEAD. REPAIRED BY FABRICATING AND INSTALLING GUSSET 4.34 BY 2. 88 BY 1.2 BY .100 FROM 7050-T7451 AND FILLER FROM 15-5PH.125 IAW DELTA ERA 461663-14AD DATED 6/7/07 REV ORIG APPROVED BY FAA FORM 8100-9, WITH AMOC TO PARAGRAPH (A) OF FAA AD 2003-18-05. 2 L 7 2 4F RT A2NM 2007061500083 20070615 00083 NM 2007 6 15 DU4R2007134 1 20070608 A 5420 BRACE BOEING 757 757232 1384965 NM NR 1 OUT OF LIMITS B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 640DL 23994 FOUND NR 1 DIAGONAL BRACE ID 2.003 OUT OF LIMITS. REPAIRED OVERSIZED LUG ON NR 1 DIAGONAL BRACE BY HONING, FABRICATING AND INSTALLING BUSHINGS IAW DELTA ERA 461664-14AD DATED 6/7/07 APPROVED BY FAA FORM 8100-9 WITH AMOC TO PARAGRAPH (A) OF AD 2003-18-05. 2 L 7 2 4F RT A2NM 2007061500084 20070615 00084 NE 2007 6 15 NACA20070014 2 20070602 A 8560 53485152 CLUTCH DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 4 ENGINE SLIPPED A NACA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AL 03 2907F 2535 2535 533265 P31426 NR 4 ENGINE SHUT DOWN DUE TO LOSS OF BMEP, (BMEP TO ZERO), LOSS OF ENGINE BLOWER. REPLACED ENGINE DUE TO CLUTCH FAILURE . 2 L 7 4 4R 4 R A781 5E8 2007061500086 20070615 00086 NM 2007 6 15 07FDEA02068 1 20070604 A 5753 ARC3151504 SKIN DOUG MD11 MD11 3023602 NM ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 EXISTING REPAIR, RT WING I/B FLAP UPPER SURFACE FOUND EXISTING PATCH AT XIFH 217 YIFH 65. EXISTING REPAIR EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007061500087 20070615 00087 NM 2007 6 15 07FDEA02070 1 20070604 A 5311 AFA00203 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 EXISTING REPAIR, UPPER CARGO COMPARTMENT, LT SIDEWALL STRUCTURE FRAME AT STA 1701, L-12L, FOUND WITH REPAIR DOUBLER. EX ISTING REPAIR EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS M AJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007061500090 20070615 00090 NM 2007 6 15 07FDEA02110 1 20070612 A 5313 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 FUSELAGE, CAC COMPARTMENT AT STA 6-100, LONGERON 40L FOUND LONGERON WITH FREEZE PLUG INSTALLED. [06-19-07] REPAIR CA RRIED OUT AT FUSELAGE - CAC COMPARTMENT AT STA 6-100, LONGERON 40L AS PER SRM 53 -10-00 FIGURE 2 VOLUME I. 2 L 7 3 4F RT A22WE 2007061500091 20070615 00091 WP 2007 6 15 07FDEA02111 1 20070613 A 5300 SKIN DOUG DC10 DC1010 3022110 WP ZONE 100 NONE A FDEA O OTHER O OTHER UK UNKNOWN 1 SO 25 389FE 46623 EXISTING REPAIR EXTERNAL FUSELAGE. PERFORMED INSPECTION OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8 -5100-7-5001 P1. 2 L 7 3 4F A22WE 2007061500092 20070615 00092 WP 2007 6 15 07FDEA02112 1 20070613 A 5300 SKIN DOUG DC10 DC1010 3022110 WP ZONE 100 UNKNOWN A FDEA R AUTOROTATION O OTHER UK UNKNOWN 1 SO 25 389FE 46623 EXISTING REPAIR EXT FUSELAGE REPLACED REPAIR PER SRM 53-20-00 FIG 6 VOL 1. 2 L 7 3 4F A22WE 2007061500093 20070615 00093 WP 2007 6 15 07FDEA02114 1 20070613 A 5300 LONGERON DOUG DC10 DC1010 3022110 WP ZONE 100 NONE A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 EXISTING LONGERON SPLICE REPAIR FWD CARGO COMPT PERFORMED INSPECTION OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQ UESTED BY EO 8-5100-7-5001 P2. 2 L 7 3 4F A22WE 2007061500094 20070615 00094 WP 2007 6 15 07FDEA02115 1 20070613 A 5300 LONGERON DOUG DC10 DC1010 3022110 WP ZONE 100 NONE A FDEA R AUTOROTATION O OTHER UK UNKNOWN 1 SO 25 389FE 46623 EXISTING 3 EA LONG SPLICE REPAIR AFT CARGO COMPT PERFORMED INSPECTION OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA RE QUEST BY EO 8-5100-7-5001 P.2. 2 L 7 3 4F A22WE 2007061500095 20070615 00095 WP 2007 6 15 07FDEA02116 1 20070613 A 5300 FRAME DOUG DC10 DC1010 3022110 WP ZONE 100 NONE A FDEA R AUTOROTATION O OTHER UK UNKNOWN 1 SO 25 389FE 46623 EXISTING FRAME REPAIR INTERNAL FUSELAGE CAC PERFORMED INSPECTION OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2. 2 L 7 3 4F A22WE 2007061500096 20070615 00096 WP 2007 6 15 07FDEA02117 1 20070613 A 5300 FRAME DOUG DC10 DC1010 3022110 WP ZONE 200 NONE A FDEA O OTHER O OTHER UK UNKNOWN 1 SO 25 389FE 46623 EXISTING FRAME REPAIR MAIN CABIN PERFORMED INSPECTION OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-51 00-7-5001 P2. 2 L 7 3 4F A22WE 2007061500097 20070615 00097 WP 2007 6 15 07FDEA02118 1 20070613 A 5300 SKIN DOUG DC10 DC1010 3022110 WP ZONE 100 UNKNOWN A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 EXISTING SKIN REPAIR EXT FUSELAGE FWD JAMB AFT CARGO DOOR APPLIED SEALANT IAW SRM 51-41-01 VOL 2 AND APPLIED PRIMER IAW SRM 51-21-01 VOL 2. 2 L 7 3 4F A22WE 2007061500098 20070615 00098 NM 2007 6 15 07FDEA02119 1 20070613 A 5315 6520827225 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 CABIN BS 620 FLOORBEAM UPPER CHORD CORRODED ON UPPER SURFACE FROM LBL 3 TO LBL22 REMOVED CORROSION, NDT FOR MATERIAL LOS S, ORIGINAL THICKNESS= .135". REMOVED .017" FLAP PEENED BLENDED AREA, TREATED AND PRIMED AND APPLIED CORROSION INHIBITO R. REF SRM 51-10-6, 51-10-2, MM 20-151, SOP M 20-10-3 AND EA NR 5310-113045. 2 L 7 3 4F RT A3WE 2007061500100 20070615 00100 SO 2007 6 15 FKDA200705199 1 20070511 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 840MJ 145429 FDM 6056 MCO-FLL (1140 PHX LCL), EMERGENCY LIGHT INOP ROW 12 A. MX RESET OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007061500105 20070615 00105 2007 6 15 R61A20070011 4 20070522 A 2210 70244401901 POWER SUPPLY EMB ERJ170 ERJ170100SU 3260403 NM CARGO BAY BURNED A R61A A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 GL 11 803MD 17000015 AUTO PILOT/AUTO THROTTLE DISENGAGED, FOLLOWED BY MAU 3 FAIL INDICATION, THEN CREW HAD SMOKE ODOR AND AFT CARGO SMOKE ALO NG WITH WARNING. CREW DIVERTED AND FOLLOWED QRH PROCEDURES, INDICATION WENT AWAY AND LANDED WITHOUT INCIDENT. MAINTENA NCE WAS DIPATCHED TO A/C INSPECTED AND NO INDICATION OF FIRE WAS FOUND IN CARGO AREA'S. MAINTENANCE FOUND MAU POWER SUP PLY MODULE TO ODOR BURNED. MAINTENANCE REPLACED MODULE OPERATIONAL CHECK GOOD AND A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A56NM 2007061500106 20070615 00106 CE 2007 6 15 LX5R200700002 1 20070605 A 5751 101130003135 BALANCE WEIGHT BEECH BEECH B300 B300 1159232 CE AILERON DETACHED B LX5A K NONE O OTHER IN INSP/MAINT 1 GL 19 971LL 3367 803 FL267 UPON PILOT PREFLIGHT, IT WAS DISCOVERED THAT THE RIGHT HAND AILERON HAD SOMETHING LOOSE INSIDE MOVING AROUND. THE AIRCR AFT WAS BROUGHT INTO MAINTENANCE AND THE AILERON WAS REMOVED AND IT WAS DISCOVERED THAT PART OF THE BALANCE WEIGHT HAD C OME LOOSE. THE LEADING EDGE OF THE AILERON WAS DRILLED LOOSE AND IT WAS DISCOVERED THAT A CENTER SECTION OF THE OUTBOAR D BALANCE WEIGHT HAD BROKE OFF, APPROX 10 INCH PIECE. THE CAUSE IS UNKNOWN, IT BROKE AT THE CENTER RIVET AND THEN WORKE D LOOSE. INSTALLED A WHOLE NEW BALANCE WEIGHT AND REINSTALLED AILERON BACK ON AIRCRAFT. 2 L 7 2 4T RT A24CE 2007061500109 20070615 00109 NM 2007 6 15 CALA0700290 1 20070605 A 5330 6545778 SKIN BOEING 737 7373T0 1384582 NM BS 947 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12313 23364 INSPECTION FOUND A .75 INCH CRACK IN FUSELAGE SKIN AT R-2 DOOR LOWER HINGE CUTOUT, STA 947.5, S14R. THE CRACKED AREA WA S REMOVED AND A DOUBLER, TRIPLER, AND FILLER WERE INSTALLED IAW SRM 53-60-01. 2 L 7 2 4F RT A16WE 2007061500110 20070615 00110 NM 2007 6 15 CALA0700291 1 20070606 A 5330 6545775 SKIN BOEING 737 7373T0 1384582 NM 753 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12313 23364 INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT STA 753, S25R. THE CRACKED AREA OF SKIN WAS CUT OUT AND REPAIR PART S WERE INSTALLED IAW SRM 53-00-01, REPAIR 31. 2 L 7 2 4F RT A16WE 2007061500111 20070615 00111 NM 2007 6 15 CALA0700292 1 20070606 A 5311 141N12043 FRAME BOEING 757 757224 1384958 NM BS 231 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 67134 29283 INSPECTION FOUND A 0.012 INCH CRACK IN BELTFRAME AT STA 231, BL 0, JUST FORWARD OF FORWARD ACCESSORY DOOR CUTOUT. THE C RACKED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW ECRA 5313-01010, REV A. 2 L 7 2 4F RT A2NM 2007061500112 20070615 00112 NM 2007 6 15 CALA0700293 1 20070606 A 5311 65C352436 FRAME BOEING 737 7373T0 1384582 NM BS 847 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12313 23364 INSPECTION FOUND A 1 INCH CRACK IN AFT CARGO DOOR CUTOUT AFT FRAME AT LOWER STOP FITTING, STA 847, S24R. A NEW FRAME WA S INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007061500114 20070615 00114 NM 2007 6 15 CALA0700295 1 20070607 A 5210 507945178 BEAM BOEING 737 7373T0 1384582 NM L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12313 23364 INSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR AFT EDGE BEAM AT NR 7 FORWARD STOP. A REPAIR DOUBLER WAS INSTALLED IAW ECR A 5210-01938 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007061500117 20070615 00117 NM 2007 6 15 UPS07M49895 1 20070331 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 15 RIGHT FOUND CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38. BOTTO M REMAIN BLENDOUT 0.050" DEEP. BORE REAMED TO 1.067" DIA REMAIN BLENDOUT 0.030" EXCEED EO LIMITS. 10X MAG DVI C/O NO C ORROSION. BORE BOTTOM & BLEND OUT PERI RADIUS & SMOOTHEN, PROTECTED SRM 51-21-01 VOL II R38. REPAIR SLEEVE BUSHING FAB & PROTECTED & INSTALLED PER EO FIG 5. REPAIR C/O AT BN BORE NR 15 RT ACCEPTABLE IAW EN1184-07. 2 L 7 3 4F RT A22WE 2007061500120 20070615 00120 NM 2007 6 15 UPS07M49898 1 20070409 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORIZ STAB, BARREL NUT BORE RIGHT NR 23 FOUND CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38. BOT TOM-BORED THRU BORE REAMED TO 1.067" DIA. REMAINING BLENDOUT 0.010" DEEP EXCEED EO LIMITS. 10X MAG DVI C/O NO CORROSIO N. BORE BLEND OUT RADIUSED, SMOOTHEN & PROTECTED SRM 51-21-01 VII R38. REPAIR BUCKET BUSHING FAB, PROTECTED & INSTALLE D PER EO FIG 5. REPAIR C/O AT BARREL NUT BORE NR 23 RIGHT IS ACCEPTABLE IAW EN1204-07. 2 L 7 3 4F RT A22WE 2007061500121 20070615 00121 NM 2007 6 15 UPS07M49899 1 20070414 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 24 RIGHT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38. BOTTOM - SURF CLEANED - BORE REAMED TO 1.067" DIA REMAIN BLEND OUT 0.075" EXCEED EO LIMITS. 10X MAG DVI C/O NO CORROSIO N. BORE FURTHER REAMED TO 1.105" DIA EN1237-07. BORE BLENDOUT & BOTTOM PERI RADIUSED, SMOOTHEN & PROTECTED SRM 51-21-0 1 VII R38. REPAIR SLEEVE BUSHING FAB, PROTECTED & INSTALLED PER EO FIG 5. REPAIR C/O IAW EN1237-07. 2 L 7 3 4F RT A22WE 2007061500122 20070615 00122 NM 2007 6 15 UPS07M49900 1 20070418 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 11 LEFT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38 BOT TOM-REMAINING BLEND OUT 0.070" DEEP BORE REAMED TO 0.988" DIA REMAIN BLEND OUT 0.056" DEEP EXCEED EO LIMITS. 10X MAG DV I C/O NO CORROSION. BORE FURTHER REAMED TO 1.048" DIA & BOTTOM 0. 050" DEEPER PER EN1245-07. REPAIR SLEEVE FAB, PROTEC TED & INSTALLED PER EO FIG 5. REPAIR C/O AT BN BORE NR 11 LEFT IS ACCEPTABLE IAW EN1245-07. 2 L 7 3 4F RT A22WE 2007061500123 20070615 00123 NM 2007 6 15 UPS07M49901 1 20070405 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORIZ STAB BARREL NUT NR 9 LEFT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38. BOTTOM -SURF CLEANED. BORE REAMED TO 0.988" DIA REMAIN BLENDOUT 0.040" DEEP EXCEED EO LIMITS. 10X MAG DVI C/O NO CORROSION. BORE BOTTOM PERI & BLENDOUT RADIUSED, SMOOTHEN & PROTECTED SRM 51-21-02 VII R38. REPAIR SLEEVE BUSHING FAB, PROTECTED & INSTALLED PER EO FIG 5. REPAIR C/O AT BARREL NUT BORE NR 9 LEFT IS ACCEPTABLE IAW EN1196-07. 2 L 7 3 4F RT A22WE 2007061400084 20070614 00084 SO 2007 6 14 LR7A07048 1 20070607 A 5310 BEAM LKHEED 382 382G 526414U SO FS 557 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 722 4698 DURING SCHEDULED B-3 CHECK PER JOB CARD HB3200, FOUND LT UPPER WHEEL WELL ARMPIT PANEL ATTACH BEAM CRACKED AT FS 557, WL 236. REPAIRED BEAM IAW MEA 382-53-07-038. 2 H 7 4 4T A1SO 2007061400087 20070614 00087 SO 2007 6 14 LR7A07051 1 20070607 A 5312 3455086L BULKHEAD LKHEED 382 382G 526414U SO FS 1012 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 722 4698 DURING SCHEDULED B-3 CHECK PER JOB CARD HB5302, FOUND AFT FUSELAGE INTERIOR BULKHEAD INNER TEE CAP CRACKED AT FS 1012, W L260, LBL62. REPLACED TEE CAP IAW SMP583 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007061400088 20070614 00088 SO 2007 6 14 LR7A07052 1 20070607 A 5230 GUSSET LKHEED 382 382G 526414U SO FS 990 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 722 4698 DURING SCHEDULED B-3 CHECK PER JOB CARD HB5302, FOUND CARGO DOOR INNER GUSSET PLATE CRACKED AT FS 990, RBL60. REPLACED GUSSET PLATE IAW SMP 583 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007061400091 20070614 00091 EA 2007 6 14 A6WA200720222 1 20070501 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA SPOILERS ILLUMINATED A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 463AW 7878 DURING APPROACH SPOILERONS CAUTION AND OUTBOARD GROUND SPOILERS CAUTION MESSAGE ILLUMINATED, COMPLIED WITH QRH, PREFORME D FLAP 20 DEGREES LANDING. PERFORMED FUNCTION TEST OF SPOILER IAW AMM 27-61-00. OPS CHECK GOOD AT THIS TIME. (M) 2 L 7 2 4F RT A21EA 2007061400096 20070614 00096 NM 2007 6 14 2007UALA01897 1 20070610 A 5610 WINDSHIELD AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT CRACKED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 822UA 948 FLIGHT DIVERTED UNDER AMBER ALERT DUE TO A CRACKED WINDSHIELD. FOUND MOISTURE PENETRATION AT BUSS BAR CAUSING DELAMINAT ION, SCRAPPED WINDOW. REPLACED CAPTAIN'S WINDSHEILD AND CAPT WINDOW HEAT COMPUTER. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061400099 20070614 00099 NM 2007 6 14 2007UALA01902 1 20070608 A 3510 REGULATOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE OXYGEN MASK LEAKING A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 831UA 1291 CREW O2 READING 1420 AFTER 2 HOURS. SERVICED TO 1770 AT 0430, 1.5 HR DROP OF 350 PSI. FOUND ALSO 2ND OBSERVERS MASK B OX LOWER B NUT LOOSE- TIGHTENED. REPLACED CREW O2 MASK REGULATOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061400100 20070614 00100 EU 2007 6 14 2007UALA01903 1 20070608 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 421UA 500 EMERGENCY LIGHT TEST FAILS WITH FAULT EXTERNAL LOAD L. [07-03-07] REPLACED OVER WING LIGHT BULBS (EXTERIOR) AND REPLAC ED EPSU PER MM 33-51-38. EMERGENCY LIGHT TEST PASSED ON GND. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061400109 20070614 00109 EU 2007 6 14 2007UALA01912 1 20070609 A 3350 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 488UA 1680 NR 3 SVC EMERGENCY LIGHT TEST FAILED. EPSU COMM LEFT AND EPSU AFT BATTERY LEFT. [07-03-07] REPLACED BATTERY PACK AT 1 3WL. SYSTEM CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061400116 20070614 00116 NM 2007 6 14 2007UALA01920 1 20070609 A 5241 TORQUE TUBE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE AFT GALLEY DOOR UNSTABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 AFT GALLEY DOOR CUTOUT TORQUE TUBE HAS MOVEMENT OF .0030 BEYOND LIMITS. [07-03-07] REPLACED THE BEARING AND TORQUE TU BE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061400118 20070614 00118 NM 2007 6 14 2007UALA01922 1 20070609 A 5241 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 FWD GALLEY DOOR SN 1269 AFT SIDE STOP PIN FITTING CUTOUT IS CRACKED 4TH FROM TOP. [07-03-07] MAJOR REPAIR: REMOVED DA MAGE. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 90-52-40-14JD. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061400120 20070614 00120 NM 2007 6 14 2007UALA01924 1 20070610 A 5230 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE AFT CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 555UA 26647 AFT CARGO DOOR UPPER AFT CORNER HAS A CRACK. [08-07-07] MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER PER UA ENGINEE RING SPECIFICATIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061400131 20070614 00131 EA 2007 6 14 SWIA200718330 1 20070525 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7089 CABIN FLOOR SUPPORT STRUCTURE IS CRACKED AT FS 484 AND RBL27, DISCOVERED AT C-CHECK. INSTALLED NEW CLIP PER CRJ200 SRM 51-42-21 PG 17 AND REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2007061400136 20070614 00136 EA 2007 6 14 A6WA200740151 1 20070321 A 4900 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY FAILED A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 437AW 7744 APU FAULT MESSAGE AND FAINT ODOR OF SOMETHING BURNING AT GATE, APU EGT NOTED IN RED. APU WAS SUPPLYING BLEEDS AND ELECT RICS. REMOVED AND REPLACED APU ASSEMBLY. (M) 2 L 7 2 4F RT A21EA 2007061400140 20070614 00140 NM 2007 6 14 XXUA200706039 1 20070606 A 5240 80330034 BOTTLE BOEING 757 7572Q8 1384972 NM PWA PW2037 PW2037M 52117 NE L4 DOOR DISCHARGED A XXUA K NONE O OTHER IN INSP/MAINT 1 EA 15 401JS 26332 DURING DAILY CHECK SERVICE FOUND L4 EMERGENCEY POWER DOOR RESERVOIR OUT OF GREEN BAND. REMOVED AND REPLACED L4 DOOR EME RGENCY POWER RESERVOIR IAW MM 52-11-33. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061400145 20070614 00145 SO 2007 6 14 BQVA200751871 1 20070516 A 5340 1159B2156227 ATTACH FITTING GULSTM G1159 G1159A 3970109 SO REAR BULKHEAD CRACKED E BQVA K NONE O OTHER IN INSP/MAINT 1 EA 01 50BH 10605 2000 359 DURING THE REQUIRED EDDY CURRENT INSPECTION OF THE FS 793 BULKHEAD CAP ANGLE, CRACK INDICATIONS WERE NOTED ON BOTH SIDES . THE CRACKS ARE ABOVE THE .5 INCH BOLT HOLES IN THE CAP ANGLE FOR VERTICAL FIN ATTACHMENT. 2 L 7 2 4F A12EA 2007061400146 20070614 00146 SO 2007 6 14 BQVA200752271 1 20070518 A 5740 ATTACH FITTING GULSTM G1159 G1159A 3970109 SO ZONE 500 CORRODED E BQVA K NONE O OTHER IN INSP/MAINT 1 EA 01 50BH 10605 359 WING TO FUSELAGE ATTACH FITTING AT FS 452 BL 33 (LEFT SIDE), CORROSION DETECTED DURING THE SCHEDULED ULTRASONIC INSPECTI ON. THE CORROSION ON THE OUTBOARD SURFACE IS .158 INCH IN DEPTH, .125 INCH IN LENGTH; AND .125 INCH IN DIAMETER. [07- 03-07] ENGINEERING HAS GRANTED A FLIGHT ALLOWANCE UNDER WO CS117819. THIS ALLOWS CONTINUED NORMAL OPERATION FOR 180 DAY S UNTIL NOV. 27, 2007 BY WHICH TIME A REPAIR IAW ASC229 WILL BE REQUIRED. 2 L 7 2 4F A12EA 2007061400150 20070614 00150 EU 2007 6 14 M2L2007F00001 1 20070428 A 8011 DRIVE GEAR BNORM BN2 BN2A20 1520220 EU LYC O540 IO540K1B5 41532 EA HARTZL HCC2Y HCC2YK1 GL STARTER BROKEN E M2LA O OTHER O OTHER NR NOT REPORTED 1 NM 11 634MA 464 L1459848A AU11938B BENDIX DRIVE GEAR OF RT ENGINE BROKE LOCKING RING GEAR OF CRANKSHAFT LOCKING ENGINE TO A STOP CONDITION. (K) 1 H 7 2 3O 3 O A17EU 1E4 5 C P920 2007061400160 20070614 00160 WP 2007 6 14 ASAA0781747 1 20070526 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 279-303 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 FUSELAGE DENTED BEYOND SRM 53-4 LIMITS. CUT OUT DAMAGED AREA OF SKIN. INSTALLED FILLERS FINGER DOUBLERS AND REPAIR DOU BLER PER SRM 53-4 AND SRM 51-10-3. 2 L 7 2 4F RT A6WE 2007061400161 20070614 00161 WP 2007 6 14 ASAA0781748 1 20070526 A 5313 27779223 LONGERON DOUG DC9 DC983 3022083 WP BS 264-323 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 LONGERON CRACKED. CUT OUT DAMAGED AREA. INSTALLED REPLACEMENT SECTION WITH LONGERON SPLICES PER SRM 51-10-4 AND SRM 53 -02. 2 L 7 2 4F RT A6WE 2007061400178 20070614 00178 NM 2007 6 14 ASAA0791753 1 20070531 A 5320 SUPPORT BOEING 737 737990 NM BS 500 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 FWD CARGO PIT STR LWR SUPPORT CORRODED. REPAIRED IAW SRM 51-40-02. 2 L 7 4 4F RT A16WE 2007061400189 20070614 00189 WP 2007 6 14 UPS07849881 1 20070526 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FS 1760 BL0 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C1 CORROSION ON FLOOR SUPPORT FITTING ON AFT VERTICAL BEAM, FS 1760 BL 0. REMOVED FLOOR SUPPORT FITTING AT STA 1760 BL 0 IAW SRM 51-03-00-0. FABRICATED AND INSTALLED FLOOR SUPPORT FITTING AT STA 1760 BL 0 IAW DWG 5773846, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007061400190 20070614 00190 WP 2007 6 14 UPS07849882 1 20070525 A 5320 FITTING DOUG DC8 DC873F 302199F WP FS 857 L19L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C1 FITTING CRACKED AT STA 857 L19L AFT. REMOVED FITTING AT STA 857 L19L IAW SRM 51-01-20D. FABRICATED AND INSTALLED END FITTING AT STA 857 L19L IAW DWG 4750422, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007061400198 20070614 00198 EA 2007 6 14 COMA0760422 1 20070603 A 2780 SLAT SYSTEM CNDAIR CL600 CL6002C10 1390015 EA MALFUNCTIONED A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 369CA 10079 FLIGHT 5466 - RECEIVED SLAT FAIL MESSAGE ON DESCENT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. CLEARED INHIBITS FRO M SLAT SYSTEM. VISUALLY INSPECTED SLATS, OPERATED SYSTEM, NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007061400209 20070614 00209 WP 2007 6 14 UPS07849911 1 20070605 A 3350 LAMP DOUG DC8 DC871F 302199D WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:N/A 2 EACH EMERGENCY LIGHT ABOVE ENTRY DOOR INOP. RELAMPED EMERGENCY LIGHTS, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2007061400215 20070614 00215 EA 2007 6 14 COMA0770031 1 20070603 A 2780 SLAT SYSTEM CNDAIR CL600 CL6002C10 1390015 EA LE SLATS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 369CA 10079 FLIGHT 5466 - RECEIVED SLAT FAIL MESSAGE ON DESCENT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. CLEARED INHIBITS FRO M SLAT SYSTEM. VISUALLY INSPECTED SLATS, OPERATED SYSTEM, NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007061400219 20070614 00219 NM 2007 6 14 UPS07649940 1 20070611 A 5321 FLOOR PANEL BOEING 767 76734AF 1385212 NM CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 325UP 27751 INSPECTION TYPE:N/A FOUND DENT WITH CRACK ON FLOOR PANEL IN BULK CARGO COMPARTMENT. POS STA 1497 LEFT BBL 16. TWO INCHE S DIA DENT AND 1 INCH CRACK AT CENTER OF DENT - DEPTH .25 INCHES. INTERIM REPAIRED PER EO B767-2550-8036-D APPX A (2). 2 L 7 2 4F RT A1NM 2007061400227 20070614 00227 CE 2007 6 14 DELA200700002 1 20070504 A 3241 423791 CONTROL BOX LEAR 60 60LEAR 5170707 CE ANTI-SKID SYS INOPERATIVE E DELA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 03 188TG 078 PIC REPORTED UNCOMMANDED LT TURN WHILE ON TAXIWAY TO RAMP WITH NOSE WHEEL STEERING FOUND KICKED OFF. NOSE WHEEL STEERIN G DID NOT ENGAGE WITH MSW. AIRCRAFT NOSE WHEEL VEERED OFF THE EDGE OF THE TAXIWAY. FOUND NORMAL BRAKING WAS INOPERATIV E. USED EMERGENCY AIR BRAKING TO STOP AIRCRAFT. REMOVED, REPAIRED, BENCH CHECKED AND REPLACED ANTI-SKID CONTROL BOX. 2 L 7 2 4F RT A10CE 2007061400229 20070614 00229 CE 2007 6 14 DJFA2007055 1 20070516 A 2163 11509761 SENSOR BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE CABIN TEMP FAILED E DJFA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 23 755TA 5029 RK324 TRIP NR 1180704 AT FL 070 IN LEVEL FLIGHT DURING INITIAL CLIMB OUT CREW REPORT A BURNING ODOR COMING FROM THE OVERHEAD V ENTS. FLOOR VENTS WERE EMINATING HOT AIR WITH SYSTEM IN MANUAL MODE SET TO FULL COLD. CABIN PRESSURE WAS FLUCTUATING + - 500 FT. CREW RETURNED TO KPBI. MAINTENANCE REPLACED THE TEMP SENSOR. 2 H 7 2 4F 4 F RT A16SW E25EA 2007061400235 20070614 00235 NE 2007 6 14 GLBA20060951 2 20070521 A 7261 CAP EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE ENGINE OIL SYS DISLODGED A GLBA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 NM 03 71GL 120071 ENGINE SHUTDOWN ON GROUND, PILOTS REPORTED LT ENGINE OIL PRESSURE DROPPED TO 50 PSI FOR A FEW SECONDS AND THE ENGINE WAS SHUTDOWN IMMEDIATELY. MX FOUND THE OIL CAP POPPED OFF. MAINTENANCE CHECKED SECURITY OF THE CAP AND SERVICED ENGINE OIL IAW BMM 12-12-00 AND 12-12-01. SPECIAL INSPECTION CHECKS PERFORMED IAW MFG 5-50 AND 5-10 AND GMM 4.22.0. ENGINE RUNS SUC CESSFUL. 6 QUARTS TOTAL WAS ADDED TO THE ENGINE. 2 L 7 2 4T 4 T RT A31SO E20NE 2007061400241 20070614 00241 CE 2007 6 14 ACE052607 1 20070526 A 2497 P30A6 WIRE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA ELECTRICAL SHORTED E YADA O OTHER O OTHER NR NOT REPORTED 1 AL 03 111AX UC81 PILOT REPORTED (CAN NOT TURN ON BATTERY POWER), LOCATED BLOWN 60 AMP. CURRENT LIMITER CAUSED BY SHORT TO GROUND ON NR 6 GAUGE WIRE (WIRE NR P30A6) AT BLEED AIR DUCT PN. 114-550159-1. REPAIRED WIRE AND DUCT (HOLE IN DUCT), REMOVED 1 FOOT O F EXCESS LENGTH OF WIRE AND INSTALLED WIRE BUNDLE CLAMP STANDOFF AT RT WING LEADING EDGE BRACKET PN 114-120069-1 TO CORR ECT LOW CLEARANCE PROBLEM. 2 L 7 2 4T 4 T RT A24CE E4EA 2007061400242 20070614 00242 CE 2007 6 14 DXTA200702225 1 20070531 A 3220 LANDING GEAR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NOSE VIBRATES E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 901QS 7500102 BAD NOSE WHEEL SHIMMY ON TAKEOFF ROLL. ABORTED TAKE OFF AT 50 KTS. [06-15-07] REPLACED LEFT & RIGHT NOSE WHEEL ASSY. I AW CE 750 MM CH 32-41-01 & 12-20-10 OP'S CHK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007061400244 20070614 00244 NM 2007 6 14 DXTA200702204 1 20070517 A 3230 LANDING GEAR AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 269QS 169 WHEN GEAR HANDLE WAS PUT IN THE DOWN POSITION, NOTHING HAPPENED. (M2B) - PERFORMED FUNCTIONAL TEST OF EXTENSION AND RETR ACTION OF LANDING GEARS AND DOORS, LANDING SAFETIES, AND MAIN DOOR PROX SWITCHES AND GEAR ACTUATOR PROX SWITCHES, AND DO OR UP LOCK AND GEAR UPLOCK. NO DEFECTS NOTED. WORK DONE IN ACCORDANCE WITH F2000 MM 32-300, 31-400, AND 32-605. 2 K 7 2 4F 4 F RT A50NM E44NE 2007061500007 20070615 00007 CE 2007 6 15 DELA200700004 1 20070602 A 3260 1EN18 UPLOCK SWITCH LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP LT MLG MALFUNCTIONED E DELA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 1324P 55098 LT GEAR UNSAFE LIGHT STAYED ON AFTER TAKEOFF. REMOVED AND REPLACED UPLOCK SWITCH. 2 L 7 2 4F 4 F A10CE E6WE 2007061500012 20070615 00012 CE 2007 6 15 DXTA200702239 1 20070603 A 3150 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL UNKNOWN E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 960QS 7500160 IN FLT CLIMBING THROUGH 17,000 FT, GOT AN AMBER (YD FAIL LOWER B) MACH TRIM OFF (CYAN FGC B, AMBER PRI STAB TRIM FAIL) A /P ALSO KICKED OFF. [06-15-07] REMOVED RIGHT HAND PITOT TUBE PN - 6708303-8 AND INSTALLED PN - 6708303-8 PERFORMED LE AK CHECK AND FUNCTION TESTED, TESTED GOOD ALL WORK PERFORMED IAW CITATION 750 MM 34-11-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007061500015 20070615 00015 CE 2007 6 15 DXTA200702243 1 20070605 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 337QS 5600437 CO-PILOTS RT BRAKE PEDAL IS VERY SPONGY. IT REQUIRES (2) TO (3) PUMPS TO PRESSURIZE THE BRAKE. [06-15-07] BLED LT & RT BRAKE SYSTEMS MULTIPLE TIMES, WITH AND WITHOUT ACCUMULATOR PUMP. SERVICED BRAKE RESERVOIR AS REQUIRED. TAXIED AIRC RAFT AND VERIFIED BRAKE SYSTEM WORKED PROPERLY IAW MODEL 560 MM 32-42-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2007061500027 20070615 00027 EU 2007 6 15 07FDEA01811 1 20070515 A 5310 A53974268 CROSSBEAM AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 CROSSBEAM C58 CORRODED REPAIR PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 2007061500037 20070615 00037 EA 2007 6 15 TRAX200700791 1 20070604 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 319 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 975EV 7599 ASD THRESHOLD, FLOOR PANEL SUPPORT AT FS 319.7 IS CORRODED. 2 L 7 2 4F RT A21EA 2007061500053 20070615 00053 WP 2007 6 15 DHL2007803520 1 20070603 A 5720 565122113 CHANNEL DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 LT WING LWR FAIRING ZEE CHANNEL CRACKED 0.750" STA XW -3.125. REMOVED ZEE CHANNEL IAW SRM 51-1-21. CLEANED, TREATED AN D PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL IAW SRM 51-1-21. REFER TO JC EC-00361-001 (WO 1028) FOR ZEE FABRI CATION. 2 L 7 4 4F RT 4A25 2007061500058 20070615 00058 WP 2007 6 15 DHL2007803527 1 20070603 A 5740 56449722 FITTING DOUG DC8 DC873 302199C WP NR 4 TANK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 NR 4 ALT TANK INTERIOR FITTING CRACKED 1" STA XW 408.000 S-58 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW JC EC-00363-00 1, DOUGLAS DWG NR 5644972. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING P/N 5644972-2SP IAW SRM 51-1-23, SRM 51-1-20D, SRM 51-3-1 (TORQUE). REFER TO J C EC-00363-001 FOR FITTING FABRICATION (WO 1028). 2 L 7 4 4F RT 4A25 2007061500060 20070615 00060 WP 2007 6 15 DHL2007807524 1 20070603 A 5710 VANE DOUG DC8 DC873 302199C WP RT WING UNKNOWN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 RT OUTBD VANE SLOT HAS AN INTERIM REPAIR AT SOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE D 06-01-07, DWG NR AD42-57-101 REV IR DATED 05-16-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTION AND FABRICATED EXTERNAL REPAIR DOUBLER (AL7075T6 0.071") INTERNAL DOUBLER (AL7075T6 0.063") AND FIL LER (AL7075T6 0.063") IAW DWG AD42-57-101. CLEANED, TREATED AND PRIMED AREA, FILLER, INTERNAL DOUBLER AND INNER FACE OF EXT REPAIR DOUBLER IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DWG AD42-57-101, SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D , SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007061500064 20070615 00064 NM 2007 6 15 DHL2007783503 1 20070602 A 5347 BAC1520841 SEAT TRACK BOEING 727 727227 1384078 NM BS 757-852 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 CABIN SEAT TRACK CORRODED BETWEEN BS 760 TO BS 825, RBL 45. REMOVED SEAT TRACK SECTION BS 757.45 TO BS 852.45, RBL 45 IAW B727 SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK P/N BAC1520-841 IAW B727 SRM 51-30-5 AND 53-10-2, FIG 7. PART AND AREA TREATED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 51-10-2, 51-30-2 AND 53-10-2, FIG 7. 2 L 7 3 4F A3WE 2007061500070 20070615 00070 SO 2007 6 15 SIMA200716302 1 20070611 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 648AE 145225 STRONG BURNING ODOR IN CABIN. PERFORMED ENGINGE RUNS SWITCHING BLEED SOURCE FROM APU TO ENGINES SEVERAL TIMES WITH NO B URNING ODOR NOTED. WORK ACCOMPLISHED IAW ROLLS ROYCE MM 72-00-00. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061500073 20070615 00073 NM 2007 6 15 DHL2007783523 1 20070531 A 7160 NOSE COWL BOEING 727 727227 1384078 NM NR 1 ENGINE GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 NR 1 ENG NOSE COWL 4 O`CLOCK POS EXISTING REPAIR DOUBLER AN ADJACENT SKIN GOUGED AT NAC STA 82.5. REMOVED DAMAGED DOUBL ER ON NR 1 ENGINE NOSE COWL 9 O`CLOCK POSITION IAW B7627 SRM 51-30-2. REMOVED DAMAGED SKIN ADJACENT TO DOUBLER AREA ON NR 1 ENG NOSE COWL IAW B727 SRM 51-10-6. FABBED NEW DOUBLER FOR NR 1 ENG NOSE COWL IAW B727 SRM 54-30-03. DOUBLER SIZE 3.95" BY 5.6". ORG CUT OUT AREA 4" BY 5.75". DOUBLER MAT 2024T3 .032" PO NR 9004384. ORG MAT ID REFERENCE B727 SRM 5 4-30-02 FIG1 SHT. 2. INSTALLED NEW DOUBLER ON NR 1 ENGINE NOSE COWL 9 O`CLOCK POSITION IAW B727 SRM 51-30-02. 2 L 7 3 4F A3WE 2007061500099 20070615 00099 NM 2007 6 15 07FDEA02120 1 20070613 A 5315 6520827225 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 CABIN BS 620, FLOORBEAM UPPER CHORD CORRODED ON UPPER SURFACE, LBL 37 TO LBL 42 REMOVED CORROSION, NDT FOR MATERIAL LOSS , ORIGINAL THICKNESS =.135, REMOVED .013". FLAP PEENED BLENDED AREA. TREATED AND PRIMED AND APPLIED CORROSION INHIBIT OR. REF SRM 51-10-2, MM 51-20-151, SOPM 20-10-3 AND EA NR 7-5310-113045. 2 L 7 3 4F RT A3WE 2007061500101 20070615 00101 SO 2007 6 15 FDKA200705200 1 20070511 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FDM 6006 CAE-ATL (0522 PHX LCL) - LT OVERWING EMERGENCY LIGHT INOP. MX RESET SYSTEM OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2007061500115 20070615 00115 NM 2007 6 15 KCSA071187 1 20070607 A 5311 FRAME BOEING 747 747221F 1384868 NM BS 2598 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 FUSELAGE FRAME AFT CHORD IS CORRODED AT STA 2598, STR 8L. 2 L 7 4 4F A20WE 2007061500118 20070615 00118 NM 2007 6 15 UPS07M49896 1 20070404 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 36 RT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38. BOT TOM REMAIN BLENDOUT 0.070" DEEP REMAIN THK 0.326" SIDEWALL REAMED TO 2.538" DIA REMAIN BLENDOUT 0.040" DEEP EXCEED EO LI MIT. 10X MAG DVI C/O NO CORROSION. BORE BLENDOUT & BOTTOM PERI RADIUS, SMOOTHEN & PROTECTED SRM 51-21-01 VII R38. REP AIR SLEEVE BUSHING, DOUBLER & FILLERS FAB & INSTALLED PER EO FIG 5 & 6. REPAIR C/O IAW EN1187-07. 2 L 7 3 4F RT A22WE 2007061500119 20070615 00119 NM 2007 6 15 UPS07M49897 1 20070409 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORT STAB, BARREL NUT BORE RIGHT NR 26 FOUND CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38. BOTT OM SURF CLEANED, BORE REAMED TO 1.067" DIA REMAIN BLENDOUT 0.025" DEEP EXCEED EO LIMITS. 10X MAG DVI C/O NO CORROSION. BORE BLENDOUT & BOTTOM PERI RADIUSED, SMOOTHEN & PROTECTED SRM 51-21-01VII R38. REPAIR SLEEVE BUSHING FAB, PROTECTED & INSTALLED PER EO FIG 5. REPAIR C/O AT BARREL NUT BORE NR 26 RIGHT IS ACCEPTABLE IAW EN1205-07. 2 L 7 3 4F RT A22WE 2007061500126 20070615 00126 NM 2007 6 15 UPS07M49904 1 20070305 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 21 LEFT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38. B OTTOM SURF CLEANED. BORE REAMED TO 1.067 "DIA. REMAIN BLENDOUT 0.020" DEEP EXCEED EO LIMITS. 10X MAG DVI C/O NO CORRO SION. BORE REAMED FURTHER TO 1.121" DIA EN1199-07. BLENDOUT & BOTTOM PERI RADIUSED, SMOOTHEN & PROTECTED SRM 51-21-01 VOLII R38. REPAIR SLEEVE BUSHING FAB & INSTALLED EO FIG 5. REPAIR C/O AT BORE NR 21 LEFT IAW EN1199-07. 2 L 7 3 4F RT A22WE 2007061500130 20070615 00130 NM 2007 6 15 UPS07M49908 1 20070416 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 29 LEFT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38. B OTTOM - REMAIN BLENDOUT 0.064" DEEP BORE REAMED TO 1.178" DIA REMAIN BLENDOUT 0.044" DEEP EXCEED EO LIMITS. 10X MAG DVI C/O NO CORROSION. BORE BLEND OUT & BOTTOM PERI RADIUSED, SMOOTHEN & PROTECTED SRM 51-21-01 VII R38. REPAIR SLEEVE BUS HING FAB, PROTECTED & INSTALLED PER EO FIG 5. REPAIR C/O AT BN BORE NR 29 LEFT IAW EN1233-07. 2 L 7 3 4F RT A22WE 2007061500131 20070615 00131 NM 2007 6 15 UPS07M49909 1 20070412 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE LEFT NR 7 FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38. BO TTOM REMAIN BLENDOUT 0.050" DEEP BORE REAMED TO 0.988" DIA REMAIN BLENDOUT 0.121" DEEP EXCEED EO LIMITS. 10X MAG DVI C/ O NO CORROSION. BORE FURTHER REAMED TO 1.048" DIA EN1220-07. BORE BLENDOUT & BOTTOM PERI RADIUSED, SMOOTHEN & PROTECTE D SRM 51-21-01 VII R38. REPAIR SLEEVE BUSHING FAB & INSTALLED EO FIG 5. BORE NR 7 LEFT REPAIR C/O IAW EN1220-07. 2 L 7 3 4F RT A22WE 2007061500133 20070615 00133 NM 2007 6 15 UPS07M49918 1 20070405 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 27 LEFT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38. B OTTOM REMAIN BLENDOUT 0.100" DEEP BORE REAMED TO 1.178" DIA REMAINING BLENDOUT 0.130" DEEP EXCEED EO LIMITS. 10X MAG DV I C/O NO CORROSION. BORE REAMED FURTHER TO 1.235" DIA EN1200-07. REPAIR SLEEVE BUSHING FAB, PROTECTED & INSTALLED PER EO FIG 5. REPAIR C/O AT BN BORE NR 27 LEFT IS ACCEPTABLE IAW EN1200-07. 2 L 7 3 4F RT A22WE 2007061500134 20070615 00134 NM 2007 6 15 UPS07M49919 1 20070416 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 4 RIGHT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38. B OTTOM SURF CLEANED. BORE REAMED TO 0.988 " DIA REMAIN BLENDOUT 0.060" DEEP EXCEED EO LIMITS. 10X MAG DVI C/O NO CORROS ION. BORE BLENDOUT & BOTTOM PERI RADIUSED, SMOOTHEN & PROTECTED SRM 51-21-01 VII R38. REPAIR SLEEVE BUSHING FAB, PROTE CTED & INSTALLED PER EO FIG 5. REPAIR C/O AT BN BORE NR 4 RIGHT IS ACCEPTABLE IAW EN1231-07. 2 L 7 3 4F RT A22WE 2007061500136 20070615 00136 NM 2007 6 15 UPS07M49921 1 20070416 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 10 RIGHT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38. BOTTOM SURF REMAINING BLENDOUT 0.050" DEEP BORE REAMED TO 0.988" DIA REMAIN BLENDOUT 0.050" DEEP EXCEED EO LIMITS. 10X MAG DVI C/O NO CORROSION. BORE BLENDOUT & BOTTOM PERI RADIUSED, SMOOTHEN & PROTECTED SRM 51-21-01 VII R38. REPAIR SLEE VE BUSHING FAB, PROTECTED & INSTALLED PER EO FIG 5. REPAIR C/O AT BN BORE NR 10 RIGHT IAW EN1232-07. 2 L 7 3 4F RT A22WE 2007061500138 20070615 00138 2007 6 15 P5CA0701524 2 20070604 A 7200 ENGINE BOEING 747 74746NF 13848BT NM NR 1 INOPERATIVE A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 450PA 30808 RETURN TO GATE, NR 1 ENGINE AUTO START EICAS MESSAGE NR 1 ENGINE FAILED TO START, IN AUTO OR MANUAL. UNSUCCESSFUL ENGIN E START. PERFORMED VISUAL INSPECTION OF ALL LINES FOR LEAKS, ALL CHECKS NORMAL IAW MM 36-11-00. PERFORMED MANUAL START BY THE CREW. ENGINE STARTED NORMAL IAW MM 80-13-00. 2 L 7 4 4F RT A20WE 2007061500139 20070615 00139 GL 2007 6 15 P5CA0701525 2 20070604 A 7310 LINE BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL NR 2 ENGINE LEAKING A P5CA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 15 452PA 30810 706122 DURING WALK AROUND, CONTINUOUS FUEL DRIP WAS FOUND COMING OUT OF NR 2 ENGINE FUEL DRAIN. CHECKED AND FOUND NAC 298 STAT ION 93 PYLON AREA FUEL LINE LEAKING. RETIGHTENED LINE AND PERFORMED GROUND ENGINE RUN-UP CHECK. ALL CHECKS OK PER MM 7 3-11-06 AND 71-00-00. 2 L 7 4 4F 4 F RT A20WE E23EA 2007061500140 20070615 00140 SO 2007 6 15 C2XA07ON005 1 20070607 A 3350 LIGHT EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14188 0929 SCHEDULE MX - 3A CHECK - ONT - RWD 724858 - DURING A/C PRELIM INSPECTION QC INSPECTOR FOUND EMERGENCY LIGHTS ON EXIT SIG NS AROUND SERVICE DOOR NOT OPERATING PROPERLY. MX PERSONAL PERFORMED GROUND FUNCIONAL CHECK OF SERVICE DOOR EMERGENCY L IGHT GOOD. A/C WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2007061500142 20070615 00142 NM 2007 6 15 HNAA0700112 1 20070607 A 3230 574205A SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM MLG MALFUNCTIONED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 825EX 6 388 GEAR FAIL TO EXTEND ON LANDING WHEN SLECTED. FERRY AIRCRAFT TO ROA AND SWAP OUT WITH SPARE AC. REMOVED AND REPLACED LA NDING GEAR SELECTOR VALVE, LEAK AND OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007061500143 20070615 00143 SO 2007 6 15 C2XA07TY027 1 20070608 A 5310 14526246003 DOOR FRAME EMB 145 EMB145EP 3260221 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15941 145035 FRAME 68 CRACKED UNDERNEATH CARGO DOOR -HOLD OPEN- HANDLE RETAINING CUP. CUT OUT AFFECTED FRAME, FABRICATED THE FRAME R EPAIR SEGMENT FROM A SECTION OF A NEW FRAME AND INSTALLED. WORK ACCOMPLISHED IAW EC 5310-01411, EMB 145 SRM 53-00-04 AN D CPM. AIRCRAFT STILL IN C-CHECK. 2 L 7 2 4F RT T00011AT 2007061500144 20070615 00144 SO 2007 6 15 C2XA07TY028 1 20070610 A 5411 RIB EMB 145 EMB145EP 3260221 SO LT NACELLE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15941 145035 LEFT LWR COWL DENTED. REMOVED AND REPLACED DAMAGED RIB IN CENTER SECTION OF COWL, RECON TOURED DENTS AT OIL SERVICE DOO R, FABRICATED AND INSTALLED EXTERNAL DOUBLER, ALODINED, PRIMED AND PAINTED IAW EC 5430-01059. AIRCRAFT STILL IN C-CHECK . 2 L 7 2 4F RT T00011AT 2007061500145 20070615 00145 NM 2007 6 15 KCSA071188 1 20070611 A 5315 FLOORBEAM BOEING 747 747221F 1384868 NM BS 440 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 MAIN DECK FLOORBEAM CORRODED AT BS 440, LBL 59. 2 L 7 4 4F A20WE 2007061500146 20070615 00146 SO 2007 6 15 C2XA07IA129 1 20070607 A 3240 38793500 VALVE EMB 145 EMB145LR 3260212 SO BRAKE ASSY INOPERATIVE A C2XA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 14923 16244 16244 145318 IAH - FLIGHT 2217, DURING TAXI THE CREW REPORTED SEVERAL OUTBOARD BRAKE INOP MESSAGES ON EICAS. THE AIRCRAFT RETURNED T O THE GATE WHERE MAINTENANCE REMOVED AND REPLACED THE OUTBOARD BRAKE SHUT OFF VALVE, OPERATIONALLY CHECKED WITH NO DEFEC TS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061500147 20070615 00147 SO 2007 6 15 C2XA07IA132 1 20070607 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO CABIN ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 34111 145659 IAH - FLIGHT 2100, THE CREW REPORTED A STRONG ODOR OF FUEL JUST AFTER APU START. MAINTENANCE OPERATIONALLY CHECKED THE APU & PACKS SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007061500149 20070615 00149 SO 2007 6 15 C2XA07IA134 1 20070606 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14991 145278 IAH - FLIGHT 2628, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN AT SEAT 12A WAS INOP. MA INTENANCE INSPECTED THE SIGN, SECURED A LOOSE CONNECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APP ROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061500151 20070615 00151 NM 2007 6 15 UPS07M49927 1 20070412 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE LEFT NR 31 FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38 BOT TOM REMAIN BLENDOUT 0.032" DEEP BORE REAMED TO 1.178" DIA - REMAIN BLENDOUT 0.059" DEEP FOUND EXCEED EO LIMITS. 10 X MA G DVI C/O NO CORROSION. BORE BLENDOUT & BOTTOM PERI RADIUSED, SMOOTHEN & PROTECTED SRM 51-21-01 VII R38. REPAIR SLEEVE BUSHING FAB, PROTECTED & INSTALLED PER EO FIG 5. REPAIR C/O AT BN BORE NR 31 LT IAW EN1229-07. 2 L 7 3 4F RT A22WE 2007061500152 20070615 00152 NM 2007 6 15 UPS07M49928 1 20070409 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZTONAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORT STAB, BARREL NUT BORE LEFT NR 14 FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01VII R38 BOT TOM REMAIN BLENDOUT 0.040" DEEP BORE REAMED TO 0.988" DIA REMAIN BLENDOUT 0.015" DEEP EXCEED EO LIMITS. 10X MAG DVI C/O NO CORROSION. BORE BLENDOUT & BOTTOM PERI RADIUSED, SMOOTHEN & PROTECTED SRM 51-21-01 VII R38. REPAIR SLEEVE BUSHING FAB, PROTECTED & INSTALLED PER EO FIG 5. REPAIR C/O AT BN BORE NR 14 LT IS ACCEPTABLE IAW EN1214-07. 2 L 7 3 4F RT A22WE 2007061500153 20070615 00153 NM 2007 6 15 UPS07M49929 1 20070419 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 34 LT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38 BOTTO M-REMAIN BLENDOUT 0.070" DEEP BORE REAMED TO 1.178" DIA REMAIN BLENDOUT 0.130" DEEP EXCEED EO LIMITS. 10X MAG DVI C/O N O CORROSION. BORE REAMED FURTHER TO 1.219" DIA EN1247-07. BORE BLENDOUT & BOTTOM PERI RADIUSED, SMOOTHEN & PROTECT SRM 51-21-01 VII R38. REPAIR SLEEVE BUSH FAB & INSTALLED EO FIG 5. REPAIR C/O AT NR 34 LT IAW EN1247-07. 2 L 7 3 4F RT A22WE 2007061500158 20070615 00158 NM 2007 6 15 UPS07M49934 1 20070405 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 18 LEFT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38 BOT TOM - REMAIN BLENDOUT 0.030" DEEP BORE REAMED TO 1.067" DIA REMAIN BLENDOUT 0.050" DEEP EXCEED EO LIMITS. 10X MAG DVI C/ O NO CORROSION. REAM BORE FURTHER TO 1.121" DIA EN1198-07. BORE BOTTOM, BLENDOUT, PERI RADIUSED, SMOOTHEN & PROTECTED. REPAIR SLEEVE BUSHING FAB & INSTALLED EO FIG 5. REPAIR C/O AT BORE NR 18LT ACCEPTABLE IAW EN1198-07. 2 L 7 3 4F RT A22WE 2007061500159 20070615 00159 NM 2007 6 15 UPS07M49938 1 20070608 A 2910 AYK7550812 LINE DOUG MD11 MD11F 3023600 NM HYD SYSTEM LEAKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 284UP 48541 INSPECTION TYPE:N/A EMERGENCY DECLARED - LOSS OF NR 2 HYD QTY. FOUND HYD PRESS LINE THAT RUNS TO NR 2 HYD MULE CONNECTI ON LEAKING. INSTALLED FLEX LINE, LEAK CHECK OK REF MD11 MM 20-10-01-2. 2 L 7 3 4F RT A22WE 2007061500161 20070615 00161 EU 2007 6 15 PG9A115814 1 20070525 A 6220 704A33640088 FREQ ADAPTER UROCOP EC130 EC130B4 8680989 EU MAIN ROTOR CRACKED B PG9A K NONE O OTHER IN INSP/MAINT 1 SW 03 136PH 2440 3896 DURING THE DAILY INSPECTION, FOUND A VERTICLE CRACK EXTENDING UP FROM THE LOWER HOLE ON THE AFT SIDE OF THE ADAPTER. IN STALLED 3 SERVICEABLE ADAPTERS. 1 G 7 2 3U H9EU 2007061500165 20070615 00165 EU 2007 6 15 PG9A115818 1 20070508 A 6700 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU COLLECTIVE PITCH MALFUNCTIONED B PG9A O OTHER J WARNING INDICATION LD LANDING 1 WP 19 133GC 124 3883 FAIL CODE 122 DISPLAYED ON VEMD AFTER FLIGHT. REPLACED COLLECTIVE PITCH POTENTIOMETER. 1 G 7 2 3U H9EU 2007061500167 20070615 00167 NM 2007 6 15 CALA0700297 1 20070608 A 5311 6546549 FRAME BOEING 737 7373T0 1384582 NM BS 767 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12313 23364 INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 767 BETWEEN STRINGERS 8R AND 9R. THE FRAME WAS REPAIRED IAW E CRA 5310-04637. 2 L 7 2 4F RT A16WE 2007061500170 20070615 00170 EU 2007 6 15 HEEA115422 1 20070504 A 6200 CONNECTOR UROCOP EC135 EC135P2 5620027 EU ACTUATOR CORRODED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 326PH 2064 00166 0435 CONNECTOR CORRODED. SENT TO MFG FOR CREDIT. 1 G 7 2 3U H88EU 2007061500178 20070615 00178 NM 2007 6 15 DXTA200702207 1 20070520 A 2700 UNKNOWN GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE UNKNOWN E DXTA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 07 725QS 105 AIRCRAFT WOULD NOT ROTATE WITH STICK FULL AFT. (M2B) PERFORMED HIGH ENERGY STOP INSPECTION REF MM 5-50-01, NO DEFECTS NO TED. MEASURED ELEVATOR UP AND DOWN TRAVEL, TRAVEL NORMAL. ELEVATORS MOVED WITH EASE. PERFORMED ELEVATOR CONTROL SYSTEM T RAVEL TEST AND FOUND BOTH ELEVATORS TO BE IN SYNCH, AND CORRECT UP TRAVEL 27.5 DEGREES DOWN TRAVEL 20 DEGREES. CHECKED E LEVATOR CABLE TENSIONS, OK IAW MM CMP 315101. NO DEFECTS NOTED. PERFORMED OPS CHECKS OF NR 1 AND NR 2 FMS GDAS C/W, NO D EFECTS NOTED. PERFORMED AIR DATA COMPUTER CHECK, NO DEFECTS NOTED. PERFORMED AIRCRAFT WEIGHT AND BALANCE CHECK BY FLIGHT PATH, NEW REPORT IN LOG BOOK. PERFORMED ENGINE PERFORMANCE CHECK, NO DEFECTS NOTED. REMOVED CVR P/N - 1603-02-12 S/N OF 2 L 7 2 4F 4 F RT A53NM E35NE 2007061500181 20070615 00181 CE 2007 6 15 DXTA200702235 1 20070601 A 3411 PITOT TUBE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CONTAMINATED E DXTA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 07 958QS 7500158 ON TAKEOFF AT 40-50 KNOTS FG B FAIL CAME ON WITH AMBER (YAW DAMP FAIL) AND MACH TRIM OFF). FOUND EXCESSIVE WATER IN THE COPILOTS PITOT TUBE. PURGED SYSTEM AND PERFORMED OPERATIONAL CHECK AND LEAK CHECK IAW CHP 34-11-08 OF MM. SYSTEM OPER ATIONAL CHECK AND LEAK CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007061500183 20070615 00183 CE 2007 6 15 DXTA200702236 1 20070601 A 3240 NAS161216 O-RING CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE BRAKE ASSY LEAKING E DXTA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 806QS 5600614 TAXING FOR DEPARTURE, ANTISKID LIGHT ILLUMINATED RETURNING., THE LOW BRAKE PRESS LITE ILLUMINATED, WE USED THE EMERGENCY BRAKES FOR PARKING. FOUND BRAKE PUMP FILTER HOUSING LEAKING REPLACED HOUSING (BOWL) WITH NEW O-RING AND HOUSING BLEED S YSTEM SERVICED EMERGENCY BRAKE SYSTEM TO FULL. TAXI AIRCRAFT OPS, LEAK CHECKS GOOD ALL WORK IAW MM CH 32-42-00. 2 L 7 2 4F 4 F RT A22CE E00053EN 2007061500185 20070615 00185 NE 2007 6 15 DXTA200702237 2 20070602 A 7200 31J190001 ENGINE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE NR 2 VIBRATION E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 612QS 4524 5605312 DURING TAKEOFF, THE NR 2 ENGINE HAD A HIGH PITCHED WHINE ACCOMPANIED BY A RT VIBE ADVISORY LIGHT, 101.1 PERCENT N2, AND AN OIL PRESSURE SPLIT OF APPROXIMATELY 30-35 PSI. T/O ABORTED. REMOVED NR 2 ENGINE AND INSTALLED SERVICEABLE UNIT. ALL O PS AND LEAK CHECKS GOOD. IAW MM 71-00-03. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007061500186 20070615 00186 CE 2007 6 15 DXTA200702238 1 20070603 A 3260 SQUAT SWITCH CESSNA 680 680CE 2076811 CE MLG OUT OF RIG E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 362QS 6800051 ON CLIMB OUT WOW MISCOMPARE ANNUN ILLUMINATED. FOUND NOSE GEAR SQUAT SWITCH OUT OF RIG. RIGGED IAW MM 32-60-00. OPS CHE CK GOOD. 2 L 7 2 4F RC T00012WI 2007061500187 20070615 00187 CE 2007 6 15 DXTA200702240 1 20070604 A 2611 47359714 SMOKE DETECTOR RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP CARGO BAY INOPERATIVE E DXTA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 07 833QS 258433 BAG FIRE LIGHT CONSISTANTLY FLASHES IN FLIGHT. NO FIRE NOTED. REMOVED FWD SMOKE DETECTOR AND INSTALLED A REPAIRED DETEC TOR. ALL WORK PERFORMED IAW MM 20-11-00. PERFORMED SELF TEST OF ALL SMOKE DETECTORS. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A3EU E6WE 2007061500203 20070615 00203 EU 2007 6 15 HEEA115520 1 20070516 A 8000 925UN01Q4AA5F SWITCH SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE STARTER INOPERATIVE E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 350LG 3690 AMBER GOV CAUTION LIGHT IN FLIGHT, RED GOV CAUTION LIGHT AFTER SHUTDOWN. MAINTENANCE REPLACED START SWITCH. 1 G 7 1 3U 3 U H9EU E00054EN 2007061500207 20070615 00207 EU 2007 6 15 FJ7A115620 1 20070517 A 6320 350A32106321 GASKET UROCOP EC130 EC130B4 8680989 EU MAIN ROTOR CRACKED E FJ7A K NONE K FLUID LOSS IN INSP/MAINT 1 SO 19 174AM 244 4007 FIBERGLASS GASKET INSTALLED ON BOTH SIDES OF RING GEAR CRACKED AND PUSHED OUT CAUSING AN OIL LEAK. 1 G 7 2 3U H9EU 2007061500209 20070615 00209 2007 6 15 FJ7A115622 2 20070525 A 7261 350A54113800 VENT LINE UROCOP EC130 EC130B4 8680989 EU ENGINE OIL SYS CRACKED E FJ7A K NONE O OTHER IN INSP/MAINT 1 SO 19 174AM 245 4007 CLAMP WELDED TO TUBE CRACKED, LEAVING TUBE UNSUPPORTED. 1 G 7 2 3U H9EU 2007071300163 20070713 00163 SO 2007 7 13 SWIA200718442 1 20070505 A 5711 SHEAR TIE EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 216SW 120285 RIGHT WING IS LEAKING OUTBOARD OF NACELLE, DISCOVERED AT C-CHECK. REPLACED CRACKED SHEAR CLIP AT RIB NR 16 PER EMB SRM 51-40-02. NO LEAKS NOTED. 2 L 7 2 4T RT A31SO 2007061500217 20070615 00217 CE 2007 6 15 052407N322CS 1 20070524 A 3260 MS25237327 BULB CESSNA 500 550 2076604 CE PWA 530 PW530A NE MLG INDICATOR INOPERATIVE E Z5FA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 63 322CS 5501052 DURING APPROACH WHEN GEAR WAS EXTENDED, THE LT MLG DOWN ANNUNCIATION FAILED TO ILLUMINATE. ABORTED APPROACH AND INITIAT ED AFM CHECKLIST PROCEDURES. COMPLIED WITH EMERGENCY EXTENSION ACTION BY BLOWING GEAR DOWN AND DECLARING EMERGENCY. AIRC RAFT LANDED WITHOUT INCIDENT. ON SITE MAINTENANCE PERSONNEL FOUND CONDITION CAUSED BY BLOWN BULB IN LT GEAR DOWN ANNUCIA TOR LIGHT ASSEMBLY. REPLACED BULB, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 4F 4 F A22CE E00053EN 2007061800001 20070618 00001 NM 2007 6 18 07FDEA02133 1 20070614 A 5753 652163586 SKIN BOEING 727 727233 138408A NM TE FLAPS MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 286FE 22623 AGING A/C INSP, FOUND EXISTING REPAIR DID NOT CONFORM TO CURRENT SRM 51-40-20, AT RT WING OB AFT FLAP T/E 8" TO 22" FROM OB END. REMOVED PREVIOUS REPAIR AND REPAIRED AFT FLAP REF SRM 51-40-20 PAR 7, 14, 15, 18, 21, 22. PRIMED AND PAINTED REPAIR REF MM 51-20151-7. 2 L 7 3 4F RT A3WE 2007061800004 20070618 00004 EA 2007 6 18 QXEA200700918 1 20070529 A 5753 PANEL CNDAIR CL600 CL6002C10 1390015 EA TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC - RIGHT FLAP PANEL 684JB CHAFED. REPAIRED IAW SRM 51-12-00 AND 51-21-11. 2 L 7 2 4F RT A21EA 2007061800005 20070618 00005 EA 2007 6 18 QXEA200700919 1 20070529 A 5753 PANEL CNDAIR CL600 CL6002C10 1390015 EA TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC - RIGHT FLAP PANEL 684GB CHAFED. REPAIRED IAW SRM 51-12-00 AND 51-21-11. 2 L 7 2 4F RT A21EA 2007061800006 20070618 00006 EA 2007 6 18 QXEA200700920 1 20070530 A 5753 PANEL CNDAIR CL600 CL6002C10 1390015 EA TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC - LEFT FLAP PANEL 584EB CHAFED. REPAIRED IAW SRM 51-12-00 AND 51-21-11. 2 L 7 2 4F RT A21EA 2007061800007 20070618 00007 EA 2007 6 18 QXEA200700921 1 20070530 A 5753 PANEL CNDAIR CL600 CL6002C10 1390015 EA TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC - LEFT FLAP PANEL 584AB CHAFED ON LEADING EDGE. REPAIRED IAW SRM 51-12-00 AND 51-21-11. 2 L 7 2 4F RT A21EA 2007061800008 20070618 00008 EA 2007 6 18 QXEA200700915 1 20070529 A 5753 PANEL CNDAIR CL600 CL6002C10 1390015 EA TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 CI OKC - FLAP PANEL 684HT UPPER LEADING EDGE DAMAGED. REPAIRED IAW SRM 51-12-00, 51-21-11. 2 L 7 2 4F RT A21EA 2007061800010 20070618 00010 EA 2007 6 18 QXEA200700923 1 20070602 A 5330 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA UNKNOWN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC - REFEREMCE ITEM 16 DAMAGE NR 7 PER E/C R-53-455/3. REPAIRED IAW REO670-52-45-014. 2 L 7 2 4F RT A21EA 2007061800012 20070618 00012 NM 2007 6 18 DU4R2007136 1 20070613 A 5330 SKIN BOEING 757 757232 1384965 NM BS 1685 DENTED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 640DL 23994 FOUND DENT AT BS 1685 FROM S-16R TO S-14R ACROSS S-15R. REPAIRED BY CUTTING OUT DENTED AREA, HFEC CUT OUT PER B757 TM P T. 6-51-00-19, NO RELEVANT INDICATIONS NOTED. FABRICATED AND INSTALLED REPAIR DOUBLER 16-1/4 BY 15-1/40 BY 15-3/4" FROM 2024-T3 .080 AND FILLER FROM 2024-T3 .071 IAW DELTA ERA 461665-14 DATED 06-13-07 APPROVED PER FAA FORM 8100-9 (2 PAGES) BOEING. REPAIR APPROVAL IS LIMITED TO 12 MONTHS SERVICE ONLY. ADDITIONAL ENGINEERING AUTHORIZATION, (ERR/A REVISION) IS REQUIRED FOR CONTINUED SERVICE OF THIS REPAIR LONGER THAN 12 MONTHS FROM FAA FORM 8100-9 DATED (JUNE 8, 2007). 2 L 7 2 4F RT A2NM 2007061800013 20070618 00013 NM 2007 6 18 DU4R2007137 1 20070607 A 3230 162N22011 DRAG LINK BOEING 757 757232 1384965 NM NLG CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 640DL 23994 FOUND CORRODED NLG LOWER DRAG LINK. REPAIRED BY REMOVING AND REPLACING P/N 162N2201-1 IAW B757 AMM 32-24-04. 2 L 7 2 4F RT A2NM 2007061800014 20070618 00014 NM 2007 6 18 DU4R2007138 1 20070525 A 3210 S113N1035 BEARING BOEING 757 757232 1384965 NM LT MLG CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 640DL 23994 FOUND OUTER HOUSING OF LT MLG AFT TRUNNION CORRODED. REPAIRED BY REMOVING AND REPLACING WITH P/N S113N103-5 IAW B757 MM 57-54-07. 2 L 7 2 4F RT A2NM 2007061800016 20070618 00016 NM 2007 6 18 DU4R2007140 1 20070524 A 3210 S113N1035 BEARING BOEING 757 757232 1384965 NM RT MLG CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 640DL 23994 FOUND RIGHT MLG AFT TRUNNION BEARING HOUSING CORRODED AT RACE AND AFT TANG FWD OF THREADS. REPAIRED BY REMOVING AND REP LACING BEARING P/N S113N103-5 IAW B757 MM 57-54-07. 2 L 7 2 4F RT A2NM 2007061800017 20070618 00017 WP 2007 6 18 ARWA20070606 1 20070613 A 3241 40581 TRANSDUCER DOUG DC8 DC863F 302198F WP ANTI SKID SYS INOPERATIVE A ARWA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 441J 45988 PRIOR TO TAKEOFF ANTI-SKID INOPERATIVE LIGHT REMAINED ILLUMINATED; RETURN TO BLOCK. REMOVED AND REPLACED NR 8 MAIN LAND ING GEAR WHEEL SPEED TRANSDUCER IN ACCORDANCE WITH M/M 32-43-02; GROUND TEST NORMAL IN ACCORDANCE WITH M/M 32-43-00. 2 L 7 4 4F 4A25 2007061800021 20070618 00021 NM 2007 6 18 AALA20070971 1 20070528 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT WRONG PART A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 907AN 29509 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR OVERHEAD EXIT SIGN HAS WRONG LENS. REPLACED LENS FOR EMERGENCY LIGHT AT L EFT NUMBER ONE DOOR OVERHEAD EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007061800022 20070618 00022 NM 2007 6 18 AALA20070972 1 20070528 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT WRONG PART A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 907AN 29509 DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR OVERHEAD EXIT SIGN HAS WRONG LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR OVERHEAD EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007061800023 20070618 00023 NM 2007 6 18 AALA20070973 1 20070528 A 3350 LENS BOEING 737 737924 13848A1 NM EMERGENCY LIGHT WRONG PART A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 907AN 29509 DFW - EMERGENCY LIGHT AT LEFT AFT DOOR OVERHEAD EXIT SIGN HAS WRONG LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LEFT AFT DOOR OVERHEAD EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007061800024 20070618 00024 NM 2007 6 18 AALA20070974 1 20070528 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT WRONG PART A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 907AN 29509 DFW - EMERGENCY LIGHT AT RIGHT AFT DOOR OVERHEAD EXIT SIGN HAS WRONG LENS. REPLACED LENS FOR EMRGENCY LIGHT AT RIGHT AF T DOOR OVERHEAD EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007061800027 20070618 00027 NM 2007 6 18 AALA20070976 1 20070528 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 907AN 29509 DFW - EMERGENCY LIGHT AT LEFT AISLE BULL NOSE AT ROW 10 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LEFT AISLE B ULL NOSE AT ROW 10. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007061800028 20070618 00028 NM 2007 6 18 AALA20070997 1 20070525 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 977AN 29550 TUL - EMERGENCY LIGHTS AT OVERWING DOORS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERWING DOORS. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007061800030 20070618 00030 NM 2007 6 18 AALA20070978 1 20070528 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 907AN 29509 DFW - AFT SEAT MOUNTED EMERGENCY LIGHT AT SEAT 14D MISSING LENS. REPLACED CLEAR LENS FOR AFT SEAT MOUNTED EMERGENCY LIG HT AT SEAT 14D. 2 L 7 2 4F RT A16WE 2007061800031 20070618 00031 WP 2007 6 18 AALA20070979 1 20070529 A 3397 WIRE HARNESS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 967TW 53617 SEA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. SECURED LOOSE WIRE FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007061800035 20070618 00035 EA 2007 6 18 QXEA200700932 1 20070531 A 5100 NONE CNDAIR CL600 CL6002C10 1390015 EA NONE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC - COMPLIED WITH NR 6 DAMAGE NR 7. REPAIRED IAW REO670-53-00-123. 2 L 7 2 4F RT A21EA 2007061800036 20070618 00036 EA 2007 6 18 QXEA200700933 1 20070531 A 5100 NONE CNDAIR CL600 CL6002C10 1390015 EA NONE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC - COMPLIED WITH NR 5 DAMAGE NR 6. REPAIRED IAW REO670-53-00-123. 2 L 7 2 4F RT A21EA 2007061800038 20070618 00038 EA 2007 6 18 QXEA200700935 1 20070531 A 5100 NONE CNDAIR CL600 CL6002C10 1390015 EA NONE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC - COMPLIED WITH NR 3 DAMAGE NR 4. REPAIRED IAW REO670-53-00-123. 2 L 7 2 4F RT A21EA 2007061800039 20070618 00039 EA 2007 6 18 QXEA200700936 1 20070531 A 5100 NONE CNDAIR CL600 CL6002C10 1390015 EA NONE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC - COMPLIED WITH NR 2 DAMAGE NR 1. REPAIRED IAW SRM 51-42-10, 51-12-00, 51-42-06. 2 L 7 2 4F RT A21EA 2007061800040 20070618 00040 EA 2007 6 18 QXEA200700937 1 20070527 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC - FOUND LEFT FS 280.00 FRAME CRACKED AT LBL9. REPAIRED IAW REO670-53-11-047 AND SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007061800041 20070618 00041 EA 2007 6 18 QXEA200700938 1 20070527 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC - RIGHT FS 280.00 FRAME CRACKED AT RBL9. REPAIRED IAW REO670-53-11-047 AND SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007061800043 20070618 00043 NM 2007 6 18 QXEA200700939 1 20070608 A 6123 SWITCH DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS FAILED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 347PH 480 PDX FLIGHT NR 2170 AUTO FEATHER SYSTEM WILL NOT TEST, FOUND 6121-S9 BAD. REPLACED SWITCH IAW DASH 8-200 WDW 61-21-01, S HEET 2 OF 6. PERFORMED AUTO FEATHER SYSTEM AND POWER UPTRIM TEST IAW DASH 8-200 ENGINE RIGGING MANUAL PARAGRAPH 6-8. T ESTS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061800044 20070618 00044 NM 2007 6 18 07FDEA02113 1 20070613 A 5343 AEA7051501 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 576FE 48501 CENTER LANDING GEAR LEFT TRUNNION FITTING AFT HOLE FOUND CORROSION. CENTER LANDING GEAR LEFT TRUNNION FITTING AFT HOLE REAMED TO DIAMETER = 1.385" AND REPAIRED AS PER FEDEX EA NR 1-5310-111115, TITLE: FUSELAGE, CENTER LANDING GEAR LEFT TRU NNION FITTING CORROSION REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007061800045 20070618 00045 EU 2007 6 18 CPCP20070038 1 20070425 A 5711 FRAME AEROSP ATR72 ATR72212 8680945 EU RT WING CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 448AM 448 AILERON CONTROL QUADRANT CORRODED RT FRAME 27 AND 28 WING RIB 1 AND 2. REPLACED QUADRANT ASSY ON AUTO-PILOT ROLL CONTRO L SYSTEM IAW AMM JIC 27-11-23 RAI 10000. 2 H 7 2 4T RT A53EU 2007061800046 20070618 00046 EU 2007 6 18 CPCP20070040 1 20070425 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 448AM 448 CORROSION FOUND ON LT I/B SEAT TRACK AT FRAME 17. SEAT TRACK LT I/B ON FRAME 13 - 23 REPLACED IAW SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007061800047 20070618 00047 EU 2007 6 18 CPCP20070039 1 20070425 A 5310 DOUBLER AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 448AM 448 GUTTER AND DOUBLER ARE CORRODED BETWEEN FRAME 13 AND 17 AT CARGO DOOR. DOUBLER BETWEEN FRAME 13 AND 17 AT CARGO DOOR RE PLACED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007061800048 20070618 00048 EU 2007 6 18 CPCP20070037 1 20070425 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 448AM 448 FOUND LT FRAME 39 TO 41 SEAT TRACK CORRODED. SEAT TRACK LT FRAME 39 - 41 REPLACED AS PER SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007061800049 20070618 00049 EU 2007 6 18 CPCP20070031 1 20070426 A 5330 SKIN AEROSP ATR72 ATR72212 8680945 EU CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 448AM 448 LOCK FASTERNER COLLARS CORRODED UNDERNEATH TOP SKIN O/B OF RIB 24 ACCESS VIA PANEL 624 AB. LOCK FASTERNER COLLARS REPLA CED UNDERNEATH TOP SKIN O/B OF RIB AS PER SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007061800050 20070618 00050 EU 2007 6 18 CPCP20070034 1 20070425 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 448AM 448 FOUND FRAME 39 FLOORBEAM CORRODED. FRAME 39 FLOORBEAM REPAIRED AS PER SRM 53-00-00 FIG 450. 2 H 7 2 4T RT A53EU 2007061400110 20070614 00110 EU 2007 6 14 2007UALA01913 1 20070610 A 3350 SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 489UA 1702 LT OVERWING EMERGENCY LIGHT STAYS ON IN CABIN. [07-03-07] RESET COCKPIT 0N-OFF-ARM SWITCH. EMERGENCY LIGHTS OPS CHECKE D OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061400119 20070614 00119 NM 2007 6 14 2007UALA01923 1 20070611 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BS 590-603 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 199UA 28717 FUSELAGE STATION 590 TO 603 BETWEEN STR 45R AND 46R IS DAMAGED. [07-31-07] FWD FUSELAGE DAMAGE TO BELLY FWD OF FWD C ARGO DOOR OPENING. HAVE DAMAGED AREA CUTOUT, STRINGER REPAIR COMPLETED, WORKING FAB OF FILLER AND DOUBLER. SUSPECT STRI NGER DAMAGE. FABRICATED REPAIR U CHANNEL FOR STR 45R REF SRM 53-00-03 REPAIR 5 DETAIL II, & ACCOMPLISHED INSTALLATION. AIRCRAFT OK FOR RETURN TO SERVICE. DAMAGE CAUSED BY LD3 CONTAINER BLOWN INTO BELLY OF ACFT JUST BELOW FWD CARGO DOOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007061400128 20070614 00128 EA 2007 6 14 SWIA200718327 1 20070525 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7089 FLOORBEAM AT FS 280 AND LBL9.0 IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLE AT FS 280 LBL 9.0 IAW CRJ200 REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 2007061400130 20070614 00130 EA 2007 6 14 SWIA200718329 1 20070525 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7089 CABIN FLOOR SUPPORT STRUCTURE IS CRACKED AT FS 484 AND LBL27, DISCOVERED AT C-CHECK. INSTALLED NEW CLIP AT FS 484 AND L BL27 IAW REO 601R-52-4-059. 2 L 7 2 4F RT A21EA 2007061400138 20070614 00138 NM 2007 6 14 DU4R2007122 1 20070508 A 5330 SKIN BOEING 757 757232 1384965 NM BS 440 DENTED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 602DL 22809 FOUND DENT BELOW STR 17L, BS 440. REPAIRED BY CUTTING OUT DENTED SECTION OF SKIN, HFEC CUT OUT IAW B757 NTM PT6, 51-00- 01, NO RELEVANT INDICATIONS NOTED. FABRICATED AND INSTALLED REPAIR DOUBLER 15-1/4 BY 13-1/2 FROM 2024-T3 .063 IAW B757 SRM 53-00-01 FIG 201, ERA NR 640840-14 REV ORIG FAA APPROVAL FAA FORM 8100-9. REPAIR APPROVAL IS LIMITED TO 12 MONTHS S ERVICE ONLY. ADDITIONAL ENGINEERING AUTHORIZATION, (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE OF THIS REPAIR LON GER THAN 12 MONTHS FROM FAA FORM 8100-9 APPROVAL DATE. 2 L 7 2 4F RT A2NM 2007061400139 20070614 00139 EU 2007 6 14 COEA0709903 1 20070109 A 5312 BULKHEAD AEROSP ATR42 ATR42320 8680930 EU RT MLG WW CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 903FX 179 CORROSION LEVEL 2, DURING HEAVY CHECK, FOUND CORROSION AT FRAME 27, RIGHT WHEEL WELL REAR SPAR BULKHEAD, BOTTOM SURFACE OF LOWER FLANGE FROM BL 0 TO BL 4R. BLENDED OUT CORROSION AND NO CRACKS NOTED. REPAIRED IAW SRM DO/TS-784/07-8383 WITH REF TO SRAS DO/TS 784.07. 3992 FOR PERMANENT REPAIR EMBODIED. (M) 2 H 7 2 4T RT A53EU 2007061400151 20070614 00151 SO 2007 6 14 JU82007F00001 1 20070518 A 2823 1908001 SELECTOR VALVE PIPER PA44 PA44180 7104402 SO LYC O360 O360* 41514 EA FUEL SYSTEM DEFECTIVE D JU8S O OTHER O OTHER NR NOT REPORTED 1 GL 25 644KS 7 4496220 FUEL SELECTOR VALVE WAS REPLACED UNDER WARRANTY IN AIRCRAFT. IMMEDIATELY AFTER INSTALLATION, FUEL SELECTOR FOUND TO OPE RATE NORMALLY. UPON THE ACCUMULATION OF 6.8 HRS, TIS, THE FUEL SELECTOR VALVE WAS FOUND TO STICK AT EACH DETENT, IE: C ROSSFEED, OFF, AND NORMAL POSITION. THE STICKING WAS SO SEVERE, THAT EVEN THE FORCE OF (2) HANDS ON THE SELECTOR VALVE WOULD NOT MOVE THE VALVE OUT OF THE DETENT POSITION. CAUSE OF PROBLEM IS UNKNOWN, HOWEVER, THIS POSES A SAFETY OF FLIG HT ISSUE DUE TO THE FACT THAT THE VALVE AT TIMES WOULD NOT MOVE OUT OF THE DETENT POSITION. THIS COULD RESULT IN THE AC OPERATING WITH ONE ENGINE ONLY. FUEL SELECTOR CABLE WAS INSPECTED FOR DEFECTS, HOWEVER, INTERNALLY THE VALVE WAS FOUND 1 L 7 2 3O 3 O A19S0 E286 2007061400166 20070614 00166 NM 2007 6 14 UPS07549866 1 20070427 A 5311 146B102885 FRAME BOEING 757 75724APF 1384969 NM BS 1320 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 404UP 23726 INSPECTION TYPE:C DENTS IN AFT CARGO FUSELAGE FRAME STA 1320 BETWEEN S25L AND S26L (2EA). ACCOMPLISHED BOTH UPPER AND L OWER DENT REPAIRS IAW EA 757-5362-27- A1666 AND UPS EO B757-5310-26894-A WITH NO DEVIATIONS. 2 L 7 2 4F RT A2NM 2007061400188 20070614 00188 EA 2007 6 14 COMA0760416 1 20070531 A 7722 6030T41P02 THERMOCOUPLE CNDAIR CL600 CL6002B19 1900309 EA NR 1 ENGINE FAULTY A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 819CA 11667 7415 FLIGHT 5400 - ABORTED TAKEOFF FOR RAPID ITT RISE ON NR 1 ENGINE. ITT NOTED AT 900 DEGREES+. INTERROGATED MDC, NO ENGIN E EXCEEDENCE LOGGED. REMOVED AND REPLACED LEFT ENGINE OUTER THERMOCOUPLE. 2 L 7 2 4F RT A21EA 2007061400207 20070614 00207 WP 2007 6 14 UPS07849888 1 20070508 A 5340 ATTACH ANGLE DOUG DC8 DC873F 302199F WP FS 857 RBL65 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C2 CENTER WING EXTERIOR FUSELAGE -L- ANGLE CRACKED AT ST 857.125 RBL 65. REMOVED CRACKED -L- ANGLE AT S TA 857.125 RBL 65 IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPAIR -L- ANGLE AT STA 857.125 RBL 65 IAW DWG 5649893, AN D SRM 51-01-20D. 2 L 7 4 4F RT 4A25 2007061400223 20070614 00223 SW 2007 6 14 AC2A115477 1 20070415 A 2121 MOTOR BELL 427 427 1182207 SW PWC PW207 PW207D NE FAN DAMAGED E AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 427CK 56043 FAN DISENGAGED FROM FAN MOTOR AND DAMAGED THE FAN HUB. 1 G 7 1 3U 3 U R00001RC E42NE 2007061400231 20070614 00231 CE 2007 6 14 DJFA2007054 1 20070507 A 7830 2256012515 THRUST REVERSER BEECH MU300 400A 1155402 CE RT ENGINE DAMAGED E DJFA E A ENGINE SHUTDOWN UNSCHED LANDING W E INADEQUATE Q C VIBRATION/BUFFET CR CRUISE 1 EA 23 469LX 884 RK463 DURING FLIGHT, THE RT TR DEPLOYED AT FL 100. CREW FELT YAWING AND VIBRATION SIMILAR TO SPEED BRAKE DEPLOYMENT. CREW C OMPLETED THE CHECKLIST ITEMS, INCLUDING SHUTTING DOWN THE RAT ENGINE. CREW DECLARED AN EMERGENCY AND RETURNED TO. TRY HAD BEEN PINNED AND MELD PRIOR TO FLIGHT. MAINTENANCE DISCOVERED THE BIG OVER-CENTER LINKS ON THE RAT TRY WERE NOT OVE R-CENTER AND THE TRY HAD PARTIALLY DEPLOYED. THE TRY WAS FOUND TO HAVE BEEN PINNED CORRECTLY YAW THE MEL. MAINTENANCE REPLACED THE RAT TR. 2 H 7 2 4F RT A16SW 2007061400238 20070614 00238 NM 2007 6 14 ASMF200705008 1 20070522 A 4920 3812761 APU DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE FAILED W ASMF K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 23 162P 2561 2561 49765 DURING TRANSIT CHECK, CAPTAIN REPORTED SMOKE IN PASSENGER CABIN. DURING MAINTENANCE CHECK IT WAS DETECTED OIL LEAKING IN THE ZONE OF LT PRIMARY AND SECONDARY HEAT EXCHANGERS AS WELL AS IN THE FLOOR ACCESS OF AIR CONDITIONED UNITS AREA. MAI NTENANCE PERSONNEL REPLACE THE AUXILIARY POWER UNIT, PRIMARY AND SECONDARY LT HEAT EXCHANGERS, TURBINE ASSY COOLING, WA TER SEPARATOR TEMPERATURE AND PNEUMATIC SHUTOFF VALVES IAW MM 49-10-00, 21-51-02, 21-51-03, 21-51-01, 21-20-03 AND 21- 51-06 RESPECTIVELY, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2007061400239 20070614 00239 SO 2007 6 14 N93A24052007 1 20070524 A 5610 1159SCB1025 WINDSHIELD GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU COCKPIT CRACKED E N93A H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 SO 13 487QS 1287 PILOTS WINDSHIELD CRACKED. 2 L 7 2 4F 4 F RT A12EA E25NE 2007061400243 20070614 00243 NM 2007 6 14 DXTA200702198 1 20070515 A 3230 LANDING GEAR AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 262QS 162 LANDING GEAR WOULD NOT EXTEND AFTER SELECTING GEAR HANDLE DOWN. AFTER APPROXIMATELY 2-3 MIN, MAIN GEAR ANNUNCIATOR ILLUM INATED BUT NOSE GEAR DID NOT EXTEND. USED MANUAL GEAR EXTENSION TO EXTEND NOSE GEAR. CHECKED ALL PROX SWITCHES FOR GAP D IMENSIONS. ACCOMPLISHED LANDING GEAR FUNCTIONAL TEST IAW MM 32-300 AND 32-302. TESTED ALL PROX SWITCHES PER MM 32-605. N O FURTHER DEFECTS NOTED AT THIS TIME. 2 K 7 2 4F 4 F RT A50NM E44NE 2007061400250 20070614 00250 CE 2007 6 14 DXTA200702215 1 20070524 A 7720 WARNING LIGHT CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LT ENGINE FALSE ACTIVATION E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 343QS 5600444 LT ENGINE N2 OVER SPEED LIGHT (RED) COMES ON DURING TAKEOFF ROLL. N1 WAS SET AT 96.7 AND N2 DIGITS INDICATE 94-95 PERCEN T. (M2B) UPON ARRIVAL RAN ACFT TO TAKEOFF POWER. OAT A 16 DEGREES C N1 BOTH ENGS AT 97.0, N2 LT ENG 94.4 RT 93.7. NO OV ERSPEED INDICATED. RAN TO POWER (3) TIMES. ALL WORK IAW MM 77-12-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007061400251 20070614 00251 CE 2007 6 14 GUUA05110702 1 20070511 A 3260 H111541 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE MLG FAILED A GUUA O OTHER N FALSE WARNING AP APPROACH 1 SO 29 87552 UE216 DURING APPROACH LANDING GEAR WOULD NOT EXTEND NORMALLY. MANUAL EXTENSION GOT SAFE FOR LT AND RT MAINS. LANDED WITHOUT A LOCKED NOSE GEAR. SHUTDOWN RT ENGINE AT 1,000 FEET AND LT ENGINE PRIOR TO TOUCHDOWN. REPLACED LT MAIN LANDING GEAR UP L OCK SWITCH AND SERVICE VALVE. LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY. 2 L 7 2 4T RT A24CE 2007061500002 20070615 00002 CE 2007 6 15 DXTA200702212 1 20070522 A 3243 99120501718 MASTER CYLINDER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE BRAKES LEAKING E DXTA O OTHER O OTHER LD LANDING 1 GL 07 361QS 9 9 5600361 CO-PILOTS BRAKES ARE SPONGY WITH EXCESSIVE TRAVEL BEFORE BECOMING EFFECTIVE. INSPECTED LT AND RT CO-PILOT BRAKE MASTER CYLINDERS FOUND LEAKING. REMOVED AND REPLACED LT AND RT BRAKE MASTER CYLINDERS WITH A OVERHAULED UNITS AND SECURED; BLE D BRAKE SYST. AS REQUIRED. OPS CHECKED SATISFACTORY IAW MM CHAPTER 32-42-02. 2 L 7 2 4F 4 F RT A22CE E25EA 2007061500016 20070615 00016 CE 2007 6 15 DXTA200702226 1 20070531 A 2700 UNKNOWN CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE UNKNOWN E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 660QS 5605647 AIRCRAFT MADE A SUDDEN YAW TO THE RT AT 105 KTS, ROTATED AT 108 KTS. C/W CHECKS OF FLIGHT CONTROLS, BRAKES AND TIRE PRE SSURES. THE RT TIRES WORN TO NEAR LIMITS. NO OTHER DISCREPANCIES NOTED. ALL WORK ACCOMPLISHED IAW MM 5-00-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007061500017 20070615 00017 CE 2007 6 15 DXTA200702227 1 20070531 A 3240 BRAKE ASSY CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 667QS 5605365 BRAKES ARE SPONGY, CAN BE FORCED TO THEIR STOPS RT SIDE MORE THAN LT. BLED BOTH LT AND RT BRAKES. ALSO CYCLED PARKING B RAKE SEVERAL TIMES DURING BLEEDING PROCEDURES. WORK DONE IAW AMM 32-42-00. SERVICED BRAKE RESERVOIR AS REQUIRED. WORK DO NE IAW AMM 12-12-02. OPERATED BRAKES WITH NO DEFECTS NOTED. OPS AND LEAK CHECKED GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007061500025 20070615 00025 CE 2007 6 15 DXTA200702233 1 20070601 A 3240 BRAKE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG WEAK E DXTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 667QS 5605365 RT BRAKE IS SPONGY, TRAVELS FURTHER THAN LT BEFORE GETTING PRESSURE, OCCURS ON BOTH PILOT & COPILOTS PEDALS. PERFORMED A NTI-SKID BRAKE SYSTEM BLEED AND OPERATIONAL TEST IAW AMM 32-42-00. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007061500032 20070615 00032 EA 2007 6 15 TRAX200700786 1 20070604 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 885AS 7521 FOUND FS 280 AT LBL 9 I/B AND O/B ANGLES ARE CRACKED. 2 L 7 2 4F RT A21EA 2007061500035 20070615 00035 EA 2007 6 15 TRAX200700789 1 20070604 A 5320 BRACE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 975EV 7599 FOUND ANGLE BRACE IS CRACKED AT FS 280.0 LBL 9.0 ON THE INSIDE. 2 L 7 2 4F RT A21EA 2007061500039 20070615 00039 EA 2007 6 15 TRAX200700793 1 20070604 A 5313 STRINGER CNDAIR CL600 CL6002B19 1900309 EA BS 654-682 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 975EV 7599 SUSPECT CORROSION ON STRINGERS FROM WL97.50 TO FLOOR, BETWEEN FS 654.5 TO FS 682. 2 L 7 2 4F RT A21EA 2007061500040 20070615 00040 EA 2007 6 15 TRAX200700795 1 20070605 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 975EV 7599 AFT PRESSURE BULKHEAD CRACKED AT ANGLE, AREA IS MARKED. IN REFERENCE TO TASKCARD AWL 53-61-153. [06-14-07] BEGAN REO 601R-53-61-1230. REMOVED ANGLE FORWARD OF STA 621. REMOVED AFT INTERCOSTAL AT STA 621. REMOVED FORWARD LINTEL FITTING AT STA 621. 2 L 7 2 4F RT A21EA 2007061500065 20070615 00065 NM 2007 6 15 DHL2007783504 1 20070602 A 5347 BAC1520841 SEAT TRACK BOEING 727 727227 1384078 NM BS 757-852 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 CABIN SEAT TRACK CORRODED BETWEEN BS 760 TO BS 825, RBL 24. REMOVED SEAT TRACK SECTION BS 757.45 TO BS 852.45, RBL 45 I AW B727 SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK P/N BAC1520-841 IAW B727 SRM 51-30-5 AND 53-10-2, FIG 7. PART AND AREA TREATED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 51-10-2, 51-30-2 AND 53-10-2, FIG 7. 2 L 7 3 4F A3WE 2007061500067 20070615 00067 WP 2007 6 15 070126 1 20070604 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 875GA 53468 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007061500079 20070615 00079 NM 2007 6 15 DU4R2007135 1 20070608 A 5420 BRACE BOEING 757 757232 1384965 NM ZONE 400 OUT OF LIMITS B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 640DL 23994 FOUND NR 2 DIAGONAL BRACE ID 2.003 (OUT OF LIMITS). REPAIRED OVERSIZED LUG ON NR 2 DIAGONAL BRACE BY HONING, FABRICATIN G AND INSTALLING BUSHINGS IAW DELTA ERA 461664-14AD DATED 6/7/07 APPROVED BY FAA FORM 8100-9 WITH AMOC TO PARAGRAPH (A) OF AD 2003-18-05. 2 L 7 2 4F RT A2NM 2007061500082 20070615 00082 NM 2007 6 15 DU4R2007133 1 20070606 A 5311 FRAME BOEING 757 757232 1384965 NM ZONE 400 DENTED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 640DL 23994 AFT PIT FRAME DENTED BS 1440, STR 27L. REMOVED OLD REPAIR, FABRICATED AND INSTALLED FRAME REPAIR 16"BY 3" BY 1" FROM 70 75-T6 .071" IAW B757 SRM 51-40-02, 51-40-05, 51-70-11, 53-00-07, 51-20-01 AND 51-20-02. 2 L 7 2 4F RT A2NM 2007061500102 20070615 00102 NM 2007 6 15 GAI2007F00001 1 20070504 A 2797 CONNECTOR BOEING 727 727214 138407R NM PWA JT8 JT8D9 52048 NE NR 4 SLAT DIRTY A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 750US 21512 (REF NR: GAIA 07-05 OP) DURING CLIMB THE FLIGHT CREW RETRACTED THE FLAPS NORMALLY HOWEVER, AT ZERO DEGREES FLAPS THE AMB ER LIGHT REMAINED ILLUMINATED ON THE FRONT PANEL. FE PANEL INDICATED NR 4 SLAT EXTENDED. FOLLOWED OPS PROCEDURE AND CY CLED FLAPS WITH SAME RESULT. THE AIRCRAFT RETURNED AND AN UNEVENTFUL LANDING WAS MADE. CLEANED AND RESEATED THE CONNEC TOR AT THE SLAT ACTUATOR. OPS CHECKED GOOD. AIRCAFT WAS RETURNED TO SERVICE. (K) 2 L 7 3 4F 4 F A3WE E2EA 2007061500108 20070615 00108 NM 2007 6 15 KCSA071186 1 20070607 A 5413 FITTING BOEING 747 747221F 1384868 NM BS 2598 S8L CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 FUSELAGE STRINGER END FITTING IS CORRODED AT STA 2598, STR 8L. 2 L 7 4 4F A20WE 2007061500113 20070615 00113 NM 2007 6 15 CALA0700294 1 20070606 A 5330 6545765102 SKIN BOEING 737 7373T0 1384582 NM BS 420-440 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 10323 23374 INSPECTION FOUND SKIN AT TOP ATC ANTENNA MOUNTING SURFACE CORRODED, STA 420-440, S1L TO 2L. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201. A DIP WAS INITIATED TO COMPLY WITH ECRA 5330-03685 STEP 6 ON OR BEFORE JUNE 4, 2008 AND TO PE RFORM A PERMANENT REPAIR IAW ECRA 5330-03685 PART 3. 2 L 7 2 4F RT A16WE 2007061500116 20070615 00116 NM 2007 6 15 CALA0700296 1 20070607 A 5320 69169966 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 196-203 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12313 23364 INSPECTION FOUND INTERCOSTAL CORRODED AT STA 196-203, RBL 5.7, S28L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 5 1-10-02 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007061500124 20070615 00124 NM 2007 6 15 UPS07M49902 1 20070417 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORIZ STAB BARREL NUT BORE NR 32 LEFT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38 BO TTOM-REMAIN BLENDOUT 0.065" DEEP BORE REAMED TO 1.178" DIA REMAIN BLENDOUT 0.039" EXCEED EO LIMITS. 10X MAG DVI C/O NO CORROSION. BORE REAMED FURTHER TO 1.219" DIA EN1239-07. BLENDOUT & BOTTOM PERI RADIUSED, SMOOTHEN & PROTECTED SRM 51-2 1-01 VII R38. REPAIR SLEEVE BUSHING FAB & INSTALLED EO FIG 5. BORE NR 32 LEFT REPAIR C/O IAW EN1239-07. 2 L 7 3 4F RT A22WE 2007061500127 20070615 00127 NM 2007 6 15 UPS07M49905 1 20070405 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 32 RIGHT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38. BOTTOM-REMAIN BLENDOUT 0.041" DEEP. BORE REAMED TO 1.178" DIA REMAIN BLENDOUT 0.030" DEEP EXCEED EO LIMITS. 10X MAG DV I C/O NO CORROSION. BORE BLENDOUT & BOTTOM PERI RADIUSED, SMOOTHEN & PROTECTED SRM 51-21-01 VII R38. REPAIR SLEEVE BUS HING FAB, PROTECTED & INSTALLED PER EO FIG 5. REPAIR C/O AT BN BORE NR 32 RIGHT ACCEPTABLE IAW EN1206-07. 2 L 7 3 4F RT A22WE 2007061500128 20070615 00128 NM 2007 6 15 UPS07M49906 1 20070414 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 21 RIGHT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38. BOTTOM-SURF CLEANED, BORE REAMED TO 1.067" REMAIN BLENDOUT 0.015" DEEP EXCEED EO LIMITS. 10X MAG DVI C/O NO CORROSION. BORE BLENDOUT & BOTTOM PERI RADIUSED, SMOOTHEN & PROTECTED SRM 51-21-01 VII R38. REPAIR SLEEVE BUSHING FAB, PROTECTED & INSTALLED AS PER EO FIG 5. REPAIR C/O AT BARREL NUT BORE IS ACCEPTABLE IAW EN1221-07. 2 L 7 3 4F RT A22WE 2007061500129 20070615 00129 NM 2007 6 15 UPS07M49907 1 20070405 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 30 LEFT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38. B OTTOM - REMAIN BLENDOUT 0.050" DEEP BORE-REAMED TO 1.178" DIA - REMAIN BLEND OUT 0.045" DEEP EXCEED EO LIMITS. 10X MAG DVI C/O NO CORROSION. BORE BLENDOUT & BOTTOM PERI RADIUSED, SMOOTHEN & PROTECTED SRM 51-21-01 VII R38. REPAIR SLEEVE B USHING FAB, PROTECTED & INSTALLED PER EO FIG 5. REPAIR C/O AT BN BORE NR 30 LEFT IAW EN1201-07. 2 L 7 3 4F RT A22WE 2007061500135 20070615 00135 NM 2007 6 15 UPS07M49920 1 20070414 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 31 RIGHT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R 38. BOTTOM - SURF CLEANED BORE REAMED TO 1.178" DIA REMAINING BLENDOUT 0.130" DEEP EXCEED EO LIMITS. 10X MAG DVI C/O NO CO RROSION. BORE REAMED FURTHER TO 1.219" DIA EN1238-07. REPAIR SLEEVE BUSHING FAB, PROTECTED & INSTALLED PER EO FIG 5. BORE BLENDOUT & BOTTOM PERI RADIUSED, SMOOTHEN & PROTECTED SRM 51-21-01 VII R38. REPAIR BORE NR 31 RIGHT IAW EN1238-07. 2 L 7 3 4F RT A22WE 2007061500150 20070615 00150 WP 2007 6 15 UPS07849925 1 20070531 A 5313 DC853B00939 LONGERON DOUG DC8 DC873F 302199F WP BS 1756 L14L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C1 L14L STA 1756 UPPER VERT FLANGE HAS A .25 INCH CRACK FROM ATTACH FASTENER HOLE. REMOVED DAMAGED LONG ERON, FABRICATED AND INSTALLED REPLACEMENT LONGERON, AND SPLICE FITTING IAW SRM 51-1-21, 53-02-02 FIG 10, 51-1-8, 51-1-2 0D. 2 L 7 4 4F RT 4A25 2007061500154 20070615 00154 NM 2007 6 15 UPS07M49930 1 20070409 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORT STAB, BARREL NUT BORE LEFT NR 36 FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01VII R 38. BOTTOM REMAIN BLENDOUT 0.095" DEEP BORE REAMED TO 2.538" DIA REMAIN BLENDOUT 0.080" DEEP EXCEED LIMITS. FURTHER REAMED TO 2.572" DIA & BOTTOM MACHINED DOWN 0.060" DEEPER. BLENDOUTS & BOTTOM PERI RADIUSED, SMOOTHEN & PROTECTED. REPAIR SLE EVE BUSHING, DOUBLER & FILLERS FAB & INSTALLED PER EO FIG 5 & 6. REPAIR C/O AT NR 36 LEFT IAW EN1217-07. 2 L 7 3 4F RT A22WE 2007061500155 20070615 00155 NM 2007 6 15 UPS07M49931 1 20070420 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 33 RIGHT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01VII R38. B OTTOM - REMAIN BLENDOUT 0.025" DEEP BORE-REAMED TO 1.178" DIA REMAIN BLENDOUT 0.095" DEEP EXCEED EO LIMITS. 10X MAG DVI C/O NO CORROSION. BORE FURTHER REAMED TO 1.203" DIA EN1246-07. BLENDOUT VOIDS & BOTTOM PERI RADIUSED, SMOOTHEN & PROT ECTED SRM 51-21-01 VII R38. REPAIR SLEEVE BUSHING FAB & INSTALLED EO FIG 5. NR 33 RIGHT REPAIR IAW EN1246-07. 2 L 7 3 4F RT A22WE 2007061500157 20070615 00157 NM 2007 6 15 UPS07M49933 1 20070416 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 27 RT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38 BOTTO M SURF REMAIN BLENDOUT 0.048" DEEP BORE REAMED TO 1.178" DIA REMAIN BLENDOUT 0.060" DEEP EXCEED EO LIMITS. 10X DVI C/O N O CORROSION. BORE BLENDOUT & BOTTOM PERI RADIUSED, SMOOTHEN & PROTECTED SRM 51-21-01 VII R38. REPAIR SLEEVE BUSHING FA B, PROTECTED & INSTALLED PER EO FIG 5. REPAIR C/O AT BN BORE NR 27 RT IS ACCEPTABLE IAW EN1230-07. 2 L 7 3 4F RT A22WE 2007061500163 20070615 00163 NE 2007 6 15 PG9A115816 2 20070421 A 7240 0292377910 SWIRLPLATE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIUS ARRIUS2B1A NE ENGINE CRACKED B PG9A K NONE O OTHER IN INSP/MAINT 1 WP 19 133GC 3883 23117 DURING INSPECTION FOUND CRACKS AROUND THE BOLTS IN THE SWIRL PLATE EXTENDING TO THE FOURTH ROW OF HOLES. ONE OF WHICH H AD TWO CRACKS INTERSECTING WITH EACH OTHER. THIS COULD HAVE POSSIBLY LED TO THAT PIECE COMING LOOSE AND FINDING ITS WAY THROUGH THE REST OF THE ENGINE. REMOVED MO2 AND MO3 AND INSTALLED SERVICEABLE MODULES. 1 G 7 2 3U 3 U H9EU E34NE 2007061500182 20070615 00182 CE 2007 6 15 85129BC 1 20070605 A 2432 1293640315 CHARGER BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MASTER BATTERY LOOSE A AMWA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 07 127ZV UE127 AFTER TAXI FROM GATE THE BATTERY CHARGE ANNUN ILLUM. AC RETURNED TO GATE WITH NO FURTHER INCIDENT. THIS BATTERY CHARGE ANNUN ILLUM WRITEUP IS CONSIDERED A NUISANCE AND EXTREME DISTRACTION TO THE PILOT. RESEATED A-130 PCB, OPS CHECKED GOO D. 2 L 7 2 4T 3 T RT A24CE E2NE 2007061500206 20070615 00206 CE 2007 6 15 07N911KD01 1 20070525 A 5302 105304061 SPAR BOLKMS BK117 BEECH 35 V35 1151538 CE CONT O520 IO520* 17032 SO TAILBOOM CRACKED E QMLA K NONE O OTHER IN INSP/MAINT 1 NM 03 911K 158 7237 DURING DETAILED INSPECTION OF TAILBOOM VERTICAL SPAR AREA FOUND 2 EA CRACKS APPROX .7500 INCHES IN LENGTH AT THE 1:00 O' CLOCK AND 7:00 O'CLOCK POSITIONS ON THE SECOND LIGHTING HOLE DOWN FROM TAIL ROTOR GEARBOX MOUNT. SUSPECT CRACKS HAVE BEE N WORKING FOR SOME TIME DUE TO (MUD) BUILD UP AROUND THE CRACKS, LAST GENERAL INSP OF AREA DONE 183.3 HOURS PRIOR AND LA ST VERTICAL SPAR (AD) SIGN OFF COMPLETED 158.3 HOURS PRIOR. DUE TO THE HISTORY OF THIS TAIL BOOM REGARDING CRACKS, SUBMI TTER RECOMMENDS THAT ALL FLEET (BK) AND (BO) OPERATORS INSPECT THIS AREA AS SOON AS PRACTICAL. 1 L 7 1 3O 3 O 3A15 E5CE 2007061500212 20070615 00212 EU 2007 6 15 FJ7A115661 1 20070529 A 2432 151CH1 BATTERY UROCOP EC130 EC130B4 8680989 EU MASTER WEAK E FJ7A O OTHER O OTHER NR NOT REPORTED 1 SO 19 174AM 248 4007 BATTERY, CONTINUALLY WEAK ON STARTS. 1 G 7 2 3U H9EU 2007061500215 20070615 00215 SW 2007 6 15 07N101VU01 1 20070523 A 6320 B632K1001051 TRANSMISSION BOLKMS 117 BK117C2 5626002 SW TMECA ARRIEL ARRIEL1E 60030 NE MAIN ROTOR WARNING LIGHT E QMLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 101VU 2063 9039 DURING CRUISE FLIGHT ENROUTE TO A LOCAL HOSPITAL FOR A PATIENT PICK UP, THE MAIN TRANSMISSION CHIP LIGHT ILLUMINATED. PE RFORMED THE EMERGENCY PROCEDURE IAW THE AIRCRAFT CHECK LIST AND LANDED AT THE NEAREST AIRPORT WITHOUT INCIDENT. CREW WAS TRANSPORTED TO THE HOSPITAL BY LOCAL EMS AND THE PROGRAM DISPATCHED ONE OF ITS OTHER AIRCRAFT TO COMPLETE THE MISSION. MECHANIC CLEANED AND INSPECTED THE MAIN TRANSMISSION CHIP PLUGS, CLEANED AND INSPECTED THE MAIN TRANSMISSION OIL FILTER S, DRAINED AND FLUSHED THE MAIN TRANSMISSION. GROUND RUN UP AND 30 MINUTE FLIGHT CHECK WERE COMPLETED BEFORE AIRCRAFT WA S RETURNED TO SERVICE. 1 G 7 2 3U 3 U H13EU E19EU 2007061800009 20070618 00009 EA 2007 6 18 QXEA200700922 1 20070602 A 5330 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA SKIN UNKNOWN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC -REFERANCE ITEM 18 DAMAGE NR 8 PER E/C R-53-455/3. REPAIRED IAW REOP670-53-45-014. 2 L 7 2 4F RT A21EA 2007061800011 20070618 00011 EA 2007 6 18 QXEA200700924 1 20070527 A 5330 NONE CNDAIR CL600 CL6002C10 1390015 EA NONE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC - REFERENCE ITEM 14 DAMAGE NR 6 PER E/C R-53-455/3. REPAIRED IAW REO670-53-00-107. 2 L 7 2 4F RT A21EA 2007061800019 20070618 00019 NM 2007 6 18 AALA20071004 1 20070607 A 3350 D71701100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 927AN 30077 TUL - EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD ENTRY DOO R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007061800026 20070618 00026 2007 6 18 AALA20070993 4 20070530 A 2565 62774415 SLIDE BOEING 777 777223 1385213 NM L4 DOOR INOPERATIVE A AALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 753AN 30261 PVG - DURING AIRCRAFT SERVICING LEFT NUMBER FOUR DOOR SLIDE WAS DISLODGED FROM BUSTLE HOUSING AND BACKBOARD. SLIDE DID NOT DEPLOY. SUSPECT HOUSING STRUCK BY CATERING EQUIPMENT. REPLACED LEFT NUMBER FOUR DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007061800032 20070618 00032 EA 2007 6 18 QXEA200700929 1 20070527 A 5100 NONE CNDAIR CL600 CL6002C10 1390015 EA NONE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC - REFERENCE ITEM 2 DAMAGE NR 1 PER E/C R-53-455/3. REPAIRED IAW REO670-53-00-107. 2 L 7 2 4F RT A21EA 2007061800033 20070618 00033 EA 2007 6 18 QXEA200700931 1 20070531 A 5100 NONE CNDAIR CL600 CL6002C10 1390015 EA NONE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC - COMPLIED WITH NR 7 DAMAGE NR 8. REPAIRED IAW REO-53-00-123. 2 L 7 2 4F RT A21EA 2007061800034 20070618 00034 EA 2007 6 18 QXEA200700930 1 20070531 A 5330 NONE CNDAIR CL600 CL6002C10 1390015 EA NONE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC - COMPLIED WITH ITEM NR 8 DAMAGE NR 9. REPAIRED IAW EEO670-53-00-123. 2 L 7 2 4F RT A21EA 2007061800037 20070618 00037 EA 2007 6 18 QXEA200700934 1 20070531 A 5100 NONE CNDAIR CL600 CL6002C10 1390015 EA NONE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC - COMPLIED WITH NR 4 DAMAGE NR 5. REPAIRED IAW REO670-53-00-123. 2 L 7 2 4F RT A21EA 2007061800052 20070618 00052 EU 2007 6 18 CPCP20070032 1 20070425 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 448AM 448 FOUND FRAME 36 FLOORBEAM CORRODED. FRAME 36 FLOOR SPLICED AS PER SRM 55-00-00. 2 H 7 2 4T RT A53EU 2007061800053 20070618 00053 EU 2007 6 18 CPCP20070036 1 20070425 A 5311 FRAME AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 448AM 448 FOUND FRAME 39 BETWEEN STRINGER LT 21 AND RT 21 CORRODED. FRAME 39 REPAIRED AS PER SRM 53-61-40 FIG 415 WITH SECTION OF NEW FRAME SEGMENT. 2 H 7 2 4T RT A53EU 2007061800055 20070618 00055 WP 2007 6 18 NWAA072129957 1 20070513 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 1004 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING "H" CHECK, FOUND CRACKS IN FRAME AT BS 1004 BETWEEN L28R AND L29R AND L28L AND L30L. REPAIRED PER EA 99-209582. 2 L 7 2 4F A6WE 2007061800057 20070618 00057 NM 2007 6 18 DHL2007783506 1 20070607 A 5347 BAC15207927178 CARGO TRACK BOEING 727 727227 1384078 NM BS 560-690 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 CABIN SEAT TRACK CORRODED BETWEEN BS 690 TO BS 560, RBL 45. REMOVED SEAT TRACK SECTION BS 590 TO BS 690, RBL 45 IAW B72 7 SRM 53-10-5, FIG 5. FABRICATED NEW SEAT TRACK, MATERIAL USED BAC1520-792-7178T6511, DIM. 99” LONG AND 2 EACH ANGLES, MATERIAL USED BAC1503-100122-7178T6, .250” BY 7 BY 2.5 IAW B727 SRM 53-10-5, FIG 1 AND 51-30-5. PART AND AREA TREATED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 51-10-2, 53-10-5, FIG.1 AND 51-30-2. 2 L 7 3 4F A3WE 2007061800060 20070618 00060 NM 2007 6 18 AALA20070980 1 20070529 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 936AN 29532 MIA - EMERGENCY LIGHT AT SEAT 12D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007061800062 20070618 00062 NM 2007 6 18 AALA20070998 1 20070525 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 977AN 29550 TUL - EMERGENCY LIGHTS AT LEFT FORWARD ENTRY DOOR HAS BROKEN LENS. REPLACED BROKEN LENS FOR EMERGENCY LIGHT AT LEFT FOR WARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007061800063 20070618 00063 NM 2007 6 18 AALA20070999 1 20070525 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 977AN 29550 TUL - EMERGENCY LIGHTS AT RIGHT AFT OVERWING DOOR HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHTS AT RIGHT AFT OVER WING DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007061800064 20070618 00064 NM 2007 6 18 AALA20070996 1 20070531 A 3397 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 JFK - EMERGENCY AISLE LIGHT AT SEAT 2D INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY AISLE LIGHT AT SEAT 2D. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007061800065 20070618 00065 NM 2007 6 18 AALA20070984 1 20070529 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 642AA 24600 TPA - EMERGENCY LIGHT AT SEAT 17D MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007061800068 20070618 00068 NM 2007 6 18 AALA20070983 1 20070529 A 3350 0201804002 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 642AA 24600 TPA - EMERGENCY LIGHT AT SEAT 17D MISSING LENS. REPLACED RED LENS FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007061800076 20070618 00076 EU 2007 6 18 AALA20070990 1 20070530 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80052 460 MIA - FOUND EMERGENCY LIGHT AT SEAT 16C INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 16C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007061800079 20070618 00079 EA 2007 6 18 QXEA200700925 1 20070527 A 5100 NONE CNDAIR CL600 CL6002C10 1390015 EA NONE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC - REFERENCE ITEM 10 DAMAGE NR 4 PER E/C R-53-455/3. REPAIRED IAW REO670-53-00-107. 2 L 7 2 4F RT A21EA 2007061800081 20070618 00081 EA 2007 6 18 QXEA200700927 1 20070525 A 5100 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA UNKNOWN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC - REFERENCE ITEM 8 DAMAGE NR 3 PER E/C R-53-455/3. REPAIRED IAW REO670-53-00-107. 2 L 7 2 4F RT A21EA 2007061800084 20070618 00084 NM 2007 6 18 QXEA200700963 1 20070614 A 3320 LENS DHAV DHC8 DHC8202 2809007 NM CABIN DISLODGED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 354PH 498 SEA FLIGHT NR 2026 PLASTIC PIECE FELL OFF FROM CEILING ABOUT 6" LONG. REPORTED BY FLIGHT ATTENDANT. MAINTENANCE RESECU RED SIDE WALL LIGHT LENS. PERFORMED GUI OF LENS. NO DEFECT NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061800085 20070618 00085 NM 2007 6 18 QXEA200700942 1 20070612 A 3010 CONTROL UNIT BOMBDR DHC8 DHC8402 1390042 NM DE ICE SYSTEM MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 419QX 4145 SEA FLIGHT NR 2257: AFTER PUSH BACK AND ENGINE START, DEICE CONT CIRCUIT BREAKER TRIPPED. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE REMOVED AND REPLACED TMCU AND NR 2 HIGH PRESSURE SOV (P/N 820971-2). PERFORMED FUNCTIONAL CHECK OF THE AIRF RAME PNEUMATIC DEICING SYSTEM IAW Q400 AMM 30-11-00-720-801. FUNCTIONAL TEST GOOD. ALL OTHER INDICATIONS NORMAL. AIRC RAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061800088 20070618 00088 NM 2007 6 18 QXEA200700941 1 20070613 A 3097 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM PROP DE ICE BROKEN A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 413QX 4060 SEA FLIGHT NR 2257: PROP DEICE CAUTION LIGHT ILLUMINATED. RECYCLED PROP HEAT PER CHECKLIST AND LIGHT CAME BACK ON. AIR CRAFT RETURNED TO FIELD. MAINTENANCE INTERROGATED CDS AND FOUND OPEN PHASE B OPEN PHASE C AND OPEN HEATER FAULTS ON TMC U 2. C/W Q400 FIM TASKS 30-61-00-810-835, 60-61-00-810-836 AND 30-61-00-810-857 BY PERFORMING AN ELECTRICAL CONTINUITY CHECK OF THE PROPELLER DEICING HEATER ELEMENTS IAW Q400 AMM TASK 30-61-00-760-801. FOUND BROKEN HEATER HARNESS ON NR 2 P ROP, NR 2 BLADE. REMOVED AND REPLACED NR 2 PROP, NR 2 BLADE HEATER HARNESS IAW Q400 AMM TASKS 61-10-06-000-801 AND 61-10 -06-400-801. OPS CHECK GOOD. FAULTS DID NOT RETURN. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061800089 20070618 00089 NM 2007 6 18 DHLA200700031 1 20070614 A 3350 BATTERY PACK BOEING 727 727225 1384077 NM EMERGENCY LIGHTS INOPERATIVE A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 FLIGHT DECK EMERGENCY EXIT LIGHT INOP ON STBY PWR CHECK. REMOVED AND REPLACED BATTERY PACK PER MM 33-50-71, OPS CK NORM AL. 2 L 7 3 4F A3WE 2007061800090 20070618 00090 NM 2007 6 18 KNNA200700033 1 20070503 A 5311 FRAME BOEING 737 7373Q8 1384670 NM PWA JT8 JT8D217 52053 NE BS 663 CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 413JG 23148 PASSENGER CABIN/CRACK ON FRAME BS-663 AND STRINGER-2L, ACO NR 075365 PROVIDES INSTRUCTION ON REPAIR OF CRACKED FRAME AT BS-663, STRINGER 2L SRM 53-10-4. 2 L 7 2 4F 4 F RT A16WE E9NE 2007061800091 20070618 00091 SO 2007 6 18 SIMA200716501 1 20070613 A 3350 110049 CHARGER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 941LT 585 31 14500926 EMERGENCY LIGHTS AFT OF ROW ONE WILL NOT EXTINGUISH, OVERWING EMERGENCY LIGHTS ALSO ILLUMINATED. REMOVED AND REPLACED N UMBER FOUR EMERGENCY BATTERY PACK AND CHARGER IAW EMB AMM 35-50-04 AND 33-50-00. OPERATIONAL CHECK GOOD, RETURNED AIRCR AFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061800093 20070618 00093 SO 2007 6 18 SIMA200716502 1 20070613 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 658AE 9267 145760 REAR CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED NUMBER SIX DC/AC INVERTER IAW EMB AMM 33-50-11. OPERATI ONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061800094 20070618 00094 2007 6 18 TSAA0779031 2 20070609 A 7261 OIL CAP BOEING 737 7372X6C 1384552 NM NR 2 LOOSE A TSAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 13 746AS 23123 NON-ETOPS FLIGHT 82 HNL - KOA - AFTER TAKEOFF, THE CREW WAS ADVISED BY ATC THAT THERE WAS DARK SMOKE TRAILING THE NR 2 E NGINE. CREW NOTED THE OIL QUANTITY DROPPING AND RETARDED THE NR 2 THROTTLE TO IDLE. AIRCRAFT RETURNED TO HNL WITHOUT F URTHER INCIDENT. MAINTENANCE FOUND THE NR 2 OIL CAP LOOSE AND SERVICED THE ENGINE OIL. MAINTENANCE RAN THE NR 2 ENGINE AND FOUND NO OIL LEAKS. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007061800095 20070618 00095 2007 6 18 TSAA0734032 4 20070610 A 3460 1714970501 COMPUTER BOEING 737 73776N 13844CH NM MALFUNCTIONED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 740AL 28640 ETOPS FLIGHT 442 HNL-OAK - DURING CLIMB, AFTER FLAPS WERE RETRACTED, THE CREW NOTED SPEED AND ALTITUDE ERRORS ON BOTH TH E LEFT AND RIGHT FMC UNITS. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED FMC BITE CHECK PER FI M 34-61-00-810-801 AND RESET THE FMC, ADIRS AND SMYD CIRCUIT BREAKERS. AIRCRAFT WAS RETURNED TO SERVICE. A FLIGHT VERI FICATION OF THE FMC SYSTEM WAS CONDUCTED ON THE NEXT FLIGHT LEG. 2 L 7 2 4F RT A16WE 2007061800096 20070618 00096 NM 2007 6 18 DHL2007740529 1 20070520 A 5312 PRESSURE PANEL BOEING 727 7272Q9 138448M NM BS 273 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 WHILE IN "C" CHECK, NOSE LANDING GEAR WHEEL WELL LT WEB UPPER PLATE CRACKED AT OPENING (BS273). REMOVED WEB IAW B727 SR M 51-30-2. FABRICATED NEW WEB FROM 7075T6 .032 PO NR 9003110 DIM 11 1/2" BY 7" IAW B727 SRM 53-10-2 FIG 3 AND 51-10-3. TREATED AND PRIMED NEW WEB IAW B727 SRM 51-10-2 AND INSTALLED NEW WEB AT NOSE LANDING WHEEL WELL LT BS 273 IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007061800098 20070618 00098 NM 2007 6 18 DHL2007783507 1 20070206 A 5753 6521634131 SKIN BOEING 727 727227 1384078 NM TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 62213 62213 21999 LT INBD FLAP, AFT FLAP INBD SIDE HAS SMALL DELAMINATION LWBL 89.6 TO 96.6, 10 TO 15 ABOVE T/E. REMOVED DAMAGED AREA 3.5 BY 3.6, CLEANED AND PREPPED AREA TO BE REPAIRED IAW B727 SRM 51-40-20, PARA 7, FIG 3. FABRICATED FILLER 3.5 BY 3.6 AND DOUBLER 6.5 BY 5.1 FROM .012, 7075-T6. ANODIZED, PRIMED AND APPLIED ADHESIVE FILM IAW B727 SRM 51-40-20, 51-40-24, FIG 1 AND 57-50-2, FIG 3. INSTALLED REPAIR PARTS, CURED AND FINISHED REPAIR AREA IAW B727 SRM 51-40-20, PARA 20, 22 AND 51 -40-24, FIG 1. 2 L 7 3 4F A3WE 2007061800100 20070618 00100 SO 2007 6 18 FDKA200705202 1 20070511 A 3350 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 847MJ 145517 FDM 6012 ATL-BGM (0917 PHX LCL) - RT ROW 12 EMERGENCY LOCATOR SIGN INOP. MX RESET OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2007061800101 20070618 00101 2007 6 18 DXTA200702248 4 20070607 A 2297 S35211 GROUND STUD CESSNA 750 750 2076810 CE FWD E/E BAY DAMAGED E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 986QS 5863 7500086 DURING FLIGHT WITH AUTOPILOT ENGAGED AIRCRAFT ROLLS BACK AND FORTH AS IF SEARCHING FOR LEVEL FLIGHT. FOUND GROUND STUDS TG532 AND TG533 AT YSAC COMPUTERS NORMAL. FOUND GROUND STUDS TG511 AND TG521 AT LOWER YD ACTUATORS WITH HIGH RESISTANCE. REMOVED AND REPLACED GROUND STUDS WITH NEW. LOWER YD OPERATIONAL CHECK NORMAL. WORK IAW CESNA 750 MM CHPT 20-20-03 2 L 7 2 4J RT T00007WI 2007061800102 20070618 00102 CE 2007 6 18 DXTA200702249 1 20070607 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE MLG WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 336QS 5600336 BOTH PILOTS + COPILOTS LEFT BRAKE SOFT. BOTH PILOTS & COPILOTS RIGHT BRAKE EXTREMLY SOFT PEDAL HAS TO BE PUSHED ALL THE WAY FORWARD TO GET ANY BRAKING ACTION ON RIGHT (COPILOTS) SIDE. BLED ANTI-SKID BRAKE SYSTEM SEVERAL TIMES. OPS & LEAK CHECKS GOOD. TAXI CHECK GOOD. IAW 560MM CHP 32-42-00. 2 L 7 2 4F RT A22CE 2007061800107 20070618 00107 CE 2007 6 18 052107N151CS 1 20070521 A 5101 STRUCTURE CESSNA 525 525 2076601 CE WILINT FJ44 FJ44 66000 GL FUSELAGE DAMAGED E Z5FA L A ABORTED APPROACH UNSCHED LANDING O OTHER AP APPROACH 1 EA 63 151CS 5250529 ON APPROACH, CREW ENCOUNTERED FLOCK OF GEESE RESULTING IN NUMEROUS STRIKES. ABORTED APPROACH, INITIATED AFM ABNORMAL CH ECKLIST WITH NO ABNORMALITIES NOTED. DIVERTED, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. AFTER LANDING AND EXITI NG AIRCRAFT, CREW NOTED SIGNIFICANT DAMAGE TO LT AND RT ENGINE INLETS, PYLONS, WINDSCREEN RAIN DOORS AND AFT FUSELAGE. AIRCRAFT PRESENTLY UNDERGOING INSPECTION FOR MAINTENANCE ACTION PLAN. 1 L 7 2 4F 4 F RT A1WI E3GL 2007061800109 20070618 00109 2007 6 18 DFJ2007F00000 4 20070409 A 6122 DCFS290D7T3 GOVERNOR CESSNA 310 310R 2074245 CE CONT O520 IO520M 17032 SO MCAULY 3AF32C 3AF32C87 GL PROPELLER MALFUNCTIONED E DFJA O OTHER O OTHER NR NOT REPORTED 1 CE 03 4264J 320 310R0201 270793R 801106 PROPELLER STARTED TO SURGE ON RT ENGINE DURING CRUISE FLIGHT CONDITIONS. AC WAS LANDED AND THE PROPELLER GOVERNOR WAS R EPLACED WITH AN OVERHAULED GOVERNOR. (K) 1 L 7 2 3O 3 O 3A10 E5CE 5 C P22EA 2007061800110 20070618 00110 CE 2007 6 18 DXTA200702199 1 20070517 A 3234 HANDLE CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE MLG LACK OF LUBE E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 809QS 5600698 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF AS INDICATED BY 3 GREEN, NO RED INDICATION, UPON BRINGING GEAR HANDLE TO UP POSITION. FOUND HANDLE TO BE STIFF. REMOVED GEAR HANDLE AND LUBED. REATTACHED HANDLE OP'S CK GOOD. GEAR SWINGS FWD IA W MM CH 32-30-00. 2 L 7 2 4F 4 F RT A22CE E00053EN 2007061800111 20070618 00111 CE 2007 6 18 DXTA200702202 1 20070517 A 3246 315381 WHEEL CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG OUT OF BALANCE E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 916QS 6559 7500116 NOSE WHEEL SHIMMY AT 60KTS, ABORTED TAKEOFF. REMOVED AND REPLACED BOTH NOSE TIRES. WORK DONE IAW MM 32-41-02. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007061800112 20070618 00112 CE 2007 6 18 DXTA200702222 1 20070529 A 3260 DOWNLOCK SWITCH BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE RIGHT OUT OF ADJUST E DXTA O OTHER N FALSE WARNING LD LANDING 1 GL 07 147QS RK436 DID NOT RECEIVE RT MAIN GEAR LIGHT ON GEAR EXTENSION. PROCEEDED WITH (LANDING GEAR NOT DOWN + LOCKED0 CHECKLIST. TROUBLE SHOT RT MAIN GEAR SWITCH, OHM CHECKED GOOD (.001 OHM) FOUND RT DOWNLOCK SWITCH OUT OF ADJUSTMENT. RERIGGED IAW 400XP MM 32-60-00 OPS CHECKED GOOD IN ALL FLAP AND GEAR CONFIGURATIONS. 2 H 7 2 4F 4 F RT A16SW E25EA 2007061800113 20070618 00113 CE 2007 6 18 DXTA200702223 1 20070529 A 3040 99120856 CONTROLLER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE ANTI ICE SYS INOPERATIVE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 371QS 7941 5600471 WITH THE W/S BLEED ANTI ICE ON LOW (APPROX 3-5 MINUTES AFTER BEING SWITCHED ON) THE W/S O'HEAT ILLUMINATED WITH SMOKE/HA ZE IN THE COCKPIT AND CABIN ALONG WITH STRONG BURNING ODOR. VERIFIED RIGGING AND OPERATION OF W/S BLEED AIR VALVES, FOU ND GOOD. VERIFIED OPERATION OF W/S BLEED AIR SHUTOFF/REGULATING VALVE, FOUND GOOD. VERIFIED TEMP SENSORS X-25,X-26, AND W/S O' HEAT SENSOR FOUND GOOD. VERIFIED 5 PSI SWITCH . FOUND GOOD. VERIFIED INPUT SIGNALS TO ANTI-ICE TEMP CONTROLLER FO UND GOOD. VERIFIED OPERATION OF TEMP CONTROLLER. FOUND CONTROLLER FAILED. OLD P/N: 9912085-6. OLD S/N: 3AN12. NEW P/N: 9 912085-6. NEW S/N: 2BC44. 2 L 7 2 4F 4 F RT A22CE E25EA 2007061400213 20070614 00213 NM 2007 6 14 UPS07M49893 1 20070418 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 35 LEFT FOUND WITH CORROSION. BN BORE CORROSION REMOVED SRM 51-21-01VII R38 BOTTOM - REMAIN BLENDOUT 0.046" DEEP REAMED TO 1.178" DIA REMAIN 0.033" DEEP EXCEED EO LIMIT. 10X MAG DVI C/O NO CO RROSION. BORE REAMED FURTHER TO 1.203" DIA EN1240-07. BLENDOUT VOID & BOTTOM PERI RADIUSED, SMOOTHEN & PROTECTED SRM 5 1-21-01VII R38. REPAIR SLEEVE BUSHING FAB PER EO BN BORE 35LT REPAIR C/O IAW EN1240-07. 2 L 7 3 4F RT A22WE 2007061400230 20070614 00230 CE 2007 6 14 DJFA2007053 1 20070430 A 5310 1284301073 SUPPORT BEAM BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE BS 190 CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 712TA 7313 RK186 DURING A SCHEDULED INSPECTION, MAINTENANCE DISCOVERED A CRACK ON THE SUPPORT BEAM BETWEEN FS 190.35 AND FS 196.46 ON THE RT SIDE. THE CRACK WAS .172 INCHES LONG AND EXTENDED FROM THE CENTER OF THE RADIUS CUT OUT ON THE IB SIDE. MAINTENANC E REPAIRED THE CRACKED STIFFNER. 2 H 7 2 4F 4 F RT A16SW E25EA 2007061500001 20070615 00001 CE 2007 6 15 DXTA200702211 1 20070522 A 2731 CONTROL SYSTEM CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE ELEVATOR TRIM OUT OF RIG E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 360QS 5600460 AT FL 280 AND 275 KTS RECEIVED AMBER ANNUNCIATOR (AP PITCH MIS-TRIM) AND (TRIM DN), MANUALLY DISCONNECTED AUTOPILOT AND ATTEMPTED TO TRIM DOWN MANUALLY AND ELECTRICALLY, BUT AIRCRAFT WAS FULLY TRIMMED NOSE DOWN TO THE STOP. IN THIS CONDITIO N AIRCRAFT STILL PITCHED UP. FOUND THE ELEVATOR TRIM CONTROL SYSTEM OUT OF RIG. RIGGED THE TRIM SYSTEM IAW MM. CHAPTER 2 7-31-00 SYSTEM OPS CHECKS GOOD AT THIS TIME 2 L 7 2 4F 4 F RT A22CE E25EA 2007061500018 20070615 00018 NE 2007 6 15 DXTA200702228 2 20070531 A 7200 ENGINE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE RIGHT FLAMED OUT E DXTA D RETURN TO BLOCK X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 315QS 5600315 DURING TAXI WHEN THE RT THROTTLE WAS ADVANCED, THEN MOVED TO IDLE, THE RT ENGINE FLAMED OUT. ADJUSTED RT THROTTLE IAW M M 76-11-00. OPS CK NORM. 2 L 7 2 4F 4 F RT A22CE E25EA 2007061500019 20070615 00019 CE 2007 6 15 DXTA200702229 1 20070531 A 2760 9156X166 COUPLER CESSNA 680 680CE 2076811 CE SPOILERS INOPERATIVE E DXTA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 07 381QS 593 6800097 ON TAKEOFF, WE RECEIVED A (NO TO CAS) MESSAGE THAT WAS CAUSED BY THE SPOILERS. REMOVED AND REPLACED RT SPEED BRAKE COUP LER. PERFORMED ELECTRONIC RIGGING IAW MM 27-60-00. OPS CHECK GOOD. 2 L 7 2 4F RC T00012WI 2007061500031 20070615 00031 EA 2007 6 15 TRAX200700785 1 20070603 A 5220 HINGE CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 906EV 7642 CREW ESCAPE HATCH LT ARM HINGE CRACKED . 2 L 7 2 4F RT A21EA 2007061500034 20070615 00034 EA 2007 6 15 TRAX200700788 1 20070604 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 559 UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 975EV 7599 PRESSURE FLOOR AFT PRESSURE BULKHEAD FS 559.0 RBL 9 SUPPORT O/B ATTACH ANGLE IS CRACKED WHERE IT ATTACHES TO FRAME 559. 2 L 7 2 4F RT A21EA 2007061500049 20070615 00049 EA 2007 6 15 TRAX200700794 1 20070605 A 5220 HANDLE CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 975EV 7599 EMERGENCY ESCAPE HATCH OUTER HANDLE CORRODED SEE EC/TC 600-52-0157 FOR ALL WORK ACCOMPLISHED. 2 L 7 2 4F RT A21EA 2007061500052 20070615 00052 WP 2007 6 15 DHL2007803522 1 20070602 A 5740 FITTING DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 RT WING T/E UPPER FITTING 0.250" CRACK STA XRS 421.000. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D. TORQUED IAW SRM 51-3-1 PG 2A. 2 L 7 4 4F RT 4A25 2007061500071 20070615 00071 EA 2007 6 15 TRAX200700784 1 20070603 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 640 S9R CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 906EV 7642 RT FRAME 640 RT IS CRACKED ON OUTBOARD FLANGE JUST ABOVE STR 9, RESOLVED ON W/O: 59833 TASKCARD: N/R-00072. FOUND CRACK ON RT FRAME 640.00 O/B FLANGE REPAIRED IAW ASA EC/TC REO 601R-53-61-2202 STEPS 1 TO 16. HFEC PERFORMED ON RT FRAME 640 .00 O/B FLANGE CUT-OUT. HEATHAIR W/O 36485. AMO NR 46.90, NO CRACKS FOUND. 2 L 7 2 4F RT A21EA 2007061500076 20070615 00076 EA 2007 6 15 TRAX200700808 1 20070607 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 909EV 7658 EXTERIOR PAX DOOR HANDLE IS CRACKED. REPAIRED IAW SRM 52-11-03. 2 L 7 2 4F RT A21EA 2007061500077 20070615 00077 NE 2007 6 15 ARWA20070605 2 20070610 A 7200 ENGINE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 LOW PRESSURE A ARWA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 19 526MD 46998 455425 DURING TAKEOFF ROLL, NR 3 ENGINE AT FIREWALL THRUST 98 PERCENT N1, N2, EGT AND FUEL FLOW LOW; ABORTED TAKEOFF. PERFORME D TROUBLESHOOTING IN ACCORDANCE WITH M/M 72-00-00; FLUSHED COMPRESSOR DISCHARGE SENSE LINE AND PERFORMED MPA RUN AT BLAS T FENCE, ALL PARAMETERS NORMAL. 2 L 7 3 4F 4 F A22WE E23EA 2007061500085 20070615 00085 NM 2007 6 15 07FDEA02065 1 20070604 A 5753 ARC27403 SKIN DOUG MD11 MD11 3023602 NM ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 EXISTING REPAIR, LT WING I/B FLAP UPPER SURFACE FOUND WITH EXTERNAL PATCH AT XIFH 233 YIFH 17. EXISTING REPAIR EVALUATE D AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-1 00. 2 L 7 3 4F RT A22WE 2007061500088 20070615 00088 NM 2007 6 15 07FDEA02084 1 20070607 A 5315 ADA8407503 FLOORBEAM DOUG MD11 MD11 3023602 NM ZONE 100 NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 EXISTING REPAIR, FUSELAGE STA 6-50 FLOORBEAM REPAIR AT RT BUTT LINE 60", AS SEEN FROM THE FWD LOWER CARGO COMPARTMENT, R EPAIR REQUIRES EVALUATION. EXISTING REPAIR EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-00-01 FIGURE 8 VOLU ME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007061500089 20070615 00089 NM 2007 6 15 07FDEA02109 1 20070612 A 5320 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 AFT CARGO RT L38, STA 1865 FOUND SPLICE DAMAGED. [06-18-07] REPAIR CARRIED OUT AS PER SRM 51-33-01 VOLUME II AND DRAWING AFA7105. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007061500104 20070615 00104 NM 2007 6 15 UPS07M49878 1 20070601 A 2432 3S2060DM169A3 CHARGER DOUG MD11 MD11F 3023600 NM MASTER BATTERY INOPERATIVE A IPXA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 01 259UP 48417 INSPECTION TYPE:N/A DIVERSION - BATTERY CHARGER LIGHT ILLUMINATED IN FLIGHT. T/S PER FIM 24-30-00 FIG 118. REPLACED BA TTERIES PER MM 24-30-02 AND BATTERY CHARGER PER MM 24-34-03. EMERGENCY POWER TEST OK PER MM 24-24-00-5, NO MSG NOTED. 2 L 7 3 4F RT A22WE 2007061500107 20070615 00107 CE 2007 6 15 LX5R200700004 1 20070605 A 5751 101130003135 BALANCE WEIGHT BEECH BEECH B300 B300 1159232 CE ZONE 600 DETACHED B LX5A K NONE O OTHER IN INSP/MAINT 1 GL 19 971LL 3367 803 FL267 UPON PILOT PREFLIGHT, IT WAS DISCOVERED THAT THE RIGHT HAND AILERON HAD SOMETHING LOOSE INSIDE MOVING AROUND. THE AIRCR AFT WAS BROUGHT INTO MAINTENANCE AND THE AILERON WAS REMOVED AND IT WAS DISCOVERED THAT PART OF THE BALANCE WEIGHT HAD C OME LOOSE. THE LEADING EDGE OF THE AILERON WAS DRILLED LOOSE AND IT WAS DISCOVERED THAT A CENTER SECTION OF THE OUTBOAR D BALANCE WEIGHT HAD BROKE OFF, APPROX 10 INCH PIECE. THE CAUSE IS UNKNOWN, IT BROKE AT THE CENTER RIVET AND THEN WORKE D LOOSE. INSTALLED A WHOLE NEW BALANCE WEIGHT AND REINSTALLED AILERON BACK ON AIRCRAFT. 2 L 7 2 4T RT A24CE 2007061500125 20070615 00125 NM 2007 6 15 UPS07M49903 1 20070419 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORIZ STAB BARREL NUT BORE NR 17 LEFT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38. BOTTOM REMAIN BLEND OUT 0.050" DEEP. BORE REAMED TO 1.067" DIA, REMAIN BLEND OUT 0.060" DEEP EXCEED EO LIMITS. 10X MAG DVI C/O NO CORROSION. BORE BLENDOUT & BOTTOM PERI, RADIUSED, SMOOTHEN & PROTECTED SRM 51-21-01 VII R38. REPAIR SLEEVE BUSHING FAB, PROTECTED & INSTALLED PER EO FIG 5. REPAIR C/O AT BORE NR 17 LEFT IAW EN1241-07. 2 L 7 3 4F RT A22WE 2007061500132 20070615 00132 NM 2007 6 15 UPS07M49910 1 20070405 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 12 LEFT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38. B OTTOM - SURF CLEANED. BORE REAMED TO 0.988" DIA REMAIN BLENDOUT 0.045" DEEP - EXCEED EO LIMITS. 10X MAG DVI C/O NO COR ROSION. BORE BLENDOUT & BOTTOM PERI RADIUSED, SMOOTHEN & PROTECTED SRM 51-21-01 VII R38. REPAIR SLEEVE BUSHING FAB, PR OTECTED & INSTALLED PER EO FIG 5. REPAIR C/O AT BARREL NUT BORE NR 12 LEFT IS ACCEPTABLE IAW EN1197-07. 2 L 7 3 4F RT A22WE 2007061500137 20070615 00137 NM 2007 6 15 UPS07M49922 1 20070331 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE LEFT NR 15 FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38. B OTTOM REMAIN BLENDOUT 0.100" DEEP. BORE REAMED TO 1.067" DIA REMAIN BLENDOUT 0.035" DEEP EXCEED EO LIMITS. 10X MAG DVI C/O NO CORROSION. BORE BOTTOM BLENDOUT & PERI RADIUSED, SMOOTHEN & PROTECTED SRM 51-21-01 VII R38. REPAIR SLEEVE BUSH ING FAB, PROTECTED & INSTALLED PER EO FIG 5. REPAIR C/O AT BN BORE NR 15 LEFT IS ACCEPTABLE IAW EN1183-07. 2 L 7 3 4F RT A22WE 2007061500141 20070615 00141 SO 2007 6 15 C2XA07ON006 1 20070607 A 3350 LIGHT EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14188 0929 SCHEDULED MX - 3A CHECK - ONT - DURING PRELIM INSPECTION QC INSPECTOR FOUND EMERGENCY LIGHTS ON EXIT SIGNS AROUND OVERWI NG EXIT INOPERATIVE. MX PERSONAL PERFORMED GROUND FUNCTIONAL CHECK OF OVERWING EMERGENCY LIGHTS GOOD. A/C WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2007061500148 20070615 00148 SO 2007 6 15 C2XA07IA133 1 20070606 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 34111 145659 IAH FLIGHT 2139, THE CREW REPORTED A STRONG ODOR OF FUEL DURING APU STARTS. MAINTENANCE OPERATIONALLY CHECKED THE APU S EVERAL TIMES WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007061500156 20070615 00156 NM 2007 6 15 UPS07M49932 1 20070414 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 34 RIGHT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38 BO TTOM - REMAIN BLENDOUT 0.050" DEEP BORE REAMED TO 1.178" DIA REMAIN BLENDOUT 0.080" DEEP EXCEED EO LIMITS. 10X MAG DVI C/O NO CORROSION. BORE BLENDOUT & BOTTOM PERI RADIUSED, SMOOTHEN & PROTECTED SRM 51-21-01VII R38. REPAIR SLEEVE BUSHIN G FAB, PROTECTED & INSTALLED PER EO FIG 5. REPAIR C/O AT BN BORE NR 34 RIGHT ACCEPTABLE IAW EN1222-07. 2 L 7 3 4F RT A22WE 2007061500166 20070615 00166 EU 2007 6 15 PG9A115821 1 20070605 A 6510 350A34021400 DRIVE SHAFT UROCOP EC130 EC130B4 8680989 EU TAIL ROTOR WORN B PG9A K NONE O OTHER IN INSP/MAINT 1 WP 19 130GC 1184 3562 DURING INSPECTION FOUND THE DRIVE SPLINES ON THE TR DS CENTER SECTION TO BE WORN BEYOND LIMITS. INSTALLED NEW TR DS. 1 G 7 2 3U H9EU 2007061500184 20070615 00184 CE 2007 6 15 AMWA85129BC 1 20070605 A 2432 1293640315 CHARGER BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MASTER BATTERY LOOSE A AMWA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 07 127ZV UE127 AFTER TAXI FROM GATE THE BATTERY CHARGE ANNUN ILLUM. AC RETURNED TO GATE WITH NO FURTHER INCIDENT. THIS BATTERY CHARGE ANNUN ILLUM WRITEUP IS CONSIDERED A NUISANCE AND EXTREME DISTRACTION TO THE PILOT. RESEATED A-130 PCB, OPS CHECKED GOO D. 2 L 7 2 4T 3 T RT A24CE E2NE 2007061800003 20070618 00003 EA 2007 6 18 QXEA200700917 1 20070529 A 5753 PANEL CNDAIR CL600 CL6002C10 1390015 EA TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC - RIGHT FLAP PANEL 684LB CHAFED. REPAIRED IAW SRM 51-12-00 AND 51-21-11. 2 L 7 2 4F RT A21EA 2007061800015 20070618 00015 NM 2007 6 18 DU4R2007139 1 20070530 A 5230 WEB BOEING 757 757232 1384965 NM CARGO DOOR CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 640DL 23994 FOUND WEB CORRODED AT AFT CARGO DOOR LOWER FWD CORNER BS 1380 AND S-27R BY REMOVING WEB. REPAIRED BY FABRICATING AND IN STALLING REPAIR WEB 4-1/2 BY 22 FROM 7075-T6 .071 IAW B757 SRM 51-40-02 AND 51-30-01. 2 L 7 2 4F RT A2NM 2007061800018 20070618 00018 EU 2007 6 18 AALA20070991 1 20070530 A 3350 LENS AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 80052 460 MIA - EMERGENCY LIGHT AT SEAT 24G HAS LENS MISSING. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 24G. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007061800020 20070618 00020 EU 2007 6 18 AALA20070992 1 20070530 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80052 460 MIA - EMERGENCY LIGHT AT SEAT 25G INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 25G. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007061800042 20070618 00042 NM 2007 6 18 QXEA200700940 1 20070610 A 7600 78249050 PCU DHAV DHC8 DHC8202 2809007 NM MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 368PH 14598 512 EUG FLIGHT NR 2166, AFTER STARTING ENGINES AND RUNNING CHECKLIST. ADDED POWER TO INITIATE RIGHT RUN OUT OF PARKING SPOT . UPON ADDING POWER TO NR 1 ENGINE, NOTICED TORQUE INCREASE RAPIDLY TO YELLOW ARC. SOUNDED AS IF PROP FEATHERED, BUT D ID NOT NOTICE NP GAUGE. RETURNED TO DISC AND ENGINE RETURNED TO NORMAL. MAINTENANCE REPLACED NR 1 ENGINE PCU IAW MTC 9 612201. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061800059 20070618 00059 NM 2007 6 18 AALA20070994 1 20070531 A 2520 10682 RECEPTACLE BOEING 757 757223 1384957 NM CABIN SHORTED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 608AA 27446 ORD T255/31MAY - PASSENGER REPORTED SPARKS AND SMOKE FROM UNDER SEAT. REMOVED VENT PANELS AT SEATS 15F AND 16F AND FOUN D AN APPARENT BEVERAGE SPILL ALONG WALL WITH SOME FLUID COMING IN CONTACT WITH A POWER PORT. REPLACED POWER PORT FROM 1 5DEF AND 17DEF, CONNECTORS, AND HARNESSES FROM POWER SUPPLY. 2 L 7 2 4F RT A2NM 2007061800066 20070618 00066 WP 2007 6 18 AALA20070981 1 20070529 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 258AA 49288 LGA - AISLE EMERGENCY LIGHTS AT RIGHT SEAT ROW 20 INOPERATIVE. RESEATED PUSH BACK PIN IN CONNECTOR FOR AISLE EMERGENCY LIGHTS AT RIGHT SEAT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007061800069 20070618 00069 NM 2007 6 18 AALA20070985 1 20070529 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 935AN 30081 DFW - AFT EMERGENCY LIGHT EXIT SIGN MISSING LENS. REPLACED LENS FOR AFT EMERGENCY LIGHT EXIT SIGN. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007061800073 20070618 00073 NM 2007 6 18 AALA20070987 1 20070530 A 3350 0201804002 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 649AA 24607 SFO - EMERGENCY LIGHT AT SEAT 17D MISSING LENS. REPLACED RED LENS FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007061800078 20070618 00078 NM 2007 6 18 AALA20071003 1 20070525 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 977AN 29550 TUL - EMERGENCY LIGHTS AT RIGHT FORWARD DOOR HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHTS AT RIGHT FORWARD DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007061800080 20070618 00080 EA 2007 6 18 QXEA200700926 1 20070525 A 5100 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA UNKNOWN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC - REFERENCE ITEM 12 DAMAGE NR 5 PER E/C R-53-455/3. REPAIRED IAW REO670-53-00-107. 2 L 7 2 4F RT A21EA 2007061800164 20070618 00164 SO 2007 6 18 UG8A2007PA03S 1 20070613 A 5740 ATTACH FITTING GULSTM G1159 G1159A 3970109 SO RROYCE SPEY SPEY5118 54523 EU LT WING CORRODED E UG8A K NONE O OTHER IN INSP/MAINT 1 GL 23 473KT 8701 438 LT AFT IB WING ATTACH FITTING HAS CORROSION AT OB EDGE AT FS 452, BL 33.COMPLIED WITH AIRCRAFT SERVICE CHANGE 229, WING TO FUSELAGE IB ATTACH CONNECTION FUSELAGE STATION 452 LT SIDE, REPLACEMENT/MODIFICATION. GENERATED FAA FORM 337. AIRCRA FT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A12EA E2EU 2007061800165 20070618 00165 CE 2007 6 18 200700017 1 20070609 A 2100 1N4005 DIODE BEECH 90 C90 1152913 CE PWA PT6 PT6* 52043 EA CONTROL SYSTEM OPEN E BAQA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 EA 03 90LF 11744 LJ852 AIR CONDITIONING CYCLING ON AND OFF, CAUSING LOAD METERS TO JUMP. TROUBLESHOT CONTROL SYSTEM FOUND HEATER/AC RELAY CORRO DED AND (2) DIODES PN 1N4005, 1 OPEN AND 1 VERY LOW RESISTANCE. IN THIS CONFIGURATION THE RESISTOR-START CONTROL OVERHE ATED CAUSING THE COMPRESSOR START RELAY, COMPRESSOR RUN RELAY, RESISTOR (START) ASSEMBLY, WIRING AND CONNECTOR TO BURN U P. REPLACED ALL FAULTY COMPONENTS, OPERATIONAL CHECK NORMAL. 1 L 7 2 3T 3 T 3A20 E2NE 2007061800167 20070618 00167 CE 2007 6 18 GUUA05280702 1 20070528 A 2730 CONTROL QUADRANT BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE ELEVATORS STUCK A GUUA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 17 231Y UE231 ELEVATOR CONTROL STUCK ON APPROACH / BINDING, ACCESSED AND INSPECTED BELLCRANKS, PULLEYS, PULLET GUIDES, CABLE RUNS, CAB LE PASS THROUGH. NO DEFECTS NOTED. ELEVATORS HAVE FREE UNOBSTRUCTED TRAVELS. TEST FLIGHT SATISFACTORY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007061800168 20070618 00168 CE 2007 6 18 GUUA06027001 1 20070602 A 3260 C2006 SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG FAILED A GUUA O OTHER N FALSE WARNING AP APPROACH 1 SO 17 190YV UE190 ON APPROACH LANDING GEAR SELECTED DOWN GEAR HORN CANNOT BE SILENCED. CLEANED LANDING GEAR SILENCE BUTTON. OPS CHECK SAT ISFACTORY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007061800169 20070618 00169 NM 2007 6 18 ASMF200706001 1 20070608 A 3250 BYPASS VALVE BOEING 777 777* UTILUSE NM NLG STEERING UNLOCKED W ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 774AM 28689 AIRCRAFT REJECTED TAKEOFF AT 50 KTS, STARTED THE TAKEOFF RUN, THE MAIN GEAR STEERING CONFIGURATION LIGHT TURNED ON AND T HE ALARM WAS ACTIVATED. MAINTENANCE PERSONNEL INSPECTED BOTH MAIN LANDING GEARS AND DETECTED THE RT SIDE BYPASS VALVE IN UNLOCK POSITION; IT WAS RE-ESTABLISHED TO THE LOCK POSITION AND TESTED IAW MM 32-53-03, ALL CORRECT. 2 L 7 2 4F RT T00001SE 2007061800171 20070618 00171 CE 2007 6 18 DXTA200702264 1 20070614 A 3244 TIRE CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE RT MLG FAILED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 672QS 5605663 RT MAIN TIRE BLEW UP UPON LANDING. [07-09-07] INSPECTED RIGHT MLG DOOR, LINKAGES, WIRING, STRUCTURE, AND HYDRAULIC LIN ES FOR DAMAGE. NO DAMAGE NOTED. REMOVED AND REPLACED WHEEL ASSY WITH O/H WHEEL ASSY IAW CE-560XL M/M CHAP 32-41-02. PERF ORMED ON GROUND POSITION OF ANTISKID FUNCTIONAL CHECK. NOTED LOOSE LOCKING WASHER ON LEFT ANTI SKID X-DUCER DRIVE CLIP. ADJUSTED LOCKING TENSION. SYSTEM CHECKS GOOD AT THIS TIME IAW CE-560XL M/M CHAP 32-44-00. TAXIED AIRCRAFT BACK TO POSITI ON BRAKING ACTION FELT NORMAL 2 L 7 2 4F 4 F RT A22CE E00059EN 2007061800172 20070618 00172 CE 2007 6 18 DXTA200702265 1 20070614 A 3150 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL WARNING LIGHT E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 910QS 7500110 PRIOR TO 80KTS (PRI STAB TRIM FAIL) AMBER CAS, CAUSED TO ABORT TAKEOFF. [07-09-07] PERFORMED OPS CHECK OF THE STAB TRI M SYTEM NO DEFECTS FOUND I/A/W CE750 M.M. CH 27-40. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007061800173 20070618 00173 CE 2007 6 18 DXTA200702266 1 20070614 A 2120 UNKNOWN CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE CABIN ODOR E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 601QS 5605301 AFTER TAKEOFF RECEIVED ACM OVERHEAT INDICATION WITH RT BLEED AIR AND RT ITT (RED FLAG) INDICATION, ALSO HAD A ODOR OF S OMETHING BURNED COMING OUT OF THE VENTS ITT WAS APPROXIMATELY BETWEEN 750-760 DEG F FOR 4-5 SECONDS. [07-09-07] REMOVE D AND REPLACED THE RT FLOW CONTROL VALVE W/A OVERHAULED UNIT AS PER THE CE560XL AMM CHAPTER 21-11-00. OPS CHECKS GOOD. L EAK CHECK SATISFACTORY 2 L 7 2 4F 4 F RT A22CE E00059EN 2007061800209 20070618 00209 2007 6 18 ASMF20070507 4 20070519 A 3442 20412170414 TRANSCEIVER DOUG DC9 DC987 3022087 WP WX RADAR FAILED W ASMF A UNSCHED LANDING O OTHER CR CRUISE 1 SW 23 754RA 3049 3049 49641 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, WEATHER RADAR FAILED IN FLIGHT. MAINTENANCE PERSONNEL REPLACED THE RADAR TRAN SCEIVER IAW MM 34-41-04 TESTED CORRECT. 2 L 7 2 4F RT A6WE 2007061800214 20070618 00214 NM 2007 6 18 AMTA200700258 1 20070520 A 2560 60B4001842 SENSOR BOEING 757 757* NM RROYCE RB211 RB211535E4 54555 NE L1 DOOR FAULTY A AMTA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 11 522TZ 32586 L1 DOOR SLIDELIGHT WILL NOT ILLUMINATE, BUT GIRT BARS VISUALLY ENGAGED RELAMP, NO HELP. REMOVED AND REPLACED NEW FWD L1 DOOR AFT SENSOR S10215, OPS CHECK NORMAL IAW WDM 25-66-11. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007061800216 20070618 00216 NM 2007 6 18 AMTA200700260 1 20070525 A 5512 SKIN BOEING 737 73783N 13844HI NM HORIZ STAB CRACKED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 305TZ 30706 LT HORIZONTAL STAB LWR SKIN CRACKED 2 PLACES 1 INCH AND 1.25 INCHES IB SIDE OF RIB STAB 129.50, STA 1131 AND 1138. REPA IRED SKIN CRACKS 55-10-01. (K) 10-26-07 INSTALL L/E SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2007061800217 20070618 00217 NE 2007 6 18 HEEA115748 1 20070601 A 3230 CONTROL VALVE SKRSKY S76 S76A 8143006 NE MLG MALFUNCTIONED B HEEA O OTHER J WARNING INDICATION CL CLIMB 1 SW 03 764P 760276 AFTER TAKEOFF FROM GC743, UNABLE TO RETRACT LANDING GEAR. RETURNED TO HOUMA WITH GEAR DOWN AS PER CHECK LIST. MAINTENA NCE RESET THE LANDING GEAR CONTROL VALVE. 1 G 7 2 3U H1NE 2007061800218 20070618 00218 2007 6 18 AMTA200700268 4 20070530 A 3460 FMC BOEING 737 73783N 13844HI NM COCKPIT MALFUNCTIONED A AMTA K NONE O OTHER TX TAXI/GRND HDL 1 GL 11 323TZ 30033 BOTH FMC LOST ALL INFORMATION ON TAXI IN. UNABLE TO RECORD DRIFT AND RES, GROUND SPEED. PERFORMED FMC BITE CHECK IAW F IM 34-61-00-810-801. SYSTEM PASSED NO FAULT FOUND. OK FOR SERVICE. (K) 2 L 7 2 4F RT A16WE 2007061800219 20070618 00219 NE 2007 6 18 HEEA115749 1 20070601 A 3110 CONNECTOR SKRSKY S76 S76C 8143008 NE DECU DIRTY B HEEA O OTHER J WARNING INDICATION CL CLIMB 1 SW 03 779P 760655 AFTER TAKE OFF FROM RIG #2 DECU DEGRADE FAULT ON CAUTION PANEL. BLEED VALVE #2 LVL-2 SHOWN. RETURNED TO HOUMA. MAINTE NANCE CLEANED CONNECTORS AND RESET DECU. 1 G 7 2 3U NC H1NE 2007061800220 20070618 00220 NM 2007 6 18 AMTA200700245 1 20070524 A 5753 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU T/E FLAP DENTED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 402TZ 24667 RT IB FLAP TRAILING WEDGE SECTION NUMEROUS NICKS AND DENTS ON LOWER SKIN. REPAIRED IAW EA 737-5753-09-A0858. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2007061800221 20070618 00221 NM 2007 6 18 AMTA200700247 1 20070524 A 4920 380029816 APU BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE APU BAY UNSERVICEABLE A AMTA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 522AT 37636 37636 29330 APU AUTO SHUTDOWN. ECU BITE SHOWS (HOT) FAULT. (K) REPLACED APU. OPS AND LEAK CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007061800227 20070618 00227 NM 2007 6 18 AMTA200700267 1 20070529 A 2160 CONTROLLER BOEING 737 73783N 13844HI NM CABIN TEMP MALFUNCTIONED A AMTA K NONE J WARNING INDICATION CL CLIMB 1 GL 11 310TZ 28243 RT PACK LIGHT CAME ON JUST AFTER TAKEOFF. LIGHT STAYED OFF AFTER RESET. MAX POWER T/O, OAT 28C. PERFORMED PACK/ZONE T EMP CONTROLLER BITE PROCEDURE IAW FIM 21-62-00-810-801. NO FAULTS NOTED, OK FOR SERVICE. (K) 2 L 7 2 4F RT A16WE 2007061800228 20070618 00228 2007 6 18 AMTA200700263 4 20070525 A 3460 1762000101 FMC BOEING 737 73783N 13844HI NM LEFT INOPERATIVE A AMTA K NONE O OTHER TX TAXI/GRND HDL 1 GL 11 304TZ 30675 LT FMC INOPERATIVE. REMOVED AND REPLACED LT FMC AND CROSS LOADED SOFTWARE INFORMATION, IAW MM 34-61-00-2. (K) 2 L 7 2 4F RT A16WE 2007061800229 20070618 00229 NM 2007 6 18 AMTA200700262 1 20070528 A 3020 7646B000 ANTI-ICE VALVE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE UNSERVICEABLE A AMTA K NONE J WARNING INDICATION CR CRUISE 1 GL 11 561TZ 9382 9382 33526 EICAS MSG LT ENG ANTI-ICE DISPLAYED AND ENGINE ANTI-ICE VALVE LIGHT. REMAINED ILLUMINATED WITH SWITCH ON. REMOVED AND REPLACED LT ENG ANTI-ICE VALVE IAW AMM 30-21-03-4. OPS CHECK NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007061800230 20070618 00230 2007 6 18 AMTA200700261 4 20070528 A 2310 TRANSCEIVER BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE HF COMM UNKNOWN A AMTA K NONE O OTHER CR CRUISE 1 GL 11 560TZ 33525 LT HF RADIO RECEPTION INOPERATIVE AT ALL CREW STATIONS. COULD NOT DUPLICATE ON GROUND IAW MM 23-11-00. SWAPPED HF TRAN CEIVER LT SN: 01412 WITH R/T TRANCEIVER SN: 01427 FOR FURTHER T/S. CONTACTED SFO AT FREQ. 5574. TRANS. 4 X 4. OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007061800231 20070618 00231 2007 6 18 AMTA200700272 4 20070603 A 3460 FMC BOEING 737 73783N 13844HI NM COCKPIT MALFUNCTIONED A AMTA K NONE J WARNING INDICATION CR CRUISE 1 GL 11 308TZ 28244 RT FMC FAIL, SINGLE FMC OPERATION NORMAL WITH FMC SELECTOR IN BOTH ON LT. UNABLE TO DUPLICATE FAULT. PERFORMED BITE IA W FIM 34-61-00-810-801, NO FAULTS NOTED. FMC OPS NORMAL. (K) 2 L 7 2 4F RT A16WE 2007061800234 20070618 00234 NM 2007 6 18 SWAA072872 1 20070607 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007061800235 20070618 00235 NM 2007 6 18 SWAA072873 1 20070607 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007061800236 20070618 00236 NM 2007 6 18 SWAA072874 1 20070607 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007061800237 20070618 00237 NM 2007 6 18 SWAA072870 1 20070607 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007061800239 20070618 00239 NM 2007 6 18 SWAA072871 1 20070607 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007061800241 20070618 00241 NM 2007 6 18 SWAA072878 1 20070607 A 5322 69353656 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007061800245 20070618 00245 NM 2007 6 18 SWAA072898 1 20070608 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 766SW 29806 DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007061800246 20070618 00246 NM 2007 6 18 SWAA072904 1 20070608 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007061800248 20070618 00248 NM 2007 6 18 SWAA072905 1 20070608 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007061800249 20070618 00249 EU 2007 6 18 UPS07149957 1 20070613 A 5610 WINDOW AIRBUS A300 A300F4622R 3930360 EU COCKPIT STUCK A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 166UP 0805 INSPECTION TYPE:N/A F/O SLIDING WINDOW WOULD NOT LATCH. RESET OUTSIDE RIGHT WINDOW. CLOSED WINDOW. 2 L 7 2 4F RT A35EU 2007061800251 20070618 00251 NM 2007 6 18 SWAA072900 1 20070608 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 766SW 29806 DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 9 ABC. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007061800256 20070618 00256 NM 2007 6 18 AMTA200700253 1 20070525 A 5320 FLOOR SUPPORT BOEING 737 73783N 13844HI NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 305TZ 30706 CORROSION ON FLOOR SUPPORT STRUCTURE STA 793, RBL 20. REMOVED CORROSION STA 793, RBL 20, SRM 51-10-02, ORIG MTL .100 LO SS IS .025 OUT OF LIMITS, SRM 53-00-53. REPLACED WITH NEW PA, RT SRM 53-60-15 AND SRM 51-40-02. (K) 10-26-07 REM OVED AND REPLACED STRAP SRM 51-40-02. INSTALLED THRESHOLD SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2007061800257 20070618 00257 NM 2007 6 18 AMTA200700259 1 20070523 A 2560 SENSOR BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE GIRT BAR OUT OF ADJUST A AMTA K NONE O OTHER TX TAXI/GRND HDL 1 GL 11 552TZ 32586 GIRT BAR ENGAGEMENT LIGHT EXTINGUISHES WITH EVACUATION SLIDE ARMING LEVER IN ARMED POS, AT ENTRY 1L. PERFORMED FIM 25-6 6-00. ADJUSTED CLEARANCE BETWEEN THE GIRT BAR SLIDER AND THE SENSOR IAW MM 25-66-11. CLEANED AND LUBRICATED GIRT BAR. OPS CHECKED GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007061800259 20070618 00259 SO 2007 6 18 RAIA00706004 1 20070605 A 4990 OIL SYSTEM EMB 145 EMB145 3260210 SO APU OVERSERVICED A RAIA D RETURN TO BLOCK W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 809HK 145187 FLT NR 5469 - STL - VISIBLE SMOKE IN COCKPIT AND CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THAT THE APU OIL WAS OVERSERVICED. MAINTENANCE DRAINED THE OIL AND OPS CHECKED THE BLEED SYSTEM. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2007061800261 20070618 00261 SO 2007 6 18 RAIA00706007 1 20070605 A 2150 7821009 PRESSURE SWITCH EMB 145 EMB145 3260210 SO NR 2 PACK MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 821HK 145068 FLT NR 5450 - STL - PACK 2 OVERLOAD. MAINTENANCE REMOVED AND REPLACED THE NR 2 PACK OVERPRESSURE SWITCH. OPS CHECKED G OOD. 2 L 7 2 4F RT T00011AT 2007061800262 20070618 00262 SO 2007 6 18 RAIA00706006 1 20070605 A 2731 4800101 SWITCH EMB 145 EMB145 3260210 SO PITCH TRIM MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 805HK 145096 FLT NR 3535 - RIC - MAIN PITCH TRIM INOP MESSAGE. MAINTENANCE REMOVED AND REPLACED TRIM SYSTEM CUTOUT SWITCH, OPS TEST GOOD AT THIS TIME. 2 L 7 2 4F RT T00011AT 2007061800263 20070618 00263 2007 6 18 SB07046 4 20070610 A 2565 D37022101 BOTTLE BOEING 737 7374B7 1384702 NM EVAC SLIDE LOW PRESSURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 1227 24556 MIA - DURING NEW LIVERY/PAINT VISIT, MAINTENANCE REPORTED THE RIGHT-HAND FORWARD SERVICE DOOR ESCAPE SLIDE NEEDLE READS NO GO. MAINTENANCE REMOVED AND REPLACED THE RIGHT-HAND FORWARD SERVICE DOOR ESCAPE SLIDE PER MM 25-61-35. 2 L 7 2 4F RT A16WE 2007061800264 20070618 00264 2007 6 18 WRNA200700028 4 20070605 A 2565 D29278123 SLIDE AIRBUS 300 A300B4203 3930306 EU LT DOOR DEPLOYED A WRNA K NONE O OTHER UK UNKNOWN 1 SO 05 510TA 100 ON GROUND, CREW OPENED LEFT HAND DOOR WITH DOOR ARMED, SLIDE WAS DEPLOYED. SLIDE WAS PLACED ON MEL 52-61-01 AND AIRCRAF T RELEASED FOR SERVICE. SLIDE WAS REPLACED ON 6-6-07 PER MM 25-61-00 PAGE 401. 2 L 7 2 4F RT A35EU 2007061800268 20070618 00268 EU 2007 6 18 WRNA200700029 1 20070607 A 2780 CHA704218 SHAFT AIRBUS 300 A300B4203 3930306 EU L/E SLAT JAMMED A WRNA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 05 505TA 271 AFTER LEAVING BLOCKS, SLATS WOULD NOT EXTEND, JAMMED, VIBRATION FELT IN AIRCRAFT. RETURNED TO BLOCKS. REPLACED SLAT TR ANSMISSION SHAFT ASSEMBLY AND SHOCK ABSORBER PER MM 27-81-12 PG 401 AND 27-81-29 PG 401. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A35EU 2007061800269 20070618 00269 NM 2007 6 18 SB07047 1 20070612 A 3260 MS25237387AS15 LIGHT BOEING 737 7374B7 1384702 NM COCKPIT BURNED OUT A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 440US 24811 IND - FLT 1215, ON APPROACH INTO IND, FROM CLT, CAPTAIN DID NOT RECEIVE A GREEN NOSE LANDING GEAR LIGHT AFTER EXTENDING GEAR. NOSE GEAR LIGHT WOULD NOT PRESS-TO-TEST OR MASTER TEST. CREW RECYCLED THE GEAR AND STILL NO GREEN LIGHT. CREW A CCOMPLISHED A MISSED APPROACH AND ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES. CREW DISCOVERED A LIGHT INDICATION PROBLEM. FLIGHT LANDED AND TAXIED TO THE GATE WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE NOSE LANDING GEAR GREEN LIGHTS BURNED OUT. RELAMPED LIGHTS. PRESS-TO-TEST AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A16WE 2007061800271 20070618 00271 2007 6 18 SWAA072919 4 20070607 A 2565 1061323468 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED MV1 CHECK, R1 DOOR EMERGENCY EVAC SLIDE DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007061800272 20070618 00272 NM 2007 6 18 SWAA072930 1 20070611 A 5610 141A481015 WINDOW BOEING 737 73776Q 13845AA NM COCKPIT ARCED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 550WN 30279 FLIGHT DECK L2 WINDOW ARCING DURING FLIGHT. REMOVED AND REPLACED L2 WINDOW PER MM. 2 L 7 2 4F RT A16WE 2007061900001 20070619 00001 NM 2007 6 19 SWAA072929 1 20070611 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 MID CABIN EMERGENCY EXIT LIGHTS STAY ON WITH SWITCH IN ARM POSITION. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007061900004 20070619 00004 NM 2007 6 19 SWAA072932 1 20070611 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 434WN 32454 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 2 ABC AND ROW 4 ABC. REMOVED AND REPLACED COVER PER M M. 2 L 7 2 4F RT A16WE 2007061900008 20070619 00008 NM 2007 6 19 SWAA072922 1 20070611 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900011 20070619 00011 2007 6 19 SWAA072920 4 20070608 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM EVAC SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM. 2 L 7 2 4F RT A16WE 2007061900012 20070619 00012 2007 6 19 SWAA072933 4 20070611 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007061900014 20070619 00014 NM 2007 6 19 SWAA072925 1 20070609 A 2560 PH22300L GLOWSTRIP BOEING 737 737317 138447P NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 4 ABC. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007061900018 20070619 00018 CE 2007 6 19 DXTA200702253 1 20070610 A 3260 65430087 UPLOCK SWITCH CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 377QS 8784 5600377 SELECTED GEAR UP ON DEPARTURE, RT MAIN AND RED GEAR UNSAFE LIGHTS STAYED ON. REMOVED AND REPLACED INOP R/H MLG UPLOCK S WITCH IAW CE560 M/M 32-30-01. OPS AND RIGGING CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2007061900020 20070619 00020 CE 2007 6 19 DXTA200702254 1 20070610 A 2930 99144644 PTU CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL HYD SYSTEM INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 913QS 1878 7500113 HYD A PRESSURE DROPPED TO 2000 PSI, FOLLOWED BY AMBER CAS (HYD LOW QTY B) AND (HYD O TEMP B) MESSAGES ILLUMINATED. REMO VED & REPLACED PTU, LH ENGINE DRIVEN HYD. PUMP & "A" HYD FILTER ASSEMBLY, IAW THE 750 MAINT. MANUAL 29-10-02, 29-10-09 & 29-20-04. OPERATIONAL/LEAK CHECK SATISFACTORY. REPLACED ALL 'A' HYD SYSTEM FILTER. LEAK CHECK SATISFACTORY. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007061900023 20070619 00023 CE 2007 6 19 DXTA200702255 1 20070610 A 2741 3094338 SWITCH CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL COCKPIT INOPERATIVE E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 978QS 4495 7500187 AFTER TAKEOFF, STAB TRIM WOULD ONLY TRIM NOSE UP ON THE LT SIDE. COULD NOT TRIM NOSE DOWN ON LT SIDE. REMOVED OLD PILOT S SIDE STAB TRIM SWITCH AND REPLACED WITH NEW SWITCH OPERATIONAL TEST GOOD. ALL WORK PERFORMED I.A.W. CH 27-13-00 OF THE CE750 M.M. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007061900024 20070619 00024 WP 2007 6 19 ASAA0781779 1 20070607 A 5320 993053875 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 RIGHT CUSP WEB CORRODED. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER PER SRM 53-05 AND 53-01. 2 L 7 2 4F RT A6WE 2007061900026 20070619 00026 CE 2007 6 19 DXTA200702256 1 20070611 A 3240 429271 CONTROL BOX CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE FWD E/E BAY FAULTED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 352QS 9237 5600352 THE BRAKES ON THE SIC SIDE OF THE AIRCRAFT MOMENTARILY FEEL INOP THEN AFTER SEVERAL MOMENTS AGGRESSIVELY GRAB WITH THE S AME AMOUNT OF PRESSURE. REMOVED FAULTY ANTI-SKID CONTROL BOX AND INSTALLED INSPECTED UNIT BY HYDRO-AIRE CRS#QD3R78SL. P ERFORMED OPERATIONAL CHECK GOOD. IAW C560 M.M. 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007061900027 20070619 00027 WP 2007 6 19 ASAA0781781 1 20070607 A 5320 993053877 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 RIGHT CUSP WEB CORRODED. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 53-01 AND 53-05. 2 L 7 2 4F RT A6WE 2007061900030 20070619 00030 NE 2007 6 19 DXTA200702257 2 20070611 A 7532 31J285704 SERVO CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LT BLEED VALVE INOPERATIVE E DXTA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 07 687QS 421 5605187 RT ENGINE WILL NOT MAKE TAKEOFF POWER 88.1 N1 WAS NEEDED AND IT WOULD ONLY GO TO 80 PERCENT. R&R BOV TORQUE MOTOR IAW P RATT & WHITNEY 545A MAINT. MANUAL 75-30-01 & COMPLETED SECONDARY ORIFICE CALIBRATION I.A.W 560 EXCEL M.M. 71-00-04 2 L 7 2 4F 4 F RT A22CE E00059EN 2007061900031 20070619 00031 SO 2007 6 19 C2XA07IA135 1 20070606 A 3350 66364 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14974 145161 DURING SCHEDULED MAINTENANCE THE LEFT AFT FLOOR PROXIMITY LIGHT WAS FOUND TO BE INOPERATIVE. THE EMERGENCY LIGHT STRIP WAS REMOVED AND REPLACED, OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED. 2 L 7 2 4T RT T00011AT 2007061900032 20070619 00032 CE 2007 6 19 DXTA200702258 1 20070612 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 371QS 5600471 ANTI SKID SEEMS TO ACTIVATE AROUND 40 KNOTS. BRAKES SEEM TO GRAB AND RELEASE SERVERAL TIMES. TAXIED AIRCRAFT WITH ANTI -SKID ON. WHEN TAXI WAY WET AND DRY. SYSTEM OPERATIONAL CHECKS GOOD. NO DEFECTS NOTED. WORK DONE IAW. CE 560 MM CHAP. 32 -41-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007061900038 20070619 00038 EA 2007 6 19 COMA0760425 1 20070608 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 409CA 7441 FLIGHT 4940 - FLAPS FAIL AT 30 DEGREES ON APPROACH, AIRCRAFT LANDED SAFELY. COMPLIED WITH AD 2006-12-21 FLAP CAUTION ME SSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAU TION MESSAGES. 2 L 7 2 4F RT A21EA 2007061900041 20070619 00041 EA 2007 6 19 COMA0760426 1 20070609 A 5346 SKIN CNDAIR CL600 CL6002B19 1900309 EA ENGINE BEAM CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 969CA 7141 ENGINE BEAM UPPER CENTER SKIN IS CRACKED ON AFT SIDE FS 640 BETWEEN RBL 0 AND RBL 9 AT FIRE LOOP FASTENER HOLE. REPAIRE D UPPER AND LOWER ENGINE BEAM CENTER SKINS WITH A PERMANENT REPAIR PER REO 601R-53-61-345 REV D. 2 L 7 2 4F RT A21EA 2007061900042 20070619 00042 EA 2007 6 19 COMA0760427 1 20070609 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA RT MLG WW CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 969CA 7141 WHEEL WELL AFT WEB IS CRACKED AT FS 559.00 BETWEEN RBL 9 AND 18 AT RIGHT AILERON BELLCRANK ATTACH HOLES. CUT OUT DAMAGE AND INSTALLED A PERMANENT REPAIR DOUBLER PER COMAIR SR10-5341-0001 REV (A) SECTION 1. 2 L 7 2 4F RT A21EA 2007061900043 20070619 00043 EA 2007 6 19 COMA0760428 1 20070609 A 7830 THRUST REVERSER CNDAIR CL600 CL6002B19 1900309 EA LEFT MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 420CA 7451 FLIGHT 5518 - LEFT THRUST REVERSER UNLOCKED MESSAGE IN FLIGHT. AIRCRAFT DIVERTED TO HPN AND LANDED SAFELY. DEFERRED PE R MEL 78-30-01. 2 L 7 2 4F RT A21EA 2007061900044 20070619 00044 EA 2007 6 19 COMA0760429 1 20070611 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 914CA 32873 7012 DURING HMV-7 INSPECTION, FOUND CRACKS IN 559 RIGHT VERTICAL WEB. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW BOMBARDIER RE O 601R-53-41-535. 2 L 7 2 4F RT A21EA 2007061900049 20070619 00049 WP 2007 6 19 UPS07849943 1 20070606 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C2 RIGHT WING O/B LEADING EDGE UPPER RIB CRACKED AT STA XFS 616. STOP DRILLED CRACKED RIB AT STA XFS 61 6 IAW SRM 57-02-00. FABRICATED AND INSTALLED REPAIR ANGLE AT STA XFS 616 IAW SRM 57-02-00 FIG 2. 2 L 7 4 4F RT 4A25 2007061900050 20070619 00050 WP 2007 6 19 UPS07849944 1 20070606 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE UPPER RIB CRACKED AT STA XFS 672. STOP DRILLED CRACKED RIB AT STA XFS 67 2 IAW SRM 57-02-00. FABRICATED AND INSTALLED REPAIR ANGLE AT STA XFS 672 IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2007061900051 20070619 00051 WP 2007 6 19 UPS07849945 1 20070608 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 RIGHT WING CENTER LEADING EDGE UPPER RIB CRACKED AT STA XS 497. STOP DRILLED CRACKED RIB AT STA XS 4 97 IAW SRM 57-2-0 FIG 2. FABRICATED AND INSTALLED REPAIR ANGLE AT STA XS 497 IAW 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2007061900052 20070619 00052 WP 2007 6 19 UPS07849946 1 20070608 A 5210 SKIN DOUG DC8 DC873F 302199F WP L2 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 L2 DOOR INNER SKIN BROKEN AT LWR HINGE ARM CUTOUT. REMOVED BROKEN STRAP AT L2 DOOR ARM CUTOUT IAW SR M 51-3-0. FABRICATED AND INSTALLED REPAIR STRAP AT L2 DOOR ARM CUTOUT IAW DWG 5750988, AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 2007061900055 20070619 00055 WP 2007 6 19 UPS07849951 1 20070530 A 5312 PRESSURE PANEL DOUG DC8 DC873F 302199F WP NLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C1 RIGHT NLG TUNNEL INTERGRANULAR CORROSION AND GUSSET MISSING ON UPPER PRESSURE DECK (CEILING) STA -32 RBL 58. REMOVED FINGER DOUBLER AND CUT OUT DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS IAW SRO 8530026, SRM 51-1-21, 51-20D AND APPROVED EA RESPONSE. 2 L 7 4 4F RT 4A25 2007061900057 20070619 00057 WP 2007 6 19 UPS07849954 1 20070609 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP CARGO BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:N/A PIT 33 HAS HOLE IN FLOOR ON LEFT SIDE APPROX 3 FEET AFT OF DOOR MARKED. REPAIRED PIT 33 FLOOR PANEL AS PER EO DC8-5320-8724-A. 2 L 7 4 4F RT 4A25 2007061900059 20070619 00059 NM 2007 6 19 UPS07M49939 1 20070611 A 2751 TRANSMITTER DOUG MD11 MD11F 3023600 NM LT FLAP INOPERATIVE A IPXA A UNSCHED LANDING N FALSE WARNING UK UNKNOWN 1 SO 01 255UP 48404 INSPECTION TYPE:N/A ATB - LEFT I/B FLAP INDICATION 20 DEGREES WITH STICKER SHAKER. EMERGENCY DECLARED TO HAVE EQUIPMENT STANDING BY PRECAUTIONARY. FOUND LEFT INBOARD FLAP POSITION XMT INOP. REPLACED PER MM 27-54-24-4, RAN SYSTEM THROUGH FULL OPS CHECK. OK FOR CONTINUED SERVICE. ACCOMPLISHED CAT IIIB TEST PER MM 24-54-00, SYSTEM TEST OK. 2 L 7 3 4F RT A22WE 2007061900060 20070619 00060 NM 2007 6 19 UPS07M49956 1 20070610 A 5610 WINDOW DOUG MD11 MD11F 3023600 NM COCKPIT BINDS A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 252UP 48768 INSPECTION TYPE:N/A F/O'S CLEARVIEW WINDOW WILL NOT CLOSE HANDLE RATCHETS OVER. BACK WINDOW WILL NOT PULL IN. ROLLER D OES NOT CONTACT BUMP STOP. CYCLED F/O'S WINDOW AND CHECKED PER MM 56-12-01-5, OPS OK AT THIS TIME. 2 L 7 3 4F RT A22WE 2007061900063 20070619 00063 SO 2007 6 19 C2XA07SH032 1 20070610 A 5730 14571503403 PANEL EMB 145 EMB145LR 3260212 SO WING CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14960 145100 SHV - DURING C-CHECK MAINTENANCE FOUND OVER THE WING TO FUSELAGE PNL 195 WITH CORRODED BONDING STRAPS. MAINTENANCE REPA IRED PNL 195 IAW EC 5750-01315, AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061900067 20070619 00067 NM 2007 6 19 MWEA070142 1 20070611 A 7830 7150923REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 918ME 55180 RIGHT ENGINE THRUST REVERSER UPPER DEFLECTOR DOOR ZEE FRAME IS CRACKED AT THE INBOARD END AT STATION 35. FABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007061900068 20070619 00068 NM 2007 6 19 MWEA070143 1 20070611 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 918ME 55180 RIGHT ENGINE TRHUST REVERSER UPPER DEFLECTOR DOOR ZEE FRAME IS CRACKED AT THE OUTBAORD END AT STATION 26. FABRICATED AN D INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007061500160 20070615 00160 EU 2007 6 15 PG9A115813 1 20070525 A 6220 704A33640088 FREQ ADAPTER UROCOP EC130 EC130B4 8680989 EU MAIN ROTOR CRACKED B PG9A K NONE O OTHER IN INSP/MAINT 1 WP 19 136PH 2440 3896 DURING THE DAILY INSPECTION, FOUND A VERTICLE CRACK EXTENDING UP FROM THE LOWER HOLE ON THE AFT SIDE OF THE ADAPTER. IN STALLED 3 SERVICEABLE ADAPTERS. 1 G 7 2 3U H9EU 2007061500164 20070615 00164 EU 2007 6 15 PG9A115817 1 20070508 A 6700 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU COLLECTIVE PITCH MALFUNCTIONED B PG9A O OTHER J WARNING INDICATION LD LANDING 1 WP 19 133GC 183 3883 FAIL CODE 122 DISPLAYED ON VEMD AFTER FLIGHT. REPLACED COLLECTIVE PITCH POTENTIOMETER. 1 G 7 2 3U H9EU 2007061500168 20070615 00168 NM 2007 6 15 CALA0700298 1 20070608 A 5311 6546551 FRAME BOEING 737 7373T0 1384582 NM BS 807 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12313 23364 INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 807 BETWEEN STRINGERS 8R AND 9R. THE FRAME WAS REPAIRED IAW E CRA 5310-04637. 2 L 7 2 4F RT A16WE 2007061500169 20070615 00169 EU 2007 6 15 HEEA115421 1 20070507 A 7700 C16196AB PROBE UROCOP EC135 EC135P2 5620027 EU UNKOWN CORRODED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 326PH 417 0435 CORRODED. SENT TO MFG FOR CREDIT. 1 G 7 2 3U H88EU 2007061500180 20070615 00180 CE 2007 6 15 DXTA200702245 1 20070606 A 2721 UNKNOWN CESSNA 680 680CE 2076811 CE RUDDER TRIM UNKNOWN E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 381QS 6800097 AIRCRAFT REQUIRES 2/3 SCALE LT RUDDER TRIM TO MAINTAIN COORDINATED FLIGHT. [07-09-07] RUDDER SKIN DAMAGED AT UPPER, MI DDLE AND LOWER RUDDER HINGE AREA. REMOVED RUDDER AND REPLACED WITH REPAIRED UNIT FROM CESSNA ICT RS CNQR918C PER 680 MM CH 55-40-00. OPERATIONAL AND TRAVEL CHECK OF RUDDER AND RUDDER TRIM GOOD. 2 L 7 2 4F RC T00012WI 2007061500208 20070615 00208 2007 6 15 FJ7A115621 2 20070524 A 7261 350A54113800 VENT LINE UROCOP EC130 EC130B4 8680989 EU ENGINE OIL SYS CRACKED E FJ7A K NONE O OTHER IN INSP/MAINT 1 SO 19 174AM 245 4007 CLAMP WELDED TO TUBE, CRACKED, LEAVING TUBE UNSUPPORTED. 1 G 7 2 3U H9EU 2007061800002 20070618 00002 EA 2007 6 18 QXEA200700916 1 20070529 A 5753 PANEL CNDAIR CL600 CL6002C10 1390015 EA TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC - RIGHT FLAP PANEL 684DB CHAFED. REPAIRED IAW SRM 51-2-00 AND 51-21-11. 2 L 7 2 4F RT A21EA 2007061800025 20070618 00025 NM 2007 6 18 AALA20070975 1 20070528 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 907AN 29509 DFW - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 5E INOPERATIVE. REPAIRED CONNECTOR UNDER SEAT 5E FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007061800029 20070618 00029 NM 2007 6 18 AALA20070977 1 20070528 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 907AN 29509 DFW - SEAT MOUNTED EMERGENCY LIGHT AT FORWARD SEAT 14D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHT AT FORWARD SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007061800061 20070618 00061 NM 2007 6 18 AALA20070995 1 20070531 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 788AN 30011 JFK - EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT T00001SE 2007061800070 20070618 00070 NM 2007 6 18 AALA20071000 1 20070525 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 977AN 29550 TUL - EMERGENCY LIGHTS AT LEFT AFT OVERWING DOOR HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHTS AT LEFT AFT OVERWI NG DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007061800072 20070618 00072 NM 2007 6 18 AALA20070986 1 20070530 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 649AA 24607 SFO - EMERGENCY LIGHT AT SEAT 17D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A2NM 2007061800074 20070618 00074 NM 2007 6 18 AALA20070988 1 20070530 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 761AJ 31478 MIA - EMERGENCY LIGHTS AT AFT CABIN CENTER INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT CABIN CENTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007061800075 20070618 00075 NM 2007 6 18 AALA20070989 1 20070530 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 761AJ 31478 MIA - EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT NUMBER FOU R DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007061800082 20070618 00082 EA 2007 6 18 QXEA200700928 1 20070527 A 5100 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA UNKNOWN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 619QX 10246 C1 OKC - REFERENCE ITEM 4 AND 6 DAMAGE NR 2A AND 2B PER E/C R-53-455/3. REPAIRED IAW REO670-53-00-107. 2 L 7 2 4F RT A21EA 2007061800083 20070618 00083 NM 2007 6 18 QXEA200700964 1 20070615 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY MALFUNCTIONED A QXEA O OTHER N FALSE WARNING AP APPROACH 1 NM 09 379PH 15890 1166 530 SEA FLIGHT NR 2015 ON APPROACH SMOKE WARNING ILLUMINATED FOUR TIMES FOR APPROXIMATELY TWO SECONDS EACH TIME. NO OTHER A BNORMAL INDICATIONS NOTED. MAINTENANCE REPLACED NR 2 AFT BAGGAGE SMOKE DETECTOR PER D8 AMM 26-15-00, PAGE 501-502. OPE RATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061800087 20070618 00087 NM 2007 6 18 HALA0700249 1 20070611 A 2720 59140665583 ACTUATOR BOEING 717 717200 1383700 NM RUDDER LEAKING A HALA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 475HA 9229 55121 ON TAXI CHECKS, RUDDER CONTROL CHECK REQUIRED APPROX TWICE THE EFFORT TO DEFLECT THE RUDDER. HYD PRESSURE = 3000 PSI. TROUBLE SHOT AND FOUND RUDDER PEDALS STIFF, FOUND POWER PACK BYPASSING. REMOVED RUDDER HYDRAULIC ACTUATOR PER AMM 27-28 -02. INSTALLED RUDDER HYDRAULIC ACTUATOR PER AMM 27-23-02-400-801, STEP 3.A-3G2. 2 L 7 2 4F TR A6WE 2007061800097 20070618 00097 NM 2007 6 18 QXEA200700943 1 20070613 A 3260 PROXIMITY SENSOR BOMBDR DHC8 DHC8402 1390042 NM RT MLG DOOR OUT OF ADJUST A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 416QX 4083 PDX FLIGHT NR 2455: IN CRUISE, LT DOOR AND RT DOOR LIGHTS CYCLED AMBER. SOUNDED AND FELT LIKE DOORS CYCLED OPEN THEN CL OSED. MAINTENANCE FOUND RT MLG DOOR PROX SENSOR IN 'FAR' CONDITION. ADJUSTED SENSOR TO 'NEAR' PROXIMITY IAW Q400 AMM T ASK 32-61-06-830-801. PERFORMED LANDING GEAR EXTENSION SPEED EXCEEDANCE CHECK IAW AM TASK 05-50-32-280-801. OPS CHECK GOOD. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061800099 20070618 00099 NM 2007 6 18 07FDEA02039 1 20070601 A 5710 ARB75801 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 EXISTING REPAIR, DOUBLER PATCH FOUND ON LT WING L/E AT XIS247. REPAIR CARRIED OUT AT DOUBLER PATCH ON LT WING L/E AT XI S247 AS PER FEDEX EA NR 1- 5710-112420, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007061800183 20070618 00183 CE 2007 6 18 AMWA84889BC 1 20070525 A 2431 11436105925 POWER UNIT BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA DC WORN A AMWA K NONE J WARNING INDICATION CR CRUISE 1 CE 07 133YV UE133 AFTER TAKEOFF, BATTERY CHARGE ANNUN ILLUM. AC CONTINUED TO LIT AND LANDED WITH NO FURTHER INCIDENT. THIS BATTERY CHARG E ANNUN ILLUM IS CONSIDERED A NUISANCE WRITEUP AND A DISTRACTION TO THE PILOT. REMOVED AND REPLACED DC POWER PANEL. 2 L 7 2 4T 3 T RT A24CE E2NE 2007061800184 20070618 00184 2007 6 18 DXTA200702250 4 20070607 A 3400 8220320003 DAU AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE NOSE AVIONICS BA INOPERATIVE E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 298QS 6653 98 WE GOT THE NO TAKE-OFF AURAL WARNING WITH NO TAKEOFF ANNUCIATE LIGHT ON TAKE OFF. REMOVED AND REPLACED DATA AQUISITION U NIT (DAU-4000) WITH OVERHAULED UNIT. PERFORMED OPS CHECK OF DAV AND TAKEOFF WARNING SYSTEM. OPS CHECK GOOD. WORK 2 K 7 2 4F 4 F RT A50NM E44NE 2007061800188 20070618 00188 NM 2007 6 18 QXEA200700949 1 20070609 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - SEAT TRACK NR 8 AT STATION X570 TO X590, X620, X634, X664 HAS MINOR SRATCHES AND CHAFES. REPAIRED IAW RD8/4-53 -884. 2 H 7 2 4T RT A13NM 2007061800199 20070618 00199 CE 2007 6 18 DJFA2007061 1 20070426 A 5511 45A21104641 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 491CW 8092 RK91 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE LT IB HORIZONTAL STA BILIZER, THE LT RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. MAINTENANCE REPLACED BOTH RIBS. 2 H 7 2 4F 4 F RT A16SW E25EA 2007061800212 20070618 00212 WP 2007 6 18 AMTA200700248 1 20070524 A 3397 CONNECTOR LKHEED 1011 1011* WP RROYCE RB211 RB211535E4 54555 NE CABIN CONTAMINATED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 162AT 293A1220 FWD GALLEY AND FIRST SECTION OF ESCAPE PATH LIGHTING RT SIDE INOPERATIVE. SYS WAS SHORTED BY WATER. DRIED CONNECTORS A ND INSULATED THEM. OPS CHECK NORMAL. (K) 2 L 7 3 4F 4 F A23WE E12EU 2007061800215 20070618 00215 CE 2007 6 18 DXTA200702213 1 20070522 A 2721 INDICATION SYS CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE RUDDER TRIM OUT OF RIG E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 328QS 5600428 RUDDER TRIM OUT OF RIG. WILL TRIM FULL LT AND BACK TO CENTER, WILL NOT TRIM FULL RT. TROUBLESHOT SYSTEM, FOUND INDICATO R OUT OF RIG AND CONTACTING PEDESTAL, RIGGED INDICATOR IN THE CONTROL WHEEL. OPERATION IS SMOOTH AND CORRECT, TRAVELS A RE WITHIN LIMITS AT THIS TIME IAW MM 27-21-00 AND 27-21-04. 2 L 7 2 4F 4 F RT A22CE E25EA 2007061800223 20070618 00223 CE 2007 6 18 DXTA200702224 1 20070530 A 2750 MP50G4 DRIVE UNIT CESSNA 750 750 2076810 CE TE FLAPS INOPERATIVE E DXTA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 07 945QS 8747 7500029 DURING FINAL APPROACH, WHEN FLAPS WERE SELECTED TO 35*, FLAPS FAIL LIGHT ILLUMINATED AND FLAPS STOPPED LOWERING AT ABOUT 20*. OPS CHECKED FLAP SYS ON GROUND. CHECKED GOOD. NO BITE CODES ON FLAP CONTROLLER. PERFORMED 750 FLAP T/S AND FOUND S USPECT PDU. REMOVED PDU AND INSTALLED OVERHAULED PDU. OPS CHECK GOOD. NO BITE CODE PRESENT. IAW CESSNA 750 M/M 27-50-00. 2 L 7 2 4J RT T00007WI 2007061800233 20070618 00233 NM 2007 6 18 AMTA200700269 1 20070601 A 5414 SKIN BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE NR 2 PYLON DAMAGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 518AT 27974 NR 2 PYLON LOWER SIDE STRUCTURE EXPOSED TO HIGHT HEAT IN AREA OF HP-6 ENGINE PNEUMATIC DUCT AREA. AREA WAS REPAIRED IAW ERA 757-54R-6102 AND SAA EA 757-54-00-09-AO778, DATED 4-20-07, FAA FORM 8100-9/ 337 TIME LIMITED. REPAIR FROM 4/20/07 VALID FOR 24 MONTHS. (K) METAL CONDITION READINGS TAKEN AND SENT TO ENGINEERING. 24 MO TEMP REPAIR SAA EA 757-5400-09-A 0778 TRACKED BY ATA ER/A757-54R-6102. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007061800242 20070618 00242 NM 2007 6 18 SWAA072877 1 20070607 A 5322 69353656 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007061800250 20070618 00250 NM 2007 6 18 SWAA072906 1 20070608 A 3350 OL3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007061800255 20070618 00255 NM 2007 6 18 KCSA071189 1 20070611 A 5315 FITTING BOEING 747 747221F 1384868 NM FUSELAGE GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 RIGHT BS 1820 FLOORBEAM END FITTING, FWD TWO FASTENERS HOLES GOUGED AND ELONGATED. 2 L 7 4 4F A20WE 2007061900003 20070619 00003 NM 2007 6 19 SWAA072924 1 20070608 A 3350 311500 LENS BOEING 737 7373T5 1384608 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED C1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT MISSING LENS AT ROW 2 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007061900005 20070619 00005 2007 6 19 SWAA072931 4 20070611 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 727SW 27859 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007061900007 20070619 00007 NM 2007 6 19 SWAA072926 1 20070611 A 5311 6546525 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900013 20070619 00013 CE 2007 6 19 DXTA200702251 1 20070610 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG SEIZED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 352QS 5600352 THE BRAKES ON THE SIC SIDE OF THE AIRCRAFT MOMENTARILY FEEL INOP THEN AFTER SEVERAL MOMENTS AGGRESSIVELY GRAB WITH THE S AME AMOUNT OF PRESSURE. BLED LT AND RT BRAKES. FOUND EVIDENCE OF AIR IN RT BRAKES. BLED BOTH L/H AND R/H AN ADDITIONAL 4 TIMES TO MAKE SURE ALL THE AIR WAS OUT OF THE SYSTEM. OPS CHECKED GOOD. WORK DONE IAW CE-560 M/M 32-42-00. ALSO INSPEC T ANTI-SKID CONTROL BOX AND FAULT DISPLAY UNIT FOR ANY LOOSE CONNECTIONS OR TRIPPED INDICATORS. OPS CHECKED GOOD IAW CE- 560 M/M 32-42-08 . 2 L 7 2 4F 4 F RT A22CE E25EA 2007061900015 20070619 00015 CE 2007 6 19 DXTA200702252 1 20070610 A 3610 W93224E SEAL CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE DUCT LEAKING E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 810QS 3313 5600625 LT FIRE LIGHT ILLUMINATED DURING CLIMBOUT, DEPARTING. TROUBLESHOT ENG FIRE LIGHT- FOUND APPROX 6" OF FIRELOOP TOUCHING BLEED AIR LINE AND 4 BLEED AIR WIGGINS FITTINGS LEAKING- REPLACED 8 EA. SEALS LEAKED CHECKED SATISFACTORY ALL WORK I/A/W CE560E MM 30-21-01. 2 L 7 2 4F 4 F RT A22CE E00053EN 2007061900022 20070619 00022 WP 2007 6 19 ASAA0781778 1 20070603 A 5321 INSERT DOUG DC9 DC983 3022083 WP FLOOR PANEL CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 CABIN FLOOR PANEL HAS NUMEROUS CORRODED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND DWG 4932106. 2 L 7 2 4F RT A6WE 2007061900028 20070619 00028 WP 2007 6 19 ASAA0781782 1 20070607 A 5320 993053866 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 RIGHT CUSP WEB CORRODED. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 53-05. 2 L 7 2 4F RT A6WE 2007061900033 20070619 00033 EA 2007 6 19 COMA0770032 1 20070606 A 2760 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA SPOILER SYS MALFUNCTIONED A COMA K NONE N FALSE WARNING AP APPROACH 1 SO 01 642CA 10125 FLIGHT 5521- ON APPROACH RECEIVED AN O/B SPOILERONS CAUTION MESSAGE AND O/B FLIGHT SPOILERONS CAUTION MESSAGE. PERFORME D SYSTEM RESET AND RAN POST TEST, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007061900046 20070619 00046 EA 2007 6 19 COMA0760430 1 20070611 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 914CA 32873 7012 CRACK ON LOWER VERTICAL STIFFENER LBL 27, FS 559. REPAIRED CRACK ON INBOARD STIFFENER AT FS 559, LBL 27 PER REO 601R-53 -41-056. 2 L 7 2 4F RT A21EA 2007061900047 20070619 00047 2007 6 19 COMA0760431 4 20070606 A 3442 RADAR CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 510CA 7802 FLIGHT 5116 - RADAR INOP, TESTED NORMAL ON THE GROUND, AIRCRAFT LANDED SAFELY IN ATL. PERFORMED SYSTEM RESET, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007061900053 20070619 00053 WP 2007 6 19 UPS07849947 1 20070606 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE UPPER RIB CRACKED AT STA XFS 634. STOP DRILLED CRACKED RIB AT STA XFS 63 4 IAW SRM 57-03-03-0. FABRICATED AND INSTALLED REPAIR ANGLE AT STA XFS 634 IAW SRM 57-02-00 FIG 2. 2 L 7 4 4F RT 4A25 2007061900064 20070619 00064 SO 2007 6 19 C2XA07SH033 1 20070610 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14960 145100 SHV - DURING C-CHECK MAINTENANCE FOUND LEFT OMEGA BEAM FROM FRAME 18 TO 23 WITH CORROSION. MAINTENANCE REPAIRED LEFT OM EGA BEAM AT FRAME 18 TO 23 IAW SRM 51-40-02. PAINTED & INSTALLED NUT PLATES IAW EC 5320-01140 & EC 5320-01137. AIRCRAF T WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061900066 20070619 00066 NM 2007 6 19 MWEA070141 1 20070611 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 918ME 55180 RIGHT ENGINE THRUST REVERSER UPPER DOOR ZEE FRAME IS CRACKED AT THE INBOARD END AT STATION 26. FABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007061900069 20070619 00069 NM 2007 6 19 MWEA070144 1 20070611 A 7830 7150923REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 918ME 55180 RIGHT ENGINE THRUST REVERSER UPPER DEFLECTOR DOOR ZEE FRAME IS CRACKED AT THE OUTBOARD END AT STATION 35. FABRICATED AN D INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007061900071 20070619 00071 NM 2007 6 19 MWEA070146 1 20070611 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 918ME 55180 LEFT ENGINE THRUST REVERSER UPPER DEFLECTOR DOOR ZEE FRAME IS CRACKED AT THE OUTBOARD END AT STATION 26. FABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007061900073 20070619 00073 NM 2007 6 19 MWEA070148 1 20070611 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM TRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 918ME 55180 LEFT ENGINE THRUST REVERSER LOWER DEFLECTOR DOOR ZEE FRAME IS CRACKED AT THE INBOARD END AT STATION 26. FABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007061900084 20070619 00084 2007 6 19 YENA2007051 4 20070613 A 3444 WARNING SYSTEM AIRBUS 320 A320232 3930326 EU GPWS SYSTEM MALFUNCTIONED A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 522JB 1464 FLT 754, CUN-JFK, APPROX 1800Z, FAINT ELECTRICAL SMELL IN COCKPIT WHEN NAV GPWS FAULT ECAM APPEARED. SMELL WENT AWAY WH EN SYSTEM WAS TURNED OFF. ACCOMPLISHED FIM TASK 24-00-00-810-823. EVIDENCE OF SMOKE ODOR DISAPPEARED AS PER FLT CREW. PERFORMED TASK AND NO DEFECT. A/C OK FOR CONTINUED SERVICE WITH GPWS SYS MEL`ED AS PER A PRECAUTIONARY REF ABOVE ITEM. [06-19-07] REMOVED AND REPLACED GROUND PROX WARNING COMPUTER (1WZ). GPWS OPS NORMAL PER MM 34-48-00-710-001. OK FOR S ERVICE. 2 L 7 2 4F RT A28NM 2007061900092 20070619 00092 NM 2007 6 19 WRNA200700030 1 20070210 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE GOUGED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, FUSELAGE SKIN WAS FOUND GOUGED AT STA 665 BETWEEN STR 40R AND 41R. REMOVED GOUGE IAW SRM 53-30-01 DETAI L II AND INSTALLED REPAIR DOUBLE IAW SRM 53-30-03 FIG 1. 2 L 7 4 4F A20WE 2007061900100 20070619 00100 NM 2007 6 19 WRNA200700032 1 20070213 A 5312 BULKHEAD BOEING 747 747212B 1384886 NM FUSELAGE DENTED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, A SMALL DENT WAS FOUND IN THE AFT PRESSURE BULKHEAD AT STA 2360 APPROX WL 200, LBL 30. REMOVED DAMAGED SECTION OF BULKHEAD WEB, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-04 FIG 9, SRM 51-10-01 AND AMM 51-21-00. 2 L 7 4 4F A20WE 2007061900104 20070619 00104 NM 2007 6 19 WRNA200700033 1 20070213 A 5414 SKIN BOEING 747 747212B 1384886 NM NR 3 PYLON DAMAGED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, THE O/B SKIN OF NR 3 PYLON WAS FOUND DAMAGED AT APPROX STA 221.9 JUST BELOW MID SPAN. REMOVED DAMAGE IA W SRM 54034-03, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 54-34-03 FIG 25, SRM 51-10-02 AND SOPM 20-42-02. 2 L 7 4 4F A20WE 2007061900105 20070619 00105 NM 2007 6 19 WRNA200700034 1 20070214 A 5730 RIB BOEING 747 747212B 1384886 NM NR 4 FUEL TANK CRACKED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, THE LOWER RIB CORD OF NR 4 FUEL TANK ACCESS PANEL 652AB, WS 972 WAS FOUND CRACKED FROM RADIUS BLOCK TO R ADIUS BLOCK. REMOVED LOWER RIB CORD IAW SRM 51-30-00, FABRICATED NEW RIB CORD IAW DRAWING 65B01073 AND INSTALLED RIB C ORD IAW SRM 51-30-02. 2 L 7 4 4F A20WE 2007061900106 20070619 00106 NM 2007 6 19 WRNA200700035 1 20070210 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE DENTED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, FOUND 3 DENTS IN FUSELAGE SKIN AT STA 265 BETWEEN STR 10A L AND 11L. REMOVED DAMAGED, FABRICATED AND IN STALLED REPAIR PARTS IAW SRM 53-30-03 FIG 1. THIS IS A CATEGORY -C- REPAIR AND WILL REQUIRE RE-INSPECTION AT 1,000 HOUR INTERVALS, LIFE LIMIT IS 6,000 HOURS IAW SRM 53-30-03 FIG 1 SHEET 14 TABLE V. 2 L 7 4 4F A20WE 2007061900107 20070619 00107 NM 2007 6 19 WRNA200700036 1 20070210 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE DENTED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, FUSELAGE SKIN WAS FOUND DENTED AT STA 228 STR 17L. CUT OUT DAMAGE IAW SRM 53-30-03 FIG 1, FABRICATED RE PAIR IAW SRM 53-30-03 FIG 1 AND INSTALLED PER SRM 53-30-01 FIG 1. 2 L 7 4 4F A20WE 2007061900108 20070619 00108 NM 2007 6 19 WRNA200700037 1 20070225 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE GOUGED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, FOUND EXTERNAL FUSELAGE SKIN GOUGED AT STA 2576 BETWEEN STR 42R AND 46R. REMOVED DAMAGED SECTION, FABRI CATED AND INSTALLED REPAIR IAW SRM 53-30-03 FIG 28. 2 L 7 4 4F A20WE 2007061900109 20070619 00109 NM 2007 6 19 WNRA200700038 1 20070211 A 5412 ANGLE BOEING 747 747212B 1384886 NM NR 1 PYLON DAMAGED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, HFEC INSPECTION, NR 1 PYLON BULKHEAD, STA 221 FORWARD SIDE, INBOARD ANGLE MISSING PIECE AT UPPER HORIZON TAL FLANGE. FABRICATED AND INSTALLED DOUBLER'S IAW SRM 54-14-03 FIG 13 AND EA 01-07016. 2 L 7 4 4F A20WE 2007061900110 20070619 00110 NM 2007 6 19 WRNA200700039 1 20070215 A 5310 DOOR FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, A CRACK WAS FOUND ON WEB AND DOUBLER ON R-1 DOOR EDGE FRAME AT STA 488 BETWEEN STR 25 AND 26 USING HFEC. REMOVED DOUBLER AND DAMAGED SECTION OF WEB, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-04 FIG 92. 2 L 7 4 4F A20WE 2007061900119 20070619 00119 2007 6 19 ASMF200706002 4 20070610 A 3445 UNKNOWN DOUG DC9 DC982 3022082 WP UNKNOWN W ASMF B EMER. DESCENT J E WARNING INDICATION VIBRATION/BUFFET CR CRUISE 1 SW 23 501AM 49188 CAPTAIN REPORTED TCAS RESOLUTION WITH AC AT 33000 FEET, AIRPLANE DESCENT 3000 FEET WITH A RATE OF 6000 FEET PER MINUTE R EACHING OVERSPEED (NO ALARMS, JUST VIBRATION). AT PLATFORM MAINTENANCE PERSONNEL PERFORMED VISUAL INSPECTION BY OVERSPE ED IAW MM 05-51-05 AS WELL AS EXCESSIVE MANEUVER AND OVERLOAD CONDITION CHECK IAW MM 05-51-02, NO DAMAGES WERE FOUND. 2 L 7 2 4F A6WE 2007061900120 20070619 00120 CE 2007 6 19 GUUA06090702 1 20070609 A 2697 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FIRE BOTTLE LOOSE A GUUA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 29 81536 UE152 FLIGHT: 9170 FLL/TCB, AFTER TAKEOFF THE NR (1) FIRE DISCHARGE ANNUNCIATOR FLICKERED ON AND OFF. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. SECURED LOOSE WIRE ON THE NR (1) FIRE BOTTLE. 2 L 7 2 4T 4 T RT A24CE E26NE 2007061900121 20070619 00121 SO 2007 6 19 GUUA06120701 1 20070612 A 3260 PROXIMITY SWITCH EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE RT MLG DIRTY A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 29 285AS 120265 FLIGHT 2043 TNT/FLL, DURING FLIGHT, RT MLG (A) LIGHT INTERMITTENT. CLEANED RT MLG PROXIMITY SWITCHES. 2 L 7 2 4T 4 T RT A31SO E20NE 2007061900122 20070619 00122 CE 2007 6 19 DXTA200702247 1 20070607 A 3150 WARNING MESSAGE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL ACTIVATED E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 970QS 7500070 RETRIM RT WING DOWN AMBER CAS MESSAGE CAME ON DURING CRUISE FLIGHT AT FL300, AFTER TRIMMING. [07-09-07] REPLACED RUDDE R COMMAND BUNGEE I/A/W CE-750 M/M CHAPTER 27-20-00. OPERATIONAL AND RIG CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007061900123 20070619 00123 SO 2007 6 19 N93A08062007 1 20070608 A 2120 UNKNOWN GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU CABIN SMOKE E N93A O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 13 460QS 7995 7995 1360 AFTER SELECTING COWL ANTI ICE, SMOKE FILLED CABIN, DISSIPATED WHEN SELECTING COWL ANTI ICE OFF. OPEN, FURTHER DATA TO F OLLOW. 2 L 7 2 4F 4 F RT A12EA E25NE 2007061900124 20070619 00124 SO 2007 6 19 GUUA06090701 1 20070609 A 3350 1317 BULB EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE EMERGENCY LIGHT INOPERATIVE A GUUA K NONE L NO TEST IN INSP/MAINT 1 SO 29 261AS 120141 AT SCHEDULED ROUTINE INSPECTION, LT AFT EMERGENCY LIGHT INOPERATIVE.REPLACED LT AFT EMERGENCY LIGHT BULB. 2 L 7 2 4T 4 T RT A31SO E20NE 2007061900126 20070619 00126 CE 2007 6 19 GUUA06120702 1 20070612 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 438 CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87550 UE205 AT SCHEDULED INSPECTION DISCOVERED SKIN CORROSION AT FS 438.250, STRINGER WL 13R. REMOVED DAMAGED SKIN AND INSTALLED EX TERNAL REINFORCEMENT DOUBLER IAW MFG STRUCTURAL REPAIR MANUAL 51-70-06. 2 L 7 2 4T 4 T RT A24CE E26NE 2007061900139 20070619 00139 NM 2007 6 19 DHL2007740548 1 20070606 A 5313 69163845 FITTING BOEING 727 7272Q9 138448M NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 STRINGER 30R END FITTING CORRODED AT BS 950 BULKHEAD. REMOVED AND REPLACED ANGLE P/N 69-16384-5, P/O 7212251 AND TWO SP ACE PLATES P/N 69-51272-2, P/O3 7212251, P/N 69-51272-1, P/O NR 7212251, AT STR 30 END FITTINGS ON BS 950 BULKHEAD, IAW B-727 SRM 51-30-5 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007061900140 20070619 00140 NM 2007 6 19 DHL2007783509 1 20070602 A 5330 2024T3 SKIN BOEING 727 727227 1384078 NM BS 720E WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 FUSELAGE TO RT WING L/E BS 720E, WBL 70.5, PREVIOUS REPAIR DOUBLER SHOW WORN OUT PATH, CHAFING WITH INBD L/E WEDGE. REM OVED PREVIOUS REPAIR DOUBLER IAW B727 SRM 51-30-2. FABRICATED REPAIR DOUBLER FROM .040, 2024T3, 26 BY 10 IAW US AIR EA 7357. TREATED, PRIMED AND INSTALLED IAW B727 SRM 51-10-2 AND US AIR EA 7357. 2 L 7 3 4F A3WE 2007061900141 20070619 00141 NM 2007 6 19 QXEA200700950 1 20070609 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - SEAT TRACK NR 13 HAS A CHAFE AT STATION X409. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007061900142 20070619 00142 NM 2007 6 19 QXEA200700951 1 20070609 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - SEAT TRACK NR 13 AT STATION X226-X560 HAS MINOR SCRATCHES AND CHAFES. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007061900143 20070619 00143 NM 2007 6 19 QXEA200700946 1 20070606 A 5410 DIAPHRAGM BOMBDR DHC8 DHC8402 1390042 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - LEFT NACELLE OUTBOARD DIAPHRAGM CRACKED. REPAIRED IAW SRM 51-42-05 AND 51-40-15. 2 H 7 2 4T RT A13NM 2007061900144 20070619 00144 NM 2007 6 19 QXEA200700947 1 20070610 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - SEAT TRACK NR 21 HAS SCRATCHES AT STATION X715. REPAIRED IAW RD8/4-53-884 AND SRM 51-21-10. 2 H 7 2 4T RT A13NM 2007061900145 20070619 00145 NM 2007 6 19 QXEA200700952 1 20070609 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - SEAT TRACK NR 7 AT STATION X224-X560 HAS MINOR NICKS, SCRATCHES AND CHAFES. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007061900146 20070619 00146 NM 2007 6 19 DHL2007740545 1 20070606 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 950D CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AFT CARGO BS 950D BETWEEN STR27L AND STR 29R RT FWD SIDE OF FRAME HAS FLANGE WITH CORROSION SEVERAL PLACES. REMOVED COR ROSION AT FRAME BS 950D BETWEEN STR29R AND 28R ORIGINAL MAT .071" MAT LOSS .036" MAT REMAINING .035" FOUND OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1 AND 53-10-2 FIG 5. CUT OUT DAMAGED AREA APPROX DIM 6" BY 2" AT FRAME 950D BETWEEN STR 29R T RU 28R IAW B727 SRM 53-10-4 FIG 15. FAB SHEAR TIE REPAIR FROM P/N 7075T6 .080" PO NR 9004670 APPROX DIM 6" BY 2" IAW B7 27 SRM 53-10-4 FIG 15 AND 51-20-1 FIG 7. INSTALLED SHEAR TIE REPAIR AT FRAME BS 950D BETWEEN STR 29R AND 28R IAW B727 S RM 53-10-4 FIG 15 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007061900147 20070619 00147 NM 2007 6 19 DHL2007740546 1 20070609 A 5313 BAC1498140 STRINGER BOEING 727 7272Q9 138448M NM BS 450-480 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 STRINGER 28 L, BS 450 CORRODED. REMOVED STR 28L, FROM BS 450-480 AND FABRICATED NEW SECTION , MAT USED BAC 1498-140 707 5 T6, PO NR 7191256, DIMENSION 28.75" AND FILLER, MAT USED BAC 1498-132 7075T6 PO NR 7207138, DIMENSION 16" IAW B-727 SR M.53-10-3 FIG-1. TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED IAW B-727. SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007061900148 20070619 00148 NM 2007 6 19 DHL2007783512 1 20070604 A 5260 7075T6 WEB BOEING 727 727227 1384078 NM AFT AIRSTAIRS CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 RT SIDE AIRSTAIRS WEB PANEL CRACKED AT LIGHTING HOLE, BS 1223, WL 156, RBL 21. CUT OUT DAMAGED AREA DIM .5 BY .5 IAW B7 27 SRM 51-40-2, FIG 1. FABRICATED DOUBLER REPAIR, MATERIAL USED 7075T6, 040, 4” BY 2.50 IAW B727 SRM 51-40-2, FIG 1 AND 53-10-2, FIG 6. TREATED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 51-10-2, 51-40-2, FIG 1 AND 53-30-2. 2 L 7 3 4F A3WE 2007061900149 20070619 00149 NE 2007 6 19 HALA0700257 2 20070614 A 7200 ENGINE BOEING 767 767300 1385204 NM PWA 4060 PW4060 52119 NE LEFT MALFUNCTIONED A HALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 581HA 28141 ETOPS SIGNIFICANT SYSTEM, LEFT ENG EPR FLUCTUATES +- .01 AT CONSTANT THRUST SETTING. N1 FLUCTUATES +- 0.2 OVER A PERIOD OF APPROX 1.5 SEC. PREV ITEM #35 (EPCS P5 FLUXES +- 0.1).//T/S PER FIM 77-11-00 PERFORMED TEST 14 PER MM 71-00-00-795. CLEANED AND CLEARED ALL PT2 LINES. RUN ENG AT GATE NO FLUX ON EPR OR N1 ALSO CLEANED PT2/TT2 PROBE AND PT 4.95 PROBE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007061900150 20070619 00150 NM 2007 6 19 HALA0700256 1 20070615 A 2420 4300702 ALTERNATOR BOEING 767 767300 1385204 NM PWA 4060 PW4060 52119 NE LT ENGINE MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 9373 9373 28140 ETOPS SIGNIFICANT SYSTEM, L ENG CONT EICAS MSG AFTER ENGINE START SHUT DOWN AND RE-STARTED ENGINE AND MESSAGE DID NOT RE -APPEAR. RESEATED L ENG N2 SPEED CARD PER MM 77-12-01-004. TESTED OK, RAN ENG, L ENG EEC MODE MSG APPEARED WITH CORRES PONDING L ENG ALTN CONT LIGHT ILLUM. T/S FIM 73-21-00/113-L PIMU CHAN A PWR LOSS, REPLACED PMA AT L ENG PER AMM73-21-05 TEST PER 71-00-00/501. TABLE EICAS MSG DID NOT RETURN PIMU MSG CLEAR. 2 L 7 2 4F 4 F RT A1NM E24NE 2007061900151 20070619 00151 NM 2007 6 19 HALA0700255 1 20070615 A 2170 1808492 COALESCER BAG BOEING 717 717200 1383700 NM CABIN AIR ODOR A HALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 13 479HA 55124 ATB - AFTER T/O SMELLED ACID ODOR, WHICH SEEMED TO DISSIPATE THEN BECAME STRONGER CLIMBING THRU 1100' RETURNED TO AIRPOR T. INSPECTED NR 1 AND NR 2 ENG FOR LEAKS. NO LEAKS NOTED. NR 1 ENG WAS JUST CHANGED. INSPECTED BOTH PACKS FOR LEAKS. NO LEAKS NOTED. REPLACED NR 1 PACK COALESCER BAG. HIGH POWER RAN UP CK OK. NO ODOR NOTED. 2 L 7 2 4F TR A6WE 2007061900152 20070619 00152 NM 2007 6 19 HALA0700258 1 20070618 A 3350 1000679 LIGHT BOEING 767 7673G5 1385126 NM CABIN INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 584HA 24258 DURING WALK THRU, FOUND CENTER CROSS AISLE EMERG TRACK LIGHTING INOP. REMOVED AND REPLACED CENTER AND RT EMERG LIGHT AS SEMBLIES IN MID GALLEY. OPS CHECKS NORMAL. 2 L 7 2 4F RT A1NM 2007061900153 20070619 00153 NM 2007 6 19 QXEA200700970 1 20070617 A 3010 7786863 SHUTOFF VALVE DHAV DHC8 DHC8202 2809007 NM DEICE SYS MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 346PH 19878 1712 477 SEA FLIGHT NR 2090 ON PUSH BACK DE-ICE PRESSURE CAUTION REMAINED ILLUMINATED AND PRESSURE GAUGE SHOWED 6 PSI. BOTH PROP S BROUGHT UP TO MAX 785 RPM DEICE PRESSURE RAISED TO 10 PSI. NO CHANGE WITH BOOT AIR ISO VALVE ON OR OFF. REPLACED NR 2 HPSOV PER TASK 21-11-16-000-801/21-11-16-400-801. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061900154 20070619 00154 NM 2007 6 19 QXEA200700968 1 20070616 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY MALFUNCTIONED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 345PH 13617 527 476 PDX FLIGHT NR 2184 - INTERMITTENT SMOKE WARNING DURING CLIMB-OUT. MAINTENANCE REPLACED NR 1 AND NR 2 CARGO SMOKE DETECT ORS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061900155 20070619 00155 2007 6 19 QXEA200700967 4 20070615 A 2340 HANDSET DHAV DHC8 DHC8202 2809007 NM INTERPHONE MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 357PH 504 PDX FLIGHT NR 2136, UNABLE TO COMMUNICATE WITH FLIGHT ATTENDANT VIA INTERPHONE SYSTEM. MAINTENANCE REPLACED FLIGHT ATTE NDANTS HANDSET. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061900156 20070619 00156 EU 2007 6 19 TRBA2007032 1 20070612 A 3397 WIRE AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHT BROKEN A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 494AE 494 DURING PHASE INSPECTION, FOUND SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REPAIRED WIRE ON CONNECTOR 68WL AS PER STD PRA CTICE JIC NR 20-00-00. PERFORMED OP CK IAW JIC NR 33-50-00. 2 H 7 2 4T RT A53EU 2007061900157 20070619 00157 EA 2007 6 19 COMA0770033 1 20070613 A 3610 CLAMP CNDAIR CL600 CL6002C10 1390015 EA BLEED AIR SYS LOOSE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 625CA 10113 FLIGHT 5448 - RECEIVED RIGHT BLEED WARNING INFLIGHT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND RIGHT INLET HE ADER CLAMP LOOSE. SECURED CLAMP. GROUND RAN RIGHT ACM. NO LEAKS NOTED. INSPECTED CROSS BLEED DUCT SENSORS. REPOSITI ONED LOOP TO ELIMINATE CONTACT. PERFORMED AILC CHECKS. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007061900158 20070619 00158 EU 2007 6 19 WRNA200700040 1 20070613 A 5754 SLAT AIRBUS 300 A300B4203 3930306 EU WING MALFUNCTIONED A WRNA K NONE J WARNING INDICATION AP APPROACH 1 SO 05 505TA 271 ON APPROACH TO IND, L/E SLATS FAILED TO EXTEND WITH ASYMMETRY, CONTINUED ON APPROACH AND MADE A SAFE LANDING. VISUALLY INSPECTED SLATS TORQUE TUBES AND TRANSMISSIONS FOR A DISCONNECT, NO DEFECTS. INSPECTED FOR DEFECTS IAW MM 27-83-00 PG 6 05, NO DEFECTS NOTED. ACCOMPLISHED SLAT ASYMMETRY ADJUSTMENT IAW MM 27-83-00 PG 501 AND ACCOMPLISHED SLAT FUNCTIONAL TE ST IAW MM 27-81-00 PG 509, OPS CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A35EU 2007061900162 20070619 00162 EA 2007 6 19 TRAX200700813 1 20070610 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 354CA 10064 F/A REPORTED, REAR FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007061900163 20070619 00163 NM 2007 6 19 SWAA072948 1 20070612 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED C3 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND BATTERY CHA RGER PER MM. 2 L 7 2 4F RT A16WE 2007061900164 20070619 00164 NM 2007 6 19 SWAA072944 1 20070611 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 487WN 33854 EEPLS COVER LOOSE AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007061900165 20070619 00165 NM 2007 6 19 SWAA072945 1 20070611 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 487WN 33854 EEPLS COVER LOOSE AT ROW 5 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007061900166 20070619 00166 NM 2007 6 19 SWAA072946 1 20070611 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 487WN 33854 EEPLS COVER LOOSE AT ROW 3 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007061900167 20070619 00167 2007 6 19 SWAA072934 4 20070610 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 764SW 27878 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007061900168 20070619 00168 NM 2007 6 19 SWAA072940 1 20070611 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 14L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900169 20070619 00169 NM 2007 6 19 SWAA072959 1 20070612 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 22L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900170 20070619 00170 NM 2007 6 19 SWAA072947 1 20070612 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 728D, STR 19R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900171 20070619 00171 NM 2007 6 19 SWAA072937 1 20070611 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 803, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007061900172 20070619 00172 NM 2007 6 19 SWAA072936 1 20070611 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 789, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900173 20070619 00173 NM 2007 6 19 SWAA072956 1 20070612 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007061900174 20070619 00174 NM 2007 6 19 SWAA072958 1 20070612 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 748, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007061900175 20070619 00175 NM 2007 6 19 SWAA072957 1 20070612 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740E, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007061900177 20070619 00177 NM 2007 6 19 SWAA072968 1 20070612 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900178 20070619 00178 NM 2007 6 19 SWAA072952 1 20070612 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900180 20070619 00180 NM 2007 6 19 SWAA072964 1 20070612 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R AND 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900181 20070619 00181 NM 2007 6 19 SWAA072963 1 20070612 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R AND 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061800051 20070618 00051 EU 2007 6 18 CPCP20070035 1 20070425 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 448AM 448 FOUND LT BETWEEN FRAME 36 AND 39 SEAT TRACK CORRODED. SEAT TRACK LT BETWEEN FRAME 36 AND 39 REPLACED AS PER SRM 51-25-0 4. 2 H 7 2 4T RT A53EU 2007061800054 20070618 00054 EU 2007 6 18 CPCP20070033 1 20070425 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 448AM 448 FOUND FRAME 38 FLOORBEAM CORRODED. FRAME 38 FLOORBEAM REPAIRED AS PER SRM 53-00-00 FIG 450. 2 H 7 2 4T RT A53EU 2007061800056 20070618 00056 NM 2007 6 18 DHL2007783505 1 20070606 A 5313 BAC14981457075 STRINGER BOEING 727 727227 1384078 NM BS 905E-950F CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 AFT CARGO PIT BETWEEN BS 950E AND 950F, STRINGER 28L HAS CORROSION AT OUTBD BOTTOM FLANGE. CUT OUT DAMAGED STR 28L STA 950D PLUS 10 TO 950F PLUS 10 AS REQUIRED IAW B727 SRM 53-10-3, FIG 1. FABRICATED STRINGER REPAIR 2 EACH MATERIAL USED B AC1498-145-7075T6, DIM 19.25 LONG AND 18.75 LONG AND 3 EACH REPAIR SPLICES MATERIAL USED BAC1498-131-7075T6, DIM 13.25, 13.75 AND 14 LONG IAW B727 SRM 53-10-2, FIG 9 AND 53-10-3, FIG 1. TREATED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 51- 10-2, 51-30-2 AND 53-10-2, FIG 9. 2 L 7 3 4F A3WE 2007061800058 20070618 00058 2007 6 18 DHLA200700030 4 20070614 A 3418 SENSOR AIRBUS 300 A300B4203 3930306 EU NR 1 AOA MALFUNCTIONED A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 05 367DH 265 AFTER CLEARED FOR T/O, AFTER PULLING GO LEVERS NO SRS. REJECTED T/O PRIOR TO 60 KTS. REPLACED NR 1 AOA SENSOR AS PER M M 27-36-15. SRS SYS TESTS NORM AS PER MM 34-24-11. 2 L 7 2 4F RT A35EU 2007061800067 20070618 00067 WP 2007 6 18 AALA20070982 1 20070529 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 258AA 49288 LGA - AISLE EMERGENCY LIGHTS AT RIGHT SEAT ROW 28 INOPERATIVE. RESET PUSH BACK PIN IN CONNECTOR FOR AISLE EMERGENCY LIG HTS AT RIGHT SEAT ROW 28. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007061800071 20070618 00071 NM 2007 6 18 AALA20071001 1 20070525 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 977AN 29550 TUL - EMERGENCY LIGHTS AT LEFT AFT SERVICE DOOR HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHTS AT LEFT AFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007061800077 20070618 00077 NM 2007 6 18 AALA20071002 1 20070525 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 977AN 29550 TUL - EMERGENCY LIGHTS AT RIGHT AFT SERVICE DOOR HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHTS AT RIGHT AFT SERVI CE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007061800086 20070618 00086 NM 2007 6 18 QXEA200700944 1 20070613 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 418QX 4143 SEA FLIGHT NR 2318: FA UNABLE TO OPEN REAR PASSENGER DOOR. MAINTENANCE FOUND PREVIOUS OPENED AND OUT OF SEQUENCE. RESE QUENCED DOOR AND PERFORMED OPS CHECK. OPS CHECK IS GOOD IAW Q400 AMM TASK 52-12-00-710-801. OK FOR CONTINUED SERVICE. NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061800092 20070618 00092 SO 2007 6 18 SIMA200716503 1 20070613 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS UNSECURE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 692AE 14500866 EMERGENCY EXIT LIGHT OVER FLIGHT ATTENDANT SEAT BURNED OUT. RESCURED NUMBER ONE AC/DC INVERTER CONNECTOR IAW EMB AMM. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE 2 L 7 2 4T RT T00011AT 2007061800103 20070618 00103 NE 2007 6 18 HEEA114545 2 20070318 A 7310 0292858560 HMU SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL2S1 60057 NE NR 2 ENGINE INOPERATIVE E HEEA D RETURN TO BLOCK J WARNING INDICATION DE DESCENT 1 SW 03 761P 2257 760588 20731TEC DURING ENROUTE DESCENT NR 2 FUEL PRESSURE LIGHT ILLUMINATED. NO SECONDARY NOTED. DIVERTED AND LANDED WITHOUT INCIDENT. DURING SUBSEQUENT START ATTEMPT FOR TROUBLESHOOTING, ENGINE WOULD NOT START. MAINTENANCE FOUND THE HMU TO BE AT FAULT . REPLACED HMU. 1 G 7 2 3U 4 U NC H1NE E00054EN 2007061800225 20070618 00225 NM 2007 6 18 AMTA200700271 1 20070527 A 2160 CONTROLLER BOEING 737 73783N 13844HI NM NR 2 MALFUNCTIONED A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 304TZ 30675 PRIOR TO TAKEOFF, SELECTED RECALL (R) PACK LIGHT ILLUMINATED. COMPLETED PACK TRIP PROCEDURES LIGHT WOULD NOT RESET RETU RN TO GATE. PERFORMED BITE ON NR 2 PACK CONTROLLER, TCV FAULTED, RESET DURING VERIFICATION, OK FOR SERVICE IAW MM 21-62 -00-810-801. (K) 2 L 7 2 4F RT A16WE 2007061800226 20070618 00226 NM 2007 6 18 AMTA200700265 1 20070525 A 3350 D71702030 POWER SUPPLY BOEING 737 73783N 13844HI NM CABIN DISCHARGED A AMTA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 11 314TZ 30640 AFT LT WING/BODY FAIRING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY SLIDE LIGHT, POWER SUPPLY, IAW 33- 51-06. OPS CHECK NORMAL. (K) 2 L 7 2 4F RT A16WE 2007061800232 20070618 00232 NM 2007 6 18 AMTA200700264 1 20070524 A 3260 WARNING SYSTEM BOEING 737 73783N 13844HI NM LANDING GEAR MALFUNCTIONED A AMTA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 308TZ 28244 PSEU LIGHT ILLUMINATED ON RECALL LIGHT EXTINGUISHES ON MASTER CAUTION RESET. PERFORMED FIM TEST IAW 32-09-00-810-801, N O DEFECTS NOTED. OK FOR SERVICE. (K) 2 L 7 2 4F RT A16WE 2007061800238 20070618 00238 NM 2007 6 18 SWAA072916 1 20070608 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 24R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007061800243 20070618 00243 NM 2007 6 18 SWAA072903 1 20070608 A 3350 767 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 14Y CHECK, FOUND LEFT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007061800247 20070618 00247 NM 2007 6 18 SWAA072907 1 20070608 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007061800252 20070618 00252 NM 2007 6 18 SWAA072899 1 20070608 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 766SW 29806 DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 7 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007061800253 20070618 00253 NM 2007 6 18 SWAA072895 1 20070608 A 2560 PH22300L GLOWSTRIP BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 5 DEF. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007061800258 20070618 00258 EU 2007 6 18 WRNA200700026 1 20070524 A 3244 C20211160 TIRE AIRBUS 300 A300B4203 3930306 EU MLG SEPARATED A WRNA K NONE O OTHER TO TAKEOFF 1 SO 05 821SC 359 359 211 NR 6 TIRE RUBBER SEPARATION ON TAKEOFF FROM SJU, FLIGHT CONTINUED TO MIA AND MADE A SAFE LANDING. ON INSPECTION OF AIRC RAFT, FOUND LEFT INBOARD FOREFLAP, AFT FLAP AND CENTER HINGE FAIRINGS DAMAGED. REPLACED TIRE AND WHEEL ASSY, FLAP ASSY AND FLAP TAB ASSY. AIRCRAFT RELEASED TO SERVICE. 2 L 7 2 4F RT A35EU 2007061800260 20070618 00260 SO 2007 6 18 RAIA00706005 1 20070605 A 3610 O-RING EMB 145 EMB145 3260210 SO BLEED AIR SYS BLOWN A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 821HK 145068 FLT NR 5549 - STL - ENGINE 1 BLEED LEAK. MAINTENANCE REMOVED AND REPLACED BLEED O-RINGS AT CARGO BAY AREA. 2 L 7 2 4F RT T00011AT 2007061800270 20070618 00270 NM 2007 6 18 WRLA2007077 1 20070611 A 2530 3111 FAN DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE CHILLER NOISY A WRLA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 801DE 48472 FLIGHT 8400 FORWARD CHILLER FAN NOISY - POSSIBLE SOURCE OF ELECTRICAL BURNING ODOR . NR 2 RADAR UNIT (FWD E/E) VERY HOT , POSSIBLE SOURCE OF ELECTRICAL BURNING ODOR. CHECKED CHILLER FOR CHAFED WIRES OR DAMAGE, NONE FOUND. NO ELECTRICAL BU RNING ODOR, BUT CHILLER FAN NOISY. ENTERED IN DMI M25JU1207-52. MEL 25-22-01-01. CHECKED RADAR RT FOR CHAFED WIRES BE HIND RT UNIT. NO DAMAGE FOUND & CHECKED RACK COOLING AIR NORMAL. NO ELECTRICAL BURNING ODOR AS PER MM 34-41-00. REMOV ED AND REPLACED CHILLER IAW MM 25-30-00. OPS CHECKED CHILLER OPERATES NORMALLY. DMI CLEARED. 2 L 7 3 4F 4 F RT A22WE E24NE 2007061900002 20070619 00002 NM 2007 6 19 SWAA072928 1 20070611 A 3350 300432 REFLECTOR BOEING 737 7373H4 1384600 NM EXTERIOR LIGHT CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT REFLECTOR CORRODED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007061900016 20070619 00016 WP 2007 6 19 ASAA0781774 1 20070603 A 5523 DOUBLER DOUG DC9 DC983 3022083 WP ELEVATOR TAB DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 EXISTING REPAIR DISBONDED ON LOWER SURFACE OF LEFT ELEVATOR GEARED TAB. PREPARED DAMAGED AREA FOR BONDING. INSTALLED F ILLER AND DOUBLER PER SRM 51-70-2. 2 L 7 2 4F RT A6WE 2007061900017 20070619 00017 WP 2007 6 19 ASAA0781775 1 20070603 A 5753 59304953 SKIN DOUG DC9 DC983 3022083 WP T/E FLAP VANE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 LEFT INBOARD FLAP OUTBOARD VANE LOWER INBOARD SURFACE HAS MULTIPLE DENTS. PREPARED DAMAGED AREA FOR BONDING. INSTALLED REPAIR DOUBLER PER SRM 51-70-2. 2 L 7 2 4F RT A6WE 2007061900021 20070619 00021 WP 2007 6 19 ASAA0781777 1 20070603 A 5753 59304944 SKIN DOUG DC9 DC983 3022083 WP T/E FLAP VANE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 RIGHT INBOARD FLAP INBOARD VANE HAS SEVERAL DENTS ON LOWER SURFACE. PREPARED DAMAGED SURFACE FOR BONDING. INSTALLED RE PAIR DOUBLER PER SRM 51-70-2. 2 L 7 2 4F RT A6WE 2007061900025 20070619 00025 WP 2007 6 19 ASAA0781780 1 20070607 A 5320 993053873 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 RIGHT CUSP WEB CORRODED. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 53-01, 51-70-4 AND 51-70-4. 2 L 7 2 4F RT A6WE 2007061900048 20070619 00048 NM 2007 6 19 UPS07649950 1 20070523 A 5420 SUPPORT BOEING 767 76734AF 1385212 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 318UP 27746 INSPECTION TYPE:C1 NR 2 PYLON AFT VERTICAL PNL SUPPORT IS CHAFED FOR ACCESS PNL 447AL. FABRICATED NEW SPLICE PLATE PER SRM 51-40-05-06, SRM 51-30-01-06 AND SRM 51-40-08-05 AND GOODRICH ER 07-2526. 2 L 7 2 4F RT A1NM 2007061900054 20070619 00054 WP 2007 6 19 UPS07849948 1 20070606 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE UPPER RIB CRACKED AT STA XFS 722. STOP DRILLED CRACKED RIB AT STA XFS 72 2 IAW SRM 57-02-00. FABRICATED AND INSTALLED REPAIR ANGLE AT STA XFS 722 IAW SRM 57-02-00 FIG 2. 2 L 7 4 4F RT 4A25 2007061900062 20070619 00062 SO 2007 6 19 C2XA07IA136 1 20070611 A 3260 8005701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO LT MLG INOPERATIVE A C2XA O OTHER N FALSE WARNING AP APPROACH 1 SW 27 13979 145181 IAH - FLIGHT 2099, THE CREW REPORTED A LANDING GEAR AIR/GRND FAILURE INDICATION ON APPROACH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND WEIGHT ON WHEELS PROXIMITY SENSOR, OPERATIONALLY CHEC KED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061900065 20070619 00065 NM 2007 6 19 DHL2007740532 1 20070616 A 5753 SKIN BOEING 727 7272Q9 138448M NM TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 WHILE AT C CHECK AT FLIGHTSTAR AIRCRAFT SERVICES, LEFT INBOARD FOREFLAP DELAMINATED AT INBOARD END WBL 71. CUTOUT DELAM INATED AREA ON LT I/B FORE FLAP APPROX 4" BY 12". REMOVED DAMAGED CORE APPROX 4" BY 12" FABRICATED CORE PLUG APPROX 4" BY 12" FROM DUR-5052-4.4-3/16- NE.-4.0 PO 6261123. FABRICATED FILLER APPROX 4" BY 12" AND DOUBLER APPROX 5" BY 12" FROM 7075-T6 .016 PO NR 9003988, CLEANED ,PREPPED, PRIMED, AND BONDED. CLEANED, TREATED, PRIMED AND SEALED EDGES. FABRICAT ED RUBSTRIP APPROX 3" BY 8" FROM 301 1/2 HARD .016 PO NR 9002615 AND INSTALLED IAW B727 SRM 57-50-2 FIG3 AND 51-40-20 FI G 2 M/M51-20-11 AND BOEING DWG 65-82738. 2 L 7 3 4F RT A3WE 2007061900070 20070619 00070 NM 2007 6 19 MWEA070145 1 20070611 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 918ME 55180 RIGHT ENGINE LOWER DEFLECTOR DOOR ZEE FRAME IS CRACKED AT THE INBOARD END AT STATION 26. FABRICATED AND INSTALLED ZEE F RAME. 2 L 7 2 4F TR A6WE 2007061900074 20070619 00074 NM 2007 6 19 CALA0700302 1 20070601 A 3350 BR964411 LIGHT BOEING 777 777224 1385225 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 77014 29862 INSPECTION FOUND EMERGENCY LIGHT INOP AT ROW 42DEF AND 43DEF. REPLACED LIGHT ASSEMBLIES ON LEFT SIDE OF SEAT GROUPS 42D EF AND 43DEF. BOTH OPS CHECKED GOOD. 2 L 7 2 4F RT T00001SE 2007061900096 20070619 00096 NM 2007 6 19 WRNA200700031 1 20070110 A 5230 SKIN BOEING 747 747212B 1384886 NM CARGO DOOR DENTED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING C-CHECK, A DENT WAS FOUND IN BULK CARGO DOOR EXTERNAL SKIN AT STA 2012 BETWEEN STR 31R AND 33R. CUT OUT DAMAGED AREA IAW SRM 52-00-03 FIG 1. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-10-02, SRM 52-00-03 FIG 1, 2 & 3 AND MM 5 1-24-01. 2 L 7 4 4F A20WE 2007061900160 20070619 00160 EA 2007 6 19 TRAX200700811 1 20070610 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 980EV 7759 F/A'S FLASHLIGHT IS INOP. 2 L 7 2 4F RT A21EA 2007061900161 20070619 00161 EA 2007 6 19 TRAX200700812 1 20070610 A 5210 STRAP CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR OUT OF POSITION A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 UNABLE TO OPEN ASD, LCL FOUND DOOR HANDLE STRAP CLOSED IN DOOR. 2 L 7 2 4F RT A21EA 2007061900183 20070619 00183 NM 2007 6 19 SWAA072966 1 20070612 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R AND 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900184 20070619 00184 NM 2007 6 19 SWAA072971 1 20070612 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900187 20070619 00187 NM 2007 6 19 SWAA072972 1 20070612 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900190 20070619 00190 NM 2007 6 19 SWAA072969 1 20070612 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900192 20070619 00192 NM 2007 6 19 SWAA072970 1 20070612 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900193 20070619 00193 NM 2007 6 19 SWAA072962 1 20070612 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900194 20070619 00194 NM 2007 6 19 SWAA072955 1 20070612 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007061900198 20070619 00198 NM 2007 6 19 SWAA072953 1 20070612 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER 4R CRACKED AT BS 732A. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007061900199 20070619 00199 NM 2007 6 19 SWAA072943 1 20070611 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 438WN 29833 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP BETWEEN ROW 2 ABC AND ROW 5 ABC. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007061900203 20070619 00203 NM 2007 6 19 SWAA072935 1 20070610 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 300SW 22940 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2007061900205 20070619 00205 NM 2007 6 19 2007UALA00797 1 20070318 A 2912 271N2007 FILTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HYDRAULIC SYS CLOGGED A UALA O OTHER J WARNING INDICATION LD LANDING 1 WP 29 569UA 26677 LANDED UNDER AMBER ALERT DUE TO LOSS OF LEFT HYDRAULIC PRESSURE. REPLACED EDP FILTER MODULE ELEMENT IN LEFT TAIL SAIL A REA. CLEANED AREA AND SERVICED HYDRAULIC SYSTEM AND OPERATED FLIGHT CONTROL SYSTEM FOR FINAL TESTING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061900206 20070619 00206 2007 6 19 2007UALA01151 4 20070414 A 2565 D31517 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 428UA 523 CABIN EMERGENCY LIGHTS CHECK SHOWS -ATA 33 -51-38 EXT LOADS FWD L- RE-SET CIDS, MESSAGE RE-APPEARED. REPLACED DOOR 1L E SCAPE SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061900207 20070619 00207 NE 2007 6 19 2007UALA01243 2 20070420 A 7261 7T0320 SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE LEAKING A UALA O OTHER K FLUID LOSS CR CRUISE 1 WP 29 548UA 25396 726583 LOST BETWEEN 8-10 QTS OF OIL AT THE BEGINNING OF THE FLIGHT & BETWEEN 4-5 QTS THE LAST TWO HOURS OF THE FLIGHT. FOUND N R 2 ENG DEOILER OIL SEAL LEAKING. REPLACED DEOILER SEAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072600010 20070726 00010 EU 2007 7 26 AWXA200700861 1 20070719 A 2560 P2070001214 FLASHLIGHT AIRBUS 320 A320232 3930326 EU AFT GALLEY FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 642AW 584 LAS - EEL - LOG NR 4149046 - CREW REPORTED AFT GALLEY FLASHLIGHT BATTERY INOP. MX REPLACED THE AFT GALLEY FLASHLIGHT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007061900209 20070619 00209 EU 2007 6 19 2007UALA01795 1 20070603 A 5210 STRAP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR OUT OF ADJUST A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 405UA 452 DOOR 2L HARD TO ARM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061900210 20070619 00210 NM 2007 6 19 2007UALA01796 1 20070603 A 3350 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 848UA 1647 LEFT FWD BATTERY PACK FAILED DURING 3 SERVICE EMERGENCY LIGHTS TEST. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061900211 20070619 00211 EU 2007 6 19 2007UALA01797 1 20070602 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE AFT GALLEY ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 445UA 826 HOT OR BURNING ELECTRICAL SMELL COMING FROM AREA OF AFT GALLEY, NO VISIBLE SIGNS OF SMOKE NOTED. NO LIGHTING ISSUES IN GALLEY OR AFT PASS CABIN NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061900212 20070619 00212 NM 2007 6 19 2007UALA01798 1 20070603 A 3260 INDICATOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 177UA 24384 THE -GEAR MONITOR- EICAS STATUS MESSAGE DISPLAYED. PRIMARY & ALTERNATE LANDING GEAR POSITION INDICATION DISAGREE. [07- 27-07] ACCOMPLISHED PROXIMITY ELECTRONICS UNIT SYSTEM TEST NO FAULTS PSEU OPERATES NORMAL. CLEANED BLEED ISOLATION VAL VE CONNECTOR. OPERATED NUMERS TIMES, CHKS OK. MESG LINKED TO NR 4 HYD SYS TEMP INDC. AFTER CHRONIC PROBLEM & REPEATED TROUBLESHOOTING, RPL TEMP XMITTER. NR 4 HYD SYS OPS CKS NORMAL. ALSO FOUND WIRES CHAFED THROUGH IN SEVERAL SPOTS IN SAI L TAIL AREA AND ONE SOCKET PUSHED BACK A LITTLE AT CONNECTOR D43700P. REPLACED WIRES W4544-231-20R & B PER SVCE TIP. QT Y INDICATION NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007061900213 20070619 00213 NM 2007 6 19 2007UALA01800 1 20070605 A 5280 DOOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RT MLG DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 671UA 30026 LARGE STRUT DOOR AT RIGHT MAIN GEAR FOUND DAMAGED DURING WALKAROUND. [07-31-07] REPLACED RT MAIN GEAR STRUT DOOR PER MM 32-12-01. ACCOMPLISHED RII INSPECTION OF RH STRUT DOOR INSTALLATION, RIGGING, GEAR SWING AND ALTERNATE EXTENSION PER MM 32-12-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072600011 20070726 00011 EU 2007 7 26 AWXA200700869 1 20070721 A 2560 P20700010214 FLASHLIGHT AIRBUS 320 A320232 3930326 EU FWD CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 662AW 1274 PHX - EEL - LOG NR 7467899 - CREW REPORTED FWD FA FLASHLIGHT BATTERY INOP. MX REPLACED THE FWD FA FLASHLIGHT. OPERATIO NAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007061900215 20070619 00215 NM 2007 6 19 2007UALA01805 1 20070601 A 3350 58673 INVERTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 563UA 26665 EEL LIGHTS INOP FROM ROW 30 TO AFT GALLEY. REPLACED INVERTER. OP CHECKS OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061900216 20070619 00216 NM 2007 6 19 2007UALA01806 1 20070601 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 563UA 26665 F/O AISLE LIGHT INOPERATIVE. [06-22-07] RELAMPED OPS CHECK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061900218 20070619 00218 NM 2007 6 19 2007UALA01809 1 20070603 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 596UA 28749 EXTERIOR EMERGENCY EXIT LIGHT OUT AT DOOR 2L. [06-22-07] RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061900219 20070619 00219 NM 2007 6 19 2007UALA01810 1 20070603 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY FLOOR LIGHTING AT SEAT 3A HANGING FROM SEAT FWD LIGHT. [06-22-07] SECURED LIGHT ASSY CHKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007061900221 20070619 00221 NM 2007 6 19 DHL2007740551 1 20070613 A 5320 INTERCOSTAL BOEING 727 7272Q9 138448M NM BS 312 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 INTERCOSTAL AT LT HORIZONTAL WALKWAY, BS 312, IS CRACKED AND CORRODED. REMOVED DAMAGED INTERCOSTAL, FABRICATED NEW INTE RCOSTAL BRACKET FROM 2024-T3, .040" BY 8" BY 4", PO NR 9005089, TREATED, PRIMED, AND INSTALLED INTERCOSTAL IAW B727 SRM 53-10-2 FIG 2, 51-20-1, 51-10-2, AND 51-302. 2 L 7 3 4F RT A3WE 2007061900222 20070619 00222 2007 6 19 QXEA200700969 2 20070616 A 7200 UNKNOWN DHAV DHC8 DHC8202 2809007 NM NR 1 ENGINE UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 345PH 476 PDX FLIGHT NR 2149, DURING DAILY SYSTEM CHECK BETA BACK UP NR 1 ENGINE MANUAL CAUTION LIGHT CAME ON. RESET BETA BACKUP SYSTEM. CAUTION LIGHT EXTINGUISHED. NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061900223 20070619 00223 NM 2007 6 19 NWAA072136729 1 20070613 A 2611 SMOKE DETECTOR BOEING 747 747251F 1384898 NM CARGO BAY MALFUNCTIONED A NWAA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 01 629US 22388 DURING CRUISE, MAIN DECK CARGO SMOKE DETECTOR NR 4 CARGO FIRE LIGHT AND MASTER FIRE WARNING CAME ON. THERE WAS NO SMOKE OR FIRE VISIBLE ON MAIN DECK. LIGHT STAYED ON UNTIL 12,000 FT ON DESCENT FOR LANDING (ON STEADY FOR 20 MIN). FLIGHT C ONTINUED ON TO NRT, AND LANDING WAS UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED BOTH 4A AND 4B MAIN DECK SMOKE DETECTO RS PER MC REQUEST. OPERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F A20WE 2007061900227 20070619 00227 EU 2007 6 19 SA07037 1 20070615 A 3350 32145410 EPSU AIRBUS 320 A320214 3930316 EU CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 119US 22963 1268 LAX - THE MID-CABIN, LEFT HAND EMERGENCY POWER SUPPLY UNIT FAILED THE OPERATIONAL CHECK. MAINTENANCE REPLACED THE MID-C ABIN, LEFT HAND EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007061900228 20070619 00228 EA 2007 6 19 TRAX200700827 1 20070613 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 973EV 7575 SERVICE DOOR LOWER SILL PLATE CORRODED. REFERTO EXELTECH W/O YUL000617 NRTC 200-24 FOR ALL WORK ACCOMPLISHED. SUPPLEME NTAL - SDR CLOSED 06/15/07. 2 L 7 2 4F RT A21EA 2007061900230 20070619 00230 EA 2007 6 19 TRAX200700814 1 20070609 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 976EV 7601 FLAPS FAIL AT 8 DEGREES AFTER TAKEOFF. COMPLIED WITH QRH LANDED FLAPS 8 DEGREES. A/C RETURNED TO ATL AFTER T/O. EMER GENCY DECLARED. FLTS 4438, 4797 CX. FOUND BROKEN WIRE ICE81C22BLU PIN B AT 1J9CE...REPAIRED WIRING IAW CRJ WMM CHAPTE R 20-11-00. INSTALLED SKEW DETECTION UNIT..FLAP SYSTEM OPS CHECKED GOOD IAW CRJ AMM 27-51-00. CHECKED GOOD. 2 L 7 2 4F RT A21EA 2007061900231 20070619 00231 EA 2007 6 19 TRAX200700815 1 20070611 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 917EV 7769 CAPTAIN'S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007061900234 20070619 00234 EA 2007 6 19 TRAX200700818 1 20070611 A 5210 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 F/A REPORTS MAIN DOOR HARD TO CLOSE AND LOCK PROPERLY. 2 L 7 2 4F RT A21EA 2007061900236 20070619 00236 EA 2007 6 19 TRAX200700821 1 20070613 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 973EV 7575 CRACK FOUND AT FS 280.00 FLOOR ANGLE IN LOWER FLANGE AT LBL 9.0. [06-21-07] REPAIR CARRIED OUT IAW REO 601R-53-11-171 REV C. 2 L 7 2 4F RT A21EA 2007061900238 20070619 00238 EA 2007 6 19 TRAX200700823 1 20070613 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 975EV 7599 LINTEL SUPPORT FITTING P/N 601R35050-109 CRACKED ON AFT PRESSUE BULKHEAD. 2 L 7 2 4F RT A21EA 2007061900239 20070619 00239 EA 2007 6 19 TRAX200700824 1 20070613 A 5210 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 390CA 10106 PAX DOOR AFT DRAG ANGLE CRACKED (MARKED). [06-21-07] REPAIRED PAX DOOR AFT DRAG ANGLE IAW BOMBARDIER REO 670-52-11-07 2. 2 L 7 2 4F RT A21EA 2007061900243 20070619 00243 NM 2007 6 19 NWAA072146729 1 20070613 A 2697 CONNECTOR BOEING 747 747251F 1384898 NM SMOKE DETECTOR DIRTY A NWAA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 01 629US 22388 WHILE IN CRUISE, MAIN DECK CARGO SMOKE DETECTOR NR 4 CARGO FIRE LIGHT AND MASTER FIRE WARNING CAME ON. NO SMOKE OR FIRE WAS VISIBLE IN MAIN DECK. FLIGHT CONTINUED ON TO ICN AND LANDING WAS UNEVENTFUL. LIGHTS STAYED ON UNTIL 5,500 FT ON D ESCENT FOR LANDING (ON STEADY FOR 20 MINUTES). MAINTENANCE CLEANED BOTH 4A AND 4B SMOKE DETECTOR ELECTRICAL PLUGS AND S ECURED LAMP HOLDER. OPERATIONAL CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F A20WE 2007061900244 20070619 00244 WP 2007 6 19 NWAA072169751 1 20070613 A 2720 YAW DAMPER DOUG DC9 DC941 302207N WP RUDDER MALFUNCTIONED A NWAA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 01 751NW 47115 IN LEVEL FLIGHT AT 12,000 FT AND 250 KNOTS WITH AUTOPILOT OFF, THE PILOT IN COMMAND EXPERIENCED UNRESPONSIVE RUDDER CONT ROL. THE CAPTAIN REQUESTED THE FIRST OFFICER ATTEMPT CONTROL AND HE DID HAVE EFFECTIVE RUDDER CONTROL. THE CAPTAIN RET RIED CONTROL OF THE RUDDER AND IT RESPONDED PROPERLY. NO APPLICABLE COM PROCEDURES TO COMPLY WITH. THE AIRCRAFT LANDED NORMALLY AND SAFELY AT SCHEDULED DESTINATION. MAINTENANCE REPLACED THE YAW DAMPENER ACTUATOR, HYDRAULIC POWER RUDDER A CTUATOR, AND THE AUTOPILOT STAB-AUG COMPUTER. FUNCTIONAL CHECKS WERE GOOD AND THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007061900245 20070619 00245 EA 2007 6 19 TRAX200700831 1 20070613 A 2560 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA MEDICAL KIT STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 850AS 7355 FLIGHT EMERGENCY MEDICAL KIT STORAGE COMPARTMENT WILL NOT OPEN. FLT 4392 DEL 34 MINS. 2 L 7 2 4F RT A21EA 2007061900246 20070619 00246 SO 2007 6 19 SIMA200716901 1 20070614 A 2750 4188001007 FLAP SYSTEM EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A SIMA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SW 21 690AE 6793 14500858 HUMMING NOISE INFLIGHT WITH FLAPS IN UP POSITION, NOISE GOES AWAY WITH FLAPS DEPLOYED. REMOVED AND REPLACED PCA AND COM PLIED WITH LEFT INBOARD FLAP SEAL PLATE MOD IAW EMB AMM 27-12-01. OPERATIONAL CHECKED GOOD WITH NO DEFECTS NOTED, RETUR NED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061900248 20070619 00248 2007 6 19 SIMA200716902 2 20070614 A 7261 1103P0620 PRESSURE SWITCH SAAB SF340 340B 7860101 EU ENGINE FAILED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 236AE 340B236 POWER SET AT 98 PERCENT WITH CTOT THE RIGHT ENGINE FELL OFF TO APPROXIMATELY 35 PERCENT TORQUE. REMOVED AND REPLACED RI GHT ENGINE P3 SWITCH ON AUTOCOARSER SYSTEM IAW SAAB AMM 61-22-00. PERFORMED CTOT AND APR OPERATIONAL CHECK WITH NO DEFE CTS IAW SAAB AMM 71-00-00. PERFORMANCE RUN WAS ACCOMPLISHED WITH NO DEFECTS IAW SAAB 71-00-00. RETURNED AIRCRAFT TO SE RVICE. 2 L 7 2 4T RT A52EU 2007061900249 20070619 00249 EA 2007 6 19 SIMA200716906 1 20070615 A 3210 492079 TORQUE LINK CNDAIR CL600 CL6002C10 1390015 EA RT MLG WORN A SIMA O OTHER E VIBRATION/BUFFET LD LANDING 1 SW 21 508AE 10914 10072 VIBRATION FELT FROM RIGHT MAIN GEAR ON LANDING. REMOVED AND REPLACED RIGHT MAIN GEAR UPPER AND LOWER TORQUE LINKS AND S HIMMY DAMPENER IAW CRJ AMM 23-11-37, 32-11-39 AND 32-11-40. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007061900250 20070619 00250 EA 2007 6 19 TRAX200700833 1 20070614 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 750EV 10161 CEILING EMERGENCY LIGHT 2ND FROM INOP. 2 L 7 2 4F RT A21EA 2007061900251 20070619 00251 EA 2007 6 19 TRAX200700834 1 20070614 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 750EV 10161 CEILING EMERGENCY LIGHT 2ND FROM AFT INOP. 2 L 7 2 4F RT A21EA 2007061900252 20070619 00252 EA 2007 6 19 TRAX200700835 1 20070614 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 846AS 7328 EMERGENCY FLOOR LIGHTING INOP AT 11CD. 2 L 7 2 4F RT A21EA 2007061900254 20070619 00254 EA 2007 6 19 TRAX200700837 1 20070614 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 751EV 10163 FLIGHT COMPARTMENT FLOORBOARD AFT LANDING BRACKET CRACKED AT FS 280.00. [06-27-07] REPAIRED IAW 51-00-00, 51-00-00, AND REO 670-53-11-047. 2 L 7 2 4F RT A21EA 2007061900256 20070619 00256 NM 2007 6 19 SWAA072982 1 20070611 A 3320 059393 LIGHT BOEING 737 7373H4 1384600 NM CABIN FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 329SW 23693 F/A REPORTED BURNING SMELL FROM OVERHEAD CABIN LIGHT AT ROW 19 DEF. REMOVED AND REPLACED LIGHT BALLAST AND LIGHT ASSY P ER MM. 2 L 7 2 4F RT A16WE 2007061900257 20070619 00257 NM 2007 6 19 SWAA072981 1 20070611 A 2530 41600019 COFFEEMAKER BOEING 737 7377H4 1384404 NM REAR GALLEY FAULTY A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 29 767SW 29807 DIVERSION, AT ALTITUDE F/A REPORTED ELECTRICAL ODOR IN REAR GALLEY, TURNED POWER OFF ODOR WENT AWAY. REMOVED AND REPLAC ED AFT COFFEEMAKER PER MM. 2 L 7 2 4F RT A16WE 2007061900258 20070619 00258 NM 2007 6 19 2007UALA01808 1 20070602 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 578UA 26694 FLOOR MOUNTED ESCAPE PATH LIGHT STRIP INOP AT MID LAV. [06-22-07] RECONNECTED LAMP TO FWD POWER CABLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061900259 20070619 00259 EU 2007 6 19 2007UALA01815 1 20070602 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 416UA 479 FWD BULKHEAD EMERGENCY EXIT SIGN HAS 1 LAMP OUT, CTR AISLE OVERWING FWD EXIT SIGN HAS 3 EA LAMPS INOP, CTR AISLE AFT SID E OVERWING EXIT SIGN HAS 4 EA LAMPS OUT, LEFT OVERWING EXIT SIGN HAS 1 EA LAMP INOP, RIGHT AFT DOOR OVERHEAD EXIT SIGN H AS 2 EA LAMPS INOP & RIGHT AFT DOOR AFT LWR SIDE WALL EXIT SIGN HAS 1 LAMP INOP. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061900261 20070619 00261 NM 2007 6 19 2007UALA01817 1 20070603 A 3397 CONNECTOR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 930UA 26655 EEL LIGHTS INOP FROM ROW 4 AFT TO ROW 12. [06-22-07] DISCONNECTED CONNECTOR FEEDER CLEANED CONTACT, RETESTED LIGHTS A LL OP CHECKED NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007061900270 20070619 00270 2007 6 19 2007UALA01821 4 20070604 A 2565 B14056015 O-RING BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EVAC SLIDE LEAKING A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 923UA 26643 LOW BOTTLE PRESSURE. THERE WAS A SMALL LEAK AROUND THE FILLER VALVE O-RING. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007061900279 20070619 00279 NM 2007 6 19 2007UALA01824 1 20070604 A 5753 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE T/E FOREFLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 174UA 24381 RIGHT WING INBOARD TRAILING EDGE FOREFLAP LOWER SURFACE CRACKED. LENGTH OF CRACK IS APPROX 7.5 FEET SPANWISE, APPROX 6 INCHES FROM LEADING EDGE. [07-27-07] REPLACED RIGHT HAND INBOARD FOREFLAP IN ACCORDANCE WITH MM 27-51-02 PAGE 401. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007061900282 20070619 00282 NM 2007 6 19 2007UALA01826 1 20070604 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 FWD PIT DOOR CUTOUT AFT FRAME IS DAMAGED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA & INSTALLED NEW FRAME P/N 6 5-20723U54. 2 L 7 2 4F 4 F RT A16WE E21EU 2007061900288 20070619 00288 EU 2007 6 19 2007UALA01828 1 20070604 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LOW A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 465UA 1341 CREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. CREW COMMENTS: OXYGEN DOWN TO 900. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061900301 20070619 00301 2007 6 19 2007UALA01833 4 20070604 A 2565 LATCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 LEFT OVERWING SLIDE COMPARTMENT NR 3 LATCH BROKEN (MISSING DRIVE PIN AND REAR SPRING). [07-31-07] REPLACED NR 3 LATC H AT LT OVERWING SLIDE COMP DOOR IAW 25-65-09 INSTALLATION TEST OF LATCH GOOD IA W 25-65-09. SLIDE PROBLEM ROOT CAUSE: VIBRATION CAUSES FRETTING IN THE LATCH ASSY & EVENTUAL FRACTURE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007061900315 20070619 00315 NM 2007 6 19 QXEA200700953 1 20070609 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - SEAT TRACK NR 12 AT STATION X116 TO X128, X142 TO X160, X176 TO X194, X206 TO X220 HAS MINOR SCRATCHES AND CHAF ES. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007061900317 20070619 00317 NM 2007 6 19 2007UALA01837 1 20070606 A 3397 58791 CABLE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN CONTAMINATED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 902UA 25002 AFT 10 FEET OF FLOOR MOUNTED EMERGENCY ESCAPE PATH LIGHTING IS INOP. FOUND HIGH MOISTURE CONTENT RUNNING THROUGH AFT SE CTION OF EEL STRIP. EXPOSED AND DRIED ALL MOISTURE. REPLACED AFT SECTION OF POWER CABLE AND CLEANED LAMP PINS. OP CHE CKS OKAY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007061900318 20070619 00318 NM 2007 6 19 2007UALA01838 1 20070606 A 2761 ACTUATOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU SPOILERS MALFUNCTIONED A UALA O OTHER O OTHER LD LANDING 1 WP 29 370UA 24539 AUTO SPEED BRAKE DID NOT DEPLOY ON LANDING. REPLACED ACTUATOR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007061900322 20070619 00322 NM 2007 6 19 2007UALA01842 1 20070605 A 3350 STRIP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN TORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 558UA 26654 EXIT PATH LIGHTING STRIP IS TORN AND A TRIPPING HAZARD AT 13ABC & 29ABC. [06-22-07] SECURED COVERS. LIGHTS OP NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061900323 20070619 00323 NM 2007 6 19 2007UALA01843 1 20070605 A 3350 SIGN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 544UA 25322 CEILING EMERGENCY EXIT SIGN AT OVERWING DOORS IN INOP. [06-22-07] REPLACED BATTERY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061900324 20070619 00324 NM 2007 6 19 2007UALA01844 1 20070605 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 544UA 25322 EMERGENCY EXIT LIGHT AT 25ABC IS INOPERATIVE. REPLACED LAMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061900325 20070619 00325 NM 2007 6 19 2007UALA01845 1 20070605 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 502UA 24623 EEL STRIP AT ROW 15ABC INOPERATIVE. [06-22-07] REPLACED 15 ABC EEL STRIP. OPS CHECK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062000001 20070620 00001 EU 2007 6 20 PNSA070601 1 20070608 A 7712 INDICATOR SAAB SF340 SF340A 7850100 EU COCKPIT FAULTY A PNSA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 AL 03 110XJ 340A110 RIGHT ENGINE ERRATIC TORQUE INDICATIONS ABORTED TAKEOFF. REMOVED AND REPLACED TORQUE INDICATOR. 2 L 7 2 4T RT A52EU 2007062000038 20070620 00038 NM 2007 6 20 2007UALA01847 1 20070606 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY LIGHT INOP DOOR 5L SLIDE ILLUMINATED. [06-22-07] RELAMPED. OPS. NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000039 20070620 00039 NM 2007 6 20 2007UALA01848 1 20070606 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 182UA 25279 D-ZONE RIGHT SIDE EEL LIGHTS BLINK ON AND OFF. [06-22-07] REPLACED BATTERY PACK OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000042 20070620 00042 NM 2007 6 20 2007UALA01851 1 20070603 A 5210 SPRING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU PAX DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 FWD ENTRY DOOR TORQUE TUBE SPRING CORRODED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062000044 20070620 00044 2007 6 20 2007UALA01853 4 20070606 A 2210 AUTOPILOT SYS BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE COCKPIT FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 665UA 29237 CENTER & RIGHT AUTOPILOTS FAILED CAUSING A DIVERSION. [07-31-07] RE-ALIGNED RT FCC. STILL HAD PROBLEM. REPLACED LE FT ELEVATOR SERVO VALVE ASSY. RELOADED NAV DATABASE. TESTS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062000046 20070620 00046 NM 2007 6 20 2007UALA01855 1 20070606 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 STA 787 STR 23R STR CLIP IS CRACKED. MAJOR REPAIR ACCOMPLISHED, INSTALLED NEW STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062000049 20070620 00049 NM 2007 6 20 2007UALA01858 1 20070606 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 AFT PIT LOWER SKIN ANTENNA CUTOUT CORRODED AT STA 1430 LBL 2. MAJOR REPAIR ACCOMPLISHED: REMOVED ANTENNA DOUBLER TO FA CILITATE CORROSION REMOVAL. FABRICATED & INSTALLED A NEW -31 DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062000051 20070620 00051 EU 2007 6 20 2007UALA01860 1 20070606 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 480UA 1555 EMERGENCY PATH LIGHTS AT 14 & 19 ABC INOPERATIVE. [07-03-07] RELAMPED OPS CK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062000059 20070620 00059 NM 2007 6 20 2007UALA01868 1 20070606 A 5320 DOUBLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 CABIN FLOOR SHEAR WEB DOUBLER AT RBL 50, BS 1680 HAS CORROSION ON UPPER SURFACE. [08-07-07] REMOVED CORROSION ONTHIC KNESS 0.080, REMAINING 0.076 FOUND TO BE WITHIN LIMITS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062000060 20070620 00060 NM 2007 6 20 2007UALA01869 1 20070606 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 524UA 24977 RIGHT AFT SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOP. [06-22-07] RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072600012 20070726 00012 EU 2007 7 26 AWXA200700870 1 20070722 A 3350 32145410 BATTERY PACK AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHT NO TEST A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 627AW 29676 3160 66 LAS - EEL - LOG NR 4123399 - CREW REPORTED FWD LEFT EMERGENCY LIGHT BATTERY PACK FAILED TEST. MX REPLACED THE BATTERY P ACK PER AMM 33-51-38. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007061800174 20070618 00174 NM 2007 6 18 CALA0700299 1 20070609 A 5311 6546552 FRAME BOEING 737 7373T0 1384582 NM BS 827 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12313 23364 INSPECTION FOUND FRAME CORRODED AT RIGHT AFT BAGGAGE BIN, STA 827, S27R. THE FRAME WAS REPAIRED IAW SRM 53-00-07, REPAI R 3. 2 L 7 2 4F RT A16WE 2007061800175 20070618 00175 NM 2007 6 18 CALA0700300 1 20070610 A 5330 6545800 SKIN BOEING 737 7373T0 1384582 NM BS 328 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12313 23364 INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT AFT LOWER CORNER OF R-1 DOOR, STA 328, S17R - S17L. THE CRACKED AR EA OF SKIN WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-10-01. 2 L 7 2 4F RT A16WE 2007061800176 20070618 00176 NM 2007 6 18 CALA0700301 1 20070610 A 5313 BAC15061773 STRINGER BOEING 737 7373T0 1384582 NM BS 878-890 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12313 23364 INSPECTION FOUND STRINGER 17R CORRODED ON UPPER FLANGES AND BELOW ATTACHING WEBS AT STA 878-890, RBL 70. THE CORRODED S ECTION OF STRINGER WAS REMOVED AND REPLACED IAW SRM 51-70-12. 2 L 7 2 4F RT A16WE 2007061800177 20070618 00177 WP 2007 6 18 MWEA070140 1 20070608 A 2150 1173T15 SWITCH DOUG DC9 DC982 3022082 WP LT PACK INOPERATIVE A MWEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 13 809ME 48071 THE LEFT PACK PRESS INDICATED 13 PSI. REMOVED AND REPLACED TEMPERATURE SWITCH. 2 L 7 2 4F A6WE 2007061800178 20070618 00178 NM 2007 6 18 SWAA072885 1 20070607 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061800179 20070618 00179 NM 2007 6 18 SWAA072867 1 20070607 A 5311 6546532 FRAME BOEING 737 7375H4 138449D NM BS 482 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061800180 20070618 00180 NM 2007 6 18 SWAA072913 1 20070608 A 5311 65C229091 FRAME BOEING 737 7373H4 1384600 NM BS 500C S20L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061800181 20070618 00181 NM 2007 6 18 SWAA072908 1 20070608 A 5754 65C26602 SKIN BOEING 737 7373H4 1384600 NM NR 2 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND LEFT WING NR 2 L/E SLAT CRACKED AT OUTBOARD AUX TRACK. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007061800182 20070618 00182 NM 2007 6 18 SWAA072883 1 20070607 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007061800186 20070618 00186 NM 2007 6 18 QXEA200700945 1 20070607 A 5350 PANEL BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - SURFACE CORROSION AT AFT OUTBOARD CORNER OF APERTURE FOR PANEL 144JZ STATION X783. REPAIRED IAW SRM 51-14-00. 2 H 7 2 4T RT A13NM 2007061800187 20070618 00187 NM 2007 6 18 QXEA200700948 1 20070609 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - SEAT TRACK NR 15 AT STATION X612 TO X624, X634, X654 TO X664 HAS MINOR SCRATCHES AND CHAFES. REPAIRED IAW RD8/ 4-53-884. 2 H 7 2 4T RT A13NM 2007061800210 20070618 00210 2007 6 18 ABXA070181 4 20070605 A 2565 101623303 SLIDE BOEING 767 767205 1385121 NM PAX DOOR UNWANTED DEPLOY A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 270 23058 FIRST OFFICER DEPLOYED SLIDE INADVERTANTLY. REMOVED AND REPLACED MAIN ENTRY DOOR SLIDE IAW B767 AMM 21-58-1-1. 2 L 7 2 4F RT A1NM 2007061800240 20070618 00240 NM 2007 6 18 SWAA072879 1 20070607 A 5322 69353656 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007061800244 20070618 00244 2007 6 18 SWAA072897 4 20070608 A 2565 D31354125 SLIDE BOEING 737 7375H4 138449D NM L2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007061800254 20070618 00254 NM 2007 6 18 SWAA072865 1 20070606 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 718SW 27852 EEPLS PHOTOLUMINESCENT STRIP LOOSE BETWEEN ROW 6 DEF AND ROW 11 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007061900006 20070619 00006 NM 2007 6 19 SWAA072923 1 20070608 A 5230 6517952 SKIN BOEING 737 7373T5 1384608 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED C1 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT DOOR HANDLE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900009 20070619 00009 NM 2007 6 19 SWAA072921 1 20070611 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900019 20070619 00019 WP 2007 6 19 ASAA0781776 1 20070603 A 5753 5930496509 SKIN DOUG DC9 DC983 3022083 WP T/E FLAP VANE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 LEFT OUTBOARD FLAP VANE LEADING EDGE IS CHAFED AT INBOARD SIDE. REMOVED DAMAGED EXISTING DOUBLER. INSTALLED REPLACEMEN T DOUBLER PER SRM 51-70-2. 2 L 7 2 4F RT A6WE 2007061900029 20070619 00029 EU 2007 6 19 SA07036 1 20070608 A 2421 740119H IDG AIRBUS A319 A319112 3930323 EU NR 1 ENGINE FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 753US 22437 458 1326 SYR - FLT 1796 EN ROUTE SYR - PHL. ON ROTATION, THE AIRCRAFT LOST ESSENTIAL AC POWER AND RELATED BUSSES, INCLUDING VHF 1 WHICH RUNS OFF THE 28V ESS DC BUS. ELECTRICAL POWER TO ESS AC BUS RETURNED WHEN AC ESS FEED WAS SELECTED TO ALTN. TH E FLIGHT RETURNED TO FIELD SYR AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NUMBER ONE ENGINE IDG. OP ERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007061900034 20070619 00034 EA 2007 6 19 COMA0760424 1 20070608 A 3234 601R751461 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 940CA 30958 7048 FLIGHT 4947 - AFTER TAKEOFF NOSE GEAR DID NOT RETRACT, AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REP LACED NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2007061900035 20070619 00035 CE 2007 6 19 DXTA200702259 1 20070612 A 2701 UNKNOWN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE CONTROL YOKE UNKNOWN E DXTA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 GL 07 303QS 5600343 ON TAKEOFF WHEN CONTROL YOKE PULLED BACK FOR ROTATION , SOMETHING APPARENTLY TRIED TO JAM CAUSING MOMENTARY INCREASE IN RESISTANCE. JAM STOPPED AND CONTROLS BROKE FREE WITH INCREASED PRESSURE. INSPECTED CONTROL YOKES AND BOOTS FOR BINDING, NONE NOTED. REMOVED TAIL PANEL FOR ACCESS TO PUSH RODS, SPRING AND BELLCRANK. MOVED FLIGHT CONTROLS FOUND NO NOISE OR G RINDING . INSPECTED CABLES IN TAILCONE NO DEFECTS NOTED. POWERED UP A/C ENGAGED AUTOPILOT RAN AUTO PILOT THRU SEVERAL FU LL TRAVELS NO DEFECTS NOTED, INSPECTED ELEVATOR ATTACH POINTS AND SURFACE NO DEFECTS NOTED. LUBED PULLEYS AND CABLES IN TAIL. APPLIED LIGHT BACK PRESSURE TO SURFACE DURING MOVEMENT OF CONTROLS WITH NO BINDING OR NOISE NOTED. SYSTEM OPS CHEC 2 L 7 2 4F 4 F RT A22CE E25EA 2007061900036 20070619 00036 CE 2007 6 19 DXTA200702260 1 20070613 A 2120 UNKNOWN CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE CABIN SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 659QS 5605359 AFTER THE APU WAS STARTED AND THE BLEED AIR SELECTED ON THE CABIN IMMEDIATELY FILLED W/SMOKE. PERFORMED SPEED BRAKE OPE RATIONAL CHECK IAW 400XP MM 27-60-00. OPS CHECKED GOOD. THE APU FAIL LIGHT CAME ON AND THE APU SHUT DOWN. REMOVED APU S/ N P-403 AND INSTALLED SERVICEABLE APU UNIT S/N P-333 I.A.W CESSNA 560XL M/M CH 49-10-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007061900037 20070619 00037 SO 2007 6 19 DJFA2007062 1 20070609 A 2150 8152403 ACM EMB 135 EMB135BJ 3260306 SO ALLSN AE300 AE3007A GL NR 1 SMOKE E DJFA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 909LX 1818 14500942 TRIP NR 1189775, CREW REPORTED AN ELECTRICAL ODOR AND DETECTED SMOKE IN THE CABIN. AIRCRAFT DIVERTED. REMOVED AND REPLA CED NR 1 AIR CYCLE MACHINE, OPS CHECKED GOOD. NO SMELL NOTED. 2 L 7 2 4F 4 F RT TE6CH 2007061900039 20070619 00039 CE 2007 6 19 DXTA200702261 1 20070613 A 2760 UNKNOWN BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE SPEEDBRAKES UNKNOWN E DXTA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 07 120QS RK409 WHILE IN A 3000FPM DESCENT, WE EXTENDED THE SPEEDBRAKES. AIRCRAFT ABRUPTLY ROLLED RT 12-15 DEGREES AND THEN JUST AS ABRU PTLY ROLLED LT AFTER APPROX 2 SECONDS. PERFORMED SPEED BRAKE OPERATIONAL CHECK IAW 400XP MM 27-60-00. OPS CHECKED GOOD 2 H 7 2 4F 4 F RT A16SW E25EA 2007061900040 20070619 00040 CE 2007 6 19 DXTA200702262 1 20070613 A 3150 WARNING MESSAGE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL ILLUMINATED E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 989QS 7500089 YD FAIL UPPER B CYAN CAS MESSAGE COME ON IN FLIGHT ABOUT 18,000 FT. COULD NOT DUPLICATE SWAPPED A AND B YAW AUGMENTATI ON COMPUTERS. OPS CHECK GOOD WORK DONE IAW CESSNA 750 MM CH 27-24-07. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007061900045 20070619 00045 EU 2007 6 19 07FDEA02131 1 20070614 A 2910 TRANSMITTER AIRBUS 310 A310324 3930206 EU HYD PRESSURE MALFUNCTIONED A FDEA R AUTOROTATION J WARNING INDICATION DE DESCENT 1 SO 25 806FD 458 LOST GREEN SYSTEM FLUID IN DESCENT. FOLLOWED ECAM PR OC AND QRH, GRAVITY EXTENDED THE GEAR PER QRH. AFTER PRESSURIZING GREEN HYD SYS DISCOVERED FLUID LEAKING FROM THE TOP OF THE GREEN SYS MANIFOLD AT THE PRESS XMITTER BASE. THE REST OF T HE STORY: AFTER TALKING WITH THE CREW THEY REPORTED A FEW MINUTES AFTER MANUALLY LOWERING THE GEAR THE GREEN SYS HYD IND ICATION CAME BACK AND IS READING IN THE MIDDLE OF THE HAT ON THE INDICATION. THE INDICATOR ON THE RESERVOIR WAS GOOD A S WELL ON WALK AROUND. FOUND DAMAGED HYD PRESSURE TRANSMITTER LT WHEEL WELL. REMOVED AND REPLACED HYD PRESSURE TRANSM ITTER ASSY PER MM 29-32-13-4. LEAK AND OPS CK GOOD. RESET GRAVITY EXTEND SYS AND STOWED CRANK HANDLE. RETURN TO SERVICE 2 L 7 2 4F RT A35EU 2007061900056 20070619 00056 WP 2007 6 19 UPS07849952 1 20070606 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 RIGHT OUTBOARD LEADING EDGE LWR RIB CRACKED AT XFS 634. STOP DRILLED CRACK. FABRICATED AND INSTALLE D 2 EA. REPAIR ANGLES IAW 57-02-0 FIG 02, 51-1-20D. 2 L 7 4 4F RT 4A25 2007061900058 20070619 00058 WP 2007 6 19 UPS07849955 1 20070609 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP CARGO BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:N/A PIT 33 HAS HOLE IN FLOOR ON RT SIDE APPROX 3 FEET AFT OF DOOR MARKED. REPAIRED HOLE IN FLOOR PIT 33 AS PER EO DC8-5320-8724-A. 2 L 7 4 4F RT 4A25 2007061900061 20070619 00061 EA 2007 6 19 COMA0760432 1 20070611 A 3234 7179015 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A COMA K NONE N FALSE WARNING CR CRUISE 1 SO 01 592SW 20652 7279 AT 4000FT AND 210KTS RECEIVED GEAR HORN, TERRAIN WARNING AND GEAR DOWN AMBER. CLEARED AFTER 45 SECONDS. GEAR IND TURNED WHITE AFTER 10 SECONDS. 2ND INCIDENT, FIRST HAD NO TERRAIN WARNING. PERFORMED OPERATIONAL TEST. REPLACED LANDING GEA R CONTROL ASSEMBLY. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007061900072 20070619 00072 NM 2007 6 19 MWEA070147 1 20070611 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM TRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 918ME 55180 LEFT ENGINE THRUST REVERSER UPPER DEFLECTOR DOOR ZEE FRAME IS CRACKED AT THE INBOARD END AT STATION 26. FABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007061900159 20070619 00159 EA 2007 6 19 TRAX200700810 1 20070607 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 976EV 7601 FLAPS FAIL CAUTION MSG WITH FLAPS AT 20 DEG. TOWER DECLARED EMERGENCY. EMERGENCY EQUIPMENT AS A PRECAUTION. 2 L 7 2 4F RT A21EA 2007061900176 20070619 00176 NM 2007 6 19 SWAA072938 1 20070611 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 971, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007061900189 20070619 00189 NM 2007 6 19 SWAA072973 1 20070612 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900191 20070619 00191 NM 2007 6 19 SWAA072960 1 20070612 A 5755 6572735 SKIN BOEING 737 7373H4 1384600 NM NR 7 SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING NR 7 SPOILER DELAMINATED AT UPPER SURFACE. REPAIRED SPOILER PER SRM. 2 L 7 2 4F RT A16WE 2007061900195 20070619 00195 NM 2007 6 19 SWAA072954 1 20070612 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007061900204 20070619 00204 NM 2007 6 19 2007UALA00699 1 20070307 A 2620 312N5503 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 BOTTLE NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 539UA 25223 BOTTLE 2 DISCHARGE LIGHT INOP, WON`T TEST. RELACED LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061900217 20070619 00217 NM 2007 6 19 2007UALA01807 1 20070602 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 578UA 26694 EXT EMERGENCY EXIT LIGHT INOP DOOR 4R. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061900240 20070619 00240 EA 2007 6 19 TRAX200700825 1 20070613 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 973EV 7575 PREVIOUSLY REPAIRED FLOOR ANGLE CRACKED AT FS 621 LT AND RT. [06-21-07] REPAIRED IAW REO 601R-53-61-117 REV:C. 2 L 7 2 4F RT A21EA 2007061900241 20070619 00241 EA 2007 6 19 TRAX200700829 1 20070613 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 973EV 7575 INTERCOSTAL CRACK BETWEEN FS 621 TO 625 LT AND RT. 2 L 7 2 4F RT A21EA 2007061900255 20070619 00255 EA 2007 6 19 TRAX200700838 1 20070614 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 846AS 7328 BOTTOM STEP ON DOOR BROKEN. 2 L 7 2 4F RT A21EA 2007061900262 20070619 00262 NM 2007 6 19 2007UALA01818 1 20070603 A 3510 BOTTLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CREW O2 LOW PRESSURE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 306UA 23667 PER CREW 2 O2 BOTTLE IN FWD CABIN LOW. REPLACED BOTTLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007061900263 20070619 00263 NM 2007 6 19 2007UALA01819 1 20070604 A 3397 58781 CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 307UA 23668 EEL LIGHTS INOP AFT OF ROW 15. REPLACED EEL CABLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007061900286 20070619 00286 NM 2007 6 19 2007UALA01827 1 20070604 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 FORWARD CARGO PIT DOORWAY FORWARD FRAME IS CRACKED AT LOWER STOP FITTING. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR DOUBLER ANGLES. 2 L 7 2 4F 4 F RT A16WE E21EU 2007061900293 20070619 00293 NM 2007 6 19 2007UALA01830 1 20070605 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 LEFT OVERWING EMERGENCY LIGHT FWD ASSY FWD BULB INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007061900297 20070619 00297 NM 2007 6 19 2007UALA01832 1 20070603 A 5320 RIVET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE MELTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 SECTION 41, STATION 399.5 HAS 6 MELTED RIVETS. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061900319 20070619 00319 NM 2007 6 19 2007UALA01839 1 20070606 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C 13802 EU CABIN MELTED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 307UA 23668 CREW REPORT: OVERHEAD LIGHT AT SEAT 5B OVERHEATED AND PRODUCED A BURNING SMELL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062000041 20070620 00041 NM 2007 6 20 2007UALA01850 1 20070606 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 WALL EEL INOP, UPPER DECK STAIRS WALL FWD WALL EEL. [06-22-07] REPAIRED FEEDER CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000043 20070620 00043 EU 2007 6 20 2007UALA01852 1 20070606 A 5610 WINDOW AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT DAMAGED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 498UA 1865 CREW REPORTS WINDOW VISIBILITY IS IMPAIRED AND HAS GOTTEN WORSE. WINDOW IS EXTREMELY HOT TO THE TOUCH. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062000047 20070620 00047 NM 2007 6 20 2007UALA01856 1 20070606 A 5320 WEB BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 PASS CABIN SHEAR WEB AT FWD ENTRY DOOR STA 360 TO 364 WL 208 TO 222 LBL 65 TO LBL 65 IS CRACKED. MAJOR REPAIR ACCOMPLIS HED, REMOVED & REPLACED SHEAR WEB. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062000048 20070620 00048 NM 2007 6 20 2007UALA01857 1 20070606 A 2120 UNKNOWN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN SMOKE A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 796UA 26931 RTFL WITH SMOKE IN THE CABIN. [07-06-07] FOUND MAT MSG 49-11150 "APU CONTROLLER FAILED". CONTINUED TROUBLE SHOOTING & DETERMINED SOURCE OF SMOKE WAS APU. REPLACED GTCP331-500B APU. ACCOMPLISHED APU VERIFICATION FLIGHT. AIRCRAFT OK FOR SERVICE. SUSPECT INTERNAL APU FAILURE ALLOWED SMOKE TO ENTER BLEED AIR SYSTEM. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007062000054 20070620 00054 NM 2007 6 20 2007UALA01863 1 20070607 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 171UA 24322 BUSSLE EMERGENCY LIGHTS FAULTY AT 5L & 2R. [06-22-07] RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000055 20070620 00055 NM 2007 6 20 2007UALA01864 1 20070607 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY LIGHT INOP AT 22GH FWD, 28ABC, 44HJK & SEAT 51HJK. [06-22-07] REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000062 20070620 00062 NM 2007 6 20 2007UALA01872 1 20070605 A 5270 PROXIMITY SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 555UA 26647 SLIDE ARMED LIGHT AT DOOR 2L IS DIM. [08-07-07] REPLACED MAIN LANDING GEAR DOOR WARNING MAGNETIC PROXIMITY SWITCH ASS Y. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062000063 20070620 00063 NM 2007 6 20 2007UALA01873 1 20070606 A 2820 FUEL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 642UA 25092 NOTICED DURING WALKAROUND INSPECTION RUNNING FUEL LEAK OUT OF UPPER PYLON AREA ON RIGHT ENGINE. [07-31-07] FOUND O-R ING ON COUPLING "AS" REF IPC 28-22-07 PAGE17 SPLIT IN TWO PIECES. PACKING WAS WRO INSTALLED REF IPC.FOUND O-RING BETWEEN COUPLING NUT AND ONE RETAINING RING INSTALLED INSTEAD OF IN BETWEEN BOTH RETAINING RINGS. REPLACED PN:MS29513-330 AT FR ONT SPAR MAIN FEED LINE COUPLING. LEAK CHECK SATIS. SUSPECT HEAT/COLD CYCLE, VIBRATION & SUBSEQUENT TIGHTENING CAUSED O -RING TO SPLIT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062000064 20070620 00064 NM 2007 6 20 2007UALA01874 1 20070606 A 5420 BUSHING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE MIGRATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 NR 2 ENG, UPPER LINK INBOARD BUSHING MIGRATED AT FWD POINT. [08-07-07] REPLACED BUSHING DURING C-CHECK NR 12 VIS IT. ALSO INSTALLED 2 EA REPAIR WASHERS. AIRCRAFT OK FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062000066 20070620 00066 CE 2007 6 20 BSAASDR0715 1 20070520 A 3620 WARNING SYSTEM BEECH 1900 1900D 1154162 CE BLEED AIR SYS MALFUNCTIONED A BSAA O OTHER N FALSE WARNING DE DESCENT 1 NM 05 237YV UE237 ON DESCENT THE RT BLEED FAIL ANNUNCIATOR ILLUMINATED. THE CREW LANDED WITH NO FURTHER INCIDENT. EXTENSIVE TROUBLESHOOT ING WAS COMPLETED WITH NO DEFECTS FOUND & MULTIPLE GROUND RUNS WERE COMPLETED, BUT COULD NOT DUPLICATE THE PROBLEM. 2 L 7 2 4T RT A24CE 2007062000067 20070620 00067 CE 2007 6 20 BSAASDR0716 1 20070530 A 3230 DIODE BEECH 1900 1900D 1154162 CE COCKPIT INTERMITTENT A BSAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 05 139ZV UE139 THE LANDING GEAR CONTROL CIRCUIT BREAKER TRIPPED WHEN GEAR DOWN WAS SELECTED. CREW EXTENDED GEAR BY MANUALLY PUMPING GE AR DOWN. REPLACED DIODES FOR THE LANDING GEAR SELECT SOLENOID, MULTIPLE GEAR SWINGS AND OPERATIONAL CHECK FLIGHT WERE B OTH GOOD. 2 L 7 2 4T RT A24CE 2007062000068 20070620 00068 CE 2007 6 20 BSAASDR0717 1 20070531 A 3610 1560283000 TUBE BEECH 1900 1900D 1154162 CE RT WING DAMAGED A BSAA O OTHER J WARNING INDICATION CR CRUISE 1 NM 05 131YV UE131 THE RIGHT BLEED AIR FAIL LIGHT CAME ON. CREW WAS CLOSEST TO DESTINATION, AND LANDED WITHOUT INCIDENT. FOUND & REPLACED DAMAGED EVA TUBING UNDER RT WING PANEL 611 NEAR NACELLE. SYSTEM OPS CHECK & LEAK CHECK GOOD. 2 L 7 2 4T RT A24CE 2007062000072 20070620 00072 NM 2007 6 20 FDKA200705221 1 20070522 A 3350 1317 LIGHT DHAV DHC8 DHC8101 2809002 NM CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 809LR 083 FDM 6182 JFK (1309 PHX LCL) - CREW REPORTED THE FLOOR AFT FLOOD LIGHT INOP. MX RELAMPED. 2 H 7 2 4T RT A13NM 2007062000074 20070620 00074 NM 2007 6 20 FDKA200706260 1 20070604 A 3350 1317 LIGHT DHAV DHC8 DHC8101 2809002 NM CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 809LR 083 FDM 6182 PVD (1732 PHX LCL) - REAR EMERGENCY ESCAPE PATH LIGHT OUT. MX RELAMPED. 2 H 7 2 4T RT A13NM 2007062000076 20070620 00076 SO 2007 6 20 FDKA200706268 1 20070610 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 853MJ 145464 FDM 6029 MCO-DAY (1609 PHX LCL) - EMERGENCY LIGHT ROW 12 OVERWING EMERG LIGHT WILL NOT ILLUMINATE. MX RECONNECTED EMERG LIGHT, OPS GOOD. 2 L 7 2 4T RT T00011AT 2007062000080 20070620 00080 WP 2007 6 20 07FDEA02121 1 20070613 A 5347 SEAT TRACK DOUG MD10 MD1010F 3022112 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CORRODED SEAT TRACK AT LBL 54 AFT BULK PIT AT STA 1801 TO 1840. [07-17-07] REMOVED, FABRICATED AND INSTALLED SEAT TRA CK IAW SRM 51-31-01 VOL II, 51-21-01 VOL II AND DWG. 3855. MINOR REPAIR. 2 L 7 3 4F RT A22WE 2007062000081 20070620 00081 WP 2007 6 20 07FDEA02122 1 20070613 A 5751 SKIN DOUG MD10 MD1010F 3022112 WP LT AILERON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 LT O/B AILERON BULGING AT FASTENERS ON SKIN. [07-17-07] REMOVED DAMAGED SKIN AND INSTALLED NEW SKIN IAW SRM 51-35-01 V OL II . MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2007062000082 20070620 00082 WP 2007 6 20 07FDEA02123 1 20070613 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 AFT SKIN DENTED AT APPROXIMATELY 5:00 POSITION ON FRAME AND IS WITHIN 18 INCHES OF RVSM (CENTER) PLATE. [07-17-07] REPAIRED SKIN IAW EA 8-5330-112937 MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2007062000086 20070620 00086 NM 2007 6 20 07FDEA02127 1 20070614 A 5347 ADA83891 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 MAIN DECK COMPARTMENT SEAT TRACK AT STA 819 RT X= -47.5" FOUND CROWN WORN. [06-29-07] MAIN DECK COMPARTMENT SEAT TRACK AT STA 819 RT X= -47.5" REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GM M 6-2-100. 2 L 7 3 4F RT A22WE 2007062000093 20070620 00093 NM 2007 6 20 KCSA071190 1 20070613 A 5315 FLOORBEAM BOEING 747 747221F 1384868 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 FLOORBEAM WEB DAMAGED AT LBL 109 TO 117 STA 1180 CRACKED 1 INCH. 2 L 7 4 4F A20WE 2007062000096 20070620 00096 NM 2007 6 20 CALA0700304 1 20070613 A 5553 65538342 FITTING BOEING 737 7373T0 1384582 NM VERTICAL STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12313 23364 INSPECTION FOUND VERTICAL STABILIZER LEFT AFT LUG FAILSAFE FITTING CORRODED AT STA 1088-1104. THE FITTING WAS REMOVED A ND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007062000100 20070620 00100 GL 2007 6 20 C2XA07IA138 2 20070614 A 7261 CARBON SEAL EMB 145 EMB145EP 3260221 SO ALLSN AE300 AE3007A GL NR 1 ENGINE WORN A C2XA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 27 13936 18715 5402 145025 CAE310025 IAH - FLIGHT 2902, DURING CLIMB THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS , AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (OPEN) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007062000103 20070620 00103 SO 2007 6 20 C2XA07IA139 1 20070614 A 2612 47359713 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO CARGO BAY MALFUNCTIONED A C2XA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SW 27 34111 13095 13095 145659 IAH - FLIGHT 2556, DURING TAKEOFF THE CREW REPORTED A BAGGAGE SMOKE WARNING. THE FIRE EXTINGUISHERS WERE DISCHARGED AS A PRECAUTION, AND THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE NR 1 CARGO SMOKE DETECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVE D FOR RETURN TO SERCVICE. 2 L 7 2 4F RT 2007062000105 20070620 00105 NM 2007 6 20 UPS07649969 1 20070512 A 5347 SEAT TRACK BOEING 767 76734AF 1385212 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 306UP 27759 INSPECTION TYPE:2C SEAT TRACK CORRODED. REPAIRED IAW SRM 53-00-52-2R REPAIR 9. 2 L 7 2 4F RT A1NM 2007062000106 20070620 00106 WP 2007 6 20 UPS07849959 1 20070609 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE STA XFS 597 INTERNAL RIB IS CRACKED AT LWR END. STOP DRILLED CRACK. FABRICAT ED AND INSTALLED 2 REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2, 51-1-20D. 2 L 7 4 4F RT 4A25 2007062000108 20070620 00108 WP 2007 6 20 UPS07849961 1 20070610 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 LEFT WING CENTER LEADING EDGE LOWER RIB CRACKED AT XFS 334. STOP DRILLED CRACK, FABRICATED AND INSTA LLED REPAIR DOUBLERS IAW SRM 57-3-3 FIG 007, 51-1-20D. 2 L 7 4 4F RT 4A25 2007062000109 20070620 00109 WP 2007 6 20 UPS07849962 1 20070608 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 LEFT WING O/B LEADING EDGE LWR RIB CRACKED AT XFS 796. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-00 FIG 2, 51-1-20D. 2 L 7 4 4F RT 4A25 2007062000111 20070620 00111 WP 2007 6 20 UPS07849964 1 20070608 A 5730 576958927 DOUBLER DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 RIGHT WING CENTER LEADING EDGE LWR INNER DOUBLER CRACKED AROUND DRAIN HOLE AT XFS 334. REMOVED, FABR ICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21, 51-1-20D AND DWG 5769589. 2 L 7 4 4F RT 4A25 2007062000113 20070620 00113 2007 6 20 UPS07849967 4 20070613 A 2565 WINDOW DOUG DC8 DC871F 302199D WP ESCAPE SLIDE DIRTY A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:N/A ESCAPE SLIDE VIEWING WINDOW INOP. REMOVED COVER FROM SLIDE. CLEANED WINDOW, SECURED SLIDE TO DOOR & VERIFIED PROPER CYLINDER PRESSURE, REF MM 25-60-01-2. 2 L 7 4 4F RT 4A25 2007062000114 20070620 00114 WP 2007 6 20 UPS07849968 1 20070613 A 3350 LIGHT DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:N/A EMERGENCY LIGHTS DISENGAGED. LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPS CHECK GOOD IAW MM 33-10-00. 2 L 7 4 4F RT 4A25 2007062000115 20070620 00115 EU 2007 6 20 200706151 1 20070614 A 3297 CONNECTOR EMB ERJ170 ERJ170100SE 3260406 EU STEERING SYS LOOSE A UHLA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 11 650RW 17000071 FLIGHT 7727 DEN TO CID WHILE ON APPROACH, EXTENDING THE LANDING GEAR, CREW RECEIVED A -STEER FAIL- EICAS MESSAGE. DECLA RED EMERGENCY AND LANDED WITHOUT INCIDENT. OCM INSPECTED NOSE GEAR AREA; FOUND STEERING FEEDBACK SENSOR CONNECTOR LOOSE . RESECURED CONNECTOR. POWERED UP ACFT, THE ONLY ACTIVE MESSAGE WAS -STEERING OFF-. APPLIED HYDRAULICS, -STEER OFF- M ESSAGE EXTINGUISHED. STEERING OPS CHECKED GOOD. 2 L 7 2 4F RT A56NM 2007062000116 20070620 00116 NM 2007 6 20 2007UALA01585 1 20070519 A 5210 S140T263157 SEAL BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE L2 DOOR OUT OF ADJUST A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 775UA 26947 DOOR 2L WON'T ARM. *S/D* ADJUSTED LOWER DOOR SEAL ON DOOR 2L. OP CHECKS NORMALLY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007062000117 20070620 00117 NM 2007 6 20 2007UALA01597 1 20070521 A 3040 SENSOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE WINDOW HEAT FAULTY A UALA O OTHER O OTHER CR CRUISE 1 WP 29 117UA 28810 WINDOW HEAT 2R COMES BACK ON AFTER 2 HRS AND WINDOW IS HOT. THERMOSTAT (S761) FAILS TO OPEN AT THE RIGHT TEMPERATURE. WIRING IS DISCONNECTED TO S761 AND NEEDS SPLICING, S761 NEEDS REPLACING. SWAPPED SENSOR S761. RESET CMC & NO REPEAT OF MESSAGE. A/C RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000122 20070620 00122 NM 2007 6 20 2007UALA01930 1 20070611 A 5420 BUSHING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT PYLON MIGRATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 RIGHT PYLON STRUT, INBOARD MIDSPAR FITTING, INBOARD LUG BUSHING MIGRATED. [08-08-07] REMOVED AND REPLACED BUSHINGS P ER SRM 54-53-90, REPAIR 3. AIRCRAFT OK FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071600002 20070716 00002 EU 2007 7 16 CPCP20070051 1 20070511 A 5320 FLOOR SUPPORT AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 260AE 263 RT FLOOR BETWEEN FRAME 36 THRU 38 IS CORRODED. RT FLOOR SUPPORT BETWEEN FRAME 36 THRU 38 REPLACED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007062000125 20070620 00125 NM 2007 6 20 2007UALA01935 1 20070610 A 3260 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT INTERMITTENT A UALA O OTHER N FALSE WARNING CL CLIMB 1 WP 29 306UA 23667 CREW REPORTS A RIGHT MAIN GEAR RED LIGHT IS INTERMITTENT WITH THE GEAR UP. CREW REPORTS AFTER TAKEOFF WITH GEAR HANDLE IN THE UP POSITION, RED RIGHT MLG LIGHT WAS ON STEADY. AFTER HANDLE CYCLED THE RED RIGHT MLG LIGHT FLICKERED. [07-06-0 7] FOUND CONNECTOR D2596 DISCONNECTED AND AN OUT OF LIMIT WIRE ON SWITCH S74. REPLACED SWITCH S74 AND SECURED CONNECTO R D2596. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062000126 20070620 00126 EU 2007 6 20 2007UALA01937 1 20070608 A 2697 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FIRE LOOP OPEN A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 452UA 955 FIRE LOOP-A FAULT DISPLAYED ON UPPER ECAM SCREEN, ENG 2. 08-31-07 OPEN WIRE IN HARNESS, REPAIRED OPEN WIRE. PO ST REPAIR TEST ALL NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072600007 20070726 00007 NM 2007 7 26 F3LA200700178 1 20070719 A 2120 UNKNOWN AIRBUS A319 A319111 3930336 NM CABIN ODOR A F3LA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 03 928FR 2236 AIRCRAFT RT ROWS 9 AND 10 - BURNING WIRE SMELL AT 02 COMPARTMENT IN OVERHEAD BIN. HOT TO TOUCH. INSPECTED LIGHTS, WIRI NG AND PAX OXYGEN GENERATORS FOR ACCIDENTAL DISCHARGE. NO DEFECTS NOTED AT SEAT ROWS 9 AND 10 DEF. REPLACED PASSENGER READING LIGHT POWER UNITS AS A PRECAUTIONARY MEASURE AT ROWS 9 AND 10 DEF IAW AMM 23-73-38, PB 401. OPS CHECKED GOOD. 2 L 7 2 4F RT A28NM 2007062000128 20070620 00128 EU 2007 6 20 2007UALA01941 1 20070609 A 2432 WARNING SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 478UA 1533 ELEC - BATTERY 1 FAULT IN FLIGHT. NO PILOT ACTION REQUIRED. REPLACED BCL1 AND BATTERY NR 1. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062000133 20070620 00133 NM 2007 6 20 2007UALA01947 1 20070610 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 558UA 26654 DOOR 1R MAY NOT BE DISARMED ACCORDING TO F/A'S. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062000134 20070620 00134 NM 2007 6 20 2007UALA01948 1 20070608 A 3350 STRIP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 566UA 26670 EMERGENCY LIGHT STRIP IS OFF THE FLOOR ABOUT TWO INCHES AT 12ABC & 13ABC. [06-22-07] FOUND EEL LIGHT STRIP SLIGHTLY DETACHED (TAPE DEGENERATED) AT ROW 13. REATTACHED. LIGHT STRIP FUNCTION WAS NEVER IMPAIRED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062000136 20070620 00136 NM 2007 6 20 2007UALA01951 1 20070609 A 2421 BRACKET BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LEFT IDG BROKEN A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 644UA 25094 PER FLT CREW - LEFT GENERATOR DRIVE LIGHT ILLUMINATED, IDG DISCONNECTED AND APU POWERING BUSS. SERVICED LT IDG, FOUND SERVICE CONNECTION FITTING BRACKET BROKEN AND DRAIN FITTING POPPET NOT COMPLETELY SEATING. REPLACED POPPET AND WELDED BR ACKET FOR INTERIM REPAIR. DPI NOT POPPED. RESET IDG AND RAN ENGINE AT THE GATE. ALL PARAMETERS NORMAL AND NO LEAKS NO TED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062000137 20070620 00137 NM 2007 6 20 2007UALA01952 1 20070609 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 658UA 27113 RIGHT FWD EEL FLOOR STRIP, EEL FLOOR STRIP BY THE RIGHT MID LAV & IN THE AFT GALLEY SMALL LEFT EEL FLOOR STRIP IS INOPER ATIVE. [07-03-07] SECURED CONNECTOR. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062000139 20070620 00139 NM 2007 6 20 2007UALA01954 1 20070608 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DAMAGED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 EMERGENCY FLOOR LIGHTING IN 1ST CLASS HAS BEEN TORN OFF OF FLOOR BY CATERING. [07-03-07] REPLACED EMERGENCY FLOOR LIGH TING. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062000145 20070620 00145 NM 2007 6 20 2007UALA01960 1 20070611 A 3397 CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN CUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 196UA 28715 EEL CABLE CUT AT G2 GALLEY RIGHT SIDEWALL. [06-22-07] REPLACED EEL STRIP, OP CHECKED OK REF MM. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000152 20070620 00152 NM 2007 6 20 2007UALA01967 1 20070611 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 EXTERIOR EMERGENCY LIGHT, RIGHT 2 ASSY FROM FWD INOP. [06-22-07] REPLAMPED AND NO HELP. REPLACED LIGHT ASSY. GRD CHECK ED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000154 20070620 00154 NM 2007 6 20 2007UALA01969 1 20070612 A 3350 EPSU AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 811UA 847 LEFT EMERGENCY EXIT EPSU 11WL INOPERATIVE AT ROW 11CD. [07-03-07] REMOVED AND REPLACED LH EMERGENCY EXIT EPSU. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062000155 20070620 00155 EU 2007 6 20 2007UALA01970 1 20070612 A 3250 STEERING SYS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG MALFUNCTIONED A UALA O OTHER O OTHER LD LANDING 1 WP 29 452UA 955 CREW HAD HARD FAULT AND LOST NWS ON LANDING ROLL ACCOMPANIED BY GEAR UNSAFE ECAM. REPLACED BSCU AND PERFORMED A FULL T EST OF MCDU AND NO FAULTS NOTED. NO REPEATS SINCE ORIGINAL 2 L 7 2 4F 4 F RT A28NM E40NE 2007062000156 20070620 00156 NM 2007 6 20 2007UALA01971 1 20070612 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE SCRATCHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 CROWN SKIN HAS 5 SCRATCHES BS 266-270, STR 3L. MAJOR REPAIR ACCOMPLISHED: INSTALLED EXTERNAL DOUBLER-TRIPLER & INTERNA L TEAR STRAP DOUBLER REPAIRS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062000158 20070620 00158 NM 2007 6 20 2007UALA01973 1 20070612 A 2622 EXTINGUISHER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 306UA 23667 COCKPIT FIRE EXTINGUISHER BELOW GREEN BAND. REPLACED THE FLIGHT DECK FIRE EXTINGUISHER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062000162 20070620 00162 NM 2007 6 20 2007UALA01977 1 20070612 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR UNDERSERVICED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 DOOR L2 UPPER HINGE CUTOUT IS UNDERSERVICED. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062000164 20070620 00164 NM 2007 6 20 2007UALA01979 1 20070613 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 772UA 26930 FLOOR EMERGENCY LIGHTS BY 11D INOP. [06-26-07] RESET SYSTEM. OPS CHECK OK 2 L 7 2 4F 4 F RT T0001SE E46NE 2007062000165 20070620 00165 NM 2007 6 20 2007UALA01980 1 20070612 A 3397 WIRE HARNESS BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 777UA 26916 EVAC LIGHTS INOP AT 3F & 2F. [06-26-07] REPLACED WIRE HARNESS AT SEAT 2F, OP CHECKS GOOD. RELAMPED AFT LIGHT AT 3F, OP CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007062000168 20070620 00168 NM 2007 6 20 2007UALA01983 1 20070612 A 3350 1619 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 325UA 23957 EEL LIGHT INOPERATIVE RIGHT OVERWING EXIT. REPLACED LAMP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062000170 20070620 00170 NM 2007 6 20 2007UALA01985 1 20070612 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 326UA 23958 ALL FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOP AFT OF ROW 15. [06-22-07] LIFTED AND DRIED AREA OF ALL MOISTURE FROM AFT GALLEY. REPLACED AFT GALLEY EEL STRIP AND AFT 15 FEET OF POWER CABLE. CLEANED, DRIED AND REINSTALLED EEL LAMPS TO NEW PO WER CABLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062000173 20070620 00173 NM 2007 6 20 2007UALA01988 1 20070613 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 EXTERNAL FUSELAGE CROWN SKIN GOUGED AT DORSAL FIN LANDING FROM CONTACT WITH SEAL RETAINER SCREW AT BS 856 LBL 1 TO RBL 1 . MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED SINGLE LAYER EXTERNAL REPAIR DOUBLER & INTERNAL REPAIR STRAPS AT S KIN BONDED DOUBLERS INCLUDING OUTER SURFACE BONDED SHIMS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062000174 20070620 00174 NM 2007 6 20 2007UALA01989 1 20070613 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 RIGHT LOWER FUSELAGE STA 727D TO STA 727D BETWEEN STR, 22R AND 23R SHEAR TIE IS CRACKED OUT OF QUARTER INCH SKIN FASTENE R HOLE. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SHEAR TIE. FABRICATED & INSTALLED NEW SHEAR TIE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062000176 20070620 00176 NM 2007 6 20 2007UALA01991 1 20070613 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 FWD CARGO BAY FRAME AT STA 500 CORRODED STA 499 - 500 LBL 3 TO LBL 3 WL 148-150. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED FRAME SHEAR TIE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007072600008 20070726 00008 NM 2007 7 26 AWXA200700859 1 20070718 A 3350 321431 BATTERY AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 819AW 1395 PHX - EEL - LOG NR 3927277 - PASSENGER EMERGENCY LIGHTS BATTERY FAILED TEST, CENTER LT SIDE. MX REPLACED EMERGENCY LIGH TS BATTERY. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007061900075 20070619 00075 NE 2007 6 19 WRNA200700027 2 20070531 A 7200 CF650E2 ENGINE BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE NR UNSERVICEABLE A WRNA J A DUMP FUEL UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 05 508MC 77660 2188 21644 528348 AFTER TAKEOFF, DURING CLIMB NR 1 ENGINE EXPERIENCED MULTIPLE STALLS. POWER WAS REDUCED, 160,000 POUNDS OF FUEL WERE DUM PED. AIRCRAFT RETURNED TO FIELD AND MADE A SAFE LANDING. ENGINE WAS VISUALLY AND BORESCOPE INSPECTED PER BOEING MM 72- 00-00 PAGE 680Q WITH NO FAULTS FOUND. ON GROUND POWER RUN, ENGINE COMPRESSOR STALLED, ENGINE WAS GIVEN A COMPLETE BORES COPE, TWO 3 INCH CONNECTING CRACKS WITH MISSING MATERIAL WERE FOUND ON THE AIR CLEANER ASSY UTILIZING THE B-3-1 PORT. A IRCRAFT FERRIED TO HKG WHERE THE NR 1 ENGINE WAS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E23EA 2007061900077 20070619 00077 SO 2007 6 19 C2XA07TY029 1 20070612 A 5330 SKIN EMB 145 EMB145EP 3260221 SO FUSELAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15941 145035 DENT ON FUSELAGE SKIN AFT OF PAX DOOR. CUT OUT DAMAGE, FABRICATED FILLER & DOUBLER AND INSTALLED IAW EMB 134/145 SRM 51 -20-03, 51-40-06, 51-40-02, 53-21-01 & CPM 51-21-04, 05, 06. 2 L 7 2 4F RT T00011AT 2007061900080 20070619 00080 SO 2007 6 19 C2XA07CL052 1 20070613 A 3230 852701 PROXIMITY SWITCH EMB 145 EMB145 3260210 SO NLG DEFECTIVE A C2XA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 27 11548 145565 CLE FLIGHT 2705 THE CREW REPORTED LOUD VIBRATION WHEN LANDING GEAR WAS RAISED. CREW AIR RETURNED TO CLE. MAINTENANCE I NSPECTED AND FOUND NOSE LANDING GEAR UPLOCK BOX PROX SWITCH DEFECTIVE. PROX SWITCH WAS REMOVED AND REPLACED. 2 L 7 2 4F RT T00011AT 2007061900081 20070619 00081 NM 2007 6 19 BB07041 1 20070612 A 3397 WIRE BOEING 767 7672B7 1385107 NM CABIN NOT SEATED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 251AY 24764 MAINTENANCE FOUND SEVERAL FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE. RESEATED WIRING AND CONNECTORS ON LIGHTS. NO FURTH ER FAULTS. 2 L 7 2 4F RT A1NM 2007061900179 20070619 00179 NM 2007 6 19 SWAA072950 1 20070612 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900182 20070619 00182 NM 2007 6 19 SWAA072965 1 20070612 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R AND 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900185 20070619 00185 NM 2007 6 19 SWAA072961 1 20070612 A 5311 6546545 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900200 20070619 00200 NM 2007 6 19 SWAA072942 1 20070611 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007061900202 20070619 00202 NM 2007 6 19 SWAA072949 1 20070612 A 3350 OL3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED C3 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 15 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007061900208 20070619 00208 2007 6 19 2007UALA01539 4 20070517 A 3120 26100801 CLOCK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT FAILED A UALA A UNSCHED LANDING O OTHER AP APPROACH 1 WP 29 180UA 25224 FLIGHT DIVERTED DUE TO LIGHTNING STRIKE TO NOSE & WEATHER AT PLANNED DESTINATION. AIRPLANE HAD LIGHTNING STRIKE ON THE NOSE. PERFORMED LIGHTNING STRIKE CHECK PER MM 05-51-13, NO FAULTS FOUND ONLY MINOR PAINT DAMAGE TO EXTERIOR. ALSO, FIR ST OFFICER'S CLOCK FAILED TO RESET & WAS REPLACED. A/C RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007061900214 20070619 00214 2007 6 19 2007UALA01802 4 20070602 A 2565 HARNESS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE TORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 DOOR L2 ESCAPE SLIDE HARNESS AT LATCH YOKE IS TORN, PEELING. [08-07-07] INSTALLED NEW HARNESS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061900224 20070619 00224 NM 2007 6 19 2007UALA01812 1 20070604 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EEL INOP: SEAT 2J AFT SECTION & SEAT 5F FWD SECTION. REPLACED LAMPS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007061900229 20070619 00229 EA 2007 6 19 TRAX200700828 1 20070613 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 973EV 7575 ANGLE CRACKED AT FS 621 CARGO DOOR SURROUND STRUCTURE SUPPORT MEMBER. REFER TO EXELTECH W/O YUL000617 NRTC 200-25 FOR A LL WORK ACCOMPLISHED. SUPPLEMENTAL - SDR CLOSED 06/15/07. 2 L 7 2 4F RT A21EA 2007061900232 20070619 00232 EA 2007 6 19 TRAX200700816 1 20070611 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 917EV 7769 RIGHT WING EXT FWD EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007061900253 20070619 00253 EA 2007 6 19 TRAX200700836 1 20070614 A 5320 INTERCOSTAL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 751EV 10163 FS 280.00 INTERCOSTAL BETWEEN LBL 9 AND RBL 9 CORRODED ON FWD FACE. 2 L 7 2 4F RT A21EA 2007061900260 20070619 00260 NM 2007 6 19 2007UALA01816 1 20070602 A 3350 SIGN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN UNSECURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 224UA 30225 MAIN AISLE EXIT SIGN AT 3L FOUND HANGING BY WIRE HARNESS. [07-06-07] ACCOMPLISHED INTERIM REPAIR OF EXIT SIGN. RECHEC K SECURITY OF INTERIM REPAIR AT EACH NR 3 SVC. MF8689 CREATED TO MONITOR FINAL FIX. SUSPECT SIGN IMPACTED BY LONG PASSE NGER CARRY-ON OBJECT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007061900264 20070619 00264 EA 2007 6 19 SIMA200716907 1 20070615 A 3240 6007300 OVERHEAT SENSOR CNDAIR CL600 CL6002C10 1390015 EA BRAKE FAILED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 504AE 2196 10044 NUMBER THREE BRAKE OVERTEMP INDICATION, ABORTED TAKEOFF. REMOVED AND REPLACED NUMBER THREE BRAKE ASSEMBLY AND BRAKE SEN SOR IAW AMERICAN EAGLE WORKCARD 32-007 AND 32-000. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007061900266 20070619 00266 SO 2007 6 19 SIMA200716909 1 20070616 A 3350 20131A BATTERY PACK EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT FAILED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 716AE 10282 295 145264 RIGHT OVERWING EXIT SIGN INOPERATIVE. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY EXIT SIGN AND ALL FOUR BATTERY PACK S IAW EMB 33-50-13 AND 33-50-14. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007061900267 20070619 00267 SO 2007 6 19 SIMA200716908 1 20070616 A 4920 INLET EMB 145 EMB145LR 3260212 SO APU CONTAMINATED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 620AE 145102 BURNING SMELL IN CABIN WITH APU AND NUMBER ONE ENGINE RUNNING, FOUND BUGS IN APU INLET. CLEANED BUGS FROM APU INLET IAW EMB AMM. OPERATIONAL CHECK GOOD WITH NO SMELL DETECTED, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061900268 20070619 00268 SO 2007 6 19 SIMA200716910 1 20070617 A 2131 2225ONO30201 CONTROLLER EMB 135 EMB135KL 3260302 SO CABIN PRESSURE FAILED A SIMA O OTHER O OTHER CL CLIMB 1 SW 21 832AE 19749 9475 145627 NO CABIN PRESSURIZATION IN CLIMB. REMOVED AND REPLACED DIGITAL PRESSURIZATION CONTROLLER IAW EMB AMM 21-21-00. OPERATI ONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007061900269 20070619 00269 SO 2007 6 19 SIMA200716912 1 20070617 A 2760 14533022409 CONTROL UNIT EMB 145 EMB145LR 3260212 SO SPOILERS FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 667GB 8631 145784 RECEIVED SPOILER FAIL MESSAGE AFTER FLAPS RETRACTED ON CLIMB-OUT, FAIL MESSAGE WENT AWAY AFTER FLAPS 22 SELECTED ON APPR OACH. REMOVED AND REPLACED SPOILER CONTROL UNIT IAW EMB AMM 27-63-02. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SER VICE. 2 L 7 2 4T RT T00011AT 2007061900271 20070619 00271 SO 2007 6 19 SIMA200716911 1 20070617 A 3350 110049 CHARGER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAILED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 651AE 10461 120 145422 LEFT OVERWING AND AFT CABIN EMERGENCY LIGHTS STAYED ILLUMINATED. REMOVED AND REPLACED BATTERY CHARGER IAW EMB AMM. OPE RATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061900272 20070619 00272 SO 2007 6 19 SIMA200716903 1 20070615 A 2750 FLAP SYSTEM EMB 145 EMB145LR 3260212 SO TE FLAPS MALFUNCTIONED A SIMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 21 615AE 145087 SELECTED FLAPS TO 9 DEGREES AND RECEIVED FLAP LOW SPEED AND FLAP FAIL MESSAGE, FLAP INDICATOR REMAINED AT ZERO, CMC SHOW ED FLAP DRIVE SENSOR FAIL MESSAGE. TROUBLESHOT FLAP DRIVE SENSOR FAIL MESSAGE WITH NO DEFECTS. RESET SYSTEM PER EMB FI M TASK 27-51-06-810-805. SYSTEM OPERATIONAL CHECKED GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061900273 20070619 00273 SO 2007 6 19 SIMA200716904 1 20070615 A 2150 8152403 ACM EMB 145 EMB145LR 3260212 SO ZONE 100 SEIZED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 21 620AE 2403 145102 DURING DEBOARDING NOISE HEARD FROM OUTSIDE OF AIRCRAFT FOLLOWED BY A SLIGHT SMOKE SMELL IN CABIN WITH APU AND NUMBER TWO PACK OPERATING, FOUND NUMBER TWO PACK SEIZED. REMOVED AND REPLACED NUMBER TWO PACK IAW EMB AMM 21-51-03. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061900274 20070619 00274 SO 2007 6 19 SIMA200716905 1 20070615 A 2760 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO ZONE 500 FAILED A SIMA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SW 21 669MB 8505 145788 SPEED BRAKE CIRCUIT BREAKER (F-13) FOUND POPPED INFLIGHT, EMERGENCY DECLARED. REMOVED AND REPLACED LEFT HORIZONTAL PROX IMITY SWITCH ON SPEED BRAKE IAW EMB AMM 27-63-04. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007061900276 20070619 00276 EA 2007 6 19 CHQA200700025 1 20070617 A 2611 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A CHQA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 652BR 7429 FLIGHT 3268 - DFW-CLE - IN CRUISE FLIGHT, FLIGHT ATTENDANT CALLED AND SAID THE BACK WAS COLD. TURNED UP THE RIGHT PACK. FLIGHT ATTENDANT CALLED BACK AND SAID IT WAS STILL COLD IN THE BACK; PULLED UP ECS PAGE AND TURNED THE PACK UP AGAIN AN D MONITORED IT. ABOUT 5 MINUTES LATER, RECEIVED SMOKE TOILET INDICATION. THERE WAS NO FIRE OR SMOKE IN THE CABIN BUT S MELL WAS ABOUND. TURNED PACK BACK DOWN TO FULL COLD, RAN QRH, SMELL DISAPPEARED. FLIGHT ATTENDANT PULLED THE SAFETY PI N ON THE HALON BOTTLE AND WENT BACK, BUT THERE WAS NO FIRE AND THE SMELL WAS GONE. MAINTENANCE REMOVED AND REPLACED THE SEAL. 2 L 7 2 4F RT A21EA 2007061900277 20070619 00277 NM 2007 6 19 DHL2004740541 1 20070616 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 990 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AFT CARGO BS 990 BETWEEN STR29R AND 30R AFT SIDE OF FRAME HAS CORROSION. REMOVED FLOOR ANGLE SUPPORT AT AFT BS 950E TO 990 IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA DIMENSION 4 5/8" BY 4" IAW B727 SRM 53-10-4 FIG 15. FABRICATED NEW PART FROM 7075T6 .063" PO NR 9003641 DIMENSION 4 5/8" BY 4" IAW B727 SRM 53-10-4 FIG 15. TREATED AND PRIMED IAW B727 SRM 51 -10-2. INSTALLED NEWSHEAR TIE IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007061900278 20070619 00278 NM 2007 6 19 DHL2007740542 1 20070614 A 5310 651986219 BEAM BOEING 727 7272Q9 138448M NM BS 294-350 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 NOSE SECTION AT WALKWAY BEAM LT MID CHORD SHOWS CORROSION SPOTS BS 294 ALL WAY BACK TO BS 350. REMOVED WALKWAY WEB I/B SIDE LT TRUNNION FITTING, FWD AND AFT TRUNNION STIFFENERS TO GAIN ACCESS IAW B727 SRM 51-30-2. REMOVED CORROSION AT LEF T MID CHORD IAW B727 SRM 51-10-6, ORIGINAL MAT. IS .180" IAW B727 SRM 53-10-2 FIG 1, MATERIAL LOSS IS FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. REMOVED LEFT MID CHORD FITTING IAW B727 SRM 51-30-2, LOCATED AND DRILLED NEW CHORD FITTING P/N 65-19862-19 NSN IAW B727 SRM 51-30-5. INSTALLED NEW LT MID CHORD IAW B727 SRM 51-30-2. REINSTALLED LEFT TR UNNION FITTING, FORWARD AND AFT TRUNNION STIFFENERS AND WALKWAY WEB I/B SIDE IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007061900281 20070619 00281 NM 2007 6 19 QXEA200700965 1 20070615 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM ILLUMINATED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 412QX 4059 LAX FLIGHT NR 2446: AVIONICS CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE CYCLED AIRCRAFT POWER. OPS CHECK NORMAL WITH NO DEFECTS NOTED. NO PARTS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007061900283 20070619 00283 NM 2007 6 19 DHL2007783516 1 20070531 A 7160 NOSE COWL BOEING 727 727227 1384078 NM NR 1 NACELLE OUT OF TOLERANCE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 NR 1 ENGINE NOSE COWL AT 11 O`CLOCK POSITION, 2 BLIND FASTENERS IMPROPERLY INSTALLED, NAC STA 81.5. REMOVED 2 BLIND FAS TENERS ON NR 1 NOSE COWL AT 11 O`CLOCK POSITION IAW B727 SRM 51-30-2. FASTENERS HOLES OUT OF LIMITS AND OVER SIZE IAW B 727 SRM 51-30-2. REMOVED, EXISTING DOUBLER AND FILLER IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA 3.5 BY 4.5 IAW B727 S RM 54-30-03, FIG 3A. FABRICATED DOUBLER FROM 2024T3, .040 BY 7 BY 1.5 BY 2.75 AND FILLER FROM 2024T3, .032 BY 3.48 BY 4 .40 IAW B727 SRM 54-30-03, FIG 3A. TREATED, PRIMED AND INSTALLED REPAIR IAW SRM 51-30-2 AND 54-30-3. 2 L 7 3 4F A3WE 2007061900284 20070619 00284 EU 2007 6 19 TRBA200733 1 20070614 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT FAILED A TRBA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 29 369AT 369 EMERGENCY LIGHTS CAME ON DURING TAXI. WILL NOT RESET. UNABLE TO EXTINGUISH LIGHTS. REMOVED AND REPLACED BATTERY PACK AT PWR SUPPLY FIN NR 61WL IAW JIC NR 33-51-21. OP CK OK. 2 H 7 2 4T RT A53EU 2007061900285 20070619 00285 EU 2007 6 19 TRBA2007037 1 20070617 A 3350 7012210 BULB AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHT FAILED A TRBA K NONE L NO TEST NR NOT REPORTED 1 SO 29 529AM 529 EMERGENCY EXIT LIGHT ON PAX DOOR STAIR IS INOPERATIVE. REMOVED AND REPLACED LIGHT BULB IAW JIC NR 33-51-24. OP CK OK. 2 H 7 2 4T RT A53EU 2007061900287 20070619 00287 EU 2007 6 19 TRBA200734 1 20070614 A 3397 WIRE AEROSP ATR72 ATR72212 8680945 EU COCKPIT LIGHTS CHAFED A TRBA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 29 399AT 399 CAPT DOME AND STORM LIGHT WHEN OUT; BURNING SMELL IN COCKPIT ALONG WITH SPARKS APPARENTLY FROM INSTRUMENT PANEL. DE-PLA NED PASSENGERS. REMOVED AND REPLACED CAPT'S DOME LIGHT BULB. PERFORMED DVI OF WIRING BEHIND INSTRUMENTS PANEL. NO ABN ORMAL CONDITION OR SMELL NOTED. AT THIS TIME REPAIRED WIRE ON CAPT YOKE CHART HOLDER IAW STD PRACTICES JIC NR 20-27-17. WIRES WERE CHAFING POPPING-OUT C/B. PERFORMED OP CK OK AS PER MM NR 33-10-00. 2 H 7 2 4T RT A53EU 2007061900289 20070619 00289 NM 2007 6 19 DHL2007742003 1 20070614 A 5753 SKIN BOEING 727 727225 1384077 NM TE FLAP DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 WHILE AT FLIGHTSTAR AIRCRAFT SERVICES FOR AN A CHECK, RT O/B FLAP, AFT FLAP LOWER AREA HAS 2 DENTS. REMOVED DAMAGED ARE A APPROX 3.2" BY 4" CLEANED AND PREPPED AREA TO ALODINED, FABRICATED FILLER 3.2 BY 4 AND DOUBLER 6.2" BY 5.5 FROM .016" 2024-T3 PO NR 92003189. ALODINED AND PRIMED IAW B727 SRM 51-40-20 PAR 7/8 FIG 3 AND 57-50-2 FIG4. INSTALLED REPAIR PAR TS, CURED AND FINISHED REPAIR AREA IAW B727 SRM 51-40-20 PAR 20, 22 AND 51-40-24 FIG 1. 2 L 7 3 4F A3WE 2007061900290 20070619 00290 NM 2007 6 19 DHL2007740543 1 20070609 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 450 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 FRAME BETWEEN STR 28R THRU STR 28L BS 450 CORRODED. REMOVED ACCESS DOOR FRAME BS 440 STR 28R-28L IAW B727 SRM 51-30-2, FABRICATED NEW FRAME, MAT USED 7075-0 PO NR 9004219, DIMENSION 5" BY 24" SRM 53-10-2 FIG 3 AND 51-20-1 FIG 7. HEAT TREA TMENT 7075-O TO 7075T6 IAW FORM NR FAS 0115 REV TR2. TREATED AND PRIMED SRM 51-10-2. INSTALLED NEW FRAME IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007061900291 20070619 00291 NM 2007 6 19 2007UALA01829 1 20070605 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 EEL AT 2A AFT, 5E FWD & 43 ABC ARE INOPERATIVE. RELAMPED LIGHTS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007061900294 20070619 00294 NM 2007 6 19 2007UALA01831 1 20070605 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 CABIN BS 616 FRAME INBOARD CHORD IS CRACKED, WL 202, RBL 64. MAJOR REPAIR ACCOMPLISHED: MANUFACTURED & INSTALLED REPAI R ANGLE & FILLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007061900295 20070619 00295 NM 2007 6 19 DHL2007783515 1 20070605 A 5534 7075T6 ANGLE BOEING 727 727227 1384078 NM VERTICAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 CRACK AT UPPER SUPPORT ANGLE INSIDE VERT STAB LT PANEL 9701, FIN STA 239.1, WL 472.6. REMOVED STAB PANELS 9701 AND 9707 TO FOM IAW B727 SRM 51-30-2. REMOVED, FABRICATED NEW ANGLE INSIDE VERT STAB PANEL 9701 FROM 7075T6, .050, 3.25 BY 6 IA W B727 SRM 51-30-2, FIG 3 AND 51-40-3. TREATED, PRIMED AND INSTALLED REPAIR AND FITTING, INTERCOSTAL IAW B727 SRM 51-10 -2 AND 53-30-2. 2 L 7 3 4F A3WE 2007061900296 20070619 00296 NM 2007 6 19 DHL2007783508 1 20070607 A 5320 INTERCOSTAL BOEING 727 727227 1384078 NM BS 1150-1166 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 FOUND CORROSION AT INTERCOSTAL BETWEEN STA 1150 TO 1166, JUST ABOVE STR 27R. REMOVED INTERCOSTAL BETWEEN STA 1150 TO 11 66, JUST ABOVE STR 27R IAW B727 SRM 51-30-2. FOUND CORROSION TO BE OUT OF LIMITS IAW B727 SRM 53-10-1, FIG 1. FABRICAT ED NEW INTERCOSTAL FROM .032”, 7075-T6, DIM 19 BY 5. TREATED, PRIMED AND INSTALLED INTERCOSTAL BETWEEN STA 1150 TO 1166, STR 27R IAW B727 SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 2007061900298 20070619 00298 EA 2007 6 19 MDGA200700001 2 20070505 A 7200 ENGINE BEECH 90 C90 1152913 CE PWA PT6 PT6A6 52043 EA RIGHT UNKNOWN E MDGA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION NR NOT REPORTED 1 SO 09 977AA LJ555 PCE21894 INFLIGHT SHUT DOWN OF RIGHT ENGINE. TIME SINCE OH WAS 1210.00 HOURS. 1 L 7 2 3T 3 T 3A20 E4EA 2007061900299 20070619 00299 NM 2007 6 19 DL757070718 1 20070613 A 5330 146N37504 SKIN BOEING 757 757232 1384965 NM FS 1690 S15R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 640DL 23994 DURING CURRENT HMV AT TIMCO LCQ, TWO DENTS WERE NOTED ON THE FUSELAGE SKIN BETWEEN BODY STATION 1681.8 AND 1701, BETWEEN S-14R AND S-16R. THE SUBJECT DAMAGE WAS BEYOND THE ALLOWABLE DAMAGE LIMITS OF THE SRM. EACH OF THE DAMAGED AREAS WAS TRIMMED OUT, AND A BOEING APPROVED REPAIR INSTALLED PER 461665-14. 2 L 7 2 4F RT A2NM 2007061900302 20070619 00302 NM 2007 6 19 DL76S070720 1 20070613 A 5347 SEAT TRACK BOEING 767 767332 1382001 NM BS 999 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 CABIN, STA 999 RBL54.75 SEAT TRACK FOUND CRACKED. REPAIRED ON NR 51787. REPAIRED PER 53-00-51 FIGURE 201 REPAIR 3. 2 L 7 2 4F RT A1NM 2007061900303 20070619 00303 NM 2007 6 19 DL76S070721 1 20070613 A 5320 AND101342009 ANGLE BOEING 767 767332 1382001 NM BS 999 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 CABIN STA 999 RBL 32 SUPPORT CRACKED. REPAIRED PER 53-00-51 FIGURE 201 ON NR 51788. 2 L 7 2 4F RT A1NM 2007061900305 20070619 00305 NM 2007 6 19 DL757070723 1 20070613 A 5230 SKIN 146N6603261 BOEING 757 757232 1384965 NM C2 DOOR GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 672DL 00433 25977 MAJOR REPAIR INSTALLED ON C2 CARGO DOOR STA 1407 STOP BEAM 4. REPAIR REF SRM 52-30-01 FIG 201. 2 L 7 2 4F RT A2NM 2007061900306 20070619 00306 NM 2007 6 19 DL757070724 1 20070613 A 5230 SKIN 146N6603261 BOEING 757 757232 1384965 NM C2 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 672DL 00433 25977 MAJOR REPAIR LOCATED AT STA 1428 BETWEEN STOP BEAMS 5 AND 6 ON C2 CARGO DOOR. 2 L 7 2 4F RT A2NM 2007061900307 20070619 00307 NM 2007 6 19 DL757070725 1 20070612 A 5210 SKIN 146N6603261 BOEING 757 757232 1384965 NM C2 DOOR GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 672DL 00433 25977 MAJOR REPAIR LOCATED STA 1384 AT STOP BEAM 3 OF CARGO DOOR. 2 L 7 2 4F RT A2NM 2007061900308 20070619 00308 NM 2007 6 19 DL764070726 1 20070614 A 5330 1338110039 PANEL BOEING 767 767432ER 1385134 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 829MH 29700 MAIN EQUIPMENT CENTER P33 STANDOFF MOUNT ATTACH POINT SKIN CRACKED (UPPER RT) MISSED ITEM ON OP 24335. REMOVED P33 IQW DELTA ERA 41526-14. REPLACED AFT SKIN PNL IAW DELTA ERA 461526-14. INSTALLED P33 IAW ERA 461526-14. PERFORMED GOOD FU NCTIONAL TEST IAW DELAT ERA 461526-14, ATTACHED RFTS #S 9 17 18 ERA 461526-14 ATTACHED JPD# 12 PG 6. 2 L 7 2 4F RT A1NM 2007061900309 20070619 00309 NM 2007 6 19 DL76G070727 1 20070614 A 3350 CHARGER BOEING 767 7673P6 1385105 NM EMERGENCY LIGHTS INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 156DL 25354 ALL AFT UPPER EMERGENCY LIGHTS INOP. REPLACED AFT BATTERY CHARGER LIGHTS CK GOOD. 2 L 7 2 4F RT A1NM 2007061900310 20070619 00310 NE 2007 6 19 DL76L070728 2 20070614 A 7532 80217010 BLEED VALVE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 197DN 28454 727620 AFTER ENG START NR 2 ENG RT ENG BLEED LIGHT REMAINED ILLUM WITH EICAS MSG. NO DUCT PRESSURE. RAN POWER UP-RECYCLED SWITC HES-SHUTDOWN AND RESTARTED ENGINE. NO HELP. REPLACED RT PRV AND PRV CONTROLLER. OPS GOOD ON ENGINE RUN. 2 L 7 2 4F 4 F RT A1NM E24NE 2007061900311 20070619 00311 2007 6 19 DL76L070730 4 20070614 A 3460 4058650930 CDU BOEING 767 767332 1382001 NM COCKPIT FAILED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 175DN 24803 RT FMC CDU WENT BLANK PRIOR TO TAKEOFF. RESET A COUPLE OF TIMES AND DID NOT FIX. REPLACED RT CDU. OPS NORMAL. 2 L 7 2 4F RT A1NM 2007061900313 20070619 00313 NM 2007 6 19 QXEA200700956 1 20070608 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - DENT WITH GOUGE ON RIGHT FUSELAGE AT STATION 4.8 BELOW STRINGER 29R. REPAIRED IAW SRM 53-20-31, 51-21-10, 51-2 5-10. 2 H 7 2 4T RT A13NM 2007061900314 20070619 00314 NM 2007 6 19 QXEA200700957 1 20070608 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - AREA OF CORROSION ON RIGHT FUSELAGE SKIN AT STATION 16.3 BELOW STRINGER 29R. REPAIRED IAW SRM 53-20-31, 51-21- 10, 51-25-10. 2 H 7 2 4T RT A13NM 2007061900321 20070619 00321 NM 2007 6 19 2007UALA01841 1 20070605 A 3350 CHARGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 504UA 24625 NR 2 LEFT MED EMERGENCY LIGHT SIGN INOPERATIVE. [06-22-07] REPLACED CHARGER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062000050 20070620 00050 NM 2007 6 20 2007UALA01859 1 20070606 A 3040 ANTI-ICE SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU WINDSHIELD INOPERATIVE A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 349UA 24253 FLIGHT DIVERTED DUE TO WINDSHIELD HEAT INOPERATIVE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062000052 20070620 00052 EU 2007 6 20 2007UALA01861 1 20070606 A 3350 321431 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 492UA 1755 EMERGENCY EXIT LIGHTS FAIL 3SVC TEST. REPLACED EMERGENCY LIGHT BATTERY PACK RIGHT AT OVERWING EXIT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062000057 20070620 00057 NM 2007 6 20 2007UALA01866 1 20070607 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY LIGHT INOP AT 34ABC & DOOR 3 CROSSAISLE. [06-22-07] RESECURED POWER CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000058 20070620 00058 NM 2007 6 20 2007UALA01867 1 20070607 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 CEILING EMERGENCY LIGHTS INOP AT ROW 26R, AFT CREW REST AREA, ROW 46L & DOOR 3R. [06-22-07] RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000061 20070620 00061 NM 2007 6 20 2007UALA01870 1 20070606 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 533UA 25073 EMERGENCY LIGHT STRIP INOPERATIVE IN FRONT OF AFT LAV. [06-22-07] REPLACED EMERG LIGHT STRIP OPS CK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062000071 20070620 00071 SO 2007 6 20 FDKA200705211 1 20070517 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN DISCONNECTED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FDM 6122 MCO-PFN (0342 PHX LCL) - EMERGENCY LIGHTS INOP AT EXIT ROW 12. MX RECONNECTED THE ELECTRICAL CONNECTOR, OPS CH ECK NORMAL. 2 L 7 2 4T RT T00011AT 2007062000075 20070620 00075 SO 2007 6 20 FDKA200706262 1 20070606 A 3350 SIGN EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 847MJ 145517 FDM 6210 JFK-PWM (0529 PHX LCL) - 12BC EMERGENCY DOOR LOCATOR SIGN INOP. MX RESET SYSTEM OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2007062000077 20070620 00077 NM 2007 6 20 DHL2007740528 1 20070517 A 5312 BULKHEAD BOEING 727 7272Q9 138448M NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 WHILE IN "C" CHECK, RT PRESSURE BULKHEAD WEB PRESENTS 3" CRACK AT BS 1180 RBL54 WL208. REMOVED CRACKED WEB IAW B727 SRM 51-30-2. FABRICATED NEW WEB FROM 2024T3 .026 .025 PO NR 9004384 DIM 16 1/2"BY 6" IAW B727 SRM 53-10-2 FIG 5 51-20-1. TREATED AND PRIMED NEW WEB IAW B727 SRM 51-10-2 AND INSTALLED NEW WEB AT RT BS 1180 BULKHEAD RBL 54 WL 208 IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007062000078 20070620 00078 NM 2007 6 20 DHL2007740530 1 20070522 A 5311 FRAME BOEING 727 7272Q9 138448M NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 WHILE IN "C", FWD CARGO COMPT STA 600 +4" REINFORCEMENT FRAME IS DENTED ABOVE STR 24L. TRIMMED OUT DAMAGED (DIM.3" BY 1 .25") IAW B727 SRM 51-10-1. FABRICATED REPAIR CHANNEL FROM 7075-0 .090 PO NR 7185240 (DIM 23" BY 5") IAW B727 SRM 53-10 -4 FIG 1. HEAT TREATED CHANNEL TO 7075T6 IAW FAS ENGINEERING REPORT NR 2-37153-801 REV 1. TREATED AND PRIMED REPAIR CH ANNEL IAW B727 SRM 51-10-2 C/W HFEC IAW B727 NDTM PT6 51-00-00 FIG 23. NO CRACKS NOTED. ENLARGED TRIMMED AREA BY .040 IAW B727 51-10-1. INSTALLED REPAIR CHANNEL IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007062000083 20070620 00083 NM 2007 6 20 07FDEA02124 1 20070613 A 5343 ACA7017501 FITTING DOUG MD11 MD11F 3023600 NM NLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 NOSE LANDING GEAR LT TRUNNION FITTING FOUND CRACKED APPROX 1.5" IN LENGTH. [06-29-07] NOSE LANDING GEAR LT TRUNNION FI TTING REPAIR CARRIED OUT AS PER SRM 53-40-00 FIG. 23 VOL.I. AND FEDEX E.A. 1-5310-109899 PART 1. REPAIR CLASSIFIED AS M AJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062000089 20070620 00089 CE 2007 6 20 BSAASDR0718 1 20070607 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE RT MLG MALFUNCTIONED A BSAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 05 139ZV UE139 THE LANDING GEAR CIRCUIT BREAKER TRIPPED WHEN CREW SELECTED GEAR DOWN DURING APPROACH. GEAR WAS EXTENDED MANUALLY AND C REW LANDED WITHOUT INCIDENT. AFTER EXTENSIVE TROUBLESHOOTING, THE RIGHT MAIN LANDING GEAR ACTUATOR WAS CHANGED DUE TO A SUSPECTED FAULT IN THE ACTUATOR'S INTERNAL GEAR DOWN MICROSWITCH. MULTIPLE GEAR SWINGS WERE PERFORMED WITH NO DEFECTS NOTED. AN OPERATIONAL CHECK FLIGHT WAS COMPLETED WITH NO DEFECTS NOTED. 2 L 7 2 4T RT A24CE 2007062000095 20070620 00095 NM 2007 6 20 CALA0700303 1 20070613 A 5553 65538344 FITTING BOEING 737 7373T0 1384582 NM VERTICAL STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12313 23364 INSPECTION FOUND VERTICAL STABILIZER LEFT AFT I/B ATTACH LUG FORWARD FAILSAFE FITTING CORRODED ON FORWARD SIDE, STA 1088 -1104. THE FAILSAFE FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007062000098 20070620 00098 WP 2007 6 20 G6OA200700001 1 20070611 A 2612 FIRE WARNING DOUG DC10 DC1030F 3023504 WP COCKPIT ACTIVATED A G6OA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION CR CRUISE 1 EA 27 606GC 47929 NR 2 ENGINE FIRE INDICATION AT FL280 WITH LOOP-B SELECTED. ENGINE SHUTDOWN AND AGENT DISCHARGED. 2 L 7 3 4F RT A22WE 2007062000104 20070620 00104 NM 2007 6 20 UPS07549958 1 20070608 A 5330 SKIN BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 444UP 27389 INSPECTION TYPE:3C A/C SKIN DENTED BS 1697, 2 INCHES ABOVE STR 13L. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER IAW ER 07-2580. 2 L 7 2 4F RT A2NM 2007062000121 20070620 00121 NM 2007 6 20 2007UALA01929 1 20070611 A 5420 BUSHING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT STRUT MIGRATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 RIGHT STRUT, DIAGONAL BRACE ATTACH FITTING, INBOARD BUSHING MIGRATED. [08-08-07] REPLACED BUSHINGS PER MM 54-53-90, REPAIR 4. AIRCRAFT OK FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062000129 20070620 00129 NM 2007 6 20 2007UALA01943 1 20070610 A 3397 58781 CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 301UA 23642 AFT SECTION CABIN EMERGENCY EEL LIGHTS INOPERATIVE. REPLACED AFT EEL CABLE SECTION. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062000130 20070620 00130 NM 2007 6 20 2007UALA01944 1 20070609 A 3397 FEEDER CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 308UA 23669 AFT SECTION OF EEL FLOOR STRIP INOPERATIVE. [06-22-07] REPLACED FEEDER CABLE, CK OK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062000131 20070620 00131 NM 2007 6 20 2007UALA01945 1 20070609 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 523UA 24932 EMERGENCY ESCAPE PATH LIGHT (FLOOR) 1EA LIGHT INOP AT SEAT 34. REPLACED LAMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062000132 20070620 00132 NM 2007 6 20 2007UALA01946 1 20070609 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 523UA 24932 LEFT OVERWING ESCAPE HATCH EXTERIOR AFT LIGHT INOP. [06-22-07] RELAMPED OPERATES NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062000138 20070620 00138 NM 2007 6 20 2007UALA01953 1 20070609 A 3350 1317 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 658UA 27113 AFT LEFT EXTERIOR EEL LIGHT IS INOPERATIVE. RELAMPED AND LIGHT CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062000141 20070620 00141 NM 2007 6 20 2007UALA01956 1 20070609 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 DOOR 5 RIGHT SILL EMERGENCY LIGHT IS INOP. [06-22-07] RELAMPED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000142 20070620 00142 NM 2007 6 20 2007UALA01957 1 20070609 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 AFT GALLEY LOWER SIDE WALL FLOOR EEL STRIP IS INOP. [06-22-07] RELAMPED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000144 20070620 00144 NM 2007 6 20 2007UALA01959 1 20070611 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 SEATS 4B & 4E AFT EEL ARE INOPERATIVE. [06-22-07] RELAMPED & REPLACED CONNECTOR. OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000153 20070620 00153 NM 2007 6 20 2007UALA01968 1 20070611 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY LIGHTS WILL TURN OFF. [06-22-07] REPLACED BROKEN SW GUARD AT DOOR 1L. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000163 20070620 00163 NM 2007 6 20 2007UALA01978 1 20070612 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INTERMITTENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 672UA 30027 FLOOR EMERGENCY LIGHTING ON LT SIDE OF AC FROM WING TO 1ST CLASS ARE COMING ON & OFF. [07-13-07] OPS CHECKED OK PER M M-PER 33-51-00. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062000167 20070620 00167 NM 2007 6 20 2007UALA01982 1 20070612 A 3510 OXYGEN MASK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT LEAKING A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 336UA 24240 F/O OXYGEN MASK HAS LEAK IN HEAD STRAP. REPLACED MASK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062000181 20070620 00181 NM 2007 6 20 2007UALA02000 1 20070614 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 LEFT OVERWING EMERGENCY LIGHT INOP AFT ASSY FWD BULB. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062200010 20070622 00010 NM 2007 6 22 2007UALA01997 1 20070613 A 5210 LEVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR OUT OF ADJUST A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 R-1 MED MODE SELECTOR NEEDS ADJUSTMENT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062200013 20070622 00013 2007 6 22 2007UALA02005 4 20070614 A 2565 CABLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR DISCONNECTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 493UA 1821 SLIDE NR 1L HAS CENTER RELEASE CABLE, AT LOWER GIRT CENTER AREA UNATTACHED. CENTER RELEASE CABLE REATTACHED, INSPECTED . 2 L 7 2 4F 4 F RT A28NM E40NE 2007062200014 20070622 00014 SO 2007 6 22 RAIA00706013 1 20070609 A 5610 SD12026136004 SEAL EMB 145 EMB145LR 3260212 SO WINDOW LEAKING A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 817HK 145058 FLT NR 5507 - STL - AFTER TAKEOFF AIRCRAFT WOULD NOT PRESSURIZE F/O WINDOW LEAKS MASSIVELY UNABLE TO PRESSURIZE. MAINTE NANCE REPLACED F/O'S DV WINDOW SEAL CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007062200015 20070622 00015 SO 2007 6 22 RAIA00706008 1 20070606 A 3350 RPS1B BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 818HK 145059 PRE FLT NR 5574 - PHL - EMERGENCY LIGHT COCKPIT FLOOD LIGHT AND AISLE FLOOD LIGHT IS INOP. MAINTENANCE REMOVED AND REPL ACED NR 1 EMERGENCY BATTERY, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007062200016 20070622 00016 SO 2007 6 22 RAIA00706009 1 20070607 A 3242 39807 CONTROL VALVE EMB 145 EMB145LR 3260212 SO BRAKE SYSTEM FAULTY A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 810HK 145231 FLT NR 8022 - IAD - BRAKE OUTBOARD INOP MESSAGE ON TAKEOFF ROLL. MAINTENANCE REMOVED AND REPLACED BRAKE CONTROL VALVE F UNCTIONAL CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT T00011AT 2007062200017 20070622 00017 SO 2007 6 22 RAIA00706011 1 20070608 A 3250 STEERING SYS EMB 145 EMB145ER 3260211 SO NLG OUT OF ADJUST A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 808HK 145157 FLT NR 8044 - RIC - STEERING PULLING HARD RIGHT. MAINTENANCE ADJUSTED STEERING SYSTEM, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007062200018 20070622 00018 SO 2007 6 22 RAIA00706010 1 20070608 A 2760 CONTROL UNIT EMB 145 EMB145 3260210 SO SPOILER SYS MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 803HK 145077 FLT NR 3573 - RDU - SPOILER FAIL MESSAGE. MAINTENANCE REMOVED AND REINSTALLED SAME SPOILER CONTROL UNIT. OPS CHECK GO OD AT THIS TIME. 2 L 7 2 4F RT T00011AT 2007062200020 20070622 00020 SO 2007 6 22 RAIA00706016 1 20070610 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT SMOKE A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 837HK 145255 FLT NR 7934 - SYR - SMOKE IN CABIN AND COCKPIT. MAINTENANCE RAN & OPS CHECKED ENGINES & PACKS, NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2007062200022 20070622 00022 SO 2007 6 22 RAIA00706015 1 20070610 A 3350 RPS1B BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 816HK 145055 PRE FLT NR 5526 - ATL - ALL EMERGENCY LIGHTS INOP EXCEPT FOR FWD 3 FLOOR STRIPS. MAINTENANCE REMOVED AND REPLACED EMERG ENCY LIGHT BATTERIES. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007062200024 20070622 00024 NM 2007 6 22 SWAA072977 1 20070613 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 232WN 32500 EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007062200026 20070622 00026 2007 6 22 SWAA072978 4 20070613 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 457WN 33856 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007062200028 20070622 00028 NM 2007 6 22 SWAA072980 1 20070613 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 490, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007062200029 20070622 00029 NM 2007 6 22 SWAA072988 1 20070614 A 5330 6545768 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING DUCT CUTOUT BS 380, BETWEEN LBL 2.8 AND BL 0. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007062200032 20070622 00032 NM 2007 6 22 SWAA072996 1 20070614 A 5210 6545871 SKIN BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR SKIN CRACKED AT UPPER FWD CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007062200033 20070622 00033 NM 2007 6 22 SWAA072995 1 20070614 A 5210 6545871 SKIN BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR SKIN CRACKED AT LOWER AFT CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007062200038 20070622 00038 NM 2007 6 22 SWAA073003 1 20070614 A 5310 6547980 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 907 AND BS 927, STR 17L. REMOVED AND REPLACED CR EASE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2007062200039 20070622 00039 NM 2007 6 22 SWAA072989 1 20070614 A 2750 65522112 TORQUE TUBE BOEING 737 7373H4 1384600 NM T/E FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, FOUND RIGHT WING INBOARD FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TU BE PER MM. 2 L 7 2 4F RT A16WE 2007062200041 20070622 00041 NM 2007 6 22 SWAA072990 1 20070614 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007062200043 20070622 00043 NM 2007 6 22 SWAA073006 1 20070614 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007062200045 20070622 00045 NM 2007 6 22 SWAA072986 1 20070614 A 5523 6959227 BUSHING BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED BRDG CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BUSHING PER MM. 2 L 7 2 4F RT A16WE 2007062200046 20070622 00046 NM 2007 6 22 SWAA072984 1 20070613 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 259WN 35554 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007062200047 20070622 00047 NM 2007 6 22 SWAA073004 1 20070614 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 27L CORRODED AT BS 950. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007062200048 20070622 00048 NM 2007 6 22 SWAA072985 1 20070613 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 14Y CHECK, FOUND STRINGER 16R CRACKED AT BS 492. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007062200049 20070622 00049 NM 2007 6 22 SWAA072999 1 20070614 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 729SW 27861 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, BETWEEN RBL 7.5 AND LBL 12. REPAIRED FLOORBEAM PER SWA E A. 2 L 7 2 4F RT A16WE 2007062200050 20070622 00050 2007 6 22 SWAA072975 4 20070613 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007062200061 20070622 00061 2007 6 22 SWAA072976 4 20070613 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007062200065 20070622 00065 EU 2007 6 22 TRBA200731 1 20070612 A 2133 2096H010800 OUTFLOW VALVE AEROSP ATR72 ATR72212A 8680902 EU CABIN PRESSURE FAILED A TRBA K NONE P NO WARNING INDICATION DE DESCENT 1 SO 29 545AT 545 DURING DESCENT A/C LOST PRESSURIZATION, ALT ON PRESS GAUGE WENT FROM 0 TO CURRENT ALTITUDE. RATE WENT FROM -500FT (NORM AL) TO THE RATE AT WHICH DESCENDING. DIFF WENT TO 0. HUMMING NOISE HEARD FROM BEHIND COCKPIT. NO ALERT OR CAUTION IND ICATING A PROBLEM. REMOVED AND REPLACED PNEUMATIC OUTFLOW VALVE IAW JIC NR 21-31-22. REMOVED AND REPLACED MANUAL PRESS CONTROLLER IAW JIC NR 21-32-82. PERFORMED FUT CK ON GND IAW JIC NR 21-31-00. OP CK OK. 2 H 7 2 4T RT A53EU 2007062200066 20070622 00066 NM 2007 6 22 AWXA200700723 1 20070605 A 5320 140N250532 FITTING BOEING 757 757225 1384959 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 MCN - MAJOR REPAIR - CRACKED CABIN FLOOR WEB CLIP AT FWD CARGO COMPARTMENT, BS 660 - BS 680, BL 0, WL 208.1. REPLACED C ABIN FLOOR WEB CLIP AT FWD CARGO COMPARTMENT, BS 660 - BS 680, BL 0, WL 208.1 IAW B757-200 SRM 51-40-02-0G FIG 3, 8, PAR A 8 AND 51-40-05-0G FIG 2. 2 L 7 2 4F RT A2NM 2007062200068 20070622 00068 NM 2007 6 22 QXEA200700954 1 20070609 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - SEAT TRACK NR 5 AT STATION X80, X80 TO X94 HAS MINOR SCRATCHES AND CHAFES. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007062200070 20070622 00070 NM 2007 6 22 QXEA200700958 1 20070607 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - CHAFE AND GOUGED AREA 1" BY 5" AFT OF LAV SERVICE DOOR ON AIRFRAME SKIN. REPAIRED IAW RD8/4-53-347 AND SRM 51- 25-15. 2 H 7 2 4T RT A13NM 2007062200071 20070622 00071 NM 2007 6 22 QXEA200700959 1 20070608 A 5320 CHANNEL BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - RIGHT AFT SERVICE DOOR UNDERLINING EDGE CHANNEL IS CORRODED AND SEVERAL NUT PLATES HAVE DRILLED OUT SCREW SHANK S. REPAIRED IAW SRM 51-21-10, 51-25-10. 2 H 7 2 4T RT A13NM 2007062200074 20070622 00074 NM 2007 6 22 QXEA200700962 1 20070612 A 5741 BARREL NUT BOMBDR DHC8 DHC8402 1390042 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - RIGHT WING TO FUSELAGE FORWARD MOUNT VERTICAL TIE BOLTS HAVE CRACKED BARREL NUTS. REPAIRED IAW RD8/4-51-102. 2 H 7 2 4T RT A13NM 2007062200075 20070622 00075 NM 2007 6 22 DLM88070693 1 20070605 A 5320 FASTENER DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 RUSTED HI-LOCK AT STA Y=351, LONGERON 4 RT. FASTENER REPLACED IAW SRM 51-30-5 NR T0056459. 2 L 7 2 4F RT A6WE 2007062200086 20070622 00086 NE 2007 6 22 DL76L070705 2 20070609 A 7321 70R270 BEARING BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE FAILED A DALA K NONE G MULTIPLE FAILURE CR CRUISE 1 SO 27 196DN 28453 727738 N2 ENGINE INOP, AUTO-THROTTLES INOP-FADEC C1 MSG. FOUND N2 STATOR /ROTOR BEARING FAILED. FOUND EEC ALTERNATOR ROTOR/ST ATOR WORN AND EEC ALTERNATOR DR GEARSHAFT AFT BEARING DAMAGED. REPLACED EEC ALTERNATOR DRIVE GEARSHAFT AND BEARING ASSE MBLY AND ROTOR AND STATOR AS PER 72-61-14 AND 73-21-05. ACCOMPLISHED ENG RUN AT IDLE AUTHORITY PER TOPP 40-20-15 AND MCC NO FAULTS. NO MSGS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062200088 20070622 00088 NM 2007 6 22 DL76S070708 1 20070611 A 5315 BAC1505100703 FLOORBEAM BOEING 767 767332 1382001 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 CABIN BS287, RBL 60-62 FLOORBEAM UPPER CORD CORRODED AS MARKED, REPAIRED PER 53-00-51D, FIG 201 ON AJN50915. 2 L 7 2 4F RT A1NM 2007062200089 20070622 00089 NM 2007 6 22 DL76G070712 1 20070611 A 4920 380029812 APU BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE LEAKING A DALA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 1612T 11752 P2631 30575 P2631 SMOKE REPORTED COMING FROM APU. FOUND EXCESSIVE OIL IN TAIL PIPE REMOVED AND REPLACED APU PER AJIC 7952. APU OPS NML N O LEAKS NOTED AIR AND GEN OPS OK. 2 L 7 2 4F 4 F RT A1NM E13NE 2007062200090 20070622 00090 2007 6 22 DL76L070713 4 20070611 A 3416 341080108 ALTIMETER BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE COCKPIT FAILED A DALA J DUMP FUEL O OTHER CR CRUISE 1 SO 27 191DN 28448 P2631 CAPT ALT INOP FAILED AT 13,000'. REMOVED AND REPLACED CAPT'S ALT INDICATOR PER MM 34-13-01-004-001. TEST OK PER MM. T EST ON ADC 1 AND 2 ALSO OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062200091 20070622 00091 NM 2007 6 22 DLM8K070714 1 20070611 A 3397 CONNECTOR DOUG MD88 MD88 3023688 NM CABIN LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DE 49997 SECURED LOOSE EMERGENCY LIGHT HARNESS PLUG AT SEAT 31DE AND 23DE, OPS CHK GOOD. 2 L 7 2 4F RT A6WE 2007062200092 20070622 00092 NM 2007 6 22 DL76L070715 1 20070611 A 3320 S527 SWITCH BOEING 767 767332 1382001 NM CABIN BROKEN A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 184DN 27111 CREW REPORTS CABIN OVERHEAD LIGHTS FLICKERING ON AND OFF THROUGH ENTIRE CABIN. PULLED C/BS ON P-33 PANEL TO STOP FLASHI NG RETURNED TO JFK FOR REPAIRS AFTER ISOLATED PROX BOX FAULTS CARD 06. REPLACED PSEU. OPS OK. FND SW S 527 P19 BROKEN . INSPECTED RT GEN FEEDER. ALL OK. INSPECTED WIRE ABOVE L1 DOOR PER BOEING . CKS OK. REPLACED PRESS SW S 527. TAXI A/C. UNABLE TO DUPLICATE ITEM. 2 L 7 2 4F RT A1NM 2007062200093 20070622 00093 NM 2007 6 22 DL777070717 1 20070612 A 2121 49100945A FAN BOEING 777 777232 1385232 NM CABIN MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 866DA 29738 BURNING RUBBER SMELL IN FWD CABIN AREA FOLLOWED APPROX 30 SECONDS LATER WITH A RECIRC FAN STATUS MESSAGE. CHECKED MX IN FO DISPLAY AND SHOWED FWD UPPER RECIRC FAN OFF. SMELL CLEARED IN LESS THAN ONE MINUTE. ATL MX ASKED THAT THE UPPER REC IRC SWITCH TO BE TURNED OFF. NO FURTHER INDICATIONS. REPLACED FAN CKS GOOD. REINSTALLED CEILING PANELS, REMOVED MCO P LAC P/N 4100945A. 2 L 7 2 4F RT T00001SE 2007061900186 20070619 00186 NM 2007 6 19 SWAA072951 1 20070612 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900188 20070619 00188 NM 2007 6 19 SWAA072967 1 20070612 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R AND 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007061900196 20070619 00196 NM 2007 6 19 SWAA072974 1 20070612 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007061900197 20070619 00197 NM 2007 6 19 SWAA072939 1 20070611 A 3350 65C34691 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 434WN 32454 DURING SCHEDULED HC1 CHECK, FOUND LEFT FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007061900201 20070619 00201 NM 2007 6 19 SWAA072941 1 20070611 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007061900226 20070619 00226 EU 2007 6 19 2007UALA01814 1 20070602 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 416UA 479 SEAT 19C EEL LIGHT HAS 1 OF 2 LAMPS INOPERATIVE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061900233 20070619 00233 EU 2007 6 19 TRAX200700817 1 20070611 A 2560 FLASHLIGHT AEROSP ATR72 ATR72 EU COCKPIT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 641AS 387 CAPTAIN'S FLASHLIGHT IS INOP. 2 H 7 2 4T RT 2007061900235 20070619 00235 EA 2007 6 19 TRAX200700820 1 20070613 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 861AS 7445 SECOND LAST CEILING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007061900242 20070619 00242 EA 2007 6 19 TRAX200700830 1 20070613 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 834AS 7254 F/O`S FLASHLIGHT WILL NOT TURN ON. 2 L 7 2 4F RT A21EA 2007061900247 20070619 00247 EA 2007 6 19 TRAX200700832 1 20070613 A 5210 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 F/A REPORTS, PAX DOOR IS HARD TO OPEN. 2 L 7 2 4F RT A21EA 2007061900265 20070619 00265 EU 2007 6 19 2007UALA01820 1 20070602 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 416UA 479 SEAT 11C EEL LIGHT RED HAS 1 OF 2 LAMPS INOPERATIVE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061900275 20070619 00275 2007 6 19 2007UALA01822 4 20070604 A 2565 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 562UA 0611 26664 LOW BOTTLE PRESSURE. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061900312 20070619 00312 EU 2007 6 19 2007UALA01835 1 20070605 A 2560 FLASHLIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 464UA 1290 EMERGENCY FLASHLIGHT INOP AT DOOR 1L. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061900320 20070619 00320 NM 2007 6 19 2007UALA01840 1 20070606 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EEL INOP: ROWS 35 & 46 ABC. [06-22-07] SECURED CONNECTOR. OPS CKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000037 20070620 00037 NM 2007 6 20 2007UALA01846 1 20070606 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 WALL EEL INOP BETWEEN MID LAVS. [06-22-07] SECURED CONNECTOR. OPS. CKS. NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000053 20070620 00053 NM 2007 6 20 2007UALA01862 1 20070606 A 5241 CAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU GALLEY DOOR WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 FWD GALLEY DOOR CUTOUT AFT BOTTOM GUIDE PLATE HAS WEAR MARK. MAJOR REPAIR REMOVED AND REPLACED LATCH CAM FITTING WITH N EW. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062000056 20070620 00056 NM 2007 6 20 2007UALA01865 1 20070607 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY LIGHT INOPERATIVE AT 17AB LOWER. [06-22-07] RESEATED PWR CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000073 20070620 00073 SO 2007 6 20 FDKA200705223 1 20070523 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN DISCONNECTED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6098 ATL-AVL (1133 PHX LCL) - EMERGENCY OVERHEAD LIGHTS INOP AT EXIT ROW 12. MX RECONNECTED THE ELECTRICAL CONNECTO R, OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007062000085 20070620 00085 EU 2007 6 20 07FDEA02126 1 20070614 A 5415 40CDV12 FITTING AIRBUS 300 A300B4605R 3930308 EU NR 2 PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 PYLON NR 2 FWD ENGINE FITTING, CORROSION ON TENSILE BOLT HOLES REPAIR PERFORMED BY REMOVAL OF CORROSION THRU OVERSIZING AND BUSH INSTALLATION IAW EA 6-5442-106473 AND RAS/052121/005/2007 ISS. A. 2 L 7 2 4F RT A35EU 2007062000087 20070620 00087 NM 2007 6 20 07FDEA02128 1 20070614 A 5347 ADA83891 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 MAIN DECK COMPARTMENT SEAT TRACK AT BS 969 LT X=47.5 FOUND CROWN WORN. [06-29-07] MAIN DECK COMPARTMENT SEAT TRACK AT STA 969 LT X=47.5" REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL I. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GM M 6-2-100. 2 L 7 3 4F RT A22WE 2007062000088 20070620 00088 NM 2007 6 20 07FDEA02129 1 20070614 A 5347 ADA83901 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 MAIN DECK COMPARTMENT SEAT TRACK AT STA 939 RT X= -27.5" FOUND CROWN WORN. [06-29-07] REPAIR CARRIED OUT AS PER SRM 53 -70-00 FIG.1 VOL I. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062000090 20070620 00090 CE 2007 6 20 BSAASDR0719 1 20070602 A 3610 1560283000 TUBE BEECH 1900 1900D 1154162 CE RT WING SPLIT A BSAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 05 131YV UE131 DURING CLIMB TO ALTITUDE, THE RT BLEED AIR FAIL ANNUNCIATOR LIGHT CAME ON AT 16,800FT. CREW FOLLOWED CHECKLIST PROCEDUR ES, SHUT OFF BLEED ON RIGHT SIDE AND RETURNED TO STATION, LIGHT WENT OUT AT 7,000FT DURING RETURN TO STATION. INITIALLY DEFERRED THE RT BLEED SYSTEM IAW THE MEL. TROUBLESHOOTING FOUND A NEW SPLIT IN THE EVA TUBING IN RT WING AREA BY PANEL 611. SYSTEM OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 2007062000092 20070620 00092 CE 2007 6 20 BSAASDR0721 1 20070607 A 3297 WIRE BEECH 1900 1900D 1154162 CE LANDING GEAR CHAFED A BSAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 05 139ZV UE139 WHEN CREW SELECTED GEAR DOWN, THE LANDING GEAR CONTROL CB IMMEDIATELY TRIPPED. CREW EXTENDED GEAR AND LANDED WITH NO FU RTHER INCIDENT. A CHAFED WIRE FOR THE GEAR DOWN MICROSWITCH WAS FOUND UNDER THE CABIN FLOOR BENEATH SEAT 4A. THE WIRE W AS GROUNDING ON A DEICE LINE. THE CHAFED SECTION WAS REMOVED, WIRE WAS RESECURED & CHAFE PROTECTED. 2 L 7 2 4T RT A24CE 2007062000094 20070620 00094 NM 2007 6 20 KCSA071191 1 20070614 A 5730 RIVET BOEING 747 747123 1384873 NM RT WING PULLED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 RIVETS PULLING THROUGH SKIN AFT OF AFT SPAR TOPSIDE OF WING AT WS-411. 2 L 7 4 4F A20WE 2007062000097 20070620 00097 NM 2007 6 20 CALA0700305 1 20070614 A 5315 6546810 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70352 23590 INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AT STA 967, RBL 28. THE FLOORBEAM WAS REPAIRED IAW SRM 53-30-51, REPAIR 2. 2 L 7 2 4F RT A16WE 2007062000099 20070620 00099 NM 2007 6 20 MWEA070149 1 20070614 A 2611 8930112B00H114 SMOKE DETECTOR BOEING 717 717200 1383700 NM CARGO BAY FAILED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 921ME 55183 CARGO SMOKE DETECTOR 2A FAILED SELF TEST. REMOVED AND REPLACED CARGO SMOKE DETECTOR 2A. 2 L 7 2 4F TR A6WE 2007062000102 20070620 00102 SO 2007 6 20 C2XA07IA140 1 20070614 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO CARGO BAY MALFUNCTIONED A C2XA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SW 27 34111 14612 14612 145659 IAH - FLIGHT 2556, DURING TAKEOFF THE CREW REPORTED A BAGGAGE SMOKE WARNING. THE FIRE EXTINGUISHERS WERE DISCHARGED AS A PRECAUTION, AND THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE NR 2 CARGO SMOKE DETECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVE D FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007062000119 20070620 00119 EU 2007 6 20 2007UALA01927 1 20070611 A 5210 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 434UA 592 DOOR 1L HAS DENT ON LOWER SKIN. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED AREA. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062000120 20070620 00120 NM 2007 6 20 2007UALA01928 1 20070611 A 5313 STRINGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 199UA 28717 STR 45R CRACKED 3 - 4FT LONG STA 640 ON I/B LOWER FLANGE. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED U-CHANNEL REPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000123 20070620 00123 NM 2007 6 20 2007UALA01931 1 20070611 A 5420 BUSHING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT PYLON MIGRATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 RIGHT PYLON STRUT OUTBOARD MIDSPAR FITTING, OUTBOARDD LUG BUSHING MIGRATED. [08-08-07] REMOVED AND REPLACED BUSHIN GS PER SRM 54-53-90, REPAIR 3. MID-SPAR FITTING OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062000124 20070620 00124 NM 2007 6 20 2007UALA01932 1 20070611 A 5420 BUSHING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT PYLON MIGRATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 LEFT PYLON INBOARD MIDSPAR FITTING, INBOARD LUG BUSHING MIGRATED. [08-08-07] REMOVED AND REPLACED BUSHINGS PER SRM 5 4-53-90, REPAIR 3. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062000140 20070620 00140 NM 2007 6 20 2007UALA01955 1 20070609 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 SEATS 23AB, 39HJK & 59ABC EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY LAMPS. ALL CHECK NORMAL. [06-22-07] REPLACED EMERGENCY LAMPS. ALL CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000146 20070620 00146 NM 2007 6 20 2007UALA01961 1 20070609 A 2810 SEAL BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RT WING LEAKING A UALA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 29 199UA 28717 PRIOR TO DEPARTURE FUEL SEEP EVIDENT ON RIGHT WING BETWEEN T/E FLAP CANOE FAIRINGS 7 & 8, NR 4 MAIN FUEL TANK. TANK ACC ESS PANEL 2ND OUTBOARD FROM STICK 21 LOCATION. [07-31-07] REMOVED PANEL AND REPLACED SEALS. NO FURTHER LEAKS NOTED AT THIS TIME. SUSPECT VIBRATION LOOSENED FASTENERS COMBINED WITH SEAL DETERIORATION CAUSED LEAK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000150 20070620 00150 NM 2007 6 20 2007UALA01965 1 20070611 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 EMERGENCY LIGHT 5F AND 4F AND RIGHT EEL GALLEY INOP. [06-22-07] FOUND UNPLUGGED. PLUGGED IN. CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000159 20070620 00159 NM 2007 6 20 2007UALA01974 1 20070612 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 199UA 28717 FUSELAGE SKIN DAMAGED AT STA 636 TO STA 651 AT STR 45R. MAJOR REPAIR ACCOMPLISHED: MFG'D & INSTALLED DOUBLER & FILLERS . 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000160 20070620 00160 NM 2007 6 20 2007UALA01975 1 20070612 A 3350 767 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 537UA 25157 LEFT WING EMERGENCY EXIT LIGHT INOP. REPLACED LAMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062000161 20070620 00161 NM 2007 6 20 2007UALA01976 1 20070612 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 571UA 26681 F/A REPORTS STRONG RUBBER BURN ODOR BY DOOR 3R. [07-03-07] FOUND BAD BALLAST FOR AFT GALLEY CEILING LIGHT, DISCONNEC TED CONNECTOR AND TIED BACK. BALLAST M10808. FOUND NO OTHER PROBABLE SOURCE IN AREA. PACKS OPERATING NORMAL WITH NO HIST ORY OF ODORS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062000169 20070620 00169 NM 2007 6 20 2007UALA01984 1 20070612 A 3350 58674 INVERTER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 325UA 23957 EEL LIGHTS FAILED. FIRST CLASS FLOOR PROXIMITY LIGHTS ARE INOP. INVERTER M1503 BAD. SWAPPED IN INVERTER M1580 TO CONF IRM. REPLACED INVERTER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062000172 20070620 00172 EU 2007 6 20 2007UALA01987 1 20070613 A 3222 SEAL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 432UA 587 NLG STRUT IS COMPLETELY FLAT AND OIL IS LEAKING FROM STRUT. 08-31-07 FAULTY DYNAMIC SEALS, REPLACED DYNAMIC SEALS W ITHIN THE NLG. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062000177 20070620 00177 NM 2007 6 20 2007UALA01992 1 20070613 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 331UA 24192 AFT GALLEY AND LAST 10 ROWS OF CABIN EEL LIGHTS INOP. [06-22-07] FOUND 1 EEL STRIP SHORTING OUT WHOLE ROW. REPLACED TH E DEFECTIVE STRIP AND EEL CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062000178 20070620 00178 NM 2007 6 20 2007UALA01993 1 20070613 A 3397 58781362624 CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 340UA 24244 EEL LIGHTS ARE INOP FROM ROW 15 AFT. REPLACED AFT EEL CABLE ASSY & AFT LAMP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062000179 20070620 00179 NM 2007 6 20 2007UALA01994 1 20070614 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 565UA 26669 LEFT OVERWING EXTERNAL AFT EMERGENCY LIGHT INOP. [06-22-07] REPLACED LAMP. OPS CK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062000180 20070620 00180 NM 2007 6 20 2007UALA01999 1 20070614 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EEL 2J AFT, 43ABC & 58ABC ARE INOPERATIVE. REPLACED LAMPS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000183 20070620 00183 NE 2007 6 20 2007UALA02002 2 20070613 A 7230 COMPRESSOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2 ENGINE STALLED A UALA C ABORTED TAKEOFF R A PARTIAL RPM/PWR LOSS FLAME/FIRE TO TAKEOFF 1 WP 29 107UA 26900 ABORTED TAKEOFF DUE TO NR 2 ENGINE COMPRESSOR STALL. [08-08-07] ACFT NR 3 ENG FERRIED TO SFO FOR ENGINE CHANGE. EN GINE REPLACED AT SFO ON 06/15/07. SHOP TEARDOWN FOUND ONE 6TH STAGE VSV VANE ARM BROKEN OFF AT THE "CLAW" TO THE ARM RA DIUS AT THE 6:00 POSITION. THE ADJACENT ARM WAS CRACKED 50% ACROSS. THE DISCONNECTED VANE RESULTED IN A VIBRATORY SOUR CE THAT EXCITED, AND INDUCED A FATIGUE FRACTURE IN, ONE 7TH STAGE BLADE AT ITS ROOT ATTACHMENT. THIS BLADE LIBERATED, R ESULTING IN HEAVY LEADING AND TRAILING EDGE DAMAGE TO THE 7TH THROUGH 15TH STAGE BLADE AIRFOILS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062200012 20070622 00012 2007 6 22 2007UALA02004 4 20070613 A 2565 GAUGE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 433UA 589 DOOR 2L SLIDE PRESSURE READING LOW. [06-22-07] BAD GAUGE GREEN TEMP BAR INOPERATIVE, ALSO HAD A SMALL LEAK AROUND GAU GE THREADS. REPLACED GAUGE, RETIGHTENED WITH THREAD TAPE, REFILLED AND WATER TESTED FOR 15 MIN, NO LEAK FOUND. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062200019 20070622 00019 SO 2007 6 22 RAIA00706012 1 20070608 A 3250 8146R5KL25SL POTENTIOMETER EMB 145 EMB145ER 3260211 SO STEERING SYS ENGAGED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 808HK 145157 FLT NR 8017 - RIC - WHEN TILLER IS ENGAGED, AIRCRAFT PULL HARD RIGHT. MAINTENANCE REMOVED AND REPLACED LOAD POTENTIOMET ER, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007062200021 20070622 00021 SO 2007 6 22 RAIA00706014 1 20070609 A 3397 WIRE EMB 145 EMB145 3260210 SO CABIN BROKEN A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 806HK 145112 POST FLT NR 3564 - RIC - EMERGENCY LIGHT AFT SIDE AFT CEILING EXIT LOCATOR INTERMITTENT AND FLICKERS ON AND OFF. MAINTE NANCE INSPECTED AND FOUND BROKEN WIRE ON LIGHT STRIP, REPAIRED WIRE, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007062200025 20070622 00025 NM 2007 6 22 SWAA072991 1 20070614 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 454WN 29851 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER MISSING AT ROW 23 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007062200034 20070622 00034 NM 2007 6 22 SWAA073002 1 20070614 A 5322 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 927, STR 27R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007062200040 20070622 00040 NM 2007 6 22 SWAA072993 1 20070614 A 5330 65737466 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 906, STR 6R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007062200069 20070622 00069 NM 2007 6 22 QXEA200700955 1 20070612 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - DENT ON LEFT UPPER FUSELAGE AFT OF ICE SHIELD AND DOUBLER REPAIR AT STATION 301 AND Z176. REPAIRED IAW SRM 53- 30-31 AND RD8/4-53-272. 2 H 7 2 4T RT A13NM 2007062200072 20070622 00072 NM 2007 6 22 QXEA200700961 1 20070611 A 5753 SKIN BOMBDR DHC8 DHC8402 1390042 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - LEFT OUTBOARD FLAP UPPER SURFACE IS CHAFED AT STATION YW193.00. REPAIRED IAW SRM 51-25-05 AND 51-14-00. 2 H 7 2 4T RT A13NM 2007062200094 20070622 00094 EU 2007 6 22 07FDEA01892 1 20070521 A 5730 A57710013 SKIN AIRBUS 310 A310222 3930315 EU LT WING MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON LT WING UPPER SURFACE, INBD OF SPOILER 3 WS 737 RIB 12. REPAIR REQUIRES EVALUATION FO R MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW OVERSIZE FASTENERS WERE INSTALLED ON EXISTING HOLES IN ACCORDANCE WITH SRM 51-40-23. 2 L 7 2 4F RT A35EU 2007062200096 20070622 00096 WP 2007 6 22 07FDEA02134 1 20070615 A 5312 DOUBLER DOUG DC10 DC1010 3022110 WP BULKHEAD CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 CAC COMPT CRACK .50" ON DOUBLER OF BULKHEAD AT STA 1156 LONG 40 LT ACCOMPLISHED EA NR 8-5330-108092. 2 L 7 3 4F A22WE 2007062200097 20070622 00097 WP 2007 6 22 07FDEA02135 1 20070615 A 5710 STRUCTURE DOUG DC10 DC1010 3022110 WP LT WING LEAKING A FDEA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 25 387FE 46621 HEAVY LEAK ON LT WING REAR SPAR AREA AT M22 DOUBLERS REMOVE CLIP TO GAIN ACCESS AND RESEAL AREA IAW SRM 51-33-01 VOL II AND MM 28-11-01-2. 2 L 7 3 4F A22WE 2007062200099 20070622 00099 WP 2007 6 22 07FDEA02137 1 20070615 A 5522 SKIN DOUG DC10 DC1010 3022110 WP RT ELEVATOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 RT O/B ELEVATOR FOUND DENT 1.25" BY 1.25 INCH DEEP 0.82" ON UPPER SKIN AT STA XE 280. REPAIR SKIN IAW SRM 55-10-00 VOL1 FIG 8. 2 L 7 3 4F A22WE 2007062200100 20070622 00100 WP 2007 6 22 07FDEA02138 1 20070615 A 5712 RIB DOUG DC10 DC1010 3022110 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 LT WING STATION XORS 346 STRINGERS 42-43 AND 43-44 LWR RIB CHORD CRACKED IN TWO PLACES IN THE VERTICAL LEG REPAIRED IAW SRM 57-20-00 FIG 27 SHEET 3 VOL 1. 2 L 7 3 4F A22WE 2007062200102 20070622 00102 WP 2007 6 22 07FDEA02140 1 20070615 A 5330 DOUBLER DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 EXISTING SKIN REPAIR AT STA 322 X=-7 EXTERNAL SKIN REPAIRED IAW SRM 53-20-00 FIG 6. 2 L 7 3 4F A22WE 2007062200104 20070622 00104 EU 2007 6 22 07FDEA02142 1 20070528 A 5730 A57970362 SKIN AIRBUS 310 A310222 3930315 EU LT WING WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 LT WING, AILERON ACTUATORS ACCESS PANEL AREA LOWER SKIN WITH BURROWS WITHOUT MARGINAL DISTANCE. IT WAS REPAIRED IN AC CORDANCE WITH FEDEX EA 6-570-106714. 2 L 7 2 4F RT A35EU 2007062200107 20070622 00107 EU 2007 6 22 AWXA200700725 1 20070613 A 5347 D53472176200 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 637AW 099 SAL - CORROSION ON CABIN SEAT RAIL, FR 54+16", FR 56+6", AND FR 57+17", +Y1292. REPAIRED CABIN SEAT RAIL, FR 54+16", FR 56+6", AND FR 57+17", +Y1292 IAW A320 SRM 53-00-15 PAGE 201-206 AND 51-21-11 PAGE 1-7. 2 L 7 2 4F RT A28NM 2007062200109 20070622 00109 GL 2007 6 22 2393 1 20070615 A 2430 14605010 CONTROL UNIT CIRRUS MCU120 CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO HARTZL HCJ3Y PHCJ3YF1 GL NR 2 ALTERNATOR FAILED E J4PA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 13 695CD 02332 1372 688086 FP3486B AT APPROXIMATELY 1300 LOCAL AND DURING CLIMB-OUT FROM KGSP GOING TO KSAV THE ALT 2 WARNING LIGHT CAME ON AND SHOW A BATT ERY DISCHARGE. ACTION TAKEN WAS TO DIVERT TO KGMU FOR TROUBLESHOOT AND REPAIR. 1 PASSENGER ON BOARD AND LANDED WITHOUT INCIDENT. FOUND THE NR 2 ALT FIELD CONTROL UNIT IN THE MCU 120 TO BE READING HIGH RESISTANCE. 1 L 7 1 3O 3 O NT A00009CH E3SO 5 C P36EA 2007062200110 20070622 00110 EU 2007 6 22 TRBA200735 1 20070613 A 3350 7012210 LIGHT AEROSP ATR72 ATR72212A 8680902 EU CABIN STAIRS INTERMITTENT A TRBA K NONE O OTHER NR NOT REPORTED 1 SO 29 536AT 536 THE EMERGENCY EXIT LIGHT ON THE MAIN CABIN STAIRS IS INTERMITTENT. REMOVED AND REPLACED LIGHT BULB IAW MM NR 33-50-00. OP CK OK. 2 H 7 2 4T RT A53EU 2007062200113 20070622 00113 NM 2007 6 22 HALA0700250 1 20070613 A 5414 SKIN BOEING 717 717200 1383700 NM LT PYLON CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 ON NR 1 ENGINE CHANGE, LT PYLON APRON UPPER AFT LATCH CUTOUT IS CRACKED. REPAIRED CRACK PER HAL M105 B10192. 2 L 7 2 4F TR A6WE 2007062200115 20070622 00115 NE 2007 6 22 HALA0700253 2 20070611 A 7261 OIL SYSTEM BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE ENGINE LOW A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 598HA 23278 ETOPS SIGNIFICANT SYSTEM, BTB OIL QUANTITY AT PUSH 18, AT START WENT TO 13-14 NEVER WENT TO REQUIRED 19 FOR DISPATCH. I NSPECTED FOR LEAKS, NONE SERVICED ENG 1 PINT MM 12-22-01. ENG OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E13NE 2007062200119 20070622 00119 NM 2007 6 22 AWXA200700730 1 20070609 A 2560 MEGAPHONE BOEING 757 7572S7 1384962 NM CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 902AW 23322 PHX - EE - CREW REPORTED AFT EMERGENCY MEGAPHONE INOP. MX REPLACED THE MEGAPHONE. 2 L 7 2 4F RT A2NM 2007062200135 20070622 00135 NM 2007 6 22 AWXA200700731 1 20070613 A 3260 UPLOCK SENSOR BOEING 737 7373S3 1384711 NM RT MLG FAILED A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 313AW 23712 PHX - PVR - EL - CREW REPORTED AFTER T/O, GEAR HANDLE RAISED UP. ALL GEAR LIGHTS EXTINGUISHED EXCEPT RIGHT GEAR LIGHT. RT GEAR RED LT REMAINED ILLUMINATE. ACCOMPLISHED GEAR LIGHT DISAGREEMENT CHECKLIST GOT 3 GREEN, NO RED LIGHTS. CREW D ECLARED AN EMERGENCY AND RETURNED TO PHX. THE LANDING WAS UNEVENTFUL. THE CREW TAXIED TO THE GATE. MX REPLACED UPLOCK SENSOR S74 IAW M/M 32-61-21-4 AND CK'D SENSOR CLEARANCE PER 32-61-21-5. (.189 INCH). MX PERFORMED L/GEAR POSITION INDI CATING AND WARNING SYSTEM TEST IAW 32-61-00-5. OPS CHECK WAS GOOD. THE A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007062200136 20070622 00136 NM 2007 6 22 DHL2007740533 1 20070616 A 5320 69133833 FITTING BOEING 727 7272Q9 138448M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 WHILE AT FLIGHTSTAR FOR A C CHECK REF N/R 053715, AFT CARGO BS 1166 STR30 AFT END DOUBLER PRIMER IS DETERIORATED. REMOV ED BS1183 STR30 FITTING IAW B727 51-30-2 FAB STRINGER REPAIR FROM 7075 T6 .090 PO3717808 BAC1498147 AND BAC1458-131 7075 -T6 PO NR 9004539 APPROX DIM 20" BY 3" FILLER AND 12" BY 3" DOUBLER AND LOCATED HOLES IAW B727 SRM 53-10-3 FIG1 AND 51-3 0-5. FITTING P/N 69-13383-3 PO NR 7212335 TREATED AND PRIMED AREA PARTS IAW B727 SRM 51-10-2. INSTALLED FITTING AT BS 1183 STR30 IAW B727 SRM 51-30-2. INSTALLED STRINGER REPAIR AT BS 1166 STR30 IAW B727 SRM 53-10-3 FIG 1 AND 51-30-2. IN STALLED FASTENERS AND ANGLE AT BS 1166 STR 30 IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007062200138 20070622 00138 NM 2007 6 22 DHL2007740535 1 20070616 A 5315 FLOORBEAM BOEING 727 7272Q9 138448M NM FUSELAGE MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 740DH 21930 C CHECK REF N/R 053923, PREVIOUS RE-WORK/ BLEND-OUT ON FLOORBEAM AND INTERCOSTAL AT BS 300 TO 312 RBL 45 WL200 THAT APPE ARS TO BE UNFINISHED AND NOT A STANDARD SRM REPAIR. REMOVED FASTENERS FOR ACCESS IAW B727 SRM 51-30-2. CUT-OUT DAMAGED FLOORBEAM LWR CHORD DIM 18" LENGTH FABRICATED REPAIR ANGLES FROM BAC1490-2773 .071 2EA DIM 12" BY 1" AND 9" BY 1" PO NR 7212328. FABRICATED FILLER FROM BAC1506-1080 PO NR 7212177 DIM 18" LENGTH IAW B727 SRM 53-10-8 FIG 9 AND 53-10-2 FIG 7 . FABRICATED FLOOR STAB REPAIR STRAP FROM 7075-T6 .040 PO NR 9004670 DIM 14" BY 2" IAW B727 SRM 53-10-8 FIG 6. TREATED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2 AND INSTALLED REPAIR PARTS AT FLOORBEAM BS 300 TO 312 RBL 45 WL200 IAW B72 2 L 7 3 4F RT A3WE 2007062200140 20070622 00140 NM 2007 6 22 DHL2007740537 1 20070617 A 5320 STRUCTURE BOEING 727 7272Q9 138448M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 DURING C CHECK, RT BS 306 RBL6.0 BILGE AREA WALKWAY NEARBY HORIZ BEAM CHORD PRESENTS CORROSION. REMOVED FASTENERS IN AR EA TO GAIN ACCESS IAW B727 SRM 51-30-2 CUT-OUT DAMAGED AREA DIMENSION 1" BY .500 AND FABRICATED REPAIR DOUBLER FROM 7075 -O .050 PO NR 9004219 DIM 4" BY 1" IAW B727 SRM 53-10-4 FIG 11 AND 53-10-2 FIG 1. HEAT TREATED REPAIR DOUBLER TO 7075-T 6 IAW FAS ENGINEERING REPORT NR 2-37153-801 REVISION A TREATED AND PRIMED REPAIR DOUBLER IAW B727 SRM 51-10-2AND INSTALL ED REPAIR DOUBLER AT RT BS 306 RBL 16 IAW B727 SRM 53-10-4 FIG 11 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007062200142 20070622 00142 NM 2007 6 22 DHL2007740539 1 20070617 A 5320 SUPPORT BEAM BOEING 727 7272Q9 138448M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 C CHECK N/R 053950, HORIZ MIDCHORD SUPPORT BEAM CORRODED AT BS 312 LT. REMOVED HORIZONTAL BEAM SUPPORT BEAM IAW B727 SR M 51-30-2. DUE TO CORROSION BEING OUT OF LIMITS, IAW B727 SRM 53-10-1 FIG 1, FABRICATED NEW SUPPORT BEAM FROM AND10137-3 001 7075-T6 PO NR 7212319 DIM 29.2 LENGTH IAW B727 SRM 53-10-2 FIG 2 AND BOEING DWG 65-18915 AND B727 SRM 51-20-1. TREA TED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED NEW SUPPORT BEAM AT BS 312 L/H IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007062200143 20070622 00143 NM 2007 6 22 DHL2007740540 1 20070617 A 5320 SUPPORT ANGLE BOEING 727 7272Q9 138448M NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 C CHECK N/R053897, NOSE SECTION WALKWAY BEAM AREA BS 294 LT WEB SUPPORT ANGLE CORRODED AND CRACKED. REMOVED ANGLE FOR A CCESS IAW B727 SRM 51-30-2. REMOVED WED SUPPORT ANGLE IAW B727 SRM 51-30-2. FABRICATED NEW WEB SUPPORT ANGLE FROM AND1 0133-2004 PO NR 42144 DIM 26 1/2" BY 1 1/2" BY 1" IAW B727 SRM 53-10-2 FIG 1 AND 51-20-1 TREATED AND PRIMED NEW ANGLE IA W B727 SRM 51-10-2. INSTALLED NEW ANGLE AT NOSE SECTION WALKWAY BEAM BS 294 LT WEB IAW B727 SRM 51-30-2 AND REINSTALLED PREVIOUSLY REMOVED ANGLE IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007062200144 20070622 00144 NM 2007 6 22 0607200701 1 20070607 A 3610 BACC10BN588LR DUCT CLAMP BOEING 727 7272F9 138407D NM NR 1 ENGINE LOOSE A PCSA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 29 199AJ 21426 FLIGHT 845 DEPARTED MIA AND CLIMBED TO CRUISE ALTITUDE, THE CREW REPORTED THE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED, THE AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT FURTHER INCIDENT. IN MIA MAINTENANCE FOUND A LOOSE CLAMP AT THE NR 1 ENGIN E BLEED VALVE, THE CLAMP WAS RETORQUED IAW B-727 MM CH 20-80-01, THE NR 1 ENGINE WAS RUN-UP TO TAKEOFF POWER AND A LEAK CHECK WAS PERFORMED, ENGINE RUN NORMAL LEAK CHECK GOOD IAW B-727 MM CH 71-00-00, THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F RT A3WE 2007062200146 20070622 00146 NE 2007 6 22 PCSA2062007SU 2 20070206 A 7230 COMPRESSOR BOEING 727 7272F9 138407D NM PWA JT8 JT8D* NE NR 1 ENGINE DAMAGED A PCSA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SO 29 199AJ 21426 696663 FLIGHT 713 ABORTED THE TAKEOFF AFTER THE FLIGHT CREW EXPERIENCED A VIBRATION COMING FROM THE NR 1 ENGINE, THE AIRCRAFT R ETURNED TO THE GATE WITHOUT ANY FURTHER INCIDENT. MAINTENANCE INSPECTED THE ENGINES AND FOUND THE NR 1 ENGINE SHOWING E VIDENCE OF DAMAGE TO THE SECOND STAGE COMPRESSOR SECTION, FURTHER INSPECTIONS ARE IN PROGRESS. THE NR 1 ENGINE VISUAL I NSPECTION NOTED LOW COMPRESSOR BLADE DAMAGE THROUGHOUT THE ENGINE POSSIBLY FROM FOD, THE NR 1 ENGINE HAS BEEN REMOVED AN D REPLACED WITH ANOTHER SERVICEABLE ENGINE. 2 L 7 3 4F 4 F RT A3WE E2EA 2007062200147 20070622 00147 SO 2007 6 22 RAIA00706018 1 20070611 A 3240 38793500 SHUTOFF VALVE EMB 145 EMB145LR 3260212 SO BRAKE SYSTEM MALFUNCTIONED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 817HK 21685 145058 FLT NR 5568 - PHL - BRAKE INBOARD INOP. MAINTENANCE REMOVED AND REPLACED INBOARD BRAKE SHUTOFF VALVE, OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT T00011AT 2007062200148 20070622 00148 SO 2007 6 22 RAIA00706017 1 20070611 A 3240 BRAKE EMB 145 EMB145 3260210 SO MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 807HK 145119 FLT NR 5568 - PHL - BRAKE INBOARD INOP. MAINTENANCE RECYCLED C/B, PERFORMED OPS CHECK OF BRAKE SYSTEM, SYSTEM OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007062200150 20070622 00150 NM 2007 6 22 HNAA0700113 1 20070614 A 2920 8290010281 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM HYDRAULIC SYSTEM LEAKING A HNAA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 07 980HA 376 THE NUMBER 1 FUEL TEMP WAS DROPPING FOLLOWED BY THE ILLUMINATION OF THE NR 1 HYD ISO VALVE CAUTION LIGHT. THE HYD QTY W ENT TO .5 QT. THE NUMBER 1 FUEL PRESSURE CAUTION LIGHT ILLUMINATED BUT THE FUEL FLOW WAS NORMAL. THE CREW TURNED ON TH E AUX PUMP AND THE NR 1 FUEL PRESSURE CAUTION LIGHT WENT OUT. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT I NCIDENT. HYD FLUID WAS LEAKING FROM THE RIGHT SIDE. 2 H 7 2 4T RT A13NM 2007062200151 20070622 00151 EU 2007 6 22 BA07005 1 20070526 A 5330 SKIN AIRBUS 330 A330323 3930335 EU FUSELAGE DAMAGED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 270AY 0315 FLIGHT 718, PHL - FCO: ON CLIMBOUT, A/C TOOK A LIGHTNING STRIKE. FLIGHT RETURNED TO PHL. MAINTENANCE ACCOMPLISHED A L IGHTNING STRIKE INSPECTION, AND THE A/C WAS FERRIED TO CLT FOR FURTHER REPAIRS. CLT MAINTENANCE ACCOMPLISHED NUMEROUS B URNISHMENTS/REPAIRS TO AFFECTED AREAS OF FUSELAGE. 2 L 7 2 4F RT A46NM 2007062200152 20070622 00152 NM 2007 6 22 HNAA0700114 1 20070615 A 2750 SWITCH DHAV DHC8 DHC8102 2809003 NM T/E FLAP DIRTY A HNAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 07 942HA 163 CREW RETURNED TO THE FIELD IN MDT AFTER THE FLAPS WOULD NOT RETRACT. NO EMERGENCY DECLARED. CLEANED AND LUB MICROSWITC H AND LINKAGE ON FLAP CONSOLE. OPS CHECK OF FLAPS GOOD. 2 H 7 2 4T RT A13NM 2007062200153 20070622 00153 SO 2007 6 22 C2XA07RI045 1 20070609 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13997 145298 RIC - DURING SCHEDULED ROUTINE INSPECTION, MX FOUND LEFT OVERWING EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED LIGHT B ULB AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007062200157 20070622 00157 GL 2007 6 22 C2XA07RI047 2 20070616 A 7200 23039621 PLUG EMB 135 EMB135ER 3260203 SO ALLSN AE300 AE3007A GL NR 1 ENGINE DAMAGED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 27512 145274 CAE311547 FLT 2189 - EWR - CREW REPORTED ENG 1 PRODUCING WHITE/LIGHT GRAY SMOKE AFTER ENGINE SHUT DOWN. LARGE QUANTITY COMING OUT FROM FRONT AND BACK. OIL, HYD, FUEL INDICATIONS ARE NORMAL. THIS IS A REPEAT WRITE UP. EWR MX PERFORMED TROUBLESHOOT ING AND FOUND AFT SUMP SHAFT PLUG NEEDED REPLACEMENT. MX REMOVED AND REPLACED AFT SUMP SHAFT PLUG IAW RR MM 72-59-10 AN D PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007062200163 20070622 00163 NM 2007 6 22 HNAA0700115 1 20070617 A 3230 3261K13K12 RELAY DHAV DHC8 DHC8102 2809003 NM LANDING GEAR FAILED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 825EX 388 JUST AFTER TAKEOFF, GEAR DID NOT GO UP WHEN SELECTED. ONLY GETTING INDICATION OF 3 GREEN AND 3 RED LIGHTS. GEAR DID NO T GO UP. REMOVED AND REPLACED RELAYS 3261 K-13 AND K2, ON 6/18/2007 SWUNG GEAR 10 TIMES IN HANGER FOR OP'S CHECK, OPS C HECK GOOD. 2 H 7 2 4T RT A13NM 2007062200164 20070622 00164 EU 2007 6 22 UPS07149965 1 20070614 A 7830 THRUST REVERSER AIRBUS A300 A300F4622R 3930360 EU NR 2 ENGINE MALFUNCTIONED A IPXA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 SO 01 174UP 0005 INSPECTION TYPE:N/A IFSD - NR 2 ENGINE T/R UNLOCK LIGHT ILLUMINATED DURING APPROACH TO DENVER. *S/D* ACCOMPLISHED T/R CHECK PER AMM 78-31-40-05 & RVDT AND STOW/DEPLOY SW ASSY. ADJ/TEST FUNCTION AND INDICATIONS NORMAL. CYCLED T/R SEVERAL TIMES PNEUMATICALLY WITH NO ABNORMAL INDICATIONS. THIS CLEARS DEFERRAL. A/C OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2007062200165 20070622 00165 EU 2007 6 22 UPS07149972 1 20070615 A 5210 ROLLER AIRBUS A300 A300F4622R 3930360 EU PAX DOOR MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 168UP 0005 INSPECTION TYPE:N/A MAIN ENTRY DOOR HARD TO CLOSE. REMOVED UPPER AFT ROLLER ASSY. REINSTALLED ROLLER ASSY. REMOVED AN D REPLACED DOOR LOWERING LEVER STOP AND PERFORMED FUNCTIONAL TEST. ALL CHECKS NORMAL. REF MM 52-10-11-05 & 52-10-31. 2 L 7 2 4F RT A35EU 2007062200166 20070622 00166 NM 2007 6 22 UPS07549980 1 20070616 A 2560 LATCH BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 467UP 25483 INSPECTION TYPE:N/A F/O EMERGENCY ESCAPE ROPE DOOR UPPER LATCH INOP. RESET ROPE DOOR AS NEEDED. OPS CHECK OK PER 25-00 . 2 L 7 2 4F RT A2NM 2007062200169 20070622 00169 WP 2007 6 22 UPS07849975 1 20070609 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 LEFT WING CENTER L/E RIB PUNCTURED AND CRACKED AT STA SX515. REMOVED AND REPLACED CRACKED RIB AT LEF T WING STA XS515 IAW SRM 57-2-0 FIG 2, AND SRM 57-3-03 FIG 4. 2 L 7 4 4F RT 4A25 2007062200170 20070622 00170 2007 6 22 UPS07849979 4 20070616 A 2565 SLIDE DOUG DC8 DC871F 302199D WP COCKPIT OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:N/A ESCAPE SLIDE PRESSURE UNREADABLE. REPOSITION SLIDE INSIDE OF COVER. 2 L 7 4 4F RT 4A25 2007062200171 20070622 00171 WP 2007 6 22 UPS07849982 1 20070616 A 2560 FASTENER DOUG DC8 DC873F 302199F WP ESCAPE ROPE FAULTY A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:N/A CAPTAINS ESCAPE ROPE FELL OUT OF STOW LOCATION. CHECK FOR PROPER STOWAGE. REPLACED FASTENER FOR DO OR CLIP. REINSTALLED ROPE AND DOOR. OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 2007062200174 20070622 00174 NM 2007 6 22 CALA0700308 1 20070616 A 5420 65C260812 FITTING BOEING 737 7373T0 1384582 NM NR 2 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12313 23364 INSPECTION FOUND A .5 INCH CRACK IN NR 2 PYLON AFT HORSE COLLAR (FITTING) AT LOWER I/B NUT PLATE, FORWARD OF NR 6 FLAP T RACK. A NEW FITTING WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007062200175 20070622 00175 NM 2007 6 22 CALA0700309 1 20070618 A 5320 65458752 SILL BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27610 27323 INSPECTION FOUND R-1 DOOR SILL LOWER CHORD CORRODED AT STA 277-360, RBL 113. THE CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007062200176 20070622 00176 EA 2007 6 22 HNAA0700116 1 20070617 A 3350 6519020 LIGHT DHAV DHC8 DHC8311 1386006 EA CABIN INOPERATIVE A HNAA K NONE O OTHER CR CRUISE 1 EA 07 328EN 281 EMERGENCY ESCAPE PATH LIGHTING FLOOR LIGHT NR 14 INOP. REMOVED AND REPLACED LIGHT BULB. 2 H 7 2 4T RT A13NM 2007062200178 20070622 00178 NM 2007 6 22 DHL2007740549 1 20070615 A 5313 65564417 STRINGER BOEING 727 7272Q9 138448M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AFT PIT BETWEEN BS 950A AND 950C, CORROSION ON STR 29L. CORROSION BEYOND ACCEPTABLE LIMITS, REF SB 727-53-0179. GAINED ACCESS BY REMOVING ALL CARGO FLOOR SUPPORTS FROM BS 950A TO BS 990, RBL 16 TO LBL 16, FRAME SECTIONS AT BS 950E AND 950 F BETWEEN STR 24R AND 24L, FRAME SECTIONS AT BS 970 AND 990 BETWEEN STR 26R AND 24L, INTERCOSTAL WEBS FROM BS 950A-950B, 950E-950F, 950D-950E, 950F-970, AND 970-990, BETWEEN STR'S 29L AND 29R, PER B727 SRM 51-30-2 AND SB 727-53-0179. REMOV ED DAMAGED STR 29L FROM BS 950 TO BS 1000. LOCATED AND DRILLED NEW STR 29L SEGMENT, P/N 65-56441-7. TREATED AND PRIMED BARE METAL AREA'S, AND INSTALLED NEW STR 29L PER B727 SRM 51-30-2, 51-10-2, AND SB 727-53-0179. REINSTALLED ALL INTERC 2 L 7 3 4F RT A3WE 2007062200184 20070622 00184 NM 2007 6 22 SWAA073026 1 20070616 A 3350 1619 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 491WN 33867 DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007062200185 20070622 00185 NM 2007 6 22 SWAA073029 1 20070616 A 3350 1619 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 718SW 27852 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007062200188 20070622 00188 NM 2007 6 22 SWAA073028 1 20070616 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007062200190 20070622 00190 NM 2007 6 22 SWAA073023 1 20070615 A 5311 6546520 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007062200192 20070622 00192 NM 2007 6 22 SWAA073017 1 20070615 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007062200195 20070622 00195 NM 2007 6 22 SWAA073025 1 20070616 A 3260 655825029 LOGIC CARD BOEING 737 7373H4 1384600 NM NOSE BAY FAULTY A SWAA K NONE N FALSE WARNING DE DESCENT 1 SW 29 625SW 27701 LOWERED GEAR HANDLE, GOT THREE GREEN LIGHTS FOLLOWED BY LEFT MLG RED LIGHT FLICKERING. RECYCLED GEAR HANDLE GOT THREE G REEN LIGHTS. REMOVED AND REPLACED DOWN LOCK SENSOR AND LOGIC CARD PER MM. 2 L 7 2 4F RT A16WE 2007062200196 20070622 00196 NM 2007 6 22 SWAA073016 1 20070615 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007062200201 20070622 00201 NM 2007 6 22 SWAA073021 1 20070615 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007062200202 20070622 00202 NM 2007 6 22 SWAA073012 1 20070615 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007062200203 20070622 00203 NM 2007 6 22 SWAA073011 1 20070615 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007062500001 20070625 00001 NM 2007 6 25 07FDEA02223 1 20070620 A 3150 Z4600103 DISPLAY BOEING 727 727200 138407E NM COCKPIT BURNED A FDEA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 25 465FE 537 537 21289 PDIS 465 26-12 0009505 20JUN07 PIT OPEN R LOGPAGES: 01339908 APPROX 1 00 HOURS INTO FLIGHT, ALL CREWMEMBERS SMELLED A BURING SMELL AND SAW LIGHT SMOKE, SOURCE UNKNOW. PREFORMED PHASE ONES RED TAB PROCEDURE. DIVERTED INTO KPI T ENT BY: 001395 RPT BY: 235667 AFTER PULLING A/C TO THE GATE. CKED E&E FOR WATER/SMOKE. E&E CKED GOOD. NO WATER OR SMOKE VERY DRY. REMOVED AND REPLACED PAT CRADLE AND TERMINAL. REF TSI 45-13/9508. 2 L 7 3 4F RT A3WE 2007062500014 20070625 00014 CE 2007 6 25 AMWA7020C 1 20070612 A 5311 1294400681 FRAME BEECH 1900 1900D 1154162 CE BS 438 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 126YV UE126 FUSELAGE FRAMES DAMAGED BY FRICTION CHAFFING. REPAIRED IAW ACFT REPORT NR 6702-1 REV 1R 2 L 7 2 4T RT A24CE 2007062500015 20070625 00015 CE 2007 6 25 AMWA7020A 1 20070612 A 5311 1294300551 FRAME BEECH 1900 1900D 1154162 CE CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 126YV UE126 FUSELAGE FRAMES DAMAGED BY FRICTION CHAFFING. REPAIRED IAW REPORT 6702-1 REV 1R. 2 L 7 2 4T RT A24CE 2007062500016 20070625 00016 CE 2007 6 25 AMWA7020B 1 20070612 A 5311 12943006017 FRAME BEECH 1900 1900D 1154162 CE BS 408 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 126YV UE126 FUSELAGE FRAMES DAMAGED BY FRICTION CHAFFING. REPAIRED IAW REPORT 6702-1 REV 1R. 2 L 7 2 4T RT A24CE 2007062500017 20070625 00017 CE 2007 6 25 AMWA7020D 1 20070612 A 5730 11943000227 SKIN BEECH 1900 1900D 1154162 CE RT WING CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 126YV UE126 RT WING SKIN CRACKED BETWEEN FS303.25 AND FS310.75 AT WS25. LENGTH OF CRACK APPROX 5.5 INCHES. REPAIRED IAW REPORT 67 02-2 REV 1R. 2 L 7 2 4T RT A24CE 2007062500018 20070625 00018 CE 2007 6 25 AMWA7020E 1 20070612 A 5330 12940003193 SKIN BEECH 1900 1900D 1154162 CE BS 466 CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 126YV UE126 FUSELAGE SKIN CRACKED, LENGTH APPROX 1.5 INCHES. REPAIRED IAW REPORT #6702-3 REV 1R. 2 L 7 2 4T RT A24CE 2007062500019 20070625 00019 CE 2007 6 25 AMWA7026A 1 20070612 A 5712 11811005010 RIB BEECH 1900 1900D 1154162 CE RWS 125 CORRODED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 126YV UE126 BIO CORROSION RT WING RIB AT WS125.00; AREA NEAR THE ATTACHMENT OF THE RIB TO THE MAIN SPAR. REPAIRED IAW A REPORT 6702 -4 REV 1R. 2 L 7 2 4T RT A24CE 2007062500020 20070625 00020 CE 2007 6 25 AMWA7026B 1 20070612 A 5414 11811001541 SKIN BEECH 1900 1900D 1154162 CE LT NACELLE CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 126YV UE126 FRICTION CHAFING DURING OPERATION HAS CAUSED WORN SEGMENTS ON THE LT NACELLE (TURTLEBACK) SKINS. REPAIRED IAW REPORT 67 02-5 REV 1R. 2 L 7 2 4T RT A24CE 2007062500021 20070625 00021 CE 2007 6 25 AMWA7026C 1 20070612 A 5414 1181100152 SKIN BEECH 1900 1900D 1154162 CE RT NACELLE CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 126YV UE126 FRICTION CHAFING DURING OPERATION HAS CAUSED WORN SEGMENTS ON THE RT NACELLE (TURTLEBACK) SKINS. REPAIRED IAW REPORT 67 02-5 REV 1R. 2 L 7 2 4T RT A24CE 2007062500022 20070625 00022 CE 2007 6 25 AMWA7026D 1 20070612 A 5712 11811005012 RIB BEECH 1900 1900D 1154162 CE LT WING CORRODED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 126YV UE126 BIO CORROSION LT WING RIB AT WS 124.588, NEAR WHERE RIB ATTACHES TO MAIN SPAR. REPAIRED IAW REPORT 6702-6 REV 1R. 2 L 7 2 4T RT A24CE 2007062000065 20070620 00065 NM 2007 6 20 2007UALA01875 1 20070606 A 1100 PLACARD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 EMERGENCY EXIT SIGN RIGHT SIDE LOOSE BETWEEN FIRST AND BUSINESS CLASS. [07-03-07] REPOSITIONED PHOTO LUMINESCENT AISLE PATH REF TO MM 33-50-99, CKD OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062000069 20070620 00069 SO 2007 6 20 FDKA200705203 1 20070513 A 2560 GLOWSTRIP EMB 145 EMB145LR 3260212 SO CABIN MISSING A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 828MJ 145218 FDM 6068 BMI-ATL (1150 PHX LCL) - CAPT CALLED SAYING PHOTOLUMINESCENT STRIP WAS MISSING. MX INSPECTED AND FOUND NO DEFE CTS. 2 L 7 2 4T RT T00011AT 2007062000070 20070620 00070 SO 2007 6 20 FDKA200705210 1 20070517 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN DISCONNECTED A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6037 CLT-CVG (0324 PHX LCL) - EMERGENCY LIGHTS INOP AT MIDDLE ROW. MX RECONNECTED THE ELECTRICAL CONNECTOR, OPS CHE CK NORMAL. 2 L 7 2 4T RT T00011AT 2007062000079 20070620 00079 NM 2007 6 20 DHL2007740531 1 20070522 A 5322 SHEAR TIE BOEING 727 7272Q9 138448M NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 WHILE IN "C" CHECK, AFT CARGO COMPARTMENT SHEAR TIE AT BS 970 BETWEEN STR.25L AND 24L IS CRACKED AT LOWER END. REMOVED CRACKED SHEAR TIE "T" EXTRUSION IAW B727 SRM 51-30-2. FABRICATED NEW SHEAR TIE FROM BAC1505-100246 PO NR 650418 DIM 7" IAW B727 SRM 53-10-2 FIG 5 AND 51-20-1. TREATED AND PRIMED NEW SHEAR TIE IAW B727 SRM 51-10-2 AND INSTALLED NEW SHEAR T IE AT AFT CARGO COMPARTMENT BS 970 BETWEEN STR 24L AND 25L IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007062000084 20070620 00084 NM 2007 6 20 07FDEA02125 1 20070613 A 5754 ARB2886504 SKIN DOUG MD11 MD11F 3023600 NM L/E SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING NR 3 SLAT TELESCOPIC DUCT CUT-OUT FOUND CRACKED APPROX 0.25" IN LENGTH. [07-03-07] REPAIR CARRIED OUT AS PER S RM 57-10-00 FIG. 43 VOL.I. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062000091 20070620 00091 CE 2007 6 20 BSAASDR0720 1 20070602 A 3610 1560283000 EVA TUBE BEECH 1900 1900D 1154162 CE RT WING DAMAGED A BSAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 05 131YV UE131 DURING CLIMB TO ALTITUDE, THE RT BLEED AIR FAIL ANNUNCIATOR LIGHT CAME ON AT 12,500FT. CREW FOLLOWED CHECKLIST PROCEDUR ES, SHUT OFF BLEED ON RIGHT SIDE AND RETURNED TO STATION, LIGHT WENT OUT AT 8,000FT DURING RETURN TO STATION. INITIALLY DEFERRED RT BLEED SYSTEM IAW THE MEL. TROUBLESHOOTING FOUND ANOTHER HOLE IN THE EVA TUBING IN THE RT WING LEADING EDGE . SYSTEM OPS CHECK GOOD. A REPLACEMENT OF ALL EVA TUBING ON THIS AIRCRAFT IS BEING EVALUATED. THE TUBING IS GETTING B RITTLE WITH AGE CAUSING CRACKS & SPLITS & IS ALSO BLOWING OUT. A FLEET CAMPAIGN TO REPLACE EVA TUBING IN ALL AIRCRAFT H AS BEEN ISSUED. 2 L 7 2 4T RT A24CE 2007062000101 20070620 00101 SO 2007 6 20 C2XA07IA141 1 20070609 A 3320 LIGHT EMB 145 EMB145EP 3260221 SO CABIN MALFUNCTIONED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 27 16927 145006 IAH - FLIGHT 2830, THE CREW REPORTED THAT THE READING LIGHT AT SEAT 5A FLICKERED ON AND OFF AND CREATED SMOKE. THE F/A PUSHED THE RESET BUTTON AND THE LIGHT WOULD NOT TURN OFF. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AFFECTED READING LIGHT AND CABIN AREA WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007062000107 20070620 00107 WP 2007 6 20 UPS07849960 1 20070609 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 LEFT WING CENTER LEADING UPPER RIB CRACKED XS497. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2 RE PAIR DOUBLERS IAW SRM 57-03-03 FIG 004, 51-1-20D. 2 L 7 4 4F RT 4A25 2007062000110 20070620 00110 WP 2007 6 20 UPS07849963 1 20070606 A 5730 DOUBLER DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE LWR INNER DOUBLER POSSIBLE CRACK AT XFS 597 AROUND DRAIN HOLE. REMOVED INNER DOUBLER. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW 57-3-3 FIG 7, 51-1-21. 2 L 7 4 4F RT 4A25 2007062000112 20070620 00112 NE 2007 6 20 UPS07849966 2 20070614 A 7200 ENGINE DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE NR 3 FLAMED OUT A IPXA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 SO 01 700UP 45900 INSPECTION TYPE:N/A IFSD - NR 3 ENGINE FLAMED OUT AT 35000FT W/BOOST PUMP OFF. CREW VERBALLY REPORTED, LEFT NR 3 MAIN B OOST PUMP SWITCH OFF. THIS WILL NOT ALLOW FUEL TO FILL RESERVOIR. ACCOMPLISHED IDLE HIGH FUEL RUN WITH BOOST/FUEL PUMP SWITCH OFF AND NASH PUMP FUEL PRESSURE WAS 18 PSI IDLE 28 PSI AT FULL. 2 L 7 4 4F 4 F RT 4A25 E2GL 2007062000127 20070620 00127 NM 2007 6 20 2007UALA01939 1 20070609 A 3260 WARNING SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT MALFUNCTIONED A UALA O OTHER N FALSE WARNING AP APPROACH 1 WP 29 543UA 25698 GEAR DISAGREE LIGHT ON FINAL. RECYCLED GEAR AND GOT NORMAL INDICATIONS. [07-10-07] BITE TEST ON PSEU SHOWS 421, 422, 423, 424. REPLACED LANDING GEAR CONTROL HANDLE MODULE. OPS AND BITE TEST OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007073000066 20070730 00066 NM 2007 7 30 07FDEA02608 1 20070725 A 5230 65561431 SKIN BOEING 727 727233 138408A NM CARGO DOOR MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 286FE 22623 ON AGING AC INSP, FOUND EXISTING REPAIR LOCATED ON NR 3 LOWER CARGO DOOR SKIN 31" FROM BOTTOM EDGE FROM 1" TO 48" FROM F WD EDGE. DID NOT CONFORM TO SRM 52-00-3 FIG 3. REMOVED 2 EXISTING DOUBLER, INSTALLED 1 DOUBLER TO REPAIR AREA REF SRM 52-00-3. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007062000135 20070620 00135 NM 2007 6 20 2007UALA01950 1 20070610 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 525UA 24978 EEL LIGHTS INOP AT ROWS 5-8 & EXIT LIGHTS OVERWING DOORS. [06-22-07] REPLACED THE BATTERY ON BATTERY EMERG BATTERY C HARGER M10567 & OPS CHECK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062000147 20070620 00147 NM 2007 6 20 2007UALA01962 1 20070611 A 5210 TORQUE TUBE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT ENTRY DOOR LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 AFT ENTRY DOOR CUTOUT TORQUE TUBE HAS PLAY OVER .0030 BEYOND LIMITS. REPLACED DOOR BODY TORQUE TUBE & UPPER AND LOWER B EARINGS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062000149 20070620 00149 NM 2007 6 20 2007UALA01964 1 20070611 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 EMERGENCY LIGHTS AT SEAT 53HJK, 32ABC & 47ABC ARE INOP. [06-22-07] REPLACED LIGHT STRIP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000151 20070620 00151 NM 2007 6 20 2007UALA01966 1 20070611 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 EMERGENCY EXTERIOR OVERWING LEFT FWD LIGHT BULB INOP. [06-22-07] RELAMPED AND NO HELP. REPLACED LIGHT ASSY. AND GRD C HECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000166 20070620 00166 NM 2007 6 20 2007UALA01981 1 20070612 A 2760 MODULE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SPOILER FAILED A UALA O OTHER O OTHER DE DESCENT 1 WP 29 210UA 30216 SPOILERS FAILURE OF ONE OR MORE SPOILER PAIRS. [07-13-07] PULLED CIRCUIT BREAKER. RERACKED ACTUATOR CONTROL ELECTRONIC S (ACE) - L2 MODULE. RESET CB AND PERFORMED PRIMARY FLIGHT CONTROL MAINT ACCESS TERMINAL (MAT) TEST, PASSED. MSG NOT AC TIVE AND SPOILER ADVISORY ON UPPER EICAS NOT IN VIEW. CKS OK FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007062000182 20070620 00182 NM 2007 6 20 2007UALA02001 1 20070613 A 3230 LANDING GEAR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C CL CLIMB 1 WP 29 304UA 23665 AFTER TAKEOFF, LANDING GEAR LEVER WOULD NOT MOVE UP. CREW USED MANUAL OVERRIDE AND GEAR RETRACTED. [07-03-07] REPLACE D THE M991 LOGIC CARD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062200008 20070622 00008 NM 2007 6 22 2007UALA01995 1 20070613 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN MISWIRED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 CIRCUIT BREAKER TRIPS WITH LED LENS CAPS INSTALLED AT DOORS 2L & 4L. [08-07-07] AIRCRAFT SIDE OF LIGHT ASSEMBLY WAS W IRED BACKWARDS PER THE INVESTIGATING OFFICER, REINSTALLED INCANDESCENT LENS CAPS AT 2L & 4L. PUT 2 LED LENS CAPS IN LOB BIN. INSTALL LED LENS CAPS AFTER REPAIRING AIRCRAFT WIRING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062200011 20070622 00011 EU 2007 6 22 2007UALA02003 1 20070613 A 5311 FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 435UA 613 FWD PIT FRAME 32 HAS A CORRODED CLEAT AT STRINGER 41R. MAJOR REPAIR ACCOMPLISHED: REPLACED WITH NEW CLEAT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062200030 20070622 00030 NM 2007 6 22 SWAA072983 1 20070613 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007062200042 20070622 00042 NM 2007 6 22 SWAA073005 1 20070614 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007062200044 20070622 00044 NM 2007 6 22 SWAA073007 1 20070614 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007062200059 20070622 00059 NM 2007 6 22 07FDEA02130 1 20070614 A 5753 STRAP DOUG MD11 MD11F 3023600 NM T/E FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT OUTBOARD FLAP INBOARD FORWARD HINGE TENSION STRAP FOUND CRACKED. [07-03-07] REMOVED AND REPLACED AS PER SRM 51-33-0 1 VOL.II. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062200060 20070622 00060 NM 2007 6 22 07FDEA02132 1 20070614 A 5330 651753073 SKIN BOEING 727 727233 138408A NM FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 286FE 22623 ON AGING A/C INSP, FOUND FWD RT CORNER OF AIR STAIR CUTOUT DID NOT CONFORM TO FED EX DWG SR27-53-024. REMOVED OLD DOUB LER, HFEC INSP TO VERIFY CRACK CONTAINMENT, MANUFACTURED NEW DOUBLER REF, FED EX DWG 27-53-024. 2 L 7 3 4F RT A3WE 2007062200062 20070622 00062 NM 2007 6 22 SWAA072994 1 20070614 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 14Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP MISSING AT ROW 13 ABC. INSTALLED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007062200064 20070622 00064 NM 2007 6 22 KCSA071192 1 20070616 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 FUSELAGE SKIN HAS CORROSION AT STA 2235, BETWEEN STR 29R & 30R. 2 L 7 4 4F A20WE 2007062200095 20070622 00095 EU 2007 6 22 07FDEA01893 1 20070521 A 5730 A57710013 SKIN AIRBUS 310 A310222 3930315 EU LT WING MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON LT WING UPPER SURFACE, OUTB OF SPOILER 3 WS935 RIB 15. REPAIR REQUIRES EVALUATION FO R MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO A SRM REPAIR. NEW OVERSIZE FASTENERS WERE INSTALLED ON EXISTING HOLES IN ACCORDANCE WITH SRM 51-40-23. 2 L 7 2 4F RT A35EU 2007062200098 20070622 00098 WP 2007 6 22 07FDEA02136 1 20070615 A 5420 AUB7063501 WEB DOUG DC10 DC1010 3022110 WP NR 3 PYLON WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 ON PYLON, NR 3 DEEP WEAR ON UPPER SURFACE OF HORIZONTAL WEB AT STA YN 200. REPAIRED IAW SRM 54-20-00 FIG 5. 2 L 7 3 4F A22WE 2007062200101 20070622 00101 WP 2007 6 22 07FDEA02139 1 20070615 A 5330 REPAIR DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 EXISTING REPAIR EXT FUSELAGE AT SAT 339 X=31 REPAIR IAW 53-20-00 FIG 6 AND SRM 57-30-00. 2 L 7 3 4F A22WE 2007062200105 20070622 00105 NM 2007 6 22 ANCF200700014 1 20070611 A 7331 TUBE BOEING 757 757236 1384971 NM RT ENGINE MALFUNCTIONED W ANCF A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 23 521NA 25592 DURING CRUISE AT FL 370 A DIFFERENCE BETWEEN BOTH ENGINE FUEL FLOWS WAS DETECTED WHILE THE OTHER ENGINE PARAMETERS WERE NORMAL LITTLE BY LITTLE THE FF DIFFERENCE WAS INCREASING UNTIL LEFT FF 5686 AND RIGHT FF 2678. THE AIRSPEED WAS AFFECTE D BY THIS CONDITION SO WE HAD TO DESCEND IN ORDER TO INCREASE THE SPEED AND THERE WAS A BIG DIFFERENCE BETWEEN THE PARAM ETERS OF BOTH ENGINE, SEE PARAMETERS BELOW. EPR1 1,711 EPR2 2.076. N1(1) 96.3 N1(2) 75.6. EGT1 701 EGT2 532 N2(1) 89.3 N2(2) 73.5 N3(1) 89.7 N3(2) 79.5 FF1 5683 FF2 2678 DUCT PRESS1 35 DUCT PRESS2 46 VN1(1)0.7 VN1(2)0.2 VB1 0.8 CB2 1.4 OIL PRESS 1 78 OIL PRESS 2 73 OIL TEMP 1 112 OIL TEMP 2 104. IN ACCORDANCE WITH AMM 77-11-04 PAGE 601 P1. TUBE WAS REPLAC 2 L 7 2 4F RT A2NM 2007062200111 20070622 00111 2007 6 22 QXEA20070966 4 20070614 A 2340 536014 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA CABIN FAILED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 617QX 9990 10130 DEN - FLIGHT 4207, ON TAXI UNABLE TO CALL OR COMMUNICATE WITH THE FLIGHT ATTENDANT ON THE PA SYSTEM. RETURNED TO THE GA TE. MAINTENANCE REPLACED THE AECU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007062200117 20070622 00117 EU 2007 6 22 MALA070068 1 20070602 A 2150 1134160 COMPRESSOR SAAB SF340 340B 7860101 EU SUPPLEMENTAL A/C MALFUNCTIONED A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 15 411XJ 340B411 SUPPLEMENTAL A/C. SMOKE SMELL IN CABIN DETERMINED SMOKE SMELL TO BE R134A REFRIGERANT THAT LEAKED FROM SUPP AC. CAPTAI N REPORTED SMELL WENT AWAY WHEN AC WAS SWITCHED OFF. SUPP AC DEACTIVATED AND DEFERRED PER MEL 21-50-02. NO SMOKE SMELL NOTED WHILE A/C WAS GROUND RAN FOR 15 MINUTES WITH LT AND RT BLEEDS ON. REPLACED COMPRESSOR BELT PN 232L100, COMPRESSO R PN ON/OFF 1134160, SN ON 1665, S/N OFF 1856, REPLACED RECEIVER DRYER PN 1134192-2. 2 L 7 2 4T RT A52EU 2007062200139 20070622 00139 NM 2007 6 22 DHL2007740536 1 20070616 A 5313 STRINGER BOEING 727 7272Q9 138448M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 DURING C CHECK REF N/R 053895, NOSE SECTION STR 24L BS305 SHOWS CORROSION SEEN FROM LT TRUNNION ACCESS AREA. ACTION CUT -OUT DAMAGED SECTION OF STRINGER DIM 6 3/8" LENGTH, FABRICATED REPAIR FILLER FROM BAC 1498-137 PO 4496178 DIM 6 5/8 REPA IR U CHANNEL FROM BAC1493-412 PO NR 7191256 DIM 13"LENGTH AND REPAIR J ANGLES 2EA FROM 7075-T6 .050 PO NR 9004670 DIM NR 9004670 DIM 13" LENGTH IAW B727 SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9. TREATED AND PRIMED REPAIR PARTS IAW B727 SRM 51-1 0-2 AND INSTALLED REPAIR PARTS AT NOSE SECTION STRINGER 24LT BS 305 IAW B727 SRM 53-10-3 FIG1 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007062200156 20070622 00156 NM 2007 6 22 DHL2007740547 1 20070610 A 5311 FRAME BOEING 727 7272Q9 138448M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AFT CARGO BS 950C STR27L TRU STR27R FWD SIDE FRAME FLANGES HAVE CORROSION. REMOVED CORROSION IAW B727 SRM 51-10-6, ORIG MAT. IS .063" IAW B727 SRM 53-10-2 FIG 5 MAT LOSS FOR STR 28R IS .004" REMAINING MAT .059" FOR 28R THRU 29R IS .005 REM AINING MAT .056" FOR STR 29R THRU 30R IS .004" REMAINING MAT .059" FOR STR 30 THRU 29L IS .006" REMAINING MAT IS .057" F OR STR 29L THRU 28L IS .005" REMAINING MAT IS .058", FOUND ALL WITHIN LIMITS MAT LOSS FOR STR 28L THRU 27L IS .O40" REMA INING MAT .023' FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. CUT OUT DAMAGED SHEAR TIE DIMENSION 7' BY 1" AT S TR 27L-28L IAW B727 SRM 53-10-4 FIG11. FAB SHEAR TIE REPAIR FROM 7075-0 .071" PO NR 9004690 DIMENSION 7" BY 3" BY 1" IA 2 L 7 3 4F RT A3WE 2007062200159 20070622 00159 EU 2007 6 22 SA07039 1 20070617 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU CABIN FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 18874 18290 0885 DCA - WHEN PLACING THE EMERGENCY EXIT LIGHT SWITCH TO ARM WITH THE AIRCRAFT POWERED, THE AFT EXIT AND AFT PORTION OF THE EMERGENCY EXIT LIGHTS COME ON. MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT AND BATTERY. OPERATIONALLY CH ECKS OK. 2 L 7 2 4F RT A28NM 2007062200167 20070622 00167 NE 2007 6 22 UPS07649926 2 20070507 A 7220 CASE BOEING 767 76734AF 1385212 NM GE CF6 CF680C2B7 NE NR 1 ENGINE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 306UP 27759 INSPECTION TYPE:C2 NR 1 ENGINE CORROSION ON AFT FAN CASE AT 5-6:30 POS AT NUT PLATES 8 INCHES FROM AFT END OF CASE. REP AIRED PER UPS ENGINEERING FILE NUMBER 80C2-72-20000. 2 L 7 2 4F 4 F RT A1NM E13NE 2007062200172 20070622 00172 NM 2007 6 22 UPS07M49971 1 20070614 A 5610 SLIDING WINDOW DOUG MD11 MD11F 3023600 NM COCKPIT OUT OF ADJUST A IPXA K NONE O OTHER UK UNKNOWN 1 SO 01 252UP 48768 INSPECTION TYPE:N/A FIRST OFFICER'S SLIDING WINDOW W/N CLOSE. *S/D* ADJUSTED WINDOW PER MM 56-10-01-5. 2 L 7 3 4F RT A22WE 2007062200173 20070622 00173 NM 2007 6 22 CALA0700307 1 20070616 A 5330 146N3531 SKIN BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 57111 27301 INSPECTION FOUND FUSELAGE SKIN CORRODED UNDER RT AIRFONE ANTENNA AT STA 1510, RBL 10, S28R-29R. A DOUBLER AND FILLER WE RE INSTALLED IAW SRM 53-00-01, REPAIR NR 5. 2 L 7 2 4F RT A2NM 2007062200187 20070622 00187 NM 2007 6 22 SWAA073009 1 20070615 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 232WN 32500 EEPLS COVER MISSING ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007062200189 20070622 00189 NM 2007 6 22 SWAA073027 1 20070616 A 5330 6545767118 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 395, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007062200197 20070622 00197 NM 2007 6 22 SWAA073019 1 20070615 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007062200198 20070622 00198 2007 6 22 SWAA073008 4 20070615 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 636WN 27709 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007062200199 20070622 00199 2007 6 22 SWAA073014 4 20070615 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007062200200 20070622 00200 2007 6 22 SWAA073013 4 20070615 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007062200204 20070622 00204 NM 2007 6 22 SWAA073010 1 20070615 A 2560 P2010001101 FLASHLIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 771SA 27879 AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2007062500023 20070625 00023 CE 2007 6 25 J00A200700001 1 20070329 A 2720 99145586 ACTUATOR CESSNA 750 750 2076810 CE RUDDER BINDING E J00A O OTHER O OTHER TX TAXI/GRND HDL 1 EA 01 32NG 5648 5648 7500039 RUDDER MOVEMENT WAS RESTRICTED TO 100% OF FULL TRAVEL AFTER LANDING AT KPBG. DISCOVERED ACTUATOR WOULD NOT MOVE ON SUBS EQUENT BENCH TESTS AFTER REMOVED FROM AIRFRAME. 2 L 7 2 4J RT T00007WI 2007062500024 20070625 00024 CE 2007 6 25 GLBA20060954 1 20070613 A 2150 ACM BEECH 1900 1900D 1154162 CE CONTAMINATED A GLBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 170GL UE170 AIR RETURN - FLIGHT 5134 - ENROUTE FROM LBF TO DEN PILOTS REPORTED SMOKE/MIST IN THE CABIN AFTER DEPARTURE. MAINTENANCE TROUBLESHOT THE ISSUE AND FOUND NO SMOKE, HOWEVER, MIST WAS WAS REPORTED AND MAINTENANCE FOUND AN EXCESSIVE AMOUNT OF MO ISTURE IN THE AIR CYCLE MACHINE. MAINTENANCE REMOVED MOISTURE PERFORMED A SYSTEM OPERATIONAL CHECK. REFERENCE 1900D MM 2 1-50. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A24CE 2007062500026 20070625 00026 EU 2007 6 25 BAQB200700018 1 20070506 A 6210 1090103019 BLADE AGUSTA A109 A109E 0260119 EU MAIN ROTOR CRACKED E BAQA O OTHER E VIBRATION/BUFFET CR CRUISE 1 EA 03 109CJ 2031 7280 DURING A MAINTENANCE CHECK FLIGHT PILOT NOTICED A UNUSUAL VIBRATION. PILOT LANDED WITHOUT INCIDENT. UPON INSPECTION MECH ANIC FOUND A CRACK IN THE MAIN ROTOR BLADE P/N 109-0103-01-9 S/N 1841R. THE CRACK STARTED AT A REPAIR IN THE BLADE. THE BLADE WAS REPLACED WITH A SERVICEABLE BLADE P/N 109-0103-01-9 S/N 1888R. GROUND RUN AND MAIN ROTOR BALANCE COMPLIED WI TH.THE DEFECTIVE BLADE WAS SENT TO AGUSTA AEROSPACE CORP. IN PHILADELPHIA, PA. NO DEFECTS NOTED. ALL WORK DONE I.A.W. A 109AII M.M. CHAPTER 65.THIS AIRCRAFT IS FROM OUR AIRLIFT NORTHWEST OLYMPIA,WA BASE. 1 G 7 2 3U RT H7EU 2007062500029 20070625 00029 EA 2007 6 25 MALA070069 1 20070609 A 3610 REGULATOR VALVE CNDAIR CL600 CL6002D24 1390016 EA NR 2 ENGINE ODOR A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 15 901XJ 15130 FA AND PASSENGERS REPORTED STRONG ODOR OF JET FUEL DURING APPROACH AFTER GEAR EXTENSION. NR 2 ENGINE SEAL PRESSURE REGUL ATOR VALVE WAS REPLACED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007062500030 20070625 00030 CE 2007 6 25 GUUA05280701 1 20070528 A 2730 ELEVATOR BEECH 1900 1900D 1154162 CE STUCK A GUUA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 17 231Y UE231 ELEVATOR CONTROL STUCK ON APPROACH / BINDING --- ACCESSED & INSPECTED BELLCRANKS, PULLEYS, PULLET GUIDES, CABLE RUNS, CA BLE PASS THROUGHS. NO DEFECTS NOTED. ELEVATORS HAVE FREE UNOBSTRUCTED TRAVELS. TEST FLIGHT SATISFACTORY. 2 L 7 2 4T RT A24CE 2007062500031 20070625 00031 CE 2007 6 25 DJFA2007063 1 20070611 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 454LX 2596 RK327 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE LEFT INBOARD HORIZON TAL STABILIZER, BOTH LEFT AND RIGHT INBOARD RIBS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN BEECHJET COMMUNIQUE' NUMBER 70. MAINTENANCE REPLACED BOTH RIB ASSEMBLIES. 2 H 7 2 4F RT A16SW 2007062500032 20070625 00032 CE 2007 6 25 DJFA2007064 1 20070611 A 2611 473054 SMOKE DETECTOR RAYTHN DH125 HAWKER800XP 7150012 CE LAVATORY INTERMITTENT E DJFA O OTHER N FALSE WARNING DE DESCENT 1 EA 23 821LX 7951 258406 TRIP NR 1188829 CREW REPORTED BAGGAGE FIRE LIGHT CAME ON INTERMITTENTLY DURING THE CLIMB AND DESCENT, NO SMOKE WAS DETEC TED. MAINTENANCE FOUND THE LAV SMOKE DETECTOR INTERMITTENT. THE DETECTOR WAS REPACED. 2 L 7 2 4F RT A3EU 2007062500033 20070625 00033 CE 2007 6 25 DJFA2007065 1 20070613 A 5514 BRACKET BEECH MU300 400A 1155402 CE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 497CW 2074 2074 RK297 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE LEFT INBOARD HORIZON TAL STABILIZER, THE AFT RH ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN BEECHJET COMMUNIQUE' NUMBER 70. MAINTENANCE REPLACED THE ROLLER BRACKET ASSEMBLIES. 2 H 7 2 4F RT A16SW 2007062500034 20070625 00034 CE 2007 6 25 DJFA2007066 1 20070614 A 5514 BRACKET BEECH MU300 400A 1155402 CE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 798TA RK198 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE LEFT INBOARD HORIZON TAL STABILIZER, THE RIGHT AFT INBOARD ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA A RE OUTLINED IN BEECHJET COMMUNIQUE' NUMBER 70. [07-02-07] MAINTENANCE REPALCED THE ROLLER BRACKET ASSEMBLY. 2 H 7 2 4F RT A16SW 2007062500118 20070625 00118 SO 2007 6 25 SWIA200718346 1 20070610 A 4900 POWER UNIT EMB 120 EMB120ER 3260203 SO APU SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 581SW 120349 APU BLEED AIR IS CAUSING SMOKE IN THE COCKPIT. REPLACED APU WITH SERVICEABLE UNIT IAW EMB MM 49-00-02, P/N 3800376-1, S /N OFF: P0445. 2 L 7 2 4T RT A31SO 2007062500131 20070625 00131 NM 2007 6 25 UIEA200700243 1 20070610 A 5314 SKIN BOEING 747 747243B 1384830 NM NR 3 NACELLE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 NR 3 PYLON ACCESS PANEL 473BL CUTOUT CRACKED AT FORWARD UPPER CORNER. NR 3 PYLON ACCESS PANEL 473BL CUTOUT SKIN REPAIR AS PER BOEING MESSAGE 1-351455345-3 AND FAA FORM 8100-9. 2 L 7 4 4F A20WE 2007062600001 20070626 00001 NM 2007 6 26 QXEA200700972 1 20070617 A 3150 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM DE ICE LIGHT UNKNOWN A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 404QX 4046 BLI FLIGHT NR 2491: INTERMITTENT DEICE PRESSURE CAUTION LIGHT WHEN BOOTS WERE SELECTED. LIGHT WENT OUT WHEN THE CHECKLI ST WAS RUN. MAINTENANCE C/W OPERATION OF CHECKLIST IAW AMM TASK 30-11-00-710-804 WITH NO DEFECTS NOTED AND OPERATED BOO TS NUMEROUS TIMES TO ENSURE DEICE PRESSURE CAUTION LIGHT DID NOT ILLUMINATE. LIGHT DID NOT COME ON. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007062600002 20070626 00002 NM 2007 6 26 QXEA200700973 1 20070616 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 405QX 4047 SEA FLIGHT NR 2436: 'CHECK PFD 1' AND 'CHECK ED' MESSAGES APPEARED ON TAXI OUT. AIRCRAFT RETURNED TO THE GATE. MAINTE NANCE C/W FIM PROCEDURE TASK 31-61-01-810-804 AND TASK 31-61-01-810-807. C/W THE OPS CHECK OF THE NR 1 AND NR 2 PFD'S A ND MFD'S AND ED PER MTC 6316104, MTC 6316101 AND AMM TASK 31-61-01-710-803. ALL CHECKS GOOD. CHECKED CDS FOR FAULTS. NO FAULTS NOTED. MESSAGE DID NOT REOCCUR. AIRCRAFT IS CAT III, REMAINS CAT III. PLACARD READS CAT III. MTX CONTROL W AS NOTIFIED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007062600004 20070626 00004 2007 6 26 QXEA200700975 2 20070618 A 7200 ENGINE BOMBDR DHC8 DHC8402 1390042 NM NR 2 VIBRATION A QXEA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 09 405QX 4047 GEG FLIGHT NR 2324: ON CLIMB-OUT OF SEA AT 14,000 FT, THE AUTOPILOT WAS SHUT OFF AND MOMENTARILY LEVELED OFF. FELT A ST EADY VIBRATION (HIGH FREQUENCY) THROUGHOUT BOTH YOKES. A/S 260, PROPS 850 POWER LEVER RATING DETENT. WHEN AUTOPILOT WA S SELECTED, VIBRATION SUBSIDED BUT WAS STILL PRESENT. ON STEEP DESCENT INTO GEG, THE VIBRATION WAS LESS. TURNED ANVS O FF AND IT DIDN'T MAKE A DIFFERENCE. AIRCRAFT DIVERTED TO GEG. MAINTENANCE PERFORMED A GVI OF AIRCRAFT AND ENGINES AND FOUND NR 2 ENGINE HCTS INDICATOR PIN LOW. SERVICED IAW AMM 71-22-00-600-801. PERFORMED BALANCE OF NR 1 AND NR 2 PROPS IAW MTC 6611001. NO PARTS REPLACED AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007062600006 20070626 00006 NM 2007 6 26 DHL2007783518 1 20070613 A 5753 6521630222 SKIN BOEING 727 727227 1384078 NM TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 RT WING INBD FOR FLAP WS 230, HAS LARGE DENT. CUT OUT DENTED/DELAMINATED APPROX AREA DIM 5 BY 10.5, REMOVED DAMAGED COR E DIM. 5 BY 10.5, APPLIED VACUUM AND HEAT TO REMOVE MOISTURE IAW B727 SRM 57-50-2, FIG 3 AND 51-40-20, PARA 7. FABRICAT ED COVE PLUG 5.1 BY 10.5 FROM DUR-5052-4.4-3/16-N-1.0. INSTALLED, CURED AND SANDED AREA IAW B727 SRM 51-40-20, PARA 5 A ND 57-50-2, FIG 3. FABRICATED DOUBLER, 13.5 BY 8.1 FROM .016, ANODIZED, PRIMED, APPLIED ADHESIVE FILM AND INSTALLED IAW B727 SRM 51-10-2, 51-40-20, PARA 8, 51-40-24, FIG 1 AND 57-50-2. 2 L 7 3 4F A3WE 2007062600007 20070626 00007 EU 2007 6 26 07FDEA01564 1 20070424 A 5313 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 FOUND THE FOLLOWING STRINGER CORRODED: P52, C67-70 LT (P/N A539-73320-201); P49, C67-69 LT (P/N A539-74203-216); P4 8, C67-70 LT (P/N A539-74203-212); P46, C65-68 LT (P/N A539-74203-208) AND P53, C66-68 LT (P/N A539-74203-222). CLIP C6 7, P56-57 LT (P/N A539-74223-214) IS ALSO CORRODED. STRINGER REPAIR PERFORMED IAW SRM 53-10-14/FIG 201 AND REPLACEMENT OF CLIP (A539-74223-214) IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007062600008 20070626 00008 EU 2007 6 26 07FDEA01882 1 20070521 A 5753 A57971311 FLAP AIRBUS 310 A310222 3930315 EU ZONE 500 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON LT LWR WING SURFACE T/E OF OUTBOARD FLAP WS 874-935 RIB 14-15. REPAIR REQUIRES EVALUAT ION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 57-53-12 FIG 208. 2 L 7 2 4F RT A35EU 2007062600010 20070626 00010 EU 2007 6 26 07FDEA01899 1 20070521 A 5753 A57971311 FLAP AIRBUS 310 A310222 3930315 EU ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON RT UPPER WING SURFACE INBD OF OUTBOARD FLAP WS 663-737 RIB 11-12. REPAIR REQUIRES EVAL UATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. THE PRESENT SDR CONCER NS THE SAME NR AS SDR 07-2201. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPL ISHED PER SRM 57-53-12 FIG 208. 2 L 7 2 4F RT A35EU 2007062600011 20070626 00011 EU 2007 6 26 07FDEA01905 1 20070521 A 5753 A57971311 FLAP AIRBUS 310 A310222 3930315 EU ZONE 600 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON RT LOWER WING SURFACE OF OUTBOARD FLAP WS 874-935 RIB 14-15. REPAIR REQUIRES EVALUATIO N FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. THE JASC/ATA CODE INDICATED SHOULD BE 5750. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 57-53-12 FIG 208 AND FEDEX EA 6-5710-112416. 2 L 7 2 4F RT A35EU 2007062600012 20070626 00012 NM 2007 6 26 07FDEA02082 1 20070607 A 5330 ADA3139503 SKIN DOUG MD11 MD11F 3023600 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 578FE 48458 APPROXIMATELY AT STA 6-100, LONGERON 40L FOUND EXISTING REPAIR. EXISTING REPAIR AT STA 6-100, LONGERON 40L EVALUATED AN D FOUND NOT CARRIED OUT AS PER SRM 53-20-00 FIG 2 VOL I. REPAIR CARRIED OUT AS PER FEDEX EA 1-5330-112421A - FUSELAGE , PLATES AND SKINS, EXISTING REPAIR AT FUSELAGE STATION 1129 L40L AND L43L - INTERIM. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062600013 20070626 00013 NM 2007 6 26 07FDEA02083 1 20070607 A 5330 ADA3139503 SKIN DOUG MD11 MD11F 3023600 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 578FE 48458 APPROXIMATELY AT STA 6-100, LONGERON 43L FOUND EXISTING REPAIR. EXISTING REPAIR AT STA 6-100, LONGERON 43L EVALUATED AN D FOUND NOT CARRIED OUT AS PER SRM 53-20-00 FIG 2 VOL I. REPAIR CARRIED OUT AS PER FEDEX EA 1-5330-112421A - FUSELAGE , PLATES AND SKIN, EXISTING REPAIR AT FUSELAGE STATION 1129 L40L AND L43L - INTERIM. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062600014 20070626 00014 EU 2007 6 26 07FDEA02187 1 20070619 A 5340 A53773644 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 CORNER FITTING C27 LT/RT WITH CORROSION REPAIR PERFORMED BY REPLACEMENT OF PARTS (P/N A537-73644-202 AND A537-73644-203) IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007062600019 20070626 00019 EU 2007 6 26 07FDEA02193 1 20070619 A 5320 BEA14101861 BEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 FWD CARGO DOOR, CORROSION ON SILL BEAM AND AROUND SEVERAL FASTENER HOLES FOUND. REPAIR PERFORMED BY REWORK AND INSTALLI NG REPAIR ANGLE IAW EA 6-5313-103279 AND RAS/DABRE/7006910/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007062600022 20070626 00022 NM 2007 6 26 07FDEA02196 1 20070619 A 5313 BAC1498131 STRINGER BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LOWER FUSELAGE STA 1082 STR 30 HAS CORROSION ON LOWER SURFACE OF STRINGER AT CUT OUT FOR SKIN. REMOVED DAMAGED SECTION OF OF STRINGER 30, AT STA 1082 AND REPAIRED REF SRM 53-10-30 FIG 1. 2 L 7 3 4F RT A3WE 2007062600024 20070626 00024 NM 2007 6 26 07FDEA02198 1 20070619 A 5347 ACA7106505 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 MAIN DECK, SEAT TRACK AT STA 755, X= -27 FOUND CRACK AT LOWER SURFACE. [06-29-07] REPAIR CARRIED OUT AS PER SRM 53-70- 00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062600025 20070626 00025 NM 2007 6 26 07FDEA02199 1 20070619 A 5340 6944555 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT PIT STA 950E STR 29L STRINGER CLIP/FLOOR SUPPORT ANGLE CORRODED. REMOVED AND REPLACED FLOOR SUPPORT ANGLE REF SRM 5 1-30-2. 2 L 7 3 4F RT A3WE 2007062600028 20070626 00028 EU 2007 6 26 07FDEA02202 1 20070514 A 5100 A57970215 FLAP AIRBUS 310 A310222 3930315 EU ZONE 600 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON THE RT UPPER WING SURFACE T/E OF INBOARD FLAP WS 0 TO WS 67. REPAIR REQUIRES MAJOR/MIN OR EVALUATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR WAS ACCOMPLISHED PER SRM 57-52-12 FIG 204. 2 L 7 2 4F RT A35EU 2007062600029 20070626 00029 EU 2007 6 26 07FDEA02203 1 20070515 A 5230 A52374263210 SKIN AIRBUS 310 A310222 3930315 EU ZONE 800 CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 452FE 313 AFT COMPARTMENT CARGO DOOR WITH INTERIOR SKIN SURFACE CRACKED AT TOP, CLOSE TO FR 62A HEAD. SKIN REPAIRED IN ACCORDANCE WITH FEDEX EA 6-5230-112412. 2 L 7 2 4F RT A35EU 2007062600033 20070626 00033 EU 2007 6 26 07FDEA02207 1 20070523 A 5512 A55178630000 PANEL AIRBUS 310 A310222 3930315 EU ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 THS PNL 331BB WITH CRACK AT RIB NR 4, P/N A55178014-004. REPAIRED IN ACCORDANCE WITH FEDEX EA 6-5510-112411. 2 L 7 2 4F RT A35EU 2007062600034 20070626 00034 EU 2007 6 26 07FDEA02208 1 20070523 A 5512 A55178630000 PANEL AIRBUS 310 A310222 3930315 EU ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 THS PANEL 331BB WITH CRACK AT RIB NR 3 P/N A55178013-004. REPAIRED IN ACCORDANCE WITH FEDEX EA 6-5510-112411. 2 L 7 2 4F RT A35EU 2007062600035 20070626 00035 NM 2007 6 26 07FDEA02209 1 20070619 A 5220 50797890 DOOR BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LEFT AFT EMERGENCY EXIT HATCH INTERIOR STRUCTURE ATTACH ANGLE AT FWD LWR CORNER OF WINDOW FRAME CORRODED REMOVED OLD ANG LE AT FWD CORNER OF WINDOW FRAME AND FABRICATED AND INSTALLED A NEW ANGLE USING 7075-T-6 .071". ORIGINAL THICKNESS WAS .071" CALIPER GAUGE NR 18238, REF SRM 52-20-1 AND 51-30-1. 2 L 7 3 4F RT A3WE 2007062600038 20070626 00038 NM 2007 6 26 07FDEA02212 1 20070619 A 5314 BAC15061464 KEELBEAM BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT PIT STA 950E-950F STR 29L KEEL BEAM CORRODED REMOVED CORROSION, REMOVED .052" MAXIMUM DEPTH ON KEEL BEAM BETWEEN STA 950E AND 950F IS OUT OF LIMITS. SPOT FACED KEEL BEAM AROUND FASTENER HOLES. FABRICATED REPAIR STRAP, FABRICATED FILLER WASHER AND INSTALLED REPAIR PARTS. REF FED EX STANDARD REWORK DRAWING, LT AND RT KEEL BEAM FLANGE CORROSION, DRAWING N UMBER SR27-53-023A. 2 L 7 3 4F RT A3WE 2007062600040 20070626 00040 EU 2007 6 26 NWAA072173247 1 20070616 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320212 3930322 EU EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 347NW 720 720 408 EMERGENCY ESCAPE LIGHTING, EPSU 13WL INOP. REPLACED EPSU 13WL AND BATTERY, CHECKS GOOD. 2 L 7 2 4F RT A28NM 2007062600041 20070626 00041 NM 2007 6 26 NWAA072183146 1 20070617 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319114 3930350 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 346NB 13712 13712 1796 EMERGENCY ESCAPE LIGHTING, EPSU INT LOAD EMER L DISPLAYED ON FORWARD CIDS PANEL. REPLACED LEFT OVERWING EPSU POWER SUPP LY AND BATTERY, CHECKS GOOD. 2 L 7 2 4F RT A28NM 2007062600046 20070626 00046 NM 2007 6 26 AWXA200700740 1 20070419 A 5311 65465262 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - FOUND CRACKED FRAME, BS 400, S9L. REPAIRED FRAME, BS 400, S9L IAW AWA ER 03-5362-07165-ES1. 2 L 7 2 4F RT A16WE 2007062600048 20070626 00048 NM 2007 6 26 AWXA200700742 1 20070419 A 5311 65465292 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - FOUND CRACKED FRAME, BS 440, S9L AND S9R. REPAIRED FRAME, BS 440, S9L AND S9R IAW AWA ER 03-5362-07165-ES1. 2 L 7 2 4F RT A16WE 2007062600052 20070626 00052 NM 2007 6 26 AWXA200700746 1 20070422 A 5320 65479573 WEB BOEING 737 73733A 1384673 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - CORROSION ON AFT CARGO COMPARTMENT DOOR CUT OUT LOWER WEB, BS 795 - BS 847, S25R. REPLACED AFT CAR GO COMPARTMENT DOOR CUT OUT LOWER WEB, BS 795 - BS 847, S25R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007062600053 20070626 00053 NM 2007 6 26 AWXA200700747 1 20070530 A 5320 146N542510 INTERCOSTAL BOEING 757 757225 1384959 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 MCN - FOUND CORROSION ON AFT CARGO COMPARTMENT INTERCOSTAL, BS 1420, S28L. REPLACED AFT CARGO COMPARTMENT INTERCOSTAL, BS 1420, S28L IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007062600054 20070626 00054 NM 2007 6 26 AWXA200700748 1 20070527 A 5754 114N407729 SKIN BOEING 757 757225 1384959 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 MCN - MAJOR REPAIR - LEFT WING NR 3 SLAT INNER COVE SKIN CRACKED, SS 471.30 - SS 483.30. REPLACED LEFT WING NR 3 SLAT I NNER COVE SKIN, SS 471.30 - SS 483.30 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007062600055 20070626 00055 NM 2007 6 26 AWXA200700749 1 20070617 A 3350 P4010021 POWER SUPPLY BOEING 757 757225 1384959 NM ZONE 200 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 913AW 22207 MCN - EEL - RIGHT AFT MID LAV EMERGENCY FLASHLIGHT BATTERY IS DISCHARGED. REPLACED RIGHT AFT MID LAV EMERGENCY FLASHLIG HT POWER SUPPLY. 2 L 7 2 4F RT A2NM 2007062600056 20070626 00056 NM 2007 6 26 AALA20071041 1 20070607 A 3350 BATTERY BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 176AA 32395 MIA - EMERGENCY LIGHTS AT SEAT ROWS 16 TO 25 INOPERATIVE. CHARGED BATTERY FOR EMERGENCY LIGHT SYSTEM FOR EMERGENCY LIGH TS AT SEAT ROWS 16 TO 25. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007062600057 20070626 00057 EU 2007 6 26 AALA20071044 1 20070608 A 2130 VALVE AIRBUS 300 A300B4605R 3930308 EU AIR CONDITIONING LEAKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 19059 469 JFK INFLIGHT T1889/08JUN - DURING CLIMB AIRCRAFT FILLED WITH SMOKE. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. FOUN D OIL COOLER REGULATOR VALVE LEAKING. REPLACED OIL COOLER REGULATOR VALVE AND PACKING. REPLACED BOTH PACK COALESCER BA GS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007062600058 20070626 00058 NM 2007 6 26 AALA20071042 1 20070607 A 3350 BATTERY BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 176AA 32395 MIA - EMERGENCY LIGHTS IN FIRST CLASS CABIN INOPERATIVE. CHARGED BATTERY FOR EMERGENCY LIGHT SYSTEM FOR EMERGENCY LIGHT S IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007062600060 20070626 00060 WP 2007 6 26 AALA20071024 1 20070605 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9681B 53631 SFO - EMERGENCY LIGHTS AT SEAT ROW 15 INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHTS AT SEAT ROW 15. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007062600061 20070626 00061 NM 2007 6 26 AALA20071012 1 20070602 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 789AN 30252 DFW - EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT T00001SE 2007062600066 20070626 00066 NM 2007 6 26 AALA20071037 1 20070607 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 JFK - SEAT MOUNTED EMERGENCY LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK M33094 AT RIGHT NUMBER ONE DOOR FOR EMERGENCY LIGHTS IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007062600067 20070626 00067 EU 2007 6 26 AALA20071040 1 20070607 A 2560 FLASHLIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14068 511 MIA - EMERGENCY FLASHLIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007062600068 20070626 00068 WP 2007 6 26 AALA20071030 1 20070607 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 249AA 49269 LGA - EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS CABI N. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007062600069 20070626 00069 NM 2007 6 26 AALA20071031 1 20070606 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 649AA 24607 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT LEFT NUMBER ONE DOOR. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007062600070 20070626 00070 NM 2007 6 26 AALA20071039 1 20070607 A 2560 STRAP BOEING 767 767323 1385205 NM FLASHLIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 392AN 29429 MIA - EMERGENCY FLASHLIGHT AT RIGHT MID GALLEY FLIGHT ATTENDANT SEAT HAS BROKEN STRAP. REPLACED STRAP FOR EMERGENCY FL ASHLIGHT AT RIGHT MID GALLEY FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007062600071 20070626 00071 NM 2007 6 26 AALA20071035 1 20070607 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 650AA 24608 DFW - EMERGENCY EXIT SIGN LIGHT IN CABIN INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT SIGN LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007062600073 20070626 00073 WP 2007 6 26 AALA20071038 1 20070607 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 110HM 49787 DFW - EMERGENCY LIGHTS AT OVERHEAD AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK IN OVERHEAD STORAGE COMPARTMENT FOR EM ERGENCY LIGHTS AT OVERHEAD AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007062600075 20070626 00075 WP 2007 6 26 AALA20071028 1 20070606 A 2822 3980001 PUMP DOUG DC9 DC983 3022083 WP FUEL BOOST INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 983TW 53633 DFW - INFLIGHT T2430/06JUN - RIGHT AC BUSS AND AFT CENTER FUEL BOOST PUMP CIRCUIT BREAKERS POPPED IN FLIGHT. RETURNED D FW AND LANDED OVERWEIGHT WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE FOR EVALUATION. REPLACED CENTER BOOST PUMP AN D HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007062600079 20070626 00079 WP 2007 6 26 AALA20071029 1 20070607 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 249AA 49269 LGA - EMERGENCY LIGHTS AT AFT RIGHT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT RIGHT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007062600082 20070626 00082 WP 2007 6 26 AALA20071020 1 20070605 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9615W 53562 LGA - OVERHEAD EMERGENCY LIGHTS AT SEAT ROWS 29 TO 32 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT SEAT ROWS 29 TO 32. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007062600083 20070626 00083 WP 2007 6 26 AALA20071014 1 20070603 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 274AA 49271 SFO - EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F A6WE 2007062600087 20070626 00087 NM 2007 6 26 AALA20071007 1 20070601 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 782AN 30003 MIA - EMERGENCY LIGHT IN CEILING ABOVE SEAT 22C INOPERATIVE. RELAMPED EMERGENCY LIGHT IN CEILING ABOVE SEAT 22C. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007062600092 20070626 00092 SO 2007 6 26 SIMA200717505 1 20070621 A 2150 A/C PACK EMB 145 EMB145LR 3260212 SO ODOR A SIMA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 635AE 145158 BURNING SMELL FROM PACKS WITH NO SMOKE. INSPECTED AND FOUND APU INTAKE SCREEN COVERED WITH CICADAS. REMOVED CICADAS. PERFORMED OPERATIONAL CHECK OF PACK SYSTEM WITH NO BURNING SMELL NOTED. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007062600094 20070626 00094 2007 6 26 F3LA200700138 4 20070610 A 2565 D5311253400000 NUT PLATE AIRBUS A319 A319112 3930323 EU GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 907FR 5061 1743 DURING C4/S1 CHECK, INSPECTION REPORTED R1 GIRT BAR FITTING NUT PLATE ASSY CORRODED, FWD AND AFT. REPLACED FWD AND AFT GIRT BAR FITTINGS AND NUT PLATE ASSEMBLIES IAW SRM 51-42-11, PAGE 44, STEP 7D AND PARA 7. 2 L 7 2 4F RT A28NM 2007062600095 20070626 00095 EU 2007 6 26 DHL2007363001 1 20070624 A 5330 TRIPLER AIRBUS 300 A300B4203 3930306 EU FUSLEAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING A WEEKEND CHECK AT AVBOURNE HEAVY MX, THE FOLLOWING DISCREPANCIES WERE NOTED; TRIPLER DAMAGED ON PREVIOUS REPAIR AT FWD SIDE OF FWD CARGO DOOR CUT-OUT, FROM STR 39R AT FRAME 20A. REMOVED AND REPLACED FWD CARGO DOOR CUT OUT TRIPLER I AW A300 SRM 53-13-00 FIG,707 AND APPLIED TOP COAT IAW A300 SRM 51-40-12, FRAME 20A,STR 20 MATL"2024-T3 .025 PO#023128. REPAIR SIZE 5.25 BY 14.24, INSTALLED IAW A300 SRM 51-13-00. 2 L 7 2 4F RT A35EU 2007062600100 20070626 00100 NM 2007 6 26 QXEA200701016 1 20070618 A 2750 C1486601 ACTUATOR BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS INOPERATIVE A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 402QX 15558 15558 4032 PDX - ON FLIGHT 2464, RETURNED TO FIELD, WHEN THE FLAPS WERE RETRACTED AFTER TAKEOFF THEY STOPPED AT 13 DEGREES AND WE G OT A FLAP DRIVE CAUTION LIGHT, AND DID NOT LAND OVERWEIGHT. ALSO KEPT THE AIRSPEED UNDER 172 KNTS. MAINTENANCE REMOVED AND REPLACED LEFT NR 3 AND NR 4 FLAP ACTUATORS AND RIGGED RIGHT OUTBOARD FLAP DRIVE AND ROLLER CARRIAGES. FUNCTIONAL C HECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007062600101 20070626 00101 WP 2007 6 26 AALA20071009 1 20070601 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 245AA 49257 TPA - EMERGENCY EXIT LIGHT ARROW MISSING AT AFT RIGHT CABIN. REPLACED EMERGENCY EXIT LIGHT ARROW AT AFT RIGHT CABIN. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007062600102 20070626 00102 NM 2007 6 26 AALA20071010 1 20070602 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 39367 25194 SFO - EMERGENCY LIGHT AT LAVATORY A5 HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LAVATORY A5. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007062600103 20070626 00103 NM 2007 6 26 AALA20071011 1 20070602 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 789AN 30252 DFW - EMERGENCY LIGHT AT SEAT 25G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 25G. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT T00001SE 2007062600104 20070626 00104 NM 2007 6 26 AALA20071021 1 20070605 A 3350 P2010031303 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 641AA 24599 LGA - EMERGENCY EXIT LIGHT AT AFT RIGHT DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT AFT RIGHT DOOR. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007062600105 20070626 00105 2007 6 26 AALA20071005 4 20070601 A 2565 SLIDE BOEING 767 767323 1385205 NM RT OVERWING UNWANTED DEPLOY A AALA O OTHER W INADEQUATE Q C DE DESCENT 1 SW 21 352AA 24033 DFW INFLIGHT T102/01JUN - RIGHT OVERWING SLIDE DEPLOYED DURING FLIGHT. AIRCRAFT REMOVED FROM SERVICE TO EVALUATE DAMAGE . REPLACED RIGHT OVERWING SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007062600106 20070626 00106 NM 2007 6 26 AWXA200700732 1 20070616 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 804AW 1043 LAS - EEL - EMERGENCY EXIT LIGHTS INOP ROWS 14, 18, AND 22, ALSO L2 AND R2 DOORS. MX REPLACED LT AFT BATTERY AND CHARGE R. OPS CHECKED GOOD PER AMM 33-51-38-401. 2 L 7 2 4F RT A28NM 2007062600107 20070626 00107 NM 2007 6 26 AWXA200700739 1 20070618 A 2560 P2070001214 FLASHLIGHT BOEING 737 7373G7 1384595 NM MAIN CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 303AW 24010 DFW - EEL - FWD FLIGHT ATT EMERG FLASH LIGHT BRACKET BROKEN. MX REPLACED FWD RT EMERGENCY FLASHLIGHT AND BRACKET. OPER ATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2007062600108 20070626 00108 NM 2007 6 26 DHL2007740554 1 20070614 A 5512 SKIN BOEING 727 7272Q9 138448M NM HORIZONTAL STAB DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 LT STAB UPPER SKIN HAS 2 DENTS, LSTAB STA 41.5. REMOVED PANEL 9113 TO GAIN ACCESS IAW B727 SRM 51-30-2, CUT OUT DAMAGED AREA (DIM 33/4" BY 13/4"), FABRICATED REPAIR DOUBLER FROM 2024T3 .050" PO NR 9005049 (DIM 9 1/4" BY 4.5") IAW B727 SRM 55-20-3 FIG 1 AND 55-10-2 FIG 1. TREATED AND PRIMED REPAIR DOUBLER IAW B727 SRM 51-10-2. INSTALLED REPAIR DOUBLER AT L T STAB UPPER SKIN IAW B727 SRM 51-30-2 AND 55-20-3 FIG 1 AND REINSTALLED PANEL 9113 IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007062600110 20070626 00110 NM 2007 6 26 DHL2007742004 1 20070620 A 5322 SHEAR TIE BOEING 727 727225 1384077 NM BS 480 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 DURING AN "A" CHECK THE FOLLOWING DISCREPANCIES WERE NOTED: FUSELAGE INTERIOR FRAME AT BS 480 AND STR 17L FRAME SHEAR TI E CRACKED (NDT) FINDING. REMOVED FASTENERS AT SHEAR TIE AND CUT OUT CRACKED SECTION (2" BY 8") OF SHEAR TIE IAW B727 SR M 53-10-4 FIG 11. FABRICATED NEW SECTION, MATL 7075-T6,PO.9004940 (6" BY 8") IAW B727 SRM 53-10-2 FIG 3 AND 53-10-4 FIG 11. TREATED AND PRIMED REPAIR PART IAW B727 SRM 51-10-2. INSTALLED REPAIR PART IAW B 727 SRM 53-10-4 FIG 11. 2 L 7 3 4F A3WE 2007062600113 20070626 00113 WP 2007 6 26 DHL2007803537 1 20070612 A 5730 5611002502 SKIN DOUG DC8 DC873 302199C WP RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 RT WING T/E UPPER PANEL SKIN DELAMINATED (STA XW 0.000 - 47.000). REMOVED DELAMINATED PANEL IAW SRM 51-3-0. CLEANED, T REATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PANEL IAW SRM 51-3-0, SRM 51-3-1 PG 2A (TORQUE). 2 L 7 4 4F RT 4A25 2007062600115 20070626 00115 WP 2007 6 26 DHL2007803544 1 20070605 A 5100 NONE DOUG DC8 DC873 302199C WP NONE NONE A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 803DH 46123 PERFORM MODIFICATION REPAIR TO THE L2 DOOR, FWD, LOWER CORNER IAW AD2000-20-08, S/B 53-075 AND SR08530021. MAKE ENTRY I N AIRCRAFT LOGBOOK AND PERMANENT RECORD (337 FORM) MAJOR REPAIR (AMOC). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATE D 05-22-07, BOEING MESSAGE NR 1-329921676-5, 1-329921676-6 DATED 05-22-07 (SKETCH JCT04174) AD2000-20-08, S/B DC8 53-075 , DOUGLAS DWG SR08530021, 5750776. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECT ION IAW SKETCH JCT04174. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 08-00-02 TO 07. NO CRACK NOR CORROSION FOUND. ENCLOSED SMN FORM 242-4. FABRICATED REPAIR DOUBLER (AL7075T6 0.090") REPAIR TRIPLER (AL7075T6 0.125") 2 FILLER (AL7075T 2 L 7 4 4F RT 4A25 2007062600116 20070626 00116 WP 2007 6 26 DHL2007803538 1 20070610 A 5414 SKIN DOUG DC8 DC873 302199C WP NOSE COWL WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 NR 3 ENG NOSE COWL EXTERNAL SKIN WORN (STA YN 147.534, AT 12 O'CLOCK POS) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN SEGMENT (AL2024T3 0. 080") AND STEEL SPLICE (17-7 PH 0.050") IAW SRM 71-5-2 FIG 2 SHEET 1, 2 ,3. HEAT TREATED SPLICE FROM 17-7 PH CRESS TO 1 7.7 PH CRESS (H1050) IAW SRM 51-1-6. CLEANED, TREATED AND PRIMED AREA AND SKIN IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 71-5-2 FIG 2 SHEET 1, 2, 3, SRM 51-1-21A. 2 L 7 4 4F RT 4A25 2007062600117 20070626 00117 WP 2007 6 26 DHL2007803540 1 20070610 A 5414 SKIN DOUG DC8 DC873 302199C WP NOSE COWL WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 NR 4 ENG NOSE COWL EXT SKIN WORN (STA YN 147.000 - 157.000 AT 12 O'CLOCK POS LT/RT) MAJOR REPAIR. PERFORMED MAJOR REPAI R IAW SRM 71-5-2 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN SEGMENT (A L2024T3 0.080") AND SPLICE (STEEL 17-7 PH CR 50") IAW SRM 71-5-2 FIG 2 SHEET 1, 2, 3. HEAT TREATED SPLICE FROM 17-7 PH CRESS TO 17-7 PH CRESS (H1050) IAW SRM 51-1-16. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN IAW SRM 51-1-8B. INSTALL ED REPAIR PARTS IAW SRM 71-5-2 FIG 2, SHEET 1, 2, 3, SRM 51-1-11, SRM 51-1-21A. 2 L 7 4 4F RT 4A25 2007062600118 20070626 00118 WP 2007 6 26 DHL2007803541 1 20070610 A 5414 SKIN DOUG DC8 DC873 302199C WP NACELLE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 NR 1 ENG NACELLE INLET COWL UPPER SIDE WORN, STA YN 147.534 AT 12 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FI G 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED AREA AND FABRICATED NEW SKIN SEGMENT (AL2024T3 0.080") AND ST EEL SPLICE 17-7PH 0.050" IAW SRM 71-5-2 FIG 2 SHEET 1, 2, 3. HEAT TREATED SPLICE FROM 17-7 PH CRESS TO 17-7 PH CRESS (H 1050) IAW SRM 51-1-6. CLEANED, TREATED AND PRIMED AREA AND SKIN IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 71-5-2 FIG 2 SHEET 1, 2, 3, SRM 51-1-11, SRM 51-1-21A. 2 L 7 4 4F RT 4A25 2007062600121 20070626 00121 WP 2007 6 26 DHL2007803542 1 20070610 A 5100 NONE DOUG DC8 DC873 302199C WP NONE NONE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 REMOVE REPAIR BELOW CARGO DOOR AT STA 176 AND INSPECT AREA. INSTALL A NEW REPAIR IAW SRM (PERMANENT) OR APPROVED DATA. ENTER INFORMATION ON 337 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-06-07, DWG NR AD42-53-11 REV IR DATED 06-01-07. REMOVED EXISTING INTERIM REPAIRS IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FAB RICATED REPAIR DOUBLER (AL7075T6 0.063") REPAIR TRIPLER (AL7075T6 0.071") 6 INTERNAL FINGER DOUBLER (AL7075T6 0.040") AN D FILLER (AL7075T6 0.063") IAW DWG NR AD42-53-111. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS (STA 156.000 - 176.000 L-22L TO L-23L) IAW DWG NR AD42-53-111, SRM 51-1-21, SRM 51-1-20D, SRM 51- 2 L 7 4 4F RT 4A25 2007062600122 20070626 00122 WP 2007 6 26 DHL2007803532 1 20070606 A 5200 ACCESS DOOR DOUG DC8 DC873 302199C WP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 LT FUS NOSE SECTION ACS MODIFICATION DOUBLER AT UPPER AFT JAMB CORNER OF HEAT EXCHANGER ACCESS DOOR, CRACKED 0.250" STA -12.000 L-24L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-04-07, DWG NR AD42-53-103 REV IR DATE D 05-16-07. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER (AL2024T3 0.050") REPAIR TRIPLER (AL2024T3 0.063") AND FILLER (2024T3 0.100") IAW DWG# AD42-53-103. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DWG NR AD42-53-103, SRM 51-1-11, SRM 51-1-21, SRM 51-3-0, SRM 51-1-20, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007062600123 20070626 00123 WP 2007 6 26 DHL2007803531 1 20070606 A 5313 LONGERON DOUG DC8 DC873 302199C WP DAMAGED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 803DH 83934 46123 FUS NOSE SECTION LONGERON HAS A MISDRILLED HOLE AT STA -32.000 L-17R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FOR M 8110-3 DATED 06-04-07, DWG NR AD42-53-109 REV IR DATED 05-25-07. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED REINF ORCEMENT (AL7075T6 511 0.063") IAW DWG NR AD42-53-109. CLEANED, TREATED AND PRIMED AREA AND REINFORCEMENT IAW SRM 51-1- 8B. INSTALLED REINFORCEMENT IAW DWG NR AD42-53-109, SRM 51-1-11, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007062600127 20070626 00127 NM 2007 6 26 DHL2007740556 1 20070612 A 5320 INTERCOSTAL BOEING 727 7272Q9 138448M NM BS 1183 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 LT PRESSURE BULKHEAD BS 1183 INTERCOSTAL CRACKED, LBL 63.0, WL 257.0. REMOVED INTERCOSTAL, CUT OUT DAMAGE, 2.125" BY 1. 5". FABRICATED 2 EA DOUBLERS FROM 7075-T6; DBLR 1 .071" BY 6" BY 4.75"/DBLR 2 .071" BY 6" BY 4", PO NR 9004940; FABRIC ATED FILLER FROM 7075-T6, .080" BY 2.125" BY 1.5", PO NR 9004670, PER B727 SRM 51-40-4 FIG 3, AND 53-10-2 FIG 5. TREATE D, PRIMED, INSTALLED REPAIR PARTS TO INTERCOSTAL, AND REINSTALLED INTERCOSTAL PER B727 SRM 51-10-2, 51-40-4 FIG 3, AND 5 1-30-2. 2 L 7 3 4F RT A3WE 2007062600129 20070626 00129 NM 2007 6 26 DHL2007742007 1 20070620 A 5320 SPLICE PLATE BOEING 727 727225 1384077 NM BS 640-660 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 DURING AN "A" CHECK AT FLIGHTSTAR AIRCRAFT SERVICES THE FOLLOWING DISCREPANCIES WERE NOTED; MCD LOWER SILL BEAM AT BS 64 0 AND 660, SPLICE PLATES ARE CRACKED AT SLOT RADIUS (2 EA.) NDT FINDING. REMOVED LOCK FITTING AND SPLICE PLATES AT BS 6 40 AND 660 IAW B727 SRM 51-30-2 FIG 7 AND 15. FABRICATED NEW PLATES USING 2024-T3 .125,PO.645745 DIM 16" BY 7" TWO EACH IAW BOEING DWG NR AE 727-1-042. TREATED AND PRIMED PARTS IAW B 727 SRM 51-10-2. INSTALLED FITTINGS AND SPLICE PLATES IAW B DWG NR AE 727-3-004. 2 L 7 3 4F A3WE 2007062600130 20070626 00130 NM 2007 6 26 DHL2007742008 1 20070620 A 5320 SPLICE PLATE BOEING 727 727225 1384077 NM BS 640-660 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 DURING AN "A" CHECK AT FLIGHTSTAR AIRCRAFT SERVICES THE FOLLOWING DISCREPANCIES WERE NOTED, MCD LOWER SILL BEAM AT BS 60 0 AND 620, SPLICE PLATES ARE CRACKED AT SLOT RADIUS (2 EA.) NDT FINDING. REMOVED LOCK FITTING AND SPLICE PLATES AT BS 6 40 AND 660 IAW B727 SRM 51-30-2 FIG 7 AND 15. FABRICATED NEW PLATES USING 2024-T3 .125,PO.645745 DIM 16" BY 7" TWO EACH IAW BOEING DWG NR AE 727-1-042. TREATED AND PRIMED PARTS IAW B 727 SRM 51-10-2. INSTALLED FITTINGS AND SPLICE PLATES IAW B DWG NR AE 727-3-004. 2 L 7 3 4F A3WE 2007062600133 20070626 00133 EU 2007 6 26 TRBA2007039 1 20070618 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS FAILED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 431AT 431 DURING PS-2 CK, FOUND CABIN RT AFT UPPER/LOWER SIGNS DOES NOT ILLUMINATE. ALSO, CABIN LT FWD SIGN DOES NOT ILLUMINATE. REMOVED AND REPLACED RT AFT EMERGENCY LIGHT POWER SUPPLY AND LT FWD EMERGENCY LIGHT POWER SUPPLY IAW JIC NR 33-51-21. OP CK OK. 2 H 7 2 4T RT A53EU 2007062600135 20070626 00135 NM 2007 6 26 CALA0700306 1 20070615 A 5340 507946117 ATTACH ANGLE BOEING 737 7373T0 1384582 NM BS 294 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12313 23364 INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL CLIP AT STA 294.5, S10L. THE CLIP WAS REPLACED AND A DIP WAS INITIATED TO INSPECT THE REPAIR AT INTERVALS NOT TO EXCEED 6000 FLIGHT CYCLES IAW ECRA 5311-01330. 2 L 7 2 4F RT A16WE 2007062200009 20070622 00009 NM 2007 6 22 2007UALA01996 1 20070613 A 5755 PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 8 SPOILER WARPED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 RT WING, NR 8 SPOILER PANEL HAS EXCESSIVE WARP ON TRAILING EDGE. [08-07-07] REPLACED TRAILING EDGE SPOILER PANEL. ADJUSTED NR 8 SPOILER GAP AND ADJUSTMENT CHECKED NR 8 PCA RVDT. CHECKED BONDING JUMPER RESISTANCE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062200023 20070622 00023 NM 2007 6 22 SWAA072992 1 20070614 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 456WN 32463 EEPLS COVER MISSING AT ROW 3 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007062200027 20070622 00027 2007 6 22 SWAA072979 4 20070613 A 2565 63551101 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007062200031 20070622 00031 NM 2007 6 22 SWAA073001 1 20070614 A 5315 6545833 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 270 , BL 0. REMOVED AND REPLACED FLOORBEAM CHORD PER SRM. 2 L 7 2 4F RT A16WE 2007062200035 20070622 00035 NM 2007 6 22 SWAA072998 1 20070614 A 5315 6546811 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 729SW 27861 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM WEB CORRODED AT BS 1016, RBL 10. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007062200036 20070622 00036 NM 2007 6 22 SWAA073000 1 20070614 A 5315 6546812 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 729SW 27861 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM WEB CORRODED AT BS 987, LBL 36. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007062200037 20070622 00037 NM 2007 6 22 SWAA072997 1 20070614 A 5315 6546816 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 729SW 27861 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM WEB CORRODED AT BS 1001, RBL 38. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007062200063 20070622 00063 NM 2007 6 22 SWAA072987 1 20070614 A 5523 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED BRDG CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BEARING AND BUS HING PER MM. 2 L 7 2 4F RT A16WE 2007062200067 20070622 00067 WP 2007 6 22 NWAA072159957 1 20070512 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING "H" CHECK, FOUND CRACK IN LT FUSELAGE SKIN AT THE UPPER FORWARD CORNER OF FORWARD PASSENGER DOOR JAMB. REPAIRED PER EA 99-209571. 2 L 7 2 4F A6WE 2007062200073 20070622 00073 NM 2007 6 22 QXEA200700960 1 20070609 A 5320 CHANNEL BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - RIGHT AFT SERVICE DOOR EDGE CHANNEL CORRODED. REPAIRED IAW SRM 51-21-10, 51-25-10, 51-42-15. 2 H 7 2 4T RT A13NM 2007062200087 20070622 00087 NM 2007 6 22 DL76S070707 1 20070611 A 5315 FLOORBEAM BOEING 767 767332 1382001 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 CABIN BS 287 , RBL 24-26 FLOORBEAM UPPER CHORD FOUND CORRODED AS MARKED, REPAIRED PER 53-00-51D FIG 201 ON NR AJN50902. 2 L 7 2 4F RT A1NM 2007062200106 20070622 00106 EU 2007 6 22 AWXA200700724 1 20070613 A 5347 D53230464200 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 637AW 099 SAL - FOUND CORROSIONS ON CABIN SEAT TRACK, FR 30+19" AND FR 33+15", +Y765. REPAIRED CABIN SEAT TRACK, FR 30+19" AND F R 33+15", +Y765 IAW A320 SRM 53-00-15 PAGE 205-206 AND 51-21-11. 2 L 7 2 4F RT A28NM 2007062200114 20070622 00114 NM 2007 6 22 HALA0700251 1 20070613 A 5414 SKIN BOEING 717 717200 1383700 NM LT PYLON CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 ON NR 1 ENGINE CHANGE, LT PYLON APRON LOWER AFT LATCH CUTOUT HAS 2 CRACKS. REPAIRED NR 1 ENGINE LOWER AFT LATCH CRACKS PER HAL M105 B10192. 2 L 7 2 4F TR A6WE 2007062200118 20070622 00118 NM 2007 6 22 AWXA200700721 1 20070611 A 2611 RAL2800M0706 SMOKE DETECTOR AIRBUS A319 A319132 3930340 NM CARGO BAY FAILED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 830AW 22832 529 1565 PHX - EE - SMOKE LAV CARGO DET FAULTED. MX REPLACED THE CARGO SMOKE DETECTOR. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007062200134 20070622 00134 WP 2007 6 22 ASMF200706003 1 20070611 A 4920 38003681 APU DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FAILED W ASMF K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 23 838AM 2566 49397 CAPTAIN REPORTED SMOKE ON AFT LAVATORIES. AT PLATFORM, MAINTENANCE PERSONNEL PERFORMED A TURBINE COOLING SYSTEM CHECK, D ETERMINING TO REPLACE THE WATER SEPARATOR OF LT AIR CONDITIONING SYSTEM IAW MM 21-20-01; SO AIRCRAFT WAS SENT TO THE HAN GAR AND DURING OVERNIGHT CHECK, THE HEAT EXCHANGERS OF BOTH AIR CONDITIONING SYSTEMS AND COOLING TURBINE WERE CHECKED, A LL CORRECT. APU WAS REPLACED IAW 49-10-00; DUCTS OF BOTH AIR CONDITIONING SYSTEM WERE CLEANED IAW MPCM 21-30-00 AND WATE R SEPARATORS WERE REPLACED IAW MM 21-20-02, TESTED CORRECT IAW MM 21-00-00. 2 L 7 2 4F 4 F RT A6WE E9NE 2007062200137 20070622 00137 NM 2007 6 22 DHL2007740534 1 20070616 A 5347 BAC15207927178 SEAT TRACK BOEING 727 7272Q9 138448M NM FUSELAGE BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 WHILE AT C CHECK REF N/RS 053820,054017, MAIN CABIN SEAT TRACK HAS BROKEN CUT OUT AT STA 950+12 LBL45. FOUND OUT OF LIM ITS IAW B727 SRM 53-10-1 FIGURE 3. REMOVED FLOOR BOARDS FROM 950 TO BS 1030 BETWEEN LBL22 AND LBL 65 AND SIDE GUIDES FR OM BS 870 TO BS 1010 LT SIDE IAW B727 SRM 51-30-2 TO GAIN ACCESS CUT-OUT AND REMOVED SEAT TRACK SECTION FROM BS 950 TO B S 1030 FABRICATED NEW TRACK SECTION FROM BAC 1520-792 7178-T6 PO NR 6003797 DI 80" LENGTH STRAP REPAIR FROM 7075-T6 .250 " PO NR 90031467 DIM 8" BY 2" AND REPAIR ANGLES FROM BAC 1503-100122 7178-T6 PO NR 9005138 DIM 13" BY 2 1/2"EACH IAW B72 7 SRM 53-10-5 FIG1. TREATED AND PRIMED ALL REPAIR PARTS IAW B727 51-10-2. INSTALLED NEW SEAT TRACK AND PARTS IAW B727 2 L 7 3 4F RT A3WE 2007062200145 20070622 00145 NM 2007 6 22 PCSA21820071 1 20070218 A 3230 651951718 UPLOCK BOEING 727 727233 138408A NM RT MLG CRACKED A PCSA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 29 994AJ 20942 FLIGHT 8714 WHILE ON TAXI FROM THE GATE AT SAP THE CREW REPORTED THAT THE RIGHT MAIN LANDING GEAR UNSAFE RED LIGHT ILLUM INATED AND WARNING HORN SOUNDED. THE AIRCRAFT RETURNED TO THE GATE WITHOUT ANY FURTHER INCIDENT. MAINTENANCE TROUBLESH OOT THE INDICATION PROBLEM AND FOUND THE RIGHT HAND MAIN LANDING GEAR SEGMENT ASSY UPLOCK CRACKED. THE CRACKED RIGHT HA ND MAIN LANDING GEAR SEGMENT ASSY UPLOCK IS IN THE PROCESS OF BEING REPLACED. THE UPLOCK WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F RT A3WE 2007062200149 20070622 00149 NM 2007 6 22 BB07042 1 20070615 A 2560 BRACKET BOEING 757 7572B7 1384964 NM L4 DOOR DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 200UU 27809 MAINTENANCE FOUND GIRT BAR ENGAGEMENT LIGHT EXTINGUISHED WITH THE EVACUATION SLIDE ARMING LEVER IN THE ARMED POSITION AT DOOR 4L. FOUND GIRT BAR WOULD NOT ENGAGE DUE TO WORN/MISSING PARTS ON DOOR MECHANISM. REPAIRED BRACKET FOR GIRT BAR. NO FURTHER FAULTS NOTED. 2 L 7 2 4F RT A2NM 2007062200160 20070622 00160 EA 2007 6 22 TRAX200700839 1 20070614 A 5220 COVER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 751EV 10163 RIGHT EMERGENCY EXIT DOOR UPPER HANDLE COVER IS CRACKED. 2 L 7 2 4F RT A21EA 2007062200161 20070622 00161 NM 2007 6 22 DHL2007783510 1 20070602 A 5330 2024T3 DOUBLER BOEING 727 727227 1384078 NM FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 FUSELAGE TO LT WING LE BS 720E, WBL 70.5, PREVIOUS REPAIR DOUBLER SHOW WORN OUT PATH, CHAFING WITH INBD L/E LEFT. REMOV ED PREVIOUS REPAIR DOUBLER IAW B727 SRM 51-30-2. FABRICATED REPAIR DOUBLER FROM .040, 2024T3, 35.25 BY 14 IAW US AIR EA 7357. TREATED, PRIMED AND INSTALLED IAW B727 SRM 51-10-2 AND US AIR EA 7357. 2 L 7 3 4F A3WE 2007062200177 20070622 00177 EA 2007 6 22 HNAA0700117 1 20070615 A 3222 88211 CYLINDER DHAV DHC8 DHC8311 1386006 EA NLG CORRODED A HNAA K NONE O OTHER CR CRUISE 1 EA 07 333EN 221 NLG INNER CYLINDER LOWER BORE CORRODED. REMOVED AND REPLACED NLG INNER CYLINDER WITH NEW BEARING AND THRUST SET 8821-1 IAW CMM 32-20-01 NLG STRUT S/N DCL291/90. 2 H 7 2 4T RT A13NM 2007062200179 20070622 00179 NM 2007 6 22 USAA070468 1 20070618 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 BS 796 S-25R, SKIN CREASE. INSTALLED DOUBLER PER EA 98668, DEFECT SIZE: 3 INCHES. 2 L 7 2 4F RT A16WE 2007062200180 20070622 00180 NM 2007 6 22 USAA070467 1 20070618 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 BS 328, LBL 28 - RBL 53, T-CAP CORRODED AT FASTENER HOLES. T-CAP OF FLOORBEAM REPAIR INSTALLED PER SRM 53-10-51; CORR T ASK C53-107-01; LEVEL 2, DEFECT SIZE: .25 X .25 INCH. 2 L 7 2 4F RT A16WE 2007062200183 20070622 00183 NM 2007 6 22 AWXA200700737 1 20070617 A 3350 BPS73 POWER SUPPLY BOEING 737 73733A 1384673 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 175AW 23634 MCN - EEL - POWER SUPPLY FOR EMERGENCY EXIT SIGN BATTERY INOP AT LT WING EMERGENCY EXIT. REPLACED POWER SUPPLY FOR EME RGENCY EXIT SIGN BATTERY AT LT WING EMERGENCY EXIT IAW B737-300 AMM 33-51-51-2. 2 L 7 2 4F RT A16WE 2007062200191 20070622 00191 NM 2007 6 22 SWAA073018 1 20070615 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007062500005 20070625 00005 SW 2007 6 25 HEEA115806 1 20070605 A 2821 222366621103 FUEL FILTER BELL 407 407 1182206 SW UNKNOWN B HEEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 09 721PH 53278 FUEL FILTER LIGHT ILLUMINATED IN FLIGHT. LANDED AT NEXT MOST PRACTICAL LANDING AREA. MAINTENANCE REPLACED FUEL FILTER ASSY. 1 G 7 1 3U O H2SW 2007062500010 20070625 00010 SO 2007 6 25 414506122007 1 20070611 A 2150 570072OA HOSE PIPER PA28 PA28181 7102807 SO A/C PACK LOOSE E QMLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 03 125L 120 4145 AIRCRAFT MODEL IS A AS 350B2, MANUFACTURE OF AIR CON SYSTEM IS INTERGRATED FLIGHT SYSTEMS - IFS. AFTER MAINTENANCE AND SERVICING THE AIRCRAFT'S AIR CONDITIONER, THE AIRCRAFT WAS LAUNCHED ON AN INTERHOSPITAL TRANSFER MISSION. AFTER APPROXI MATELY 3 MINUTES ENROUTE THE AIRCRAFT INTERIOR WAS FILLED WITH A FOG LIKE SUBSTANCE. THE CREW ABORTED THE MISSION, PERF ORMED THE SMOKE AND FUME ELIMINATION PROCEDURES, RETURNED TO THE BASE HOSPITAL, AND MADE AN UNEVENTFUL LANDING. UPON POS TFLIGHT, IT WAS DISCOVERED THAT A REFRIGERANT LINE ON THE AIR CONDITIONING SYSTEM WAS LOOSE {FROM ORIGINAL INSTALLATION} AND HAD VENTED R134A THROUGH THE ECS SYSTEM INTO THE CABIN. THE AIR CONDITIONER WAS REPAIRED, RESERVICED AND THE AIRCR 1 L 7 1 3O 2A13 2007062500011 20070625 00011 CE 2007 6 25 061307N300CS1 1 20070609 A 3240 MS252531 SWITCH CESSNA 500 550 2076604 CE MLG FAILED E Z5FA O OTHER S AFFECT SYSTEMS LD LANDING 1 EA 63 300CS 5500818 BRAKES FAILED ON LANDING, WITH LOW PRESSURE LIGHT ILLUMINATED AS WELL AS THE ANTI SKID LIGHT ILLUMINATED. EMERGENCY BRAK E HANDLE USED TO STOP AIRCRAFT. 1 L 7 2 4F A22CE 2007062500035 20070625 00035 EU 2007 6 25 TRBA200736 1 20070615 A 5340 MS21905D6 TEE FITTING AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE BROKEN A TRBA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 29 529AM 529 UPON SELECTING L/G UP, THE NOSE AND RT GEAR RETRACTED. THE LT MLG UNLOCKED, HOWEVER IT REMAINED IN THE DOWN POSITION WI TH BOTH INDICATING SYSTEMS DISPLAYING RED UNLK AND GREEN DOWN TRIANGLE SIMULTANEOUSLY. ATC TOWER CONFIRMED THE GEAR APP EARED DOWN. AFTER SLOWING TO 120 KTS, THE GEAR WAS CYCLED DOWN AND THEN RETRACTED NORMALLY. AT THIS TIME FOUND LT MLG PLUMBING TEE FITTING BROKEN. REMOVED AND REPLACED TEE FITTING AS PER MM NR 32-31-50 (FIG 16 ITEM NR 50). PERFORMED EXT ENSION AND RETRACTION AS PER JIC NR 32-31-00 AND FOUND SYSTEM WORKING PROPERLY. 2 H 7 2 4T RT A53EU 2007062500036 20070625 00036 NM 2007 6 25 DHL2007783511 1 20070604 A 5740 BRACKET BOEING 727 727227 1384078 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 NR 2 K-FLAP ACTUATOR SUPPORT ANGLES INBD AND OUTBD ARE CRACKED W/S 235. REMOVED NR 2 K-FLAP ACTUATOR TRUNNION SUPPORT A NGLES INBD AND OUTBD IAW B727 SRM 51-30-2. FABRICATED SUPPORT ANGLES FROM 7075T6, .071, 8.25 BY 6.25 IAW B727 SRM 57-20 -2, FIG 1 AND 51-20-1, FIG 7. TREATED, PRIMED AND INSTALLED PARTS IAW B727 SRM 51-10-2, 51-30-2 AND 57-20-2, FIG 1. 2 L 7 3 4F A3WE 2007062500037 20070625 00037 WP 2007 6 25 07FDEA01452 1 20070412 A 5710 DOUBLER DOUG DC10 DC1010 3022110 WP ZONE 600 NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 397FE 46631 MODIFICATION AND REPAIR ASSESSMENT PROGRAM. FOUND 3 DOUBLER ON CENTER WS 1257 TO STA 1319 RT SIDE B/T XCW47 TO XCW81 DO UBLER INSTALLED PER P TO F MOD, REF DWG SM10570002 AND VSP0022 (SEE FAA FORM 307,DATED 26 JUNE 1998) SEE ENGINEERING REC OMENDED ACTION. THIS SDR NEEDS TO BE VOIDED DUE TO A NCR AGAINST THIS WO- ADMISTRATOR 06/15/07. 2 L 7 3 4F A22WE 2007062500038 20070625 00038 EU 2007 6 25 07FDEA01871 1 20070521 A 5330 SKIN AIRBUS 310 A310222 3930315 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED RT FS 3514-3567 FR65-66 AND STR33-38. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMIN ATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXI STING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 53-10-12, FIG 225 (SHEET 2). REPAIR EVALUATED PER GMM 6-2-100 AND CL ASSIFIED MAJOR. 2 L 7 2 4F RT A35EU 2007062500039 20070625 00039 EU 2007 6 25 07FDEA01875 1 20070521 A 5330 A536102658326 SKIN AIRBUS 310 A310222 3930315 EU ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED LT FS 1870-1923 FR 34-35 AND STR 35-37. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETE RMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FEDEX EA 6-5330-112415A. THE NON ROUTINE NUMBER I NDICATED IN THE RIGHT TO CORNER SHOULD BE N00210 AND NOT N00202. THE JASC/ATA CODE SHOULD READ 5330 INSTEAD OF 52. 2 L 7 2 4F RT A35EU 2007062500040 20070625 00040 EU 2007 6 25 07FDEA01878 1 20070521 A 5330 A52372020 CROSSBEAM AIRBUS 310 A310222 3930315 EU ZONE 800 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON FWD CARGO COMPARTMENT DOOR FR 21-21A BETWEEN BEAM 3 AND 4. REPAIR REQUIRES EVALUATIO N FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 52-30-00 FIG 203. 2 L 7 2 4F RT A35EU 2007062500041 20070625 00041 EU 2007 6 25 07FDEA01900 1 20070521 A 5755 A57710013 SPOILER AIRBUS 310 A310222 3930315 EU ZONE 600 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON RT UPPER WING SURFACE INBD OF SPOILER 3 WS 737-813 RIB 12-13. REPAIR REQUIRES EVALUA TION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOU ND NOT TO CONFORM TO A SRM REPAIR. REPAIR DOUBLER WAS REMOVED AND NO DAMAGE WAS FOUND. NEW OVERSIZE FASTENERS WERE INS TALLED ON EXISTING HOLES IN ACCORDANCE WITH SRM 51-40-23. 2 L 7 2 4F RT A35EU 2007062500042 20070625 00042 EU 2007 6 25 07FDEA01901 1 20070521 A 5730 A57710013 SKIN AIRBUS 310 A310222 3930315 EU ZONE 600 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON RT UPPER WING SURFACE INBD OF SPOILER 3 WS 737-813 RIB 12-13. REPAIR REQUIRES EVALUA TION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FO UND NOT TO CONFORM TO A SRM REPAIR. REPAIR DOUBLER WAS REMOVED AND NO DAMAGE WAS FOUND. NEW OVERSIZE FASTENERS WERE IN STALLED ON EXISTING HOLES IAW SRM 51-40-23. 2 L 7 2 4F RT A35EU 2007062500043 20070625 00043 EU 2007 6 25 07FDEA01902 1 20070521 A 5755 A57710013 SPOILER AIRBUS 310 A310222 3930315 EU ZONE 600 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON RT UPPER WING SURFACE OUTB OF SPOILER 4 WS 1119-1182 RIB 18-19. REPAIR REQUIRES EVALU ATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUN D NOT TO CONFORM TO AN EXISTING SRM REPAIR. REPAIR DOUBLER WAS REMOVED AND NO DAMAGE WAS FOUND. NEW OVERSIZE FASTENERS WERE INSTALLED ON EXISTING HOLES IN ACCORDANCE WITH SRM 51-40-23. 2 L 7 2 4F RT A35EU 2007062500044 20070625 00044 EU 2007 6 25 07FDEA01903 1 20070521 A 5755 A57710013 SPOILER AIRBUS 310 A310222 3930315 EU ZONE 600 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON RT UPPER WING SURFACE INBD OF SPOILER 4 WS 935-996 RIB 15-16. REPAIR REQUIRES EVALU ATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FO UND NOT TO CONFORM TO A SRM REPAIR. REPAIR DOUBLER WAS REMOVED AND NO DAMAGE WAS FOUND. NEW OVERSIZE FASTENERS WERE IN STALLED ON EXISTING HOLES PER SRM 51-40-23. 2 L 7 2 4F RT A35EU 2007062500045 20070625 00045 NM 2007 6 25 07FDEA02063 1 20070604 A 5330 AGA3102501 SKIN DOUG MD11 MD11F 3023600 NM ZONE 100 NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 EXISTING REPAIR, CTR CARGO, AFT DOOR JAMB EXTERIOR FOUND EDGE PATCH. EXISTING REPAIR AT CTR CARGO, AFT DOOR JAMB EXTERI OR EDGE PATCH EVALUATED AND FOUND ACCOMPLISHED AS PER SRM 53-50-00 FIGURE 17 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PE R GMM 6-2-100. THIS SDR SUBMITTED IN ERROR- ADMINISTRATOR. 2 L 7 3 4F RT A22WE 2007062500046 20070625 00046 NM 2007 6 25 07FDEA02064 1 20070604 A 5710 ARC27403 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 EXISTING REPAIR, LT WING I/B FLAP UPPER SURFACE FOUND WITH EXTERNAL PATCH AT XIFH 216 YIFH 70. EXISTING REPAIR AT LT WI NG I/B FLAP UPPER SURFACE XIFH 216, YIFH 70, EVALUATED AND FOUND ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 38 VOLUME I. R EPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. THIS SDR SUBMITTED IN ERROR- ADMINISTRATOR. 2 L 7 3 4F RT A22WE 2007062500047 20070625 00047 NM 2007 6 25 07FDEA02066 1 20070604 A 5710 ARB24444 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 EXISTING REPAIR, RT WING I/B FLAP UPPER SURFACE FOUND EXISTING PATCH AT XIFH 157 YIFH 64. EXISTING REPAIR AT RT WING I/ B FLAP UPPER SURFACE XIFH 157, YIFH 64, EVALUATED AND FOUND ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. THIS SDR SUBMITTED IN ERROR- ADMINISTRATOR 2 L 7 3 4F RT A22WE 2007062500048 20070625 00048 NM 2007 6 25 07FDEA02067 1 20070604 A 5710 ARB24444 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 EXISTING REPAIR, RT WING I/B FLAP UPPER SURFACE FOUND EXISTING PATCH AT XIFH 168, YIFH 64. EXISTING REPAIR AT RT WING I /B FLAP UPPER SURFACE XIFH 168, YIFH 64, EVALUATED AND FOUND ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAI R CLASSIFIED AS MAJOR AS PER GMM 6-2-100. THIS SDR SUBMITTED IN ERROR- ADMINISTRATOR. 2 L 7 3 4F RT A22WE 2007062500049 20070625 00049 NM 2007 6 25 07FDEA02069 1 20070604 A 5710 ARC3151504 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 EXISTING REPAIR, RT WING I/B FLAP UPPER SURFACE FOUND EXISTING PATCH AT XIFH 283, YIFH 30. EXISTING REPAIR AT RT WING I /B FLAP UPPER SURFACE XIFH 283, YIFH 30, EVALUATED AND FOUND ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAI R CLASSIFIED AS MAJOR AS PER GMM 6-2-100. THIS SDR SUBMITTED IN ERROR- ADMINISTRATOR. 2 L 7 3 4F RT A22WE 2007062500050 20070625 00050 NM 2007 6 25 07FDEA02079 1 20070607 A 5330 ADA30001 SKIN DOUG MD11 MD11F 3023600 NM ZONE 200 NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 APPROXIMATELY BETWEEN STA 790-808, LONGERON 4L-5L FOUND EXISTING REPAIR. REPAIR CARRIED OUT AT APPROXIMATELY BETWEEN ST A 790-808, LONGERON 4L-5L AS PER 53-20-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. THIS SDR S UBMITTED IN ERROR- ADMINISTRATOR. 2 L 7 3 4F RT A22WE 2007062500051 20070625 00051 NM 2007 6 25 07FDEA02080 1 20070607 A 5310 AFA779511 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 EXISTING REPAIR, REF EA NR 1-5310-85955, TITLE: FUSELAGE, MAINFRAME, SEAT TRACK SPLICE REPAIRS Y=1781, X=27.50, 47.5 AND -27.5. EXISTING REPAIR EVALUATED AND FOUND ACCOMPLISHED AS PER FEDEX EA NR 1-5310-85955, TITLE: "FUSELAGE - MAIN FRAME , SEAT TRACK SPLICE REPAIRS Y=1781, X=27.50, 47.5 AND -27.5". REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. THIS SD R SUBMITTED IN ERROR- ADMINISTRATOR. 2 L 7 3 4F RT A22WE 2007062500052 20070625 00052 EU 2007 6 25 07FDEA02143 1 20070615 A 5310 R53781053 FLOORBEAM AIRBUS 310 A310222 3930315 EU ZONE 100 NONE A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR LOCATED ON THE FLOORBEAM FS 1067 - 1184 FR 12A - 14 AND Y-953. REPAIR REQUIRES EVALUATION FOR MAJOR/MI NOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR CONFORMS TO FEDEX EA 6-53 10-106718. 2 L 7 2 4F RT A35EU 2007062500053 20070625 00053 EU 2007 6 25 07FDEA02144 1 20070615 A 5750 A57843700 FLAP AIRBUS 310 A310222 3930315 EU ZONE 500 NONE A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 452FE 313 LT WING, KRUEGER FLAP, PREVIOUS PATCH REPAIR FOUND LOCATED ON KRUEGER FLAP BETWEEN RIB 2A AND RIB3, WS 67. REPAIR REQUI RES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR CONFORM S TO EXISTING FEDEX EA 6-5750-81817. 2 L 7 2 4F RT A35EU 2007062500054 20070625 00054 EU 2007 6 25 07FDEA02145 1 20070615 A 5750 A57970651 FLAP AIRBUS 310 A310222 3930315 EU ZONE 600 NONE A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 452FE 313 WING RT, FLAP INBOARD, PREVIOUS FLUSH REPAIR LOCATED ON FLAP VANE LEADING EDGE BETWEEN RIB 6 - 8. REPAIR REQUIRES EVALU ATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR CONFORMS TO EXISTING FEDEX EA 6-5750-65125. 2 L 7 2 4F RT A35EU 2007062500055 20070625 00055 WP 2007 6 25 07FDEA02146 1 20070615 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CENTER LANDING GEAR WHEEL WELL,CORROSION ON FUSELAGE SKIN AT STA 1501 TO 1521, LONGERON 51R TO 50R. [07-17-07] REPLA CED ON N00616 WITH EA 8-5330-112939. 2 L 7 3 4F RT A22WE 2007062500056 20070625 00056 WP 2007 6 25 07FDEA02147 1 20070615 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CORROSION ON FUSELAGE SKIN INTERIOR AT STA 1441 TO 1481, LONGERON 50L TO 50R, CENTER LANDING GEAR WHEEL WELL CAVITY. [07-13-07] REMOVED AND REPLACED SKIN WITH NEW SECTION FS1391-1521, LONGERON 48L - 48R IAW FEDEX EA 8-5330-112939 (FU SELAGE SKIN REPAIR AT STA 1381 - 1531, L48L - L 48R - REPAIR) 2 L 7 3 4F RT A22WE 2007062500057 20070625 00057 NM 2007 6 25 07FDEA02148 1 20070615 A 5711 ARB74132 SPAR CAP DOUG MD11 MD11F 3023600 NM ZONE 600 OVERSIZED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING TRAILING EDGE UPPER CAP AREA, XORS 577 FOUND HOLE ELONGATED. [06-29-07] REPAIR CARRIED OUT AS PER FEDEX E.A. 1 -5710-109910, REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062500058 20070625 00058 NM 2007 6 25 07FDEA02149 1 20070615 A 5347 ACA7106505 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 FWD CABIN COURIER AREA FOUND SEAT TRACK AT STA 482 X= -27" WITH CORROSION. [06-29-07] REPAIR CARRIED OUT AS PER SRM 53 -70-00 FIG 1 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062500059 20070625 00059 NM 2007 6 25 07FDEA02150 1 20070615 A 5330 APB74411 SKIN DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 MAIN DECK COMPARTMENT, UNDER FLOOR CENTER TANK AT STA 1227 RT= -75" FOUND WITH CORROSION. [07-02-07] COMPLIED WITH FED EX E.A. 1-5720-109912, CLASSIFIED AS A MINOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062500060 20070625 00060 NM 2007 6 25 07FDEA02151 1 20070615 A 5740 ARB76111 FITTING DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LT WING LOWER WINGLET AFT FITTING AFT HOLE FOUND CORRODED. [06-29-07] COMPLIED WITH FEDEX EA 1-5730-109909, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062500061 20070625 00061 NM 2007 6 25 07FDEA02152 1 20070615 A 5712 ARB29238 RIB DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING LEADING EDGE RIB NEAR XOS 762 FOUND CRACKED. [06-29-07] REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. RIB F ABRICATED AS PER DOUGLAS DRAWING NR ARB2923. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062500062 20070625 00062 NM 2007 6 25 07FDEA02153 1 20070615 A 5347 ADA73491 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STA 1169-1219 RT X= -47" FOUND WITH CORROSION. [06-29-07] REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062500063 20070625 00063 NM 2007 6 25 07FDEA02154 1 20070616 A 5730 ARB74022 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 CRACK FOUND AT RHW LOWER SURFACE ACCESS PANEL 636AB CUT OUT. CRACK CAN BE SEEN AT NR 4 FASTENER HOLE FROM 12 O'CLOCK PO SITION COUNTER CLOCKWISE DIRECTION. [06-29-07] REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5710-109908. REPAIR CLASSIFIE D AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062500064 20070625 00064 EU 2007 6 25 07FDEA02155 1 20070616 A 2131 82010B040901 CONTROLLER SEMCA AIRBUS 310 A310222 3930315 EU CABIN PRESSURE FAILED A FDEA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 25 446FE 334 224 ON CLIMB-OUT, AIRCRAFT DID NOT PRESSURIZE. BOTH FWD AND AFT REG NR 2 VALVES WERE STUCK FULL OPEN AND SHOWING AMBER ON T HE ECAM. DUPLICATED PROBLEM AT GATE, REPLACED NR 2 CABIN PRESSURE CONTROLLER PER A310-200 AMM21-31-11-4, OPERATIONAL C HECK NORMAL. PREMATURE REMOVAL/INSTALLATION OFF MFG 82010B040901, POS RH SRL 334, TAG 482A64, ON MFG 82010B040901, SRL 208,TAG 56432A. 2 L 7 2 4F RT A35EU 2007062500065 20070625 00065 NM 2007 6 25 07FDEA02156 1 20070616 A 5730 ARB74021 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 CRACK FOUND AT LT WING LOWER SURFACE ACCESS PANEL 536AB CUT OUT. CRACK CAN BE SEEN AT NR 4 FASTENER HOLE, COUNTING FROM 12 O'CLOCK POSITION IN A CLOCKWISE DIRECTION. [06-29-07] REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5710-109907, REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062500066 20070625 00066 NM 2007 6 25 07FDEA02157 1 20070616 A 5730 ARB74021 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 CRACK FOUND AT LT WING LOWER SURFACE ACCESS PANEL 536AB CUT OUT. CRACK CAN BE SEEN AT NR 5 FASTENER HOLE, COUNTING FROM 12 O'CLOCK POSITION IN A CLOCKWISE DIRECTION. [06-29-07] REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5710-109907, REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062500067 20070625 00067 NM 2007 6 25 07FDEA02158 1 20070616 A 5730 ARB74021 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 CRACK FOUND AT LT WING LOWER SURFACE ACCESS PANEL 536AB CUT OUT. CRACK CAN BE SEEN AT NR 6 FASTENER HOLE, COUNTING FROM 12 O'CLOCK POSITION IN A CLOCKWISE DIRECTION. [06-29-07] REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5710-109907, REPAI R CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062500068 20070625 00068 NM 2007 6 25 07FDEA02159 1 20070616 A 5730 ARB74021 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 CRACK FOUND AT LT WING LOWER SURFACE ACCESS PANEL 536AB CUT OUT. CRACK CAN BE SEEN AT NR 4 FASTENER HOLE, COUNTING FROM 6 O'CLOCK POSITION IN A CLOCKWISE DIRECTION. [06-29-07] REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5710-109907, REPAIR C LASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062500069 20070625 00069 NM 2007 6 25 07FDEA02160 1 20070616 A 5730 ARB74021 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 CRACK FOUND AT LT WING LOWER SURFACE ACCESS PANEL 536AB CUT OUT. CRACK CAN BE SEEN AT NR 5 FASTENER HOLE, COUNTING FROM 6 O'CLOCK POSITION IN A CLOCKWISE DIRECTION. [06-29-07] REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5710-109907, REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062500070 20070625 00070 NM 2007 6 25 07FDEA02161 1 20070616 A 5712 ARB29313 RIB DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LT WING LEADING EDGE RIB AT XOS 584 FOUND CRACKED. [06-29-07] REMOVED AND REPLACED AS PER SRM 51-33-01 VOL.II. NEW FO RMER FABRICATED AS PER DOUGLAS DWG ARB2931. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062500071 20070625 00071 NM 2007 6 25 07FDEA02162 1 20070617 A 5730 ARB12302 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 FOUND DENT, RT WING FIXED LEADING EDGE, NEAR XW 344. [07-03-07] COMPLIED WITH FEDEX E.A 1-5720-109914. CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062500072 20070625 00072 NM 2007 6 25 07FDEA02163 1 20070617 A 5730 ARC27364 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT INBOARD FLAP LOWER SURFACE, INBD LOWER SKIN SEGMENT FOUND WITH DENT. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 3 V OL.I. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062500073 20070625 00073 NM 2007 6 25 07FDEA02164 1 20070618 A 5730 ARB75801 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LT WING UPPER FIXED LEADING EDGE SURFACE AT XIS 247 FOUND WITH CHAFING MARK. [06-29-07] REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 24 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062500074 20070625 00074 NM 2007 6 25 07FDEA02165 1 20070618 A 5730 ARB75802 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING FIXED LEADING EDGE UPPER SURFACE, XIS 247 FOUND CHAFED AT EXISTING REPAIR. [07-02-07] REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 24, VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062500075 20070625 00075 NM 2007 6 25 07FDEA02166 1 20070618 A 5320 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 AFT ACCESSORY COMPARTMENT, FOUND FRAME CLIP AT STA 2140 CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2007062500076 20070625 00076 NM 2007 6 25 07FDEA02167 1 20070618 A 5753 VANE DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT OUTBOARD FLAP VANE NR 4 AND NR 5 TRACK (COUNT FROM INBOARD) UPPER MOUNTING AREA FOUND CORROSION. [06-29-07] REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT CARRIED OUT AS PER AMM 27-50-32-5 AND OPERATIONAL TEST CARRIED OUT AS PE R AMM 27-50-00-860-801 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007062500077 20070625 00077 EU 2007 6 25 07FDEA02168 1 20070618 A 5230 A52378000002 DOOR AIRBUS 300 A300B4622R 3930312 EU ZONE 800 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 FOUND OLD DOUBLER INSTALLED ON BULK CARGO DOOR FWD LOWER CORNER, WHICH WAS NOT CONFIRM TO RAS (THICKNESS AND MATERIAL) R EPAIR WAS PERFORMED BY INSTALLING A NEW DOUBLER IAW EA 6-5234-103320 AND RAS/DABRE/7006375/2006 ISS A. 2 L 7 2 4F RT A35EU 2007062500078 20070625 00078 EU 2007 6 25 07FDEA02169 1 20070618 A 5330 A53610567280 PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 726FD 575 FOUND OLD DOUBLER REPAIR C19-20, P 43-44 RT, NOT CONFORM TO SRM. REPAIR PERFORMED BY NEW DOUBLER INSTALLATION IAW EA 6- 5312-103293 AND RAS/AS/137/2006 ISS A. 2 L 7 2 4F RT A35EU 2007062500079 20070625 00079 EU 2007 6 25 07FDEA02170 1 20070618 A 5330 A53770355204 DOUBLER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 NONE A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 726FD 575 OLD DOUBLER REPAIR C 19-20, P 38-40 LT, IN CONFLICT WITH P TO F CONVERSION REPAIR PERFORMED BY NEW DOUBLER INSTALLATION IAW EA 6-5313-103273 AND RAS/DABRE/7006901/2006 ISS A. 2 L 7 2 4F RT A35EU 2007062500080 20070625 00080 EU 2007 6 25 07FDEA02171 1 20070618 A 5330 A53981600205 DOUBLER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 726FD 575 FOUND OLD DOUBLER REPAIR , C77-78, P27 RT NOT CONFORM TO SRM REPAIR PERFORMED BY NEW DOUBLER INSTALLATION IAW SRM 53-10 -12 FIG 228, APPROVED BY EA 6-5318-103319. 2 L 7 2 4F RT A35EU 2007062500081 20070625 00081 EU 2007 6 25 07FDEA02172 1 20070618 A 5730 A57661002218 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 OLD BONDING REPAIR LT AILERON LOWER SKIN T/E WITH NEW DELAMINATION REPAIR PERFORMED BY METAL SKINNED HONEYCOMB PATCH REP AIR IAW SRM 51-77-12 PB 200 PARA 4. 2 L 7 2 4F RT A35EU 2007062500082 20070625 00082 EU 2007 6 25 07FDEA02173 1 20070618 A 5730 A57661002208 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 UNKNOWN A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 726FD 575 OLD BONDING REPAIR RT AILERON LOWER SKIN T/E WITH NEW DELAMINATION REPAIR PERFORMED BY METAL SKINNED HONEYCOMB PATCH REP AIR IAW SRM 51-77-12 PB 200 PARA 4 AND RAS/FOK/097/ 2004 ISS A. 2 L 7 2 4F RT A35EU 2007062500083 20070625 00083 EU 2007 6 25 07FDEA02174 1 20070618 A 5750 A57865058203 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 UNKNOWN A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 726FD 575 OLD REPAIR (FLUSH DOUBLER) REPAIR ON RT OUTBOARD SLAT NR 3 JACK RIB 6 NOT CONFORM TO SRM (FILLER MATERIAL, RIVET PITCH, USED FASTENER). REPAIR PERFORMED BY NEW FLUSH REPAIR, APPROVED BY EA 6-5744-103280 REV A AND RAS/FOK/213/2006 ISS. C. 2 L 7 2 4F RT A35EU 2007062500084 20070625 00084 EU 2007 6 25 07FDEA02175 1 20070618 A 5320 SEE4A SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 UNKNOWN A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 726FD 575 LT/RT ON SILL BEAM AND EXTERNAL SKIN, INTERNAL DOUBLER CORROSION AND DAMAGED HL, COLLARS (FOLLOWING P/N AFFECTED: A539-8 0110-207, A539-80071-205, A539-80071-205, A539-80108- 205, A539-81259-211, A539-80177-201, A539-80108-204, A539-81259-2 10, A539-80177-200). REPAIR PERFORMED BY REWORK OF STRUCTURE AND SPOT FACING IAW EA 6-5318-103295 AND RAS/DAHAM/4021175 /2006 ISS A. 2 L 7 2 4F RT A35EU 2007062500085 20070625 00085 EU 2007 6 25 07FDEA02176 1 20070618 A 5310 A53970875 PLATE AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 FRETTING MARKS ON INNER FLANGE C55 AND 57.2 LT AND C58 RT, P14-15 LT/RT, AND TOOL MARKS ON EMERGENCY EXIT TOP COVERPLATE LT/RT REPAIR PERFORMED BY BLEND OUT AND POLISHING TO SMOOTH CONTOUR IAW EA 6-5316-103275 AND RAS/DATLS/0003334/2006 IS S A AND RAS/DATLS/0003335/2006 ISS. A. 2 L 7 2 4F RT A35EU 2007062500119 20070625 00119 NM 2007 6 25 AWXA200700736 1 20070608 A 5210 FE240004 DAMPER AIRBUS A319 A319132 3930340 NM ZONE 200 BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 29329 29323 1049 SAL - EES - BROKEN ASSIST DAMPER ASSEMBLY ON R1 DOOR, FR 16 - FR 20. REPLACED ASSIST DAMPER ASSEMBLY ON R1 DOOR, FR 16 - FR 20 IAW A319 AMM 52-11-14. [06-19-07] REMOVED INFORMATION FROM STRUCTURE CAUSING DIFFICULTY SECTION SINCE DEFECTIV E ITEM IS NOT A STRUCTURAL ITEM AND MADE CORRECTIONS TO THE PROBLEM DESCRIPTION SECTION. 2 L 7 2 4F RT A28NM 2007062500120 20070625 00120 WP 2007 6 25 ARWA20070607 1 20070617 A 3241 42241 CONTROL UNIT DOUG DC8 DC863F 302198F WP ANTI SKID SYS UNKNOWN A ARWA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 661AV 45969 L/F I/B ANTI-SKID LIGHT ILLUMINATED. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT IN ACCORDANCE WITH M/M 32-43-1; CHECK GOOD IN ACCORDANCE WITH M/M 32-43-0. 2 L 7 4 4F 4A25 2007062500121 20070625 00121 NM 2007 6 25 KCSA071193 1 20070619 A 5412 BULKHEAD BOEING 747 747209B 138489B NM NR 1 NACELLE CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 NR 1 PYLON, HYDRAULIC PRESSURE LINE UNION AT STA 221.9 BULKHEAD CHAFING THRU REPAIR DOUBLER. 2 L 7 4 4F RT A20WE 2007062500132 20070625 00132 NM 2007 6 25 UIEA200700244 1 20070610 A 5330 SKIN BOEING 747 747243B 1384830 NM BS 340 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 FLAT SIDED SKIN AT BS 340 STRINGERS 6-8L FOUND 9 EACH HOLES CRACKED AT SKIN. FLAT SKIN CRACKED HOLES REPAIRED AS PER BO EING MESSAGE 1-343396688-2 AND FAA 8100-9 2 L 7 4 4F A20WE 2007062500133 20070625 00133 NM 2007 6 25 UIEA200700247 1 20070616 A 5330 SKIN BOEING 747 747228F 1384895 NM BS 108 UNKNOWN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 RADOME SKIN HAS A 2.0 INCH BY 4.0 INCH PREVIOUS REPAIR FILLER ERODED AT 11 O'CLOCK POSITION. ACCOMPLISHED PERMANENT REP AIR AS PER 747-200 SRM 53-50-03 PAGE 23, PAR 15. ALSO REFERENCE ATLAS AIR XEO 53-061507-1. 2 L 7 4 4F A20WE 2007062500135 20070625 00135 NM 2007 6 25 UIEA200700248 1 20070616 A 5330 SKIN BOEING 747 747228F 1384895 NM BS 660 DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 LOWER FUSELAGE, RT SIDE AT STA 660 HAS A DENT BETWEEN S43 AND S44 RT CAUSED BY ACCIDENT DURING STORM. ACCOMPLISHED PERM ANENT REPAIR OF EXTERIOR SKIN AS PER 747-200 SRM 53-30-03 FIG 17, ALSO, PERMANENT REPAIR OF BROKEN SHEAR TIE AT BS 660 S 43R-S44R WAS REPAIRED PER SRM 53-10-04 FIG 3. ALSO, REFERENCE ATLAS AIR XEO 53-061507. 2 L 7 4 4F A20WE 2007062500136 20070625 00136 NM 2007 6 25 QXEA200701006 1 20070617 A 2430 400SG163Q GENERATOR BOMBDR DHC8 DHC8402 1390042 NM NR 2 MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 403QX 8052 1024 4037 BIL FLIGHT NR 2417: NR 2 DC GENERATOR WILL NOT RESET. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED NR 2 STARTER GENE RATOR AND INSTALLED NEW STARTER GENERATOR IAW AMM 24-31-01-000-801 AND 24-31-01-400-801. OPS CHECK GOOD. AIRCRAFT RETU RNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007062600009 20070626 00009 EU 2007 6 26 07FDEA01897 1 20070521 A 5753 A57970215 FLAP AIRBUS 310 A310222 3930315 EU ZONE 600 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON RT UPPER WING SURFACE T/E OF INBOARD FLAP WS0-67 RIB 1-2. REPAIR REQUIRES EVALUATION F OR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. THE PRESENT SDR CONCERNS THE S AME NR AS SDR 07-2202. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PE R SRM 57-52-12 FIG 204. 2 L 7 2 4F RT A35EU 2007062600018 20070626 00018 EU 2007 6 26 07FDEA02192 1 20070619 A 5100 A53773487 PLATE AIRBUS 300 A300B4605R 3930308 EU ZONE 100 NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 OLD REPAIR DOUBLER AT C20, P51-54 RT, NOT COMPATIBLE WITH P TO F CONVERSION. REPAIR PERFORMED BY INSTALLATION OF NEW EX TERNAL DOUBLER IAW EA 6-5313-106478 AND RAS/DABRE/7007753/2007 ISSUE "A". 2 L 7 2 4F RT A35EU 2007062600020 20070626 00020 EU 2007 6 26 07FDEA02194 1 20070619 A 5320 A53770625216EF FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 CORROSION AT MANHOLE FITTING BETWEEN C38.1-C38.2, WHICH WAS GRINDED THROUGH THE FITTING WITH THE SKIN PANEL AFFECTED. R EPAIR PERFORMED BY BLEND OUT AND INSTALLATION WASHER IN BLEND VOID AND ADDITIONAL FASTENER IAW SRM 53-14-12/FIG 208, EA 6-5334-103277 AND RAS/DATLS/0003381/2006. 2 L 7 2 4F RT A35EU 2007062600027 20070626 00027 EU 2007 6 26 07FDEA02201 1 20070514 A 5101 NONE AIRBUS 310 A310222 3930315 EU ZONE 600 NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON RT UPPER WING SURFACE INBD OF OUTBD FLAP WS 663-737 RIB 11-12. REPAIR REQUIRES EVALUAT ION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOU ND TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 57-53-12 FIG 208. THIS SDR SUBMITTED IN ERROR - ADMINISTRATOR. 2 L 7 2 4F RT A35EU 2007062600031 20070626 00031 NM 2007 6 26 07FDEA02205 1 20070619 A 5315 6520827231 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 286FE 22623 AGING A/C INSP, FOUND EXISTING REPAIR DID NOT CONFORM TO FED EX DWG SR27-53-034 AT BS 680 LBL 3'' TO 23''. REMOVED OLD REPAIR, FABRICATED NEW PARTS AND INSTALLED REF SRM 51-10-1 AND FED EX DWG SR27-53-034. 2 L 7 3 4F RT A3WE 2007062600039 20070626 00039 NM 2007 6 26 07FDEA02213 1 20070619 A 5314 BAC15061464 KEELBEAM BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT PIT STR 29L/KEEL BEAM CHORD CORRODED BETWEEN STA 950D - 950E REMOVED CORROSION, FABRICATED REPAIR STRAP, SPOT FACED KEEL BEAM AROUND FASTENER HOLES. FABRICATED FILLER WASHER AND INSTALLED REPAIR PARTS. REF FED EX STANDARD REWORK DRA WING, LT AND RT KEEL BEAM FLANGE CORROSION, DWG NR SR27-53-023. 2 L 7 3 4F RT A3WE 2007062600050 20070626 00050 NM 2007 6 26 AWXA200700744 1 20070501 A 5313 6545800179 STRINGER BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - CRACKED STRINGER, BS 357, S4L. REPAIRED STRINGER, BS 357, S4L IAW B737-300 SRM 53-00-03-2R1. 2 L 7 2 4F RT A16WE 2007062600051 20070626 00051 NM 2007 6 26 AWXA200700745 1 20070418 A 5210 65458713 SKIN BOEING 737 73733A 1384673 NM ZONE 800 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - CRACKED R1 DOOR SKIN, BS 296, S14R, AT THE LOWER HINGE CUT OUT. REPAIRED R1 DOOR SKIN, BS 296, S14 R, AT THE LOWER HINGE CUT OUT IAW AWA ER 03-5210-07159-ES1. 2 L 7 2 4F RT A16WE 2007062600080 20070626 00080 NM 2007 6 26 AALA20071032 1 20070606 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 649AA 24607 DFW - EMERGENCY GROUND FLOOD LIGHT AT LEFT CABIN INOPERATIVE. RELAMPED EMERGENCY GROUND FLOOD LIGHT AT LEFT CABIN. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007062600081 20070626 00081 WP 2007 6 26 AALA20071022 1 20070605 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 76201 53291 SAN - EMERGENCY LIGHT AT FORWARD RIGHT DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD RIGHT DOO R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007062600084 20070626 00084 NM 2007 6 26 AALA20071019 1 20070604 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 623AA 24581 MIA - EMERGENCY LIGHT AT SEAT 23D INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007062600086 20070626 00086 NM 2007 6 26 AALA20071016 1 20070603 A 3350 BATTERY BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 690AA 25696 MIA - EMERGENCY FLASHLIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT LEFT NUMBE R ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007062600097 20070626 00097 NM 2007 6 26 QXEA200701014 1 20070620 A 3150 NONE BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS NONE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 401QX 4031 SEA - ON FLIGHT 2380, RETURNED TO GATE, FLAP POWER CAUTION AFTER START AND SELECTING TAKEOFF FLAPS -0 -15. COMPLIED WIT H ABNORMAL CHECKLIST AND CIRCUIT BREAKER FLAP CONTROL RESET, SAME RESULT. MAINTENANCE INTEROGATED CDS AND FOUND ECU POW ER ON BIT FAULT, CLEARED FAULTS, GROUND RAN ENGINE AND CYCLED FLAPS NUMEROUS TIMES WITH NO FAULTS NOTED. AIRCRAFT RETUR NED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007062600098 20070626 00098 NM 2007 6 26 QXEA200701010 1 20070621 A 3150 NONE BOMBDR DHC8 DHC8402 1390042 NM WARNING LIGHT NONE A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 417QX 4086 SEA - ON FLIGHT 2332, RETURNED TO GATE, AFTER PUSHBACK AVIONICS CAUTION LIGHT WAS ILLUMINATED. NO ASSOCIATED ED MESSAGE S AFTER RETURNING TO GATE. BAD CONFIG ED MESSAGE APPEARED. MAINTENANCE CYCLED POWER SEQUENTIALLY ON ALL EFIS DU'S "DU BAD CONFIG" MESSAGE ON ED WENT AWAY AND AVIONICS CAUTION EXTINGUSHED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED . 2 H 7 2 4T RT A13NM 2007062600099 20070626 00099 2007 6 26 QXEA200701015 4 20070620 A 3420 42000332501 COMPUTER BOMBDR DHC8 DHC8402 1390042 NM NR 1 AHRS INOPERATIVE A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 401QX 8305 8305 4031 SEA - ON FLIGHT 2438, RETURNED TO GATE, WHILE TAXING FOR TAKEOFF THE YAW DAMPER DISENGAGED FOLLOWED BY ROLL MISMATCH MES SAGE. CAPT'S ADI 3 DEGREES RIGHT BANK, FO'S ADI = 0. LATER DURING RIG, PITCH MISMATCH MESSAGE CAPT'S ADI =10 DEGREES PI TCH, FO'S ADI = 0 DEGREES, ALSO GOT HEADING MESSAGE. MAINTENANCE REMOVED AND REPLACED NR 1 AHRS COMPUTER. OPERATIONAL TEST PASSED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007062600137 20070626 00137 EU 2007 6 26 USAA070469 1 20070618 A 5320 PROFILE AIRBUS A321 A321211 3930370 EU CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 180US 1525 FR 48 STR 38 LEFT, FLOOR CORNER PROFILE HAS CRACK. INSTALLED DOUBLER PER EA 84652, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A28NM 2007062600138 20070626 00138 EU 2007 6 26 MAC060701 1 20070606 A 5751 ATTACH FITTING AEROSP AEROSP ATR42 ATR42300 8680920 EU AILERON CORRODED A MTNA K NONE O OTHER IN INSP/MAINT 1 SO 33 920FX NT1236 325 DURING A 2 YEAR INSPECTION, LEVEL 2 CORROSION WAS FOUND ON THE T-FITTINGS ATTACHING THE RIBS TO THE SPAR. THE FITTINGS AFFECTED ARE LOCATED AT THE I/B, AND O/B HINGE ATTACH POINTS. THE PROBABLE CAUSE IS DISSIMILAR MATERIALS (STEEL BOLTS I N ALUMINUM ALLOYED FITTINGS). THE FITTINGS WERE REPLACED AT RIBS 4, 11/12, AND 19. REFERENCE SRM 57-61-10 FIG 101. 2 H 7 2 4T RT A53EU 2007062600139 20070626 00139 EU 2007 6 26 SA07040 1 20070619 A 3350 321431 EPSU AIRBUS A319 A319112 3930323 EU ZONE 200 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 722US 1097 CLT - THE LEFT, MID-CABIN EMERGENCY POWER SUPPLY UNIT BATTERY SHOWS FAULT ON TEST. MAINTENANCE REPLACED THE BATTERY ON THE LEFT, MID-CABIN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007062600142 20070626 00142 SO 2007 6 26 RAIA00706023 1 20070615 A 3240 NONE EMB 145 EMB145EP 3260221 SO BRAKES NONE A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 826HK 145016 FLT NR 5459 - MEM - ABORTED TAKEOFF PRIOR TO 80 KIAS. BRAKE INBOARD INOPERATIVE EICAS MESSAGE. MAINTENANCE PERFORMED B RAKE SYSTEM, OPS CHECK. CHECKS GOOD AT THIS TIME. 2 L 7 2 4F RT T00011AT 2007062600143 20070626 00143 SO 2007 6 26 RAIA00706024 1 20070615 A 2913 971808 PUMP EMB 145 EMB145LR 3260212 SO NR 1 HYD OVERHEATED A RAIA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 CE 03 819HK 12450 145062 FLT NR 5589 - STL - HYDRAULIC SYSTEM NR 1 OVERHEAT. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007062600144 20070626 00144 SO 2007 6 26 RAIA00706026 1 20070617 A 3240 NONE EMB 145 EMB145LR 3260212 SO BRAKES NONE A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 831HK 145232 FLT NR 7944 - MLI - ABORTED TAKEOFF DUE TO BRAKE OUTBOARD INOP MESSAGE AT 60 KNOTS. MAINTENANCE RESET BRAKE CONTROL UNI T. OPS TEST OF BRAKE SYSTEM OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT T00011AT 2007062600147 20070626 00147 SO 2007 6 26 RAIA00706022 1 20070614 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 807HK 145119 PRE FLT NR 3542 - STL - EMERGENCY LIGHT AFT SIDE AFT CEILING EXIT LOCATOR INOP. MAINTENANCE RESET CONNECTORS ON EMERGEN CY EXIT OVERHEAD REAR SIGN, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007062600148 20070626 00148 SO 2007 6 26 RAIA00706020 1 20070613 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 817HK 145058 POST FLT NR 5530 - STL - EMERGENCY LIGHT AT FWD BULKHEAD INOP. MAINTENANCE RESECURED LIGHT CONNECTOR, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007062600150 20070626 00150 NM 2007 6 26 ASAA0741784 1 20070614 A 5320 65479573 WEB BOEING 737 7374Q8 138447Q NM BS 807-847 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 AFT CARGO DOOR SILL WEB HAS AREAS OF CORROSION. REMOVED DAMAGED WEB SILL LOCATED AND DRILLED NEW SILL AND INSTALLED IAW SRM 51-40-02, 51-10-02 AND SOPM 20 41 05. 2 L 7 2 4F RT A16WE 2007062600152 20070626 00152 SO 2007 6 26 C2XA07IA143 1 20070616 A 3320 7287503517 LIGHT EMB 145 EMB145EP 3260221 SO CABIN SHORTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 15926 145005 IAH - FLIGHT 2091, DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL AT ROW 3A. MAINTENANCE REMOVED AND REP LACED THE SIDEWALL LIGHT ASSY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. 2 L 7 2 4F RT T00011AT 2007062600157 20070626 00157 EA 2007 6 26 TRAX200700843 1 20070614 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 390CA 10106 PAX DOOR OUTER HANDLE FLAP IS CRACKED. [06-26-07] REPAIRED IAW SRM 51-42-06, 51-25-01, AMM 11-20-00, & AMM 52-11-00 . 2 L 7 2 4F RT A21EA 2007062600158 20070626 00158 EA 2007 6 26 TRAX200700844 1 20070614 A 5210 SKIN CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 390CA 10106 PAX DOOR STAIRS FWD SKIN CRACKED IN RADIUS UNDER UPPER MID STEP. 2 L 7 2 4F RT A21EA 2007062600159 20070626 00159 EA 2007 6 26 TRAX200700845 1 20070614 A 5210 SKIN CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 390CA 10106 PAX DOOR STAIRS AFT SKIN CRACKED IN RADIUS UNDER UPPER MID STEP. 2 L 7 2 4F RT A21EA 2007062600160 20070626 00160 EA 2007 6 26 TRAX200700846 1 20070614 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 390CA 10106 RIGHT FS 280 CROSSBEAM CRACKED O/B OF RBL 9. [06-26-07] ALL WORK DONE IAW CRJ 700, 51-42-06, 51-42-06, 51-42-21. 2 L 7 2 4F RT A21EA 2007062600166 20070626 00166 NM 2007 6 26 ASAA0741785 1 20070615 A 5753 6546430189 SKIN BOEING 737 737490 1384715 NM DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 LEFT I/B FORE FLAP UPPER SIDE 77 INCHES FROM INBOARD END DELAMINATED. RECORDED AND DOUBLER OVERLAY PER SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007062600167 20070626 00167 NM 2007 6 26 ASAA0741786 1 20070619 A 5753 6546430189 SKIN BOEING 737 737490 1384715 NM TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 LEFT I/B FORE FLAP UPPER SIDE 82 INCHES FROM I/B HAS CHAFING DAMAGE. LEFT I/B FORE FLAP UPPER SIDE 82 INCHES FROM I/B D AMAGE REPAIRED IAW SRM 51-70-10 REPAIR 4. 2 L 7 2 4F RT A16WE 2007062600168 20070626 00168 NM 2007 6 26 ASAA0741787 1 20070619 A 5753 SKIN BOEING 737 737490 1384715 NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 LEFT WING I/B FORE FLAP UPPER CAMBER HAS 2 EACH DENTS. RECORDED AND DOUBLER OVER LAY PER SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007062600169 20070626 00169 NM 2007 6 26 ASAA0741789 1 20070619 A 5751 65C2591130A SKIN BOEING 737 7374Q8 138447Q NM RT AILERON DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 RIGHT AILERON FWD SPAR IS SEPARATING AT I/B UNDER LWR SURFACE. REPAIRED RIGHT AILERON I/B LWR SURFACE DAMAGE IAW SRM 51 -70-03 REPAIR 6 PG 16 AND EA 5760 01011. 2 L 7 2 4F RT A16WE 2007062600170 20070626 00170 NM 2007 6 26 ASAA0741790 1 20070619 A 5751 65C2591130A SKIN BOEING 737 7374Q8 138447Q NM RIGHT AILERON DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 RIGHT AILERON I/B FWD UPPER SURFACE PANEL IS SEPARATING AT EDGE. REPAIRED RIGHT AILERON UPPER SURFACE DAMAGE IAW SRM 51 -70-03 REPAIR 6 PG 16. 2 L 7 2 4F RT A16WE 2007062600171 20070626 00171 NM 2007 6 26 ASAA0741791 1 20070619 A 5751 65C2591130A SKIN BOEING 737 7374Q8 138447Q NM RIGHT AILERON DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 RIGHT AILERON LOWER SURFACE IS SEPARATING. REPAIRED RIGHT AILERON LOWER SURFACE DAMAGE IAW SRM 51-70-03 REPAIR 6 PG 16. 2 L 7 2 4F RT A16WE 2007062600172 20070626 00172 WP 2007 6 26 ASAA0781792 1 20070619 A 5330 5920323249 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 RIGHT EXTERNAL FUSELAGE MULITPLE PROTRUDING DENTS. CUT OUT DAMAGED AREA, FABRICATED A REPAIR DOUBLER, STRIP DOUBLER FIL LERS AND INSTALLED IAW SRM 53-04 FIG 12B. 2 L 7 2 4F RT A6WE 2007062600173 20070626 00173 WP 2007 6 26 ASAA0781793 1 20070619 A 5320 2912555501 INTERCOSTAL DOUG DC9 DC983 3022083 WP BS 842-848 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 RIGHT BSTA 845 GUSSET INTERCOSTAL SPLICE AT LONGERON 17R CORRODED. FABRICATED A REPLACEMENT GUSSET, LOCATED DRILLED AND INSTALLED GUSSET IAW SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F RT A6WE 2007062600174 20070626 00174 NM 2007 6 26 SWAA073032 1 20070618 A 3350 101114 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 725SW 27857 L1 DOOR EMERGENCY EXIT LIGHT SIGN LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007062600175 20070626 00175 NM 2007 6 26 SWAA073034 1 20070618 A 2612 20035008300 ELEMENT BOEING 737 7373H4 1384600 NM MLG W/W FAULTY A SWAA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 29 354SW 25219 WHEEL WELL FIRE LIGHT ILLUMINATED AND FIRE BELL SOUNDED INFLIGHT, FOR APPROX 5 - 10 SECONDS THEN WENT OUT. REMOVED AND REPLACED WHEEL WELL FIRE ELEMENT AND OVERHEAT DETECTION UNIT PER MM. 2 L 7 2 4F RT A16WE 2007062600177 20070626 00177 NM 2007 6 26 SWAA073037 1 20070618 A 3350 3071BPEGPL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 14Y CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007062600180 20070626 00180 2007 6 26 SWAA073031 4 20070618 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007062600181 20070626 00181 NM 2007 6 26 SWAA073040 1 20070618 A 3350 MS155721 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED 14Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007062600183 20070626 00183 NM 2007 6 26 SWAA073036 1 20070618 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 14Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP CRACKED BETWEEN ROW 16 DEF AND ROW 22 DEF. REMOVED AND R EPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007062200103 20070622 00103 WP 2007 6 22 07FDEA02141 1 20070615 A 5730 DOUBLER DOUG DC10 DC1010 3022110 WP RT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 EXISTING SKIN REPAIR RIGHT WING L/E SKIN AT STA XOS 800 REPAIRED IAW SRM 57-10-00 FIG 20 VOL 1. 2 L 7 3 4F A22WE 2007062200108 20070622 00108 NM 2007 6 22 AWXA200700729 1 20070607 A 5320 143N834214 WEB BOEING 757 757225 1384959 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 MCN - CRACKED INTERCOSTAL WEB AFT OF R2 DOOR, BS740, STR 9R. REPLACED INTERCOSTAL WEB AFT OF R2 DOOR, BS740, STR 9R IAW B757 SRM 51-40-02-0G FIG 8, 12 AND 51-30-01-0G FIG 7. 2 L 7 2 4F RT A2NM 2007062200141 20070622 00141 NM 2007 6 22 DHL2007740538 1 20070617 A 5313 STRINGER BOEING 727 7272Q9 138448M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 DURING C CHECK, NOSE SECTION STR 24 LT BS305 SHOWS CORROSION SEEN FROM LT TRUNNION ACCESS AREA. CUT-OUT DAMAGED SECTION OF STRINGER DIM 6 5/8" LENGTH, FABBED REPAIR FILLER FROM BAC1498-137 PO NR 4496178 DIM 6 5/8" REPAIR U CHANNNEL FROM .0 50 PO NR 9004670 DIM 13" LENGTH AND REPAIR J ANGLES 2EA FROM 7075-T6 .050" PO NR 9004670 DIM 13"LENGTH IAW B727 SRM 53-1 0-3 FIG1 AND 53-10-2 FIGURE 9. TREATED AND PRIMED REPAIRED PARTS AT NOSE SECTION STRINGER 24 LT BS 305 IAW B727 SRM 53- 10-3 FIG 1 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007062200154 20070622 00154 SO 2007 6 22 C2XA07RI046 1 20070608 A 3397 WIRE EMB 135 EMB135ER 3260203 SO CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18511 145267 FLT 2393 - EWR - CREW REPORTED EMERGENCY LIGHT, AT ROWS 3 AND 4 INOP. EWR MX REPAIRED BROKEN WIRE AND PERFORMED OPERATI ONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO FLIGHT. 2 L 7 2 4F RT T00011AT 2007062200155 20070622 00155 SO 2007 6 22 CHQA200700024 1 20070617 A 3244 316311 TIRE EMB 145 EMB145EP 3260221 SO LT MLG SEPARATED A CHQA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 11 978RP 4049 326 145169 FLIGHT 3022 - RDU-LGA - ON TAKEOFF ROLL, VERY HARD SHAKING AND SHIMMY THROUGHOUT AIRCRAFT. CLIMBED-OUT AND ASKED TOWER IF THEY SAW ANYTHING; THEY STATED NO. AFTER CHECKING WITH DEPARTURE, TOWER CALLED BACK AND SAID THEY FOUND A 2 FOOT CHU NK OF RUBBER ON RUNWAY THAT APPEARS TO BE A TIRE. RAN CHECKLISTS AND PREPARED CABIN FOR EMERGENCY LANDING. LANDED WITH OUT INCIDENT, FIRE RESCUE STATED THE LEFT MAIN INBOARD TIRE WAS SHREDDED. MAINTENANCE REMOVED AND REPLACED THE LEFT INB OARD MAIN TIRE. 2 L 7 2 4F RT T00011AT 2007062200158 20070622 00158 EU 2007 6 22 SA07038 1 20070615 A 4920 APU AIRBUS 320 A320214 3930316 EU MALFUNCTIONED A USAA H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 112US 1134 LAS FLT 971 EN ROUTE, BOS TO LAS. APPROXIMATELY 380 NM FROM LAS, THE APU AUTO SHUTDOWN WITH THE NUMBER TWO IDG WAS INO PERATIVE ON MEL. SINCE THERE WAS NO SUITABLE DIVERSION AIRPORT CLOSER, THE FLIGHT CONTINUED TO LAS AND LANDED WITHOUT F URTHER INCIDENT. MAINTENANCE SERVICED THE APU. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007062200162 20070622 00162 EU 2007 6 22 WRNA200700042 1 20070616 A 2560 A5211060100400 GIRT BAR AIRBUS 300 A300B4203 3930306 EU L1 DOOR CORRODED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 821SC 211 DURING REPLACEMENT OF SLIDE, FOUND L1 DOOR SLIDE GIRT BAR ASSEMBLY CORRODED BEYOND LIMITS. REPLACED GIRT BAR ASSEMBLY I AW MM 25-61-15 PG 401. 2 L 7 2 4F RT A35EU 2007062200168 20070622 00168 WP 2007 6 22 UPS07849974 1 20070612 A 5753 CHANNEL DOUG DC8 DC873F 302199F WP T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 LEFT UPPER TRAILING EDGE PANEL FROM OUTBOARD TO INBOARD SIDE Z-CHANNEL CRACKED. REMOVED CRACKED Z-CH ANNEL AT LEFT TRAILING EDGE PANEL FROM OUTBOARD TO INBOARD SIDE IAW SRM 51-1-21D. FABRICATED AND INSTALLED REPAIR Z-CHA NNEL IAW DWG 5707670, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007062200181 20070622 00181 NM 2007 6 22 AWXA200700733 1 20070529 A 5242 143N6939 STRUCTURE BOEING 757 757225 1384959 NM E&E BAY DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 MCN - CRACKED LT FWD RADIUS AT E/E COMPARTMENT DOOR, BS 459 - BS 477, LBL 18, WL 153. REPAIRED LT FWD RADIUS AT E/E CO MPARTMENT DOOR , BS 459 - BS 477, LBL 18,WL 153 IAW B757-200 SRM 51-70-11-0G, FIG 1. 2 L 7 2 4F RT A2NM 2007062200182 20070622 00182 NM 2007 6 22 AWXA200700734 1 20070530 A 5313 143N311027 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 MCN - CRACKED STRINGER, BS 620 - BS 644, S16L. REPLACED STRINGER, BS 620 - BS 644, S16L IAW B757-200 SRM 51-40-02-06, PAR 4, FIG 8 AND PAR 70, FIG 12. 2 L 7 2 4F RT A2NM 2007062200186 20070622 00186 NM 2007 6 22 SWAA073020 1 20070615 A 3350 1619 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007062200193 20070622 00193 NM 2007 6 22 SWAA073022 1 20070615 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007062200194 20070622 00194 NM 2007 6 22 SWAA073015 1 20070615 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007062200205 20070622 00205 NM 2007 6 22 SWAA073024 1 20070615 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 750SA 29802 DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN BETWEEN ROW 3 ABC AND ROW 6 ABC. REMOVED AND REPLAC ED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007062600185 20070626 00185 NM 2007 6 26 SB07048 1 20070620 A 3397 WIRE BOEING 737 7374B7 1384702 NM EMERGENCY LIGHT BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 460UW 25024 FLL - MAINTENANCE REPORTED THE MID-CABIN, FLOOR LEVEL, SEAT END EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPAIRED BROKE N WIRING UNDER SEAT IN ASSOCIATION WITH WIRING SPM. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007062600186 20070626 00186 NM 2007 6 26 2007UALA01688 1 20070525 A 5270 TARGET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE PROX SENSOR DIRTY A UALA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 WP 29 515UA 24840 LEFT AFT ENTRY DOOR EICAS ON GROUND TAXIING IN. INDICATIONS NORMAL AT GATE. *S/D* CLEANED DEBRIS FROM PROXIMITY TARGE T PLATE AND GROUND PROX SENSOR. NO COMPONENTS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062600188 20070626 00188 EU 2007 6 26 2007UALA02007 2 20070614 A 7532 ACTUATOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LT BLEED SYS FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 308UA 23669 RTFL DUE TO LOSS OF LEFT ENGINE BLEED. FOUND FAULTY BLEED AIR REGULATOR. REPLACED BLEED AIR REGULATOR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062600190 20070626 00190 EU 2007 6 26 2007UALA02009 1 20070614 A 5300 STRUCTURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LH EXTERNAL FUSE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 424UA 506 LEFT EXTERNAL FUSELAGE AT STA 204, STR 24L IS DAMAGED. *S/D* MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062600192 20070626 00192 NM 2007 6 26 2007UALA02011 1 20070614 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSLEAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 FLOORBEAM T-CAP CORRODED AT BS 1640. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA. FABRICATED & INSTALLED NEW T-C AP SECTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062600193 20070626 00193 NM 2007 6 26 2007UALA02012 1 20070614 A 3200 DOOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE MLG UNKNOWN A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 197UA 26901 AFTER TAKEOFF GEAR RETRACTED & SOON AFTER GOT EICAS GEAR DOOR MESSAGE WITH SYNOPTIC SHOWING RIGHT BODY GEAR DOOR NOT CLO SED & ASSOCIATED AIRFRAME VIBRATION NOTED. [07-31-07] CYCLED GEAR DOOR NUMEROUS TIMES, OPERATION NORMAL. INSPECTED P RIMARY AND ALTERNATE SENSORS AND TARGETS, ALL OK. ACCOMPLISHED PSEU TEST, PRIMARY AND ALTERNATE INDICATION TESTS ALL PAS SED. UNABLE TO DUPLICATE REPORTED PROBLEM. NO REPEAT OCCURRENCE IN NEXT MONTH OF OPERATION. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072600015 20070726 00015 NM 2007 7 26 AWXA200700849 1 20070705 A 5340 693535222 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961326, CRACKED STRINGER CLIP, BS 787, S24R. REPLACED STRINGER CLIP, BS 787, S24 R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007062600200 20070626 00200 NM 2007 6 26 2007UALA02025 1 20070615 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 727 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 PASSENGER CABIN RT SIDE STA 727 FRAME IS CRACKED AT UPPER I/B CORNER FRAME CUTOUT FOR STR 14R. MAJOR REPAIR ACCOMPLISHE D: FABRICATED & INSTALLED ANGLE & 2EA FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062600201 20070626 00201 NM 2007 6 26 2007UALA02026 1 20070615 A 2611 SMOKE DETECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE AFT CARGO FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 567UA 26673 AFT CARGO SMOKE DETECTOR CHECK FAILS CHECK. [08-07-07] REPLACED NR 1 DETECTOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062600204 20070626 00204 NM 2007 6 26 2007UALA02029 1 20070615 A 5320 ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 695 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 LEFT WW AREA BS 695 INNER CHORD ANGLE CRACKED IN RADIOUS LOCATED JUST ABOVE AND AFT OF UPLOCK. MAJOR REPAIR ACCOMPLISHE D: REMOVED & REPLACED THE ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062600206 20070626 00206 EA 2007 6 26 TRAX200700852 1 20070615 A 5320 CROSSBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 751EV 10163 LT 280 CROSSBEAM CORRODED AND CRACKED. REPAIRED IAW CRJ700 SRM 51-42-21, CRJ700 SRM 51-42-06, CRJ 700 SRM 51-42-00, REO 670-53-11-00026, & REO 670-53-11-047. 2 L 7 2 4F RT A21EA 2007062600212 20070626 00212 NM 2007 6 26 2007UALA02036 1 20070615 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1540 S25-26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 MAIN FRAME, STA 1540 BETWEEN STR 25L-26L, FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR SPLICE AND NEW S PLICE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062600214 20070626 00214 NM 2007 6 26 2007UALA02038 1 20070615 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1460 S25-26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 MAIN FRAME, STA 1460 BETWEEN STR 25L-26L, FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED -J- ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062600216 20070626 00216 NM 2007 6 26 2007UALA02040 1 20070615 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1480 S25-26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 MAIN FRAME, STA 1480 BETWEEN STR 25L-26L, FRAME HAS 2 EACH DENTS. MAJOR REPAIR ACCOMPLISHED: INSTALLED -J- ANGLE REPAI R. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062600217 20070626 00217 NM 2007 6 26 2007UALA02041 1 20070615 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1340, S26R DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 MAIN FRAME, STA 1340, STR 26R, FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED -J- ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062600218 20070626 00218 NM 2007 6 26 2007UALA02042 1 20070615 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1560 S26R DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 MAIN FRAME, STA 1560 AT STR 26R, FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED -J- ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062600222 20070626 00222 NM 2007 6 26 2007UALA02046 1 20070616 A 5313 STRINGER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 360 S15L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 STR SOLICE 15L IS CRACKED ON LOWER FLANGE APPROX ONE HALF INCH AFT OF STA 360 FRAME. MAJOR REPAIR ACCOMPLISHED: REPLAC ED STRINGER SPLICE 15L AT STA 360. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062600223 20070626 00223 NM 2007 6 26 2007UALA02047 1 20070617 A 3200 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU MLG UNKNOWN A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 313UA 23674 AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. CREW USED OVERRIDE TRIGGER TO RETRACT GEAR, WITH FLAP RETRACT TAKEOFF WAR NING HORN SOUNDED. [07-06-07] FOUND RELAY R276 AT FAULT. REPLACED RELAY R276. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062600225 20070626 00225 2007 6 26 2007UALA02049 4 20070617 A 3442 TRANSCEIVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WX SYSTEM FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 576UA 26690 RTFL DUE TO WEATHER RADAR FAILURE. [08-07-07] REPLACED WX RADAR TRANSCEIVER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062600226 20070626 00226 EU 2007 6 26 2007UALA02050 1 20070617 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE BULGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 425UA 508 RIGHT AFT FUSELAGE SKIN AT LAV TANK VENT TUBE WAS FOUND BULGED WITH 3 EA MISSING FASTENERS. SKIN WAS BULGED OUT APPROX .385 INCH WITH EXFOLIATED CORROSION. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062600227 20070626 00227 NM 2007 6 26 2007UALA02051 1 20070617 A 5320 PANEL BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BS 1680 PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 119UA 28812 AFT CARGO COMPARTMENT WALKWAY PANEL AT STATION 1680 RIGHT FOUND PUNCTURE HOLE APPROXIMATELY 1 X 2.5 INCHES. [07-31-07] ACCOMPLISHED REPAIR ON AFT PIT STN 1680 TORQUE BOX UPPER WEB PER SRM 51-70-13. OK FOR RETURN TO SERVICE. SUSPECT CAR GO OR CARGO LOADING IMPLEMENT PENETRATED PANEL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062600228 20070626 00228 NM 2007 6 26 2007UALA02052 1 20070617 A 5313 STRINGER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 368-369 S27L GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 E&E BAY STRINGER 27L HAS HOLE GOUGED IN IT AT STA 368-369 INBOARD SIDE. MAJOR REPAIR ACCOMPLISHED: MFG'D & INSTALLED - U- CHANNEL SECTION REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062600229 20070626 00229 NM 2007 6 26 2007UALA02053 1 20070617 A 4900 APU BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 175UA 24382 CREW REPORTS APU FLAMED OUT AT DEPARTURE TIME. FIRE CARGO AFT EICAS MSG CAME ON AFTER APU FAILED. [07-27-07] AFTER SEVERAL APU SHUT-DOWNS & ABORTED STARTS, CONDUCTED CICADA CHECK OF INLET SCREEN. CLEANED OFF LOT OFF DEAD BUGS. 10% B LOCKAGED LWR PARTS OF INLET SCREEN. APU OPERATES NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062600230 20070626 00230 NM 2007 6 26 2007UALA02054 1 20070617 A 3510 OXYGEN SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 CREW REPORT: CREW O2 LOW. [07-06-07] SERVICED O2 TO FULL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062700004 20070627 00004 EA 2007 6 27 N6WA00706001 1 20070613 A 3397 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS DISCONNECTED A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 163 10255 EMERGENCY LIGHTS INOP AT LOWER AFT SERVICE DOOR, CLASS DIVIDER, ROW 12 CEILING FWD. FOUND DISCONNECTED CONNECTOR ON RT S IDE OF CEILING PANEL AT ROW 6, RECONNECTED AND OPS CHECK GOOD IAW MM 33-51-00. 2 L 7 2 4F RT A21EA 2007062700009 20070627 00009 CE 2007 6 27 DXTA200702268 1 20070616 A 4910 UNKNOWN CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE APU SMOKE E DXTA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 677QS 5605367 GROUND CONTROLLERS REPORTED SMOKE FROM RT SIDE OF AIRPLANE. UPON APU SHUTDOWN, SMOKE WAS OBSERVED COMING FROM APU INTAKE AND EXHAUST. BOTH RED AND YELLOW APU OIL LIGHTS ILLUMINATED. APU OIL LEVEL WAS VERIFIED NORMAL PRIOR TO THIS EVENT. [ 07-09-07] REMOVED AND REPLACED APU IAW 560XL MM 49-10-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007062700011 20070627 00011 CE 2007 6 27 DXTA200702270 1 20070617 A 2120 UNKNOWN BEECH MU300 400A 1155402 CE SMOKE E DXTA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 139QS RK483 NOTICED SMOKE COMING FROM AIR CONDITIONING VENTS, SMOKE FILLED LAV AREA. [07-10-07] REMOVED AFT EVAPORATOR MODULE AND INSTALLED NEW EVAPORATOR MODULE RECEIVED NEW FROM RAPID. SYSTEM SERVICED IAW HAWKER 400XP MM 12-00. PERFORMED OPERATION CHECK OF AIR CONDITIONING SYSTEM IAW 21-51-00. OP CHECKS GOOD. 2 H 7 2 4F RT A16SW 2007062700016 20070627 00016 SO 2007 6 27 N93A15062007 1 20070615 A 3297 1159SCAV4581 WIRE HARNESS GULSTM G1159 GIV 3980115 SO PWA PT6 PT6* 52043 EA NLG UNKNOWN E N93A O OTHER J WARNING INDICATION LD LANDING 1 SO 13 420QS 1320 NOSE WHEEL STEERING FAIL MESSAGE ON TOUCH DOWN 2 L 7 2 4F 3 T RT A12EA E2NE 2007062700021 20070627 00021 SO 2007 6 27 135N69SC 2 20070612 A 8530 CYLINDER CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO NR 6 FAILED E HYIA E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 NE 01 69SC 402C0041 831969R LEFT ENGINE FAILURE WITH CASE PENETRATION BELIEVED TO BE CAUSED BY A VALVE FAILURE AT THE NR 6 CYLINDER. A TCM ENGINEER WAS ON HAND AT THE TIME AND THE ENGINE HAS BEEN SENT TO TCM FOR TEARDOWN. LEFT ENGINE WAS REMOVED AND REPLACED AS A CO RRECTIVE ACTION ON 6/13/2007. 1 L 7 2 3O 3 O A7CE E8CE 2007062700024 20070627 00024 SO 2007 6 27 SIMA200717104 1 20070619 A 2760 M835366022M RELAY EMB 145 EMB145LR 3260212 SO SPOILERS FAILED A SIMA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SW 21 667GB 8640 145784 SPOILER FAIL MESSAGE, ABORTED TAKEOFF AT 50 KNOTS. REMOVED AND REPLACED RELAYS K0059, K0112, K4363 AND K4363 IAW EMB AM M 20-13-02 AND OPERATIONAL CHECKED IAW AMM 37-63-01 WITH NO DEFECTS. PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007062700025 20070627 00025 EU 2007 6 27 SIMA200717101 1 20070616 A 2910 8120 DUMP VALVE SAAB SF340 340B 7860101 EU ZONE 200 FAILED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 323AE 23074 340B323 MAIN HYDRAULIC PRESSURE DROPS FROM 3000 PSI TO 2100 PSI WITHIN 35 SECONDS ON GROUND AND INFLIGHT. REMOVED AND REPLACED HYDRAULIC ACCUMULATOR PRESSURE DUMP VALVE IAW SAAB AMM. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007062700026 20070627 00026 SO 2007 6 27 SIMA200717102 1 20070618 A 3350 3025103 LIGHT EMB 135 EMB135KL 3260302 SO ZONE 600 FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 825AE 12520 145589 RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT EMERGENCY EXTERNAL WING LIGHT IAW EMB 53-04-10 A ND PERFORMED OPERATIONAL CHECK IAW EMB AMM 33-50-00 WITH NO DEFECTS. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007062700028 20070627 00028 SO 2007 6 27 SIMA200717105 1 20070619 A 2760 8005701 SWITCH EMB 145 EMB145LR 3260212 SO ZONE 700 FAILED A SIMA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SW 21 667GB 8641 145784 SPOILER FAIL MESSAGE, ABORTED TAKEOFF AT 50 KNOTS. REMOVED AND REPLACED NOSE LANDING GEAR WEIGHT ON WHEEL SWITCH IAW EM B AMM 32-63-02. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007062700037 20070627 00037 EU 2007 6 27 07FDEA01904 1 20070521 A 5100 NONE AIRBUS 310 A310222 3930315 EU NONE NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON RT LOWER WING SURFACE OF INBOARD FLAP WS 139-207 RIB 3-4. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR CONFORMS TO EXISTING FEDEZ EA 6-5750-81811. SDR SUBMITTED IN ERROR- ADMINISTRATOR. 2 L 7 2 4F RT A35EU 2007062700044 20070627 00044 NM 2007 6 27 07FDEA02219 1 20070620 A 5712 RIB DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 575FE 48500 RIGHT WING FIXED LEADING EDGE RIB FOUND CRACKED AT XOS 911. [07-06-07] CRACKED RIB REMOVED AND REPLACED AS PER SRM 51- 33-01 VOLUME II. NEW RIB FABRICATED PER DOUGLAS DRAWING ARB2921. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062700049 20070627 00049 NM 2007 6 27 DHL2007742009 1 20070620 A 5320 SUPPORT ANGLE BOEING 727 727225 1384077 NM BS 1273 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 DURING AN "A" CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED, CRACK INDICATION ON RT AIRSTAIR ACTUATOR SUPPORT ANGLE INSI DE TORQUE BOX WEB AT BS 1273. REMOVED CRANKED ANGLE AT RT TORQUE BOX BS 1273 IAW B727 SRM 51-30-2 FIG 7. FABRICATED NE W SUPPORT ANGLE, MAT BAC1503-100145, PO NR 7185277(27") IAW B727 SRM 53-10-2 FIG 6 AND DRAWING NR 65C27136 REV B. TREAT ED AND PRIMED ANGLE IAW B727 SRM 51-10-2. INSTALLED NEW SUPPORT ANGLE AT RT TORQUE BOX BS 1273 IAW B727 SRM 51-30-2 FIG 4. 2 L 7 3 4F A3WE 2007062700050 20070627 00050 NM 2007 6 27 DHL2007740557 1 20070618 A 5522 SKIN BOEING 727 7272Q9 138448M NM RT ELELVATOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 RT ELEVATOR UPPER SKIN HAS 3 DENTS AT ELEV STA'S 40-0, 47.0, AND 79.0 APPROX. DENT AT ELEV STA 40.0 WITHIN LIMITS. 2 D ENTS EVALUATED AS BEYOND LIMITS, AT ELEV STA 47.0 (DENT 1) AND 79.0 (DENT 2). CUT OUT DAMAGE; DENT 1" BY 1" AND DENT 2 .25" BY .75". FABRICATED REPAIR DOUBLERS, NR 1 FROM 2024-T3, .032" BY 8.25" BY 3.125"; NR 2 FROM 2024-T3, .032" BY 3. 25" BY 2.5", PO NR 9005049, PER B727 SRM 55-20-3 FIG 1. TREATED, PRIMED, AND INSTALLED 2 REPAIR DOUBLERS PER B727 SRM 5 1-10-2 AND 55-20-3 FIG 1. COMPLIED WITH REBALANCE REQUIREMENTS OF B727 SRM 51-80-7: CALCULATIONS REVEALED NO REBALANCE REQUIRED FOR WEIGHT CHANGE AT REPAIR MOMENTS. 2 L 7 3 4F RT A3WE 2007062700051 20070627 00051 EA 2007 6 27 QXEA20071009 1 20070619 A 2810 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA RT ENGINE LEAKING A QXEA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 NM 09 602QX 10010 DEN - FLIGHT 4325 - SMALL FUEL DRIP FROM THE RIGHT ENGINE. MAINTENANCE GROUND RAN THE ENGINE AND CLEANED THE AREA. NOT ICED NO LEAKS OR DEFECTS. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007062700052 20070627 00052 NM 2007 6 27 AWXA200700750 1 20070601 A 5313 654988621 STRINGER BOEING 737 73733A 1384673 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - CORROSION ON STRINGER 27L, BS 381 AND BS 384. REPAIRED STRINGER 27L, BS 360 - BS 390 IAW B737-300 SRM 53-00-03-2R1, FIGURE 201. 2 L 7 2 4F RT A16WE 2007062700055 20070627 00055 NM 2007 6 27 AWXA200700753 1 20070417 A 5330 6545774 SKIN BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - CRACKED FUSELAGE SKIN, BS 727D + 12" - BS 780, S22L - S24L. REPAIRED FUSELAGE SKIN, BS 727D + 12" - BS 780, S22L - S24L IAW AWA ER 03-5361-07166-ES1. 2 L 7 2 4F RT A16WE 2007062700058 20070627 00058 EU 2007 6 27 F3LA200700131 1 20070610 A 5310 D539749600000 DOOR FRAME AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 907FR 5061 1743 DURING C4/S1 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR FRAME 61 COVER SHEET FOR NUT PLATES CORRODED AROUND SEVERAL RIVET HEADS. REMOVED AND REPLACED WEB IAW A319 SRM 51-42-11 AND 51-44-21. 2 L 7 2 4F RT A28NM 2007062700059 20070627 00059 EA 2007 6 27 QXEA20071011 1 20070618 A 3620 GG670800053 SENSOR CNDAIR CL600 CL6002C10 1390015 EA RT ENGINE FAILED A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 601QX 1039 10009 TUL- FLIGHT 4202, JUST AFTER ROTATION RECEIVED A RIGHT ENGINE BLEED CAUTION MESSAGE. PERFORMED THE CHECKLIST AND NO FUR THER ACTION TAKEN. MAINTENANCE REPLACED THE LEFT BLEED AIR TEMP SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007062700061 20070627 00061 NE 2007 6 27 HALA0700260 2 20070619 A 7397 WIRE BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE FMU SHORTED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 593HA 33424 ETOPS SIGNIFICANT SYSTEM, R ENG SHUTDOWN DID NOT DISPLAY AND AURAL WARNING AND APPROPRIATE ENGINE RELATED MESSAGES WERE NOT INHIBITED WITH ENG SHUTDOWN. REMOVED AND REPLACED RT ENGINE FUEL METERING UNIT PER AMM 73-21-01, CONDITION SAME FOU ND CONNECTOR WIRES SHORTED TO CASE. REPAIRED PER SWPM 20-10-13. OPS CHK FMU AND LEAK CHK GOOD, 73-21-01, NO LEAKS NOTE D. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062700066 20070627 00066 NM 2007 6 27 DHL2007740011 1 20070619 A 5410 NOSE COWL BOEING 727 727225 1384077 NM NR 1 NACELLE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 NR 1 ENG NOSE COWL AT O/B SIDE 9 O`CLOCK POSITION HAS EXISTING REPAIR PULLING LOOSE AND CHAFF MARK. REMOVED PREVIOUS RE PAIR IAW B727 SRM 51-30-2 FABRICATED NEW REPAIR USING 2024-T3 .040 PO#9005138 DIM 9" BY 4" AND FILLER USING 2024T3 .032 PO NR 9005049 DIM 5" BY 2 3/4 IAW B727 SRM 54-30-2 FIG 1. ALODINED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTA LLED PARTS IAW B727 SRM 54-30-3 FIG 8. 2 L 7 3 4F A3WE 2007062700071 20070627 00071 NM 2007 6 27 QXEA200700982 1 20070609 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - SEAT TRACK NR 16 HAS CORROSION AT STATION X783. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007062700075 20070627 00075 NM 2007 6 27 QXEA200700981 1 20070609 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 783 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - SEAT TRACK NR 9 HAS CORROSION AT STATION 783. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007062700077 20070627 00077 NM 2007 6 27 QXEA200700983 1 20070609 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 125 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - NR 1 SEAT TRACK HAS MINOR PITTING CORROSION AT STATION 125.5. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007062700079 20070627 00079 NM 2007 6 27 QXEA200700992 1 20070614 A 5310 DOOR FRAME BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY EXIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - CORROSION UNDER SILL PLATE OF FORWARD RIGHT EMERGENCY EXIT. REPAIRED IAW RD8/4-53-1942. 2 H 7 2 4T RT A13NM 2007062700081 20070627 00081 NM 2007 6 27 QXEA200700994 1 20070609 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 83 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - NR 1 SEAT TRACK HAS CORROSION ON PREVIOUSLY BLENDED AREA AT STATION 83.0. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007062700083 20070627 00083 NM 2007 6 27 QXEA200700989 1 20070610 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 351 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - SEAT TRACK NR 19 HAS MINOR PITTING CORROSION AT STATION 351. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007062700084 20070627 00084 NM 2007 6 27 QXEA200700993 1 20070609 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 603-612 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - SEAT TRACK NR 14 AT STATION X603 TO X612 HAS MINOR SCRATCHES AND CHAFES. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007062700086 20070627 00086 NM 2007 6 27 QXEA200700987 1 20070610 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 216 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - SEAT TRACK NR 18 HAS MINOR PITTING CORROSION AT STATION 216. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007062700095 20070627 00095 NM 2007 6 27 AALA20071056 1 20070612 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 928AN 39103 TUL - EMERGENCY LIGHT BATTERY PACK AT LEFT OVERWING EXIT FAILED OPERATIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK AT LEFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007062700096 20070627 00096 NM 2007 6 27 AALA20071047 1 20070524 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 766AN 32880 AFW - EMERGENCY LIGHT BATTERY PACK M33093 FAILED OPERATIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK M33093. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007062700098 20070627 00098 NM 2007 6 27 AALA20071048 1 20070524 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 766AN 32880 AFW - EMERGENCY LIGHT BATTERY PACK M33096 FAILED OPERATIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK M33096. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007062700099 20070627 00099 NM 2007 6 27 AALA20071050 1 20070524 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 766AN 32880 AFW - EMERGENCY LIGHT BATTERY PACK M33098 FAILED OPERATIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK M33098. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007062700100 20070627 00100 2007 6 27 QXEA200701013 4 20070620 A 3440 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA WINDSHEAR WARN UNKNOWN A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 616QX 10128 DEN FLIGHT NR 4334, AFTER TAKEOFF RECEIVED A RED WINDSHEAR WARNING. AFTER RECOVERY RECEIVED "R ITT EXCEED B" MESSAGE. WENT TO "MAX THRUST" APPROXIMATELY 5-10 SECONDS. MAINTENANCE REQUESTED A RETURN TO FIELD. INTERROGATED MDC AND FOUND A PR DID NOT EXCEED 5 MINUTES. NO PARTS REPLACED. AIRCRAFT K FOR CONTINUED SERVICE PER AMM 71-00-00-866-801-AA1, PAGE 24 8. 2 L 7 2 4F RT A21EA 2007062700101 20070627 00101 NM 2007 6 27 QXEA200700998 1 20070613 A 5710 BARREL NUT BOMBDR DHC8 DHC8402 1390042 NM WING TO BODY CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX-LEFT HAND WING TO FUSELAGE FORWARD MOUNT VERTICAL TIE BOLTS HAVE CRACKED BARREL NUTS. REPAIRED IAW RD8/4-51-102. 2 H 7 2 4T RT A13NM 2007062700102 20070627 00102 NM 2007 6 27 QXEA200700995 1 20070614 A 5310 DOOR FRAME BOMBDR DHC8 DHC8402 1390042 NM PAX DOORWAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - MAIN CABIN DOOR FORWARD APERTURE FRAME HAS A CHAFE FROM FLOOR PANEL 131CZ AT STATION X1.00. REPAIRED IAW RD8/4 -53-1941. 2 H 7 2 4T RT A13NM 2007062700103 20070627 00103 NM 2007 6 27 QXEA200700996 1 20070609 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 274-573 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - SEAT TRACK NR 14 AT STATION X274 TO 573 HAS MINOR SCRATCHES AND CHAFES. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007062700105 20070627 00105 NM 2007 6 27 07FDEA02226 1 20070620 A 5753 SKIN BOEING 727 727233 138408A NM LT WING TE FLAP MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 286FE 22623 AGING A/C INSPECTION, FOUND EXISTING REPAIR LOCATED AT LT WING AFT FLAP UPPER SURFACE 18" FROM I/B END 12" FROM T/E DID NOT CONFORM TO SRM 51-40-20 PARA 7. REMOVED PREVIOUS REPAIR AND BONDED ON NEW REPAIR REF SRM 51-40-20 PARAGRAGHS 7, 14, 15, 18, 20, 21, AND 22 TAP TEST GOOD, PRIMED AND PAINTED REF MM 51-20-151-7. 2 L 7 3 4F RT A3WE 2007062700106 20070627 00106 NM 2007 6 27 07FDEA02227 1 20070620 A 5753 BAC14902734 FLAP TRACK BOEING 727 727233 138408A NM NR 5 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 NR 5 FLAP TRACK FAIRING INBD MIDDLE ATTACH BRACKET IS CRACKED. THIS SDR WAS ENTERED IN ERROR. THIS IS A DUPLICATE OF T RACKING NR 07-2224 KEEP NR 07-2224 AS ORIGINAL AND ACTIVE. THIS SDR WAS SUBMITTED IN ERROR- ADMINISTRATOR. 2 L 7 3 4F RT A3WE 2007062700108 20070627 00108 NM 2007 6 27 07FDEA02229 1 20070620 A 5712 ARB293113 RIB DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 575FE 48500 LT WING FIXED LEADING EDGE CAVITY AT XORS = 492 RIB STIFFENER FOUND CRACKED. [07-09-07] REMOVED CRACKED RIB STIFFENER AND FABRICATED NEW RIB STIFFENER AS PER DOUGLAS DRAWING ARB2931. INSTALLED NEW RIB STIFFENER AT LT WING FIXED LEADING E DGE CAVITY AT XORS 492. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062700111 20070627 00111 NM 2007 6 27 07FDEA02232 1 20070621 A 5347 A5A7082501 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT BS 5-23 TO 5-33 LT X = 75 FOUND WITH CORROSION. [06-29-07] REPAIR CARR IED OUT AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062700112 20070627 00112 WP 2007 6 27 07FDEA02233 1 20070621 A 5330 SKIN DOUG DC10 DC1010 3022110 WP ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 387FE 46621 EXISTING REPAIR EXT FUS FROM STA 1901 TO 1921 BETWEEN LONGERONS 37 LT AND 35 LT REPAIRED IAW SRM 53-20-00 FIG 6 VOL I. 2 L 7 3 4F A22WE 2007062700115 20070627 00115 NM 2007 6 27 07FDEA02236 1 20070621 A 5320 65609924 STRUCTURE BOEING 727 727233 138408A NM BS 720D-720E CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LWR FWD CARGO PIT, CORROSION ON LT AND RT SIDES AT MOUNTING HOLES, FWD OF WORK PLATFORM THATS AT STA 720D TO 720E. ACCO MPLISHED 2 TYPICAL FORMED REPAIRS AT STA 720D AND STA 720E LOWER CARGO PIT WORK PLATFORM PANEL REF SRM 51-40-3 PG 1-6. 2 L 7 3 4F RT A3WE 2007062700117 20070627 00117 NM 2007 6 27 07FDEA02238 1 20070621 A 5740 652678930 ATTACH ANGLE BOEING 727 727233 138408A NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 RT WING O/B T/E UPPER SURFACE PANEL JUST INBD OF AILERON, JACKSCREW FAIRING ATTACH ANGLE CRACKED INSIDE FAIRING. REMOVE D DAMAGED ANGLE, DRILLED UP, PRIMED AND PAINTED NEW ANGLE ON PANEL INBD OF AILERON, REF SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007062700122 20070627 00122 NM 2007 6 27 07FDEA02243 1 20070621 A 5320 FLOOR SUPPORT BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT PIT STRINGER CLIP FLOOR SUPPORT ANGLE CORRODED STA 950F, STR 29L REMOVED FLOOR SUPPORT, ORDERED NEW FLOOR SUPPORT. FABRICATED SHIM AND DRILLED UP. INSTALLED NEW FLOOR SUPPORT AND SHIM REF SRM 51-30-2 PG 3, 5-7, SRM 51-10--2 PG 1, S RM 51-20-1, FIG 10. 2 L 7 3 4F RT A3WE 2007062700123 20070627 00123 NM 2007 6 27 07FDEA02244 1 20070621 A 5320 651960247 FLOOR SUPPORT BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 UPPER MAIN DECK FLOOR SUPPORT STRUCTURE, INTERCOSTAL LWR STRAP HAS CORROSION (VIEW FROM PIT) FROM STA 1115 TO 1130, RBL 46. REMOVED CORROSION AT STA 1115 TO 1130 RBL 46, IAW B727 SRM 51-10-6. 100 PERCENT MATERIAL LOSS, OUT OF LIMITS. RE MOVED DAMAGED SECTION OF FLOOR STABILIZER IAW SRM 51-40-2 FIG 1. FABRICATED REPAIR PLATE FROM 7075-T6 .040, TREATED AND PRIMED REPAIR PLATE IAW SRM 51-10-2. INSTALLED REPAIR PLATE IAW SRM 51-40-2. 2 L 7 3 4F RT A3WE 2007062700125 20070627 00125 NM 2007 6 27 DHL2007782507 1 20070417 A 5320 STRUCTURE BOEING 727 727227 1384078 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 782DH 21998 CORROSION AT UPPER AND LOWER CHORD AND SPLICES, AIRSTAIR CUTOUT BS 1223 LBL22- RBL22, BELOW STEP. REMOVED FASTENERS AND UPPER AND LOWER SPLICES FOR ACCESS IAW B727 SRM 51-30-2. FOUND 3 SPLICES OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. RE MOVED CORROSION FROM UPPER AND LOWER CHORD IAW B727 SRM 51-10-6. ORIGINAL MATERIAL THICKNESS .100 IAW B727 SRM 53-10-2 F IG 6 AND BOEING DWG 65-17512, MATERIAL LOSS FOR LOWER CHORD .008, REMAINING MATERIAL THICKNESS .092. FOUND WITHIN LIMIT S IAW B727 SRM 53-10-1 FIG 1. MATERIAL LOSS FOR UPPER CHORD .016, REMAINING MATERIAL .084, FOUND WITHIN LIMITS IAW B727 SRM 53-10-1 FIG 1 (SEE CONTINUATION ON NR# 137781). TREATED AND PRIMED CHORDS IAW B727 SRM 51-10-2. FABRICATED 3 NEW 2 L 7 3 4F A3WE 2007062700128 20070627 00128 SO 2007 6 27 CHQA200700026 1 20070619 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO ODOR A CHQA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 11 281SK 145391 FLIGHT 6248 - RIC-CVG - DURING DESCENT, A BURNING SMELL FILLED THE CABIN AND COCKPIT, NO VISIBLE SMOKE. APU WAS OFF, PA CKS WERE ON. CREW CYCLED PACK SWITCHES AND NOTED SMELL SEEMED TO BE COMING FROM PACK NR 2. MAINTENANCE PERFORMED AN OP S CHECK OF THE LEFT AND RIGHT PACK SYSTEMS IAW ERJ MM 21-00-00. NO SMELLS NOTED AT THIS TIME. 2 L 7 2 4T RT T00011AT 2007062700132 20070627 00132 NM 2007 6 27 AWXA200700757 1 20070422 A 5330 654577566 SKIN BOEING 737 73733A 1384673 NM BS 796 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - CORROSION ON FUSELAGE SKIN INTERIOR SURFACE, BS 796, S23R - S25R. REPAIRED FUSELAGE SKIN INTERIOR SURFACE, BS 796, S23R - S25R IAW B737-300 53-00-01-2R32, FIGURE 201. 2 L 7 2 4F RT A16WE 2007062700134 20070627 00134 NM 2007 6 27 AWXA200700754 1 20070620 A 3350 BATTERY PACK BOEING 737 7373G7 1384595 NM EMERGENCY LIGHTS INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 302AW 24009 SEA - EEL - EMERGENCY PATHWAY LIGHTS FROM ROW 20 TO 23 INOP. MX FOUND BATTERY POWER PACK FUSES BAD. MX REPLACED THE FU SES. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2007062700135 20070627 00135 NM 2007 6 27 AWXA200700758 1 20070618 A 5297 BMS13311122 WIRE BOEING 737 7373S3 1384711 NM DOOR SENSOR BROKEN A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 313AW 23712 PHX - DFW - EL - CREW REPORTED DURING CLIMB, WERE NOT ABLE TO PRESSURIZE THE A/C. CREW DECLARED AN EMERGENCY AND RETURN ED TO PHX. MX FOUND BROKEN WIRE ON E/E DOOR SENSOR SWITCH S197. MX REPAIRED WIRE IAW MM CH 20. EQUIPMENT DOOR LIGHT A ND WARNING OPERATIONAL CHECKS WERE GOOD. THE A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007062700136 20070627 00136 EA 2007 6 27 SWIA200718347 1 20070617 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA RIGHT SMOKE A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 454SW 7749 PASSENGERS AND FLIGHT ATTENDANT REPORTED SMOKE IN ROW 12, RETURNED TO TULSA. FOUND TO BE CONDENSATION FROM RIGHT PACK S YSTEM DUE TO HIGH HUMIDITY. 2 L 7 2 4F RT A21EA 2007062700137 20070627 00137 NE 2007 6 27 SWIA200718348 2 20070617 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RIGHT UNKNOWN A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 960SW 7853 RIGHT ENGINE OIL MESSAGE CAME ON IN FLIGHT WITH ENGINE OIL PRESSURE AT 0° ON SHORT FINAL. REPLACED RIGHT ENGINE PER AM M 71-00-00. OPS AND LEAK CHECK GOOD, P/N: CF34-3B1, S/N ON: 873098, S/N OFF: 873799. 2 L 7 2 4F 4 F RT A21EA E15NE 2007062700139 20070627 00139 EA 2007 6 27 SWIA200718350 1 20070618 A 3520 OXYGEN MASK CNDAIR CL600 CL6002B19 1900309 EA CABIN UNWANTED DEPLOY A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 416SW 7089 OXYGEN MASKS FROM PANEL OVER SEATS 12A AND 12B DEPLOYED DURING CLIMB-OUT. RETURNED TO FIELD. INSPECTED AND RESTOWED O2 MASKS. 2 L 7 2 4F RT A21EA 2007062700141 20070627 00141 EA 2007 6 27 SWIA200718352 1 20070615 A 2760 PCU CNDAIR CL600 CL6002C10 1390015 EA SPOILERS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 709SK 10159 RIGHT OUTBOARD SPOILERON DEPLOYED IN FLIGHT. REPLACED RIGHT MULTIFUNCTION SPOILER PCU IAW AMM 27-62-01. OPS CHECKS GOO D, P/N: 51200-11, S/N OFF: MAL-0776. 2 L 7 2 4F RT A21EA 2007062700142 20070627 00142 SO 2007 6 27 SWIA200718353 1 20070617 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DAMAGED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 567SW 120342 FOUND EMERGENCY EXIT SIGN OVER ROW 9 IS INOP. REPLACED SPLICE FOR EXIT SIGN AT ROW 9. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007062700148 20070627 00148 EA 2007 6 27 SWIA200718359 1 20070523 A 5210 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 774SK 10240 PAX DOOR CRACKED ON FORWARD SIDE OF STEP NR 2. INSTALLED EXTERNAL DOUBLER AND REPAIR ANGLES PER CRJ700/900 SRM 51-42-06 . 2 L 7 2 4F RT A21EA 2007062700149 20070627 00149 EA 2007 6 27 SWIA200718360 1 20070524 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 776SK 10241 PAX DOOR AFT WEB IS CRACKED IN 2 PLACES BETWEEN SECOND AND THIRD STEPS, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS P ER BOMBARDIER REO 670-52-11-104 REV B. 2 L 7 2 4F RT A21EA 2007062700150 20070627 00150 EA 2007 6 27 SWIA200718361 1 20070524 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 776SK PAX DOOR FORWARD WEB IS CRACKED AT SECOND STEP, DISCOVERED AT C-CHECK. REPAIRED FORWARD PAX DOOR WEB PER CRJ7/9 REO 670 52-11-104. 2 L 7 2 4F RT A21EA 2007062700152 20070627 00152 EA 2007 6 27 SWIA200718363 1 20070529 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 778SK 10242 PAX DOOR AFT WEB IS CRACKED AT SUPPORT BRACKET, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLES AND EXTERNAL DOUBLER IAW REO 670-52-11-104 P 2-6. 2 L 7 2 4F RT A21EA 2007062700153 20070627 00153 EA 2007 6 27 SWIA200718364 1 20070421 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT MLG WW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 926SW 7687 BRAKE TRANSDUCER BRACKET IS CRACKED IN RIGHT WHEEL WELL, DISCOVERED AT C-CHECK. REPLACED RIGHT BRAKE TRANSDUCER BRACKET IAW CRJ200 SRM 51-77-00 PG 1 PARA 3. 2 L 7 2 4F RT A21EA 2007062700160 20070627 00160 EA 2007 6 27 VNAA0706005 1 20070606 A 5100 NONE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE NONE NONE A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 708PS 10160 CLT - FLT 2292 - CREW REPORTED ON TAKEOFF SEVERAL BIRDS STRUCK THE AIRCRAFT ON THE RIGHT WING, THE NOSE WHEEL ASSEMBLY A ND ALSO THE RIGHT ENGINE. CREW CONTINUED ON TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE RIGHT WING F OR DAMAGE AND FOUND NO DAMAGE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007062700167 20070627 00167 2007 6 27 UIEA200700237 4 20070603 A 2220 ALTIMETER BOEING 747 747243B 1384830 NM OUT OF LIMITS A UIEA O OTHER J WARNING INDICATION CR CRUISE 1 EA 15 517MC 23300 A A/P PORPOISED 200-300' ABOVE AND BELOW SELECTED ALTITUDE AT FL 410 IN CRUISE. A/P OK. TRANSFERRED TO DMI M07-117IAW MEL 22-1-2B CAT C. A/C IS CAT II RESTRICTED. 2 L 7 4 4F A20WE 2007062700169 20070627 00169 NM 2007 6 27 UIEA200700239 1 20070610 A 5322 SHEAR TIE BOEING 747 747243B 1384830 NM BS 860 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 BS 860R FRAME TO TENSION TIE CONNECTION FOUND HOLE NR 9 HOLE CRACKED AT FORWARD CHANNEL. BS 860 FRAME TO TENSION TIE CO NNECTION CRACKED FORWARD CHANNEL REPAIRED AS PER BOEING MESSAGE 1-339630379-21-1 AND FAA 8100-9. 2 L 7 4 4F A20WE 2007062700170 20070627 00170 NM 2007 6 27 UIEA200700240 1 20070610 A 5322 SHEAR TIE BOEING 747 747243B 1384830 NM BS 880 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 BS 880R FRAME TO TENSION TIE CONNECTION FOUND CRACKED HOLE NR 5 AT FRAME. BS 880R FRAME TO TENSION TIE CONNECTION CRACK ED FRAME REPAIRED AS PER BOEING MESSAGE 1-339629649-2 AND FAA FORM 8100-9. 2 L 7 4 4F A20WE 2007062700176 20070627 00176 EA 2007 6 27 TRAX200700854 1 20070615 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 751EV 10163 RT 280 BULKHEAD LOWER WEB CORRODED. REPAIRED IAW CRJ700 SRM 51-42-06, REO 670-53-11-052, SRM 51-00-00, AND EO 700-5 3-0062. 2 L 7 2 4F RT A21EA 2007062700178 20070627 00178 EA 2007 6 27 TRAX200700857 1 20070615 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA BS 349-364 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 751EV RT SEAT TRACK CORRODED BETWEEN FS349-364. REPAIRED IAW SRM`S 53-21-49 AND 51-21-06, AND 51-41-02. 2 L 7 2 4F RT A21EA 2007062700179 20070627 00179 EA 2007 6 27 TRAX200700858 1 20070615 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA CABIN WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 889AS 7538 PAX DOOR 'EXIT' PLACARD WORN. REMOVED AND REPLACED PAX DOOR 'EXIT' PLACARD IAW CRJ 200 AMM 11-30-00. 2 L 7 2 4F RT A21EA 2007062700180 20070627 00180 NM 2007 6 27 2007UALA02076 1 20070618 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE MID GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 MID GALLEY EEL CROSS AISLE LIGHT IS INOPERATIVE. *S/D* REPLACED LIGHT STRIP. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062700181 20070627 00181 NM 2007 6 27 2007UALA02078 1 20070616 A 3350 767 LAMP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 217UA 30550 DOOR 1R EXTERIOR EMERGENCY EXIT SLIDE LIGHT INOP. *S/D* REPLACED LAMP, OP CHECKED OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007062700182 20070627 00182 NM 2007 6 27 2007UALA02109 1 20070618 A 3397 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 AFT GALLEY RIGHT EEL STRIP IS INOP. *S/D* SECURED FEEDER CABLE. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062800002 20070628 00002 NM 2007 6 28 2007UALA02111 1 20070618 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 ALL RIGHT AISLE CEILING EEL LIGHTS ARE INOP FROM ROW 31 TO AFT GALLEY. *S/D* SECURED BATTERY CONNECTOR. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062800003 20070628 00003 NM 2007 6 28 2007UALA02112 1 20070618 A 3350 1317 LAMP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 AFT RIGHT & LEFT DOOR EXTERNAL EEL LIGHTS ARE INOPERATIVE. *S/D* RELAMPED, CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062800004 20070628 00004 NM 2007 6 28 2007UALA02136 1 20070620 A 3397 78671 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 SEAT 40ABC EEL LIGHT STRIP CONNECTOR PULLED ON SEAT SIDE. *S/D* REPAIRED EEL LIGHT STRIP CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062800005 20070628 00005 NM 2007 6 28 2007UALA02145 1 20070619 A 3350 D71701100 BATTERY PACK BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 777UA 26916 ALL EEL LIGHTS IN -D SECTION- INOPERATIVE. *S/D* AFTER TROUBLESHOOTING, DETERMINED THAT BATTERY PACK M33401 HAD FAILED . INSTALLED SERVICABLE PACK. SYS OPS NORMAL. RETURNED AC BACK TO NORMAL, OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007062800006 20070628 00006 SO 2007 6 28 C2XA07ON008 1 20070621 A 2824 2770138101 FLAPPER VALVE EMB 145 EMB145LR 3260212 SO LT WING MISSING A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 27 13553 585 FLT 41 - GEG TO GEG - FUEL LEAKING FROM LEFT WING DURING CLIMB. MX REPO'D 568 FROM ONT WITH MX PERSONAL AND PARTS. MX INSPECTED FUEL TANK AND FOUND MOST O/B FLAPPER VALVE MISSING ON LEFT WING. MX INSTALLED NEW LEFT WING FLAPPER VALVE AND PERFORMED OPERATIONAL CHECKS SUCCESFULLY. THE A/C WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007062800007 20070628 00007 WP 2007 6 28 07FDEA02262 1 20070622 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CLG WHEEL WELL CAVITY, CORROSION ON FUSELAGE SKIN INTERIOR SURFACE AT STA 1441, LONGERON 51R TO 51L. SKIN SECTION FRO M 1401 TO 1541 IS BEING REPLACED ON N/R N00616 ATTACHED EA 8-5330- 112939/FUSELAGE-SKIN SPLICE AT STA.1381-1531,L48LTO L48R-REPAIR. 2 L 7 3 4F RT A22WE 2007062800085 20070628 00085 2007 6 28 SWAA073056 4 20070619 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007062800086 20070628 00086 NM 2007 6 28 USAA070464 1 20070608 A 5320 143N832854 ANGLE BOEING 757 7572B7 1384964 NM BS 719-745 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 BS 719.6 - 745.6 RBL 62.45 ANGLE HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-30-15, 51-10-02, 51-40-02, DEFECT SIZE: 6 X 1 INCHES. 2 L 7 2 4F RT A2NM 2007062800087 20070628 00087 EU 2007 6 28 YENA2007054 1 20070619 A 3610 342B030000 CONTROLLER AIRBUS 320 A320232 3930326 EU AIR VALVE INOPERATIVE A YENA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 542JB 14258 10218 1802 ON CLIMBOUT NOTICED PACK A FAULT & ENGINE 1 BLEED FAULT. INITIATED DESCENT TO 10K. FOLLOWED ECAM QRC & QRH. REMOVED N R 1 ENG FAN AIR THERMOSTAT 7170HM1 PER 36-11-43-04 AS PER PFR FAULT. INSTALLED FAN AIR VALVE CONTROL THERMOSTAT PER36-1 1-43-04. OPS CHECK OK. 2 L 7 2 4F RT A28NM 2007062800088 20070628 00088 EU 2007 6 28 USA2007F00000 1 20070518 A 5310 STRUCTURE AIRBUS A321 A321211 3930370 EU CFMINT CFM56 CFM565B3P 13006 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 178US 21305 1519 CORRODED RIVET TAILS WERE FOUND IN FUSELAGE CARGO COMPARTMENT BETWEEN FRAME 35.1 TO 35.7, STRINGER 39L TO 39R. APPROXIM ATELY 1,000 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD THE PAIN T FLAKING OFF THE RIVET TAILS THAT WERE CLEANED AND HAD PRIMER AND PAINT REAPPLIED. AIRCRAFT WAS MFG JUNE 14, 2001. (K ) 2 L 7 2 4F 4 F RT A28NM E37NE 2007062800091 20070628 00091 EU 2007 6 28 USA2007F00002 1 20070326 A 5330 ASNA2051DKJ SKIN AIRBUS A321 A321211 3930370 EU CFMINT CFM56 CFM565B3P 13006 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 172US 21172 1472 CORRODED RIVET TAILS ON FUSELAGE FORWARD CARGO COMPARTMENT BETWEEN FRAME 24 TO 35, STRINGER 38L AND 38R. APPROXIMATELY 100 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD PAINT FLAKING OF F THE RIVET TAILS THAT WERE CLEANED AND HAD PRIMER AND PAINT REAPPLIED. AC MFG 4/18/2001. (K) 2 L 7 2 4F 4 F RT A28NM E37NE 2007062800092 20070628 00092 SO 2007 6 28 C2XA07ON007 1 20070619 A 3350 BA50900901 CHARGER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14162 0808 SCHEDULE MX - SVC/RTN - ONT - DURING OVERNIGHT INSPECTION MX PERSONAL FOUND LEFT AND RIGHT HANDS EXTERIOR OVERWING EMERG ENCY LIGHTS INOPERATIVE. MX PERSONAL REMOVED AND REPLACED NR 4 BATTERY CHARGER ASSY MAS PER EMB 145 AMM 33-50-04, OPS C HECKS GOOD. A/C WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007062800093 20070628 00093 EU 2007 6 28 USA2007F00003 1 20070327 A 5330 ASNA2051DKL SKIN AIRBUS A321 A321211 3930370 EU CFMINT CFM56 CFM565B3P 13006 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 173US 21672 1481 CORRODED RIVET TAILS ON FUSELAGE FORWARD CARGO COMARTMENT BETWEEN FRM 24-35 STRINGER 38L AND 38R. APPROXIMATELY 500 RIV ETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD PAINT FLAKING OFF THE R IVET TAILS THAT WERE CLEANED AND HAD PRIMER AND PAINT REAPPLIED. AIRCRAFT MFG 4/23/2001. (K) 2 L 7 2 4F 4 F RT A28NM E37NE 2007062800094 20070628 00094 EU 2007 6 28 USA2007F00004 1 20070403 A 5330 SKIN AIRBUS A321 A321211 3930370 EU CFMINT CFM56 CFM565B3P 13006 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 174US 21452 1492 CORODED RIVET TAILS WERE FOUND IN FUSELAGE FORWARD CARGO COMARTMENT BETWEEN FRM 32-35.5, STRINGER 44L AND 42R. APPROXIM ATELY 500 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD PAINT FLAK ING OFF THE RIVET TAILS THAT WERE CLEANED AND HAD PRIMER AND PAINT REAPPLIED. AC MFG 5/10/2001. (K) 2 L 7 2 4F 4 F RT A28NM E37NE 2007062800095 20070628 00095 EU 2007 6 28 USA2007F00005 1 20070426 A 5330 ASNA2051DKJ SKIN AIRBUS A321 A321211 3930370 EU CFMINT CFM56 CFM565B3P 13006 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 176UW 21773 1499 CORRODED RIVET TAILS WERE FOUND IN FUSELAGE FORWARD CARGO COMPARTMENT BETWEEN FRM 26-35, STRINGER 40L AND 42R. APPROXIM ATELY 500 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD PAIN FLAKI NG OFF THE RIVET TAILS THAT WERE CLEANED AND HAD PRIMER AD PAINT REAPPLIED. AIRCRAFT MFG 5/15/2001. (K) 2 L 7 2 4F 4 F RT A28NM E37NE 2007062800096 20070628 00096 EU 2007 6 28 USA2007F00006 1 20070503 A 5330 ASNA2051DKJ SKIN AIRBUS A321 A321211 3930370 EU CFMINT CFM56 CFM565B3P 13006 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 170US 21574 1462 CORRODED RIVET TAILS WERE FOUND IN FUSELAGE FWD CARGO COMPARTMENT BETWEEN FRM 24-35, STRINGER 38L AND 38R. APPROXIMATEL Y 50 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD PAINT FLAKING O FF THE RIVET TAILS THAT WERE CLEANED AND HAD PRIMER AND PAINT REAPPLIED. AC MFG 5/21/2001. (K) 2 L 7 2 4F 4 F RT A28NM E37NE 2007062800097 20070628 00097 NM 2007 6 28 BA07043 1 20070619 A 5230 S140T2639 SEAL BOEING 767 767201 1385125 NM CARGO DOOR FAILED A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 246AY 23898 FLIGHT 742, PHL-BCN: CREW REPORTED A VIBRATION AT APPROXIMATELY ROWS 4 - 6 ON THE RIGHT SIDE OF THE AIRCRAFT. FLIGHT RE TURNED TO PHL. MAINTENANCE REPLACED THE FORWARD CARGO DOOR SEAL. NO FURTHER FAULTS. 2 L 7 2 4F RT A1NM 2007062800098 20070628 00098 EU 2007 6 28 USA2007F00007 1 20070507 A 5330 ASNA2051DKJ SKIN AIRBUS A321 A321211 3930370 EU CFMINT CFM56 CFM565B3P 13006 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 179UW 21172 1521 CORRODED RIVET TAILS ON FUSELAGE FORWARD CARGO COMPARTMENT BETWEEN FRM 28-35, STRINGER 38L. APPROXIMATELY 900 RIVETS WE RE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD PAINT FLAKING OFF THE RIVET T AILS THAT WERE CLEANED AND HAD PRIMER AND PAINT REAPPLIED. AC MFG 6/20/2001. (K) 2 L 7 2 4F 4 F RT A28NM E37NE 2007062800099 20070628 00099 EU 2007 6 28 SA07041 1 20070620 A 2120 UNKNOWN AIRBUS A319 A319112 3930323 EU CABIN ODOR A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 712US 1038 PHL FLT 1429 EN-ROUTE SYR TO PHL. DURING DESCENT, WITH APU OFF, A VERY BAD ODOR WAS NOTED IN THE CABIN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. 2 L 7 2 4F RT A28NM 2007062800100 20070628 00100 EU 2007 6 28 SA07042 1 20070620 A 4900 4951985 PRESSURE SWITCH AIRBUS 320 A320214 3930316 EU APU INOPERATIVE A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 117UW 1224 MCO FLT 1576 EN ROUTE FLL TO CLT - DURING ORIGINATION OF FLIGHT, THE NUMBER ONE GENERATOR FAILED. THE FLIGHT CONTINUE D WITH THE APU GENERATOR ON-LINE, AND ALTITUDE RESTRICTIONS. WHILE STILL SOUTH OF MCO, THE APU AUTO-SHUTDOWN WITH AN -L P FUEL VALVE FAULT-. THE FLIGHT DIVERTED TO MCO AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NUMBER O NE ENGINE IDG AND THE APU LO OIL PRESSURE SWITCH. OPERATIONALLY AND LEAK CHECKED OK. 2 L 7 2 4F RT A28NM 2007062800101 20070628 00101 EA 2007 6 28 TRAX200700860 1 20070617 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 916EV 7757 LEFT EXTERIOR FWD OVERWING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 20080908 EU 2008 9 8 2008UALA03896 1 20070717 A 2810 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUEL SYS MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 426UA 510 AUTO FEED FAULT DISPLAYED ON UPPER ECAM SCREEN, 560 LBS IN CTR TANK WHICH WAS PREV EMPTY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062500086 20070625 00086 EU 2007 6 25 07FDEA02177 1 20070616 A 5200 HANDLE AIRBUS 310 A310222 3930315 EU DOOR UNSECURE A FDEA C ABORTED TAKEOFF W INADEQUATE Q C TO TAKEOFF 1 SO 25 419FE 345 AT APPROX 85KIAS, RIGHT FORWARD COMPT DOOR AMBER LIGHT CAME ON WITH SINGLE CHIME, ABORTED T/O. RETURNED TO RAMP. FOUND RT ACCESS DOOR BETWEEN AVIONICS COMP AND FWD LWR CARGO HOLD DOOR HANDLE NOT UP COMPLETELY AND SECURE. MOVED HANDLE UP INTO LOCKED SECURE POS. ALL IND BACK TO NML. NO HISTORY ON DOOR OR DOOR INDICATION. 2 L 7 2 4F RT A35EU 2007062500087 20070625 00087 EU 2007 6 25 07FDEA02178 1 20070618 A 5540 R55370209 ARM AIRBUS 310 A310222 3930315 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 RUDDER HINGE ARM NR 5 WITH CORROSION. THE HINGE ARM WAS REPLACED IN ACCORDANCE WITH AMM 55-36-46. 2 L 7 2 4F RT A35EU 2007062500088 20070625 00088 EU 2007 6 25 07FDEA02179 1 20070618 A 5750 A57970167 VANE AIRBUS 310 A310222 3930315 EU ZONE 500 NONE A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 452FE 313 WING LT, FLAP INBD, PREVIOUS REPAIR FOUND LOCATED ON FLAP VANE UPPER SKIN IN BETWEEN RIB 17-18. REPAIR REQUIRES EVALUAT ION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR CONFORMS TO FEDEX ENGINEERING AUTHORIZATION 6-5720-112413. THIS SDR SUBMITTED IN ERROR- ADMINISTRATOR. 2 L 7 2 4F RT A35EU 2007062500089 20070625 00089 EU 2007 6 25 07FDEA02180 1 20070618 A 5320 A53781841 CROSSBEAM AIRBUS 310 A310222 3930315 EU ZONE 100 UNKNOWN A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 452FE 313 CROSSBEAM CRACKED AT FR 35 BETWEEN Y-450 AND Y-953. CROSSBEAM WAS REPAIRED IN ACCORDANCE WITH SRM SUPP 53-10-15 FIG 201 SHEET 2. ON THE JASC/ATA CODE ABOVE PLEASE CONSIDER 5320 INSTEAD OF 5230. 2 L 7 2 4F RT A35EU 2007062500090 20070625 00090 EU 2007 6 25 07FDEA02181 1 20070618 A 5315 A53275336 FLOORBEAM AIRBUS 310 A310222 3930315 EU ZONE 100 CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 452FE 313 N00528 MDCC - CABIN FLOOR - FLOORBEAM AT CABIN WITH CRACK AT FRAME 54.3 AND BETWEEN TRACKS Y-45 AND Y-953. IT WAS REPA IRED IN ACCORDANCE SRM 53-10-15 FIG 201 SHEET 8. 2 L 7 2 4F RT A35EU 2007062500091 20070625 00091 EU 2007 6 25 07FDEA02182 1 20070618 A 5230 A52374351 DOOR FRAME AIRBUS 310 A310222 3930315 EU ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 AFT CARGO COMPARTMENT DOOR FRAME WITH CRACK AT HEAD, FR 61A. REPAIR ACCOMPLISHED PER FEDEX EA 6-5230-112412. 2 L 7 2 4F RT A35EU 2007062500092 20070625 00092 EU 2007 6 25 07FDEA02183 1 20070618 A 5347 A53611610 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 452FE 313 MDCC - TRACK WITH CORROSION BETWEEN FRAMES 15A AND 19 AT Y-1959. THE CORRODED PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007062500093 20070625 00093 EU 2007 6 25 07FDEA02184 1 20070618 A 5347 A5327842220400 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 MDCC - FLOOR - WEAR AT TRACK Y-1456 BETWEEN FR 62 AND 63. REPAIRED IN ACCORDANCE WITH SRM 53-10-16 FIG 208 SHEET 1 - PA GE 243 TO 248. 2 L 7 2 4F RT A35EU 2007062500094 20070625 00094 EU 2007 6 25 07FDEA02185 1 20070618 A 5347 A25775020 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 AFT COMPARTMENT, TRACK Y14710 WITH CORROSION BETWEEN FR 61 AND FR62. THE TRACK WAS REPLACED IN ACCORDANCE WITH AMM 25-5 2-21. 2 L 7 2 4F RT A35EU 2007062500095 20070625 00095 EU 2007 6 25 07FDEA02186 1 20070618 A 5347 A2577502400051 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 AFT COMPARTMENT, TRACK Y140 WITH DEEP CORROSION BETWEEN FR 61 AND FR 62. THE TRACK WAS REPLACED IN ACCORDANCE WITH AMM 25-52-21. 2 L 7 2 4F RT A35EU 2007062500122 20070625 00122 NM 2007 6 25 QXEA200701007 1 20070618 A 2750 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM TE FLAP UNKNOWN A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 400QX 4030 GTF FLIGHT: FLAP POWER ON DEPARTURE OUT OF GTF. RAN CHECKLIST AND FLAP POWER STILL ILLUMINATED. LANDED WITH A ZERO FLA P LANDING CHECKLIST. MAINTENANCE C/W WING FLAP SYSTEM ELECTRICAL CHECKS IAW Q400 AMM 27-50-00-760-801. NO FAULTS REPOR TED. SYSTEM CALIBRATION VALVES IN CORRECT RANGE. OPERATIONAL TEST GOOD IAW TASK 27-50-00-710-810. FUNCTIONAL TEST C/W IAW TASK 27-51-00-720-801. ALL CHECKS NORMAL. NO FAULTS AT THIS TIME. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVI CE. 2 H 7 2 4T RT A13NM 2007062500123 20070625 00123 SO 2007 6 25 SIMA200717501 1 20070619 A 2760 14533022405 CONTROL UNIT EMB 145 EMB145LR 3260212 SO ZONE 100 FAILED A SIMA C ABORTED TAKEOFF J F WARNING INDICATION FLT CONT AFFECTED TO TAKEOFF 1 SW 21 667GB 12833 9 145784 RECEIVED SPOILER FAIL MESSAGE AT 50 KNOTS, ABORTED TAKEOFF. REMOVED AND REPLACED SPOILER CONTROL UNIT IAW EMB AMM 27-63 -02. OPERATIONAL CHECKED GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007062500124 20070625 00124 2007 6 25 SIMA200717502 4 20070620 A 3417 7014700626 AIR DATA MODULE EMB 135 EMB135KL 3260302 SO ZONE 100 FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 856AE 6581 5386 145748 RECEIVED AIR SPEED AND SPS ADVANCE WARNING MESSAGES WITH BURNT SMELL IN THE FLIGHT DECK, RETURNED TO DFW. REMOVED AND R EPLACED NUMBER TWO AIR DATA COMPUTER AND ISIS IAW EMB AMM 34-01-01. OPERATIONAL CHECKED GOOD. RETURNED AIRCRAFT TO SER VICE. 2 L 7 2 4F RT T00011AT 2007062500125 20070625 00125 EU 2007 6 25 SIMA200717504 1 20070620 A 3350 SWITCH SAAB SF340 340B 7860101 EU EMERGENCY LIGHT LOOSE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 313AE 340B313 PASSENGER CABIN EMERGENCY LIGHT INOPERATIVE. FOUND LIGHT SWITCH LOOSE, RESEATED SWITCH IAW SAAB AMM 33-50-00. LIGHTS O PERATIONAL CHECKED GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007062500137 20070625 00137 NM 2007 6 25 NWAA072213166 1 20070621 A 2121 FAN AIRBUS A319 A319114 3930350 NM FAILED A NWAA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 366NB 2026 IN CRUISE, FLIGHT CREW HEARD A NOISE COMING FROM FORWARD PART OF FLIGHT STATION (RUMBLING NOISE), THEN DETECTED FUMES (E LECTRICAL) AND WENT THRU SMOKE ELIMINATION AND AVIONICS SMOKE COM PROCEDURES. DIVERTED INTO STL, DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. BLOWER FAN FOUND FAILED, SWAPPED UNIT WITH EXTRACT FAN, EXTRACT FAN PLACED ON MEL 21-26-02A. 2 L 7 2 4F RT A28NM 2007062600003 20070626 00003 NM 2007 6 26 QXEA200700974 1 20070619 A 3150 WARNING HORN BOMBDR DHC8 DHC8402 1390042 NM FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 401QX 4031 SEA FLIGHT NR 2336: AT THE END OF THE RUNWAY, COULD NOT SILENCE THE TAKEOFF WARNING HORN WHEN TRYING TO CONDUCT THE T/O WARNING TEST. AIRCRAFT RETURNED TO GATE. MAINTENANCE C/W OPERATIONAL TEST OF THE TAKEOFF WARNING SYSTEM IAW AMM 31-40- 00-710-802, SUBTASK 31-41-00-710-022. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007062600017 20070626 00017 EU 2007 6 26 07FDEA02191 1 20070619 A 5101 A577960778203 SKIN AIRBUS 300 A300B4605R 3930308 EU ZONE 600 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 731FD 709 OUTER FLAP RT, OLD STATIC DISCHARGER REPAIR FOUND NOT CONFORM TO RAS/FOK/110/2003 (DOUBLER THICKNESS). REPAIR PERFORMED BY INSTALLATION OF NEW DOUBLER IAW RAS/FOK/110/2003 ISSUE "A". 2 L 7 2 4F RT A35EU 2007062600037 20070626 00037 NM 2007 6 26 07FDEA02211 1 20070619 A 5320 65595912 CHANNEL BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT PIT ANTENNA DOUBLER CORRODED AT STA 1030-1050 BETWEEN STR 29R-30. REMOVED NR 3 VHF ANTENNA AND DOUBLERS REF SRM 51- 30-02. REMOVED HAT CHANNEL. REMOVED CORROSION FROM DOUBLERS. ORIGINAL THICKNESS .196" REMOVED .002 REMAINING .194" WI THIN LIMITS REF SRM 51-10-01. REMOVED CORROSION FROM SKIN. ORIGINAL THICKNESS .071" REMOVED .009", REMAINING .065" FO UND TO BE WITHIN LIMITS REF SRM 53-30-01. FAB`D NEW HAT CHANNEL, AND T-ANGLE REF DWG 65-59591 AND 10136-2004. REINSTAL LED HAT CHANNEL REF SRM 51-30-02 NR 3 VHF ANTENNA REINSTALL ON SNRM N00997. 2 L 7 3 4F RT A3WE 2007062600043 20070626 00043 NM 2007 6 26 AWXA200700727 1 20070418 A 5311 90526911 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - FOUND CRACKED FRAME, BS 807, S9R. REPAIRED FRAME, BS 807, S9R IAW AWA ER 03-5362-7165-ES1. 2 L 7 2 4F RT A16WE 2007062600045 20070626 00045 NM 2007 6 26 AWXA200700738 1 20070418 A 5311 654655734 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - FOUND CRACKED FRAME, BS 887, S9R. REPAIRED FRAME, BS 887, S9R IAW AWA ER 03-5362-07165-ES1. 2 L 7 2 4F RT A16WE 2007062600049 20070626 00049 NM 2007 6 26 AWXA200700743 1 20070419 A 5311 90526911 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - C-20 CHECK - FOUND CRACKED FRAME, BS 480, S9L AND S9R. REPAIRED FRAME, BS 480, S9L AND S9R IAW AWA ER 03-5362-07165-ES1. 2 L 7 2 4F RT A16WE 2007062600062 20070626 00062 NM 2007 6 26 AALA20071017 1 20070603 A 2560 STRAP BOEING 757 757223 1384957 NM FLASHLIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 690AA 25696 MIA - EMERGENCY FLASHLIGHT AT LEFT NUMBER ONE DOOR MISSING HOLD DOWN STRAP. REPLACED HOLD DOWN STRAP FOR EMERGENCY FLAS HLIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007062600063 20070626 00063 WP 2007 6 26 AALA20071025 1 20070605 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9681B 53631 SFO - EMERGENCY LIGHTS AT SEAT ROW 24 INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHTS AT SEAT ROW 24. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007062600064 20070626 00064 NM 2007 6 26 AALA20071045 1 20070608 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 JFK - EMERGENCY LIGHTS AT AFT RIGHT DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT RIGHT DOOR. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007062600077 20070626 00077 WP 2007 6 26 AALA20071026 1 20070605 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9681B 53631 SFO - EMERGENCY LIGHTS AT TAIL COMPARTMENT INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHTS AT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007062600078 20070626 00078 NM 2007 6 26 AALA20071027 1 20070606 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 771AN 29579 SFO - EMERGENCY LIGHTS AT SEAT 26C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHTS AT SEAT 26C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007062600088 20070626 00088 NM 2007 6 26 AALA20071013 1 20070602 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 789AN 30252 DFW - EMERGENCY LIGHT AT SEAT 24C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT T00001SE 2007062600091 20070626 00091 NE 2007 6 26 AALA20071008 2 20070601 A 7210 GEARBOX DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LT ENGINE FAILED A AALA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 21 465A 49595 717866 STL INFLIGHT T2491 ORD TO AUS - LEFT ENGINE UNCOMMANDED SHUTDOWN AT FLIGHT LEVEL 340. POSSIBLE FLAMEOUT. LANDED STL WI THOUT INCIDENT. SINGLE ENGINE TIME 12 MINUTES. FOUND CASE DAMAGE AT GEAR BOX MOUNT. REPLACED LEFT ENGINE ON 02JUN AT STL. 2 L 7 2 4F 4 F A6WE E9NE 2007062600096 20070626 00096 NM 2007 6 26 QXEA200701019 1 20070622 A 2421 28B5551 GENERATOR BOMBDR DHC8 DHC8402 1390042 NM NR 2 AC INOPERATIVE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 400QX 3497 3497 4030 PDX - ON FLIGHT 2466, RETURNED TO GATE, NR 2 AC GENERATOR DID NOT COME ON LINE. MAINTENANCE REMOVED AND REPLACED NR 2 A C GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007062600111 20070626 00111 NM 2007 6 26 DHL2007742005 1 20070620 A 5322 SHEAR TIE BOEING 727 727225 1384077 NM BS 480 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 DURING AN "A" CHECK THE FOLLOWING DISCREPANCIES WERE NOTED: FUSELAGE INTERIOR FRAME AT BS 480 AND STR 17L FRAME SHEAR TI E CRACKED, (NDT) FINDING. REMOVED FASTENERS AT SHEAR TIE AND CUT OUT CRACKED SECTION (2" BY 8") OF SHEAR TIE IAW B727 S RM 53-10-4 FIG 11. FABRICATED NEW SECTION, MATL 7075-T6, PO9004940 (6" BY 8") IAW B727 SRM 53-10-2 FIG 3 AND 53-10-4 FI G 11. TREATED AND PRIMED REPAIR PART IAW B727 SRM 51-10-2. INSTALLED REPAIR PART IAW B 727 SRM 53-10-4 FIG 11. 2 L 7 3 4F A3WE 2007062600119 20070626 00119 WP 2007 6 26 DHL2007803539 1 20070610 A 5414 SKIN DOUG DC8 DC873 302199C WP NACELLE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 NR 2 ENG NACELLE INLET COWL UPPER SIDE WORN, STA YN 147.534 AT 12 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FI G 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN SEGMENT (AL2024T3 0.080") AND STEEL SPLICE 17.7 PH 0.050" IAW SRM 71-5-2 FIG 2 SHEET 1, 2, 3. HEAT TREATED SPLICE FROM 17-7 PH CRESS TO 17-7 CRESS ( H1050) IAW SRM 51-1-6. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 7 1-5-2 FIG 2 SHEET 1 ,2, 3, SRM 51-1-11, SRM 51-1-21A. 2 L 7 4 4F RT 4A25 2007062600124 20070626 00124 WP 2007 6 26 DHL2007803533 1 20070608 A 5100 NONE DOUG DC8 DC873 302199C WP NONE NONE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 RT INBD VANE SLOT HAS AN INTERIM REPAIR AT STA XILD 42 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-06-2007, DWG NR AD42-57-107 REV IR DATED 05-21-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-0. CU T OUT DAMAGED SECTION AND FABRICATED EXTERNAL REPAIR DOUBLER (AL7075T6 0.071") INTERNAL DOUBLER (AL7075T6 0.063") AND FI LLER (AL7075T6 0.063") IAW AD42-57-107. CLEANED, TREATED AND PRIMED INTERNAL DOUBLER, FILLER AND EXTERNAL REPAIR DOUBLE R INNER FACE IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DWG NR AD42-57-107, SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D, SR M 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007062600125 20070626 00125 WP 2007 6 26 DHL2007803534 1 20070608 A 5730 SKIN DOUG DC8 DC873 302199C WP TE FLAP WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 RT OUTBD FLAP UPPER SKIN WORN, STA XF 224.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-06-07 , DWG NR AD42-57-106 REV IR DATED 05-21-07. REMOVED EXISTING REPAIR PLATING AND INNER DOUBLER IAW SRM 51-1-21. FABRICA TED NEW PLATING SEGMENT (AL2024T3 0.071") AND INNER DOUBLER (AL2024T3 0.080") IAW DWG NR AD42-57-106. CLEANED, TREATED AND PRIMED AREA, INNER DOUBLER AND INNER FACE OF NEW PLATING SEGMENT IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DWG NR AD42-57-106, SRM 51-1-11, SRM 51-1-21, SRM 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007062600132 20070626 00132 NM 2007 6 26 DU4R2007142 1 20070608 A 5753 113N21052 TORQUE TUBE BOEING 757 757232 1384965 NM ZONE 500 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 640DL 23994 FOUND LT I/B FLAP I/B FAIL SAFE TORQUE TUBE CORRODED. REPAIRED CORRODED LT WING I/B FLAP FAIL SAFE TORQUE TUBE BY REMOV ING AND REPLACE TORQUE TUBE WITH P/N’S 113N2105-1 AND 113N2108-1 IAW B757 MM 57-53-44. 2 L 7 2 4F RT A2NM 2007062600136 20070626 00136 NM 2007 6 26 CALA0700310 1 20070616 A 2612 356104400 ELEMENT BOEING 737 737800* NM MLG W/W INOPERATIVE A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 27239 28951 THE WHEEL WELL FIRE WARNING LIGHT AND BELL ACTIVATED AFTER LANDING GEAR RETRACTED. THE LANDING GEAR WAS EXTENDED AND TH E WARNING LIGHT EXTINGUISHED. THE AIRCRAFT WAS RETURNED TO LAS WHERE IT LANDED WITHOUT INCIDENT. T/S IAW FIM 26-18-00 FOUND M270 WW DETECTOR AT FAULT. THE DETECTOR WAS REPLACED IAW MM 26-18-02. ALSO REPLACED OVERHEAT DETECTION UNIT AS A PRECAUTIONARY MEASURE IAW MM REF 26-18-01. ALSO REPLACED NR 3 MLG BRAKE. PERFORMED WW OVERHEAT DETECTION SYSTEM OPERA TIONAL TEST WITH NO FAULTS FOUND. 2 L 7 2 4F RT A16WE 2007062600140 20070626 00140 NM 2007 6 26 NOCA12007 1 20070616 A 3231 SEQUENCE VALVE BOEING 767 76736N 1385152 NM RT MLG DOOR MALFUNCTIONED A NOCA O OTHER J WARNING INDICATION CL CLIMB 1 EA 15 768NA 29898 WHEN RETRACTING THE LANDING GEAR AFTER T/O, THE RT GEAR LIGHT CAME ON WHEN BRINGING THE LEVER TO OFF POS, LANDING GEAR D ISAGREE EICAS CAME ON ALSO. REPLACED DOOR LATCH ACTUATOR AND SEQUENCE VALVE ITEM IS STILL OPEN. 2 L 7 2 4F RT A1NM 2007062600141 20070626 00141 EU 2007 6 26 MAC060702 1 20070606 A 5751 ATTACH FITTING AEROSP AEROSP ATR42 ATR42300 8680920 EU AILERON CORRODED A MTNA K NONE O OTHER IN INSP/MAINT 1 SO 33 920FX 1263 325 DURING A 2 YEAR INSPECTION, LEVEL 2 CORROSION WAS FOUND ON THE T-FITTINGS ATTACHING THE RIBS TO THE SPAR. THE FITTINGS AFFECTED ARE LOCATED AT THE I/B, O/B HINGE POINTS. THE PROBABLE CAUSE IS DISSIMILAR MATERIALS (STEEL BOLTS IN ALUMINUM ALLOYED FITTINGS (2024T351). THE FITTINGS WERE REPLACED AT RIBS 4, 11/12, AND 9. REFERENCE ATR42 SRM 57-61-10 FIG 101. 2 H 7 2 4T RT A53EU 2007062600151 20070626 00151 SO 2007 6 26 C2XA07IA142 1 20070618 A 3397 WIRE HARNESS EMB 145 EMB145EP 3260221 SO CABIN LIGHTS DAMAGED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 15926 145005 IAH - FLIGHT 2760, DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL IN THE CABIN AT SEAT 3A. MAINTENANCE I NSPECTED THE AIRCRAFT AND PLACED THE CABIN LIGHTING ON MEL 3320-00/1/C CONTROL NUMBER 123251, AND THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. MAINTENANCE REMOVED AND REPLACED THE OVERHEAD LIGHTING WIRE HARNESS AT ROW 7A. 2 L 7 2 4F RT T00011AT 2007062600155 20070626 00155 EA 2007 6 26 TRAX200700841 1 20070613 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 390CA 10106 CEILING EMERGENCY LIGHT AT FS 605.00 INOP (FLAGGED). [06-26-07] REPAIRED IAW AMM 33-50-00 & AMM 35-51-00. 2 L 7 2 4F RT A21EA 2007062600176 20070626 00176 NM 2007 6 26 SWAA073038 1 20070618 A 3350 3071BPEGPL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 14Y CHECK, FOUND LEFT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007062600179 20070626 00179 NE 2007 6 26 SWAA073033 2 20070616 A 7200 CFM567B25G22 ENGINE BOEING 737 7377H4 1384404 NM GE CFM56 CFM567B24 NE LEFT FOD A SWAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 29 239WN 34714 892884 INFLIGHT SHUTDOWN / DIVERSION / DECLARED EMERGENCY. AT FL 380 NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. INSPECT ED ENGINE FOUND METAL CHIPS IN FWD CHIP DETECTOR AND OIL FILTER OF NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE PER MT . 2 L 7 2 4F 4 F RT A16WE E00055EN 2007062600197 20070626 00197 NM 2007 6 26 2007UALA02022 1 20070615 A 4900 CONTROL UNIT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE APU MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 APU AUTO SHUTDOWN AFTER PUSHBACK. RESTART WAS NORMAL, BUT HAS HISTORY. [07-20-07] REPLACED APU CONTROL UNIT PER MM 49 -61-05 AND P2 SENSOR PER MM 49-61-04. CK'D P2 SENSOR LINE FOR OBSTRUCTION, NONE FOUND. RAN APU FULLY LOADED WITH ELEC AN D PNEUMATICS. NO FAULTS. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062600198 20070626 00198 NM 2007 6 26 2007UALA02023 1 20070614 A 5330 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE BS 397 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 771UA 26932 REWORKED SKIN GOUGE AT STA 397 BETWEEN STR 30L-31L IS CRACKED. MARKED ENDS OF CRACK. [07-13-07] DOUBLER INSTALLED PER SRM 53-00-01 REPAIR 10. A/C OK FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007062700014 20070627 00014 CE 2007 6 27 DXTA200702273 1 20070617 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE FAILED E DXTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 393QS 5600393 POWER BRAKE SYSTEM FAILURE (POWER BRAKE LOW PRESS AND ANTI-SKID INOP LIGHT ON) LIGHT STAYS ON. [07-10-07] FOUND THE B RAKE PRESSURE RELIEF VALVE STUCK IN THE OPEN POSITION. REMOVED AND REPLACED THE RELIEF/BLEED VALVE IAW CESSNA CITATION 5 60 ULTRA 20-10-06. OPERATIONAL CHECK WAS SATISFACTORY & NO LEAKS NOTED AT THIS TIME 2 L 7 2 4F 4 F RT A22CE E25EA 2007062700017 20070627 00017 CE 2007 6 27 GLBA0956 1 20070618 A 5320 ANGLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 288 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 170GL UE170 UPON ROUTINE INSPECTION MAINTENANCE DISCOVERED CRACK AT RT FS 288 WL 70.0. LENGTH OF CRACK 1.75 INCHES. UPON COMPLETION OF REPAIRE RII INSPECTION IS REQUIRED. [OPEN] 2 L 7 2 4T 4 T RT A24CE E26NE 2007062700018 20070627 00018 SW 2007 6 27 061907 1 20070614 A 6420 B642M1009103 CONTROL ARM BOLKMS 117 BK117C2 5626002 SW TMECA ARRIEL ARRIEL1E 60034 NE TIAL ROTOR CRACKED E E3MA O OTHER O OTHER NR NOT REPORTED 1 EA 03 304ME 225 225 9097 TAIL ROTOR CONTROL LEVER FOUND CRACKED 1 G 7 2 3U 3 U H13EU E19EU 2007062700022 20070627 00022 NM 2007 6 27 QXEA200701005 1 20070619 A 6120 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM PROPELLER UNKNOWN A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 423QX 4153 GEG FLIGHT NR 2393: ON START, NR 2 NH HUNG AT 16-17 PERCENT FOR SEVERAL SECONDS. THEN WAS SLOW TO ACCELERATE WHEN BROUG HT OUT OF FEATHER. 'RDC TOP' WOULD NOT ADJUST PRIOR TO RESET. AIRCRAFT RETURNED TO GATE. MAINTENANCE INTERROGATED CDS AND FOUND FAULT CODE 968. C/W FIM TASK 73-20-00-810-821. PERFORMED FUNCTIONAL TEST OF THE PROPELLER TIME TO UNFEATHER IAW AMM 61-20-00, PG 515-516. SYSTEMS OPERATE NORMALLY. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007062700030 20070627 00030 EU 2007 6 27 07FDEA01880 1 20070521 A 5100 NONE AIRBUS 310 A310322 3930334 EU NONE NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON LT LWR WING SURFACE T/E OF INBOARD FLAP WS207-270 RIB4-5. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR CONFORMS TO EXISTING FEDEX EA 6-5750-81810. SDR SUBMITTED IN ERROR- ADMINISTRATOR. 2 L 7 2 4F RT A35EU 2007062700032 20070627 00032 EU 2007 6 27 07FDEA01891 1 20070521 A 5100 NONE AIRBUS 310 A310222 3930315 EU NONE NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON LT WING UPPER SURFACE, SPOILER 2 WS 270-339 RIB5-6. REPAIR REQUIRES EVALUATION FOR MAJ OR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. A VISUAL INSPECTION AND A TAP TEST W ERE PERFORMED IN ACCORDANCE WITH FEDEX EA 6- 5770-106717. SDR SUBMITTED IN ERROR- ADMINISTRATOR. 2 L 7 2 4F RT A35EU 2007062700039 20070627 00039 NM 2007 6 27 07FDEA02214 1 20070619 A 5314 BAC15061464 KEELBEAM BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT PIT STR 29L KEEL BEAM CHORD CORRODED STA. 970-990 REMOVED A MAXIMUM OF .048" CORROSION ON KEEL BEAM BETWEEN STA 970 AND 990 AND IS OUT OF LIMITS. SPOT FACED FASTENER HOLES AND ACCOMPLISHED FABRICATION OF FILLERS AND REPAIR STRAP AND INSALLATION OF REPAIR PARTS ON SNRM N00644/JPF ITEM 7-18. 2 L 7 3 4F RT A3WE 2007062700040 20070627 00040 NM 2007 6 27 07FDEA02215 1 20070619 A 5314 BAC15061464 KEELBEAM BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT PIT STR 29L, KEEL BEAM CHORD CORRODED STA 950F-970 REMOVED A MAXIMUM OF .032" OF CORROSION ON KEEL BEAM BETWEEN STA 950F AND 970 AND IS OUT OF LIMITS. SPOT FACED HOLES AND ACCOMPLISHED FABRICATION OF FILLERS AND REPAIR STRAP. INSTALL ATION OF REPAIR PARTS ON SNRM N00644/JPF ITEMS 7-18. 2 L 7 3 4F RT A3WE 2007062700042 20070627 00042 NM 2007 6 27 07FDEA02217 1 20070620 A 5730 ARB2886504 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 575FE 48500 RIGHT WING FIXED LEADING EDGE TELESCOPE DUCT CUTOUT FOUND CRACKED. [07-06-07] CRACK AT RIGHT HAND WING FIXED LEADING E DGE TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57-10-00 FIGURE 43 VOLUME I AND FEDEX E.A. #1-5710-112342, REPAIR CLASSI FIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062700056 20070627 00056 EA 2007 6 27 QXEA20071010 1 20070619 A 2612 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA FIRE WARNING UNKNOWN A QXEA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 606QX 10023 BOI- FLIGHT 4276. FIRE SYSTEM FAULT ILLUMINATED. GOES OUT AFTER NR 1 ENGINE START. MAINTENANCE PLACED THE FIDEEX SYSTE M ON MEL 26-00-1. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007062700060 20070627 00060 NM 2007 6 27 HALA0700259 1 20070618 A 4940 5189588 STARTER BOEING 767 76733A 1385209 NM APU MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 589HA 16780 16780 33422 ETOPS SIGNIFICANT SYSTEM, APU ON START UP SHOWED APU FAULT AND SHUT DOWN AUTOMATICALLY EICAS MSG APU FAULT. BITE CK ECD "START ABORTED" FAULT. FOUND STARTER BRUSH IND LOW/BATT VOLTAGE LOW W/LOAD. REMOVED AND REPLACED APU BATT PER MM 24-3 1-04. REMOVED AND REPLACED APU STARTER PER MM49-41-01. OPS CK OK BATT PN BA06-01 SN ON 49975 OFF 118341, STARTER PN 51 9858-8, SN ON 5480 OFF 5318. 2 L 7 2 4F RT A1NM 2007062700069 20070627 00069 NM 2007 6 27 QXEA200700977 1 20070608 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - DENTS ABOVE LEFT ICE SHIELD AT STATION 272 BETWEEN STRINGERS 4L AND 5L. REPAIRED IAW RD8/4-53-1935. 2 H 7 2 4T RT A13NM 2007062700072 20070627 00072 NM 2007 6 27 QXEA200700976 1 20070613 A 5310 STOP FITTING BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - FORWARD MAIN CABIN DOOR AFT STOPS ARE WORN. REPAIRED IAW SRM 51-14-00 AND RD8/4-53-1934. 2 H 7 2 4T RT A13NM 2007062700078 20070627 00078 NM 2007 6 27 QXEA200700991 1 20070610 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 605 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - SEAT TRACK NR 20 HAS PITTING CORROSION AT STATION 605. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007062700089 20070627 00089 NM 2007 6 27 AALA20071057 1 20070609 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 751AN 30798 NRT - EMERGENCY LIGHT BATTERY PACK AT FIRST CLASS CLOSET BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY AT FIRST CLASS CLOSE T. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007062700090 20070627 00090 NM 2007 6 27 AALA20071054 1 20070607 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 927AN 30077 TUL - EMERGENCY LIGHT BATTERY PACK ABOVE FORWARD ENTRY LIGHT FAILED OPERATIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK ABOVE FORWARD ENTRY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007062700091 20070627 00091 NM 2007 6 27 AALA20071053 1 20070607 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 927AN 30077 TUL - EMERGENCY LIGHT BATTERY PACK ABOVE FORWARD ENTRY LIGHT FAILED OPERATIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK ABOVE FORWARD ENTRY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007062700092 20070627 00092 NM 2007 6 27 AALA20071051 1 20070524 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 766AN 32880 AFW - EMERGENCY LIGHT BATTERY PACK M33400 FAILED OPERATIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK M33400. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007062700093 20070627 00093 NM 2007 6 27 AALA20071052 1 20070524 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 766AN 32880 AFW - EMERGENCY LIGHT BATTERY PACK M33094 FAILED OPERATIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK M33094. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007062700094 20070627 00094 NM 2007 6 27 AALA20071055 1 20070612 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 928AN 29528 TUL - EMERGENCY LIGHT BATTERY PACK AT STATION 722 RIGHT SIDE IN COACH FAILED OPERATIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK AT STATION 722 RIGHT SIDE IN COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007062700097 20070627 00097 NM 2007 6 27 AALA20071049 1 20070524 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 766AN 32880 AFW - EMERGENCY LIGHT BATTERY PACK M33401 FAILED OPERATIONAL TEST. REPLACED EMERGENCY LIGHT BATTERY PACK M33401. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007062700116 20070627 00116 NM 2007 6 27 07FDEA02237 1 20070621 A 5347 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 RBL SEAT TRACK HAS CORROSION BETWEEN UPPER CHANNEL AND LWR MOUNT FLANGE STA 783-849. REMOVED CORROSION REF SRM 53-10-1 FIG 3 SHT 5. .015" MAT. REMOVED. OUT OF LIMITS REF SRM 53-10-1 FIG 3. REMOVED FLOORBEAM AND SEAT TRACK BS 740 TO 850 R BL 45. FABRICATED NEW FLOORBEAM OUT OF BAC1506-1108. REF FED EX GMM7-0-1001, SRM 51-30-02 TREATED AND PRIMED FLOORBEAM REF MM 51-20-031-1, 51-20-21-7. INSTALLED FLOORBEAM AND SEAT TRACK REF BAC DWG 65-16279, SRM 51-20-2. 2 L 7 3 4F RT A3WE 2007062700127 20070627 00127 SO 2007 6 27 CHQA200700027 1 20070621 A 3040 HEATER EMB 145 EMB145LR 3260212 SO WINDSHIELD SMOKE A CHQA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 11 281SK 5502 5502 145391 FLIGHT 6221 - CVG-ORF - SMOKE APPEARED FROM LOWER LEFT CORNER OF CAPTAIN’S WINDSHIELD DURING DESCENT. SWITCHED OFF WIND SHIELD HEAT AND SMOKE SUBSIDED. MAINTENANCE REMOVED AND REPLACED TINE CAPTAIN’S WINDSHIELD. 2 L 7 2 4T RT T00011AT 2007062700129 20070627 00129 EA 2007 6 27 CHQA200700028 1 20070620 A 7830 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER FALSE ACTIVATION A CHQA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 11 656BR 7485 FLIGHT 3338 - CLE-PVD - DURING CRUISE AT FL270, "RT REV UNLOCK" CAUTION MESSAGE APPEARED. RAN THE QRH WHILE STARTING DE SCENT. DECLARED AN EMERGENCY WITH ATC, LANDED WITH NO FURTHER INDICATIONS. MAINTENANCE DEFERRED THE THRUST REVERSER. 2 L 7 2 4F RT A21EA 2007062700138 20070627 00138 EA 2007 6 27 SWIA200718349 1 20070606 A 2497 POWER CABLE CNDAIR CL600 CL6002C10 1390015 EA GENERATOR CHAFED A SWIA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 07 726SK 10190 RIGHT IDG T1 CABLE SHOWS EVIDENCE OF RUBBING AND ARCING AFT OF GENERATOR. REPLACED IDG POWER CABLE T1 FROM RIGHT IDG TO TB19 IAW WDM 20-11-00. 2 L 7 2 4F RT A21EA 2007062700143 20070627 00143 SO 2007 6 27 SWIA200718354 1 20070311 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 568SW 120343 FORWARD SEAT TRACK ON LEFT SIDE OF FLOOR IS CORRODED IN MULTIPLE AREAS.REPLACED LEFT FLOOR SEAT TRACK FORWARD SECTION IA W EMB120 MM 53-01-05. 2 L 7 2 4T RT A31SO 2007062700144 20070627 00144 SO 2007 6 27 SWIA200718355 1 20070311 A 5210 RIB EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 568SW 120343 PAX DOOR RIB MIDWAY UP THE AFT SIDE OF DOOR IS CRACKED. REPLACED RIB IAW SRM 51-10-02 PG 3 SEC 3A. 2 L 7 2 4T RT A31SO 2007062700162 20070627 00162 EU 2007 6 27 COEA0704903 1 20070109 A 5310 S531711012040 WINDOW FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE DENTED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 903FX 179 DURING HEAVY CHECK MAINTENANCE FOUND DENT ON CAPTAIN WINDSHIELD FRAME UPPER POST. REMOVED WINDSHIELD, NO CRACKS FOUND. DENT DRESSED BACK PER DO/TS-386/07-8256. WINDSHIELD INSTALLED. REFERENCE SRAS DO/TS-386/07. 3978 AS A PERMANENT REPA IR. (M) 2 H 7 2 4T RT A53EU 2007062700174 20070627 00174 EU 2007 6 27 COEA0701903 1 20070126 A 5340 S5357500201 FITTING AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 903FX 179 AREAS OF LEVEL 2 CORROSION ON FORWARD OUTBOARD CORNER OF RIGHT MAIN LANDING GEAR BULKHEAD FRONT SPAR ON FRAME 25. BLEND ED OUT CORROSION AND REINFORCED FITTING AND STRAP. COMPLIED WITH SB ATAR42-53-0155 ON RT SIDE AND FOUND SB ATR42-53-015 5 PCW ON LT SIDE. REPAIRS ARE PERMANENT PER SRAS DO/TS-682/07, 4002. (M) 2 H 7 2 4T RT A53EU 2007062700177 20070627 00177 EA 2007 6 27 TRAX200700855 1 20070615 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 751EV 10163 LT 280 BULKHEAD LOWER WEB CORRODED. REPAIRED IAW SRM 51-42-06, 70-53-11-052, REO 670-53-11-052, ALL WORK COMPLETE COM PLIED WITH EO 700-53-0062 01 2 L 7 2 4F RT A21EA 2007062800001 20070628 00001 NM 2007 6 28 2007UALA02110 1 20070618 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SEAT 29J INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 SEAT 29J EEL LIGHT IS INOPERATIVE. *S/D* REPLACED LIGHT. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062800057 20070628 00057 EA 2007 6 28 TRAX200700859 1 20070616 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 FWD F/A FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007062800058 20070628 00058 NM 2007 6 28 UPS07549993 1 20070619 A 3150 WARNING MESSAGE BOEING 757 75724APF 1384969 NM LT ENGINE UNKNOWN A IPXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 402UP 23724 LEFT ENGINE TAT PROBE HEAT MESSAGE. LEFT ENGINE HIGH STAGE LIGHT. OPEN 2 L 7 2 4F RT A2NM 2007062800059 20070628 00059 WP 2007 6 28 UPS07849981 1 20070522 A 5330 5613862 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C1 FUSELAGE SKIN CORRODED AT FS 60 BETWEEN L34R AND L35R. REMOVED AND REPLACED FUSELAGE SKIN FROM STA - 21.92 - STA 70 L31L TO L31R IAW UPS EO DC8-5330-8942-D. 2 L 7 4 4F RT 4A25 2007062800060 20070628 00060 WP 2007 6 28 UPS07849984 1 20070602 A 5340 DC853020001 FITTING DOUG DC8 DC873F 302199F WP FS 759 L18L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 BOOT FITTING CRACKED AT STA 759 L18L. REMOVED AND REPLACED CRACKED BOOT FITTING AT STA 759 L18L IAW UPS EO DC8-5310-22792-B, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007062800061 20070628 00061 WP 2007 6 28 UPS07849985 1 20070609 A 5311 FRAME DOUG DC8 DC873F 302199F WP FS 120 L31R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 A-PIT STA 120 L31R, FRAME HAS CRACK EXTENDING PAST STOP DRILL. STOP DRILLED CRACK AT FRAME STA 120 L 31R IAW SRM 53-02-00-0. FABRICATED AND INSTALLED REPAIR ANGLE AT STA 120 FRAME L31R IAW SRM EO DC8-5320-6176-C. 2 L 7 4 4F RT 4A25 2007062800062 20070628 00062 WP 2007 6 28 UPS07849986 1 20070613 A 5313 LONGERON SPLICE DOUG DC8 DC873F 302199F WP FS 1270 L31L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 SPLICE FITTING CRACKED (C-PIT) L31L STA 1270. REMOVED AND REPLACED LONGERON SPLICE FITTING AT STA 12 70 L31L IAW SRM 51-1-20D, AND SRM 51-3-2. 2 L 7 4 4F RT 4A25 2007062800063 20070628 00063 WP 2007 6 28 UPS07849987 1 20070608 A 5754 VANE DOUG DC8 DC873F 302199F WP RT WING LE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 RIGHT WING CENTER LEADING EDGE SLOT VANE INBOARD UPPER SURFACE HEAVY CORROSION. CORROSION BLENDOUT W ENT OUT OF LIMITS IAW SRM 57-03-00 FIG 23. FABRICATED AND INSTALLED FILLER AND DOUBLER AT RT WING CENTER L/E SLOT VANE INBOARD UPPER SURFACE IAW SRM 57-03-00-0 FIG 024 AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 2007062800064 20070628 00064 WP 2007 6 28 UPS07849988 1 20070608 A 5320 CHANNEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 HAT CHANNEL HEAVILY CORRODED IN MAIN CABIN SUBFLOOR AT L1 DOOR STA 30 LBL 50. REMOVED HAT CHANNEL AT STA 30 LBL 50 IAW SRM 51-01-21. FABRICATED AND INSTALLED REPLACEMENT HAT CHANNEL AT STA 30 LBL 50 IAW SRM DWG 3713239, AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 2007062800065 20070628 00065 WP 2007 6 28 UPS07849989 1 20070609 A 5320 FITTING DOUG DC8 DC873F 302199F WP FS 1766 L10L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 L10L AT STA 1766 HAS CRACKED END FITTING. REMOVED AND REPLACED L10L END FITTING AT STA 1766 IAW SRM 51-03-02- O, AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 2007062800066 20070628 00066 WP 2007 6 28 UPS07849990 1 20070618 A 3350 UNKNOWN DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS UNKNOWN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:N/A EMERGENCY LIGHTS WOULD NOT COME ON WHEN PERFORMING TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTE RY AND RELAY UNIT AND TESTED IAW 33-50-01-2. TESTS OK. 2 L 7 4 4F RT 4A25 2007062800067 20070628 00067 WP 2007 6 28 UPS07849992 1 20070606 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP FS 1766 L10R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 AFT PRESS BULKHEAD RT L10R AREA 2EA CRACKS AT STA 1766. CUT OUT DAMAGED AREA AT STA 1766 L10R IAW SR M 53-2-5 FIG 14A. FABRICATED AND INSTALLED REPAIR DOUBLER, FINGER DOUBLER, AND FILLER AT STA 1766 L10R IAW SRM 53-2-5 F IG 14A, AND SRM TR 53-194. THIS REPAIR REQUIRES A DAMAGE TOLERANCE INSP INITIAL AT 16,000 LANDINGS AND REPETIVE INSP AT 4,000 THERE AFTER IAW TR 53-194. 2 L 7 4 4F RT 4A25 2007062800068 20070628 00068 EU 2007 6 28 WRNA200700041 1 20070616 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE DAMAGED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 501TR 53 DURING WALKAROUND, FOUND FUSELAGE SKIN DAMAGED AT C-1 DOOR FRAME, RIGHT SIDE AT FRAME 24B STA 1701. INSTALLED DOUBLER R EPAIR ON C-1 DOOR FRAME 24B STA 1701 IAW A300 SRM 53-13-00. 2 L 7 2 4F RT A35EU 2007062800069 20070628 00069 NM 2007 6 28 SWAA073047 1 20070618 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 729SW 27861 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 986, RBL 42 TO LBL 42. REPAIRED FLOORBEAM CHORD PER ER. 2 L 7 2 4F RT A16WE 2007062800070 20070628 00070 NM 2007 6 28 SWAA073054 1 20070619 A 3350 20131A BATTERY BOEING 737 7375H4 138449D NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED A1 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007062800071 20070628 00071 NM 2007 6 28 SWAA073051 1 20070619 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM BS 482 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 482, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007062800072 20070628 00072 NM 2007 6 28 SWAA073049 1 20070619 A 5330 6545768208 SKIN BOEING 737 7373H4 1384600 NM BS 386 S17R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 386, STR 17R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007062800073 20070628 00073 NM 2007 6 28 SWAA073053 1 20070619 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM BS 747 S19R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 19R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007062800074 20070628 00074 NM 2007 6 28 SWAA073057 1 20070619 A 5330 6545800219 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007062800075 20070628 00075 NM 2007 6 28 SWAA073043 1 20070618 A 5330 6545800219 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 603SW 27954 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007062800076 20070628 00076 NM 2007 6 28 SWAA073055 1 20070619 A 5753 6546435277 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED HC2 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP INBOARD END DELAMINATED. REMOVED AND REPLACED FLAP PE R MM. 2 L 7 2 4F RT A16WE 2007062800077 20070628 00077 NM 2007 6 28 SWAA073041 1 20070618 A 5755 FITTING BOEING 737 7373H4 1384600 NM LT WING SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED MV2 CHECK, FOUND LEFT WING NR 4 GROUND SPOILER INBOARD FITTING CRACKED. REMOVED AND REPLACED SPOILER A SSY AND ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2007062800078 20070628 00078 NM 2007 6 28 SWAA073042 1 20070618 A 5553 6547450 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED BRDG CHECK, FOUND VERTICAL STAB FITTING FWD AND AFT CLEVIS LUG FACES CORRODED. REPAIRED FITTING PER ER . 2 L 7 2 4F RT A16WE 2007062800079 20070628 00079 2007 6 28 SWAA073046 4 20070618 A 2565 6557463 GIRT BAR BOEING 737 7373H4 1384600 NM R2 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER MM. 2 L 7 2 4F RT A16WE 2007062800080 20070628 00080 2007 6 28 SWAA073045 4 20070618 A 2565 6557463 GIRT BAR BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER MM. 2 L 7 2 4F RT A16WE 2007062800081 20070628 00081 2007 6 28 SWAA073044 4 20070618 A 2565 6557463 GIRT BAR BOEING 737 7373H4 1384600 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER MM. 2 L 7 2 4F RT A16WE 2007062800082 20070628 00082 NM 2007 6 28 SWAA073052 1 20070619 A 5754 65C226602 SKIN BOEING 737 737301 1384611 NM RT WING SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 6 L/E SLAT CRACKED AT FWD END. REPAIRED SLAT PER SWA EA. 2 L 7 2 4F RT A16WE 2007062800083 20070628 00083 NM 2007 6 28 SWAA073048 1 20070618 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 762SW 27876 DURING SCHEDULED MV2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007062800084 20070628 00084 NM 2007 6 28 SWAA073050 1 20070619 A 5753 SKIN BOEING 737 7373H4 1384600 NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED MV2 CHECK, FOUND LEFT WING OUTBOARD FOREFLAP INBOARD T/E DELAMINATED. REMOVED AND REPLACED FLAP PER MM . 2 L 7 2 4F RT A16WE 2007062800102 20070628 00102 EA 2007 6 28 TRAX200700861 1 20070617 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 760EV 10212 EMERGENCY FLOOR LIGHTING TAPE WORN AWAY NEAR GALLEY CARTS. 2 L 7 2 4F RT A21EA 2007062800103 20070628 00103 2007 6 28 TRAX200700862 2 20070617 A 7200 ENGINE CNDAIR CL600 CL6002C10 1390015 EA LEFT VIBRATION A ASOA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 27 744EV 10157 DIVERTED TO PVD. INFLIGHT LT ENGINE N1 VIB READS 2.0. FOLLOWED QRH FOR SINGLE ENGINE OPERATION. LT ENGINE N1 VIB REMA IN IN AMBER UNTIL ENGINE SHUTDOWN. EMERGENCY DECLARED. EN ROUTE TO ATL A/C DIVERTED TO PVD DUE TO MTC. RELATED TO DEF ECT 360406-3, 360407-1, 2, 3 AND 360408-1. FLT 4140 DEL 110 MINS. 2 L 7 2 4F RT A21EA 2007062800104 20070628 00104 EA 2007 6 28 TRAX200700863 1 20070617 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 920EV 7810 F/A'S STATION FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007062800105 20070628 00105 EA 2007 6 28 TRAX200700864 1 20070618 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 884AS 7513 RT OVERWING EXIT HARD TO OPEN. FLT 4725 CX. 2 L 7 2 4F RT A21EA 2007062800106 20070628 00106 EA 2007 6 28 TRAX200700865 1 20070618 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 884AS 7513 LEFT OVERWING EXIT HARD TO OPEN. 2 L 7 2 4F RT A21EA 2007062800107 20070628 00107 EA 2007 6 28 TRAX200700866 1 20070618 A 5310 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA BS 349 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 889AS 7538 FS 349 CORRODED AT SERVICE DOOR. 2 L 7 2 4F RT A21EA 2007062800108 20070628 00108 EA 2007 6 28 TRAX200700868 1 20070618 A 5320 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 889AS 7538 LBL 9 INBOARD & OUTBOARD CLIPS CRACKED AT FS 280. 2 L 7 2 4F RT A21EA 2007062800109 20070628 00109 EA 2007 6 28 TRAX200700869 1 20070618 A 5320 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 889AS 7538 RBL 9 INBOARD & OUTBOARD CLIPS CRACKED AT FS 280. 2 L 7 2 4F RT A21EA 2007062800110 20070628 00110 EA 2007 6 28 TRAX200700870 1 20070618 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 889AS 7538 FS 280 WEB CRACKED OUTBOARD OF LBL 9 AND OUTBOARD OF RBL 9. 2 L 7 2 4F RT A21EA 2007062800111 20070628 00111 EA 2007 6 28 TRAX200700871 1 20070618 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 889AS 7538 FWD FLOOR SUPPORT ANGLE AT FS 280 IS CORRODED. 2 L 7 2 4F RT A21EA 2007062800112 20070628 00112 EA 2007 6 28 TRAX200700872 1 20070618 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA BS 461 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 973EV 7575 CRACK FOUND ON FLOOR STRUCTURE AT FS 461.00 LBL 9 AND RBL 9. 2 L 7 2 4F RT A21EA 2007062800113 20070628 00113 EA 2007 6 28 TRAX200700873 1 20070618 A 3150 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS UNKNOWN A ASOA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 829AS 7232 FLAPS FAIL CAUTION MSG AT CRUISE. FOLLOWED QRH (BTMS DID NOT GO RED). EMERGENCY DECLARED. FLT 4319 CX. 2 L 7 2 4F RT A21EA 2007062800114 20070628 00114 EA 2007 6 28 TRAX200700874 1 20070619 A 5260 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 970EV 7527 ASD FWD ANCHOR FITTING CRACKED. 2 L 7 2 4F RT A21EA 2007062800115 20070628 00115 EA 2007 6 28 TRAX200700875 1 20070619 A 5230 ANGLE CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 937EV 8042 CRACK FOUND ON CARGO DOOR STRUCTURE ANGLE AT FS 621 LBL 36.00 WL 112.00 (CARGO POST LOWER ANGLE). 2 L 7 2 4F RT A21EA 2007062800116 20070628 00116 EA 2007 6 28 TRAX200700876 1 20070619 A 5240 SERVICE DOOR CNDAIR CL600 CL6002C10 1390015 EA STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 F/A UNABLE TO OPEN SERVICE DOOR. 2 L 7 2 4F RT A21EA 2007062800117 20070628 00117 EA 2007 6 28 TRAX200700877 1 20070619 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 683BR 7692 EMERGENCY TRACK LIGHTING AT ROWS 2 THRU 5 INOP. FLT 4678 DEL 93 MINS. NC FLTS 4390, 4496 CX. [07-26-07] CLEANED TRA CK LIGHTING CONNECTIONS AT ROWS 2,3,4 AND 5 OPS CK GOOD. 2 L 7 2 4F RT A21EA 2007062800118 20070628 00118 EA 2007 6 28 TRAX200700878 1 20070620 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 PAX DOOR DIFFICULT TO OPEN, HANDLE DIFFICULT TO STOW. 2 L 7 2 4F RT A21EA 2007062800119 20070628 00119 EA 2007 6 28 TRAX200700879 1 20070615 A 5100 NONE CNDAIR CL600 CL6002B19 1900309 EA NONE NONE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 886AS 7531 PAX DOOR INNER SKIN CRACKED UNDER STEP 832ET (FWD SIDE). [06-28-07] UPON FURTHER EVALUATION FOUND TO BE LIMITED TO PAI NT ONLY. 2 L 7 2 4F RT A21EA 2007062800120 20070628 00120 SO 2007 6 28 C2XA07IA144 1 20070620 A 2150 8152403 ACM EMB 145 EMB145LR 3260212 SO NR 1 ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 14972 19401 19401 145151 IAH - FLIGHT 2492, DURING PREFLIGHT INSPECTION, THE CREW REPORTED BURNING SMELL WITH THE PACKS ON. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE AIR CYCLE MACHINE (ACM), OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVE D FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007062800121 20070628 00121 SO 2007 6 28 CSXA07ON008 1 20070616 A 2824 2770138101 FLAPPER VALVE EMB 145 EMB145LR 3260212 SO LT WING MISSING A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 27 13553 585 FLT 41 - GEG TO GEG - FUEL COMING FROM LT WING DURING CLIMBING - REPO'D 568 FROM ONT WITH MX PERSONAL AND PERTS. MX INS PECTED FUEL TANK AND FOUND MOST OUTBOARD FLAPPER VALVE MISSING. MX INSTALLED NEW LT WING FLAPPER VALVE AND PERFORMED OP ERATIONAL CHECKS SUCCESFULLY. THE A/C WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007062800122 20070628 00122 NM 2007 6 28 NOCA13307 1 20070612 A 3320 BALLAST BOEING 767 767324 1385203 NM GALLEY LIGHT SPARKS A NOCA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 15 767NA 27569 F/A COMPLAINED THAT A SPARK FELL OUT THE FRONT GALLEY FROM THE TOP CEILING AREA. REMOVED AND REPLACED BALLAST M660 PER WDM 33-22-11, ALL OPS OK. AS PRECAUTION INSPECTED ABOVE GALLEY CEILING AREA FOR ANY CHAFED WIRES, BURNED SMELL. NO FAU LTS FOUND. PERFORMED OPS CHECK OF FWD GALLEY C/M OVEN, CEILING & AREA LIGHTS AND OPS CHECKS OKAY. 2 L 7 2 4F RT A1NM 2007062800123 20070628 00123 NM 2007 6 28 NOCA13107 1 20070525 A 2530 OVEN BOEING 767 767324 1385203 NM GALLEY SPARKS A NOCA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 EA 15 767NA 27569 ON TOUCHDOWN, FWD GALLEY CENTER OVEN SPARKED. NO SMOKE NOTED, NO SMELL NOTED. PULLED & SECURED C/B FOR FWD CENTER GALL EY OVEN NR 105 OPEN CI 25-57 PER MEL 25-20-1. 2 L 7 2 4F RT A1NM 2007062800124 20070628 00124 NM 2007 6 28 NOCA13207 1 20070605 A 2520 UNKNOWN BOEING 767 767324 1385203 NM GALLEY UNKNOWN A NOCA O OTHER O OTHER NR NOT REPORTED 1 EA 15 767NA 27569 PURSER ADVISE POPPING SOUND ACCOMPANIED BY WHITE FLASH OBSERVED FROM ABOVE AFT SECTION OF FWD GALLEY (COFFEEMAKER SECTIO N) NO SECONDARY INDICATION. REMOVED COFFEEMAKER & ELECTRICAL PANEL FROM FWD GALLEY AREA VISUALLY CHECKED ALL WIRING AND CONNECTOR FOR EVIDENCE OF FAULT. NO DEFECTS FOUND. OPENED CEILING PANELS ABOVE SEAL ROWS AND VISUALLY CHECKED AREA FO R CHAFE WIRING AND ELECTRICAL SHORT ODOR. NO DEFECTS FOUND. NO EVIDENCE OF ANY CIRCUIT BREAKER POPPED. RESTORED ALL C OFFEEMAKERS AND OPS AND LEAK CHECK NORMAL, UNABLE TO DUPLICATE OR FIND ANY DEFECTS. OPS CHECKS ALL GALLEY LIGHTS, OPS C HECKS NORMAL. 2 L 7 2 4F RT A1NM 2007062800125 20070628 00125 NM 2007 6 28 SWAA073064 1 20070620 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 360 S14R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007062800126 20070628 00126 NM 2007 6 28 SWAA073061 1 20070620 A 2750 69466493 TORQUE TUBE BOEING 737 7373H4 1384600 NM LT WING TE FLAP WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED HC2 CHECK, FOUND LEFT WING OUTBOARD T/E FLAP TORQUE TUBE WORN OUTBOARD OF 120 DEGREE GEARBOX. REMOVED AND REPLACED TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007062800127 20070628 00127 NM 2007 6 28 SWAA073062 1 20070620 A 2750 69466493 TORQUE TUBE BOEING 737 7373H4 1384600 NM RT WING TE FLAP WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED HC2 CHECK, FOUND RIGHT WING 90 DEGREE TORQUE TUBE WORN AT NR 6 TRANSMISSION. REMOVED AND REPLACED TORQ UE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007062800128 20070628 00128 NM 2007 6 28 SWAA073059 1 20070620 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 500 S27R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED SPV CHECK, FOUND STRINGER 27R CORRODED AT BS 500. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007062800129 20070628 00129 NM 2007 6 28 SWAA073058 1 20070620 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 480-492 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED SPV CHECK, FOUND STRINGER 28R CORRODED BETWEEN BS 480 AND BS 492. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007062800130 20070628 00130 NM 2007 6 28 SWAA073073 1 20070620 A 3350 MS155721 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED A1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007062800131 20070628 00131 NM 2007 6 28 SWAA073070 1 20070617 A 2560 P2070001 FLASHLIGHT BOEING 737 73776Q 13845AA NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 551WN 30280 DURING SCHEDULED BRDG CHECK, FOUND FWD OUTBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2007062500096 20070625 00096 EU 2007 6 25 AWXA200700735 1 20070614 A 2913 887673 PUMP AIRBUS 320 A320232 3930326 EU NR 1 ENGINE FAILED A AWXA O OTHER K FLUID LOSS CR CRUISE 1 WP 28 642AW 26921 6322 584 LAS - EWR - AT CRUISE, THE CREW RECEIVED A GREEN PUMP LO PRESS RVR AND GREEN RESVR LOW LEVEL ECAM MESSAGES. CREW DECLAR ED AN EMERGENCY AND PERFORMED AN EMERGENCY EXTENSION OF LANDING GEAR. THE LANDING WAS UNEVENTFUL. REMOVED AND REPLACED NR 1 (GREEN) ENGINE DRIVEN PUMP PER AMM 29-11-51 PB 401, OPS LEAK CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007062500097 20070625 00097 NM 2007 6 25 DHL2007783513 1 20070604 A 5320 7075T6 WEB BOEING 727 727227 1384078 NM AFT AIRSTAIRS CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 LT SIDE AIRSTAIRS WEB PANEL CRACKED AT LIGHTING HOLE, BS 1223, WL 156, LBL 21. CUT OUT DAMAGED AREA DIM .5 BY .5 IAW B7 27 SRM 51-40-2, FIG 1. FABRICATED DOUBLER REPAIR, MATERIAL USED 7075T6, 040, 4 BY 2.50 IAW B727 SRM 51-40-2, FIG 1 AND 53-10-2, FIG 6. TREATED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 51-10-2, 51-40-2, FIG 1 AND 53-30-2. 2 L 7 3 4F A3WE 2007062500098 20070625 00098 NM 2007 6 25 DHL2007740550 1 20070608 A 5340 BRACKET BOEING 727 7272Q9 138448M NM BS 970 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AFT PIT BS 970 BETWEEN STR 26L AND 25L, ANGLE SUPPORT BRACKET ATTACHED TO FRAME CRACKED AND CORRODED. REMOVED CRACKED B RACKET, FABRICATED NEW BRACKET FROM BAC1505-01210, PO NR 7161380, 7.25" BY 2.5", PER B727 SRM 53-10-4 FIG 13 AND 53-10-2 FIG 5. TREATED, PRIMED, AND INSTALLED SPT BRACKET PER B727 SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007062500099 20070625 00099 NM 2007 6 25 DHL2007783514 1 20070605 A 5310 DOOR FRAME BOEING 727 727227 1384078 NM BS 950E DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 NR 2 CARGO DOOR CUT-OUT FWD FRAME, BS 950E INNER CHORD IS DENTED BETWEEN STR 25R AND 26R. REMOVED CORROSION RT NR 2 CAR GO DOOR CUT OUT IAW B727 SRM 57-10-1, FIG 1. MATERIAL LOSS, .027, ORIGINAL THICKNESS .150, MATERIAL REMAINING .113 OUT OF LIMITS IAW B727 SRM 57-10-1, FIG 1. REMOVED INTERCOSTAL BETWEEN 950D TO 950E, STR 26R IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA DIM. .4 BY 1.25 IAW B727 SRM 51-40-4, FIG 1. FABRICATED REPAIR ANGLES 2 EACH, MATERIAL USED 7075T6, .040 , 12.50 BY 3 AND 1 EACH STRAP, MATERIAL USED 7075T6, .125, 14.50 BY 1.25 AND 2 EACH FILLERS, MATERIAL USED 7075T6, .160, 4 BY 1.25 IAW B727 SRM 51-40-4, FIG 1 AND 53-10-2, FIG 2. TREATED, PRIMED AND INSTALLED REPAIR AND FITTING, INTERCOSTA 2 L 7 3 4F A3WE 2007062500100 20070625 00100 NM 2007 6 25 DHL2007783517 1 20070605 A 5310 DOOR FRAME BOEING 727 727227 1384078 NM AFT LWR CARGO CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 NR 2 CARGO DOOR CUT-OUT AFT FRAME, BS 990, RBL 22, WL 147.6 INNER CHORD SHOWS CORROSION SPOTS INNER SIDE AND DENT FROM O UTER SIDE. BLENDED OUT DAMAGED AREA AT NR 2 CARGO DOOR CUT OUT AFT FRAME BS 990 IAW B727 SRM 51-10-1, MATERIAL LOSS .01 7, ORIGINAL MATERIAL THICKNESS .150, MATERIAL REMAINING .133”, FOUND TO BE OUT OF LIMITS IAW B727 SRM 51-10-1 FIG 1. RE MOVED FITTING IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA DIM 1.75 BY 1.25 IAW B727 SRM 51-40-4, FIG 1. FABRICATED REPA IR 2 EACH ANGLES, MATERIAL USED 7075T6, .040, DIM 8.25” BY 3.25, 1 EACH STRAP, MATERIAL USED 7075T6, .125, DIM 10.25” BY 1.25, 1 EACH FILLER, MATERIAL USED 7075T6, .160, DIM 1.75 BY 1.25 IAW B727 SRM 51-40-4, FIG 1, 53-10-2, FIG 8. TREATED 2 L 7 3 4F A3WE 2007062500101 20070625 00101 NM 2007 6 25 DHL2007740552 1 20070614 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 1148 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AFT CARGO BS 1148 BETWEEN STR'S 28L AND 29L, AFT SIDE OF FRAME HAS CORROSION BELOW FAIL/SAFE CHORD. CORROSION BEYOND LI MITS PER B727 SRM 53-10-1 FIG 1. CUT OUT DAMAGED AREA 5" BY 1.5", FABRICATED REPAIR DOUBLER FROM 7075-T6, .071" BY 6" B Y 4", PO NR 9004940, FILLER FROM 7075-T6, .063" BY 5" BY 2", PO NR 9004960, PER B727 SRM 53-10-4 FIG 13 AND 53-10-2 FIG 5. TREATED, PRIMED, AND INSTALLED REPAIR PARTS PER B727 SRM 51-10-2 AND 53-10-4 FIG 13. 2 L 7 3 4F RT A3WE 2007062500102 20070625 00102 NM 2007 6 25 DHL2007740553 1 20070613 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 1030 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AFT CARGO BS 1030 AT STR 25L, FRAME DENTED ON INNER CHORD. CUT OUT DAMAGED FRAME SECTION, 2" BY .050", FABRICATED REPAI R ANGLE FROM 7075-T0, .071" BY 10.5" BY 1" BY .075", PO NR 9004690 AND FILLER FROM 7075-T6, .063" BY 2" BY .050", PO NR 9005138, PER B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1. HEAT TREATED REPAIR ANGLE TO T6 CONDITION PER FASI ENGINEERING R EPORT NR 2-37153-801 REV A. TREATED, PRIMED, AND INSTALLED REPAIR PARTS PER B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2007062500103 20070625 00103 EU 2007 6 25 MALA070067 1 20070612 A 2120 UNKNOWN SAAB SF340 340B 7860101 EU CABIN ODOR A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 15 423XJ 340B423 CREW REPORTED BURNING SMELL IN CABIN. SUPPLEMENTAL AC SHUT OFF IN FLIGHT AND WOULDN'T TURN ON AGAIN. AC LANDED WITHOUT FURTHER INCIDENT. INSPECTED AC, TRANSFERRED TO DMR IAW MEL 21-50-2 SAAB 340 CAT C. ALL PLACARDS INSTALLED. C/B N18 A ND N19 PULLED PER MX CONTROL. 2 L 7 2 4T RT A52EU 2007062500104 20070625 00104 2007 6 25 QXEA200700971 4 20070615 A 3418 501177004 ACTUATOR BOMBDR DHC8 DHC8402 1390042 NM STALL WARNING MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 402QX 15531 15531 4032 BIL FLIGHT NR 2417: PUSHER SYSTEM FAIL DURING T/O ROLL. ABORTED THE TAKEOFF AND WAS ADVISED TO RETURN TO THE GATE. MAI NTENANCE REMOVED AND REPLACED THE STICK PUSHER IAW AMM 27-33-06-000-801 AND 27-33-06-400-801. PERFORMED OPS CHECK IAW A MM 27-33-00-710-807. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007062500105 20070625 00105 SO 2007 6 25 SWIA200718333 1 20070612 A 5210 ROLLER EMB 120 EMB120ER 3260203 SO PAX DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 250YV 120250 COULD NOT OPEN THE CABIN DOOR FROM THE OUTSIDE. ADJUSTED THE FORWARD AND AFT PAX DOOR UPPER ROLLERS ON FUSELAGE CUT OUT . OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007062500106 20070625 00106 EA 2007 6 25 SWIA200718334 1 20070614 A 3310 LIGHT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT SHORTED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 701SK 10133 CAPTAINS CHART HOLDER LIGHT ON THE YOKE IS SHORTED AND THE CIRCUIT BREAKER IS POPPED. TIGHTENED SCREW ON BACK OF CHARTH OLDER AND RESET CIRCUIT BREAKER. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007062500107 20070625 00107 EA 2007 6 25 SWIA200718335 1 20070613 A 3350 CHARGER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 772SK 10235 CREW REPORTS THAT EMERGENCY LIGHTS STAY ON WITH THE SWITCH IN THE OFF POSITION. REPLACED NR 2 ELBP CHARGER IAW CRJ 700 AMM 33-51-17. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007062500108 20070625 00108 EA 2007 6 25 SWIA200718336 1 20070609 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA LEFT SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 864AS 7502 LEFT PACK TEMPERATURE WILL NOT COOL DOWN AND SMELLS OF SMOKE. REPLACED LEFT PACK IAW AMM 21-57-10. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007062500109 20070625 00109 SO 2007 6 25 SWIA200718337 1 20070610 A 3397 LIGHT EMB 120 EMB120ER 3260203 SO CABIN MISWIRED A SWIA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 NM 07 251YV 120251 LIGHT INOP ON EMERGENCY LIGHT STRIP AT SEAT 9A. REWIRED EMERGENCY TRACK FLOOR LIGHT AT SEAT 9A. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007062500110 20070625 00110 SO 2007 6 25 SWIA200718338 1 20070609 A 5610 NP1513112 WINDSHIELD EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 568SW 2146 2146 120343 FIRST OFFICERS WINDSHIELD IS CRACKED ON OUTER LAYER. REPLACED WINDSHIELD IAW MM 56-10-01. 2 L 7 2 4T RT A31SO 2007062500112 20070625 00112 EA 2007 6 25 SWIA200718340 1 20070612 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 956SW 7825 LIGHTED EMERGENCY EXIT SIGN IN GALLEY DOES NOT ILLUMINATE. RELAMPED THE EMERGENCY EXIT SIGN IAW AMM 33-51-21. 2 L 7 2 4F RT A21EA 2007062500113 20070625 00113 EA 2007 6 25 SWIA200718341 1 20070609 A 3230 TORQUE LINK CNDAIR CL600 CL6002B19 1900309 EA MLG DISCONNECTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 433SW 7550 RECEIVED A GEAR DISAGREE WARNING AND A NOSE DOOR OPEN WARNING WHEN SELECTING GEAR UP. RETURNED TO DFW. FOUND TORQUE LI NKS DISCONNECTED AND NOSE TIRES SHOWING CHORD. REMOVED AND REPLACED BOTH NOSE WHEEL ASSYS IAW AMM 32-42-01, PN 5010598, SN OFF NOV02-4502 PN 5010598, SN OFF: MAY03-0142. 2 L 7 2 4F RT A21EA 2007062500114 20070625 00114 EA 2007 6 25 SWIA200718342 1 20070608 A 3350 AD20131A POWER SUPPLY CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 800SK 48 48 15060 MAIN CABIN VERTICAL EMERGENCY EXIT AND BOTH OVERWING EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED NR 3 EMERGENCY BATT ERY PACK IAW MM 33-51-17. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007062500115 20070625 00115 EA 2007 6 25 SWIA200718343 1 20070616 A 2730 PIN CNDAIR CL600 CL6002B19 1900309 EA PCU BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 413SW 7102 RIGHT ELEVATOR NR 2 HYDRAULIC SYSTEM PCU ATTACH END FITTING LOWER SHEAR PIN IS BROKEN. REPLACED RIGHT ELEVATOR NR 2 HYD RAULIC SYSTEM PCU LOWER SHEAR PIN IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007062500116 20070625 00116 EA 2007 6 25 SWIA200718344 1 20070615 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 905SW 7437 GALLEY EMERGENCY EXIT LIGHT IS INOP. RELAMPED EMERGENCY EXIT LIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007062500117 20070625 00117 EA 2007 6 25 SWIA200718345 1 20070615 A 2710 BEARING CNDAIR CL600 CL6002B19 1900309 EA TORQUE TUBE ROUGH A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 423SW 7456 NOTCH IS FELT ON FIRST OFFICERS YOKE WHEN TURNED TO THE LEFT OR RIGHT. REPLACED AILERON TORQUE TUBE RIGHT BEARING IAW A MM 20-26-00. 2 L 7 2 4F RT A21EA 2007062500126 20070625 00126 SO 2007 6 25 SIMA200717506 1 20070620 A 5310 STRUCTURE EMB 135 EMB135LR 3260305 SO FUSELAGE DAMAGED A SIMA O OTHER O OTHER LD LANDING 1 SW 21 731BE 145356 AIRCRAFT STRUCK RUNWAY WITH ALL THREE LANDING GEAR IN THE UP AND STOWED POSITION, GO AROUND PROCEDURE WAS EXECUTED. REC EIVED FLAP FAIL MESSAGE DURING SECOND APPROACH. EMERGENCY DECLARED. EMERGENCY GEAR EXTENSION PROCEDURES WAS PERFORMED WITH THREE GREEN DOWN AND LOCKED LIGHTS. GEAR POSITION VERIFIED WITH TOWER. A NO FLAP LANDING WAS PERFORMED. PASSENGE RS WERE DEPLANED BY STAIRS. POSTFLIGHT INSPECTION REVEALED DAMAGE TO THE FLAPS AND BELLY. 2 L 7 2 4F RT T00011AT 2007062500127 20070625 00127 SO 2007 6 25 SIMA200717503 1 20070620 A 3397 860CC01 CONTACT EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHTS FAILED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 851AE 9836 145734 RECEIVED EMERGENCY LIGHT NOT ARM MESSAGE, ABORTED TAKEOFF. REMOVED AND REPLACED ESSENTIAL BUS TIE CONTACTOR IAW EMB AMM 24-60-03. OPERATIONAL CHECKED GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007062500128 20070625 00128 NM 2007 6 25 UIEA200700255 1 20070621 A 5330 PANEL BOEING 747 7472D7B 1384803 NM BS 1112 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 LOWER FUSELAGE CENTER PANELS 191HH AND 191JJ BETWEEN NR 1 AND NR 3 ACM'S HAVE AREA OF CORROSION. PERMANENT REPAIR WAS A CCOMPLISHED AS PER 747-200 SRM 51-40-02 FIG 1. ALSO, REFERENCE ATLAS AIR XEO NR 53-062007. 2 L 7 4 4F RT A20WE 2007062500129 20070625 00129 NM 2007 6 25 UIEA200700246 1 20070610 A 5330 SKIN BOEING 747 747243B 1384830 NM BS 2605 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 BS 2605 FOUND DENT AND CRACK BETWEEN STRINGER 46R AND 49R AREA JUST BETWEEN 2 PREVIOUS DOUBLERS. SKIN REPAIRED AS PER B OEING MESSAGE 1-343200877-4 AND FAA FORM 8100-9. 2 L 7 4 4F A20WE 2007062500130 20070625 00130 NM 2007 6 25 UIEA200700245 1 20070610 A 5414 SKIN BOEING 747 747243B 1384830 NM NR 3 NACELLE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 NR 3 PYLON OVAL PANEL 473AR CUTOUT CRACKED LOWER AFT SKIN. NR 3 PYLON OVAL PANEL 473AR CRACKED SKIN REPAIRED AS PER BOE ING MESSAGE 1-351859671-9 AND FAA FORM 8100-9. 2 L 7 4 4F A20WE 2007062600005 20070626 00005 2007 6 26 DHLA200700032 4 20070616 A 2565 UNKNOWN AIRBUS 300 A300B4203 3930306 EU SLIDE LIGHT UNKNOWN A DHLA O OTHER N FALSE WARNING CR CRUISE 1 GL 05 367DH 265 RED SLIDE WARNING LIGHT FLASHING ON RIGHT DOOR IN FLT, TRANSFERED TO NR 087010. PERFORMED OPERATIONAL TEST OF EMERGENCY ESCAPE SLIDE RELEASE WARNING AND LIMIT SWITCHES IAW A300 MM 52-73-00 AND 52-73-13, CHKED NORMAL. 2 L 7 2 4F RT A35EU 2007062600015 20070626 00015 EU 2007 6 26 07FDEA02188 1 20070619 A 5330 A53985255203 DOUBLER AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 UPPER SKIN PANEL C87 RT JOINT STRAP DOUBLER WITH CORROSION REPAIR PERFORMED BY BLEND OUT THE CORRODED AREA IAW EA 6-5431 9-112442 AND RAS/DAHAM/4022370/2007 ISS. B. 2 L 7 2 4F RT A35EU 2007062600016 20070626 00016 EU 2007 6 26 07FDEA02190 1 20070619 A 5340 SUPPORT FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 726FD 575 CORROSION ON Y-Z LATCH SUPPORT FITTING, C25A, RT. REPAIR PERFORMED IAW SRM 53-13-13 / FIG 204, SHEET 1 AND 2. 2 L 7 2 4F RT A35EU 2007062600021 20070626 00021 EU 2007 6 26 07FDEA02195 1 20070619 A 5313 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 DAMAGED STRINGERS FOUND BETWEEN C28-29, STRG 53 RT AND BETWEEN C27-28, STRG 40 LT. STRINGER REPAIR PERFORMED IAW SRM 53 -10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007062600023 20070626 00023 EU 2007 6 26 07FDEA02197 1 20070619 A 3150 WARNING LIGHT AIRBUS 300 A300F4605R 3930327 EU ACTIVATED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 674FE 781 PASSING FL250 ECAM WARNING ALERT FOR MAIN DECK CARGO DOOR UNSAFE. RTN TO DEN AIRPORT. NO SIGN OF ACTUAL UNSAFE DOOR. WARNING STOPPED AT 500 FEET ABOVE GROUND. RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 29JUN07 " MEL 52-71-01: MAIN CARGO DECK DOOR CLOSED AND LOCKED INDICATION ON ECAM DOOR PAGE, INOP. MAIN CARGO DECK DOOR VISUALLY CHECKED CLOSED AND LOCKED. [07-03-07] ADJUSTED SWITCH 49WS USING TEST BOX 35M5M01160001 REF A300 M/M 52-71-11-5-02. ALL INDICATIONS NORMAL AT THIS TIME. ITEM CLEARED A/C OK TO CONT. 2 L 7 2 4F RT A35EU 2007062600026 20070626 00026 NM 2007 6 26 07FDEA02200 1 20070619 A 5315 65162796 FLOORBEAM BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 CABIN FLOOR SUPPORT WEB AT STA 804 RBL 45 IS CRACKED OUT FASTENER HOLE. REMOVED, FABRICATED AND INSTALLED FLOOR SUPPORT WEB STA 804, RBL 5, SRM 51-30-2, DWG 65-16279. 2 L 7 3 4F RT A3WE 2007062600032 20070626 00032 NM 2007 6 26 07FDEA02206 1 20070619 A 5322 65561251 SHEAR TIE BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT PIT SHEAR TIE CORRODED STA 950E BETWEEN STR 28-29L. REMOVED CORRODED SHEAR TIE AND REPAIRED PER SRM 53-10-4 FIG 15. 2 L 7 3 4F RT A3WE 2007062600036 20070626 00036 NM 2007 6 26 07FDEA02210 1 20070619 A 5330 6572702 SKIN BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LOWER EXTERNAL SKIN IS CRACKED AT BS 1082, RBL 4. R EMOVED SURROUNDING STRUCTURE TO ACCESS DAMAGE. REMOVED DAMAGE, NDT VERIFIED DAMAGE REMOVAL, NO DEFECTS. INSTALLED DOUBLER AND FILLER WHERE DAMAGE WAS REMOVED. INSTALLED SURROUNDING ST RUCTURE REF SRM 51-30-2, SRM 53-30-2 FIG 2 AND 3, NDT MAN PART 6 51-00-00, FIG 23. 2 L 7 3 4F RT A3WE 2007062600042 20070626 00042 NM 2007 6 26 AWXA200700726 1 20070618 A 5311 90526911 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - FOUND CRACKED FRAME, BS 787, S9R. REPAIRED FRAME, BS 787, S9R IAW AWA ER 03-5362-07165-ES1. 2 L 7 2 4F RT A16WE 2007062600044 20070626 00044 NM 2007 6 26 AWXA200700728 1 20070418 A 5311 654655514 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - FOUND CRACKED FRAME, BS 867, S9R. REPAIRED FRAME, BS 867, S9R IAW AWA ER 03-5362-07165-ES1. 2 L 7 2 4F RT A16WE 2007062600047 20070626 00047 NM 2007 6 26 AWXA200700741 1 20070418 A 5311 65465525002 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - FOUND CRACKED FRAME, BS 827, S9R. REPAIRED FRAME, BS 827, S9R IAW AWA ER 03-5362-07165-ES1. 2 L 7 2 4F RT A16WE 2007062600059 20070626 00059 WP 2007 6 26 AALA20071023 1 20070605 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9681B 53631 SFO - EMERGENCY LIGHTS AT SEAT ROW 11 INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHTS AT SEAT ROW 11. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007062600065 20070626 00065 NM 2007 6 26 AALA20071043 1 20070608 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 792AN 30253 ORD - EMERGENCY EXIT LIGHT AT LEFT NUMBER ONE DOOR OVERHEAD INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT LEFT NUMBER O NE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007062600074 20070626 00074 NM 2007 6 26 AALA20071034 1 20070607 A 3397 WIRE HARNESS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 760AN 31477 ORD - SEAT MOUNTED EMERGENCY LIGHTS IN AFT COACH CABIN INOPERATIVE. REPAIRED PINS IN HARNESS AT SEAT ROW 32DEF FOR EMER GENCY LIGHTS IN AFT COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007062600076 20070626 00076 NM 2007 6 26 AALA20071033 1 20070606 A 3397 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 DFW - EMERGENCY LIGHTS AT SEAT ROW 13 INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHTS AT SEAT ROW 13. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007062600085 20070626 00085 NM 2007 6 26 AALA20071018 1 20070603 A 2560 STRAP BOEING 757 757223 1384957 NM FLASHLIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 690AA 25696 MIA - EMERGENCY FLASHLIGHT AT LEFT NUMBER TWO FLIGHT ATTENDANT SEAT HAS MISSING STRAP. REPLACED STRAP FOR EMERGENCY FLA SHLIGHT AT LEFT NUMBER TWO FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007062600089 20070626 00089 NE 2007 6 26 AALA20071006 2 20070601 A 7200 ANNULAR FILLER BOEING 757 757223 1384957 NM RROYCE RB211 RB211535* NE LT ENGINE FAILED A AALA A UNSCHED LANDING N Y FALSE WARNING ENGINE STOPPAGE CL CLIMB 1 SW 21 179AA 32397 31844 ORD INFLIGHT T225/01JUN - AFTER TAKEOFF, LEFT ENGINE FAIL AND FIRE WARNING. FIRE HANDLE PULLED AND BOTH BOTTLES DISCHA RGED. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. NO FIRE FOUND. SINGLE ENGINE TIME 5 TO 6 MINUTES. REPLACED NUMBER ONE ENGINE ON 03 JUN AT ORD DUE TO THREE ANNU7LUS FILLERS DEPARTED BLADE HUB AND DAMAGED ENGINE CASE. ONE FILLER LODGE D IN ENGINE STARTER DUCT AND DAMAGED ONE OF THE FIRE WARNING DETECTOR LOOPS AT APPROXIMATELY 7 O`CLOCK POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2007062600090 20070626 00090 WP 2007 6 26 AALA20071015 1 20070603 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 274AA 49271 SFO - EMERGENCY LIGHT AT SEAT 17D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F A6WE 2007062600093 20070626 00093 EU 2007 6 26 F3LA200700135 1 20070609 A 5315 D5347218820200 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 907FR 5061 1743 DURING C4/S1 CHECK, INSPECTION REPORTED ONE AREA OF CORROSION ON FLOORBEAM +Y1292 AT FR67. REPLACED FLOORBEAM IAW SRM 5 1-42-11, SRM 51-44-11, AND EA #A0-53T-11472. 2 L 7 2 4F RT A28NM 2007062600109 20070626 00109 NM 2007 6 26 DHL2007740555 1 20070618 A 5330 SKIN BOEING 727 7272Q9 138448M NM BS 196 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 LOWER HALF OF FUSELAGE EXTERIOR SURFACE, DENT AT BS 196, BETWEEN STR 22L AND 23L. CUT OUT DAMAGED AREA, .750" DIA CIRCL E CUT, FABRICATED REPAIR DOUBLER FROM 2024-T3, .050" BY 4" DIA, PO NR 9005049; AND FILLER FROM 2024-T3, .040" BY .750" DIA, PO NR 9005089, PER B727 SRM 53-30-3 FIG 13, DETAIL I. TREATED, PRIMED, AND INSTALLED REPAIR PARTS PER B727 SRM 51 -10-2 AND 53-30-3 FIG 13. 2 L 7 3 4F RT A3WE 2007062600112 20070626 00112 WP 2007 6 26 DHL2007803536 1 20070610 A 5100 NONE DOUG DC8 DC873 302199C WP NONE NONE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 REMOVE REPAIR BELOW MAIN CARGO DOOR AT STA 226 AND INSPECT AREA. INSTALL NEW REPAIR IAW SRM (PERMANENT) AND APPROVED DAT A. ENTER INFORMATION ON 337 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-08-07, DWG NR AD42-53- 112 REV IR DATED 06-01-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED REPAIR DOUBLER (A L7075T6 0.080") AND INTERNAL FINGER DOUBLER (AL7075T6 0.050") IAW DWG NR AD42-53-112. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DWG NR AD42-53-112, SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D , SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007062600114 20070626 00114 WP 2007 6 26 DHL2007803545 1 20070614 A 5330 5653568501 SKIN DOUG DC8 DC873 302199C WP FUSELAGE DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 LT AFT ADF SENSE ANTENNA SKIN DELAMINATED. REMOVED AND REPLACED LT AFT ADF SENSE ANTENNA IAW SRM 51-3-0. 2 L 7 4 4F RT 4A25 2007062600120 20070626 00120 WP 2007 6 26 DHL2007803543 1 20070610 A 5411 FRAME DOUG DC8 DC873 302199C WP GE CFM56 CFM562C1 13802 NE NACELLE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 NR 3 ENG T/R FIXED STRUCTURE AND FWD FRAME WORN STA YN 202.000 AT 5 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3- DATED 06-08-07, DWG NR AD42-78-110 REV IR DATED 05-30-07. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED FRAME SEGMENT (AL6061T6 0.071") IAW DWG AD42-78-110. INSTALLED FRAME SEGMENT IAW DWG AD42-78-110 REV IR, SRM 51-1-11, SRM 51-1-21, SRM 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F 4 F RT 4A25 E2GL 2007062600126 20070626 00126 WP 2007 6 26 DHL2007803535 1 20070608 A 5280 CHANNEL DOUG DC8 DC873 302199C WP BS 870 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 83934 46123 RT MLG INBD DOOR ZEE CHANNEL WORN STA 870.000 RBL 50" (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-06-07, DWG NR AD42-52-0108 REV IR DATED 05-22-07. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER (STEEL 301 1/2H 0.040") AND FILLER (AL7075T6 0.063") IAW DWG3 AD42-52-108. CLEANE D, TREATED AND PRIMED AREA AND FILLER IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DWG3 AD42-52-108, SRM 51-1-11, SRM 51 -1-21. OPS CHECKED GOOD IAW MM 32-30-0 PG 201. 2 L 7 4 4F RT 4A25 2007062600128 20070626 00128 NM 2007 6 26 DHL2007783519 1 20070605 A 5322 BAC1505100246 SHEAR TIE BOEING 727 727227 1384078 NM BS 620 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 PILLOWING AT FASTENERS ON LWR FUSELAGE STR 27L, BS 620. REMOVED SHEAR TIE AT STA 620 BETWEEN STR 26L AND 27L IAW B727 S RM 51-30-2. FABRICATED NEW T-ANGLE SHEAR TIE FROM BAC1505-100246 7075T6, .063, 6.50 BY 2 IAW B727 SRM 53-10-2, FIG 3 AN D 51-10-3, FIG 1. TREATED, PRIMED AND INSTALLED SHEAR TIE IAW B727 SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 2007062600131 20070626 00131 NM 2007 6 26 DU4R2007141 1 20070608 A 5753 113N21052 TORQUE TUBE BOEING 757 757232 1384965 NM TE FLAP CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 640DL 23994 FOUND RUSTED RT I/B FLAP I/B TORQUE TUBE. REPAIRED BY REMOVING AND REPLACING TORQUE TUBE AND FAIL SAFE TUBE WITH P/N’S 113N2105-2 AND 113N2108-1 IAW B757 MM 57-53-44. 2 L 7 2 4F RT A2NM 2007062600134 20070626 00134 2007 6 26 UPS07849983 4 20070617 A 2565 SLIDE DOUG DC8 DC873F 302199F WP CABIN DOOR MISINSTALLED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 818UP 46108 MAIN EXIT ESCAPE SLIDE IS IMPROPERLY LOCATED INSIDE HOUSING. PRESSURE CANNOT BE READ. REMOVED AND REPLACED MAIN EXIT E SCAPE SLIDE CONTAINER IAW MM 25-60-01-2. PRESSURE INDICATOR VISIBLE THROUGH WINDOW. 2 L 7 4 4F RT 4A25 2007062600145 20070626 00145 SO 2007 6 26 RAIA00706019 1 20070613 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX STUCK A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 850HK 145003 POST FLT NR 7976 - STL - PAX DOOR HARD TO OPEN. MAINTENANCE INSPECTED DOOR, OPENED AND CLOSED SEVERAL TIMES BY MAINTENA NCE AND FLIGHT ATTENDANT, NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2007062600146 20070626 00146 SO 2007 6 26 RAIA00706025 1 20070615 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 833HK 145240 PRE FLT NR 8018 - STL - EMERGENCY LIGHT LEFTHAND OVERWING EXIT MARKER INOP. MAINTENANCE CYCLED POWER SYSTEM CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007062600149 20070626 00149 NM 2007 6 26 ASAA0741783 1 20070613 A 5330 6545768300 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 FUSELAGE SKIN IS DENTED OVER A STRINGER AND IN ADJACENT BAYS. CUT OUT DAMAGED AREA OF SKIN FABRICATED AND INSTALLED REP AIR FILLER DOUBLER AND TRIPLER IAW SRM 53-00-01 FIG 201 REPAIR 31. 2 L 7 2 4F RT A16WE 2007062600153 20070626 00153 EU 2007 6 26 YENA2007052 1 20070616 A 3610 10010502009 PROCESSOR EMB ERJ190 ERJ190100IGW 3260408 EU CONTROLLER UNKNOWN A YENA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 15 179JB 3068 19000006 INFLIGHT AT FL380 APU WAS OFF, GOT CAUTION -BLEED APU LEAK-. WOULDN'T CLEAR FOLLOWED QRH. BLEED 1 OFF X BLEED OPEN. C LEARED THE AMBER LINE ON THE ECS PAGE. DECLARED EMERGENCY. T/S PER FIM 36-22-00. REPLACED BOTH AMS CONTROLLER PROCESS OR MODULES, PER MM 21-00-01. OPS CHECK OK, NO FURTHER MESSAGES. OK FOR SERVICE. 2 L 7 2 4F RT A57NM 2007062600154 20070626 00154 EA 2007 6 26 TRAX200700840 1 20070612 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 390CA 10106 FS 280 FWD FLOOR SUPPORT ANGLE CORRODED. [06-26-07] REPAIRED IAW CRJ SRM 51-42-06, 51-42-21 AND 51-45-00. 2 L 7 2 4F RT A21EA 2007062600156 20070626 00156 EA 2007 6 26 TRAX200700842 1 20070613 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 973EV 7575 LEFT FLOOR SILL CORRODED BETWEEN FS 574 TO FS 621. 2 L 7 2 4F RT A21EA 2007062600161 20070626 00161 EA 2007 6 26 TRAX200700847 1 20070614 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 973EV 7575 CORROSION ON FWD AND AFT BRACKET OF PASSENGER DOOR FLOOR SILL NEAR HINGE ATTACHMENT POINTS. 2 L 7 2 4F RT A21EA 2007062600162 20070626 00162 EA 2007 6 26 TRAX200700848 1 20070614 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 937EV 8042 AT I/S 484.00 RIGHT INTERCOSTAL AND CLIP ARE CRACKED, LEFT INTERCOSTAL IS CRACKED. 2 L 7 2 4F RT A21EA 2007062600163 20070626 00163 EA 2007 6 26 TRAX200700849 1 20070614 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 349 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 973EV 7575 CORROSION FOUND ON TOP OF BEAM BETWEEN LBL 27 TO 40 FS 349.00. 2 L 7 2 4F RT A21EA 2007062600164 20070626 00164 EA 2007 6 26 TRAX200700850 1 20070614 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 973EV 7575 CLIP CRACKED AT FS 484 LBL 36 UNDER FLOOR. 2 L 7 2 4F RT A21EA 2007062600165 20070626 00165 EA 2007 6 26 TRAX200700856 1 20070615 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 886AS 7531 PAX DOOR EXTERNAL HANDLE FLAPPER IS CRACKED. [06-26-07] REPAIRED IAW CRJ SRM 51-42-06, 51-25-06, 51-25-16, AND CRJ MM 1 1-20-00. 2 L 7 2 4F RT A21EA 2007062600178 20070626 00178 NE 2007 6 26 SWAA073030 2 20070615 A 7200 CFM567B24G22 ENGINE BOEING 737 7377H4 1384404 NM GE CFM56 CFM567B24 NE RH WING FAILED A SWAA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SW 29 466WN 30677 890869 INFLIGHT SHUTDOWN / DECLARED EMERGENCY. AT 24,000 FT NR 2 ENGINE OIL BYPASS LIGHT ILLUMINATED. OIL PRESSURE LIGHT ALSO ILLUMINATED AND NR 2 ENGINE FAILED. REMOVED AND REPLACED NR 2 ENGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007062600182 20070626 00182 NM 2007 6 26 SWAA073039 1 20070618 A 3350 MS155721 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED 14Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007062600187 20070626 00187 2007 6 26 2007UALA01691 4 20070525 A 3417 4040800911 COMPUTER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CAPTAIN ADC FAULTY A UALA O OTHER O OTHER AP APPROACH 1 WP 29 179UA 25158 EICAS IAS DISAGREE ON FINAL. CAPTS IAS 8K LOWER THAN F/O AND STBY. *S/D* REPLACED L-AIR DATA COMPUTER PER MM 34-1 2-0 1, ACCOMPLISHED LOW RANGE LEAK TEST PER MM 34-11-00. TESTED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062600194 20070626 00194 NM 2007 6 26 2007UALA02013 1 20070614 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 1R CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 R-1 DOOR UPPER GATE CORRODED. [08-07-07] REMOVED GATE ASSY FROM DOOR AND REMOVED HINGE FROM OLD GATE. REASSEMBLED HIN GE ONTO NEW GATE, AND INSTALLED NEW GATE ON DOOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062600195 20070626 00195 2007 6 26 2007UALA02018 4 20070614 A 2565 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L AFT DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 LEFT AFT DOOR WILL NOT ARM. [08-07-07] REMOVED DOOR BUSTLE AND INSPECTED DOOR ARMING MECHANISM. NO FAULTS NOTED. LUBED ALL DOOR ARMING MECHANISM. NO PROBABLE CAUSE REPORTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062600196 20070626 00196 2007 6 26 2007UALA02021 4 20070614 A 2565 PUSHROD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 2L OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 DOOR 2L DOES NOT FULLY DISARM WHEN HANDLE IS HALFWAY ENGAGED. [08-07-07] CHECKED PAX DOOR 2L EMERGENCY MECHANISM RIG PIN PD5, AND FOUND ITS SETTING OUT OF LIMITS. ADJUSTED PUSH ROD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062600199 20070626 00199 NM 2007 6 26 2007UALA02024 1 20070614 A 2421 GENERATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MALFUNCTIONED A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 570UA 26678 CREW REPORT: RIGHT GENERATOR TRIPPED IN DESCENT WHEN GEN DRIVE LIGHT FLASHED. [08-07-07] ACCOMPLISHED RECHECK FOUN D RT IDG TOOK 90 PUMPS OR 4 PINTS TO FULL, AND FOUND OIL LEAK SIX DROPS PER MIN FROM FUEL OIL COOLER BY PASS VALVE DRAIN LINE. REPLACED FUEL OIL HEAT EXCHANGER BY-PASS VALVE AND IDG. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062600207 20070626 00207 NM 2007 6 26 2007UALA02031 1 20070615 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1540 S26R DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 MAIN FRAME, STA 1540 AT STR 26R, FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062600215 20070626 00215 NM 2007 6 26 2007UALA02039 1 20070615 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1440 S25-26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 MAIN FRAME, STA 1440 BETWEEN STR 25L-26L, FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED -J- ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062600219 20070626 00219 NM 2007 6 26 2007UALA02043 1 20070615 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 DOOR R2 AT UPPER HINGE CUTOUT IS UNDERSERVICED. MAJOR REPAIR ACCOMPLISHED: ACCOMPLISHED INSURANCE CUT AND INSTALLED DO UBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062600220 20070626 00220 NM 2007 6 26 2007UALA02044 1 20070618 A 2530 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 662UA 27159 CREW REPORTS ELECTRICAL BURNING ODOR EMANATING FROM AFT GALLEY AREA. [07-20-07] SUSPECT GALLEY HI-TECH FOODCART TO BE ODOR SOURCE PULLED AFT GALLEY LEFT CIRCUIT BREAKER U7 AND AFT GALLEY RIGHT CB U34 ON PANEL P11 TO ISOLATE POWER. RES ET CBS U7 AND U34 0N P1 1 RAN ALL AFT GALLEY CHILLERS COFFEEMAKERS AND HI-TEC CARTS UNAB LE TO DUPLICATE PROBLEM. FAULT REMOVED. SENT SUSPECT PROBLEM HI-TEC CART FOR SERVICING AT CATERING UNIT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062600221 20070626 00221 NM 2007 6 26 2007UALA02045 1 20070615 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1400 S25-27L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 MAIN FRAME, STA 1400 BETWEEN STR 25L-27L, FRAME HAS 2 EACH DENTS. MAJOR REPAIR ACCOMPLISHED: INSTALLED -J- ANGLE AND N EW PRODUCTION SPLICE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062700002 20070627 00002 CE 2007 6 27 AMWA14030 1 20070615 A 5753 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE TE FLAP WORN A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 161YV 19235 1154 UE161 RIVET IN LT IB FLAP DOVETAIL PULLED THROUGH THE SKIN. REPAIRED IAW BSRM 51-70-00 TYPICAL SKIN REPAIRS RIVET SPACING AND PANEL SIZE WERE AS ORIGINAL 2 L 7 2 4T 4 T RT A24CE E26NE 2007062700003 20070627 00003 CE 2007 6 27 AMWA85394BC 1 20070617 A 2432 CONNECTOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BATTERY CORRODED A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 10675 20031 176 10675 BATT CHARGE ANNUN ILLUMINATES 3-5 MIN, EXTINGUISHES BRIEFLY, RE-ILLUMINATES FOR 2+ MIN, THEN REMAINED EXTINGUISHED FOR R EMAINDER OF FLT. CONTINUED TO DESTINATION W/O FURTHER INCIDENT. CLEANED CORROSION OFF OF CONNECTOR 2 L 7 2 4T 4 T RT A24CE E26NE 2007062700006 20070627 00006 EU 2007 6 27 47106172007 1 20070617 A 2120 UNKNOWN UROCOP EC135 EC135P2 5620027 EU PWA PW206 PW206B 0 NE COCKPIT ODOR E QMLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 530LN 0471 PCEBJ03334 AIRCRAFT AND CREW RETURNING FROM A MEDICAL RUN WHEN A SUDDEN STRONG ODOR OF BURNING FILLED THE COCKPIT AND CREW AREA. NO SMOKE WAS NOTED IN THE AIRCRAFT. PILOT DECLARED AN EMERGENCY AND LANDED. AS OF TIME OF THIS REPORT AIRCRAFT IS GROUNDE D WITH A MECHANIC AND PILOT ATTEMPTING TO ISOLATE PROBLEM AND NO DETERMINATION HAS BEEN MADE. 1 G 7 2 3U 3 U H88EU E42NE 2007062700010 20070627 00010 CE 2007 6 27 DXTA200702269 1 20070616 A 3220 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NOSE WHEEL VIBRATION E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 939QS 7500193 ABORTED TAKEOFF, DUE TO VERY BAD NOSE WHEEL VIRBRATION. KNOCKED OFF YAW DAMP AND FGC. [07-09-07] REMOVED AND REPLACED BOTH NOSE WHEEL ASSY'S DUE TO VIBRATION CHECKED BALANCE OF NEW WHEEL ASSY. COMPLIED WITH NETJETS NOSE GEAR SHIMMY LIST NO DEFECTS NOTED ALL WORK I/A/W CE750 M.M 33-20-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007062700029 20070627 00029 EU 2007 6 27 07FDEA01879 1 20070521 A 5100 NONE AIRBUS 310 A310222 3930315 EU NONE NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON LT LWR WING SURFACE T/E OF INBOARD FLAP WS0-139 RIB1-3. REPAIR REQUIRES EVALUATION F OR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR CONFORMS TO EXISTING FE DEX EA 6-5750-81810. SDR SUBMITTED IN ERROR- ADMINISTRATOR. 2 L 7 2 4F RT A35EU 2007062700031 20070627 00031 EU 2007 6 27 07FDEA01881 1 20070521 A 5753 A57970100002 SKIN AIRBUS 310 A310222 3930315 EU ZONE 500 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON LT LWR WING SURFACE OF INBOARD FLAP WS 339-409 RIB 6-7. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT T O CONFORM TO AN SRM REPAIR. NEW REPAIR ACCOMPLISHED IN ACCORDANCE WITH FEDEX EA 6-5710-112425. 2 L 7 2 4F RT A35EU 2007062700033 20070627 00033 EU 2007 6 27 07FDEA01894 1 20070521 A 5100 NONE AIRBUS 310 A310222 3930315 EU NONE NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON RT WING, L/E OF SLAT 1 WS 139-207 RIB 3-4. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. INSPECTION OF FILLER WAS PERFORMED IAW SRM 57 -40-00. REPAIR IS COVERED BY WRI 5750/4864. REQUIRES INSPECTION OF FILLER AT NEXT C-CHECK. RE-INSPECTION TRACKED UNDE R WRI 5750/6797. SDR SUBMITTED IN ERROR- ADMINISTRATOR. 2 L 7 2 4F RT A35EU 2007062700034 20070627 00034 EU 2007 6 27 07FDEA01895 1 20070521 A 5100 NONE AIRBUS 310 A310222 3930315 EU NONE NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON RT WING, L/E OF SLAT 1 WS270-339 RIB 5-6. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR D ETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. INSPECTION OF FILLER WAS PERFORMED IN ACCORDAN CE WITH SRM 57-40-00. REPAIRS IS COVERED BY WRI 5750/4864. REQUIRES INSPECTION OF FILLER AT NEXT C-CHECK. RE-INSPECTI ON TRACKED UNDER WRI 5750/6797. 2 L 7 2 4F RT A35EU 2007062700036 20070627 00036 EU 2007 6 27 07FDEA01898 1 20070521 A 5100 NONE AIRBUS 310 A310222 3930315 EU NONE NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON RT UPPER WING SURFACE T/E OF INBOARD FLAP WS 67-139 RIB2-3. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR CONFORMS TO EXISTING FEDEX EA 6-5750-81811. SDR SUBMITTED IN ERROR- ADMINISTRATOR. 2 L 7 2 4F RT A35EU 2007062700038 20070627 00038 EU 2007 6 27 07FDEA02189 1 20070619 A 5315 A53778801208 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 726FD 575 OLD CORROSION REPAIR ON TOP CAP BEAM C38.2 LT, THIS SPLICE REPAIR IN FWD CARGO COMPARTMENT IS NOT REPAIRED IAW OLD DOCUM ENTATION OR ALLOWABLE SRM REFERENCE. TOP CAP BEAM WAS REPAIRED FOLLOWING PRINCIPLE OF SRM 53-10-15 / FIG 207. 2 L 7 2 4F RT A35EU 2007062700045 20070627 00045 NM 2007 6 27 07FDEA02220 1 20070620 A 5720 STIFFENER DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 575FE 48500 LEFT WING FIXED LEADING EDGE CAVITY, AT XOS = 570, STIFFENER FOUND CRACKED. [07-06-07] REPAIRED AS PER FEDEX EA 1-571 0-111129, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062700046 20070627 00046 NM 2007 6 27 07FDEA02221 1 20070620 A 5313 BAC1498131 STRINGER BOEING 727 727233 138408A NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 286FE 22623 FOUND ON AGING A/C INSP EXISTING REPAIR AT STR S-27R FROM BS 610 TO BS 630 DOES NOT CONFORM TO CURRENT SRM 53-10-3 FIG 1 . REMOVED OLD REPAIR AND INSTALLED NEW REPAIR ON STR 27R, BS 610 TO BS 630, REF SRM 53-10-3 PG 3. INSTALLED STRINGER SPLICE REPAIR HAT CHANNEL, REF SRM 53-10-3 PG 3. 2 L 7 3 4F RT A3WE 2007062700047 20070627 00047 NM 2007 6 27 07FDEA02222 1 20070620 A 5315 651759393 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD ENTRY FLOOR SUPPORT UPPER FLANGE CRACKED BS 310, LBL32. REMOVED AND INSTALLED NEW FLOOR SUPPORT ANGLE IAW SRM 53-3 0-2. 2 L 7 3 4F RT A3WE 2007062700053 20070627 00053 NM 2007 6 27 AWXA200700751 1 20070527 A 5754 114N407635 SKIN BOEING 757 757225 1384959 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 MCN - MAJOR REPAIR - LEFT WING NR 2 SLAT INTERNAL COVE SKIN CRACKED, SS 655 - SS 677.50. REPLACED LEFT WING NR 2 SLAT I NTERNAL COVE SKIN, SS 655 - SS 677.50 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007062700054 20070627 00054 NM 2007 6 27 AWXA200700752 1 20070527 A 5754 114N407731 SKIN BOEING 757 757225 1384959 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 MCN - MAJOR REPAIR - LEFT WING NR 3 SLAT INTERNAL COVE SKIN CRACKED, SS 438.1 - SS 471.3. REPLACED LEFT WING NR 3 SLAT INTERNAL COVE SKIN, SS 438.1 - SS 471.3 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007062700062 20070627 00062 NM 2007 6 27 HALA0700261 1 20070619 A 2720 UNKNOWN BOEING 767 76733A 1385209 NM RUDDER UNKNOWN A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 580HA 28140 ETOPS SIGNIFICANT SYSTEM, RUDDER RATIO EICAS OVERHEAD PANEL ILLUM. RUDDER RATIO SYS CHECKS GOOD PER FIM 27 21 00 FIG 10 4 MSG CLEARED DID NOT RETURN. 2 L 7 2 4F RT A1NM 2007062700063 20070627 00063 EU 2007 6 27 F3LA200700132 1 20070613 A 5321 FLOORBOARD AIRBUS A319 A319112 3930323 EU CABIN PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 907FR 5061 1743 DURING C4/S1 CHECK, INSPECTION REPORTED PUNCTURE IN LT CORNER AREA OF FLOORBOARD 231MF. REPAIRED SMALL PUNCTURE TO THE TOP SKIN, FWD LT CORNER SURFACE OF FLOORBOARD PANEL 231MF IAW A319 SRM 53-02-00, PARA 8A, FIG 201 AND 202. 2 L 7 2 4F RT A28NM 2007062700064 20070627 00064 NM 2007 6 27 DHL2007742010 1 20070619 A 5320 FLOOR SUPPORT BOEING 727 727225 1384077 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 A CHECK REF N/R 138248 DISCREPANCY, CRACKED INDICATION ON LT AIRSTAIR AREA UPPER FLOOR SUPPORT INSIDE TORQUE BOW WEB BS 1263. STOPPED DRILLED CRACK TERMINATED CRACK PER B727 SRM 51-10-1. NDT CONFIRMED. FABRICATED REPAIR PART 7075-T6, .063 PO NR 9005314 11 BY 4 IAW B727 SRM 53-10-2 FIG 6 AND 51-40-3 FIG 1. TREATED AND PRIMED REPAIR PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR PART IAW B727 SRM 51-40-3 FIG1. 2 L 7 3 4F A3WE 2007062700067 20070627 00067 NM 2007 6 27 DHL2007742512 1 20070620 A 5320 SPLICE PLATE BOEING 727 727225 1384077 NM BS 560-580 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 WHILE AT FLIGHTSTAR AIRCRAFT SERVICES FOR AN "A"CHECK REF N/R 138282,138287,138292. MCD LWR SILL BEAM BS 560 TO BS580 S PLICE PLATE CRACKED AT SLOT RADIUS. REMOVED LOCK FITTINGS AND SPLICE PLATES AT BS 560 AND BS 580. FABRICATED NEW SPLIC E PLATES AT BS 560 AT BS 580. FABRICATED NEW SPLICE PLATES MAT 2024-T3 .125 PO NR 645747, 16" BY 7" 2EACH IAW AEI DWG N R 727-1-042 REVE TREATED AND PRIMED PARTS IAW B727 SRM51-10-2. INSTALLED 2 SPLICE PLATES BS 560 AND BS 580 IAW B727 SRM 51-30-2 FIG 4 AND FIG 15 AND AEI DWG 727-3-004. 2 L 7 3 4F A3WE 2007062700073 20070627 00073 NM 2007 6 27 QXEA200700979 1 20070609 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - SEAT TRACK NR 16 AT STATION 715 HAS NICKS. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007062700080 20070627 00080 NM 2007 6 27 QXEA200700990 1 20070610 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 370 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - SEAT TRACK NR 19 HAS MINOR PITTING CORROSION AT STATION 370. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007062700082 20070627 00082 NM 2007 6 27 QXEA200700988 1 20070610 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 291 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - SEAT TRACK NR 19 HAS MINOR PITTING CORROSION AT STATION 291. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007062700085 20070627 00085 NM 2007 6 27 QXEA200700986 1 20070610 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 130 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - SEAT TRACK NR 18 HAS MINOR PITTING CORROSION AT STATION 130. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007062700087 20070627 00087 NM 2007 6 27 QXEA200700985 1 20070609 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 373 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - NR 2 SEAT TRACK HAS MINOR CORROSION AT STATION 373. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007062700109 20070627 00109 NM 2007 6 27 07FDEA02230 1 20070620 A 5720 ARB2932505 STIFFENER DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 575FE 48500 LT WING FIXED LEADING EDGE CAVITY AT XOS = 665, STIFFENER FOUND WITH CRACK. [07-09-07] COMPLIED WITH FEDEX E.A. 1-5710 -111130. CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062700110 20070627 00110 NM 2007 6 27 07FDEA02231 1 20070620 A 5711 ARB74132 SPAR CAP DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 575FE 48500 RT WING REAR SPAR UPPER CAP FOUND WITH CORROSION AT XORS 1043 - 1045. [07-09-07] COMPLIED WITH FEDEX E.A. 1-5710-11113 2. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062700113 20070627 00113 WP 2007 6 27 07FDEA02234 1 20070621 A 5330 SKIN DOUG DC10 DC1010 3022110 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 1 CRACK LONG 1" ON EXT SKIN LOWER AT STA 485 RT SIDE DOOR FWD W/W REPAIRED IAW SRM 53-50-00 FIG 25 VOL 1. 2 L 7 3 4F A22WE 2007062700114 20070627 00114 NM 2007 6 27 07FDEA02235 1 20070621 A 5315 69436761 FLOORBEAM BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD PIT FLOOR SUPPORT STIFFENER STA 580, RBL 9, IS CRACKED REMOVED AND REPLACED STIFFENER AT STA 580 RBL 9, IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007062700124 20070627 00124 NM 2007 6 27 07FDEA02245 1 20070621 A 5322 65561241 SHEAR TIE BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT PIT SHEAR TIE CORRODED STA 950F STR 25L-29L. REMOVED SHEAR TIE, REMOVED CORROSION ON SIDE OF FRAME. CUT SHEAR TIE FROM FRAME. FABRICATED SHEAR TIE REPAIR FROM 7075-0 .071" SENT TO HEAT TREAT ON SNRM NR N00976 FORM 8130 TRACKING NR 20 07-05-157 TO T-6. DRILLED AND INSTALLED SHEAR TIE, REPAIR REF SRM 53-10-4 FIG 15, SRM 51-30-02, SRM 51-10-1 AND SRM 53- 10-4 . 2 L 7 3 4F RT A3WE 2007062700126 20070627 00126 SO 2007 6 27 CHQA200700029 1 20070620 A 2750 FLAP SYSTEM EMB 145 EMB145LR 3260212 SO TE FLAPS MALFUNCTIONED A CHQA O OTHER J WARNING INDICATION DE DESCENT 1 GL 11 276SK 145348 FLIGHT 3438 - ATL-CLE - ON DESCENT WHEN FLAPS SELECTED TO 9, EICAS MESSAGES SPS ADV AND FLAP FAIL APPEARED. PERFORMED T HE QRH AND DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. MAINTENANCE RESET FLAPS AND CYCLED THROUGH, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007062700133 20070627 00133 NM 2007 6 27 NWAA072196732 1 20070619 A 2611 CIRCUIT CARD BOEING 747 747251B 1384892 NM FIRE DETECTION BURNED A NWAA B EMER. DESCENT A FLAME/FIRE CR CRUISE 1 GL 01 632NW 23112 DURING CRUISE, HAD INDICATION OF FAULT ON NR 4 ENGINE FAULT GAUGE. NEEDLE BOUNCING BETWEEN 6 AND 8 WITH FLASHING FAULT LIGHT/FIRE DETECTION LIGHT. FAULT LIGHT CAME ON STEADY. THEN PERFORMED COM 2.26.32. THEN SMELLED ODOR OF BURNING INSUL ATION AND/OR ELECTRICAL FLAMES. S/O OBSERVED ODOR/FLAMES WITHIN THE P-6 C/B PANEL UPPER PORTION BEHIND FIRE DETECTION C ONTROL PANEL. AT THAT POINT, PERFORMED ELECTRICAL FIRE OR SMOKE RED BORDERED CHECKLIST AND INITIATED EMERGENCY DESCENT, DECLARED EMERGENCY. ENGINE FIRE DETECTION 3A-4A C/B OPENED POPPED. CONTINUED COM 2.26.6. FLAMES STILL IN VIEW AND INCR EASING IN INTENSITY. AT THE POINT OF TRIPPING GB’S FOR THE NR 1 AND NR 2 GENERATORS, THE FLAMES DIMINISHED AND EVENTUAL 2 L 7 4 4F A20WE 2007062700145 20070627 00145 EA 2007 6 27 SWIA200718356 1 20070511 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 766SK 10232 PASSENGER DOOR AFT WEB IS CRACKED UNDER THE HANDRAIL STOW BRACKET, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS AND DO UBLER IAW CRJ700 REO 670-52-11-104 REV B. 2 L 7 2 4F RT A21EA 2007062700146 20070627 00146 EA 2007 6 27 SWIA200718357 1 20070511 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 766SK 10232 PASSENGER DOOR FORWARD WEB IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED DOUBLER REPAIR ANGLE IAW CRJ700 SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007062700155 20070627 00155 EA 2007 6 27 SWIA200718366 1 20070620 A 2910 O-RING CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 460SW 7803 ON TAXI OUT IN SLC, LOST ALL HYDRAULIC FLUID IN SYSTEM NR 2. RETURNED TO GATE. REPLACED O-RING ON PRESSURE SIDE OF MLG EMERGENCY EXTENSION VALVE. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2007062700156 20070627 00156 EA 2007 6 27 SWIA200718367 1 20070421 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 926SW 7687 PAX DOOR FORWARD WEB IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS PER REO 601R-52-11-702 REV A. 2 L 7 2 4F RT A21EA 2007062700158 20070627 00158 EA 2007 6 27 SWIA200718369 1 20070421 A 5320 THRESHOLD CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 926SW 7687 SERVICE DOOR THRESHOLD PLATE HAS EVIDENCE OF CORROSION, DISCOVERED AT C-CHECK. REPLACED SERVICE DOOR THRESHOLD PLATE WI TH A NEW PLATE PER CRJ 200 AMM 53-20-31-00-801. 2 L 7 2 4F RT A21EA 2007062700159 20070627 00159 SO 2007 6 27 LR7A07054 1 20070612 A 5330 SKIN LKHEED 382 382G 526414U SO FS 848, WL 232 PUNCTURED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 335 4606 DURING PREFLIGHT INSPECTION CREW NOTED, RT AFT FUSELAGE SKIN SLIGHTLY DENTED WITH A SMALL HOLE AT FS 848, WL232, RBL83. REPAIRED SKIN IAW SMP583 51-140. 2 H 7 4 4T A1SO 2007062700164 20070627 00164 NM 2007 6 27 UIEA200700234 1 20070604 A 2750 65B1565110 PUSHROD BOEING 747 7472D7B 1384803 NM TE FLAPS BROKEN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 ON W/A, FOUND RT INBOARD TRAILING EDGE FLAP PUSH-ROD ASSY BROKEN. REMOVED AND REPLACED INBOARD TRAILING EDGE FLAP PUSH- ROD ASSY IAW MM 27-51-39. SYSTEM OPERATIONS CHECKED OK. 2 L 7 4 4F RT A20WE 2007062700165 20070627 00165 NM 2007 6 27 UIEA200700235 1 20070601 A 3620 3206251 PRESSURE VALVE BOEING 747 7472D7B 1384803 NM ENGINE UNRESPONSIVE A UIEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 524MC 21784 NR 3 ENGINE ON CLIMB-OUT, ENGINE NACELLE FAULT LIGHT ON NR 3 ENGINE A LOOP READ 8.5- B LOOP READ 4.5. AS SOON AS THROTTL E PULLED BACK THE B LOOP TEMP DROPPED DOWN TO 3.0. NR 3 THROTTLE PULLED TO IDLE TO GET A LOOP TO DROP DOWN TO 3.0. ON G ROUND AT IDLE NACELLE TEMPS READ 2.8, ENGINE BLOW OUT DOORS OPEN ON GROUND. NR 3 ENGINE PRESS CHECK FOR AIR LEAKS OK. REPLACED PRESSURE RELIEF VALVE AS PER BOEING MM 36-11-03. REPLACED PRESSURE REGULATING VALVE AS PER BOEING MM 36-11-19. ENGINE RUN AT HIGH POWER TO CHECK VALVES, RUN OK. 2 L 7 4 4F RT A20WE 2007062700166 20070627 00166 2007 6 27 UIEA200700236 2 20070602 A 7532 73836222 BLEED VALVE BOEING 747 7472D7B 1384803 NM NR 4 ENGINE UNRESPONSIVE A UIEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 523MC 21782 WHILE TAXIING AFTER ENGINE START NR 4 ENGINE BLEED VALVE, VALVE CLOSED LIGHT ON, FOUND NO DUCT PRESSURE, WHEN ISOLATED F OR TROUBLE SHOOTING. PER MEL 36-5-1 TRANSFERRED TO FROM T0219M, DMI M07-100 ISSUED BY MCC HECTOR, ORANGE PLACARD INSTAL LED. 2 L 7 4 4F RT A20WE 2007062700168 20070627 00168 NM 2007 6 27 UIEA200700238 1 20070610 A 5322 SHEAR TIE BOEING 747 747243B 1384830 NM BS 840 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 BS 840R FRAME TO TENSION TIE CONNECTION FOUND NR 14 AND 19 HOLE CRACKED. BS 840 FRAME TO TENSION TIE CONNECTION REPAIRE D AS PER BOEING MESSAGE 1-340418286-2 AND FAA FORM 8100-9. 2 L 7 4 4F A20WE 2007062700171 20070627 00171 NM 2007 6 27 UIEA200700241 1 20070610 A 5322 SHEAR TIE BOEING 747 747243B 1384830 NM BS 900 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 BS 900R FRAME TO TENSION TIE CONNECTION FOUND CRACKED HOLE NR 9 AT FORWARD CHANNEL. BS 900R FRAME TO TENSION TIE CONNEC TION REPAIRED AS PER BOEING MESSAGE 1-343193942-4 AND FAA FORM 8100-9. 2 L 7 4 4F A20WE 2007062700172 20070627 00172 NM 2007 6 27 UIEA200700242 1 20070610 A 5322 SHEAR TIE BOEING 747 747243B 1384830 NM BS 920 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 BS 920R FRAME TO TENSION TIE CONNECTION FOUND HOLE NR 4 CRACKED. BS 920R FRAME TO TENSION TIE CONNECTION REPAIRED AS PE R BOEING MESSAGE 1-340126164-4 AND 8100-9. 2 L 7 4 4F A20WE 2007062700173 20070627 00173 EU 2007 6 27 COEA0706903 1 20070109 A 5320 S53575104202 SILL AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 903FX 179 DURING HEAVY CHECK MAINTENANCE, FOUND CORROSION ON LT AND RT UPPER SURFACES OF LOWER SIDEBOX AT STRINGER 14 CREASEBEAM B ETWEEN FRAME 26 AND 27. REMOVED CORROSION AND REPAIRED IAW SRI DO/TS-709/07-8327 AND DO/TS-709/07-8327 WITH REFERENCE T O SRAS DOTS-640/07, 3981 ISSUE A FOR FINAL APPROVAL OF REPAIR. TWO YEAR REINSPECTION (DVI) REQUIRED BY ISSUED SRAS. (M ) 2 H 7 2 4T RT A53EU 2007062700175 20070627 00175 WP 2007 6 27 07FDEA02263 1 20070622 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CLG WHEEL WELL CAVITY CORROSION ON FUSELAGE SKIN BETWEEN LONGERON 51L AND 52 STA 1350 TO 1370. CLEANED AREA IAW DC/MD 10 SRM51-21-01 PARA.22 VOL. II. NO CORROSION NOTED. MECH 7951 QC281 2 L 7 3 4F RT A22WE 2007062800152 20070628 00152 NM 2007 6 28 2007UALA02079 1 20070617 A 4900 APU BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SMOKE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 219UA 30551 APU SMOKING FROM TAIL PIPE. [07-17-07] REPLACED APU PER MM 49-11- 01. SUSPECT APU INTERNAL OIL LINE LEAK CAUSED SMOK E. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007062800153 20070628 00153 NM 2007 6 28 2007UALA02080 1 20070616 A 3510 OXYGEN SYSTEM BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 797UA 26924 CREW OXYGEN 1200 PSI. [07-17-07] SERVICED CREW OXYGEN. NO LEAKS DETECTED. OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007062800154 20070628 00154 NM 2007 6 28 2007UALA02081 1 20070616 A 3350 20131A POWER SUPPLY BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHTS BY SEATS 35-44 HJ TURN ON UNCOMMANDED. *S/D* REPLACED POWER SUPPLY AT DOOR 3R. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062800155 20070628 00155 NM 2007 6 28 2007UALA02082 1 20070617 A 3350 362624 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE SEAT 3A INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 SEAT 3A EMERGENCY LIGHT STRIP INOPERATIVE. *S/D* REPLACED LIGHT ASSY AND OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062800156 20070628 00156 NM 2007 6 28 2007UALA02083 1 20070616 A 3500 BOTTLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE OXYGEN READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 107UA 26900 CREW REPORTS WALKAROUND, O2 BOTTLE LOW AT 4L. [07-27-07] REPLACED O2 BOTTLE AT DOOR 4L. SUSPECT VALVE LEAKAGE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062800157 20070628 00157 2007 6 28 2007UALA02084 4 20070615 A 2565 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE DOOR 3L FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 175UA 24382 DOOR 3L SLIDE PRESSURE GAUGE IS BELOW GREEN BAND. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062800158 20070628 00158 NM 2007 6 28 2007UALA02085 1 20070616 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 5J AFT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY EEL LIGHT INOP AT SEAT 5J AFT LIGHT ASSY. REPLACED LIGHT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062800159 20070628 00159 NM 2007 6 28 2007UALA02086 1 20070616 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY EXIT LIGHT INOP AT DOOR 2L CEILING ENTRY LIGHT. RELAMPED, OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062800160 20070628 00160 NM 2007 6 28 2007UALA02087 1 20070616 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY EEL LIGHT INOP AT SEAT 44 HJK. *S/D* SECURED CONNECTOR, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062800161 20070628 00161 NM 2007 6 28 2007UALA02088 1 20070618 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 DOOR 5R CROSS AISLE & SEAT 50 HJK EMERGENCY LIGHTS ARE INOP. *S/D* SECURED CONNECTION. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062800162 20070628 00162 NM 2007 6 28 2007UALA02089 1 20070618 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 5E AFT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 SEAT 5E AFT EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062800163 20070628 00163 NM 2007 6 28 2007UALA02090 1 20070617 A 3397 WIRE HARNESS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY LIGHT INOPERATIVE SEAT 49 HJK, SEAT WIRE HARNESS. [07-13-07] REPLACED SEAT WIRE HARNESS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062600184 20070626 00184 NM 2007 6 26 SWAA073035 1 20070618 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 14Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP CRACKED BETWEEN ROW 3 ABC AND ROW 10 ABC. REMOVED AND RE PLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007062600189 20070626 00189 NM 2007 6 26 2007UALA02008 1 20070614 A 2130 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN PRESSURE UNKNOWN A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 339UA 24243 RIGHT BLEED TRIPPED 3 TIMES IN A 10 MINUTE PERIOD AT FL370. DESCENDED TO FL310 TO STABILIZE CABIN PRESSURE. [07-06-07] ACCOMPLISHED BLEED CHECK. NO DEFECTS NOTED. BLEED RESET JUST BY PUSHING THE RESET BUTTON. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062600202 20070626 00202 NM 2007 6 26 2007UALA02027 1 20070615 A 5240 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 567UA 26673 NR 2 LT MED FWD DOOR FRAME (ON DOOR) UPPER HINGE CUTOUT SKIN IS CRACKED AT CUTOUT LWR RADIUS. [08-07-07] MAJOR REPAIR ACCOMPLISHED PER ENGINEERING SPECIFICATION. CRACK ROUTED OUT AND TREATED BARE EDGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062600203 20070626 00203 EU 2007 6 26 2007UALA02028 1 20070615 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 435UA 613 LEFT FUSE SKIN IS DENTED AT FRAME 7, 6 INCHES ABOVE THE STRIPES. DENT IS OUT OF LIMITS FOR DISTANCE FROM FRAME AND IS L OCATED WITHIN THE RVSM AREA. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062600205 20070626 00205 NM 2007 6 26 2007UALA02030 1 20070615 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 EXTERNAL FUSELAGE SKIN IS GOUGED AT BS 809 STR 18R. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. INSTALLED DOUBLER/TRIP LER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062600208 20070626 00208 NM 2007 6 26 2007UALA02032 1 20070615 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1580 S23R DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 MAIN FRAME, STA 1580 AT STR 23R, FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED -J- ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062600209 20070626 00209 NM 2007 6 26 2007UALA02033 1 20070615 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1420 S25-26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 MAIN FRAME, STA 1420 BETWEEN STR 25L-26L, FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062600210 20070626 00210 NM 2007 6 26 2007UALA02034 1 20070615 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1500 S25-26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 MAIN FRAME, STA 1500 BETWEEN STR 25L-26L, FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED ANGLE REPAIR AND NEW SP LICE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062700023 20070627 00023 NM 2007 6 27 QXEA200701008 1 20070619 A 6120 AUTOFEATHER SYS DHAV DHC8 DHC8202 2809007 NM MALFUNCTIONED A QXEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 09 349PH 486 YVR FLIGHT NR 2025 - AUTOFEATHER FAILED TO ARM ON TAKEOFF ROLL WITH POWER SET ABORTED TAKEOFF, AUTOFEATHER SYSTEM INOP. MAINTENANCE PERFORMED AUTO FEATHER SYSTEM ADJUSTMENT AND TEST IAW DHC-8-200 ENGINE RIGGING MANUAL. RT ER 10, PARAGRAPH 5-1-A 1 38. PERFORMED FUNCTIONAL TEST OF THE AUTOFEATHER SYSTEM OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT R ETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007062700027 20070627 00027 SO 2007 6 27 SIMA200717103 1 20070619 A 3260 852701 PROXIMITY SWITCH EMB 135 EMB135LR 3260305 SO ZONE 700 FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 21 734EK 14648 145371 AIR/GROUND FAIL MESSAGE FOLLOWED BY E 1/2 REV DISAGREE MESSAGE, DIVERTED TO JFK. REMOVED AND REPLACED NOSE LANDING GEAR WEIGHT ON WHEEL PROXIMITY SWITCH IAW EMB AMM 32-36-02 AND OPERATIONAL CHECK PERFORMED IAW AMM 32-60-00 WITH NO DEFECTS. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007062700035 20070627 00035 EU 2007 6 27 07FDEA01896 1 20070521 A 5100 NONE AIRBUS 310 A310222 3930315 EU NONE NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 452FE 313 PREVIOUS REPAIR FOUND LOCATED ON RT WING, L/E OF SLAT 3 WS 1246-1311 RIB 20-21. REPAIR REQUIRES EVALUATION FOR MAJOR/MI NOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 57-40-00 FIG 102 - SHEET 7. SDR SUBMITTED IN ERROR- ADMINISTRATOR. 2 L 7 2 4F RT A35EU 2007062700041 20070627 00041 EU 2007 6 27 07FDEA02216 1 20070620 A 5730 A57241132202 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 CHAFING MARK FOUND ON LEADING EDGE NOSE SKIN, RT WING, BETWEEN TRACK 3 AND WOFX-69.00. REPAIR PERFORMED BY REWORK OF SK IN AND IS APPROVED BY EA 6-5741-103287 AND RAS/BAE/1003389/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007062700043 20070627 00043 NM 2007 6 27 07FDEA02218 1 20070620 A 5730 ARB2886503 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 575FE 48500 LEFT WING FIXED LEADING EDGE, AT 3 SLAT ANTI-ICE TELESCOPE DUCT CUT-OUT, FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FI GURE 43 VOLUME I AND FEDEX E.A. 1-5710-112343, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007062700048 20070627 00048 NM 2007 6 27 07FDEA02224 1 20070620 A 5740 ATTACH BRACKET BOEING 727 727233 138408A NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 NR 5 FLAP TRACK FAIRING INBD MIDDLE ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET REF, FED EX J/C 76C07500 A ND BOEING DWG 65-21795 AND SRM 51-30-2 PG 4&5. 2 L 7 3 4F RT A3WE 2007062700057 20070627 00057 2007 6 27 QXEA20071012 4 20070617 A 3140 8221310104 DCU CNDAIR CL600 CL6002C10 1390015 EA NR 1 INOPERATIVE A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 601QX 5044 1163 10009 DEN - FLIGHT 4207 - RECEIVED A DCU 1 INOP MESSAGE AND ALSO A AURAL WARNING. RETURNED TO THE GATE. MAINTENANCE REPLACED THE NR 1 DCU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007062700065 20070627 00065 EU 2007 6 27 F3LA200700133 1 20070614 A 5321 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CABIN DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 907FR 5061 1743 DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 221PF DELAMINATED NEAR THE LAV MOUNTS AND A PUNCTURE NEAR THE LAV DO OR AREA. REPAIRED DAMAGE TO THE TOP SKIN PANEL OF FLOOR PANEL 221PF IAW A319 SRM 53-02-00, PARA 8A, FIG 201 AND 202. D ELAMINATION WAS DETERMINED TO BE A DENSITY CHANGE IN THE PANEL DUE TO THE INSERTS INTEGRATED INTO THE SANDWICH STRUCTURE . 2 L 7 2 4F RT A28NM 2007062700068 20070627 00068 NE 2007 6 27 IXXA070032O 2 20070620 A 7261 9026M70G01 ENGINE DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C1 13802 NE LEAKING A IXXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 11 820BX 39515 7521 46065 692527 DURING CRUISE FROM KRFD TO KLRD, THE CREW OBSERVED THE NUMBER THREE ENGINE OIL QUANTITY DECREASING. THE ENGINE WAS SHUT DOWN FOR LOSS OF OIL QUANTITY. THE CREW LANDED AT KLRD WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THE LEAK WAS FROM THE DRAIN MAST. MAINTENANCE ISOLATED THE LEAK TO THE TRANSFER GEARBOX MANUAL HAND CRANKING DRIVE PAD. MAINTENANCE CAPPED THE DRAIN LINE PER UAL DC-8 M/M 71-70-02. MAINTENANCE RAN THE ENGINE AFTER CAPPING THE LINE AT IDL E AND HIGH POWER SETTINGS, NO LEAK NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2007062700070 20070627 00070 NM 2007 6 27 QXEA200700978 1 20070605 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - DENT ON LEFT FUSELAGE ABOVE DOUBLER REPAIR AT STATION 308 BETWEEN STRINGERS 3L AND 4L. REPAIRED IAW RD8/4-53-6 66. 2 H 7 2 4T RT A13NM 2007062700074 20070627 00074 NM 2007 6 27 QXEA200700980 1 20070609 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - SEAT TRACK NR 9 AT STATION 715, 722 TO 747 HAS NICKS AND SCRATCHES. REPAIRED IAW RD8/4-53-844. 2 H 7 2 4T RT A13NM 2007062700076 20070627 00076 NM 2007 6 27 QXEA200700984 1 20070609 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 281 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - NR 2 SEAT TRACK HAS MINOR PITTING CORROSION AT STATION 281. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007062700088 20070627 00088 WP 2007 6 27 AALA20071046 1 20070607 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN OUT OF POSITION A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 592AA 53255 DFW - EMERGENCY PATH LIGHTS ON SEATS 28D AND 29D NOT IN CORRECT POSITION. REPOSITIONED EMERGENCY PATH LIGHTS FOR SEATS 28D AND 29D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007062700104 20070627 00104 NM 2007 6 27 QXEA200700997 1 20070612 A 5312 PRESSURE PANEL BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - FUSELAGE NOSE PRESSURE PANEL 121AL GOUGED IN INTERIOR FRAME AT LOWER FORWARD CORNER. REPAIRED IAW RD8/4-53-193 9. 2 H 7 2 4T RT A13NM 2007062700107 20070627 00107 NM 2007 6 27 07FDEA02228 1 20070620 A 5753 SKIN BOEING 727 727233 138408A NM TE FLAP MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 286FE 22623 ON AGING A/C INSPECTION, FOUND EXISTING REPAIR LOCATED AT LT WING I/B AFT FLAP UPPER SURFACE 30" FROM O/B END, 9" FROM T /E DID NOT CONFORM TO SRM 51-40-20. REMOVED PREVIOUS REPAIR AND BONDED ON REPAIR REF SRM 51-40-20 PARAGRAPHS, 7, 14, 18 , 20, 21, AND 22. TAP TEST GOOD. PRIMED AND PAINTED REF. 2 L 7 3 4F RT A3WE 2007062700118 20070627 00118 NM 2007 6 27 07FDEA02239 1 20070621 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 MAIN CABIN, STRINGER CLIP GOUGED IN RADIUS AT STA 680 AT STR 7L REPLACED DAMAGED STRINGER CLIP AT BS 680 STR 7L REF SRM 51-30-2 PG 1&2. 2 L 7 3 4F RT A3WE 2007062700119 20070627 00119 NM 2007 6 27 07FDEA02240 1 20070621 A 5347 6586245 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT UPPER MAIN DECK, SEAT TRACK HAS CORROSION, ON UPPER INBD FLANGE, STA 1070 2 LBL 45. REMOVED CORROSION ORIG THICKNES S .530. REMOVED .036, REMAINING .494" MATERIAL. REMOVED IS WITHIN LIMITS. TREATED AND APPLIED PRIMER REF SRM 53-10-1 PG 13-17. 2 L 7 3 4F RT A3WE 2007062700120 20070627 00120 NM 2007 6 27 07FDEA02241 1 20070621 A 5347 BAC1520792 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT UPPER MAIN DECK, CORROSION ON SEAT TRACK LWR O/B UPPER SURFACE STA 950 LBL 26K. REMOVED CORROSION REF SRM 51-10-1, VERIFIED REMAINING MATERIAL WITHIN LIMITS REF SRM 53-10-1 FIG 3. TREATED AND PRIMED REF MM 51-20-002-7. 2 L 7 3 4F RT A3WE 2007062700121 20070627 00121 NM 2007 6 27 07FDEA02242 1 20070621 A 5320 69445593 FLOOR SUPPORT BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT PIT STR CLIP/FLOOR SUPPORT ANGLE CORRODED AT STA 990 STR 29L REMOVED CORRODED STIFFENER REF SRM 51-30-2. REMOVED CO RROSION FROM STIFFENER REF SRM 51-10-01 PG 14-16. FABED FILLER FROM 7075-T6- .071. TREATED AND PRIMED STIFFENER AND FILLLER REF MM 51-20-021-7 AND MM 51-20-031-7 AND INSTALLED STIFFENER AND FILLER REF SRM 51-30-02. 2 L 7 3 4F RT A3WE 2007062700130 20070627 00130 EU 2007 6 27 AWXA200700755 1 20070616 A 5321 D5367002200000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU ZONE 200 DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 PHX - AFT PASSENGER COMPARTMENT FLOORBOARD 251RF, BS 2670 - BS 2936, -Z240, +Y254 TO -Y254 IS DELAMINATED. REPLACED AFT PASSENGER COMPARTMENT FLOORBOARD 251RF, BS 2670 - BS 2936, -Z240, +Y254 TO -Y254 IAW AWA TASK CARD R1C25306. 2 L 7 2 4F RT A28NM 2007062700131 20070627 00131 NM 2007 6 27 AWXA200700756 1 20070422 A 5311 654654965 FRAME BOEING 737 73733A 1384673 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - CORROSION ON FRAME FOOT, BS 767, S26R - S27R, WL 147. REPAIRED FRAME FOOT, BS 767, S26R - S27R, WL 147 IAW AWA ER 03-5311-07170-SS2. 2 L 7 2 4F RT A16WE 2007062700140 20070627 00140 EA 2007 6 27 SWIA200718351 1 20070617 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 947SW 7786 FORWARD OVERHEAD EMERGENCY LIGHT IS INOP. REPLACED LAMP. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007062700147 20070627 00147 EA 2007 6 27 SWIA200718358 1 20070523 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 774SK 10240 PAX DOOR WEB CRACKED AT AFT SIDE OF NR 2 STEP, DISCOVERED AT C-CHECK. INSTALLED EXTERNAL DOUBLER AND REPAIR ANGLES IAW CRJ 700 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007062700151 20070627 00151 EA 2007 6 27 SWIA200718362 1 20070529 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 778SK 10242 PAX DOOR FORWARD WEB IS CRACKED AT SUPPORT BRACKET, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLES AND DOUBLER AS PER R EO 670-52-11-104. 2 L 7 2 4F RT A21EA 2007062700154 20070627 00154 EA 2007 6 27 SWIA200718365 1 20070421 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 926SW 7687 PAX DOOR HAS CRACK AT LOWER AFT CORNER, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS AT LOWER AFT AND LOWER FORWARD PA X DOOR UNDER TOP STEP PER CRJ200 REO 601R 52-11-279 REV NC. 2 L 7 2 4F RT A21EA 2007062700157 20070627 00157 EA 2007 6 27 SWIA200718368 1 20070421 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 926SW 7687 PAX DOOR AFT WEB IS CRACKED AT HANDRAIL SUPPORT BRACKET, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 REO 6 01R 52-11-702 REV 'A'. 2 L 7 2 4F RT A21EA 2007062700161 20070627 00161 2007 6 27 VNAA0706004 2 20070607 A 7261 CARBON SEAL CNDAIR CL600 CL6002B19 1900309 EA ENGINE LEAKING A VNAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 05 215PS 7880 CREW REPORTED ON CLIMB-OUT A RIGHT ENGINE LOW OIL PRESSURE WARNING MESSAGE. CREW DIVERTED TO DAY AND LANDED WITHOUT INC IDENT. MAINTENANCE REMOVED AND REPLACED THE IDG AND STARTER CARBON SEAL IAW THE GE MANUAL 72-00-00. MAINTENANCE PERFOR MED LEAK CHECKS AND OPS CHECKED GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2007062700163 20070627 00163 EU 2007 6 27 COEA0705903 1 20070109 A 5311 S53372410200 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE DAMAGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 903FX 179 DURING HEAVY CHECK MAINTENANCE FOUND DENT AND CRACK IN CARGO COMPARTMENT FRAME 23 BETWEEN STRINGERS 19-20 RT. FABRICATE D REPAIR DOUBLER AND INSTALLED TO FRAME 23 BETWEEN STRINGERS 19-20 RIGHT SIDE IAW ATR42 SRM. (M) 2 H 7 2 4T RT A53EU 2007062800008 20070628 00008 NM 2007 6 28 2007UALA02056 1 20070618 A 3260 SENSOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU MLG MALFUNCTIONED A UALA O OTHER N FALSE WARNING AP APPROACH 1 WP 29 349UA 24253 COULD NOT SILENCE GEAR WARNING HORN WITH FLAPS 10 AND IDLE POWER FOR 15 SECONDS. CLEANED SENSOR S845. ADJUSTED SENSOR TARGET GAP FOR NOSE GEAR DOWN SENSOR S845. CHECKED RIGHT MAIN GEAR SENSOR S73 AND TARGET. CHECKED LEFT MAIN GEAR SENSOR S71 AND TARGET. M989 CARD TEST PER MM 32-09-20-415 TEST GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007073000149 20070730 00149 NM 2007 7 30 AWXA200700880 1 20070629 A 5313 143N3110227 STRINGER BOEING 757 757225 1384959 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - NR 5950467, CRACKED STRINGER, BS 640, S16L. REPAIRED STRINGER, BS 640, S16L IAW B757- 200 SRM 53-00-03-2R1. 2 L 7 2 4F RT A2NM 2007062800009 20070628 00009 NM 2007 6 28 2007UALA02058 1 20070617 A 3040 CONTROLLER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE WINDOW HEAT INOPERATIVE A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 846UA 1600 LT WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN, ANTI-ICE. REPLACE CAPTS WINDOW HEAT CONTROLLER/COMPUTER. NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062800010 20070628 00010 NM 2007 6 28 2007UALA02059 1 20070615 A 3520 ACTUATOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE OXYGEN MASK DOOR FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 806UA 788 CABIN OXYGEN MASK DOOR AT SEAT ROW 13 LT, SEAT 18 RT & SEAT ROW 22 RT FAILED TO OPEN DURING MANUAL CHECK. REPLACED ALL ACTUATORS AT POSITIONS THAT FAILED TEST. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062800011 20070628 00011 NM 2007 6 28 2007UALA02060 1 20070615 A 3350 BR964421 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE SEAT 16C DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 838UA 1477 EMERGENCY LIGHT ON SEAT 16C BROKEN OFF. REPLACED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062800012 20070628 00012 EU 2007 6 28 2007UALA02061 1 20070616 A 3350 BR964421 LAMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 411UA 464 EMERGENCY LIGHTS AT SEATS 3B, 12C AND 16C HAVE INOPERATIVE LAMPS. RELAMPED, OPS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062800014 20070628 00014 EU 2007 6 28 2007UALA02063 1 20070616 A 3397 CIRCUIT BREAKER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 448UA 842 DURING 3 SERVICE CHECK, EMERGENCY LIGHT CHECK HAD EPSU BATT EMER R FAULT. RESET EMERGENCY LIGHT C/B`S, PERFORMED OPS CH ECK REF AMM 33-51-38, CHECKS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062800015 20070628 00015 NM 2007 6 28 2007UALA02064 1 20070617 A 4900 APU BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FIRE A UALA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 WP 29 919UA 25386 ON APU START, FLAMES REPORTED COMING OUT OF REAR OF AIRCRAFT. APU SHUT DOWN WITH FAULT LIGHT. [07-06-07] REFERENCE SE RVICE TIP 49-00-02 PG 200A. PROBABLE CAUSES ARE IF THE APU HAS BEEN SHUTDOWN FOR A TIME LESS THAN ONE HOUR OR IF THE PRE-START EXHAUST GAS TEMPERATURE (EGT) IS GREATER THAN 100 DEGREES F AND/OR RESIDUAL FUEL IN THE COMBUSTOR PRIOR TO S TARTING. THE BRIEF FLAME DOES NOT POSE ANY OPERATIONAL RISK TO THE AIRCRAFT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062800016 20070628 00016 NM 2007 6 28 2007UALA02065 1 20070615 A 2752 ACTUATOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 4 TE FLAPS FAULTY A UALA O OTHER N FALSE WARNING CL CLIMB 1 WP 29 372UA 24637 AFTER TAKEOFF, CREW NOTED THE FWD PANEL L/E FLAPS INTRANSIT LIGHT REMAINED ON ALONG WITH THE OVERHEAD PNL NR 4 L/E FLAP INTRANSIT LIGHT. FOUND NR 4 LEADING EDGE FLAP FLOATING AND ACTUATOR VERY WARM. REPLACED NR 4 ACTUATOR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062800017 20070628 00017 NM 2007 6 28 2007UALA02066 1 20070617 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY EXIT CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 EXTERIOR EMERGENCY EXIT LIGHT CORRODED AT FWD RT SERVICE DOOR. REPLACED LIGHT ASSY 2 L 7 2 4F 4 F RT A16WE E21EU 2007062800018 20070628 00018 NM 2007 6 28 2007UALA02067 1 20070617 A 5210 TORQUE TUBE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU PAX DOOR WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 FWD ENTRY DOOR FUSELAGE TORQUE TUBE HAS WEAR ON UPPER SPIGOT. INSTALLED SERVICEABLE TORQUE TUBE. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062800019 20070628 00019 NM 2007 6 28 2007UALA02068 1 20070616 A 2780 SLAT SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 2 SLOW A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 338UA 24242 NR 2 L/E SLAT SLOW TO EXTEND. LAGS NR 1 & 3 L/E SLATS IN EXTEND AND RETRACT. [07-06-07] FOUND FAULTY NR 2 ACTUATOR. REPLACED NR 2 ACTUATOR. FOUND WORN SEALS. REPLACED SEALS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062800020 20070628 00020 EU 2007 6 28 2007UALA02069 1 20070615 A 2420 IDG AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 INOPERATIVE A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 418UA 485 NR 1 IDG INOP, AND APU AUTO SHUT DOWN AT DEPARTURE. REPLACED FUEL/OIL HEAT EXCHANGER FOR IDG NR 1 AND ALSO REPLACED I DG NR 1 AS A PRECAUTION. NO APU HISTORY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062800021 20070628 00021 NM 2007 6 28 2007UALA02070 1 20070613 A 3250 COLLAR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NLG STEERING BINDING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 NOSE WHEEL STEERING BINDING DUPLICATED ISOLATED TO STEERING COLLAR: DISASSEMBLED STEERING COLLAR FOUND LITTLE TO NO GRE ASE AND A LARGE AMOUNT OF WATER PRESENT. INSPECTED PARTS NO DAMAGE NOTED, LUBED PARTS AND REASSEMBLED STEERING COLLAR R EF MM 32-51-61 PG 401. NO BINDING NOTED DURING STEERING TEST AND TAXI TEST. [07-24-07] REPLACED STERRING METERING V ALVE. VALVE PASSED ALL FUNCTIONAL TESTING. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062800022 20070628 00022 NM 2007 6 28 CALA0700311 1 20070618 A 5330 6545775594 SKIN BOEING 737 7373T0 1384582 NM BS 730 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12313 23364 INSPECTION FOUND A 1.25 INCH CRACK IN FUSELAGE SKIN AT STA 730, S24R. A REPAIR WAS INSTALLED IAW ECRA 5330-03690. 2 L 7 2 4F RT A16WE 2007062800023 20070628 00023 NM 2007 6 28 CALA0700312 1 20070619 A 5315 BAC1505100617 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 946 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70352 23590 INSPECTION FOUND MAIN CABIN FLOORBEAM HAD CORROSION EXTENDING UNDER FLOOR MOUNT AT STA 946, LBL 13. THE UPPER FLANGE I- BEAM WAS REMOVED AND REPLACED FROM RBL 35 TO LBL 35 IAW SRM 53-00-51, FIGURE 201. 2 L 7 2 4F RT A16WE 2007062800024 20070628 00024 NM 2007 6 28 CALA0700313 1 20070619 A 5311 65528747 FRAME BOEING 737 7373T0 1384582 NM BS 950 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12313 23364 INSPECTION FOUND A .75 INCH CRACK IN L-2 DOOR FORWARD STUB FRAME AT STA 950 AT UPPER HINGE. THE CRACKED AREA WAS REMOVE D AND A REPAIR ANGLE WAS INSTALLED IAW ECRA 5311-01332. 2 L 7 2 4F RT A16WE 2007062800025 20070628 00025 NM 2007 6 28 CALA0700314 1 20070619 A 5320 65558722 CLOSEOUT PANEL BOEING 737 7373T0 1384582 NM BS 950 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12313 23364 INSPECTION FOUND A .75 INCH CRACK IN CLOSEOUT PLATE JUST FORWARD OF L-2 DOOR CUTOUT AND BELOW DOOR ASSIST HANDLE ATTACH POINT, STA 950. THE CLOSEOUT PLATE WAS REMOVED AND REPLACED IAW ECRA 5311-01332. 2 L 7 2 4F RT A16WE 2007062800026 20070628 00026 NM 2007 6 28 KCSA071194 1 20070620 A 5730 SKIN BOEING 747 747123 1384873 NM CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 STA 990 ABOVE NR 2 RAM AIR INLET DUCT, LOWER SIDE OF CENTER WING TANK HAS AREA OF CORROSION AT LBL 82. 2 L 7 4 4F A20WE 2007062800027 20070628 00027 2007 6 28 C2XA07CL054 2 20070618 A 7532 8166011 BLEED VALVE EMB 145 EMB145LR 3260212 SO NR 2 ENGINE STICKING A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 16919 15064 145393 MKE FLIGHT 2266, THE CREW REPORTED THE NR 2 HIGH STAGE BLEED VALVE C/B POPPED IN FLIGHT AND NOTICED A SMOKE SMELL IN THE CABIN. MAINTENANCE INSPECTED AND REPLACED THE NR 2 HIGH STAGE BLEED VALVE. ALSO REPLACED THE NR 2 HIGH STAGE VALVE PR ESSURE SWITCH. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007062800028 20070628 00028 NM 2007 6 28 NOCA12207 1 20070617 A 5320 146T1552 BRACE BOEING 767 767306 1385148 NM BS 1329 CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 765NA 28098 CORROSION ON ANGLE BRACE STA 1329. REPLACED ANGLE BRACE PER SRM 53-60-07. 2 L 7 2 4F RT A1NM 2007062800029 20070628 00029 NM 2007 6 28 NOCA12407 1 20070617 A 5315 FLOORBEAM BOEING 767 767306 1385148 NM BS 1417 CRACKED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 765NA 28098 BULK CARGO FLOORBEAM ATTACH POINT CRACKED STA 1417 LEFT BL 10. REPLACED FLOORBEAM ATTACH POINT PER SRM 51-10-02. 2 L 7 2 4F RT A1NM 2007062800030 20070628 00030 2007 6 28 NOCA10907 2 20070606 A 7230 COMPRESSOR BOEING 757 75728A 1384976 NM LT ENGINE STALLED A NOCA O OTHER O OTHER CL CLIMB 1 EA 15 754NA 29381 LEFT ENGINE HAD TWO COMPRESSOR STALLS PASSING THROUGH 1500 FEET ON DEPT WHILE ADDING POWER ON THE LT ENGINE. MAINTENANC E WILL ACCOMPLISH A BITE ON THE BPCU AND TPU AND GET FAULT CODES, WILL FOLLOW FIM REF 71-06-00 FIG 105A FOR ENGINE SURGE (STALL) IN FLIGHT DURING ACCEL/DECEL BELOW 17,500 FEET. [06-29-07] REMOVED AND REPLACED NR 1 ENGINE PER AA MCM 71-94- 01, 71-92-01. CAPTURED IN PL 754-0706-02. 2 L 7 2 4F RT A2NM 2007062800031 20070628 00031 NM 2007 6 28 NOCA11907 1 20070617 A 5312 146T1261 STIFFENER BOEING 767 767306 1385148 NM BS 1439 CRACKED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 765NA 28098 BULKHEAD STIFFENER / FLOORBEAM SUPPORT IS CRACKED AT STA 1439 LEFT BL 16. REMOVED AND REPLACED STIFFENER AS PER SRM 51- 10-02. 2 L 7 2 4F RT A1NM 2007062800032 20070628 00032 NM 2007 6 28 NOCA11107 1 20070617 A 5313 146T3001160 STRINGER BOEING 767 767306 1385148 NM BS 1325 CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 765NA 28098 CORROSION ON STRINGER 19R AT STA 1325. REMOVED CORROSION AND REPAIRED STRINGER PER MRB CMRB-015. 2 L 7 2 4F RT A1NM 2007062800033 20070628 00033 NM 2007 6 28 NOCA12607 1 20070617 A 5320 BRACKET BOEING 767 767306 1385148 NM BS 1330 CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 765NA 28098 ANGLE BRACKET HAS CORROSION STA 1330. REPLACED ANGLE BRACKET PER SRM 51-10-02. 2 L 7 2 4F RT A1NM 2007062800034 20070628 00034 NM 2007 6 28 NOCA11807 1 20070617 A 5320 STIFFENER BOEING 767 767306 1385148 NM BS 1307 CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 765NA 28098 CORROSION ON BELLFRAME J STIFFENER. REPLACED BELLFRAME J STIFFENER PER SRM 51-10-02. 2 L 7 2 4F RT A1NM 2007062800035 20070628 00035 NM 2007 6 28 NOCA12507 1 20070617 A 5315 FLOORBEAM BOEING 767 767306 1385148 NM BS 1417 CRACKED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 765NA 28098 BULK CARGO FLOORBEAM ATTACH POINT CRACKED STA1417. REPLACED FLOORBEAM ATTACH POINT AS PER SRM 51-10-02. 2 L 7 2 4F RT A1NM 2007062800036 20070628 00036 NM 2007 6 28 NOCA11507 1 20070617 A 5312 STIFFENER BOEING 767 767306 1385148 NM BS 1461 BENT A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 765NA 28098 BULKHEAD STIFFENER / FLOORBEAM SUPPORT IS BENT STA 1461 LEFT BL 24. REMOVED AND REPLACED STIFFENER AS PER SRM 51-10-02. 2 L 7 2 4F RT A1NM 2007062800037 20070628 00037 NM 2007 6 28 NOCA12907 1 20070617 A 5712 4031877 RIB BOEING 767 767306 1385148 NM LT WING CRACKED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 765NA 28098 FIXED L/E RIB CRACKED AT REAR SPAR. REPLACED AIR LOAD RIB AND SUPPORT CLIP PER SRM 51-10-02. 2 L 7 2 4F RT A1NM 2007062800038 20070628 00038 NM 2007 6 28 NOCA13007 1 20070617 A 5712 4146767 RIB BOEING 767 767306 1385148 NM NR 6 SLAT CRACKED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 765NA 28098 RIB CRACKED AFT OF NR 6 SLAT AT REAR SPAR. REPLACED RIB SEALED AND PAINTED AS PER 57-11-00-1. 2 L 7 2 4F RT A1NM 2007062800039 20070628 00039 NM 2007 6 28 NOCA12807 1 20070617 A 5347 MOUNT BOEING 767 767306 1385148 NM GALLEY CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 765NA 28098 AFT INBOARD GALLEY FLOOR MOUNT CORRODED. REPLACED GALLEY FLOOR MOUNT PER SRM 53-11-54. 2 L 7 2 4F RT A1NM 2007062800040 20070628 00040 NM 2007 6 28 NOCA12707 1 20070617 A 5340 STRINGER CLIP BOEING 767 767306 1385148 NM BS 1324 CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 765NA 28098 STRINGER CLIP AT STA 1324 HAS CORROSION. REPLACED STRINGER CLIP PER SRM 51-10-02. 2 L 7 2 4F RT A1NM 2007062800041 20070628 00041 NM 2007 6 28 NOCA12107 1 20070617 A 5311 146T1511 FRAME BOEING 767 767306 1385148 NM BS 1307 CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 765NA 28098 AREA OF CORROSION OUTBOARD FWD SIDE OF FRAME 22 INCHES ABOVE FLOOR STA 1307. REPLACED BELLFRAME PER SRM 51-10-02. 2 L 7 2 4F RT A1NM 2007062800042 20070628 00042 NM 2007 6 28 NOCA11607 1 20070617 A 5312 STIFFENER BOEING 767 767306 1385148 NM BULKHEAD BENT A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 765NA 28098 BULKHEAD STIFFENER / FLOORBEAM SUPPORT IS BENT AT STA 1461. REPLACED STIFFENER AS PER SRM 51-10-02. 2 L 7 2 4F RT A1NM 2007062800043 20070628 00043 NM 2007 6 28 NOCA11307 1 20070617 A 5347 SEAT TRACK BOEING 767 767306 1385148 NM BS 960-1085 CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 765NA 28098 CORROSION ON SEAT TRACK OUT OF SRM LIMITS AT NUMEROUS LOCATIONS FROM STA 960 - 1085. REMOVED AND REPLACED SEAT TRACK AS PER MM 53-00-52. 2 L 7 2 4F RT A1NM 2007062800044 20070628 00044 NM 2007 6 28 NOCA11407 1 20070617 A 5347 SEAT TRACK BOEING 767 767306 1385148 NM BS 962-1095 CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 765NA 28098 SEAT TRACK CORROSION BEYOND SRM LIMITS NUMEROUS LOCATIONS 962 - 1095. REMOVED AND REPLACED SEAT TRACK AS PER SRM 53-00- 52. 2 L 7 2 4F RT A1NM 2007062800045 20070628 00045 NM 2007 6 28 NOCA11707 1 20070617 A 5312 STIFFENER BOEING 767 767306 1385148 NM BULKHEAD BENT A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 765NA 28098 BULKHEAD STIFFENER / FLOORBEAM SUPPORT IS BENT AT STA 1480 LEFT BL16. REMOVED AND REPLACED STIFFENER PER SRM 51-10-02. 2 L 7 2 4F RT A1NM 2007062800046 20070628 00046 NM 2007 6 28 NOCA12307 1 20070617 A 5312 146T1261 STIFFENER BOEING 767 767306 1385148 NM BULKHEAD BENT A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 765NA 28098 BULKHEAD STIFFENER / FLOORBEAM SUPPORT IS BENT STA 1480 LEFT LBL 24. REPLACED STIFFENER PER SRM 51-10-02. 2 L 7 2 4F RT A1NM 2007062800047 20070628 00047 NM 2007 6 28 NOCA11207 1 20070617 A 5315 141T5113 FLOORBEAM BOEING 767 767306 1385148 NM BS 325 CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 765NA 28098 FLOORBEAM AT STA 325 LBL 27 HAS CORROSION BEYOND SRM LIMITS. REPAIRED FLOORBEAM PER MRB CMRB-014. 2 L 7 2 4F RT A1NM 2007062800048 20070628 00048 NM 2007 6 28 NOCA11007 1 20070617 A 5311 FRAME BOEING 767 767306 1385148 NM BS 1346 CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 765NA 28098 FAIL SAFE STRAP ON FRAME AT STA 1346 HAS CORROSION AT FLOOR LINE BEYOND SRM LIMITS. REPAIRED FAIL SAFE STRAP CORROSION AT STA 1346 PER MRB 767-2986. 2 L 7 2 4F RT A1NM 2007062800049 20070628 00049 2007 6 28 YENA2007053 4 20070618 A 3414 INDICATOR AIRBUS 320 A320232 3930326 EU AIRSPEED READS LOW A YENA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 EA 15 624JB 2520 DURING TAKEOFF ROLL F/O'S AIRSPEED INDICATION WAS LOW AND 40KTS LOWER THAN CAPT. NO BETTER AT 75KTS. T/O ABORTED. FOU ND F/O'S PITOT PROBE OBSTRUCTED. PERFORMED TASK 34-10-00-00-170-001, FLUSHING OF TOTAL PRESSURE LINE. RECONNECTED PITO T LINE. PERFORMED LEAK CHECK OF SYSTEM IAW AMM 34-13-00-790-002. FOUND WITHIN MM LIMITS. 2 L 7 2 4F RT A28NM 2007062800050 20070628 00050 CE 2007 6 28 BSYA20070010 1 20070620 A 5610 WINDOW BEECH 58 58 1152740 CE COCKPIT OPEN E BSYA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 696BD TH352 ON TAKEOFF OUT OF TEB CO-PILOTS EMERGENCY WINDOW POPPED OPEN. ABORTED TAKEOFF, WENT BACK TO RAMP AND SECURED WINDOW, CO NTINUED WITH FLIGHT TO BDL. 1 L 7 2 3O 3A16 2007062800051 20070628 00051 CE 2007 6 28 BSYA200700011 1 20070620 A 3297 WIRE BEECH 58 58 1152740 CE MLG BROKEN E BSYA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 4AW TH450 ON TAKEOFF OUT OF BHM PILOT SELECTED GEAR UP BUT NOTHING HAPPENED. RETURNED TO BHM WHERE MAINTENANCE FOUND BROKEN WIRE OFF THE LEFT GEAR SQUAT SWITCH. REPAIRED WIRE, OPS CHECKS GOOD. 1 L 7 2 3O 3A16 2007062800052 20070628 00052 EU 2007 6 28 2007UALA01823 1 20070605 A 2130 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN PRESSURE UNKNOWN A UALA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 401UA 435 RTFL DUE TO SLOW CABIN DEPRESSURIZATION. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062800053 20070628 00053 WP 2007 6 28 ABXA070182 1 20070613 A 2432 2634006106 CHARGER DOUG DC9 DC941 302207N WP E/E BAY DEFECTIVE A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 970AX 2411 47494 WHILE STARTING APU, NOTICED NOISE AND SMOKE EMITTING FROM BATTERY CHARGER. REPLACED BATTERY CHARGER IAW DC9 MM 24-30-02 -2-0001. ALSO, REPLACED BOTH AIRCRAFT BATTERIES AND BATTERY TEMPERATURE SENSOR IAW DC9 MM 24-30-01-0-0001. 2 L 7 2 4F A6WE 2007062800054 20070628 00054 NM 2007 6 28 MWEA070151 1 20070618 A 3220 39206391 RETAINING RING DOUG MD88 MD88 3023688 NM NLG BROKEN A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 822ME 49759 NOSE GEAR WILL NOT RETRACT ON TAKEOFF. FOUND STRUT NOT FULLY EXTENDING, REMOVED STRUT & FOUND UPPER SLEEVE RETAINING RI NG BROKEN & BUSHINGS DAMAGED. REMOVED AND REPLACED RETAINING RING & BUSHINGS. 2 L 7 2 4F RT A6WE 2007062800055 20070628 00055 NM 2007 6 28 MWEA070150 1 20070615 A 3520 E7406900 OXYGEN MASK BOEING 717 717200 1383700 NM CABIN OUT OF POSITION A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 902ME 55166 WHILE PERFORMING 02 MASK DROP FUNCTIONAL CHECK IN CABIN, FAILED TO OPEN. OPEN DOOR MANUALLY & REPOSITION MASK AND HOSE. CHECKED DROP OPERATION. 2 L 7 2 4F TR A6WE 2007062800056 20070628 00056 NM 2007 6 28 ASAA0741788 1 20070619 A 5313 654688139 STRINGER BOEING 737 737490 1384715 NM BS 1081 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 DENT ON TOP OF STRINGER. REPAIRED DENT IAW SRM 53-00-53 FIG 201 REPAIR 1. 2 L 7 2 4F RT A16WE 2007062800089 20070628 00089 EA 2007 6 28 TRAX200700851 1 20070614 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 937EV 8042 CRACK FOUND ON PAX DOOR HANDLE. OUTER HANDLE ASSEMBLY REMOVED IAW MM 52-11-03 / TASK 52 11 03 020 07. LATCH LOCK BOX R EMOVED FOR ACCESS AND INSTALLED IAW 52-11-21. LATCH LOCK BOX AND OUTER HANDLE INSTALLED IAW 32-11-03 AND 52-11-25. FUN CTIONAL TEST OF PASSENGER DOOR C/O IAW 52-11-03 720 802. SUPPLEMENTAL - SDR CLOSED 06/21/07. 2 L 7 2 4F RT A21EA 2007062800090 20070628 00090 EU 2007 6 28 USA2007F00001 1 20070228 A 5330 ASNA2051DKJ SKIN AIRBUS A321 A321211 3930370 EU CFMINT CFM56 CFM565B3P 13006 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 167US 21122 1442 CORRODED RIVET TAILS WERE FOUND IN FUSELAGE FORWARD CARGO COMPARTMENT BETWEEN FRAME 35 TO AFT PRESSURE BULKHEAD FROM S38 L TO 38R. APPROXIMATELY 100 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RI VETS HAD THE PAINT FLAKING OFF THE RIVET TAILS THAT WERE CLEANED AND HAD PRIMER AND PAINT REAPPLIED. AC WAS MFG 3/21/01 . (K) 2 L 7 2 4F 4 F RT A28NM E37NE 2007062800134 20070628 00134 NM 2007 6 28 BB07044 1 20070622 A 2497 ELECTRICAL BOX BOEING 757 7572B7 1384964 NM SEAT 10AC SMOKE A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 942UW 27807 FLIGHT 1729, BOS-CLT: ON DESCENT INTO CLT, SMOKE BEGAN TO FILL THE CABIN. CREW ACCOMPLISHED SMOKE IN CABIN PROCEDURES AND THE CABIN CLEARED. MAINTENANCE FOUND THE SEB AT ROW 10AC TO BE THE SOURCE. REMOVED SEB AND CABLE. RELEASED PER ME L. [07-10-07] REPLACED SEAT ROW 10AC AND WIRING HARNESS AT 10B. 2 L 7 2 4F RT A2NM 2007062800135 20070628 00135 EU 2007 6 28 BA07006 1 20070621 A 3350 321491 POWER SUPPLY AIRBUS 330 A330323 3930335 EU EMERGENCY LIGHTS FAULTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 276AY 0375 MAINTENANCE FOUND THE STANDBY POWER SUPPLY UNIT FAULTED. REPLACED POWER SUPPLY UNIT. NO FURTHER FAULTS. 2 L 7 2 4F RT A46NM 2007062800136 20070628 00136 NM 2007 6 28 BB07045 1 20070619 A 3350 321491 POWER SUPPLY BOEING 757 7572B7 1384964 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 936UW 27244 MAINTENANCE FOUND THE R1 SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A2NM 2007062800137 20070628 00137 WP 2007 6 28 ABXA070184 1 20070612 A 3350 5708458503 BATTERY DOUG DC8 DC863F 302198F WP EMERGENCY LIGHTS DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 EMERGENCY EXIT LIGHT BATTERY PACK DEAD UNABLE TO CHANGE. REMOVED AND REPLACED EMERGENCY LIGHT PACK ASSEMBLY IAW DC8 AMM 33-50-01. 2 L 7 4 4F 4A25 2007062800138 20070628 00138 SO 2007 6 28 C2XA07IA145 1 20070620 A 3350 3025103 LIGHT EMB 135 EMB135LR 3260305 SO LT OVERWING INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27523 145389 IAH - DURING A-CHECK INSPECTION, THE LEFT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007062800139 20070628 00139 2007 6 28 2007UALA01161 4 20070413 A 2200 UNK POWER SUPPLY 3945122506 AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ELAC 1 FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 443UA 2 2168 820 FLIGHT DIVERTED WITH A RUDDER PROBLEM. *S/D* REPLACED ELAC 1. UNIT FAILED MPS STRESS TEST AT OVERHAUL AND MPS T1 WAS REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062800140 20070628 00140 EU 2007 6 28 2007UALA01260 1 20070420 A 2741 422081100 TRANSDUCER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE THS ACTUATOR FAULTY A UALA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 490UA 17278 2413 1728 PITCH TRIM KEEPS HUNTING NOSE UP ATTITUDE. *S/D* FAULT TRACED TO FAULTY THS ACTUATOR POSITION TRANSDUCER. REPLACED BO TH COMMAND AND MONITOR TRANSDUCERS AS A PRECAUTIONARY MEASURE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062800141 20070628 00141 NM 2007 6 28 2007UALA02015 1 20070614 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 565UA 26669 EMERGENCY LIGHT INOP IN OVERHEAD PANEL SEAT 6AB. *S/D* REPLACED EMERGENCY LIGHT IN OVERHEAD PANEL AT SEAT 6AB PER MM 3 3-51-01, PERFORMED OPS CHECK, CHECK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062800142 20070628 00142 NM 2007 6 28 2007UALA02016 1 20070614 A 3350 362624 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 565UA 26669 EMERGENCY LIGHT ON AFT CARGO DOOR INOPERATIVE. *S/D* REPLACED LAMP, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062800143 20070628 00143 NM 2007 6 28 2007UALA02017 1 20070614 A 3350 362624 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 565UA 26669 R-4 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. *S/D* REPLACED LAMP. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062800165 20070628 00165 NM 2007 6 28 2007UALA02092 1 20070618 A 5100 NONE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NONE NONE A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 781UA 26945 777047 FLIGHT DIVERTED DUE TO REPORT OF FUMES IN THE CABIN ISOLATED TO THE NR 2 ENGINE. [07-17-07] CHECKED APU INLET & FOUND INTAKE SCREEN FULL OF CICADAS. SUSPECT ALL SMOKE AND ODOR RELATED LOG ITEMS CAUSED BY CICADAS WHICH WERE BURNED BY LO AD COMPRESSOR OF APU. REPLACED APU DUE TO POSSIBLE FOREIGN OBJECT INGESTION. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007062800183 20070628 00183 NM 2007 6 28 2007UALA02114 1 20070619 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 AFT CABIN FLOOR CREASE BEAM HAS AREAS OF CORROSION JUST BELOW AFT ENTRY DOOR CUTOUT BS 967-986. MAJOR REPAIR ACCOMPLISH ED: INSTALLED NEW INNER CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062900001 20070629 00001 NM 2007 6 29 SWAA073072 1 20070620 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 261WN 32517 FWD CABIN EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007062900002 20070629 00002 NM 2007 6 29 SWAA073071 1 20070620 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 231WN 32499 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 3 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007062900003 20070629 00003 2007 6 29 SWAA073068 4 20070620 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 405WN 27893 DURING SCHEDULED 8Y CHECK, R1 DOOR EMERGENCY EVAC SLIDE FAILED OPS CHECK. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007062900004 20070629 00004 NM 2007 6 29 SWAA073067 1 20070620 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 410 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, LBL 1. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007062900005 20070629 00005 NM 2007 6 29 SWAA073076 1 20070620 A 5330 6545767 SKIN BOEING 737 7373G7 1384595 NM BS 415 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 415, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007062900008 20070629 00008 NM 2007 6 29 SWAA073060 1 20070620 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM BS 271 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 271, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007062900009 20070629 00009 NM 2007 6 29 SWAA073078 1 20070620 A 5752 654645518 TAB BOEING 737 7373G7 1384595 NM RT AILERON WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED C4 CHECK, FOUND RT WING AILERON TAB OUTBOARD HINGE FITTING WORN. REMOVED AND REPLACED AILERON TAB PER MM. 2 L 7 2 4F RT A16WE 2007062900010 20070629 00010 NM 2007 6 29 SWAA073080 1 20070620 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007062900012 20070629 00012 NM 2007 6 29 SWAA073063 1 20070620 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007062900013 20070629 00013 NM 2007 6 29 SWAA073074 1 20070620 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 16L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007062900014 20070629 00014 NM 2007 6 29 SWAA073066 1 20070620 A 2730 656531018 TORQUE TUBE BOEING 737 7373H4 1384600 NM RT ELEVATOR FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED BRDG CHECK, LT AND RT ELEVATORS FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR OUTPUT TORQUE TU BE PER MM. 2 L 7 2 4F RT A16WE 2007062900016 20070629 00016 EA 2007 6 29 COMA0770034 1 20070615 A 2780 5912999 BPSU CNDAIR CL600 CL6002C10 1390015 EA LT WING SLATS FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 369CA 5089 10079 FLIGHT 5535 - SLATS FAIL CAUTION MESSAGE AND NO DEPLOYMENT WHEN SELECTED ON APPROACH. REMOVED AND REPLACED LEFT SLAT BP SU. 2 L 7 2 4F RT A21EA 2007062900017 20070629 00017 EA 2007 6 29 COMA0770035 1 20070620 A 2780 SLAT SYSTEM CNDAIR CL600 CL6002C10 1390015 EA LE SLATS MALFUNCTIONED A COMA O OTHER O OTHER DE DESCENT 1 SO 01 371CA 10082 FLIGHT 5077 - SLATS FAILED AT 0 DEGREES. FLAPS OPS NORMAL. CREW DECLARED AN EMERGENCY, AIRCRAFT LANDED SAFELY. PERFOR MED MECHANICAL RIGGING OF RIGHT SIDE SLAT SYSTEM. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007062900018 20070629 00018 EA 2007 6 29 COMA0760433 1 20070613 A 5100 NONE CNDAIR CL600 CL6002B19 1900309 EA RT WING NONE A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 960CA 28211 7117 TEMPORARY REPAIR INCORPORATED FOR RIGHT LOWER WING PLANK CRACK AT WS 148.019 IAW REO 601R-57-21-138. COMPLIED WITH PERM ANENT REPAIR OF THE RIGHT LOWER WING PLANK CRACK IAW REO 601R-57-21-130 REV G AND CRJ REO 601R-57-21-829. 2 L 7 2 4F RT A21EA 2007062900019 20070629 00019 EA 2007 6 29 COMA0760434 1 20070613 A 5100 NONE CNDAIR CL600 CL6002B19 1900309 EA NONE NONE A COMA O OTHER O OTHER NR NOT REPORTED 1 SO 01 960CA 28211 7117 TEMPORARY REPAIR INCORPORATED FOR LEFT LOWER WING PLANK CRACK AT WS 148.019 IAW REO 601R-57-21-138. COMPLIED WITH PERMA NENT REPAIR OF THE LEFT LOWER WING PLANK CRACK IAW REO 601R-57-21-130 REV G AND CRJ REO 601R-57-21-829. 2 L 7 2 4F RT A21EA 2007062900024 20070629 00024 EA 2007 6 29 COMA0760439 1 20070616 A 2750 860D10018ABC FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 914CA 23957 7012 EN ROUTE CVG-CXO RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO CVG. FLIGHT LANDED WI THOUT INCIDENT. REPLACED THE FLAP ELECTRONIC UNIT. 2 L 7 2 4F RT A21EA 2007062900025 20070629 00025 2007 6 29 COMA0760440 2 20070617 A 7210 GEARBOX CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE OVERHEATED A COMA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 01 713CA 7245 FLIGHT 5589 - EN ROUTE CVG-NAS RECEIVED A RIGHT ENGINE OIL HIGH TEMPERATURE INDICATION. FLIGHT RETURNED TO CVG. SERVIC ED RIGHT ENGINE AGB. 2 L 7 2 4F RT A21EA 2007062900026 20070629 00026 2007 6 29 COMA0760441 2 20070618 A 7261 R1310P022 SEAL CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE MISSING A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 712CA 7244 FLIGHT 4945 - EN ROUTE CVG-OKC RECEIVED A LEFT ENGINE OIL PRESSURE FLUCTUATION WITH INTERMITTENT OIL PRESSURE WARNING. CREW DECLARED AN EMERGENCY AND FLIGHT RETURNED TO CVG LANDING WITHOUT INCIDENT. INSTALLED A STARTER MATING SEAL. 2 L 7 2 4F RT A21EA 2007062900028 20070629 00028 EA 2007 6 29 COMA0760443 1 20070618 A 5346 601350065 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 442CA 16080 7483 DURING INSPECTION FOUND THE ENGINE SUPPORT BEAM CRACKED ON BOTTOM WEB LEFT SIDE, FORWARD CORNER. REPAIRED IAW REO 601R- 53-61-358. 2 L 7 2 4F RT A21EA 2007062900029 20070629 00029 EA 2007 6 29 COMA0760444 1 20070618 A 5346 601350065 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 442CA 16080 7483 DURING INSPECTION FOUND THE ENGINE SUPPORT BEAM CRACKED ON BOTTOM WEB LEFT SIDE, FORWARD CORNER. REPAIRED IAW REO 601R- 53-61-358. 2 L 7 2 4F RT A21EA 2007062900030 20070629 00030 EA 2007 6 29 COMA0760445 1 20070619 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FS 559 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 33218 7026 FOUND CRACK EXTENDING THROUGH TOP OF STOP DRILL ON TEMP REPAIR, 559.00 RIGHT SIDE SEMI PRESSURE BULKHEAD. PERFORMED PER MANENT REPAIR ON FS 559 RIGHT SIDE PER SR10-5341-001 REV A SECTION II. 2 L 7 2 4F RT A21EA 2007062900031 20070629 00031 EA 2007 6 29 COMA0760446 1 20070619 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FS 235 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 962CA 28084 7123 FUSELAGE SKIN AFT OF NOSE LANDING GEAR CUTOUT AT RIGHT RADIUS IS CRACKED. REPAIRED FUSELAGE SKIN AFT OF NOSE LANDING GE AR CUTOUT RIGHT SIDE, IAW REO 601R-53-11-048. 2 L 7 2 4F RT A21EA 2007062900033 20070629 00033 NM 2007 6 29 ASAA0791795 1 20070531 A 5310 146A750352 RAIL BOEING 737 737990 NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT SUPPORT RAILS CORRODED. REPAIRED IAW EA5310 02724. 2 L 7 4 4F RT A16WE 2007062900034 20070629 00034 NM 2007 6 29 ASAA0791796 1 20070531 A 5310 146A750344 RAIL BOEING 737 737990 NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT SUPPORT RAIL CORRODED. REPAIRED IAW EA5310 02724. 2 L 7 4 4F RT A16WE 2007062900035 20070629 00035 NM 2007 6 29 ASAA0791797 1 20070531 A 5310 146A750343 RAIL BOEING 737 737990 NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT SUPPORT RAIL CORRODED. REPAIRED IAW EA5310 02724. 2 L 7 4 4F RT A16WE 2007062900036 20070629 00036 NM 2007 6 29 ASAA0791798 1 20070531 A 5310 146A750351 RAIL BOEING 737 737990 NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT SUPPORT RAIL CORRODED. REPAIRED IAW EA5310 02724. 2 L 7 4 4F RT A16WE 2007062900037 20070629 00037 NM 2007 6 29 ASAA0791799 1 20070531 A 5310 146A750359 RAIL BOEING 737 737990 NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT SUPPORT RAIL CORRODED. REPAIRED IAW EA 5310 02724. 2 L 7 4 4F RT A16WE 2007062900038 20070629 00038 NM 2007 6 29 ASAA0791800 1 20070531 A 5347 146A750129 CARGO TRACK BOEING 737 737990 NM BS 794-847 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO RT CARGO TIE DOWN TRACK CORRODED. SPLICED IN NEW SECTION. 2 L 7 4 4F RT A16WE 2007062900042 20070629 00042 NM 2007 6 29 ASAA0791804 1 20070531 A 5310 146A750340 RAIL BOEING 737 737990 NM BS 727D CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT SUPPORT RAIL CORRODED. REPAIRED IAW EA 5310 02724. 2 L 7 4 4F RT A16WE 2007062900043 20070629 00043 NM 2007 6 29 ASAA0791805 1 20070531 A 5310 146A750348 RAIL BOEING 737 737990 NM BS 727D CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT FLOOR RAIL CORRODED. REPAIRED IAW EA5310 02724. 2 L 7 4 4F RT A16WE 2007062900044 20070629 00044 NM 2007 6 29 ASAA0791806 1 20070531 A 5347 146A750613 CARGO TRACK BOEING 737 737990 NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT TIE DOWN SPLICE CORRODED. REPAIRED IAW SRM 51-40-02 AND 51-40-05. 2 L 7 4 4F RT A16WE 2007062900045 20070629 00045 NM 2007 6 29 ASAA0791807 1 20070531 A 5347 146A750614 CARGO TRACK BOEING 737 737990 NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT TIE DOWN TRACK SPLICE CORRODED. REPAIRED IAW 51-40-02 AND 51-40-05. 2 L 7 4 4F RT A16WE 2007062900047 20070629 00047 NM 2007 6 29 ASAA0791809 1 20070531 A 5310 146A750611 RAIL BOEING 737 737990 NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT RAIL SPLICE CORRODED. REPAIRED IAW 51-40-05 AND 51-40-02. 2 L 7 4 4F RT A16WE 2007062900049 20070629 00049 WP 2007 6 29 07FDEA02225 1 20070620 A 5310 AFA70981 LONGERON DOUG MD10 MD1010F 3022112 WP BS 1781 CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 398FE 46634 CENTER LOWER CARGO COMPTMENT, LONGERON 46R IS CORRODED OUT OF LIMITS AT FS 1781 AFTER CLEAN UP. [07-27-07] REPAIRE D LONGERON 46R IAW FEDEX EA 8-5310-112950. REMOVED AND REINSTALLED SUBSTRUCTURE AS REQUIRED FOR ACCESS IAW DC/MC 10 SRM 51-31-01, 51-33-01 AND 51-35-01 VOL II. THIS IS A MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2007062800132 20070628 00132 NM 2007 6 28 SWAA073069 1 20070617 A 2560 P2070001 FLASHLIGHT BOEING 737 73776Q 13845AA NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 551WN 30280 DURING SCHEDULED BRDG CHECK, FOUND FWD INBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2007062800133 20070628 00133 NM 2007 6 28 SWAA073075 1 20070620 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007062800144 20070628 00144 NM 2007 6 28 2007UALA02019 1 20070614 A 3350 362624 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 512UA 24809 EXTERIOR EMERGENCY LIGHT AT DOOR 2R INOP. *S/D* RELAMPED, OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062900006 20070629 00006 NM 2007 6 29 SWAA073065 1 20070620 A 5314 6545776 PANEL BOEING 737 7373H4 1384600 NM BS 714 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED BRDG CHECK, FOUND KEEL BEAM STRESS PANEL CRACKED AT BS 714, STR 27R. REPAIRED PANEL PER SRM. 2 L 7 2 4F RT A16WE 2007062900051 20070629 00051 2007 6 29 TSAA0734034 4 20070618 A 3417 HG480B42 ADC BOEING 737 737282C 13844AU NM COCKPIT FAILED A TSAA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 13 826AL 23051 NON-ETOPS FLIGHT 946 HNL- KOA - DURING CLIMB, THE CREW NOTED LOSS OF INDICATION ON THE AIRSPEED INDICATOR, ALTIMETER AND VERTICAL SPEED INDICATOR. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE DIGITAL AIR DATA COMPUTER AND FOUND ALL OPERATIONAL CHECKS OKAY. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007062900052 20070629 00052 NM 2007 6 29 TSAA0753035 1 20070619 A 5310 654655055 SKIN BOEING 737 737236 1384476 NM BS 787 DAMAGED A TSAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 13 836AL 23225 AT HNL, A BAGGAGE BELT LOADER WAS DRIVEN UNDER THE AIRCRAFT DAMAGING UNDERNEATH THE AFT CARGO DOOR. THE DAMAGE EXTENDS TO AN EXISTING REPAIR AT BODY STATION 787, BETWEEN STRINGER 26-27R. A TECHNICAL IN-SERVICE REQUEST HAS BEEN SUBMITTED T O BOEING FOR A REPAIR. [07-09-07] REPAIR HAS BEEN COMPLETED PER ECO 3662 R.1. , BOEING AND ALOHA AGREEMENT NO. 6-1171- RE-01567 DATED 6-29-07, BOEING MESSAGE FRR-PK764-001, DATED 7-1-07 & BOEING MESSAGE 1-3863310666-12 DATED 7-5-07. FORM 337 AND 8100-9 HAVE BEEN RECEIVED FOR THE REPAIR. FINAL REPAIR DIMENSIONS APPROX 181 IN. X 57 IN.. 2 L 7 2 4F RT A16WE 2007062900053 20070629 00053 EU 2007 6 29 COEA0702903 1 20070126 A 5313 STRINGER AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A COEA O OTHER O OTHER NR NOT REPORTED 1 NM 13 903FX 179 DURING HEAVY CHECK MAINTENANCE, FOUND AREAS OF LEVEL 2 CORROSION ALONG STRINGER 17R FROM FRAME 15 TO 23 WITH A MAXIMUM D EPTH OF .010 INCH. THE STRINGER WILL NEED TO BE INSTALLED IN SECTIONS WITH REPAIR SLICES. THIS WILL RESULT IN A MAJOR REPAIR. (M) 2 H 7 2 4T RT A53EU 2007062900054 20070629 00054 EU 2007 6 29 COEA0703903 1 20070212 A 5313 S53371311202 STRINGER AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 903FX 179 DURING HEAVY CHECK, MAINTENANCE FOUND CORROSION ALONG STRINGER 16R BETWEEN FRAME 22 AND FRAME 23. THE STRINGER WILL NEE D TO BE INSTALLED IN SECTIONS WITH REPAIR SLICES. THIS WILL RESULT IN A MAJOR REPAIR. REMOVED STRINGER 16R FROM FRAME 22 TO FRAME 23. INSTALLED NEW STRINGER SECTION AND FABRICATED STRINGER SPLICE AT STRINGER 16R BETWEEN FRAME 22 AND FRAM E 23 IAW ATR42 SRM. (M) 2 H 7 2 4T RT A53EU 2007062900062 20070629 00062 NM 2007 6 29 QXEA200701002 1 20070610 A 5240 CHANNEL BOMBDR DHC8 DHC8402 1390042 NM FUEL DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - INBOARD FLANGE OF AFT CHANNEL IS CRACKED JUST ABOVE SINGLE POINT FUELING HOOKUP. REPAIRED IAW SRM 52-42-05. 2 H 7 2 4T RT A13NM 2007062900064 20070629 00064 NM 2007 6 29 QXEA200701001 1 20070610 A 5250 DOUBLER BOMBDR DHC8 DHC8402 1390042 NM LAV DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - LAV DOOR INTERNAL DOUBLER CORROSION ON BOTTOM AFT SURFACE. REPAIRED IAW RD8/4-53-347. 2 H 7 2 4T RT A13NM 2007062900065 20070629 00065 NM 2007 6 29 QXEA200701018 1 20070621 A 3310 LAMP DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHTS BURNED OUT A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 352PH 494 PDX FLIGHT NR 2162 RIGHT TRU CAUTION DOES NOT LAMP TEST. MAINTENANCE RELAMPED. OPERATIONAL CHECK GOOD. AIRCRAFT RETUR NED TO SERVICE. 2 H 7 2 4T RT A13NM 2007062900067 20070629 00067 NM 2007 6 29 UIEA200700253 1 20070621 A 7830 9105M20G14 SKIN BOEING 747 7472D7B 1384803 NM THRUST REVERSER DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 NR 4 ENGINE RT REVERSER AT NAC STATION 206.10 UPPER SIDEWALL SKIN DELAMINATED. PERMANENT REPAIR WAS ACCOMPLISHED AS PER CF6-50 ENGINE MANUAL 78-32-03, REPAIR NR 13, REF: FIG 1. ALSO, REFERENCE ATLAS AIR XEO NR 78-062007. 2 L 7 4 4F RT A20WE 2007062900071 20070629 00071 NM 2007 6 29 UIEA200700252 1 20070621 A 5753 FAIRING BOEING 747 7472D7B 1384803 NM FLAP TRACK DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 RT WING, NR 8 FLAPTRACK FORWARD FIXED FAIRING HAS SEVERAL SMALL HOLES AT LEADING EDGE AREA. ACCOMPLISHED PERMANENT REPA IR AS PER 747-200 SRM 51-40-09, FIG 6, TABLE I AND 747-200 SRM 51-40-12. ALSO, REFERENCE ATLAS AIR XEO NR 57-061907. 2 L 7 4 4F RT A20WE 2007062900073 20070629 00073 NM 2007 6 29 NWAA072205801 1 20070620 A 3150 UNKNOWN BOEING 757 757351 1384991 NM UNKNOWN A NWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 01 581NW 32982 AFT LEFT CABIN DOOR DISPLAY DURING TAKEOFF. TAKEOFF ABORTED AT 120KTS WITH AIRCRAFT TAKEOFF GROSS WEIGHT AT 256,900 NR. INSPECTED DOOR 4 LEFT. NO DEFECTS NOTED. OPERATED DOOR SEVERAL TIMES. ALL INDICATIONS NORMAL. DEFERRED DOOR 4 LEFT INDICATOR LIGHT TO MEL 52-71-1. DDG C/W. PER MEL 52-71-1 DDG, PRIOR TO FLIGHT INSPECTED DOOR 4 LEFT, DOOR IS CONFIRME D CLOSED AND LOCKED. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2007062900074 20070629 00074 NM 2007 6 29 DLM88070722 1 20070614 A 3097 WIRE DOUG MD88 MD88 3023688 NM WINDSHEILD BURNED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 977DL 53258 WIRE CABLE ON CAPT SIDE BLEW, OCCURED IMMEDIATELY AFTER TURNING WINDSHEILD ANTI FOG ON. REMOVED DAMAGED ANTI FOG WIRING TO CAPT CLEARVIEW SLIDING WINDOW AND CAPPED OFF ENDS AND SECURED WIRES. PULLED AND COLLARED CBS FOR WINDOW ANT FOG SYS X-26 Z-26 Z-25 VERIFIED WINDSHEILD ANTI ICE SYS. OPERATIONAL FWD ANTI FOG SYS TO MCO AND PLACARDED PER MEL 30-00-20B. REPLACED WIRE SPLICES CKS NML MCO/PLAC REMOVED. 2 L 7 2 4F RT A6WE 2007062900076 20070629 00076 NM 2007 6 29 DL76S070732 1 20070615 A 2120 UNKNOWN BOEING 767 767332 1382001 NM CABIN ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 131DN 24852 BURNING L ELECT SMELL IN AFT PART OF CABIN. SMELL WENT AWAY WHEN CEILING LIGHTS TURNED OFF. TURNED ON ALL ELECT UNITS AND LIGHT THROUGHOUT AIRCRAFT. NO BURNING SMELL DETECTED. 2 L 7 2 4F RT A1NM 2007062900077 20070629 00077 NM 2007 6 29 DL76S070733 1 20070615 A 5312 PRESSURE PANEL BOEING 767 767332 1382001 NM BS 977 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 CABIN BS 977 RBL 23 MLG PRESSURE WEB SKIN CRACKED AND REPAIRED PER 53-50-51 FIGURE 201 REPAIR 1 ON NR CARD AJN 53146. 2 L 7 2 4F RT A1NM 2007062900079 20070629 00079 NM 2007 6 29 DL764070735 1 20070617 A 5100 NONE BOEING 767 767432ER 1385134 NM NONE NONE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 835MH 29708 AFTER PUSHBACK CABIN STARTED TO DESCEND AT 2000FM AND BOTH AUTO CONTROLLERS FAILED, RETURNED TO GATE. BITE CK BOTH CONT ROLLERS ALL CKS NML. RESET, TESTS NORMAL FOR SVC. 2 L 7 2 4F RT A1NM 2007062900080 20070629 00080 NM 2007 6 29 DLM88070736 1 20070617 A 4990 LINE DOUG MD88 MD88 3023688 NM APU LOOSE A DALA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 910DL 49541 AFTER TAKEOFF (APPROX 60 SECOND) ALL 3 LAV SMOKE DETECTORS SOUNDED FA'S AND PAX'S REPORTED SMOKE SMELL AND HAZE EMERG RETURN TO ATL. FOUND OIL CONTAMINATION IN APU INLET. LK CKD APU. FOUND B-NUT LEAKING ON OIL LINE AFT FILTER MODULE. TIGHTENED SAME. LK CK GOOD. REMOVED LOWER DOOR ASSY CLEANED INLET AND DOOR ASSY. REPLACED SEPARATOR BAGS AND CLEANED OIL FROM DUCTS. PERFORMED FULL DUCT BURNOUT OPN 5089. RAN ENGS TO T/O PWR SEVERAL TIMES. ALL CK GOOD, BORO OF 6TH 7 TH STG COMPRESSOR ON BOTH ENGS CKD GOOD. NO OIL PRESENT. 2 L 7 2 4F RT A6WE 2007062900084 20070629 00084 NE 2007 6 29 DL76L070740 2 20070614 A 7532 BLEED VALVE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 197DN 28454 727620 AFTER ENG START ON NR 2 ENG RT ENG BLEED LIGHT REMAINED ILLUMINATED WITH EICAS MSG. NO RT DUCT PRESSURE. RAN POWER UP RECYCLED SWITCHES SHUTDOWN AND RESTARTED ENGINE WITH NO CHANGE. REPLACED RT PRV VALVE IAW MM 254267. ALSO REP LACED CONTROLLER FOR PRV VALVE. OPS GOOD ON GROUND ENGINE RUN. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062900085 20070629 00085 NM 2007 6 29 DL76L070741 1 20070614 A 2160 CONTROLLER BOEING 767 767332 1382001 NM CABIN TEMP MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 178DN 25143 AFT CABIN TEMP CONTROLLER INOP AFT CABIN TEMP VARIED WIDELY. UNABLE TO CONTROL IN ANY MODE. ZONE TEMP CONTROLLER FAULT S AFT CABIN TRIM VALVE. REPLACED AFT CABIN TRIM VALVE PER AMM. CHKS OK. 2 L 7 2 4F RT A1NM 2007062900086 20070629 00086 NM 2007 6 29 DLM88070747 1 20070618 A 5330 5911401211 SKIN DOUG MD88 MD88 3023688 NM BS 215 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 A DENT AND A CREASE WAS REPAIRED WITH A DOUBLER. THE DOUBLER WAS INSTALLED AT FS 215 BETWEEN L-29R AND L-30. THIS REPA IR IS NEAR THE JACK POINT SUPPORT AND THE ATC TRANSPONDER ANTENNA FINGER DOUBLER. DTA REQUIRES A INSPECTION EVERY 8000 CYCLES. 2 L 7 2 4F RT A6WE 2007062900087 20070629 00087 NM 2007 6 29 DL764070749 1 20070618 A 3297 CONNECTOR BOEING 767 767432ER 1385134 NM PSEU DAMAGED A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 828MH 29699 DURING CLIMB-OUT, RECEIVED THE FOLLOWING MSGS EICAS, FLAPS RED A/T DISCONNECT GRD PROX SYS LDG GEAR MONITOR. R ICE DET LICE DET LDG GEAR INDICATING DOWN AND LOCKED WHEN IT WAS UP AND LOCKED. DURING THIS TIME WE RECEIVED A NON-SILENABLE AU RAL WARNING. THE MAX AIRSPEED ZIPPER LINE WAS SET AT 270 KTS. DURING THE APPR PHASE THE GEAR INDICATION DID NOT CHANGE WHEN THE GEAR WAS CYCLED. EMERGENCY DECLARED. UNEVENTFUL LDG, UPON ARRIVAL FOUND CARD 011 SENSOR 233 AND 264. CKD CONNECT DB17121J AND DA8121P FOR BENT PINS. REPLACED PSEU. PERFORMED BITE AND NUMEROUS GEAR SWINGS. ALL INDICATIONS NORMAL. 2 L 7 2 4F RT A1NM 2007062900088 20070629 00088 NM 2007 6 29 DLM88070750 1 20070619 A 5330 593666751 SKIN DOUG MD88 MD88 3023688 NM BS 1193 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 TWO SKIN DENTS AT FS 1193 BETWEEN L-29L AND L-30. REPAIRED WITH AN INTERNAL FINGER DOUBLER AND EXTERNAL SKIN DOUBLER. DTA RESTRICTION OF 8000 CYCLE INSPECTION INTERVALS APPLIES TO THIS REPAIR. 2 L 7 2 4F RT A6WE 2007062900089 20070629 00089 NE 2007 6 29 DL76L070751 2 20070619 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 MAKING METAL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 196DN 42935 9808 727738 28453 727738 METAL ON MASTER CHIP DETECTOR. REPLACED ENGINE PER ROUTINE TRANSMITTAL, RC CARDS 28-30. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062900095 20070629 00095 NM 2007 6 29 DLM88070757 1 20070201 A 5311 9923405504 FRAME DOUG MD88 MD88 3023688 NM FS 864 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 938DL 49811 DURING HMV-3 A CRACK WAS FOUND IN THE FS 864 RT OVERWING FRAME JUST BELOW THE FLOOR LINE. A NEW FRAME WAS INSTALLED PER S/B MD80-53A301. 2 L 7 2 4F RT A6WE 2007062900096 20070629 00096 NM 2007 6 29 DLM88070758 1 20070221 A 5311 9923405503 FRAME DOUG MD88 MD88 3023688 NM FS 886 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 939DL 49812 DURING HMV-3 A CRACK WAS FOUND IN THE FS 886 LT OVERWING FRAME JUST BELOW THE FLOORLINE. FURTHER INSPECTION REVEALED A CRACK IN THE ADJACENT FRAME AT FS 864 LT. TWO NEW FRAMES WERE INSTALLED PER S/B MD80-53A301. 2 L 7 2 4F RT A6WE 2007062900097 20070629 00097 NM 2007 6 29 DLM90070760 1 20070603 A 5530 3912078504 ATTACH FITTING DOUG MD900 MD900 3027375 NM VERTICAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 RT I/B VERTICAL STAB TO HORIZONTAL ATTACH PLATE HAS CORROSION ON PLATE FACE AND BORE. REPAIRED RT I/B VERTICAL STAB TO HORIZONTAL HINGE IAW MD90 SRM 55-30-05 PAR 5. 1 G 7 2 3U NC H19NM 2007062900103 20070629 00103 NM 2007 6 29 DL76S070770 1 20070621 A 5315 BAC1507100682 FLOORBEAM BOEING 767 767332 1382001 NM BS 1219 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 FOUND AFT CARGO FLOOR PLANEL SUPPORT RIB AT STA 1219 LBL 40 CORROSION. REPAIRED PER 53-00-07 REPAIR 4 FIGURE 201 ON AJN 50830. 2 L 7 2 4F RT A1NM 2007062900105 20070629 00105 NM 2007 6 29 DL76S070772 1 20070621 A 5315 BAC1509100682 FLOORBEAM BOEING 767 767332 1382001 NM BS 1197 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 AFT CARGO FLOOR PANEL SUPPORT RIB AT STA 1197+66 LBL 38 SIGN OF CORROSION. REPAIRED PER 53-00-07 FIGURE 201 REPAIR 4 ON AJN 51016. 2 L 7 2 4F RT A1NM 2007062900107 20070629 00107 2007 6 29 07FDEA02246 4 20070621 A 3424 H321AKM1 INDICATOR BOEING 727 727227 1384078 NM COCKPIT FAILED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 491FE 21529 DURING CLIMB-OUT STBY ATT IND 5 MORE NOSE UP THAN CAT/FO ADI'S SHORTLY THERE AFTER STBY ATT IND RAPID PRECESSION TO -25 WITH INAPPRECIATE BANK INDICATIONS. FOR TROUBLESHOOTING RECAGED TWICE RESET BREAKER. PROBLEM REOCCURRED. REPLACED STA NDBY ARTIFICIAL HORIZON PER 727 AMM 34-25 -011-4. CHECKS NORMAL. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MF G H321AKM1, POS ONL SRL 8236, TAG 78861B ON MFG H321AKM1, SRL 7030 TAG 126A10. 2 L 7 3 4F A3WE 2007062900109 20070629 00109 WP 2007 6 29 07FDEA02247 1 20070621 A 5320 ANGLE DOUG MD10 MD1010F 3022112 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 UPON REMOVAL OF LOWER TORQUE BOX WEB FOR SKIN REPLACEMENT ON N/R N00337, FOUND INNER CHORD ANGLE ADA0055-7 DENTED AT S TA 886 JUST ABOVE L41 RIGHT. [07-17-07] REPAIRED PER EA 8-5310-112940. 2 L 7 3 4F RT A22WE 2007062900111 20070629 00111 WP 2007 6 29 07FDEA02249 1 20070621 A 5313 LONGERON DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CLG WHEEL WELL CAVITY, CORROSION ON LONGERON 51R STA 1441 TO 1501. [07-13-07] FOUND TO BE WITHIN LIMITS IAW MD10-10 S RM 53-00- 01 VOL 1 , ORIGINAL THICKNESS 0.150, MATERIAL LOSS 0.010, REMAINING MATERIAL 0.140. SAT 1481 - 1521 FOUND T O BE OUT OF LIMITS IAW MD10-10 SRM 53-00-01 VOL1, MATERIAL LOSS 0.045, REMAINING MATERIAL 0.105. FABRICATED LONGERON SECTION IAW DAC DWG A4B7013 REV AC, FABRICATED REPAIR SPLICE IAW MD10-10 SRM 50-00-01 FIG 9, VOL 1. INSTALLED REPAIR IAW MD 10-10 SRM 51-35-01 VOL 2. 2 L 7 3 4F RT A22WE 2007062900112 20070629 00112 WP 2007 6 29 07FDEA02250 1 20070621 A 5313 LONGERON DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CORROSION ON LONGERON 52 STA 1461 TO 1501,CLG WHEEL WELL CAVITY. [07-13-07] FOUND TO BE OUT OF LIMITS IAW MD10-10 SRM 51-33-01 VOL 2. FABRICATED NEW LONG SECTION IAW DAC DWG A4B7013 REV AC, AND REPAIR SPLICES IAW MD10-10 SRM 53-00-01 FIG 9, VOL 1. REMOVED AND REPLACED CORRODED LONGERON SECTION WITH NEW SECTION AND SPLICES IAW MD10-10 SRM 51-33-01 VOL 2. 2 L 7 3 4F RT A22WE 2007070200003 20070702 00003 NM 2007 7 2 07FDEA02251 1 20070621 A 5320 69445593 FLOOR SUPPORT BOEING 727 727233 138408A NM BS 970 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT PIT STR CLIP FLOOR SUPPORT ANGLE CORRODED STR 29L, STA 970 REMOVED FLOOR SUPPORT, ORDERED NEW FLOOR SUPPORT, FABRICA TED SHIM AND DRILLED UP NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT AND SHIM REF SRM 51-30-2 PG 3, 5-7, SRM 51-10-2 PG 1 , SRM 51-20-1 FIG 10. 2 L 7 3 4F RT A3WE 2007070200007 20070702 00007 NM 2007 7 2 07FDEA02256 1 20070622 A 5310 DOOR FRAME BOEING 727 727233 138408A NM ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 HIDDEN DAMAGE INSPECTION LT AFT SERVICE DOOR, 2ND FRAME, 4" FROM FWD EDGE UPPER SURFACE OF LOWER SHEAR TIE IS CORRODED. THIS SDR IS A DUPLICATE OF SDR NR 07-2257 AND INADVERTENTLY ENTERED IN ERROR. SDR SUBMITTED IN ERROR- ADMINISTRATOR. 2 L 7 3 4F RT A3WE 2007070200009 20070702 00009 NM 2007 7 2 07FDEA02258 1 20070622 A 5310 DOOR FRAME BOEING 727 727233 138408A NM ZONE 800 NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FOUND ON HIDDEN INSPECTION LT AFT SERVICE DOOR, 3RD FRAME, 9" FROM FWD EDGE, LOWER SHEAR TIE, LOWER SURFACE IS CORRODED. [07-26-07] BLENDED OUT DAMAGE, ORIGINAL MATERIAL IS .045", MATERIAL LOSS OF .001, REMAINING MATERIAL IS .044" T OOL USED IN17-0458 CAL DATE 4-24-08 WITHIN LIMITS REF SRM 52-00-02 TREATED AND PRIMED SRM 51-10-2 ' 2 L 7 3 4F RT A3WE 2007070200014 20070702 00014 NM 2007 7 2 AWXA200700760 1 20070529 A 5320 143N835817 INTERCOSTAL BOEING 757 757225 1384959 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 MCN - MAJOR REPAIR - CRACKED L-2 DOOR CUT OUT INTERCOSTAL WEB, BS 660, S11L AT THE NR 3 DOOR STOP. REPLACED L-2 DOOR CU T OUT INTERCOSTAL WEB, BS 660, S11L AT THE NR 3 DOOR STOP IAW AWA TASK CARD M1C53604. 2 L 7 2 4F RT A2NM 2007070200017 20070702 00017 NM 2007 7 2 AWXA200700763 1 20070501 A 5330 654576987 SKIN BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - C-20 CHECK - FOUND CRACKED FUSELAGE SKIN, BS 379 - BS 402, S28L - S28R. REPAIRED FUSELAGE SKIN, B S 379 - BS 402, S28L - S28R IAW AWA ER 03-5330-07170-SS3. 2 L 7 2 4F RT A16WE 2007070200018 20070702 00018 NM 2007 7 2 AWXA200700764 1 20070504 A 5311 6547959 FRAME BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - AFT CARGO COMPARTMENT DOOR CUT FORWARD FRAME CRACKED, BS 793.4, S24R. REPAIRED AFT CARGO COMPARTME NT DOOR CUT FORWARD FRAME, BS 793.4, S24R IAW AWA ER 03-5362-07163-SS1. 2 L 7 2 4F RT A16WE 2007070200020 20070702 00020 EU 2007 7 2 F3LA200700136 1 20070609 A 5320 D5311282600101 DUMMY RAIL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 907FR 5061 1743 DURING C4/S1 CHECK, INSPECTION REPORTED HEAVY CORROSION ON TOP FLANGE OF DUMMY RAIL AT Y81, BETWEEN FR12 AND FR14. REPL ACED DUMMY RAIL IAW SRM 51-42-11, PARA. 8, AND SRM 51-41-11, PARA 3. 2 L 7 2 4F RT A28NM 2007070200022 20070702 00022 2007 7 2 F3LA200700139 4 20070610 A 2565 GIRT BAR AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 907FR 5061 1743 DURING C4/S1 CHECK, INSPECTION REPORTED LIGHT CORROSION ON L2 DOOR GIRT BAR FITTING AFT OF C66, JUST FWD AND INBD OF SCR EW HOLE. FOUND L2 DOOR SILL TO BE OUT OF LIMITS IAW SRM 53-41-14, FIG 101. REPLACED L2 DOOR SILL IAW SRM'S 51-42-11, 5 1-44-11, 51-41-11 AND EA NR A0-51T-11976. 2 L 7 2 4F RT A28NM 2007070200025 20070702 00025 EU 2007 7 2 F3LA200700141 1 20070614 A 5321 FLOORBOARD AIRBUS A319 A319112 3930323 EU FUSELAGE DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 907FR 5061 1743 DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBOARD 231EF DELAMINATED AROUND ONE OF THE FWD SCREW HOLES. REPAIRED DAMAGE TO TOP SKIN OF FLOORBOARD 231EF IAW EA NR A9-53R-11965. 2 L 7 2 4F RT A28NM 2007070200026 20070702 00026 EU 2007 7 2 F3LA200700142 1 20070623 A 5340 ATTACH ANGLE AIRBUS A319 A319112 3930323 EU FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 907FR 5061 1743 DURING C4/S1 CHECK, INSPECTION REPORTED ANGLE AT FR67 JUST BELOW L2 DOOR SILL WHICH ATTACHES DOOR SILL TO FRAME WAS FOUN D DAMAGED. 2 L 7 2 4F RT A28NM 2007070200028 20070702 00028 NM 2007 7 2 07FDEA02255 1 20070622 A 3233 651781212 ACTUATOR BOEING 727 727227 1384078 NM NLG FAILED A FDEA O OTHER O OTHER LD LANDING 1 SO 25 479FE 9974 9974 21461 UPON LOWERING LANDING GEAR HANDLE, NOSE GEAR DID NOT COME DOWN INITIALLY WITH RED NOSE GEAR LIGHT AND NO NOSE GEAR DOOR LIGHT ON FE'S ANNUNCIATOR PANEL. AFTER APPROX 20 SECONDS, COULD HEAR NOSE GEAR DOORS OPEN AND NOSE GEAR COME DOWN AND L OCKED. LANDING GEAR HANDLE WAS STIFF WHEN LOWERING HANDLE. REMOVED AND REPLACED RETRACT ACTUATOR AND LOCK ACTUATOR. 2 L 7 3 4F A3WE 2007070200029 20070702 00029 NM 2007 7 2 07FDEA02264 1 20070623 A 5312 652555742 BULKHEAD BOEING 727 727227 1384078 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 RT LOWER FUSELAGE AFT OF RT WHEEL WELL, FUSELAGE PANEL NR 3622 IS CRACKED AT INNER I/B AREA. REMOVED CRACK ON UNDER S IDE OF PANEL NR 3622 REF SRM 51-40-9 PARAGRAPHS 4A AND4E. 2 L 7 3 4F A3WE 2007070200030 20070702 00030 NM 2007 7 2 07FDEA02265 1 20070623 A 5322 651593920 SHEAR TIE BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD PIT BILGE BODY FRAME, SHEAR TIE, IS CORRODED, BS 720, STR 27L-28L, WL 148. LEVEL 1 CORROSION. REMOVED CORROSION , TREATED AND PRIMED REF SRM 51-10-6 AND 51-10-2. ORIGINAL THICKNESS .050". REMAINING .047" MATERIAL LOSS IS .003" WITH IN LIMITS REF SRM 53-10-1 NR TOOL NR 18172 CAL. 2 L 7 3 4F RT A3WE 2007070200031 20070702 00031 NM 2007 7 2 07FDEA02266 1 20070625 A 5710 DUCT DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 LEFT WING ANTI-ICE TELESCOPING DUCT CUT OUT CORNER FOUND CRACKED. [07-13-07] REPAIR CARRIED OUT AT LEFT HAND WING ANTI ICE TELESCOPING DUCT CUT OUT CORNER AS PER FEDEX EA 1-5710-111133, REPAIR CLASSIFIED AS MIN0R AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007070200032 20070702 00032 NM 2007 7 2 07FDEA02267 1 20070625 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 LANDING GEAR, NOSE GEAR LT TRUNNION FITTING FOUND CRACKED. [07-06-07] REPAIR CARRIED OUT AT NOSE LANDING GEAR LT TRUNN ION FITTING AS PER SRM 53- 40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007070200037 20070702 00037 NM 2007 7 2 07FDEA02272 1 20070625 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 575FE 48500 CENTER CARGO AT STA 5-123 LONGERON 47R FOUND 1EA LOCK FASTENER HOLE CRACKED. [07-09-07] REMOVED SPLICE AT STA 5-123 ST R 47R AS PER SRM 51-33-01 VOLUME II AND HFEC INSPECTION CARRIED OUT PER NDT SPM 06-10-01.001 REV 13 FOUND NO CRACK E VIDENT. INSTALLED EXISTING SPLICE AT CENTER CARGO AT 5-123 STR 47R AREA AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFI ED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007070200038 20070702 00038 NM 2007 7 2 DHL2007783522 1 20070620 A 5531 7075T6 SUPPORT ANGLE BOEING 727 727227 1384078 NM VERTICAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 VERTICAL STAB INTERNAL WEB LT UPPER ANGLE IS CRACKED STA 1323, SHORT WEB ANGLE W/L 259. REMOVED DAMAGED ANGLE VERITCAL STAB INTERIOR WEB IAW B727 SRM 51-30-2, FIG 7. VERIFIED MATERIAL TO BE 7075T6 IAW HARDNESS TESTER B727 SRM 51-10-3, FIG 2. FABRICATED NEW ANGLE MATERIAL 7075T6, .071, BY 7 BY 5 IAW B727 SRM 51-10-2. TREATED, PRIMED AND INSTALLED NEW ANGL E IAW B727 SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 2007070200039 20070702 00039 NM 2007 7 2 DHL2007783524 1 20070621 A 5320 7075T6 INTERCOSTAL BOEING 727 727227 1384078 NM CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 ASTAR N/R 062541: FWD CARGO COMPARTMENT STA 580 THRU 600, INTERCOSTAL AT STR 29L HAS CORROSION ON LWR INBD SIDE. REMOVE D INTERCOSTAL AT SRT 29L BETWEEN STA 580-600 IAW B727 SRM 53-10-1. FABRICATED NEW INTERCOSTAL FROM 7075-T6, .032, DIM 19 .5 BY 19.5 IAW B727 SRM 51-20-1, MATERIAL ID IAW B727 SRM 53-10-2. TREATED, PRIMED AND INSTALLED INTERCOSTAL IAW B727 SR M 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 2007070200042 20070702 00042 SO 2007 7 2 CHQA200700030 1 20070622 A 2752 3632001003 DRIVE UNIT EMB 135 EMB135KL 3260302 SO TE FLAPS INOPERATIVE A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 297SK 15914 15914 145522 FLIGHT 5349 - ORF-STL - DURING CLIMB, AFTER SELECTING FLAPS UP, EICAS MESSAGES "FLAP FAIL" AND "SPS ADV" APPEARED. FO L OOKED AT FLAPS AND SAW '9' ON BOTH SIDES. RAN THE QRH, DIVERTED TO RIC. CALLED FOR EMERGENCY EQUIPMENT TO BE ON STANDB Y AS PRECAUTION. THE LANDING AND TAXI WERE UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED THE FLAP POWER DRIVE UNIT. 2 L 7 2 4F RT T00011AT 2007070200045 20070702 00045 NM 2007 7 2 HALA0700262 1 20070620 A 3411 0856LU6 PITOT SYSTEM BOEING 767 76733A 1385209 NM MALFUNCTIONED A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 593HA 33424 ETOPS SIGNIFICANT SYSTEM - BTB: FO'S PITOT HEAT EICAS MESSAGE AFTER ENGINE START. T/S PER FIM 30-31-01-05 IDENTIFIED F/ OS PITOT STATIC PROB B28 INOP. REMOVED AND REPLACED PER AMM 34-11-01. PERFORMED PITOT STATIC PROBE TEST PER AMM TASK 3 4-11-01-725-001. LK TEST OF F/O PITOT STATIC PROBE CHECKED PASSED. 2 L 7 2 4F RT A1NM 2007070200050 20070702 00050 NM 2007 7 2 AWXA200700768 1 20070417 A 5330 65C384501 SKIN BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - CRACKED FUSELAGE SKIN, BS 360 - BS 540, S4L. REPAIRED FUSELAGE SKIN, BS 360 - BS 540, S4L IAW AWA ER 03-5330-07173-HC1. 2 L 7 2 4F RT A16WE 2007070200051 20070702 00051 NM 2007 7 2 AWXA200700769 1 20070417 A 5330 65C384502 SKIN BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - CRACKED FUSELAGE SKIN, BS 360 - BS 540, S4R. REPAIRED FUSELAGE SKIN, BS 360 - BS 540, S4R IAW AWA ER 03-5330-07173-HC1. 2 L 7 2 4F RT A16WE 2007070200056 20070702 00056 NM 2007 7 2 NWAA072233114 1 20070623 A 3350 NWAD321430 BATTERY PACK AIRBUS A319 A319114 3930350 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 314NB 1191 EMERGENCY ESCAPE LIGHTING SYSTEM CHECK FOUND EPSU INT LOAD LIGHT DISPLAYED. REPLACED EMERGENCY LIGHT BATTERY PACK 32-33 00-4-0074, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 2007070200062 20070702 00062 NM 2007 7 2 07FDEA02278 1 20070626 A 5330 65545839 SKIN BOEING 727 727233 138408A NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 286FE 22623 ON AGING A/C INSP, FOUND EXTERNAL REPAIR LOCATED AT BS 1120 TO 1130, STR S-18L TO S-19L, DID NOT CONFORM TO SRM 53-30-1. REMOVED EXISTING DOUBLER PER SRM 51-30-2. BLENDED OUT DAMAGE, EXTENDED CUT OUT TO REMOVE FASTENER HOLES WITH NO EDGE DISTANCE, REF 53-30-3 PG 5. FABRICATED DOUBLER TREATED AND PRIMED, AND INSTALLED DOUBLER REF MM 51-20-31-7 AND MM 51-20 -21-7. 2 L 7 3 4F RT A3WE 2007070200065 20070702 00065 EU 2007 7 2 07FDEA02281 1 20070626 A 5711 A57110436 SPAR AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 DAMAGED HOLES (CRACKS IN HOLE 1, 2, 3, 4, 5, 6, 8) ON C44 CENTER SPAR WEB REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL CRACKS ARE REMOVED IAW EA 6-5710-103327 AND RAS 046993/014/2006 ISS A. 2 L 7 2 4F RT A35EU 2007070200066 20070702 00066 WP 2007 7 2 07FDEA02282 1 20070626 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CLG WHEEL WELL CAVITY, CORROSION ON LONGERON END FITTING AT STA 1501 TO 1521, LONGERON 49L. [07-13-07] REMOVED LON GERON 49L END FITTING IAW DC/MD10-10 SRM 51-33-01 VOL 2. REMOVED CORROSION IAW SRM 51-21-01 VOL 2. ORIG THICKNESS 0.130" , MATERIAL LOSS 0.007", REMAINING THICKNESS 0.123", FOUND TO BE WITHIN LIMITS IAW SRM 53-00- 01 FIG 1B, VOL 1 AND SRM 51-21-01 VOL 2. REINSTALLED LONGERON 49L END FITTING IAW SRM 51-33-01 VOL 2. 2 L 7 3 4F RT A22WE 2007070200067 20070702 00067 NM 2007 7 2 07FDEA02283 1 20070626 A 5322 69436833 SHEAR TIE BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD PIT BILGE, BODY FRAME SHEAR TIE, IS BUCKLED/CRACKED BS 720B, STR 25L - 26L, WL 152. REPLACED DAMAGED SHEAR TIE A T FWD PIT STA 720B, BETWEEN STR 25L AND 26L, REF SRM 51-30-2 PG 1-12. 2 L 7 3 4F RT A3WE 2007070200069 20070702 00069 WP 2007 7 2 07FDEA02285 1 20070626 A 5312 BULKHEAD DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CLG - WHEEL WELL CAVITY,CORROSION ON BULKHEAD LOWER CIRCUMFERENCIAL ANGLE AT STA 152, LONGERON 50R TO 49R. [07-17-07] REMOVED,FABRICATED AND INSTALLED 4 EACH END FITTINGS 49R TO 50R IAW SRM 51-33-01 VOL II AND 51-35-01 VOL II PAGE 1. 2 L 7 3 4F RT A22WE 2007070200070 20070702 00070 WP 2007 7 2 07FDEA02286 1 20070626 A 5312 BULKHEAD DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CLG WHEEL WELL CAVITY CORROSION ON CIRCUMFERENTIAL ANGLE AT FWD OF STA 1521, BETWEEN LONGERON 51L AND 52. [07-17-07] REMOVED,FABRICATED AND INSTALLED IAW SRM 51-33-01. 2 L 7 3 4F RT A22WE 2007070200071 20070702 00071 NM 2007 7 2 HALA0700266 1 20070618 A 3233 59713305001 ACTUATOR BOEING 717 717200 1383700 NM MLG DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 486HA 8170 8170 55131 LEFT MAIN GEAR RETRACT ACTUATOR PISTON HAS CHROME CHIPPING OFF AT THE LOWER END WHERE SEAL CONTACTS PISTON WHEN GEAR IS RETRACTED. REMOVED AND REPLACED ACTUATOR PER MM 32-33-01. 2 L 7 2 4F TR A6WE 2007070200072 20070702 00072 NM 2007 7 2 HALA0700265 1 20070626 A 3150 UNKNOWN BOEING 767 7673CB 1385187 NM UNKNOWN A HALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 13 592HA 33468 ETOPS SIGNIFICANT SYSTEM, STATUS ALERT ON FINAL EICAS STATUS ALERT "R IDG VALVE" DISPLAYED. RUN BITE OF BPCU PER FIM 24 -20-00 TABLE 102, NO FAULTS MSG CLEARED. 2 L 7 2 4F RT A1NM 2007070200073 20070702 00073 EU 2007 7 2 SIMA200717703 1 20070622 A 3150 UNKNOWN SAAB SF340 340B 7860101 EU UNKNOWN A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 394AE 340B394 TAIL PIPE HOT LIGHT ILLUMINATED, ABORTED TAKEOFF. PERFORMED OPERATIONAL TEST OF THE RIGHT ENGINE NACELLE FIRE DETECTION SYSTEM IAW SAAB AMM 26-11-00 AND AMERICAN EAGLE WORK CARD G1-26AD-017R1 WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SE RVICE. 2 L 7 2 4T RT A52EU 2007070200078 20070702 00078 SO 2007 7 2 SIMA200717701 1 20070621 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 935AE 14500920 WITH APU BLEEDS TO PACKS A STRONG ODOR FILLED THE FLIGHT DECK. AFTER DESELECTING BLEEDS TO BOTH PACKS ODOR BECOMES STRO NGER, DISSIPATED BY 15,000 FEET. FOUND APU INLET FILLED WITH LOCUST. REMOVED LOCUST FROM INLET AND PERFORMED OPERATION AL CHECK OF APU, ENGINE BLEED SYSTEMS WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007070200080 20070702 00080 NM 2007 7 2 ASAA0791810 1 20070531 A 5347 146A750611 CARGO TRACK BOEING 737 737990 NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT RAIL SPLICE CORRODED. REPAIRED IAW SRM 51-40-02 AND 51-40-03. 2 L 7 4 4F RT A16WE 2007070200084 20070702 00084 NM 2007 7 2 ASAA0741814 1 20070622 A 5753 FLAP TRACK BOEING 737 7374Q8 138447Q NM NR 4 FLAP WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 NR 4 FLAP TRACK SIDE LOAD LINK LOOSE. REMOVED AND REPLACED NR 4 FLAP TRACK SIDE LOAD LINK IAW AMM 27-51-27 STEP 5D (2) (B) PG 411 AND AMM 20-50-11. 2 L 7 2 4F RT A16WE 2007070200085 20070702 00085 2007 7 2 ASAA0741815 4 20070622 A 2565 65C261966 GIRT BAR BOEING 737 7374Q8 138447Q NM L2 DOOR SLIDE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 L2 DOOR SLIDE GIRT BAR CORRODED AND PITTED. REMOVED FROM SLEEVE PER TC 45125011. REMOVED AND REPLACED L2 DOOR SLIDE GI RT BAR PER CMM 25-66-07 PG 664 STEPS 14 (A, B, C AND D). 2 L 7 2 4F RT A16WE 2007070200090 20070702 00090 NM 2007 7 2 2007UALA02117 1 20070619 A 3397 CONNECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 EMERGENCY EXIT LIGHTING NOT LIT FROM ROW 15 TO BACK. *S/D* SECURED PLUG FROM SIDEWALL FEEDER TO FLOOR STRIP, OPS CHECK ED GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007070200091 20070702 00091 NM 2007 7 2 2007UALA02118 1 20070620 A 5520 ROD END AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE ELEVATOR DAMAGED A UALA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 819UA 893 VIBRATION - NOISE ENCOUNTERED IN FLIGHT. STRONG VIBRATION FROM TAIL, FELT ALL LOCATIONS. STOPPED WHEN SLOWED BELOW 280 KIAS. FOUND MULTIPLE POSSIBLE ISSUES, LEADING EDGE TAPE WAS PEELING AND BUNCHING UP ON THE LE OF VERT STAB AND ELEV/R UD FREEPLAY CHECKS FAILED- WORN SERVO ROD ENDS. RETAPED POLY TAPE ON VERT STAB AND PERFORMED ELEV BLUE AND YELLOW SYST EM ROD END REPLACEMENT- ALSO REPLACED RUDDER HINGE BEARING PLATES AT POS 1 THRU 5 AND 7 AT HMV/SSR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007070200092 20070702 00092 NM 2007 7 2 2007UALA02119 1 20070620 A 5520 BEARING AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE ELEVATOR WORN A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 812UA 850 VIBRATION FELT DURING CLIMB & DESCENT. FOUND FREEPLAY IN ELEVATOR SYSTEM. REPLACED ELEVATOR HINGE BEARINGS PLATES POS 1-6 AT HMV-SSR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007070200095 20070702 00095 NM 2007 7 2 2007UALA02122 1 20070620 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 470 S14R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 EXTERNAL FUSELAGE SKIN CRACKED BS 470 STR 14R. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SECTION. INSTALLED DOUBLER/ FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007070200097 20070702 00097 NM 2007 7 2 2007UALA02124 1 20070620 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1198 S17L CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 MAIN CABIN STRINGER 17L HAS CORROSION AT BS 1198. MAJOR REPAIR ACCOMPLISHED: REMOVED STRINGER AND FABRICATED & INSTALL ED A NEW -3 CHORD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007070200100 20070702 00100 NM 2007 7 2 2007UALA02127 1 20070620 A 2612 MODULE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 2 FIRE DETECT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 NR 2 ENGINE FIRE LIGHT DOES NOT ILLUMINATE DURING FIRE TEST. [07-13-07] REPLACED FIRE DETECTION CONTROL MODULE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007070200102 20070702 00102 NM 2007 7 2 2007UALA02129 1 20070620 A 8011 SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE STARTER DRIVE LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 533UA 25073 NR 1 ENGINE HIGH OIL CONSUMPTION EXCEEDS LIMITS. [08-07-07] REPLACED NR 1 ENG STARTER DRIVE SEAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007070200104 20070702 00104 NM 2007 7 2 2007UALA02131 1 20070619 A 3350 58781 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FLOOR AT 7C UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 EMERGENCY EXIT LIGHT STRIP COMING UP OFF FLOOR AT 7C. SECURED STRIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007070200106 20070702 00106 NM 2007 7 2 2007UALA02133 1 20070619 A 3350 58781 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 330UA 24191 EMERGENCY LIGHT STRIP COMING UP AT 6C. RESECURED LIGHT STRIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007070200109 20070702 00109 NM 2007 7 2 2007UALA02137 1 20070620 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 195UA 26899 WALL EEL INOP BETWEEN MID LAVS. RESECURED CONNECTOR. CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007070200110 20070702 00110 NM 2007 7 2 2007UALA02138 1 20070620 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE DOOR 2 RH SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EMERGENCY LIGHT INOP, DOOR 2 RIGHT SLIDE ILLUM. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007070200123 20070702 00123 NM 2007 7 2 2007UALA02153 1 20070620 A 2721 CONTROL PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RUDDER TRIM MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 578UA 26694 RUDDER TRIM INTERMITTENT TWICE DURING FLIGHT. WORKED AFTER SEVERAL SHORT RE-ATTEMPTS. [08-07-07] REMOVED AND RE PLACED RUDDER TRIM ACTUATOR AND RUDDER TRIM CONTROL PANEL 2 L 7 2 4F 4 F RT A2NM E17NE 2007070200128 20070702 00128 NM 2007 7 2 ZZDA070621179 1 20070621 A 3220 PIN BOEING 737 7377BD 1384511 NM NLG INSTALLED A ZZDA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SO 15 290AT 33925 NOSE GEAR WILL NOT RETRACT. FOUND NOSE GEAR LOCKOUT PIN INSTALLED. REMOVED NOSE GEAR LOCKOUT PIN, OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2007070200131 20070702 00131 NM 2007 7 2 SWAA073082 1 20070619 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 251WN 32510 EEPLS COVER LOOSE AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007070200138 20070702 00138 NM 2007 7 2 SWAA073110 1 20070621 A 5311 6546525 FRAME BOEING 737 7375H4 138449D NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007070200141 20070702 00141 NM 2007 7 2 SWAA073113 1 20070621 A 5311 6546540 FRAME BOEING 737 7373H4 1384600 NM BS 639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 18L. REPAIRED FRAME PER EA. 2 L 7 2 4F RT A16WE 2007070200142 20070702 00142 NM 2007 7 2 SWAA073105 1 20070621 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM BS 747 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 747, STR 27R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007070200143 20070702 00143 NM 2007 7 2 SWAA073106 1 20070621 A 5311 6546549 FRAME BOEING 737 7373H4 1384600 NM BS 767 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, STR 27R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007070200150 20070702 00150 NM 2007 7 2 SWAA073101 1 20070621 A 5523 65C2638416M TAB BOEING 737 7373H4 1384600 NM RT ELEVATOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND RT ELEVATOR TAB CRACKED AT LOWER HINGE CUTOUT. REMOVED AND REPLACED ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2007070200151 20070702 00151 NM 2007 7 2 SWAA073092 1 20070621 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM L1 DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 724SW 27856 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007070200155 20070702 00155 NM 2007 7 2 SWAA073085 1 20070621 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 360 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 360, STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007070200162 20070702 00162 NM 2007 7 2 SWAA073089 1 20070621 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 412WN 29818 DURING SCHEDULED HC1 CHECK, LT MID CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007070200164 20070702 00164 NM 2007 7 2 USAA070481 1 20070622 A 5322 SHEAR TIE BOEING 737 737401 1384701 NM BS 1040 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 STA 1040 BETWEEN S2L AND S3L HAS CRACK. FABRICATED SHEAR TIE, HEAT TREATED & INSTALLED PER SRM 51-40-02, 51-20-01, DEFE CT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007070200166 20070702 00166 NM 2007 7 2 USAA070479 1 20070622 A 5311 FRAME BOEING 737 737401 1384701 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 BS 440 FWD CARGO DOOR FWD FRAME WL 180 HAS CRACK. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER SRM 51-10-02 & DWG 65-207 22, DEFECT SIZE: .125 INCH. 2 L 7 2 4F RT A16WE 2007070200169 20070702 00169 NM 2007 7 2 USAA070476 1 20070622 A 5313 STRINGER BOEING 737 737401 1384701 NM BS 295 S10L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 BS 295 S-10L HAS CRACK. FABRICATED STRINGER REPAIR PER SRM 51-70-11, DEFECT SIZE: .250 INCH. 2 L 7 2 4F RT A16WE 2007070200172 20070702 00172 NM 2007 7 2 USAA070473 1 20070622 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM BS 312 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 BL 0 FASTENER HOLE AT ATTACH POINT TO BS 312 FLOORBEAM UPPER CHORD HAS CRACK. FAB'D & INSTALLED NEW REPAIR ANGLE PER SR M 51-70-13, DEFECT SIZE: .500 INCH. 2 L 7 2 4F RT A16WE 2007070200176 20070702 00176 NM 2007 7 2 ASAA0741818 1 20070622 A 5730 654645528 SKIN BOEING 737 7374Q8 138447Q NM DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 RT AILERON CONTROL TAB HAS DELAM DAMAGE AT TRAILING EDGE I/B CORNER. REPAIRED RT AILERON TAB IAW SRM 51-70-16 PG 12 REP AIR 1. 2 L 7 2 4F RT A16WE 2007070200179 20070702 00179 NM 2007 7 2 HNAA0700099 1 20070601 A 2933 3810047106 INDICATOR DHAV DHC8 DHC8102 2809003 NM HYD QTY MALFUNCTIONED A HNAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 07 846EX 326 DURING NR 2 HYD SYS SERVICE BOTH INDICATORS MOVED TO .5 QT AND STOPPED WHILE SYS CONTINUED TO ACCEPT APPROX 3.5 QTS OF F LUID UNTIL SPILLED INTO OVER SPILL CANISTER. FERRY TO MDT. DURING TAXI OUT CREW REPORTED QTY GAUGE CORRECTED AFTER OPS OF FLT CONTROL SYS AND FOR THE DURATION OF FLT. GND RAN ACFT AND OPERATED VARIOUS FLT CONTROL SYSTEMS. BLED NR 2 HYD SYS AND CLEANED C/P AT QTY IND IN NACELLE. OPS GOOD. 2 H 7 2 4T RT A13NM 2007070200180 20070702 00180 NM 2007 7 2 HNAA0700080 1 20070421 A 5610 17180003 WINDSCREEN DHAV DHC8 DHC8102 2809003 NM COCKPIT CRACKED A HNAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 07 809EX 17059 17059 302 AIRCRAFT DEPARTED DCA, ON CLIMBOUT, THE CREW HEARD A CRACKING NOISE COMING FROM THE CAPTAIN'S SIDE WINDSHIELD. LEVELED OFF AT 5000 FT AND THE NOISE WENT AWAY. CAPTAIN MADE AN INSPECTION OF WINDSHIELD AND FOUND LIKE WINDOW IS CRACKING. THE CAPTAIN DIVERTED TO BWI. MAINTENANCE INSPECTED WINDOW AND FOUND NO CRACKS. NO DEFECTS FOUND. CAPTAINS SIDE WINDOW RE PLACED 4/22/07 AS A PRECAUTION. 2 H 7 2 4T RT A13NM 2007070200181 20070702 00181 NM 2007 7 2 HNAA0700118 1 20070501 A 2760 82740124001 ROD DHAV DHC8 DHC8102 2809003 NM LT WING CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 937HA 148 ON LEFT HAND WING, CORROSION ON I/B AND O/B ROLL SPOILER ACTUATOR CONNECTING RODS. REMOVED AND REPLACED I/B AND O/B CON NECTING RODS FOR ROLL SPOILER ACTUATOR. 2 H 7 2 4T RT A13NM 2007070200183 20070702 00183 EA 2007 7 2 HNAA0700120 1 20070620 A 2910 AE2460501E0180 FLEX LINE DHAV DHC8 DHC8311 1386006 EA HYD SYSTEM LEAKING A HNAA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 EA 07 327EN 261 NR 1 HYD QTY DROPPED TO 1.3, SYSTEM WENT INTO ISO, PRESSURE REMAINED GOOD AND FLUID DRIPPING FROM NR 2 NACELLE. INSTALL ED TFL AT RT WING I/B SPOILER ACTUATOR ON REAR SPAR. REF MP&P VOL 2 20.1. LEAK CHECK GOOD. SERVICE HYD SYSTEM. 2 H 7 2 4T RT A13NM 2007070200189 20070702 00189 NE 2007 7 2 ABXA070185 2 20070620 A 7200 CF680A ENGINE BOEING 767 767281 1385109 NM GE CF6 CF680A 30025 NE NR 1 DEFECTIVE A ABXA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 23 791AX 2793 23141 580237 LEFT ENGINE HAD LOUD BANG, LOTS OF YAW AND THE ODOR OF SMOKE. EGT REACHED 1100 AFTER SHUTDOWN, HAPPENED AT 14000FT, AIR TURNBACK TO ILN. REMOVED AND REPLACED NR 1 ENGINE IAW JOB CARD 7010, WORKPACK WO 600274113, L/P 034277-13/1. 2 L 7 2 4F 4 F RT A1NM E13NE 2007070200195 20070702 00195 SO 2007 7 2 RAIA00706032 1 20070620 A 3350 CONNECTOR EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHTS LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 826HK 145016 PRE FLT NR 5559 - STL - EMERGENCY LIGHT IN GALLEY INTERMITTENT. MAINTENANCE RESECURED CONNECTION; SYSTEM OPS CHECK GOOD . 2 L 7 2 4F RT T00011AT 2007070300001 20070703 00001 EA 2007 7 3 A6WA200740238 1 20070510 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 455AW 7848 FS484.0 ANGLE AT RBL 36 IS CRACKED APPROX 1.0 INCH. (K) [07-17-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW BOMBAR DIER REO 601R-53-41-059 AND BSC SR 601R-53-0030A. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300004 20070703 00004 EA 2007 7 3 A6WA200740241 1 20070510 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 455AW 7848 FS 484.0 ANGLE AT LBL 27 IS CRACKED APPROX 1.0 INCH. (K) [07-17-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW BOMBA RDIER SRM 601R-53-0029B AND CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300008 20070703 00008 EA 2007 7 3 A6WA200740244 1 20070513 A 5340 601R75262157 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT MGL WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 458AW 7861 RT MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER HAT CHANNEL PN 601R75262157, IS CRACKED THRU ON IB LEGS. (K) [07-17-07] MAINTENANCE REPLACED CHANNEL IAW SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300011 20070703 00011 EA 2007 7 3 A6WA200740247 1 20070514 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 458AW 7861 FS 280 FLOORBEAM CLIP AT OB SIDE OF RBL 9.0 IS CRACKED IN RADIUS APPROX .60 INCH LONG. (K) [07-17-07] MAINTENANCE REP LACED CLIP IAW BSC EO 601R-53-0057A. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300013 20070703 00013 EA 2007 7 3 A6WA200740249 1 20070514 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 458AW 7861 FS280, FLOORBEAM CLIP AT IB SIDE OF LBL 9.0 IS CRACKED IN RADIUS APPROX. .20 INCH LONG. S/D - MAINTENANCE REPLACED CLI P IAW BSC EO 601R-53-0057A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300017 20070703 00017 EA 2007 7 3 A6WA200740253 1 20070514 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 458AW 7861 INTERCOSTAL AT FS 484.00 HAS CRACKED FLANGE AT LBL 36.0 CRACK MEASURES APPROX .20 INCH LONG. S/D MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-53-41-059. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300024 20070703 00024 SO 2007 7 3 RAIA00706036 1 20070624 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 813HK 145044 PRE FLT 5578 - STL - EMERGENCY LIGHT AT SERVICE DOOR INOPERATIVE. MAINTENANCE INSPECTED AND FOUND CONNECTION TO BE LOOS E, RESECURED THE CONNECTION AND OPS CHECKED THE LIGHTS WITH NO FURTHER DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2007070300029 20070703 00029 NM 2007 7 3 UPS07450012 1 20070606 A 5313 65B044218 STRINGER SPLICE BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C FWD CARGO COMPT STR 39L AT BS 740 SPLICE CORROSION FOUND. REMOVED (CORROSION BLEND OUT 0.029" X .5 X .75 INCH OUT OF LIMITS SRM 53-10-01 FIG 1) FWD CARGO COMPT BS 740 LT STR 39 STRINGER SPLICE, REPLACED AND INSTALLED AS P ER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007070300031 20070703 00031 NM 2007 7 3 UPS07450014 1 20070601 A 5320 WEB BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C FX LOWER FUSELAGE OF INTERIOR SUPPORT WEB FOUND CRACKED AT STA 2220 TO STA 2240 STR 42L (CRACK LENGTH 2 INCHES). FX LOWER FUSELAGE OF INTERIOR SUPPORT WEB AT STA 2220 TO STA 2240 STR 42L REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007070300033 20070703 00033 NM 2007 7 3 UPS07450015 1 20070530 A 5313 65B0765834 STRINGER BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C FWD CARGO COMPT STRINGER FOUND CRACKED AT STA 280 S41R (CRACK LENGTH .375 INCH). FWD CARGO COMPT STA 260-280 STR 41R STRINGER REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007070300034 20070703 00034 NM 2007 7 3 UPS07450016 1 20070603 A 5414 SKIN BOEING 747 747212B 1384886 NM NR 1 PYLON DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C NR 1 PYLON STRUT O/B LOWER EDGE SKIN FOUND DAMAGED AT STA 236. NR 1 PYLON STRUT O/B LOWER EDGE SKIN R EPAIRED AT STA 236 AS PER SRM 54-34-03 FIG 25. 2 L 7 4 4F A20WE 2007070300041 20070703 00041 NM 2007 7 3 UPS07450022 1 20070528 A 5311 65B0173780 DOUBLER BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C THROUGH THICKNESS CRACK FOUND AT BS 880 STR 9R TENSION TIE AT NR 10 FASTENER HOLE OF FRAME DOUBLER THE CRACK RUNNING AT UPWARD DIRECTION (CRACK LENGTH .25 INCH). M/DECK BS 880 RIGHT STR 9R FRAME ATTACH DOUBLER REPLACED AN D INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007070300042 20070703 00042 NM 2007 7 3 UPS07450023 1 20070528 A 5340 65B3860043 STRINGER CLIP BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C THROUGH THICKNESS CRACK FOUND AT BS 880 STR 9R TENSION TIE AT AFT ATTACHED TIE CLIP THE CRACK RUNNING AT UPWARD DIRECTION (CRACK LENGTH .125 INCH). M/DECK BS 880 STR 9R STRINGER ATTACH TIE CLIP REPLACED AND INSTALLED AS P ER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007070300044 20070703 00044 NM 2007 7 3 SWAA073146 1 20070623 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 619SW 28035 R2 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007070300049 20070703 00049 NM 2007 7 3 SWAA073120 1 20070622 A 5330 6545766 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 745, STR 25R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007070300052 20070703 00052 EA 2007 7 3 A6WA200740258 1 20070517 A 2751 855D10011 SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A A6WA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 31 415AW 10951 7593 FLAPS FAIL MASTER CAUTION OCCURRED 15 MINUTS AFTER DEPARTURE. QRH WAS ACCOMPLISHED. FLAPS FAILED AT ZERO DEGREES. EME RGENCY LANDING DECLARED FOR PRECAUTIONARY MEASURES. INTERROGATED FECU, FOUND L-BPSU MISRIGGED, NO EVIDENCE OF TWISTING OR ABNORMAL DEFORMATION DETECTED. NO JAMMED, DISCONNECTED OR DRAGGING COMPONENTS FOUND. REMOVED AND REPLACED L-BPSU IA W SUPP 98-018B. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300054 20070703 00054 NM 2007 7 3 SWAA073119 1 20070622 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 736D, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007070300055 20070703 00055 NE 2007 7 3 A6WA200740259 2 20070519 A 7261 CARBON SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENGINE OIL SYS LEAKING A A6WA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 31 436AW 7734 AT FL320 RT ENGINE OIL PRESSURE MASTER WARNING ILLUMINATED OIL PRESSURE INDICATED 20 PSI. COMPLIED WITH QRH WITH REDUCE D POWER SETTING, OIL PRESSURE IMPROVED TO 26 PSI MOMENTARILY, THEN LEVELED OFF TO 20 PSI. OIL TEMP NEVER EXCEEDED 115 D EGREES (C). [07-31-07] REMOVED AND REPLACED CARBON SEAL IAW EMM SP 38 LEAK CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300056 20070703 00056 NM 2007 7 3 SWAA073122 1 20070622 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740D, STR 21R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007070300059 20070703 00059 NE 2007 7 3 A6WA200740260 2 20070519 A 7261 CARBON SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SCAV PUMP LEAKING A A6WA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 31 436AW NMADB378 7734 AT FL320 RT ENGINE OIL PRESS MASTER WARNING ILLUMINATED OIL PRESS INDICATED 20 PSI. C/W QRH WIGH REDUCED POWER SETTING OIL PRESS INCREASED TO 26 PSI MOMENTARILY, THEN LEVELED OFF AT 23 PSI. OIL NEVER EXCEEDED 115 DEGREES. PERFORMED PRECA UTIONARY IFSD. REMOVED AND REPLACED NR 7 CARBON SEAL, IDG CARBON SEALS LEAKING, INSPECTED RT OIL PUMP, FOUND SCAV SCREE N 80 PERCENT CLOGGED. REMOVED AND REPLACED BB AXIS CARBON SEAL AND MATING RING. REMOVED AND REPLACED SCAVENGE OIL LUBE PUMP. CK AND LEAK CK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300063 20070703 00063 EA 2007 7 3 A6WA200740261 1 20070522 A 2913 887055 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HYD SYSTEM FAILED A A6WA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 31 426AW 11372 7669 ENROUTE FROM DCA T 1252Z HYD2 LOW PRESSURE MESSAGE COMPLIED WITH QRH DIVERTED. HYD QTY NR 2 SYSTEM READS ZERO. PRESSED FDR EVENT BUTTON. LANDING WEIGHT 46900, BRAKE TEMP READS 4,5,4,4. REMOVED AND REPLACED ENGINE DRIVEN HYDRAULIC PUMP N R 2. OPERATIONAL AND LEAK CHECKS GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300064 20070703 00064 NM 2007 7 3 SWAA073136 1 20070622 A 5311 6546552 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007070300065 20070703 00065 EA 2007 7 3 A6WA200740262 1 20070521 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 456ZW 7849 LT 621 IS CRACKED .5 INCH LONG. S/D - MAINTENANCE CUT AWAY DAMAGED ANGLE AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R53-61-117 REVC. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300066 20070703 00066 NM 2007 7 3 SWAA073137 1 20070622 A 5311 6546555 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007070300067 20070703 00067 EA 2007 7 3 A6WA200740263 1 20070521 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 456ZW 7849 LT IB AND OB 280 CLIPS ARE CRACKED APPROX .5 INCH. S/D MAINTENANCE REPLACED INBOARD AND OUTBOARD CLIPS WITH NEW CLIPS P /N 601R31113-57 IAW BSC STANDARD REPAIR 601R-53-0057A AND CRJ SRM 51-42-13, 51-42-21. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300068 20070703 00068 EA 2007 7 3 A6WA200740265 1 20070521 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 456ZW 7849 RT 484 ANGLE IS CRACKED APPROX .2500 INCH LONG. S/D MAINTENANCE CUT AWAY CRACKED FLANGE AND INSTALLED REPAIR FLANGE IA W BOMBARDIER REO 601R-53-41-059 REV A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007062800145 20070628 00145 NM 2007 6 28 2007UALA02020 1 20070614 A 3350 20131A BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 512UA 24809 EXIT LOCATOR SIGN ABOVE SEAT ROW 7AB INOP. *S/D* TROUBLESHOT SYSTEM AND FOUND BATTERY PACK WITH LOW VOLTAGE. REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062800146 20070628 00146 NM 2007 6 28 2007UALA02071 1 20070616 A 2612 WARNING SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FIRE PANEL FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 364UA 24533 CREW REPORTS NO FIRE BELL IN COCKPIT WHEN FIRE PANEL TESTED. CAN HEAR BELL IN WHEEL WELL. [07-24-07] REPLACED AURAL WARNING UNIT. UNIT CHECKED OK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062800147 20070628 00147 NM 2007 6 28 2007UALA02072 1 20070615 A 3350 20131A BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 534UA 25129 BULLNOSE EMERGENCY LIGHTS ABOVE ROWS 10 AND 13, ALL FIRST CLASS FLOOR EEL LIGHTS & DOOR 2R OUTSIDE EMERGENCY LIGHT ARE I NOPERATIVE. *S/D* REPLACED BATTERY ASSEMBLY OVER 2 RIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062800148 20070628 00148 NM 2007 6 28 2007UALA02073 1 20070615 A 3397 58781 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 534UA 25129 FIRST EEL FLOOR LIGHT IN FIRST CLASS IS INOPERATIVE. *S/D* REPLACED FEEDER CABLE, OP CHECK GOOD PER MM 33-51-96. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062800149 20070628 00149 NM 2007 6 28 2007UALA02074 1 20070615 A 3350 60253 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 562UA 26664 EEL LIGHT IN FRONT OF MID LAV INOPERATIVE. REPLACED EEL STRIP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062800150 20070628 00150 2007 6 28 2007UALA02075 4 20070618 A 2565 MR25223 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 4L FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 546UA 25367 DURING 3SVC CHECK FOUND 4L SLIDE PRESSURE AT LOWEST SIDE OF GREEN BAND. [08-07-07] SLIDE REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062800151 20070628 00151 NM 2007 6 28 2007UALA02077 1 20070616 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE 3F SEAT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 779UA 26941 THE 3F EMERGENCY LIGHT INOP. *S/D* REPLACED LIGHT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007062800173 20070628 00173 NM 2007 6 28 2007UALA02100 1 20070617 A 3150 WARNING MESSAGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ILLUMINATED A UALA O OTHER J WARNING INDICATION LD LANDING 1 WP 29 571UA 26681 THE -L ELEV PCU- STATUS MESSAGE RECEIVED. [08-07-07] FOUND LT INBOARD ELEVATOR POWER CONTROL UNIT FAULTING. REPLACE D LT INBD PCU. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062800174 20070628 00174 NM 2007 6 28 2007UALA02101 1 20070619 A 5313 STRINGER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 STRINGER IS CRACKED AT FASTENER LOCATION. [07-06-07] MAJOR REPAIR: REPAIRED STRINGER PER LINE EVA NR EVA-70345. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062800175 20070628 00175 NM 2007 6 28 2007UALA02102 1 20070618 A 5320 CUSP WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 996-1020 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 CORROSION ON UPPER SURFACE OF RIGHT CUSP WEB, BS 996 TO 1020. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION. FABRICATE D & INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062800176 20070628 00176 NM 2007 6 28 2007UALA02103 1 20070618 A 5322 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1460 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 AFT PIT SHEAR TIE CORRODED AT STA 1460, LBL 3. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION, FABRICATED & INSTALLED A NEW SHEAR TIE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062800178 20070628 00178 NM 2007 6 28 2007UALA02105 1 20070618 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1400-1420 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 AFT PIT BETWEEN STA 1400 TO 1420, INTERCOSTAL BETWEEN STR 27L TO 28L IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REMOVED I NTERCOSTAL. FABRICATED & INSTALLED A NEW INTERCOSTAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062800180 20070628 00180 NM 2007 6 28 2007UALA02107 1 20070618 A 5100 STRUCTURE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 806UA 788 EXTERIOR DAMAGE DUE TO JETWAY COLLISION. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062800181 20070628 00181 EU 2007 6 28 2007UALA02108 1 20070618 A 3510 OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 424UA 506 COCKPIT OXYGEN HAS A SLOW LEAK, LOST 150 PSI IN 2 HOURS. RESERVICED O2 SYSTEM TO FULL AND FULLY RESEATED ALL COCKPIT 02 MASKS. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062800182 20070628 00182 NM 2007 6 28 2007UALA02113 1 20070618 A 2121 FAN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 187UA 26877 TURNED OFF UPPER RECIRC FAN AND ODOR WENT AWAY, ODOR PROMINENT BETWEEN ROWS 37+44. [07-27-07] ON ARRIVAL SWITCHED ON UPPER RECIRCULATION FAN AND CHECKED CONCERNED CABIN AREA. NO SMOKE ODOR NOTED. BUT FOUND CB ON PANEL P415 TRIPPED. SUS PECT UPPER RT RECIRCULATION FAN AT FAULT. REPLACED RECIRCULATION FAN 1 PER MM21-25-01. OPS NORMAL & CIRCUIT BREAKER STA YS IN. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062900020 20070629 00020 EA 2007 6 29 COMA0760435 1 20070614 A 5270 DOOR CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 588SW 7069 FLIGHT 5354 - DURING CLIMB PAX DOOR OUTER HANDLE MESSAGE DISPLAYED, AIRCRAFT RETURNED BACK TO CHS AND LANDED SAFELY. IN SPECTED PAX DOOR OUTER HANDLE FOR PROPER OPERATION. ALL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007062900022 20070629 00022 EA 2007 6 29 COMA0760437 1 20070615 A 2760 586510702 RELAY CNDAIR CL600 CL6002B19 1900309 EA SPOILERONS FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 416CA 7450 FLIGHT 5563 - EN ROUTE RDU-JFK RECEIVED A SPOILERON FAULT AND INBOARD GROUND SPOILER MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO RDU. FLIGHT LANDED WITHOUT INCIDENT. REPLACED RELAY IN JB11. 2 L 7 2 4F RT A21EA 2007062900023 20070629 00023 EA 2007 6 29 COMA0760438 1 20070616 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA RT WING FLAPS FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 914CA 14422 7012 EN ROUTE CVG-CXO RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO CVG. FLIGHT LANDED WI THOUT INCIDENT. REPLACED THE RIGHT BRAKE POSITION SENSING UNIT. 2 L 7 2 4F RT A21EA 2007062900027 20070629 00027 EA 2007 6 29 COMA0760442 1 20070618 A 3150 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA COOL CAUTION UNKNOWN A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 420CA 7451 FLIGHT 5231 - EN ROUTE RDU-ATL RECEIVED A DISPLAY COOL CAUTION MESSAGE, FLIGHT DIVERTED TO GSP. INSPECTED DISPLAY COOL DUCTING, AIR SUPPLY FILTER, LOW AIR FLOW SENSOR, WITH NO DEFECTS NOTED. PERFORMED AN OPERATIONAL CHECK ON GROUND WITH N O DISCREPANCIES NOTED. 2 L 7 2 4F RT A21EA 2007062900041 20070629 00041 NM 2007 6 29 ASAA0791803 1 20070531 A 5310 146A750339 RAIL BOEING 737 737990 NM BS 727D CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT SUPPORT RAIL CORRODED. REPAIRED IAW EA5310 02724. 2 L 7 4 4F RT A16WE 2007062900046 20070629 00046 NM 2007 6 29 ASAA0791808 1 20070531 A 5310 146A750611 RAIL BOEING 737 737990 NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT RAIL SPLICE IS CORRODED. REPAIRED IAW 51-40-02 AND 51-40-05. 2 L 7 4 4F RT A16WE 2007062900075 20070629 00075 NM 2007 6 29 DL76S070731 1 20070605 A 5310 BAC15063123 STRUCTURE BOEING 767 767332 1382001 NM BS 1197 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 130DL 24080 DURING HMV 3 AT MAE, FOUND AFT PIT STA 1197+66 LBL 36 T CHORD CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-00-07. REPAIRED PER SRM 53-00-07 REPAIR 4. 2 L 7 2 4F RT A1NM 2007062900091 20070629 00091 NM 2007 6 29 DLM88070753 1 20070619 A 5753 SKIN DOUG MD88 MD88 3023688 NM TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 RT INBD FLAP LOWER SKIN WAS SPLICED BETWEEN XIFO 47.5 AND XIFO 99.5. THIS 43" SPLICE WAS A HOT BONDED REPAIR PER MD88 S RM 51-70-2 PAR. 18.B. THIS REPAIR WAS DUE TO A TIME-LIMITED SRM REPAIR TO THE SKIN. 2 L 7 2 4F RT A6WE 2007062900092 20070629 00092 NM 2007 6 29 DLM88070754 1 20070619 A 2432 249001128 CHARGER DOUG MD88 MD88 3023688 NM E/E BAY BURNED A DALA H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 914DL 49545 BATTERY CHARGER CAUGHT ON FIRE AND POPPED C/B. INSTALLED NEW R2-56 RELAY NEW TEMP SENSORS, REINSTALLED BATTERY TRAY. I NSTALLED NEW BATTERY CHARGER. REMOVED AND INSTALLED NEW BATTERY CHARGER C/B. BATTERIES LT S/N OFF 1030768 ON 10503139. RT S/N OFF 10503142 ON 10403938 DAL P/ 249701544. 2 L 7 2 4F RT A6WE 2007070200001 20070702 00001 EA 2007 7 2 A6WA200740282 1 20070528 A 5330 60033052141 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FS 169-174 DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 RT NOSE SKIN PANEL PN 600-33052-141 IS DENTED 3 INCHES LONG BY 2 INCHES WIDE BY 0.100 DEEP BETWEEN FS 169.00 AND FS 174 .00. S/D - MAINTENANCE REMOVED AND REPLACED SKIN PANEL P/N 600-33052-141 BETWEEN FS 169.00 AND 174 IAW CRJ 200 SRM 51-4 2-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070200008 20070702 00008 NM 2007 7 2 07FDEA02257 1 20070622 A 5240 DOOR FRAME BOEING 727 727233 138408A NM ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 HIDDEN DAMAGE INSPECTION LT AFT SERVICE DOOR, 2ND FRAME, 4" FROM AFT EDGE UPPER SURFACE OF LOWER FRAME, SHEAR TIE IS COR RODED. [07-26-07] BLENDED OUT DAMAGE. ORIGINAL MATERIAL IS .050", REMOVED .005", REMAINING MATERIAL IS .045". CH ECKED MATERIAL LOSS WITH TOOL IN17-0458 CAL DATE 4/24/07 WITHIN LIMITS REF SRM 52-10-2 2 L 7 3 4F RT A3WE 2007070200013 20070702 00013 NM 2007 7 2 AWXA200700759 1 20070529 A 5320 143N8336U15 INTERCOSTAL BOEING 757 757225 1384959 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 MCN - MAJOR REPAIR - CRACKED L-2 DOOR CUT OUT INTERCOSTAL WEB, BS 660, S15L AT THE NR 6 DOOR STOP. REPLACED L-2 DOOR CU T OUT INTERCOSTAL WEB, BS 660, S15L AT THE NR 6 DOOR STOP IAW AWA TASK CARD M1C53614. 2 L 7 2 4F RT A2NM 2007070200019 20070702 00019 EU 2007 7 2 F3LA200700134 1 20070609 A 5315 D5347217228200 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 907FR 5061 1743 DURING C4/S1 CHECK, INSPECTION REPORTED TWO AREAS OF CORROSION ON FLOORBEAM +Y1292 AT FR68. REPLACED FLOORBEAM IAW SRM 51-42-11, SRM 51-44-11 AND EA #A0-53T-11472. 2 L 7 2 4F RT A28NM 2007070200047 20070702 00047 NM 2007 7 2 AWXA200700765 1 20070617 A 5743 65C365451 FITTING BOEING 737 73733A 1384673 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - LEFT WING MAIN LANDING GEAR SUPPORT BEAM FITTING CRACKED, RSS 224.14. REPLACED LEFT WING MAIN LANDING GEAR SUPPOR T BEAM FITTING, RSS 224.14 IAW AWA ER 03-5751-07157-SS2. 2 L 7 2 4F RT A16WE 2007070200064 20070702 00064 EU 2007 7 2 07FDEA02280 1 20070626 A 5320 CROSSBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 726FD 575 FOUND CORROSION AT CROSSBEAM C58 RT ( P/N A539-74268) OUTBOARD OUT OF LIMIT AND OLD REPAIR ON CROSSBEAM C62 LT (P/N A539 -70091) NOT CONFORM TO SRM REPAIR PERFORMED IAW SRM 53-10-15 FIG 207 AT CROSSBEAM C 62 LT AND 58 RT. 2 L 7 2 4F RT A35EU 2007070200068 20070702 00068 NM 2007 7 2 07FDEA02284 1 20070626 A 5315 BAC1518338 FLOORBEAM BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT UPPER MAIN DECK , FLOORBEAM TOP CAP HAS CORROSION AND A DRILL START ON UPPER SURFACE, STA 950E, LBL 35. REMOVED DAM AGE AREA OF FLOORBEAM AT STA 950E LBL 35 IAW B727 SRM 53-10-8. FABRICATED REPAIR ANGLES (2 EA) AND FILLER FROM BAC1490- 2888 PO NR 10156633 A TAG NR 03969 IAW B272 SRM 51-10-8. TREATED AND PRIMED REPAIR AREA AND REPAIR PARTS IAW SRM 53-10- 8. 2 L 7 3 4F RT A3WE 2007070200075 20070702 00075 SO 2007 7 2 SIMA200717702 1 20070622 A 3230 355022002 ELECTRONIC UNIT EMB 135 EMB135LR 3260305 SO ZONE 200 FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 706RG 17038 145194 GEAR HANDLE FOUND TO BE UNMOVABLE FOLLOWED BY A LANDING GEAR AIR/GROUND FAIL MESSAGE, RETURNED TO YYZ. MESSAGE EXTINGUI SHED ON APPROACH. REMOVED AND REPLACED LANDING GEAR ELECTRONIC CONTROL UNIT, LANDING GEAR CONTROL LEVER AND AIR/GROUND POSITION RELAY IAW EMB AMMS 32-32-01, 32-32-02, AND 32-13-02. PERFORMED OPERATIONAL CHECKS IAW AMM 32-30-00 AND 32-52-0 0 WITH NO FURTHER DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007070200076 20070702 00076 SO 2007 7 2 SIMA200717704 1 20070623 A 3230 355022002 ELECTRONIC UNIT EMB 145 EMB145LR 3260212 SO ZONE 200 FAILED A SIMA O OTHER J WARNING INDICATION LD LANDING 1 SW 21 653AE 11636 8161 145433 DURING GEAR EXTENSION RECEIVED LANDING GEAR DISAGREE, LANDING GEAR AIR/GROUND FAIL MESSAGE WITH THREE GREEN LIGHTS. PER FORMED MANUAL GEAR EXTENSION, DECLARED EMERGENCY. PERFORMED CENTRAL MAINTENANCE SYSTEM DOWNLOAD IAW EMB AMM 45-900-00 A ND FLIGHT DATA RECORDER DOWNLOAD IAW AMERICAN EAGLE WORKCARD 31-700-05. PERFORMED OPERATIONAL CHECK OF AIR/GROUND SYSTE M IAW AMERICAN EAGLE WORKCARD32-700-16 WITH NO DEFECTS NOTED. REMOVED AND REPLACED LANDING GEAR ELECTRONIC CONTROL UNIT AND PERFORMED OPERATIONAL CHECKS IAW EMB AMM. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007070200077 20070702 00077 SO 2007 7 2 SIMA200717708 1 20070624 A 3230 355022002 ELECTRONIC UNIT EMB 135 EMB135KL 3260302 SO ZONE 200 FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 800AE 18687 6348 145425 LANDING GEAR SELECTED TO UP POSITION WITH INDICATIONS SHOWING IN TRANSIT WITH NO GEAR MOVEMENT, CYCLED GEAR WITH NO CHAN GE. PLACED GEAR LEVER IN DOWN POSITION FOLLOWED WITH THREE GREEN LIGHTS, RETURNED TO LAX. REMOVED AND REPLACED LANDING GEAR ELECTRONIC CONTROL UNIT IAW EMB AMM 32-32-01. PERFORMED EXTENSION AND RETRACTION CHECKS WITH NO DEFECTS IAW EMB A MM 32-30-00. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007070200083 20070702 00083 WP 2007 7 2 ASAA0781813 1 20070615 A 2560 5913350515 CONTROL UNIT DOUG DC9 DC983 3022083 WP TAILCONE JETTISO MALFUNCTIONED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 A TEST DEPLOYMENT (PER TASK CARD 28653000) OF THE TAIL CONE EMERGENCY SLIDE FAILED. A SUBSEQUENT TEST PER THE REFERENCE PROCEDURE IN MM 53-53-00 WAS SUCCESSFUL. AN INVESTIGATION HAS BEEN INITIATED TO DETERMINE THE CAUSE OF FAILURE BUT SUB SEQUENTLY CANCELED DUE TO THE MD 80 FLEET BEING RETIRED BEFORE ITS COMPLETION. 2 L 7 2 4F RT A6WE 2007070200086 20070702 00086 NM 2007 7 2 ASAA0741816 1 20070622 A 5310 654580770 FRAME BOEING 737 7374Q8 138447Q NM CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 R1 DOOR SURROUND STRUCTURE FWD STUB FRAME CRACKED 3/4 WAY UP IN O/B FLANGE RADIUS. REMOVED R1 STUB FRAME, FABRICATED, T REATED & PRIMED, TOPCOATED AND INSTALLED NEW STUB FRAME IAW SRM 51-30-01, 51-40-02 AMM 51-21-21 PG 704 & 706 AND ASA EA 5210 01133. 2 L 7 2 4F RT A16WE 2007070200088 20070702 00088 NM 2007 7 2 2007UALA02115 1 20070620 A 5240 DOOR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU RT SERVICE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 912UA 25290 AFT RIGHT SERVICE DOOR IS DAMAGED. [07-13-07] REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLERS, TRIPLER AND FILLER. REFERENCR SRM 53-00-01 REPAIR 32. 2 L 7 2 4F 4 F RT A16WE E21EU 2007070200112 20070702 00112 NM 2007 7 2 2007UALA02141 1 20070620 A 4920 CONTROL VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE APU MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 APU SHUT DOWN ON START, ATTEMPTED 2 STARTS, BOTH FAILED WITH FAULT INDICATION. [07-20-07] REPLACED APU SURGE CONTROL VALVE PER MM 49-53-01-401. ACCOMPLISHED MAIN ENG START PER JRH. OP CHECKS SATISFACTORY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007070200116 20070702 00116 NE 2007 7 2 2007UALA02146 2 20070618 A 7311 IDG AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 CONTAMINATED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 424UA 506 NR 1 IDG CONTAMINATED WITH FUEL IN THE OIL. FOUND IDG FUEL/OIL COOLER LEAKING. REPLACED IDG FUEL/OIL COOLER AND IDG 1 AS WELL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007070200125 20070702 00125 NM 2007 7 2 2007UALA02155 1 20070620 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 857 PINCHED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 648UA 25285 MAIN CABIN EMERGENCY EXIT LIGHT WIRES ARE PINCHED. REPAIRED PINCHED WIRES TO L977 AT STA 857, LBL 85 PER WDM 33-51-14 A ND BSWPM 20-10-13. OPS TESTS GOOD PER MM 33-51-01 ON NON ROUTINE E2116I. 2 L 7 2 4F 4 F RT A1NM E24NE 2007070200126 20070702 00126 NM 2007 7 2 2007UALA02156 1 20070620 A 2797 WIRE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SLATS SHORTED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 677UA 30029 L/E SLAT ASYMMETRY LIGHT AND EICAS MESSAGE ON PRIOR TO DEPARTURE. [07-20-07] FOUND SHORT IN WIRE SPLICE. REPLACED S PLICE SM7, WIRE W480-007-18, AND SHIELD ASSEMBLY. REINSTALLED D4378 CONNECT OR ASSY, AND SECURED WIRE BUNDLE. SYSTEM C HECKED OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007070200129 20070702 00129 NM 2007 7 2 SWAA073108 1 20070621 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 14Y CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007070200147 20070702 00147 NM 2007 7 2 SWAA073094 1 20070621 A 5311 65C229081 FRAME BOEING 737 7373H4 1384600 NM BS 500B CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007070200160 20070702 00160 NM 2007 7 2 SWAA073086 1 20070621 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 412WN 29818 DURING SCHEDULED HC1 CHECK, RT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007070200163 20070702 00163 NM 2007 7 2 SWAA073088 1 20070621 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 412WN 29818 DURING SCHEDULED HC1 CHECK, LT AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007070200165 20070702 00165 NM 2007 7 2 USAA070480 1 20070622 A 5311 FRAME BOEING 737 737401 1384701 NM BS 492 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 BS 492 FWD CARGO DOOR AFT FRAME S-24R WL 163 HAS CRACK. REMOVED & REPLACED FWD CARGO AFT FRAME PER SRM 51-10-02, DWG 65 -20723, DEFECT SIZE: .500 INCH. 2 L 7 2 4F RT A16WE 2007070200167 20070702 00167 NM 2007 7 2 USAA070478 1 20070622 A 5311 FRAME BOEING 737 737401 1384701 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FUSELAGE FRAME STA 787 BETWEEN STR 8L & 9L AT A/C PSU RAIL ATTACH BRACKET HAS CRACK. CUT OUT DAMAGE & INSTALLED REPAIR DOUBLERS PER TR 53-10-20E, DEFECT SIZE: .0625 INCH. 2 L 7 2 4F RT A16WE 2007070200168 20070702 00168 NM 2007 7 2 USAA070477 1 20070622 A 5712 RIB BOEING 737 737401 1384701 NM LEFT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 LEFT WING RIB STA 135.5 AFT END JUST BEFORE REAR SPAR HAS CRACK. REMOVED DAMAGE & INSTALLED REPAIR PER EA 98713, DEFECT SIZE: .625 INCH. 2 L 7 2 4F RT A16WE 2007070200174 20070702 00174 EU 2007 7 2 USAA070471 1 20070622 A 5320 SILL AIRBUS A321 A321211 3930370 EU R4 DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 181UW 1531 R4 DOOR SILL AT FRAME C66 HAS CORROSION. INSTALLED DOUBLER REPAIR IAW TYP REP 53-41-01, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A28NM 2007070200175 20070702 00175 NM 2007 7 2 USAA070470 1 20070622 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 AFT ENTRY DOOR LOWER HINGE SKIN CUTOUT HAS CRACK. REMOVED DAMAGE & INSTALLED FABRICATED REPAIR PARTS PER TR 53-60-10, D EFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007070200177 20070702 00177 NM 2007 7 2 KPVA20076 1 20070621 A 6123 30005000034 TSCU DHAV DHC8 DHC8103 1386005 NM HAMSTD 14SF 14SF7 NE RT ENGINE MALFUNCTIONED A KPVA D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 WP 13 809WP 032 860202 (PIREP) WITH CONDITION LEVERS MAX WHEN TAXIING ON TO RUNWAY FOR TAKEOFF, NR 2 PROP EXPERIENCED AN UNCOMMANDED FEATHER. POWER LEVERS SLIGHTLY ABOVE IDLE, NR 2 TQ INCREASED TO 60 PERCENT, NR 2 PROP DOWN TO APPROX 300. (MX) REMOVED AND REPLA CED NR 2 ENGINE TORQUE SIGNAL CONDITIONER. OPS CHECK GOOD IAW PWC MM 72-01-10 PAR A & B. 2 H 7 2 4T RT A13NM 6 C P7NE 2007070200182 20070702 00182 NM 2007 7 2 HNAA0700119 1 20070622 A 3150 HA1555 MASTER CAUTION DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 838EX 220 MASTER CAUTION LIGHT. PUSH TO RESET LIGHT INOP. REMOVED AND REPLACED MASTER CAUTION LIGHTS PANEL AND PUSH TO RESET MOD . OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007070200194 20070702 00194 SO 2007 7 2 RAIA00706031 1 20070620 A 3350 RPS1B BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS NO TEST A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 816HK 145055 PRE FLT NR 5534 - DAL - EMERGENCY LIGHTS OUT AT AFT. CEILING EXIT LOCATOR, LT & RT OVERWING EXIT IDENTIFIER, LT & RT EM ERGENCY DOOR FLOOD LIGHT, LT & RT OVERWING EXIT MARKER AND FLOOR PROXIMITY LIGHTS. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY NR 3. 2 L 7 2 4T RT T00011AT 2007070200196 20070702 00196 SO 2007 7 2 RAIA00706033 1 20070620 A 5210 DOOR EMB 145 EMB145ER 3260211 SO MAIN PAX STUCK A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 808HK 145157 POST FLT NR 8048 - ORD - PAX DOOR WILL NOT OPEN. MAINTENANCE RIGGED PAX DOOR. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007070200198 20070702 00198 SO 2007 7 2 RAIA00706029 1 20070618 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 811HK 145256 POST FLT NR 5528 - STL - PAX DOOR FLOOD LIGHT INOP. MAINTENANCE REPLACED MAIN DOOR LIGHT BULB, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007070300015 20070703 00015 EA 2007 7 3 A6WA200740251 1 20070514 A 5320 S6144A14 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 458AW 7861 INTERCOSTAL AT FS 484.00 HAS CRACKED FLANGE AT RBL 27.0 CRACK MEASURES APPROX .20 INCH LONG. S/D MAINTENANCE REPLACED CLIP IAW BSC SR 601R-53-0029B. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300016 20070703 00016 EA 2007 7 3 A6WA200740252 1 20070514 A 5320 601R3117117 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 458AW 7861 INTERCOSTAL AT FS 484.00 HAS CRACKED FLANGE AT LBL 27.0 CRACK MEASURES APPROX .50 INCH LONG. S/D MAINTENANCE REPLACED CLIP IAW BSC SR 601R-53-0029B. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300028 20070703 00028 NM 2007 7 3 UPS07450011 1 20070604 A 5311 65B01717516 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C CABIN BS 480 S15R FRAME FOUND CRACK. CRACK LENGTH 2.5 INCHES. CABIN BS 480 STR 13AR TO STR 16R FRAME REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007070300045 20070703 00045 NM 2007 7 3 SWAA073118 1 20070622 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 467WN 33830 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 15 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007070300069 20070703 00069 EA 2007 7 3 A6WA200740266 1 20070521 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 456ZW 7849 LT 484 ANGLE IS CRACKED APPROX .2500 INCH LONG. S/D MAINTENANCE PERFORMED EDDY CURRENT INSPECTION IAW CRJ NDTM 51-20-0 6 PART 6 AND FOUND NO RECORDABLE INDICATIONS. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300070 20070703 00070 NM 2007 7 3 SWAA073138 1 20070622 A 5311 6546558 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007070300071 20070703 00071 EA 2007 7 3 A6WA200740267 1 20070521 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 456ZW 7849 RT 621 IS CRACKED APPROX .5 INCH LONG. S/D MAINTENANCE REMOVED DAMAGED SECTION ANGLE AND INSTALLED REPAIR ANGLE AND DOU BLER IAW BOMBARDIER REO 601R-53-61-117 REVC. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300072 20070703 00072 EA 2007 7 3 A6WA200740268 1 20070522 A 5320 6013501252 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FS 625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 456ZW 7849 RT FS 625.00, OBLIQUE ANGLE IS CRACKED 1.5 INCH ON AFT RADIUS. S/D MAINTENANCE REMOVED AND REPLACED RT FS 625 OBLIQUE ANGLE IAW CRJ 200 SRM 51-42-21 AND BOMBARDIER REO 601R-53-61-422. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300073 20070703 00073 EA 2007 7 3 A6WA200740269 1 20070522 A 5320 6013501251 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FS 625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 456ZW 7849 LT FS 625 OBLIQUE ANGLE IS CRACKED 1.5 INCH LONG IN AFT RADIUS. S/D MAINTENANCE REMOVED AND REPLACED LEFT FS 625 OBLIQ UE ANGLE IAW CRJ200 SRM 51-42-21 AND BOMBARDIER REO 601R-53-61-422. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300075 20070703 00075 EA 2007 7 3 A6WA200740270 1 20070522 A 5340 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 529 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 456ZW 7849 LT MLG WHEEL WELL HYDRAULIC SUPPORT BRACKET IS CRACKED .2500 INCH ON OB RADIUS. S/D MAINTENANCE REMOVED BRACKET AND INS TALLED NEW BRACKET P/N 601R75262-159 IAW CRJ SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300076 20070703 00076 NM 2007 7 3 SWAA073139 1 20070622 A 5311 6546596 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007070300077 20070703 00077 EA 2007 7 3 A6WA200740271 1 20070522 A 5340 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 529 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 456ZW 7849 LT MLG WHEEL WELL HYDRAULIC SUPPORT BRACKET IS CRACKED .2500 INCH ON OB RADIUS. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300078 20070703 00078 NM 2007 7 3 SWAA073125 1 20070622 A 5754 65C26601 SLAT BOEING 737 7375H4 138449D NM LT WING WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND LEFT WING NR 5 L/E SLAT WORN AT INBOARD T/E. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007070300079 20070703 00079 EA 2007 7 3 A6WA200740272 1 20070522 A 5340 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 529 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 456ZW 7849 RT MLG WHEEL WELL HYDRAULIC SUPPORT BRACKETS ARE CRACKED .2500 INCH ON OB RADIUS. S/D - MAINTENANCE REMOVED BRACKETS AN D INSTALLED NEW BRACKETS P/N 601R75262-153 AND 601R75262-157 IAW CRJ SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300080 20070703 00080 EA 2007 7 3 A6WA200740273 1 20070527 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 459AW 7863 LT 484 ANGLE IS CRACKED AT LBL 36 AND LBL 27 APPROX .2500 INCH LONG. (K) [07-12-07] MAINTENANCE REPAIRED LT 484 ANGLE AT LBL 36 AND 27 IAW REO 601R-53-41-059 REV A, STANDARD REPAIR 601R-53-0029B AND STANDARD REPAIR 601R-53-0030A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300082 20070703 00082 EA 2007 7 3 A6WA200740274 1 20070527 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 459AW 7863 RT 484 ANGLE IS CRACKED AT RBL 27 APPROX .2500 INCH LONG. (K) [07-12-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW R EO 601R-53-41-059, REV A AND BSC STANDARD REPAIR 601R-53-0029B. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300084 20070703 00084 EA 2007 7 3 A6WA200740275 1 20070527 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 459AW 7863 RT FS 621.00 FLOOR ATTACHMENT SUPPORT ANGLE IS CRACKED .5 INCH LONG IN OB RADIUS. (K) [07-12-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW REO 601R-53-61-117 REV C. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300085 20070703 00085 EA 2007 7 3 A6WA200740276 1 20070527 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 459AW 7863 RT FS 621.00 FLOOR ATTACHMENT SUPPORT ANGLE IS CRACKED .5 INCH LONG IN OB RADIUS. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300086 20070703 00086 EA 2007 7 3 A6WA200740277 1 20070527 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 459AW 7863 LT FS 621.00 FLOOR ATTACHMENT SUPPORT ANGLE IS CRACKED .5 INCH LONG ON OB RADIUS. (K) [07-12-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW REO 601R-53-61-117, REV C. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300087 20070703 00087 NM 2007 7 3 SWAA073127 1 20070622 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007070300088 20070703 00088 EA 2007 7 3 A6WA200740278 1 20070528 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 459AW 7863 RT 625, OBLIQUE ANGLE IS CRACKED APPROX 1 INCH LONG. (K) [07-12-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW SRM 5 1-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300089 20070703 00089 EA 2007 7 3 A6WA200740279 1 20070528 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 459AW 7863 LT 625, OBLIQUE ANGLE IS CRACKED APPROX 1 INCH LONG. (K) [07-12-07] MAINATENANCE REMOVED AND REPLACED ANGLE IAW SRM 5 1-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300090 20070703 00090 NM 2007 7 3 SWAA073126 1 20070622 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007070300092 20070703 00092 EA 2007 7 3 A6WA200740284 1 20070530 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 418AW 7618 LT SIDE FS 621.00 TO 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. [07-31-07] MAINTENANC E REMOVED CRACKED INTERCOSTAL AT LT STR 14L AND INSTALLED NEW INTERCOSTAL IAW CRJ200 SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300093 20070703 00093 EA 2007 7 3 A6WA200740206 1 20070418 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 417AW 7610 RT HYDRAULIC TRANSDUCER BRACKET (PN 601R75262-157) CRACKED APPROX .2 INCH LONG IN RT MLG WHEEL WELL CEILING. INSTALLED NEW BRACKET IAW SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300094 20070703 00094 EA 2007 7 3 A6WA200740212 1 20070424 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 454AW 7842 LT FS 621.00 FLOOR SUPPORT ANGLE CRACKED. MAINTENANCE REPAIRED CRACK IAW REO 601R-53-61-117, REV C. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300095 20070703 00095 NM 2007 7 3 SWAA073132 1 20070622 A 5311 65C33511 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007070300096 20070703 00096 EA 2007 7 3 A6WA200740214 1 20070424 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RWS 95 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 417AW 7610 RT WING PLANK AT ACCESS HOLE 640DB HAS CORROSION ON LOWER IB SIDE MEASURES APPROX .5 X .25 X .002 IN NON-CRITICAL AREA. REPAIRS ACCOMPLISHED IAW EO E06/021/457. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300097 20070703 00097 NM 2007 7 3 SWAA073142 1 20070622 A 5315 65C33948 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5, LBL 5. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007070300098 20070703 00098 NM 2007 7 3 SWAA073140 1 20070622 A 5311 65C34356 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007070300101 20070703 00101 2007 7 3 SWAA073116 4 20070622 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007070300107 20070703 00107 NM 2007 7 3 UPS07450024 1 20070608 A 5320 65B0183534 STRUCTURE BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C CRACK FOUND AT 1EA FASTENER HOLE BELOW STR 15ER AT BS 420 FWD INNER CHORD (P/N: 65B01835-34) CRACKED T HROUGH THICKNESS 0.040 INCH LONG RUNNING O/B AT 3 O`CLOCK POSITION (LOOKING FWD), (CRACK LENGTH 0.040 INCH). CABIN BS 4 20 FRAME ATTACH INNER CHORD BETWEEN STR 10AR TO STR 16R REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007070300110 20070703 00110 EA 2007 7 3 A6WA200740235 1 20070501 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 455AW 7848 LT FS 621.00 AND 625.00 OBLIQUE ANGLE HAS A 1.5 INCH LONG CRACK IN AFT RADIUS. (K) [07-17-07] MAINTENANCE REMOVED CRA CKED ANGLE AND INSTALLED NEW ANGLE IAW CRJ200 SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300111 20070703 00111 EA 2007 7 3 A6WA200740236 1 20070503 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 455AW 7848 RT FS 621..00 FLOOR SUPPORT ANGLE IS CRACKED 1.2500 INCH LONG IN OB RADIUS. (K) [07-17-07] MAINTENANCE CUT AWAY DAMAGE D AREA AND INSTALLED SERVICEABLE REPAIR IAW BOMBARDIER REO 601R-53-61-117. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300112 20070703 00112 EA 2007 7 3 A6WQA200740237 1 20070503 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 455AW 7848 LT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED 1.2500 INCH LONG IN OB RADIUS. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300113 20070703 00113 NE 2007 7 3 DATA200700005 2 20070620 A 7200 ENGINE STBROS SD3 SD360 8100606 EU PWA PT6 PT6A65AR 52043 NE LEFT POWER LOSS E DATA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 13 617FB 27261 23006 SH3617 PS97128 WHILE IN CRUISE, LEFT ENGINE LOST POWER WITH INCREASE OF ITT TO 1200 FOLLOWED BY LOUD NOISE. FOLLOWED PROCEDURES AND SH UT DOWN ENGINE. DIVERTED TO MWA. ENGINE REPLACEMENT IN WORK. 2 H 7 2 4T 4 T A41EU E4EA 2007070300114 20070703 00114 CE 2007 7 3 K452007F00000 1 20070601 A 2750 65651201CR CONTROL CABLE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE TE FLAPS BROKEN E K45A O OTHER O OTHER AP APPROACH 1 GL 25 103BG 5600091 FLAPS WOULD NOT EXTEND DURING APPROACH. AN UNEVENTFUL (NO FLAP)LANDING WAS ACCOMPLISHED. INSPECTION REVEALED THE FLAP FOLLOWUP CABLE (AFT) HAD BROKEN WHERE IT PASSES OVER 1 PULLEY FORMING AN (S) ROUTING. THIS IS A HIGH WEAR AREA AND COMM ON PROBLEM ON THIS MODEL AC. THE CABLE WAS REPLACED. (K) 2 L 7 2 4F 4 F RT A22CE E25EA 2007070300115 20070703 00115 CE 2007 7 3 OYE2007F00000 1 20070530 A 3210 07410017LH LEG ASSY CESSNA 185 A185F 2072821 CE CONT O520 IO520D 17032 SO MCAULY D3A34 D3A34C401 GL LT MLG BROKEN E OYEA O OTHER O OTHER NR NOT REPORTED 1 NM 13 104DE 18504009 812905R 060627 AFTER LANDING THE LT GEAR LEG BROKE AT UPPER AXEL BOLTS. THIS CAUSED LOSS OF CONTROL OF AIRCRAFT. IT APPEARED THAT THE LANDING GEAR LEG HAD BEEN CRACKED FOR SOME TIME DUE TO CORROSION NOTED AT BREAK. (K) 1 H 7 1 3O 3 O 3A24 E5CE 5 C P47GL 2007070300116 20070703 00116 CE 2007 7 3 ODR2007F00000 1 20070522 A 5730 SKIN CESSNA 402 402B 207590P CE CONT O520 TSIO520EB 17040 SO MCAULY 3AF32C 3AF32C87 GL LT WING CRACKED E ODRA O OTHER O OTHER NR NOT REPORTED 1 WP 07 87193 402B1019 7-8 INCH CRACK IN SKIN OF WING LOCATED BETWEEN LT NACELLE AND FUSELAGE; AFT OF LEADING EDGE; ON TOP OF WING. APPARENT C AUSE IS FATIGUE DUE TO PREVIOUS OWNER WALKING ON WING. CRACK BECAME APPARENT DURING PRE-FLIGHT INSPECTION ON 5/22/2007. (K) 1 L 7 2 3O 3 O A7CE E8CE 5 C P22EA 2007070300117 20070703 00117 NM 2007 7 3 GAIA0706OP 1 20070526 A 3297 WIRE BOEING 727 727243 138408D NM PWA JT8 JT8D7B 52053 NE GOUND SENSOR BROKEN A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 1269Y 21269 ON TAKEOFF THE LANDING GEAR LEVER WOULD NOT GO PAST THE OFF POSITION FOR GEAR UP. THE CREW LEFT THE GEAR HANDLE IN THE DODWN POSITION AND RETURNED TO DEPARTURE. AN UNEVENTFUL LANDING WAS MADE. THE GEAR HANDLE LOCK SOLENOID AND THE GEAR G ROUND MODE PROXIMITY SENSORS WERE REPLACED. REPAIRED BROKEN WIRES IN SPLICES TO BOTH AIR GROUND SENSORS. ACCOMPLISHED TEST IN GROUND AND AIR MODES. OPS CHECKED GOOD. AC WAS RETURNED TO SERVICE. (K) 2 L 7 3 4F 4 F RT A3WE E2EA 2007070300118 20070703 00118 EU 2007 7 3 SIMA200717709 1 20070625 A 3230 D49412001 CONTROL PANEL SAAB SF340 340B 7860101 EU ZONE 100 FAILED A SIMA O OTHER O OTHER CL CLIMB 1 SW 21 218AE 19010 2912 340B218 PLACED GEAR LEVER IN DOWN POSITION WITH NO TRANSIT LIGHT, CYCLED GEAR WITH NO TRANSIT LIGHT. REMOVED AND REPLACED LANDI NG GEAR CONTROL PANEL IAW SAAB AMM 32-31-05. OPERATIONAL CHECK GOOD WITH NO DEFECTS. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007070300119 20070703 00119 SO 2007 7 3 SIMA200717707 1 20070624 A 3297 355022002 ELECTRONIC UNIT EMB 135 EMB135LR 3260305 SO ZONE 200 FAILED A SIMA O OTHER J WARNING INDICATION LD LANDING 1 SW 21 729AE 14129 1081 145343 LANDING GEAR EXTENSION INDICATIONS (ALL THREE) WENT FROM UP TO DOWN WITH NO TRANSITION, LANDING GEAR LEVER DISAGREE WARN ING MESSAGE ALERTED THEN CLEARED WITH THREE GREEN LIGHTS, FLYBY PERFORMED FOR EXTENSION. PERFORMED OPERATIONS CHECKS OF THE EXTENSION AND RETRACTIONS WITH NO DEFECTS IAW EMB AMM 32-32-00. PERFORMED OPERATIONAL CHECK OF LANDING GEAR CONTRO L LEVER IAW EMB AMM 32-32-01 WITH NO DEFECTS. REMOVED AND REPLACED LANDING GEAR ELECTRONIC CONTROL UNIT AS PRECAUTIONAR Y IAW EMB AMM 32-32-01. PERFORMED GEAR RETRACTION AND EXTENSION CHECKS WITH NO DEFECTS, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007070300120 20070703 00120 EA 2007 7 3 SWIA200718370 1 20070429 A 5346 BEAM CNDAIR CL600 CL6002B19 1900309 EA CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 449SW 7699 LEFT LOWER ENGINE BEAM PANEL CUTOUT IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS TO LEFT LOWER ENGINE BEAM WEB PER CRJ200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007070300121 20070703 00121 EA 2007 7 3 SWIA200718371 1 20070429 A 5346 BEAM CNDAIR CL600 CL6002B19 1900309 EA CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 449SW 7699 RIGHT LOWER ENGINE BEAM PANEL CUTOUT IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS TO RIGHT LOWER ENGINE BE AM WEB PER CRJ200 SRM 51-42-06 P 11. 2 L 7 2 4F RT A21EA 2007070300122 20070703 00122 EA 2007 7 3 SWIA200718372 1 20070429 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 449SW 7699 FS 280 LBL9 AND RBL9 LOWER FRAMES ARE CRACKED, DISCOVERED AT C-CHECK. REPLACED FS 280 LBL9 INBOARD AND OUTBOARD CLIPS, FS 280 RBL9 INBOARD AND OUTBOARD CLIPS, AND REPAIR PARTS PER CRJ200 REO 601R 53-11-1177 REV 'A'. 2 L 7 2 4F RT A21EA 2007070300123 20070703 00123 EA 2007 7 3 SWIA200718373 1 20070429 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 449SW 7699 FS 484 INTERCOSTAL CRACKED AT RBL36.00, DISCOVERED AT C-CHECK. INSTALLED P/N 601R-53-41-059-2 ANGLE PER CRJ200 REO 601R -53-41-059 (REV A). 2 L 7 2 4F RT A21EA 2007070300124 20070703 00124 EA 2007 7 3 SWIA200718374 1 20070429 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 449SW 7699 FS484 INTERCOSTAL CRACKED AT LBL36.00, DISCOVERED AT C-CHECK. INSTALLED P/N 601R-53-41-059-1 ANGLE PER CRJ200 REO 601R- 53-41-059 (REV A). 2 L 7 2 4F RT A21EA 2007070300125 20070703 00125 EA 2007 7 3 SWIA200718375 1 20070429 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA PAX DOORWAY CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 449SW 7699 PASSENGER DOOR SILL IS CORRODED AT CENTER AND AFT SECTIONS DISCOVERED AT C-CHECK. REMOVED CORROSION FROM PAX DOOR SILL FRAME AT CENTER AND AFT SECTIONS PER CRJ200 SRM 51-21-06 PG 1. 2 L 7 2 4F RT A21EA 2007070300126 20070703 00126 EA 2007 7 3 SWIA200718376 1 20070429 A 5320 THRESHOLD CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOORWAY CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 449SW 7699 SERVICE DOOR THRESHOLD IS SEVERELY CORRODED, DISCOVERED AT C-CHECK. INSTALLED NEW SERVICE DOOR THRESHOLD PER CRJ200 SRM 51-41-02 PG 5. 2 L 7 2 4F RT A21EA 2007070300127 20070703 00127 EA 2007 7 3 SWIA200718377 1 20070510 A 5346 BEAM CNDAIR CL600 CL6002B19 1900309 EA CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 930SW 7713 ENGINE SUPPORT BEAM UPPER WEB FOUND TO BE CRACKED AT STA 640 AND RBL 8, DISCOVERED AT C-CHECK. INSTALLED UPPER DOUBLER, FILLER, SHIMS, AND ANGLES PER REO 601R-53-61-345 REV D. 2 L 7 2 4F RT A21EA 2007070300128 20070703 00128 EA 2007 7 3 SWIA200718378 1 20070510 A 5346 BEAM CNDAIR CL600 CL6002B19 1900309 EA CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 930SW 7713 ENGINE SUPPORT BEAM LEFT LOWER WEB CUTOUT IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED REPAIR FILLER, DOUBLER, SHIM AND ANGLE ON LOWER LEFT WEB PER CRJ200 REO 601R 53-61-358 REV A PG 1-4. 2 L 7 2 4F RT A21EA 2007070300129 20070703 00129 EA 2007 7 3 SWIA200718379 1 20070510 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 930SW 7713 ENGINE SUPPORT BEAM RIGHT LOWER WEB IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED REPAIR DOUBLER, WEB FILLER, SHIM, STRA P AND ANGLE PER CRJ200 REO 601R 53-61-358 REV A. 2 L 7 2 4F RT A21EA 2007070300130 20070703 00130 EA 2007 7 3 SWIA200718380 1 20070510 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 930SW 7713 FS 280 FLOOR SUPPORT BEAM IS CRACKED AT LBL9, DISCOVERED AT C-CHECK. INSTALLED INBOARD AND OUTBOARD CLIPS AT LBL9 FS280 FLOOR SUPPORT AND REPAIR ANGLE PER CRJ200 REO 601R53-171 REV C. 2 L 7 2 4F RT A21EA 2007070300131 20070703 00131 EA 2007 7 3 SWIA200718381 1 20070510 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 930SW 7713 FS 280 FLOOR SUPPORT BEAM IS CRACKED AT RBL9, DISCOVERED AT C-CHECK. REPAIRED LOWER SUPPORT BEAM AND INBOARD OUTBOARD C LIPS AT FS 280 RBL9 PER CRJ200 REO 601R-53-11-171 REV "C". 2 L 7 2 4F RT A21EA 2007070300132 20070703 00132 EA 2007 7 3 SWIA200718382 1 20070510 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 640 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 930SW 7713 STA 640 LEFT FRAME REINFORCEMENT DOUBLER IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED NEW STA640 FRAME DOUBLER PER CRJ SRM 51-42-06/51-42-21. 2 L 7 2 4F RT A21EA 2007070300133 20070703 00133 EA 2007 7 3 SWIA200718383 1 20070510 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 640 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 930SW 7713 STA 640 RIGHT SIDE FRAME REINFORCEMENT DOUBLER IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED STA640 RIGHT SIDE FRAME DOU BLER PER CRJ200 SRM 51-42-06 AND 51-42-21. 2 L 7 2 4F RT A21EA 2007070300134 20070703 00134 EA 2007 7 3 SWIA200718384 1 20070522 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT WW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 506CA 7793 RIGHT WHEEL WELL TRANSDUCER BRACKET IS CRACKED, DISCOVERED AT C-CHECK. REPLACED TRANSDUCER BRACKET PER CRJ200 SRM 51-42 -06 PG 11 ITEM 9 AND PG 15 FIG 8. 2 L 7 2 4F RT A21EA 2007070300135 20070703 00135 EA 2007 7 3 SWIA200718385 1 20070522 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT WW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 506CA 7793 LEFT WHEEL WELL TRANSDUCER BRACKET IS CRACKED, DISCOVERED AT C-CHECK. REPLACED TRANSDUCER BRACKET PER CRJ200 SRM 51-42- 06 PG 11 ITEM 9 AND PG 15 FIG 8. 2 L 7 2 4F RT A21EA 2007070300136 20070703 00136 EA 2007 7 3 SWIA200718386 1 20070522 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 506CA 7793 STA 280 UPPER SUPPORT ANGLES LBL 9 AND RBL 9 ARE CRACKED, DISCOVERED AT C-CHECK. INSTALLED REPLACEMENT PARTS AT STA 280 LBL9 AND RBL9 PER REO 601R-53-11-136 REV NC. 2 L 7 2 4F RT A21EA 2007070300137 20070703 00137 EA 2007 7 3 SWIA200718387 1 20070522 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 506CA 7793 PAX DOOR AFT WEB STEPS 1 AND 2 ARE CRACKED, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS ON AFT SIDE OF PAX DOOR PER R EO 601R 52-11-702 REV A. 2 L 7 2 4F RT A21EA 2007070300138 20070703 00138 EA 2007 7 3 SWIA200718388 1 20070522 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 506CA 7793 PAX DOOR FORWARD WEB IS CRACKED AT THE CORNER OF STEP 1 AND STEP 2, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS ON FO RWARD WEB PER CRJ200 REO 601R 52-11-702 REV A STEPS 8-17. 2 L 7 2 4F RT A21EA 2007070300139 20070703 00139 EA 2007 7 3 SWIA200718389 1 20070618 A 2780 TORQUE TUBE CNDAIR CL600 CL6002C10 1390015 EA SLATS DISCONNECTED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 609SK 10020 SLATS FAIL CAUTION MESSAGE AFTER TAKEOFF. RETURNED TO BIL. RECONNECTED TORQUE TUBE IAW CRJ 700 MM 27-81-01 AND RIGGED IAW CRJ 700 M 27-81-00. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007070300140 20070703 00140 EA 2007 7 3 SWIA200718390 1 20070624 A 5240 ROLLER CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 405SW 7029 SERVICE DOOR IS DIFFICULT TO OPEN. REPLACED CAM ROLLER ON SERVICE DOOR INNER HANDLE ROLLER LATCH IAW MM 52-41-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007070300141 20070703 00141 EA 2007 7 3 SWIA200718391 1 20070620 A 2120 UNKNOWN CNDAIR CL600 CL6002D24 1390016 EA CABIN ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 810SK 15093 CREW REPORTS STRONG FUEL ODOR FROM FORWARD AND AFT LAVS. PERFORMED CLEANING AND FLUSHING PROCEDURES IAW MONOGRAM CMM 38 -35-04 ON BOTH THE FORWARD AND AFT LAVS. SNIFFER INDICATED AIR CONCENTRATION IS WITHIN LIMITS. 2 L 7 2 4F RT A21EA 2007070300180 20070703 00180 NM 2007 7 3 QXEA200701037 1 20070624 A 2420 28B5551 GENERATOR BOMBDR DHC8 DHC8402 1390042 NM NR 2 INTERMITTENT A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 400QX 6497 6497 4030 SEA FLIGHT 2332: THE NR 2 AC GENERATOR LIGHT COMES ON INTERMITTENTLY. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE REMOVED AND REPLACED THE NR 2 AC GENERATOR IAW Q400 TASK CARD 6242101. SYSTEM OPS CHECK GOOD IAW Q400 AMM 24-21-00-710-801. AI RCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007070300181 20070703 00181 NM 2007 7 3 QXEA200701038 1 20070622 A 5100 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 414QX 4061 SEA FLIGHT NR 2312: DURING CLIMB, BOTH FA'S REPORTED A 1/4 INCH WIDE BY 2 INCH LONG CRACK IN BOTTOM LEFT REAR OF L2. DU RING LANDING FA REPORTED DOOR MOVEMENT AND EXPANSION OF CRACK. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED AFT P ASSENGER DOOR SEAL WITH NO DEFECTS NOTED. CLEANED SEAL AND OPENING. PRESSURIZED A/C IAW Q400 AMM 21-00-00, TR 21-048. NO DEFECTS NOTED. NO FLUXIONS IN FLIGHT DECK AND NO GAP AND NO CRACK NOTED AFTER PRESSURIZATION. PERFORMED OPS TEST O F AFT PASSENGER DOOR IAW AMM 52-12-00-710-802. NO DEFECTS NOTED. DOOR OPERATES NORMALLY. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007070300182 20070703 00182 NM 2007 7 3 QXEA200701035 1 20070624 A 2930 9752535 SWITCH BOMBDR DHC8 DHC8402 1390042 NM ISOLATION VALVE FAILED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 428QX 4160 PDX FLIGHT NR 2454: NR 3 HYD PRESSURE INDICATION INOPERATIVE. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE REPLACED NR 3 IS O VALVE SWITCH ASSEMBLY. OPERATED NR 3 HYD SYSTEM. ALL INDICATIONS AND OPERATIONS NORMAL. AIRCRAFT RETURNED TO SERVIC E. 2 H 7 2 4T RT A13NM 2007070300183 20070703 00183 EU 2007 7 3 AWXA200700772 1 20070624 A 5322 D53470494000 SHEAR WEB AIRBUS 320 A320231 3930325 EU ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 SAL - CORROSION ON BULK CARGO COMPARTMENT SHEAR WEB, FR 62 TO FR 63, S38L. REPLACED BULK CARGO COMPARTMENT SHEAR WEB, F R 62 TO FR 63, S38L IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007070300184 20070703 00184 EU 2007 7 3 AWXA200700773 1 20070624 A 5320 D53472189204 DUMMY RAIL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 667AW 1710 SAL - MAJOR REPAIR - CORROSION ON CABIN DUMMY RAIL, FR 67 + 18", -Y1162. REPLACED CABIN DUMMY RAIL, FR 67 + 15" - FR 68 + 4", -Y1162 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007070300185 20070703 00185 EU 2007 7 3 AWXA200700774 1 20070624 A 5320 D53472172205 DUMMY RAIL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 667AW 1710 SAL - MAJOR REPAIR - CORROSION ON CABIN DUMMY RAIL, FR 66 + 4" - FR 67 + 15", -Y1162 TO -Y1292. REPLACED CABIN DUMMY RA IL, FR 66 + 4" - FR 67 + 15", -Y1162 TO -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007070300186 20070703 00186 EU 2007 7 3 AWXA200700775 1 20070624 A 5320 D53472190211 DUMMY RAIL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 667AW 1710 SAL - CORROSION ON CABIN DUMMY RAIL, FR 65 + 21", -Y1292. REPLACED CABIN DUMMY RAIL, FR 64 - FR 66, -Y1292 IAW A320 S RM 51-72-11. 2 L 7 2 4F RT A28NM 2007070300187 20070703 00187 EU 2007 7 3 AWXA200700776 1 20070622 A 5347 D57130147200 SEAT TRACK AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 667AW 1710 SAL - MAJOR REPAIR - CORROSION ON CABIN SEAT TRACK, -Y765, FR 38 +13", FR 39+ 4.5" AND FR 40+ 14". REPLACED CABIN SEAT TRACK, -Y765, FR 36 - FR 41 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007070300188 20070703 00188 EU 2007 7 3 AWXA200700777 1 20070622 A 5347 D53371110070 SEAT TRACK AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 667AW 1710 SAL - MAJOR REPAIR - CORROSION ON CABIN SEAT TRACK, -Y765, FR 41 + 10.5", FR 42, FR 42 + 18", FR 46 + 16". REPLACED CAB IN SEAT TRACK, -Y765, FR 41 - FR 47 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007070300189 20070703 00189 NM 2007 7 3 HALA0700267 1 20070618 A 3210 4935815503 BUSHING BOEING 717 717200 1383700 NM RT MLG DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 486HA 55131 RT GEAR FWD TRUNNION NR 2 SPACER PITTED AT APPROX 10 O'CLOCK POSITION. REMOVED AND REPLACED NR 3 BUSHING AND SPACER ON RT MLG HOUSING BORE PER CMM 57-40-1. EDGE SEAL PENDING. SEALED EDGE PER BOEING OVERHAUL MANUAL 57-40-1. 2 L 7 2 4F TR A6WE 2007070300190 20070703 00190 WP 2007 7 3 AALA20071097 1 20070613 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 572AA 49458 BOS - EMERGENCY EXIT LIGHT AT SEAT ROW 8 INOPERATIVE. REPAIRED CONNECTOR FOR EMERGENCY EXIT LIGHT AT SEAT ROW 8. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007070300191 20070703 00191 NE 2007 7 3 AALA20071119 2 20070617 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE POWER LOSS A AALA A UNSCHED LANDING R E J PARTIAL RPM/PWR LOSS VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 21 7536A 49990 717851 DFW INFLIGHT T1412/17JUN - DURING CLIMB HEARD THUMP AND FELT VIBRATION THROUGHOUT AIRCRAFT. RIGHT ENGINE ROLLED BACK T O IDLE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND METAL DEBRIS IN TAIL CONE. REPLACED RIGHT ENGINE ON 18JUN2 007 AT DFW. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007070300192 20070703 00192 NM 2007 7 3 AALA20071124 1 20070618 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 MIA - OVERHEAD EMERGENCY LIGHT AT SEAT 30C INOPERATIVE. RELAMPED OVERHEAD EMERGENCY EXIT LIGHT AT SEAT 30C. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007062800167 20070628 00167 EU 2007 6 28 2007UALA02094 1 20070618 A 5340 STRUCTURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 435UA 613 FWD PIT HAS CLEAT WITH CORROSION AT FR33 AND STR 41R. MAJOR REPAIR ACCOMPLISHED: REPLACED CLEAT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062800168 20070628 00168 NM 2007 6 28 2007UALA02095 1 20070618 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 FWD ENTRY DOOR LOWER HINGE CUTOUT IN FUSELAGE HAS TWO FASTENER HOLES WITH CRACK INDICATIONS LOCATED APPROXIMATELY 1 INCH ABOVE AND 1 INCH FWD END OF LOWER HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED STAINLESS DOUBLER & FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062800169 20070628 00169 NM 2007 6 28 2007UALA02096 1 20070618 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 FWD ENTRY DOOR UPPER HINGE CUTOUT IN FUSELAGE HAS ONE FASTENER HOLE WITH CRACK INDICATION LOCATED APPROXIMATELY 1 INCH B ELOW FWD END OF UPPER HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED STAINLESS DOUBLER & FILLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062800170 20070628 00170 NM 2007 6 28 2007UALA02097 1 20070618 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 UPPER FUSELAGE SKIN CRACKED AT CHEM-MILLED STEP BELOW STR 12L AT BS 518 TO BS 519. MAJOR REPAIR ACCOMPLISHED: FABRICAT ED & INSTALLED EXTERNAL DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062800171 20070628 00171 NM 2007 6 28 2007UALA02098 1 20070618 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 RIGHT AFT LOWER FUSELAGE HAS A DENT APPROX 13 INCHES LONG BELOW AFT CARGO DOOR CUTOUT, 2 INCHES INBOARD OF STR 25R SKIN LAP BETWEEN BS 827-847. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SKIN & CORRODED BEAR STRAP. INSTALLED EXTERNAL SKI N DOUBLER-TRIPLER & STRUCTURAL FILLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007062800172 20070628 00172 NM 2007 6 28 2007UALA02099 1 20070618 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 847, CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 AFT PIT, BS 847, STR 26R, BEAR STRAP CORRODED ON UPPER SURFACE AND IS EMITTING CORROSION BETWEEN STRAP & SKIN (SKIN BULG ING). MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED SHEAR TIE DOUBLER REPAIR. BEAR STRAP REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007070300193 20070703 00193 WP 2007 7 3 AALA20071118 1 20070616 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 44503 49797 LGA - OVERHEAD EMERGENCY EXIT LIGHT AT SEAT ROWS 3 TO 8 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY EXIT LIGHT AT SEAT ROWS 3 TO 8. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007070300194 20070703 00194 NM 2007 7 3 AALA20071125 1 20070618 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 MIA - OVERHEAD EMERGENCY EXIT LIGHT AT SEAT 4B INOPERATIVE. RELAMPED OVERHEAD EMERGENCY EXIT LIGHT AT SEAT 4B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007070300195 20070703 00195 EU 2007 7 3 AALA20071126 1 20070613 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80084 675 JFK - EMERGENCY EXIT LIGHTS AT SEAT ROWS 19G TO 28G INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS AT SEA T ROWS 19G TO 28G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007070300196 20070703 00196 EU 2007 7 3 AALA20071117 1 20070616 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 34078 615 MIA - EMERGENCY EXIT LIGHT AT SEAT 9C INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT SEAT 9C. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A35EU 2007070300197 20070703 00197 NM 2007 7 3 AALA20071109 1 20070615 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 773AN 29583 JFK - EMERGENCY EXIT LIGHT AT SEAT ROW 30C MISSING LENS. REPLACED LENS FOR EMERGENCY EXIT LIGHT AT SEAT ROW 30C. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007070300198 20070703 00198 NM 2007 7 3 AALA20071110 1 20070615 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 350AN 33089 MIA - OVERHEAD EMERGENCY EXIT LIGHT AT SEAT 21B INOPERATIVE. RELAMPED OVERHEAD EMERGENCY EXIT LIGHT AT SEAT 21B. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007070300199 20070703 00199 NM 2007 7 3 AALA20071103 1 20070614 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 782AN 30003 ORD - EMERGENCY EXIT LIGHT AT LEFT NUMBER THREE DOOR MISSING COVER. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT LEFT NUMB ER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007070300200 20070703 00200 WP 2007 7 3 AALA20071098 1 20070613 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 572AA 49458 BOS - EMERGENCY EXIT LIGHT AT SEAT ROW 31 INOPERATIVE. REPAIRED CONNECTOR FOR EMERGENCY EXIT LIGHT AT SEAT ROW 31. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007070300201 20070703 00201 NM 2007 7 3 AALA20071102 1 20070614 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 353AA 24034 JFK - EMERGENCY EXIT LIGHT AT LEFT AND RIGHT NUMBER FOUR DOORS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LI GHT AT LEFT AND RIGHT NUMBER FOUR DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007070300204 20070703 00204 NM 2007 7 3 UPS07450030 1 20070531 A 5320 WEB BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C M/D HORIZONTAL SUPPORT WEB FOUND CRACKED JUST AT BS 820 STR 10L. (CRACK LENGTH .75 INCH). M/DECK BS 820 STR 10L HORIZONTAL SUPPORT WEB REPAIRED AS PER SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 2007070300205 20070703 00205 NM 2007 7 3 UPS07550009 1 20070610 A 5532 175N20013 PANEL BOEING 757 75724APF 1384969 NM VERTICAL STAB DEBONDED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 407UP 23729 INSPECTION TYPE:C DEF: D352152 AND EO B757-5530-26995- DAMAGE TO VERTICAL STAB LOWER SIDE PANEL DISBONDED INNER & OUTER SKIN AT SAME LOCATION. ACCOMPLISHED LEFT VERTICAL PANEL REPAIR IAW FINAL EA 757-5530-27-A1685 AND UPS ENG FILE NUMBER 7 57-55-20029 WITH NO DEVIATIONS. 2 L 7 2 4F RT A2NM 2007070300209 20070703 00209 NM 2007 7 3 SB07049 1 20070623 A 3230 BACC18Z7R CIRCUIT BREAKER BOEING 737 737401 1384701 NM COCKPIT FAULTY A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 425US 23992 CLT FLT1053 JUST AFTER TAKEOFF FROM CLT, EN ROUTE TO NAS, CREW COULD NOT RAISE THE LANDING GEAR HANDLE. CREW FOLLOWED Q UICK REFERENCE HANDBOOK PROCEDURES AND THEN RAISED THE GEAR. FOUND THE -LANDING GEAR LATCH & PRESSURE WARNING- CIRCUIT BREAKER POPPED. CONSULTED WITH DISPATCH AND MAINTENANCE AND RETURNED TO FIELD AT CLT. FLIGHT LANDED WITHOUT FURTHER IN CIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE -LANDING GEAR LATCH & PRESSURE WARNING- CIRCUIT BREAKER C00129. ACCOMPLISHED MAIN AND NOSE LANDING GEAR EXTENSION AND RETRACTION CHECKS PER MM 32-32-00-715 AND MM 32- 33-00-735. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007070300211 20070703 00211 EU 2007 7 3 SA07044 1 20070624 A 2730 PITCH CONTROL AIRBUS A319 A319112 3930323 EU PITCH SYSTEM MALFUNCTIONED A USAA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 EA 19 753US 1326 PHL FLT 1099 EN ROUTE PHL TO LAX. AFTER TAKEOFF, THE AIRCRAFT REQUIRED FORWARD CONTROL STICK INPUT IN ORDER TO MAINTAI N CORRECT ATTITUDE. THE FLIGHT RETURNED TO FIELD AN LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. 2 L 7 2 4F RT A28NM 2007070300219 20070703 00219 SO 2007 7 3 FDKA200700140 1 20070329 A 7331 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO FUEL SYSTEM MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 847MJ 145517 FDM 6000 FLL-MCO (0616 PHX LCL). ABORTED T/O AND RTG DUE TO FUEL 1 AND 2 LOW PSI WARNING MESSAGE. CREW PERFORMED ENGIN E RUNS WITH NO DEFECTS NOTED, OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007070300222 20070703 00222 NM 2007 7 3 FDKA200704148 1 20070401 A 5210 STRUT DHAV DHC8 DHC8102 2809003 NM DOOR DEFECTIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 806LR 093 FDM 6144 BWI-JFK (0821 PHX LCL) DOOR WILL NOT CLOSE. MX REMOVED AND REPLACED DOOR STRUT. 2 H 7 2 4T RT A13NM 2007070300223 20070703 00223 SO 2007 7 3 FDKA200704149 1 20070404 A 5230 HANDLE EMB 145 EMB145LR 3260212 SO CARGO DOOR UNSECURE A FDKA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 07 831MJ 145273 FLT 6005 ATL-ROA (0745 PHX LCL). CREW ABORTED T/O DUE TO BAGGAGE DOOR WARNING INDICATION. RAMP REPORTED DOOR HANDLE WA S NOT SECURED FULLY. MX INSPECTED DOOR, NO DEFECTS. 2 L 7 2 4T RT T00011AT 2007070300224 20070703 00224 SO 2007 7 3 FDKA200704151 1 20070408 A 2760 14533022409 CONTROL UNIT EMB 145 EMB145LR 3260212 SO SPOILER SYS FAILED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 835MJ 14476 145353 FDM 6010 RDU-FLL (0534 PHX LCL). RTG DUE TO SPOILER FAIL MESSAGE ON TAXI. MX REPLACED THE SPOILER CONTROL UNIT AND OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007070300228 20070703 00228 NM 2007 7 3 FDKA200704159 1 20070417 A 2751 44281508011 INDICATOR DHAV DHC8 DHC8101 2809002 NM T/E FLAP FAILED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 802LR 1449 205 FDM 6208 PHL-JFK (1732 PHX LCL). AIRCRAFT RETURNED TO THE GATE DUE TO RIGHT STALL WARNING LIGHT. MX REMOVED AND REPLAC ED FLAP POSITION INDICATOR. 2 H 7 2 4T RT A13NM 2007070300229 20070703 00229 SO 2007 7 3 FDKA200704160 1 20070420 A 5240 MECHANISM EMB 145 EMB145LR 3260212 SO SERVICE DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 FDM 6108 MCO-HSV (1123 PHX LCL). SERVICE DOOR WOULD NOT CLOSE. MX LUBED DOOR AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2007070300230 20070703 00230 NM 2007 7 3 ZZDA070622182 1 20070622 A 2913 861555 PUMP BOEING 717 717200 1383700 NM HYDRAULIC SYS INOPERATIVE A ZZDA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 15 940AT 55004 ON TAKEOFF RECEIVED -A- RIGHT HYD PRESSURE LOW, RIGHT QUANTITY LOW, AND HYDRAULIC POWER OFF. THERMAL PLUG BLOWN, REMOVE D AND REPLACED NR 2 EDP AND ELECTRIC AUX PUMP. SERVICED SYSTEM, ALL OPS NORMAL. 2 L 7 2 4F TR A6WE 2007070300233 20070703 00233 SO 2007 7 3 FDKA200704168 1 20070405 A 5320 14525480603 BEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 848MJ 145530 THE CARGO DOOR THRESHOLD IS CORRODED BEYOND ALLOWABLE LIMITS. REMOVED AND REPLACED BEAM. 2 L 7 2 4T RT T00011AT 2007070300236 20070703 00236 NM 2007 7 3 FDKA200704170 1 20070425 A 5220 DOOR DHAV DHC8 DHC8102 2809003 NM EMERGENCY EXIT LEAKING A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 801LR 047 FDM 6183 MHT-JFK (1935 PHX LCL). ROW 1CD EMERGENCY EXIT DOOR LEAKING IN FLIGHT. MX CLEANED DOOR AND RESEATED. 2 H 7 2 4T RT A13NM 2007070300237 20070703 00237 SO 2007 7 3 FDKA200704173 1 20070420 A 5320 14529150007 ANGLE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 852MJ 145567 FLOOR CROSSBEAM ANGLE, ABOVE FRAME 23, JUST TO THE RIGHT OF THE CENTER LINE IS CORRODED BEYOND ALLOWABLE LIMITS. REMOVE D AND REPLACED CROSSBEAM ANGLE. 2 L 7 2 4T RT T00011AT 2007070300238 20070703 00238 WP 2007 7 3 ABXA070194 1 20070521 A 5230 4920233505 MOUNT DOUG DC9 DC932F 3022067 WP AFT CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 UPPER STOP MOUNT ON AFT LOWER CARGO DOOR FORWARD FLANGE WAS CRACKED. REMOVED AFT LOWER CARGO DOOR. REPLACED HINGE. RE INSTALLED DOOR AND TESTED DOOR WARNING IAW DC9 MM 51-31-00. 2 L 7 2 4F A6WE 2007070300241 20070703 00241 WP 2007 7 3 ABXA070203 1 20070612 A 5320 9921839 ATTACH BRACKET DOUG DC9 DC932F 3022067 WP CARGO BAY CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 FORWARD LOWER CARGO ATTACH BRACKETS CORRODED AT NUT PLATES - STA 389 AND 408, LEFT BUTT LINE 33. REMOVED CORROSION AT S TA 389 AND 408, LEFT BUTT LINE 33 IAW DC9 SRM. 2 L 7 2 4F A6WE 2007070300243 20070703 00243 WP 2007 7 3 ABXA070188 1 20070521 A 5320 99236693 STRUCTURE DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 CORROSION ON SUBFLOOR AT APPROXIMATELY FS 178, RIGHT BUTT LINE 44 - 54. REPAIRED DAMAGED AREA IAW DC9 SRM 53-01 AND DWG 9923669. 2 L 7 2 4F A6WE 2007070300247 20070703 00247 WP 2007 7 3 ABXA070191 1 20070522 A 5347 S2914913M2400 SEAT TRACK DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 SEAT TRACK CORRODED AT FS 590, LEFT BUTT LINE 22.5 AT SPLICE. REMOVED AND REPLACED SEAT TRACK LEFT BUTT LINE 22.5, FS 5 90 - 661 IAW DC9 SRM 51-30-1 AND 51-10-4. 2 L 7 2 4F A6WE 2007070300248 20070703 00248 WP 2007 7 3 ABXA070192 1 20070522 A 5347 S4925848M36000 SEAT TRACK DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 CENTER SEAT TRACK CORRODED AT FS 590. REMOVED AND REPLACED SEAT TRACK IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 2007070300249 20070703 00249 WP 2007 7 3 ABXA070193 1 20070529 A 5347 S2914913M24000 SEAT TRACK DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 SEAT TRACK AT STA 237 - 313, LEFT BUTT LINE 22 UNDER FLOOR PANEL 2B WAS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW D C9 SRM 51-30-1. 2 L 7 2 4F A6WE 2007070300251 20070703 00251 WP 2007 7 3 ABXA070198 1 20070523 A 5320 99105035 CUSP WEB DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 LEFT CUSP WEB AT STA 960 CRACKED AT LIGHTNING HOLE. REPAIRED AREA IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 2007070900002 20070709 00002 WP 2007 7 9 AALA20071111 1 20070615 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 568AA 49349 LGA - EMERGENCY EXIT LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT AT FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007070900005 20070709 00005 WP 2007 7 9 AALA20071100 1 20070614 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 TPA - EMERGENCY EXIT LIGHT AFT OF FORWARD GALLEY MISSING LENS. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT LOWER AFT OF F ORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007070900006 20070709 00006 NM 2007 7 9 AALA20071105 1 20070614 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 378AN 25447 MIA - EMERGENCY LIGHT AT SEAT 35B INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 35B. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A1NM 2007070900007 20070709 00007 WP 2007 7 9 AALA20071106 1 20070614 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 LGA - EMERGENCY FLASHLIGHT AT AFT CABIN HAS BROKEN STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007070900012 20070709 00012 NM 2007 7 9 AALA20071101 1 20070614 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 353AA 24034 JFK - EMERGENCY EXIT LIGHT AT SEAT ROW 12HG INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT SEAT ROW 12HG. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007070900015 20070709 00015 WP 2007 7 9 AALA20071088 1 20070612 A 3350 LIGHT DOUG DC9 DC982 3022082 WP EMERGENCY EXIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7536A 49990 LGA - EXTERIOR EMERGENCY EXIT LIGHT AT RIGHT AFT OF CABIN INOPERATIVE. RECYCLED EMERGENCY EXIT LIGHTS. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007070900016 20070709 00016 NM 2007 7 9 AALA20071093 1 20070613 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 373AA 25200 MIA - EMERGENCY EXIT LIGHT AT LEFT NUMBER THREE ENTRY DOOR INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT LEFT NUMBER TH REE ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007070900018 20070709 00018 WP 2007 7 9 AALA20071115 1 20070616 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7548A 53030 LGA - EMERGENCY LIGHT AT OVERHEAD TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD T AIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007070900023 20070709 00023 WP 2007 7 9 AALA20071122 1 20070618 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 465A 49595 LGA - OVERHEAD EMERGENCY EXIT LIGHTS AT SEAT ROWS 20 TO 34 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY EX IT LIGHTS AT SEAT ROWS 20 TO 34. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007070900024 20070709 00024 NM 2007 7 9 AALA20071123 1 20070617 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7667A 25301 MIA - EMERGENCY EXIT LIGHT AT SEAT 14D INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007070900031 20070709 00031 WP 2007 7 9 AALA20071091 1 20070612 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7536A 49990 LGA - EMERGENCY EXIT LIGHT AT TAIL CAT WALK INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT TAIL CAT WALK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007070900032 20070709 00032 WP 2007 7 9 AALA20071089 1 20070612 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7536A 49990 LGA - EMERGENCY LIGHT AT OVERWING EXIT INOPERATIVE. RESECURED BATTERY PACK FOR EMERGENCY LIGHT AT OVERWING EXIT. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007070900036 20070709 00036 EU 2007 7 9 07FDEA02290 1 20070627 A 2750 4909505 COMPUTER AIRBUS 300 A300B4622R 3930312 EU NR 2 FAULTED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 722FD 15009 479 ATB - AFTER T/O - ECAM AND OVH SYS 2 FLAP FAULT. UNABLE TO CLEAR FAULT. FOUND NR 2 SFCC FAULTING MAIN CONTROL VALVE UP ON ARRIVAL. RESET SFCC AND RAN FLAPS, AGAIN FAULTED MAIN CONTROL VALVE. BOTH TIMES NR 2 FLAP SYS FAULT LIGHT ON OVERHE AD CAME ON AND WOULD NOT RESET. SWAPPED NR 2 AND NR 1 SFCC AND RAN FLAPS. FLAP SYS NR 1 BEGAN FAULTING. PUT BOXES BAC K IN ORIGINAL POSITION. PLACING BOX ON ORDER. RAN NR 2 ENG AND TIMED FLAPS WITH NR 2 SFCC BREAKERS PULLED PER AMM 27-5 4-00-5. ALL TIMES WERE WITHIN LIMITS AND FLAPS MOVED SYMMETRICALLY ON SYSTEM NR 1. REPLACED NR 2 SFCC FLAP/SLAT SYSTEM TEST OK PER MM 27-51-18-4 27-51-00-5. 2 L 7 2 4F RT A35EU 2007070900037 20070709 00037 NM 2007 7 9 07FDEA02291 1 20070627 A 5311 65561131 FRAME BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD PIT BILGE BODY FRAME SHEAR TIE IS BUCKLED/CORRODED BS 720A, STR 27L-28L, WL 148. REMOVED CORROSION, ORIGINAL .050", REMAINING- .045", MATERIAL LOSS- .005", WITHIN LIMITS REF SRM 51-10-1 AND 53-10-1, TOOL NR 2221 CAL DUE 4-24-08, STRAIG HTENED SHEAR TIE REF SRM 51-40-1, NDT. NO DEFECTS NOTED REF NDT -00-00 PT 6 FIG 23, TOOL NR IN22-0044, CAL DUE 5-21-08. TREATED AND PRIMED REF SRM 51-10-2, LEVEL 1 CORROSION. 2 L 7 3 4F RT A3WE 2007070900038 20070709 00038 NM 2007 7 9 07FDEA02292 1 20070627 A 5311 65561131 FRAME BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD PIT BILGE BODY FRAME, SHEAR TIE IS CORRODED, BS 720A, 2" OB OF STR 28R, WL 148. REMOVED CORROSION. ORIGINAL - .050 ", REMAINING - .046", MATERIAL LOSS - .004", WITHIN LIMITS REF SRM 53-10-1, TOOL NR 18172, CAL DUE 1-19-08. TREATED AND PRIMED REF 51-10-6 AND 51-10-2. LEVEL 1 CORROSION. 2 L 7 3 4F RT A3WE 2007070900039 20070709 00039 NM 2007 7 9 07FDEA02293 1 20070627 A 5720 652165849 PANEL BOEING 727 727233 138408A NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LT WING OB TE FLAP WELL LWR FIXED PANEL CORRUGATED SUPPORT PLATE IS CRACKED RSS 516-523. REPLACED CORRUGATED SPLICE IAW SRM 51-30-02. 2 L 7 3 4F RT A3WE 2007070900040 20070709 00040 NM 2007 7 9 07FDEA02294 1 20070627 A 5347 652363713 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 CABIN, LBL 25 SEAT TRACK IB FLANGE HAS CORROSION ON UPPER SURFACE BETWEEN BS 400 AND BS 460. REMOVED CORROSION IAW B72 7 SRM 51-10-1, ORIGINAL .080", REMAINING .059" REF EA NR 7- 5310-113056, ROTO PEENED SEAT TRACK FLANGE AT STA 400-460 LB L 25. TREATED AND PRIMED SEAT TRACK REF EA 7-5310-113056. 2 L 7 3 4F RT A3WE 2007070900041 20070709 00041 NM 2007 7 9 07FDEA02295 1 20070627 A 5311 65561131 FRAME BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD PIT BILGE, BODY FRAME SHEAR TIE IS CORRODED, BS 72OF STR 28L- 28R, WL148. REMOVED CORROSION, REFERENCING SRM 51-10 -1, ORIGINAL THICKNESS .072", BLENDED TO .067" MATERIAL LOSS .005" WITHIN LIMITS, REFERENCING SRM MEASURED WITH TOOL N R IN17-9593 CAL DUE 5-16-08 TREATED AND PRIMED REF SRM 51-10-2. LEVEL 1 CORROSION 2 L 7 3 4F RT A3WE 2007070900042 20070709 00042 WP 2007 7 9 07FDEA02299 1 20070622 A 4920 ENGINE HONEYWELL DOUG DC10 DC1030F 3023504 WP APU FAILED A FDEA O OTHER C F.O.D. NR NOT REPORTED 1 SO 25 311FE P90675 46871 RETURN TO RAMP DUE TO INABILITY TO SHUT DOWN APU. FOUND PORTIONS OF N1 HAD EXITED DOWN PASSED APU AIR INLET BOOT AT CLA MPS, SLICED THRU APU PRESSURE OIL LINE AND THEN BECAME LODGED INTO APU COMPARTMENT ACCESS DOOR. APU REF WRI 52-40 2307 FOR THE APU ACCESS DOOR REPAIR. REMOVED AND REPLACED APU REF AMM 49-00-00-4. 2 L 7 3 4F RT A22WE 2007070900044 20070709 00044 NM 2007 7 9 HALA0700268 1 20070618 A 3210 4935813503 BUSHING BOEING 717 717200 1383700 NM LT MLG TRUNNION CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 486HA 55131 LT GEAR AFT TRUNNION NR 3 BUSHING PITTED AT APPROX 10 O'CLOCK POSITION. REMOVED AND REPLACED NR 4 BUSHING AND SPACER ON LT MLG HOUSING BORE PER CMM 57-40-1. EDGE SEAL PENDING. SEALED EDGE PER BOEING OVERHAUL MANUAL 57-40-1. 2 L 7 2 4F TR A6WE 2007070900053 20070709 00053 WP 2007 7 9 070129 1 20070624 A 2133 OUTFLOW VALVE DOUG DC9 DC983 3022083 WP CABIN PRESSURE OBSTRUCTED A WX0A A UNSCHED LANDING C J F.O.D. WARNING INDICATION CL CLIMB 1 WP 19 860GA 49786 AIRCRAFT 860 DEPARTED LAS FLT 418 AND CLIMBING THROUGH 18,000 FEET THE CABIN PRESSURIZATION FLOW LIGHT ILLUMINATED. CRE W WAS UNABLE TO EXTINGUISH LIGHT AND RETURNED TO LAS. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED THE PRESSURIZATION SYS TEM AND DISCOVERED INSULATION IN THE OUTFLOW VALVE LINKAGE. REMOVING THE DEBRIS THE PRESSURIZATION SYSTEM OPERATIONAL C HECK PERFORMED IN A SATISFACTORY CONDITION. THE AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007070900057 20070709 00057 NM 2007 7 9 NWAA07283146 1 20070626 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319114 3930350 NM EMERGENCY LIGHTS MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 346NB 9943 56 1796 CHARGER IS OVERCHARGING LEFT OVERWING EMERGENCY EXIT EPSU BATTERIES. REPLACED LEFT OVERWING EPSU, CHECKS OK. 2 L 7 2 4F RT A28NM 2007070900058 20070709 00058 NM 2007 7 9 NWAA072306301 1 20070625 A 3397 WIRE BOEING 747 747451 1384940 NM EMERGENCY LIGHTS DISCONNECTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 661US 23719 FLIGHT ATTENDANT REPORTED THAT B ZONE FLOOR RIGHT EMERGENCY LIGHTS ARE INOP. MAINTENANCE RECONNECTED LIGHT ASSEMBLY. O PERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007070900059 20070709 00059 EU 2007 7 9 COEA0711908 1 20070307 A 5320 S53571401209 PANEL AEROSP ATR42 ATR42300 8680920 EU BS 11660 SCRATCHED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 908FX 023 SCRATCHES FOUND ON RIGHT EXTERNAL FUSELAGE LOWER SKIN AT STRINGER 14R 2 INCHES FORWARD OF FR 25 CLOSE TO STATION 11660. REMOVED EXISTING REPAIR DOUBLER AND INSTALLED A STEEL DOUBLER, EXTENDED TO COVER CORRODED SKIN CUT OUT AT FRAME 25 STRI NGER 14 RT FOLLOWING REPAIR DWG 15S535R0211 ISSUE B IAW SRI DOTS-4103/06-7439. REF SRAS S535R0206...2734. (M) 2 H 7 2 4T RT A53EU 2007070900061 20070709 00061 EU 2007 7 9 COEA0712908 1 20070307 A 5330 S53671201200 PANEL AEROSP ATR42 ATR42300 8680920 EU FUSELAGE DENTED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 908FX 023 DENT FOUND ON EXTERNAL LT LATERAL UPPER SKIN PANEL AT STRINGER 10L ABD 3 INCHES FORWARD OF FRAME 40. REMOVED DAMAGE. F ABRICATED DOUBLER AND FILLER AND INSTALLED ON AC IAW ATR42 SRM. (M) 2 H 7 2 4T RT A53EU 2007070900064 20070709 00064 EU 2007 7 9 COEA0715908 1 20070307 A 5330 S53671305200 PANEL AEROSP ATR42 ATR42300 8680920 EU STR 14 DAMAGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 908FX 023 TOOLING DAMAGE FOUND ON RIGHT FUSELAGE LATERAL LOWER SKIN PANEL BELOW STRINGER 14R FROM FR 29 TO FR 30. DAMAGE REMOVED. FABRICATED REPAIR DOUBLER AND INSTALLED ON AIRCRAFT IAW ATR 42 SRM. (M) 2 H 7 2 4T RT A53EU 2007070900065 20070709 00065 EU 2007 7 9 COEA0706908 1 20070307 A 5414 S54310252200201 PANEL AEROSP ATR42 ATR42300 8680920 EU RT NACELLE DAMAGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 908FX 023 FRETTING DAMAGE FOUND ON RT NACELLE REBATE FLANGE COMMON TO PANEL 486AL AND 486AR. REPLACED FABRICATED REBATE PANELS IA W ATR SRM. (M) 2 H 7 2 4T RT A53EU 2007070900066 20070709 00066 EU 2007 7 9 COEA0707908 1 20070307 A 5330 S53671201200 PANEL AEROSP ATR42 ATR42300 8680920 EU FUSELAGE DAMAGED A COEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 13 908FX 023 TOOLING MARKS FOUND BEHIND ANGLE BRACKET AT FS 29 TO FR 30 AND STR 5L TO STR 6L ON SKIN OF LT LATERAL UPPER PANEL. FABR ICATED AND REPAIRED DOUBLER. INSTALLED AND COMPLETED REPAIR SCHEME IAW ATR SRM. (M) 2 H 7 2 4T RT A53EU 2007070900067 20070709 00067 EU 2007 7 9 COEA0708908 1 20070307 A 5313 S53571400216 STRINGER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 908FX 023 FOUND LEVEL 2 CORROSION ON STRINGER 16L 3 INCHES FORWARD OF FS 25. STRINGER 16L WAS REMOVED. STRINGER 16L WAS FABRICAT ED, HEAT TREATED AND INSTALLED ON AIRCRAFT IAW ATR SRM. (M) 2 H 7 2 4T RT A53EU 2007070900068 20070709 00068 EU 2007 7 9 COEA0709908 1 20070307 A 5330 S53571401209 PANEL AEROSP ATR42 ATR42300 8680920 EU FUSELAGE GOUGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 908FX 023 GOUGES DETECTED ON FUSELAGE SECTION 15RT FRAME 25 ON MLG STRUT ATTACHMENT FITTING HOLES. BUSHINGS INSTALLED ON FRAMES, NEW BUSHINGS INSTALLED ON SKIN AND STRAP AT FS 11RT MLG FITTING UPPER FORWARD HOLE PER SRI DO/TS-5448/06-8109, REF SRAS A/C MSN 023...614. (M) 2 H 7 2 4T RT A53EU 2007070900070 20070709 00070 NM 2007 7 9 NWAA072336716 1 20070624 A 5330 SKIN BOEING 747 747251F 1384898 NM BS 320-340 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 616US 21120 DURING "L" CHECK, FOUND CRACK IN FUSELAGE SKIN BETWEEN BS 320-340 S7L-S9L. REPAIRED PER EA 67-209718. 2 L 7 4 4F A20WE 2007070900077 20070709 00077 EU 2007 7 9 COEA0711903 1 20070109 A 5313 S53574300200 STRINGER AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 903FX 179 DURING HEAVY CHECK, FOUND CORROSION ON LT MLG KEEL BEAM SPECIAL STRINGER FROM FRAME 25 TO FRAME 27. REMOVED CORROSION F ROM KEEL BEAM STRINGER 21. REMOVED AND REPLACED SPECIAL STRINGER 21 IAW ATR42 SRM. (M) 2 H 7 2 4T RT A53EU 2007070900080 20070709 00080 EU 2007 7 9 COEA0708903 1 20070109 A 5330 S53671406200 SKIN AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 903FX 179 DURING HEAVY CHECK, FOUND CORROSION ON FUSELAGE SKIN COMMON TO VHF 1 LOWER ANTENNA MATING SURFACE. LEVEL 2 CORROSION RE QUIRED REPLACEMENT OF ANTENNA DOUBLER. REMOVED LOWER VHF 1 ANTENNA DOUBLER AND FABRICATED AND INSTALLED NEW DOUBLER IAW ATR42 SRM. (M) 2 H 7 2 4T RT A53EU 2007070900081 20070709 00081 NM 2007 7 9 HNAA0700123 1 20070627 A 5542 SKIN DHAV DHC8 DHC8102 2809003 NM RUDDER CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 912HA 040 SIX BLIND FASTENERS FOUND CORRODED ON RIGHT SIDE OF SKIN OF FORE RUDDER NEXT TO LOWER ACTUATOR FITTING. RIGHT SIDE OF S KIN OF FORE RUDDER NEXT TO ACTUATOR FITTING 6 BLIND FASTENERS REPLACED IAW RD8-55-024. 2 H 7 2 4T RT A13NM 2007070900082 20070709 00082 NM 2007 7 9 HNAA0700124 1 20070626 A 5730 857118018722005 PANEL DHAV DHC8 DHC8102 2809003 NM WING CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 912HA 040 ELEVEN CORRODED HOLES ON STRESS PANEL 521AT. ELEVEN BUSHINGS FABRICATED LOCALLY IAW WITH RD 8-53-2674 ACCESS PANEL 521 AT REPLACED ON SEQ 5042. 2 H 7 2 4T RT A13NM 2007070900083 20070709 00083 WP 2007 7 9 07FDEA02297 1 20070627 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 398FE 46634 RIGHT FUSELAGE SKIN HAS A DENT WITHIN 12 INCHES OF PRIMARY STATIC PORT. REPAIRED DENT BY CUTOUT AND EXTERNAL DOUBLER IA W MD/DC10 SRM 53-20-00 FIG 9 VOL I. REPAIR DOUBLER IS ACCEPTABLE FOR RVSM OPERATION IAW MD/DC 10 SRM 53-00-02 FIG1 SHEET 2 VOL I. THIS IS A CATAGORY B REPAIR INITIAL INSPECTION IS 34,000 AND REPETITIVE AT 24,000. 2 L 7 3 4F RT A22WE 2007070900084 20070709 00084 SO 2007 7 9 FDKA200706272 1 20070614 A 2710 CONNECTOR EMB 145 EMB145LR 3260212 SO CONTROLLER LOOSE A FDKA O OTHER O OTHER CR CRUISE 1 SW 07 825MJ 145179 FDM 5982 MCO-FLL (0510 PHX LCL). PITCH TRIM FAIL IN FLIGHT. MX RESET THE CONNECTOR ON HORIZONTAL CONTROL UNIT, OPS CHE CK GOOD. 2 L 7 2 4T RT T00011AT 2007070900085 20070709 00085 NM 2007 7 9 HNAA0700127 1 20070628 A 2822 CLAMP DHAV DHC8 DHC8102 2809003 NM FUEL BOOST PUMP DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 912HA 040 RIGHT WING AUX FUEL BOOST PUMP CLAMP RING FOUND DAMAGED AND CORRODED. RIGHT WING AUX FUEL BOOST PUMP CLAMP RING REPLACE D AS PER S/B 8-57-28, LEAK CHECK REF SEQ 23. 2 H 7 2 4T RT A13NM 2007070900134 20070709 00134 NM 2007 7 9 SWAA073157 1 20070624 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007070900135 20070709 00135 NM 2007 7 9 SWAA073154 1 20070624 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007070900136 20070709 00136 NM 2007 7 9 SWAA073167 1 20070625 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007070900137 20070709 00137 NM 2007 7 9 SWAA073181 1 20070625 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007070900138 20070709 00138 NM 2007 7 9 SWAA073161 1 20070623 A 3350 417A5700 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 251WN 32510 EEPLS LENS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007070900139 20070709 00139 NM 2007 7 9 SWAA073162 1 20070625 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 400WN 27891 EEPLS COVER MISSING AT ROW 3 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007070900140 20070709 00140 2007 7 9 SWAA073164 4 20070625 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 768SW 30587 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007070900141 20070709 00141 2007 7 9 SWAA073163 4 20070625 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 720WN 27854 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007070900142 20070709 00142 2007 7 9 SWAA073148 4 20070623 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 793SA 27888 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007070900143 20070709 00143 NM 2007 7 9 SWAA073147 1 20070623 A 2121 6454051 FAN BOEING 737 7377H4 1384404 NM E&E BAY FAULTY A SWAA K NONE O OTHER NR NOT REPORTED 1 SW 29 436WN 32456 F/A REPORTED A RUBBER SMELL AT MID CABIN. TURNED OFF RECIRCULATION FAN SMELL DISSIPATED. REMOVED AND REPLACED RECIRCUL ATION FAN PER MM. 2 L 7 2 4F RT A16WE 2007070900144 20070709 00144 NM 2007 7 9 SWAA073159 1 20070624 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM BS 506A S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506A, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007070900145 20070709 00145 NM 2007 7 9 SWAA073165 1 20070625 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 514C S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514C, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007070900146 20070709 00146 NM 2007 7 9 SWAA073170 1 20070625 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM BS 410 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER CUTOUT BS 410, LBL 3. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2007070900147 20070709 00147 NM 2007 7 9 SWAA073158 1 20070624 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM BS 485 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 485, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007070900148 20070709 00148 NM 2007 7 9 SWAA073156 1 20070624 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 739D S19R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739D, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007070900149 20070709 00149 NM 2007 7 9 SWAA073149 1 20070624 A 5315 6545810 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CRACKED AT BS 312, RBL 24. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007070900150 20070709 00150 NM 2007 7 9 SWAA073180 1 20070625 A 5315 6545833 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312-356 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM CORRODED AT BETWEEN BS 312 AND BS 356, STR 17L. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2007070900151 20070709 00151 NM 2007 7 9 SWAA073173 1 20070625 A 5311 65458805124 FRAME BOEING 737 7373H4 1384600 NM BS 277 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND BELTFRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007070900152 20070709 00152 NM 2007 7 9 SWAA073174 1 20070625 A 5311 6546538 FRAME BOEING 737 7373H4 1384600 NM BS 600 S13L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 600, STR 13L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071000002 20070710 00002 SO 2007 7 10 FDKA200705250 1 20070529 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 840MJ 145429 FLOOR EMERGENCY LIGHTS BY SEAT ROWS 12 TO AFT WERE INOPERATIVE. RESET WITH THE CREW AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2007071000005 20070710 00005 SO 2007 7 10 RAIA00706038 1 20070622 A 5730 14567011007 SKIN EMB 145 EMB145 3260210 SO LT WING CRACKED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 821HK 145068 STL - DURING INSPECTION, LT WING TRAILING EDGE SKIN WAS FOUND TO HAVE A 1.125 INCH CRACK PROPAGATING FROM RIVET TO TRAIL ING EDGE NEAR GROUND SPOILER ACTUATOR CUTOUT. MAINTENANCE INSPECTED IAW MANUFACTURER'S SERVICE INFORMATION AND PLACED O N TIME CARRYOVER FOR REOCCURRING INSPECTIONS AT 100 FH WITH DEFINITIVE REPAIR OR REPLACEMENT AT 500 FH. 2 L 7 2 4F RT T00011AT 2007071000012 20070710 00012 NM 2007 7 10 SWAA073191 1 20070626 A 5330 6545766 SKIN BOEING 737 7373A4 1384585 NM BS 578 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 578, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007071000014 20070710 00014 NM 2007 7 10 SWAA073192 1 20070626 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM BS 787 S23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 23L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007071000016 20070710 00016 NM 2007 7 10 SWAA073196 1 20070626 A 5311 6546539 FRAME BOEING 737 7375H4 138449D NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT LT BS 616, LOWER ATTACH FASTENERS WL 201. REPAIRED FRAME PE R SB. 2 L 7 2 4F RT A16WE 2007071000018 20070710 00018 NM 2007 7 10 SWAA073189 1 20070626 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071000019 20070710 00019 NM 2007 7 10 SWAA073198 1 20070626 A 5310 6546956 CREASE BEAM BOEING 737 7375H4 138449D NM BS 420-440 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 420 AND BS 440, LBL 69. REPAIRED CREASE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2007071000021 20070710 00021 NM 2007 7 10 SWAA073195 1 20070626 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 927 S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071000024 20070710 00024 NM 2007 7 10 HNAA00125 1 20070626 A 5240 PANEL DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 912HA 040 CORROSION FOUND IN VARIOUS PLACES IN LAV SERVICE PANEL. LAVATORY MACHINED SERVICE DOOR DOUBLER REPAIRED AS PER 8-53-07- 3235 AND INSTALLED WITH SOLID RIVETS AS PER SRM 51-40-00 HFEC CUTOUT NO CRACKS. 2 H 7 2 4T RT A13NM 2007071000028 20070710 00028 SO 2007 7 10 FDKA200705185 1 20070504 A 2720 14521333401 CONTROL PANEL EMB 145 EMB145LR 3260212 SO RUDDER SYSTEM MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 13989 145481 RUDDER SYSTEM 1 & 2 INOP MSG. MX REPLACED OVERHEAD CONTROL PANEL AND REPAIRED BLEED LEAK IN AFT AVIONICS. 2 L 7 2 4T RT T00011AT 2007071000030 20070710 00030 SO 2007 7 10 FDKA200705187 1 20070505 A 2720 SWITCH EMB 145 EMB145LR 3260212 SO RUDDER SYSTEM INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 840MJ 145429 RUDDER SYSTEM 2 SWITCH INOP. MX CLEANED SWITCH, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007071000033 20070710 00033 NM 2007 7 10 FDKA200705190 1 20070507 A 3150 UNKNOWN DHAV DHC8 DHC8101 2809002 NM UNKNOWN A FDKA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 802LR 205 ABORTED TAKEOFF DUE TO CONFIG WARN. CREW CYCLED ALL PARAMETERS, FAULT CLEARED. 2 H 7 2 4T RT A13NM 2007071000034 20070710 00034 SO 2007 7 10 FDKA200705191 1 20070507 A 3150 UNKNOWN EMB 145 EMB145LR 3260212 SO RUDDER UNKNOWN A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 852MJ 145567 RUDDER HARD OVER PROTECTION FAIL MESSAGE. MX RESET WITH THE FLIGHT CREW AND MESSAGES CLEARED, OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007071000035 20070710 00035 2007 7 10 FDKA200705192 4 20070507 A 2200 UNKNOWN EMB 145 EMB145LR 3260212 SO AUTOPILOT SYSTEM UNKNOWN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 854MJ 145490 AUTO PILOT ROLLED RIGHT IN FLIGHT AND AUTO PILOT FAILED IN FLIGHT. MX PERFORMED OPS CHECK OF AUTO PILOT SYSTEM AND OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007071000037 20070710 00037 SO 2007 7 10 FDKA200705194 1 20070508 A 2741 SWITCH EMB 145 EMB145LR 3260212 SO STAB TRIM DIRTY A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 853MJ 145464 STAB BACK UP TRIM INOPERATIVE IN UP POSITION. MX CLEANED SWITCH AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007071000038 20070710 00038 SO 2007 7 10 FDKA200705195 1 20070508 A 2720 M835362024M RELAY EMB 145 EMB145LR 3260212 SO RUDDER FAILED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 831MJ 145273 RETURNED TO GATE DUE TO RUDDER HARD OVER PROTECTION FAIL. MX REMOVED AND REPLACED RELAYS K0834, K0367. 2 L 7 2 4T RT T00011AT 2007071000040 20070710 00040 NM 2007 7 10 FDKA200705198 1 20070511 A 2910 HYDRAULIC SYSTEM DHAV DHC8 DHC8101 2809002 NM CONTAMINATED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 806LR 093 UPON FLAP EXTENSION RUD PRESS, RUD FULL PRESS, FLAP DRIVE & NR 1 ENG HYD PUMP CAUTION LIGHTS & FLAPS ARE SLOW TO EXTEND. MX BLED AIR FROM SYSTEM AND OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2007071000045 20070710 00045 SO 2007 7 10 FDKA200705207 1 20070516 A 2560 P2070009120 FLASHLIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 FDM 6159 RDU-FLL (1114 PHX LCL). F/A FLASHLIGHT INOP. MX REMOVED AND REPLACED FLASHLIGHT, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007071000047 20070710 00047 NM 2007 7 10 FDKA200705209 1 20070517 A 2720 6500757 SWITCH DHAV DHC8 DHC8101 2809002 NM RUDDER FAULTY A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 807LR 070 FDM 6159 ALB-JFK (0500 PHX LCL). FLIGHT CREW REPORTED RUDDER FULL PRESS, RUDDER PRESS, & NR 2 RUDDER HYD CAUTION LIGHTS ILLUMINATED IN FLT. MX REMOVED AND REPLACED RUDDER HYD CUTOFF SWITCH. 2 H 7 2 4T RT A13NM 2007071000048 20070710 00048 NM 2007 7 10 FDKA200705212 1 20070518 A 3150 SWITCH DHAV DHC8 DHC8101 2809002 NM COCKPIT DIRTY A FDKA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 07 802LR 205 FDM 6189 BDL. ABORTED T/O DUE TO T/O WARNING HORN GOES OFF ON T/O ROLL. MX CLEANED THROTTLE AND FLAP MICRO SWITCHES, O P CHECKS GOOD. 2 H 7 2 4T RT A13NM 2007071000049 20070710 00049 SO 2007 7 10 FDKA200705213 1 20070518 A 5210 HANDLE EMB 145 EMB145LR 3260212 SO PAX DOOR OUT OF ADJUST A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 852MJ 145567 FDM 5998 ATL-GPT (1131 PHX LCL). MAIN CABIN DOOR HARD TO OPEN. MX ADJUSTED INNER HANDLE, OPS GOOD. 2 L 7 2 4T RT T00011AT 2007071000051 20070710 00051 SO 2007 7 10 FDKA200705217 1 20070519 A 2750 FLAP EMB 145 EMB145LR 3260212 SO WING MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 850MJ 145568 FDM 5989 MCO (1625 PHX LCL). FLAP LOW SPEED. MX RESET SYSTEM, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007071000052 20070710 00052 NM 2007 7 10 FDKA200705215 1 20070520 A 2720 RELAY DHAV DHC8 DHC8101 2809002 NM RUDDER FAILED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 808LR 073 FDM 6205 RUDDER PRESS LIGHT FAILED TO ILLUMINATE. ACFT FERRIED TO JFK WHERE MX REPLACED RELAY, OPS CHECK WAS GOOD. 2 H 7 2 4T RT A13NM 2007071000053 20070710 00053 NM 2007 7 10 FDKA200705216 1 20070520 A 2797 CONNECTOR DHAV DHC8 DHC8101 2809002 NM RUDDER DIRTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 808LR 073 FDM 6178 JFK (1415 PHX LCL) RETURNED TO GATE DUE TO RUDDER PRESS LIGHT FAILED TO ILLUMINATE. MX CLEANED CONNECTOR. 2 H 7 2 4T RT A13NM 2007071000057 20070710 00057 NM 2007 7 10 DHL2007785003 1 20070627 A 5710 6521655461 BEAM BOEING 727 727214 138407R NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 RT WING T/E UPPER EXTRUDED "I" BEAM HAS A .375" CRACK AT RWBL 114. ROUTED OUT CRACK; MATERIAL REMOVED BEYOND SERVICE LI MITS PER B727 SRM 57-20-1 FIG 2. REMOVED "I" BEAM, FABRICATED NEW BEAM FROM BAC1506-1659 EXTRUSION, 85.5" IN LENGTH, PO NR 72485, PER B727 SRM 51-20-1 AND BAC DWG 65-21655 REV J. TREATED, PRIMED, AND INSTALLED NEW "I" BEAM PER B727 SRM 51 -30-2. 2 L 7 3 4F A3WE 2007071000060 20070710 00060 NM 2007 7 10 DHL2007783528 1 20070621 A 5322 SHEAR TIE BOEING 727 727227 1384078 NM BS 1166 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 AFT CARGO COMPARTMENT, CORROSION ON SHEAR TIE BS 1166 BETWEEN STR 29R AND 30R. CUT OUT DAMAGED SHEAR TIE 4 BY 2. FABRI CATED AND INSTALLED SHEAR TIE IAW B727 SRM 53-10-4, FIG 5. MATERIAL USED 7075T6, .090, 4.7 BY 5.5 AND 5.5’ BY 2. TREAT ED, PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. 2 L 7 3 4F A3WE 2007071000061 20070710 00061 SO 2007 7 10 FDKA200705222 1 20070523 A 5210 MECHANISM EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 FDM FLT 6159 RDU-FLL (1036 PHX LCL). PASSENGER DOOR IS HARD TO OPEN AND CLOSE. MX LUBED THE PASSENGER DOOR, OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007071000062 20070710 00062 NM 2007 7 10 DHL2007783526 1 20070605 A 5312 BULKHEAD BOEING 727 727227 1384078 NM BS 740 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 EXFOLIATION CORROSION IN FWD BILGE, STA 740 BULKHEAD LWR CHORD AT STR 27R, (INBD OF STR 27R). FOUND SKIN SUPPORT ANGLE IN FWD BILGE AT STA 740 BULKHEAD TO BE BEYOND LIMITS AT STR 27R. FABRICATED AND INSTALLED NEW SKIN SUPPORT ANGLE IAW B7 27 SRM 51-30-2 AND BOEING DWG 69-64841. MATERIAL USED 7075-T0, .190, DIM 12 BY 10.7. HEAT TREATED TO T6 CONDITION IAW FLIGHTSTAR ENG REPORT 2-37153-801 REV A. ALL PARTS TREATED AND PRIMED IAW B727 SRM 51-10-2. 2 L 7 3 4F A3WE 2007071000064 20070710 00064 NM 2007 7 10 DHL2007785004 1 20070627 A 5711 SPAR BOEING 727 727214 138407R NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 RIGHT WING T/E AT RWBL 120, HAS A 1.5" CRACK IN RADIUS OF FALSE SPAR LOWER CHORD ANGLE. CUT OUT DAMAGED CHORD AND WEB S ECTIONS, FABRICATED NEW WEB SECTION FROM 7075-T6, .032" BY 12" BY 9.5", PO NR 9003458; REPAIR DOUBLER FROM 2024-T3, .05 0" BY 11" BY 12", PO NR 9003958; LOWER CHORD ANGLE FROM BAC1514-1437, 20", PO NR 9004179, 2 EA CHORD SPLICE ANGLES FROM 7075-T6, .071" BY 15" BY 3" (#1) AND .071" BY 12.125" BY 3" (NR 2), PO NR 9005314; RADIUS FILLER STRAP FROM 7075-T6, .0 90" BY 12.125" BY 2", PO NR 9004147; AND RADIUS FILLER, 2 EA, FROM 7075-T6, .160" BY 2.25" BY 1.25", ALL PER BOEING SB 7 27-57-158 REV 1. TREATED, PRIMED, AND INSTALLED ALL REPAIR PARTS PER B727 SRM 51-10-2 AND SB 727-57-158 REV 1. 2 L 7 3 4F A3WE 2007071000067 20070710 00067 SO 2007 7 10 FDKA200705230 1 20070507 A 5411 14576631621 FRAME EMB 145 EMB145LR 3260212 SO LT COWLING CHAFED A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 850MJ 145568 LEFT LOWER COWL AFT FRAME IS CHAFED OUT OF LIMITS. REPLACED AFT FRAME WITH NEW ONE. 2 L 7 2 4T RT T00011AT 2007071000068 20070710 00068 NM 2007 7 10 C1HA200785001 1 20070621 A 5320 THRESHOLD BOEING 727 7272S7 138407Z NM FUSELAGE CRACKED A C1HA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 GL 15 685CA 22492 FLIGHT ATTENDANTS REPORTED VIBRATION IN FLOOR IN FRONT OF AFT ENTRY DOOR AND GRINDING NOISE. ON DESCENT PULLED POWER LE VERS TO IDLE CABIN STARTED TO CLIMB AND NOISE AND VIBRATION WENT AWAY, WHEN POWER LEVERS ADVANCED CABIN DESCENDED AND VI BRATION AND NOISE RETURNED INSPECTED AREA, FOUND CRACKED THRESHOLD. REMOVED AND REPLACED THRESHOLD AS PER SRM 51-10-1. 2 L 7 3 4F A3WE 2007071000070 20070710 00070 NM 2007 7 10 07FDEA02301 1 20070628 A 5313 STRINGER BOEING 727 727227 1384078 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 FWD CARGO PIT STRINGER IS CRACKED AT RIVET IN LOWER CHANNEL BS 72 10, STR 27R. REMOVED STRINGER SPLICE AT BS 720 10". FABRICATED, LOCATED AND DRILLED AND DEBURRED NEW STRINGER SPLICE USING BAC1498-132 MATERIAL. TREATED AND PRIMED AND INS TALLED STRINGER AT BS720 10 REF SRM 51-30-2, 53-10-3 PG 9, FIG 1, MM 51-20-021-7, 51-20-151-7. 2 L 7 3 4F A3WE 2007071000071 20070710 00071 NM 2007 7 10 07FDEA02302 1 20070628 A 5330 65545776 SKIN BOEING 727 727227 1384078 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 FWD CARGO BAY BS 720 13 STR S-23R FUSELAGE SKIN FASTENER HOLE DAMAGED. FABRICATED FILLER AND DOUBLER FOR FWD CARGO BAY BS 720 13" STR S-27R FUSELAGE SKIN REF SRM 53-30-03, 53-10-03, 53-30-02, SEALANT 51-20-04. 2 L 7 3 4F A3WE 2007071000072 20070710 00072 NM 2007 7 10 07FDEA02303 1 20070628 A 5313 BAC1498144 STRINGER BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 FWD CARGO BAY BS 720+10 TO 720+14, S27R FWD END OF ORIGINAL CUT STR UNDER SPLICE IS CORRODED. I/B AND OB SIDE REMOVED S 27R SPLICE AT BS 720. REMOVED DAMAGE SECTION STR-27R, AFT OF SPLICE. REMOVED DAMAGE SKIN, FABRICATED NEW STRINGER SECT ION SPLICE, TREATED AND PRIMED REPAIR PARTS AND SKIN. INSTALLED STRINGER AND SPLICE, REF SRM 51-30-02, SRM 51-10-01, SR M 53-10-03 PG 3, SRM 53-10-3 FIG 1 SHT 1-4, MM 51-20-021-7, MM 51-20-151-7. 2 L 7 3 4F A3WE 2007071000073 20070710 00073 NM 2007 7 10 07FDEA02304 1 20070628 A 5100 655623620 STRINGER BOEING 727 727233 138408A NM ZONE 100 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FOUND REPAIR LOCATED AT STR S-27R FROM BS 674 TO 700 REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING REPAIR IAW BOEING 727 SRM 51-10-2. REPAIRED STRINGE R USING NEW STRINGER, SPLICE AND 3 FILLERS. FABRICATED AND INSTALLED AT STA 696, STRINGER 27R USING BOEING 727 SRM 53-1 0-3 PAGE 4B DETAIL I AND 51-10-2, ALL PARTS TREATED AND PRIMED. ALSO, BEFORE INSTALLATION USING BOEING 727 SRM 51-10-2, PG 1 REF. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007071000076 20070710 00076 NM 2007 7 10 07FDEA02307 1 20070628 A 5330 6517510 SKIN BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 PNEU GROUND CONNECTION SERVICE DOOR (#3903) CUTOUT HAS CRACK AT I/B AFT CORNER. FABRICATED DOUBLER, TREATED AND PRIMED AND INSTALLED. REF EA 7-53330-10732, SRM 51-10-2, 51-30-2 THIS IS CLASSIFIED AS A MINOR REPAIR STOP DRILLED CRACK REF BO EING 727 SRM 51-10-1 AND HFEC, NO DEFECTS NOTED. 2 L 7 3 4F RT A3WE 2007071000078 20070710 00078 NM 2007 7 10 07FDEA02309 1 20070628 A 5315 652082757 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 CABIN FLOORBEAM AT BS 480 HAS SCRATCHES ON UPPER SURFACE OF UPPER TEE BETWEEN RBL 27 AND RBL 40 BLENDED DAMAGED AREA, ND T FOR MATERIAL LOSS ORIGINAL .130 REMOVAL .008, SELF CONTAINED SHOT PEEN AREA, APPLIED ALODINE AND PRIMED. APPLIED CORR OSION INHIBITING COMPOUND, REF SRM 51-10-1, 51-20-5, MM 51-20-151, SOPM 20-10-3, EA NR 7-5310-113038. CLASSIFIED MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007071000079 20070710 00079 NM 2007 7 10 07FDEA02310 1 20070628 A 5315 652082757 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 CABIN BS 480 FLOORBEAM UPPER CHORD HAS SCRATCHES BETWEEN RBL 48 AND RBL 60 BLENDED DAMAGED AREA, NDT FOR MATERIAL LOSS O RIGINAL .130 REMOVAL .002, SELF CONTAINED SHOT PEEN AREA, APPLIED ALODINE AND PRIMED. APPLIED CORROSION INHIBITING CO MPOUND, REF SRM 51-10-1, 51-10-2 51-20-05, MM 51-20-151, SOPM 20-10-3, EA NR 7-5310-113038. CLASSIFIED MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007071000080 20070710 00080 NM 2007 7 10 746003 1 20070627 A 7500 2155M39G01 MANIFOLD BOEING 747 747206B 1384856 NM GE CF6 CF650E2 30018 NE NR 3 ENGINE FAILED A Q2SA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 63 746SA 21111 517881 AFTER TAKE OFF FROM RKSI, NR 3 ENGINE FIRE WARNING CAME ON. PERFORMED QRH PROCEDURE. DUMPED 176,000 LBS OF FUEL AND SH UTDOWN THE ENGINE. RETURNED TO RKSI. FOUND LEFT CDP TUBE FLEX JOINT FAILED. REPLACED FAILED CDP TUBE IN ACCORDANCE WI TH AMM 75-25-00. LEAK CHECK GOOD IN ACCORDANCE WITH AMM 71-00-00. NACELLE TEMPERATURE NORMAL. 2 L 7 4 4F 4 F RT A20WE E23EA 2007071000082 20070710 00082 EU 2007 7 10 MALA070071 1 20070627 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN BROKEN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 340B426 CABIN FLOOR PROXIMITY EMERGENCY LIGHT STRIP WAS INOPERATIVE SEATS 7A-9A. FOUND EMERGENCY LIGHT STRIP BROKEN. REMOVED A ND REPLACED INOPERATIVE EMERGENCY LIGHT STRIP FROM 7A-9A, P/N ON MA66363 IAW SAAB 340 AMM 33-50-20-04. 2 L 7 2 4T RT A52EU 2007071000091 20070710 00091 EA 2007 7 10 A6WA200740306 1 20070601 A 5315 6003106819 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 460 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 418AW 7618 FS 460 PRESSURE FLOORBEAM SUPPORT ANGLE IS CRACKED APPROX .2 INCH LONG OUTBOARD SIDE OF RBL. (M) 2 L 7 2 4F RT A21EA 2007071000092 20070710 00092 EA 2007 7 10 A6WA200740293 1 20070531 A 5320 601R75262153 BRACKET CNDAIR CL600 CL6002B19 1900309 EA HYD LINE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 418AW 7618 HYDRAULIC LINE Z-BRACKET CRACKED APPROX .1 INCH LONG IN RT WHEEL WELL CEILING FORWARD OF PRESSURE TRANSDUCERS. (M) 2 L 7 2 4F RT A21EA 2007071000093 20070710 00093 SO 2007 7 10 FDKA200705233 1 20070507 A 5414 SKIN EMB 145 EMB145LR 3260212 SO RT COWLING CHAFED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 850MJ 145568 RIGHT LOWER COWL INTERNAL SKIN IS DAMAGED BEYOND LIMITS BETWEEN FRAMES 6&7 AT CENTER LINE. REPAIRED SKIN. 2 L 7 2 4T RT T00011AT 2007062900007 20070629 00007 NM 2007 6 29 SWAA073077 1 20070620 A 5330 6545776 SKIN BOEING 737 7373G7 1384595 NM BS 925 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 925, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007062900015 20070629 00015 NM 2007 6 29 WRNA200700043 1 20070619 A 5330 SKIN BOEING 747 747212B 1384886 NM BS 765-775 DAMAGED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING -B- CHECK, OUT OF LIMIT LIGHTNING STRIKE DAMAGE WAS FOUND BETWEEN BS 765 & 775 AT LBL 4.5. DRILLED OUT DAMAGE IA W SRM 53-30-03 FIG 3A AND INSTALLED RIVETS IAW SRM 51-30-02. THIS IS A CATEGORY-C REPAIR AND REQUIRES INSPECTION AT 1,0 00 CYCLES. 2 L 7 4 4F A20WE 2007062900040 20070629 00040 NM 2007 6 29 ASAA0791802 1 20070531 A 5310 146A750347 RAIL BOEING 737 737990 NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT SUPPORT RAIL CORRODED. REPAIRED IAW EA 5310 02724. 2 L 7 4 4F RT A16WE 2007062900048 20070629 00048 CE 2007 6 29 EWCR07060001 1 20070605 A 3260 602EN6026 SWITCH CESSNA 650 650 2076802 CE MLG DEFECTIVE B EWCA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 39 750CK 7532 6507015 GEAR SELECTED UP AFTER TAKEOFF. USAFE LIGHT WOULD NOT EXTINGUISH AND AIR NOISE FROM NOSE GEAR DOORS OPEN. ATTEMPTS TO GE T DOORS TO CLOSE ON GEAR RETRACTION FAILED. RETURNED TO DEPARTURE AIRPORT AND ACFT.DELIVERED TO CITATION SERVICE CENTER AT GSO. NOSE GEAR UP LOCK SWITCH SWITCH FOUND DEFECTIVE: REPLACED AND OPERATION CHECKED GEAR NORMAL OPERATION. 2 L 7 2 4F A9NM 2007062900056 20070629 00056 EU 2007 6 29 COEA0702742 1 20070220 A 7700 1004PGSB TRANSMITTER FOKKER F27 F27MK600 4990706 EU LT ENGINE MALFUNCTIONED A COEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 13 742FE 10349 ABORTED TAKEOFF, LEFT ENGINE INDICATED ZERO TORQUE AT TAKEOFF AND TAXI POWER SETTINGS. AIRCRAFT RETURNED TO RAMP AT GEG . MAINTENANCE REMOVED AND REPLACED LT TORQUE TRANSMITTER, INSPECTED INLET OIL LINE AND BLEED TRANSMITTER. AIRCRAFT RET URNED TO SERVICE. (M) 2 H 7 2 4T A817 2007062900069 20070629 00069 NM 2007 6 29 UIEA200700251 1 20070621 A 5753 FAIRING BOEING 747 7472D7B 1384803 NM FLAP TRACK CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 RT WING NR 7 FLAP TRACK CANOE FAIRING DAMAGED AT LOWER SIDE, AFT OF ACCESS PANEL 667CB. ACCOMPLISHED PERMANENT REPAIR A S PER 747-200 SRM 51-40-09, FIG 6 TABLE I AND 747-200 SRM 51-40-12. ALSO REFERENCE ATLAS AIR XEO NR 57-061907. 2 L 7 4 4F RT A20WE 2007062900072 20070629 00072 NM 2007 6 29 UIEA200700250 1 20070616 A 2913 6506606 PUMP BOEING 747 7472D3B 1384805 NM HYD SYSTEM LEAKING A UIEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 15 506MC 21252 NR 2 HYD LEAK STOPPED WITH 1.8 GALLONS REMAINING. EDP TO SUPPLY OFF. REMOVED AND REPLACED HYD PUMP AND CASE DRAIN RETU RN FILTER, OPS AND LEAK CHECKED OKAY. 2 L 7 4 4F RT A20WE 2007062900093 20070629 00093 NM 2007 6 29 DLM88070755 1 20070618 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 494-532 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 926DL 49713 GROUND DAMAGE CAUSED BY RAMP DURING GROUND OPERATIONS. REPAIRED FUSELAGE SKIN AT FS 494-532 AT STR 24R-26R PER SRM 53-0 4 FIG 12B SHEET 4-6. 2 L 7 2 4F RT A6WE 2007062900100 20070629 00100 NM 2007 6 29 DL76S070765 1 20070621 A 5315 BAC1509100682 FLOORBEAM BOEING 767 767332 1382001 NM BS 1197 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 AFT CARGO COMPT -STA 1197+66 LBL 10 TO LBL 30 FLOOR PANEL SUPPORT RIB SIGN OF CORROSION. REPAIRED PER 53-00-01 REPAIR 4 FIGURE 201 ON NR AJN51001. 2 L 7 2 4F RT A1NM 2007062900106 20070629 00106 NM 2007 6 29 DL76S070773 1 20070621 A 5315 BAC1509100682 FLOORBEAM BOEING 767 767332 1382001 NM BS 434 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 FWD CARGO BS 434 RBL 41 TO RBL 45 FLOOR SUPPORT TOP SURFACE CORRODED. REPAIRED PER 53-00-07 FIGURE 201. REPAIR 4 ON AJN 52963. 2 L 7 2 4F RT A1NM 2007062900108 20070629 00108 NM 2007 6 29 CALA0700321 1 20070624 A 2612 WIRE BOEING 737 7373T0 1384582 NM APU FIRELOOP BROKEN A CALA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 27 14342 23580 THE APU FIRE LIGHT ILLUMINATED ACCOMPANIED BY ACTIVATION OF THE FIRE BELL WHILE AT CRUISE ENROUTE FROM SFO TO IAH. THE A PU DETECTOR INOP LIGHT ALSO ILLUMINATED. THE APU FIRE EXTINGUISHING BOTTLE WAS DISCHARGED AND THE AIRCRAFT WAS DIVERTED TO SAT WHERE IT LANDED WITHOUT INCIDENT. THE APU AND APU COMPARTMENT WAS INSPECTED AND MAINTENANCE FOUND NO EVIDENCE OF FIRE. TROUBLESHOOTING FOUND BROKEN WIRE TO TAILCONE FIRE LOOP AND LOWER APU FIRE LOOP. WIRE CONNECTORS WERE REPLACED IAW MM 20-62-16. THE M279 AND SHROUD DETECTOR WERE REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. IN ADDITION, THE APU FI RE EXTINGUISHING BOTTLE WAS REMOVED AND REPLACED IAW MM 26-22-11. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2007070200005 20070702 00005 NM 2007 7 2 07FDEA02253 1 20070622 A 5315 65649504 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 CABIN FLOOR PANEL SUPPORT AT BS 418 HAS CORROSION ON UPPER SURFACE BETWEEN RBL 13 AND RBL 23. REMOVED AND REPLACED SUPP ORT REF SRM 51-30-02. 2 L 7 3 4F RT A3WE 2007070200006 20070702 00006 EU 2007 7 2 07FDEA02254 1 20070622 A 5320 A5378193620200 TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 662FE 761 MAIN CABIN, ADAPTER TRACK, FRAME 30, BL Y60, DAMAGED. REMOVED AND REPLACED ADAPTER TRACK IAW A300-600 SRM 51-40-20, PAR AGRAPH 7. 2 L 7 2 4F RT A35EU 2007070200016 20070702 00016 NM 2007 7 2 AWXA200700762 1 20070604 A 5320 143N8334U27 INTERCOSTAL BOEING 757 757225 1384959 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 MCN - FOUND CRACKED INTERCOSTAL WEB, BS 690, S12L. REPLACED INTERCOSTAL WEB, BS 690, S12L IAW AWA TASK CARD M1C53608. 2 L 7 2 4F RT A2NM 2007070200021 20070702 00021 EU 2007 7 2 F3LA200700137 1 20070609 A 5321 D5367180500400 FLOOR PANEL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 907FR 5061 1743 DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 261FF CORRODED AT FWD INBD CORNER ON UNDERSIDE OF PANEL. REPLACED F LOOR PANEL IAW AMM 53-32-12-400-002. 2 L 7 2 4F RT A28NM 2007070200023 20070702 00023 EU 2007 7 2 F3LA200700140 1 20070610 A 5321 D5367180500500 FLOOR PANEL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 907FR 5061 1743 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON UNDERSIDE OF FLOOR PANEL 262FF. REPLACED FLOOR PANEL 262FF AND R2 DOOR THRESHOLD IAW SRM 53-42-12, PB 401. 2 L 7 2 4F RT A28NM 2007070200058 20070702 00058 NM 2007 7 2 07FDEA02274 1 20070626 A 5310 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 575FE 48500 CENTER CARGO BETWEEN STA 1559 AND STA 1565 LONGERON 48R FOUND CORROSION. [07-09-07] CENTER CARGO BETWEEN STA 1559 AND STA 1565 LONGERON 48R CARRIED OUT REPAIR AS PER SRM 53- 10-00 VOLUME I FIGURE 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007070200060 20070702 00060 NM 2007 7 2 07FDEA02276 1 20070626 A 5330 65545907 SKIN BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K O NONE OTHER O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FUSELAGE BS 720 TO BS 740, S-27L TO S-26L EXTERNAL DOUBLER CORRODED ON BOTH SIDES AROUND DUCT CUTOUT. REMOVED CORROSI ON REFERENCING SRM 51-10-1 VERIFIED MATERIAL TO BE .125". REMOVED .OO6". REMAINING MATERIAL .119" FOUND TO BE WITH IN LIMITS REFERENCING SRM 53-30-1. TOOL NR IN17-9593 CAL DATE 5/16/08 TREATED AND PRIMED REFERENCING SRM 51-10-2 2 L 7 3 4F RT A3WE 2007070200061 20070702 00061 NM 2007 7 2 07FDEA02277 1 20070626 A 5311 65163434 FRAME BOEING 727 727233 138408A NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 286FE 22623 ON AGING A/C INSP, FOUND REPAIR LOCATED AT BS 1050 FRAME BETWEEN STR S-26R AND S-28R DID NOT CONFORM TO SRM 51-40-3. RE MOVED EXISTING REPAIR, REMOVED Z-ANGLE, GUSSET, TIE DOWN BRACKET FOR ACCESS. FABRICATED NEW REPAIR PARTS, REF SRM 51-4O -3 FIG 1. HEAT TREATED PART, DRILLED UP PART, TREATED AND PRIMED REF SRM 51-10-2. INSTALLED REPAIR, TIE DOWN BRACKET, GUSSET AND Z ANGLE. 2 L 7 3 4F RT A3WE 2007070200081 20070702 00081 NM 2007 7 2 ASAA0791811 1 20070531 A 5347 146A750611 CARGO TRACK BOEING 737 737990 NM BS 727I CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT RAIL SPLICE IS CORRODED. REPAIRED IAW 51-40-02 AND 51-40-03. 2 L 7 4 4F RT A16WE 2007070200087 20070702 00087 NM 2007 7 2 ASAA0741817 1 20070622 A 5310 654796039 FRAME BOEING 737 7374Q8 138447Q NM GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 AFT CARGO DOOR AFT FRAME REPAIR IS GOUGED. REPAIRED FRAME IAW ASA EA 5310 02725. 2 L 7 2 4F RT A16WE 2007070200089 20070702 00089 NM 2007 7 2 2007UALA02116 1 20070620 A 2620 FIRE BOTTLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CARGO BAY FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 CARGO FIRE BOTTLE 2 DISCHARGE LIGHT ON. [07-13-07] REPLACED BOTH FIRE BOTTLES. 2 L 7 2 4F 4 F RT A16WE E21EU 2007070200093 20070702 00093 NM 2007 7 2 2007UALA02120 1 20070619 A 5330 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 806UA 788 EXTERNAL FUSELAGE SKIN FRAME 22LT AT STR 12LT TO STR 13LT IS DAMAGED. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REP AIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007070200094 20070702 00094 NM 2007 7 2 2007UALA02121 1 20070619 A 5330 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 806UA 788 EXTERNAL FUSELAGE SKIN FRAME 23LT AT STR 10LT TO STR 11LT IS DAMAGED. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REP AIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007070200098 20070702 00098 NM 2007 7 2 2007UALA02125 1 20070620 A 2432 CHARGER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE MAIN BATTERY FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 229UA 30557 AT DEPARTURE MAIN BATTERY CHARGER MESSAGE. [07-17-07] REPLACED MAIN BATTERY CHARGER PER MM 24-31-02 . SUSPECT INTER NAL SHORT IN CHARGER. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007070200103 20070702 00103 NM 2007 7 2 2007UALA02130 1 20070619 A 2611 SMOKE DETECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FWD LAVATORY FAILED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 822UA 948 LAVATORY SMOKE DETECTOR FAULT ON UPPER ECAM. FOUND SMOKE DETECTOR FAILURE. REPLACED SMOKE DETECTOR IN FWD LAVATORY. AL SO REPLACED SECURITY SEALS, JUNE 22. 2 L 7 2 4F 4 F RT A28NM E40NE 2007070200105 20070702 00105 NM 2007 7 2 2007UALA02132 1 20070618 A 3350 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 377UA 24642 EMERGENCY EXIT LIGHT AFT OF RIGHT WING (BY RIGHT INBOARD FLAP FAIRING) INOP. RELAMPED EMERGENCY EXIT LIGHT RIGHT OVERWI NG LIGHT & OP'S CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007070200132 20070702 00132 NM 2007 7 2 SWAA073081 1 20070620 A 3350 417A57042 CAP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 232WN 32500 DURING SCHEDULED MV1 CHECK, FOUND EEPLS END CAP MISSING. INSTALLED END CAP PER MM. 2 L 7 2 4F RT A16WE 2007070200133 20070702 00133 2007 7 2 SWAA073084 4 20070621 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 443WN 29838 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007070200135 20070702 00135 NM 2007 7 2 SWAA073099 1 20070621 A 5312 65458197 PRESSURE PANEL BOEING 737 7373H4 1384600 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND NLG RIGHT PRESSURE WEB CRACKED AT BS 246, WL 170. REPAIRED PRESSURE WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2007070200136 20070702 00136 NM 2007 7 2 SWAA073100 1 20070621 A 5312 65458197 PRESSURE PANEL BOEING 737 7373H4 1384600 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND NLG LEFT PRESSURE WEB CRACKED AT BS 246, WL 170. REPAIRED PRESSURE WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2007070200137 20070702 00137 NM 2007 7 2 SWAA073102 1 20070621 A 5752 6546455 STRUCTURE BOEING 737 7373H4 1384600 NM AILERON TAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND LEFT WING AILERON TAB DELAMINATED ON OUTBOARD T/E. REMOVED AND REPLACED AILERON TAB PER MM. 2 L 7 2 4F RT A16WE 2007070200148 20070702 00148 NM 2007 7 2 SWAA073095 1 20070621 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM BS 500C CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007070200152 20070702 00152 NM 2007 7 2 SWAA073096 1 20070621 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007070200159 20070702 00159 NM 2007 7 2 SWAA073090 1 20070621 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 412WN 29818 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2007070200170 20070702 00170 NM 2007 7 2 USAA070475 1 20070622 A 5311 FRAME BOEING 737 737401 1384701 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 AROUND INBOARD LOCK FASTENER HEAD AT STA 867 BETWEEN S81 & S91 HAS CRACK. CUT OUT DAMAGE & INSTALLED DOUBLER PER TR 53- 10-20E, DEFECT SIZE: .0625 INCH. 2 L 7 2 4F RT A16WE 2007070200171 20070702 00171 NM 2007 7 2 USAA070474 1 20070622 A 5320 STIFFENER BOEING 737 737401 1384701 NM BS 328 RBL 31 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 STA 328, RBL 31.5 HAS CRACK. REMOVED, FAB'D & INSTALLED NEW VERTICAL STIFFENER PER SRM 51-10-02, DEFECT SIZE: .500 INC H. 2 L 7 2 4F RT A16WE 2007070200178 20070702 00178 SO 2007 7 2 C2XA07TY031 1 20070622 A 5532 SPAR EMB 145 EMB145LR 3260212 SO VERTICAL STAB CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14991 145278 VERT STAB SPAR 1 INTERNAL SUPPORT BRACKET ON FRM 75 FRETTING. REMOVED FITTING AND BLENDED FITTING AND SKIN. FOUND TO B E WITHIN LIMITS. PERFORMED DYE PEN INSPECTION AND FOUND NO CRACKS. ALODINED, PRIMED, SEALED, INSTALLED FITTING AND APP LIED FILLET SEALANT IAW EC5310-01317. AIRCRAFT STILL IN C-CHECK. 2 L 7 2 4T RT T00011AT 2007070200186 20070702 00186 NM 2007 7 2 HNAA0700088 1 20070513 A 3350 82410162001 CONTROLLER DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS MALFUNCTIONED A HNAA O OTHER N FALSE WARNING CR CRUISE 1 EA 07 837 217 EMERGENCY LIGHTS CAME ON FOR 3 SEC DURING FLIGHT SEVERAL TIMES. REMOVED AND REPLACED EMERGENCY LIGHTS CONTROLLER, OPS C HECK GOOD, A/C OK FOR SERVICE. 2 H 7 2 4T RT A13NM 2007070200187 20070702 00187 NM 2007 7 2 KCSA071195 1 20070625 A 5311 FRAME BOEING 747 747123 1384873 NM BS 1810 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 AFT PIT FUSELAGE FRAME WEB DAMAGED AT BS 1810 BETWEEN STR 39R AND STR 40R. 2 L 7 4 4F A20WE 2007070200188 20070702 00188 NM 2007 7 2 ABXA070183 1 20070617 A 8011 7755503 STARTER BOEING 767 767232 1385132 NM GE CF680 CF680A2 NE NR 1 ENGINE UNKNOWN A ABXA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 23 748AX 28 22225 580128 OUT OF SJO EN ROUTE TO MIA, THE NR 1 ENGINE OIL QUANTITY STARTED TO DECREASE. THE CREW ELECTED TO DIVERT TO GCM. CREW PULLED THE THROTTLE BACK TO IDLE AND MAINTAINED GOOD OIL PRESSURE. DID NOT HAVE TO SHUT THE ENGINE DOWN BUT DID DECLARE AN EMERGENCY. REMOVED STARTER AND FOUND O-RING CUT DUE TO A BURR ON THE STARTER THRUST LINK. REMOVED SHARP EDGE OF BU RR AS REQUIRED. INSTALLED NEW PACKING AND REPLACED STARTER IAW AMM 80-11-01 AS PRECAUTION. SERVICED OIL TANK AS PER AM M 12-13-01. ACCOMPLISHED ENGINE RUN-UP FOR 10 MINUTES. NO LEAKS NOTED AS PER B767 AMM 71-00-00. (LEFT ENGINE) 2 L 7 2 4F 4 F RT A1NM E13NE 2007070300005 20070703 00005 EA 2007 7 3 A6WA200740242 1 20070510 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 455AW 7848 PAX DOOR AFT DRAG ANGLE CRACKED. (K) [07-17-07] MAINTENANCE REMOVED DAMAGED SECTION OF DRAG ANGLE AND INSTALLED SERV ICEABLE SECTION IAW BOMBARDIER REO 601R-52-11-513. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300007 20070703 00007 EA 2007 7 3 A6WA200740243 1 20070513 A 3210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT MLG CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 458AW 7861 RT MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER PLUMBING (Z) MEMBER ASSY PN 601R75262-153, IS CRACKED THRU ON OB LEG. (K) [07-17-07] MAINTENANCE REPLACED ZEE MEMBER IAW CRJ SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300023 20070703 00023 GL 2007 7 3 C2XA07CL056 2 20070620 A 7200 VIBRATORY NODE EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL NR 2 ENGINE CRACKED A C2XA B EMER. DESCENT Y ENGINE STOPPAGE CR CRUISE 1 SW 27 34110 145658 CAE312281 RDU FLIGHT NR 3028 THE CREW REPORTED THE NR 2 ENGINE FAILED IN FLIGHT AT 29,000 FT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE. [07-17-07] THE ENGINE SHUTDOWN DUE TO THE FRACTURE OF THE UPPER BEVEL GEAR. THE ROOT CAUSE OF THIS FRACTURE IS A VIBRATORY NODE (3DOC) IN THE GEAR WHICH CAUSES A CRACK AND SUBSEQUENT BREAKAGE. 2 L 7 2 4F 4 F RT TE6CH 2007070300027 20070703 00027 NM 2007 7 3 UPS07450010 1 20070607 A 5712 65B0787241 RIB BOEING 747 747212B 1384886 NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C LEFT WING L/E UPPER PANEL AT WS 970 FOUND BULGED UP. CORROSION BLEND OUT 0.030 X 1 X 2 INCHES LT WING L/E UPPER WS 970 UPPER CHORD REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007070300039 20070703 00039 NM 2007 7 3 UPS07450020 1 20070604 A 5311 65B01716516 DOUBLER BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C CABIN BS 460 S14R FRAME DOUBLER FOUND CRACKED (CRACK LENGTH 1.5 INCH). CABIN BS 460 BETWEEN STR 11R T O STR 14ER AREA FRAME ATTACH DOUBLER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007070300047 20070703 00047 NM 2007 7 3 SWAA073117 1 20070622 A 3350 417A5701 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 EEPLS COVER LOOSE AT ROW 9 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007070300062 20070703 00062 NM 2007 7 3 SWAA073135 1 20070622 A 5311 6546550 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007070300083 20070703 00083 NM 2007 7 3 SWAA073128 1 20070622 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007070300202 20070703 00202 NM 2007 7 3 UPS07450027 1 20070608 A 5320 65B018357 STRUCTURE BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C CRACK FOUND AT 1EA FASTENER HOLE BELOW STR 15ER AT BS 420 AFT INNER CHORD (P/N: 65B01835-7) THROUGH TH ICKNESS CRACK 0.040 INCH LONG RUNNING O/B AT 3 O`CLOCK POSITION (LOOKING FWD). CABIN BS 420 FRAME ATTACH INNER CHORD BE TWEEN STR 10AR TO STR 16R REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007070300206 20070703 00206 WP 2007 7 3 UPS07850008 1 20070621 A 3297 CONNECTOR DOUG DC8 DC871F 302199D WP RT MLG BROKEN A IPXA K NONE N FALSE WARNING AP APPROACH 1 SO 01 700UP 45900 INSPECTION TYPE:N/A UNSAFE INDICATION RT MLG CYCLED TWICE. WHILE HOLDING FOR 20 MINUTES, CAME ON. IN UNSAFE CONDITION LIGHT CHECK DID NOT WORK. CHANGED LIGHTS WITH UNSAFE INDICATION & FLAPS 35 - THERE WAS NO HORN. FOUND RT MLG DOWNLOCK IND CONNECTOR CORRODED, PIN 5 WOULD NOT LOCK IN, & BACKSHELL ADAPTOR BROKEN. REPLACED CONNECTOR REF SWM 20-31-12. TEMP REPAIRED BACK/CONDUIT WITH REF TO EO DC8-3260-27089A. TEMP REPAIR TO RT MLG DOWNLOCK INDICATION SWITCH CONDUIT IAW EO DC8-3260-27089A TO BE PERMANENTLY REPAIRED IN 30 DAYS. 2 L 7 4 4F RT 4A25 2007070300213 20070703 00213 EA 2007 7 3 TRAX200700883 1 20070621 A 5210 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 PAX DOOR WILL NOT UNLOCK. 2 L 7 2 4F RT A21EA 2007070300217 20070703 00217 NM 2007 7 3 FDKA200703138 1 20070328 A 3230 HANDLE DHAV DHC8 DHC8102 2809003 NM RT MLG OUT OF POSITION A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 804LR 324 FDM 6112 JFK-BWI (1135 PHX LCL). AIRCRAFT RETURNED TO THE FIELD FOR THE LEFT MLG DOOR, NLG DOOR WILL NOT CLOSE AND RT M LG WILL NOT RETRACT. MX FOUND RT MLG PUMP HANDLE WEDGED INTO THE GEAR, MX REMOVED OBSTRUCTION AND GEAR SWING GOOD. 2 H 7 2 4T RT A13NM 2007070300220 20070703 00220 SO 2007 7 3 FDKA200703144 1 20070321 A 5320 14525480603 THRESHOLD EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 847MJ 145517 CARGO DOOR THRESHOLD IS CORRODED OUT OF LIMITS. THE DAMAGED THRESHOLD HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2007070300226 20070703 00226 SO 2007 7 3 FDKA200704157 1 20070416 A 2750 3631001011 CONTROL UNIT EMB 145 EMB145LR 3260212 SO FLAP MALFUNCTIONED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 842MJ 12803 145457 FDM 6017 MCO-BNA (2040 PHX LCL). FLAP LOW SPEED MESSAGE. MX REMOVED AND REPLACED FECU & RELAYS OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007070300234 20070703 00234 SO 2007 7 3 FDKA200704169 1 20070406 A 7830 BEAM EMB 145 EMB145LR 3260212 SO THRUST REVERSER CRACKED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 848MJ 145530 LEFT OUTBOARD SIDE BEAM ON THRUST REVERSER CRACKED. REPLACED BEAM. 2 L 7 2 4T RT T00011AT 2007070300244 20070703 00244 WP 2007 7 3 ABXA070187 1 20070518 A 5280 59106345 SKIN DOUG DC9 DC931 3022065 WP LT MLG DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 LEFT MAIN LANDING GEAR DOOR LOWER SKIN FORWARD, 22 INCHES FROM OUTBOARD EDGE EXFOLIATED. REPAIRED DOOR IAW DC9 SRM. 2 L 7 2 4F A6WE 2007070900003 20070709 00003 WP 2007 7 9 AALA20071121 1 20070618 A 3350 P4010051111 MODULE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 465A 49595 LGA - OVERHEAD EMERGENCY EXIT LIGHTS AT SEAT ROWS 20 TO 34 INOPERATIVE. REPLACED MODULE FOR OVERHEAD EMERGENCY EXIT LIG HTS AT SEAT ROWS 20 TO 34 . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007070900017 20070709 00017 WP 2007 7 9 AALA20071094 1 20070613 A 3350 P2010031701 LIGHT DOUG DC9 DC982 3022082 WP EMERGENCY EXIT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70524 49916 JFK - EMERGENCY EXIT LIGHT AFT OF FORWARD GALLEY DAMAGED. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AFT OF FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007070900019 20070709 00019 WP 2007 7 9 AALA20071116 1 20070616 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 568AA 49349 LGA - OVERHEAD EMERGENCY EXIT LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY EXI T LIGHT AT FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007070900046 20070709 00046 SO 2007 7 9 SIMA200717901 1 20070625 A 5610 WINDOW EMB 145 EMB145LR 3260212 SO COCKPIT LEAKING A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 623AE 145109 CAPTAIN DV WINDOW SQUEALING THROUGH 20,000 FEET WITH CABIN ALTITUDE 6.8 PSI. RETORQUED FRONT FRONT WINDSHIELD IAW EMB AMM 56-10-01. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007070900047 20070709 00047 EA 2007 7 9 SIMA200717705 1 20070623 A 2150 A/C PACK CNDAIR CL600 CL6002C10 1390015 EA LEFT UNKNOWN A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 509AE 10078 LT PACK TEMPERATURE CAUTION FOLLOWED BY LEFT PACK FAULT CAUTION, RECEIVED RIGHT BLEED DUCT CAUTION AT 20,000 FEET. RETU RNED TO DFW. PERFORMED WORK SCOPE DEVELOPED BY AMERICAN EAGLE REPEATER DEPARTMENT WITH NO DEFECTS NOTED. PERFORMED FUN CTIONAL CHECK FLIGHT ACCOMPLISHED WITH NO DEFECTS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007070900050 20070709 00050 NM 2007 7 9 NWAA072276732 1 20070623 A 2497 WIRE BOEING 747 747251B 1384892 NM NR 4 ENGINE GEN CHAFED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 632NW 23112 AT ROTATION THE FIRE DETECTION LIGHT ON THE FOREWARD PANEL AND THE FAULT LIGHT ON THE S/O PANEL FLASHED (4 TO 5 TIMES). THE NACELLE TEMP GAUGE NR 4 ENGINE, A LOOP WAS FLUCTUATING BETWEEN 3 AND 8. DUE TO PREVIOUS HISTORY RETURNED TO LAND. RETURNED TO YWG AND LANDING WAS UNEVENTFUL. MAINTENANCE PREPARED AIRCRAFT FOR A 3 ENGINE FERRY FLIGHT TO MSP FOR REPAIR S. MAINTENANCE FOUND NR 4 ENGINE GENERATOR WIRES WERE CHAFED AND SHORTED TO NR 4 ENGINE A LOOP. REMOVED AND REPLACED N R 4 ENGINE. OPERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F A20WE 2007070900054 20070709 00054 NM 2007 7 9 TSAA0731036 1 20070625 A 2780 655280726 ACCESSORY UNIT BOEING 737 737282C 13844AU NM LE FLAP/SLATS FAILED A TSAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 13 826AL 23051 NON-ETOPS FLIGHT 226 HNL-OGG - WHEN THE CREW APPLIED TAKEOFF POWER, THE CONFIGURATION WARNING HORN SOUNDED. CREW ABORTE D TAKE OFF AT 60 KNOTS INDICATED AIRSPEED. CREW RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REP LACED THE FLAP SLAT LEADING EDGE POSITION INDICATOR ACCESSORY UNIT. CONFIGURATION WARNING SYSTEM OPERATIONAL CHECK OK P ER AMM 31-26-0. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007070900055 20070709 00055 2007 7 9 TSAA0731037 4 20070624 A 3100 UNKNOWN BOEING 737 7372X6C 1384552 NM UNKNOWN A TSAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 13 746AS 23123 NON-ETOPS FLIGHT 93 HNL-OGG, ON THROTTLE UP, THE TAKE OFF CONFIGURATION WARNING ALARM SOUNDED. CREW ABORTED TAKE OFF AT 50 KNOTS INDICATED AIRSPEED. CREW DID NOT RETURN TO GATE. CREW RECHECKED ALL SYSTEMS AND TOOK OFF WITHOUT ANY FURTHER INCIDENT. MAINTENANCE PERFORMED TAKE OFF WARNING SYSTEM OPERATIONAL CHECK PER AMM 31-26-0. SYSTEM OPERATED OK ON THE GROUND. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007070900060 20070709 00060 EA 2007 7 9 SWIA200718395 1 20070420 A 3350 SIGN CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 708SK 10156 EMERGENCY EXIT SIGN ABOVE THE SERVICE DOOR DOES NOT ILLUMINATE. REPLACED 10 BULBS IN EXIT SIGN IAW AMM 33-51-07. 2 L 7 2 4F RT A21EA 2007070900069 20070709 00069 EU 2007 7 9 COEA0710908 1 20070307 A 5330 S53371312200 PANEL AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CRACKED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 908FX 023 FOUND CRACK AND DENT ON EXTERNAL FUSELAGE SKIN BETWEEN FR 22 AND FR 23 AND BETWEEN STRINGER 15R AND 16R. DAMAGE REMOVED FROM EXTERNAL FUSELAGE SKIN. FABRICATED AND INSTALLED NEW REPAIR DOUBLER IAW ATR SRM. (M) 2 H 7 2 4T RT A53EU 2007070900115 20070709 00115 NM 2007 7 9 ASAA0791819 1 20070622 A 5297 WIRE HARNESS BOEING 737 737990 NM DOOR LOCK SHORTED A ASAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 02 305AS 30013 DURING CRUISE AT FL 350 VHF COM NR 2 & VHF NAV NR 1 AND ADF NR 2 PANEL DISPLAYS WERE ALL ILLUM'D FULL BRIGHT WITH ALLIED LIGHTS FLASHING. CARGO FIRE DETECTION PANEL LIGHTS ALL ILLUM'D FULL BRIGHT FLIGHT DECK DOOR ANNUNCIATOR LIGHTS ILLUM'D STEADY. SHORTLY AFTER AN ACRID ELECTRICAL SMELL FILLED THE COCKPIT. DURING THE COURSE OF DIVERSION THE ODOR WAS NOTIC EABLE IN THE CABIN, BUT TO A LESSER DEGREE. INSP WIRE BUNDLE IN P8 AISLE CNTL STAND, NO DEFECTS NOTED. FOUND COCKPIT D OOR LOCK LIGHT PNL SHORTED. REPLACED PANEL. OP CHECKS GOOD. REF EO5250 01062. REF MM 27-41-00, ALL DISPLAYS TEST NOR MAL WITH MASTER DIM & TEST. 2 L 7 4 4F RT A16WE 2007070900116 20070709 00116 NM 2007 7 9 ASAA0741820 1 20070625 A 5751 65C2591130A SKIN BOEING 737 7374Q8 138447Q NM RT AILERON DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 RT AILERON IS DAMAGED AT FWD SPAR UPPER SKIN. REPAIRED AILERON IAW SRM 51-70-17 REPAIR 7 AND ASA EA 5750 02373. 2 L 7 2 4F RT A16WE 2007070900117 20070709 00117 NM 2007 7 9 ASAA0741821 1 20070624 A 5210 654965516 LINER BOEING 737 737490 1384715 NM L1 DOOR LOOSE A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 703AS 28893 L1 FWD ENTRY DOOR JAMMED ON ARRIVAL AT YVR. UNJAMMED DOOR LINING AND REMOVED FOR INSPECTION OF CONTROL RODS DOOR CAM AN D DOOR JAMB LATCHING ROLLERS PER AMM 52-11-00. DOOR OPERATION CHECKED NUMEROUS TIMES AND UNABLE TO DUPLICATE. AIRCRAFT PRESSURIZATION CARRIED OUR PER AMM 21 00 05 AND NO AIR LEAKS FOUND. AIRCRAFT CONSIDERED SERVICABLE FOR FLIGHT. 2 L 7 2 4F RT A16WE 2007070900118 20070709 00118 NM 2007 7 9 ASAA0741822 1 20070625 A 3350 SG81911 LIGHT BOEING 737 7374Q8 138447Q NM ROW 16 RH MISSING A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 778AS 25110 SEVEN INCHES OF PHOTOLUMINSCENT EMERGENCY TRACK LIGHTING MISSING. MISSING STRIP LOCATED AT ROW 16 OVER THE MLG VIEWING WINDOW COVER. REPLACED THE MISSING SECTION OF THE PHOTOLUMINSCENT STRIP. 2 L 7 2 4F RT A16WE 2007070900119 20070709 00119 EA 2007 7 9 TRAX200700885 1 20070622 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 871AS 7537 PAX DOOR OUTER HANDLE IS CRACKED. [07-26-07] REPAIRED IAW AMM 52-11-03, MM 52-11-25, MM 52-11-03, SRM 51-25-16, A ND AMM 52-11-03 2 L 7 2 4F RT A21EA 2007070900120 20070709 00120 EA 2007 7 9 TRAX200700886 1 20070622 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 871AS 7537 PAX DOOR UPPER STEP FWD WEB IS CRACKED IN THE RADIUS OF THE CORNER, UNDER THE HANDRAIL SUPPORT FITTING. 2 L 7 2 4F RT A21EA 2007070900121 20070709 00121 EA 2007 7 9 TRAX200700887 1 20070622 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 871AS 7537 PAX DOOR UPPER STEP AFT WEB IS CRACKED IN THE RADIUS OF THE CORNER UNDER THE HANDRAIL SUPPORT FITTING. 2 L 7 2 4F RT A21EA 2007070900122 20070709 00122 EA 2007 7 9 TRAX200700888 1 20070622 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 909EV 7658 LEFT SIDE FWD EMERGENCY EXIT LIGHT INOP. 2 L 7 2 4F RT A21EA 2007070900123 20070709 00123 EA 2007 7 9 TRAX200700889 1 20070622 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 835AS 7258 STATION REPORTING THE PAX DOOR OUTER HANDLE BROKEN OFF WHILE CLOSING DOOR. 2 L 7 2 4F RT A21EA 2007070900124 20070709 00124 2007 7 9 YENA2007055 4 20070616 A 2330 3042865102 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU 10 ABC ODOR A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 635JB 5062 2725 FLT 488, APPROX 0300Z, LGB-BOS, INTERMITTENT ELECTRICAL SMOKE ODOR COMING FROM ROW 10ABC, AIRCRAFT LEFT. F/A CHECKED LT V CONTROL BOXES, NONE WERE HOT. COMPLIED WITH JB TSM TASK 23-39-00-810-801, PART B, LTV SEB AT 10B WAS REMOVED AND REPL ACED AS PRECAUTIONARY MEASURE, AS PER LTV M/M 23-39-00. OPS CHECK OK. 2 L 7 2 4F RT A28NM 2007070900125 20070709 00125 EU 2007 7 9 YENA2007056 1 20070624 A 2432 2726CH1 BATTERY EMB ERJ190 ERJ190100IGW 3260408 EU #2 POSITION OVERTEMP A YENA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 EA 15 184JB 1919 414 19000008 ON TAKEOFF ROLL BATTERY NR 2 OVERTEMP EICAS MESSAGE. T/S TSM 24-36-810-804-A. REMOVED AND REPLACED NR 2 MAIN BATTERY, GROUND CHECK OK. 2 L 7 2 4F RT A57NM 2007070900126 20070709 00126 NM 2007 7 9 CALA0700320 1 20070625 A 5311 6520722U70 FRAME BOEING 737 7373T0 1384582 NM BS 440 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70352 23590 INSPECTION FOUND A .75 INCH CRACK IN FORWARD CARGO DOOR CUTOUT FORWARD FRAME AT LOWER STOP PAD, STA 440, S16R TO S27R. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007070900127 20070709 00127 NM 2007 7 9 SWAA073169 1 20070625 A 3350 10107451 SIGN BOEING 737 7377H4 1384404 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 251WN 32510 DURING SCHEDULED MV2 CHECK, FOUND AFT CABIN EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007070900128 20070709 00128 NM 2007 7 9 SWAA073152 1 20070623 A 2530 1105011 COFFEEMAKER BOEING 737 7377H4 1384404 NM GALLEY FAULTY A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 29 280WN 32533 DIVERSION, CREW REPORTED STRONG ELECTRICAL ODOR. TURNING OFF GALLEY POWER ODOR DISSIPATED. REMOVED AND REPLACED AFT CO FFEEMAKER PER MM. 2 L 7 2 4F RT A16WE 2007070900129 20070709 00129 NM 2007 7 9 SWAA073155 1 20070624 A 3350 1619 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SERVICE CHECK, FOUND R2 EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007070900130 20070709 00130 NM 2007 7 9 SWAA073150 1 20070623 A 3350 1619 LAMP BOEING 737 7373A4 1384585 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER M M. 2 L 7 2 4F RT A16WE 2007070900131 20070709 00131 NM 2007 7 9 SWAA073171 1 20070625 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STABILIZER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007070900132 20070709 00132 NM 2007 7 9 SWAA073153 1 20070624 A 3260 189915 SENSOR BOEING 737 7373A4 1384585 NM RT MLG OUT OF ADJUST A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 29 680AA 23505 AIRTURN BACK / DECLARED EMERGECNY, ON CLIMBOUT THE RIGHT MLG LIGHT STAYED ON WITH LANDING GEAR HANDLE PLACED TO UP AND O FF. ADJUSTED RIGHT MLG UPLOCK SENSOR PER MM. 2 L 7 2 4F RT A16WE 2007071000003 20070710 00003 SO 2007 7 10 FDKA200706269 1 20070611 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 838MJ 145384 EMERGENCY EXIT SIGN AT ROW 12 INOP. MX SECURED THE ELECTRICAL CONNECTOR AND OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007071000006 20070710 00006 SO 2007 7 10 RAIA00706040 1 20070623 A 5730 14567011007 SKIN EMB 145 EMB145LR 3260212 SO LT WING CRACKED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 817HK 145058 STL - DURING INSPECTION, LT WING TRAILING EDGE SKIN WAS FOUND TO HAVE A 1.125 INCH CRACK PROPAGATING FROM RIVET TO TRAIL ING EDGE NEAR GROUND SPOILER ACTUATOR CUTOUT. MAINTENANCE INSPECTED IAW MANUFACTURER'S SERVICE INFORMATION AND PLACED O N TIME CARRYOVER FOR RE-OCCURRING INSPECTIONS AT 100 FH WITH DEFINITIVE REPAIR OR REPLACEMENT AT 500 FH. 2 L 7 2 4T RT T00011AT 2007071000007 20070710 00007 SO 2007 7 10 RAIA00706039 1 20070622 A 5700 14567011007 SKIN EMB 145 EMB145LR 3260212 SO ZONE 500 CRACKED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 815HK 145048 STL - DURING INSPECTION, LT WING TRAILING EDGE SKIN WAS FOUND TO HAVE A 1.125 INCH CRACK PROPAGATING FROM RIVET TO TRAIL ING EDGE NEAR GROUND SPOILER ACTUATOR CUTOUT. MAINTENANCE INSPECTED IAW MANUFACTURER'S SERVICE INFORMATION AND PLACED O N TIME CARRYOVER FOR REOCCURING INSPECTIONS AT 100 FH WITH DEFINITIVE REPAIR OR REPLACEMENT AT 500 FH. 2 L 7 2 4T RT T00011AT 2007071000008 20070710 00008 NM 2007 7 10 SWAA073186 1 20070626 A 3350 20131A BATTERY BOEING 737 7373K2 13844BA NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER PE R MM. 2 L 7 2 4F RT A16WE 2007071000009 20070710 00009 NM 2007 7 10 SWAA073188 1 20070626 A 3350 3071BPEGPL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 17 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007071000011 20070710 00011 2007 7 10 SWAA073184 4 20070626 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 757LV 29850 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071000013 20070710 00013 NM 2007 7 10 SWAA073190 1 20070626 A 5330 6545766 SKIN BOEING 737 7373A4 1384585 NM BS 382 S26L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 382, STR 26L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007071000020 20070710 00020 NM 2007 7 10 SWAA073194 1 20070626 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 597 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071000036 20070710 00036 SO 2007 7 10 FDKA200705193 1 20070507 A 3150 UNKNOWN EMB 145 EMB145LR 3260212 SO UNKNOWN A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 831MJ 145273 RTG DUE TO RUDDER HARD OVER PROTECTION FAIL MESSAGE. MX RESET AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007071000039 20070710 00039 SO 2007 7 10 FDKA200705197 1 20070509 A 2720 UNKNOWN EMB 145 EMB145LR 3260212 SO RUDDER UNKNOWN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 847MJ 145517 RUDDER HARD OVER PROTECTION FAIL. MX RESET SYSTEM, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007071000043 20070710 00043 SO 2007 7 10 FDKA200705205 1 20070514 A 3150 UNKNOWN EMB 145 EMB145LR 3260212 SO UNKNOWN A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 847MJ 145517 RUDDER HARD OVER PROTECTION FAIL. RESET NO FURTHER ACTION REQUIRED. 2 L 7 2 4T RT T00011AT 2007071000063 20070710 00063 SO 2007 7 10 FDKA200705225 1 20070526 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6129 RDU (1038 PHX LCL). MAIN CABIN DOOR HARD TO CLOSE. MX LUBED DOOR ROLLER, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007071000065 20070710 00065 NM 2007 7 10 DHL2007785005 1 20070627 A 5740 651922226 SUPPORT FITTING BOEING 727 727214 138407R NM NR 8 SPOILER ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 NR 8 SPOILER ACTUATOR SUPPORT FITTING IS CRACKED. REMOVED FITTING AND REPLACED WITH NEW FITTING PER B727 SRM 51-30-2 FI G 1, FIG 15, AND B727 MM 27-61-91. 2 L 7 3 4F A3WE 2007071000066 20070710 00066 SO 2007 7 10 FDKA200705229 1 20070507 A 5320 14526437001 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 850MJ 145568 RIGHT FLOOR SUPPORT GUSSET, BETWEEN FRAME 59 AND 60 IS CORRODED. THE DAMAGED PART HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2007071000069 20070710 00069 NM 2007 7 10 DU4R2007143 1 20070624 A 5330 SKIN BOEING 757 757232 1384965 NM BS 607 S16L DENTED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 638DL 23761 FOUND DENT IN FUSELAGE SKIN BS 606 AND DENTED STRINGER 16L. REPAIRED BY CUTTING OUT DENTED AREA, FABRICATING AND INSTAL LING REPAIR DOUBLER 9-3/4 BY 7-1/2 FROM 2024-T3 .050, STRINGER REPAIR 10-1/2 BY 3-1/4 FROM BAC1498-200 IAW B757 SRM 53- 00-03 FIG 201 AND DELTA ERA NR 456427-14 REV A DATED 06/15/07 APPROVED BY 14 CFR 121.379(B). 2 L 7 2 4F RT A2NM 2007071000074 20070710 00074 NM 2007 7 10 07FDEA02305 1 20070628 A 5322 65163401 SHEAR TIE BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT PIT SHEAR TIE CORRODED STA 990 STR 28-29L FAB SHEAR TIE AND SHIM REF SRM 53-10-4. TREATED AND PRIMED REPAIR MATERIA L FOR SHEAR TIE 7075-O-071. HEAT TREATED TO T6, CUT OUT DAMAGED AREA, INSTALLED REPAIR PART REF SRM 53-10-3. THIS REPA IR CLASSIFIED AS MAJOR. 2 L 7 3 4F RT A3WE 2007071000096 20070710 00096 EA 2007 7 10 A6WA200740295 1 20070531 A 5320 601R75262159 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 418AW 7618 HYDRAULIC PRESSURE TRANSDUCER BRACKET CRACKED APPROX .1 INCH LONG IN LT WHEEL WELL CEILING. (M) 2 L 7 2 4F RT A21EA 2007071000112 20070710 00112 SO 2007 7 10 FDKA200705237 1 20070509 A 5350 FLANGE EMB 145 EMB145LR 3260212 SO TAILCONE DOOR CRACKED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 850MJ 145568 TAIL CONE FAIRING DOOR, 313CL, INNER FLANGE IS CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER TO REPAIR THE DAMAGE. 2 L 7 2 4T RT T00011AT 2007071000113 20070710 00113 SO 2007 7 10 FDKA200705238 1 20070508 A 5512 14534370414 ELEVATOR EMB 145 EMB145LR 3260212 SO RT ELEVATOR DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 850MJ 145568 UPPER SURFACE OF RIGHT ELEVATOR IS DAMAGED 3.6 INCHES FROM THE OUTBOARD END. THE DAMAGE HAS BEEN REPAIRED. 2 L 7 2 4T RT T00011AT 2007071000114 20070710 00114 NM 2007 7 10 AMTA200700290 1 20070614 A 2150 6259283 SENSOR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT A/C PACK FAILED A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 514AT 27971 EICAS MSGS RT PACK OFF & PACK TEMP DISPLAYED RT INOP & PACK OFF LGTS ILLUM, LIGHTS EXTINGUISHED WHEN PACK RESET SWITCH I N STANDBY, OPERATION NORMAL IN STANDBY. OCCURED AT FL 350 MACH .79. PERFORMED PACK TEMP CONTROLLER BITE PROC, IAW FIM 21-51-00, FIG 104, FOUND COMPRESSOR SENSOR FAULT, REMOVED AND REPLACED RT PACK COMPRESSOR SENSOR IAW 21-51-06-4, OPS CHE CKS NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007071000115 20070710 00115 NM 2007 7 10 DLM90070761 1 20070619 A 5310 SKIN DOUG MD900 MD900 3027375 NM BS 218 S17-18L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 UPPER FUSELAGE SKIN HAS 2 DENTS CONTAINED IN ONE BAY STA 218 LONGERON 17-18L. DEPTH = .031 BY MINOR = .75 DEPTH = .015 BY MINOR = .25 2ND DENT CLOSER THAN 1 INCH FROM STRUCTURE. REPAIRED SKIN IAW MD90 SRM 53-30-01 FIG 5. 1 G 7 2 3U NC H19NM 2007071000116 20070710 00116 SO 2007 7 10 FDKA200705240 1 20070523 A 5312 FIREWALL EMB 145 EMB145LR 3260212 SO APU BAY CRACKED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 831MJ 145273 THE APU FIREWALL IS CRACKED AT THE RIGHT UPPER MOUNT BRACKET. THE DAMAGE HAS BEEN REPAIRED. 2 L 7 2 4T RT T00011AT 2007071000117 20070710 00117 SO 2007 7 10 FDKA200705241 1 20070523 A 5312 FIREWALL EMB 145 EMB145LR 3260212 SO APU BAY CRACKED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 831MJ 145273 THE APU FIREWALL IS CRACKED AT THE LEFT UPPER MOUNT BRACKET. THE DAMAGE HAS BEEN REPAIRED. 2 L 7 2 4T RT T00011AT 2007071000118 20070710 00118 NM 2007 7 10 DL76L070768 1 20070621 A 3810 288235 COMPRESSOR BOEING 767 767332 1382001 NM WATER ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 27 180DN 25985 FLIGHT ATTENDANT REPORTS BURNING ODOR IN AFT GALLEY. FWD TO MCO AND PLACARD PER MEL M38-10-01A. T/S SUSPECT WATER COMP RESSOR. DISCONNECTED COMPRESSOR C/P AND FWD TO MCO PER MEL 38-10-01A. REPLACED WATER COMP PER IPC 38-15-01-03 ITEM 38 0 OPERATIONAL CK OK. 2 L 7 2 4F RT A1NM 2007071000119 20070710 00119 NM 2007 7 10 DLM88070774 1 20070621 A 3230 329001564 CONTROL VALVE DOUG MD88 MD88 3023688 NM MLG BYPASSING A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 909DL 49540 UNSAFE UP INDICATION AFTER SELECTING GEAR UP. ALL GEAR INDICATED UNSAFE. GEAR DOOR OPEN LIGHTS REMAINED ON, ALL PUMPS WERE CHECKED ON AND HYD PRESS WAS GOOD. REMOVED AND BEGAN INSTALLING LANDING GEAR CONTROL VALVE PER 32-32-01. COMPLET ED LANDING GEAR CONTROL VALVE CHANGE AS PER MCC REQUEST REF MM32-32-01-201. GEAR OPS CHK GOOD. 2 L 7 2 4F RT A6WE 2007071000120 20070710 00120 NM 2007 7 10 SWAA073201 1 20070627 A 3350 10107451 SIGN BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 458WN 33857 R2 DOOR EMERGENCY EXIT SIGN BROKEN. R&R EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007071000121 20070710 00121 NM 2007 7 10 DL76S070775 1 20070622 A 5420 112T7010 NUT CLIP BOEING 767 767332 1382001 NM NACELLE UNKNOWN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 DURING ACCOMPLISHMENT OF EA 01-074906-03AD, NEED TEE CLIPS ARE ATTACHED TO THE SUBJECT PITCH LOAD FITTINGS, HOWEVER THEY HAD SHORT EDGE MARGIN. BACO GAVE AMOC APPROVAL FOR THE SHORT EDGE MARGIN CONDITION. REFERENCE ER/A 461700-14AD. 2 L 7 2 4F RT A1NM 2007071000122 20070710 00122 NM 2007 7 10 SWAA073199 1 20070627 A 3260 18991 DOWNLOCK SENSOR BOEING 737 7373H4 1384600 NM LT MLG FAULTY A SWAA K NONE N FALSE WARNING NR NOT REPORTED 1 SW 29 392SW 27379 DECLARED EMERGENCY, LT MAIN LANDING GEAR LIGHT FLUCTUATED BETWEEN GREEN AND RED WITH NORMAL EXTENSION. R&R LT MAIN LAN DING GEAR DOWN LOCK SENSOR PER MM. 2 L 7 2 4F RT A16WE 2007071000124 20070710 00124 NM 2007 7 10 DLM88070776 1 20070618 A 5100 NONE DOUG MD88 MD88 3023688 NM NONE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 903DE 53380 DURING SCHEDULED INSPECTION OF THE OVERWING HEATER BLANKET AN ADDITIONAL VOID WAS REPORTED IN THE BONDLINE BETWEEN THE H EATER BLANKET AND THE WING UPPER SKIN. ENGINEERING EVALUATION DETERMINED THE VOID WAS NOT NEW. THE DIFFERENCE FROM PRI OR INSPECTION WAS BECAUSE OF THE ACCURACY OF THE NDI METHOD. THE VOID WAS STILL WITHIN MANUAL LIMITS. DISPOSITIONED PE R ER/A 09-093771-14AD. 2 L 7 2 4F RT A6WE 2007071000125 20070710 00125 NM 2007 7 10 DL76S070777 1 20070622 A 5415 FITTING BOEING 767 767332 1382001 NM NACELLE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 DURING INSPECTION OF THE AFT PITCH LOAD FITTING PER EA 01-074906-03AD, SEVERAL HOLES WERE FOUND TO BE OVERSIZED BEYOND T HE ALLOWABLE LIMITS. BOEING WAS CONTACTED AND THEY ALLOWED THE OVERSIZED HOLES WITH CORRESPONDING MATCHING FASTENERS AS REFERENCED IN ERA 462299-14AD. 2 L 7 2 4F RT A1NM 2007071000126 20070710 00126 NM 2007 7 10 DL76S070778 1 20070622 A 5712 RIB BOEING 767 767332 1382001 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 DURING ACCOMPLISHMENT OF SIP EO, THE LHS WING FRONT SPAR AT RIB NR 8 WAS FOUND CRACKED AT A FASTENER HOLE. THE CRACK WA S APPROXIMATELY 0.030 INCH IN LENGTH. THE SUBJECT HOLE FROM WHICH THE CRACK EMANATED WAS ALREADY BEYOND THE EA ALLOWABL ES. BOEING APPROVED REPAIR INSTALLED PER 461698-14AD. 2 L 7 2 4F RT A1NM 2007071000128 20070710 00128 NM 2007 7 10 DLM88070779 1 20070622 A 2120 DUCT DOUG MD88 MD88 3023688 NM AIR DISTRIBUTION CONTAMINATED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 953DL 49884 DURING PUSHBACK AFT SMOKE DETECTORS WENT OFF WITH A SLIGHT ODOR OF SMOKE IN CABIN. FOUND SMALL AMT OF SYDROL STAINS IN APU INLET CLEANED SAME PERFORMED OPN 5090 ALT DUCT BURNOUT AND PERF OP 7804 WATER BAG REPLACED. RAN A/C SYSTEMS NO OD ORS OR SMOKE PRESENT OK FOR SVC 2 L 7 2 4F RT A6WE 2007071000131 20070710 00131 NM 2007 7 10 DLM88070780 1 20070621 A 2432 203BC1021 CHARGER DOUG MD88 MD88 3023688 NM E/E BAY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 27 914DL 49545 ON PREFLIGHT, FOUND BATTERY CHARGER C/B POPPED. RESET AND RAN EMERGENCY POWER CHECK. FOUND BATTERY CHARGER C/B RE-POPP ED. T/S PER WDM FOUND A AND C PHASE WIRES FROM C/B TO CHARGER BOTH MOUNTED ON C PHASE LUG. REWIRED C/B PER WDM. REPLA CED BATTERIES AND CHARGER AND C/B. ALL REST PER M/M NML. OK FOR SERVICE. 2 L 7 2 4F RT A6WE 2007071000132 20070710 00132 NM 2007 7 10 DLM88070781 1 20070620 A 5753 VANE DOUG MD88 MD88 3023688 NM RT WING TE FLAP DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 DAMAGE PREVIOUS REPAIR AND DENTS ON RT WING OUTBD FLAP INBD GUIDE VANE. REPAIRED PER SRM 57-03D PARA 8A FIG 9A. 2 L 7 2 4F RT A6WE 2007071000134 20070710 00134 NM 2007 7 10 DL76G070782 1 20070622 A 3350 LIGHT BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1611B 30595 EMERGENCY LIGHTS SEAT MOUNTED FROM 24AB TO 32AB INOP. SWAPPED BATTERIES, NO HELP. CHECKED OPERATION OF EMERGENCY LIGHT S IN A/C CABIN, ALL EMERGENCY LIGHTS CK GOOD PER FIM, UNABLE TO DUPLICATE. 2 L 7 2 4F RT A1NM 2007071000135 20070710 00135 NM 2007 7 10 SWAA073210 1 20070627 A 5240 6545849 HINGE BOEING 737 7375H4 138449D NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR LOWER GATE HINGE CRACKED. R&R LOWER GATE HINGE PER SRM. 2 L 7 2 4F RT A16WE 2007071000136 20070710 00136 NM 2007 7 10 DL76L070783 1 20070622 A 5100 UNKNOWN BOEING 767 767332 1382001 NM UNKNOWN A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 197DN 28454 RT ENG VALVE AND SPAR VALVE FAIL TO OPEN DURING START. RESET SPAR VALVE C/B, VISUAL INSP SPAR VALVE OK. RESET FIRE HAN DLE ENG RUN TEST GOOD. 2 L 7 2 4F RT A1NM 2007071000138 20070710 00138 NE 2007 7 10 DL757070784 2 20070622 A 7261 PW2037RTC ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 LEAKING A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 6700 47839 30337 716593 AFTER T/O FROM SNA RIGHT ENGINE OIL PRESSURE LIGHT FOLLOWED BY EICAS MSG THEN OIL QTY WENT TO ZERO SHUTDOWN ENGINE IN FL IGHT. COMPLETED ENGINE SHUTDOWN REPORT. REPLACED LEAKING AIR/OIL COOLER. NO METAL FOUND ON CHIP DETECTORS OR MAIN OIL FILTER. RAN ENGINE AT IDLE FOR 5 MINUTES. THEN REPLACED THE MAIN OIL FILTER AGAIN. NO LEAKS AFTER ENGINE RUN. TOPPE D OFF OIL TO FULL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071000139 20070710 00139 NM 2007 7 10 DLM88070788 1 20070620 A 5712 RIB DOUG MD88 MD88 3023688 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 CRACKED RIB ON LT WING OUTBD REMOVABLE TRAILING EDGE. REPAIRED PER SRM 57-01 FIG 3 ON N/R T0058787 HMV/GDL. 2 L 7 2 4F RT A6WE 2007071000140 20070710 00140 NM 2007 7 10 SWAA073206 1 20070627 A 5311 6546559 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 927, STR 19L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007071000141 20070710 00141 NM 2007 7 10 DLM88070789 1 20070619 A 5712 RIB DOUG MD88 MD88 3023688 NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 CRACKED RT WING OUTBD REMOVABLE TRAILING EDGE RIB. REPAIRED PER SRM 57-01 FIG 3 ON N/R T0058792 HMV/GDL. 2 L 7 2 4F RT A6WE 2007071000142 20070710 00142 NM 2007 7 10 DLM88070790 1 20070620 A 5313 LONGERON DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 CRACKED LONGERON 6RH AT STA. Y=927. REPAIRED PER SRM 53-02 FIG 18 ON N/R T0058771 HMV/GDL. 2 L 7 2 4F RT A6WE 2007071000143 20070710 00143 NM 2007 7 10 DLM88070791 1 20070620 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 CORROSION ON LEFT CUSP WEB AT STA Y=878, TASK 58-53313. REPAIRED PER ERA 398191MA ON N/R T0058322. 2 L 7 2 4F RT A6WE 2007071000144 20070710 00144 NM 2007 7 10 DLM88070792 1 20070619 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 984-1003 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 CORROSION ON LEFT CUSP WEB BETWEEN STA Y=984 AND Y=1003, TASK 58-53313. REPAIRED PER ERA 398191-14MA ON N/R T0058324 HM V/GDL. 2 L 7 2 4F RT A6WE 2007071000145 20070710 00145 NM 2007 7 10 DLM88070793 1 20070618 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 CORROSION ON CUSP WEB IN PASSENGER CABIN AT STA Y-589. REPAIRED PER EA 398191-14MA ON N/R T0058363 HMV/GDL. 2 L 7 2 4F RT A6WE 2007071000146 20070710 00146 NM 2007 7 10 DLM88070794 1 20070617 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 513 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 CORROSION ON CUSP WEB IN PASSENGER CABIN AT STA Y=513 TASK 58-53313. REPAIRED PER ERA 398191-14MA ON NR T0058366 HMV/GD L. 2 L 7 2 4F RT A6WE 2007071000147 20070710 00147 NM 2007 7 10 DLM88070795 1 20070616 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 CORROSOIN ON CUSP WEB IN PASSENGER CABIN BETWEEN STA Y=1071-1098 TASK 58-53313. REPAIRED PER ERA 398191-14MA ON N/R T00 58367 HMV/GDL. 2 L 7 2 4F RT A6WE 2007071000148 20070710 00148 NM 2007 7 10 DLM88070796 1 20070620 A 5310 DOOR FRAME DOUG MD88 MD88 3023688 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 GALVANIC CORROSION ON FWD CARGO COMPARTMENT DOOR JAMB LOWER BEAM TASK 51-53300. REPAIRED PER SRM 53-05D FIG 804D SHEET 1 ON N/R TOO58462 HMV/GDL. 2 L 7 2 4F RT A6WE 2007071000149 20070710 00149 NM 2007 7 10 DLM88070797 1 20070619 A 5340 FITTING DOUG MD88 MD88 3023688 NM CARGO DOOR FRAME CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 GALVANIC CORROSION ON AFT CARGO COMPARTMENT DOOR JAMB LOWER BEAM. TASK 51-53300. REMOVED AND REPLACED IAW DWG 5936038 ON N/R T0058464 HMV/GDL. 2 L 7 2 4F RT A6WE 2007071000150 20070710 00150 NM 2007 7 10 DLM88070798 1 20070615 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 CRACKED LT CUSP WEB AT STA Y=1186. REPAIRED PER ERA 398191-14MA ON N/R T0058897 HMV/GDL. 2 L 7 2 4F RT A6WE 2007071000151 20070710 00151 NM 2007 7 10 DLM88070799 1 20070620 A 5310 DOOR FRAME DOUG MD88 MD88 3023688 NM OVERWING DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 CRACKED AFT DOOR JAMB FRAME ON LT AFT OVERWING DOOR. REPAIRED PER SRM 52-05D FIG 51 ON N/R T0058927 HMV/GDL. 2 L 7 2 4F RT A6WE 2007062900011 20070629 00011 NM 2007 6 29 SWAA073079 1 20070620 A 5230 STRUCTURE BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FWD CARGO DOOR CRACKED AT LOWER DOOR STOP FITTING NEAR TEE BEAM. REPAIRED DOOR PER S RM. 2 L 7 2 4F RT A16WE 2007062900021 20070629 00021 EA 2007 6 29 COMA0760436 1 20070615 A 3260 750005000 VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 408CA 17530 7440 FLIGHT 5508 - EN ROUTE BNA-JFK RECEIVED A LANDING GEAR DISAGREE WITH ASSOCIATED VIBRATION, FLIGHT RETURNED TO CVG. REPL ACED THE MAIN LANDING GEAR SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2007062900032 20070629 00032 NM 2007 6 29 ASAA0791794 1 20070531 A 5310 146A750355 RAIL BOEING 737 737990 NM BS 727D CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT SUPPORT RAIL CORRODED. REPAIRED IAW EA5310 02724. 2 L 7 4 4F RT A16WE 2007062900039 20070629 00039 NM 2007 6 29 ASAA0791801 1 20070531 A 5320 SILL BOEING 737 737990 NM BS 727-767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT DUST SILL CORRODED. REPAIRED IAW SRM 53-00-53. 2 L 7 4 4F RT A16WE 2007062900055 20070629 00055 EU 2007 6 29 COEA0701913 1 20070328 A 5315 S53372411204 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 913FX 250 DURING CHECK, FOUND CORROSION ON LEFT FLOORBEAM FS 17 AT NUT PLATE HOLE. REMOVED CORROSION, CUT OUT DAMAGED SECTION, FA BRICATED AND INSTALLED FABRICATED FLOORBEAM SECTION IAW ATR42 SRM. (M) 2 H 7 2 4T RT A53EU 2007062900057 20070629 00057 EU 2007 6 29 COEA0716908 1 20070307 A 5340 S27381833218 ATTACH ANGLE AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 908FX 023 CORROSION FOUND BETWEEN FS 46 AND FS 47 UPPER AFT WEB COMMON TO QUADRANT INTERCOSTALS. REMOVED QUADRANT INTERCOSTALS. FABRICATED AND INSTALLED INTERCOSTAL ATTACH ANGLES IAW ATR42 SRM. (M) 2 H 7 2 4T RT A53EU 2007062900061 20070629 00061 NM 2007 6 29 QXEA200701003 1 20070612 A 5740 BARREL NUT BOMBDR DHC8 DHC8402 1390042 NM WING TO BODY CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - WHEN DISASSEMBLING RIGHT WING TO FUSELAGE FORWARD OUTBOARD MOUNT VERTICAL TIE BOLT, TO CHANNEL NUT BARREL FOUND NUT CRACKED AND PLI WASHER INNER AND OUTER RINGS. REPAIRED IAW RD8/4-51-102. 2 H 7 2 4T RT A13NM 2007062900063 20070629 00063 NM 2007 6 29 QXEA200701000 1 20070611 A 5753 SKIN BOMBDR DHC8 DHC8402 1390042 NM LT WING TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - LEFT INBOARD FLAP UPPER SURFACE IS CHAFED AT YW 117.50. REPAIRED IAW SRM 57-51-30, 51-25-05. 2 H 7 2 4T RT A13NM 2007062900081 20070629 00081 NM 2007 6 29 DL76P070737 1 20070616 A 2150 UNKNOWN BOEING 767 767332 1382001 NM A/C PACK UNKNOWN A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 143DA 25991 WHEN L PACK SELECTED OFF NO PACK OFF LIGHT AND NO L PACK OFF MSG. TRIED PACK RESET AND BLEED RESETS BEFORE RETURNING TO GATE AT SHUTDOWN GOT PAC OFF MSG AND OFF LIGHT. CHECKED FLOW CONT VALVE L PACK CONNECTIONS. RESEATED L PACK CONTROLLE R AND L PAC FLOW CONTROL CARD M863, ALL CKS NML. 2 L 7 2 4F RT A1NM 2007062900110 20070629 00110 NM 2007 6 29 07FDEA02248 1 20070621 A 5311 65163391 FRAME BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT PIT SHEAR TIE CORRODED STA 970 BETWEEN STRINGER 28-29L REMOVED SHEAR TIE, REMOVED CORROSION ON SIDE OF FRAME. CUT S HEAR TIE FROM FRAME. FABRICATED SHEAR TIE REPAIR FROM 7075-0 .071, HEAT TREATED TO T-6 CONDITION ON SNRM NR N01032, 81 30 TRACKING NR 2007-06-30. DRILLED AND INSTALLED SHEAR TIE REPAIR REF 53-10-4 FIG 15, SRM 51-30-2, SRM 51-10-1. 2 L 7 3 4F RT A3WE 2007070200004 20070702 00004 NM 2007 7 2 07FDEA02252 1 20070621 A 5330 SKIN BOEING 727 727233 138408A NM BS 680-740 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD LOWER FUSELAGE BELLY SKIN, BS 680 TO 740 STR 26L TO S-26R NEEDS TO BE REPLACED DUE TO MULTIPLE AREAS OF CORROSION AND DAMAGES. [08-29-07] BELLY SKIN AT STA. 680 TO 740, BETWEEN STR 26L TO 26R, WAS REMOVED. NEW SKIN WAS DRILLED UP TO MATCH EXISTING STRUCTURE. DOUBLER/ TRIPLER WAS INSTALLED AT STA 700 TO 740, STR 26L TO 26R, REF FED EX EA 7-5330-1 13938. INSTALLED NEW SKIN (65-54590-7) AND RELATED WING TO BODY STRUCTURE. REF' S USED SRM 51-10-1, 51-30-2. 2 L 7 3 4F RT A3WE 2007070200012 20070702 00012 NM 2007 7 2 07FDEA02261 1 20070622 A 5240 DOOR FRAME BOEING 727 727233 138408A NM ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 HIDDEN DAMAGE INSPECTION LT AFT SERVICE DOOR, BOTTOM FRAME, INNER SURFACE IS CORRODED UNDER LEVELING COMPOUND FROM FWD T O AFT END OF FRAME. [07-06-07] DRILLED UP NEW BEAM PER SRM 51-30-5 PG.1, INSTALLED LOWER BEAM ON AFT SERVICE DOOR, P ER SRM 51-10-1 PG.10 51-30-2 PG 1-5 INSTALLED LOWER GATE PER OHM 52-40-07 PG 505 AND INSTALLED COVER PANELS PER SRM 51-30-2 PG 2-5 2 L 7 3 4F RT A3WE 2007070200015 20070702 00015 NM 2007 7 2 AWXA200700761 1 20070604 A 5320 143N8338U25 INTERCOSTAL BOEING 757 757225 1384959 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 MCN - MAJOR REPAIR - FOUND CRACKED INTERCOSTAL WEB, BS 690, S11L. REPLACED INTERCOSTAL WEB, BS 690, S11L IAW AWA TASK C ARD M1C53606. 2 L 7 2 4F RT A2NM 2007070200027 20070702 00027 NM 2007 7 2 DHL2007783521 1 20070607 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1250 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 FUSELAGE SKIN AT MOVABLE AIRSTAIRS BS 1250 CREASED AND DENTED. REMOVED DAMAGED SECTION OF AFT AIRSTAIRS EXTERNAL SKIN F ROM BS 1223 TO BS 1329 IAW B727 SRM 52-10-2, FIG 4. FABRICATED NEW SKIN SECTION, FROM 2024T3 .040, 106 BY 52.5 IAW B727 SRM 52-10-1 FIG 3 AND 52-10-2, FIG 4. TREATED, PRIMED AND INSTALLED PARTS IAW B727 SRM 51-10-2 AND 52-10-2, FIG 4. 2 L 7 3 4F A3WE 2007070200033 20070702 00033 NM 2007 7 2 07FDEA02268 1 20070625 A 5280 STRUCTURE DOUG MD11 MD11F 3023600 NM LT MLG DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 LANDING GEAR, LT MLG FLIPPER DOOR, FWD EDGE FOUND CRACKED. [07-13-07] REPAIR CARRIED OUT AT MLG - LT MLG FLIPPER DOOR , FWD EDGE AS PER SRM 52-10-00 FIGURE 18 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007070200034 20070702 00034 NM 2007 7 2 07FDEA02269 1 20070625 A 5280 HINGE DOUG MD11 MD11F 3023600 NM MLG DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 LANDING GEAR, FLIPPER DOOR OUTBOARD EDGE ADJACENT TO FORWARD HINGE FOUND CRACKED. [07-16-07] REPAIR CARRIED OUT AT LA NDING GEAR - RT FLIPPER DOOR OUTBOARD EDGE ADJACENT TO FORWARD HINGE AS PER SRM 52-10-00 FIGURE 18 VOLUME I. REPAIR CLA SSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007070200035 20070702 00035 NM 2007 7 2 07FDEA02270 1 20070625 A 5710 DUCT DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 RIGHT WING LEADING EDGE PANEL NEAR TELESCOPING DUCT AREA FOUND CRACKED. 2 L 7 3 4F RT A22WE 2007070200036 20070702 00036 NM 2007 7 2 07FDEA02271 1 20070625 A 5754 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 575FE 48500 RIGHT WING, AFTER REMOVING NR 3 SLAT FOUND OUTBOARD MOUNTING HOLE WORN. [07-06-07] WORN OUTBOARD MOUNTING HOLE AT RIGH T HAND WING NR 3 SLAT REWORKED AND INSTALLED WITH NEW FABRICATED BUSHING AS PER FEDEX E.A. 1-5740-112339, REPAIR CL ASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007070200040 20070702 00040 NM 2007 7 2 070128 1 20070618 A 3246 26088911 WHEEL DOUG MD80 MD83 3023681 NM MLG FAILED A WX0A O OTHER O OTHER LD LANDING 1 WP 19 872GA 53295 UPON LANDING AT FAT, RIGHT OUTBOARD TIRE BLOWN OUT ON LANDING. AIRCRAFT PROCEEDED TO THE TERMINAL WITHOUT INCIDENT. IN SPECTION BY MAINTENANCE DEPARTMENT PERSONNEL FOUND SEVERAL DISCREPANCIES ASSOCIATED WITH THE DESTRUCTION OF THE TIRE. B ROKEN BRAKE LINES, ANTI-SKID VALVE, NR 4 BRAKE, WING FLAP BUTE DOORS AND DENTS IN THE RIGHT WING FLAP. AIRCRAFT WAS REP AIRED AND RELEASED FOR FERRY FLIGHT TO ALLEGIANT AIR CONTRACTED MAINTENANCE FACILITY FOR CONTINUED REPAIRS. THE AIRCRAF T WILL RETURN TO SERVICE UPON COMPLETION OF ALL REPAIRS. 2 L 7 2 4F RT 2007070200043 20070702 00043 NM 2007 7 2 QXEA200701021 1 20070624 A 6120 LIMIT SWITCH DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS OUT OF ADJUST A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 349PH 486 SEA FLIGHT NR 2104 AUTOFEATHER DID NOT ARM. MAINTENANCE ADJUSTED THE NR 1 POWER LEVER LIMIT SWITCH. OPERATIONAL CHECK GOOD. NO PARTS REPLACED AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007070200044 20070702 00044 NE 2007 7 2 HALA0700264 2 20070624 A 7261 SEAL BOEING 767 7673CB 1385187 NM PWA 4060 PW4060 52119 NE ENGINE LEAKING A HALA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 WP 13 590HA 33467 ETOPS SIGNIFICANT SYSTEM - PER TECH SERVICE TSI "NR 2 ENG OIL CONSUMPTION" ADDED 6 PINTS TO NR 2 ENGINE. ACCOMPLISHED FIM 71-05-00 FIG 106 STEPS 1 AND 2 FOUND OIL COMING OUT (DURING DRY MOTOR) OF "OIL SEAL DRAIN FOR THE EEC ALTERNATOR DRI VE". REMOVED AND REPLACED EEC ALT DR OIL SEAL PER AMM 72-61-05 OPS AND LEAK CHK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007070200048 20070702 00048 EU 2007 7 2 AWXA200700766 1 20070621 A 5321 D5367005000200 FLOOR PANEL AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 SAL - MAJOR REPAIR - CORROSION ON CABIN FLOORBOARD 261FF, FR 66 - FR 68, +Y1292 TO +Y1732. REPLACED CABIN FLOORBOARD 26 1FF, FR 66 - FR 68, +Y1292 TO +Y1732 IAW AWA TASK CARD C1C53308. 2 L 7 2 4F RT A28NM 2007070200053 20070702 00053 SO 2007 7 2 CHQA200700032 1 20070625 A 2910 NAS16124 O-RING EMB 145 EMB145LR 3260212 SO HYD SYSTEM LEAKING A CHQA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 11 576RP 14500856 FLIGHT 6267 - SBN-CVG - DESCENDING 10000FT, OBSERVED HYD 1 LOW QTY EICAS MESSAGE. RAN QRH AND OBSERVED A DECREASE IN HY DRAULIC FLUID FOLLOWED BY A DECREASE IN HYDRAULIC PRESSURE. OBSERVED A COMPLETE LOSS OF ENGINE DRIVEN HYDRAULIC PRESSUR E, ELECTRIC PUMP ON, AND A SLOW LOSS OF ELECTRIC HYDRAULIC PRESSURE. RAN QRH FOR E1 HYD PUMP FAIL EICAS MESSAGE AND DEC LARED AN EMERGENCY. LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A LEAK ON THE NOSE LANDING GEAR DOOR ACTUATOR LEFT FITT ING. REMOVED AND REPLACED THE FITTING O-RING IAW EMB MM 32-33-05. 2 L 7 2 4T RT T00011AT 2007070200055 20070702 00055 EU 2007 7 2 NWAA072223358 1 20070624 A 2530 COFFEEMAKER AIRBUS A330 A330* EU GALLEY SMOKE A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 858NW 0718 SMOKE REPORTED IN THE GALLEY 1B FROM RIGHT COFFEEMAKER. DE-POWERED COFFEE MAKER VIA PUSH BUTTON CIRCUIT BREAKER AND SMO KE DISSIPATED, LANDING WAS UNEVENTFUL. COFFEE MAKER REMOVED AND REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A46NM 2007070200057 20070702 00057 NM 2007 7 2 07FDEA02273 1 20070626 A 5753 BUSHING DOUG MD11 MD11F 3023600 NM TE FLAPS WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 575FE 48500 LEFT WING INBOARD FLAP VANE OUTBOARD TEE FITTING BUSHING FOUND WORN. [07-09-07] COMPLIED WITH FEDEX E.A. 1-5750-112340 , REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007070200063 20070702 00063 NM 2007 7 2 07FDEA02279 1 20070626 A 5311 65561001 FRAME BOEING 727 727233 138408A NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 286FE 22623 ON AGING A/C INSP, FOUND EXISTING REPAIR LOCATED AT BS 560 ON FRAME BETWEEN STR S-22L AND S-26, DID NOT COMFORM TO SRM 5 1-40-3 PG 1-6. REMOVED OLD DOUBLER AND FILLER, FABRICATED NEW DOUBLER AND FILLER, HEAT TREATED, ALODINED AND PRIMED REF SRM 51-40-3 PG 1-6. 2 L 7 3 4F RT A3WE 2007070200079 20070702 00079 EA 2007 7 2 SIMA200717706 1 20070624 A 2730 70744 PITCH CONTROL CNDAIR CL600 CL6002C10 1390015 EA ZONE 300 FAILED A SIMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 503AE 11971 10021 CAPTAIN'S YOKE HAD PLAY ON CLIMB-OUT, COULD FEEL TWO INCHES OF CONTROL MOVEMENT AFTER TRIMMED. ATC DECLARED EMERGENCY. REMOVED AND REPLACED MOTOR CONTROL UNIT IAW CRJ AMM 27-42-07 AND OPERATIONAL CHECKS IAW CRJ AMM 27-40-00 WITH NO DEFECT S. PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007070200082 20070702 00082 NM 2007 7 2 ASAA0791812 1 20070531 A 5347 146A750611 CARGO TRACK BOEING 737 737990 NM BS 727I CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO PIT FLOOR RAIL SPLICE CORRODED. REPAIRED IAW SRM 51-40-05 AND 51-40-02. 2 L 7 4 4F RT A16WE 2007070200107 20070702 00107 NM 2007 7 2 2007UALA02134 1 20070619 A 4900 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE APU MALFUNCTIONED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 107UA 26900 AT DEPARTURE -BAT CHARGER APU- AGAIN. WOULD NOT CLEAR. [07-20-07] REPLACED BATTERY WITH NEW PER MM24 -31-06 PG401. MESSAGE CLEARED. OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007070200111 20070702 00111 NM 2007 7 2 2007UALA02139 1 20070619 A 3510 MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT DEFECTIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 OXYGEN MASK DEFECTIVE AT (1=CAPT, 2=1ST OFF, 3=1ST OBS), CREW COMMENTS, TEST BUTTON STICKS IN WHEN PUSHED. [08-07-07] REPLACED MASK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007073100057 20070731 00057 2007 7 31 2007UALA02678 4 20070716 A 2565 SLIDE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 927UA 26649 CABIN 1L DOOR ESCAPE SLIDE HAS SHIFTED AFT IN CONTAINER, GIRT IS MISROUTED AROUND AFT GIRT BAR STOW BRACKET. [08-08-0 7] ADJUSTED SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007070200113 20070702 00113 NM 2007 7 2 2007UALA02142 1 20070619 A 5210 HINGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE PAX DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 567UA 26673 THE 2R MED PASS DOOR CRACKED AT UPPER HINGE. [08-07-07] MAJOR REPAIR ACCOMPLISHED. REPAIRED 2R MED UPPER HINGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007070200115 20070702 00115 NM 2007 7 2 2007UALA02144 1 20070619 A 3350 3071BPEGPL LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 777UA 26916 THE 18C & 32G EEL LIGHTS ARE INOP. RELAMPED, OP CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007070200118 20070702 00118 NM 2007 7 2 2007UALA02148 1 20070620 A 5523 HINGE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU ELEVATOR TAB DAMAGED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 373UA 24638 TAB HINGE FREE PLAY CHECK FOUND RIGHT ELEV TAB HINGE NR 3, .046 AND NR 4, .062 OUT OF LIMITS. TRIM TAB REPLACED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007070200119 20070702 00119 NM 2007 7 2 2007UALA02149 1 20070620 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 57HJK INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EEL INOP ROW 57HJK. REPLACED SEAT EEL LIGHT AT 57H, OPS CHECK GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2007070200120 20070702 00120 NM 2007 7 2 2007UALA02150 1 20070620 A 3350 276005 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RH OVERWING 2 FW INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EMERGENCY LIGHTS INOP, RT OVERWING 2 FWD ASSEMBLIES. REPLACED FUSE FOR OVERWING ESCAPE LIGHTS. OPS CHECKS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2007070200122 20070702 00122 NM 2007 7 2 2007UALA02152 1 20070620 A 3520 OXYGEN BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ROW 16ABC READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 590UA 28708 OXYGEN BOTTLE AT ROW 16ABC LOW PRESSURE 1000 PSI. [08-07-07] REPLACED BOTTLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007070200124 20070702 00124 2007 7 2 2007UALA02154 4 20070620 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L3 DOOR UNKNOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 581UA 26701 THE 3L DOOR HARD TO ARM AND DISARM. [08-07-07] NO ABNORMAL FORCES NOTED. OPENED BOTH DOORS AND CHECKED FOR DEBRIS, NONE NOTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007070200127 20070702 00127 NM 2007 7 2 2007UALA02157 1 20070620 A 3350 1507129 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 792UA 26934 FWD PIT LIGHTS DIM AND CIRCUIT BREAKER F8 IN PNL P35 KEEPS POPPING WHEN CEILING LIGHT AT STA 980 RT IS PUSHED ON. REPLA CED LIGHT ASSEMBLY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007070200130 20070702 00130 NM 2007 7 2 SWAA073093 1 20070621 A 5315 141A5504 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 729SW 27861 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 328, RBL 39 TO RBL 41. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2007070200139 20070702 00139 NM 2007 7 2 SWAA073111 1 20070621 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM BS 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007070200144 20070702 00144 NM 2007 7 2 SWAA073107 1 20070621 A 5311 6546551 FRAME BOEING 737 7373H4 1384600 NM BS 807 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, STR 27R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007070200146 20070702 00146 NM 2007 7 2 SWAA073097 1 20070621 A 5312 6549892 BULKHEAD BOEING 737 7373H4 1384600 NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP CRACKED AT BS 1016, STR 23R, RBL 1. REPAIRED DOME CAP PER SRM. 2 L 7 2 4F RT A16WE 2007070200149 20070702 00149 NM 2007 7 2 SWAA073103 1 20070621 A 5523 65C25796 TAB BOEING 737 7373H4 1384600 NM LT ELEVATOR DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 14Y CHECK, FOUND LT ELEVATOR TAB OUTBOARD END DELAMINATED. REPAIRED ELEVATOR TAB PER SRM. 2 L 7 2 4F RT A16WE 2007070200173 20070702 00173 EU 2007 7 2 USAA070472 1 20070622 A 5315 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 181UW 1531 FLOORBEAM -Y254 AT FRAME 20 HAS CORROSION. INSTALLED NESTED ANGLE REPAIR & FILLER PER SRM 53-00-14, DEFECT SIZE: .75 I NCH. 2 L 7 2 4F RT A28NM 2007070200184 20070702 00184 NM 2007 7 2 HNAA0700121 1 20070619 A 3350 OL3071BPEGPL BULB DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS BURNED OUT A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 807EX 292 CABIN FLOOR - EMERGENCY LIGHT OUT ON FLOOR, AT SEAT 4DF. REMOVED BULB FROM ASSY AND INSTALLED NEW BULB INTO POSITION. 2 H 7 2 4T RT A13NM 2007070200185 20070702 00185 NM 2007 7 2 HNAA0700086 1 20070509 A 2420 DH103024600C INVERTER DHAV DHC8 DHC8102 2809003 NM UNKNOWN A HNAA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 804EX 227 SECONDARY INVERTER CAUTION LIGHT AND RIGHT 26VOLT CAUTION LIGHT ILLUMINATED ASSOCIATED WITH SMOKE IN COCKPIT. MEL INVER TERS. REPLACED SECONDARY INVERTER, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007070200192 20070702 00192 NM 2007 7 2 ABXA070186 1 20070623 A 2120 UNKNOWN BOEING 767 767281 1385109 NM CABIN ODOR A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 768AX 22786 SMELL OF SMOKE DETECTED ON FLIGHT DECK AND MAIN CARGO DECK WITH LEFT PACK ON. SHUT PACK OFF, SMELL CONTINUED. SMELL AP PEARED OF ELECTRICAL ORIGIN. INSPECTED LOWER E&E COMPARTMENT, UPPER AND LOWER CARGO COMPARTMENTS WITH PACKS ON AND OFF. INSPECTED BOXES AND ASSOCIATED WIRING AND CIRCUIT BREAKER PANEL. INSPECTED LEFT AND RIGHT PACK COMPONENTS. NO DEFECT S NOTED. RAN PACK FOR 1/2 HOUR WITH NO SMELL NOTICED. COULD NOT DUPLICATE. 2 L 7 2 4F RT A1NM 2007070200193 20070702 00193 SO 2007 7 2 C2XA07CL055 1 20070622 A 3350 UNKNOWN EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS UNKNOWN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14117 145674 EWR FLIGHT 2240, THE CREW REPORTED THE EMERGENCY LIGHTS NOT ARMED MESSAGE WAS ON THE EICAS. MAINTENANCE INSPECTED AND P ERFORMED ELECTRICAL RESET. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2007070200199 20070702 00199 SO 2007 7 2 RAIA00706030 1 20070618 A 3150 UNKNOWN EMB 145 EMB145LR 3260212 SO BRAKES UNKNOWN A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 817HK 145058 FLT NR 5558 - ATL - INBOARD BRAKE INOP MESSAGE ON EICAS DURING TAKEOFF ROLL. MAINTENANCE RESET POWER TO BRAKE SYSTEM AN D PERFORMED OPS CHECK. 2 L 7 2 4T RT T00011AT 2007070300002 20070703 00002 EA 2007 7 3 A6WA200740239 1 20070510 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 455AW 7848 FS 484.0 ANGLE AT LBL36 IS CRACKED APPROX 1.0. CORRECTIVE ACTION IN PROGRESS. (K) [07-17-07] MAINTENANCE REMOVED AND R EPLACED ANGLE IAW BOMBARDIER REO 601R-53-41-059. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300010 20070703 00010 EA 2007 7 3 A6WA200740246 1 20070513 A 5310 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 458AW 7861 PASSENGER DOOR AFT DRAG ANGLE IS CRACKED. (K) [07-17-07] MAINTENANCE REMOVED DAMAGED SECTION OF DRAG ANGLE AND INSTAL LED REPAIR PARTS IAW REO 601R-52-11-513 REV A. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300014 20070703 00014 EA 2007 7 3 A6WA200740250 1 20070514 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 458AW 7861 FS 280 FLOORBEAM CLIP AT OB SIDE OF LBL 9.0 IS CRACKED IN RADIUS APPROX .20 INCH LONG. (K) [07-17-07] MAINTENANCE REP LACED CLIP IAW BSC EO 601R-53-0057A. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300018 20070703 00018 EA 2007 7 3 A6WA200740254 1 20070515 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 458AW 7861 LT WING LOWER PLANK ACCESS HOLE NR 2 FOR PANEL 510AB HAS FRETTING/ CORROSION DAMAGE AT IB END, ALL ALONG FWD SIDE AND OB END, IN AND OUT OF CRITICAL AREA. S/D MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 2 PANEL 510AB IAW BOMBA RDER REO 601R-57-21-0303 REV A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300026 20070703 00026 SO 2007 7 3 RAIA0706037 1 20070624 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 829HK 145281 PRE FLT 7976 - STL - EMERGENCY LIGHT AT CENTER AISLE FLOOD LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BUL B. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007070300030 20070703 00030 NM 2007 7 3 UPS07450013 1 20070606 A 5313 65B044217 STRINGER SPLICE BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C FWD CARGO COMPT STR 40L AT BS 740 SPLICE CORROSION FOUND. REMOVED CORROSION BLEND OUT 0.025 X .375 X .625 INCH OUT OF SRM 53-10-01 FIG 1 LIMITS. FWD CARGO COMPT BS 740 AT LT STR 40 STRINGER SPLICE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007070300032 20070703 00032 EU 2007 7 3 07FDEA02296 1 20070627 A 7897 CONNECTOR AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D* NE THRUST REVERSER LOOSE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 449FE 217 715430 ON TAKEOFF REC'D NR 1 REVERSER UNLOCKED LIGHT AT 2 SEPARATE TIMES. ONCE DURING ENG OVERTEMP AND AFTER THROTTLE WAS REDU CED. ON TAKEOFF, ECAM NR 1 ENG OVERTEMP, FOLLOWED QRH A/C IN WORK. FOUND CONNECTOR DS307 LH REVERSER STOW CONNECTOR VER Y LOOSE. CLEANED CONNECTOR AND SECURED. A/C OK FOR SERVICE 2 L 7 2 4F 4 F RT A35EU E20EA 2007070300036 20070703 00036 NM 2007 7 3 07FDEA02298 1 20070627 A 3220 LANDING GEAR BOEING 727 7272S2F 1384O81 NM NOSE UNKNOWN A FDEA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 SO 25 201FE 22924 WHEN CONFIGURING FOR LANDING, NOSE GEAR STAYED UP. GO AROUND INITIATED AND NOSE GEAR EXTENDED BEFORE QRH STARTED. HYD PRESSURE NORMAL THROUGH-OUT. WHEN NOSE GEAR DID EXTEND, DOOR LIGHT CAME ON FOR ABOUT 20 SECS BEFORE GEAR CAME DOWN. INSP NLG, WHEEL WELL AND DOORS. NO DEFECTS NOTED. LUBRICATED NLG AND DOORS PER M/M 12-21-011-2. JACKED A/C NLG PER MM 0 7-11-000-2. PERFORMED NLG EXTENSION AND RETRACTION TEST PER MM 32-33-000-5. CYCLED GEAR HANDLE 5 T0 6 CYCLES EACH GEAR RETRACT TIME 7 SEC (MAX TIME IS 10 SEC). NOSE GEAR EXTEND TIME 10 SEC EACH CYCLE. 2 L 7 3 4F A3WE 2007070300040 20070703 00040 NM 2007 7 3 UPS07450021 1 20070531 A 5320 WEB BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C M/D HORIZONTAL SUPPORT WEB FOUND CRACKED JUST AT BS 820 STR 10L (CRACK LENGTH .5 INCH). M/DECK HORIZO NTAL SUPPORT WEB AT BS 820 STR 10L AREA REPAIRED AS PER SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 2007070300046 20070703 00046 NM 2007 7 3 SWAA073145 1 20070622 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 456WN 32463 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER BROKEN AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007070300053 20070703 00053 NM 2007 7 3 SWAA073121 1 20070622 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733, STR 21R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007070300074 20070703 00074 NM 2007 7 3 SWAA073130 1 20070622 A 5322 6546569 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 967, STR 8R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007070300091 20070703 00091 NM 2007 7 3 SWAA073131 1 20070622 A 5311 65C33509 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007070300099 20070703 00099 NM 2007 7 3 SWAA073124 1 20070622 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED MV1 CHECK, FOUND STRINGER 21R CORRODED AT BS 727D. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007070300100 20070703 00100 EA 2007 7 3 A6WA200740215 1 20070426 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 417AW 7610 RT FWD FLOOR SUPPORT ANGLE (PN 601R31148-79) BETWEEN FS 310.00 AND FS319.70 CORRODED ON AFT END. REMOVED AND REPLACED S UPPORT (PN 601R31148-79) IAW SRM 51-23-00, SRM 51-42-06 AND DRWG 601R31148. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300102 20070703 00102 EA 2007 7 3 A6WA200740216 1 20070427 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 349 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 417AW 7610 PAX DOOR ASSIST MOTOR BRACKET (PN 601R317743-7) CRACKED AT BOTTOM END APPROX. 12 INCHES LONG. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300103 20070703 00103 EA 2007 7 3 A6WA200740231 1 20070429 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 452AW 7835 PASSENGER DOOR AFT DRAG ANGLE CRACKED APPROX .5 INCHES LONG AT DOOR ASSIST CABLE PULLEY BRACKET. (K) [07-17-07] MAINT ENANCE CUT AWAY CRACKED ANGLE AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R52-11-513 REV A. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300104 20070703 00104 EA 2007 7 3 A6WA200740232 1 20070430 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 452AW 7835 LT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED .5 INCH LONG ON OB RADIUS. (K) [07-17-07] MAINTENANCE CUT AWAY DAMAGED AN GLE AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R53-61-117 REV C. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300106 20070703 00106 EA 2007 7 3 A6WA200740234 1 20070501 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 455AW 7848 RT FS 621.00 TO 625.00 OBLIQUE ANGLE HAS A 1.2500 INCH LONG CRACK IN AFT RADIUS. (K) [07-17-07] MAINTENANCE REMOVED C RACKED ANGLE AND INSTALL NEW ANGLE IAW CRJ200 SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300108 20070703 00108 NM 2007 7 3 UPS07450025 1 20070601 A 5313 STRINGER BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C FWD CARGO COMPT S40L STRINGER FOUND CORROSION AT STA 740. (CORROSION BLEND OUT 0.040 X .75 X 1 INCH OUT OF SRM 53-10-01 FIG 1 LIMITS). FWD CARGO COMPT BS 710 TO BS 740 STR 40L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1 . 2 L 7 4 4F A20WE 2007070300214 20070703 00214 EU 2007 7 3 TRAX200700884 1 20070621 A 3350 SIGN AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 632AS 338 AFT PAX DOOR LOWER EMERGENCY EXIT SIGN HAS BULBS BURNED OUT. 2 H 7 2 4T RT 2007070300218 20070703 00218 SO 2007 7 3 FDKA200703139 1 20070318 A 5270 SWITCH EMB 145 EMB145LR 3260212 SO CARGO DOOR LACK OF LUBE A FDKA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 847MJ 145517 FDM 6026 BNA-MCO (1611 PHX LCL). AIRCRAFT RETURNED TO THE FIELD FOR A CARGO DOOR OPEN EICAS INDICATION IN FLIGHT. MX L UBRICATED MICRO SWITCH AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2007070300227 20070703 00227 SO 2007 7 3 FDKA200704158 1 20070416 A 2150 A/C PACK EMB 145 EMB145LR 3260212 SO CABIN ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 855MJ 145614 FDM 6052 HSV-MCO. SMOKE SMELL COMING FROM PACK 1. MX TROUBLESHOT AND OPS CHECKED GOOD, NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2007070300246 20070703 00246 WP 2007 7 3 ABXA070199 1 20070524 A 5320 99236872 INTERCOSTAL DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 INTERCOSTAL AT 28 RIGHT WAS CRACKED AROUND BOLT HOLE AT FS 596. REPAIRED INTERCOSTAL IAW DC9 SSRM DWG K05159. 2 L 7 2 4F A6WE 2007070900001 20070709 00001 WP 2007 7 9 AALA20071104 1 20070614 A 2410 CSD DOUG DC9 DC982 3022082 WP RT ENGINE LOW PRESSURE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7541A 49995 DFW INFLIGHT T1436/14JUN - RIGHT ENGINE CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ILLUMINATED. RETURNED TO DFW AND LA NDED WITHOUT INCIDENT. REPLACED RIGHT CONSTANT SPEED DRIVE AND RIGHT GENERATOR. SYSTEM GROUND CHECKED NORMAL OPERATION . 2 L 7 2 4F A6WE 2007070900008 20070709 00008 WP 2007 7 9 AALA20071112 1 20070615 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 568AA 49349 LGA - EMERGENCY LIGHTS IN TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007070900026 20070709 00026 EU 2007 7 9 AALA20071085 1 20070611 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14077 612 JFK - EMERGENCY EXIT LIGHT AT RIGHT NUMBER ONE ENTRY DOOR INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT RIGHT NUMBER ON E ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007070900027 20070709 00027 EU 2007 7 9 AALA20071083 1 20070611 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14077 612 JFK - EMERGENCY EXIT LIGHT AT LEFT NUMBER FOUR ENTRY DOOR INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT LEFT NUMBER FOU R ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007070900030 20070709 00030 WP 2007 7 9 AALA20071090 1 20070612 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7536A 49990 JFK - EMERGENCY LIGHTS AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007070900034 20070709 00034 WP 2007 7 9 07FDEA02288 1 20070626 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 900 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 DENT IN FUSELAGE SKIN FWD OF R-1 DOOR SILL. REMOVED DENT, FABRICATED AND INSTALLED SKIN AND FILLER IAW DC/MD10 SRM 53- 20-00 VOL I FIG 6 SHT 4, 53-10-00 VOL II PAGE 75 AND 53-20-00 VOL I PAGE 23. 2 L 7 3 4F RT A22WE 2007070900045 20070709 00045 SO 2007 7 9 SIMA200717801 1 20070622 A 3260 8527018005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO RT MLG FAILED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 654AE 14608 145437 LOUD CLUNKING NOISE HEARD ON CLIMB-OUT, DIVERTED TO ABI. INSPECTED BOTH RIGHT MAIN LANDING GEAR UPLOCK PROXIMITY SWITCH ES HARNESS WITH NO DEFECTS NOTED. REMOVED AND REPLACED BOTH RIGHT MAIN LANDING GEAR UPLOCK PROXIMITY SWITCHES IAW EMB A MM 32-61-01. OPERATIONAL CHECK GOOD IAW AMM 32-63-05. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007070900052 20070709 00052 NM 2007 7 9 070130 1 20070625 A 2611 UNKNOWN DOUG MD80 MD83 3023681 NM UNKNOWN A WX0A O OTHER N FALSE WARNING CR CRUISE 1 WP 19 883GA 49710 AIRCRAFT 883GA, FLIGHT 762 DURING CRUISE FLIGHT THE CARGO SMOKE DETECTOR LOOP LIGHT ILLUMINATED. FLIGHT CREW FOLLOWING QRH PROCEDURES TESTED THE SYSTEM BY PRESSING AND HOLDING THE WARN/CAUTION LTS TEST SWITCH AND ALL CDSCP LIGHTS ILLUMINAT ED. RETESTING THE SYSTEM AND ALL CHECKS WERE NORMAL. THE MAINTENANCE CONTROL DEPARTMENT DISPATCHED ON CALL MAINTENANCE AND VISUALLY INSPECTED ALL DETECTORS, NO DAMAGE NOTED. PERFORMED SEVERAL BITE TESTS AND ALL CHECKS WHERE NORMAL. AIRC RAFT WAS RELEASED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007070900062 20070709 00062 EU 2007 7 9 COEA0713908 1 20070307 A 5330 S53671205200 PANEL AEROSP ATR42 ATR42300 8680920 EU FUSLEAGE DENTED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 908FX 30172 023 DENT FOUND ON LT FUSELAGE 1 INCH BELOW STRINGER 14 AND 5 INCHES FORWARD OF FRAME 35. REMOVED DAMAGE. FABRICATED DOUBLE R AND INSTALLED ON AIRCRAFT IAW ATR SRM. (M) 2 H 7 2 4T RT A53EU 2007070900063 20070709 00063 EU 2007 7 9 COEA0714908 1 20070307 A 5330 S53571401209 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE DENTED A COEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 13 908FX 023 DENT WITH TOOLING MARKS FOUND ON PREVIOUS TEMPORARY REPAIR ON RT FUSELAGE 1 INCH BELOW STRINGER 12 AND 5 INCHES AFT OF F RAME 23. DAMAGE REMOVED. FABRICATED DOUBLER AND INSTALLED ON AIRCRAFT IAW ATR42 SRM. (M) 2 H 7 2 4T RT A53EU 2007070900079 20070709 00079 EU 2007 7 9 COEA0707903 1 20070109 A 5314 S53574100204 KEELBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 903FX 179 FOUND EXFOLIATING CORROSION ON UNDERSIDE OF KEEL BEAM WEB PLATE BETWEEN FRAME 27 AND 27A. REMOVED FAIRING ATTACH BRACKE T FROM KEEL BEAM WEB PLATE AT FRAME 26BL0. REMOVED AND INSTALLED NEW FABRICATED WEB PLATE AND FAIRING ATTACH BRACKET AT FRAME 26 BL0 IAW ATR42 SRM. (M) 2 H 7 2 4T RT A53EU 2007070900090 20070709 00090 SO 2007 7 9 FDKA200705179 1 20070502 A 2720 UNKNOWN EMB 145 EMB145LR 3260212 SO RUDDER UNKNOWN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 FDM 6012 ATL-BGM. RUDDER SYSTEM 1 AND 2 INOP MESSAGE. MX RESET AND OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007070900091 20070709 00091 SO 2007 7 9 FDKA200705180 1 20070502 A 3250 UNKNOWN EMB 145 EMB145LR 3260212 SO NLG STEERING UNKNOWN A FDKA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 849MJ 145534 FDM FLT 6025 ATL TO MCO. ABORTED T/O AND RTG DUE TO NWS STEERING INOP MESSAGE. MX TROUBLESHOT AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007070900092 20070709 00092 NM 2007 7 9 MASA200700003 1 20070101 A 2750 UNKNOWN DHAV DHC8 DHC8202 2809007 NM TE FLAPS UNKNOWN A MASA O OTHER O OTHER AP APPROACH 1 SW 07 437YV 437 ASH 2905 PHX. CAPTAIN REPORTED FLAPS FAILED TO MOVE ON APPROACH INTO GJT FROM 15 DEGREES TO 35 DEGREES. MX INSPECTED S YSTEM AND PERFORMED NUMEROUS OPERATIONAL CHECKS AND COULD NOT DUPLICATE MALFUNCTION. 2 H 7 2 4T RT A13NM 2007070900093 20070709 00093 NM 2007 7 9 MASA200700034 1 20070116 A 2611 UNKNOWN DHAV DHC8 DHC8202 2809007 NM SMOKE WARNING UNKNOWN A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 456YV 456 ASH 7057 DEN. FALSE SMOKE WARNING IN THE LAV. MX INSPECTED THE SMOKE DETECTOR AND IT APPEARED TO BE WORKING NORMALLY. 2 H 7 2 4T RT A13NM 2007070900094 20070709 00094 NM 2007 7 9 MASA200700071 1 20070202 A 2611 PU90461S SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY MALFUNCTIONED A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 987HA 7159 425 ASH 2841 FLG. CREW REPORTED NUMEROUS FALSE SMOKE WARNING CALLS FROM THE LAV. MX REPLACED THE SMOKE DETECTOR. 2 H 7 2 4T RT A13NM 2007070900095 20070709 00095 NM 2007 7 9 MASA200700092 1 20070211 A 3350 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 434YV 434 ASH 7034 DEN. CREW RETURNED TO THE GATE DUE TO ONE EMERGENCY EXIT FLOOR PATCH LIGHT INOP. MX PLACED ON MEL. 2 H 7 2 4T RT A13NM 2007070900096 20070709 00096 2007 7 9 MASA200700129 2 20070228 A 7200 UNKNOWN DHAV DHC8 DHC8202 2809007 NM NR 2 ENGINE UNKNOWN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 456YV 456 ASH 7059 GJT. NR 2 ENGINE OUTBOARD NACELLE HAD BUBBLING PAINT & SMOKE COMING OUT OF THE VENTS. MX INSPECTED AND RAN EN G, NO LEAKS NOTED. 2 H 7 2 4T RT A13NM 2007070900097 20070709 00097 NM 2007 7 9 MASA200700134 1 20070304 A 2120 UNKNOWN DHAV DHC8 DHC8202 2809007 NM CABIN ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 449YV 449 ASH 2855 PHX. LOUD NOISE, SMOKE AND SMOKY SMELL. MX PERFORMED HIGH POWERED MAINT RUN. SYSTEM OP CHECK GOOD AND COULD NOT DUPLICATE THE DISCREPANCY. 2 H 7 2 4T RT A13NM 2007070900098 20070709 00098 NM 2007 7 9 MASA200700147 1 20070315 A 2697 CONNECTOR DHAV DHC8 DHC8202 2809007 NM SMOKE DETECTOR LOOSE A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 989HA 427 ASH 2763 CLD. REPORTED A FALSE CARGO SMOKE WARNING IN FLIGHT. MX RESECURED A LOOSE CONNECTOR ON THE SMOKE DETECTOR. 2 H 7 2 4T RT A13NM 2007070900099 20070709 00099 NM 2007 7 9 MASA200700195 1 20070407 A 5220 STRUCTURE DHAV DHC8 DHC8202 2809007 NM EMERGENCY EXIT DISLODGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 437YV 437 ASH 2745 PHX. TRIM UNDER GALLEY EMERGENCY EXIT DOOR FELL OFF. MX SECURED THE TRIM. 2 H 7 2 4T RT A13NM 2007070900100 20070709 00100 NM 2007 7 9 MASA200700204 1 20070414 A 5210 DOOR DHAV DHC8 DHC8202 2809007 NM MAIN PAX OUT OF RIG A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 437YV 437 ASH 2904 GJT. MAIN CABIN DOOR HARD TO OPEN FROM INSIDE AND OUTSIDE. MX RIGGED THE DOOR, OPS NORMAL. 2 H 7 2 4T RT A13NM 2007070900101 20070709 00101 NM 2007 7 9 MASA200700225 1 20070423 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DIRTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 987HA 425 ASH 2760 PHX. F/A JUMP SEAT DOES NOT AUTO RECLINE. MX CLEANED AND LUBED THE SEAT TRACKS, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007070900102 20070709 00102 NM 2007 7 9 MASA200700294 1 20070601 A 3397 SOCKET DHAV DHC8 DHC8202 2809007 NM BURNED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 987HA 425 ASH 2805 PHX. AIRCRAFT WAS ON GROUND, CREW SMELLED SOMETHING BURNING. MX REMOVED AND REPLACED SOCKET. 2 H 7 2 4T RT A13NM 2007070900103 20070709 00103 NM 2007 7 9 MASA200700303 1 20070604 A 2120 DUCT DHAV DHC8 DHC8202 2809007 NM CABIN AIR DIRTY A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 987HA 425 ASH 2858 FLG. UNCOMMANDED HEAT IN AUTO & MANUAL MODE OF THE AIR CONDITIONING PACK IN FLIGHT AND A POSSIBLE FIRE IN THE AFT EQUIPMENT BAY. MX INSPECTED AND FOUND IT TO BE DIRT. 2 H 7 2 4T RT A13NM 2007070900104 20070709 00104 NM 2007 7 9 CALA0700315 1 20070620 A 5315 6546811 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70352 23590 INSPECTION FOUND AFT ENTRY FLOORBEAM UPPER CHORD CORRODED IN NUMEROUS AREAS THE ENTIRE LENGTH, STA 986.5, LBL 40 TO RBL 40. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03851. 2 L 7 2 4F RT A16WE 2007070900105 20070709 00105 NM 2007 7 9 CALA0700316 1 20070621 A 5320 141A8513 INTERCOSTAL BOEING 737 737824 13844BZ NM BS 344-360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14214 28774 INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT STA 344-360, BL 0. THE INTERCOSTAL WAS REPAIRED IAW ECRA 5321-01484. 2 L 7 2 4F RT A16WE 2007070900106 20070709 00106 NM 2007 7 9 CALA0700317 1 20070624 A 5311 6520723U66 FRAME BOEING 737 7373T0 1384582 NM BS 480-500 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70352 23590 INSPECTION FOUND A .5 INCH CRACK IN FORWARD CARGO DOOR CUTOUT AFT FRAME AT LOWER PAD FITTING, STA 480-500, S16R TO S27R. A NEW FRAME WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007070900107 20070709 00107 NM 2007 7 9 CALA0700318 1 20070624 A 5330 65C33756 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70352 23590 INSPECTION FOUND A 2.2 INCH CRACK IN THE FUSELAGE SKIN AT THE AFT LOWER CORNER OF THE R-1 DOOR. REPAIRED IAW SRM 53-10- 01, REPAIR 2. 2 L 7 2 4F RT A16WE 2007070900108 20070709 00108 NM 2007 7 9 CALA0700319 1 20070625 A 5315 6545818 FLOORBEAM BOEING 737 737824 13844BZ NM BS 360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14214 28774 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 360, LBL 8. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01485. 2 L 7 2 4F RT A16WE 2007070900110 20070709 00110 EU 2007 7 9 BA07007 1 20070625 A 2120 DUCT AIRBUS 330 A330323 3930335 EU CABIN AIR OBSTRUCTED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 276AY 0375 FLIGHT 705, FRA-CLT: CREW REPORTED A STRONG ELECTRICAL BURNING ODOR IN THE AFT GALLEY AREA. FLIGHT DIVERTED TO SNN. M AINTENANCE REMOVED AN AFT GALLEY CEILING PANEL AND FOUND A CLOTH LODGED IN A VENTILATION DUCT. REMOVED THE CLOTH, RE-AS SEMBLED THE DUCT AND CEILING PANEL, AND RAN AFT GALLEY SYSTEMS AND AIR DISTRIBUTION SYSTEMS. NO SMOKE OR ODORS NOTED. A/C WAS RELEASED FOR SERVICE WITH NO FURTHER DIFFICULTIES. 2 L 7 2 4F RT A46NM 2007070900111 20070709 00111 NM 2007 7 9 KCSA071196 1 20070626 A 5310 STANCHION BOEING 747 747221F 1384868 NM BS 1920 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 AFT PIT SIDEWALL STANCHION CORRODED AT BS 1920, RBL 61. 2 L 7 4 4F A20WE 2007070900112 20070709 00112 EA 2007 7 9 TRAX200700867 1 20070618 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 886AS 7531 FS 280 I/B CLIP ON RBL 9 IS CRACKED. REMOVED CRACKED ANGLE. DUPLICATED ANGLE USING PERFORMED ANGLE P/N S6144-3. INSTA LLED SERVICEABLE ANGLE IAW CRJ SRM 51-42-21. NEW ANGLE INSTALLED AT FS 280 RBL 9. SUPPLEMENTAL - SDR CLOSED 06/26/07. 2 L 7 2 4F RT A21EA 2007070900113 20070709 00113 EA 2007 7 9 TRAX200700880 1 20070615 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 886AS 7531 PAX DOOR INTERNAL SKIN IS CRACKED AT AFT CORNER OF LOWER STEP. REMOVED LOWER PAX DOOR STEP SUPPORT ANGLE LOWER SECTION OF PAX DOOR AFT DRAG ANGLE TO GAIN ACCESS FOR MEASUREMENT OF DAMAGE AND REPAIR. DH752 MADE ALL DETAILS, DEBURRED ALL, T OUCH UP ALODINE, PRIME. INSTALLED ALL DETAILS EXCEPT PULLEY WHEEL BRACKET, 5 NUT PLATES AND 3 SOLID RIVETS IAW REO 601R -52-11-1264 WRR 586 6-21-07. INSTALLED PULLEY BRACKET, RIVETS & NUT PLATES IAW CRJ 200 SRM 51-42-06 & 51-42-15. COMPL IED WITH EC/TC REO 601R-52-11-1264. SUPPLEMENTAL - SDR CLOSED 06/26/07. 2 L 7 2 4F RT A21EA 2007071000015 20070710 00015 NM 2007 7 10 SWAA073193 1 20070626 A 5315 6545833 FLOORBEAM BOEING 737 7375H4 138449D NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 294, RBL 38. REPAIRED FLOORBEAM CHORD PER SRM. 2 L 7 2 4F RT A16WE 2007071000017 20070710 00017 NM 2007 7 10 SWAA073197 1 20070626 A 5311 6546539 FRAME BOEING 737 7375H4 138449D NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT RT BS 616, LOWER ATTACH FASTENERS WL 201. REPAIRED FRAME PE R SB. 2 L 7 2 4F RT A16WE 2007071000022 20070710 00022 NM 2007 7 10 SWAA073185 1 20070626 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071000026 20070710 00026 NM 2007 7 10 ASAA0741823 1 20070627 A 5330 6546881152 SKIN BOEING 737 7374Q8 138447Q NM BS 1032 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 DENT ON EMPENNAGE SKIN AT STA 1032 BETWEEN STRINGERS 25L AND 24L, 2.5 INCHES FROM LAP SEAM RIVET ROW. REPAIRED SKIN IAW ASA EA 5330 02216, CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F RT A16WE 2007071000027 20070710 00027 SO 2007 7 10 FDKA200705184 1 20070504 A 2750 FLAP SYSTEM EMB 145 EMB145LR 3260212 SO TE FLAPS OUT OF RIG A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 837MJ 145367 FLAP FAIL AT 45 DEGREES. MX RIGGED FLAPS. 2 L 7 2 4T RT T00011AT 2007071000029 20070710 00029 SO 2007 7 10 FDKA200705186 1 20070504 A 2720 SWITCH EMB 145 EMB145LR 3260212 SO RUDDER SYSTEM INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 RUDDER SYSTEM 1 AND 2 INOPERATIVE IN FLIGHT. MX REPLACED SWITCH RH3, IC 600 1, MICRO SWITCHES K0364, K0546, K0544, K054 5, K0347, K0363. 2 L 7 2 4T RT T00011AT 2007071000031 20070710 00031 SO 2007 7 10 FDKA200705188 1 20070505 A 2720 15793101 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO RUDDER SYSTEM INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 6493 145481 RUDDER SYSTEM 2 INOPERATIVE ON TAXI. MX REMOVED AND REPLACED RUDDER NR 1 AND NR 2 PRESSURE SWITCHES. 2 L 7 2 4T RT T00011AT 2007071000042 20070710 00042 2007 7 10 FDKA200705204 4 20070514 A 3100 7014300901 DISPLAY EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 836MJ 2021 145359 AIRCRAFT DIVERTED TO SAV DUE TO STRONG ELECTRICAL ODOR IN COCKPIT WITH ELECTRICAL PROBLEMS. MX REMOVED AND REPLACED F/O 'S MFD. 2 L 7 2 4T RT T00011AT 2007071000044 20070710 00044 SO 2007 7 10 FDKA200705206 1 20070515 A 2741 TRIM SYSTEM EMB 145 EMB145LR 3260212 SO STAB LACK OF LUBE A FDKA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SW 07 835MJ 145353 STAB BACKUP TRIM INOPERATIVE. MX LUBED AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007071000050 20070710 00050 SO 2007 7 10 FDKA200705214 1 20070519 A 3150 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 852MJ 145567 FDM 6078 ATL (1410 PHX LCL). RTG RUDDER HARD OVER PROTECTION FAIL. MX RESET FADEC'S AND PERFORMED RUNS, OPS CHECK GOOD . 2 L 7 2 4T RT T00011AT 2007071000059 20070710 00059 NM 2007 7 10 DHL2007783527 1 20070605 A 5720 WEB BOEING 727 727227 1384078 NM LT WING TIP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 LEFT WING TIP, VERTICAL WEB SHOWS MULTIPLE CRACKS BY FWD NAV LIGHT, WBL 640. CUT OUT DAMAGED AREA OF LEFT WING TIP, VER TICAL WEB AT NAV LIGHT AREA IAW B727 SRM 51-40-3, DIM 7.875 BY 3. FABRICATED AND INSTALLED REPAIR DOUBLER IAW B727 SRM 51-40-3, MATERIAL ID IAW B727 SRM 57-20-2, FIG 3. MATERIAL USED 7075T6, .050”, 10.5 BY 7 AND FILLER 7075T6, .040, 7.875 BY 3. ALL PARTS AND AREA TREATED, PRIMED IAW B727 SRM 51-10-2. 2 L 7 3 4F A3WE 2007071000081 20070710 00081 SO 2007 7 10 J4PA062807001 2 20070627 A 7421 RHB32S SPARK PLUG CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO HARTZL HCJ3Y PHCJ3YF1 GL ENGINE CRACKED E J4PA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 13 851CD 1450 1493 917741 FP3777B AT APPROXIMATELY 1600 LOCAL FLYING FROM KPDK TO KGSO AT CRUISE DEVELOPED AN ENGINE VIBRATION AND ROUGH RUNNING. DIVERTE D INTO KGMU WITH 1 PASSENGER, WITHOUT INCIDENT. AFTER GROUND CHECKS FOUND THAT A SPARK PLUG FIRING SIDE INSULATOR WAS C RACKED CAUSING THE MISS FIRE. 1 L 7 1 3O 3 O NT A00009CH E3SO 5 C P36EA 2007071000090 20070710 00090 SO 2007 7 10 FDKA200705231 1 20070507 A 5312 FIREWALL EMB 145 EMB145LR 3260212 SO APU BAY CRACKED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 850MJ 145568 APU FIREWALL HAS CRACK UNDER UPPER RIGHT MOUNT FLOOR. REPAIRED CRACK. 2 L 7 2 4T RT T00011AT 2007071000095 20070710 00095 SO 2007 7 10 FDKA200705234 1 20070508 A 5320 THRESHOLD EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 850MJ 145568 SERVICE DOOR THRESHOLD AREA IS CORRODED OUT OF LIMITS IN 3 AREAS. THE DAMAGE HAS BEEN REPAIRED. 2 L 7 2 4T RT T00011AT 2007071000133 20070710 00133 NM 2007 7 10 SWAA073209 1 20070627 A 5311 6545810 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 304, STR 16L. REPAIRED FRAME PER SB. 2 L 7 2 4F RT A16WE 2007071000152 20070710 00152 NM 2007 7 10 DLM88070800 1 20070619 A 5340 FITTING DOUG MD88 MD88 3023688 NM DOOR FRAME CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 CRACK ON AFT UPPER DOOR JAMB AT RT FWD OVERWING DOOR. CLIP REPLACED PER DWG 9957735 ON N/R T0058935 HMV/GDL. 2 L 7 2 4F RT A6WE 2007071000153 20070710 00153 NM 2007 7 10 DLM88070801 1 20070620 A 5320 FITTING DOUG MD88 MD88 3023688 NM DOOR FRAME CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 CRACKS ON FWD AND AFT DOOR JAMB CLIPS AT LF FWD OVERWING DOOR. REPLACED CLIPS PER DWG 9957735 ON N/R T0058929 HMV/GDL. 2 L 7 2 4F RT A6WE 2007071000154 20070710 00154 NM 2007 7 10 DLM88070802 1 20070620 A 5313 LONGERON DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 CRACK ON LONGERON 4 RH STA Y=522 AND Y=541. REPAIRED PER SRM 53-02 FIG 18 ON NR T0058606. 2 L 7 2 4F RT A6WE 2007071000155 20070710 00155 NM 2007 7 10 DLM88070803 1 20070620 A 5523 TAB DOUG MD88 MD88 3023688 NM RT ELEVATOR DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 DENT AND LIGHTNING STRIKE ON RT ELEVATOR ANTI-FLOAT TAB. REPAIRED PER DRD 55-04D PARA 2D FIG 1 ON N/R T0059182 HMV/GDL. 2 L 7 2 4F RT A6WE 2007071000156 20070710 00156 NM 2007 7 10 DLM88070804 1 20070620 A 5313 LONGERON DOUG MD88 MD88 3023688 NM BS 200 L8R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 CRACK ON LONGERON 8RH STA Y=200. REPAIRED PER SRM 53-02 FIG 18 ON NR T0058590. 2 L 7 2 4F RT A6WE 2007071000157 20070710 00157 NM 2007 7 10 DLM88070805 1 20070614 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 CRACKED RT CUSP WEB AT STA. Y=560. REPAIRED PER ERA 398191-14MA ON N/R T0059229 HMV/GDL. 2 L 7 2 4F RT A6WE 2007071000158 20070710 00158 NM 2007 7 10 DLM88070806 1 20070620 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 1200 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 CRACK ON RT CUSP WEB AT STA =1200. REPAIRED PER SRM 51-70-4 FIG 2. ON N/R T0058357 HMV/GDL. 2 L 7 2 4F RT A6WE 2007071000159 20070710 00159 NM 2007 7 10 SWAA073203 1 20070627 A 5310 6547959 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT BS 792, STR 24R. REPAIRED FRAME PER ACO. 2 L 7 2 4F RT A16WE 2007071000160 20070710 00160 NM 2007 7 10 DLM88070807 1 20070620 A 5313 LONGERON DOUG MD88 MD88 3023688 NM BS 1437 L16L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 CRACK ON LONGERON 16 LT STA 1437 IN AFT ACCESORY COMP. REPAIRED PER DRW S910228 ITEM 47 ON HR T0058497. 2 L 7 2 4F RT A6WE 2007071000161 20070710 00161 NM 2007 7 10 SWAA073223 1 20070627 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. R&R STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007062900050 20070629 00050 NM 2007 6 29 TSAA0732033 1 20070615 A 3233 ACTUATOR BOEING BOEING 737 737230 1384401 NM NLG MALFUNCTIONED A TSAA O OTHER O OTHER AP APPROACH 1 WP 13 821AL 23155 FLIGHT 90 HNL- KOA. ON APPROACH TO KOA WHEN THE CREW LOWED THE GEAR HANDLE, THE TWO MAIN GEAR SHOWED DOWN AND LOCKED BU T THE NOSE GEAR SHOWED UP AND CREW DIDN’T HEAR THE NLG EXTEND. AFTER APPROXIMATELY 20 SECONDS, THE NLG EXTENDED AND SHO WED DOWN AND LOCKED. CREW FLEW A LOW PASS TO HAVE ATC VISUALLY CHECK THAT ALL GEAR WERE DOWN. ATC REPORTED ALL GEAR DO WN AND CREW VERIFIED THE NLG WAS DOWN WHEN CHECKED THROUGH THE FLIGHT DECK VIEWING PORT. CREW LANDED WITHOUT FURTHER IN CIDENT. THE AIRCRAFT WAS THEN FERRIED TO HNL WITH THE GEAR DOWN AND LOCK PINS INSTALLED. AIRCRAFT COMPLETED FERRY FLIG HT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NLG MODULAR PACKAGE AND NLG TRANSFER CYLINDER. AIRCRAFT FAIL 2 L 7 2 4F RT A16WE 2007062900058 20070629 00058 EU 2007 6 29 COEA0717908 1 20070307 A 5414 S54310252200 PANEL AEROSP ATR42 ATR42300 8680920 EU LT NACELLE DAMAGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 908FX 30172 023 FRETTING DAMAGE ON LT NACELLE REBATE FLANGE COMMON TO PANEL 475AL. REBATE PANEL REMOVED. FABRICATED AND INSTALLED NEW REBATE PANEL IAW ATR42 SRM. (M) 2 H 7 2 4T RT A53EU 2007062900059 20070629 00059 NM 2007 6 29 QXEA200701004 1 20070618 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM BS 182 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - RIGHT LOWER FUSELAGE HAS A DENT WITH GOUGE AT STATION X182 BELOW STRINGER 27R. REPAIRED IAW SRM 51-20-00 AND R D8/4-53-1950. 2 H 7 2 4T RT A13NM 2007062900060 20070629 00060 NM 2007 6 29 QXEA200700999 1 20070614 A 5753 SKIN BOMBDR DHC8 DHC8402 1390042 NM LT TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 C4 PDX - LEFT INBOARD FLAP UPPER SURFACE IS CHAFED AT STATION YW 60.00. REPAIRED IAW SRM 57-51-30, AND RS8/4-57-817. 2 H 7 2 4T RT A13NM 2007062900066 20070629 00066 NM 2007 6 29 QXEA200701017 1 20070620 A 6120 30006000056 TSCU DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 358PH 17827 542 506 PDX FLIGHT NR 2170 AUTOFEATHER TEST 1 WILL NOT TEST, NO UPTRIM. REPLACED NR 1 ENGINE TSCU IAW P&W MM 72-01-10, PG 420-4 24, STEP 7. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007062900070 20070629 00070 NM 2007 6 29 UIEA200700254 1 20070621 A 5320 BAC1505100607 SUPPORT BOEING 747 7472D7B 1384803 NM BS 1112 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 LOWER FUSELAGE AIR CONDITIONING ACCESS DOOR AREA, BELOW KEEL BEAM BOX, EXTERIOR CENTER PANEL SUPPORT EXTRUSION HAS CORRO SION. PERMANENT REPAIR WAS ACCOMPLISHED AS PER 747-200 SRM 51-40-04, FIG 1. ALSO REFERENCE ATLAS AIR XEO NR 53-062007. 2 L 7 4 4F RT A20WE 2007062900083 20070629 00083 NM 2007 6 29 DL76G070739 1 20070615 A 2780 PSEU BOEING 767 767332 1382001 NM LE SLAT SYSTEM UNKNOWN A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 176DZ 29697 LE SLAT DISAGREE ILLUMINATED ON EICAS WHEN FLAPS POSITIONED TO 5. FAULT CODE 423 ON PSEU AND RVDT 603 ON FSEU. REPLACE D PSEU AS PRECAUTION. CLEANED/CHECK/TIGHTENED TERM BLOCK FOR FLAP HANDLE RVDTS RAN FLAPS, OPS OK. 2 L 7 2 4F RT A1NM 2007062900090 20070629 00090 NM 2007 6 29 DL757070752 1 20070619 A 2597 WIRE HARNESS BOEING 757 75726D 1384907 NM PWA 4060 PW4060 52119 NE FWD GALLEY OVEN SHORTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 900PC 28446 727738 FWD GALLEY OVEN SPARKED SMOKED AND POPPED CIRCUIT BREAKER. FOUND TWO WIRES SHORTED ON OVEN WIRING HARNESS, REPAIRED WI RES. OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E24NE 2007062900094 20070629 00094 NM 2007 6 29 DL738070756 1 20070620 A 5330 147A34005 SKIN BOEING 737 737832 13844CF NM FS 904 S23R GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 383DN 30346 AIRCRAFT STUCK BY GROUND EQUIP AT FS 904, S-23R LAP JOINT. SKIN CUT OUT, DOUBLER INSTALLED. UNDERLYING STRUCTURE REMOV ED AND REPLACED. 2 L 7 2 4F RT A16WE 2007062900099 20070629 00099 NM 2007 6 29 DL76G070763 1 20070620 A 2913 326879210 PUMP BOEING 767 767332 1382001 NM FUEL SYSTEM INOPERATIVE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 171DZ 29690 ADP LOW PRESSURE LIGHT WITH SWITCH IN -ON- POSITION. FOUND NO OIL IN ADP CHECKED CHIP DETECTOR AND SERVICED. ADP STILL INOP REPLACED ADP. 2 L 7 2 4F RT A1NM 2007062900101 20070629 00101 NM 2007 6 29 DL76S070766 1 20070621 A 5315 BAC1509100682 FLOORBEAM BOEING 767 767332 1382001 NM BS 1197 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 AFT CARGO FLOOR PANEL SUPPORT RIB AT STA 1197+110 RBL 24 AND RBL 40 BOLT HOLE CORRODED. REPAIRED PER 53-00-07 REPAIR 4 FIGURE 201 ON AJN 51009. 2 L 7 2 4F RT A1NM 2007062900102 20070629 00102 NM 2007 6 29 DL76S070769 1 20070621 A 5315 BAC1509100682 FLOORBEAM BOEING 767 767332 1382001 NM BS 1197 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 AFT CARGO COMPT FLOOR PNL SUPPORT RIB RBL 42 AT STA 1197+88 HOLE CUTOUT SIGN OF CORROSION. REPAIRED PER 53-00-07 FIG 20 1 REPAIR 6 ON AJN 51468. 2 L 7 2 4F RT A1NM 2007062900104 20070629 00104 NM 2007 6 29 DL76S070771 1 20070621 A 5315 BAC1509100682 FLOORBEAM BOEING 767 767332 1382001 NM BS 1197 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 AFT CARGO COMPARTMENT STA 1197 BELOW FLOOR FRAME UPPER CORD LBL 11 UPPER AND LOWER SURFACES CORRODED REPAIRED ON AJN5289 3 PER 53-00-07 FIRURE 2O1 REPAIR 4. 2 L 7 2 4F RT A1NM 2007070200002 20070702 00002 EA 2007 7 2 A6WA200740283 1 20070528 A 5330 6003301027 PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FS 169 DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 RT NOSE SKIN PANEL PN 600-33010-27 IS DENTED 5 INCH LONG X 4 INCHES WIDE X 0.125 INCHES DEEP FROM FS 169.00 TO FS 193.00 . S/D - MAINTENANCE REMOVED AND REPLACED SKIN PANEL P/N 600-33010-27, IAW CRJ 200 SRM 51-42-06 AND BSC EO 601R-53-11942 . (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070200010 20070702 00010 NM 2007 7 2 07FDEA02259 1 20070622 A 5240 DOOR FRAME BOEING 727 727233 138408A NM ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 HIDDEN DAMAGE INSPECTION LT AFT SERVICE DOOR 2ND FRAME, 4" FROM FWD EDGE, UPPER SURFACE OF LOWER FRAME SHEAR TIE IS CORR ODED. [07-26-07] BLENDED OUT DAMAGE, ORIGINAL MATERIAL IS .050", MATERIAL LOSS OF .001", REMANING MATERIAL IS .04 9", WITHIN LIMITS. TOOL USED IN17-0458 CAL DATE 4-24-08 REF SRM 52-00-2, TREATED AND PRIMED REF 51-10-2. 2 L 7 3 4F RT A3WE 2007070200011 20070702 00011 NM 2007 7 2 07FDEA02260 1 20070622 A 5240 DOOR FRAME BOEING 727 727233 138408A NM ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 HIDDEN DAMAGE INSP LT AFT SERVICE DOOR LOWER AFT STOP FITTING HAS CORROSION. [07-06-07] DRILLED UP NEW STOP FITTING PE R. SRM 51-30-5 PG 1, INSTALLED IT, PER SRM 51-10-1 PG. 10 AND 51-30-2 PG. 2-5. INSTALLED CORROSION INHIBITING COMPOUND TO THE LOWER PART OF DOOR PER OHM 52-036-21 PG. 404 AND INSTALLED COVER PANEL PER SRM 51-30-2 PG 2-5 2 L 7 3 4F RT A3WE 2007070200024 20070702 00024 NM 2007 7 2 DHL2007783520 1 20070602 A 5313 BAC14981467075 STRINGER BOEING 727 727227 1384078 NM BS 560 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 LIGHT CORROSION AT STA 560, STR 27R FWD SIDE, FWD BILGE AREA. REMOVED CORROSION IAW B727 SRM 51-10-6, MATERIAL THICKNES S .090, MATERIAL REMAINING .058, FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. CUT OUT DAMAGED SECTION OF STRINGER 27 R AT STA 560, 18 LONG IAW B727 SRM 53-10-3 FIG 1. FABRICATED REPAIR PARTS, MATERIAL USED BAC1498-146-7075T6, 18 LONG, 2 EACH SPLICES, MATERIAL USED BAC 1498-131-7075T6 7075T6, 11.5 LONG IAW B727 SRM 53-10-3 FIG 1. TREATED, PRIMED AND INST ALLED REPAIR PARTS IAW B727 SRM 51-10-2 AND 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2007070200041 20070702 00041 SO 2007 7 2 CHQA200700031 1 20070624 A 2750 7013348949 ACQUISITION UNIT EMB 135 EMB135KL 3260302 SO COCKPIT INOPERATIVE A CHQA K NONE J WARNING INDICATION TO TAKEOFF 1 GL 11 297SK 2921 2921 145522 FLIGHT 5349 - ORF-STL- AFTER TAKEOFF, "SPS ADV" EICAS MESSAGE AND FLAP INDICATOR WAS DASHED AMBER. VISUALLY VERIFIED FL APS WERE UP. RAN QRH, CONTINUED FLIGHT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED DAU NR 2. 2 L 7 2 4F RT T00011AT 2007070200054 20070702 00054 EU 2007 7 2 MALA070070 1 20070622 A 2120 UNKNOWN SAAB SF340 340B 7860101 EU CABIN/COCKPIT ODOR A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 442XJ 340B442 ELECTRICAL ODOR PRESENT IN CABIN AND FLT DECK WITH INTAKE SYSTEM ON. CREW SHUT OFF INTAKE HEAT SYS AND ODOR DIMINISHED. RIGHT INTAKE HEAT INOP. ELECTRICAL ODOR WHEN ENGINE AND ICE SELECTED ON ODOR NOTED ON COCKPIT AND CABIN NO CAUTION LI GHTS. DEFERRED RIGHT INTAKE HEAT ANTI-ICE SYSTEM PER MEL 30-20-1-1B AUTO IGNITION TEST GOOD PER CREW VERIFIED A SMALL B URN MARK ON LOWER INSIDE DUCT DAMAGE STILL INTAKE OF LOWER DUCT ENTERED INTO DMR MXC NOTIFIED 4488. REPLACED LOWER DUCT , FROM LOG SHEET 1665486. REMOVED AND REPLACED RIGHT LOWER INLET DUCT PN NH24668-169 SN OFF UNKNOWN, SN ON L290548 IAW SAAB JOB CARD NR 7160-301. OPS CHECK GOOD. REMOVED FROM DMR/MXC NOTIFIED (1376). 2 L 7 2 4T RT A52EU 2007070200059 20070702 00059 EU 2007 7 2 07FDEA02275 1 20070626 A 5100 NONE AIRBUS 300 A300B4605R 3930308 EU NONE NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 CONFLICT BETWEEN OLD REPAIR AT RT INBOARD FLAP LOWER SKIN AND EMBODIMENT OF SB A300-57-6100 REPAIR PERFORMED BY PATCH AN D SHIM REPAIR IAW SRM 57-50-00 FIG 206, APPROVED BY EA 6-5753-106461 AND RAS/FOK/109/2007 ISS A. 2 L 7 2 4F RT A35EU 2007070200074 20070702 00074 EA 2007 7 2 SIMA200717710 1 20070625 A 2780 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA SLATS UNKNOWN A SIMA O OTHER J WARNING INDICATION LD LANDING 1 SW 21 506AE 10056 SELECTED FLAPS AND RECEIVED SLATS FAIL CAUTION MESSAGE, NO FLAPS OR SLATS DEPLOYMENT. PERFORMED DETAILED VISUAL INSPECT ION OF SLAT SYSTEM WITH NO FINDINGS. CLEARED INHIBITS IAW CRJ AMM 45-45-00. PERFORMED OPERATIONAL CHECK OF FLAPS AND S LATS IAW CRJ AMM 27-50-00-710-801. PERFORMED SELF TEST OF SLAT FLAP ELECTRONIC UNIT IAW CRJ AMM 27-51-05. RETURNED AIR CRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007070200096 20070702 00096 NM 2007 7 2 2007UALA02123 1 20070620 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 290 S2L GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 FWD UPPER FUSELAGE CROWN AT STA 290 STR 2L SKIN IS GOUGED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007070200099 20070702 00099 EU 2007 7 2 2007UALA02126 1 20070620 A 2620 FIRE BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 NACELLE FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 496UA 1845 ENG 1 AGENT 1 DISCHARGE LIGHT ILLUMINATED AFTER 3 HRS OF FLIGHT. FOUND ENGINE FIRE BOTTLE FAILED. REPLACED ENGINE 1 FIRE BOTTLE. SYSTEM CHECK OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007070200114 20070702 00114 2007 7 2 2007UALA02143 4 20070619 A 2210 COMPUTER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE THRUST MANAGE NO TEST A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 662UA 27159 NO LAND THREE DISPLAYED NO MALFUNCTION NOTED. [07-20-07] MCDP CODE "SLAT SW-FCC L", ACP MM 22-00-03 & CAT III CHK PER MM 22-10-00, THRUST MANAGEMENT COMPUTER FAILED TEST. RPL TMC PER MM 22-31-01, OP CK GOOD. AC REMAINS IN CAT III STATUS . 2 L 7 2 4F 4 F RT A1NM E24NE 2007070200117 20070702 00117 NM 2007 7 2 2007UALA02147 1 20070620 A 2560 FLASHLIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FWD JUMPSEAT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 937UA 26668 FWD JUMPSEAT FLASHLIGHT DOES NOT BLINK. [07-13-07] BAD BATTERY, REPLACE FLASHLIGHT BATTERY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007070200121 20070702 00121 NM 2007 7 2 2007UALA02151 1 20070620 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 5E UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EEL INOP, SEAT 5E BOTH SECTIONS. RESECURED CONNECTOR ON EEL LAMPS, OPS CHECK GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2007070200134 20070702 00134 NM 2007 7 2 SWAA073114 1 20070621 A 5712 6545445 RIB BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND RIGHT WING RIB CRACKED AT STA 135.5, BETWEEN S2 AND S3. REPAIRED RIB PER ACO. 2 L 7 2 4F RT A16WE 2007070200140 20070702 00140 NM 2007 7 2 SWAA073112 1 20070621 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, STR 17R. REPAIRED FRAME PER EA. 2 L 7 2 4F RT A16WE 2007070200145 20070702 00145 NM 2007 7 2 SWAA073104 1 20070621 A 5311 6546554 FRAME BOEING 737 7373H4 1384600 NM BS 847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE STUB FRAME CORRODED AT BS 847, STR 13R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007070200153 20070702 00153 NM 2007 7 2 SWAA073109 1 20070621 A 5753 65C30462 SKIN BOEING 737 7375H4 138449D NM FORE FLAP DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND RIGHT WING INBOARD FORE FLAP LOWER SURFACE DISBONDED. REPAIRED FORE FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007070200154 20070702 00154 NM 2007 7 2 SWAA073098 1 20070621 A 5311 69353656 BELTFRAME BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 360, STR 14L. REPAIRED BELTFRAME PER SRM. 2 L 7 2 4F RT A16WE 2007070200156 20070702 00156 NM 2007 7 2 SWAA073091 1 20070621 A 3397 8100022605 CONNECTOR BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 443WN 29838 DURING SCHEDULED HC2 CHECK, FOUND EEPLS INOP BETWEEN ROW 1 ABC AND ROW 4 ABC. FOUND LOOSE CONNECTOR, SECURED CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2007070200157 20070702 00157 NM 2007 7 2 SWAA073115 1 20070621 A 5315 BAC15091000146 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 772 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 405WN 27893 DURING SCHEDULED 6Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, RBL 2. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007070200158 20070702 00158 2007 7 2 SWAA073083 4 20070621 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007070200161 20070702 00161 NM 2007 7 2 SWAA073087 1 20070621 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 412WN 29818 DURING SCHEDULED HC1 CHECK, RT AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007070200197 20070702 00197 SO 2007 7 2 RAIA00706028 1 20070618 A 3350 CONNECTOR EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHTS LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 827HK 145021 POST FLT NR 5588 - STL - EMERGENCY FLOOR PROXIMITY LIGHT AT LEFTHAND OVERWING EXIT IDENTIFIER AND RIGHTHAND OVERWING EXI T IDENTIFIER INOP. MAINTENANCE RESECURED CONNECTOR ON EMERGENCY LIGHTS CHECKS GOOD. 2 L 7 2 4F RT T00011AT 2007070300003 20070703 00003 EA 2007 7 3 A6WA200740240 1 20070510 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 455AW 7848 FS 484.0 ANGLE AT RBL 27 IS CRACKED APPROX 1.0 INCH. (K) [07-17-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW BOMBA RDIER SR 601R-53-0029B AND CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300009 20070703 00009 EA 2007 7 3 A6WA200740245 1 20070513 A 5320 601R75262159 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT MGL WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 458AW 7861 LT MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER HAT CHANNEL, PN 601R75262159, IS CRACKED AT OB LEGS LONGEST CRACK IS APPROX. .25 INCH LONG. (K) [07-17-07] MAINTENANCE REPLACED CHANNEL IAW CRJ SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300020 20070703 00020 EA 2007 7 3 A6WA200740256 1 20070515 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 458AW 7861 LT WING LOWER PLANK ACCESS HOLE NR 1 FOR PANEL 540BR HAS FRETTING/ CORROSION DAMAGE AREA ABOUT 2 INCHES LONG AT FWD/ OB QUADRANT, NO IN CRITICAL AREA. S/D MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 1 PANEL 540BB IAW BOMBARDIE R REO 601R-57-21-030 REV A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007070300025 20070703 00025 SO 2007 7 3 RAIA00706035 1 20070624 A 3350 LIGHT EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 808HK 145157 PRE FLT 7911 - RIC - EMERGENCY LIGHT ABOVE ROW 7 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB FOR SUBJECT LIG HT. 2 L 7 2 4F RT T00011AT 2007070300035 20070703 00035 NM 2007 7 3 UPS07450017 1 20070604 A 5320 65B08301555 ATTACH ANGLE BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C CABIN L1 DOOR CUTOUT FWD UPPER ATTACH ANGLE FOUND CRACKED APPROX AT BS 440 S16L (CRACK LENGTH .5 INCH) . CABIN L1 DOOR CUTOUT FWD UPPER CORNER ATTACH ANGLE AT BS 440 S16L REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007070300037 20070703 00037 NM 2007 7 3 UPS07450018 1 20070604 A 5320 65B0831556 ATTACH ANGLE BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C CABIN R1 DOOR CUTOUT FWD UPPER CORNER ATTACH ANGLE FOUND CRACK (CRACK LENGTH .375 INCH). CABIN R1 DOO R CUTOUT FWD UPPER CORNER ATTACH ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007070300038 20070703 00038 NM 2007 7 3 UPS07450019 1 20070604 A 5311 65B01714518 DOUBLER BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C CABIN BS 420 S14ER FRAME DOUBLER FOUND CRACKED. (CRACK LENGTH 6 INCHES) CABIN BS 420 STR 13AR TO STR 15R FRAME ATTACH DOUBLER AND BETWEEN STR 10AR TO STR 16R FRAME ATTACH INNER CHORD & INNER ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02. 2 L 7 4 4F A20WE 2007070300050 20070703 00050 NM 2007 7 3 SWAA073144 1 20070622 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007070300051 20070703 00051 NM 2007 7 3 SWAA073123 1 20070622 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 734D, STR 21R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007070300057 20070703 00057 NM 2007 7 3 SWAA073143 1 20070622 A 5753 6546435 SKIN BOEING 737 7375H4 138449D NM T/E FLAP DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP UPPER SKIN DISBONDED AT INBOARD END. REPAIRED FLAP P ER SRM. 2 L 7 2 4F RT A16WE 2007070300058 20070703 00058 NM 2007 7 3 SWAA073141 1 20070622 A 5311 6546534 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007070300060 20070703 00060 NM 2007 7 3 SWAA073133 1 20070622 A 5311 6546538 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007070300061 20070703 00061 NM 2007 7 3 SWAA073134 1 20070622 A 5311 6546548 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007070300081 20070703 00081 NM 2007 7 3 SWAA073129 1 20070622 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER S RM. 2 L 7 2 4F RT A16WE 2007070300109 20070703 00109 NM 2007 7 3 UPS07450026 1 20070529 A 5720 CHANNEL BOEING 747 747212B 1384886 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C LT WING NR 4 L/E PDU AFT SUPPORT CHANNEL FOUND CRACKED AT MOUNT BOLT AREA. (CRACK LENGTH .375 INCH). LT WING NR 4 L/E PDU AFT SUPPORT CHANNEL REPAIRED AS PER SRM 51-40-03 FIG 2. 2 L 7 4 4F A20WE 2007070300142 20070703 00142 EA 2007 7 3 SWIA200718392 1 20070620 A 2120 UNKNOWN CNDAIR CL600 CL6002D24 1390016 EA CABIN ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 802SK 15061 CREW REPORTS STRONG FUEL ODOR COMING FROM FORWARD AND AFT LAVS. PERFORMED CLEANING AND FLUSHING PROCEDURES ON FORWARD A ND AFT LAVS IAW MONOGRAM CMM 38-35-04. SNIFFER INDICATIONS ARE WITHIN LIMITS. 2 L 7 2 4F RT A21EA 2007070300143 20070703 00143 EA 2007 7 3 SWIA200718393 1 20070620 A 2120 UNKNOWN CNDAIR CL600 CL6002D24 1390016 EA LAVATORY ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 820SK 15108 AIRCRAFT GROUNDED FOR FUEL VAPOR ODOR IN LAV. FLUSHED LAV IAW MONOGRAM CMM 38-35-04. TESTED FOR FUEL VAPORS WITH SNIFF ER AND FOUND INDICATIONS TO BE WITHIN LIMITS. 2 L 7 2 4F RT A21EA 2007070300144 20070703 00144 EA 2007 7 3 SWIA200718394 1 20070620 A 2120 UNKNOWN CNDAIR CL600 CL6002D24 1390016 EA CABIN ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 807SK 15082 CREW REPORTS STRONG FUEL ODOR FROM FORWARD LAV. PERFORMED FLUSHING PROCEDURES IAW MONOGRAM CMM 38-35-04. SNIFFER INDIC ATIONS ARE WITHIN LIMITS. 2 L 7 2 4F RT A21EA 2007070300145 20070703 00145 WP 2007 7 3 AALA20071066 1 20070609 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9402W 53138 LGA - EMERGENCY LIGHT AT SEAT ROWS 28ABC AND 30ABC INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROWS 28ABC AND 30ABC. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007070300146 20070703 00146 EU 2007 7 3 AALA20071070 1 20070609 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 25071 514 MIA - EMERGENCY LIGHT AT SEAT 13C DAMAGED. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 13C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007070300147 20070703 00147 NM 2007 7 3 AALA20071079 1 20070611 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 914AN 29515 MIA - EMERGENCY LIGHT AT SEAT 8B INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 8B. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F RT A16WE 2007070300148 20070703 00148 WP 2007 7 3 AALA20071082 1 20070612 A 3213 PISTON DOUG DC9 DC982 3022082 WP STRUT INOPERATIVE A AALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 21 443AA 49469 STL INFLIGHT T1642/12JUN - NOSE WHEEL VIBRATION AFTER ROTATION. BEFORE DURING AND AFTER RETRACTION VIBRATION EXTREME. RETURNED TO STL AND LANDED WITHOUT INCIDENT. REPLACED LOWER STRUT PISTON ASSEMBLY AND LEFT STEERING CYLINDER AND LEFT AND RIGHT NOSE TIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007070300149 20070703 00149 NM 2007 7 3 AALA20071080 1 20070611 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 914AN 29515 MIA - EMERGENCY LIGHT AT SEAT 8B HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 8B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007070300150 20070703 00150 NM 2007 7 3 AALA20071081 1 20070611 A 3350 COVER BOEING 737 737823 13844BZ NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 914AN 29515 MIA - EMERGENCY WINDOW LIGHT AT AFT CABIN MISSING COVER. REPLACED EMERGENCY WINDOW LIGHT COVER AT AFT CABIN. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007070300151 20070703 00151 WP 2007 7 3 AALA20071076 1 20070611 A 4990 OIL TANK DOUG DC9 DC983 3022083 WP APU LEAKING A AALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 962TW 53612 YYZ INFLIGHT T1311/11JUN - CREW REPORTED ODOR AND HAZE IN CABIN DURING ROTATION. RETURNED TO YYZ AND LANDED WITHOUT IN CIDENT. FOUND OIL DRIPPING FROM APU INLET AND OIL TANK OVER SERVICED. ACCOMPLISHED WORK CARD 21 96 01 FOR CABIN ODOR A ND PACK BURN WORKCARD 21 92 12. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007070300152 20070703 00152 NM 2007 7 3 AALA20071073 1 20070610 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 666A 25300 MIA - EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007070300153 20070703 00153 NM 2007 7 3 AALA20071075 1 20070610 A 3350 767 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 372AA 25199 LAX - EXTERIOR EMERGENCY EXIT LIGHT AT RIGHT NUMBER ONE INOPERATIVE. RELAMPED EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007070300154 20070703 00154 EU 2007 7 3 AALA20071074 1 20070610 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 34078 615 MIA - EMERGENCY LIGHT AT SEAT 2G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 2G. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F RT A35EU 2007070300155 20070703 00155 NM 2007 7 3 AALA20071077 1 20070611 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 902AN 29504 MIA - EMERGENCY EXIT LIGHT ASSEMBLY AT RIGHT NUMBER TWO DOOR AFT BULKHEAD MISSING. REPLACED EMERGENCY LIGHT ASSEMBLY AT RIGHT NUMBER TWO DOOR AFT BULKHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007070300156 20070703 00156 EU 2007 7 3 AALA20071069 1 20070609 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 25071 514 MIA - EMERGENCY LIGHT AT SEAT 11C DAMAGED. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 11C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007070300157 20070703 00157 2007 7 3 AALA20071067 4 20070609 A 2565 LANYARD DOUG DC9 DC983 3022083 WP R1 DOOR SLIDE FRAYED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9402W 53138 LGA - RIGHT NUMBER ONE DOOR SLIDE LANYARD CABLE FRAYED. REPLACED RIGHT NUMBER ONE DOOR SLIDE LANYARD. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007070300158 20070703 00158 NM 2007 7 3 AALA20071072 1 20070610 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 JFK - EMERGENCY CEILING LIGHT AT SEAT 26C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT T00001SE 2007070300159 20070703 00159 WP 2007 7 3 AALA20071058 1 20070608 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 470AA 49600 LGA - EMERGENCY FLASHLIGHT AT AFT SERVICE DOOR HAS BROKEN STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007070300160 20070703 00160 WP 2007 7 3 AALA20071059 1 20070608 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 470AA 49600 LGA - EMERGENCY LIGHT AT SEAT 22D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007070300161 20070703 00161 WP 2007 7 3 AALA20071061 1 20070608 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 470AA 49600 LGA - EMERGENCY EXIT LIGHTS AT AFT STAIRWELL INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS AT AFT STAIRW ELL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007070300162 20070703 00162 WP 2007 7 3 AALA20071060 1 20070608 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 470AA 49600 LGA - EMERGENCY LIGHT AT SEAT 22D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F A6WE 2007070300163 20070703 00163 NM 2007 7 3 AALA20071062 1 20070609 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 JFK - EMERGENCY LIGHT AT SEAT 26C MISSING BULB. REPLACED BULB FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007070300164 20070703 00164 NM 2007 7 3 AALA20071063 1 20070609 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 JFK - EMERGENCY LIGHT AT SEAT 26C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007070300165 20070703 00165 NM 2007 7 3 AALA20071064 1 20070609 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 JFK - EMERGENCY LIGHT AT SEAT 40C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 40C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007070300166 20070703 00166 NM 2007 7 3 AALA20071065 1 20070609 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 JFK - EMERGENCY LIGHT AT SEAT 40C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 40C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007070300167 20070703 00167 NE 2007 7 3 AALA20071068 2 20070609 A 7261 565016 STRAINER DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LEFT ENGINE CLOGGED A AALA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 SW 21 972TW 53622 717386 ATL INFLIGHT T2441/09JUN - UPON DESCENT NUMBER ONE ENGINE OIL STRAINER CLOGGED LIGHT ILLUMINATED. SHUT DOWN NUMBER ONE ENGINE. LANDED ATL WITHOUT INCIDENT AND TAXIED TO GATE UNDER OWN POWER. FOUND CARBON IN FILTER AT SECOND FILTER CHANG E. REPLACED LEFT HAND OIL TANK AND CLEARED OIL LINES AT GEAR BOX BANJO FITTINGS AND RESTRICTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A6WE E9NE 2007070300168 20070703 00168 EU 2007 7 3 AALA20071071 1 20070609 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 25071 514 MIA - EMERGENCY LIGHT AT SEAT 34C DAMAGED. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 34C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007070300169 20070703 00169 NM 2007 7 3 AALA20071078 1 20070611 A 3230 VALVE BOEING 767 767323 1385205 NM RT MLG OUT OF RIG A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 385AM 27059 MIA INFLIGHT T69/11JUN - RIGHT MAIN GEAR UNSAFE INDICATION ON APPROACH. PERFORMED GEAR CHECKLIST AND RECEIVED THREE GR EEN GEAR INDICATIONS. LANDED MIA WITHOUT INCIDENT. AIRCRAFT OUT OF SERVICE FOR EVALUATION. FOUND RIGHT GEAR OPERATED SEQUENCE VALVE OUT OF RIG. ADJUSTED RIGHT GEAR OPERATED SEQUENCE VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007070300170 20070703 00170 NM 2007 7 3 NWAA072245646 1 20070521 A 5414 SKIN PANEL BOEING 757 757256 1384925 NM RT PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 546US 33392 DURING "M" CHECK FOUND CRACK IN NR 2 PYLON RT SKIN PANEL ASSEMBLY HOLE CUTOUT NEAR NAC STA 132. REPAIRED PER EA 56-1941 74. 2 L 7 2 4F RT A2NM 2007070300171 20070703 00171 EU 2007 7 3 TRBA2007038 1 20070626 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHT FAULTED A TRBA O OTHER O OTHER NR NOT REPORTED 1 SO 29 529AM 529 PAX DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED AFT BATTERY PACK IAW JIC NR 33-51-21. OP CK OK. 2 H 7 2 4T RT A53EU 2007070300172 20070703 00172 NM 2007 7 3 QXEA200701031 1 20070622 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - CABIN UNDER FLOOR CENTER AT FRAME X488.5 AND STRINGER 31L-32L HAS CORROSION ON THE FRAME CASTELLATION AT THE OU TBOARD EDGE. REPAIRED IAW SRM 51-20-11, 51-20-16. 2 H 7 2 4T RT A13NM 2007070300173 20070703 00173 NM 2007 7 3 QXEA200701032 1 20070622 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - CABIN UNDER FLOOR CENTER AT FRAME X488.5 AND STRINGER 31L, THE VERTICAL SEAT RAIL SUPPORT CHANNEL HAS CORROSION ON THE FORWARD SIDE BETWEEN FRAME AND SUPPORT. REPAIRED IAW SRM 51-20-11, 51-20-16. 2 H 7 2 4T RT A13NM 2007070300174 20070703 00174 NM 2007 7 3 QXEA200701029 1 20070622 A 5340 STRINGER CLIP DHAV DHC8 DHC8202 2809007 NM FUSLEAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - CABIN UNDER FLOOR CENTER AT FRAME X488.5 AND STRINGER 32L HAS CORROSION ON THE STRINGER ATTACH CLIP SPLICE. RE PAIRED IAW SRM 51-20-11, 51-20-16. 2 H 7 2 4T RT A13NM 2007070300175 20070703 00175 NM 2007 7 3 QXEA200701030 1 20070622 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - CABIN UNDER FLOOR CENTER AT FRAME X488.5 AND STRINGER 32L - 33 HAS CORROSION ON THE FRAME CASTELLATION. REPAIR ED IAW SRM 51-20-11, 51-20-16. 2 H 7 2 4T RT A13NM 2007070300176 20070703 00176 NM 2007 7 3 NWAA2256302 1 20070621 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK TEST FOUND UPPER DECK RT EMERGENCY DOOR POWER SUPPLY AND BATTERY PACK INOPERATIVE. MNL MAINTENANCE RE MOVED AND REPLACED POWER SUPPLY AND BATTERY PACK PER AMM 33-51-04. SECURED AND FUNCTIONAL TEST OK. 2 L 7 4 4F RT A20WE 2007070300177 20070703 00177 SO 2007 7 3 LR7A07055 1 20070615 A 5330 SKIN LKHEED 382 382G 526414U SO FS 807 DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 358 4606 DURING SCHEDULED A CHECK PER JOB CARD HA1200, FOUND RT AFT FUSELAGE SKIN DENTED AT FS 807, WL144, RBL63. REPAIRED SKIN IAW SMP583 51-140 AND LAC MEA 382-53-07-045. 2 H 7 4 4T A1SO 2007070300178 20070703 00178 SO 2007 7 3 LR7A07056 1 20070615 A 5330 SKIN LKHEED 382 382G 526414U SO FS 813, WL145 DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 358 4606 DURING SCHEDULED A CHECK PER JOB CARD HA1200, FOUND RT AFT FUSELAGE SKIN DENTED AT FS 813, WL145, RBL63. REPAIRED SKIN IAW SMP583 51-140 AND LAC MEA 382-53-07-047. 2 H 7 4 4T A1SO 2007070300179 20070703 00179 NM 2007 7 3 QXEA200701036 1 20070623 A 5100 NONE BOMBDR DHC8 DHC8402 1390042 NM NONE NONE A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 405QX 4047 SEA FLIGHT NR 2259: PSU PANEL OVERHEAD ROW 7 OPENED UP DURING TAXI OUT. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE RESECU RED PSU OVERHEAD PANEL AT ROW 7. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007070300207 20070703 00207 WP 2007 7 3 UPS07850031 1 20070623 A 3350 LIGHT DOUG DC8 DC873F 302199F WP COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. EMERGENCY LIGHTING OPS NORMAL IN REF TO AMM 33-50-00. 2 L 7 4 4F RT 4A25 2007070300215 20070703 00215 SO 2007 7 3 FDKA200703131 1 20070324 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 829MJ 145228 FDM 6085 MCO-NAS. SMELL OF SMOKE IN COCKPIT. MX INSPECTED SYSTEMS WITH NO DEFECTS FOUND. 2 L 7 2 4T RT T00011AT 2007070300221 20070703 00221 SO 2007 7 3 FDKA200703146 1 20070321 A 5320 14522461011 WEB EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 848MJ 145530 WEB AT FRAME 22, Y=479R IS CORRODED OUT OF LIMITS. WEB WAS REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2007070300231 20070703 00231 SO 2007 7 3 FDKA200704165 1 20070401 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 848MJ 145530 SERVICE DOOR IS CORRODED OUT OF LIMITS AT FRAME 19 & 20. INSTALLED REPAIRS. 2 L 7 2 4T RT T00011AT 2007070300239 20070703 00239 WP 2007 7 3 ABXA070202 1 20070612 A 5347 S2914913 SEAT TRACK DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 FLOOR TRACK CRACKED AND CORRODED AT STA 389, LEFT BUTT LINE 44. REPAIRED TRACK IAW DC9 SRM. 2 L 7 2 4F A6WE 2007070300242 20070703 00242 WP 2007 7 3 ABXA070196 1 20070522 A 5711 3913527513 SUPPORT BRACKET DOUG DC9 DC932F 3022067 WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 LEFT WING AFT SPAR HAD CRACKED VERTICAL SUPPORT BRACKET NEAR INBOARD SPOILER ACTUATOR. REPLACED BRACKET IAW DC9 SRM. 2 L 7 2 4F A6WE 2007070900011 20070709 00011 NM 2007 7 9 AALA20071114 1 20070616 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 383AN 26995 MIA - EMERGENCY EXIT LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007070900013 20070709 00013 NM 2007 7 9 AALA20071113 1 20070615 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 939AN 30883 MIA - EMERGENCY EXIT LIGHT AT SEAT 9D INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A16WE 2007070900020 20070709 00020 NM 2007 7 9 AALA20071120 1 20070617 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 670AA 25335 BOS - EMERGENCY EXIT LIGHT AT SEAT ROWS 9 TO 16 INOPERATIVE. REPLACED BATTERY PACK AT STATION 692 FOR EMERGENCY EXIT LI GHT AT SEAT ROWS 9 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007070900021 20070709 00021 WP 2007 7 9 AALA20071087 1 20070612 A 3200 DEFLECTOR DOUG DC9 DC983 3022083 WP NOSE GEAR LOOSE A AALA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 SW 21 9405T 53141 SEA INFLIGHT T820/12JUN - DURING CLIMB NOSE GEAR RED LIGHT REMAINED ON WITH NOISE AND BUFFETING. RETURNED TO SEA AND L ANDED WITHOUT INCIDENT. FOUND LEFT NOSE GEAR DEFLECTOR LOOSE AND MISSING AFT BOLTS. REPLACED NOSE DEFLECTOR. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007070900022 20070709 00022 NM 2007 7 9 AALA2071108 1 20070615 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 773AN 29583 JFK - EMERGENCY EXIT LIGHT AT SEAT ROW 3C MISSING LENS. REPLACED LENS FOR EMERGENCY EXIT LIGHT AT SEAT ROW 3C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007070900033 20070709 00033 WP 2007 7 9 07FDEA02287 1 20070626 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CLG WHEEL WELL CAVITY CORROSION ON FUSELAGE CIRCUMFERENTIAL ANGLE AT STA.1521, BETWEEN LONGERON 52 AND 51R. [07-13-07 ] REMOVED INTERCOSTAL AT LONG 51R, FS 1501-1521 IAW SRM 51-33-01 VOL2 PG1. REMOVED CORROSION ON TEE CHORD FS 1521 FRO M LONG 51R-52R IAW SRM 51-21-01 PG1 VOL2 AND DAC DWG AEA0018. ORIGINAL THICKNESS 0.200", MATERIAL LOSS 0.032" REMAINING THICKNESS 0.168", FOUND TO BE WITHIN LIMITS IAW FEDEX EA 8-5310-112948 (FUSELAGE - STA 1521 BULKHEAD TEE CAP REPAIR). I NSTALLED INTERCESTAL ON L51R FS 1501-1521 IAW SRM 51-33-01 VOL2 PG 1 & 51-35-01 VOL2. 2 L 7 3 4F RT A22WE 2007070900043 20070709 00043 EU 2007 7 9 07FDEA02300 1 20070627 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 652FE 735 MAIN CARGO DECK, RT, SEAT TRACK AT -Y953, BETWEEN FR 55 (BS 3566) AND FR 57.2 (BS 3778) IS CORRODED. REMOVED AND REPLA CED CORRODED SEAT TRACK SECTION, FR 54.2 TO FR 58, IAW A300-600 SRM 53-10-16 FIG 201. NEW SEAT TRACK SECTION LOCATED AN D DRILLED IAW A300-600 SRM 53-10-16 FIG 201. ALODINED IAW A300-600 SRM 51-21-10, PRIMED AND PAINTED IAW A300-600 SRM 51 -23-10. 2 L 7 2 4F RT A35EU 2007070900048 20070709 00048 EA 2007 7 9 SIMA200717902 1 20070627 A 3350 YAD4F RELAY CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS FAILED A SIMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 514AE 9417 10119 EMERGENCY LIGHTS STATUS MESSAGE CYCLING ON AND OFF WITH LIGHTS FOLLOWING. REMOVED AND REPLACED RELAY K135 ON PCB NR 5 O F JB11 IAW CRJ AMM 24-06-11. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2007070900049 20070709 00049 EA 2007 7 9 SIMA200715002 1 20070527 A 5610 NP1393226 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SIMA O OTHER O OTHER LD LANDING 1 SW 21 517AE 9098 10124 "SUP" CO-PILOT SIDE WINDOW CRACKED. REMOVED AND REPLACED CO-PILOT SIDE WINDOW IAW CRJ AMM. PRESSURE CHECKED WITH NO DE FECTS NOTED. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007070900056 20070709 00056 NM 2007 7 9 TSAA0732038 1 20070624 A 3260 65C161772 TARGET BOEING 737 7372X6C 1384552 NM MLG LOOSE A TSAA O OTHER N FALSE WARNING AP APPROACH 1 WP 13 746AS 23123 NON-ETOPS FLIGHT 93 HNL-OGG, WHEN CREW SELECTED THE LANDING GEAR TO THE DOWN POSITION, THE LEFT MAIN GEAR DID NOT SHOW D OWN AND LOCKED. CREW EXECUTED A LOW PASS SO THAT ATC COULD OBSERVE THE CONDITION OF THE LANDING GEAR. INDICATION SHOWE D DOWN AND LOCKED BEFORE LANDING. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT MAIN LANDING GEAR P RIMARY TARGET LOOSE AND ADJUSTED PER AMM 32-61-31. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007070900071 20070709 00071 EU 2007 7 9 COEA0701908 1 20070307 A 5510 S53372400200 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSLEAGE GOUGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 908FX 023 GOUGE LOCATED ON THE INBOARD AFT RADIUS OF FR 13 LOCATED 3 INCHES UP FROM FLOOR. DAMAGE BLENDED OUT AND REINFORCING DOU BLER INSTALLED PER DO/TS-2986-06-7405 REPAIR INSTRUCTIONS. REF SRAS DO/TS-2986/06..3782. (M) 2 H 7 2 4T RT A53EU 2007070900072 20070709 00072 EU 2007 7 9 COEA07002908 1 20070307 A 5311 S53572601200 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE DAMAGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 908FX 023 TOOLING DAMAGE TO UPPER FUSELAGE FRAME 25 AFT FLANGE BETWEEN STRINGER 4-5 LT. DAMAGE BLENDED OUT PER SRAS DO/TS-3859/06 -7653 REPAIR INSTRUCTIONS. REF SRAS DO/TS-3859/06...3772 ISSUE B FOR REPETITIVE INSPECTION. (M) 2 H 7 2 4T RT A53EU 2007070900075 20070709 00075 EU 2007 7 9 COEA0705908 1 20070307 A 5420 S54310252201 FLANGE AEROSP ATR42 ATR42300 8680920 EU LT ENG NACELLE DAMAGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 908FX 023 FRETTING DAMAGE FOUND ON LEFT NACELLE REBATE FLANGE COMMON TO PANEL 476AR. REMOVED REBATE PANEL. FABRICATED AND INSTAL LED NEW REBATEPANEL IAW ATR SRM. (M) 2 H 7 2 4T RT A53EU 2007070900114 20070709 00114 NE 2007 7 9 ABXA070204 2 20070624 A 7200 JT8D11 ENGINE DOUG DC9 DC941 302207N WP PWA JT8 JT8D11 52044 NE NR 1 FAILED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 3925 47494 676177 NR 1 ENGINE, 1ST STAGE TURBINE HAD SEVERAL BLADES WITH CRACKED LEADING EDGE TIPS. ALSO SEVERAL BLADES HAD MOLTEN METAL ON TIPS. OUT OF SERVICABLE LIMITS IAW JT8D MM 72-50-00-210-002. REMOVED AND REPLACED NR 1 ENGINE IAW DC9 MM ON JOB CAR D 9090010. 2 L 7 2 4F 4 F A6WE E2EA 2007070900153 20070709 00153 NM 2007 7 9 SWAA073172 1 20070625 A 5315 65465682 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS BS 1016, RBL 40 TO LBL 40. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007070900154 20070709 00154 NM 2007 7 9 SWAA073166 1 20070625 A 5754 STRUCTURE BOEING 737 7373H4 1384600 NM NR 1 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED 10Y CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007070900155 20070709 00155 NM 2007 7 9 SWAA073176 1 20070625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 312 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 312, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007070900156 20070709 00156 NM 2007 7 9 SWAA073177 1 20070625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 328 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 2007070900157 20070709 00157 NM 2007 7 9 SWAA073178 1 20070625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 336 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 336, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 2007070900158 20070709 00158 NM 2007 7 9 SWAA073179 1 20070625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 344 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007070900159 20070709 00159 NM 2007 7 9 SWAA073160 1 20070624 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM BS 747 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED MV2 CHECK, FOUND STRINGER 18L CRACKED AT BS 747. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007070900160 20070709 00160 NM 2007 7 9 SWAA073175 1 20070625 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 360 S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 7L CRACKED AT BS 360. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007070900161 20070709 00161 NM 2007 7 9 SWAA073182 1 20070625 A 5315 BAC15091000146 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 772 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 406WN 27894 DURING SCHEDULED 6Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, RBL 3. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007070900162 20070709 00162 NM 2007 7 9 SWAA073151 1 20070623 A 3350 D71701100SWA BATTERY BOEING 737 737705 13844SC NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 270WN 29089 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY PER MM. 2 L 7 2 4F RT A16WE 2007071000004 20070710 00004 SO 2007 7 10 FDKA200706285 1 20070617 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 EMERGENCY FLOOR LIGHT STRIP AT ROW 12 THRU 18 INOP. MX REPOSITIONED AND SECURED THE FLOOR STRIPS AND OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007071000010 20070710 00010 NM 2007 7 10 SWAA073183 1 20070626 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 BULLNOSE EMERGENCY EXIT LIGHT LENS FELL OFF AT ROW 3 DEF. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007071000023 20070710 00023 2007 7 10 SWAA073187 4 20070626 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMRGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071000032 20070710 00032 NM 2007 7 10 FDKA200705189 1 20070506 A 3010 Q50E RELAY DHAV DHC8 DHC8101 2809002 NM PITOT HEAT INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 808LR 073 PITOT HEAT NR 1 LIGHT ILLUM AND BURNING ODOR IN THE FLIGHT DECK. MX REMOVED AND REPLACED RELAY CURRENT SENSOR. 2 H 7 2 4T RT A13NM 2007071000041 20070710 00041 SO 2007 7 10 FDKA200705201 1 20070511 A 2710 UNKNOWN EMB 145 EMB145LR 3260212 SO AILERONS UNKNOWN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 835MJ 145353 AILERON SYSTEM 1 DOES NOT SHUT OFF DURING FLIGHT CONTROL TEST. MX RESET AIRCRAFT POWER OPS GOOD. 2 L 7 2 4T RT T00011AT 2007071000055 20070710 00055 SO 2007 7 10 FDKA200705219 1 20070521 A 2720 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO RUDDER MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 852MJ 145567 FDM 6154 BMI-ATL (0942 PHX LCL). RUDDER HARDOVER PROTECTION MSG. MX RESET SYSTEM, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007071000075 20070710 00075 NM 2007 7 10 07FDEA02306 1 20070628 A 5322 65133381 SHEAR TIE BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT PIT SHEAR TIE CORRODED STA 950D BETWEEN STR 28-29L CUT OUT DAMAGE AREA OF SHEAR TIE AT STA 950D, BETWEEN STRINGER 28 -29 L IAW BOEING SRM 53-10-4, REPAIR 3. FABRICATED REPAIR BRACKET AND FILLER IAW BOEING SRM 53-10-4. REPAIR 3. HEAT T REATED REPAIR BRACKET IAW AAR 111HT, REVISION 5-1-07 NR 2007-06-11 AND TO SPECIFICATIONS FOR REPAIR MATERIAL IN BOEING 7272 SRM 53-10-4 REPAIR 3 SHEET (2). LOCATED, DRILLED AND INSTALLED REPAIR BRACKET AND FILLER IAW BOEING 727 SRM 53-1 0-4 REPAIR 3, 51-30-2, 51-20-4. THIS IS CLASSSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007071000085 20070710 00085 EA 2007 7 10 A6WA200740287 1 20070608 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS UNKNOWN A A6WA O OTHER O OTHER AP APPROACH 1 GL 31 453AW 7838 ON APPROACH INTO LGA, FLAP FAIL CAUTION ILLUMINATED FLAPS AT 30 DEGREES, COMPLIED WITH Q2RH. TOUCHDOWN AT 138 KNOTS, LA NDING WEIGHT = 45,020 MAX BTMS READING = 6, 5, 6, 6. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1 .3 AND 1.4, FLAPS RESET. AIRCRAFT RELEASED FOR SERVICE. LANDING WEIGHT AND BTMS IN LIMITS, NO FURTHER ACTION REQUIRED. (M) 2 L 7 2 4F RT A21EA 2007071000094 20070710 00094 EA 2007 7 10 A6WA200740289 1 20070531 A 5320 601R75262159 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 418AW 7618 HYDRAULIC PRESSURE TRANSDUCER BRACKET CRACKED APPROX .1 INCH LONG IN LT WHEEL WELL CEILING. (M) [07-31-07] MAINTENA NCE REMOVED LT HYDRAULIC PRESSURE TRANSDUCER BRACKET AND PICKED UP HOLES ON SERVICEABLE TRANDUCER BRACKET AND INSTALLED IAW CRJ 300 SRM 51-42-06, 51-40-11 AND 51-41-02. (K) 2 L 7 2 4F RT A21EA 2007071000097 20070710 00097 EA 2007 7 10 A6WA200740294 1 20070531 A 5320 601R75262157 BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 418AW 7618 HYDRAULIC PRESSURE TRANSDUCER BRACKET CRACKED APPROX .1 INCH LONG IN RT WHEEL WELL CEILING. (M) 2 L 7 2 4F RT A21EA 2007071000098 20070710 00098 EA 2007 7 10 A6WA200740299 1 20070601 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 418AW 7618 RT FS 484 INTERCOSTAL PREVIOUS REPAIR ANGLE CRACKED APPROX .3 INCH LONG AT RBL 36 ON PRESSURE FLOORBEAM. (M) [07-31-0 7] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED REPAIR ANGLE IAW BSC SR 601R-53-0030A AND MFG REO 601R53-41-059, RE V A. (K) 2 L 7 2 4F RT A21EA 2007071000099 20070710 00099 EA 2007 7 10 A6WA200740290 1 20070531 A 5320 601R75262157 BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 418AW 7618 HYDRAULIC PRESSURE TRANSDUCER BRACKET CRACKED APPROX .1 INCH LONG IN RT WHEEL WELL CEILING. (M) [07-31-07] MAINTENA NCE REMOVED RT HYDRAULIC PRESSURE TRANSDUCER BRACKET PICKED UP HOLES ON SERVICEABLE TRANSDUCER BRACKET AND INSTALLED IAW SRM. (K) 2 L 7 2 4F RT A21EA 2007071000100 20070710 00100 EA 2007 7 10 A6WA200740300 1 20070601 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 418AW 7618 RIGHT FS 484 INTERCOSTAL ANGLE CRACKED APPROX .1 INCH LONG AT RBL 27 ON PRESSURE FLOORBEAM. (M) [07-31-07] MAINTENA NCE REMOVED CRACKED ANGLE, MANUFACTURED AND DRILLED NEW ANGLE IAW BAS STANDARD REPAIR 601R53-0029B AND CRJ 200 SRM INSTA LLED NEW FABRICATED ANDLE AT RT FS 484, RBL 27 IAW MFG STANDARD REPAIR 601R-53-0029B. (K) 2 L 7 2 4F RT A21EA 2007070300203 20070703 00203 NM 2007 7 3 UPS07450028 1 20070601 A 5313 STRINGER BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C FWD CARGO COMPT S39L STRINGER FOUND CORROSION AT STA 745. (CORROSION BLEND OUT 0.063 X .875 X 1.25 IN CH OUT OF SRM 53-10-01 FIG 1 LIMITS). FWD CARGO COMPT BS 740 TO BS 770 STR 39L REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007070300208 20070703 00208 NM 2007 7 3 UPS07M50032 1 20070623 A 3350 POWER SUPPLY DOUG MD11 MD11F 3023600 NM COCKPIT FAULTY A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:N/A EMERGENCY LIGHT FLICKERS ON AND OFF INTERMITTENTLY. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW 33-51-01-1. OPS CHECK OK. 2 L 7 3 4F RT A22WE 2007070300210 20070703 00210 EU 2007 7 3 SA07043 1 20070623 A 2120 UNKNOWN AIRBUS A321 A321211 3930370 EU CABIN ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 170US 1462 PHX FLT 732 EN-ROUTE, LAX TO CLT. AFTER TAKEOFF, A STRONG ODOR WAS NOTICED IN THE AFT CABIN. THE FLIGHT CREW ELECTED TO DIVERT TO PHX FOR MAINTENANCE. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. 2 L 7 2 4F RT A28NM 2007070300212 20070703 00212 EA 2007 7 3 TRAX200700882 1 20070621 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 MAIN CABIN DOOR HARD TO OPEN AND CLOSE. FLTS 4094, 4467, 4801 CX AND ON 6/22/07 FLT 4813 CX. (PASSENGER DOOR POWER ASS IST SYSTEM) 2 L 7 2 4F RT A21EA 2007070300216 20070703 00216 SO 2007 7 3 FDKA200703137 1 20070327 A 5241 SEAL EMB 145 EMB145LR 3260212 SO GALLEY DOOR LOOSE A FDKA O OTHER O OTHER CR CRUISE 1 SW 07 830MJ 145259 FDM 6129 RDU-FLL (1441 PHX LCL). GALLEY DOOR WAS SQUEALING IN FLIGHT. MX RE-SECURED THE DOOR SEAL. 2 L 7 2 4T RT T00011AT 2007070300225 20070703 00225 SO 2007 7 3 FDKA200704154 1 20070415 A 1100 PLACARD EMB 145 EMB145LR 3260212 SO FLASHLIGHT MISSING A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 849MJ 145534 FDM 6148 MCO-MIA (0354 PHX LCL). FWD & AFT EMERGENCY FLASHLIGHT M106 STICKERS MISSING. MX INSPECTED AND REPLACED STICK ERS. 2 L 7 2 4T RT T00011AT 2007070300232 20070703 00232 SO 2007 7 3 FDKA200704166 1 20070404 A 5720 DOUBLER EMB 145 EMB145LR 3260212 SO WING CORRODED A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 848MJ 145530 DOUBLER ON PANEL 6732 IS CORRODED. REMOVED AND REPLACED DOUBLER. 2 L 7 2 4T RT T00011AT 2007070300235 20070703 00235 SO 2007 7 3 FDKA200704162 1 20070424 A 5210 CAM EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 831MJ 145273 FDM 6053 PHF-ATL (0615 PHX LCL). MAIN PASSENGER DOOR IS HARD TO OPEN AND CLOSE. MX LUBED CAM, DOOR SEAL. 2 L 7 2 4T RT T00011AT 2007070300240 20070703 00240 WP 2007 7 3 ABXA070200 1 20070524 A 5320 992209239 INTERCOSTAL DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 INTERCOSTAL CRACKED IN CEILING STRUCTURE AT FL 256, LEFT BUTT LINE 22. REPAIRED INTERCOSTAL IAW DC9 SSRM DWG K05159. 2 L 7 2 4F A6WE 2007070300245 20070703 00245 WP 2007 7 3 ABXA070201 1 20070527 A 5320 59217181 ATTACH BRACKET DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 FUSELAGE FRAME UPPER ATTACH BRACKET CRACKED AT LEFT BUTT LINE 54, APPROXIMATELY FS 412. REMOVED AND REPLACED FITTING IA W DC9 REA D953-55887-MR. 2 L 7 2 4F A6WE 2007070300250 20070703 00250 WP 2007 7 3 ABXA070197 1 20070523 A 5320 991050313 CUSP WEB DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 RIGHT CUSP WEB AT STA 943 - 965 CRACKED AT 4 PLACES. REPAIRED CUSP WEB IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 2007070900004 20070709 00004 NM 2007 7 9 AALA20071099 1 20070613 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 DFW - EMERGENCY EXIT LIGHT AT LEFT NUMBER THREE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT AT LEF T NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007070900009 20070709 00009 NM 2007 7 9 AALA20071095 1 20070613 A 3350 8039001 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9414W 53189 LGA - EMERGENCY EXIT LIGHT AT SEAT ROW 29 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT AT SEAT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2007070900010 20070709 00010 NM 2007 7 9 AALA20071096 1 20070613 A 3350 8039001 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9414W 53189 LGA - EMERGENCY EXIT LIGHT AT SEAT ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT AT SEAT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2007070900014 20070709 00014 NM 2007 7 9 AALA20071107 1 20070615 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 766AN 32880 ORD - EMERGENCY EXIT LIGHT AT SEAT ROW 30 CENTER AISLE INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT SEAT ROW 30 CENTER AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007070900025 20070709 00025 WP 2007 7 9 AALA20071092 1 20070612 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7536A 49990 LGA - EMERGENCY LIGHT AT AFT JUMP SEAT INOPERATIVE. RELAMPED EMERGENCY LIGHT AT AFT JUMP SEAT. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F A6WE 2007070900028 20070709 00028 EU 2007 7 9 AALA20071084 1 20070611 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14077 612 JFK - EMERGENCY EXIT LIGHT AT RIGHT NUMBER FOUR ENTRY DOOR INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT RIGHT NUMBER F OUR ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007070900029 20070709 00029 NM 2007 7 9 AALA20071086 1 20070612 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 JFK - EMERGENCY LIGHT ABOVE SEAT 26C INOPERATIVE. RELAMPED EMERGENCY LIGHT ABOVE SEAT 26C. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT T00001SE 2007070900035 20070709 00035 NM 2007 7 9 07FDEA02289 1 20070627 A 5311 655611414 FRAME BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD PIT BILGE BODY FRAME SHEAR TIE IS BUCKLED/CORRODED BS 720B, STR 28L-28R, WL 148. REMOVED CORROSION, ORIGINAL THICK NESS- .063", REMAINING- .058", MATERIAL LOSS- .005". WITHIN LIMITS REFERENCING SRM 51-10-6 AND 53-10-1 USING NR 2221 CA L DUE 4-24-08. STRAIGHTEN SHEAR TIE, REF SRM 51-40-1, NDT, NO DEFECTS NOTED REF NDT 51-00-00 PT 6 FIG 23, TOOL NR IN 22 -0044, DUE 5-21-08. TREATED AND PRIMED SHEAR TIE REF SRM 51-10-2. LEVEL 1 CORROSION. 2 L 7 3 4F RT A3WE 2007070900051 20070709 00051 NM 2007 7 9 NWAA072266731 1 20070626 A 2913 PUMP BOEING 747 747251B 1384892 NM NR 1 HYD SYSTEM FAILED A NWAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 631NW 23111 AFTER TAKEOFF NR 1 HYDRAULIC QUANTITY WENT TO ZERO. FLIGHT CONTINUED ON TO ANC AND LANDING WAS UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED ENGINE DRIVEN PUMP (EDP) AND AIR DRIVEN PUMP FLEX HOSE. OPERATIONAL CHECKED GOOD AND AIRCRAFT RET URNED TO SERVICE. 2 L 7 4 4F A20WE 2007070900073 20070709 00073 EU 2007 7 9 COEA0703908 1 20070307 A 5311 S53172158200 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE DAMAGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 908FX 023 GOUGE LOCATED ON THE VERTICAL WEB OF FRAME 7 AT BL 0 IN THE NLG WELL. DAMAGE CUTOUT AND FABRICATED DOUBLER INSTALLED P ER DO/TS-3265/06-7477 AND DO/TS-3926/06-7477. REF SRAS DO/TS03265/06...3787. (M) 2 H 7 2 4T RT A53EU 2007070900074 20070709 00074 EU 2007 7 9 COEA0704908 1 20070307 A 5300 S53172149200 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CRACKED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 908FX 023 CRACK FOUND ON FUSELAGE FRAME 5 LOWER FLANGE CLOSE TO LT NLG WHEEL WELL. CRACK REMOVED AND REINFORCING ANGLE INSTALLED PER ATR REPAIR INSTRUCTIONS DO/TS-3825/06-7654. REF SRAS DO/TS-3825/06...3816. (M) 2 H 7 2 4T RT A53EU 2007070900078 20070709 00078 EU 2007 7 9 COEA0712903 1 20070109 A 5312 S53572601206 BULKHEAD AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 903FX 179 DURING HEAVY CHECK, FOUND CRACK ON FRAME 25 LT AND RT OUTBOARD LOWER SIDE OF HYDRAULIC LINE CUTOUT. MAINTENANCE FOUND S B ATR42-53-0120 HAD BEEN PREVIOUSLY COMPLIED WITH. COMPLIED WITH SB ATR42-53-0121 ON BOTH LT AND RT SIDES FOR FRAME 25 HYDRAULIC LINES CUT OUT. VERIFIED CRACKS HAD NOT EXTENDED FURTHER PAST PREVIOUSLY COLD WORKED STOP DRILLED HOLES. (M) 2 H 7 2 4T RT A53EU 2007070900086 20070709 00086 WP 2007 7 9 ABXA070189 1 20070521 A 5347 391620502 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 CRACK FROM UPPER OUTBOARD BOLT HOLE TO EDGE OF FITTING - BELOW SEAT TRACK AT RIGHT BUTT LINE 44, FS 680. REMOVED AND RE PLACED FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2007070900087 20070709 00087 WP 2007 7 9 ABXA070190 1 20070522 A 5347 S2914913M24000 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 590 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 SEAT TRACK CORRODED AT SPLICE FS 590, RIGHT BUTT LINE 44.5. REMOVED AND REPLACED TRACK IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 2007070900088 20070709 00088 2007 7 9 FDKA200704175 4 20070428 A 2210 DAU EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 FDM 5975 ATL-BMI (0948 PHX LCL). AUTO FAIL AND RUDDER SYSTEM 1 AND 2 INOPERATIVE. MX RE-RACKED IC 600 AND DAU 1 AND OP S CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007070900089 20070709 00089 SO 2007 7 9 FDKA200704177 1 20070429 A 2720 3603001001 PCU EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 13378 145481 FDM 6107 MCO-MIA (1408 PHX LCL). RTF DUE TO RUDDER SYSTEM 1 AND 2 INOP MESSAGE. MX REMOVED AND REPLACED PCU. 2 L 7 2 4T RT T00011AT 2007071000025 20070710 00025 NM 2007 7 10 HNAA0700126 1 20070626 A 5730 SKIN DHAV DHC8 DHC8102 2809003 NM RT WING CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 912HA 040 RIGHT WING AUX FUEL BOOST PUMP SKIN DOUBLER CORROSION SUSPECTED ON PREVIOUS BLENDED AREA (INSIDE TANK). RIGHT WING AUX FUEL PUMP WING BLENDED AS PER RD 8-57-1907 (.45 MIN REMAINING) SB 8-57-28 FOUND PREVIOUSLY COMPLIED WITH. HFEC & DISBON D C/O IAW RD 8-57-1907, NO DEFECTS. 2 H 7 2 4T RT A13NM 2007071000046 20070710 00046 SO 2007 7 10 FDKA200705208 1 20070516 A 5210 DOOR EMB 145 EMB145LR 3260212 SO PAX DOOR DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 145416 FDM 6116 PFN-MCO (1552 PHX LCL). MAIN CABIN DOOR DAMAGED BY TUG. A/C FERRIED TO BNA FOR REPAIRS. 2 L 7 2 4T RT T00011AT 2007071000054 20070710 00054 SO 2007 7 10 FDKA200705218 1 20070520 A 2720 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO RUDDER MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 852MJ 145567 FDM 9960 TRI (1625 PHX LCL). RUDDER HARDOVER PROTECTION FAIL DURING TAXIING. RESET WITH THE CAPTAIN AND MESSAGE CLEARE D. 2 L 7 2 4T RT T00011AT 2007071000056 20070710 00056 SO 2007 7 10 FDKA200705220 1 20070522 A 2720 RELAY EMB 145 EMB145LR 3260212 SO RUDDER FAILED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 852MJ 145567 FDM RON MCO. RUDDER HARD OVER PROTECTION. MX T/S SYSTEM WITH BREAK OUT BOX AND REPLACED RELAYS K0544, K0545, K0546, K0 547, K0773, K0059, K0385. SYSTEM FUNCTIONAL CHECK AND RUNS GOOD. 2 L 7 2 4T RT T00011AT 2007071000058 20070710 00058 NM 2007 7 10 DHL2007783525 1 20070621 A 5320 CHANNEL BOEING 727 727227 1384078 NM BS 1040 S29-30R CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 CRACK AT VHF NR 3 ANT CHANNEL LT SIDE BETWEEN STR 30R AND 29R STA 1040. REMOVED VHF NR 3 ANTENNA IAW B727 51-30-2. REM OVED ANTENNA CHANNEL IAW B727 SRM 51-30-2. FABRICATED NEW CHANNEL FROM MATERIAL 7075-T6, .050, DIM 20” BY 7.5 IAW B727 SRM 51-20-1 AND EC-00412-001. TREATED, PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED NEW PARTS IAW B727 SRM 51 -30-2 AND 51-20-1. INSTALLED NR 3VHF ANTENNA IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007071000083 20070710 00083 NM 2007 7 10 DHLA200700033 1 20070628 A 3350 BATTERY BOEING 727 7272B7 138407L NM EMERGENCY LIGHTS INOPERATIVE A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 770AT 21953 DURING STBY PWR CHECK, THE EXIT LIGHTS WOULD NOT ILLUMINATE. REMOVED AND REPLACED FLIGHT COMPT AND MAIN ENTRY DOOR EMER GENCY LIGHT BATTERIES. OPS CHECKS OK IAW 727MM 33-50-71 PN OFF AND ON 37067-001. 2 L 7 3 4F A3WE 2007071000084 20070710 00084 EA 2007 7 10 A6WA200740288 1 20070608 A 3220 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA SELECTOR VALVE DIRTY A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 406AW 7402 GEAR DISAGREE AND DOOR WARNING MESSAGE INFLIGHT, COMPLIED WITH QRH AND RETURNED TO PHL. FOUND ERROR CODE D046/SELECTOR VALVE IN PSEU. CLEANED CONNECTOR AND FILTER AT NLG SELECTOR VALVE. PERFORMED NLG EXTENSION AND RETRACTION TEST IAW AMM 32-33-00. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007071000086 20070710 00086 EA 2007 7 10 A6WA200740286 1 20070606 A 2150 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA LT A/C PACK MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 453AW 7838 LT PACK OVERPRESSURE ON CLIMB-OUT OF 5000 FT, RESET PACK UPON CLIMBING LT PACK OVERTEMP MESSAGE. AIR RETURN TO ORF. LA NDING WEIGHT = 41,300. MAX BTMS = 4. REMOVED AND REPLACED LT PRSOV IAW 21-51-43, OPS AND LEAK CHECK GOOD. AIRCRAFT LA NDING WEIGHT WITHIN LIMITS, NO FURTHER ACTION REQUIRED. (M) 2 L 7 2 4F RT A21EA 2007071000087 20070710 00087 EA 2007 7 10 A6WA200740285 1 20070601 A 5240 GUST LOCK CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR INOPERATIVE A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 435AW 7724 GUST LOCK ON SERVICE DOOR INOPERATIVE. INSPECTED AND FOUND HANDLE ROLL PIN BROKEN. REMOVED AND REPLACED PIN, PERFORMED OPS CHECK IAW AMM 52-41-00, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007071000088 20070710 00088 EA 2007 7 10 A6WA200740302 1 20070601 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 418AW 7618 LT FS 484 INTERCOSTAL ANGLE CRACKED APPROX .2 INCH LONG AT LBL 27 ON PRESSURE FLOORBEAM. (M) [07-31-07] MAINTENANC E REMOVED CRACKED ANGLE AND INSTALLED REPAIR ANGLE IAW BSC STANDARD REPAIR 601R-53-0029B. (K) 2 L 7 2 4F RT A21EA 2007071000089 20070710 00089 EA 2007 7 10 A6WA200740305 1 20070601 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 418AW 7618 AFT PAX DOOR DRAG ANGLE IS CRACKED APPROX 1 INCH LONG. (M) [07-31-07] MAINTENANCE FOUND DAMAGE TO BE LOCATED ON PREV IOUS REPAIR. REMOVED PREVIOUS REPAIR ANGLE FABRICATED NEW ANGLE INSTALLED AND SEALED PAINTED IAW REO 601R52-11513. (K) 2 L 7 2 4F RT A21EA 2007071000101 20070710 00101 EA 2007 7 10 A6WA200740297 1 20070531 A 5320 601R75262157 BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 418AW 7618 HYDRAULIC PRESSURE TRANSDUCER BRACKET CRACKED APPROX .1 INCH LONG IN RT WHEEL WELL CEILING. (M) 2 L 7 2 4F RT A21EA 2007071000102 20070710 00102 EA 2007 7 10 A6WA200740298 1 20070601 A 5315 6003106819 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 460 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 418AW 7618 FS 460 PRESSURE FLOORBEAM SUPPORT ANGLE CRACKED APPROX .2 INCH LONG OUTBOARD SIDE OF RBL. (M) [07-31-07] MAINTENANC E REMOVED CRACKED FITTING, DRILLED AND INSTALLED NEW SERVICEABLE FITTING PN 600-31068-19, IAW SRM. (K) 2 L 7 2 4F RT A21EA 2007071000103 20070710 00103 EA 2007 7 10 A6WA200740292 1 20070531 A 5320 601R75262159 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 418AW 7618 HYDRAULIC PRESSURE TRANSDUCER BRACKET CRACKED APPROX .1 INCH LONG IN LT WHEEL WELL CEILING. (M) 2 L 7 2 4F RT A21EA 2007071000104 20070710 00104 EA 2007 7 10 A6WA200740307 1 20070608 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 418AW 7618 FLOORBEAM ANGLE AT FS 280, LBL 11, CRACKED IN RADIUS APPROX .5 INCH LONG. (M) [07-31-07] MAINTENANCE REPAIRED ANGLE IAW REO 601R-53-11-138. (K) 2 L 7 2 4F RT A21EA 2007071000105 20070710 00105 EA 2007 7 10 A6WA200740291 1 20070531 A 5320 601R75262153 BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 418AW 7618 HYDRAULIC LINE Z-BRACKET CRACKED APPROX .1 INCH LONG IN RT WHEEL WELL CEILING FORWARD OF PRESSURE TRANSDUCERS. (M) [ 07-31-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW BRACKET IAW CRJ 200 SRM. (K) 2 L 7 2 4F RT A21EA 2007071000106 20070710 00106 EA 2007 7 10 A6WA200740301 1 20070601 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 418AW 7618 LT FS 484 INTERCOSTAL PREVIOUS REPAIR ANGLE CRACKED APPROX .3 INCH LONG AT LBL 36 ON PRESSURE FLOORBEAM. (M) [07-31-0 7] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED REPAIR ANGLE IAW BSC STANDARD REPAIR 601R-53-0030A AND REO 601R-53- 41-059 REV A. (K) 2 L 7 2 4F RT A21EA 2007071000107 20070710 00107 EA 2007 7 10 A6WA200740296 1 20070531 A 5320 601R75262153 BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 418AW 7618 HYDRAULIC LINE Z-BRACKET CRACKED APPROX .1 INCH LONG IN RT WHEEL WELL CEILING FORWARD OF PRESSURE TRANSDUCERS. (M) 2 L 7 2 4F RT A21EA 2007071000108 20070710 00108 SO 2007 7 10 FDKA200705235 1 20070508 A 5320 14525480603 THRESHOLD EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 850MJ 145568 CARGO DOOR THRESHOLD IS CORRODED OUT OF LIMITS. THE THRESHOLD HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2007071000109 20070710 00109 EA 2007 7 10 A6WA200740303 1 20070531 A 5300 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 418AW 7618 FOUND FS 280 CLIPS INBOARD AND OUTBOARD AT LBL 9 ARE CRACKED. (M) [07-31-07] MAINTENANCE REMOVED AND REPLACED CLIPS AT FS 280, LBL 9 WITH NEW CLIPS PN 601R3111357. (K) 2 L 7 2 4F RT A21EA 2007071000110 20070710 00110 NM 2007 7 10 AMTA200700288 1 20070612 A 4930 4419214 FUEL CONTROL BOEING 737 73783N 13844HI NM APU INOPERATIVE A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 310TZ 8494 8494 28243 APU WOULD NOT START FAULT LIGHT ILLUM. REPLACED FCU IAW AMM 49-31-11-4 AND PERFORMED APU BITE CHECK. NO FAULTS ON SEVE RAL STARTS. (K) 2 L 7 2 4F RT A16WE 2007071000123 20070710 00123 NM 2007 7 10 SWAA073200 1 20070627 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 274WN 32529 EEPLS COVER LOOSE AT ROW 3 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007071000127 20070710 00127 NM 2007 7 10 SWAA073219 1 20070627 A 2752 56970 MOTOR BOEING 737 7373H4 1384600 NM T/E FLAP FAILED A SWAA K NONE O OTHER TX TAXI/GRND HDL 1 SW 29 336SW 23940 FLAPS WOULD NOT EXTEND AFTER PUSH BACK. R&R FLAP HYD POWER MOTOR PER MM. 2 L 7 2 4F RT A16WE 2007071000129 20070710 00129 2007 7 10 SWAA073202 4 20070627 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 468WN 33858 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071000130 20070710 00130 2007 7 10 SWAA073217 4 20070627 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 767SW 29807 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071000137 20070710 00137 NM 2007 7 10 SWAA073211 1 20070627 A 5753 6546434 FLAP BOEING 737 7375H4 138449D NM RT WING DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DISBONDED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007071000162 20070710 00162 NM 2007 7 10 DLM88070808 1 20070620 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 1380 L14R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 CRACKED FUSELAGE SKIN AROUND FASTENERS AT STA 1380 LONG 14 RT. REPAIRED PER SRM 53-04D FIG 18 ON N/R T0059314 HMV/GDL. 2 L 7 2 4F RT A6WE 2007071000163 20070710 00163 NM 2007 7 10 DLM88070809 1 20070619 A 5313 LONGERON DOUG MD88 MD88 3023688 NM BS 1437 L3R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 CRACK ON LONGERON 3RH STA1437. REPAIRED PER SRM 53-02 FIG 18 ON NR T0058495 2 L 7 2 4F RT A6WE 2007071000165 20070710 00165 NM 2007 7 10 SWAA073205 1 20070627 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L AND 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071000166 20070710 00166 NM 2007 7 10 DLM88070810 1 20070620 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 244-246 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 SURFACE CORROSION ON INNER FUSELUGE SKIN BETWEEN STA 244 AND LONGERONS 29-30 LT. REPAIRED PER DWG 5936434 ON N/R T00592 77 HMV/GDL. 2 L 7 2 4F RT A6WE 2007071000167 20070710 00167 NM 2007 7 10 SWAA073212 1 20070627 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071000168 20070710 00168 NM 2007 7 10 DLM88070811 1 20070620 A 5311 FRAME DOUG MD88 MD88 3023688 NM BS 1416 L6L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 CRACK ON FRAME ANGLE AT STA 1416 CANT LONGERON 6 LT. REPAIRED PER DRAWING 9977858 ITEM 160 ON NR T0058491. 2 L 7 2 4F RT A6WE 2007071000169 20070710 00169 NM 2007 7 10 SWAA073222 1 20070627 A 5315 65C33942 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FLOOR BEAM CORRODED AT BS 328, LBL 56 TO RBL 56. REPAIRED FLOOR BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007071000170 20070710 00170 NM 2007 7 10 DLM88070812 1 20070620 A 5313 LONGERON DOUG MD88 MD88 3023688 NM BS 1437 L4L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 CRACK ON LONGERON 4 LH STA 1473. REPAIRED PER SRM 53-02 FIG 18 ON NR T0058494. 2 L 7 2 4F RT A6WE 2007071000171 20070710 00171 NM 2007 7 10 SWAA073221 1 20070627 A 5315 65C34597 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5, LBL 53 TO RBL 52. REPAIRED FLOOR BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007071000172 20070710 00172 NM 2007 7 10 DLM88070813 1 20070623 A 3397 CONNECTOR DOUG MD88 MD88 3023688 NM EMERGENCY LIGHT DISCONNECTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 903DL 49534 ON LAYOVER, FOUND SEATROW 18ED EMERGENCY PATHWAY LIGHTS INOP FOUND ELECTRICAL CONNECTOR UNDER SEAT UNPLUGGED. RECONNECT ED ELECTRICAL CONNECTOR, OPS CK GOOD. 2 L 7 2 4F RT A6WE 2007071000173 20070710 00173 NM 2007 7 10 SWAA073220 1 20070627 A 5315 BAC15091000146 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 406WN 27894 DURING SCHEDULED 6Y CHECK, FOUND FLOORBEAM CORRODED BETWEEN BS 767 AND BS 787, RBL 14. REPAIRED FLOOR BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007071000174 20070710 00174 NM 2007 7 10 DLM88070814 1 20070623 A 3397 CONNECTOR DOUG MD88 MD88 3023688 NM EMERGENCY LIGHT BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 903DL 49534 ON LAYOVER FOUND SEATROW 1DC EMERGENCY PATHWAY LIGHTS INOP. FOUND ELECTRICAL CONNECTION UNDER SEAT BROKEN. REPAIRED EL ECTRICAL CONNECTOR. OPS NML. 2 L 7 2 4F RT A6WE 2007071000176 20070710 00176 2007 7 10 DL76L070815 4 20070621 A 3444 341080163 COMPUTER BOEING 767 767332 1382001 NM LT IRS MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 171DN 24759 LT IRS FAULT LIGHT CAME ON, DURING TAXI PRIOR TO TAKE OFF. REMOVED AND REPLACED LT IRS COMPUTER PER M/M. 2 L 7 2 4F RT A1NM 2007071000177 20070710 00177 NM 2007 7 10 SWAA073216 1 20070627 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 760SW 27874 DURING SCHEDULED SPV CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007071000179 20070710 00179 NM 2007 7 10 DL76L070816 1 20070622 A 2800 VALVE BOEING 767 767332 1382001 NM RIGHT UNKNOWN A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 197DN 28454 RT ENG VLV AND SPAR VLV FAIL TO OPEN DURING START. RESET SPAR VLV C/B, VISUAL INSP SPAR VLV OK, RESET. FIREHANDLE ENG RUN TEST GOOD. 2 L 7 2 4F RT A1NM 2007071000180 20070710 00180 NM 2007 7 10 SWAA073215 1 20070627 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 734SA 27866 DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007071000181 20070710 00181 NM 2007 7 10 SWAA073213 1 20070627 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 734SA 27866 DURING SCHEDULED HC2 CHECK, LH OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007071000182 20070710 00182 NM 2007 7 10 DLM90070817 1 20070624 A 5330 5924802133 SKIN DOUG MD900 MD900 3027375 NM BS 245 L17-18L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 903DA 53383 DENT NEAR STA 245 BETWEEN L-17L AND L-18L. CUT OUT DENT AND INSTALL REPAIR DOUBLER. 1 G 7 2 3U NC H19NM 2007071000183 20070710 00183 NM 2007 7 10 SWAA073204 1 20070627 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT INOP. R&R FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2007071000185 20070710 00185 SO 2007 7 10 FDKA200705232 1 20070507 A 5414 SKIN EMB 145 EMB145LR 3260212 SO RT COWLING CHAFED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 850MJ 145568 RIGHT LOWER COWL INTERNAL SKIN IS DAMAGED BEYOND LIMITS BETWEEN FRAMES 4&5 AT CENTER LINE. REPAIRED SKIN. 2 L 7 2 4T RT T00011AT 2007071000187 20070710 00187 SO 2007 7 10 FDKA200705243 1 20070525 A 7830 14578322004 SEAL DEPRESSOR EMB 145 EMB145LR 3260212 SO THRUST REVERSER DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 831MJ 145273 OUTBOARD SEAL DEPRESSOR ON THE RIGHT UPPER THRUST REVERSER IS DAMAGED. THE SEAL DEPRESSOR HAS BEEN REMOVED AND REPLACED . 2 L 7 2 4T RT T00011AT 2007071000188 20070710 00188 NM 2007 7 10 DL76S070818 1 20070624 A 5340 141T992110 FITTING BOEING 767 767332 1382001 NM BS 276 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 125DL 24075 RT NLG TRUNNION BORE CORRODED AND TOOLING DAMAGE FOUND ON WEB. BORE OVERSIZED AND AN OVERSIZED BUSHING INSTALLED. TOOL ING DAMAGE OVERSIZED AND A BUSHING INSTALLED. 2 L 7 2 4F RT A1NM 2007071000189 20070710 00189 2007 7 10 DLM88070819 4 20070624 A 2297 WIRE DOUG MD88 MD88 3023688 NM AUTOTHROTTLES CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 902DE 53379 WKG MCO - AUTOTHROTTLES DISCONNECTED. DURING T/S FOUND CHAFED WIRES AT AUTOTHROTTLE SERVO. CUT BACK ALL A/T SERVOMOTOR WIRES PRIOR TO DAMAGED AREA AND REPLACED A/T SERVOMOTOR C/P P10-430. MADE REPAIR TO DAMAGED SYSTEM WIRES PER MM. RTS ON DFGC 1 AND 2 GOOD. PERFORMED TESTS ON ALL AFFECTED SYSTEMS ASSOCIATED WI DAMAGED WIRING ALL A/C SYSTEMS TEST GOOD. A/T CHKS GOOD, CLEARED MCO AND REMOVED PLACARD. 2 L 7 2 4F RT A6WE 2007071000190 20070710 00190 SO 2007 7 10 FDKA200705244 1 20070525 A 5420 ANGLE EMB 145 EMB145LR 3260212 SO LT COWLING DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 831MJ 145273 LEFT UPPER COWLING, INBOARD ANGLE IS DAMAGED. THE DAMAGED ANGLE HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2007071000191 20070710 00191 NM 2007 7 10 DL777070821 1 20070625 A 5100 NONE BOEING 777 777232 1385232 NM NONE NONE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 865DA 29737 WINDSHEAR MSG DISPLAYED. FWD WINDSHEAR TO MCO PER MEL 34-43-01D. NO FAULT HIST IN MAT. RAN WXR TEST NO FAULTS. MCO A ND PLACARD REPLACED. 2 L 7 2 4F RT T00001SE 2007071000193 20070710 00193 NM 2007 7 10 DL76L070822 1 20070625 A 4920 380029817 ENGINE BOEING 767 767332 1382001 NM APU MAKING METAL A DALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 184DN 33888 27111 APU AUTO SHUTDOWN AT DEPARTURE, DELAY TAKEN JFK WORKING MCO FOUND METAL ON CHIP DETECTOR. FOUND HEAVY METAL ACCUMULATIO N ON OIL CHIP DETECTORS. REMOVED AND REPLACED AP PER MM. OPS AND LEAK CHK OK. MCO AND PLACARD REMOVED. 2 L 7 2 4F RT A1NM 2007071000195 20070710 00195 NM 2007 7 10 DL76G070823 1 20070625 A 2910 VALVE BOEING 767 7673P6 1385105 NM HYD SYSTEM UNKNOWN A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 1501P 24983 AFTER PUSHBACK CTR HYD PRESS WOULD NOT RISE PAST 460 PSI. RTB, RESET HMG VALVE. 2 L 7 2 4F RT A1NM 2007071000196 20070710 00196 NM 2007 7 10 DL76S070825 1 20070626 A 5330 148T3121 SKIN BOEING 767 767332 1382001 NM BS 1725 S7R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 DURING INSPECTION OF THE FS 1725.5 SKIN AND CHORD STRAP AT S-7R WAS FOUND CRACKED THAT WAS OUTSIDE OF THE 767 SRM 53-80- 01 REPAIR 5. BOEING APPROVED REPAIR WAS INSTALLED PER 462298-14AD. 2 L 7 2 4F RT A1NM 2007071000197 20070710 00197 NM 2007 7 10 DL76L070826 1 20070626 A 2560 FLASHLIGHT BOEING 767 767332 1382001 NM L1 DOOR FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 186DN 27962 AT FWD ENTRY DOOR EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY AT FWD ENTRY DOOR LEFT SIDE EMERGENCY FLASHLIGHT AND INST ALLED PLASTIC GUARDS OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007071000198 20070710 00198 NM 2007 7 10 DL76G070827 1 20070626 A 2133 211080120 OUTFLOW VALVE BOEING 767 767332 1382001 NM CLABIN PRESSURE INOPERATIVE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 172DZ 29691 CABIN AUTO INOP EICAS AUTO 1 AND 2. PERFORMED BITE ON CABIN PRESS CONTROLLERS. NO FAULTS NOTED. DUE TO HIST REMOVED A ND REPLACED CABIN OUTFLOW VALVE PER AMM. ALL OPS CHK NORMAL. 2 L 7 2 4F RT A1NM 2007071000199 20070710 00199 SO 2007 7 10 FDKA200705248 1 20070529 A 5320 14522226003 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 831MJ 145273 THE LEFT GUSSET, AT THE FLOOR LEVEL AND AT FRAME 62 (LAV GUSSET) IS CORRODED OUT OF LIMITS. THE DAMAGED PART HAS BEEN R EMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2007071000200 20070710 00200 NM 2007 7 10 DL76S070828 1 20070627 A 5415 311T1231 FITTING BOEING 767 767332 1382001 NM NR 1 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 DURING INSPECTION PER SIP EO MOD, NR 1 PYLON BULKHEAD FITTING WAS FOUND CRACKED AT BOLT HOLE COMMON TO UPPER SPAR FITTIN G. THE DISCREPANT HOLE ON BULKHEAD FITTING WAS OVERSIZED TO A FINAL DIAMETER OF 1.125" UNTIL THE CRACK INDICATION WAS R EMOVED. BOEING APPROVED REPAIR INSTALLED PER ERA 461699-14AD. 2 L 7 2 4F RT A1NM 2007071000201 20070710 00201 NM 2007 7 10 DL76S070829 1 20070627 A 5511 182T13202 FITTING BOEING 767 767332 1382001 NM HORIZONTAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 A CRACK INDICATION WAS FOUND DURING ACCOMPLISHMENT OF HORIZONTAL STABILIZER PIVOT FITTINGS PER OPN 5927AD, LHS OUTBOARD FITTING, LOWER RIB CHORD, AND LOWER SPLICE PLATE. BOEING WAS CONTACTED FOR REPAIR INSTRUCTIONS FOR HOLE OVERSIZING. TH E REPAIR WAS APPROVED AND IS DOCUMENTED IN ERA 462304-14AD. 2 L 7 2 4F RT A1NM 2007071000202 20070710 00202 NM 2007 7 10 DL76S070830 1 20070628 A 5312 BULKHEAD BOEING 767 767332 1382001 NM BS 1809 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 ON HMV, FOUND BULKHEAD CRACKED. REPAIRED PER SRM 53-80-00. REPAIR NR 9 FIG 201. AREA OF REPAIR WAS BS 1809 BETWEEN ST RINGER 4R AND 8R. 2 L 7 2 4F RT A1NM 2007071000203 20070710 00203 NM 2007 7 10 DL76G070831 1 20070627 A 3800 LINE BOEING 767 767332 1382001 NM LWR DRAIN CLOGGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1607B 30388 DRAIN AT L1 DOOR BLOCKED UP WASTE WATER FOUND ON DRIP PAN OVER EICAS COMPUTERS. ON INSPECTION, FOUND EXCESSIVE WASTE WA TER ABOVE EICAS COMPUTER DRIP TRAY. TRACED BLOCKAGE TO DRAIN LINE ADJACENT TO FWD DRAIN MAST. REMOVED DEBRIS INCLUDI NG BOTTLE TOPS ETC. FLUSHED LINE, RETURNED A/C TO NML. OK FOR SVC. 2 L 7 2 4F RT A1NM 2007071000205 20070710 00205 NM 2007 7 10 DL76S070833 1 20070628 A 5311 146T12804 FRAME BOEING 767 767332 1382001 NM FS 1417 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 DURING THE CURRENT HMV IN HKG, A FASTENER HOLE WAS FOUND ELONGATED IN THE FS 1417 FRAME NEAR STRINGER 36L. A BOEING APP ROVED REPAIR WAS INSTALLED PER 462310-14. 2 L 7 2 4F RT A1NM 2007071000206 20070710 00206 NM 2007 7 10 07FDEA02311 1 20070628 A 5315 652082760 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 CABIN BS 540 FLOORBEAM UPPER CHORD HAS SCRATCHES ON UPPER SURFACE BETWEEN RBL2 AND RBL 10 BLENDED DAMAGED AREA, NDT FOR MATERIAL LOSS ORIGINAL .125 REMOVAL .005, SELF CONTAINED SHOT PEEN AREA. APPLIED ALODINE AND PRIME, APPLIED CORROSION I NHIBITING COMPOUND, REF SRM 51-10-1, 51-10-2, 51-20-5, MM 51-20-151, SOPM 20-10-3, EA NR 7-5310-113040. CLASSIFIED MINO R REPAIR. 2 L 7 3 4F RT A3WE 2007071000207 20070710 00207 NM 2007 7 10 07FDEA02312 1 20070628 A 5315 6518745306 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 CABIN STA 940 FLOORBEAM HAS CORROSION BETWEEN BEAM UPPER FLANGE AND SEAT TRACK AT BL 0 REMOVED CORROSION FROM FLOORBEAM AT STA 940 BL 0 IAW B727 SRM 51-10-1, ORIGINAL .125 REMAINING .123. HFEC NO DEFECTS NOTED ROTO PEENED FLOORBEAM. TREAT ED AND PRIMED REWORKED AREA IAW EA 7-5310-113050. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007071000208 20070710 00208 NM 2007 7 10 07FDEA02313 1 20070628 A 5315 652082758 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 CABIN BS 500 FLOORBEAM UPPER CHORD HAS SCRATCHES ON UPPER SURFACE BETWEEN BL 0 AND RBL 25 BLENDED AREA, VERIFIED MATERIA L LOSS, AND NO CRACK BY NDT, FLAP PEENED REF EA 7-5310-113039, TREATED AND PRIMED AREA. APPLIED CORROSION RESISTANT COM POUND THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007071000209 20070710 00209 SO 2007 7 10 FDKA200705251 1 20070529 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO CARGO BAY MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 842MJ 3349 145457 FDM 6127 FLL (0335 PHX LCL). BAGGAGE COMPARTMENT FIRE EXTINGUISHER LIGHT STAYS ON AFTER FIRE TEST. MX REMOVED AND REPL ACED NR 2 SMOKE DETECTORS. 2 L 7 2 4T RT T00011AT 2007071000210 20070710 00210 NM 2007 7 10 07FDEA02315 1 20070628 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM LT MLG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 CTR LANDING GEAR, LT TRUNNION FITTING AFT HOLE FOUND CORRODED. [07-10-07] COMPLIED WITH FEDEX E.A. 1-5310-112351. CLA SSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007071000211 20070710 00211 NM 2007 7 10 07FDEA02316 1 20070628 A 5343 AEA70511 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 CTR LANDING GEAR, LT TRUNNION FITTING FWD HOLE FOUND CORRODED. [07-10-07] REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-40-00 FIG. 16 VOL.I. ORIGINAL HOLE DIAMETER: 1.341"; REWORKED HOLE TO 1.379". MAXIMUM HOLE DIAMETER: 1.385". BUSHING FABRICATED AND INSTALLED AT CLG LT TRUNNION FITTING FWD HOLE AS PER SRM 53-40-00 FIG.16 VOL.I. REPAIR CLASSIFIED AS MAJ OR AS PER FEDEX GMM 6-2- 100. 2 L 7 3 4F RT A22WE 2007071000212 20070710 00212 SO 2007 7 10 FDKA200705252 1 20070529 A 2621 33700271 BOTTLE EMB 145 EMB145LR 3260212 SO CARGO BAY BLOWN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 842MJ 7560 145457 FDM 6127 FLL-MCO (0410 PHX LCL). CARGO BOTTLE BLOWN. MX REMOVED AND REPLACED CARGO FIRE BOTTLES. 2 L 7 2 4T RT T00011AT 2007071000213 20070710 00213 NM 2007 7 10 07FDEA02317 1 20070628 A 5343 AEA70511 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 CTR LANDING GEAR, LT TRUNNION FITTING MATING SURFACE FOUND CORRODED AFTER PILLOW BLOCK REMOVAL. [07-10-07] REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-40-00 FIG. 16 VOL.I. FWD SIDE - ORIGINAL THICKNESS: 2.536"; MATERIAL REMOVED: 0 .044" REMAINING THICKNESS: 2.492"; MIN. THICKNESS: 2.430". AFT SIDE - ORIGINAL THICKNESS: 2.534"; MAT'L REMOVED: 0.04 6"; REMAINING THICKNESS: 2.488"; MIN. THICKNESS: 2.430". REWORK AREA REPROTECTED AS PER SRM 51-20-00 VOL.II.REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007071000214 20070710 00214 NM 2007 7 10 07FDEA02318 1 20070628 A 5343 AEA70511 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 CTR LANDING GEAR, LT TRUNNION FITTING ALIGNMENT HOLE FOUND CORRODED AFTER PILLOW BLOCK REMOVAL. [07-10-07] REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-40-00 FIG. 16 VOL I. ORIGINAL HOLE DIAMETER: 1.500"; REWORKED HOLE TO 1.666". M AXIMUM HOLE DIAMETER: 1.680". BUSHING FABRICATED AND INSTALLED AS PER SRM 53-40-00 FIG.16 VOL I. REPAIR CLASSIFIED A S MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007071000217 20070710 00217 NM 2007 7 10 07FDEA02320 1 20070628 A 5343 AEA70512 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 CTR LANDING GEAR, RT TRUNNION FITTING ALIGNMENT HOLE FOUND CORRODED. [07-10-07] REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-40-00 FIG. 16 VOL.I. ORIGINAL HOLE DIAMETER: 1.500"; REWORKED HOLE TO 1.6664". MAXIMUM HOLE DIAMETER: 1 .680". BUSHING FABRICATED AND INSTALLED AS PER SRM 53-40-00 FIG.16 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GM M 6-2-100. 2 L 7 3 4F RT A22WE 2007071000218 20070710 00218 NM 2007 7 10 07FDEA02321 1 20070628 A 5343 AEA70512 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 CTR LANDING GEAR, RT TRUNNION FITTING AFT HOLE FOUND CORRODED. [07-10-07] COMPLIED WITH FEDEX E.A. 1-5310-112350, CLA SSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007071000219 20070710 00219 NM 2007 7 10 07FDEA02322 1 20070628 A 5343 AEA70512 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 CTR LANDING GEAR, RT TRUNNION FITTING FWD HOLE FOUND CORRODED. [07-10-07] COMPLIED WITH FEDEX E.A. 1-5310-112350, CLA SSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007071000220 20070710 00220 EU 2007 7 10 07FDEA02323 1 20070629 A 5754 A57340088 SKIN AIRBUS 300 A300B4605R 3930308 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 CHAFING MARK ON LEADING EDGE SKIN BETWEEN RIB 28 AND WING TIP REPAIR PERFORMED BY BLEND OUT THE AREA TO SMOOTH CONTOUR IAW EA 6-5741-106450 AND RAS/BAE/1004799/2007 ISS. A 2 L 7 2 4F RT A35EU 2007071000221 20070710 00221 EU 2007 7 10 07FDEA02325 1 20070629 A 5730 A57241132201 SKIN PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 SKIN LEADING EDGE RT WING NEAR WOFX-69.0 CHAFING MARKS REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5741-106 450 AND RAS/BAE/1004799/2007 ISS.A. 2 L 7 2 4F RT A35EU 2007071000222 20070710 00222 WP 2007 7 10 07FDEA02326 1 20070629 A 5312 AEA0501502 BULKHEAD DOUG DC10 DC1010F 3022111 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 CLG WHEEL WELL AREA CRACK 8.5" LONG ON VERTICAL BULKHEAD WEB. REPAIRED CRACK IAW SRM 53-00-01 FIG 10 VOL 1. 2 L 7 3 4F A22WE 2007071000223 20070710 00223 WP 2007 7 10 07FDEA02327 1 20070629 A 5100 SKIN DOUG DC10 DC1010F 3022111 WP RT WING UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 EXISTING REPAIR RT WING O/B FLAP LOWER SKIN. REPAIRED AREA IAW SRM 57-10-00 FIG 7 VOL 1. 2 L 7 3 4F A22WE 2007071000224 20070710 00224 WP 2007 7 10 07FDEA02328 1 20070629 A 5310 BEAM DOUG DC10 DC1010F 3022111 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 FWD CARGO COMPT DOOR SILL ON BEAM FOUND SEVERE CORROSION WITH EXFOLIATION. REPAIRED IAW SRM 53-00-01 VOL 1 FIG 9 SHT 7 . 2 L 7 3 4F A22WE 2007071000225 20070710 00225 WP 2007 7 10 07FDEA02329 1 20070629 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 AFT FUSE COMPT FOUND 1 CRACK 1" LONG ON "T" VERTICAL ANGLE AFT VERTICAL BULKHEAD. REPAIRED IAW SRM 53-00-01 FIG 9 VOL 1. 2 L 7 3 4F A22WE 2007071000226 20070710 00226 WP 2007 7 10 07FDEA02330 1 20070629 A 5320 CHANNEL DOUG DC10 DC1010F 3022111 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 CTR CARGO COMPT BILGE ON "T" CAP ANGLE UNDER CHANNEL ON BLKHD FOUND CRACK 1" LONG. REPAIRED TEE IAW SRM 53-00-01 VOL 1 FIG 9 SHT 3. 2 L 7 3 4F A22WE 2007071000227 20070710 00227 WP 2007 7 10 07FDEA02331 1 20070629 A 5320 CHANNEL DOUG DC10 DC1010F 3022111 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 CTR CARGO COMPT ON CHANNEL FOUND CORROSION. REPAIRED CHANNEL IAW SRM 53-70-00 VOL 1 FIG 7 SHT 5. 2 L 7 3 4F A22WE 2007071000228 20070710 00228 WP 2007 7 10 07FDEA02332 1 20070629 A 5310 BEAM DOUG DC10 DC1010F 3022111 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 FWD CARGO COMPT DOOR SILL ON BEAM FOUND SEVERE CORROSION WITH EXFOLIATION. REPAIRED BEAM IAW SRM 53-00-01 VOL 1 FIG 9 S HT 7. 2 L 7 3 4F A22WE 2007071000229 20070710 00229 WP 2007 7 10 07FDEA02333 1 20070629 A 5347 SEAT TRACK DOUG DC10 DC1010F 3022111 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 MAIN CABIN CRACK 1' LONG ON SEAT TRACK. REPAIRED IAW SRM 53-70-00 FIG 1 VOL 1. 2 L 7 3 4F A22WE 2007071000230 20070710 00230 SO 2007 7 10 FDKA200705254 1 20070529 A 3222 STRUT EMB 145 EMB145LR 3260212 SO NLG LOW A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 FDM 6105 AVL-ATL (0600 PHX LCL). UNUSUAL NOISE FROM NOSE GEAR ON GEAR RETRACTION. MX INSPECTED GEAR AND WHEEL ASSY, N O DEFECTS. FERRIED TO MCO WHERE MX RE-SERVICED NOSE STRUT. 2 L 7 2 4T RT T00011AT 2007071000231 20070710 00231 WP 2007 7 10 07FDEA02334 1 20070629 A 5100 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 100 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 EXISTING DOUBLER EXTERNAL SKIN. REPAIRED IAW SRM 53-20-00 FIG 6 VOL 1. 2 L 7 3 4F A22WE 2007071000232 20070710 00232 WP 2007 7 10 07FDEA02335 1 20070629 A 5347 SEAT TRACK DOUG DC10 DC1010F 3022111 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 MAIN CABIN SEVERE CORROSION WITH EXFOLIATION ON SEAT TRACK. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1. 2 L 7 3 4F A22WE 2007071000233 20070710 00233 WP 2007 7 10 07FDEA02336 1 20070629 A 5753 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 LT WING T/E OUTBD FLAP ON SKIN UPPER SURFACE FOUND 3 EA CRACKS 0.50" LONG. INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 FI G 85 VOL 1. 2 L 7 3 4F A22WE 2007071000234 20070710 00234 NM 2007 7 10 FDKA200705255 1 20070530 A 2751 SWITCH DHAV DHC8 DHC8101 2809002 NM T/E FLAP DIRTY A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 802LR 205 FDM 6184 BWI-JFK (0428 PHX LCL). TAKEOFF CONFIG WARNING HORN ON TAKEOFF ROLL. MX CLEANED FLAP SWITCHES, OPS CHECKED GO OD. 2 H 7 2 4T RT A13NM 2007071000235 20070710 00235 WP 2007 7 10 07FDEA02337 1 20070629 A 5730 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 RT WING L/E CRACK .50" LONG ON EXTERNAL SKIN LOWER L/E ( SLAT TRACK NR 7). REPAIRED AREA IAW SRM 57-10-00 VOL 1FIG 68 S HT 1 & 3. 2 L 7 3 4F A22WE 2007071000236 20070710 00236 WP 2007 7 10 07FDEA02338 1 20070629 A 5347 SEAT TRACK DOUG DC10 DC1010F 3022111 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 SEAT TRACK BALL MAT AREA CRACK 4" LONG AND SEVERE CORROSION WITH EXFOLIATION ON SEAT TRACK. REPAIRED AREA IAW SRM 53-70 -00 FIG 1 VOL 1 7 SRM 53-60-00 FIG 2-11 VOL 1. 2 L 7 3 4F A22WE 2007071000237 20070710 00237 WP 2007 7 10 07FDEA02339 1 20070629 A 5330 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 EXT FUSELAGE LWR SURFACE FOUND 1 CRACK 0.25" LONG ON SKIN. REPAIRED AREA IAW SRM 53-20-00 FIG 2 VOL 1. 2 L 7 3 4F A22WE 2007071000238 20070710 00238 2007 7 10 J4PA062907002 4 20070628 A 3416 16600001 CONTROL UNIT CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO HARTZL HCJ3Y PHCJ3YF1 GL ALTIMETER FAILED E J4PA O OTHER J WARNING INDICATION CR CRUISE 1 SO 13 134AJ 545 1511 917726 FP3800B WHILE FLYING FROM KRIC TO KGGE A NR 1 ALT WARNING LIGHT COME ON. FOLLOWED PROCEDURES AND FAILED AGAIN. MADE AN UNSCHED ULED LANDING AT KRDU. TWO PASSENGERS WERE ONBOARD. NO PROBLEMS DURING LANDING. 1 L 7 1 3O 3 O NT A00009CH E3SO 5 C P36EA 2007071000240 20070710 00240 EU 2007 7 10 MALA070072 1 20070627 A 2150 COMPRESSOR SAAB SF340 340B 7860101 EU CABIN AIR CON FAILED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 450XJ 340B450 CREW REPORTED SMOKE IN THE CABIN AND FLOORBOARD IS HOT. AIRCRAFT WAS EVACUATED ON THE TAXI-WAY. SMOKE IN CABIN OBSERVE D COMING THROUGH FLOOR NEAR SEATS 3 AND 4 AFTER LEAVING THE GATE. NO INJURIES WERE REPORTED. CFR RESPONDED AND SMOKE D ISSIPATED WHEN POWER REMOVED FROM THE AIRCRAFT. FREON A/C COMPRESSOR FRIED. SUP AC INOP. 2 L 7 2 4T RT A52EU 2007071000245 20070710 00245 NM 2007 7 10 AALA20071127 1 20070618 A 2497 CIRCUIT BREAKER BOEING 767 767323 1385205 NM FLIGHT CONTROLS BURNED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 344AN 33083 SJU INFLIGHT T1647/18JUN MIA TO POS - CREW REPORTED SOUNDS OF ELECTRICAL SHORT IN OVERHEAD PANEL ALONG WITH BURNING ODOR . LEADING EDGE FLAP ASYMMETRY INDICATOR BOUNCING FROM ZERO TO 15 AND AIRSPEED INDICATOR AT 250 KNOTS WITH SPEED BREAKS OUT. LANDED SJU WITHOUT INCIDENT. FOUND RT FLT CONTROL COMPARTMENT SERVO CIRCUIT BREAKER BURNED. REPLACED CIRCUIT BR EAKER E36. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007071000246 20070710 00246 NM 2007 7 10 AALA20071128 1 20070618 A 2130 CHECK VALVE BOEING 757 757223 1384957 NM AIR CONDITIONING OBSTRUCTED A AALA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 606AA 27057 MIA INFLIGHT T2039/18JUN - DURING CLIMB CABIN ALTITUDE ALERT MESSAGE SOUNDED AND DISPLAYED. CREW MANUALLY DEPLOYED MASK S IN CABIN AND MADE AN EMERGENCY DESCENT. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. FOUND REMOVED BROKEN SECTION OF AIR STRAIGHTENED FROM CHECK VALVE AND REPLACED ALL OXYGEN GENERATORS AND MASKS. REPLACED CABIN ALTITUDE WARNING SWITCH . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071000247 20070710 00247 NM 2007 7 10 AALA20071129 1 20070619 A 2560 FLASHLIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AA 25201 SFO - EMERGENCY FLASHLIGHT AT RIGHT AFT FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT AT RIGHT AFT F LIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007071000248 20070710 00248 WP 2007 7 10 AALA20071136 1 20070620 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 241AA 49254 LGA - EMERGENCY FLASHLIGHT AT LEFT SERVICE DOOR MISSING STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT LEFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071000249 20070710 00249 NM 2007 7 10 AALA20071137 1 20070621 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 776AN 29582 ORD - EMERGENCY LIGHT AT LEFT AISLE CENTER ROW IN FIRST CLASS MISSING BULB. REPLACED BULB FOR EMERGENCY LIGHTS AT LEFT AISLE CENTER ROW IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007071000250 20070710 00250 NM 2007 7 10 AALA20071138 1 20070621 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 776AN 29582 ORD - EMERGENCY LIGHT AT LEFT AISLE CENTER ROW IN FIRST CLASS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHTS AT LEFT AISLE CENTER ROW IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007071000251 20070710 00251 NM 2007 7 10 AALA20071139 1 20070621 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 347AN 33086 SFO - EXTERIOR EMERGENCY LIGHT JUST AFT OF RIGHT TRAILING EDGE WING INOPERATIVE. RELAMPED EXTERIOR EMERGENCY LIGHT JUST AFT OF RIGHT TRAILING EDGE WING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007071000253 20070710 00253 SO 2007 7 10 FDKA200706261 1 20070605 A 5241 ROLLER EMB 145 EMB145LR 3260212 SO GALLEY DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 FDM 6083 MCO (0742 PHX LCL). GALLEY DOOR WILL NOT SHUT. MX LUBED DOOR ROLLERS AND LINKAGES, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007071000254 20070710 00254 SO 2007 7 10 FDKA200706266 1 20070608 A 2720 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO RUDDER SYS MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 829MJ 145228 FDM 6013 MTH-ATL (1146 PHX LCL) RUDDER SYSTEM 1 AND 2 INOP CAUTION MESSAGE. MX RESET THE SYSTEM AND OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007071000257 20070710 00257 SO 2007 7 10 FDKA200706265 1 20070607 A 5210 WINDOW EMB 145 EMB145LR 3260212 SO COCKPIT OUT OF ADJUST A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 840MJ 145429 FDM 6019 ATL (1655 PHX LCL). CAPTAIN'S SIDE WINDOW WON'T STAY LOCKED. MX ADJUSTED WINDOW. 2 L 7 2 4T RT T00011AT 2007071000259 20070710 00259 SO 2007 7 10 FDKA200706270 1 20070611 A 3240 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO BRAKE SYS MALFUNCTIONED A FDKA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 07 853MJ 145464 FDM 6169 MCO-FLL (1109 PHX LCL). ABORTED T/O AND RTG DUE TO INBOARD BRAKE INOP MESSAGE. MX RESET THE SYSTEM AND OPS CH ECK NORMAL. 2 L 7 2 4T RT T00011AT 2007071000260 20070710 00260 SO 2007 7 10 FDKA200706271 1 20070613 A 4930 FUEL SYS EMB 145 EMB145LR 3260212 SO APU LEAKING A FDKA O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 07 835MJ 145353 FDM 6055 TPA-TLH (0930 PHX LCL). SMELL OF FUEL DURING USE OF APU. MX FOUND LEAK COMING FROM APU AND PLACED APU ON MEL. 2 L 7 2 4T RT T00011AT 2007071000261 20070710 00261 SO 2007 7 10 FDKA200706273 1 20070614 A 2740 CONTROL UNIT EMB 145 EMB145LR 3260212 SO HORIZ STAB FAILED A FDKA O OTHER O OTHER CR CRUISE 1 SW 07 825MJ 145179 FDM 5984 FLL-MCO (0510 PHX LCL). PITCH TRIM FAIL IN FLIGHT. MX REMOVED AND REPLACED HSCU, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007071000265 20070710 00265 SO 2007 7 10 FDKA200706277 1 20070615 A 2720 15793101 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO RUDDER FAULTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 841MJ 12715 145448 FDM FLT 6134 MCO-PNS (1616 PHX LCL). RUDDER SYSTEM 1 WON'T SHUT OFF. MX REMOVED AND REPLACED RUDDER PRESSURE SWITCH. 2 L 7 2 4T RT T00011AT 2007071000266 20070710 00266 SO 2007 7 10 FDKA200706278 1 20070615 A 2740 3621001013 CONTROL UNIT EMB 145 EMB145LR 3260212 SO HORIZ STAB MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 7709 145179 FDM 6079 FLL-MCO (1658 PHX LCL). PITCH TRIM BACK UP SYSTEM INOPERATIVE. MX REMOVED AND REPLACED HSCU. 2 L 7 2 4T RT T00011AT 2007071000273 20070710 00273 EU 2007 7 10 AALA20071149 1 20070624 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80058 466 MIA - EMERGENCY LIGHT AT SEAT 6C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 6C. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F RT A35EU 2007071000164 20070710 00164 NM 2007 7 10 SWAA073208 1 20070627 A 5755 6567179 CASTING BOEING 737 7373TO 138447G NM RT SPOILER WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED C2 CHECK, FOUND RT WING NR 5 SPOILER OUTBOARD ACTUATOR CASTING WORN. REPAIRED SPOILER CASTING PER SWA EA. 2 L 7 2 4F RT A16WE 2007071000175 20070710 00175 NM 2007 7 10 SWAA073218 1 20070627 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 796SW 27889 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. R&R BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007071000178 20070710 00178 NM 2007 7 10 SWAA073214 1 20070627 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 734SA 27866 DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. R&R BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007071000184 20070710 00184 NM 2007 7 10 SWAA073207 1 20070627 A 2560 PH22300L STRIP BOEING 737 7373TO 138447G NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED C2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 1 ABC. R&R STRIP PER MM. 2 L 7 2 4F RT A16WE 2007071000186 20070710 00186 SO 2007 7 10 FDKA200705242 1 20070525 A 7830 SEAL DEPRESSOR EMB 145 EMB145LR 3260212 SO THRUST REVERSER DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 831MJ 145273 OUTBOARD SEAL DEPESSOR ON THE LEFT LOWER THRUST REVERSER IS DAMAGED. THE SEAL DEPRESSOR HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2007071000192 20070710 00192 SO 2007 7 10 FDKA200705245 1 20070525 A 5414 SKIN EMB 145 EMB145LR 3260212 SO RT COWLING CHAFED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 831MJ 145273 RIGHT ENGINE, LOWER COWLING, IS CHAFED, OUT OF LIMITS, AT THE AFT END ON THE INNER SKIN. THE DAMAGE HAS BEEN REPAIRED. 2 L 7 2 4T RT T00011AT 2007071000194 20070710 00194 SO 2007 7 10 FDKA200705247 1 20070525 A 5320 14526437001 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 831MJ 145273 RIGHT GUSSET, AT FLOOR LEVEL, BETWEEN FRAME 59 & 60 IS CORRODED OUT OF LIMITS. THE DIGITAL HAS BEEN REMOVED AND REPLACE D. 2 L 7 2 4T RT T00011AT 2007071000204 20070710 00204 SO 2007 7 10 FDKA200705249 1 20070529 A 2611 SMOKE WARNING EMB 145 EMB145LR 3260212 SO CARGO BAY MALFUNCTIONED A FDKA F ACTIVATE FIRE EXT. N FALSE WARNING NR NOT REPORTED 1 SW 07 855MJ 7739 145614 FDM 6084 MIA-MCO. ABORTED T/O DUE TO BAGGAGE SMOKE INDICATION ON EICAS. PILOT BLEW BOTTLES AND DE-BOARDED AIRCRAFT. M X INSPECTED CARGO PIT NO EVIDENCE OF SMOKE OR FIRE, AND REPLACED THE BOTTLE. 2 L 7 2 4T RT T00011AT 2007071000215 20070710 00215 SO 2007 7 10 FDKA200705253 1 20070529 A 2720 RUDDER EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FDM 6002 MCO-NAS (0410 PHX LCL). RUDDER SYSTEM 1 & 2 INOP. MX RESET SYSTEM, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007071000239 20070710 00239 SO 2007 7 10 FDKA200705256 1 20070531 A 5210 HANDLE EMB 145 EMB145LR 3260212 SO PAX DOOR UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 FDM 6049 VPS-MCO (0514 PHX LCL). MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE. MX SECURED THE INNER DOOR HANDLE, OPS CHEC K NORMAL. 2 L 7 2 4T RT T00011AT 2007071000241 20070710 00241 SO 2007 7 10 FDKA200705257 1 20070531 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR DIRTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 831MJ 145273 FDM 6000 BNA-MCO (0623 PHX LCL). MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE. MX CLEANED AND LUBED THE DOOR ROLLERS, OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007071000242 20070710 00242 NM 2007 7 10 ANCF200700015 1 20070606 A 2120 FILTER BOEING 757 7572T7 1384914 NM CABIN AIR DIRTY W ANCF A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 23 513NA 23895 DURING CLIMB CROSSING FL 300 ASC TO FL 370, HAD SMOKE COMING FROM THE PEDALS IN THE COCKPIT. CHECK LIST WAS PERFORMED A ND THEN DECIDED GOING TO MIA BECAUSE OF THE SMOKE AND ALSO THE CABIN CREW TOLD US THAT THERE WAS A LOT OF SMOKE IN THE P ASSENGER CABIN. WHEN START DESCENT THE SMOKE WENT OFF. CONFIRMED A NON IDENTIFIABLE ODOR UPON ENTERING THE CABIN AND C OCKPIT. IN ACCORDANCE WITH THE REPORTED SITUATION, PERFORMED PROCEDURES IN THE FIM 21-00-01 P.101 AS PART OF THIS TROUB LESHOOTING, IAW AM 36-11-00 /501. THE PNEUMATIC SYS CHECK SHOWED NO PROBLEMS. APU PNEUMATIC SYSTEM UNABLE TO CHECK DUE TO APU PNEUMATIC INOP (APU NEVER USED PNEUMATIC DURING FLIGHT OR DEPART) IAW AMM 21-25-02 /401. REMOVED FILTERS FOR RE 2 L 7 2 4F RT A2NM 2007071000243 20070710 00243 SO 2007 7 10 FDKA200706258 1 20070601 A 3260 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO LANDING GEAR MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 857MJ 145765 FDM 6128 FLL-RDU (1925 PHX LCL). LANDING GEAR WARNING MESSAGE AT FL 100 WITH R/A RED ON PFD'S. MX RESET SYSTEM, OPS GO OD. 2 L 7 2 4T RT T00011AT 2007071000244 20070710 00244 NM 2007 7 10 ANCF200700016 1 20070627 A 2120 DUCT BOEING 767 767259 1385136 NM LEFT LOOSE W ANCF A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 23 986AN 24835 L DUCT LEAK LGT ILLUM, EICAS MSG BLD DUCT LEAK DISPLAYED, LGT EXTINGUISH AFTER ENG BLEED AIR SUPPLY AND ISOLATION VALVES CLOSED. PERFORMED PNEUMATIC DUCT FLEXIBLE BALL JOINTS INSPECTION IN ACCORDANCE WITH AMM 36-11-01 FOUND 1 OF 5 FLEXIBLE JOINT LOOSE. RETIGHTEN IN ACCORDANCE JOB CARD. ALSO PERFORMED WING AND BODY DUCT LEAK DETECTION BITE PROCEDURE. IN A CCORDANCE WITH 26-18-00 BLOCK 6. ALL DUCTS INTEGRITY FROM ENGINES TO ISOLATED VALVE AND APU LEAK DETECTOR ELEMENTS. FO UND WITH LIMITS (LESS THAN 1 MEGOHM). RUN ENGINE AND NO FAULT NOTED. ANTI-ICING SYSTEM CHECK DUE OBVIOUS LEAKS, OK. 2 L 7 2 4F RT A1NM 2007071000252 20070710 00252 SO 2007 7 10 FDKA200706259 1 20070601 A 3150 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A FDKA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 07 829MJ 145228 FDM 6084 MIA-MCO (1323 PHX LCL). ABORTED T/O DUE TO ENGINE REFERENCE ANTI ICE DISAGREE AND NO T/O CONFIGURATION MESSAGE . MX AND THE FLT CREW PERFORMED HIGH POWER ENGINE RUNS AND ALL OPS CHECK NORMAL WITH NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2007071000255 20070710 00255 2007 7 10 FDKA200706263 4 20070606 A 3425 AHRS EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 851MJ 145572 FDM 6174 MCO (1829 PHX LCL). SPS ADVANCE MESSAGE. MX RESET AHARS. 2 L 7 2 4T RT T00011AT 2007071000256 20070710 00256 SO 2007 7 10 FDKA200706264 1 20070607 A 5610 TRACK EMB 145 EMB145LR 3260212 SO COCKPIT LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 848MJ 145530 FDM 6059 ATL (1428 PHX LCL). CAPTAIN SIDE DV WINDOW WILL NOT CLOSE. MX RE-SECURED DV WINDOW IN TRACKS & LUBED TRACKS, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007071000258 20070710 00258 SO 2007 7 10 FDKA200706267 1 20070608 A 2910 HYDRAULIC SYSTEM EMB 145 EMB145LR 3260212 SO NR 1 LOW A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 834MJ 145340 FDM 6029 MCO-DAY (1839 PHX LCL). EMERGENCY DECLARED DUE TO ENGINE 1 HYDRAULIC PUMP FAILURE. MX OPS CHECKED THE PUMP WI TH THE CREW RUNNING THE ENGINE. HYD SYSTEM 1 WAS LOW AND WAS SERVICED. NO FURTHER DEFECTS WERE NOTED AFTER THE OPS CHE CK. 2 L 7 2 4T RT T00011AT 2007071000262 20070710 00262 SO 2007 7 10 FDKA200706274 1 20070614 A 2740 TRIM SYSTEM EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 838MJ 145384 FDM 6116 PFN-MCO (1700 PHX LCL). ABORTED TAKEOFF FOR CONFIGURATION WARNING MESSAGE DUE TO PITCH TRIM WAS OUT OF THE GRE EN. CONTRACT MX COMPLIED WITH HIGH ENERGY STOP INSPECTION AND FOUND NO DEFECTS, OPS CHECKED THE STAB TRIM SYSTEM AND FO UND NO DEFECTS. 2 L 7 2 4T RT T00011AT 2007071000263 20070710 00263 SO 2007 7 10 FDKA200706275 1 20070615 A 5240 SEAL EMB 145 EMB145LR 3260212 SO GALLEY DOOR DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 854MJ 145490 FDM 6086 MCO-HSV (1432 PHX LCL). LOUD SQUEAL COMING FROM GALLEY DOOR WHEN PRESSURIZED. MX REPAIRED DOOR SEAL. 2 L 7 2 4T RT T00011AT 2007071000264 20070710 00264 SO 2007 7 10 FDKA200706276 1 20070615 A 2740 TRIM SWITCH EMB 145 EMB145LR 3260212 SO COCKPIT INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 847MJ 145517 FDM 6038 CVG-CLT (1500 PHX LCL). CAPTAIN'S PITCH TRIM SWITCH INOPERATIVE. MX REMOVED AND REPLACED TRIM SWITCH. 2 L 7 2 4T RT T00011AT 2007071000267 20070710 00267 SO 2007 7 10 FDKA200706279 1 20070615 A 2740 TRIM SWITCH EMB 145 EMB145LR 3260212 SO COCKPIT DIRTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 847MJ 145517 FDM 6035 DAY-CVG (1033 PHX LCL). CAPTAINS TRIM SWITCH IN DOWN POSITION INOP. MX CLEANED THE TRIM SWITCH, OPS CHECK GOO D. 2 L 7 2 4T RT T00011AT 2007071000268 20070710 00268 NM 2007 7 10 AALA20071140 1 20070621 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 689AA 25731 LAX - EMERGENCY LIGHT AT SEAT 3E MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 3E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071000269 20070710 00269 NM 2007 7 10 AALA20071141 1 20070622 A 3350 COVER BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 636AM 24594 MIA - EMERGENCY LIGHT SIGN AT RIGHT AFT DOOR MISSING COVER. REPLACED COVER FOR EMERGENCY LIGHT AT RIGHT AFT DOOR. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071000270 20070710 00270 NM 2007 7 10 AALA20071144 1 20070623 A 3350 LIGHT BOEING 737 737823 13844BZ NM GALLEY BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 974AN 30098 MIA - EMERGENCY LIGHT EXIT SIGN AT AFT LEFT GALLEY BROKEN. REPLACED EMERGENCY LIGHT EXIT SIGN ASSEMBLY AT AFT LEFT GALL EY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007071000271 20070710 00271 EU 2007 7 10 AALA20071145 1 20070623 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14077 612 JFK - EMERGENCY AMBER LIGHT AT OVERHEAD DOES NOT ILLUMINATE WHEN SWITCH IS IN DISARMED POSITION. RELAMPED DISARM LIGHT FOR EMERGENCY AMBER LIGHT AT OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007071000272 20070710 00272 NM 2007 7 10 AALA20071148 1 20070624 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 ORD - EMERGENCY LIGHTS AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK M33093 FOR EMERGENCY LIGHTS AT LEFT N UMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007071000274 20070710 00274 EU 2007 7 10 AALA20071150 1 20070624 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80058 466 MIA - EMERGENCY LIGHT AT SEAT 23G INOPERATIVE. REPAIRED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 23G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007071000275 20070710 00275 EU 2007 7 10 AALA20071151 1 20070624 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80058 466 MIA - EMERGENCY LIGHT AT SEATS 6G TO 18G INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEATS 6G TO 18G. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007071000277 20070710 00277 NM 2007 7 10 AALA20071152 1 20070624 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHT MISLOCATED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 395AN 29432 MIA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 21H AFT HAS RED LENS INSTEAD OF CLEAR. REPLACED RED LENS WITH CLEAR LENS FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 21H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007071000278 20070710 00278 SO 2007 7 10 FDKA200706282 1 20070615 A 2742 362209015 ACTUATOR EMB 145 EMB145LR 3260212 SO HORIZ STAB MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 8495 145179 FDM 9964 MCO-FLL (1005 PHX LCL). PITCH TRIM MAIN INOP MESSAGE. MX REMOVED AND REPLACED HSA. 2 L 7 2 4T RT T00011AT 2007071000279 20070710 00279 WP 2007 7 10 AALA20071153 1 20070624 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 563AA 49345 SFO - EMERGENCY LIGHT AT SEAT ROW 27 IS BROKEN. REPAIRED EMERGENCY LIGHT AT SEAT ROW 27. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007071000280 20070710 00280 WP 2007 7 10 AALA20071135 1 20070620 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 241AA 49254 LGA - EMERGENCY FLASHLIGHT AT AFT FLIGHT ATTENDANT SEAT HAS MISSING STRAPS. REPLACED STRAPS FOR EMERGENCY FLASHLIGHT AT AFT FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071000281 20070710 00281 EU 2007 7 10 AALA20071130 1 20070619 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7062A 474 MIA - EMERGENCY LIGHTS AT SEAT ROWS 6C TO 18C INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 6C T O 18C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007071000282 20070710 00282 SO 2007 7 10 FDKA200706281 1 20070616 A 2760 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO SPOILER SYS MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6009 ATL- GPT (0529 PHX LCL). SPOILER FAIL MESSAGE IN FLT. MX RESET THE SYSTEM AND OPS CHECK NORMAL ON THE GROUND. 2 L 7 2 4T RT T00011AT 2007071000284 20070710 00284 2007 7 10 FDKA200706284 4 20070617 A 2210 AUTOPILOT SYS EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 857MJ 145765 FDM 6203 ATL-CAE (0443 PHX LCL). AUTO PILOT FAIL MESSAGE. MX RESET THE AUTO PILOT AND OPS CHECK NORMAL ON THE GROUND. 2 L 7 2 4T RT T00011AT 2007071000286 20070710 00286 SO 2007 7 10 FDKA200706287 1 20070618 A 3350 STRIP EMB 145 EMB145LR 3260212 SO CABIN OUT OF POSITION A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM 6020 ATL-DAY (1256 PHX LCL). EMERGENCY FLOOR LIGHT STRIP AT ROW 8 THRU 11 INOP. MX REPOSITIONED AND SECURED THE FL OOR STRIPS AND OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007071000292 20070710 00292 SO 2007 7 10 FDKA200706291 1 20070621 A 2710 TRIM PANEL EMB 145 EMB145LR 3260212 SO FAULTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FDM 6201 FLL-MCO (0336 PHX LCL). ROLL TRIM INOP. MX REMOVED AND REPLACED ROLL TRIM PANEL, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007071000295 20070710 00295 SO 2007 7 10 FDKA200706292 1 20070621 A 5210 HANDLE EMB 145 EMB145LR 3260212 SO PAX DOOR OUT OF ADJUST A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 831MJ 145273 FDM 6061 RIC-MCO (0409 PHX LCL). MAIN CABIN DOOR DIFFICULT TO CLOSE. MX ADJUSTED DOOR HANDLE. 2 L 7 2 4T RT T00011AT 2007071000312 20070710 00312 SO 2007 7 10 FDKA200706294 1 20070622 A 3350 SIGN EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 847MJ 145517 FDM 6003 RIC (0400 PHX LCL). RIGHT OVERWING EMERGENCY SIGN INOP. RESET AIRCRAFT POWER, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007071000319 20070710 00319 NM 2007 7 10 FDKA200706299 1 20070623 A 2770 PLUNGER DHAV DHC8 DHC8101 2809002 NM GUSTLOCK LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 802LR 205 FDM 6285 JFK (1100 PHX LCL) CREW REPORTED A GUST LOCK INOP. MX LUBED GUSTLOCK PLUNGER OPS GOOD. 2 H 7 2 4T RT A13NM 2007071000321 20070710 00321 2007 7 10 FDKA200706300 4 20070625 A 3425 AHRS EMB 145 EMB145LR 3260212 SO OUT OF ALIGNMENT A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 857MJ 145765 FDM 6119 MCO-FLL (0335 PHX LCL). SPS ADVANCE MESSAGE. MX ALIGNED AHRS. SYSTEM CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007071000322 20070710 00322 NM 2007 7 10 QXEA200701041 1 20070628 A 2913 7G773 SWITCH DHAV DHC8 DHC8202 2809007 NM HYD PUMP MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 367PH 5361 511 MFR FLIGHT NR 2080 - NR 2 ENGINE HYDRAULIC PUMP CAUTION ON TAKEOFF BETWEEN 50-70 KTS. REPLACED NR 2 ENGINE DRIVEN PUMP LOW PRESSURE SWITCH. GROUND RAN NR 2 ENGINE. OPERATIONAL AND LEAK CHEK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071000323 20070710 00323 NM 2007 7 10 AWXA200700771 1 20070624 A 3397 CONNECTOR BOEING 737 7373G7 1384595 NM EMERGENCY LIGHT DAMAGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 307AW 24634 EMERGENCY EXIT LIGHTS ROWS 12 THRU 17 INOP. MX REPINED THE CONNECTOR. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2007071000325 20070710 00325 EA 2007 7 10 SWIA200718396 1 20070624 A 3310 LIGHT CNDAIR CL600 CL6002C10 1390015 EA 1ST OFF MAP SHORTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 774SK 10240 FIRST OFFICERS MAP LIGHT POPPED CIRCUIT BREAKER 2G7 WHEN KNOB WAS ROTATED IT. REPLACED MAP LIGHT IAW AMM 33-13-07. 2 L 7 2 4F RT A21EA 2007071000326 20070710 00326 EA 2007 7 10 SWIA200718397 1 20070622 A 5241 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GALLEY DOOR LACK OF LUBE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 947SW 7786 GALLEY DOOR WON'T OPEN FROM THE OUTSIDE. LUBRICATED DOOR HANDLE. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007071000327 20070710 00327 NM 2007 7 10 CALA0700322 1 20070626 A 5330 6545769 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70352 23590 INSPECTION FOUND A 1.5 INCH CRACK IN THE FUSELAGE SKIN AT AFT EDGE INSTRUMENT COOLING AIR DUCT OUTLET, STA 380, LBL 4, S 28L TO S28R. THE CRACK WAS STOP DRILLED AND AN EXTERNAL DOUBLER AND INTERNAL DOUBLER WERE INSTALLED IAW ECRA 5330-02894 . 2 L 7 2 4F RT A16WE 2007071000328 20070710 00328 EA 2007 7 10 SWIA200718398 1 20070619 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR LACK OF LUBE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 740SK 10196 FLIGHT ATTENDANT REPORTS THAT MAIN CABIN DOOR IS DIFFICULT TO OPEN. LUBRICATED INNER HANDLE SPRING ROLLER AND OVER CENT ER GROOVE. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007071000329 20070710 00329 EA 2007 7 10 SWIA200718399 1 20070617 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA LEFT ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 910SW 14770 14770 7566 BURNING SMELL ALONG WITH LEFT PACK FAILURE. REPLACED LEFT ACM WITH SERVICEABLE UNIT. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007071000331 20070710 00331 EA 2007 7 10 SWIA200718400 1 20070618 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA LT OVERWING STUCK A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 982CA 7168 LEFT OVERWING EMERGENCY EXIT DOOR WILL NOT OPEN. DRESSED OVERWING EXIT DOOR UPPER FORWARD AND UPPER AFT CORNERS FOR A B ETTER FIT. DOOR NOW OPENS SMOOTHLY. 2 L 7 2 4F RT A21EA 2007071000332 20070710 00332 NM 2007 7 10 CALA0700324 1 20070626 A 5320 6935352Y1 FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND A 0.65 INCH CRACK IN CLIP AT STA 616, S8L. THE CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071000333 20070710 00333 NM 2007 7 10 CALA0700325 1 20070626 A 5313 BAC1498156 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70352 23590 INSPECTION FOUND A .25 INCH CRACK IN TAIL COMPARTMENT STRINGER 21R BETWEEN STA 1040 AND 1064. A REPAIR ANGLE AND SHIM W ERE INSTALLED IAW SRM 53-00-00. 2 L 7 2 4F RT A16WE 2007071000334 20070710 00334 EA 2007 7 10 SWIA200718401 1 20070616 A 3350 SIGN CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT INOPERATIVE A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 771SK 10244 RED AND WHITE INDICATOR LIGHTS ON AFT SIDE OF CEILING EXIT SIGN WILL NOT ILLUMINATE. REPLACED AFT SIDE OF CEILING EMERG ENCY SIGN ASSEMBLY IAW CRJ 700 MM 33-00-00. 2 L 7 2 4F RT A21EA 2007071000336 20070710 00336 EA 2007 7 10 SWIA200718402 1 20070623 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002C10 1390015 EA ILLUMINATED A SWIA C ABORTED TAKEOFF B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 NM 07 613SK 10038 "SMOKE FWD TOILET" WARNING MESSAGE DURING TAKEOFF ROLL. ABORTED TAKEOFF. REPLACED FORWARD LAV FAN IAW CRJ 700 MM 21-23 -93. OPS CHECK GOOD, P/N 66670-95028-3, S/N OFF 00784. 2 L 7 2 4F RT A21EA 2007071000337 20070710 00337 NM 2007 7 10 CALA0700327 1 20070627 A 5315 BAC1506210 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND FLOORBEAM CORRODED ON UPPER AND LOWER SURFACE AT STA 986.5, LBL 43. THE CORRODED T-CHORD SECTION OF BE AM WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071000338 20070710 00338 NM 2007 7 10 CALA0700328 1 20070620 A 5542 SKIN 173N210113 BOEING 757 757224 1384958 NM RUDDER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 57111 0111 27301 THE RUDDER TRAILING EDGE SKIN WAS FOUND DELAMINATED OVER AN AREA OF APPROXIMATELY 0.50 INCH BY 1.9 INCH AT RUDDER STA 17 5. THE DELAMINATION WENT THROUGH THE ENTIRE THICKNESS OF THE LT RUDDER PANEL AND APPROXIMATELY 20% OF THE THICKNESS OF THE RT RUDDER PANEL. THE RUDDER SKIN WAS REPAIRED IAW ECRA 5540-01236. 2 L 7 2 4F RT A2NM 2007071000339 20070710 00339 WP 2007 7 10 ABXA070205 1 20070626 A 3260 BULB DOUG DC9 DC932 3022066 WP COCKPIT INOPERATIVE A ABXA O OTHER O OTHER AP APPROACH 1 GL 23 985AX 47522 NO NOSE GEAR INDICATION IN FLIGHT. FOUND NOSE GEAR BULBS MUSHROOMED AT TIPS AND BULBS INOPERATIVE. RELAMPED AS REQUIRE D. INSPECTED WIRE BUNDLE AT NOSE DOWNLOCK SWITCH, NO DISCREPANCIES NOTED. 2 L 7 2 4F A6WE 2007071000341 20070710 00341 SO 2007 7 10 SWIA200718403 1 20070623 A 3150 80055711 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION UK UNKNOWN 1 NM 07 565SW 10984 10984 120340 FIREBELL, ACCOMPANIED WITH INTERMITTENT MAP LIGHTS. REPLACED AURAL WARNING UNIT IAW MM 31-53-02, OPS CK GOOD. 2 L 7 2 4T RT A31SO 2007071000342 20070710 00342 EA 2007 7 10 SWIA200718404 1 20070624 A 5610 NP13932211 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 770SK 10243 LEFT SIDE WINDOW IS CRACKED. REPLACED LEFT SIDE WINDOW IAW MM 56-12-01. 2 L 7 2 4F RT A21EA 2007071000343 20070710 00343 EA 2007 7 10 SWIA200718405 1 20070622 A 3520 OXYGEN MASK CNDAIR CL600 CL6002B19 1900309 EA LAVATORY UNWANTED DEPLOY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 408SW 7055 O2 MASK DEPLOYED IN LAVATORY. REPACKED LAVATORY OXYGEN MASKS IAW 35-21-09. 2 L 7 2 4F RT A21EA 2007071000344 20070710 00344 EA 2007 7 10 SWIA200718406 1 20070621 A 3520 OXYGEN MASK CNDAIR CL600 CL6002C10 1390015 EA LAVATORY UNWANTED DEPLOY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 614SK 10051 O2 MASKS IN FORWARD LAV HAVE DEPLOYED. RESTOWED O2 MASK IN FORWARD LAV. 2 L 7 2 4F RT A21EA 2007071000345 20070710 00345 EA 2007 7 10 SWIA200718407 1 20070619 A 5320 STRIKER CNDAIR CL600 CL6002B19 1900309 EA DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 935SW AFT STRIKER SEAL IS DAMAGED. REPAIRED AFT STRIKER IAW BOMBARDIER REO 601R-53-22-003 TYPE III REPAIR. 2 L 7 2 4F RT A21EA 2007071000346 20070710 00346 EA 2007 7 10 SWIA200718408 1 20070624 A 3397 RELAY CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 772SK 10235 SOME EMERGENCY LIGHTS ARE COMING ON WHEN SWITCH IS IN THE ARMED POSITION. REPLACED RELAY K135. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007071000347 20070710 00347 NM 2007 7 10 NWAA072316716 1 20070625 A 5330 SKIN BOEING 747 747251F 1384898 NM BS 560 S34-35R DENTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 616US 21120 DURING "L" CHECK, FOUND DENT IN FUSELAGE SKIN AT BS 560 S34R TO S35R. REPAIRED PER EA 67-209722. 2 L 7 4 4F A20WE 2007071000349 20070710 00349 EU 2007 7 10 YENA2007059 1 20070622 A 2797 19019566401 WIRE HARNESS EMB ERJ190 ERJ190100IGW 3260408 EU L/E SLAT DEFECTIVE A YENA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 197JB 6565 19000020 SLAT FAIL AFTER TAKEOFF. FLT 1094, CMH-JFK RETURNED FOR LANDING AT CMH. REPLACED RIGHT SLAT 2/3 & 3/4 SKEW SENSOR HARN ESSES PER AMM 27-83-07-400-801. CLEARED SF-ACE INHIBITS. NO EICAS MSG PRESENT. OPS CHECK OF SLATS IS NORMAL PER AMM 2 7-710-801. OK FOR RETURN TO SERVICE. 2 L 7 2 4F RT A57NM 2007071000350 20070710 00350 EU 2007 7 10 YENA2007060 1 20070624 A 2913 5116403 PUMP EMB ERJ190 ERJ190100IGW 3260408 EU HYDRAULIC SYS LEAKING A YENA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 EA 15 206JB 2599 1448 19000025 HYD SYSTEM NR 1 QTY DEPLETED TO 2% IN FLIGHT. SERVICED SYSTEM. PERFORMED LEAK CHECK, FOUND NR 1 ENGINE DRIVEN PUMP LEA KING BEYOND LIMITS. REMOVED AND REPLACED AS PER AMM 29-11-01. PERFORMED OPS AND LEAK CHECK, ALL NORMAL. 2 L 7 2 4F RT A57NM 2007071000351 20070710 00351 NM 2007 7 10 HNAA070128 1 20070628 A 5730 DOUBLER DHAV DHC8 DHC8102 2809003 NM LT WING CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 912HA 040 LEFT AUX BOOST PUMP (FUEL) WING DOUBLER FOUND CORRODED INSIDE AND OUTSIDE FUEL TANK. LEFT AUX BOOST PUMP (FUEL) WING DO UBLER INSIDE AND OUTSIDE OF FUEL TANK CORROSION REMOVED IAW RD8-57-3679 (MATERIAL REMAINING .415") S/B 8-57-28 PREVIOUSL Y COMPLIED WITH. HFEC AND DISBOND C/O NO DEFECTS FOUND. 2 H 7 2 4T RT A13NM 2007071000352 20070710 00352 NM 2007 7 10 KCSA071197 1 20070628 A 3350 LIGHT BOEING 747 747212B 1384886 NM EXTERIOR INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 703CK 21939 EMERGENCY SLIDE LIGHT RIGHT SIDE OF FUSELAGE INOP. 2 L 7 4 4F A20WE 2007071000353 20070710 00353 NM 2007 7 10 KCSA071198 1 20070628 A 3350 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 703CK 21939 EMERGENCY LIGHT AFT UPPER DECK INOP. 2 L 7 4 4F A20WE 2007071000354 20070710 00354 NM 2007 7 10 QXEA200701070 1 20070627 A 6120 699018002 CONTROLLER BOMBDR DHC8 DHC8402 1390042 NM NR 1 MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 429QX 5 5 4161 SEA FLIGHT NR 2322: POWER PLANT MESSAGE DISPLAYED ON ED AFTER BRINGING CONDITION LEVERS FROM START FEATHER TO MAX. MAIN TENANCE INTERROGATED CDS AND FOUND FAULT CODE 242A&B ON THE NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE TQ B PROBE (P N 3047252-01) PER FIM 61-20-05 PG 227-230, AMM Q400 TASK 77-11-06-000-801 AND 77-11-06-400-801. THIS DID NOT FIX THE FA ULT. REMOVED AND REPLACED NR 1 ENGINE PEC PER Q400 FIM 61-20-05 PG 227-230 AND Q400 AMM TASKS 61-20-36-000-801 AND 61-2 0-36-400-801. FAULT CLEARED AND DID NOT REOCCUR. PERFORMED POWER ASSURANCE CHECK OF THE NR 1 ENGINE IAW Q400 MTC NR 67 0005. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071000355 20070710 00355 NM 2007 7 10 QXEA200701071 1 20070627 A 3297 471509 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM NLG DAMAGED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 403QX 2375 2375 4037 SEA FLIGHT NR 2396: TURNING ONTO THE RUNWAY, NWS FAIL, WEIGHT ON WHEELS AND IAS FAIL MESSAGES. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REMOVED NLG ELECTRICAL HARNESS NR 1 IAW AMM 32-11, TR NR 32-202. INSTALLED SERVICEABLE NLG ELECTRIC AL HARNESS NR 1 IAW AMM 32-21-11, TR NR 32-203. NO IAS FAIL MESSAGE. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071000356 20070710 00356 EA 2007 7 10 VNAA0706002 1 20070605 A 3244 711772 TIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NLG FAILED A VNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 05 228PS 18 7897 CREW REPORTED ON TAKEOFF ROLL THE RIGHT HAND NOSE TIRE WENT FLAT. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED BOTH NOSE TIRES IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 32-42-01 . MAINTENANCE FOUND DAMAGE TO THE NOSE GEAR DOOR AND COMPLIED WITH TEMP REPAIR PER REO 601R-52-81-132. MAINTENANCE ALS O FOUND NUMEROUS DENTS ON FUSELAGE AND COMPLIED WITH TEMP REPAIR PER REO 601R-53-11-1192. AIRCRAFT WAS RELEASED FOR SER VICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007071000361 20070710 00361 EA 2007 7 10 VNAA0706014 1 20070621 A 2910 16480101 MANIFOLD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HYDRAULIC SYS FAILED A VNAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 05 216PS 5795 7882 CREW REPORTED ON APPROACH A NOSE WHEEL STEERING INOP MESSAGE WAS DISPLAYED. CREW AS A PRECAUTION DECLARED AN EMERGENCY. CREW LANDED IN CLT WITHOUT INCIDENT AND WAS TOWED FROM THE TAXIWAY TO THE GATE. MAINTENANCE INSPECTED THE NOSE LANDIN G GEAR ASSEMBLY. MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC MANIFOLD IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MA NUAL. OPERATIONAL CHECKS GOOD AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007071000367 20070710 00367 EA 2007 7 10 VNAA0706012 1 20070619 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE DAMAGED A VNAA O OTHER O OTHER DE DESCENT 1 GL 05 250PS 7929 CREW REPORTED ON DESCENT A LIGHTNING STRIKE. MAINTENANCE COMPLIED WITH AN EN ROUTE AND DETAILED LIGHTNING STRIKE INSPEC TION. MAINTENANCE INSPECTED AND FOUND EVIDENCE OF A STRIKE TO THE LOWER RIGHT FORWARD FUSELAGE. MAINTENANCE FOUND ALL DAMAGE TO BE WITHIN LIMITS IN ACCORDANCE WITH THE STRUCTURE REPAIR MANUAL 53-00-31. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007071000368 20070710 00368 NM 2007 7 10 NWA07225630 1 20070621 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK TEST, FOUND UPPER DECK RT EMERGENCY DOOR POWER SUPPLY AND BATTERY PACK INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED POWER SUPPLY AND BATTERY PACK PER AMM 33-51-04. SECURED AND FUNCTIONAL TEST OK. 2 L 7 4 4F RT A20WE 2007071000369 20070710 00369 EA 2007 7 10 VNAA0706011 1 20070620 A 2750 860D10018 ECU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE T/E FLAP FAILED A VNAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 05 249PS 5868 7926 CREW REPORTED ON APPROACH A FLAPS FAIL CAS MESSAGE AT 45 DEGREES. MAINTENANCE INSPECTED AND FOUND FECU BITE CHECK NOT W ORKING AND RIGHT HAND BPSU RIG INDICATION ERRATIC. MAINTENANCE REMOVED AND REPLACED THE FECU IN ACCORDANCE WITH THE MAI NTENANCE MANUAL 27-51-05-000/400-801. OPERATIONAL CHECKS GOOD AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007071000370 20070710 00370 NM 2007 7 10 NWAA072283146 1 20070626 A 3350 CHARGER AIRBUS A319 A319114 3930350 NM BATTERY PACK MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 346NB 9943 56 1796 CHARGER IS OVERCHARGING LEFT OVERWING EMERGENCY EXIT EPSU BATTERIES. REPLACED LEFT OVERWING EPSU, CHECKS OK. 2 L 7 2 4F RT A28NM 2007071000371 20070710 00371 NM 2007 7 10 DLM88070835 1 20070630 A 3297 WIRE DOUG MD88 MD88 3023688 NM DOWNLOCK SENSOR DAMAGED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 915DL 49546 ON DEPARTURE AFTER GEAR HANDLE UP RED LIGHT ILLUMINATED IN NOSE GEAR LANDING GEAR LIGHT. ALL OTHERS INCLUDING GEAR DOOR LIGHTS WERE EXTINGUISHED. RAN QRH PROCEDURE GEAR DOWN THREE GREEN ILLUMINATED. NOSE GEAR DOWN LIGHT ILLUMINATED WITHI N ONE SEC OF GEAR HANDLE DOWN. MTC IN PROGRESS ON LANDING GEAR SYSTEM. FOUND WIRING BAD ON DOWN LOCK SENSOR. REPAIRED WIRE WITH RAY SPLICE CYCLED NOSE GEAR SEVERAL TIMES ALL INDICATION GOOD. 2 L 7 2 4F RT A6WE 2007071000372 20070710 00372 EA 2007 7 10 VNAA0706010 1 20070620 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE WING MALFUNCTIONED A VNAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 05 249PS 7926 CREW REPORTED ON APPROACH A FLAPS FAIL CAS MESSAGE AT 20 DEGREES. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDEN T. MAINTENANCE INSPECTED AND PERFORMED A RESET OF THE SDU. MAINTENANCE INSPECTED FLAP LEFT HAND AND RIGHT HAND, NO SKE W NOTED IN ACCORDANCE WITH THE MAINTENANCE MANUAL 27-51-15. MAINTENANCE PERFORMED OPS CHECK OF THE FLAPS IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 27-54-00-866-801 AND 27-54-00-866-802. OPERATIONAL CHECKS GOOD AT THIS TIME. AIRC RAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007071000374 20070710 00374 2007 7 10 VNAA0706006 4 20070613 A 3425 AHRS CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE MALFUNCTIONED A VNAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 05 247JS 7922 CREW REPORTED DURING CRUISE THE LOSS OF THE FIRST OFFICERS ATTITUDE AND HEADING INDICATIONS. CREW ELECTED TO DIVERT TO GSO AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CYCLED THE AHRS 2 CIRCUIT BREAKERS. MAINTENANCE ALSO COMPLI ED WITH THE FUNCTIONAL AND OPERATIONS CHECK IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 34-21-00-720-801 AND 34-2 1-01-946-021. SYSTEM OPS CHECKS NORMAL AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007071000379 20070710 00379 NM 2007 7 10 ABXA070206 1 20070628 A 7797 CONNECTOR BOEING 767 767232 1385132 NM GE CF680 CF680A2 NE VIBRATION SENSOR LOOSE A ABXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 23 742AX 79 22217 580163 DURING CRUISE, RIGHT ENGINE VIBRATION EXCEEDED INDICATION, BECAME INTERMITTENT. MADE PRECAUTIONARY LANDING AT KIX. FOU ND N1 VIBRATION SENSOR CONNECTOR LOOSE, TIGHTENED CONNECTOR. PERFORMED FIM PROCEDURE 77-31-00. REMOVED AND REPLACED RI GHT AVM. BITE CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E13NE 2007071000381 20070710 00381 NM 2007 7 10 CALA0700330 1 20070629 A 5312 6545409 PRESSURE PANEL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND A 1.5 INCH CRACK IN RT WHEEL WELL CEILING PRESSURE DECK ABOVE O/B END OF GROUND SPOILER CONTROL VALVE, STA 664, RBL 40. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-60-51 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007071000383 20070710 00383 NM 2007 7 10 CALA0700331 1 20070630 A 5310 6520722U70 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD CARGO DOOR CUTOUT FORWARD FRAME AT LOWER STOP FITTING, STA 440. THE FORWAR D FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071000391 20070710 00391 NM 2007 7 10 CALA0700335 1 20070701 A 5313 6549914545 FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND STRINGER 27R END FITTING CORRODED IN BOLT HOLES AT STA 1016. THE END FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071000394 20070710 00394 NM 2007 7 10 2007UALA02231 1 20070625 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY LIGHTS INOP AT SEAT 4J FWD. REPLACED LIGHT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071000397 20070710 00397 NM 2007 7 10 2007UALA02232 1 20070624 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INTERMITTENT A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 174UA 24381 AFT GALLEY CEILING FLICKER ON AND OFF. RELAMPED AS REQUIRED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071000402 20070710 00402 NM 2007 7 10 2007UALA02233 1 20070623 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY LIGHT INOP LEFT OVERWING FAIRING 2ND ASSY FROM AFT, AFT BULB. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071000405 20070710 00405 NM 2007 7 10 2007UALA02236 1 20070623 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY LIGHT INOP DOOR 2R CEILING ENTRY. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071000407 20070710 00407 NM 2007 7 10 2007UALA02238 1 20070625 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY LIGHTS INOP AT SEATS 35ABC & 40 HJK. RELAMPED EMERGENCY LIGHTS. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071000411 20070710 00411 NM 2007 7 10 2007UALA02240 1 20070624 A 3350 9F19948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY LIGHTS INOP RIGHT OVERWING BODY FAIRING, 2 AFT ASSY'S. REPLACED LIGHT ASSY 2ND FROM AFT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071000417 20070710 00417 EU 2007 7 10 2007UALA02254 1 20070626 A 3350 321431 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 486UA 1620 CABIN EMERGENCY LIGHT TEST FAILS WITH -EPSU BATTERY EMER L- MSG. REPLACED EPSU BATTERY AT LEFT OVERWING EXIT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071000420 20070710 00420 NM 2007 7 10 2007UALA02274 1 20070627 A 3350 1619 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 326UA 23958 LEFT SIDE EXTERIOR EMERGENCY OVERWING LIGHT INOP. RELAMPED, TEST NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071000433 20070710 00433 NM 2007 7 10 2007UALA02289 1 20070628 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY LIGHT INOP DOOR 4 GALLEY CEILING. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071000436 20070710 00436 EU 2007 7 10 2007UALA02297 1 20070629 A 5320 STRUCTURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 428UA 523 WATER WASTE VENT OUTLET AT RIGHT FUSELAGE BETWEEN FR 68 & 69 HAS HEAVY CORROSION. MAJOR REPAIR ACCOMPLISHED: REMOVED D AMAGE. FABRICATED & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071000437 20070710 00437 EU 2007 7 10 2007UALA02298 1 20070628 A 3350 32145410321431 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 432UA 587 EEL TEST FAILS LEFT OVERWING POWER SUPPLY. REPLACED POWER SUPPLY & BATTERY PACK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112900050 20071129 00050 NM 2007 11 29 2007UALA04770 1 20071120 A 5754 SLAT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 3 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 577UA 26693 NR 3 OUTBOARD L/E SLAT HAS DAMAGE. NR 3 SLAT WAS DAMAGED AND REMOVED AND SENT TO SHOP FOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071000439 20070710 00439 NM 2007 7 10 2007UALA02301 1 20070628 A 5310 TORQUE TUBE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT ENTRY DOOR EXCESS PLAY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 AFT ENTERY DOOR UPPER AND LOWER LATCH TORQUE TUBE HAS EXCESSIVE LATERAL PLAY. ADDED SHIMS TO UPPER & LOWER TORQUE TUBES . OPS CHECKED OKAY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071000440 20070710 00440 NM 2007 7 10 2007UALA02302 1 20070628 A 5240 TORQUE TUBE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU GALLEY DOOR OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 AFT GALLEY DOOR FWD UPPER LATCH TORQUE TUBE END FITTING OUTER SURFACE IS CONTACTING ROLLER GUIDE FITTING. ADJUSTED SHIM S BEHIND UPPER LATCH TORQUE TUBE TO CLEAR FITTING. OPS CHECKED OKAY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071000441 20070710 00441 EU 2007 7 10 CPCP20070046 1 20070511 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 260AE 263 RT SEAT TRACK BETWEEN FRAME 39 AND FRAME 40 IS CORRODED. RT SEAT TRACK BETWEEN FRAME 39 AND FRAME 40 REPLACED AS PER SR M 51-25-04. 2 H 7 2 4T RT A53EU 2007071000442 20070710 00442 EU 2007 7 10 CPCP20070047 1 20070511 A 5320 THRESHOLD AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 260AE 263 RT THRESHOLD BETWEEN FRAME 36 AND FRAME 39 IS CORRODED. RT THRESHOLD BETWEEN FRAME 36 AND FRAME 39 REPLACED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007071000443 20070710 00443 NM 2007 7 10 07FDEA02314 1 20070628 A 5754 652165337 SKIN BOEING 727 727227 1384078 NM KRUGER FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 LT WING, PNL JUST AFT OF NR 2 KRUGER FLAP IS DELAMED AROUND VENT. REPAIRED DELAMED ON LT WING PNL JUST AFT OF NR 2 KRU GER FLAP REF SRM 51-40-9 PG 9 PARA 7. 2 L 7 3 4F A3WE 2007071000445 20070710 00445 EU 2007 7 10 07FDEA02324 1 20070629 A 5730 A57241132201 SKIN PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 SKIN LEADING EDGE LT WING NEAR WOFX-69.0 CHAFING MARKS REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5741-106 450 AND RAS/BAE/1004799/2007 ISS A. 2 L 7 2 4F RT A35EU 2007071000446 20070710 00446 NM 2007 7 10 07FDEA02346 1 20070630 A 5720 652165827 CHANNEL BOEING 727 727227 1384078 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 LEFT WING FIXED TRAILING PANEL SUPPORT BRACKETS, ARE CRACKED AT SUPPORT ROD. SUPPORT ROD ATTACHS TO, TWO PANELS LOCATED JUST INBD OF THE NR 2 SPOILER. REMOVED, LOCATED, DRILLED AND INSTALLED Z BRACKET LT WING T/E PANEL SUPPORT BRACKET INB D OF NR 2 SPOILER PER SRM 51-30-2. 2 L 7 3 4F A3WE 2007071000447 20070710 00447 NM 2007 7 10 07FDEA02347 1 20070630 A 5315 652082756 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 ON AGING A/C INSP, FOUND EXISTING REPAIR LOCATED AT BS 460 FLOORBEAM UPPER CHORD RBL 33" TO 49" DOES NOT CONFORM TO S RM. REMOVED EXISTING REPAIR ANGLES IAW SRM 51-30-2 FABRICATED NEW REPAIR ANGLE FOR BS 460 FLOORBEAM UPPER CHORD RBL 33" TO 48", IAW FED EX DWG SR27-53-034. SENT OUT REPAIR ANGLES FOR HEAT TREAT AND CAD PLATE AND INSTALLED REPAIR REF SR27- 53-034 REPAIR NR 1. 2 L 7 3 4F RT A3WE 2007071000448 20070710 00448 NM 2007 7 10 2007UALA02304 1 20070628 A 2710 ACTUATOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LT AILERON MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 104UA 26902 LEFT AILERON LOCKOUT ACTUATOR -NO RESPONSE- (SRM-R) MESSAGE 27321 HARD FAULT LAST FOUR LEGS. [07-24-07] REPLACED LT AILERON LOCK OUT ACTUATOR. COMPLETED INSTALLATION & TEST PER MM 27-11-16. ALL TESTS NORMAL PER PROCEDURE NR 4. AIRCRAFT OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071000450 20070710 00450 NM 2007 7 10 07FDEA02348 1 20070701 A 2120 356632255 ELEMENT DOUG MD11 MD11F 3023600 NM CABIN AIR FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 617FE 48748 AT SFS DURING PRE-FLIGHT, GOT AIR SYSTEM TEST FAIL. TRIED SECOND TIME WITH SAME ALERT. CALLED MX, THEY TEST AIR SYSTEM AND GAVE OK TO GO. UPON DEPARTURE DURING CLIMB, GOT AVIONICS FAN OVRD PASSING FL230 FOLLOWED SHORTLY BY LEVEL 2 AIR MA NF 1 FAIL. FOLLOWED QRH AND RETURNED TO SFS. REMOVED AND REPLACED MANIFOLD FAILURE SENSING ELEMENT D1-44C, P/N 35663-2 -255, PER MM 36-23-07-4. SYSTEM TEST PASSED AS PER MM 36-23-07-5, A/C OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2007071000451 20070710 00451 EU 2007 7 10 07FDEA02349 1 20070702 A 5414 A54611752 PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 CRACKED HOLE (ABOUT 8MM ) AT RIB 8A PYLON NR 1, INBOARD SIDE. REPAIR PERFORMED BY DOUBLER INSTALLATION IAW SRM 54-51-31 PB 200, APPROVED BY EA 6-5451-106447 A. 2 L 7 2 4F RT A35EU 2007071000452 20070710 00452 NM 2007 7 10 2007UALA02306 1 20070629 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY LIGHT ROW 43ABC INOPERATIVE. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071000453 20070710 00453 NM 2007 7 10 2007UALA02307 1 20070629 A 3397 7945243 CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY LIGHT ROW 52 RIGHT INOPERATIVE. REPLACED CABLE FROM FEEDER TO EMERGENCY LIGHT ON ROW 52 RIGHT. OP CHECK NORM AL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071000457 20070710 00457 2007 7 10 2007UALA02312 4 20070629 A 3400 PROBE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TAT OBSTRUCTED A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 563UA 26665 RTFL DUE TO RESTRICTED ENGINE THRUST. [07-31-07] ON CLIMBOUT ENGINES PRODUCED ENOUGH THRUST FOR AN APPROX 1000' PER-M IN CLIMB RATE. TRUE AIR TEMP SHOWING +48C ON UPPER EICAS. SHOULD BE ABOUT 12 DEG-C. TAT PROBE HAD A BIRD STRIKE DURING TAKEOFF AND THE NORMALLY ASPERATED PROBE WAS CLOGGED WITH BIRD REMAINS CAUSING INACCURATE TAT READINGS. REPLACED TAT PR OBE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071000461 20070710 00461 NM 2007 7 10 2007UALA02316 1 20070628 A 2421 GENERATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE FAILED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 545UA 25323 LEFT GENERATOR FAILED IN FLIGHT. COULD NOT RESET. [08-08-07] LT IDG REMOVED FOR INSPECTION AND TROUBLESHOOTING. ID G REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071000462 20070710 00462 NM 2007 7 10 SWAA073228 1 20070628 A 3350 101331 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 421LV 32452 RT OVERWING EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007071000465 20070710 00465 NM 2007 7 10 SWAA073226 1 20070627 A 3244 26066712 TIRE BOEING 737 7373G7 1384595 NM RT MLG SEPARATED A SWAA K NONE O OTHER NR NOT REPORTED 1 SW 29 691WN 23781 NR 1 MAIN TIRE TREAD SEPARATED. R&R NR 1 MAIN WHEEL AND TIRE ASSY PER MM. R&R NR 4 GROUND SPOILER AND LT INBOARD FWD F LAP PER MM. 2 L 7 2 4F RT A16WE 2007071000467 20070710 00467 NM 2007 7 10 SWAA073248 1 20070628 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 442WN 32459 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 22 ABC. R&R EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2007071000468 20070710 00468 NM 2007 7 10 SWAA073230 1 20070628 A 3350 417A5701 COVER BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED SPV CHECK, FOUND RT MID CABIN EEPLS COVER CRACKED. R&R COVER PER MM. 2 L 7 2 4F RT A16WE 2007071000469 20070710 00469 NM 2007 7 10 SWAA073229 1 20070628 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 434WN 32454 EEPLS COVER CRACKED AT ROW 1 ABC. R&R COVER PER MM. 2 L 7 2 4F RT A16WE 2007071000471 20070710 00471 2007 7 10 SWAA073256 4 20070628 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 789SW 29816 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071000473 20070710 00473 NM 2007 7 10 SWAA073242 1 20070628 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 755, STR 21R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007071000474 20070710 00474 NM 2007 7 10 SWAA073232 1 20070628 A 5315 6545833 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CRACKED AT BS 328, LBL 27. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007071000478 20070710 00478 NM 2007 7 10 2007UALA02318 1 20070629 A 2425 WARNING LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT INTERMITTENT A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 583UA 26705 NR 2 ENG GENERATOR DRIVE LIGHT COMES ON INTERMITTANTLY. DISCONNECTED GENERATOR IN FLIGHT. [08-08-07] SERVICED IDG T OOK 57 PUMPS TO FILL. RAN ENGINE AND FOUND IDG LEAKING AT A MATTING SURFACE BEHIND WHERE ELECT FEEDER WIRES CONNECT. R EPLACED IDG. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071000479 20070710 00479 NM 2007 7 10 2007UALA02319 1 20070630 A 2421 GENERATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE MALFUNCTIONED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 506UA 24627 LEFT GENERATOR OFF, APU DID NOT START AT 30,000 FT, DESCENDED TO 20,000 FT, APU STARTED NORMALLY. [08-08-07] REPLACE D IDG FOR INSPECTION AND TROUBLESHOOTING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071000480 20070710 00480 NM 2007 7 10 2007UALA02320 1 20070630 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 MED 2L IS DAMAGED AT UPPER HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071100001 20070711 00001 CE 2007 7 11 GUUA06020701 1 20070602 A 3260 H111541 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG SHORTED A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 29 16540 UE172 FLIGHT: 9282, DURING APPROACH WHEN LANDING GEAR SELECTED DOWN NO (3) GREEN INDICATION CIRCUIT BREAKER POPPED RESET BREAK ER AND ALL INDICATIONS OPERATED NORMALLY. REPLACED RIGHT MAIN LANDING GEAR UPLOCK SWITCH. LANDING GEAR OPERATIONAL CHEC K NORMAL. TEST FLIGHT SATISFACTORY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007071100002 20070711 00002 CE 2007 7 11 DXTA200702276 1 20070616 A 3260 INDICATOR CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE RT MLG INOPERATIVE E DXTA O OTHER P NO WARNING INDICATION LD LANDING 1 GL 07 683QS 5605643 RT MLG INDICATOR LIGHT DID NOT ILLUMINATE WHEN GEAR LOWERED. PULLED T-HANDLE, BUT DID NOT BLOW GEAR DOWN. [07-11-07] R EMOVED AND REPLACED RIGHT MAIN GEAR BULB IAW CE560XLS M/M 32-61-00 BULBS FROM AIRCRAFT F.A.K. C. REW RESTORED HANDLE. VE RIFIED BLOW DOWN BOTTLE NOT BLOWN. SAFETY INTACT. NO FURTHER ACTION REQUIRED. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007071100004 20070711 00004 NM 2007 7 11 2007UALA02323 1 20070630 A 2612 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FIRE WARNING SYS FAULTY A UALA O OTHER L NO TEST IN INSP/MAINT 1 WP 29 565UA 26669 CARGO FIRE SYSTEM FAIL LIGHT ON PED SEEMS INCORRECT. [08-08-07] REPLACED KORRY SWITCH IN FIRE TEST PANEL, AND OPS CH ECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071100005 20070711 00005 SO 2007 7 11 C2XA07RI048 1 20070618 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN LOOSE A C2XA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 27 13955 145075 FLT 2796 - SDF - CREW REPORTED ELECTRICAL FIRE OVERHEAD BETWEEN SEATS 1A AND 2A. VISUAL CONFIRMATION OF SMOKE (NOT COND ENSATION) BY FLIGHT ATTENDANT AND PAX ACCOMPANIED BY ACRID ELECTRICAL SMELL. MX PERFORMED INSPECTION AND FOUND NO EVIDE NCE OF FIRE. FOUND BULB LOOSE FROM CONNECTORS. MX REINSTALLED BULB AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007071100006 20070711 00006 SO 2007 7 11 C2XA07IA146 1 20070619 A 2150 14525793401 NOZZLE EMB 145 EMB145EP 3260221 SO LT A/C PACK CLOGGED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14945 145049 FLIGHT 2553 - CREW REPORTED A BURNING SMELL IN THE COCKPIT AND CABIN WHEN THE AIR CONDITIONING PACKS WERE SELECTED TO MA NUAL. MAINTENANCE CLEANED THE LEFT AIR CONDITIONING PACK SPRAY NOZZLE, OPERATIONALLY CHECKED THE SYSTEM AND CLEARED THE DISCREPANCY. 2 L 7 2 4F RT T00011AT 2007071100007 20070711 00007 SO 2007 7 11 C2XA07IA147 1 20070622 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 16963 145116 FLIGHT 2431 - THE FLIGHT CREW NOTED A STRONG FUEL SMELL DURING THE LATE STAGES OF TAKEOFF. MAINTENANCE PERFORMED INSPEC TIONS OF THE ENGINES AND AUXILIARY POWER UNIT. HIGH POWER ENGINE RUNS AND OPERATIONAL TESTS OF THE BLEED AIR SYSTEM WER E PERFORMED AND THE DISCREPANCY COULD NOT BE DUPLICATED. THE DISCREPANCY WAS CLEARED AND THE AIRCRAFT RETURNED TO SERVI CE. 2 L 7 2 4T RT T00011AT 2007071100008 20070711 00008 SO 2007 7 11 C2XA07IA148 1 20070623 A 3231 22250100003 SOLENOID VALVE EMB 145 EMB145XR 3260214 SO NLG LEAKING A C2XA K NONE E VIBRATION/BUFFET CL CLIMB 1 SW 27 24128 12173 12173 145700 AFTER TAKEOFF, THE CREW THOUGHT THAT THE NOSE LANDING GEAR DOORS MAY NOT HAVE SHUT COMPLETELY. THE AIRCRAFT LANDED AT I AH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR DOOR SOLENOID VALVE. THE NOSE LANDING GEAR DOORS WERE OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED. 2 L 7 2 4F RT 2007071100009 20070711 00009 SO 2007 7 11 C2XA07IA149 1 20070623 A 3350 B6245 LIGHT EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 24517 145332 DURING SCHEDULED MAINTENANCE, THE SERVICE DOOR EMERGENCY LIGHT FAILED TO ILLUMINATE WHEN TESTED. MAINTENANCE REPLACED T HE LIGHT ASSEMBLY. OPERATIONALLY TESTED THE SYSTEM AND CLEARED THE DISCREPANCY. 2 L 7 2 4F RT T00011AT 2007071100011 20070711 00011 SO 2007 7 11 C2XA07IA151 1 20070625 A 3350 1317 LIGHT EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 18101 145590 DURING MAINTENANCE, THE EMERGENCY LIGHT AT THE COCKPIT THRESHOLD WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BULB, OPERATIONALLY TESTED THE LIGHT AND CLEARED THE DISCREPANCY. 2 L 7 2 4F RT 2007071000276 20070710 00276 SO 2007 7 10 FDKA200706280 1 20070615 A 5210 HANDLE EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6183 SYR-JFK (1932 PHX LCL). OUTSIDE PAX DOOR HANDLE STUCK OPEN WHEN INSIDE SHOWS SECURED. MX LUBRICATED HANDLE, O PS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007071000283 20070710 00283 SO 2007 7 10 FDKA200706283 1 20070617 A 2720 SWITCH EMB 145 EMB145LR 3260212 SO RUDDER SYS MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 840MJ 145429 FDM 6111 ATL-BMI (0332 PHX LCL). RUDDER SYSTEM 2 WILL NOT SHUT OFF DURING HYDRAULIC TEST. MX REMOVED AND REINSTALLED T HE SWITCH LIGHT. 2 L 7 2 4T RT T00011AT 2007071000285 20070710 00285 2007 7 10 FDKA200706286 4 20070618 A 2210 AUTOPILOT SYS EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 834MJ 145340 FDM 6159 ATL-GPT (1105 PHX LCL). CREW RETURNED TO THE GATE DUE TO AUTO PILOT/ YAW DAMP FAIL MESSAGE. MX RESET, OPS CHE CKED NORMAL. 2 L 7 2 4T RT T00011AT 2007071000287 20070710 00287 SO 2007 7 10 FDKA200706289 1 20070620 A 5210 12029702001 SEAL EMB 145 EMB145LR 3260212 SO PAX DOOR NOISY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 145416 FDM RON MCO (0135 PHX LCL). MAIN CABIN DOOR SQUEALING. MX REMOVED AND REPLACED MAIN CABIN DOOR SEAL. 2 L 7 2 4T RT T00011AT 2007071000288 20070710 00288 EU 2007 7 10 AALA20071131 1 20070619 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7062A 474 MIA - EMERGENCY LIGHTS AT SIDEWALL SEAT ROWS 19G TO 28G INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SIDE WALL SEAT ROWS 19G TO 28G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007071000289 20070710 00289 NM 2007 7 10 AALA20071132 1 20070620 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 678AN 29428 LGA - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071000290 20070710 00290 2007 7 10 FDKA200706290 4 20070620 A 2215 4006719906 SERVO EMB 145 EMB145LR 3260212 SO RUDDER FAILED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 841MJ 14147 145448 FDM 9964 JFK (1250 PHX LCL) YAW DAMPER FAIL. MX REMOVED & REPLACED RUDDER SERVO, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007071000291 20070710 00291 WP 2007 7 10 AALA20071133 1 20070619 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 424AA 49336 LGA - EMERGENCY LIGHTS AT OVERHEAD AFT FLIGHT ATTENDANT JUMP SEAT INOPERATIVE. RESECURED BATTERY PACK FOR EMERGENCY LIG HTS AT OVERHEAD AFT FLIGHT ATTENDANT JUMP SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071000293 20070710 00293 NM 2007 7 10 AALA20071134 1 20070620 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 779AN 29955 MIA - EMERGENCY LIGHT AT FORWARD CLOSET OUTBOARD CRACKED. REPLACED EMERGENCY LIGHT ASSEMBLY AT FORWARD CLOSET OUTBOARD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007071000294 20070710 00294 NM 2007 7 10 AALA20071142 1 20070622 A 3350 210019 SWITCH BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 386AA 27060 ORD - EMERGENCY LIGHTS IN CABIN TURN ON WITH SWITCH OFF. REPLACED FORWARD FLIGHT ATTENDANTS SWITCH FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007071000296 20070710 00296 NM 2007 7 10 AALA20071143 1 20070623 A 3240 BRAKE BOEING 737 737823 13844BZ NM MLG LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 964AN 30093 YYZ INFLIGHT T2071/23JUN - AFTER LANDING NUMBER 3 BRAKES WERE STUCK FOR FOUR OR FIVE MINUTES THEN RELEASED. FOUND HYDRA ULIC LEAK NEAR RIGHT MAIN GEAR. TAXIED TO GATE. REPLACED NUMBER TREE BRAKE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F RT A16WE 2007071000297 20070710 00297 SO 2007 7 10 FDKA200706293 1 20070622 A 5210 14525311403 SEAL EMB 145 EMB145LR 3260212 SO PAX DOOR UNKNOWN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 831MJ 145273 FDM RON RDU (0634 PHX LCL). PAX DOOR SEAL REQUIRES REPLACEMENT. MX REPLACED THE DOOR SEAL. 2 L 7 2 4T RT T00011AT 2007071000298 20070710 00298 NM 2007 7 10 AALA20071146 1 20070623 A 3350 P2010031302 COVER BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 654A 24612 FLL - EMERGENCY EXIT LIGHT AT RIGHT NUMBER TWO DOOR MISSING COVER. REPLACED COVER FOR EMERGENCY EXIT LIGHT AT RIGHT NUM BER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071000299 20070710 00299 EU 2007 7 10 AALA20071156 1 20070625 A 3350 BULB AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14077 612 JFK - EMERGENCY LIGHT EXIT SIGN IN CEILING AT LEFT NUMBER TWO DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT EXIT SIGN IN C EILING AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007071000300 20070710 00300 NM 2007 7 10 AALA20071147 1 20070623 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 679AN 29589 SFO - EMERGENCY LIGHT AT SEAT 28D INOPERATIVE. REPAIRED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071000301 20070710 00301 EU 2007 7 10 AALA20071155 1 20070625 A 2780 JACKSCREW AIRBUS 300 A300B4605R 3930308 EU SLAT INOPERATIVE A AALA O OTHER O OTHER LD LANDING 1 SW 21 70073 516 MIA INFLIGHT T918/25JUN - LEADING EDGE SLATS WOULD NOT EXTEND FOR LANDING. LANDED MIA WITHOUT INCIDENT. REPLACED NUMBE R THREE RIGHT JACK SCREW. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007071000302 20070710 00302 NE 2007 7 10 AALA20071154 2 20070625 A 7532 BLEED VALVE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE ZONE 600 INOPERATIVE A AALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SW 21 7508 49802 708559 DFW INFLIGHT T1365/25JUN AT FLIGHT LEVEL 320 WITH ENGINE AND AIRFOIL ANTI-ICE ON RIGHT ENGINE COMPRESSOR STALLED WHEN POWER WAS REDUCED TO ONE THIRD ENGINE PRESSURE RATIO FOR DESCENT. NO LIMITS EXCEEDED. LANDED DFW WITHOUT INCIDENT. RE PLACED PRESSURE RATIO BLEED CONTROL VALVE ASSEMBLY AND REPLACED RIGHT ENGINE FUEL CONTROL. ACCOMPLISHED BLEED VALVE LUB RICATION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007071000303 20070710 00303 SO 2007 7 10 FDKA200706295 1 20070622 A 3150 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 830MJ 145259 FDM 5999 ATL (1723 PHX LCL). RUDDER HARDOVER PROTECTION FAIL MESSAGE. MX RESET FADEC AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007071000304 20070710 00304 SO 2007 7 10 LR7A07057 1 20070624 A 6120 AN5H5 BOLT LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL DRIVE BRACKET SHEARED A LR7A E ENGINE SHUTDOWN X ENGINE FLAMEOUT DE DESCENT 1 AL 03 403LC 156 4590 NR 4 ENGINE FLAMED OUT DURING DESCENT. FOUND CONTROL DRIVE BRACKET (ANTI-ROTATION) BOLTS SHEARED, AND EXCESSIVE PLAY ON PUMP HOUSING GEAR. REPLACED DRIVE BRACKET BOLTS IAW HAMILTON STANDARD P5059 PG 1-402, REPLACED NR 4 PUMP HOUSING IAW H AMILTON STANDARD MM P5059 PG 1-338 - 1-340, REPLACED NR 4 VALVE HOUSING PRECAUTIONARY IAW LAC JC 61135, GROUND RUNS AND LEAK CHECKS SATISFACTORY. 2 H 7 4 4T 4 T A1SO E282 2007071000305 20070710 00305 NM 2007 7 10 DL76S070785 1 20070622 A 5315 BAC1509100682 FLOORBEAM BOEING 767 767332 1382001 NM BS 676 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 FWD CARGO BS 676 LBL42 FLOORBEAM ANCHOR NUT CORRODED ON BOTTOM SIDE, REPAIRED ON AJN 52957 PER 53-00-07 FIGURE 201 REPAI R 4. 2 L 7 2 4F RT A1NM 2007071000306 20070710 00306 NM 2007 7 10 DL76S070786 1 20070622 A 5320 FLOOR SUPPORT BOEING 767 767332 1382001 NM BS 1197 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 AFT CARGO STA 1197+66 LBL10 TO LBL 30 FLOOR PNL SUPPORT RIB SIGN OF CORROSION REPAIRED ON AJN 51001 PER 53-00-07 REPAIR 4 FIG 201. 2 L 7 2 4F RT A1NM 2007071000307 20070710 00307 NM 2007 7 10 DL76S070787 1 20070622 A 5320 FLOOR SUPPORT BOEING 767 767332 1382001 NM BS 1197 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 AFT CARGO FLOOR PANEL SUPPORT RIB AT STA 1197+66 LBL 38 CORRODED, REPAIRED ON AJN 51016 PER 53-00-07 FIGURE 201 REPAIR 4 . 2 L 7 2 4F RT A1NM 2007071000308 20070710 00308 SO 2007 7 10 FDKA200706296 1 20070623 A 7930 INDICATOR EMB 145 EMB145LR 3260212 SO COCKPIT FAULTY A FDKA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 831MJ 145273 FDM 6067 BHM (0510 PHX LCL). ABORTED TAKEOFF DUE TO ENGINE 2 OIL FILTER IMPENDING BY PASS ON T/O ROLL. MX REMOVED AND REPLACED OIL FILTER IMPENDING BYPASS INDICATOR. 2 L 7 2 4T RT T00011AT 2007071000309 20070710 00309 NM 2007 7 10 DL757070834 1 20070629 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM FS 608 S16L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 663DN 24992 FUSELAGE SKIN HAS A DENT AT FS608, S-16L. CUT OUT DAMAGED SKIN AND INSTALLED A REPAIR DOUBLER. 2 L 7 2 4F RT A2NM 2007071000310 20070710 00310 EU 2007 7 10 NWAA072293257 1 20070626 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320212 3930322 EU EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 357NW 360 360 830 TEST OF EMERGENCY LIGHT SYSTEM (CIDS) EPSU INT LOAD EMERG L DISPLAYED. REPLACED EPSU 11WL, TESTS OK.. 2 L 7 2 4F RT A28NM 2007071000311 20070710 00311 NM 2007 7 10 AWXA200700779 1 20070621 A 5320 D53480048202 SILL AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 808AW 1088 MCN - MAJOR REPAIR - BC-06 CHECK - NR 5980887, CORROSION ON THE R2 DOOR CUT OUT SHAPE SILL, BS 2880 - BS 2884, RBL 1732, WL 240. REPAIRED THE R2 DOOR CUT OUT SHAPE SILL, BS 2880 - BS 2884, RBL 1732, WL 240 IAW A319 SRM 53-41-14. 2 L 7 2 4F RT A28NM 2007071000313 20070710 00313 NM 2007 7 10 AWXA200700780 1 20070628 A 2560 P4010021 POWER SUPPLY AIRBUS A319 A319132 3930340 NM FLASHLIGHT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 808AW 1088 MCN - EEL - BC-06 CHECK - NR# 5941740, THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT IS INOPERATIVE. REPLACED AND OPERATIONAL CHECKED THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT POWER UNIT. 2 L 7 2 4F RT A28NM 2007071000314 20070710 00314 NM 2007 7 10 AWXA200700781 1 20070624 A 2560 P2070003001 FLASHLIGHT AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 808AW 1088 MCN - EEL - BC-06 CHECK - NR# 5981399, LEFT AFT FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT IS INOPERATIVE. REPLACED AND OPERATIONAL CHECKED THE LEFT AFT FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT. 2 L 7 2 4F RT A28NM 2007071000315 20070710 00315 SO 2007 7 10 FDKA200706297 1 20070623 A 2720 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 830MJ 145259 FDM 6142 MCO (1051 PHX LCL). RUDDER HARDOVER PROTECTION FAIL MESSAGE. CREW SHUT DOWN ENGINES AND RESTARTED ENGINES, ME SSAGE CLEARED. 2 L 7 2 4T RT T00011AT 2007071000316 20070710 00316 NM 2007 7 10 QXEA200701039 1 20070627 A 6120 POTENTIOMETER DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS OUT OF ADJUST A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 369PH 513 YKM FLIGHT NR 2017 - UPON APPLICATION OF TAKEOFF POWER AUTO FEATHER DID NOT ARM, AUTO FEATHER SYSTEM INOP. ADJUSTED AUT O FEATHER ARMING POTENTIOMETER IAW AMM 76-10-15-820-802, FUNCTIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED T O SERVICE. 2 H 7 2 4T RT A13NM 2007071000317 20070710 00317 2007 7 10 FDKA200706298 4 20070623 A 2210 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO AUTOPILOT SYS MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6152 FLL (1250 PHX LCL). YAW DAMPER FAIL MESSAGE. MOC RESET WITH THE CREW AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2007071000318 20070710 00318 NM 2007 7 10 QXEA200701040 1 20070628 A 5100 NONE DHAV DHC8 DHC8202 2809007 NM NONE NONE A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 353PH 496 SEA - FLIGHT CREW NOTICED ACRID BURNING ODOR IN COCKPIT, NO SMOKE NOTED. ODOR IS STILL NOTICEABLE AFTER PARKING. FOUND CAPTAINS HAT WAS HUNG ON OBSERVERS MAP LIGHT THAT WAS ON. MELTING CAPTAINS HAT CAUSING ACRID ODOR IN COCKPIT. NO OTHE R DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071000320 20070710 00320 SO 2007 7 10 FDKA200706302 1 20070624 A 2121 GASPER FAN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 843MJ 145478 FDM 6148 MCO-RDU. FLIGHT DECK ODOR DISTRACTED CREW FROM PERFORMING DUTIES. MX FOUND ODOR COMING FROM GASPER. PLACED G ASPER ON MEL. 2 L 7 2 4T RT T00011AT 2007071000324 20070710 00324 SO 2007 7 10 FDKA200706301 1 20070625 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN DISCONNECTED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6147 TLH-FLL (0920 PHX LCL). EMERGENCY AILSE CEILING LIGHT PLACARD AT ROW 12 INOP. MX RE-CONNECTED LIGHT ASSEMBLY. OPS GOOD. 2 L 7 2 4T RT T00011AT 2007071000330 20070710 00330 NM 2007 7 10 CALA0700323 1 20070626 A 5320 6935352Y1 FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND A .5 INCH CRACK IN CLIP AT STA 597, S8L. THE CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071000335 20070710 00335 NM 2007 7 10 CALA0700326 1 20070627 A 5315 6546811 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND SURFACE CORROSION AROUND SCREW HOLES ON FLOORBEAM AT STA 1016 FROM LBL 30 TO LBL 34, S19L-S21L. THE CO RROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 2007071000340 20070710 00340 EU 2007 7 10 YENA2007057 1 20070625 A 2120 19055086405 DUCT EMB ERJ190 ERJ190100IGW 3260408 EU CABIN DAMAGED A YENA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 15 198JB 19000021 FLT 1004, JFK-BOS, BURNING SMELL SIMILAR TO BURNING CURLING IRON, COMING FROM OVERHEAD COCKPIT VENT, DID NOT SEE SMOKE. SMELLED DURING CLIMBOUT, ON APPROACH NO EICAS MSG WITH SMELL. FOUND DAMAGED CABIN SUPPLY DUCT. REMOVED AND REPLACED D UCT PER AMM 21-24-03, RAN PACKS, OPS CHECK. 2 L 7 2 4F RT A57NM 2007071000348 20070710 00348 EU 2007 7 10 YENA2007058 1 20070622 A 2797 19019564401 WIRE HARNESS EMB ERJ190 ERJ190100IGW 3260408 EU L/E SLAT DEFECTIVE A YENA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 197JB 3565 19000020 SLAT FAIL AFTER TAKEOFF. FLT 1094, CMH-JFK RETURNED FOR LANDING AT CMH. REPLACED RIGHT SLAT 2/3 & 3/4 SKEW SENSOR HARN ESSES PER AMM 27-83-07-400-801. CLEARED SF-ACE INHIBITS. NO EICAS MSG PRESENT. OPS CHECK OF SLATS IS NORMAL PER AMM 2 7-80-710-801. OK FOR RETURN TO SERVICE. 2 L 7 2 4F RT A57NM 2007071000357 20070710 00357 NM 2007 7 10 QXEA200701072 1 20070628 A 5230 DOOR BOMBDR DHC8 DHC8402 1390042 NM CARGO STUCK A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 407QX 4049 BOI FLIGHT NR 2302: RAMP WORKERS UNABLE TO OPEN REAR CARGO DOOR AFTER PAX DEPARTING. MAINTENANCE OPENED REAR CARGO DOOR . FOUND BAGGAGE JAM AGAINST INSIDE OF THE DOOR. INSPECTED DOOR ROLLERS AND MECHANISM. NO DEFECTS NOTED. DOOR OPS NOR MAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071000358 20070710 00358 EU 2007 7 10 AWXA200700782 1 20070619 A 5311 D53571550226 FRAME AIRBUS 320 A320231 3930325 EU ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 CORROSION ON FRAME SUPPORT ANGLE, FR 71, BS 3046, S27R - S32R. REPLACED FRAME SUPPORT ANGLE, FR 71, BS 3046, S27R - S32 R IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007071000359 20070710 00359 EA 2007 7 10 VNAA0706003 1 20070608 A 5350 601R33038963 RADOME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE DAMAGED A VNAA O OTHER O OTHER CR CRUISE 1 GL 05 253PS 7219 7934 CREW REPORTED A LIGHTNING STRIKE WHILE IN FLIGHT. CREW LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE PERFORMED AN EN ROU TE LIGHTNING STRIKE INSPECTION. MAINTENANCE REMOVED AND REPLACED THE RADOME IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 53-81-01-400-801. MAINTENANCE REPAIRED ALL DAMAGE. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007071000360 20070710 00360 NM 2007 7 10 AWXA200700783 1 20070627 A 5330 6545775 SKIN BOEING 737 7373S3 1384711 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 CRACKED FUSELAGE SKIN, BS 727D, S23R. REPAIRED FUSELAGE SKIN, BS 727D, S23R IAW USAIRWAYS EA 120072. 2 L 7 2 4F RT A16WE 2007071000362 20070710 00362 NM 2007 7 10 AWXA200700784 1 20070622 A 3397 D9299200900200D WIRE HARNESS AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 808AW 1088 EMERGENCY ESCAPE PATH LIGHTING WIRE HARNESS DAMAGED AT SEAT ROWS 4L, 10L, 12L AND 22L. REPLACED AND OPERATIONAL CHECKED THE EMERGENCY ESCAPE PATH LIGHTING HARNESS DAMAGED AT SEAT ROWS 4L, 10L, 12L AND 22L IAW A319 AMM 33-51-19. 2 L 7 2 4F RT A28NM 2007071000363 20070710 00363 EU 2007 7 10 AWXA200700778 1 20070626 A 2611 RAI2800M0706 CONTROL BOX AIRBUS 320 A320231 3930325 EU E/E BAY FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 625AW 29049 624 064 CREW REPORTED SMOKE LAV & CARGO DET FAULT. MX REPLACED SDCU PER MM26-17-34. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007071000364 20070710 00364 NM 2007 7 10 NWAA072346716 1 20070623 A 5330 SKIN BOEING 747 747251F 1384898 NM BS 390 S5R CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 616US 21120 DURING "L" CHECK, FOUND CRACK AT FORWARD UPPER CORNER OF UPPER DECK DOOR CUTOUT SKIN AT BS 390 S5R. REPAIRED PER EA 67- 209244. 2 L 7 4 4F A20WE 2007071000366 20070710 00366 NM 2007 7 10 NWAA072326716 1 20070625 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 1800 S11R CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 616US 21120 DURING "L" CHECK, FOUND CRACK IN FRAME AT BS 1800 S11R. REPAIRED PER EA 67-209723. 2 L 7 4 4F A20WE 2007071000373 20070710 00373 EA 2007 7 10 VNAA0706007 1 20070614 A 5753 SCREW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FLAP FAIRING DAMAGED A VNAA O OTHER O OTHER DE DESCENT 1 GL 05 209PS 7874 CREW REPORTED DURING DESCENT A LIGHTNING STRIKE. CREW LANDED IN CHA WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFOR MED AN EN ROUTE VISUAL LIGHTNING STRIKE INSPECTION IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 05-51-05-210-801. DAMAGE WAS FOUND ON RIGHT HAND INBOARD FLAP FAIRING SCREW AND LEFT OUTBOARD ELEVATOR STATIC WICK. MAINTENANCE REPAIRED ALL DAMAGE. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007071000375 20070710 00375 NM 2007 7 10 CALA0700329 1 20070628 A 5320 6545856 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND WEB CORRODED FROM STA 986.5 TO 1006, S21R. THE WEB WAS REMOVED AND REPLACED IAW SRM 53-60-15 AND 51-40 -02. 2 L 7 2 4F RT A16WE 2007071000376 20070710 00376 NM 2007 7 10 DL757070836 1 20070630 A 2760 SPOILER BOEING 757 757232 1384965 NM LT STUCK A DALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 27 685DA 27588 ON APPROACH, "R YAW DAMP INOP" ILLUMINATED ON EICAS FOLLOWED BY "SPOILER" LIGHT. ALMOST FULL RT AILERON NEEDED TO MAINT AIN LEVEL FLIGHT. ALSO STAB TRIM LIGHT ILLUMINATED ON LANDING. ON CLIMB-OUT C-HYD SYSTEM PRESSURE AND OVERHEAD SYS PRE SSURE LIGHTS ILLUMINATED. QTY AND PRESSURE CKS OK ON HYD PAGE. UPON ARRIVAL AT GATE MTC FOUND LT OUTBD SPOILER STICKIN G UP. PER POM CTR HYD WAS SHUTDOWN DUE TO PREVIOUS LOG ITEM. NO MESSAGES WITH C HYDRAULICS OPERATING. 2 L 7 2 4F RT A2NM 2007071000377 20070710 00377 NM 2007 7 10 KCSA071199 1 20070629 A 5320 FITTING BOEING 747 747221F 1384868 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 LEFT SIDE NOSE CARGO DOOR PORTAL C-3 FRAME UPPER CLOSER FITTING FASTENER HOLE IS CRACKED AT STA 285.5, WL 323. 2 L 7 4 4F A20WE 2007071000380 20070710 00380 NM 2007 7 10 DL764070841 1 20070701 A 3150 UNKNOWN BOEING 767 767432ER 1385134 NM UNKNOWN A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 829MH 29700 R ENG FAN VIBRATION CYCLED CONTINUOUSLY BETWEEN 0.0 AND 5.00 ON TAXI OUT AND RTN TO GATE. NO VIB WAS FELT. ENG WAS STA BILIZED AT IDLE. INSP INLET AND EXH AND CHIP DET. FWD TO MCO AND PLACARD. T/S PER FIM 77-31-00 FIG 103. PERFORMED AV M BITE PROCEDURE. ALL CHECKS NORMAL. A/C OK FOR SERVICE. MCO AND PLACARD REMOVED. 2 L 7 2 4F RT A1NM 2007071000382 20070710 00382 2007 7 10 AMTA200700277 4 20070606 A 3460 1741010301 CDU BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE COCKPIT FAILED A AMTA O OTHER P NO WARNING INDICATION CR CRUISE 1 GL 11 308TZ 28244 RT FMS CDU BLANK. REPLACED CDU IAW AMM 34-61-01-2. (K) 2 L 7 2 4F 4 F RT A16WE E2GL 2007071000384 20070710 00384 NM 2007 7 10 AMTA200700278 1 20070606 A 4900 UNKNOWN BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE APU UNKNOWN A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 308TZ 28244 APU AUTO SHUTDOWN. NO FAULT LIGHT ILLUMINATED. MSG FCU DISAGREE WITH COMMAND 49-31171 FAULT CLEARED AFTER APU RESTART. FOUND FUEL QUANTITY LOW. (K) 2 L 7 2 4F 4 F RT A16WE E2GL 2007071000385 20070710 00385 NM 2007 7 10 CALA0700332 1 20070630 A 5311 6546539 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14613 27326 INSPECTION FOUND A 1.75 INCH CRACK AT LOWER FASTENER ON FUSELAGE STUB FRAME FORWARD SIDE, STA 616, S16L. THE CRACKED AR EA OF FRAME INNER CHORD WAS REMOVED AND A REPAIR ANGLE AND FILLER WERE INSTALLED IAW ECRA 5311-01158. 2 L 7 2 4F RT A16WE 2007071000386 20070710 00386 NM 2007 7 10 AMTA200700279 1 20070608 A 4900 380029816 APU BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE APU BAY UNKNOWN A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 522AT 37636 37636 29330 CAPT BRIEFED APU SHUTDOWN TWICE, APU FAULT MSG. (MX MSG) REPLACED APU IAW W/C M57-49-02 AND 49-11-01-4. OPS AND LEAK CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007071000387 20070710 00387 NM 2007 7 10 CALA0700333 1 20070701 A 5320 6549574411 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND AFT PRESSURE BULKHEAD FORWARD FACE LOWER CHORD ANGLE CORRODED AT STA 1016 FROM S27L T0 S27R. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071000388 20070710 00388 2007 7 10 AMTA200700291 4 20070614 A 2310 TRANSCEIVER BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE NR 1 HF UNDERTORQUED A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 323TZ 30033 NR 1 HF UNABLE TO TRANSMIT OR RECEIVE DATA ON NR 1 HF CHECKS GOOD. ON SECOND ATTEMPT NR 1 HF WORKED NORMALY. PERFORM B ITE TEST ON NR 1 HF RECEIVER NO FAULTS FOUND IAW FIM 23-11-810-801 SYSTEM OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A16WE E2GL 2007071000389 20070710 00389 2007 7 10 AMTA200700292 4 20070616 A 2310 9640453011 COUPLER BOEING 737 73783N 13844HI NM NR 1 HF FAILED A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 315TZ 28245 HF 1 WILL NOT TUNE. RECEIVES OK. T/S IAW 23-11-00-810-804, FOUND HF COUPLER NR 1 BAD. REMOVED AND REPLACED NR 1 HF CO UPLER IAW 23-11-61-4, OPS NORMAL, NO FAULTS ON TRANSCEIVER. OK FOR SERVICE. (K) 2 L 7 2 4F RT A16WE 2007071000390 20070710 00390 NM 2007 7 10 CALA0700334 1 20070701 A 5313 6549914545 FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND STRINGER 27L END FITTING CORRODED IN BOLT HOLES, STA 1016. THE END FITTING WAS REMOVED AND REPLACED IA W SRM 51-40-12. 2 L 7 2 4F RT A16WE 2007071000392 20070710 00392 NM 2007 7 10 AMTA200700295 1 20070620 A 5270 UNKNOWN BOEING 737 73783N 13844HI NM OVERWING EXIT UNKNOWN A AMTA C ABORTED TAKEOFF N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 318TZ 28247 FWD OVERWING AND AFT OVERWING DOOR LIGHT CAME ON, ON TAKEOFF. FOUND LT FWD OVERWING FLT LOCK BREAKER POPPED. RESET C/B . PERFORMED FIM TASK 52-20-00-810-801. SYSTEM TEST NORMAL OVERWING EXIT LIGHTS OUT. (K) 2 L 7 2 4F RT A16WE 2007071000393 20070710 00393 NM 2007 7 10 AMTA200700296 1 20070620 A 3600 UNKNOWN BOEING 737 73783N 13844HI NM WARNING LIGHT UNKNOWN A AMTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 321TZ 28249 AT START OF TAKEOFF, WITH BLEEDS OFF, LT BLEED TRIP LIGHT CAME ON. ABORTED TO AT SLOW SPEED. RESET BLEED TRIP LIGHT. (K) 2 L 7 2 4F RT A16WE 2007071000395 20070710 00395 2007 7 10 AMTA200700297 4 20070620 A 2310 NONE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE HF RADIO NONE A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 550TZ 32584 LT HF RADIO RECEIVER GARBLED AND UNREADABLE. PERFORMED ADJ AND TEST ON LT HF SYSTEM, CALLED SFO ON 8843 AND 5574 RECEIV ED AND TRANSMITT 5X5, COULD NOT FAULT, OK FOR CONTINUED SERVICE. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007071000396 20070710 00396 NM 2007 7 10 AMTA200700306 1 20070623 A 3150 NONE BOEING 737 73783N 13844HI NM NONE NONE A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 321TZ 28249 ON TAXI OUT, LT PACK LIGHT ILLUMINATED. RETURNED TO GATE. PERFORMED TEST STEP E IAW AMM 21-51-10-4,, LT PACK OPERATES N ORMAL. (K) 2 L 7 2 4F RT A16WE 2007071000398 20070710 00398 NM 2007 7 10 AMTA200700307 1 20070618 A 2840 INDICATOR BOEING 737 73783N 13844HI NM FUEL QTY INOPERATIVE A AMTA O OTHER P NO WARNING INDICATION CR CRUISE 1 GL 11 321TZ 28249 CENTER TANK FUELING PANEL GAUGE INOPERATIVE. COCKPIT FUEL QTY INDICATOR READS CORRECT. FOUND CONNECTOR PLUG LOOSE AND DIRTY. CLEANED AND SECURED. OPS CHECKS GOOD. (K) 2 L 7 2 4F RT A16WE 2007071000399 20070710 00399 NM 2007 7 10 AMTA200700308 1 20070622 A 2150 32144464 VALVE BOEING 737 73783N 13844HI NM LT A/C PACK UNSERVICEABLE A AMTA K NONE J WARNING INDICATION IN INSP/MAINT 1 GL 11 321TZ 28249 IMMEDIATELY AFTER TAKEOFF, LT PACK LIGHT CAME ON, TRIED TO RESET. LT BLEED TRIP OFF LIGHT CAME ON, LEVELED AT 10,000, L IGHT RESET. CLIMB TO 25,000. OPS NORMAL. REF FIM 36-10-00, REMOVED AND REPLACED NR 1 HIGH STAGE VALVE IAW AMM 36-11- 06, RAN ENGINES AND PRESSURIZED AC WITH LT PACK ONLY IAW AMM 21-31-00, OPS AND LEAK CHECK, OK. (K) 2 L 7 2 4F RT A16WE 2007071000400 20070710 00400 NM 2007 7 10 AMTA200700309 1 20070618 A 4920 APU BOEING 737 73783N 13844HI NM INOPERATIVE A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 321TZ 28249 APU QUIT, HAD A FAULT LIGHT. (K) REMOVED AND RECONNECTED CONNECTOR PLUG P6. PERFORMED OPS CHECK AND LEAK CHECK IAW MM 49-11-00-4. NO FAULTS NOTED. OK FOR SERVICE. (K) 2 L 7 2 4F RT A16WE 2007071000401 20070710 00401 NM 2007 7 10 AMTA200700301 1 20070622 A 5320 FLOOR SUPPORT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 795-847 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 403TZ 24664 AFT CARGO FLOOR SUPPORT STRUCTURE HAS HEAVY CORROSION AT EDGE OF THRESHOLD EXISTING UNDER FLOOR PANEL 1537X FROM STA 795 TO 847. REMOVED CORROSION SRM 51-10-02 FROM THRESHOLD WEB ON LIMITS 53-60-53. REMOVED CORROSION FROM BEAM OUT OF LIMI TS 53-60-53. REPLACED TRACK STRUCTURE SRM 53-00-53 AND 51-40-02 TREATED 51-20-01. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2007071000403 20070710 00403 NM 2007 7 10 2007UALA02234 1 20070623 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EEL IN 4F AFT, 5A AFT, 33 HJK & 46 ABC ARE INOPERATIVE. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071000404 20070710 00404 NM 2007 7 10 2007UALA02235 1 20070623 A 3350 80541 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE R3 DOOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY LIGHT INOP DOOR 3R SLIDE ILLUMINATION. REPLACED LIGHT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071000406 20070710 00406 NM 2007 7 10 2007UALA02237 1 20070623 A 3397 SPLICE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EEL INOP DOOR 5R LOWER AFT WALL. REPAIRED SPLICE NEAR LAMP CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071000408 20070710 00408 NM 2007 7 10 AMTA200700310 1 20070625 A 3040 CONTROLLER BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE WINDOW HEAT MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 560TZ 33525 EICAS MSG DISPLAYED RT FWD WINDOW HEAT INOPERATIVE LIGHT ILLUMINATED. WINDOW HEAT COULD BE RESET. RESET WINDOW HEAT CO NTROLLER IAW MM 30-00-00. PERFORMED BITE TEST. NO FAULTS NOTED. OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007071000410 20070710 00410 2007 7 10 AMTA200700311 4 20070627 A 3460 FMC BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE MALFUNCTIONED A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 519AT 27975 ON PUSH BACK, RT ENG STARTED. FMC LIGHT AND FMC MSG TURNED RT THEN BACK TO LT FMC SCREEN BLANK. (LT FMC). PERFORMED B ITE ON LT FMC NO DEFECTS NOTED. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007071000412 20070710 00412 NM 2007 7 10 2007UALA02241 1 20070624 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EEL INOP AT 26 AB FWD, 32 HJK & 47 ABC. RELAMPED EMERGENCY LIGHTS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071000414 20070710 00414 NM 2007 7 10 AMTA200700285 1 20070611 A 5270 STRIKER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE PAX DOOR CONTAMINATED A AMTA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 519AT 27975 RT FWD ENT DOOR LIGHT ILLUMINATED AND SLIDE DOOR ARM WILL OT ENGAGE. INSPECTED DOOR, CLEAR DEBRIS OFF STRIKER PLATES,, CYCLED AND ARMED DOOR, DOOR OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2007071000415 20070710 00415 EU 2007 7 10 CPCP20070041 1 20070510 A 5210 SUPPORT AEROSP ATR72 ATR72212 8680945 EU PAX DOOR CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 260AE 263 THREAD SUPPORT NR 1 (BOTTOM) OF PASSENGER DOOR STAIRCASE IS CORRODED UNDER NUT PLATES. THREAD SUPPORT NR 1 FROM BOTTOM REPLACED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007071000416 20070710 00416 EU 2007 7 10 DHL2007364001 1 20070701 A 5311 FRAME AIRBUS 300 A300B4203 3930306 EU BS 1499 BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 DURING A "A"-8 CHECK AT AVBOURNE HVY MX IN MIAMI, THE FOLLOWING DISCREPANCIES WERE NOTED. EXISTING FRAME DOUBLER AT STA 1499 FRAME 21 BETWEEN STR 6 AND 7R WAS BENT. REMOVED EXISTING REPAIR IAW A300 SRM 53-10-10, FABRICATED REPAIR DOUBLER FROM 2024-O .071, HEAT TREATED AND PRIMED IAW A300 SRM 51-40-30, TREATED AND PRIMED IAW A300 SRM 51-40-12 AND 53-10-10. INSTALLED IAW A300 SRM 53-10-10. 2 L 7 2 4F RT A35EU 2007071000418 20070710 00418 2007 7 10 AMTA200700286 4 20070611 A 2310 RADIO BOEING 737 73783N 13844HI NM NR 1 HF MALFUNCTIONED A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 315TZ 28245 HF 1 WILL NOT DETUNE ON 8843, 5574, 13352, CONTINIOUS TURNING SIGNAL WHEN RETUNING NEW FREQ AT BOTH CAPT AND F/O MICS. PERFORMED ADJ AND TEST IAW 23-22-00-730, CALLED SFO ON 5574 AND 8843, RECEIVED AND TRANSMITT 5X5, COULD NOT FAULT, NR 1 AND NR2 HF. OPS CHECK NORMAL. (K) 2 L 7 2 4F RT A16WE 2007071000419 20070710 00419 NM 2007 7 10 2007UALA02264 1 20070626 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 542UA 25276 DOOR 4 RIGHT EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT, OP CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071000421 20070710 00421 NM 2007 7 10 AMTA200700287 1 20070612 A 3397 CONNECTOR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHT DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 517AT 27973 L2 DOOR LOWER EMERGENCY LIGHT INOPERATIVE. PLUGGED EMERGENCY LIGHT RECEPTICAL INTO SIDE WALL SOCKET OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2007071000423 20070710 00423 2007 7 10 AMTA200700280 4 20070602 A 2310 UNKNOWN BOEING 737 73783N 13844HI NM HF RADIO UNKNOWN A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 301TZ 28239 SELCAL ON HF 1 AND HF 2, WILL NOT PROVIDE AURAL NOTIFICATION. LIGHT ON COMMUNICATION PANEL ILLUMINATES OK. ACCOMPLISHE D FIM 23-28-00-810-803, NO DEFECT FOUND ON GROUND. SYS OPERATES NORMAL. (K) 2 L 7 2 4F RT A16WE 2007071000424 20070710 00424 2007 7 10 AMTA200700281 4 20070605 A 3460 FMC BOEING 737 73783N 13844HI NM NR 2 INOPERATIVE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 308TZ 28244 SINGEL FMC OPERATION MESSAGE SHOWS ON THE CDU (NR2 FMC INOPERATIVE). (K) 2 L 7 2 4F RT A16WE 2007071000426 20070710 00426 NM 2007 7 10 QXEA200701073 1 20070629 A 6120 30005000056 TSCU DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER MALFUNCTIONED A QXEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 09 369PH 8376 513 RDM FLIGHT NR 2112 - AUTO FEATHER FAILED TO ARM ON TAKEOFF ROLL. REPLACED NR 1 TSCU AS PRECAUTIONARY MEASURES. GROUND RUN COMPLIED WITH. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071000427 20070710 00427 EU 2007 7 10 CPCP20070042 1 20070510 A 5312 BULKHEAD AEROSP ATR72 ATR72212 8680945 EU BS 2962 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 260AE 263 CORROSION FOUND ON FORWARD PRESSURE BULKHEAD AT GROUND POINTS (8) LOCATIONS. FORWARD BULKHEAD LT AND RT UPPER AT STA 29 62 REPAIRED AS PER SRM 53-11-10 FIG 404. 2 H 7 2 4T RT A53EU 2007071000428 20070710 00428 EU 2007 7 10 CPCP20070043 1 20070511 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 260AE 263 LT SEAT TRACK BETWEEN FRAME 36 AND FRAME 39 IS CORRODED. LT SEAT TRACK BETWEEN FRAME 39 AND FRAME 39 REPLACED AS PER SR M 51-25-04 2 H 7 2 4T RT A53EU 2007071000429 20070710 00429 EU 2007 7 10 CPCP20070044 1 20070511 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 260AE 263 LT SEAT TRACK BETWEEN FRAME 39 AND FRAME 41 IS CORRODED. LT SEAT TRACK BETWEEN FRAME 39 AND FRAME 41 REPLACED AS PER SR M 51-25-04. 2 H 7 2 4T RT A53EU 2007071000430 20070710 00430 NM 2007 7 10 2007UALA02288 1 20070628 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN IMPROPER PART A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY LIGHT INOP OVERHEAD MAIN STAIR ILLUM. FOUND WRONG BULBS INSTALLED, INSTALLED NEW BULBS, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071000431 20070710 00431 EU 2007 7 10 CPCP20070045 1 20070511 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 260AE 263 RT SEAT TRACK BETWEEN FRAME 36 AND FRAME 39 IS CORRODED. RT SEAT TRACK BETWEEN FRAME 36 AND FRAME 39 REPLACED AS PER SR M 51-25-04. 2 H 7 2 4T RT A53EU 2007071000432 20070710 00432 NM 2007 7 10 QXEA200701074 1 20070701 A 2730 AOA BOMBDR DHC8 DHC8402 1390042 NM OUT OF ALIGNMENT A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 401QX 4031 SEA FLIGHT NR 2418: ELEVATOR PITCH FEEL CAUTION ILLUMINATED. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE FOUND AOA VANES O UT OF ALIGNMENT. REPOSITIONED AOA VANES TO LEVEL POSITION. CYCLED SHIPS POWER. ELEVATOR FEEL CAUTION DID NOT RETURN. NO FURTHER FAULTS OR DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071000434 20070710 00434 2007 7 10 2007UALA02295 4 20070628 A 2565 FLANGE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE ESCAPE SLIDE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 831UA 1291 RIGHT OFFWING ESCAPE SLIDE HAS A CRACK IN VERTICAL AFT FLANGE LOWER END, (AREA 2) 5 INCHES. REPLACED RT OVERWING SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071000438 20070710 00438 EU 2007 7 10 2007UALA02300 1 20070628 A 3150 PANEL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EVACUATION ALARM MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 412UA 465 EVAC ALARM SOUNDS INTERMITTENTLY. EVAC PANEL AT 2L,CHECKS NORMAL. AFTER CHECKING THIS PANEL, NO REPEAT INSTANCES HAVE BEEN RECORDED. (SINCE JUNE, 07) 2 L 7 2 4F 4 F RT A28NM E40NE 2007071000444 20070710 00444 NM 2007 7 10 2007UALA02303 1 20070628 A 2560 GIRT BAR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD ENTRY DOOR LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 FWD ENTRY DOOR AFT GIRT HANGER ON DOOR IS LOOSE. TIGHTENED SCREWS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071000449 20070710 00449 NM 2007 7 10 2007UALA02305 1 20070629 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY CEILING LIGHT ABOVE ROW 16 INOPERATIVE. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071000455 20070710 00455 NM 2007 7 10 2007UALA02310 1 20070627 A 3620 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 671UA 30026 724700 ON DESCENT RECEIVED, LT ENG HPSOV EICAS MESSAGE. [07-24-07] AFTER TROUBLESHOOTING WITH INCONCLUSIVE RESULTS, CONDUCT ED BORESCOPE ON NR 2 ENG SN 724700. ENGINE FAILED BORESCOPE INSPECTION ON EC6271 DUE TO COMBUSTION CHAMBER CONTINOUS AXI AL CRACKS THRU MORE THAN 3 LOUVERS. THIS IS BEYOND REDUCED INTERVAL LIMIT PER MM 72-00-00. DAMAGE LOCATED AT 7:30 ON OU TER COMBUSTION CHAMBER, VERIFIED ON COLD SIDE.REPLACED NR 2 ENGINE PER MM- 71-00-02. ENGINE & PNEU SYSTEM CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071000456 20070710 00456 NM 2007 7 10 2007UALA02311 1 20070629 A 2612 FIRE DETECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD CARGO PIT NO TEST A UALA K NONE L NO TEST TO TAKEOFF 1 WP 29 367UA 24536 FWD CARGO PIT FIRE DETECTOR LIGHT NO TEST, A AND B CHANNELS NO TEST. REPLACED B LOOP DETECTORS. INSTALLED 2 A LOOP DE TECTORS IN FORWARD PIT. REPLACED 3 EACH A LOOP AFT CARGO COMPARTMENT SMOKE DETECTORS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071000458 20070710 00458 EU 2007 7 10 2007UALA02313 1 20070629 A 2910 HYDRAULIC SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE BLUE SYSTEM FAILED A UALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 WP 29 407UA 456 RTFL WITH BLUE SYSTEM HYDRAULICS FAILURE. FLT HAD IDENTICAL PROBLEM ON PREVIOUS LEG. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071000459 20070710 00459 EU 2007 7 10 2007UALA02314 1 20070630 A 3830 TOILET AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LAVATORY MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 455UA 1105 FLIGHT DIVERTED DUE TO INABILITY TO FLUSH BOTH AFT LAVS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071000463 20070710 00463 NM 2007 7 10 SWAA073254 1 20070628 A 5753 113A37007 SKIN BOEING 737 7377H4 1384404 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 727SW 27859 DURING SCHEDULED HC2 CHECK, FOUND LH WING OUTBOARD T/E AFT FLAP INBOARD LOWER SURFACE DELAMINATED. R&R AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2007071000464 20070710 00464 NM 2007 7 10 SWAA073249 1 20070628 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 442WN 32459 DURING SCHEDULED HC2 CHECK, FOUND RH HORIZONTAL STAB SKIN CRACKED BETWEEN STA 129.50 AND STA 138.70. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007071000466 20070710 00466 NM 2007 7 10 SWAA073247 1 20070628 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 405WN 27893 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED. R&R COVER PER MM. 2 L 7 2 4F RT A16WE 2007071000470 20070710 00470 2007 7 10 SWAA073227 4 20070628 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 245WN 32506 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071000472 20070710 00472 2007 7 10 SWAA073257 4 20070628 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 789SW 29816 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071000475 20070710 00475 NM 2007 7 10 SWAA073231 1 20070628 A 5753 6546435 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP INBOARD UPPER SURFACE DELAMINATED. R&R AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2007071000476 20070710 00476 NM 2007 7 10 SWAA073239 1 20070628 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071000477 20070710 00477 NM 2007 7 10 2007UALA02317 1 20070630 A 2910 HYDRAULIC SYSTEM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 MALFUNCTIONED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 193UA 26890 LANDED UNDER AMBER ALERT DUE TO LOSS OF NR 4 HYDRAULIC SYSTEM PRESSURE. NORMAL LANDING AND TAXI TO GATE. [07-27-07] AFTER EXTENSIVE TROUBLE-SHOOTING, REPLACED NR 4 HYDRAULIC QUANTITY TRANSMITTER, PER FIM 29-30. SERVICED HYD TO FULL. A IRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071000481 20070710 00481 NM 2007 7 10 2007UALA02321 1 20070630 A 3397 582240 STRIP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN LOOSE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 FIRST CLASS EMERGENCY EVACUATION STRIP IS LOOSE. REPLACED POWER CABLE AND 2 EA ELEMENTS. OPS CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071100003 20070711 00003 NM 2007 7 11 2007UALA02324 1 20070701 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 LOWER FUSELAGE SKIN CRACKED AT STA 943 STR 24L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED. INSTALLED A DOUBLER/TRIPL ER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071100010 20070711 00010 SO 2007 7 11 C2XA07IA150 1 20070623 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 11109 145657 FLIGHT 2023 - AFTER TAKEOFF, THE CREW NOTICED A FUEL SMELL WITH THE APU RUNNING THE AIR CONDITIONING PACKS. MAINTENANCE PERFORMED SYSTEM CHECKS OF THE APU BLEED SYSTEM AND AIR CONDITIONING PACKS. THE DISCREPANCY COULD NOT BE DUPLICATED AN D THE DISCREPANCY WAS CLEARED. 2 L 7 2 4F RT 2007071100012 20070711 00012 SO 2007 7 11 C2XA07IA152 1 20070623 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN LOW A C2XA K NONE O OTHER NR NOT REPORTED 1 SW 27 16951 145063 DURING PREFLIGHT INSPECTION, THE EMERGENCY LIGHTS WERE FOUND TO BE DIM. NO SPECIFIC PROBLEM COULD BE DETECTED WITH THE LIGHTING SYSTEM AND THE EMERGENCY LIGHT BATTERIES WERE CHARGED THROUGH NORMAL AIRCRAFT POWER. 2 L 7 2 4T RT T00011AT 2007071100013 20070711 00013 CE 2007 7 11 DXTA200702277 1 20070618 A 2700 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL UNKNOWN E DXTA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 07 986QS 7500086 AIRCRAFT CONSTANTLY ROLLS LT AND RT IN LEVEL CRUISE. WORSE AT HIGHER ALTITUDE AND HIGHER SPEED. [07-11-07] RESET RT A ILERON DROOP TO SPEC. AND ADJUSTED AILERON SERVO CABLES. IAW 750 MM. 22-10-01. ADJUSTED FEEL BUNGEE IAW 750 MM. 27-11-05 . ADJUSTED UPPER RUDDER CHANNELS A+B IAW 750 MM. 27-24-01. FOUND RUDDER BUNGEE STICKING AND REPLACED BUNGEE. IAW 750 MM 27-24-00. RIGGED LWR. RUDDER TO SPEC'S IAW 750 MM 27-20-00. TRAVELS AND OP'S CHECKS GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071100016 20070711 00016 SO 2007 7 11 C2XA07SH035 1 20070625 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 SHV - DURING C-CHECK MAINTENANCE, FOUND LT OMEGA BEAM LOWER FLANGE WITH PITTING CORROSION AT FRAME 23. MAINTENANCE REPA IRED LT OMEGA BEAM LWR FLANGE AT FRAME 23 IAW EMB 145 EC 5320-01370. NO FURTHER ACTION REQUIRED. A/C WAS APPROVED TO R ETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007071100018 20070711 00018 CE 2007 7 11 DXTA200702280 1 20070619 A 2120 UNKNOWN CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE COCKPIT SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 639QS 5605139 SMOKE WAS SEEN AND SMELLED IN THE COCKPIT. WITH APU RUNNING. [07-12-07] REMOVED AND REPLACED APU IAW 560XL M/M 49-10- 00. APU LEAK CHECKS AND OPERATES NORMAL AT THIS TIME. THIS CLEARS MEL 49-1 AREA. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007071100024 20070711 00024 SO 2007 7 11 C2XA07CL057 1 20070628 A 2750 3631101005 SELECTOR EMB 145 EMB145EP 3260221 SO COCKPIT FAULTY A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 12946 145052 CLE FLIGHT NR 2092 - THE CREW REPORTED A LANDING GEAR AURAL WARNING AT 8,OOO FT. MAINTENANCE INSPECTED AND REPLACED THE FLAP SELECTOR HANDLE. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2007071100028 20070711 00028 SO 2007 7 11 C2XA07TY032 1 20070628 A 3230 7455503 CONTROL LEVER EMB 145 EMB145LR 3260212 SO COCKPIT INOPERATIVE A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 14916 145415 BNA - FLIGHT NR 2175 - AFTER TAKEOFF, LANDING GEAR DID NOT RETRACT AND CYCLE PROCEDURE PER QRC DID NOT WORK AND A/C DIVE RTED INTO TYS. TYS REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER IAW EMB 145 AMM 32-32-02-400-801A AND EVERYTHING . OPS CHECKED GOOD IAW EMB 145 AMM 32-30-00-700-801A. 2 L 7 2 4T RT T00011AT 2007071100030 20070711 00030 SO 2007 7 11 C2XA07SH036 1 20070701 A 5320 14521713605 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27962 145110 SHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 20. MX REMOVED AND REPLACED CENTER OMEGA BEAM AT FR 20 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 2007071100031 20070711 00031 CE 2007 7 11 GLBA20060956 1 20070618 A 5320 ANGLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FUSELAGE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 170GL UE170 UPON ROUTINE INSPECTION MAINTENANCE DISCOVERED CRACK AT RT FS 288 WL 70.0. LENGTH OF CRACK 1.75 INCHES. UPON COMPLETION OF REPAIRE RII INSPECTION IS REQUIRED. MAINTENANCE REPAIRED AFFECTED AREA AT FS 288 WS 70.0 IAW SRM 53-90-23-001. IWO NR 94109. RII COMPLIED WITH IAW TASKCARD 8.2.1, INSPECTION SATISFACTORY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007071100032 20070711 00032 CE 2007 7 11 GLBA20060955 1 20070618 A 5320 ANGLE BEECH 1900 1900D 1154162 CE BS 288 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 170GL UE170 UPON ROUTINE INSPECTION, MAINTENANCE DISCOVERED CRACK AT LT FS 288 WL.70.0. LENGTH OF CRACK 1.75 NR. UPON COMPLETION OF REPAIRE RII INSPECTION IS REQUIRED. MAINTENANCE REPAIRED AFFECTED AREA AT FS 288 WS 70.0 IAW SRM 53-90-23-001. IWO NR 9 4109. RII COMPLIED IAW TASKCARD 8.2.1. INSPECTION SATISFACTORY. 2 L 7 2 4T RT A24CE 2007071100033 20070711 00033 SO 2007 7 11 C2XA07RI024 1 20070417 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO LAVATORY DEFECTIVE A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 11193 4130 4130 14500938 FLT 54 - ONT - CREW REPORTED LAV SMOKE INDICATION ON EICAS. ONT MX REMOVED AND REPLACED LAV SMOKE DETECTOR IAW EMB 145 AMM 26-14-01. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007071100037 20070711 00037 SO 2007 7 11 N93A18062007 1 20070618 A 5311 1159B2156225 FRAME GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU BS 793 CRACKED E N93A K NONE O OTHER IN INSP/MAINT 1 SO 13 411QS 1311 DURING 5000 LANDING INSPECTION, THE FRAME AT THE 793 BULKHEAD WAS FOUND CRACKED. 2 L 7 2 4F 4 F RT A12EA E25NE 2007071100038 20070711 00038 CE 2007 7 11 AMWA31034A 1 20070620 A 5311 1294400681 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 438 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 138YV UE138 FUSELAGE FRAMES DAMAGED BY CHAFFING. REPAIRED IAW ENGINEERING REPORT NR 6732-2 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007071100041 20070711 00041 CE 2007 7 11 AMWA531030 1 20070620 A 5310 1294400681 DOOR FRAME BEECH 1900 1900D 1154162 CE BS 150 CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 138YV UE138 THE PASSENGER ENTRY DOOR FRAME AT FS150 HAS 6 SMALL CRACKS TOTALING APPROX 1.5 INCHES IN LENGTH. THE CRACKS WERE LOCATE D AT THE TOP DOOR STRUT ATTACH BRACKET MOUNTING HOLE (3 EA) AND THE BOTTOM DOOR STRUT ATTACH BRACKET MOUNTING HOLE. REP AIRED IAW ENGINEERING REPORT NR 6732-3 REV A. 2 L 7 2 4T RT A24CE 2007071100042 20070711 00042 SO 2007 7 11 C2XA07CL058 1 20070630 A 3350 20131A BATTERY PACK EMB 135 EMB135ER 3260203 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 19503 145176 DURING ROUTINE MAINTENANCE, THE NR 1 AISLE PATH EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLAC ED THE NR 1 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2007071100045 20070711 00045 EU 2007 7 11 07FDEA02350 1 20070702 A 5414 A54611752 PANEL AIRBUS 300 A300B4605R 3930308 EU NR 2 PYLON DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 OLD REPAIR ON PYLON NR 2 INBOARD SIDE, RIB 8 NOT CONFORM TO SRM DOUBLER REPAIR RENEWED IAW SRM 54-51-31 FIG 201. APPROV ED BY EA 6-5451-1067447 REV A. 2 L 7 2 4F RT A35EU 2007071100047 20070711 00047 NM 2007 7 11 07FDEA02352 1 20070702 A 5315 6520832130 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT UPPER MAIN DECK, CORROSION AROUND NUT PLATE HOLE ON UPPER SURFACE OF UPPER T-CAP STA 950C LBL27.5". REMOVED CORROSI ON FROM AFT MAIN DECK UPPER SURFACE NUTPLATE HOLE ON T-CAP STA 950C LBL 27.5. HFEC AREA, NO DEFECTS NOTED. SHOT PEEN A REA, TREAT PRIMED, AND APPLIED BMS 3-23 REF SRM 51-10-01, EA 7-5310-113041 THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007071100049 20070711 00049 NM 2007 7 11 07FDEA02354 1 20070702 A 5712 651724122 RIB BOEING 727 727227 1384078 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 RT WING INBD L/E FORMER WEB CRACKED AT AFT UPPER AREA INBD SIDE. FORMER LOCATED AT O/B END OF NR 6 FLAP. FABRICATED REPAIR DOUBLER, ON RT WING INBD L/E FORMED WEB TREATED AND PRIMED, AND INSTALLED IAW B727 SRM 51-40-2 FIG 1, 51-10-2, 51 -30-2, CLASSIFIED MINOR REPAIR. 2 L 7 3 4F A3WE 2007071100051 20070711 00051 NM 2007 7 11 07FDEA02357 1 20070702 A 5753 WEDGE BOEING BOEING 727 727227 1384078 NM LT WING DEBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 LT I/B MID FLAP AFT WEDGE HAS DISBONDED JUST O/B OF THE AFT FLAP TRACK. REMOVED LT I/B AFT FLAP REF M/M 27-51-001-4 REPA IRED MID FLAP REF SRM 51-40-21 PARA 4D AND 4E AND SRM 51-40-20 PARA 7, 14, 15, 18, 20, 21, 22 LT I/B AFT FLAP ASSY INSTA LLED ON SNRM N00328. COOK TICKET ATTACHED THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007071100014 20070711 00014 NM 2007 7 11 DXTA200702278 1 20070619 A 3150 UNKNOWN AMD FALC50 FALCON2000 2730170 NM UNKNOWN E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 210QS 211 RECEIVED A YELLOW MASTER CAUTION WARNING LIGHT UPON THROTTLE ADVANCE FOR TAKEOFF. [07-11-07] COMPLIED WITH TAKE-OFF SA FTIES INDICATION LOGIC AND ALARM TEST WITH NO DEFECTS NOTED IAW MM 31-301 AND 31-301. COMPLIED WITH ENGINE RUN AND OPERA TIONAL CHECKS OF PCB 413JE IAW F2000 M/M 20-500. ALL CHECKS GOOD 2 K 7 2 4F RT A50NM 2007071100017 20070711 00017 CE 2007 7 11 DXTA200702279 1 20070619 A 3230 LANDING GEAR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LEFT MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 604QS 5605204 WHEN GEAR SELECTED DOWN, LT MAIN GEAR DID NOT SHOW GREEN LIGHT. WENT TO GEAR WOULD NOT EXTEND CK LIST AND BLEW GEAR DOWN . UNEVENTFUL LANDING. [07-11-07] TROUBLESHOT TO A FAULTY DOWN & LOCK SWITCH ON LT MLG ACTUATOR. REMOVED LT MLG ACTUATO R, INSTALLED A REPAIRED ACTUATOR (REF. CESSNA CNQR918C, WO 2-59802). PERFORMED MLG WHEEL CAMBER ADJUSTMENT. PERFORMED GE AR BLOWDOWN CHECK, CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007071100020 20070711 00020 2007 7 11 AMTA200700276 4 20070606 A 2300 UNKNOWN BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE UNKNOWN A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 519AT 27975 HF TRANSMISSION WEAK AT CAPT STATION ALL OTHER STATIONS ARE NORMAL. TRANSMITTED FROM CAPTAINS STATION, STOCKHOLM RADIO REPORT GOOD SIGNAL, OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007071100025 20070711 00025 CE 2007 7 11 GUUA06150701 1 20070615 A 2697 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FIRE BOTTLE LOOSE A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 29 231YV UE231 FLIGHT: 9278, DURING FLIGHT, RT DISCHARGE LIGHT ILLUMINATED INTERMITTENTLY. CONTINUED TO DESTINATION, LANDED WITHOUT INC IDENT. SECURED LOOSE WIRE AT THE RT FIRE BOTTLE. 2 L 7 2 4T 4 T RT A24CE E26NE 2007071100034 20070711 00034 CE 2007 7 11 DXTA200702281 1 20070620 A 3234 HANDLE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG INOPERATIVE E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 912QS 7500012 AFTER TAKEOFF, THE LANDING GEAR HANDLE COULD NOT BE MOVED TO THE UP POSITION. [07-12-07] JACKED A/C FOUND NOSE STRUT DID NOT FULLY EXTEND. SERVICED STRUT PER 750 MM. CH. 12-10-38. GEAR HANDLE OPERATIONAL CHECK GOOD. GEAR SWING CLEARANCE CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071100036 20070711 00036 SO 2007 7 11 N93A18062007A 1 20070618 A 5311 1159B2156225 FRAME GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU BS 793 CRACKED E N93A K NONE O OTHER IN INSP/MAINT 1 SO 13 411QS 1311 DURING 5000 LANDING INSPECTION, THE FRAME AT THE 793 BULKHEAD WAS FOUND CRACKED. 2 L 7 2 4F 4 F RT A12EA E25NE 2007071100046 20070711 00046 NM 2007 7 11 07FDEA02351 1 20070702 A 5322 65561261 SHEAR TIE BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT PIT STA 990 STR 26-27 L SHEAR TIE CORRODED STR 26-27 L. REMOVED 2 EA FASTENERS REF 51-30-2. REMOVED CORROSION REF SRM 51-10-1 NDT'D IAW B727 NDT MAN PART 4 51-00-00 FIG 2 ORIGINAL THICKNESS .063. REMOVED .003 ;.060 MATERIAL REMAINING WITHIN LIMITS REF SRM 51-00-00 FIG 1 DETAIL I. TREATED AND PRIMED REF SRM 51-10-2. INSTALLED 2 EA FASTENERS REF SRM 51-30-2. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007071100044 20070711 00044 SO 2007 7 11 C2XA07IA154 1 20070627 A 3350 110049 FUSE EMB 145 EMB145EP 3260221 SO POWER SUPPLY BLOWN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15926 145005 DURING PREFLIGHT INSPECTION, THE CREW NOTICED THAT THE FLOOR EMERGENCY LIGHTING STRIP DID NOT ILLUMINATE WHEN TESTED. M AINTENANCE REMOVED AND REPLACED A FUSE ON THE NR 2 EMERGENCY LIGHT POWER SUPPLY. THE LIGHTS WERE OPERATIONALLY TESTED A ND THE DISCREPANCY CLEARED. 2 L 7 2 4F RT T00011AT 2007071100048 20070711 00048 NM 2007 7 11 07FDEA02353 1 20070702 A 5340 66118092 STRINGER CLIP BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT PIT STRINGER CLIP CRACKED STA 950E STR 28L REMOVED CRACKED STRINGER CLIP REPLACED WITH NEW CLIP PART NR 6611809-2 IA W SRM 51-30-2 PG 3. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007071100050 20070711 00050 NM 2007 7 11 07FDEA02356 1 20070702 A 5753 652163480 FLAP BOEING 727 727227 1384078 NM RT WING DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 RT WING, I/B FLAPS, AFT FLAP O/B END T/E IS DELAMINATED. REMOVED, REPAIRED, AND REINSTALLED RT WING I/B FLAP, AFT FLAP ASSY REF'S MM 27-51-002-4 AND SRM 51-40-20 THIS IS CLASSIFIED AS A MAJOR REPAIR. PLAY AND POSITION CHECK TO BE PERFORME D ON ROUTINE CARD W/C 76C017-00. 2 L 7 3 4F A3WE 2007071100053 20070711 00053 CE 2007 7 11 DXTA200702282 1 20070621 A 3230 LANDING GEAR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 330QS 5600329 ON DEPARTURE, LANDING GEAR WOULD NOT RETRACT. AUXILLARY GEAR CONTROL WAS ACTIVATED AS A PRECAUTION. [07-12-07] T/S F OUND LEFT GEAR SQUAT SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH. IAW CESSNA 560 MM. CH. 32-30-01. OPS. CHECK SATISFACTORY . ALSO BLED MLG. RESET BLOWDOWN BOTTLE. SAFTIED AND SERVICED. 2 L 7 2 4F 4 F RT A22CE E25EA 2007071100058 20070711 00058 CE 2007 7 11 DXTA200702286 1 20070622 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 354QS 5600356 RT SIDE BRAKE FOR BOTH CO-PILOT AND PILOTS SIDE IS UNRESPONSIVE AND THEN WILL ALL OF A SUDDEN GRAB. [07-12-07] BLED BR AKES. TAXI CHECKED GOOD. IAW. CE-560 MM. CH. 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007071100060 20070711 00060 EU 2007 7 11 07FDEA02359 1 20070702 A 5730 A54640086 SKIN AIRBUS 300 A300B4605R 3930308 EU RT WING WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 ELONGATED HOLES ON PYLON NR 2 TO BOTTOM WING SKIN REPAIR PERFORMED BY OVERSIZING THE HOLES AND INSTALLING FREEZE PLUGS I AW DRAWING R571-50532, APPROVED BY EA 6-5720-106472 REV A AND RAS/BAE/1004873/2007 ISS A. 2 L 7 2 4F RT A35EU 2007071100064 20070711 00064 CE 2007 7 11 GLBA20060958 1 20070620 A 2697 CONNECTOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FIRE LOOP LOOSE A GLBA A UNSCHED LANDING S N AFFECT SYSTEMS FALSE WARNING CL CLIMB 1 NM 03 245GL UE245 AIR RETURN, ENROUTE, PILOTS REPORTED THAT THE NR 1 ENGINE FIRELOOP ANNUCIATOR AND T-HANDLE FLICKERED. AIRCRAFT RETURNE D TO DEPARTURE AND A SUBSEQUENT FERRY FLIGHT WAS PERFORMED FOR REPAIRS. MAINTENANCE INSPECTED THE AFFECTED SYSTEM AND DI SCOVERED A SHORTED WIRE ON THE LT FIRELOOP. UPON FURTHER INSPECTION, NO SHORT NOTED, REPOSITIONED FIRELOOP AND RE-SECURE D LOOSE CONNECTOR IAW MM 20-13. OPERATIONAL CHECK OF SYS OK. 2 L 7 2 4T 4 T RT A24CE E26NE 2007071100067 20070711 00067 CE 2007 7 11 AMWA85564BC 1 20070624 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER WEAK A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 142ZV 22220 317 UE142 DURING FLT, THE BATTERY CHARGE ANNUN ILLUMINATED. CONTINUED TO DESTINATION WITH NO FURTHER INCIDENT. THIS BATTERY CHAR GE ANNUNCIATOR WRITEUP UP IS A NUISANCE WRITEUP WITH SEVERE DISTRACTION TO THE AIR CREW.REMOVED AND REPLACED BATTERY AND ADJUSTED VOLTAGE REGULATOR 2 L 7 2 4T 4 T RT A24CE E26NE 2007071100069 20070711 00069 NM 2007 7 11 2007UALA02327 1 20070701 A 2611 2156656 SMOKE DETECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FWD CARGO BAY FAULTY A UALA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 29 178UA 24385 MAINTENANCE MSG -CARGO FWD-1 LOOP-A- ON ARRIVAL. [07-27-07] CONDUCTED TROUBLE-SHOOTING BASED ON MAINT MSG "CARGO FW D-1 LOOP-A" ON ARRIVAL. PERFORMED GND TEST & SYSTEM FAILED. REPLACED FWD CARGO NR 1 LOOP A DETECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071100074 20070711 00074 NM 2007 7 11 DXTA200702288 1 20070623 A 2750 FLAP SYSTEM AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE TE FLAPS INOPERATIVE E DXTA O OTHER F FLT CONT AFFECTED LD LANDING 1 GL 07 278QS 77 FLAPS DID NOT EXTEND WHEN COMMANDED. TRIED 10, 20, AND 40 DEGREES AND THE FLAPS NEVER MOVED. THE SLATS EXTENDED NORMALLY . [07-12-07] PERFORMED FUNCTION TEST OF SLAT POSITION DETECTORS AND FLAP POSITION MICRO SWITCHES IAW FALCON 2000 M.M. CHAPT 27-802, ALL RESISTANCE VALUES WERE NORMAL. AFTER RECONNECTING CANNON PLUGS PERFORMED OPERATIONAL CHECKS OF FLAPS AND SLATS IAW FALCON 2000 MM CHAPT 27-305 & 2727-805, OPS CHECK GOOD. REPLACE FLAPS 7* RELAY, (503CF) AND PERFORMED OPS CHECKS IAW FALCON 2000 MM CHAPT 27-505 & 27-805, OPS CHECKS GOOD. NO FAULTS NOTED. 2 K 7 2 4F 4 F RT A50NM E44NE 2007071100076 20070711 00076 CE 2007 7 11 DXTA200702290 1 20070623 A 3220 WHEEL CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG VIBRATION E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 949QS 7500049 SEVERE NOSE WHEEL VIBRATION ABOVE 40 KNOTS ON TAKEOFF ROLL. ABORTED TAKEOFF. [07-12-07] REMOVED AND REPLACED LT AN D RT NOSE TIRE ASSEBLIES WITH OVERHAULED ASSY. ALL WORK ACCOMPLISHED IAW CE-750 MM 32-41-02. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071100077 20070711 00077 NM 2007 7 11 DXTA200702291 1 20070623 A 2612 FIRE LOOP GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE APU BAY MALFUNCTIONED E DXTA F ACTIVATE FIRE EXT. J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 728QS 116 APU FIRE INDICATION ON GROUND. BLEW BOTTLE INTO APU DURING CHECKLIST. RT FIRE BOTTLE IS EMPTY. [07-12-07] REMOVED TAIL CONE AND INSPECTED APU FOR DAMAGE. FOUND NO DAMAGE. REMOVED APU FIRE DETECT LOOP AND INSTALLED A NEW GAC FURNISHED BO TTLE. PERFORMED SATISFACTORY OPS CHECKS OF THE APU AND ENGINE ARE DETECT SYS. REF G200 MM 26-10-25, 26-10-20 2 L 7 2 4F 4 F RT A53NM E35NE 2007071100078 20070711 00078 CE 2007 7 11 DXTA200702292 1 20070624 A 7720 ENGINE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE RIGHT UNKNOWN E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 115QS RK383 UPON SETTING TAKEOFF POWER, THE RT ENGINE ITT BEGAN FLUCTUATION BETWEEN 400 - 650 DEGREES. TAKEOFF ABORTED BELOW 70 KTS . [07-12-07] RAN AIRCRAFT TO TAKEOFF POWER FOUND NO FLUCTATION PERFORMED 5 POINT RUNS AND FAXED RESULTS TO MTX ALL PRA MITERS WITHIN LIMITS. PERFORMED TROUBLESHOOTING STEPS FOR HAWKER 400XP AMM 77-21-00. CHECKED T1 AND T6 HARNESS REF P & W MM 77-00-01 AND 77-00-02 NO DISCREPANCIES FOUND. REMOVED AND REPLACED NR 2 ITT INDICATOR AND PERFORMED OPS CHECK OPS CH ECKED GOOD REF HAWKER 400XP AMM 31-10-00-701 AND 77-21-00. 2 H 7 2 4F 4 F RT A16SW E25EA 2007071100083 20070711 00083 EU 2007 7 11 2007UALA02330 1 20070630 A 3510 OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 420UA 489 FIRST OFFICERS O2 MASK IS LEAKING. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100085 20070711 00085 2007 7 11 2007UALA02332 4 20070701 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 428UA 523 EMERGENCY LIGHTS FAULTING EXTERNAL LOADS FWD LEFT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100086 20070711 00086 EU 2007 7 11 2007UALA02333 1 20070629 A 2560 RELEASE SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE OVERWING EXIT FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 461UA 1266 RIGHT OVERWING SLIDE INDICATION ON ECAM NOT SHOWING ARMED AFTER DOOR WAS INSTALLED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112100016 20071121 00016 NM 2007 11 21 CALA0700681 1 20071110 A 5322 65465677 SHEAR TIE BOEING 737 7373T0 1384582 NM BS 1006 S27L CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND FUSELAGE SKIN BULGED WITH RIVETS PULLED TO THE RIGHT OF STRINGER 27L AT STA 1006. A CORRODED SKIN CLIP WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007071100087 20070711 00087 EU 2007 7 11 2007UALA02335 1 20070701 A 2720 LIMITER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RUDDER INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 438UA 678 RUDDER TRAVEL LIMITER SYSTEM 1 INOP. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100090 20070711 00090 EU 2007 7 11 2007UALA02337 1 20070629 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN ODOR A UALA D RETURN TO BLOCK W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 451UA 865 SMELL THRU OUT A-C. UNKNOWN SMELL. PAX EYES AND NOSES BURNING. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100096 20070711 00096 WP 2007 7 11 ABXA070218 1 20070626 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 903AX 47427 EMERGENCY LIGHTS WOULD NOT TURN ON WITH THE EMERGENCY LIGHT SWITCH IN ON POSITION. REPLACED EMERGENCY LIGHT POWER SUPPL Y BATTERIES IAW DC9 MM 33-53-02-4. 2 L 7 2 4F A6WE 2007071100099 20070711 00099 NM 2007 7 11 ABXA070216 1 20070601 A 5522 183T30731 SKIN BOEING 767 767200 1385120 NM LT ELEVATOR DEBONDED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 797AX 23147 LEFT ELEVATOR OUTBOARD HAD INTERPLY DISBOND AT EACH ACTUATOR FITTING AREA ON LOWER LEADING EDGE. REPLACED LEFT ELEVATOR ON NON ROUTINE 0395 IAW BOEING SRM. 2 L 7 2 4F RT A1NM 2007071100101 20070711 00101 CE 2007 7 11 DXTA200702297 1 20070625 A 2910 HYDRAULIC SYSTEM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL B SIDE FAILED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 908QS 7500108 DURING CRUISE AT FL480, THE B SIDE HYDRAULIC SYSTEM FAILED. AMBER CAS MESSAGE B PUMP FAIL, THE B QTY LOW, B PRESSURE DR OPPED TO 0 PSI, QTY DROPPED TO 2 PERCENT, BTEMP AT 60 DEGREES. [07-13-07] FOUND RT ENGINE DRIVEN HYD PUMP FAILED INTE RNALLY. REMOVED PUMP INSTALLED OVERHAULED UNIT. RAN ENGINE WITH MULE PRESS ASSIST. SYSTEM OPS CHECKS GOOD AT THIS TIME IAW CITATION X MM 29-10-02. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071100105 20070711 00105 NM 2007 7 11 ABXA070210 1 20070523 A 5320 141T51999 STIFFENER BOEING 767 767200 1385120 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 797AX 23147 CRACKED STIFFENER COCKPIT FLOORBEAM STA 266.5 APPROXIMATELY LEFT BUTT LINE 10.50. REMOVED, FABRICATED AND INSTALLED STI FFENER ON FLOORBEAM STA 266.5, LEFT BUTT LINE 10.50 IAW BOEING SRM. 2 L 7 2 4F RT A1NM 2007071100106 20070711 00106 CE 2007 7 11 DXTA200702298 1 20070625 A 2720 RUDDER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL VERTICAL STAB OSCILLATES E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 921QS 7500241 RUDDER OSCILLATED IN CRUISE FLT AND THROUGHOUT DESCENT. YD FAIL UPPER B CAME ON DURING THE FLIGHT AND REMAINED ON, OSCIL LATION STOPPED AFTER SLOWING BELOW 300KTS. [07-13-07] REMOVED AND REPLACED THE UPPER RUDDER CHANNEL B POSITION SENSOR. OPS CHECKED GOOD IAW CESSNA 750 MM CHPT 27-24-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071100107 20070711 00107 NM 2007 7 11 ABXA070211 1 20070524 A 5551 PIN BOEING 767 767200 1385120 NM LT HORIZ STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 797AX 23147 LEFT OUTER HORIZONTAL STABILIZER PIVOT PIN CRACKED. REPLACED PIVET PIN AND OUTBOARD PIVOT SPACER IAW B767 JOB CARD 7302 001. 2 L 7 2 4F RT A1NM 2007071100108 20070711 00108 CE 2007 7 11 DXTA200702299 1 20070625 A 2840 SENSOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL FLOAT MALFUNCTIONED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 937QS 7500137 WHEN THE POWER LEVERS ARE ADVANCED TO THE TAKEOFF POSITION AND THE AIRCRAFT BEGINS TO ACCELERATE THE NO TAKEOFF MESSAGE AND CHIMES COME ON. THE TAKEOFF WAS ABORTED. [07-13-07] THE NO TAKE OFF BOX ON THE NR 2 MFD WAS CHECKED BUT DISPLAYED NO MESSAGES . TAKE OFF WAS ATTEMPTED AGAIN. SAME PROBLEM. TRIMS WERE THEN CYCLED, ENGINE SYNC CYCLED, IAC'S WERE RESET ON IMT PAGE, AND CONFIGURATION RESET FOR TAKEOFF. ANOTHER TAKEOFF ATTEMPT. SAME PROBLEM. R & R BOTH LT & RT FUEL FLOA T SENSORS. ALL WORK WAS PERFOMRED I.A.W. 28-20-07. NO FURTHER DISCREPANCIES NOTED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071100109 20070711 00109 NM 2007 7 11 ABXA070212 1 20070524 A 5320 141T3330 DOUBLER BOEING 767 767200 1385120 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 797AX 23147 L1 DOOR CUTOUT LOWER CORNER INTERNAL DOUBLER AFT CORNER HAD CRACK INDICATION. TWO CRACKS, ONE .275 INCH AND ONE .210 IN CH. REPAIRED AREA IAW REA B653-55867-MR. 2 L 7 2 4F RT A1NM 2007071100113 20070711 00113 CE 2007 7 11 DXTA200702300 1 20070625 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 335QS 5600335 DURING AIRCRAFT TAXI, CAPTAINS SIDE RT BRAKE PEDAL LOSSES PRESSURE WHEN APPLYING BRAKES. WHEN LOSING PRESSURE, PEDAL GO ES IN ABOUT 2 INCHES FARTHER, THEN SEEMS TO PRESSURIZE AND EXTEND BRAKE TO NORMAL POSITION. [07-13-07] INSPECTED RUDDE R TORQUE TUBE, RUDDER PEDAL ATTACHMENTS AND CONNECTED HARDWARE FOR SECURITY AS REQUESTED. NO DEFECTS. PERFORMED AN ANTIS KID BRAKE SYSTEM BLEEDING. OPERATIONAL CHECKS NORMAL. NO LEAKS NOTED. PERFORMED IAW THE CE560 M/M CHAPTER 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007071100114 20070711 00114 EU 2007 7 11 YENA2007061 1 20070610 A 5210 FE240004 BOTTLE AIRBUS 320 A320232 3930326 EU L1 DOOR CRACKED A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 570JB 15990 2099 L-1 ENTRY DOOR ASSIST BOTTLE LEAKING (CRACKED). REPLACED L-1 ENTRY DOOR ASSIST BOTTLE PER AMM 52-11-14, LEAK CHECK OK. 2 L 7 2 4F RT A28NM 2007071100115 20070711 00115 NE 2007 7 11 DJFA2007067 2 20070619 A 7220 45A35042003 INLET BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE NR 2 ENGINE CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 445LX 5818 RK298 PCEJA0243 TRIP NR 1174419 ON POST FLIGHT CREW DISCOVERED A CRACK AT THE 1 O'CLOCK POSITION ON THE NR 2 INLET. MAINTENANCE REPLACE D THE NR 2 INLET. 2 H 7 2 4F 4 F RT A16SW E25EA 2007071100119 20070711 00119 CE 2007 7 11 GUUA06240701 1 20070624 A 3234 1013841377 HANDLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG FAILED A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 29 87551 UE206 FLIGHT: 9128, DURING APPROACH NOSE GEAR DID NOT IMMEDIATELY SAFE INDICATION AFTER APPROXIMATELY 5 SECONDS NOSE GEAR SHOW ED DOWN AND LOCKED WITH AN ASSOCIATED POPPED CIRCUIT BREAKER. REPLACED LANDING GEAR CONTOL HANDLE. OPERATIONAL CHECK NO RMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007071100121 20070711 00121 SO 2007 7 11 GUUA06250702 1 20070625 A 3297 WIRE HARNESS EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE MLG INDICATOR DAMAGED A GUUA O OTHER N FALSE WARNING CL CLIMB 1 SO 29 280AS 120231 FLIGHT 9231, DURING FLIGHT BOTH (B) LANDING GEAR LIGHTS FOR NOSE WHEEL ILLUMINATED. REMOVED INSPECTED AND REINSTALLED L ANDING GEAR PROXIMITY HARNESS. 2 L 7 2 4T 4 T RT A31SO E20NE 2007071100122 20070711 00122 CE 2007 7 11 DXTA200702301 1 20070626 A 3220 LANDING GEAR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NOSE INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 970QS 7500070 NOSE GEAR FAILED TO RETRACT ON TAKEOFF, RED UNLOCK AND GREEN NOSE INDICATORS ILLUMINATED. [07-13-07] OPERATED GEAR OPE RATIONALLY 30 CYCLES AND FOUND NO DEFECTS. REMOVED, REPLACED, OPS CK GOOD OF RENTAL ACTUATOR IAW 750MM 32-30-03. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071100128 20070711 00128 WP 2007 7 11 ABXA070230 1 20070613 A 5311 4911383501 ATTACH FITTING DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 FRAME FOOT CORRODED - 832 LEFT. REMOVED AND REPLACED FS 832 LEFT FRAME FOOT IAW DC9 SRM. 2 L 7 2 4F A6WE 2007071100130 20070711 00130 WP 2007 7 11 ABXA070231 1 20070615 A 5315 9911544505 FLOORBEAM DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 FLOORBEAM AT STA 313, FORWARD SIDE UNDER CUSP WEB HAD CORROSION AROUND NUT PLATE. REPAIRED DAMAGED AREA IAW DC9 SRM K05 159. 2 L 7 2 4F A6WE 2007071100131 20070711 00131 WP 2007 7 11 ABXA070232 1 20070605 A 5315 99115451 FLOORBEAM DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 FLOORBEAM AT FS 275, RIGHT BUTT LINE 44.5 HAD CORROSION AT GROUNDING STUD. REPAIRED AREA IAW DC9 SRM 53-05. 2 L 7 2 4F A6WE 2007071100132 20070711 00132 WP 2007 7 11 ABXA070233 1 20070619 A 5320 4924659501 ANGLE DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 SUBFLOOR ANGLE WAS CRACKED FORWARD END LEFT BUTT LINE FS 996. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 2007071100134 20070711 00134 WP 2007 7 11 ABXA070234 1 20070620 A 5320 991050111 CUSP WEB DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 CUSP WEB CRACKED AFT OF FS 313, RIGHT BUTT LINE 56. REPAIRED CUSP WEB AT FS 315 IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 2007071100135 20070711 00135 2007 7 11 45165062507 4 20070625 A 3417 703070071704 ADC LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE7312 01518 WP NR 2 MALFUNCTIONED E J7SA A B UNSCHED LANDING EMER. DESCENT G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 SW 05 429FX 165 AT FL350 CREW GOT (RUDDER BOOST INOP), (PRIMARY PITCH TRIM), (MACH TRIM FAIL) FAULTS. CABIN PRESSURE BEGAN DUMPING AND A SPLIT BETWEEN THE PILOT/ COPILOT AIRSPEED OF 140KTS. CREW INITIATED EMERGENCY DESCENT RED CABIN ALT CAS ILLUMINATED DUR ING DESCENT WITH CABIN DIFFERENTIAL INDICATION DASHED OUT SECOND OCCURRENCE OF SIMILAR PROBLEM. TO CORRECT PREVIOUS EVE NT, MX REPLACED AN AIR DATA COMPUTER. FSR BELIEVES A BAD ADC WAS INSTALLED (POSSIBLY AN NFF UNIT) MX INSTALLED A RECERTI FIED ADC IN THE NR 2 POSITION AND MOVED THE NR 2 ADC TO THE NR 1 POSITION. GROUND TESTING AND RUNS NORMAL CHECK FLIGHT WILL BE PERFORMED AND AIRCRAFT MONITORED CLOSELY. 2 L 7 2 4F 4 F RT T00008WI E6WE 2007071100136 20070711 00136 SW 2007 7 11 BAQA200700020 1 20070625 A 6410 222016001139M BLADE BELL 222 222UT 1182148 SW LYC LTS101 LTS101750C1 41560 NE TAIL ROTOR LOOSE E BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 222LF 1777 2 47528 WHILE COMPLETING A DAILY INSPECTION, FOUND THE IB FEATHERING BEARING ON THE TAIL ROTOR BLADE LOOSE IN THE BORE. NEW STYL E BEARINGS 222-312-761-101 INSTALLED IAW TB 222U-06-99 AT TIME SINCE REPAIRED. 1 G 7 2 3U 3 U H9SW E5NE 2007071100137 20070711 00137 SW 2007 7 11 BAQA200700021 1 20070625 A 6410 222016001139M BLADE BELL 222 222UT 1182148 SW LYC LTS101 LTS101750C1 41560 NE TAIL ROTOR LOOSE E BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 222LF 233 233 47528 WHILE COMPLETING A DAILY INSPECTION, FOUND THE OB FEATHERING BEARING ON THE TAIL ROTOR BLADE LOOSE IN THE BORE. NEW STYL E BEARINGS 222-312-761-101 INSTALLED IAW TB 222U-06-99 AT TIME SINCE REPAIR. 1 G 7 2 3U 3 U H9SW E5NE 2007071100138 20070711 00138 SW 2007 7 11 BAQA200700022 1 20070627 A 6410 222016001139M BLADE BELL 222 222U 1182140 SW LYC LTS101 LTS101750C1 41560 NE TAIL ROTOR LOOSE E BAQA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 EA 03 587MG 1683 35 47566 WHILE COMPLETING A GROUND RUN FOR MAINTENANCE, A VIBRATION WAS FELT, AIRCRAFT WAS SHUTDOWN, AND FOUND THE IB FEATHERING BEARING ON THE TAIL ROTOR BLADE LOOSE IN THE BORE. NEW STYLE BEARINGS 222-312-761-101 INSTALLED IAW TB 222U-06-99 AT TIM E SINCE REPAIRED. 1 G 7 2 3U 3 U H9SW E5NE 2007071100143 20070711 00143 NM 2007 7 11 ASMF200706004 1 20070617 A 5720 VORTEX GEN DOUG MD88 MD88 3023688 NM RT WING DAMAGED W ASMF K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 23 169PL 53175 DURING TRANSIT CHECK, THE AIRCRAFT WAS HIT BY A GROUND HANDLING TRUCK IN THE LOWER SECTION OF RIGHT WING, DAMAGING IN TH E VORTILON AND IN THE FORWARD INBOARD FLAP HINGE FAIRING. MAINTENANCE PERSONNEL REPLACED VORTILION IAW MM 57-20-04 AND T HE FORWARD INBOARD FLAP HINGE FAIRING IAW MM 57-20-04 AND MM 27-52-02,OPERATIONAL TESTS WERE CORRECT IAW MM 27-50-00. 2 L 7 2 4F RT A6WE 2007071100144 20070711 00144 NE 2007 7 11 ASMF200706005 2 20070625 A 7321 76960615 FUEL CONTROL DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE LEFT ENGINE FAILED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 162PL 7871 49765 718082 CAPTAIN REPORTED THAT AFTER LT ENGINE WAS STARTED, THE EGT INCREASED UNTIL 475 DEGREES (C) WITH N2 IN 47 PERCENT, SO AB NORMAL PROCEDURE (SLOW ENGINE(S) ACCELERATION ON GROUND) WAS PERFORMED CONTINUING THE FAILURE. MAINTENANCE PERSONNEL SE RVICED AND TESTED THE FUEL CONTROL PRESS SENSE LINE MOISTURE TRAP IAW MM 73-20-03, ALL CORRECT. DURING OVERNIGHT CHECK, THE RIGGING THROTTLES WERE VERIFIED IAW MM 76-11-00, THE LT FCU WAS REPLACED IAW MM 73-20-01, TRIM TO BOTH ENGINES WAS P ERFORMED IAW MM 71-00-00, OPERATIONAL CHECK WAS ACCOMPLISHED IAW MPCM 71-00-01 AND ENGINE ACCELERATION CHECK WAS PERFORM ED TO BOTH ENGINES IAW MM 71-00-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007071100145 20070711 00145 NE 2007 7 11 ASMF200706006 2 20070628 A 7250 TURBINE BLADES DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE LT ENGINE CRACKED W ASMF K NONE C F.O.D. IN INSP/MAINT 1 SW 23 803ML 44078 3780 49726 716781 DURING LT ENGINE BOROSCOPIC INSPECTION WAS DETECTED A FIRST STAGE TURBINE BLADE WITH A CRACK OF 0.500 INCH IN TIP. ENGIN E WAS REPLACED IAW MM 71-00-02 AND OPERATIONALLY TESTED IAW MM 71-00-01, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007071100146 20070711 00146 NM 2007 7 11 AMTA200700282 1 20070607 A 3040 8300005604 MODULE BOEING 737 73783N 13844HI NM WINDOW HEAT UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 319TZ 30643 LT SIDE WINDOW HEAT OFF LIGHT REMAINS ILLUMINATED WITH LT SIDE WINDOW HEAT OFF LIGHT REMAINS ILLUMINATED WITH SWITCH ON. T/S IAW FIM 31-40-00-810-813, FOUND PS-9/ CONTROL POWER LIGHT ON LT SIDE WINDOW HEAT CONTROL UNIT. REMOVED AND REPLAC ED CONTROL UNIT IAW AMM 30-41-11-081. OPS NORMAL. (K) 2 L 7 2 4F RT A16WE 2007071100147 20070711 00147 2007 7 11 AMTA200700283 4 20070606 A 3422 C16221KA02 DISPLAY BOEING 737 73783N 13844HI NM ALTIMETER UNSERVICEABLE A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 321TZ 28249 IFSD ALTIMETER PUSH BUTTON STUCK. REMOVED AND REPLACED ISFD INDICATOR IAW AMM 34-24-02-4. OPS CHECK GOOD. (K) 2 L 7 2 4F RT A16WE 2007071100148 20070711 00148 NM 2007 7 11 AMTA200700284 1 20070609 A 2613 ELEMENT BOEING 737 73783N 13844HI NM OVERHEAT MALFUNCTIONED A AMTA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 11 310TZ 28243 WING-BODY OVERHEAT LIGHT ON RT SIDE (LIGHT CAME ON WHEN CONFIGURED FOR A APU ON/NO BLEED TAKE-OFF. REMOVED AND REPLACED M269 ELEMENT. IAW MM 26-18-02-400-801. OPS CHECK NORMAL. NO FAULTS NOTED IAW FIM. OK FOR SERVICE. (K) 2 L 7 2 4F RT A16WE 2007071100149 20070711 00149 CE 2007 7 11 AW42007F00000 1 20070608 A 5510 MS21042L5 NUT CESSNA 172 172R 2072401 CE CONT IO360 IO360* 17025 CE HORIZONTAL STAB LOOSE B AW4R K NONE O OTHER IN INSP/MAINT 1 WP 11 784WW 691 17280816 DURING THE PERFORMANCE OF A 100 HOUR INSPECTION, SLIGHT MOVEMENT OF THE HORIZONTAL STABILIZER WAS NOTED RELATIVE TO THE RT SIDE OF THE FUSELAGE. INVESTIGATION FOUND THAT THE RT FWD ATTACH BOLT NUT APPEARED TO BE SLIGHTLY LOOSE OR UNDER-TOR QUED. REMOVED ATTACH BOLT AND INSPECTED HARDWARE AND HOLE. BOLT AND HOLE DID NOT SHOW ANY APPRECIABLE WEAR. CHECKED L T FWD ATTACH POINT AND NUT TORQUE ALSO SEEMED TO BE LOW ALTHOUGH THERE WAS NO NOTICEABLE PLAY AT THIS ATTACH POINT. NON E OF THE ATTACH HARDWARE FOR THE HORIZONTAL OR VERTICAL STABILIZER HAD TORQUE SEAL ON THE NUTS OR BOLT HEADS AND THERE W AS NO EVIDENCE THAT ANY HAD EVER BEEN INSTALLED. AS A PRECAUTION, ALL THE MS21042L5 NUTS FOR ALL THE HORIZONTAL AND VER 1 H 7 1 3O 3 O NT 3A12 E1CE 2007071100151 20070711 00151 NM 2007 7 11 ABXA070235 1 20070629 A 3397 WIRE BOEING 767 767200 1385120 NM CABIN OUT OF POSITION A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 797AX 23147 EMERGENCY 02 TEST LIGHT WOULD NOT PRESS TO TEST (INOPERATIVE) SUPERNUMERARY AREA. REPOSITIONED WIRING AT DEPRESS LIGHT L9003 IAW WDM 33-24-11. OPS CHECKED GOOD IAW BOEING MM. 2 L 7 2 4F RT A1NM 2007071100153 20070711 00153 CE 2007 7 11 IMJ2007F00000 1 20070418 A 7500 65550381 ELBOW CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE BLEED AIR SYS CRACKED E IMJA K NONE O OTHER IN INSP/MAINT 1 EA 25 15SK 5600395 PCEJC0274 DURING AN ENGINE REPLACEMENT (INSTALLATION OF A RENTAL ENGINE WHILE THE ORIGINAL ENGINE IS BEING OVERHAULED) WE CAREFULL Y EXAMINED THE BLEED AIR ELBOW ASSY FOR CRACKING. PREVIOUSLY HAD SUCH AN ASSY RUPTURE ON THE OPPOSITE ENGINE DURING CLI MBOUT AND TRIP THE FIRE WARNING RESULTING AN EMERGENCY RETURN TO THE AIRPORT. THE (ELBOW) IS AN ACCORDION STYLE FLEX LI NE COVERED WITH WIRE BRAIDING WITH A 90 DEGREE FITTING ON ONE END AND A STRAIT (V-BAND) FITTING ON THE OTHER. THE AREA THAT CRACKS IS THE ACCORDION FLEX LINE WHICH IS HIDDEN BY THE OVER BRAIDING. WE FOUND THE CRACK BY USING A PROBE TYPE F LASHLIGHT PASSED INTO THE INSIDE OF THE ELBOW ASSEMBLY. LIGHT SHINES THROUGH THE OVERBRAID REVEALING THE CRACK. LOOKI 2 L 7 2 4F 4 F RT A22CE E25EA 2007071100154 20070711 00154 NM 2007 7 11 ABXA070236 1 20070629 A 3397 WIRE BOEING 767 767200 1385120 NM CABIN DETACHED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 797AX 23147 R1 EMERGENCY EXIT LIGHT DID NOT ILLUMINATE WHEN EMERGENCY TEST SWITCH WAS DEPRESSED. FOUND WIRES TO EXIT LIGHT NOT ATTA CHED. CHECKED AND ATTACHED WIRES, OPS CHECKED GOOD IAW BOEING MM. 2 L 7 2 4F RT A1NM 2007071100157 20070711 00157 WP 2007 7 11 ABXA070221 1 20070608 A 5320 49125401 FITTING DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 FLOORBEAM SUPPORT UPPER END FITTING CRACKED, 965 LEFT SIDE. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30- 5. 2 L 7 2 4F A6WE 2007071100162 20070711 00162 WP 2007 7 11 ABXA070223 1 20070611 A 5320 3915134517 ATTACH FITTING DOUG DC9 DC931 3022065 WP RT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 RIGHT WHEEL WELL BULKHEAD TO KEEL ATTACH FITTING CRACKED. REMOVED AND REPLACED ATTACH FITTING IAW DC9 SRM. 2 L 7 2 4F A6WE 2007071100164 20070711 00164 WP 2007 7 11 ABXA070225 1 20070611 A 5320 9915558235 FITTING DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 UPPER SECTION OF AFT PRESSURE BULKHEAD LEFT SIDE HAD A CRACK UNDER HORIZONTAL STIFFENER NR 6. REMOVED AND REPLACED CLIP IAW DC9 SRM 51-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 2007071100165 20070711 00165 WP 2007 7 11 ABXA070226 1 20070612 A 5312 591013037 ANGLE DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 AFT PRESSURE BULKHEAD ANGLE AT THRESHOLD WAS CRACKED. REMOVED AND REPLACED ANGLE IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2007071100166 20070711 00166 WP 2007 7 11 ABXA070227 1 20070613 A 5311 4911383503 ATTACH FITTING DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 FRAME FOOT AND CUSP WEB CORRODED. REMOVED AND REPLACED FRAME FITTING AND REMOVED CORROSION FROM CUSP WEB IAW DC9 SRM. 2 L 7 2 4F A6WE 2007071100168 20070711 00168 WP 2007 7 11 ABXA070228 1 20070613 A 5320 49113831 CUSP WEB DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 FRAME FOOT AND CUSP WEB CORRODED -3/3, RIGHT. REPAIRED DAMAGED AREA IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 2007071100171 20070711 00171 WP 2007 7 11 ABXA070224 1 20070612 A 5320 9923668 MEMBRANE DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 SUBFLOOR CRACKED AT STA 120 AROUND BUTT LINE 0. REPAIRED SUBFLOOR IAW DC9 SRM. 2 L 7 2 4F A6WE 2007071100172 20070711 00172 NM 2007 7 11 2007UALA01719 1 20070526 A 2841 1810KTU01 SENSOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT WING FAILED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 774UA 26936 FUEL IMBALANCE LEFT AND RIGHT MAIN TANK QUANTITIES DIFFER BY A PRE-DETERMINED AMOUNT. ADVISORY CREW COMMENTS: UNEXPLAI NED IMBALANCE - LEFT WING TANK LOW. TOTAL FUEL USED NORMAL. REPLACED RIGHT WING NR 10 TANK FUEL QUANTITY UNIT AND WATE R-IN-FUEL DETECTOR PER MM 28-41-02 AND 28-41-04, OPS CHECKED PER MM 28-41-00. STICKED TANK PER FUEL MANUAL 2-4-1, CHECK S GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007071100189 20070711 00189 EU 2007 7 11 COEA0706911 1 20070605 A 3000 B03AA1031 VALVE AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE HAMSTD 14SF 14SF5 NE NR 2 ENGINE INOPERATIVE A COEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 13 911FX 687 045 120214 861214 NR 2 ENGINE ANTI-ICE FAULT LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. PILOT ELECTED TO TURN BACK. AIRCRAFT LANDED WITHOU T INCIDENT. THE NR 2 DUEL DISTRIBUTOR DEICE VALVE WAS REPLACED. AIRCRAFT RETURNED TO SERVICE. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 6 C P7NE 2007071100191 20070711 00191 EU 2007 7 11 2007UALA02162 1 20070621 A 5210 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 405UA 452 FOUND DOOR 1L BOTTLE AT 1500 PSI READS LOW. SERVICED DOOR ASSIST SYSTEM TO PROPER PRESSURE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100193 20070711 00193 NM 2007 7 11 2007UALA02163 1 20070621 A 2611 SMOKE DETECTOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CARGO BAY FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 925UA 26646 AT THE TEST OF CARGO DETECTION SYSTEM THE A & B FAIL LIGHTS ILLUMINATE FOR THE FWD CARGO PIT DETECTORS. REPLACED FWD " B" AND FWD " A" SMOKE DETECTORS IN THE FWD PIT. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071100194 20070711 00194 SO 2007 7 11 BOO2007F00000 2 20070531 A 8520 536421 GEAR BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO CRANKSHAFT WORN E BOOA K NONE O OTHER IN INSP/MAINT 1 GL 19 827TS 1376 TH836 823754R CRANKSHAFT GEAR FAILURE. GEAR TEETH WORN OUT .5 WIDTH, CAUSED ENGINE FAILURE WHEN DRIVEN GEAR LOST CONTACT. (K) 1 L 7 2 3O 3 O 3A16 E5CE 2007071100197 20070711 00197 NM 2007 7 11 2007UALA02166 1 20070621 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 840UA 1522 CREW REPORT: CREW OXYGEN INDICATES 600 PSI, READS LOW. INSPECTED ALL MASKS IN COCKPIT FOUND NO LEAKS, RESTOWED EACH PROPERLY, SERVICED CREW O2 SYSTEM TO 1500PSI, NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100199 20070711 00199 CE 2007 7 11 OYE2007F00001 1 20070530 A 3213 LEG ASSY CESSNA 185 A185F 2072821 CE CONT O520 IO520* 17032 SO LT MLG BROKEN E OYEA K NONE O OTHER IN INSP/MAINT 1 NM 13 104DE 8017 18504009 LT GEAR LEG BROKE ALONG LINE BETWEEN TOP (2) AXEL BOLTS. CORROSION IN CRACK INDICATES CRACK WAS PRESENT FOR SOME TIME. NTSB LAB HAS PART. (K) 1 H 7 1 3O 3 O 3A24 E5CE 2007071100216 20070711 00216 NE 2007 7 11 ILD2007F00001 2 20070607 A 7320 0292208230 MANIFOLD SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE FUEL INJECTOR COKED E ILDA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 13 251H 693 3975 19005 ON THE FIRST FLIGHT OF THE DAY PILOT COULDN`T START THE AC. INSPECTED ENGINE ASSY AND FOUND FUEL COKING AT GAS GENERATO R INJECTION MANIFOLD. REMOVED AND REPLACED INJECTION MANIFOLD ASSY WITH SAME TYPE. ON GROUND RUN, LEAK CHECK OPERATION AL FLIGHT CHECKED AND FUNCTIONALLY CHECKED GOOD. ALL WORK DONE IAW MM IAW INSTRUCTION MM. (K) 1 G 7 1 3U 3 U H9EU E19EU 2007071100217 20070711 00217 NM 2007 7 11 2007UALA02178 1 20070620 A 5210 BUTTON BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE R4 DOOR MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 783UA 26950 DOOR 4 RIGHT IS MISSING EPIS BUTTON. [07-20-07] NEW TYPE OF EPAS BATTERY PACK INSTALLED PER AMM 52-11-20 CONFIG 2 PG 401 & TEST OK PER AMM. PUSH BUTTON SECURED. OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007071100223 20070711 00223 EU 2007 7 11 I2W2007F00001 1 20070530 A 2435 BRUSHES SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE STARTER GEN ARCED E I2WA O OTHER O OTHER CR CRUISE 1 WP 13 197BH 1468 5349XL2 2666 (10) MINUTES INTO A TOUR FLIGHT, THE PILOT NOTICED LOW VOLTAGE AND LOW FUEL PRESSURE, WITH NO (GEN) LIGHT ILLUMINATED. THE PILOT RETURNED TO THE HELIPORT. UPON INSPECTION, IT WAS FOUND THAT THE STARTER GENERATOR HAD A BURNING SMELL TO IT . THE STARTER GENERATOR WAS CHANGED AND THE AIRCRAFT OPERATED NORMALLY. IT APPEARS AT LEAST ONE SET OF BRUSHES WERE AR CING. (K) 1 G 7 1 3U 3 U H9EU E19EU 2007071100225 20070711 00225 NM 2007 7 11 2007UALA02182 1 20070623 A 7330 WARNING LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 302UA 23643 RTFL DUE TO FUEL FILTER BYPASS LIGHT ON NR 2 ENGINE. 10-11-07 FOUND BAD FUEL FILTER DIFFERENTIAL SWITCH. REPLACED SWITCH. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071100226 20070711 00226 EU 2007 7 11 2007UALA02183 1 20070623 A 2421 GENERATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 FAULTED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 452UA 955 RTFL DUE TO NR 1 GENERATOR FAULT. FOUND IDG FAILED. REPLACED IDG. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100227 20070711 00227 NM 2007 7 11 2007UALA02184 1 20070623 A 2613 WARNING LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 308UA 23669 RTFL DUE TO ILLUMINATED WING BODY OVERHEAT LIGHT. FOUND PACK EXHAUST DUCT FROM AFT HEAT EXCHANGER COMING APART. REPLACE D DUCT. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071100230 20070711 00230 EU 2007 7 11 2007UALA02189 1 20070624 A 4920 APU AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SHUTDOWN A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 424UA 506 APU AUTO SHUTDOWN WITH SMOKE IN CABIN. FOUND THREADS STRIPPED AT THE GEARBOX HOUSING OIL OUTLET PORT. THIS CONDITION LEA D TO AN EXTERNAL OILLEAK. THE OIL WAS THEN DRAWN INTO THE INLET THUS CAUSING THE SMOKE IN CABIN. BORESCOPE OF THE POWER SECTION REVEALED DIFFUSER VANE EROSION AND HOT SECTION DETERIORATION. REPLACED APU 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100231 20070711 00231 EU 2007 7 11 2007UALA02190 1 20070623 A 5310 RIVET AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 435UA 613 FWD PIT HAS NUMEROUS CORRODED FASTENERS FROM FRAME 24 THROUGH 35 BETWEEN STRINGER 38L AND 38R. REPLACED A TOTAL OF 1918 RIVETS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100235 20070711 00235 EU 2007 7 11 2007UALA02192 1 20070623 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 435UA 613 STR 42R HAD CORROSION AND DRILL MARKS BETWEEN FR 26 AND 27. INSTALLED A SPLICE REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100239 20070711 00239 NM 2007 7 11 2007UALA02197 1 20070623 A 5210 DOOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE R2 STIFF A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 937UA 26668 F-A REPORTS DOOR 2R IS VERY DIFFICULT TO ARM (STIFF). [07-17-07] FOUND SLIDE OUT OF PLACE IN PACK. ADJUSTED SLIDE POSITION IN PACK AND REINSTALLED SLIDE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071100240 20070711 00240 NM 2007 7 11 2007UALA02198 1 20070624 A 3397 5878258791 POWER CABLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 303UA 23644 CABIN FLOOR EEL LIGHTS INOP FROM ROW 16 TO AFT GALLEY. REPLACED POWER LEAD CABLE. ALSO, REPLACED FEEDER CABLE FOR AFT SECTION OF ACFT. OPS CKS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071100241 20070711 00241 NM 2007 7 11 2007UALA02200 1 20070624 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR SLIDE INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 DOOR 1R SLIDE LIGHT SWITCH BROKEN. [07-27-07] REPLACED GIRT BAR SLIDE ARMED LIGHT ON R-1 DOORWAY LINING PANEL. OPS CH ECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071100245 20070711 00245 NE 2007 7 11 DXT2007F00000 2 20070507 A 7200 MS955608 BOLT CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE ENGINE LOOSE E DXTA K NONE O OTHER IN INSP/MAINT 1 GL 07 636QS 5605304 AIRCRAFT CAME INTO THE REPAIR STATION DUE TO THE ENGINE NR1 HIGH TT. DURING BORESCOPE INSPECTION OF THE HP COMPRESSOR A S PART OF THE TROUBLESHOOTING, THE TECHNICIAN OBSERVED 2 EACH LOOSE BOLTS (GAS GENERATOR CASE TO INTERMEDIATE CASE FLANG E, FLANGE C) THE ENGINE WAS REMOVED FOR REPAIR DUE TO THE LOOSE BOLTS AND THE DEGRADATION OF THE HOT SECTION. THE HIGH ITT WAS DETERMINED TO BE DUE TO THE HOT SECTION CONDITION AND NOT THE LOOSE BOLTS. THE ENGINE WAS DISASSEMBLED TO ACCE SS THE LOOSE BOLTS. BOLTS WERE INSPECTED IN SITU BY ATTEMPTING TO INSERT A .001 INCH FEELER STOCK BETWEEN THE BOLT HEAD AND THE FLANGE OF THE GAS GEN CASE. 25 OF THE 36 BOLTS HAD AT LEAST A 001 INCH GAP, AND THESE BOLTS WERE IDENTIFIED AS 2 L 7 2 4F 4 F RT A22CE E00059EN 2007071100248 20070711 00248 NM 2007 7 11 2007UALA02208 1 20070623 A 5210 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 554UA 26644 MED 2R FWD FRAME CRACKED, 3-8 INCH LONG, AT UPPER HINGE CUTOUT LWR RADIUS. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071100015 20070711 00015 SO 2007 7 11 C2XA07IA153 1 20070626 A 3397 7137215501 CONNECTOR EMB 145 EMB145XR 3260214 SO CABIN LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11140 145732 DURING SCHEDULED MAINTENANCE, THE EMERGENCY LIGHT ABOVE ROW 12 DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE FOUND A LOOS E CONNECTOR ON THE LIGHT ASSEMBLY. THE CONNECTOR WAS RESET, THE SYSTEM OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED . 2 L 7 2 4F RT 2007071100019 20070711 00019 2007 7 11 AMTA200700275 4 20070604 A 3460 1762000101 FMC BOEING 737 73783N 13844HI NM NR 2 INOPERATIVE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 308TZ 28244 NR 2 FMS INOPERATIVE, OK WHEN SWITCHED TO BOTH ON LT. REMOVED AND REPLACED FMS COMUTER IAW AMM 34-61-02-4. NR 2 FMC SY STEM OPS NORMAL. ALL SOFTWARE VERIFIED CORRECT. (K) 2 L 7 2 4F RT A16WE 2007071100039 20070711 00039 CE 2007 7 11 AMWA31034B 1 20070620 A 5410 STRUCTURE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NACELLE DAMAGED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 138YV UE138 FRICTION CHAFING DURING OPERATION HAS CREATED WORN SEGMENTS ON THE LT AND RT ENGINE NACELLES. DAMAGE WAS ALONG THE ENTI RE LENGTH OF THE NACELLE SHAPE, DEPTH VARIED AS INDICATED ON THE REPAIR AUTHORIZATION. REPAIRED IAW AIRCRAFT ENGINEERIN G REPORT NR 6732-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007071100054 20070711 00054 CE 2007 7 11 DXTA200702283 1 20070621 A 2700 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL UNKNOWN E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 966QS 7500166 PCU MONITOR CB POPPED AND FLIGHT CONTROL FAULT EICAS MESSAGE APPEARED DESENDING THROUGH 6000 FT RUDDER FLT CONTROL SHUT OFF SW ALSO ILLUMINATED. [07-12-07] T/S TO BAD ELEVATOR OUTOBARD PCU ("B" SYS) REMOVED AND REPLACED PCU. PERFORMED RIG CHECKS. SYSTEM LEAKS & OP'S CHECKS SATISFACTORY AT THIS TIME. ALL WORK DONE IAW CE750 M/M 27-30-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071100055 20070711 00055 2007 7 11 DXTA200702284 4 20070621 A 2200 UNKNOWN BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE AUTOPILOT UNKNOWN E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 132QS RK427 AT 13,000 FT, WITH THE AUTOPILOT ENGAGED, THE AIRCRAFT BEGAN AN UNCOMMANDED ROLL TO THE RT. THE ALTITUDE REMAINED LEVEL. [07-12-07] INSPECTED AUTOPILOT SYSTEM NO FAULT CODES WERE RECORDED IN THE FCC COMPUTER. FOUND CIRCUIT BOARD CARD A 194 LOOSE. RESECURED CIRCUIT BOARD CARD A194, AUTOPILOT SYSTEM GROUND CHECKED GOOD IAW H400XP MM CH. 22-13-00 2 H 7 2 4F 4 F RT A16SW E25EA 2007071100056 20070711 00056 WP 2007 7 11 DXTA200702285 2 20070621 A 7200 ENGINE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP NR 2 FAILED E DXTA E C ENGINE SHUTDOWN ABORTED TAKEOFF E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 GL 07 898QS 258593 NR 2 ENGINE SHUDDERED FAIRLY VIOLENTLY FOLLOWED BY FAILURE INDICATIONS, ITT ROSE TO 1066. ENGINE SHUTDOWN ACCOMPLISHED. FL260 APPROX ISA + 20. [07-12-07] REMOVED AND REPLACED NR 2 ENGINE SN: P-107918 WITH SN: P-107422, OP'S CHECK GOOD, A LL WORK DONE IAW HAWKER 800XP AMM 71-00-01. REF HBS 19-993-2.1 AND 19-993-2.3 2 L 7 2 4F 4 F RT A3EU E6WE 2007071100071 20070711 00071 NE 2007 7 11 SUPGUUA040307 2 20070403 A 7200 3044900 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RIGHT CONTAMINATED A GUUA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 29 190YV UE190 PCE114194 FLIGHT: 9171, DURING FLIGHT AT 17,000 FEET RT ENGINE TORQUE FLUCTUATES FROM 3,000 LBS TO 2,500 LBS FOR 3 SECONDS. TORQU E STABILIZED AT 2,700 LBS FOR 10 SECONDS FOLLOWED BY ERRATIC TORQUE READINGS FROM 3,000 LBS TO 1,500 LBS WITH ITT AT 850 DEGREES. PERFORMED MEMORY ITEMS FOR ENGINE FAILURE IN FLIGHT TO SECURE ENGINE. DIVERTED TO FPO LANDED WITHOUT INCIDEN T. THE REPORTED TORQUE FLUCTUATION AND HIGH ITT WAS CAUSED BY FRACTURE OF THE 1ST STAGE PT BLADES. THE PT BLADES FRACTU RED BY OVERLOAD DUE TO LOSS OF RADIAL SUPPORT CAUSED BY OIL STARVATION AND SUBSEQUENT DISTRESS OF THE NR 3 BEARING. THE OIL STARVATION WAS CAUSED BY BLOCKAGE DUE TO CARBON BUILD UP. 2 L 7 2 4T 4 T RT A24CE E26NE 2007071100075 20070711 00075 GL 2007 7 11 DXTA200702289 2 20070623 A 7320 FUEL FILTER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LEFT BYPASSING E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 901QS 7500102 LT FUEL FILTER BYPASS AMBER CAS MESSAGE AS POWER WAS APPLIED FOR TAKEOFF. [07-12-07] ACCOMPLISHED INSPECTION OF BYPASS INDICATORS IAW 3007C MM 73-30-00-200-801. REMOVED & REPLACED FUEL FILTER IAW SAME. LEAK CHECK GOOD. OPS CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071100091 20070711 00091 NM 2007 7 11 ABXA070207 1 20070629 A 5730 113T1613 PANEL BOEING 767 767281 1385109 NM RT WING MISSING A ABXA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 GL 23 793AX 23143 THE RIGHT WING 651VB AND 651WB PANELS MISSING, THE SCREWS PULLED THROUGH PART OF PANEL. REPLACED RIGHT WING LANDING GEA R SUPPORT BEAM ACCESS PANELS IAW REA B657-50994 AND B657-55014. 2 L 7 2 4F RT A1NM 2007071100104 20070711 00104 NM 2007 7 11 ABXA070208 1 20070522 A 5320 141T3330 STRUCTURE BOEING 767 767200 1385120 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 797AX 23147 R1 DOOR CUTOUT HAD DEFECT EXTENDING FROM RIVET AND LOWER AFT CORNER. REPAIRED AREA IAW REA B653-55851-MR. 2 L 7 2 4F RT A1NM 2007071100123 20070711 00123 EU 2007 7 11 YENA2007062 1 20070626 A 2797 19102186401 WIRE HARNESS EMB ERJ190 ERJ190100IGW 3260408 EU RT WING FAULTY A YENA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 EA 15 198JB 3724 19000021 DURING CONFIGURATION FROM FLAPS 3 TO FLAPS 5 GOT FAIL MESSAGE. AIRSPEED WAS APPROX 150 KTS. QRH ACCOMPLISHED AND LANDE D AT FLAPS 5 SETTING. REMOVED AND REPLACED RIGHT WING HARNESS (W611) IAW 27-83-01. RESET INHIBITS & OPS CHECKED PER AM M 27-83-02. NO FAULTS. 2 L 7 2 4F RT A57NM 2007071100129 20070711 00129 CE 2007 7 11 DXTA200702274 1 20070608 A 3297 66187235 CIRCUIT BOARD CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE MLG INOPERATIVE E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 672QS 5605663 HYDRAULIC PUMP WOULD NOT BRING THE LANDING GEAR UP, WITH GEAR HANDLE UP, GEAR STAYED DOWN AND LOCKED. REMOVED PCB P/N 6 618723-5 S/N 0267. INSTALLED NEW PCB 6618723-5 S/N 0335. OP CHECK GEAR GOOD. ALL WORK PERFORMED IAW CESSN ACE-560XL MAIN T MANUAL CHAP 24-50-03 AND 32-01-00. FOR DETAILS REF FAS W/O 07-1520. ALSO REMOVED GEAR CONTROL HANDLE P/N 9912550-1 S/N H8055. INSTALLED A REPAIRED UNIT SAME P/N S/N F6034. OPS CHECK GOOD. REPLACED PCB P/N 6618735-1 S/N 0266 WITH A NEW PCB SAME P/N S/N 0325 OPS CHECK GOOD I/A/W 32-01-00 2 L 7 2 4F 4 F RT A22CE E00059EN 2007071100133 20070711 00133 2007 7 11 DXTA200702275 4 20070615 A 2210 4006719918 ROLL SERVO CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL AUTOPILOT INOPERATIVE E DXTA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 07 986QS 133 7500086 DURING DESCENT FROM CRUISE AUTOPILOT ROCKS WINGS BACK AND FORTH BETWEEN FL410 AND FL360 WITH A/P DISCONNECTED AIRCRAFT F LIES LEVEL WITH NO ROLL. REMOVED AND REPLACED THE ALLERON SERVO MOTOR WITH A MODIFIED SERVO MOTOR IAW CESSNA CITATION 7 50 AMM 22-10-01. OPERATIONAL CHECK WAS SATISFACTORY AT THIS TIME. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071100190 20070711 00190 NM 2007 7 11 2007UALA02161 1 20070621 A 5347 SEAT TRACK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 AFT RT LAV AREA FLOOR STRUCTURE OB SEAT TRACK STA 995-1016 LBL 39 LBL40 WL 208-208 UPPER SURFACE HAS CORROSION. REMOVED AND REPLACED FLOOR TRACK AND WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071100195 20070711 00195 NE 2007 7 11 2007UALA02165 2 20070621 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 OIL CONSUMPTION A UALA O OTHER O OTHER CR CRUISE 1 WP 29 516UA 24860 726631 NR 1 ENGINE HIGH OIL COMSUMPTION. [08-08-07] REPLACED DEOILER CARBON SEAL AND STARTER CARBON SEAL. ATTRIBUTE THE PROBLEMS TO FUEL OIL HEAT EXCHANGER MR79230 (645-9029) HAZMAT & FUEL OIL HEAT EXCHANGER BYPASS VALVE PCN 645-9061(HAZMA T) & THEIR ASSOCIATED SEALS & PACKINGS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071100203 20070711 00203 NM 2007 7 11 2007UALA02169 1 20070621 A 2622 EXTINGUISHER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN UNSERVICEABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 795UA 26927 WATER EXTINGUISHER-DOOR 1R MISSING SAFETY WIRE. [07-20-07] REPLACED EXTINGUISHER WITH SERVICABLE ONE. AIRCRAFT OK F OR RETURN TO SERVICE.SUSPECT SAFETY WIRE SNAGGED BY PASSENGER SERVICE EQUIPMENT AND BROKEN OFF. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007072400102 20070724 00102 WP 2007 7 24 AALA20071290 1 20070713 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 208AA 49159 DFW - EMERGENCY LIGHT AT LEFT FORWARD EXIT SIGN HAS CRACKED LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LEFT FORWARD EX IT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071100228 20070711 00228 NM 2007 7 11 2007UALA02186 1 20070624 A 3350 BR964421 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 842UA 1569 EMERGENCY EXIT GUIDANCE LIGHT AT 1B MISSING. REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100237 20070711 00237 NM 2007 7 11 2007UALA02195 1 20070624 A 5522 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE RT ELEVATOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 923UA 26643 RT ELEVATOR UPPER SURFACE APPROX 56" FROM IB END TEMP REPAIR DETERIORATED. REMOVED DAMAGED SKIN AND COMPLETED COMPOSITE LAY-UP REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071100238 20070711 00238 NM 2007 7 11 2007UALA02196 1 20070624 A 5310 DOOR FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 923UA 26643 FWD CARGO DOOR CUTOUT AFT FRAME IS CRACKED ON AFT SIDE OF FRAME AT IB RADIOUS JUST ABOVE UPPER IB CORNER OF LOWER BOTTOM DOOR STOP FITTING. NEW FRAME SECTION. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071100250 20070711 00250 NM 2007 7 11 2007UALA02209 1 20070622 A 5414 ACCESS PANEL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 NR 2 PYLON FWD OF ACCESS PNL NR 442BR WEB FWD OF FUEL FEED LINE IS CRACKED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071100253 20070711 00253 NM 2007 7 11 2007UALA02213 1 20070622 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 221UA 30552 EMERGENCY LIGHT AT SEAT 3E AFT LIGHT IS OUT. RELAMPED. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007071100254 20070711 00254 NM 2007 7 11 2007UALA02215 1 20070622 A 2432 BATTERY BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE MAIN FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 227UA 30555 FOUND MAIN BATTERY AT 17V AND DISCHARGING AT 4A. [07-20-07] REPLACED MAIN BATTERY PER MM24-31-01. TESTS OK FOR RETUR N TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007071100264 20070711 00264 NM 2007 7 11 NWAA072365650 1 20070624 A 3397 WIRE BOEING 757 757251 1384970 NM CABIN PINCHED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 550NW 26497 PILOT REPORTED SLIDE LIGHT AT DOOR 2L INOP. MAINTENANCE REPAIRED PINCHED WIRES. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007071100267 20070711 00267 NM 2007 7 11 NWAA072375501 1 20070628 A 2130 UNKNOWN BOEING 757 757251 1384970 NM CABIN PRESSURE MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION IN INSP/MAINT 1 GL 01 501US 23190 DURING CLIMB, LOST PRESSURIZATION CONTROL AT 35,000 FT, CABIN PRESSURE AT 10,000 FT AND CLIMBING, AND AURAL WARNING SOUN DED. NEITHER AUTO 1 OR AUTO 2 WOULD WORK, TO MANUAL-CLOSED OUTFLOW VALVE, CABIN STILL CLIMBING. CONDUCTED RAPID DESCEN T TO 10,000 FT, AND AUTO CONTROL BEGAN WORKING. ACCOMPLISHED COM RED BORDERED CHECK LIST AND RETURNED TO DTW. LANDING WAS UNEVENTFUL. MAINTENANCE IS STILL WORKING ON PRESSURIZATION PROBLEM. 2 L 7 2 4F RT A2NM 2007071100275 20070711 00275 NM 2007 7 11 AWXA200700790 1 20070629 A 3350 AD321431 BATTERY AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 808AW 1088 MCN - EEL - BC-6 CHECK - NR# 5980805, EMERGENCY RIGHT MID CABIN POWER SUPPLY UNIT INDICATES UNIT FAILURE DURING TEST. C HARGED AND OPERATIONAL CHECKED THE EMERGENCY RIGHT MID CABIN EMERGENCY BATTERY IAW A319 AMM, 33-51-00. 2 L 7 2 4F RT A28NM 2007071100277 20070711 00277 NM 2007 7 11 07FDEA02355 1 20070702 A 5753 652163480 FLAP BOEING 727 727227 1384078 NM RT WING DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 RT WING, I/B FLAPS, AFT FLAP O/B END T/E IS DELAMINATED. REMOVED, REPAIRED, AND REINSTALLED RT WING I/B FLAP, AFT FLAP ASSY REF'S MM 27-51-002-4 AND SRM 51-40-20. THIS IS CLASSIFIED AS A MAJOR REPAIR. PLAY AND POSITION CHECK TO BE PERFOR MED ON ROUTINE CARD W/C 76C017-00. 2 L 7 3 4F A3WE 2007071100280 20070711 00280 EU 2007 7 11 07FDEA02361 1 20070703 A 5751 A57661001175 SKIN AIRBUS 300 A300B4605R 3930308 EU RT AILERON DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 RT AILERON IS AT RIB 1 UPPER SKIN TRAILING EDGE DAMAGED REPAIR PERFORMED BY INSTALLING EXTERNAL PATCH IAW SRM 517712 PB. 200 PARA 4. 2 L 7 2 4F RT A35EU 2007071100283 20070711 00283 NM 2007 7 11 07FDEA02362 1 20070703 A 5322 69436835 SHEAR TIE BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD PIT BILGE BODY FRAME SHEAR TIE IS BUCKLED/CRACKED BS 720, 1" I/B OF STR 26L, WL 151 (MKD). REPLACED DAMAGED SHEAR T IE AT FWD PIT STA 720, 1" INBD OF STR 26L. REF SRM 51-30-02 PG 1-12, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007071100285 20070711 00285 NM 2007 7 11 07FDEA02363 1 20070703 A 5322 69436835 SHEAR TIE BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD PIT BILGE BODY FRAME SHEAR TIE IS CRACKED/BROKEN BS 720A, STR 26R-27R, WL 150 (MKD). REPLACED DAMAGED SHEAR TIE AT FWD PIT STA 720A , 1" INBD OF STR 26R. REF SRM 51-30-2 PG 1-12, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007071100294 20070711 00294 WP 2007 7 11 070133 1 20070620 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 862GA 49556 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007071100295 20070711 00295 WP 2007 7 11 070135 1 20070619 A 3350 7961021511 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 891GA 49423 IT HAS BEEN REPORTED BY THE FLIGHT CREW THE EMERGENCY EVACUATION LIGHTING SYSTEM HAS BEEN FOUND TO BE DEFECTIVE. FLOOR PATH LIGHTING STRIP IS INOPERATIVE. MAINTENANCE DEPARTMENT PERSONNEL HAVE INSPECTED THE SYSTEM AND MADE ALL REQUIRED CO RRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007071100296 20070711 00296 WP 2007 7 11 070136 1 20070621 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN EXPOSED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 860GA 49786 IT HAS BEEN REPORTED BY THE FLIGHT CREW THE EMERGENCY EVACUATION LIGHTING SYSTEM HAS BEEN FOUND TO BE DEFECTIVE. AISLE LIGHT WIRES HAVE BECOME EXPOSED. MAINTENANCE DEPARTMENT PERSONNEL HAVE INSPECTED THE SYSTEM AND MADE ALL REQUIRED CORRE CTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007071100297 20070711 00297 NM 2007 7 11 2007UALA02164 1 20070621 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN DAMAGED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 FLOOR EMERGENCY LIGHTS AFT CABIN MANGLED. REPAIRED, REPLACED INOP SECTION OF LIGHT. OPS RESTORED TO NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071100298 20070711 00298 NM 2007 7 11 SWAA073234 1 20070628 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071100299 20070711 00299 NM 2007 7 11 SWAA073236 1 20070628 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071100300 20070711 00300 NM 2007 7 11 SWAA073238 1 20070628 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071100302 20070711 00302 NM 2007 7 11 SWAA073240 1 20070628 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071100304 20070711 00304 NM 2007 7 11 SWAA073235 1 20070628 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071100306 20070711 00306 NM 2007 7 11 SWAA073255 1 20070628 A 2560 6557463 FITTING BOEING 737 7377H4 1384404 NM L1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 747SA 29799 DURING SCHEDULED 8Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. R&R GIRT BAR FITTING PER S RM. 2 L 7 2 4F RT A16WE 2007071100307 20070711 00307 NM 2007 7 11 SWAA073233 1 20070628 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071100312 20070711 00312 2007 7 11 SWAA073245 4 20070628 A 2565 6949956 CABLE BOEING 737 7375H4 138449D NM EVAC SLIDE BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE BROKEN. R&R EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2007071100314 20070711 00314 2007 7 11 SWAA073225 4 20070626 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071100315 20070711 00315 NM 2007 7 11 SWAA073251 1 20070628 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 442WN 32459 DURING SCHEDULED HC2 CHECK, RT OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007071100316 20070711 00316 NM 2007 7 11 SWAA073252 1 20070628 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 442WN 32459 DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. R&R BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007071100317 20070711 00317 NM 2007 7 11 SWAA073253 1 20070628 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 442WN 32459 DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007071100318 20070711 00318 NM 2007 7 11 SWAA073250 1 20070628 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 442WN 32459 DURING SCHEDULED HC2 CHECK, FWD LT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007071100319 20070711 00319 NM 2007 7 11 USAA070488 1 20070627 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND STA 500C ACTION: INSTALLED DOUBLER PER INSTALLED DOUBLER PER T/R 53-10-20E, DEFECT SIZE: 1". 2 L 7 2 4F RT A16WE 2007071100320 20070711 00320 NM 2007 7 11 USAA070483 1 20070627 A 5340 ATTACH ANGLE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 VERT STIFFENER ATTACH ANGLE, AFT SIDE OF BS 328 FLOORBEAM AT LBL 45. REMOVED CRACKED ANGLE AND REPLACED WITH NEW PART P ER SRM 51-10-02 DEFECT SIZE: 1/8". 2 L 7 2 4F RT A16WE 2007071100321 20070711 00321 NM 2007 7 11 USAA070484 1 20070627 A 5340 ATTACH ANGLE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 VERT STIFFENER/ATTACH ANGLE FWD SIDE BS 328 FLOORBEAM LBL 45. REMOVED AND REPLACED ATTACH ANGLE PER SRM 51-10-02, DEFEC T SIZE: .050. 2 L 7 2 4F RT A16WE 2007071100323 20070711 00323 NM 2007 7 11 USAA070486 1 20070627 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND CRACKED STA 747 BETWEEN STRINGERS 8R AND 9R. INSTALLED DOUBLER PER T/R 53-10-20E, DEFECT SIZE: 2". 2 L 7 2 4F RT A16WE 2007071100325 20070711 00325 NM 2007 7 11 F3LA200700144 1 20070627 A 5321 TRANSITION PANEL AIRBUS A319 A319111 3930336 NM FWD CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT TRANSITION PANEL 132DG DAMAGED. REPAIRED TRANSITION PANEL 1 32DG IAW SRM 53-02-00, FIG 204. 2 L 7 2 4F RT A28NM 2007071100326 20070711 00326 NM 2007 7 11 2007UALA02168 1 20070621 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCONNECTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 EEL LIGHT RT AISLE TORN LOOSE AT BUSINESS CLASS GALLEY. FOUND CONNECTORS DISCONNECTED AND TRANSPARENT COVER APPR 8 INCH ES TOO SHORT. RECONNECTED PLUGS, APPLIED INTERIM REPAIR TO PROTECT. REPAIR DOES NOT OBSTRUCT LIGHTED PORTION OF STRIP. NEEDS TRANSPARENT COVER CUT TO PROPER LENGTH TO REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071100328 20070711 00328 NM 2007 7 11 USAA070487 1 20070627 A 5320 STIFFENER BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND BS 328 FLOORBEAM AT LBL 27, VERTICAL STIFFENER. REPLACED STIFFENER PER SRM 52-10-01, DEFECT SIZE: 1". 2 L 7 2 4F RT A16WE 2007071100335 20070711 00335 NM 2007 7 11 2007UALA02204 1 20070624 A 3350 COVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DETACHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 EXIT SIGN COVER DETACHED AT 2L. REINSTALLED EXIT SIGN COVER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071100337 20070711 00337 NM 2007 7 11 2007UALA02214 1 20070622 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 221UA 30552 EMERGENCY LIGHT IN AFT GALLEY AT FLOOR LEVEL CTR POST IS OUT. RELAMPED. OPS CHECKS GOOD . 2 L 7 2 4F 4 F RT T0001SE E46NE 2007071100338 20070711 00338 NM 2007 7 11 2007UALA02216 1 20070625 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 117UA 28810 UPPER DECK STAIR CASE EEL LIGHTING MISSING OR LOOSE. SECURED EEL LIGHTING AND OPS CKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071100339 20070711 00339 EU 2007 7 11 2007UALA02338 1 20070629 A 3350 3071BPEGPL LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 452UA 955 EEPM LIGHT AT SEAT 19C INOPERATIVE. RELAMPED OPS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100342 20070711 00342 NM 2007 7 11 2007UALA02341 1 20070702 A 4920 APU BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE SHUTDOWN A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 379UA 24654 HEARD FIRE BELL NO LIGHT NOTED THEN APU SHUT DOWN. [07-24-07] FOUND SHORTED CONNECTOR FOR TAILPIPE ELEMENT. REPLACE D CONNECTOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071100345 20070711 00345 NM 2007 7 11 2007UALA02344 1 20070629 A 5210 PLATE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD ENTRY DOOR LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 FWD ENTERY DOOR, UPPER BODY TORQUE TUBE BEARING PLATE IS LOOSE. INSTALLED UPPER FWD DOOR SURROUND. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071100346 20070711 00346 NM 2007 7 11 2007UALA02345 1 20070630 A 2560 65C168201 HOOK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE R1 DOOR BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 1R DOOR RETAINER HOOK FOR DOOR SLIDE FOUND BROKEN. INSTALLED NEW RETAINER FOR GIRT BAR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007081500125 20070815 00125 NM 2007 8 15 CALA0700392 1 20070802 A 5320 6555872 STRAP BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND A 1 INCH CRACK IN WEB STRAP JUST FORWARD OF L-2 DOOR AT STA 947.5, S10L TO S11L. A NEW WEB STRAP WAS I NSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071100351 20070711 00351 NM 2007 7 11 2007UALA02351 1 20070702 A 2800 UNKNOWN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUEL SYSTEM NONE A UALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 WP 29 932UA 26658 RTFL DUE TO SUSPECTED FUEL LEAK. [07-24-07] PERFORMED TROUBLESHOOTING. NO LEAK FOUND. ALL OPERATIONAL CHECKS PASSED. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071100353 20070711 00353 NM 2007 7 11 2007UALA02353 1 20070630 A 3397 60253 POWER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 LIGHT STRIP NR 20 MOST FWD RT IS DAMAGED. REPLACED POWER CABLE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071100354 20070711 00354 NM 2007 7 11 2007UALA02354 1 20070701 A 3397 POWER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 FEEDER CABLE FOR RT LIGHT STRIP IS DAMAGED AND NEEDS REPLACED. REPAIRED POWER CABLE. OPS CHKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071100355 20070711 00355 NM 2007 7 11 2007UALA02355 1 20070701 A 2612 FIRE LOOP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE LT ENGINE FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 664UA 29236 STATUS MESSAGE L ENG FIRE LOOP 2 LIGHT IS ON. [07-27-07] TROUBLE-SHOOTING FOUND UPPER AFT FIRE DETECTION LOOP OPEN. REPLACED LOOP 1 & LOOP 2 FIRE DET ASSY PER WDG 26-11-11 OPS CHECKED OK AND SECURED LH ENG COWL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071100358 20070711 00358 NM 2007 7 11 AALA20071167 1 20070625 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 919AN 29520 DFW - EMERGENCY EXIT IDENTIFIER LIGHT AT RIGHT FORWARD SERVICE DOOR L1186 HAS BROKEN BASE. REPLACED EMERGENCY EXIT LIGH T ASSEMBLY L1186 FOR EMERGENCY LIGHT AT RIGHT FORWARD SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007071200002 20070712 00002 NM 2007 7 12 USAA070490 1 20070628 A 5313 STRINGER SPLICE BOEING 737 737401 1384701 NM BS 360 S15L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND CRACK BS 360 S-15L. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-10-02, DEFECT SIZE: .250". 2 L 7 2 4F RT A16WE 2007071200003 20070712 00003 NM 2007 7 12 USAA070497 1 20070628 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 847 RBL 36 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 23704 FOUND BS 847 RBL 36. REPAIRED PER SRM 51-40-02, DEFECT SIZE: 1/16". 2 L 7 2 4F RT A16WE 2007071200004 20070712 00004 NM 2007 7 12 USAA070491 1 20070628 A 5340 ATTACH ANGLE BOEING 737 737401 1384701 NM BS 294 S12L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND CRACK STA 294.5 AT STRINGER 12L. REMOVED, FABRICATED AND INSTALLED NEW ATTACH ANGLE PR BOEING DWG 65-17684, DEFEC T SIZE: .250. 2 L 7 2 4F RT A16WE 2007071200005 20070712 00005 NM 2007 7 12 USAA070492 1 20070628 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM BS 294 S11L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND CRACK STA 294.5 STRINGER 11L. REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL PER BOEING DWG 66-14208 AND JOB C ARD, DEFECT SIZE: 3". 2 L 7 2 4F RT A16WE 2007071200008 20070712 00008 NM 2007 7 12 USAA070495 1 20070628 A 5320 6545834U551 FLOOR SUPPORT BOEING 737 737401 1384701 NM BS 328-344 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND BS 328 AND BS 344 AT LBL 45. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-10-02, DEFECT SIZE: 1/2". 2 L 7 2 4F RT A16WE 2007071200009 20070712 00009 NM 2007 7 12 USAA070496 1 20070628 A 5311 FRAME BOEING 737 737401 1384701 NM BS 867 S9R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND CRACK STA 867; S-9R. FABRICATED FRAME REPAIR PER TR 53-10-20E, DEFECT SIZE: .250". 2 L 7 2 4F RT A16WE 2007071200013 20070712 00013 NM 2007 7 12 USAA070509 1 20070629 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND CORROSION BS 328 FLOORBEAM FROM BL0 TO LBL 58. CUT OUT DAMAGE AND INSTALLED DOUBLER AND FILLER PER SRM 53-10-51; CORROSION TASK C53-107-01; LEVEL 2, DEFECT SIZE: 36" BY .750". 2 L 7 2 4F RT A16WE 2007071200014 20070712 00014 NM 2007 7 12 USAA070499 1 20070629 A 5754 65C26603012A SKIN BOEING 737 737401 1384701 NM NR 5 LE SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND DELAMINATION NR 5 L/E SLAT ON O/B AND T/E WEDGE. ADDED DOUBLER REPAIR PER T/R 57-42-04, DEFECT SIZE: 2" BY 6". 2 L 7 2 4F RT A16WE 2007071200016 20070712 00016 NM 2007 7 12 USAA070501 1 20070629 A 5414 SKIN BOEING 737 737401 1384701 NM NR 2 NACELLE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND CRACK AT 2 PYLON AT PANEL NR 5827R. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER TR 54-30-07, DEFECT SIZE: .200". 2 L 7 2 4F RT A16WE 2007071200017 20070712 00017 NM 2007 7 12 USAA070502 1 20070629 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 986 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND CORROSION TOP OF FLOORBEAM AT STA 986, LBL 37 - RBL 25. REMOVED AND REPLACED T CAP PER T/R 53-60-01; CORR TASK 53 C-107-01; CORR LEVEL 2, DEFECT SIZE: 12". 2 L 7 2 4F RT A16WE 2007071200018 20070712 00018 NM 2007 7 12 USAA070503 1 20070629 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND BS 344, RBL 10 - LBL 50, CORROSION AND CLIP NUT WEAR MARKS ON TOP UPPER CHORD. REMOVED DAMAGE AND INSTALLED REPAI R ANGLES PER SRM 53-10-51; CORROSION TASK C53-107-01; LEVEL 2, DEFECT SIZE: 1". 2 L 7 2 4F RT A16WE 2007071200023 20070712 00023 NM 2007 7 12 USAA070508 1 20070629 A 5320 FLOOR SUPPORT BOEING 737 737401 1384701 NM BS 294-312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND FLOOR SUPPORT CORRODED, BS 294.5 - BS 312. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-10-02; CORR TASK C53-107 -02; LEVEL 2, DEFECT SIZE: 16". 2 L 7 2 4F RT A16WE 2007071200024 20070712 00024 NM 2007 7 12 USAA070518 1 20070629 A 5311 FRAME BOEING 737 737401 1384701 NM BS 794 S24R CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND CORROSION FWD FRAME AFT CARGO DOOR BS 794 1" BELOW STR 24R. INSTALLING STRUCTURE REMOVED FOR DOOR FRAME CHANGE, R EF DWG 65-47959, DEFECT SIZE: 1/4". 2 L 7 2 4F RT A16WE 2007071200025 20070712 00025 NM 2007 7 12 USAA070510 1 20070629 A 5340 STOP BOEING 737 737401 1384701 NM BS 492 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND DOOR STOP PITTED, STA 492.4 AT 522R, AFT DOOR FRAME (FUSELAGE) 3RD FROM BOTTOM. REPLACED WITH IDENTICAL PART PER STANDARD PRACTICE MANUAL; CORROSION TASK C53-100-01; LEVEL 2, DEFECT SIZE: 1" BY .5". 2 L 7 2 4F RT A16WE 2007071200031 20070712 00031 SO 2007 7 12 SIMA200718401 1 20070629 A 2120 UNKNOWN EMB 135 EMB135KL 3260302 SO CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 800AE 145425 STRONG OIL ODOR IN BLEED SYSTEM FROM TAKEOFF TO 14,000 FEET. PERFORMED ENGINE RUNS WITH BLEEDS ON WITH NO DEFECTS. PER FORMED BOROSCOPE INSPECTION PER ROLLS ROYCE FAULT ISOLATION MANUAL 72-00-00 WITH NO DEFECTS. RETURNED AIRCRAFT TO SERVI CE. 2 L 7 2 4F RT T00011AT 2007071200034 20070712 00034 NM 2007 7 12 AALA20071166 1 20070625 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 919AN 29520 DFW - EMERGENCY EXIT IDENTIFIER LIGHT AT LEFT AFT CABIN DOOR L1190 HAS BROKEN BASE. REPLACED EMERGENCY EXIT LIGHT ASSEM BLY L1190 FOR EMERGENCY LIGHT AT LEFT AFT CABIN DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007071200035 20070712 00035 NM 2007 7 12 AALA20071157 1 20070625 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 780AN 29956 JFK - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 20C INOPERATIVE. RELAMPED SEAT MOUNTED EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007071200036 20070712 00036 NM 2007 7 12 AALA20071168 1 20070625 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 919AN 29520 DFW - EMERGENCY EXIT IDENTIFIER LIGHT AT LEFT FORWARD SERVICE DOOR L1187 HAS BROKEN BASE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY L1187 FOR EMERGENCY LIGHT AT LEFT FORWARD SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007071200037 20070712 00037 NM 2007 7 12 AALA20071161 1 20070625 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 937AN 30082 MIA - EMERGENCY LIGHT IN AFT CABIN INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT IN AFT CABIN. 2 L 7 2 4F RT A16WE 2007071200038 20070712 00038 NM 2007 7 12 AALA20071163 1 20070625 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 919AN 29520 DFW - EMERGENCY LIGHT AT RIGHT AFT GALLEY DOOR MISSING LENS COVER. REPLACED LENS COVER FOR EMERGENCY LIGHT AT RIGHT AFT GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007071200039 20070712 00039 NM 2007 7 12 AALA20071164 1 20070625 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 919AN 29520 DFW - EMERGENCY LIGHT AT LEFT AFT GALLEY DOOR MISSING LENS COVER. REPLACED LENS COVER FOR EMERGENCY LIGHT AT LEFT AFT G ALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007071200040 20070712 00040 NM 2007 7 12 AALA20071169 1 20070625 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 919AN 29520 DFW - EMERGENCY SEAT MOUNTED LIGHT AT AFT SEAT 14D INOPERATIVE. REPLACED EMERGENCY SEAT MOUNTED LIGHT ASSEMBLY AT AFT S EAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007071200041 20070712 00041 WP 2007 7 12 AALA20071159 1 20070625 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 477AA 49652 LGA - EMERGENCY LIGHTS AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD ENTRY D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071200043 20070712 00043 NM 2007 7 12 AALA20071162 1 20070625 A 7700 MEC BOEING 767 767323 1385205 NM RT ENGINE INOPERATIVE A AALA O OTHER O OTHER DE DESCENT 1 SW 21 384AA 26996 LAX INFLIGHT T284/25JUN - INFLIGHT EMERGENCY DECLARED DUE TO INABILITY TO REDUCE POWER ON RIGHT ENGINE BELOW 68 PERCENT N1 AND 4500 FUEL FLOW DURING DESCENT. LANDED LAX WITHOUT INCIDENT. REPLACED RIGHT ENGINE MAIN ENGINE CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007071200045 20070712 00045 NM 2007 7 12 AALA20071170 1 20070625 A 3350 SHROUD BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 919AN 29520 DFW - EMERGENCY LIGHT AT SEAT 8D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 18D. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007071200046 20070712 00046 NM 2007 7 12 AALA20071171 1 20070625 A 3350 SHROUD BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 919AN 29520 DFW - EMERGENCY LIGHT AT SEAT 10D HAS BROKEN SHROUD. REPLACED SHROUD EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007071200048 20070712 00048 NM 2007 7 12 AALA20071173 1 20070625 A 3350 SHROUD BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 919AN 29520 DFW - EMERGENCY LIGHT AT SEAT 18D HAS BROKEN SHROUD. REPLACED SHROUD EMERGENCY LIGHT AT SEAT 18D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007071200049 20070712 00049 NM 2007 7 12 AALA20071174 1 20070625 A 3350 SHROUD BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 919AN 29520 DFW - EMERGENCY LIGHT AT SEAT 24D HAS BROKEN SHROUD. REPLACED SHROUD EMERGENCY LIGHT AT SEAT 24D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007071200050 20070712 00050 NM 2007 7 12 AALA20071178 1 20070626 A 3350 COVER BOEING 757 757231 1384950 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 717TW 28485 DFW - EMERGENCY ESCAPE PATH FLOOR TRACK LIGHT AT SEAT 25C HAS MISSING COVER. REPLACED PATH FLOOR EMERGENCY LIGHTING COV ER AT SEAT 25C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071200051 20070712 00051 NM 2007 7 12 AALA20071179 1 20070626 A 3350 COVER BOEING 757 757231 1384950 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 717TW 28485 DFW - EMERGENCY ESCAPE PATH TRACK LIGHT AT SEAT 33C HAS MISSING COVER. REPLACED PATH FLOOR EMERGENCY LIGHTING COVER AT SEAT 33C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071200055 20070712 00055 SO 2007 7 12 SWIA200718411 1 20070630 A 5210 DOOR EMB 120 EMB120ER 3260203 SO MAIN PAX OUT OF ADJUST A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 295UX 120295 FLT 5774 - MAIN CABIN DOOR GETS JAMMED WHEN TRYING TO OPEN FROM INSIDE. REPLACED THE TOP SHIM STACK ATTACH SCREW AND AD JUSTED GAP TO PROPER CLEARANCES. DOOR OPERATES NORMALLY. 2 L 7 2 4T RT A31SO 2007071200057 20070712 00057 EA 2007 7 12 SWIA200718413 1 20070627 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT DAMAGED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 438SW 7574 FLT 3875 - EMERGENCY LIGHT ON LOWER WINDSCREEN IS DAMAGED. REPLACED ASSEMBLY WITH A SERVICEABLE UNIT. OPS CHECKS GOOD, P/N BR9279-232. 2 L 7 2 4F RT A21EA 2007071200059 20070712 00059 SO 2007 7 12 SWIA200718415 1 20070501 A 2730 TORQUE TUBE EMB 120 EMB120ER 3260203 SO LT ELEVATOR CORRODED A SWIA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 NM 07 234SW 120308 LEFT ELEVATOR TORQUE TUBE INBOARD BEARING HAS PITTING CORROSION, DISCOVERED AT C-CHECK. REPLACED LEFT ELEVATOR TORQUE T UBE INBOARD BEARING IAW EMB 120 MM 20-40-03, P/N MS27648-33. 2 L 7 2 4T RT A31SO 2007071200060 20070712 00060 SO 2007 7 12 SWIA200718416 1 20070501 A 2731 ROD END EMB 120 EMB120ER 3260203 SO ELEVATOR TRIM CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 234SW 120308 LEFT ELEVATOR TRIM INPUT ROD-ENDS HAVE CORROSION, DISCOVERED AT C-CHECK. REPLACED LEFT ELEVATOR TRIM INPUT ROD-ENDS IAW AMM 27-32-01, P/N NAS659-4-7. 2 L 7 2 4T RT A31SO 2007071200066 20070712 00066 SO 2007 7 12 SWIA200718422 1 20070416 A 5210 RIB EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 233SW 120307 PAX DOOR MID SECTION AFT INTERNAL RIB IS CRACKED, DISCOVERED AT C-CHECK. REPLACED PAX DOOR INTERNAL RIB IAW SRM 120 51- 100-02 PG 3 SEC 3A. 2 L 7 2 4T RT A31SO 2007071200069 20070712 00069 NM 2007 7 12 AWXA200700786 1 20070630 A 3350 321431 BATTERY AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHT FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 814AW 1281 LAS - EEL - LOG# 7779890 - EMERGENCY EXIT LIGHTS RAN DOWN THEIR BATTERIES. EMERGENCY LIGHT SWITCH WAS LEFT ON AND A/C P OWER WAS LOST WHEN JET BRIDGE WAS MOVED. MX REMOVED AND REPLACED ALL FOUR EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW T/ C A1C33302. 2 L 7 2 4F RT A28NM 2007071200071 20070712 00071 SO 2007 7 12 SIMA200718601 1 20070701 A 2530 COFFEEMAKER EMB 135 EMB135KL 3260302 SO GALLEY ODOR A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 845AE 145685 RUBBER BURNING ODOR COMING FROM GALLEY, HOT JUG SYSTEM TURNED OFF. FOUND BURNT WIRES IN HOT JUG SYSTEM MEL ISSUED. AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071200072 20070712 00072 EU 2007 7 12 SIMA200718603 1 20070701 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU ZONE 200 FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 329AE 20233 282 340B329 EMERGENCY FLOOR LIGHTING INOPERATIVE. REMOVED AND REPLACED 20LN EMERGENCY POWER SUPPLY IAW SAAB AMM. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007071200073 20070712 00073 EU 2007 7 12 SIMA200718604 1 20070701 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU ZONE 200 FAILED A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 240DS 23227 803 340B240 EXIT 8A EMERGENCY LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED 23LN EMERGENCY POWER SUPPLY IAW SAAB AMM 30-54-10. O PERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007071200074 20070712 00074 SO 2007 7 12 SIMA200718605 1 20070704 A 3350 78251 INVERTER EMB 135 EMB135KL 3260302 SO ZONE 200 FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 839AE 11784 145653 FOWARD OVERHEAD EXIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED INVERTER IAW EMB AMM. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071200075 20070712 00075 WP 2007 7 12 070137 1 20070702 A 2150 92078339 RELAY DOUG DC9 DC983 3022083 WP A/C PACK FAILED A WX0A D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 19 864GA 49912 AIRCRAFT 864GA WHILE TAXING FOR TAKEOFF FROM GPT ON FLT 778, FLIGHT CREW DETECTED A PUNGENT ODOR AND LIGHT SMOKE HAZE IN THE COCKPIT AND FWD CABIN, AFTER NR 2 ENGINE STARTED. ADDITIONALLY IT WAS NOTED AT THE GATE THE LEFT PACK FAN DID NOT COME ON. FLIGHT CREW RETURNED TO THE GATE AND NOTIFIED MTX CONTROL. ON CALL MTX WAS DISPATCHED AND THE ACM WAS DEFERRE D IAW MEL 21-01 SITUATION NR 1, M PROCEDURE COMPLIED WITH. AIRCRAFT PROCEEDED TO SFB AND MAINTENANCE DEPARTMENT PERSONN EL INSPECTED AND TROUBLESHOOT THE AIR CONDITIONING SYSTEM, DETERMINING THE COOLING FAN TIME DELAY RELAY WAS INOPERATIVE. THE RELAY WAS REPLACED AND A SYSTEM OPERATIONAL CHECK WAS PERFORMED IAW AMM 21-20-06. SYSTEM OPS CHECKS NORMAL AND TH 2 L 7 2 4F RT A6WE 2007071200077 20070712 00077 NM 2007 7 12 DHLA200700034 1 20070705 A 5270 WARNING SYSTEM BOEING 727 727227 1384078 NM PAX DOOR INOPERATIVE A DHLA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 GL 05 783DH 21999 WITH FORWARD ENTRY DOOR OPEN, FORWARD ENTRY DOOR LIGHT IS NOT ILLUMINATED. 2 L 7 3 4F A3WE 2007071200078 20070712 00078 NM 2007 7 12 UIEA200700257 1 20070629 A 5280 65B1166810099 DOOR BOEING 747 7472D7B 1384803 NM LT MLG ERODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 RT AND LT WING GEAR UPPER STRUT DOORS HAS EROSION AND MATERIAL SEPARATING ON FORWARD LEADING EDGE. PERMANENT REPAIR WAS ACCOMPLISHED PER 747-200 SRM 51-40-09 FIG 18, SHEET 4, TABLE II AND 51-40-12 FIG 16 SHEET 1. ALSO, REFERENCE ATLAS AIR XEO NR 57-062707. 2 L 7 4 4F RT A20WE 2007071200079 20070712 00079 NM 2007 7 12 UIEA200700258 1 20070629 A 5730 ACCESS PANEL BOEING 747 7472D7B 1384803 NM RT WING DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 RT WING LOWER SIDE FUELING BAY ACCESS PANEL HAS 2 EACH AREAS OF INNER SKIN DELAMINATION. INBOARD SIDE AREA IS 4.0 BY 5. 0 INCHES AND OUTBOARD SIDE IS 8.0 BY 10.0. PERMANENT REPAIR WAS ACCOMPLISHED ON AREAS AS PER 747-200 SRM 51-40-09 FIG 1 8, SHEET 1, 3 AND 5, TABLE 1, PREPEG 250 DEGREE F CURE. ALSO, REFERENCE ATLAS AIR XEO NR 57-062807. 2 L 7 4 4F RT A20WE 2007071200080 20070712 00080 WP 2007 7 12 IXXA070033O 1 20070703 A 3220 LANDING GEAR DOUG DC8 DC862F 3021972 WP NOSE MALFUNCTIONED A IXXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 11 799AL 80385 996 45922 DURING CLIMB OUT FROM OBBI, THE CREW FELT VIBRATION FROM NOSE GEAR AREA AFTER GEAR RETRACTION. THE CREW CYCLED THE GEAR AND STILL FELT VIBRATION. THE CREW RETURNED TO OBBI WITH OUT INCIDENT. MAINTENANCE INSPECTED NOSE GEAR AREA AND FOUND LEFT NOSE GEAR DOOR WAS OPENED, MAINTENANCE INSPECTED ALL HINGES, ALL ATTACHED HARDWARE, LINKAGE, AND LOCKING MECHANISM , ALL CHECKED GOOD. MAINTENANCE LUBRICATED ALL LOCKING MECHANISMS AND OPERATED DOOR SEVERAL TIMES, IAW DACO DC8 MAINTEN ANCE MANUAL CX/AP20. OPERATIONAL CHECK GOOD AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2007071200081 20070712 00081 SO 2007 7 12 C2XA07RI049 1 20070629 A 3397 WIRE EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS DAMAGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11155 145782 RIC - MX - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY LIGHT AT ROW 3BC INOP (AFT SIDE OF GALLEY). MX FOUND WIRE IMP ROPERLY CONNECTED. MX CONNECTED WIRES PROPERLY IAW AMM 33-50-14 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007071200085 20070712 00085 WP 2007 7 12 IXXA07SMN159S 1 20070411 A 5340 FITTING DOUG DC8 DC871F 302199D WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND AFT LOWER CARGO BILGE INTERIOR FITTING CRACKED AT STATION 1260.000 LONGERON33 R IGHT. REMOVED CRACKED FITTING. FABRICATED FITTING. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. CLEANE D TREATED AND PRIMED AREA AND FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, ATI REPAIR SPECIFICATION NUMBER 2003 -05 AND DOUGLAS DRAWING NUMBER 3750277,NDT SPM PART 08-00-02 TO 07, DC8 SRM 51-1-8B, AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007071200086 20070712 00086 SO 2007 7 12 C2XA07RI051 1 20070613 A 3241 429515 CONTROL UNIT EMB 145 EMB145EP 3260221 SO BRAKES INOPERATIVE A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 14939 12927 4035 145030 FLT 2489 - EWR - CREW REPORTED OB BRAKE INOP MSG ON EICAS AND DECLARED EMERGENCY. ACFT LANDED WITHOUT INCIDENTS. EWR M X REMOVED AND REPLACED BRAKE CONTROL UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071200087 20070712 00087 EU 2007 7 12 AWXA200700792 1 20070704 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 667AW 1710 SAL - EEL - BC-4 CHECK - NR 5948498, DURING EMERGENCY LIGHT TEST AN "EMER R MESSAGE" WAS INDICATED. REPLACED AND OPERAT IONAL CHECKED RIGHT CABIN POWER SUPPLY UNIT IAW A320 AMM 33-51-88. 2 L 7 2 4F RT A28NM 2007071200088 20070712 00088 EU 2007 7 12 AWXA200700793 1 20070704 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 667AW 1710 SAL - EEL - BC-4 CHECK - NR 5964019, DURING EMERGENCY LIGHT TEST AN "EMER L MESSAGE" WAS INDICATED. REPLACED AND OPERAT IONAL CHECKED LEFT CABIN POWER SUPPLY UNIT IAW A320 AMM 33-51-88. 2 L 7 2 4F RT A28NM 2007071200089 20070712 00089 EU 2007 7 12 AWXA200700795 1 20070704 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 667AW 20376 20376 1710 SAL - EEL - BC-4 CHECK - NR 5984497, DURING EMERGENCY LIGHT TEST AN "FWD L MESSAGE" WAS INDICATED. REPLACED AND OPERATI ONAL CHECKED L2 DOOR POWER SUPPLY UNIT IAW A320 AMM 33-51-88. 2 L 7 2 4F RT A28NM 2007071200090 20070712 00090 EU 2007 7 12 AWXA200700796 1 20070630 A 3350 321451 POWER SUPPLY AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHTS INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 629AW 3822 3822 076 SAL - EEL - C-06 CHECK - NR 5978239, CABIN LIGHT EMERGENCY 21WL IS INOPERATIVE. REPLACED AND OPERATIONAL CHECKED CABIN POWER SUPPLY UNIT FOR CABIN LIGHT EMERGENCY 21WL IAW A320 AMM 33-51-88. 2 L 7 2 4F RT A28NM 2007071200091 20070712 00091 NM 2007 7 12 F3LA200700145 1 20070627 A 5320 TRANSITION PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT TRANSITION PANEL 131EG DAMAGED. REPAIRED TRANSITION PANEL 1 31EG IAW SRM 53-02-00, FIG 204. 2 L 7 2 4F RT A28NM 2007071200094 20070712 00094 NM 2007 7 12 F3LA200700148 1 20070627 A 5320 TRANSITION PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT TRANSITION PANEL 131DG DAMAGED. REPAIRED TRANSITION PANEL 1 31DG IAW SRM 53-02-00, FIG 204. 2 L 7 2 4F RT A28NM 2007071200095 20070712 00095 NM 2007 7 12 F3LA200700149 1 20070627 A 5320 TRANSITION PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT TRANSITION PANEL 131DF DAMAGED. REPAIRED TRANSITION PANEL 1 31DF IAW SRM 53-02-00, FIG 204. 2 L 7 2 4F RT A28NM 2007071200096 20070712 00096 NM 2007 7 12 F3LA200700150 1 20070627 A 5321 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT FLOOR PANEL 131CG DAMAGED. REPAIRED FLOOR PANEL 131CG IAW S RM 53-02-00, FIG 204. 2 L 7 2 4F RT A28NM 2007080600001 20070806 00001 NM 2007 8 6 2007UALA02739 1 20070719 A 5310 DOOR FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 927UA 26649 FWD CARGO DOOR CUTOUT, AFT FRAME, CRACKED AT INNER RADIUS JUST ABOVE LOWER STOP PAD FITTING. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007080600002 20070806 00002 NM 2007 8 6 2007UALA02740 1 20070719 A 5310 DOOR FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU GALLEY DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 927UA 26649 RIGHT AFT GALLEY DOOR CUTOUT HAS CRACK AT FWD LOWER CORNER. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. ACCOMPLISHED 2 EA DOUBLER & 1EA TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007080600004 20070806 00004 NM 2007 8 6 2007UALA02743 1 20070719 A 2120 CLAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN AIR LOOSE A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 122UA 29168 RTBL DUE TO STRONG ODOR IN COCKPIT AND CABIN. [08-14-07] FOUND FWD CARGO EE COOLING DUCTING CONNECTION CLAMPS LOOSE A ND OPEN IN THREE POSITIONS SECURED EE COOLING DUCTING AND REPLACED ALL LOWER AND UPPER RECIRCULATION FAN FILTERS PER MM 21-51-08. EE COOLING BITE TEST. TESTED GOOD & NO SMELL IN COCKPIT OR CABIN. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080600005 20070806 00005 NM 2007 8 6 2007UALA02744 1 20070718 A 5210 411N21033B SPRING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR LEVER BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 595UA 28748 CABIN DOOR 1R ARM-DISARM LEVER COVER SPRINGS BROKEN. 09-07-07 AFTER DIAGNOSING THE PROBLEM, DISARMED LEVER AT DOOR. REPLACED COVER FOR ARM. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080600009 20070806 00009 NM 2007 8 6 2007UALA02748 1 20070719 A 3510 OXYGEN SYSTEM BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CREW READS LOW A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 225UA 30554 FOUND CREW OXYGEN PRESSURE READING 710 PSI. [08-14-07] REPRESSURIZED CREW O2 CYLINDERS MANY TIMES. AFTER TROUBLESHO OTING, REPLACEMENT OF THE O2 MASK STOWAGE BOX RESOLVED PROBLEM. NO RECURRENCE. AIRPLANE OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007082900189 20070829 00189 EA 2007 8 29 TRAX200701223 1 20070819 A 2740 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A ASOA K NONE J WARNING INDICATION CL CLIMB 1 SO 27 900EV 7608 STAB TRIM, MACH TRIM CAUTION MSG. EMERGENCY DECLARED. EMERGENCY EQUIP ON STANDBY. 2 L 7 2 4F RT A21EA 2007080600011 20070806 00011 NM 2007 8 6 2007UALA02752 1 20070720 A 2611 SMOKE DETECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT LAVATORY FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 AT GATE, AFT RIGHT LAV SMOKE DETECTOR ALARM IS SOUNDING WITH NO EVIDENCE OF SMOKE OR FUMES. [08-17-07] REPLACED SMOKE DETECTOR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007080600012 20070806 00012 NM 2007 8 6 2007UALA02753 1 20070717 A 5510 STRUCTURE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU HORIZONTAL STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 935UA 26663 CREW REPORTS DENT IN RT HORIZONTAL STABILIZER LEADING EDGE. [08-17-07] MAJOR REPAIR: PER UA EVA-70388 INTERM REPAIR MADE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007080600028 20070806 00028 NM 2007 8 6 2007UALA02778 1 20070722 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 EMERGENCY FLOOR LIGHTS 2EF SOME LIGHTS ARE INOP. [08-14-07] SECURED LIGHT STRIP. OP CHECKS OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080600031 20070806 00031 NM 2007 8 6 2007UALA02781 1 20070722 A 2800 FUEL SYS BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE UNKNOWN LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 673UA 29241 FLIGHT DIVERTED & LANDED UNDER AMBER ALERT DUE TO A FUEL LEAK INDICATION. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080600041 20070806 00041 SO 2007 8 6 C2XA07RI061 1 20070723 A 3350 110049 CHARGER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 26545 145558 DURING A ROUTINE MX INSPECTION IT WAS FOUND THAT THE FWD LT, FWD AISLE AND COCKPIT FLOOD EMERGENCY LIGHTS WERE INOPERATI VE. MAINTENANCE TROUBLESHOOT AND FOUND NR 1 EMERGENCY BATTERY CHARGER TO BE THE CAUSE AND REMOVED AND REPLACED IT WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007080600049 20070806 00049 NM 2007 8 6 CALA0700370 1 20070721 A 5320 654587570 ANGLE BOEING 737 7373T0 1384582 NM BS 294.5-360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND R-1 DOOR Z-ANGLE CORRODED IN SEVERAL AREAS FROM STA 294.5 TO 360, RBL 48. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007080600069 20070806 00069 NM 2007 8 6 SWAA073618 1 20070723 A 5753 6546435278 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED MV4 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD CORNER. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2007080600081 20070806 00081 2007 8 6 SWAA073617 4 20070723 A 2565 65C16820 HOOK BOEING 737 7377H4 1384404 NM L1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 794SW 30605 L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2007080600085 20070806 00085 NM 2007 8 6 SWAA073631 1 20070724 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 867 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080600100 20070806 00100 WP 2007 8 6 ASAA0781892 1 20070725 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 CANT REPAIR BRACKET BROKEN. REPLACED EXISTING REPAIR BRACKET PER SRM 51-30-5. 2 L 7 2 4F RT A6WE 2007080600110 20070806 00110 WP 2007 8 6 ASAA0781895 1 20070725 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 1231-1250 BULGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 FUSELAGE SKIN BULGED. RECONTOURED SKIN AND INSTALLED INTERIOR DOUBLER PER SRM 53-04. 2 L 7 2 4F RT A6WE 2007080600114 20070806 00114 WP 2007 8 6 ASAA0781883 1 20070724 A 5753 5930494501 VANE DOUG DC9 DC983 3022083 WP TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 LEFTHAND INBOARD FLAP INBOARD VANE HAS DENTS ON LOWER SURFACE. REMOVED DAMAGED AREA. INSTALLED REPAIR SKIN AND DOUBLER PER SRM 51-70-6. 2 L 7 2 4F RT A6WE 2007080600117 20070806 00117 NM 2007 8 6 ZZDA2007212 1 20070605 A 5313 LONGERON BOEING 717 717200 1383700 NM BS 898.5-1053 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT LONGERON 22L BETWEEN BS 898.5 AND BS 1053. INSTALLED LONGERON 22L AT AFT CARGO COMPA RTMENT BETWEEN STA 898.5 AND STA 1053 AS PER B717 SRM 51-41-02. 2 L 7 2 4F TR A6WE 2007080600122 20070806 00122 NM 2007 8 6 ZZDA2007217 1 20070605 A 5313 LONGERON BOEING 717 717200 1383700 NM BS 1053 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO WASTE TANK AREA AT LONG 30 END TIE FITTING. INSTALLED NEW END TIE FITTING LONGERON 30 AT AFT CAR GO COMPARTMENT STA 1053 IAW B717 SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007080600124 20070806 00124 NM 2007 8 6 ZZDA2007219 1 20070605 A 5313 LONGERON BOEING 717 717200 1383700 NM BS 1053 L29L CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT (WASTE TANK AREA) AT LONGERON 29L END TIE FITTING. INSTALLED NEW END TIE FITTING LON GERON 29L AT AFT CARGO COMPARTMENT STA 1053 IAW B717 SRM 51-41-02 AND SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007080600127 20070806 00127 NM 2007 8 6 TIPR200736005 1 20070726 A 5310 STRUCTURE BOEING 767 767222 1385122 NM NLG WW CRACKED B TIPR K NONE O OTHER IN INSP/MAINT 1 SO 05 609UA 21870 CRACK INDICATIONS ON LT AND RT VERTICAL STIFFENERS IN NOSE WHEEL WELL APPROX 12 INCHES DOWN FROM TOP OF CHORD. REPAIRED LT AND RT CHORDS IN ACCORDANCE WITH B767 SRM 51-70-12 FIG 1 AND AD 2005-02-02. REFERENCE SERVICE ORDER 599125 OPERATIO N 26110. 2 L 7 2 4F RT A1NM 2007080600129 20070806 00129 WP 2007 8 6 ABXA070245 1 20070705 A 5310 99236685 STRUCTURE DOUG DC9 DC941 302207N WP COCKPIT CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 COCKPIT SUBFLOOR CHAFED IN SEVERAL LOCATIONS AT STA 160 AND 148. REPAIRED AREA IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 2007080600136 20070806 00136 2007 8 6 SWAA073672 4 20070725 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM R1 DOOR GIRTBAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM. 2 L 7 2 4F RT A16WE 2007080600141 20070806 00141 NM 2007 8 6 SWAA073661 1 20070725 A 5340 65C27314 STRINGER CLIP BOEING 737 7373K2 13844BA NM BS 685 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080600142 20070806 00142 NM 2007 8 6 SWAA073668 1 20070725 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 867 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080600149 20070806 00149 NM 2007 8 6 SWAA073663 1 20070725 A 3397 W146005920 WIRE BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND LT FWD CABIN EMERGENCY EXIT LIGHTS INOP. INSPECTED AND FOUND LOOSE WIRING, REPAIRED W IRING PER MM AND WDM. 2 L 7 2 4F RT A16WE 2007080600154 20070806 00154 NM 2007 8 6 KCSA071260 1 20070726 A 5414 SKIN BOEING 747 7472B4B 138481B NM NR 3 NACELLE WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NR 3 PYLON I/B SIDE LOWER SKIRT SKIN WORN AT NAC STA-200 TO 236. 2 L 7 4 4F RT A20WE 2007080600180 20070806 00180 EA 2007 8 6 TRAX200701058 1 20070725 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 854AS 7382 PAX DOOR BOTTOM STEP LEFT BETA LIGHT STRIP MISSING. 10-18-07 REMOVED UNSERVICEABLE PAX DOOR HANDLE "EXIT PULL" BET A LIGHT. INSTALLED SERVICEABLE PAX DOOR HANDLE "EXIT PULL", P/N 601R38774-13, IAW CRJ 200 AMM 52-11-02. FUNCTIONAL CHEC K GOOD, IAW CRJ 200 AMM 33-51-09. 2 L 7 2 4F RT A21EA 2007080600185 20070806 00185 EA 2007 8 6 TRAX200701066 1 20070726 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 873AS 7549 INTERCOSTAL AT BL 1.0 L IS CORRODED. 10-18-07 BLENDED CROSSION ON INTERCOSTAL BETWEEN F.S.349 AND F.S.333 AT B.L. 1.0. BLENDED CORROSION WITHIN LIMITS. REMOVED .006 MATERIAL. TREATED PRIMED AND PAINTED IAW CRJ 200 SRM 51-23-00 AND 51- 12-00 JOB COMPLETE MS 7022223. 2 L 7 2 4F RT A21EA 2007080600202 20070806 00202 NM 2007 8 6 SWAA073682 1 20070726 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM BS 520 S8-8LR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080600204 20070806 00204 WP 2007 8 6 ASAA0781906 1 20070726 A 5321 99366401 FLOOR PANEL DOUG DC9 DC983 3022083 WP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND DAC DWG 9936640. 2 L 7 2 4F RT A6WE 2007080600208 20070806 00208 WP 2007 8 6 ASAA0781912 1 20070726 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 207-255 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 FUSELAGE SKIN DENTED. REPAIRED PER SRM 53-04. 2 L 7 2 4F RT A6WE 2007080600210 20070806 00210 NM 2007 8 6 HNAA0700156 1 20070726 A 2120 7786848 MIXER BOX DHAV DHC8 DHC8102 2809003 NM CONDENSOR WORN A HNAA O OTHER O OTHER TO TAKEOFF 1 EA 07 982HA 18862 5247 380 CABIN GOT VERY HOT AFTER TAKEOFF FLIGHT DECK COLD. AFTER SEVERAL PAX GOT SICK, F/A INFORMED CREW THAT THE CABIN WAS TOO HOT TO CONTINUE. ACFT WAS APPROX 20 MILES OUT OF LGA, ACFT RETURNED TO FIELD. CONTACTED LGA MX. ACFT HAS BEEN WRITTE N UP TWICE BEFORE. DUCTING UNDER FLOOR APPEARS TO BE IN GOOD SHAPE. FLIGHT DECK IS COLD WITH GOOD DUCTING TEMP. LGA H AS SEVERAL BROKE ACFT WILL FERRY TO MDT. CLAMP UNDER DORSAL FIN LOOSE TIGHTENED AND REMOVED AND REPLACED CONDENSER MIXE R. 2 H 7 2 4T RT A13NM 2007080700018 20070807 00018 NM 2007 8 7 2007UALA02839 1 20070725 A 2121 FAN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN ODOR A UALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 WP 29 782UA 26948 FA'S REPORTED FAINT ELECTRICAL ODOR IN CABIN. ODOR MAINLY NOTED BY FIRST CLASS GALLEY TO BUSINESS CLASS AREA. CREW NOT ED UPPER RECIRC FAN STATUS MSG. [08-21-07] FOUND FWD UPPER RECIRC FAN C-B POPPED. :REPLACED UPPER RECIRC FAN PER MM 21 -25-01. ALSO, REPLACED FILTERS. ACCOMPLISHED LEAK CHK AND OP CHECKED OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007080700022 20070807 00022 NM 2007 8 7 2007UALA02843 1 20070725 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 669UA 30025 EMERGENCY EXIT PATHWAY LIGHTING DIM ON RIGHT SIDE, ROWS 26 THROUGH 36. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080700038 20070807 00038 WP 2007 8 7 IXXA07SMN175S 1 20070630 A 5522 SKIN DOUG DC8 DC873F 302199F WP ZONE 300 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR HAD IMPROPER REPAIR ON LOWER SKIN AT STATION XE 84.968. REMOVED EXISTING. FABRICATED NEW SKIN AND DOUBLER. BONDED BOTH PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA A ND REPAIR PART. INSTALLED REPAIR PARTS AND NEW FASTENERS FROM STATION XAR 0 TO STATION XE 132.000. PERFORMED BALANCE T O LEFT ELEVATOR FOUND WITHIN ALLOWABLE TOLERANCE LIMITS. MOMENT 1450.87 IN LBS IAW DC8 SRM 55-1-0 FIGURE 1, DC8 SRM 51- 1-21,DC8 SRM 55-4-1 FIGURE 1 SHEETS 1 AND 2 ITEM "E" AND "F. DRAWING DOUGLAS NUMBER 5654970-5, DC8 SRM 51-1-9, DC8 SRM 51-1-8B, AND DC8 SRM 51-4-4 PAGES 1 AND 2. 2 L 7 4 4F RT 4A25 2007080700042 20070807 00042 WP 2007 8 7 IXXA07SMN180S 1 20070630 A 5340 4772397UI FITTING DOUG DC8 DC873F 302199F WP ZONE 200 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE FITTING HAS A CRACK LONGERON 17 LEFT STATION 1768.000. REMOVED CR ACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, 51-1-20D, 51-3-0, SRM 51-1 -8B, DC8 SRM 51-1-21, 51-1-20D, 51-3-0, AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007080700044 20070807 00044 NM 2007 8 7 UPS07450251 1 20070705 A 5310 DOOR FRAME BOEING 747 747212B 1384886 NM APU DOOR CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C APU COMPT AFT DOOR CUTOUT SUPPORT FRAME LWR FLANGE LWR SURFACE FOUND CHAFED MARKED. APU COMPT AFT DOO R CUTOUT SUPPORT FRAME LWR FRAME REPAIRED AS PER SRM 51-40-03 FIG 2. 2 L 7 4 4F A20WE 2007080700062 20070807 00062 NM 2007 8 7 UPS07450269 1 20070704 A 5315 FLOORBEAM BOEING 747 747212B 1384886 NM BS 2280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D STA2280 LBL39 FLOORBEAMS WEB REAR SIDE FOUND SEVERAL CRACKS, CRACK LENGTH 1/4". M/D BS 2280 LBL 3 9 FLOORBEAM WEB REPAIRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2007080700063 20070807 00063 NM 2007 8 7 UPS07450270 1 20070704 A 5730 PANEL BOEING 747 747212B 1384886 NM LT WING BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C LWS 888 L/E LOWER FIXED PANEL FWD BULGED AS MARKED. CORROSION BLEND OUT 0.040" BY 1" BY 2". LHW L/E WS888 LOWER FIXED PANEL FWD SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 1. 2 L 7 4 4F A20WE 2007080700083 20070807 00083 NM 2007 8 7 DHL2007741519 1 20070726 A 5512 SKIN BOEING 727 7272Q9 138448M NM HORIZONTAL STAB DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 DENT ON LOWER SURFACE, RT HORIZ STAB, STAB STA 114.97. DENT BEYOND SERV LIMITS PER B727 SRM 55-10-1 FIG 2. CUT OUT DAM AGE, 3" BY 1.5", REMOVED PREVIOUS REPAIR DOUBLER ADJACENT TO DENTED AREA, FABRICATED SINGLE REPAIR DOUBLER FROM 2024-T3, .063" BY 17" BY 17.5", PO NR 9005467; 3 EA FILLERS FROM 7075-T6, .063" BY 6" BY 1.5"(NR 1), .063" BY 3" BY .5"(NR 2 AND NR 3), PO NR 9005314; AND 4 EA TAPERED FILLERS FROM 2024-T3, .071" BY 6" BY 1.5"(4 EA), PO NR 9005461, ALL PER B727 SR M 55-10-3 FIG 4. TREATED, PRIMED, AND INSTALLED REPAIR PARTS PER B727 SRM 51-10-2, AND 55-10-3 FIG 4. 2 L 7 3 4F RT A3WE 2007080700085 20070807 00085 NM 2007 8 7 HNAA0700159 1 20070726 A 3350 6013211 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS FAILED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 835HA 4903 4 142 EMERGENCY LIGHTS AT 1DF INOP. REMOVED AND REPLACED EMERGENCY LT PWR SUPPLY BASE AND BATTERY, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007080700087 20070807 00087 NM 2007 8 7 USAA070548 1 20070717 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 294 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 FOUND STA 294.5 31" LBL0, FLOORBEAM. REMOVED DAMAGED PART AND INSTALLED REPAIR PART PER SRM 51-20-00, DEFECT SIZE: 1.5. 2 L 7 2 4F RT A16WE 2007080700096 20070807 00096 EA 2007 8 7 MASA200700322 1 20070611 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 922FJ 15022 ASH 2697 PSP - PILOT REPORTED THE EMERGENCY LIGHT INOP AT ROW 15 AND 16 CEILING AND SIDEWALL. MX APPLIED EXTERNAL POWER TO THE AIRCRAFT AND OPS CHECKED NORMAL. 2 L 7 2 4F RT A21EA 2007080700105 20070807 00105 EA 2007 8 7 QXEA200701213 1 20070729 A 3397 WIRE CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 SEA-FLIGHT 2539, DURING REPAIR OF CEILING PANEL 263ALC FOUND A BROKEN WIRE AT THE EMERGENCY LIGHT PLUG P358. MAINTENANC E REPAIRED THE BROKEN WIRE AT PLUG P358 PER STANDARD PRACTICES. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007080700107 20070807 00107 WP 2007 8 7 IXXA07SMN182S 1 20070630 A 5740 3645612U BRACKET DOUG DC8 DC873F 302199F WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND NUMBER 1 ALT FUEL TANK BOOSTER PUMP SUPPORTS CRACKED AT STRINGER 59 STATION XW 456.000. REMOVED CRACKED BRACKET. INSTALLED NEW BRACKET AT STATION XW 456.000, STRINGER 59 IAW DC8 SRM 51-1-20D AND 51 -3-1. 2 L 7 4 4F RT 4A25 2007080700118 20070807 00118 SO 2007 8 7 SIMA200721101 1 20070725 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 21 660CL 145764 STRONG ELECTRICAL ODOR ON FLIGHT DECK, NO SMOKE NOTED, DISAPATED AFTER 10 MINUTES. REMOVED DEBRIS IN FOWARD AVIONIC ARE A. OPERATIONAL CHECK GOOD IAW EMB AMM. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007080700120 20070807 00120 2007 8 7 MALA070093 4 20070724 A 3420 6226320002 INDICATOR SAAB SF340 340B 7860101 EU COCKPIT INOPERATIVE A MALA A UNSCHED LANDING O OTHER UK UNKNOWN 1 GL 15 457XJ 340B457 AFTER DEPARTING MEM, LOST ALL INDICATIONS FROM NAV 1 AND NAV2 ON BOTH EHSI'S AS WELL AS FMS DATA. REPLACED NR 2 DCP PN ON AND OFF 6226320002, SN ON 382 SN OFF 1184 TESTS ARE GOOD REF AMM 34-24-25-02. 2 L 7 2 4T RT A52EU 2007080700131 20070807 00131 NM 2007 8 7 AWXA200700919 1 20070704 A 5311 90526911 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5981841, CRACKED FRAME, BS 787, S9L. REPAIRED FRAME, BS 787, S9L IAW USAIRWAYS EA 120121. 2 L 7 2 4F RT A16WE 2007080700140 20070807 00140 NM 2007 8 7 DL764070957 1 20070725 A 2760 SPOILER BOEING 767 767432ER 1385134 NM LEFT WING DAMAGED A DALA A UNSCHED LANDING C F.O.D. CR CRUISE 1 SO 27 834MH 29707 TIRE RECAP REMAINS FOUND IN ATL AFTER T/O OF FLT 1273 CREW REPORTED NO PROBLEMS AT THIS TIME LATER IN CRZ FLT CREW DISCO VERED APPROX 3 INCH HOLE IN NR 6 SPOILER PANEL. DIVERTING TO LAX FOR REPAIRS. REPLACED NR 6 SPOILER ASSY MFG P/N 113T4 100-401G PER MM 27-61-01-024-001. THE REQUIRED INSPECTION HAS BEEN PERFORMED FOR INSTALLATION OF SPOILER SIX ASSY PER A MM 27-61-01-424. 2 L 7 2 4F RT A1NM 2007080700155 20070807 00155 CE 2007 8 7 GUUA07140702 1 20070714 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CABIN ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 29 87557 UE246 FLIGHT: 9131- DURING FLIGHT, STRONG ODOR COMING FROM THE OVERHEAD BLOWERS. PERFORMED OPERATIONAL CHECK OF VCM COULD NOT DUPLICATE ODOR. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080700161 20070807 00161 CE 2007 8 7 GST2007F00000 1 20070613 A 3297 GROUND WIRE BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO MLG BROKEN E GSTA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 13 770LA TH517 WHILE RETURNING, ON A REVENUE FLIGHT AND ARRIVING IN THE AIRPORT TRAFFIC PATTERN, THE GEAR HANDLE WAS SELECTED TO THE DO WN POSITION. PILOT HEARD THE GEAR EXTEND, BUT DID NOT RECEIVE A POSITIVE DOWN AND LOCKED INDICATION, NO GREEN LIGHTS. PILOT TOOK C/A TO DETERMINE THE STATUS OF THE LANDING GEAR AND CONFIRMED THAT THE GEAR WAS INDEED DOWN BY PERFORMEING A FLYBY OF THE CONTROL TOWER. AN UNEVENTFUL LANDING WAS PERFORMED. MAINTENANCE DETERMINED THAT THERE WAS A BROKEN GROUND WIRE AND RETURNED THE AC TO SERVICE. (K) 1 L 7 2 3O 3 O 3A16 E5CE 2007080800008 20070808 00008 EA 2007 8 8 A6WA200740188 1 20070406 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT ODOR A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 427ZW 7685 STRONG FUEL ODOR IN COCKPIT AFTER ENGINE SHUTDOWN, APU IS RUNNING. PERFORMED INSPECTION OF FUEL LINES AND FUEL DRAINS, NO FUEL ODORS OR LEAKS DETECTED AT THIS TIME, OK FOR RETURN TO SERVICE. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007080800019 20070808 00019 CE 2007 8 8 DJFA2007074 1 20070716 A 5411 67513209 RIB CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LT PYLON CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 707LX 5370 7500078 DURING A SCHEDULED INSPECTION, MAINTENANCE DISCOVERED A RIB IN THE LT PYLON CRACKED. THE RIB WAS CRACKED AT THE UPPER A ND LOWER FLANGES. BOTH CRACKS WERE APPROX. 2 INCHES LONG. THE RIB WAS REPLACED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007080800025 20070808 00025 WP 2007 8 8 ASMF200707014 1 20070719 A 5241 5910084511 DOOR DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE FWD SERVICE DAMAGED W ASMF K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 23 205AM 49405 DURING TRANSIT CHECK, AIRCRAFT WAS HIT IN THE FORWARD SERVICE DOOR BY A CATERING SERVICE TRUCK. MAINTENANCE PERSONNEL RE PLACED THE DOOR IAW MM 52-41-00, PRESSURIZATION TEST WAS CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007080800048 20070808 00048 CE 2007 8 8 DJFA2007078 1 20070720 A 5710 BEARING RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP WING MISSING E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 720TA 258320 DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE BEARING CAP CRACKED. THE BEARING, BEARING HOUSING, AND CAP WERE RE PLACED. 2 L 7 2 4F 4 F RT A3EU E6WE 2007080800067 20070808 00067 GL 2007 8 8 YTRR116570 2 20070711 A 7323 23065125 GOVERNOR BELL 206 206L4 1182110 SW ALLSN 250C 250C30 03013 GL ENGINE FLUCTUATES B YTRR O OTHER O OTHER CR CRUISE 1 SW 03 852RL 52081 AIRCRAFT EXPERIENCED TORQUE FLUCTUATIONS OF 10 PERCENT TO 15 PERCENT DURING CRUISE FLIGHT. 1 G 7 1 3U 3 U NC H2SW E1GL 2007080800071 20070808 00071 CE 2007 8 8 AMWA06032F 1 20070725 A 5311 1294300311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 258 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080800088 20070808 00088 CE 2007 8 8 AMWA06032H 1 20070725 A 5311 12943003721 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 318 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080800091 20070808 00091 CE 2007 8 8 AMWA06032D 1 20070725 A 5311 1294300311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 228 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080800100 20070808 00100 WP 2007 8 8 ASMF200707015 1 20070725 A 3242 392492 VALVE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE BREAKES FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 838AM 7180 49397 AIRCRAFT RETURNED TO PLATFORM DURING TAXING, CAPTAIN REPORTED THAT BRAKES SYSTEM FELT JAMMED. DURING CHECK WAS DETECTED THE BRAKES NR 3 AND 4 JAMMED. TECHNICAL PERSONNEL REPLACED THE RT CONTROL BRAKE VALVE AND BOTH DUAL SERVO VALVES IAW MM 32-42-0 Y 32-43-00, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2007080800103 20070808 00103 EU 2007 8 8 UPS07150343 1 20070729 A 5320 PANEL AIRBUS A300 A300F4622R 3930360 EU PWA 4158 PW4158 NE CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 152UP 0835 DURING REMOVAL AND REPLACEMENT OF AFT LOWER CARGO CEILING PANEL FOUND SUPPORTING STRUCTURE CRACKED AND DENTED. REMOVED DAMAGE AND REPAIRED IAW EO A300-5320-27329-A AND RESTORED FINISH IAW SRM 51-23-10. 2 L 7 2 4F 4 F RT A35EU E24NE 2007080900002 20070809 00002 NM 2007 8 9 UPS07550342 1 20070727 A 2120 UNKNOWN BOEING 757 75724APF 1384969 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT ODOR A IPXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 468UP 25484 BTB AT 2050Z DUE TO FUMES. NOTICED PAINT ACTONE-LIKE ODOR PRIOR TO TAKEOFF. UNABLE TO DETERMINE SOURCE. PERFORMED HARM FUL SUBSTANCE SPILL PROCEDURES IAW GMM 3-32-1. COMPLETED FORM 32-44-01 DATED 2-10-06. NO SPILL ON LEAKAGE FOUND. PERFOR MED MM 21-00-01 FAULT ISOLATION STEPS TO PAGE 5 RAN LT ENG NO FAULTS. RT ENG NO FAULTS AND OPERATED LT AND RT PACKS. 2 L 7 2 4F 4 F RT A2NM E12EU 2007080900003 20070809 00003 WP 2007 8 9 UPS07850338 1 20070723 A 5310 ANGLE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE FS 986 LBL 46 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE: C2 C-PIT FWD BULKHEAD STA 986 LBL 46, ANGLE CRACKED. STOP DRILLED CRACKED ANGLE AT STA 986 LBL 46 IAW SRM 53-02-00-0 FIG 001B. FABRICATED AND INSTALLED REPAIR ANGLE AT STA 986 LBL 46 IAW SRM 53-02-00-0, AND DWG 5704721 2 L 7 4 4F 4 F RT 4A25 E2GL 2007080900005 20070809 00005 WP 2007 8 9 UPS07850344 1 20070728 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE: N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-50-0 1-2. OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 2007080900006 20070809 00006 NM 2007 8 9 UPS07M50341 1 20070728 A 3234 HANDLE DOUG MD11 MD11F 3023600 NM PWA 4460 PW4460 NE LANDING GEAR INOPERATIVE A IPXA A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 SO 01 277UP 48578 LANDING GEAR HANDLE WILL NOT MOVE TO UP POSITION. PERFORMED CHECKLIST, GEAR WOULD NOT RETRACT. FOUND RT TRUCK BEAM ACT PRESS RELIEF VALVE AND ONE WAY RESTRICTOR FAILED. BOTH REPLACED IAW AMM 32-37-01 AND 04. ALSO REPLACED TWO-WAY RESTRIC TOR AND TRIM ACTUATOR. SYSTEM BLEEDING AND LEAK CHECK PERFORMED. LANDING GEARS SWING TEST PERFORMED. ALL ARE OK. 2 L 7 3 4F 4 F RT A22WE E24NE 2007080900007 20070809 00007 NM 2007 8 9 ASMF200707019 1 20070729 A 2400 9008D093 RELAY DOUG MD80 MD83 3023681 NM PWA 4460 PW4460 NE APU BUSS CLOGGED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 838AM 28852 5592 49397 AIRCRAFT RETURNED TO PLATFORM, AC CROSS TIE AND APU RT BUSS LIGHTS TURNED ON. BCU WAS REPLACED IAW MM 24-20-00 AND AC CROSS TIE LIGHT TURNED OFF, BUT RT BUSS LIGHT CONTINUED ON. RT BUSS LIGHT WAS DEFERRED BY MEL 24-1-1 AND AIRCRAFT WAS DI SPATCHED. AFTER, AIRCRAFT RETURNED OF FLIGHT DUE TO THE SAME FAILURE AND CAPTAIN PERFORMED ABNORMAL PROCEDURE. DURING MA INTENANCE CHECK, THE RT AUX POWER RELAY WAS DETECTED CLOGGED. THE RELAY WAS REPLACED IAW MM 24-20-06, TESTED CORRECT. 2 L 7 2 4F 4 F RT E24NE 2007080900008 20070809 00008 NM 2007 8 9 KCSA071266 1 20070730 A 5412 BULKHEAD BOEING 747 7472B4B 138481B NM PWA JT9 JT9D7F 52054 NE NR 1 PYLON SCRATCHED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NR1 PYLON STA-221, AFT BULKHEAD HAS SCRATCH ABOVE HYDRULIC LINE FEED THROUGH. 2 L 7 4 4F 4 F RT A20WE E20EA 2007080900009 20070809 00009 NM 2007 8 9 KCSA071267 1 20070730 A 5313 STRINGER BOEING 747 7472B4B 138481B NM PWA JT9 JT9D7F 52054 NE BS 668 S44L DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 BS 668 STRINGER 44L HAS SMALL DAMAGED AREA. 2 L 7 4 4F 4 F RT A20WE E20EA 2007080900010 20070809 00010 NM 2007 8 9 KCSA071268 1 20070730 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM PWA JT9 JT9D7F 52054 NE BS 1250 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA-1250 LBL-99 SEAT TRACK HAS DAMAGE TO CARGO SYSTEM LOCKING HOLES. 2 L 7 4 4F 4 F RT A20WE E20EA 2007080900011 20070809 00011 NM 2007 8 9 AMTA200700349 1 20070717 A 2160 3987505 CONTROL VALVE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE RT A/C PACK UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 552TZ 32586 EICAS MSG RT PACK TEMP DISPLAYED R PACK INOP LGT ILLUM. LT EXSITING WHEN STBY SELECTED. OPERATED NORMAL IN STBY. REPL ACED RT PACK TEMP CONTROL VALVE IAW MM 21-51-12. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007080900013 20070809 00013 2007 8 9 AMTA200700352 4 20070718 A 3420 DISPLAY BOEING 737 73783N 13844HI NM COCKPIT MALFUNCTIONED A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 314TZ 30640 ISFD VIDEO SCREEN IS SPLIT IN THE VERTICAL, SHOWS RIGHT HALF OF NORMAL SCREEN TWICE, NO FIRM CODE FOUND. PERFORMED ISFD BITE TEST, SCREEN RETURNED TO NORMAL. PERFORMED ISFD BITE TEST AGAIN IAW AMM34-20-00-8. OPS CHECK GOOD. OK FOR SERVI CE. (K) 2 L 7 2 4F RT A16WE 2007080900016 20070809 00016 NM 2007 8 9 AMTA200700356 1 20070719 A 7500 1296662 SENSOR BOEING 737 73783N 13844HI NM PRECOOLER UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 310TZ 28243 RT BLEED TRIPOFF LIGHT ILLUMINATED IN FLIGHT. WOULD NOT RESET WITH TRIP RESET BUTTON. REMOVED AND REPLACED PRECOOLER C ONTROL VALVE SENSOR IAW MM 36-12-03-4. OPS CHECK NORMAL. OK FOR SERVICE. (K) 2 L 7 2 4F RT A16WE 2007080900017 20070809 00017 2007 8 9 AMTA200700358 4 20070721 A 3460 COMPUTER BOEING 737 73783N 13844HI NM FLT MANAGE FAILED A AMTA O OTHER O OTHER CL CLIMB 1 GL 11 305TZ 30706 DUAL FMC FAILURE APPROX 25 MIN AFTER T/O. PERFORMED BITE IAW FIM 34-61-00-810-801. NO CURRENT FAULTS. NO HISTORY PAST 90 DAYS. IB CREW REPORTS NO FAULTS. OK FOR SERVICE. (K) 2 L 7 2 4F RT A16WE 2007080900019 20070809 00019 2007 8 9 AMTA200700360 4 20070721 A 2310 9640452012 TRANSCEIVER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT HF SYSTEM MALFUNCTIONED A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 522AT 29330 RT HF RADIO DOES NOT CHANNELIZE ONLY ABOUT A 15 SECOND LOUD HUM FOLLOWS CHANNELIZATION ATTEMPT. REMOVED AND REPLACED TR ANSCEIVER OPS CHECK OK IAW MM 23-11-03. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007080900023 20070809 00023 SO 2007 8 9 GUUA07250701 1 20070725 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN INOPERATIVE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 285AS 120265 FLIGHT: 9259 FLL/MHH PILOT REPORTED ONE EMERGENCY FLOOR LIGHT INOPERATIVE AT ROW 2. SECURED EMERGENCY FLOOR LIGHT. 2 L 7 2 4T 4 T RT A31SO E20NE 2007080900025 20070809 00025 SO 2007 8 9 GUUA07260702 1 20070726 A 3297 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE LT MLG LOOSE A GUUA O OTHER P NO WARNING INDICATION CR CRUISE 1 SO 29 268AS 120202 FLIGHT: 9298 TCB/FLL DURING CRUISE TOP 3 RED (A) GEAR LIGHTS FLASH ON AND OFF. CLEANED AND TIGHTENED CONNECTORS ON RT M AIN LANDING GEAR, LT MAIN LANDING GEAR AND NOSE LANDING GEAR UP/DOWNLOCK SENSORS OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2007080900027 20070809 00027 EA 2007 8 9 VNAA0707011 1 20070719 A 2420 761339D ADG CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RIGHT DAMAGED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 253PS 7471 7934 CREW REPORTED THE ADG DEPLOYED IN FLIGHT WITH NO CAUSE. MAINTENANCE REMOVED AND REPLACED THE ADG IAW THE AIRCRAFT MM. O PERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007080900028 20070809 00028 WP 2007 8 9 MWEA070163 1 20070730 A 2560 EFB6220 BATTERY DOUG DC9 DC981 3022081 WP FLASHLIGHT INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 813ME 48007 AFT CABIN EMERGENCY FLASHLIGHT BATTERY INDICATOR DOES NOT FLASH. REMOVED AND REPLACED BATTERIES. 2 L 7 2 4F A6WE 2007080900029 20070809 00029 NM 2007 8 9 ZZDA2007250 1 20070726 A 5330 SKIN BOEING 737 737 UTILSYS NM BS 802 S26R CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 284AT 32668 DURING INSPECTION OF AN EXISTING DENT (11 INCHES BELOW THE FWD LWR CORNER OF THE AFT CARGO DOOR AT STA 802 AND STRINGER 26R), IT WAS DISCOVERED THE SKIN WAS CRACKED. C/W EDDY CURRENT C/W SECTION 1 OF E.A. 37-53-00115 HF EDDY CURRENT. INST ALLED TEMPORARY REPAIR DOUBLER IAW NEW EA 37-53-00600IR SECTION 1. 2 L 7 2 4F RT A16WE 2007080900030 20070809 00030 EA 2007 8 9 TRAX200701071 1 20070727 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 854AS 7382 2 SEAT TRACKS IN CARGO BAY CORRODED, 1 MARKED, 1 REMOVED. 10-18-07 INSTALLED SEAT RAIL, FOR RIGHT 9G WALL, PN 601R 38779-9 IAW CRJ 200 53-01-11 MM13267 7-28-07. UPON INSTALLION OF SEAT TRACK FOR CENTER 9G WALL FOUND INCORRECT PART HAD BEEN OREDERED. REMOVED SEAT TRACK AND REORDERED CORRECT PART - INSTALLED NEW SERVICEABLE SEAT TRACK IAW CRJ AMM 53-01-11 . 2 L 7 2 4F 4 F RT A21EA E15NE 2007080900031 20070809 00031 EA 2007 8 9 TRAX200701072 1 20070727 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 854AS 7382 FS 280 WEB IS CRACKED OB OF RBL 9. REPAIRED 280 WEB RBL 9 C/W IAW EC/TC REO 601R-53-11-1218. 2 L 7 2 4F 4 F RT A21EA E15NE 2007080900032 20070809 00032 EA 2007 8 9 TRAX200701074 1 20070728 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 758EV 10210 PAX DOOR PLACARD MISSING. 2 L 7 2 4F 4 F RT A21EA E15NE 2007080900033 20070809 00033 EA 2007 8 9 A6WA2007410323 1 20070618 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 220 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 434AW 7322 NLG AFT DOOR CUTOUT CRACKED IN LT AND RT RADIUS .5 INCH EACH SIDE. MAINTENANCE REPAIRED CRACKED AREAS IAW REO 601R53-11 -010, REV C. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007080900034 20070809 00034 CE 2007 8 9 DXTA200702359 1 20070729 A 3240 BRAKE ASSY CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 950QS 7500050 TO GET EVEN BRAKING FROM THE CAPTAINS BRAKE PEDALS, THE RT PEDAL MUST BE PUSHED DOWN APPROX TWICE AS MUCH AS THE LT. TH E CO-PILOTS PEDALS ARE THE SAME EXCEPT THE SPLIT IS MUCH LESS. [08-23-07] INSPECTED POWER BRAKE METERING VALVE. NO DE FECTS NOTED. PERFORMED COMPLETE BRAKE BLEED, SYSTEM LEAK AND OPS CHECK GOOD. IAW C750 M.M. 32-42-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007080900045 20070809 00045 EA 2007 8 9 COMA0760499 1 20070724 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 7014 FLIGHT 5542 - EMERGENCY LIGHTS FROM 9A BACK DO NOT WORK. PERFORMED OPS CHECK OF EMERGENCY LIGHTS. OPS CHECK NORMAL. 2 L 7 2 4F RT A21EA 2007080900046 20070809 00046 EA 2007 8 9 COMA0760500 1 20070726 A 3350 OL3071BPEGPL LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS FAILED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 7022 FLIGHT 5576 - OVERHEAD EMERGENCY LIGHTS IN CABIN INOP. RELAMPED OVERHEAD EMERGENCY EXIT LIGHTS. 2 L 7 2 4F RT A21EA 2007080900048 20070809 00048 WP 2007 8 9 ABXR070251 1 20070716 A 5312 591013085 GUSSET DOUG DC9 DC915F 3022037 WP BULKHEAD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 563PC 47055 PASSENGER AFT ENTRANCE DOOR AFT PRESSURE BULKHEAD CUTOUT LOWER LEFT CORNER LEAKED AND SHOWED EVIDENCE OF A CRACK IN THE DOUBLERS. REPAIRED LOWER AFT PRESSURE BULKHEAD IAW REA D953-56099-MR. P/N'S: 5910130-85/87, CRACK LENGTHS: 2.250" AND 1.625". 2 L 7 2 4F A6WE 2007080900049 20070809 00049 EA 2007 8 9 VNAA0707006 1 20070711 A 3260 895304 PSEU CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE MLG FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 723PS 6502 10181 CREW REPORTED ON CLIMBOUT A GEAR DISAGREE WARNING, WOW INPUT CAUTION AND PROXY SYSTEM FAIL MESSAGES. CREW FOLLOWED THE QRH, RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, THEN REMOVED AND REPLACED A FAULTY PROXIMITY S ENSOR ELECTRONIC UNIT (PSEU) IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 32-61-00-400-801. OPERATIONAL CHECKS WE RE PERFORMED. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007080900052 20070809 00052 CE 2007 8 9 BSYA200700013 1 20070730 A 2612 24403915 FIRE LOOP LEAR 35 35A 5170602 CE LT NACELLE DEFECTIVE E BSYA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 07 400JE 120 AIRCRAFT EN ROUTE FROM ILG TO SDF WHEN THE LT ENGINE FIRE LIGHT CAME ON, PULLED FIRE HANDLE AND FIRED BOTH FIRE BOTTLES THEN DIVERTED TO LCK, LANDED NO PROBLEMS. MAINTENANCE FOUND ENGINE ACCESSORY FIRE LOOP DEFECTIVE, REMOVED AND REPLACED FIRE LOOP, OPS CHECKS GOOD. 2 L 7 2 4F A10CE 2007080900054 20070809 00054 2007 8 9 SWAA073717 4 20070727 A 2565 1061323468 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR UNWANTED DEPLOY A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM . 2 L 7 2 4F RT A16WE 2007080900055 20070809 00055 NM 2007 8 9 SWAA073733 1 20070729 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 449WN 32469 EEPLS INOP AT ROW 5 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007080900060 20070809 00060 NM 2007 8 9 SWAA073718 1 20070727 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 431WN 29845 EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007080900061 20070809 00061 2007 8 9 SWAA073729 4 20070728 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 441WN 29837 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007080900064 20070809 00064 NM 2007 8 9 SWAA073737 1 20070729 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 485 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 485, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007080900065 20070809 00065 NM 2007 8 9 SWAA073722 1 20070727 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 740D S19R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740D, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007080900066 20070809 00066 NM 2007 8 9 SWAA073723 1 20070727 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM BS 807-827 S17L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 807 AND BS 827, STR 18L AND STR 17L. REPAIRED SKIN P ER SWA EA. 2 L 7 2 4F RT A16WE 2007080900067 20070809 00067 NM 2007 8 9 SWAA073736 1 20070729 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 790 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 790, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007080900074 20070809 00074 NM 2007 8 9 SWAA073734 1 20070729 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM EMERGENCY EXIT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 484WN 33841 L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007080900075 20070809 00075 NM 2007 8 9 SWAA073716 1 20070727 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM EMERGENCY EXIT DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 L2 DOOR EMERGENCY EXIT LIGHT ASSY FELL OFF. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007080900076 20070809 00076 NM 2007 8 9 SWAA073731 1 20070729 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 219WN 32490 FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007080900077 20070809 00077 NM 2007 8 9 SWAA073761 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 500A S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900080 20070809 00080 NM 2007 8 9 SWAA073763 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 360 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900082 20070809 00082 NM 2007 8 9 SWAA073758 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 500D S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900083 20070809 00083 NM 2007 8 9 SWAA073757 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 360 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900084 20070809 00084 NM 2007 8 9 SWAA073764 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 597 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900085 20070809 00085 NM 2007 8 9 SWAA073756 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 887 S1 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900086 20070809 00086 NM 2007 8 9 SWAA073755 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 847 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080600013 20070806 00013 NM 2007 8 6 2007UALA02754 1 20070720 A 2730 CONTROL UNIT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ELEVATORS MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 535UA 25130 CREW REPORTS RT ELEVATOR PCU EICAS MESSAGE. 09-07-07 FOUND MIDDLE ACTUATOR FAULT ON RT ELEVATOR DURING CHECK. REPLA CED RT CENTER ELEVATOR POWER CONTROL UNIT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080600017 20070806 00017 NM 2007 8 6 2007UALA02758 1 20070719 A 3244 TIRE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE MLG FAILED A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 772UA 26930 LEFT WING INBD FLAP LEADING EDGE AND LOWER SKIN SUSTAINED DAMAGED. [08-14-07] 1R MLG TIRE RECAP CAME OFF DURING TAKE OFF ROLL. DAMAGE TO PANELS 552CB, 551FB AND BULLNOSE OF LT INBD MID FLAP HAS DAMAGE REQUIRING GLASS LAYUP REPAIRED. WI NG INBD FLAP LEADING EDGE AND LOWER SKIN SUSTAINED DAMAGED DUE TO TIRE FAILURE. DAMAGE IS LOCATED 78" INBD OF OUTBD EDGE . DAMAGED OCCURED OVER THE FWD SPAR WHERE FASTENERS ARE PULLED AND LOWER SKIN IS CRACKED ACROSS 5 FASTENERS TOTALING 6" IN LENGTH. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007080600038 20070806 00038 NM 2007 8 6 2007UALA02797 1 20070722 A 2822 CHECK VALVE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUEL TRANSFER FAILED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 843UA 1573 UNWANTED FUEL TRANSFER FROM RT WING TO CTR TANK. TRANSFER RATE APPROX 500 LBS PER HOUR. CENTER BOOST PUMP CHECK VALVE LEAKING FUEL. REPLACED CENTER BOOST PUMP CHECK VALVE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080600043 20070806 00043 NM 2007 8 6 TIPR200736002 1 20070724 A 5330 SKIN BOEING 767 767222 1385122 NM BS 1356-1359 CORRODED B K NONE O OTHER IN INSP/MAINT 1 WP 29 609UA 21870 AFT PIT SKIN CORRODED AT FS 1356 TO FS 1359 STRINGER 39L TO STRINGER 38L. REMOVED CORROSION AND FOUND TO BE OUT OF LIMI TS IN ACCORDANCE WITH B767-200 SRM 53-00-01. ORIGINAL MATERIAL THICKNESS IS .105 MATERIAL REMAINING .057 MATERIAL REMOV ED .048. FABRICATED AND INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH B767-200 SRM 53-00-01. UT GAUGE TOOL T8225I. 2 L 7 2 4F RT A1NM 2007080600045 20070806 00045 EA 2007 8 6 TRAX200701029 1 20070720 A 5720 PLATE CNDAIR CL600 CL6002C10 1390015 EA RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 724EV 10138 LEFT TELESCOPE DUCT CLOSING PLATE CRACKED (LT OR RT WING SLAT CLOSING PLATES). 10-18-07 INSTALLED NEW ANT-ICE TELES COPIC DUCT CLOSING PLATE IAW CRJ 700 AMM 57-40-01. OPS CK GOOD. 2 L 7 2 4F RT A21EA 2007080600053 20070806 00053 EU 2007 8 6 USAA070579 1 20070724 A 5315 D5311281820401 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 183UW 1539 FLOORBEAM Y254 AT FRAME 16 HAS CORROSION. FABRICATED FILLER AND REPAIR ANGLES, INSTALLED WITH LOCK FASTENERS; CORR TASK JA-220-53500; LEVEL 1, DEFECT SIZE: 1 X 1 INCH. 2 L 7 2 4F RT A28NM 2007080600054 20070806 00054 EU 2007 8 6 USAA070578 1 20070724 A 5321 FLOORBOARD AIRBUS A321 A321211 3930370 EU CABIN DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 183UW 1539 FWD CABIN FLOOR HAS DELAMINATION. FABRICATED PER MCGILL IRM 970 REV F PER MCGILL MANUAL; CORR TASK JA-220-53500, DEFECT SIZE: 6 X 12 INCHES. 2 L 7 2 4F RT A28NM 2007080600064 20070806 00064 SO 2007 8 6 C2XA07IA170 1 20070720 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 13978 145180 CAE310095 FLT 2072, CREW REPORTED THAT FIRST ENG START HAD BEEN ABORTED DUE TO A HUNG START & A STRONG ODOR OF FUEL, ENGINE DRY MO TORED, & STARTED SUCCESSFULLY OFF OF FADEC B. ACFT LANDED WITHOUT INCIDENT. MX PLACED IGNITION SYSTEM ON MEL 74-20-00 CAT B CTL 125656, & ACFT APPROVED FOR RETURN TO SERVICE. 10-9-07 MX R & R "A" IGNITION EXCITER, OPERATIONALL CHECKED WITH NO DEFECTS, REMOVED MEL, & ACFT APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007080600086 20070806 00086 NM 2007 8 6 SWAA073630 1 20070724 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 787 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080600087 20070806 00087 NM 2007 8 6 SWAA073629 1 20070724 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 747 S6L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080600089 20070806 00089 NM 2007 8 6 SWAA073633 1 20070724 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 767 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080600093 20070806 00093 2007 8 6 SWAA073614 4 20070723 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007080600097 20070806 00097 NM 2007 8 6 SWAA073623 1 20070724 A 2560 P4010021 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 712SW 27846 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERIES PER MM. 2 L 7 2 4F RT A16WE 2007080600113 20070806 00113 WP 2007 8 6 ASAA0781882 1 20070724 A 5753 5930479513 SKIN DOUG DC9 DC983 3022083 WP TE FLAP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 LEFTHAND WING INBOARD FLAP T/E IS DELAMINATED. BONDED DOUBLER IN PLACE PER SRM 51 03. 2 L 7 2 4F RT A6WE 2007080600128 20070806 00128 WP 2007 8 6 ABXA070243 1 20070703 A 5340 39261591AX FITTING DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 FITTING EXFOLIATED ON SLANT PANEL UNDER LEFT BUTT LINE 22 AT STA 737. REPLACED FITTING IAW DC9 SRM. 2 L 7 2 4F A6WE 2007080600133 20070806 00133 NM 2007 8 6 ABXA070247 1 20070704 A 5330 141T3330 SKIN BOEING 767 767200 1385120 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AX 23432 R1 DOOR LOWER AFT CUTOUT CORNER WAS CRACKED. REPAIRED AREA IAW B767 SRM. 2 L 7 2 4F RT A1NM 2007080600134 20070806 00134 EA 2007 8 6 TRAX200701041 1 20070722 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 851AS 7360 CAPTAIN'S FLASHLIGHT IS INOP. 2 L 7 2 4F RT A21EA 2007080600138 20070806 00138 2007 8 6 SWAA073671 4 20070725 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM L1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM. 2 L 7 2 4F RT A16WE 2007080600151 20070806 00151 NM 2007 8 6 KCSA071257 1 20070726 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1902 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 AFT PIT SEAT TRACK WEB AT LBL-25 HAS AN OPEN HOLE AT STA-1902. 2 L 7 4 4F RT A20WE 2007080600157 20070806 00157 NM 2007 8 6 2007UALA02774 1 20070722 A 3350 58791 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 595UA 28748 EMERGENCY FLOOR LIGHTS INOP (EEL) FROM DOOR 2 LEFT TO ROW 15. *S/D* SECURED BATTERY CONNECTOR, OPS CHECK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080600161 20070806 00161 NM 2007 8 6 2007UALA02789 1 20070722 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EMERGENCY LIGHT ROW 50 ABC INOPERATIVE. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080600169 20070806 00169 EU 2007 8 6 YENA2007067 1 20070724 A 5270 INDICATOR EMB ERJ190 ERJ190100IGW 3260408 EU PAX DOOR OBSTRUCTED A YENA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 206JB 19000025 FLT 1100, RDU TO JFK, AIR RETURN TO RDU DUE L2 PAX DOOR OPEN INDICATION ON EICAS. RAN CHECK LIST ONLY ONE INDICATOR WAS GREEN, RETURNED TO FIELD. ITEM PLACED ON MEL 52-70-01 COND 2 CAT C. [08-06-07] FOUND L2 DOOR AFT VISUAL-LOCK INDICA TOR RETAINING RING MISSING. THIS CAUSED THE INDICATOR TO BIND AND NOT SHOW AN ACCURATE INDICATION. INSTALLED NEW RETAINI NG RING AS PER AMM REF 52-12-22, L2 DOOR INDICATION CHECKS GOOD ON DOOR AND ON EICAS DISPLAYS STATUS PAGE 2 L 7 2 4F RT A57NM 2007080600172 20070806 00172 EA 2007 8 6 TRAX200701046 1 20070724 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A AOSA K NONE O OTHER IN INSP/MAINT 1 SO 27 873AS 7549 THE 280 FRAME CLIP IS CRACKED AT O/B SIDE OF THE RBL 9. 2 L 7 2 4F RT A21EA 2007080600174 20070806 00174 EA 2007 8 6 TRAX200701048 1 20070724 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA LT OVERWING INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 848AS 7339 LEFT OVERWING EMERGENCY EXIT LIGHT INOP. 2 L 7 2 4F RT A21EA 2007080600177 20070806 00177 EA 2007 8 6 TRAX200701051 1 20070725 A 5220 HANDLE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 833AS 7246 CREW ESCAPE HATCH OUTER HANDLE DOES NOT LATCH PROPERLY. 10-18-07 REPAIRED AFT DRAG ANGLE ON PAX DOOR IAW REO 601R- 52-11-513. 2 L 7 2 4F RT A21EA 2007080600179 20070806 00179 EA 2007 8 6 TRAX200701057 1 20070725 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 854AS 7382 THE 280 AFT ANGLE COMMON TO THE EMERGENCY RELEASE CABLE O/B OF LBL 9 IS CRACKED. [08-09-07] REMOVED AND REPLACED 280 AFT ANGLE IAW REO 601R-53-11-1218. 2 L 7 2 4F RT A21EA 2007080600183 20070806 00183 EA 2007 8 6 TRAX200701061 1 20070726 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 349 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 873AS 7549 FS 349 FRAME IS CORRODED AT BL 0.0. [08-06-07] WORK COMPLETED IN ACCORDANCE WITH: SRM 51-42-21, 51-42-06, 51-41-02, 51-21-06, 51-40-11, 51-42-02, 51-21-11, 51-23-00, AND 12-21-00. 2 L 7 2 4F RT A21EA 2007080600187 20070806 00187 SO 2007 8 6 RAIA00707041 1 20070725 A 3350 BULB EMB 145 EMB145 3260210 SO EMERGENCY LIGHT INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 803HK 145077 PRE FLT 3514 - PIT - EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB AT THE AFFECTED LIGHT . 2 L 7 2 4F RT T00011AT 2007080600201 20070806 00201 NM 2007 8 6 SWAA073696 1 20070726 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM BS 520 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080600212 20070806 00212 NM 2007 8 6 KCSA071264 1 20070728 A 5311 FRAME BOEING 747 7472B4B 138481B NM BS 1265 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 LEFT FUSELAGE FRAME WEB AT FLOOR INTERCOSTAL IS CRACKED AT STA 1265, BETWEEN STR 23L AND 27L. 2 L 7 4 4F RT A20WE 2007080700010 20070807 00010 EU 2007 8 7 2007UALA02831 1 20070724 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE AFT GALLEY ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 465UA 1341 F/A REPORTS BURNING PLASTIC ODOR IN AFT GALLEY. INSPECTED OVENS AND COFFEE MAKERS NOTHING. PLASTIC STUCK TO BOTTOM O F AN OVEN TRAY LOADED INTO OVEN AND COOKED, REPLACED OVEN IN AFT GALLEY AS WELL AS CIRCUIT BREAKER PANEL FOR AFT GALLE Y OVENS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080700017 20070807 00017 NM 2007 8 7 2007UALA02838 1 20070725 A 3350 60243 LAMP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 348UA 24252 EMERGENCY ESCAPE PATH LIGHTS INOP, AFT 15 FEET OF CABIN INCLUDING LIGHT STRIP AT AFT GALLEY. REPLACED AFT SOLID LAMP AT AFT GALLEY AND AFT TRIPLE ELEMENT LAMP OF MAIN STRIP. DRIED MOISTURE FROM CONNECTIONS AT GALLEY WET AREA. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080700019 20070807 00019 NM 2007 8 7 2007UALA02840 1 20070725 A 3350 60443 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE ROWS 20AB-23A SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 MID GALLEY CROSSAISLE EMERGENCY EEL STRIP INOP. REPLACED EEL STRIP AT CROSSAISLE MID GALLEY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080700040 20070807 00040 NM 2007 8 7 NWAA072645514 1 20070726 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHTS MALFUNCTIONED A NWAA O OTHER O OTHER CR CRUISE 1 GL 01 514US 23202 DURING FLIGHT EMERGENCY LIGHTS FROM DOOR 3 AFT, INCLUDING GALLEY'S AND AISLE CAME ON AND REMAINED ON. RE-CYCLED FLIGHT DECK AND FORWARD CABIN ATTENDANT'S EMERGENCY LIGHT SWITCHES AND NO CHANGE. LATER IN FLIGHT LIGHTS BEGAN FLASHING ON AND OFF. FLIGHT CONTINUED ON AND LANDING WAS UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHEC KED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007080700049 20070807 00049 NM 2007 8 7 UPS07450256 1 20070704 A 5320 65B0433350 SUPPORT BOEING 747 747212B 1384886 NM BS 1920 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C AFT CARGO COMPT DIVIDER SUPPORT HOOK AREA FOUND CRACKED AT STA 1920 LBL 4 TO RBL 4 FLOOR AREA, CRACK L ENGTH 2". AFT CARGO COMPT DIVIDER SUPPORT AT BS 1920 LBL 42 TO RBL 42 REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 A ND 51-30-02. 2 L 7 4 4F A20WE 2007080700061 20070807 00061 NM 2007 8 7 UPS07450268 1 20070707 A 5320 65B11751606 REVEAL BOEING 747 747212B 1384886 NM R3 DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D R3 DOOR FWD LOWER CUTOUT CORNER REVEAL FOUND CRACK AS MARKED, CRACK LENGTH 1/2" APPROX. M/D R3 DO OR FWD LOWER CUTOUT CORNER REVEAL FTG REPLACED AN INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007080700064 20070807 00064 NM 2007 8 7 UPS07450271 1 20070709 A 5320 SILL BOEING 747 747212B 1384886 NM BS 434-440 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D L1 DOOR SILL FOUND CRACK, CRACK LENGTH 1" APPROX. M/D L1 DOOR SILL AT BS 434 TO BS 440 WEB REPAIR ED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2007080700065 20070807 00065 NM 2007 8 7 UPS07450272 1 20070705 A 5315 65B043525 FLOORBEAM BOEING 747 747212B 1384886 NM BS 2300 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D BS 2300 LBL50 FLOORBEAMS WEB REAR SIDE STIFFENER FOUND CRACKED AS MARKED, CRACK LENGTH 3/8". M/D BS 2300 LBL50 FLOORBEAM WEB REAR SIDE STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007080700066 20070807 00066 NM 2007 8 7 UPS07450273 1 20070706 A 5311 FRAME BOEING 747 747212B 1384886 NM BS 2231 S23-25R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D RT BS 2231 FRAME INNER CHORD S23R-25R FOUND 2 HOLES CRACK AT FRAME STRAP, CRACK LENGTH 1/16" AND 0 .040". M/D BS 2231 FRAME ATTACH INNER CHORD AND STRAP AT BEN STR 22R TO STR26R AREA REPAIRED AS PER SRM 53-10-04 FIG 11 5. CONTINUE INSP REQUIRED AS PER SRM 53-10-04 FIG 115. REFER NRC51555 FOR WORKING DETAIL. UPS MPI#P19305 RAISED. 2 L 7 4 4F A20WE 2007080700070 20070807 00070 NM 2007 8 7 UPS07450277 1 20070710 A 5315 FLOORBEAM BOEING 747 747212B 1384886 NM BS 1920 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C AFT CARGO COMPT CARGO FLOORBEAM UPPER TEE FOUND CORROSION AT STA 1920 CARGO NET ATT HOOK RBL4 TO LBL4. CORROSION BLEND OUT 0.045" BY 1.5" BY 2". AFT CARGO COMPT BS 1920 LBL 42 TO RBL 42 FLOORBEAM UPPER CHORD REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007080700077 20070807 00077 NM 2007 8 7 UPS07450288 1 20070708 A 5311 FRAME BOEING 747 747212B 1384886 NM BS 2231 S23-26R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D AFTER FURTHER FASTENER REMOVED, RT BS 2231 FRAME INNER CHORD AREA S23R-26R FOUND TOTAL 4 HOLES CRA CK AT DIFFERENT STACK UP STRUCTURES (FRAME STRAP, INNER CHORD) (CRACK LENGTH 0.040",1/16", THROUGH THICKNESS). M/DECK BS 2231 FRAME ATTACH INNER CHORD AND STRAP AT BETWEEN STR 22R TO STR 26R AREA REPAIRED AS PER SRM 53-10-04 FIG 115, CONT INUE INSP ARE REQUIRED AS PER SRM 53-10-04 FIG 115 (UPS MPI NR P19305 RAISED FOR CONTINUE INSP.) 2 L 7 4 4F A20WE 2007080700091 20070807 00091 EA 2007 8 7 MASA200700314 1 20070609 A 3350 GUARD CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17275 7275 ASH 2764 PHX - FA EMERGENCY LIGHT SWITCH GUARD WAS BROKEN. MX REPLACED THE GUARD. 2 L 7 2 4F RT A21EA 2007080700095 20070807 00095 EA 2007 8 7 MASA200700321 1 20070611 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 592ML 7410 ASH 7157 DSM - NR 6 EXTERNAL EMERGENCY LIGHT WAS INOP. MX REPLACED THE LAMP, OP CHECK GOOD. 2 L 7 2 4F RT A21EA 2007080700098 20070807 00098 EA 2007 8 7 MASA200700327 1 20070612 A 2570 DOOR CNDAIR CL600 CL6002B19 1900309 EA STORAGE BIN STUCK A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77286 7286 ASH 2782 LAS - FLIGHT ATTENDANT STORAGE BIN FOR EMERGENCY EQUIPMENT WILL NOT OPEN. MX GOT THE DOOR OPEN. 2 L 7 2 4F RT A21EA 2007080700101 20070807 00101 EA 2007 8 7 MASA200700333 1 20070617 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN CONTAMINATED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77278 7278 ASH 2704 PHX - LT EMERGENCY OVERWING EXIT LIGHT INOP. MAINTENANCE CLEANED MOISTURE. 2 L 7 2 4F RT A21EA 2007080700110 20070807 00110 EU 2007 8 7 07FDEA02649 1 20070728 A 5710 A5726021320600 BEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 657FE 748 LT WING TIP INBD T/E UPPER SURFACE STATIC WICK BASE HAS 2 SQ IN AREA OF CORROSION EXTENDING UNDER BASE BETWEEN BASE AND UPPER SKIN SURFACE. REF A300 AMM 57-00-00. REMOVED AND REPLACED UPPER BEAM ON WING TIP IAW A300-600 SRM 57-30-11-4 AND SRM 51-40-21. REMOVED AND REINSTALLED WING TIP IAW A300-600 AMM 57-30-11-4. REMOVED AND REPLACED STATIC WICK IAW A300 -600 AMM 23-61-21-4, RESISTANCE CHECK GOOD, NAV PARK LIGHTS OPS CHECK GOOD IAW A300-600 AMM 33-41-31. 2 L 7 2 4F RT A35EU 2007080700115 20070807 00115 WP 2007 8 7 07FDEA02667 1 20070730 A 5312 PRESSURE PANEL DOUG DC10 DC1010F 3022111 WP ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 NLG W/W ON VERTICAL PRESSURE PANEL FOUND CRACKED. REPAIRED WEB IAW SRM 53-40-00 FIG 34 VOL 1. 2 L 7 3 4F A22WE 2007080700117 20070807 00117 GL 2007 8 7 SIMA200721103 2 20070726 A 7261 AE3007A1 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LEFT LEAKING A SIMA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SW 21 619AE 14095 930 145101 CAE311467 LAVATORY SMOKE ALARM GOING OFF INFLIGHT, NO SMOKE NOTED. REMOVED AND REPLACED NUMBER 1 ENGINE IAW AMERICAN EAGLE WORKCA RD 72-000-00. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007080700132 20070807 00132 NM 2007 8 7 AWXA200700920 1 20070704 A 5311 654655514 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5981850, CRACKED FRAME, BS 867, S9R. REPAIRED FRAME, BS 867, S9R IAW USAIRWAYS EA 120121. 2 L 7 2 4F RT A16WE 2007080700142 20070807 00142 NM 2007 8 7 DL76S070962 1 20070702 A 5330 146T3261 SKIN BOEING 767 767332 1382001 NM BS 785-915 S8L DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 130DL 24080 DURING HMV3 AT MOBILE AREOSPACE ENGINEERING, FOUND LT FUSELAGE STA 785.9-915, S2L, S8L HAS LIGHTNING STRIKES. REMOVED D AMAGE AND FAB`D DOUBLER REF SRM 530001 REPAIR 4. 2 L 7 2 4F RT A1NM 2007080700143 20070807 00143 NM 2007 8 7 DL76S070963 1 20070701 A 5330 146T3330 SKIN BOEING 767 767332 1382001 NM BS 915-1065 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 130DL 24080 LT FUSE STA 915-1065, S4-7L HAS LIGHTNING STRIKE DAMAGE. REMOVE DAMAGED AREA INSTALLED DOUBLER REF SRM 530001 REPAIR 4. 2 L 7 2 4F RT A1NM 2007080700151 20070807 00151 NM 2007 8 7 DU4R2007148 1 20070709 A 5311 FRAME BOEING 757 757 UTILUSE NM PWA 2037 PW2037 NE BS 1520 DENTED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 638DL 23761 S/O 291043, NR22684, FOUND DENT ON FUSELAGE FRAME AFT PIT BS 1520 LBL 26. REPAIRED BY TRIMMING OUT DENTED AREA, HFEC CUT OUT IAW D6-34N301, PT. 6 51-00-19, NO RELEVANT INDICATIONS. FABRICATED AND INSTALLED REPAIR DOUBLER 19-1/4, X 2-3/4 , X 1-1/2, FROM 7075-T6 .063 IAW SRM 53-60-07, 51-20-01 AND 51-40-02. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080700182 20070807 00182 NM 2007 8 7 AMTA200700332 1 20070707 A 5210 1281T10015 ACTUATOR LKHEED 1011 1011 N/A-SDR NM RROYCE RB211 RB211524B4 54555 NE L1 DOOR UNSERVICEABLE A AMTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 11 163AT 293A1229 L1 DOOR WILL NOT CLOSE ELECTRICALLY, SOLENOID LUBED, NO HELP. REPLACED UP/DOWN LOCK LIMIT SWITCH. OPS CK GOOD. (K) 2 L 7 3 4F 4 F RT A23WE E12EU 2007080800001 20070808 00001 NM 2007 8 8 AMTA200700336 1 20070710 A 3350 LENS BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHTS MISSING A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 RED EGRESS LENS AND 1 WHITE EGRESS LENS MISSING BY R-2 DOOR. REPLACED 1 RED AND 1 WHITE EGRESS LENS BY R-2 DOOR. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007080800002 20070808 00002 NM 2007 8 8 AMTA200700337 1 20070711 A 3040 UNKNOWN BOEING 737 73783N 13844HI NM WINDOW HEAT WARNING LIGHT A AMTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 321TZ 28249 REJECTED T/O AT 90 KIAS FOR MASTER CAUTION/ WINDOW HEAT LIGHT. PERFORMED BITE TEST IAW AMM 30-41-00 SYSTEM CHECKS NORMA L, NO FAULTS. (K) 2 L 7 2 4F RT A16WE 2007080800009 20070808 00009 EA 2007 8 8 A6WA200740332 1 20070620 A 3610 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE 10TH STAGE VALVE FAILED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 10TH STAGE ISO VALVE WILL NOT OPEN. REINSTALLED CONNECTOR ON 10TH STAGE VALVE, OPS CHECK GOOD, OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007080800011 20070808 00011 EA 2007 8 8 A6WA200740333 1 20070626 A 2910 ADA686301 FILTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HYD SYSTEM FAILED A A6WA O OTHER L NO TEST NR NOT REPORTED 1 GL 31 418AW 7618 AIRCRAFT FAILED HYDRAULIC SYSTEM TEST ON THE FIRST FLIGHT OF THE DAY CHECK. (NR2 SYSTEM) REMOVED AND REPLACED HYDRAULI C MANIFOLD NR 2, REF 29-11-05. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007080800012 20070808 00012 EA 2007 8 8 A6WA200740383 1 20070709 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY EXIT OUT OF RIG A A6WA K NONE L NO TEST IN INSP/MAINT 1 GL 31 419AW 7633 110612 MWC NR 53 CREW ESCAPE HATCH FAILED FUNCTIONAL TEST, ADJUSTMENT TO BE CARRIED OUT IAW AMM 52-22-00-820-801. CREW ESCAPE HATCH RIGGED IAW AMM 52-22-00-820-801. CREW ESCAPE HATCH RIGGED IAW AMM 52-22-00-820-002. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007080800031 20070808 00031 2007 8 8 DJFA2007077 4 20070718 A 2210 8221019313 COMPUTER BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE AUTOPILOT FAILED E DJFA O OTHER F FLT CONT AFFECTED CR CRUISE 1 EA 23 790TA 6408 RK252 TRIP NR 1204871- CREW REPORTED A PITCH TRIM FAILURE. CREW PERFORMED EMERGENCY PROCEDURES AND CONTINUED TO DESTINATION. MAINTENANCE DISCOVERED THE AUTOPILOT COMPUTER MALFUNCTIONED. THE COMPUTER WAS REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007080800034 20070808 00034 SO 2007 8 8 GLBA20060964 1 20070721 A 2910 LINE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE HYD SYSTEM LEAKING A GLBA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 03 71GL 120071 HYDRAULIC SYSTEM FLUID LOSS. PILOTS REPORTED UPON LANDING APPROACH WHEN THE GEAR WAS EXTENDED, THE GREEN HYDRAULIC SYST EM APPEARED TO HAVE LOST ALL HYDRAULIC FLUID. MAINTENANCE SPLICED A RIGID STAINLESS STEEL HYDRAULIC LINE IN THE LT NACE LLE AREA IAW MM 20-10. BOTH HYDRAULIC SYSTEMS WERE SERVICED IAW MM 12-13 AND A LEAK CHECK OF THE SYSTEM WAS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2007080800039 20070808 00039 CE 2007 8 8 DXTA200702344 1 20070718 A 2160 64641PAR SEAL RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP TEMP VALVE LEAKING E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 816QS 7012 258416 DURING CLIMB THROUGH 9000 FT REAR BAY OVERHEAT ANNUNCIATOR CAME ON INTERMITTENTLY 3 TIMES. THEN STEADY FOR 5 SECONDS THE N OUT. LIGHT STAYED OUT UNTIL SHUTDOWN. FOUND CABIN TEMPERATURE CONTROL VALVE SEALS LEAKING. REMOVED AND REPLACED VAL VE SEALS. RAN ENGINES. OPS AND LEAK CHECKS GOOD. IAW MM CH 21-10-00 2 L 7 2 4F 4 F RT A3EU E6WE 2007080800072 20070808 00072 CE 2007 8 8 AMWA06032J 1 20070725 A 5311 1294300311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 378 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080800085 20070808 00085 CE 2007 8 8 AMWA06032A 1 20070725 A 5410 STRUCTURE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT NACELLE CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 FRICTION CHAFING DURING OPERATION HAS CREATED WORN SEGMENTS ON THE LT ENGINE NACELLE. DAMAGE WAS ALONG THE ENTIRE LENGT H OF THE NACELLE SHAPE: DEPTH VARIED AS INDICATED ON THE REPAIR AUTHENTICATION. REPAIRED IAW ACFT ENGINEERING REPORT 67 99-2 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080800115 20070808 00115 NE 2007 8 8 H3V2007F00000 1 20070708 A 6320 PIN SKRSKY SKRSKY S64 CH54A 8142501 NE PWA JFTD12 JFTD12A4A 52047 NE M/R GEARBOX MISSING L H3VL O OTHER O OTHER NR NOT REPORTED 1 WP 17 44094 A6046 6718421 ON JULY 8, 2007, HLH EXPERIENCED A HARD GROUND ROLLOVER OF AC. INITIAL INSPECTION OF THE WRECKAGE REVEALED A SERVO PIN, PN 6465-20201-101, FROM THE LT LATERAL SERVO, PN S1565-20421-042, WAS MISSING FROM THE TRANSMISSION LUG CAUSING THE SER VO TO REMOVE ITSELF FROM THE TRANSMISSION LUG CAUSING THE SERVO TO REMOVE ITSELF FROM THE TRANSMISSION MOUNT. THE LOCKI NG PIN HOLDER, PN 6465-20202, PIN PN 6465-20201-101, BOLT PN AN6H5, AND NUT PN NAS509-4 WERE ALL FOUND INTACT AND LOCKWI RED TOGETHER. NUT HAD BEEN PULLED FROM STUD O TRANSMISSION MOUNT. THIS HAS NOT BEEN DETERMINED TO BE THE CAUSE OF THE ACCIDENT, HOWEVER, HLH FEELS IT IMPORTANT TO SHARE THIS INFORMATION WITH OTHER OPERATORS, IN INTEREST OF SAFETY. (K) 2 G 7 2 4U 4 U H16NM E15EA 2007080900014 20070809 00014 NM 2007 8 9 AMTA200700353 1 20070718 A 3040 CONTROL UNIT BOEING 737 73783N 13844HI NM WINDOW HEAT MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 319TZ 30643 WINDOW HEAT OVERHEAT LIGHT. LIGHT ON-R FWD. PERFORMED FIM 30-41-00. SWAPPED RT FWD AND RT SIDE WINDOW HEAT CONTROL UN ITS. TESTED ALL WINDOW HEAT UNITS IAW AMM 30-41-11-5. OPS NORMAL ALL WINDOWS ON FLIGHT DECK. (K) 2 L 7 2 4F RT A16WE 2007080900020 20070809 00020 NM 2007 8 9 AMTA200700363 1 20070725 A 3350 20131 BATTERY PACK BOEING 757 75723N 1384973 NM EMERGENCY LIGHTS INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 519AT 27975 EGRESS LIGHTING INOP (B) ZONE LT SIDE. REMOVED AND REPLACED BATTERY PACK OVERHEAD AT L-2 DOOR, (B) ZONE EGGRESS LIGHTIN G OPS CHECKS NORMAL IAW 33-51-07. (K) 2 L 7 2 4F RT A2NM 2007080900044 20070809 00044 EA 2007 8 9 COMA0760498 1 20070723 A 5270 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR WARNING MESSAGE A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 594SW 7285 FLIGHT 5153 - PAX DOOR OUTER HANDLE MESSAGE IN FLIGHT. RAN QRH PROCEDURE AND DIVERTED TO ACY AND LANDED SAFELY. TRANSF ERRED TO DMI LIST PER 52-70-01-1. 2 L 7 2 4F RT A21EA 2007080900057 20070809 00057 NM 2007 8 9 SWAA073728 1 20070727 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 236WN 34631 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 20 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007080900058 20070809 00058 NM 2007 8 9 SWAA073720 1 20070727 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 453WN 29847 EEPLS COVER MISSING AT ROW 11 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007080900063 20070809 00063 NM 2007 8 9 SWAA073725 1 20070727 A 5330 6545765 SKIN BOEING 737 7375H4 138449D NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT GROUND AIR HOOK UP CUTOUT BS 520, RBL 7.5. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007080900072 20070809 00072 NM 2007 8 9 SWAA073721 1 20070727 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 847 S13R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 847, STR 13R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007080900081 20070809 00081 NM 2007 8 9 SWAA073754 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 787 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900087 20070809 00087 NM 2007 8 9 SWAA073759 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 578 S2L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900091 20070809 00091 NM 2007 8 9 SWAA073751 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 827 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900096 20070809 00096 NM 2007 8 9 SWAA073765 1 20070730 A 5313 65C27314 STRINGER CLIP BOEING 737 7373K2 13844BA NM BS 400 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900097 20070809 00097 NM 2007 8 9 SWAA073742 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 420 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900098 20070809 00098 NM 2007 8 9 SWAA073743 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 460 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900099 20070809 00099 NM 2007 8 9 SWAA073744 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 480 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900101 20070809 00101 NM 2007 8 9 SWAA073753 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727D S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900102 20070809 00102 2007 8 9 SWAA073726 4 20070727 A 2565 6949956 CABLE BOEING 737 7375H4 138449D NM R2 DOOR SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2007080900103 20070809 00103 NM 2007 8 9 SWAA073771 1 20070730 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 467WN 33830 DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 2 ABC AND ROW 5 ABC. REMOVED AND REPLACED COVER PER M M. 2 L 7 2 4F RT A16WE 2007080900104 20070809 00104 NM 2007 8 9 SWAA073769 1 20070730 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 251WN 32510 DURING SCHEDULED MV2 CHECK, FOUND EEPLS END CAP MISSING AT ROW 1 ABC. INSTALLED END CAP PER MM. 2 L 7 2 4F RT A16WE 2007080900108 20070809 00108 NM 2007 8 9 SWAA073775 1 20070731 A 5311 6546525 FRAME BOEING 737 7373K2 13844BA NM BS 380 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080900109 20070809 00109 NM 2007 8 9 SWAA073793 1 20070731 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM BS 380 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080900111 20070809 00111 NM 2007 8 9 SWAA073801 1 20070731 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM BS 380 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080900117 20070809 00117 NM 2007 8 9 SWAA073779 1 20070731 A 5311 6546529 FRAME BOEING 737 7373K2 13844BA NM BS 440 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080900118 20070809 00118 NM 2007 8 9 SWAA073802 1 20070731 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080900119 20070809 00119 NM 2007 8 9 SWAA073818 1 20070731 A 5311 6546529 FRAME BOEING 737 737317 138447P NM BS 440 S8-8LR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080900122 20070809 00122 2007 8 9 DL777070965 4 20070729 A 3442 ANTENNA BOEING 777 777232 1385232 NM WX RADAR SYS INOPERATIVE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 864DA 29736 CREW REPORTED WEATHER RADAR PROBLEMS UNABLE TO USE WEATHER RADAR MEL. RETURNING TO GATE FOR REPAIRS. WXR ANTENNA DRIVE UNIT REPLACED IAW AMM 34-43-03-000-802. OP CKS OK, MFG P/N 622-5136-202. 2 L 7 2 4F RT T00001SE 2007080900125 20070809 00125 NM 2007 8 9 DL76G070970 1 20070730 A 3610 361002241 SHUTOFF VALVE BOEING 767 767332 1382001 NM NR 2 ENGINE INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 177DZ 29698 UKN 1707 FLT 150/30 JFK-VCE ATB DUE TO RT ENG HPSOV INOP. REMOVED AND REPLACED RT ENG HPSOV PER MM. OPS AND LEAK CHK OK. 2 L 7 2 4F RT A1NM 2007080900126 20070809 00126 NM 2007 8 9 NWAA072665514 1 20070727 A 3350 SWITCH BOEING 757 757251 1384970 NM EMERGENCY LIGHTS SHORTED A NWAA O OTHER O OTHER CR CRUISE 1 GL 01 514US 23202 PILOT REPORTED WITH OVERRIDE SWITCH IN "ARMED" POSITION THE EMERGENCY AISLE LIGHTS FROM DOOR 3 AFT COME ON INTERMITTENTL Y. FLIGHT CONTINUED ON AND LANDING WAS UNEVENTFUL. MAINTENANCE FOUND A SHORTED SWITCH, WHICH THEY REPLACED, AND ALSO R EMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007080900127 20070809 00127 NM 2007 8 9 2007UALA02529 1 20070709 A 2700 UNKNOWN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE ELEVATOR UNKNOWN A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 308UA 23669 PILOT REPORTED HEAVY ELEVATOR. COULD NOT DUPLICATE ISSUE. NO FINDINGS. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080900130 20070809 00130 NM 2007 8 9 2007UALA02853 1 20070726 A 5320 SILL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 AFT CARGO DOOR LWR SILL-FLOOR SUPPORT ANGLE APPROX STA 815 AT STR 25R IS CRACKED IN RADIUS. SUPPLEMENTAL DATA UPDATE MA JOR REPAIR ACCOMPLISHED: REPLACED DAMAGED SILL FLOOR SUPPORT ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080900134 20070809 00134 NM 2007 8 9 2007UALA02857 1 20070726 A 3397 58781 FEEDER CABLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 304UA 23665 AFT CABIN EEL LIGHTS INOP FROM ROW 15 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT. R EPLACED EEL CABLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080900135 20070809 00135 NM 2007 8 9 2007UALA02858 1 20070726 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 559UA 26657 EXTERIOR EMERGENCY LIGHT AT DOORS 1R, 2R AND 4R ARE INOPERATIVE. REPLACED LAMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080900136 20070809 00136 NM 2007 8 9 2007UALA02859 1 20070726 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 EEL FLOOR STRIP LIGHT CONNECTION DAMAGED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080900139 20070809 00139 NM 2007 8 9 2007UALA02862 1 20070727 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 FOUND EMERGENCY LIGHTS INOP AT 2A FWD, 34 ABC AND 44 HJK. [08-21-07] REPLACED LIGHT ASSEMBLIES AT EACH SEAT POSITION . ALL EEL LIGHTS CHECKED READY FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080900141 20070809 00141 NM 2007 8 9 2007UALA02865 1 20070727 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 842 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 351UA 24319 AFT CARGO DOOR OPENING HAS SKIN AND BEAR STRAP DAMAGE ON LOWER AFT PART OF OPENING AT STA 842. MAJOR REPAIR ACCOMPLISH ED. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080900142 20070809 00142 NM 2007 8 9 2007UALA02866 1 20070729 A 2120 UNKNOWN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE GALLEY ODOR A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 854UA 1731 STRONG ELECTRICAL FUMES REPORTED IN AFT GALLEY. NO FURTHER INCIDENTS AS OF 8/22/07, UNABLE TO DUPLICATE SMELL, 2 L 7 2 4F 4 F RT A28NM E40NE 2007080900144 20070809 00144 NM 2007 8 9 2007UALA02868 1 20070727 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 871 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 AFT PASSENGER CABIN STA 871 BL 9 STR 1, 2 FASTENER HOLE FOR DORSAL FIN ARE OUT OF ROUND, WORN AND KNIFE EDGE INSIDE STRI NGER CHANNEL. MAJOR REPAIR ACCOMPLISHED: FABRICATED AND INSTALLED STRINGER NESTED REPAIR ANGLES. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080900145 20070809 00145 NM 2007 8 9 2007UALA02869 1 20070727 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 600 MISREPAIRED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 515UA 24840 EXTERNAL FUSELAGE EXTERNAL DOUBLER AT STA 600 LT SIDE HAS NO MINIMUM DISTANCE FROM EXISTING FLUSH REPAIR. MAJOR REP AIR ACCOMPLISHED. PERFORMED A FUSELAGE EXTERNAL DOUBLER REPAIR AT STA 600 LH SIDE WITHOUT A MINIMUM DISTANCE FROM EXIST ING FLUSH REPAIR. THIS IS AN INTERM REPAIR REQUIRING SUPPLEMENTAL INSPECTIONS STARTING AT 50000FC. THEN INSPECT UPPER A ND LOWER SKIN PANEL LAP SPLICE EVERY 3000FC. A DETAILED VISUAL INSPECTION IS THEN REQUIRED EVERY 12000FC. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080900147 20070809 00147 NM 2007 8 9 2007UALA02871 1 20070727 A 2910 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE HYD SYSTEM LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 658UA 27113 CREW REPORTED THAT CENTER HYDRAULIC SYSTEM QUANTITY WAS DECREASING EN ROUTE. SYSTEM WAS TURNED OFF AND FLIGHT CONTINUED . AMBER ALERT WAS DECLARED, FLIGHT LANDED UNEVENTFULLY AND PROCEEDED TO THE GATE UNDER IT'S OWN POWER. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080900149 20070809 00149 NM 2007 8 9 2007UALA02873 1 20070728 A 5512 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZONTAL STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 DENT ON RT HORIZONTAL STABILIZER LEADING EDGE CAUSED BY BIRD STRIKE. REMOVED DAMAGE. INSTALLED INTERNAL DOUBLER REPAIR AND REPLACED DAMAGED RIB. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080900150 20070809 00150 NM 2007 8 9 2007UALA02874 1 20070728 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 368 MISMANUFACTURED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 649UA 25286 CABIN FLOORBEAM AT BS 368 AND RBL 58 HAS 2 EACH MISDRILLED HOLES, ONE THROUGH UPPER CHORD AND WEB AND THE OTHER IN THE U PPER CHORD RADIUS. CUTOUT DAMAGE IN WEB AND OVERSIZED THE 2 MISDRILLED HOLES. FABRICATED 1 REPAIR ANGLE FOR THE FWD AN D AFT SIDE OF THE FLOORBEAM WEB. FABRICATED AND INSTALLED FILLERS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080900156 20070809 00156 NM 2007 8 9 2007UALA02880 1 20070728 A 3510 OXYGEN SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 CREW 02 LOW READS 1300 PSI. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080900158 20070809 00158 2007 8 9 2007UALA02882 4 20070729 A 2565 SLIDE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE L1 DOOR UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 DOOR 1L SLIDE PACK HAS 5 INCHES OF EXTRA SLIDE HANGING DOWN BELOW PACK. REINSTALLED SLIDE PACK IN CONTAINER. NO REPEA TS. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080900162 20070809 00162 EU 2007 8 9 2007UALA02886 1 20070729 A 5210 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 461UA 1266 DOOR 2L DOOR BOTTLE PRESSURE LOW. SERVICED DOOR 2L ASSIST BOTTLE- NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080900164 20070809 00164 EU 2007 8 9 2007UALA02888 1 20070727 A 3350 LAMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 469UA 1409 DOOR 2R EMERGENCY LIGHT LAMP INOP. LAMP ASSY BELOW EXIT SIGN. REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080900168 20070809 00168 NM 2007 8 9 2007UALA02892 1 20070727 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 346UA 24250 EEL LIGHT LAMP INOP, LOCATED AT SEAT ROW 3ABC. REPLACED LIGHT STRIP OPS CHK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080900170 20070809 00170 NM 2007 8 9 2007UALA02894 1 20070727 A 2800 UNKNOWN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUEL TRANSFER UNKNOWN A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 116UA 26908 APPARENT UNWANTED FUEL TRANSFER FROM CTR TANK TO TANK NR 3. FUEL INCREASE FROM 85.6 TO 86.4 IN APPROX 90 MINS HAS HISTO RY, CREW ALSO ADVISES THAT NR 3 AFT OVRD GREEN FLOW BAR ON SYNOPTIC IS ILLUMINATED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080900172 20070809 00172 2007 8 9 2007UALA02896 4 20070729 A 2565 GIRT BAR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE R5 DOOR DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 171UA 24322 DOOR 5R WILL NOT STAY IN ARMED POSITION. HANDLE POPS UP TO DISARMED POSITION AFTER ARM. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080900176 20070809 00176 NM 2007 8 9 2007UALA02900 1 20070729 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY LIGHT LT WALL OF AFT GALLEY INOPERATIVE . 2 L 7 4 4F 4 F RT A20WE E24NE 2007080900177 20070809 00177 NM 2007 8 9 2007UALA02901 1 20070729 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE SEAT 7C UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 815UA 867 FOUND SEAT 7C EEPM LIGHT HANGING OUT OF SEAT. REPLACED SEAT EEPM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080900178 20070809 00178 NM 2007 8 9 2007UALA02902 1 20070727 A 3350 LAMP AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 821UA 944 SMALL LOWER EMERGENCY EXIT SIGN AT DOOR 2L HAS ONE INOP LAMP. RELAMPED SIGN. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080900180 20070809 00180 NM 2007 8 9 2007UALA02904 1 20070728 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT OVERWING INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 538UA 25222 EEL LIGHT RIGHT WING EXIT DOOR INOP. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080900183 20070809 00183 CE 2007 8 9 RU3A0706 1 20070718 A 3150 UNKNOWN BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60A 52043 NE HARTZL HCB4M HCB4MP3 GL PROPELLER WARNING LIGHT E RU3A L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 SW 15 71 FF6 PCE95329 FWA2830 DURING FLARE FOR LANDING, THE AIRCRAFT ABRUPTLY AND WITHOUT WARNING YAWED HARD RIGHT. TOUCHDOWN OCCURRED DURING THE GO- AROUND. THE PILOT NOT FLYING REPORTED THAT THE RIGHT PROP PITCH LIGHT ILLUMINATED IMMEDIATELY PRIOR TO THE EXCURSION. AFTER THE GO-AROUND, THE PROPELLERS WERE RESET TO 1500 RPM AND A POWER-ON APPROACH TO LANDING WAS ACCOMPLISHED. DURING THAT TOUCHDOWN, THE RIGHT PROP PITCH LIGHT ILLUMINATED AGAIN. 2 L 7 2 4T 4 T A24CE E4EA 6 C P56GL 2007080900184 20070809 00184 WP 2007 8 9 IXXA07SMN174S 1 20070630 A 5313 LONGERON DOUG DC8 DC873F 302199F WP ZONE 200 BROKEN B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND IN MAIN CARGO COMPARTMENT FLANGE ON LONGERON 19 RIGHT BROKEN AT STATION 200.000 TO 212.000. LONGERON FLANGE FROM AT STATION 200.000 TO 212.000, LONGERON19 RIGHT WAS TRIMMED OFF IN PRODUCTION. NO RE PAIR IS REQUIRED. FOUND NO ADDITIONAL DAMAGE, IAW MESSAGE BOEING NUMBER 1-397537201-2 OF DATA 06-29-07, AND DRAWING 570 2880. 2 L 7 4 4F RT 4A25 2007080900186 20070809 00186 SO 2007 8 9 SIMA200721203 1 20070720 A 5320 14525480603 SILL EMB 135 EMB135KL 3260302 SO ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 821AE 13157 5000 145577 BAGGAGE DOOR CUTOUT CORRODED. REMOVED AND REPLACED SILL IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007080900187 20070809 00187 SO 2007 8 9 SIMA200721201 1 20070729 A 3260 852701 SWITCH EMB 135 EMB135KL 3260302 SO ZONE 700 FAILED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 807AE 14198 145506 RECEIVED AIR TO GROUND WARNING MESSAGE AND GEAR FAILED TO RETRACT, RETURNED TO IND. REMOVED AND REPLACED NOSE LANDING G EAR WEIGHT ON WHEEL SWITCH IAW EMB AM 32-63-02 AND RIGHT MAIN LANDING GEAR NUMBER 2 PROXIMITY SWITCH IAW EMB AMM 32-63-0 1. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007080900188 20070809 00188 SO 2007 8 9 SIMA200721205 1 20070730 A 3350 20131A POWER SUPPLY EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT FAILED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 703MR 10344 1039 145173 EMERGENCY INTERIOR LIGHTS INOPERATIVE. REMOVED AND REPLACED NUMBER 3 AND NUMBER 4 BATTERY POWER SUPPLIES IAW EMB 33-50- 04. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007080900189 20070809 00189 SO 2007 8 9 SIMA200721204 1 20070720 A 5210 14533996401 SUPPORT BRACKET EMB 135 EMB135KL 3260302 SO ZONE 800 CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 821AE 13157 5000 145577 MAIN DOOR HANDLE BRACKET CRACKED. REPAIRED DOOR BRACKET IAW EMB IC2007-145/05000 DATED JULY 24, 2007. 2 L 7 2 4F RT T00011AT 2007080900193 20070809 00193 EU 2007 8 9 07FDEA02674 1 20070730 A 5730 FX2241702502 PANEL AIRBUS 310 A310203 3930313 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 PNL 486BR HAS FRETTING CORRSION AND BARE METAL EXPOSED REMOVED CORRSION FOUND TO OUT OF LIMITS IAW A310-200 SRM 54-55-51 . FABRICATED NEW PANEL IAW A310-200 SRM AND GMM. ALODINED AND PRIMED IAW A310-200 SRM 51-21-10 AND 51-23-10. 2 L 7 2 4F RT A35EU 2007080600033 20070806 00033 NM 2007 8 6 2007UALA02783 1 20070722 A 3350 INVERTER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 775UA 26947 THE 2E BOTH EEL LIGHTS INOPERATIVE. [08-14-07] TROUBLESHOOTING FOUND INVERTER FAILED, INSTALLED SERVICEABLE REF WDG25 -25-21 SHT6. OPS CHECKED, SYS OPS NORMAL. RETURNED AC BACK TO NORM, OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007080600034 20070806 00034 NM 2007 8 6 2007UALA02786 1 20070722 A 2497 TERMINAL BLOCK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BURNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 FOUND BUNDY BLOCK BURNED AND DETERIORATED AT TB0158A POSITION 12. REF WDM76-11-11 PG 2A BETWEEN S37 L ENG FIRE SWITCH A ND P36. DIODE IS LOCATED IN FWD E&E UNDER P8 CONTROL STAND, RIGHT SIDE, MOUNTED JUST BELOW FLOOR LEVEL ABOVE DOOR. 09- 14-07 SUSPECT DAMAGED AISLE STANDBY LIGHTING RELAY. REPLACED DIODE BLOCK AT TB59 POS 12. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080600039 20070806 00039 NM 2007 8 6 2007UALA02798 1 20070722 A 5100 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE UNKNOWN A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 552UA 26641 FLIGHT DIVERTED DUE TO GEAR DOOR EICAS MESSAGE AND IRREGULAR FUEL BURN. INCREASE IN LOUD RUMBLE FROM MID CABIN AREA. SEVERAL MESSAGES ON GEAR DOOR WARNING. RH MAIN LANDING GEAR DOOR HANGS DURING GEAR SWING. SUSPECT SEQUNCE VALVE UPLOC K SEQUENCE VALVE MALFUNCTIONING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080600040 20070806 00040 SO 2007 8 6 C2XA07CL063 1 20070723 A 3350 74441 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12957 145080 MSP FLIGHT 3155 - THE CREW REPORTED THE EMERGENCY EXIT SIGN AT SEATS 3B AND 12A WERE INOPERATIVE. THE CREW PERFORMED A SYSYTEM RESET AND OPERATIONAL CHECKS WERE GOOD. UPON ARRIVAL IN CLEVELAND THE EXIT SIGN WAS INOPERATIVE. MAINTENANCE I NSPECTED AND REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007080600048 20070806 00048 NM 2007 8 6 CALA0700369 1 20070721 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 328-360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND FORWARD ENTRY RIGHT I/B SEAT TRACK CORRODED BETWEEN STA 328 AND 360, RBL 20. A REPAIR WAS INSTALLED IA W SRM 53-00-52. 2 L 7 2 4F RT A16WE 2007080600057 20070806 00057 NM 2007 8 6 HNAA0700139 1 20070707 A 5313 85300291101 STRINGER DHAV DHC8 DHC8102 2809003 NM BS 291 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 839EX 226 LIGHT CORROSION AT STR 29 AND STA X291.400 JOINING AREA. 2 H 7 2 4T RT A13NM 2007080600061 20070806 00061 NM 2007 8 6 ASAA0741877 1 20070719 A 5322 6948204505 SHEAR TIE BOEING 737 7374Q8 138447Q NM BS 360 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 BODY FRAME TO SKIN ATTACHMENT SHEAR TIE CRACKED. SHEAR TIE REPLACED WITH MADE REPAIR PART IAW SRM 51-40-05. 2 L 7 2 4F RT A16WE 2007080600062 20070806 00062 NM 2007 8 6 ASAA0741878 1 20070719 A 5330 6545775102 SKIN BOEING 737 7374Q8 138447Q NM BS 767-787 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 THREE INCH GOUGE AT FUSELAGE SKIN. REPAIRED GOUGE IAW SRM 53-00-01 FIG 201 REPAIR 31. 2 L 7 2 4F RT A16WE 2007080600106 20070806 00106 WP 2007 8 6 ASAA0781886 1 20070724 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 RADIO ALTIMETER ANTENNA CUTOUT FLANGE ON FUSELAGE IS CORRODED. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 53 -04, 51-30-02 AND 51-30-05. 2 L 7 2 4F RT A6WE 2007080600107 20070806 00107 WP 2007 8 6 ASAA0781888 1 20070725 A 5330 5920323249 SKIN DOUG DC9 DC983 3022083 WP BS 229-240 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 FUSELAGE SKIN DENTED. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR DOUBLER PER SRM 53-04. 2 L 7 2 4F RT A6WE 2007080600108 20070806 00108 WP 2007 8 6 ASAA0781889 1 20070725 A 5330 5920323249 SKIN DOUG DC9 DC983 3022083 WP BS 478-528 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 FUSELAGE SKIN DENTED. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR DOUBLER PER SRM 53-04. 2 L 7 2 4F RT A6WE 2007080600112 20070806 00112 WP 2007 8 6 ASAA0781881 1 20070724 A 5543 5955545503 TAB DOUG DC9 DC983 3022083 WP RUDDER CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 RUDDER TAB COATING (FLAME SPRAY) IS CRACKED. BONDED ASTROSTRIKE AL28 AND GLASS CLOTH TO RUDDER PER SRM 51-70. 2 L 7 2 4F RT A6WE 2007080600118 20070806 00118 NM 2007 8 6 ZZDA2007213 1 20070605 A 5313 LONGERON BOEING 717 717200 1383700 NM BS 898.5-1053 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT LONGERON 23L BETWEEN BS 898.5 AND BS 1053. INSTALLED LONGERON 23L AT AFT CARGO COMPA RTMENT BETWEEN STA 898.5 AND STA 1053 AS PER B717 SRM 51-41-02. 2 L 7 2 4F TR A6WE 2007080600143 20070806 00143 NM 2007 8 6 SWAA073669 1 20070725 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 747 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080600144 20070806 00144 NM 2007 8 6 SWAA073660 1 20070725 A 5340 65C27314 STRINGER CLIP BOEING 737 7373K2 13844BA NM BS 663 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080600153 20070806 00153 NM 2007 8 6 KCSA071259 1 20070726 A 5414 SKIN BOEING 747 7472B4B 138481B NM NR 3 NACELLE WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NR 3 PYLON O/B SIDE LOWER SKIRT WORN IN SEVERAL AREAS AT NAC STA-180 TO 236. 2 L 7 4 4F RT A20WE 2007080600159 20070806 00159 NM 2007 8 6 2007UALA02785 1 20070720 A 5754 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LE FLAP DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 RIGHT INBOARD FLAP AT MIDSPAN ON AFT FLAP TRAILING EDGE DELAMINATION OF 1-4 INCH BY 3 INCHES EXISTS. MAJOR REPAIR: REP LACED RIGHT HAND INBOARD AFT FLAP PER MM 27-51-11. 2 L 7 2 4F 4 F RT A16WE E21EU 2007080600168 20070806 00168 NM 2007 8 6 HNAA0700153 1 20070716 A 7500 310848501 VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE AIR SWITCH STICKING A HNAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 07 980HA 376 120911 UPON DESCENT INTO HHH POWER LEVERS AT FLY IDLE FLT DECK/CABIN STARTED TO FILL WITH SMOKE WITH ENGINE BLEEDS ON. TURNED OFF BLEEDS AND SMOKE STARTED TO DISSIPATE. CONTACTED CONTRACT MX AT 1055 WILL HEAD TO A/C ETA 10 MIN. GOING TO LOOK AT OIL LEVELS AND RUN A/C WITH CREW TO EVAL PROBLEM. OIL LEVELS RIGHT JUST ABOVE 1 QT LEFT 1/3 BELOW MAX LINE, GOING TO R UN A/C. RAN A/C WITH AND WITHOUT BLEEDS, WITH NR 2 ENGINE BLEEDS OFF NO OILY SMELL. GOING TO FERRY TO ROA TO GET SPARE A/C 826. CHECKED BOTH ENGING OIL LEVELS RIGHT 3/4 QT AND LEFT AT 1/3 QT BELOW MAX LINE. RAN A/C WITH CREW CONFIRMED O ILY SMOKE IN BLEED SYSTEM WITH ENGINE BLEEDS ON WITH NR 2 ENGINE BLEED OFF, NO OILY SMELL (MECH SHORT SINGED). REPLACED 2 H 7 2 4T 4 T RT A13NM E20NE 2007080600170 20070806 00170 EA 2007 8 6 TRAX200701042 1 20070723 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 838AS 7276 FLAP ASYMMETRY IN FLIGHT LT AT ZERO AND RT AT 8-9. AFTER AIR RETURN RT INDICATION SHOWS 11 DEGREES BUT THE FLAPS PHYSIC ALLY SHOW AT ZERO. A/C RETURNED TO PIA AFTER T/O. EMERGENCY DECLARED. FLT 4678 DEL 495 MINS. 2 L 7 2 4F RT A21EA 2007080600171 20070806 00171 EA 2007 8 6 TRAX200701045 1 20070724 A 5533 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 833AS 7246 ATTACH ANGLE FOR RB 2 ON AFT SIDE OF MID SPAR IS CRACKED UNDER ACCESS PANEL 325AL ON VERTICAL STABILIZER. [08-07-07] PERFORMED FPI OF ATTACH ANGLE FOR R/B NR 2 ON AFT SIDE. NO DEFECTS NOTED PER CRJ 200 NDTM 51-20-08. 2 L 7 2 4F RT A21EA 2007080600184 20070806 00184 EA 2007 8 6 TRAX200701065 1 20070726 A 5313 STRINGER CNDAIR CL600 CL6002B19 1900309 EA BS 349-333 S26R CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 873AS 7549 STR 26R IS CORRODED BETWEEN FS 349 AND FS 333. [08-06-07] APPLIED FILLED SEAL AROUND STRINGER SPLICE IAW SRM 51-21-1 1. 2 L 7 2 4F RT A21EA 2007080600188 20070806 00188 SO 2007 8 6 RAIA00707039 1 20070723 A 5210 DOOR EMB 145 EMB145ER 3260211 SO MAIN PAX LACK OF LUBE A RAIA K NONE W INADEQUATE Q C TX TAXI/GRND HDL 1 CE 03 808HK 145157 FLT 3521 - PIT - PASSENGER DOOR WOULD NOT OPEN FROM INSIDE THE CABIN. MAINTENANCE LUBRICATED THE DOOR AND OPS CHECKED I T GOOD. 2 L 7 2 4F RT T00011AT 2007080600190 20070806 00190 SO 2007 8 6 RAIA00707042 1 20070726 A 3397 WIRE EMB 145 EMB145 3260210 SO EMERGENCY LIGHT BROKEN A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 801HK 145053 PRE FLT 3504 - STL - GALLERY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE SUBJECT L IGHT. 2 L 7 2 4F RT T00011AT 2007080600198 20070806 00198 NM 2007 8 6 SWAA073700 1 20070726 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080600216 20070806 00216 EA 2007 8 6 COMA0760497 1 20070723 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 721CA 7259 FLIGHT 5120 - FLAPS FAIL AT 30 DEGREES ON APPROACH, AIRCRAFT LANDED SAFELY. COMPLIED WITH AD 2006-12-21 FLAP CAUTION ME SSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C) FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTI ON MESSAGES. 2 L 7 2 4F RT A21EA 2007080700004 20070807 00004 NE 2007 8 7 2007UALA02824 2 20070724 A 7200 ENGINE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 1 SEIZED A UALA D RETURN TO BLOCK R Y J PARTIAL RPM/PWR LOSS ENGINE STOPPAGE WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 925UA 26646 721710 NR 1 ENGINE N1 SEIZED AND METAL IN TAIL PIPE. N1 SEIZED DUE TO SCATTERED BROKEN STAGE 1 LPT BLADES. FOLLOWING SEIZURE, STAGE 2 NGV'S AND REMAINDER OF BLADES IN STAGE 1 BURNED/MELTED. NO KNOWN CAUSE FOR INITIAL BROKEN 1ST STAGE BLADES. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080700006 20070807 00006 NM 2007 8 7 2007UALA02827 1 20070725 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE BS 420 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 914UA 25381 FRAME DAMAGE AT STA 420, ACROSS STRINGER BAYS 28L-28R, AND 27R-28R. [08-21-07] MAJOR REPAIR: REMOVED DAMAGE. REPAIR A CCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080700012 20070807 00012 NM 2007 8 7 2007UALA02833 1 20070725 A 3150 WARNING MESSAGE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ILLUMINATED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 122UA 29168 'BAT CHARGER APU' EICAS STATUS MSG DISPLAYED. [08-21-07] REPLACED APU BATTERY . CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080700015 20070807 00015 EU 2007 8 7 2007UALA02836 1 20070725 A 3150 MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE OXYGEN SYS MISINSTALLED A UALA K NONE W J INADEQUATE Q C WARNING INDICATION IN INSP/MAINT 1 WP 29 420UA 489 REGUL LO PR DISPLAYED ON DOOR-OXY SYSTEM ECAM PAGE, DOOR-OXY. IMPROPER STOWAGE OF MASK. RESTOWED FIRST OFFICER'S M ASK AND RESERVICED CREW O2 SYSTEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080700023 20070807 00023 NM 2007 8 7 2007UALA02844 1 20070726 A 3397 794640 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 WALL EEL INOP: MID GALLEY LT WALL. REPAIRED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080700024 20070807 00024 NM 2007 8 7 2007UALA02845 1 20070726 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EEL INOP:ROW 42 LT, REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080700032 20070807 00032 NM 2007 8 7 DHL2007784521 1 20070707 A 5410 NOSE COWL BOEING 727 727227 1384078 NM NR 3 NACELLE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 NR 3 ENGINE NOSE COWL INTERNAL TAI DUCT SUPPORT BRACKET BROKEN AT APPROX 8 O`CLOCK POSITION, NAC STA 77.5, NAC LBL 28, N AC WL 180. CUT ACCESS HOLE IN NOSE COWL AT 9 O`CLOCK POSITION TO FOM 6 IN DIA IAW B727 SRM 54-30-3, FIG 3. REMOVED BRO KEN SUPPORT BRACKET IAW B727 SRM 51-30-2. FABRICATED NEW SUPPORT BRACKET FROM 2024T3, .040”, 3.0625 BY 4 IAW B727 SRM 5 4-10-2, FIG 1. FABRICATED DOUBLER FROM 2024T3, .040”, 7.75 DIA IAW B727 SRM 54-30-3, FIG 3. FABRICATED FILLER FROM 202 4T3, .032, 6 DIA IAW B727 SRM 54-30-3, FIG 3. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW B727 SRM 51-10-2. 2 L 7 3 4F A3WE 2007080700036 20070807 00036 NM 2007 8 7 DHL2007784525 1 20070710 A 5330 SKIN BOEING 727 727227 1384078 NM ZONE 100 BURNED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 DENT ON LOWER FUSELAGE SKIN BS 630 STR 27L. CUT OUT DAMAGED AREA DIM 1.5 BY 1.5 IAW B727 SRM 53-30-3, FIG 3. FABRICATE D DOUBLER FROM 2024T3, .063, DIM. 10 BY 8 IAW B727 SRM 53-30-3, FIG 3. TREATED, PRIMED AND INSTALLED REPAIR IAW B727 SR M 51-10-2 AND 53-30-3, FIG 3. 2 L 7 3 4F A3WE 2007080700043 20070807 00043 NM 2007 8 7 UPS07450250 1 20070706 A 5311 FRAME BOEING 747 747212B 1384886 NM BS 2231 S24-25L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D LT BS2231 FRAME INNER CHORD S24L-25L FOUND 1 HOLE CRACK AT FRAME STRAP RUNNING FWD APPROX 1/8". M /D BS2231 FRAME ATTACH INNER CHORD AND STRAP REPAIRED BTN STR22L TO 26L AREA AS PER SRM 53-10-04 FIG 115. CONTINUE INSP ECTION ARE REQ AS PER SRM 53-10-04 FIG 115. REFER NRC51556 FOR WORKING DETAIL. (UPS MPI#P19306 RAISED FOR CONTINUE INSP ECTION) 2 L 7 4 4F A20WE 2007080700052 20070807 00052 NM 2007 8 7 UPS07450259 1 20070705 A 5310 65B3848821 CREASE BEAM BOEING 747 747212B 1384886 NM BS 960-980 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C LT FX CROWN BS 960-980 UPPER CREASE BEAM FWD FRAME ATTACH ANGLE RADIUS FOUND CRACK APPROX 1/2" LONG. FX CROWN BS960-980 LT UPPER CREASE BEAM FWD FRAME ATTACH ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30 -02. 2 L 7 4 4F A20WE 2007080700067 20070807 00067 NM 2007 8 7 UPS07450274 1 20070705 A 5310 65B04913330 CREASE BEAM BOEING 747 747212B 1384886 NM BS 980-1000 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C RT FX CROWN BS980-1000 UPPER CREASE BEAM FWD RADIUS FOUND CRACK APPROX 1" LONG. FX CROWN BS 980-1000 RT UPPER CREASE BEAM REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007080700073 20070807 00073 NM 2007 8 7 UPS07450280 1 20070706 A 5330 BEAR STRAP BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C NR 3R MED CUTOUT AFT UPPER CORNER FOUND SKIN AND BEARSTRAP EDGE CRACKED, CRACK LENGTH 1/8" TO 2". NR 3R MED CUTOUT AFT UPPER CORNER SKIN AND BEARSTRAP REPAIRED AS PER UPS EO B747-5330-24674 APPENDIX P & L. 2 L 7 4 4F A20WE 2007080700078 20070807 00078 NM 2007 8 7 UPS07450289 1 20070708 A 5310 DOOR FRAME BOEING 747 747212B 1384886 NM BS 2231 S23-26L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D AFTER FURTHER FASTENER REMOVED INNER CHORD AREA S23L - 26L FOUND TOTAL HOLES CRACK AT DIFFERENT ST ACK UP STRUCTURES (FRAME,STRAP, INNER CHORD OR REVEAL) (CRACK LENGTH 0.050" & THROUGH THICKNESS) M/D BS2231 FRAME AT TACH REVEAL REPAIRED AT BETWEEN STR 21.5L TO STR 25L AREA AS PER SRM 53-10-04 FIG 34. FRAME ATTACH INNER CHORD & STRAP R EPAIRED BETWEEN STR 22L TO STR 26L AREA AS PER SRM 53-10-04 FIG 115. CONTINUE INSP. AREA REQUIRED AS PER SRM 53-10-04 FI G 115. 2 L 7 4 4F A20WE 2007080700082 20070807 00082 NM 2007 8 7 DHL2007741518 1 20070726 A 5347 BAC1520792 SEAT TRACK BOEING 727 7272Q9 138448M NM BS 480-720 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 MAIN CABIN RT SEAT TRACKS, RBL 25.0, CORRODED BETWEEN BS 480 AND BS 690. CORROSION ON SEAT TRACK BEYOND LIMITS PER B727 SRM 53-10-1. REMOVED SEAT TRACK SECTION FROM BS 480 TO BS 720, FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 EXT RUSION, 210" LONG, PO NR 9003467; REPAIR STRAP FROM 7075-T6, .250" BY 7" BY 2", PO NR 9003467; 2 EA REPAIR ANGLES FROM BAC1503-100122 EXTRUSION, 17" LONG, PO NR 9005461; TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND SEAT TRACK SECTION P ER B727 SRM 53-10-5 FIG 1, 53-10-2 FIG 7, AND 51-10-2. 2 L 7 3 4F RT A3WE 2007080700104 20070807 00104 NM 2007 8 7 HALA0700308 1 20070728 A 2612 473465 CONTROL UNIT BOEING 717 717200 1383700 NM FIRE DETECTION MALFUNCTIONED A HALA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 WP 13 476HA 55118 AFTER LANDING APU FIRE WARNING DISPLAYED (APU DO NOT USE). REPLACED APU CONTROL UNIT PER AMM 26-12-01. TEST OKAY. 2 L 7 2 4F TR A6WE 2007080700108 20070807 00108 2007 8 7 QXEA200701216 4 20070727 A 3160 C12432AA05 TRANSDUCER BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 403QX 14843 14843 4037 SEA FLIGHT NR 2397: OP FAIL STATUS MESSAGE. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED NR 1 IOP. OPS CHECK GOOD IAW MTC 6314101. AIRCRAFT UPGRADED TO CAT III. COCKPIT PLACARD REFLECTS SAME AND MTX CONTROL WAS NOTIFIED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007080700123 20070807 00123 NM 2007 8 7 AWXA200700911 1 20070705 A 5320 65558854 CUSP WEB BOEING 737 7373G7 1384595 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5962163, CORROSION ON CUSP SHEAR WEB, BS 767 - BS 787, S17R. REPLACED CUSP SHEAR W EB, BS 767 - BS 787, S17R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007080700127 20070807 00127 NM 2007 8 7 AWXA200700915 1 20070704 A 5311 65465491 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5981840, CRACKED FRAME, BS 767, S9L. REPAIRED FRAME, BS 767, S9L IAW USAIRWAYS EA 120121. 2 L 7 2 4F RT A16WE 2007080700145 20070807 00145 NE 2007 8 7 HEEA116395 1 20070710 A 2910 SS48CT3A132000 HOSE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 2 HYD SYSTEM RUPTURED B HEEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 03 5435V 760158 AFTER TAKEOFF, LANDING GEAR FAILED TO RETRACT, RED WARNING UNSAFE GEAR LIGHT ILLUMINATED PFN COMMENCED CHECKLIST AND TRO UBLESHOOTING. APPROXIMATELY 2 MINUTES LATER, NR 2 HYD SYSTEM CAUTION LIGHT ILLUMINATED. NR 2 HYD PRESSURE GAUGE TO LO W RED LINE. PNF COMPLETED UNSAFE GEAR CHECKLIST AND BEGAN HYD SYSTEM MALFUNCTION CHECKLIST. ONCE NR 2 HYD SYSTEM WAS S ECURED, NR 2 HYD PRESSURE GAUGE INDICATED PRESSURE LEVEL IN LIMITS LOW END OF GREEN ARC AND LANDING GEAR COMPLETED CYCLE TO 3 DOWN AND LOCKED. AIRCRAFT DIVERTED, LANDING AND SHUTDOWN WERE UNEVENTFUL. POST FLIGHT INSPECTION REVEALED COMPL ETE LOSS OF NR 2 HYDRAULIC FLUID FROM FORWARD LANDING GEAR BOX AREA. MAINTENANCE REPLACED RUPTURED HOSE. 1 G 7 2 3U 3 U H1NE E1GL 2007080700148 20070807 00148 NM 2007 8 7 C36002 1 20070714 A 7830 65B928411 DUCT BOEING 747 7473B5 1384920 NM PWA JT9 JT9D7R4G2 52054 NE NR 3 ENGINE CRACKED A Q4TA E J F A ENGINE SHUTDOWN DUMP FUEL ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 01 301JD 24194 P715143 AFTER TAKEOFF, ENGINE NR 3 FIRE INDICATION AT 400 FEET. FOUND T/R PNEUMATIC FEED DUCT SEPARATED AT 3-WAY VLV MOUNTING F LANGE. HIGH STAGE AIR CAUSED MELTING OF ENG FIREWALL ELECTRICAL HARNESSES ON ENG. (THIS IS A GOOD MODEL, IN PROCESS OF UPDATING). 2 L 7 4 4F 4 F RT A20WE E3NE 2007080700149 20070807 00149 NM 2007 8 7 GTIA200700017 1 20070715 A 3350 77233700 POWER SUPPLY AIRBUS A321 A321231 3940032 NM IAE V2500 V2500A1 NE EMERGENCY LIGHTS NO TEST A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 584NK 1408 14WL EMERGENCY LIGHTING SYSTEM POWER SUPPLY UNIT FAILED TEST. REPLACED SAME. 2 L 7 2 4F 4 F RT A28NM E311NE 2007080700150 20070807 00150 NM 2007 8 7 DU4R2007147 1 20070701 A 5320 146N852257 SILL BOEING 757 757 UTILUSE NM PWA 2037 PW2037 NE BS 1380-1440 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 638DL 23761 S/O NR 291043, NR 22641 FOUND HEAVY CORROSION UNDER NUT PLATES IN AFT PIT AT (T) EXTRUSION JUST IB OF C2 DOOR SILL WEB FROM BS 1380 TO BS 1440 S-27R. REPAIRED BY REMOVING AND REPLACING CHORD PN 146N8522-57 AND ANGLE PN 146N8515-8 IAW SRM 53-00-53 AND 51-40-02. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080700152 20070807 00152 NM 2007 8 7 DU4R2007150 1 20070712 A 5311 FRAME BOEING 757 757 UTILUSE NM PWA 2037 PW2037 NE BS 1500 DENTED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 638DL 23761 S/O NR 291043, N/R 22832, FOUND DENT ON MAIN FRAME UPPER CAP (UNDER FLOOR SUPPORT Z CHANNEL) AT BS 1500 RBL 11 IN AFT P IT. REPAIRED BY CUTTING OUT DENTED AREA, HFEC CUT OUT IAW NTM 51-00-19 PT. 6, NO RELEVANT INDICATIONS. FABRICATED AND I NSTALLED CHANNEL REPAIR 8.5 X 2 X .5 FROM 7075-T6 .063 IAW SRM 53-00-57 FIG. 201, 51-20-01 AND 53-00-07. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080700178 20070807 00178 SW 2007 8 7 910207192007 1 20070719 A 2810 B281K2770051 FUEL TANK BOLKMS 117 BK117C2 5626002 SW TMECA ARRIEL ARRIEL1E 60034 NE LEAKING E QMLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 145SU 123 9102 HAD 3 OCCURRENCES OF FUEL ODOR IN CABIN. 5 MIN AFTER DEPARTURE, THERE WAS A STRONG FUEL ODOR IN CABIN. ODOR WOULD DISS IPATE AND THEN RETURN. UPON THE THIRD RECURRENCE, PILOT ELECTED TO MAKE PRECAUTIONARY LANDING. AIRCRAFT WAS INSPECTED FOR FUEL LEAKS AND NONE FOUND. FUEL ODOR HAD GONE. AIRCRAFT THEN FLOWN BACK TO BASE. ON RETURN FLIGHT, FUEL ODOR CAME AND WENT THREE TIMES. AIRCRAFT LANDED BACK AT BASE AND WAS TAKEN OUT OF SERVICE. MECHANIC FOUND SMALL LEAK AT EXPANSI ON TANK AND ORDERED NEW TANK. 1 G 7 2 3U 3 U H13EU E19EU 2007080700181 20070807 00181 SO 2007 8 7 93A19072007 1 20070719 A 3250 UNKNOWN GULSTM GIV GIVG400 3980204 SO RROYCE TAY TAY6118 EU NLG STEERING WARNING LIGHT E N93A O OTHER J WARNING INDICATION CL CLIMB 1 SO 13 413QS 1521 AFTER TAKEOFF, NOSE WHEEL STEERING FAIL MESSAGE ILLUMINATED. OPEN 2 L 7 2 4F 4 F RT A12EA E25NE 2007080700184 20070807 00184 2007 8 7 AMTA200700335 4 20070710 A 2210 PITCH CONTROL LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE OUT OF RIG A AMTA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 GL 11 164AT 1238 EITHER AUTOPILOT WHEN ENGAGED AC INITALLY PITCHED THEN TRIMS NOSE DOWN UNTIL REACHING A/P LIMIT AND BEGINS UNDEMANDED DE SCENT. RIGGED MECH PITCH FEEL/ TRIM ASSY IAW MM 27-41-17. (INPUT AND SERIES TRIM PUSH RODS WERE OFF) CKD RIG OF A/P ST AB SERVO IAW MM 22-11-05. PERFORMED TRIM AUG TEST IAW MM 22-18-00. ALL CHECKS GOOD. (K) 2 L 7 3 4F 4 F A23WE E12EU 2007080800006 20070808 00006 NM 2007 8 8 AMTA200700344 1 20070614 A 5330 SKIN BOEING 737 737322 1384676 NM BS 453 S26R DENTED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 403TZ 24664 DENT ON EXTERIOR FUSELAGE SKIN AT FS 453 ABOVE STR 26R. REPAIR IAW ER/A 733-53R-6125. (K) 2 L 7 2 4F RT A16WE 2007080800013 20070808 00013 2007 8 8 WNH2007F00001 4 20070522 A 3416 2871101 ALTIMETER BEECH 90 C90A 1152911 CE PWA PT6 PT6* 52043 EA COCKPIT FAILED E WNHA K NONE O OTHER IN INSP/MAINT 1 WP 25 73PG LJ1607 ENCODING ALTIMETER DISPLAY FADES IN AND OUT TO THE POINT THAT THE INFORMATION DISPLAYED IS ILLEGIBLE TO THE PILOT. (K) 1 L 7 2 3T 3 T RT 3A20 E2NE 2007080800042 20070808 00042 NE 2007 8 8 DXTA200702348 2 20070718 A 7420 IGNITION LEAD CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE ENGINE MISINSTALLED E DXTA C ABORTED TAKEOFF W R J INADEQUATE Q C PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 07 336QS 5600336 NR1 ENGINE (LT) WOULD NOT MAKE TAKEOFF POWER. AIRPORT, 318 FT ELEV,TEMP 18C, TARGET T/O PWR 97.8 PERCENT. COULD ONLY GET 87.2 PERCENT AT 580 ITT. POWER LEVEL FULL FORWARD. TROUBLESHOT TO THE IB IGNITER LEAD POSITIONED INCORRECTLY AND OB STRUCTING THE THROTTLE LINKAGE. REPOSITIONED IGNITER LEAD. OPERATIONAL CHECK GOOD FOR POD. ALL WORK IAW CH 71-01-03 OF THE MM. 2 L 7 2 4F 4 F RT A22CE E25EA 2007080800053 20070808 00053 NE 2007 8 8 ZES2007F00001 2 20070427 A 7322 324470813 FUEL CONTROL BELL 222 222B 1182124 SW PWA PT6 PT6A42 52043 NE RT ENGINE MALFUNCTIONED E ZESA O OTHER O OTHER AP APPROACH 1 EA 03 8WU 40 47145 ON APPROACH, THE RT ENG LOST POWER AND WAS UNRESPONSIVE TO THROTTLE MOVEMENT. FUEL CONTROL WAS REPLACED AND AIRCRAFT RE TURNED TO SERVICE. (K) 1 G 7 2 3U 4 T H9SW E4EA 2007080800075 20070808 00075 CE 2007 8 8 AMWA06032N 1 20070725 A 5311 1294400671 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 438 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080800078 20070808 00078 CE 2007 8 8 AMWA06032Q 1 20070725 A 5311 1294300391 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 273 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080800090 20070808 00090 CE 2007 8 8 AMWA06032C 1 20070725 A 5311 1294300311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 213 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080900021 20070809 00021 NM 2007 8 9 AMTA200700364 1 20070725 A 3350 CHARGER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHTS INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 519AT 27975 EGGRESS LIGHTING INOPERATIVE (C) ZONE RT SIDE. REMOVED AND REPLACED AFT GALLEY BATTERY PACK CHARGER IAW MM 33-57-07, OP S CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007080900024 20070809 00024 CE 2007 8 9 GUUA07260701 1 20070726 A 3260 1013645789 PCB BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG SHORTED A GUUA O OTHER N FALSE WARNING AP APPROACH 1 SO 29 81536 UE152 FLIGHT: 9162 FLL/FPO DURING APPROACH NO GREEN LANDING GEAR INDICATION WHEN GEAR HANDLE DOWN. RETURNED, LANDED WITHOUT IN CIDENT. REPLACED ANNUNCIATOR PCB A125 LANDING GEAR OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080900047 20070809 00047 EA 2007 8 9 COMA0760501 1 20070727 A 2750 860D10018ABC CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 955CA 19382 7229 FLIGHT 5135 - FLAP FAIL MESSAGE RECEIVED ON DESCENT. DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. REPLACED FECU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007080900062 20070809 00062 2007 8 9 SWAA073732 4 20070729 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 409WN 27896 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007080900070 20070809 00070 NM 2007 8 9 SWAA073724 1 20070727 A 5330 6545800 SKIN BOEING 737 7375H4 138449D NM BS 295 S14R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 295, STR 14R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007080900078 20070809 00078 NM 2007 8 9 SWAA073760 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 420 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900079 20070809 00079 NM 2007 8 9 SWAA073762 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 500C S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900089 20070809 00089 NM 2007 8 9 SWAA073752 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 827 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900092 20070809 00092 NM 2007 8 9 SWAA073750 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727C S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900100 20070809 00100 NM 2007 8 9 SWAA073745 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500D S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900105 20070809 00105 2007 8 9 SWAA073767 4 20070730 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 718SW 27852 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007080900114 20070809 00114 NM 2007 8 9 SWAA073776 1 20070731 A 5311 6546526 FRAME BOEING 737 7373K2 13844BA NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080900115 20070809 00115 NM 2007 8 9 SWAA073831 1 20070731 A 5311 6546526 FRAME BOEING 737 7373K2 13844BA NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080900124 20070809 00124 NE 2007 8 9 DL76G070967 2 20070728 A 7200 CF680C2B6 ENGINE BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6 30025 NE NR 2 HOT START A DALA O OTHER M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 155DL 36299 19677 690372 25269 690372 PENDING HOT START IN STR. PRECAUTIONARY BORO SHOWED DAMAGE TO 10 BLADES OF HPC. CHANGED NR 2 ENGINE PER ROUTINE TRANSM ITTAL 1T161. 2 L 7 2 4F 4 F RT A1NM E13NE 2007080900131 20070809 00131 NM 2007 8 9 2007UALA02854 1 20070726 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GALLEY DOORWAY DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 FWD GALLEY DOOR SN1223 LWR AFT FRAME CORNER HAS 3 ELONGATED HOLES AND ONE HOLE CRACKED. REPLACED DAMAGED FRAME SECTION. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080900137 20070809 00137 NM 2007 8 9 2007UALA02860 1 20070726 A 4900 APU BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE ODOR A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 211UA 30217 STRONG ELECTRICAL ODOR IN COCKPIT. [80-21-07] ACCOMPLISHED FIM 21-00 TASK 808 AND FOUND THE APU TO BE THE SOURCE OF THE ODOR IN THE FLT DECK AND CABIN. ACCOMPLISHED PACK BURN USING ENG BLEED TO OPERATE PACKS, OPS NORMAL NO DEFECTS NOTE D. REPLACED BOTH OZONE CONVERTERS DUE TO APU OIL SMOKE CONTAMINATION. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007080900138 20070809 00138 NM 2007 8 9 2007UALA02861 1 20070727 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 CEILING EMERGENCY LIGHTS INOP AT 9R AND ROW 14. [08-21-07] REPLACED CEILING LIGHTS IN BOTH POSITIONS. LIGHTS CHECKE D READY FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080900143 20070809 00143 NM 2007 8 9 2007UALA02867 1 20070727 A 5320 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 AFT CARGO DOOR SN2573 STOP FTG WEB ANGLE AT LWR AFT CORNER HAS 4 EACH WORKING FASTENERS, CRACK FOUND BETWEEN 1ST AND 2ND LOCK FASTENER. [08-21-07] MAJOR REPAIR: MAJOR REPAIR ACCOMPLISHED. REPLACED CRACKED CHORD PER SRM 51-40-02 ON AAR E R NR1242 9-8300-0010. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080900151 20070809 00151 NM 2007 8 9 2007UALA02875 1 20070728 A 5240 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 R-2 DOOR IS DAMAGED AT UPPER HINGE CUTOUT. FABRICATED AND INSTALLED A FORMED ANGLE DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080900155 20070809 00155 NM 2007 8 9 2007UALA02879 1 20070728 A 3510 MASK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COPILOT'S O2 FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 CREW OXYGEN MASK PROBLEM, POSITION 2. (1=CAPT,2=FO, 3=1ST OBS, 4=2ND OBS). CREW COMMENTS: COPILOTS O2 MASK HAS LEAK IN HEAD BAND AND DOES NOT FULLY EXPAND. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080900157 20070809 00157 2007 8 9 2007UALA02881 4 20070730 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R1 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 408UA 457 R FWD CABIN DISPLAYED ON UPPER ECAM SCREEN. DOOR CREW COMMENTS: DOES NOT LOCK PROPERLY MECH INFORMS LOOSE OR MISSING. STRAPS COMING LOOSE FROM THE SLIDE AND INTERFERING WITH THE GIRT BAR. REPLACED R1 DOOR SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080900165 20070809 00165 2007 8 9 2007UALA02889 4 20070727 A 2565 7A1323113 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE UNWANTED DEPLOY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 182UA 25279 747 STRETCHED UPPER DECK SLIDE DEPLOYED INSIDE THE SHIPPING CONTAINER DURING TRANSPORT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080900167 20070809 00167 NM 2007 8 9 2007UALA02891 1 20070728 A 3350 58781362624 LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 941UA 26676 AFT CABIN EEL LIGHTS INOP FROM ROW 8 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT. RE PLACED CABLE AND 3 EEL LIGHT STRIPS. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080900173 20070809 00173 NM 2007 8 9 2007UALA02897 1 20070729 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY LIGHTS AT ROWS 5F FWD, 33 RT, 46 LT AND 61 RT ARE INOPERATIVE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080900191 20070809 00191 WP 2007 8 9 IXXA07SMN162S 1 20070630 A 5320 SILL DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT MAIN CARGO DOOR COVER SILL AT FS235 LONGERON 21 LT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, OR CORROSION FOUND. FABRICATED REPAIR PA RTS. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING AREAS. INSTALLED REPAIR PARTS IAW FORM FAA 8100-9 DATED 07-27-07, BOEING MESSAGE NUMBER 1-41443541-4 DATED 07-16-07, MESSAGE NUMBER 1-441363702-5 DATED 07 -27-07, SERVICE BULLETIN, DC8-53-079 REV 2, DRAWING DOUGLAS NR SR08530027, SEMAN DRAWING NUMBER ED 4569-2, ADJUST SEMAN FORM NUMBER 242-2, DC8 SRM 51-1-21, 51-1-20, AND DC8 NDT SPM PART NUMBER 6-10-01.001. 2 L 7 4 4F RT 4A25 2007080900194 20070809 00194 EU 2007 8 9 07FDEA02675 1 20070730 A 5730 FX2241702502 PANEL AIRBUS 310 A310203 3930313 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 PNL 486BR HAS FRETTING CORROSION AND BARE METAL EXPOSED REMOVED CORROSION FOUND TO OUT OF LIMITS IAW A310-200 SRM 54-55- 51. FABRICATED NEW PANEL IAW A310-200 SRM AND GMM. ALODINED AND PRIMED IAW A310-200 SRM 51-21-10 AND 51-23-10. 2 L 7 2 4F RT A35EU 2007080900195 20070809 00195 NM 2007 8 9 07FDEA02677 1 20070731 A 5730 ARC27361 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 LT WING, I/B FLAP LOWER SKIN (I/B HALF) FOUND WITH NUMEROUS DENTS. [08-15-07] REPAIRED AS PER SRM 57-10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007080900196 20070809 00196 NM 2007 8 9 07FDEA02678 1 20070731 A 5343 ACA7017501 FITTING DOUG MD11 MD11F 3023600 NM NLG WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 NOSE LANDING GEAR LT TRUNNION FITTING FOUND CRACKED. [08-20-07] REPAIRED AS PER SRM 53-40- 00 FIGURE 23 VOLUME I. R EPETITIVE INSPECTION REQUIRED FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS REQUIRED IN SRM 53-40-00 FIGU RE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007080900201 20070809 00201 EU 2007 8 9 07FDEA02683 1 20070731 A 5347 A53813106 SEAT TRACK AIRBUS 310 A310203 3930313 EU CABIN CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 ARTICULATING SEAT TRACK AT Y1456 BETWEEN FR 38.2 AND FR 40 IS CRACKED ON UPPER FLANGE FWD EDGE REMOVED AND REPLACED ARTI CULATING SEAT TRACK PER A310-200 SRM 51-40-44, 51-40-21, ALODINED AND PRIMED PER A310-200 SRM 51-21-10. 2 L 7 2 4F RT A35EU 2007081000001 20070810 00001 EU 2007 8 10 07FDEA02684 1 20070731 A 5311 A5397422220200 FRAME AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT PIT FRAME 66 T CAP ABOVE STRINGER 46L CORRODED REMOVED AND REPLACED T-CAP PER A310-200 SRM 53-17-15 FIG 11 SHEET2 , 51-72-10, ALODINED AND PRIMED PER A310-200 51-21-10, 51-23-10. 2 L 7 2 4F RT A35EU 2007081000002 20070810 00002 EU 2007 8 10 07FDEA02685 1 20070731 A 5753 2024T3 VANE AIRBUS 310 A310203 3930313 EU TE FLAPS CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 RT WING I/B FLAP VANE BULL NOSE CENTER DOUBLER CHAFED. 08-30-07 REMOVED DAMAGED DOUBLER, INSPECTED AREA , FABRICATED REPLACEMENT DOUBLER AND INSTALLED PER EA 6-5750-112956. FLAP VANE P/N A57970651201 2 L 7 2 4F RT A35EU 2007081000006 20070810 00006 EU 2007 8 10 07FDEA02689 1 20070731 A 5340 A5377364420100 FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 FRAME FITTING C35 IS CRACKED AT RBL 60 FWD PIT FLOOR LEVEL. REMOVED AND REPLACED FRAME FITTING PER A310-200 SRM 51-40-2 1 PARAGRAPH 6. 2 L 7 2 4F RT A35EU 2007081000007 20070810 00007 NM 2007 8 10 HALA0700312 1 20070728 A 3150 UNKNOWN BOEING 767 7673CB 1385187 NM EICAS COMPUTER UNKNOWN A HALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 588HA 33466 ETOPS SIGNIFICANT SYSTEM, MX LEVEL EICAS MSG 'EICAS BITE' DISPLAYED. MULTIPLE DATA FIELDS BLANK W/RIGHT EICAS COMPUTER SELECTED. ACCOMPLISHED EICAS BITE TEST NO FAULTS NOTED. CKS NML PER MM 31-41-02. 2 L 7 2 4F RT A1NM 2007081000008 20070810 00008 NM 2007 8 10 HALA0700313 1 20070730 A 2612 NONE BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE FIRE LOOP NONE A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM, FOUND 'LEFT ENG FIRE LOOP NR 1' EICAS MSG DURING OVERNIGHT CHECK. PERFORMED TEST, MSG CLEARED PER FIM 26-11-00 FIG-105. 2 L 7 2 4F 4 F RT A1NM E24NE 2007081000011 20070810 00011 EU 2007 8 10 AWXA200700929 1 20070729 A 5753 D57570086 SKIN AIRBUS 320 A320231 3930325 EU ZONE 600 DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 627AW 66 LAS -NR 4165277, RIGHT WING INBOARD FLAP TRAILING EDGE HAS A 10" AREA DEBONDED, WS 0 /RIB 1 TO WS 406 / RIB 8. TEMPORAR ILY REPAIRED RIGHT WING INBOARD FLAP TRAILING EDGE, WS 0 /RIB 1 TO WS 406/RIB 8 IAW A320 SRM 57-52-00 AND PLACED ON MONI TOR TO HAVE THE PERMANENT REPAIR ACCOMPLISHED WITHIN 3 MONTHS I/A/W A320 SRM 57-52-00. 2 L 7 2 4F RT A28NM 2007081000013 20070810 00013 NM 2007 8 10 AWXA200700934 1 20070704 A 5311 90526913 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5981847, CRACKED FRAME, BS 727E, S9R. REPAIRED FRAME, BS 727E, S9R IAW USAIRWAYS E A 120121. 2 L 7 2 4F RT A16WE 2007081000015 20070810 00015 NM 2007 8 10 AALA20071301 1 20070714 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 776AN 29582 JFK - EMERGENCY LIGHT AT ROW 33G IS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT ROW 33G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007081000017 20070810 00017 NM 2007 8 10 AALA20071308 1 20070715 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 668AA 25333 MIA - EMERGENCY LIGHT AT SEAT 35D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 35D. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A2NM 2007081000019 20070810 00019 NM 2007 8 10 AALA20071310 1 20070716 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 959AN 30828 MIA - EMERGENCY LIGHTS FROM SEAT ROW 15D TO 21D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT ROW 1 5D TO 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007081000020 20070810 00020 NM 2007 8 10 AALA20071311 1 20070716 A 3397 CONNECTOR BOEING 767 767223 1385123 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 327AA 22327 LAX - EMERGENCY FLOOR LIGHT AT MID GALLEY INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY FLOOR LIGHT AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007081000021 20070810 00021 NM 2007 8 10 AALA20071302 1 20070714 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 776AN 29582 JFK - EMERGENCY LIGHT AT ROW 37C IS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT ROW 37C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007081000022 20070810 00022 NM 2007 8 10 AALA20071299 1 20070713 A 3040 WINDSHIELD BOEING 777 777223 1385213 NM COCKPIT ARCED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 789AN 30252 BOS INFLIGHT T174/13JUL RDU TO LGW - FIRST OFFICERS WINDSHIELD CRACKED AND ARCING. HEAT TURNED OFF AND LANDED BOS WITHO UT INCIDENT. REPLACED FIRST OFFICERS WINDSHIELD IN ACCORDANCE WITH MAINTENANCE MANUAL 56 11 01 4. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007081000024 20070810 00024 NM 2007 8 10 AALA20071303 1 20070714 A 3350 BEZEL BOEING 767 767323 1385205 NM EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 363AA 24044 ORD EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. RESEATED LAMP HOLDER FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007081000027 20070810 00027 WP 2007 8 10 AALA20071300 1 20070714 A 3213 SCHRADER VALVE DOUG DC9 DC983 3022083 WP NOSE GEAR STRUT INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 596AA 53286 BOS INFLIGHT T631/14JUL - CREW REPORTED NOSE GEAR TAKEOFF WARNING. UNABLE TO RETRACT NOSE LANDING GEAR. RETURNED TO BO S AND LANDED WITHOUT INCIDENT. INSPECTED AND COMPLETED NOSE LANDING GEAR STRUT REPACK. REPLACED THE SCHRADER VALVE AND PACKING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007081000028 20070810 00028 EU 2007 8 10 AWXA200700928 1 20070728 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU COCKPIT ODOR A AWXA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 WP 28 654AW 1050 CREW REPORTED AVIONICS SMOKE MASTER WARNING AT 10,000 CLIMBING OUT OF PHILADELPHIA. AN ELECTRICAL BURNING ODOR WAS NOTI CED IN COCKPIT WITH NO VISIBLE SIGNS OF SMOKE. CREW DECLARED AN EMERGENCY, THE CABIN WAS PREPPED AND EMERGENCY EQUIPMEN T WAS DISPATCHED. THE LANDING WAS UNEVENTFUL. MX RAN ENGINES AND ALL AVIONICS TO TRY TO DUPLICATE BURNING ODOR. NO SM OKE NOTED AND NO ECAM WARNING FAULTS. NO FAULTS NOTED. THE A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2007081000031 20070810 00031 EU 2007 8 10 AWXA200700933 1 20070728 A 2930 520913 GENERATOR AIRBUS 320 A320232 3930326 EU LT WHEEL WELL FAILED A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 651AW 33755 33744 866 CREW REPORTED THE BLUE HYDRAULIC SYSTEM FAILED DURING CLIMB-OUT OF PHX. THE CREW DECLARED AN EMERGENCY AND RETURNED TO PHX. THE LANDING WAS UNEVENTFUL. MX REPLACED THE CONSTANT SPEED MOTOR/GENERATOR (8XE) IAW AMM 24-24-51-400-001. OPERATI ONAL CHECK WAS GOOD. THE A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2007081000033 20070810 00033 CE 2007 8 10 DXTA200702360 1 20070729 A 3240 BRAKE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LT MLG INOPERATIVE E DXTA O OTHER O OTHER LD LANDING 1 GL 07 639QS 5605139 LT MAIN BRAKE SPONGY ON BOTH SIDES OF COCKPIT. BLED LEFT MAIN BRAKE. OPS AND LEAK CHECK GOOD. TAXIED ACFT TO RUN-UP ARE A AND BACK. NO DEFECTS NOTED. DONE IN REF. TO CE-560XL MM 32-42-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007081000034 20070810 00034 CE 2007 8 10 DXTA200702361 1 20070729 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LT MLG INOPERATIVE E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 394QS 5600394 WHILE TAXING CAPT LT BRAKE PEDAL BLEEDS DOWN SLIGHTLY, SOFT PEDAL. BLEED & SERVICED BRAKES. OPS + LEAK CHECKS GOOD. IAW CE560 MM. 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007081000035 20070810 00035 CE 2007 8 10 DXTA200702362 1 20070729 A 3230 LANDING GEAR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RIGHT MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 971QS 7500071 RT MAIN LANDING GEAR DID NOT SHOW GREEN DOWN AND LOCKED INDICATION WHEN GEAR WAS SELECTED DOWN. IAW CHECKLIST: GEAR DOW N BOTTLE HANDLE WAS PULLED AND MAIN MANUAL RELEASE HANDLE PULLED. [08-23-07] RESET N2 BOTTLE, RESET LANDING GEAR CONTR OL MANIFOLD, PURGED GEAR SYSTEM OF AIR CYCLED GEAR 20 TIMES WITH NO DEFECTS NOTED. OPERATIONAL CHECK GOOD PER 750 MM CH 32-00-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007081000036 20070810 00036 NM 2007 8 10 DXTA200702363 1 20070729 A 2780 SLAT SYSTEM GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE LE SLATS OUT OF RIG E DXTA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 07 752QS 152 SLATS WOULD NOT RETRACT ALL THE WAY THEY ARE STUCK IN THE MIDDLE . SEVERAL FAULTS ON THE FSEU. [08-23-07] COMPLIED WI TH RIGGING BOX FUNCTION CHECK AS OUTLINED IN GULFSTREAM G200 MM 27-50-05 & FOUND FLAP/SLAT SYSTEM TO FUNCTION NORMALLY O N GROUND AT THIS TIME. 2 L 7 2 4F 4 F RT A53NM E35NE 2007081000037 20070810 00037 CE 2007 8 10 DXTA200702364 1 20070729 A 3234 CONTROL HANDLE CESSNA 680 680CE 2076811 CE MLG MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 387QS 6800119 LANDING GEAR DID NOT EXTEND NORMALLY, USING CHECKLIST TO EXTEND GEAR (EMERGENCY EXTENSION) 3 GREEN LIGHTS ILLUMINATED R ED INTRANSIT LIGHT REMAINED ILLUMINATED. ON ROLLOUT, RUDDER PEDALS INEFFECTIVE FOR NOSE WHEEL STEERING. STEERING TILL OP ERATED NORMALLY. FOUND LANDING GEAR CONTROL HANDLE INOP. REMOVED & REPLACED LANDING GEAR CONTROL HANDLE. IAW CE680MM 32 -30-40 2 L 7 2 4F RC T00012WI 2007081000038 20070810 00038 NM 2007 8 10 TIPR360200706 1 20070731 A 5330 SKIN BOEING 767 767222 1385122 NM PWA JT9 JT9D* NE BS 1835 GOUGED B K NONE O OTHER IN INSP/MAINT 1 EA 03 609UA 21870 AFT FUSELAGE SKIN UNDER UPPER LT STAB FAIRING STA 1835 DEEP GOUGES. FABRICATED AND REPLACED REPAIR DOUBLER IAW SRM 53-8 0-01- REFERENCE SERVICE ORDER 599125 OPERATION 25071. 2 L 7 2 4F 4 F RT A1NM E20EA 2007080700089 20070807 00089 EA 2007 8 7 MASA200700308 1 20070607 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 908FJ 15008 ASH 2709 PHX - EMERGENCY EXIT CEILING LEVEL FLOOD LIGHT INOP AT ROW 20. RELAMPED EMERGENCY FLOOD LIGHT AT ROW 20/OPS CK GOOD. 2 L 7 2 4F RT A21EA 2007080700090 20070807 00090 EA 2007 8 7 MASA200700313 1 20070608 A 3350 1317 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 507MJ 10077 ASH 7292 ORD - EMERGENCY OVHD LIGHT INOP SEAT ROW 16. MX RELAMPED. 2 L 7 2 4F RT A21EA 2007080700094 20070807 00094 EA 2007 8 7 MASA200700318 1 20070610 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH 2875 LAS - FWD EMERGENCY CEILING LIGHT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2007080700099 20070807 00099 EA 2007 8 7 NASA2007329 1 20070614 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75984 7489 ASH 7131 ORD - CAPTAIN REPORTED NR 3 OVERHEAD CEILING EMERGENCY LIGHT INOP. EMERGENCY LIGHT WAS PLACED ON MEL, ACFT CON TINUED OPERATIONS. 2 L 7 2 4F RT A21EA 2007080700102 20070807 00102 EU 2007 8 7 F3LA200700187 1 20070728 A 5321 D5361060500000 FLOOR PANEL AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 803FR 5201 2017 DURING C-3 CHECK, INSPECTION REPORTED L1 DOOR THRESHOLD FLOOR PANEL 221FF CORRODED. REPLACED FLOOR PANEL 221FF IAW AIRB US AMM 53-12-12-400-001. 2 L 7 2 4F RT 2007080700103 20070807 00103 NM 2007 8 7 HALA0700307 1 20070728 A 7710 889313 PROBE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE N2 FAILED A HALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 476HA 55118 ATB - ENG L SYS FAIL CAME ON IN FLIGHT. FOUND N2 PROBE ELECTRICAL FAULT CH-B "771202" NR 1 ENGINE. REMOVED AND REPLACE D NR 1 ENGINE CH-B N2 PROBE PER AM77-12-01. OPS AND LEAK CHK OK. NO FAULT NOTED, MPN 889-3-113; S/N ON 7358; S/N OFF 3 072. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007080700109 20070807 00109 NM 2007 8 7 QXEA200701217 1 20070723 A 2750 FLAP SYSTEM BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 415QX 4081 YYC FLIGHT NR 2480: FLAP POWER CAUTION LIGHT ILLUMINATED DURING FLIGHT. FLAPS STUCK AT 10 DEGREES. CREW RAN CHECKLIST IN FLIGHT AND FLAP POWER LIGHT DID NOT EXTINGUISH. MAINTENANCE INTERROGATED CDS. NO CURRENT FAULTS. CLEARED NVM. C/W SL-DH8-400-SL-27-002A. CAUTION CLEARED. C/W OPS CHECK IAW AMM TASK 27-50-00-710-801. NO PARTS REPLACED. AIRCRAFT RE TURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007080700124 20070807 00124 NM 2007 8 7 AWXA200700912 1 20070705 A 5320 654797321 CUSP WEB BOEING 737 7373G7 1384595 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961275, CORROSION ON CUSP SHEAR WEB, BS 616 - BS 639, S17L. REPLACED CUSP SHEAR W EB, BS 616 - BS 639, S17L I/A/W B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007080700129 20070807 00129 NM 2007 8 7 AWXA200700917 1 20070705 A 5311 65465292 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961278, CRACKED FRAME, BS 440, S9L. REPAIRED FRAME, BS 440, S9L IAW USAIRWAYS EA 120121. 2 L 7 2 4F RT A16WE 2007080700138 20070807 00138 NM 2007 8 7 AWXA200700926 1 20070725 A 5754 WEDGE BOEING 757 757225 1384959 NM ZONE 600 SEPARATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 000008 22208 MCN - MAJOR REPAIR - C-12 - CHECK - RIGHT WING NR 6 SLAT TRAILING EDGE WEDGE SEPARATED, SS 133.15 - SS 134.15. REPAIRED RIGHT WING NR 6 SLAT TRAILING EDGE, SS 133.15 - SS 134.15 IAW B757-200 SRM 51-70-10-2R4. 2 L 7 2 4F RT A2NM 2007080700141 20070807 00141 NM 2007 8 7 DL76L070960 1 20070724 A 2420 IDG BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE RIGHT FAILED A DALA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION AP APPROACH 1 SO 27 195DN 12304 28452 P2559 JFK-NCE - ON WAY TO NCE RT IDG FAILED. STARTED APU AND CONTINUED. ON FILAL APPROACH APU GEN FAILED AND THEN APU AUTO S HUT DOWN. REMOVE/INSTALL RIGHT IDG PER AMM 24-11-01. REMOVE AND INSTALLED RIGHT GCU PER AMM 24-11-01. OPERTIONAL TEST PERFORM OK FOR RIGHT IDG PER AMM 24-11-00. APU RESET ON GROUND. OPS SATIS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080700146 20070807 00146 NE 2007 8 7 HEEA116396 1 20070712 A 2840 TRANSMITTER SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL FUEL FLOW FLUCTUATES E HEEA O OTHER J WARNING INDICATION CR CRUISE 1 SW 03 5435V 760158 IN CRUISE FLIGHT THE NR1 ENGINE FUEL FLOW STARTED TO FLUCTUATE BETWEEN 200 TO 300 LBS. T5 AND N2 REMAINED NORMAL. RETU RNED TO BOOTHVILLE. MAINTENANCE CLEANED THE CONNECTOR AT THE FUEL FLOW TRANSMITTER. 1 G 7 2 3U 3 U H1NE E1GL 2007080700154 20070807 00154 CE 2007 8 7 GUUA07140701 1 20070714 A 3200 UNKNOWN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67 52043 NE LANDING GEAR UNKNOWN A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 29 69549 UE194 DURING APPROACH LANDING GEAR WOULD NOT EXTEND WITH THE GEAR HANDLE DOWN, CYCLED LANDING GEAR AND THE RT GEAR EXTENDED PA RTIALLY THEN 10 SECONDS LATER ALL GEARS EXTENDED. INSPECTED LANDING GEAR SYSTEM NO DEFECTS NOTED. LANDING GEAR OPERATIO NAL TEST NORMAL. TEST FLIGHT SATISFACTORY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080700168 20070807 00168 EU 2007 8 7 HAEA200700201 1 20070719 A 5311 FRAME AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D2 30010 NE FUSELAGE CORRODED E HAEA K NONE O OTHER IN INSP/MAINT 1 SW 05 221TW 23613 221 DURING MCI INSPECTION FRAME 7 ON THE LT SIDE, DIRECTLY BEHIND AFT EDGE OF PILOTS SIDE WINDOW WAS FOUND TO BE CORRODED IN THE UPPER TUB. ENGINEERING EVALUATED THE CORROSION AND DETERMINED THAT REPAIR WAS NEEDED AND ISSUED AN ENGINEERING INST RUCTION FOR THE REPAIR. MAINTENANCE PERFORMED REPAIR IAW THE ISSUED ENGINEERING INSTRUCTION. NO FURTHER ACTION REQUIRED. (CLOSED) 2 L 7 2 4F 4 F A7EU E7EA 2007080800007 20070808 00007 NM 2007 8 8 AMTA200700342 1 20070715 A 2150 A/C PACK BOEING 737 73783N 13844HI NM RIGHT MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 305TZ 30706 RT BLEED TRIP OFF LIGHT ILLUMINATED RESET OPERATED NORMALLY WITH LT PACK PRESS 38 PSI AND RT PACK 18 PSI AFTER 1 MINUTE TRIPPED OFF AGAIN. PERFORMED RT ENG BLEED AIR CROSSOVER OPS TEST IAW MM 36-11-00. NO DEFECTS FOUND. (K) 2 L 7 2 4F RT A16WE 2007080800018 20070808 00018 CE 2007 8 8 DJFA2007072 1 20070716 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 731TA 6125 RK273 DURING A SCHEDULED MAINTENANCE VISIT, WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STAB ILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT IB ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF T HIS AREA ARE OUTLINED IN MFG COMMUNIQUÉ' NR 70. THE RIB WAS REPLACED WITH THE NEW UPGRADED RIB. 2 H 7 2 4F 4 F RT A16SW E25EA 2007080800043 20070808 00043 CE 2007 8 8 DXTA200702349 1 20070719 A 3244 TIRE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP NLG LOW PRESSURE E DXTA C ABORTED TAKEOFF W INADEQUATE Q C TO TAKEOFF 1 GL 07 870QS 258732 AIRPLANE TURNS TO THE LEFT WHEN TRYING TO TRACK STRAIGHT, ESPECIALLY DURING TAKEOFF ROLL REQUIRING ALMOST FULL RT RUDDER AT HIGHER SPEEDS. TROUBLESHOT SYSTEM AND FOUND NOSE WHEEL STEERING OPERATING NORMALLY IAW MM, CH. 32-50. FOUND NOSE WH EEL TIRE PRESSURES LOW (84 LT)(95 RT). SERVICED TIRES TO 110 PSI WITH NITROGEN IAW MM CH 12-30. 2 L 7 2 4F 4 F RT A3EU E6WE 2007080800054 20070808 00054 NE 2007 8 8 ZES2007F00002 2 20070615 A 7322 81850012 HYDROMECH UNIT CESSNA 500 550 2076604 CE PWA 530 PW530A NE LT ENGINE INOPERATIVE E ZESA O OTHER O OTHER NR NOT REPORTED 1 EA 03 824CB 5500824 PCEDA0048 LT ENGINE ON AIRCRAFT, WOULD NOT REDUCE POWER TO IDLE, GROUND RAN AIRCRAFT TO CONFIRM POWER WOULD NOT REDUCE BELOW 75 PE RCENT N2. REMOVED AND REPLACED HFO (HYDROMECHANICAL FUEL CONTROL). GROUND RUN AND PERFORMED FUNCTIONAL CHECK FLIGHT AN D RETURNED TO SERVICE. (K) 1 L 7 2 4F 4 F A22CE E00053EN 2007080800073 20070808 00073 CE 2007 8 8 AMWA06032K 1 20070725 A 5311 1294300311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 393 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080800083 20070808 00083 CE 2007 8 8 AMWA06032T 1 20070725 A 5311 12943003623 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 363 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080800102 20070808 00102 NE 2007 8 8 HEEA116619 1 20070728 A 3260 824037 PROXIMITY SWITCH SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL2S2 60036 NE NLG OUT OF ADJUST B HEEA O OTHER N FALSE WARNING CL CLIMB 1 SW 03 784P 760634 AFTER TAKEOFF, NOSE WHEEL CENTERING LIGHT STAYED ON. UNABLE TO RETRACT GEAR. RETURNED TO DEPARTURE. MAINTENANCE ADJUS TED GAP ON NOSE WHEEL POSITIONING ADVISORY SYSTEM. 1 G 7 2 3U 4 U NC H1NE E00054EN 2007080800106 20070808 00106 WP 2007 8 8 UPS07850337 1 20070725 A 5320 WEB DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE FS 70 L21L PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE: C2 WEB PUNCTURED AT STA 70 L21L. CUT OUT DAMAGED AREA ON WEB AT STA 70 L21L IAW SRM 53-02-00-0 FIG1F FABRICATED AND INSTALLED REPAIR DOUBLER AT STA 70 L21L IAW SRM 53-03 -03-0. 2 L 7 4 4F 4 F RT 4A25 E2GL 2007080800108 20070808 00108 NM 2007 8 8 ASMF200707018 1 20070728 A 2840 UNKNOWN BOEING 737 737* NM CFMINT CFM567 CFM567B22 13802 NE FUEL TANK UNKNOWN W ASMF O OTHER N FALSE WARNING CL CLIMB 1 SW 23 852AM 33787 AIRCRAFT RETURNED OF FLIGHT DUE TO LT TANK FUEL UNBALANCED LIGHT TURNED ON WITH INDICATION OF CENTRAL TANK 2360 KGS, LT TANK 3140 KGS AND RT TANK 3750 KGS. DURING MAINTENANCE CHECK AN UNBALANCE OF 700 KGS WAS DETECTED WITH INDICATIONS OF LT TANK 3000 KGS AND RT TANK 3700 KGS. THE FILL VALVE WAS CHECKED AND OVERWEIGHT INSPECTION WAS PERFORMED IAW MM 05-51-35, ALL CORRECT. DURING OVERNIGHT CHECK, THE FUEL CONSUMED WAS CHECKED, BEING CORRECT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007080900004 20070809 00004 WP 2007 8 9 UPS07850339 1 20070718 A 5730 SKIN DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE LWS 100 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 LH INBD UPPER SURFACE SKIN EXSISTING REPAIR DOUBLER HAS DEEP GOUGE AT STA 100 REMOVED DAMAGED DOU BLER AT L/WING STA 100 IAW SRM 51-01-21-0 FABRICATED AND INSTALLED REPAIR DOUBLER AT LH WING INBD UPPER SURFACE STA 100 IAW SRM 57-07-01-0 AND EO DC8-5720-7767-A 2 L 7 4 4F 4 F RT 4A25 E2GL 2007080900015 20070809 00015 NM 2007 8 9 AMTA200700354 1 20070718 A 3040 SENSOR BOEING 737 73783N 13844HI NM WINDSHIELD HEAT INOPERATIVE A AMTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 11 319TZ 30643 RT WINDSHIELD OVERHEAT LIGHT ILLUMINATED DURING CLIMBOUT. T/S SYS FOUND SENSOR INOPERATIVE, SWITCHED TO NR 2 SENSOR, AL L SYS OPS CHECKED NORMAL IAW MM 30-41-00-810-812. (K) 2 L 7 2 4F RT A16WE 2007080900018 20070809 00018 NM 2007 8 9 AMTA200700359 1 20070720 A 3610 1296942 THERMOSTAT BOEING 737 73783N 13844HI NM RT LEAKING A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 323TZ 30033 LT AND RT POINTERS NOT THE SAME (SPLIT), THE ENGINE IS THE BLEED SOURCE. LT 40 PSI RT 20 PSI. T/S IAW FIM 36-10-00-81 0-804 FOUND EXCESSIVE LEAKAGE OF 450 THERMOSTAT. REMOVED AND REPLACED 450 THERMOSTAT IAW AMM 36-11-05-4. OPS CHECK AND LEAK CHECK GOOD. (K) 2 L 7 2 4F RT A16WE 2007080900050 20070809 00050 EA 2007 8 9 VNAA0707005 1 20070710 A 5270 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SERVICE DOOR FAILED A VNAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 05 262PS 2966 7962 CREW REPORTED A SERVICE DOOR CAUTION MESSAGE AND THEN A MAIN CABIN DOOR WARNING MESSAGE IN CRUISE. DURING DESCENT CABIN ALT CAS MESSAGE CAME ON. PASSENGER O2 MASKS WERE DEPLOYED DURING CABIN ALT EPISODE. CREW FOLLOWED THE QRH AND DECLARE D AN EMERGENCY AND LANDED IN PHL WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND A FAULTY PROXY SENSOR ELECTRONIC UNI T. MAINTENANCE REMOVED AND REPLACED THE PSEU IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 32-61-01-000(400)-801. MAINTENANCE REPLACED DEPLETED O2 GENERATORS AND REPACKED O2 MASKS. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT RELEAS ED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007080900051 20070809 00051 EA 2007 8 9 VNAA0707008 1 20070717 A 5200 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE GROUND SERVICE OPEN A VNAA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 GL 05 245PS 7919 CREW REPORTED AFTER TAKEOFF A GROUND SERVICE WAS LEFT OPEN. CREW RETURNED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENA NCE INSPECTED AND RESECURED DOOR CLOSED. MAINTENANCE FOUND NO DEFECTS IN ACCORDANCE WITH THE SMP. AIRCRAFT WAS RELEASE D FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007080900053 20070809 00053 NM 2007 8 9 SWAA073730 1 20070729 A 3350 101073 LENS BOEING 737 7373G7 1384595 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 FWD CABIN EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007080900056 20070809 00056 NM 2007 8 9 SWAA073727 1 20070727 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 236WN 34631 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007080900059 20070809 00059 NM 2007 8 9 SWAA073719 1 20070727 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 442WN 32459 EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007080900068 20070809 00068 NM 2007 8 9 SWAA073739 1 20070729 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 913 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 913, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007080900069 20070809 00069 NM 2007 8 9 SWAA073735 1 20070729 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 930 S23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 23L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007080900071 20070809 00071 NM 2007 8 9 SWAA073740 1 20070729 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM BS 272 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 272.5, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007080900073 20070809 00073 NM 2007 8 9 SWAA073738 1 20070729 A 5310 6547952524 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED HC2 CHECK, FOUND AFT CARGO DOOR AFT LOWER FRAME CRACKED. REMOVED AND REPLACED CARGO DOOR PER MM. 2 L 7 2 4F RT A16WE 2007080900088 20070809 00088 NM 2007 8 9 SWAA073741 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 400 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900090 20070809 00090 NM 2007 8 9 SWAA073746 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727A S6L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900106 20070809 00106 2007 8 9 SWAA073821 4 20070731 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 703SW 27837 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007080900110 20070809 00110 NM 2007 8 9 SWAA073813 1 20070731 A 5311 6546525 FRAME BOEING 737 737317 138447P NM BS 380 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080900113 20070809 00113 NM 2007 8 9 SWAA073800 1 20070731 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8-8LR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080900116 20070809 00116 NM 2007 8 9 SWAA073773 1 20070731 A 5311 6546526 FRAME BOEING 737 7373K2 13844BA NM BS 400 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080900128 20070809 00128 EU 2007 8 9 2007UALA02851 1 20070726 A 2500 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY POWER NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 401UA 435 DURING OPERATIONAL TEST FOR THE EMERGENCY POWER SUPPLY UNITS, EPSU EXT LOAD AFT L IS SHOWN ON PTP PANEL (CIDS DIS). EL ECTRICAL LEAD FAILURE IN 2L SLIDE PACK. REPLACED 2L SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080900129 20070809 00129 EU 2007 8 9 2007UALA02852 1 20070726 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 476UA 1508 R2 DOOR SILL HAS CORROSION JUST FWD OF FRAME 66. REMOVED AND DRAIN AND FWD GIRT BAR PLATE. FABRICATED 2 REPAIR ANGLES. INSTALLED REPAIR. REINSTALLED DRAIN AND GIRT BAR PLATE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080900152 20070809 00152 NM 2007 8 9 2007UALA02876 1 20070728 A 5210 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 L-2 DOOR IS DAMAGED AT UPPER HINGE CUTOUT. FABRICATED AND INSTALLED A FORMED ANGLE DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080900153 20070809 00153 NM 2007 8 9 2007UALA02877 1 20070728 A 3510 OXYGEN SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 336UA 24240 CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. SERVICED O2 SYSTEM TO PROPER LEVEL. NO REPEATS SINCE ORI GINAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080900154 20070809 00154 NM 2007 8 9 2007UALA02878 1 20070728 A 3211 BRAKE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 MLG FIRE A UALA O OTHER A FLAME/FIRE LD LANDING 1 WP 29 648UA 25285 ON ARRIVAL HAD BRAKE FIRE ON NR 1 FWD MLG BRAKE ASSY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080900160 20070809 00160 NM 2007 8 9 2007UALA02884 1 20070729 A 5210 BOTTLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE DOOR 1R ASSIST READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 834UA 1420 DOOR 1R DOOR ASSIST BOTTLE LOW. LOW CYLINDER PRESSURE (UNKNOWN) SERVICED CYLINDER TO PROPER PRESSURE, NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080900161 20070809 00161 EU 2007 8 9 2007UALA02885 1 20070727 A 5240 STRUCTURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 461UA 1266 DOOR 2R DENTED ON THE BOTTOM. REMOVED DAMAGE AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080900163 20070809 00163 EU 2007 8 9 2007UALA02887 1 20070729 A 2622 EXTINGUISHER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LAVATORY READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 442UA 780 LAV F FIRE EXTINGUISHER SYSTEM, SMOKE. CHECKED DETECTOR-OK, REPLACED LAV FIREXT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080900169 20070809 00169 NM 2007 8 9 2007UALA02893 1 20070727 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE ROWS 3-9 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 346UA 24250 FLOOR EEL LIGHTS INOP FROW ROW 3 TO ROW 9. REPLACED LIGHT AT ROW 3 OPS CHK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080900171 20070809 00171 NM 2007 8 9 2007UALA02895 1 20070727 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY EXIT STRIP LIGHT INOP AT 3F. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080900174 20070809 00174 NM 2007 8 9 2007UALA02898 1 20070729 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 22AB INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY CEILING LIGHT ROW 22AB INOP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080900175 20070809 00175 NM 2007 8 9 2007UALA02899 1 20070729 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 40 UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY LIGHT ROW 40 LT INOPERATIVE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080900182 20070809 00182 WP 2007 8 9 IXXA07SMN191S 1 20070630 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1520 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND IN AFT CARGO COMPARTMENT FLOORBEAM UPPER FLANGE SHOWS CORROSION AT STATION 1520 .000 RIGHT BOTTOM LINE 44". REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PA RTS. APPLIED SEALANT TO FAYING SURFACES INSTALLED REPAIR PART IAW DC8 SRM 51-1-21 IAW DC8 SRM 57-7-1 FIGURE 1 PAGE 2 IT EM "F", DC8 SRM 57-1-0 PAGE 1 DC8 SRM 51-1-8B, AND, DC8 51-1-11. 2 L 7 4 4F RT 4A25 2007080900192 20070809 00192 EU 2007 8 9 07FDEA02673 1 20070730 A 5730 FX2241702501 PANEL AIRBUS 310 A310203 3930313 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 PNL 438BL HAS SURFACE CORROSION AND BARE METAL EXPOSED REMOVED CORROSION FOUND OUT OF LIMITS IAW A310-200 SRM 54-55-51. FABRICATED NEW PANEL IAW A310-200 SRM AND GMM 7-1-1001. ALODINED AND PRIMED PER 51-23-10 AND 51-21- 10. 2 L 7 2 4F RT A35EU 2007080900200 20070809 00200 EU 2007 8 9 07FDEA02682 1 20070709 A 5330 A53611658 SKIN AIRBUS 310 A310222 3930315 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 420FE 339 LOWER FUSELAGE: PREVIOUS REPAIR FOUND LOCATED ON LT, FR 17/18 AND STGR26/27. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 53-10-12 FIG 225 SHEET 1. 2 L 7 2 4F RT A35EU 2007081000012 20070810 00012 NM 2007 8 10 AWXA200700930 1 20070726 A 5320 D5348004800001 SILL AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 807AW 1064 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5983472, CORROSION ON THE L2 DOOR CUT OUT LOWER SHAPE SILL, BS 2835 / FR 67, +Y1974 , WL -240. REPLACED THE L2 DOOR CUT OUT LOWER SHAPE SILL, BS 2835 / FR 67, +Y1974, WL -240 IAW A319 SRM 51-42-11. 2 L 7 2 4F RT A28NM 2007081000014 20070810 00014 WP 2007 8 10 IXXA07SMN163S 1 20070630 A 5320 SILL DOUG DC8 DC873F 302199F WP BS 235 L21L MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT LONGERON 21 LEFT AT FS 235 MAIN CARGO DOOR LOWER AFT SILL TO AFT JAMB CORNER. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FO UND. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA REPAIR PARTS. INSTALLED REPAIR PART FROM STATION FS 12 0.000 TO STATION FS 280.000 IAW DC-8 SRM 51-3-0, DC-8 SRM 51-3-1, FORM FAA 8100-9 DATED 07-27-07, BOEING MESSAGE NUMBER 1-41443541-4 DATED 07-16-07, MESSAGE NUMBER 1-441363702-5 DATED 07-27-07, SERVICE BULLETIN DC8-53-079 REV 2, DRAWING DO UGLAS NUMBER SR08530027, SEMAN DRAWING NUMBER ED 4569-2, ROD SKETCH JCTO4203, DC8 SRM 51-1-21, 51-1-20D, DC8 NDT SPM PAR 2 L 7 4 4F RT 4A25 2007081000016 20070810 00016 NM 2007 8 10 AALA20071307 1 20070715 A 7500 VALVE BOEING 757 757223 1384957 NM LEFT ENGINE LEAKING A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 185AN 32379 LAX INFLIGHT T267/15JUL - NUMBER ONE ENGINE OVERHEAD EICAS MESSAGE AND NUMBER ONE ENGINE OVERHEAT WARNING ILLUMINATED. REDUCED LEFT ENGINE TO IDLE AND LANDED LAX WITHOUT INCIDENT. NO FIRE FOUND. FOUND HIGH PRESSURE VALVE LEAKING AT LOWER FLANGE. REPLACED HIGH STAGE VALVE SEALS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081000023 20070810 00023 NM 2007 8 10 AALA20071306 1 20070715 A 3350 LENS BOEING 767 767223 1385123 NM EMERGENCY LIGHTS LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AA 22320 JFK - EMERGENCY LIGHT AT RIGHT FIRST CLASS GALLEY FLOOR HAS BROKEN LENS. LENS NOT BROKEN. SECURED LENS FOR EMERGENCY L IGHT AT RIGHT FIRST CLASS GALLEY FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007081000029 20070810 00029 NM 2007 8 10 AWXA200700931 1 20070727 A 2913 3508807 PUMP BOEING 757 7572S7 1384962 NM LT ENGINE LEAKING A AWXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 903AW 27453 2434 23323 CREW REPORTED LOSS OF HYDRAULIC PRESSURE ON LEFT HYDRAULIC SYSTEM. CREW DECLARED AN EMERGENCY. THE LANDING WAS UNEVENT FUL. MX REPLACED THE LT ENGINE HYDRAULIC PUMP. LEAK/OPERATIONAL CHECKS WERE GOOD. THE A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007081000030 20070810 00030 2007 8 10 AWXA200700932 2 20070728 A 7200 ENGINE BOEING 757 7572G7 1384963 NM LEFT VIBRATION A AWXA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 WP 28 908AW 24233 CREW REPORTED LEFT ENGINE VIBRATION. CREW THROTTLED BACK LT ENGINE TO FLT IDLE. VIBRATION INDICATION WAS STABLE AT .8 A ND VIBRATION MESSAGE EXTINGUISHED. THE CREW DID NOT SECURE THE ENGINE AND DIVERTED TO ITO. EMERGENCY EQUIPMENT WAS DIS PATCHED. THE LANDING WAS UNEVENTFUL. MX IN WORK ON LEFT ENGINE REPLACEMENT. 2 L 7 2 4F RT A2NM 2007081000039 20070810 00039 2007 8 10 DXTA200702365 4 20070729 A 2210 MOTOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL HORIZONTAL STAB FAILED E DXTA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 960QS 7500160 WITH AUTOPILOT ENGAGED, TRIM CLACKER AUDIBLE MORE THAN NORMAL. AFTER DISENGAGING AUTOPILOT, WE DISCOVERED NEITHER YOKE PRIMARY TRIM SWITCH HAD ANY AUTHORITY, NO CAS MESSAGE. WE ENGAGED SECONDARY TRIM SYSTEM AND MADE A PRECAUTIONARY LANDI NG WITHOUT INCIDENT. [08-23-07] INSTALLED NEW MOTOR, CLUTCH AND BRAKE ASSY FOR HORIZONTAL STAB TRIM IAW 750 MM 27-40 -00. OPS CKED GOOD. (NOTE REPLACED L/H PRIMARY). 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007081000040 20070810 00040 CE 2007 8 10 DXTA200702366 1 20070730 A 3250 STEERING SYS CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG MALFUNCTIONED E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 937QS 7500137 SEVERE NOSE WHEEL SHIMMY ON TAKE-OFF, BELOW 40 KTS. IT STARTED JUST AFTER TAKE-OFF ROLL AND LASTED UNTIL NORMAL TAXI SP EED. REMOVED AND REPLACED POWER STEERING UNIT. OPS CHECK GOOD IAW CE750 M/M 32-50-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007081000045 20070810 00045 NM 2007 8 10 CALA0700383 1 20070730 A 5320 6545783502 CHANNEL BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE BS 500-500A CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A 1 INCH CRACK IN NR 1 VHF ANTENNA MOUNT CHANNEL ON BOTH ENDS AT STA 500-500A, S29R TO 29L. THE ANTENNA CHANNEL WAS REPLACED IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2007081000047 20070810 00047 NM 2007 8 10 CALA0700385 1 20070730 A 5340 65C80736156 RAIL BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE BS 727E CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A 1 INCH CRACK IN AFT BAGGAGE BIN TIE DOWN RAIL AT STA 727E, S27R. THE TIE DOWN RAIL WAS REMOVED AND A NEW SECTION OF TIE DOWN RAIL WAS INSTALLED IAW SRM 53-00-53, REPAIR 2, PAGE 202. 2 L 7 2 4F 4 F RT A16WE E2GL 2007081000049 20070810 00049 EU 2007 8 10 MAC070707 1 20070714 A 5751 TEE FITTING AEROSP AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE AILERON CORRODED A MTNA K NONE O OTHER IN INSP/MAINT 1 SO 33 918FX NT1228 262 DURING INSPECTION, LEVEL 2, CORROSION WAS FOUND ON THE (T-FITTINGS) ATTACHING THE RIBS TO THE SPAR. THE FITTINGS AFFECTE D ARE LOCATED AT RT IB, CENTER, AND OB HINGE FITTINGS. THE PROBABLE CAUSE IS DISSIMILAR MATERIALS (STEEL BOLTS IN ALUMIN UM ALLOYED FITTINGS). THE FITTINGS WERE REPLACED AT RIBS 4, 11/12, AND 19. REFERENCE ATR42 SRM 57-61-10 FIG 101 RT AIL ERON. 2 H 7 2 4T 4 T RT A53EU E20NE 2007081000053 20070810 00053 CE 2007 8 10 DXTA200702371 1 20070731 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MALFUNCTIONED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 334QS 5600434 DURING TAXI AFTER LANDING BOTH BRAKE PEDALS WENT TO THE FLOOR. ANTI-SKID INOP ANNUNCIATOR AND POWER BRAKE LOW PRESS ANN UNCIATOR BOTH CAME ON, WAS ABLE TO STOP BY PUMPING THE BRAKES. TROUBLESHOT SYSTEM FOUND AIR IN SYS. BLED ANTISKID BRAKE SYS ON 8/03/07. LET AIRCRAFT SET DURING PAINT PROCESS. BLED ANTISKID BRAKE SYS. AGAIN ON 8/08/07. ALL OPS CK GOOD IAW C ESSNA 560 MM 32-42-00 2 L 7 2 4F 4 F RT A22CE E25EA 2007081000054 20070810 00054 NM 2007 8 10 CALA0700388 1 20070801 A 3350 252005 FUSE BOEING 737 737300 1384610 NM GE CFM56 CFM563B1 13802 NE BATTERY PACK INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14358 THE EMERGENCY LIGHT OVER COCKPIT DOOR WAS FOUND INOPERATIVE. THE F2 FUSE ON BATTERY PACK M1133 WAS REMOVED AND REPLACED IAW AMM 33-51-51. 2 L 7 2 4F 4 F RT A16WE E2GL 2007081000056 20070810 00056 NM 2007 8 10 MWEA070164 1 20070731 A 2560 P401001 BATTERY BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE FLASHLIGHT INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 919ME 55181 EMERGENCY FLASHLIGHT AT FLIGHT ATTENDANT STATION IS NOT SHOWING CHARGING LIGHT. REMOVED AND REPLACED FLASHLIGHT BATTERY . 2 L 7 2 4F 4 F TR A6WE E00061EN 2007081000057 20070810 00057 EA 2007 8 10 A6WA200740356 1 20070625 A 5320 601R3111358 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FS 280 RBL 9 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AW 7878 (2) EA CRACKED ANGLES AT FS 280.0, RBL 9.0. MAINTENANCE REMOVED AND REPLACED ANGLES AT FS 280.00, RBL 9 IAW SRM AND BSC SR 601R-53-0057A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007081000060 20070810 00060 SO 2007 8 10 C2XA07ON014 1 20070728 A 2432 32845001 BATTERY EMB 145 EMB145LR 3260212 SO MASTER OVERTEMP A C2XA O OTHER M J OVER TEMP WARNING INDICATION LD LANDING 1 SW 27 22909 9755 1815 145459 FLT 7756 -IN FLIGHT, CREW REPORTED BATTERY NR 2 OVERTEMP. CREW PERFORMED QRH WAS 59 DEGREES CELSIUS, DURING LANDING BATT ERY TEMP INCREASED SLOWLY TO 70 DEGREES CELSIUS. CREW RECOMMENDED TO SHUT ALL POWER. FIRE TRUCKS WERE CALLED UPON LANDIN G BUT CREW NEVER DECLARED EMERGENCY. MX REMOVED AND REPLACED NR 2 BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND T HE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007081000061 20070810 00061 EU 2007 8 10 BA07011 1 20070731 A 5270 893301 PROXIMITY SENSOR AIRBUS 330 A330323 3930335 EU PWA 4168 PW4168A NE CARGO DOOR INOPERATIVE A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 274AY 0342 FLIGHT 1071: FLIGHT RETURNED TO DEPARTURE DUE TO AN AFT CARGO DOOR OPEN INDICATION. MAINTENANCE REPLACED PROXIMITY SENSO R 28MJ. 2 L 7 2 4F 4 F RT A46NM 2007081000066 20070810 00066 EA 2007 8 10 A6WA200740358 1 20070703 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621-625 S14 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 409AW 7447 LT FS 621.00 TO 625.00 OBLIQUE ANGLE IS CRACKED 1.5 INCH LONG IN AFT RADIUS. (K) MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED A NEW ANGLE P/N 601-35012-51 IAW CRJ SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007081000067 20070810 00067 EA 2007 8 10 A6WA200740361 1 20070707 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 409AW 7447 INTERCOSTAL FLANGE AT FS 484.00, RBL 9.0, IS CRACKED NEAR RADIUS APPROX .15 INCH LONG. (K) MAINTENANCE REMOVED AND RE PLACED INTERCOSTAL FLANGE AT FS 484 RBL 9 IAW BSC STANDARD REPAIR 601R-53-0029B AND CRJ200 SRM 51-42-21. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007081000068 20070810 00068 EA 2007 8 10 A6WA200740362 1 20070707 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 409AW 7447 INTERCOSTAL FLANGE AT FS 484.00, LBL 9.0, IS CRACKED NEAR RADIUS APPROX .20 INCH LONG. (K) MAINTENANCE REMOVED AND RE PLACED INTERCOSTAL FLANGE AT FS 484 LBL 9 IAW BSC STANDARD REPAIR 601R-53-0029B AND SRM 51-42-21. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007081000071 20070810 00071 EA 2007 8 10 A6WA200740365 1 20070709 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 409AW 7447 LT WING PLANK ACCESS HOLE NR 11, (550CB) WS 209.040 HAS PITTING ON IB AND OB ENDS APPROX .005 INCH DEEP LOCATED IN NON CRITICAL AREA. (K) MAINTENANCE REMOVED PITTING, NDT, ROTO PEENED AND PROTECTED TREATED AREA. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007081000073 20070810 00073 EA 2007 8 10 A6WA200740366 1 20070709 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 409AW 7447 RT WING PLANK ACCESS HOLE R 2 (610AB) WS 12.245 HAS PITTING ALONG FWD HALF OF HOLE, APPROX .007 DEEP LOCATED IN CRITICAL AREA. (K) MAINTENANCE REMOVED MINOR PITTING, NDT, ROTO-PEENED AND TREATED AREA. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007081000074 20070810 00074 SO 2007 8 10 GLBA20060967 1 20070730 A 2150 1945463 HEAT EXCHANGER EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT A/C PACK UNKNOWN A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NM 03 293UX 120293 FLIGHT 5008 PILOTS REPORTED THAT ON LOW POWER DESCENT THE LT PACK SYSTEM WAS PRODUCING SMOKE/ODOR IN THE AIRCRAFT. BLEED S AND PACK SYSTEMS WERE SET AT LOW SETTING. MAINTENANCE REMOVED AND REPLACED THE LT HEAT EXCHANGER ASSEMBLY IAW EMB-120 MM 21-50. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2007081000075 20070810 00075 EU 2007 8 10 TRBA2007060 1 20070730 A 3350 167006 LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT BROKEN A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 369AT 369 LOWER EMERGENCY EXIT SIGN ON SERVICE DOOR BROKEN. REMOVED AND REPLACED LIGHT BULBS AND EMERGENCY EXIT SIGN COVER IAW JI C NR 33-51-24. PERFORMED OPT CK IAW JIC NR 33-50-00 AND FOUND WORKING PROPERLY. 2 H 7 2 4T RT A53EU 2007081000076 20070810 00076 EA 2007 8 10 A6WA200740367 1 20070708 A 2620 8990741 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT UNKNOWN A A6WA K NONE L NO TEST IN INSP/MAINT 1 GL 31 445AW 9620 7804 MAINTENANCE REPORTED RT ENGINE BOTTLE NR 2 PUS-TO DISCHARGE GREEN PUSHBUTTON WOULD NOT ILLUMINATE WHEN TESTED. REMOVED AND REPLACED RT ENGINE FIRE BOTTLE FIRE BOTTLE. OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007081000078 20070810 00078 EA 2007 8 10 A6WA200740369 1 20070706 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 461AW 7870 RT FS 621 FLOOR SUPPORT ANGLE CRACKED APPROX .2 INCH LONG. (K) MAINTENANCE REPAIRED RIGHT FLOOR SUPPORT ANGLE AT FS 62 1 IAW BOMBARDIER REO 601R-53-61-117. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007081000079 20070810 00079 EA 2007 8 10 A6WA200740372 1 20070706 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 461AW 7870 LT 484 ANGLE IS CRACKED APPROX .5 INCH L AT LBL 27. (K) MAINTENANCE REMOVED ANGLE IAW SRM 51-42-06 AND 51-42-21. FAB RICATED AND INSTALLED REPAIR ANGLE IAW BSC SR 601R-53-0039B. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007081000080 20070810 00080 EA 2007 8 10 A6WA200740373 1 20070706 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 461AW 7870 LT 484 ANGLE IS CRACKED APPROX .2500 INCH AT LBL 36. (K) MAINTENANCE REMOVED FLANGE IAW BOMBARDIER REO 601R-53-41-059 REV A. FABRICATED AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R-53-1-059 AND BSC SR 601R-53-0030A. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007081000083 20070810 00083 EA 2007 8 10 A6WA200740375 1 20070706 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 461AW 7870 RT 484 ANGLE IS CRACKED APPROX .5 INCH LONG AT RBL 27. (K) MAINTENANCE REMOVED FLANGE IAW BOMBARDIER REO 601R-53-41-05 9 REV A. FABRICATED AND INSTALLED REPAIR ANGLE IAW REO 601R-53-41-059 AND BSC SR 601R-53-0030A. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007081000086 20070810 00086 EA 2007 8 10 A6WA200740378 1 20070707 A 5710 PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 461AW 7870 LT FUEL PANEL 540BB HAS CORROSION DAMAGE IN THE NON-CRITICAL AREA COMPLY WITH E06/21/457 (WING PLANK CUTOUT) (K) MAINT ENANCE REPAIRED WING PLANK IAW BOMBARDIER REO 601R-57-21-030. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007081000088 20070810 00088 2007 8 10 A6WA200740380 4 20070708 A 2565 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CARGO DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 461AW 7870 CARGO DOOR FWD SLIDE RAIL LOWER BRACKET CRACKED. (K) MAINTENANCE REMOVED AND REPLACED CHANNEL IAW CRJ SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007081000089 20070810 00089 EA 2007 8 10 A6WA200740381 1 20070709 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621-625 S14L CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 461AW 7870 LT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.5 INCH LONG. (K) REMOVED AND REP LACED FS 621 TO 625.30 INTERCOSTAL IAW BOMBARDIER AERO SPACE REO 601R-53-61-422 AND CRJ SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007081000090 20070810 00090 NM 2007 8 10 UPS07450346 1 20070727 A 5730 65B10730112 PANEL BOEING 747 747123F NM PWA JT9 JT9D7A 52054 NE RT WING DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 RT WING LEADING EDGE, TOP FILLER PANELS OF NR 3 ENGINE 4 INCH X 10 INCH DELAMINATED. DISCOVERED ADDITIONAL DELAM OF INN ER SKIN OPPOSITE EXTERIOR SOFT SPOT. REMOVED PANEL FROM AIRCRAFT XZ 1227688, TRIMMED AND PICKED UP HOLES IN NEW PANEL IA W INSTALLED NEW PANEL, USED WAS STEEL SCREWS REF SRM 51-30-03. 2 L 7 4 4F 4 F A20WE E20EA 2007081000091 20070810 00091 NM 2007 8 10 UPS07550352 1 20070703 A 5754 STRUCTURE BOEING 757 75724APF 1384969 NM PWA 2037 PW2040 NE NR 2 SLAT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 421UP 25281 N/A NR 2 LEADING EDGE SLAT HAS VARIOUS DENTS FROM HAIL DAMAGE. NR 2 SLAT HAS 98 DENTS FROM HAIL DAMAGE. DENTS GREATER THAN .010 INCH ARE DOCUMENTED IN FIG 1 EO B757-5750-27018-A. 10-8-07 ACCOMPLISHED REMOVAL OF NR 1 L/E SLAT UP THROUG H STEP D14 OF MM 27-81-02-4. COMPLETED REMOVAL INSTALLATION AND TEST OF SLAT WITH REF TO MM 27-81-02-4. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081000092 20070810 00092 NM 2007 8 10 UPS07550356 1 20070719 A 5330 2024T3050 SKIN BOEING 757 75724APF 1384969 NM PWA 2037 PW2040 NE BS 563 BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 401UP 23723 INSPECTION TYPE: C LWR EXT FUSELAGE SKIN BULGING APPROX BSTA 563 BETWEEN S24L S25L. REMOVED FAST AT AFFECTED AREA COMMO N TO REPAIR IAW SRM 51-40-02 AND CUT OUT DAMAGED SECTION L 2.8 INCH X W 2.4 INCH IAW SRM 53-00-01-2R3. HFEC INSPECTED CU TOUT IAW NTM 51-00-01 PT 6. NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER IAW SRM 53-00-01 2R3 FIG 201, TBL 1. (P/N 2024T3 .050 AND B/N 1276774) LOCATED AND DRILLED IAW SRM 51-40-05. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081000117 20070810 00117 EA 2007 8 10 TRAX200701043 1 20070724 A 5260 HANDLE CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 873AS 7549 ASD EXTERNAL HANDLE CRACKED. INSTALLED NEW ASD SPLINE SHAFE , CAM, AND ASD HANDLE IAW CRJ 200 SRM 51-00-00 AND CRJ 200 A MM 52-11-03. 2 L 7 2 4F RT A21EA 2007081000118 20070810 00118 EA 2007 8 10 TRAX200701044 1 20070724 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 4848 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 833AS 7246 FS 484 RIGHT I/B CLIP CRACKED UNDER FLOOR PANEL 262 DRF. PERFORMED FPI ON FS 484.00 R/H I/B CLIP UNDER 263DRF. DEFEC TS NOTED PER CRJ 200 NDTM 51-20-28. REMOVED DAMAGED CLIP FROM RT I/B FS 484, FABRICATED NEW SERVICEABLE CLIP USING, .063 , 2024-T3, PO# 950028, LOCATED AND DRILLED HOLES, ALODINED, PRIMED, AND PAINTED IAW CRJ SRM 51-25-16. INSTALLED NEW SERV ICEABLE CLIP. ALL WORK DONE IAW ASA REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2007081000119 20070810 00119 EA 2007 8 10 TRAX200701049 1 20070725 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 559-589 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 873AS 7549 CARGO COMPARTMENT FLOORBOARD SUPPORT STRUCTURE AT FS 559+96.00 TO FS 589.00 ALONG WALL AT FLOORBOARD LEVEL, CORROSION ON SURFACE UNDER FLOORBOARD ALSO ALL NUT PLATES IN SAME AREA CORRODED. IAW BOMBARDIER REO 601R-53-00215.COMPLIED WITH EC/ TC REO 601R-53-00-215. 2 L 7 2 4F RT A21EA 2007081000120 20070810 00120 EU 2007 8 10 YENA2007068 1 20070726 A 2910 ZCV6361 CHECK VALVE AIRBUS 320 A320232 3930326 EU HYD SYSTEM FAILED A YENA O OTHER J WARNING INDICATION CR CRUISE 1 EA 15 517JB 27456 1327 FLT 1012, JFK TO BOS, DECLARED EMERGENCY, YELLOW RSVR OVERHEAT INDICATION BOTH ON ECAM & OVERHEAD ON ENG & ELECTRIC PUMP S. T/S TSM 29-13-00-810-802. FOUND ELEC PUMP DELIVERY CHECK VALVE BAD. REMOVED AND REPLACED CHECK VALVE PER AMM 29-24 -21-04. DID VISUAL INSP OF REMOVED CHECK VALVE PER TSM 29-13-00-810-802 4A ITEM 2, NO MISSING PARTS. FOUND VALVE TURNE D SIDEWAYS. LEAK CHECK GOOD. NR 2 ENG EDP NEEDS REPLACEMENT PRECAUTIONARY DUE TO MULTIPLE SYSTEM OVERHEATING OF YELLOW SYSTEM. REPLACED NR 2 ENG EDP PRECAUTIONARY PER AMM 29-13-51-04, SYS OPS CHECK NORMAL. 2 L 7 2 4F RT A28NM 2007081000121 20070810 00121 WP 2007 8 10 UPS07850287 1 20070726 A 7830 THRUST REVERSER DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 2 ENGINE INOPERATIVE A IPXA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SO 01 803UP 46073 NUMBER 2 ENG DUE TO THRUST REVERSER WOULD NOT STOW COMPLETED ALL CHECKLIST. PER CAPTAIN ENGINE HAD POSITIVE OIL PRESSUR E REMAINDER OF FLIGHT. DEF NR M 355263 OPENED. DEFERRED NR 2 ENG THRUST REVERSER ACCOMPLISHED DEACTIVATION PROCEDURES REF MEL 78-1 AND M/M 78-00-00-2 A/C OK TO CONTINUE. REVISED REACTIVATED NR 2 THRUST REVERSER, INSPECTED WIRING ON E NGINE, TESTED, PER MM 78-00-00-2. BOTH NORMAL & EMERGENCY STOW ALL CHECK GOOD. OPS CHECKED GOOD, NO LEAKS NOTED. THIS CL EARS M355263. 2 L 7 4 4F 4 F RT 4A25 E2GL 2007081000122 20070810 00122 NM 2007 8 10 DHL2007784533 1 20070710 A 5347 BAC15205417170 SEAT TRACK BOEING 727 727227 1384078 NM ZONE 100 GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 MAIN CARGO NICKS AND GOUGES ON SEAT TRACK TOP SURFACE, BS 741 TO 868, RBL 45, WL 208.5 AS MARKED. REMOVED SEAT TRACK OU T OF LIMITS STA 760 TO 850 IAW B727 SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK FROM P/N BAC1520-541-7170T6511, DIM . 99.25 IAW B727 SRM 53-10-2, FIG 7 AND 51-30-2. TREATED, PRIMED AND INSTALLED SEAT TRACK IAW B727 SRM 51-10-2 AND 51-3 0-2, FIG 1. 2 L 7 3 4F A3WE 2007081000123 20070810 00123 NM 2007 8 10 DHL2007784536 1 20070723 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1223 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 EXTERIOR FUSELAGE STA 1223, RBL 10, STR 30 A PREVIOUS REPAIR IS CRACKED. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2. FABRICATED NEW REPAIR FROM 2024T3,.050, 8.5 BY 8.5 IAW B727 SRM 53-30-2, FIG 3 AND 53-30-3, FIG 1. TREATED, PRIMED AND INSTALLED NEW ANGLE IAW B727 SRM 51-10-2, 51-30-2 AND 53-30-3, FIG 1 IAW B727 SRM 53-30-3, TABLE 3 THIS REPAIR IS A CAT EGORY C AND REQUIRES REINSPECTION AT 3000 CYCLES WITH A 10,000 CYCLE LIMIT. 2 L 7 3 4F A3WE 2007081000124 20070810 00124 EU 2007 8 10 07FDEA02650 1 20070728 A 5313 A53970701215 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT PIT, STR 46R CORRODED AT BS 3037. REMOVED AND REPLACED CORRODED SECTION OF S46R FR 54.2 TO 54.3 IAW FEDEX A310-200 SRM 53-10-14 PG 203/204. TREATED AND PRIMED AND TOP COATED PER A310-200 SRM 51-21-10, 51-23-10 2 L 7 2 4F RT A35EU 2007081000125 20070810 00125 EU 2007 8 10 07FDEA02651 1 20070728 A 5313 DAN50809 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT PIT STR 54R CORRODED BETWEEN BS 3143-3302, REMOVED AND REPLACED STRINGER PER A310-200 SRM 53-10-14 PG 203 AND 204. ALODINED AND PRIMED AND TOP COATED PER A310-200 SRM 51-23-10 AND 51-21-10. 2 L 7 2 4F RT A35EU 2007081000126 20070810 00126 EU 2007 8 10 07FDEA02652 1 20070728 A 5313 DAN50809 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT PIT, STR 53R CORRODED BETWEEN BS 3146-3302, REMOVED AND REPLACED STRINGER PER A310-200 SRM 53-10-14 AND 53-12-14. ALODINED AND PRIMED PER A310-200 SRM 51-23-10 AND 51-21-10. 2 L 7 2 4F RT A35EU 2007081000127 20070810 00127 NM 2007 8 10 07FDEA02655 1 20070729 A 5313 AFA7105513 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 DAMAGED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 602FE 48402 LONGERON 38R AT STA 1865 FOUND WITH SHORT PITCHES. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-114762. REPAIR CLASSIFI ED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007081000134 20070810 00134 WP 2007 8 10 07FDEA02668 1 20070730 A 5753 NRC6060 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 RT WING INBD FLAP EXT SKIN UPPER SIDE FOUND DENT 1.50" BY 1" DEEP .078". REPAIRED SKIN IAW SRM 57-00-01 VOL 1 FIG 4 SHT 2. 2 L 7 3 4F A22WE 2007081300001 20070813 00001 NM 2007 8 13 SWAA073780 1 20070731 A 5311 6546532 FRAME BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300002 20070813 00002 NM 2007 8 13 SWAA073772 1 20070731 A 5311 6546532 FRAME BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300004 20070813 00004 NM 2007 8 13 SWAA073833 1 20070731 A 5311 6546536 FRAME BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080900093 20070809 00093 NM 2007 8 9 SWAA073749 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727A S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900094 20070809 00094 NM 2007 8 9 SWAA073748 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 706 S3R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900095 20070809 00095 NM 2007 8 9 SWAA073747 1 20070730 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727D S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080900107 20070809 00107 2007 8 9 SWAA073768 4 20070730 A 2565 63551101 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 777QC 30592 DURING SCHEDULED MV1 CHECK, R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED E VAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007080900112 20070809 00112 NM 2007 8 9 SWAA073794 1 20070731 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080900120 20070809 00120 NM 2007 8 9 SWAA073795 1 20070731 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080900121 20070809 00121 NM 2007 8 9 DL76S070964 1 20070719 A 5330 7075T62 SKIN BOEING 767 767332 1382001 NM BS1175-1197 S36R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 130DL 24080 DURING HMV3 AT MOBILE AEROSPACE ENGINEERING, FOUND AFT PIT AT S36R OTBD LOWER FLANGE EXFOLIATED BS 1175 TO BS1197. REMO VED DAMAGED AREA AND INSTALLED REPAIR STRINGER AND FUSE DOUBLER REF SRM 53 00 01 FIG 201 REPAIR 12. 2 L 7 2 4F RT A1NM 2007080900123 20070809 00123 NM 2007 8 9 DL757070966 1 20070728 A 2750 TRANSMISSION BOEING 757 757232 1384965 NM LT TE FLAP TRIPPED A DALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 27 6714Q 30485 T/E FLAP DISAGREE MESSAGE AND LIGHT ON APPROACH. COMPLETED NON-NORMAL CHECKLIST. FLAPS WENT TO 20 ELECTRICALLY. LIGHT S WENT OUT. T/S PER FIM. BITE CKD FSEU NR 1 FAULT MSG 305 FLAP DISAGREE. BITE CHECK OF FSEU 2 AND 3, NO FAULTS. FOUN D LT INBD FLAP TRANS OVERLOAD INDIC SHOWING. RESET SAME. LUBED INBD TRANS AND CKD FLUID LEVELS. ALL CKD GOOD. RAN FL APS SEVERAL TIMES ,NO EVIDENCE OF BINDING. NO FAULT MSGS PRESENT. 2 L 7 2 4F RT A2NM 2007080900132 20070809 00132 NM 2007 8 9 2007UALA02855 1 20070726 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GALLEY DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 FWD GALLEY DOOR SN1223 LWR FWD FRAME CORNER HAS 2 HOLES CRACKED. INSTALLED KIT SPLICE FRAME REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080900133 20070809 00133 NM 2007 8 9 2007UALA02856 1 20070726 A 3350 LAMP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 303UA 23644 EEL LAMP IS INOP IN AFT CABIN. REPLACED EEL LIGHT LAMP, OPS.CK OK 2 L 7 2 4F 4 F RT A16WE E2GL 2007080900146 20070809 00146 EU 2007 8 9 2007UALA02870 1 20070727 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN SMOKE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 440UA 702 POSSIBLE SMOKE IN THE CABIN. RECIRC FAN FAILURE- SHOP FINDINGS INDICATE ROUGH BEARINGS, WASHERS AND PACKINGS WORN. (WO ULD NOT ROTATE) REPLACED FAN. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080900148 20070809 00148 EU 2007 8 9 2007UALA02872 1 20070728 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE BUCKLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 476UA 1508 FUSELAGE SKIN BUCKLED, RT SIDE AFT OF PIT DOOR BETWEEN FR 59-61 STR 35-39. WHEN RIVETS REMOVED FROM CLIPS, FOUND GAP BE TWEEN SKIN AND CLIPS EXCEEDING .031". MAJOR REPAIR ACCOMPLISHED: REPLACED 4 CLIPS AND INSTALLED DOUBLER REPAIR AT FRAM E 59 AND STRINGER 35R. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080900159 20070809 00159 NM 2007 8 9 2007UALA02883 1 20070730 A 2797 GROUND WIRE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE WING DISCONNECTED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 914UA 25381 NR 3 LE FLAP FULL EXTEND AND FWD PNL INTRANSIT LIGHTS ON WITH FLAPS RETRACTED. ALL WIRE BUNDLE CLAMPS FROM S173 SENSOR TO SPLICES AT PRESSURE FEED THRU LOCATED 3 FEET OB OF WING ROOT ARE LOOSE. GROUND WIRES AT GD148AC ARE ALSO DISCONNECTE D. SECURED WIRING AND GROUND WIRES. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080900179 20070809 00179 NM 2007 8 9 2007UALA02903 1 20070727 A 3350 LAMP AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 821UA 944 EMERGENCY ESCAPE PATH LIGHTING AT SEATS 13C, 14C AND 18C HAVE ONE INOP LAMP. RELAMPED SEAT LOCATIONS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080900185 20070809 00185 SO 2007 8 9 SIMA200721202 1 20070720 A 5320 14521700007 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 821AE 13157 5000 145577 LEFT OMEGA BEAM CORRODED AT FRAME 20. REPAIRED CORRODED AREA IAW EMB SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007080900198 20070809 00198 NM 2007 8 9 07FDEA02680 1 20070731 A 5313 AFA7105513 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 AFT CARGO COMPARTMENT, RT TUNNEL AREA LONGERON 38R SPLICE BETWEEN STA 1853 TO STA 1871 FOUND CRACKED. [08-15-07] REM OVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007080900199 20070809 00199 NM 2007 8 9 07FDEA02681 1 20070731 A 5713 ARB293210 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 RT WING LEADING EDGE CAVITY STRINGER AT XOS 789 FOUND CRACKED. [08-17-07] REPAIRED AS PER FEDEX E.A. 1-5710-112372, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007081000003 20070810 00003 EU 2007 8 10 07FDEA02686 1 20070731 A 5340 A5377364420100 FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 FRAME FITTING C37 IS CRACKED AT RBL 60 FWD PIT FLOOR LEVEL REMOVED AND REPLACED FITTING PER A310-200 SRM 51-40-21 PARAGR AGH 5 AND 6. 2 L 7 2 4F RT A35EU 2007081000004 20070810 00004 EU 2007 8 10 07FDEA02687 1 20070731 A 5315 LN9497A420 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 T-CAP CORRODED FR35 AT RBL 56 TO 62 FWD PIT REMOVED AND REPLACED T-CAP PER A310-200 SRM 51-40-21 PARAGRAGH 7 AND 53-10-1 5, PAGE 241 AND 242. 2 L 7 2 4F RT A35EU 2007081000009 20070810 00009 NM 2007 8 10 HALA0700314 1 20070731 A 2897 CONNECTOR BOEING 767 767332 1382001 NM BOOST PUMP DIRTY A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, R AFT BOOST PUMP LOW PRESS LGT FAILED TO ILLUM AND EICAS MSG FAILED TO DISPLAY WITH SW OFF. C LEANED CONTACTS AT PRESS SWITCH CONNECTOR. PRESS LIGHT AND EICAS MSG FUNCT NORMAL. OPS CK R AFT BOOST PUMP PER AMM 28- 27-00, OPS NORMAL. 2 L 7 2 4F RT A1NM 2007081000025 20070810 00025 NM 2007 8 10 AALA20071304 1 20070714 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 608AA 27446 DFW - EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081000044 20070810 00044 EU 2007 8 10 MAC070706 1 20070714 A 5751 FITTING AEROSP AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE AILERON CORRODED A MTNA K NONE O OTHER IN INSP/MAINT 1 SO 33 918FX NT1227 262 DURING INSPECTION, LEVEL 2 CORROSION WAS FOUND ON THE (T- FITTINGS) ATTACHING THE RIBS TO THE SPAR. THE FITTINGS AFFECTE D ARE LOCATED AT THE IB, CENTER, AND OB HINGE FITTINGS. THE PROBABLE CAUSE IS DISSIMILAR MATERIALS (STEEL BOLTS IN ALUMI NUM ALLOYED FITTINGS). THE FITTINGS WERE REPLACED AT RIBS 4, 11/12, AND 19. REFERENCE ATR42 SRM 57-61-10 FIG 101. 2 H 7 2 4T 4 T RT A53EU E20NE 2007081000050 20070810 00050 SW 2007 8 10 PNSA070705 1 20070729 A 3230 UPLOCK SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP NLG BENT A PNSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 41NE AC741B AFTER DEPARTURE THE LANDING GEAR WAS SELECTED UP THEN THE NOSE GEAR TRANSIT LIGHT ILLUMINATED, THE NOSE GEAR WOULD NOT L OCK UP. AN UNEVENTFUL LANDING WAS MADE AT DEPARTURE AIRPORT. MX FOUND THAT THE NOSE GEAR UP LOCK STRICKER EXTENSION WA S LOOSE AND BENT. REPLACED STRICKER EXTENSION GEAR. OP'S CHECKED NORMAL. 2 L 7 2 4T 4 T RT A8SW E4WE 2007081000052 20070810 00052 NE 2007 8 10 DXTA200702370 2 20070731 A 7200 ENGINE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D1 52060 NE LEFT MALFUNCTIONED E DXTA E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 303QS 5600343 LT ENGINE QUIT AFTER NORMAL START SEQUENCE AND STABILIZATION. AFTER PERFORMING GENERATOR CHECK NOTICED LT FUEL BOOST PU MP ANNUNCIATOR ON, THEN N2 ROLLING DOWN. THROTTLE LEVER WAS PLACED ON GATE AND NEVER MOVED. PERFORMED LEFT ENGINE STA RT PROCEDURES PER NJA CHECKLIST OPENED LEFT COWL INSPECTED FUEL CONTROL AND FLOW DIVIDER RIGGING PER CE560 MM 76-11-00 A LL RIGGING CHECKS GOOD. MULTIPLE START AND SHUTDOWN PROCEDURES PRODUCE NO DISCREPANCIES. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A22CE E1NE 2007081000063 20070810 00063 NM 2007 8 10 PIDA07038 1 20070730 A 5330 SKIN BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 583CC 21069 DURING C-CHECK, REMOVED PREVIOUS REPAIR AT RT FWD CORNER OF ELECTRONIC ACCESS DOOR FOR EVALUATION AND NOTED ADDITIONAL C RACK IN SKIN UNDER DOUBLER. REPAIRED AREA IAW SRM 52-00-3 FIGURE 5. 2 L 7 2 4F 4 F A16WE E2EA 2007081000064 20070810 00064 NM 2007 8 10 PIDA07037 1 20070731 A 5330 SKIN BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE BS 341-351 CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 583CC 21069 DURING C-CHECK, NOTED CORROSION AROUND INNER SKIN OF FUSELAGE AT ELECTRONIC BAY DOOR OPENING. REPAIRED AREA IAW EA 53-1 99. 2 L 7 2 4F 4 F A16WE E2EA 2007081000070 20070810 00070 EA 2007 8 10 A6WA200740364 1 20070709 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 409AW 7447 LT WING PLANK ACCESS HOLE NR 2, (510AB) WS 12.245 HAS PITTING AT IB AND OB ENDS APPROX .005 INCH DEEP LOCATED IN NON-CR ITICAL AREA. (K) MAINTENANCE REMOVED PITTING, NDT, ROTO-PEENED AND PROTECTIVE TREATED. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007081000081 20070810 00081 EA 2007 8 10 A6WA200740374 1 20070706 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 461AW 7870 RT 484 ANGLE IS CRACKED APPROX .2500 INCH LONG AT RBL36. (K) MAINTENANCE REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51 -42-06 AND 51-42-21. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007081000128 20070810 00128 NM 2007 8 10 07FDEA02656 1 20070729 A 5313 AGA79931 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 LONGERON 39R AT STA 1857 FOUND WITH FASTENER HOLE ELONGATED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-114762, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007081000129 20070810 00129 NM 2007 8 10 07FDEA02657 1 20070729 A 5313 NGA6313515 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 LONGERON 37R AT STA 1841 FOUND WITH FASTENER HOLE AS 1/4" SIZE. REPAIR CARRIED OUT PER FEDEX EA 1-5310-114762. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007081000130 20070810 00130 NM 2007 8 10 07FDEA02658 1 20070729 A 5313 NGA6313515 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 LONGERON 38R AT STA 1864 FOUND WITH HOLE DIAMETER AS 1/4" SIZE. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-114762. REPA IR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007081000131 20070810 00131 NM 2007 8 10 07FDEA02659 1 20070729 A 5313 AGA7026503 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 LONGERON 38R AT STA 1863 FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 53-10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007081000132 20070810 00132 NM 2007 8 10 07FDEA02660 1 20070729 A 5330 NGA6312511 SKIN DOUG MD11 MD11F 3023600 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 FUSELAGE RT SIDE AT STA 1841-1855 BETWEEN X = 35 AND X = 36 FOUND DENTED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-11 4762. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007081000133 20070810 00133 WP 2007 8 10 07FDEA02662 1 20070729 A 5720 ARB0029506 SUPPORT BRACKET DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 RT WING O/B FLAP, I/B HINGE, O/B ATTACH BRACE CRACKED AT REAR SPAR. REMOVED AND REPLACED CRACKED SUPPORT ARB0029-506. REF SRM 57-00-01. 2 L 7 3 4F A22WE 2007081300003 20070813 00003 NM 2007 8 13 SWAA073826 1 20070731 A 5311 6546534 FRAME BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300005 20070813 00005 NM 2007 8 13 SWAA073777 1 20070731 A 5311 6546536 FRAME BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300006 20070813 00006 NM 2007 8 13 SWAA073814 1 20070731 A 5311 6546538 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300007 20070813 00007 NM 2007 8 13 SWAA073796 1 20070731 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300009 20070813 00009 NM 2007 8 13 SWAA073804 1 20070731 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300011 20070813 00011 NM 2007 8 13 SWAA073805 1 20070731 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300013 20070813 00013 NM 2007 8 13 SWAA073815 1 20070731 A 5311 6546552 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300014 20070813 00014 NM 2007 8 13 SWAA073774 1 20070731 A 5311 6546552 FRAME BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300015 20070813 00015 NM 2007 8 13 SWAA073782 1 20070731 A 5311 6546554 FRAME BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300018 20070813 00018 NM 2007 8 13 SWAA073827 1 20070731 A 5311 6546555 FRAME BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300019 20070813 00019 NM 2007 8 13 SWAA073817 1 20070731 A 5311 6546555 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300020 20070813 00020 NM 2007 8 13 SWAA073799 1 20070731 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300021 20070813 00021 NM 2007 8 13 SWAA073830 1 20070731 A 5311 6546557 FRAME BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300022 20070813 00022 NM 2007 8 13 SWAA073783 1 20070731 A 5311 6546557 FRAME BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300025 20070813 00025 NM 2007 8 13 SWAA073803 1 20070731 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300027 20070813 00027 NM 2007 8 13 SWAA073819 1 20070731 A 5311 6546593 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300028 20070813 00028 NM 2007 8 13 SWAA073778 1 20070731 A 5311 6546593 FRAME BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300031 20070813 00031 NM 2007 8 13 SWAA073812 1 20070731 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300034 20070813 00034 NM 2007 8 13 SWAA073784 1 20070731 A 5340 65C27314 STRINGER CLIP BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300035 20070813 00035 NM 2007 8 13 SWAA073785 1 20070731 A 5340 65C27314 STRINGER CLIP BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007081300036 20070813 00036 NM 2007 8 13 SWAA073786 1 20070731 A 5340 65C27314 STRINGER CLIP BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300037 20070813 00037 NM 2007 8 13 SWAA073787 1 20070731 A 5340 65C27314 STRINGER CLIP BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007081300039 20070813 00039 NM 2007 8 13 SWAA073789 1 20070731 A 5340 65C27314 STRINGER CLIP BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300040 20070813 00040 NM 2007 8 13 SWAA073809 1 20070731 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300041 20070813 00041 NM 2007 8 13 SWAA073806 1 20070731 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300042 20070813 00042 NM 2007 8 13 SWAA073810 1 20070731 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300043 20070813 00043 NM 2007 8 13 SWAA073807 1 20070731 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300044 20070813 00044 NM 2007 8 13 SWAA073791 1 20070731 A 5315 65C34537 FLOORBEAM BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 660, RBL 24. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300045 20070813 00045 NM 2007 8 13 SWAA073825 1 20070731 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 703SW 27837 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 17 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2007081300046 20070813 00046 NM 2007 8 13 SWAA073824 1 20070731 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 703SW 27837 DURING SCHEDULED HC1 CHECK, AFT RT EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007081300049 20070813 00049 NM 2007 8 13 SWAA073838 1 20070801 A 3350 1619 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 606SW 27926 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007081300050 20070813 00050 NM 2007 8 13 SWAA073842 1 20070801 A 3350 1619 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PE R MM. 2 L 7 2 4F RT A16WE 2007081300051 20070813 00051 NM 2007 8 13 SWAA073854 1 20070801 A 3350 20131A BATTERY PACK BOEING 737 7373Y0 1384671 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007081300052 20070813 00052 NM 2007 8 13 SWAA073853 1 20070801 A 3350 3071BPEGPL LIGHT BOEING 737 7377AD 1384502 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 798SW 28436 DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 9 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007081300054 20070813 00054 NM 2007 8 13 SWAA073852 1 20070801 A 3350 311500 LENS BOEING 737 7373A4 1384585 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED SPV CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007081300055 20070813 00055 NM 2007 8 13 SWAA073834 1 20070801 A 3233 65448105 ACTUATOR BOEING 737 7373H4 1384600 NM RT MLG FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 611SW 27697 DECLARED EMERGENCY / DIVERSION. RIGHT MLG STAYED DOWN AND LOCKED DURING CLIMB. FERRY TO HOU FOR MAINTENANCE. REMOVED AND REPLACED RIGHT MLG RETRACT ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2007081300056 20070813 00056 NM 2007 8 13 SWAA073877 1 20070801 A 5330 6545767 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 413, LBL 3. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300059 20070813 00059 NM 2007 8 13 SWAA073876 1 20070801 A 5312 6545819 PRESSURE PANEL BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND NLG W/W PRESSURE WEB CRACKED AT LEFT BS 245. REPAIRED WEB PER ACO. 2 L 7 2 4F RT A16WE 2007081300060 20070813 00060 NM 2007 8 13 SWAA073875 1 20070801 A 5312 6545819 PRESSURE PANEL BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND NLG W/W PRESSURE WEB CRACKED AT RIGHT BS 245. REPAIRED WEB PER ACO. 2 L 7 2 4F RT A16WE 2007081300061 20070813 00061 NM 2007 8 13 SWAA073844 1 20070801 A 5311 6546521 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300062 20070813 00062 NM 2007 8 13 SWAA073845 1 20070801 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300063 20070813 00063 NM 2007 8 13 SWAA073840 1 20070801 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, STR 18L. REPAIRED FRAME PER SB. 2 L 7 2 4F RT A16WE 2007081300064 20070813 00064 NM 2007 8 13 SWAA073843 1 20070801 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, STR 18L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300065 20070813 00065 NM 2007 8 13 SWAA073869 1 20070801 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300069 20070813 00069 NM 2007 8 13 SWAA073859 1 20070801 A 5322 6546546 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007081300070 20070813 00070 NM 2007 8 13 SWAA073860 1 20070801 A 5322 6546546 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007081300071 20070813 00071 NM 2007 8 13 SWAA073862 1 20070801 A 5322 6546546 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007081300072 20070813 00072 NM 2007 8 13 SWAA073861 1 20070801 A 5322 6546546 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007081300073 20070813 00073 NM 2007 8 13 SWAA073841 1 20070801 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300075 20070813 00075 NM 2007 8 13 SWAA073847 1 20070801 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300076 20070813 00076 NM 2007 8 13 SWAA073864 1 20070801 A 5312 6546568 PRESSURE BLKHD BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 7L. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 2007081300077 20070813 00077 NM 2007 8 13 SWAA073836 1 20070801 A 5311 6546595 FRAME BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300078 20070813 00078 NM 2007 8 13 SWAA073867 1 20070801 A 5330 6546768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 344, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007081300082 20070813 00082 NM 2007 8 13 SWAA073848 1 20070801 A 2560 6557463 FITTING BOEING 737 7373Q8 1384670 NM R1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007081300084 20070813 00084 NM 2007 8 13 SWAA073850 1 20070801 A 2560 6557463 FITTING BOEING 737 7373Q8 1384670 NM L1 DOOR GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FIT TING PER SRM. 2 L 7 2 4F RT A16WE 2007081300085 20070813 00085 NM 2007 8 13 SWAA073851 1 20070801 A 2560 6557463 FITTING BOEING 737 7373Q8 1384670 NM L1 DOOR GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FIT TING PER SRM. 2 L 7 2 4F RT A16WE 2007081300092 20070813 00092 NM 2007 8 13 SWAA073855 1 20070801 A 3350 MS155721 LIGHT BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007081300094 20070813 00094 NM 2007 8 13 SWAA073897 1 20070802 A 5315 6545410145 FLOORBEAM BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED BETWEEN BS 664 AND BS 660, RBL 1. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300095 20070813 00095 NM 2007 8 13 SWAA073898 1 20070802 A 5712 6545445 RIB BOEING 737 7373K2 13844BA NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING LOWER RIB CHORD CRACKED AT STA 135.5. REPAIRED CHORD PER ACO. 2 L 7 2 4F RT A16WE 2007081300096 20070813 00096 NM 2007 8 13 SWAA073879 1 20070802 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 582, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300098 20070813 00098 NM 2007 8 13 SWAA073893 1 20070802 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 28R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007081300101 20070813 00101 NM 2007 8 13 SWAA073894 1 20070802 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300102 20070813 00102 NM 2007 8 13 SWAA073902 1 20070802 A 5230 6547953 CHANNEL BOEING 737 7373G7 1384595 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR FRAME UPPER U-CHANNEL CRACKED. REMOVED AND REPLACED U-CHANNEL PER SRM. 2 L 7 2 4F RT A16WE 2007081300111 20070813 00111 NM 2007 8 13 SWAA073887 1 20070802 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300113 20070813 00113 NM 2007 8 13 SWAA073890 1 20070802 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300115 20070813 00115 NM 2007 8 13 SWAA073880 1 20070802 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 380, STR 13R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007081300116 20070813 00116 NM 2007 8 13 SWAA073881 1 20070802 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER 8R CRACKED AT BS 500C. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007081300120 20070813 00120 EA 2007 8 13 COMA0760504 1 20070730 A 3350 60206 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 597SW 7293 FLIGHT 5460 - LOWER GREEN EMERGENCY EXIT LIGHT BY MAIN PAX DOOR INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. 2 L 7 2 4F RT A21EA 2007081300125 20070813 00125 NM 2007 8 13 SWAA073915 1 20070805 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 464WN 32468 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007081300126 20070813 00126 NM 2007 8 13 SWAA073913 1 20070804 A 3350 417A5701 COVER BOEING 737 737705 13844SC NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 270WN 29089 DURING SCHEDULED MV1 CHECK, FOUND EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007081300127 20070813 00127 2007 8 13 SWAA073903 4 20070803 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 480WN 33998 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007081300130 20070813 00130 NM 2007 8 13 SWAA073907 1 20070803 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 14L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300131 20070813 00131 NM 2007 8 13 SWAA073908 1 20070803 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 791, STR 14R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300133 20070813 00133 NM 2007 8 13 SWAA073909 1 20070803 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 490, STR 28R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300134 20070813 00134 NM 2007 8 13 SWAA073917 1 20070805 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007081300137 20070813 00137 NM 2007 8 13 SWAA073905 1 20070803 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300139 20070813 00139 NM 2007 8 13 SWAA073906 1 20070803 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 420, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007081300140 20070813 00140 NM 2007 8 13 SWAA073914 1 20070804 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 725SW 27857 DURING SCHEDULED MV2 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007081300142 20070813 00142 NM 2007 8 13 SWAA073924 1 20070806 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 784SW 29810 R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007081300146 20070813 00146 2007 8 13 SWAA073928 4 20070806 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 770SA 30589 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007081300147 20070813 00147 2007 8 13 SWAA073923 4 20070806 A 2565 63562101 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR UNWANTED DEPLOY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 729SW 27861 R2 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007081300149 20070813 00149 NM 2007 8 13 SWAA073930 1 20070806 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 967, BL 0. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300153 20070813 00153 NM 2007 8 13 SWAA073931 1 20070807 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 205WN 34010 DURING SCHEDULED MV1 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007081300155 20070813 00155 NM 2007 8 13 SWAA073932 1 20070807 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 228WN 32496 EEPLS COVER LOOSE AT ROW 5 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007081300156 20070813 00156 NM 2007 8 13 SWAA073936 1 20070807 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007081300158 20070813 00158 NM 2007 8 13 SWAA073940 1 20070807 A 2761 6573730 ACTUATOR BOEING 737 7373H4 1384600 NM NR 4 SPOILER LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED HC2 CHECK, FOUND LEFT WING NR 4 SPOILER INBOARD ACTUATOR CASTING LOOSE. REMOVED AND REPLACED ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2007081300160 20070813 00160 NM 2007 8 13 SWAA073933 1 20070807 A 3350 65C27093 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 246LV 32507 R1 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007081300162 20070813 00162 2007 8 13 SWAA073939 4 20070807 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007081300164 20070813 00164 NM 2007 8 13 SWAA073938 1 20070807 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2007081300168 20070813 00168 NM 2007 8 13 SWAA073946 1 20070808 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 24R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007081300171 20070813 00171 EU 2007 8 13 SWAA073943 2 20070808 A 7200 CFM567B24622 ENGINE BOEING 737 7377H4 1384404 NM CFMINT CFM56 CFM563B2 13802 EU NR 2 MAKING METAL A SWAA E ENGINE SHUTDOWN E K VIBRATION/BUFFET FLUID LOSS NR NOT REPORTED 1 SW 29 706SW 27840 892214 INFLIGHT SHTDOWN / DIVERSION / DECLARED EMERGENCY. VIBRATION NR 2 ENGINE FOLLOWED BY LOSS OF OIL QUANTITY AND PRESSURE. INSPECTED CHIP DETECTORS, FOUND FOD IN MIDDLE DETECTOR. REMOVED AND REPLACED NR 2 ENGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081300173 20070813 00173 2007 8 13 SWAA073945 4 20070808 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 R1 DOOR SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007081300174 20070813 00174 2007 8 13 ZZDA2007251 4 20070731 A 3160 DISPLAY BOEING 717 717200 1383700 NM COCKPIT MALFUNCTIONED A ZZDA B EMER. DESCENT G MULTIPLE FAILURE CL CLIMB 1 SO 37 987AT 55088 AFTER TAKEOFF AIRCRAFT NAVIGATION SYSTEMS WERE UNRELIABLE. COULD NOT INPUT ANY DATA ON MCDU, AUTOPILOT AND THROTTLES WO ULD NOT ENGAGE. NO NAVIGATION. REBOOTED AIRCRAFT PWR, PERFORMED RTS ON FCC 1 & 2, GPC, MMR 1 & 2, DME 1 & 2, VIA 1 & 2, VOR 1 & 2, ALL CHECKS GOOD REF'S 22-00, 34-35, 34-35, 34-52, 31-43, 34-32. 2 L 7 2 4F TR A6WE 2007081300176 20070813 00176 NM 2007 8 13 UPS07550359 1 20070719 A 5330 70750050B SKIN BOEING 757 75724APF 1384969 NM FUSELAGE BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 401UP 23723 INSPECTION TYPE:C EXT LOWER FUSELAGE SKIN BULGING AT BS 600 BETWEEN S27L-S28R. REMOVED SHEAR TIES AT STA 600 STR 28R TO 27L IAW SRM 53-00-01-2R-9. REMOVED WEBS BETWEEN STA 600-580 BETWEEN STR 28L-28R IAW SRM 51-40-02. HFEC INSPECTED SKIN , SHEAR TIES & FRAMES PER NTM 51-00-01 PT 6, NO DEFECTS NOTED. FABRICATED FILLER IAW SRM 53-00-01-2R. 2 L 7 2 4F RT A2NM 2007081300177 20070813 00177 NM 2007 8 13 UPS07550360 1 20070719 A 5330 70750050B SKIN BOEING 757 75724APF 1384969 NM FUSELAGE BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 401UP 23723 INSPECTION TYPE:C EXT LOWER FUSELAGE SKIN BULGING AT BS 580 BETWEEN S27L-S28R. REMOVED SHEAR TIES AT STA 580 STR 28R TO 27L IAW SRM 53-00-01-2R-10. CUT FWD END OF INTERCOSTAL IAW SRM 53-00-01 2R N. HFEC INSPECTED BULGING AREA PER NTM 51- 00-01 PT.6, NO DEFECTS NOTED. FABRICATED FILLERS IAW SRM 53-00-01-2R N. 2 L 7 2 4F RT A2NM 2007080900197 20070809 00197 NM 2007 8 9 07FDEA02679 1 20070731 A 5347 AFA7789552 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 FORWARD CABIN , FOUND CARGO SEAT TRACK AT STA 500 RBL 62" WORN. 2 L 7 3 4F RT A22WE 2007081000005 20070810 00005 EU 2007 8 10 07FDEA02688 1 20070731 A 5315 LN9497A420 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 T-CAP CORRODED FR35 AT RBL 56 TO 62 FWD PIT REMOVED AND REPLACED T-CAP PER A310-200 SRM 51-40-21 PARAGRAGH 7 AND 53-10-1 5, PAGE 241 AND 242. 2 L 7 2 4F RT A35EU 2007081000010 20070810 00010 NM 2007 8 10 AWXA200700927 1 20070722 A 5321 D5367180500400 FLOOR PANEL AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 834AW 2302 SAL - MAJOR REPAIR - BC-2 CHECK - NR 5979393, CORROSION ON CABIN FLOORBOARD 261FF, BS 2786/FR 66 TO BS 2884/FR 68, +Y129 2 TO +Y1732. REPLACED CABIN FLOORBOARD 261FF, BS 2786/FR 66 TO BS 2884/FR 68, +Y1292 TO +Y1732 IAW AWA TASK CARD C1C533 03. 2 L 7 2 4F RT A28NM 2007081000018 20070810 00018 2007 8 10 AALA20071309 4 20070716 A 2565 SLIDE BOEING 777 777223 1385213 NM R2 DOOR DISENGAGED A AALA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 778AN 29587 RDU - EMERGENCY SLIDE AT RIGHT NUMBER TWO DOOR FELL OFF DOOR AND FELL SIX INCHES ONTO CATERING TRUCK. CATERING TRUCK PR EVENTED SLIDE FROM DEPLOYING. REPLACED EMERGENCY SLIDE AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATIO N. 2 L 7 2 4F RT T00001SE 2007081000026 20070810 00026 NM 2007 8 10 AALA20071305 1 20070714 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 608AA 27446 DFW - EMERGENCY LIGHT AT SEAT 28D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081000032 20070810 00032 WP 2007 8 10 NWAA072689936 1 20070727 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1799U 47370 DURING "H" CHECK, FOUND CORROSION ON AFT CORNER OF FORWARD CARGO DOOR LOWER CUTOUT SKIN. REPAIRED PER EA 99-209907. 2 L 7 2 4F A6WE 2007081000042 20070810 00042 CE 2007 8 10 DXTA200702368 1 20070730 A 5280 BOLT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG DOOR LATCH LOOSE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 923QS 7500023 ON CLIMBOUT AT APPROXIMATELY 1000 FT MSL, A LOUD POP WAS HEARD FROM THE RT NOSE AREA OF THE AIRCRAFT, ACCOMPANIED BY THE AMBER CAS MSG (NOSE DOOR OPEN - R). CHECKLIST WAS DONE AND AN UNEVENTFUL NORMAL LANDING WAS MADE. ON POST FLIGHT, FOUN D THAT THE RT NOSE DOOR REAR LATCH HAD POPPED. LATCH WAS RESET AND FOUND TO OPEN AGAIN AT THE SLIGHTEST TOUCH. INSPEC TED LATCH AND DOOR FOUND NO DAMAGE. CLEANED GROOVE ON LATCH AND ADJUSTED T-BOLT 1/2 TURN IN TIGHTEN DIRECTION. LATCH N OW REMAINS ENGAGED PROPERLY AND DOOR GAP TO SKIN IS OK. FWD LATCH OK. REF CE750 MM 52-40-01 FOR WORK PERFORMED. ANNUN CIATOR OP'S CHECKS OK ALSO. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007081000046 20070810 00046 NM 2007 8 10 CALA0700384 1 20070730 A 5320 65C80736156 CHANNEL BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE BS 727D CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND AFT BAGGAGE BIN FLOOR CHANNEL CORRODED AT STA 727D + 8 INCHES, RBL 3. REPAIRED IAW SRM 53-00-53. 2 L 7 2 4F 4 F RT A16WE E2GL 2007081000048 20070810 00048 NM 2007 8 10 CALA0700386 1 20070730 A 5320 147A8540U8 STRUCTURE BOEING 737 737824 13844BZ NM CFMINT CFM56 CFM567B26US NE BS 807-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 36207 30579 INSPECTION FOUND A CHORD CORRODED AT R-2 DOOR STA 807-1016, RBL 56. THE CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007081000059 20070810 00059 CE 2007 8 10 GLBA20060966 1 20070720 A 5712 RIB BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT WING CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 201GL UE201 LT WING RIB OB OF POWER PACK CRACKED AT (L) BRACKET APPROX. 1 INCH BY 1 INCH IN LENGTH ORIGINATING FROM RIVET HEAD. MAI NTENANCE REPAIRED THE LT WING RIB OB OF HYDRAULIC POWER PACK ONE INCH CRACK AT W.S. 79.65 IAW SRM 51-70. REPAIR DIMENSIO N 4 INCH BY 2.7500 INCH. MATERIAL 2024 T-3 .063 INCH. 2 L 7 2 4T 4 T RT A24CE E26NE 2007081000065 20070810 00065 EA 2007 8 10 A6WA200740357 1 20070624 A 2731 DL2428M4 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT PITCH LINEAR INOPERATIVE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 457AW 9041 7854 ELEVATOR STIFF DURING FLIGHT CONTROL CHECK. REMOVED AND REPLACED PITCH FEEL LINEAR ACTUATOR NR 2, DUE LOW INPUT IMPEDAN CE. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007081000069 20070810 00069 EA 2007 8 10 A6WA200740363 1 20070709 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 409AW 7447 LT WING PLANK ACCESS HOLE NR 1, (540BB) WS 54.897 HAS PITTING ON IB END ON NON CRITICAL AREA APPROX .002 INCH DEEP, AND ALONG AFT EDGE IN CRITICAL AREA APPROX .005 INCH DEEP. (K) MAINTENANCE REMOVED MINOR PITTING, NDT, ROTO PEENED AND PR OTECTIVE TREAT NR 1 ACCESS HOLE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007081000072 20070810 00072 NM 2007 8 10 ZZDA2007252 1 20070727 A 3350 LIGHT BOEING 737 73776N 13844CH NM CABIN MALFUNCTIONED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 176AT 32654 LT SIDE EMERGENCY LIGHTS ON. RESET CIRCUIT BREAKER A-10 AFT EMERGENCY LIGHTS--ALL OPS CHECK OK CYCLED SWITCH TO OPS CHE CK AGAIN. OK FOR SERVICE IAW MM 33-50. 2 L 7 2 4F RT A16WE 2007081000082 20070810 00082 SO 2007 8 10 C2XA07CL064 1 20070731 A 3097 102AU1AF SENSOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL COCKPIT SHORTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 15973 145159 FLIGHT NR 2666 THE CREW REPORTED A TAT 1 HEAT INOP MESSAGE ON THE EICAS WITH A FAINT ELECTRICAL BURNING ODOR THAT LASTED FOR 1 TO 2 MINUTES.MAINTENANCE INSPECTED AND REPLACED THE NR 1 TAT CURRENT SENSOR KO064. OPERATIONAL CHECKS OF THE SYST EM WERE GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007081000093 20070810 00093 NM 2007 8 10 UPS07550357 1 20070722 A 5532 112N70075 SKIN BOEING 757 75724APF 1384969 NM PWA 2037 PW2040 NE VERTICAL STAB GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 401UP 23723 INSPECTION TYPE: C VERT STAB. UPPER MOST AFT PANEL SKIN GOUGED AS SEEN THRU PANEL 324EL. ACCOMPLISHED REPAIR AT VERT. S TAB IAW EA NR 757-5530-27-A1720 AND UPS EO NR 57-55-20030. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081300008 20070813 00008 NM 2007 8 13 SWAA073781 1 20070731 A 5311 6546549 FRAME BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300010 20070813 00010 NM 2007 8 13 SWAA073828 1 20070731 A 5311 6546551 FRAME BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300012 20070813 00012 NM 2007 8 13 SWAA073797 1 20070731 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300016 20070813 00016 NM 2007 8 13 SWAA073829 1 20070731 A 5311 6546554 FRAME BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300023 20070813 00023 NM 2007 8 13 SWAA073820 1 20070731 A 5311 6546558 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300030 20070813 00030 NM 2007 8 13 SWAA073808 1 20070731 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300032 20070813 00032 NM 2007 8 13 SWAA073811 1 20070731 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300047 20070813 00047 NM 2007 8 13 SWAA073822 1 20070731 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 703SW 27837 DURING SCHEDULED HC1 CHECK, FWD LT EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007081300053 20070813 00053 NM 2007 8 13 SWAA073837 1 20070801 A 3350 311500 LENS BOEING 737 7373K2 13844BA NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 20Y CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 16 ABC. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007081300068 20070813 00068 NM 2007 8 13 SWAA073858 1 20070801 A 5322 6546546 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007081300079 20070813 00079 NM 2007 8 13 SWAA073839 1 20070801 A 5230 6547953 SKIN BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT FWD LOWER END. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007081300080 20070813 00080 NM 2007 8 13 SWAA073856 1 20070801 A 5310 6547959 DOOR FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007081300083 20070813 00083 NM 2007 8 13 SWAA073849 1 20070801 A 2560 6557463 FITTING BOEING 737 7373Q8 1384670 NM R1 DOOR GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FIT TING PER SRM. 2 L 7 2 4F RT A16WE 2007081300086 20070813 00086 NM 2007 8 13 SWAA073865 1 20070801 A 5314 6562125 KEELBEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND KEEL BEAM CORRODED BETWEEN BS 727 AND BS 727A, RBL 7 AND LBL 17. REPAIRED KEEL BEAM PER ER. 2 L 7 2 4F RT A16WE 2007081300087 20070813 00087 NM 2007 8 13 SWAA073870 1 20070801 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007081300088 20070813 00088 NM 2007 8 13 SWAA073871 1 20070801 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007081300090 20070813 00090 NM 2007 8 13 SWAA073872 1 20070801 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER 26R CORRODED AT BS 360. REMOVED AND REPLACED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007081300104 20070813 00104 NM 2007 8 13 SWAA073899 1 20070802 A 5310 65479737 CREASE BEAM BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 574, STR 17L. REMOVED AND REPLACED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300105 20070813 00105 NM 2007 8 13 SWAA073882 1 20070802 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300112 20070813 00112 NM 2007 8 13 SWAA073888 1 20070802 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300121 20070813 00121 EA 2007 8 13 COMA0760505 1 20070731 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 931CA 7037 FLIGHT 5120 - FLAPS FAIL AT 0 DEGREES IN CRUISE FLIGHT. AIRCRAFT LANDED SAFELY IN JFK. COMPLIED WITH AD 2006-12-21 FLA P CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURT HER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007081300129 20070813 00129 NM 2007 8 13 SWAA073918 1 20070805 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 521, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300135 20070813 00135 NM 2007 8 13 SWAA073911 1 20070803 A 5311 65C22909 FRAME BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 22L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007081300138 20070813 00138 NM 2007 8 13 SWAA073904 1 20070803 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727, STR 24L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300144 20070813 00144 NM 2007 8 13 SWAA073926 1 20070806 A 3350 20121A CHARGER BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED MV4 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 19 DEF. REMOVED AND REPLACED BATTERY CHARG ER PER MM. 2 L 7 2 4F RT A16WE 2007081300151 20070813 00151 NM 2007 8 13 SWAA073921 1 20070803 A 2913 887477 PUMP BOEING 737 7377H4 1384404 NM HHYDRAULIC SYS LEAKING A SWAA A UNSCHED LANDING K FLUID LOSS NR NOT REPORTED 1 SW 29 757LV 29850 DIVERSION - HYDRAULIC -A- SYSTEM LEAKED TO ZERO. REMOVED AND REPLACED HYDRAULIC ELECTRIC PUMP PER MM. 2 L 7 2 4F RT A16WE 2007081300154 20070813 00154 NM 2007 8 13 SWAA073934 1 20070807 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 441WN 29837 EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007081300157 20070813 00157 NM 2007 8 13 SWAA073937 1 20070807 A 5311 6546543 FRAME BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300169 20070813 00169 NM 2007 8 13 SWAA073949 1 20070808 A 5340 65C27314 STRINGER CLIP BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300178 20070813 00178 WP 2007 8 13 UPS07850336 1 20070728 A 2910 CONTROL VALVE DOUG DC8 DC871F 302199D WP HYDRAULIC SYS LEAKING A IPXA O OTHER K FLUID LOSS AP APPROACH 1 SO 01 701UP 45938 INSPECTION TYPE:N/A DURING DESCENT INTO SDF THE CREW RECEIVED AN AILERON LIGHT MESSAGE & BEGAN LOSING HYDRAULIC FLUID. THE CREW LATER DECLARED AN EMERGENCY. REMOVED AND REPLACED WING SLOT CONTROL VALVE WHILE RIGHT MANIFOLD WAS REMOVED IN REF TO AMM 27-80-04-2. 2 L 7 4 4F RT 4A25 2007081300179 20070813 00179 WP 2007 8 13 UPS07850350 1 20070724 A 3350 BATTERY DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST NR NOT REPORTED 1 SO 01 819UP 46019 INSPECTION TYPE:N/A ON PREFLIGHT AIRCRAFT FAILED EMERGENCY EXIT LIGHTS CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING B ATTERY & RELAY PACK IAW DC8 MM 33-50-1-2. OPS CHECKS NORMAL. 2 L 7 4 4F RT 4A25 2007081300182 20070813 00182 WP 2007 8 13 UPS07850363 1 20070731 A 5320 STRUCTURE DOUG DC8 DC873F 302199F WP CARGO BAY TORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 APPROX 1 INCH TEAR IN FLOOR OF PIT 33 APPROX 24 INCHES A/C LEFT OF CENTER & APPROX 36 INCHES FROM AFT BULKHEAD. C/W UPS EO DC8-5320-8724 APPROX A. D355594 ISSUED BY AMC. REPAIRED PIT 33 FLOOR PER EO DC8-5320-8724. PERMANENT REPAIR INSTALL ED. D355594 CLEARED. 2 L 7 4 4F RT 4A25 2007081300183 20070813 00183 NM 2007 8 13 UPS07M50348 1 20070702 A 5720 STRUCTURE DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C RIGHT WING - WING T/E INBOARD ISLANDS UPPER SURFACE FOUND CRACK ON FWD SIDE APPROX AT XORS 455 AS MARK ED. HFEC INSP C/O DAC NDTSPM REV13 06-10-01.001 & FOUND CRACK OF .375 INCH. FASTENERS AT AFFECTED AREA REMOVED FOR ACC ESS SRM 51-31-01VII R38. CRACKED AT TRIM OUT SRM 57-10-00 FIG 34 VI R38. HFEC INSP C/O DAC NDTSPM R13 06-10- 01.001 ON TRIM OUT AREA. NO CRACK FOUND. NEW FILLER & DOUBLER FAB. NEW FILLER & DOUBLER INSTALLED SRM 51-35-01VII R38 & SRM 51 -33-01VII R38. 2 L 7 3 4F RT A22WE 2007081300184 20070813 00184 NM 2007 8 13 UPS07M50349 1 20070716 A 5720 STRUCTURE DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C RIGHT WING - WING T/E INBOARD ISLANDS UPPER SURFACE FOUND CRACK ON FWD SIDE APPROX AT XORS 444 AS MARK ED. HFEC INSP C/O DAC NDTSPM R13P6 06-10-01.001 & 05 EA CRACKS END CON- FIRMED. FASTENERS AT AFFECTED AREA REMOVED FOR ACCESS SRM 51-31-01VII R38. CRACKED AREA TRIM OUT SRM 57-10-00 FIG 34 VI R38. HFEC INSP C/O DAC NDTSPM R13 06-10-01.0 01 ON TRIM OUT AREA. NO CRACK EVIDENT. NEW FILLER & DOUBLER FAB & INSTALLED. 2 L 7 3 4F RT A22WE 2007081300185 20070813 00185 NM 2007 8 13 UPS07M50353 1 20070703 A 5753 SKIN DOUG MD11 MD11F 3023600 NM T/E FLAP DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C LEFT I/B FLAP LOWER SURFACE FOUND WITH SEVERAL DENTS AT 64 INCHES FROM I/B END AS MARKED. LEFT WING I /B FLAP LOWER I/B SEGMENT LOWER SKIN REMOVED SRM 51-35-01VII R38. NEW SKIN FAB BOEING DWG ARC2736, USE MATL 2024T3-0.04 0". HOLES PICK UP PER SRM 51-31-01VII R38 & REPROTECTED PER SRM 51-21-01 VII R38. NEW SKIN PAINTED PER SRM 51-21-01 VI I R38 & INSTALLED PER SRM 51-35-01 VII R38. 2 L 7 3 4F RT A22WE 2007081300188 20070813 00188 NM 2007 8 13 ZZDA2007255 1 20070731 A 5330 SKIN BOEING 737 7377BD 1384511 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 166AT 33917 FELL FROM JACKS RESULTING IN DAMAGE TO THE FUSELAGE FROM FS 1072-1088. THE FUSELAGE SKIN WAS PUNCTURED IN THE AREA. FA BRICATED REPAIR PARTS AND INSTALLED PER AIRTRAN EA 37-53-00614IR. 2 L 7 2 4F RT A16WE 2007081300190 20070813 00190 NM 2007 8 13 UPS07M50354 1 20070703 A 5753 SKIN DOUG MD11 MD11F 3023600 NM T/E FLAP DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C LEFT I/B FLAP LOWER SURFACE FOUND WITH SEVERAL SMALL DENTS AT 63 INCHES FROM O/B END AS MARKED. LEFT WING I/B FLAP LWR O/B SEGMENT LWR SKIN REMOVED PER SRM 51-35-01VII R38. NEW SKIN FAB PER BOEING DWG ARC2443, USE MATL 2024T3-0.040". HOLES PICK UP ON NEW SKIN PER SRM 51-31-01 VII R38. REPROTECTED & PAINTED PER SRM 51-21-01VII R38V. FAB NEW SKIN INSTALLED PER SRM 51-35-01VII R38. 2 L 7 3 4F RT A22WE 2007081300195 20070813 00195 NM 2007 8 13 NOCA14607 1 20070802 A 3350 IN68 INVERTER BOEING 767 767324 1385203 NM CABIN MALFUNCTIONED A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 767NA 27569 CROSS AISLE EMERGENCY EXIT LIGHTS ARE INOP AT DOORS L1-R1. REPLACED STATIC INVERTER PER WD 33-51-18 2 L 7 2 4F RT A1NM 2007081300198 20070813 00198 NM 2007 8 13 ABXA070252 1 20070727 A 2612 7350 FIRE LOOP BOEING 767 767232 1385132 NM RT ENGINE DEFECTIVE A ABXA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 23 747AX 22224 RIGHT ENGINE FIRE WARNING ALERT IN FLIGHT, EICAS MESSAGE: FIRE RIGHT ENGINE. STATUS PAGE: RIGHT ENGINE FIRE LOOP 1 A ND 2. SECURED RIGHT ENGINE, NO FIRE BOTTLES USED. AIR TURNBACK TO MIA. REMOVED AND REPLACED RIGHT ENGINE LOWER AFT FI RE DETECTION LOOP IAW B767 MM 26-11-02. BITE AND RUN UP TEST NORMAL. 2 L 7 2 4F RT A1NM 2007081300199 20070813 00199 NM 2007 8 13 KCSA071272 1 20070802 A 5330 SKIN BOEING 747 7472B4B 138481B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 EXTERNAL FUSELAGE SKIN HAS NUMEROUS AREAS WITH DAMAGE AT STA 688, STR 41R TO 42R. 2 L 7 4 4F RT A20WE 2007081400003 20070814 00003 2007 8 14 F3LA200700188 4 20070730 A 2565 PLATE AIRBUS A318 A318111 3940019 EU GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 803FR 5201 2017 DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR FWD AND AFT GIRT BAR FITTING BLANKING PLATES CORRODED. REPLACED BLANKING PLATES IAW A318 SRM 51-42-11 AND AMM 52-13-31-400-007. 2 L 7 2 4F RT 2007081400004 20070814 00004 EU 2007 8 14 07FDEA02695 1 20070706 A 5330 A53973276206 SKIN AIRBUS 310 A310222 3930315 EU ZONE 100 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 FUSELAGE, MISSING MATERIAL AT AFT CARGO COMPARTMENT DOOR LOWER FORWARD FRAME SKIN SURFACE AT FRAME 59A AND BETWEEN STR 4 1 AND 43 RT. IT WAS REPAIRED IN ACCORDANCE WITH SRM 53-17-12 AND EA 6-5310-112433. 2 L 7 2 4F RT A35EU 2007081400005 20070814 00005 EU 2007 8 14 07FDEA02697 1 20070709 A 5330 A53610091201 SKIN AIRBUS 310 A310222 3930315 EU ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 420FE 339 UPPER FUSELAGE: PREVIOUS REPAIR FOUND LOCATED ON CENTER LINE, FR 1/2 UPPER CL. REPAIR REQUIRES EVALUATION FOR MAJOR/MIN OR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO A N SRM REPAIR. NEW REPAIR ACCOMPLISHED IAW FEDEX EA NR 6-5330-112436 AND SRM 53-11-12 FIG 201. 2 L 7 2 4F RT A35EU 2007081400006 20070814 00006 SO 2007 8 14 SIMA200721401 1 20070730 A 3250 3085701007 MANIFOLD EMB 145 EMB145LR 3260212 SO ZONE 700 FAILED A SIMA O OTHER O OTHER LD LANDING 1 SW 21 908AE 6200 14500897 UNABLE TO STEER AIRCRAFT AFTER LANDING, AIRCRAFT VEERED STRIKING RUNWAY INFORMATION SIGN. REMOVED AND REPLACED NOSE STR UT ASSEMBLY AND NOSE WHEEL STEERING MANIFOLD IAW EMB AMM 32-20-01 AND 32-50-04. OPERATIONAL CHECK GOOD - AIRCRAFT RETURN ED TO SERVICE 2 L 7 2 4T RT T00011AT 2007081400007 20070814 00007 WP 2007 8 14 NWAA072679925 1 20070719 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1004 S28-28RL CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 925US 47472 DURING "H" CHECK, FOUND CRACKS IN APU FORWARD FRAME AT BS 1004 BETWEEN L28L-L29L AND L28R-L29R. REPAIRED PER EA 99-2101 63. 2 L 7 2 4F A6WE 2007081400008 20070814 00008 NM 2007 8 14 NWAA072705503 1 20070718 A 5310 CREASE BEAM BOEING 757 757251 1384970 NM CORRODED CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 503US 23192 DURING "M" CHECK, FOUND CORROSION ON RT CREASE BEAM INNER CHORD FROM BS 760 TO 780 RBL 64. REPAIRED PER EA 55-209992. 2 L 7 2 4F RT A2NM 2007081400009 20070814 00009 NM 2007 8 14 NWAA072715503 1 20070720 A 5414 SKIN BOEING 757 757251 1384970 NM NR 2 NACELLE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 503US 23192 DURING "M" CHECK, FOUND CRACK IN NR 2 PYLON SKIN PANEL AT NAC STATION 128. REPAIRED PER EA 55-194182. 2 L 7 2 4F RT A2NM 2007081400010 20070814 00010 NM 2007 8 14 NWAA072695503 1 20070717 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM BS 1717 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 503US 23192 DURING "M" CHECK, FOUND CORROSION ON AFT DECK PLATE SUB FLOOR STRUCTURE AT BS 1717 LBL 60 TO RBL 60. REPAIRED PER EA 55 -194183. 2 L 7 2 4F RT A2NM 2007081400011 20070814 00011 EU 2007 8 14 07FDEA02690 1 20070801 A 5330 A53978233200 SKIN AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORROSION FOUND ON EXTERNAL STRAP (P/N: A539-78233-200) NEAR C69 AND P'47, RT. REPAIR PERFORMED BY BLEND OUT CORROSION, REMAINING THICKNESS OUT OF LIMIT, APPROVED BY RAS/DAHAM/4022567/2007 ISSUE "A" AND EA 6-5317-112473. 2 L 7 2 4F RT A35EU 2007081400012 20070814 00012 EU 2007 8 14 07FDEA02691 1 20070801 A 5320 SEE4A WEB AIRBUS 300 A300B4605R 3930308 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 SEVERAL CRACKED WEBS FOUND BETWEEN TRACKS 1-2 AND 3-4 LT/RT AT C47. WEB P/N: A538-32100 A538-32103. REPAIR PERFORMED B Y DRILLING CRACK STOP HOLES AND INSTALLING DOUBLERS IAW RAS 053425/005/2007, ISSUE "A" AND EA 6-5315-112499. 2 L 7 2 4F RT A35EU 2007081400013 20070814 00013 EU 2007 8 14 07FDEA02692 1 20070801 A 5320 A25572172202 ANGLE AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORRODED PROFILE ANGLE FOUND BETWEEN C63-67, RT. REPAIR PERFORMED BY BLEND OUT, REMAINING THICKNESS WAS OUT OF LIMIT AN D PART IS REPLACED. 2 L 7 2 4F RT A35EU 2007081400014 20070814 00014 EU 2007 8 14 07FDEA02693 1 20070801 A 5320 SEE4A WEB AIRBUS 300 A300B4605R 3930308 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 SEVERAL CRACKS FOUND ON WEBS, TRACK 1-2 AND 3-4 LT/RT AT C47. WEB P/N, A538-32100 AND A538-32103 REPAIR PERFORMED BY DR ILLING CRACK STOP HOLES AND INSTALLING REPAIR DOUBLERS IAW RAS 052969/004/2007 ISSUE "A" AND E 6-5315-106499. 2 L 7 2 4F RT A35EU 2007081400015 20070814 00015 NM 2007 8 14 07FDEA02694 1 20070801 A 5343 ACA7017502 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 NOSE LANDING GEAR RT TRUNNION FITTING CRACKED. [08-20-07] REPAIRED AS PER SRM 53- 40-00 FIGURE 23 VOLUME I. REPETITI VE INSPECTION REQUIRED FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS AS REQUIRED IN SRM 53-40-00 FIGURE 23 VO LUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007081400016 20070814 00016 EU 2007 8 14 07FDEA02696 1 20070710 A 5311 A53973004204 FRAME AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 AFT CARGO COMPARTMENT, CORROSION FOUND ON FR 59, BETWEEN STR 28 AND 30 RH. IT WAS REPAIRED IN ACCORDANCE WITH SRM 53-13- 13 FIG 202 AND FEDEX ENGINEERING AUTHORIZATION EA 6-5310-112435. 2 L 7 2 4F RT A35EU 2007081400017 20070814 00017 EU 2007 8 14 07FDEA02698 1 20070712 A 5347 A5381312720000 TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 DUMMY TRACK Y450 BETWEEN FR 54 AND FR 54.2 WITH CORROSION AND CRACK AT CARGO KIT ATTACHMENT AREA. IT WAS REPLACED IAW S RM 53-15-16. 2 L 7 2 4F RT A35EU 2007081400018 20070814 00018 EU 2007 8 14 07FDEA02699 1 20070712 A 5347 A5381312720000 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 DUMMY TRACK Y-450 BETWEEN FR 54 AND FR 54.2 WITH CORROSION AND CRACK AT CARGO KIT ATTACHMENT AREA. PART WAS REPLACED IN ACCORDANCE WITH SRM 53-15-16. 2 L 7 2 4F RT A35EU 2007081400019 20070814 00019 EU 2007 8 14 07FDEA02700 1 20070712 A 5347 A5381312720000 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 DUMMY-TRACK Y-953 BETWEEN FR 4 AND FR 54.2 WITH CORROSION AND CRACK AT KIT CARGO ATTACHMENT AREA. THE PART WAS REPLAC ED IN ACCORDANCE WITH SRM 53-15-16. 2 L 7 2 4F RT A35EU 2007081400020 20070814 00020 EU 2007 8 14 07FDEA02701 1 20070712 A 5347 A5381312720000 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 DUMMY-TRACK AT Y-1456 BETWEEN FR 54 AND FR 54.2 WITH CORROSION AND CRACK AT CARGO KIT ATTACHMENT. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 53-15-16. 2 L 7 2 4F RT A35EU 2007081400021 20070814 00021 SO 2007 8 14 SWIA200718537 1 20070726 A 5330 SKIN EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 223SW 120291 BELLY FUSELAGE SKIN IS CRACKED AND CORRODED BY FRAME 22. REPAIRED DAMAGED AREA PER EMB APPROVED REPAIR IC2007-120/00663 AND SRM 53-00-03. 2 L 7 2 4T RT A31SO 2007081400024 20070814 00024 EA 2007 8 14 SWIA200718540 1 20070723 A 3520 OXYGEN MASK CNDAIR CL600 CL6002C10 1390015 EA CABIN UNWANTED DEPLOY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 367CA 10069 PAX O2 MASK IN FORWARD LAV DEPLOYED. RESTOWED OXYGEN MASK IN FORWARD LAV. 2 L 7 2 4F RT A21EA 2007081500003 20070815 00003 WP 2007 8 15 ASAA0781921 1 20070730 A 5321 99365813 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 FLOOR PANEL TOP PLY DISBONDED. BOND REPAIRED PANEL WITH GLASS CLOTH PER SRM 51-90-0. 2 L 7 2 4F RT A6WE 2007081500006 20070815 00006 WP 2007 8 15 ASAA0781925 1 20070730 A 7620 S4913801AS86416 CABLE DOUG DC9 DC983 3022083 WP COCKPIT SEPARATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 949AS 53022 LEFTHAND ENGINE EMERGENCY SHUTDOWN HANDLE CABLE SEPARATED DURING EMERGENCY SHUTDOWN SYSTEM TEST. REPLACED CABLE, TESTED OK. 2 L 7 2 4F RT A6WE 2007081500007 20070815 00007 NM 2007 8 15 ASAA0741926 1 20070731 A 5512 657378354 SKIN BOEING 737 7374S3 1384711 NM HORIZ STAB DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 RIGHT HORIZONAL STAB DENT AT STA 212.3 TO 221.5. DENT IS 5" L X 2.2" W X .082 DEEP. RECHECKED DIMENSIONS. DENT IS NOW A ZONE 3 DENT. INSPECTED INTERNAL VISUAL INSPECTION OF DAMAGE AREA EVERY 400 FLT HRS OR LESS. IF CRACKS ARE FOUND OR D AMAGE BECOMES BIGGER REPAIR IMMEDIATELY. INSTALL A PERM REPAIR AFTER NO MORE THAN 5K FLT HRS OR 18 MONTHS WHICHEVER COM ES FIRST. 2 L 7 2 4F RT A16WE 2007081500008 20070815 00008 NM 2007 8 15 CALA0700389 1 20070621 A 5320 65528943 INTERCOSTAL BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14214 28774 INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL AT STA 540, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40 -2. 2 L 7 2 4F RT A16WE 2007081500011 20070815 00011 EA 2007 8 15 SWIA200718545 1 20070724 A 2701 BEARING CNDAIR CL600 CL6002C10 1390015 EA CONTROL COLUMN WORN A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 766SK 10232 FLT 5922 - AILERONS FEEL STIFF WHEN MOVED TO THE LEFT IN FLT. REPLACED LT CONTROL COLUMN SHAFT BEARING PER AMM CH 27-31 -01. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2007081500015 20070815 00015 2007 8 15 SIMA200721404 4 20070801 A 2200 SWITCH EMB 145 EMB145LR 3260212 SO AUTOPILOT PINCHED A SIMA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 905JH 14500892 PTRIM MAIN INOP MESSAGE FOLLOWED BY PTRIM BACKUP INOP MESSAGE. FOUND PILOTS AUTO PILOT/TRIM/PUSHER DISCONNECT SWITCH PI NCHED. REPOSITIONED WIRES. SYSTEM OPERATIONAL CHECK GOOD IAW EMB 27-11-00-700-803A AND AMM 27-40-00. AIRCRAFT RETURNE D TO SERVICE. 2 L 7 2 4T RT T00011AT 2007081500016 20070815 00016 SO 2007 8 15 SIMA200721403 1 20070731 A 3230 355022002 ELECTRONIC UNIT EMB 135 EMB135LR 3260305 SO MLG FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 734EK 3801 145371 RECEIVED LANDING GEAR AIR/GROUND EICAS MESSAGE, LANDING GEAR NO RETRACT, RETURNED TO BNA. REMOVED AND REPLACED LANDING GEAR ELECTRONIC CONTROL IAW EMB AMM. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007081500019 20070815 00019 NM 2007 8 15 DHL2007741520 1 20070801 A 5343 651767639 SUPPORT FITTING BOEING 727 7272Q9 138448M NM BS 304 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 LT NLG TRUNNION SUPPORT FITTING HAS CORROSION ON UPPER CAP SURFACE. REMOVED AND REPLACED LT NLG TRUNNION SUPPORT FITTIN G DUE TO CORROSION REMOVAL WOULD HAVE EXCEEDED BORE DIAMETER LIMITS. REMOVED AND REPLACED COMPLIED WITH PER B727 SRM 51 -330-5 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007081500020 20070815 00020 NM 2007 8 15 DHL2007741522 1 20070801 A 5320 FLOOR SUPPORT BOEING 727 7272Q9 138448M NM BS 950E-990 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AFT PIT, RT AT BS 950E TO 990, STR 27R, UPPER "T" CAP LOWER STRAP HAS CORROSION AROUND NUT PLATES. CORROSION REMOVAL EX CEEDED LIMITS PER B727 SRM 53-10-1 FIG 1. REMOVED UPPER "T" CAP SECTION, FABRICATED NEW SECTION FROM BAC1506-1946, 89" IN LENGTH, PO NR 7232139, PER B727 SRM 53-10-2 FIG 5, 51-20-1, AND 51-30-5. TREATED, PRIMED, AND INSTALLED "T" CAP SECT ION FROM BS 950E-990 PER B727 SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007081500021 20070815 00021 NM 2007 8 15 DHL2007741523 1 20070801 A 5343 BAC15201247 SUPPORT BOEING 727 7272Q9 138448M NM BS 910-943 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 CORROSION ON APU INLET SCREEN LWR FWD SUPPORT FRAME IN LMLG W/WELL, AT BS 910. REMOVED FRAME SECTION, FABRICATED NEW FR AME SECTION FROM BAC1520-1247 EXTRUSION, 33" IN LENGTH, PO NR 994061, PER B727 SRM 53-10-2 FIG 4 AND 51-20-1. TREATED, PRIMED, AND INSTALLED FRAME SECTION PER B727 SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007081500023 20070815 00023 NM 2007 8 15 DHL2007741525 1 20070731 A 5322 SHEAR TIE BOEING 727 7272Q9 138448M NM BS 990 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AFT PIT AT BS 990, BETWEEN STR 28L AND 29L, FRAME SHEAR TIE CRACKED/CORRODED, AND EXISTING REPAIR CUT-OUT IMPROPER. REM OVED CRACKED SHEAR TIE, FABRICATED NEW SHEAR TIE FROM 7075-T6, .071" BY 5.5" BY 2.25", PO NR 9004779, PER B727 SRM 53-10 -2 FIG 5 AND 53-10-4 FIG 11. TREATED, PRIMED, AND INSTALLED NEW SHEAR TIE PER B727 SRM 51-10-2 AND 53-10-4 FIG 11. TRI MMED OUT FRAME SECTION AT EXISTING REPAIR PER B727 SRM 51-10-1. 2 L 7 3 4F RT A3WE 2007081500024 20070815 00024 NE 2007 8 15 IXXA070036O 2 20070801 A 7320 71128721 FUEL CONTROL DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 1 ENGINE MALFUNCTIONED A IXXA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 SW 11 799AL 47744 4081 45922 671011 DURING CRUISE FROM WSAP TO RJTY NR 1 ENGINE LOST POWER EPR REDUCED 1.2 AND FUEL FLOW DECREASED 1000 POUNDS PER HOUR. TH E CREW PERFORMED THE ENGINE SHUTDOWN CHECKLIST AND SHUTDOWN THE ENGINE, THE AIRCRAFT LANDED AT RJTY WITHOUT INCIDENT. M AINTENANCE INSPECTED THE ENGINE AND USING PROPER TECHNICAL DATA, REPLACED THE FUEL CONTROL. THE OPERATIONAL CHECK WAS G OOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4 F 4A25 1E8 2007081500026 20070815 00026 2007 8 15 NWAA072736745 4 20070731 A 2565 SLIDE BOEING 747 747222B 1384904 NM DISLODGED A NWAA O OTHER O OTHER CL CLIMB 1 GL 01 646NW 23737 DURING TAKEOFF AT ROTATE UPPER DECK ESCAPE SLIDE MOVED AFT, ABOUT 12 TO 15 INCHES WITH THE LOCK LEVER IN THE LOCKED POSI TION. UNABLE TO MOVE ESCAPE SLIDE BACK INTO POSITION. FLIGHT CONTINUED ON AND LANDING WAS UNEVENTFUL. MAINTENANCE INS PECTED UPPERDECK ESCAPE SLIDE PACK BOARD RELEASE MECHANISM FOR OPERATION, IAW AMM 25-68-00. NO DEFECTS WERE NOTED, AND PACK BOARD LOCKS IN FWD AND AFT POSITION. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007081500028 20070815 00028 EA 2007 8 15 TRAX200701078 1 20070729 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA COCKPIT ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 707EV 10057 AFT CARGO DOOR INDICATES OPEN IN FLIGHT. AFT CARGO DOOR AMBER CAUTION MSG ILLUMINATED. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007081500029 20070815 00029 EA 2007 8 15 TRAX200701079 1 20070729 A 3260 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 936EV 8038 LEFT MLG DISAGREE. A/C RETURNED TO OMA AFTER T/O. EMERGENCY DECLARED. LANDING GEAR RETRACTION SYSTEM. 2 L 7 2 4F RT A21EA 2007081500031 20070815 00031 NM 2007 8 15 TSAA0736042 1 20070731 A 3610 69438854 DUCT BOEING 737 737230 1384401 NM APU FAILED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 821AL 23155 NON-ETOPS FLIGHT 40 HNL - ITO, AFTER LANDING IN ITO THE CREW STARTED THE APU AND HAD A WING TO BODY OVERHEAT INDICATION. THE APU WAS SHUT DOWN. MAINTENANCE FOUND THE APU BLEED AIR DUCT HAD RUPTURED CAUSING THE OVERHEAT AND ALSO CAUSING TH E APU FIRE EXTINGUISHER BOTTLE TO THERMAL DISCHARGE. THE APU WAS PLACED ON MEL AND THE AIRCRAFT RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THREE SECTIONS OF BLEED DUCT. MAINTENANCE ALSO REPLACED THE APU FI RE EXTINGUISHER BOTTLE PER AMM 26-22-11. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007081500034 20070815 00034 SO 2007 8 15 C2XA07ON015 1 20070730 A 2824 2770138101 FLAPPER VALVE EMB 145 EMB145LR 3260212 SO LT WING WORN A C2XA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 27 15555 145594 FLT 41 - GEG TO ONT - PASSENGER REPORTED STREAM OF FUEL COMING FROM LEFT WING. MX PERSONNEL INSPECTED THE LEFT WING FLA PPER VALVE LEAKING. MX REMOVED AND REPLACED LEFT WING FLAPPER VALVE AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. THE A/C WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007081500037 20070815 00037 NM 2007 8 15 NWAA07256313 1 20070801 A 2612 FIRE LOOP BOEING 747 747451 1384940 NM APU BAY MALFUNCTIONED A NWAA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 01 673US 30268 DURING FLIGHT HAD A FALSE EICAS, APU FIRE WARNING. NO OTHER INDICATIONS NOTICED. FLIGHT CONTINUED ON AND LANDING WAS U NEVENTFUL. MAINTENANCE REMOVED AND REPLACED BOTH A&B LOOP DETECTORS AND LUGS ON THE ACCESS DOOR. OPERATIONAL CHECKED G OOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007081500042 20070815 00042 NM 2007 8 15 AWXA200700939 1 20070717 A 5510 183N130317 WEB BOEING 757 757225 1384959 NM ZONE 300 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - NR 5956473, CORROSION ON LEFT HORIZONTAL STABILIZER TRAILING EDGE WEB, STABILIZER STAT ION 224. REPLACED LEFT HORIZONTAL STABILIZER TRAILING EDGE WEB, STABILIZER STATION 224 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007081500045 20070815 00045 NM 2007 8 15 AWXA200700942 1 20070705 A 5340 69353502 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961282, CRACKED STRINGER CLIP, BS 500A, S16L. REPLACED STRINGER CLIP, BS 500A, S1 6L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007081500048 20070815 00048 NM 2007 8 15 AWXA200700945 1 20070705 A 5340 69353506 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961296, CRACKED STRINGER CLIP, BS 500B, S16R. REPLACED STRINGER CLIP, BS 500B, S1 6R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007081500049 20070815 00049 NM 2007 8 15 AWXA200700946 1 20070705 A 5340 69353506 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961297, CRACKED STRINGER CLIP, BS 500A, S16R. REPLACED STRINGER CLIP,BS 500A, S16 R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007081500050 20070815 00050 NM 2007 8 15 AWXA200700947 1 20070705 A 5313 654988630 STRINGER BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961286, CRACKED STRINGER, BS 500D, S16L. REPAIRED STRINGER, BS 500D, S16L IAW AWA ER 03-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2007081500052 20070815 00052 NM 2007 8 15 AALA20071330 1 20070718 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 939AN 30883 DFW - EMERGENCY EXIT LIGHT AT SEAT ROW 22D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AND CONNECTOR FOR SEAT R OW 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007081500053 20070815 00053 WP 2007 8 15 AALA20071338 1 20070721 A 2170 COALESCER BAG DOUG DC9 DC982 3022082 WP AIR CONDITIONING DISCONNECTED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 283AA 49296 TUL INFLIGHT T2528/21JUL - DURING CLIMB FLIGHT ATTENDANT REPORTED ODOR AND SMOKE IN CABIN. RETURNED TO TUL AND LANDED W ITHOUT INCIDENT. FOUND RIGHT COALESCER BAG OFF AND STUCK TO BOTTOM OF DUCT. REPLACED BOTH COALESCER BAGS. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081500054 20070815 00054 NM 2007 8 15 AALA20071332 1 20070719 A 3397 WIRE BOEING 767 767323 1385205 NM EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 392AN 29429 MIA - SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT ROW 5H INOPERATIVE. REPAIRED BROKEN WIRE FOR SEAT MOUNTED EMERGENCY EXI T LIGHT AT SEAT ROW 5H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007081500055 20070815 00055 WP 2007 8 15 BSYA200700014 2 20070731 A 7261 TUBE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP OIL SYSTEM BENT E BSYA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 07 813AS 167 P74214 AIRCRAFT ON IT'S WAY FROM DAL TO LCK WHEN THE PILOT NOTICED THE OIL PRESSURE DROPPING, HE THEN ELECTED TO SHUT THE ENG D OWN AND DIVERTED INTO MEM. ENGINE SHOP FOUND OIL TUBES BENT AND GASKET BAD. REPLACED ALL TUBES AND ONE GASKET AT THE N 1 MONOPOLE. 2 L 7 2 4F 4 F A10CE E6WE 2007081500056 20070815 00056 NM 2007 8 15 KCSA071273 1 20070802 A 5313 STRINGER BOEING 747 7472B4B 138481B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STRINGER 27-L DAMAGED BETWEEN STA 500-520. 2 L 7 4 4F RT A20WE 2007081500057 20070815 00057 NM 2007 8 15 KCSA071274 1 20070802 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA 2280 TO 2290 LBL 36 SEAT TRACK HAS CORROSION WL 200. 2 L 7 4 4F RT A20WE 2007081500062 20070815 00062 EA 2007 8 15 TRAX200701063 1 20070726 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 873AS 7549 AFT PRESSURE BULKHEAD CRACKED AT LINTEL FITTING (MARKED). COMPLIED WITH EC/TC REO 601R-53-61-1230 JOB COMPLETE. SUPPLE MENTAL - SDR CLOSED 08/03/07. 2 L 7 2 4F RT A21EA 2007081500065 20070815 00065 NM 2007 8 15 AALA20071335 1 20070720 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 372AA 25199 SFO - EMERGENCY EXIT LIGHT AT LEFT OVERHEAD FORWARD GALLEY INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT LIGHT AT LEFT OVERHEAD FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007081500066 20070815 00066 NM 2007 8 15 AALA20071336 1 20070721 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 790AN 30251 MIA - EMERGENCY EXIT LIGHT AT SEAT ROW 22C INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT LIGHT AT SEAT ROW 22C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007081500069 20070815 00069 WP 2007 8 15 AALA20071325 1 20070718 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7544A 53026 LGA - EMERGENCY EXIT LIGHTS AT SEAT ROWS 21A AND 21F INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS AT SE AT ROWS 21A AND 21F. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081500070 20070815 00070 WP 2007 8 15 AALA20071326 1 20070718 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7544A 53026 LGA - EMERGENCY EXIT LIGHTS FROM SEAT ROWS 9B TO 11B INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY EXIT LIGHTS FROM SEAT ROWS 9B TO 11B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081500073 20070815 00073 NM 2007 8 15 AALA20071331 1 20070719 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 396AN 29603 DFW - EXTERNAL EMERGENCY EXIT LIGHTS AT RIGHT FUSELAGE INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY EXIT LIGHT AT RIGHT FUSELAGE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007081500076 20070815 00076 WP 2007 8 15 UPS07850345 1 20070718 A 5753 DOUBLER DOUG DC8 DC873F 302199F WP T/E FLAP PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 LEFT WING INBOARD FLAP STA 110 UPPER SURFACE SKIN DENT AND EXISTING DOUBLER PUNCTURED. REMOVED DAMAG ED DOUBLER ON LEFT WING INBOARD FLAP STA 110 UPPER SURFACE IAW SRM 51-01-21-0. FABRICATED AND INSTALLED REPAIR DOUBLER AT LEFT WING UPPER SURFACE STA 110 IAW EO DC8-5720-7767-A, AND SRM 57-07-01-01. 2 L 7 4 4F RT 4A25 2007081500079 20070815 00079 SO 2007 8 15 C2XA07IA179 1 20070730 A 3260 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 16999 145307 IAH - FLIGHT 2115, THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL MESSAGE AT 1500 FT ON FINAL APPROACH. THE AIRCRAFT LA NDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, WITH NO DEFECTS, OR MESSAGES FOUND, AND THE AIRCR AFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007081500084 20070815 00084 WP 2007 8 15 AALA20071321 1 20070717 A 3350 LENS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 978TW 53628 LGA - EMERGENCY EXIT LIGHT AT SEAT ROW 7C MISSING LENS. REPLACED LENS FOR EMERGENCY EXIT LIGHT AT SEAT ROW 7C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007081500085 20070815 00085 NM 2007 8 15 AALA20071322 1 20070717 A 3397 WIRE BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 681AA 25338 DFW - EMERGENCY EXIT LIGHT AT SEAT ROW 35D INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT AT SEAT ROW 35D. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081500086 20070815 00086 NM 2007 8 15 AALA20071323 1 20070717 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 681AA 25338 DFW - OVERHEAD EMERGENCY LIGHT AT SEAT ROW 18C INOPERATIVE. REPLACED BULB FOR OVERHEAD EMERGENCY EXIT LIGHT AT SEAT ROW 18C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081500087 20070815 00087 EA 2007 8 15 TRAX200701082 1 20070718 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR PEELING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 PAX DOOR EXIT PLACARD PEELING. 2 L 7 2 4F RT A21EA 2007081500088 20070815 00088 WP 2007 8 15 AALA20071316 1 20070717 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 485AA 49678 LGA - EMERGENCY LIGHTS AT FORWARD CAT WALK INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD CAT WALK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081500089 20070815 00089 EA 2007 8 15 TRAX200701083 1 20070730 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 838AS 7276 SECOND FROM AFT CEILING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007081500090 20070815 00090 NM 2007 8 15 AALA20071314 1 20070717 A 2820 PRESSURE SWITCH BOEING 757 757223 1384957 NM FUEL SYSTEM INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 184AN 29594 HNL INFLIGHT T246/17JUL KOA TO LAX AIR INTERRUPT DUE TO CENTER FUEL BOOST PUMP FAULT. LANDED HNL WITHOUT INCIDENT. RE SET UNIVERSAL FAULT INTERRUPTER AND REPLACED PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081500091 20070815 00091 WP 2007 8 15 AALA20071317 1 20070717 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 485AA 49678 LGA - OVERHEAD EMERGENCY LIGHTS AT SEAT ROWS 19, 20, 21 AND 28 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENC Y LIGHTS AT SEAT ROWS 19, 20, 21, AND 28. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081500092 20070815 00092 EA 2007 8 15 TRAX200701084 1 20070730 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 838AS 7276 EMERGENCY LIGHT SWITCH IN COCKPIT HAS SEVERAL INOP BULBS. 2 L 7 2 4F RT A21EA 2007081500093 20070815 00093 NM 2007 8 15 AALA20071315 1 20070717 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 792AN 30253 JFK - EMERGENCY LIGHT AT RIGHT FORWARD FIRST CLASS CEILING INOPERATIVE. REPLACED BATTERY PACK AND LEFT NUMBER ONE DOOR CEILING FOR EMERGENCY LIGHT AT RIGHT FORWARD FIRST CLASS CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007081500096 20070815 00096 EA 2007 8 15 TRAX200701085 1 20070730 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOOR WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 719EV 10099 ASD 'EXIT' PLACARD WORN. 2 L 7 2 4F RT A21EA 2007081500097 20070815 00097 NM 2007 8 15 AALA20071341 1 20070721 A 3350 GUARD BOEING 737 737800* NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 951AA 29538 DFW - EMERGENCY EXIT LIGHT AT SEAT ROW 11 MISSING GUARD. REPLACED GUARD FOR EMERGENCY EXIT LIGHT AT SEAT ROW 11. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007081500099 20070815 00099 WP 2007 8 15 AALA20071313 1 20070717 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 266AA 49291 LGA - EMERGENCY LIGHT AT SEAT ROW 4EF INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 4EF. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081500103 20070815 00103 EA 2007 8 15 TRAX200701092 1 20070731 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 833AS 7246 LEFT INTERCOSTAL AT FS 625 STRINGER 13L CRACKED. 2 L 7 2 4F RT A21EA 2007081500106 20070815 00106 EU 2007 8 15 07FDEA02702 1 20070801 A 5340 A5377364420100 FITTING AIRBUS 310 A310203 3930313 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 FRAME FITTING C38.1 CRACKED AT RBL 60, FWD PIT FLOOR. REMOVED AND REPLACED FRAME FITTING IAW A310-200 SRM 51-40-24 PAR 7. 2 L 7 2 4F RT A35EU 2007081500111 20070815 00111 EA 2007 8 15 TRAX200701093 1 20070731 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 977EV 7720 EMERGENCY LIGHTING INOP. 2 L 7 2 4F RT A21EA 2007081500113 20070815 00113 EA 2007 8 15 TRAX200701097 1 20070801 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 713EV 10081 OVERHEAD EMERGENCY LIGHT AT ROW 4 INOP. CABIN EMERGENCY LIGHTS - CEILING LEVEL FLOODLIGHTS. 2 L 7 2 4F RT A21EA 2007081500114 20070815 00114 EA 2007 8 15 TRAX200701098 1 20070801 A 3620 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA BLEED AIR SYS ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 709EV 10068 L BLEED LEAK WARNING MSG ILLUMINATED ON CLIMBOUT AFTER DEPARTURE FROM ATL. COMPLIED WITH QRH. RETURNED TO ATL UNPRESSU RIZED. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007081500115 20070815 00115 EU 2007 8 15 07FDEA02711 1 20070802 A 5340 A539736102000 ATTACH FITTING AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 CRACKED ATTACHMENT FITTING WHICH CONNECTS THE CROSSBEAM AND THE FRAME SEGMENT C60 RHS WITH THE SILLBEAM P/N ATTACH FITTI NG C60: A539-73610-200-51, ATTACH FITTING C60: A539-73610-200-00 AND ECKBESCHLAG: DR012131-200. REPAIR PERFORMED BY CUT THE TORSION BOX AREA AND REPAIR IT IAW SRM 53-17-18/FIG 206, SH 1(C), SH 2 (D) AND BY REPLACEMENT DAMAGED ATTACH FITTIN GS IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007081500116 20070815 00116 EU 2007 8 15 07FDEA02712 1 20070802 A 5311 A53981311202 FRAME AIRBUS 300 A300B4605R 3930308 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 SCRATCHED AND DENTED OUTER FLANGE OF C74, P26 RT AND LT. REPAIR PERFORMED BY REWORK SCRATCH AREA AND NOT DRESSING BACK THE DENT IAW RAS/DAHAM/4022387/2007 ISSUE "A" AND EA 6-5318-106496. 2 L 7 2 4F RT A35EU 2007081500120 20070815 00120 NM 2007 8 15 07FDEA02715 1 20070802 A 5311 65163411 FRAME BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT PIT FRAME CORRODED AT STA 1010 BETWEEN STR 29-30R. REMOVED FASTENERS REF SRM 51-30-2. REMOVED CORROSION REF SRM 5 1-10-1. INSTALLED FASTENERS REF SRM 51-30-2. TREATED AND PRIMED REF MM 51-20-013 AND PAINTED REF MM 51-20-013. CORROS ION LEVEL 1. 2 L 7 3 4F RT A3WE 2007081500122 20070815 00122 EU 2007 8 15 07FDEA02717 1 20070802 A 5320 A53973085210 SILL AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 CORROSION FOUND ON AFT CARGO DOOR SILL BEAM UPPER FLANGE BETWEEN C59-59A, RT. REPAIR PERFORMED BY REWORK, EXCEEDING LIM IT AND IS APPROVED BY RAS/DATLS/0003788/2007 ISSUE "A" AND EA 6-5317-112483. 2 L 7 2 4F RT A35EU 2007081500123 20070815 00123 SO 2007 8 15 C2XA07TY041 1 20070805 A 5544 12067385004 BRACKET EMB 145 EMB145LR 3260212 SO RUDDER DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13994 145291 TYS - DURING A CURRENT C-CHECK INSPECTION, ELONGATED HOLES WERE FOUND ON NR 2 RUDDER AT SPAR 1. HOLES MEASURED (1) .249 (2) .228 AND (3) .338. HOLES WERE REAMED IAW EC5540-01074. ALODINED PRIMED HOLES. INSTALL NEW BUSHIONS IN THE NR 3 HO LE. ALL WORK WAS ACCOMPLISHED IAW THE EC. AIRCRAFT WAS RELEASED AT THE END OF THE C-CHECK. 2 L 7 2 4T RT T00011AT 2007081000041 20070810 00041 CE 2007 8 10 DXTA200702367 1 20070730 A 2120 UNKNOWN RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP CABIN ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 858QS 258691 APU DID A NORMAL START. WHEN THE BLEED AIR WAS TURNED ON, IT DETECTED A FUNNY ODOR AND FILLED THE CABIN WITH SMOKE. S USPECT LT ENGINE INTRODUCTED OIL INTO THE A/C SYSTEM, LT ENGINE WAS CHANGED FOR HIGH GEARBOX OIL PRESSURES, INSPECTED WATER SEPERATOR AND SILENCER DUCT ON B INSPECTION, NO DISCREPANCIES NOTED, RAN APU AIR FOR APPROX. 3 PLUS HRS. NO ODOR N OTED. 2 L 7 2 4F 4 F RT A3EU E6WE 2007081000084 20070810 00084 EA 2007 8 10 A6WA200740376 1 20070707 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 461AW 7870 PAX DOOR AFT DRAG ANGLE IS CRACKED APPROX 1.0 INCH LONG NEAR PULLEY BRACKET. (K) MAINTENANCE REPAIRED BY REMOVING DAMA GED SECTION, FABRICATING AND INSTALLING A SPLICE REPAIR IAW BOMBARDIER REO 601R-53-11-513 REV A. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007081300026 20070813 00026 NM 2007 8 13 SWAA073832 1 20070731 A 5311 6546593 FRAME BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300029 20070813 00029 NM 2007 8 13 SWAA073792 1 20070731 A 5313 6551698 STRINGER SPLICE BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360. STR 4L. REPAIRED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007081300033 20070813 00033 NM 2007 8 13 SWAA073790 1 20070731 A 5340 65C27314 STRINGER CLIP BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300038 20070813 00038 NM 2007 8 13 SWAA073788 1 20070731 A 5340 65C27314 STRINGER CLIP BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300058 20070813 00058 NM 2007 8 13 SWAA073866 1 20070801 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, RBL 3. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2007081300066 20070813 00066 NM 2007 8 13 SWAA073857 1 20070801 A 5322 6546546 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007081300074 20070813 00074 NM 2007 8 13 SWAA073846 1 20070801 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300089 20070813 00089 NM 2007 8 13 SWAA073874 1 20070801 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300093 20070813 00093 NM 2007 8 13 SWAA073895 1 20070802 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 411WN 29821 DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007081300097 20070813 00097 NM 2007 8 13 SWAA073892 1 20070802 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, STR 28L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007081300099 20070813 00099 NM 2007 8 13 SWAA073878 1 20070802 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300106 20070813 00106 NM 2007 8 13 SWAA073891 1 20070802 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300109 20070813 00109 NM 2007 8 13 SWAA073884 1 20070802 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300114 20070813 00114 NM 2007 8 13 SWAA073889 1 20070802 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300118 20070813 00118 EA 2007 8 13 COMA0760502 1 20070728 A 2120 VALVE CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 918CA 7018 FLIGHT 5540 - OVERBOARD COOL CAUTION MESSAGE ON IN FLIGHT. AIRCRAFT DID NOT PRESSURIZE NORMALLY. AIRCRAFT RETURNED BAC K TO SAV AND LANDED SAFELY. TRANSFERRED TO DEFERRED LIST PER MEL 21-24-06-2. 2 L 7 2 4F RT A21EA 2007081300119 20070813 00119 EA 2007 8 13 COMA0760503 1 20070729 A 3222 16154103 TORQUE LINK CNDAIR CL600 CL6002B19 1900309 EA NLG WORN A COMA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SO 01 442CA 7483 FLIGHT 5243 - REJECTED TAKEOFF AT 95 KTS DUE TO MODERATE NOSE WHEEL VIB AND LOUD CLANKING NOISE. C/W RTO INSPECTION. R EMOVED AND REPLACED NLG LOWER TORQUE LINK. 2 L 7 2 4F RT A21EA 2007081300122 20070813 00122 EA 2007 8 13 COMA0760506 1 20070731 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DIRTY A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 991CA 7216 FLIGHT 5347 - FLOOR EMERGENCY LIGHT INOP. CLEANED CONNECTOR ON FLOOR EMERGENCY LIGHTS, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007081300136 20070813 00136 NM 2007 8 13 SWAA073919 1 20070805 A 5753 65C263107A FLAP BOEING 737 7373K2 13844BA NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND LEFT WING INBOARD MID FLAP CRACKED AT INBOARD END. REMOVED AND REPLACED MIDFLAP PER MM. 2 L 7 2 4F RT A16WE 2007081300145 20070813 00145 NM 2007 8 13 SWAA073925 1 20070806 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 EEPLS COVER CRACKED AT ROW 3 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007081300148 20070813 00148 NM 2007 8 13 SWAA073920 1 20070804 A 2782 65445519 ACTUATOR BOEING 737 7373H4 1384600 NM L/E SLAT FAULTY A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 378SW 26585 AIRTURN BACK. NR 2 L/E FLAP INTRANSIT LIGHT ILLUMINATED ON OVERHEAD AND FWD PANEL. REMOVED AND REPLACED SLAT ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2007081300161 20070813 00161 NM 2007 8 13 SWAA073941 1 20070807 A 5313 BAC1498 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 27R CORRODED AT BETWEEN BS 376 AND BS 380, WL 149. REPAIRED STRINGER PER SR M. 2 L 7 2 4F RT A16WE 2007081300163 20070813 00163 NM 2007 8 13 SWAA073935 1 20070807 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007081300165 20070813 00165 NM 2007 8 13 SWAA073944 1 20070808 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED MV1 CHECK, MID CABIN EMERGENCY EXIT LIGHTS STAY ILLUMINATED WITH SWITCH IN ARMED POSITION. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007081300166 20070813 00166 NM 2007 8 13 SWAA073951 1 20070808 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739A, STR 2R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007081300175 20070813 00175 NM 2007 8 13 UPS07550358 1 20070719 A 5330 2024T3050 SKIN BOEING 757 75724APF 1384969 NM FUSELAGE BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 401UP 23723 INSPECTION TYPE:C LOWER EXT FUSELAGE SKIN BULGING APPROX BS 543 BETWEEN S24L- S25L. REMOVED FASTENER AT AFFECTED AREA C OMMON TO REPAIR IAW SRM 51-40-02 AND CUT OUT DAMAGED SECTION L.2.9" X W2.4" IAW SRM 53-00-01-2R3. HFEC INSPECTED CUTOUT PER NTM51-00-01PT6 NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER (P/N 2024T3.050W B.N. 1276774) IAW SRM 53-00 -01-2R 3 F IG 201 TBL 1, LOCATED & DRILLED IAW SRM 51-40-05. 2 L 7 2 4F RT A2NM 2007081300180 20070813 00180 WP 2007 8 13 UPS07850361 1 20070731 A 2560 ESCAPE ROPE DOUG DC8 DC873F 302199F WP COCKPIT OUT OF POSITION A IPXA K NONE O OTHER AP APPROACH 1 SO 01 868UP 45968 INSPECTION TYPE:N/A ESCAPE ROPE CAPTAINS SIDE FELL OUT ON SHORT FINAL. REPACKED CAPTAINS ESCAPE TAPE PER MM 25-60-02-2. 2 L 7 4 4F RT 4A25 2007081300189 20070813 00189 NM 2007 8 13 ZZDA2007256 1 20070803 A 3260 WARNING SYSTEM BOEING 717 717200 1383700 NM COCKPIT ACTIVATED A ZZDA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 37 950AT 55012 GEAR DOOR OPEN ALERT ON CONFIG PAGE. LUBED GEAR DOORS, PERFORMED EMERGENCY GEAR EXTENSION AND SWUNG GEAR SEVERAL TIMES WHILE ON JACKS. SERVICED HYD'S, A/C OK FOR SERVICE REF AMM 32-00 AND 12-00. 2 L 7 2 4F TR A6WE 2007081300191 20070813 00191 NM 2007 8 13 UPS07M50355 1 20070703 A 5753 SKIN DOUG MD11 MD11F 3023600 NM T/E FLAP CANNING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C LEFT I/B FLAP UPPER SURFACE FOUND OIL CANNING AT 4.75 INCHES FROM O/B END AND 33.75 INCHES FROM T/E AS MARKED. DAMAGES / AFFECTED AREA TRIM OUT SRM 57-10-00 FIG 34 VI R38. REWORKED AREA REPROTECTED SRM 51-21-01VII R38. HFEC INSP C/O NDTSPM R13 06-10-01.001 ON TRIM OUT AREA, FOUND NO CRACK EVIDENT. REPAIR DOUBLER FAB SRM 57-10-00 FIG 34 VI R38, USE MATL 2024T3-0.040". C/O BONDING OF DOUBLER TO SKIN SRM 51-71-00 VII R38. REPAIR DOUBLER INSTALLED SRM 51-3 5-01VII R38. 2 L 7 3 4F RT A22WE 2007081300194 20070813 00194 2007 8 13 NOCA14507 4 20070730 A 3417 4040800912 ADC BOEING 757 75728A 1384976 NM NR 1 MALFUNCTIONED A NOCA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 EA 15 750NA 26277 REJECTED TAKEOFF DUE TO NO AIRSPEED INDICATION ON CAPT AIRSPEED INDICATOR. REPLACED AIRSPEED INDICATOR AND LEFT AIR DAT A COMPUTER ITEM REMAINS OPEN, SECOND TIME REJECTED TAKEOFF DUE TO NO AIRSPEED INDICATION ON CAPTAINS AIRSPEED INDICATOR . REPLACED NR 1 ADC PER MM 34-11-00, OPS CHECK OK PERFORMED PRESSURIZATION OF PITOT STATIC SYSTEM PER MM 34-11-00, ALL CHECK OK INTEGRITY CHECK REF MM 34-11-00 LOW RANGE ACCOMPLISHED ITEM CLOSED. 2 L 7 2 4F RT A2NM 2007081300196 20070813 00196 NM 2007 8 13 KCSA071269 1 20070802 A 5412 BULKHEAD BOEING 747 7472B4B 138481B NM NR 2 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NR 2 PYLON, NAC STA 221.9 BULKHEAD LOWER TOP CHORD CRACKED ON THE OUTBOARD SIDE. 2 L 7 4 4F RT A20WE 2007081300197 20070813 00197 NM 2007 8 13 KCSA071270 1 20070802 A 5412 BULKHEAD BOEING 747 7472B4B 138481B NM NR 2 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NR 2 PYLON, NAC STA 221.9 BULKHEAD LOWER FORWARD OUTBOARD CHORD IS CRACKED IN TWO PLACES. 2 L 7 4 4F RT A20WE 2007081400001 20070814 00001 WP 2007 8 14 07FDEA02669 1 20070730 A 5315 FLOORBEAM DOUG DC10 DC1010F 3022111 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 FWD CARGO COMPT BILGE AREA ON BEAM FOUND CRACK. REPAIRED BEAM IAW SRM 53-60-01 VOL 1 FIG 3 SHEET 1-2. 2 L 7 3 4F A22WE 2007081400002 20070814 00002 WP 2007 8 14 07FDEA02672 1 20070730 A 5347 WSP0413509 SEAT TRACK DOUG DC10 DC1010F 3022111 WP ZONE 200 WORN A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 68052 47806 MAIN CABIN SEAT TRACK DEEP WEAR ON UPPER SIDE. REPAIRED IAW SRM 53-70-000 FIG 1 VOL 1. 2 L 7 3 4F A22WE 2007081400025 20070814 00025 2007 8 14 SWIA200718541 4 20070726 A 2210 BUTTON CNDAIR CL600 CL6002C10 1390015 EA STICKING A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 743SK 10199 AIRCRAFT PITCHED RAPIDLY 7-9 DEGREES NOSE UP. THE AIRCRAFT RESPONDED TO CORRECTIVE ACTION FROM FLIGHT CONTROL PANEL. F IRST OFFICER FD BUTTON STICKS. REPLACED FDP IAW AMM 22-11-07. OPS CHECKED GOOD, PN: 822-0044-001, SN OFF: 1GL1L. 2 L 7 2 4F RT A21EA 2007081400026 20070814 00026 EA 2007 8 14 SWIA200718542 1 20070727 A 3620 LOOP CNDAIR CL600 CL6002C10 1390015 EA DUCT SENSOR MALFUNCTIONED A SWIA G A O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 726SK 10190 RECEIVED A RIGHT DUCT AND CABIN ALT WARNING MESSAGE AND THE OXYGEN MASKS IN CABIN DEPLOYED. REPLACED DUCT SENSOR LOOPS MT144, MT143 IAW MM CH 36-21-03. OPS CHECK GOOD, PN: 04-31102-A072. 2 L 7 2 4F RT A21EA 2007081400027 20070814 00027 EA 2007 8 14 SWIA200718543 1 20070728 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 976SW 7952 EXIT LIGHT NEAR MAIN CABIN DOOR IS DETACHED FROM WALL. REPLACED LIGHT ASSEMBLY IAW CRJ 200 AMM 33-51-10. OPS CHECK GOO D, PN/ON BR9279-232, PN/OFF BR9279-013. 2 L 7 2 4F RT A21EA 2007081400028 20070814 00028 SO 2007 8 14 SWIA200718544 1 20070717 A 5297 WIRE EMB 120 EMB120ER 3260203 SO DOOR WARNING CORRODED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 582SW 120350 LEFT TANK DOES NOT ACCEPT PRESSURE REFUELING. REPLACED CORRODED SPLICES FOUND ON FUEL SERVICE DOOR MICROSWITCH WIRING. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2007081500001 20070815 00001 WP 2007 8 15 ASAA0781919 1 20070730 A 5321 99365813 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 CABIN FLOOR PANEL TOP PLY PULLED LOOSE. BOND REPAIRED WITH GLASS CLOTH PER SRM 51-90-0. 2 L 7 2 4F RT A6WE 2007081500009 20070815 00009 NM 2007 8 15 CALA0700390 1 20070802 A 5330 6545774 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE BURNED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A BURN SPOT ON FUSELAGE SKIN 2.25 INCHES AFT OF STA 727 AND 2.25 INCHES ABOVE S23L. A REPAIR WAS INSTA LLED IAW SRM 53-00-01, FIGURE 201, REPAIR 31, PAGE 231. 2 L 7 2 4F RT A16WE 2007081500014 20070815 00014 SO 2007 8 15 SIMA200721402 1 20070731 A 3320 7281000501 CONTROL MODULE EMB 135 EMB135LR 3260305 SO CABIN LIGHTS BURNED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 720AE 2823 145279 BURNING ODOR FROM GALLEY AREA. REMOVED AND REPLACED LIGHT BALLAST IAW EMB AMM 33-21-05 AND REMOVED AND REPLACED CONTROL MODULE ASSEMBLY IAW EMB AMM 33-21-01, BOTH COMPONENTS OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007081500017 20070815 00017 SO 2007 8 15 SIMA200721206 1 20070730 A 2612 FIRE DETECTOR EMB 145 EMB145LR 3260212 SO APU BAY ACTIVATED A SIMA F ACTIVATE FIRE EXT. J WARNING INDICATION CR CRUISE 1 SW 21 693AE 14500868 RECEIVED APU FIRE WARNING AND APU FIRE DET FAIL AT 12,000 FEET, FIRED APU EXTINGUISHER BOTTLE, POST INSPECTION FOUND NO EVIDENCE OF FIRE. ISSUED AMERICAN EAGLE MEL 26-01, 26-05 AND 49-01. REPLACED FIRE BOTTLE IAW AMERICAN EAGLE WORK CARD 26-200-01. RESTORED MEL, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007081500018 20070815 00018 NM 2007 8 15 DHL2007741521 1 20070801 A 5343 65198639 SUPPORT BEAM BOEING 727 7272Q9 138448M NM NLG TRUNNION CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 NLG LT TRUNNION VERTICAL SUPPORT BEAM AT BS 312.0 HAS CORROSION. CORROSION REMOVAL EXCEEDED LIMITS PER B727 SRM 53-10-1 FIG 1. REMOVED AND REPLACED VERTICAL SUPPORT BEAM PER B727 SRM 51-30-2 AND 51-30-5. 2 L 7 3 4F RT A3WE 2007081500022 20070815 00022 NM 2007 8 15 DHL2007741524 1 20070728 A 5320 SUPPORT BOEING 727 7272Q9 138448M NM BS 720B CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 STRINGER 26L, BS 720B, FRAME SUPPORT CLIP IS CORRODED. REMOVED CORRODED STR CLIP, FABRICATED NEW CLIP FROM 2024-T3, .04 0" BY 4" BY 3.25", PO NR 9005138, PER B727 SRM 53-10-2 FIG 3, 51-10-3, AND 51-20-1. TREATED, PRIMED, AND INSTALLED NEW CLIP PER B727 SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007081500030 20070815 00030 NM 2007 8 15 TSAA0732043 1 20070731 A 3230 65446915 MODULE BOEING 737 7372Y5 1384554 NM LT MLG FAILED A TSAA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 13 810AL 24031 NON-ETOPS FLIGHT 221 OGG - HNL. WHEN THE CREW SELECTED THE LANDING GEAR TO UP, THE LT MAIN GEAR DOWN LIGHT TOOK A FEW S ECONDS LONGER TO EXTINGUISH THAN THE OTHER GEAR INDICATIONS. AFTER THE GEAR LEVER WAS SELECTED TO OFF, THE LT MAIN GEAR EXTENDED UNCOMMANDED. CREW FELT ASSOCIATED VIBRATION AND HEARD AIR NOISE FROM THE DOWN LT GEAR. CREW CONTINUED THE FL IGHT AT 250 KNOTS TO HNL. ATC CONFIRMED THE LT GEAR WAS EXTENDED. CREW SELECTED THE LANDING GEAR TO DOWN AND LANDED WI THOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT LANDING GEAR MODULAR PACKAGE PER AMM 32-32-61 AND PERFO RMED A LANDING GEAR EXTENSION AND RETRACTION TEST PER AMM 32-32-0 WITH ALL CHECKS NORMAL. THE AIRCRAFT ALSO COMPLETED A 2 L 7 2 4U RT A16WE 2007081500036 20070815 00036 NM 2007 8 15 NWAA072745518 1 20070729 A 7900 UNKNOWN BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 2 ENGINE UNKNOWN A NWAA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION DE DESCENT 1 GL 01 518US 23206 727189 DURING DESCENT, ENGINE NR 2 "VALVE LIGHT" ILLUMINATED FOLLOWED BY LOSS OF ENGINE OIL PRESSURE. ENGINE SHED ALL ELECTRIC AL POWER. FLIGHT CREW SECURED ENGINE AND LANDED AT DESTINATION AIRPORT. MAINTENANCE REMOVED AND REPLACED ENGINE NR 2. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081500064 20070815 00064 NM 2007 8 15 AALA20071333 1 20070718 A 2121 FAN BOEING 757 757223 1384957 NM AIR CONDITIONING INOPERATIVE A AALA A UNSCHED LANDING B E SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET CR CRUISE 1 SW 21 663AM 25297 MKE INFLIGHT T164/18JUL LAX TO EWR - THREE HOURS INTO FLIGHT CREW HEARD LOUD BANG ACCOMPANIED BY VIBRATIONS AND STRONG E LECTRIC SMOKE ODOR. FLIGHT ATTENDANTS REPORTED HAZE IN THE AFT CABIN. SMOKE DISSAPATED BEFORE LANDING. LANDED MKE WITH OUT INCIDENT. REPLACED RIGHT RECIRCULATION FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081500068 20070815 00068 NM 2007 8 15 AALA20071319 1 20070717 A 3397 CONNECTOR DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 951TW 53470 LGA - EMERGENCY LIGHT AT SEAT ROW 30 INOPERATIVE. SECURED LOOSE CONNECTOR PLUG FOR EMERGENCY LIGHT AT SEAT ROW 30. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2007081500072 20070815 00072 NM 2007 8 15 AALA20071328 1 20070718 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 789AN 30252 DFW - EMERGENCY EXIT LIGHT AT SEAT ROW 21C INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT LIGHT AT SEAT ROW 21C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007081500078 20070815 00078 WP 2007 8 15 UPS07850372 1 20070724 A 5522 SKIN DOUG DC8 DC873F 302199F WP LT ELEVATOR CANNING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 LEFT ELEVATOR UPPER SKIN INBOARD OIL CANNED. REMOVED, FABRICATED, AND INSTALLED ELEVATOR SKIN IAW SR M 51-1-21, 55-0 2-01, 51-1-8 AND 51-1-21A. 2 L 7 4 4F RT 4A25 2007081500083 20070815 00083 EA 2007 8 15 TRAX200701081 1 20070628 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 877AS 7579 REFER TO DML 344262 ITEM 3, ALL EMERGENCY LIGHTS INOP. RELATED TO DEFECT 344262-3. 2 L 7 2 4F RT A21EA 2007081500094 20070815 00094 NM 2007 8 15 AALA20071339 1 20070721 A 3350 BULB BOEING 757 7572Q8 1384972 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 709TW 28168 DFW - EMERGENCY BULL NOSE LIGHT AT ROW 16 RIGHT SIDE INOPERATIVE. REPLACED LAMP FOR EMERGENCY BULL NOSE LIGHT AT ROW 16 RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081500095 20070815 00095 NM 2007 8 15 AALA20071340 1 20070721 A 3350 GUARD BOEING 737 737823 13844BZ NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 951AA 29538 DFW - EMERGENCY EXIT LIGHT AT SEAT ROW 9 MISSING GUARDS. REPLACED GUARDS FOR EMERGENCY EXIT LIGHT AT SEAT ROW 9. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007081500104 20070815 00104 WP 2007 8 15 AALA20071334 1 20070719 A 5280 DOOR DOUG DC9 DC982 3022082 WP NLG DAMAGED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 454AA 49559 DFW INFLIGHT T2055/19JUL - UNABLE TO EXTINGUISH RED NOSE GEAR LIGHT ON GEAR RETRACTION. CREW REPORTED LOUD AIR NOISE C OMING FROM NOSE GEAR AREA. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPAIRED NOSE GEAR DOORS. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081500110 20070815 00110 NM 2007 8 15 07FDEA02706 1 20070801 A 5347 AFA77958 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 AFTER CENTER CARGO CEILING PANEL REMOVED, FOUND MAIN DECK CARGO SEAT TRACK AT STA 1815, X = -27.5 CORRODED. [08-15-07] REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 6 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007081500117 20070815 00117 EU 2007 8 15 07FDEA02713 1 20070802 A 5330 A53980664204 SKIN PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 FOUR OVERSIZED HOLES (DIA. 4.8MM) FOUND AT C74, P'39-43, RHS. THE ORIGINAL RIVET SIZE IS 4.0MM. REPAIR PERFORMED PER I NSTALLING FASTENERS NAS1241D6 IAW SRM 51-40-20 (-21), RAS/DAHAM/4022495/2007 ISSUE "A" AND EA 6-5318-112475. 2 L 7 2 4F RT A35EU 2007081500118 20070815 00118 EU 2007 8 15 07FDEA02714 1 20070802 A 5311 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 FOUND MISDRILLED HOLE AT C40, P'13, RHS. REPAIR PERFORMED BY INSTALLING FASTENER DAN6-8-12Y WITH TRANSITION FIT AND USI NG RADIUS FILLER IAW RAS/DAHAM/4022410/2007 ISSUE "B" AND EA 6-5315-106497. 2 L 7 2 4F RT A35EU 2007081500119 20070815 00119 EA 2007 8 15 TRAX200701099 1 20070802 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 730EV 10141 FWD F/A FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007081500124 20070815 00124 EU 2007 8 15 07FDEA02720 1 20070802 A 5330 SKIN AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 TWO CORROSION SPOTS AT INTERNAL SKIN IN THE AREA OF C69, P'47 RHS. HEAVY CORROSION AT CONNECTING SECTION AT C67, P'48 R HS (P/N: A539-78339-200 AND A539-78339-200-90). REPAIR PERFORMED BY BLEND OUT CORROSION SPOTS AT INTERNAL SKIN IAW SRM 51-74-10, IN LIMIT. CROSSBEAM CONNECTION IS REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007081500132 20070815 00132 NM 2007 8 15 CALA0700395 1 20070803 A 5311 6546552 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 827, S9R. REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5310-04647. 2 L 7 2 4F RT A16WE 2007081500133 20070815 00133 WP 2007 8 15 07FDEA02727 1 20070802 A 5310 DOOR FRAME DOUG MD10 MD1010F 3022112 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 MAIN CARGO DOOR CUT-OUT LOWER JAMB TOP SIDE, JUST FWD OF NR 3 LATCH SPOOL FITTING WEB CORRODED. 09-04-07 REMOVED AND REPLACED MAIN CARGO DOOR JAMB UPPER BEAM ACA7226-1 IN REF TO DC/MD10 SRM 51-33-01 VOL II PAGE1 AND DAC DRAWING ACA7224 REV G. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2007081500134 20070815 00134 WP 2007 8 15 07FDEA02728 1 20070802 A 5340 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 MAIN CARGO DOOR FITTING NR 3 BORES A, C AND D SHOWS CRACK INDICATION WITH BHEC BORES MARKE DIN BLACK. 09-04-07 REMOV ED AND REPLACED NR 3 DOOR FITTING AT STA 666 IN REF TO DC/MD10 SRM 51-33-01 VOL II PAGE 1. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2007081500135 20070815 00135 NM 2007 8 15 CALA0700396 1 20070803 A 5311 6546551 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 807, S9R. REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5310-04647. 2 L 7 2 4F RT A16WE 2007081500136 20070815 00136 NM 2007 8 15 CALA0700397 1 20070803 A 5311 BAC15171470 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 847, S9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04643. 2 L 7 2 4F RT A16WE 2007081500137 20070815 00137 NM 2007 8 15 CALA0700398 1 20070803 A 5311 BAC15171470 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 787, S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04643. 2 L 7 2 4F RT A16WE 2007081500138 20070815 00138 NM 2007 8 15 CALA0700399 1 20070803 A 5311 6546549 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 767, S9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04643. 2 L 7 2 4F RT A16WE 2007081500140 20070815 00140 EU 2007 8 15 07FDEA02731 1 20070725 A 5347 A5381310620010 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 NR 3 LT SEAT-TRACK, BETWEEN FR 38.2 AND FR 40 AT Y953, FOUND CRACKED. IT WAS REPAIRED IN ACCORDANCE WITH SRM SUPP 53-15 -15. 2 L 7 2 4F RT A35EU 2007081500141 20070815 00141 NM 2007 8 15 07FDEA02732 1 20070802 A 5330 6554581 SKIN BOEING 727 727233 138408A NM ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 AFT LT FUSELAGE, STA 988 TO 990, BETWEEN STR 23L AND 24L HAS 2 DEEP GOUGES. BLENDED GOUGES AND FOUND TO BE OUT OF ALLOW ABLE LIMITS REF SRM 53-30-1. TRIMMED OUT DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED REF 53-30-1 FIG 1, THIS IS CLA SSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007081500142 20070815 00142 EU 2007 8 15 07FDEA02733 1 20070725 A 5347 A5381310620010 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 NR 2 LT SEAT-TRACK BETWEEN FR 38.2 AND FR40 AT Y450 FOUND CRACKED. IT WAS REPLACED IN ACCORDANCE WITH SRM SUPP 53-15-15 . 2 L 7 2 4F RT A35EU 2007081500144 20070815 00144 EU 2007 8 15 07FDEA02735 1 20070725 A 5347 A5381310620010 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 NR 4 RT SEAT TRACK BETWEEN FR 38.2 AND FR 40 AT Y-1456 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM SUPP 53-15-15. 2 L 7 2 4F RT A35EU 2007081500145 20070815 00145 NM 2007 8 15 07FDEA02737 1 20070802 A 5330 6554575 SKIN BOEING 727 727233 138408A NM BS 720D S19R CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 RT LWR FUSELAGE SKIN CHAFED STA 720D 14" STR 19R FABRICATED AND INSTALLED DOUBLER IAW SRM 53-30-3 FIG 5, PAGE 20-22. TH IS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007081500149 20070815 00149 NM 2007 8 15 CALA0700402 1 20070803 A 5311 6546526 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A .25 INCH CRACK IN FRAME AT RIVET THAT ATTACHES AIR GRILL, STA 400, S9L. A FRAME REPAIR WAS INSTALLED IAW ECRA 5310-04643. 2 L 7 2 4F RT A16WE 2007081500150 20070815 00150 NM 2007 8 15 07FDEA02716 1 20070802 A 5315 6520832 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 CABIN STA 950 FLOORBEAM BET RBL 45 AND 62 HAS CORROSION ON UPPER AND LWR, AND AROUND FASTENER HOLES REMOVED CORROSION. HFEC NO DEFECT NOTED, ROTO PEENED REF SOPM 20-10-3. TREATED AND PRIMED REF SRM 51-10-2, LEVEL 1 CORROSION. 2 L 7 3 4F RT A3WE 2007081500151 20070815 00151 NM 2007 8 15 CALA0700403 1 20070803 A 5311 6546525 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A .25 INCH CRACK IN FRAME AT RIVET THAT ATTACHES AIR GRILL, STA 380, S9R. REPAIRED IAW ECRA 5310-04643 . 2 L 7 2 4F RT A16WE 2007081500152 20070815 00152 EU 2007 8 15 07FDEA02741 1 20070803 A 5313 A53778561207 STRINGER AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORRODED STRINGER P'53 IN FWD CARGO COMPARTMENT BETWEEN C28-29. REPAIR PERFORMED BY REPLACEMENT IAW SRM 53-10-14/FIG 20 1. 2 L 7 2 4F RT A35EU 2007081500153 20070815 00153 EU 2007 8 15 07FDEA02742 1 20070803 A 5320 A53980149201 SUPPORT AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CRACKED SUPPORT STRUT BETWEEN C77-78 AT P'48 RT, SHOWN IN SRM53-18-18/FIG 5/ITEM 70. REPAIR PERFORMED BY REPLACEMENT OF SUPPORT STRUT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007081500154 20070815 00154 NM 2007 8 15 CALA0700404 1 20070803 A 5311 6546557 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 887, S9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04643. 2 L 7 2 4F RT A16WE 2007081500156 20070815 00156 EU 2007 8 15 07FDEA02749 1 20070713 A 5347 A5381192220251 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 MDCC - SEAT TRACK AT Y-450 FOUND CORRODED BETWEEN FR 45 AND 54. THE PART WAS REPAIRED IN ACCORDANCE WITH FEDEX ENGINEER ING AUTHORIZATION 6- 5310-113152. 2 L 7 2 4F RT A35EU 2007081500157 20070815 00157 EU 2007 8 15 07FDEA02750 1 20070713 A 5347 A5381192220251 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 N00736 MDCC - SEAT TRACK AT Y0 FOUND CORRODED BETWEEN FR 45 AND FR 54. SEAT TRACK REPLACED IN ACCORDANCE SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007081500160 20070815 00160 EU 2007 8 15 07FDEA02753 1 20070710 A 5347 A5327923220000 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 N00568 MDCC - SEAT TRACK AT Y1447 BETWEEN FR 74 AND FR 78 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007081500162 20070815 00162 NM 2007 8 15 07FDEA02755 1 20070803 A 5320 69455772 FITTING BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT PIT CARGO DOOR THRESHHOLD STANCHION FITTINGS STA 950E-990 RBL 22-27 4 EA. FITTINGS CORRODED UPON FURTHER REVIEW 2 FITTINGS WITHIN LIMITS AFTER BLEND OUT PER DWG 69-45577-2 AND 69-45576-3. 2 OUT OF LIMITS. REPLACED AT STA 950F AND 950 G, ALL FITTINGS REPLACED, INSTALLED REF SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007081500163 20070815 00163 NM 2007 8 15 07FDEA02756 1 20070803 A 5712 RIB BOEING 727 727233 138408A NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 254FE 20936 RT WING L/E SLAT NR 5 INBD END PORK CHOP SEAL MOUNTING PLATE DEFORMED AND CRACKED. REMOVED CRACKED RIB, FABBED NEW RIB ON TRAVLER T/682663. INSTALLED NEW RIB. 2 L 7 3 4F RT A3WE 2007081500164 20070815 00164 NM 2007 8 15 CALA0700405 1 20070803 A 5311 BAC15171470 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 867, S9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04643. 2 L 7 2 4F RT A16WE 2007081500165 20070815 00165 NM 2007 8 15 F3LA200700189 1 20070801 A 3610 6730C010000 VALVE AIRBUS A319 A319111 3930336 NM NR 1 ENGINE FAILED A F3LA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 NM 03 922FR 5204 2012 DURING TAKEOFF FROM KMDW, FLIGHT CREW RECEIVED AN ECAM AIR BLEED 2 FAULT. RAN ECAM ACTION FOR FAULT. APPROX 1 HR INTO THE FLIGHT, THEY RECEIVED AN ECAM AIR BLEED 1 FAULT, THEN LOST BOTH PACKS. PERFORMED AN EMERGENCY DESCENT TO 10,000 FT AND DECLARED AN EMERGENCY. AIRCRAFT LANDED AT KDEN WITHOUT INCIDENT. NR 1 AND NR 2 ENGINE FAN AIR VALVES FAILED FUNCTI ONAL TEST IAW AMM 36-11-54-720-001. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE FAN AIR VALVES IAW AMM 36-11-54-000-001 A ND 36-11-54-400-001. PERFORMED LEAK CHECK OF NR 1 AND NR 2 ENGINE FAN AIR VALVE CONNECTIONS IAW AMM 36-11-54-790-050, S TEP B. (3) AND (4). PERFORMED OPERATIONAL TEST OF NR 1 AND NR 2 ENGINE FAN AIR VALVES IAW AMM 36-11-54-790-050 AND 36-1 2 L 7 2 4F RT A28NM 2007081500173 20070815 00173 SO 2007 8 15 SWIA200718555 1 20070730 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 564SW 10965 10965 120339 SEVERAL EMERGENCY LIGHTS ARE INOP, FLIGHT NR 3684. REPLACED CENTER EMERGENCY LIGHT BATTERY IAW MM 33-50-02. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007081500174 20070815 00174 WP 2007 8 15 IXXA07SMN166S 1 20070630 A 5330 SKIN DOUG DC8 DC873F 302199F WP ZONE 100 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT FS 380 LONGERON 33RIGHT, RIGHT FORWARD FUSELAGE JUST AFT OF A-PIT DOOR OPENING. AVERAGE AND MAXIMUM RIVET SPACING EXCEEDED. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION AFTER CUT. FABRICATED NEW S KIN, EXTERNAL, AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW FAA FORM 8110-3 NUMBER 07330 DATED 07-18-07, DRAWING SEMAN NUMBER ED 4570 REVISION "04" DATED 06-25-07, D C8 SRM 51-1-21, SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, FORM SEMAN 242-2, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND SRM 2 L 7 4 4F RT 4A25 2007081500177 20070815 00177 WP 2007 8 15 IXXA07SMN184S 1 20070630 A 5340 3750498U1 FITTING DOUG DC8 DC873F 302199F WP BS 660 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND MID SHIP ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 660.000 LONGERON 35LE FT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING BETWEEN STATION 660.000 AND LONGERON 35LEFT IAW DC8 SRM 51-1-20D, 5 1-3-1. 2 L 7 4 4F RT 4A25 2007081500178 20070815 00178 EU 2007 8 15 TRBA2007061 1 20070728 A 2611 E028402840 RELAY AEROSP ATR72 ATR72212A 8680902 EU SMOKE DETECTION INTERMITTENT A TRBA O OTHER N FALSE WARNING DE DESCENT 1 SO 29 529AM 529 AFT SMOKE WARNING ILLUMINATED DURING DESCENT, IT WAS A FALSE WARNING. REMOVED AND REPLACED RELAY FIN NR 170WW AND PERFO RMED OPT CK IAW JIC NR 26-15-00 AND FOUND WORKING PROPERLY. 2 H 7 2 4T RT A53EU 2007081500179 20070815 00179 NM 2007 8 15 CALA0700406 1 20070803 A 5311 6546557 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 887, S9R. REPAIRED IAW ECRA 5310-04643. 2 L 7 2 4F RT A16WE 2007081500181 20070815 00181 2007 8 15 HALA0700317 4 20070730 A 3420 UNKNOWN BOEING 767 7673G5 1385126 NM UNKNOWN A HALA K NONE O OTHER AP APPROACH 1 WP 13 584HA 24258 ETOPS SIGNIFICANT SYSTEM, STANDBY ATT IND G/S AND LOC FLAGS STAY IN VIEW. ON ARRIVAL NO FLAG IN VIEW PERFORMED BITE CHE CK ON BOTH MMR RECEIVERS, PASS PERFORMED MCDP TEST 40, PASS A/C LMP STATUS REMAIN IN LAND 3. 2 L 7 2 4F RT A1NM 2007081500184 20070815 00184 NE 2007 8 15 HALA0700321 2 20070802 A 7310 7321330001 ACTUATOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE FUEL VALVE INOPERATIVE A HALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 13 594HA 5713 5713 23275 ETOPS SIGNIFICANT SYSTEM, NR 2 ENG WOULD NOT START AFTER LEAK CK. FOUND NR 2 ENG FUEL VALVE ACTUATOR INOP. REPLACED EN G VLV WITH BORROWED AA PART PER AMM 76-11-04-4. RAN ENG. CKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007081500185 20070815 00185 NM 2007 8 15 CALA0700409 1 20070803 A 5311 65C25229 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 727D, S9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04643. 2 L 7 2 4F RT A16WE 2007081500186 20070815 00186 2007 8 15 HALA0700320 4 20070801 A 3422 POWER SUPPLY BOEING 767 767332 1382001 NM WEU UNKNOWN A HALA O OTHER O OTHER CR CRUISE 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM, ADFS LIMIT MODE SPD LIM ANNUNCIATED ON F/O EADI (A/T) MODE BEFORE SPEED LIMIT IS APPROACHED. F/O MMO INDICATOR (RED BARS) MISSING REF. AFTER REPLACEMENT OF WEU POWER SUPPLY MODULE "A" T/S PER FIM 34-12-00 AND NO FAULTS NOTED. ACCOMPLISHED TEST 30 AND CK OK, A/C REMAINS IN LAND 3 STATUS. 2 L 7 2 4F RT A1NM 2007081500187 20070815 00187 NM 2007 8 15 HALA0700316 1 20070801 A 2612 NONE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE FIRE LOOP NONE A HALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM - LT ENG FIRE LOOP 2 ILLUMINATED ON EICAS. PERFORMED FIM 26-11-00 FIG 105. SYSTEM TEST OK. O K FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007081500188 20070815 00188 NM 2007 8 15 CALA0700410 1 20070803 A 5330 6545775 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A .25 INCH CRACK IN RIGHT FUSELAGE SKIN ABOVE SKIN LAP S25R APPROXIMATELY 6 INCHES FORWARD OF STA 887. THE SKIN WAS REPAIRED IAW SRM 53-00-01, PRODECURE 5, PAGE 203, REPAIR 31. 2 L 7 2 4F RT A16WE 2007081500191 20070815 00191 NM 2007 8 15 CALA0700412 1 20070805 A 5322 6546530 SHEAR TIE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND SHEAR TIE CORRODED AT STA 460 BETWEEN STRINGERS 27R AND S28R. THE SHEAR TIE WAS REPAIRED IAW SRM 53-00 -07. 2 L 7 2 4F RT A16WE 2007081500195 20070815 00195 NM 2007 8 15 HALA0700319 1 20070801 A 2410 INDICATOR BOEING 767 767332 1382001 NM IDG POPPED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM, NR 1 ENG IDG DPI POPPED, FOUND ON OVERNIGHT. ACCOMPLISHED AMM 24-11-01, 8-1-07, 6091 LEAK CK OF FILTER AND MAG DRAIN PLUG AND RESERVICE AFTER ENG RUN PENDING. OPS CK LK CK OF FILTER MAG DRAIN PLUG OIL QUANTITY CK OK FOR SVC. NO FAULTS NOTED ON EICAS. 2 L 7 2 4F RT A1NM 2007081500197 20070815 00197 SO 2007 8 15 C2XA07CL065 1 20070803 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO FWD CARGO BAY FAULTY A C2XA K NONE N FALSE WARNING TO TAKEOFF 1 SW 27 15572 3252 646 145636 CLE FLIGHT 2932 - THE CREW REPORTED A -BAG SMOKE- WARNING BRIEFLY ON THE EICAS IN FLIGHT. THE BAG COMPARTMENT WAS CHECK ED AND NO SMOKE OR FIRE WAS DETECTED. MAINTENANCE INSPECTED AND REPLACED THE FORWARD BAG SMOKE DETECTOR. OPERATIONAL C HECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007081500199 20070815 00199 NM 2007 8 15 DL76P070973 1 20070730 A 3350 20131A BATTERY BOEING 767 767332 1382001 NM EMERGENCY LIGHT UNSERVICEABLE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1402A 25989 AFT RIGHT CEILING EMERGENCY LIGHTS AND EXIT SIGNS INOP. REPLACED ONE FUSE AND BATTERY ON M734 POWER SUPPLY TESTS GOOD. 2 L 7 2 4F RT A1NM 2007081500200 20070815 00200 NM 2007 8 15 DL76S070974 1 20070715 A 5320 FLOOR SUPPORT BOEING 767 767332 1382001 NM STA 999 LBL 33 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 129DL 24079 BS 999 LBL 33 FLOOR SUPPORT FOUND CRACKED. REPAIRED FLOOR SUPPORT PER SRM 53-00-51 REPAIR NR 3 FIG 201. 2 L 7 2 4F RT A1NM 2007081500202 20070815 00202 NM 2007 8 15 DLM90070977 1 20070731 A 5320 CUSP WEB DOUG MD900 MD900 3027375 NM BS 873 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 LT CUSP WEB OUT OF LIMITS, CRACKED AT LIGHTEN HOLE FS 873. REPAIRED CUSP WEB IAW MD-88 SRM 53-05D FIG 827D. 1 G 7 2 3U NC H19NM 2007081500203 20070815 00203 NM 2007 8 15 DLM90070978 1 20070731 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 773 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 LT CUSP WEB OUT OF LIMITS AT LIGHTING HOLE FS 773. REPAIRED CUSP WEB IAW MD88 SRM 53-05D FIG 827D. 2 L 7 2 4F RT A6WE 2007081500208 20070815 00208 SO 2007 8 15 C2XA07RI063 1 20070726 A 2910 14570262403 HYDRAULIC LINE EMB 135 EMB135ER 3260203 SO MLG ACTUATOR LEAKING A C2XA K NONE K FLUID LOSS TO TAKEOFF 1 SW 27 14508 145220 FLT 4923 - EWR - AT MLG RETRACTION, CREW REPORTED THAT RT MLG RETRACTED FASTER THAN LF MLG CAUSING YAW MOTION TO THE RIG HT. EWR MX REMOVED AND REPLACED MLG ACTUATOR EXTENSION LINE AND BLEED THE SYSTEM. MX PERFORMED LG OPERATIONAL CHECK SU CCESSFULLY. ACFT PERFORMED FLIGHT TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007081500212 20070815 00212 NM 2007 8 15 DLM88070988 1 20070624 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 950DL 49881 PUNCTURE ON LT CUSP WEB AT STA Y=986. REPAIRED PER ERA 398191-14MA. 2 L 7 2 4F RT A6WE 2007081500213 20070815 00213 NM 2007 8 15 DLM88070989 1 20070731 A 5312 ANGLE DOUG MD88 MD88 3023688 NM BULKHEAD CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 950DL 49881 CRACKED LT FWD UPPER FACE P-DOME ANGLE BETWEEN LONGERONS 3 AND 4 LT. REPAIRED PER DWG 9915562 REV P ON N/R TOO63359 AT HMV-3. 2 L 7 2 4F RT A6WE 2007081500214 20070815 00214 2007 8 15 C2XA07RI064 4 20070713 A 3160 7014300901 DISPLAY EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 22909 145459 FLT 7756 - SMF - CREW REPORTED CAPTAIN SIDE PFD BLANKED OUT WITH ELECTRICAL SMELL. LAX MX REMOVED AND REPLACED PFD IAW EMB145 AMM 34-22-01 AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007081500216 20070815 00216 NM 2007 8 15 DLM88070990 1 20070624 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 950DL 49881 PUNCTURED ON LT CUSP WEB AT STA Y=819, REPAIRED PER ERA 398191-14MA. 2 L 7 2 4F RT A6WE 2007081500218 20070815 00218 NM 2007 8 15 DLM88070992 1 20070624 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 950DL 49881 EXFOLIATION CORROSION ON LT CUSP WEB AT STA Y=910 TO 921. REPAIRED PER ERA 398191-14MA REVA. 2 L 7 2 4F RT A6WE 2007081500222 20070815 00222 SO 2007 8 15 RAIA00708002 1 20070801 A 3213 SHOCK ABSORBER EMB 145 EMB145LR 3260212 SO MLG LOW A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 838HK 145321 FLT NR 7902 - ALB - "LANDING GEAR AIR/GROUND FAIL" MESSAGE ON EICAS DURING FLIGHT. MAINTENANCE SERVICED MAIN LANDING GE AR SHOCK ABSORBER CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007081500224 20070815 00224 SO 2007 8 15 RAIA00708004 1 20070801 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO EXTERIOR INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 844HK 14500838 PRE FLT NR FLMX - RIC - EMERGENCY LIGHT LEFT FORWARD WING/FUSELAGE FAIRING EXTERIOR FLOOD LIGHT INOP. MAINTENANCE DEFER RED PER MEL. 2 L 7 2 4T RT T00011AT 2007081500225 20070815 00225 SO 2007 8 15 RAIA00708005 1 20070801 A 7830 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT ACTIVATED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 815HK 145048 FLT NR 5530 - BNA - NR 2 T/R DISAGREE MESSAGE ON TAKEOFF. MAINTENANCE DEFERRED PER MEL. 2 L 7 2 4T RT T00011AT 2007081500226 20070815 00226 SO 2007 8 15 RAIA00708006 1 20070802 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 802HK 145066 PRE FLT NR 3551 - SDF - EMERGENCY FLOOR LIGHT INOP AT ROW 6. MAINTENANCE DEFERRED PER MEL. 2 L 7 2 4F RT T00011AT 2007081500230 20070815 00230 NM 2007 8 15 DLM88070996 1 20070622 A 5753 VANE DOUG MD88 MD88 3023688 NM LT TE FLAP MISREPAIRED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 950DL 49881 UNSUITABLE REPAIR ON LT INBD FLAP INBD GUIDE VANE. REPAIRED PER SRM 57-03D. 2 L 7 2 4F RT A6WE 2007081500232 20070815 00232 NM 2007 8 15 DLM88070998 1 20070731 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 950DL 49881 GENERAL CORROSION ON RT CUSP WEB STA Y=1030 TO Y=1036, 1045 TO 1058 AND 1064 TO 1075 TASK CARD 58-53313. REPAIRED PER E RA 398191-14MA ON N/R T0062851 AT HMV-3. 2 L 7 2 4F RT A6WE 2007081500234 20070815 00234 SO 2007 8 15 RAIA00708010 1 20070803 A 3297 D3899926FA98SN CONNECTOR EMB 145 EMB145EP 3260221 SO LANDING GEAR UNKNOWN A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 826HK 145016 FLT NR 5530 - STL - LANDING GEAR AIR/GROUND FAIL IN-FLIGHT. MAINTENANCE REMOVED AND REPLACED WEIGHT ON WHEEL LEFTHAND P ROX SWITCH CONNECTORS NR 1 AND NR 2 CHECKS GOOD. 2 L 7 2 4F RT T00011AT 2007081500235 20070815 00235 SO 2007 8 15 RAIA00708011 1 20070803 A 2421 GENERATOR EMB 145 EMB145LR 3260212 SO NR 3 & 4 DISCONNECTED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 819HK 145062 FLT NR 5507 - STL - GENERATOR NR 3 & 4 DISCONNECTED FROM SYSTEM IN FLIGHT, NO EICAS ASSOCIATED MESSAGES. MAINTENANCE PE RFORMED OPS CHECK OF ALL GENERATORS, NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2007081500236 20070815 00236 NM 2007 8 15 DLM88070999 1 20070731 A 5315 FLOORBEAM DOUG MD88 MD88 3023688 NM FUSLEAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 950DL 49881 FOUND CRACKED FLOOR SUPPORT AT STATION Y=905, X =42. REPAIRED PER DWG 9923417 ON N/R T0062835 AT HMV-3. 2 L 7 2 4F RT A6WE 2007081500237 20070815 00237 NM 2007 8 15 DLM88071000 1 20070731 A 5315 FLOORBEAM DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 950DL 49881 CRACKED FRAME AT FLOORBEAM JOINT STA Y=864 X=56. REPAIRED PER DWG SR 09530282 ON N/R T0062703 AT HMV-3. 2 L 7 2 4F RT A6WE 2007081500240 20070815 00240 SO 2007 8 15 RAIA00708013 1 20070804 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO CABIN NOT SEATED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 821HK 145068 PRE FLT NR 5493 - STL - EMERGENCY LIGHT SERVICE DOOR EXIT MARKER IS OUT. MAINTENANCE RESEATED CONNECTOR IN OVERHEAD PAN EL, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007081500241 20070815 00241 EU 2007 8 15 AWXA200700950 1 20070731 A 2420 SENSOR AIRBUS 320 A320231 3930325 EU RT GENERATOR FAILED A AWXA O OTHER J WARNING INDICATION CR CRUISE 1 WP 28 644AW 317 SEA - LAS - EL - LOG 7757269 - AT CRUISE, THE CREW REPORTED THE RT ENGINE GENERATOR HAD DROPPED OFF LINE. THE APU WAS O N MEL. THE CREW DECLARED AN EMERGENCY. THE LANDING WAS UNEVENTFUL. MX REPLACED SENSOR 50XU2 PER MM 24-22-18. OPERATI ONAL CHECK WAS GOOD DURING ENGINE RUN-UP. THE A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2007081500244 20070815 00244 SO 2007 8 15 C2XA07TY042 1 20070806 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13913 145438 THE RIGHT EMERGENCY LIGHT OVER THE WING IS INOP. REMOVED AND REPLACED THE BULB IAW EMB 145 MM 33-30-07 OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007081500245 20070815 00245 EU 2007 8 15 AWXA200700951 1 20070731 A 2710 SERVO VALVE AIRBUS 320 A320231 3930325 EU LT AILERON LEAKING A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 620AW 052 DFW - PHX - EL - LOG 7827212 - CREW REPORTED, DURING CRUISE THEY RECEIVED A GREEN HYD RESERVOIR LOW LEVEL ECAM MESSAGE. THE CREW DECLARED AN EMERGENCY. THE LANDING WAS UNEVENFUL. MX REPLACED THE LEFT AILERON SERVO VALVE DUE TO IT LEAKING . OPERATIONAL/LEAK CHECK WAS GOOD. THE A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2007081500246 20070815 00246 SO 2007 8 15 C2XA07ON16 1 20070806 A 3350 SIGN EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12569 145630 FLT MX - ONT MX HANGAR - WHILE PERFORMING A TEST ON EMERGENCY LIGHTS, MX PERSONNEL FOUND EMERGENCY EXIT SIGN AT AFT GALL EY FACING PASSENGER CABIN THAT DOES NOT ILLUMINATE. MX PERSONNEL RESET EMERGENCY LIGHT SYSTEM AND FOUND THE EMERGENCY E XIT SIGN AT AFT GALLEY FACING PASSENGER CABIN TO ILLUMINATE. OPERATIONALLY CHECK GOOD AND AIRCRAFT WAS RELEASE TO RETUR N FOR SERVICE IN AIRWORTHY CONDITIONS. 2 L 7 2 4T RT T00011AT 2007081500247 20070815 00247 GL 2007 8 15 C2XA07SH043 2 20070804 A 7230 14575001409 CASE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 ENGINE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 21537 145523 SHV - DURING C-CHECK MAINTENANCE FOUND NR 1 ENGINE FAN CASE ASSY & ENGINE INLET MOUNTING ATTACHMENT BOLTS HOLES WITH COR ROSION. MAINTENANCE REPAIRED NR 1 ENGINE FAN CASE ASSY & ENGINE INLET ATTACHMENT BOLT HOLES IAW EC5420-01097. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007081500250 20070815 00250 WP 2007 8 15 ABXA070254 1 20070804 A 3040 30631 THERMAL SWITCH DOUG DC9 DC941 302207N WP COCKPIT DEFECTIVE A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 23 979AX 47492 DURING DESCENT INTO PIE, THERE WAS A ELECTRICAL SMELL IN THE COCKPIT NEAR FIRST OFFICER'S CLEARVIEW WINDOW. INSPECTED W IRING BEHIND RIGHT CONSOLE, OVERHEAD CONSOLE AND WIRING HARNESS IN E & E COMPARTMENT. NO BURNT OR DAMAGED WIRING NOTED. SUSPECT FIRST OFFICER'S CLEARVIEW WINDOW THERMAL SWITCH. REPLACED THERMAL SWITCH IAW DC9 MM 30-41-02. 2 L 7 2 4F A6WE 2007081500251 20070815 00251 SO 2007 8 15 C2XA07ON016 1 20070806 A 3350 375921 SIGN EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12569 145630 FLT MX - ONT MX HANGAR - WHILE PERFORMING A TEST ON EMERGENCY LIGHTS, MX PERSONNEL FOUND EMERGENCY EXIT SIGN AT AFT GALL EY FACING PASSENGER CABIN THAT DOES NOT ILLUMINATE. MX PERSONNEL RESET EMERGENCY LIGHT SYSTEM AND FOUND THE EMERGENCY E XIT SIGN AT AFT GALLEY FACING PASSENGER CABIN TO ILLUMINATE. OPERATIONALLY CHECK GOOD AND AIRCRAFT WAS RELEASE TO RETUR N FOR SERVICE IN AIRWORTHY CONDITIONS. 2 L 7 2 4T RT T00011AT 2007081500252 20070815 00252 SO 2007 8 15 C2XA07RI065 1 20070719 A 3350 375921 SIGN EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 11536 145520 FLT 2686 - EWR - CREW REPORTED GALLEY EMERGENCY LIGHT (SEAT 1A) INOP. EWR MX REMOVED AND REPLACED EMERGENCY SIGN AND PE RFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007081300017 20070813 00017 NM 2007 8 13 SWAA073816 1 20070731 A 5311 6546554 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300024 20070813 00024 NM 2007 8 13 SWAA073798 1 20070731 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300048 20070813 00048 NM 2007 8 13 SWAA073823 1 20070731 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 703SW 27837 DURING SCHEDULED HC1 CHECK, AFT LT EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007081300057 20070813 00057 NM 2007 8 13 SWAA073835 1 20070801 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 328, STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300067 20070813 00067 NM 2007 8 13 SWAA073863 1 20070801 A 5322 6546546 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007081300081 20070813 00081 NM 2007 8 13 SWAA073873 1 20070801 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 22L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007081300091 20070813 00091 2007 8 13 SWAA073868 4 20070801 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007081300100 20070813 00100 NM 2007 8 13 SWAA073896 1 20070802 A 5311 6546552 FRAME BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300103 20070813 00103 NM 2007 8 13 SWAA073901 1 20070802 A 5310 6547955 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 2 STOP. REPAIRED FRAME PER ACO. 2 L 7 2 4F RT A16WE 2007081300107 20070813 00107 NM 2007 8 13 SWAA073885 1 20070802 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300108 20070813 00108 NM 2007 8 13 SWAA073883 1 20070802 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300110 20070813 00110 NM 2007 8 13 SWAA073886 1 20070802 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007081300117 20070813 00117 NM 2007 8 13 SWAA073900 1 20070802 A 3350 MS155721 LIGHT BOEING 737 7373A4 1384585 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007081300123 20070813 00123 EA 2007 8 13 COMA0760507 1 20070731 A 3250 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING MALFUNCTIONED A COMA K NONE N FALSE WARNING CR CRUISE 1 SO 01 995CA 7229 FLIGHT 5181 - NWS INOP CAUTION MESSAGE 3 TIMES IN ROUTE. PERSISTED AFTER QRH PROCEDURE. AIRCRAFT LANDED SAFELY IN MEM. RESET NWS WITH NO FAULTS FOUND IN NWS ECU. TAXI CHECK GOOD. 2 L 7 2 4F RT A21EA 2007081300124 20070813 00124 EA 2007 8 13 COMA0760508 1 20070731 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 786CA 7333 FLIGHT 5298 - FLAPS FAIL MESSAGE DURING RETRACTION. LEVER WAS AT 20 DEGREES. FAILURE WAS AT 28 DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENACE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS R ESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007081300128 20070813 00128 NM 2007 8 13 SWAA073910 1 20070803 A 5310 6516352 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT UPPER INBOARD CORNER. REPAIRED FRAME PER S RM. 2 L 7 2 4F RT A16WE 2007081300132 20070813 00132 NM 2007 8 13 SWAA073916 1 20070805 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 460, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300141 20070813 00141 NM 2007 8 13 SWAA073912 1 20070804 A 3350 MS155721 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 261WN 32517 DURING SCHEDULED MV1 CHECK, FOUND AFT RIGHT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007081300143 20070813 00143 NM 2007 8 13 SWAA073922 1 20070806 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 RIGHT OVERWING EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007081300150 20070813 00150 NM 2007 8 13 SWAA073929 1 20070806 A 5322 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 967, BL 0. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007081300152 20070813 00152 NM 2007 8 13 SWAA073927 1 20070806 A 2560 P4010021 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 726SW 27858 DURING SCHEDULED MV1 CHECK, FOUND AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERIES PER MM . 2 L 7 2 4F RT A16WE 2007081300159 20070813 00159 NM 2007 8 13 SWAA073942 1 20070807 A 5512 6573782 SKIN BOEING 737 7373T5 1384608 NM HORIZ STAB DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED 22Y CHECK, FOUND LEFT HORIZONTAL STAB OUTBOARD T/E LOWER SKIN SURFACE DELAMINATED. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 2007081300167 20070813 00167 NM 2007 8 13 SWAA073948 1 20070808 A 5311 6546538 FRAME BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007081300170 20070813 00170 NM 2007 8 13 SWAA073947 1 20070808 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER 24R CORRODED AT BS 357. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007081300172 20070813 00172 2007 8 13 SWAA073950 4 20070808 A 2565 D31354 SLIDE BOEING 737 7373K2 13844BA NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007081300187 20070813 00187 2007 8 13 ZZDA2007254 4 20070805 A 2565 PIN BOEING 717 717200 1383700 NM EVAC SLIDE MISSING A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 920AT 2468 55083 L1 SLIDE PACK MISSING A PIN. REMOVED AND REPLACED L1 DOOR SLIDE REF 25-61-01. 2 L 7 2 4F TR A6WE 2007081300193 20070813 00193 NM 2007 8 13 NOCA14407 1 20070725 A 3350 BPS73 POWER SUPPLY BOEING 767 76736N 1385152 NM CABIN DISCHARGED A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 768NA 29898 EMERGENCY LIGHTS INOP AT ROW 20-24. REMOVED AND REPLACED POWER SUPPLY AS PER MM 33-51-07. 2 L 7 2 4F RT A1NM 2007081300200 20070813 00200 WP 2007 8 13 ASAA0781915 1 20070730 A 5321 INSERT DOUG DC9 DC983 3022083 WP FLOOR PANEL DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 CABIN FLOOR PANEL HAS BROKEN AND CORRODED INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007081300202 20070813 00202 WP 2007 8 13 ASAA0781917 1 20070730 A 5321 INSERT DOUG DC9 DC983 3022083 WP FLOOR PANEL CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 FLOOR PANEL HAS CORRODED INSERTS. REPLACED PANEL PER SRM 53-24-0 AND 53-05. 2 L 7 2 4F RT A6WE 2007081300203 20070813 00203 WP 2007 8 13 ASAA0781918 1 20070730 A 5321 INSERT DOUG DC9 DC983 3022083 WP FLOOR PANEL CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 CABIN FLOOR PANEL HAS CORRODED INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007081400022 20070814 00022 EA 2007 8 14 SWIA200718538 1 20070727 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 438SW 7574 REAR CEILING EMERGENCY LIGHT OUT. REPLACED LAMP. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007081400023 20070814 00023 SO 2007 8 14 SWIA200718539 1 20070728 A 5753 SKIN EMB 120 EMB120ER 3260203 SO RT TE FLAP CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 250YV 120250 RIGHT NACELLE FLAP HAS A CRACK ON THE UPPER SURFACE SKIN. REPLACED RIGHT NACELLE FLAP WITH SERVICEABLE UNIT IAW MM 27-5 0-03. 2 L 7 2 4T RT A31SO 2007081500002 20070815 00002 WP 2007 8 15 ASAA0781920 1 20070730 A 5321 993665147 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 FLOOR PANEL TOP PLY DISBONDED. BOND REPAIRED WITH GLASS CLOTH PER SRM 51-90-0. 2 L 7 2 4F RT A6WE 2007081500010 20070815 00010 NM 2007 8 15 CALA0700391 1 20070801 A 5314 6562125 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND LEFT KEEL BEAM CORRODED IN A/C DISTRIBUTION BAY AT STA 500D-520. THE KEEL BEAM WAS REPAIRED IAW SRM 53 -30-12, FIGURE 201. 2 L 7 2 4F RT A16WE 2007081500012 20070815 00012 EA 2007 8 15 SWIA200718546 1 20070725 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 730SK 10193 FLT 6733 - 3 EMERGENCY LIGHTS NEAR GALLEY SERVICE DOOR ARE INOP. REPLACED EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-00. OP S CHECK GOOD. 2 L 7 2 4F RT A21EA 2007081500025 20070815 00025 NM 2007 8 15 P5CA0701528 1 20070729 A 2150 UNKNOWN BOEING 747 74746NF 13848BT NM CARGO OVERTEMP UNKNOWN A P5CA D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 EA 15 454PA 30812 EQUIPMENT COOLING EICAS MSG DISPLAYED DURING PUSHBACK FOLLOWED BY "E/E COOLING CARD" EICAS. A/C RETURN TO GATE. A/C TE MP IN FWD CARGO COMP HAD INCREASED TO 37°C. A/C SHUTDOWN AND COOLED W/ AN AC CART FOR 30 MIN. ALL MSGS CLEARED PER AMM 21-23-00 AND 12-01-00. A/C MX RD AT 0200Z/29. 2 L 7 4 4F RT A20WE 2007081500032 20070815 00032 NM 2007 8 15 DHL2007784537 1 20070731 A 5330 SKIN BOEING 727 727227 1384078 NM ZONE 100 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 BLIND FASTENERS INSTALLED IN REPAIR AT STA 1194, STR 19R. REMOVED BLIND FASTENERS ON REPAIR IAW B727 SRM 51-30-2. CUT 4 ACCESS HOLE IN AFT AIRSTAIRS STA 1194 RBL 60 AT TORQUE BOX UPR WEB IAW B727 SRM 51-40-2. OVER SIZED BLIND FASTENER HOL ES .03125 IAW B727 SRM 53-30-3, FIG 27. HFEC HOLES IAW B727 NDTM PT.6, 51-00-00, NO DEFECTS NOTED. TREATED, PRIMED AND INSTALLED SOLID FASTENERS IAW B727 SRM 51-10-2, 51-30-2 AND 53-30-3, FIG 5. FAB`D DOUBLER FOR ACCESS FROM 7075T6, .040 , 6 BY 6 IAW B727 SRM 53-10-3, FIG 1 AND 51-40-2, FIG 1. TREATED, PRIMED AND INSTALLED DOUBLER IAW B727 SRM 51-10-2 AND 51-30-2.THIS REPAIR IS A CATEGORY B IAW B727 SRM 53-30-3, PG.20. 2 L 7 3 4F A3WE 2007081500033 20070815 00033 NM 2007 8 15 DHL2007784538 1 20070731 A 5330 SKIN BOEING 727 727227 1384078 NM ZONE 100 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 BLIND FASTENERS INSTALLED IN REPAIR AT STA 1215, BL 0. REMOVED BLIND FASTENERS ON REPAIR IAW B727 SRM 51-30-2. CUT 4 A CCESS HOLE IN AFT AIRSTAIRS STA 1194 RBL 60 AT TORQUE BOX UPPER WEB IAW B727 SRM 51-40-2. OVER SIZED BLIND FASTENER HOL ES .03125 IAW B727 SRM 53-30-3, FIG 27. HFEC HOLES IAW B727 NDTM PT.6, 51-00-00, NO DEFECTS NOTED. TREATED, PRIMED AN D INSTALLED SOLID FASTENERS IAW B727 SRM 51-10-2, 51-30-2 AND 53-30-3, FIG 5. THIS REPAIR IS A CATEGORY B IAW B727 SRM 53-30-3, PG 6. 2 L 7 3 4F A3WE 2007081500035 20070815 00035 NM 2007 8 15 C8GA20070006 1 20070608 A 7997 BACC63BD12SC3S CONNECTOR BOEING 727 727227 1384078 NM PWA JT8 JT8D15A 52051 NE TEMP BULB LOOSE A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 308AS 55728 22002 687407 FLT 716 FROM TOL TO MEM, AFTER TAKEOFF, NR 2 ENGINE OIL TEMPERATURE PEGGED HIGH. CREW PERFORMED PRECAUTIONARY ENGINE SH UT DOWN, DECLARED EMERGENCY, AND RETURNED TO TOL. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND OIL TEMP BULB CONNECTOR BACKED OFF. RESECURED CONNECTOR. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2007081500040 20070815 00040 NM 2007 8 15 C8GA20070007 1 20070727 A 2797 4816R147S CONNECTOR BOEING 727 727225 1384077 NM TE FLAPS DIRTY A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 755DH 21857 FLT 738 FROM SLW TO GDL, DURING CLIMB-OUT FROM SLW, THE INBOARD FLAPS WOULD NOT RETRACT BEYOND 15 DEGREES. APPROPRIATE CHECKLIST WAS FOLLOWED AND THE AIRCRAFT RETURNED TO SLW WHERE IT LANDED WITHOUT INCIDENT. ON POST FLIGHT PERFORMED THOR OUGH INSPECTION CHECK OF INBOARD TRAILING EDGE FLAP SYSTEM, FOUND BYPASS VALVE CONNECTOR CONTAMINATED. CLEANED CONNECTO R AND RESET FLAP POSITION INDICATOR CIRCUIT BREAKERS, CYCLED FLAPS SEVERAL TIMES, OPS CHECK GOOD. NO OTHER DEFECTS NOTE D. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2007081500041 20070815 00041 NM 2007 8 15 AWXA200700938 1 20070705 A 5313 6545768210 STRINGER BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961294, CRACKED STRINGER, BS 500C + 5", S16R. REPAIRED STRINGER, BS 500C + 5", S1 6R IAW AWA ER 03-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2007081500051 20070815 00051 NM 2007 8 15 AALA20071318 1 20070717 A 3397 WIRE DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 951TW 53470 LGA - EMERGENCY LIGHT AT SEAT ROW 17 INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHT AT SEAT ROW 17. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT 2007081500058 20070815 00058 NM 2007 8 15 KCSA071275 1 20070802 A 5330 SKIN BOEING 747 7472B4B 138481B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA 700 TO 720 STR 41R SKIN DAMAGED. 2 L 7 4 4F RT A20WE 2007081500059 20070815 00059 NM 2007 8 15 KCSA071276 1 20070802 A 5311 FRAME BOEING 747 7472B4B 138481B NM FUSELAGE CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 APU PNEUMATIC DUCT SUPPORT CLAMP IS CHAFING INTO FRAME AT STA 2460 WL 260. 2 L 7 4 4F RT A20WE 2007081500067 20070815 00067 NM 2007 8 15 AALA20071337 1 20070721 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 790AN 30251 MIA - EMERGENCY EXIT LIGHT AT SEAT ROW 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT LIGHT AT SEAT ROW 23C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007081500071 20070815 00071 NM 2007 8 15 AALA20071329 1 20070718 A 3350 LIGHT BOEING 737 737823 13844BZ NM SEAT ROW 10D INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 939AN 30883 DFW - EMERGENCY EXIT LIGHT AT SEAT ROW 10D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT ROW 10D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007081500075 20070815 00075 NM 2007 8 15 UPS07550375 1 20070802 A 3350 LIGHT BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 446UP 27735 INSPECTION TYPE:N/A EIGHT LAMPS INOP IN EMERGENCY LIGHT ASSEMBLY. RELAMPED EIGHT LAMPS IN EMERGENCY LIGHT ASSEMBLY PER MM 33-51-01-2. 2 L 7 2 4F RT A2NM 2007081500077 20070815 00077 WP 2007 8 15 UPS07850371 1 20070724 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 FLOORBEAM STA 1300 RBL 24 CRACKED AND CORRODED. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER & DO UBLER IAW SRM 5 3-2-0, 51-02-00 FIG 1, 51-1-8, 51-1-20D, AND DWG 2759472. 2 L 7 4 4F RT 4A25 2007081500082 20070815 00082 NM 2007 8 15 AALA20071327 1 20070718 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 789AN 30252 DFW - EMERGENCY EXIT LIGHT AT MID GALLEY LEFT AISLE INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT LIGHT AT MID GALLEY L EFT AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007081500100 20070815 00100 EA 2007 8 15 TRAX200701089 1 20070730 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 872AS 7542 SERVICE DOOR WILL NOT CLOSE. 2 L 7 2 4F RT A21EA 2007081500107 20070815 00107 NM 2007 8 15 07FDEA02703 1 20070801 A 5740 ARB76112 FITTING DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 RT WING LOWER WINGLET AFT FITTING FORWARD AND AFT HOLES FOUND CORRODED. [08-17-07] REPAIRED AS PER FEDEX EA 1-5730- 114786, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007081500109 20070815 00109 NM 2007 8 15 07FDEA02705 1 20070801 A 5347 AFA77953 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 AFTER CEILING PANEL REMOVED, FOUND MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STA 1756, X = -8.5 CORRODED. [08-15-07] REPAIRED BY REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007081500121 20070815 00121 NM 2007 8 15 KCSA071278 1 20070804 A 5320 WEB BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA 664 TORQUE BOX WEB IS CRACKED 2 INCHES AT RBL 36 WL 118. 2 L 7 4 4F RT A20WE 2007081500127 20070815 00127 NM 2007 8 15 CALA0700393 1 20070803 A 5311 654795978 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND AFT BAGGAGE BIN FRAME CORRODED AT STA 794.3, S25R TO S26R. A NEW FRAME WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007081500128 20070815 00128 NM 2007 8 15 07FDEA02724 1 20070802 A 5310 65C2029617 CREASE BEAM BOEING 727 727233 138408A NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LT AFT FUSELAGE UNDER REMOVED CENTER ENG SUPPORT EXT SKIN PANEL, CREASE ANGLE IS CRACKED UNDER TRIANGULAR RIB, UPPER IB CORNER ATTACHED TO OB SIDE OF VERT STAB SKIN BS 1360 THE CREASE CHORD WAS REPAIRED REF EO NR 7-5530-7-2303 PRT 5, REV Q. JPF STEPS 20-30 AND SRM 51-40-03 FIG, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007081500143 20070815 00143 EU 2007 8 15 07FDEA02734 1 20070725 A 5347 A5381310620010 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 NR 2 RT SEAT TRACK BETWEEN FR 38.2 AND FR 40 AT Y-450 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM SUPP 53-15-15. 2 L 7 2 4F RT A35EU 2007081500155 20070815 00155 EU 2007 8 15 07FDEA02746 1 20070803 A 5310 A53978267208 CROSSBEAM AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 AFTER BLENDING CORROSION ON CROSSBEAM C67 RT, Y-1200 WAS OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT IAW SRM 51-72-10 . 2 L 7 2 4F RT A35EU 2007081500158 20070815 00158 EU 2007 8 15 07FDEA02751 1 20070712 A 5347 A5327478820400 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 N00547 MDCC - SEAT TRACK AT YO FOUND CORRODED BETWEEN FR 58 AND FR 72. SEAT TRACK WAS REPAIRED IN ACCORDANCE SRM 53-10 -16 FIG 202. 2 L 7 2 4F RT A35EU 2007081500159 20070815 00159 EU 2007 8 15 07FDEA02752 1 20070710 A 5347 A5327923620200 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 N00577 MDCC - SEAT TRACK FOUND CORRODED AT Y1137 BETWEEN FR74/80. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-1 0. 2 L 7 2 4F RT A35EU 2007081500175 20070815 00175 WP 2007 8 15 IXXA07SMN179S 1 20070630 A 5522 SKIN DOUG DC8 DC873F 302199F WP ZONE 300 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON LEFT ELEVATOR ON LOWER SKIN AT STATION XE 39.188. REMOVED F ASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN AND FINGER DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS AND NEW FASTENERS FROM STATION XAR 0 TO STATION XE 132.000. PERFORMED BALANCE TO LEFT ELEVATOR AND FOUND TO BE WITHIN ALLOWABLE TOLERANCE LIM ITS. MOMENT 1450.87 IN LBS IAW DC8 SRM 51-4-4 PAGES 1-2. DC8 SRM 55-1-0 FIGURE 1, DC8 SRM 51-1-21, DC8 SRM 55-4-1 FIGUR E 1 SHEETS 1AND2 ITEM "E" AND "F", DOUGLAS DRAWING NUMBER 5654970-5, DC8 SRM 51-1-9, DC8 SRM 51-1-8B, 2 L 7 4 4F RT 4A25 2007081500176 20070815 00176 NM 2007 8 15 QXEA200701231 1 20070802 A 2497 CONTACTOR DHAV DHC8 DHC8202 2809007 NM NR 1 AC DAMAGED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 349PH 486 SEA FLIGHT NR 2070 WITH NR 1 FEATHERED AND NR 2 UNFEATHERED THE LEFT TRU CAUTION ILLUMINATED. WITH NR 2 FEATHERED AND N R 1 UNFEATHERED THE LIGHT WAS NOT ILLUMINATED. FOUND NO AC POWER ON LEFT BUSS WHILE NR 1 AC GENERATOR OFF LINE AND NR 2 GENERATOR ON LINE. REMOVED AND REPLACED NR 1 AC CROSS TIE CONTACTOR 24-21-K1. PERFORMED FUNCTION TEST OF THE AC GENER ATOR SYSTEM IAW -8 Q200 AMM 24-21-00-720-801. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007081500183 20070815 00183 NM 2007 8 15 HALA0700322 1 20070801 A 2410 IDG BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 LEAKING A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 236277 ETOPS SIGNIFICANT SYSTEM, NR 1 ENG IDG DPI POPPED, FOUND ON OVERNIGHT. ACCOMPLISHED AMM 24-11-01. LEAK CK OF FILTER AN D MAG DRAIN PLUG AND RESERVICE AFTER ENG RUN PENDING. OPS CK LK CK OF FILTER MAG DRAIN PLUG OIL QUANTITY CK OK FOR SVC. NO FAULTS NOTED ON EICAS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007081500205 20070815 00205 NM 2007 8 15 DL75E070979 1 20070801 A 5730 112N310118 SKIN BOEING 757 7572Q8 1384972 NM WING DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 702TW 28162 DAMAGE LED TO A 0.500" OVERSIZED WING SKIN HOLE AND A 0.310" OVERSIZED STRINGER U-9.5 HOLE AT A COMMON FASTENER LOCATION JUST INBD OF WING STATION 537 (3RD NEW FASTENER FROM RIB NR 17). REPAIR CONSISTED OF A COUNTERSUNK FREEZE PLUG AND AN OVERSIZED FASTENER. THIS REPAIR RELATES TO THE APB BLENDED WINGLET PROGRAM MODIFICATION AND INSTALLATION. 2 L 7 2 4F RT A2NM 2007081500206 20070815 00206 NM 2007 8 15 DL76G070980 1 20070801 A 3610 361002241 SHUTOFF VALVE BOEING 767 767332 1382001 NM NR 2 ENGINE INOPERATIVE A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 177DZ 29698 RTO DUE TO HPSOV MESSAGE, RT HPSOV LOCKED OUT PER MEL 36-11-02 AND STEP 3 STATES BLEED LIGHT MAY ILLUMINATED AND R ENG H PSOV MESSAGE MAY DISPLAY. THIS IS WHAT CREW HAD. REPLACED HPSOV VALVE PER AMM. ALSO, REACTIVATED RT THRUST REVERSER P ER AMM. OPS CK OK ENG RUN. 2 L 7 2 4F RT A1NM 2007081500211 20070815 00211 NM 2007 8 15 DLM88070987 1 20070731 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 950DL 49881 EXFOLIATION CORROSION ON LT CUSP WEB FROM STA Y=1174 TO Y=1193, TASK 46-53305. REPAIRED PER ERA 398191-14MA ON N/R T00 63373 AT HMV-3. 2 L 7 2 4F RT A6WE 2007081500249 20070815 00249 GL 2007 8 15 C2XA07RI062 2 20070806 A 7250 BLADE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 ENGINE FAILED A C2XA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SW 27 15986 145254 CAE311433 FLT 2497 CREW REPORTED ENGINE NR 1 UNCOMMANDED IN-FLIGHT SHUTDOWN ON CLIMBING. CREW PERFORMED AIR RETURN AND LANDED UNE VENTFULLY. MX PERFORMED TROUBLESHOOTING AND DETERMINED ENGINE NR 1 NEEDS REMOVED AND REPLACED. 10-9-07 ENGINE WAS SEN T TO ROLLS ROYCE FOR REPAIR. DURING ENGINE REPAIR, IT WAS FOUND THAT THE HCF FAILURE OF HPT1 BLADE, P/N 23076976, DUE TO VANE BURN THROUGH. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007081500255 20070815 00255 EU 2007 8 15 AWXA200700953 1 20070725 A 5320 D53480043202 SILL AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 SAL - MAJOR REPAIR - C-06 CHECK - NR 5990462, CORROSION ON THE L2 DOOR CUT OUT LOWER SILL BEAM, BS 3158/FR 66 TO BS 3257 /FR 68. REPAIRED L2 DOOR CUT OUT LOWER SILL BEAM, BS 3158/FR 66 TO BS 3257/FR 68 IAW A320 SRM 53-41-14. 2 L 7 2 4F RT A28NM 2007081500256 20070815 00256 NM 2007 8 15 QXEA200701230 1 20070730 A 7933 304814801 SENSOR BOMBDR DHC8 DHC8402 1390042 NM OIL TEMP MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 407QX 8286 8286 4049 PDX FLIGHT NR 2333: NR 2 ENGINE OIL TEMP NOT REGISTERING. AIRCRAFT DIVERTED. MAINTENANCE REMOVED AND REPLACED NR 2 ENG INE MOT SENSOR AND NR 2 ENGINE FUEL CONT WIRE HARNESS. OPS CHECK GOOD WITH NO FAULTS FOUND. AIRCRAFT RETURNED TO SERVI CE. 2 H 7 2 4T RT A13NM 2007081500257 20070815 00257 NM 2007 8 15 AALA20071362 1 20070727 A 3350 SIGN BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 792AN 30253 MIA - EMERGENCY EXIT SIGN LIGHT AT RIGHT NUMBER THREE DOOR IS BROKEN. REPLACED EXIT SIGN FOR EMERGENCY LIGHT AT RIGHT N UMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007081500261 20070815 00261 SO 2007 8 15 C2XA07IA181 1 20070803 A 3350 78241 INVERTER EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12530 145533 IAH - DURING MAINTENANCE INSPECTION, THE LT & RT EXIT IDENTIFIER LIGHTS ON THE CABIN EXITS AND THE NUMBER FOUR AISLE PAT H LIGHTING STRIP WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTE R, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007081500262 20070815 00262 SO 2007 8 15 C2XA07IA182 1 20070802 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 19554 165 165 145587 AUS - DURING MAINTENANCE INSPECTION, THE FORWARD THREE AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAF T WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007081500263 20070815 00263 SO 2007 8 15 C2XA07RI067 1 20070801 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO LAVATORY INTERMITTENT A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 21129 12262 12262 145703 FLT 2994 - EWR - CREW REPORTED FALSE LAV SMOKE ALARM IN FLIGHT. EWR MX REMOVED AND REPLACED LAV SMOKE SENSOR IAW EMB145 AMM 26-14-01 AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007081500265 20070815 00265 SO 2007 8 15 C2XA07RI066 1 20070801 A 7603 CU09625138 RESOLVER EMB 145 EMB145LR 3260212 SO THRUST LEVER INOPERATIVE A C2XA E ENGINE SHUTDOWN O OTHER TX TAXI/GRND HDL 1 SW 27 14991 145278 FLT 2723 EWR - CREW REPORTED THAT AFTER LANDING T/R DISAGREE & FAILURE MESSAGES ON EICAS. AFTER T/R STOWED ENGINE 1 WEN T TO UNCOMMANDED T/O THRUST. CREW SHUT DOWN THE ENGINE USING FIRE HANDLE. NO ENGINE PARAMETERS WERE EXCEEDED. EWR MX REMOVED AND REPLACED NR 1 THRUST LEVER RESOLVER IAW EMB145 AMM 76-12-01 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. A CFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007081500269 20070815 00269 SO 2007 8 15 C2XA07ON017 1 20070808 A 2752 8855001003 ACTUATOR NA EMB 145 EMB145XR 3260214 SO T/E FLAP DAMAGED A C2XA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED LD LANDING 1 SW 27 12172 7932 7932 858 1450864 FLT 7782 - SJC TO ONT - FLIGHT CREW REPORTED FLAP FAIL ON LANDING AT 33 DEGREES, ATTEMP TO RESET AS PER MX INSTRUCTIONS AND IT GOT STUCK AT 11 DEGREES. MX SET ALL FLAPS AT 9 DEGREES AND THE OPERATING LIMITATIONS WERE NOT TO EXCEED 200 KNOT S AND RELEASED THE AIRCRAFT ON A FERRY PERMIT TO ONT WERE MX PERSONNEL REMOVED BOTH RIGHT I/B FLAP O/B P/N 885500-1003, S/N 00262 TSN 7932 CSN 4237 TSO 7932 AND I/B P/N 885500-1001, S/N 00258 TSN 7935 CSN 4240 TSO 7935 ACTUATORS AND REPLACE D THEM. OPERATIONALLY CHECK WITH NO DEFECTS AND THE A/C WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2007081500271 20070815 00271 NM 2007 8 15 CALA0700416 1 20070809 A 3230 LANDING GEAR BOEING 737 7373T0 1384582 NM NLG & MLG MALFUNCTIONED A CALA O OTHER O OTHER CL CLIMB 1 SW 27 14341 23579 ALL LANDING GEAR EXTENDED ON ITS OWN WITH GEAR HANDLE IN OFF POSITION DURING CLIMBOUT AT 18,000 FEET AND 290 KNOTS. THE GEAR LIGHTS INDICATED THREE GREEN AND THREE RED. THE GEAR HANDLE WAS PLACED TO UP AND THE GEAR RETRACTED WITH NORMAL I NDICATIONS. NO ABNORMAL FLIGHT CHARACTERISTICS WERE NOTED AND THE FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEM. THE GEA R EXTENDED NORMALLY FOR LANDING AT IAH. MAINTENANCE PERFORMED A LANDING GEAR CONTROL SYSTEM ADJUSTMENT/TEST PER MM 32-3 1-00, PAGE 501 AND SYSTEM CHECKS WERE GOOD. A NOSE/MAIN GEAR MANUAL EXTENSION SYSTEM TEST WAS ALSO PERFORMED IAW MM 32- 34-00 AND 32-35-00 AND ALL CHECKS WERE GOOD. IN ADDITION, A LANDING GEAR OPERATION ABOVE DESIGN SPEED CONDITION INSPECT 2 L 7 2 4F RT A16WE 2007081500273 20070815 00273 NM 2007 8 15 UPS07M50365 1 20070525 A 5730 SKIN PANEL DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C RIGHT FIXED L/E LWR COMPT THRU ACCESS 619CB (REFUEL PANEL) UPPER SKIN DOUBLER SUSPECTED CRACK AT STA X ORS 537. RIGHT WING REFUELING/DEFUELING ADAPTOR O/B REMOVED PER AMM28-21-08R.55. DAMAGE AREA TRIM OFF & REPAIR ANGLES FAB PER ADV EN1375-07. REPAIR FILLER & DOUBLER FAB & HOLES ON REP PARTS P/UP PER ADV EN1375-07. OK TO INSTALL REPAIR P ARTS. HFEC CUT OUT PER DAC NDTSPM R13 06-10-01.001 NO CRACK EVIDENT. RIGHT WING REFUELING/DEFUELING ADAPTOR INSTALLED PER AMM28-21-08 R55. 2 L 7 3 4F RT A22WE 2007081500274 20070815 00274 WP 2007 8 15 AALA20071367 1 20070728 A 3220 LANDING GEAR DOUG DC9 DC983 3022083 WP NOSE MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SW 21 433AA 49451 DFW INFLIGHT T1676/28JUL - CREW REPORTED NOSE LANDING GEAR WOULD NOT EXTEND. MANUALLY EXTENDED GEAR. LANDED DFW WITHOU T INCIDENT. INSPECTED WITH NO DEFECTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007081500276 20070815 00276 WP 2007 8 15 AALA20071369 1 20070728 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DISLODGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 406A 49317 LGA - EMERGENCY LIGHT AT OVERHEAD CATWALK INOPERATIVE. RESET BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD CATWALK. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081500277 20070815 00277 NM 2007 8 15 AALA20071371 1 20070729 A 3350 A3060737 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 183AN 29593 LAS - EMERGENCY LIGHT AT AFT GALLEY LEFT NUMBER FOUR DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LEFT NUMBE R FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081500278 20070815 00278 NM 2007 8 15 AALA20071372 1 20070729 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 JFK - EMERGENCY LIGHT AT SEAT ROWS 10B TO 12B INOPERATIVE. SECURED CONNECTOR AT SEAT ROW 10B FOR EMERGENCY LIGHT AT SEA T ROWS 10B TO 12B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007081500279 20070815 00279 NM 2007 8 15 AALA20071373 1 20070730 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 JFK - EMERGENCY LIGHTS AT SEAT ROWS 10 TO 13 LEFT SIDE INOPERATIVE. REPLACED BATTERY PACK M1208 FOR EMERGENCY LIGHTS AT SEAT ROWS 10 TO 134 LEFT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007081500280 20070815 00280 NM 2007 8 15 AALA20071375 1 20070730 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 949AN 29537 DTW - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DO OR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007081500283 20070815 00283 NM 2007 8 15 UPS07M50366 1 20070515 A 5754 SKIN DOUG MD11 MD11F 3023600 NM L/E SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C EXISTING REPAIR FOUND ON RIGHT DROOP ASSY UPPER SURFACE O/B SIDE AS MARKED. EXISTING REPAIR REMOVED A S PER SRM 51-31-01 V2 R38. REPAIR DOUBLER FABRICATED PER EN1349-07. HFEC INS CARRIED OUT PER DAC NDTSPM R13 06-10-01.0 01 FOUND CRACK APPROX 4 1/8" & CRACK END AS MARKED. DOUBLER HEAT TREATED PER DPS 5.00-2 & HARDNESS VALUES 41.8 PER DPS1 .05.5. HOLES ON NEW DOUBLER P/UP PER ADV EN1349-07. DOUBLER INSTALLED PER EN1349-07. 2 L 7 3 4F RT A22WE 2007081500284 20070815 00284 WP 2007 8 15 AALA20071353 1 20070725 A 3610 DUCT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LEFT ENGINE LEAKING A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7543A 53025 728144 LAS INFLIGHT T2274/25JUL - LEFT ENGINE FIRE WARNING ILLUMINATED. REDUCED NUMBER ONE ENGINE TO IDLE AND WARNING INDICAT ION WENT OUT. LANDED LAS WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE ON 26 JUL AT LAS DUE TO AIR DUCT LEAK AT 13TH ST AGE MANIFOLD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007081500285 20070815 00285 NM 2007 8 15 UPS07M50367 1 20070603 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C CTR CARGO STA 5-11 LONGERON R51 FOUND WITH CORROSION AS MARKED. DAMAGED LONG STA 5-11 TO 5-21 TRIMMED OFF AS PER SRM 53-10-00V1 R38. HFEC INSP CUTOUT PER DACNDTSPM R13 06-10-01.001 FOUND NO CRACK EVIDENT. REPAIR LONG & SPLICE FAB PER SRM 53-10-00 V2 R38. FASTENER HOLES P/UP PER SRM 53-10-00 V1 R38 & SRM 51-31-01 V2 R38. REPAIR PARTS IN SP OK TO INSTALL REPAIR LONG & SPLICE INSTALLED PER SRM 51-31-01 V2 R38. 2 L 7 3 4F RT A22WE 2007081500286 20070815 00286 2007 8 15 AALA20071378 4 20070731 A 2565 100505201 COVER DOUG DC9 DC983 3022083 WP L2 DOOR SLIDE INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 975TW 53625 ORD LEFT NUMBER TWO DOOR SLIDE MANUAL INFLATION HANDLE VELCRO DOES NOT HOLD. REPLACED SLIDE ASSEMBLY FOR LEFT NUMBER TW O DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007081500290 20070815 00290 GL 2007 8 15 220 1 20070731 A 3244 269K431 TIRE BOMBDR BD100 BD1001A10 1390044 GL NR 2 MLG BULGED A KKYA O OTHER O OTHER LD LANDING 1 EA 63 375WB 266 20025 NR 2 MLG TIRE HAS A BULGE IN THE SIDEWALL OF THE TIRE. 2 L 7 2 4F RT T00005NY 2007081500293 20070815 00293 NM 2007 8 15 AALA20071356 1 20070726 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 182AN 29592 MIA - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 16D TO 26D INOPERATIVE. SECURED CONNECTOR FOR SEAT MOUNTED EMERGENCY L IGHTS AT SEAT ROWS 16D TO 26D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081500295 20070815 00295 WP 2007 8 15 AALA20071374 1 20070730 A 2897 WIRE HARNESS DOUG DC9 DC983 3022083 WP BOOST PUMP INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 9406W 53126 ORD INFLIGHT T346/30JUL - FORWARD CENTER FUEL BOOST PUMP CIRCUIT BREAKER TRIPPED AFTER TAKEOFF. UNABLE TO BURN CENTER F UEL. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED FORWARD CENTER FUEL BOOST PUMP AND HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007081500296 20070815 00296 NM 2007 8 15 AALA20071365 1 20070727 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 662AA 25296 DFW - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT RIGHT NUMBE R FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081500297 20070815 00297 WP 2007 8 15 AALA20071359 1 20070726 A 3350 LENS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT MISINSTALLED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 435AA 49453 DFW - EMERGENCY LIGHTS AT SEAT ROWS 28DEF AND 29DEF OUT OF CONFIGURATION. CORRECTED CONFIGURATION FOR EMERGENCY LIGHTS AT SEAT ROWS 28DEF AND 29DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007081500299 20070815 00299 NM 2007 8 15 AALA20071363 1 20070727 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 344AN 33083 DFW - EMERGENCY LIGHT IN COCKPIT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IN COCKPIT. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT A1NM 2007081500300 20070815 00300 2007 8 15 AALA20071379 4 20070731 A 8300 GEARBOX BOEING 757 757223 1384957 NM LEFT ENGINE LEAKING A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 641AA 24599 DEN INFLIGHT T1425/31JUL - LEFT GENERATOR FAIL INDICATION ILLUMINATED AND LEFT ENGINE LOW OIL PRESSURE INDICATION ILLUMI NATED. SHUT DOWN LEFT ENGINE. LANDED DEN WITHOUT INCIDENT. SINGLE ENGINE TIME 10 MINUTES. FOUND OIL LEAKING FROM LEF T ENGINE GEARBOX. CHIP DETECTOR WAS CONTAMINATED WITH METEL. REPLACED LEFT ENGINE GEARBOX PER MAINTENANCE CHECK MANUAL 72 94 02. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081500301 20070815 00301 2007 8 15 AALA20071380 4 20070731 A 2565 100504205 COVER DOUG DC9 DC982 3022082 WP L1 DOOR SLIDE INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7549A 53031 ORD - LEFT NUMBER ONE DOOR SLIDE MANUAL INFLATION HANDLE VELCRO DOES NOT HOLD. REPLACED SLIDE ASSEMBLY FOR LEFT NUMBER ONE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081500302 20070815 00302 NE 2007 8 15 AALA20071342 2 20070724 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 1 OIL CONSUMPTION A AALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 931TW 49527 717339 ORD INFLIGHT T1817/24JUL - OIL PRESSURE LIGHT ILLUMINATED ACCOMPANIED BY INDICATION OF QUANTITY DECREASE TO ZERO. CREW SHUT DOWN ENGINE AND RETURNED TO ORD AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME 20 MINUTES. REPLACED NUMBER ONE E NGINE ON 23 JUL 2007 AT ORD DUE TO OIL PRESSURE BEING OUT OF LIMITS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A6WE E9NE 2007081500306 20070815 00306 NM 2007 8 15 AALA20071357 1 20070726 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 694AN 26974 DFW - EMERGENCY LIGHT AT SEAT 17A INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 17A. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081500307 20070815 00307 NM 2007 8 15 AALA20071358 1 20070726 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 694AN 26974 DFW - EMERGENCY LIGHT AT SEAT 18F INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 18F. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081500308 20070815 00308 NM 2007 8 15 AALA20071351 1 20070724 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 794AN 30256 JFK - EMERGENCY LIGHT AT SEAT 21G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007081500311 20070815 00311 WP 2007 8 15 AALA20071349 1 20070724 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 76201 53291 LGA - EMERGENCY LIGHTS AT SEAT ROWS 3 TO 6 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 3 TO 6. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007081500312 20070815 00312 NM 2007 8 15 AALA20071350 1 20070724 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 794AN 30256 JFK - EMERGENCY LIGHT AT SEAT 21G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007081500313 20070815 00313 NM 2007 8 15 AALA20071354 1 20070725 A 3397 WIRE BOEING 777 777223 1385213 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 797AN 30012 ORD - EMERGENCY LIGHTS AT FROM SEAT ROWS 20 TO 27 INOPERATIVE. REPAIRED PINS ON WIRING FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007081500314 20070815 00314 WP 2007 8 15 AALA20071347 1 20070723 A 3350 0201804001 LENS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9405T 53141 BOS - EMERGENCY LIGHT AT SEAT 5E FORWARD MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007081500315 20070815 00315 2007 8 15 QXEA200701232 4 20070803 A 3450 TRANSPONDER BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 413QX 4060 PDX FLIGHT NR 2309: ATC UNABLE TO PICK UP TRANSPONDERS. IT WAS ON STANDBY AND UNABLE TO CYCLE ON ALT. TRIED BOTH CHANN ELS. WORKED AFTER LANDING. AIRCRAFT RETURNED TO GATE. MAINTENANCE COULD NOT DUPLICATE. CYCLED AIRCRAFT POWER. OPS C HECK GOOD IAW MTC 6345401. PUT A/C IN 'AIR' MODE AND CYCLED TRANSPONDER POWER ON AND OFF. READ TRANSPONDER CODES & ALT ITUDES AT 500 FT, 1300 FT, 2700 FT, 10,000 FT, 14,800 FT. CHECKED ALL ALTS & CODES WITH BOTH TRANSPONDERS. NO FAULTS O N THE ENGINE DISPLAY. BOT ADC SOURCES AND BOTH TRANSPONDERS CHECKED GOOD. NO PARTS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007081500316 20070815 00316 NM 2007 8 15 QXEA200701233 1 20070801 A 3230 483023 SELECTOR VALVE BOMBDR DHC8 DHC8402 1390042 NM MLG MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 425QX 13125 13125 4039 SEA FLIGHT NR 2382: AFTER TAKEOFF, RIGHT GEAR DOOR LIGHT REMAINED ON. PER CHECKLIST, LOWERED GEAR. RIGHT MAIN GEAR DID NOT EXTEND. ACCOMPLISHED 'ALT GEAR EXTENSION' CHECKLIST. AIRCRAFT TAKEN BACK TO SEA. MAINTENANCE REMOVED AND REPLACE D RT MOG DOOR SOLENOID SEQUENCING VALVE. REMOVED AND REPLACED SECONDARY MLG SELECTOR VALVE FILTER FITTING (P/N 48300-3) . BLED NR 2 HYD SYSTEM FOR LANDING GEAR CIRCUIT AFTER COMPONENT REPLACEMENT. PERFORMED FUNCTIONAL TEST OF LANDING GEAR . OPERATED LANDING GEAR APPROX 3 DOZEN TIMES THEN BLED NR 2 HYD RESERVIOR. GEAR OPERATES NORMALLY. FUNCTIONAL TEST GO OD. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007081500317 20070815 00317 2007 8 15 QXEA200701198 4 20070712 A 3418 C12851AA03 COMPUTER CNDAIR CL600 CL6002C10 1390015 EA STALL WARNING FAILED A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 606QX 15686 10023 PDX - FLIGHT 2560, STALL FAIL CAUTION MESSAGE AS WELL AS RIGHT AND LEFT FADEC MESSAGES IN CRUISE. PERFORMED CHECKLIST A ND CAPTAIN'S STALL SWITCH STILL LEFT OFF. MAINTENANCE REPLACED THE STALL PROTECTION COMPUTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007081500318 20070815 00318 CE 2007 8 15 259 1 20070720 A 3150 9901579002 WARNING SYSTEM RAYTHN DH125 HAWKER800XP 7150012 CE COCKPIT MALFUNCTIONED E KKYA O OTHER N FALSE WARNING CL CLIMB 1 EA 63 516TH 30 258418 DURING INITIAL CLIMB THE ALTITUDE ALERTER SOUNDED AT 2000 MSL FOR AN INITIAL ALTITUDE OF 3000 FT. THE ALTITUDE ALERTER NEVER CEASED AND CONTINUED TO SOUND FOR THE DURATION OF THE FLIGHT. INSTALLED NEW ADC FOUND THAT THE SAME CONDITION STI LL EXISTED. REPLACED ADC AGAIN WITH A NEW ONE AND SAME CONDITION STILL EXISTED. CONTACTED HONEYWELL FOR SUPPORT AND TO UBLESHOOTING ASSISTANCE. FOUND THAT THE CHIME UNIT WAS LEAKING TO MUCH AMPERAGE CAUSING THE ADC TO FAIL. MEASURED THE AMPERAGE FROM THE CHIME UNIT TO THE ADC AND IT READ 247 MILLIAMPS AFTER INSTALLING A NEW CHIME UNIT IT MEASURED 5 MILLIA MPS. PERFORMED OPS TEST OF ALTITUDE ALERTER SYSTEM WITH NO DEFECTS. 2 L 7 2 4F RT A3EU 2007081500319 20070815 00319 SO 2007 8 15 RAIA00708016 1 20070805 A 2910 22260001007 PRIORITY VALVE EMB 145 EMB145LR 3260212 SO HYDRAULIC SYS UNKNOWN A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 819HK 16519 145062 FLT NR 5473 - ICT - NR 1 HYD OVERHEAT / NR 1 HYD SYSTEM FAIL. MAINTENANCE AT ICT VERIFIED NR 1 HYD SYSTEM PUMPS OPERATI ONAL. FERRIED TO STL WITH LANDING GEAR PINNED DOWN. AT STL REMOVED AND REPLACED PRIORITY VALVE, OPS AND LEAK CHECK GOO D. 2 L 7 2 4T RT T00011AT 2007081500321 20070815 00321 2007 8 15 RAIA00708018 4 20070807 A 2230 AUTOTHRUST SYS EMB 145 EMB145LR 3260212 SO UNKNOWN A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 830HK 145313 FLT NR 5479 - STL - ENGINE 2 AUTOMATIC TAKEOFF THRUST CONTROL SYSTEM NO MARGIN. MAINTENANCE PERFORMED HIGH POWER ENGINE RUNS AND INSPECTED BLEED LINES ON NR 2 ENGINE, NO ENGINE EXCEEDANCES ON CMC. 2 L 7 2 4T RT T00011AT 2007081500322 20070815 00322 SO 2007 8 15 RAIA00708019 1 20070808 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 833HK 145240 PRE FLT NR 8023 - TYS - EMERGENCY LIGHT GALLEY WALL EXIT LOCATOR INOP. MAINTENANCE RESECURED CONNECTION GALLEY WALL EXI T LOCATOR, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007081500324 20070815 00324 SO 2007 8 15 RAIA00708021 1 20070809 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 840HK 145341 PRE FLT NR 7998 - STL - EMERGENCY LIGHT RIGHTHAND EMERGENCY DOOR FLOOD LIGHT IS INOP. MAINTENANCE REMOVED AND REPLACED BULB, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007081500327 20070815 00327 EU 2007 8 15 SA07049 1 20070804 A 3350 32145410 EPSU AIRBUS A321 A321211 3930370 EU CABIN FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 187US 18521 15966 1704 PIT - THE EMERGENCY LIGHTS TEST PRODUCED FAILURE MESSAGE -EMER POWER SUPPLY EXIT R-. MAINTENANCE REPLACED THE MID-CABIN , RIGHT SIDE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007081500329 20070815 00329 NM 2007 8 15 SB07059 1 20070803 A 3260 655825029 CIRCUIT CARD BOEING 737 7373B7 1384580 NM E&E BAY UNKNOWN A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 527AU 23862 PHL FLT1407 - AFTER TAKEOFF FROM PHL, CREW RECEIVED BOTH MAIN LANDING GEAR RED UNSAFE LIGHTS AFTER RAISING GEAR AND RETU RNING GEAR LEVER TO OFF POSITION. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES, CONSULTED MAINTENANCE AND RETU RNED TO FIELD AT PHL. FLIGHT LANDED WITH ALL THREE GEAR GREEN SAFE LIGHTS AND WITHOUT FURTHER INCIDENT. MAINTENANCE JA CKED AIRCRAFT AND ACCOMPLISHED NUMEROUS GEAR SWINGS. COULD NOT DUPLICATE FAULT. AS PRECAUTIONARY, REPLACED M986 CARD P ER MM 32-09-20-004-001. OPERATIONAL CHECK GOOD PER MM 32-09-20-724-031. OPERATED GEAR AFTER CARD REPLACEMENT. ALL IND ICATIONS NORMAL. 2 L 7 2 4F RT A16WE 2007081500330 20070815 00330 NM 2007 8 15 USAA070584 1 20070806 A 5514 BUSHING BOEING 737 737401 1384701 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 RIGHT HORIZ STAB INTERSPAR BOX STAB STA 0, BUSHING, R9 LUG BORE CORRODED. FABRICATED BUSHING, INSTALLED INTO BORE PER S RM 55-10-10; CORR TASK C53-701-02; LEVEL 2, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007081500331 20070815 00331 NM 2007 8 15 USAA070599 1 20070807 A 5420 ANGLE BOEING 737 737401 1384701 NM NR 2 PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 NR 2 PYLON AFT I/B ANGLE CRACKED. INSTALLED FABRICATED REPAIR PART PER SRM 51-10-02; 51-20-01, BOEING DWG 65-26300-29, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007081500332 20070815 00332 NM 2007 8 15 USAA070585 1 20070807 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 LEFT Z-ANGLE AT AFT ENTRY DOOR BETWEEN STA 947 & 986 CORRODED. REPLACED Z-ANGLE PER SRM 51-20-01, 51-40-03; CORR TASK C 53-701-01; LEVEL 2, DEFECT SIZE: 3 X 36 INCHES. 2 L 7 2 4F RT A16WE 2007081500333 20070815 00333 NM 2007 8 15 USAA070586 1 20070807 A 5320 ATTACH ANGLE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 BS 328 FLOORBEAM AT LBL 45, VERTICAL STIFFENER / INTERCOSTAL ATTACH ANGLE CRACKED. FAB'D NEW STIFFENER & INSTALLED PER DWG 65-45812, SRM 51-10-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007081500334 20070815 00334 NM 2007 8 15 USAA070587 1 20070807 A 5340 STRINGER CLIP BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 RIGHT STA 727A, STR 6, STRINGER TIE CLIP CRACKED. REMOVED & REPLACED CLIP PER SRM 51-40-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007081500335 20070815 00335 NM 2007 8 15 USAA070588 1 20070807 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 STA 500G BL 0, SHEAR WEB TOP FLOOR ANGLE CRACKED. REMOVED CRACKED METAL MADE REPAIR, TREATED & PRIMED PER SRM 51-70-13, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007081500336 20070815 00336 NM 2007 8 15 USAA070589 1 20070807 A 5320 TIE CLIP BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 TIE CLIP, STR 25L AT BS 807 CRACKED. REMOVED & REPLACED TIE CLIP PER SRM 51-20-01, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007081500339 20070815 00339 NM 2007 8 15 USAA070592 1 20070807 A 5230 6547952337 WEB BOEING 737 737401 1384701 NM AFT CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 AFT CARGO DOOR, FWD FRAME, LOWER CLOSEOUT WEB CRACKED. FAB'D NEW WEB PER BOEING DWG 65-53583, SRM 51-19-02, DEFECT SIZE : 1 INCH. 2 L 7 2 4F RT A16WE 2007081500341 20070815 00341 NM 2007 8 15 USAA070594 1 20070807 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 STA 907 BETWEEN STR 8L & 9L AT A/C RAIL ATTACH POINT CRACKED. REMOVED & INSTALLED REPAIR PARTS PER TR 53-10-20E, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007081500343 20070815 00343 EU 2007 8 15 EMB07002 1 20070801 A 2440 1701337D MODULE EMB ERJ190 ERJ190100IGW 3260408 EU EXTERNAL POWER FAILED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 19 945UW 920 19000062 FLIGHT 1906, PHL-BDL: AS FLIGHT TAXIED IN TO THE GATE, THE CREW STARTED THE APU. SMOKE BEGAN TO FILL THE CABIN AS PASS ENGERS WERE LEAVING THE AIRCRAFT. UPDATED 8/3/07: PILOT REPORT INDICATES THAT WHEN CHANGING FROM GROUND POWER TO EXTER NAL POWER, POWER DROPPED OFF LINE, THEN THE CABIN FILLED WITH SMOKE. MAINTENANCE REPLACED THE EXTERNAL POWER MODULE. N O FURTHER FAULTS. 2 L 7 2 4F RT A57NM 2007081500344 20070815 00344 NM 2007 8 15 SB07060 1 20070807 A 3350 20121 POWER SUPPLY BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 511AU 23594 BOS - MAINTENANCE REPORTED THE R2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUP PLY ALONG WITH THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007081500350 20070815 00350 NM 2007 8 15 WRNA200700044 1 20070705 A 2710 UNKNOWN BOEING 747 747212B 1384886 NM AILERON SPARKS A WRNA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 05 526UP 21937 ON TAXI OUT, DURING FLIGHT CONTROL CHECK, CREW IN AIRCRAFT FOLLOWING BEHIND REPORTED SPARKS COMING FROM RT AILERONS, RET URNED TO BLOCKS. RAN NR 3 AND NR 4 ENGINES IAW 71-00-00, ACCOMPLISHED OPERATION CHECK OF GENERATORS IAW 24-21-01 PG 601 . OPENING AND CLOSING FIELD WHILE VISUALLY CHECKING, NO DEFECTS NOTED. ACCOMPLISHED INSPECTION OF NR 3 AND NR 4 ENGINE INLET, TUBES, HOSES, ELECTRICAL LEADS AND REAR TURBINE THROUGH TAIL PIPE, NO DEFECTS NOTED. PERFORMED OPERATIONAL TEST OF AILERONS IAW 27-11-00 PG 501, SYSTEM CHECKS GOOD, NO DEFECTS NOTED. AIRCRAFT RELEASED TO SERVICE. 2 L 7 4 4F A20WE 2007081500351 20070815 00351 EU 2007 8 15 WRNA200700047 1 20070729 A 2780 CHA1063007B FRICTION BRAKE AIRBUS 300 A300B4203 3930306 EU L/E SLAT OUT OF LIMITS A WRNA J A DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 05 505TA 271 AFTER TAKEOFF FROM IND, THE SLATS FAILED TO RETRACT. DUMPED 22,000 POUNDS OF FUEL. DIVERTED TO GSO AND MADE A SAFE LAN DING. FOUND RT FRICTION BRAKE OUT OF TORQUE LIMITS, REPLACED FRICTION BRAKE IAW 27-81-47 PG401. OPERATIONAL CHECK GOOD . AIRCRAFT RELEASED TO SERVICE. 2 L 7 2 4F RT A35EU 2007081500354 20070815 00354 EU 2007 8 15 TRAX200701140 1 20070808 A 5711 FRAME AEROSP ATR72 ATR72 EU RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 RIGHT WING BOX FRAME 28A FRAME AND FACING CRACKED. [08-16-07] WING BOX FR28A FRAME REPAIRED AS PER ANA/YUL07/192/375- 004 AND FACING REPLACED AS PER SRM 51-25-01 REPAIR DETERMINED NOT TO BE A MAJOR REPAI IAW SP663 AND FAR 43 QAPENDEX A RE PAIR ACCOMPLISHED IAW SRM 51-25-01. 2 H 7 2 4T RT 2007081500355 20070815 00355 EA 2007 8 15 TRAX200701106 1 20070803 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ODOR A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 900EV 7608 PILOT REPORT GARBAGE LIKE SMELL IN COCKPIT DURING DESCENT. 2 L 7 2 4F RT A21EA 2007081500357 20070815 00357 EU 2007 8 15 YENA2007072 1 20070809 A 2130 10010502009 PROCESSOR EMB ERJ190 ERJ190100IGW 3260408 EU CABIN PRESSURE FAILED A YENA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 EA 15 279JB 111 19000090 FLT 1090, CMH-JFK, AMS CTRL FAIL CAS MESSAGE APPLIED AT FL350 WITH CLOSURE OF BOTH BLEEDS AND PACKS ON THE ECS SYS PAGE . PRESSURES IN CABIN STARTED CLIMBING FROM 800-1000 FPM. AN EMERGENCY DESCENT WAS STARTED TO 10000 FEET. PRESSURE NEV ER RETURNED. TROUBLESHOT SYS PER FIM TASK 21-00-00-810-805A. FOUND AMS FAILURE: FAULT CODES 21001510AM1 & 21001510AM2 . CONTROL PROCESSOR AT FAULT. REMOVED AND REPLACED BOTH AMS CONTROLLER PROCESSORS AT SPDA 2 SLOTS 18 & 25 PER AMM 21-0 0-01. CHECK CONFIGURATION AND OPS CHECK NORMAL. 2 L 7 2 4F RT A57NM 2007081500359 20070815 00359 NM 2007 8 15 USAA070600 1 20070807 A 5340 STRINGER CLIP BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 BS 685 S-4R HAS CRACK. REPLACED STRINGER TIE CLIP PER SRM 51-40-02, DEFECT SIZE: .250 INCH. 2 L 7 2 4F RT A16WE 2007081500361 20070815 00361 NM 2007 8 15 USAA070602 1 20070807 A 5320 65535954 FITTING BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 STA 303, STR 7R - 8R FWD UPPER CORNER OF DOOR CUTOUT ON AIRFRAME CORNER FITTING CRACKED. REMOVED & REPLACED CORNER FITT ING, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007081500362 20070815 00362 NM 2007 8 15 USAA070603 1 20070807 A 5340 STRINGER CLIP BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 STA 277 STR 15R HAS CRACK. FAB'D & REPLACED STRINGER CLIP PER BOEING DWG 69-37272, SRM 51-20-01, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007081500365 20070815 00365 NM 2007 8 15 USAA070606 1 20070807 A 5320 SUPPORT ANGLE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 BACKSIDE OF 178 BULKHEAD AT DEAD CENTER OF BULKHEAD FLOORLINE LEVEL, SUPPORT ANGLE CRACKED. FAB'D NEW ANGLE & INSTALLED PER BOEING DWG 3-94762, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007081500366 20070815 00366 NM 2007 8 15 USAA070607 1 20070807 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 BS 178 WL 216 LBBL 12, 178 BULKHEAD WEB CRACK. INSTALLED DOUBLER & FILLER PER SRM 53-10-08, FIG 201 REPAIR 9, DEFECT SI ZE: 5 INCHES. 2 L 7 2 4F RT A16WE 2007081500367 20070815 00367 NM 2007 8 15 USAA070608 1 20070807 A 5313 STRINGER BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 BS 420, S-4L, CRACKS AT STRINGER TO TIE CLIP ATTACH FASTENER HOLES. INSTALLED REPAIR FILLER, ANGLES & NEW TIE CLIP, DEF ECT SIZE: .5 & .25 INCH. 2 L 7 2 4F RT A16WE 2007081500368 20070815 00368 NM 2007 8 15 USAA070609 1 20070807 A 5340 STRINGER CLIP BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 BS 685 S-4R HAS CRACK. REPLACED STRINGER TIE CLIP PER SRM 51-40-02, DEFECT SIZE: .250 INCH. 2 L 7 2 4F RT A16WE 2007081500369 20070815 00369 EA 2007 8 15 TRAX200701062 1 20070726 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 873AS 7549 FS 333 FRAME CORRODED AT BL 0.0. WET INSTALLED FRAME AT STA 333, INSTALLED FASTENERS THROUGH OUTER SKIN. SUPPLEMENTAL - SDR CLOSED 08/06/07. 2 L 7 2 4F RT A21EA 2007081300181 20070813 00181 WP 2007 8 13 UPS07850362 1 20070728 A 5320 STRUCTURE DOUG DC8 DC871F 302199D WP COCKPIT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:N/A HOLE IN FLOOR PIT 31 STA 320. C/W INTERIM REPAIR REF EO DC8-5320-8724 APPX C, PERMANENT REPAIR. 2 L 7 4 4F RT 4A25 2007081300186 20070813 00186 NM 2007 8 13 ZZDA2007253 1 20070804 A 3260 LIGHT BOEING 717 717200 1383700 NM NLG INDICATOR INOPERATIVE A ZZDA B EMER. DESCENT O OTHER LD LANDING 1 SO 37 944AT 55007 NOSE GEAR INDICATOR DOES NOT INDICATE GREEN. RELAMPED NLG INDICATOR, OPS CHECKS GOOD REF AMM 33-00. 2 L 7 2 4F TR A6WE 2007081300192 20070813 00192 EA 2007 8 13 DATA200700007 2 20070802 A 7200 PT6A65R ENGINE STBROS SD3 SD360 8100606 EU PWA PT6 PT6A65R 52043 EA RIGHT FAILED E DATA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 13 151CA 25852 2233 SH3653 PCE32153 N151CA DEPARTED MKE AT 00:00 ON A REPOSITION FLIGHT TO DNV. UPON REACHING CRUISE (5000FT) ALTITUDE, CRUISE POWER WAS SE T BY THE FIRST OFFICER AS THE CAPTAIN WAS THE PILOT FLYING. SHORTLY AFTER CRUISE POWER WAS SET THE RIGHT ENGINE FAILED. BOTH TORQUE AND ITT DROPPED TO APPROXIMATELY ZERO SHORTLY FOLLOWED BY A DROP IN PROP RPM. THE AIRCRAFT ENGINE WAS SEC URED BY THE FOLLOWING APPROPRIATE CHECKLIST. AN EMERGENCY WAS DECLARED TO ATC AND FLIGHT RETURNED TO MKE WITH NO FURTHE R INCIDENTS. 2 H 7 2 4T 4 T A41EU E4EA 2007081300201 20070813 00201 WP 2007 8 13 ASAA0781916 1 20070730 A 5321 INSERT DOUG DC9 DC983 3022083 WP FLOOR PANEL DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 CABIN FLOOR PANEL HAS CORRODED AND BROKEN INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007081500004 20070815 00004 WP 2007 8 15 ASAA0781922 1 20070730 A 5321 993665147 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 CABIN FLOOR PANEL TOP PLY IS DISBONDED. BOND REPAIR WITH GLASS CLOTH PER SRM 51-90-0. 2 L 7 2 4F RT A6WE 2007081500005 20070815 00005 WP 2007 8 15 ASAA0781923 1 20070730 A 5321 993658211 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 CABIN FLOOR PANEL TOP PLY IS DISBONDED. BOND REPAIR PANEL WITH GLASS CLOTH PER SRM 51-90-0. 2 L 7 2 4F RT A6WE 2007081500013 20070815 00013 NM 2007 8 15 NWAA072726309 1 20070731 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 DURING OVERNIGHT CHECK, FOUND EMERGENCY PATH LIGHT AT ZONE C LEFT WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007081500027 20070815 00027 EA 2007 8 15 TRAX200701064 1 20070726 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 873AS 7549 AFT CARGO DOOR TRACK SUPPORT TO BULKHEAD ATTACH ANGLE CRACKED. REMOVED AND REPLACED CRACK CLIP ON AFT BULKHEAD AT CARGO DOOR SUPPORT TRACK ALL WORK PER CRJ200, SRM 51-42-00 JOB COMPLETED RI17912. REMOVED AND REPLACED CRACK CLIP ON AFT BU LKHEAD AT CARGO DOOR SUPPORT TRACK ALL WORK PER CRJ200, SRM 51-42-00 JOB COMPLETED RI17912. SUPPLEMENTAL - SDR CLOSED 0 8/02/07. 2 L 7 2 4F RT A21EA 2007081500038 20070815 00038 NM 2007 8 15 NWAA072766717 1 20070801 A 2612 CIRCUIT CARD BOEING 747 747251F 1384898 NM FIRE WARNING SYS MALFUNCTIONED A NWAA O OTHER N FALSE WARNING DE DESCENT 1 GL 01 617US 21121 DURING APPROACH, HAD THE MASTER FIRE WARNING LIGHT AND BELL SOUNDED FOR 1 TO 3 SECONDS THEN STOPPED. IT HAPPENED AGAIN 3 OR 4 TIMES. THERE WERE NO OTHER FIRE INDICATIONS IN ANY ENGINE FIRE HANDLE, APU, OR CARGO. FLIGHT CONTINUED ON AND L ANDING WAS UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED FIRE WARNING CARDS A6 THRU A11 AND A5 AND A12. OPERATIONAL CHE CKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F A20WE 2007081500043 20070815 00043 NM 2007 8 15 AWXA200700940 1 20070705 A 5340 69387902 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961274, CRACKED STRINGER CLIP, BS 597, S10L. REPLACED STRINGER CLIP, BS 597, S10L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007081500044 20070815 00044 NM 2007 8 15 AWXA200700941 1 20070702 A 5210 5079454 SKIN BOEING 737 7373G7 1384595 NM ZONE 800 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5981414, CRACKED L1 DOOR INNER SKIN, BS 348 AT THE NR 4 STOP. REPAIRED L1 DOOR INN ER SKIN, BS 348 AT THE NR 4 STOP IAW USAIRWAYS EA 120113. 2 L 7 2 4F RT A16WE 2007081500046 20070815 00046 NM 2007 8 15 AWXA200700943 1 20070705 A 5340 69353502 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961284, CRACKED STRINGER CLIP, BS 500B, S16L. REPLACED STRINGER CLIP, BS 500B, S1 6L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007081500047 20070815 00047 NM 2007 8 15 AWXA200700944 1 20070705 A 5340 69353502 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961292, CRACKED STRINGER CLIP, BS 520, S16R. REPLACED STRINGER CLIP, BS 520, S16R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007081500060 20070815 00060 NM 2007 8 15 KCSA071277 1 20070802 A 5330 SKIN BOEING 747 7472B4B 138481B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA 2185 TO 2200 STR 29L SKIN DAMAGED. 2 L 7 4 4F RT A20WE 2007081500061 20070815 00061 SO 2007 8 15 RAIA00707043 1 20070727 A 3350 66364 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 817HK 145058 POST FLT NR 5452 - STL - EMERGENCY LIGHT FLOOR PROXIMITY LIGHT IS INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGH T STRIP OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007081500063 20070815 00063 NM 2007 8 15 UPS07550369 1 20070801 A 3350 LIGHT BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 448UP 27737 INSPECTION TYPE:N/A TWELVE LAMPS INOP IN EMERGENCY LIGHT. RELAMPED THE EMERGENCY LIGHT ASSEMBLY PER MM 33-51-01-20. 2 L 7 2 4F RT A2NM 2007081500074 20070815 00074 NM 2007 8 15 UPS07550374 1 20070801 A 3350 LIGHT BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS - UNARMED - ANNUNCIATOR 1 LAMP INOP. RELAMPED AND CHECKS GOOD PER 33-13-00-2. 2 L 7 2 4F RT A2NM 2007081500080 20070815 00080 SO 2007 8 15 C2XA07IA178 1 20070729 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145XR 3260214 SO LT MLG MALFUNCTIONED A C2XA O OTHER N FALSE WARNING UK UNKNOWN 1 SW 27 11107 145654 IAH - FLIGHT 2317, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAILURE MESSAGE ON EICAS DURING FLIGHT. THE AIRCRAFT LAN DED IN IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LEFT HAND MAIN LANDING GEAR DOWNLOCK PROXIMITY SW ITCH, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007081500081 20070815 00081 EA 2007 8 15 TRAX200701080 1 20070628 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 877AS 7579 ALL EMERGENCY LIGHTS INOP. FLTS 4390, 4496 CX. RELATED TO DEFECT 344264-1. 2 L 7 2 4F RT A21EA 2007081500098 20070815 00098 WP 2007 8 15 AALA20071320 1 20070717 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 510AM 49804 LGA - EMERGENCY LIGHTS FROM SEAT ROWS 22 TO 26 INOPERATIVE. REPLACED BATTERY PACK AT ROW 25 OVERHEAD BIN FOR EMERGENCY LIGHTS FROM SEAT ROWS 22 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081500101 20070815 00101 WP 2007 8 15 AALA20071312 1 20070716 A 2120 5953625521 DUCT DOUG DC9 DC982 3022082 WP ACM BLOWN A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 462AA 49592 SAN INFLIGHT T237/16JUL - REPEATER DURING CLIMB TAIL COMPARTMENT TEMPERATURE WARNING LIGHT ILLUMINATED. LIGHT EXTINGUIS HED AFTER NUMBER ONE ENGINE TO IDLE AND LEFT PACK TURNED OFF. RETURNED TO SAN AND LANDED WITHOUT INCIDENT. FOUND BLOWN DUCT. REPLACED DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081500102 20070815 00102 EA 2007 8 15 TRAX200701090 1 20070731 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 716EV 10084 AFTMOST CABIN CEILING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007081500105 20070815 00105 NM 2007 8 15 AALA20071324 1 20070718 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 39367 25194 DFW - EMERGENCY LIGHT AT BASE OF RIGHT AFT LAVATORY MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT BASE OF RIGHT AF T LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007081500108 20070815 00108 NM 2007 8 15 07FDEA02704 1 20070801 A 5740 ARB76111 FITTING DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 LT WING LOWER WINGLET AFT FITTING FORWARD AND AFT HOLES FOUND CORRODED. [08-17-07] REPAIRED AS PER FEDEX EA 1-5730-1 14787, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007081500112 20070815 00112 EA 2007 8 15 TRAX200701094 1 20070731 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 875AS 7559 SERVICE DOOR WILL NOT CLOSE. 2 L 7 2 4F RT A21EA 2007081500129 20070815 00129 NM 2007 8 15 CALA0700394 1 20070803 A 5314 65C385021 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND LEFT KEEL BEAM CORRODED ON O/B FLANGE IN FORWARD BAGGAGE BIN AT STA 520, S28L. THE KEEL BEAM WAS REPAI RED IAW SRM 53-60-12. 2 L 7 2 4F RT A16WE 2007081500131 20070815 00131 WP 2007 8 15 07FDEA02726 1 20070802 A 5340 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 MAIN CARGO DOOR FITTING NR 7 BORES A, B, C AND D SHOW CRACK INDICATIONS WITH BHEC BORES MARKED IN BLACK. 09-04-07 RE MOVED AND REPLACED FITTING NR 7 IN REF TO DC/MD10 SRM 51-33-01 VOLI PAGE 1. MAJOR REPAIR MECH 3934 QC348 2 L 7 3 4F RT A22WE 2007081500139 20070815 00139 NM 2007 8 15 CALA0700400 1 20070803 A 5311 6546532 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A .25 INCH CRACK IN FRAME AT RIVET THAT ATTACHES AIR GRILL, STA 480, S9R. REPAIRED IAW ECRA 5110-04643 . 2 L 7 2 4F RT A16WE 2007081500146 20070815 00146 NM 2007 8 15 CALA0700401 1 20070803 A 5313 6561777503 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A .25 INCH CRACK IN STRINGER 14L AT STA 360. REPAIRED IAW ECRA 5311-01346. 2 L 7 2 4F RT A16WE 2007081500147 20070815 00147 NM 2007 8 15 QXEA200701226 1 20070730 A 2430 400SG163Q GENERATOR BOMBDR DHC8 DHC8402 1390042 NM NR 2 DC UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 427QX 650 650 4156 BIL FLIGHT NR 2411: NR 2 DC GENERATOR CAUTION. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE REMOVED AND REPLACED THE NR 2 D C STARTER/GENERATOR IAW MTC 6243101 (1-4). OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007081500161 20070815 00161 EU 2007 8 15 07FDEA02754 1 20070713 A 5347 A5381192220251 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 N00738 MDCC - SEAT TRACK AT Y-953 BETWEEN FR 45 AND FR 54 FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007081500170 20070815 00170 EA 2007 8 15 SWIA200718552 1 20070731 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 938SW 7741 AFT PORTION OF PAX DOOR IS CRACKED UNDERNEATH TOP STEP. REPAIRED CRACK IAW REO 601R-52-11-279. 2 L 7 2 4F RT A21EA 2007081500172 20070815 00172 EA 2007 8 15 SWIA200718554 1 20070730 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 953SW 7813 LEFT WINDSHIELD CRACKED. DIVERTED TO DLH, FLIGHT NR 5951. REPLACED LEFT WINDSHIELD IAW AMM 56-11-01, LEAK AND OPS CHEC K GOOD, PN: NP-139321-13, SN OFF: 03076H8781. 2 L 7 2 4F RT A21EA 2007081500180 20070815 00180 NM 2007 8 15 CALA0700407 1 20070803 A 5311 6546555 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 867, S9R. REPAIRED IAW ECRA 5310-04643. 2 L 7 2 4F RT A16WE 2007081500182 20070815 00182 NM 2007 8 15 CALA0700408 1 20070803 A 5313 6561777503 STRINGER SPLICE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A .25 INCH CRACK IN STRINGER SPLICE AT STA 359, S15L. REPAIRED IAW ECRA 5311-01346. 2 L 7 2 4F RT A16WE 2007081500189 20070815 00189 NE 2007 8 15 HALA0700315 2 20070801 A 7200 ENGINE BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE NR 1 FLAMED OUT A HALA D RETURN TO BLOCK X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, BTB, NR 1 ENGINE FLAMED OUT AFTER INITIAL START. PERFORMED FIM 73-21-00, C/W PIMU BITE PROCED URE, NO CURRENT FAULTS FOUND, NO MTC OR EICAS MSGS. ACCOMPLISHED AMM TASK 28-22-11-404-008, STEP H. OPS TEST NR 1 ENG FUEL S/OFF ACT. NO FAULTS FOUND. ACCOMPLISHED SUCCESSFUL ENG START AT GATE AMM 71-00-00-712-021. START NML, NO FAULT INDICATIONS, DISAGREE LTS EICAS MSG'S. OK FOR SERV. 2 L 7 2 4F 4 F RT A1NM E24NE 2007081500190 20070815 00190 NM 2007 8 15 CALA0700411 1 20070804 A 5330 6545768 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND A HOLE IN FUSELAGE SKIN CAUSED BY A LIGHTNING STRIKE AT STA 375, S24R. A SKIN REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201. 2 L 7 2 4F RT A16WE 2007081500192 20070815 00192 NM 2007 8 15 CALA0700413 1 20070805 A 5313 654576987 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND O/B SIDE OF STRINGER 27L CORRODED APPROXIMATELY 2 INCHES FORWARD OF STA 500D IN FORWARD BAGGAGE BIN. A DOUBLER REPAIR WAS INSTALLED IAW SRM 5331-01336. 2 L 7 2 4F RT A16WE 2007081500196 20070815 00196 NE 2007 8 15 DLM88070969 2 20070730 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 FAILED A DALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 27 966DL 39286 725939 53115 725939 FLIGHTCREW REPORTED THAT EN ROUTE TO ATL LEFT ENGINE OIL FILTER CLOGGED MESSAGE ILLUMINATED ON OAP FOLLOWED BY THE LOSS OF OIL PRESSURE AND OIL QTY. FLIGHTCREW SHUT DOWN ENGINE AND DIVERTED TO STL. REPLACED NR 1 ENG PER TRANS 9T102. 2 L 7 2 4F 4 F RT A6WE E9NE 2007081500207 20070815 00207 NM 2007 8 15 DLM88070984 1 20070731 A 5320 STIFFENER DOUG MD88 MD88 3023688 NM BS 1474 L22-23L BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 950DL 49881 BROKEN STIFFENER ON STA 1474 CANT BETWEEN LONG 22 AND 23 LT. STIFFENER REPLACED PER DWG 9911946. 2 L 7 2 4F RT A6WE 2007081500209 20070815 00209 NM 2007 8 15 DL777070985 1 20070725 A 4920 ENGINE BOEING 777 777232 1385232 NM APU MAKING METAL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 867DA 16059 29743 APU GEN WOULD NOT COME ONLINE TS PER FIM ALL APU CHIP DETECTORS HAVE LARGE AMOUNT OF METAL REPLACED APU PER MM GEN, OPS CKS OK. 2 L 7 2 4F RT T00001SE 2007081500215 20070815 00215 SO 2007 8 15 RAIA00707044 1 20070730 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 815HK 145048 PRE FLT NR 5584 - RIC - EMERGENCY LIGHT MAIN DOOR FLOOD LIGHT IS INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BULB, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007081500217 20070815 00217 NM 2007 8 15 DLM88070991 1 20070624 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 950DL 49881 CRACKED RT CUSP WEB AT STA Y=218, REPLACED WEB. 2 L 7 2 4F RT A6WE 2007081500221 20070815 00221 NM 2007 8 15 DLM88070994 1 20070731 A 5312 ANGLE DOUG MD88 MD88 3023688 NM BULKHEAD CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 950DL 49881 EXFOLIATION CORROSION ON AFT PRESSURE DOME 'T' EXTRUSION. TASK CARD 57-53300/57-53301. "T" REPLACED PER DWG 5910130 AT STA 1338,X=0 ON N/R T0063245 AT HMV-3. 2 L 7 2 4F RT A6WE 2007081500223 20070815 00223 SO 2007 8 15 RAIA00708003 1 20070801 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO COCKPIT INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 841HK 145382 PRE FLT NR 8021 - IAD - EMERGENCY LIGHT AT COCKPIT DOOR INOP. MAINTENANCE REMOVED AND REPLACED LAMP CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007081500231 20070815 00231 NM 2007 8 15 DLM88070997 1 20070622 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 629 LBL 5 BULGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 950DL 49881 FUSELAGE SKIN BULGED WITH A 1/4 IN CRACK STA 629 LBL 5. REPAIRED PER SRM 53-04D. 2 L 7 2 4F RT A6WE 2007081500238 20070815 00238 SO 2007 8 15 RAIA00708012 1 20070804 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145EP 3260221 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 826HK 145016 PRE FLT NR 5515 - STL - EMERGENCY LIGHT BATTERY RAN DOWN. MAINTENANCE REMOVED AND REPLACED ALL 4 EMERGENCY LIGHT BATTER Y POWER SUPPLY, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007081500239 20070815 00239 2007 8 15 AWXA200700949 4 20070802 A 2565 D31517317 SLIDE AIRBUS 320 A320232 3930326 EU L-2 DOOR NO TEST A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 665AW 14370 652 1644 LAS - EES - LOG 4165381 - MX REPORTED AFT LEFT ESPU FAULT ON EMERGENCY TEST. MX TROUBLESHOT PER TSM 33-51-810 FOUND L2 D OOR SLIDE BAD. MX REPLACED THE L-2 DOOR SLIDE ASSY IAW R1C25305. OPERATIONAL TEST WAS GOOD. 2 L 7 2 4F RT A28NM 2007081500259 20070815 00259 SO 2007 8 15 C2XA07ON018 1 20070809 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO CARGO BAY FALSE ACTIVATION A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 14162 14842 14842 1450808 FLT 9 - COS TO ONT - FLIGHT CREW REPORTED BAG SMOKE INDICATION IN-FLIGHT. CONTRACT MX PERSONEL INSPECTED CARGO COMPARTM ENT AND NO ABNORMALITIES WERE NOTED. AIRCRAFT WAS RELEASE IN ACCORDANCE WITH MEL 26-15-00 CAT -C- CONTROL 126970. WHEN AIRCRAFT ARRIVED TO ONT, EXPRESSJET MX PERSONEL REMOVED THE FWD AND THE AFT BAGGAGE COMPARTMENT SMOKE DETECTORS (FWD: P /N 473597-13, S/N 1777 TSN 14842 CSN 11464 TSO 14842. AFT:P/N 47359-13, S/N 2935 TSN 10975 CSN 8517 TSO 10975) AND REPL ACED THEM. OPERATIONALLY CHECK WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2007081500264 20070815 00264 SO 2007 8 15 C2XA07IA177 1 20070730 A 3350 SIGN EMB 145 EMB145EP 3260221 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13936 145025 IAH - FLIGHT 2760, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN EMERGENCY LIGHT SIGN AS BEING INOPERATIVE. MAINTENA NCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007081500266 20070815 00266 SO 2007 8 15 C2XA07IA183 1 20070808 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12175 14500878 IAH - DURING MAINTENANCE INSPECTION THE EMERGENCY EXIT LIGHT ON THE AFT GALLEY WALL WAS FOUND TO BE INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIR CRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007081500267 20070815 00267 SO 2007 8 15 C2XA07IA184 1 20070810 A 3350 7287580501 LIGHT EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15926 145005 IAH - FLIGHT 2213, DURING PREFLIGHT INSPECTION THE AISLE PATH LIGHT STRIP NEXT TO THE LEFT HAND EXIT WAS FOUND TO BE INO PERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIR CRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007081500268 20070815 00268 SO 2007 8 15 C2XA07RIO68 1 20070805 A 2612 FIRE WARNING EMB 145 EMB145XR 3260214 SO CARGO BAY MALFUNCTIONED A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 17138 145727 FLT 2557 - EWR - CREW REPORTED BAGG FIRE LIGHT CAME ON IN FLIGHT WITH NO WARNING SOUND. EWR MX RESET ELECTRICAL POWER A ND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007081500275 20070815 00275 WP 2007 8 15 AALA20071368 1 20070728 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 406A 49317 LGA - EMERGENCY LIGHT AT SEAT ROW 7 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 7. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081500288 20070815 00288 NM 2007 8 15 AALA20071376 1 20070730 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 671AA 25336 DFW - EMERGENCY AISLE LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY AISLE LIGHTS AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081500292 20070815 00292 NM 2007 8 15 AALA20071355 1 20070725 A 3397 WIRE BOEING 767 767323 1385205 NM EMERGENCY LIGHT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 389AA 27449 DFW - EMERGENCY LIGHT AT FORWARD RIGHT OVERWING NUMBER ONE DOOR SLIDE INOPERATIVE. REPAIRED WIRE NEAR MODULE M731 FOR EM ERGENCY LIGHT AT FORWARD RIGHT OVERWING NUMBER ONE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007081500303 20070815 00303 NM 2007 8 15 AALA20071343 1 20070723 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 772AN 29580 NRT EMERGENCY LIGHT AT FIRST CLASS CLOSET HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT FIRST CLASS CLOSET. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007081500310 20070815 00310 WP 2007 8 15 AALA20071348 1 20070723 A 3350 0L1098BPEGPL BULB DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9405T 53141 BOS - EMERGENCY LIGHT AT SEAT 5E FORWARD MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007081500342 20070815 00342 NM 2007 8 15 USAA070595 1 20070807 A 5313 STRINGER SPLICE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 STA 907 STR 4L, STRINGER SPLICE CRACKED. INSTALLED REPAIR PARTS PER SRM 51-10-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007081500345 20070815 00345 NM 2007 8 15 BB07058 1 20070728 A 2121 6066224 FAN BOEING 767 7672B7 1385107 NM CABIN MALFUNCTIONED A USAA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 253AY 70245 1680 24894 FLIGHT 253, PHL-ATH: AIRCRAFT RETURNED TO PHL DUE TO A RECIRCULATION FAN MESSAGE AND SMOKE IN THE CABIN. MAINTENANCE P LACED THE RECIRC FAN ON MEL AND RETURNED THE A/C TO SERVICE. 08/07/07 UPDATE: MAINTENANCE REPLACED THE RECIRC FAN. 2 L 7 2 4F RT A1NM 2007081500353 20070815 00353 EU 2007 8 15 TRAX200701139 1 20070808 A 5311 FRAME AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 FRAME 39 CORRODED BETWEEN STR 21 RT TO 21 LT. REPAIRED AS PER SRM 53-61-40 FIG 415 MATERIAL THICKNESS 0.080 MATERIAL R EMOVED 0.075 OUT OF LIMITS AS PER SRM 53-61-00 FIG 307 2 H 7 2 4T RT 2007081500356 20070815 00356 EA 2007 8 15 TRAX200701107 1 20070803 A 5240 DOOR CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 706EV 10054 SERVICE DOOR WON'T CLOSE. 2 L 7 2 4F RT A21EA 2007081500360 20070815 00360 NM 2007 8 15 USAA070601 1 20070807 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 INTERCOSTAL, STA 294.5, STR 11L CRACKED. INSTALLED FABRICATED REPAIR PARTS PER SRM 51-20-01, DEFECT SIZE: 3 INCHES. 2 L 7 2 4F RT A16WE 2007081500364 20070815 00364 NM 2007 8 15 USAA070605 1 20070807 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 BS 827 FRAME CRACKED BETWEEN STR 8L & 9L. ALL WORK REPAIRED IAW TR 53-10-20E, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007081500373 20070815 00373 NM 2007 8 15 USAA070597 1 20070807 A 5313 STRINGER BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 STA 400 STR 4L HAS CRACK. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-10-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007081500375 20070815 00375 2007 8 15 YENA2007071 4 20070805 A 3442 066500080409 RADAR AIRBUS 320 A320232 3930326 EU E&E BAY MALFUNCTIONED A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 561JB 10928 3603 1927 FLT 471, BOS-SJC, APPROX 03:15Z, WX RADAR WENT OUT FOLLOWED BY A ELECTRICAL BURNING SMELL. PULLED CB K13. CARRIED OUT INSP ON THE FWD AVIONICS BAY, FOUND WEATHER RADAR UNIT SMELLS BURNED, INSPECTED CONNECTORS, CHECKED GOOD. REMOVED AND R EPLACED WX RADAR UNIT PER AMM 34-41-33, OPS TEST GOOD PER AMM 34-41-00-05. CARRIED OUT ELECTRICAL BURNING INSPECTION PE R TSM 24-00-00-810-825. 2 L 7 2 4F RT A28NM 2007081500376 20070815 00376 EA 2007 8 15 TRAX200701055 1 20070725 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 854AS 7382 INBOARD 280 CLIP AT LBL 9 IS CRACKED. REMOVED DAMAGED 280 CLIP. DUPLICATED PART FROM 2024T3 .050 PO 950029 & ALODINED & PRIMED IAW CRJ SRM 51-24-16, 51-25-06 JB13225. OK TO INSTALL JB13225. INSTALLED CLIP AT LBL 9 IAW CRJ 200 SRM 51-42- 21 LC14030 8-4-07. SUPPLEMENTAL - SDR CLOSED 08/07/07. 2 L 7 2 4F RT A21EA 2007081500378 20070815 00378 NM 2007 8 15 USAA920070794 1 20070727 A 5311 19572030024 FRAME BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 923UW 22203 PIT - C4 CHECK, CRACKED FRAME, BS 1070, BL 65. REPLACED FRAME, BS 1070, BL 65 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007081500380 20070815 00380 NM 2007 8 15 USAA920070796 1 20070731 A 5320 19572030023 BEAM BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 923UW 22203 PIT - MAJOR REPAIR - C4 CHECK, CRACKED BEAM, BS 1070, BL 65. REPLACED BEAM BS 1070, BL 65 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007081500384 20070815 00384 EA 2007 8 15 TRAX200701075 1 20070725 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 854AS 7382 EMERGENCY EXIT LIGHT ON O/B TRIM PANEL OF GALLEY IS BROKEN. 2 L 7 2 4F RT A21EA 2007081600001 20070816 00001 EA 2007 8 16 QXEA200701234 1 20070801 A 8000 ENGINE CNDAIR CL600 CL6002C10 1390015 EA RIGHT DEFECTIVE A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 617QX 10130 BOI- FLIGHT 4276 - RIGHT ENGINE FAILS TO START AFTER PUSHBACK. FLIGHT CREW REPORTED STARTER CUT-OUT AT 10 PERCENT. MAI NTENANCE CHECKED THE MDC WITH NO FAULTS RECORDED. COMPLIED WITH 2 STARTS WITH NO DEFECTS. AIRCRAFT RETURNED TO SERVICE . NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007081600002 20070816 00002 EA 2007 8 16 QXEA200701235 1 20070802 A 8010 4120T05P02 CONTROL VALVE CNDAIR CL600 CL6002C10 1390015 EA STARTER FAILED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 601QX 11924 10009 DEN - UPON PUSHBACK, THE LEFT ENGINE WOULD NOT START. RETURNED TO THE GATE, MAINTENANCE REPLACED THE STARTER AND CONTRO L VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007081600004 20070816 00004 EA 2007 8 16 QXEA200701229 1 20070731 A 2150 GG670950103 CONTROL VALVE CNDAIR CL600 CL6002C10 1390015 EA RT A/C PACK FAILED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 603QX 15688 10011 GEG - FLIGHT 2597, ON TAXI RECEIVED A RIGHT PACK CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENANCE REPLACED THE RIGHT TEMPERATURE CONTROL VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERCICE. 2 L 7 2 4F RT A21EA 2007081600008 20070816 00008 NM 2007 8 16 DHL2007741527 1 20070803 A 5310 651986219 BEAM BOEING 727 7272Q9 138448M NM BS 298 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 NOSE SECTION INTERIOR HORIZ WALKWAY BEAM LEFT SIDE MID CHORD CORRODED AT FWD END, BS 298, LWR SIDE. REMOVED CORROSION, MATERIAL REMOVAL EXCEEDED LIMITS PER B727 SRM 53-10-1 FIG 1. REMOVED, LOCATED, DRILLED UP, TREATED, PRIMED, AND INSTALL ED NEW MID CHORD PER B727 SRM 51-10-2, 51-30-2, AND 51-30-5. 2 L 7 3 4F RT A3WE 2007081600011 20070816 00011 WP 2007 8 16 FX7A200700005 1 20070730 A 2420 CSD DOUG DC9 DC982 3022082 WP LEFT OVERHEATED A FX7A A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 19 905TA 49905 LEFT CSD TEMP INCREASED TOWARDS RED MARK. LEFT CSD PRESS LOW LIGHT AND MASTER CAUTION LIGHT ILLUMINATED. APU FAILED TO START CAUSING AIR TURN-BACK. 2 L 7 2 4F A6WE 2007081600012 20070816 00012 SO 2007 8 16 SIMA200721808 1 20070805 A 5330 14520595003 SKIN EMB 145 EMB145LR 3260212 SO ZONE 200 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 908AE 6201 14500897 FUSELAGE SKIN BETWEEN FRAME 7 AND 8 GOUGED. REPAIRED SKIN IAW EMB SRM 53-10-01. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007081600013 20070816 00013 SO 2007 8 16 SIMA200721803 1 20070804 A 3234 8271013 CONTROL HANDLE EMB 145 EMB145LR 3260212 SO MLG FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 622AE 1126 145108 RECEIVED AIR/GROUND FAIL MESSAGE AND GEAR HANDLE STUCK IN DOWN POSITION - RETURNED TO BNA. PERFORMED AIR/GROUND SYSTEM SIMULATION IAW EMB 32-63-00 AND LANDING GEAR EXTENSION AND RETRACTION IAW EMB 32-30-00 WITH NO DEFECTS NOTED. REMOVED A ND REPLACED LANDING GEAR HANDLE IAW EMB 32-30-00. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007081600016 20070816 00016 SO 2007 8 16 SIMA200721809 1 20070804 A 5330 14520552001 SKIN EMB 145 EMB145LR 3260212 SO ZONE 200 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 687JS 7529 14500846 LIGHTNING STRIKE DAMAGE ON RIGHT UPPER SKIN BETWEEN FRAME 22 AND 23. CUTOFF DAMAGED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-21-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007081600019 20070816 00019 SO 2007 8 16 SIMA200721801 1 20070802 A 3350 14531116401 RELAY EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHTS FAILED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 712AE 16703 145247 EMERGENCY LIGHTS NOT ARM AND ELECTRICAL EMERGENCY ABNORMAL MESSAGE, ABORTED TAKEOFF. REMOVED AND REPLACED BATTERY RELAY BOX IAW EMB AMM 24-33-02. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007081600020 20070816 00020 EU 2007 8 16 SIMA200721807 1 20070725 A 5315 7253721493 FLOORBEAM SAAB SF340 340B 7860101 EU ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 387AE 17940 5000 340B387 PREVIOUS REPAIR ON GALLEY FLOOR SUPPORT AT STATION 258 FOUND CORRODED. REMOVED PREVIOUS REPAIR AND INSTALLED NEW FILLER IAW SAAB SRM 53-70-30. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007081600021 20070816 00021 CE 2007 8 16 135N223PB 1 20070805 A 2497 WIRE CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO LT ALTERNATOR UNSECURE E HYIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 01 223PB 402C0105 ON 08-05-07, LEFT ALTERNATOR OUT LIGHT CAME ON IN FLIGHT AND RT ALT OUT CAME ON INTERMITTENTLY. MX INSPECTED AND REPAIR ED WIRING TO LT ALT AND SECURED WIRE TO RT ALT FUSE IN COCKPIT, SECONDARY INSP AND RUN UP WAS PERFORMED ON 08-06-07 WITH NO DEFECTS NOTED. 1 L 7 2 3O 3 O A7CE E8CE 2007081600022 20070816 00022 EU 2007 8 16 TRBA2007065 1 20070802 A 2761 BHC1021 VALVE AEROSP ATR72 ATR72212 8680945 EU LT SPOILER FAILED A TRBA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 29 410AT 410 ON TAKEOFF, EXCESSIVE ROLL TO THE LEFT. REMOVED AND REPLACED LEFT WING SPOILER VALVE BLOCK AS PER M/M 27-64-72. OP AND LEAK CHECK SATISFACTORY. 2 H 7 2 4T RT A53EU 2007081600023 20070816 00023 NM 2007 8 16 MZZA0700008 1 20070723 A 5340 BAC1498156X STRINGER CLIP BOEING 737 737824 13844BZ NM BS 500-500D CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 25201 28958 INSPECTION FOUND STRINGER CLIP CORRODED BETWEEN BAY 13 AND 14 AT STA 500-500A, S28R. THE CLIP WAS REPLACED IAW SRM 51-4 0-02. 2 L 7 2 4F RT A16WE 2007081600025 20070816 00025 2007 8 16 HALA0700323 4 20070804 A 3160 CONNECTOR BOEING 717 717200 1383700 NM DISPLAY DIRTY A HALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 13 480HA 55125 ATB - AFTER TAKEOFF, LOST NR 1DU NR 6 DU STARTED TO FAIL NR 4 CU FAILED FOR A FEW MINUTES. REMOVED AND CLEANED CONNECTO RS OF DU'S 1, 4 AND 6. GND OPS CHK OK 31-43-01. 2 L 7 2 4F TR A6WE 2007081600027 20070816 00027 NM 2007 8 16 HALA0700325 1 20070803 A 2611 UNKNOWN BOEING 717 717200 1383700 NM SMOKE DETECTOR UNKNOWN A HALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 13 477HA 55122 FWD CARGO SMOKE DETECTOR "PUSH" SWITCH FLASHING. ACCOMP FIM 26-11 TASK 803 GND CK OK NO FAULTS. OK FOR SERVICE. 2 L 7 2 4F TR A6WE 2007081600028 20070816 00028 NM 2007 8 16 NWAA072776308 1 20070802 A 3350 FUSE BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 668US 24223 DURING OVERNIGHT CHECK, LEFT DOOR OVERWING EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED FUSE. OPERATIONAL C HECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007081600030 20070816 00030 EU 2007 8 16 AWXA200700955 1 20070731 A 5340 D53480048707 FITTING AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 SAL - MAJOR REPAIR - C-06 CHECK - NR 5964872, CORROSION ON THE L2 DOOR CUT OUT LOWER SILL CENTER FITTING, BS 3158/FR 66 TO BS 3257/FR 68. REPLACED THE L2 DOOR CUT OUT LOWER SILL CENTER FITTING, BS 3158/FR 66 TO BS 3257/FR 68 IAW A320 SRM 5 1-72-11. 2 L 7 2 4F RT A28NM 2007081600031 20070816 00031 NM 2007 8 16 AWXA200700956 1 20070701 A 2560 POWER SUPPLY BOEING 737 7373G7 1384595 NM FLASHLIGHT INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - EEL - C-20 CHECK - NR 5981248, FORWARD GALLEY EMERGENCY FLASHLIGHT IS INOPERATIVE. REPLACED FORWARD GALLEY FLASHL IGHT POWER SUPPLY AND FLASHLIGHT. 2 L 7 2 4F RT A16WE 2007081600036 20070816 00036 EU 2007 8 16 AWXA200700962 1 20070726 A 5210 D5311245600100 STOP FITTING AIRBUS 320 A320231 3930325 EU ZONE 800 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 SAL - MAJOR REPAIR - C-06 CHECK - NR 5990364, R2 DOOR LOWER STOP FITTING WORN, BS 709/FR 16. REPLACED R2 DOOR LOWER DOO R STOP FITTING, BS 709/FR 16 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007081600037 20070816 00037 EU 2007 8 16 AWXA200700963 1 20070726 A 5210 D52111417201 COVER AIRBUS 320 A320231 3930325 EU ZONE 800 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 SAL - MAJOR REPAIR - C-06 CHECK - NR 5979694, R2 DOOR UPPER PANEL/PLATE COVER WORN, BS 3158/FR 66 TO BS 3257/FR 68. REP LACED R2 DOOR UPPER PANEL/PLATE COVER, BS 3158/FR 66 TO BS 3257/FR 68 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007081600038 20070816 00038 EU 2007 8 16 AWXA200700964 1 20070726 A 5210 D52111417200 COVER AIRBUS 320 A320231 3930325 EU ZONE 800 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 SAL - MAJOR REPAIR - C-06 CHECK - NR 5979695, L2 DOOR UPPER PANEL/PLATE COVER WORN, BS 3158/FR 66 TO BS 3257/FR 68. REP LACED L2 DOOR UPPER PANEL/PLATE COVER, BS 3158/FR 66 TO BS 3257/FR 68 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007081600039 20070816 00039 NM 2007 8 16 07FDEA02738 1 20070802 A 2910 NONE BOEING 727 727233 138408A NM HYD SYSTEM NONE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 265FE 21671 AFTER GEAR RETRACTION ON CLIMB-OUT, SYS A HYD ENG NR 1 PUMP LOW PRESS LIGHT ILLUMINATED AND NOTICED HYD SYS A QUANTITY D ECREASING. JACKED AIRCRAFT IAW THE B727-200 AMM 07-11-000-2. CYCLED THE LANDING GEAR 15 PLUS TIMES WHILE CYCLING. THE FLT CONTROL NUMEROUS TIMES. NO HYDRAULIC QUANTITY DEVIATION AT ANY TIME DURING THE GEAR OR FLIGHT CONTROL MOVEMENT. C HECKED THAT HYDRAULIC HEAD PRESSURE WAS 45 PSI WITH ENGINES RUNNING. NO LEAKS WERE NOTED DURING ANY OF THESE CHECKS. R EMOVED AIRCRAFT FROM JACKS AND RETURNED IT TO THE RAMP. AIRCRAFT IS OKAY FOR CONTINUED SERVICE. 2 L 7 3 4F RT A3WE 2007081600040 20070816 00040 NM 2007 8 16 07FDEA02739 1 20070803 A 2913 623337 PUMP BOEING 727 727233 138408A NM HYD SYSTEM CRACKED A FDEA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 25 257FE 10489 8971 20939 APPROX 30 SECS AFTER GOING TO FLAPS 30. TOTAL LOSS OF A HYDRAULIC SYSTEM. ALTERNATE FLAP SYSTEM USED TO RAISE FLAPS TO 15. GPWS SYSTEM INHIBITED. PER CREW DEBRIEF, BOTH HYDRAULIC PUMPS WERE SHUT OFF IMMEDIATELY AFTER PRESSURE LOSS. FOU ND NR 1 ENG DRIVEN HYD PUMP CRACKED. REMOVED AND REPLACED NR 1 ENG DRIVEN HYDRO PUMP AND HYD CASE DRAIN. FILTER MANIFO LD ASSY REF M/M 29-11-033-4 AND M/M 29-11-041-2. SERV HYDRO. 2 L 7 3 4F RT A3WE 2007081600042 20070816 00042 EU 2007 8 16 07FDEA02764 1 20070803 A 2760 UNKNOWN AIRBUS 300 A300B4605R 3930308 EU SPOILERS UNKNOWN A FDEA B EMER. DESCENT F FLT CONT AFFECTED CR CRUISE 1 SO 25 731FD 709 DURING CR FLT, LT WING SPOILER NR 4 DEPLOYED IN FLT. A/C ROLLED HARD TO LT. DISCONNECTED A/P AND COUNTERED RT SPLRS ON BOTH WINGS DEPLOYED FOR REMAINDER OF FLT. SPLR NR 4 DEFERRED. ON DEBRIEFING CREW, RT WING SPOILERS DEPLOYED FOR CONT ROL CORRECTION ONLY. FOUND FAULT CODES EFCU POSITION 1 M-2 3 AND 6. SWAPPED EFCU'S FAULT CODED EFCU POSITION 1 M-2 4 AND 7. EFCU'S RETURNED TO ORIGINAL POSITIONS. ORDERED 1 CPN 2711299 SERVO VALVE PER TSM 27-61-06 AND 2 EFCU'S CPN 2711099 AS PRECAUTION. INSP 4L SPOILER SURFACE AND HINGES FOR ANY DAMAGE. CHECK WIRING FROM THE EFCU' TO THE 4L ACT A ND VALVE GROUP. REPLACED THE 4L SPOILER VALVE GROUP. REMOVED AND REPLACED 4L SPOILER GROUP VLV PER MM 27-64-12-4. OPS 2 L 7 2 4F RT A35EU 2007081600048 20070816 00048 EU 2007 8 16 07FDEA02771 1 20070710 A 5340 A5378193620200 ADAPTER AIRBUS 310 A310222 3930315 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 MDCC - CLS ADAPTER ON CABIN FLOOR FR 37 BETWEEN Y1456 AND Y1959 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007081600049 20070816 00049 EU 2007 8 16 07FDEA02772 1 20070710 A 5340 A5378193620200 ADAPTER AIRBUS 310 A310222 3930315 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 MDCC FWD - CLS ADAPTER AT FR38 BETWEEN Y1456 AND Y1959 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM. 2 L 7 2 4F RT A35EU 2007081600050 20070816 00050 EU 2007 8 16 07FDEA02773 1 20070710 A 5340 A5378193720600 ADAPTER AIRBUS 310 A310222 3930315 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 MDCC FWD - CLS ADAPTER AT FR38 BETWEEN Y953 AND Y1456 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72 -10. 2 L 7 2 4F RT A35EU 2007081600051 20070816 00051 EU 2007 8 16 07FDEA02774 1 20070712 A 5347 A5361164020000 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 MDCC - SEAT TRACK WITH CORROSION BETWEEN FR18 AND FR19 AT Y950. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007081600052 20070816 00052 EU 2007 8 16 07FDEA02775 1 20070712 A 5340 A538193620200 ADAPTER AIRBUS 310 A310222 3930315 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 MDCC - CLS ADAPTER AT FR 36 BETWEEN Y1456 AND Y1459 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-1 0. 2 L 7 2 4F RT A35EU 2007081600054 20070816 00054 EU 2007 8 16 AWXA200700958 1 20070804 A 2611 RAI2800M0706 CONTROL BOX AIRBUS 320 A320232 3930326 EU SMOKE DETECTION FAILED A AWXA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 28 658AW 15845 5035 1110 PHX - OTH - LOG 4109980 - MX REPORTED LAV AND CARGO SMOKE FAULT ON ECAM, WOULD NOT RESET. MX REPLACED THE SMOKE DETECTO R CONTROL UNIT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007081600055 20070816 00055 NM 2007 8 16 QXEA200701236 1 20070805 A 6123 AUTOFEATHER SYS BOMBDR DHC8 DHC8402 1390042 NM FAULTED A QXEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 09 412QX 4059 RNO FLIGHT NR 2256: AUTOFEATHER DID NOT ARM. TAKEOFF ABORTED AT 70 KTS. AIRCRAFT RETURNED TO GATE. MAINTENANCE INTERR OGATED CDS AND FOUND FAULT CODE 494 ON BOTH ENGINES. C/W AMM TASK 61-20-00-710-805. OPS CHECK OF AUTO FEATHER SYSTEM P ASSED TEST. MESSAGES WERE CLEARED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007081600056 20070816 00056 NM 2007 8 16 QXEA200701237 1 20070806 A 3150 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM WARNING LIGHT UNKNOWN A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 09 402QX 4032 EUG FLIGHT NR 2298: MASTER CAUTION AND PUSHER SYSTEM CAUTION ILLUMINATED DURING TAKEOFF ROLL AT APPROX 70 KNOTS. TAKEOF F WAS ABORTED. PUSHER SYSTEM FAIL CAUTION WENT OUT AND REMAINS OUT. AIRCRAFT RETURNED TO GATE. MAINTENANCE INTERROGAT ED CDS WITH NO RELATED FAULTS FOUND. COMPLIED WITH OPS CHECK OF THE ELEVATOR CONTROL STICK PUSHER SYSTEM IAW Q400 AMM T ASK 27-33-00-710-802. OPS TEST IS GOOD WITH NO DISCREPANCIES NOTED AND NO REOCCURRENCE OF CAUTION LIGHT. NO PARTS REPL ACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007081600057 20070816 00057 NM 2007 8 16 QXEA200701238 1 20070805 A 3620 8209083 SWITCH BOMBDR DHC8 DHC8402 1390042 NM NR 1 NACELLE MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 414QX 4061 SJC FLIGHT: NR 1 BLEED HOT CAUTION LIGHT AT CRUISE. C/W CHECK LIST AND SELECTED BLEED OFF. LIGHT EXTINGUISHED. MAINTE NANCE REMOVED AND REPLACED NR 1 NACELLE DUCT LEAK OVERTEMP SWITCH IAW TASK 36-11-21-000-801 AND 36-11-21-400-801. OPS C HECK GOOD. AIRCRAFT RETURNED TO SERIVCE. 2 H 7 2 4T RT A13NM 2007081600059 20070816 00059 EU 2007 8 16 MALA070094 1 20070805 A 3020 DUCT SAAB SF340 340B 7860101 EU RT ENGINE BURNED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 453XJ 340B453 DURING DESCENT, NOTED BURNING PLASTIC ODOR IN COCKPIT AS WELL AS FORWARD CABIN. TURNED ENGINE ANTI-ICE OFF WHEN OUT OF ICING CONDITIONS, ODOR DISSIPATED. ON POST FLIGHT INSPECTION, RT ENGINE MATS BURNED THROUGH IN SEVERAL PLACES. REMOVED AND REPLACED RT LOWER INLET DUCT ASSY I.E. SF3 AM 71-60-05. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 2007081600060 20070816 00060 2007 8 16 F3LA200700191 4 20070731 A 2565 GIRT BAR AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 803FR 5201 2017 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON L2 DOOR SEAL NUT PLATE HOLE AFT OF AFT GIRT BAR FITTING PLATE. REPAI RED PER EA A8-53R-12044. 2 L 7 2 4F RT 2007081600061 20070816 00061 EU 2007 8 16 F3LA200700192 1 20070801 A 5320 D5348015800600 PLATE AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 803FR 5201 2017 DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR FWD AND AFT GIRT BAR FITTING BLANKING PLATES CORRODED. REPLACED L2 DOOR F WD AND AFT GIRT BAR FITTING BLANKING PLATES IAW AMM 52-11-31-991-011/012. 2 L 7 2 4F RT 2007081600062 20070816 00062 SO 2007 8 16 LR7A07061 1 20070728 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FS 836, LBL 83 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 319 4763 DURING SCHEDULED A-1 CHECK PER JOB CARD HA1201, FOUND LEFT BULKHEAD WEB CRACKED AT FS 836, LBL 83, WL 212-223. REPAIRED BULKHEAD WEB IAW LAC MEA 382-53-07-053. 2 H 7 4 4T A1SO 2007081600063 20070816 00063 SO 2007 8 16 LR7A07062 1 20070728 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FS 836 RBL 83 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 319 4763 DURING SCHEDULED A-1 CHECK PER JOB CARD HA1201, FOUND RIGHT BULKHEAD WEB CRACKED AT FS 836, RBL 83, WL 212-222. REPAIRE D BULKHEAD WEB IAW LAC MEA 382-53-07-053. 2 H 7 4 4T A1SO 2007081600064 20070816 00064 SO 2007 8 16 LR7A07063 1 20070726 A 5330 SKIN LKHEED 382 382G 526414U SO FS 815E, LBL 63 DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 325 4590 DURING SCHEDULED A-1 CHECK PER JOB CARD HA1201, FOUND EXTERIOR FUSELAGE SKIN DENTED AT FS 815E, LBL 63, WL 144. REPAIRE D SKIN IAW LAC MEA 382-53-07-051. 2 H 7 4 4T A1SO 2007081600067 20070816 00067 EU 2007 8 16 F3LA200700190 1 20070803 A 5320 FLOOR SUPPORT AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 803FR 5201 2017 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT AT FR 66 TO FR 70 AT Y1292, FWD INBD FASTENER LOCATIONS . REPLACED FLOOR SUPPORT BETWEEN FR 66 AND FR 68 PER SRM 51-42-11. REPAIRED OTHER DAMAGE TO FLOOR SUPPORT IAW EA A8-53 R-12042. 2 L 7 2 4F RT 2007081600070 20070816 00070 NM 2007 8 16 07FDEA02765 1 20070804 A 5730 ARB74021 SKIN DOUG MD11 MD11F 3023600 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48792 CRACK INDICATIONS REVEALED IN 06 EA FASTENER HOLES TOWARDS EDGE OF ACCESS C/OUT IN LT WING LOWER SKIN ACCESS DOOR CUT OU T BETWEEN STA XORS= 683.400 TO XORS= 713.600. REPAIRED AS PER FEDEX EA 1-5710-112375, REPAIR CLASSIFIED AS MAJOR AS PE R GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007081600071 20070816 00071 WP 2007 8 16 07FDEA02778 1 20070806 A 5313 STRINGER DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 CENTER WHEEL WELL AREA L51R END FITTING HAS CORROSION IN AREAS STA 1509 TO 1521. [08-21-07] REMOVED, FABRICATED, AN D INSTALLED FITTING P/N AYB 7020-1 STA.1509 TO 1521 L51R IAW DC/MD10 SRM 51-33-01 VOLII,53-00-01 FIG. 1B VOLII,51-21-01 VOLII,51-21-02 VOLII AND DAC DWG AYB 7020. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2007081600072 20070816 00072 WP 2007 8 16 07FDEA02779 1 20070806 A 5313 STRINGER DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 CENTER WHEEL WELL AREA L52 END FITTING HAS CORROSION IN AREAS STA1509 TO 1521. [08-21-07] RMEOVED, FABRICATED, IN STALLED FITTING P/N AYB7020-2 IAW DC/MD10 SRM 51-33-01 VOLII, 53-00-01FIG 1B VOLII, 51-21-01 VOLII, 51-21-02 VOL II A ND DAC DWG AYB 7020. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2007081600074 20070816 00074 NM 2007 8 16 07FDEA02781 1 20070807 A 5753 65192508 FLAP TRACK BOEING 727 727233 138408A NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 ON NON-ROUTINE, RIGHT OUTBD FLAP TRACK HAS CORROSION. ON NON- ROUTINE, RIGHT OUTBD FLAP TRACK HAS WEAR ON TOP OF TRACK . NON- ROUTINE, RIGHT OUTBD FLAP TRACK HAS LIGHT RUST IN FWD HORIZONTAL HOLE AT MOUNT PAD. REPLACED NR 8 FLAP TRACK. NEW FLAP TRACK IS INSTALLED ON W/C 27X5710-03 , REPLACING FLAP TRACK WILL ADDRESS NON ROUTINE, N00435, N00436, N00437. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007081600077 20070816 00077 NM 2007 8 16 07FDEA02784 1 20070807 A 5753 65192493 FLAP TRACK BOEING 727 727233 138408A NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 NR 3 (LT) FLAP OB TRACK, HAS RUST AT UPPER MOUNTING SURFACE C/T SPOILER BEAM ATTACH PT. REPLACED NR 3 TRACK, NEW TRACK IS INSTALLED ON W/C 27X5705-03, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007081600078 20070816 00078 NM 2007 8 16 07FDEA02785 1 20070807 A 5320 ANGLE BOEING 727 7272S2F 1384O81 NM LWR FUS CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 212FE 22934 LOWER FUSELAGE ANGLE BRACKET SUPPORT HAS HEAVY CORROSION AT STA 804 - STA 825.94 LBL 0 CUT OUT DAMAGED AREA IAW SRM 51 -40-3. FABRICATED 9 REPAIR PARTS IAW SRM 51-40-4. LOCATED AND DRILLED IAW SRM 51-30-5, TREATED AND PRIMED IAW SRM 51-1 0-2, AND INSTALLED ANGLES IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2007081600079 20070816 00079 NM 2007 8 16 07FDEA02786 1 20070807 A 2611 774001 SMOKE DETECTOR BOEING 727 727277 138408S NM NR 6 FAILED A FDEA B EMER. DESCENT N FALSE WARNING DE DESCENT 1 SO 25 246FE 8799 8799 22068 DESCENT BELL SOUNDED MAIN FIRE LIGHT ILLUMINATED, SMOKE ILLUMINATED. EMERGENCY DECLARED. FUMES WERE PRESENT IN THE C OCKPIT. ALL EMERGENCY QRH CHECKLIST ACCOMPLISHED. WHILE ENTERING A/C NOTICED NO ODOR OF ANY SORT, INSPECTED A/C FOR A NY SIGNS OF HEAT STRESS OR FIRE NONE FOUND, SUSPECT BAD SMOKE DETECTOR. REMOVED AND REPLACED NR 6 SMOKE DETECTOR OPS CH ECKS NORMAL AS PER 727 M/M 26-16-001-4. A/C OK TO CONTINUE. 2 L 7 3 4F RT A3WE 2007081600080 20070816 00080 2007 8 16 DHLA200700038 4 20070807 A 3417 ADC AIRBUS 300 A300B4203 3930306 EU NR 1 FAULTED A DHLA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 05 366DH 249 REJECTED T/O NO CAPT AIRSPEED INDICATION EITHER ANALOG OR DIGITAL. REJECTED AT 90 KTS 275,000 LBS +26C BRAKE ENERGY NO RMAL. RII REQ 1. REPLACED NR 1 ADC AS PER MM 34-12-34. GROUND TEST NR 1 ADC PER MMS 34-11-20. SYS OPS TEST NORMAL.PIT OT/STATIC TEST PERFORMED PER MMS 34-11-20. A/C RVSM COMPLIANT W/ ADC RVSM CK-OUT TEST. 2 L 7 2 4F RT A35EU 2007081600081 20070816 00081 WP 2007 8 16 IXXA070037O 1 20070805 A 2797 WIRE DOUG DC8 DC872 302199B WP TERMINAL BLOCK ARCED A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 11 721CX 84175 2422 46013 DURING APPROACH INTO KBWI, THE FLIGHT ATTENDANT NOTICED A FLASH AT THE CIRCUIT PANEL ABOVE THE RIGHT AFT SERVICE DOOR. T HE CREW CONTINUED WITH THE APPROACH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND POWER WIRES CONTACTING LATCH OTHER BEHIND TERMINAL BLOCK, REPOSITIONED WIRES IAW DC8 MAINTENANCE MANUAL 20-512-1. AIRCRAFT WAS RETURNED TO SE RVICE. 2 L 7 4 4F RT 4A25 2007081600082 20070816 00082 NM 2007 8 16 KNNA200700036 1 20070426 A 5330 SKIN BOEING 737 7372Q8 138448K NM PWA JT8 JT8D17 52049 NE BS 995-1000 DENTED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 413JG 23148 UPPER LOBE/SEVERAL DENTS ON FUSELAGE SKIN FROM BS 995 TO BS1000 BETWEEN S-15L TO S-16L, NEAR DOOR L2.ACO NR 075385 REV 0 . PROVIDES INSTRUCTIONS ON REPAIR OF FUSELAGE SKIN AFT OF L2 DOOR, SRM 53-30-3 FIG 46 AND FIG 48 BOEING MESSAGE 1-37724 7518-4 WITH FAA 8100-9. 2 L 7 2 4F 4 F RT A16WE E2EA 2007081600084 20070816 00084 WP 2007 8 16 IXXA07SMN187S 1 20070630 A 5713 STRINGER DOUG DC8 DC873F 302199F WP WS 190 S58 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND NR 4 MAIN TANK CRACKED STRINGER AT STATION XRS 190.000 AND STRINGER 58. ACCES S THROUGH 505D DOOR. REMOVED FUEL PUMP MOUNT BRACKET. REMOVED DAMAGED AREA AT UPPER HORIZONTAL AND VERTICAL FLANGES. PERFORMED NDT INSPECTION. AFTER CUT NO CRACK, OR CORROSION AFTER NDT INSPECTION. FABRICATED ZETA REPAIR AND CHANNEL RE PAIR. PERFORMED HEAT TREATMENT. CLEANED AND APPLIED POLYURETHANE TO COATING YELLOW. APPLIED SEALANT TO FAYING SURFACE S. INSTALLED REPAIR PARTS IAW FAA FORM 8100-9 DATED 07/25/07, BOEING MESSAGE NUMBER1-441074632-2 DATED 07-25-07 AND MES SAGE NUMBER 1-405802251-5 DATED 07-11-07 SKETCH JCTO4211, SEMAN DRAWING ED-4588-1, DC8 SRM 51-1-20D, DC8 NDT SPM PAR 06- 2 L 7 4 4F RT 4A25 2007081600086 20070816 00086 NM 2007 8 16 AALA20071382 1 20070731 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 395AN 29432 DFW - EMERGENCY LIGHT AT LEFT OVERWING MID POSITION INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT OVERWING MID POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007081600087 20070816 00087 NM 2007 8 16 AALA20071383 1 20070731 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 391AA 27451 MIA - EMERGENCY LIGHT AT OVERHEAD RIGHT MID GALLEY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD RIGHT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007081600088 20070816 00088 2007 8 16 AALA20071384 4 20070731 A 2565 HOOK AND LOOP DOUG DC9 DC982 3022082 WP L2 DOOR INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 ORD - L2 DOOR SLIDE GIRT BAR HOOK AND LOOP STRIP IS DIRTY AND WILL NOT HOLD. REPLACED LEFT NUMBER TWO DOOR SLIDE. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081600089 20070816 00089 WP 2007 8 16 AALA20071385 1 20070731 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7534A 49988 STL - EMERGENCY LIGHT AT FORWARD RIGHT VENTRAL STAIRWAY INOPERATIVE. REPLACED CONNECTOR FOR EMERGENCY LIGHT AT FORWARD RIGHT VENTRAL STAIRWAY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081600091 20070816 00091 NM 2007 8 16 AALA20071397 1 20070804 A 3350 0201720003 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 386AA 27060 ORD - EMERGENCY LIGHT AT SEAT 21F INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 21F. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007081600092 20070816 00092 EU 2007 8 16 AALA20071387 1 20070801 A 2820 SENSOR AIRBUS 300 A300B4605R 3930308 EU GRAVITY CONTROL INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 18066 509 MIA INFLIGHT T2251/01AUG MCO TO SJU - AIRCRAFT EXPERIENCED UNWANTED FUEL TRANSFER INTO THE TRIM TANK. LANDED MIA WITHOU T INCIDENT. REPLACED CENTER OF GRAVITY CONTROL SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007081600093 20070816 00093 NM 2007 8 16 AALA20071388 1 20070801 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 389AA 27449 DFW - EMERGENCY LIGHT AT RIGHT OVERWING FORWARD POSITION INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT OVERW ING FORWARD POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007081600098 20070816 00098 NM 2007 8 16 AALA20071403 1 20070804 A 3350 BALLAST BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 972AN 30097 MIA - EMERGENCY LIGHT AT SEAT 13A SIDEWALL AT OVERHEAD EMERGENCY DOOR INOPERATIVE. REPLACED BALLEST FOR EMERGENCY LIGHT AT SEAT 13A SIDEWALL AT OVERHEAD EMERGENCY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007081600099 20070816 00099 NM 2007 8 16 AALA20071391 1 20070802 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 683A 25340 ORD - EMERGENCY LIGHT AT SEAT 17D BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081600101 20070816 00101 NM 2007 8 16 AALA20071394 1 20070802 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 371AA 25198 DFW - EXTERIOR EMERGENCY LIGHT AT OVERWING INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007081600102 20070816 00102 NM 2007 8 16 AALA20071398 1 20070804 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 776AN 29582 MIA - EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007081600103 20070816 00103 NM 2007 8 16 AALA20071399 1 20070804 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 776AN 29582 MIA - EMERGENCY LIGHT AT SEAT 22C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007081600106 20070816 00106 WP 2007 8 16 AALA20071411 1 20070803 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 DFW - EMERGENCY LIGHT MARKER AT RIGHT AFT EXIT BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT MARKER AT RIGHT AFT EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081600107 20070816 00107 WP 2007 8 16 AALA20071412 1 20070803 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 DFW - EMERGENCY LIGHT AT FORWARD GALLEY WALL BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FORWARD GALLEY WAL L. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081600109 20070816 00109 NM 2007 8 16 AALA20071417 1 20070806 A 3350 6011779 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9420D 49824 DFW - EMERGENCY LIGHTS AT AFT SERVICE DOOR EXIT IDENTIFIERS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT SERVICE DOOR EXIT IDENTIFIERS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2007081600110 20070816 00110 NM 2007 8 16 AALA20071414 1 20070805 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 908AN 29510 MIA - EMERGENCY LIGHTS AT SEAT ROWS 12D TO 14D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 12D TO 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007081500126 20070815 00126 NM 2007 8 15 07FDEA02722 1 20070802 A 5320 6556129 THRESHOLD BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT PIT CARGO DOOR THRESHOLD AREA BEAM WEB CORRODED, STA 950E - 990 RBL 21"-22", WL 145 - 148 REMOVED CORROSION FROM AFT PIT CARGO DOOR THRESHOLD WEB BEAM AREA, FOUND TO BE OUT OF LIMITS. REMOVED Z- ANGLE FWD/AFT FOR ACCESS UPPER CHORD BEA M. FABRICATED AND INSTALLED WEB/CHORD, Z-ANGLES FWD/AFT REF SRM 51-30-2 PG 2GMM7-0-1001 PG 2. 2 L 7 3 4F RT A3WE 2007081500130 20070815 00130 EU 2007 8 15 07FDEA02725 1 20070802 A 5340 A53773644203 FITTING AIRBUS 300 A300B4605R 3930308 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 ELONGATED HOLE (DIA 6,6MM), FOUND IN CORNER FITTING (P/N: A537-73644-203) AT C31, P'40-41, RT. REPAIR PERFORMED BY INST ALLING A BUSHING (RE0016-202, DIA. 8MM) IAW EFW CONCESSION DD-0713005. 2 L 7 2 4F RT A35EU 2007081500148 20070815 00148 SO 2007 8 15 LR7A07060 1 20070727 A 2612 CONTROL BOX LKHEED 382 382G 526414U SO FIRE DETECTION MALFUNCTIONED A LR7A E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 AL 03 402LC 1066 4698 DURING CRUISE FLIGHT, FLIGHT CREW REPORTED NR 3 ENGINE FIRE WARNING LIGHT CAME ON. ENGINE SHUT DOWN IAW PROCEDURES. MA INTENANCE FOUND FIRE DETECTION CONTROL BOX MALFUNCTIONED AND REPLACED WITH SERVICEABLE UNIT IAW SMP581 26-10. 2 H 7 4 4T A1SO 2007081500166 20070815 00166 EA 2007 8 15 SWIA200718548 1 20070731 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 614SK 10051 PAX EMERGENCY LIGHT INOP NEAR LAST ROW, FLIGHT NR 4032. RELAMPED EMERGENCY LIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007081500167 20070815 00167 EA 2007 8 15 SWIA200718549 1 20070728 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 367CA 10069 AFT CEILING EMERGENCY EXIT LIGHT IS INOP, FLIGHT NR 1001. RELAMPED AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007081500168 20070815 00168 EA 2007 8 15 SWIA200718550 1 20070801 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 935SW 7725 OVERHEAD EMERGENCY EXIT LIGHT IN CABIN INOP, FLIGHT NR 5879. RELAMPED EMERGENCY OVERHEAD LIGHT AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007081500169 20070815 00169 EA 2007 8 15 SWIA200718551 1 20070731 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 938SW 7741 FORWARD PORTION OF PAX DOOR IS CRACKED UNDERNEATH TOP STEP. REPAIRED CRACK IAW AMM REO 601R-52-11-279. 2 L 7 2 4F RT A21EA 2007081500171 20070815 00171 EA 2007 8 15 SWIA200718553 1 20070729 A 3610 DUCT CNDAIR CL600 CL6002C10 1390015 EA RT BLEED CRACKED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 726SK 10190 RIGHT BLEED DUCT WARNING ON CLIMB-OUT. RETURNED TO FIELD, FLIGHT NR 6781. REPLACED CRACKED DUCTS AND SENSING ELEMENTS ON RIGHT SIDE. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007081500193 20070815 00193 NM 2007 8 15 HALA0700318 1 20070731 A 2897 CONNECTOR BOEING 767 767332 1382001 NM PRESSURE SWITCH DIRTY A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM - R AFT BOOST PUMP LOW PRESS LGT FAILED TO ILLUM AND EICAS MSG FAILED TO DISPLAY WITH SW OFF. CLEANED CONTACTS AT PRESS SWITCH CONNECTOR. PRESS LIGHT AND EICAS MSG FUNCT NORMAL. OPS CK R AFT BOOST PUMP PER AMM 28 -27-00, OPS NORMAL. 2 L 7 2 4F RT A1NM 2007081500194 20070815 00194 NM 2007 8 15 CALA0700414 1 20070806 A 3350 AD20131A BATTERY PACK BOEING 757 757200 1384950 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13110 27300 INSPECTION FOUND EMERGENCY AISLE LIGHTS AT ROW 7 THROUGH 14 INOPERATIVE. THE BATTERY PACK AND CHARGER WERE REMOVED AND REPLACED. 2 L 7 2 4F RT A2NM 2007081500198 20070815 00198 NM 2007 8 15 DL764070972 1 20070725 A 5755 STRUCTURE BOEING 767 767432ER 1385134 NM NR 5 SPOILER DAMAGED A DALA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SO 27 834MH 29707 LEFT INBOARD MAIN AND AFT FLAPS AND NUMBER 5 GROUND SPOILER DAMAGED AS A RESULT OF NUMBER 5 TIRE FAILURE. REPLACED LEFT INBOARD MAIN AND AFT FLAP AND GROUND SPOILER FLIGHT ORIGINALLY SCHEDULED FROM ATL-HNL DIVERTED TO LAX. 2 L 7 2 4F RT A1NM 2007081500201 20070815 00201 NM 2007 8 15 DL757070975 1 20070801 A 5711 112N20086 SPAR BOEING 757 757232 1384965 NM RT WING DAMAGED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 635DL 23762 DURING REMOVAL OF A RT WING LOWER PANEL, A FASTENER HOLE WAS MISDRILLED AND OVERSIZED THROUGH THE PANEL EXTERIOR SKIN AN D THE FRONT SPAR LOWER CHORD. PERMANENT REPAIR WAS ACCOMPLISHED BY ACTS IN VANCOUVER. 2 L 7 2 4F RT A2NM 2007081500204 20070815 00204 NE 2007 8 15 ABXA070253 2 20070802 A 7200 JT8D15 ENGINE DOUG DC9 DC941 302207N WP PWA JT8 JT8D15 52051 NE RIGHT MALFUNCTIONED A ABXA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 23 969AX 40738 47464 686238 RIGHT OIL STRAINER CLOGGING ANNUNCIATOR ILLUMINATED IN FLIGHT. SECURED RIGHT ENGINE. REPLACED RIGHT ENGINE IAW JOB CAR D 9090010, W/O 60027628. 2 L 7 2 4F 4 F A6WE E2EA 2007081500210 20070815 00210 NM 2007 8 15 DLM88070986 1 20070731 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 950DL 49881 CRACK ON RT CUSP WEB AT STA Y=807 TASK CARD 58-533139 IN PAX CABIN. REPAIRED PER ERA 398191-14MA ON N/R TOO63499 AT HMV -3. 2 L 7 2 4F RT A6WE 2007081500219 20070815 00219 SO 2007 8 15 RAIA00708001 1 20070801 A 3260 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO LANDING GEAR DIRTY A RAIA B EMER. DESCENT N FALSE WARNING LD LANDING 1 CE 03 838HK 145321 FLT NR 8030 - PHL - LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS. MAINTENANCE CLEANED PROXIMITY SWITCHES AND CHECKED S YSTEM NO FAULTS NOTED AT THIS TIME. 2 L 7 2 4T RT T00011AT 2007081500220 20070815 00220 NM 2007 8 15 DLM88070993 1 20070624 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 950DL 49881 FOUND CRACK ON LT CUSP WEB AT STA Y=703. REPAIRED PER ERA 398191-14MA REV A. 2 L 7 2 4F RT A6WE 2007081500227 20070815 00227 SO 2007 8 15 RAIA00708007 1 20070802 A 3340 Q4681 LIGHT EMB 145 EMB145LR 3260212 SO LANDING GEAR INOPERATIVE A RAIA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 CE 03 836HK 145695 FLT NR 7992 - IAD - ALL 3 LANDING LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED ALL LANDING LIGHT BULBS, OPS CHECK GOOD . 2 L 7 2 4T RT T00011AT 2007081500228 20070815 00228 SO 2007 8 15 RAIA00708008 1 20070802 A 2120 A/C PACK EMB 145 EMB145LR 3260212 SO NR 1 FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 840HK 145341 FLT NR 8042 - IAD - PACK 1 FAIL. MAINTENANCE DEFERRED PER MEL. 2 L 7 2 4T RT T00011AT 2007081500229 20070815 00229 NM 2007 8 15 DLM88070995 1 20070624 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 950DL 49881 FOUND CRACK ON LT CUSP WEB AT STA Y=226, REPAIRED PER ERA 398191-14 MA REV A. 2 L 7 2 4F RT A6WE 2007081500233 20070815 00233 SO 2007 8 15 RAIA00708009 1 20070803 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 813HK 145044 PRE FLT NR 5511 - STL - EMERGENCY LIGHT FLOOR PROXIMITY LIGHT INOP. MAINTENANCE REPAIRED BROKEN WIRE TO LIGHT STRIP, OP S CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT T00011AT 2007081500242 20070815 00242 SO 2007 8 15 RAIA00708014 1 20070805 A 3150 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO AUTO THRUST SYS ACTIVATED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 810HK 145231 FLT NR 8087 - DEN - AUTOMATIC TAKEOFF THRUST CONTROL SYSTEM RED WARNING ON TAKEOFF. MAINTENANCE PERFORMED EMB SP-22 REF ERENCE ENGINE EXCEEDANCE MESSAGE, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007081500243 20070815 00243 SO 2007 8 15 RAIA00708015 1 20070806 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 838HK 145321 PRE FLT NR 8036 - IAD - EMERGENCY LIGHT SERVICE DOOR FLOOD LIGHT, SERVICE DOOR EXIT MARKER AND GALLEY WALL EXIT LOCATOR INOP. MAINTENANCE FOUND LOOSE CONNECTOR AND RESECURED, OPS CHECK OK. 2 L 7 2 4T RT T00011AT 2007081500248 20070815 00248 SO 2007 8 15 C2XA07SH044 1 20070804 A 5310 145254800003 DOOR FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12540 145537 SHV - DURING C-CHECK MAINTENANCE FOUND CARGO DOOR CUTOUT WITH VARIOUS AREAS OF CORROSION AT LOWER SECTION. MAINTENANCE INSTALLED NEW LOWER SECTION AT CARGO DOOR CUTOUT IAW EMB 145 SRM 51-40-02 & CPM 51-21-07. AIRCRAFT WAS APPROVED TO RETU RN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007081500254 20070815 00254 NM 2007 8 15 AWXA200700952 1 20070802 A 5610 5893543130 WINDSHIELD BOEING 737 7373B7 1384580 NM COCKPIT CRACKED A AWXA O OTHER O OTHER CR CRUISE 1 WP 28 332AW 19326 19326 23384 IAH - PHX - DIV - LOG 7829027 - CREW REPORTED, AT CRUISE THE AIRCRAFT WAS STRUCK FROM AN UNKNOWN OBJECT CRACKING THE FO' S SIDE WINDOW. THE CREW DEPRESSURIZED, DESCENDED TO FL 100, DECLARED AN EMERGENCY AND DIVERTED TO ELP. THE LANDING WAS UNEVENTFUL. MX REPLACED THE FIRST OFFICERS NR 1 WINDOW. AS A PRECAUTION, MX ALSO REPLACED THE WINDOW HEAT CONTROL UNI T. OPERATIONAL/LEAK CHECK WAS GOOD. UNIT, WINDOW HEAT CONTROL, MFG P/N- 231-2, S/N 6507, TSR: 4862. 2 L 7 2 4F RT A16WE 2007081500270 20070815 00270 SO 2007 8 15 C2XA07CL066 1 20070809 A 3350 110049 POWER SUPPLY EMB 145 EMB145XR 3260214 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16151 145758 DURING ROUTINE MAINTENANCE THE RIGHT FORWARD EMERGENCY LIGHT WOULD NOT ILLUMINATE. THE NR 2 EMERGENCY BATTERY LIGHT POW ER SUPPLY WAS REPLACED. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2007081500272 20070815 00272 NM 2007 8 15 UPS07M50364 1 20070517 A 5753 SKIN DOUG MD11 MD11F 3023600 NM T/E FLAP DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C RIGHT WING I/B FLAP LOWER SURFACE I/B SEGMENT SKIN TO REPLACE DUE TO BADLY PITTED. RIGHT WING I/B FLA P LOWER SURFACE I/B SEGMENT LOWER SKIN REMOVED PER SRM 51-31-01 V2 R38. NEW SKIN FAB PER BOEING DRAWING ARC2736 REV B. NEW SKIN HOLES PICKED UP PER SRM 51-31-01 V2.R38. NEW SKIN PROTECTED PER SRM 51-21-01 V2 R38. NEW SKIN INSTALLED PER SRM 51-31-01V2 R38. RIGHT WING I/B FLAP I/B SEGMENT INSTALLED PER SRM 20-50-02. 2 L 7 3 4F RT A22WE 2007081500282 20070815 00282 WP 2007 8 15 AALA20071346 1 20070723 A 3350 0202226001 SHROUD DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9405T 53141 BOS - EMERGENCY LIGHT AT SEAT 5E FORWARD MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007081500287 20070815 00287 NM 2007 8 15 AALA20071370 1 20070728 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 934AN 29531 DFW - EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A16WE 2007081500298 20070815 00298 WP 2007 8 15 AALA20071360 1 20070726 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 435AA 49453 DFW - EMERGENCY LIGHTS AT FORWARD GALLEY CEILING AND ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD GALLEY CEILING AND ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007081500304 20070815 00304 WP 2007 8 15 AALA20071344 1 20070723 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 553AA 53083 LGA - EMERGENCY LIGHTS AT TAILCONE INOPERATIVE. REPLACED BATTERY PACK AT LEFT AFT LAVATORY OVERHEAD FOR EMERGENCY LIGHT S AT TAILCONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081500320 20070815 00320 SO 2007 8 15 RAIA00708017 1 20070807 A 3350 LIGHT EMB 145 EMB145 3260210 SO EXTERIOR INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 807HK 145119 POST FLT NR 3565 - PIT - EMERGENCY LIGHT ON HANDRAIL MAIN DOOR EXTERIOR FLOOD LIGHT INOP. MAINTENANCE DEFERRED PER MEL. 2 L 7 2 4F RT T00011AT 2007081500323 20070815 00323 SO 2007 8 15 RAIA00708020 1 20070808 A 3397 WIRE EMB 145 EMB145 3260210 SO CABIN SHORTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 805HK 145096 PRE FLT NR 3567 - RIC - FLOOR STRIP EMERGENCY LIGHTS INOP. MAINTENANCE INSPECTED FLOOR STRIP FOUND A SHORTED WIRE AND R EPAIRED IT, OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT T00011AT 2007081500325 20070815 00325 SO 2007 8 15 RAIA00708022 1 20070809 A 2720 14520226601 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO RUDDER DEFECTIVE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 811HK 145256 FLT NR 5467 - STL - EICAS MESSAGE - NR 2 RUDDER SYSTEM INOP. MAINTENANCE REMOVED AND REPLACED NR 2 PRESSURE SWITCH, NO LEAKS NOTED CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2007081500326 20070815 00326 SO 2007 8 15 RAIA00708023 1 20070809 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN UNSECURE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 817HK 145058 PRE FLT NR 5599 - STL - EMERGENCY LIGHT GALLEY WALL EXIT LOCATOR INOP. MAINTENANCE RESET POWER TO EMERGENCY LIGHT SYSTE M AND RESECURED WIRING, OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT T00011AT 2007081500328 20070815 00328 NM 2007 8 15 USAA070596 1 20070807 A 5313 STRINGER BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 STA 400 STR 4R CRACKED. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-10-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007081500338 20070815 00338 NM 2007 8 15 USAA070591 1 20070807 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 BS 328 & LBL 45 CRACKED. REMOVED & REPLACED INTERCOSTAL PER SRM 51-70-11, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007081500340 20070815 00340 NM 2007 8 15 USAA070593 1 20070807 A 5320 FLOOR SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 STA 663, LBL 32 FLOOR SKIN AT AILERON QUADRANT CRACKED. INSTALLED REPAIR DOUBLER & SHIMS PER TR 53-60-04, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007081500346 20070815 00346 EU 2007 8 15 BA07012 1 20070801 A 5270 867803 COMPUTER AIRBUS 330 A330323 3930335 EU DOOR WARNING FAILED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 274AY 34207 2360 0342 FLIGHT 1071, PHL-SJU: FLIGHT RETURNED TO PHL DUE TO AN AFT CARGO DOOR OPEN INDICATION. UPDATED 8/3/07: MAINTENANCE RE PLACED THE PROXIMITY SENSOR COMPUTER. NO FURTHER FAULTS. 2 L 7 2 4F RT A46NM 2007081500349 20070815 00349 NM 2007 8 15 BB07060 1 20070807 A 3350 S417N5092 LIGHT BOEING 767 7672B7 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 253AY 24894 L1 DOOR FLOOR LEVEL LIGHT FOUND INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. 2 L 7 2 4F RT A1NM 2007081500374 20070815 00374 EA 2007 8 15 TRAX200701100 1 20070802 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR PEELING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 884AS 7513 ASD EXIT PLACARD PEELING LOOSE. 2 L 7 2 4F RT A21EA 2007081500382 20070815 00382 NM 2007 8 15 USAA920070798 1 20070728 A 5320 141N516079 ANGLE BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 923UW 22203 PIT - MAJOR REPAIR - C4 CHECK, CORROSION ON Z-ANGLE, BS 345, S17R. REPLACED Z-ANGLE, BS 345, S17R IAW B757-200 SRM 51-4 0-02. 2 L 7 2 4F RT A2NM 2007081500383 20070815 00383 EA 2007 8 15 TRAX200701056 1 20070725 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 854AS 7382 INBOARD 280 CLIP AT RBL 9 IS CRACKED. REMOVED DAMAGED 280 CLIP. DUPLICATED PART FROM 2024T3 .050 PO 950029, ALODINED & PRIMED IAW CRJ SRM 51-24-16, 51-25-06 JB13225. OK TO INSTALL JB13225. INSTALLED CLIP AT LBL 9 IAW CRJ 200 SRM 51-42-2 1 LC14030 8-4-07. SUPPLEMENTAL - SDR CLOSED 08/07/07. 2 L 7 2 4F RT A21EA 2007081600005 20070816 00005 EA 2007 8 16 QXEA200701228 1 20070731 A 5230 DOOR CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY OPEN A QXEA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 NM 09 605QX 10022 SFO- FLIGHT 2524, AFTER TAKEOFF, DURING CLIMB RECEIVED A CABIN ALTITUDE MESSAGE. DIVERTED AIRCRAFT TO OAKLAND AND ACCOM PLISHED A UNEVENTFUL LANDING. MAINTENANCE FOUND THE AFT CARGO DOOR NOT PROPERLY CLOSED, AFT SECTION OF DOOR NOT SECURE. PERFORMED OPERATIONAL CHECK OF DOOR WITH NO DEFECTS FOUND. PERFORMED PRESSURIZATION CHECK WITH NO DEFECTS FOUND. AIR CRAFT RETURNED TO SERVICE WITH NO PARTS REPLACEMENTS. 2 L 7 2 4F RT A21EA 2007081600006 20070816 00006 EA 2007 8 16 MDGA2007977AA 2 20070804 A 7200 ENGINE BEECH 90 C90 1152913 CE PWA PT6 PT6A20 52043 EA LEFT SHUTDOWN E MDGA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 09 977AA LJ555 PCE21234 LEFT ENGINE INFLIGHT SHUT DOWN, PILOTS REPORT LOSS OF TORQUE AND RISE IN ITT, ENGINE SHUT DOWN AND A SAFE LANDING COMPLE TED. 1 L 7 2 3T 3 T 3A20 E4EA 2007081600009 20070816 00009 NM 2007 8 16 DHL2007741528 1 20070803 A 5320 CHANNEL BOEING 727 7272Q9 138448M NM BS 312 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 NOSE SECTION INTERIOR HORIZ WALKWAY BEAM LEFT SIDE WEB SUPPORT ANGLE ("C" CHANNEL) CORRODED AT BS 312. REMOVED CORROSIO N, MATERIAL REMOVAL EXCEEDED LIMITS PER B727 SRM 53-10-1 FIG 1. REMOVED "C" CHANNEL, FABRICATED NEW CHANNEL FROM AND 10 137-3001 7075-T6 EXTRUSION, 29.5" LONG, PO NR 7212319, PER B727 SRM 53-10-2 FIG 1 AND 51-20-1. TREATED, PRIMED, AND INS TALLED NEW "C" CHANNEL PER B727 SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007081600010 20070816 00010 WP 2007 8 16 FX7A200700004 1 20070429 A 3222 PACKING DOUG DC9 DC982 3022082 WP NLG STRUT CRACKED A FX7A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 905TA 36626 7003 49905 NOSE GEAR RED UNSAFE LIGHT ON WITH GEAR UP. TROUBLESHOOT AND FOUND THE NLG STRUT NITROGEN FILL VALVE PACKING CRACKED. REMOVED AND REPLACED THE PACKING AND SERVICED NLG IAW MM REF 32-21-02. 2 L 7 2 4F A6WE 2007081600015 20070816 00015 SO 2007 8 16 SIMA200721805 1 20070804 A 2430 806CC01 CONTACTOR EMB 145 EMB145LR 3260212 SO ESSENTIAL BUSS FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 933JN 5716 14500918 RECEIVED EMERGENCY ABNORMAL AND EMERGENCY LIGHT NOT ARMED MESSAGE. ALL FOUR GENERATORS AMPS DOUBLED AFTER APU START, DI VERTED TO GGG. REMOVED AND REPLACED NR 2 ESSENTIAL BUSS CONTACTOR IAW EMB AMM 24-60-03 AND ESSENTIAL TIMER RELAY ONE IA W EMB AMM 20-13-02. ALL OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007081600018 20070816 00018 EA 2007 8 16 SIMA200721806 1 20070805 A 3350 2013BR POWER SUPPLY CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 523AE 3395 852 10152 ALL EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED ALL FOUR EMERGENCY POWER SUPPLIES IAW CRJ AMM 33-51-17. OPERATI ONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007081600032 20070816 00032 NM 2007 8 16 AWXA200700957 1 20070705 A 5754 65C267943 SKIN BOEING 737 7373G7 1384595 NM NR 2 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961254, LEFT WING NR 2 SLAT LOWER SURFACE SKIN CRACKED, SS 235, SS 245 AND SS 253. 5. REPAIRED LEFT WING NR 2 SLAT LOWER SURFACE SKIN, SS 235, SS 245 AND SS 253.5 IAW B737-300 SRM 57-43-01. 2 L 7 2 4F RT A16WE 2007081600041 20070816 00041 NM 2007 8 16 07FDEA02763 1 20070803 A 5242 SEAL DOUG MD11 MD11F 3023600 NM E/E DOOR TORN A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 592FE 48550 PDIS AT FL210 AND CLIMBING HEARD LOUD BANG FOLLOWED BY SOUND OF RUSHING AIR. CABIN ALTITUDE BEGAN CLIMB. STOPPED CLIMB AT 230 AND CABIN CONTINUED TO CLIMB. SUSPECT LOSS OF AVIONICS DOOR SEAL AND RTB. FOUND E/E DOOR SEAL TORN, MPN ABA780 0-1. REMOVED AND REPLACED AVIONICS DOOR SEAL ASSY AS PER SMP. PERFORMED ADJ/TEST OF AVIONICS DOOR ASSY AS PER MD-11 A MM 52-41-01-5. OPS TEST FOUND OKAY, ALSO PERFORMED FUSELAGE PRESSURE DECAY ADJ/TEST AS PER MD 11 AMM 21-00-00-5, OPS TES T FOUND "SATIS ". 2 L 7 3 4F RT A22WE 2007081600058 20070816 00058 NM 2007 8 16 QXEA200701239 1 20070804 A 3610 SWITCH BOMBDR DHC8 DHC8402 1390042 NM OVERTEMP MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 431QX 4164 SEA FLIGHT NR 2393: NR 1 BLEED HOT CAUTION LIGHT ILLUMINATED WHILE IN CRUISE AT 10,000. ACCOMPLISHED NR 1 BLEED HOT CAU TION CHECKLIST AND ASSOCIATED RAM VENTILATION CHECKLIST. NR 1 BLEED HOT CAUTION LIGHT REMAINED ILLUMINATED FOR DURATION OF FLIGHT AND ALL GROUND UPS. MAINTENANCE REMOVED AND REPLACED NR 1 BLEED AIR OVERTEMP SWITCH IAW Q400 36-11-16, PAGES 401-504. FUNCTIONAL CHECK GOOD. FAULTS CLEARED AND DID NOT REOCCUR. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007081600066 20070816 00066 EU 2007 8 16 SIMA200721901 1 20070806 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 313AE 25655 438 340B313 FOUR EMERGENCY TRACK LIGHTS INOPERATIVE. REMOVED AND REPLACED 24LN EMERGENCY LIGHTING POWER SUPPLY IAW SAAB AMM 33-50-1 0. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007081600076 20070816 00076 NM 2007 8 16 07FDEA02783 1 20070807 A 5753 65192497 FLAP TRACK BOEING 727 727233 138408A NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 RT WING NR 6 FLAP TRACK UPPER ATTACH POINT AT SPOILER BEAM HAS CORROSION. REPLACED NR 6 TRACK, NEW TRACK IS INSTALLED O N W/C 27X5708-03. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007081600090 20070816 00090 WP 2007 8 16 AALA20071386 1 20070731 A 2160 BOOT DOUG DC9 DC982 3022082 WP RT ENGINE LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 3515 49892 LBB INFLIGHT T389/31JUL DFW TO ABQ - DURING FLIGHT CREW RECEIVED TAIL COMPARTMENT HIGH INDICATION. LANDED LBB WITHOUT I NCIDENT. SECURED BOOT AT RIGHT TEMPERATURE CONTROL VALVE INLET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081600094 20070816 00094 NM 2007 8 16 AALA20071389 1 20070801 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 173AN 32399 SFO - EMERGENCY LIGHT AT SEAT ROW 26D INOPERATIVE. REPLACED BATTERY PACK M100801 FOR EMERGENCY LIGHT AT SEAT ROW 26D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081600095 20070816 00095 NM 2007 8 16 AALA20071393 1 20070802 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 643AA 24601 LAX - EMERGENCY EXIT SIGN LIGHT AT RIGHT SIDE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN LIGHT AT RIGH T SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081600097 20070816 00097 NE 2007 8 16 AALA20071402 2 20070804 A 7200 N14FF104 TRANSDUCER BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 684AA 25341 31345 IAD INFLIGHT T127/04AUG JFK TO SAN - NR 2 ENGINE INDICATED HIGH ENGINE GAS TEMPERATURE AND COMPRESSOR STALLED. LANDED I AD WITHOUT INCIDENT. REPLACED POWER LEVEL ANGLE TRANSDUCER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2007081600100 20070816 00100 EU 2007 8 16 AALA20071392 1 20070802 A 2913 PUMP AIRBUS 300 A300B4605R 3930308 EU HYD SYSTEM INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 70079 619 JFK INFLIGHT 1171/02AUG - AIRCRAFT LOST GREEN HYDRAULIC SYSTEM FLUID. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REP LACED NUMBER ONE ENGINE GREEN SYSTEM HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007081600111 20070816 00111 NM 2007 8 16 AALA20071415 1 20070806 A 3350 8039001 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9420D 49824 DFW - EMERGENCY LIGHTS AT COCKPIT AND FORWARD CABIN OVERHEAD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT COCKPIT AND FORWARD CABIN OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2007081600112 20070816 00112 NM 2007 8 16 AALA20071419 1 20070806 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 611AM 24487 LAX - EMERGENCY LIGHT AT MID COACH INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT MID COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081600113 20070816 00113 NM 2007 8 16 AALA20071421 1 20070806 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 ORD - EMERGENCY LIGHT AT LEFT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT FORWARD ENTRY D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007081600114 20070816 00114 NM 2007 8 16 AALA20071422 1 20070806 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 ORD - EMERGENCY LIGHT AT AFT LEFT ENTRY DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT AFT LEFT ENTRY DOOR. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007081600115 20070816 00115 NM 2007 8 16 AALA20071423 1 20070806 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 183AN 29593 ORD - EXTERIOR EMERGENCY LIGHT AT RIGHT MID PASSENGER ENTRANCE DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY L IGHT AT RIGHT MID PASSENGER ENTRANCE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081600116 20070816 00116 2007 8 16 AALA20071401 4 20070804 A 2565 CDK1107505 LANYARD DOUG DC9 DC982 3022082 WP DOOR SLIDE FRAYED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 292AA 49304 MSP - FORWARD GALLEY DOOR SLIDE LANYARD CABLE IS FRAYED. REPLACED LANYARD FOR FORWARD GALLEY DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081600117 20070816 00117 NM 2007 8 16 AALA20071420 1 20070806 A 3350 SWITCH BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 ORD - EMERGENCY LIGHTS AT SEAT ROWS 10 TO 13A INOPERATIVE. RESET CABIN AND FLIGHT DECK SWITCHES FOR EMERGENCY LIGHTS AT SEAT ROWS 10 TO 13A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007081600119 20070816 00119 NM 2007 8 16 AALA20071405 1 20070804 A 3350 SHIELD BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AA 24488 SEA - EMERGENCY LIGHT AT SEAT 9D HAS BROKEN SHIELD. REPLACED SHIELD FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081600122 20070816 00122 NM 2007 8 16 AALA20071408 1 20070804 A 3350 LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 324AA 22325 JFK - EMERGENCY LIGHT AT SEAT 19B INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 19B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007081600124 20070816 00124 2007 8 16 AALA20071410 4 20070804 A 2565 HOOK AND LOOP DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 470AA 49600 MSP - LEFT NUMBER ONE DOOR SLIDE HOOK AND LOOP STRIP INOPERATIVE. REPLACED LEFT NR 1 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081600125 20070816 00125 NM 2007 8 16 AALA20071418 1 20070806 A 3397 WIRE DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9420D 49824 DFW - EMERGENCY LIGHT AT OVERHEAD TAIL COMPARTMENT INOPERATIVE. REPAIRED WIRE NUMBER L795B16 AT L2 637 FOR EMERGENCY LI GHT AT OVERHEAD TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2007081600126 20070816 00126 NM 2007 8 16 HALA0700326 1 20070806 A 3240 26124121A BRAKE ASSY BOEING 767 76733A 1385209 NM NR 7 SMOKE A HALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 13 593HA 33424 INFO TO MAINTENANCE ATC GROUND ADVISED SOME SMOKE COMING FROM RT LDG GEAR (BRAKE AND TIRES JUST CHANGED). REMOVED AND R EPLACED NR 7 BRAKE PER M/M 32-41-08 AND REINSTALLED TIRE PER M/M/ 32-45-01. 2 L 7 2 4F RT A1NM 2007081600127 20070816 00127 NM 2007 8 16 HALA0700327 1 20070805 A 3040 6240663 CONTROLLER BOEING 767 7673G5 1385126 NM WINDOW HEAT MALFUNCTIONED A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 584HA 24258 ETOPS SIGNIFICANT SYSTEM, RT FWD WINDOW HEAT SWITCH LIGHT INOPERATIVE DISPLAYED. REMOVED AND REPLACED WINDOW HEAT CONTR OLLER RT SIDE PER AM 30-41-06, OPS CHECKS OK. 2 L 7 2 4F RT A1NM 2007081600128 20070816 00128 NM 2007 8 16 AWXA200700967 1 20070705 A 5313 654988630 STRINGER BOEING 737 7373G7 1384595 NM BS 500D S16R CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961293, CRACKED STRINGER, BS 500D, S16R. REPAIRED STRINGER, BS 500D, S16R IAW AWA ER 03-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2007081600134 20070816 00134 EU 2007 8 16 DHLA200700039 1 20070808 A 3411 PITOT LINE AIRBUS 300 A300B4203 3930306 EU OBSTRUCTED A DHLA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 GL 05 364DH 141 NO AIRSPEED INDICATION ON STANDBY A/S IND AT 80KTS ONCA AND FO IND REJECTED T/O WEIGHT 273.6 26C OAT P.A 73FT BRAKE TEMP 230 1. FLUSHED PITOT STATIC SYSTEM AS PER 34-11-10. OPS NORM AS PER MM 34-11-22 A/C RVSM COMPLIANT. 2 L 7 2 4F RT A35EU 2007081600136 20070816 00136 NM 2007 8 16 DHL2007741532 1 20070804 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 680 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 FWD PIT, RT BS 680.0 MAIN FRAME UPPER FLANGE DENTED, 3 PLACES, BETWEEN STR 21R AND 22R. CUT OUT DAMAGED AREA, 3 EA, 1.5 " BY 1" EA. NOTE: ORIGINAL REPAIR WAS REJECTED AT TIME OF INSTALLATION. REMOVED REJECTED REPAIR PARTS, FABRICATED NEW REPAIR DOUBLER FROM 7075-T0, .071" BY 18" BY 4" BY 1", PO NR 9004650, PER B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1. HE AT TREATED DOUBLER TO T6 CONDITION PER F.A.S.I. ER NR 2-37153-801 REV A. LOCATED, DRILLED UP, TREATED, PRIMED, AND INST ALLED NEW REPAIR DOUBLER PER B727 SRM 51-10-2 AND 51-40-3 FIG 1. COMPLETED REPAIR FINALIZED ON N/R 127496. 2 L 7 3 4F RT A3WE 2007081600137 20070816 00137 EU 2007 8 16 CPCP20070058 1 20070608 A 5320 SUPPORT BRACKET AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 447AM 447 RT "T" SUPPORT BRACKET FOR THRESHOLD AT FR 37 CORRODED. RT "TEE" SUPPORT BRACKET AT FR 37 FABRICATED AS PER SRM 53-67-7 0 FIG 104 AND INSTALLED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007081600139 20070816 00139 EU 2007 8 16 CPCP20070062 1 20070606 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 447AM 447 CORROSION FOUND ON LT SEAT TRACK BETWEEN FRAME 36-39. LEFT SEAT TRACK BETWEEN FRAME REPLACED IAW SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007081600146 20070816 00146 2007 8 16 DL757071008 4 20070803 A 2565 3961899501 LANYARD BOEING 757 757232 1384965 NM R1 DOOR SLIDE BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 655DL 24395 DURING OPERATION 58108 GIRT BAR INSPECTION, THE CABLE WAS NOT ATTACHED TO THE LANYARD. THE CABLE WAS BROKEN. REPLACED LANYARD ASSY. REPLACED LANYARD ASSY PART NUMBER 3961899-501. 2 L 7 2 4F RT A2NM 2007081600147 20070816 00147 NM 2007 8 16 DLM90071010 1 20070802 A 5510 HINGE DOUG MD90 MD9030 3023690 NM HORIZONTAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 VERTICAL TO HORIZONTAL STAB RT I/B HINGE PLATE HAS PITTING CORROSION IN BORES. REMOVED CORROSION AND INSTALLED REPAIR B USHINGS IAW MD90 SRM51-30-05 AND 55-30-05 PARA 5. 2 L 7 2 4F RT A6WE 2007081600149 20070816 00149 NM 2007 8 16 DLM90071012 1 20070802 A 5510 HINGE DOUG MD90 MD9030 3023690 NM HORIZONTAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 VERT TO HORZ STAB LT I/B HINGE PLATE HAS PITTING AND CORROSION ON O/B SURFACE AND IN BORES. REPAIRED IAW MD-90 SRM 55-3 0-05 PARA 5 2 L 7 2 4F RT A6WE 2007081600150 20070816 00150 NM 2007 8 16 DLM90071013 1 20070802 A 5530 HINGE DOUG MD90 MD9030 3023690 NM VERTICAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 VERT TO HORIZ STAB RT O/B HINGE PLATES HAS CORROSION ON I/B AND O/B SURFACES AND PITTING CORROSION IN BORES. REPAIRED R T O/B HINGE PLATE IAW MD-90 SRM 55-30-05 PARA 5. 2 L 7 2 4F RT A6WE 2007081600152 20070816 00152 NM 2007 8 16 DLM90071015 1 20070720 A 5310 59360381 BEAM DOUG MD90 MD9030 3023690 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 AFT PIT DOOR CUT OUT LOWER BEAM CORRODED ON VERTICAL AND HORIZONTAL FLANGE. REPAIRED AFT PIT DOOR CUT OUT LOWER BEAM IA W MD-80 SRM 53-05D FIG 63 AND SRM 51-00-01 PG 2 MD90. 2 L 7 2 4F RT A6WE 2007081600154 20070816 00154 NM 2007 8 16 DLM90071019 1 20070805 A 3230 BYPASS SWITCH DOUG MD90 MD9030 3023690 NM MLG OUT OF ADJUST A DALA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 SO 27 901DA 53381 LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. FOUND BYPASS HANDLE IN BYPASS POSITION. CYCLED AND STOWED HANDLE SEVERAL TI MES. ALL OPERATIONS NORMAL. 2 L 7 2 4F RT A6WE 2007081600155 20070816 00155 NM 2007 8 16 DL76L071020 1 20070803 A 2913 887673 PUMP BOEING 767 767332 1382001 NM HYD SYSTEM LOW PRESSURE A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 197DN 28454 LEFT PRIMARY HYD PUMP EICAS MSG CAME ON. LOW SYSTEM PRESSURE. LOW ENG HYD PUMP OUTPUT. REMOVED AND REPLACED LEFT ENG EDP PER AMM. REMOVED AND REPLACED PRESSURE AND CASE DRAIN FILTER PER AMM. OP AND LEAK CHECK OKAY. 2 L 7 2 4F RT A1NM 2007081600157 20070816 00157 NM 2007 8 16 DL757071024 1 20070805 A 2120 UNKNOWN BOEING 757 757232 1384965 NM CABIN SMOKE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 640DL 23994 ON TOP OF CLIMB-OUT FLT CREW REPORTED A SLIGHT SMOKE HAZE WITH A RUBBER SMELL LOC AROUND SEAT ROW 36. AFTER LANDING, FL T CREW TRIED TO DUPLICATE PROBLEM BY RUNNING ENGS/PACKS/BLEED SYS/LIGHTING/GALLEY EQUIP. UNABLE TO DUPLICATE PROBLEM. ALSO, PERFORMED AN OVERWEIGHT LANDING INSPECTION PER AMM. 2 L 7 2 4F RT A2NM 2007081600158 20070816 00158 NM 2007 8 16 DLM90071025 1 20070805 A 2150 3965821 CONTROL VALVE DOUG MD90 MD9030 3023690 NM LT A/C PACK INOPERATIVE A DALA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 27 906DA 53386 LEFT PACK COULD NOT PRESSURIZE A/C BECAUSE TO FLOW CONTROL VALVE WAS INOP AND WOULD NOT OPEN BEYOND 1/4 OF A INCH. 2 L 7 2 4F RT A6WE 2007081600159 20070816 00159 2007 8 16 DL76G071028 4 20070802 A 2330 RDKA100601 ENTERTAIN SYS BOEING 767 767332 1382001 NM INOPERATIVE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 174DZ 29693 INFLIGHT ENTERTAINMENT SYSTEM IS INOP. SYSTEM CONTINUES TO REBOOT, RTB. FAULT CONFIRMED T/S IFE SYSTEM FOUND CP BAD. REMOVED AND REPLACED CP IAW 44-24-17, ALL OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 2007081600160 20070816 00160 NM 2007 8 16 DL76P071029 1 20070802 A 2760 CONTROL MODULE BOEING 767 767332 1382001 NM SPOILERS MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 144DA 27584 SPOILERS CAUTION LIGHT ON TAXI OUT. RESET PCA3 FAULT ON 2L SPOILER CONTROL MODULE. OPERATED SPOILERS ALL MODES WITH DI FFERENT POWER SOURCES. 2 L 7 2 4F RT A1NM 2007081600161 20070816 00161 NM 2007 8 16 DL76S071030 1 20070806 A 5315 141T511439 FLOORBEAM BOEING 767 767332 1382001 NM BS 347 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 129DL 24079 FLOORBEAM BS 347 HAD CRACKS IN UPPER CHORD BETWEEN LBL 10 AND RBL 20. DUE TO A WEB REPAIR NEAR RBL 29.5. A SPLICE REPA IR WAS DONE BETWEEN LBL 27 AND RBL 30.5. 2 L 7 2 4F RT A1NM 2007081600165 20070816 00165 NM 2007 8 16 DLM90071036 1 20070803 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 1080 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 RT CUSP WEB CORRODED OUT OF LIMITS FS 1080, TRIMMED OFF DAMAGED CUSP SECTION FABRICATED NEW AND INSTALLED IAW DAL ERA 39 8191-14MA, MD90 SRM 51-30-02, 51-30-01, 51-30-05 AND 51-10-03. 2 L 7 2 4F RT A6WE 2007081600169 20070816 00169 EU 2007 8 16 DHLA200700040 1 20070808 A 3411 PITOT TUBE AIRBUS 300 A300B4203 3930306 EU MALFUNCTIONED A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 05 364DH 141 NO AIRSPEED INDICATION ON STANDBY AIRSPEED INDICATION AT 80 KTS ON CAPT AND FO'S INDICATORS. REJECTED T/O TO WEIGHT 231 .2 OAT 26 DEGS C PA 103FT BRAKE TEMP 200 DEGS C 1. REMOVED AND REPLACED STANDBY AIRSPEED PITOT PROBE AS PER A300 MM 34- 11-15. PERFORMED LEAK CHECK. NO LEAKS NOTED. 2 L 7 2 4F RT A35EU 2007081600170 20070816 00170 EU 2007 8 16 CPCP20070063 1 20070606 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 447AM 447 CORROSION FOUND ON RT SEAT TRACK BETWEEN FRAME 39-40. RIGHT SEAT TRACK BETWEEN FRAME 39-40 REPLACED IAW SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007081600171 20070816 00171 EU 2007 8 16 CPCP20070064 1 20070606 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 447AM 447 CORROSION FOUND ON LT SEAT TRACK BETWEEN FRAME 39-41. NEW SEAT TRACK INSTALLED LEFT BETWEEN FRAME 39-41 AS PER SRM 51-2 5-04. 2 H 7 2 4T RT A53EU 2007081600176 20070816 00176 NM 2007 8 16 QXEA200701242 1 20070806 A 3150 INDICATION SYS BOMBDR DHC8 DHC8402 1390042 NM BLEED DUCT TEMP MALFUNCTIONED A QXEA O OTHER N FALSE WARNING AP APPROACH 1 NM 09 415QX 4081 SMF FLIGHT NR 2415: ON APPROACH, RECEIVED NR 1 BLEED HOT CAUTION LIGHT. SHUT BLEED OFF PER EM CHECKLIST. BUT, LIGHT RE MAINED ON UNTIL AFTER SHUTDOWN. BLEED TEMP ON DUCT TEMP INDICATOR NOT HOT AT TIME OF OCCURRENCE. MAINTENANCE C/W FIM T ASK 36-20-00-810-801. OPS CHECK GOOD. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007081600180 20070816 00180 EU 2007 8 16 CPCP20070069 1 20070606 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 447AM 447 FLOORBEAM 41 CORRODED. FLOORBEAM 41 IS REPAIRED IAW SRM 53-61-40 FIG 412 SHEET 1. 2 H 7 2 4T RT A53EU 2007081600181 20070816 00181 EU 2007 8 16 CPCP20070060 1 20070606 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 447AM 447 CORROSION FOUND ON LT I/B SEAT TRACK BETWEEN FRAME 34-36. LEFT INBOARD FRAME 33-36 SEAT TRACK REPAIR SPLICING AS PER SR M 53-00-00 FIG 435. 2 H 7 2 4T RT A53EU 2007081600182 20070816 00182 EU 2007 8 16 CPCP20070070 1 20070606 A 5313 STRINGER AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 447AM 447 FOUND STR 21-L BETWEEN FRAME 41-40 CORRODED. STR21 L BETWEEN FRAME 40-41 IS REPAIRED IAW SRM 53-00-00 FIG 428 (SHEET 2) . 2 H 7 2 4T RT A53EU 2007081700001 20070817 00001 EU 2007 8 17 YENA2007073 1 20070812 A 3240 C202163382D32 CONTROL UNIT AIRBUS 320 A320232 3930326 EU BRAKE SYSTEM MALFUNCTIONED A YENA K NONE J WARNING INDICATION LD LANDING 1 EA 15 558JB 22127 1746 1915 FLT 919, JFK-ORD, ON LANDING AT APPROX 30KT, AUTOBRAKE FAIL & BRAKE SYSTEM NR 1 FAIL ECAM, AT GATE FOUND BOTH OUTBOARD M AINS FLAT. PERFORMED NORMAL BRAKE CHECK IAW AMM 32-42-00-05, CHECKS NORMAL, PERFORMED BRAKES AND STEERING BITE TEST, NO FAILURES IAW AMM 32-46-00-05, PERFORMED WHEEL FAILURE INSPECTION CHECK. NO DAMAGE NOTED IAW 05-51-15-06. REMOVED & RE PLACED BSCU IAW 32-42-34-04. BITE CHECK GOOD IAW AMM 32-46-00-05. REPLACED & REMOVED ALL 4 MAIN TIRES IAW 32-41-9-0001 . 2 L 7 2 4F RT A28NM 2007081700002 20070817 00002 NM 2007 8 17 UPS07650389 1 20070801 A 3697 CONNECTOR BOEING 767 76734AF 1385212 NM LT ENGINE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 314UP 27742 INSPECTION TYPE:ETOP LT ENGINE PRSOV INOP. FOUND CONNECTOR D17066P RUBBER DETERIORATED AND PIN 1 LOCK BROKEN. REMOVED AND REPLACED CONNECTOR PER WEM 36-11-62 & CHECKED PER MM 36-11-005 & ALL CHECKS NORMAL. ALL VALVES RETURNED TO NORMAL C ONFIGURATION. 2 L 7 2 4F RT A1NM 2007081700006 20070817 00006 WP 2007 8 17 UPS07850380 1 20070714 A 5330 5773863125 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 FUSELAGE EXTERIOR SKIN HAS DEEP GOUGE AND DENT AT STA 160 L21L TO L22L. REPAIR EXTERIOR SKIN IAW SAA EA 008-5330-01-A0966, UPS RAA DC8-53-2064 3. 2 L 7 4 4F RT 4A25 2007081700009 20070817 00009 NM 2007 8 17 UPS07M50382 1 20070608 A 5514 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C RIGHT HORIZONAL STAB NR 36 BARREL NUT BORE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED PER S RM 51-21-01 V2 R38 BOTTOM REM BLEND OUT 0.110" DEEP BORE REAMED 0.2538" DIA REM BLEND OUT 0.090" FOUND EXCEEDING EO LIMI TS. BORE REAMED TO 2.602" & BOTTOM BORED DOWN FURTHER 0. 080" PER EN1364-07. BARREL NUT BORE BLEND OUT & BOTTOM PERIPH ERY SMOOTHEN & PR PROTECTED. BARREL NUT BORE REP C/OUT IS ACCEPTABLE PER EN1364.07. 2 L 7 3 4F RT A22WE 2007081700010 20070817 00010 NM 2007 8 17 UPS07M50383 1 20070627 A 5514 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C LEFT HORIZONAL STAB NR 23 BARREL NUT HOLE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED PER SR M 51-21-01 V2 R38. BORE BOTTOM - SURFACE CLEANED & BORE REAMED TO 1.067" DIA REM B/OUT 0.050" DEEP FOUND EXCEEDING EO L IMITS. BARREL NUT BORE B/OUT & BOTTOM PERIPHERY RADIUS SMOOTHENED & PR PROTECTED PER SRM 51-21-01V2 R38. REP SLEEVE BU SHING FAB & PROTECTED PER EO BARREL NUT BORE REP C/OUT IS ACCEPTABLE PER EN1410-07. 2 L 7 3 4F RT A22WE 2007081700011 20070817 00011 NM 2007 8 17 UPS07M50384 1 20070511 A 5753 NRC6753504 STOP FITTING DOUG MD11 MD11F 3023600 NM T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C RIGHT O/B TRAILING EDGE FLAP STOP FITTING SUSPECTED CRACK (VANE TRACK NR 4 FROM I/B). RIGHT WING O/B TRAILING EDGE FLAP ASSY REMOVED PER AMM27-50-30 R55. HFEC INSP C/OUT PER DA DACNDTSPM R.13 PART 06-10-01-001 ON STOP FI TTING FOUND CRACK. HINGE PANEL SUPPORT AT RIGHT O/B TRAILING EDGE FLAP REMOVED & INSTALLED PER SRM 51-31-01 V2 R38. RI GHT WING O/B TRAILING EDGE NEW FLAP INSTALLED PER AMM 27-50-30 R55. FLAP ADJUSTMENT AND OPERATIONAL CHECK REFER TO EO M D11-5750-23556-E. 2 L 7 3 4F RT A22WE 2007081700012 20070817 00012 NM 2007 8 17 UPS07M50385 1 20070726 A 5210 RETAINER DOUG MD11 MD11F 3023600 NM R1 DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C CABIN - TOOL MARKS ON R1 DOOR LWR LINING FWD VIEWER RETAINING BRACKET. TOOL MARKS ON RETAINING BRACKE T REMOVED PER SRM 51-21-01VII R38. BRACKET ORIGINAL THK 0.063", REMOVED 0.023" REMN 0.040" FOUND EXCEEDED LIMIT PER SRM 52-00-01 FIG 1AVIR38. BRACKET FAB FROM MAT'L 6061-T6-0.063" AS PER DULAS DWG: AWE7304. NEW BRACKET INSTALLED PER SRM 51-31-01 VII R38. 2 L 7 3 4F RT A22WE 2007081700013 20070817 00013 NM 2007 8 17 MWEA070165 1 20070805 A 3350 60030451 BATTERY PACK DOUG MD88 MD88 3023688 NM COCKPIT DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 701ME 49760 COCKPIT EMERGENCY LIGHTS DO NOT COME ON WHEN EMERGENCY LIGHT SWITCH MOVED TO ON. REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F RT A6WE 2007081700014 20070817 00014 NM 2007 8 17 MWEA070166 1 20070805 A 5753 5930496510 VANE DOUG MD88 MD88 3023688 NM T/E FLAP CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 701ME 49760 RIGHT OUTBOARD FLAP, INBOARD FIXED VANE IS CHAFED ON THE INBOARD SIDE AT THE FLAP HINGE. INSTALLED FASTENERS. 2 L 7 2 4F RT A6WE 2007081700017 20070817 00017 NM 2007 8 17 UPS07M50387 1 20070706 A 5320 SHEAR WEB DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C CABIN - CORROSION ON UPPER & LWR SURFACE OF SHEAR WEB AT STA 1966 - 1976 L27 LT. UPPER & LWR SURFACE OF SHEAR WEB CORROSION REMOVED MAT'L ORG THK 0.040" REMV 0.018" REMAIN 0.022" FOUND EXCEED LIMIT PER SRM 53-00-01VI FIG 1A R38. CORROSION SHEAR WEB REMV PER SRM 51-31-01VII R38. NEW WEB FAB USING MAT'L 7075-0-0.040" AS PER DOUGLAS DWG: AG A7145-503. NEW FAB WEB INSTALLED AS PER SRM 51-31-01 VII R38. 2 L 7 3 4F RT A22WE 2007081700018 20070817 00018 NM 2007 8 17 ASAA0741928 1 20070803 A 5320 6517684634 INTERCOSTAL BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 INTERCOSTAL CRACKED. REPLACED INTERCOSTAL IAW EA 5310 02729. 2 L 7 2 4F RT A16WE 2007081700020 20070817 00020 NM 2007 8 17 ASAA0741930 1 20070711 A 5320 6517684642 INTERCOSTAL BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 INTERCOSTAL WEB CRACKED. INTERCOSTAL WEB REPLACED IAW ERO 6993 AND EA 5310 02729. REPAIR TO BE INSPECTED PER ASA DWG A 5310023893. 2 L 7 2 4F RT A16WE 2007081700021 20070817 00021 NM 2007 8 17 ASAA0741931 1 20070731 A 5512 657378354 SKIN BOEING 737 7374S3 1384711 NM HORIZ STAB DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 RIGHT HORIZONAL STAB DENTED AT STA 212.3 TO STA 221.5. DENT IS 5" L X 2.2" W X .082 DEEP. RECHECKED DIMS. DENT IS NOW A ZONE 3 DENT. INSP INTERNAL VISUAL INSPECTION OF DAMAGE AREA EVERY 400 FLT HRS OR LESS. IF CRACKS ARE FOUND OR DAMAGE BECOMES BIGGER REPAIR IMMEDIATELY. INSTALL A REPAIR AFTER NO MORE THAN 5000 FLT HRS OR 18 MONTHS WHICHEVER COMES FIRST . 2 L 7 2 4F RT A16WE 2007081700022 20070817 00022 NM 2007 8 17 MASA200700450 1 20070723 A 3350 PIN DHAV DHC8 DHC8202 2809007 NM CABIN PULLED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 446YV 446 ASH 7065 DEN. ALL EMERGENCY LIGHTS INOP. MX FOUND WIRE PULLED OUT OF PIN FROM DIODE, REPINNED. 2 H 7 2 4T RT A13NM 2007081700023 20070817 00023 EA 2007 8 17 MASA200700454 1 20070725 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7305V 7305 ASH RON DSM. MX REPORTED THAT THE LEFT EXTERIOR EMERGENCY LIGHT WAS INOP. MX RELAMPED, OPS CHECK WAS GOOD. 2 L 7 2 4F RT A21EA 2007081700026 20070817 00026 EA 2007 8 17 MASA200700306 1 20070606 A 2560 FITTING CNDAIR CL600 CL6002B19 1900309 EA ESCAPE ROPE MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 593ML 7465 ASH 7379 ORD. EMERGENCY ESCAPE ROPE CLIP MISSING RIGHT SIDE. MX INSTALLED NEW CLIP. 2 L 7 2 4F RT A21EA 2007081700027 20070817 00027 EA 2007 8 17 MASA200700335 1 20070618 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 928LR 15028 ASH 2615 CLT, AFT EMERGENCY FLOOD LIGHT INOP. MAINTENANCE REMOVED AND REPLACED LAMP. 2 L 7 2 4F RT A21EA 2007081700029 20070817 00029 EA 2007 8 17 MASA200700401 1 20070707 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75993 12293 7372 ASH 7153 ORD. PILOT REPORTED THAT THE EMERGENCY LIGHTS WERE LEFT ON AND ALL THE EMERGENCY LIGHTS WERE INOP. MX REPLACE D THE BATTERY PACKS TO THE EMERGENCY LIGHTS. 2 L 7 2 4F RT A21EA 2007081700030 20070817 00030 EA 2007 8 17 MASA200700402 1 20070708 A 3350 1317 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 928LR 15028 ASH 2639 CLE. CABIN CEILING EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2007081700032 20070817 00032 EA 2007 8 17 MASA200700405 1 20070709 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 75994 7367 ASH RON DSM. MX REPORTED THAT THE RIGHT FORWARD OVERWING EXIT LIGHT WAS INOP. MX RELAMPED THE LIGHT. 2 L 7 2 4F RT A21EA 2007081700033 20070817 00033 EA 2007 8 17 MASA200700389 1 20070702 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17337 7337 ASH RON DSM. MX REPORTED THE LT MID EXTERIOR OVERWING EMERGENCY EXIT LIGHT WAS INOP. MX RELAMPED THE LIGHT. 2 L 7 2 4F RT A21EA 2007081700035 20070817 00035 EA 2007 8 17 MASA200700411 1 20070711 A 2520 SHADE CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH 2705 LAX CREW REPORTED THE WINDOW SHADE AT AN EXIT ROW INOP. MX CHANGED THE WINDOW SHADE. 2 L 7 2 4F RT A21EA 2007081700036 20070817 00036 EA 2007 8 17 MASA200700418 1 20070712 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A MASA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 515MJ 10117 FLT 7127 - CAPT REPORTED ONE EACH CEILING LEVEL EMERGENCY FLOOD LIGHT INOPERATIVE PRIOR DEPARTURE. RELAMPED FLOOD LIGH T. 2 L 7 2 4F RT A21EA 2007081700039 20070817 00039 EA 2007 8 17 MASA200700425 1 20070714 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH 2878 PHX. EMERGENCY ESCAPE PATH LIGHTING INOP FROM EMERGENCY EXIT TO LAV. RESECURED LIGHTING. 2 L 7 2 4F RT A21EA 2007081700040 20070817 00040 EA 2007 8 17 MASA2007427 1 20070715 A 3320 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 154SF 7154 ASH 7121 MDT. MID CABIN EMERGENCY CALL LIGHT INOP. MX RELAMPED LIGHT. 2 L 7 2 4F RT A21EA 2007081700041 20070817 00041 EA 2007 8 17 MASA200700428 1 20070715 A 3350 LENS CNDAIR CL600 CL6002C10 1390015 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 503MJ 10058 ASH 7388 ORD. CENTER ORDINANCE AISLE SIGN RED EMERGENCY LENS MISSING. REMOVED AND REPLACED COVER. 2 L 7 2 4F RT A21EA 2007081700045 20070817 00045 EA 2007 8 17 MASA200700438 1 20070718 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27318 7318 ASH 2748 DSM. LEFT AFT EMERGENCY OVERWING EXIT LIGHT INOP. MX RELAMPED THE LIGHT. 2 L 7 2 4F RT A21EA 2007081700046 20070817 00046 NM 2007 8 17 MASA200700440 1 20070718 A 3350 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 449YV 449 ASH 2843 PHX. EMERGENCY LIGHTS WILL NOT TURN OFF. MX RESET SYSTEM. NO FURTHER DEFECTS NOTED. 2 H 7 2 4T RT A13NM 2007081700047 20070817 00047 EA 2007 8 17 MASA200700441 1 20070722 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75991 8638 7422 ASH 7014 ORD. ALL EMERGENCY LIGHTS INOP. MX REPLACED ALL BATTERY PACKS. 2 L 7 2 4F RT A21EA 2007081700048 20070817 00048 EA 2007 8 17 MASA200700442 1 20070721 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17275 12278 7275 ASH 2889 PHX. CABIN MID OVERHEAD, LT AND RT EXTERIOR EMERGENCY LIGHTS. MX REMOVED AND REPLACED THE NR 2 BATTERY PACK A ND CHARGER OPS NORMAL. 2 L 7 2 4F RT A21EA 2007081700051 20070817 00051 EU 2007 8 17 CPCP20070073 1 20070605 A 5240 HINGE AEROSP ATR72 ATR72212 8680945 EU SERVICE DOOR CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 447AM 447 SERVICE DOOR UPPER AND LOWER DOOR SIDE HINGE FITTING CORRODED. CORROSION ON SERVICE DOOR UPPER AND LOWER DOOR SIDE HING E FITTING REMOVED IAW SRM 51-21-42. FOUND WITHIN LIMITS IAW SRM 51-10-10. 2 H 7 2 4T RT A53EU 2007081700052 20070817 00052 EU 2007 8 17 CPCP20070074 1 20070529 A 5313 STRINGER AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 429AT 429 STR 21R , BETWEEN FRAME 39-38 NEXT TO TAIL BUMPER BOX FOUND CORRODED. STRINGER 21R BETWEEN FRAME 38-39 REPAIRED AS PER SRM 53-00-00 FIG 428. 2 H 7 2 4T RT A53EU 2007081700053 20070817 00053 EA 2007 8 17 MASA200700448 1 20070723 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 650ML 7137 ASH 7148 ORD. PILOT REPORTED THAT THE FORWARD HALF OF THE EMERGENCY FLOOR LIGHTING STRIPS WERE INOP. MX REMOVED AND RE PLACED POWER STRIP. 2 L 7 2 4F RT A21EA 2007081700054 20070817 00054 EU 2007 8 17 07FDEA02777 1 20070710 A 5753 SKIN AIRBUS 310 A310222 3930315 EU ZONE 500 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 420FE 339 PREVIOUS REPAIR FOUND LOCATED ON INBD FLAP, RIB 2/4 (UPPER SKIN, TRALING EDGE). REPAIR REQUIRES EVALUATION FOR MAJOR/MI NOR DETERMINATION AND IF WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT CONFORM TO SRM. NEW REPAIR ACCOMPLISHED IAW FEDEX EA 6-5710-112434. 2 L 7 2 4F RT A35EU 2007081700055 20070817 00055 EU 2007 8 17 07FDEA02788 1 20070731 A 5753 SKIN AIRBUS 310 A310222 3930315 EU TE FLAP DEBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 RT WING, INBD FLAP WITH DEBONDING T/E BETWEEN RIB 14 AND RIB 15. IT WAS REPAIRED IN ACCORDANCE WITH SRM 57-52-12. 2 L 7 2 4F RT A35EU 2007081700056 20070817 00056 EU 2007 8 17 07FDEA02789 1 20070710 A 5753 SKIN AIRBUS 310 A310222 3930315 EU ZONE 500 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 PREVIOUS REPAIR LOCATED ON LT OUTBD FLAP, RIB 2/3 (UPPER SKIN). REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATIO N AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REP AIR. NEW REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 57-53-12 FIG 207. 2 L 7 2 4F RT A35EU 2007081700057 20070817 00057 EU 2007 8 17 07FDEA02790 1 20070720 A 5510 A2737120000051 FRAME AIRBUS 310 A310222 3930315 EU ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 ELEVATOR - ARTIFICIAL FELL UNIT LOWER FRAME FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH AMM27-31-26 AND FED EX EA 6-2730-113153. 2 L 7 2 4F RT A35EU 2007081700058 20070817 00058 EU 2007 8 17 07FDEA02791 1 20070807 A 5311 A5377364420600 FRAME AIRBUS 310 A310203 3930313 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 FRAME FITTING C35 IS CRACKED AT LBL 60 IN FWD PIT UNDER T-CAP REMOVED FITTING, FWD LOWER LT AT FR 35 REF A310 SRM 51-40 -21 PARA 6. LOCATED AND DRILLED NEW FITTING REF A310 SRM 51-40-44 PARA 2. INSTALLED NEW FITTING REF A310 SRM 51-40-21 PARA 7. 2 L 7 2 4F RT A35EU 2007081700059 20070817 00059 NM 2007 8 17 07FDEA02792 1 20070808 A 5313 ACA37962 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 DURING INSPECTION ON TRIMMED AREA ON NOSE LANDING GEAR RIGHT SIDE TRUNNION FITTING, 03 EACH CRACKS FOUND ON LONGERON FRO M LOWER FASTENER HOLE COMMON TO THE REPAIR AREA. [08-17-07] REPAIRED AS PER FEDEX EA 1-5310-112374, REPAIR CLASSIFI ED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007081700060 20070817 00060 WP 2007 8 17 07FDEA02794 1 20070808 A 5347 49291501200 SEAT TRACK DOUG MD10 MD1010F 3022112 WP BS 1099-1159 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 GOUGED, CABIN SEAT TRACK SCALLOPS AT STA 1159 TO STA 1099, RBL 27.5 STA 1099-1119, RBL 27.5 REMOVED GOUGE, REMAINING .43 4, FOUND TO BE WITHIN LIMITS IAW DC10/MD10 SRM 53-70-00, FIGURE 5 VOL 1 STA 1119-1159 RBL 27.5. REMOVED GOUGE AND FOUND TO BE OUT OF LIMITS. FABBED NEW SEAT TRACK IAW DC10/MD10 SRM 53-70-00, VOL1, PG 3 P.O: 571947.1. INSTALLED THE NEW SEAT TRACK IAW DC10/MD10 SRM 51-31-01, VOL 2, PAGE 1-5. THIS REPAIR IS CLASSIFIED AS MAJOR. 2 L 7 3 4F RT A22WE 2007081500258 20070815 00258 WP 2007 8 15 AALA20071361 1 20070726 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 435AA 49453 DFW - EMERGENCY LIGHT AT EXTERIOR OFF WING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT EXTERIOR OFF WING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007081500260 20070815 00260 GL 2007 8 15 C2XA07IA180 2 20070802 A 7200 AE3007A1E ENGINE EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL NR 2 SHUTDOWN A C2XA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 SW 27 21154 10888 10888 145772 CAE312306 OKC - FLIGHT 2726, THE CREW REPORTED THAT THE NUMBER TWO ENGINE SHUTDOWN IN FLIGHT. THE AIRCRAFT LANDED IN OKC WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AI RCRAFT WAS APPROVED FOR RETURN TO SERVICE. OPEN 2 L 7 2 4F 4 F RT TE6CH 2007081500281 20070815 00281 2007 8 15 AALA20071377 4 20070731 A 2565 COVER DOUG DC9 DC982 3022082 WP L2 DOOR SLIDE INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7539A 49993 ORD - LEFT NUMBER TWO DOOR SLIDE MANUAL INFLATION HANDLE COVER DOES NOT HOLD. REPLACED LEFT NUMBER TWO DOOR SLIDE ASSEM BLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081500289 20070815 00289 NM 2007 8 15 UPS07M50373 1 20070802 A 2612 80380203 CONTROL UNIT DOUG MD11 MD11F 3023600 NM FIRE DETECTION MALFUNCTIONED A IPXA F ACTIVATE FIRE EXT. G MULTIPLE FAILURE LD LANDING 1 SO 01 278UP 48577 INSPECTION TYPE:N/A ON LANDING ROLL OUT HAD A LEVEL 3 ALERT -APU FIRE- PULLED APU FIRE HANDLE AND DISCHARGED FIRE BOTTLE INTO APU. CONTINUED TO HAVE APU FIRE INTERMITTENT INDICATION. NOTE FIRE DEP WAS CALLED OUT AND A/C TOWED. LEFT ENTRY DOOR USED FOR EMERGENCY EXIT BY CREW. PNEUMATIC STORAGE RESERVOIR DISCHARGE. REPLACED APU FIRE BOTTLE, AND CARTRIDGE AS PER (EO MD11-2620-27353-A PART B). REPLACED APU FIRE DETECTION CONTROL UNIT. PRESSURIZED L1 DOOR PNEUMATIC STORAGE SYSTEM. RECHECKED PRESSURE AFTER 10 MIN FOUND OK. 2 L 7 3 4F RT A22WE 2007081500291 20070815 00291 WP 2007 8 15 AALA20071364 1 20070727 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 454AA 49559 AUS INFLIGHT T1560/27JUL - NOSE LANDING GEAR DID NOT RETRACT WHEN HANDLE WAS SELECTED UP. RETURNED TO AUS AND LANDED WI THOUT INCIDENT. DEFLATED STRUT COMPLETELY AND ACCOMPLISHED FULL OIL AND AIR SERVICE. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F A6WE 2007081500294 20070815 00294 NM 2007 8 15 AALA20071366 1 20070728 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 623AA 24581 SFO - EMERGENCY LIGHT AT OVERHEAD RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERH EAD RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081500305 20070815 00305 WP 2007 8 15 AALA20071345 1 20070723 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 218AA 49168 LGA - EMERGENCY LIGHTS AT FIRST CLASS GALLEY OVERHEAD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS GALLEY OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081500309 20070815 00309 WP 2007 8 15 AALA20071352 1 20070724 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 559AA 53089 LGA - EMERGENCY LIGHTS FROM SEAT ROWS 20 TO AFT OF CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SE AT ROWS 20 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081500337 20070815 00337 NM 2007 8 15 USAA070590 1 20070807 A 5320 TIE CLIP BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 TIE CLIP AT STA 706 STR 10-L CRACKED. REMOVED & REPLACED TIE CLIP PER SRM 51-10-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007081500347 20070815 00347 NM 2007 8 15 SB07058 1 20070802 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 453UW 24980 FLL - MAINTENANCE REPORTED THE AFT LEFT AND AFT RIGHT EMERGENCY LIGHT BATTERY PACKS WILL NOT HOLD A CHARGE. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT AND AFT RIGHT EMERGENCY LIGHT BATTERY PACKS. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007081500348 20070815 00348 NM 2007 8 15 USAA070598 1 20070807 A 5320 ATTACH ANGLE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 STA 706 RBL 24 CRACKED. INSTALLED FABRICATED REPAIR PART PER SRM 51-40-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007081500352 20070815 00352 EU 2007 8 15 WRNA200700048 1 20070802 A 3350 AD3128 BATTERY PACK AIRBUS 300 A300B4203 3930306 EU CABIN DISCHARGED A WRNA K NONE L NO TEST IN INSP/MAINT 1 SO 05 504TA 216 DURING DAILY CHECK, EMERGENCY LIGHTS FOR L1 AND R1 DOOR DID NOT COME WHEN TESTED. REPLACED EMERGENCY EXIT LIGHT BATTERY PACKS IAW 33-51-14 PG 301, OPS CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A35EU 2007081500358 20070815 00358 NM 2007 8 15 USAA070613 1 20070807 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 STA 500A, FRAME, I/B FASTENER FOR A/C SUPPORT BRACKET, STR 8+9R ELONGATED HOLE. INSTALLED 2ND OVERSIZED HI-LOK PER SRM 51-40-00, DEFECT SIZE: .250 INCH. 2 L 7 2 4F RT A16WE 2007081500363 20070815 00363 NM 2007 8 15 USAA070604 1 20070807 A 5414 SKIN BOEING 737 737401 1384701 NM NR 1 PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 PYLON NR 1 ENGINE UNER PANEL 5727 HAS CRACK. STOP DRILLED & INSTALLED DOUBLER PER TR 54-30-07, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007081500370 20070815 00370 NM 2007 8 15 USAA070610 1 20070807 A 5240 6545871132 STOP FITTING BOEING 737 737401 1384701 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 CUTOUTS OF THE 3RD & 4TH STOPS DOWN FROM THE TOP, AFT SIDE OF FWD SERVICE DOOR CRACKED. INSTALLED REPAIR DOUBLERS PER T R 52-10-11, DEFECT SIZE: .025 INCH. 2 L 7 2 4F RT A16WE 2007081500372 20070815 00372 NM 2007 8 15 USAA070612 1 20070807 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 STR S-22R, AFT OF STA 727F HAS CRACK. INSTALLED REPAIR DOUBLER PER SRM 53-00-01, DEFECT SIZE: 3 INCHES. 2 L 7 2 4F RT A16WE 2007081500379 20070815 00379 NM 2007 8 15 USAA920070795 1 20070803 A 5210 143N808720 INTERCOSTAL BOEING 757 757225 1384959 NM R2 DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 923UW 22203 PIT - MAJOR REPAIR - C4 CHECK, R2 DOOR INTERCOSTAL CRACKED. REPLACED R2 DOOR INTERCOSTAL IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007081500381 20070815 00381 NM 2007 8 15 USAA920070797 1 20070728 A 5320 18270030011 FLOOR SUPPORT BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 923UW 22203 PIT - MAJOR REPAIR - C4 CHECK, CORROSION ON FLOOR SUPPORT CHANNEL, BS 1661 - BS 1681. REPLACED FLOOR SUPPORT CHANNEL, B S 1661 - BS 1681 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007081600029 20070816 00029 NM 2007 8 16 AWXA200700954 1 20070804 A 5752 654645522C TAB BOEING 737 7373G7 1384595 NM AILERON DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 305AW 14125 14125 24012 PHX - MAJOR REPAIR - NR 4109975, RIGHT WING AILERON TRIM TAB TRAILING EDGE IS DELAMINATED, WS 431.5. REPLACED RIGHT WIN G AILERON TRIM TAB TRAILING EDGE, WS 417 - WS 480 IAW AWA TASK CARD R3M27014. 2 L 7 2 4F RT A16WE 2007081600034 20070816 00034 NM 2007 8 16 AWXA200700960 1 20070705 A 5313 6545767120 STRINGER BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961285, CRACKED STRINGER, BS 500C, S16L. REPAIRED STRINGER, BS 500C, S16L IAW USA IRWAYS EA 120126. 2 L 7 2 4F RT A16WE 2007081600043 20070816 00043 NM 2007 8 16 07FDEA02766 1 20070804 A 5730 ARB74022 SKIN DOUG MD11 MD11F 3023600 NM WS 683-713 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 CRACK INDICATIONS REVEALED IN 09 EA FASTENER HOLES TOWARDS EDGE OF ACCESS. C/OUT IN RT WING LWR SKIN ACCESS DOOR C/OUT (BETWEEN STA XORS= 683.400 TO XORS= 713.600). [08-17-07] REPAIRED AS PER FEDEX EA 1-5710-112376, REPAIR CLASSIFIED A S MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007081600045 20070816 00045 EU 2007 8 16 07FDEA02768 1 20070804 A 2760 30829100 VALVE AIRBUS 300 A300B4605R 3930308 EU SPOILERS INOPERATIVE A FDEA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 731FD 28 28 709 DURING CRUISE FLT, LT WING SPOILER NR 4 DEPLOYED INFLT. A/C ROLLED HARD LT. DISC A/P AND COUNTERED RT. SPOILERS ON BO TH WINGS DEPLOYED FOR REMAINDER OF FLT. SPOILER NR 4 PREV MEL. ON DEBRIEFING CREW, RT WING SPOILERS DEPLOYED FOR CTRL . CORRECTION ONLY. RDU - MX FOUND FAULT CODES EFCU1 M-2 3 AND 6. SWAPPED EFCU FAULT CODED EFCU POSITION 1 M-2 4 AND 7. EFCU'S RETURNED TO ORIG POS. DO THE FOLLOWING. INSPECT 4L SPOILER SURFACE AND HINGES FOR DAMAGE. CHECK WIRING FROM THE EFCU' TO THE 4L ACTUATOR AND VALVE GROUP. REPLACE 4L SPOILER VALVE GROUP. REMOVED AND REPLACED 4L SPOILER GR OUP VALVE PER MM 27-64-12-4. OPS CHECKS LEAK CHECKS GOOD. 2 L 7 2 4F RT A35EU 2007081600053 20070816 00053 EU 2007 8 16 07FDEA02776 1 20070712 A 5340 A5378193720100 ADAPTER AIRBUS 310 A310222 3930315 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 MDCC - CLS ADAPTER AT FR38 BETWEEN Y-450 AND Y-950 FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10 . 2 L 7 2 4F RT A35EU 2007081600073 20070816 00073 WP 2007 8 16 07FDEA02780 1 20070806 A 5313 STRINGER DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 CENTER WHEEL AREA L48L END FITTING CORRODED IN AREAS STA1509 TO 1521. [08-21-07] ALL WORK ACCOMPLISHED ON SDR 07-3006 -W/O 37284. 2 L 7 3 4F RT A22WE 2007081600075 20070816 00075 NM 2007 8 16 07FDEA02782 1 20070807 A 5753 65192508 FLAP TRACK BOEING 727 727233 138408A NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 ON NON-ROUTINE, RIGHT OUTBD FLAP INBD FLAP TRACK HAS CORROSION AT THE OUTBD AND CENTER MOUNT HOLES AT MOUNT PAD. ON N ON- ROUTINE, OUTBD FLAP INBD FLAP TRACK MOUNT BOLTS ARE WORN AND GOUGED. ON NON-ROUTINE, FLAP TRACK HAS WEAR ON TOP OF FLAP TRACK ON OUTBD SIDE 13" FROM AFT END. ON NON-ROUTINE, FLAP HAS RUST IN HORIZONTAL HOLES AT THE TRACK MOUNT PAD . REPLACED NR 7 FLAP TRACK, NEW FLAP TRACK IS INSTALLED ON W/C 27X5709-03. REPLACING WITH NEW FLAP TRACK ADDRESSES NON -ROUTINE N00430, N00432, N00433, N00434, THIS IS CLASSIFIED AS A MINOR. 2 L 7 3 4F RT A3WE 2007081600083 20070816 00083 NM 2007 8 16 QXEA200701240 1 20070807 A 2133 10306814 OUTFLOW VALVE DHAV DHC8 DHC8202 2809007 NM CABIN PRESSURE MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 357PH 21717 504 PDX FLIGHT NR 2190 AT 15,000' ON DESCENT HAD A RAPID DEPRESSURIZATION OF CABIN. ALL EMERGENCY PROCEDURES WERE FOLLOWED. UTILIZED OXYGEN. SUSPECT FORWARD OUTFLOW VALVE FAILURE AS NOISE CAME FROM COCKPIT LOWER SIDE. REPLACED BROKEN NUTPLA TES WITH SOLID RIVETS ON FORWARD AND AFT PANELS ON LEFT SIDE OF AIRCRAFT. REPLACED SAFETY OUTFLOW VALVE. OPERATIONAL T EST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007081600105 20070816 00105 NM 2007 8 16 AALA20071390 1 20070802 A 2613 285T03855 MODULE BOEING 767 767323 1385205 NM WARNING BELL INOPERATIVE A AALA O OTHER N FALSE WARNING CR CRUISE 1 SW 21 360AA 24041 CDG INFLIGHT T120/02AUG - FIRE BELL AURAL WARNING SOUNDED AND WOULD NOT RESET. ALL OTHER INDICATIONS NORMAL. REPLACED AURAL WARNING BELL MODULE. SYSTEM GROUND CHECKED NORMAL OPERATIONS. 2 L 7 2 4F RT A1NM 2007081600108 20070816 00108 NM 2007 8 16 AALA20071416 1 20070806 A 3350 6011779 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9420D 49824 DFW - EMERGENCY LIGHTS AT FORWARD EXIT IDENTIFIERS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD E XIT IDENTIFIERS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2007081600120 20070816 00120 NM 2007 8 16 AALA20071406 1 20070804 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 612AA 24488 SEA - EMERGENCY LIGHT AT SEAT 9D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT A2NM 2007081600123 20070816 00123 WP 2007 8 16 AALA20071409 1 20070803 A 2560 BATTERY DOUG DC9 DC982 3022082 WP FLASHLIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 470AA 49600 ORD - EMERGENCY FLASHLIGHT AT FIRST CLASS INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT FIRST CLASS. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081600130 20070816 00130 NM 2007 8 16 AWXA200700969 1 20070705 A 5340 69353521 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961319, CRACKED STRINGER CLIP, BS 727A, S25L. REPLACED STRINGER, BS 727A, S25L IA W B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007081600140 20070816 00140 NM 2007 8 16 DL757071002 1 20070803 A 5410 112N701123 BUSHING BOEING 757 757232 1384965 NM NR 2 PYLON MIGRATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 635DL 23762 THE DIAGONAL BRACE WING END FITTINGS OF BOTH THE NR 1 AND NR 2 PYLONS WERE FOUND WITH MIGRATED BUSHINGS DURING ACCOMPLI SHMENT OF 6-75079-3. NEW BUSHINGS WERE INSTALLED AS AN AMOC TO AD 2003-18-05. 2 L 7 2 4F RT A2NM 2007081600141 20070816 00141 NM 2007 8 16 DL757071003 1 20070803 A 5415 012N88879 ATTACH FITTING BOEING 757 757232 1384965 NM NR 2 PYLON MISALIGNED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 635DL 23762 NUMBER 2 PYLON SIDE LINK ATTACH FITTING HOLE NR 3 WAS FOUND MISALIGNED WHILE ACCOMPLISHING DELTAS EO 6-70332-3 COVERING SB 757-54-0034. A TAPERED RADIUS FILLER WAS INSTALLED PER ANAMOC TO AD 2003-18-05. 2 L 7 2 4F RT A2NM 2007081600144 20070816 00144 NM 2007 8 16 DL76L071006 1 20070803 A 2750 SHUTOFF VALVE BOEING 767 767332 1382001 NM TE FLAPS MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 185DN 20832 27961 ON DEPT WHEN RAISING FLAPS FROM 5 TO 1 TE FLAP DISAGREE LIGHT ILLUMINATED FLAPS RAISED OK WITH ALT SYSTEM. DIVERTING TO JFK FOR REPAIRS, T/S PER FIM. FSEU AND FSPM SHOW NO FAULTS. TE PDU NOT BYPASSED. CHECKED ALL FLAP ROTARY ACTUATOR TO RQUE LIMIT INDICATORS. NONE TRIPPED. REMOVED AND REPLACED FLAP/SLAT SOV PER AMM ALSO R/RFSEU PER AMM. RAN FLAPS NUMER OUS TIMES. NO MSGS. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007081600148 20070816 00148 NM 2007 8 16 DLM90071011 1 20070802 A 5510 HINGE DOUG MD90 MD9030 3023690 NM HORIZONTAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 LT O/B HINGE PLATE HAS CORROSION ON I/B AND O/B SURFACE AND LIGHT FRETTING IN BORES. REPAIRED IAW MD-90 SRM 55-30-05 PA RA 5. 2 L 7 2 4F RT A6WE 2007081600162 20070816 00162 NM 2007 8 16 DL76L071032 1 20070806 A 2120 UNKNOWN BOEING 767 767332 1382001 NM GALLEY ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 198DN 28455 PRIOR TO DEPT CREW REPORTED ELECTRICAL ODOR FROM AFT MID GALLEY INSPECTED WIRING TO MID AFT GALLEY, NO DAMAGE FOUND. NO ELECT ODOR NOTED. MCO AND PLACARD REMOVED. 2 L 7 2 4F RT A1NM 2007081600172 20070816 00172 EU 2007 8 16 CPCP20070065 1 20070606 A 5320 FLOOR SUPPORT AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 447AM 447 RT "Z" FLOOR BETWEEN FRAME 39-41 CORRODED. RIGHT "Z" FLOOR BETWEEN FRAME 39-41, REPLACED IAW SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007081600173 20070816 00173 EU 2007 8 16 CPCP22070066 1 20070606 A 5320 INTERCOSTAL AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 447AM 447 RT INTERCOSTAL BETWEEN FRAME 38-39 CORRODED. NOW RT INTERCOSTAL BETWEEN FRAME 38-39 INSTALLED IAW SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007081600174 20070816 00174 NM 2007 8 16 QXEA200701241 1 20070806 A 5210 SEAL BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR CONTAMINATED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 406QX 4048 BOI FLIGHT NR 2303: FA REPORTS DIFFICULTY IN OPERATING AFT PASSENGER DOOR. MAINTENANCE INSPECTED THE DOOR AND FOUND SEA L TO BE DIRTY. CLEANED SEAL OF DEBRIS. CYCLED AFT PAX DOOR SEVERAL TIMES. NO DEFECTS NOTED. NO PARTS REPLACED. AIRC RAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007081600175 20070816 00175 EU 2007 8 16 CPCP20070067 1 20070606 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 447AM 447 FLOORBEAM 36 CORRODED. FLOORBEAM 36 REPAIRED IAW SRM 53-00-00 FIG 435. 2 H 7 2 4T RT A53EU 2007081600177 20070816 00177 EU 2007 8 16 SIMA200722001 1 20070804 A 2750 UNKNOWN SAAB SF340 340B 7860101 EU TE FLAPS UNKNOWN A SIMA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 21 340RC 340B340 RECEIVED MASTER CAUTION FLAPS FAIL LIGHT, FLAPS WOULD NOT EXTEND - VIBRATION FELT RIGHT SIDE OF AIRCRAFT. RETURNED TO L AX. PERFORMED OPERATIONAL AND FUNCTIONAL SYSTEM CHECKS IAW SAAB AMM 27-51-00 WITH NO DEFECTS NOTED. PERFORMED ENGINE A DJUSTMENT IAW SAAB AMM 71-00-00 AND GE MM 72-00-00. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007081700005 20070817 00005 NM 2007 8 17 UPS07650392 1 20070803 A 2432 BATTERY BOEING 767 76734AF 1385212 NM APU DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 307UP 27760 INSPECTION TYPE:ETOP APU INOP. FOUND APU BATTERY SHOWS 1 VOLT. REMOVED AND REPLACED APU BATTERY PER MM 24-31-04. RAN APU WITH NO FAULTS. 2 L 7 2 4F RT A1NM 2007081700007 20070817 00007 NM 2007 8 17 UPS07M50376 1 20070529 A 5320 CHANNEL DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C AFT CARGO STA 1960, LONGERON R43 LONGERON CHANNEL STIFFENER FOUND WITH CORROSION AS MARKED. NEW CHANN EL FAB AS PER DOC DWG NGA6313 MATL USED:7075-0-0.071. CHANNEL HEAT TREATED PER DPS7.00-1 & HARDNESS VALUES 86.9 PER DPS 1.05-3. NEW CHANNEL FASTENER HOLES PICKED UP PER SRM 51-31-01 V2 R38. NEW CHANNEL REPROTECTED & PAINT TOUCHED UP PER SRM 51-21-01 V1 R38. NEW CHANNEL INSTALLED PER SRM 51-31-01 V2 R38. 2 L 7 3 4F RT A22WE 2007081700025 20070817 00025 EA 2007 8 17 MASA200700456 1 20070726 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 508MJ 10087 ASH 7290 ORD, CAPTAIN REPORTED EMERGENCY LIGHT IN GALLEY TO BE INOP. MX RELAMPED LIGHT, ACFT CONTINUED OPERATIONS. 2 L 7 2 4F RT A21EA 2007081700028 20070817 00028 EA 2007 8 17 MASA200700403 1 20070706 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 651BR 7426 ASH 1006 HNL. CABIN DOOR FLOOR EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED THE LIGHT SEGMENT AT ROW 6, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007081700031 20070817 00031 NM 2007 8 17 ARWA20070801 1 20070803 A 5280 NNB6086511 DOOR DOUG DC10 DC1040F 3023507 NM MLG DAMAGED A ARWA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 140WE 46920 AFTER GEAR RETRACTION RED LEFT LGD GEAR LIGHT ON FWD AND F/E PANELS REMAINED ON. PERFORMED THE APPROPRIATE CHECK-LIST A ND RETURN TO LANDING AFTER DUMPING FUEL TO MAX LANDING WEIGHT. REMOVED AND REPLACED MAIN LANDING GEAR DOOR IN ACCORDANC E WITH M/M 32-14-01; ACCOMPLISHED ADJ AND TEST IN ACCORDANCE WITH M/M 32-30-00, ALL OPERATIONAL CHECKS NORMAL. 2 L 7 3 4F RT A22WE 2007081700061 20070817 00061 WP 2007 8 17 07FDEA02795 1 20070808 A 5347 54929405 SEAT TRACK DOUG MD10 MD1010F 3022112 WP BS 1019-1039 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 ELONGATED SCALLOPS ON CABIN SEAT TRACK AT RBL 47.5, STA 1019 TO 1039 CHECKED LIMITS, SEAT TRACK HAS SEVERAL BROKEN SCALL OPS OUT OF LIMITS IAW DC/MD10 SRM 53-70-00 VOL 1 PG 21. REMOVED OLD TRACK AND INSTALLED NEW TRACK IAW MD-DC10 SRM 53- 42-01 VOL 3 PG 13/14 AND 53-70-00 VOL 1 PG 3 AND 4. ALODINED AND PRIMED TRACK IAW DC/MD-10 SRM 51-21-01 VOL 2 PG 1 AND 4. 2 L 7 3 4F RT A22WE 2007081700063 20070817 00063 WP 2007 8 17 07FDEA02797 1 20070808 A 5347 S4929405 SEAT TRACK DOUG MD10 MD1010F 3022112 WP BS 939-1019 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 ELONGATED SCALLOPS AT CABIN SEAT TRACK LBL 47.5, STA 939 TO 1019 (2-PLACES) REMOVED SEAT TRACK AT STA 879-1019 IAW DC10- SRM 53-70-00 VOL 1 PG5. SEAT TRACK WAS OUT OF LIMITS IAW DC10 SRM 53-20-00 PG 21. REPLACED SEAT TRACK IAW DC10 SRM 53- 70-00 VOL 1 PG 1-10, AT STA 879-1019 LBL 47.5. REPAIR CLASSIFIED AS MAJOR. 2 L 7 3 4F RT A22WE 2007081700064 20070817 00064 NM 2007 8 17 07FDEA02798 1 20070808 A 5347 BAC1520792 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 MAIN DECK SEAT TRACK CORRODED STA 1030-1070, RBL 24 ON CROWN AND FLANGE, WL208. REMOVED CORROSION AT SEAT TRACK STA 103 0 TO 1070, RBL 24, IAW 51-10-6, FOUND TO BE OUT OF LIMITS ON STA 1030, ORIGINAL THICKNESS ON FLANGE OF .070" MATERIAL L OSS .030". REMAINING .040, IAW SRM 53-10-1 FIG 16. REMOVED SEAT TRACK SECTION FROM STA 1030 -1050, RBL 24, IAW SRM 51 -30-2. FABRICATED NEW SEAT TRACK SECTION, TREATED, PRIMED, AND INSTALLED IAW B272 SRM 53-10-5 FIG 7, 51-10-2, 51-30-2 T HIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007081700065 20070817 00065 NM 2007 8 17 07FDEA02799 1 20070808 A 5340 65453135 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 PASSENGER CABIN STA 950E STR 7R, STRINGER CLIP CRACKED REPLACED CRACKED STRINGER CLIP W/NEW, REF SRM 51-30-2, THIS IS CL ASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007081700066 20070817 00066 NM 2007 8 17 07FDEA02800 1 20070808 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 STINGER CLIP CRACKED AT STA 800 AND STR 7L REMOVED AND REPLACED STRINGER CLIP AT FS 800 STR 7L, IAW B727 SRM 51-30-2, TH IS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007081700067 20070817 00067 NM 2007 8 17 07FDEA02801 1 20070808 A 5340 654531313 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 STRINGER CLIP CRACKED AT ATR 9L AND 950 C REMOVED AND REPLACED STRINGER CLIP, STR 9L, STA 950C REF SRM 51-30-2 PG 2 8, T HIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007081700068 20070817 00068 EA 2007 8 17 SWIA200718556 1 20070805 A 3230 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 924SW 7681 NOSE GEAR FAILED TO EXTEND. ON THIRD TRY, NOSE GEAR EXTENDED NORMALLY, FLIGHT NR 5903. REPLACED SELECTOR VALVE AND PRI ORITY VALVE IAW CRJ 200 MM 32-33-15, P/N: 750006000 S/N OFF: 2019. 2 L 7 2 4F RT A21EA 2007081700071 20070817 00071 EA 2007 8 17 SWIA200718559 1 20070717 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 800SK 15060 TWO EMERGENCY CEILING LIGHTS ARE OUT, FLIGHT NR 2012. RE-LAMPED EMERGENCY CEILING LIGHTS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007081700073 20070817 00073 EA 2007 8 17 SWIA200718561 1 20070804 A 3350 COVER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS MISSING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 765SK 10231 LOWER RIGHT EXIT LIGHT COVER IS MISSING, FLIGHT NR 6427. INSTALLED SERVICEABLE LENS. 2 L 7 2 4F RT A21EA 2007081700074 20070817 00074 EA 2007 8 17 SWIA200718562 1 20070803 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS LOOSE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 442SW 7609 SEVERAL CABIN EMERGENCY LIGHTS ARE NOT ILLUMINATING, FLIGHT NR 3999. RESECURED CONNECTOR PLUG. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007081700076 20070817 00076 EA 2007 8 17 SWIA200718564 1 20070802 A 2913 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 912SW 7595 IN FLIGHT, HYDRAULIC SYSTEM NR 2 QUANTITY WENT TO ZERO. SYSTEM MAINTAINED 3000 PSI, FLIGHT NR 5873. REPLACED NR 2 ENGI NE DRIVEN HYDRAULIC PUMP IAW CRJ 200 AMM 29-11-01. OPS AND LEAKS CHECKS GOOD, P/N 887055, S/N OFF MX659434. 2 L 7 2 4F RT A21EA 2007081700077 20070817 00077 EA 2007 8 17 SWIA200718565 1 20070729 A 3520 OXYGEN MASK CNDAIR CL600 CL6002C10 1390015 EA LAVATORY UNLATCHED A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 604SK 10249 FORWARD LAV OXYGEN MASKS FELL DURING FLIGHT, FLIGHT NR 4012. RESTOWED FORWARD LAVATORY OXYGEN MASKS. 2 L 7 2 4F RT A21EA 2007081700079 20070817 00079 NM 2007 8 17 KCSA071282 1 20070807 A 5330 SKIN BOEING 747 7472B4B 138481B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 EXTERNAL FUSELAGE SKIN IS DAMAGED AT STA 750, BETWEEN STR 46R TO 47R. 2 L 7 4 4F RT A20WE 2007081700080 20070817 00080 EA 2007 8 17 MASA20070037 1 20070619 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75984 7489 ASH 7244 DSM. LEFT NR 3 EMERGENCY EXTERIOR LIGHT INOP. MX RELAMPED THE LIGHT. 2 L 7 2 4F RT A21EA 2007081700082 20070817 00082 EA 2007 8 17 MASA200700341 1 20070619 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75993 7372 ASH 7409 IAD. MID AND AFT CABIN EMERGENCY CEILING LIGHTS INOP. MAINTENANCE REPLACED THE LAMPS AND IT OP CHECKED GOOD. 2 L 7 2 4F RT A21EA 2007081700083 20070817 00083 EA 2007 8 17 MASA200700344 1 20070620 A 2560 FIRST AID KIT CNDAIR CL600 CL6002B19 1900309 EA CABIN OPEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 693BR 7761 ASH 1030 HNL-KOA. FIRST AID KIT WAS OPENED. MX REPLACED THE FIRST AID KIT. 2 L 7 2 4F RT A21EA 2007081700084 20070817 00084 EA 2007 8 17 MASA200700352 1 20070622 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 522LR 10262 ASH 7388 ORD. EMERGENCY LIGHT WILL NOT STAY ON. MAINTENANCE RESTARTED, OP'S CHECKED THE SYSTEM OK. 2 L 7 2 4F RT A21EA 2007081700085 20070817 00085 EA 2007 8 17 MASA200700350 1 20070622 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 593ML 7465 ASH 7304 IAD. PILOT REPORTED THE RIGHT MID EMERGENCY EXIT LIGHT WAS INOP. MX RELAMPED THE LIGHT. 2 L 7 2 4F RT A21EA 2007081700086 20070817 00086 EA 2007 8 17 MASA200700353 1 20070622 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37178 7178 ASH 2903 PHX. AFT EMERGENCY CEILING FLOOD LIGHT INOP. RELAMPED FLOOD LIGHT. 2 L 7 2 4F RT A21EA 2007081700088 20070817 00088 EA 2007 8 17 MASA200700348 1 20070623 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37228 7228 ASH 2872 PHX. PILOT REPORTED THE ROW 8 LOWER LEFT EXIT SIGN WAS INOP. MX REPLACED THE FORWARD EMERGENCY FLOOR STRIP. 2 L 7 2 4F RT A21EA 2007081700091 20070817 00091 2007 8 17 YENA2007070 4 20070731 A 2397 POWER CABLE AIRBUS 320 A320232 3930326 EU CABIN FAULTY A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 590JB 28 2231 FLT 728, APPROX 8 AM, BQN TO JFK - ELECTRICAL/SMOKE ODOR AT ROW 24/25. SMELL CEASED WHEN TV'S WERE SHUT OFF. PERFORMED TSM 23-39-00-810-801 PROCEDURE. FOUND VDU CABLE ON SEB AT 23DEF WHICH POWERS THE VDU'S ON ROW 24DEF TO BE AT FAULT. C ONNECTOR CONTAINS LIQUID RESIDUE AND REQUIRES MAINTENANCE. REMOVED AND REPLACED VDU CABLE AT 23DEF AND SEB AT 23E AS PR ECAUTIONARY MEASURE. PERFORMED ELECTRICAL ODOR SYSTEM INTEGRITY CHECK IAW 23-39-00 PG 5043-5045. SYSTEM OPS OK IAW 23- 39-00. 2 L 7 2 4F RT A28NM 2007081700092 20070817 00092 EA 2007 8 17 SWIA200718566 1 20070801 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 613SK 10038 OVERHEAD CABIN EMERGENCY LIGHT IS INOP, FLIGHT NR 4012. RELAMPED EMERGENCY LIGHT. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007081700097 20070817 00097 NM 2007 8 17 2007UALA02974 1 20070802 A 3297 WIRE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RT MLG SHORTED A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 305UA 23666 RIGHT MAIN GEAR INDICATION FAULT. FOUND SHORTED WIRING IN THE INDICATION SYSTEM. FOUND UPPER LOCK SENSOR RED WIRE SHO RTED- REPLACED BOTH UP LOCK AND DOWN LOCK INDICATION SENSORS. SWUNG GEAR- ALL INDICATIONS NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700100 20070817 00100 NM 2007 8 17 2007UALA02977 1 20070803 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY LIGHT INOP 43 ABC. REPLACED EEL LIGHT ASSEMBLY. OP CHECKS READY FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007081700102 20070817 00102 NM 2007 8 17 2007UALA02279 1 20070628 A 2613 360154 OVERHEAT LOOP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 581UA 26701 RIGHT ENG OVERHEAT LOOP 2 STATUS MSG. ONE OF THE OVERHEAT LOOP AT FAN BROKEN IN HALF. REPLACED LOOP AND SYSTEM TESTED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081700104 20070817 00104 NM 2007 8 17 2007UALA02226 1 20070625 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 586UA 26710 SLIDE LIGHT AT 4L BURNT OUT. OPERATED ARM AND DISARM HANDLE AT DOOR 3L. SLIDE LIGHT CAME ON WHEN ARMED AND WENT OFF WH EN DISARMED. COULD NOT DUPLICATE PROBLEM. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081700105 20070817 00105 NM 2007 8 17 2007UALA02278 1 20070627 A 7830 MR78380 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE THRUST REVERSER DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 55146 55146 24931 NR 2 ENG REVERSER MAKING HEAVY POPPING AND CRACKLING SOUNDS. AFTER INVESTIGATION FOUND UPPER SIDEWALL (UPPER BI-FURCATI ON PANEL) OF REVERSER 90 PERCENT DELAMINATION ON INNER SKIN. DELAMINATION WAS CAUSED BY THE FAILURE OF BOND LINE BETWEE N OUTER SKIN AND HONECOMB SECTION. BOND LINE FAILURE IS DUE TO HIGH HEAT IN THIS AREA IN COMBINATION WITH UPPER REVERSE R COMPRESSION RODS HAVING A GAP LARGER THAN 0.050 IN. THIS ALLOWS FLEXING OF PANEL BY THE PRESSURE IN C-DUCT DURING THR UST. COULD BE REQUIRING PERIODIC REVERSER FIT CHECKS, WHICH ENGINEERING IS CONSIDERING ADDING TO MAINT PROG AT HMV. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081700106 20070817 00106 NM 2007 8 17 AWXA200700972 1 20070703 A 5542 SKIN BOEING 737 7373G7 1384595 NM RUDDER CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5981803, RUDDER LEADING EDGE SKIN CRACKED, LEFT SIDE, RUDDER STATION 4.5. REPAIRED RUDDER LEADING EDGE SKIN, LEFT SIDE, RUDDER STATION 4.5. IAW USAIRWAYS 120134. 2 L 7 2 4F RT A16WE 2007081700109 20070817 00109 NM 2007 8 17 2007UALA02445 1 20070705 A 2560 81020401 PROXIMITY SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BIRT BAR OBSTRUCTED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 DOOR 2R GIRT BAR ENGAGEMENT LIGHT WILL NOT COME ON WHEN ARMING DOOR. *S/D* REMOVED DEBRIS FROM PROX SENSOR AREA. REPL ACED FWD GIRT BAR PROX SENSOR & ADJUSTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081700110 20070817 00110 NM 2007 8 17 2007UALA02906 1 20070729 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 566UA 26670 EMERGENCY LIGHT STRIP AT ROW 13-14 ON FLOOR NOT ATTACHED. RESECURED EMERGENCY EQUIPMENT LIGHT COVER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081700113 20070817 00113 NM 2007 8 17 2007UALA02909 1 20070727 A 3510 OXYGEN MASK BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT LEAKING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 776UA 26937 OXYGEN MASK PROBLEM CREW COMMENTS: F/O MASK HARNESS LEAKS WHEN HARNESS INFLATED. REPLACED FIRST OFFICER'S O2 MASK PER MM. SUSPECT LEAK DUE TO INFLATION CYCLING OF HARNESS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007081700114 20070817 00114 NM 2007 8 17 AWXA200700973 1 20070708 A 5311 6520722 FRAME BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5962327, CRACKED FORWARD CARGO COMPARTENT DOOR CUT OUT FORWARD FRAME, BS 440, S24R, WL 160. REPAIRED FORWARD CARGO COMPARTENT DOOR CUT OUT FORWARD FRAME, BS 440, S24R, WL 160 I/A/W USAIRWAYS EA 120139. 2 L 7 2 4F RT A16WE 2007081700116 20070817 00116 2007 8 17 2007UALA02993 4 20070805 A 2564 COVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 412UA 465 SLIDE RAFT COVER FELL OFF AT 2R. 09-07-07 SECURED SLIDE COVER. 2 L 7 2 4F 4 F RT A28NM E40NE 2007081700118 20070817 00118 EU 2007 8 17 CPCP20070059 1 20070606 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 447AM 447 CORROSION FOUND ON RT I/B SEAT TRACK BETWEEN FRAME 34-36. RT INBD SEAT TRACK BETWEEN 34-36 REPAIR SPLICING AS PER SRM 5 3-00-00 FIGURE 434 (SHEET1). 2 H 7 2 4T RT A53EU 2007081700119 20070817 00119 NM 2007 8 17 2007UALA02994 1 20070803 A 5350 RADOME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NOSE CONTAMINATED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 523UA 24932 FLIGHT DIVERTED DUE TO INOPERABLE WEATHER RADAR. UNRELIABLE WEATHER RADAR CELLS. RADOME FAILED MOISTURE TEST, REPLA CED RADOME WEATHER RADAR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081700120 20070817 00120 EU 2007 8 17 CPCP20070075 1 20070529 A 5320 THRESHOLD AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 429AT 429 RT THRESHOLD BETWEEN FRAME 36-39 BRACKET ON FRAME 37 CORRODED. RT THRESHOLD BETWEEN FRAME 36-39 BRACKET ON FRAME 37 FAB RICATED (W/C 172780) AND INSTALLED IAW SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007081700121 20070817 00121 EU 2007 8 17 CPCP20070077 1 20070529 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 429AT 429 FOUND FLOORBEAM 39 CORRODED. FLOORBEAM 39 REPAIRED AS PER SRM 53-00-00 FIG 435. 2 H 7 2 4T RT A53EU 2007081700122 20070817 00122 NM 2007 8 17 2007UALA02995 1 20070803 A 2697 WIRE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FIRE LIGHT SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 922UA 26642 CAPTAIN'S FIRE LIGHT INOP. FOUND ELECTRICAL SHORT WITHIN THE MASTER WARNING CAPT FIRE ASSY. REPLACED THE MASTER WARNIN G CAPT FIRE ASSY L340. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700123 20070817 00123 EU 2007 8 17 CPCP20070078 1 20070529 A 5320 ANGLE AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 429AT 429 RT CHORD ANGLE BTWEEN FRAME 13-17 CORRODED. RT CHORD ANGLE REPAIRED AS PER SRM 53-31-50. 2 H 7 2 4T RT A53EU 2007081700126 20070817 00126 NM 2007 8 17 2007UALA02996 1 20070804 A 5310 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE VIBRATION A UALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 29 580UA 26698 FLIGHT DIVERTED DUE TO VIBRATION IN THE AFT GALLEY FLOOR. CREW REPORTS NO WATER PRESS IN ALL GALLEY AND LAVS. ALSO REPORT VIBRATION IN AFT GALLEY FLOOR AREA , CHECKED EXTERIOR SERVICE PANEL DOOR FOR SECURITY AND VERIFIED THAT SERVICE H ANDLE WAS FULLY CLOSED AND NO AIR WAS DUMPING OVERBOARD. FOUND WATER FILL VALVE HANDLE IN THE OPEN POSITION WITH DOOR C LOSED. RE-SERVICED PER UA ENGINEERING SPECIFICATIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081700130 20070817 00130 NM 2007 8 17 2007UALA02998 1 20070803 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 EXTERNAL FUSELAGE FWD CARGO DOOR CUTOUT FRAME. FWD CARGO DOOR CUTOUT AFT FRAME IS CRACKED ON FWD SIDE IN THREE PLACES. AFT SIDE ON TOP OF CREASE, FWD SIDE AT BOTTOM OF STOP FITTING, UPPER CORNER OF STOP FITTING, OB LOWER CORNER OF STOP FIT TING AND THROUGH IB LOWER BOLT HOLE OF STOP FITTING AFT SIDE CRACK IS IN RADIUS ADJACENT TO UPPER IB CORNER OF STOP FITT ING, REPAIRED INSPECTION REQUIRED EVERY 4000 CYCLES. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700131 20070817 00131 EU 2007 8 17 CPCP20070076 1 20070529 A 5320 FLOOR SUPPORT AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 429AT 429 LT "Z" FLOOR BETWEEN FRAME 39-40 CORRODED ON LOWER SURFACE. LT "Z" FLOOR BETWEEN FRAME 39-40 REPLACED AS PER SRM 51-25- 02. 2 H 7 2 4T RT A53EU 2007081700132 20070817 00132 NM 2007 8 17 DHL2007741534 1 20070807 A 5313 BAC1498146 STRINGER BOEING 727 7272Q9 138448M NM BS 950B-950F CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AFT PIT LT AT STR 27L, BS 950B TO 950F, IS CORRODED AROUND RIVETS. CORROSION REMOVAL OF .015" MATERIAL EXCEEDED LIMITS PER B727 SRM 53-10-1 FIG 1. CUT OUT DAMAGED SECTION OF STRINGER, 65.5" IN LENGTH PER B727 SRM 53-10-3 FIG 1. VERIFIED NO CORROSION ON MATING SKIN. FABRICATED NEW STRINGER SECTION FROM BAC1498-146, 65.5" IN LENGTH, PO NR 7220244, AND REPA IR "HAT" SECTION FROM BAC1498-196, 13.5" LONG, PO NR 7220244, PER B727 SRM 53-10-2 FIG 9 AND 53-10-3 FIG 1. TREATED, PR IMED, AND INSTALLED REPAIR PARTS PER B727 SRM 51-10-2 AND 53-10-3 FIG 1. NOTE: NEW STRINGER SECTION ATTACHED AT EXISTI NG SPLICES AT BS 1010. 2 L 7 3 4F RT A3WE 2007081700133 20070817 00133 NM 2007 8 17 2007UALA02999 1 20070803 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 UPPER FUSE SKIN CHAFED BELOW LT SIDE SECTION OF DORSAL FIN BETWEEN STA 887 AND 1006. MAJOR REPAIR ACCOMPLISHED: BLENDE D DAMAGE. INSTALLED WEAR STRIPS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700134 20070817 00134 NM 2007 8 17 2007UALA03000 1 20070803 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 UPPER FUSE SKIN CHAFED BELOW RT SIDE SECTION OF DORSAL FIN BETWEEN STA 887 AND 1006. MAJOR REPAIR ACCOMPLISHED: BLENDE D DAMAGE AND INSTALLED WEAR STRIPS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700139 20070817 00139 NM 2007 8 17 QXEA200701244 1 20070807 A 5230 502212 SEAL BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR DAMAGED A QXEA O OTHER O OTHER DE DESCENT 1 NM 09 410QX 4053 SEA FLIGHT NR 2324: WHILE DESCENDING THROUGH APPROX 9000 FT, A LOUD POP WAS HEARD FROM THE AFT PAX DOOR FOLLOWED BY DEPR ESSURIZATION OF THE AIRCRAFT. CABIN INDICATED +3000 FPM CLIMB. AS THE AIRCRAFT DESCENDED THROUGH 5000 FT, THE A/C BEGA N TO PRESSURIZE INDICATION A , 3000 FPM DESCENT. THERE WERE NO CAUTION OR WARNING LIGHTS WITH THE EVENT. MAINTENANCE R EMOVED AND REPLACED THE MCD AND AFT CARGO DOOR SEAL. PRESSURIZATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007081700142 20070817 00142 EU 2007 8 17 CPCP20070084 1 20070705 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 431AT 431 FOUND FRAME 40 FLOORBEAM CORRODED. FRAME 40 FLOORBEAM REPLACED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007081700144 20070817 00144 EU 2007 8 17 CPCP20070085 1 20070705 A 5320 FLOOR SUPPORT AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 431AT 431 FOUND FRAME 39-41 RT Z FLOOR CORRODED. RT "Z" FLOOR REPLACED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007081700145 20070817 00145 NM 2007 8 17 2007UALA03005 1 20070803 A 5320 DOUBLER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 STRUCTURE AT STR 12R STATION 518.5 IS DAMAGED. MAJOR REPAIR ACCOMPLISHED: REPLACED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700147 20070817 00147 NM 2007 8 17 2007UALA03007 1 20070805 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 AFT CARGO DOOR CUTOUT AFT FRAME IS CRACKED AT LOWER BOTTOM STOP FITTING OUTBOARD LOWER CORNER AROUND BOTTOM FASTENER. M AJOR REPAIR ACCOMPLISHED: REPLACED AFT CARGO PIT AFT FRAME AROUND DOOR CUTOUT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700148 20070817 00148 NM 2007 8 17 2007UALA03008 1 20070804 A 5320 ATTACH ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 ANGLE CRACKED, PASS CABIN FWD OF GALLEY DOOR STA 290 JUST ABOVE STR 10R, INTERCOSTAL WEB ATTACH ANGLE CRACKED. MAJOR RE PAIR ACCOMPLISHED: REPLACED CRACKED ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700150 20070817 00150 NM 2007 8 17 2007UALA03010 1 20070803 A 3350 1317 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 382UA 24657 EMERGENCY AISLE LIGHT IN BULLNOSE AT ROW 1 2 INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700152 20070817 00152 NM 2007 8 17 2007UALA03011 1 20070804 A 3510 OXYGEN MASK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 385UA 24660 OBSERVERS OXYGEN MASK HARD TO BREATH THROUGH. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700154 20070817 00154 NM 2007 8 17 2007UALA03012 1 20070803 A 3510 HARNESS BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU O2 MASK FRAYED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 331UA 24192 CAPTAIN'S O2 MASK HARNESS IS FRAYED. REPLACED CAPTAIN'S O2 MASK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700156 20070817 00156 NM 2007 8 17 2007UALA03013 1 20070805 A 3397 58781 CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 334UA 24229 EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT INOP AND EEL LIGHTS ROWS 15-21 ARE DIM. REPLACED CABLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700159 20070817 00159 NM 2007 8 17 07FDEA02802 1 20070808 A 5710 652165832 SUPPORT ANGLE BOEING 727 7272S2F 1384O81 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 212FE 22934 RT WING OB T/E LOWER PANEL SUPPORT ANGLE HAS A CRACK UNDER SPOILER NR 13. REMOVED AND REPLACED SUPPORT ANGLES IAW SRM 5 1-30-2. 2 L 7 3 4F A3WE 2007081700160 20070817 00160 NM 2007 8 17 2007UALA03015 1 20070805 A 2910 HYDRAULIC SYSTEM BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RIGHT LEAKING A UALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 WP 29 668UA 30024 RTFL UNDER AMBER ALERT DUE TO RIGHT HYDRAULIC SYSTEM QUANTITY LOSS. 08-31-07 NR 2 ENGINE EDP FAILURE AND LOSS OF R IGHT HYDRAULIC SYSTEM FLUID. REPLACED PUMP AND FILTERS. DRAINED REMAINING FLUID & FLUSHED. REPLACED FILTERS & RESERV ICED FLUID. LEAK CHECKED OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007081700161 20070817 00161 NM 2007 8 17 07FDEA02803 1 20070808 A 5730 PANEL BOEING 727 7272S2F 1384O81 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 212FE 22934 RT WING REAR SPAR LWR CHORD WAVY PANEL HAS 2 EA CRACKS APPROX FROM RSS 542-RSS 563. REMOVED SEAL IAW SRM 51-30-2. FABR ICATED NEW SPLICES ON TRAVELER T7/691015 2024 T3 .063. FABRICATED LWR CHORD PANEL OB SIDE ON TRAVELER T7/691016 2024 T3 .063. INSTALLED REPAIR PARTS IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2007081700163 20070817 00163 NM 2007 8 17 07FDEA02804 1 20070808 A 5753 SKIN BOEING 727 7272S2F 1384O81 NM ZONE 600 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 212FE 22934 REPAIR ON RT WING OB AFT FLAP LWR SIDE AT W-STA 650. REPAIR EVALUATED AND FOUND NOT TO BE IAW SRM 51-40-20. PREVIOUSLY INSTALLED REPAIR WAS REMOVED AND REPAIRED IAW SRM 51-40-20. 2 L 7 3 4F A3WE 2007081700166 20070817 00166 EA 2007 8 17 TRAX200701101 1 20070725 A 2560 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 854AS 7382 EMERGENCY EXIT SIGN ON GALLEY DAMAGED. 10-18-07 REMOVED DAMAGE. REPLACED WITH SERVICEABLE EMERGENCY EXIT SIGN PNBR 9219-106 IAW CRJ AMM 33-51-00. PERFORMED OPS CHECK IAW CRJ AMM 33-51-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007081700167 20070817 00167 NM 2007 8 17 07FDEA02807 1 20070808 A 5313 654531314 STRINGER BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 PASSENGER CABIN STA 950D, STR 9R STRINGER CLIP CRACKED REMOVED AND REPLACED STRINGER CLIP 950D, STR 9R REF SRM 51-30-2, THIS IS CLASSIFIED AS A MAJOR. 2 L 7 3 4F RT A3WE 2007081700168 20070817 00168 EU 2007 8 17 07FDEA02810 1 20070809 A 5320 A53989317228 ANGLE AIRBUS 300 A300B4605R 3930308 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 ANGLE FRONT SIDE AND L-SHEET REARSIDE AT FR 92 ARE CORRODED REPAIR IN ACCORDANCE WITH EA 6-5319-112453 AND RAS/DAHAM/402 2472/2007 ISSUE "B" PERFORMED. 2 L 7 2 4F RT A35EU 2007081700169 20070817 00169 EA 2007 8 17 TRAX200701102 1 20070731 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 833AS 7246 LEFT INTERCOSTAL AT FS 625 STRINGER 14L CRACKED. 2 L 7 2 4F RT A21EA 2007081700171 20070817 00171 EA 2007 8 17 TRAX200701103 1 20070803 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 927EV 7844 PAX DOOR BOTTOM STEP CRACKED. 2 L 7 2 4F RT A21EA 2007081700172 20070817 00172 NM 2007 8 17 07FDEA02812 1 20070809 A 5320 656725034 ANGLE BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LWR AFT CARGO PIT, STA 1166 BULKHEAD WALL STRUCTURE. VERTICAL Z-ANGLE IN CENTERLINE, BL 0" ABOVE DIFFERENTIAL PRESSUR E VALVE HAS CORROSION AT LWR AND UPPER LT SIDE. REMOVED DAMAGE AREA, DRILLED NEW PART, Z-ANGLE PN NR 65-67250-34, IAW B 727 SRM 51-30- 2 PG 1. INSTALLED NEW Z-ANGLE, IAW B727 SRM 51-30-2, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007081700173 20070817 00173 EA 2007 8 17 TRAX200701104 1 20070803 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 927EV 7844 PAX DOOR OUTER HANDLE CRACKED. 2 L 7 2 4F RT A21EA 2007081700175 20070817 00175 EA 2007 8 17 TRAX200701105 1 20070803 A 5210 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 833AS 7246 PAX DOOR FS 320.10 FRAME IS CRACKED. 2 L 7 2 4F RT A21EA 2007081700176 20070817 00176 NM 2007 8 17 07FDEA02814 1 20070809 A 5320 65585393 INTERCOSTAL BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD CARGO AREA, STA 702 TO 705 AT STR 28R ABOUT RBL 8 INTERCOSTAL IS CORRODED IN LOWER FWD CORNER. REMOVED STIFFENER AT STA 700 RBL 8, AND STA 720 RBL 8. REMOVED INTERCOSTAL AT RBL 8 BTW STA 700-720. FABRICATED NEW INTERCOSTAL AND INSTAL LED. INSTALLED STIFFENER AT RBL 8 STA 720. INSTALLED STIFFENER AT STA 700, REF SRM 51-30-2. THIS IS CLASSIFIED AS A M INOR REPAIR. 2 L 7 3 4F RT A3WE 2007081700177 20070817 00177 NM 2007 8 17 07FDEA02815 1 20070809 A 5347 60104527075T65 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT UPPER MAIN DECK, CORROSION ON SEAT TRACK STA 1166 IN CENTERLINE BL 0" AND LBL 2" ON FLANGE REMOVED, FABRICATED NEW T RACK, INSTALLED SEAT TRACK AT BS 1166 BL 0" PER SRM 51-30-2, 51-30-5, 51-30-08, 51-30-02. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007081700179 20070817 00179 NM 2007 8 17 07FDEA02816 1 20070809 A 5754 SKIN BOEING 727 7272S2F 1384O81 NM NR 8 SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 212FE 22934 RT WING NR 8 SLAT UNDERSIDE SKIN AT OTBD END HAS SEVERAL SHEARED FASTENERS AND A POSSIBLE CRACK AT ONE OF THE FASTENER H OLES. REMOVED AND REPLACED NR 8 SLAT ASSY IAW 27-81-011-4. 2 L 7 3 4F A3WE 2007081700180 20070817 00180 EU 2007 8 17 AWXA200700975 1 20070804 A 5320 D53231335200 FITTING AIRBUS 320 A320231 3930325 EU ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 SAL - MAJOR REPAIR - C-06 CHECK - NR 5979624, CORROSION ON FORWARD CARGO COMPARTMENT DOOR CUT OUT LOWER SILL, AFT CORNER THRESHOLD SHEET FITTING, BS 1163, FR 28, S39R. REPLACED FORWARD CARGO COMPARTMENT DOOR CUT OUT LOWER SILL, AFT CORNER THRESHOLD SHEET FITTING, BS 1163, FR 28, S39R IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007081700182 20070817 00182 EU 2007 8 17 AWXA200700976 1 20070806 A 5320 D53475529204 PROFILE AIRBUS 320 A320231 3930325 EU ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 SAL - MAJOR REPAIR - C-06 CHECK - NR 5990559, CORROSION ON AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL SEALING PROFILE , BS 2563/FR 55+16". REPLACED AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL SEALING PROFILE BS 2403/FR 52 TO BS 2616/F R 56 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007081700183 20070817 00183 EA 2007 8 17 TRAX200701086 1 20070730 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 854AS 7382 ACFT EXTERNAL BELLY SKIN CORRODED IN AREA OF TCAS LOWER ANTENNA. UPON FURTHER INVESTIGATION, FOUND CORROSION UNDER TCAS BELLY ANTENNA TO MINOR SURFACE CORROSION. REMOVED MINOR SURFACE CORROSION IAW CRJ SRM 51-21-06 AND TREATED AREA IAW CR J SRM 51-21-16. SUPPLEMENTAL - SDR CLOSED 08/07/07. 2 L 7 2 4F RT A21EA 2007081700185 20070817 00185 EU 2007 8 17 AWXA200700978 1 20070725 A 5544 D5537123500600 HINGE FITTING AIRBUS 320 A320231 3930325 EU ZONE 300 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 SAL - MAJOR REPAIR - C-06 CHECK - NR 5964983, THE NR 3 RUDDER HINGE FITTING HAS EXCESSIVE PLAY, RUDDER STATION 2279/RIB 5. REPLACED THE NR 3 RUDDER HINGE FITTING, RUDDER STATION 2279/RIB 5 IAW A320 AMM 27-21-41. 2 L 7 2 4F RT A28NM 2007081700186 20070817 00186 EU 2007 8 17 AWXA200700979 1 20070725 A 5544 D5537123500600 HINGE FITTING AIRBUS 320 A320231 3930325 EU ZONE 300 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 SAL - MAJOR REPAIR - C-06 CHECK - NR 5964981, THE NR 4 RUDDER HINGE FITTING HAS EXCESSIVE PLAY, RUDDER STATION 2632/RIB 6. REPLACED THE NR 4 RUDDER HINGE FITTING, RUDDER STATION 2632/RIB 4 IAW A320 AMM 27-21-41. 2 L 7 2 4F RT A28NM 2007081700187 20070817 00187 EU 2007 8 17 AWXA200700980 1 20070725 A 5544 D5537123500600 HINGE FITTING AIRBUS 320 A320231 3930325 EU ZONE 300 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 SAL - MAJOR REPAIR - C-06 CHECK - NR 5964984, THE NR 5 RUDDER HINGE FITTING HAS EXCESSIVE PLAY, RUDDER STATION 2985/RIB 7. REPLACED THE NR 5 RUDDER HINGE FITTING, RUDDER STATION 2985/RIB 7 IAW A320 AMM 27-21-41. 2 L 7 2 4F RT A28NM 2007081700188 20070817 00188 EU 2007 8 17 AWXA200700981 1 20070729 A 5712 D5725218100100 RIB AIRBUS 320 A320231 3930325 EU ZONE 600 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 SAL - MAJOR REPAIR - C-06 CHECK - NR 5990411, CORROSION ON RIGHT WING RIB 5 FORWARD LUG, WS 2508/RIB 5. REPAIRED THE NR 5 RIGHT WING RIB 5 FORWARD LUG, WS 2508/RIB 5 IAW A320 SRM 57-26-13. 2 L 7 2 4F RT A28NM 2007081700192 20070817 00192 EU 2007 8 17 AWXA200700984 1 20070804 A 5320 D5347209800 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 632AW 81 SAL - MAJOR REPAIR - C-7 CHECK - NR 5963562, CORROSION ON FLOORBEAM, BS 3101/FR 65 - BS 3207/FR 67, +Y919. REPLACED FLO ORBEAM, BS 3101/FR 65 - BS 3207/FR 67, +Y919 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007081700194 20070817 00194 EU 2007 8 17 F3LA200700196 1 20070809 A 3350 32146210 EPSU AIRBUS A318 A318111 3940019 EU EMERGENCY LIGHTS INOPERATIVE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 802FR 759 1991 FLIGHT CREW REPORTED EMERGENCY EXIT LIGHT OVER AFT GALLEY ENTRY INOP. REPLACED EPSU 13WL IAW AMM 33-51-35. 2 L 7 2 4F RT 2007081700196 20070817 00196 NM 2007 8 17 QXEA200701265 1 20070809 A 2133 88060B010003 OUTFLOW VALVE BOMBDR DHC8 DHC8402 1390042 NM CABIN PRESSURE MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 431QX 66 66 4164 LAX FLIGHT NR 2334: CABIN ALT CLIMBING EXCESSIVELY. NOTICED FAULT LIGHT ILLUMINATED ON PRESSURE CONTROLLER. RAN EMERGE NCY CHECKLIST. HAD THEM RUNNING IN MANUAL MODE. MAINTENANCE REMOVED AND REPLACED AFT OUTFLOW VALVE IAW Q400 AMM TASK 2 1-31-10-000-801 AND 21-31-10-400-801. FUNCTIONAL TEST GOOD IAW 21-31-00-720-801. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007081700197 20070817 00197 EA 2007 8 17 TRAX200701091 1 20070731 A 5553 ATTACH ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 719EV 10099 LEFT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE HAS SUSPECT CRACK AFT. PERFORMED ET INSPECTION OF SUSPECT AREA IAW CR J 700 NDTM 51-20-006. ATTACH ANGLE IS CRACKED. PERFORMED EDDY CURRENT INSPECTION OF LEFT VERTICAL STABILIZER TO FUSELA GE ATTACH ANGLE TO DETERMINE END OF CRACK IAW CRJ 700 NDTM 51-20-006. PERFORMED EDDY CURRENT INSPECTION OF CUT LINE ON VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE, LEFT SIDE, IAW REO 670-55-31-018 PER CRJ 700 NDTM 51-20-006. NO DEFECTS N OTED. FABRICATED FILLER -2 AND DOUBLER -1 FROM 2024T3 .090" BATCH 677878. INSTALLED REPAIR PER 670-55-31-018. SUPPLEM ENTAL - SDR CLOSED 08/06/07. 2 L 7 2 4F RT A21EA 2007081700198 20070817 00198 NM 2007 8 17 QXEA200701266 1 20070808 A 7810 VALVE BOMBDR DHC8 DHC8402 1390042 NM P2 CONTAMINATED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NM 09 402QX 4032 PDX FLIGHT NR 2265: FA REPORTS EXHAUST ODOR IN REAR OF AC ON APPROACH. PAX REPORTS FEELING SICK FROM ODOR. MAINTENANCE DUPLICATED ODOR USING NR 2 BLEED. C/W FIM 71-00-00-810-817. NO FAULT CODE IN CDS. NO OILY RESIDUE FOUND ON P2.2, P2.7 VALVES, P3.0 DUC OR THE HPSOV PRE COOLER DUCT. C/W BSI IAW Q400 AMM TASK 72-00-00-290-803, PAR 4 AND TASK 72-00-00-290 -804. NO DEFECTS NOTED. COMPLETED GROUND RUNS FOR FCS CONTAMINATION IAQ Q400 SL 21-012A. NO FURTHER UNPLEASANT ODORS FOUND. COMPLETED FIM TASK 71-00-00-810-817. FOUND VERT-STAB LOWERED DUCT CHECK VALVE NOT COMPLETELY CLOSING. CLEANED AND LUBED DUCT CHECK VALVE. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007081700200 20070817 00200 EA 2007 8 17 TRAX200701095 1 20070801 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 719EV 10099 RIGHT 280 WEB CORRODED. BLENDED CORROSION AT RIGHT 280 WEB AND FOUND TO BE WELL OUT OF LIMITS PER REO 670-53-11-052 CJ7 020938. BEGAN REMOVAL OF RT 280 WEB WORK DONE IAW CRJ 700 SRM 51-42-06 DK 7022603. REMOVED RT FS 280 WEB, LOCATED AND DRILLED NEW WEB IAW CRJ 700 SRM 51-42-06 SG7020421. COMPLETED ALL WORK PER REO670-53-11-052. SUPPLEMENTAL - SDR CLOSED 08/06/07. 2 L 7 2 4F RT A21EA 2007081700203 20070817 00203 2007 8 17 SIMA200722202 4 20070807 A 3460 6227491210 COMPUTER SAAB SF340 340B 7860101 EU FLIGHT CONTROL FAILED A SIMA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SW 21 340RC 21280 30 340B340 VIBRATION SHUDDER OCCURS AT HIGH SPEED ABOVE 230 KNOTS, FEELS LIKE LOW FREQUENCY SHAKE LIKE BUFFETING. REMOVED AND REPL ACED FLIGHT CONTROL COMPUTER IAW SAAB AMM 34-22-05. OPERATIONAL CHECK GOOD, PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DE FECTS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007081700204 20070817 00204 2007 8 17 SIMA200722203 4 20070808 A 3420 HG2010AC02 COMPUTER EMB 135 EMB135LR 3260305 SO AHRS FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 706RG 11376 4870 145194 ON TAKEOFF ROLL ENGINE POWER WITH TO TAKEOFF RESERVE FOLLOWED BY YAW DAMPER AND AHRS FAIL MESSAGES. REMOVED AND REPLACE D NUMBER ONE AHRS COMPUTER IAW EMB AMM 31-21-01, OPERATIONAL CHECKED GOOD. PERFORMED HIGH POWER RUNS IAW EMB AMM 76--12 -01 WITH NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECKS OF YAW DAMPER IAW EMB AMM 22-11-00 WITH NO DEFECTS. AIRCRAFT R ETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007081700205 20070817 00205 NM 2007 8 17 KCSA07061 1 20070703 A 2120 UNKNOWN BOEING 747 747209F 1384800 NM COCKPIT ODOR A KCSA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 704CK 22299 WHILE OPERATING FLT DECK FAN NOTICED ELECTRICAL ODOR. PERFORMED OPERATION TEST OF THE RECIRCULATION SYSTEM PER B747 M/M 21-25-00. COULD NOT DUPLICATE. NO DEFECTS NOTED AT THIS TIME OPS CHECK OK. 2 L 7 4 4F RT A20WE 2007081700206 20070817 00206 NM 2007 8 17 KCSA071281 1 20070807 A 5414 SKIN BOEING 747 7472B4B 138481B NM NR 2 PYLON WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NR 2 PYLON OUTBOARD SIDE SKIN FILLER OF PREVIOUS REPAIR WORN AND SKIN WORN FORWARD OF EXISTING REPAIR AT NAC STA 180 TO 221.9, ABOVE MIDSPAR. 2 L 7 4 4F RT A20WE 2007081500377 20070815 00377 2007 8 15 YENA2007069 4 20070731 A 2330 M835366022M RELAY EMB ERJ190 ERJ190100IGW 3260408 EU ENTERTAIN SYS DEFECTIVE A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 15 198JB 19000021 FLT 1053, AT APPROX 1:15 PM JFK-PIT, ON DESCENT FUMES/POSSIBLE SMOKE IN CABIN/COCKPIT, SEEMS TO DISSIPATE UPON SECURING LIVE TV. INSPECTED CABIN, COCKPIT & AFT MID & FWD AVIONICS BAYS, NO DEFECTS NOTED. FOUND CV C/B POPPED ON LTV RAC, ENE RGIZED LTV SYSTEM. PERFORMED TROUBLESHOOTING CHECK OF EQUIPMENT VENTILATION SYSTEM IAW 21-28-00. GROUND SHUT OFF VALVE FAILED. TROUBLESHOT COOLING SYSTEM IAW E190 WDM 21-28-51. FOUND RELAY KO367 DEFECTIVE AND CAUSE OF C/B POPPING. REMO VED AND REPLACED RELAY IAW E190 SWPM 20-32-02. PERFORMED TROUBLESHOOTING CHECK OF EQUIPMENT VENTILATION SYSTEM AGAIN. NOW PASSED. COMPLETED CABIN CHECK OF LTV AND ALL CHECKED GOOD IAW LTV MM 44-20-10. 2 L 7 2 4F RT A57NM 2007081600003 20070816 00003 EA 2007 8 16 QXEA200701225 1 20070730 A 3610 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA ENGINE UNKNOWN A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 600QX 10005 PDX - FLIGHT 2262, AFTER ENGINE START, RT BLEED CLOSED AND LT BLEED CLOSED. MAINTENANCE PLACED ON MEL 36-12-2. 8/1. P ERFORMED OPERATIONAL TEST WITH NO DEFECTS. CLEARED MEL. AIRCRAFT RETURNED TO SERVICE WITH NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007081600007 20070816 00007 NM 2007 8 16 DHL2007741526 1 20070803 A 5320 SUPPORT ANGLE BOEING 727 7272Q9 138448M NM BS 294.5 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 NOSE SECTION INTERIOR HORIZ WALKWAY BEAM LT SIDE WEB SUPPORT ANGLE AT BS 294.5 AND LBL 30 SHOWS CORROSION FROM LOWER SID E. REMOVED ANGLE, FABRICATED ANGLE FROM BAC1503-100195, 26.75" LONG, PO NR 7385277, PER B727 SRM 53-10-2 FIG 1 AND 51-2 0-1. TREATED, PRIMED, AND INSTALLED NEW ANGLE PER B727 SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007081600014 20070816 00014 SO 2007 8 16 SIMA200721804 1 20070804 A 2612 14534156401 CONTROL PANEL EMB 145 EMB145LR 3260212 SO FIRE DETECTION MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 693AE 7282 14500868 INFLIGHT RECEIVED APU FIRE INDICATION WITH FIRE DETECT FAIL MESSAGE. DIVERTED TO SAT. REMOVED AND REPLACED FIRE TEST P ANEL IAW EMB AMM 26-00-01. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007081600017 20070816 00017 SO 2007 8 16 SIMA200721802 1 20070803 A 3260 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO RT MLG OUT OF ADJUST A SIMA O OTHER N FALSE WARNING CL CLIMB 1 SW 21 616AE 145092 LANDING GEAR NO RETRACT, RETURNED TO DFW. FOUND PROXIMITY SENSOR OUT OF ADJUSTMENT. ADJUSTED RIGHT MAIN LANDING GEAR N UMBER ONE AND TWO WEIGHT ON WHEEL PROXIMITY SENSORS IAW EMB 32-63-05. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SER VICE. 2 L 7 2 4T RT T00011AT 2007081600024 20070816 00024 NM 2007 8 16 MZZA0700009 1 20070723 A 5313 BAC1498156X STRINGER BOEING 737 737824 13844BZ NM STA 500-500D CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 25201 28958 INSPECTION FOUND STRINGER 27L AT BAY 14 IN FORWARD CARGO COMPARTMENT WITH ROWS OF RIVETS CORRODED, STA 500-500A. 2 L 7 2 4F RT A16WE 2007081600026 20070816 00026 NM 2007 8 16 HALA0700324 1 20070803 A 2697 CONNECTOR BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE FIRE LOOP DAMAGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM, EICAS MESSAGE"L ENG FIRE LP 1". ACCOMPLISHED FIM 26-11-00. REMOVED AND REPLACED LOWER FWD FI RE LOOP, COND SAME. FOUND CONNECTOR AT AFT LOWER LOOP BAD. INSTALLED NEW LUG. OPS/TEST OK (REF WDM 26-11-11). 2 L 7 2 4F 4 F RT A1NM E24NE 2007081600033 20070816 00033 NM 2007 8 16 AWXA200700959 1 20070723 A 5340 6953207501 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5982104, CRACKED STRINGER CLIP, BS 663, S4L. REPLACED STRINGER CLIP, BS 663, S4L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007081600035 20070816 00035 EU 2007 8 16 AWXA200700961 1 20070726 A 5210 D5311245800000 STOP FITTING AIRBUS 320 A320231 3930325 EU ZONE 800 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 SAL - MAJOR REPAIR - C-06 CHECK - NR 5990363, R2 DOOR UPPER DOOR STOP FITTING WORN, BS 709/ FR 16. REPLACED R2 DOOR UPP ER DOOR STOP FITTING, BS 709/FR 16 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007081600044 20070816 00044 NM 2007 8 16 07FDEA02767 1 20070804 A 5415 MOUNT DOUG MD11 MD11F 3023600 NM NR 3 NACELLE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 ENG NR 3: AFTER ENGINE REMOVAL FOUND PYLON FWD MOUNT LT MOUNT LT AFT BORE HOLE, SUSPECT PITTING CORROSION. [08-20-07] REPAIR CARRIED OUT AT ENG NR 3 PYLON FWD MOUNT LH AFT BORE HOLE AS PER FEDEX EA 1-5410-112377, REPAIR CLASSIFIED AS M AJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007081600046 20070816 00046 NM 2007 8 16 07FDEA02769 1 20070805 A 5730 ARB74024 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 WITH REFERENCE TO EA NR 1-5710-90773 DURING ACCOMPLISHMENT OF ALI 57.23.01.2. TWO MOUNTING BORES THE TANKS ACCESS PLATE AT STA XORS = 713.6 GAVE A CRACK INDICATION. THE BORES WERE INCREASED TO 0.310" WHERE CRACK INDICATION CEASED. COMPLI ED WITH FEDEX EA NR 1-5710-112360, TITLE: AD 2007-07-04 - WINGS - RIGHT LOWER SKIN PLANK CUT OUT ATT 636AB - FOUR ACCESS DOOR ATTACHMENT BORES WITH CRACK INDICATIONS PSE 57.23.01 ALI - REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007081600047 20070816 00047 NM 2007 8 16 07FDEA02770 1 20070806 A 5730 ARB2888501 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 LT WING, LEADING EDGE EXTERIOR SKIN BETWEEN SLAT TRACK NR 10 AND NR 11 FOUND CHIPPED. [08-17-07] CHIPPED AREA SMOOTH ENED OFF AS PER SRM 51-21-01 VOLUME II. EXCEEDED LIMIT AS PER SRM 57-00-01 FIGURE 2 VOLUME I. REWORKED AREA REPAIRED A S PER SRM 57-10-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007081600065 20070816 00065 SO 2007 8 16 LR7A07064 1 20070726 A 5330 SKIN LKHEED 382 382G 526414U SO BS 807E, RBL 63 DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 325 4590 DURING SCHEDULED A-1 CHECK PER JOB CARD HA1201, FOUND EXTERIOR FUSELAGE SKIN DENTED AT FS 807E, RBL 63, WL 144. REPAIRE D SKIN IAW LAC MEA 382-53-07-051. 2 H 7 4 4T A1SO 2007081600068 20070816 00068 EU 2007 8 16 F3LA200700193 1 20070803 A 5321 D5367180500400 FLOOR PANEL AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 803FR 5201 2017 DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR THRESHOLD CORRODED ON SURFACE OF PANEL 261FF. REPLACED FLOOR PANEL 261FF IAW AMM 53-42-12-400-002. 2 L 7 2 4F RT 2007081600069 20070816 00069 NM 2007 8 16 NWAA072785521 1 20070805 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 521US 23209 DURING OVERNIGHT CHECK, AFT CABIN EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CH ECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007081600085 20070816 00085 NM 2007 8 16 AALA20071381 1 20070731 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 395AN 29432 DFW EMERGENCY LIGHT AT LEFT OVERWING FORWARD POSITION INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT OVERWING FORWARD POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007081600096 20070816 00096 WP 2007 8 16 AALA20071395 1 20070803 A 2910 LINE DOUG DC9 DC982 3022082 WP HYD SYSTEM INOPERATIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 452AA 49553 EWR INFLIGHT T558 - LEFT HYDRAULIC PRESSURE INDICATION AS THEY ENTERED HOLDING. LEFT PRESSURE READ ZERO POUNDS PER SQUA RE INCH. LANDED EWR WITHOUT INCIDENT. FOUND EXCESSIVE AIR IN LEFT AND RIGHT HYDRAULIC SYSTEMS. PERFORMED EXCESSIVE AI R CHECK AND BLED AIR FROM LEFT AND RIGHT HYDRAULIC SYSTEMS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007081600104 20070816 00104 NM 2007 8 16 AALA20071400 1 20070804 A 3397 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 776AN 29582 MIA - EMERGENCY LIGHT AT SEAT 4G INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 4G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007081600121 20070816 00121 NM 2007 8 16 AALA20071407 1 20070804 A 3350 P4010049 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 324AA 22325 JFK - EMERGENCY LIGHTS FROM SEATS ROWS 10AB TO 11AB INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT R OWS 10AB TO 11AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007081600135 20070816 00135 NM 2007 8 16 DHL2007741531 1 20070804 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 950F DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AFT PIT, LT BS 950F, FRAME DENTED BETWEEN STR 23L AND 26L. CUT OUT DAMAGED AREAS, 2 EA, 1.5" BY 1", FABRICATED ANGLE RE PAIR FROM 7075-T0, .071" BY 12" BY 4" BY 1", IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1. HEAT TREATED REPAIR ANGLE TO T6 CONDITION IAW F.A.S.I. ER NR 2-37153-801 REV A. TREATED, PRIMED, AND INSTALLED REPAIR ANGLE PER B727 SRM 51-10-2 AN D 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2007081600142 20070816 00142 NM 2007 8 16 DL757071004 1 20070803 A 5415 012N88861 ATTACH FITTING BOEING 757 757232 1384965 NM NR 2 PYLON MISALIGNED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 635DL 23762 INSTALLATION OF NEW NR 1 AND NR 2 PYLON WING ATTACH TENSION CLIPS WOULD HAVE REQUIRED SPOTFACE GREATER THAN THE 0.005" A LLOWABLE PER EO 6-070332-03 WHICH PERTAINED TO S/B 757-54-0034 REV 1 FOR THE SIP MODIFICATION. TAPERED RADIUS FILLERS W ERE FABRICATED AND INSTALLED FOR EACH HOLE. 2 L 7 2 4F RT A2NM 2007081600143 20070816 00143 NM 2007 8 16 DL76P071005 1 20070803 A 3350 202121 MODULE BOEING 767 767332 1382001 NM EMERGENCY LIGHTS INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1402A 25989 RT CEILING EMERGENCY LIGHTS FROM 37EF AFT INOP. SEAT TRACK LIGHTS INOP AFT CABIN RIGHT SIDE ROW 25 EF TO 45EF. REPLACE D CHARGER AND BATTERY MODULE NR M737. OPS NORMAL. BATTERY VOLTAGE LOW. REPLACED BATTERY PACK AT M732. OPS CHECKED NO RMAL. PART BORROWED FROM NW. 2 L 7 2 4F RT A1NM 2007081600145 20070816 00145 NM 2007 8 16 DL76P071007 1 20070803 A 2610 261201241 LOOP BOEING 767 767332 1382001 NM UNKNOWN A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 144DA 27584 PASSING 28000 FT T/O PLUS 15 MIN CLIMB PWR RT DUCT BLEED LIGHT AND EICAS MSG. COMPLETED WITH QRH PROCEDURE RT DUCT BLEE D LEAK EXTINGUISHED PASSING 32500 FEET. VISUALLY INSPECTED PNEU DUCTING AND CLAMPS ALONG WITH CHECKING FOR LEAKS FROM R T ENG PYLON TO RT ECS BAY NO DISCREPANCIES FOUND. VISUALLY INSP OVERHEAT ELEMENTS AND CLAMPING FROM ABOVE PYLON TO RT E CS BAY NO DISCREPANCIES NOTED. REPLACED LOOPS TS216 TS 217 TS218 TS 219 TS215. REPLACED BOTH TERMINAL STRUT SWITCHES R AN RT ENG TO T/O AND CLB PWR NO EICAS MSG OR LIGHT. 2 L 7 2 4F RT A1NM 2007081600153 20070816 00153 NM 2007 8 16 DL76S071016 1 20070804 A 5610 561701281 WINDOW BOEING 767 767332 1382001 NM COCKPIT CRACKED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 123DN 23437 F/O WINDSHIELD CRACKED AND IS ARCHING. REPLACED R1 WINDOW WINDOW HEAT CONTROL UNIT PER AMM. BITE CHECKED CONTROL UNIT IT VERIFIED GOOD. 2 L 7 2 4F RT A1NM 2007081600163 20070816 00163 NM 2007 8 16 DLM90071034 1 20070806 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 676-746 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 RT CUSP WEB CORRODED OUT OF LIMITS FS 676-746. REPAIRED CUSP WEB IAW EA 398191-14MA DATED 9/18/02. 2 L 7 2 4F RT A6WE 2007081600164 20070816 00164 NM 2007 8 16 DLM90071035 1 20070720 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 1344 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 CRACK IN FLOOR WEB LEFT CUSP WEB AT LT FUSELAGE STA 1344 UNDER GALLEY. REPAIRED CUSP WEB IAW DELTA ERA 413196-14MA REV ORG 05/15/03. 2 L 7 2 4F RT A6WE 2007081600168 20070816 00168 NM 2007 8 16 DL76G071039 1 20070807 A 3150 RELAY BOEING 767 767332 1382001 NM UNKNOWN FAILED A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 173DZ 29692 RTB FWD CARGO OVERHEAT EICAS MSG. REPLACED RELAY K231 PER FIM. 2 L 7 2 4F RT A1NM 2007081600179 20070816 00179 EU 2007 8 16 CPCP20070068 1 20070606 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 447AM 447 FOUND FLOORBEAM 38 CORRODED. FLOORBEAM 38 REPAIRED IAW SRM 53-00-00 FIG 435. 2 H 7 2 4T RT A53EU 2007081700003 20070817 00003 NM 2007 8 17 UPS07650390 1 20070804 A 2612 FIRE LOOP BOEING 767 76734AF 1385212 NM RT ENGINE BROKEN A IPXA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 01 332UP 32843 INSPECTION TYPE:ETOP RT ENGINE FIRE LOOP 2 MESSAGE DISPLAYED ON ENGINE SHUTDOWN. UPON INSPECTION FOUND NR 2 LOOP BROKEN AT TERMINAL,FWD MOST ATTACH POINT OF LOWER, FWD ENGINE FIRE DETECTOR. REPAIR MADE IAW SSWD 20-15-2 & OPS CHECKED IAW A MM 20-11-00-5, 20-11-00 AND 20-11-00-5. GOOD FOR SERVICE. 2 L 7 2 4F RT A1NM 2007081700004 20070817 00004 NM 2007 8 17 UPS07650391 1 20070801 A 2432 S282T0026 CHARGER BOEING 767 76734AF 1385212 NM MAIN BATTERY MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 320UP 27747 INSPECTION TYPE:ETOP EICAS MSG MAIN BATTERY CHARGER DISPLAYED. BATTERY DISCHARGE LIGHT DID NOT ILLUMINATE. SWAPPED APU BATTERY CHARGER WITH MAIN BATTERY CHARGER IAW 24-31-02-4 & 24-31-05-4. MAIN BATTERY CHARGER OPS NORMAL. 2 L 7 2 4F RT A1NM 2007081700008 20070817 00008 NM 2007 8 17 UPS07M50381 1 20070529 A 5320 STRUCTURE DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C CABIN T-CHORD AT STA 2007 LBL 53 FOUND CORRODED AS MARKED. CABIN T-CHORD REMOVED STA 2007 LBL 53 CORR OSION REMOVED & FOUND OUT OF LIMIT PER SRM 53-40-00 V1 R38. NEW T-CHORD FAB PER SRM 53-40-00 V1 R38 & DWG NJC6040. HOL ES P/UP ON FAB T-CHORD PER SRM 51-31-01 V2 R38. FAB T-CHORD ALODINE CARRIED OUT PER SRM 51-21-01V2 R38. NEW T-CHORD IN STALLED PER SRM 51-31-01V2 R38. 2 L 7 3 4F RT A22WE 2007081700015 20070817 00015 NM 2007 8 17 KCSA071279 1 20070806 A 5313 STRINGER BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 FUSELAGE STRINGER IS CRACKED IN RADIUS AT STR 27R, BETWEEN STA 460 TO 480. 2 L 7 4 4F RT A20WE 2007081700016 20070817 00016 NM 2007 8 17 UPS07M50386 1 20070706 A 5320 SHEAR WEB DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C CABIN - CORROSION ON UPPER & LWR SURFACE OF SHEAR WEB AT STA 1966 - 1996 L27 RT. SHEAR WEB CORROSION REMOVED PER SRM 53-00-01VI FIG 1AR38. WEB ORG THK 0.040" REMV 0.012" REMAIN 0.028" FOUND EXCEED LIMIT. NEW SHEAR WEB AGA7145-5 AND AGA7145-23 FAB USING MAT'L 7075-0-0.040" AS PER DOUGLAS DWG AGA 7145-503. NEW WEB INSTALLED PER SRM 51-3 1-01 VII R38. 2 L 7 3 4F RT A22WE 2007081700038 20070817 00038 EA 2007 8 17 MASA200700414 1 20070712 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17231 7231 ASH 2765 PHX. EMERGENCY PATH LIGHTING AT ROW 9 INOP. OPS CHECKED NORMAL. 2 L 7 2 4F RT A21EA 2007081700044 20070817 00044 NM 2007 8 17 MASA200700439 1 20070718 A 3350 SIGN DHAV DHC8 DHC8202 2809007 NM CABIN BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 989HA 427 ASH 2960 PHX. EXIT SIGN BROKEN RIGHT EMERGENCY EXIT ROW. MX REPLACED THE EXIT SIGN, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007081700049 20070817 00049 EU 2007 8 17 CPCP20070071 1 20070606 A 5313 STRINGER AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 447AM 447 CORROSION FOUND CHORD ANGLE AT RT STR 14 BETWEEN FRAME 13 AND 17 UPPER AND LOWER SURFACE. CORROSION FOUND CHORD ANGLE AT RT STR 14 BETWEEN FRAME 13 AND 17 UPPER AND LOWER SURFACE REPAIRED AS PER 53-31-50 FIGURE 402. 2 H 7 2 4T RT A53EU 2007081700050 20070817 00050 EU 2007 8 17 CPCP20070072 1 20070606 A 5210 STEP AEROSP ATR72 ATR72212 8680945 EU PAX DOOR CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 447AM 447 CORROSION FOUND ON ALL PAX DOOR STEPS UNDER NUTPLATES. CORROSION REMOVED ON ALL PAX DOOR STEPS UNDER NUTPLATE BY SRM 51 -10-10. 2 H 7 2 4T RT A53EU 2007081700075 20070817 00075 EA 2007 8 17 SWIA200718563 1 20070804 A 3230 LINE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA O OTHER K FLUID LOSS NR NOT REPORTED 1 NM 07 410SW 7066 HYDRAULIC SYSTEM NR 3 FLUID LEVEL IS 0%, FLIGHT NR 3763. REPLACED NOSE GEAR ACTUATOR AND PUMP 3B PRESSURE FLEXLINES IAW 32-33-01 AND 29-12-03. SERVICED NR 3 HYD SYSTEM. 2 L 7 2 4F RT A21EA 2007081700087 20070817 00087 EA 2007 8 17 MASA200700349 1 20070623 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37218 7218 ASH 7218 LAS. PILOT REPORTED THE EMERGENCY LIGHTS AFT OF ROW 8 WERE INOP. MX RESECURED THE CONNECTION TO THE FLOOR STR IP, OPS CHECK WAS GOOD. 2 L 7 2 4F RT A21EA 2007081700090 20070817 00090 NM 2007 8 17 KPVA200710 1 20070806 A 2760 406034 INDICATOR DHAV DHC8 DHC8103 1386005 NM COCKPIT FAULTY A KPVA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 13 806WP 357 (PIREP) PFCS INDICATOR GIVING REVERSE READING FOR INBOARD (L)SPOILER. (MX) REMOVE & REPLACED PFCS INDICATOR IAW DHC-8 M M CHAP 27-05-00 PG 201-206. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007081700093 20070817 00093 WP 2007 8 17 WRLA2007078 1 20070701 A 3230 SWITCH DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE COCKPIT LOCKED A WRLA O OTHER O OTHER DE DESCENT 1 SO 11 14075 46922 RME/BWI CENTER GEAR TOOK 30 SEC TO RETRACT DID NOT EXTEND NORMALLY, EMERGENCY EXTENSION RELEASED. GEAR EXTENDED IN APPR OXIMATLEY 15 SEC. FOUND CENTER GEAR SWITCH ON F/O PANEL LOCKED IN UP POSITION, RETURNED TO NORMAL. DEFLATED CENTER GEA R STRUT, CYCLED CENTER GEAR UP AND DOWN SEVERAL TIMES, ALL INDICATIONS NORMAL. SERVICED STRUT AND REMOVED PINS. 2 L 7 3 4F 4 F A22WE E23EA 2007081700107 20070817 00107 NM 2007 8 17 2007UALA02291 1 20070625 A 2910 251N12429 HYDRAULIC LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT AILERON BROKEN A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 507UA 24743 AILERON MOVEMENT ON EICAS DOESN'T MATCH MOVEMENTS FROM CONTROL WHEEL. TURNING WHEEL TO LEFT GETS STIFF FROM 3 TO 6 DEG. ON INSPECTION FOUND NUT -LOOSE HARDWARE- IN RT LATERAL CONTROL OVERRIDE QUADRANT. PART REMOVED. NO DAMAGE NOTED TO C ABLE OR QUADRANT. ADJUSTED TRIM ACTUATOR, LT AILERON O/B PCU HYDRAULIC PRESSURE LINE BROKEN NEAR PCU ATTACH. INSTALLED AILERON POWER CONTROL TUBE ASSY LINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081700112 20070817 00112 NM 2007 8 17 2007UALA02908 1 20070727 A 5210 HANDLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR STICKS A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 560UA 26660 FLT ATTENDANT STATED DOOR 4R DISARM HANDLE STICKS. FOUND DIRT AND GARBAGE IN GIRT BAR RETAINER. CLEANED AND LUBRICATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081700125 20070817 00125 EU 2007 8 17 CPCP20070081 1 20070529 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 429AT 429 FOUND FLOORBEAM AT FRAME 40 CORRODED. FLOORBEAM AT FRAME 40 REPAIRED AS PER SRM 53-00-00 FIG 435. 2 H 7 2 4T RT A53EU 2007081700138 20070817 00138 NM 2007 8 17 2007UALA03002 1 20070803 A 5210 DOOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD ENTRY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 FWD ENTRY DOOR HAS 2 EA HOLES WITH CRACK INDICATIONS ABOVE AND BELOW FWD END OF LOWER HINGE CUTOUT. REPAIRED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700143 20070817 00143 NM 2007 8 17 2007UALA03004 1 20070803 A 5313 STRINGER SPLICE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 FWD CABIN LT AT STR 15L SPLICE CHANNEL IS CRACKED AT LWR FLANGE AT BS 360. MAJOR REPAIR ACCOMPLISHED: REPLACED SPLICE CHANNEL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700151 20070817 00151 NM 2007 8 17 QXEA200701246 1 20070807 A 3620 8209074 SWITCH BOMBDR DHC8 DHC8402 1390042 NM NACELLE MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 431QX 4164 RNO FLIGHT NR 2444: NR 2 BLEED AIR CAUTION IS ON. DUCT TEMP WAS NORMAL. RAN CHECKLIST AND TURNED OFF NR 2 DUCT. CAUTI ON REMAINED ON AFTER LANDING AND SHUTDOWN. NO OTHER ABNORMAL INDICATIONS NOTED. MAINTENANCE REMOVED AND REPLACED NACEL LE DUCT LEAK OVERTEMP SWITCH IAW TASK 36-11-21-000-801 AND 36-11-21-400-801. OPS CHECK GOOD. NR 2 BLEED HOT CAUTION LI GHT REMAINS NORMALLY OFF. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007081700155 20070817 00155 NM 2007 8 17 C8GA20070008 1 20070807 A 3260 69499175 ROD BOEING 727 727223 1384074 NM DOWNLOCK SENSOR BROKEN A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 898AA 22014 FLT 723 FROM ROC TO TOL, AFTER TAKEOFF WHEN GEAR WAS RAISED THE RIGHT MAIN LANDING GEAR GREEN AND RED INDICATIONS LIGHTS REMAINED ON, SECONDARY RIGHT MAIN GEAR LIGHT ON FO'S PANEL REMAINED ON. ALL INDICATIONS WERE NORMAL WITH GEAR DOWN. A IRCRAFT RETURNED TO ROC AND LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE RIGHT MAIN LANDING GEAR D OWNLOCK SENSOR ROD WAS BROKEN. ROD WAS REMOVED AND REPLACED, OPS CHECKED GOOD AND NO FURTHER DEFECTS WERE NOTED. AIRCR AFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2007081700164 20070817 00164 WP 2007 8 17 07FDEA02805 1 20070808 A 2910 LINE DOUG MD10 MD1010F 3022112 WP HYD SYSTEM RUPTURED A FDEA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 569FE 47828 PDIS: AT ROTATION LOSS OF HYD "SYS 1", 0.0. FOUND INLET HOSE ON LOWER HYDRAULIC PUMP RUPTURED. NEEDS NEW HOSE, PUMPS, FILTERS. FOUND HYD LINE NR 1 ENGINE DRIVEN PUMP LINE RUPTURED, REPLACED LINE,BOTH ENG DRIVEN PUMPS, ALL RELATED FILTERS AND LEAK CHECKED PER MM 29-11-01, AND MM 29-11-02, OPS GOOD. 2 L 7 3 4F RT A22WE 2007081700178 20070817 00178 EA 2007 8 17 TRAX200701070 1 20070726 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 833AS 7246 LEFT FS 640 BONDED SKIN DOUBLER IS CRACKED AT WL 120, 1 INCH BELOW STRINGER 9L. COMPLIED WITH EC/TC REO 601R-53-61-506 ON LT BONDED SKIN DOUBLER, 1EA 409B ATTACHED TO DOCUMENT STEP SIGN OFFS. SUPPLEMENTAL - SDR CLOSED 08/07/07. 2 L 7 2 4F RT A21EA 2007081700189 20070817 00189 EA 2007 8 17 TRAX200701088 1 20070730 A 5532 SKIN CNDAIR CL600 CL6002B19 1900309 EA VERTICAL STAB CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 854AS 7382 CORROSION ON VERT STAB SKIN UNDER LT VOR ANTENNA. FOUND CORROSION TO BE WITHIN REPAIRABLE LIMITS IAW CRJ 200 SRM 55-00- 31. REMOVED CORROSION IAW CRJ 200 SRM 51-21-06. SUPPLEMENTAL - SDR CLOSED 08/07/07. 2 L 7 2 4F RT A21EA 2007081700207 20070817 00207 SO 2007 8 17 SIMA200722201 1 20070807 A 5100 NONE EMB 135 EMB135KL 3260302 SO NONE NONE A SIMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 812AE 145531 AFT EMERGENCY LIGHT FLOOR PROXIMITY STRIP INOPERATIVE. PERFORMED OPERATIONAL CHECK IAW EMB AMM WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007081700208 20070817 00208 NM 2007 8 17 KCSA071280 1 20070806 A 5313 STRINGER BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 FUSELAGE STRINGER IS CORRODED AT STA 880, STR 39L. 2 L 7 4 4F RT A20WE 2007081700211 20070817 00211 EU 2007 8 17 AWXA200700985 1 20070808 A 5320 D53475521001 SILL AIRBUS 320 A320231 3930325 EU ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 SAL - MAJOR REPAIR - C-06 CHECK - NR 5985617, CORROSION ON AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL CORNER SEALING, BS 2616/FR 56, S39R. REPLACED AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL CORNER SEALING, BS 2616/BS 56, S39R IAW A3 20 51-72-11. 2 L 7 2 4F RT A28NM 2007081700212 20070817 00212 NM 2007 8 17 HALA0700329 1 20070807 A 3350 LIGHT BOEING 767 7673CB 1385187 NM SEAT 20H INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 588HA 33466 FLOOR EMERGENCY LIGHTING INOP SEAT 20H TO AFT OF LAV D. REPLACED POWER STRIP AFT OF LAV D PER AMM 33-51-10, OPS CK GOOD . 2 L 7 2 4F RT A1NM 2007081700214 20070817 00214 2007 8 17 HALA0700328 4 20070807 A 3416 6224542103 RECEIVER BOEING 767 767332 1382001 NM INTERMITTENT A HALA K NONE J WARNING INDICATION DE DESCENT 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, CAPT "RA" FLAG IN VIEW INTERMITTENTLY. "NO LAND 3" ON AUTOLAND STATUS. RED CONFIGURATION AND MASTER WARNING ON DESCENT. REPLACED CAPTS R/A T/R. GND CHECK OK PER M/M 34-33-01-004-001 TEST 30 OK LMP REMAINS IN LA ND 3. 2 L 7 2 4F RT A1NM 2007081700217 20070817 00217 2007 8 17 MASA200700354 4 20070624 A 2300 FASTENER CNDAIR CL600 CL6002D24 1390016 EA E&E BAY BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 923FJ 15023 ASH 2827 PHX. MX FOUND A BROKEN ZIP-TIE ON A RADIO IN AVIONICS BAY. REMOVED IT AND ACFT CONTINUED OPERATIONS. 2 L 7 2 4F RT A21EA 2007081700218 20070817 00218 NE 2007 8 17 HALA0700331 2 20070809 A 7261 OIL SYSTEM BOEING 767 767300 1385204 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE LOW A HALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, ON ETOPS CHECK HAD TO SERVICE NR 1 ENG WITH 10 PINTS OF OIL. SERVICED NR 1 ENG WITH 10 PINTS OF OIL PER AMM 12-13-01-613-001-003. PERFORMED ENG GROUND TEST AT IDLE PER AMM 71-00-00-795-003-NDD. NO LEAKS NOTED. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007081700219 20070817 00219 EA 2007 8 17 MASA200700361 1 20070625 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 922FJ 15022 ASH 2612 ATL. ROW 17 EMERGENCY FLOOD LIGHT INOPERATIVE. RELAMPED FLOOD LIGHT. 2 L 7 2 4F RT A21EA 2007081700220 20070817 00220 NE 2007 8 17 HALA0700332 2 20070809 A 7261 OIL SYSTEM BOEING 767 767300 1385204 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE LOW A HALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, ON ETOPS CHECK HAD TO SERVICE NR 2 ENG WITH 6 PINTS OF OIL. SERVICED NR 2 ENG WITH 6 PINTS OF OIL PER AMM 12-13-01-613-001-003. PERFORMED ENG GROUND TEST AT IDLE PER AMM 71-00-00-795-003-N99. NO LEAKS NOTED. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007081700221 20070817 00221 SO 2007 8 17 MASA200700364 1 20070626 A 2560 SEAL EMB 145 EMB145LR 3260212 SO PBE FAILED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 ASH 7411 IAD. FWD CABIN PBE VACUUM SEAL FAIL. MX REMOVED AND REPLACED FORWARD CABIN PBE. 2 L 7 2 4T RT T00011AT 2007081700223 20070817 00223 WP 2007 8 17 07FDEA02819 1 20070810 A 5712 NRB6027 RIB DOUG DC10 DC1010 3022110 WP ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 LT WING L/E AT STA XOS 460 ON LOWER RIB AREA DOOR 513AB FOUND DEEP WEAR REPAIRED TEE IAW SRM 57-00-01 VOL I FIG 9. FABR ICATED PARTS IAW SRM 57-00-01 FIG 9 VOL 1. 2 L 7 3 4F A22WE 2007081700226 20070817 00226 NM 2007 8 17 07FDEA02823 1 20070810 A 5720 SUPPORT BOEING 727 727233 138408A NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 254FE 20936 LT WING AT T/E REAR SPAR AREA APROX RS STA 383 UPPER FIXED PANEL LOWER C CHANNEL BRACKET MOUNT SUPPORT HAS A CRACK AT FWD SECTION ABOVE NR 3 TRANS ASSY. REMOVED AND REPLACED C CHANNEL SUPPORT IAW SRM 51-30-2. C CHANNEL SUPPORT, FABRICAT ED ON TRAVELER NR T7/693316. 2 L 7 3 4F RT A3WE 2007081700227 20070817 00227 NM 2007 8 17 07FDEA02824 1 20070810 A 5730 PANEL BOEING 727 727233 138408A NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 254FE 20936 RT WING T/E LOWER HINGE PANEL 8506R INNER SURFACE HAS CORROSION AROUND EDGE REPAIRED IAW SRM 51-20-151-7. 2 L 7 3 4F RT A3WE 2007081700228 20070817 00228 NM 2007 8 17 07FDEA02826 1 20070810 A 5330 65545832 SKIN BOEING 727 727233 138408A NM ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 ON AGING A/C INSPECTION, FOUND EXISTING REPAIR AT STA 1070-1090, STR 25R-27R, DID NOT CONFORM TO SRM 53-30-03. REMOVED OLD REPAIR, FABRICATED AND INSTALLED NEW SKIN REPAIR FROM 2024-T3, .063 FILLER 2024-T3 .071" DOUBLER PER EA NR I070489 I R,THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007081700229 20070817 00229 2007 8 17 07FDEA02827 4 20070810 A 2565 24D3005371 SLIDE DOUG MD10 MD1010F 3022112 WP R1 DOOR FAILED A FDEA K NONE L NO TEST IN INSP/MAINT 1 SO 25 375FE 46613 AFTER LANDING AND BLOCK-IN, COULD NOT GET R1 DOOR ELECTRICAL SWITCH TO ENGAGE. R-1 DOOR OPENED PNEUMATICALLY, SLIDE DEP LOYED BUT DID NOT INFLATE. INSTALLED SLIDE/CONTAINER ASSY REF AMM CH 25-61-01-2 RII:445700. 2 L 7 3 4F RT A22WE 2007081700235 20070817 00235 EU 2007 8 17 SIMA200722503 1 20070812 A 6100 NONE SAAB SF340 340B 7860101 EU PROPELLER NONE A SIMA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SW 21 393AE 340B393 RIGHT PROPELLER VIBRATION, RETURNED TO DFW. PERFORMED DYNAMIC BALANCING OF THE RIGHT PROPELLER ASSEMBLY IAW SAAB AMM 61 -10-00. BALANCE LEVEL ACCEPTABLE AT 0.127 IPS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007081700237 20070817 00237 SO 2007 8 17 SIMA200722501 1 20070810 A 2730 14526259407 VALVE EMB 145 EMB145LR 3260212 SO ZONE 100 FAILED A SIMA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SW 21 619AE 18710 145101 VIBRATION IN FLIGHT CONTROLS FELT THROUGH ELEVATOR AND FUSELAGE. REMOVED AND REPLACED LEFT RAM VALVE IAW EMB AMM. OPER ATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007081700238 20070817 00238 WP 2007 8 17 NWAA072819917 1 20070807 A 5743 ATTACH ANGLE DOUG DC9 DC932 3022066 WP LT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 967N 47573 DURING "H" CHECK, FOUND CRACK IN LT TRAPEZOIDAL PANEL ATTACH ANGLE AT L20L. ANGLE HAS 11 HOLES FROM PREVIOUS TRAPEZOIDAL PANEL REPAIR. CRACK WAS DISCOVERED BEYOND THE 11TH HOLE. REPAIRED PER EA 99-210170. 2 L 7 2 4F A6WE 2007081700240 20070817 00240 NM 2007 8 17 QXEA200701276 1 20070811 A 2120 UNKNOWN DHAV DHC8 DHC8202 2809007 NM CABIN ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 368PH 512 PDX - EVIL, FOUL FISH ODOR EMINATING FROM AFT CABIN AREA. MAINTNEANCE COULD NOT DUPLICATE DISCREPANCY. NO PARTS REPLAC ED. AIRCRAFT RETURNED TO SREVICE. 2 H 7 2 4T RT A13NM 2007081700241 20070817 00241 2007 8 17 QXEA200701277 4 20070812 A 3420 7003360941 AHRS DHAV DHC8 DHC8202 2809007 NM NR 2 MALFUNCTIONED A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 347PH 19554 124 480 PDX FLIGHT NR 2159, NR 2 AHRS FAILURE. REPLACED NR 2 AHAS. PERFORMED OPERATIONAL TEST OF NR 2 AHRS IAW MTX 8340019. A LL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007081700247 20070817 00247 2007 8 17 MASA200700369 4 20070627 A 2561 LIFE VEST CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 646BR 7392 ASH 1027 HNL. INFANT LIFE VEST WAS MISSING. MX INSTALLED A NEW LIFE VEST. 2 L 7 2 4F RT A21EA 2007081700248 20070817 00248 EA 2007 8 17 MASA200700386 1 20070629 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37228 7228 ASH 2818 PHX. MX REPORTED THE RIGHT FORWARD OVERWING EMERGENCY LIGHT WAS INOP. MX RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2007081700250 20070817 00250 SO 2007 8 17 MASA200700387 1 20070629 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 ASH 7372 CHS. EMERGENCY EXIT ROW 12 LT INOP. CYCLED SWITCH. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007081700252 20070817 00252 NE 2007 8 17 MASA200700390 2 20070703 A 7532 311669101 BLEED VALVE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 1 ENGINE MALFUNCTIONED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 434YV 10606 434 ASH 7086 DEN. SMOKE IN COCKPIT AFTER NR 1 ENGINE START. MX REMOVED AND REPLACED NR 1 IBV AND P2.5 AND 3 AIR SWITCHING VALVE OPS CHECKED GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2007081700256 20070817 00256 NM 2007 8 17 MWEA070174 1 20070810 A 7830 7150922 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 919ME 55181 RIGHT THRUST REVERSER UPPER BUCKET ZEE FRAME AT STATION 26 IS CRACKED. FABRICATED AND INSTALLED SPLICE ANGLE. 2 L 7 2 4F TR A6WE 2007081700258 20070817 00258 NM 2007 8 17 MWEA070176 1 20070810 A 7830 7150923 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 919ME 55181 RIGHT THRUST REVERSER UPPER BUCKET ZEE FRAME AT STATION 26 IS CRACKED AT INBOARD SIDE. FABRICATED AND INSTALLED SPLICE ANGLE. 2 L 7 2 4F TR A6WE 2007081700260 20070817 00260 NM 2007 8 17 MWEA070178 1 20070814 A 7830 7150922505 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 914ME 55177 UPPER THRUST REVERSER DEFLECTOR DOOR HAS A CRACK IN ZEE FRAME AT OUTBOARD END IN RADIUS AT STATION 26.666 APPROXIMATELY .125 INCH LENGHT. 2 L 7 2 4F TR A6WE 2007081700261 20070817 00261 NM 2007 8 17 07FDEA02793 1 20070808 A 2497 WIRE DOUG MD11 MD11F 3023600 NM DAMAGED A FDEA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SO 25 582FE 48420 PASSING FL 270 ON CLIMB A/P TRIPPED OFF FOLLOWED BY MULTIPLE OTHER ALERTS. ENGINE NR 3 FLAMED OUT WITH "0" FUEL FLOW. FOLLOWED CHECKLIST FOR RESTART WITH NO SUCCESS. TANK NR 3 PUMPS WERE UNPOWERED. ENG NR 3 WAS SUCTION FEEDING. ATTEM PTED RESTART WITH FUEL SYSTEM IN MANUAL AND CROSSFEEDING TO NR 3 WITH NO SUCCESS, BATTERY BUSS T/R2A AND GS BUSSES WERE UNPOWERED. LATERAL FUEL IMBALANCE OCCURRED. ACCOMPLISHED EA 1-2400-114788 PART-1 AS FOLLOW INSTRUCTIONS, REPAIRED DAMA GED WIRES. REMOVED AND REPLACED ASSOCIATED COMPONENTS AND R-T-S RELATED SYSTEMS. A/C OK FOR CONTINUE SERVICE. 2 L 7 3 4F RT A22WE 2007081700263 20070817 00263 NM 2007 8 17 MWEA070168 1 20070810 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 909ME 55173 RIGHT THRUST REVERSER CRACKED AT UPPER OUTBOARD STATION 26. FABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007081700264 20070817 00264 NM 2007 8 17 MWEA070169 1 20070810 A 7830 7150923REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 909ME 55173 RIGHT THRUST REVERSER OUTBOARD FRAME CRACKED AT STATION 35. FABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007081700268 20070817 00268 NM 2007 8 17 07FDEA02820 1 20070810 A 3150 UNKNOWN BOEING 727 727233 138408A NM UNKNOWN A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 268FE 21674 AFT AIRSTAIR LIGHT ILLUMINATED DURING CRUISE FLIGHT AT FL 350 NEGLIGIBLE TURBULENCE. REPEAT WRITE-UP. RELEASED FOR SERV ICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 20AUG07 "MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP. VE RIFY AFT AIRSTAIR IS CLOSED LOWER AFT AIRSTAIR CONTROL STATION RED LIGHT OUT. 2 L 7 3 4F RT A3WE 2007081700269 20070817 00269 NM 2007 8 17 07FDEA02825 1 20070810 A 5414 311N504651 SKIN BOEING 757 7572B7 1384964 NM NR 1 NACELLE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 NUMBER ONE STRUT/PYLON, LT SIDE SKIN, AT APPROXIMATE NAC STA 144, INTERNAL, IS CORRODED ON SKIN AND UNDER LOWER FRAME/CH ORD. REMOVED CORROSION IAW SRM 54-50-01. ORIGINAL MATERIAL THICKNESS WAS .090", AFTER REWORK REMAINING MATERIAL THICKN ESS WAS .079", OUT OF LIMITS IAW SRM 54-50-01. REPLACED NUMBER ONE STRUT/PYLON LT SIDE SKIN ASSY, P/N 311N5046-51, IAW SRM 51-40-02 AND DRAWING 311N5002, SHEET 13, REV E. 2 L 7 2 4F RT A2NM 2007081700272 20070817 00272 NM 2007 8 17 2007UALA03027 1 20070804 A 3040 CONTROLLER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU WINDSHIELD HEAT FAILED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 325UA 23957 CREW REPORT: F/O'S SLIDING WINDOW ARCING SMOKING & GLASS SPIDER WEB CRACKING. C/B`S DID NOT POP HAD TO REMOVE ELEC POW ER WITH WINDOW HEAT SWITCHES. FOUND WINDOW HEAT CONTROLLER FAILURE. REPLACED FO'S SLIDING WINDOW AND ASSOCIATED WINDOW HEAT CONTROLLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700278 20070817 00278 EU 2007 8 17 2007UALA02992 1 20070804 A 2621 FIRE BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE APU DISCHARGED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 419UA 487 APU FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED ON OVERHEAD PANEL. 09-07-07 INADVERTANT DISCHARGE ON APU FIRE BOTTLE CA USED INDICATION. REPLACED FIRE BOTTLE AND SQUIB, RESET INDICATION. 2 L 7 2 4F 4 F RT A28NM E40NE 2007081700279 20070817 00279 NM 2007 8 17 2007UALA03017 1 20070805 A 3260 WARNING LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT ILLUMINATED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 503UA 24624 EICAS MESSAGE -GEAR DOORS & GEAR DISAGREE- DISPLAYED WITH GEAR HANDLE UP. DOORS & GEAR AMBER LIGHTS ILLUMINATED. GE AR MOVEMENT WAS SO SLOW THAT EICAS MESSAGES "GEAR DOORS AND GEAR DISAGREE" WERE DISPLAYED DURING GEAR RETRACTION. ALL G EAR INDICATION "GREEN" WHEN GEAR FULLY RETRACTED. FOUND FOD IN FILTER FOR EDP. REPLACED NR 1 EDP AND FILTERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081700281 20070817 00281 NM 2007 8 17 2007UALA03019 1 20070802 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 597UA 28750 DOOR 1R WILL NOT ARM. CYCLED DOOR. REMOVED FOREIGN MATERIAL FROM DOORWAY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081700282 20070817 00282 2007 8 17 2007UALA03020 4 20070802 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR SEPARATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 597UA 28750 FOUND DOOR 1L SLIDE APRON SEPARATED FROM SLIDE LOWER ATTACH POINT. PINNED SLIDE AND DOOR ASSIST BOTTLE. REMOVED SLI DE ASSEMBLY IN TO GALLEY AREA FOR REPLACEMENT. REPLACED DOOR 1L SLIDE AND SLIDE ATTACHMENT HARNESS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081700286 20070817 00286 NM 2007 8 17 2007UALA03024 1 20070805 A 5754 DOUBLER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L/E SLAT PEELING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 NR 5 LEADING EDGE SLAT TRAILING EDGE WEDGE, UNDER SIDE HAS OLD HOT BOND METAL PATCH PEELING OFF. PATCH IS 4 X 4 INCH. PATCH IS JUST INBOARD OF SLAT ACT ON UNDER SIDE OF SLAT. DELAM IS LOCATED 59 INCHES FROM INBOARD EDGE OF NR 5 SLAT ON T HE TRAILING EDGE WEDGE INSIDE SURFACE. NR 5 SLAT REMOVED AND REPAIRED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700287 20070817 00287 NM 2007 8 17 2007UALA03025 1 20070805 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 671UA 30026 SEAT 4HJ EMERGENCY LIGHT STRIP ON SIDE OF SEAT FALLS OFF. 08-31-07 REPLACED EEL STRIP AT 4HJ. OP CHECKD EEL SYSTEM. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007081700289 20070817 00289 NM 2007 8 17 2007UALA02979 1 20070803 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 DOOR SILL EMERGENCY LIGHT INOP 5R AFT. RELAMPED DOOR SILL EEL. OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007081700290 20070817 00290 NM 2007 8 17 2007UALA02980 1 20070803 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY LIGHT INOPERATIVE 53 ABC. REPLACED CABLE. OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007081700291 20070817 00291 2007 8 17 2007UALA02981 4 20070803 A 2565 PUSHROD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR GIRT BAR FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 DOOR 1R: DIFFICULT TO ARM, TOOK NUMEROUS ATTEMPTS BEFORE IT ARMED. SAMC TEXT: ARM LT INTERMITTENT IN FLT. ADJUSTED GIRT BAR PUSH ROD 2 L 7 2 4F 4 F RT A2NM E17NE 2007081700293 20070817 00293 NM 2007 8 17 2007UALA02983 1 20070802 A 3350 SIGN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 534UA 25129 EEL EXIT SIGN INOP AT SEAT 15A. REPLACED SIGN. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081700294 20070817 00294 NM 2007 8 17 2007UALA02984 1 20070802 A 2750 INDICATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT SPLIT A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 576UA 26690 FLAP INDICATORS ARE SPLIT. SPLIT IN MOTION AND AT 1-5-15. RT FLAP INDICATION NEEDLE LAG BEHIND ONE NEEDLE WIDTH. REPL ACED FLAP POSITION INDICATOR / TRANSMITTER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081700295 20070817 00295 2007 8 17 2007UALA02985 4 20070802 A 2565 CYLINDER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE INADEQUATE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 RIGHT OVERWING SLIDE INFLATION CYLINDER IS INADEQUATE. REPLACED SLIDE INFLATION CYLINDER TO ACCOMPLISH COA 616942. A LSO FOUND COLLAPSED INFLATION HOSE DUE TO HYD FLUID CONTAMINATION. CHECKED OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007081700297 20070817 00297 NM 2007 8 17 2007UALA02987 1 20070802 A 3510 TRANSDUCER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE O2 SYSTEM READS LOW A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 779UA 26941 O2 PRESSURE TRANSDUCER READS 300 PSI TO LOW. REPLACED TRANSDUCER. READINGS NOW IN CORRECT RANGE. AIRCRAFT OK FOR S ERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007081700298 20070817 00298 EU 2007 8 17 2007UALA02988 1 20070731 A 2160 CONDENSER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 A/C PACK MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C CL CLIMB 1 WP 29 460UA 1248 COCKPIT TEMPERATURE DIFFICULT TO CONTROL. 09-07-07 NR 2 PACK CONDENSOR CRACKED, 2 OTHER AREAS OF PNEUMATIC LEAKS. RE PLACED NR 2 PACK CONDENSOR AND REPAIRED ALL PNEUMATIC LEAKS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007081700300 20070817 00300 NM 2007 8 17 SWAA074014 1 20070812 A 3350 MS155721 LIGHT BOEING 737 7373T5 1384608 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007081700301 20070817 00301 NM 2007 8 17 SWAA074039 1 20070814 A 3350 417N5101007 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 734SA 27866 DURING SCHEDULED 8Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007081700303 20070817 00303 2007 8 17 SWAA074040 4 20070814 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 734SA 27866 DURING SCHEDULED 8Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007081700310 20070817 00310 NM 2007 8 17 2007UALA02912 1 20070727 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EEL CROSSAISLE STRIP INOP 5R. FOUND LOOSE CONNECTION IN FEEDER. RESECURED FEEDER CABLE. CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007081700313 20070817 00313 NM 2007 8 17 2007UALA02915 1 20070730 A 3510 HARNESS AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT LEAKING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 832UA 1321 F/O'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). REPLACED CREW O2 HARNESS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007081700315 20070817 00315 NM 2007 8 17 SWAA074013 1 20070812 A 3350 MS155721 LIGHT BOEING 737 7373T5 1384608 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007081700316 20070817 00316 NM 2007 8 17 SWAA074012 1 20070812 A 3350 MS155721 LIGHT BOEING 737 7373T5 1384608 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007081700317 20070817 00317 NM 2007 8 17 SWAA074011 1 20070811 A 3350 MS155721 LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007081700318 20070817 00318 NM 2007 8 17 SWAA074015 1 20070812 A 3350 MS155721 LIGHT BOEING 737 7373T5 1384608 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007081700321 20070817 00321 NM 2007 8 17 SWAA073974 1 20070809 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 748SW 29800 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, BETWEEN RBL 29 AND LBL 41. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007081700323 20070817 00323 NM 2007 8 17 HALA0700334 1 20070812 A 5100 NONE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE NONE NONE A HALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 13 480HA 55125 ATB AFTER ROTATION AND DURING CLIMB-OUT TOWER REPORTED VAPOR TRAILING FROM LEFT SIDE OF AIRCRAFT. RETURNED FOR NORMAL L ANDING. DE-BRIEFED CREW AND THEY REPORTED NO ENG ABNORMALITIES. PERFORMED ENG EXCEED BITE PER FIM 71-00 TASK 801, NO E XCEEDANCE NOTED. PERFORMED PNEUMATIC SYSTEM BITE PER FIM 36-10 TASK 801. PERFORMED CABIN PRESS CONT SYS BITE PER FIM 2 1-30 TASK 801, NO FAULTS FOUND. PERFORMED ENG IDLE RUN AND LEAK CHECK PER AMM 71-00-11. NO LEAK NOTED, ALL PARAMETERS NORMAL VISUALLY CHECKED FOR HYD LEAKS NONE NOTED. HYD QTY GOOD. VISUALLY CHECKED FOR FUEL LEAKS, NONE NOTED VISUALLY C HECKED APU FOR LEAKS, NONE NOTED ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007081700324 20070817 00324 NM 2007 8 17 HALA0700335 1 20070811 A 2410 ADAPTER BOEING 767 767300 1385204 NM PWA 4060 PW4060 52119 NE RT IDG NOT CLOSED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, FOUND RT IDG PRESSURE ADAPTER WOULD NOT CLOSE AFTER SERVICING IDG. REPLACED PRESSURE ADAPTER LEAK CKS GOOD SERVICED IDG PER OVERNIGHT CHECK INSTRUCTIONS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082000001 20070820 00001 NM 2007 8 20 07FDEA02833 1 20070811 A 2910 SHUTOFF VALVE DOUG MD11 MD11F 3023600 NM HYD SYSTEM MALFUNCTIONED A FDEA J A DUMP FUEL UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 596FE 48554 LOSS OF HYD SYS 3, COMPLETED QRH EMERGENCY PROCEDURES. RETURNED TO ANC. RESEALED PRIMARY TRIM CONTROL SOLENOID OPERATE D SHUT-OFF VALVE. REF MM 27-43-41-4. OPS AND LK CK GOOD. 2 L 7 3 4F RT A22WE 2007082000002 20070820 00002 EU 2007 8 20 07FDEA02834 1 20070812 A 2120 UNKNOWN AIRBUS 310 A310304 3930339 EU CABIN ODOR A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 816FD 593 AFTER LIFT-OFF ACRID SMOKE ODOR AND EYES HAD BURNING SENSATION. LEVEL OFF AT 10,000 FT. NO CLEARING. OPENED RAM AIR ON DESCENT TO CLEAR AIR. SHUT OFF NR 2 PACK AS IT HAD A HIGH TEMP 55 DEG C. NO OTHER WARNINGS. REPLACED CHECK VALVES 291394,293388,291388,292388. CLEANED AND BLEW OUT BLEED AIR PRESSURE LINE STARTING AT 14TH STAGE RESTRICTOR 291392 END ING AT CHECK VALVE 291378 PERFORMED POWER ASSURANCE CHECK PER JRH. RAN NR 1 PACK FULL HOT/FULL COLD DURING POWER ASSU RANCE CHECK WITH NUMBER ONE ENGINE BLEED. UPON RETURN TO THE GATE, FOUND ONLY MOISTURE IN FILTER 291376, REF MM 29-14-0 0-0. CHANGED FILTER PER 29-14-00-0. NO HYDRAULIC FLUID ODOR IN CABIN/COCKPIT DURING RUN. 2 L 7 2 4F RT A35EU 2007082000003 20070820 00003 EU 2007 8 20 07FDEA02835 1 20070813 A 5330 A53773485 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 STRUCTURE DAMAGE IN LOWER SKIN C25, P44-46 LT SKIN AND STRINGER REPAIR PERFORMED IAW SRM 53-10-12 FIG 229 AND 53-10-14 . 2 L 7 2 4F RT A35EU 2007082000004 20070820 00004 EU 2007 8 20 07FDEA02836 1 20070813 A 5730 A57661001174 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND OLD REPAIR ON LT AILERON , LOWER SKIN TRAILING EDGE WITH SIGN OF DELAMINATION. REPAIR RENEWED IAW SRM 517712 PB 2 01, PARA 4. 2 L 7 2 4F RT A35EU 2007082000007 20070820 00007 EU 2007 8 20 07FDEA02840 1 20070813 A 5415 A54611024003 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 PYLON NR 2 LOWER FITTING CORROSION IN BEARING HOLE REPAIR PERFORMED BY SB A300-54-6018, APPROVED BY EA 6-5451-106505. 2 L 7 2 4F RT A35EU 2007082000009 20070820 00009 EU 2007 8 20 07FDEA02842 1 20070813 A 5754 A57864200168 SKIN AIRBUS 300 A300B4605R 3930308 EU NR 2 SLAT CHAFED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 732FD 713 SLAT NR 2 LT WITH CHAFING MARKS ON UPPER SKIN AT NOSE SECTION. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS IAW EA 6 -5743-112493 AND RAS/FOK/177/2007 ISS A . 2 L 7 2 4F RT A35EU 2007082000010 20070820 00010 EU 2007 8 20 07FDEA02843 1 20070813 A 5312 A53989334316 DOUBLER AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 DOUBLER CRACKED AT FIRE WALL C95 REPAIR PERFORMED BY DOUBLER INSTALLATION, APPROVED BY EA 6-5319-112476 AND RAS/DATLS/00 03777/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082000014 20070820 00014 EU 2007 8 20 07FDEA02848 1 20070813 A 5320 A53771417206 SILL AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 CORROSION SPOTS ON SILL BEAM C20 AND C25A REPAIR PERFORMED BY BLEND OUT THE CORROSION AND INSTALL A BUSH IN C 20 AND A M ACHINED ANGLE IN C25 A IAW EA 6-5313-106503 AND RAS/DABRE/7007983/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082000017 20070820 00017 NM 2007 8 20 07FDEA02851 1 20070813 A 5347 6519602 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 UPPER DECK STA 1110-1122 LBL 1 WL 208 CENTER SEAT TRACK FLANGE HAS AREAS OF CORROSION REMOVED CORROSION FROM SEAT TRAC K AND FOUND TO BE OUT OF LIMITS ORIGINAL FLANGE WAS .100 THICKNESS AFTER REMOVAL .053 LEFT SO REMOVED SEAT TRACK FABRICA TED NEW SEAT TRACK OUT OF MATERIAL 1520-792 AND REINSTALLED NEW SEAT TRACK AND INSTALLED ANGLES TO WEB AND TRACK, REF SR M'S 51-10-2, 51-10-6, 51-30-2, 51-10-5, 53-10-1, 53-10-2. 2 L 7 3 4F RT A3WE 2007082000018 20070820 00018 NM 2007 8 20 07FDEA02852 1 20070813 A 5347 53FX939 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 MAIN CABIN FLOOR, SEAT TRACK UPPER FLANGE SPLICE DOUBLERS, BOTH CRACKED IN HALF, BS : 1130, RBL 1 AND LBL: 1 REMOVED CRA CKED DOUBLERS AND FABRICATED NEW DOUBLERS AND INSTALLED REF 53FX939, 51-30-2. 2 L 7 3 4F RT A3WE 2007082000021 20070820 00021 NM 2007 8 20 07FDEA02855 1 20070813 A 5340 6545313Y14 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 PASSENGER CABIN STA 950C STR 9R, STRINGER CLIP CRACKED. REPLACED STRINGER CLIP STA 950C STR 9R REF SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007082000022 20070820 00022 EU 2007 8 20 07FDEA02856 1 20070813 A 5712 A57240810214 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 749FD 536 CORROSION FOUND ON LT MLG RIB 5 FWD LUG REPAIR PERFORMED BY OVERSIZING THE BORE AND CORROSION REMOVAL IAW DRAWING R572-4 0221, APPROVED BY EA 6-5751-112446 AND RAS/BAE/100519/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082000023 20070820 00023 NM 2007 8 20 07FDEA02857 1 20070813 A 5320 6519604 WEB BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 MAIN DECK FLOOR SHEAR WEB CORRODED STA 1148-1153 RBL 35-38 WL 208 CORROSION REMOVAL RESULTED IN OUT OF LIMITS MATERIAL L OSS. REMOVED DAMAGED PORTION OF WEB. MFG DOUBLER/FILLER REF SRM 51-40-2 INSTALLED REPAIR PARTS AND RIVETS WET. 2 L 7 3 4F RT A3WE 2007082000024 20070820 00024 EU 2007 8 20 07FDEA02859 1 20070813 A 5340 A5377364420600 FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 FRAME FITTING C38.1 IS CRACKED AND CORRODED AT LBL 60 IN FWD PIT UNDER T-CAP REMOVED AND REPLACED FITTING IAW A310-200 S RM 51-40-21 PARA 5-7 PO NR 583026.8. 2 L 7 2 4F RT A35EU 2007082000025 20070820 00025 EU 2007 8 20 07FDEA02860 1 20070813 A 5313 A53974202216 STRINGER AIRBUS 310 A310203 3930313 EU AFT PIT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 ALC STR 49L CORRODED BETWEEN FR 58 AND FR 60 REPLACED STRINGER 49L BETWEEN FRAME 58 AND 60 IN AFT PIT IAW A310-200 SRM 5 3-10-14, FIG 201 PG 203/204. 2 L 7 2 4F RT A35EU 2007082000027 20070820 00027 CE 2007 8 20 DXTA200702373 1 20070801 A 4920 APU CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 920QS 7500120 WHILE RUNNING APU ON THE GROUND WITH COCKPIT PAC ON HIGH GOT SMOKE IN COCKPIT. COCKPIT PAC SUPPLY TEMP ROSE RAPIDLY. COC KPIT PAC OIL RESEVOIR WAS CLEAR ON PREFLIGHT NOW BLACK. REPLACED COCKPIT PAC ACM & COALESCER SOCK OPS CK GOOD REF CE75 0 M/M 21-51-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007081600118 20070816 00118 NM 2007 8 16 AALA20071404 1 20070804 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AA 24488 SEA - EMERGENCY LIGHT AT SEAT 9D HAS BROKEN RED LENS. REPLACED RED LENS FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007081600129 20070816 00129 NM 2007 8 16 AWXA200700968 1 20070706 A 5320 65557572 STIFFENER BOEING 737 7373G7 1384595 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5962210, CORROSION ON STIFFENER, BS 271, RBL 60, WL 271. REPLACED STIFFENER, BS 27 1, RBL 60, WL 271 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007081600131 20070816 00131 NM 2007 8 16 AWXA200700970 1 20070705 A 5311 6546541504 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961307, CRACKED FRAME WEB/UPPER RING, BS 663.75, S2L. REPAIRED FRAME WEB/UPPER RI NG, BS 663.75, S3L - S3R IAW B737-300 SRM 53-00-07-2R9 FIGURE 201. 2 L 7 2 4F RT A16WE 2007081600132 20070816 00132 NM 2007 8 16 DHL2007741529 1 20070806 A 5343 651986310 STIFFENER BOEING 727 7272Q9 138448M NM BS 312 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 NOSE LANDING GEAR RT TRUNNION AFT STIFFENER CORRODED OUT OF LIMITS. LOCATED AND DRILLED NEW STIFFENER, TREATED, PRIMED, AND INSTALLED NEW STIFFENER PER B727 SRM 51-10-2, 51-30-5, AND 51-30-2. 2 L 7 3 4F RT A3WE 2007081600133 20070816 00133 NM 2007 8 16 DHL2007741530 1 20070804 A 5330 SKIN BOEING 727 7272Q9 138448M NM BS 1346 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 NR 2 ENGINE SUPPORT STRUCTURE SKIN HAS A DENT AT BS 1346, BETWEEN STR 9L AND 10L. REMOVED PREVIOUS REPAIR DOUBLER ADJAC ENT TO DENT. CUT OUT DAMAGED AREA'S, 2 EA, 1.5" BY 1" AND 1" BY .625", FABRICATED 1 REPAIR DOUBLER FROM 2024-T3, .063" BY 28" BY 10.25", PO NR 9005314, PER B727 SRM 54-30-3 FIG 7 AND 54-30-2 FIG 4. TREATED, PRIMED, AND INSTALLED REPAIR DO UBLER PER B727 SRM 51-10-2 AND 54-30-3 FIG 7. 2 L 7 3 4F RT A3WE 2007081600138 20070816 00138 EU 2007 8 16 CPCP20070061 1 20070606 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 447AM 447 CORROSION FOUND ON RT SEAT TRACK BETWEEN FRAME 36-39. RT SEAT TRACK BETWEEN FRAME 36-39. REPLACED AS PER SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007081600151 20070816 00151 NM 2007 8 16 DLM90071014 1 20070802 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 530 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 RT CUSP WEB CORRODED OUT OF LIMITS O/B EDGE FS 530. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW MD-80 53-05D. 2 L 7 2 4F RT A6WE 2007081600156 20070816 00156 NM 2007 8 16 DL76L071021 1 20070802 A 2820 POPPET VALVE BOEING 767 767332 1382001 NM FUEL SYSTEM FAILED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 195DN 28452 FUEL LEAK LEFT MIDWING, RTB. FOUND LEFT WING SURGE PRESS RELIEF VALVE LEAKING FUEL. REPLACED TANK PLATE/SURGE POPPET V ALVE ASSY ADDED FUEL LEAK CHECKS OK. 2 L 7 2 4F RT A1NM 2007081600166 20070816 00166 NM 2007 8 16 DLM88071037 1 20070807 A 2910 AE7055381 HOSE DOUG MD88 MD88 3023688 NM HYD SYSTEM LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 944DL 49817 FLT 456 ATL-DCA DIVERTING TO IAD DUE TO RT SYSTEM HYD QTY LOSS AT CRUISE. RT SYSTEM QTY DECREASING AT CRUISE FL 330 AT APPROX 2 QUARTS QTY NOTICED RT SYSTEM PRESSURE DECREASING AS WELL. SHUTDOWN RT SYSTEM HYD PER NNC.13.12 AND REVIEWED PR OCEDURES. DUE TO POSSIBILITY OF ALT GEAR EXTENSION THE CREW HAS ELECTED TO DECLARE AN EMERGENCY AND DIVERT TO IAD FROM DCA. MTC FOUND HOSE ASSY AE705537-1 IPC 29-10-00-11B ITEM 30 ENG DRIVEN HYD PUMP PRESSURE LINE BROKEN. REPLACED LINE A ND SERVICED HYD SYSTEM CLEANED RESIDUE. A/C OK FOR SERVICE. 2 L 7 2 4F RT A6WE 2007081600167 20070816 00167 NM 2007 8 16 DLM88071038 1 20070807 A 5343 9911585509 FITTING DOUG MD88 MD88 3023688 NM NLG SUPPORT BENT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DE 53416 NLG SUPPORT BEAM FITTING BENT AND WHEELWELL WEB CRACKED. REPLACED SUPPORT BEAM FITTING AND REPAIRED WEB. 2 L 7 2 4F RT A6WE 2007081600178 20070816 00178 SO 2007 8 16 SIMA200722002 1 20070806 A 3230 355022002 CONTROL UNIT EMB 135 EMB135KL 3260302 SO MLG FAILED A SIMA O OTHER J WARNING INDICATION CL CLIMB 1 SW 21 848AE 10943 145710 ON TAKEOFF WHEN GEAR HANDLE WAS MOVED UP DID NOT GET RIGHT MAIN GEAR IN TRANSIENT INDICATION. REMOVED AND REPLACED LAND ING GEAR ELECTRONIC UNIT IAW EMB AMM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007081700019 20070817 00019 NM 2007 8 17 ASAA0741929 1 20070719 A 5320 65785041 ATTACH ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 INTERCOSTAL O/B FLANGE ATTACHMENT ANGLE CRACKED. INTERCOSTAL ATTACHMENT ANGLE REPAIRED IAW ERO 6993 AND EA 5310 02729. REPAIR TO BE INSPECTED PER ASA DWG A 5310023893 EVERY 6000 FLT CYCLES. 2 L 7 2 4F RT A16WE 2007081700024 20070817 00024 SO 2007 8 17 MASA200700455 1 20070726 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 860MJ 10444 145773 ASH 7407 IAD - CABIN EMERGENCY LIGHTS INOP. MX REMOVED AND REPLACED CABIN EMERGENCY BATTERIES. OPS GOOD. 2 L 7 2 4T RT T00011AT 2007081700034 20070817 00034 EA 2007 8 17 MASA200700407 1 20070710 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DEFECTIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 75995 7361 ASH RON IAD. MX REPORTED THAT THE EMERGENCY FLOOR LIGHTS ROW 2-5 WERE INOP. REPLACED CONNECTOR DS13LY, OP CHECK WAS GO OD. 2 L 7 2 4F RT A21EA 2007081700037 20070817 00037 EA 2007 8 17 MASA200700415 1 20070712 A 3397 CONNECTOR CNDAIR CL600 CL6002D24 1390016 EA CABIN LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 928LR 15028 ASH 2695 CLT. EMERGENCY CEILING FLOOD LIGHT INOP. SECURED LOOSE CONNECTOR. 2 L 7 2 4F RT A21EA 2007081700042 20070817 00042 EA 2007 8 17 MASA200700432 1 20070717 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 97325 7325 ASH 2903 PHX. FORWARD EMERGENCY FLOOR LIGHTS INOP. MX RE-SECURED LIGHT TRACK. 2 L 7 2 4F RT A21EA 2007081700043 20070817 00043 EA 2007 8 17 MASA200700434 1 20070717 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27318 7318 ASH 2709 PHX. OVERWING EXIT EMERGENCY LIGHT CENTER BULB, BURNED OUT. MX RELAMPED CENTER BULB. 2 L 7 2 4F RT A21EA 2007081700062 20070817 00062 WP 2007 8 17 07FDEA02796 1 20070808 A 5347 54929405 SEAT TRACK DOUG MD10 MD1010F 3022112 WP BS 700-815 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 BROKEN SCALLOPS ON CABIN SEAT TRACK AT STA 755 REMOVED FLOOR PANEL IAW DC10/MD10 SRM 51-31-01 VOL 2 PGS 1-5. REMOVED SE AT TRACK AT STA 700-760 LBL 47.5 IAW DC10/MD10 SRM 51-31-01 VOL 2 PG 1-5, MAT ID 54929405 AND PO NR 570769.5 FOR SEAT TR ACK IAW DC10/MD10 SRM 53-42-01 VOL 3. FABRICATED AND INSTALLED SEAT TRACK IAW FEDEX DC10/MD10 SRM 53-70-00 VOL 1 PG 21- 22. FABRICATED SPLICE AND SPLICE PLATE AND INSTALLED IAW FEDEX DC10/MD10 SRM 53-70-00 VOL1 PG 3 AND 4. ALODINED AND PR IMED IAW FEDEX DC10/MD10 SRM 51-21-01 VOL 2 PG 25 AND 21. INSTALLED FLOOR PANEL IAW FEDEX DC10/MD10 SRM 51-30-01, MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2007081700069 20070817 00069 SO 2007 8 17 SWIA200718557 1 20070730 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY EXIT BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 301YV 120301 EXIT ROW "EXIT" SIGN BROKEN AT ROW 6, FLIGHT NR 5471. REPLACED EXIT SIGN WITH A SERVICEABLE UNIT. OPS TEST GOOD, P/N: 10-1262-1. 2 L 7 2 4T RT A31SO 2007081700072 20070817 00072 EA 2007 8 17 SWIA200718560 1 20070806 A 3230 BYPASS VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 924SW 7681 NOSE GEAR DISAGREE WARNING ON EXTENSION, FLIGHT NR 5827. REPLACED NOSE GEAR BYPASS VALVE IAW AMM 32-34-35. LEAK CHECK GOOD. OPS CHECK GOOD, PN 400019000-001, SN OFF 1454. 2 L 7 2 4F RT A21EA 2007081700078 20070817 00078 2007 8 17 MASA200700336 4 20070618 A 2561 SEAL CNDAIR CL600 CL6002B19 1900309 EA LIFE VEST TORN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37228 7228 ASH 2764 PHX. CREW REPORTED THE OBSERVER'S LIFE VEST COMPARTMENT SEAL WAS TORN. MAINTENANCE INSPECTED THE LIFE VEST AN D RESEALED THE COMPARTMENT. 2 L 7 2 4F RT A21EA 2007081700089 20070817 00089 EA 2007 8 17 MASA200700358 1 20070624 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 912FJ 15012 ASH 2601 BWI. CAPTAIN REPORTED ROW 17 CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED FLOOD LIGHT. 2 L 7 2 4F RT A21EA 2007081700094 20070817 00094 EA 2007 8 17 SWIA200718567 1 20070731 A 3397 CONTACT CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DIRTY A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 926SW 7687 LOWER EMERGENCY EXIT SIGN ON LEFT SIDE EMERGENCY EXIT ROW DOES NOT ILLUMINATE, FLIGHT NR 6156. CLEANED CONTACTS ON FLOO R LEVEL STRIP. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007081700095 20070817 00095 NM 2007 8 17 AWXA200700971 1 20070708 A 5311 652072354 FRAME BOEING 737 7373G7 1384595 NM BS 492 S24R CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5962328, CRACKED FORWARD CARGO COMPARTMENT DOOR CUT OUT, AFT FRAME, BS 492, S24R, W L 160. REPAIRED FORWARD CARGO COMPARTMENT DOOR CUT OUT, AFT FRAME, BS 492, S24R, WL 160 I/A/W USAIRWAYS EA 120120. 2 L 7 2 4F RT A16WE 2007081700101 20070817 00101 NM 2007 8 17 2007UALA02978 1 20070803 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 FLIGHT DECK CEILING EMERGENCY LIGHT INOP. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007081700103 20070817 00103 NM 2007 8 17 2007UALA02225 1 20070625 A 2560 141N6250 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 583UA 26705 DOOR 1R, GIRT BAR ENGAGEMENT LT INOP. FOUND GIRT BAR LOOSE. REINSTALLED GIRT BAR DOOR AND NOW IT ARMS OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081700124 20070817 00124 EU 2007 8 17 CPCP20070080 1 20070531 A 5320 ANGLE AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 429AT 429 TAIL BUMPER AFT BTM ANGLE CORRODED. TAIL BUMPER AFT BTM ANGLE CORROSION REMOVED AS PER SRM 51-21-42 FOUND OUT OF LIMITS 51-10-10 TAIL BUMPER ANGLE REPLACED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007081700136 20070817 00136 NM 2007 8 17 2007UALA03001 1 20070803 A 5210 DOOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD ENTRY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 FWD ENTRY DOOR HAS 2 EACH FASTENER HOLES WITH CRACK INDICATIONS ABOVE AND BELOW FWD END OF UPPER HINGE CUTOUT, MARKED. REPAIRED DAMAGED FASTENER HOLES ABOVE AND BELOW UPPER HINGE CUTOUT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700137 20070817 00137 EU 2007 8 17 CPCP20070082 1 20070705 A 5320 BRACKET AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 431AT 431 FOUND FRAME 36 FWD FOLDING STEP BRACKET CORRODED. BRACKET IS FABRICATED AS PER SRM 53-67-70 FIG 137 AND REPLACED AS PER AMM 20-21-12. 2 H 7 2 4T RT A53EU 2007081700140 20070817 00140 EU 2007 8 17 CPCP20070083 1 20070705 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 431AT 431 FOUND FRAME 36-39 LT SEAT TRACK CORRODED. NOW LT SEAT TRACK BETWEEN FRAME 36-39 REPLACED IAW SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007081700149 20070817 00149 NM 2007 8 17 2007UALA03009 1 20070805 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FWD CARGO DOOR CUTOUT FWD FRAME IS CRACKED AT LOWER BOTTOM STOP FITTING OUTBOARD LOWER CORNER. MAJOR REPAIR ACCOMPLISHE D: REMOVED CARGO COMPARTMENT COMPONENTS TO ACCESS FRAME REPAIR, FABRICATED DOUBLERS, NDT, INSTALLED DOUBLERS, RIG DOOR, OPS CHECK DOOR SWITCH. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700153 20070817 00153 EU 2007 8 17 CPCP20070086 1 20070705 A 5320 THRESHOLD AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 431AT 431 FOUND FRAME 36-39- RT GUTTER CORRODED. RT THRESHOLD GUTTER REPLACED AS PER SRM 51-21-42. GUTTER FABRICATED ON W/C 1806 22. 2 H 7 2 4T RT A53EU 2007081700157 20070817 00157 NM 2007 8 17 2007UALA03014 1 20070804 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN CONTAMINATED A UALA L ABORTED APPROACH L NO TEST IN INSP/MAINT 1 WP 29 341UA 24245 FLOOR PROXIMITY LIGHTING INOP FROM ROW 16 AFT TO AFT GALLEY. CLEANED & DRIED PROXIMITY LIGHTS. TESTED GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700162 20070817 00162 NM 2007 8 17 2007UALA03016 1 20070805 A 3350 587215834161441 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 EMERGENCY EXIT LIGHT STRIP CAME UP BY LAST ROW OF COACH. REPLACED APPROX 4 FEET OF AFT EEL TRACK COVER & INSTALLED END CAP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700170 20070817 00170 NM 2007 8 17 07FDEA02811 1 20070809 A 5347 651627910 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 MAIN CABIN TRACK HAS CORROSION AROUND NUTPLATE HOLES AND OTBD SIDE OF SEAT TRACK FROM BS 774 - 848, LBL 45. REMOVED COR ROSION REF SRM 51-10-1, FOUND TO BE OUT OF LIMITS REF SRM 53-10-1, ORIGINAL THICKNESS .090", REMOVED .020", REMAINING .0 70", REPLACED SEAT TRACK T-CAP SRM 51-30-2. REPAIR IS CLASSIFIED AS MAJOR. 2 L 7 3 4F RT A3WE 2007081700181 20070817 00181 EA 2007 8 17 TRAX200701073 1 20070728 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 873AS 7549 UPPER CENTER ENGINE SUPPORT BEAM IS CRACKED (CTR BOXBEAM). WORK DONE IAW REO 601R-53-61-345. SUPPLEMENTAL - SDR CLOSED 08/06/07. 2 L 7 2 4F RT A21EA 2007081700184 20070817 00184 EU 2007 8 17 AWXA200700977 1 20070725 A 5544 D5537123500600 HINGE FITTING AIRBUS 320 A320231 3930325 EU ZONE 300 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 SAL - MAJOR REPAIR - C-06 CHECK - NR 5964982, THE NR 2 RUDDER HINGE FITTING HAS EXCESSIVE PLAY, RUDDER STATION 1926/RIB 4. REPLACED THE NR 2 RUDDER HINGE FITTING, RUDDER STATION 1926/RIB 4 IAW A320 AMM 27-21-41. 2 L 7 2 4F RT A28NM 2007081700190 20070817 00190 EU 2007 8 17 AWXA200700982 1 20070724 A 2570 DME1141 PROXIMITY SWITCH AIRBUS 320 A320231 3930325 EU ZONE 200 FAILED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 SAL - EEL - C-06 CHECK - NR 5964456, WHILE PERFORMING A FUNCTIONAL CHECK TO CHECK THE ABILITY OF THE L1 DOOR PROXIMITY S WITCH TO ACTIVATE THE EMERGENCY ESCAPE LIGHTS, THE PROXIMITY SWITCH WAS FOUND TO HAVE AN OPEN CIRCUIT AND FAILED THE FUN CTIONAL CHECK. REPLACED THE L1 DOOR PROXIMITY SWITCH 4WN1 IAW A320 AMM 52-71-00. 2 L 7 2 4F RT A28NM 2007081700193 20070817 00193 EU 2007 8 17 F3LA200700195 1 20070807 A 2910 LINE AIRBUS A318 A318111 3940019 EU HYDRAULIC SYS LEAKING A F3LA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 NM 03 807FR 235 2276 FLIGHT CREW REPORTED GREEN HYD QTY LOW IN CRUISE. PERFORMED LANDING GRAVITY EXTENSION PER FOM VOL II. REPLACED NR 1 EN GINE T/R ISOLATION VALVE PRESSURE HYDRAULIC LINE. PERFORMED OPS AND LEAK CHECK IAW 8-37-51-PB-401. CHECKED GOOD. RESE T FREE FALL EXTENSION HANDLE AND STOWED GEAR DOORS IAW AMM 32-33-00-720-001. 2 L 7 2 4F RT 2007081700195 20070817 00195 NM 2007 8 17 TSAA0732044 1 20070805 A 3297 84000003 SWITCH BOEING BOEING 737 7372X6C 1384552 NM ACCESSORY UNIT FAILED A TSAA O OTHER J WARNING INDICATION CL CLIMB 1 WP 13 841AL D00410 23123 NON-ETOPS FLIGHT 62 HNL - OGG - DURING CLIMB-OUT OF HNL, THE CREW REPORTED THE LANDING GEAR HANDLE STAYED IN THE DOWN PO SITION WHEN THEY ATTEMPTED TO RAISE IT TO THE UP POSITION. THE CREW USED THE QRH PROCEDURES AND RAISED THE GEAR HANDLE USING THE OVER-RIDE SWITCH. CREW CONTINUED TO OGG WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE LANDING GEAR AND INSTALLED THE LANDING GEAR LOCK PINS. THE AIRCRAFT FLEW TO HNL WITH THE GEAR DOWN WITHOUT INCIDENT. MAINTENANCE REMOV ED AND REPLACED THE S1 TEST SWITCH ON THE LANDING GEAR ACCESSORY UNIT WITH ALL CHECKS NORMAL PER CMM 32-66-44. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007081700201 20070817 00201 EA 2007 8 17 SIMA200722205 1 20070807 A 2750 BPSU CNDAIR CL600 CL6002C10 1390015 EA TE FLAPS OUT OF RIG A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 524AE 10154 FLAP FAIL MESSAGE, LEFT FLAP AT 4 DEGREES, RIGHT FLAP AT 3 DEGREES AND SLATS EQUAL AT 20 DEGREES. DECLARED EMERGENCY, R ETURNED TO LIT. FOUND FLAP DRIVE TORQUE TUBE DISCONNECTED, INSTALLED TORUE TUBE IAW CRJ AMM 27-52-01. PERFORMED MECHAN ICAL AND ELECTRICAL RIGGING OF FLAP BPSU IAW CRJ 27-52-03 AND FLAT/SLAT OPERATIONAL CHECKS IAW CRJ AMM 27-50-00 WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007081700202 20070817 00202 EU 2007 8 17 UPS07150351 1 20070730 A 5270 WARNING LIGHT AIRBUS A300 A300F4622R 3930360 EU EVAC SLIDE INOPERATIVE A IPXA K NONE O OTHER NR NOT REPORTED 1 SO 01 146UP 0829 INSPECTION TYPE:N/A EVAC SLIDE WARNING LIGHT INOP. DEFERRED PER MEL 52-73-01-1. M 355534 PLACARD INSTALLED. RESET PLUG ON ASPSU. PERFORMED BITE TEST OF FASPSU PER 52-73-00-05, OPS CHECK NORMAL. PLACARD REMOVED. 2 L 7 2 4F RT A35EU 2007081700210 20070817 00210 WP 2007 8 17 NWAA072809946 1 20070808 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8926E 45863 TAIL COMPARTMENT EMERGENCY ESCAPE PATH LIGHTING INOP. REPLACED POWER SUPPLY. 2 L 7 2 4F A6WE 2007081700233 20070817 00233 NM 2007 8 17 KNNA200700040 1 20070720 A 5230 2024T3 SKIN BOEING 737 7372Q8 138448K NM PWA JT8 JT8D17 52049 NE CARGO DOOR CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 413JG 23148 AFT CARGO DOOR/CRACKED SKIN NEAR OF LATCH HANDLE, ACO NR 0753101 PROVIDE INSTRUCTIONS ON REPAIRING CRACK IN AFT CARGO DO OR SKIN NEAR HANDLE, SRM 52-30-2 FIG 3. 2 L 7 2 4F 4 F RT A16WE E2EA 2007081700251 20070817 00251 EA 2007 8 17 MASA200700381 1 20070701 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 715SF 7115 ASH 7358 ORD. MX REPORTED THAT THE RIGHT HAND AFT OVERWING EMERGENCY EXIT LIGHT WAS INOP. MX RELAMPED THE LIGHT. 2 L 7 2 4F RT A21EA 2007081700259 20070817 00259 NM 2007 8 17 MWEA070177 1 20070814 A 7830 7150922505 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 914ME 55177 UPPER THRUST REVERSER DEFLECTOR DOOR HAS A CRACK IN THE ZEE FRAME AT INBOARD END IN RADIUS AT STATION 26.666. FABRICATE D AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2007081700266 20070817 00266 NM 2007 8 17 MWEA070171 1 20070810 A 7830 7150923REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 909ME 55173 RIGHT THRUST REVERSER INBOARD FRAME 35 IS CRACKED. FABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007081700267 20070817 00267 NM 2007 8 17 MWEA070172 1 20070810 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 909ME 55173 RIGHT THRUST REVERSER UPPER INBOARD FRAME 26 IS CRACKED. FABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007081700277 20070817 00277 NM 2007 8 17 2007UALA03031 1 20070806 A 2910 LINE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE HYD SYSTEM FAILED A UALA O OTHER O OTHER AP APPROACH 1 WP 29 223UA 30224 C-HYD FAILURE AFTER FINAL APPROACH. 08-31-07 REPLACED INBOARD. NOSE STEERING HYDRAULIC LINE. PRESSURE CHECKED SYSTE M. CHECKED OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007081700283 20070817 00283 NM 2007 8 17 2007UALA03021 1 20070805 A 2612 FIRE LOOP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE FAULTY A UALA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 WP 29 517UA 24861 NO R ENG OVERHEAT EICAS MESSAGE DISPLAYED DURING FIRE TEST. RIGHT ENGINE OVERHEAT LOOP 1 AND 2 DISPLAY MESSAGE DID NOT DISAPPEAR UNTIL TEST SWITCH WAS RELEASED. SWITCHED EICAS COMPUTER TO RIGHT AND PERFORMED TEST. RIGHT ENGINE FIRE LOOP TEST CARD WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081700285 20070817 00285 EU 2007 8 17 2007UALA03023 1 20070805 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS OPEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 427UA 512 EMERGENCY LIGHTS INOP AT ROWS 7ABC, 8ABC, 24ABC, 25ABC, 26ABC. 09-07-07 REPAIRED OPEN WIRE IN SIDEWALL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007081700304 20070817 00304 NM 2007 8 17 SWAA074034 1 20070814 A 2560 6557463 BRACKET BOEING 737 7377H4 1384404 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 262WN 32519 R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR BRACKET LOOSE. SECURED BRACKET PER MM. 2 L 7 2 4F RT A16WE 2007082000005 20070820 00005 EU 2007 8 20 07FDEA02837 1 20070813 A 5415 A54611031 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 400 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 PYLON NR 1 FWD PYLON-WING ATTACH FITTING LUG WITH LITTLE WAVE DAMAGE REPAIR PERFORMED BY BLEND OUT IAW SRM 51-74-10, APP ROVED BY EA 6-5451-106518 AND RAS /BAE/1005084/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082000006 20070820 00006 EU 2007 8 20 07FDEA02838 1 20070813 A 5310 A53974219220 CROSSBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 749FD 536 OLD SPLICE REPAIR ON TOP CAP BEAM C 63 NOT CONFORM TO SRM REPAIR RENEWED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 2007082000026 20070820 00026 EU 2007 8 20 07FDEA02861 1 20070813 A 5340 A5377364420600 FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 FRAME FITTING C38.2 CRACKED AND CORRODED AT LBL 60 IN FWD PIT UNDER T-CAP REMOVED AND REPLACED FITTING IAW A310-200 SRM 51-40-21 PARA 6 PO NR 583026.5. 2 L 7 2 4F RT A35EU 2007082100001 20070821 00001 EA 2007 8 21 A6WA200740382 1 20070709 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 461AW 7870 RT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14 IS CRACKED NEAR RADIUS APPROX 1.5 INCH L. (K) MAINTENANCE REMOVE D AND REPLACED RT FS 621-625.30 INTERCOSTAL IAW BOMBARDIER AEROSPACE REO 601R-53-61-422 AND SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082100003 20070821 00003 CE 2007 8 21 YNTA200777003 1 20070806 A 2730 BOLT LEAR 35 35A 5170602 CE ELEVATOR INCORRECT E YNTA K NONE W INADEQUATE Q C TX TAXI/GRND HDL 1 SW 05 770JP 210 BINDING OF ELEVATOR FLIGHT CONTROL SYSTEM WITH RUBBING SOUND. DURING REMOVAL OF RIGHT HAND NOSE PANEL TO GAIN ACCESS TO BOB WEIGHT PANEL FOUND ONE BOLT SECURING BOB WEIGHT PANEL TO BE INCORRECT LENGTH AND TYPE PER THE LEAR 35/36 ILLUSTRATE D PARTS CATALOG 27-33-05. REPLACED BOLT WITH CORRECT TYPE AND LENGTH. PERFORMED AN OPERATIONAL CHECK OF THE ELEVATOR F LIGHT CONTROL SYSTEM WITH NO DEFECTS FOUND IN ACCORDANCE WITH LEAR JET 35/36 MAINTENANCE MANUAL CHAPTER 27. 2 L 7 2 4F A10CE 2007082100007 20070821 00007 NM 2007 8 21 2007UALA02991 1 20070804 A 5347 SEAT TRACK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 841UA 1545 RIGHT INBOARD & OUTBOARD SEAT TRACKS FROM FR 41 TO FR 51 HAVE SCRATCHES AND GOUGES BEYOND LIMITS. MAJOR REPAIR ACCOMPLI SHED: REPLACED SEAT TRACK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082100008 20070821 00008 EA 2007 8 21 A6WA200740387 1 20070711 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 589 S23-26L DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 461AW 7870 LT SIDE LOWER FUSELAGE DENTS FWD OF FS 589 BETWEEN STRINGERS 23L AND 24L APPROX 5 INCHES LONG X 4 INCHES WIDE .035 INCH DEEP AND ABOVE STRINGER 26L APPROX 2.9375 LONG X 3.9375 INCHES WIDE X .023 DEEP. (K) MAINTENANCE REPAIRED LEFT SIDE L OWER FUSELAGE DAMAGE IAW SRM 53-00-31 REPAIR NR 1. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082100013 20070821 00013 NM 2007 8 21 KCSA071283 1 20070808 A 5414 SKIN BOEING 747 7472B4B 138481B NM NR 4 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NR 4 PYLON AFT LOWER SPAR INBOARD SIDE SKIRT IS CHAFED AT NAC STA 180 TO 265.4. 2 L 7 4 4F RT A20WE 2007082100014 20070821 00014 EA 2007 8 21 A6WA200740392 1 20070715 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 423AW 7636 RT FS 484 INTERCOSTAL ANGLE CRACKED AT RBL 27 APPROX .1 INCH LONG UNDER CABIN FLOOR PANEL 262DRF. (K) MAINTENANCE REMO VED CRACKED ANGLE, FABRICATED NEW ANGLE AND INSTALLED IAW BSC STANDARD REPAIR 601R-53-0029B AND 601R-53-41-059. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082100015 20070821 00015 EA 2007 8 21 A6WA200740393 1 20070715 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 423AW 7636 RT FS 484 INTERCOSTAL CRACKED AT RBL 36 APPROX .1 INCH LONG UNDER CABIN FLOOR PANEL 262DRH. (K) MAINTENANCE REMOVED CR ACKED ANGLE, FABRICATED AND INSTALLED NEW ANGLE IAW BSC STANDARD REPAIR 601R-53-0030A AND REO 601R-53-41-059. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082100016 20070821 00016 EA 2007 8 21 A6WA200740394 1 20070715 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 423AW 7636 LT FS 484 INTERCOSTAL PREVIOUS REPAIR ANGLE AT LBL 36 CRACKED APPROX .1INCH LONG UNDER CABIN FLOOR PANEL 261DLF. (K) M AINTENANCE REMOVED CRACKED ANGLE, FABRICATED AND INSTALLED NEW ANGLE IAW BSC STANDARD REPAIR 601R-53-0030A AND REO 601R- 53-41-059. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082100018 20070821 00018 EA 2007 8 21 A6WA200740396 1 20070715 A 5320 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 574 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 423AW 7636 U-CHANNEL AT BOTTOM OF CARGO DOOR FWD ROLLER TRACK IS CRACKED .2500 INCH LONG. (K) MAINTENANCE REMOVED AND REPLACED U-CHANNEL IAW CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007081700070 20070817 00070 SO 2007 8 17 SWIA200718558 1 20070803 A 3097 CONNECTOR EMB 120 EMB120ER 3260203 SO RCCB PANEL LOOSE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 579SW 120347 CREW REPORTS HOT PLASTIC ODOR FROM RIGHT RCCB PANEL. TIGHTENED TERMINAL TO PROP HEAT RCCB CONNECTOR. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007081700081 20070817 00081 EA 2007 8 17 MASA200700338 1 20070619 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXIT SIGN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77278 7278 ASH 2719 PHX. REPORTED ONE LAMP IN THE OVERHEAD EXIT SIGN INOP. MAINTENANCE RELAMPED THE EXIT SIGN. 2 L 7 2 4F RT A21EA 2007081700098 20070817 00098 NE 2007 8 17 2007UALA02975 2 20070802 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 STALLED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 WP 29 427UA 512 V10167 FLIGHT DIVERTED DUE TO NR 2 ENGINE STALL WITH OIL FILTER CLOG LIGHT AND ECAM MESSAGE. 09-07-07 ENGINE FAILED IN SER VICE. THE CORRECTIVE ACTION WAS REPLACEMENT OF THE ENGINE. AS FOR THE SPECIFICS OF THE ENGINE FAILURE, IT HAS BEEN TRA CED TO THE FAILURE OF THE NR 3 BEARING. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007081700099 20070817 00099 NM 2007 8 17 2007UALA02976 1 20070802 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EEL INOPERATIVE 42 HJK. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007081700108 20070817 00108 NM 2007 8 17 2007UALA02326 1 20070630 A 3830 FLAPPER VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MID LAVATORY STUCK A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 524UA 24977 FLIGHT DIVERTED DUE TO ALL LAVATORIES NEED SERVICING. MID LAV TOILET FLAP STUCK. SERVICED MID LAV FLAPPER TO UNSTUCK P OSITION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081700115 20070817 00115 NM 2007 8 17 2007F00042 1 20070716 A 3260 L369 INDICATOR BOEING 737 7373Y0 1384671 NM MLG STUCK G AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 314AW 23748 AFTER TAKEOFF AT DFW, RIGHT MAIN GEAR LIGHT RED, GEAR HANDLE WAS IN THE OFF POSITION. FLIGHT DECK CREW CHECKED QRH, BUR NED OFF FUEL TO PREVENT OVERWEIGHT LANDING AND PERFORMED AN "AIR RETURN TO DFW", LANDED WITHOUT FURTHER INCIDENT AT DFW. THE AWXA MAINTENANCE CORRECTIVE ACTION SIGN OFF WAS AS FOLLOWS. 'PERFORMED VISUAL INSPECTION OF RIGHT UPLOCK, NO DEFE CTS NOTED. T/S, OHMED OUT S74 RIGHT UPLOCK INDICATOR SENSOR IAW AMM 32-61-00-1, (BLUE TO YELLOW=3500 OHMS "OK"), (RED TO YELLOW 300 OHMS "OK"). IN THE FLIGHT DECK NOTICE THE RIGHT MAIN GEAR RED LIGHT (L369) WOULD NOT TEST WITH THE TOGGLE SWITCH. WHEN MECHANIC PRESSED TO TEST THE L369 IT STUCK ON. THE L369 STAYED IN (ILLUMINATED) UNTIL PRYING CAP ASSY OU 2 L 7 2 4F RT A16WE 2007081700127 20070817 00127 NM 2007 8 17 QXEA200701221 1 20070728 A 2930 9702811 TRANSDUCER BOMBDR DHC8 DHC8402 1390042 NM HYD PRESSURE MALFUNCTIONED A QXEA D RETURN TO BLOCK P NO WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 429QX 4161 SEA FLIGHT NR 2498: STANDBY HYD PRESSURE INDICATOR INOP. AIRCRAFT RETURNED TO BLOCK, MAINTENANCE HAS PLACED THIS ON MEL . AIRCRAFT WAS RETURNED TO SERVICE. MAINTENANCE FOUND THE NR 3 HYD SYSTEM TO BE DASHES. REMOVED AND REPLACED NR 3 HYD PRESSURE TRANSDUCER IAW Q400 AMM TASK 29-30-01-400-801. OPERATED NR 3 AND STBY HYD SYSTEMS, INDICATIONS NORMAL. AIRCRA FT RETURNED TO SERVICE 2 H 7 2 4T RT A13NM 2007081700128 20070817 00128 NM 2007 8 17 2007UALA02997 1 20070803 A 5320 STIFFENER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 BEHIND FWD LAV SERVICE PANEL HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: REPLACED THE FWD LAV SERVICE PANEL STIFFENER & HAT CHANNEL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700129 20070817 00129 NM 2007 8 17 DHL2007741533 1 20070808 A 5322 SHEAR TIE BOEING 727 7272Q9 138448M NM BS 970 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AFT PIT, BS 970, SHEAR TIE BETWEEN STR 28L AND 29L CORRODED. REMOVED DAMAGED SHEAR TIE, 6.25" BY 1.5", FABRICATED NEW S HEAR TIE FROM 7075-T0, .071" BY 6.5" BY 4.25", PO NR 9004150, PER B727 SRM 53-10-2 FIG 5 AND 53-10-4 FIG 11. HEAT TREAT ED REPAIR PART TO T6 CONDITION PER FASI ER NR 2-37153-801 REV A. TREATED, PRIMED, AND INSTALLED SHEAR TIE PER B727 SRM 51-10-2 AND 53-10-4 FIG 11. 2 L 7 3 4F RT A3WE 2007081700135 20070817 00135 NM 2007 8 17 QXEA200701243 1 20070805 A 5100 NONE BOMBDR DHC8 DHC8402 1390042 NM NONE NONE A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 428QX 4160 YEG FLIGHT NR 2319: ON PUSHBACK, BOTH MFD HAVE ALT FAIL MESSAGE. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE CYCLED SHIP S POWER AND REPOWERED WITH APU. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007081700141 20070817 00141 NM 2007 8 17 2007UALA03003 1 20070803 A 5320 FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 INTERCOSTAL WEB TO FRAME TIE CLIP AT STATION 360 AND STR 10L IS CRACKED. MAJOR REPAIR ACCOMPLISHED: REPLACED FRAME TIE CLIP AT STA 360 STR 10L. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700158 20070817 00158 GL 2007 8 17 2618 1 20070808 A 7933 12634001 SENSOR CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO HARTZL HCJ3Y PHCJ3YF1 GL OIL TEMP MALFUNCTIONED E J4PA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 13 134AJ 1511 917726 FP3800B FLYING FROM GSP TO LRO APPROXIMATELY 1500 HOURS LOCAL DEVELOPED A HIGH OIL TEMP. MADE AN UNSCHEDULED LANDING AT CAE WIT HOUT INCIDENT. THERE WAS TWO PASSENGERS ON BOARD. IT WAS DETERMINED THAT THE OIL TEMP SENSOR WAS MALFUNCTIONING. REPL ACED SENSOR AND FLEW TO GMU WITHOUT INCIDENT. 1 L 7 1 3O 3 O NT A00009CH E3SO 5 C P36EA 2007081700165 20070817 00165 NM 2007 8 17 07FDEA02806 1 20070808 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 PASSENGER CABIN STA 780 STR 7R, STRINGER CLIP CRACKED REPLACED STA 780 STR 7R, STRINGER CLIP, IAW SRM 51-30-2. THIS REP AIR CLASSIFIED AS MAJOR. 2 L 7 3 4F RT A3WE 2007081700174 20070817 00174 NM 2007 8 17 07FDEA02813 1 20070809 A 5320 652954811 ANGLE BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 UPPER MAIN DECK FLOOR STRUCTURE, ARCHED CLOUSER WEB COVER FWD ATTACH ANGLE IS CRACKED OUT OF NUTPLATE HOLE STA 1178, RBL 50" (VIEW FROM LWR PIT) REMOVED ARCHED CLOSER WEB ASSY. FABRICATED NEW WEB, STIFFENER, AND ANGLE REF DWG 65-29548. TREATED AND PRIMED REF SRM 51-10-2, INSTALLED ARCHED WEB ASSY REF DWG 65-29548 AND SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007081700191 20070817 00191 EU 2007 8 17 AWXA200700983 1 20070803 A 5330 D53480030202 SKIN AIRBUS 320 A320231 3930325 EU ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 632AW 81 SAL - MAJOR REPAIR - C-7 CHECK - NR 5963450, CORROSION ON EXTERNAL FUSELAGE SKIN PRE-EXISTING REPAIR DOUBLER, BS 3310/FR 69 TO BS 3366/FR 70, S28R - S34R. REPLACED EXTERNAL FUSELAGE SKIN REPAIR DOUBLER, BS 3310/FR 69 TO BS 3366/FR 70, S28R - S34R IAW A320 SRM 53-41-11. 2 L 7 2 4F RT A28NM 2007081700199 20070817 00199 SO 2007 8 17 SIMA200722204 1 20070809 A 3320 BR900022 BALLAST EMB 135 EMB135LR 3260305 SO CABIN LIGHTS BURNED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 720AE 15981 145279 ELECTRICAL ODOR IN CABIN AT SEAT 1A. FOUND BALLAST RT8425 AND RT8400 BURNED. REMOVED AND REPLACED BALLAST IAW EMB AMM 33-21-03. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007081700224 20070817 00224 EU 2007 8 17 07FDEA02821 1 20070810 A 5330 A53989352200 SKIN PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 SKIN PANEL UNDER ANTI CHAFING PLATE FR 92 - FR 95 CRACKED AND IN SOME SMALL AREAS CORRODED STRUCTURE REPAIR IN ACCORDANC E WITH EA 6-5319-106511 AND RAS /DAHAM/4022481/2007 PERFORMED. 2 L 7 2 4F RT A35EU 2007081700232 20070817 00232 NM 2007 8 17 KNNA200700039 1 20070426 A 5330 2024T3 SKIN BOEING 737 7372Q8 138448K NM PWA JT8 JT8D17 52049 NE BS 360-420 CANNING A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 413JG 23148 OIL-CAN EFFECT ON FUSELAGE SKIN AT BS 384 BETWEEN STR-16L/17L, ACO NR 0753100 REV.0, PROVIDE INSTRUCTIONS ON REPAIR OF D AMAGE SKIN, BETWEEN BS 360L TO BS 420L SRM 53-30-3 AND BOEING MESSAGE 1-326794229-28 AND FAA 8100-9. 2 L 7 2 4F 4 F RT A16WE E2EA 2007081700236 20070817 00236 EU 2007 8 17 SIMA200722505 1 20070812 A 5100 UNKNOWN SAAB SF340 340B 7860101 EU VIBRATION A SIMA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SW 21 340RC 340B340 SHUDDER IN AIRFRAME, LOW FREQUENCY, CYCLICAL VIBRATION FELT AT SPEEDS LESS THAN 200 KNOTS. MOST EVIDENT BETWEEN 200 TO 240 KNOTS. 2 L 7 2 4T RT A52EU 2007081700245 20070817 00245 EA 2007 8 17 MASA200700372 1 20070627 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75993 7372 ASH 7495 IAD. EMERGENCY PATH LIGHTING TORN UP WHEN PASSENGERS DE-PLANED. MX REPAIRED EMERGENCY PATH LIGHTING. 2 L 7 2 4F RT A21EA 2007081700246 20070817 00246 EA 2007 8 17 MASA200700367 1 20070627 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75995 7361 ASH 7191 LAN. ROWS 1-5 EMERGENCY FLOOR PATH LIGHTING WAS INOP. MX CONTROL RESET THE SYSTEM WITH THE CREW AND OP CHECKS WERE GOOD. 2 L 7 2 4F RT A21EA 2007081700257 20070817 00257 NM 2007 8 17 MWEA070175 1 20070810 A 7830 7150922 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 919ME 55181 RIGHT THRUST REVERSER UPPER BUCKET ZEE FRAME AT STATION 35 IS CRACKED AT INBOARD SIDE. FABRICATED AND INSTALLED SPLICE ANGLE. 2 L 7 2 4F TR A6WE 2007081700271 20070817 00271 EU 2007 8 17 07FDEA02830 1 20070811 A 5311 FRAME AIRBUS 310 A310203 3930313 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT PIT FRAME 67 BETWEEN STRINGER 49R AND 50R DENTED FORMED FRAME TO ORIGINAL CONTOUR REF: A310-200 SRM 51-73-10. PERFO RMED HFEC, INSPECTION OF AREA IAW A310-200 NTM 51-10-08, NO CRACKS NOTED. 2 L 7 2 4F RT A35EU 2007081700284 20070817 00284 EU 2007 8 17 2007UALA03022 2 20070806 A 7397 WIRE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 ENGINE BURNED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 377UA 24642 NR 1 ENGINE FUEL FLOW. FOUND BURNED WIRE AT FIREWALL CONNECTOR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700288 20070817 00288 NM 2007 8 17 2007UALA03026 1 20070805 A 5753 FLAP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RT WING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 118UA 28811 RIGHT INBOARD MIDFLAP HAS DAMAGE APPROX 2 FEET IN LENGTH ALONG THE INBOARD MOST LEADING EDGE. 08-31-07 REMOVED DAMAG ED SKIN AND CORE,FLUSHED CORE WITH ALCOHOL & DRIED AREA. REPAIRED RUBSTRIP AND TEFLON COATED AS REQUIRED. REPAIRED FLA P BULB SEAL RE TAINER CAUSING DAMAGE. REPAIRED FLAP DAMAGE. COMPLETED REPAIR PER SRM 5 7-53-01 & UA ENGRNG VARIATION AU THORIZTN. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007081700299 20070817 00299 EU 2007 8 17 2007UALA02989 1 20070801 A 2824 ACTUATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUEL SYSTEM MALFUNCTIONED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 447UA 836 IN FLIGHT BOTH OUTER TANK FUEL XFEED VALVES OPEN WITH 25.0 FOB. 09-07-07 REPLACED CONDESICON AND RT INTERCELL TRANSF ER VALVE ACTUATORS. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007081700302 20070817 00302 2007 8 17 SWAA074035 4 20070814 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 448WN 33721 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007081700305 20070817 00305 NM 2007 8 17 SWAA074038 1 20070814 A 5523 65C25798 HINGE FITTING BOEING 737 7373G7 1384595 NM LT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2007081700306 20070817 00306 2007 8 17 SWAA074037 4 20070814 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007081700307 20070817 00307 2007 8 17 SWAA074036 4 20070814 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007081700308 20070817 00308 NM 2007 8 17 2007UALA02910 1 20070728 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 782UA 26948 EEL LIGHTS INOP AT SEATS 2F AND 3F AFT LIGHTS ONLY. RESPLICED NEW EEL SYSTEM ASSY AT SEATS 2F AND 3F. SYSTEM OK CHECKE D OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007081700311 20070817 00311 NM 2007 8 17 2007UALA02913 1 20070727 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMEGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY LIGHT INOP 29 HJK. REPLACED EEL LAMP. OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007081700312 20070817 00312 NM 2007 8 17 2007UALA02914 1 20070727 A 3350 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 CEILING EMERGENCY INOP UPPER CREW REST AREA. REPLACED CEILING EMERGENCY LIGHT BATTERY. OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007081700319 20070817 00319 NM 2007 8 17 SWAA074026 1 20070813 A 2560 PH22300L GLOWSTRIP BOEING 737 7375H4 138449D NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED C2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT RT OVERWING EMERGENCY EXIT ROW. REMOVED AND REPLA CED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007081700320 20070817 00320 NM 2007 8 17 SWAA074010 1 20070811 A 3397 W146070920 WIRE BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 603SW 27954 DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. FOUND BROKEN WIRE, REPAIRED WIRE PER WDM. 2 L 7 2 4F RT A16WE 2007082000008 20070820 00008 EU 2007 8 20 07FDEA02841 1 20070813 A 5415 A54611024003 FITTING AIRBUS 300 A300B4605R 3930308 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 PYLON NR 1 LOWER FITTING WITH CORROSION IN BEARING HOLE REPAIR PERFORMED BY SB A300-54-6018, APPROVED BY EA 6-5451-10650 4 2 L 7 2 4F RT A35EU 2007082000011 20070820 00011 EU 2007 8 20 07FDEA02845 1 20070813 A 5315 A53773560 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 OLD SPLICE REPAIR ON TOP CAP BEAM C 33 , -Y140-805 IN FWD CARGO COMPARTMENT NOT CONFORM TO SRM. REPAIR RENEWED IAW, SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 2007082000012 20070820 00012 EU 2007 8 20 07FDEA02846 1 20070813 A 5320 A53974504220 WEB AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 CORROSION ON WEB C63, P49-50 LT OUT OF LIMIT REPAIR PERFORMED BY CORROSION REMOVAL IAW SRM 51-74-10, APPROVED BY EA 6-53 17-112487 AND RAS/DATLS/0003810/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082000013 20070820 00013 EU 2007 8 20 07FDEA02847 1 20070813 A 5313 A53974202477 STRINGER AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 CORROSION SPOT ON STRINGER P52 RT, C62-63, REPAIR PERFORMED BY REWORK OF THE AREA IAW EA 6-5317-112485 AND RAS/DATLS/000 3791/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082000019 20070820 00019 NM 2007 8 20 07FDEA02853 1 20070813 A 5340 654531314 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 PASSENGER CABIN 720E STR 9R, STRINGER CLIP CRACKED. REMOVED BRACKET PER SRM 51-30-2 PG 32 FIG 7. INSTALLED NEW BRACKET REF SRM 51-30-2 PG 1. 2 L 7 3 4F RT A3WE 2007082000020 20070820 00020 EU 2007 8 20 07FDEA02854 1 20070813 A 5320 A53832103206 WEB AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 749FD 536 UNKNOWN REPAIR ON WEB A538-32103-206, C47, TRACK 3-4 RT REPAIR RENEWED (DOUBLER REPAIR) IAW EA 6-5315-112439 AND RAS 052 826/005/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082100004 20070821 00004 EU 2007 8 21 2007UALA02990 1 20070801 A 2913 PUMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYDRAULIC SYSTEM MALFUNCTIONED A UALA O OTHER K FLUID LOSS CR CRUISE 1 WP 29 402UA 439 CREW REPORTS AT 370 HAD YEL HYD ENG PUMP LO PRESS AND PUMP FAULT LIGHT WITH THE PRESSURE DROPPING TO 2100 PSI. PTU THEN CAME ON LINE. ENG PUMP TURNED OFF. 09-07-07 REPLACED EDP, FILTERS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082100005 20070821 00005 EA 2007 8 21 A6WA200740385 1 20070615 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 434AW 7322 LT WING PLANK AT PANEL 540BB HAS CORROSION APPROX .004 DEEP X 4 INCHES LONG X .2500 INCHES WIDE IN NON-CRITICAL AREA. M AINTENANCE PERFORMED MAJOR REPAIR TO WING PLANK ACCESS HOLE AT WS 54.897 (LT) BY REMOVING CORROSION IN NON-CRITICAL AREA S IAW REO 601R-57-21-030, REV F. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082100009 20070821 00009 NM 2007 8 21 USAA200708001 1 20070805 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 444US 24862 A .5 INCH CRACK FOUND AT RT AFT SERVICE DOOR CUTOUT IN FUSELAGE SKIN AT UPPER HINGE AREA. REMOVED DAMAGE & INSTALLED DO UBLER REPAIR PER SRM 53-60-01 FIG 201. 2 L 7 2 4F RT A16WE 2007082100011 20070821 00011 EA 2007 8 21 A6WA200740390 1 20070707 A 5320 601R75262157 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 527 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 409AW 7447 CHANNEL (PN 601R75262-157) IN RT MLG WHEEL WELL IS CRACKED APPROX .5 LONG. (K) MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED A NEW BRACKET P/N 601R75262-157 IAW CRJ SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082100021 20070821 00021 NM 2007 8 21 2007UALA02920 1 20070730 A 5210 RESERVOIR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 DOOR 1L EMERGENCY POWER RESERVOIR PSI LOW. REPLACED EMERGENCY POWER RESERVOIR FOR DOOR 1R AND ACCOMPLISHED BOTTLE INSPE CTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082100022 20070821 00022 NM 2007 8 21 2007UALA02921 1 20070730 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 L-1 DOOR UPPER GATE CORRODED. REPLACED UPPER GATE FOR DOOR 1L. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082100027 20070821 00027 EA 2007 8 21 A6WA200740398 1 20070715 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 423AW 7636 FS 280 FRAME CRACKED APPROX 2 INCH LONG OB AT RBL 9, BELOW W/L 73. (K) MAINTENANCE REMOVED DAMAGED SECTION AND INSTALL ED REPAIR IAW BOMBARDIER REO 601R-53-11-171. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082100028 20070821 00028 EA 2007 8 21 A6WA200740399 1 20070715 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 423AW 7636 LT FS 280 FLOOR SUPPORT CLIPS CRACKED APPROX .2 INCH LONG AT LBL 9 IB AND OB LOCATIONS. (K) MAINTENANCE REMOVED AND IN STALLED SERVICEABLE CLIPS TWO P/N 601R3113-57 IAW BSC STANDARD REPAIR 601R-53-0057A AND CRJ 200 SRM 51-42-21 AND 51-42-1 3. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082100029 20070821 00029 EU 2007 8 21 COEA0701902 1 20070423 A 5230 S52176226204 ANGLE AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE CARGO DOOR CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 902FX 175 AFT LT CARGO DOOR LOWER AFT INER ANGLE HAS LEVEL 2 CORROSION. REMOVED LOWER AFT INNER ANGLE. INSTALLED NEWLY FABRICATE D LOWER AFT INNER ANGLE. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007082100030 20070821 00030 EU 2007 8 21 COEA0702902 1 20070424 A 5230 S52176226204 ANGLE AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE CARGO DOOR CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 902FX 175 AFT LT CARGO DOOR LOWER CENTER ANGLE HAS LEVEL 2 CORROSION. REMOVED LOWER CENTER ANGLE. INSTALLED NEWLY FABRICATED LOW ER CENTER ANGLE. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007082100031 20070821 00031 EU 2007 8 21 COEA0703902 1 20070510 A 5330 S53671406200 SKIN AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE ZONE 800 CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 902FX 175 SURFACE CORROSION (LEVEL 2) FOUND ON FUSELAGE SKIN COMMON TO NR 2 LOWER VHF ANTENNA. REMOVED CORROSION FROM DOUBLER COM MON TO VHF ANTENNA. FOUND DOUBLER TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW DOUBLER. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007082100055 20070821 00055 NM 2007 8 21 2007UALA02948 1 20070801 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY LIGHTS AT ROWS 36 RT & 43 RT ARE INOPERATIVE. RELAMPED 36 RT LIGHT & REPLACED 43 RT LIGHT. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082100056 20070821 00056 NM 2007 8 21 2007UALA02949 1 20070801 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY CEILING LIGHT ABOVE ROW 42 LT INOP. RESECURED CONNECTOR. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082100033 20070821 00033 NM 2007 8 21 2007UALA02924 1 20070730 A 3260 WARNING SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT MALFUNCTIONED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 508UA 24744 GEAR DISAGREE LIGHT ON WITH GEAR HANDLE UP-GONE AFTER CYCLING HANDLE TO OFF THEN UP. PERFORMED BITE TEST ON PROXIMITY S ENSE ELECTRONIC UNIT (PSEU), WHICH SHOWED BOTH NOSE LANDING GEAR LOCK SENSORS 065 AND 078 ON MEMORY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082100034 20070821 00034 NM 2007 8 21 2007UALA02925 1 20070730 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN EXPOSED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 SOME EMERGENCY LIGHT STRIP WIRES EXPOSED. REINSTALLED EEL LIGHTS WITH EXPOSED WIRING. OP CHECKED OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082100036 20070821 00036 NM 2007 8 21 2007UALA02927 1 20070731 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 669UA 30025 IN SEAT EMERGENCY LIGHTS ARE INOPERATIVE AT SEATS 14AB & 33AB. REMOVED AND REPLACED EEL LIGHTS IN BOTH SEAT LOCATI ONS. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082100037 20070821 00037 NM 2007 8 21 2007UALA02928 1 20070731 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN WRONG PART A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 669UA 30025 SEAT 21H HAS WRONG SEAT MOUNTED EPL LIGHT STRIP INSTALLED. REPLACED LIGHT ASSY WITH CORRECT PART. OPS CK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082100040 20070821 00040 NM 2007 8 21 2007UALA02931 1 20070730 A 2910 LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HYDRAULIC SYSTEM LEAKING A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 506UA 24627 LEFT HYD SYSTEM INDICATES ZERO WITH LEFT SYSTEM PRESSURE AND PUMP PRESSURE LIGHTS ILLUMINATED. ALSO HAVE L REV STOW SIG AND L REV ISLN VAL MESSAGES WITH NO VIBRATION PER CREW. REPLACED RELAY AND OPS CHECKED REVERSER SEVERAL TIMES. FOU ND NR 1 ENG THRUST REVERSER HYDRAULIC PRESSURE LINE BROKEN BENEATH STRUT FAIRING. REPLACED LINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082100042 20070821 00042 NM 2007 8 21 2007UALA02933 1 20070801 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 807UA 798 CABIN FLOORBEAM Y-1292 (RBL 51) UPPER FLANGE HAS EXFOLIATION CORROSION FROM FRAME C17 TO FRAME C20. MAJOR REPAIR ACCOMP LISHED: REMOVED & REPLACED CABIN FLOORBEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082100043 20070821 00043 NM 2007 8 21 2007UALA02934 1 20070731 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 UPPER FUSELAGE CROWN SKIN ABOVE ENTRY DOOR 1L STA 289 STA 289 STR 3L HAS GOUGES IN SKIN. MAJOR REPAIR ACCOMPLISHED: FA BRICATED EXTERNAL SKIN DOUBLER-TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082100044 20070821 00044 NM 2007 8 21 2007UALA02935 1 20070731 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 FWD GALLEY CARGO PIT AFT OF DOOR CUTOUT APPROX STA 455, STR 24R CRACKED. MAJOR REPAIR ACCOMPLISHED: INSTALLED NESTED R EPAIR ANGLES & U-CHANNEL REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082100045 20070821 00045 NM 2007 8 21 2007UALA02936 1 20070731 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 UPPER FUSELAGE SKIN HAS PREVIOUS BLEND OUT LOCATED BELOW FORWARD SECTION OF DORSEL FIN BETWEEN STA 887. MAJOR REPAIR AC COMPLISHED: FABRICATED EXTERNAL SKIN DOUBLER-TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082100046 20070821 00046 NM 2007 8 21 2007UALA02937 1 20070731 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 FUSELAGE SKIN HAS THREE INCH CRACK ONE FOOT BEHIND EMERGENCY LIGHT JUST BEHIND LEFT WING. MAJOR REPAIR ACCOMPLISHED: R EPLACED LT BELLY SKIN FROM STA 727-908, STR 20-25. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082100048 20070821 00048 EU 2007 8 21 2007UALA02939 1 20070730 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 436UA 638 CREW O2 SUPPLY SLOWLY LEAKING. REPLACED O2 REGULATOR. NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082100050 20070821 00050 NM 2007 8 21 2007UALA02943 1 20070731 A 3260 WARNING SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT MALFUNCTIONED A UALA O OTHER N FALSE WARNING LD LANDING 1 WP 29 852UA 1671 CREW COMMENTS: LANDING GEAR SYSTEM DISAGREE ECAM UPON LANDING, WENT AWAY AFTER 30 SECONDS. REPLACED PROX SENSOR 2 9GA AND LGCIU2. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082100051 20070821 00051 EU 2007 8 21 2007UALA02944 1 20070801 A 3350 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 485UA 1617 LEFT AFT EMERGENCY BATTERY INOPERATIVE. REPLACED BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082100052 20070821 00052 NM 2007 8 21 2007UALA02945 1 20070731 A 2432 BATTERY BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU MASTER SHORTED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 BATTERY CHARGER C/B P6-4 D8 WILL NOT STAY SET, IT CONTINUOUSLY POPS. FOUND SHORTED BATTERY. REPLACED THE BATTERY AND B ATTERY CHARGER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082100054 20070821 00054 NM 2007 8 21 2007UALA02947 1 20070801 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY CEILING LIGHTS ABOVE ROWS 37 LT, 39 LT & 44 LT ARE INOPERATIVE. RELAMPED EMERGENCY CEILING LIGHTS, OP CHECK N ORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082100058 20070821 00058 NM 2007 8 21 2007UALA02951 1 20070731 A 4997 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU DAMAGED A UALA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 WP 29 594UA 28145 CREW COMMENTS: DURING TAXI APU SHUT DOWN WITH LOUD GRINDING MECHANICAL NOISE IN AFT GALLEY. SOME OIL SEEPING DOWN A-C IN APU AREA. DID NOT ATTEMPT APU START FOR SAFETY REASONS. ECU BITE SHOWED "REVERSE FLOW". SOME OIL FOUND SEEPING D OWN IN APU AREA. FOUND WIRE ASSEMBLY APU GENERATOR HARNESS BURNED AT GENERATOR TERMINAL. NO METAL NOTED IN CHIP DETECTO RS. APU TURBINE FREE WHEELS EASILY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082100060 20070821 00060 EU 2007 8 21 COEA0703914 1 20070717 A 2910 S291805638200 LINE AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE METERING VALVE BROKEN A COEA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 NM 13 914FX 139 293 ON TAXI OUT ON FLIGHT NR 7091; CREW DISCOVERED NORMAL BRAKES AND GREEN HYDRAULICS LOST DURING BRAKE CHECK. THEY TAXIED BACK USING EMERGENCY HAND BRAKE TO PARK AIRCRAFT. AIRCRAFT PARKED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED L T OB METERING VALVE OUTLET PIPE. AIRCRAFT RETURNED TO SERVICE. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007082100061 20070821 00061 EU 2007 8 21 COEA0702912 1 20070727 A 5320 S52176207216 INTERCOSTAL AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE FUSELAGE CRACKED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 912FX 047 IN HEAVY CHECK AT COE FOUND CRACKED INTERCOSTAL IN AFT CARGO DOOR UPPER FWD POSITION. REMOVED AND REPLACED INTERCOSTAL. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007082100066 20070821 00066 NM 2007 8 21 2007UALA02954 1 20070802 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 807UA 798 CABIN FLOORBEAM Y-765 (RBL 30) UPPER FLANGE HAS EXFOLIATION CORROSION - 1 TO 2 INCHES FWD OF FRAME C20. REPLACED FLOORB EAM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082100069 20070821 00069 NM 2007 8 21 2007UALA02955 1 20070802 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 807UA 798 CABIN FLOORBEAM Y-254 (RBL 10) UPPER FLANGE HAS EXFOLIATION CORROSION FROM FRAME C19 TO FRAME C20 AND UNDER THE GALLEY F LOORBOARD. REPLACED FLOORBEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082100071 20070821 00071 NM 2007 8 21 2007UALA02956 1 20070801 A 3510 MR35114 OXYGEN MASK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 844UA 1581 F/O OXYGEN MASK DOES NOT FULLY INFLATE. SHOP FINDINGS INDICATE A CRACKED MAIN CASE WHICH WILL ALLOW LEAKAGE TO OCCUR. MASK REMOVED AND SENT TO SHOP FOR COMPLETE OVERHAUL. NEW MASK INSTALLED ON A/C. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082100073 20070821 00073 EU 2007 8 21 2007UALA02957 1 20070801 A 3350 LAMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 455UA 1105 EPSU INT LOAD EMER R. RELAMPED. CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082100077 20070821 00077 NM 2007 8 21 2007UALA02959 1 20070802 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EEL 1J AFT & 58 ABC ARE INOPERATIVE. REPLACED EEL LAIGHT ASSY BOTH POSITIONS. OP CHECKED GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082100079 20070821 00079 SO 2007 8 21 BOO2007F00001 2 20070531 A 8520 536421 GEAR BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO CRACKSHAFT WORN E BOOA K NONE O OTHER IN INSP/MAINT 1 GL 19 827TS 1376 TH836 CRANK SHAFT GEAR FAILURE. GEAR TEETH WORN OUT (.5) WIDTH CAUSED ENGINE FAILURE WHEN DRIVEN GEAR LOST CONTACT. (K) 1 L 7 2 3O 3 O 3A16 E5CE 2007082100089 20070821 00089 NM 2007 8 21 2007UALA02964 1 20070801 A 5270 STATIC LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR GIRT BAR TANGLED A UALA D RETURN TO BLOCK O OTHER IN INSP/MAINT 1 WP 29 584UA 26706 ARMING LIGHT DID NOT ILLUMINATE DOOR 1R. 08-31-07 FOUND STATIC LINE TANGLED IN GIRT BAR CAUSING NO INDICATION. SECU RED STATIC LINE PER UAL ENGINEERING SPECIFICATIONS AND SERVICE TIP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082100090 20070821 00090 NM 2007 8 21 2007UALA02965 1 20070801 A 2611 CIRCUIT BOARD BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SMOKE DETECTION FAULTED A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 791UA 26933 DET ZONE 1 CARGO AFT MESSAGE. REPLACED CARGO SMOKE DETECTOR. TESTED THRU THE MAINTENANCE ACCESS TERMINAL. NO MESSEGE F OUND GROUND TESTED NORMAL. SUSPECT ELECTRONIC CIRCUIT FAULT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007082100092 20070821 00092 NM 2007 8 21 2007UALA02967 1 20070801 A 5270 PROXIMITY SENSOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE DOOR WARNING FAULTY A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 815UA 867 RTFL DUE TO CABIN DOOR INDICATION PROBLEM. REPLACED PROX SENSOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082100096 20070821 00096 EU 2007 8 21 2007UALA02969 1 20070801 A 3610 SOLENOID AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE BLEED AIR SYS MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 412UA 465 RTFL DUE TO RIGHT PACK OVERHEAT INDICATION. REPLACED STAT 10HA2, BPRV SOLENOID 10HA2 2 L 7 2 4F 4 F RT A28NM E40NE 2007082100108 20070821 00108 EU 2007 8 21 UPS07150411 1 20070806 A 5320 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 151UP 0834 INSPECTION TYPE:N/A FLOOR PANEL HAS .250 INCH DIAMETER HOLE, 4 INCHES AFT OF FRAME 67 AND 6 INCHES RIGHT OF CL. ACCOMPL ISHED TEMP REPAIR PER A300 SRM 53-10-20 FIG 110. PERMANENT REPAIR DUE WITHIN 3350 FLT HOURS. THIS IS D355945. 2 L 7 2 4F RT A35EU 2007082100111 20070821 00111 NM 2007 8 21 UPS07550404 1 20070807 A 5610 WINDOW BOEING 757 75724APF 1384969 NM COCKPIT MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 457UP 25478 INSPECTION TYPE:N/A F/O'S NR 2 SIDE WINDOW WILL NOT OPEN WITHOUT PUSHING HANDLE BUTTON. C/W EO B757 5610-5738. 2 L 7 2 4F RT A2NM 2007082100112 20070821 00112 2007 8 21 UPS07850370 4 20070802 A 2565 SLIDE DOUG DC8 DC871F 302199D WP COCKPIT OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:N/A ESCAPE SLIDE OUT OF ITS ENCLOSURE. DEFERRED IAW MEL 52-7-1 M355759. RE-INSTALLED ESCAPE SLIDE. 2 L 7 4 4F RT 4A25 2007082100115 20070821 00115 WP 2007 8 21 UPS07850394 1 20070723 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 A-PIT STA 120 LBL 26 FLOORBEAM GOUGED AND FASTENER SHEARED. CUT OUT DAMAGED AREA ON FLOORBEAM AT STA 120 LBL 26 IAW SRM 51-02-00, FABRICATED AND INSTALLED REPAIR ANGLES AT STA 120 LBL 26 IAW SRM 51-02-00 FIG 1, AND SRM 5 3-02-00 FIG 1F. 2 L 7 4 4F RT 4A25 2007082100116 20070821 00116 WP 2007 8 21 UPS07850395 1 20070718 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 CREASE ON UPPER FUSE SKIN AT STA 1800 L9L. CUT OUT DAMAGED AREA ON FUSE SKIN AT STA 1800 L9L IAW SRM 53-2-1 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER, AND FILLER AT STA 1800 L9L IAW SRM 53-2-1 FIG 7, AND SRM 53-5-3 FIG 1 SHEET 1. 2 L 7 4 4F RT 4A25 2007082100118 20070821 00118 WP 2007 8 21 UPS07850397 1 20070718 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 FUSE SKIN CRACKED AND BULGING AT STA 1692 L28R. REPAIRED FUSELAGE EXTERIOR SKIN AT STA 1692 L28R IAW UPS EO DC8- 5330-20248-D APPX E AND SRM SRO8530032. 2 L 7 4 4F RT 4A25 2007082100119 20070821 00119 WP 2007 8 21 UPS07850403 1 20070806 A 3350 BATTERY DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:N/A EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND RELAY UNIT IAW MM 33-50-01-2. TESTS OK. 2 L 7 4 4F RT 4A25 2007082100121 20070821 00121 2007 8 21 UPS07850406 4 20070808 A 2565 SLIDE DOUG DC8 DC871F 302199D WP COCKPIT OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:N/A F/E DUMPED SLIDE ON DOOR OPEN. RE-INSTALLED SLIDE PER DC8 MM 25-60-01-2. 2 L 7 4 4F RT 4A25 2007082100122 20070821 00122 WP 2007 8 21 UPS07850407 1 20070721 A 5514 ANGLE DOUG DC8 DC873F 302199F WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 LT HORIZ STAB UPPER MOVEABLE FAIRING MOST AFT H-ANGLE CRACKED. REMOVED AND REPLACED LT HORIZ STAB MO VEABLE FAIRING AFT H-ANGLE IAW SRM 51-03-00-0, DWG 3702464, AND SRM 51-03-02. 2 L 7 4 4F RT 4A25 2007082100123 20070821 00123 2007 8 21 UPS07850408 4 20070807 A 2565 SLIDE DOUG DC8 DC871F 302199D WP COCKPIT TORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:N/A GIRT BAR HARD TO FASTEN ON ESCAPE SLIDE. FOUND ESCAPE SLIDE TORN NEAR GIRT BAR. REMOVED AND REPLAC ED ESCAPE SLIDE PER AMM 25-60-01-2, OPS CHECK OK. 2 L 7 4 4F RT 4A25 2007082100124 20070821 00124 WP 2007 8 21 UPS07850409 1 20070807 A 3242 BRAKE DOUG DC8 DC871F 302199D WP NR 8 FIRE A IPXA K NONE A FLAME/FIRE TX TAXI/GRND HDL 1 SO 01 703UP 45939 INSPECTION TYPE:N/A NR 8 BRAKE ON FIRE AT BLOCK IN. REMOVED AND REPLACED NR 8 BRAKE ASSY. INSPECTED AREA AND FOUND NO FURTHER DAMAGE. REPLACED WHEEL AND TIRE ASSY PER MM 32-40-01-2 DUE TO HEAT DISTRESS TO WHEEL. BRAKE ASSY INSTALLED PER MM 32-42-01-4. OK FOR CONTINUED SERVICE. 2 L 7 4 4F RT 4A25 2007082100125 20070821 00125 NM 2007 8 21 UPS07M50398 1 20070607 A 5330 SKIN DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C RT EXTERIOR FUSELAGE SKIN FOUND WITH CORROSION ADJACENT TO FWD SIDE OF APU EXHAUST DOOR LOWER PORTION AS MARKED. RT EXTERIOR FUSELAGE SKIN AJC7164-502 DAMAGED AREA TRIMMED OUT PER EN1416-07. HFEC INSP C/OUT PER DAC NDTSP M R.13 06-10-01.001 ON SKIN & FOUND NO CRACK EVIDENT. REPAIR DOUBLER, FILLER, SHIM FAB PER EN1416-07 USING MATL 7075T6- 0.150,0.125 A7 0.032". HOLES P/UP PER SRM 51-31-01 V2 R38 & PROTECTED PER SRM 51-21-01 V2 R38. APU EXHAUST DOOR LWR HI NGE INSTALLED. 2 L 7 3 4F RT A22WE 2007082100129 20070821 00129 EA 2007 8 21 TRAX200701109 1 20070725 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 833AS 7246 AFT DRAG ANGLE ON PAX DOOR IS CRACKED. 2 L 7 2 4F RT A21EA 2007082100130 20070821 00130 EA 2007 8 21 TRAX200701110 1 20070727 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 854AS 7382 CREW ESCAPE WATCH 832 IS MISSING EXTERIOR PLACARDS. 2 L 7 2 4F RT A21EA 2007082100131 20070821 00131 EU 2007 8 21 TRAX200701115 1 20070804 A 5311 FRAME AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 AFT AVIONICS COMPARTMENT CORROSION FOUND ON FR A55 AT L&LO. 2 H 7 2 4T RT 2007082100136 20070821 00136 NM 2007 8 21 USAA070616 1 20070808 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 STA 950 LBL 51, INTERCOSTAL HAS CORROSION. REMOVED & REPLACED INTERCOSTAL; CORR TASK C53-107-01; LEVEL 2, DEFECT SIZE: 3 INCHES. 2 L 7 2 4F RT A16WE 2007082100137 20070821 00137 NM 2007 8 21 USAA070617 1 20070808 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CANNING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 RIGHT SIDE OF 178 BULKHEAD, JUST TO LEFT OF BOTTOM RIGHT INSPECTION HOLE OIL CANNING. FAB'D NEW DOUBLER & FILLERS PER S RM 53-10-08 FIG 201, DEFECT SIZE: 18 X 12 INCHES. 2 L 7 2 4F RT A16WE 2007081700209 20070817 00209 WP 2007 8 17 NWAA072799946 1 20070726 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8926E 45863 AFT EMERGENCY CAT-WALK LIGHT OUT DURING EMERGENCY LIGHT CHECK. REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 2007081700213 20070817 00213 NM 2007 8 17 HALA0700330 1 20070807 A 2150 A/C PACK BOEING 767 76733A 1385209 NM LEFT MALFUNCTIONED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 593HA 33424 ETOPS SIGNIFICANT SYSTEM, EICAS MTC MSG 'LT PACK BITE'. PERFORMED BITE ON LT PACK, LOW LIMIT VALVE FAULT LIGHT. VERIFI ED OK, CLEARED MSG. 2 L 7 2 4F RT A1NM 2007081700216 20070817 00216 NM 2007 8 17 HALA0700333 1 20070809 A 3350 LAMP BOEING 767 76733A 1385209 NM EMERGENCY LIGHT INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 591HA 33423 OVERHEAD AISLE EMERGENCY LIGHT ADJACENT TO 39 B INOP. RELAMPED PER AMM 33 51 05, OPS NML. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007081700222 20070817 00222 WP 2007 8 17 07FDEA02818 1 20070810 A 5347 WSP0413509 SEAT TRACK DOUG DC10 DC1010F 3022111 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 MAIN CABIN DEEP WEAR ON SEAT TRACK AT STA 1497, X=-47 CUT DAMAGED SECTION OF SEAT TRACK FROM STA 1491 TO 1531. FABRICAT ED AND INSTALLED NEW SECTION REPAIR AND SPLICE IAW SRM 53-70-00 FIG 1 VOL 1. 2 L 7 3 4F A22WE 2007081700230 20070817 00230 EA 2007 8 17 QXEA200701267 1 20070807 A 3240 5013642 BRAKE CNDAIR CL600 CL6002C10 1390015 EA MLG UNKNOWN A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 614QX 10805 2064 10049 DEN - FLIGHT 4325, ON TAXI OUT, THE RIGHT OUTBOARD (NR 4) BRAKE TEMP WENT FROM 4 IN THE GREEN TO 8 IN THE WHITE. RETURN ED TO THE GATE. BRAKE WAS NOT DRAGGING. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE INDICATION ON MEL 32-46-1. THE MEL WAS CLEARED BY REPLACING THE NR 4 BRAKE AND THE THERMOCOUPLE SENSOR FOR THE TEMP INDICATION. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007081700231 20070817 00231 NM 2007 8 17 KNNA200700038 1 20070426 A 5330 SKIN BOEING 737 7372Q8 138448K NM PWA JT8 JT8D17 52049 NE BS 328-360 DENTED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 413JG 23148 DENT ON FUSELAGE SKIN AT BS 358/STR-17L NEAR DOOR L-1. ACO NR 075398 REV. 0, PROVIDE INSTRUCTIONS ON REPAIR OF GOUGE FW D OF BS 360 SRM 53-30-3 AND BOEING MESSAGE 1-326794229-26 AND FAA 8100-9. 2 L 7 2 4F 4 F RT A16WE E2EA 2007081700234 20070817 00234 SO 2007 8 17 SIMA200722504 1 20070812 A 3350 LIGHT EMB 135 EMB135LR 3260305 SO CABIN UNKNOWN A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 711PH 145235 RECEIVED ELECTRIC EMERGENCY ABNORMAL AND EMERGENCY LIGHTS NOT ARMED MESSAGES, RETURNED TO DCA. REINITIALIZED ELECTRICAL SYSTEM IAW EMB AMM 24-36-00 WITH NO DEFECTS NOTED. PERFORMED ENGINE RUNS WITH ELECTRICAL LOAD TRANSFER NORMAL AND OPER ATIONAL CHECK OF EMERGENCY LIGHTS WITH NO DEFECTS. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007081700242 20070817 00242 EU 2007 8 17 AWXA200700987 1 20070804 A 5347 D53112830200 DUMMY RAIL AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 632AW 81 SAL - MAJOR REPAIR - C-7 CHECK - NR 5963571, CORROSION ON CABIN RAIL DUMMY, BS 605/FR 12 - BS 709/FR 16, -Y81. REPLACED CABIN RAIL DUMMY, BS 605/FR 12 - BS 709/FR 16, -Y81 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007081700243 20070817 00243 EU 2007 8 17 AWXA200700988 1 20070810 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU ZONE 200 INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 633AW 082 SAL - EEL - C-06 CHECK - NR 5963744, WHILE PERFORMING A FUNCTIONAL CHECK TO CHECK THE EMERGENCY ESCAPE LIGHTS, AFT RT AN D FWD LT EMERGENCY DOOR EPSU FAILED THE FUNCTIONAL CHECK. REPLACED AFT RT AND FWD LT EMERGENCY DOOR EPSU IAW A320 AMM 33-51-38. 2 L 7 2 4F RT A28NM 2007081700244 20070817 00244 EU 2007 8 17 AWXA200700989 1 20070811 A 5321 D536700500200 FLOOR PANEL AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 632AW 81 SAL - MAJOR REPAIR - C-7 CHECK - NR 5980239, CORROSION FOUND ON FLOOR PANEL 261FF, BS 3158/FR66 - BS 3257/FR68. REPLACE D FLOOR PANEL 261FF, BS 3158/FR66 - BS 3257/FR68 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007081700249 20070817 00249 EA 2007 8 17 MASA200700385 1 20070629 A 2560 GLOWSTRIP CNDAIR CL600 CL6002D24 1390016 EA CABIN WORN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 934FJ 15034 ASH 2734 PHX. PILOT REPORTED THE PHOTO ILLUMINSCENT LIGHTING STRIP 16AC DEGRADED. MX PERFORMED OPS CHECK OF LIGHTING S TRIP AND FOUND NO FAULTS/DEFECTS NOTED, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007081700253 20070817 00253 NM 2007 8 17 MASA200700391 1 20070703 A 3350 COVER DHAV DHC8 DHC8202 2809007 NM CABIN BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 987HA 425 ASH 2894 PHX. EMERGENCY PATH LIGHTING AT SEAT 1D COVER BROKEN. MX REPLACED COVER. 2 H 7 2 4T RT A13NM 2007081700254 20070817 00254 EA 2007 8 17 MASA200700393 1 20070705 A 3350 1317 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 914FJ 15014 ASH 2682 CLT. EMERGENCY LIGHT ROW 10 INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2007081700255 20070817 00255 NM 2007 8 17 MWEA070173 1 20070810 A 7830 7150923 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 919ME 55181 RIGHT THRUST REVERSER LOWER BUCKET ZEE FRAME AT STATION 35 IS CRACKED AT INBOARD SIDE. FABRICATED AND INSTALLED SPLICE ANGLE. 2 L 7 2 4F TR A6WE 2007081700262 20070817 00262 NM 2007 8 17 MWEA070167 1 20070810 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 909ME 55173 RIGHT THRUST REVERSER INBOARD FRAME CRACKED AT STATION 26. FABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007081700265 20070817 00265 NM 2007 8 17 MWEA070170 1 20070810 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 909ME 55173 RIGHT THRUST REVERSER LOWER OUTBOARD FRAME 26 IS CRACKED. FABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007081700270 20070817 00270 EU 2007 8 17 07FDEA02829 1 20070811 A 5313 A53974202229 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT PIT, STR 55R CORRODED FROM FR 61 TO FR 63 (STA X 3302 - X 3408). THIS SDR ALSO INCORPORATES DISCREPANCY AND REPAIR DONE ON NON ROUTINE NR N000443, W/O 00037436, (STR 55R CORRODED FROM FR61 - 62). REMOVED AND REPLACED CORRODED SECTION OF STR 55R FROM FR 61 TO FR 63 (STA X 3302 - X 3408) IAW A310-200 SRM 53-17-14 AND 51-10-14. 2 L 7 2 4F RT A35EU 2007081700273 20070817 00273 WP 2007 8 17 07FDEA02832 1 20070811 A 2510 MOTOR DOUG DC10 DC1030F 3023504 WP COCKPIT SEAT BURNED A FDEA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 25 320FE 47835 UPON TAKING RUNWAY, FUMES NOTICED IN THE COCKPIT. TAXIED CLEAR BACK TO THE RAMP. FUMES INCREASED, DECLARED EMERGENCY, EVACUATED THE AIRCRAFT. UPON FURTHER INSPECTION, FOUND S/O'S SEAT CONTROL C/B POPPED, AND STRONG ODOR FROM SEAT MOTOR. UPON FURTHER INSPECTION, FOUND S/O'S SEAT CONTROL C/B POPPED, AND STRONG ODOR FROM SEAT MOTOR. REMOVED AND REPLACED S EAT IAW MM 25-11-03-4, OPS CHECKS GOOD. RAN PACKS FOR ONE HOUR THREE DIFFERENT TIMES, NO EVIDENCE OF FUMES. WHILE SERV ICING O2, DID NOT NOTICE ANY EVIDENCE OF FUMES IN E/E COMPARTMENT. 2 L 7 3 4F RT A22WE 2007081700274 20070817 00274 NM 2007 8 17 2007UALA03028 1 20070805 A 2612 FIRE DETECTOR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU NR 2 ENGINE FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 924UA 26645 NORMAL FIRE TEST OF NR 2 ENGINE DOES NOT TEST. FOUND HIGH TEMP TERMINALS AT CORE DETECTOR M1122 IMPROPERLY CRIMPED. R EPAIRED WIRING AND CRI MPED ON NEW TERMINALS. RAN ENGINE FOR TEN MINUTES AND PERFORMED FIRE TEST NUMEROUS TIMES, NO FAUL T NOTED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700275 20070817 00275 NM 2007 8 17 2007UALA03029 1 20070803 A 5310 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 FWD CARGO DOOR CUTOUT AFT FRAME IS CRACKED ON FWD SIDE IN THREE PLACES. AFT SIDE ON TOP OF CREASE, FWD SIDE AT BOTTOM O F STOP FITTING, UPPER CORNER OF STOP FITTING, O/B LOWER CORNER OF STOP FITTING AND THROUGH I/B LOWER BOLT HOLE OF STOP F ITTING AFT SIDE CRACK IS IN RADIUS ADJACENT TO UPPER I/B CORNER OF STOP FITTING. REPAIRED PER MM 53-30-75- 801. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081700276 20070817 00276 NM 2007 8 17 2007UALA03030 1 20070803 A 3510 OXYGEN SYSTEM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 195UA 26899 OXY MASK STOWAGE COMPT DEFECTIVE - 1ST OFFICER. CREW COMMENTS: TEST - RESET SWITCH DOES NOT RESET COM OR AIR ON F/O O2 COMPARTMENT. 08-31-07 REPLACED F-O'S O2 STOWAGE BOX AND CLEANED MASK AT EMERGENCY FLOW KNOB. OPS CHKS GOOD. CREW O2 BOTTLE CLOSED DURING REPLACEMENT, REOPENED AND SAFETY WIRED AFTER COMPLETION. CHKS READY FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007081700280 20070817 00280 NM 2007 8 17 2007UALA03018 1 20070804 A 4920 APU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OIL CONSUMPTION A UALA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 29 595UA 28748 APU OIL CONSUMPTION ABOVE LIMIT. REPLACED GEARBOX SHUTOFF VALVE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081700292 20070817 00292 NM 2007 8 17 2007UALA02982 1 20070802 A 2730 PULLEY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ELEVATOR CONTROL CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 CABIN CEILING AREA, ELEVATOR CONTROL CABLE PULLEY IS CRACKED AT STA 340, STR 4L. REMOVED AND REPLACED PULLEY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081700309 20070817 00309 NM 2007 8 17 2007UALA02911 1 20070727 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 THRESHOLD EMERGENCY LIGHT INOP DOOR 2R & BUSSEL EMERGENCY LIGHT INOP AT DOOR 4L. REPLACED LAMPS IN BOTH POSITIONS. OP CHECKED READY FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007081700322 20070817 00322 NM 2007 8 17 SWAA073973 1 20070809 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 744SW 29490 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007082000016 20070820 00016 NM 2007 8 20 07FDEA02850 1 20070813 A 5347 651960135 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 UPPER DECK STA 1086 - 1105 LBL 44 WL 208 SEAT TRACK I/B FLANGE HAS AREAS OF CORROSION. REMOVED CORROSION FROM LBL45 S TA 1090-1110, ORIGINAL .080 REMAINING .071 WITHIN LIMITS IAW SRM 53-10-1. TREATED AND PRIMED SEAT TRACK FROM STA 1090-1 110; REMOVED CORROSION FROM SEAT TRACK LBL 45 STA 1086-1090, ORIGINAL .080 REMAINING .055 OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK FROM STA 1030-1090 IAW SRM 51- 30-2. FABRICATED NEW TRACK FROM BAC1520-792 IAW SRM 51-30- 1. TREATED AND PRIMED NEW SEAT TRACK IAW SRM 51-10-2; INSTALLED NEW TRACK IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007082100017 20070821 00017 EA 2007 8 21 A6WA200740395 1 20070715 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 423AW 7636 FS 625.0 INTERCOSTAL OBLIQUE ANGLE (UPPER) CRACKED. (K) MAINTENANCE REMOVED AND REPLACED INTERCOSTAL P/N 601-35012-51 IAW BOMBARDIER REO 601R-53-61-422. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082100032 20070821 00032 EU 2007 8 21 COE2007F00000 1 20070606 A 5320 S53575104202 WEB AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 902FX 175 CARGO COMPARTMENT, PRESSURIZED ZONE BETWEEN LT MLG WHEEL WELL FRAME 25 TO 27 LOWER SIDE BOX WEB ASSEMBLY HAS SEVERAL ARE AS OF LEVEL 2 SURFACE CORROSION. CORROSION SPOTS BLENDED IAW SRI DO/TS 2302/07-8813 AND ANA/E4162/2007/E-002. THIS IS PERMANENT REPAIR IAW SRAS DOTS-2302/07 4130 WITH SUPPLEMENTARY INSPECTIO TASK OF A DVI OF BLENDED AREAS EVERY 2 YEARS FOR NEW CORROSION DETECTION. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007082100035 20070821 00035 NM 2007 8 21 2007UALA02926 1 20070730 A 3350 POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 649UA 25286 RIGHT SIDE BUSINESS CLASS EXIT STRIP LIGHTING ON AND OFF INTERMITTENTLY. PER FLT ATTENDANT, THE RT SIDE IN FIRST CLASS ONLY & AROUND DOOR 1R HAD THE PROBLEM. REPLACED POWER SUPPLY M1552. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082100039 20070821 00039 NM 2007 8 21 2007UALA02930 1 20070727 A 5754 015T1507157 PANEL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE L/E SLAT PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 644UA 25094 LEFT LEADING.EDGE SLAT NR 1 CLOSURE PANEL HAS 3 INCHES PUNCTURE, CRACKED, APPROX 20 INCHES FROM INBOARD EDGE. PERFORME D TEMPORARY REPAIR PER ENGINEERING VARIATION AUTHORITY. SLAT TO BE PERMANENTLY REPAIRED WITHIN 300 HOURS. PUNCTURE CAU SED BY GROUND EQUIPMENT CONTACT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082100041 20070821 00041 NM 2007 8 21 2007UALA02932 1 20070731 A 5610 WINDOW BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT OPEN A UALA A UNSCHED LANDING W INADEQUATE Q C TO TAKEOFF 1 WP 29 507UA 24743 ON TAKEOFF, FIRST OFFICERS WINDOW OPENED IN FLIGHT. ACCOMPLISHED COMPLETE INSPECTION OF FIRST OFFICER WINDOW RIGGING. A DJUSTED WINDOW MECHANICAL LATCH AND LOCK. LUBED ROLLER AND TRACK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082100053 20070821 00053 NM 2007 8 21 2007UALA02946 1 20070731 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 350UA 24301 LAST 20 FEET OF EEL LIGHT INOPERATIVE IN AFT MAIN CABIN. REPLACED EEL LT POWER CORD OPS CK GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082100063 20070821 00063 NE 2007 8 21 T522007F00000 2 20070626 A 8530 CYLINDER HEAD DHAV DHC2 DHC2* 2800108 EA PWA R985 R985* 52008 NE NR 2 CRACKED E T52C K NONE O OTHER IN INSP/MAINT 1 AL 03 695TK 920 NR 2 CYLINDER WAS FOUND TO HAVE A CRACK ALL THE WAY AROUND THE HEAD JUST ABOVE THE SECOND COOLING FIN. (K) 1 H 7 1 3R 3 R A806 5E1 2007082100078 20070821 00078 NM 2007 8 21 2007UALA02960 1 20070802 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY LIGHT INOPERATIVE OVER DOOR 4L. RELAMPED EEL LIGHT OVER DOOR 4L. OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082100091 20070821 00091 EU 2007 8 21 2007UALA02966 1 20070731 A 2750 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE TE FLAPS MALFUNCTIONED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 403UA 442 FLAPS WOULD NOT GO TO FLAPS 2 WHEN SELECTED. RECEIVED A FLAPS LOCK MESSAGE. FLAPS WOULD NOT LEAVE FLAPS 1. TROUBLESH OOTING PER TSM REVEALED NO FAULTS. NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082100106 20070821 00106 EU 2007 8 21 UPS07150410 1 20070807 A 5320 STRUCTURE AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 144UP 0827 INSPECTION TYPE:N/A MAIN DECK POSITION 1 HAS 1 X 1 INCH HOLE IN FLOOR (INBOARD OF FRONT MCD). PERFORMED INTERIM REPAIR IAW A300 53-10-20 FIG 104. PERM REPAIR WITHIN 350 FLIGHT HOURS. 2 L 7 2 4F RT A35EU 2007082100109 20070821 00109 NM 2007 8 21 UPS07550402 1 20070807 A 3350 LIGHT BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 424UP 25369 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT, UNARMED LAMP INOP. RELAMPED W/REFERENCE TO AMM 33-16-02-2. 2 L 7 2 4F RT A2NM 2007082100117 20070821 00117 WP 2007 8 21 UPS07850396 1 20070721 A 5514 ANGLE DOUG DC8 DC873F 302199F WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 RT HORIZ STAB MOVEABLE FAIRING 2ND AFT H-ANGLE UPPER, CRACKED. REMOVED CRACKED H-ANGLE ON RT HORIZ S TAB MOVEABLE FAIRING IAW SRM 51-03-00-0. FABRICATED AND INSTALLED RT HORIZ STAB FAIRING ATTACH H-ANGLE IAW SRM 51-03-02 , DWG 3702464, AND SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007082100133 20070821 00133 SW 2007 8 21 AC2A116668 1 20070719 A 2432 SM20ACD200A21 RELAY BELL 206 206L1 1182107 SW ALLSN 250B 250B* GL FUSELAGE LOWER UNKNOWN E AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 39LR 45654 RELAY INTERNAL PROBLEM. 1 G 7 1 3U 3 T H2SW E10CE 2007082100134 20070821 00134 NM 2007 8 21 USAA070625 1 20070808 A 5553 BUSHING BOEING 737 737401 1384701 NM ELEVATOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 RIGHT AFT I/B ATTACH FITTING FUW FACE OF BUSHING PITTED & CORRODED, R-8 LUG. REMOVED BUSHING, LUG BORE, FACES CLEANED, INSTALLED NEW BUSHING PER EA 98801; CORR TASK C55-706-11, DEFECT SIZE: .250 X .250 INCH. 2 L 7 2 4F RT A16WE 2007082100138 20070821 00138 NM 2007 8 21 USAA070618 1 20070808 A 5534 LUG BOEING 737 737401 1384701 NM VERTICAL STAB GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 AFT FACE OF L-8 LUG OF VERTICAL FIN GOUGED. REMOVED DAMAGED BUSHING, PITTING & REPLACED BUSHING PER EA 98801. CORROSIO N RESULT OF GOUGE. DEFECT SIZE: .250 INCH. 2 L 7 2 4F RT A16WE 2007082100139 20070821 00139 NM 2007 8 21 USAA070619 1 20070808 A 5514 BUSHING BOEING 737 737401 1384701 NM RT HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 RIGHT HORIZ STAB INTERSPAR BOX STAB STA 0, R7 LUG BORE HAS CORROSION. FAB'D BUSHING INSTALLED INTO BORE PER SRM 55-10-1 0; CORR TASK C53-701-02, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007082100140 20070821 00140 NM 2007 8 21 USAA070620 1 20070808 A 5514 BUSHING BOEING 737 737401 1384701 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 LEFT STAB INTERSPAR BOX STAB STA 0, NR 7 LEFT LUG HAS CORROSION. FAB'D BUSHING INTO REWORKED BORE PER SRM 55-10-10, SB 737-55-1058, CORR LEVEL 2; TASK C53-701-02, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007082100141 20070821 00141 NM 2007 8 21 USAA070621 1 20070808 A 5514 BUSHING BOEING 737 737401 1384701 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 LEFT STAB INTERSPAR BOX TAB STA 0, BUSHING/BORE NR 9 LEFT LUG HAS CORROSION. FAB'D BUSHING, INSTALLED INTO REWORKED BOR E PER SRM 55-10-10, SB 737-55-1058; CORR LEVEL 2, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007082100143 20070821 00143 NM 2007 8 21 USAA070622 1 20070808 A 5534 BUSHING BOEING 737 737401 1384701 NM VERTICAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 BUSHING, VERT STAB LEFT AFT O/B ATTACH FITTING FWD FACE LUG L-5 HAS CORROSION. REMOVED CORROSION, INSTALLED NEW BUSHING S PER EA 98801; CORR LEVEL 2; TASK C55-706-11, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007082100147 20070821 00147 NM 2007 8 21 USAA070624 1 20070808 A 5345 69773083 BRACKET BOEING 737 737401 1384701 NM LT LAVATORY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 LEFT LAV TIE DOWN BRACKET STA 947 LBL 51 CORRODED AROUND MOUNT HOLES. REMOVED & REPLACED TIE DOWN BRACKET; CORR TASK C5 3-107-01; LEVEL 2, DEFECT SIZE: .250 INCH. 2 L 7 2 4F RT A16WE 2007082100153 20070821 00153 NM 2007 8 21 USAA070627 1 20070808 A 5553 LUG BOEING 737 737401 1384701 NM VERTICAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 VERT FWD FACE OF LUG R4 ON FUSELAGE AT 4:00 POSITION HAS CORROSION. REMOVED CORROSION REAMED BORE, CHAMFERED EDGES, INS TALLED NEW BUSHING PER EA 98800; CORR TASK C55-70, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007082100155 20070821 00155 CE 2007 8 21 DJFA2007083 1 20070730 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 740TA RK123 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER INBOARD RIB AND BRACKET ASSEMBLIES, THE RIGHT INBOARD ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRU CTIONS OF THIS AREA ARE OUTLINED IN BEECHJET COMMUNIQUE' NUMBER 70. MAINTENANCE REPLACED THE RIB ASSMEBLY. 2 H 7 2 4F 4 F RT A16SW E25EA 2007082100156 20070821 00156 CE 2007 8 21 DJFA2007084 1 20070731 A 5511 45A210863 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 436LX 6058 RK279 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THI S AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. RIB WAS REPLACED WITH NEW UPGRADED RIB. 2 H 7 2 4F 4 F RT A16SW E25EA 2007082100157 20070821 00157 NM 2007 8 21 USAA070629 1 20070808 A 5534 LUG BOEING 737 737401 1384701 NM VERTICAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 FWD FACE OF L8 LUG ON VERT FIN CORRODED & LITE GOUGE. FAB'D BUSHING PER EA 98801; CORR TASK C55-706-11, DEFECT SIZE: . 25 X .25 INCH. 2 L 7 2 4F RT A16WE 2007082100158 20070821 00158 NM 2007 8 21 USAA070630 1 20070808 A 5534 BUSHING BOEING 737 737401 1384701 NM VERTICAL STAB DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 AFT FACE OF BUSHING, FWD FACE OF R8 LUG ON VERT FIN PITTED. REMOVED PITTING & INSTALLED NEW BUSHING PER EA 98801; CORR TASK C55-706-11, DEFECT SIZE: .250 X .250 INCH. 2 L 7 2 4F RT A16WE 2007082100159 20070821 00159 NM 2007 8 21 USAA070631 1 20070808 A 5553 LUG BOEING 737 737401 1384701 NM VERTICAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 PITTING ON FWD FACE OF L6 LUG ON FUSELAGE CORRODED. REMOVED BUSHING, CLEANED CORROSION & RE-INSTALLED PER EA 98800; COR R TSK C55-706-11, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007082100160 20070821 00160 NM 2007 8 21 USAA070632 1 20070808 A 5553 LUG BOEING 737 737401 1384701 NM VERTICAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 AFT FACE OF L6 LUG ON FUSELAGE VERT STAB LUG CORRODED. REMOVED LUG BUSHING, CORROSION, TREATED & REPLACED PER EA 98800; CORR TASK C55-706-11, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007082100162 20070821 00162 CE 2007 8 21 DJFA2007085 1 20070801 A 7830 20200081 IDLER LINK BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE THRUST REVERSER BROKEN E DJFA O OTHER O OTHER NR NOT REPORTED 1 EA 23 454LX RK327 ON POST FLIGHT, CREW NOTICED THE RT TR FAIRING DAMAGED. MAINTENANCE FOUND THE DRIVER LINK BROKEN. THE IDLER LINK CRACK ED IN TWO PLACES 180 DEG APPART AT THE BEARING WHERE THE ARM IS CONNECTED TO THE TR DOOR CAUSING THE ARM TO SEPARATE FRO M THE BEARING. MAINTENANCE REPLACE THE TR ASSEMBLY. 2 H 7 2 4F 4 F RT A16SW E25EA 2007082100163 20070821 00163 NM 2007 8 21 USAA070623 1 20070808 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 NUT PLATE HOLE, RBL 12, STA 987 CORRODED. REMOVED & REPAIRED T-CAP AREA PER SRM 53-00-01; CORR TASK C53-107-01, DEFECT SIZE: 2 X INCHES. 2 L 7 2 4F RT A16WE 2007082100165 20070821 00165 CE 2007 8 21 DJFA2007086 1 20070802 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 438LX 7324 RK202 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER IB RIB AND BRACKET ASSEMBLIES, BOTH THE RT AND LT IB ROLLER BRACKETS WERE FOUND CRACKED. DETAILED INSPECTION INSTR UCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. MAINTENANCE REPLACED THE RIB WITH UPGRADED RIB ASSMEBLY. 2 H 7 2 4F 4 F RT A16SW E25EA 2007082100168 20070821 00168 NM 2007 8 21 SB07062 1 20070808 A 3350 1012721 LIGHT BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 506AU 23381 DCA - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. MAINTENANCE REPAIRED THE LIGHT ASSEMBLY AT SEAT 22C. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007082100170 20070821 00170 EU 2007 8 21 7217071607 1 20070716 A 6510 11731542 DRIVE SHAFT BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE TAIL ROTOR DAMAGED E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 170MC 7217 FOUND DURING INSPECTION, THE FORWARD TAIL ROTOR DRIVESHAFT WAS FOUND TO HAVE A DEEP GROOVE WORN INTO THE TUBE NEAR THE END OF THE SHAFT EXCEEDING THE MECHANICAL DAMAGE LIMITS. DAMAGE WAS CAUSED BY LOOSE REINFORCING WIRE FROM A NEARBY SCAT TUBE FOR THE AIR CONDITIONING DUCT. THE DUCT HAD SEPARATED EXPOSING THE WIRE. 1 G 7 2 3U 3 U H13EU E5NE10 2007082100172 20070821 00172 NM 2007 8 21 BB07061 1 20070808 A 2130 S210T17043 EXHAUST VALVE BOEING 767 767201 1385125 NM CABIN PRESSURE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 245AY 81860 1531 23897 FLIGHT 706, PHL-FRA: AFTER TAKEOFF, CABIN WOULD NOT PRESSURIZE AND CREW RECEIVED AN EQUIPMENT COOLING VALVE LIGHT. RET URNED TO PHL. MAINTENANCE REPLACED THE OVERBOARD EXHAUST VALVE AND DUCT. NO FURTHER DIFFICULTIES. 2 L 7 2 4F RT A1NM 2007082100173 20070821 00173 NE 2007 8 21 AC2A116707 1 20070805 A 2510 7621002001001 SEAT BACK SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL COCKPIT CRACKED E AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 72649 760292 SEAT BACK FRAME CRACKED. 1 G 7 2 3U 3 U H1NE E1GL 2007082100174 20070821 00174 2007 8 21 AC2A116734 4 20070803 A 3422 BEARING SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL GYRO ROUGH E AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 72649 760292 GYRO REMOVED FOR ROUGH BEARINGS AND LOUD NOISE. 1 G 7 2 3U 3 U H1NE E1GL 2007082100175 20070821 00175 NM 2007 8 21 UIAA07012 1 20070805 A 3244 TIRE DOUG MD90 MD9030 3023690 NM NLG FAILED Z O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 WP 23 17926 53567 BOTH NOSE TIRES EXPLODED AFTER LANDING AT TAXI SPEED WHEN VACATE R/W.2. IAW ND MANUAL MDC93K0393 PART 08 PERFORM NDI/FPI FOR NLG AXLE , NO CRACK WAS FOUND IAW AMM 32-42-01 RPL BOTH NOSE WHEEL/ TIRE ASSY AND SVC TIRE PRESS TO 155 PSI.3. A/C BACK SVC. 2 L 7 2 4F RT A6WE 2007082100176 20070821 00176 NE 2007 8 21 KCSA07062 2 20070808 A 7200 ENGINE BOEING 747 747SR46 1384816 NM PWA JT9 JT9D7A 52054 NE NR 4 MALFUNCTIONED A KCSA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 GL 23 719CK 20923 AT FL 360 AT 0230Z, SMOKE APPEARED IN THE COCKPIT. THREE SECONDS LATER THE NR 4 EGT WENT TO RED LINE, THE RED EGT LIGHT ILLUMINATED, THE OIL QUANTITY WENT TO ZERO, THE OIL PRESSURE WENT TO ZERO, THE OIL TEMPERATURE WENT TO THE RED LINE, AN D N2 WENT TO ZERO. SEVER ENGINE CHECK LIST WAS COMPLETED. N1 GAUGE INDICATED 33 PERCENT, BUT VISUAL OBSERVATION SHOWED NO ROTATION OF THE N1 FAN BLADES. THE COCKPIT SMOKE CEASED AFTER THE IMMEDIATE ACTION ITEMS WERE ACCOMPLISHED. 2 L 7 4 4F 4 F RT A20WE E20EA 2007082100178 20070821 00178 NM 2007 8 21 ASAA0741933 1 20070808 A 5210 65528547 GUIDE ARM BOEING 737 737490 1384715 NM L2 DOOR WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 713AS 30161 L2 DOOR HITTING LEFT TOP OF DOOR FRAME. REPLACED ENTRY DOOR GUIDE ARM. 2 L 7 2 4F RT A16WE 2007082100179 20070821 00179 NM 2007 8 21 ASAA0741935 1 20070809 A 5322 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 FUSELAGE SKIN BULGING. FRAME TO SKIN ATTACH SHEAR TIE REMOVED AND REPLACED IAW SRM 53-00-07 FIG 201 REPAIR 5. 2 L 7 2 4F RT A16WE 2007082100181 20070821 00181 EA 2007 8 21 TRAX200701116 1 20070805 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 931EV 8015 SERVICE DOOR DIFFICULT TO CLOSE. 2 L 7 2 4F RT A21EA 2007082100182 20070821 00182 NM 2007 8 21 KCSA071286 1 20070809 A 5230 SKIN BOEING 747 747249F 1384849 NM CARGO DOOR DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 MAIN DECK CARGO DOOR SKIN IS DAMAGED AT FORWARD LOWER AREA AT STA 1790, WL 221. 2 L 7 4 4F A20WE 2007082100183 20070821 00183 NM 2007 8 21 SCNA07009 1 20070807 A 3350 BATTERY PACK BOEING 737 7378Q8 13844BX NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 805SY 30032 DURING A FUNCTIONAL TEST OF THE EMERGENCY LIGHTS MAINTENANCE FOUND THAT THE LIGHTS AT ROWS 14-18 FAILED THE TEST. MAINT ENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK AND THE LIGHTS OPERATE NORMAL. 2 L 7 2 4F RT A16WE 2007082100184 20070821 00184 CE 2007 8 21 4520578022007 1 20070802 A 7797 CONNECTOR LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE7312 01518 WP WIRE HARNESS DAMAGED E J7SA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 05 616FX 2057 P116741C RT ENGINE OVERTEMP AT 40000 FL, NO OTHER CAS MESSAGES ILLUMINATED. NO VIBES MAINTENANCE WAS ABLE TO DUPLICATE THE SQUAWK WITH JUST BATTERY POWER ON AND NO ENGINES RUNNING. THE ITT MAXED OUT AND THEN WENT TO DASH LINES. AFTER ACCESSING THE W IRING HARNESS, FOUND P205 (2) CLICKS LOOSE. TIGHTENED PAST HAND TIGHT AND OP CHECK GOOD AT HIGH POWER. THIS IS SECOND OC CURRENCE FROM OUR FLEET OF THIS EXACT PROBLEM. THE CONNECTOR PLUG INVOLVED IS A STEEL SHELL, INTERNAL LOCKING PLUG WITH NO SAFETY WIRE PROVISIONS. PUTTING MX PROCEDURES INTO OUR CAMP TO USE CONNECTOR PLUG PLIERS TO TIGHTEN THE PLUG, A BIT P AST HAND TIGHT. HOWEVER, THIS AREA IS NOT NORMALLY ACCESSED EXCEPT FOR HIGHER INTERVAL ENGINE INSPECTIONS AS IT IS LOCA 2 L 7 2 4F 4 F RT T00008WI E6WE 2007082100185 20070821 00185 CE 2007 8 21 GUUA08040701 1 20070804 A 3233 11238002223 ACTUATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NLG LEAKING A GUUA O OTHER J WARNING INDICATION CR CRUISE 1 SO 29 87551 199 UE206 FLIGHT: 9179, DURING FLIGHT RT MAIN LANDING GEAR EXTENDED ON ITS OWN WITH NOSE AND LT STILL RETRACTED. ATTEMPTED TO EXT END LANDING GEAR, AND WAS UNABLE. PERFORMED MANUAL GEAR EXTENSION,GEAR EXTENDED AND LOCKED WITH (3) GREEN LIGHTS. RETU RNED TO FLL LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR ACTUATOR OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007082100186 20070821 00186 CE 2007 8 21 GUUA08010701 1 20070801 A 3260 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG OUT OF ADJUST A GUUA O OTHER J WARNING INDICATION CR CRUISE 1 SO 29 81546 UE187 FLIGHT: 5404, DURING FLIGHT LANDING GEAR HANDLE LIGHT ILLUMINATED. INSPECTED LANDING GEAR SYSTEM RIGGED LT LANDING GEAR UPLOCK SWITCH. LANDING GEAR OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2007082100188 20070821 00188 NM 2007 8 21 SCNA07008 1 20070807 A 3350 BATTERY PACK BOEING 737 7378Q8 13844BX NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 805SY 30032 DURING A TEST OF THE EMERGENCY LIGHTING MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS FROM ROW 19 AND AFT WERE INOP. MAIN TENANCE INSTALLED AND CHARGED A NEW BATTERY PACK AND THE EMERGENCY LIGHTS NOW OP CHECK NORMAL. 2 L 7 2 4F RT A16WE 2007082100189 20070821 00189 NM 2007 8 21 KCSA071287 1 20070809 A 5230 INTERCOSTAL BOEING 747 747249F 1384849 NM CARGO DOOR DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 MAIN DECK CARGO DOOR FRAME INTERCOSTAL IS DAMAGED AT STA 1790, WL 219. 2 L 7 4 4F A20WE 2007082100190 20070821 00190 EU 2007 8 21 7237080807 1 20070808 A 6720 TAIL ROTOR BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101750B1 41560 NE MALFUNCTIONED E QMLA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 911KD 7237 WHILE LANDING AT A HOSPITAL PAD THE AIRCRAFT NOSE TUCKED LT AND BEGAN A UNCOMMANDED RT ROTATION. POWER WAS APPLIED TO CR UISE TORQUE 60 PERCENT AND WAS FLOWN INTO THE RT ROTATION AND BACK TO CRUISE FLIGHT. APPROACH TO HOSPITAL WAS TERMINATE D AND DECIDED TO FLY TO 1H2 AIRPORT AND PERFORM A RUN ON LANDING. WHILE ENROUTE TO AIRPORT, TESTED T/R PEDALS AND AIRCRA FT DID NOT RESPOND TO THE INPUTS. WHILE APPROACH TO LANDING THE AIRCRAFT BEGAN A LT LEAN. RUN ON LANDING WAS ACCOMPLISHE D JUST ABOVE ETL WITHOUT INCIDENT. 1 G 7 2 3U 3 U NC H13EU E5NE10 2007082100191 20070821 00191 SO 2007 8 21 GLBA20060973 1 20070804 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE COCKPIT SMOKE A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 03 293UX 120293 SMOKE/SMELL, FLIGHT 5161, PILOTS REPORTED SMOKE IN THE COCKPIT AFTER STARTING THE ENGINE WITH PACKS OFF AND BLEEDS CLOSE D. BOTH PACK FAIL LIGHTS ILLUMINATED WITH PACKS OFF. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE PACK SYSTEMS IAW MM 21-50. OPERATIONAL CHECKS GOOD WITH NO FAULTS FOUND. 2 L 7 2 4T 4 T RT A31SO E20NE 2007082100192 20070821 00192 EU 2007 8 21 2007F00041 1 20070807 A 6210 BLADE UROCOP EC135 EC135P2 5620027 EU MAIN ROTOR CRACKED E O OTHER O OTHER NR NOT REPORTED 1 EA 23 935MC 409 0485 VISUAL INSPECTION REVEALED CRACK IN M/R BLADE APPROX. 103 INCHES FROM BLADE ROOT. CRACK RUN FROM AFT OF SPAR TO THE TRA ILING EDGE. 1 G 7 2 3U H88EU 2007082100196 20070821 00196 NM 2007 8 21 ASAA0741937 1 20070209 A 5311 65C352436 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 AFT CARGO AFT FRAME EXISTING REPAIRS INSTALLED. REPLACED EXISTING REPAIR FRAME IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007082100199 20070821 00199 CE 2007 8 21 AMWA86499 1 20070807 A 2720 ROD BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RUDDER CONTROL BROKEN A AMWA O OTHER F FLT CONT AFFECTED AP APPROACH 1 CE 07 163YV UE163 ON APPROACH TO GRI, CAPT PEDALS LOST RUDDER CONTROL. CAPT TRANSFERRED CONTROL OF THE ACFT TO THE FO. FO PEDALS HAD RUD DER CONTROL. FO LANDED WITH NO FURTHER INCIDENT. OCCURENCE REPORT FILED. REMOVED AND REPLACED RUDDER INTERCONNECT ROD (ROD END), RIGGED RUDDER. 2 L 7 2 4T 4 T RT A24CE E26NE 2007082100200 20070821 00200 CE 2007 8 21 DJFA2007088 1 20070805 A 2170 18084928 COALESCER BAG BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE DIRTY E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 EA 23 796TA RK289 ON LANDING, CREW REPORTED SMOKE IN THE COCKPIT. SMOKE APPEARED TO BE COMING FROM THE WEMACS; AIRCRAFT LANDED SAFELY. M AINTENANCE FOUND THE COALESCER SOCK DIRTY. THE SOCK WAS REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007082100201 20070821 00201 NM 2007 8 21 ASAA0741939 1 20070209 A 5322 69785041 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 SHEAR TIE CRACKED REPLACED SHEAR TIE IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007082100205 20070821 00205 2007 8 21 AMTA200700366 4 20070727 A 3460 1762000101 COMPUTER BOEING 737 73783N 13844HI NM PWA PT6 PT6A28 EA FLT MANAGE UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 11 305TZ 30706 LT FMC FAILED. REMOVED AND REPLACED LT FMC COMPUTER IAW AMM 34-61-02-4 AND OPS CHECK IAW AMM 34-61-00-5. (K) 2 L 7 2 4F 4 T RT A16WE E4EA 2007082100206 20070821 00206 NM 2007 8 21 USAA920070799 1 20070808 A 5320 143N808725 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 923UW 22203 PIT - MAJOR REPAIR - C4 CHECK, L2 DOOR CUTOUT INTERCOSTAL CRACKED, BS 680, S11L. REPLACED L2 DOOR CUTOUT INTERCOSTAL, B S 660 - BS 686, S11L IAW USAIRWAYS EO 5304R143. 2 L 7 2 4F RT A2NM 2007082100207 20070821 00207 NM 2007 8 21 AMTA20070368 1 20070727 A 2400 CIRCUIT BREAKER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE TRIPPED A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 517AT 27973 APU AUTO SHUTDOWN WHEN APU ELECTRIC SELECTED. GROUND POWER SOURCE CONNECTED TO AC APU BATTERY BUSS CB POPPED. RESET CB AND REMOVED GROUND POWER SOURCE CB STAYS SET. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007082100211 20070821 00211 SO 2007 8 21 N93A09082007 1 20070809 A 5534 1159B2154361 FITTING GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU VERTICAL STAB CORRODED E N93A K NONE O OTHER IN INSP/MAINT 1 SO 13 495QS 9903 1295 DURING INSPECTION FOUND ON VERTICAL STAB ATTACH BULKHEAD AND FITTING CORRODED. 2 L 7 2 4F 4 F RT A12EA E25NE 2007082100213 20070821 00213 NM 2007 8 21 KCSA071290 1 20070809 A 5320 SUPPORT ANGLE BOEING 747 7472B4B 138481B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 AFT PIT SIDE LOCK SUPPORT ANGLE IS DAMAGED AT STA 1700 RBL 65. 2 L 7 4 4F RT A20WE 2007082100214 20070821 00214 CE 2007 8 21 AMWA86534 1 20070808 A 3240 1145800015 BRAKE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG WEAK A AMWA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 07 143YV UE143 WHEN AIRCRAFT LANDED CREW CALLED MAINT CONTROL AND WROTE BRAKES UP AS BEING SPONGY. MAINTENANCE BLED BRAKES, OPS NORMAL . 2 L 7 2 4T 4 T RT A24CE E26NE 2007082100216 20070821 00216 CE 2007 8 21 GUUA08080701 1 20070808 A 3260 39EN66 SQUAT SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG LOOSE A GUUA O OTHER N FALSE WARNING CL CLIMB 1 SO 29 53545 UE185 FLIGHT: 9223 AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. ADJUSTED RT MAIN LANDING GEAR SQUAT SWITCH. LANDING GEAR OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007082100217 20070821 00217 WP 2007 8 21 ASMF200708002 1 20070808 A 3610 12294411 SHUTOFF VALVE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D* NE PNEUMATIC SYS FAILED W ASMF B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 23 216AM 42407 871 49586 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, DUE TO A CABIN PRESSURE FAILURE AT FL340 USING ANTI ICE AND DE ICE FLOW, THIS CONDITION BECOME WORST WHEN TAIL DE ICE WAS USED AND THE PRESSURIZATION WAS UNCONTROLLABLE IN MANUAL AND AUTO. MAINTENA NCE PERSONNEL PERFORMED SYSTEM CHECK IAW MM 36-10-00 MODE 1 AND 2 AND AIR CONDITIONED PACKAGES LEAK TEST IAW MM 21-00- 00, ALL CORRECT. LATER, OVERWEIGHT LANDING CHECK WAS PERFORMED IAW MM 05-51-04 NO DAMAGE WAS FOUND; ADDITIONALLY MAINTE NANCE PERSONNEL REPLACED THE PNEUMATIC REGULATOR PILOT VALVE, THE REGULATOR AIR CONDITIONED PILOT PRESSURE AND THE WING ICE PROTECTION SHUTOFF VALVE LT SIDE IAW MM 36-10-02, MM 21-31-11 AND MM 30-10-02, TESTED ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2007082100218 20070821 00218 NM 2007 8 21 TAMF20070003S 1 20070802 A 5754 SKIN BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE NR 2 SLAT CORRODED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 767QT 23804 DURING C-CHECK INSPECTION (TASK CARD 57-500-00) WAS FOUND A CORROSION ON SLAT NR 2 LOWER SKIN STA OSS 953.48 LT. DAMAGE D AREA WAS REPAIRED IAW MFG SERVICE REQUEST 1-495025537 AND EWO 767-57-022. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007082100219 20070821 00219 NM 2007 8 21 TAMF20070004S 1 20070804 A 5754 SPAR BOEING 767 767200 1385120 NM SLAT CORRODED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 767QT 23804 DURING C-CHECK INSPECTION (TASK CARD 06-099-01-2) WAS FOUND A CRACK ON LOWER CHORD AT FRONT SPAR STA ISS 256-261 RT. DA MAGED AREA WAS REPAIRED IAW MFG SERVICE REQUEST 1-495025865 AND EWO 767-57-020. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F RT A1NM 2007082100220 20070821 00220 NM 2007 8 21 TAMF20070005S 1 20070801 A 5310 141T2939 BEAM BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE NLG WW CORRODED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 767QT 23804 DURING C-CHECK INSPECTION (TASK CARD 53-426-00) WAS FOUND CORROSION ON NLG W/W BULKHEAD, STA 287, CENTER BEAM PN 141T293 9. CORRODED AREA WAS REMOVED IAW SRM 51-10-02 PAG 12-13 AND IT WAS FOUND OUT OF LIMITS (MAX 0.190 IN, MIN 0.160 IN) IAW SRM 53-10-14 FIGURE 101. MFG SERVICE REQUEST 1-496045086 APPROVED THIS BLEND OUT AS CATEGORY A PERMANENT REPAIR. THIS R EPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007082100221 20070821 00221 NM 2007 8 21 TAMF20070006S 1 20070805 A 5754 SPAR BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE SLAT CRACKED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 767QT 23804 DURING C-CHECK INSPECTION (MFG TASK CARD 06-099-01-1) WAS FOUND A CRACK ON LOWER CHORD AT FRONT SPAR STA ISS 256-261 RT. DAMAGED AREA WAS REPAIRED IAW MFG SERVICE REQUEST 1-499965004 AND EWO 767-57-021. THIS REPAIR CONSTITUTES A MAJOR REPA IR. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007082100223 20070821 00223 NM 2007 8 21 TAMF20070008S 1 20070805 A 5411 FRAME BOEING 767 767200 1385120 NM NACELLE DAMAGED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 767QT 23804 DURING INSPECTION OF C-CHECK (MFG TASK CARD 06-091-01-2) WAS FOUND CORE COWL P/N: 224-2301-541 S/N: 0217 WITH ELONGATED HOLE AT FRAME STA NAC 294 - CF6-80C2 ENGINE NR 2. DAMAGED AREA WILL BE REPAIRED IAW CV07-1678-01 AND EWO 767-54-015. 2 L 7 2 4F RT A1NM 2007082100225 20070821 00225 CE 2007 8 21 GLBA20060975 1 20070809 A 5320 SHIM BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 298-300 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 251GL UE251 BELLY SHIM CRACKED AT RT FS 298 TO FS 300 APPROXIMATELY 8.5 INCHES AFT OF WING SPAR. CRACK LENGTH APPROXIMATELY 1.7500 I NCHES. MAINTENANCE INSTALLED PRESSURIZED COVER PATCH AT AFFECTED AREA IAW SRM 51-70. RII INSPECTION COMPLIED WITH IAW TA SKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007082100226 20070821 00226 NM 2007 8 21 ASAA0741942 1 20070730 A 5330 6545776 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 779AS 25111 DENT IN FUSELAGE SKIN. REPAIRED IAW EA 5330 02224 AND SRM 53-00-01 REPAIR 31 DETAIL 9. 2 L 7 2 4F RT A16WE 2007082100227 20070821 00227 EU 2007 8 21 UPS07150418 1 20070808 A 5321 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU CARGO BAY PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 165UP 0005 INSPECTION TYPE:N/A AFT BULK CARGO COMPARTMENT PIT FOUND FLOOR PANEL PUNCTURED. ACCOMPLISHED PERMANENT REPAIR PER SRM 5 3-10-20. 2 L 7 2 4F RT A35EU 2007082100228 20070821 00228 CE 2007 8 21 DJFA2007092 1 20070810 A 2160 LINE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE TEMP CONTROL VA MISINSTALLED E DJFA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 EA 23 743TA RK271 ON CLIMB OUT, CREW REPORTED VERY HOT AIR COMING FROM THE AIR VENTS. CABIN TEMP WAS UNCONTROLLABLE AND REACHED 120 DEG F . AIRCRAFT DIVERTED AND LANDED SAFELY. MAINTENANCE DISCOVERED COCKPIT TEMP CONTROL VALVE LINE SWAPPED WITH CABIN TEMP CONTROL LINE. LINES WERE CORRECTED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007082100229 20070821 00229 CE 2007 8 21 DJFA2007090 1 20070808 A 2910 AE2463739G0166 LINE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HYD SYSTEM FAILED E DJFA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 23 425CW 3877 RK345 DURING PREFLIGHT, CREW NOTED HYDRAULIC FLUID AT THE LT TR AREA. MAINTENANCE FOUND THE HYDRAULIC LINE FOR THE TR ACTUATO R STOW PRESSURE TO HAVE BURST. THE LINE WAS REPLACED 2 H 7 2 4F 4 F RT A16SW E25EA 2007082100231 20070821 00231 CE 2007 8 21 DJFA2007089 1 20070806 A 2910 LINE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HYD SYSTEM LOOSE E DJFA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 EA 23 425CW RK345 ON LANDING CREW REPORTED HYD LOW LEVEL LIGHT WITH 0 QTY INDICATED. BRAKES FAILED AND EMERGENCY BRAKING WAS USED. MAINT ENANCE FOUND A LOOSE HYDRAULIC LINE AT THE PYLON. THE LINE WAS TIGHTENED 2 H 7 2 4F 4 F RT A16SW E25EA 2007082100232 20070821 00232 CE 2007 8 21 DXTA200702399 1 20070813 A 2750 CLUTCH CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS SLIPPED E DXTA O OTHER F FLT CONT AFFECTED LD LANDING 1 GL 07 986QS 7500086 FLAPS INOP. RAN CHECKLIST, DID NOT RESET. 3 DEGREES RESET SWITCH DID NOT WORK. FLAPS FAIL AS SOON AS 5 DEGREES SELECTED. 5 DEGREE FLAPS DID NOT EXTEND. CLUTCH CHECK ON PDU - SLIPPING. REPLACED PDU IAW 750 M/M 27-52-00 RIG AND OPS CHECKED IAW 750 M/M 27-50-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007082100234 20070821 00234 EU 2007 8 21 BAQA200700025 1 20070518 A 7601 945UN01Q4AA8B SWITCH UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE COCKPIT WORN E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 969ME 0089 DURING REGULAR FUNCTIONAL CHECK OF ENGINE START SWITCHES, DISCOVERED THE NR1 AND NR2 ENGINE STARTING SWITCHES TO HAVE WO RN DETENT IN THE SWITCH. THE SWITCH WAS ABLE TO BE MOVED FROM THE FLY POSITION TO THE OFF POSITION WITH OUT PULLING OUT OF DETENT. 1 G 7 2 3U 3 U H88EU E34NE 2007082100236 20070821 00236 SW 2007 8 21 BAQA200700026 1 20070811 A 6410 406016100119 BLADE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TAIL ROTOR FAILED E BAQA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 EA 03 302LE 2142 277 53572 AIRCRAFT DEVELOPED VIBRATION IN CRUISE FLIGHT UPON LANDING DISCOVERED TIP WEIGHT MISSING FROM TAIL ROTOR BLADE. 1 G 7 1 3U 3 U O H2SW E1GL 2007082100237 20070821 00237 WP 2007 8 21 ASMF200708003 1 20070812 A 2910 37723745503 SHUTOFF VALVE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE HYD SYSTEM LEAKING W ASMF D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 214AM 49585 AIRCRAFT RETURN TO PLATFORM DURING TAXI, CREW SELECTED SLATS EXTEND AND THE HYDRAULIC QUANTITY LIGHT TURNED ON. MAINTEN ANCE DETECTED HYDRAULIC LEAK IN RT SYSTEM AND QUANTITY ZERO, SO THE SYSTEM WAS SERVICED AND HYDRAULIC PRESSURE WAS APPLI ED AND THE LEAK WAS LOCATED AT THE RUDDER SHUTOFF VALVE, THIS VALVE WAS REPLACED IAW MM 27-20-09 TESTED CORRECT, ADDITIO NALLY, WATER SEPARATORS OF BOTH AIR CONDITIONED PACKAGES WERE REPLACED IAW MM 21-20-02, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007082100238 20070821 00238 CE 2007 8 21 80807N550CS 1 20070809 A 3240 99124877 BRAKE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE RT MLG SEIZED E Z5FA O OTHER E A VIBRATION/BUFFET FLAME/FIRE LD LANDING 1 EA 63 550CS 346 5605551 UPON LANDING, RT BRAKE WAS SEIZED. BOTH THE WHEEL AND TIRE WERE GROUND DOWN SIGNIFICANTLY. AIRCRAFT STOPPED ON THE RUNWA Y AND CREW EXTINGUISHED A PIECE OF TIRE THAT HAD SHEARED AWAY. BRAKE WAS FROZEN, BRAKE AND WHEEL WERE REPLACED AND AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007082100239 20070821 00239 NM 2007 8 21 UPS07550420 1 20070720 A 5412 311N32713 BULKHEAD BOEING 757 75724APF 1384969 NM NR 1 PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 431UP 25462 INSPECTION TYPE:C NR 1 PYLON AFT BULKHEAD LOWER OUTBOARD CORNER IS CHAFED. BULKHEAD MILL WAS DONE ON TRAV T7/693383 PER PRELIMINARY 1 EA B757-5453-27-A1716. HFEC WAS DONE ON TRAV T7/693383 PER PRELIM EA B757-5453-27-A1716. LENGTH OF BLEN D 2.1 X 1.250W X .080D PER PRELIMINARY 1 EA B757-5453-27-A1716. 2 L 7 2 4F RT A2NM 2007082100241 20070821 00241 SO 2007 8 21 GLBA20060976 1 20070812 A 3200 LANDING GEAR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LEFT UNKNOWN A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 NM 03 297UX 120297 FLIGHT 5146 PILOTS REPORTED IDLE UNLOCK LIGHTS ILLUMINATED ON LANDING CAUSING PACKS TO OVERHEAT RESULTING IN SMOKE IN TH E COCKPIT. MAINTENANCE SERVICED THE LT MAIN LANDING GEAR SYSTEM AND OPERATIONALLY CHECKED THE SYSTEMS WHICH WERE FOUND G OOD IAW MM 12-13 & 32-62 AND 76-13. 2 L 7 2 4T 4 T RT A31SO E20NE 2007082100244 20070821 00244 SO 2007 8 21 GLBA20060977 1 20070813 A 2100 922FS26A6N735 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RIGHT MALFUNCTIONED A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 03 297UX 120297 SMOKE/SMELL FLIGHT 5010 PILOTS REPORTED THE IDLE UNLOCK LIGHT ILLUMINATED IMMEDIATELY AFTER LIFTOFF. LIGHT EXTINGUISHED AFTER 3-4 MINUTES. LIGHT ILLUMINATED AGAIN AT TOUCHDOWN ACCOMPANIED BY SMOKE IN THE COCKPIT. MAINTENANCE REMOVED AND R EPLACED THE LANDING GEAR RELAY BOX AND OPERATIONALLY CHECKED THE SYSTEM IAW MM 32-31 ON GROUND ALL OK. SUBSEQUENT OPERA TIONAL CHECK FLIGHT WAS UNSATISFACTORY. MAINTENANCE REMOVED AND REPLACED THE RT AIR/GROUND PROX SENSOR IAW MM 32-01. RII INSPECTION COMPLIED WITH IAW GMM 4.3.8. 2 L 7 2 4T 4 T RT A31SO E20NE 2007082100002 20070821 00002 EA 2007 8 21 A6WA200740384 1 20070615 A 5730 PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 434AW 7322 RT WING PLANK AT PANEL 640BB HAS CORROSION APPROX .004 DEEP X 4 INCH LONG X .2500 INCH WIDE IN NON-CRITICAL AREAS. MAIN TENANCE PERFORMED MAJOR REPAIR TO WING PLANK ACCESS HOLE AT WS 54.897 (RT) BY REMOVING CORROSION IN NON-CRITICAL AREAS O F HOLE IAW REO 601R-57-21-030, REF F. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082100006 20070821 00006 EA 2007 8 21 A6WA200740386 1 20070711 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 602 DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 461AW 7870 LT SIDE LOWER FUSELAGE SKIN DAMAGED 3 INCHES AFT OF FS 605 BETWEEN STRINGERS 24L AND 25L. DENT MEASURES 4.25 X 4.75 INC HES AND CREASE MEASURES 4.25 INCHES X 0.095 INCHES DEEP. (K) MAINTENANCE REPAIRED LT LOWER SKIN DAMAGE USING EXTERNAL DOUBLER IAW BSC EO 601R-53-12317. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082100010 20070821 00010 EA 2007 8 21 A6WA200740389 1 20070707 A 5320 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 527 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 409AW 7447 CHANNEL (PN 601R75262-159) IN LT MLG WHEEL WELL CRACKED. (K) MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED A NEW B RACKET, P/N 601R75262-159 IAW CRJ SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082100012 20070821 00012 EA 2007 8 21 A6WA200740391 1 20070707 A 5320 601R75262153 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 520 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 409AW 7447 Z-ANGLE (PN 601R75262-153) IN RT MLG WHEEL WELL IS CRACKED. (K) MAINTENANCE INSTALLED SERVICEABLE ANGLE P/N 601R75262- 153 IAW CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082100020 20070821 00020 2007 8 21 2007UALA02919 4 20070730 A 2565 WEBBING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE GIRT BAR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 PASSENGER ENTRY-SERVICE DOORS L FWD EVAC SLIDE ARM LEVER DIFFICULT TO POSITION. REPOSITIONED SLIDE GIRT BAR WEBBING FRO M DOOR ARMING MECHANISM. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082100023 20070821 00023 NM 2007 8 21 2007UALA02922 1 20070730 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 AFT PIT FRAME DENTED AT STA 1480 AND STR 25L. MAJOR REPAIR ACCOMPLISHED: ROUTED OUT DAMAGED AREA. FABRICATED AND INST ALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082100049 20070821 00049 NE 2007 8 21 2007UALA02941 2 20070731 A 7297 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE DAMAGED A UALA D RETURN TO BLOCK X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 518UA 24871 726528 CREW REPORTS: LEFT ENG STARTED NORMAL, DURING RT ENG START, LEFT ENG SPOOL DOWN & FLAMED OUT, LEFT SPAR VALVE LIGHT CAM E ON & LEFT VALVE LIGHT ALSO CAME ON. ON TROUBLESHOOTING FOUND ACTUATOR CONNECTOR PIN 5 BROKEN. REPINNED WIRE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082100062 20070821 00062 EU 2007 8 21 COEA0703912 1 20070727 A 5311 S53675103204 FRAME AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE FUSELAGE DAMAGED A COEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 13 912FX 047 IN HEAVY CHECK AT COE, FOUND TOOLING DAMAGE ON FUSELAGE FRAME 42 AFT PRESSURE BULKHEAD RT LWR DOUBLER. DAMAGE DOUBLER C UT AWAY AND SPLICE PERFORMED IAW ATR SRAS DO/TS-2637/07 4169. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007082100094 20070821 00094 NE 2007 8 21 2007UALA02968 2 20070801 A 7230 BLADE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE HPC DAMAGED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 215UA 30221 777104 RTFL UNDER AMBER ALERT AFTER EXPERIENCING SURGE ON NR 2 ENGINE. ENGINE WAS REPLACED AT SFO. SHOP TEARDOWN FOUND HEAVY HPC BLADE DAMAGE THROUGHOUT THE COMPRESSOR. THE DAMAGE RESULTED FROM LIBERATION OF OF SEVERAL STAGE-6 VARIABLE STATOR VANE TRUNNION 'BUTTONS'. THIS IS A KNOWN INDUSTRY PROBLEM. CURRENT FIXES ARE TO RTV THE INNER SHROUD CAVITIES TO CONTA IN BROKEN BUTTONS, AND PREVENT THEM FROM ENTERING THE GASPATH. THE SECOND FIX IS TO INSTALL NEW MATERIAL INNER TRUNNION BUSHINGS THAT ARE MORE RESISTANT TO WEAR. UA INCORPORATES BOTH AT HPC REBUILD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007082100098 20070821 00098 2007 8 21 2007UALA02970 4 20070801 A 2565 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 497UA 1847 DOOR 2R SLIDE BOTTLE PRESSURE LOW. 09-07-07 SERVICE DOOR SLIDE BOTTLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082100105 20070821 00105 NM 2007 8 21 2007UALA02973 1 20070801 A 3510 OXYGEN MASK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 833UA 1401 F/O'S OXYGEN MASK WILL NOT TEST. NO SHOP FINDINGS COULD BE LOCATED FOR THIS UNIT- FO'S O2 BOX WAS REPLACED ON AIRCRAFT - NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082100120 20070821 00120 WP 2007 8 21 UPS07850405 1 20070807 A 3350 BATTERY DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY UNIT PER MM 33-50-01-2. OPS CH ECK GOOD. 2 L 7 4 4F RT 4A25 2007082100128 20070821 00128 EA 2007 8 21 TRAX200701108 1 20070724 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 833AS 7246 FS 484 RIGHT INTERCOSTAL O/B SIDE UNDER FLOOR PANEL 262DRF CRACKED. 2 L 7 2 4F RT A21EA 2007082100145 20070821 00145 WP 2007 8 21 ASMF200708001 1 20070802 A 2710 38546421 PLATE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE SPIRAL DRIVE BROKEN W ASMF O OTHER F FLT CONT AFFECTED CR CRUISE 1 SW 23 754RA 49641 CAPTAIN REPORTED THAT DURING CRUISE THE AILERON GOT STUCK WHEN THE COMPENSATOR KNOB IS TURNED TO THE RT SIDE. DURING CHE CK, A SCREW WAS DAMAGED AND PLATE SPIRAL DRIVE BROKEN. THEY WERE REPLACED AND TRIM WAS PERFORMED TO CONTROL MECHANISM IA W MM 27-10-07, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007082100148 20070821 00148 CE 2007 8 21 DJFA2007080 1 20070724 A 5510 45A630824 BRACKET BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 439LX 6074 RK284 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER IB RIB AND BRACKET ASSEMBLIES, THE RT ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS A REA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. THE RIGHT AND LEFT RIB ASSEMBLIES WERE REPLACED WITH THE NEW IMPROVED RIB ASS EMBLIES. 2 H 7 2 4F 4 F RT A16SW E25EA 2007082100149 20070821 00149 CE 2007 8 21 DJFA2007081 1 20070725 A 5511 45A630824 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 796TA 5950 RK289 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER IB RIB AND BRACKET ASSEMBLIES, THE RT ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AR EA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. THE RIGHT AND LEFT RIB ASSEMBLIES WERE REPLACED WITH THE NEW IMPROVED RIB ASSE MBLIES. 2 H 7 2 4F 4 F RT A16SW E25EA 2007082100150 20070821 00150 NM 2007 8 21 USAA070634 1 20070808 A 5553 BUSHING BOEING 737 737401 1384701 NM VERTICAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 BUSHING & FLANGE, VERT AFT FACE OF R5 LUG ON FUSELAGE AT 5:00-9:00 POSITION HAS CORROSION. REPLACE FLANGE BUSHING, BLEN DED FLANGE TO REMOVE DAMAGE TREATED PER EA 98800; CORR TASK C55-706-01, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007082100152 20070821 00152 NM 2007 8 21 USAA070626 1 20070808 A 5534 BUSHING BOEING 737 737401 1384701 NM VERTICAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 R5 O/B AFT ATTACH FITTING FWD FACE OF BUSHING PITTED, R5 LUG HAS CORROSION. REMOVED BUSHING, CORROSION & INSTALLED NEW BUSHING PER EA 98801; CORR TSK C55-706-11, DEFECT SIZE: .250 X .250 INCH. 2 L 7 2 4F RT A16WE 2007082100154 20070821 00154 NM 2007 8 21 USAA070628 1 20070808 A 5534 LUG BOEING 737 737401 1384701 NM VERTICAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 RIGHT AFT I/B ATTACH FITTINGG FUW FACE OF BUSHING R8 LUG ON VERT FIN HAS CORROSION. FAB'D BUSHING & INSTALLED PER SOMP 20-50-03 BOEING DWG 65-52274; EA 98801; CORR TASK C55-706-01, DEFECT SIZE: .250 X .250 INCH. 2 L 7 2 4F RT A16WE 2007082100161 20070821 00161 NM 2007 8 21 USAA070633 1 20070808 A 5553 LUG BOEING 737 737401 1384701 NM VERTICAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 PITTED & CORRODED VERT FWD FACE OF L4 LUG ON FUSELAGE. REMOVED BUSHING & BLENDED LUG TO REMOVE CORROSION, TREATED & REP LACED PER EA 98800; CORR TASK C55-70, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007082100187 20070821 00187 EA 2007 8 21 TRAX200701069 1 20070726 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 854AS 7382 AAR-Z2020 280 AFT ANGLE COMMON TO THE EMERGENCY RELEASE CABLE OB OF LBL 9 IS CRACKED. (RESOLVED ON W/O: 65467 TASKCARD: N/R-00059 ) DUPLICATE WRITE-OFF. {SUPPLEMENTAL - SDR CLOSED 08/08/07} 2 L 7 2 4F 4 F RT A21EA E15NE 2007082100198 20070821 00198 NM 2007 8 21 ASAA0741938 1 20070209 A 5320 INTERCOSTAL BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 INTERCOSTAL CRACKED. REPLACED INTERCOSTAL IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007082100222 20070821 00222 NM 2007 8 21 SB07063 1 20070809 A 2133 106120923 RELIEF VALVE BOEING 737 7374B7 1384702 NM CABIN PRESSURE LEAKING A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 443US 87608 4744 24842 CLT - FLT923 EN ROUTE FROM CLT TO ORD, CLIMBING THROUGH FL250, THE CABIN ALTITUDE EXCEEDED 10,000 FEET AND WAS CLIMBING 1,500 FEET PER MINUTE WITH OUTFLOW VALVE SHOWING FULL CLOSED. FLIGHT DESCENDED TO 10,000 FEET AND RETURNED TO FIELD AT CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT-HAND SAFETY RELIEF VALVE LEAKING. REPLACED V ALVE PER MM 21-31-00. PRESSURIZED AIRCRAFT. OPERATIONAL CHECK OF SYSTEM GOOD. 2 L 7 2 4F RT A16WE 2007082100224 20070821 00224 EA 2007 8 21 TRAX200701076 1 20070729 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 873AS 7549 TRANSVERSE BEAM CORRODED BY SERVICE DOOR FS 349.00. PERFORMED EC/TC 601R-53-21-788 ON TRANSVERSE BEAM BY SERVICE DOOR A T STA 349. JOB COMPLETE. SUPPLEMENTAL - SDR CLOSED 08/10/07. 2 L 7 2 4F RT A21EA 2007082100242 20070821 00242 WP 2007 8 21 UPS07850413 1 20070808 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK PER MM 33-50-01. OPS CHE CK GOOD. 2 L 7 4 4F RT 4A25 2007082100245 20070821 00245 WP 2007 8 21 UPS07850419 1 20070803 A 5313 3779762U501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 680 L10R FWD. REMOVED AND REPLACED LONGERON END FITTING AT STA 6 80 L10R FWD IAW SRM 51-3-0, SRM 51-1-21D, AND 51-01-23. 2 L 7 4 4F RT 4A25 2007082100247 20070821 00247 WP 2007 8 21 UPS07850422 1 20070809 A 2560 ESCAPE ROPE DOUG DC8 DC871F 302199D WP COCKPIT DEPLOYED A IPXA K NONE O OTHER TO TAKEOFF 1 SO 01 755UP 46055 INSPECTION TYPE:N/A CAPTAINS ESCAPE ROPE AND COVER CAME OUT DURING T/O IN PHL. RESTOWED ROPE. OPS NORMAL. 2 L 7 4 4F RT 4A25 2007082100249 20070821 00249 NM 2007 8 21 UPS07M50421 1 20070517 A 5330 SKIN DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C CTR CARGO UNDERFLOOR SPACE STA 5-11 LONGERON R51, SKIN & ATTACHMENTS FOUND WITH CORROSION AS MARKED. CORROSION THROUGH SKIN TRIMMED OUT AS PER EN1397-07. HFEC INS C/OUT PER DAC NDTSPM R.13 06-10-01.001 FOUND NO CRACK EVI DENT. REPAIR I/O DBLR, FINGER DBLR & FILLER 02EA FAB PER EN1397-07. REP PARTS FASTENER HOLES P/UP PER EN1397-07. REPA IR FINGER DOUBLER, INNER DOUBLER & OUTER DOUBLER INSTALLED PER EN1397-07. 2 L 7 3 4F RT A22WE 2007082100250 20070821 00250 EA 2007 8 21 TRAX200701117 1 20070806 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 683BR 7692 CABIN CEILING EMERGENCY LIGHT 2ND FROM AFT INOP. 2 L 7 2 4F RT A21EA 2007082100252 20070821 00252 EA 2007 8 21 TRAX200701123 1 20070806 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 755EV 10185 LEFT SIDE SEAT RAIL HAS CORROSION IN ONE PLACE AFT OF EMERGENCY DOOR (MARKED IN RED). 2 L 7 2 4F RT A21EA 2007082100256 20070821 00256 EU 2007 8 21 TRAX200701128 1 20070806 A 3350 SIGN AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 630AS 336 EMERGENCY EXIT SIGN BY PAX DOOR IS INOP. 2 H 7 2 4T RT 2007082100260 20070821 00260 EA 2007 8 21 TRAX200701130 1 20070807 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 740EV 10151 G2 EMERGENCY LIGHT BY SERVICE DOOR HAS SEVERAL INOP BULBS. 2 L 7 2 4F RT A21EA 2007082100261 20070821 00261 EU 2007 8 21 TRAX200701131 1 20070807 A 5320 INTERCOSTAL AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 LEFT INTERCOSTAL BETWEEN 36-38 CORRODED. 2 H 7 2 4T RT 2007082100262 20070821 00262 EU 2007 8 21 TRAX200701132 1 20070807 A 5210 SKIN AEROSP ATR72 ATR72 EU PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 PAX DOOR FWD CORNER CRACK FOUND ON INNER SKIN. PAX DOOR BTM FWD CORNER CRACK ON INNER SKIN REPAIRED AS PER SRM 52-11-10 FIG 414 2 H 7 2 4T RT 2007082100265 20070821 00265 CE 2007 8 21 DXTA200702405 1 20070815 A 3260 INDICATOR CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE MLG INOPERATIVE E DXTA O OTHER P NO WARNING INDICATION LD LANDING 1 GL 07 660QS 5605647 LT MAIN GEAR LIGHT FAILED TO ILLUMINATE CHECKED BULB VIA ROTARY SWITCH. BULB WAS GOOD. PERFORMED EMER GEAR EXTENSION CHE CK LIST AND LANDED OK GOT AUDIO GEAR WARNINGS TO TOUCH DOWN. REMOVED AND REPLACED LEFT MAIN LANDING GEAR ACTUATOR. WIT H REPAIRED ACTUATOR FROM CESSNA RS CNQR918C. OPERATIONAL AND LEAK CHECK GOOD. WORK DONE PER 560XL MM CH 32-30-04. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007082100266 20070821 00266 CE 2007 8 21 DXTA200702406 1 20070815 A 3240 VALVE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE BRAKES FAILED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 341QS 5600341 BRAKES FAILED ON LANDING. REMOVED AND REPLACED BRAKE BLEED VALVE WITH NEW , PERFORMED FUNCTIONAL CHECKED GOOD. I.A.W. 5 60 M/M 32-42-04. NO LEAKS NOTED P/N 77B62 REMOVED AND REPLACED ANTISKID SERVO VALVE WITH OVERHAULED ASSY. PERFORMED FUNC TIONAL CHECK, CHECKED GOOD I.A.W. 560 M/M 32-42-05. NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A22CE E25EA 2007082100271 20070821 00271 EA 2007 8 21 TRAX200701135 1 20070807 A 2560 BATTERY CNDAIR CL600 CL6002B19 1900309 EA DEFIBRILLATOR DISCHARGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 841AS 7300 DEFIB BATTERY DEAD. AED, AUTOMATIC EXTERNAL DEFIBRILLATOR, AND/OR ASSOCIATED EQUIPMENT. 2 L 7 2 4F RT A21EA 2007082100278 20070821 00278 EA 2007 8 21 TRAX200701138 1 20070807 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 718EV 10095 F/A FLASHLIGHT FWD WILL NOT STAY ON. 2 L 7 2 4F RT A21EA 2007082100282 20070821 00282 EU 2007 8 21 TRAX200701142 1 20070808 A 5320 BRACKET AEROSP ATR72 ATR72 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 CRACK FOUND ON OMEGA BRACKET ON RIGHT SIDE OF FR 39 BETWEEN STR 10R-9R. 2 H 7 2 4T RT 2007082100283 20070821 00283 EA 2007 8 21 TRAX200701143 1 20070808 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 684BR 7708 ASD BOTTOM STEP CRACKED. 2 L 7 2 4F RT A21EA 2007082100290 20070821 00290 EA 2007 8 21 TRAX200701145 1 20070809 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 833AS 7246 MAIN PASSENGER DIFFICULT TO OPEN AND TO LOCK CLOSE. INITIAL ATTEMPT TO OPEN FROM OUTSIDE WAS TOO HARD TO TURN OUTER HAN DLE AND UNLOCK DOOR. 2 L 7 2 4F RT A21EA 2007082100292 20070821 00292 EA 2007 8 21 TRAX200701146 1 20070809 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 835AS 7258 PAX DOOR HANDLE MSG. EN ROUTE TO MLI A/C DIVERTED TO CHA DUE TO MTC. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007082100293 20070821 00293 NM 2007 8 21 SWAA073956 1 20070809 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED SPV CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007082100294 20070821 00294 NM 2007 8 21 SWAA073972 1 20070809 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 237WN 34632 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007082100300 20070821 00300 NM 2007 8 21 SWAA073970 1 20070809 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 494, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007082100307 20070821 00307 NM 2007 8 21 DHL2007741544 1 20070809 A 5313 BAC1498145 STRINGER BOEING 727 7272Q9 138448M NM BS 720 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 CORROSION INSIDE STR 27R, AT BS 720 TO 720+10. CUT OUT DAMAGED STR SECTION, 22 LONG, FABRICATED NEW STR SECTION FROM BA C 1498-145 EXTRUSION, 22 LONG, PO NR 9005461, AND SPLICE, 1 EA, FROM BAC 1498-131 EXTRUSION, 12 LONG, PO NR 7232174, PER B727 SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9. TREATED, PRIMED, AND INSTALLED STR REPAIR PER B727 SRM 51-10-2 AND 53-10-3 F IG 3, USING NEW SPLICE AND EXISTING SPLICE. 2 L 7 3 4F RT A3WE 2007082100308 20070821 00308 NM 2007 8 21 DHL2007741545 1 20070723 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 880 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 CRACK NOTED ON LT LOWER CHORD OF KEEL BEAM AT BS 880. GAINED ACCESS AS REQ, TRIMMED DAMAGE AT UPPER FLANGE OF KEEL BEAM CHORD, APPROX 1 BY 2, PER SB 727-53-208 FIG 3. CRACK REMOVAL CONFIRMED BY HFEC METHOD. FABRICATED DOUBLER REPAIR FROM 15.5 PH STEEL, .071 BY 8.5 BY 3.625, PO NR 6522231, HEAT TREATED REPAIR DOUBLER TO 170-190 KSI, PER SB 727-53-208 FIG 3, REF PO NR 7232119 FOR HEAT TREAT. CAD PLATED REPAIR DOUBLER PER SB 727-53-208 AND FASI FORM NR FAS0036 REV 4. TREAT ED, PRIMED, AND INSTALLED DOUBLER REPAIR PER B727 SRM 51-10-2 AND SB 727-53-208 FIG 3. RETURNED AREA TO NORMAL. 2 L 7 3 4F RT A3WE 2007082100309 20070821 00309 NM 2007 8 21 DHL2007741546 1 20070809 A 5313 BAC1498131 STRINGER BOEING 727 7272Q9 138448M NM BS 1013 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AFT PIT, BS 1013, AT STR 29L, CORROSION NOTED. CORROSION LIMITED TO STR SPLICE. REMOVED SPLICE SECTION, FABRICATED NEW SPLICE FROM BAC1498-131 EXTRUSION, 14.75" LONG, PO NR 7232174. TREATED, PRIMED, AND INSTALLED NEW SPLICE SECTION, PER B727 SRM 51-30-5, 53-10-3 FIG 1, 51-10-2, AND 51-30-2. 2 L 7 3 4F RT A3WE 2007082100310 20070821 00310 NM 2007 8 21 DHL2007741547 1 20070810 A 5330 SKIN BOEING 727 7272Q9 138448M NM BS 950D-950E GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 GOUGE NOTED AT FWD UPPER CORNER OF C2 DOOR CUT-OUT, EXT FUSE, AT BS 950E ABOVE STR 18R. REMOVED ADJACENT FASTENERS, AND BLENDED OUT GOUGE: ORIGINAL MATERIAL 0.138, MAT REMOVED 0.028, BLEND EXCEEDS LIMITS PER B727 SRM 53-30-1FIG 1 AND 2. FABRICATED REPAIR DOUBLER FROM 2024-T3, .080 BY 17 BY 16.5, PO NR 9005551, PER BOEING SERVICE REQUEST (BSR) NR 1-4605699 07. TREATED, PRIMED, AND INSTALLED REPAIR DOUBLER PER B727 SRM 51-10-2 , BSR NR 1-460569907, AND BAC SUPPLIED FORM 8100 -9 DATED 8/7/2007. 2 L 7 3 4F RT A3WE 2007082100311 20070821 00311 NM 2007 8 21 DHL2007741548 1 20070808 A 5347 BAC1520792 SEAT TRACK BOEING 727 7272Q9 138448M NM BS 480-740 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 CABIN SEAT TRACK CORRODED AT RBL 45.0, FROM BS 480-680, 690-720, AND 720-740. CORROSION EXCEEDS LIMITS IN SEVERAL AREAS . REMOVED SEAT TRACK SECTION FROM BS 480 TO 740, FABRICATED NEW SEAT TRACK SECTION FROM BAC1520-792 EXTRUSION, 400 LONG , PO NR 9004831, 3 TRACK SPLICES FROM 7075-T6, .250 BY 8.1 BY 1.9, PO NR 9003467, AND 6 EA ANGLE REPAIRS FROM BAC1503-10 0122 EXTRUSION, 14 LONG, PO NR 9005537, PER B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 1. TREATED, PRIMED, AND INSTALLED NE W SEAT TRACK SECTION, SPLICES, AND ANGLE REPAIRS PER B727 SRM 51-10-2, 51-30-2, AND 51-30-5 FIG 1. 2 L 7 3 4F RT A3WE 2007082100312 20070821 00312 NM 2007 8 21 DHL2007741549 1 20070808 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 720 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 DENT ON FRAME AT BS 720, BETWEEN STR 24L AND 25L. CUT OUT DAMAGED AREA, DIMENSIONS 1.75 BY 1.875,; FABRICATED REPAIR D OUBLER FROM 7075-T0, .063 BY 15.875 BY 3.75, PO NR 9005314, PER B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3. HEAT TREATED DOUBLER TO T-6 CONDITION PER FASI ER NR 2-37153-801 REV A. TREATED, PRIMED, AND INSTALLED REPAIR DOUBLER, PER B727 SRM 51-10-2 AND 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2007082100313 20070821 00313 NM 2007 8 21 DHL2007741550 1 20070808 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 320 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 NOSE SECTION INTERIOR, HORIZ WALKWAY BEAM, BS 320, FRAME CORRODED BETWEEN STR 25R AND 26R. CUT OUT DAMAGED AREA, DIMENS IONS 24.125 IN LENGTH, FABRICATED FRAME REPAIR, AND DOUBLER FROM 7075-T0, .040 BY 17.0 BY 5.0, PO NR 9004201 (FRAME SEC T), AND 11 BY 5 (DOUBLER), PER B727 SRM 51-40-3 FIG 1, 51-30-5, 51-20-1, AND 53-10-2 FIG 1. HEAT TREATED FRAME REPAIR AND DOUBLER TO T-6 CONDITION PER FASI ER NR 2-37153-801 REV A. TREATED, PRIMED, AND INSTALLED FRAME REPAIR AND DOUBLER, PER B727 SRM 51-10-2 AND 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2007082100314 20070821 00314 NM 2007 8 21 DHL2007741551 1 20070726 A 5311 FRAME BOEING 727 7272Q9 138448M NM 950C DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AFT PIT, BS 950C AT STR 26R, FRAME DENTED AT UPPER CAP. CUT OUT DAMAGED AREA, DIMENSIONS 2.125 BY 1.187; FABRICATED RE PAIR DOUBLER FROM 7075-T0, .071 BY 25 BY 4.0, PO NR 9004690, PER B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 5. HEAT TREATED DOUBLER TO T-6 CONDITION PER FASI ER NR 2-37153-801 REV A. TREATED, PRIMED, AND INSTALLED REPAIR DOUBLER, PER B727 SRM 51-10-2 AND 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2007082100315 20070821 00315 NM 2007 8 21 DHL2007741552 1 20070803 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 970 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AFT PIT, BS 970 BETWEEN STR 23L & 24L, FRAME DENTED. CUT OUT DAMAGED AREA, DIMENSIONS 1.5 BY 1.75; FABRICATED REPAIR D OUBLER FROM 7075-T0, .071 BY 16 BY 3.813, PO NR 9004690, PER B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 5. HEAT TREATED DOU BLER TO T-6 CONDITION PER FASI ER NR 2-37153-801 REV A. TREATED, PRIMED, AND INSTALLED REPAIR DOUBLER, PER B727 SRM 51- 10-2 AND 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2007082100316 20070821 00316 NM 2007 8 21 DHL2007741553 1 20070726 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 990 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AFT PIT, BS 990 AT STR 26L, FRAME DENTED. CUT OUT DAMAGED AREA, DIMENSIONS 1.0 BY .625; FABRICATED REPAIR DOUBLER FRO M 7075-T0, .071 BY 10 BY 4.25, PO NR 9004690, PER B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 5. HEAT TREATED DOUBLER TO T-6 CONDITION PER FASI ER NR 2-37153-801 REV A. TREATED, PRIMED, AND INSTALLED REPAIR DOUBLER, PER B727 SRM 51-10-2 AND 51 -40-3 FIG 1. 2 L 7 3 4F RT A3WE 2007082100317 20070821 00317 NM 2007 8 21 DHL2007741554 1 20070731 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 950B DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AFT PIT, BS 950B BETWEEN STR 23R AND 26R, FRAME DENTED 2 PLACES. CUT OUT DAMAGED AREA’S, DIMENSIONS 1.187 BY 1.688, AND 1.187 BY 1.125; FABRICATED REPAIR DOUBLER FROM 7075-T0, .071 BY 16.5 BY 4.063, PO NR 9004690, PER B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 5. HEAT TREATED DOUBLER TO T-6 CONDITION PER FASI ER NR 2-37153-801 REV A. TREATED, PRIMED, AND INS TALLED REPAIR DOUBLER, PER B727 SRM 51-10-2 AND 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2007082100318 20070821 00318 NM 2007 8 21 DHL2007741555 1 20070812 A 5320 WEB BOEING 727 7272Q9 138448M NM BS 298-350 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 NOSE SECTION INTERIOR HORIZ WALKWAY BEAM WEB AT BS 298 TO 350, LT SIDE, CORRODED IN SEVERAL AREAS. CORROSION REMOVAL EX CEEDS ALLOWABLE LIMITS. REMOVED WEB SECTION, FABRICATED NEW WEB SECTION FROM 2024-T3, .040 BY 56 BY 10.125, PO NR 90054 00, PER B727 SRM 53-10-2 FIG 2 AND 51-20-1. TREATED, PRIMED, AND INSTALLED WEB SECTION PER B727 SRM 51-10-2 AND 51-30-2 . 2 L 7 3 4F RT A3WE 2007082100319 20070821 00319 NM 2007 8 21 DHL2007741556 1 20070812 A 5310 65198620 BEAM BOEING 727 7272Q9 138448M NM BS 300 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 NOSE SECTION INTERIOR, HORIZ WALKWAY BEAM RT SIDE MID CHORD CORRODED AT FWD END, BS 300. CORROSION REMOVAL EXCEEDS ALLO WABLE LIMITS. GAINED ACCESS AS REQUIRED. REMOVED RT MID CHORD, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW MI D CHORD, P/N 65-1986-20, PER B727 SRM 51-10-2, 51-30-2, 51-30-5, AND 53-10-1 FIG 1. RETURNED AFFECTED AREA TO NORMAL. 2 L 7 3 4F RT A3WE 2007082100320 20070821 00320 NM 2007 8 21 DHL2007750001 1 20070813 A 5322 BAC1505100246 SHEAR TIE BOEING 727 7272M7 138407S NM BS 700 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 WHILE AT FLIGHTSTAR AIRCRAFT SERVICES FOR AN A CHECK.REFERENCE ASTAR N/RS 093661,093687 DISCREPANCY: PILLOWING AT FASTEN ERS ON FUSELAGE SKIN BS 700 BETWEEN STRINGER 25R-26R. REMOVED SHEAR TIE AT BS 700 BETWEEN S25R-26R. REMOVED CORROSION O N INNER SKIN MAT LOSS .005",ORIG. THK .080" REMAINING IS .075 AND IS WITHIN LIMITS B727 SRM 53-30-1 FIG1 AND 53-10-2 FIG 5. TREATED AND PRIMED INNER SKIN IAW B727 SRM 53-10-2. FABRICATED NEW SHEAR TIE P/N BAC1505-100246 PO NR 650418 7" IA W B727 SRM 53-10-2 FIG3 AND 51-20-01 FIG 7. TREATED AND PRIMED SHEAR TIE IAW B727 SRM 51-10-2. INSTALLED SHEAR TIE IAW B727 SRM 51-30-2 FIG 4. 2 L 7 3 4F A3WE 2007082100322 20070821 00322 NM 2007 8 21 DHL2007750502 1 20070813 A 5320 SUPPORT ANGLE BOEING 727 7272M7 138407S NM BS 1243 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 AFT AIRSTAIRS BS 1243 LT UPPER SUPPORT ANGLE CRACKED INSIDE OF TORQUE BOX. REMOVED CRACKED ANGLE IAW B727 SRM 51-30-2 F IG7. FABRICATED NEW ANGLE 7075-0 .063 PO NR 9005314 29 1/4" BY 4 3/4" IAW B727 SRM 53-10-2 FIG 6 AND 51-20-1. HEAT TRE ATED NEW PART TO 7075-T6 PER FASI ER NR 2-37153-801 REVA TREATED AND PRIMED PART IAW B727 SRM 51-10-2. INSTALLED ANGLE IAW B727 SRM 51-30-2 FIG 4. 2 L 7 3 4F A3WE 2007082100324 20070821 00324 NM 2007 8 21 SWAA073966 1 20070809 A 5330 6545767 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED HOU CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 466, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007082100325 20070821 00325 NM 2007 8 21 DHL2007750503 1 20070813 A 5320 WEB BOEING 727 7272M7 138407S NM BS 1243 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING A CHECK DISCREPANCY, LT TORQUE BOX UPPER WEB HAS 2 DENTS AT APPROX STA 1243. CUTOUT DAMAGED AREA TWO 4" DIM IAW B727 SRM 51-40-2 FIG 1. FAB REPAIR DOUBLERS TWO 7075-T6 .040 PO NR 9005551 6.5"DIA AND 4 NUT PLATE CHANNEL DIA 1" BY 6 " IAW B727 SRM 51-40-2 FIG 1 AND 53-10-2 FIG 6. INSTALLED DOUBLERS IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007082100326 20070821 00326 NM 2007 8 21 SWAA073968 1 20070809 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007082100327 20070821 00327 NM 2007 8 21 DHL2007750504 1 20070813 A 5310 DOOR FRAME BOEING 727 7272M7 138407S NM BS 990 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 C2 DOOR LWR AFT FRAME CORRODED. REMOVED DOOR AFT CORNER AND DISPLACED WEB TO GAIN ACCESS IAW B727 SRM 51-30-2. CUT-OUT DAMAGED SECTION OF FRAME DIM 13 1/2" BY 6" IAW B727 51-10-1 AND 51-40-3 FIG 1. FABRICATED NEW FRAME SECTION FROM 7075- T6 .063" PO NR 9005314 DIM 13" 1/2 BY 6" AND SPLICE ANGLE FROM 7075-T6 .071"PO NR 9003585 DIM 7" BY 6" IAW B727 SRM 51-4 0-3 FIG1 NAD 52-30-1 FIG 4. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2 AND INSTALLED REPAIR PARTS IAW B727 SRM 51-30 -2 AND 51-40-3 FIG 1 AND REINSTALLED DOOR AFT CORNER AND WEB IAW B727 SRM51-30-2 2 L 7 3 4F A3WE 2007082100341 20070821 00341 NM 2007 8 21 SWAA073965 1 20070809 A 5523 69633915 BOLT BOEING 737 7373Q8 1384670 NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED BRDG CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BOLT AND BUSHING P ER MM. 2 L 7 2 4F RT A16WE 2007082100343 20070821 00343 NM 2007 8 21 SWAA073964 1 20070809 A 5523 69633915 BOLT BOEING 737 7373Q8 1384670 NM LT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED BRDG CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BOLT AND BUSHING P ER MM. 2 L 7 2 4F RT A16WE 2007082100344 20070821 00344 2007 8 21 SWAA073952 4 20070809 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007082100345 20070821 00345 2007 8 21 SWAA073953 4 20070809 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007082100352 20070821 00352 EU 2007 8 21 USAA070647 1 20070810 A 5315 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 177US 1517 AROUND FASTENER HOLES & TOPSIDE OF FLOORBEAM, FR 66-69 HAS CORROSION. INSTALLED NEW FLOORBEAM PER SR 51-72-11; CORR TAS K JA-260-53500, DEFECT SIZE: 1.5 X 1.5 INCH. 2 L 7 2 4F RT A28NM 2007082100356 20070821 00356 EU 2007 8 21 USAA070644 1 20070810 A 5320 D5311281820401 BEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 177US 1517 Y254 BEAM ABOVE FRS C16, C18, C21 HAS CORROSION. PART REPLACED WITH LIKE PART PER SRM 51-72-00; CORR TASK JA-220-53500, DEFECT SIZE: 3 EA, 1.5 X 1.5 INCH. 2 L 7 2 4F RT A28NM 2007082100360 20070821 00360 EU 2007 8 21 USAA070642 1 20070810 A 5347 D53459039200 SEAT TRACK AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 177US 1517 LEFT INBOARD SEAT TRACK FRAME 46 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PER SRM 51-72-11, DEFECT SIZE: 1 INCH DIA. 2 L 7 2 4F RT A28NM 2007082100361 20070821 00361 EU 2007 8 21 USAA070641 1 20070810 A 5320 SILL AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 177US 1517 FR 66 Y1732 (LEFT DOOR SILL) HAS CORROSION. OVERSIZED FASTENER HOLE, TRIMMED, INSTALLED FILLER & REPAIR ANGLES PER SRM 53-41-14; CORR TASK JA-26, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A28NM 2007082100364 20070821 00364 EU 2007 8 21 USAA070640 1 20070810 A 5315 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 177US 1517 FASTENER HOLE AT FR 66 FOORBEAM (-Y1732) HAS CORROSION. REMOVED CORRODED SECTION & INSTALLED FILLER & DOUBLERS PER SRM 53-41-14; CORR TASK JA-260-53500, DEFECT SIZE: 1 X 1 INCH. 2 L 7 2 4F RT A28NM 2007082100366 20070821 00366 NM 2007 8 21 QXEA200701261 1 20070804 A 5340 ATTACH FITTING DHAV DHC8 DHC8202 2809007 NM BS 427 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX-STRINGER 31P CLEAT IS GOUGED AT STATION X427. REPAIRED IAW SRM 51-40-11, AND RD8-53-9737. 2 H 7 2 4T RT A13NM 2007082100367 20070821 00367 NM 2007 8 21 QXEA200701258 1 20070805 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - CORROSION NOTED ON NR 4 SEAT TRACK AT STATION 224 UNDER ANGLE. REPAIRED IAW RD8-53-4698, RD8-53-1102, AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007082100368 20070821 00368 NM 2007 8 21 QXEA200701257 1 20070808 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - GOUGE ON BOTTOM OF FUSELAGE AT X510 BETWEEN STRINGER 28L AND 29L. REPAIRED IAW RD8-53-5384, AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2007082100370 20070821 00370 NM 2007 8 21 QXEA200701264 1 20070809 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - SCRATCH ON INSIDE OF FUSELAGE SKIN AT STATION X510 BETWEEN STRINGER 28R AND 29R. REPAIRED IAW RD8-53-384, SRM 51-20-16, 51-20-36. 2 H 7 2 4T RT A13NM 2007082100371 20070821 00371 EU 2007 8 21 USAA070637 1 20070810 A 5347 D5311278220201 SEAT TRACK AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 177US 1517 SEAT TRACK Y1292 JUST FWD OF FR 23 HAS CORROSION. CUT OUT BAD SECTION, SPLICED IN NEW PER SRM 51-72; CORR TASK JA-900-0 9000, DEFECT SIZE: .25 INCH DIA X .030 INCH DEEP. 2 L 7 2 4F RT A28NM 2007082100372 20070821 00372 EA 2007 8 21 813200701 2 20070814 A 8530 72877 ROCKER SHAFT GULSTM 500 500B 0141106 SW LYC O540 IO540E1A5 41532 EA ENGINE BROKEN E ZJWA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CE 05 518TM 794 500B99526 L479448 LEFT ENGINE PILOT NOTICED PARTIAL POWER LOSS. AFTER LANDING THERE WAS A LARGE OIL LEAK FROM THE NR 6 EXHAUST PUSHROD TU BE WHICH HAD BEEN JARRED LOOSE AND UNCLIPPED. THE CAM FOLLOWER WAS BROKEN. THE TANG ON THE ROCKER COVER THAT HOLDS THE EXHAUST ROCKER SHAFT IN WAS BROKEN POSSIBLY LODGING IN THE VALVE SPRING CAUSE EXCESSIVE VALVE LASH. 1 H 7 2 3O 3 O 6A1 1E4 2007082100373 20070821 00373 NM 2007 8 21 DHL2007741557 1 20070813 A 5315 FLOORBEAM BOEING 727 7272Q9 138448M NM BS 312 DEFORMED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 NON STANDARD REPAIR/MODIFICATION NOTED ON FLOORBEAM LOWER CAP AT BS 312, RBL 45. CUT OUT LOWER CHORD SECTION FROM RBL 3 6 TO END OF BEAM, 23.5" IN LENGTH, FABRICATED NEW LOWER CHORD SECTION FROM BAC 1505-29222 EXTRUSION, PO NR 9004174, 23.5 " LONG, AND 4 REPAIR ANGLES FROM 7075-T6, .071" BY 9" BY 1" BY 1", PO NR 9003585, PER B727 SRM 53-10-8 FIG 9 AND 53-10-2 FIG 7. TREATED, PRIMED, AND INSTALLED CHORD REPAIR PER B727 SRM 51-10-2, 51-30-2, AND 51-30-5. 2 L 7 3 4F RT A3WE 2007082100374 20070821 00374 NM 2007 8 21 DHL2007741558 1 20070809 A 5313 65564417 STRINGER BOEING 727 7272Q9 138448M NM BS 950F-990 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AFT PIT, STRINGER 29L CORRODED BETWEEN BS 950F AND 990. CORROSION EXCEEDED ALLOWABLE LIMITS. REMOVED DAMAGED STR 29L S ECTION, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW STR 29L SECTION P/N 65-56441-7, PO NR 7232208, PER BOEING S B 727-53-0179 REV 00, AND B727 SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007082100375 20070821 00375 WP 2007 8 21 NWAA072829952 1 20070810 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 916RW 47144 3 EGRESS LIGHTS IN TAIL COMPARTMENT INOP. REPLACED POWER SUPPLY. OPERATION CHECKS GOOD. 2 L 7 2 4F A6WE 2007082100379 20070821 00379 NM 2007 8 21 KCSA071294 1 20070810 A 5420 ATTACH ANGLE BOEING 747 7472B4B 138481B NM NR 1 PYLON DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 COMP DUCT ATTACH ANGLE DAMAGE O/B SIDE LOWER SURFACE OF NR 1 PYLON. 2 L 7 4 4F RT A20WE 2007082200003 20070822 00003 NM 2007 8 22 DHL2007741561 1 20070809 A 5330 SKIN BOEING 727 7272Q9 138448M NM BS 720E S27L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 CRACK ON FUSELAGE SKIN AT HILOCK, AT BS 720E+8 AND STR 27L. CRACK CAUSED BY CORROSION ON STRINGER AND SKIN. CUT OUT DA MAGED SKIN, 6.75" BY 3.5", FABRICATED DOUBLER FROM 2024-T3, .125" BY 18" BY 11", PO NR 9005400, PER B727 SRM 53-30-3 FIG 1 AND 53-30-2 FIG 2. TREATED, PRIMED, AND INSTALLED REPAIR DOUBLER PER B727 SRM 51-10-2 & 53-30-1 FIG 1. CUT OUT CORR ODED STRINGER SECTION, 18" LONG, FABRICATED FILLER REPAIR FROM BAC1498-147 EXTRUSION, 18" LONG, PO NR 6320105, AND STR S PLICE FROM BAC1498-131 EXTRUSION, 12" LONG, PO NR 7232174, PER B727 SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9. TREATED, PRIME D, AND INSTALLED STRINGER REPAIR PARTS PER B727 SRM 51-10-2 AND 53-10-3 FIG 1. 2 L 7 3 4F RT A3WE 2007082200006 20070822 00006 NM 2007 8 22 QXEA200701278 1 20070810 A 2930 ACCUMULATOR BOMBDR DHC8 DHC8402 1390042 NM HYD SYSTEM UNDERSERVICED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 427QX 4156 EUG FLIGHT NR 2280: NR 3 HYD CAUTION LIGHT ILLUMINATES DURING NR 3 HYD SYSTEM CHECK AFTER START. AIRCRAFT RETURNED TO B LOCK. MAINTENANCE SERVICED NR 3 SYSTEM MAIN ACCUMULATOR IAW Q400 AMM TASK 12-30-00. PERFORMED ENGINE RUN, SYSTEM OPS C HECK GOOD. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007082200007 20070822 00007 NM 2007 8 22 QXEA200701279 1 20070811 A 2930 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM HYD SYSTEM FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 430QX 4163 LAX FLIGHT NR 2444: NR 3 HYD CAUTION LIGHT ILLUMINATED DURING PUSH BACK. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE OPERA TED NR 3 HYD ISO VALVE AND CYCLED ELEVATOR SEVERAL TIMES. C/W PRESSURIZATION CHECK OF NR 3 HYD SYSTEM IAW Q400 AMM TASK 29-00-00-863-803. OPS CHECK GOOD. CAUTION LIGHT REMAINED EXTINGUISHED. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCR AFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007082200011 20070822 00011 NM 2007 8 22 QXEA200701283 1 20070811 A 5270 465161 SPRING BOMBDR DHC8 DHC8402 1390042 NM MLG DOOR UNKNOWN A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 413QX 4060 PDX FLIGHT NR 2495: AFTER EXTENDING GEAR FOR LANDING, L DOOR, N DOOR, R DOOR CAUTION LIGHT ILLUMINATED. GREEN NOSE AND RIGHT GREEN ILLUMINATED AND LEFT AMBER LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE LT AND RT STABLIZER BRAC E LOCK SPRING IAW AMM TASK 32-11-16-000-802 AND 32-11-16-400-802. RETRACTED AND EXTENDED THE LANDING GEAR IAW AMM TASK 32-31-000-867-801. ALL WORKS NORMALLY. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007082200012 20070822 00012 NM 2007 8 22 QXEA200701284 1 20070810 A 3350 XD4N RELAY BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY LIGHTS MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 421QX 4149 BOI FLIGHT NR 2360: DURING TAXI OUT, FA REPORTS THE EMERGENCY LIGHTS REMAIN ON WHEN THE COCKPIT EM SWITCH IS IN THE ARM POSITION. FA'S EM SWITCH IS WHERE IT IS SUPPOSED TO BE. THE COCKPIT EM SWITCH IS PUT IN THE OFF POSITION. THE LIGHT GO ES OUT. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE REMOVED AND REPLACED 3351-K2 RELAY IAW FIM 33-50-00. ALL OPS AND INDICAT IONS ARE NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007082200013 20070822 00013 NM 2007 8 22 DL764070961 1 20070727 A 2530 72077500 OVEN BOEING 767 767432ER 1385134 NM FWD GALLEY ODOR A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 827MH 29698 FWD GALLEY NR 2 OVEN MADE POPPING NOISE AND BURNING ODOR. FWD TO MCO AND PLACARD PER MEL 25-20-01H. DEACTIVATED C/B CO LLARED. REPLACED NR 2 FWD OVEN, OPS NOW CKS GOOD. REMOVED MCO/PLAC. 2 L 7 2 4F RT A1NM 2007082200014 20070822 00014 NE 2007 8 22 DL76S071022 2 20070805 A 7261 CF680A2 ENGINE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 1 MAKING METAL A DALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 27 133DN 49676 1226 24982 580325 LT ENGINE OIL PRESSURE WENT TO 16-18 PSI (AMBER NUMBERS). OIL QTY AT ZERO. LEFT ENGINE STOP WORKING. REMOVED AND INSP ECTED LT ENG OIL FILTER. FOUND FULL OF DEBRIS MAIN ENG OIL CHIP DETECTOR SAME. COULD NOT REINSTALL MAIN E OIL FILTER D UE TO DEBRIS ON HOUSING. REPLACED NR 1 ENG PER TRANS 1T144. 2 L 7 2 4F 4 F RT A1NM E13NE 2007082200017 20070822 00017 NM 2007 8 22 DLM88071040 1 20070808 A 2120 UNKNOWN DOUG MD88 MD88 3023688 NM CABIN ODOR A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 940DL 49813 ODOR OF SMOKE, RUBBERY, DURING TAXI OUT. INSPECTED TAIL COMPARTMENT, AND APU COMPARTMENT, NO PROBLEMS FOUND, RAN APU AI RALL NORMAL. 2 L 7 2 4F RT A6WE 2007082200018 20070822 00018 NM 2007 8 22 DLM88071041 1 20070807 A 2910 240S58950310 LINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE HYDRAULIC SYS LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 944DL 49817 718134 NUMBER 2 ENGINE HYDRAULIC PRESSURE LINE LEAK AND CAUSE TO LOSE MOST OF THE HYDRAULIC FLUID. REPLACED FLEX LINE FROM NR 2 ENGINE TO PYLON LEAK CHECKS NORMAL. 2 L 7 2 4F 4 F RT A6WE E9NE 2007082200020 20070822 00020 NM 2007 8 22 DL757071044 1 20070808 A 5330 141N32152 SKIN BOEING 757 757232 1384965 NM FS221 S23L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 609DL 22816 DENTS IN FUSELAGE SKIN NEAR RADOME AT FS 220, LT SIDE, S-23L. CUTOUT DENTS AND INSTALLED DOUBLER. 2 L 7 2 4F RT A2NM 2007082200021 20070822 00021 NM 2007 8 22 DLM88071045 1 20070802 A 2432 203BC1021 CHARGER DOUG MD88 MD88 3023688 NM FWD E&E BURNED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 936DL 5170 49723 DURING PREFLIGHT, BATTERY CHARGER C/B POPPED WITH ODOR/SMOKE IN COCKPIT/CABIN. BATTERY CHARGER REPLACED. UPON TEAR DOW N IN THE SHOP BATTERY CHARGER WAS SEVERELY CHARRED INTERNALLY. THERE WAS SUFFICIENT HEAT TO DISTORT THE ALUMINUM COVER. 2 L 7 2 4F RT A6WE 2007082200023 20070822 00023 GL 2007 8 22 DL764071048 2 20070808 A 7200 CF680C2B8F ENGINE BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 1 FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 840MH 19593 29717 706446 REPLACED NR 1 ENG PER ROUTINE DECK. 2 L 7 2 4F 4 F RT A1NM E23EA 2007082200024 20070822 00024 NM 2007 8 22 DL76L071050 1 20070807 A 4920 ENGINE BOEING 767 767332 1382001 NM APU MALFUNCTIONED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 193DN 30597 P1295 28450 APU AIR LOW DUCT PRESSURE--13 PSI. REMOVED AND REPLACED APU PER MM. RETURNED APU BLEED VALVE TO NORMAL. 2 L 7 2 4F RT A1NM 2007082200026 20070822 00026 NM 2007 8 22 DLM88071055 1 20070810 A 5743 5935811501 FITTING DOUG MD88 MD88 3023688 NM MLG DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 DURING HMV, MLG FITTING WAS FOUND WITH BORE OVERSIZED BEYOND AD AND SERVICE REWORK DRAWING LIMITS. BOEING WAS CONTACTED FOR APRPOVAL TO INSTALL OVERSIZED BUSHING, AND PROVIDED APPROPRIATE APPROVALS AS DETAILED IN 273922-14AD REVISION A. 2 L 7 2 4F RT A6WE 2007082200027 20070822 00027 NM 2007 8 22 DLM88071056 1 20070810 A 5330 593600419 SKIN DOUG MD88 MD88 3023688 NM BS 661 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 A OF FUSELAGE SKIN AND DOOR SURROUND DOUBLER CORRODED BELOW THE C2 DOOR THRESHOLD. THE LOWER AFT DOUBLER CORNER AND THE SKIN AFT OF FS 661 WERE REPLACED AND ATTACHED WITH A SPLICE REPAIR. THIS SPLICE REPAIR ELIMINATED ER/A 385988-14. 2 L 7 2 4F RT A6WE 2007082200029 20070822 00029 NE 2007 8 22 DL757071059 2 20070811 A 7200 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 MAKING METAL A DALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 606DL 51712 22813 716570 RT ENG IFSD DUE TO OIL PRESS GOING INTO THE RED POSITIVE OIL PRESS NOTED PER FLT CREW. NO INDICATION OF OIL LOSS AS OI L QTY INDICATED 18 PTS AT GATE. T/S OIL PRESS SYSTEM FOUND METAL ON MAIN CHIP DETECTOR. NO METAL ON ALL OTHER CHIP DET ECTORS. AIR SPUN ENG RT OIL PRESS 40 A 26 PERCENT N1 HIGH. RAN ENG OIL PRESS CLIMBED TO 80 PLUS BEF IDLE AT STARTER CUT OUT. OIL PRESS DROPPED. S/D ENGINE AT 4 PSI. FOUND MORE METAL ON MAIN CHIP DETECT. SPUN 2 MORE TIME OIL PRESS AT ID LE LIMITS. AT 26-28 PERCENT N2. FOUND METAL CHIP DETECTOR EACH TIME, 4 TIMES. REPLACED ENG PER TANS 6T1. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082200033 20070822 00033 WP 2007 8 22 070144 1 20070810 A 3350 408822101 BATTERY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS NO TEST A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 892GA 49826 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007082200034 20070822 00034 NM 2007 8 22 NWAA072836310 1 20070812 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING OVERNIGHT CHECK, 2 OVERWING EXTERIOR AND DOOR 3 RIGHT EXIT SIGN (AFT OF DOOR) ARE INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007082200035 20070822 00035 NM 2007 8 22 TSAA0757045 1 20070811 A 5720 65826711 WEB BOEING 737 737210C 1384459 NM BS 663.5 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 834AL 20917 WHILE PERFORMING INSPECTIONS TO COMPLY WITH AD 93-08-04 A CRACK APPROXIMATELY 3 INCHES LONG WAS DISCOVERED AT BS 663.5 R BBL 40 WL 20. REPAIRED IN ACCORDANCE WITH ALOHA ECO 3667. FORM 8100-9 APPROVING REPAIR HAS BEEN RECEIVED. FINAL REPA IR SIZE APPROX 6 X 9. 2 L 7 2 4F A16WE 2007082200037 20070822 00037 EU 2007 8 22 AWXA200700991 1 20070812 A 5347 D53112782200 SEAT TRACK AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 632AW 81 SAL - MAJOR REPAIR - C-7 CHECK - NR 5963569, CORROSION FOUND ON CABIN SEAT TRACK, BS 605/FR 12 - BS 950/FR 24, -Y765. R EPLACED CABIN SEAT TRACK, BS 605/FR12 - BS 950 / FR 24, -Y765, IAW A320 SRM 51-72-11 PAGE 1-2. 2 L 7 2 4F RT A28NM 2007082200038 20070822 00038 EU 2007 8 22 AWXA200700992 1 20070802 A 5347 D5311278220201 SEAT TRACK AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 632AW 81 SAL - MAJOR REPAIR - C-07 CHECK - NR 5963570, CORROSION FOUND ON CABIN SEAT TRACK, BS 605/FR 12 - BS 950/FR 24, -Y1292. REPLACED CABIN SEAT TRACK, BS 605/FR 12 - BS 950/FR 24, -Y1292, IAW A320 SRM 51-72-11, PAGE 1-2. 2 L 7 2 4F RT A28NM 2007082200040 20070822 00040 EU 2007 8 22 AWXA200700994 1 20070804 A 5320 D53230524200 WEB AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 632AW 81 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980315, CORROSION FOUND ON FWD CARGO COMPARTMENT LOWER EDGE WEB, BS 1163/FR 28 - B S 1217/FR 29, S41R. REPLACED FWD CARGO COMPARTMENT LOWER EDGE WEB, BS 1163/FR 28 - BS 1217/FR 29, S41R, IAW A320 SRM 51 -72-11. 2 L 7 2 4F RT A28NM 2007082200041 20070822 00041 EU 2007 8 22 AWXA200700995 1 20070804 A 5320 D53472094002 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 632AW 81 SAL - MAJOR REPAIR - C-07 CHECK - NR 5963564, CORROSION FOUND ON CABIN FLOOR SUPPORT, BS 3043/FR 64 - BS 3366/FR 70, +Y5 12. REPLACED CABIN FLOOR SUPPORT, BS 3043/FR 64 - BS 3366/FR 70, +Y512, IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007082200042 20070822 00042 NM 2007 8 22 EIA2007099 1 20070515 A 2150 A/C PACK BOEING 747 747132 1384882 NM NR 1 SMOKE A EIAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 479EV 19898 AFTER TAKEOFF PASSING THROUGH APPROXIMATELY 4,000 MSL, SMOKE AND A STRONG ODOR FOLLOWED BY THE LAVATORY SMOKE DETECTOR A URAL WARNING. SMOKE BEGIN TO DISSIPATE ON FINAL APPROACH. TRANSFERRED NR 1 PACK TO DMI PER MEL 21-1-20 AFTER HAVING T ROUBLE SHOOT AND FOUND SMOKE AND ODOR TO BE COMING FROM NR 1 PACK. TO REMAIN OPEN TILL FINAL FIX FINAL FIX SEE SDR EIA2 007119. 2 L 7 4 4F A20WE 2007082200043 20070822 00043 NM 2007 8 22 EIA2007100 1 20070516 A 2120 UNKNOWN BOEING 747 747132 1384882 NM LAVATORY SMOKE A EIAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 479EV 19898 AFTER TAKEOFF IN CLIMB LAV SMOKE DETECTOR SOUNDED WITH EVIDENCE OF SMOKE AND ODOR IN CABIN. REMAIN OPEN TILL FINAL FIX AN TIMES FINAL FIX SEE SDR EIA2007119 2 L 7 4 4F A20WE 2007082200045 20070822 00045 NM 2007 8 22 EIA2007145 1 20070713 A 5420 CLOSEOUT PANEL BOEING 747 747230B 1384889 NM NR 3 PYLON GOUGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 488EV 23287 NR 3 PYLON INBOARD DOOR 473AL RING IS GOUGED INSIDE. REPAIRED NR 3 PYLON INBD ACCESS DOOR CUT OUT FOR ACCESS PANEL 473A L PER ECRA 488-54-018-2 PART 1. 2 L 7 4 4F A20WE 2007082200046 20070822 00046 NM 2007 8 22 EIA2007146 1 20070713 A 5712 RIB BOEING 747 747230B 1384889 NM LT WING LOOSE A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 488EV 23287 LEFT WING LEADING EDGE HAS RIVETS LOOSE AT FORMER RIB INBOARD OF NR 3 KREUGER FLAP. REPAIRED LEFT WING LEADING EDGE AT FORMER RIB INBOARD OF NR 3 KREUGER FLAP PER ECRA 488-57-020-2. 2 L 7 4 4F A20WE 2007082100019 20070821 00019 2007 8 21 2007UALA02918 4 20070730 A 2565 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RIGHT UNSERVICEABLE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 122UA 29168 RIGHT UPPER DECK SLIDE INOP DUE TO SLIDE NOT SERVICEABLE. LOWER AFT FACIAL MOUNT PULLING OUT. FOUND LOWER AFT FACIAL MOUNT "PULLING OUT" AND PREVENTING SLIDE FROM PROPER MOUNTING. REPLACED UPPER DECK RH SLIDE. ACCOMPLISHED RII CHECK FOUND NORMAL. AIRCRAFT RETURNED TO SERVICE. SLIDE PROBLEM ROOT CAUSE: SLIDE MOUNT NOT FITTED WITH HELICOILS TO RETAIN F ASTENERS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082100025 20070821 00025 NM 2007 8 21 2007UALA02923 1 20070730 A 5414 311N31504 PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 PYLON GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 NR 1 PYLON AFT BULKHEAD UPPER CLOSE OUT PANEL HAS DEEP GOUGE. BLENDED GOUGE AND FABRICATED PANEL PER BOEING DWG 311N31 50 AND INSTALLED REPAIR PER UA ENGINEERING SPECIFICATIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082100026 20070821 00026 EA 2007 8 21 A6WA200740397 1 20070715 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 423AW 7636 RT FS 280 FLOOR SUPPORT CLIPS CRACKED APPROX .2 INCHES LONG AT RBL 9, IB AND OB LOCATIONS. (K) MAINTENANCE REMOVED AND REPLACED SUPPORT CLIPS IAW BSC STANDARD REPAIR 601R-53-0057A AND CRJ 200 SRM 51-42-21. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082100047 20070821 00047 NM 2007 8 21 2007UALA02938 1 20070731 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 RIGHT SIDE FUSELAGE SKIN CRACK JUST BELOW AND FWD OF AFT CARGO COMPT EMERGENCY LIGHT. CRACK IS APPROX 1.25 INCHES LENGT H. MAJOR REPAIR ACCOMPLISHED: REPLACED RIGHT FUSELAGE SKIN PANEL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082100057 20070821 00057 NM 2007 8 21 2007UALA02950 1 20070801 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY LIGHT ROW 54 ABC INOPERATIVE. RESECURRED CONNECTOR. OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082100059 20070821 00059 NM 2007 8 21 2007UALA02952 1 20070731 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 669UA 30025 FIRST CLASS SEAT 6H IS MISSING SEAT MOUNTED EPL LIGHT STRIP. REPLACED LIGHT STRIP AT SEAT 6H PER MM 25-25-10 AND OPS C HECK IS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082100100 20070821 00100 NM 2007 8 21 2007UALA02971 1 20070801 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 BEFORE DEPARTURE FOUND F-C SEATS 1A-5A, 4E, 5E EEL LIGHT INOP. AFTER TROUBLESHOOTING, FOUND SHORT IN EEL CABLE HARNE SS AT SEAT 5E. REPLACED HARNESS. OP CHECKS GOOD FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082100113 20070821 00113 WP 2007 8 21 UPS07850388 1 20070720 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 STA 70 FRAME CRACKED AND CORRODED BETWEEN L31R AND L32R IN A/C COMPT. REPAIRED CRACKED AND CORRODED FRAME AT STA 70 BETWEEN L31R AND L32R IN A/C BAY IAW SRM 53-02-05 FIG 08C2. 2 L 7 4 4F RT 4A25 2007082100114 20070821 00114 WP 2007 8 21 UPS07850393 1 20070721 A 5514 SEO85500094 ANGLE DOUG DC8 DC873F 302199F WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 RIGHT HORIZ STAB FRONT SPAR INBOARD LWR ANGLE CRACKED. REMOVED AND REPLACED RIGHT HORIZ STAB FRONT S PAR INBOARD LWR ANGLE IAW SRM 51-3-0, 51-1-20D, SRM 51-3-2, AND DC8 AMM 55-10-00-2. 2 L 7 4 4F RT 4A25 2007082100126 20070821 00126 NM 2007 8 21 UPS07M50399 1 20070515 A 5330 SKIN DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C RT EXTERIOR FUSELAGE SKIN FOUND WITH CORROSION AT SEVERAL AREAS ADJACENT TO FWD SIDE OF APU EXHAUST DO OR AS MARKED (UPPER PORTION). RT EXTERIOR FX SKIN FWD SIDE OF APU EXHAUST DOOR UPPER PORTION DAMAGED SKIN TRIMMED OUT P ER EN1416-07 & PARTS REMVD PER SRM 51-31-01V2 R38. HFEC INSP C/OUT PER DAC NDTSPM R.13 06-10-01.001 ON SKIN P/N: AJC70- 506 & FOUND NO CRACK EVIDENT. REP FILLER, DOUBLER & TAPER SHIM FAB PER EN1416-07 USING MATL 707 5T6-0.125, 0.071&0.040" . HOLES P/UP PER SRM 51-31-01 V2 R38. OK TO INSTALL. 2 L 7 3 4F RT A22WE 2007082100127 20070821 00127 NM 2007 8 21 UPS07M50400 1 20070511 A 5753 NRC6753503 STOP FITTING DOUG MD11 MD11F 3023600 NM T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP STOP FITTING FOUND CRACK (VANE TRACK NR 4 FROM I/B VICINITY) LEFT WING O/B TRAILING EDGE FLAP ASSY REMOVED PER AMM27-50-30R.55. LEFT WING O/B FLAP I/B & O/B CARRIAGE ROLLERS ASSY REMOVED PE R CMM 57-52-04 R.58. HINGE PNL SUPPORT AT LEFT TRAILING EDGE FLAP REMVD PER SRM 51-31-01 V2 R38. CARRIAGE ROLLERS INST ALLED PER CMM57-52-04R.58 ON SERVICEABLE FLAP. HINGE PANEL SUPPORT INSTALLED PER SRM 51-31-01V2 R38. FLAP ADJ & OPS CH ECK REFER TO EOMD11-5750-23556-E. 2 L 7 3 4F RT A22WE 2007082100132 20070821 00132 CE 2007 8 21 BSAASRD0723 1 20070801 A 3040 1143840206 TERMINAL BEECH 1900 1900D 1154162 CE WINDSHIELD SHORTED A BSAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 NM 05 140ZV UE140 PUFF OF WHITE SMOKE FROM THE BOTTOM OF THE FIRST OFFICER'S FRONT WINDSHIELD. FOUND -S- TERMINAL THAT WAS CURRENTLY BEIN G USED BURNED (SHORTED). SWAPPED THE WIRE TO OTHER -S- TERMINAL, WINDSHIELD OP CHECK GOOD. 2 L 7 2 4T RT A24CE 2007082100135 20070821 00135 NM 2007 8 21 USAA070615 1 20070808 A 5210 6545871132 DOOR FRAME BOEING 737 737401 1384701 NM DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 CUTOUTS FOR THE 3RD & 4TH STOPS DOWN FROM TOP, AFT SIDE OF DOOR CRACKED. FAB'D & INSTALLED REPAIR DOUBLERS PER TR52-10- 11, DEFECT SIZE: .025 INCH. 2 L 7 2 4F RT A16WE 2007082100144 20070821 00144 NM 2007 8 21 USAA070614 1 20070808 A 5314 KEELBEAM BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 STA 768-772, S27R, RT KEEL BEAM MEMBER HAS CORROSION. INSTALLED FILLERS & ANGLE/SPLICE PER EA 98782, 98787, 98793, CORR TASK C53-202-01, DEFECT SIZE: 5 INCHES. 2 L 7 2 4F RT A16WE 2007082100167 20070821 00167 NM 2007 8 21 SB07061 1 20070808 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 574US 23739 BOS - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT 6ABC IS LOOSE AND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY AT SEAT 6ABC. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007082100180 20070821 00180 NM 2007 8 21 ASAA0741936 1 20070809 A 5320 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 AFT CARGO PIT FLOOR SUPPORT CHANNEL CORRODED. FLOOR SUPPORT CHANNEL REPAIRED IAW SRM 53-00-53 FIG 201 REPAIR 1. 2 L 7 2 4F RT A16WE 2007082100202 20070821 00202 NM 2007 8 21 ASAA0741940 1 20070809 A 5320 INTERCOSTAL BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 INTERCOSTAL CRACKED. REPLACED INTERCOSTAL IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007082100204 20070821 00204 NM 2007 8 21 ASAA0741941 1 20070209 A 5340 STRINGER CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 STRINGER CLIP CRACKED. REPLACED CLIP IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007082100210 20070821 00210 NM 2007 8 21 KCSA071288 1 20070809 A 5420 STIFFENER BOEING 747 7472B4B 138481B NM NR 2 PYLON WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NR 2 PYLON O/B LOWER WEB STIFFENER BY MAIN PNEUMATIC DUCT HAS WORN HOLE AT DUCT ATTACHMENT. 2 L 7 4 4F RT A20WE 2007082100215 20070821 00215 NM 2007 8 21 KCSA071291 1 20070810 A 5230 SILL BOEING 747 747249F 1384849 NM CARGO DOOR CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 C-2 DOOR SILL UPPER CHORD IS CORRODED APPROX AT 1860. 2 L 7 4 4F A20WE 2007082100253 20070821 00253 EA 2007 8 21 TRAX200701124 1 20070806 A 5210 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 755EV 10185 PAX DOOR AFT DRAG ANGLE AND PULLEY CRACKED. 2 L 7 2 4F RT A21EA 2007082100255 20070821 00255 EA 2007 8 21 TRAX200701127 1 20070806 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 884AS 7513 CAPT'S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007082100257 20070821 00257 CE 2007 8 21 DJFA2007087 1 20070802 A 2120 UNKNOWN BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE CABIN ODOR E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 23 796TA RK289 ON DECENT, CREW NOTED A BURNING ODOR IN THE CABIN. CREW WAS UNABLE TO ISOLATE THE PROBLEM. MAINTENANCE WAS UNABLE TO D UPLICATE THE DISCREPANCY. PROBLEM HAS NOT REPEATED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007082100258 20070821 00258 CE 2007 8 21 DJFA2007093 1 20070811 A 3260 5EN16 UPLOCK SWITCH BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE LT MLG INOPERATIVE E DJFA O OTHER N FALSE WARNING AP APPROACH 1 EA 23 789TA RK268 ON APPROACH, CREW REPORTED GEAR UNSAFE LIGHT IN CONJUNCTION WITH DOWN AND LOCKED INDICATION. CREW USED EMEREGENCY GEAR EXTENSION PROCEDURE AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MLG UPLOCK SWITCH INOPERATIVE. THE SWITCH WA S REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007082100274 20070821 00274 EA 2007 8 21 TRAX200701136 1 20070807 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 924EV 7830 FOUR INCH SECTION OF EMERGENCY FLOOR LIGHTING SYSTEM INOP AT ROW 12. 10-18-07 REPLACED LIGHTED EMERG FLOOR STRIP AT ROW 12 IAW CRJ200 AMM 33-51-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007082100276 20070821 00276 EA 2007 8 21 TRAX200701137 1 20070807 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN UNSECURE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 834AS 7254 EMERGENCY LIGHT NEXT TO SERVICE DOOR NEEDS TO BE RESECURED. 2 L 7 2 4F RT A21EA 2007082100280 20070821 00280 EU 2007 8 21 TRAX200701141 1 20070808 A 5320 INTERCOSTAL AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 RIGHT INTERCOSTAL BETWEEN FR 36-38 CORRODED. 2 H 7 2 4T RT 2007082100298 20070821 00298 NM 2007 8 21 SWAA073971 1 20070809 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 385, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007082100328 20070821 00328 NM 2007 8 21 SWAA073963 1 20070809 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007082100335 20070821 00335 NM 2007 8 21 SWAA073967 1 20070809 A 5523 65C25798 HINGE BOEING 737 7373T5 1384608 NM LT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED CABIN VISIT, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE ASSY PER SWA EA. 2 L 7 2 4F RT A16WE 2007082100348 20070821 00348 NM 2007 8 21 SWAA073955 1 20070809 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007082100358 20070821 00358 EU 2007 8 21 USAA070643 1 20070810 A 5347 D53456038202 SEAT TRACK AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 177US 1517 Y765 ABOVE FR C47.2, BEAM (SEAT TRACK) HAS CORROSION. SEAT TRACK SPLICE REPAIR 4.25 INCH SECTION PER SRM 53-00-15; CORR TASK JA-251-53500, DEFECT SIZE: 2 X 3 INCHES. 2 L 7 2 4F RT A28NM 2007082100365 20070821 00365 EU 2007 8 21 USAA070639 1 20070810 A 5315 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 177US 1517 FLOORBEAM Y495 BETWEEN FR 14-16 HAS CORROSION. REMOVED AND REPLACED PAX FLOORBEAM PER SRM 51-72-11; CORR TASK JA-220-53 500, DEFECT SIZE: 3 INCH SQ ON SURFACE. 2 L 7 2 4F RT A28NM 2007082200001 20070822 00001 NM 2007 8 22 DHL2007741559 1 20070726 A 5322 SHEAR TIE BOEING 727 7272Q9 138448M NM BS 720A CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 CORROSION ON FRAME SHEAR TIE AT BS 720A, BETWEEN STR 27R AND 28R. CORROSION EXCEEDED LIMITS ON SHEAR TIE. REMOVED SHEA R TIE, FABRICATED NEW SHEAR TIE FROM 7075-T6, .050" BY 5.5" BY 3.25", PO NR 9005314, PER B727 SRM 53-10-4 FIG 15 AND 53- 10-2 FIG 3. TREATED, PRIMED, AND INSTALLED NEW SHEAR TIE PER B727 SRM 51-10-2 AND 53-10-4 FIG 15. 2 L 7 3 4F RT A3WE 2007082200009 20070822 00009 NM 2007 8 22 QXEA200701281 1 20070811 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR OUT OF RIG A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 406QX 4048 STS FLIGHT NR 2467: AFT PAX DOOR DIFFICULT TO OPEN OR CLOSE. MAINTENANCE RIGGED THE AFT PAX DOOR IAW Q400 AMM 52-12-01- 400-801 AND 52-12-01-400-802. DOOR OPENS AND CLOSES NORMALLY. LEAK CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007082200010 20070822 00010 NM 2007 8 22 QXEA200701282 1 20070814 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM NR 2 BLEED FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 409QX 4051 BZN FLIGHT 2328: THE NR 2 BLEED HOT CAUTION ILLUMINATED. C/W EMERGENCY AND ABNORMAL CHECKLIST. THE LIGHT EXTINGUISHED. MAINTENANCE C/W FIM TASK 36-20-00-801-802 AND C/W AMM TASK 36-11-00-710-802. NO DEFECTS NOTED. NO PARTS REPLACED. A IRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007082200015 20070822 00015 NM 2007 8 22 DLM90071027 1 20070805 A 2150 212010004 CONTROL VALVE DOUG MD90 MD9030 3023690 NM GE CF680 CF680A2 NE A/C PACK FLOW STICKING A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 906DA 53386 580325 RETURNED TO SLC BECAUSE WITH ONLY THE LEFT PACK ON FLOW LIGHT ILLUMINATED. WITH CLIMB POWER AT 7000'. FLOW LEVEL AT 10 000 TO RETURN FOR LANDING, CABIN CLIMBED TO 7000'. VERY HOT IN CABIN. FOUND LT FLOW CONTROL VALVE STICKING INTERMITTEN TLY. REPLACED LEFT FLOW CNTL VALVE PER M/M. LT PACK FLOWS NORMALLY AND SUPPLIES 40 DEGREE AIR. 2 L 7 2 4F 4 F RT A6WE E13NE 2007082200019 20070822 00019 NM 2007 8 22 DL764071042 1 20070808 A 2933 291080111 MONITOR BOEING 767 767432ER 1385134 NM HYD QTY SYSTEM MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 828MH 29699 ON CLIMB-OUT, RT HYD QTY WENT TO .48 RF, INSP A/C NO LEAKS NOTED. CK FLUID AT RRVR AND REFILL BAY ALL CKD FULL FWD RT H YD QTY IND TO MCO AND PLAC M29-33-02. T/S PER FIM 29-11-00 FIG 113. REMOVED AND REPLACED HYD QUANTITY MONITOR UNIT FIM . PER AMM. OPS CK GOOD MCO AND PLAC REMOVED. 2 L 7 2 4F RT A1NM 2007082200032 20070822 00032 NM 2007 8 22 DLM88071069 1 20070813 A 3350 RPS1B POWER SUPPLY DOUG MD88 MD88 3023688 NM EMERGENCY LIGHTS INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 928DL 49715 ON L/O, FOUND ROWS 27DE AND AFT E-PATH LIGHTS INOP. REPLACED POWER SUPPLY. OPS NML, S/N ON 11284, S/N OFF 3796, P/N 33 3701650. 2 L 7 2 4F RT A6WE 2007082200036 20070822 00036 EU 2007 8 22 AWXA200700990 1 20070811 A 5347 D53230464200 SEAT TRACK AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 632AW 81 SAL - MAJOR REPAIR - C-7 CHECK, NR 5963328, CORROSION FOUND ON CABIN SEAT TRACK, BS 950/FR 24 - BS 1537/FR 35, -Y765. R EPAIRED CABIN SEAT TRACK, BS 950/FR 24 - BS 1537/FR 35, -Y765, IAW A320 SRM 51-00-15, FIG 201. 2 L 7 2 4F RT A28NM 2007082200047 20070822 00047 NM 2007 8 22 EIA2007148 1 20070716 A 3350 1317 BULB BOEING 747 747230B 1384889 NM EMERGENCY LIGHT INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487EV 23286 UPPER DECK AFT EMERGENCY AISLE LIGHT INOP. REPLACED BOTH BULBS AND OPS CHECKED PER B747MM 33-51-07. 2 L 7 4 4F A20WE 2007082200048 20070822 00048 NM 2007 8 22 EIA2007149 1 20070720 A 2611 LAMP BOEING 747 747230B 1384889 NM DETECTOR LOOSE A EIAA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 488EV 23287 DURING FLIGHT, NR 2 MAIN CARGO DETECTOR CAME ON; THERE WAS NO CARGO LOADED. BEACON LAMP FOUND LOOSE, TIGHTENED AND DETE CTOR OPS NORMAL. A SYSTEM NO DEFECT. MAIN DECK NR 2 SMOKE DETECTOR SYSTEM OPS NORMAL PER MM 26-14-00. 2 L 7 4 4F A20WE 2007082200052 20070822 00052 NM 2007 8 22 EIA2007119 1 20070601 A 2611 0914 SMOKE DETECTOR BOEING 747 747132 1384882 NM LAVATORY FALSE INDICATION A EIAA O OTHER N FALSE WARNING DE DESCENT 1 NM 09 479EV 19898 LAV SMOKE DETECTOR SOUNDED DURING DESCENT. NO SMOKE OR MIST NOTED BY CREW, AIRCRAFT WAS STAGING EMPTY FROM MHR TO SUU. SMOKE DETECTOR REPLACED WITH NEW UNIT. DO NOT PROCESS, AWAITING AIRCRAFT TIMES. 2 L 7 4 4F A20WE 2007082200054 20070822 00054 NM 2007 8 22 EIA2007124 1 20070605 A 3350 3004185 LIGHT BOEING 747 747200 1384847 NM R5 DOOR NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 471EV 20651 RT DOOR 5R EMERGENCY LIGHT INOP. REMOVED AND REPLACED 5R EMERGENCY EXIT LIGHT ASSY PER B747 MM 33-51-00. 2 L 7 4 4F RT A20WE 2007082200055 20070822 00055 NM 2007 8 22 EIA2007125 1 20070605 A 3350 S1356B37 LIGHT BOEING 747 747273C 1384896 NM CABIN NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 471EV 20651 LT CEILING EMERGENCY LIGHT INOP BY STATION 2040-2060. REPLACED LT CEILING LIGHT ASSY OPS CKD NORMAL PER B747 MM 33-51-0 0. 2 L 7 4 4F A20WE 2007082200056 20070822 00056 NM 2007 8 22 EIA2007126 1 20070613 A 3350 S1356B37 LIGHT BOEING 747 747132 1384882 NM SERVICE DOOR DEFECTIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481EV 19896 EMERGENCY LIGHT BY UPPER DECK SERVICE DOOR LIGHT STAYS ILLUMINATED IN THE ARMED POSITION. REMOVED AND REPLACED EMERGENC Y LIGHT ASSY OPS CKD NORMAL IAW B747 MM 33-51-07. 2 L 7 4 4F A20WE 2007082200063 20070822 00063 NM 2007 8 22 EIA2007133 1 20070628 A 3350 S1356B37 LIGHT BOEING 747 747121 1384871 NM CABIN NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480EV 20348 EMERGENCY LIGHT AT THE TOP OF THE STAIRS GOES ON AND GOES RIGHT OUT. REPLACED EMERGENCY LIGHT AT TOP OF STAIRS, OPS CK` D NORMAL PER B747 MM 33-51-07. 2 L 7 4 4F A20WE 2007082200065 20070822 00065 NM 2007 8 22 EIA2007135 1 20070710 A 5312 PRESSURE PANEL BOEING 747 747230B 1384889 NM NLG WW CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 488EV 23287 NOSE WHEEL WELL TOP WEB IS CRACKED BETWEEN STA 280-300 LBL 20 AT LEFT BRAKE PAD MOUNT. REPAIRED NOSE WHEEL WELL TOP WEB BETWEEN STA 280-300 LBL 20 PER B747 SRM 53-10-04 PG 713-721. 2 L 7 4 4F A20WE 2007082200066 20070822 00066 NM 2007 8 22 EIA2007136 1 20070703 A 5330 SKIN BOEING 747 747230B 1384889 NM BS 2364 DENTED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 488EV 23287 OUTWARD DENT IN FUSELAGE SKIN STA 2364 STRINGER 15 RIGHT. CUT OUT DAMAGE AREA FABRICATED -1 AND -2 REPAIR PARTS, INSTAL LED FILLER AND DOUBLER PER B747 SRM 53-30-03 FIG 47 AND 51-30-02. ALL WORK ACCOMPLISHED AT BS 2346 STRINGER 15R. 2 L 7 4 4F A20WE 2007082200071 20070822 00071 NM 2007 8 22 EIA2007141 1 20070717 A 5315 65B157795 FLOORBEAM BOEING 747 747230B 1384889 NM BS 1345 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 488EV 23287 RT STA 1345 BL 117 O/B FLOORBOARD SUPPORT HAS ELONGATED HOLE (UNDER FLOOR BOARD). REPAIRED RT STA 1345 BL 117 O/B FLOOR BOARD SUPPORT PER ECRA 488-53-024-2A. 2 L 7 4 4F A20WE 2007082200072 20070822 00072 NM 2007 8 22 EIA2007142 1 20070717 A 5315 65B1036417 FLOORBEAM BOEING 747 747230B 1384889 NM BS 1345 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 488EV 23287 LT STA 1345 BL 117 O/B FLOORBOARD SUPPORT HAS ELONGATED HOLE (UNDER FLOOR BOARD). REPAIRED LT STA 1345 BL 117 O/B FLOOR BOARD SUPPORT PER ECRA 488-53-024-2A. 2 L 7 4 4F A20WE 2007082200074 20070822 00074 NM 2007 8 22 07FDEA02808 1 20070808 A 5330 65186291 SKIN BOEING 727 727233 138408A NM BS 940 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 LWR AFT CARGO PIT DOOR, S/N 508, OUTER SKIN HAS LIGHT PITTING CORROSION ON LWR CONTACT AREA OF BODY FAIRING BLENDED CORR OSION, NDT VERIFIED ORIGINAL MATERIAL THICKNESS TO BE .036". MATERIAL LOSS AT DEEPEST POINT IS .002" MATERIAL IS WITHIN LIMITS WITH .034" REMAINING. TREATED AND PRIMED BLENDED AREA, REF SRM 51-10-6/51-10-2 AND NDT MAN, PART 4 51-00-00 FI G 2/ SRM 53-30-1, PG 2C FIG 2, THIS IS LEVEL 1 CORROSION. 2 L 7 3 4F RT A3WE 2007082200076 20070822 00076 NM 2007 8 22 07FDEA02858 1 20070813 A 5712 6516275 RIB BOEING 727 727233 138408A NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 LEFT WING LEADING EDGE CAVITY INBOARD OF NR 2 SLAT OUTBOARD TRACK RIB AT SLAT STATION 318 IS CRACKED AT FORWARD LOWER AT TACH FASTENER. REMOVED RIB AND HAD CRACK NDT AND STOP DRILLED CRACK, FORMED DOUBLER AND INSTALLED. REPAIR DOUBLER TO R IB ALODINED, PRIMED SEALED AND INSTALLED ON AIRCRAFT REF 51-40-2, 51-30-2. 2 L 7 3 4F RT A3WE 2007082200080 20070822 00080 NM 2007 8 22 07FDEA02866 1 20070814 A 5313 6527132 STRINGER BOEING 727 727233 138408A NM ZONE 100 DAMAGED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 286FE 22623 CUSTOMER REQUEST FOR PREVIOUS WORKMANSHIP, BS 680, STR S-23L STRINGER UPPER FLANGE WAS BLENDED, ON AND HAS TOOLING MARK IN AREA UNDER PREVIOUS REPAIR. BLEND OUT TOOLING MARK IAW B727 SRM 51-10-1 FIG 2. INSTALLED STRINGER TYPICAL REPAIR IA W B727 51-10-3-FIG 2, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007082200081 20070822 00081 NM 2007 8 22 07FDEA02867 1 20070814 A 5315 6520833 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT UPPER MAIN DECK SURFACE OF FLOORBEAM HAS CORROSION AT NUT PLATE HOLE STA 1030, LBL 9". REMOVED CORROSION FROM AFT U PPER MAIN DECK UPPER SURFACE FLOORBEAM STA 1030, LBL 9". FOUND AREAS OF CORROSION REMOVAL TO BE OUT OF LIMITS. REMOVED DAMAGE SECTION OF FLOORBEAM AND INSTALLED REPAIR REF SRM 53-10-8 FIG 3. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007082200082 20070822 00082 NM 2007 8 22 07FDEA02868 1 20070814 A 5320 53FX1465 CHANNEL BOEING 727 727233 138408A NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LWR FWD CARGO PIT U-CHANNEL HAS 3 EXTRA HOLES ON UPPER LEG INBD END AT FWD SIDE OF STA 640 BELOW FRAME SPLICE AGAINST SK IN SHEAR TIE, BETWEEN STR 22L AND 23L. REMOVED U CHANNEL, REF SRM 51-30-2. FABRICATED NEW CHANNEL REF DWG 53FX1465 AND SENT FOR HEAT TREAT. LOCATED FASTENER HOLES ON U-CHANNEL REF SRM 51-30-5. ALODINE NAD PRIMED U-CHANNEL REF MM 51-20-2 1 AND 51-30-2. INSTALLED U-CHANNEL REF 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007082200084 20070822 00084 NM 2007 8 22 07FDEA02870 1 20070814 A 5320 69463461 WEB BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD LWR CARGO PIT, VERTICAL WEB HAS CORROSION AT LWR, BETWEEN STA 700 AND 720 STR 28L. REMOVED AND REPLACED VERTICAL WE B P/N 69-46346-1 REF SRM 51-30-2 DUE TO CORROSION. FASTENER COMMON TO SKIN WILL BE INSTALLED ON N/R N01157. THIS IS CL ASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007082200087 20070822 00087 EU 2007 8 22 07FDEA02874 1 20070814 A 5311 A305300101 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 653FE 736 FWD CARGO DOOR CUT-OUT STRUCTURE FR 20 HAS INCOMING CONDITION IMPACT DENT ON FRAME W/APPROX SIZE 4-IN LONG BY 2-IN WIDTH BY 0.25 DEPTH. (REF A300-600 AMM 53-13-11-6) SRM 53-10-13. CUT OUT DAMAGED SECTION AND DRILLED UP, REPAIR SECTION AND INSTALLED IAW FEDEX DRAWING SR30-53-001. 2 L 7 2 4F RT A35EU 2007082200089 20070822 00089 EU 2007 8 22 07FDEA02876 1 20070814 A 3411 PITOT HEAD AIRBUS 310 A310222 3930315 EU OBSTRUCTED A FDEA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 SO 25 453FE 267 REJECTED TAKEOFF AT APPROX 90 KNOTS DUE TO NO F/O A/S. FOUND BUG DEBRIS IN F/O PITOT PROBE CLEANED. INSPECTED PROBE PE R AMM 34-11-15-6, NO DEFECTS NOTED. F/O'S AIRSPEED CHECKED GOOD WITH PITOT TESTER. INSPECTED A/C BRAKES PER AMM 05-51- 16-0. NO DEFECTS NOTED. ALL TIRE PRESSURE CHECKED GOOD PER SERVICE CHECK. 2 L 7 2 4F RT A35EU 2007082200090 20070822 00090 WP 2007 8 22 07FDEA02877 1 20070814 A 5310 DOOR FRAME DOUG MD10 MD1010F 3022112 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 FOUND MAIN CARGO LOWER DOOR JAMB HAS CORROSION ON LOWER BEAM AT STA 750. 09-04-07 REMOVED AND REPLACED MAIN CARGO DOOR JAMB LOWER DOOR JAMB LOWER BEAM IN REF TO DC/MD10 SRM 51-33-01 VOL II PAGE 1, AND DAC DRAWING ACA7224 REV.G. MAJOR R EPAIR. 2 L 7 3 4F RT A22WE 2007082200091 20070822 00091 NM 2007 8 22 07FDEA02878 1 20070814 A 5313 65453132 STRINGER BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 PASSENGER CABIN STA 950D, STR 6R, STRINGER CLIP CRACKED. REMOVED STRINGER CLIP THAT WAS EXISTING, IAW SRM 51-30-02. RE PLACED WITH NEW STRINGER CLIP IAW SRM 51-30-02. THIS IS CLASSIFIED A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007082200092 20070822 00092 WP 2007 8 22 07FDEA02879 1 20070814 A 5511 ALC70082N SPAR DOUG MD10 MD1010F 3022112 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 RT HORIZONTAL STAB REAR SPAR CAP CRACKED ON AFT SIDE NEAR RT UPPER AFT BARREL NUT AT STA XE 48.500 CRACK EXTENDS APPROX 3.0", HORIZONTALLY FROM INBD END OF FITTING PER EDDY CURRENT TEST. ACCOMPLISHED EA 8-5510-109187"STABILIZER-HORIZ- AD92 -22-10-RH UPPER AFT SPAR SPLICE-REPAIR. MAJOR REPAIR MECH 7198 QC227 2 L 7 3 4F RT A22WE 2007082200093 20070822 00093 NM 2007 8 22 07FDEA02880 1 20070814 A 5330 SKIN BOEING 727 727233 138408A NM FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 286FE 22623 ON AGING A/C INSP FOUND, EXISTING INTERNAL SKIN REPAIR. REPAIR DID NOT CONFORM TO SRM 53-30-3 FIG 1. [08-28-07] REM OVED AND REPLACED PREVIOUS REPAIR REF. FED EX EA 7-5330-113262, REPLACED CORRODED STRINGER SECTION REF SRM 53-10-3, 51-3 0-2 TREATED AND PRIMED REF SRM 51-10-2. 2 L 7 3 4F RT A3WE 2007082200094 20070822 00094 EU 2007 8 22 07FDEA02881 1 20070814 A 5347 60224577075T76 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 653FE 736 FUSELAGE MAIN DECK SEAT TRACK 5L I/B FLANG PANEL LANDING HAS WEAK AROUND 7 EA FASTENER HOLES BETWEEN FRAMES 47-51 (ZONE 240) REF A300-600 SRM 51-10-00. BLENDED 7 AREAS AT LT 5L FR47-51 IAW A300-600 SRM 51-73-10. AFTER REWORK ALL 7 AREAS W ERE OUT OF LIMITS IAW A300-600 SRM 53-10-16. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW A300-600 SRM 5 1-72-10, 51-40-21 AND DWG A538-12915. 2 L 7 2 4F RT A35EU 2007082200095 20070822 00095 EU 2007 8 22 07FDEA02882 1 20070814 A 5347 60224577075T76 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 653FE 736 FUSELAGE MAIN DECK SEAT TRACK 2L GOUGED ON I/B FLANGE, AROUND 7 FASTENER HOLES BETWEEN FRAMES 43-47. REF A300-600 SRM 5 1-10-00 TOTAL AREA GOUGED 7 INCH APPROX BY 0.010 DEEP. BLENDED GOUGES IAW A300-600 SRM 51-73-10. SEAT TRACK OUT OF LIM ITS IAW A300-600 SRM 53-10-16. FABRICATED NEW SEAT TRACK IAW AIRBUS DWG A53832020. ALODINED NEW SEAT TRACK IAW A300 SR M 51-21-10. PRIMED TRACK IAW A300 SRM 51-75-10. TOP COATED TRACK IAW A300 SRM 51-75-10. INSTALLED TRACK IAW A300 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007082200096 20070822 00096 EU 2007 8 22 07FDEA02883 1 20070814 A 5311 20240080 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 653FE 736 MDCC AT FR 22 BETWEEN STG 17R AND STG 9R HAS 7 GOUGES APPROX 4" ZONE 230 REF A300-600 SRM 51-10-00. BLENDED 7 GOUGES FR 22 BETWEEN STR 7 AND 17R IAW A300-600 SRM 51-73-10 1EA AREA OUT OF LIMITS IAW A300 SRM 53-10-00 PG 101 B=.063 A=.046 L= .017. FABRICATED AND INSTALLED FRAME REPAIR IAW A300-600 FREIGHTER SRM 53-10-13 FIG 202. ALODINED IAW A300 SRM 51-21-1 0. PRIMED AREA IAW A300 SRM 51-75-10. 2 L 7 2 4F RT A35EU 2007082200098 20070822 00098 NM 2007 8 22 07FDEA02885 1 20070814 A 5720 652165831 CHANNEL BOEING 727 7272S2F 1384O81 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 212FE 22934 LT WING AR T/E REAR SPAR AREA APPROX RS STA491. LOWER FIXED PANEL UPPER INBD CHORD MOUNT BRACKET HAS A CRACK BELOW SPOI LER PNL NR 3. REMOVED AND REPLACED BRACKET IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2007082200099 20070822 00099 EU 2007 8 22 07FDEA02886 1 20070814 A 5313 DAN50806 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT PIT FRAME 63 STRINGER 48R CORRODED REMOVED CORRODED AREA FABBED REPAIR PARTS (STRINGER AND COUPLING) INSTALLED REPAI R PER A310-200 SRM 53-10-14, 51-21-10, 51-23-10, AND DRAWING A53974202. 2 L 7 2 4F RT A35EU 2007082200100 20070822 00100 EU 2007 8 22 07FDEA02887 1 20070814 A 5313 DAN50806 STRINGER AIRBUS 310 A310203 3930313 EU FUSLEAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 ALC STR 48R CORRODED BETWEEN FR 58 AND FR 60 REMOVED CORRODED AREA PER A310-200 SRM 51-40-21. FABBED REPAIR (STRINGER A ND COUPLING) PER A310-200 SRM 53-10-14 PG 203, 51-21-10,51-23-10. INSTALLED REPAIR PARTS PER A310-200 SRM 53-10-14. 2 L 7 2 4F RT A35EU 2007082200101 20070822 00101 EA 2007 8 22 SWIA200718568 1 20070807 A 3320 BALLAST CNDAIR CL600 CL6002B19 1900309 EA CABIN LIGHTS ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 432SW 7548 FLIGHT NR 3968, FLIGHT ATTENDANT SMELLED ELECTRICAL SMOKE NEAR AN OVERHEAD BIN. REPLACED SIDEWALL LIGHT BALLAST IAW 33- 21-10. OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2007082200103 20070822 00103 EA 2007 8 22 SWIA200718570 1 20070809 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCONNECTED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 710BR 7852 FORWARD BULKHEAD EXIT SIGN IS INOP, FLIGHT NR 2878. RESECURED CONNECTOR. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007082200105 20070822 00105 SO 2007 8 22 SWIA200718572 1 20070731 A 5210 DOOR EMB 120 EMB120ER 3260203 SO MAIN PAX BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 566SW 120341 MAIN CABIN DOOR IS DIFFICULT TO OPEN, FLIGHT NR 5553. CLEANED AND LUBED MAIN CABIN DOOR. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007082200107 20070822 00107 2007 8 22 SWIA200718574 4 20070812 A 2562 CONNECTOR EMB 120 EMB120ER 3260203 SO ELT DISCONNECTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 583SW 120351 ELT TOGGLE SWITCH HAS A RED LIGHT BLINKING. RECONNECTED ELT CONNECTOR IAW MM 25-61-03. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007082200108 20070822 00108 EA 2007 8 22 SWIA200718575 1 20070812 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 978SW 7953 ON GEAR EXTENSION, RECEIVED GEAR DISAGREE MESSAGE. CYCLED GEAR AND NORMAL INDICATIONS APPEARED, FLIGHT NR 5953. REPLAC ED LANDING GEAR SELECTOR VALVE IAW 32-33-10. GEAR SWING OPS CHECK GOOD AND VALVE LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2007082200109 20070822 00109 SO 2007 8 22 SWIA200718576 1 20070808 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DISCHARGED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 569SW 13661 13661 120344 FLIGHT ATTENDANT REPORTS THAT 4 FLOOR EMERGENCY LIGHTS DO NOT WORK, FLIGHT NR 5572. REPLACED EMERGENCY BATTERY PACK. 2 L 7 2 4T RT A31SO 2007082200110 20070822 00110 SO 2007 8 22 SWIA200718577 1 20070805 A 3350 FUSE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS BLOWN A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 561SW 120335 EMERGENCY LIGHT OVER ROW 3 IS INOP, FLIGHT NR 5578. REPLACED BLOWN FUSE. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007082200112 20070822 00112 EA 2007 8 22 SWIA200718579 1 20070810 A 3397 CIRCUIT CARD CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 702SK 10136 EMERGENCY LIGHTS IN CABIN FLASH ON AND OFF WHEN SWITCH IS IN THE ARMED POSITION, FLIGHT NR 6465. REPLACED CIRCUIT CARD NR 5 IN JB11 IAW CRJ 700 MM 24-10-01. 2 L 7 2 4F RT A21EA 2007082200114 20070822 00114 NE 2007 8 22 F3LA200700198 2 20070813 A 7532 39680012 MOTOR AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE BLEED VALVE INOPERATIVE A F3LA O OTHER O OTHER DE DESCENT 1 NM 03 938FR 3019 2406 577206 FLIGHT CREW REPORTED ENG 1 COMPRESSOR VANE ECAM MILD COMPRESSOR STALLS DURING DESCENT. CONTINUED FLIGHT WITH AUTOTHRUST OFF. REPLACED NR 1 ENGINE BLEED VALVE FUEL GENERATOR MOTOR ASSY. PERFORMED FADEC MOTORING TEST, NO FAULTS NOTED. NO LEAKAGE NOTED ON MIN IDLE LEAK CHECK IAW AMM 75-31-10, PB 401 AND TSM 75-30-00-810-801. ACCOMPLISHED BORESCOPE IAW AMM 72-31-00-290-002. NO DAMAGE NOTED. INSPECTED BLADES IAW AMM 72-31-290-051. NO DAMAGE NOTED. 2 L 7 2 4F 4 F RT A28NM E37NE 2007082200115 20070822 00115 CE 2007 8 22 ZLWA0702 1 20070812 A 4990 SEAL GARRTT GTCP36150W CESSNA 650 650 2076802 CE ZONE 400 BLOWN E ZLWA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 05 650K 1850 P211 6507034 WITH APU BLEED AIR ON, GOT BLUE SMOKE IN COCKPIT AND CABIN. 2 L 7 2 4F A9NM 2007082200116 20070822 00116 CE 2007 8 22 ZLWA0701 1 20070812 A 4990 SEAL GARRTT GTCP36150W CESSNA 650 650 2076802 CE APU BAY BLOWN E ZLWA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 05 650K 1850 P211 6507034 WITH APU BLEED AIR ON, GOT BLUE SMOKE IN COCKPIT AND CABIN. 2 L 7 2 4F A9NM 2007082200120 20070822 00120 SO 2007 8 22 SIMA200722711 1 20070813 A 5347 13500439003 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 724AE 15687 5000 145301 LEFT OUTBOARD SEAT TRACK NUMBER 2 FOUND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW IAW EMB AMM 53-01-06. OPERATIONA L CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082200121 20070822 00121 SO 2007 8 22 SIMA200722713 1 20070813 A 5347 13500439001 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 724AE 15687 5000 145301 LEFT INBOARD SEAT TRACK NUMBER 2 FOUND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERATIONAL CHE CK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082200122 20070822 00122 EA 2007 8 22 SIMA200722716 1 20070807 A 5315 CC670341757 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 506AE 11507 5000 10056 FOUND STATION 280 FLOORBEAM CORRODED ALONG TOP FLANGE. SPLICED IN FRAME 280, SUPPORT AND EXTENTION MOUNTS IAW AMERICAN EAGLE ENGINEERING ORDER CR-53MR-119. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007082200123 20070822 00123 EU 2007 8 22 SIMA200722714 1 20070810 A 5347 7253001029 SEAT TRACK SAAB SF340 340B 7860101 EU ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 387AE 17939 5000 340B387 SEAT TRACK AT BL 18.3 FOUND CORRODED. REMOVED CORROSION IAW SAAB REPAIR STATEMENT 340D012793, DATED 31 JULY 2007. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007082200124 20070822 00124 SO 2007 8 22 SIMA200722705 1 20070814 A 3350 375911 SIGN EMB 135 EMB135LR 3260305 SO EMEGENCY LIGHTS FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 724AE 145301 CEILING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT SIGN IAW EMB AMM. OPERATIONAL CHECK GOOD. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082200125 20070822 00125 SO 2007 8 22 SIMA200722707 1 20070813 A 5347 1453260517 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 724AE 15687 5000 145301 RIGHT OUTBOARD SEAT TRACK NUMBER 4 FOUND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERATIONAL C HECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082200126 20070822 00126 SO 2007 8 22 SIMA200722709 1 20070813 A 5347 13500438001 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 724AE 15687 5000 145301 RIGHT INBOARD SEAT TRACK NUMBER 1 FOUND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERATIONAL CH ECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082200127 20070822 00127 SO 2007 8 22 SIMA200722712 1 20070813 A 5347 13500438003 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 724AE 15687 5000 145301 RIGHT OUTBOARD SEAT TRACK NUMBER 2 FOUND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW IAW EMB AMM 53-01-06. OPERATION AL CHECK GOOD - AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082200128 20070822 00128 SO 2007 8 22 SIMA200722708 1 20070813 A 5347 14532605015 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 724AE 15687 5000 145301 RIGHT OUTBOARD SEAT TRACK NUMBER 3 FOUND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW IAW EMB AMM 53-01-06. OPERATION AL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082200131 20070822 00131 EU 2007 8 22 SIMA200722717 1 20070813 A 5510 7255110009 ANGLE SAAB SF340 340B 7860101 EU ZONE 300 CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 298AE 20649 5000 340B298 LEFT HORIZONTAL STABILIZER FORWARD SPAR TO LEADING EDGE NOSE RIB ATTACHMENT ANGLE CRACKED. REPAIRED ANGLE IAW SAAB REPA IR STATEMENT 340 SDS 012809, DATED AUG 13, 2007. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007082200132 20070822 00132 EU 2007 8 22 SIMA200722715 1 20070808 A 5311 7253721493 FRAME SAAB SF340 340B 7860101 EU ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 298AE 20646 5000 340B298 FRAME 258 FOUND CORRODED. REPAIRED FRAME 258 IAW SAAB SRM 53-70-30. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007082200133 20070822 00133 WP 2007 8 22 IXXA070038O 1 20070810 A 3233 ACTUATOR DOUG DC8 DC873F 302199F WP LT MLG OUT OF ADJUST A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 603AL 98159 16 46003 DURING CLIMB-OUT FROM KTOL, THE GEAR DOORS NOT LATCHED LIGHT ILLUMINATED. THE CREW PERFORMED AN UP-LATCH CHECK AND THE LEFT MAIN GEAR DOOR OPEN YELLOW LIGHT ILLUMINATED. THE CREW RECYCLED GEAR AND HAD A SUCCESSFUL UPLATCH CHECK BUT DOOR N OT LATCHED LIGHT REMAINED ON. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE GEAR SY STEM AND FOUND THE LEFT MAIN LANDING GEAR ACTUATOR OUT OF ADJUSTMENT. MAINTENANCE ADJUSTED THE ACTUATOR IAW DACO MM 32- 32-2. MAINTENANCE JACKED THE AIRCRAFT AND CYCLED THE GEAR SEVERAL TIMES WITH NO FURTHER PROBLEMS. THE AIRCRAFT WAS RET URNED TO SERVICE. 2 L 7 4 4F RT 4A25 2007082200137 20070822 00137 NM 2007 8 22 QXEA200701328 1 20070310 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - AFT CARGO DOOR THRESHOLD HAS 2 NUTPLATE HOLES THAT APPEAR TO HAVE CORROSION ON DOUBLERS NUTPLATES ARE ATTACHED TO STATION 574 AND 590. REPAIRED IAW SRM 51-20-11, 51-20-16, AND 51-20-36. 2 H 7 2 4T RT A13NM 2007082200138 20070822 00138 NM 2007 8 22 QXEA200701329 1 20070309 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - RIGHT WING LEADING EDGE BRACKET IS CRACKED AT YW 138.00. REPAIRED IAW SRM 51-40-11 AND 51-40-00. 2 H 7 2 4T RT A13NM 2007082200139 20070822 00139 NM 2007 8 22 QXEA200701330 1 20070309 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM LT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - AT LEFT WING STATION YW 222.4 THERE IS AN AREA OF SMALL NICKS. REPAIRED IAW RD8-57-2996 AND SRM 51-20-11. 2 H 7 2 4T RT A13NM 2007082200142 20070822 00142 NM 2007 8 22 F3LA200700200 1 20070813 A 3240 BRAKE AIRBUS A319 A319111 3930336 NM MLG INOPERATIVE A F3LA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 03 927FR 2209 BLOCK TURN BACK, FLIGHT CREW REPORTED RT AFT BRAKE INOPERATIVE. SERVICED ALTERNATE BRAKE CONTROL RESERVOIR IAW AMM 32- 43-00-011-051. SYSTEM CHECKED NORMAL. 2 L 7 2 4F RT A28NM 2007082200144 20070822 00144 EU 2007 8 22 AWXA200700997 1 20070803 A 5330 D53231318200 SKIN AIRBUS 320 A320231 3930325 EU ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 632AW 81 SAL - MAJOR REPAIR - C-07 CHECK - NR 5963515, CORROSION FOUND ON FWD CARGO COMPARTMENT INNER SKIN, BS 1217/FR 29+12" - B S 1270/FR 30, S43L, +Y50. REPAIRED FWD CARGO COMPARTMENT INNER SKIN, BS 1217/FR 29+12" - BS 1270/FR 30, S43L, +Y50 IAW A320 ARM 53-00-11, FIG 203. 2 L 7 2 4F RT A28NM 2007082200145 20070822 00145 NM 2007 8 22 AALA20071445 1 20070629 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 930AN 29529 TUL - EMERGENCY LIGHT AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT 7F FOR EMERGENCY LIGHT AT FORWARD CAB IN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007082200146 20070822 00146 NM 2007 8 22 AALA20071442 1 20070629 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 930AN 29529 TUL - EMERGENCY LIGHTS AT FORWARD COACH INOPERATIVE. REPLACED BATTERY PACK AT SEAT 12B FOR EMERGENCY LIGHT AT FORWARD C OACH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007082200147 20070822 00147 NM 2007 8 22 AALA20071426 1 20070805 A 3350 LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 324AA 22325 JFK - EMERGENCY LIGHT AT SEAT ROW 19B INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007082200148 20070822 00148 NM 2007 8 22 AALA20071431 1 20070807 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 187AN 32381 LAX - EMERGENCY EXIT SIGN LIGHT AT RIGHT FORWARD OVERWING INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY EXIT SIGN LIGHT AT RIGHT HAND FORWARD OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007082200149 20070822 00149 NM 2007 8 22 AALA20071437 1 20070626 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 967AN 29545 TUL - EMERGENCY LIGHT IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007082200150 20070822 00150 NM 2007 8 22 AALA20071438 1 20070626 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 967AN 29545 TUL - EMERGENCY LIGHT IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007082200151 20070822 00151 NM 2007 8 22 AALA20071439 1 20070626 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 967AN 29545 TUL - EMERGENCY LIGHT IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007082200152 20070822 00152 NM 2007 8 22 AALA20071440 1 20070629 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 930AN 29529 TUL - EMERGENCY LIGHT AT AFT GALLEY OVERHEAD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT GALLEY OVERH EAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007082200153 20070822 00153 NM 2007 8 22 AALA20071428 1 20070807 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 796AN 30796 LGW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007082200155 20070822 00155 NM 2007 8 22 AALA20071435 1 20070618 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 929AN 30078 TUL - EMERGENCY LIGHT AT AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT GALLEY. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007082200157 20070822 00157 NM 2007 8 22 AALA20071441 1 20070629 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 930AN 29529 TUL - EMERGENCY LIGHT AT FORWARD ENTRY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007082200158 20070822 00158 NM 2007 8 22 AALA20071425 1 20070805 A 3350 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 324AA 22325 JFK - EMERGENCY LIGHTS AT SEAT ROWS 10 AND 11 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 10 A ND 11. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007082200160 20070822 00160 NE 2007 8 22 AALA20071429 2 20070807 A 7210 GEARBOX BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4 54555 NE LEFT ENGINE CONTAMINATED A AALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SW 21 692AA 26972 31141 DEN INFLIGHT T844/07AUG SNA TO ORD - LEFT ENGINE VIBRATION FOLLOWED BY LOW ENGINE GAS TEMPERATURE AND LOW OIL PRESSURE I NDICATIONS. SHUT DOWN LEFT ENGINE AND LANDED DEN WITHOUT INCIDENT. SINGLE ENGINE TIME 19 MINUTES. FOUND GEARBOX CHIP DETECTORS CONTAMINATED WITH METAL. REPLACED NUMBER ONE ENGINE ON 07 AUGUST AT DEN. SYSTEM GROUND CHECKED NORMAL OPERATI ON. 2 L 7 2 4F 4 F RT A2NM E12EU 2007082200161 20070822 00161 NM 2007 8 22 AALA20071424 1 20070807 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 966AN 30094 MIA - EMERGENCY LIGHT AT SEAT ROW 22D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 22D. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007082200163 20070822 00163 NM 2007 8 22 AALA20071430 1 20070807 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 345AN 33084 DFW - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED BULB FOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOO R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007082200164 20070822 00164 WP 2007 8 22 AALA20071433 1 20070807 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 471AA 49601 BOS - EMERGENCY LIGHTS AT RIGHT AND LEFT AFT AUXILIARY DOORS INOPERATIVE. REPLACED BATTERY PACK AT BIN 20DEF FOR EMERGE NCY LIGHT AT SEAT ROW 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007082200167 20070822 00167 WP 2007 8 22 07FDEA01276 1 20070403 A 5330 ACA38541 SKIN DOUG MD10 MD1010F 3022112 WP FUSELAGE UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 EXTERNAL FUSELAGE STA 475 RT LOWER FUSELAGE CUT OUT NOSE W/W. REPAIRED IAW FEDEX EA8-5310-105639. 2 L 7 3 4F RT A22WE 2007082200168 20070822 00168 NM 2007 8 22 07FDEA02888 1 20070814 A 5340 654531346 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 PASSENGER CABIN STA 990 STR 9R, STRINGER CLIP CRACKED. REMOVED AND REPLACED PASSENGER CABIN STRINGER CLIP, AT STA 990 A T STR 9R CLIP IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007082200171 20070822 00171 EU 2007 8 22 07FDEA02891 1 20070815 A 5320 A53812635203 SPLICE AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 CRACKS FOUND ON FUSELAGE CENTER SECTION, C47 SPLICE FITTING, P24-26 RT IN SEVERAL HOLES (B, D, K, M, A3). REPAIR PEROFR MED BY REAM UP UNTIL CRACK REMOVAL IAW EA 6-5315-106505 AND RAS/053356/009/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082200173 20070822 00173 EU 2007 8 22 07FDEA02893 1 20070815 A 5711 A57110431200 SPAR AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 CRACKED HOLES AT CENTER SPAR DOUBLER RUN OUT AT C44 LT, RELATED P/N WEB A571-10431-200, HOLE C, D IAW SB 53-242. REPAIR PERFORMED BY REAM UP UNTIL CRACK REMOVAL IAW EA 6-5710-112482 AND RAS/053466/009/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082200176 20070822 00176 NM 2007 8 22 07FDEA02896 1 20070815 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 STATION 720 AND STR 6L HAS A STRINGER CLIP CRACKED REPLACED STR CLIP AT STA 720, STR 6L REF SRM 51-30-2. THIS IS CLASSI FIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007082200178 20070822 00178 NM 2007 8 22 07FDEA02898 1 20070815 A 5340 654531313 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 STRINGER CLIP CRACKED AT 970, STR 9L INSTALLED STRINGER CLIP AS PER SRM 51-30-02, THIS IS CLASSIFID AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007082200179 20070822 00179 NM 2007 8 22 07FDEA02899 1 20070815 A 5754 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 595FE 48553 LEFT WING FIXED LEADING EDGE SLAT COVER CUTOUT OUTBOARD CORNER AT STA XOS = 774 FOUND CRACKED. 08-31-07 REPAIR CARRIE D OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. FABRICATED FILLER AND DOUBLER INSTALLED AS PER SRM 51-33-01 VOLUME II. REP AIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007082200180 20070822 00180 NM 2007 8 22 07FDEA02900 1 20070815 A 5754 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 595FE 48553 LEFT WING FIXED LEADING EDGE SLAT TRACK COVER CUTOUT OUTBOARD CORNER AT STA XOS = 832, FOUND CRACKED. REPAIR CARRIED OU T AT LEFT HAND WING FIXED LEADING EDGE STA XOS = 889 SLAT TRACK COVER CUTOUT AREA AS PER SRM 57-100-00 FIGURE 21 VOL UME I. REPAIR CLASSIFIED AS MINOR PER GMM 6 -2-100. 2 L 7 3 4F RT A22WE 2007082200182 20070822 00182 NM 2007 8 22 07FDEA02902 1 20070815 A 5754 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 595FE 48553 RIGHT WING NR 6 SLAT FOUND WITH DENTS. 08-31-07 MEASURED AND FOUND 4 AREAS EXCEEDED LIMIT. REPAIR CARRIED OUT AS PE R SRM 57-10-00 FIGURE 16 VOLUME I. ALL DENT AREAS REPROTECTED AS PER SRM 51-21-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007082200183 20070822 00183 NM 2007 8 22 07FDEA02903 1 20070815 A 5712 RIB DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 595FE 48553 RIGHT WING SLAT TRACK NR 16 RIB FOUND CRACKED. 08-31-07 REMOVED AND REPLACED AS PER SRM 51- 35-01 VOLUME II AND SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007082200184 20070822 00184 NM 2007 8 22 07FDEA02904 1 20070815 A 5340 654531314 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 PASSENGER CABIN STA 620, STR 9R, STRINGER CLIP CRACKED REMOVED CRACKED STRINGER CLIP. REPLACED STRINGER CLIP WITH NEW C LIP REF SRM 51-30-02, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007082200186 20070822 00186 EU 2007 8 22 07FDEA02906 1 20070815 A 5320 STRUCTURE AIRBUS 300 A300B4605R 3930308 EU EMERGENCY EXIT CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 SCRUB MARKS ON RT AFT EMERGENCY EXIT CROSS SHEET REPAIR PERFORMED BY BLEND OUT IAW SRM 51-73-10, APPROVED BY EA 6-5316-1 12503 AND RAS/DAHAM/4022567/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082200187 20070822 00187 EU 2007 8 22 07FDEA02907 1 20070815 A 5330 A53973402200 SKIN AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORROSION FOUND ON BULK CARGO DOOR CUT OUT INTERNAL DOUBLER REPAIR PERFORMED BY BLEND OUT THE CORROSION AND FLAP PEENING IAW EA 6-5317-112502 AND RAS/DATLS/0003796/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082200188 20070822 00188 EU 2007 8 22 07FDEA02909 1 20070815 A 5320 A53612213212 FLOOR SUPPORT AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORROSION ON SUPPORT FLOOR, C12A-15A RT, Y-1959 SPLICE REPAIR PERFORMED IAW. SRM 53-12-15 FIG 207. 2 L 7 2 4F RT A35EU 2007082200189 20070822 00189 EU 2007 8 22 07FDEA02910 1 20070815 A 5320 A53612213202 FLOOR SUPPORT AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORROSION ON FLOOR SUPPORT CC11-14, Y232 SPLICE REPAIR PERFORMED IAW SRM 53-12-15 FIG 207. 2 L 7 2 4F RT A35EU 2007082300001 20070823 00001 NM 2007 8 23 KCSA071295 1 20070812 A 5330 SKIN BOEING 747 747246B 1384864 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 700CK 22990 FUSELAGE SKIN DAMAGED, BS 670 TO 685 BETWEEN STR 37R AND STR 38R. 2 L 7 4 4F RT A20WE 2007082300002 20070823 00002 NM 2007 8 23 BB07062 1 20070808 A 3233 19323040005 ACTUATOR BOEING 757 757225 1384959 NM RT MLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 924UW 22204 FLIGHT 871, CLT-AUA: AFTER TAKEOFF, CREW RECEIVED GEAR DOORS AND GEAR DISAGREE MESSAGES. FLIGHT RETURNED TO CLT. MAIN TENANCE REPLACED THE RIGHT GEAR RETRACT ACTUATOR. NO FURTHER FAULTS. 2 L 7 2 4F RT A2NM 2007082300004 20070823 00004 EU 2007 8 23 07FDEA02912 1 20070815 A 5313 A53986212 STRINGER AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORROSION ON STRINGER P56 RT, C63-69 AND P56 LT, C65-69 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007082300009 20070823 00009 EU 2007 8 23 SA07050 1 20070810 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU CABIN FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 754UW 19969 488 1328 TPA - DURING THE TEST OF THE EMERGENCY LIGHTS SYSTEM, THE RIGHT SIDE, OVERWING EXIT SEAT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE RIGHT SIDE, MID-CABIN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007082300011 20070823 00011 EU 2007 8 23 UPS07150423 1 20070728 A 5330 SKIN AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 133UP 0816 INSPECTION TYPE:1C3C DENT ON RT SIDE FUSELAGE FWD FR 9.1" BELOW PITOT MAST. CUT OUT DENT, FABRICATED AND INSTALLED DOUB LER AND FILLER IAW SRM 53-11-12 FIG 201. 2 L 7 2 4F RT A35EU 2007082300012 20070823 00012 NM 2007 8 23 UPS07650416 1 20070808 A 4920 APU BOEING 767 76734AF 1385212 NM MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 314UP 27742 INSPECTION TYPE:ETOP APU INOP, WILL NOT START DEFERRED PER MEL 49-11-1-0-2. INSTALLED NEW ECU, NO HELP. PLACARD INSTAL LED. D356179 *SUPPLEMENTAL SDR* APU OPS CHECK IAW AMM 49-11-00 SATISFACTORY. DMI 356179 NOW CLOSED. 2 L 7 2 4F RT A1NM 2007082100164 20070821 00164 NM 2007 8 21 KCSA071284 1 20070808 A 5711 SPAR BOEING 747 7472B4B 138481B NM RT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 COMPOSITE FILLER BULGING NEAR AFT SPAR RT WING UPPER SURFACE WS 597. 2 L 7 4 4F RT A20WE 2007082100166 20070821 00166 NM 2007 8 21 KCSA071285 1 20070808 A 5320 SUPPORT FITTING BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 C-2 DOOR CUTOUT LOWER AFT LATCH I/B SUPPORT FITTING IS CORRODED ON THE AFT FLANGE AT STA 1918 RBL 52. 2 L 7 4 4F RT A20WE 2007082100177 20070821 00177 EA 2007 8 21 TRAX200701087 1 20070730 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 854AS 7382 FS 280 CENTER WEB HAS CORROSION FOUND TO BE OUT OF LIMITS, REQUIRES REO 601R-53-11-926. C/W EC/TC REO 601R-53-11-1218 J A13231 8-4-07 & REO 601R-53-11-926 TH13774, SEE ATTACHED 409A FOR REMOVAL STEPS: SEE ATTACHED 409B FOR STEPS COMPLETED. SUPPLEMENTAL - SDR CLOSED 08/09/07. 2 L 7 2 4F RT A21EA 2007082100193 20070821 00193 NM 2007 8 21 WRLA2007080 1 20070804 A 5720 STRUCTURE DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE LT WING CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 801DE 48472 DURING 1C+12A CHECK, EGAT MAINT FOUND CRACK ON LT WING ANTI-ICING TELESCOPING DUCT DOOR CUTOUT AT STA XOS=464 & XOS=470. CRACK REPAIRED PER MD-11 SRM VOL 1 57-10-00 FIG 43 REV 39 & EI 2006P20A-124 REV 00. (REPAIR DOUBLER) 2 L 7 3 4F 4 F RT A22WE E24NE 2007082100208 20070821 00208 NM 2007 8 21 USAA920070800 1 20070807 A 5210 141N6100216 DOOR FRAME BOEING 757 757225 1384959 NM L1 DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 923UW 22203 PIT - MAJOR REPAIR - C4 CHECK, CORROSION ON THE L1 DOOR AFT FRAME, BS 375, S11L - S12L. REPAIRED THE L1 DOOR AFT FRAME, BS 375, S11L - S12L IAW B757-200 SRM 51-70-13 AND 52-10-02. 2 L 7 2 4F RT A2NM 2007082100212 20070821 00212 NM 2007 8 21 KCSA071289 1 20070809 A 5420 STIFFENER BOEING 747 7472B4B 138481B NM NR 2 PYLON WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NR 2 PYLON I/B LOWER WEB STIFFENER BY MAIN PNEUMATIC DUCT HAS WORN HOLE AT DUCT ATTACHMENT. 2 L 7 4 4F RT A20WE 2007082100235 20070821 00235 NM 2007 8 21 UPS07450412 1 20070727 A 2612 FIRE LOOP BOEING 747 747200 1384847 NM NR 4 ENGINE DAMAGED A IPXA K NONE N FALSE WARNING CL CLIMB 1 SO 01 523UP 22381 INSPECTION TYPE:N/A ON CLIMBOUT THE FWD PANEL FIRE DETECTION LIGHT WAS FLICKERING; NR 4 ENGINE NACELLE TEMP IND -A- WAS FLICKERING FROM 0 TO 9 AT SAME TIME & RATE AS FIRE DETECTION LIGHT. THIS IS INTERMITTENT; SELECTED LOOP-B. THE SYSTEM TEST AND WORKS. FOUND ALL ENG LOOP -A- MODULE HEAT DAMAGED. REMOVED AND REPLACED PER MM 26-11-03. OPS CHECK GOOD. 2 L 7 4 4F RT A20WE 2007082100240 20070821 00240 NM 2007 8 21 UPS07650415 1 20070808 A 4950 BLEED AIR SYS BOEING 767 76734AF 1385212 NM APU INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 323UP 27749 INSPECTION TYPE:ETOP NO APU BLEED AIR. BTB FOR EXTERNAL AIR CART. C/O OPERATIONAL TEST OF APU BLEED AIR IAW AMM 49-52- 00-00. FOUND SATISFACTORY. 2 L 7 2 4F RT A1NM 2007082100243 20070821 00243 2007 8 21 UPS07850414 4 20070803 A 2565 SLIDE DOUG DC8 DC871F 302199D WP CREW ENTRY DOOR OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:N/A CREW REPORTED TO MX THAT EMERGENCY SLIDE PACK ON CREW ENTRY DOOR FELL OUT OF COMPARTMENT. RE-INSTAL LED EMERGENCY SLIDE ON THE CREW ENTRY DOOR, OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2007082100251 20070821 00251 EA 2007 8 21 TRAX200701122 1 20070806 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A AOSA K NONE O OTHER IN INSP/MAINT 1 SO 27 755EV 10185 RIGHT SIDE SEAT RAIL HAS CORROSION IN TWO PLACES AFT OF EMERGENCY DOOR (MARKED IN RED). 2 L 7 2 4F RT A21EA 2007082100254 20070821 00254 EU 2007 8 21 TRAX200701125 1 20070806 A 5753 BRACKET AEROSP ATR72 ATR72 EU T/E FLAP CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 LEFT WING INBOARD FLAP BEAM NR 2, 3 OMEGA BRACKET CRACKED. 2 H 7 2 4T RT 2007082100259 20070821 00259 EA 2007 8 21 TRAX200701129 1 20070806 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 930EV 8014 F/A'S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007082100264 20070821 00264 EU 2007 8 21 TRAX200701134 1 20070807 A 5720 ANGLE AEROSP ATR72 ATR72 EU LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 LEFT WING BOX FR 28 FAIRING FRAME ANGLE CRACKED. REPAIRED AS PER ANA/YUL07/192/375-004 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SP663 AND FAR 43 APPENDIX A. 2 H 7 2 4T RT 2007082100321 20070821 00321 NM 2007 8 21 SWAA073969 1 20070809 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 488A, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007082100323 20070821 00323 NM 2007 8 21 SWAA073959 1 20070809 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007082100329 20070821 00329 NM 2007 8 21 SWAA073957 1 20070809 A 5311 6546550 FRAME BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007082100333 20070821 00333 NM 2007 8 21 SWAA073954 1 20070809 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 23L. REPAIRED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007082100339 20070821 00339 NM 2007 8 21 SWAA073962 1 20070809 A 5330 65C34798 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 619SW 28035 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007082100350 20070821 00350 EU 2007 8 21 USAA070648 1 20070810 A 5315 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 177US 1517 AROUND FASTENER HOLES & TOPSIDE OF FLOORBEAM, FR 66-69 HAS CORROSION. INSTALLED NEW FLOORBEAM PER SRM 51-72-11; CORR TA SK JA-260-53500, DEFECT SIZE: 1.5 X 1.5 INCH. 2 L 7 2 4F RT A28NM 2007082100378 20070821 00378 NM 2007 8 21 KCSA071293 1 20070810 A 5420 ATTACH ANGLE BOEING 747 7472B4B 138481B NM NR 1 PYLON DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 COMP DUCT ATTACH ANGLE DAMAGE I/B SIDE LOWER SURFACE OF NR 1 PYLON. 2 L 7 4 4F RT A20WE 2007082200002 20070822 00002 NM 2007 8 22 DHL2007741560 1 20070806 A 5313 STRINGER BOEING 727 7272Q9 138448M NM BS 480 S26R CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 STRINGER 26R CORRODED AT BS 480. CORROSION FOUND TO EXIST ON STR SPLICE AT BS 480. REMOVED, STR SPLICE, FABRICATED NEW SPLICE FROM 7075-T6, .040" BY 13" BY 5", PO NR 9004940, PER B727 SRM 53-10-2 FIG 9, 51-10-3, AND 51-20-1. TREATED, PRI MED, AND INSTALLED NEW STR SPLICE SECTION PER B727 SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007082200008 20070822 00008 NM 2007 8 22 QXEA200701280 1 20070812 A 2750 C1486561 DRIVE UNIT BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 417QX 9120 9120 4086 GEG FLIGHT NR 2354: CREW REPORTED FLAP DRIVE CAUTION LIGHT. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE C/W FIM TASK 27-50 -00-810-801. REPLACED FPU IAW AMM 27-52-01-000-801 AND 27-52-01-400-801. FUNCTIONAL CHECK IAW 27-52-00-720-801. TESTS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007082200016 20070822 00016 NM 2007 8 22 DL76L071033 1 20070806 A 7932 TRANSMITTER BOEING 767 767332 1382001 NM NR 2 ENG OIL SYS MALFUNCTIONED A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 183DN 10735 N 27110 RTB DUE TO RT ENG OIL QTY DROPPED TO 6 AFTER ENG START. FWD OIL QTY INDICATION TO MCO PER MEL 79-31-01. VERIFIED OIL T ANK FULL. NO OIL WAS ADDED. REPLACED OIL QUANTITY TRANSMITTER T 675 PER M/M RAN NR 2 ENG PER PFHB OIL TEMP ROSE OIL PR ESSURE GOOD AFTER ENG SHUTDOWN CHECKED OIL LEVEL ENG REQUIRED 11 PINTS TO BRING TO FULL MC AND PLACARD REMOVED. 2 L 7 2 4F RT A1NM 2007082200022 20070822 00022 NE 2007 8 22 DL76S071046 2 20070808 A 7320 8062644 MEC BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 ENGINE MALFUNCTIONED A DALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 124DE 23438 RTO DUE TO RT ENGINE WOULD NOT MAKE TAKEOFF POWER. REPLACED RT ENGINE MEC. AFTER RUNUP ENGINE MAKES TAKEOFF POWER. 2 L 7 2 4F 4 F RT A1NM E13NE 2007082200044 20070822 00044 NM 2007 8 22 EIA2007144 1 20070717 A 5315 FLOORBEAM BOEING 747 747230B 1384889 NM FUSELAGE LOOSE A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 488EV 23287 2 FASTENERS MISSING AND 2 NOT TIGHTENED ON UPPER TEE OF FLOORBEAM STA 1460 BELOW CARGO TIE DOWN FITTING RBL 57 (BELOW FL OOR PANEL). REPAIRED STA 1460 FLOORBEAM AT RBL 57 PER ECRA 488-53-025-2. 2 L 7 4 4F A20WE 2007082200050 20070822 00050 NM 2007 8 22 EIA2007102 1 20070511 A 3350 1317 BULB BOEING 747 747131 1384881 NM EMERGENCY LIGHTS INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481EV 19806 DOOR FRAME AT R5 EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW MM 33-51-00. 2 L 7 4 4F A20WE 2007082200051 20070822 00051 NM 2007 8 22 EIA2007118 1 20070529 A 3244 2600356152 TIRE BOEING 747 747273C 1384896 NM NLG FAILED A EIAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 470EV 20653 ON TAKEOFF, TOWER REPORTED SMOKE FROM NOSEGEAR RETURNED TO JFK. ON WALKAROUND, FOUND DAMAGE ON RT NLG TIRE (RECAP CAME OFF). ALL NOSE TIRES REPLACED IAW. 2 L 7 4 4F A20WE 2007082200060 20070822 00060 NM 2007 8 22 EIA2007130 1 20070613 A 3350 S1356B37 LIGHT BOEING 747 747132 1384882 NM CABIN INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481EV 19896 EMERGENCY LIGHT RT AFT UPPER DECK LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY, OPS CHECKED NORMAL PER B747 MM 33-51-07. 2 L 7 4 4F A20WE 2007082200064 20070822 00064 NM 2007 8 22 EIA2007134 1 20070628 A 3350 3004181A LIGHT BOEING 747 747121 1384871 NM L5 DOOR NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480EV 20348 L/5 EMERGENCY LIGHT INOP. REMOVED AND REPLACED L/5 EMERGENCY LIGHT, OPS CK`D NORMAL PER B747 MM 33-51-06. 2 L 7 4 4F A20WE 2007082200067 20070822 00067 NM 2007 8 22 EIA2007137 1 20070612 A 5330 SKIN BOEING 747 747230B 1384889 NM BS 2364 DENTED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 488EV 23287 OUTWARD DENT IN FUSELAGE SKIN STA 2364 STRINGER 15L. REPAIRED SKIN AT STA 2364 STRINGER 15L PER B747 SRM 53-30-03 FIG 4 7. 2 L 7 4 4F A20WE 2007082200068 20070822 00068 NM 2007 8 22 EIA2007138 1 20070713 A 5311 65B05002186 FRAME BOEING 747 747230B 1384889 NM BS 800 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 488EV 23287 NR 2R DOOR FRAME STA 800 STR 18R WEB CRACKED. REPAIRED PER EOA ECRA 488-53-023-2 PAGE 1. 2 L 7 4 4F A20WE 2007082200079 20070822 00079 WP 2007 8 22 07FDEA02864 1 20070813 A 5347 S4929405 SEAT TRACK DOUG MD10 MD1010F 3022112 WP BS 1199-1219 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 GOUGED/SCUFFED SCALLOPS ON CABIN SEAT TRACK AT STA 1199, TO 1219, RBL 47.5 REMOVED SEAT TRACK SECTION AT STA 1209-1269 R BL 47 IAW DC-10/MD-10 SRM 51-31-01, VOL2, PG 1. MAT ID FOR SEAT TRACK SECTION IS S4929405 PO 571558.2 IAW DC-10/MD10 SR M 53-42-01, VOL 2 PG 13 AND 14. INSTALLED SEAT TRACK SECTION AT STA 1209-1269 RBL 47 IAW DC-10/MD-10 SRM 51-31-01, VOL 2 PG 1. THIS REPAIR IS CLASSIFIED AS MAJOR. 2 L 7 3 4F RT A22WE 2007082200085 20070822 00085 NM 2007 8 22 07FDEA02871 1 20070814 A 5720 311N50584 BUSHING BOEING BOEING 757 7572B7 1384964 NM ZONE 400 MISALIGNED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 901FD 27122 ACCOMPLISHED DVI OF THE LT WING OUT BOARD DRAG FITTING AND FOUND THE INBOARD SIDE BUSHING MIGRATED .060 INCH. REMOVED B USHINGS IAW SOPM 20-50-03. HFEC INSPECTED FITTING IAW NTM 51-00-16, PT.6. NO DEFECTS NOTED. HONED, CHAMFERED AND FLAP PENNED LUG BORES IAW EA F-5450-108892. FINAL LUG BORE DIAMETER 1.7507. TREATED AND PRIMED LUGS IAW EA F-5450-108892. INSTALLED BUSHINGS, SEALANT AND WASHERS IAW EA F-5450-108892. 2 L 7 2 4F RT A2NM 2007082200134 20070822 00134 WP 2007 8 22 IXXA070039O 1 20070814 A 3297 WIRE DOUG DC8 DC871F 302199D WP ZONE 700 DAMAGED A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 829BX 92115 2443 45994 DURING CLIMB FROM KEWR, THE GEAR DOOR LIGHT ILLUMINATED DURING THE UPLATCH CHECK. THE CREW CYCLED THE GEAR. THE DOOR L IGHT REMAINED ON DURING AND AFTER THE UPLATCH CHECK. THE CREW CONTINUED THE FLIGHT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE GEAR SYSTEM AND REPLACED WIRE FROM GYRO BAY TO DOOR LIGHT DIMMER. PERFORMED OPERATIONAL CHE CK WAS GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 4 4F RT 4A25 2007082200136 20070822 00136 NE 2007 8 22 QXEA200701274 2 20070812 A 7200 3038400 ENGINE DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE MALFUNCTIONED A QXEA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 09 367PH 21277 534 511 SEA FLIGHT NR 2109 - DC GENERATOR FAIL, CUSTOMER NOTICED LEAK NR 2 NACELLE, ENGINE SHUTDOWN, CFR CALL. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 2 ENGINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007082200154 20070822 00154 NM 2007 8 22 AALA20071434 1 20070807 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 175AN 32394 LAX - EMERGENCY LIGHTS AT MID COACH INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID COACH. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007082200156 20070822 00156 NM 2007 8 22 AALA20071436 1 20070618 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 929AN 30078 TUL - EMERGENCY LIGHT AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD GALLEY. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007082200169 20070822 00169 2007 8 22 07FDEA02889 4 20070814 A 3460 COMPUTER DOUG MD10 MD1010F 3022112 WP FLT CONTROL MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 560FE 46938 ON APPROACH TO PDX, RECEIVED LVL 2 SLAT DISAG WHEN SELECTING 35 FLAPS. EXECUTED GO-AROUND AND RAN SLAT DISAG CHECKLIST IN QRH. LANDED WITH FLAPS 22/EXTEND. ON CHECK OPERATION OF SLATS PER MAINTENANCE MANUAL 27-84-00-5. SLAT OPERATES NO RMAL. FOUND FCC'S FAULTED AND AOA FAULTED. REMOVED AND REPLACED RT AOA SENSOR AND OPS CHECK PER MAINTENANCE MANUAL 22- 00-05-5. REMOVED AND REPLACED NR 1 FCC AND PERFORMED RTS AND AFS TEST PER MAINTENANCE MANUAL 22-00-00-5. TEST PASS. 2 L 7 3 4F RT A22WE 2007082200170 20070822 00170 EU 2007 8 22 07FDEA02890 1 20070815 A 5320 A53812635202 SPLICE AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 CRACKS IN SEVERAL HOLES ON FUSELAGE CENTER SECTION, C47 SPLICE FITTING, P24-26 LT, (HOLE G ,I ,L , M, A3, A4 ,A5 ,A6 , A 7, A8). REPAIR PERFORMED BY REAM UP THE HOLES UNTIL CRACK REMOVAL IAW EA 6-5315-106504 AND RAS/053351/014/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082200175 20070822 00175 EU 2007 8 22 07FDEA02895 1 20070815 A 5313 A53971006223 STRINGER AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 CORROSION FOUND ON P56 RT, C57.2-57.3 STRINGER REPAIR (CORROSION BLEND OUT AND COUPLING REPAIR) PERFORMED IAW EA 6-5316- 112484 A AND RAS/DATLS/0003790/2007 ISS B. 2 L 7 2 4F RT A35EU 2007082200181 20070822 00181 NM 2007 8 22 07FDEA02901 1 20070815 A 5100 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 600 NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 595FE 48553 RIGHT WING NR 7 SLAT FOUND WITH DENTS. CARRIED OUT AS PER DAC NDT SPM REV. 13 06- 10-01.001 AND FOUND NO CRACKS ON D ENTS. ALL DENT MARKS MEASURED AND FOUND WITHIN LIMIT AS PER SRM 57-10-00 FIGURE 16 VOLUME I. REWORKED AREA PROTECTED AS PER SRM 51-21-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007082200185 20070822 00185 NM 2007 8 22 07FDEA02905 1 20070815 A 5340 654531313 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 STRINGER CLIP CRACKED AT STA 950F AND STR. 9L REMOVED AND REPLACED CLIP REF SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007082300003 20070823 00003 EU 2007 8 23 07FDEA02911 1 20070809 A 2910 B-NUT AIRBUS 310 A310304 3930339 EU HYD LINE LEAKING A FDEA D RETURN TO BLOCK K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 25 816FD 593 AFTER ENGINE START CREW REPORTED SMOKE IN THE COCKPIT COMING FROM THE CASPER VENTS. FOUND HYDRAULIC RETURN LINE B NUT L EAKING AT PYLON ON NR 1 ENGINE. SECURED AND OPERATED ENGINE WITH NO LEAKS REMOVED AND REPLACED NR 1 PACK COALESCER BAG PER MM 21-51-16-3. OPERATED PACKS USING ENGINE BLEED AIR WITH NO SKYDROL VAPOR. COMPLETED PROCEDURE FOR CLEARING CONTA MINATION FROM A/C PACKS PER AMM 21-50-00-3. CLEANED COALESCER BAGS PER AMM 21-51-16-3. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2007082300010 20070823 00010 EA 2007 8 23 TRAX200701147 1 20070809 A 2612 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA COCKPIT INTERMITTENT A ASOA K NONE J WARNING INDICATION NR NOT REPORTED 1 SO 27 751EV 10163 FIRE SYS FAULT, STATUS MSG. COMES ON & OFF THROUGHOUT FLIGHT. 2 L 7 2 4F RT A21EA 2007082300014 20070823 00014 NM 2007 8 23 UPS07650428 1 20070812 A 2150 6806404 ACM BOEING 767 76734AF 1385212 NM A/C BAY SEIZED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 307UP 27760 INSPECTION TYPE:ETOP LEFT PACK TEMP DISPLAYED AFTER PUSHBACK - STBY & PACK RESET DID NOT FIX PROBLEM. BTB REQUIRED. PE RFORMED T/S AS PER FIM 21-51-00, FOUND LEFT AIR CYCLE MACHINE SEIZED. REMOVED AND REPLACED PER MM 21-51-03-4. OPS AND LEAK CHECKED. ALL SATISFACTORY. 2 L 7 2 4F RT A1NM 2007082300016 20070823 00016 WP 2007 8 23 UPS07850427 1 20070803 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 AFT PRESS BULKHEAD CRACKED RBL 24 L10R TO L12R. CUT OUT DAMAGED AREA ON AFT PRESS BULKHEAD STA 1766 RBL 24 L10R TO L12R IAW SRM 53-2-5. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER AT AFT PRESS BULKHEAD STA 1766 L 10R TO L12R IAW SRM 53-2-5 FIG 14A. 2 L 7 4 4F RT 4A25 2007082300018 20070823 00018 EU 2007 8 23 07FDEA02917 1 20070815 A 5320 A53970091216 CROSSBEAM AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORROSION ON CROSSBEAM C61 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007082300024 20070823 00024 NM 2007 8 23 07FDEA02921 1 20070815 A 5310 655714051 BEAM BOEING 727 727233 138408A NM ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 NR 1 LWR CARGO DOOR, LWR BEAM ANGLE, 3RD FROM AFT EDGE REMOVED, LOCATED AND DRILLED, AND INSTALLED LOWER BEAM ANGLE REF SRM 51-30-2 PG 1. RESTORED LEVELING COMPOUND REF OM MM 52-36-21,G. 406A. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007082300026 20070823 00026 2007 8 23 HALA0700338 4 20070814 A 2397 9640453011 COUPLER BOEING 767 76733A 1385209 NM NR 2 HF SYSTEM INOPERATIVE A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 593HA 33424 ETOPS SIGNIFICANT SYSTEM, NR 2 HF INOP. REMOVED AND REPLACED NR 2HF COUPLER GND CHK OK PER 23-11-01. 2 L 7 2 4F RT A1NM 2007082300028 20070823 00028 NM 2007 8 23 CALA0700419 1 20070811 A 5311 694654050 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND A 1 INCH CRACK AT TWO EACH HOLES IN I/B CHORD AT STA 639, S16R TO S17R. THE INNER CHORD WAS REPLACED A ND A REPAIR WAS INSTALLED IAW ECRA 5311-01347. 2 L 7 2 4F RT A16WE 2007082300029 20070823 00029 NE 2007 8 23 HALA0700340 2 20070814 A 7320 114E7842G120 EEC BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE NR 1 FAULTED A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 475HA 55121 FIM 732102 "LEFT ENG SYS FAIL" CAME ON AFTER ENGINE START. FOUND NR 1 ENG EEC1 FAULT. REPLACED NR 1 ENG EEC PER 73-21 -01-741-801. RTS CK OK. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007082300030 20070823 00030 NE 2007 8 23 HALA0700341 2 20070814 A 7397 CONNECTOR BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE EEC UNKNOWN A HALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 475HA 55121 "ENG L SYS FAIL" ANNUNCIATED ON TAXI IN. PERF EEC-1 BITE, FOUND CURRENT FAULT 732102 ENG POSITION ID CIRCUIT CH-A, T/S PER FIM 73-21-00-810-804, RESEATED CONNECTOR P1-8204, EEC-1 FAULTS CLEARED, RTS PASSED, GRD ENG RUN CHECK GOOD. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007082300031 20070823 00031 NM 2007 8 23 QXEA200701297 1 20070806 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - DENT IN FUSELAGE SKIN, PROTRUDING OUTWARD AT STATION X216 BETWEEN STRINGER 30R AND 31R. REPAIRED IAW RD8-53-97 39 AND RD8-53-5384. 2 H 7 2 4T RT A13NM 2007082300033 20070823 00033 NM 2007 8 23 CALA0700420 1 20070811 A 5347 6545410200 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND A 1 INCH CRACK IN RIGHT I/B SEAT TRACK O/B MOUNT FLANGE AT STA 727B, RBL 45.5. A LONGITUDINAL FLOORBEA M REPAIR WAS INSTALLED IAW ECRA 55321-01492. 2 L 7 2 4F RT A16WE 2007082300036 20070823 00036 NM 2007 8 23 CALA0700423 1 20070811 A 5230 6547952537 SKIN BOEING 737 7373T0 1384582 NM AFT CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND A 1 INCH CRACK IN AFT CARGO DOOR INNER SKIN BETWEEN LIGHTENING HOLES ABOVE HANDLE. A DOUBLER REPAIR WA S INSTALLED IAW ECRA 5232-01089. 2 L 7 2 4F RT A16WE 2007082300037 20070823 00037 NM 2007 8 23 CALA0700424 1 20070812 A 5330 6545800 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND TWO 1 INCH CRACKS IN R-1 DOOR SKIN CUTOUT AT STA 328, S16R. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 53 31-01337. 2 L 7 2 4F RT A16WE 2007082300038 20070823 00038 NM 2007 8 23 CALA0700425 1 20070812 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14609 27322 INSPECTION FOUND A .25 INCH CRACK IN FRAME AT BRACKET ATTACH RIVET, STA 787, S8R. THE FRAME WAS REPAIRED IAW ECRA 5310- 04649. 2 L 7 2 4F RT A16WE 2007082300039 20070823 00039 NM 2007 8 23 CALA0700426 1 20070812 A 5311 6546529 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND A 1 INCH CRACK IN FORWARD BAGGAGE BIN FRAME AT DRAIN HOLE, STA 440, BL 0. A REPAIR WAS INSTALLED IAW S RM 53-00-07, FIGURE 201. 2 L 7 2 4F RT A16WE 2007082300040 20070823 00040 NM 2007 8 23 CALA0700427 1 20070812 A 5320 651768471 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR JAMB LOWER HINGE INTERCOSTAL AT STA 294.5, S13L TO S14L. A REPAIR WAS INSTA LLED IAW ECRA 5311-01349. 2 L 7 2 4F RT A16WE 2007082300041 20070823 00041 NM 2007 8 23 CALA0700428 1 20070812 A 5320 651768465 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR JAMB UPPER HINGE INTERCOSTAL AT STA 294.5, S10L. A REPAIR WAS INSTALLED IAW ECRA 5311-01350. 2 L 7 2 4F RT A16WE 2007082300045 20070823 00045 2007 8 23 SWAA073996 4 20070810 A 2565 1061323468 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007082300046 20070823 00046 NM 2007 8 23 SWAA073993 1 20070809 A 5315 147A5502 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 733SA 27865 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 294.5, RBL 11 TO RBL 12. REPAIRED FLOORBEAM CHORD PER ER. 2 L 7 2 4F RT A16WE 2007082300048 20070823 00048 NM 2007 8 23 SWAA074005 1 20070811 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 276WN 32530 DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007082300049 20070823 00049 NM 2007 8 23 SWAA074004 1 20070811 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 235WN 34630 EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007082300050 20070823 00050 NM 2007 8 23 SWAA073980 1 20070809 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 422WN 29826 DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007082300051 20070823 00051 NM 2007 8 23 SWAA073975 1 20070809 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 555, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007082300052 20070823 00052 NM 2007 8 23 QXEA200701292 1 20070808 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 347 S30R DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - DENT IN FUSELAGE,PROTRUDING OUTWARD, STATION X347, STRINGER 30R. REPAIRED IAW RD8-53-5384. 2 H 7 2 4T RT A13NM 2007082300054 20070823 00054 NM 2007 8 23 SWAA074006 1 20070811 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 4R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007082300056 20070823 00056 NM 2007 8 23 QXEA200701296 1 20070808 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 326 S30-31L DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - DENT IN FUSELAGE SKIN, PROTRUDING OUTWARD AT STATION X326 BETWEEN STRINGER 30L AND 31L. REPAIRED IAW RD8-53-538 4. 2 H 7 2 4T RT A13NM 2007082300057 20070823 00057 NM 2007 8 23 QXEA200701293 1 20070805 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 299 S23-24R DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - DENT IN FUSELAGE BELOW ICE SHIELD AT STATION X299 BETWEEN STRINGER 23R AND 24R. REPAIRED IAW RD8-53-9734. 2 H 7 2 4T RT A13NM 2007082300058 20070823 00058 NM 2007 8 23 SWAA073989 1 20070809 A 5330 6545767 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 466, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007082300060 20070823 00060 NM 2007 8 23 SWAA073995 1 20070810 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 746, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007082300062 20070823 00062 NM 2007 8 23 SWAA073994 1 20070810 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 25L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007082300066 20070823 00066 NM 2007 8 23 QXEA200701288 1 20070809 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 486 S32R GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - GOUGE ON BOTTOM OF FUSELAGE AT X486 AT STRINGER 32R. REPAIRED IAW RD8-53-5384, SRM 51-20-26. 2 H 7 2 4T RT A13NM 2007082300067 20070823 00067 NM 2007 8 23 QXEA200701289 1 20070805 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - 1/2" DIAMETER DENT IN FUSELAGE 5" FORWARD OF RIGHT PITOT MAST. REPAIRED IAW RD8-53-9732. 2 H 7 2 4T RT A13NM 2007082300069 20070823 00069 EU 2007 8 23 MALA070095 1 20070813 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 430XJ 340B430 FORWARD COVE EMERGENCY LIGHT INOP. REPLACED FORWARD COVE EMERGENCY LIGHT HOUSING, PN 2LA005115-20 IAW SF340 AMM 33-50-5 5. 2 L 7 2 4T RT A52EU 2007082300070 20070823 00070 NM 2007 8 23 QXEA200701331 1 20070815 A 3010 4100S01806 TMU BOMBDR DHC8 DHC8402 1390042 NM DEICE SYSTEM MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 403QX 10594 10594 4037 SEA FLIGHT NR 2271: PITOT HEAT STBY, DEICE TIMER, DEICE PRESSURE ILLUMINATED AFTER PUSH AND PROPS AT MAX. ALL BUSSES PO WERED NORMALLY. DEICE PRESS 18 PSI. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE REMOVED AND REPLACED TIMER AND MONITOR UN IT IAW Q400 AMM 30-11-01, PAGE 401-406. NO REOCCURRENCE OF ABOVE MENTIONED CAUTION LIGHTS. AIRCRAFT RETURNED TO SERVIC E. 2 H 7 2 4T RT A13NM 2007082300071 20070823 00071 NM 2007 8 23 SWAA073978 1 20070809 A 5511 6547983 RIB BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND LT HORIZONTAL STAB RIB CRACKED AT STA 95.96. REMOVED AND REPLACED RIB PER SRM. 2 L 7 2 4F RT A16WE 2007082300073 20070823 00073 NM 2007 8 23 QXEA200701332 1 20070814 A 7930 OIL SYSTEM BOMBDR DHC8 DHC8402 1390042 NM NR 2 FLUCTUATES A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 424QX 4006 SEA FLIGHT NR 2382: NR 2 OIL PRESSURE FLUCTUATES AFTER START. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE CLEANED AND INSP ECTED NR 2 ENGINE OIL PRESSURE TRANSDUCER CONNECTOR. RAN OPS CHECK OF OIL PRESSURE SYSTEM IAW AMM 71-00-00-868-805. SYS TEM OPSC CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007082300074 20070823 00074 NM 2007 8 23 SWAA073987 1 20070809 A 5314 6562125 KEELBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED BRDG CHECK, FOUND KEEL BEAM WEB CRACKED AT BS 711, LBL 4. REPAIRED WEB PER EA. 2 L 7 2 4F RT A16WE 2007082300075 20070823 00075 NM 2007 8 23 SWAA073999 1 20070810 A 5755 6573730 SPOILER BOEING 737 7373T5 1384608 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 6 FLIGHT SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007082300076 20070823 00076 WP 2007 8 23 070142 1 20070803 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 871GA 53296 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007082300077 20070823 00077 NM 2007 8 23 SWAA073986 1 20070809 A 5753 6573731 FLAP BOEING 737 7373Q8 1384670 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED BRDG CHECK, FOUND LEFT WING INBOARD MID FLAP T/E DELAMINATED. REMOVED AND REPLACED MID FLAP PER MM. 2 L 7 2 4F RT A16WE 2007082300078 20070823 00078 NM 2007 8 23 SWAA074000 1 20070810 A 5755 6573735 SPOILER BOEING 737 7373T5 1384608 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 9 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007082300081 20070823 00081 WP 2007 8 23 070145 1 20070813 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 866GA 49910 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENC Y EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BA TTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007082300083 20070823 00083 EU 2007 8 23 07FDEA02908 1 20070815 A 5743 A57240810214 ATTACH FITTING AIRBUS 300 A300B4605R 3930308 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 IMPACT DAMAGE TO LT MLG FITTING LUG REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW SRM 51-73-10, APPROVED BY EA 6-5 751-112498 AND RAS/BAE/1005258/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082300089 20070823 00089 EU 2007 8 23 07FDEA02930 1 20070816 A 5730 A57440088 SKIN AIRBUS 300 A300B4605R 3930308 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 LT WING LOWER SKIN RIB 20-21 AROUND MAGNETIC LEVEL INDICATOR CORROSION ON WING SKIN REPAIR PERFORMED BY BLEND OUT THE CO RROSION IAW SRM 51-74-10, APPROVED BY EA 6-5720-112490 AND RAS/BAE/100535/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082300090 20070823 00090 NM 2007 8 23 SWAA073981 1 20070809 A 3210 69421992 BOLT BOEING 737 7373H4 1384600 NM RT MLG WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 603SW 27954 DURING SCHEDULED BRDG CHECK, FOUND RT MLG WALKING BEAM INBOARD BOLT WORN. REMOVED AND REPLACED BOLT PER MM. 2 L 7 2 4F RT A16WE 2007082300093 20070823 00093 NM 2007 8 23 SWAA073979 1 20070809 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM FUSELAGE INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 401WN 29813 DURING SCHEDULED MV2 CHECK, FOUND RT AFT FUSELAGE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007082300094 20070823 00094 EU 2007 8 23 07FDEA02934 1 20070816 A 5311 A53989300204 FRAME AIRBUS 300 A300B4605R 3930308 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 CORROSION FOUND ON FRAME WEB PLATE ON C92, P15-17 RT REPAIR PERFORMED BY CUT THE WEB AND INSTALL A FILLER AND AN ANGLE I AW EA 6-5319-112477 AND RAS/DAHAM/22468/2007 ISS B. 2 L 7 2 4F RT A35EU 2007082300098 20070823 00098 2007 8 23 SWAA073985 4 20070809 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 613SW 27931 DURING SCHEDULED MV1 CHECK, R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED E VAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007082300100 20070823 00100 EU 2007 8 23 07FDEA02938 1 20070816 A 5312 A53984650202 BULKHEAD AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 CORROSION ON AFT PRESSURE BULKHEAD REPAIR PERFORMED BY BLEND OUT THE CORROSION TO SMOOTH CONTOUR AND REPLACEMENT OF AFFE CTED FASTENER IAW SRM 51-74-10 AND 51-40-21, APPROVED BY EA 6-5318-112443 AND RAS/DAHAM/4022393/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082300102 20070823 00102 2007 8 23 SWAA073997 4 20070810 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007082300104 20070823 00104 EU 2007 8 23 07FDEA02941 1 20070816 A 5313 A53811360 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 CORROSION SPOT ON STRINGER P51, C39-40 RT REPAIR PERFORMED BY BLEND OUT CORROSION TO SMOOTH CONTOUR IAW SRM 51-74-10, AP PROVED BY EA 6-5315-106536 AND RAS 052622/004/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082300108 20070823 00108 EU 2007 8 23 07FDEA02945 1 20070816 A 5310 A53973085210 BEAM AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORROSION ON AFT CARGO DOOR SILL BEAM, C59-62 REPAIR PERFORMED BY REPLACEMENT OF UPPER FLANGE OF SILL BEAM IAW SRM 53-17 -18 AND DRAWING 17R53970133, APPROVED BY EA 6-5317-114839 AND RAS/DATLS/0003813/2007 ISS B. 2 L 7 2 4F RT A35EU 2007082300111 20070823 00111 2007 8 23 SWAA073990 4 20070809 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007082300112 20070823 00112 EU 2007 8 23 07FDEA02948 1 20070816 A 5311 A53610318367 FRAME AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORROSION ON FRAME C 12-12A LAVATORY BOX PANEL REPAIR PERFORMED B REPLACEMENT OF PART. 2 L 7 2 4F RT A35EU 2007082300113 20070823 00113 EU 2007 8 23 07FDEA02949 1 20070816 A 5320 A53610873222 STIFFENER AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORROSION ON STIFFENER C12-12A LAVATORY SERVICE BOX PANEL REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007082300118 20070823 00118 NM 2007 8 23 QXEA200701305 1 20070803 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - DENT IN RIGHT FUSELAGE AT STATION 334 AND Z108. REPAIRED IAW RD8-53-5384. 2 H 7 2 4T RT A13NM 2007082300120 20070823 00120 NM 2007 8 23 NOCA14707 1 20070804 A 5270 893501 PROXIMITY SWITCH BOEING 767 767306 1385148 NM L1 DOOR FAULTY A NOCA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 15 765NA 28098 ON TAKEOFF ROLL BELOW 80 KTS HAD A L1 DOOR FWD ENTRY DOOR OPEN EICAS MESSAGE A/C REJECTED TAKEOFF AT 65 KTS. ACTION DEF ERRED PER MEL 52-71-1, A/C INSPECTED OK FOR SERVICE, DOOR MUST BE VERIFIED CLOSED AND LOG BOOK ENTRY MADE PRIOR TO EACH DEPARTURE. REPLACED DOOR CLOSE PROX SWITCH (S194) PER MM 52-71-01-964-502. ACCOMPLISHED PROX BITE, NO FAULTS, SDR CLOS ED. 2 L 7 2 4F RT A1NM 2007082300122 20070823 00122 NM 2007 8 23 QXEA200701307 1 20070805 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 488 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - FRAME 488.5 CASTELLATION BETWEEN STRINGER 32S AND 33 IS CORRODED. REPAIRED IAW SRM 51-20-11 51-20-26, 51-40-11 . 2 H 7 2 4T RT A13NM 2007082300124 20070823 00124 NM 2007 8 23 QXEA200701298 1 20070805 A 5310 THRESHOLD DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - MAIN CABIN DOOR THRESHOLD IS CORRODED ON UPPER SURFACE AT STATION X222.7 - X253.4. REPAIRED IAW SRM 51-40-11, 51-40-00. 2 H 7 2 4T RT A13NM 2007082300125 20070823 00125 NM 2007 8 23 QXEA200701299 1 20070809 A 5320 GUSSET DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - GUSSET IS CORRODED AT FRAME X240.5, Z101, AND Y42S. REPAIRED IAW SRM 51-40-11, 51-20-16, 51-20-36, AND RD8-53- 9749. 2 H 7 2 4T RT A13NM 2007082300126 20070823 00126 NM 2007 8 23 QXEA200701300 1 20070809 A 5320 INTERCOSTAL DHAV DHC8 DHC8202 2809007 NM BS 426 S23L CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - INTERCOSTAL IS CORRODED AT STATION X426 AND STRINGER 23P. REPAIRED IAW SRM 51-40-11, 51-40-00. 2 H 7 2 4T RT A13NM 2007082300127 20070823 00127 NM 2007 8 23 QXEA200701301 1 20070810 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - AT FS X568, Z111.5, Y11L THERE IS A CORRODED N/P IN OUTBOARD SIDE OF TRACK. REPAIRED IAW SRM 51-20-11, 51-20-3 6-, AND 51-20-16, AND RD8-53-9753. 2 H 7 2 4T RT A13NM 2007082300128 20070823 00128 NM 2007 8 23 QXEA200701334 1 20070815 A 6123 AUTOFEATHER SYS DHAV DHC8 DHC8202 2809007 NM NR 2 MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 358PH 506 SEA FLIGHT NR 2055 - AUTOFEATHER TEST ON NR 2 CAUSES NR 1 TO FEATHER IMMEDIATELY. MAINTENANCE COULD NOT DUPLICATE. NO PARTS REPLACED AIRCRAFT RETURNED TO SERVICE, 2 H 7 2 4T RT A13NM 2007082300131 20070823 00131 NM 2007 8 23 DLM90071072 1 20070813 A 5340 3912075514N ATTACH FITTING DOUG MD90 MD9030 3023690 NM BS 1079 L18R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 FRAME FITTING RT FS 1079 UNDERSIDE OF CUSP (BELOW L18R) IS CRACKED. REMOVED AND INSTALLED NEW FRAME FITTING IAW SRM MD- 90 51-30-5. 2 L 7 2 4F RT A6WE 2007082300132 20070823 00132 NM 2007 8 23 ABXA070255 1 20070809 A 3350 SWITCH BOEING 767 767232 1385132 NM CABIN INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 747AX 22224 EMERGENCY / DEPRESS TEST LIGHTS SWITCH INOPERATIVE (WOULD NOT TEST). WIRED SYSTEM TO WDM 33-24-11, SYSTEM TESTS NORMAL. 2 L 7 2 4F RT A1NM 2007082300136 20070823 00136 NM 2007 8 23 CALA0700429 1 20070813 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14609 27322 INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 827 BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04649. 2 L 7 2 4F RT A16WE 2007082300137 20070823 00137 NM 2007 8 23 DLM90071076 1 20070720 A 5347 593054769 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 1148-1180 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 FOUND CABIN SEAT TRACK LBL-54 OUT OF LIMITS STA 1148-1180. REPLACED SEAT TRACK AT LBL-54 STA 1088-1193 IAW MD-90 SRM 51 -30-1. 2 L 7 2 4F RT A6WE 2007082300138 20070823 00138 NM 2007 8 23 DLM90071077 1 20070720 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 1212-1269 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 AFT CUSP WEB STA 1212-1269 RT CORRODED 3 EA PLACES 1269,1240,1216. REPAIRED CUSP WEB AT STA 1240 RT SIDE IAW DELTA ERA 398191-14MA REV A 9/18/02 2 L 7 2 4F RT A6WE 2007082300140 20070823 00140 2007 8 23 DL76L071078 4 20070815 A 3418 0861FL SENSOR BOEING 767 767332 1382001 NM RT AOA FAILED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 194DN 28451 RTB DUE RT AOA PROBE LIGHT AND EICAS MSG. FOUND AOA SENSOR AT FAULT. REPLACED PER MM AND OPS OK. 2 L 7 2 4F RT A1NM 2007082300141 20070823 00141 NM 2007 8 23 CALA0700431 1 20070812 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14609 27322 INSPECTION FOUND A .5 INCH CRACK IN FRAME AT STA 827, S8L. THE FRAME WAS REPAIRED IAW ECRA 5310-04649. 2 L 7 2 4F RT A16WE 2007082300143 20070823 00143 NM 2007 8 23 DL76L071080 1 20070815 A 3610 233T323727 CONTROL PANEL BOEING 767 767332 1382001 NM PNEUMATIC SYS MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 185DN 27961 LEFT ISOLATION VALVE WOULD NOT EXTENGISH AFTER ENGINE START. REMOVED AND REPLACED RELAY K-16, NO HELP REMOVED AND PNEUM ATIC CONTROL PANEL. OPS CHK GOOD. 2 L 7 2 4F RT A1NM 2007082300146 20070823 00146 NM 2007 8 23 DL76S071082 1 20070815 A 3246 WHEEL BOEING 767 767332 1382001 NM RT NLG WORN A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 138DL 25409 ON TAKEOFF AT V1 SIGNIFICANT YAW-TRANSIENT EVENT AND LOUD BANG HEARD IN CABIN. SUSPECTED BLOWN TIRE. ON ARRIVAL INSPEC TED ALL WHEEL ASSYS AND GEAR. RT NOSE WHEEL ASSY HAD SOME PLAY. REPLACED BOTH NOSE WHEEL ASSYS. 2 L 7 2 4F RT A1NM 2007082300150 20070823 00150 NM 2007 8 23 HALA0700343 1 20070815 A 2913 211C233297 PRESSURE SWITCH BOEING 767 767332 1382001 NM EDP MALFUNCTIONED A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, L HYD PRI PUMP AND L ENG HYD PUMP EICAS MSG, AND ASSOCIATED PUMP LIGHT ILLUMINATED. PERFORMED FIM 29-11-00 REPLACED EDP PRESSURE SWITCH S26 ON NR 1 ENG 29-11-17, OPS CHECK LEAK CHECK OK. 2 L 7 2 4F RT A1NM 2007082300151 20070823 00151 NM 2007 8 23 CALA0700435 1 20070813 A 5230 6547953 SKIN BOEING 737 7373T0 1384582 NM AFT CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR SKIN AT AFT EDGE OF HANDLE CUTOUT. A DOUBLER WAS INSTALLED IAW SRM 5 2-00-01, REPAIR 3. 2 L 7 2 4F RT A16WE 2007082300152 20070823 00152 NM 2007 8 23 HALA0700342 1 20070813 A 3244 416K421 TIRE BOEING 717 717200 1383700 NM MLG FAILED A HALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 13 486HA 55131 NR 1 MAIN TIRE SEPARATION LEFT SIDE ON T/O. FOUND TIRE PRESS TO BE 190 PSI. REPLACED NR 1 MAIN TIRE PER MM 32-41-01. COND CK GOOD. WITH DAMAGE TO THE FOLLOWING:LEFT FLY DOOR AFT EDGE BENT UP ABOUT 9". REMOVED LHS FLY DOOR. REPAIRED FL Y DOOR EDGE BENT DAMAGE PER HAL-M105 FILE #486075. CLEARANCE CHK PEND. CLEARANCE CHK NOT REQ DUE TO SAME DOOR INSTALLE D. LT MAIN LANDING GEAR SPLASH GUARD BENT UP AFT OF NR 1 TIRE. REPLACED SPLASH GUARD AND BENT DOUBLER PLATE. DENT ON LOWER LT FLAP BELOW LE EDGE CAP BY LFS 105,5 1/2" BY 6 1/2"AND DENT ON LOWER LEFT FLAP XFL5 110 5" BY 6". BOTH REPAIRED PER HAL M 105 FILE NR 486078, INTRIM REPAIR. HONEYCOMB GOUGED NOSE COWL INLET 11 O'CLOCK 5" BY 1-1/2". PERF AMM 72-34 2 L 7 2 4F TR A6WE 2007082300153 20070823 00153 NM 2007 8 23 CALA0700436 1 20070814 A 5320 6546539 ANGLE BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33608 27321 INSPECTION FOUND A 1.5 INCH CRACK IN BELTFRAME ANGLE AT STA 616, S17R TO S18R, JUST BELOW FLOOR. REPAIRED IAW ECRA 5311 -01158. 2 L 7 2 4F RT A16WE 2007082300159 20070823 00159 2007 8 23 IXXA070040O 4 20070816 A 3418 C264064 COMPUTER DOUG DC8 DC871F 302199D WP MALFUNCTIONED A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 821BX 88101 2207 45811 DURING CLIMB-OUT FROM KSJC STALL WARNING ACTIVATED AT START OF ROTATION AND REMAINED ON. THE CREW PULLED CIRCUIT BREAKE R AND RETURNED TO KSJC AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LIFT COMPUTER, PERFORMED OPERATIONAL CHECK WAS GOOD IAW UAL 41-10-2. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2007082300162 20070823 00162 NM 2007 8 23 QXEA200701337 1 20070814 A 2430 11521102 TRU BOMBDR DHC8 DHC8402 1390042 NM NR 1 SMOKE A QXEA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 402QX 15997 15997 4032 PDX FLIGHT NR 2296: AFTER ENGINE START, FO NOTICED PUFF OF SMOKE BY NOSE AREA. ELECTRICAL PAGE SHOWED NO LOAD ON NR 1 T RU WITH .25 LOAD ON NR 2 TRU AND .5 LOAD ON BOTH GENERATORS. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE REMOVED AND REPLA CED NR 1 TRU IAW AMM 24-31-21. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007082300163 20070823 00163 NM 2007 8 23 HALA0700346 1 20070817 A 3350 LAMP BOEING 767 76733A 1385209 NM EMERGENCY LIGHT INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 589HA 33422 RT SIDE OVERWING EMERGENCY LIGHT INOP. RELAMPED. OPS CKS NORMAL 2 L 7 2 4F RT A1NM 2007082300164 20070823 00164 NM 2007 8 23 2007UALA03085 1 20070809 A 2612 FIRE LOOP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 2 FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 664UA 29236 RIGHT ENGINE FIRE LOOP 2. 08-31-07 FOUND BAD LOOP DETECTOR ELEMENT AT LWR AFT SECTION TS662, REPLACED PER MM 26-11-0 2, OPS CK NORMAL 2 L 7 2 4F 4 F RT A1NM E24NE 2007082300165 20070823 00165 EU 2007 8 23 2007UALA03086 1 20070809 A 2910 O-RING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYDRAULIC SYS FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 432UA 587 FLIGHT DIVERTED DUE TO YELLOW HYDRAULIC SYSTEM INOPERATIVE MESSAGE. 09-07-07 REPLACED FAILED O-RINGS AT FLIGHT CONTR OL PRESSURE SWITCH. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300167 20070823 00167 NM 2007 8 23 2007UALA03032 1 20070805 A 5310 DOOR FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 FWD CARGO PIT, FOUND CORROSION ON ANGLE FRAME INSIDE NEXT TO ROLLOUT STOP 3RD FROM MOST FORWARD POSITION AT STA 575. 0 8-31-07 REMOVED CORROSION VERIFIED MATERIAL LOSS WITHIN LIMIT. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082300168 20070823 00168 NM 2007 8 23 2007UALA03033 1 20070805 A 3397 WIRE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHT SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 796UA 26931 EMERGENCY EXIT LIGHTS AT SEATS 3E (AFT SIDE) AND 3F (AFT POSN) ARE INOPERATIVE. 08-31-07 FOUND SHORT IN-SEAT EEL STR IP. REPLACED EEL LIGHT ASSY. OP CHECKS OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007082300169 20070823 00169 NM 2007 8 23 2007UALA03034 1 20070805 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SEAT 35CD INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 796UA 26931 EMERGENCY EEL LT INOP AT SEAT 35CD. 08-31-07 REPLACED LT ASSY AT SEAT 35CD. OP CHECKED OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007082300170 20070823 00170 NM 2007 8 23 2007UALA03087 1 20070809 A 3260 WARNING SYSTEM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT ACTIVATED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 175UA 24382 GEAR MONITOR, EICAS STATUS MESSAGE DISPLAYED. PRI & ALT LANDING GEAR POSITION INDICATION DISAGREE. SELECTED LANDING GE AR MAINTENANCE MESSAGE OR LOSS OF EITHER PSEU BUS OR SELECTED PSEU FAULT. 08-31-07 FOUND EICAS MSG 28649 & 28651. FOU ND CIRCUIT BREAKER OPEN "CTR R MAIN 2 JETT VALVE". RESET. OPS NML. NO FOLLOWUP PROBLEMS REPORTED FOR 14 DAYS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082300171 20070823 00171 NM 2007 8 23 2007UALA03088 1 20070809 A 5743 FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LT MLG CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 FITTING CRACKED, LEFT MLG O/B AFT SUPPORT FITTING IS CRACKED AT THE NR 2 BOLT HOLE AT THE 6:00 POSITION. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082300173 20070823 00173 2007 8 23 2007UALA03090 4 20070809 A 2565 SOCKET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 594UA 28145 SLIDE LIGHT AT DOOR 1R NOT ILLUMINATED WITH DOOR ARMED. ON TROUBLESHOOTING DIAGNOSED PROBLEM WITH LIGHT SOCKET/RECEPTA CLE. REPLACED SOCKET AND LIGHTING CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082300175 20070823 00175 NE 2007 8 23 2007UALA03092 2 20070809 A 7200 ENGINE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 STALLED A UALA K NONE R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 846UA 1600 V11087 ECAM WARNING ENGINE 2 STALL. 09-07-07 NR 2 ENG STALL IN CLIMB FROM 370-380. ENGINE RECOVERED IMMEDIATELY ON ITS OWN WITH NO INPUT. REPLACED NR 2 LT HP 7 STAGE VALVE 2 L 7 2 4F 4 F RT A28NM E40NE 2007082100246 20070821 00246 SO 2007 8 21 GLBA20060978 1 20070814 A 2150 1945463 HEAT EXCHANGER EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE MALFUNCTIONED A GLBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 293UX 120293 SMOKE/SMELL, FLIGHT 5010, PILOTS REPORTED LT ENGINE DUCT LEAK LIGHT AND DUCT OVERHEAT LIGHT ILLUMINATED. RT PACK APPEAR ED TO BLOW OUT HOT AIR AND SMOKE WAS REPORTED IN THE CABIN. MAINTENANCE REMOVED AND REPLACED SEVERAL COMPONENTS INCLUDIN G A TEMP THERMOSTAT IAW MM 21-10-09, LT AIR CYCLE MACHINE IAW MM 21-50-05, PRESSURE REGULATING VALVE IAW MM 21-50. THE F INAL FIX OCCURRED WHEN THE LT HEAT EXCHANGER WAS REMOVED AND REPLACED IAW MM 21-50. LEAK AND OPERATIONAL TESTS GOOD IAW MM 21-50-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2007082100248 20070821 00248 EU 2007 8 21 FJ7A116867 1 20070809 A 3411 6700615101 PITOT HEAD UROCOP EC130 EC130B4 8680989 EU UNKNOWN E FJ7A K NONE O OTHER IN INSP/MAINT 1 SO 19 174AM 4007 INDICATION OF NO PITOT HEAT ON ANNUNCIATOR PANEL. 1 G 7 2 3U H9EU 2007082100263 20070821 00263 EU 2007 8 21 TRAX200701133 1 20070807 A 5710 FRAME AEROSP ATR72 ATR72 EU LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 LEFT WING BOX FR 28A FAIRING FRAME FACING CRACKED. REPLACED AS PER SRM 51-25-01. REPAIR DETERMINED NOT TO BE A MAJOR R EPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 57-25-01. 2 H 7 2 4T RT 2007082100273 20070821 00273 EU 2007 8 21 398908162007 1 20070816 A 2121 050143 BLOWER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE CABIN AIR BURNED OUT E QMLA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 03 128LN 3989 9859 RETURNING FROM INTER-FACILITY TRANSFER, ON LONG FINAL TO BASE, WHEN PILOT AND CREW DETECTED A VERY STRONG BURNING ODOR I N COCKPIT. NO SMOKE WAS DETECTED BUT COULD HAVE BEEN PRESENT AND NOT SEEN DUE TO DARKNESS. THE ODOR SMELLED AS IF IT WAS ELECTRICAL IN NATURE BUT SINCE WE HAVE HAD SO MUCH TROUBLE WITH THE AIR CONDITIONING IN THE 350'S, SUSPECTED IT MIGHT B E THE PROBLEM. TURNED AIR OFF AND ODOR DISSIPATED. LANDING AT BASE WAS UNEVENTFUL. UPON SHUTTING DOWN AND SECURING AIRCR AFT, LIFTED TRANSMISSION COWLING TO INSPECT COMPRESSOR UNIT. THE AIR CONDITIONING BELT WAS INTACT AND APPEARED TO HAVE P ROPER TENSION. PLACED AIRCRAFT OUT OF SERVICE UNTIL SOURCE OF FUMES COULD BE DETERMINED. APPROPRIATE PERSONNEL TO INCLUD 1 G 7 1 3U 3 U H9EU E19EU 2007082100275 20070821 00275 SO 2007 8 21 DJFA2007094 1 20070813 A 4930 O-RING EMB 135 EMB135BJ 3260306 SO ALLSN AE300 AE3007A GL APU FUEL CONTROL LEAKING E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 EA 23 908LX E145528 THE CREW REPORTED A VERY STRONG ODOR OF RAW FUEL DURING TAKEOFF BUT STATED THAT THE FUMES DISSIPATED QUICKLY AFTER TAKE OFF. THE ODOR WAS THROUGHOUT THE CABIN AND ONLY OCCURED WHEN APU BLEED IS ON. MX REPLACED THE APU FUEL CONTROL FLANGE GASKET (O-RING) IAW CPT 49 MM, NO LEAKAGE NOTED DURING FUNCTIONAL CHECK. 2 L 7 2 4F 4 F RT TE6CH 2007082100277 20070821 00277 NM 2007 8 21 TAMF20070009S 1 20070805 A 5711 SPAR BOEING 767 767200 1385120 NM RT WING CORRODED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 767QT 23804 RT WING FRONT SPAR UPPER FWD CHORD AT STA OSS 456.98 HAS CORROSION. REMOVED CORROSION FROM UPPER FWD CHORD AT RT WING F RONT SPAR, STA OSS 456.98 IAW SRM 51-10-02 PAGE 12-13. THICKNESS FOUND, MAX: 0.078 INCH, MIN: 0.055 INCH. NO CRACKS FOUN D. BLENDING LIMITS ON THE UPPER SKIN, LEADING EDGE SPLICE PLATE ACCEPTED AS PERMANENT REPAIR IAW MFG SERVICE REQUEST 1-4 99965626. FAA FORM 8100-9 WILL BE ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F RT A1NM 2007082100279 20070821 00279 NM 2007 8 21 TAMF20070011S 1 20070809 A 5414 SKIN BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE NACELLE DAMAGED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 767QT 23804 DURING C CHECK INSPECTION (MFG TASK CARD 06-084-01-2) WAS FOUND WEAR ON STRUT SKIN STA 148.50. THE MINIMUM THICKNESS IS 0.047 INCH. CF6-80C2 ENGINE NR 2. DAMAGED AREA WAS REPAIRED IAW EWO 767 54-017 AND MFG SERVICE REQUEST 1-512263744. THI S REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007082100284 20070821 00284 NE 2007 8 21 LX5R200700005 1 20070815 A 2120 BREATHER TUBE SKRSKY S76 S76B 8143007 NE PWA PT6 PT6B36 52043 EA BAGGAGE COMPT DISCONNECTED B LX5A A O UNSCHED LANDING OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 19 751LL 4386 760318 PS36027 DURING CRUISE FLIGHT THE BAGGAGE SMOKE WARNING LIGHT CAME ON, THE AIR CONDITIONER BLOWER WAS TURNED OFF AND THIS MADE NO EFFECT ON THE WARNING LIGHT. THE HELICOPTER LANDED IN AN OPEN FIELD AND THE PIC CHECKED BAGAGE COMPARTMENT FOR FIRE. NO FIRE WAS NOTED AND ONLY SLIGHT AMOUNT OF OIL MIST WAS NOTED. THE WARNING LIGHT WENT OUT. THE CREW TOOK OFF AND LANDED A T THE NEAREST AIRPORT WITHOUT INCIDENT. THEY CALLED THE MAINTENANCE BASE AND IT WAS SUSPECTED THAT THE ENGINE BREATHER L INE HAD BROKE. THE MAINTENANCE CREW FLEW UP AND INSPECTED THE AIRCRAFT. FOUND THE NR1 ENGINE BREATHER VALVE LINE HAD CO ME DISCONNECTED IN THE OVERHEAD OF THE BAGAGE COMPARTMENT. THIS IS A RUBBER TUBE. THE TUBE WAS RE-ATTACHED AND SECURED. 1 G 7 2 4U 4 U H1NE E4EA 2007082100285 20070821 00285 CE 2007 8 21 GUUA08120701 1 20070812 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CABIN ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 29 53545 UE185 FLIGHT:9249 DURING FLIGHT MILD CHEMICAL ODOR LIKE HYDRAULIC FLUID COMING THRU THE ENVIRONMENTAL SYSTEM. PERFORMED OPERA TIONAL CHECK OF THE ENVIRONMENTAL SYSTEM COULD NOT DUPLICATE. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2007082100286 20070821 00286 NM 2007 8 21 TAMF20070012S 1 20070802 A 5730 SKIN BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE WING DAMAGED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 767QT 23804 DURING C CHECK INSPECTION (MFG TASK CARD 57-666-00) WAS FOUND A LIGHTNING STRIKE ON WING UPPER SKIN STA 1018.2 RT. DAMA GED AREA WAS REPAIRED IAW MFG SERVICE REQUEST 1-490432776 AND EWO 767 57-023. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FA A FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007082100287 20070821 00287 NM 2007 8 21 TAMF20070010S 1 20070805 A 5414 2242301517 SKIN BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE NACELLE DAMAGED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 767QT 73497 23804 DURING C CHECK INSPECTION (MFG TASK CARD 06-091-01-2) WAS FOUND CORE COWL P/N:224-2301-517, S/N: 0115 WITH ELONGATED HOL E AT FRAME STA NAC 294, ENGINE NR 2.DAMAGED AREA WAS REPAIRED IAW EWO 767 54-016 AND AUTHORIZATION CV07-1674-01. 2 L 7 2 4F 4 F RT A1NM E13NE 2007082100288 20070821 00288 EA 2007 8 21 TRAX200701144 1 20070809 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 F/A REPORTS PAX DOOR DIFFICULT TO OPEN. HANDLE FEELS AS IF IT'S BINDING TOWARDS TOP OF TRAVEL LIMIT. 2 L 7 2 4F RT A21EA 2007082100291 20070821 00291 NE 2007 8 21 ASMF200708004 2 20070815 A 7320 1853M33P06 EEC BOEING 737 737 UTILSYS NM CFMINT CFM567 CFM567B22 13802 NE LT ENGINE FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 906AM 8769 8769 29356 892110 AIRCRAFT RETURNED TO PLATFORM DURING TAXI, LT ENGINE CONTROL LIGHT TURNED ON AND STAY ILLUMINATED. MAINTENANCE CLEANED P S3 AIR TUBE WITH HIGH PRESSURE NITROGEN, PERFORMED THE FIM PROCEDURE 73-26 TASK 803 AND VERIFIED AND TEST THE ELECTRICAL CONNECTOR PLUGS ON EEC BOX IAW MM 71-00-00-700/801 ALL CORRECT. IT WAS PERFORMED A GROUND ENGINE RUN UP TO 70 RPMS WIT H NO ENGINE CONTROL LIGHT INDICATIONS. LATER, THE LT ELECTRONIC ENGINE CONTROL WAS REPLACED IAW MM 73-21-60 AND WAS TES TED CORRECT IAW MM 73-21-00. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007082100295 20070821 00295 NM 2007 8 21 DHL2007741535 1 20070806 A 5343 651767640 FITTING BOEING 727 7272Q9 138448M NM BS 304 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 RT SIDE NLG TRUNNION SUPPORT FITTING SHOWS SIGNS OF CORROSION ON UPPER CAP, BS 304. CORROSION CLEAN UP WOULD EXCEED TRU NNION BORE DIA LIMITATIONS. REMOVED, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW TRUNNION SPT FITTING, P/N 65- 17676-40, PER B727 SRM 51-30-5, 51-10-2, AND 51-30-2. 2 L 7 3 4F RT A3WE 2007082100296 20070821 00296 NM 2007 8 21 SWAA073958 1 20070809 A 5315 6545410 FLOORBEAM BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CHORD CRACKED AT BS 664, BL 0. REMOVED AND REPLACED FLOORBEAM CHORD PER SRM . 2 L 7 2 4F RT A16WE 2007082100297 20070821 00297 NM 2007 8 21 DHL2007741536 1 20070808 A 5320 69441771 INTERCOSTAL BOEING 727 7272Q9 138448M NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 SFT PIT STRINGER 30 BETWEEN BS 950+10" AND 950A, IS CORRODED. REMOVED "T" CHORD (INTERCOSTAL), CORROSION ON CHORD EXCEE DED LIMITS PER B727 SRM 53-10-1 FIG 1. LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW INTERCOSTAL "T" CHORD P/N 6 9-44177-1 AT BS 950 BETWEEN STR 29L AND 29R, PER B727 SRM 51-30-5, 51-10-1, 51-10-2, AND 51-30-2. 2 L 7 3 4F RT A3WE 2007082100299 20070821 00299 NM 2007 8 21 DHL2007741537 1 20070808 A 5320 WEB BOEING 727 7272Q9 138448M NM BS 1179 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AFT PIT, BS 1179, RBL 30, SPT WEB FOR MAIN CABIN CRACKED. REMOVED SPT WEB SECTION, FABRICATED WEB FROM 2024-T3, .032" B Y 11.25" BY 5.375", PO NR 9005482, PER B727 SRM 51-10-3 AND 51-30-5. TREATED, PRIMED, AND INSTALLED SPT WEB PER B727 SR M 51-10-2 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007082100301 20070821 00301 NM 2007 8 21 DHL2007741538 1 20070726 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 420 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 BS 420, CORROSION NOTED SURROUNDING THE AFT E-BAY DOOR LOCKING PIN FITTING ON FRAME. REMOVED FRAME SECTION, FABRICATED FRAME FROM 7075-T0, .063" BY 7" BY 24", PO NR 9005314, PER B727 SRM 53-10-2 FIG 5 AND 51-20-1 FIG 3. HEAT TREATED MAT T O T6 CONDITION PER FASI ER NR 2-37153-801 REV A. TREATED, PRIMED, AND INSTALLED NEW FRAME PER B727 SRM 51-10-2, 51-30-5 , AND 51-30-2. 2 L 7 3 4F RT A3WE 2007082100302 20070821 00302 NM 2007 8 21 DHL2007741539 1 20070723 A 5710 BAC1506860 BEAM BOEING 727 7272Q9 138448M NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 LT WING T/E UPPER "I" BEAM IS CRACKED FWD OF NR 7 SPOILER SPT FITTING, LWBL 118. REMOVED BEAM, FABRICATED NEW "I" BEAM FROM BAC 1506-860 EXTRUSION, PO NR 7232109, 81" IN LENGTH, PER B727 SRM 51-30-5 AND 57-10-2 FIG 3. TREATED, PRIMED, AND INSTALLED NEW "I" BEAM PER B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007082100303 20070821 00303 NM 2007 8 21 DHL2007741540 1 20070726 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 1030 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AFT PIT, BS 1030 FRAME DENTED BETWEEN STR 25L AND 26L. CUT OUT DENTED AREA, 1.5" BY .875", FABRICATED REPAIR DOUBLER FR OM 7075-T0, .071" BY 11" BY 4", PO NR 9004690, PER B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 5. HEAT TREATED TO T-6 CONDIT ION PER FASI ER NR 2-37153-801 REV A. TREATED, PRIMED, AND INSTALLED PER B727 SRM 51-10-2 AND 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2007082100304 20070821 00304 NM 2007 8 21 DHL2007741541 1 20070723 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 450 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 5 RIVET HEADS DISHED AND SHEARED AT AFT SIDE OF E/E DOOR CUTOUT, BS 450. REMOVED FRAME SECTION, FABRICATED FRAME FROM 7 075-T0, .063" BY 7" BY 24", PO NR 9005314, PER B727 SRM 53-10-2 FIG 5 AND 51-20-1 FIG 3. HEAT TREATED MAT TO T6 CONDITI ON PER FASI ER NR 2-37153-801 REV A. TREATED, PRIMED, AND INSTALLED NEW FRAME PER B727 SRM 51-10-2, 51-30-5, AND 51-30- 2. 2 L 7 3 4F RT A3WE 2007082100305 20070821 00305 NM 2007 8 21 DHL2007741542 1 20070805 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 660 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 FWD PIT, BS 660, AT STR 22R, MAIN FRAME UPPER FLANGE DENTED. CUT OUT DAMAGED AREA, DIMENSIONS 1.625 BY .5, REMOVED EXIS TING REPAIR TO INCORPORATE WITH NEW REPAIR. FABRICATED REPAIR DOUBLER FROM 7075-T0, .063 BY 25 BY 3.75 PER B727 SRM 51- 40-3 FIG 1 AND 53-10-2 FIG 5. HEAT TREATED DOUBLER TO T-6 CONDITION PER FASI ER NR 2-37153-801 REV A. TREATED, PRIMED, AND INSTALLED REPAIR DOUBLER BETWEEN STR 22R AND 24R, BS 660, PER B727 SRM 51-10-2 AND 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2007082100306 20070821 00306 NM 2007 8 21 DHL2007741543 1 20070804 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 950B DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AFT PIT, BS 950B, AT STR 25L TO 27L, MAIN FRAME DENTED BENEATH SIDEWALL PANELS. CUT OUT DAMAGED AREA, 3 EA, DIMENSIONS 1.187 BY 1.125, 1.75 BY 1.125, 1.75 BY 1.125; FABRICATED REPAIR DOUBLER FROM 7075-T0, .071 BY 25 BY 4.0, PO NR 9005571, PER B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 5. HEAT TREATED DOUBLER TO T-6 CONDITION PER FASI ER NR 2-37153-801 REV A. TREATED, PRIMED, AND INSTALLED REPAIR DOUBLER BETWEEN STR 25L AND 27L, BS 950B, PER B727 SRM 51-10-2 AND 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2007082100330 20070821 00330 NM 2007 8 21 HALA0700337 1 20070813 A 3350 LAMP BOEING 767 7673CB 1385187 NM EMERGENCY LIGHTS INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 592HA 33468 CEILING EMERG LIGHT INOP OVER ROW 28 LEFT. RELAMPED WITH GE1317 BULB. OPS NORMAL PER B767 AMM 33-51-00. 2 L 7 2 4F RT A1NM 2007082100331 20070821 00331 NM 2007 8 21 DHL2007750505 1 20070813 A 5330 SKIN BOEING 727 7272M7 138407S NM BS 1203-1214 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 WHILE AT FLIGHTSTAR FOR AN A CHECK DISCREPANCY FUSELAGE REPAIR HAS BLIND FASTENERS INSTALLED AT STA 1203 STR22R AND DOUB LER IS DENTED. REMOVED PREVIOUS REPAIR IAW B727SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER FROM 2024-T3 .063" PO NR 900 5089 DIM 11 1/2" BY 7" IAW B727 SRM 53-30-3 FIG3 AND 53-30-2 FIG 2. TREATED AND PRIMED NEW DOUBLER IAW B727 SRM 51-10-2 . INSTALLED NEW REPAIR AT FUSELAGE BS 1203 STR 22R IAW B727 SRM 53-30-3 FIG 3 AND 51-30-2. THIS IS A CATEGORY B REPAIR . 2 L 7 3 4F A3WE 2007082100332 20070821 00332 NM 2007 8 21 P5CA0701529 1 20070805 A 5310 NP103801113 WINDSHIELD BOEING 747 74746NF 13848BT NM COCKPIT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 451PA 30809 CAPT'S L1 WINDSHIELD CRACKED ON OUTER PANE ORIG IN PVG. REMOVED AND REPLACED WINDSHIELD BOR PART FROM KOREAN AIR PER AM M REF 56-11-01-404-016. 2 L 7 4 4F RT A20WE 2007082100334 20070821 00334 NM 2007 8 21 QXEA200701249 1 20070809 A 5410 SUPPORT ANGLE DHAV DHC8 DHC8202 2809007 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - LEFT NACELLE AT STATION YW139.200 AND XN209.00 AND ZN8.00. THERE IS A CRACK THROUGH THE LOWER AFT FASTENER HOL E IN THE VERTICAL SUPPORT ANGLE FOR LEFT NACELLE SKIN. REPAIRED IAW RD8-54-1726. 2 H 7 2 4T RT A13NM 2007082100336 20070821 00336 NM 2007 8 21 QXEA200701250 1 20070806 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - LEFT OUTBOARD SEAT TRACK HAS A GOUGE ON THE OUTBOARD TOP CAP AT STATION X343. REPAIRED IAW RD8-53-1342. 2 H 7 2 4T RT A13NM 2007082100337 20070821 00337 NM 2007 8 21 QXEA200701251 1 20070805 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - LEFT OUTBOARD SEAT TRACK HAS SOME CORROSION AT STATION X541 TO X545.50. REPAIRED IAW RD8-53-3644, SRM 51-40-00 , 51-40-11. 2 H 7 2 4T RT A13NM 2007082100338 20070821 00338 NM 2007 8 21 SWAA073961 1 20070809 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED C1 CHECK, FOUND LT WING NR 2 L/E SLAT CRACKED AT OUTBOARD T/E. REPAIRED SLAT PER SWA EA. 2 L 7 2 4F RT A16WE 2007082100340 20070821 00340 NM 2007 8 21 QXEA200701252 1 20070806 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 422-451 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - RIGHT CENTER SEAT TRACK NR 8 HAS SCRATCH AT STATION 422 TO 451. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2007082100342 20070821 00342 NM 2007 8 21 QXEA200701253 1 20070806 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - LEFT SEAT TRACK NR 5 HAS SCRATCHES AT STATION X480. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2007082100346 20070821 00346 NM 2007 8 21 QXEA200701254 1 20070806 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 422-451 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - LEFT SEAT TRACK NR 5 HAS SCRATCHES AT STATION 422 TO 451. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2007082100347 20070821 00347 2007 8 21 SWAA073960 4 20070809 A 2565 D31354433 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED C1 CHECK, L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EV AC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007082100349 20070821 00349 NM 2007 8 21 QXEA200701255 1 20070809 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX-CORROSION ON THE ANGLE AT STATION 224 THAT CAME OFF THE OUTBOARD SIDE OF SEAT TRACK #4. REPAIRED IAW SRM 51-40-11 . 2 H 7 2 4T RT A13NM 2007082100351 20070821 00351 NM 2007 8 21 QXEA200701256 1 20070806 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 218-244 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - SEAT TRACK NR 7 HAS CORROSION ON THE TOP BETWEEN STATION 218 AND 244. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2007082100353 20070821 00353 NE 2007 8 21 TRBA2007066 2 20070811 A 7320 8108001002 EEC AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE RT ENGINE INTERMITTENT A TRBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 355AT 355 127105 RT TORQUE DROP TO 0 WHILE CLIMBING, NOTICEABLE PWR DROP AFTER 3 MINUTES PWR CAME BACK. REPLACED RT ENG EEC AS PER JIC 7 3-23-61. PERFORMED RT ENGINE TRIMMING AS PER JIC 73-23-61. PERFORMED POWER RUN-UP AS PER JIC 72-00-00 AND NO TQ DROP N OTED AT THIS TIME. 2 H 7 2 4T 4 T RT A53EU E20NE 2007082100354 20070821 00354 EU 2007 8 21 USAA070646 1 20070810 A 5315 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 177US 1517 AROUND FASTENER HOLES & TOPSIDE OF FLOORBEAM, FR 66-69 HAS CORROSION. INSTALLED NEW FLOORBEAM PER SRM 51-72-11; CORR TA SK JA-260-53500, DEFECT SIZE: 1.5 X 1.5 INCH. 2 L 7 2 4F RT A28NM 2007082100355 20070821 00355 EU 2007 8 21 USAA070645 1 20070810 A 5315 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 177US 1517 FR 12 - FR 16 -Y81 (FLOORBEAM) HAS CORROSION. REMOVED AND REPLACED FLOORBEAMS PER SRM 51-72-11; CORR TASK JA-220-53500, DEFECT SIZE: 2 SQ INCHES. 2 L 7 2 4F RT A28NM 2007082100357 20070821 00357 NM 2007 8 21 QXEA200701263 1 20070805 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 545 S26-27R CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - CORROSION AROUND RIVET ON FRAME AT STATION X545.5 BETWEEN STRINGER 26R AND 27R. REPAIRED IAW SRM 51-20-11, 51- 20-16, AND 51-20-26. 2 H 7 2 4T RT A13NM 2007082100359 20070821 00359 NM 2007 8 21 QXEA200701262 1 20070804 A 5340 STRINGER CLIP DHAV DHC8 DHC8202 2809007 NM BS 424 S24L CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - CORROSION ON STRINGER BRACKET, STRINGER 24L AT STATION 424.12. REPAIRED IAW SRM 51-20-11, 51-20-26, AND 51-20- 16. 2 H 7 2 4T RT A13NM 2007082100362 20070821 00362 NM 2007 8 21 QXEA200701259 1 20070803 A 5340 MOUNT DHAV DHC8 DHC8202 2809007 NM GALLEY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - LIGHT CORROSION AT GALLEY AFT OUTBOARD MOUNT POINT ON FUSELAGE AT STATION X237 - X239. REPAIRED IAW SRM 51-20- 11, 51-20-16, AND 51-20-36. 2 H 7 2 4T RT A13NM 2007082100363 20070821 00363 NM 2007 8 21 QXEA200701260 1 20070805 A 5321 FLOORBOARD DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX-AT FS 565 Z111.5 Y26L THERE IS CORROSION AT THE FLOOR BOARD NUT PLATE AND ITS SUPPORT. REPAIRED IAW SRM 51-20-11 , 51-40-11, 51-20-16, AND 51-20-36. 2 H 7 2 4T RT A13NM 2007082100369 20070821 00369 EU 2007 8 21 USAA070638 1 20070810 A 5322 D5347112420000 SHEAR TIE AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 177US 1517 LEFT REAR SHEAR TIE BETWEEN FRAMES F69 AND F70 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72 -11, DEFECT SIZE: 2 INCH SQ. 2 L 7 2 4F RT A28NM 2007082100376 20070821 00376 NM 2007 8 21 USAA070636 1 20070810 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 BS 907 FRAME AT A/C RAIL ATTACH POINT BETWEEN STRINGERS 8L & 9L CRACKED. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER TR 53-10-20E, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007082100377 20070821 00377 NM 2007 8 21 USAA070635 1 20070810 A 5753 654845521C SKIN BOEING 737 7374B7 1384702 NM T/E FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 443US 24842 THREE INCH AREA, T/E WEDGE SKIN HAS DELAMINATION. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER EA 98827, DEFECT SIZE: 3 INCHES. 2 L 7 2 4F RT A16WE 2007082200004 20070822 00004 NM 2007 8 22 QXEA200701248 1 20070809 A 3340 MS354782233 BULB BOMBDR DHC8 DHC8402 1390042 NM EXTERIOR INOPERATIVE A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 431QX 4164 LAX FLIGHT NR 2334: DURING TAXI, NOTICED POSITION LIGHT NOT ON. TURNED ON SWITCH AND C/B POPPED. AIRCRAFT RETURNED TO B LOCKS. MAINTENANCE REPLACED BULB AND PERFORMED OPS TEST IAW Q400 AMM TASK 33-42-00-710-801. NO DEFECTS NOTED. OPS CHE CK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007082200005 20070822 00005 NM 2007 8 22 QXEA200701247 1 20070807 A 2840 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM FUEL TANK LOW UNKNOWN A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 431QX 4164 LAX FLIGHT NR 2442: NR 1 FUEL TANK LOW CAUTION ON. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE REFUELED AND DEFUELED A/C S EVERAL TIMES LEAVING 2000 LBS A SIDE. NO DEFECTS NOTED. OPERATION PERFORMED IAW Q400 MM TASK 12-10-28-650-802 AND 12-1 0-28-650-801. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007082200025 20070822 00025 NM 2007 8 22 DLM88071052 1 20070809 A 2913 623337 PUMP DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 HYD SYS FAILED A DALA A UNSCHED LANDING S J AFFECT SYSTEMS WARNING INDICATION CR CRUISE 1 SO 27 900DE 53372 725896 AT ALT 230 CLEAN CONFIG LEFT HYD SYSTEM PRESSURE WENT TO ZERO. RAN CHECKLIST AND PER PROCEDURES REGAINED LEFT SYS PRESS URE AFTER TURNING ON AUX AND TRANS PUMPS. REPLACED LT ENGINE HYD PUMP, CASE DRAIN AND IN LINE PRESS FILTERS. RAN ENGIN E CKS OK. LEAK CK OK. 2 L 7 2 4F 4 F RT A6WE E9NE 2007082200028 20070822 00028 NM 2007 8 22 DL764071057 1 20070810 A 5753 SPAR BOEING 767 767432ER 1385134 NM TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830MH 29701 DAMAGE OCCURRED TO THE INBD MAIN FLAP, REAR SPAR, LOWER CHORD DUE TO A BLOWN TIRE. SPAR CHORD CONDITION WAS DENTED. RE PAIRED PER DELTA ERA 463277-14. 2 L 7 2 4F RT A1NM 2007082200030 20070822 00030 NE 2007 8 22 DL757071061 2 20070812 A 7321 FUEL CONTROL BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 SO 27 697DL 59547 30318 716488 ON APPROACH INTO SNA, GOT THE FOLLOWING ORDER OF EVENTS, LT ENGINE OIL PRESSURE ON EICAS AND THE OIL PRESSURE DISCREET L IGHT CAME ON, FOLLOWED BY THE ENGINE ROLLING BACK TO OFF. FLIGHT CREW ELECTED TO DIVERT TO LAX AND NOT LAND IN SNA. R EPLACED FUEL CONTROL AND EEC, NEED LEAK CK ON F/C AND OPS CK ON EEC. RAN END AND LEAK CHECKED FUEL CONTROL, RAN TE STS 7 AND 15 TESTS PASSED AND FUEL CONTROL LEAK CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082200031 20070822 00031 NM 2007 8 22 DLM88071063 1 20070813 A 5310 59360381 DOOR FRAME DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 THE NR 2 CARGO DOOR OPENING LOWER THRESHOLD HAD CORROSION REVOAL IN SEVERAL LOCATIONS. LOCAL BLENDING RESULTED IN THE A FT C/L DOOR STOP HOLE BREAKING OUT. REPAIR PER SRM 53-05 FIG 63 INSTALLED. 2 L 7 2 4F RT A6WE 2007082200039 20070822 00039 EU 2007 8 22 AWXA200700993 1 20070804 A 5320 D53472284002 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 632AW 81 SAL - MAJOR REPAIR - C-07 CHECK - NR 5963565, CORROSION FOUND ON CABIN FLOOR SUPPORT, BS 3043/FR 64 - BS 3207/FR 67, -Y3 18. REPLACED CABIN FLOOR SUPPORT, BS 3043/FR 64 - BS 3207/FR 67, -Y318, IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007082200058 20070822 00058 NM 2007 8 22 EIA2007128 1 20070612 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486EV 20888 EMERGENCY LIGHT UPPER DECK CEILING L3 DOES NOT TEST, REPLACED EMERGENCY LIGHT ASSY UPPER DECK L3 PER B747 MM 33-51-00. OPS CHECKED NORMAL PER SAME. 2 L 7 4 4F A20WE 2007082200059 20070822 00059 NM 2007 8 22 EIA2007129 1 20070513 A 3350 900815 POWER SUPPLY BOEING 747 747132 1384882 NM EMERGENCY LIGHTS INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481EV 19896 UPPER DECK EMERGENCY CREW ESCAPE OVERHEAD DOOR EXIT SIGN INOP. REPLACED UPPER DECK EMERGENCY EXIT DOOR POWER SUPPLY PER B747 MM 33-51-00, OPS CKD NORMAL. 2 L 7 4 4F A20WE 2007082200062 20070822 00062 NM 2007 8 22 EIA2007132 1 20070621 A 3350 900835A LIGHT BOEING 747 747212B 1384886 NM SERVICE DOOR NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482EV 20713 BOTH CREW SERVICE DOOR EMERGENCY SILL LIGHTS INOP. REPLACED BATTERY PACK REF 33-51-00 PAGE 201. SYS OPS CKS NORMAL REF MM 33-51-00 PAGE 501. 2 L 7 4 4F A20WE 2007082200083 20070822 00083 NM 2007 8 22 07FDEA02869 1 20070814 A 5740 311N500118 BUSHING BOEING BOEING 757 7572B7 1384964 NM ZONE 400 MISALIGNED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 901FD 27122 RT WING OUTBOARD UPPER LINK FITTING HAS MIGRATING BUSHINGS. REMOVED BUSHINGS PER SOPM 20-50-03. INSPECTED FITTING PER NTM 51-00-00, PT.6, NO DEFECTS NOTED. HONED, CHAMFERED FLAP PEENED AND SWAGED PER F-5450-108892 FINAL DIA OF THE LUG BORE IS 1.7507. TREATED AND PRIMED PER F-5450-108892. INSTALLED BUSHINGS AND APPLIED SEALANT PER 5450-108892. INSTALL ED WASHERS AND SEALED PER 5450-108892. 2 L 7 2 4F RT A2NM 2007082200088 20070822 00088 EU 2007 8 22 07FDEA02875 1 20070814 A 5347 R5307008820600 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 653FE 736 SEAT TRACK 2R AT FR 78 AND FR75 HAS 1 SQ IN OF CORROSION EACH ZONE 260 REF A300-600 SRM 51-10-00. REMOVED CORRODED FOUN D TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-16. CUT OUT SECTION OF SEAT TRACK IAW A300-600 SRM 53-10-16 FIG 201. INST ALLED NEW REPAIR SECTION OF SEAT TRACK AND SPLICE IAW A300-600 SRM 53-10-16 FIG 201. 2 L 7 2 4F RT A35EU 2007082200102 20070822 00102 SO 2007 8 22 SWIA200718569 1 20070802 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DISCHARGED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 232SW 120306 FORWARD EMERGENCY LIGHTS DO NOT ILLUMINATE, FLIGHT NR 3696. REMOVED AND REPLACED ELBP 1 AND 3. OPS CHECK GOOD. NR 3 P /N D366-04-001, S/N ON 1121, OFF 1268/08-96, NR 1 P/N D366-04-001, S/N ON 489 OFF 794/10-90. 2 L 7 2 4T RT A31SO 2007082200106 20070822 00106 SO 2007 8 22 SWIA200718573 1 20070804 A 3350 LENS EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 233SW 120307 EMERGENCY EXIT SIGN LENS IS CRACKED, FLIGHT NR 5658. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007082200111 20070822 00111 SO 2007 8 22 SWIA200718578 1 20070808 A 3350 COVER EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS MISSING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 221SW 120290 EXIT LIGHT COVER IS MISSING AT ROW 9, FLIGHT NR 5595. REPLACED EMERGENCY EXIT SIGN COVER. 2 L 7 2 4T RT A31SO 2007082200129 20070822 00129 SO 2007 8 22 SIMA200722706 1 20070813 A 5347 13500412007 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 724AE 15687 5000 145301 SEAT TRACK NUMBER 5 FOUND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERATIONAL CHECK GOOD. AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082200143 20070822 00143 EU 2007 8 22 AWXA200700996 1 20070804 A 5321 D5361060500100 FLOOR PANEL AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 632AW 81 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980238, CORROSION FOUND ON FLOORBOARD 222 FF, BS 709/ FR 16 - BS 808/ FR 20, -Y129 2 TO -Y1732. REPLACED FLOORBOARD 222 FF, BS 709/ FR 16 - BS 808/ FR 20, -Y1292 TO -Y1732 I/A/W A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007082200159 20070822 00159 WP 2007 8 22 AALA20071427 1 20070807 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 446AA 49472 LGA - SEAT MOUNTED EMERGENCY LIGHT AT POSITION AB53 INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHT AT POSITION AB53. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007082200165 20070822 00165 NM 2007 8 22 AALA20071443 1 20070629 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 930AN 29529 TUL - EMERGENCY LIGHT AT MID COACH INOPERATIVE. REPLACED BATTERY PACK AT SEAT 19F FOR EMERGENCY LIGHT AT MID COACH. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007082200172 20070822 00172 EU 2007 8 22 07FDEA02892 1 20070815 A 5711 A57110122200 SPAR AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 CRACKED HOLES AT CENTER SPAR DOUBLER RUN OUT AT C44 LT (RELATED P/N TEE A571-10122-200, HOLE C, D IAW SB 53-242). REPAI R PERFORMED BY REAM UP UNTIL CRACK REMOVAL IAW EA 6-5710-112482 AND RAS/053466/009/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082200174 20070822 00174 EU 2007 8 22 07FDEA02894 1 20070815 A 5320 A52472050 FAIRING AIRBUS 300 A300B4605R 3930308 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 CORROSION FOUND ON APU EXHAUST ACCESS FAIRING C103A DOUBLER REPAIR PERFORMED IAW EA 6-5319-112491 AND RAS/DATLS/0003798/ 2007 ISS A. 2 L 7 2 4F RT A35EU 2007082200177 20070822 00177 NM 2007 8 22 07FDEA02897 1 20070815 A 5340 65453135 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 STRINGER CLIP AT STA 720A AND STR. 7L IS CRACKED. REPLACED STRINGER CLIP STA 720A, STR 7L REF SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007082300006 20070823 00006 NM 2007 8 23 KCSA071292 1 20070810 A 5315 FLOORBEAM BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA 880 LBL 42 UPPER CHORD CORRODED WL 118. 2 L 7 4 4F RT A20WE 2007082300015 20070823 00015 WP 2007 8 23 UPS07850426 1 20070704 A 5313 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 FITTING CRACKED AT STA 1160 L19R FWD. REMOVED AND REPLACED LONGERON END FITTING AT STA 1160 L19R IAW SRM 51-1-20D, AND SRM 51-01-24. 2 L 7 4 4F RT 4A25 2007082300019 20070823 00019 NM 2007 8 23 CALA0700417 1 20070810 A 5315 65C33949 FLOORBEAM BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14609 27322 INSPECTION FOUND AFT ENTRY FLOORBEAM CORRODED AT STA 986.5, RBL 21. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, PAGE 2 01-204. 2 L 7 2 4F RT A16WE 2007082300020 20070823 00020 EU 2007 8 23 07FDEA02918 1 20070815 A 5310 A53978476200 CROSSBEAM AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 733FD 715 FOUND CORROSION ON CROSSBEAM C 61 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007082300025 20070823 00025 NM 2007 8 23 07FDEA02924 1 20070815 A 5310 655699213 DOOR FRAME BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 254FE 20936 LT AFT SERVICE DOOR FWD UPPER CAM ROLLER FRAME HAS A CRACK. REMOVED AND REPLACED FWD FRAME IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007082300027 20070823 00027 NM 2007 8 23 HALA0700339 1 20070814 A 3030 UNKNOWN BOEING 767 7673G5 1385126 NM AOA WARNING LIGHT A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, BTB DUE TO PROBE HEAT EICAS MSG CAPT PITOT, R AUX PITOT, L AOA PROBE HEAT LIGHT ILLUMINATED. RESET C/B FOR CAPT PITOT AND L AOA ACCOMPLISHED AMM 30-34-00 OPERATIONAL TEST OF PROBE HEAT SYSTEM. TEST OK. ACCOMPLIS HED AMM 30-32-00 OPERATIONAL TEST OF THE ANGLE OF ATTACK PROBE HEAT SYS TEST OK. ACCOMPLISHED AMM 30-31-00 OPERATIONAL TEST OF THE PITOT STATIC PROBE HEAT SYS, TEST OK. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007082300032 20070823 00032 NM 2007 8 23 QXEA200701291 1 20070806 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 210 S31R DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - DENT IN FUSELAGE, PROTRUDING OUTWARD STATION X210, STRINGER 31R. REPAIRED IAW RD8-53-5384 AND RD8-53-7939. 2 H 7 2 4T RT A13NM 2007082300034 20070823 00034 NM 2007 8 23 CALA0700421 1 20070811 A 5347 6545410199 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND A 1 INCH CRACK IN LEFT O/B SEAT TRACK I/B MOUNT FLANGE AT STA 727B, LBL 45.5. A LONGITUDINAL FLOORBEAM REPAIR WAS INSTALLED IAW ECRA 5321-01492. 2 L 7 2 4F RT A16WE 2007082300042 20070823 00042 CE 2007 8 23 N71CK81307 1 20070813 A 2612 FIRE WARNING LEAR 35 36A 5170603 CE RT ENGINE FALSE ACTIVATION E KC8A K NONE N FALSE WARNING AP APPROACH 1 GL 23 71CK 035 RT ENGINE HAD A FIRE WARNING LIGHT ILLUMINATE. THE CAUSE OF THE WARNING HAS NOT BEEN DETERMINED AS OF THIS DATE. THERE IS NO INDICATION OF A FIRE OR A HOT SPOT ON THIS ENGINE OR ENGINE NACELLE. THERE WILL BE A FOLLOW-UP SDR WITH THE RESU LTS OF INVESTIGATION. AS OF NOW, IT SEEMS TO BE A FALSE INDICATION. 2 L 7 2 4F A10CE 2007082300043 20070823 00043 NM 2007 8 23 SWAA074003 1 20070810 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 768SW 30587 R2 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007082300047 20070823 00047 NM 2007 8 23 SWAA073992 1 20070809 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 733SA 27865 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986, RBL 5. REPAIRED FLOORBEAM CHORD PER ER. 2 L 7 2 4F RT A16WE 2007082300063 20070823 00063 NM 2007 8 23 QXEA200701286 1 20070809 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 638 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - RIGHT SEAT TRACK NR 9 HAS LIGHT CORROSION AT STATION 638. REPAIRED IAW RD8-53-784 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2007082300065 20070823 00065 NM 2007 8 23 SWAA073982 1 20070809 A 3210 654610914L BUSHING BOEING 737 7373H4 1384600 NM RT MLG WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 603SW 27954 DURING SCHEDULED BRDG CHECK, FOUND RT MLG WALKING BEAM BUSHING WORN. REMOVED AND REPLACED BUSHING PER MM. 2 L 7 2 4F RT A16WE 2007082300068 20070823 00068 NM 2007 8 23 SWAA073983 1 20070809 A 3210 6546150 BEARING BOEING 737 7373H4 1384600 NM RT MLG WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 603SW 27954 DURING SCHEDULED BRDG CHECK, FOUND RIGHT MLG WALKING BEAM BEARING WORN. REMOVED AND REPLACED BEARING PER MM. 2 L 7 2 4F RT A16WE 2007082300084 20070823 00084 NM 2007 8 23 SWAA073991 1 20070809 A 5523 65C25773 HINGE BOEING 737 7373T5 1384608 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED CABIN VISIT CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE PER SWA EA. 2 L 7 2 4F RT A16WE 2007082300088 20070823 00088 EU 2007 8 23 07FDEA02928 1 20070816 A 5313 A53989507201 STRINGER AIRBUS 300 A300B4605R 3930308 EU ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 CRACKED STRINGER P 9 RT, C97-100 STRINGER REPAIR PERFORMED BY SPLICING IAW. EA 6-5319-106510 AND RAS/DAHAM/4022477/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082300099 20070823 00099 EU 2007 8 23 07FDEA02937 1 20070816 A 5340 A25313792202 MOUNT AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 CORROSION ON FLANGE AT GALLEY ATTACHMENT C12A-13, Y450-953 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007082300106 20070823 00106 EU 2007 8 23 07FDEA02943 1 20070816 A 5310 A53985135205 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 CORROSION ON UPPER CORNER FITTING C88 RT REPAIR PERFORMED BY DOUBLER INSTALLATION IAW EA 6-5319-10651 AND RAS/DATLS/0003 749/2007 ISS B. 2 L 7 2 4F RT A35EU 2007082300110 20070823 00110 EU 2007 8 23 07FDEA02947 1 20070816 A 5754 SKIN AIRBUS 300 A300B4605R 3930308 EU ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 SLAT 32 RT DENT IN SKIN, RIB 48 DENT IS ACCEPTABLE AS IT IS, FASTENER CHANGED TO TO NAS1739E5, APPROVED BY EA 6-5740-112 472 AND RAS/FOK/183/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082300114 20070823 00114 NM 2007 8 23 SWAA073977 1 20070809 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007082300115 20070823 00115 EU 2007 8 23 07FDEA02950 1 20070816 A 5230 A52370083202 FITTING AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORNER FITTING FWD CARGO DOOR C 20 CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007082300116 20070823 00116 EU 2007 8 23 07FDEA02951 1 20070816 A 5230 A52372062202 FITTING AIRBUS 300 A300B4605R 3930308 EU ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORROSION ON CARGO DOOR CORNER FITTING C 25A REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007082300117 20070823 00117 NM 2007 8 23 QXEA200701304 1 20070811 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSLEAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - DENT WITH GOUGE ON RIGHT FUSELAGE AT STATION 219 AND Z113. REPAIRED IAW RD8-53-5384, AND RD8-53-9743. 2 H 7 2 4T RT A13NM 2007082300121 20070823 00121 NM 2007 8 23 QXEA200701306 1 20070809 A 5313 STRINGER DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - STRINGER 23P CLEAT IS CORRODED AT STATION X429. REPAIRED IAW SRM 51-40-11, AND RD8-53-9747. 2 H 7 2 4T RT A13NM 2007082300135 20070823 00135 NM 2007 8 23 DLM90071075 1 20070720 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 CUSP WEB IS CORRODED UNDER L-2 GIRT BAR FITTING. CUT OUT DAMAGED AREAS REPAIRED IAW ERA 39819-14MA REV ORG 9/18/02. 2 L 7 2 4F RT A6WE 2007082300139 20070823 00139 NM 2007 8 23 CALA0700430 1 20070812 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14609 27322 INSPECTION FOUND A .5 INCH CRACK IN FRAME AT STA 867 BELOW S8L. THE FRAME WAS REPAIRED IAW ECRA 5310-04649. 2 L 7 2 4F RT A16WE 2007082300147 20070823 00147 NM 2007 8 23 DL764071084 1 20070815 A 2150 2780539103 ISOLATION VALVE BOEING 767 767432ER 1385134 NM LT ACM UNSERVICEABLE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 844MH 29717 LEFT ISOLATION VALVE WILL NOT OPEN. REPLACED LEFT ISOLATION VALVE PER AMM. VALVE OPS CKS GOOD MFG P/N 2780539-103. 2 L 7 2 4F RT A1NM 2007082300148 20070823 00148 NM 2007 8 23 CALA0700434 1 20070813 A 5230 65C80735183 CHANNEL BOEING 737 7373T0 1384582 NM FWD CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR CHANNEL AT FORWARD LOWER STOP. REPAIRED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007082300156 20070823 00156 EU 2007 8 23 SIMA200722901 1 20070814 A 6120 78249052 PCU HAMSTD SAAB SF340 340B 7860101 EU HAMSTD 14RF 14RF19 NE RT PROPELLER FAILED A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 219AE 19724 937 385 340B219 385 RIGHT PROPELLER SURGING, TORQUE FLUCTUATED PLUS/MINUS 3 PERCENT WITH ITT INCREASING AND DECREASING PLUS/MINUS 5 PERCENT WITH TORQUE. REMOVED AND REPLACED RIGHT PROPELLER CONTROL UNIT IAW SAAB AMM 61-20-05. PERFORMED OPERATIONAL CHECKS IAW SAAB AMM 61-00-00 AND 71-00-00 WITH NO DEFECTS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 6 C P11NE 2007082300157 20070823 00157 NM 2007 8 23 2007UALA02733 1 20070718 A 2820 MS29563014 O-RING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CENTER FUEL TANK LEAKING A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 654UA 25392 RIGHT WING FUEL TRANSFERRING INTO CENTER FUEL TANK AT A RATE OF 350LBS PER HOUR. FOUND LEAKY COUPLING IN CENTER RIGHT A UX TANK UPPER RIB, SCAVENGE LINE TO CENTER TANK, ORDERED PACKING PCN 750-7006. FOUND THE RIGHT CENTER AUX SCAVENGE LINE LEAKING. REPLACED THE O-RING. LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082300158 20070823 00158 EA 2007 8 23 SIMA200722902 1 20070815 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA A/C DUCT SMOKE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 523AE 10152 ON TAXI SMOKE NOTICED COMING FROM AIR CONDITIONING DUCT, APPLIED SMOKE PROCEDURES AND SMOKE STOPPED. ISSUED MEL 21-13. 2 L 7 2 4F RT A21EA 2007082300161 20070823 00161 NM 2007 8 23 2007UALA03084 1 20070807 A 3240 BRAKE ASSY BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE MLG MALFUNCTIONED A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 795UA 26927 LANDED UNDER AMBER ALERT DUE TO HYDRAULIC QUANTITY INDICATION. 08-31-07 AFTER TROUBLESHOOTING, THERE WAS EVIDENCE OF LEAKING & BRAKE CONTAMINATION W/ HYD FLUID, REPLACED NR 2 CENTER BRAKE ASSY, INCLUDING SUSPECTED LEAK SOURCE, THE HYDR AULIC COUPLING TO BRAKE. NO MORE LEAKS DETECTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007082300166 20070823 00166 NM 2007 8 23 2007UALA02694 1 20070717 A 2820 UNKNOWN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUEL TRANSFER SY UNKNOWN A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 783UA 26950 UNEVEN FUEL TANKS AND CTR SCAVENGE SYS CTR TANK APPEARS TO BE TRANSFERING TO RT MAIN IMMEDIATELY. LT MAIN QTY UNCHANGED AND RT INCREASES ABOUT 2.3 DURING 1ST 2 HRS. IT ONLY TRANSFERED WHEN CENTER PUMPS WERE ON AND APPEARED TO FILL RT TANK TO LIMIT. OPTED RIGHT FUEL SCAVENGE SYSTEM. REVIEWED PREVIOUS HISTORY OF EARLY FUEL TRANSFER INTO RT MAIN FROM CENTER FUEL TANK. MX PERFORMED FUEL TRANSFER CHECK AND WAS NOT SUCCESSFUL IN DUPLICATING EARLY TRANSFER FROM THE CENTER RT FUE L SCAVANGE PUMP. THIS ITEM IS TO REMAIN OPEN FOR 3 FLT CYCLES FOR CREW COMMENTS ON REOCCURRING PROBLEM. NO PROBLEMS IN LAST SIX LEGS AS OF 24JUL2007. AIRCRAFT RETURNED TO SERVICEABLE STATUS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007082300172 20070823 00172 NM 2007 8 23 2007UALA03089 1 20070809 A 5754 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L/E SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 307UA 23668 NR 4 SLAT UPPER TRAILING EDGE SURFACE HAS DELAMINATION APPROX FIVE INCHES LONG AND SIX INCHES WIDE STICKING UP AT FORTY FIVE DEGREE ANGLE. PERFORMED COMPOSITE REPAIR ON NR 2 PYLON FAIRING. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082300177 20070823 00177 EU 2007 8 23 AWXA200700999 1 20070815 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT FAULTY A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 656AW 1079 MCN - EES - BC-6 CHECK - NR 5961062, AFT FLIGHT ATTENDANT SEAT OUTBOARD FLASHLIGHT INOPERATIVE DUE TO BATTERY FAILED TO BE CHARGED. REPLACED AFT FLIGHT ATTENDANT SEAT OUTBOARD FLASHLIGHT BATTERY AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 2007082300180 20070823 00180 NM 2007 8 23 2007UALA03036 1 20070805 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 DOOR 2R EMERGENCY SILL LIGHTS 2EA IS INOPERATIVE. 08-31-07 RELAMPED. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082300183 20070823 00183 NM 2007 8 23 2007UALA03039 1 20070805 A 3350 CHARGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 FOUND RIGHT OVERWING EMERGENCY LIGHTS 4EA IS INOPERATIVE. 08-31-07 REPLACED BATTERY CHARGER. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082300185 20070823 00185 NM 2007 8 23 2007UALA03041 1 20070804 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 NR 2R EXTERIOR EMERGENCY LIGHT ASSY INOPERATIVE. 08-31-07 REPLACED EMERGENCY LIGHT ASSY UNIT. CHECKS NORMAL 2 L 7 4 4F 4 F RT A20WE E24NE 2007082300186 20070823 00186 NM 2007 8 23 2007UALA03042 1 20070804 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 FOUND ONE BULB INOP IN LEFT EXTERIOR EMERGENCY LIGHT ASSY NR 2. 08-31-07 RELAMPED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082300187 20070823 00187 NE 2007 8 23 2007UALA03043 2 20070806 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 STALLED A UALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 29 598UA 28751 727199 RTFL DUE TO NR 1 ENGINE STALL. NR 1 ENG, WINDMILLING INSPECTION WAS ACCOMPLISHED AS PART OF TROUBLESHOOTING. FILTERS AND CHIPS FOUND CLEAN AFTER FIRST RECHECK. REPLACED EEC ALTERNATOR STATOR AND ROTOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082300189 20070823 00189 NM 2007 8 23 2007UALA03045 1 20070806 A 2750 FLAP SYSTEM BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE TE FLAPS NONE A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 674UA 29242 LE SLAT AND TE FLAP DISAGREE EICAS ON FINAL. 08-31-07 CONFIGURED FLAPS AND CYCLED SEVERAL TIMES 0-30 UNITS, INDICATION S NORMAL. FESU BIT TESTS DETECT NO FAULTS. GREEN TEST COMPLETE LIGHT SHOWS. UNABLE TO DUPLICATE REPORTED PROBLEM. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082300192 20070823 00192 EU 2007 8 23 2007UALA03049 1 20070806 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN SMOKE A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 465UA 1341 DURING PUSHBACK AND TAXI PASSENGERS IN ROWS 10-13 REPORT STRONG ODOR OF BURNING RUBBER. NO VISIBLE SMOKE NOTED. FOUND I NTERNAL APU OIL LEAK. REPLACED THE APU. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300193 20070823 00193 NM 2007 8 23 2007UALA03050 1 20070807 A 3200 UNKNOWN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BRAKES SMOKE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 WP 29 370UA 24539 AFTER LANDING SMOKE REPORTED COMING FROM RT OUTBD MLG BRAKE AREA. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082300195 20070823 00195 NM 2007 8 23 2007UALA03052 1 20070806 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE SEAT ROW 18 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 303UA 23644 EEL STRIP INOP FROM SEAT ROW 18 AFT. REPLACED EEL LIGHT POWER STRIP AND GALLEY LAMP ASSY, ALL EEL LIGHTS OPERATE NORMAL . 2 L 7 2 4F 4 F RT A16WE E2GL 2007082300196 20070823 00196 NM 2007 8 23 2007UALA03053 1 20070806 A 3220 TORQUE LINK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NLG DAMAGED A UALA O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 WP 29 318UA 23950 NOSE WHEEL SHIMMY AT TAXI SPEEDS, NORMAL AT HIGH SPEEDS. NOSE WHEEL TORQUE LINKS WORN BEYOND LIMITS CAUSING LOW SPEED SHIMMY. REPLACED BOTH NOSE LANDING TORSION LINKS, PERFORMED TAXI TEST, 2 L 7 2 4F 4 F RT A16WE E2GL 2007082300197 20070823 00197 2007 8 23 2007UALA03054 4 20070806 A 2565 GIRT BAR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE DOOR 2L FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 936UA 26667 CREW REPORT, DOOR 2L WILL NOT ARM PROPERLY. HOOK AND LOOP HOLDING GIRT BAR ASSY CAME LOOSE, ALLOWING IT TO MOVE OUT OF POSITION. REMOVED SLIDE AND REPOSITIONED GIRT BAR AND HOOK AND LOOP, REINSTALLED SLIDE. ARMS NORMALLY. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122800078 20071228 00078 NM 2007 12 28 2007UALA05108 1 20071215 A 2751 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE TE FLAPS ILLUMINATED A UALA C ABORTED TAKEOFF J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 676UA 30028 ABORTED TAKEOFF AT 90 KNOTS DUE TO AURAL FLAP WARNING AS WELL AS EICAS INDICATION. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082300199 20070823 00199 2007 8 23 2007UALA03096 4 20070809 A 2565 SLIDE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE OVERWING UNSERVICEABLE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 841UA 1545 RIGHT OVERWING SLIDE UNSERVICEABLE. WATER CONTAMINATION/INTRUSION REPLACED SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300200 20070823 00200 NM 2007 8 23 2007UALA03097 1 20070809 A 2560 PLATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GIRT BAR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 DOOR 1R, 2L & 4L GIRT BAR RESTRAINING PLATES ARE CORRODED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082300203 20070823 00203 NM 2007 8 23 2007UALA03100 1 20070809 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 569UA 26677 VARIOUS EMERGENCY EXIT LIGHTS ARE ON AND WILL NOT TURN OFF WITH SWITCHES. FLOOR LIGHTS AT ROWS 23-31 AND CEILING AT 14- 23. ACCOMPLISHED TEST OF EACH SECTION AND ALL LIGHTS TEST. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082300204 20070823 00204 EU 2007 8 23 2007UALA03101 1 20070809 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 403UA 442 FWD FACING AISLE, OVERHEAD-OVERWING EMERGENCY EXIT SIGN HAS SEVERAL BULBS INOP. RELAMPED 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300208 20070823 00208 EU 2007 8 23 2007UALA03105 1 20070809 A 3350 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 449UA 851 EMERGENCY LIGHT SYSTEM FAILED TO TEST. EPSU BATTERY FAILURE. REPLACED FAULTY BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300209 20070823 00209 NM 2007 8 23 2007UALA03106 1 20070810 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY OVERWING LIGHT RIGHT 3RD LIGHT FROM TOP, FWD BULB INOP. 08-31-07 RELAMPED EMERGENCY LIGHT. OP CHECKS NORM ALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082300210 20070823 00210 NM 2007 8 23 2007UALA03107 1 20070810 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY LIGHT ROWS 2J & 3A AFT ARE INOPERATIVE. 08-31-07 REPLACED EMERGENCY LIGHT IN BOTH ROWS. OP CHECKS NORMALLY . 2 L 7 4 4F 4 F RT A20WE E24NE 2007082300211 20070823 00211 NM 2007 8 23 2007UALA03108 1 20070810 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY LIGHT ROW 47 ABC INOPERATIVE. 08-31-07 EMERGENCY LIGHT ROW 47 ABC RELAMPED. CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082300212 20070823 00212 NM 2007 8 23 2007UALA03109 1 20070810 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY LIGHT MID GALLEY LEFT BOTTOM WALL INOP. 08-31-07 RELAMPED. OP CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082300213 20070823 00213 NM 2007 8 23 2007UALA03110 1 20070809 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 673UA 29241 THE 1B EXIT PATH LIGHT ON SEATS SIDE LOOSE. 08-31-07 REPLACED EEL STRIP, CHECKS OK. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082300214 20070823 00214 NM 2007 8 23 2007UALA03111 1 20070809 A 2497 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 1 GENERATOR ARCED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 675UA 29243 NR 1 ENG GENERATOR FEEDER CABLE FOUND ARCING TO CLAMP, APPROX 3-16TH INCH DEEP AND 1-4 INCH WIDE. CLAMP SUPPORT BRACKED AT 9 O'CLOCK POSITION IS ONE THIRD BURNED AWAY. 09-04-07 REMOVED AND REPLACED NR 1 ENG IDG FEEDER CABLE FROM LE SPL ICE TO IDG. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082300215 20070823 00215 NM 2007 8 23 2007UALA03112 1 20070809 A 3350 BATTERY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 675UA 29243 EEL LIGHT INOPERATIVE ON SEAT 40AB. 08-31-07 RETERMINATED CONNECTOR AND REPLACED BATTERY PACK. OPS CK GOOD PER SWPM 20-64-17 AND MM 33-51-07. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082300218 20070823 00218 EU 2007 8 23 2007UALA03115 1 20070808 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 434UA 592 EMERGENCY LIGHT TEST FAILURE EPSU EXT LOAD FWD LEFT. FOUND EPSU FAILED. REPLACED FWD LEFT EPSU, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300219 20070823 00219 2007 8 23 2007UALA03116 4 20070810 A 2565 62510101 ASPIRATOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SLIDE RAFT LEAKING A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 228UA 0090 30556 BOTH ASPIRATORS ARE LEAKING FROM THE FLAPPER VALVES. REPLACED ASPIRATORS. 08-31-07 SUSPECT ASPIRATOR BODIES CRUSHED D URING PACKING. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007082300222 20070823 00222 2007 8 23 2007UALA03119 4 20070810 A 2565 DISC AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EVAC SLIDE MISSING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 848UA 1647 THE 2L & 2R SLIDE PRESS INDICATOR CLEAR DISC MISSING. REPLACED INDICATOR DISC. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300223 20070823 00223 NM 2007 8 23 2007UALA03120 1 20070812 A 3350 LENS AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 852UA 1671 SEAT 11C EMERGENCY ESCAPE PATH RED LIGHT LENSE BROKEN. REPLACED THE LENS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082200049 20070822 00049 NM 2007 8 22 EIA2007150 1 20070806 A 3350 S1356B37 LIGHT BOEING 747 747273C 1384896 NM CABIN INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 470EV 20653 L1 DOOR EMERGENCY SILL LIGHTS INOP (2). 2 L 7 4 4F A20WE 2007082200053 20070822 00053 NM 2007 8 22 EIA2007123 1 20070605 A 3350 S1356B37 LIGHT BOEING 747 747273C 1384896 NM CABIN NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 471EV 20651 RT CEILING EMERGENCY LIGHT AT STATION 2040-2065 INOP. REMOVED AND REPLACED CEILING EMERGENCY LIGHT, OPS CHECKED NORMAL PER B747 MM33-51-00. 2 L 7 4 4F A20WE 2007082200057 20070822 00057 NM 2007 8 22 EIA2007127 1 20070613 A 3350 S1356B37 LIGHT BOEING 747 747132 1384882 NM CABIN NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481EV 19896 EMERGENCY LIGHT RT UPPER DECK LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY, OPS CHECKED NORMAL IAW 33-51-07. 2 L 7 4 4F A20WE 2007082200061 20070822 00061 NM 2007 8 22 EIA2007131 1 20070613 A 3350 S1356B37 LIGHT BOEING 747 747132 1384882 NM CABIN MALFUNCTIONED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481EV 19896 EMERGENCY LIGHT BY UPPER DECK SERVICE DOOR STAYS IN THE ARM POSITION. REMOVED AND REPLACED LIGHT ASSY OPS CKD NORMAL PE R B747 MM 33-51-07. 2 L 7 4 4F A20WE 2007082200069 20070822 00069 NM 2007 8 22 EIA2007139 1 20070713 A 3350 900835A BATTERY PACK BOEING 747 747230B 1384889 NM EMERGENCY LIGHTS NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 488EV 23287 EMERGENCY LIGHT IN UPPER DECK LOUNGE DID NOT COME ON DURING TEST. INSTALLED BATTERY PACK POWER SUPPLY MODULE PER B747 M M 33-51-04 PAGE 201-204, OPS CHECKED PER B747 MM 33-51-04 PAGE 204-205. 2 L 7 4 4F A20WE 2007082200070 20070822 00070 NM 2007 8 22 EIA2007140 1 20070716 A 5414 65B9405315 SKIN PANEL BOEING 747 747230B 1384889 NM NR 3 PYLON GOUGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 488EV 23287 NR 3 PYLON OUT BOARD ACCESS DOOR NR 473AR THE DOOR RING HAS DEEP GOUGE AT INNER SIDE. REPAIRED NR 3 PYLON OUTBOARD ACC ESS DOOR NR 473AR PER ECRA 488-54-019-2. 2 L 7 4 4F A20WE 2007082200073 20070822 00073 NM 2007 8 22 EIA2007143 1 20070613 A 5315 FLOORBEAM BOEING 747 747230B 1384889 NM BS 840 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 488EV 23287 RT 840 BL 46 SCREW IS DOUBLE DRILLED AND DEEP DRILL STARTS ON FLOORBEAMS. REPAIRED RT STA 840 BL 46 FLOORBEAM PER ECRA 488-53-014-2. 2 L 7 4 4F A20WE 2007082200077 20070822 00077 WP 2007 8 22 07FDEA02862 1 20070813 A 5347 SEAT TRACK DOUG MD10 MD1010F 3022112 WP BS 899-919 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 ELONGATED SCALLOPS AT CABIN SEAT TRACK, STA 899 TO 919, RBL47.5. [08-29-07] CHECKED LIMITS, MAX ALLOW BETWEEN EDGE OF SCALLOP IS .500. FOUND TO BE GREATER THAN .500. OUT OF LIMITS IAW DC/MD-10 SRM 53-70-00 VOL 1 PG 21. DIAL CALIPER T8878F REMOVED AND REINSTALLED (2) FLR BOARDS AT STA 819-879 RBL 27-76 IAW MD-10 MM 53-21-08-2 REMOVED OLD SEAT TRACK A ND INSTALLED NEW SEAT TRACK IAW DC/MD-10 SRM 51-31-01 VOL 2 PG1. MAT ID AND FABED SEAT TRACK IAW DC/MD-10 SRM 53-42-01 VOL 3 PG 13&14 AND 53-70-00 VOL 1 PG 3. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01 VOL 2 PG 1&21, PART MARKED IAW FED-EX GMM 7-0-10-00. MAJOR REPAIR 2 L 7 3 4F RT A22WE 2007082200078 20070822 00078 WP 2007 8 22 07FDEA02863 1 20070813 A 5347 492914713500 SEAT TRACK DOUG MD10 MD1010F 3022112 WP BS 1039 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 GOUGED, CABIN SEAT TRACK AT STA 1039 TO 1059, LBL 27.5 CHECKED LIMITS, GAP BETWEEN SCALLOPS FOUND TO BE GREATER THAN .50 0 (MAX ALLOWED) OUT OF LIMITS IAW DC/MD-10 SRM 53-70-00 VOL 1 PG 21. REMOVED DAMAGE SEAT TRACK SECTION AND INSTALLED FA B`D SEAT TRACK SECTION IAW DC/MD-10 SRM 53-70-00 VOL 1 PG 3 AND 51-31-01 VOL 2 PG 1. MAT ID SECTION IAW DC/MD-10 SRM 53 -42-01 VOL 3 PG 13 AND 14. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01 VOL 2 PG 1 AND 21. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2007082200086 20070822 00086 EU 2007 8 22 07FDEA02873 1 20070814 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 653FE 736 MDCC AT FR22 BETWEEN STG 9R AND 8R HAS 1 EA GOUGE APPROX 1" ZONE 230 REF A300-600 SRM 51-10-00. REMOVED DAMAGE FRAME SP LICE PER A300-600 SRM 51-40-21. CUT OUT CRACKED FRAME INNER FLANGE AND INSTALLED REPAIR SPLICE PER FEDEX EA 6-5310-1105 21. 2 L 7 2 4F RT A35EU 2007082200097 20070822 00097 EU 2007 8 22 07FDEA02884 1 20070814 A 5315 7075T7 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 653FE 736 LATE FIND FLOORBEAM FR 30 BETWEEN SEAT TRACK NR 2L AND 3L HAS A .5 INCH CRACK AT STIFFENER. CUT OUT DAMAGED SECTION OF FLOORBEAM IAW A300-600 FREIGHTER SRM 53-10-15. FABRAICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW A300-600 FREIGHTER SRM 53-10-15. ALODINED ALL PARTS IAW A300 SRM 51-21-10. PRIMED ALL PARTS IAW A300 SRM 51-75-10. TOPCOATED REPAIR IAW A300 SRM 51-75-10. 2 L 7 2 4F RT A35EU 2007082200104 20070822 00104 SO 2007 8 22 SWIA200718571 1 20070803 A 3350 BULB EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 251YV 120251 FORWARD EMERGENCY FLOOD LIGHTS WILL NOT TEST, FLIGHT NR 3747. INSTALLED NEW BULBS. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007082200113 20070822 00113 NM 2007 8 22 F3LA200700197 1 20070811 A 3350 LIGHT AIRBUS A319 A319111 3930336 NM CABIN UNKNOWN A F3LA O OTHER J WARNING INDICATION CR CRUISE 1 NM 03 922FR 2012 FLIGHT CREW REPORTED C/B H05 TRIPPED IN FLIGHT, WHICH IS AN EMERGENCY LIGHT C/B. MAINTENANCE INSPECTED THE EMERGENCY LI GHT SYSTEM AND FOUND NO FAULTS. RESET C/B AND PERFORMED SYSTEM TEST. NO FAULTS FOUND. 2 L 7 2 4F RT A28NM 2007082200118 20070822 00118 SO 2007 8 22 SIMA200722702 1 20070814 A 3242 38793500 SHUTOFF VALVE EMB 145 EMB145LR 3260212 SO ZONE 700 FAILED A SIMA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SW 21 635AE 18456 145158 ABORTED TAKEOFF, BRAKE OVERHEAT WARNING MESSAGE. REMOVED AND REPLACED INBOARD BRAKE SHUTOFF VALVE IAW EMB AMM 32-41-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007082200119 20070822 00119 SO 2007 8 22 SIMA200722704 1 20070814 A 3350 LIGHT EMB 135 EMB135KL 3260302 SO CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 841AE 145667 EMERGENCY FLOOR STRIP LIGHTS AT ROW 3 THROUGH ROW 6 INOPERATIVE. 2 L 7 2 4F RT T00011AT 2007082200130 20070822 00130 SO 2007 8 22 SIMA200722710 1 20070813 A 5347 13500439007 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 724AE 15687 5000 145301 LEFT INBOARD SEAT TRACK NUMBER 1 FOUND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW IAW EMB AMM 53-01-06. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082200135 20070822 00135 NE 2007 8 22 NACA20070015 2 20070809 A 8530 356993 CYLINDER HEAD DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE ENGINE CRACKED A NACA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AL 03 2907F 1045 533265 31026 NR 2 ENGINE SHUTDOWN DUE TO HIGH CHT, 150 DEGREES AT IDLE, 250+ DEGREES AT 30 INCHES WITH COWL FLAP AT 6 DEGREES. NR 2 ENGINE, NR 18 CYLINDER CRACKED HEAD. REPLACED NR 18 CYLINDER PER NAC DC-6 MM SECTION V PG 16. OP CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2007082200140 20070822 00140 NM 2007 8 22 F3LA200700199 1 20070808 A 5320 SUPPORT BEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 935FR 5379 2318 DURING C-2 CHECK, INSPECTION REPORTED FR C-20 TOP SUPPORT BEAM IN LT FWD ELECTRICAL EQUIPMENT COMPARTMENT FRETTING. FOU ND FITTING TO BE OUT OF LIMITS IAW AIRBUS DRAWING D53113988. PERFORMED HFEC OF FR C-20 INBD SUPPORT BEAM LUG ON NLG WHE EL WELL UPPER AFT LT CORNER IAW NTM 51-10-08, PART 6. NO CRACKS FOUND ON LUG. OVERSIZED SLOT AND FABRICATED BUSHING IA W EA A9-53R-12068. INSTALLED NEW BUSHING IAW A319 SRM 51-42-11, P6, AND EA A9-53R-12068. 2 L 7 2 4F RT A28NM 2007082200141 20070822 00141 NM 2007 8 22 NWAA072846623 1 20070812 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 623US 21705 DURING OVERNIGHT CHECK FOUND LEFT SIDE EXTERIOR EMERGENCY OVERWING SLIDE LIGHTS ARE INOP. MAINTENANCE REMOVED AND REPLA CED POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F A20WE 2007082200166 20070822 00166 NM 2007 8 22 AALA20071444 1 20070629 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 930AN 29529 TUL - EMERGENCY LIGHTS AT FORWARD COACH INOPERATIVE. REPLACED BATTERY PACK AT SEAT 12A FOR EMERGENCY LIGHTS AT FORWARD COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007082300005 20070823 00005 NM 2007 8 23 BB07063 1 20070811 A 2910 12275190002 MODULE BOEING 767 767201 1385125 NM HYDRAULIC SYS LEAKING A USAA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 EA 19 249AU 23901 FLIGHT 707, MUC-PHL: FLIGHT DIVERTED TO LGW DUE TO CENTER HYDRAULIC SYSTEM QUANTITY DROPPING. MAINTENANCE REPLACED THE FLAP/SLAT HYDRAULIC SHUTOFF VALVE MODULE. 2 L 7 2 4F RT A1NM 2007082300007 20070823 00007 NM 2007 8 23 KCSA071296 1 20070813 A 5311 FRAME BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 RIGHT BODY GEAR WHEEL WELL, BS 1416 OVERWING LONGERON SUPPORT FRAME CORRODED AT LOWER END RBL 120. 2 L 7 4 4F RT A20WE 2007082300008 20070823 00008 NM 2007 8 23 BB07064 1 20070813 A 3350 2012 CHARGER BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 930UW 27145 MAINTENANCE FOUND THE L4 AND R4 DOOR ESCAPE SLIDE LIGHTS INOPERATIVE. REPLACED THE BATTERY CHARGER. NO FURTHER FAULTS. 2 L 7 2 4F RT A2NM 2007082300013 20070823 00013 NM 2007 8 23 UPS07650417 1 20070809 A 4950 MODULE BOEING 767 76734AF 1385212 NM APU MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 330UP 27756 INSPECTION TYPE:ETOP APU BLEED INOP DEFERRED M 356254. T/S PER FIM APU BITE SHOWED PT SENSOR WITH MINIFLAG 14. REMOVED AND REPLACED FLOW SENSING MODULE PER MM 49-53-08-4. OPS AND BITE CHECK GOOD. THIS CLEARS M356254. 2 L 7 2 4F RT A1NM 2007082300035 20070823 00035 NM 2007 8 23 CALA0700422 1 20070811 A 5347 6545410155 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND A 1 INCH CRACK IN RIGHT I/B SEAT TRACK I/B MOUNT FLANGE AT STA 727B, RBL 24.8. A LONGITUDINAL FLOORBEA M REPAIR WAS INSTALLED IAW ECRA 5321-01492. 2 L 7 2 4F RT A16WE 2007082300044 20070823 00044 NM 2007 8 23 SWAA073998 1 20070810 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007082300064 20070823 00064 NM 2007 8 23 QXEA200701287 1 20070809 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 543 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - LEFT CENTER SEAT TRACK NR 6 HAS LIGHT CORROSION AT STATION 543. REPAIRED IAW RD8-53-784 AND SRM 51-40-00, 51-4 0-11. 2 H 7 2 4T RT A13NM 2007082300072 20070823 00072 NM 2007 8 23 SWAA073984 1 20070809 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 603SW 27954 DURING SCHEDULED BRDG CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007082300079 20070823 00079 WP 2007 8 23 070143 1 20070808 A 3350 408822101 BATTERY PACK DOUG DC9 DC987 3022087 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 945MA 49725 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007082300080 20070823 00080 NM 2007 8 23 SWAA074001 1 20070810 A 5755 6573735 SPOILER BOEING 737 7373T5 1384608 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED 22Y CHECK, FOUND LEFT WING NR 1 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007082300085 20070823 00085 NM 2007 8 23 SWAA073976 1 20070809 A 5753 65C30462 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD FORE FLAP UPPER SURFACE DISBONDED AT OUTBOARD END. REPAIRED FORE FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007082300086 20070823 00086 EU 2007 8 23 07FDEA02926 1 20070816 A 5330 A53810775200 SKIN PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 CORROSION ON SKIN PANEL C54, P56-57 REPAIR PERFORMED BY BLEND OUT THE CORROSION IAW EA 6-5315-112494 AND RAS/053735/004/ 2007 ISS A. 2 L 7 2 4F RT A35EU 2007082300087 20070823 00087 EU 2007 8 23 07FDEA02927 1 20070816 A 5311 A53989388201 FRAME AIRBUS 300 A300B4605R 3930308 EU ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 CRACKED FRAME SEGMENT (A539-89388-201) ON C98 WITH CRACKED FIREWALL (P/N A539-89596-000). REPAIR PERFORMED BY REPLACEME NT OF DAMAGED PART ON FRAME SECTION C98 AT P10 AND DOUBLER INSTALLATION ON FIREWALL, APPROVED BY EA 6-5319-106510 AND RA S/DAHAM/4022477/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082300092 20070823 00092 EU 2007 8 23 07FDEA02932 1 20070816 A 5320 A53980669204 PROFILE AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 CORROSION ON STRINGER P56 LHM C76-77, REPAIR PERFORMED BY BLEND OUT THE CORROSION IAW SRM 51-74-10 AND OVERSIZING RIVET HOLES IAW EA 6-5318-106512 A AND RAS/DATLS/0003775/2007 ISS B. 2 L 7 2 4F RT A35EU 2007082300096 20070823 00096 NM 2007 8 23 SWAA073988 1 20070809 A 5313 BAC1498 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 1 CRACKED AT BS 344. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007082300101 20070823 00101 EU 2007 8 23 07FDEA02939 1 20070816 A 5313 A53833367202 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 CORROSION SPOT ON STRINGER P39 LT, C46-47 REPAIR PERFORMED BY BLEND OUT CORROSION TO SMOOTH CONTOUR IAW SRM 51-74-10, AP PROVED BY EA 6-5315-106536 AND RAS 052622/004/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082300105 20070823 00105 EU 2007 8 23 07FDEA02942 1 20070816 A 5320 A53832100 WEB AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 CENTER SECTION FOUND WEB CRACKS AT C47, TRACK 2 LT AND 2 RT REPAIR PERFORMED BY INSTALLING DOUBLER ON WEB IAW EA 6-5315- 112438 AND RAS 052577/010/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082300133 20070823 00133 NM 2007 8 23 DLM90071073 1 20070811 A 5310 DOOR FRAME DOUG MD90 MD9030 3023690 NM BS 685-757 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 MID PIT DOOR JAMB BEAM HAS CORROSION FROM FS 685 TO 757. REPAIRED MID PIT DOOR JAMB BEAM IAW MD80 SRM 53-05D. 2 L 7 2 4F RT A6WE 2007082300142 20070823 00142 NM 2007 8 23 DLM90071079 1 20070807 A 5313 LONGERON DOUG MD90 MD9030 3023690 NM BS 1364 L29L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 AFT PIT LONGERON 29L IS CORRODED AT STA 1364. REPLACED LONGERON 29L IAW MD90 SRM 51-30-05 AND 51-30-02. 2 L 7 2 4F RT A6WE 2007082300145 20070823 00145 NM 2007 8 23 CALA0700433 1 20070812 A 5311 BAC15171470 BELTFRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14609 27322 INSPECTION FOUND A .5 INCH CRACK IN BELT FRAME AT STA 400 BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04649. 2 L 7 2 4F RT A16WE 2007082300149 20070823 00149 NM 2007 8 23 HALA0700344 1 20070815 A 3397 POWER CABLE BOEING 767 76733A 1385209 NM EMERGENCY LIGHTS DAMAGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 581HA 28141 EMERGENCY LIGHTS AT 17-22AB AND MID LAV INOP. REMOVED AND REPLACED 2 EA EMERGENCY POWER CABLE PER HAL MM 33-51-00-032-0 01 HA MM 33-51-00-032-002. EMERGENCY LIGHTS TEST PER HA MM 33-51-00-715-001. EMERGENCY LIGHTS OPERATE NORMALLY. 2 L 7 2 4F RT A1NM 2007082300160 20070823 00160 NE 2007 8 23 QXEA200701336 2 20070817 A 7230 3045593 VALVE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE P3 MALFUNCTIONED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 348PH 484 SEA - ON FLIGHT 2010, BLUE HAZE AND MUSTY ODOR IN COCKPIT AFTER ENGINES START AND BLEEDS SELECT ON. MAINTENANCE REMOVED AND REPLACED P2.5/P3 VALVE. RAN ENGINES, NO SMOKE NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007082300188 20070823 00188 NM 2007 8 23 2007UALA03044 1 20070807 A 5230 STRUCTURE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 FUSELAGE DAMAGED BELOW BULK CARGO DOOR. 08-31-07 ACP'D MAT'L LOSS INSP USING ULTRASONIC THICKNESS TESTER ON REPAIRED SKIN DAMAGE BELOW BULK CARGO DOOR. BLENDED DAMAGED AREA. REPAIR OK PER EVA 70500 IS FAA APPROVED VIA FAA 8100-9 FORM. AIRCRAFT OK FOR RETURN TO SERVICE. SUSPECT DAMAGE DUE TO CONTACT BY GROUND SERVICE EQUIPMENT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082300190 20070823 00190 NM 2007 8 23 2007UALA03046 1 20070806 A 4990 SENSOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE OIL PRESSURE LEAKING A UALA O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 WP 29 785UA 26954 FOUND OIL LEAKING FROM COVER PLATE ABOVE OIL PRESSURE SENSOR AT APU LUBE CLUSTER, ALSO FOUND OIL LEAKING FROM GENERATOR FEEDER CABLES. FOUND GENERATOR SOAKED WITH OIL AND GENERATOR FEEDER CABLES ARCING AND BURNED. APU WAS FOUND LOW ON OIL . 08-31-07 REPLACED APU GENERATOR PER MM 24-21-01, REPLACED LUBE PRESSURE SENSOR O-RING, REPLACED BURNED GENERATOR FE EDER CABLE. OP CK OK, NO LEAKS NOTED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007082300191 20070823 00191 NM 2007 8 23 2007UALA03047 1 20070806 A 3397 CONNECTOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 785UA 26954 FIRST CLASS SEATS 1E, 1F, 2E AND 2F FWD AND AFT EMERGENCY LIGHT ASSEMBLIES ARE INOPERATIVE. 08-31-07 SECURED POWER JU MPER PLUGS AT SEAT 2E. EEL LIGHT ASSY TESTED OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007082300194 20070823 00194 EU 2007 8 23 2007UALA03051 1 20070806 A 3220 LANDING GEAR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NOSE VIBRATION A UALA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 WP 29 469UA 1409 NOSE GEAR VIBRATION ON TAKEOFF. 09-07-07 BOTH TIRES CHANGED AND GEAR LUBE PERFORMED. NO REPEATS SINCE AUG 6. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300201 20070823 00201 NM 2007 8 23 2007UALA03098 1 20070809 A 3510 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 556UA 26650 CAPTAINS OXYGEN MASK LEAKING OXYGEN CONTINUOUSLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082300217 20070823 00217 NM 2007 8 23 2007UALA03114 1 20070809 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 675UA 29243 SEAT 34AB EPL SEAT MOUNTED LIGHT IS INOPERATIVE. 08-31-07 REPLACED LIGHT ASSY PER MM 33-51-10 & OP CHECKED GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082300220 20070823 00220 NM 2007 8 23 2007UALA03117 1 20070813 A 3350 LAMP AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 833UA 1401 EEL AT SEAT ROW 16 ABC INOPERATIVE. REPLACED EMERGENCY LIGHT LAMP OPS CHECK OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300225 20070823 00225 EU 2007 8 23 2007UALA03122 1 20070812 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 469UA 1409 CABIN EMERGENCY LIGHT TEST FAIL. REPLACED POWER SUPPLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300226 20070823 00226 NM 2007 8 23 2007UALA03123 1 20070812 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN UNKNOWN A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 AFT CABIN DOOR EMERGENCY EXIT LIGHTS WILL NOT TURN OFF. NO FAULT FOUND. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082300227 20070823 00227 NM 2007 8 23 2007UALA03124 1 20070812 A 5753 REPAIR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU L/E SLAT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 910UA 25254 NR 4 SLAT HAS EXPOSED HONEYCOMB FROM A MISSING REPAIR, 5 INCHES BY 5.5 INCHES AT INBOARD TRAILING EDGE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082300232 20070823 00232 NM 2007 8 23 2007UALA03129 1 20070812 A 5241 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 FWD GALLEY DOOR LOWER FWD FRAME IS CRACKED AT 2 EA FASTENER HOLES. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082300236 20070823 00236 NM 2007 8 23 2007UALA03134 1 20070810 A 3510 OXYGEN MASK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 CAPTAINS OXYGEN MASK REGULATOR DAMAGED AND DOES NOT TEST PROPERLY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082300237 20070823 00237 NM 2007 8 23 2007UALA03135 1 20070812 A 3510 OXYGEN MASK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 FLIGHT DECK CREW'S FIRST OBSERVER'S OXYGEN MASK DAMAGED AND WILL NOT PASS TEST. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082300240 20070823 00240 NM 2007 8 23 2007UALA03138 1 20070811 A 3397 CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 351UA 24319 AFT CABIN EEL LIGHTS FROM ROW 15 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT ARE INOP . REPLACED CABLE FROM ROW 15 TO 21. ALL SYSTEMS CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082300241 20070823 00241 NM 2007 8 23 2007UALA03139 1 20070812 A 5210 POWER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR OUT OF ADJUST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 516UA 24860 NR 4R EMERGENCY POWER CABLE TRIGGER FAILED TEST. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082300242 20070823 00242 NM 2007 8 23 2007UALA03140 1 20070810 A 2611 SMOKE DETECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FWD CARGO BAY FAULTY A UALA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 29 520UA 24890 STATUS MSG: FWD CARGO DETECTOR 2. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082300243 20070823 00243 NM 2007 8 23 2007UALA03141 1 20070813 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 573UA 26685 THE FOLLOWING EMERGENCY LIGHTS ARE INOP: SLIDE LIGHT DOOR 4L, EXIT MARKERS DOORS 4L & 4R, EXIT SIGN OVER DOOR 4L, AFT G ALLEY EXIT SIGN, AISLE LIGHT ROW 32. REPLACED BATTERY PACK & CHARGER ASSEMBLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082300245 20070823 00245 NM 2007 8 23 2007UALA03143 1 20070810 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 586UA 26710 EXTERIOR EMERGENCY LIGHTS INOP AT DOORS 2L, 4L AND 4R. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082300246 20070823 00246 NM 2007 8 23 2007UALA03144 1 20070812 A 3397 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 661UA 27158 EMERGENCY LIGHT STRIP AT SEATS 14ABC INOPERATIVE. REPLACED FEEDER CABLE 2 L 7 2 4F 4 F RT A1NM E24NE 2007082300247 20070823 00247 NM 2007 8 23 2007UALA03145 1 20070812 A 3350 COVER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN MISSING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 671UA 30026 THE 1HJ EMERGENCY EXIT LIGHTING PLASTIC COVER MISSING. REPLACED LIGHT. TESTS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082300249 20070823 00249 NM 2007 8 23 2007UALA03147 1 20070811 A 5210 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR MISLOCATED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 DOOR 1R WAS HARD TO ARM. A CHORD WITH A HOOK IS ON THE GALLEY FLOOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082300250 20070823 00250 NM 2007 8 23 2007UALA03148 1 20070811 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 675UA 29243 EMERGENCY EXIT AND FLOOR LIGHTING AT 1R ON WITH COCKPIT SWITCH IN ARMED. REPLACED M1552 & M730 BATTERY PACKS. TEST OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082300255 20070823 00255 NM 2007 8 23 2007UALA03056 1 20070807 A 2750 FLAP SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TE FLAPS MALFUNCTIONED A UALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 WP 29 578UA 26694 FLAPS WILL NOT RETRACT OR EXTEND. INSPECTED FLAP AND LEADING EDGE FOR DAMAGE AND NO DEFECTS NOTED. OPERATIONAL CHECK WAS GOOD. REPLACED NR 1 FLAP SLAT ELECTRONIC UNIT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082300257 20070823 00257 EU 2007 8 23 2007UALA03058 1 20070806 A 3350 BULB AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 464UA 1290 FOUND EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. 09-07-07 REPLACED LAMP 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300259 20070823 00259 NM 2007 8 23 KCSA071299 1 20070814 A 5330 SKIN BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 FUSELAGE SKIN CORRODED AT BUTT SPLICE AT BS 2360, STR 34L TO STR 23L. 2 L 7 4 4F RT A20WE 2007082300260 20070823 00260 EA 2007 8 23 COMA0770041 1 20070809 A 3620 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA BLEED AIR SYS MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 690CA 10182 FLIGHT 5535 - RECEIVED LEFT BLEED DUCT WARNING IN FLIGHT. EXTINGUISHED AFTER 50 SECONDS. RECEIVED LEFT BLEED MESSAGE, BLEED DUCTS CLOSED RESULTING IN PRESSURIZATION LOSS. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. PERFORMED TEST OF BLEED LEAK DETECTION SYSTEM AND INSPECTED DUCTS FOR LEAKS. NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2007082300261 20070823 00261 EA 2007 8 23 COMA0770042 1 20070804 A 2916 9604501 RESERVOIR CNDAIR CL600 CL6002C10 1390015 EA HYDRAULIC SYS FAULTY A COMA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 SO 01 669CA 7566 10176 FLIGHT 5311 - HYD SYS NR 3B OVERHEAT CAUTION MESSAGE ILLUMINATED IN FLIGHT. AIRCRAFT RETURNED BACK TO CVG AND LANDED SA FELY. REMOVED AND REPLACED NR 3 HYD RESERVOIR. 2 L 7 2 4F RT A21EA 2007082300262 20070823 00262 NE 2007 8 23 COMA0760509 2 20070801 A 7261 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LT ENGINE LOW A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 709CA 7238 FLIGHT 5387 - DURING CLIMBOUT RECEIVED LEFT ENGINE LOW OIL PRESS WARNING MESSAGE. AIRCRAFT RETURNED BACK TO CID AND LAN DED SAFELY. INSPECTED LEFT ENGINE AND FOUND IT TO BE LOW ON OIL. SERVICED ENGINE AND PERFORMED GROUND RUNS. 2 L 7 2 4F 4 F RT A21EA E15NE 2007082300263 20070823 00263 EU 2007 8 23 2007UALA03059 1 20070806 A 3397 PIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CONNECTOR OUT OF POSITION A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 464UA 1290 FOUND EMERGENCY LIGHT AT SEAT 2B INOP. 09-07-07 PIN IS PUSHED BACK OUT OF CONNECTOR IN SEAT BOX. PUSHED PIN BACK IN TO CONNECTOR. OPS CHECK OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300265 20070823 00265 EU 2007 8 23 2007UALA03061 1 20070807 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN SMOKE A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 465UA 1341 RTFL WITH SMOKE REPORTED IN THE AFT CABIN AREA. 09-07-07 OIL LEAKING INTERNALLY IN APU PNEUMATIC SYSTEM. REPLACED AP U. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300267 20070823 00267 SO 2007 8 23 RAIA0708025 1 20070810 A 3150 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 831HK 145232 FLT 7941 - DEN - CREW REPORTED NR 2 ENGINE ATTCS NO MARGIN MESSAGE ON THE EICAS WHEN POWER EVER WAS ADVANCED. MAINTENAN CE PERFORMED A DOWNLOAD OF THE CMC AND FOUND NO DEFECTS OR RELATED MESSAGES, PERFORMED A GROUND PERFORMANCE RUN IN ALT T O AND TO 1 WITH NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2007082300269 20070823 00269 EU 2007 8 23 2007UALA03063 1 20070806 A 5300 CONTROL BOX AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO BAY LOOSE A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 440UA 702 RTFL DUE TO ENGINE VIBRATION SHORTLY AFTER TAKEOFF. 09-07-07 RESECURED LOB. VIBE SURVEY FLIGHT (TEST FLIGHT) PERFO RMED, NO VIBES NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300270 20070823 00270 NM 2007 8 23 2007UALA03064 1 20070807 A 5610 WINDOW BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 351UA 24319 RTFL DUE TO FIRST OFFICER'S SHATTERED WINDOW. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082300274 20070823 00274 EU 2007 8 23 2007UALA03069 1 20070808 A 3350 LAMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 464UA 1290 FOUND EMERGENCY LIGHT AT SEAT 21C INOP. RELAMPED, GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300275 20070823 00275 NM 2007 8 23 2007UALA03070 1 20070808 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHT INOP AT SEATS 4F AFT, 5F AFT, 3J AFT. REPLACED LIGHT ASSY. OP CKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082300277 20070823 00277 NM 2007 8 23 2007UALA03072 1 20070808 A 5320 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 290 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 FOUND PASSENGER CABIN STA 290 JUST BELOW STR 11R ANGLE CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKED ANGLE. REPL ACED WITH NEW ANGLE (REF SRM 51-40-02 PGS 1-2-6) 2 L 7 2 4F 4 F RT A16WE E2GL 2007082300278 20070823 00278 NM 2007 8 23 2007UALA03073 1 20070808 A 3350 362624 LAMP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 907UA 25007 FOUND EEL LAMP INOP ROW 10. REPLACED LAMP. CHKS OKAY. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082300284 20070823 00284 NM 2007 8 23 2007UALA03079 1 20070808 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 127UA 28813 FOUND EMERGENCY EEL LIGHT INOP AT SEAT 1J AFT AND SEAT 54 ABC. REPLACED LIGHT ASSY. OPS CKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082300285 20070823 00285 NM 2007 8 23 2007UALA03080 1 20070809 A 3350 80541 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 127UA 28813 EMERGENCY EEL LIGHT INOP AT DOOR 5L AFT LOWER WALL CROSS AISLE. REPLACED LIGHT ASSY. OPS CKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082300289 20070823 00289 NM 2007 8 23 07FDEA02929 1 20070816 A 2750 POWER UNIT BOEING 727 727233 138408A NM TE FLAPS FAILED A FDEA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 267FE 21673 ENGINE NR 1 AND NR 2 HYDRAULIC LIGHTS ILLUMINATED 22 MINUTES AFTER TAKEOFF, FOLLOWED BY OBSERVING "A" SYSTEM QTY ZERO. FL 260 AT THE TIME AND NO CONTROL INPUTS WERE BEING MADE. COMPLIED WITH QRH, DECLARED AN EMERGENCY AND HAD AN UNEVENTFU L LANDING. FOUND EVIDENCE OF LEAK AT OTBD FLAP POWER UNIT HYDRAULIC MOTOR. REMOVED MOTOR AND FOUND CONFIRMED FAILURE. SCREW HEADS POPPED AND PACKING PROTRUDING. REPLACED MOTOR PER AMM 27-51-062-4. NEEDS LEAK CHECK AFTER ENG PUMPS AND F ILTERS CHANGED. SEE MTSI 29-30/9628 FOR PARTS CHANGE INFO. 2 L 7 3 4F RT A3WE 2007082300293 20070823 00293 NM 2007 8 23 07FDEA02955 1 20070817 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM BS 1521 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 595FE 48553 FUSELAGE, LEFT EXTERIOR SURFACE LONGERON END CAP FITTING AT STA 1521 LONGERON 30L FOUND CRACKED. 08/31/07 REMOVED AS PER SRM 51-33-01 VOLUME II. NEW SPLICE END CAP FITTING FABRICATED AS PER DOUGLAS DRAWING AEA7643 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007082300295 20070823 00295 NM 2007 8 23 07FDEA02957 1 20070817 A 5710 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 LEFT WING, LEADING EDGE TELESCOPING DUCT CUTOUT OUTBOARD CORNER FOUND CRACK. 09-04-07 COMPLIED WITH FEDEX E.A. 1-57 10-115160, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007082300296 20070823 00296 NM 2007 8 23 07FDEA02958 1 20070817 A 5710 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 RIGHT WING, ANTI-ICE TELESCOPING DUCT DOOR CUTOUT CORNER FOUND CRACK. 09-04-07 COMPLIED WITH FEDEX EA 1-5710-115161, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007082300298 20070823 00298 NM 2007 8 23 07FDEA02960 1 20070817 A 5754 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 500 BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 LEFT WING, NR 3 LEADING EDGE SLAT OUTBOARD SUPPORT FITTING BROKEN. 09-04-07 REMOVED & REPLACED AS PER AMM 27-80-30. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-80-30, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007082300299 20070823 00299 NM 2007 8 23 07FDEA02961 1 20070817 A 5320 69205885 BRACKET BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 UNDERSIDE OF FRAME 294.5, LBL 10 BRACKET BROKEN BY PULLEYS FABRICATED NEW BRACKET ON UNDERSIDE OF FRAME 294.5, LBL 10, I AW DWG 69-20588 ID 001. TREATED AND PRIMED, INSTALLED IAW B727 SRM 51-10-2 AND 51-30-2. REPAIR IS CLASSIFIED AS MINO R. 2 L 7 3 4F RT A3WE 2007082300302 20070823 00302 EA 2007 8 23 QXEA200701333 1 20070815 A 3150 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA WARNING LIGHT A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 09 610QX 10033 SEA - FLIGHT 2185, GLD UNSAFE MESSAGE ILLUMINATED FOR ABOUT 5 SECONDS DURING THE TAKEOFF ROLL. ABORTED TAKEOFF AT ABOUT 50 KNOTS AND RETURNED TO THE GATE. MAINTENANCE CHECKED THE MDS AND FOUND NO FAULTS STORED. COMPLIED WITH FIM TASK 27- 64-00-810-803-A01. CHECKS GOOD AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007082300305 20070823 00305 EA 2007 8 23 QXEA200701273 1 20070809 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA CARGO DOOR FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 600QX 10005 SEA - AT FLIGHT LEVEL 34,000, AFT CARGO DOOR WARNING ILLUMINATED FOLLOWED BY A PROX SYSTEM 2 FAULT MESSAGE. MAINTENANCE INSPECTED THE DOOR AND SURROUND WITH NO DEFECTS NOTED. OPERATIONAL CHECK OF THE AFT CARGO DOOR GOOD. AIRCRAFT RETURNE D TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007082300306 20070823 00306 EA 2007 8 23 QXEA200701268 1 20070811 A 3150 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 609QX 10031 GEG - AFTER ENGINE START RECEIVED A AUTO FLOW INHIBIT AND XFLOW CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENANCE CYC LED THE FUEL SYSTEM CIRCUIT BREAKERS. SYSTEM OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED . 2 L 7 2 4F RT A21EA 2007082300308 20070823 00308 EU 2007 8 23 SIMA200723202 1 20070819 A 3350 74449 SIGN SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 393AE 18309 340B393 LEFT OVERWING EMERGENCY EXIT SIGN IS INOPERATIVE. REMOVED AND REPLACED EXIT SIGN IAW SAAB AMM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007082300309 20070823 00309 SO 2007 8 23 SIMA200723205 1 20070817 A 5347 13500412007 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 15794 5000 145312 RIGHT OUTBOARD SEAT TRACK BETWEEN FRAMES 53 AND 55 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082300312 20070823 00312 SO 2007 8 23 SIMA200723210 1 20070817 A 5347 14530659007 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 15794 5000 145312 LEFT INBOARD SEAT TRACK BETWEEN FRAMES 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082300315 20070823 00315 SO 2007 8 23 SIMA200723207 1 20070817 A 5347 13500438001 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 15794 5000 145312 RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 23 AND 34 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082300316 20070823 00316 SO 2007 8 23 SIMA200723212 1 20070817 A 5347 13500439003 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 15794 5000 145312 LEFT OUTBOARD SEAT TRACK BETWEEN FRAMES 23 AND 34 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082300319 20070823 00319 SO 2007 8 23 SIMA200723203 1 20070819 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 634AE 145150 BURNING ODOR NOTED IN CABIN. PERFORMED OPERATIONAL CHECKS IAW AMM WITH NO ODOR DETECTED. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007082300320 20070823 00320 SO 2007 8 23 SIMA200723204 1 20070817 A 5347 14532605017 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 15794 5000 145312 RIGHT OUTBOARD SEAT TRACK BETWEEN FRAMES 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082300321 20070823 00321 SO 2007 8 23 SIMA200723209 1 20070817 A 5347 13530658005 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 15794 5000 145312 RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 37 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082300322 20070823 00322 SO 2007 8 23 SIMA200723218 1 20070817 A 5347 14532606015 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 15794 5000 145312 RIGHT OUTBOARD SEAT TRACK BETWEEN FRAMES 23 AND 34 CORRODED, NICKED AND GOUGED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082300326 20070823 00326 SO 2007 8 23 SIMA200723220 1 20070816 A 5315 14521700007 FLOORBEAM EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 857AE 9662 145752 OMEGA BEAM CORRODED AT FRAME 20. REPAIRED OMEGA BEAM IAW EMB SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082300327 20070823 00327 SO 2007 8 23 SIMA200723221 1 20070817 A 5320 13500469403 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 15794 5000 145312 FLOOR SUPPORT BETWEEN FRAMES 22 AND 22A CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW EMB SRM 51-40-02. AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082300345 20070823 00345 NM 2007 8 23 SWAA074033 1 20070812 A 2170 1808494 COALESCER BAG BOEING 737 7375H4 138449D NM A/C BAY CONTAMINATED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 29 523SW 26565 AIRTURN BACK, ENCOUNTERED HYDRAULIC FLUID SMELL ON TAKEOFF. REMOVED AND REPLACED WATER SEPARATOR BAGS PER MM. 2 L 7 2 4F RT A16WE 2007082300346 20070823 00346 NM 2007 8 23 SWAA074025 1 20070813 A 3350 3071BPEGPL LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED C2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007082300347 20070823 00347 NM 2007 8 23 SWAA074031 1 20070813 A 5420 311A11102 LUG BOEING 737 7373H4 1384600 NM NR 2 PYLON CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED BRDG CHECK, FOUND NR 2 ENGINE STRUT UPPER LINK FORWARD LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 2007082300349 20070823 00349 2007 8 23 SWAA074021 4 20070813 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 740SW 29276 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007082300350 20070823 00350 NM 2007 8 23 SWAA074024 1 20070813 A 5712 6545445 RIB BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED SPV CHECK, FOUND LT WING RIB CRACKED AT STA 135.5. REPAIRED RIB PER ACO. 2 L 7 2 4F RT A16WE 2007082300351 20070823 00351 NM 2007 8 23 SWAA074007 1 20070811 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 801, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007082300354 20070823 00354 NM 2007 8 23 SWAA074028 1 20070813 A 5753 6546435238 FLAP BOEING 737 7373K2 13844BA NM RT WING WARPED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP WARPED AT OUTBOARD END. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2007082300355 20070823 00355 NM 2007 8 23 SWAA074017 1 20070812 A 2750 6573271 TORQUE TUBE BOEING 737 7373H4 1384600 NM T/E FLAP WORN A SWAA K NONE O OTHER AP APPROACH 1 SW 29 319SW 23340 FLAPS SETTING FROM 25 TO 30, FLAPS LOCKED OUT. REMOVED AND REPLACED RT FLAP TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007082300357 20070823 00357 NM 2007 8 23 SWAA074030 1 20070813 A 5315 BAC1509100046 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 748SW 29800 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 727D, LBL 17 TO RBL 13. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007082300361 20070823 00361 2007 8 23 SWAA074022 4 20070813 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 603SW 27954 DURING SCHEDULED BRDG CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007082300362 20070823 00362 NM 2007 8 23 KCSA071300 1 20070814 A 3350 LIGHT BOEING 747 7472B4B 138481B NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 710CK 21097 L-5 DOOR EMERGENCY LIGHT INOP STA 2260. 2 L 7 4 4F RT A20WE 2007082300364 20070823 00364 NM 2007 8 23 KCSA071302 1 20070815 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 CORROSION ON MAIN DECK SEAT TRACK AT RBL 12, BS 1690 TO 1830. 2 L 7 4 4F RT A20WE 2007082300366 20070823 00366 NM 2007 8 23 CALA0700437 1 20070815 A 3350 D71701100 BATTERY BOEING 737 737924 13848A1 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 72405 30122 THE EMERGENCY LIGHT BATTERY ABOVE AFT GALLEY A/C RIGHT WOULD ONLY HOLD CHARGE FOR 1 MINUTE. REMOVED AND REPLACED EMERGE NCY LIGHT BATTERY. CHECKS GOOD IAW AMM 33-51-06-960-805. 2 L 7 2 4F RT A16WE 2007082300367 20070823 00367 NM 2007 8 23 CALA0700438 1 20070814 A 3350 D71701100 BATTERY BOEING 737 737924 13848A1 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 72405 30122 THE EMERGENCY LIGHT BATTERY AT 21 DEF WOULD ONLY HOLD 4 MIN CHARGE. THE BATTERY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW AMM 33-51-06-960-805. 2 L 7 2 4F RT A16WE 2007082300370 20070823 00370 EU 2007 8 23 TRAX200701149 1 20070807 A 5753 BRACKET AEROSP ATR72 ATR72 EU T/E FLAP BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 RIGHT INBOARD FLAP BEAM RIB NR 5 1 OMEG BRACKET BROKEN. 2 H 7 2 4T RT 2007082300371 20070823 00371 EA 2007 8 23 TRAX200701151 1 20070809 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 839AS 7284 LEFT SIDE OF NLG AFT DOOR CUTOUT HAS CRACK IN FUSELAGE SKIN PROTRUDING OUT OF LEFT RADIUS. 08-30-07 REPAIRED IAW REO 601R-53-11-048. 2 L 7 2 4F RT A21EA 2007082300372 20070823 00372 EA 2007 8 23 TRAX200701152 1 20070809 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 839AS 7284 RIGHT SIDE OF NLG DOOR CUTOUT HAS CRACK IN FUSLELAGE SKIN PROTRUDING OUT OF RIGHT RADIUS. REPAIRED RT FUSELAGE SKIN R ADIUS AT FS 235 IAW BOMBARDIER REO 601R-53-11-048 2 L 7 2 4F RT A21EA 2007082300373 20070823 00373 EA 2007 8 23 TRAX200701156 1 20070811 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 874AS 7551 FWD FLOOR SUPPORT AT FS 280 HAS MINOR CORROSION. 2 L 7 2 4F RT A21EA 2007082300375 20070823 00375 EA 2007 8 23 TRAX200701159 1 20070811 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 839AS 7284 CREW ESCAPE HATCH MISSING EMERGENCY EXIT PUSH RELEASE TURN HANDLE TO OPEN PUSH EXIT IN PLACARD. 2 L 7 2 4F RT A21EA 2007082300376 20070823 00376 EA 2007 8 23 TRAX200701161 1 20070811 A 5210 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 839AS 7284 PAX DOOR INNER AFT FRAME FS 338.00 IS CRACKED AT LOWER END. REPAIRED IAW REO 601R-52-11-402. 2 L 7 2 4F RT A21EA 2007082300381 20070823 00381 NM 2007 8 23 KCSA071309 1 20070815 A 3350 LIGHT BOEING 747 7472B4B 138481B NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 710CK 21097 CEILING EMERGENCY LIGHT LEFT AT STA 560 IS INOP. 2 L 7 4 4F RT A20WE 2007082300382 20070823 00382 EA 2007 8 23 COMA0760511 1 20070802 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION CR CRUISE 1 SO 01 995CA 7229 FLIGHT 5178 - RECEIVED FLAPS FAIL CAUTION MESSAGE AT 18,000 FT. FLAPS FAILED AT 0 DEGREES. AIRCRAFT LANDED SAFELY. CO MPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007082300385 20070823 00385 EA 2007 8 23 COMA0760514 1 20070803 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 917CA 7017 FLIGHT 5080 - LEFT WING FORWARD EMERGENCY EXIT LIGHT INOP. TRANSFERRED TO DEFERRED LIST PER MEL 33-51-02-1. 2 L 7 2 4F RT A21EA 2007082300386 20070823 00386 EA 2007 8 23 COMA0760515 1 20070803 A 2750 1104SD100501 SHAFT CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP DAMAGED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 809CA 7366 FLIGHT 5051 - ON APPROACH TO JAN, FLAPS SELECTED TO 45 DEGREES, FLAPS FAIL CAUTION MESSAGE AT 30 DEGREES. AIRCRAFT LAND ED SAFELY. REMOVED AND REPLACED RIGHT SIDE NR 5 FLEX SHAFT. 2 L 7 2 4F RT A21EA 2007082300387 20070823 00387 EA 2007 8 23 COMA0760516 1 20070804 A 3350 362624 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 926CA 7027 FLIGHT 5387 - FLOOR EMERGENCY LIGHTS FOR ROWS 2, 3, 4 AND 5 ARE INOP. REMOVED AND REPLACED EMERGENCY FLOOR LIGHT STRIP FOR ROWS 2, 3, 4 AND 5. 2 L 7 2 4F RT A21EA 2007082300389 20070823 00389 NE 2007 8 23 COMA0760518 2 20070804 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 1 MALFUNCTIONED A COMA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 01 416CA 7450 FLIGHT 5141 - ON TAKEOFF ROLL, NR 1 ENGINE WOULD NOT ACCELERATE PAST 43 PERCENT. THE ITT WENT TO 500 DEGREES BUT NOT BE YOND. PERFORMED ENGINE GROUND RUNS. FOUND ENGINE TO RUN WITHIN LIMITS. 2 L 7 2 4F 4 F RT A21EA E15NE 2007082300391 20070823 00391 EA 2007 8 23 COMA0760520 1 20070806 A 3350 364911 PIN CNDAIR CL600 CL6002B19 1900309 EA CABIN DAMAGED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 595SW 7292 FLIGHT 5255 - OVERWING FLOOR EXIT LIGHTS (ORANGE BAR) ARE INOP. FOUND PIN ON ORANGE BAR DAMAGED. REMOVED DAMAGED STRIP AND INSTALLED SERVICEABLE STRIP. 2 L 7 2 4F RT A21EA 2007082400001 20070824 00001 WP 2007 8 24 NWAA072859946 1 20070816 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8926E 45863 TAIL CONE PATH LIGHTS INOP. REPLACED BATTERY PACK. OPERATION CHECKS GOOD. 2 L 7 2 4F A6WE 2007082400003 20070824 00003 NM 2007 8 24 WRLA2007082 1 20070814 A 5280 FRAME DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE GEAR DOOR CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 275WA 48631 DURING 3C+12A CHECK, EGAT MECHANIC FOUND RT CENTERLINE LANDING GEAR DOOR FORWARD FRAME EXISTING DOUBLER CRACK AT STA Y=1 378.225. 09-26-07 REPLACED THE CRACKED FRAME WITH NEW PART PER MD-11 SRM VOL.II 51-35-01 & 51-33-01 REV.40 2 L 7 3 4F 4 F RT A22WE E24NE 2007082400004 20070824 00004 NM 2007 8 24 WRLA2007084 1 20070814 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 275WA 48631 DURING 3C+12A CHECK, EGAT MECHANIC FOUND MAIN DECK SEAT TRACK CROWN WORN AT STA Y=625, X=75.25. REPAIRED IAW MD-11 SRM VOL.1 53-70-00 FIGURE 1 REV.40 2 L 7 3 4F 4 F RT A22WE E24NE 2007082400005 20070824 00005 SO 2007 8 24 LR7A07065 1 20070816 A 6120 582855 VALVE LKHEED 382 382G 526414U SO HAMSTD 54H 54H6091 NE NR 4 PROPELLER MALFUNCTIONED A LR7A E ENGINE SHUTDOWN O OTHER CL CLIMB 1 AL 03 405LC 1187 5025 DURING CLIMB, FLIGHT CREW REPORTED NR 4 PROPELLER OVERSPEED TO 106 PERCENT. ENGINE SHUT DOWN IAW PROCEDURES. MAINTENAN CE FOUND VALVE HOUSING MALFUNCTIONED AND REPLACED WITH SERVICABLE UNIT IAW LAC JOB CARD HN61135 . 2 H 7 4 4T A1SO 6 C P906 2007082300017 20070823 00017 NM 2007 8 23 ZZDA2007257 1 20070809 A 3244 3910797513 TIRE BOEING 717 717200 1383700 NM NR 3 BLOWN A ZZDA A UNSCHED LANDING E VIBRATION/BUFFET TO TAKEOFF 1 SO 37 959AT 55021 TIRE BLEW AT VR WITH ENG VIBE HIGH. REMOVED AND REPLACED NR 3 MLG TIRE. 2 L 7 2 4F TR A6WE 2007082300021 20070823 00021 EU 2007 8 23 07FDEA02919 1 20070815 A 5310 A53973085 BEAM AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 SEVERAL CORROSION SPOTS ON AFT CARGO DOOR SILL BEAM, OUT OF LIMIT IAW SRM 53-10-00. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10, SRM 53-17-18 FIG 207 AND DRAWING R539-70133-000. 2 L 7 2 4F RT A35EU 2007082300022 20070823 00022 EU 2007 8 23 07FDEA02920 1 20070815 A 5310 A53973100200 BEAM AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORROSION ON BULK CARGO DOOR SILL BEAM REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007082300023 20070823 00023 NM 2007 8 23 CALA0700418 1 20070810 A 5311 65C22908 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND FORWARD BAGGAGE BIN FRAME CORRODED AT STA 500B BETWEEN STRINGER 25R AND S26R. A SHEAR TIE REPAIR WAS I NSTALLED IAW SRM 53-00-07, REPAIR 7. 2 L 7 2 4F RT A16WE 2007082300053 20070823 00053 NM 2007 8 23 QXEA200701294 1 20070805 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 306 S23-24R DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - DENT IN FUSELAGE BELOW ICE SHIELD AT STATION X306 BETWEEN STRINGER 23R AND 24R. REPAIRED IAW RD8-53-9734. 2 H 7 2 4T RT A13NM 2007082300055 20070823 00055 NM 2007 8 23 QXEA200701295 1 20070805 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 336 S30-31L DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - DENT IN FUSELAGE SKIN, PROTRUDING OUTWARD AT STATION X336 BETWEEN STRINGER 30L AND 31L. REPAIRED IAW RD8-53-57 84. 2 H 7 2 4T RT A13NM 2007082300059 20070823 00059 NM 2007 8 23 QXEA200701285 1 20070809 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 543 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - SEAT TRACK RIGHT NR 9 HAS LIGHT CORROSION AT STATION 543. REPAIRED IAW RD8-53-4936 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2007082300061 20070823 00061 NM 2007 8 23 QXEA200701290 1 20070806 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 205 S30R DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - DENT IN FUSELAGE SKIN, PROTRUDING OUTWARD STATION X 205, STRINGER 30R. REPAIRED IAW RD8-53-5384 AND RD8-53-973 9. 2 H 7 2 4T RT A13NM 2007082300082 20070823 00082 NM 2007 8 23 SWAA074002 1 20070810 A 5755 6573735 SPOILER BOEING 737 7373T5 1384608 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED 22Y CHECK, FOUND LT WING 0 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007082300091 20070823 00091 EU 2007 8 23 07FDEA02931 1 20070816 A 5730 A57340088 SKIN AIRBUS 300 A300B4605R 3930308 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 RT WING LOWER SKIN RIB 20-21 AROUND MAGNETIC LEVEL INDICATOR CORROSION ON LOWER SKIN REPAIR PERFORMED BY BLEND OUT THE C OROSION IAW SRM 51-74-10, APPROVED BY EA 6-57820-112490 AND RAS/BAE/1005335/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082300095 20070823 00095 EU 2007 8 23 07FDEA02935 1 20070816 A 5754 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 OLD REPAIR ON SLAT NR 1 INBOARD EDGE WITHOUT ANY DOCUMENTATION REPAIR RENEWED IAW EA 6-5742-106524 AND RAS/FOK/148/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082300103 20070823 00103 EU 2007 8 23 07FDEA02940 1 20070816 A 5313 A53811367 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 CORROSION SPOT ON STRINGER P50 RT, C39-40 REPAIR PERFORMED BY BLEND OUT CORROSION TO SMOOTH CONTOUR IAW SRM 51-74-10, AP PROVED BY EA 6-5315-106536 AND RAS 052622/004/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082300107 20070823 00107 EU 2007 8 23 07FDEA02944 1 20070816 A 5340 A53973612204 ATTACH FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CRACK IN ATTACHMENT FITTING FOR CROSSBEAM C62. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007082300109 20070823 00109 EU 2007 8 23 07FDEA02946 1 20070816 A 5711 A57110431200 SPAR AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CRACKS FOUND ON CENTER SPAR WEB AND DOUBLER C44 (AROUND HOLE 1 (LT) ,5 (LT) , 8 (RT)) REPAIR PERFORMED BY REAM UP UNTIL CRACK REMOVAL AND DOUBLER CUT-OUT IAW SB A300-53-242, APPROVED BY EA 6-5710-112510 AND RAS 053726/005/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082300119 20070823 00119 NM 2007 8 23 QXEA200701302 1 20070810 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - FS X546, Z111.5, Y11L. THERE IS A CORRODED N/P ON OUTBOARD SIDE OF TRACK. REPAIRED IAW RD8-53-9753, SRM 51-20- 36, 51-40-11, AND 51-20-16. 2 H 7 2 4T RT A13NM 2007082300129 20070823 00129 NM 2007 8 23 QXEA200701335 1 20070816 A 2120 UNKNOWN DHAV DHC8 DHC8202 2809007 NM CABIN SMOKE A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 368PH 512 PDX FLIGHT NR 2187, AFTER AND DURING ENGINE START FLIGHT DECK CREW NOTICED BLUE HAZE (SMOKE) ON FLIGHT DECK (FO TURNED B LEEDS OFF, HAD A TAIL WIND ON 10-15 KNOTS). DURING TAXI WITH BLEEDS ON SITUATION SEEMED NORMAL. DURING FLIGHT IDLE DES CENT CREW COULD SMELL AN ABNORMAL SOMETHING, PASSENGERS COULD TOO. COMPLIED WITH PWC TROUBLESHOOTING GUIDE 72-00-01, NO DEFECTS NOTED. CYCLED BLEEDS OFF/ON AT VARIOUS POWER SETTINGS, CHECKED OIL LEVEL FOR CORRECT SERVICE LEVEL. NO DEFECT S NOTED. ALL PARAMETERS OPERATIONAL CHECK GOOD. NO SMELL OF VAPOR FROM AIR DUCTS. NO PARTS REPLACED. AIRCRAFT RETURN ED TO SERVICE. 2 H 7 2 4T RT A13NM 2007082300130 20070823 00130 EU 2007 8 23 SA07051 1 20070813 A 3350 32145510 EPSU AIRBUS A321 A321211 3930370 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 183UW 1539 LAX - THE 3L DOOR EXIT SIGN APPEARED INOPERATIVE. MAINTENANCE REPLACED THE RIGHT SIDE, MID-CABIN EMERGENCY POWER SUPPLY UNIT, FIN 14WL. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007082300134 20070823 00134 NM 2007 8 23 DLM90071074 1 20070809 A 5347 593054768 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 1150-1364 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 CABIN SEAT TRACK RBL 24 OUT OF LIMITS MULTIPLE AREAS FS 1150-1364 (REF 1002862 2700-0062). REPAIRED SEAT TRACK IAW MD-9 0 SRM 53-40-01 FIG 6 VOL I. 2 L 7 2 4F RT A6WE 2007082300144 20070823 00144 NM 2007 8 23 CALA0700432 1 20070813 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14609 27322 INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 867 BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04649. 2 L 7 2 4F RT A16WE 2007082300155 20070823 00155 EA 2007 8 23 SIMA200722703 1 20070814 A 2613 6007300 OVERHEAT SENSOR CNDAIR CL600 CL6002C10 1390015 EA ZONE 700 FAILED A SIMA B A EMER. DESCENT UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 514AE 10119 "SUP" BRAKE OVERTEMP MESSAGE IN FLIGHT, DECLARED EMERGENCY. DIVERTED TO BNA. REMOVED AND REPLACED RIGHT OUTBOARD BRAKE TEMPERATURE SENSOR IAW CRJ AMM 32-46-01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007082300176 20070823 00176 EU 2007 8 23 AWXA200700998 1 20070814 A 3350 AD321430 BATTERY PACK AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS FAULTY A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 656AW 1079 MCN - EEL - BC-6 CHECK - LT MID CABIN EMERGENCY LIGHT BATTERY PACK FAULT. REPLACED LT MID CABIN EMERGENCY LIGHT BATTERY PACK IAW/ A320 AMM 33-51-38 AND OPERATIONAL CHECK GOOD I/A/W A320 AMM 33-51-00-710-00. 2 L 7 2 4F RT A28NM 2007082300178 20070823 00178 EU 2007 8 23 AWXA200701000 1 20070804 A 5320 D5347575800090 SILL AIRBUS 320 A320232 3930326 EU ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 656AW 1079 MCN - MAJOR REPAIR - BC-6 CHECK - NR 5984021, CORROSION FOUND ON BULK CARGO DOOR SILL BS 2830 / FR 60 - BS 2936 / FR 62, -Y685.8, -Z1219.2. REPLACED BULK CARGO DOOR SILL BS 2830 / FR 60 - BS 2936 / FR 62, -Y685.8, -Z1219.2 IAW A320 SRM 53- 41-49, FIG 202. 2 L 7 2 4F RT A28NM 2007082300182 20070823 00182 NM 2007 8 23 2007UALA03038 1 20070805 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 FOUND UPPER DECK CEILING EMERGENCY LIGHT IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082300184 20070823 00184 NM 2007 8 23 2007UALA03040 1 20070804 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 FOUND CEILING EMERGENCY LIGHTS INOP AT ROWS 12 AND 16. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082300198 20070823 00198 NM 2007 8 23 2007UALA03095 1 20070809 A 2621 FIRE BOTTLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FWD LAVATORY DISCHARGED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 809UA 825 FWD LAV GARBAGE CAN FIRE EXTINGUISHER BOTTLE EMPTY. 09-07-07 REPLACED FIRE BOTTLE 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300216 20070823 00216 NM 2007 8 23 2007UALA03113 1 20070809 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE AFT GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 675UA 29243 AFT GALLEY EEL LIGHT BAR INOPERATIVE. 08-31-07 REPAIRED AND REINSTALLED LIGHT BAR. OP CHECKS GOOD PER MM 33-51-10 . AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082300229 20070823 00229 NM 2007 8 23 2007UALA03126 1 20070811 A 3350 58674 INVERTER BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 906UA 25006 THREE SEGMENTS OF EEL LIGHTS INOP AFT CABIN AFT GALLEY. REPLACED INVERTER. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082300233 20070823 00233 2007 8 23 2007UALA03130 4 20070812 A 2565 PIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT GALLEY DOOR MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 AFT GALLEY DOOR HAS MISSING SLIDE PIN NEAR GIRT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082300234 20070823 00234 2007 8 23 2007UALA03132 4 20070812 A 2565 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C 13802 EU L1 DOOR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 304UA 23665 DOOR 1L SLIDE PACK FELL OUT OF HOLDER WHEN DOOR WAS OPENED. SLIDE DID NOT DEPLOY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082300238 20070823 00238 NM 2007 8 23 2007UALA03136 1 20070811 A 3510 OXYGEN MASK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 CAPTAIN'S OXYGEN MASK RUNS CONTINUOUSLY IN RESET TEST. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082300244 20070823 00244 NM 2007 8 23 2007UALA03142 1 20070810 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 586UA 26710 EEL LIGHTS INOP FROM ROW 9 - ROW 12. RECONNECTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082300254 20070823 00254 NM 2007 8 23 KCSA071297 1 20070814 A 5534 WEB BOEING 747 7472B4B 138481B NM VERTICAL STAB CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 VERTICAL STAB HORZ WEB AT FIN STA 562 HAS 1 INCH CRACK AT 5TH FASTENER FROM REAR SPAR. 2 L 7 4 4F RT A20WE 2007082300256 20070823 00256 NM 2007 8 23 2007UALA03057 1 20070807 A 3350 SIGN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 848UA 1647 FOUND EMERGENCY EXIT SIGN JUST FWD OF DOOR 1R BROKEN UNSECURE. 09-07-07 REPAIRED/REPLACED HARDWARE, EXIT SIGN RESECUR ED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300266 20070823 00266 EA 2007 8 23 COMA0760510 1 20070801 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 809CA 7366 FLIGHT 5367 - FLAP FAIL CAUTION MESSAGE. AIRCRAFT LANDED SAFELY ON SECOND APPROACH. COMPLIED WITH AD 2006-12-21 FLAP C AUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHE R FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007082300273 20070823 00273 EU 2007 8 23 2007UALA03068 1 20070807 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 427UA 512 FOUND EMERGENCY LIGHTS AT SEAT ROWS 7, 8, 24, 25, 26 ABC INOP. 09-07-07 REPAIRED WIRE AND REPLACED SOCKET IN CONNECTO R. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300276 20070823 00276 NM 2007 8 23 2007UALA03071 1 20070808 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 616 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 FOUND OVERWING FRAME INNER CHORD IS CRACKED AT BS 616L, JUST BELOW STR 17. MAJOR REPAIR ACCOMPLISHED: REPAIRED FRAME IN NER CHORD AT STA 616L BELOW S17L WITH STIFFENER ANGLE AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082300281 20070823 00281 NM 2007 8 23 2007UALA03076 1 20070808 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 FOUND EEL LIGHT IN INOP BY FWD COAT CLOSET IN FIRST CLASS. REPLACED LIGHT. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082300287 20070823 00287 EU 2007 8 23 2007UALA03082 1 20070808 A 2700 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 452UA 955 FLIGHT LOST 1 AND 2 FAC ON TAKEOFF. CREW RAN ECAM AND BOTH CAME BACK. UNABLE TO DUPLICATE PROBLEM SINCE FIRST REPORT. NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300288 20070823 00288 EU 2007 8 23 2007UALA03083 1 20070808 A 5101 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE VIBRATION A UALA O OTHER E VIBRATION/BUFFET CR CRUISE 1 WP 29 482UA 1584 ACFT FLOWN AT 250 KTS/LWR ALTS TO REDUCE AIRFRAME VIBRATIONS EXPERIENCED AT HIGHER SPEEDS. 09-07-07 CHECKED ALL ACCES S PANEL DOORS FOR FIT AND FAIR, NOTHING NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300291 20070823 00291 EU 2007 8 23 07FDEA02953 1 20070816 A 5315 102519ITL FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 FWD PIT CORRODED ON FLOORBEAM LATERAL ANGLE AT FR 38 UNDER ROLLER TRAY, RBL 28R TO 34R REMOVED CORRODED PART, FABBED REP AIR PARTS AND INSTALLED REPAIR ANGLE PER A310-200 SRM 51-74-10 PARA 6B, 53-14-15 FIG 41, 51-31-20 FIG 17, 53-10-15. 2 L 7 2 4F RT A35EU 2007082300292 20070823 00292 WP 2007 8 23 07FDEA02954 1 20070816 A 5522 SKIN DOUG MD10 MD1010F 3022112 WP RT ELEVATOR ACTIVATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 399FE 48262 RT INBD ELEV LOWER SURFACE PUNCTURED APPROX 5 ' FROM INBD END AND 1' FROM L/E DOT N5102 RPAIRED RT INBOARD ELEVATOR LOWE R SURFACE IAW DC/MD 10-10 SRM 55-00-01 VOL 1 PG 9. 2 L 7 3 4F RT A22WE 2007082300297 20070823 00297 WP 2007 8 23 07FDEA02959 1 20070817 A 5320 AJC736311 ANGLE DOUG DC10 DC1010 3022110 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 AFT CARGO COMPT AT STA 1997.750 L NR 52 CRACK 1" ON CAP ANGLE REPAIR IAW SRM 53-00-01 VOL 1 FIG 8. 2 L 7 3 4F A22WE 2007082300301 20070823 00301 NM 2007 8 23 07FDEA02963 1 20070817 A 5414 311N500296 SKIN BOEING 757 7572B7 1384964 NM NR 2 NACELLE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 NR 2 STRUT, RT SIDE, SIDE SKIN AT APPROXIMATELY NAC STA 144 INTERNAL, IS CORRODED ON SKIN AND UNDER LOWER FRAME/CHORD. REMOVED CORROSION FROM INTERNAL SKIN AS MARKED PER SRM 54-50-01. ORIGINAL SKIN THICKNESS (DOUBLER SIDE) .090", AFTER REWORK .075" AT LOWEST POINT AT NAC STA 144. NO CRACKS NOTED PER EA F-5450- 110760. MATERIAL REMAINING IS ACCEPTABLE PER EA F-5450-110760. NO FOLLOW UP ACTIONS ARE IMPOSED BY EA F-5450-110760. 2 L 7 2 4F RT A2NM 2007082300310 20070823 00310 SO 2007 8 23 SIMA200723206 1 20070817 A 5347 145320605015 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 15794 5000 145312 RIGHT OUTBOARD SEAT TRACK BETWEEN FRAMES 34 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082300313 20070823 00313 SO 2007 8 23 SIMA200723215 1 20070817 A 5347 14530659005 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 15794 5000 145312 LEFT INBOARD SEAT TRACK BETWEEN FRAMES 34 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082300314 20070823 00314 SO 2007 8 23 SIMA200723211 1 20070817 A 5347 14532606015 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 15794 5000 145312 LEFT OUTBOARD SEAT TRACK BETWEEN FRAMES 34 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082300328 20070823 00328 EU 2007 8 23 TRBA2007068 1 20070819 A 3350 7012210 LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS INTERMITTENT A TRBA O OTHER O OTHER NR NOT REPORTED 1 SO 29 342AT 345 FOUND MAIN ENTRY DOOR EMERGENCY LIGHT INOP. ADJUSTED MAIN ENTRY DOOR EMERGENCY LIGHT AS PER MM 33-50-00. 2 H 7 2 4T RT A53EU 2007082300329 20070823 00329 NM 2007 8 23 QXEA200701309 1 20070809 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT WING TE FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - LEFT WING NR 2 FLAP TRACK, UPPER SURFACE OF UPPER TRACK HAS PITTING. REPAIRED IAW RD8-57-986. 2 H 7 2 4T RT A13NM 2007082300330 20070823 00330 SO 2007 8 23 RAIA00708026 1 20070811 A 3260 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO MLG OUT OF ADJUST A RAIA O OTHER J WARNING INDICATION DE DESCENT 1 CE 03 838HK 145321 FLT 7947 - STL - LG AIR/GND FAIL MESSAGE ON THE EICAS. MAINTENANCE ADJUSTED THE MLG WOW SWITCHES AND PERFORMED AN OPS C HECK OF THE LANDING GEAR SYSTEM. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007082300337 20070823 00337 EA 2007 8 23 TRAX200701118 1 20070806 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 755EV 10185 LEFT FS 280 CROSSBEAM CRACKED ON UPPER FLANGE O/B OF LBL 9.0. REMOVED LEFT FS 280 DAMAGED BEAM. LOCATED NEW LEFT FS 28 0 FLOORBEAM, P/N CC670-304175-7, IAW CRJ SRM 51-42-21. OK TO INSTALL. INSTALLED LEFT FS 280 BEAM, IAW CRJ SRM 51-42-06 AND 51-42-21. OK TO TOPCOAT. PAINTED, IAW CRJ SRM 51-25-16. SUPPLEMENTAL - SDR CLOSED 08/14/07. 2 L 7 2 4F RT A21EA 2007082300343 20070823 00343 NM 2007 8 23 SWAA074027 1 20070813 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 734SA 27866 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 986.5, LBL 35. REPAIRED FLOORBEAM CHORD PER ER. 2 L 7 2 4F RT A16WE 2007082300356 20070823 00356 NM 2007 8 23 SWAA074016 1 20070812 A 5314 65C38502 KEELBEAM BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED 22Y CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 500D AND BS 545. REMOVED AND REPLACED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2007082300359 20070823 00359 2007 8 23 SWAA074018 4 20070813 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007082300363 20070823 00363 NM 2007 8 23 KCSA071301 1 20070814 A 3350 LIGHT BOEING 747 7472B4B 138481B NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 710CK 21097 UPPER DECK EGRESS/ESCAPE DOOR EMERGENCY LIGHTS INOP. 2 L 7 4 4F RT A20WE 2007082300368 20070823 00368 NM 2007 8 23 CALA0700439 1 20070814 A 3320 05939108 BALLAST BOEING 757 757224 1384958 NM CABIN MALFUNCTIONED A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14120 27562 SMOKE WITH AN ELECTRICAL ODOR WAS NOTED BY F/A'S IN AREA OF MID GALLEY WHILE AT CRUISE PORTION OF FLIGHT. BOTH UTILITY BUSSES WERE DEACTIVATED AND THE SMOKE STOPPED. THE FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEM. MAINTENANCE INSPECTED THE MID GALLEY AREA PER AMM 05-51-58 AND FOUND AN OVERHEAD FLUORESCENT LIGHT BALLAST HOT. THE BALLAST WAS REMOVED AND REPLACED. 2 L 7 2 4F RT A2NM 2007082300369 20070823 00369 NM 2007 8 23 KCSA071304 1 20070815 A 5330 SKIN BOEING 747 7472B4B 138481B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 FUSELAGE SKIN DAMAGED AT BS 2300, STR 15L. 2 L 7 4 4F RT A20WE 2007082300374 20070823 00374 EA 2007 8 23 TRAX200701158 1 20070811 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 839AS 7284 ANGLE IS CRACKED AT FS 484 O/B OF RBL 27. 2 L 7 2 4F RT A21EA 2007082300377 20070823 00377 NM 2007 8 23 KCSA071305 1 20070815 A 5330 SKIN BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 INNER SKIN HAS CORROSION AT STA 2200 BETWEEN STR 41R TO 46R. 2 L 7 4 4F RT A20WE 2007082300390 20070823 00390 EA 2007 8 23 COMA0760519 1 20070805 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 809CA 14547 7366 FLIGHT 5460 - ON APPROACH INTO CVG, RECEIVED FLAPS FAIL CAUTION MESSAGE WITH FLAPS SELECTED TO 30 DEGREES. FLAPS FAILED AT 20 DEGREES. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED LEFT BPSU. 2 L 7 2 4F RT A21EA 2007082400002 20070824 00002 NE 2007 8 24 NWAA072866717 2 20070816 A 7200 ENGINE BOEING 747 747251F 1384898 NM PWA JT9 JT9D7J 52054 NE NR 3 FLAMED OUT A NWAA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 01 617US 21121 662715 DURING CRUISE, THE NR 3 ENGINE FLAMED OUT. APPROXIMATELY 60 SECONDS AFTER THE FLAME-OUT, THE NR 3 ENGINE FUEL ICING LIG HT ILLUMINATED. THE COM PROCEDURE WAS FOLLOWED AND THE ENGINE WAS RESTARTED AT FL380. THE FLIGHT CONTINUED TO NRT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SUMPED THE NR 3 MAIN FUEL TANK AND REPLACED THE FUEL FILTER. NO WATER OR CONTAMINATION WAS NOTED. THE FUEL FILTER DIFFERENTIAL PRESSURE SWITCH WAS REPLACED. 2 L 7 4 4F 4 F A20WE E20EA 2007082400006 20070824 00006 NM 2007 8 24 WRLA2007083 1 20070814 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 275WA 48631 DURING 3C+12A CHECK, EGAT MECHANIC FOUND MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN WORN AT STA Y=585, X=27.50. REPA IR IAW MD-11 SRM VOL.1 53-70-00 FIGURE 1 REV.40. 2 L 7 3 4F 4 F RT A22WE E24NE 2007082400007 20070824 00007 SO 2007 8 24 C2XA07TY043 1 20070815 A 5544 12007254005 BUSHING EMB 145 EMB145LR 3260212 SO RUDDER WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14993 145289 TYS DURING A CURRENT 2C INSPECTION THE MIDDLE BUSHION ON THE RUDDER 2 WAS FOUND WORN. MAINTENANCE REMOVED AND REPLACED THE BRACKET WITH A NEW BUSHION IAW EMB 135/145 SRM 51-40-02 AND EC 5540-01028. ALL WORK WAS ACCOMPLISHED AND WILL BE RE LEASED AT THE END OF THE C-CHECK. 2 L 7 2 4T RT T00011AT 2007082400009 20070824 00009 EA 2007 8 24 COMA0760521 1 20070806 A 2752 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 809CA 26260 7366 FLIGHT 5461 - FLAPS FAIL MESSAGE AT 30 DEGREES WHEN SELECTED TO 45 DEGREES. REMOVED AND REPLACED FLAP SYS PDU. 2 L 7 2 4F RT A21EA 2007082400011 20070824 00011 SO 2007 8 24 RAIA00708030 1 20070814 A 3260 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO LANDING GEAR DIRTY A RAIA B A EMER. DESCENT UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 810HK 145231 FLT 7981 - ROA - LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE EICAS AFTER TAKEOFF AND LANDING GEAR LEVER WOULD NOT MOVE U P WITHOUT USING THE DOWN LOCK RELEASE BUTTON. MAINTENANCE INSPECTED AND CLEANED DEBRIS FROM THE LANDING GEAR PROXIMITY SWITCHES. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007082400013 20070824 00013 NM 2007 8 24 QXEA200701317 1 20070809 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 4 FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - RIGHT NR 4 FLAP TRACK BOTTOM SURFACE OF LOWER INBOARD RAIL IS PITTED. REPAIRED IAW RD8-57-988. 2 H 7 2 4T RT A13NM 2007082400018 20070824 00018 NM 2007 8 24 QXEA200701319 1 20070809 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 4 FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - RIGHT NR 4 FLAP TRACK OUTBOARD SIDE OF VERTICAL RAIL IS PITTED. REPAIRED IAW RD8-57-988. 2 H 7 2 4T RT A13NM 2007082400021 20070824 00021 NM 2007 8 24 QXEA200701320 1 20070809 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 4 FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - RIGHT NR 4 FLAP TRACK TOP SURFACE OF LOWER INBOARD RAIL IS PITTED. REPAIRED IAW RD8-57-988. 2 H 7 2 4T RT A13NM 2007082400023 20070824 00023 NM 2007 8 24 QXEA200701321 1 20070809 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 4 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - RIGHT NR 4 FLAP TRACK TOP RAIL IS PITTED. REPAIRED IAW RD8-57-988. 2 H 7 2 4T RT A13NM 2007082400024 20070824 00024 NM 2007 8 24 QXEA200701322 1 20070809 A 5755 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 5 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - RIGHT NR 5 FLAP TRACK TOP RAIL IS PITTED. REPAIRED IAW RD8-57-988. 2 H 7 2 4T RT A13NM 2007082400025 20070824 00025 NM 2007 8 24 QXEA200701323 1 20070806 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 5 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - RIGHT NR 5 FLAP TRACK VERTICAL OUTBOARD RAIL IS PITTED. REPAIRED IAW RD8-57-988. 2 H 7 2 4T RT A13NM 2007082400026 20070824 00026 NM 2007 8 24 QXEA200701324 1 20070809 A 5755 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 5 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - RIGHT NR 5 FLAP TRACK LOWER SURFACE OF INBOARD UPPER RAIL IS PITTED. REPAIRED IAW RD8-57-989. 2 H 7 2 4T RT A13NM 2007082400027 20070824 00027 NM 2007 8 24 QXEA200701325 1 20070809 A 5340 ATTACH FITTING DHAV DHC8 DHC8202 2809007 NM BS 429 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - CLEAT AT STRINGER 23P AT STATION X429 HAS A MISDRILLED HOLE THRU COUNTERSINK. REPAIRED IAW RD8-53-9747. 2 H 7 2 4T RT A13NM 2007082400028 20070824 00028 2007 8 24 QXEA200701338 4 20070816 A 3420 IRS BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 416QX 4083 SEA FLIGHT NR 2419: IRS ALIGN FAULT AFTER ATTEMPTING ALIGNMENT. RECEIVED CPU PMC MESSAGE. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE PERFORMED IRS OPS TEST. CHECKS GOOD IAW Q400 TAC 6343508. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVIC E. 2 H 7 2 4T RT A13NM 2007082400029 20070824 00029 EU 2007 8 24 TRAX200701112 1 20070804 A 5320 INTERCOSTAL AEROSP ATR72 ATR72 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 IN RIGHT MLG CLIP AT INTERCOSTAL FOUND CRACKED AT RBL 23. REMOVED CLIP OF INTERCOSTAL AS PER SRM 51-25-04, FABRICATION IS TRANSFERRED ON W/C 2000-160. REINSTALLED CLIP OF INTERCOSTAL AS PER SRM 51-25-04 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SP663 AND FAR 43 APPENDIX A REPAIR ACCOMPLISHED IAW SRM 51-25-04. SUPPLEMENTAL - SDR CLOSED 08/16/07. 2 H 7 2 4T RT 2007082400031 20070824 00031 NM 2007 8 24 QXEA200701340 1 20070815 A 2730 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM ELEVATOR FALSE ACTIVATION A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 420QX 4147 PDX FLIGHT NR 2364: ELEVATOR ASYMMETRY CAUTION. C/W CHECK LIST. CAUTION LIGHT OUT AT TOUCHDOWN. MAINTENANCE TROUBLE S HOT PER Q400 FIM TASK 27-30-00-810-801 AND COULD NOT CONFIRM FAULTS. PUSHED ON ELEVATOR WHILE PERFORMING THE OPERATIONA L CHECK TO SIMULATED WIND SPEED. NO DEFECTS NOTED. OPS CHECK GOOD. CAUTION LIGHT DID NOT RETURN. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007082400036 20070824 00036 EA 2007 8 24 TRAX200701168 1 20070811 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 839AS 7284 ANGLE IS CRACKED AT FS 484 O/B OF LBL 27. 2 L 7 2 4F RT A21EA 2007082400037 20070824 00037 NM 2007 8 24 HALA0700348 1 20070818 A 5210 SKIN BOEING 717 717200 1383700 NM PAX DOOR CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 485HA 55130 MAIN DOOR LATCH ON, FUSELAGE, SKIN DAMAGE DURING OPENING OF MAIN DOOR. JETTWAY CAUGHT THE DOOR. FERRY FLIGHT REQUIRED, THIS AIRCRAFT HAS BEEN INSPECTED THIS DATE AND IS SAFE FOR THE INTENDED FLIGHT. BLEND SKIN DAMAGE L 1.5" D .3" MIN 2D E.D. TO NEAREST FASTENERS OF BLENDOUT. EDDY CURRENT TO ENSURE CRACK REMOVED, SEALED AREA. PROTECT, PRIMED AND PAINTED. HAL M105 PENDL. OK PER HAL M-105 FILE NR 405092. 2 L 7 2 4F TR A6WE 2007082400038 20070824 00038 EU 2007 8 24 AWXA200701002 1 20070804 A 5320 D53421124200 SHEAR PLATE AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 632AW 81 SAL - MAJOR REPAIR - C-7 CHECK - NR 5963561, CORROSION ON CABIN SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70, +Y1732. REPLACED CABIN SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70, +Y1732 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007082400039 20070824 00039 EA 2007 8 24 TRAX200701169 1 20070811 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 839AS 7284 ANGLE IS CRACKED AT FS 484 O/B OF RBL 9. 2 L 7 2 4F RT A21EA 2007082400041 20070824 00041 EU 2007 8 24 AWXA200701004 1 20070804 A 5321 D5367180500300 FLOORBOARD AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 632AW 81 SAL - MAJOR REPAIR - C7 CHECK - NR 5980302, CORROSION ON CABIN FLOORBOARD 262FF, BS 3158 / FR 66 - BS 3257 /FR 68, -Y129 2. REPLACED CABIN FLOORBOARD 262FF, BS 3158 / FR 66 - BS 3257 /FR 68, -Y1292 IAW AWA TASK CARD C1D25318. 2 L 7 2 4F RT A28NM 2007082400042 20070824 00042 EA 2007 8 24 TRAX200701173 1 20070812 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 874AS 7551 CORROSION ON THE FS 349 TRANSVERSE BEAM NEXT TO SERVICE DOOR ENTRANCE. 2 L 7 2 4F RT A21EA 2007082400043 20070824 00043 EU 2007 8 24 AWXA200701005 1 20070725 A 5544 D5537131800400 HINGE FITTING AIRBUS 320 A320231 3930325 EU ZONE 300 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 SAL - MAJOR REPAIR - C-06 CHECK - NR 5964976, THE NR 7 RUDDER HINGE FITTING HAS EXCESSIVE PLAY, RUDDER STATION 5605 / RI B 11. REPLACED THE NR 7 RUDDER HINGE FITTING, RUDDER STATION 5605 / RIB 11 IAW A320 AMM 27-21-41. 2 L 7 2 4F RT A28NM 2007082400044 20070824 00044 EA 2007 8 24 TRAX200701176 1 20070812 A 3350 COVER CNDAIR CL600 CL6002C10 1390015 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 EXIT SIGN COVER MISSING FROM F/A GALLEY AREA NEAR FLOOR. 2 L 7 2 4F RT A21EA 2007082400045 20070824 00045 EU 2007 8 24 07FDEA02828 1 20070811 A 5315 A53974339204 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 ALC, FR 64, T-CAP CORRODED, BL 36R. (-Y910) REMOVED AND REPLACED T-CAP SECTION IAW A310-200 SRM 51-21-10 AND 53-10-15. 2 L 7 2 4F RT A35EU 2007082400046 20070824 00046 WP 2007 8 24 07FDEA02967 1 20070818 A 5340 AFA71321 FITTING DOUG DC10 DC1030 3023501 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 318FE 46837 NR 3 MAIN CARGO DOOR JAMB SUPPORT FITTING P/N AFA7132-1 REQUIRES REPLACEMENT DUE TO CRACKS REMAINING AFTER REAMING TO .5 20. REMOVED SUPPORT BRACE, STRAP, VERTICAL STRAP, 2 EACH INTERCOSTALS, CLIP, WEB AND BACKUP FITTING IAW SRM 51-31-01. INSTALLED NEW BACKUP FITTING AND REINSTALLED SUPPORT BRACE, STRAP, VERTICAL STRAP, 2 EACH INTERCOSTALS, CLIP AND WEB I AW SRM 51-31-01. DOOR RIG ACCOMPLISHED ON ORIGINAL EO T 5230-110698. 2 L 7 3 4F A22WE 2007082400050 20070824 00050 EA 2007 8 24 TRAX200701177 1 20070812 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 920EV 7810 SERVICE DOOR WILL NOT OPEN FROM THE OUTSIDE. 2 L 7 2 4F RT A21EA 2007082400051 20070824 00051 NM 2007 8 24 07FDEA02971 1 20070819 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM BS 1956 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 595FE 48553 AFT CARGO, LONGERON 51L SPLICE END AROUND STA 1956 FOUND CRACKED. 08-31-07 REMOVED AND REPLACED AS PER SRM 51-31-01 V OLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007082400052 20070824 00052 NM 2007 8 24 07FDEA02972 1 20070819 A 5730 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 CRACK INDICATIONS REVEALED IN FASTENER HOLES TOWARDS EDGE OF ACCESS CUTOUT IN RT WING LOWER SKIN ACCESS DOOR, BETWEEN ST A XORS=683.400 TO STA XORS=713.600. 09-04-07 COMPLIED WITH FEDEX EA 1-5710-115155, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007082400053 20070824 00053 NM 2007 8 24 07FDEA02973 1 20070819 A 5730 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 CRACK INDICATIONS REVEALED IN FASTENER HOLES TOWARDS EDGE OF ACCESS CUTOUT IN LHW LOWER SKIN ACCESS DOOR, BETWEEN STA XO RS=683.400 TO STA XORS=713.600. 09-04-07 COMPLIED WITH FEDEX E.A. 1-5710-115154, CLASSIFIED AS MAJOR REPAIR AS PER FE DEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007082400054 20070824 00054 NM 2007 8 24 07FDEA02974 1 20070819 A 5753 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 CRACK FOUND ON OUTBOARD FASTENER HOLE OF LOWER ROW FASTENERS OF ARC4009 RIGHT OUTBOARD FLAP HINGE SUPPORT FITTING. 09-0 4-07 RT OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 2 7-50-00-830-805, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007082400061 20070824 00061 EU 2007 8 24 07FDEA02979 1 20070820 A 5552 A55276115000 ATTACH FITTING AIRBUS 300 A300B4605R 3930308 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORROSION ON INNER SIDE OF LT ELEVATOR ATTACH FITTING NR 4. REPAIR PERFORMED BY REMOVING CORROSION AND FLAP PEENING OF REWORKED AREA IAW RAS/CASA/5708/2007 ISSUE: A AND EA 6-5520-112509. 2 L 7 2 4F RT A35EU 2007082400062 20070824 00062 WP 2007 8 24 07FDEA02980 1 20070820 A 5347 S49321541200 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 GOUGED CABIN SEAT TRACK SCALLOPS AT STA 879 TO 899 LBL 85 REMOVED AND REPLACED SEAT TRACK IAW DC-10 SRM 53-70-00 VOL 1 P G 51. FABRICATED SPLICE PLATES AND SPLICE HATS IAW DC-10 SRM 53-70-00 PG 4 VOL 1. INSTALLED SEAT TRACK SPLICE PLATE AN D SPLICE HAT IAW DC10 SRM 51-31-01 VOL 2 PG 1-10. [08-29-07] REPAIR CLASSIFIED AS MAJOR. PART MARKED IAW GMM 7-0-1 000. 2 L 7 3 4F RT A22WE 2007082400063 20070824 00063 EU 2007 8 24 07FDEA02981 1 20070820 A 5310 A53771417206 BEAM AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORROSION ON FWD CARGO DOOR SILL BEAM AT FRAME LOCATIONS 25 AND 25A. REPAIR PERFORMED WITH CUTOUT OF UPPER FLANGE AND I NSTALLATION OF A MACHINED ANGLE IAW TD/K7/S1/08107/2007 IN EA 6-5313-112452, APPROVED BY RAS/DABRE/7008107/2007 ISSUE "B ". 2 L 7 2 4F RT A35EU 2007082400064 20070824 00064 WP 2007 8 24 07FDEA02982 1 20070820 A 5347 S492914727700 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 CABIN SEAT TRACK FLANGE IS CRACKED AT STA 449 LBL 28.5 REMOVED SEAT TRACK AT STA 449 LBL 28.5 IAW DC-10 SRM 51-31-01 VOL 2 PG 1-10. FABRICATED IAW DC-10 SRM 53-70-00 PG 51 VOL 1. INSTALLED SEAT TRACK AT STA 449LBL 28.5 IAW DC 10 SRM 51-51 -01 VOL 2 PG 1-2 . 2 L 7 3 4F RT A22WE 2007082400066 20070824 00066 EU 2007 8 24 07FDEA02984 1 20070820 A 5320 A53611656202 VALVE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 HEAVY CORROSION ON SUPPORT VALVE BETWEEN C16A AND C17. REPAIR PERFORMED BY INSTALLING NEW SUPPORT VALVE IAW SRM 51-72-1 0. 2 L 7 2 4F RT A35EU 2007082400067 20070824 00067 EU 2007 8 24 07FDEA02985 1 20070820 A 5330 A53812189200 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 EXTERNAL CORROSION AT UPPER FWD CORNER ON SKIN PANEL A538-12189-200 AT C39-40, P28-29, LHS. REPAIR PERFORMED BY REWORK IAW EA 6-5315-112437 AND RAS: 052738/008/2007 ISSUE "A". 2 L 7 2 4F RT A35EU 2007082400068 20070824 00068 EU 2007 8 24 07FDEA02986 1 20070820 A 5330 A53812189201 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION AT UPPER FWD CORNER ON SKIN PANEL A538-12189-201 AT C39-40, P'28-29, RHS. REPAIR PERFORMED BY REWORK AN D INSTALLING INTERNAL REPAIR DOUBLER IAW EA 6-5315-112437 AND RAS: 052738/008/2007 ISSUE "A". 2 L 7 2 4F RT A35EU 2007082400069 20070824 00069 EU 2007 8 24 07FDEA02987 1 20070820 A 5315 A53974322200 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND A WRONG PERFORMED OLD TOP CAP BEAM REPAIR IN AFT CARGO COMPARTMENT, C61, RHS. REPAIR PERFORMED BY INSTALLING NEW SPLICE REPAIR IAW SRM 53-10-15 / FIG 207. 2 L 7 2 4F RT A35EU 2007082400070 20070824 00070 WP 2007 8 24 07FDEA02988 1 20070820 A 5313 LONGERON DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 399FE 48262 AFT CARGO PIT AT FS 1950 LONGERON 51L IS CORRODED AND CRACKED. [08-29-07] REMOVED CORRODED SHOVEL END FITTING IAW MD /DC10 SRM 51-33-01 PAGE 1 VOL II. DRILLED NEW SHOVEL END FITTING P/N AGA3092-503 TO FIT IAW MD/DC10 SRM 51-31-01 PAGE 7 VOL II. INSTALLED NEW SHOVEL END FITTING IAW MD/DC10 SRM 51-33-01 PAGE 1 VOL II. 2 L 7 3 4F RT A22WE 2007082400071 20070824 00071 EA 2007 8 24 COMA0760523 1 20070809 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 933CA 7040 FLIGHT 5419 - RECEIVED FLAP FAIL MESSAGE AT GATE. COMPLIED WITH AD 2006-12-21. FLAP CAUTION MESSAGE -FIRST EVENT- MAIN TENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2007082400072 20070824 00072 EU 2007 8 24 07FDEA02989 1 20070820 A 5310 A53778689 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND IN MANHOLE FITTING AN EXISTING POCKED REPAIR IN BAD CONDITION AT C38.2. REPAIR PERFORMED BY INSTALLING NEW FILLER IAW EA 6-5314-112469, APPROVED BY RAS/DABRE/70008163/2007 ISSUE "A". 2 L 7 2 4F RT A35EU 2007082400074 20070824 00074 EU 2007 8 24 07FDEA02990 1 20070820 A 5730 A53740086206 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 CHAFING MARKS WERE FOUND ON LT LOWER SURFACE BOTTOM SKIN REINFORCING PLATE AT RIB 7 FRONT SPAR INBOARD. REPAIR PERFORME D BY BLENDING OUT IAW EA 6-5720-106522, APPROVED BY RAS/BAE/1005107/2007 ISSUE "A". 2 L 7 2 4F RT A35EU 2007082400079 20070824 00079 NM 2007 8 24 SWAA074042 1 20070815 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 602SW 27953 DURING SCHEDULED BRDG CHECK, FOUND RT WING OUTBOARD T/E FLAP DELAMINATED INBOARD END. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2007082400080 20070824 00080 NM 2007 8 24 SWAA074045 1 20070815 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007082400081 20070824 00081 NM 2007 8 24 SWAA074043 1 20070815 A 3350 65C27093 LIGHT BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007082400082 20070824 00082 NM 2007 8 24 SWAA074041 1 20070815 A 3350 767 LAMP BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 427WN 29831 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007082400084 20070824 00084 NM 2007 8 24 SWAA074048 1 20070815 A 2560 PH22300L GLOWSTRIP BOEING 737 7373Q8 1384670 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED BRDG CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP MISSING AT ROW 16 ABC. INSTALLED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007082400085 20070824 00085 NM 2007 8 24 KCSA071311 1 20070816 A 5330 SKIN BOEING 747 7472B4B 138481B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA 2160 AT STR 12L SKIN DAMAGED. 2 L 7 4 4F RT A20WE 2007082400086 20070824 00086 NM 2007 8 24 KCSA071310 1 20070816 A 5420 STIFFENER BOEING 747 747132 1384882 NM NR 2 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 709CK 20247 NR 2 PYLON LOWER I/B STIFFENER AFT BULKHEAD AT NAC STA 267 HAS 1.5 INCH CRACK. 2 L 7 4 4F A20WE 2007082400087 20070824 00087 EA 2007 8 24 COMA0770043 1 20070813 A 2150 GG670950093 ACM CNDAIR CL600 CL6002C10 1390015 EA A/C BAY SEIZED A COMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 378CA 4775 10097 FLIGHT 5642 - SMOKE REPORTED ENTERING CABIN DURING TAXI. DECLARED EMERGENCY, RETURNED TO BLOCK. REPLACED RIGHT PACK (A CM). NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007082400092 20070824 00092 EU 2007 8 24 YENA2007074 1 20070816 A 3234 215TS07Y00 CONTROL HANDLE AIRBUS 320 A320232 3930326 EU COCKPIT MALFUNCTIONED A YENA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 15 606JB 7182 15 2384 FLT 705, JFK-LGB, ON CLIMB, LANDING GEAR HANDLE WOULD NOT COME UP AFTER TAKEOFF. REMOVED AND REPLACED LANDING GEAR CONT ROL LEVER PER AMM 32-31-11-04. OPS CHECK OK. PERFORMED GEAR SWING PER AMM 32-30-00-02. NO DEFECTS NOTED. A/C OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2007082400093 20070824 00093 EA 2007 8 24 TRAX200701157 1 20070811 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 874AS 7551 FS 280 WEB CRACKED AT RBL 9. INSTALLED RT DRIP TRAY ALL WORK DONE IAW CRJ 200 SRM 51-42-16 DK 7022603, JOB COMPLETE. S UPPLEMENTAL - SDR CLOSED 08/17/07. 2 L 7 2 4F RT A21EA 2007082400096 20070824 00096 EA 2007 8 24 TRAX200701179 1 20070813 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 839AS 7284 ANGLE IS CRACKED AT FS 484 O/B OF RBL 27. 2 L 7 2 4F RT A21EA 2007082400098 20070824 00098 NM 2007 8 24 SWAA074071 1 20070816 A 3350 20131A BATTERY BOEING 737 7373G7 1384595 NM CABIN FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED MV4 CHECK, FWD CABIN EMERGENCY EXIT LIGHTS STAY ILLUMINATED WITH SWITCH IN OFF POSITION. REMOVED AND R EPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007082400099 20070824 00099 NM 2007 8 24 SWAA074052 1 20070816 A 5610 2315MODB WINDOW BOEING 737 7377H4 1384404 NM COCKPIT ARCED A SWAA K NONE O OTHER NR NOT REPORTED 1 SW 29 450WN 32470 FLIGHT DECK R2 WINDOW ARCED. REMOVED AND REPLACED R2 WINDOW AND CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 2007082400100 20070824 00100 NM 2007 8 24 SWAA074053 1 20070816 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 235WN 34630 EEPLS COVER MISSING AT ROW 3 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007082400101 20070824 00101 2007 8 24 SWAA074072 4 20070816 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 482WN 29852 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007082400102 20070824 00102 2007 8 24 SWAA074076 4 20070816 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 739GB 29275 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007082400103 20070824 00103 2007 8 24 SWAA074075 4 20070816 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 739GB 29275 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007082400104 20070824 00104 NM 2007 8 24 SWAA074056 1 20070816 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007082400105 20070824 00105 NM 2007 8 24 SWAA074073 1 20070816 A 5330 6545767 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BETWEEN BS 425 AND BS 435, LBL 2 TO RBL 3. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007082400106 20070824 00106 NM 2007 8 24 SWAA074057 1 20070816 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 373, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007082400107 20070824 00107 NM 2007 8 24 SWAA074055 1 20070816 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 952, STR 22R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007082400109 20070824 00109 NM 2007 8 24 SWAA074068 1 20070816 A 5755 654645262A HINGE BOEING 737 7373K2 13844BA NM NR 5 SPOILER WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND RT WING NR 5 GROUND SPOILER OUTBOARD HINGE WORN. REMOVED AND REPLACED SPOILER PER MM . 2 L 7 2 4F RT A16WE 2007082400110 20070824 00110 NM 2007 8 24 SWAA074062 1 20070816 A 5312 6546576 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 23L. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007082400111 20070824 00111 NM 2007 8 24 SWAA074061 1 20070816 A 5312 6546576 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 23R. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007082400112 20070824 00112 NM 2007 8 24 SWAA074060 1 20070816 A 5312 6546576 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 15R. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007082400116 20070824 00116 NM 2007 8 24 SWAA074067 1 20070816 A 5523 65C2638426A TAB BOEING 737 7373K2 13844BA NM RT ELEVATOR FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2007082400117 20070824 00117 NM 2007 8 24 SWAA074064 1 20070816 A 5754 65C26601 SLAT BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT LOWER OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007082400119 20070824 00119 NM 2007 8 24 SWAA074066 1 20070816 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503C, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007082400120 20070824 00120 2007 8 24 SWAA074070 4 20070816 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007082400123 20070824 00123 EA 2007 8 24 TRAX200701180 1 20070813 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 839AS 7284 ANGLE IS CRACKED AT FS 484 O/B OF LBL 9. 2 L 7 2 4F RT A21EA 2007082400124 20070824 00124 EA 2007 8 24 TRAX200701181 1 20070813 A 5347 CARGO TRACK CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 874AS 7551 CARGO FLOOR TRACKS AT LBL 27 AND LBL 9 CORRODED LT AND RT SIDE. 2 L 7 2 4F RT A21EA 2007082300202 20070823 00202 2007 8 23 2007UALA03099 4 20070809 A 2565 5A28701 ASPIRATOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SLIDE RAFT LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 181UA GJ987 25278 ASPIRATOR LEAKS FROM THE FLAP VALVES. REPLACED ASPIRATOR, CAUSE UNKNOWN. 08-31-07 SUSPECT IMPROPER ASSY OF JET PLATE ASSY DURING RESTORATION. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082300205 20070823 00205 EU 2007 8 23 2007UALA03102 1 20070809 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 403UA 442 RED EMERGENCY PATH LIGHT AT SEAT 10C HAS ONE INOP LAMP. RELAMPED 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300206 20070823 00206 EU 2007 8 23 2007UALA03103 1 20070810 A 5270 TARGET AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY EXIT LOOSE A UALA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 29 409UA 462 L AFT EMER EXIT DISPLAYED ON UPPER ECAM SCREEN, DOOR. FOUND PROX TARGET LOOSE UPON INSPECTION, RE-SECURED TARGET. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300221 20070823 00221 NM 2007 8 23 2007UALA03118 1 20070811 A 5330 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 841UA 1545 FUSELAGE DENT REPORTED BY RAMP AFTER ACFT DEPARTURE. DENT ON RIGHT SIDE FUESLAGE 6.75 INCHES AFT OF FRAME 12 WHICH IS F WD OF THE DOOR 1R & JUST ABOVE FLOOR LINE. MAJOR REPAIR ACCOMPLISHED AT HMV. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300228 20070823 00228 NM 2007 8 23 2007UALA03125 1 20070810 A 3350 58781 POWER STRIP BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN CONTAMINATED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 904UA 25004 FLOOR MOUNTED EEL LIGHTS INOP FROM ROW 11 TO AFT GALLEY. REPLACED WET POWER STRIP. REPLACED WET POWER STRIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082300239 20070823 00239 NM 2007 8 23 2007UALA03137 1 20070811 A 3350 1619 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 351UA 24319 EXTERIOR EMERGENCY OVERWING LIGHT, AFT OF LEFT WING TRAILING EDGE ON SIDE OF FUSELAGE INOP. RELAMPED OVERWING LIGHT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082300248 20070823 00248 NM 2007 8 23 2007UALA03146 1 20070810 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 675UA 29243 LEFT INBOARD FLAP EMERGENCY EXIT LIGHT INOPERATIVE. RESEATED CONNECTOR AND BATTERY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082300251 20070823 00251 NM 2007 8 23 2007UALA03149 1 20070811 A 2421 IDG BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE LT ENGINE FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 677UA 30029 LEFT GEN DRIVE DISCONNECTED FOLLOWING L GEN DRIVE LIGHT ILLUMINATION. REPLACED LT IDG PER MM 24-11-01. OPS CHECK GOOD 2 L 7 2 4F 4 F RT A1NM E24NE 2007082300258 20070823 00258 NM 2007 8 23 KCSA071298 1 20070814 A 5311 FRAME BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 C-2 DOOR OPENING PALLET SIDE LOCK SUPPORT ANGLE (FRAME) CORRODED AT BS 1903, RBL 61. 2 L 7 4 4F RT A20WE 2007082300283 20070823 00283 NM 2007 8 23 2007UALA03078 1 20070808 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 127UA 28813 EMERGENCY EXIT LIGHT INOP, UPPER DECK AT TOP OF STAIRS. REPLACED LIGHT ASSEMBLY, OPS CKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082300286 20070823 00286 2007 8 23 2007UALA03081 4 20070808 A 2565 DISK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE R1 DOOR SLIDE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 303UA 23644 FOUND 1 RT DOOR SLIDE GAUGE OUT GREEN. FOUND RUPTURE DISK HAS SMALL PIN HOLE LEAK. REPLACED DISK, REFILLED BOTTLE AN D CHECKED FOR LEAKS. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082300294 20070823 00294 NM 2007 8 23 07FDEA02956 1 20070817 A 5710 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 LEFT WING, LEADING EDGE SLAT DROOP LOWER SURFACE FOUND CRACK. 09-04-07 LT WING LEADING EDGE SLAT DROOP ASSY REMOVED AND REPLACED AS PER AMM 27-80-10. ADJUSTMENT CARRIED OUT AS PER AMM 27-80-10, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007082300300 20070823 00300 NM 2007 8 23 07FDEA02962 1 20070817 A 5347 BAC15201466 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 MID CABIN MAIN FLOOR STRUCTURE STA 856 TO 861, RBL 46 , WL 208, SEAT TRACK I/B FLANGE CORRODED ON UPPER SURFACE. REMO VED CORROSION, FOUND TO BE OUT OF LIMITS, ORG THICKNESS .100". REMOVED THICKNESS .073", LOSS OF 27 PERCENT, REF SRM 53- 10-01 FIG. REMOVED AND FAB, NEW SEAT TRACK. INSTALLED NEW SEAT TRACK, REF SRM 51-30-2. REPAIR IS CLASSIFED AS MAJOR. 2 L 7 3 4F RT A3WE 2007082300303 20070823 00303 EA 2007 8 23 QXEA200701272 1 20070812 A 2910 AE7178121 HOSE CNDAIR CL600 CL6002C10 1390015 EA HYD SYSTEM LEAKING A QXEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION NR NOT REPORTED 1 NM 09 613QX 10045 PDX - RECEIVED A HYDRAULIC LOW PRESSURE CAUTION FOR SYSTEM 2. PER THE CHECKLIST CLOSED THE RIGHT SHUTOFF VALVE AND CONT INUED TO PDX (35 MINUTES). MAINTENANCE FOUND THE PRESSURE OUTPUT LINE FOR THE DAMPER TO BE LEAKING. REPLACED LINE. O PERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007082300304 20070823 00304 EA 2007 8 23 QXEA200701269 1 20070810 A 3610 54011485 ANTI-ICE VALVE CNDAIR CL600 CL6002C10 1390015 EA RT NACELLE FAILED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 609QX 10031 GEG - RECEIVED A RIGHT COWL ANTI-ICE VALVE OPEN CAUTION MESSAGE AND A RIGHT START VALVE CAUTION MESSAGE. RETURNED TO TH E GATE. MAINTENANCE REPLACED THE COWL ANTI-ICE VALVE AND CROSS BLEED VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNE D TO SERVICE. 2 L 7 2 4F RT A21EA 2007082300307 20070823 00307 EA 2007 8 23 SIMA200723201 1 20070817 A 7740 4120T73P02 ACCELEROMETER CNDAIR CL600 CL6002C10 1390015 EA RT ENGINE FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 521AE 8459 10142 NUMBER TWO ENGINE N1 VIBRATION INDICATION WENT 1.8 - DIVERTED TO LIT. REMOVED AND REPLACED RIGHT ENGINE VIBRATION ACCEL EROMETER IAW CRJ AMM 77-31-01. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007082300317 20070823 00317 SO 2007 8 23 SIMA200723213 1 20070817 A 5347 14532606017 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 15794 5000 145312 LEFT OUTBOARD SEAT TRACK BETWEEN FRAMES 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082300331 20070823 00331 NM 2007 8 23 QXEA200701308 1 20070804 A 5320 BRACKET DHAV DHC8 DHC8202 2809007 NM BS 424 S24R CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - CORROSION ON STRINGER BRACKET STRINGER 24R AT STATION X 424.12. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-20-36. 2 H 7 2 4T RT A13NM 2007082300332 20070823 00332 SO 2007 8 23 RAIA0708024 1 20070810 A 5210 HANDLE EMB 145 EMB145ER 3260211 SO AIRSTAIR DOOR OUT OF ADJUST A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 808HK 145157 FLT 7878 - IAD - AIRSTAIR DOOR WILL NOT OPEN FROM THE INSIDE. MAINTENANCE FOUND THE MAIN DOOR INTERNAL HANDLE TO BE OUT OF ADJUSTMENT. INTERNAL HANDLE WAS ADJUSTED AND OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2007082300333 20070823 00333 NM 2007 8 23 QXEA200701310 1 20070809 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - LEFT WING NR 2 FLAP TRACK, LOWER SURFACE OF UPPER TRACK HAS PITTING. REPAIRED IAW RD8-57-986. 2 H 7 2 4T RT A13NM 2007082300335 20070823 00335 NM 2007 8 23 QXEA200701311 1 20070809 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - LEFT WING NR 2 FLAP TRACK UPPER SURFACE OF LOWER TRACK HAS PITTING. REPAIRED IAW RD8-57-986. 2 H 7 2 4T RT A13NM 2007082300336 20070823 00336 NM 2007 8 23 QXEA200701313 1 20070808 A 5313 STRINGER DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - FLIGHTDECK UNDERFLOOR AFT BULKHEAD, RIGHT STRINGER NR 31. HAS LIGHT CORROSION 15" FORWARD OF BULKHEAD TO ABOUT 5" FORWARD OF BULKHEAD. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-20-36. 2 H 7 2 4T RT A13NM 2007082300338 20070823 00338 NM 2007 8 23 QXEA200701312 1 20070810 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - LEFT WING FRONT SPAR LOWER CAP HAS FRETTING CORROSION AT YW 134.00 - YW 137. REPAIRED IAW RD8-57-1150 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2007082300339 20070823 00339 NM 2007 8 23 QXEA200701314 1 20070806 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 3 FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX-THE LEFT INBOARD NR 3 FLAP TRACK HAS EVIDENCE OF DISHING ON THE LOWER SIDE OF THE TOP RACK AFT OF FORWARD EDGE. REPAIRED IAW RD8-57-987. 2 H 7 2 4T RT A13NM 2007082300341 20070823 00341 NM 2007 8 23 QXEA200701315 1 20070807 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 4 FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - LEFT NR 4 FLAP TRACK OUTBOARD SIDE OF TRACK "E" THE SIDE ROLLER SHOWS SIGNS OF DISHING. REPAIRED IAW RD8-57-98 7. 2 H 7 2 4T RT A13NM 2007082300348 20070823 00348 NE 2007 8 23 SWAA074020 2 20070811 A 7200 332A1000 ENGINE BOEING 737 7373Y0 1384671 NM GE CFM56 CFM563B1 13802 NE RIGHT FLAMED OUT A SWAA K NONE X ENGINE FLAMEOUT LD LANDING 1 SW 29 682SW 23496 723109 UPON LANDING AND DECELERATION IN PHX NR 2 ENGINE FLAMED OUT. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082300352 20070823 00352 NM 2007 8 23 SWAA074008 1 20070811 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 415, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007082300365 20070823 00365 NM 2007 8 23 KCSA071303 1 20070815 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 CORROSION ON MAIN DECK SEAT TRACK AT RBL 12, BS 1590 TO 1690. 2 L 7 4 4F RT A20WE 2007082300378 20070823 00378 NM 2007 8 23 KCSA071306 1 20070815 A 5322 SHEAR TIE BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 SKIN ATTACHMENT SHEAR TIE HAS CORROSION AT STA 2200 AT STR 44R. 2 L 7 4 4F RT A20WE 2007082300379 20070823 00379 NM 2007 8 23 KCSA071307 1 20070815 A 5313 STRINGER BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STR 44R AT APPROX STA 2185 CORRODED UNDER SPLICE. 2 L 7 4 4F RT A20WE 2007082300380 20070823 00380 NM 2007 8 23 KCSA071308 1 20070815 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 SEAT TRACK AT LBL 46 HAS DAMAGED I/B FLANGE AT STA 1505 AT WL 118. 2 L 7 4 4F RT A20WE 2007082300383 20070823 00383 EA 2007 8 23 COMA0760512 1 20070802 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A COMA K NONE J WARNING INDICATION CR CRUISE 1 SO 01 995CA 12118 7229 FLIGHT 5178 - RECEIVED FLAPS FAIL CAUTION MESSAGE AT 16,000 FT. FLAPS INDICATED FAILING AT 0 DEGREES. AIRCRAFT LANDED SAFELY IN JFK. REMOVED AND REPLACED RIGHT BPSU. 2 L 7 2 4F RT A21EA 2007082400010 20070824 00010 NM 2007 8 24 QXEA200701316 1 20070807 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 5 FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - THE LEFT NR 5 FLAP TRACK OUTBOARD OF TRACK E SHOWS SIGNS OF DISHING. REPAIRED IAW RD8-57-987. 2 H 7 2 4T RT A13NM 2007082400014 20070824 00014 SO 2007 8 24 RAIA00708029 1 20070814 A 3350 744412 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 817HK 145058 PRE FLT 5564 - STL - EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007082400017 20070824 00017 NM 2007 8 24 QXEA200701318 1 20070809 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 4 FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - RIGHT NR 4 FLAP TRACK TOP SURFACE OF LOWER OUTBOARD RAIL IS PITTED. REPAIRED IAW RD8-57-988. 2 H 7 2 4T RT A13NM 2007082400030 20070824 00030 NM 2007 8 24 QXEA200701339 1 20070819 A 5246 DOOR BOMBDR DHC8 DHC8402 1390042 NM FUEL DOOR OPEN A QXEA O OTHER W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 NM 09 407QX 4049 BIL FLIGHT NR 2412: AT APPROXIMATELY 10,000 FEET, FUELING LIGHT CAME ON. RAN CHECKLIST. MAINTENANCE, UPON ARRIVAL OF A IRCRAFT, FOUND THE FUELING DOOR OPEN. INSPECTED DOOR AND FUELING DOOR HOUSING AND FOUND NO DAMAGE TO AIRCRAFT. LATCHED DOOR AND FUELING LIGHT WENT OUT. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007082400032 20070824 00032 EU 2007 8 24 TRAX200701113 1 20070804 A 5311 FRAME AEROSP ATR72 ATR72 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 IN MLG (RT) ON FR 27 AT RBL 15 FOUND CRACKED. ON MLG RT ON FR 27 AT RBL 15 DIAPHRAM HAS BEEN REPLACED IAW SRM 51-25-01. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SP 663 AND FAR 43 APPENDIX A REPAIR ACCOMPLISHED IAW SRM 51-25-01. SUP PLEMENTAL - SDR CLOSED 08/16/07. 2 H 7 2 4T RT 2007082400048 20070824 00048 WP 2007 8 24 07FDEA02969 1 20070818 A 5340 AFA71321 FITTING DOUG DC10 DC1030 3023501 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 318FE 46837 NR 6 MAIN CARGO DOOR JAMB SUPPORT FITTING P/N AFA 7132-1 REQUIRES REPLACEMENT DUE TO CRACKS REMAIN AFTER REAMING TO .520 . REMOVED BACKUP FITTING, ANGLE, INTERCOSTAL AND WEB IAW SRM 51-31-01. INSTALLED NEW BACKUP FITTING AND REINSTALLED AN GLE, INTERCOSTAL, AND WEB IAW SRM 51-31-01. DOOR RIGGED ON ORIGINAL EO T 8-5230-110698. 2 L 7 3 4F A22WE 2007082400049 20070824 00049 WP 2007 8 24 07FDEA02970 1 20070818 A 5340 AFA731321 FITTING DOUG DC10 DC1030 3023501 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 318FE 46837 NR 7 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING P/N AFA7132-1 REQUIRES REPLACEMENT DUE TO CRACKS REMAINING AFTER REAMI NG TO .520. REMOVED BACKUP FITTING, SUPPORT BRACE, STRAP, VERTICAL STRAP, SEAT TRACK SPLICE, INTERCOSTAL IAW SRM 51-3 1-01. CUT WEB IAW SRM 53-50-00. INSTALLED NEW BACKUP FITTING AND REINSTALLED SUPPORT BRACE, STRAP, VERTICAL STRAP, S EAT TRACK SPLICE, AND INTERCOSTAL IAW SRM 51-31-01. MANUFACTURED REPAIR DOUBLER FOR WEB AND INSTALLED REPAIR IAW SRM 51 -31-01 AND SRM 53-00-01. 2 L 7 3 4F A22WE 2007082400055 20070824 00055 EA 2007 8 24 TRAX200701178 1 20070812 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 744EV 10157 F/A FWD FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007082400060 20070824 00060 EU 2007 8 24 07FDEA02978 1 20070820 A 5310 A539730057202 BEAM AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 AFTER BLEND OUT OF HEAVY CORROSION ON FOLLOWING PART AT C67-69 BULK CARGO DOOR CUT OUT, REMAINING THICKNESS IS UP TO 50 PERCENT. BEAM SECTION: A539-730057-202 REPAIR PERFORMED BY REPLACEMENT OF BEAM SECTION IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007082400078 20070824 00078 NM 2007 8 24 SWAA074046 1 20070815 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 685, STR 27R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007082400113 20070824 00113 NM 2007 8 24 SWAA074069 1 20070816 A 5312 6549574 BULKHEAD BOEING 737 7373K2 13844BA NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD CORRODED AT BS 1016, LBL 1. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 2007082400130 20070824 00130 CE 2007 8 24 DXTA200702376 1 20070801 A 2751 POSITION SENSOR CESSNA 680 680CE 2076811 CE TE FLAPS MALFUNCTIONED E DXTA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 07 338QS 6800011 AMBER CAS (FLAPS FAIL) MESSAGE PUSHED EVENT MARKER, AT FL410, FOLLOWED CHECKLIST FLAP ON NR 2 DISPLAYED MOVED TO 7 DEGRE ES, WHEN IND = 0 DEGREES. R & R BOTH NR 1 & 2 FLAP POSITION SENSOR'S , OPS CHECKS GOOD, I/A/W 860 MM 27-50-00. 2 L 7 2 4F RC T00012WI 2007082400131 20070824 00131 CE 2007 8 24 DXTA200702377 1 20070801 A 2720 ACTUATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RUDDER FAILED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 918QS 7500223 ON TAKEOFF, AFTER GEAR UP, BEFORE FLAPS UP, GOT CAS (RUD LIMIT FAIL A), CONTROL PAGE MSG RUDDER LIMIT 99 PERCENT. IN STALLED NEW ACTUATOR IAW 750 M/M 27-23-00 RIG AND OPS CHECK GOOD IAW 750 M/M 27-20-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007082400133 20070824 00133 EA 2007 8 24 TRAX200701187 1 20070815 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 659CA 10153 RIGHT EMERGENCY EXIT LOWER EMERGENCY LIGHT HAS SEVERAL INOP BULBS. 2 L 7 2 4F RT A21EA 2007082400134 20070824 00134 EA 2007 8 24 TRAX200701188 1 20070815 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 PAX DOOR EXIT PLACARD WORN PER FA. 2 L 7 2 4F RT A21EA 2007082400135 20070824 00135 CE 2007 8 24 DXTA200702379 1 20070802 A 3240 PEDAL CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE RT BRAKE STIFF E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 322QS 5600421 RT SEAT BRAKE PEDALS REQUIRE LARGE AMOUNT OF MOVEMENT TO WORK. RT PEDAL TRAVELS HALFWAY TO THE FLOOR BEFORE ANY PRESSURE IS FELT. BLED BRAKE SYSTEM IAW 560 MM 32-42-00. OPS CHECK GOOD ON TAXI CHECK. 2 L 7 2 4F 4 F RT A22CE E25EA 2007082400136 20070824 00136 EA 2007 8 24 TRAX200701189 1 20070815 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 MAIN PASSENGER DOOR IS VERY HARD TO OPEN. T-HANDLE FEELS LIKE IT POPS OUT BUT THE HANDLE CANNOT BE TURNED FROM OUTSIDE OR THE LEVER HANDLE RAISED INSIDE THE AIRCRAFT. 2 L 7 2 4F RT A21EA 2007082400137 20070824 00137 EA 2007 8 24 TRAX200701190 1 20070815 A 3350 STRIP CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 826AS 7210 EMERGENCY LIGHT STRIP LOOSE. 2 L 7 2 4F RT A21EA 2007082400139 20070824 00139 SW 2007 8 24 HEEA116677 1 20070731 A 2435 23046020 STARTER GEN BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA ENGINE BURNED E HEEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 03 27805 31106 SMELLED BURNED ELECTRICAL ODOR IN THE COCKPIT. MAINTENANCE REPLACED NR 2 STARTER GENERATOR. 1 G 7 1 4U 4 U H4SW E22EA 2007082400142 20070824 00142 EA 2007 8 24 TRAX200701193 1 20070816 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 752EV 10166 LEFT FS 280 BULKHEAD LOWER WEB CORRODED. REMOVED AND REPLACED LT LOWER WEB OF FS280 IAW REO 670-53-11-052 2 L 7 2 4F RT A21EA 2007082400144 20070824 00144 EA 2007 8 24 TRAX200701197 1 20070816 A 5320 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 752EV 10166 FS 280 CENTER CROSSBEAM CORRODED. DRILLED AND INSTALLED NEW 280 CENTER CROSSBEAM PER CRJ 700 51-42-06 AND PAINTED. 2 L 7 2 4F RT A21EA 2007082400148 20070824 00148 NM 2007 8 24 KCSA071314 1 20070817 A 5330 SKIN BOEING 747 7472B4B 138481B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA 800 STR 24L HAS DAMAGED SKIN. 2 L 7 4 4F RT A20WE 2007082400149 20070824 00149 SW 2007 8 24 YTRR116739 1 20070722 A 2821 174364001 FUEL FILTER BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL CLOGGED B YTRR O OTHER O OTHER NR NOT REPORTED 1 SW 03 598RL 27 45598 FUEL FILTER IMPENDING BYPASS SWITCH KEPT ILLUMINATING CAUTION LIGHT. ON INSPECTION OF FILTER NO CLOGGING WAS NOTED. FILT ER WAS REPLACED AND BYPASS LIGHT ILLUMINATED AGAIN. FILTER HOUSING WAS REPLACED AND DISCREPANCY WAS CLEARED. 1 G 7 1 3U 3 U H2SW E1GL 2007082400151 20070824 00151 CE 2007 8 24 DXTA200702384 1 20070806 A 2750 SWITCH CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS MALFUNCTIONED E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 947QS 7500047 WHILE ENROUTE, AMBER FLAPS FAIL EICAS MSG ILLUMINATED. ALSO AMBER SYNOPTIC FLAP INDICATOR ILLUMINATED SHOWING FLAPS AT 1 0 DEGREES AND AIRSPEED READOUT WENT RED. FLAPS NEVER EXTENDED, SLATS DID WORK PROPERLY. REMOVED & REPLACED LEFT FLAP P OSITION SWITCH WITH NEW SWITCH. PERFORMED ELECTRICAL RIG USING FLAP BREAKOUT BOX. RAN SYSTEM SEVERAL TIMES WITH NO FAU LTS NOTED. WORK DONE IAW 750 MM 27-52-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007082400152 20070824 00152 CE 2007 8 24 DXTA200702385 1 20070806 A 3240 BRAKE ASSY CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MALFUNCTIONED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 639QS 5605139 ON LANDING, CAPTS LT BRAKE PEDAL WENT TO FLOOR WITH NO BRAKING ACTION. REMOVED AND REPLACED PILOTS LT WHEEL BRAKE MAST ER CYLINDER. PERFORMED BRAKE BLEED. PERFORMED LEAK CHECK. NO LEAKS NOTED. RAN AIRCRAFT FOR TAXI BRAKE CHECK. NO DISCREPA NCYS NOTED. WORK PERFORMED I.A.W. CH. 32-42-02. OF THE CITATION 560XL MM. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007082400153 20070824 00153 NM 2007 8 24 KCSA071316 1 20070817 A 5330 SKIN BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 AFT CARGO PIT DOOR CUTOUT FWD UPPER CORNER AT BONDING WIRE POINT CORRODED STA 1820 WL 180. 2 L 7 4 4F RT A20WE 2007082400154 20070824 00154 CE 2007 8 24 DXTA200702386 1 20070806 A 2750 COMPUTER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS FAULTED E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 930QS 7500130 FLAPS FAIL EICAS MESSAGE ANNUNCIATED IN CRUISE FLIGHT. FLAPS WOULD NOT RESET AND REMAINED INOPERATIVE. INSPECTED FLAP SYSTEM FOUND BITE CODE 1, 8, AND 9 RESET FLAP COMPUTER PER CE750 CH- 27-50-00, PERFORMED OPS CHECK OF FLAP SYSTEM NO FAULTS NOTED IAW CE750 MM CH. 27-50-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007082400157 20070824 00157 CE 2007 8 24 DXTA200702381 1 20070805 A 2120 UNKNOWN CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE CABIN SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 802QS 5600706 SMOKE DISCOVERED IN CABIN AFTER TAKEOFF. REMOVED AND INSTALLED ACM IAW R70.3G CMM CHAPTER 21-50-03. OPERATIONAL AND L EAK CHECK NORMAL. 2 L 7 2 4F 4 F RT A22CE E00053EN 2007082400158 20070824 00158 2007 8 24 DXTA200702382 4 20070805 A 2210 UNKNOWN RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP AUTOPILOT UNKNOWN E DXTA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 GL 07 882QS 258482 WHILE CLIMBING THROUGH FL350 LT AFCS FAILED. COULD NOT ENGAGE R AFCS OR YAW DAMPER. COULD NOT SELECT BETWEEN L & R AFCS. NO A/P OR YAW DAMPER OPERATION. REMOVED AND REPLACED WITH INSPECTED UNITS, BOTH NR 1&2 FLIGHT GUIDANCE COMPUTERS. OP S CHECK OF SYSTEM SHOWS NO DEFECTS. ALL WORK PERFORMED IAW HAWKER 800XP MM CHP- 34-22. 2 L 7 2 4F 4 F RT A3EU E6WE 2007082400159 20070824 00159 CE 2007 8 24 DXTA200702383 1 20070805 A 3240 BRAKE CESSNA 750 750 2076810 CE RIGHT WEAK E DXTA O OTHER O OTHER LD LANDING 1 GL 07 982QS 7500182 RIGHT BRAKE PEDAL IS VERY SPONGY ON BOTH PILOTS AND COPILOTS SIDE. PEDAL GOES ALMOST TO THE BOTTOM BEFORE SOLID BRAKING OCCURS. BLED BRAKES IAW 750 MM 32-42-00. TAXI CHECK GOOD. 2 L 7 2 4J RT T00007WI 2007082400161 20070824 00161 CE 2007 8 24 DXTA200702388 1 20070807 A 2150 ACM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL FAILED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 978QS 7500187 DURING DESCENT WITH POWER REDUCED TO APPROX 75-80 PERCENT N1 A PUFF OF SMOKE COME FROM BOTH OF THE COCKPIT WEMACS BELOW THE GLARESHIELD FOLLOWED BY VERY STRONG SULFUR ODOR. TROUBLESHOT DISCREPANCY TO A FAILED COCKPIT ACM. REMOVED AND REPL ACED ACM IAW 750 MM CHAPTER 21-50-01 OPS CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007082400163 20070824 00163 NE 2007 8 24 HEEA116744 1 20070803 A 3297 7655200904044 WIRE HARNESS SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL2S1 60057 NE LANDING GEAR DAMAGED B HEEA O OTHER J WARNING INDICATION CR CRUISE 1 SW 03 766P 760594 ON CRUISE CHECK, NOTED RT MAIN GEAR GREEN LIGHT ILLUMINATED. LOWERED GEAR TO 3 GREEN INDICATION. RETURNED TO DEPARTURE . MAINTENANCE REPLACED THE RT LANDING GEAR SENSOR HARNESS. 1 G 7 2 3U 4 U NC H1NE E00054EN 2007082400164 20070824 00164 NE 2007 8 24 HEEA116767 1 20070806 A 6340 9235115809102 BYPASS VALVE SKRSKY S92 S92A NE MAIN ROTOR INOPERATIVE B HEEA O OTHER J WARNING INDICATION CR CRUISE 1 SW 03 592PH 920027 MGB OIL BYPASS LIGHT CAME ON IN CRUISE FLIGHT. RETURNED TO DEPARTURE. MAINTENANCE REPLACED THE OIL BYPASS VALVE. 2 G 7 2 4U R00024BO 2007082400171 20070824 00171 EA 2007 8 24 A6WA200740400 1 20070716 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SERVICE OUT OF RIG A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 466AW 7899 (DURING WALKAROUND) SERVICE DOOR OUTER HANDLE IS DIFFICULT TO OPEN. RIGGED SERVICE DOOR UPPER STABILIZER BAR AND CLEANE D SERVICE DOOR SEAL AND OUTER HANDLE. OPS CHECK GOOD IAW AMM 52-41-00. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400172 20070824 00172 EA 2007 8 24 A6WA200740401 1 20070720 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 LT FS 621- 625 INTERCOSTAL ANGLE (PN 601-35012-51) CRACKED APPROX .3 INCH LONG IN AFT EQUIPMENT BAY. (K) MAINTENANCE R EMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-42-06, 51-42-21 AND BOMBARDIER REO 601R-53-61-422 REV C. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400173 20070824 00173 EA 2007 8 24 A6WA200740402 1 20070720 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 RT FS 621-FS 625 INTERCOSTAL ANGLE (PN 601-35012-52) CRACKED APPROX .2 INCH LONG IN AFT EQUIPMENT BAY. (K) MAINTENANC E REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-42-06, 51-42-21 AND BOMBARDIER REO 601R-53-61-422 REV NC. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400174 20070824 00174 EA 2007 8 24 A6WA200740403 1 20070721 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 460 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 RT FS 460 FLOOR SUPPORT FITTING (PN 600-31068) AT OB SIDE OF RBL 9 CRACKED APPROX 1.5 INCHES LONG. (K) MAINTENANCE REM OVED AND REPLACED FITTING P/N 600-31068-19 IAW CRJ 200 SRM 51-42-13, 51-42-21, AND 51-23-00. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400175 20070824 00175 NM 2007 8 24 WRLA2007086 1 20070816 A 5710 ARB2886 DOOR FRAME DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE RT WING CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 275WA 48631 RIGHT WING FIXED LEADING EDGE ANTI-ICING TELESCOPING DUCT DOOR CUT OUT CORNER FOUND CRACK AT STA XOS464 AND XOS470. 09 -26-07 PERFORM NDT/ET FOR REWORK AREA REF JC0032000. REPAIR DAMAGE PER MD-11 SRM 57-10-00 VOL.1 REV.40 AND EI NR 2006P 20A-124 REV.00. REF JC 0031848. 2 L 7 3 4F 4 F RT A22WE E24NE 2007082400176 20070824 00176 EA 2007 8 24 A6WA200740404 1 20070721 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 RT FS 484 FLOOR SUPPORT INTERCOSTAL AT RBL 36 CRACKED APPROX .2 INCH LONG. MAINTENANCE REPAIRED IAW REO 601R-53-41-059 AND EO 601R-53-003A. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400177 20070824 00177 EA 2007 8 24 A6WA200740405 1 20070721 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 RT FS 484 FLOOR SUPPORT INTERCOSTAL ANGLE AT RBL 27 CRACKED APPROX .2 INCH LONG. (K) MAINTENANCE REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400178 20070824 00178 2007 8 24 YENA2007075 4 20070816 A 2330 ENTERTAIN SYS AIRBUS 320 A320232 3930326 EU CABIN MALFUNCTIONED A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 528JB 1591 SEAT 19B ODOR OF ELECTRICAL SMOKE. NO VISIBLE SMOKE. LTV PLACED IN STBY AND ODOR DISSIPATED. C/W TSM 24-00-00-810-823 NO FINDING. SUSPECT LTV SYS AT 19B AT FAULT. PLACED LTV SYS ON MEL UNTIL LTV CAN ACCOMPLISH TSM TASK 23-39-300-810-80 1. NO EVIDENCE OF ELECTRICAL ODOR OR BURNED PINS. ALL TV'S OPS CHECK GOOD. REPLACED XEB AT 19B & VDU'S AT 20ABC AS PRE CAUTIONARY MEASURE PER TSM. ALL WORK IAW AMM 23-39-00-844-20-17. 2 L 7 2 4F RT A28NM 2007082400179 20070824 00179 EA 2007 8 24 A6WA200740406 1 20070721 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 LT FS 484 FLOOR SUPPORT INTERCOSTAL AT LBL 36 CRACKED APPROX .2 INCH LONG. MAINTENANCE REMOVED FLANGE FABRICATED AND IN STALLED ANGLE IAW BSC SR 601R-53-0030A AND BOMBARDIER REO 601R-53-41-059 REV A. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400183 20070824 00183 EA 2007 8 24 A6WA200740409 1 20070721 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 589 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 FLOOR EDGE MEMBER CRACKED AT FS 589.00. (K) MAINTENANCE REMOVED DAMAGED AND INSTALLED REPAIR IAW REO 601R-53-61-1574 R EV A. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400185 20070824 00185 EA 2007 8 24 A6WA200740411 1 20070722 A 5340 MOUNT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ASSIST MOTOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 PASSENGER DOOR ASSIST MOTOR MOUNT BRACKET (PN 601R317743-7) CRACKED APPROX .2 INCH LONG AT BOTTOM OF BRACKET. (K) MAI NTENANCE REMOVED AND REPLACED BRACKET IAW CRJ200 SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400186 20070824 00186 EA 2007 8 24 A6WA200740412 1 20070722 A 5310 TRACK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CARGO DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 CARGO DOOR FWD ROLLER TRACK U-CHANNEL (PN 601R35050-25) CRACKED APPROX .2 INCH LONG AT BOTTOM OF TRACK. (K) MAINTENAN CE REMOVED AND REPLACED U-CHANNEL IAW CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400188 20070824 00188 EA 2007 8 24 A6WA200740414 1 20070722 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 530 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 HYDRAULIC PRESSURE TRANSDUCER BRACKET (PN 601R75262-157) CRACKED APPROX .2 INCH LONG IN RT MLG WHEEL WELL CEILING. (K) MAINTENANCE REMOVED DAMAGED BRACKET AND INSTALLED SERVICEABLE BRACKET IAW CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400189 20070824 00189 EA 2007 8 24 A6WA200740415 1 20070722 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 530 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 HYDRAULIC PRESSURE TRANSDUCER BRACKET (PN 601R75262-159) CRACKED APPROX .2 INCH LONG IN LT MLG WHEEL WELL CEILING. (K) MAINTENANCE REMOVED AND REPLACED BRACKET IAW CRJ 200 SRM 51-42-13. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400190 20070824 00190 EA 2007 8 24 A6WA200740429 1 20070727 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 AFT PAX DOOR DRAG ANGLE (PN 601R31772-5) IS CRACKED AT PREVIOUS REPAIR APPROX .5 INCH LONG. (K) MAINTENANCE REMOVED A ND REPLACED DRAG ANGLE ON AFT PAX DOOR IAW REO 601R-52-11-513. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400193 20070824 00193 EA 2007 8 24 A6WA200740417 1 20070726 A 5340 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 465AW 7893 LT OBLIQUE ANGLE AT STA 625 HAS .5 INCH CRACKED IN RADIUS. (K) MAINTENANCE INSTALLED NEW ANGLE CRJ SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400194 20070824 00194 EA 2007 8 24 A6WA200740418 1 20070726 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 465AW 7893 RT OBLIQUE ANGLE AT STA 625.00 HAS A .5 INCH CRACKED IN RADIUS. (K) MAINTENANCE INSTALLED NEW ANGLE IAW CRJ SRM 51-42 -06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400197 20070824 00197 EA 2007 8 24 A6WA200740422 1 20070727 A 5340 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 465AW 7893 RT 484 ANGLE IS CRACKED AT RBL 27 APPROX 1 INCH LONG. (K) MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BOMBARDIER STANDARD REPAIR 601R-53-0029B. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400198 20070824 00198 EA 2007 8 24 A6WA200740423 1 20070727 A 5340 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 465AW 7893 LT 484 ANGLE IS CRACKED AT LBL 27 APPROX .5 INCHES LONG. (K) MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-53-41- 059 REV A AND BOMBARDIER STANDARD REPAIR 601R-53-0029B. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400199 20070824 00199 EA 2007 8 24 A6WA200740424 1 20070727 A 5340 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 465AW 7893 LT 484 ANGLE IS CRACKED AT LBL 36 APPROX .5 INCH LONG. (K) MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-53-41-05 9 REV A AND BOMBARDIER STANDARD REPAIR 601R-53-0030A. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400200 20070824 00200 EU 2007 8 24 YENA2007076 1 20070819 A 2751 WARNING SYSTEM EMB ERJ190 ERJ190100IGW 3260408 EU COCKPIT MALFUNCTIONED A YENA K NONE N FALSE WARNING CR CRUISE 1 EA 15 183JB 19000007 FLT 1094, CMH TO JFK. FLAP FAIL EICAS AT FL310. LDG WITH FLAPS 0. PERFORMED FIM TASK 27-51-00-810-802A. CLEARED FAUL TS. PERFORMED OPERATIONAL CHECKS SEVERAL TIMES AND NO FAULTS FOUND AT THIS TIME. ALL OKAY FOR SERVICE. 2 L 7 2 4F RT A57NM 2007082400201 20070824 00201 EA 2007 8 24 A6WA200740425 1 20070728 A 5753 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAP GOUGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 465AW 7893 RT WING IB FLAP LOWER SKIN GOUGED/DENTED APPROX 3 INCHES LONG X 3 INCHES WIDE X .205 INCH DEEP, ADJACENT TO RIB AT WS 74 .8, APPROX 8 INCHES AFT OF LEADING EDGE OF FLAP. (K) MAINTENANCE REPAIRED FLAP LOWER SKIN IAW BSC EO 601R-57-12572. ( M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400205 20070824 00205 NM 2007 8 24 HNAA0700162 1 20070809 A 7931 APT761000100DW TRANSMITTER DHAV DHC8 DHC8102 2809003 NM NR 1 ENGINE MALFUNCTIONED A HNAA E ENGINE SHUTDOWN O OTHER TO TAKEOFF 1 EA 07 914HA 53 NR 1 ENG OIL PRESS WENT TO 40 PSI IN FLT NO WARNING LIGHT. SHUT DOWN NR 1 ENGINE. REMOVED AND REPLACED NR 1 OIL PRESSU RE TRANSMITTER. LEAK AND OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007082400209 20070824 00209 NM 2007 8 24 CALA0700442 1 20070818 A 5320 69489856 ATTACH FITTING BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14609 27322 INSPECTION FOUND A .5 INCH CRACK IN ATTACHMENT CLIP AT STA 360, S11L. A REPAIR WAS INSTALLED IAW ECRA 5311-01352. 2 L 7 2 4F RT A16WE 2007082400210 20070824 00210 SO 2007 8 24 XGN2007F00021 2 20070730 A 8530 TISN712ACA CYLINDER HEAD BEECH 55 D55 1152730 CE CONT O520 IO520CB 17032 SO NR 6 CYLINDER CRACKED E XGNA K NONE O OTHER IN INSP/MAINT 1 SW 05 69RP 744 TE766 NR 6 CYLINDER WAS NEW ECI, REV 3, E SERIES, CRACKED BETWEEN FINS 1-3 BEHIND FUEL INJECTOR. THIS IS 6TH ECI, REV 3, E SE RIES, TO CRACK IN THE SAME LOCATION. (K) 1 L 7 2 3O 3 O 3A16 E5CE 2007082400213 20070824 00213 2007 8 24 GAIA0709 4 20070726 A 2215 54093031 SERVO BOEING 727 727224 1384076 NM PWA JT8 JT8D9A 52048 NE AILERON INOPERATIVE A GAIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 07 69735 20664 ON DOWN WIND LEG TO LANDING WITH THE AUTO PILOT ON THE FLIGHT CREW TURNED THE YOKE LEFT AND RIGHT WITH NO MOVEMENT OF TH E AIRCRAFT. A RATCHETING SOUND WAS OBSERVED. THE AUTO PILOT WAS TURNED OFF AND THE CONDITION CONTINUED FOR 1 MINUTE TH EN NORMAL OPERATION RESUMED. AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED THE AI LERON SERVO STOP MECHANISM. OPS CHECKED GOOD ON THE GROUND. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 3 4F 4 F A3WE E2EA 2007082400215 20070824 00215 NM 2007 8 24 KCSA071317 1 20070820 A 5312 PRESSURE PANEL BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 CORROSION ON LOWER SIDE OF PRESSURE DECK WEB AT BS 1319, LBL 118, WL 186. 2 L 7 4 4F RT A20WE 2007082400216 20070824 00216 EA 2007 8 24 TRAX200701203 1 20070816 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE J WARNING INDICATION CL CLIMB 1 SO 27 837AS 7271 FLAPS FAIL CAUTION AT 14K FT WHILE CLIMBING OUT OF ATL. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007082400222 20070824 00222 NM 2007 8 24 SWAA074100 1 20070818 A 3350 1619 LIGHT BOEING 737 7375H4 138449D NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007082400225 20070824 00225 NM 2007 8 24 SWAA074098 1 20070818 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 432WN 33715 EEPLS LENS LOOSE AT ROW 5 ABC. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007082400229 20070824 00229 NM 2007 8 24 SWAA074103 1 20070819 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007082400230 20070824 00230 NM 2007 8 24 SWAA074104 1 20070819 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 758, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007082400231 20070824 00231 NM 2007 8 24 SWAA074080 1 20070817 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 769, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007082400234 20070824 00234 NM 2007 8 24 SWAA074088 1 20070817 A 5322 6546529 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE BROKEN AT BS 520, STR 16L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007082400235 20070824 00235 CE 2007 8 24 081407N505CS1 1 20070814 A 3230 CABLE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE EMER EXTENSION MISRIGGED E Z5FA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 EA 63 505CS 5605252 AFTER TAKEOFF, AND CLIMBING THROUGH FL310, CREW DISCOVERED GEAR UNLOCK ANNUNCIATION FOLLOWED BY HYD PRESS ON. RAN APPROP RIATE AFM CHECKLIST AND DETERMINED ONE GEAR FELL OUT OF WELL. CYCLED GEAR TO DOWN AND LOCK WITH (3) GREENS DIVERTED BACK TO ICT LANDED WITHOUT INCIDENT. ON SITE MAINTENANCE FOUND LANDING GEAR EMERGENCY EXTENSION CABLE RIGGING TO BE TOO TIG HT. RERIGGED EMERGENCY GEAR CABLES AND OPS CHECKED SATISFACTORY, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007082400236 20070824 00236 NM 2007 8 24 SWAA074108 1 20070819 A 3260 655825029 LOGIC CARD BOEING 737 7373G7 1384595 NM LANDING GEAR FAULTY A SWAA K NONE N FALSE WARNING CL CLIMB 1 SW 29 690SW 23783 RAISED LANDING GEAR LEVER ON CLIMBOUT AND HAD RED NLG INDICATION WITH NO OTHER LIGHTS ILLUMINATED. CYCLED GEAR, LIGHTS NORMAL. ADJUSTED NLG DOWNLOCK SENSOR, REMOVED AND REPLACED M983 LOGIC CARD PER MM. 2 L 7 2 4F RT A16WE 2007082400243 20070824 00243 NM 2007 8 24 SWAA074090 1 20070817 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007082400244 20070824 00244 CE 2007 8 24 N4C2007F00000 1 20070726 A 3220 ROD END BEECH 58 58 1152740 CE CONT O520 IO520CB 17032 SO NLG BROKEN A N4CA K NONE O OTHER IN INSP/MAINT 1 GL 09 703NC TH224 299031R NOSE GEAR WOULD NOT LOCK DOWN BECAUSE OF A BROKEN ROD END ON THE NOSE GEAR RETRACT ROD. ROD END CONNECTS THE RETRACT RO D TO THE APR NOSE GEAR DRAG BRACE. RESULTED IN NOSE GEAR UP LANDING. (K) 1 L 7 2 3O 3 O 3A16 E5CE 2007082400245 20070824 00245 NM 2007 8 24 SWAA074091 1 20070817 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007082400246 20070824 00246 NM 2007 8 24 SWAA074093 1 20070817 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007082400248 20070824 00248 NM 2007 8 24 SWAA074095 1 20070817 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007082400250 20070824 00250 NM 2007 8 24 SWAA074106 1 20070819 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 27R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007082400252 20070824 00252 NM 2007 8 24 SWAA074082 1 20070817 A 5330 65C381921 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 513D, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007082400253 20070824 00253 NM 2007 8 24 SWAA074081 1 20070817 A 5330 65C381921 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 513D, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007082400254 20070824 00254 NM 2007 8 24 SWAA074109 1 20070819 A 3350 8100022601 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 202WN 33999 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 2 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007082400257 20070824 00257 2007 8 24 SWAA074101 4 20070819 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007082400258 20070824 00258 NM 2007 8 24 SWAA074099 1 20070818 A 5523 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM ELEVATOR TAB FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED 10Y CHECK, LEFT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HORN BEARING PER MM. 2 L 7 2 4F RT A16WE 2007082400259 20070824 00259 2007 8 24 SWAA074079 4 20070817 A 2565 S313597475 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007082400262 20070824 00262 NM 2007 8 24 CALA0700446 1 20070820 A 5320 69353521 FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A .25 INCH CRACK IN STRINGER TIE AT STA 727E, S3R. THE STRINGER TIE WAS REMOVED AND REPLACED IAW SRM 5 1-10-02. 2 L 7 2 4F RT A16WE 2007082400263 20070824 00263 SO 2007 8 24 RAIA00708032 1 20070815 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO CABIN NOT SEATED A RAIA O OTHER L NO TEST IN INSP/MAINT 1 CE 03 821HK 145068 PRE FLT 5586 - STL - EMERGENCY LIGHT AT SERVICE DOOR INOPERATIVE. MAINTENANCE RESEATED THE CONNECTOR TO THE LIGHT ASSEM BLY. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2007082400264 20070824 00264 SO 2007 8 24 RAIA00708033 1 20070816 A 3350 RPS1B BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 812HK 145373 PRE FLT 5530 - BNA - SEVERAL EMERGENCY LIGHTS IN THE CABIN ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 E MERGENCY LIGHT BATTERY. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007082400274 20070824 00274 EA 2007 8 24 TRAX200701198 1 20070816 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 752EV 10166 SEVERAL RT FLOOR SEAT RAILS HAVE MINOR CORROSION FS 364.00 TO FS 693.00. REMOVED CORROSION FROM SEAT RAILS FROM VARIOU S SPOTS BETWEEN RT FS 364.00 TO FS 693.00. BRUSHED REWORKED AREAS WITH ALODINE. ALL DIMENSIONS WITHIN ALLOWABLE LIMITS . EACH REWORKED SEAT TRACK IDENTIFIED WITH THE WORDS REO 670-53-00-013. ALL WORK DONE IN REFERENCE TO CRJ 700 SRM 53-2 1-49. ALL WORK DONE IAW CRJ 700 SRM 51-12-00, 51-21-06, 51-21-16, AND 53-21-49. JOB COMPLETE. SUPPLEMENTAL - SDR CLOS ED 08/21/07. 2 L 7 2 4F RT A21EA 2007082400276 20070824 00276 EA 2007 8 24 TRAX200701199 1 20070816 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 752EV 10166 SEVERAL LT FLOOR SEAT RAILS HAVE MINOR CORROSION FS 379.00 TO 693.00. REMOVED CORROSION FROM SEAT RAILS FROM VARIOUS SP OTS BETWEEN LT FS 379.00 TO FS 693.00. BRUSHED REWORKED AREAS WITH ALODINE. ALL DIMENSIONS WITHIN ALLOWABLE LIMITS. E ACH REWORKED SEAT RAILS IDENTIFIED WITH THE WORDS REO 670-53-00-013. ALL WORK DONE IN REFERENCE TO CRJ 700 SRM 53-21-49 . ALL WORK DONE IAW CRJ 700 SRM 51-12-00, 51-21-06, 51-21-16, AND 53-21-49. JOB COMPLETE. SUPPLEMENTAL - SDR CLOSED 0 8/21/07. 2 L 7 2 4F RT A21EA 2007082400277 20070824 00277 NM 2007 8 24 SWAA074113 1 20070820 A 3350 3071BPEGPL LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGH T BULB PER MM. 2 L 7 2 4F RT A16WE 2007082400278 20070824 00278 NM 2007 8 24 SWAA074110 1 20070820 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 219WN 32490 EEPLS LENS MISSING AT ROW 3 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007082400279 20070824 00279 NM 2007 8 24 SWAA074112 1 20070820 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 400, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007082400280 20070824 00280 NM 2007 8 24 SWAA074119 1 20070820 A 5330 6545767129 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503C, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007082400281 20070824 00281 NM 2007 8 24 SWAA074116 1 20070820 A 5312 6545819 PRESSURE PANEL BOEING 737 7373Q8 1384670 NM NLG W/W CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED BRDG CHECK, FOUND RIGHT NLG W/W PRESSURE WEB CORRODED AT BS 251.6. REPAIRED WEB PER EA AND SRM. 2 L 7 2 4F RT A16WE 2007082400282 20070824 00282 NM 2007 8 24 SWAA074118 1 20070820 A 3350 65C27093 LIGHT BOEING 737 7373Y0 1384671 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007082400283 20070824 00283 NM 2007 8 24 SWAA074117 1 20070820 A 5322 69353656 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 360, LBL 2. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007082400284 20070824 00284 EU 2007 8 24 COEA0701901 1 20070730 A 5754 S57210627211 STRIP AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE RT WING SLAT CHAFED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 02 901FX 172 IN HEAVY CHECK IN COE, FOUND CHAFING ON LOWER SLAT STRIP AT RIB 20 COMMON TO SINGLE POINT REFUEL ACCESS DOOR RT WING. R EPAIRED CHAFING ON FWD SPAR, LOWER FLANGE AT FUEL DOOR BY INSTALLATION OF REPAIR DOUBLER IAW ART DWG S572R0093. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007082400286 20070824 00286 EU 2007 8 24 PRI2007F00000 1 20070801 A 5797 WIRE HARNESS AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE7313D WP WING DAMAGED E PRIA K NONE O OTHER IN INSP/MAINT 1 GL 03 751JC 129 DURING A ROUTINE BLOCK INSPECTION, A VISUAL INSPECTION OF THE WINGS REVEALED MULTIPLE WIRES SHOWING DAMAGE IN THE FLAP W ELL AREA, FWD OF THE IB FLAPS. THE CAUSE DAMAGE TO THE WIRE BUNDLES F50B602101A1 AND F50B602102A1 COULD NOT BE DETERMIN ED. SOME SHOWED SIGNS OF HEAT DAMAGE AND OTHERS SEEMED FRAYED OR CHAFED OR CHEWED. NO SYSTEM MALFUNCTIONS WERE NOTED B Y THE FLIGHT CREW PRIOR TO THE NSPECTION. THE AC WAS ON AN INTERNATIONAL FLIGHT PRIOR TO THE INSPECTION. THE WIRES WER E REPLACED IAW THE MFG MM AND STANDARD PRACTICES AND ADDITIONAL SHIELDING WAS APPLIED. INSPECTION OF OTHER AC IN THE FL EET SHOWED NO SIMILAR DAMAGE. RECOMMENDATIONS ARE TO SHIELD WIRE BUNDLES BETTER AND PAY MORE ATTENTION TO FLAP WELL ARE 2 L 7 3 4F 4 F A46EU E6WE 2007082400287 20070824 00287 2007 8 24 SWAA074115 4 20070820 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007082400288 20070824 00288 NM 2007 8 24 SWAA074111 1 20070820 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 225WN 34333 DURING SCHEDULED MV1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHTS INOP BETWEEN ROW 9 ABC AND ROW 11 ABC. REMOVED AND RE PLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007082400289 20070824 00289 EA 2007 8 24 TRAX200701204 1 20070816 A 5210 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 881AS 7496 PAX DOOR IS CRACKED ON THE INNER AFT SUPPORT ANGLE 35.3 INCHES FROM LWR EDGE OF DOOR. CRACK IS APPROX 1.5 INCH LONG. R EWORK DONE AS REFERENCED IN CRJ 200 SERIES SRM 51-21-11, 51-23-00, 51-42-13, & 51-42-22. 2 L 7 2 4F RT A21EA 2007082400293 20070824 00293 EA 2007 8 24 TRAX200701208 1 20070817 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 881AS 7496 FS 280 AT RBL 9 O/B CLIP CRACKED. REWORK ACCOMPLISHED USING CRJ 200 SERIES SRM 51-21-11, 51-23-00, 51-24-16, 51-25 -16, 51-25-16, 51-42-21, & REO PL601R-53-11-926. 2 L 7 2 4F RT A21EA 2007082300224 20070823 00224 EU 2007 8 23 2007UALA03121 1 20070810 A 2530 OVEN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RIGHT ODOR A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 422UA 503 AFT RIGHT OVEN HAS ELECTRICAL ODOR. ODOR WENT AWAY AFTER LANDING AND NEVER RETURNED. ALL VISUAL CHECKS OF COMPONENTS C OMPLETED, NO UNUSUAL DEFECTS DEFECTS. NO REPEATS SINCE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300230 20070823 00230 NM 2007 8 23 2007UALA03127 1 20070810 A 5210 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU PAX DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 FWD ENTRY DOOR CRACK ON INNER SKIN AND FRAME AFT SIDE AT SEVENTH STOP FITTING FROM TOP. MAJOR REPAIR ACCOMPLISHED: FA BRICATED & INSTALLED DOUBLER/ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082300235 20070823 00235 NM 2007 8 23 2007UALA03133 1 20070813 A 3350 58781 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 309UA 23670 FLOOR EMERGENCY EXIT LIGHTS 21 ABC INOP. REPLACED STRIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082300252 20070823 00252 NM 2007 8 23 2007UALA03150 1 20070811 A 3350 COVER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 778UA 26940 EMERGENCY LIGHT COVER OFF AT 19C. 10-23-07 REPLACED EEL LIGHT ASSY TO PROVIDE COVER WITH RETAINERS. AIRCRAFT OK F OR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007082300253 20070823 00253 NM 2007 8 23 2007UALA03151 1 20070810 A 4920 APU BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SHUTDOWN A UALA O OTHER O OTHER TO TAKEOFF 1 WP 29 215UA 30221 APU AUTO SHUT DOWN AT DEPARTURE. 10-23-07 REPLACED APU PER MM 49-11-01. ACCOMPLISHED APU VERIFICATION FLIGHT. A CCEPTED BY FLT CREW AND RETURNED TO FULL ETOPS SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007082300271 20070823 00271 NM 2007 8 23 2007UALA03065 1 20070807 A 2910 SWIVEL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE MLG HYD LINE LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 808UA 804 RTFL DUE TO GREEN HYDRAULIC SYSTEM FAILURE. 09-07-07 BROKEN HYD SWIVEL FITTING ON GEAR. REPLACED BROKEN SWIVEL FITT ING. RESET ALL SYSTEMS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300272 20070823 00272 NM 2007 8 23 2007UALA03066 1 20070807 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 FLOORBEAM CORRODED: CABIN BS 294.5, LBL 6-7 WATERLINE 208, UPPER FLANGE CAP. REMOVED CORROSION. FABRICATED AND INSTALLE D REPAIR ANGLE AND SHIM. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082300279 20070823 00279 NM 2007 8 23 2007UALA03074 1 20070808 A 3350 1317 LAMP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 907UA 25007 FOUND EMERGENCY AISLE LIGHT INOP ROW 15D. RELAMPED. OPS CK NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082300280 20070823 00280 NM 2007 8 23 2007UALA03075 1 20070808 A 3350 363674 LAMP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 907UA 25007 FOUND EEL LAMP DIM ROW 15. REPLACED LAMP. CKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082300282 20070823 00282 NM 2007 8 23 2007UALA03077 1 20070808 A 3350 362624 LAMP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 EXTERIOR EEL LIGHT BY DOOR 1L IS INOP. RELAMPED OPS CK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082300311 20070823 00311 SO 2007 8 23 SIMA200723208 1 20070817 A 5347 13500412001 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 15794 5000 145312 RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 53 AND 55 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082300318 20070823 00318 SO 2007 8 23 SIMA200723214 1 20070817 A 5347 12500439007 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 15794 5000 145312 LEFT INBOARD SEAT TRACK BETWEEN FRAMES 18 AND 23 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082300323 20070823 00323 SO 2007 8 23 SIMA200723219 1 20070817 A 5521 14527287401 HINGE FITTING EMB 135 EMB135LR 3260305 SO ZONE 300 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 15794 5000 145312 LEFT ELEVATOR SERVO TAB INBOARD HINGE FITTING CORRODED. REMOVED AND REPLACED HINGE FITTING IAW EMB 55-22-01. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082300324 20070823 00324 SO 2007 8 23 SIMA200723216 1 20070817 A 5347 14530658007 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 15794 5000 145312 RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082300325 20070823 00325 SO 2007 8 23 SIMA200723217 1 20070817 A 5347 14532606015 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 725AE 15794 5000 145312 LEFT INBOARD SEAT TRACK BETWEEN FRAMES 23 AND 34 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082300334 20070823 00334 SO 2007 8 23 C2XA07CL067 1 20070813 A 3350 7287100507 CONTROL PANEL EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 23139 145731 CLE FLIGHT 2320 - THE CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT TEST FROM THE F/A CONTROL PANEL. ALSO THE CABIN LIGH TS WOULD NOT OPERATE. MAINTENANCE INSPECTED AND REPLACED THE F/A'S CABIN CONTROL PANEL. OPERATIONAL CHECKS OF ALL THE LIGHTS WERE GOOD. 2 L 7 2 4F RT 2007082300340 20070823 00340 NM 2007 8 23 ASAA0741943 1 20070810 A 5312 657378337 SKIN BOEING 737 7374S3 1384711 NM HORIZ STAB DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 LEFT HORIZONAL STABILIZER LEADING EDGE DAMAGED IN TWO LOCATIONS FROM FORKLIFT. INSTALLED TWO TEMPORARY EXTERNAL DOUBLER S THAT MUST BE INSPECTED EVERY A-CHECK. PERMANENT REPAIR TO BE INSTALLED AT NEXT HEAVY CHECK. 2 L 7 2 4F RT A16WE 2007082300342 20070823 00342 NM 2007 8 23 SWAA074032 1 20070811 A 2910 00915202002 CHECK VALVE BOEING 737 7375H4 138449D NM HYDRAULIC SYS FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 29 523SW 26565 DURING FLIGHT WITH RT PACK RUNNING, BAD HYDRAULIC FLUID SMELL IN CABIN. REMOVED AND REPLACED HYDRAULIC CHECK VALVES ON RESERVOIR PRESSURIZATION MODULE PER MM. 2 L 7 2 4F RT A16WE 2007082300344 20070823 00344 NM 2007 8 23 SWAA074023 1 20070813 A 3350 1619 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND RT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB P ER MM. 2 L 7 2 4F RT A16WE 2007082300353 20070823 00353 NM 2007 8 23 SWAA074009 1 20070811 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 474, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007082300358 20070823 00358 NM 2007 8 23 SWAA074029 1 20070813 A 5315 BAC1509100046 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 748SW 29800 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 773, LBL 17 TO RBL 13. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007082300360 20070823 00360 2007 8 23 SWAA074019 4 20070813 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007082300384 20070823 00384 EA 2007 8 23 COMA0760513 1 20070802 A 7830 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER ACTIVATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 523CA 7821 FLIGHT 5555 - LEFT THRUST REV CAUTION MESSAGE CAME ON DURING CLIMBOUT AT 9000 FT. AIRCRAFT RETURNED BACK TO GSO, MESSAG E WENT OUT DESCENDING THROUGH 3000 FT. AIRCRAFT LANDED SAFELY. TRANSFERRED TO DEFERRED LIST PER MEL 78-30-01. 2 L 7 2 4F RT A21EA 2007082300388 20070823 00388 NE 2007 8 23 COMA0760517 2 20070804 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE UNKNOWN A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 735CA 7267 FLIGHT 5337 - EN ROUTE FROM BOS TO SAV, FLIGHT DIVERTED TO JFK AFTER CREW NOTICED WHAT APPEARED TO BE A LACK OF ENGINE P OWER, AIRCRAFT LANDED SAFELY. PERFORMED ENGINE GROUND RUNS AND FOUND ENGINES TO OPERATE WITHIN LIMITS. 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400008 20070824 00008 GL 2007 8 24 J4PA2663 1 20070817 A 2420 646843 ALTERNATOR CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO HARTZL HCJ3Y PHCJ3YF1 GL ENGINE OPEN E J4PA O OTHER J WARNING INDICATION CR CRUISE 1 SO 13 134AJ 1511 917726 FP3800B WHILE AT CRUISE, ALT 1 LIGHT ILLUMINATED. PILOT DIVERTED TO PDK. ONE PASSENGER WAS ONBOARD. LAND WITH INCIDENT. MAIN TENANCE REPLACED THE NR 1 ALTERNATOR AND FIELD CONTROL MODULE. 1 L 7 1 3O 3 O NT A00009CH E3SO 5 C P36EA 2007082400015 20070824 00015 SO 2007 8 24 RAIA00708028 1 20070813 A 3350 100845 POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 819HK 145062 PRE FLT 5517 - STL - EMERGENCY LIGHT IN THE FORWARD CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPL Y. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007082400016 20070824 00016 WP 2007 8 24 ABXA070256 1 20070809 A 2913 AS66411LS666 PUMP DOUG DC9 DC932 3022066 WP LT ENGINE LEAKING A ABXA K NONE K FLUID LOSS CL CLIMB 1 GL 23 989AX 47314 DURING CLIMBOUT THRU 17,000 FEET, LEFT HYDRAULIC QUANTITY DROPPED TO ZERO WITH LOSS OF LEFT HYDRAULIC PRESSURE. FOUND T HE LEFT ENGINE DRIVEN HYDRAULIC PUMP LEAKING. REPLACED THE LEFT ENGINE DRIVEN HYDRAULIC PUMP IAW DC9 MM 29-10-05-2-0001 . 2 L 7 2 4F A6WE 2007082400019 20070824 00019 NM 2007 8 24 QXEA200701326 1 20070809 A 5320 INTERCOSTAL DHAV DHC8 DHC8202 2809007 NM BS 425 S23L CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - FORWARD INTERCOSTAL ANGLE BRACKET ON STRINGER 23L AT STATION X425 IS CRACKED. REPAIRED IAW SRM 51-40-11 AND 51 -40-00. 2 H 7 2 4T RT A13NM 2007082400022 20070824 00022 EU 2007 8 24 TRAX200701111 1 20070804 A 5311 FRAME AEROSP ATR72 ATR72 EU LT MLG WW CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 LEFT WW FRAME HOLDING BELLY PANEL 193AL CRACKED. LEFT WHEEL WELL FRAME HOLDING BELLY PANEL 193AL REPLACED IAW SRM 51-25 -01. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SP663 AND FAR 43 APPENDIX A REPAIR ACCOMPLISHED IAW SRM 57-25-01. SUPPLEMENTAL - SDR CLOSED 08/16/07. 2 H 7 2 4T RT 2007082400047 20070824 00047 WP 2007 8 24 07FDEA02968 1 20070818 A 5340 AFA71321 FITTING DOUG DC10 DC1030 3023501 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 318FE 46837 NR 5 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING P/N AFA 7132-1 REQUIRES REPLACEMENT DUE TO CRACKS REMAINING AFTER REAM ING TO .520. REMOVED 2 EACH SUPPORT BRACES, STRAP, WEB, INTERCOSTAL, AND BACKUP FITTING IAW SRM 51-31-01. INSTALLED NE W BACKUP FITTING AND REINSTALLED 2 EACH SUPPORT BRACES, STRAP, WEB, AND INTERCOSTAL IAW SRM 51-31-0. DOOR RIG ON ORIG INAL EO T 8-5230-110698. 2 L 7 3 4F A22WE 2007082400065 20070824 00065 EU 2007 8 24 07FDEA02983 1 20070820 A 5315 A53773651 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 OLD WRONG PERFORMED TOP CAP BEAM REPAIR IN FWD CARGO COMPARTMENT, C30, RT. REPAIR PERFORMED BY INSTALLING NEW TOP CAP B EAM REPAIR IAW SRM 53-10-15/FIG 207. 2 L 7 2 4F RT A35EU 2007082400073 20070824 00073 NM 2007 8 24 SWAA074049 1 20070815 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 235WN 34630 FWD CABIN L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007082400090 20070824 00090 EA 2007 8 24 COMA0760525 1 20070813 A 4920 38004883 APU CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 912CA 21147 7011 FLIGHT 5002 - APU OIL TEMP CAUTION RECEIVED EN ROUTE. DIVERTED TO SDF, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED A PU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007082400091 20070824 00091 EA 2007 8 24 COMA0760526 1 20070813 A 4970 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA APU MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 912CA 7011 FLIGHT 5318 - APU OIL TEMP CAUTION RECEIVED EN ROUTE. DIVERTED TO BNA, LANDED WITHOUT INCIDENT. INSPECTED OIL LEVEL, C HECKED OIL TEMP SENSOR AND CLEANED ELECTRICAL CONNECTOR. RAN APU WITH BOTH PACKS ON, NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007082400095 20070824 00095 NM 2007 8 24 CALA0700441 1 20070730 A 5210 507945264 DOOR FRAME BOEING 737 7373T0 1384582 NM L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND A CRACK EMANATING FROM THE DOORSTOP CUTOUT IN THE AFT EDGE BEAM OF THE L-1 DOOR. THE EDGE BEAM WAS REP AIRED IAW ECRA 5210-01944. 2 L 7 2 4F RT A16WE 2007082400097 20070824 00097 NM 2007 8 24 SWAA074054 1 20070816 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 LEFT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007082400121 20070824 00121 NM 2007 8 24 SWAA074077 1 20070816 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 787SA 29812 DURING SCHEDULED MV2 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007082400122 20070824 00122 NM 2007 8 24 SWAA074074 1 20070816 A 3350 MS155721 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 718SW 27852 DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007082400126 20070824 00126 EA 2007 8 24 TRAX200701183 1 20070814 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 841AS 7300 RIGHT FWD EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007082400128 20070824 00128 EA 2007 8 24 TRAX200701185 1 20070814 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR BINDS A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 UNABLE TO OPEN ASD. FLT 4306 CX. 2 L 7 2 4F RT A21EA 2007082400129 20070824 00129 CE 2007 8 24 DXTA200702375 1 20070801 A 3240 BRAKE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE RIGHT WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 142QS RK432 RT SEAT BRAKES FADE EXCESSIVELY AFTER DEPRESSING PEDALS. LT SEAT BRAKES ARE GOOD. REMOVED COPILOT RH MASTER CYLINDER, P/N 45AS38401-012, SN 2807. INSTALLED A NEW MASTER CYLINDER PN 45AS38401-012, SN 3274. WORK PERFORMED IAW HS-400XP MM CHAPTER 32-40-00. OPERATIONAL CHECKS AND LEAK CHECKS GOOD. 2 H 7 2 4F 4 F RT A16SW E25EA 2007082400140 20070824 00140 EA 2007 8 24 TRAX200701191 1 20070815 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 907EV 7648 CAPT'S FLASHLIGHT INOP (DIM). 2 L 7 2 4F RT A21EA 2007082400141 20070824 00141 EA 2007 8 24 TRAX200701192 1 20070816 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 859AS 7421 RIGHT FWD EXT EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007082400143 20070824 00143 EA 2007 8 24 TRAX200701194 1 20070816 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 752EV 10166 RIGHT FS 280 BULKHEAD LOWER WEB CORRODED. REMOVED AND REPLACED RT FS 280 LOWER WEB IAW REO 670-53-11-052 2 L 7 2 4F RT A21EA 2007082400146 20070824 00146 NM 2007 8 24 KCSA071313 1 20070817 A 5320 ATTACH ANGLE BOEING 747 747212B 1384886 NM FUSELAGE WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 ATTACH ANGLE HAS WORN HOLES AT STA 1480 WL 100 LBL 113. 2 L 7 4 4F A20WE 2007082400150 20070824 00150 NM 2007 8 24 KCSA071315 1 20070817 A 5312 SPLICE BOEING 747 7472B4B 138481B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA 2598 BULKHEAD SPLICE AT STR 11R DAMAGED AT WL 320 RBL 50. 2 L 7 4 4F RT A20WE 2007082400160 20070824 00160 NE 2007 8 24 WRLA2007085 2 20070816 A 7220 2215061507 BELLMOUTH DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE NR 2 ENGINE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 275WA 48631 THREE EA CRACKS AT NUMBER 2 ENGINE BELLMOUTH BETWEEN 6-7 O'CLOCK POSITION. REPLACED NR 2 ENGINE BELLMOUTH ASSYWITH NEW P ARTS AS PER AMM 71-11-04-000-868/71-11-04-400-868 REV.59 2 L 7 3 4F 4 F RT A22WE E24NE 2007082400165 20070824 00165 NE 2007 8 24 HEEA116772 1 20070807 A 6730 7690001802106 SERVO SKRSKY S76 S76C 8143008 NE NR 1 PITCH FAILED B HEEA O OTHER J WARNING INDICATION CR CRUISE 1 SW 03 748P 891 760629 DURING CRUISE, APPROX. 20 MINUTES AFTER TAKEOFF NR 1 PITCH SERVO FAILED 1E40 CAME ON. 10 MINUTES AFTER THAT THE NR 1 A HRS FAILED LIGHT CAME ON. THERE WAS NO PITCH CONTROL AVAILABLE THROUGH THE AFCS AND THERE WAS CONTINUOUS FEEDBACK IN TH E PITCH AXIS. RETURNED TO DEPARTURE. MAINTENANCE REPLACED THE PITCH SERVO. PROBLEM REOCCURRED ON LATER FLIGHT. 1 G 7 2 3U NC H1NE 2007082400167 20070824 00167 CE 2007 8 24 DXTA200702389 1 20070808 A 2120 UNKNOWN RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP CABIN ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 840QS 258340 DURING DESCENT, WHEN APU BLEED WAS SELECTED, HAD A STRONG FUEL SMELL IN CABIN. INSPECTED SPR VALVE DOOR - AFT EQUIPMEN T BAY FOR FUEL ODOR, OPENED WHEEL WELLS AND PANELS IN WHEEL WELLS, LOWER FLAPS, INSP FUEL LINE CONNECTIONS, NO FUEL NOTE D ANYWHERE. LAST LEG VENTRAL TANK WAS USED - SPR. SUSPECT FUEL SPILLAGE. CLOSED DOOR IN CABIN. 2 L 7 2 4F 4 F RT A3EU E6WE 2007082400168 20070824 00168 CE 2007 8 24 DXTA200702390 1 20070808 A 2150 A/C PACK CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 921QS 7500241 COCKPIT PAC HAS OIL BURNING ODOR DURING WARM PAC OPERATIONS. REMOVED AND REPLACED COCKPIT ACM TURBINE. I.A.W. CE-750 CH . 21-51-00. OPERATIONAL LEAK CHECKS GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007082400181 20070824 00181 EA 2007 8 24 A6WA200740407 1 20070721 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 LT FS 484 FLOOR SUPPORT INTERCOSTAL ANGLE AT LBL 27 CRACKED APPROX .2 INCH LONG. (K) MAINTENANCE REPAIRED FS 484, LBL 27 ANGLE IAW BOMBARDIER STANDARD REPAIR 601R-53-0029B. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400187 20070824 00187 EA 2007 8 24 A6WA200740413 1 20070722 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 530 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 HYDRAULIC LINE Z-BRACKET (PN 601R75262-153) CRACKED APPROX .1 INCH LONG IN RT MLG WHEEL WELL CEILING. (K) MAINTENANCE REMOVED DAMAGED BRACKET AND INSTALLED SERVICEABLE BRACKET IAW CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400195 20070824 00195 EA 2007 8 24 A6WA200740419 1 20070727 A 5340 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 465AW 7893 HYDRAULIC PRESSURE TRANSDUCER HAT CHANNEL CRACKED APPROX .1 LONG IN LT MLG WHEEL WELL CEILING. (K) MAINTENANCE REMOVED AND REPLACED HAT CHANNEL P/N 601R75262-159 IAW CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400208 20070824 00208 SO 2007 8 24 XGN2007F00020 2 20070718 A 8530 TISN712ACA CYLINDER HEAD BEECH 36 36BEECH 1151602 CE CONT O520 IO520BA 17032 SO ENGINE CRACKED A XGNA O OTHER O OTHER NR NOT REPORTED 1 SW 05 1194A 611 E159 135 ECI, REV 3, E SERIES, CYLINDER ASSY, 611.9. SINCE NEW CRACKED ON TOP OF CYLINDER BEHIND FUEL INJECTOR BETWEEN THE (1ST) AND (3RD) FIN. COMPRESSION CHECK WITH SOAPY WATER REVEALED CRACK. CAN NOT BE SEEN WITH THE NAKED EYE. (K) 1 L 7 1 3O 3 O 3A15 E5CE 2007082400217 20070824 00217 NM 2007 8 24 KCSA071318 1 20070821 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 AFT PIT SEAT TRACK LOWER FLANGE CRACKED AT BS 1490, RBL 46. 2 L 7 4 4F RT A20WE 2007082400219 20070824 00219 NM 2007 8 24 KCSA071319 1 20070821 A 5313 STRINGER BOEING 747 7472B4B 138481B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STR 29L DAMAGED AT SKIN ATTACHMENT FLANGE, BS 2186. 2 L 7 4 4F RT A20WE 2007082400220 20070824 00220 NM 2007 8 24 KCSA071320 1 20070821 A 5311 FRAME BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 FUSELAGE FRAME UPPER CHORD CORRODED AT BS 1860, RBL 6 TO LBL 7. 2 L 7 4 4F RT A20WE 2007082400221 20070824 00221 NM 2007 8 24 SWAA074078 1 20070817 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 619SW 28035 FWD CABIN EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007082400224 20070824 00224 NM 2007 8 24 SWAA074107 1 20070819 A 3350 20131A BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007082400228 20070824 00228 NM 2007 8 24 SWAA074086 1 20070817 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, RBL 5. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2007082400251 20070824 00251 NM 2007 8 24 SWAA074092 1 20070817 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007082400256 20070824 00256 NM 2007 8 24 SWAA074096 1 20070817 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER 23L CORRODED AT BS 370. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007082400270 20070824 00270 EU 2007 8 24 COEA0702901 1 20070730 A 5311 S53572601207 FRAME AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE FUSELAGE CRACKED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 02 901FX 172 IN HEAVY CHECK IN COE PERFORMED PERMENANT REPAIR TO CRACK ON RT HYDRAULIC LINE CUTOUT AT FRAME 25. COMPLIED WITH PERMEN ANT REPAIR IAW SB ATR42-53-0121. WO 69645 NR 903003 (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007082400272 20070824 00272 EA 2007 8 24 TRAX200701172 1 20070812 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 874AS 7551 FS 349 FRAME IS CORRODED AT BL 0.0. INSTALLED RADIUS BLOCKS AND HI-LOK FASTENERS AT OUTBOARD ENDS OF FRAME SECTION. IN STALLED FASTENERS RELATED TO DRAIN MAST DOUBLER AND CLIPS AT END OF DOUBLER VERTICAL STRUCTURE, AND INTERCOSTAL INBOARD OF DRAIN MAST. INSTALLED HI-LOK RELATED TO DOOR TRACK SLIDE RAILS MOUNTED TO THE TOP PORTION OF FRAME ASSY AT FS 349. ALL WORK ACCOMPLISHED IAW CRJ 200 51-42-06, 51-42-21. SUPPLEMENTAL - SDR CLOSED 08/21/07. 2 L 7 2 4F RT A21EA 2007082400273 20070824 00273 EA 2007 8 24 TRAX200701175 1 20070812 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 874AS 7551 FRAME 625 CLIPS ARE CRACKED ON THE LT AND RT SIDE (MARKED). REMOVED AND REPLACED LT AND RT 625 CLIPS IAW CRJ 200 SRM 51 -00-00, LT 10397. SUPPLEMENTAL - SDR CLOSED 08/21/07. 2 L 7 2 4F RT A21EA 2007082400285 20070824 00285 NM 2007 8 24 SWAA074114 1 20070820 A 3350 767 LIGHT BOEING 737 7373Q8 1384670 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED SERVICE CHECK, FOUND RIGHT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007082400290 20070824 00290 EA 2007 8 24 TRAX200701205 1 20070817 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 874AS 7551 LEFT BONDED SKIN DOUBLER IS CRACKED. FS 640 AT ENGINE SUPPORT BEAM. WORK DONE IAW REO 601R-53-61-506. 2 L 7 2 4F RT A21EA 2007082400291 20070824 00291 EA 2007 8 24 TRAX200701206 1 20070817 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 880AS 7606 LEFT BONDED SKIN DOUBLER CRACKED AT FS 640.00. REO 601R-53-61-506 REV-C CARRIED OUT. 2 L 7 2 4F RT A21EA 2007082400294 20070824 00294 EA 2007 8 24 TRAX200701209 1 20070817 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 881AS 7496 LEFT FS 621 TO FS 625 OBLIQUE ANGLE CRACKED. LOCATED AND DRILLED SERVICEABLE OBLIQUE ANGLE IAW CRJ 200 SRM 51-40-11. 2 L 7 2 4F RT A21EA 2007082400297 20070824 00297 EA 2007 8 24 TRAX200701212 1 20070817 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 355CA 10067 CAPT`S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007082400299 20070824 00299 EA 2007 8 24 VNAA0708002 1 20070807 A 3610 MS9068038 O-RING CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE A/C BAY DAMAGED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 719PS 10177 CREW REPORTED A RIGHT HAND BLEED DUCT MASTER WARNING MESSAGE DURING CLIMBOUT. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE O-RING DAMAGED ON THE FLANGE FROM THE RIGHT HAND PACK HEAT EXCHAN GER TO THE ACM CONNECTION. MAINTENANCE REMOVED AND REPLACED THE O-RING IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANU AL. OPS CHECKS GOOD AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007082400301 20070824 00301 CE 2007 8 24 2007F00043 1 20070705 A 5610 10150413S WINDSHIELD BEECH 200 B200 1152922 CE PWA PT6 PT6* 52043 EA COCKPIT CRACKED E WAIA O OTHER O OTHER DE DESCENT 1 SW 09 177LA 7118 BB1203 AIRCRAFT DEPARTED, ENROUTE, ABOUT 45 MINUTES INTO FLIGHT, CREW REPORTED THEY WERE AROUND FL220 AND STARTED THEIR DESCEN T INTO CMS, WHEN AT FL190 THE PILOTS WINDSHIELD CRACKED AND SPIDERWEBBED ACROSS THE ENTIRE WINDSHIELD. CREW LANDED THE AIRCRAFT WITHOUT ANY OTHER ISSUES. REPLACED WINDSHIELD AS REQUIRED IAW MM. (K) 1 L 7 2 4T 3 T A24CE E2NE 2007082400303 20070824 00303 SO 2007 8 24 XGN2007F00023 2 20070718 A 8530 TISN712ACA CYLINDER BEECH 36 36BEECH 1151602 CE CONT O520 IO520BA 17032 SO NR 2 CRACKED A XGNA O OTHER O OTHER NR NOT REPORTED 1 SW 05 1194A 611 E159 907201R REV 3, E SERIES, CYL ASSY 611.9 SINCE NEW. CRACKED ON TOP OF CYLINDER BEHIND FUEL INJECTOR BETWEEN THE FIRST AND THIRD FIN. COMPRESSION CHECK WITH SOAPY WATER REVEALED CRACK CAN NOT SEE WITH THE NAKED EYE. (K) 1 L 7 1 3O 3 O 3A15 E5CE 2007082400318 20070824 00318 NM 2007 8 24 TAMF20070013S 1 20070805 A 5230 STRUCTURE BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE FWD CARGO DOOR CORRODED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 767QT 23804 DURING C-CHECK INSPECTION (MFG TASK CARD 53-456-00) WAS FOUND A CORROSION ON FWD CARGO COMPARTMENT CARGO DOOR UPPER SURF ACE, INNER CHORD AT MAIN SILL LARGE CARGO DOOR, BETWEEN STA 544-566. DAMAGED AREA WAS BLENDED OUT AND CORROSION REMOVED IAW SRM 51-10-02 PAGE 12-13. THICKNESS MEASUREMENT WAS MAX: 0.190 IN AND MIN: 0.149 IN. THIS AREA IS WITHIN LIMITS IAW MFG SERVICE REQUEST 1-507196673. FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007082400319 20070824 00319 NM 2007 8 24 TAMF20070014S 1 20070807 A 5410 015T05638 FAIRING BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE NR 2 NACELLE CRACKED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 767QT 23704 DURING C-CHECK INSPECTION WAS FOUND NR 2 NACELLE STRUT NR 446CL ACCESS PANEL DELAMINATED AND CRACKED. ACCESS PANEL WAS FABRICATED AND INSTALLED IAW MFG SERVICE REQUEST 1-50853397 AND DRAWING 015T0563-8. 2 L 7 2 4F 4 F RT A1NM E13NE 2007082400326 20070824 00326 EU 2007 8 24 07FDEA02991 1 20070820 A 5730 A57340086207 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 CHAFING MARKS WERE FOUND ON RT LOWER SURFACE BOTTOM SKIN REINFORCING PLATE AT RIB 7 FRONT SPAR INBOARD. REPAIR PERFORME D BY BLENDING OUT IAW EA 6-5720-106522, APPROVED BY RAS/BAE/1005107/2007 ISSUE "A". 2 L 7 2 4F RT A35EU 2007082400327 20070824 00327 EU 2007 8 24 07FDEA02992 1 20070820 A 5311 A53980044225 FRAME AIRBUS 300 A300B4605R 3930308 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 FOUND SCRATCHED AND DENTED RUN OUT OF FRAME 74 AT P'26-27, RHS. REPAIR PERFORMED BY REWORK IAW EA 6-5318-112466 AND RAS /DAHAM/4022689/2007 ISSUE "A". 2 L 7 2 4F RT A35EU 2007082400328 20070824 00328 EU 2007 8 24 07FDEA02994 1 20070820 A 5730 SKIN AIRBUS 310 A310203 3930313 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 LEFT WING BOTTOM SKIN PANEL NR 2, SKIN CRACKED I/B OF RIB 11, AFT OF REAR SPAR, WRI 57-10 9572, W/C T 6-5710-91017. STO P DRILLED CRACK, AND PERFORMED HFEC INSPECTION IAW A310 NTM 51-10-08 PT6, TO CONFIRM NO CRACK PAST STOP DRILLED AREA. I NSTALLED SKIN DOUBLER IAW BA AIRBUS DWG R57249152, REF: E.A. 6-5710-91017, WINGS LT WING BOTTOM SKIN PANEL NR 2 SKIN, C RACK INBD OF RIB 11, AFT OF REAR SPAR. 2 L 7 2 4F RT A35EU 2007082400329 20070824 00329 EU 2007 8 24 07FDEA02995 1 20070820 A 5313 104155ITL STRINGER AIRBUS 310 A310203 3930313 EU AFT PIT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT LOWER CARGO PIT, CORROSION ON STRINGER 53L BETWEEN FR 64 AND 65. REMOVED, FABRICATED REPAIR SECTION OF STRINGER AND COUPLING AND INSTALLED PER A310-200 SRM 51-40-11, 53-17-14, 51-40-44, 51-40-21DAN 50-04, DAN320B14. 2 L 7 2 4F RT A35EU 2007082400331 20070824 00331 NE 2007 8 24 QXEA200701342 3 20070817 A 6111 SFA13S1P0A BLADE DHAV DHC8 DHC8202 2809007 NM HAMSTD 14SF 14SF* NE NR 2 PROPELLER MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 355PH 89 500 BOI FLIGHT NR 2115, SPARKS OBSERVICED FROM NR 2 PROP ON CLIMB-OUT. REPLACED BLADES NR 1 AND NR 4 ON NR 2 PROP PER TC 96 11003. S/N 9801028-23, TSN 89.53, CSN 134. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 6 C P7NE 2007082400332 20070824 00332 EA 2007 8 24 VNAA0707018 1 20070728 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE WING MALFUNCTIONED A VNAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 05 221PS 7889 CREW REPORTED A FLAPS FAIL AT 20 DEGREES BOTH SIDES ON TAKEOFF. CREW FOLLOWED THE QRH, DIVERTED TO ILM AND LANDED WITH OUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL TESTS OF THE FLAPS IN ACCORDANCE WITH THE AIRCRAFT MAINTE NANCE MANUAL 27-54-00-710-801. NO DEFECTS NOTED AND MESSAGE CLEARED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400333 20070824 00333 EU 2007 8 24 TRAX200701150 1 20070807 A 5311 FRAME AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 FRAME 38 LWR FLANGE BETWEEN STR 21L & 2DL CORRODED. CORROSION REMOVED IAW SRM 57-21-42 ON FR 38. ON CUTOUT IAW NTRU NO EVIDENCE OF CRACKING, FOUND LWR FLANGE 38 REPAIRED IAW TC EO 72-53-0249 MATERIAL THICKNESS .063 MATERIAL REMOVED .030 O UT OF LIMITS PER SRM 53-61-00 FIG 301. SUPPLEMENTAL- SDR CLOSED 08/22/07. 2 H 7 2 4T RT 2007082400334 20070824 00334 EU 2007 8 24 TRAX200701153 1 20070810 A 5720 ANGLE AEROSP ATR72 ATR72 EU LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 CRACK FOUND AT FR 27 STR 4L BEHIND WING FITTING ON FORMED PART. EC PERFORMED IAW NTM CRACK CONFIRMED TO RIVET AND DOES NOT EXTEND BEYOND. CRACK CONFIRMED IN RADIUS FROM AFT EDGE RUNNING FWD. CRACK ON LEFT WING PRESSURE DECK SPLICE ANGLE INSPECTED AND FOUND ACCEPTABLE PER EO 72-53-0250. SUPPLEMENTAL - SDR CLOSED 08/22/07. 2 H 7 2 4T RT 2007082400335 20070824 00335 EU 2007 8 24 TRAX200701155 1 20070810 A 5210 SKIN AEROSP ATR72 ATR72 EU PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 THREE CRACKS FOUND ON PAX DOOR INNER SKIN 2 UPPER AFT CORNER & 1 UPPER MIDDLE. THREE CRACKS ON PAX DOOR INNER SKIN. UP PER AFT CORNER AND UPPER MIDDLE REPAIRED IAW SRM 52-11-00 FIG 412. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORD ANCE WITH SP 663 AND FAR 43 APPENDIX A. REPAIR ACCOMPLISHED IN WORK COMPLETED WITH SRM 52-11-00 FIG 412. SUPPLEMENTAL - SDR CLOSED 08/22/07. 2 H 7 2 4T RT 2007082400336 20070824 00336 EU 2007 8 24 TRAX200701162 1 20070811 A 5210 INTERCOSTAL AEROSP ATR72 ATR72 EU PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 PAX DOOR 2 INTERCOSTALS CRACKED FWD & AFT OF BOTTOM ROLLER. PAX DOOR 2 INTERCOSTALS REPLACED FWD AND AFT OF BOTTOM ROLL ER IAW SRM 51-25-01 AND 51-25-04, FABRICATION OF 2 INTERCOSTALS COVER ON W/C 2000-158 REPAIR DETERMINED NOT TO BE A MAJO R REPAIR IAW SP663 AND FAR 43 APPENDIX A. REPAIR ACCOMPLISHED IAW SRM 51-25-01 AND 51-25-04. SUPPLEMENTAL - SDR CLOSED 08/22/07. 2 H 7 2 4T RT 2007082400343 20070824 00343 EA 2007 8 24 TRAX200701217 1 20070818 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDS A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 880AS 7606 PAX DOOR HARD TO CLOSE. 2 L 7 2 4F RT A21EA 2007082400344 20070824 00344 EA 2007 8 24 TRAX200701218 1 20070818 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 880AS 7606 LEFT BONDED SKIN CRACKED AT FS 640.00 REO 601R-53-61-506 REV C TO BE CARRIED OUT. 2 L 7 2 4F RT A21EA 2007082400346 20070824 00346 NM 2007 8 24 SWAA074135 1 20070821 A 3350 20131A BATTERY PACK BOEING 737 7373Q8 1384670 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED BRDG CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007082400347 20070824 00347 NM 2007 8 24 SWAA074124 1 20070821 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 358SW 26595 FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007082400349 20070824 00349 NM 2007 8 24 SWAA074137 1 20070821 A 5330 6545766 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 374, STR 26L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007082400350 20070824 00350 NM 2007 8 24 SWAA074138 1 20070821 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CREASED AT BS 426, STR 17R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007082400351 20070824 00351 NM 2007 8 24 SWAA074120 1 20070821 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, BETWEEN RBL 3 AND LBL 3. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007082400353 20070824 00353 NM 2007 8 24 SWAA074130 1 20070821 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007082400354 20070824 00354 NM 2007 8 24 SWAA074131 1 20070821 A 5311 6546541 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 1. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007082400355 20070824 00355 NM 2007 8 24 SWAA074132 1 20070821 A 5310 6546817 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 500A AND BS 500C, STR 17L. REMOVED AND REPLACED C REASE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2007082400356 20070824 00356 NM 2007 8 24 SWAA074126 1 20070821 A 5330 6546881 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1016, STR 20L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007082400357 20070824 00357 NM 2007 8 24 SWAA074134 1 20070821 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2007082400361 20070824 00361 NM 2007 8 24 SWAA074122 1 20070821 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007082400365 20070824 00365 NM 2007 8 24 CALA0700450 1 20070821 A 5320 6545819U45 GUSSET BOEING 737 7373T0 1384582 NM NLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A .5 INCH CRACK IN RADIUS OF NOSE WHEEL WELL GUSSET AT AFT END OF NLG ACTUATOR SUPPORT FITTING, NWW STA 251, BL 0. THE GUSSET WAS REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007082400374 20070824 00374 NM 2007 8 24 GAIA0711OP 1 20070802 A 2612 FIRE DETECTOR BOEING 727 727214 138407R NM APU BAY FALSE INDICATION A GAIA F ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SW 07 750US 21512 FLT 706 - DFW-IAH - DURING CLIMB, THE FLIGHT CREW HAD AN INDICATION OF AN APU FIRE. THE APU FIRE HANDLE WAS PULLED AND THE FIRE BOTTLE WAS DISCHARGED. THE AIRCRAFT CONTINUED TO IAH AND AN UNEVENTFUL LANDING WAS MADE. INSPECTED APU AREA A ND FOUND NO EVIDENCE OF FIRE. REMOVED AND REPLACED APU FIRE BOTTLE AND DISCHARGE INDICATOR DISK. APU FIRE TEST NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2007082400375 20070824 00375 NM 2007 8 24 GAIA07012OP 1 20070802 A 3350 1000679 LIGHT BOEING 727 727214 138407R NM COCKPIT INOPERATIVE A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 751US 21513 DURING PS CHECK, FOUND CONTROL CABIN EMERGENCY EXIT LIGHT WOULD STAY ON WITH THE SWITCH IN THE OFF POSITION. REMOVED AN D REPLACED EMERGENCY EXIT LIGHT. OPS CHECK NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2007082400376 20070824 00376 EA 2007 8 24 A6WA200740434 1 20070731 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 466AW 7899 LT SIDE FS 621 TO FS 625.30 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX .8 INCH LONG. (M) 2 L 7 2 4F RT A21EA 2007082400377 20070824 00377 EA 2007 8 24 A6WA200740435 1 20070731 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 466AW 7899 FOUND RT SIDE FS 621 TO FS 625.30 INTERCOSTAL AT STRINGER 14R IS CRACKED NEAR RADIUS APPROX 1 INCH LONG. (M) 2 L 7 2 4F RT A21EA 2007082400379 20070824 00379 EA 2007 8 24 A6WA200740437 1 20070804 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 466AW 7899 FOUND PASSENGER DOOR AFT DRAG ANGLE IS CRACKED. (M) 2 L 7 2 4F RT A21EA 2007082400381 20070824 00381 EA 2007 8 24 A6WA200740439 1 20070806 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 466AW 7899 FOUND RIGHT 621 FLOOR SUPPORT ANGLE IS CRACKED. (M) 2 L 7 2 4F RT A21EA 2007082400382 20070824 00382 EA 2007 8 24 A6WA200740440 1 20070803 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 465AW 7893 FOUND LEFT FS 621 FLOOR SUPPORT ANGLE CRACKED. (M) MAINTENANCE REPAIRED IAW REO 601R-53-61-117. (M) 2 L 7 2 4F RT A21EA 2007082400383 20070824 00383 EA 2007 8 24 A6WA200740441 1 20070803 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 465AW 7893 FOUND RIGHT FS 621 FLOOR SUPPORT ANGLE CRACKED. (M) MAINTENANCE REPAIRED IAW REO 601R-53-61-117. (M) 2 L 7 2 4F RT A21EA 2007082400384 20070824 00384 EA 2007 8 24 A6WA200740388 1 20070712 A 2121 FAN CNDAIR CL600 CL6002B19 1900309 EA LAVATORY INOPERATIVE A A6WA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 31 444ZW 7788 BURNING RUBBER SMELL IN LAV. FOUND LAV EXHAUST FAN INOPERATIVE. REMOVED AND REPLACED LAV EXHAUST FAN IAW AMM 21-23-13. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007082400385 20070824 00385 EA 2007 8 24 A6WA200740431 1 20070730 A 2730 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA PITCH TRIM FAILED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 GL 31 462AW 7875 CAUTION MESSAGE INFLIGHT, STAB TRIM, MACH TRIM, AUTOPILOT TRIM NOSE DOWN. PITCH STUCK AT 6.0. WHEN AUTOPILOT DISENGAGE D AT 1000` AGL ALL MESSAGES DISAPPEARED PITCH TRIM WAS OPERATIONAL. HSTCU FAIL, REMOVED AND REPLACED HSTCU IAW 27-41-01 , NO FAULTS NOTED. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007082400388 20070824 00388 NM 2007 8 24 NWAA072876301 1 20070818 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 661US 23719 DURING OVERNIGHT CHECK, FOUND 2 AFT EMERGENCY RIGHT OVERWING LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY . OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007082400389 20070824 00389 WP 2007 8 24 NWAA072889858 1 20070820 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 767NC 47724 TAIL COMPARTMENT EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. OPERATION CHECKS GOOD. 2 L 7 2 4F RT A6WE 2007082400390 20070824 00390 EU 2007 8 24 TRBA2007069 1 20070820 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT FAILED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 355AT 355 SEVERAL FLOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK 61WL AS PER JIC 33-51-21. 2 H 7 2 4T RT A53EU 2007082400392 20070824 00392 NM 2007 8 24 2007UALA03205 1 20070816 A 2560 COFFEEMAKER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE GALLEY ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 WP 29 905UA 25005 BURNING WIRE ODOR REPORTED IN CABIN. CLEANED BURNED COFFEE OFF FWD GALLEY COFFEE MAKER HOT PLATE. NO WIRES FOUND BURNE D. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082800001 20070828 00001 2007 8 28 2007UALA03207 4 20070816 A 3417 ADC BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 119UA 28812 RTFL DUE TO FIRST OFFICER'S ASI HUNG FOLLOWED BY IAS DISAGREE. REPLACED RIGHT AIR DATA COMPUTER. BITE TESTED THRU CENTR AL MTCE COMPUTER. TEST PASSES. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082800003 20070828 00003 NM 2007 8 28 2007UALA03209 1 20070816 A 5532 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE VERTICAL STAB DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 DORSAL FIN SKIN STA 860 PHENOLIC STRIP TORN AND POSSIBLE SKIN WEAR WHERE STRIP WAS TORN. REPAIRED AND INSTALLED DORSAL FIN. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082800006 20070828 00006 NM 2007 8 28 2007UALA03212 1 20070816 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 639 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 FOUND CREASE BEAM WEB CRACKED AT BS 639L, LBL 62. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR ON CREASE BEAM W EB. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082800007 20070828 00007 NM 2007 8 28 2007UALA03213 1 20070816 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 327UA 24147 FWD CARGO DOOR OPENING, AFT FRAME IS CRACKED AT LOWER STOP FITTING. REPAIRED FWD CARGO DOOR AFT FRAME PER MM 53-30-75 P G 801-815. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082800012 20070828 00012 NM 2007 8 28 2007UALA03218 1 20070817 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 FOUND SEAT 2A AFT EMERGENCY LIGHT AND ROW 47 HJK EMERGENCY LIGHTS INOPERATIVE. 08-31-07 RELAMPED EMERGENCY LIGHTS, BOTH POSITIONS. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082800013 20070828 00013 NM 2007 8 28 2007UALA03219 1 20070817 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 42 ABC UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 FOUND ROW 42 ABC EMERGENCY LIGHT INOPERATIVE. 08-31-07 RESECURED EMERGENCY LIGHT CONNECTOR. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082800014 20070828 00014 NM 2007 8 28 2007UALA03220 1 20070817 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 53 ABC INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 FOUND ROW 53 ABC EMERGENCY LIGHT INOP. 08-31-07 RESECURED EMERGENCY LIGHT. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082800015 20070828 00015 NM 2007 8 28 2007UALA03221 1 20070817 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 FOUND ROW 24 EMERGENCY LIGHTS INOP. 08-31-07 RELAMPED EMERGENCY CEILING LIGHT . OP CK NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082800016 20070828 00016 NM 2007 8 28 2007UALA03222 1 20070817 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 VCC CABINET OUTER WALL, EEL WIRE BROKEN. 08-31-07 REPLACED EEL CABLE, OP CHECKED OK PER MM 33-50-96. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082800017 20070828 00017 EU 2007 8 28 2007UALA03223 1 20070816 A 2150 A/C PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 INOPERATIVE A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 413UA 470 CAPTS EMERGENCY AUTHORITY USED TO OPERATE PACK 1 DUE TO FAILURE OF PACK 2 TO COOL AC. PACK 2 WEAK AIRFLOW AND OUTLET TEMP (REPORTED BY CREW) ACTUAL CAUSE NEVER DETERMINED. ALL TESTS PERFORMED ON BOTH PACKS ON GROUND WERE NORMAL. COULD NOT DUPLICATE ON GROUND. REPORT: PACK 2 UNABLE TO COOL CABIN. COMPRESSOR OUTLET TEMP 115 PACK OUTLET TEMP 15. POST FLIGHT, NO FAULTS. BITE CK NO FAULTS. OP CK BOTH PACKS,TEMP INDICATIONS SAME ON GRND . VISUAL INSP CK OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082400020 20070824 00020 NM 2007 8 24 QXEA200701327 1 20070808 A 5755 WEB DHAV DHC8 DHC8202 2809007 NM LT WING SPOILER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 C5 PDX - WEB STRUCTURE BELOW LEFT WING OUTBOARD SPOILER OUTBOARD LIGHTNING HOLE CRACKED. REPAIRED IAW SRM 51-40-00 AND 51-40-11. 2 H 7 2 4T RT A13NM 2007082400033 20070824 00033 NM 2007 8 24 TSAA0721046 1 20070815 A 2160 6075103 SENSOR BOEING 737 737282 13844AT NM TEMP FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 824AL 23045 NON-ETOPS FLIGHT 63 HNL-LIH, DURING CLIMB, THE CREW NOTED LOUD NOISE AND ICE EMANATING FROM THE AIR CONDITIONING SYSTEM. THE CREW ATTEMPTED TO CONTROL THE NOISE AND ICE BY SELECTING A WARMER TEMPERATURE WITH NO CHANGE IN CONDITION. THE NO ISE WAS DISRUPTIVE TO THE CREW AND THEY ELECTED TO RETURN TO HNL. THE AIRCRAFT LANDED IN HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE 35º TEMPERATURE SENSOR AND THE 35º TEMPERATURE CONTROL PER AMM 21-51-0 WITH ALL CH ECKS NORMAL. 2 L 7 2 4F RT A16WE 2007082400034 20070824 00034 EU 2007 8 24 TRAX200701114 1 20070804 A 5320 INTERCOSTAL AEROSP ATR72 ATR72 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 IN RT MLG ON FR 27 INTERCOSTAL FOUND CRACKED AT RBL 23. RT MLG ON FR 27 INTERCOSTAL REPLACED AS PER SRM 51-25-01. REPA IR DETERMINED NOT TO BE A MAJOR REPAIR IAW SP 663 AND FAR 43 APPENDIX A REPAIR ACCOMPLISHED IAW SRM 51-25-01. SUPPLEMEN TAL - SDR CLOSED 08/16/07. 2 H 7 2 4T RT 2007082400035 20070824 00035 2007 8 24 HALA0700347 4 20070817 A 2565 LAMP BOEING 767 767332 1382001 NM SLIDE INDICATOR INTERMITTENT A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 597HA 23277 1R SLIDE INDICATOR FLICKERING. RE-LAMPED 1R SLIDE INDICATOR LIGHT. OP CK GOOD. 2 L 7 2 4F RT A1NM 2007082400040 20070824 00040 EU 2007 8 24 AWXA200701003 1 20070804 A 5321 D536106050000 FLOORBOARD AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 632AW 81 SAL - MAJOR REPAIR - C-7 CHECK - NR 5980237, CORROSION ON CABIN FLOORBOARD 221FF, BS 709 / FR 16 - BS 808 / FR 20, +Y129 2 TO +Y1732. REPLACED CABIN FLOOR BOARD 221FF, BS 709 / FR 16 - BS 808 / FR 20, +Y1292 TO +Y1732 IAW AWA TASK CARD C1D2 5306. 2 L 7 2 4F RT A28NM 2007082400056 20070824 00056 EU 2007 8 24 07FDEA02975 1 20070820 A 5330 A57110203 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 DENT ON C48-49 CENTER SECTION UPPER SKIN BETWEEN TRACK 1-2 RT DENT ACCEPTABLE AS IT IS APPROVED BY EA 6-5315-112438 AND RAS 052577/013/2007 ISS A. 2 L 7 2 4F RT A35EU 2007082400057 20070824 00057 EU 2007 8 24 07FDEA02976 1 20070820 A 5310 STRUCTURE AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 STRUCTURE CORRODED BETWEEN C65- 70, P 56-57 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007082400058 20070824 00058 EA 2007 8 24 COMA0760522 1 20070806 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 814CA 7387 FLIGHT 5179 - DURING CLIMB PAX DOOR OUTER HANDLE CAUTION MESSAGE APPEARED. FOLLOWED QRH MESSAGE WENT AWAY. AIRCRAFT LA NDED SAFELY BACK AT RIC. TRANSFERRED TO DEFERRED LIST PER MEL 52-70-01-1. 2 L 7 2 4F RT A21EA 2007082400059 20070824 00059 EU 2007 8 24 07FDEA02977 1 20070820 A 5310 STRUCTURE AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 AFTER BLEND OUT OF HEAVY CORROSION ON FOLLOWING PART AT 69 BULK CARGO DOOR CUT OUT, REMAINING THICKNESS IS UP TO 50 PERC ENT. REPAIR PERFORMED BY REPLACEMENT OFF MENTIONED PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007082400075 20070824 00075 NM 2007 8 24 SWAA074050 1 20070815 A 2121 6454051 FAN BOEING 737 7377H4 1384404 NM E&E BAY MALFUNCTIONED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 29 231WN 32499 CABIN HAD A BURNING PLASTIC ODOR, WHEN GASPER FAN TURNED, ODOR DISSIPATED. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2007082400076 20070824 00076 NM 2007 8 24 SWAA074044 1 20070815 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 385, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007082400077 20070824 00077 NM 2007 8 24 SWAA074047 1 20070815 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007082400083 20070824 00083 NE 2007 8 24 SWAA074051 2 20070812 A 7200 CFM567B24G22 ENGINE BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B22 13802 NE NR 2 FAILED A SWAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS DE DESCENT 1 SW 29 244WN 34864 892931 NR 2 ENGINE FAILED DURING POWER ON DESCENT PASSING FL 320. AFTER SHUT DOWN N2 WAS AT ZERO. REMOVED AND REPLACED NR 2 E NGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007082400088 20070824 00088 EA 2007 8 24 COMA0760527 1 20070811 A 2760 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA SPOILER SYS MALFUNCTIONED A COMA K NONE N FALSE WARNING CR CRUISE 1 SO 01 735CA 7267 FLIGHT 5599 - RECEIVED FLIGHT SPOILER CAUTION IN FLIGHT. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. RESET SPOILER SYSTEM PER FIM. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007082400089 20070824 00089 EA 2007 8 24 COMA0760524 1 20070812 A 2697 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA FIRE BOTTLE DIRTY A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 798CA 7348 FLIGHT 5195 - RECEIVED CARGO BOTTLE LOW MESSAGE. RETURNED TO SAV, LANDED WITHOUT INCIDENT. CLEANED FIRE BOTTLE CONNECT OR ON LOW PRESSURE SWITCH. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007082400094 20070824 00094 NM 2007 8 24 CALA0700440 1 20070718 A 5310 65479592 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A CRACK IN THE AFT CARGO DOOR CUTOUT STA 794.3 FRAME. THE FRAME WAS REPAIRED IAW ECRA 5311-01344. 2 L 7 2 4F RT A16WE 2007082400108 20070824 00108 NM 2007 8 24 SWAA074058 1 20070816 A 5311 6545815 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE FUSELAGE FRAME CRACKED AT BS 344, STR 24L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007082400114 20070824 00114 NM 2007 8 24 SWAA074065 1 20070816 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2007082400115 20070824 00115 NM 2007 8 24 SWAA074059 1 20070816 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007082400118 20070824 00118 NM 2007 8 24 SWAA074063 1 20070816 A 5754 65C26601 SLAT BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 5 L/E SLAT CRACKED AT LOWER INBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007082400156 20070824 00156 CE 2007 8 24 DXTA200702380 1 20070804 A 2150 SWITCH CESSNA 560 560XL 2076702 CE ACM FAILED E DXTA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 GL 07 659QS 5605359 ACM OVERHEAT ANNUNCIATOR ILLUMINATED AFTER TAKEOFF WITH ASSOCIATED LOUD AIR NOISE AND BURNING ODOR. REMOVED ACM OVERHE AT SWITCH. INSTALLED NEW SWITCH. PERFORMED OSP CHECK AND LEAK CHECK. ALL CHECKS GOOD. ALL WORK DONE I.A.W CE-560XL M/M CH.21-51-00. 2 L 7 2 4F RT A22CE 2007082400184 20070824 00184 EA 2007 8 24 A6WA200740410 1 20070721 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 574 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 FLOOR EDGE MEMBER CRACKED AT FS 574.00. (K) MAINTENANCE REMOVED AND REPLACED DAMAGED PART IAW REO 601R-53-61-1574. (M ) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400191 20070824 00191 EA 2007 8 24 A6WA200740430 1 20070727 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 SKIN UNDER PAX DOOR AFT DRAG ANGLE IS CRACKED AT 3RD FASTENER DOWN APPROX .5 INCH LONG. (K) MAINTENANCE REPAIRED AFT DRAG ANGLE IAW EO 601R-52-12354. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400202 20070824 00202 EA 2007 8 24 A6WA200740426 1 20070728 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 465AW 7893 RT WING LOWER PLANK ACCESS HOLE NR 1 640BB HAS MINO CORROSION IN NON-CRITICAL AREAS APPPROX .003 DEEP AND 2.5 INCH LONG IN (2) PLACES. (K) MAINTENANCE REPAIRED IAW BSC REO 601R-57-21-030 REV F. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400207 20070824 00207 EU 2007 8 24 YENA2007077 1 20070820 A 2150 10007004 ACM EMB ERJ190 ERJ190100IGW 3260408 EU A/C BAY FAULTY A YENA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 EA 15 198JB 4096 19000021 FLT 422, PBI-BOS, ON SHORT FINAL COCKPIT VENTILATION DELIVERED WARM AIR THEN CREW SMELLED SMOKE. REPLACED AIR CYCLE MAC HINE IN PACK IAW 21-51-00, OPS NORMAL. OLD ONE FOUND SMELLED OUT. 2 L 7 2 4F RT A57NM 2007082400211 20070824 00211 EA 2007 8 24 A6WA200740420 1 20070727 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 465AW 7893 HYDRAULIC PRESSURE BRACKET IS CRACKED APPROX .1 INCH LONG IN RT MLG WHEEL WELL CEILING. (K) MAINTENANCE REMOVED AND RE PLACED HAT CHANNEL P/N 601R75262-157 IAW CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400212 20070824 00212 NM 2007 8 24 GAIA0708 1 20070724 A 2697 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE NR3 ENG PYLON SHORTED A GAIA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 SW 07 180AX 20041 DURING DECENT, THE NR 3 ENGINE HAD A FIRE INDICATION. THE FLIGHT CREW ACCOMPLISHED THE CHECK LIST AND SHUTDOWN THE ENGI NE AND FIRED BOTH FIRE BOTTLES. THE ENGINE FIRE LIGHT NEVER EXTINGUISHED. AN UNEVENTFUL LANDING WAS MADE. INSPECTION REVEALED A SHORTED WIRE IN THE NR 3 ENGINE PYLON AT PLUG P400. THE WIRE WAS REPAIRED AND THE ENGINE, OIL FILTER AND CHI P DETECTOR WERE CHECKED. THE ENGINE FIRE BOTTLES WERE REPLACED AND THE ENGINE OPS CHECKED GOOD ON THE GROUND. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 3 4F 4 F A3WE E2EA 2007082400218 20070824 00218 NM 2007 8 24 GAIA07007 1 20070712 A 3350 1000679 LIGHT BOEING 727 727251 138408H NM PWA JT8 JT8D15 52051 NE COCKPIT INOPERATIVE A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 NO FLIGHT: THE COCKPIT DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED EMERGENCY COCKPIT LIGHT. OPS CHECK NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 3 4F 4 F A3WE E2EA 2007082400232 20070824 00232 NM 2007 8 24 SWAA074083 1 20070817 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733E, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007082400233 20070824 00233 NM 2007 8 24 SWAA074105 1 20070819 A 5753 6546434302 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED MV1 CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD T/E END. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007082400237 20070824 00237 CE 2007 8 24 081507N316CS1 1 20070815 A 3240 57C57652 ACCUMULATOR CESSNA 500 550 2076604 CE BRAKES MALFUNCTIONED E Z5FA D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 EA 63 316CS 5501010 POWER BRAKE VALVE REPLACED FOR MAKING UNUSUAL NOISES DURING BRAKING. ON TAXI OUT, COPILOT'S RT BRAKE PEDAL LOST BRAKING ACTION. AIRCRAFT RETURNED TO GATE, MAINTENACE TROUBLESHOOTING FOUND BRAKE ACCUMULATOR TO BE AT FAULT, REINSTALLED ORIGIN AL POWER BRAKE VALVE, REPACED ACCUMULATOR AND BLED BRAKES, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 4F A22CE 2007082400238 20070824 00238 NM 2007 8 24 SWAA074087 1 20070817 A 5754 65C26603137A SLAT BOEING 737 7373A4 1384585 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED C2 CHECK, FOUND LEFT WING NR 3 L/E SLAT DELAMINATED AT INBOARD END. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 2007082400241 20070824 00241 NM 2007 8 24 SWAA074089 1 20070817 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007082400260 20070824 00260 NM 2007 8 24 CALA0700444 1 20070820 A 5313 BAC1498157 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A 1 INCH CRACK IN STRINGER 16L AT STA 500C + 5. REPAIR PARTS WERE INSTALLED IAW SRM 53-00-03, FIGURE 2 01, REPAIR 1. 2 L 7 2 4F RT A16WE 2007082400261 20070824 00261 NM 2007 8 24 CALA0700445 1 20070819 A 5315 65C33950 FLOORBEAM BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33608 27321 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 986, LBL 12 TO LBL 31. A REPLACEMENT T-CHORD SECTION WAS INSTALLED IAW REPAIR -B- OF ECRA 5310-04494. 2 L 7 2 4F RT A16WE 2007082400271 20070824 00271 EA 2007 8 24 TRAX200701171 1 20070812 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 874AS 7551 FS 333 FRAME IS CORRODED AT BL 0.0. INSTALLED LEFT AND RIGHT OUTBOARD HI-LOKS AND RADIUS BLOCKS, DRAIN MAST SUPPORT CLI PS, AND INTERCOSTAL ADJACENT TO DRAIN MAST DOUBLER. ALL WORK ACCOMPLISHED IAW CRJ 200 SRM 51-42-06 AND 51-42-21. SUPPL EMENTAL - SDR CLOSED 08/21/07. 2 L 7 2 4F RT A21EA 2007082400295 20070824 00295 EA 2007 8 24 TRAX200701210 1 20070817 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 881AS 7496 RIGHT FS 621 TO FS 625 OBLIQUE ANGLE CRACKED. LOCATED AND DRILLED NEW OBLIQUE ANGLE PER CRJ 200 SRM 51-42-20, AND REO 601R-53-61-422. 2 L 7 2 4F RT A21EA 2007082400296 20070824 00296 EA 2007 8 24 TRAX200701211 1 20070817 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 680BR 7679 F/A'S FLASHLIGHT IS INOP. 2 L 7 2 4F RT A21EA 2007082400300 20070824 00300 EA 2007 8 24 VNAA0708001 1 20070801 A 2710 TRIM SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AILERON SYSTEM OUT OF LIMITS A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 259PS 7945 CREW REPORTED ON TAKEOFF ROLL, RECEIVED A RED WARNING MESSAGE INDICATING A TAKEOFF CONFIGURATION. CREW ABORTED THE TAKE OFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE AILERON TRIM OUT OF LIMITS FOR TAKEO FF CONFIGURATION. MAINTENANCE CONFIGURED THE AILERON TRIM WITHIN LIMITS IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MAN UAL. OPS CHECKS GOOD AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400330 20070824 00330 EU 2007 8 24 07FDEA02996 1 20070820 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT LOWER CARGO PIT STRINGER 52R HAS CORRODED ANGLE WITH MISSING FASTENERS BETWEEN FR 58 AND 59. [08-29-07] REMOVED STRINGER SECTION AND ANGLE IAW A310-200 51-40-21 PARA 6. FABRICATED NEW STRINGER 52R SECTION AND COUPLING IAW SRM 51-1 0-14 FIG 201. ALODINED IAW A310 SRM 51-21-10. PRIMED AND PAINTED IAW A310 SRM 51-23-10. INSTALLED STRINGER AND COUPLIN G IAW A310 SRM 53-10-14 FIG 201. ANGLE IS NOT EFFECTIVE TO THIS A/C PER AIRBUS DRAWING A53974202 WAS NOT RE-INSTALLE D 2 L 7 2 4F RT A35EU 2007082400337 20070824 00337 EU 2007 8 24 TRAX200701163 1 20070811 A 5210 BEAM AEROSP ATR72 ATR72 EU PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 PAX DOOR BEAM ENTRY NR 2 CRACKED. PAX DOOR ENTRY NR 2 REPLACED IAW SRM 51-25-01 AND 51-25-04. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SP663 AND FAR 43 APPENDIX A. REPAIR ACCOMPLISHED IAW SRM 51-25-01 AND 51-25-04. SUPPLEMENTAL - SDR CLOSED 08/22/07. 2 H 7 2 4T RT 2007082400342 20070824 00342 EA 2007 8 24 TRAX200701216 1 20070818 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 902EV 7620 CEILING EMERGENCY LIGHT AT SEAT 5AB INOP. 2 L 7 2 4F RT A21EA 2007082400359 20070824 00359 NM 2007 8 24 SWAA074128 1 20070821 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007082400360 20070824 00360 NM 2007 8 24 SWAA074127 1 20070821 A 5310 65C35243 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER ACO. 2 L 7 2 4F RT A16WE 2007082400362 20070824 00362 NM 2007 8 24 SWAA074121 1 20070821 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007082400363 20070824 00363 NM 2007 8 24 SWAA074123 1 20070821 A 5523 REP4HE8 BEARING BOEING 737 7373K2 13844BA NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 20Y CHECK, LEFT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BEARING PER MM. 2 L 7 2 4F RT A16WE 2007082400378 20070824 00378 EA 2007 8 24 A6WA200740436 1 20070801 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA BS 586 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 466AW 7899 FUSELAGE EXTERIOR LOWER SKIN HAS 2 AREAS OF CORROSION LOCATED AT FS 586 FUSELAGE DRAIN HOLES .1 AREA MEASURES APPROX 1 I NCH BY .75 INCH OTHER AREA MEASURES APPROX .50 INCH BY .50 INCH. BOTH AREAS ARE APPROX .005 INCH DEEP. (M) 2 L 7 2 4F RT A21EA 2007082800018 20070828 00018 EU 2007 8 28 2007UALA03224 1 20070816 A 3230 SELECTOR VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MLG FAILED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 469UA 1409 LGCIU 2 FAULT DISPLAYED ON UPPER ECAM SCREEN, L-G CREW COMMENTS: GOT L-G LGCIU2 FAULT ECAM WHEN GEAR LOWERED FOR LANDING . FOUND SELECTOR VALVE FAILED. REPLACED SELECTOR VALVE 40 GA. NO SHOP FINDINGS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082800019 20070828 00019 NM 2007 8 28 2007UALA03225 1 20070816 A 3250 C24736000CTD CONTROL MODULE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NLG STEERING MALFUNCTIONED A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 832UA 1321 UNCOMMANDED NOSE WHEEL STEERING. NOSE GEAR STEERING SERVO CONTROL MODULE FAILURE. REPLACED NLG STEERING SERVO CONTRO L MODULE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082800020 20070828 00020 2007 8 28 2007UALA03226 4 20070816 A 2565 HOSE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE OVERWING SLIDE CONTAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 RT OVERWING SLIDE INFLATION HOSE (FROM VESSEL TO AIRFRAME) COLLAPSED AND SPONGY. REPLACED SLIDE INFLATION HOSE DUE TO S PONGY & COLLAPSED CONDITION. HOSE ON OVERWING SLIDE INSTALLATION IS IN PROXIMITY OF HYDRAULIC SERVICING ACCESS CONNECTI ONS. SPILLED HYD FLUID COMES IN CONTACT WITH THE HOSE AND DETERIORATES THE HOSE WALLS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082800024 20070828 00024 NM 2007 8 28 2007UALA03230 1 20070818 A 2612 FIRE WARNING BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE APU ILLUMINATED A UALA F ACTIVATE FIRE EXT. J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 222UA 30553 DURING PUSH-BACK, CREW HAD AN APU FIRE WARNING INDICATION. 08-31-07 REPLACED APU. ALSO, ACCOMPLISHED APU FIRE EXTI NQUISHUNG BOTTLE REPLACEMENT PER MM 26-22-01-401. SUSPECT INTERNAL APU FAILURE: SYMPTOMS CONSISTENT WITH T1 BLADE FAI LURE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007082800025 20070828 00025 EU 2007 8 28 2007UALA03231 1 20070819 A 2720 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RUDDER VIBRATION A UALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 29 481UA 1559 RTFL WITH MODERATE RUDDER VIBRATIONS. UPPER AND LOWER RUDDER ACTUATOR ROD ENDS WORN. REPLACED BOTH UPPER AND LOWER SE RVO ROD ENDS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082800026 20070828 00026 EU 2007 8 28 2007UALA03232 1 20070819 A 2612 FIRE WARNING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO BAY ILLUMINATED A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 448UA 842 LANDED UNDER AMBER ALERT DUE TO REAR CARGO COMPARTMENT FIRE INDICATION. NORMAL LANDING AND TAXIED TO GATE. REPLACED S MOKE DETECTION CONTROL UNIT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082800027 20070828 00027 NM 2007 8 28 2007UALA03233 1 20070819 A 2131 CONTROLLER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN PRESSURE FAILED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 326UA 23958 EN ROUTE AIRCRAFT LOST CABIN PRESSURE. FLIGHT DESCENDED AND MADE NORMAL LANDING. REPLACED CABIN PRESSURE CONTROLLER AN D AFT OUTFLOW VALVE. REPLACED UPPER CABIN SAFETY VALVE. FWD CARGO PIT, AFT BULKHEAD BLOWOUT PANEL IS POPPED OUT ALONG T HE LOWER EDGE. SECURED LOWER EDGE OF PANEL INTO RUBBER GASKET. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082800029 20070828 00029 NE 2007 8 28 2007UALA03235 2 20070819 A 8530 VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EXHAUST STICKING A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 642UA 25092 A-C EXPERIENCING EQUIP COOLING FAULTS. V12 OVERBOARD EXHAUST VALVE FOUND TO BE STICKING IN THE PARTIALLY CLOSED POSITIO N. REPLACED V12 EXHAUST VALVE. DIDN'T SOLVE PROBLEM. :REMOVED & REPLACED EQUIPMENT COOLING OVERHEAT SWITCH. FOUND SUFF ICIENT AIR SOURCE IN DUCTING. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082800031 20070828 00031 NM 2007 8 28 2007UALA03237 1 20070819 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SEAT 1F AFT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 786UA 26938 FOUND SEAT 1F HAS AFT EEL LIGHT INOPERATIVE. 08-31-07 REPLACED LIGHT ASSY. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007082800032 20070828 00032 NM 2007 8 28 2007UALA03238 1 20070816 A 2530 OVEN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY FIRE A UALA F ACTIVATE FIRE EXT. A FLAME/FIRE NR NOT REPORTED 1 WP 29 657UA 27112 GALLEY OVEN R42 CAUGHT ON FIRE. FIRE EXTINGUISED WITH HALON. REPLACED R42 GALLEY OVEN. OPS CKS OK. SUSPECT SHORT IN H EATING ELEMENT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082800035 20070828 00035 NM 2007 8 28 2007UALA03241 1 20070818 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 583UA 26705 R-1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082800038 20070828 00038 NM 2007 8 28 2007UALA03244 1 20070818 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 646UA 25283 FOUND EEL LIGHTS INOP COACH RIGHT SIDE. REPLACED BATTERY PACK. TESTS OK . 2 L 7 2 4F 4 F RT A1NM E24NE 2007082800040 20070828 00040 NM 2007 8 28 2007UALA03246 1 20070817 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 FOUND CONNOISSEUR CLASS EEL FLOOR RIBBON DAMAGED LEFT AFT SIDE. REPAIRED EEL RIBBON, LEFT HAND, AFT SIDE. LIGHT OP CHEC KED GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082800043 20070828 00043 NM 2007 8 28 2007UALA03249 1 20070817 A 3510 OXYGEN SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 FOUND OXYGEN BELOW 1650 PSI. OXYGEN SYSTEM SERVICED TO FULL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082800046 20070828 00046 NM 2007 8 28 2007UALA03252 1 20070819 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 S14-15L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 FOUND FWD CABIN BS 360 VERTICAL SHEAR TIE IS CRACKED BTWN STR 14L AND 15L. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPLACE MENT SHEAR TIE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082800048 20070828 00048 EU 2007 8 28 2007UALA03254 1 20070717 A 7331 O-RING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUEL FLOW IND LEAKING A UALA O OTHER Y K J ENGINE STOPPAGE FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 436UA 638 DURING TEST FLIGHT, NR 1 ENGINE WOULD NOT RELIGHT IN FLIGHT. HUNG START ECAMS. TRIED 3 WINDMILL AND 3 STARTER ASSIST F OUND FUEL LEAK AT FUEL FLOW INDICATOR REPLACED RING AND RAN ENGINE REF 73-31-17 AND JRH 2-40-1. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082800050 20070828 00050 NM 2007 8 28 2007UALA03256 1 20070819 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 509UA 24763 FOUND DOOR 3L EXTERIOR EMERGENCY LIGHT INOP. REPLACED LAMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082800051 20070828 00051 NM 2007 8 28 2007UALA03259 1 20070818 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1420 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 AFT PIT LEFT FRAME STA 1420 HAS 3 DENTS. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE AND MADE INSURANCE CUT. INSTALLED R EPAIR PER SRM 53-00-07 TR53-20 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082800053 20070828 00053 EU 2007 8 28 2007UALA03261 1 20070820 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 477UA 1514 CREW OXYGEN SYSTEM IS LEAKING. F/O OXYGEN MASK HAS A SLOW LEAK. REPLACED F/O OXYGEN MASK AND SERVICED CREW OXYGEN SYS TEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082800054 20070828 00054 EU 2007 8 28 07FDEA02999 1 20070821 A 5330 A53776532200 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 WEAR MARKS ON THE FUSELAGE SKIN (KARMAN STRUCTURE AREA) BETWEEN FRAME 38.1/39 AND STRINGER 30/32 RT. REPAIR WITH SMOOTH BLEND OUT AND REINSTALLATION OF ORIGINAL OR OVERSIZED FASTENERS IAW EA 6-5314-103265 AND RAS/DA/BRE/7006916/2006 ISS "C ". 2 L 7 2 4F RT A35EU 2007082800055 20070828 00055 EU 2007 8 28 07FDEA03000 1 20070821 A 5330 A53776532200 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 MISDRILLED HOLE (DOUBLEHOLE DIA 9 MM) IN OUTER SKIN BETWEEN FRAME 38.1-38.2, STRINGER 27, LHS. REPAIR PERFORMED WITH REPAIR BUSHING DUE TO MISSDRILLED HOLE IAW SRM 53-10-12/FIG 221 AND EA 6-5314-103335. 2 L 7 2 4F RT A35EU 2007082800056 20070828 00056 EU 2007 8 28 07FDEA03002 1 20070821 A 5320 A53981011200 GUSSET AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 CORRODED GUSSET PLATE AT FRAME 79, STRG 26, LT AND RT. REPAIR PERFORMED BY REPLACEMENT OF PLATES IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007082800060 20070828 00060 WP 2007 8 28 07FDEA03006 1 20070821 A 5313 AYB70201 STRINGER DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 CENTER W/WELL AREA L48L END FITTING CORRODED IN AREAS STA 1509 TO 1521. REMOVED, FABRICATED AND INSTALLED FITTING P/N A YB7020-1 STA 1509-1521 L48L IAW DC/MD10 SRM 51-33-01 VOL II, 53-00-01 FIG 1B VOLII , 51-21-01 VOL1, 51-21-02 VOLII AND D AC DWG AYB 7020. 2 L 7 3 4F RT A22WE 2007082800061 20070828 00061 EU 2007 8 28 07FDEA03007 1 20070821 A 5711 576064A01 SPAR AIRBUS 300 A300F4605R 3930327 EU LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 653FE 736 A 1.5 INCH CRACK EXIST AT LT WING REAR SPAR BETWEEN RIBS 8/9 ACCESS PROVISIONS THROUGH PNL 575FB REF 57-00-00-6 ZONE 500 . INSTALLED S/B NR A300-57-6064 DOUBLERS AT RIB NR 9 AFT OF REAR SPAR (REINFORCEMENT DOUBLERS) COMPLIED WITH EA 6-573 0-110509. 2 L 7 2 4F RT A35EU 2007082800062 20070828 00062 EU 2007 8 28 07FDEA03008 1 20070821 A 5730 R57340199001 SKIN AIRBUS 300 A300F4605R 3930327 EU ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 653FE 736 RT WING LOWER SKIN CRACKED AT T/E ACCESS PANEL 675FB CUTOUT. FORWARD O/B CORNER AREA TOTAL CRACKED LENGTH 1.25 APPROX REF A300-600 SRM 51-10-00. COMPLIED WITH EA 6-5730-110509 REF SB'S A300-600 57-6064 AND 57-6029 DWG R57340199, SMALL R EPAIR PLATE. 2 L 7 2 4F RT A35EU 2007082800066 20070828 00066 EU 2007 8 28 AWXA200701008 1 20070808 A 5320 D53472172200 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSLEAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 632AW 81 SAL - MAJOR REPAIR - C-7 CHECK - NR 5963560, CORROSION ON CABIN FLOORBEAM, BS 3158 / FR 66 TO BS 3207 / FR 68. REPLACED CABIN FLOORBEAM, BS 3158 / FR 66 TO BS 3207 / FR 68 I/A/W A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007082800067 20070828 00067 EA 2007 8 28 SWIA200718580 1 20070630 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 716SK 10180 STA 280 FLOORBEAM IS CRACKED AT RBL9/RBL11, DISCOVERED AT C-CHECK. PERFORMED REPAIR PER CRJ700/900 SRM 51-42-21-001-001 -A01 AND AMM 51-23-00-390-826-A01 DWG SH670-32157. 2 L 7 2 4F RT A21EA 2007082800069 20070828 00069 EA 2007 8 28 SWIA200718582 1 20070630 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 716SK 10180 LT STA 280 WEB CORRODED BEYOND LIMITS, FOUND AT C-CHECK. INSTALLED LT STA 280 WEB PER CRJ700/900 SRM 51-42-06-001. 2 L 7 2 4F RT A21EA 2007082800071 20070828 00071 EA 2007 8 28 SWIA200718584 1 20070630 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 716SK 10180 PAX DOOR AFT WEB IS CRACKED AT 3RD STEP, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO 670-52-11-104 REV 3. 2 L 7 2 4F RT A21EA 2007082800072 20070828 00072 EA 2007 8 28 SWIA200718585 1 20070630 A 5210 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 716SK 10180 PAX DOOR AFT DRAG ANGLE IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REO 670-52-11-072 REV C. 2 L 7 2 4F RT A21EA 2007082800073 20070828 00073 EA 2007 8 28 SWIA200718586 1 20070701 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 724SK 10189 STA 280 BEAM IS CRACKED AT LT AND RT BUTTLINE 9. FOUND AT C-CHECK. REPLACED INBOARD AND OUTBOARD INTERCOSTALS AT LEFT A ND RIGHT POSITIONS AT FS 280.00 PER CRJ700 SRM 51-42-21-001-001-A01. 2 L 7 2 4F RT A21EA 2007082800074 20070828 00074 EA 2007 8 28 SWIA200718587 1 20070701 A 5210 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 724SK 10189 PAX DOOR DRAG ANGLE IS CRACKED, FOUND AT C-CHECK. INSTALLED DRAG ANGLE REPAIR SECTION AND END SPLICE ANGLES PER BOMBARD IER EO 670-52-11-072-C. 2 L 7 2 4F RT A21EA 2007082800075 20070828 00075 EA 2007 8 28 SWIA200718588 1 20070701 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 724SK 10189 FOUND CRACKED AFT WEB BETWEEN STEPS 3 AND 4 ON PAX DOOR, FOUND AT C-CHECK. INSTALLED REPAIR DOUBLER AND SHIMS PER BOMBA RDIER REO 670-52-11-104. 2 L 7 2 4F RT A21EA 2007082800078 20070828 00078 EA 2007 8 28 SWIA200718591 1 20070621 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 452SW 7716 FS 280 FLOOR SUPPORT BEAM IS CRACKED AT RBL9, FOUND AT C-CHECK. COMPLIED WITH REO 601R-53-11-171 REVISION "D" TO REPAIR FS 280 RBL9 FLOOR SUPPORT BEAM. 2 L 7 2 4F RT A21EA 2007082800080 20070828 00080 EA 2007 8 28 SWIA200718593 1 20070628 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 932SW 7714 PAX DOOR AFT DRAG ANGLE IS CRACKED, FOUND AT C-CHECK. INSTALLED NEW PAX DOOR AFT DRAG ANGLE PER CRJ200 SRM 51-42-10 AND 51-42-22 PG 17. 2 L 7 2 4F RT A21EA 2007082800081 20070828 00081 EA 2007 8 28 SWIA200718594 1 20070810 A 5313 STRINGER CNDAIR CL600 CL6002B19 1900309 EA FUSLEAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 CENTER STRINGER JUST AFT OF RADOME IS CRACKED AND NEEDS REPLACEMENT. REPLACED STRINGER AFT OF RADOME IAW CRJ SRM 51-42- 06. 2 L 7 2 4F RT A21EA 2007082800082 20070828 00082 EA 2007 8 28 SWIA200718595 1 20070810 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 RIGHT TRU DOOR SURROUND UPPER STIFFENER IS DAMAGED. REPLACED UPPER STIFFENER ABOVE TRU DOOR IAW CRJ SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007082800083 20070828 00083 EA 2007 8 28 SWIA200718596 1 20070810 A 5310 RIB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 SECOND RIB JUST AFT OF RADOME IS DAMAGED. REPLACED SECOND RIB AFT OF RADOME IAW CRJ SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007082800085 20070828 00085 SO 2007 8 28 SWIA200718598 1 20070630 A 5520 ROD END EMB 120 EMB120ER 3260203 SO LT ELEVATOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 237SW 120314 BOTH ROD ENDS ON AFT LEFT ELEVATOR TRIM TAB HORN ARE CORRODED AND WORN, FOUND AT C-CHECK. REPLACED BOTH ROD ENDS ON LEF T ELEVATOR TRIM TAB WITH SERVICEABLE UNIT IAW MM 27-32-00. 2 L 7 2 4T RT A31SO 2007082800089 20070828 00089 SO 2007 8 28 SWIA200718602 1 20070718 A 2710 CONTROL CABLE EMB 120 EMB120ER 3260203 SO LT AILERONS CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 580SW 120348 LEFT LOWER AILERON CABLE CORRODED AT PULLEY, DISCOVERED AT C-CHECK. REPLACED LEFT LOWER AILERON CABLE IAW AMM 27-00-01. 2 L 7 2 4T RT A31SO 2007082800091 20070828 00091 NM 2007 8 28 F3LA200700202 1 20070817 A 3233 HINGE AIRBUS A319 A319111 3930336 NM MLG ACTUATOR GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 944FR 5528 2700 DURING C-1 CHECK, INSPECTION REPORTED GOUGE ON LT MLG UPPER ACTUATOR HINGE POINT. BLENDED DAMAGE IAW EA A9-53R-12084 AN D SRM 51-73-00. RE-COATED SURFACE IAW SRM 51-75-12. 2 L 7 2 4F RT A28NM 2007082800095 20070828 00095 NM 2007 8 28 QXEA200701345 1 20070820 A 3010 4100S00502 VALVE BOMBDR DHC8 DHC8402 1390042 NM DEICE SYSTEM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 406QX 6665 2394 4048 SEA FLIGHT: DEICE PRESSURE CAUTION LIGHT ILLUMINATED. RUNNING THE CHECKLIST, THE CREW NOTICED THE LEFT OUTBOARD BOOT LI GHT DIDN'T ILLUMINATE. THE DEICE PRESSURE IS NORMAL THROUGH ALL CYCLES. MAINTENANCE REMOVED AND REPLACED NR 5 DDV IAW AMM TASK 30-11-16-000-801 AND TASK 30-11-16-400-801. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007082800097 20070828 00097 NM 2007 8 28 DL76S071049 1 20070809 A 5720 111T20055 STIFFENER BOEING 767 767332 1382001 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 129DL 24079 DURING HMV AT HAECO, THE WING CENTER SECTION FRONT SPAR LBL 10.94 STIFFENER WAS FOUND CRACKED. 2 L 7 2 4F RT A1NM 2007082800098 20070828 00098 NM 2007 8 28 DL76S071053 1 20070809 A 5330 141T3820115 SKIN BOEING 767 767332 1382001 NM BS 228-236 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 129DL 24079 DURING HMV AT HAECO, EXISTING REPAIRS WERE FOUND IN THE CROWN SKIN AREA WHICH WERE DIMPLED AND WAVY. THERE WERE ALSO UN REPAIRED DENTS IN THE ADJACENT AREA. 2 L 7 2 4F RT A1NM 2007082800099 20070828 00099 NE 2007 8 28 DLM90071060 2 20070812 A 7200 ENGINE DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 1 VIBRATION A DALA E ENGINE SHUTDOWN E M J VIBRATION/BUFFET OVER TEMP WARNING INDICATION CR CRUISE 1 SO 27 903DA 24595 53383 020079 AT FL300 THE LT STATOR VANE MSG ILLUMINATED, THE CREW DISCONNECTED THE AUTOTHROTTLES AND KEPT THE LT ENG ABOVE IDLE AS P ER THE QRH. WITH INCREASING VIBS AND EGT CLIMBING THE CREW REDUCED THE THROTTLE TO IDLE AND SHUT DOWN THE ENGINE. LT E NG WINDMILLED FOR LESS THAN 30 MIN WITH AN UNKNOWN BUT POSITIVE OIL PRESSURE. REMOVED AND REPLACED NR 1 ENG PER TRANS 2 T102. 2 L 7 2 4F 4 F RT A6WE E40NE 2007082800100 20070828 00100 NM 2007 8 28 DL76S071066 1 20070813 A 5412 BULKHEAD BOEING 767 767332 1382001 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 129DL 24079 DURING HMV AT HAECO, THE NR 2 PYLON AFT BULKHEAD WAS FOUND CRACKED IN ONE HOLE. 2 L 7 2 4F RT A1NM 2007082800101 20070828 00101 NM 2007 8 28 DL738071071 1 20070813 A 5330 146A320110 SKIN BOEING 737 737832 13844CF NM BS 787 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3748Y 30489 AIRCRAFT STRUCK BY GROUND EQUIPMENT IN MBJ. TEMP REPAIR INSTALLED BY ER/A 463434-14 USING DOUBLER AND TRIPLER OVER DAMA GE TO ALLOW FERRY FLIGHT TO ATL. IN ATL, DAMAGE CUTOUT AND REPAIRED WITH DOUBLER AND STRUCTURAL FILLERS PER ER/A 463435 -14. 2 L 7 2 4F RT A16WE 2007082800103 20070828 00103 NM 2007 8 28 DLM90071085 1 20070720 A 5330 SKIN DOUG MD90 MD9030 3023690 NM BS 218 L18L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 DENT BELOW LONGERON 18L AT STA 218, DENT IS AT A FRAME. REPAIRED IAW MD-80 SRM 53-04D FIG 12B, MD-90 SRM 51-00-01 PG 2 ID REPAIR IAW DAL PROCESS STANDARD 900-5-1 NO 4. 2 L 7 2 4F RT A6WE 2007082800104 20070828 00104 NM 2007 8 28 DLM90071086 1 20070815 A 5730 SKIN DOUG MD90 MD9030 3023690 NM LT WING CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 L WING L/E SKIN CHAFED 2 EA PLACES AT NR 5 SLAT TRACK. REPAIRED LT WING L/E IAW MD-90 SRM 57-20-01 FIG 11 VOL 1. 2 L 7 2 4F RT A6WE 2007082800106 20070828 00106 NM 2007 8 28 DL76S071088 1 20070816 A 5311 145T10017 FRAME BOEING 767 767332 1382001 NM BS 903.5 WL 190 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 129DL 24079 DURING HMV, THE LT AND RT STA 903.5 FRAME INNER CHORDS WERE FOUND CRACKED AT WL 190. THE STUB BEAM FITTINGS WERE ALSO C RACKED. 2 L 7 2 4F RT A1NM 2007082800108 20070828 00108 NM 2007 8 28 DL76L071090 1 20070816 A 2822 PUMP BOEING 767 767332 1382001 NM RT FUEL BOOST FAILED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 174DN 24802 AT PUSHBACK, RT AFT FUEL BOOST PUMP POPPED C/B, RESET NO GOOD. FWD TO MEL 28-22-01A. IT WAS POSSIBLE TO FLT CREW PLAC ARD TO APPLY THIS MEL. THE AIRCRAFT NEEDED MORE FUEL SO HAD TO RETURN TO GATE. REMOVED AND REPLACED BOOST PUMP W MFG P /N 5006003D PER AMM REMOVED MCO AND PL PER MEL 28-22-01A. 2 L 7 2 4F RT A1NM 2007082800111 20070828 00111 NM 2007 8 28 DLM88071093 1 20070817 A 5280 39567851 LINK DOUG MD88 MD88 3023688 NM RT NLG DOOR BROKEN A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 947DL 49878 AFTER GEAR RETRACTION, EXCESSIVE VIBRATION IN NOSE WHEEL AREA. EXTENDED GEAR AND DECLARED EMERGENCY. VIBRATION CONTINU ED AFTER GEAR EXTENSION. FOUND RT NOSE GEAR DOOR LINK BROKEN. REMOVED AND REPLACED RT FWD DOOR LINK PER MM. NOSE GEA R AND DOORS OPERATE NORMAL. 2 L 7 2 4F RT A6WE 2007082800112 20070828 00112 NM 2007 8 28 DLM90071094 1 20070817 A 5330 SKIN DOUG MD90 MD9030 3023690 NM BS 237 L18L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 DENTED BELOW LONG 18L STA 237.8 DENT IS AT FRAME. REPAIRED IAW MD90 SRM 53-30-01 FIG 5. 2 L 7 2 4F RT A6WE 2007082800115 20070828 00115 NM 2007 8 28 DLM90071098 1 20070720 A 5347 900398 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 1212-1304 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 FOUND SEAT TRACK LBL 54 FS 1212 TO 1304 EXFOLIATED CORROSION. REMOVED DAMAGED SEAT TRACK AND REPLACED WITH NEW IAW MD-9 0 SRM 51-30-05, 51-30-1, 51-10-05, 53-40-01 AND 51-10-03. 2 L 7 2 4F RT A6WE 2007082800116 20070828 00116 NM 2007 8 28 DLM90071099 1 20070818 A 5320 5912494501 PAN DOUG MD90 MD9030 3023690 NM CARGO DOOR FRAME CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 FWD PIT DOOR JAMB PAN OUT OF LIMITS STA 375 TO 422 (CORROSION). REPAIRED DOOR JAMB PAN IAW/MD-90 SRM 51-30-01, 51-30-02 , 51-10-05, 53-05D FIG 804. 2 L 7 2 4F RT A6WE 2007082800117 20070828 00117 NM 2007 8 28 DL76L071100 1 20070815 A 4920 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE APU UNKNOWN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 195DN 12363 28452 DURING TRANSIT TIME, APU FAULT. REPLACED APU PER M/M. LEAK CKS OK. APU-AIR GENERATOR, OPS OK. APU OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082800118 20070828 00118 NM 2007 8 28 DL76S071102 1 20070820 A 2710 CONTROL CABLE BOEING 767 767332 1382001 NM LT AILERONS BROKEN A DALA O OTHER F FLT CONT AFFECTED DE DESCENT 1 SO 27 136DL 23146 LEFT OUTBOARD AILERON LOCKED IN DOWN POSITION. FOUND CABLE A3B-3 FOR LT O/B AIL BROKEN JUST O/B OF THE LT O DROOP QUADR ANT. REMOVED BROKEN CABLE RECEIVED NEW CABLE FROM BOEING P/N BACC2C4C04961FG. REPLACED CABLE A3B PER OPN 2000 CABLE RE PLACEMENT AND RIGGED. CHECKED PER M/M. 2 L 7 2 4F RT A1NM 2007082800119 20070828 00119 NM 2007 8 28 DLM88071103 1 20070817 A 5730 SKIN DOUG MD88 MD88 3023688 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 CRACK ON LEFT WING FIXED LEADING EDGE AT STA. XFS=238. REPAIRED PER ERA 380953-14MA ON N/R T0064417 AT HMV IN GDL. 2 L 7 2 4F RT A6WE 2007082800120 20070828 00120 NM 2007 8 28 DLM88071104 1 20070817 A 5310 DOOR FRAME DOUG MD88 MD88 3023688 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 FOUND CORROSION ON C-2 LOWER DOOR JAMB FROM FS=636 TO FS 693 (TASK 51-53300). REPAIRED PER SRM 53-05D FIG 63 ON N/R T00 64848 AT HMV IN GDL. 2 L 7 2 4F RT A6WE 2007082800123 20070828 00123 NM 2007 8 28 DLM88071107 1 20070817 A 5320 SILL DOUG MD88 MD88 3023688 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 PITTING CORROSION ALONG BEAM OF LOWER C-3 DOOR JAMB, TASK 57-53300. REPAIRED PER SRM 53-05 FIG 63 ON N/R T0064677 ON HM V IN GDL. 2 L 7 2 4F RT A6WE 2007082800124 20070828 00124 NM 2007 8 28 DLM88071108 1 20070817 A 5101 SKIN DOUG MD88 MD88 3023688 NM BS 218 NONE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 TEMPORARY REPAIR ON STA 218 AND LONG 23-25 RT, REPAIRED PER SRM 53-04D FIG 12B ON N/R T0064057 ON HMV IN GDL. 2 L 7 2 4F RT A6WE 2007082800125 20070828 00125 NM 2007 8 28 DLM88071109 1 20070817 A 5101 SKIN DOUG MD88 MD88 3023688 NM BS 180 NONE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 TEMPORARY REPAIR ON STA 180 AND BETWEEN LONG 23 AND 25 RT. REPAIRED PER SRM 53-04D FIG 12B ON N/R T0064056 ON HMV IN GD L. 2 L 7 2 4F RT A6WE 2007082800127 20070828 00127 NM 2007 8 28 DLM88071111 1 20070817 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 467-473 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 EXFOLIATION CORROSION ON RT CUSP WEB BETWEEN STA Y=467 TO 473. REPAIR PER ERA 398191-14MA. 2 L 7 2 4F RT A6WE 2007082800128 20070828 00128 NM 2007 8 28 DLM88071112 1 20070817 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 CRACK ON FUSELAGE SKIN FROM FS Y=1439 AND BETWEEN LONGERON 3 RT AND 5 RT, TASK 50-53300. REPAIRED PER SRM 53-04D FIG.27 ON N/R T0064049 ON HMV IN GDL. 2 L 7 2 4F RT A6WE 2007082800130 20070828 00130 NM 2007 8 28 DLM88071114 1 20070817 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 727 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 EXFOLIATION CORROSION ON LT CUSP WEB AT STA 727, REPAIR PER ERA 398191-14MA. 2 L 7 2 4F RT A6WE 2007082800135 20070828 00135 NM 2007 8 28 DLM88071119 1 20070817 A 5340 FITTING DOUG MD88 MD88 3023688 NM BS 1348 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 CRACK ON STRUCTURE OF RIGHT OF AFT PASSENGER DOOR JAMB FITTING WAS REPLACED IAW DWG 5917579. 2 L 7 2 4F RT A6WE 2007082800138 20070828 00138 NM 2007 8 28 DLM88071122 1 20070816 A 5310 STRUCTURE DOUG MD88 MD88 3023688 NM PAX DOOR FRAME CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 FOUND CRACK ON STRUCTURE OF RIGHT SIDE OF AFT PASSENGER DOOR JAMB STA 1348 Z 20. REPLACED IAW DWG 5917579. 2 L 7 2 4F RT A6WE 2007082800139 20070828 00139 NM 2007 8 28 DLM88071123 1 20070817 A 5310 FITTING DOUG MD88 MD88 3023688 NM DOOR FRAME CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 EXFOLIATION CORROSION ON FITTING IN FWD LWR CORNER OF C-3 AT JOINT WITH FUSELUGE SKIN AND DOOR JAMB BEAM. (TASK 57-53300 ). REPLACED PER DRWG, 5930483 ON N/R T0064934 IN HMV AT GDL. 2 L 7 2 4F RT A6WE 2007082800140 20070828 00140 NM 2007 8 28 DLM88071124 1 20070817 A 5320 STIFFENER DOUG MD88 MD88 3023688 NM BS 1338 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 FOUND CRACK ON STIFFENER ON STA 1338 AT 12 HRS POSITION. REPLACED IAW DWG 9915562. 2 L 7 2 4F RT A6WE 2007082800144 20070828 00144 NM 2007 8 28 DLM88071128 1 20070817 A 5320 BRACKET DOUG MD88 MD88 3023688 NM SERVICE DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 FOUND CRACKED AFT BRACKET AT R-1 SERVICE DOOR BEAM NR 4. REPLACED BRACKET PER DRWG 9911582 ON N/R T0065303 IN HMV AT GD L. 2 L 7 2 4F RT A6WE 2007082800145 20070828 00145 NM 2007 8 28 DLM88071129 1 20070817 A 5210 STIFFENER DOUG MD88 MD88 3023688 NM L1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 FOUND CRACKED STIFFENER AT L1 DOOR BEAM NR 8. REPLACED IAW DWG 4916056. 2 L 7 2 4F RT A6WE 2007082800147 20070828 00147 NM 2007 8 28 HALA0700351 1 20070821 A 2612 FIRE LOOP BOEING 767 76733A 1385209 NM LT NACELLE MALFUNCTIONED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM, NR 1 ENG NR 1 FIRE LOOP ON STATUS PAGE. REPLACED TS682 LEFT ENG LOWER AFT FIRE DETECTION LOOP A LUG PER767 WDM26-11-11. OPS CHECKED OK PER FIM 26-11-00. 2 L 7 2 4F RT A1NM 2007082800148 20070828 00148 NM 2007 8 28 HALA0700350 1 20070821 A 4940 97980612 VALVE BOEING 767 76733A 1385209 NM APU STUCK A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 591HA 15194 15194 33423 ETOPS SIGNIFICANT SYSTEM, BTB, APU HAD AUTO SHUT DOWN FAULT LT ILLUMINATED. F/A HEARD UNUSUAL NOISE BEHIND AFT GALLEY. FOUND SURGE VALVE STUCK IN CLOSED POSITION REMOVED AND REPLACED SURGE CONTROL VALVE PER AMM 49-53-01, OPS CK OK. NO FA ULTS NOTED APU OK TO CONTINUE. 2 L 7 2 4F RT A1NM 2007082800149 20070828 00149 NM 2007 8 28 07FDEA02993 1 20070820 A 2131 CONTROLLER BOEING 727 727227 1384078 NM CABIN PRESSURE MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 479FE 21461 CABIN ALT WARNING CLIMBING THROUGH FL270, CABIN ALT SHOWED 10,000, CLOSED CARGO HEAT OUTFLOW VALVE, NO CHANGE IN CABIN A LTITUDE. PERFORMED QRH CABIN ALT WARNING CHECKLIST. THEN PERFORMED FAILURE OF PRESSURIZATION OF CONTROL CHECKLIST. SY STEM WOULD NOT PRESSURIZE IN AUTO OR STBY. IT DID WORK IN MANUAL. OUTFLOW VALVE INDICATED FULL CLOSED IN AUTO AND STBY MODES. REMOVED AND REPLACED PRESSURE CONTROLLER PER M/M 21-31-010-4. OP'S CHECK NORMAL ON GROUND. 2 L 7 3 4F A3WE 2007082800150 20070828 00150 EU 2007 8 28 07FDEA02997 1 20070821 A 5720 A57241993203 ANGLE AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 DAMAGED REINFORCING ANGLE IN KRUEGER FLAP AREA RT WING. REPAIR PERFORMED BY REPLACEMENT OF REINFORCEMENT ANGLE IAW SRM 57-41-11. 2 L 7 2 4F RT A35EU 2007082800152 20070828 00152 EU 2007 8 28 07FDEA03011 1 20070822 A 5230 A52378014204 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 CORROSION ON BULK CARGO DOOR SKIN PANEL (AROUND THE DOOR HANDLE), OUTSIDE. REPAIR PERFORMED BY BLEND OUT UNTIL CORROSIO N REMOVAL IAW EA 6-5234-103310 AND RAS/DABRE/7006925/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007082800154 20070828 00154 EU 2007 8 28 07FDEA03013 1 20070822 A 5311 A53810967 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 SEVERAL DENTS IN DIAPHRAGM FRAME 47-52, TR 1-2 LT AND FRAME 51-53, TR. 2-3 RT, DENTS ACCEPTED IN STATE WITH NDT INSPECTI ON (CRACK FREE) IAW EA 6-5315-103290 AND RAS: 046817/006/2006 ISS."A". 2 L 7 2 4F RT A35EU 2007082400125 20070824 00125 EA 2007 8 24 TRAX200701182 1 20070814 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 857AS 7411 ASD AFT ANCHOR FITTING CRACKED. 2 L 7 2 4F RT A21EA 2007082400132 20070824 00132 EA 2007 8 24 TRAX200701186 1 20070814 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 835AS 7258 SERVICE DOOR WILL NOT OPERATE FROM THE OUTSIDE. 2 L 7 2 4F RT A21EA 2007082400145 20070824 00145 NM 2007 8 24 KCSA071312 1 20070817 A 5313 LONGERON BOEING 747 747212B 1384886 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 LONGERON BOX LOWER CHANNEL AT STA 1438 TO1480 IS DAMAGED AT AFT END WL 100 LBL 113. 2 L 7 4 4F A20WE 2007082400147 20070824 00147 NE 2007 8 24 SROM200700005 2 20070731 A 7220 633758 CASTING BOEING 737 737201 1384454 NM PWA JT8 JT8D15 52051 NE ZONE 600 BROKEN C SROM E A ENGINE SHUTDOWN UNSCHED LANDING E M J VIBRATION/BUFFET OVER TEMP WARNING INDICATION CL CLIMB 1 AL 03 245US 1847 22751 696531 DURING TAKEOFF, AT APPROXIMATELY 300 FEET, CREW EXPERIENCED NR 2 ENGINE COMPRESSOR STALL WITH RAPIDLY RISING EGT. SHUTDO WN NR 2 ENGINE AND MADE UNEVENTFUL LANDING AT DEPARTURE AIRPORT. INSPECTION REVEALED THE NOSE DOME HAD SEPARATED FROM IT S MOUNT DAMAGING THE ENGINE INLET COWL AND C1 COMPRESSOR BLADES. THE FRONT ACCESSORY DRIVE CASTING, NOSE DOME MOUNTING L UG AT THE 2:00 POSITION HAD SEPARATED FROM THE CASTING AND WAS MISSING, PRESUMED INGESTED BY THE ENGINE. THERE IS ALSO E VIDENCE OF FOD FURTHER DOWN THE COMPRESSOR AS WELL AS IN THE ENGINE EXHAUST TAILPIPE. REPLACED NR 2 ENGINE AND ASSOCIATE D INLET COWLING. 2 L 7 2 4F 4 F A16WE E2EA 2007082400155 20070824 00155 CE 2007 8 24 DXTA200702387 1 20070807 A 3230 LANDING GEAR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LEFT MALFUNCTIONED E DXTA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 07 399QS 5600510 LT MAIN GEAR DOWN /LOCKED LIGHT DID NOT ILLUMINATE UPON GEAR EXTENSION, (RED UNSAFE LIGHT DID NOT ILLUMINATE). WHILE PER FORMING EMERG. CHECKLIST AFTER APPROX 10 MINUTES, LEFT GEAR DOWN/LOCK LIGHT ILLUMINATED WITHOUT PILOT INPUT.PERFORMED NUMEROUS GEAR SWINGS. IAW C560 M/M TASK 52-01-00-710. NO LEFT GEAR DISCREPANCIES NOTED. ALL GEAR INDICATIONS NORMAL. 2 L 7 2 4F 4 F RT A22CE E25EA 2007082400162 20070824 00162 NM 2007 8 24 TIPR200736007 1 20070808 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D* NE FUSELAGE CORRODED B K NONE O OTHER IN INSP/MAINT 1 SO 23 609UA 21870 AFT PIT STA 1540, STRINGER 39R, CORROSION AS MARKED. FABRICATED AND INSTALLED STRINGER REPAIR IAW SRM 53-00-03. 2 L 7 2 4F 4 F RT A1NM E20EA 2007082400166 20070824 00166 NE 2007 8 24 HEEA116773 1 20070807 A 6797 WIRE SKRSKY S76 S76C 8143008 NE GE CF34 CF34* NE PITCH SERVO CHAFED B HEEA O OTHER J WARNING INDICATION CR CRUISE 1 SW 03 748P 891 760629 DURING CRUISE, 11 MINUTES AFTER TAKEOFF, NR1 PITCH SERVO FAILED LIGHT CAME ON AND 6 MINUTES LATER NR 2 AHRS FAILED LIGHT CAME ON. THERE WAS NO PITCH CONTROL AVAILABLE THROUGH THE AFCS. THERE WAS NO BEEP TRIM RESPONSE IN THE PITCH AXIS. R ETURNED TO DEPARTURE. MAINTENANCE REPAIRED A CHAFED WIRE. 1 G 7 2 3U 4 F NC H1NE E15NE 2007082400169 20070824 00169 CE 2007 8 24 DXTA200702391 1 20070808 A 3240 BRAKE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG UNKNOWN E DXTA O OTHER O OTHER LD LANDING 1 GL 07 901QS 7500102 BRAKING IS VERY POOR DURING LANDING ROLL. INSPECTED NR 4 BRAKE ASSEMBLY. FOUND WEAR TO BE WITHIN LIMITS. WEAR PIN IS PR OTRUDING 1/16 FROM BRAKE HOUSING WITH PARKING BRAKE SET. PERFORMED BLEEDING PROCEDURES OF ALL FOUR BRAKE ASSEMBLIES. ALS O PERFORMED POWER BRAKE SYSTEM FUNCTIONAL CHECK WITH NO DISCREPANCIES NOTED. CE750 32-42-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007082400180 20070824 00180 CE 2007 8 24 DXTA200702392 1 20070809 A 3240 VALVE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE BRAKE STICKING E DXTA O OTHER O OTHER LD LANDING 1 GL 07 102QS RK380 ON LANDING AND ROLLOUT WHILE BRAKING LT, BRAKE DID NOT OPERATE FROM 3-4 SECONDS THEN GRABS AND PULLS LT SHARPLY. CONFI RMED DISCREPANCY, FOUND POWERBRAKE VALVE STICKING. GAINED ACCESS TO VALVE. REMOVED VALVE AND INSTALLED AN OVERHAULED VA LVE. BLED SYSTEM, PERFORMED FUNCTIONAL TEST AND TAXI CHECKED TO 40KTS. LEAK AND OPS CHECKS GOOD AT THIS TIME. WORK DONE I/A/W HAWKER 400XP M/M 32-40-00. RESTORED ACCESS ITEMS. 2 H 7 2 4F 4 F RT A16SW E25EA 2007082400192 20070824 00192 EA 2007 8 24 A6WA200740416 1 20070725 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 202 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 423AW 7636 FORWARD PRESSURE BULKHEAD AT FS 202.75 CRACKED AT HYDRAULIC SYS NR 3 RT IB BRAKE FITTING LT LOWER SIDE. (K) MAINTENAN CE REPAIRED BULKHEAD IAW BOMBARDIER SERVICES CORP EO 601R-53-12466. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400196 20070824 00196 EA 2007 8 24 A6WA200740421 1 20070727 A 5340 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 465AW 7893 RT 484 ANGLE IS CRACKED AT RBL 36 APPROX .25 INCH LONG. (K) MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-53-41-0 59 REV A AND BOMBARDIER STANDARD REPAIR 601R-53-0030A. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400203 20070824 00203 EA 2007 8 24 A6WA200740427 1 20070728 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 465AW 7893 LT WING LOWER PLANK ACCESS HOLE NR 1 540BB HAS MINOR CORROSION IN NON-CRITICAL AREAS APPROX .003 INCH DEEP AND 5 INCH LO NG IN (2) PLACES. (K) MAINTENANCE REPAIRED IAW REO 601R-57-21-030. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400204 20070824 00204 EA 2007 8 24 A6WA200740428 1 20070728 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 465AW 7893 LT WING PLANK LOWER ACCESS HOLE NR 2 510AB HAS MINOR CORROSION IN NON-CRITICAL AREAS APPROX .005 DEEP AND 5 INCHES LONG. (K) MAINTENANCE REPAIRED IAW REO 601R-57-21-030. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007082400214 20070824 00214 NM 2007 8 24 CALA0700443 1 20070818 A 5311 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 INSPECTION FOUND FORWARD CORROSION AT ACCESS DOOR AFT FRAME IN BULKHEAD CHORD, BS 227.8 BETWEEN LBL 5.7 AND RBL 5.7. RE PAIRED IAW ECRA 5311-01353. 2 L 7 2 4F RT A16WE 2007082400223 20070824 00223 NM 2007 8 24 SWAA074084 1 20070817 A 3350 20131A BATTERY PACK BOEING 737 7373TO 138447G NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007082400226 20070824 00226 NM 2007 8 24 SWAA074097 1 20070817 A 3397 487191 CONNECTOR BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 451WN 32495 DURING SCHEDULED MV2 CHECK, FOUND AFT LEFT CABIN EEPLS INOP. INSPECTED FOUND LOOSE CONNECTOR, SECURED CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2007082400227 20070824 00227 2007 8 24 SWAA074102 4 20070819 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 401WN 29813 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007082400240 20070824 00240 NM 2007 8 24 SWAA074094 1 20070817 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007082400255 20070824 00255 NM 2007 8 24 SWAA074085 1 20070817 A 3350 8100022605 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 235WN 34630 EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007082400267 20070824 00267 2007 8 24 RAIA00708034 4 20070817 A 2215 4006719906 SERVO EMB 145 EMB145LR 3260212 SO RUDDER MALFUNCTIONED A RAIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CE 03 822HK 21913 21913 145069 FLT 5450 - STL - AFTER CLIMBOUT, YAW DAMPER KEPT ON TURNING ON AND OFF ALL BY ITSELF. THE BALL ON THE INCLINOMETER WAS TO THE RIGHT ALL THE WAY. WHEN THE RIGHT RUDDER WAS TAPPED THE BALL WENT ALL THE WAY TO THE LEFT AND AC STARTED TO GO B ACK TOWARDS THE RIGHT. MAINTENANCE REMOVED AND REPLACED THE RUDDER SERVO. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007082400292 20070824 00292 EA 2007 8 24 TRAX200701207 1 20070817 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 881AS 7496 FS 280 AT LBL 9 I/B & O/B CLIPS CRACKED. ALL WORK ACCOMPLISHED USING CRJ 200 SERIES SRM 51-21-11, 51-23-00, 51-24-16, 5 1-25-06, 51-25-16, 51-42-06, 51-42-13, 51-42-21, & 51-42-02. 2 L 7 2 4F RT A21EA 2007082400302 20070824 00302 SO 2007 8 24 XGN2007F00022 2 20070718 A 8530 TISN712ACA CYLINDER BEECH 36 36BEECH 1151602 CE CONT O520 IO520BA 17032 SO NR 1 CRACKED E XGNA O OTHER O OTHER NR NOT REPORTED 1 SW 05 1194A 611 E159 807201R REV 3, E SERIES CYLINDER ASSY 611.9 SINCE NEW CRACKED O TOP OF CYLINDER BEHIND FUEL INJECTOR BETWEEN THE FIRST AND THIRD FIN. COMPRESSION CHECK WITH SOAPY WATER REVEALED CRACK. CAN NOT BE SEEN WITH THE NAKED EYE. (K) 1 L 7 1 3O 3 O 3A15 E5CE 2007082400306 20070824 00306 SO 2007 8 24 XGN2007F00025 2 20070730 A 8530 TISN712ACA CYLINDER BEECH 55 D55 1152730 CE CONT O520 IO520CB 17032 SO 6TH CRACKED E XGNA O OTHER O OTHER NR NOT REPORTED 1 SW 05 69RP 744 TE766 282253R NR 6 CYLINDER WAS NEW, REV 3, E SERIES, CRACKED BETWEEN FINS 1-3 BEHIND FUEL INJECTOR. THIS IS 6TH REV 3, E SERIES TO C RACK IN THE SAME LOCATION. (K) 1 L 7 2 3O 3 O 3A16 E5CE 2007082400314 20070824 00314 CE 2007 8 24 081607N515CS1 1 20070816 A 3260 GE387 BULB CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG INDICATOR INOPERATIVE E Z5FA O OTHER P NO WARNING INDICATION AP APPROACH 1 EA 63 515CS 5605335 ON APPROACH, WHEN GEAR WAS EXTENDED, LT MLG DOWN LIGHT FAILED TO ILLUMINATE. CREW FOLLOWED AFM CHECKLIST AND BLEW GEAR D OWN. AIRCRAFT LANDED WITHOUT INCIDENT. ON SITE MAINTENANCE FOUND BULBS BLOWN, REPLACE BULBS, RESET EMERGENCY BOTTLE AND SERVICED. NO RESOURCES TO PERFORM GEAR SWING. AIRCRAFT FERRIED FOR GEAR SWING, GEAR SWING PERFORMED SATISFACTORY, AIRCRA FT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007082400339 20070824 00339 EA 2007 8 24 TRAX200701174 1 20070812 A 5220 HINGE CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 874AS 7551 CREW ESCAPE HATCH HINGE ARM IS CRACKED IN THE RADIUS. REMOVED AND REPLACED CREW ESCAPE HATCH HINGE ARM IAW CRJ 200 AMM 52-22-00. SUPPLEMENTAL - SDR CLOSED 08/22/07. 2 L 7 2 4F RT A21EA 2007082400340 20070824 00340 EU 2007 8 24 TRAX200701184 1 20070814 A 5720 INTERCOSTAL AEROSP ATR72 ATR72 EU LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 LEFT WING BOX FR 28 INTERCOSTAL CRACKED. LEFT WING BOX FR28 INTERCOSTAL REPLACED IAW SRM 57-25-01. REPAIR DETERMINED N OT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 FAR 43 APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE SRM 57-25-01. S UPPLEMENTAL - SDR CLOSED 08/22/07. 2 H 7 2 4T RT 2007082400345 20070824 00345 NM 2007 8 24 SWAA074136 1 20070821 A 3350 101331 LENS BOEING 737 7373A4 1384585 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED C2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007082400348 20070824 00348 2007 8 24 SWAA074125 4 20070821 A 2565 63562101 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 734SA 27866 L2 DOOR EMERGENCY EVAC SLIDE WILL NOT ARM. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007082400352 20070824 00352 NM 2007 8 24 SWAA074133 1 20070821 A 5753 6546435 FLAP BOEING 737 7373K2 13844BA NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 20Y CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD T/E. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007082400364 20070824 00364 NM 2007 8 24 CALA0700449 1 20070821 A 5320 654580731 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A 1 INCH CRACK IN ANGLE AT STA 291 JUST BELOW S11R. A NEW ANGLE WAS INSTALLED IAW SRM 51-40-00. 2 L 7 2 4F RT A16WE 2007082400366 20070824 00366 NM 2007 8 24 CALA0700451 1 20070822 A 5320 6546568520 STIFFENER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND AFT PRESSURE BULKHEAD CHANNEL STIFFENER CORRODED ON LOWER END, BOTH SIDES, STA 1016 FRAME ASSEMBLY. TH E CORRODED SECTION OF APB CHANNEL STIFFENER WAS REMOVED AND A REPAIR WAS INSTALLED IAW BOEING DRAWING 65C28106-1 AND EA 5310-04045, REV A, OP 02, STEP 1. 2 L 7 2 4F RT A16WE 2007082400370 20070824 00370 EA 2007 8 24 TRAX200701222 1 20070819 A 2560 MEGAPHONE CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 354CA 10064 FLIGHT ATTENDANTS MEGAPHONE INOP. 2 L 7 2 4F RT A21EA 2007082400371 20070824 00371 NE 2007 8 24 QXEA200701341 2 20070817 A 7230 VALVE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE ENGINE SMOKE A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 348PH 484 SEA FLIGHT NR 2003, BLUE HAZE AND MUSTY SMELLING COCKPIT AFTER ENGINES START AND BLEEDS SELECTED ON. REPLACED NR 2 ENGI NE P2.5/P3 VALVE IAW PW MM 72-30-00 PAGE 207 THROUGH 214. RAN ENGINE NO SMOKE NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007082400380 20070824 00380 EA 2007 8 24 A6WA200740438 1 20070806 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 466AW 7899 FOUND LEFT 621 FLOOR SUPPORT ANGLE IS CRACKED. (M) 2 L 7 2 4F RT A21EA 2007082400386 20070824 00386 NM 2007 8 24 DU4R2007162 1 20070808 A 5210 SKIN BOEING 757 757232 1384965 NM BS 618 GOUGED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 6712B 30484 FOUND GOUGE IN EXT SKIN AT AFT LWR CORNER OF FWD PIT DOOR. REPAIRED BY FABRICATING AND INSTALLING REPAIR DOUBLER 12 BY 12 FROM 2024-T3 .071 IAW B757 SRM 52-30-01, 51-20-01 AND B757 AMM 51-41-00-352-013. 2 L 7 2 4F RT A2NM 2007082400387 20070824 00387 NM 2007 8 24 DU4R2007163 1 20070803 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM BS 1640 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 6710E 30482 FOUND CORROSION ON CABIN FLOORBEAM AT BS 1640, LBL 24 TO RBL 4. CUT OUT 30 INCH CORRODED SECTION OF T-CAP. FABRICATED AND INSTALLED T-CAP REPAIR 36-3/4" FROM BAC1505-100617, 2 EA. SPLICE PLATES 9" BY 1-1/2" BY 1" AND 2 EA. 6-1/2" BY 1-1/2 "FROM 7075-T6 .050", 2 EA. REPAIR STRAPS 10" BY 1" AND 6-1/2" BY 1" FROM 7075-T6 .090" IAW B757 SRM 53-60-51-2-205D FIG 205. 2 L 7 2 4F RT A2NM 2007082400393 20070824 00393 EU 2007 8 24 2007UALA03206 1 20070816 A 3230 CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MLG MALFUNCTIONED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 417UA 483 ECAM WARNING LANDING GEAR NOT DOWN AND LOCKED. TWO TIMES NO LGCIU FAULTS OR OTHER INDICATIONS. UNABLE TO DUPLICATE ON GROUND, BUT REPLACED LGCIU AS PRECAUTION. SEVERAL GEAR SWINGS, SYSTEM CHECKS OUT NORMAL. NO REPEATS SINCE ORIGINAL . 2 L 7 2 4F 4 F RT A28NM E40NE 2007082800004 20070828 00004 NM 2007 8 28 2007UALA03210 1 20070816 A 5210 TORQUE TUBE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE PAX DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 AFT ENTRY DOOR CUTOUT TORQUE TUBE HAS MOVEMENT BEYOND .003. REPLACED UPPER AND LOWER BEARING TORQUE TUBE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082800008 20070828 00008 NM 2007 8 28 2007UALA03214 1 20070816 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 781 S17R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 327UA 24147 AFT PIT OPENING, NEED TO CUT RT CREASE BEAM INNER CHORD AT CABIN FLOOR STR 17R TO REMOVE SEGMENT TO FACILITATE FRAME REP AIR AT BS 781. REPAIRED PER SRM 51-70-12 FIG 1 SHEET 3 PAGE 5-6. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082800042 20070828 00042 NM 2007 8 28 2007UALA03248 1 20070819 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SEAT 6AB LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 FOUND EEL STRIP AT SEAT 6AB INOPERATIVE. RECONNECTED LOOSE EEL STRIP, OP CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082800044 20070828 00044 NM 2007 8 28 2007UALA03250 1 20070817 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 727A S20-21L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 AFT PIT SHEAR TIE DAMAGED STA 727A STR 20L TO 21L. MAJOR REPAIR ACCOMPLISHED: REMOVED OLD SHEAR TIE MFG AND INSTALLED N EW SHEAR TIE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082800049 20070828 00049 NM 2007 8 28 2007UALA03255 1 20070817 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOORWAY GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 327UA 24147 AFT CARGO DOOR OPENING, FWD FRAME HAS DEEP GOUGE AT LOWER END, MAJOR REPAIR ACCOMPLISHED: REMOVED AND REPLACED FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082800052 20070828 00052 NM 2007 8 28 2007UALA03260 1 20070820 A 3350 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS WEAK A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 803UA 748 3 SERVICE CABIN EMERGENCY LIGHTING CHECK GIVES THE MESSAGE EPSU INT LOAD EMERGENCY LIGHT. FOUND WEAK BATTERY. REPLACE D AFT LT EMERGENCY LIGHT BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082800063 20070828 00063 EU 2007 8 28 07FDEA03009 1 20070821 A 5330 2024T3 SKIN AIRBUS 310 A310203 3930313 EU MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 405FE 237 EXTERNAL REPAIR DOUBLER LT FUSELAGE FR26/32 STR39L-40L REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR W AS ACCOMPLISHED USING FAA APPROVED DATA VISUALLY INSPECTED REPAIR DOUBLER LT FUSELAGE FR26/32 STR39L-40L. FOUND NOT TO BE WITHIN ANY FAA APPROVED DATA. REMOVED AND REPLACED REPAIR DOUBLER ON FEDEX EA 6-5330-109186, SKIN PANEL DAMAGE FORWA RD OF FR 26/32 STRG 39L-40L REPAIR. 2 L 7 2 4F RT A35EU 2007082800065 20070828 00065 NM 2007 8 28 AWXA200701006 1 20070820 A 5330 6545774 SKIN BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 PHX - MAJOR REPAIR - LOG PAGE 7818967, CRACKED FUSELAGE SKIN, BS 727E, S23L, AFT OF EMERGENCY EXIT LIGHT. REPAIRED FUSEL AGE SKIN, BS 727E, S23L, AFT OF EMERGENCY EXIT LIGHT IAW B737-300 SRM 53-00-01, FIGURE 201. 2 L 7 2 4F RT A16WE 2007082800068 20070828 00068 EA 2007 8 28 SWIA200718581 1 20070630 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 716SK 10180 COCKPIT FLOOR SUPPORT IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED NEW COCKPIT FLOOR SUPPORT PER SB 670BA-53-026. 2 L 7 2 4F RT A21EA 2007082800070 20070828 00070 EA 2007 8 28 SWIA200718583 1 20070630 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 716SK 10180 EMERGENCY LIGHTS ABOVE NR 2 SEAT WON'T COME ON, FOUND AT C-CHECK. REPLACED LIGHT BULB IN OVERHEAD EMERGENCY LIGHT IAW C RJ700 AMM 33-51-00-710-802. 2 L 7 2 4F RT A21EA 2007082800076 20070828 00076 EA 2007 8 28 SWIA200718589 1 20070617 A 5520 HINGE CNDAIR CL600 CL6002B19 1900309 EA LT ELEVATOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 411SW 7067 LEFT ELEVATOR OUTBOARD HINGE HARDWARE IS CORRODED, FOUND AT C-CHECK. REPLACED CORRODED HARDWARE AND BUSHINGS PER CRJ200 AMM 27-34-01-000-801 STEPS G THRU-1-5. 2 L 7 2 4F RT A21EA 2007082800090 20070828 00090 SO 2007 8 28 SWIA200718603 1 20070817 A 5230 RETAINER EMB 120 EMB120ER 3260203 SO CARGO DOOR LOOSE A SWIA G O2 MASK DEPLOYED J WARNING INDICATION CL CLIMB 1 NM 07 301YV 120301 THE O2 MASKS DROPPED AFTER TAKEOFF FLIGHT NR 5774. RESECURED CARGO DOOR SEAL AND RETAINER. PRESSURIZATION CHECK GOOD. 2 L 7 2 4T RT A31SO 2007082800092 20070828 00092 2007 8 28 QXEA200701344 4 20070820 A 3420 UNKNOWN DHAV DHC8 DHC8202 2809007 NM AHRS MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 347PH 480 PDX FLIGHT NR 2147, ADI ROLL MISMATCH. FIRST OFFICERS ADI SHOWED 10 DEGREES RIGHT BANK AND 5 DEGREES PITCH DOWN. REINI TIALIZED AHRS. ADI'S CHECK GOOD. ADI ROLL MISMATCH MESSAGE EXTINGUISHED. NO PARTS REPLACED AIRCRAFT RETURNED TO SERVI CE. 2 H 7 2 4T RT A13NM 2007082800093 20070828 00093 SW 2007 8 28 L8318 1 20070613 A 5343 AN331A BOLT FRCHLD SA227 SA227DC 3377521 SW TRUNNION MISSING E KY7A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 03 882DC 7351 DC882B PILOT REPORTED LEFT MAIN GEAR UNSAFE INDICATION ON ROLL OUT. VISUALLY CHECKED THE GEAR AND FOUND THE OUTBOARD TRUNNION PIN MISSING. 2 L 7 2 4T RT A18SW 2007082800094 20070828 00094 NE 2007 8 28 NACA20070016 2 20070821 A 8530 356994 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 1 FAILED A NACA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AL 03 2907F 355 355 533265 CP450668 NR 4 ENGINE SHUT DOWN DUE TO RUNNING ROUGH AND DOUBLE SHORTED SECONDARY ON NR 1 CYLINDER. REMOVED AND REPLACED NR 1 CYL INDER DUE TO RING LAND FAILURE, REF: NAC DC-6 MM SECT. V PG. 16 & 16A. CHECK GOOD. 2 L 7 4 4R 4 R A781 5E8 2007082800096 20070828 00096 NM 2007 8 28 DU4R2007164 1 20070808 A 5315 146N5090 FLOORBEAM BOEING 757 757232 1384965 NM BS 1661 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 6712B 30484 FOUND CORROSION AROUND FASTENER HOLE AT FLOORBEAM BS 1661 LBL 10. REPAIRED BY CUTTING OUT CORRODED AREA. FABRICATED AN D INSTALLED REPAIR CHORD 16 LONG FROM BAC1505-100617, 2 EA. REPAIR ANGLES 24 LONG FROM BAC1490-2734 AND BAC1490-2865 AND TWO 24 REPAIR STRAPS FROM 7075-T6 .071, IAW B757 SRM 53-00-51 FIG 201, 51-40-02 AND BAC DWG 146N5230. 2 L 7 2 4F RT A2NM 2007082800107 20070828 00107 NM 2007 8 28 DL764071089 1 20070816 A 3610 8253071 CONTROL UNIT BOEING 767 767432ER 1385134 NM E/ E BAY UNSERVICEABLE A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 845MH 29719 RIGHT ENGINE BLEED OVHT LIGHT ILLUMINATED ON TAXI OUT. BITE THE ASCTU. FAULTS RT ASCTU. T/S PER FIM. REPLACED ASCTU PER MM CHKS OK. 2 L 7 2 4F RT A1NM 2007082800114 20070828 00114 NM 2007 8 28 DL764071096 1 20070819 A 2410 241040020 GCU BOEING 767 767432ER 1385134 NM LT ENGINE FAULTED A DALA D RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 830MH 29701 ON ENG STARTING, LEFT ENG BOTH GEN OFF LIGHTS AND RT BUSS OFF LIGHTS WERE ON RESET L AND RT GEN AND POWER RETURNED. FOU ND LT AND RT FAULTS ON BPCU. LEFT WAS 24-30101 AND RT CODE 24-34002. REPLACED LT AND RT GCUS. ALL OK PER FIM. 2 L 7 2 4F RT A1NM 2007082800122 20070828 00122 NM 2007 8 28 DLM88071106 1 20070817 A 5315 FLOORBEAM DOUG MD88 MD88 3023688 NM BS 905 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 CRACKED FLOOR SUPPORT FITTING AT STA. 905 AND X=44. REPLACED FITTING PER DRWG 9923417 REV.B ON N/R T0064339 ON HMV IN G DL. 2 L 7 2 4F RT A6WE 2007082800129 20070828 00129 NM 2007 8 28 DLM88071113 1 20070817 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 612 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 EXFOLIATION CORROSION ON RT CUSP WEB STA Y=612, REPAIR PER ERA 398191-14MA. 2 L 7 2 4F RT A6WE 2007082800142 20070828 00142 NM 2007 8 28 DLM88071126 1 20070817 A 5320 ANGLE DOUG MD88 MD88 3023688 NM BS 693 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 CRACK ON ANGLE (RACK SUPPORT) AT FS 693, LONG 21 LT (TASK 51-53300). REPLACED PER DRWG 5939741 ON N/R T0064838 ON HMV I N GDL. 2 L 7 2 4F RT A6WE 2007082800151 20070828 00151 EU 2007 8 28 07FDEA03001 1 20070821 A 5330 A53776532 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 726FD 575 FOUND SEVERAL MISDRILLED/ELONGATED HOLES BETWEEN FRAME 38.1-38.2, STGR 31, LT. REPAIR PERFORMED WITH BUSHING REPAIR AND INSTALLING 4, 8MM DIA LOCK FASTENERS IAW EA 6-5314-103278 AND RAS/DABRE/7006911/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007082800155 20070828 00155 EU 2007 8 28 07FDEA03014 1 20070822 A 5330 A53772018202 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 TWO SCRATCHES ON FRAME C25 AND C27, STRG 35 LHS. REPAIR PERFORMED WITH CUTOUT OF DAMAGED SKIN AND EXTERNAL DOUBLER, INS TALLATION IAW EA 6-5315-103323 AND RAS/DABRE/7006935/2006. 2 L 7 2 4F RT A35EU 2007082800156 20070828 00156 EU 2007 8 28 07FDEA03015 1 20070822 A 5312 A53810896201 BULKHEAD AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 HOLE FOUND ON PRESSURE BULKHEAD AT FRAME 39, Y-2244, Z-1425 CLOSE TO BRACKET A534-10096-204. REPAIR PERFORMED BY TRIMMI NG THE PRESSURE BULKHEAD AROUND THE DAMAGED AREA AND INSTALLATION OF REPAIR DOUBLER IAW EA 6-5314-103312 AND RAS: 046974 /011/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007082800157 20070828 00157 EU 2007 8 28 07FDEA03016 1 20070822 A 5315 A53974219220 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 726FD 575 OLD TOP CAP BEAM REPAIR FRAME 63 LT NOT CONFORM TO RAS/DAHAM/11513/1999 ISS. "A". SPLICE REPAIR RENEWED IAW RAS/DAHAM/1 1513/1999 ISS "A". 2 L 7 2 4F RT A35EU 2007082800158 20070828 00158 EU 2007 8 28 07FDEA03017 1 20070822 A 5310 A53810876 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 FOUND OLD TOOLING MARKS AT GANTRIES 4 AND 5 RT AND 5 LT, FRAME 47-48. REPAIR PERFORMED WITH SMOOTH REWORK AND INSTALLIN G CORNER ANGLES AND STRAPS IAW EA 6-5315-103326 AND RAS: 046958/010/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007082800160 20070828 00160 EU 2007 8 28 07FDEA03019 1 20070822 A 5710 A53810653200 BEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 TOOLING MARK WAS CAUSED IN THE EDGE OF FLANGE SPAR RADIUS AT BEAM 2 RT AT FRAME 42. REPAIR PERFORMED BY SMOOTH REWORK I AW EA 6-5710-103336 AND RAS/046790/014/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007082800161 20070828 00161 EU 2007 8 28 07FDEA03020 1 20070822 A 5310 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 FOUND DAMAGED HOLES (COUNTERSUNK) IAW SB A300-53-6063 AT C40-41 RT, HOLE 24, 25, 26 AND 27. REPAIR PERFORMED BY REMOVIN G FASTENERS, ROTO-TEST AND INSTALLING FASTENERS HL13VF10 WITH NEW COUNTERSUNK IAW EA 6-5315-103324. 2 L 7 2 4F RT A35EU 2007082800162 20070828 00162 EU 2007 8 28 07FDEA03021 1 20070822 A 5311 A53771281201 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 CHAFING MARKS ON THE INNER FLANGE OF FRAME 22 BETWEEN STRG 14-15 RT. REPAIR PERFORMED BY BLEND OUT AND INSTALLING A REP AIR ANGLE AS PER SRM53-10-13/FIG 202 IAW EA 6-5310-103329 AND RAS/DABRE/7006981/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007082800163 20070828 00163 EU 2007 8 28 07FDEA03023 1 20070822 A 5311 A53776902200 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 CHAFING MARK ON THE INNER FLANGE OF FRAME 38.2 BETWEEN STRG 14-15 LT. REPAIR PERFORMED BY BLEND OUT AND INSTALLING A RE PAIR ANGLE AS PER SRM 53-10-13/FIG 202 IAW EA 6-5310-103329 AND RAS/DABRE/7006981/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007082800165 20070828 00165 EU 2007 8 28 07FDEA03025 1 20070822 A 5712 A57240876205 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 CHAFING MARK AT END OF RIB 6-A, OUTBOARD SIDE RT WING T/E. REPAIR PERFORMED BY BLEND IAW EA 6-5751-103339 AND RAS/BAE/1 003495/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007082800166 20070828 00166 EU 2007 8 28 07FDEA03026 1 20070822 A 5101 A53776533200 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 FOUND OLD DOUBLER REPAIR AT FRAME 26-27, STRG 24-26 RT. THE REPAIR WAS PERFORMED IAW DRW: R537B1730-002 BUT FOUR HOLE S HAVE DIA: 7, 5MM INSTEAD OF 4,8MM. REPAIR PERFORMED BY REAM UP THE DIAMETERS TO 8, 8-9, 0MM AND INSTALL FOUR SHOULDER ED BUSHES IAW EA 6-5314-103330 AND RAS/DABRE/7006980/2006 ISS. "A". 2 L 7 2 4F RT A35EU 2007082800167 20070828 00167 EU 2007 8 28 07FDEA03027 1 20070822 A 5730 SKIN AIRBUS 300 A300B4622R 3930312 EU LT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 WING BOTTOM SKIN PANEL NR 1 LT, INCOMPLETE RECORDS OF EMBODIMENT OF DRW: R572-40179 AT FWD EDGE JUST OUTBOARD OF PYLON. IN ADDITION FOUND NUMEROUS DEVIATIONS (AT HOLE 7 & 9) AND CRACK IN HOLE 23 REPAIR PERFORMED BY RE-EMBODIMENT OF DRW: R5 72-40179 WITH CRACK STOP HOLE NR 7 AND NR 9 IAW EA 6-5720-99219 AND RAS/BAE/1003499/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007082800168 20070828 00168 WP 2007 8 28 07FDEA03028 1 20070822 A 5310 AFA00433 BEAM DOUG DC10 DC1010F 3022111 WP BS 899 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 FWD CARGO COMPT BILGE AREA ON BEAM FOUND SEVERE EXFOLIATION CORROSION. REPAIRED AREA IAW SRM 53-60-01 VOL 1 FIG 3. 2 L 7 3 4F A22WE 2007082800170 20070828 00170 WP 2007 8 28 07FDEA03030 1 20070822 A 5730 SKIN DOUG DC10 DC1010F 3022111 WP LT WING UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 LT WING TIP EXTERNAL DOUBLER ON SKIN. ACCOMPLISHED EA NR 8-5760-112423. 2 L 7 3 4F A22WE 2007082800172 20070828 00172 WP 2007 8 28 07FDEA03032 1 20070822 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 LWR FWD COMPT FOUND CRACK .50" LONG ON LONGERON. REPAIRED AREA IAW SRM 53-10-00 FIG 5 VOL 1. 2 L 7 3 4F A22WE 2007082800173 20070828 00173 WP 2007 8 28 07FDEA03033 1 20070822 A 5310 SCOOP DOUG DC10 DC1010 3022110 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 INT CAC CRACK ON SUGAR SCOOP. REPAIR AREA IAW SRM 53-40-00 VOL I FIG 8. 2 L 7 3 4F A22WE 2007082800176 20070828 00176 EU 2007 8 28 07FDEA03036 1 20070822 A 5710 A57942553 BEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 CHAFING MARKS FOUND ON VERTICAL WEB OF FLAP TRACK BEAM 3 OUTBOARD CHANNEL LHS, BEAM 3 INBOARD CHANNEL RHS. REPAIR PERFO RMED BY BLEND OUT WITH NDT INSPECTION IAW EA 6-5720-103376 AND RAS/BAE/1003599/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007082800177 20070828 00177 EU 2007 8 28 07FDEA03037 1 20070822 A 5710 A57942554 BEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 CHAFING MARKS ON VERTICAL WEB OF FLAP TRACK BEAM NR 4 RT, OUTBOARD SIDE. REPAIR PERFORMED BY BLEND OUT WITH NDT INSPECT ION IAW EA 6-5720-103376 AND RAS/BAE/1003599/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007082800178 20070828 00178 EU 2007 8 28 07FDEA03039 1 20070822 A 5330 A53778080 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 FOUND SEVERAL MISDRILLED/ELONGATED HOLES BETWEEN FRAME 38.1-38.2, STGR 31, LHS. REPAIR PERFORMED WITH BUSHING REPAIR AN D INSTALLING 4,8MM DIA HI-LOKS IAW EA 6-5314-103278 AND RAS/DABRE/7006911/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007082800179 20070828 00179 EU 2007 8 28 07FDEA03040 1 20070822 A 5330 A53778089 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 726FD 575 FOUND SEVERAL MISDRILLED/ELONGATED HOLES BETWEEN FRAME 38.1-38.2, STGR 31, LHS. REPAIR PERFORMED WITH BUSHING REPAIR AN D INSTALLING 4, 8MM DIA HI-LOKS IAW EA 6-5314-103278 AND RAS/DABRE/7006911/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007082800180 20070828 00180 EU 2007 8 28 07FDEA03041 1 20070822 A 5320 A53510166200 ANGLE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 726FD 575 FOUND SEVERAL MISDRILLED/ELONGATED HOLES BETWEEN FRAME 38.1-38.2, STGR. 31, LHS. REPAIR PERFORMED BY REPLACEMENT OF ANG LE WITH BUSHING REPAIR AND INSTALLING 4, 8MM DIA HI-LOKS TOGETHER WITH TWO SKIN PANELS AND A STRINGER IAW EA 6-5314-1032 78 AND RAS/DABRE/7006911/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007082800181 20070828 00181 NM 2007 8 28 07FDEA03042 1 20070822 A 5330 6554583 SKIN BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 LWR FUSELAGE SKIN IS DETERIORATED AT VHF ANTENNA LOCATION. INTERNAL KIN SURFACE HAS CORROSION, EXTERNAL SKIN SURFACE HA S CORROSION, BS 1030-1050, STR 29R -30, WL140 REMOVED CORROSION AT LWR FUSELAGE INTERNAL SKIN SURFACE, AND EXTERNAL SKIN SURFACE IAW B 727 SRM 53-30-1 FIG 2. FABRICATED DOUBLER AND FILLER, IAW B727 SRM 53-30-3. TREATED AND PRIMED AND INST ALLED REPAIR DOUBLER, AND FILLER IAW B727 SRM 53-30-3 FIG 1, SHEET 4, 51-10-2, 51-30-2. 2 L 7 3 4F RT A3WE 2007082800182 20070828 00182 NM 2007 8 28 07FDEA03043 1 20070822 A 5322 6516348137 SHEAR TIE BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 AFT LOWER PIT STATION 1148 BILGE AREA, SHEAR TIE FRAME CORRODED, BETWEEN STR 30 AND STR 29L REMOVED CORROSION REF SRM 51 -10-01. FOUND TO BE OUT OF LIMITS, ORIGINAL THICKNESS .066" REMAINING THICKNESS .043". REMOVED .023". REMOVED DAMAGE, FAB NEW FRAME REPAIR. INSTALLED NEW SHEAR TIE. REF SRM 53-10-4 FIG 11. 2 L 7 3 4F RT A3WE 2007082800186 20070828 00186 WP 2007 8 28 07FDEA03047 1 20070822 A 5730 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 LT WING LWR SURFACE FOUND CRACK ON SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 SHT 2 VOL I. 2 L 7 3 4F A22WE 2007082800190 20070828 00190 NM 2007 8 28 07FDEA03051 1 20070822 A 5320 6946347 INTERCOSTAL BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FWD PIT FLOOR INTERCOSTAL WEB CORRODED, STA. 580 AT STR. 27R - 28R LOCATED AT BS 582, "Z" OB OF STR 28R REMOVED INTERCO STAL. REMOVED CORROSION REF SRM 51-10-06. FOUND TO BE OUT OF LIMITS, REF SRM 51-10-01. REMOVED DAMAGE AND FABRICATED REPAIR DOUBLER. REF SRM 51-40-03, RECIEVED DOUBLER FROM HEAT TREAT REF 8130-2007-08-105. FABRICATED TAPERED SHIM REF S RM 51-20-01. INSTALLED DOUBLER AND SHIM REF SRM 51-30-02 AND INSTALLED INTERCOSTAL. 2 L 7 3 4F RT A3WE 2007082800191 20070828 00191 NM 2007 8 28 07FDEA03052 1 20070822 A 5311 651766445 FRAME BOEING 727 727233 138408A NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 286FE 22623 ON AGING A/C INSP, FOUND EXISTING REPAIR ON FRAME 680 BETWEEN STR 22L AND 25L DID NOT CONFORM TO SRM 51-40-3. REMOVED E XISTNG REPAIR, REMOVED EXISTING SLICE PLATE AT STR 25L. FABICATED REPAIR AND INSTALLED REF SRM 51-40-3 AND FED EX EO NR 7-5310-113081 THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007082800192 20070828 00192 EU 2007 8 28 07FDEA03053 1 20070822 A 5347 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 446FE 224 MAIN CABIN RT SEAT TRACK NR Y-1456 AT FRAME C63 LUGS BROKEN OUT. 09-11-07 REMOVED DAMAGED SECTION OF SEAT TRACK IAW A3 10 SRM 53-10-16. INSTALLED NEW SECTION OF SEAT TRACK AND SPLICE IAW A310 SRM 53-10-16 2 L 7 2 4F RT A35EU 2007082800194 20070828 00194 NM 2007 8 28 07FDEA03057 1 20070822 A 2612 UNKNOWN DOUG MD11 MD11F 3023600 NM FIRE LOOP UNKNOWN A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 593FE 48551 AT CRUISE FL340 MOMENTARY ENGINE FIRE INDICATION ON ENGINE ONE. NO OTHER ENGINE INDICATIONS OF FIRE. RETARDED THROTTL E TO IDLE. REMAINED AT IDLE FOR DIVERT TO LAX. CHECKED RESISTANCE FOR LOOP B AND WAS GOOD, IAW FIM 26-11. FOUND SEV ERAL CLAMPS WITH OUT FOIL, FOILED CLAMPS, UNABLE TO REPEAT LOOP B FAULT. PERFORMED RTS, RTS PASS. 2 L 7 3 4F RT A22WE 2007082800195 20070828 00195 WP 2007 8 28 NWAA072899851 1 20070821 A 2120 UNKNOWN DOUG DC9 DC951 3022051 WP CABIN SMOKE A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 760NC 21218 1620 47708 SHORTLY AFTER DEPARTURE, SMOKE AND FUMES APPEARED IN THE CABIN AND COCKPIT. THE FLIGHT CREW SHUT DOWN BOTH PACKS, DECLA RED AN EMERGENCY AND RETURNED TO AN UNEVENTFUL LANDING BACK AT DTW. NO MENTION OF COM COMPLIANCE. THE AIRCRAFT WAS TOW ED TO THE GATE. MAINTENANCE COULD NOT FIND A POSITIVE SOURCE OF THE SMOKE BUT DID REPLACE BOTH COALESCER BAGS, THE APU, AND THE CABIN TEMPERATURE CONTROLLER. PACK BURNOUT COMPLETED AND THE LEAK CHECKS WERE GOOD SO THE AIRCRAFT WAS RETURNE D TO SERVICE. 2 L 7 2 4F RT A6WE 2007082800196 20070828 00196 EU 2007 8 28 AWXA200701001 1 20070818 A 2611 RAI2800M0706 CONTROL UNIT AIRBUS 320 A320232 3930326 EU SMOKE DETECTION FAILED A AWXA O OTHER G MULTIPLE FAILURE CR CRUISE 1 WP 28 665AW 18324 8325 1644 PHX - OTH - LOG 7848748 - CREW REPORTED WHILE EN ROUTE, SMOKE LAV/CARGO DETECTION FAULT MESSAGE ILLUMINATED. MX REPLACE D THE SDCU. OPERATIONAL CHECK WAS GOOD IAW AMM 26-17-34. 2 L 7 2 4F RT A28NM 2007082800197 20070828 00197 EU 2007 8 28 AWXA200701007 1 20070821 A 2560 P2070001214 FLASHLIGHT AIRBUS 320 A320232 3930326 EU AFT CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 648AW 770 SEA - EEL - LOG 4111250 - MX REPORTED EMERGENCY FLASHLIGHT AT AFT LEFT F/A SEAT IS INOP. MX REPLACED THE FLASHLIGHT. 2 L 7 2 4F RT A28NM 2007082800198 20070828 00198 EU 2007 8 28 AWXA200701009 1 20070802 A 5743 D3215303200000 PIN AIRBUS 320 A320231 3930325 EU MLG CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 SAL - MAJOR REPAIR - C-06 CHECK - NR 5990415, CORROSION ON THE LEFT MAIN LANDING GEAR PINTLE PIN. REPLACED THE LEFT MAI N LANDING GEAR PINTLE PIN IAW AWA TASK CARD R4M32304. 2 L 7 2 4F RT A28NM 2007082800199 20070828 00199 NM 2007 8 28 DHL2007746500 1 20070823 A 5710 BAC1506860 SUPPORT BEAM BOEING 727 727224 1384076 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 WHILE AT C CHECK, RT WING TRAILING EDGE UPPER PANEL SUPPORT I BEAM IS CRACKED AT WBL 118 ON FWD SIDE OF NR 8 SPOILER FIT TING. REMOVED DAMAGED I BEAM AT T/E WBL 118 IAW B727 SRM 51-30-2. FABRICATED AND INSTALLED NEW BEAM IAW B727 SRM 51-20 -1 AND 57-20-2 FIG2 MAT USED BAC1506-860 7075-T6 82" LONG PO NR 7268125. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007082800200 20070828 00200 EA 2007 8 28 SIMA200723501 1 20070820 A 3240 5013642 BRAKE CNDAIR CL600 CL6002C10 1390015 EA RIGHT OVERTEMP A SIMA O OTHER M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 506AE 8574 39 10056 NUMBER 4 BRAKE WAS DRAGGING WITH BRAKE TEMPERATURE RISING TO 13C - ELECTED TO DEPLANE ION RAMP AND BUS PASSENGER TO TERM INAL, POST INSPECTION FOUND NUMBER 4 BRAKE DISCONNECT BACKING OFF. REMOVED AND REPLACED NUMBER 4 BRAKE AND TIRE ASSEMBL Y IAW CRJ AMM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007082800201 20070828 00201 SO 2007 8 28 SIMA200723503 1 20070821 A 3350 20131A BATTERY PACK EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 612AE 11673 145079 EMERGENCY FLOOR LIGHTS BETWEEN ROW 8 AND 12 INOPERATIVE, FERRIED AIRCRAFT FROM BUF TO ORD. REMOVED AND REPLACED EMERGEN CY LIGHT BATTERY PACK IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007082800202 20070828 00202 SO 2007 8 28 SIMA200723504 1 20070822 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 658AE 9731 145760 OVERHEAD EXIT SIGN INOPERATIVE. REMOVED AND REPLACED NR 4 LIGHT DC/AC INVERTER IAW EMB AMM 33-50-11. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007082800204 20070828 00204 NM 2007 8 28 DHL2007746501 1 20070822 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM BS 680-740 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 SURFACE CORROSION OVER LENGTH OF SEAT TRACK BS 680-740 RBL24. REMOVED DAMAGED SEAT TRACK SECTION IAW B727 SRM 51-30-2 A T RBL 24.75 FROM STA 680-740 IAW B727 SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW B727 SRM 53-10-5 FIG1 AND 53-10-2 FIG 7 MAT USED BAC 1520-792 7178-T6511 PO NR 9003797 16' 2 EA SPLICE ANGLES BAC 1503-100122 7178-T6 13 " PO NR 9005571 AND 1 EA STRAP .250 7075-T6 PO NR 9003464 7 1/8" BY 2", ALL PARTS AND AREA TREATED AND PRIMED IAW B727 S RM 51-10-2. 2 L 7 3 4F A3WE 2007082800205 20070828 00205 NM 2007 8 28 DHL2007746502 1 20070820 A 5311 FRAME BOEING 727 727224 1384076 NM BS 680 S17R DAMAGED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 746DH 22252 WHILE AT FLIGHTSTAR AIRCRAFT SERVICES FOR A C CHECK, N/R 099360 DOUBLER DRILLED HOLES IN FRAME BS 680 STR 17R. CUTOUT D AMAGED AREA DIM 1" BY 1" IAW B727 SRM 51-40-3 FIG 1. FABRICATED ANGLE REPAIR FROM 7075 T6 .050 DIM 9" BY 4" IAW B727 SR M 53-10-2 FIG3 AND 51-40-03 FIG 1 PO 9004940 LOCATED AND DRILLED IAW B727 SRM 51-30-5. ALODINED AND PRIMED ANGLE AND AR EA IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 51-30-2 AND 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2007082800207 20070828 00207 NM 2007 8 28 DHL2007746504 1 20070820 A 5311 FRAME BOEING 727 727224 1384076 NM BS 700 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 WHILE AT FLIGHTSTAR FOR A C CHECK,N/R 099359 DISCREPANCY: HOLE DRILLED IN RADIUS OF FRAME BS 700 STR17R. CUTOUT DAMAGED AREA DIM 1" BY 1" IAW B727 SRM 51-40-03 FIG. FABRICATED ANGLE REPAIR FROM 7075T6 .O50 DIM 9" BY 4" IAW B727 SRM 51-40- 03 FIG 1, 53-10-2 FIG 1. LOCATED AND DRILLED ANGLE IAW B727 SRM 51-30-5, PO NR 9004940. ALODINED AND PRIMED ANGLE AND AREA IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 51-30-2 AND 51-40-03 FIG 1. 2 L 7 3 4F A3WE 2007082800209 20070828 00209 NM 2007 8 28 07FDEA03056 1 20070822 A 5330 SKIN PANEL BOEING 757 757200 1384950 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 LT SIDE OF FUSELAGE HAS A DIVOT IN SKIN AT BS 726, APPROXIMATELY 5" ABOVE STRINGER 23L. MEASURED AND EVALUATED DAMAGE IA W SRM 53-00-01, FIGURE 101, DETAIL 2 AND SRM 53-00- 01, FIGURE 201, SECTION 1, PARA 2.C. L = 1.0", W = .700", D = .013" . OUT OF LIMITS IAW SRM 53- 30-01, FIGURE 1, SHEETS 3 AND 4. ACCOMPLISHED REPAIR IAW EA F-5310-110755, DATED 7/30/07. NO FOLLOW UP ACTION IS REQUIRED. 2 L 7 2 4F RT A2NM 2007082800210 20070828 00210 EU 2007 8 28 07FDEA03058 1 20070821 A 2760 3905300101 CONTROL UNIT AIRBUS 310 A310203 3930313 EU ZONE 100 MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 435FE 8053 8053 369 AFTER T/O, NR 5 SPOILER FAULTED W/ RT WING NR 5 SPOILER INDICATING UP. RAN QRH PROCEDURE NO RELIEF. RTB IND. REMOVED AND REPLACED NR 1 AND 2 EFCU'S IAW A310-200 MM 27-61-34-4. OPS CK GOOD PERFORMED GROUND SPOLIER, OPS TEST IAW 27-61-00 -5 SUPPLIED FROM AIRBUS WEB SITE. VISUAL INSPECTION OF NR 1 AND 5 RT SPOILERS SHOW NO DEFECTS. 2 L 7 2 4F RT A35EU 2007082800213 20070828 00213 EU 2007 8 28 07FDEA03061 1 20070823 A 5330 A53974208 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 811FD 457 FOUND OLD UNIDENTIFIABLE RIVET IN THE SKIN NEAR FRAME 68 BETWEEN STRG 45-46, LHS. REPAIR PERFORMED REMOVING FASTENER AN D INSTALLING A FREEZE PLUG IAW. SRM 51-40- 51 APPROVED BY EA 6-5317-101277 AND RAS/DATLS/0003278/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007082800214 20070828 00214 WP 2007 8 28 07FDEA03080 1 20070823 A 5310 ACA72251 BEAM DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 399FE 48262 MAIN CARGO DOOR SPOOL NR 7, AFT OUTBOARD ATTACH HOLE SHOWS SIGN OF CRACK INDICATION IAW NTSPM 06-10-01.0003 REAMED HOLE UP TO .520 AND ACCOMPLISHED A BHEC INSPECTION. NO CRACK NOTED IAW NTSPM 06-10-01.0003. FABRICATED, INSTALLED AND REAM ED TO SIZE REPAIR BUSHING IAW MD/DC 10 SRM 53-50-00 VOLI PG 81. 2 L 7 3 4F RT A22WE 2007082800215 20070828 00215 NM 2007 8 28 HALA0700352 1 20070821 A 2911 41003106 PTU BOEING 717 717200 1383700 NM HYD SYSTEM INOPERATIVE A HALA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 WP 13 479HA 55123 LEFT SYSTEM HYD ACCUMULATOR RUPTURED. TROUBLESHOT LT SYS, FOUND PTU INOP. REMOVED AND REPLACED PTU PER AMM 29-22-01. OPS CK OK. SERVICED ACCUM FOUND OK. 2 L 7 2 4F TR A6WE 2007082800216 20070828 00216 EA 2007 8 28 SWIA200718604 1 20070819 A 2752 FLEX DRIVE CNDAIR CL600 CL6002B19 1900309 EA NR 1 ACTUATOR CORRODED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 431SW 7536 RIGHT WING NR 1 ACTUATOR NEEDS TO BE REPLACED BECAUSE OF CORROSION AT FLEX SHAFT DRIVE POINT. REPLACED NR 1 FLAP ACTUAT OR IAW MM 27-53-00. 2 L 7 2 4F RT A21EA 2007082800217 20070828 00217 EA 2007 8 28 SWIA200718605 1 20070819 A 2750 FLEX DRIVE CNDAIR CL600 CL6002B19 1900309 EA TE FLAP CORRODED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 431SW 7536 RIGHT INBOARD FLEX DRIVE SHAFT IS CORRODED AT NR 1 ACTUATOR. REPLACED RIGHT INBOARD FLEX CABLE AS REQUIRED, PN: 601R931 06-107, SN OFF: 5676. 2 L 7 2 4F RT A21EA 2007082800219 20070828 00219 SO 2007 8 28 SWIA200718607 1 20070815 A 5210 HANDLE EMB 120 EMB120ER 3260203 SO PAX DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 576SW 120345 MAIN CABIN DOOR IS DIFFICULT TO OPEN, FLIGHT NR 5469. CLEANED AND LUBED DOOR HANDLE MECHANISM AND LINKAGE IAW EMB 120 M M 52-11-00. 2 L 7 2 4T RT A31SO 2007082900002 20070829 00002 WP 2007 8 29 AALA20071396 1 20070803 A 2120 59535625521 DUCT DOUG DC9 DC982 3022082 WP LT A/C PACK LEAKING A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 293AA 49305 TAIL COMPARTMENT OVERHEAT INDICATION ON CLIMB OUT. LEFT AIR CONDITIONING PACK WAS TURNED OFF AND LIGHT EXTINGUISHED AFT ER ONE MINUTE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CL OSED) 2 L 7 2 4F A6WE 2007082900004 20070829 00004 EA 2007 8 29 TRAX200701120 1 20070806 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 755EV 10185 LEFT LOWER FS 280 WEB HAS CORROSION. REMOVED LITE SURFACE CORROSION .004" DEEP IAW CRJ SRM 51-21-06. LEFT LOWER FS 280 WEB AREA UNDER BEAM (BLENDED AREA) IS WITHIN SERVICEABLE LIMITS IAW REO 670-53-11-052. OK TO ALODINE AND PRIME BARE ME TAL. ALODINED AND PRIMED BARE METAL ON THE LT LOWER FS 280 WEB, IAW CRJ SRM 51-21-11 AND 51-25-06. OKAY TO PAINT. PAI NTED IAW CRJ SRM 51-25-16. SUPPLEMENTAL - SDR CLOSED 08/14/07. 2 L 7 2 4F RT A21EA 2007082900005 20070829 00005 EA 2007 8 29 TRAX200701121 1 20070806 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 755EV 10185 RIGHT LOWER FS 280 WEB HAS CORROSION. REMOVED LITE SURFACE CORROSION, .0035 INCH DEEP IAW CRJ SRM 51-21-06. RIGHT LOWE R FS 280 WEB AREA UNDER BEAM (BLENDED AREA) IS WITHIN SERVICEABLE LIMITS IAW REO 67053-11-052. OK TO ALODINE AND PRIME BARE METAL. ALODINED AND PRIMED BARE METAL ON THE RIGHT LOWER FS 280 WEB IAW CRJ SRM 51-21-11 AND 51-25-06. OK TO PAIN T. PAINTED IAW CRJ SRM 51-25-16. SUPPLEMENTAL - SDR CLOSED 08/14/07. 2 L 7 2 4F RT A21EA 2007082900006 20070829 00006 EA 2007 8 29 TRAX200701148 1 20070806 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 755EV 10185 FS 280 FWD CENTER FLOOR SUPPORT ANGLE CORRODED. 2 L 7 2 4F RT A21EA 2007082900008 20070829 00008 CE 2007 8 29 N71CK81407 1 20070813 A 2612 896416 FIRE LOOP LEAR 35 36A 5170603 CE RT ENGINE OUT OF POSITION E KC8A K NONE N FALSE WARNING UK UNKNOWN 1 GL 23 71CK 035 THIS IS AN UPDATE TO THE PREVIOUS SDR DATED 8/13/2007. RT ENGINE FIRE WARNING LIGHT ILLUMINATED DURING FLIGHT. INVESTI GATION FOUND THE AFT FIRE SENSE LOOP IN THE TAIL CONE OF THE ENGINE WAS CHAFING ON THE TAIL PIPE AT A CERTAIN POWER SETT ING. DUPLICATED DISCREPANCY. CORRECTED POSITIONING OF THE FIRE LOOP AND TESTED SYSTEM. ALL WORK PERFORMED IAW THE LEA RJET 35 / 36 / 35A / 36A MAINTENANCE MANUAL. 2 L 7 2 4F A10CE 2007082900010 20070829 00010 NM 2007 8 29 UPS07650429 1 20070813 A 2120 FITTING BOEING 767 76734AF 1385212 NM LT A/C PACK LEAKING A IPXA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 01 327UP 27753 INSPECTION TYPE:ETOP LEFT BLEED DUCT LEAK LIGHT ILLUMINATED EICAS MSG L BLD DUCT LEAK DISPLAYED. LIGHT EXTINGUISHED AFT ER ENG BLEED AIR SUPPLY AND ISOLATION VALVES CLOSED. FOUND WIGGINS FITTING LEAK LEFT PACK DOWNSTREAM OF FLOW CONTROL VA LVE AT T-FITTING. REMOVED AND REPLACED SEALS ON COUPLING HOUSING AND INSTALLED MISSING CABLE ASSY PER EO B767-2160-2742 6A. LEAK CHECK AND OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2007082900013 20070829 00013 WP 2007 8 29 UPS07850434 1 20070813 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. EMERGENCY LIGHT BATT & RELAY REMOVED AND REPLACED ON L/P 686282. OPERA TES NORMALLY AT THIS TIME, ALSO PER TECH REQUEST, PERFORMED VOLTAGE/CHARGING TEST IAW MM 33-50-01-2, NO FAULTS, OK FOR S ERVICE. 2 L 7 4 4F RT 4A25 2007082900015 20070829 00015 NM 2007 8 29 UPS07M50436 1 20070725 A 5514 FITTING DOUG MD11 MD11F 3023600 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORZ STAB CONSTANT SECTION BARREL NUT BORE RT NR 14 FOUND WITH CORROSION. SPLICE FITTING REMOVED SRM 51-32-01 VII R38. CORROSION AT BARREL NUT BORE REMOVED BOTTOM REMAIN BLEND OUT 0.198" BORE REAMED TO 0.988" DIA REMAIN BLEND OUT 0.050" FOUND EXCEED LIMIT PER EO MD11-5510-19409-L. HOLES PICK UP ON TO NEW FITTING DOUGLAS DWG ALC8100. NEW SPLICE FITTING INSTALLED AT NR 14 BARREL NUT BORE SRM 51-38-01VII R38. FITTING, FILLET SEALED SRM 51-41-01VII R38. 2 L 7 3 4F RT A22WE 2007082900018 20070829 00018 NM 2007 8 29 UPS07M50439 1 20070715 A 5720 CABLE GUARD DOUG MD11 MD11F 3023600 NM RT WING CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C RIGHT WING - L/E PANEL NR 627AB CABLE GUARD U-CHANNEL FOUND CHAFED AS MARKED. RIGHT WING - L/E PANEL NR 627AB CABLE GUARD U-CHANNEL CHAFE MARK REMOVED. ORG THK 0.063" MATL REMAIN 0.033" MATL REMOVED 0.030". FOUND EXCEED LIMIT SRM 57-00-01 FIG 1A VII R38. CHAFED CHANNEL REMOVED SRM 51-33-01 VII R38. NEW CABLE GUARD FAB USE MATL 2024T3-0 .063" THK PER DOUGLAS DWG ARB2946. FAB U-CHANNEL INSTALLED PER SRM 51-33-01 VII R38. 2 L 7 3 4F RT A22WE 2007082900019 20070829 00019 NM 2007 8 29 UPS07M50440 1 20070702 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C CABIN - CORROSION ON SEAT TRACK AT STA 1966 X=107. AFFECTED AREA CORROSION REMOVED & REPROTECTED SRM 51-21-01VII R38. CROWN AREA ORG THK 0.145" MATL REMAIN 0.045" MATL REMV 0.100". FLANGE AREA ORG THK 0.080" MATL REMAIN 0.048" MATL REMV 0.032". FOUND EXCEED LIMITS RM53-70-00 FIG 3 VI R38. CORR SEAT TRACK TRIM OFF AT STA 1831 & REMOVED FRM STA 1831-STA 2007. SEAT TRACK, SPLICE HAT & PLATE FAB & INSTALLED SRM 51-31-01 VII R38. 2 L 7 3 4F RT A22WE 2007082900020 20070829 00020 NM 2007 8 29 PIDA07040 1 20070811 A 3350 BATTERY PACK BOEING 737 7372K5 138448X NM CABIN DISCHARGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 250TR 22597 DURING MAINTENANCE, FOUND RIGHT OVERWING EMERGENCY DOOR LIGHT OUT. REPLACED BATTERY PACK AND OPS CHECKED OK. 2 L 7 2 4F RT A16WE 2007082900021 20070829 00021 SO 2007 8 29 C2XA07CL068 1 20070815 A 4930 4504616A FUEL CONTROL EMB 145 EMB145EP 3260221 SO APU LEAKING A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 12946 145052 CLE FLIGHT 2912 - THE CREW REPORTED A FUEL ODOR WHEN APU BLEED WAS SELECTED. MAINTENANCE REPLACED THE APU FUEL CONTROL ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2007082900022 20070829 00022 NM 2007 8 29 BB07065 1 20070814 A 4900 32021303 CHECK VALVE BOEING 757 75723N 1384973 NM APU CHATTERING A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 205UW 2324 789 30887 FLIGHT 728, PHL-GLA: CREW REPORTED A RHYTHMIC KNOCKING SOUND IN THE AREA OF SEAT 13A. FLIGHT RETURNED TO PHL. MAINTEN ANCE REPLACED THE APU CHECK VALVE. 2 L 7 2 4F RT A2NM 2007082900023 20070829 00023 NM 2007 8 29 BB07066 1 20070814 A 2120 CD01068F2 FILTER BOEING 757 7572B7 1384964 NM CABIN DETERIORATED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 206UW 27808 FLIGHT 725, SNN-PHL: AFTER TAKEOFF, FLIGHT ATTENDANTS REPORTED INSULATION LIKE MATERIAL COMING FROM OVERHEAD VENTS. FL IGHT RETURNED TO SNN. MAINTENANCE FOUND THAT THE LEFT RECIRC FILTER HAD BROKEN DOWN, ALLOWING MATERIAL FROM FILTER INTO THE DUCT SYSTEM. THE FILTER WAS REPLACED AND THE DUCT SYSTEM CLEARED OF EXCESS DEBRIS. 2 L 7 2 4F RT A2NM 2007082900025 20070829 00025 NE 2007 8 29 N973081107 3 20070810 A 6140 INDICATION SYS STBROS SD3 SD360 8100606 EU PWA PT6 PT6A67R 52043 NE HARTZL HCA6A HCA6A3A NE COCKPIT MALFUNCTIONED E EXDA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 SW 09 973AA SH3749 PCE106016 GP108 WHILE EN ROUTE TO MCI THE FLIGHT CREW ELECTED TO SHUT DOWN THE RIGHT ENGINE AS A PRECAUTIONARY MEASURE DUE TO ERRATIC PR OPELLER SPEED INDICATION AND DIVERTED TO COU. EXDA MAINTENANCE WAS DISPATCHED TO COU AND INSPECTED THE PROPELLER RIGGIN G IAW SHORTS MAINTENANCE MANUAL, NO DEFECTS FOUND. THE AIRCRAFT WAS OPERATIONALLY CHECKED AND THE MAXIUM STATIC TAKEOFF POWER RUNS WERE SATISFACTORILY PERFORMED IAW THE SHORTS MAINTENANCE MANUAL. THE DISCREPANCY COULD NOT BE DUPLICATED ALL SYSTEMS OPERATIONALLY CHECKED NORMAL. N973AA WAS RETURNED TO SERVICE ON 8/11/2007. 2 H 7 2 4T 4 T A41EU E26NE 6 C P14NE 2007082900026 20070829 00026 NM 2007 8 29 MWEA070179 1 20070814 A 7830 7150923REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 923ME 55185 LEFT THRUST REVERSER UPPER BRACKET OUTBOARD FRAME STATION 35 IS CRACKED. FABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007082900027 20070829 00027 2007 8 29 BB07067 4 20070817 A 2565 101651303 SLIDE BOEING 767 767201 1385125 NM DOOR FAILED A USAA K NONE Z SIGNIFICANT FAILURE REPORT IN INSP/MAINT 1 EA 19 246AY 11074 1720 23898 DURING OPERATIONAL CHECK, AFT RIGHT DOOR SLIDE FAILED TO INFLATE. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. 2 L 7 2 4F RT A1NM 2007082900028 20070829 00028 CE 2007 8 29 JBGA200700015 1 20070816 A 2121 66082672 BLOWER MOTOR LEAR 35 31A 5170531 CE COCKPIT MALFUNCTIONED E JBGA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 91DP 079 AIRCRAFT EN ROUTE FROM MDW TO MYGF AT FLIGHT LEVEL 45,000FT WHEN CREW NOTICED SMOKE COMING FROM OVERHEAD VENT. CREW DEC LARED AN EMERGENCY AND INITIATED AN EMERGENCY DESCENT INTO SDF. THE CREW DISENGAGED CABIN VENTILATION WHICH CAUSED SMOK E TO CEASE. CONTINUED WITH DESCENT INTO SDF WITH NO FURTHER PROBLEMS. MAINTENANCE FOUND COCKPIT BLOWER MOTOR TO BE THE CAUSE OF SMOKE, REMOVED AND REPLACED MOTOR, OPS CHECKS GOOD. 2 L 7 2 4F RT A10CE 2007082900030 20070829 00030 NM 2007 8 29 UPS07550452 1 20070717 A 5311 146N103074 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 431UP 25462 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1580, APPROX. S26L. ACCOMPLISHED REPAIR PER FINAL EA 757-5362-A1 711 AND OPS EO B757- 5310-27394-A. 2 L 7 2 4F RT A2NM 2007082900031 20070829 00031 NM 2007 8 29 UPS07550453 1 20070717 A 5311 146N10025 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 431UP 25462 INSPECTION TYPE:C DENT IN AFT FUSELAGE FRAME STA 1220 APPROX S26R. REPAIR ACCOMPLISHED PER FINAL EA 757-5362-A1712 AND UPS EO B757- 7-5310-27419-A. 2 L 7 2 4F RT A2NM 2007082900032 20070829 00032 WP 2007 8 29 UPS07850442 1 20070806 A 5320 FINGER DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 CENTER WING BOX SUBFLOOR FINGER DOUBLER CRACKED AT STA 890 LBL 5. REMOVED CRACKED FINGER DOUBLER AT STA 890 LBL 5 IAW SRM 51-1-20D, FABRICATED AND INSTALLED REPAIR FINGER DOUBLER AT STA 890 LBL 5 IAW SRM 53-07-03-0 FIG 0 04. 2 L 7 4 4F RT 4A25 2007082900033 20070829 00033 WP 2007 8 29 UPS07850443 1 20070722 A 5534 ATTACH ANGLE DOUG DC8 DC873F 302199F WP VERTICAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 LEFT SIDE OF VERT STAB LWR ATTACH ANGLE CRACKED AT STA 1766. REPAIRED LEFT SIDE OF VERT STAB LWR ATT ACH ANGLE AT STA 1766 IAW SRM 53-02-05-0 FIG 016A. 2 L 7 4 4F RT 4A25 2007082900034 20070829 00034 WP 2007 8 29 UPS07850444 1 20070725 A 5313 4641324U501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 L-31R END FITTING CRACKED AT STA 1690. REMOVED AND REPLACED LONGERON END FITTING AT STA 1690 L31R IA W SRM 51-1-21, AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 2007082900037 20070829 00037 NM 2007 8 29 UPS07M50447 1 20070715 A 5730 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C RIGHT WING L/E CORRUGATED SKIN FOUND CRACKED AT 04 EA PLACES AROUND RIVETS AT 14 INCHES O/B OF REFUEL PANEL I/B EDGE AS MARKED. CRACKED AREA TRIM OUT PER SRM TEMP REV 57-10-00 FIG 25B R38. HFEC INSP C/O PER DAC NDT SPM R EV13 PART6 06-10-01.001 ON TRIM OUT AREA. NO CRACK EVIDENT. REPAIR FILLER, DOUBLER & ANGLES FAB PER SRM TEMP REV 57-10 -00 FIG 28B R38. NEW REPAIR FILLER, DOUBLER & ANGLES INSTALLED PER SRM 51-35-01 VII R38 & SRM 51-33-01VII R38. 2 L 7 3 4F RT A22WE 2007082900039 20070829 00039 NM 2007 8 29 UPS07M50449 1 20070705 A 5730 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C RIGHT WING L/E LOWER ACCESS WELL AREA FOUND CRACKED 6 INCHES LONG ON UPPER SKIN REINFORCED STRAP AT 6 INCHES O/B OF SLAT TRACK NR 10 AS MARKED. CRACKED STRAP AT AFFECTED AREA REMOVED PER SRM 51-31-01 VII R38. NEW STRAP F AB PER DWG ARB3954-6. NEW STRAP, RIB AND CLIP INSTALLED PER SRM 51-31-01 VII R38 AT AFFECTED AREA. 2 L 7 3 4F RT A22WE 2007082900040 20070829 00040 NM 2007 8 29 ASAA0741949 1 20070813 A 5210 MS166242037 SNAP RING BOEING 737 737490 1384715 NM L1 DOOR MISSING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 705AS 29318 L1 DOOR DIFFICULT TO OPEN. FOUND RETAINING RING FOR GUIDE ARM MISSING. REINSTALLED SNAP RING, OPS NORMAL. 2 L 7 2 4F RT A16WE 2007082900041 20070829 00041 NM 2007 8 29 ASAA0771953 1 20070814 A 5755 113A44001 SKIN BOEING 737 737790 13844CN NM NR 4 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 NR 4 SPOILER HAS DENT ON LOWER SURFACE. REPAIRED IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007082900042 20070829 00042 NM 2007 8 29 ASAA0771954 1 20070814 A 5755 113A46002 SKIN BOEING 737 737790 13844CN NM NR 7 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 NR 7 SPOILER HAS DENT ON LOWER SURFACE. REPAIRED IAW MM 27-62-12. 2 L 7 2 4F RT A16WE 2007082900045 20070829 00045 NM 2007 8 29 ASAA0771952 1 20070814 A 5321 453A26101 FLOORBOARD BOEING 737 737790 13844CN NM CARGO BAY DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 AFT PIT FLOORBOARD DAMAGED AT STA 771 887. REPAIRED IAW SRM 51-40-05. 2 L 7 2 4F RT A16WE 2007082400305 20070824 00305 SO 2007 8 24 XGN2007F00024 2 20070718 A 8530 TISN712ACA CYLINDER BEECH 36 36BEECH 1151602 CE CONT O520 IO520BA 17032 SO NR 3 CRACKED E XGNA K NONE O OTHER IN INSP/MAINT 1 SW 05 1194A 611 E159 REV 3, E SERIES CYLINDER ASSY 611.9. SINCE NEW, CRACKED ON TOP OF CYLINDER BEHIND FUEL INJECTOR BETWEEN FIRST AND THIRD FIN. COMPRESSION CHECK WITH SOAPY WATER REVEALED CRACK. CAN NOT SEE WITH THE NAKED EYE. (K) 1 L 7 1 3O 3 O 3A15 E5CE 2007082400325 20070824 00325 WP 2007 8 24 ARWA20070802 1 20070818 A 7722 INDICATOR DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 2 ENGINE MALFUNCTIONED A ARWA A UNSCHED LANDING R N PARTIAL RPM/PWR LOSS FALSE WARNING CL CLIMB 1 SO 19 441J 45988 POWER REDUCTION REQUIRED ON NR 2 ENGINE AFTER TAKEOFF IN ORDER TO MAINTAIN EGT LIMIT. 09-04-07 REMOVED AND REPLACED N R 2 EGT INDICATOR IN ACCORDANCE WITH MM 77-20-1. REMOVED AND REPLACED FCU IN ACCORDANCE WITH DC-8 M/M 7320-1; ACCOMPLIS HED ENGINE RUN-UP IN ACCORDANCE WITH DC-8 MM 71-00, FOUND NORMAL, EGT OK, NO LEAKS. 2 L 7 4 4F 4 F 4A25 1E8 2007082400338 20070824 00338 EA 2007 8 24 TRAX200701167 1 20070809 A 5720 ATTACH BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 839AS 7284 RIGHT WING I/B LEADING EDGE O/B ATTACH BRACKET CRACKED. REMOVED RIGHT WING I/B LEADING EDGE O/B ATTACH BRACKET. OK TO INSTALL SERVICEABLE RT WING I/B LEADING EDGE O/B ATTACH BRACKET P/N 600-12025-8. INSTALLED SERVICEABLE RT WING I/B LEAD ING EDGE O/B ATTACH BRACKET P/N 600-12025-8 IAW CRJ 200 AMM SECTION 20-21-0. SUPPLEMENTAL - SDR CLOSED 08/22/07. 2 L 7 2 4F RT A21EA 2007082400341 20070824 00341 EA 2007 8 24 TRAX200701215 1 20070816 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 976EV 7601 FLAPS FAILED AT 0 DEGREES. EMERGENCY DECLARED. SKEW DETECTION SYSTEM. 09-06-07 REMOVED SKEW DET. DUMMY UNIT AND INS TALLED NEW SKEW DETECTION UNIT IAW CRJ AMM 27-51-15. PERFORMED OPS TEST OF SKEW DETECTION SYSTEM IAW TASK 27-51-15-710-8 02. OPS CK GOOD. PEFORMED OPS TEST OF FLAP SYSTEM TASK 27-54-00-710-801. OPS CK GOOD. 2 L 7 2 4F RT A21EA 2007082400358 20070824 00358 NM 2007 8 24 SWAA074129 1 20070821 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007082400367 20070824 00367 NM 2007 8 24 CALA0700452 1 20070807 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND CRACKS TO THE LONGITUDINAL FLOORBEAM FLANGES AT STA 727B, LBL 45.5, RBL 45.5 AND RBL 24.8. REPAIRS WER E PERFORMED IAW ECRA 5321-01492. 2 L 7 2 4F RT A16WE 2007082400368 20070824 00368 NM 2007 8 24 QXEA200701343 1 20070818 A 2197 CONNECTOR DHAV DHC8 DHC8202 2809007 NM OUTFLOW VALVE LOOSE A QXEA O OTHER O OTHER CL CLIMB 1 NM 09 349PH 486 PDX FLIGHT NR 2093, AFTER TAKEOFF AIRCRAFT BEGAN PRESSURIZATION AT HIGH RATE, CABIN DIFF OF 5.75 REACHED BY 4000 FEET MS L. SWITCHED TO MAIN MODE, NO CONTROL. ATTEMPTED TO DUMP CABIN WOULDN'T DUMP. FINALLY DUMPED CABIN PRESSURE FOR LANDIN G BY OPENING FORWARD OUTFLOW VALVE. RE-SECURED CONNECTOR ON CABIN PRESSURE CONTROLLER. PRESSURIZED AIRCRAFT ON GROUND IN DUMP, AUTO AND MANUAL IAW DHC-8-200 AMM 21-30-00. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007082400369 20070824 00369 EA 2007 8 24 TRAX200701221 1 20070819 A 3350 COVER CNDAIR CL600 CL6002B19 1900309 EA CABIN OUT OF POSITION A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 972EV 7534 EMERGENCY EXIT ROW LIGHT COVER AT ROW 8 FELL OFF. 2 L 7 2 4F RT A21EA 2007082400372 20070824 00372 NM 2007 8 24 F3LA200700201 1 20070817 A 3350 LAMP AIRBUS A319 A319111 3930336 NM EMERGENCY LIGHT INOPERATIVE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 932FR 2258 DURING HEAVY CHECK, INSPECTION REPORTED EMERGENCY FLOOR PATH WHITE LIGHT AT ROW 5 INOPERATIVE. RELAMPED BOTH LAMPS AT R OW 5 EMERGENCY FLOOR PATH WHITE LIGHT. OPS CHECKED GOOD IAW AMM 33-51-19-400-002. 2 L 7 2 4F RT A28NM 2007082400373 20070824 00373 EA 2007 8 24 TRAX200701119 1 20070806 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 755EV 10185 RIGHT FS 280 CROSSBEAM CRACKED ON UPPER FLANGE O/B OF RBL 9.0. REMOVED RIGHT FS 280 DAMAGED BEAM. LOCATED NEW RIGHT, F S 280 FLOORBEAM, P/N CC670-34175-7, IAW CRJ 700 SRM 51-40-11. OK TO INSTALL. INSTALLED RIGHT FS 280 BEAM, IAW CRJ SRM 51-42-06 AND 51-42-21. OKAY TO TOPCOAT PAINTED IAW CRJ SRM 51-25-16. SUPPLEMENTAL - SDR CLOSED 08/14/07. 2 L 7 2 4F RT A21EA 2007082800002 20070828 00002 EU 2007 8 28 2007UALA03208 1 20070816 A 3320 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN LIGHTS UNKNOWN A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 461UA 1266 CABIN LIGHTS FLICKER AND EMERGENCY LIGHT RIGHT SIDE WINDOW INTERMITTENT. CYCLING SWITCH DIDN`T FIX. CREW REPORTING LIG HTS FLICKING THROUGHOUT CABIN ON BOTH LT AND RT SIDES WITH RESET NO HELP, AND FLT ATTENDANT STATED APPEARED TO BE FLASHI NG WITH SPEED CHANGES. INSPECTED BOTH IDG'S AND SERVICED. INSPECTED AND CLEANED FEEDER FROM IDG'S TO FIREWALL CONNECT ORS, ALL GOOD. NO DEFECTS NOTED, NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082800005 20070828 00005 NM 2007 8 28 2007UALA03211 1 20070816 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 814-816 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 EXTERNAL FUSELAGE SKIN HAS CRACK INDICATION AT STR 14L CHEM MILL STEP BTWN BS 814 AND BS 816. MAJOR REPAIR ACCOMPLISHED : REMOVED DAMAGE. INSTALLED EXTERNAL FUSELAGE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082800010 20070828 00010 NE 2007 8 28 2007UALA03216 2 20070816 A 7297 WIRE HARNESS BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE ENGINE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 214UA 30220 FOUND ENGINE HARNESS W0623 DAMAGED AT 9 O'CLOCK POSITION. BUNDLE MELTED THRU TO INNER WIRES. FOUND ENG HARNESS W0623 D AMAGED AT 9 O'CLOCK. BUNDLE MELTED THRU TO INNER WIRES. REPLACED HARNESS, READJUSTED CLAMPS, RAN ENGINE AND ALL CHECKE D NORMALLY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007082800023 20070828 00023 NM 2007 8 28 2007UALA03229 1 20070818 A 2420 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GENERATOR UNKNOWN A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 551UA 25399 RTFL DUE TO A GENERATOR PROBLEM. EICAS MESSAGE FOR RIGHT GENERATOR DRIVE DISPLAYED WHILE CLIMB OUT AT 10000 FT. THE ROOT CAUSE OF THIS ACTION BY THE PILOT WAS DUE TO ILLUMINATION OF GENERATOR DRIVE LIGHT AS A RESULT OF A DISCONNECTED GE NERATOR DRIVE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082800030 20070828 00030 NM 2007 8 28 2007UALA03236 1 20070819 A 2611 CONTROLLER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SMOKE DETECTOR FAULTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 224UA 30225 DET CHAN 1 CARGO FWD FORWARD CARGO COMPARTMENT SMOKE DETECTOR CONTROLLER CHANNEL NR 1 FAILURE STATUS. 08-31-07 PERFO RMED MTCE ACCESS TERMINAL FWD CARGO SMOKE DETECTOR TEST. SHOWS INTERMITTENT FAULT, MSG 26-20021. :REPLACED CARGO SMOKE DETECTOR. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007082800037 20070828 00037 NM 2007 8 28 2007UALA03243 1 20070818 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 646UA 25283 FOUND AFT GALLEY RT EEL STRIP INOPERATIVE. REPLACED LAMP STRIP. TEST OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082800041 20070828 00041 NM 2007 8 28 2007UALA03247 1 20070819 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 FOUND RIGHT LAV AT MID GALLEY EEL STRIP INOPERATIVE. REPAIRED EEL STRIP, OP CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082800045 20070828 00045 NM 2007 8 28 2007UALA03251 1 20070817 A 5511 SPAR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZONTAL STAB DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 LT HORIZ STAB TE CAVITY 2ND BALANCE BAY OB INBD SIDEWALL HAS GROOVE WORN 3-5" AFT OF REAR SPAR. MAJOR REPAIR ACCOMPLISH ED: FILLED GOUGE SMOOTH AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082800047 20070828 00047 NM 2007 8 28 2007UALA03253 1 20070819 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 938 S25L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 308UA 23669 FUSELAGE SKIN CRACKED AT STA 938 AND 1FT ABOVE STRINGER 25L.CRACK STARTS FROM SKIN RADIUS AND EXTENDS BEYOND RIVET HOLE, APPROX LOCATION IS 1FT FWD OF WATER SERVICE PANEL. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082800058 20070828 00058 EU 2007 8 28 07FDEA03004 1 20070821 A 5313 A53980877 STRINGER AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 CORROSION ON STRG 56 LT AND RT OUTER FLANGE BETWEEN C76-77. REPAIR PERFORMED BY BLEND OUT WITHIN THE LIMITS AS PER REPA IR REF EA 6-5318-103300, APPROVED BY RAS/DATLS/0003345/2006 ISS "B". 2 L 7 2 4F RT A35EU 2007082800077 20070828 00077 EA 2007 8 28 SWIA200718590 1 20070621 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 452SW 7716 FS 280 FLOOR SUPPORT BEAM IS CRACKED AT LBL9, FOUND AT C-CHECK. COMPLIED WITH STANDARD REPAIR 601R 53-00-57A TO REPAIR FS280 LBL9 UPPER FLANGE OF FLOOR SUPPORT BEAM. 2 L 7 2 4F RT A21EA 2007082800086 20070828 00086 SO 2007 8 28 SWIA200718599 1 20070703 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 236SW 120312 RIGHT WING, NR 2 FUEL PANEL, FORWARD STRINGER IS CRACKED, FOUND AT C-CHECK. APPLIED STRINGER SPLICE SECTION IAW SRM 120 57-20-03. 2 L 7 2 4T RT A31SO 2007082800087 20070828 00087 SO 2007 8 28 SWIA200718600 1 20070703 A 5210 SUPPORT BRACKET EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 236SW 120312 CRACK ON PAX DOOR AFT SIDE NEAR 4TH SHIM STOP, DISCOVERED AT C-CHECK. REPLACED PAX DOOR AFT MID CLEAT SUPPORT BRACKET I AW 120 SRM 51-10-02 PG 3, SEC 3. 2 L 7 2 4T RT A31SO 2007082800088 20070828 00088 SO 2007 8 28 SWIA200718601 1 20070718 A 5210 RIB EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 580SW 120348 PAX DOOR, AFT MID INTERNAL RIB IS CRACKED, FOUND AT C-CHECK. NEW RIB INSTALLED IAW SRM 120 51-10-02 PG 3 SEC 3A. 2 L 7 2 4T RT A31SO 2007082800105 20070828 00105 NM 2007 8 28 DLM90071087 1 20070816 A 5330 5936667143 SKIN DOUG MD90 MD9030 3023690 NM FS 1350 L26-28R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 DURING HMV, DETN AND GOUGE DAMAGE WERE FOUND ON THE SKIN ADJACENT TO AN EXISTING REPAIR INSTALLED PER 365416-14. THIS R EPAIR WAS REMOVED, THE ADDITIONAL DAMAGE WAS CUTOUT, AND A BOEING APPROVED REPAIR WAS INSTALLED PER 462740-14 2 L 7 2 4F RT A6WE 2007082800110 20070828 00110 NM 2007 8 28 DL764071092 1 20070817 A 5730 SKIN BOEING 767 767432ER 1385134 NM LT WING DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830MH 29701 LEFT WING OB END OF RAKED WING LOWER SKIN HAS EDGE DELAMINATION. REPAIRED LOWER SKIN DELAMINATION BY APPLYING GRAPHITE LAYUP REPAIRS IAW DELTA ERA 463393. REPAIR COMPLIED WITH BYTIMCO DURING HMV-1 IN GSO. 2 L 7 2 4F RT A1NM 2007082800132 20070828 00132 NM 2007 8 28 DLM88071116 1 20070817 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 1098 -1117 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 EXFOLIATION CORROSION ON RT CUSP WEB FRON STA 1098 TO 1117 REPAIR PER ERA 398191-14MA REV A. 2 L 7 2 4F RT A6WE 2007082800141 20070828 00141 NM 2007 8 28 DLM88071125 1 20070817 A 5320 PAN DOUG MD88 MD88 3023688 NM FWD CARGO DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 EXFOLIATION CORROSION ON FWD CARGO COMPARTMENT DOOR JAMB LWR BEAM. REPLACED IAW SRM 53-05D FIG 804. 2 L 7 2 4F RT A6WE 2007082800143 20070828 00143 NM 2007 8 28 DLM88071127 1 20070817 A 5300 ANGLE DOUG MD88 MD88 3023688 NM STA.787 27/28LH CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 CRACKED FITTING BETWEEN FRAME AND INTERCOSTAL AT STA 787 BETWEEN LONGERON 27 LH AND 28LH. REPLACED FITTING PER DRWG 595 6034 ON N/R T0065338 IN HMV AT GDL. 2 L 7 2 4F RT A6WE 2007082800171 20070828 00171 WP 2007 8 28 07FDEA03031 1 20070822 A 5330 NDA60141 SKIN DOUG DC10 DC1010 3022110 WP BS 1039 L52R CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 LOWER EXT FUSELAGE PERFORMED INSPECTION AFTER ADF ANTENNA REMOVAL WITH OAN J/C SP10240167-7004-1JR. FOUND SEVERE CORROS ION WITH EXFOLIATION ON EXT SKIN C/L. REPAIRED AREA IAW SRM 53-20-00 VOL 1 FIG 6 SHT 3-4. 2 L 7 3 4F A22WE 2007082800175 20070828 00175 EU 2007 8 28 07FDEA03035 1 20070822 A 5710 A577942552 BEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 CHAFING MARKS FOUND ON VERTICAL WEB OF FLAP TRACK BEAM 2 INBOARD CHANNEL LHS. REPAIR PERFORMED BY BLEND OUT WITH NDT IN SPECTION IAW EA 6-5720-103376 AND RAS/BAE/1003599/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007082800183 20070828 00183 EU 2007 8 28 07FDEA03044 1 20070822 A 5714 A57111092202 ANGLE AIRBUS 300 A300B4605R 3930308 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 DAMAGES, CRACKS AND CORROSION FOUND IN ANGLE FITTING HOLES IN CENTER WING BOX FRAME 47. REPAIR PERFORMED BY OVERSIZING THE HOLES IAW EA 6-5710-112481 AND RAS/013359/011/2001 ISS "A" AND RAS/053362014/2007 ISS "A". 2 L 7 2 4F RT A35EU 2007082800185 20070828 00185 WP 2007 8 28 07FDEA03046 1 20070822 A 5730 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 LT WING L/E CRACK ON EXTERNAL LOWER SKIN. 2 L 7 3 4F A22WE 2007082800187 20070828 00187 WP 2007 8 28 07FDEA03048 1 20070822 A 5330 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 EXT FUSELAGE RT SIDE FOUND DENT .45" BY .25" DEEP 0.027" ON SKIN. 09-19-07 REPAIRED SKIN IAW SRM 53-20-00 FIG 13 SHT 3 -5 VOL I. 2 L 7 3 4F A22WE 2007082800212 20070828 00212 EU 2007 8 28 07FDEA03060 1 20070823 A 5210 A52175004203 SKIN AIRBUS 310 A310324 3930206 EU ZONE 800 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 OLD REPAIR DOUBLER ON AFT PAX DOOR RT (ZONE 843) THIS ONES MATERIAL DOES NOT CONFORM TO SRM 52-10-00/FIG 204. REPAIR PE RFORMED BY RENEWING SKIN REPAIR IN ACCORDING SRM 52-10-00/FIG 204. 2 L 7 2 4F RT A35EU 2007082800218 20070828 00218 SO 2007 8 28 SWIA200718606 1 20070819 A 5330 SKIN EMB 120 EMB120ER 3260203 SO FUSELAGE DENTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 578SW 120346 DENT ON RIGHT SIDE OF AIRCRAFT AFT OF LAV SERVICE DOOR. REPAIRED RIGHT SIDE FUSELAGE SKIN IAW SRM 53-00-01. 2 L 7 2 4T RT A31SO 2007082900001 20070829 00001 SO 2007 8 29 SWIA200718608 1 20070812 A 5210 ROLLER EMB 120 EMB120ER 3260203 SO PAX DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 564SW 120339 MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN, FLIGHT NR 5752. LUBED ROLLERS AS REQUIRED. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2007082900009 20070829 00009 NM 2007 8 29 UPS07550433 1 20070717 A 5311 146N102911 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 431UP 25462 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1460, APPROX S25L. ACCOMPLISHED REPAIR PER EA 757-5362-27-A1710 AND UPS EO B757-5310-27393-A. 2 L 7 2 4F RT A2NM 2007082900017 20070829 00017 NM 2007 8 29 UPS07M50438 1 20070717 A 5720 CABLE GUARD DOUG MD11 MD11F 3023600 NM LT WING CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C LEFT WING - L/E PANEL NR 527AB U-BRACKET GUARD FOUND CHAFING AS MARKED. LEFT WING - L/E PANEL NR 527A B U-BRACKET GUARD CHAFE MARK REMOVED. ORG THK 0.0 63" MATL REMAIN 0.040" MATL REMOVED 0.023". FOUND EXCEED LIMIT SRM 5 1-00-01F IGAVIR38. CHAFED BRACKET GUARD REMOVED SRM 51-33-01 VII R38. CABLE GUARD FAB USE MATL 2024T3-0.063" THK PER D OUGLAS DWG ARB2946. FAB U-BRACKET INSTALLED PER SRM 51-33-01VII R38. 2 L 7 3 4F RT A22WE 2007082900029 20070829 00029 NM 2007 8 29 UPS07550445 1 20070720 A 5412 311N32713 BULKHEAD BOEING 757 75724APF 1384969 NM NR 1 PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 431UP 25462 INSPECTION TYPE:C NR 1 PYLON AFT BULKHEAD LOWER OUTBOARD CORNER IS CHAFED. BULKHEAD MILL WAS DONE ON TRAV T7/693383 PER PRELIMINARY 1 EA B757-5453-27-A1716. HFEC WAS DONE ON TRAVELER T7/693383 PER PRELIMINARY EA B757-5453-27-A1716. LENGT H OF BLEND 2.1X1.250WX. .080D PER PRELIMINARY 1 EA B757-5453-A1716. 2 L 7 2 4F RT A2NM 2007082900035 20070829 00035 WP 2007 8 29 UPS07850451 1 20070806 A 5340 WEB DOUG DC8 DC873F 302199F WP SERVICE DOOR PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 HOLE PUNCTURED IN INTERIOR WEB OF RIGHT FWD SERVICE DOOR FWD CENTER AREA. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM5 2-02-00 FIG 4, SRM 52-03-01 FIG 3, 52-02-00, 51-01-21, AND 51-01-11. 2 L 7 4 4F RT 4A25 2007082900043 20070829 00043 WP 2007 8 29 ASAA0781951 1 20070815 A 5320 993053875 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 943AS 53018 CABIN RIGHTHAND CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED DOUBLER PER SRM 51-70-4. 2 L 7 2 4F RT A6WE 2007082900048 20070829 00048 NM 2007 8 29 ASAA0771955 1 20070814 A 5754 SKIN BOEING 737 737790 13844CN NM L/E SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 NR 5 SLAT LOWER SIDE CHAFED. REPAIRED IAW SRM 51-70-70. 2 L 7 2 4F RT A16WE 2007082900049 20070829 00049 NM 2007 8 29 ASAA0771956 1 20070814 A 5754 SKIN BOEING 737 737790 13844CN NM L/E SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 NR 8 SLAT LOWER SIDE T/E CHAFED. REPAIRED IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007082900050 20070829 00050 NM 2007 8 29 ASAA0771957 1 20070814 A 5754 114A50204 SLAT BOEING 737 737790 13844CN NM WING CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 NR 7 SLAT LOWER SIDE EG IS CHAFED. REPAIRED IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007082900053 20070829 00053 NM 2007 8 29 ASAA0771961 1 20070814 A 5754 SKIN BOEING 737 737790 13844CN NM L/E SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 NR 3 SLAT LOWER SIDE T/E IS CHAFED. REPAIRED IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007082900054 20070829 00054 NM 2007 8 29 ASAA0771962 1 20070814 A 5754 SKIN BOEING 737 737790 13844CN NM L/E SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 NR 2 SLAT LOWER SIDE T/E CHAFED. REPAIRED IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007082900055 20070829 00055 NM 2007 8 29 ASAA0771963 1 20070814 A 5754 SKIN BOEING 737 737790 13844CN NM L/E SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 NR 1 SLAT LOWER SIDE T/E IS CHAFED. REPAIRED IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007082900057 20070829 00057 NE 2007 8 29 WRLA2007081 2 20070809 A 7200 PW4460 ENGINE DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 3 OVERTEMP A WRLA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 11 803DE 28761 48474 P723923 KBGR/EINN, IN CRUISE FLIGHT EXPERIENCED MODERATE VIBRATION FOLLOWED BY LEVEL 2 ALERT SELECT FADEC ALT NR 3. RETARDED TH ROTTLE HALF WAY & SELECTED NR 3 FADEC TO ALT. EGT CONTINUED TO RISE. IN FLIGHT ENGINE SHUT DOWN CHECKLIST WAS ACCOMPLI SHED. EMERGENCY DECLARED, DIVERTED TO EINN. EMERGENCY FIRE & RESCUE EQUIPMENT WAS REQUESTED IN EINN. REMOVED AND REPL ACED NR 3 ENGINE IAW WOA WORK ORDER D10113 AND WOA TASK CARD 0104. 2 L 7 3 4F 4 F RT A22WE E24NE 2007082900059 20070829 00059 NM 2007 8 29 ASAA0741966 1 20070814 A 2131 7638101 CONTROLLER BOEING 737 737490 1384715 NM CABIN PRESSURE MALFUNCTIONED A ASAA K NONE J WARNING INDICATION CR CRUISE 1 NM 02 788AS 28885 AT CRUSE ALTITUDE HORN CAME ON (FLT LVL 330). CABIN CLIMBING TO 11000 FT. FOLLOWED QRH. NO OTHER INDICATIONS BESIDES ALTITUDE WARNING HORN AND CABIN CLIMBING. LANDED AT KTN, REMOVED AND REPLACED CABIN PRESSURE CONTROLLER PER AMM. 2 L 7 2 4F RT A16WE 2007082900060 20070829 00060 NE 2007 8 29 SIMA200722502 2 20070811 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE NR 1 BIRD INGESTION A SIMA A UNSCHED LANDING C R J F.O.D. PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 SW 21 263AE 16870 484 340B263 GEE785605 BIRD STRIKE TO NUMBER 2 ENGINE FOLLOWED BY COMPRESSOR STALLS AND ITT OVERTEMP LIGHT. RETURNED TO FIELD. REMOVED AND RE PLACED NUMBER ONE ENGINE IAW AMERICAN EAGLE WORK CARD 72-4903. OP[ERATIONAL CHECK GOOD - RETURNED AIRCRAFT TO SERVICE 2 L 7 2 4T 4 T RT A52EU E8NE 2007082900061 20070829 00061 NM 2007 8 29 ASAA0741967 1 20070814 A 3520 417N31401SP DOOR BOEING 737 737490 1384715 NM PSU OBSTRUCTED A ASAA O OTHER O OTHER CR CRUISE 1 NM 02 788AS 28885 O2 MASK AT SEAT 7ABC DID NOT DEPLOY. O2 MASK IN RIGHT AFT LAV DID NOT DEPLOY. FOUND MASK HOSES CAUGHT ON PSU DOOR. RE PACKED MASK, REMOVED AND REPLACED RIGHT AFT LAV OXY GEN REF MM 35-22-11. COMPLETED ACTIVATION PROCEDURE REF MM 35-22-11 STEPS 3D(4). OPS CK GOOD. REF MM 35-22-00 PG 506, 507. 2 L 7 2 4F RT A16WE 2007082900062 20070829 00062 NM 2007 8 29 ASAA0741968 1 20070817 A 5754 65C26603191 SKIN BOEING 737 737490 1384715 NM L/E SLAT WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 NR 3 SLAT INBOARD T/E LWR SURFACE SKIN WORN. REPAIRED SLAT DAMAGE IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007082900063 20070829 00063 NM 2007 8 29 TAMF20070007S 1 20070804 A 5751 WEB BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE LT AILERON WORN W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 767QT 23804 DURING (C) CHECK INSPECTION (TASK CARD 57-592-00) WAS FOUND WORN OUT OF LIMITS ON IB AILERON LT - OB CLOSURE RIB WEB. D AMAGE WAS REPAIRED IAW BOEING SERVICE REQUEST 1-500301558 AND EWO 767-57-024. ALSO, FAIL-SAFE FITTING PN 113T6145-11 WAS FABRICATED AND INSTALLED IAW BOEING SMAL AUTHORIZATION (PO 201008703). MAJOR REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007082900064 20070829 00064 NM 2007 8 29 ASAA0741969 1 20070817 A 5753 6546486 SKIN BOEING 737 737490 1384715 NM MID FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 RIGHT INBOARD MID FLAP DENT ON UNDERSIDE LOCATED 9 INCHES OUTBOARD OF INBOARD END AND 3 INCHES FWD OF T/E. FLAP DENT RE PAIRED IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007082900066 20070829 00066 NM 2007 8 29 ASAA0741971 1 20070817 A 5320 69774772 ANGLE BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 AFT CABIN ZEE ANGLE CORRODED. REPLACED WITH FABRICATED REPAIR IAW SRM 51-40-03 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007082900067 20070829 00067 NM 2007 8 29 ASAA0741972 1 20070817 A 5320 69774771 ANGLE BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 AFT CABIN ZEE ANGLE CORRODED. REPLACED WITH FABRICATED REPAIR PART IAW SRM 51-40-02 AND 51-40-05. 2 L 7 2 4F RT A16WE 2007082900068 20070829 00068 NM 2007 8 29 ASAA0741973 1 20070817 A 5320 6517684156 STRAP BOEING 737 737490 1384715 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 INTERCOSTAL STRAP CRACKED. REPLACED WITH NEW PART IAW EA 5310 02732. 2 L 7 2 4F RT A16WE 2007082900071 20070829 00071 NM 2007 8 29 ASAA0741976 1 20070817 A 5320 6552878U102 SILL BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 AFT CABIN DOORWAY SILL CHORD CORRODED. REPLACED WITH NEW PART PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007082900072 20070829 00072 NM 2007 8 29 ASAA0741977 1 20070817 A 5754 65C2679914 SKIN BOEING 737 737490 1384715 NM L/E SLAT CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 RIGHT WING NR 6 SLAT I/B CORNER 2 INCH CRACK FOUND. RIGHT WING NR 6 SLAT I/B CORNER CRACK REPAIRED IAW SRM 57-43-01 FIG 201. 2 L 7 2 4F RT A16WE 2007082900073 20070829 00073 NM 2007 8 29 ASAA0741978 1 20070817 A 5753 6546435281 SKIN BOEING 737 737490 1384715 NM T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 LEFT O/B AFT FLAP HAS NUMEROUS DENTS AT LWR SURFACE. LEFT O/B AFT FLAP LWR SURFACE AT RSS 300 312 REPAIRED IAW SRM 51-7 0-10. 2 L 7 2 4F RT A16WE 2007082900074 20070829 00074 SO 2007 8 29 C2XA07SH047 1 20070815 A 5751 14573900420 SHROUD EMB 145 EMB145LR 3260212 SO RT AILERON DEBONDED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26545 145558 SHV - DURING C-CHECK MAINTENANCE FOUND RIGHT LWR AILERON SHROUD HAS BAD BONDING ON OUTBOARD END. MAINTENANCE REPAIRED R IGHT LWR AILERON SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007082900075 20070829 00075 SO 2007 8 29 C2XA07SH048 1 20070815 A 5751 1457400416 SHROUD EMB 145 EMB145LR 3260212 SO RT AILERON DEBONDED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26545 145558 SHV - DURING C-CHECK MAINTENANCE FOUND RIGHT UPPER AILERON SHROUD HAS CORRODED BONDING PLATE OUTBOARD END. MAINTENANCE REPAIRED RIGHT UPPER AILERON SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007082900078 20070829 00078 SO 2007 8 29 C2XA07IA185 1 20070809 A 3350 110049 POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 19554 145587 AUS - FLIGHT 308, DURING PREFLIGHT INSPECTION AN EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY FOR THE EMERGENCY EXIT ROWS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND TH E AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007082900081 20070829 00081 NM 2007 8 29 R61A20070013 1 20070806 A 3250 1855A000003 MODULE EMB ERJ170 ERJ170100SU 3260403 NM STEERING SYS MALFUNCTIONED A R61A O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 806MD 17000019 PILOT REPORTED AVIONICS MAU 2 FAIL, AND DCA TOWER DIVERTED AIRCRAFT TO IAD. MAINTENANCE REMOVED AND REPLACED STEERING C ONTROL MODULE SYSTEM, OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A56NM 2007082900083 20070829 00083 SO 2007 8 29 C2XA07CL069 1 20070816 A 2697 14522756405 WIRE HARNESS EMB 135 EMB135ER 3260203 SO NR 1 ENGINE FAULTY A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 16502 145166 CLE FLIGHT 2457 - THE CREW REPORTED A INTERMITTANT ENGINE NR 1 FIRE DETECT FAIL MESSAGE IN FLIGHT. MAINTENANCE INSPECTE D AND REPLACED THE NR 1ENGINE HARNESS. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2007082900084 20070829 00084 SO 2007 8 29 C2XA07CL070 1 20070818 A 3000 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13992 145284 CLE FLIGHT 2310 - THE CREW REPORTED A STRONG BURNING SMELL DURING THE ICE TEST. MAINTENANCE INSPECTED AND PERFORMED ANT -ICE OPERATIONAL CHECKS. NO DEFECTS WERE FOUND. 2 L 7 2 4T RT T00011AT 2007082900086 20070829 00086 CE 2007 8 29 ERYA200715901 1 20070811 A 2721 884151 SWITCH RAYTHN 390 390 7150030 CE RUDDER TRIM MALFUNCTIONED E ERYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 146JF 532 RB159 UNCOMMANDED PITCH, ROLL, AND YAW. UNABLE TO ARREST UNCOMMANDED INPUTS OR CORRECT UNCOORDINATED FLIGHT CONTROLS WITH ANY THING OTHER THAN REDUCTION OF THRUST TO REDUCE FORCE ON FLIGHT CONTROL SURFACES. RUDDER TRIM SWITCH REPLACED. 1 L 7 2 3F RT A00010WI 2007082900089 20070829 00089 NM 2007 8 29 UPS07550460 1 20070805 A 5330 DOUBLER BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 475UP 28845 INSPECTION TYPE:C4 UPPER EXTERIOR DOUBLER AT 1090 ANTENNA, DOUBLER AND SKIN DENTED. REPAIRED PER ENGINEERING REPAIR 07- 3003. 2 L 7 2 4F RT A2NM 2007082900090 20070829 00090 EU 2007 8 29 07FDEA02865 1 20070814 A 7830 32142368 SHUTOFF VALVE AIRBUS 310 A310222 3930315 EU THRUST REVERSER INOPERATIVE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 449FE 217 AFTER LIFTOFF (KATL) ENG NR 1 THRUST REVERSER SHOWED "UNLOCKED". ON TAKEOFF ROLL LIGHT FLICKERED MOMENTARILY THEN WENT OUT. FOLLOWED QRH AND ECAM PROCEDURE AND DECLARED EMERGENCY. REPLACED NR 1 THRUST REVERSER PRESSURE REGULATOR SHUTOFF VALVE PER A310-200 AMM 78-31-05-4 03 AND VALVE CONNECTOR DH9 PER AIRBUS ESPM. NR 1 REVESER OPS CHECKS GOOD. 2 L 7 2 4F RT A35EU 2007082900091 20070829 00091 NM 2007 8 29 UPS07650430 1 20070811 A 2150 UNKNOWN BOEING 767 76734AF 1385212 NM COOLING SYSTEM MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 331UP 27757 INSPECTION TYPE:ETOP BTB - EQUIPMENT COOLING INOP IN AUTO AND STANDBY. T/S SYSTEM PER FIM 21-56-00 FIG 116, NO DEFECTS NOTED. OK TO CONTINUE. 2 L 7 2 4F RT A1NM 2007082900094 20070829 00094 WP 2007 8 29 UPS07850461 1 20070806 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 FITTING CRACKED AT STA 1240 L20R. REMOVED CRACKED FITTING AT STA 1240 L20R IAW SRM 51-01-20D. FABRI CATED AND INSTALLED REPAIR FITTING AT STA 1240 L20R IAW DWG 4750419, AND SRM 51-01-24-0 FIG 002. 2 L 7 4 4F RT 4A25 2007082900095 20070829 00095 WP 2007 8 29 UPS07850462 1 20070811 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 INTERCOSTAL CRACKED AT STA 1650 LBL 3. STOP DRILLED CRACKED INTERCOSTAL AT STA 1650 LBL 3 IAW SRM 51 -1-21, FABRICATED AND INSTALLED REPAIR DOUBLER ON INTERCOSTAL AT STA 1650 LBL 3 IAW DWG 3704315, AND SRM 53-02-00-0 FIG 001B. 2 L 7 4 4F RT 4A25 2007082900097 20070829 00097 EA 2007 8 29 TRAX200701160 1 20070811 A 5210 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 839AS 7284 PAX DOOR INNER FWD FRAME FS 320.10 IS CRACKED AT LOWER END. REMOVED REQUIRED FASTENERS FROM INNER SKIN & FS 338.00 FRAM E IAW REO 601R-52-11-402 CUT AWAY DESIGNATED PORTION OF INNER SKIN IAW REO 601R-52-11-402. COMPLETED STEPS 1 & 2 OF RE0 601R-52-11-402. CUTLIINES REQUIRE LPI 13374 8-16-07. PERFORMED LPI ON PAX DOOR INNER FRAME REPAIR CUTLINES IAW REO 601R- 52-11-402 AND NDTM 51-20-08. NO DEFECTS NOTED. TOUCHED UP CUTLINES IAW REO601R-52-11-402.OK TO INSTALL REPAIR ITEMS. INS TALL REPAIR ITEMS IAW REO601R-52-11-402 13374 8-21-07 . 2 L 7 2 4F RT A21EA 2007082900098 20070829 00098 WP 2007 8 29 UPS07850464 1 20070806 A 5240 WEB DOUG DC8 DC873F 302199F WP SERVICE DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 LARGE PUNCTURE AND 2EA CRACKS IN WEB AT AFT UPPER SECTION OF INTERIOR OF RIGHT FWD SERVICE DOOR. CUT OUT DAMAGED AREA FROM WEB ON RIGHT FWD SERVICE DOOR IAW SRM 52-02-00 FIG 4. FABRICATED AND INSTALLED REPAIR DOUBLER ON RIGHT FWD SERVICE DOOR UPPER WEB IAW SRM 52-03-01 FIG 3 AND 4. 2 L 7 4 4F RT 4A25 2007082900100 20070829 00100 NM 2007 8 29 07FDEA02922 1 20070815 A 5330 6554583164 SKIN BOEING 727 727233 138408A NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 254FE 20936 EXT FUSELAGE SKIN DENT APPROX STA 1153 BETWEEN S-17L - S-19L, REPAIRED IAW SRM 53-30-3. 2 L 7 3 4F RT A3WE 2007082900101 20070829 00101 WP 2007 8 29 UPS07850466 1 20070804 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 FITTING CRACKED AT STA 1230 TO STA 1240 L19R. REMOVED CRACKED FITTING AT STA 1230 TO 1240 L19R IAW S RM 51-01-20D, FABRICATED AND INSTALLED REPAIR FITTING AT STA 1230 TO 1240 L19R IAW SRM 51-01-20D, AND DWG 3758513. 2 L 7 4 4F RT 4A25 2007082900103 20070829 00103 NM 2007 8 29 07FDEA02923 1 20070815 A 5320 653954811 WEB BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 254FE 20936 CABIN FS 1183 BULKHEAD LT OB FLOOR WEB HAS CRACKS. REMOVED AND REPLACED FLOOR WEB IAW SRM 51-30-2. FABRICATED NEW FLOO R WEB .020 ON TRAVELER T7/1695713 IAW SRM 51-30-6 TABLE 1. 2 L 7 3 4F RT A3WE 2007082900104 20070829 00104 NM 2007 8 29 UPS07M50459 1 20070518 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C CABIN - SEAT TRACK AT STA 1965 LBL 107 FOUND CORRODED. CORRODED EXISTING TRACK TRIMMED OFF FR STA 183 1-2007 PER SRM 53-70-00 V1 FIG 7R.38. HFEC INSP C/OUT PRT DAC NDTSPM R.13 06-10-01.001 FOUND NO CRACK EVIDENT. SEAT TR ACK SPLICE HAT, SPLICE PLATE FAB PER SRM 53-70-00 V1 R38. HOLES P/UP TO FAB PARTS & ALODINE C/OUT PER SRM 51-31-01 & 51 -21-01 V2 R38. HOLES P/UP TO SEAT TRACK. SEAT TRACK & FAB PARTS INSTALLED PER SRM 51-31-01 V2 R38. 2 L 7 3 4F RT A22WE 2007082900105 20070829 00105 NM 2007 8 29 UPS07M50467 1 20070714 A 5712 RIB DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C RIGHT WING FIXED WING L/E INTERIOR AREA APPROX STA XOS 667 FOUND RIB CRACKED. CRACKED RIB REMOVED (RE F C/N: MD072549, STEP FOR WORK DETAILS). NEW RIB FAB PER DWG ARB2930-20. RIB HEAT - TREATED PER DPS 7.00-1 & HARDNESS VALUE HRB 81.7 PER DPS1.05-3. HOLE PICKED UP SRM 51-31-01 VII R38. NEW RIB REPROTECTED AND PAINTED SRM 51--21-01 VII R 38. RIB INSTALLED REF C/N: MD072549 FOR WORK DETAILS. 2 L 7 3 4F RT A22WE 2007082900106 20070829 00106 NM 2007 8 29 07FDEA02925 1 20070815 A 5320 69457282 WEB BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 254FE 20936 FWD CARGO COMPT BETWEEN BS 580-600 S28R OUTER WEB LOWER ANGLE HAS SURFACE CORROSION. REMOVED AND REPLACED WEB IAW SRM 5 1-30-2. FABRICATED WEB ON TRAVELER T7/695113. 2 L 7 3 4F RT A3WE 2007082900109 20070829 00109 NM 2007 8 29 SB07064 1 20070815 A 3397 WIRE BOEING 737 7374B7 1384702 NM EMERGENCY LIGHTS BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 444US 24862 BDL - MAINTENANCE REPORTED THE FORWARD COAT CLOSET EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE COAT CLOSET. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007082900111 20070829 00111 NM 2007 8 29 SB07065 1 20070815 A 2133 7110033 OUTFLOW VALVE BOEING 737 737301 1384611 NM AFT FUSELAGE STICKING A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 503UW 42993 42993 23237 CLT FLT 1107 - DURING CRUISE, EN ROUTE FROM EWR TO CLT AT FL340, THE AIRCRAFT LOST CABIN PRESSURE. CABIN ALTIUDE CLIMBE D TO 14,000 FEET. CREW DESCENDED FLIGHT AND REPRESSURIZED CABIN AT FL280. SYSTEM OPERATED OK IN MANUAL, BUT STANDBY WA S INOPERATIVE. APPEARS AFT OUTFLOW VALVE IS STICKING. FLIGHT LANDED AT CLT WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE AFT OUTFLOW VALVE PER MM 21-31-11. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007082900113 20070829 00113 2007 8 29 UPS07650450 4 20070815 A 3460 COMPUTER BOEING 767 76734AF 1385212 NM FLT MANAGE INOPERATIVE A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 315UP 27743 INSPECTION TYPE:ETOP BTB - LT FMC SINGLE SOURCE MESSAGE. (08-17-07] ACCOMPLISHED FIM 34-61-00 FIG 108A, ALL TESTS PASS ED. THE SYSTEM IS OK. 2 L 7 2 4F RT A1NM 2007082900114 20070829 00114 NE 2007 8 29 TRBA2007067 2 20070813 A 7322 32448716 HMU AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE NR 2 ENGINE FAILED A TRBA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 29 355AT 355 127105 TQ DROP TO 0 PERCENT SUDDENLY ON NR 2 ENGINE (IFSD). PERFORMED ENGINE FAILURE CHECKLIST. ATTEMPTED RE-START UNSUCCESSF UL. SECURED NR 2 ENGINE. DECLARE EMERGENCY. LANDING IN PUJ UNEVENTFUL. PERFORMED DFDR DOWNLOAD PROCEDURE USING PORTA BLE INTERFACE MODEL FA210 AS PER ETN NR E2-31-031 PAGE 1 AND 2. REMOVED AND REPLACED FUEL PUMP IAW PWC MM NR 72-01-40. REMOVED AND REPLACED HMU AS PER MM NR 73-21-61. REMOVED AND REPLACED TQ SENSOR IAW MM NR 77-13-61 AND REMOVED AND REPL ACED AUTOFEATHER UNIT IAW MM NR 77-13-62. PERFORMED SEVERAL ENGINE RUNS IAW MM NR 72-00-00 WITH SATISFACTORY RESULTS. NO FLUCTUATIONS NOR LEAKS NOTED. A/C RELEASED FOR FCF TO VERIFY FOR TQ FLUCTUATIONS. FCF FOUND SATISFACTORY. 2 H 7 2 4T 4 T RT A53EU E20NE 2007082900115 20070829 00115 NE 2007 8 29 G6OA200700006 2 20070816 A 7200 ENGINE DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE NR 2 MALFUNCTIONED A G6OA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 27 606GC 47929 NR 2 ENGINE OIL PRESSURE STARTED TO DECREASE FOLLOWED BY LOW OIL PRESSURE LIGHT AND RAPID LOSS OF OIL QUANTITY. ENGINE WAS SHUTDOWN. 2 L 7 3 4F 4 F RT A22WE E23EA 2007082900116 20070829 00116 NM 2007 8 29 KCSA071321 1 20070821 A 5315 FLOORBEAM BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 MAIN DECK FLOORBEAM UPPER CAP CORRODED AT BS 460, LBL 89. 2 L 7 4 4F RT A20WE 2007082900122 20070829 00122 EA 2007 8 29 TRAX200701201 1 20070816 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 752EV 10166 SEVERAL RIGHT SIDE SEAT RAILS HAVE MINOR CORROSION FS 379.00 TO FS 977.00. REMOVED CORROSION FROM SEAT RAILS FROM VARIO US SPOTS BETWEEN RIGHT FS 379.00 TO FS 977.00. BRUSHED REWORKED AREAS WITH ALODINE. ALL DIMENSIONS WITHIN ALLOWABLE LI MITS. EACH REWORKED SEAT RAIL IDENTIFIED WITH THE WORDS REO 670-53-00-013. ALL WORK DONE IN REFERENCE TO CRJ 700 SRM 5 3-21-49. ALL WORK DONE IAW CRJ 700 SRM 51-12-00, 51-21-06, 51-21-16, AND 53-21-49. JOB COMPLETE. SUPPLEMENTAL - SDR C LOSED 08/21/07. 2 L 7 2 4F RT A21EA 2007082900123 20070829 00123 WP 2007 8 29 MWEA070180 1 20070713 A 5230 PAN DOUG DC9 DC981 3022081 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 805ME 48031 LOWER CENTER CARGO DOOR PAN CRACKED 1.5 INCH IN OUTER PAN RADIUS. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2007082900124 20070829 00124 SO 2007 8 29 C2XA07RI071 1 20070819 A 3350 1317 LIGHT EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 11113 145662 FLT 2246 - CHS - CREW REPORTED EMERGENCY EXIT LIGHT OVER SEAT 12C NOT WORKING. MX REMOVED AND REPLACED LIGHT BULB IAW E MB145 AMM 33-50-14 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007082900125 20070829 00125 NE 2007 8 29 PCSA818200701 2 20070818 A 7200 JT8D15 ENGINE BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE NR 1 MALFUNCTIONED A PCSA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 29 395AJ 76321 5489 21100 695316 FLIGHT 861 DEPARTED SJU AND DURING THE TOP OF THE CLIMB THE CREW REPORTED THE NUMBER 1 ENGINE OIL PRESSURE DROPPED TO ZE RO, THE NUMBER 1 ENGINE WAS SHUTDOWN AND THE AIRCRAFT CONTINUED TO MIA AND LANDED WITHOUT INCIDENT. THE NUMBER 1 ENGINE WAS REMOVED AND REPLACED IAW AMERIJET WORKCARDS B-48, B-49, B-41. THE NUMBER 1 ENGINE WAS LEAK CHECKED AND OPERATIONAL LY CHECKED GOOD, THE AIRCRAFT WAS RETURNED TO SERVICE. A FOLLOW-UP SUPPLEMENT SDR WILL BE SUBMITTED WITH THE ENGINE TEA RDOWN REPORTS WHEN AVAILABLE. 2 L 7 3 4F 4 F RT A3WE E2EA 2007082900127 20070829 00127 EA 2007 8 29 VNAA0708004 1 20070809 A 2621 365000183 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CARGO BAY DISCHARGED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 245PS 8007 7919 CREW REPORTED A CARGO BOTTLE LOW CAUTION MESSAGE ON CLIMBOUT OF CLT. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT I NCIDENT. MAINTENANCE INSPECTED AND DEFERRED THE CARGO FIRE EXTINGUISHING SYSTEM PER MEL 26-25-01. MAINTENANCE REMOVED AND REPLACED THE CARGO FIRE BOTTLE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. MEL WAS CLEARED. AIRCRAFT WAS R ELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007082900128 20070829 00128 EA 2007 8 29 VNAA0708005 1 20070809 A 3610 9093A001201 GASKET CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE PYLON LEAKING A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 719PS 10177 CREW REPORTED A RIGHT BLEED DUCT MESSAGE ON CLIMBOUT OF CLT. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND A LEAKING GASKET ON THE PYLON DUCT BLOWING AIR ONTO THE BLEED LOOP 204 AND 205. MAINT ENANCE REMOVED AND REPLACED THE GASKET IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SE RVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007082900130 20070829 00130 EA 2007 8 29 VNAA0708007 1 20070811 A 3244 704792 TIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NLG SEPARATED A VNAA B EMER. DESCENT O OTHER NR NOT REPORTED 1 GL 05 260JS 14 7957 CREW REPORTED THE RIGHT HAND NOSE TIRE TREAD SEPARATED ON TAKEOFF. CREW DECLARED AN EMERGENCY AND CONTINUED ON TO CLT W HERE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CONFIRMED THE RIGHT HAND NOSE TIRE TREAD HAD SEPARATED AND CAUSED DAMAGE TO THE AFT NOSE LANDING GEAR DOOR. MAINTENANCE REMOVED AND REPLACED BOTH NOSE TIRES IN ACCORDANCE WI TH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE REMOVED AND REPLACED THE AFT NOSE LAN DING GEAR DOOR ALONG WITH REPAIRING ALL DAMAGE. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007082900132 20070829 00132 EA 2007 8 29 VNAA0708009 1 20070811 A 3244 H29X9015 TIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT MLG SEPARATED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 207PS 86 7873 CREW REPORTED THE RIGHT HAND MAIN TIRE LOST ITS TREAD. MAINTENANCE INSPECTED AND CONFIRMED THE TREAD LOSS IN ADDITION T O DAMAGE TO THE RIGHT HAND INBOARD FLAP BOTTOM SIDE. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND INBOARD TIRE IN AC CORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE ALSO REMOVED AND REPLACED THE RIGHT HAND INBOARD FLAP AND RE PAIRED ALL DAMAGE. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007082900133 20070829 00133 WP 2007 8 29 G6OA200700007 1 20070822 A 5610 NBA6045502 WINDSHIELD DOUG DC10 DC1030F 3023504 WP COCKPIT CRACKED A G6OA B J A EMER. DESCENT DUMP FUEL UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 600GC 46965 AT FL 310, THE CREW HEARD A LOUD POP ON THE F/O'S SIDE. NOTICED A MAJOR CRACK WITH SPIDER VEINS ON THE F/O'S WINDSHIELD . CABIN ALTITUDE WAS 4000 FT. 2 L 7 3 4F RT A22WE 2007082900134 20070829 00134 WP 2007 8 29 G6OA200700004 1 20070712 A 2612 FIRE WARNING DOUG DC10 DC1030F 3023504 WP COCKPIT ACTIVATED A G6OA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 EA 27 607GC 46978 NR 1 ENGINE FIRE WARNING IN FLIGHT. 2 L 7 3 4F RT A22WE 2007082900135 20070829 00135 WP 2007 8 29 G6OA200700005 1 20070712 A 2612 FIRE WARNING DOUG DC10 DC1030F 3023504 WP COCKPIT ACTIVATED A G6OA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 EA 27 607GC 46978 NR 1 ENGINE FIRE WARNING IN FLIGHT. 2 L 7 3 4F RT A22WE 2007082900136 20070829 00136 WP 2007 8 29 G6OA200700003 1 20070712 A 2612 FIRE WARNING DOUG DC10 DC1030F 3023504 WP COCKPIT ACTIVATED A G6OA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 EA 27 607GC 46978 NR 1 ENGINE FIRE WARNING IN FLIGHT. 2 L 7 3 4F RT A22WE 2007082900137 20070829 00137 WP 2007 8 29 ABXA070258 1 20070814 A 5311 99115057 FRAME DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 WHILE COMPLYING WITH EA 53300036, FOUND CENTER FRAME CRACKED AT BOTH ENDS, REF AD 2002-21-09. REPAIRED BOTH ENDS OF FRA ME IAW DC9 SRM 53-03 FIG 34. TWO CRACKS: .75 INCH AND .86 INCH. 2 L 7 2 4F A6WE 2007082900138 20070829 00138 WP 2007 8 29 ABXA070259 1 20070814 A 5320 995789924 FITTING DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 WHILE COMPLYING WITH EA 53300036, FOUND CRACKED INTERCOSTAL CLIP, REF AD 2002-21-09. FABRICATED AND INSTALLED IAW DWG 9 957899 AND DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2007082900141 20070829 00141 WP 2007 8 29 ABXA070263 1 20070815 A 5320 99578606 BRACKET DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 WHILE COMPLYING WITH EA 53300036, FOUND CRACKED BRACKET, REF AD 2002-21-09. REPLACED BRACKET IAW DC9 SRM 51-30-02 AND 5 1-30-05. 2 L 7 2 4F A6WE 2007082900144 20070829 00144 EU 2007 8 29 WRNA200700049 1 20070818 A 2781 CHA1067003A INDICATION SYS AIRBUS 300 A300B4203 3930306 EU COCKPIT MALFUNCTIONED A WRNA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 05 510TA 100 DURING TAKEOFF FOR TEST FLIGHT AFTER HEAVY MAINTENANCE VISIT, CONFIGURATION LIGHT AND WARNING HORN CAME ON, TAKEOFF ABOR TED. REPLACED LEADING EDGE INSTRUMENTATION UNIT IAW MM 27-84-11. AIRCRAFT RELEASED, TEST FLIGHT COMPLETED SATISFACTORY . 2 L 7 2 4F RT A35EU 2007082900146 20070829 00146 EA 2007 8 29 TRAX200701196 1 20070816 A 5320 BEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 752EV 10166 RIGHT FS 280 TRANSVERSE BEAM CORRODED. JOB COMPLETE. CUT AND REMOVED RIGHT FS 280 BEAM, INTERCOSTALS AT RBL 9.0 AND 27 .0 (FOM), PULLEY BRACKET, AND T-BRACKET PER CRJ 700 SRM 51-42-06. FABRICATED T-BRACKET NR 5 FOR RIGHT TRANSVERSE BEAM P ER IS 670531100026. FABRICATED U-CHANNEL 7075T6, .063 DRILLED UP AND FINAL SIZE ALL HOLES IN U-CHANNEL AND TRANSVERSE B EAM ALL WORK PER REO670-53-11-00026 READY TO BE INSTALLED. STRESS RELIEVED TITANIUM DOUBLERS FOR RIGHT TRANSVERSE BEAM PER CRJ 700 SRM 51-24-28. INSTALLED FIELD FASTENERS IN TITANIUM DOUBLERS AND INSTALLED CHERRY MAX FASTENERS IN OUTBOARD CORNER UNDER FLOOR SILL PER REO 670-53-11-052. FINISH INSTALLING SOLID RIVETS AND INSTALLED DRIP PAN AND PULLEY BRACKE 2 L 7 2 4F RT A21EA 2007082900147 20070829 00147 WP 2007 8 29 ASAA0781981 1 20070817 A 5320 993053877 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 943AS 53018 CUSP WEB CORRODED. REMOVED DAMAGED AREA. INSTALLED DOUBLER AND FILLER PER SRM 51-70-4. 2 L 7 2 4F RT A6WE 2007082900148 20070829 00148 WP 2007 8 29 ASAA0781982 1 20070817 A 5321 9936640501 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 943AS 53018 FLOOR PANEL IS DELAMINATED. REPLACED PANEL PER SRM 53-05. 2 L 7 2 4F RT A6WE 2007082900149 20070829 00149 WP 2007 8 29 ASAA0781983 1 20070817 A 5321 99366401 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 943AS 53018 CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND SRM 53-20-01. 2 L 7 2 4F RT A6WE 2007082900150 20070829 00150 WP 2007 8 29 ASAA0781984 1 20070817 A 5321 99366401 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 943AS 53018 CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND 53-20-01. 2 L 7 2 4F RT A6WE 2007082900154 20070829 00154 WP 2007 8 29 ASAA0781988 1 20070817 A 5347 593056675 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 943AS 53018 SEAT TRACK CORRODED. REMOVED DAMAGED SECTION OF TRACK. INSTALLED REPAIR PLUG PER SRM 53-05. 2 L 7 2 4F RT A6WE 2007082900155 20070829 00155 WP 2007 8 29 ASAA0781989 1 20070817 A 5330 59360073 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 943AS 53018 FUSELAGE SKIN GOUGED AT PREVIOUS BLEND. REMOVED DAMAGED AREA. INSTALLED REPAIR PARTS PER SRM 53-04. 2 L 7 2 4F RT A6WE 2007082900156 20070829 00156 WP 2007 8 29 ASAA0781990 1 20070817 A 5330 5920323249 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 943AS 53018 FUSELAGE IS DENTED. REMOVED DAMAGED SECTION. INSTALLED SKIN FINGER DOUBLERS AND STRAPS PER SRM 53-04. 2 L 7 2 4F RT A6WE 2007082900157 20070829 00157 WP 2007 8 29 ASAA0781991 1 20070817 A 5753 SKIN DOUG DC9 DC983 3022083 WP T/E FLAP VANE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 943AS 53018 LEFTHAND WING OUTBOARD FLAP OUTBOARD VANE IS DENTED ON INBOARD LEADING EDGE. REPAIRED CLUSTER OF DENTS PER SRM 51-60-0, 51-70-2 AND 57-50-14. 2 L 7 2 4F RT A6WE 2007082900159 20070829 00159 WP 2007 8 29 ASAA0781994 1 20070817 A 3350 601177 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 982AS 53473 OVERWING EMERGENCY EXIT LIGHT INOPERATIVE DURING TEST. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A6WE 2007082900160 20070829 00160 NM 2007 8 29 ASAA0741995 1 20070821 A 5753 6546435281 SKIN BOEING 737 737490 1384715 NM T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 LEFT OUTBOARD AFT FLAP DENTED IN 2 PLACES ON UPPER SURFACE. LEFT OUTBOARD AFT FLAP UPPER SURFACE AT APPROX RSS 300 312 REPAIRED IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007082900161 20070829 00161 EU 2007 8 29 TRAX200701154 1 20070810 A 5320 ANGLE AEROSP ATR72 ATR72 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 CRACK FOUND AT FR 27 STG 4R BEHIND WING FITTING ON FORMED PART. EC PERFORMED IAW NTM CRACK CONFIRMED TO RIVET AND DOES NOT EXTEND BEYOND. CRACK CONFIRMED IN RADIUS FROM AFT EDGE RUNNING FWD. CRACK ON RIGHT WING PRESSURE DECK SPLICE ANGLE INSPECTED AND FOUND ACCEPTABLE PER EO 72-53-0250. SUPPLEMENTAL - SDR CLOSED 08/22/07. 2 H 7 2 4T RT 2007082900163 20070829 00163 NM 2007 8 29 UPS07650441 1 20070815 A 3610 SHUTOFF VALVE BOEING 767 76734AF 1385212 NM RT ENGINE MALFUNCTIONED A IPXA K NONE J WARNING INDICATION NR NOT REPORTED 1 SO 01 322UP 27748 INSPECTION TYPE:ETOP ENG START - RIGHT BLEED LIGHT ON M356673. REPLACED RT ENG PRSOV, OPS CHECK NORMAL, REF MM 36-11-0 9-2. THIS CLEARS M356673. 2 L 7 2 4F RT A1NM 2007082900165 20070829 00165 NM 2007 8 29 UPS07650469 1 20070820 A 4990 OIL SYSTEM BOEING 767 76734AF 1385212 NM APU OVERSERVICED A IPXA K NONE W INADEQUATE Q C TX TAXI/GRND HDL 1 SO 01 332UP 32843 INSPECTION TYPE:ETOP APU AUTO SHUTDOWN M356966. APU RUN C/OUT IAW AMM 49-11-00. APU AUTO SHUTDOWN OCCURRED WITH -LOP- ON BITE. FIM TASK 49-11-00 FIG 109 C/W. FOUND APU OIL LEVEL OVER SERVICED. OIL DRAINED TO CORRECT LEVEL AND APU OPS N OW SATIS. DMI M356966 CLEARED AND PLACARD REMOVED. 2 L 7 2 4F RT A1NM 2007082900166 20070829 00166 NM 2007 8 29 UPS07650479 1 20070822 A 3697 CONNECTOR BOEING 767 76734AF 1385212 NM RT SHUTOFF VALVE DIRTY A IPXA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 306UP 27759 INSPECTION TYPE:ETOP RT ENG PRV EICAS MSG WITH STATUS MSG AND BLEED LIGHT ON RIGHT SIDE. REMOVED AND CLEANED CONNECTOR ON RT PRSOV. CYCLED VALVE MANUALLY. RAN ENGINE, NO MSG OR BLEED LIGHT. OPERATES NORMAL PER MM 36-11-00. 2 L 7 2 4F RT A1NM 2007082900167 20070829 00167 WP 2007 8 29 UPS07850471 1 20070815 A 5313 37584952N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 CRACKED END FITTING AT STA 1240 L35R. REMOVED AND REPLACED LONGERON END FITTING AT STA 1240 L35R IAW SRM 51-1-20D AND SRM 51-3-2. 2 L 7 4 4F RT 4A25 2007082900168 20070829 00168 WP 2007 8 29 UPS07850472 1 20070801 A 5544 WEB DOUG DC8 DC873F 302199F WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 RUDDER HAS 1.5 INCH CRACK IN LWR STRUCTURE JUST AFT OF TORQUE TUBE MOUNTING. REMOVED CRACKED WEB ON RUDDER IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR WEB ON RUDDER STA ZR 59.54 IAW SRM 51-03-00-0, AND DWG 5701251. 2 L 7 4 4F RT 4A25 2007082900170 20070829 00170 2007 8 29 UPS07850475 4 20070817 A 2565 SLIDE DOUG DC8 DC871F 302199D WP EMERGENCY EXIT OUT OF POSITION A IPXA K NONE O OTHER NR NOT REPORTED 1 SO 01 703UP 45939 INSPECTION TYPE:N/A EMERGENCY EXIT SLIDE AT CREW ENTRY DOOR IS PARTIALLY OUT OF PACK. SECURED EVAC SLIDE AS PER AMM 25- 60-01. NO DEFECTS NOTED. 2 L 7 4 4F RT 4A25 2007082900172 20070829 00172 NM 2007 8 29 ABXA070266 1 20070811 A 2742 251T43101 ACTUATOR BOEING 767 767200 1385120 NM STABILIZER FAILED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 752AX 4814 23434 DURING MAINTENANCE, REF JOB CARD 12-003-C1, STABILIZER TRIM BALL NUT UPPER SEAL APPEARED TO HAVE FAILED - STEP (23) (B) NOTE 2 (BEAVER UNIT). REMOVED AND REPLACED TRIM BALL SCREW ACTUATOR IAW B767 MM 27-41-10. 2 L 7 2 4F RT A1NM 2007082900174 20070829 00174 NM 2007 8 29 USAA200708002 1 20070814 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 FOUND 2 CRACKS, 2.25 INCHES AND 1.25 INCH AT STA 727D & S27R AND STA 727G S-23R. 2 L 7 2 4F RT A16WE 2007082900175 20070829 00175 WP 2007 8 29 ABXA070265 1 20070802 A 5230 2772981501 HINGE PIN DOUG DC8 DC863F 302198F WP CARGO DOOR SHEARED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 DURING MAINTENANCE ON WO 600267980, UPPER FORWARD CARGO DOOR FORWARD HINGE PIN WAS SHEARED. REMOVED AND REPLACED FORWAR D HINGE PIN IAW DC8 AMM 20-10-0. 2 L 7 4 4F 4A25 2007082900177 20070829 00177 WP 2007 8 29 ABXA070269 1 20070729 A 5320 5913093504 SUPPORT FITTING DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 986AX 47543 FITTING ON CANTED STA 1143, RIGHT BUTT LINE 6 WAS CRACKED AT LOWER END. REMOVED AND REPLACED RUDDER BEARING SUPPORT FIT TING IAW DC9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2007082900178 20070829 00178 EU 2007 8 29 07FDEA02964 1 20070817 A 5311 A53973599204 FRAME AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT PIT T CAP FRAME 60, CENTER, ABOVE S57 CORRODED. REMOVED CORROSION PER A310-200 SRM 51-74-10. FOUND TO BE OUT OF LI MITS PER A310-200 SRM 53-10-00 PG 123. REMOVED DAMAGED CROSSBEAM, FABBED NEW CROSSBEAM SECTION. INSTALLED NEW CROSSBEA M SECTION PER A310-200 SRM 53-10-15. 2 L 7 2 4F RT A35EU 2007082900179 20070829 00179 WP 2007 8 29 ABXA070268 1 20070728 A 5320 J0602283 PAN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 986AX 47543 DOUBLER BULGED AND CRACKED AT CENTER OF FORWARD LOWER CARGO DOOR CUTOUT, STA 394, BETWEEN THRESHOLD AND SCUFF PLATE. RE MOVED AND REPLACED NEW DOOR PAN IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 2007082900180 20070829 00180 EU 2007 8 29 07FDEA02965 1 20070817 A 5313 A53974202222 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 ALC STR 52L CORRODED BETWEEN FR 64 AND 65. REMOVED CORROSION IAW A310 SRM 51-40-11. FOUNDED OUT OF LIMITS IAW A310 SRM 53-17-14. NEW MATERIAL ID FOR STRINGER IS DANS 0B09P0081641.218 COUPLING THAT IS DAN 200IT 79511 MAT EXTRUSION PO NR 5 80294.2. FABRICATED IAW A310 SRM 51-40-44. INSTALLED STRINGER AND ASSOCIATED PARTS IAW A310 SRM 53-1014. 2 L 7 2 4F RT A35EU 2007082900181 20070829 00181 WP 2007 8 29 ABXA070270 1 20070716 A 5330 59114013 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 978AX 47628 DENT NR 34 AT LEFT FS 171, CRACK INDICATION DISPLAYED. REPAIRED SKIN IAW DC9 SRM 53-04 FIG 38, VIEW J. CUT OUT AIRSTAI R PAN REPAIRED WITH COVER PLATE PER ENGINEERING APPROVAL. REMOVED AND REPLACED RAIL IN E&E TO FOM, REINSTALLED IAW DC9 SRM 51-30-1. PRIMED AND PAINTED AREA IAW DC9 SRM 51-10-3B. 2 L 7 2 4F A6WE 2007082900182 20070829 00182 NM 2007 8 29 SB07066 1 20070819 A 3350 20131ASMI BATTERY PACK BOEING 737 737301 1384611 NM EMERGENCY LIGHTS DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 501UW 23231 CLT - MAINTENANCE REPORTED THE LAST 5 ROWS OF SEAT EMERGENCY LIGHTS WERE DIM. MAINTENANCE REMOVED AND REPLACED THE BATT ERY PACK AT POWER SUPPLY M1197. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007082900184 20070829 00184 2007 8 29 SB07067 4 20070819 A 3441 HG1050AD05 IRU BOEING 737 7374B7 1384702 NM E3-5 SHELF FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 454UW 41202 41202 24996 CLT - FLT 1840 ON CLIMBOUT FROM CLT, EN ROUTE TO EWR, CAPTAIN REPORTED THE LEFT IRU FAULT LIGHT ILLUMINATED. FLIGHT RE TURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACE D THE NR 1 IRU AND ACCOMPLISHED A SATISFACTORY FUNCTIONAL TEST. 2 L 7 2 4F RT A16WE 2007082800021 20070828 00021 NM 2007 8 28 2007UALA03227 1 20070816 A 3250 MODULE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NLG STEERING FAILED A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 808UA 804 PLANE PULLS TO RIGHT ON TAXI AND ON T/O AND LANDING. FOUND STEERING ELECTRO-HYD MODULE 6GC FAILED. REPLACED STEERING ELECTRO-HYD MODULE 6GC. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082800022 20070828 00022 NM 2007 8 28 2007UALA03228 1 20070817 A 2410 CSD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 GENERATOR FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 349UA ZI11687 24253 FLIGHT DIVERTED UNDER AMBER ALERT DUE TO APU DEFERRED AND A FAILED GENERATOR. REPLACED NR 1 GENERATOR AND CONSTANT SPEE D DRIVE. FOUND OVERHAULED GENERATOR. ON CSD REPLACED ALL WORN/DAMAGED GEARS, O/H DIFF & HYDRAULIC LOGS, REPLACED SCAVE NGE PUMP & BOTH SEAL ASSEMBLIES. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082800028 20070828 00028 NM 2007 8 28 2007UALA03234 1 20070818 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 568UA 26674 FLT EXPERIENCED OZONE ENCOUNTER. DESCENDED TO FL290. FLIGHT CREW WAS ON O2 FOR A SHORT DURATION DUE TO STRONG ODOR IN THE COCKPIT. COCKPIT OXYGEN PRESSURE WAS AT 1070 PSI, BELOW MINIMUM SPECIFICATIONS. SERVICED OXYGEN. CAUSE OF ODOR N OT ESTABLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082800039 20070828 00039 NM 2007 8 28 2007UALA03245 1 20070818 A 3397 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 646UA 25283 FOUND EEL LIGHTS INOP MID LAV. REPAIRED EEL FEEDER CABLE. TESTS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082800057 20070828 00057 EU 2007 8 28 07FDEA03003 1 20070821 A 5320 A53981113200 SHEAR PLATE AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 CRACKED SHEARPLATE BETWEEN FRAME 79-80, STRG. 26, LHS. REPAIR PERFORMED BY REPLACEMENT OF SHEARPLATE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007082800059 20070828 00059 EU 2007 8 28 07FDEA03005 1 20070821 A 5710 A57111092 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 FINDING CRACKS DURING ACCOMPLISHMENT OF SB A300-57-6049 AND A300-57-6086 IN CENTER WING BOX CORNER ANGLE FITTING (HOL E A (LT/RT), Q, G , I (LT). REPAIR PERFORMED BY REAM UP UNTIL CRACK REMOVAL IAW EA 6-5710-103311 AND RAS/AS/0159/2006 ISS A AND RAS /046825/029/2006 ISS A. 2 L 7 2 4F RT A35EU 2007082800064 20070828 00064 NM 2007 8 28 HALA0700349 1 20070820 A 4940 BA0601 BATTERY BOEING 767 76733A 1385209 NM APU STARTER WEAK A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM, UNABLE TO START APU. EICAS MESSAGE APU FAULT. FOUND MINI FLAG 34 DURING BITE OF APU CONTROL UNIT, REPLACED APU BATT PER M/M. APU STARTED SEVERAL TIMES SATISFACTORLY. BITE PROCEDURE 49-11-00 FIG 103 M/M24-31-04. NO FAULTS PRESENT. START IS NORMAL. 2 L 7 2 4F RT A1NM 2007082800079 20070828 00079 EA 2007 8 28 SWIA200718592 1 20070621 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 452SW 7716 FS 280 FLOOR SUPPORT BEAM IS CRACKED AT LBL9, FOUND AT C-CHECK. INSTALLED REPAIR PARTS TO FS 280 SUPPORT BEAM AT LBL9 L OWER PER CRJ200 SRM 51-42-06 P11. 2 L 7 2 4F RT A21EA 2007082800084 20070828 00084 EA 2007 8 28 SWIA200718597 1 20070810 A 5610 WINDSCREEN CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 CAPTAINS WINDSCREEN IS CRACKED. REPLACED THE CAPTAINS WINDSCREEN IAW MM 56-11-01 AND RII 56-220-1000, PN/OFF 139321-9, SN/OFF 01250H7456. 2 L 7 2 4F RT A21EA 2007082800102 20070828 00102 NM 2007 8 28 DL76G071081 1 20070815 A 3610 CONTROLLER BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6 30025 NE NR 1 ENGINE MALFUNCTIONED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 1501P 24983 695374 LEFT ENG PRV MESSAGE REMOVED AND REPLACED PRV CONTROLLER GRD, OPS CK GOOD. 2 L 7 2 4F 4 F RT A1NM E13NE 2007082800109 20070828 00109 NM 2007 8 28 DL764071091 1 20070817 A 5730 SKIN BOEING 767 767432ER 1385134 NM LT WING DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830MH 29701 LT WING OB END OF RAKED WING UPPER SKIN HAS DELAMINATION. REPAIRED UPPER SKIN DLAMINATION BY APPLYING GRAPHITE LAYUP RE PAIRS IAW DELTA ERA 463393-14. COMPLIED WITH REPAIR ON TIMCO NR OPERATION 26942 DURING HMV-1 IN GSO. 2 L 7 2 4F RT A1NM 2007082800113 20070828 00113 NM 2007 8 28 DL76S071095 1 20070818 A 8012 GRND AIR VALVE BOEING 767 767332 1382001 NM LEFT OPEN A DALA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 27 135DL 25145 AFTER TAKEOFF, GOT FWD EQPT OVHT EICAS WENT TO STBY AS PER QRH. 5 MINS LATER CAME BACK ON WENT TO OVRD AS PER QRH. AT 35K, ALT CABIN PRESS CLIMBED ABOVE 11K AND CABIN ALT EICAS WARNING CAME ON. AFTER PERFORMING IMMEDIATE ACTION ITEMS. E MERGENCY DESCENT TO 12K CABIN ALT WARNING LIGHT CAME ON PASSING 33K ON THE WAY DOWN. RAN BITE ON BOTH CABIN PRESS AND P ACK CONTROLLERS NO FAULTS. PRESSURIZED A/C TO 4 PSI FOUND GRND AIR CONNECTION PART OPEN. NO OTHER LEAKS NOTED. 2 L 7 2 4F RT A1NM 2007082800121 20070828 00121 NM 2007 8 28 DLM88071105 1 20070817 A 5315 FLOORBEAM DOUG MD88 MD88 3023688 NM BS 886 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 FOUND BROKEN FLOOR SUPPORT FITTING AT STA.886 AND X=22. REPLACED PER DRWG 3925817 REV C ON N/R T0064394 AT HMV IN GDL. 2 L 7 2 4F RT A6WE 2007082800126 20070828 00126 NM 2007 8 28 DLM88071110 1 20070817 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 1136-1174 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 EXFOLIATION CORROSION ON RT CUSP WEB FRONT STA 1136 TO 1174 DAMAGE, REMOVED PER SRM 53-01 AND ERA 398191-14MA. 2 L 7 2 4F RT A6WE 2007082800131 20070828 00131 NM 2007 8 28 DLM88071115 1 20070817 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 892-897 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 952DL 49883 EXFOLIATION CORROSION ON RT CUSP WEB AT STA 892 AND 897, REPAIR PER ERA 398191-14MA. 2 L 7 2 4F RT A6WE 2007082800146 20070828 00146 WP 2007 8 28 IXXA070042O 1 20070822 A 2612 FIRE LOOP DOUG DC8 DC862F 3021972 WP NR 2 MALFUNCTIONED A IXXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 11 41CX 82504 2271 46129 DURING TAKEOFF FROM TAPA, THE NUMBER TWO FIRE WARNING INDICATION LIGHT AND BELL CAME ON, THE LIGHT AND BELL WENT OUT WHE N THE CREW RETARDED POWER LEVERS TO IDLE. THE CREW RETURNED TO BLOCKS AT TAPA WITHOUT INCIDENT. MAINTENANCE REPLACED T HE NUMBER TWO LOWER FIRE LOOP AND PERFORMED OPERATIONAL CHECK WAS GOOD IAW DACO DC8 MAINTENANCE MANUAL 26-10-1, AIRCRAF T WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2007082800153 20070828 00153 EU 2007 8 28 07FDEA03012 1 20070822 A 5330 A53611654220 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 EXISTING OLD EXTERNAL DOUBLER AT FRAME 17-18, STRG 39-41 LT DID NOT FIND IAW, REPAIR DRAWING R53610848. REPAIR RENEWED WITH INSTALLING OVERSIZE FASTENERS IAW EA 6-5312-103314 AND RAS/AS/143/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007082800159 20070828 00159 EU 2007 8 28 07FDEA03018 1 20070822 A 5710 A57112385201 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 ELONGATED HOLE IN CORNER FITTING OF CENTER WING TANK, FRAME 40, RIB 1 RHS. REPAIR PERFORMED BY REAM UP THE HOLE TO FINAL DIA 14,247-14,287 MM AND SPOT FACING IAW EA 6-5710-103331 AND RAS/047032/008/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007082800164 20070828 00164 EU 2007 8 28 07FDEA03024 1 20070822 A 5311 A53988724207 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 CORROSION AT CROSSBEAM FRAME 87 RT AFT FACE, OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007082800169 20070828 00169 WP 2007 8 28 07FDEA03029 1 20070822 A 5730 SKIN DOUG DC10 DC1010F 3022111 WP RT WING UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 RT WING TIP EXTERNAL DOUBLER ON SKIN. ACCOMPLISHED EA NR 8-5760-112423. 2 L 7 3 4F A22WE 2007082800184 20070828 00184 EU 2007 8 28 07FDEA03045 1 20070822 A 5714 A57111092203 ANGLE AIRBUS 300 A300B4605R 3930308 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 DAMAGES, CRACKS AND CORROSION FOUND IN ANGLE FITTING HOLES IN CENTER WING BOX FRAME 47 RHS. REPAIR PERFORMED BY OVERSIZ ING THE HOLES AND CUT OUT THE EXTERNAL FITTING IAW EA 6-5710-112481 AND RAS/053362014/2007 ISS "A". 2 L 7 2 4F RT A35EU 2007082800193 20070828 00193 NM 2007 8 28 07FDEA03055 1 20070822 A 5311 651766347 FRAME BOEING 727 727233 138408A NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 286FE 22623 ON AGING A/C INSP FOUND EXISTING REPAIR ON FRAME 720A BETWEEN STR 24L AND 25L DID NOT CONFORM TO SRM 51-40-3. REMOVED E XISTING REPAIR, FABRICATED FORMED SECTION REPAIR REF SRM 51-40-3 AND INSTALLED REF FED EX EA NR 7-5310-113941 THIS IS CL ASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007082800203 20070828 00203 EU 2007 8 28 SIMA200723502 1 20070821 A 2120 UNKNOWN SAAB SF340 340B 7860101 EU CABIN ODOR A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 324AE 340B324 STRONG ODOR OF CLEANING FLUID DURING CLIMB-OUT. RETURNED TO DFW. PERFORMED ENGINE RUNS WITH BLEEDS OPEN IAW SAAB AMM 7 2-00-00 AND AMM 21-50-00. ODOR DISSIPATED AFTER 30 MINUTES, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007082800206 20070828 00206 NM 2007 8 28 DHL2007746503 1 20070821 A 5753 SKIN BOEING 727 727224 1384076 NM FORE FLAP CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 AT C CHECK RT INBD FORE FLAP L/E WBL 124 IS CHAFED ON REPAIR AND ADJACENT SKIN. REMOVED PREVIOUS REPAIR AT RT INBD FORE FLAP L/E WBL 124 IAW B727 SRM 51-30-2. FABRICATED NEW REPAIR MATERIAL USED 7075-T6 .050 PO NR 9005314 DIM 4" BY 4" IAW B727 SRM 57-50-2 FIG3 AND 57-50-4 FIG1. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED NEW REPAIR IAW B727 SRM 51 -30-2. 2 L 7 3 4F A3WE 2007082800208 20070828 00208 NM 2007 8 28 07FDEA03054 1 20070822 A 5330 SKIN PANEL BOEING 757 7572B7 1384964 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 LT SIDE OF FUSELAGE HAS A DIVOT IN THE SKIN AND RUNNING INTO A RIVET AT STATION 700, APPROXIMATELY 5" ABOVE STRINGER 23L . MEASURED THE DAMAGED AREA PER SRM 53-00-01 AND SRM 53-00-01. OUT OF LIMITS IAW SRM 53-30- 01. ACCOMPLISHED REPAIR IAW EA F-5310-110755, DATED 7/30/07. THERE IS NO FOLLOW UP ACTION REQUIRED. 2 L 7 2 4F RT A2NM 2007082800211 20070828 00211 EU 2007 8 28 07FDEA03059 1 20070823 A 5210 A52111008200 PLATE AIRBUS 310 A310203 3930313 EU ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION BETWEEN PLATE SHEET METAL AND SLIDING PROTECTION AT FWD CREW DOOR 831 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007082900011 20070829 00011 WP 2007 8 29 UPS07850431 1 20070803 A 5313 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 902 L9L AFT. REMOVED AND REPLACED LONGERON END FITTING AT STA 90 2 L9L AFT IAW SRM 51-1-20D, AND SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007082900012 20070829 00012 WP 2007 8 29 UPS07850432 1 20070805 A 5240 WEB DOUG DC8 DC873F 302199F WP SERVICE DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 WEB CRACKED ON RIGHT AFT SERVICE DOOR AFT SIDE BELOW BAYONET. STOP DRILLED END OF CRACK ON WEB IAW S RM 52-02-00 FIG 02. FABRICATED AND INSTALLED REPAIR DOUBLER ON RIGHT AFT SERVICE DOOR WEB IAW SRM 52-02- 00 FIG 02. 2 L 7 4 4F RT 4A25 2007082900016 20070829 00016 NM 2007 8 29 UPS07M50437 1 20070730 A 5514 FITTING DOUG MD11 MD11F 3023600 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORZ STAB CONSTANT SECTION BARREL NUT BORE LT NR 14 FOUND WITH CORROSION. SPLICE FITTING REMOVED SRM 51-32-01 VII R38. CORROSION AT BARREL NUT BORE REMOVED SRM 51-21-01 VII R38. BORE REAMED TO 0.988" DIA REMAIN BLEND OU T 0.020" BORE BOTTOM REMAIN BLEND OUT 0.165" DEEP. MATL REMAIN 0.040" FOUND EXCEED LIMIT PER EO MD11-5510-19409-L. NEW FITTING INSTALLED SRM 51-38-01 VII R38. FITTING, FILLET SEALED PER SRM 51-41-01VII R38. 2 L 7 3 4F RT A22WE 2007082900024 20070829 00024 SO 2007 8 29 C2XA07RI069 1 20070816 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17984 145246 RIC - MX - DURING ROUTINE MAINTENANCE, MX FOUND CEILING EMERGENCY LIGHTS AT ROW 3 AND ROW 14 INOPERATIVE. MX REMOVED AN D REPLACED LIGHT BULBS IAW EMB145 AMM 33-50-08 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETUR N TO SERVICE. 2 L 7 2 4T RT T00011AT 2007082900038 20070829 00038 NM 2007 8 29 UPS07M50448 1 20070705 A 5730 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C RIGHT WING L/E LOWER ACCESS WELL AREA FOUND CRACKED 5 INCHES LONG ON UPPER SKIN REINFORCED STRAP AT 13 INCHES O/B OF SLAT TRACK NR 12 AS MARKED. CRACKED REINFORCED STRAP AT AFFECTED AREA (APPROX XOS 789), REMOVED PER SRM 51-31-01 VII R38. NEW STRAP FAB AS PER DWG ARB3954-8. NEW STRAP, RIB & CLIP INSTALLED PER SRM 51-31-01VII R38. 2 L 7 3 4F RT A22WE 2007082900046 20070829 00046 NM 2007 8 29 ASAA0771964 1 20070814 A 5321 453A161043 FLOOR PANEL BOEING 737 737790 13844CN NM CARGO BAY DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 FWD PIT FLOOR PANE HAS SHARP DENTS. REPAIRED IAW SRM 51-40-05. 2 L 7 2 4F RT A16WE 2007082900056 20070829 00056 NM 2007 8 29 ASAA0771959 1 20070814 A 5755 SKIN BOEING 737 737790 13844CN NM NR 6 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 NR 6 SPOILER LOWER SURFACE DENTED. REPAIRED IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007082900058 20070829 00058 SO 2007 8 29 C2XA07RI070 1 20070813 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 11551 145411 FLT 534 - RDU - DURING PREFLIGHT, CREW REPORTED ELECTRICAL BURNING SMELL IN CABIN. MX POWERED ACFT AND TURNED ON LIGHTS AND EQUIPMENT IN CABIN, BUT COULD NOT DUPLICATE THE BURNING SMELL. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007082900065 20070829 00065 NM 2007 8 29 ASAA0741970 1 20070817 A 5320 6948985Y6 ATTACH FITTING BOEING 737 737490 1384715 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 FRAME TO INTERCOSTAL ATTACH CLIP CRACKED. REPLACED CRACKED CLIP WITH NEW PAR IAW EA 5310 02732. 2 L 7 2 4F RT A16WE 2007082900069 20070829 00069 NM 2007 8 29 ASAA0741974 1 20070817 A 5320 6517684Y642 INTERCOSTAL BOEING 737 737490 1384715 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 INTERCOSTAL CRACKED. REPLACED WITH NEW PART IAW EA 5310 02732. 2 L 7 2 4F RT A16WE 2007082900088 20070829 00088 NM 2007 8 29 UPS07550454 1 20070817 A 2131 CONTROLLER BOEING 757 75724APF 1384969 NM CABIN PRESSURE MALFUNCTIONED A IPXA K NONE J WARNING INDICATION DE DESCENT 1 SO 01 402UP 23724 INSPECTION TYPE:N/A CRUISING AT FL370 WITH LEFT PACK OFF AND RIGHT PACK ON, PRESSURIZATION AUTO CONTROLLER WAS IN AUTO 2 WITH DESTINATION SET AT 10 FT. ON INITIAL DESCENT PASSING THROUGH FL330, THE CABIN ATLITUDE EICAS WARNING LIGHTS CAME ON AND INDICATED 10,000 FT. REMOVED AND REPLACED # W AUTO PRESS CONTROLLER AS PRECAUTION, BITE CHECKS GOOD. CLOSED ON M356854. 2 L 7 2 4F RT A2NM 2007082900119 20070829 00119 CE 2007 8 29 2007F00047 1 20070816 A 2497 WIRE LEAR 35 35A 5170602 CE COCKPIT BURNED E O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 11 55FN 202 ON DESCENT INTO HLN, SMOKE WAS NOTICED IN THE COCKPIT. THIS WAS PRECEDED BY AN AUG/AIL ANNUNCIATOR LIGHT ON THE GLARESH IELD. AN EMERGENCY WAS DECLARED, THE EMERGENCY CHECKLIST WAS ACCOMPLISHED, AND AN EMERGENCY LANDING WAS MADE. TWO COCK PIT CREW AND TWO MEDICAL TECHNICIANS WERE ONBOARD. IT WAS FOUND THAT A BURNED OUT WIRE BEHIND THE CIRCUIT BREAKER PANEL ON THE F/O SIDE WAS RESPONSIBLE. REPAIRS WERE MADE IAW COMPANY PROCEDURES AND THE A/C RETURNED TO SERVICE. 2 L 7 2 4F A10CE 2007082900131 20070829 00131 NE 2007 8 29 VNAA0708008 2 20070811 A 7261 6087T04P06 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT ENGINE FAILED A VNAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 05 218PS 8373 7885 CREW REPORTED RECEIVING A LOW OIL PRESSURE WARNING MESSAGE FOR THE RIGHT HAND ENGINE. CREW DECLARED AN EMERGENCY AND SH UT DOWN THE ENGINE. CREW LANDED IN PIT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE SCAVENGE OIL PUMP IN ACC ORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007082900142 20070829 00142 WP 2007 8 29 ABXA070264 1 20070815 A 5320 591235099 ANGLE DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 WHILE COMPLYING WITH EA 53300036, FOUND CRACKED ANGLE, REF AD 2002-21-09. REPLACED ANGLE IAW DC9 SRM 51-30-05. 2 L 7 2 4F A6WE 2007082900190 20070829 00190 EA 2007 8 29 TRAX200701224 1 20070819 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 976EV 7601 FLAP FAILED AT BASE TO FINAL ATL, 8 SELECTED FAILED AT 2. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007082900192 20070829 00192 EA 2007 8 29 TRAX200701226 1 20070820 A 5312 PRESSURE PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 881AS 7496 FS 621 PRESSURE WEB IS CRACKED AROUND LINTEL FITTING. REPAIRED FS 621 PRESSURE WEB AT LINTEL FITTING IAW REO 601R-53-61 -1230; REO 601R-53-61-2312; AND ASA EC/TC REO 601R-53-61-2312; EC/TC REO 601R-53-61-1230. 2 L 7 2 4F RT A21EA 2007082900193 20070829 00193 EA 2007 8 29 TRAX200701227 1 20070820 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 718EV 10095 MAIN CABIN DOOR IS HARD TO CLOSE. 2 L 7 2 4F RT A21EA 2007082900195 20070829 00195 EA 2007 8 29 TRAX200701229 1 20070822 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 FLOOR EMERGENCY LIGHTS BROKEN BETWEEN ROWS 2 AND 3. 2 L 7 2 4F RT A21EA 2007082900199 20070829 00199 NM 2007 8 29 ZZDA2007258 1 20070815 A 5320 PAN BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 929AT 55075 CORROSION ON FWD CARGO DOOR CUTOUT LOWER JAMB AREA, OUT OF AMM LIMITS. INSTALLED FWD CARGO DOOR LOWER JAMB PAN CORROSIO N SPLICE REPAIR PER SRM 53-20-15 FIG 201. 2 L 7 2 4F TR A6WE 2007082900200 20070829 00200 NM 2007 8 29 ZZDA2007259 1 20070823 A 3350 0L3071BPEGPL LIGHT BOEING 717 717200 1383700 NM CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 952AT 55014 EMERGENCY PATH LIGHT AT 31D DID NOT ILLUMINATE. REMOVED AND REPLACED BULBS AT EMERGENCY PATH LIGHT 31D IN REF TO MM 25- 60 AND GMM 8103. 2 L 7 2 4F TR A6WE 2007082900201 20070829 00201 NM 2007 8 29 MWEA070183 1 20070821 A 7830 7150021507 BRACKET BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 903ME 55167 RIGHT THRUST REVERSER BRACKET IS CRACKED AT OUTBOARD FRAME STATION 35. FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F TR A6WE 2007082900202 20070829 00202 NM 2007 8 29 MWEA070184 1 20070821 A 7830 7150021507 BRACKET BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 903ME 55167 RIGHT THRUST REVERSER LOWER BRACKET IS CRACKED AT FRAME STATION 26 INBOARD. FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F TR A6WE 2007082900204 20070829 00204 NM 2007 8 29 SWAA074148 1 20070822 A 3350 101073 LENS BOEING 737 7377AD 1384502 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 798SW 28436 MID CABIN EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007082900205 20070829 00205 NM 2007 8 29 SWAA074156 1 20070822 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 409WN 27896 FWD CABIN EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007082900208 20070829 00208 NM 2007 8 29 SWAA074149 1 20070822 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 221WN 34259 EEPLS END CAP LOOSE AT ROW 1 ABC. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 2007082900209 20070829 00209 NM 2007 8 29 SWAA074144 1 20070822 A 5330 6545766 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 374, STR 26L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007082900210 20070829 00210 NM 2007 8 29 SWAA074152 1 20070822 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, LBL 3. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007082900215 20070829 00215 NM 2007 8 29 SWAA074161 1 20070822 A 5311 6546593 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 14L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007082900223 20070829 00223 NM 2007 8 29 SWAA074163 1 20070822 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007082900225 20070829 00225 NM 2007 8 29 SWAA074158 1 20070822 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007082900227 20070829 00227 NM 2007 8 29 SWAA074150 1 20070822 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER 26R CORRODED AT BS 867. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007082900228 20070829 00228 NM 2007 8 29 SWAA074160 1 20070822 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER 23L CORRODED AT BS 370. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007082900230 20070829 00230 CE 2007 8 29 GLBA20060979 1 20070820 A 5311 FRAME BEECH 1900 1900D 1154162 CE BS 177 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 220GL UE220 MAJOR REPAIR - FUSELAGE FRAME CRACKED AT F.S. 177.35 RT STRINGER 9 AT RELIEF HOLE. MAINTENANCE STOP DRILLED AND PATCHE D AFFECTED AREAS I.A.W. BEECH SRM 51-70. PATCH DIMENSIONS 3 INCH BY 2.4 INCH. .080 2024 T3 . RII COMPLIED WITH PER TASK CARD 8.2.1. 2 L 7 2 4T RT A24CE 2007082900231 20070829 00231 CE 2007 8 29 GLBA20060986 1 20070815 A 5511 SPAR BEECH 1900 1900D 1154162 CE HORIZONTAL STAB CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 208GL UE208 MAJOR REPAIR - HORIZONTAL STAB SPAR WEB CRACKED AROUND DE-ICE TUBE HOLE. MAINTENANCE REPAIRED HORZONTAL STAB SPAR WEB I. A.W. BEECH 1900D SRM 55-91. REPAIR APPROXIMATELY 5 3/4 INCHE BY 4 3/4 INCH. RII INSPECTION COMPLIED WITH PER TASKCARD 8. 2.1. 2 L 7 2 4T RT A24CE 2007082900232 20070829 00232 EU 2007 8 29 07FDEA02998 1 20070821 A 2760 3905300101 CONTROL UNIT AIRBUS 310 A310 EU NR 5 SPOILER FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 435FE 597 597 369 AFTER T/O, NR 5 SPOILER FAULTED W/RT WING NR 5 SPOILER INDICATING UP. RAN QRH PROCEDURE NO RELIEF. REMOVED AND REPLACE D NR 1 AND 2 EFCU'S IAW A310-200 MM 27-61-34-4. OPS CK GOOD, PERFORMED GROUND SPOILER OPS TEST IAW 27-61-00-5. SUPPLIE D FROM AIRBUS WEB SITE. VISUAL INSPECTION OF NR 1 AND 5 RT SPOILERS SHOW NO DEFECTS. 2 L 7 2 4F RT A35EU 2007082900233 20070829 00233 CE 2007 8 29 DXTA200702398 1 20070812 A 3240 991205018 MASTER CYLINDER CESSNA 500 560CESSNA 2076750 CE BRAKES BYPASSING E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 371QS 464 464 5600471 DURING TAXI BRAKE CHECK, FOUND COPILOT BRAKE PEDALS WERE VERY SPONGY AND THE PEDAL TRAVEL IS 3 TIMES MORE THAN THE CAPTA INS SIDE. THE RIGHT COPILOT PEDAL IS WORSE AND TRAVELS FARTHER. REMOVED AND REPLACED PILOT AND COPILOT BRAKE MASTER CYLI NDERS WITH NEW DUE TO FAIL THE PRESSURE TEST. OPS CHECKED GOOD LEAK CHECKED GOOD, WORK DONE IAW 560 M.M. CHAPTER 32-42-0 2. 2 L 7 2 4F RT A22CE 2007082900234 20070829 00234 NM 2007 8 29 SB07070 1 20070821 A 3397 WIRE BOEING 737 737401 1384701 NM EMERGENCY LIGHTS SHORTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 CLT - MAINTENANCE REPORTED THE AFT CABIN EMERGENCY LIGHTS AT SEAT ROWS 24 AND 25 INOPERATIVE. MAINTENANCE REPLACED LIGH T ASSEMBLIES ON SEAT ROWS 24 AND 25 DUE TO SHORTED WIRING. REPAIRED WIRING. ALSO, REPLACED FUSE IN POWER SUPPLY. OPER ATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007082900235 20070829 00235 NM 2007 8 29 SB07068 1 20070821 A 3397 WIRE BOEING 737 737401 1384701 NM EMERGENCY LIGHTS INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 CLT - MAINTENANCE REPORTED THE L1 DOOR OVERHEAD INTERIOR EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPAIRED WIRI NG TO REFLECT 737 WDM 33-51-12. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007082900236 20070829 00236 NM 2007 8 29 SB07069 1 20070821 A 3397 036000570010 FUSE BOEING 737 737401 1384701 NM EMERGENCY LIGHTS BLOWN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 CLT - MAINTENANCE REPORTED THE R2 DOOR EXTERIOR ESCAPE SLIDE EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY FUSE. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007082900237 20070829 00237 CE 2007 8 29 DXTA200702403 1 20070814 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE MLG UNKNOWN E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 371QS 5600471 COPILOT BRAKE PEDALS NEED TO BE PUSHED ALMOST FULL DOWN BEFORE ANY BRAKE APPLICATION IS FELT. ONCE YOU REACH THAT POINT, THE BRAKE PEDAL "FEEL" IS NORMAL. BLED BRAKE SYSTEM 10 TIMES PER CE560M/M. OPS CHECKS GOOD. PEDALS FEEL NORMAL. SERVICE D RESERVOIR. I/A/W CE560M/M 32-42-00. 2 L 7 2 4F RT A22CE 2007082900238 20070829 00238 CE 2007 8 29 DXTA200702408 1 20070815 A 3260 SWITCH BEECH MU300 400A 1155402 CE MLG INDICATOR LOOSE E DXTA O OTHER P NO WARNING INDICATION DE DESCENT 1 GL 07 131QS RK431 ON APPROACH TO FTY THE LEFT MAIN LANDING GEAR LIGHT WOULD NOT ILLUMINATE. WE RECYCLED THE GEAR TWO TIMES, AND ALSO VERIF IED THE LIGHT BULB WORKED WITH THE IND LIGHTS TEST. WE ALSO USED THE ALTERNATE GEAR EXTENSION PROCEDURE AND THE LIGHT WO ULD NOT ILLUMIATE. TROUBLE SHOT AND FOUND MAIN LANDING GEAR DOWN LOCK SWITCH JAMB NUTS LOOSE. RE-RIGGED SWITCH, TIGHTEN ED AND SAFETIED JAMB PERFORMED IAW HAWKER 400 AP AMM CHAP 32-10-00. 2 H 7 2 4F RT A16SW 2007082900239 20070829 00239 2007 8 29 DXTA200702409 2 20070816 A 7320 FUEL CONTROL CESSNA 500 560CESSNA 2076750 CE ENGINE OUT OF RIG E DXTA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 340QS 5600514 RIGHT FUEL BOOST PUMP CAME ON AND THEN RIGHT ENGINE SHUTDOWN. RAN ENGINE, VERIFIED ENGINE SQK, FOUND THROTTLE CABLE TO FCU OUT OF RIG. RERIGGED THROTTLE CABLE & PERFORMED OPS CHECKS. OPS CHECKS GOOD. RIGHT GEN REVER DROPPED OFF LINE DURING ALL ENGINE RUNS. WORK DONE IAW CE-560MM CH 76-11-00. ALSO FOUND HIGH IDLE SETTING LOW - ADJUSTED TO PROPER SETTING IAW P & W JT15D MM CH 73-00-00 2 L 7 2 4F RT A22CE 2007082900240 20070829 00240 WP 2007 8 29 IXXA070044O 1 20070824 A 3230 UPLOCK DOUG DC8 DC862F 3021972 WP MLG STIFF A IXXA O OTHER O OTHER CR CRUISE 1 SW 11 799AL 45922 DURING CRUISE FROM PHIK BOTH MAIN GEAR DOORS OPENED DURING UPLATCH CHECK, THE CREW CYCLED THE GEARS THREE TIMES REQUIRED TO GETTING A VALID UPLATCH CHECK. THE CREW LANDED AT KSUU WITHOUT INCIDENT. MAINTENANCE INSPECTED MAIN GEAR DOORS AND F OUND BOTH UPLATCH OVERCENTER LOCKS STIFF AND NOT LOCKING COMPLETELY, MAINTENANCE CLEANED AND LUBED AS REQUIRED FOR FREE MOVEMENT, JACKED AIRCRAFT AND PERFORMED SEVERAL EXTENSION AND RETRACTION CYCLES AND UPLATCH CHECKS OPERATIONAL CHECK WAS GOOD IAW DACO DC8 MAINTENANCE MANUAL 7-11-0, AND DACO DC8 MAINTENANCE MANUAL 32-30-0.AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2007082900241 20070829 00241 NE 2007 8 29 IXXA070043O 2 20070823 A 7261 B-NUT DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE ENGINE OIL LOOSE A IXXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 11 41CX 57059 6180 46129 671376 DURING CRUISE FROM KBWI NUMBER THREE ENGINE OIL QUANITY SLOWLY DECREASED UNTIL INDICATING ZERO. PRESSURE AND TEMPERATURE REMAINED NORMAL UNTIL THE OIL PRESSURE BEGAN TO FLUCTUATE APPROXIMATELY 15 PSI WITH NR 3 OIL PRESSURE LIGHT COMING ON AND OFF. THE CREW SHUTDOWN NR 3 ENGINE AT 1317Z WINDMILLING OIL PRESSURE 15PSI. ON DESCENT OIL PRESSURE WENT TO ZERO AT 1445Z. THE CREW LANDED AT BGTL WITHOUT INCIDENT. MAINTENANCE INSPECTED NR 3 ENGINE FOR OIL LEAKS AND FOUND LOOSE B-NUT F ITTING ON ENGINE OIL FILTER HOUSING. MAINTENANCE TIGHTENED B-NUT IAW DACO MAINTENANCE MANUAL CHAPTER 20-10. MAINTENANCE ACCOMPLISHED OPERATIONAL CHECK WAS GOOD AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F 4A25 1E8 2007083000014 20070830 00014 EA 2007 8 30 TRAX200701233 1 20070823 A 5260 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 FWD ASD ANCHOR FITTING CRACKED. REMOVED AND REPLACED FWD ASD ANCHOR FITTING IAW AMM CH 52-10-00. RII SATIFACTORY FOR AN CHOR FITTING REPLACEMENT IAW SP 607. 2 L 7 2 4F RT A21EA 2007083000015 20070830 00015 CE 2007 8 30 GLBA2006980 1 20070820 A 5320 1144300027180 ANGLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA BS 288 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 220GL UE220 MAJOR REPAIR - RT HEAVY ANGLE CRACKED AT F.S. 288. MAINTENANCE REPAIRED R/H HEAVY ANGLE AT F.S. 288. IAW BEECH 1900 SRM 53-90. REPAIR LENGTH APPROX 13 1/2 INCHES. RII C/W IAW TASKCARD 8.2.1. 2 L 7 2 4T 3 T RT A24CE E2NE 2007083000016 20070830 00016 CE 2007 8 30 GLBA20060981 1 20070820 A 5320 ANGLE BEECH 1900 1900D 1154162 CE BS 288 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 220GL UE220 MAJOR REPAIR - LT HEAVY ANGLE CRACKED AT F.S. 288. APPROXIMATELY 2 INCHES IN LENGTH. MAINTENANCE REPAIRED THE LT HEAVY ANGLE AT F.S. 288.0 I.A.W. BEECH 1900D SRM 53-90. REPAIR APPROXIMATELY 13 INCHES. 2 L 7 2 4T RT A24CE 2007083000017 20070830 00017 CE 2007 8 30 GLBA20060988 1 20070822 A 5511 SPAR BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA HORIZONTAL STAB CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 220GL UE220 MAJOR REPAIR - UPON ROUTINE INSPECTION THE HORIZONTAL STABILIZER SPAR WEB WAS FOUND TO HAVE TWO CRACKS RADIATING FROM DE ICE TUBE HOLE APPROXIMATELY 1/4 INCH & 1/2 INCH. MAINTENANCE REPAIRED MAIN SPAR CENTER WEB ON HORIZONTAL STAB I.A.W. BEE CH 1900D SRM 55-91. REPAIR APPROXIMATELY 3 3/4 INCH BY 4 3/4 INCH. .063 2024 T3. RII C/W PER TASKCARD 8.2.1. 2 L 7 2 4T 3 T RT A24CE E2NE 2007083000018 20070830 00018 WP 2007 8 30 IXXA070041O 1 20070821 A 2121 X702256D FAN DOUG DC8 DC862F 3021972 WP RECIRCULATION FAILED A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 11 799AL 80653 1264 45922 DURING CRUISE FROM PKWA, THE CREW DETECTED A BURNING ODOR IN COCKPIT. LEFT RECIRC FAN BECAME NOISY, THE CREW TURNED OFF THE RECIRC FAN AND ODOR WENT AWAY. THE CREW LANDED IN PHIK WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT RECIRC FAN IAW DC MAINTENANCE MANUAL 21-21-1 OPERATIONAL CHECK WAS GOOD AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2007083000019 20070830 00019 SO 2007 8 30 SIMA200723601 1 20070822 A 5610 NP15131111 WINDSHIELD EMB 135 EMB135KL 3260302 SO COCKPIT DELAMINATED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 851AE 10328 145734 CAPTAINS WINDSHIELD DELAMINATED AFTER TAKEOFF. REMOVED AND REPLACED WINDSHIELD IAW EMB AMM 56-10-01. OPERATIONAL CHECK GOOD - AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT T00011AT 2007083000022 20070830 00022 WP 2007 8 30 NWAA072909859 1 20070822 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 768NC 47729 TAIL COMPARTMENT EMERGENCY LIGHT WILL NOT ILLUMINATE. REPLACED BATTERIES IN POWER PACK. OPERATION CHECKS GOOD. 2 L 7 2 4F RT A6WE 2007083000023 20070830 00023 2007 8 30 QXEA200701346 4 20070822 A 3420 42000332501 AHRS BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 410QX 10691 10691 4053 SEA FLIGHT NR 2316: WHILE TAXING OUT, YAW DAMPER WOULD NOT ENGAGE ALONG WITH RECEIVING A PITCH MISMATCH ON THE FLIGHT DI RECTORS. COMMAND BARS WERE SPLIT (5 DEG ON CA SIDE/10 DEG ON FO SIDE) MAINTENANCE REMOVED AND REPLACED NR 2 AHRS IAW MT C 6342101. OPS CHECK GOOD. PITCH MISMATCH GONE. FD BARS MATCH AND YAW DAMPER ENGAGES. AIRCRAFT PLACARD AND STATUS AR E NOW CAT III. MTX CONTROL WAS NOTIFIED. RSI PLACARDS REMOVED (373249). AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007083000024 20070830 00024 NM 2007 8 30 QXEA200701347 1 20070823 A 7921 D2887715ATIF380 OIL COOLER BOMBDR DHC8 DHC8402 1390042 NM NR 2 ENGINE ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 404QX 8199 1253 4046 RNO FLIGHT NR 2256: AFTER ENGINE START AND BLEEDS SELECTED, ELECTRICAL AND OILY ODOR CONSUMED FLIGHT DECK AND GALLEY. M AINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE OIL COOLER, BORESCOPED THE NR 2 ENGINE AND COMPRESSOR AND WASHED THE NR 2 ENGINE. ALL GROUND RUNS AND OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007083000025 20070830 00025 EU 2007 8 30 07FDEA03062 1 20070823 A 5753 A57971480203 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 811FD 457 FOUND OLD BONDED REPAIR ON RT OUTBOARD FLAP WITH NEW DISBONDING AND DOUBLER DIMENSION NOT IAW TO SRM. REPAIR RENEWED IA W SRM 57-53-12 / FIG 208. 2 L 7 2 4F RT A35EU 2007083000026 20070830 00026 NM 2007 8 30 07FDEA03064 1 20070823 A 7120 BEARING RACE DOUG MD11 MD11 3023602 NM NR 3 PYLON MIGRATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 595FE 48553 NR 3 PYLON AFT MOUNT BEARING AFT FACE OUTER RACE FOUND MIGRATED. 08-31-07 REMOVED AND REPLACED AS PER FEDEX E.A. 1-5 410-112388. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007083000027 20070830 00027 NM 2007 8 30 07FDEA03067 1 20070823 A 5320 6556129 WEB BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 LWR AFT CARGO PIT DOOR CUTOUT, LWR SILL SLANT WEB HAS CORROSION COMING FROM UNDER THRESHOLD SUPPORT FITTING AT STA 986, WEB ALSO HAS MANY OTHER SPOTS MARKED FWD TO STA 950E PLUS 10". REMOVED THRESHOLD SUPPORT FITTING PER SRM 51-30-2. REMO VED CORROSION PER 51-10-6 PG 4 AND 5, NDT FOR MATERIAL LOSS, .003". WITHIN LIMITS PER SRM 53-10-1 PG 1-3. TREATED AND PRIMED PER SRM 51-30-2, PG 13 AND 14. THIS IS A CORROSION LEVEL 1. 2 L 7 3 4F RT A3WE 2007083000028 20070830 00028 NM 2007 8 30 07FDEA03069 1 20070823 A 5210 507945 BEAM BOEING 727 727233 138408A NM PAX DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 MAIN DECK 1L ENTRY DOOR SN 24, BOTTOM CROSS BEAM WEB IS CRACKED AT AFT STOP FITTING. REMOVED STOP FITTING, REMOVED DAMA GE, REPAIRED WEB. INSTALLED DOUBLER AND REINSTALLED STOP FITTING REF SRM 51-40-2 AND FED EX DWG SR27-52-015, THIS IS CL ASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007083000029 20070830 00029 EU 2007 8 30 07FDEA03070 1 20070823 A 5340 A53989161200 FITTING AIRBUS 300 A300B4605R 3930308 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 CORROSION AT FRAME 91 LOWER HIP FITTING RT, LOWER ATTACHMENT LUG REPAIR PERFORMED BY CORROSION REMOVAL AND INSTALLING BU SHING IAW EA 6-5319-112489 AND RAS/DAHAM/022566/2007 ISS D. 2 L 7 2 4F RT A35EU 2007083000030 20070830 00030 EU 2007 8 30 07FDEA03071 1 20070823 A 5312 A53811601200 BULKHEAD AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 FOUND CORROSION ON PRESSURE BULKHEAD AT T-SECTION FRAME 39 LOWER AREA BETWEEN STRG 52 LT TO 52 RT. REPAIR PERFORMED B Y CUT OUT THE BEAM AND INSTALL A NEW LOWER BEAM PORTION WITH A SPLICE APPROVED BY EA 6-5314-101269 AND RAS: 046044/048/2 006 ISS "A". 2 L 7 2 4F RT A35EU 2007083000031 20070830 00031 EU 2007 8 30 07FDEA03072 1 20070823 A 5311 A53778418228 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION FOUND ON REEINFORCING ANGLE FRAME 38.1-39, STRG 54 LT. REPAIR PERFORMED BY REPLACEMENT OF ANGLE WITHOUT CUTTI NG OF FRAME IAW EA 6- 5314-101270 AND RAS/DABRE/7006844/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007083000032 20070830 00032 EU 2007 8 30 07FDEA03073 1 20070823 A 5340 A53775406002 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 DAMAGED EXTERNAL FITTING ON FRAME 38, STRG 29 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007083000033 20070830 00033 EU 2007 8 30 07FDEA03074 1 20070823 A 5315 A53773616205 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 HEAVY CORROSION ON TOP CAP BEAM AT FRAME 33, OUT OF LIMIT. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 / FIG 207. 2 L 7 2 4F RT A35EU 2007083000034 20070830 00034 EU 2007 8 30 07FDEA03075 1 20070823 A 5320 A53811651200 FLOOR SUPPORT AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION FOUND ON PRESSURIZED FLOOR FRAME 39-40 LT. REPAIR PERFORMED BY BLEND OUT THE CORROSION AND OVERSIZING FASTENE R HOLE IAW EA 6-5314-103252 AND RAS/AS/0136/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007083000035 20070830 00035 EU 2007 8 30 07FDEA03076 1 20070823 A 5730 A57350141 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION AROUND OVERWING REFUELING PORT RT OUTER WING BETWEEN RIB 27-28, STRG 12-13. REPAIR PERFORMED BY BLEND OUT COR ROSION, NDT INSPECTION FOR CRACK FREE IAW EA 6-5720-103253 AND RAS/BAE/1003233/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007083000036 20070830 00036 NM 2007 8 30 07FDEA03078 1 20070823 A 5311 651766334 FRAME BOEING 727 727233 138408A NM ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 ON AGING, A/C INSP FOUND EXISTING REPAIR ON FRAME AT BS 700 BETWEEN STR 24L AND 26L DID NOT CONFORM TO SRM 51-40-3. REM OVED EXISTING REPAIR, FABRICATED REPAIR, HFEC FRAME TRIM OUT, NO CRACKS EXIST. INSTALLED FORMED REPAIR. REF FED EX EA 7-53-113940. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007083000037 20070830 00037 NM 2007 8 30 07FDEA03079 1 20070817 A 2131 7909601 CONTROLLER BOEING 727 727233 138408A NM CABIN PRESSURE MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 479FE 3668 3668 21461 CABIN ALT WARNING CLIMBING THROUGH FL270, CABIN ALT SHOWED 10,000, CLOSED CARGO HEAT OUTFLOW VALVE, NO CHANGE IN CABIN A LTITUDE. PERFORMED QRH CABIN ALT WARNING CHECKLIST. THEN PERFORMED FAILURE OF PRESSURIZATION OF CONTROL CHECKLIST. S YSTEM WOULD NOT PRESSURIZE IN AUTO OR STBY. IT DID WORK IN MANUAL. OUTFLOW VALVE INDICATED FULL CLOSED IN AUTO AND STB Y MODES. REMOVED AND REPLACED PRESSURE CONTROLLER PER M/M 21-31-010-4. PREMATURE REMOVAL/INSTALLATION, OFF MFG 790960- 1, SRL 8711490, ON MFG 790960-1, SRL 79K3611. 2 L 7 3 4F RT A3WE 2007083000038 20070830 00038 NM 2007 8 30 AALA20071457 1 20070718 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 940AN 30598 TUL- EMERGENCY LIGHTS IN MID COACH CABIN INOPERATIVE. REPLACED BATTERY PACK AT STATION 727 FOR EMERGENCY LIGHTS AT MID COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007083000039 20070830 00039 NM 2007 8 30 AALA20071452 1 20070714 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 751AN 30798 AFW - EMERGENCY LIGHTS AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY PACK AT RIGHT NUMBER TWO DOOR FOR EMERGEN CY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007083000040 20070830 00040 NM 2007 8 30 AALA20071456 1 20070717 A 3350 D71702991 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 969AN 29546 TUL - EMERGENCY LIGHTS IN COACH CABIN INOPERATIVE. REPLACED BATTERY PACK M1672 AT STATION 952 FOR EMERGENCY LIGHTS IN C OACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007083000041 20070830 00041 NM 2007 8 30 AALA20071446 1 20070702 A 5320 STRAP BOEING 767 767323 1385205 NM BS 1725 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 380AN 25449 AFW - CHORD STRAP AT STATION 1725 WAS DAMAGED. TRIMMED OUT DAMAGED PORTION OF CHORD STRAP. FABRICATED A REPAIR PIECE U SING 7075 T6 0.125 INCH THICK MATERIAL. INSTALLED THE REPAIR PIECE USING RIVETS OF THE SAME TYPE AND SIZE AS THE ORIGIN AL. 2 L 7 2 4F RT A1NM 2007083000042 20070830 00042 NM 2007 8 30 AALA20071448 1 20070702 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 968AN 30095 TUL - EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT STATION 322 FOR EMERGENCY LIGHTS IN FORWA RD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007083000043 20070830 00043 NM 2007 8 30 AALA20071449 1 20070710 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 932AN 29530 TUL - EMERGENCY LIGHTS IN MID COACH CABIN INOPERATIVE. REPLACED BATTERY PACK BETWEEN STATION 700 AND 800 FOR EMERGENCY LIGHTS AT MID COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007083000044 20070830 00044 NM 2007 8 30 AALA20071451 1 20070710 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 932AN 29530 TUL - EMERGENCY LIGHTS IN MID CABIN INOPERATIVE. REPLACED BATTERY PACK BETWEEN STATION 600 AND 650 FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007083000045 20070830 00045 NM 2007 8 30 AALA20071453 1 20070716 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 934AN 29531 TUL - EMERGENCY LIGHTS AT AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK AT STATION 967 FOR EMERGENCY LIGHTS AT AFT GALL EY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007083000046 20070830 00046 NM 2007 8 30 AALA20071447 1 20070702 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 901AN 29503 TUL - EMERGENCY LIGHTS IN MID COACH CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT 19A FOR EMERGENCY LIGHTS AT MID CO ACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007083000047 20070830 00047 NM 2007 8 30 AALA20071454 1 20070716 A 3350 D71701100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 934AN 29531 TUL - EMERGENCY LIGHTS IN FORWARD COACH CABIN INOPERATIVE. REPLACED BATTERY PACK BETWEEN STATION 460 AND 540 FOR EMERGE NCY LIGHTS AT FORWARD COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007083000048 20070830 00048 NM 2007 8 30 AALA20071455 1 20070717 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 969AN 29546 TUL- EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK M1671 AT STATION 727 FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007083000049 20070830 00049 NM 2007 8 30 AALA20071450 1 20070710 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 932AN 29530 TUL- EMERGENCY LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK AT STATION 325 FOR EMERGENCY LIGHTS AT FORWA RD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007083000050 20070830 00050 EU 2007 8 30 AWXA200701012 1 20070815 A 5347 D57130147200 SEAT TRACK AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 SAL - MAJOR REPAIR - C-6 CHECK - CORROSION ON CABIN SEAT TRACK, BS 1590/FR 36 - BS 1810 / FR 41, +Y765. REPLACED CABIN SEAT TRACK, BS 1590/FR 36 - BS 1810/FR 41, +Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007083000051 20070830 00051 SO 2007 8 30 SWIA200718609 1 20070817 A 2150 A/C PACK EMB 120 EMB120ER 3260203 SO SMOKE A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 561SW 120335 RECEIVED "SMOKE" WARNING AND FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN, FLIGHT NR 5429. THAWED OUT FROZEN PACK AND O PS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2007083000052 20070830 00052 EA 2007 8 30 SWIA200718610 1 20070815 A 2530 COFFEEMAKER CNDAIR CL600 CL6002B19 1900309 EA GALLEY ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 986SW 7967 FLIGHT ATTENDANT REPORTS BURNING ODOR FROM GALLEY, FLIGHT NR 6205. REPLACED LEFT HOT JUG PER CRJ MM 25-32-02. OPS CHEC KED GOOD. 2 L 7 2 4F RT A21EA 2007083000053 20070830 00053 SO 2007 8 30 SWIA200718611 1 20070809 A 5610 NP1513111 WINDSHIELD EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 301YV 2696 2696 120301 LEFT WINDSHIELD CRACKED, FLIGHT NR 5778. REPLACED WINDSHIELD IAW MM 56-00-00, OPS CHK GOOD. 2 L 7 2 4T RT A31SO 2007083000054 20070830 00054 EA 2007 8 30 SWIA200718612 1 20070815 A 5610 601R3303317 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 466SW 7856 CAPTAINS WINDSHIELD CRACKED IN FLIGHT. DIVERTED TO BIS, FLIGHT NR 3876. REPLACED CAPTAINS WINDSHIELD IAW 56-11-01. 2 L 7 2 4F RT A21EA 2007083000055 20070830 00055 EA 2007 8 30 SWIA200718613 1 20070813 A 2913 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 07 417SW 7400 RECEIVED HYDRAULIC SYSTEM 1 LOW PRESSURE CAUTION MESSAGE. RETURNED TO RDU, FLIGHT NR 2702. REPLACED FLEX LINE AND NR 1 EDP IAW 32-29-01. OPS AND LEAK CHECK GOOD, PN 88705, SN OFF MX-600582. 2 L 7 2 4F RT A21EA 2007083000056 20070830 00056 SO 2007 8 30 SWIA200718614 1 20070814 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DISCHARGED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 576SW 120345 FORWARD CABIN EMERGENCY LIGHTS DO NOT STAY ON, FLIGHT NR 5706. REPLACED FORWARD EMERGENCY BATTERY PACK IAW 33-50-02 EMB 120 MM. 2 L 7 2 4T RT A31SO 2007083100005 20070831 00005 NM 2007 8 31 USAA070661 1 20070823 A 5320 FITTING BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 CLIP AT STA 947.5 STR 24L, FWD OF WATER SERVICE PANEL HAS CRACK. FAB'D NEW ANGLE PER BOEING DWG 65-51626 & INSTALLED PE R SRM 51-10-02, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007083100006 20070831 00006 NM 2007 8 31 USAA070660 1 20070823 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 STR 15L AT STA 360 HAS CRACK. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SM 51-40-00, DEFECT SIZE: 0.7 INCH. 2 L 7 2 4F RT A16WE 2007083100007 20070831 00007 NM 2007 8 31 USAA070659 1 20070823 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 457UW 25021 STA 900, S-1R, SKIN HAS WEAR. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER SRM 53-60-01, REP 10, DEFECT SIZE: 6 INCH. 2 L 7 2 4F RT A16WE 2007083100008 20070831 00008 NM 2007 8 31 USAA070658 1 20070823 A 5720 ANGLE BOEING 737 737401 1384701 NM RT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 ON RIGHT WING, LOWER -T- CRACKED AT WBL 135.5. REMOVED & REPLACED WING LOWER ANGLE PER EA 98794, DEFECT SIZE: .75 INCH . 2 L 7 2 4F RT A16WE 2007083100010 20070831 00010 NM 2007 8 31 USAA070656 1 20070823 A 5313 6561777 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 517AU 23703 BS 360 STR 15L HAS CRACK. DEFECTIVE PART REPLACED WITH IDENTICAL PER SRM 51-10-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007083100011 20070831 00011 NM 2007 8 31 USAA070655 1 20070823 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 517AU 23703 BS 407 RBL 1.5, RADIUS ALTIMETER CUTOUT HAS CRACK. INSTALLED REPAIR DOUBLER, FILLER & ADIO ALT PER T/R 53-30-71, DEFECT SIZE: .25. 2 L 7 2 4F RT A16WE 2007083100012 20070831 00012 NM 2007 8 31 USAA070654 1 20070823 A 5320 6517684Y642 INTERCOSTAL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 517AU 23703 BS 294.5, S-15L, WEB INTERCOSTAL HAS CRACK. REPLACED INTERCOSTAL IAW SRM 51-10-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007083100015 20070831 00015 NM 2007 8 31 USAA070651 1 20070823 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 442US 24841 727E AT S24R HAS CRACK. INSTALLED PATCH PER SRM 53-00-01 REP 31, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007083100016 20070831 00016 EU 2007 8 31 USAA070650 1 20070823 A 5347 SEAT TRACK AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 177US 1517 SEAT TRACK AT FR 24 - Y1292 CORRODED. CUT OUT CORRODED PORTION & SPLICED IN NEW PER SRM 53-00-15 FIG 202; CORR TASK JA- 900-0900-137, LEVEL 1, DEFECT SIZE: 2 INCH SQ. 2 L 7 2 4F RT A28NM 2007083100017 20070831 00017 NM 2007 8 31 USAA070649 1 20070823 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 UPPER HINGE CUTOUT AT RIGHT AFT SERVICE DOOR AREA, ST 951, WL 251.77 HAS CRACK. PER SRM 53-60-01 DOUBLER RETAIL 1 CAT B , DEFECT SIZE: .75 INCH. 2 L 7 2 4F RT A16WE 2007083100019 20070831 00019 EU 2007 8 31 YENA2007078 1 20070823 A 2150 17055785401 BELLOWS EMB ERJ190 ERJ190100IGW 3260408 EU RT A/C PACK TORN A YENA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 15 206JB 19000025 FLT 1263, BOS-AUS DIVERTED TO JFK, CABIN PRESSURE STARTED CLIMBING AT 26,000 FT AND WOULD NOT MAINTAIN ALTITUDE (MAX CAB IN ALTITUDE 9600FT). ACCOMPLISHED REMOVAL AND REPLACEMENT OF RIGHT PACK OUTLET FLEX BELLOW PER AMM 21-51-21. PERFORMED CPCS OPERATIONAL TEST AND ADJUSTMENT TEST PER AMM 21-31-00. GROUND TEST NORMAL. NO LEAKS NOTED. 2 L 7 2 4F RT A57NM 2007083100020 20070831 00020 NM 2007 8 31 MWEA070182 1 20070817 A 2560 P4010021 BATTERY BOEING 717 717200 1383700 NM FLASHLIGHT DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 909ME 55173 FORWARD FLIGHT ATTENDANT STATION LOWER FLASHLIGHT CHARGE INOPERATIVE. REMOVED AND REPLACED BATTERY. 2 L 7 2 4F TR A6WE 2007083100023 20070831 00023 EA 2007 8 31 SWIA200718617 1 20070812 A 2913 6619003 PUMP CNDAIR CL600 CL6002D24 1390016 EA NR 2 HYD SYSTEM LEAKING A SWIA O OTHER K FLUID LOSS AP APPROACH 1 NM 07 804SK 15067 RECEIVED A "HYD 2 LO PRESS" CAUTION MESSAGE ON ARRIVAL, FLIGHT NR 2056. REPLACED NR 2 EDP IAW CRJ 900 AMM 29-11-01. 2 L 7 2 4F RT A21EA 2007083100026 20070831 00026 EA 2007 8 31 SWIA200718619 1 20070819 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 439SW 7578 FORWARD FLOOR EMERGENCY LIGHTS ARE INOP, FLIGHT NR 3916. INSTALLED NEW EMERGENCY LIGHT FLOOR SEGMENT. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007083100027 20070831 00027 2007 8 31 SB07072 4 20070823 A 2565 D37022101 BOTTLE AIRCRUISERS BOEING 737 7374B7 1384702 NM EVAC SLIDE LOW PRESSURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 0742 24781 MCO - MAINTENANCE REPORTED THE FORWARD ENTRY DOOR EMERGENCY ESCAPE SLIDE REQUIRES REPLACEMENT DUE TO INADEQUATE BOTTLE P RESSURE. MAINTENANCE REMOVED AND REPLACED THE FORWARD ENTRY DOOR EMERGENCY ESCAPE SLIDE. 2 L 7 2 4F RT A16WE 2007083100028 20070831 00028 2007 8 31 UPS07250488 4 20070817 A 2565 SLIDE BOEING 727 727185C 138406N NM CREW ENTRY OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:N/A CREW ENTRY ESCAPE SLIDE FELL OUT OF CASE. REPLACED ESCAPE SLIDE AS NEEDED, OKAY FOR SERVICE. REF M /M 25-60-14- 2. 2 L 7 3 4F A3WE 2007083100029 20070831 00029 NM 2007 8 31 UPS07450487 1 20070823 A 3350 BATTERY PACK BOEING 747 747200 1384847 NM CABIN LOOSE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:N/A EMERGENCY -EXIT- SIGN AT CREW SERVICE DOOR INOP. FOUND BATTERY PACK LOOSE. SECURED, OPERATIONAL NO RMAL PER AMM 33-51-02. 2 L 7 4 4F RT A20WE 2007083100031 20070831 00031 NM 2007 8 31 UPS07650455 1 20070817 A 2841 INDICATOR BOEING 767 76734AF 1385212 NM COCKPIT FAULTY A IPXA K NONE O OTHER UK UNKNOWN 1 SO 01 329UP 27755 INSPECTION TYPE:ETOP ALL 3 F/Q INDICATOR WINDOWS IN COCKPIT UNREADABLE. BUBBLES IN FUEL INDICATOR LEFT & RIGHT. *SUPPL EMENTAL SDR* REMOVED AND REPLACED FUEL QUANTITY INDICATOR PER MM 28-41-04-4. PERFORMED ADJ AND TEST IAW MM 28-41-00-5. 2 L 7 2 4F RT A1NM 2007083100033 20070831 00033 NM 2007 8 31 UPS07650485 1 20070823 A 3620 WARNING SYSTEM BOEING 767 76734AF 1385212 NM COCKPIT MALFUNCTIONED A IPXA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 306UP 27759 INSPECTION TYPE:ETOP BTB - RIGHT PRV MSG ON START. PERFORMED ENGINE START AND EICAS MESSAGE WENT AWAY. OK FOR AIRCRAFT TO CONTINUE PER FIM 36-10-00. 2 L 7 2 4F RT A1NM 2007083100036 20070831 00036 NE 2007 8 31 NACA20070017 2 20070822 A 7421 RHB32E SPARK PLUG DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 4 ENGINE FAILED A NACA E ENGINE SHUTDOWN W R J INADEQUATE Q C PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 AL 03 43872 190 190 533294 P33688 NR 4 ENGINE SHUT DOWN DUE TO CONTINUOUS BACKFIRE IN CLIMB. INSPECTION REVEALED NO CRACKED CYLINDERS, FRONT CAM NO DEFEC T. COMPRESSION TEST OF NR 12 CYLINDER CHECKED GOOD, NR 12 EXHAUST VALVE GUIDE CHECKED GOOD IAW PURDUE DC-6 MM MB31-3-1 (7). MULTIPLE SPARK PLUGS FOUND WITH EXCESSIVE GAP. NR 8R AND NR 12L SPARK PLUGS WERE FOUND INOPERATIVE. REPLACED ALL PLUGS. GROUND RUN CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2007083100039 20070831 00039 WP 2007 8 31 UPS07850482 1 20070803 A 5313 3779762U501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 680 L9L FWD. REMOVED CRACKED END FITTING AT STA 680 L9L IAW SRM 51-1-21. LOCATED, DRILLED UP, AND INSTALLED NEW LONGERON END FITTING AT STA 680 L9L IAW SRM 51-01-20D, AND DWG 377972. 2 L 7 4 4F RT 4A25 2007083100041 20070831 00041 WP 2007 8 31 070151 1 20070817 A 3297 CONNECTOR DOUG DC9 DC983 3022083 WP TRANSDUCER DAMAGED A WX0A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 19 869GA 53294 DURING TAKEOFF ROLL, WHEEL NOT TURNING LIGHT ILLUMINATED AT 80 KNOTS. NO DRAG FROM WHEELS WAS NOTED. TAKEOFF WAS ABORT ED AND AIRCRAFT RETURNED TO THE GATE AT LAS VEGAS. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED AND REPLACED BROKEN TRANS DUCER PINS ON THE NR 1 WHEEL ASSY AS REQUIRED. OPERATIONAL CHECK NORMAL IAW MM 32-43-02, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007083100043 20070831 00043 WP 2007 8 31 UPS07850484 1 20070806 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 FITTING CRACKED AT STA 1260 L20R. REMOVED AND REPLACED FITTING AT STA 1260 L20R IAW SRM 51-01-20D AN D SRM 51-3-2. 2 L 7 4 4F RT 4A25 2007082800174 20070828 00174 WP 2007 8 28 07FDEA03034 1 20070822 A 5730 SKIN DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 L/E RT WING CRACK ON EXTERNAL SKIN L/E . 2 L 7 3 4F A22WE 2007082800188 20070828 00188 WP 2007 8 28 07FDEA03049 1 20070822 A 5330 SKIN DOUG DC10 DC1010 3022110 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 EXT SURFACE RT SIDE FOUND DENT 2" BY 1" DEEP 0.062" ON SKIN. 09-19-07 REPAIRED SKIN IAW SRM 53-20-00 FIG 13 SHT 3-5 V OL I. 2 L 7 3 4F A22WE 2007082800189 20070828 00189 NM 2007 8 28 07FDEA03050 1 20070822 A 5320 6558352273 FLOOR SUPPORT BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FWD PIT, CARGO FLOOR SUPPORT HAS CORROSION AROUND NUTPLATES AT BS 640-646, LBL 9" FLOOR SUPPORT OUT OF LIMITS AFTER CLEA N UP, NEW FLOOR SUPPORT FABRICATION BY BACK SHOP ON N00727 REF BAC DWG 65-58352 AND HEAT TREATED ON 8130-3 FORM TRACKING NR 2007- 08-106 AND INSTALLED REF SRM 51-40-4 FIG 1 SHEET 5. 2 L 7 3 4F RT A3WE 2007082900003 20070829 00003 EU 2007 8 29 AALA20071413 1 20070805 A 5344 A5377868420200 HINGE AIRBUS 300 A300B4605R 3930308 EU A/C DOOR INOPERATIVE A AALA G A O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7082A 643 CABIN ALTITUDE CONTROL PROBLEM. OXYGEN MASKS AUTO DEPLOYED. DESCENDED TO 10000 FEET AND THE CABIN PRESSURE KEPT CLIMBI NG. REPLACED BROKEN DOOR HINGE FOR GROUND AIR CONDITIONING COVER. REPLACED BOTH SAFETY VALVES AND OUT FLOW VALVES. SYSTE M GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A35EU 2007082900007 20070829 00007 NM 2007 8 29 F3LA200700194 1 20070807 A 2121 20092455102 FAN AIRBUS A319 A319111 3930336 NM E/E SEIZED A F3LA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 917FR 2235 1890 DURING FLIGHT FROM KPDX TO KDEN, FLIGHT CREW REPORTED LIVE TV SMOKE DETECTION ALARM SOUNDED. AIRCRAFT DIVERTED TO KSLC AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LIVE TV EQUIPMENT FAN TO BE THE SOURCE OF LIVE TV SMOKE DETECTION. DEACTIVATED LIVE TV SYSTEM PER MEL 44-20-01AA, C/N 1029316. RAN APU AND PACKS. NO SMOKE SMELL DETECTED. PERFORMED OVE RWEIGHT LANDING INSPECTION IAW MP05510-4. NO DAMAGED OR DEFECTED NOTED. REPLACED THE LIVE TV EQUIPMENT COOLING FAN IAW LTV AMM 44-25-00. OPS CHECKED GOOD. REMOVED PLACARD. REPLACED THE LIVE TV EQUIPMENT COOLING FAN IAW LTV AMM 44-25-00. OPS CHECKED GOOD. REMOVED PLACARD. 2 L 7 2 4F RT A28NM 2007082900014 20070829 00014 WP 2007 8 29 UPS07850435 1 20070813 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:N/A EMERGENCY BATTERY PACK INOP. REPLACED EMERGENCY BATTERY PACK. OPS CHECKED NORMAL. 2 L 7 4 4F RT 4A25 2007082900036 20070829 00036 WP 2007 8 29 UPS07850457 1 20070816 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:N/A PIT 31 HAS HOLE IN FLOOR PANEL. A .375 INCH HOLE IN PIT 31 FLOOR PANEL IS LOCATED 33 INCHES AFT OF DOORSILL AND 41 INCHES LEFT OF CENTERLINE. ACCOMPLISHED INTERIM REPAIR PER EO DC8-5320-8724, APPROX A. DEFERRAL OPENED FOR PERMANENT REPAIR WITHIN 30 DAYS. PIT IS USABLE DURING THIS TIME. 2 L 7 4 4F RT 4A25 2007082900044 20070829 00044 WP 2007 8 29 ASAA0781950 1 20070815 A 5347 593056677 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 943AS 53018 G3 GALLEY FORWARD INBOARD SEAT TRACK MOUNTING IS CORRODED. REMOVED DAMAGED SECTION. INSTALLED PLUG REPAIR PER SRM 53-0 5. 2 L 7 2 4F RT A6WE 2007082900047 20070829 00047 NM 2007 8 29 ASAA0771965 1 20070814 A 5321 453A26105 FLOOR PANEL BOEING 737 737790 13844CN NM CARGO BAY DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 AFT PIT FLOOR PANEL AS STA 727 DENTED. REPAIRED IAW SRM 51-40-05. 2 L 7 2 4F RT A16WE 2007082900070 20070829 00070 NM 2007 8 29 ASAA0741975 1 20070817 A 5320 6517684634 INTERCOSTAL BOEING 737 737490 1384715 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 INTERCOSTAL CRACKED. REPLACED WITH NEW PART IAW EA 5310 02732. 2 L 7 2 4F RT A16WE 2007082900077 20070829 00077 SO 2007 8 29 C2XA07SH046 1 20070815 A 5751 14574000415 SHROUD EMB 145 EMB145LR 3260212 SO LT AILERON DEBONDED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26545 145558 SHV - DURING C-CHECK MAINTENANCE FOUND LEFT UPPER AILERON SHROUD HAS BAD BONDING ON OUTBOARD END. MAINTENANCE REPAIRED LEFT UPPER AILERON SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007082900079 20070829 00079 SO 2007 8 29 C2XA07SH049 1 20070815 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26545 145558 SHV - DURING C-CHECK MAINTENANCE FOUND LEFT OMEGA BEAM HAS CORROSION AT FRAME 20 AT CARBON CROSSMEMBER. MAINTENANCE REP AIRED LEFT OMEGA BEAM AT FRAME 20 IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007082900082 20070829 00082 NM 2007 8 29 BB07068 1 20070819 A 3350 2012 CHARGER BOEING 757 7572B7 1384964 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 929UW 27144 MAINTENANCE FOUND THE AFT RIGHT EMERGENCY LIGHT BATTERY AND CHARGER INOPERATIVE. REPLACED BATTERY AND CHARGER. NO FURT HER FAULTS. 2 L 7 2 4F RT A2NM 2007082900099 20070829 00099 WP 2007 8 29 UPS07850465 1 20070806 A 5240 WEB DOUG DC8 DC873F 302199F WP SERVICE DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 FWD LWR CORNER OF FWD RIGHT SERVICE DOOR HAS CRACK IN WEB. CUT OUT DAMAGED AREA ON FWD LWR CORNER WE B ON RIGHT FWD SERVICE DOOR IAW SRM 52-02-00 FIG 4. FABRICATED AND INSTALLED REPAIR DOUBLER ON RIGHT FWD SERVICE DOOR F WD LWR CORNER IAW SRM 52-02-00 FIG 4, AND SRM 51-09-00 FIG 68. 2 L 7 4 4F RT 4A25 2007082900102 20070829 00102 NM 2007 8 29 UPS07M50458 1 20070816 A 3310 SWITCH DOUG MD11 MD11F 3023600 NM COCKPIT LOOSE A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 256UP 48405 INSPECTION TYPE:N/A ELECTRICAL SPARK AND SMOKE FROM OVERHEAD PANEL NOSE LIGHTT SWITCH, BUT LIGHT WORKED WITH C/B POPPED. FOUND NOSE LANDING LIGHT SWITCH LOOSE. TOUCHED HOUSING OF RIGHT RWY TURN OFF LIGHT. TIGHTENED SWITCH IAW AMM 33-42-0 7-4. OPS CHECK OK. 2 L 7 3 4F RT A22WE 2007082900118 20070829 00118 NM 2007 8 29 KCSA071323 1 20070821 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 MAIN DECK SEAT TRACK CORRODED AT LBL 12 BETWEEN BS 1680 AND 1720. 2 L 7 4 4F RT A20WE 2007082900120 20070829 00120 NM 2007 8 29 ABXA070257 1 20070819 A 3260 LIGHT BOEING 767 767281 1385109 NM COCKPIT INOPERATIVE A ABXA O OTHER O OTHER AP APPROACH 1 GL 23 775AX 22790 ON APPROACH AT ILN, RIGHT GEAR GREEN DOWN LIGHT FAILED TO ILLUMINATE WITH GEAR HANDLE DOWN. EICAS MESSAGE GEAR DISAGREE DISPLAYED, DOOR AMBER LIGHTS WERE EXTINGUISHED AND GEAR LIGHTS ILLUMINATED. EMERGENCY DECLARED. INDICATION NORMAL AFT ER ALTERNATE GEAR EXTENSION. TESTED RIGHT MAIN LANDING GEAR POSITION INDICATION SYSTEM, LANDING GEAR MONITOR AND POSITI ONER / GROUND CIRCUIT BREAKER IAW B767 AMM 32-61-00-5 PARA 3 H, K, J. NO FAULTS NOTED. REPLACED RIGHT MAIN LANDING GEA R KORRY LIGHT BULB RECEPTICAL. JACKED AIRCRAFT, CYCLED LANDING GEAR SEVERAL TIMES, NO DEFECTS NOTED. PSEU BITE CHECK O KAY, MEMORY CLEARED. 2 L 7 2 4F RT A1NM 2007082900126 20070829 00126 EA 2007 8 29 VNAA0707019 1 20070731 A 7722 6030T41P02 THERMOCOUPLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENGINE FAULTY A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 05 258PS 7434 7941 CREW REPORTED AN EICAS COMP MON IN FLIGHT WITH ERRATIC ITT INDICATIONS TO THE LEFT HAND ENGINE. CREW RETURNED TO CLT AN D LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND TROUBLESHOT THE LEFT HAND ENGINE OUTBOARD THERMO COUPLE ASSEMBLY. MAINTENANCE REMOVED AND REPLACED THE THERMO COUPLE ASSEMBLY IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 77-11-05 -400-801. OPS CHECKS GOOD AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007082900139 20070829 00139 WP 2007 8 29 ABXA070260 1 20070815 A 5320 995789923 FITTING DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 WHILE COMPLYING WITH EA 53300036, FOUND CRACKED CLIP FOR INTERCOSTAL, REF AD 2002-21-09. FABRICATED AND INSTALLED NEW C LIP IAW DWG 9957899 AND DC9 SRM 51-30-05. 2 L 7 2 4F A6WE 2007082900140 20070829 00140 WP 2007 8 29 ABXA070261 1 20070815 A 5311 99115055 FRAME DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 WHILE COMPLYING WITH EA 53300036, FOUND CRACKED FRAME, REF AD 2002-21-09. REPAIRED AREA IAW DC9 SRM 5303 FIG 34. 2 L 7 2 4F A6WE 2007082900151 20070829 00151 WP 2007 8 29 ASAA0781985 1 20070817 A 5321 99365841 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 943AS 53018 CABIN FLOOR PANEL IS PUNCTURED. REPAIRED WITH BONDED DOUBLER PER SRM 51-70-02. 2 L 7 2 4F RT A6WE 2007082900152 20070829 00152 WP 2007 8 29 ASAA0781986 1 20070817 A 5321 99365813 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 943AS 53018 CABIN FLOOR PANEL DELAMINATED (TOP FIBER LAYER PULLED LOOSE). APPLIED GLASS FABRIC LAYER PER MM 25-00-00 PP 804-805. 2 L 7 2 4F RT A6WE 2007082900153 20070829 00153 WP 2007 8 29 ASAA0781987 1 20070817 A 5321 99365853 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 943AS 53018 CABIN FLOOR PANEL DELAMINATED (TOP FIBER LAYER PULLED LOOSE). APPLIED GLASS FABRIC LAYER PER MM 25-00-00 PP 804-805. 2 L 7 2 4F RT A6WE 2007082900171 20070829 00171 WP 2007 8 29 UPS07850477 1 20070807 A 5320 265247987 SUPPORT ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 CORROSION UNDER NUT PLATES IN AFT CABIN SUBFLOOR, STA 1746-1756 ALONG RBL 17. REMOVED SUPPORT, REMOV ED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED SUPPORT ANGLE SRM 51-1-8, 51-1-21, 53-02-00, 51-3-0 D WG 2652479-87. REF TR GMM188. 2 L 7 4 4F RT 4A25 2007082900183 20070829 00183 WP 2007 8 29 ABXA070271 1 20070719 A 5313 39248091AX FITTING DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 978AX 47628 LONGERON 29 LEFT AT APPROXIMATELY STA 636, END FITTING WAS CORRODED. REMOVED AND REPLACED END FITTING IAW DC9 SRM 51-30 -2. 2 L 7 2 4F A6WE 2007082900186 20070829 00186 WP 2007 8 29 ABXA070267 1 20070728 A 5320 99557501 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 986AX 47543 MAIN ENTRY DOOR INTERCOSTAL CRACKED PAST PREVIOUS STOP DRILL IN UPPER FORWARD CORNER AREA. REMOVED AND REPLACED REPAIR IAW DC9 SRM 51-30-5 AND 51-30-1. 2 L 7 2 4F A6WE 2007082900191 20070829 00191 EA 2007 8 29 TRAX200701225 1 20070819 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR JAMMED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 908EV 7654 MAIN CABIN DOOR HANDLE JAMMED AND WILL NOT CLOSE. 2 L 7 2 4F RT A21EA 2007082900194 20070829 00194 EA 2007 8 29 TRAX200701228 1 20070820 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 741EV 10155 CABIN CEILING SECOND EMERGENCY LIGHT DO NOT ILLUMINATE. 2 L 7 2 4F RT A21EA 2007082900196 20070829 00196 EU 2007 8 29 TRAX200701230 1 20070822 A 2560 SIGN AEROSP ATR72 ATR72 EU CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 EMERGENCY EXIT SIGN MISSING INSIDE AIRCRAFT NEXT TO SERVICE DOOR. 2 H 7 2 4T RT 2007082900197 20070829 00197 EA 2007 8 29 TRAX200701231 1 20070822 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 852AS 7369 F/A FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007082900203 20070829 00203 NM 2007 8 29 MWEA070185 1 20070821 A 7830 7150021507 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 903ME 55167 RIGHT THRUST REVERSER UPPER FRAME IS CRACKED AT OUTBOARD STATION 36. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2007082900207 20070829 00207 NM 2007 8 29 SWAA074162 1 20070822 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 787SA 29812 EEPLS LENS LOOSE AT ROW 3 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007082900212 20070829 00212 NM 2007 8 29 SWAA074145 1 20070822 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 775, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007082900214 20070829 00214 NM 2007 8 29 SWAA074155 1 20070822 A 5315 6545833 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 270, LBL 4 TO RBL 4. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2007082900217 20070829 00217 WP 2007 8 29 07FDEA02966 1 20070818 A 5340 AFA71321 FITTING DOUG DC10 DC1030 3023501 WP CARGO DOORWAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 318FE 46837 NR 4 MAIN CARGO DOOR JAM SUPPORT FITTING P/N AFA 7132-1, REQUIRES REPLACEMENT DUE TO CRACKS REMAINING AFTER REAMING TO . 520. REMOVED SUPPORT BRACE, STRAP, CLIP, INTERCOSTAL AND BACKUP FITTING IAW SRM 51-31-01. INSTALLED NEW BACKUP FITTING AND REINSTALLED SUPPORT BRACE, STRAP, CLIP, AND INTERCOSTAL IAW SRM 51-31-01. DOOR RIG ACCOMPLISHED ON ORIGINAL EO T 8 -5230-110698. 2 L 7 3 4F A22WE 2007082900221 20070829 00221 NM 2007 8 29 SWAA074154 1 20070822 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007082900226 20070829 00226 NM 2007 8 29 SWAA074146 1 20070822 A 5330 65C381921 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503L, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007083000001 20070830 00001 EU 2007 8 30 07FDEA03105 1 20070824 A 5340 A5377364420600 FITTING AIRBUS 310 A310203 3930313 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 FWD PIT, FRAME FITTING CRACKED, FR38 (X2082), BL 60L (Y1520), AT PIT FLOOR LEVEL.. REMOVED CRACKED FITTING IAW FEDEX A 31 SRM 51-40-21 LOCATED DRILLED NEW FITTING PO 583026.6 IAW FEDEX SRM 51-40-44 PARA2. INSTALLED NEW FRAME FITTING IAW FEDEX SRM 51- 40-27 PARA 7. 2 L 7 2 4F RT A35EU 2007083000002 20070830 00002 CE 2007 8 30 DXTA200702394 1 20070809 A 2750 99143742 CONVERTER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS FAULTY E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 930QS 6431 7500130 FLAPS FAIL EICAS IN FLIGHT FOLLOWED FLAP RESET PROCEDURE IAW CHECK LIST NO RESPONSE. DID NO FLAP LANDING. REMOVED FAULT Y LEFT FLAP POWER CONVERTER AND #2 FLAP POSITION SENSOR. INSTALLED INSPECTED FLAP SENSOR BY MPC PRODUCTS CRS M 74R907N A ND INSTALLED NEW LEFT CONVERTER AND PERFORMED FLAP OPS CHECK GOOD. IAW C750 M.M. 27-50-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007083000003 20070830 00003 CE 2007 8 30 DXTA200702395 1 20070809 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE RT SEAT WEAK E DXTA O OTHER O OTHER LD LANDING 1 GL 07 371QS 5600471 RT SEAT BRAKES VERY MUSHY WHEN BRAKE PRESSURE APPLIED. M2B- BLED BRAKE SYSTEM PER CHAPTER 32-42-00 OF THE CITATION 560 MM OPERATIONAL AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2007083000005 20070830 00005 CE 2007 8 30 DXTA200702397 1 20070812 A 2910 AS11604K0171 HOSE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG STEERING ACT FAULTY E DXTA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 07 912QS 7516 7500012 UPON DEPARTURE, UPON GEAR RETRACTION, OBSERVED A LOUD SINGLE (THUD), FOLLOWED BY A HIGH PRESSURE (HISSING) SOUND, THEN A STRONG ODOR OF HYDRAULIC FLUID. WITHIN 2-5 SECONDS, MASTER CAUTION ILLUMINATED ALONG WITH THE FOLLOWING CAS MESSAGES: AMBER - HYD PTU. REMOVED FAULTY NLG STEERING ACTUATOR HOSES. BLED HYD SYSTEM. NG STEERING OPS CHECK GOOD. WORK DONE I/A/W C750 MM 12-10-03. LEAK CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007083000006 20070830 00006 CE 2007 8 30 DXTA200702401 1 20070813 A 2910 MP50B1 MOTOR CESSNA 560 560XL 2076702 CE HYD PUMP INOPERATIVE E DXTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 576QS 156 5605708 AFTER CLEARING RUNWAY ON TAXI IN, LO BRAKE PRESSURE LIGHT CAME ON, AND HAD NO BRAKES SO PULLED EMERGENCY BRAKE LEVER TO STOP THE A/C. FOUND BRAKE HYDRAULIC PUMP "ELECTRIC MOTOR" BAD. REPLACED WITH OVERHAULED UNIT IAW CE560XLS MM CH 32-42- 00 AND ANTISKID BLEED IAW CE560XLS MM CH 32-42-00. PERFORMED GEAR RETRACTION IAW CE560XLS MM CH 32-30-08. OPS CHECK GOOD . 2 L 7 2 4F RT A22CE 2007083000007 20070830 00007 CE 2007 8 30 DXTA200702402 1 20070814 A 3240 RESERVOIR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE BRAKES OVERSERVICED E DXTA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 GL 07 322QS 5600421 DURING ROLL OUT, THE BRAKES FAILED MOMENTARILY BUT HAD PRESSURE AT THE PEDALS. TROUBLESHOT SYSTEM AND FOUND BRAKE RESE RVOIR TO BE OVERSERVICED. REMOVED SOME OF THE FLUID FROM THE RESERVOIR. RAN AIRCRAFT AND PERFORMED BRAKE SYSTEM FUNCTION AL CHECK WITH NO DEFECTS NOTED. ALL WORK PERFORMED IAW CESSNA CITATION V 560 MM 32-40 AND 12-00 2 L 7 2 4F 4 F RT A22CE E25EA 2007083000010 20070830 00010 EU 2007 8 30 TRBA2007070 1 20070820 A 2797 25712588 WIRE AEROSP ATR72 ATR72212 8680945 EU COCKPIT OPEN A TRBA O OTHER J WARNING INDICATION AP APPROACH 1 SO 29 408AT 408 FLAPS DID NOT MOVE FROM "0" TO "15" DEGREES ON APPROACH. PERFORMED "0" FLAPS LANDING AT SJU. AFTER TROUBLESHOOTING FOU ND AND REPAIRED OPEN WIRE NR 2571-2588 AS PER STANDARD PRACTICES JIC NR 20-25-22. 2 H 7 2 4T RT A53EU 2007083000011 20070830 00011 CE 2007 8 30 GLBA20060982 1 20070813 A 5320 ANGLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 288 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 208GL UE208 RT HEAVY ANGLE CRACKED AT RADIUS AT FS 288. CRACK IS APPROXIMATELY 2.2500 INCH LONG. MAINTENANCE REPAIRED THE RT HEAVY A NGLE IAW SRM 53-90. REPAIR APPOXIMATELY 13.5 INCHES. RII INSPECTION COMPLIED WITH IAW TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007083000012 20070830 00012 CE 2007 8 30 GLBA20060984 1 20070814 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 202 S15R CANNING A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 208GL UE208 EVIDENCE OF OIL CANNING PRESENT AT FS 202.25 2 INCHES FROM CENTER OF REPAIR TO STRINGER 15 R APPROXIMATELY 2 INCHES SQUA RE. MAINTENANCE REPAIRED AFFECTED AREA IAW SRM 51-70. INSERTION PATCH DIMENSION APPROXIMATELY 2 INCH X 2 INCH WITH REPAI R APPROXIMATELY 4.5 INCH X 4.5 INCH. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007083000013 20070830 00013 SO 2007 8 30 SIMA200723505 1 20070821 A 2121 4611028900 FAN EMB 135 EMB135KL 3260302 SO ZONE 100 FAILED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 818AE 11901 1041 145561 ELECTRICAL BURNING ODOR, TURNED SHED BUSSES OFF ODOR DISSIPATED. REMOVED AND REPLACED RECIRCULATION FAN IAW EMB AMM - O PERATIONAL CHECK GOOD - PERFORMED FUNCTIONAL; CHECK FLIGHT WITH NO DEFECTS NOTED - AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT T00011AT 2007083100001 20070831 00001 CE 2007 8 31 2007F00048 1 20070816 A 2497 WIRE LEAR 35 35A 5170602 CE COCKPIT BURNED E Y6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 11 55FN 202 ON DESCENT INTO HLN, SMOKE WAS NOTICED IN THE COCKPIT. THIS WAS PRECEDED BY AN AUG/AIL ANNUNCIATOR LIGHT ON THE GLARESH IELD. AN EMERGENCY WAS DECLARED, THE EMERGENCY CHECKLIST WAS ACCOMPLISHED, AND AN EMERGENCY LANDING WAS MADE. TWO COCK PIT CREW AND TWO MEDICAL TECHNICIANS WERE ONBOARD. IT WAS FOUND THAT A BURNED OUT WIRE BEHIND THE CIRCUIT BREAKER PANEL ON THE F/O SIDE WAS RESPONSIBLE. REPAIRS WERE MADE IAW COMPANY PROCEDURES AND THE A/C RETURNED TO SERVICE. 2 L 7 2 4F A10CE 2007083100002 20070831 00002 CE 2007 8 31 8172007 1 20070817 A 3310 2N3055 TRANSISTOR BCRAFT BEECH 99 B99 1154004 CE COCKPIT FAILED E AXSA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 65 199WA 34380 34380 U154 DURING DESCENT ON FLIGHT 1045 (BGR-MHT) THE PILOT ACTIVATED THE OVERHEAD PANEL LIGHT SWITCH. WITHIN 60 SECOND THE PILOT NOTED A BURNING ODOR (ELECTRICAL) BUT COULD NOT IDENTIFY THE SOURCE. THE PILOT CONTINUED THE APPROACH AND LANDING WITH OUT INCIDENT BUT BY THE TIME THE PILOT WAS READY TO TAXI THE SMOKE WAS NOTICEABLE IN THE COCKPIT. THE PILOT TAXIED AND PARKED THE AIRCRAFT WITHOUT INCIDENT AND CONTACTED MAINTENANCE CONTROL. MAINTENANCE ISOLATED THE PROBLEM TO THE SW PANE L FAILING WHICH POPPED THE CIRCUIT BREAKER. MAINTENANCE COLLARED THE C/B, RAN THE AIRCRAFT AND ELECTRICAL SYSTEMS WITH NO OTHER DEFECTS NOTED. THE LIGHTING WAS DEFERRED IN ACCORDANCE WITH MEL 33-1. FURTHER TROUBLESHOOTING REVEALED A FAUL 1 L 7 2 3T A14CE 2007083100003 20070831 00003 NM 2007 8 31 USAA070663 1 20070823 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 STA 727 RBL 40 FWD BULKHEAD, AFT CARGO CRACKED. FABRICATED WEB STIFFENER BRACKET & INSTALLED PER SRM 52-40-02, DEFECT S IZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007083100004 20070831 00004 NM 2007 8 31 USAA070662 1 20070823 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 STA 500 & 500A STR 26L AT LIGHTENING HOLE HAS CRACK. MANUFACTURED NEW PART PER SRM 51-10-02, 53-30-04, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007083100009 20070831 00009 NM 2007 8 31 USAA070657 1 20070823 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 517AU 23703 STA 294.5, S-11L, INTERCOSTAL WEB, CRACK IN RADIUS. REMOVED WEB, FABRICATED NEW & INSTALLED PER DWG 50-07946, SRM 51-10 -02, DEFECT SIZE: 0.25 INCH. 2 L 7 2 4F RT A16WE 2007083100021 20070831 00021 EA 2007 8 31 SWIA200718615 1 20070814 A 2913 PUMP CNDAIR CL600 CL6002B19 1900309 EA NR 2 HYD SYSTEM LEAKING A SWIA O OTHER K FLUID LOSS NR NOT REPORTED 1 NM 07 943SW 7762 RECEIVED THE HYDRAULIC SYSTEM 2 LOW PRESSURE CAUTION MESSAGE, FLIGHT NR 6229. REMOVED AND REPLACED NR 2 ACMP BALL ATTEN UATOR PACKING AND NR 2 EDP IAW AMM 29-11-01, PN 887055, SN/OFF MX662435. 2 L 7 2 4F RT A21EA 2007083100025 20070831 00025 EA 2007 8 31 SWIA200718618 1 20070819 A 3350 SIGN CNDAIR CL600 CL6002C10 1390015 EA CABIN MISSING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 705SK 10145 REAR MOST OVERHEAD PAX EXIT SIGN MISSING, FLIGHT NR 5875. INSTALLED SERVICEABLE EXIT SIGN AS REQUIRED. 2 L 7 2 4F RT A21EA 2007083100032 20070831 00032 EA 2007 8 31 SWIA200718621 1 20070818 A 3397 INVERTER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 439SW 7578 FOUND FORWARD FLOOR EMERGENCY LIGHTS ARE INOP. REPLACED INVERTER IAW MM 55-51-04. OPS CHECK GOOD, P/N - 5925-2. 2 L 7 2 4F RT A21EA 2007083100034 20070831 00034 EA 2007 8 31 QXEA200701349 1 20070817 A 3150 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 619QX 10246 PDX - FLIGHT 2571, ON TAXI RECEIVED A AFT CARGO SHUTOFF VALVE MESSAGE. RETURNED TO THE GATE. MAINTENANCE CYCLED THE EL ECTRICAL POWER, NO FAULTS IN HISTORY, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007083100045 20070831 00045 WP 2007 8 31 UPS07850490 1 20070725 A 2560 GIRT BAR DOUG DC8 DC871F 302199D WP ESCAPE SLIDE UNKNOWN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:N/A CAN'T STOW GIRT BAR ON ESCAPE SLIDE. STOWED GIRT BAR ON SLIDE. 2 L 7 4 4F RT 4A25 2007083100047 20070831 00047 WP 2007 8 31 WX0A070146 1 20070813 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 879GA 53486 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007083100050 20070831 00050 WP 2007 8 31 WX0A070152 1 20070819 A 7700 PROBE DOUG DC9 DC983 3022083 WP PT 2 OBSTRUCTED A WX0A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 19 892GA 49826 DURING TAKEOFF ROLL, RIGHT AND LEFT ENGINES FAILED TO OBTAIN MINIMUM N1 SPEED AT 90 KNOTS. BOTH ENGINES INDICATED BETWE EN 79-80 N1 SPEED AT 1.86 EPR. ABORTED TAKEOFF AND RETURN TO THE GATE. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED AND REMOVED DEBRIS FROM THE RIGHT ENGINE PT2 PROBE. GROUND RUN OPERATIONAL CHECK NORMAL, BOTH ENGINES PERFORMED WITHIN LIMI TS IAW 71-00-00, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007083100052 20070831 00052 NM 2007 8 31 ABXA070273 1 20070814 A 3350 BPS73 BATTERY PACK BOEING 767 767281 1385109 NM CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 786AX 23019 EMERGENCY EXIT LIGHTS INOPERATIVE. SWITCHED BATTERY PACKS IAW B767 MM 33-52-07. OPS CHECKED GOOD. USED SPARE EMERGENC Y EXIT LIGHT BATTERY PACK. PART IS -F- CLASS, NOT RELIABILITY PART. 2 L 7 2 4F RT A1NM 2007083100055 20070831 00055 SO 2007 8 31 C2XA07CL071 1 20070823 A 3260 8005701 PROXIMITY SWITCH EMB 135 EMB135ER 3260203 SO LT MLG FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 27 19503 145176 DAY FLIGHT 2386 - THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE EICAS. THE GEAR WOULD NOT RETRACT. M AINTENANCE INSPECTED AND REPLACED THE LEFT MAIN GEAR PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2007083100056 20070831 00056 EU 2007 8 31 07FDEA03082 1 20070824 A 5311 A53870033201 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CRACKED HOLE (H22) IN UPPER FRAME FEET AT FRAME 45, STRG 26-27 RT REPAIR PERFORMED BY OVERSIZING, COLD WORKING AND INSTA LLATION OF FASTENER WITH HIGH INTERFERENCE FIT IAW EA 6-5315-103254 AND RAS: 046149/010/2006 ISS "A" 2 L 7 2 4F RT A35EU 2007083100058 20070831 00058 EU 2007 8 31 07FDEA03083 1 20070824 A 5311 A53870064203 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 TWO CRACKED HOLES (H1, H2) WERE FOUND AT FRAME 43, STRG 26-27 RT, REPAIR PERFORMED BY REPLACING FITTING AND APPLY SB A31 0-53-2124 ON THE NEW FITTING HOLES IAW EA 6-5315-103254. 2 L 7 2 4F RT A35EU 2007083100059 20070831 00059 NM 2007 8 31 MWEA070181 1 20070817 A 3350 4TL115 SWITCH BOEING 717 717200 1383700 NM CABIN DIRTY A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 916ME 55178 EMERGENCY LIGHTS IN CEILING FORWARD HALF ARE INOPERATIVE. CLEANED CONTACTS ON SWITCH, CYCLED SWITCH SERVERAL TIME WITH PROPER OPERATION EACH TIME. 2 L 7 2 4F TR A6WE 2007083100060 20070831 00060 WP 2007 8 31 07FDEA03084 1 20070824 A 5730 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 600 DEFORMED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 RT WING T/E LOWER SKIN OF ISLAND DEFORMATION. REPAIRED AREA IAW SRM 57-00-01 VOL 1 SHT 2 FIG 4. 2 L 7 3 4F A22WE 2007083100061 20070831 00061 WP 2007 8 31 07FDEA03086 1 20070824 A 5730 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 LT WING OUTBOARD FLAP CORROSION UNDER UPPER SKIN. 10-11-07 REPAIRED AREA IAW SRM 57-10-00 VOL I FIG 85. 2 L 7 3 4F A22WE 2007083100062 20070831 00062 EU 2007 8 31 2007UALA02185 1 20070623 A 2161 775D000001 CONTROLLER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN TEMP MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 463UA 1282 RTFL DUE TO ALL 3 ZONES INDICATING 100F. *S/D* FAULTY ZONE TEMP CONTROLLER. REPLACED ZONE TEMP (150) CONTROLLER. SHO P FINDINGS: NO FAULT FOUND. 2 L 7 2 4F 4 F RT A28NM E40NE 2007083100064 20070831 00064 WP 2007 8 31 07FDEA03088 1 20070824 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 CTR W/W SPACE: CRACKS ON VERTICAL BULKHEAD. REPAIRED AREA IAW SRM 53-00-01 FIG 10 SHT 4 VOL I. 2 L 7 3 4F A22WE 2007083100065 20070831 00065 EU 2007 8 31 07FDEA03089 1 20070824 A 5311 A53870030200 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 DAMAGES, CRACKS AND CORROSION IN HOLE H4, H5, AND H6 AND MISDRILLED HOLE IN FITTING AND FRAME 44, BETWEEN STRG 26-27 L T REPAIR PERFORMED BY OVERSIZING HOLES, COLD WORKING, REPLACEMENT OF FITTING AND INSTALLING FASTENERS (NSA5357-5) WITH H IGH INTERFERENCE FIT. MISDRILLED HOLE IS OVERSIZED WITH FASTENER ASNA2027V5. WORKS COVERED BY EA 6-5315-103255 AND RAS : 046120/021/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007083100066 20070831 00066 NE 2007 8 31 2007UALA02268 2 20070626 A 7220 5R0279 ACOUSTIC LINER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE OUT OF POSITION A UALA A UNSCHED LANDING O OTHER AP APPROACH 1 WP 29 457UA 16144 1146 V10007 FLIGHT DIVERTED DUE TO NR 2 ENGINE COMPRESSOR STALL DURING GO-AROUND AT ORD. FAN BYPASS AIR STALL DUE TO AIR BLOCKAGE F ROM ACOUSTIC LINING. ENGINE REMOVAL: SB ENG-72-0392 ISSUED TO ADDRESS PROBLEM OFF WING. 2 L 7 2 4F 4 F RT A28NM E40NE 2007083100067 20070831 00067 EU 2007 8 31 07FDEA03090 1 20070824 A 5311 A53870033200 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CRACK IN DOUBLER FOUND IN HOLE H22 ON FRAME 45, STRG 26-28 LT REPAIR PERFORMED BY OVERSIZING, COLD WORKING AND INSTALLIN G NSA5359-5 FASTENER WITH HIGH INTERFERENCE FIT IAW EA 6-5315-103255 AND RAS: 046120/021/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007083100068 20070831 00068 EU 2007 8 31 07FDEA03091 1 20070824 A 5311 A53879304200 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CRACK FOUND IN HOLE H27 OF AFT FRAME 46, STRG 27-28 LT REPAIR PERFORMED BY OVERSIZING COLD WORKING AND INSTALLING NSA535 7-5 FASTENER WITH HIGH INTERFERENCE FIT IAW EA 6-5315-103255 AND RAS: 046120/021/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007083100069 20070831 00069 NM 2007 8 31 07FDEA03092 1 20070824 A 5347 53FX9762 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 UPPER MAIN CARGO DECK FLOOR STRUCTURE, SEAT TRACK BETWEEN STA 1130 TO 1166 PLUS 8", RBL 25", HAS CORROSION ON LOWER FAYI NG SURFACE AT AFT END. FABRICATED NEW SEAT TRACK, REF DWG 53FX 976, SEAT TRACK INSTALLED ON N/R N00816. THIS IS CLASSI FIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007083100072 20070831 00072 NM 2007 8 31 07FDEA03095 1 20070824 A 5322 652557714 SHEAR TIE BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LOWER FUSELAGE SKIN ATTACH ANGLE TO FAIRING WEB SUPPORT HAS CORROSION AT BS 720F AND RBL 11-22. REMOVED CORRODED ANGLE AND 65-25577-14 REPLACED. REFERENCE SRM 51-30-02 AND BOEING DOCUMENT NR 65-25577/ID NR 0003/FRAME NR 1, THIS IS CLASSIF IED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007083100073 20070831 00073 EU 2007 8 31 07FDEA03096 1 20070824 A 5730 A57350143200 SKIN AIRBUS 310 A310324 3930206 EU ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 ELONGATED HYDRAULIC FITTING HOLES IN LOWER SKIN PANEL LT. REPAIR PERFORMED BY OVERSIZING AND BUSHING OF AFFECTED HOLES IAW EA 6-5720-101266 AND RAS/BAE/1003250/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007083100074 20070831 00074 EU 2007 8 31 07FDEA03097 1 20070824 A 5730 A57350143202 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 ELONGATED HYDRAULIC FITTING HOLES IN LOWER SKIN PANEL RT. REPAIR PERFORMED BY OVERSIZING AND BUSHING OF AFFECTED HOLES IAW EA 6-5720-101266 AND RAS/BAE/1003250/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007083100080 20070831 00080 EU 2007 8 31 2007UALA03264 1 20070819 A 3350 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 456UA 1128 EMERGENCY LIGHT TEST FAILED FOR LEFT EPSU LOAD FAULT. PERFORMED BATTERY PACK RESET. SYSTEM CHECKS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007083100081 20070831 00081 NM 2007 8 31 2007UALA03265 1 20070818 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 308UA 23669 FLOOR EEL LIGHTS INOP FROM ROW 15 ON BACK. REPLACED LIGHT AT ROW 21, OPS CK GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007083100082 20070831 00082 NM 2007 8 31 2007UALA03266 1 20070818 A 3350 1317 A/C PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY EXIT CEILING LIGHT INOP AT ROW 6 RIGHT. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100083 20070831 00083 NM 2007 8 31 2007UALA03267 1 20070818 A 3350 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY EXIT CEILING LIGHTS INOP ROWS 48 THRU 61 RIGHT AND ROW 46 THRU 61 LEFT. 08-31-07 REPLACED BATTERY AT POWER SUPPLY M7928. LIGHTS OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100098 20070831 00098 NM 2007 8 31 2007UALA03282 1 20070820 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 CREASE BEAM CORRODED: LT PASS CABIN CREASE BEAM WEB CORRODED AT STA 727C+17 WL 208. REMOVED CORROSION. FABRICATED & I NSTALLED FILLER & REPAIR STRAP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007083100099 20070831 00099 NM 2007 8 31 2007UALA03283 1 20070820 A 5514 LUG BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU STABILIZER CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 LEFT STAB CORRODED: CENTER SECTION, REAR SPAR UPPER FWD, ATTACH CLEVIS HAS CORROSION. REMOVED BUSHING, SPOT FACED & RE AMED LUG TO REMOVED CORROSION. ROTO PEENED. FABRICATED OVERSIZE BUSHING, FPI AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007083100100 20070831 00100 NM 2007 8 31 2007UALA03284 1 20070820 A 5514 LUG BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZ STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 LEFT HORIZ STAB CORRODED: CENTER SECTION, REAR SPAR UPPER AFT CLEVIS HAS CORROSION. REMOVED BUSHING, REAMED LUG, ROTO PEENED TREAT & PRIME. FABRICATED OVERSIZE BUSHING, CAD PLATE, FPI AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007083100102 20070831 00102 EU 2007 8 31 07FDEA03100 1 20070824 A 5313 A53974202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 HEAVY CORROSION AT STR 50, FRAME 64 LHS. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007083100103 20070831 00103 EU 2007 8 31 07FDEA03101 1 20070824 A 5310 A53970707202 SHEAR PLATE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORRODED SHEAR PLATE ANGLE IN BILGE AREA FRAME 54.2-55/58, STRG.45 RT REPAIR PERFORMED BY REMOVING CORROSION AND REPLACE MENT OF ANGLE IAW SRM 51-52-10. 2 L 7 2 4F RT A35EU 2007083100106 20070831 00106 NM 2007 8 31 2007UALA03287 1 20070820 A 5514 LUG BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZ STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 LEFT HORIZ STAB CENTER SECTION FWD LOWER ATTACH CLEVIS AFT LUG HAS CORROSION ON AFT FACE. REMOVED BUSHING, SPOTFACED & REAMED LUG, HFEC, ROTO PEENED, TREAT & PRIMED. FAB OVERSIZED BUSHING, FPI , CAD PLATE & INSTALLED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007083100107 20070831 00107 NM 2007 8 31 2007UALA03288 1 20070820 A 5514 LUG BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZ STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 LEFT HORIZONTAL STAB CENTER SECTION FWD LWR ATTACH CLEVIS FWD LUG HAS CORROSION ON FWD FACE LIP OF BORE. REMOVED BUSHIN GS, SPOT FACED & REAMED LUG, HFEC, ROTO PEENED, TREAT & PRIMED. FAB OVERSIZED BUSHING, FPI, CAD PLATE & INSTALLED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007083100109 20070831 00109 EU 2007 8 31 07FDEA03104 1 20070824 A 5320 A53970707202 BRACKET AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CRACKED HYDRAULIC BRACKET AT FRAME 55/58-59 BETWEEN STRG 52-53 RT REPLACEMENT OF BRACKET IAW SRM 51-52-10. 2 L 7 2 4F RT A35EU 2007083100110 20070831 00110 EU 2007 8 31 07FDEA03106 1 20070824 A 5311 A53980044233 FRAME AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 DEFORMED FRAME CAP STRIP ON FRAME 74, STRG 26 RHS REPAIR PERFORMED BY INSTALLING NEW PARTS IN ZONE 170. 2 L 7 2 4F RT A35EU 2007083100111 20070831 00111 NM 2007 8 31 2007UALA03290 1 20070820 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 DENTS IN FRAME AT BS 1440, STR 25 AND 26L IN AFT PIT. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE, FABRICATED AND INSTAL LED REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007083100112 20070831 00112 NM 2007 8 31 2007UALA03291 1 20070820 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 DENT IN AFT PIT FRAME BS 1460, STR 26L. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007083100113 20070831 00113 NM 2007 8 31 2007UALA03293 1 20070821 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 DOOR 4R EMERGENCY EXIT SIGN LIGHT INOPERATIVE. 08-31-07 REPLACED BATTERY PACK, OP CHECKED OK REF MM 33051-04. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100114 20070831 00114 NM 2007 8 31 2007UALA03294 1 20070821 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 UPPER DECK RIGHT EXIT EMERGENCY EXIT LIGHT INOP. 08-31-07 REPLACED BATTERY PACK, OP CHECKED OK REF MM 33-51-04. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100115 20070831 00115 NM 2007 8 31 2007UALA03295 1 20070821 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY LIGHT INOPERATIVE AT 3A AFT. 08-31-07 REPLACED LAMP ASSY. OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100119 20070831 00119 NM 2007 8 31 2007UALA03299 1 20070820 A 3397 WIRE HARNESS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EEL LIGHT INOP AT SEAT 5F FWD LIGHT ASSY. 08-31-07 REPLACED THE HARNESS UNDER THE SEAT. EEL LIGHT CHECKED O K. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100120 20070831 00120 NM 2007 8 31 2007UALA03300 1 20070820 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY LIGHT INOP AT DOOR 1 LEFT BUSTLE LIGHT. 08-31-07 REPLACED THE LAMP. CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100121 20070831 00121 NM 2007 8 31 2007UALA03301 1 20070820 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EEL LIGHT INOP AT SEAT 4A AFT ASSEMBLY. REPLACED THE LAMP, CHECKED OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100122 20070831 00122 EU 2007 8 31 2007UALA03303 1 20070821 A 5270 DOOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO UNKNOWN A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 414UA 472 CARGO DOOR OPEN WARNING. MESSAGE RECURRED ON 'SOME' FOLLOWING FLIGHTS. REPLACED FLAP HANDLE SPRING, CLEANED PROX SENSOR S AND READJUSTED HANDLE FLAP LINKAGE. THIS ITEM HAS NOT REAPPEARED OR REPEATED SINCE AUG 21. 2 L 7 2 4F 4 F RT A28NM E40NE 2007083100123 20070831 00123 2007 8 31 2007UALA03305 4 20070821 A 2565 ASPIRATOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EVAC SLIDE LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 127UA 28813 ASPIRATOR LEAKS. ASPIRATOR HAS A CRACK IN IT. REPLACED ASPIRATOR. SLIDE OK FOR SERVICE. SLIDE PROBLEM ROOT CAUSE: S USPECT ASPIRATOR WAS CRUSHED DURING SLIDE ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100124 20070831 00124 2007 8 31 2007UALA03306 4 20070821 A 2565 DISC BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EVAC SLIDE RUPTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 912UA 25290 LOW BOTTLE PRESSURE. FOUND RUPTURED PRESSURE DISC. REPLACED DISC, RECHECKED FOR LEAKS, NO LEAKS FOUND. RESERVICED BO TTLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007083100125 20070831 00125 EU 2007 8 31 2007UALA03307 1 20070821 A 2497 BUSS BAR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ELECTRICAL SHORTED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 437UA 655 FLIGHT DIVERTED DUE TO ELECTRICAL ODOR. FOUND 1 PHASE OF CB 3XN2(B US 2SUPPLY 204XP)MISSING, CB 3XN2 POPPED WITH CAP BR OKEN. ALL USERS OF SOURCE 204XP POWER FAILED DOWNLINE. REPLACED CB 3XN2, AB2, BUS 2 204XP SUPPLY- INSPECTION FOR SHOR TS IN WIRING BETWEEN CB , 3 PHASE BUSS BAR 2XP & 42XU4 CONTACTOR. CHECKED A LL ASSOCIATED WIRING ON BUSS BAR AND 094005 ALL WIRING UNDER 123VU. NO DEFECTS NOTED 2 L 7 2 4F 4 F RT A28NM E40NE 2007083100128 20070831 00128 NM 2007 8 31 2007UALA03310 1 20070821 A 5210 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 DOOR 1L SKIN CRACKED: LT FWD ENTRY DOOR INNER SKIN AFT EDGE CRACKED AT STOP PIN CUTOUTS 6 & 7. MAJOR REPAIR ACCOMPLISH ED: INSTALLED DOUBLER ON INNER SKIN AT THE 6 & 7 CUTOUTS ON THE AFT SIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007083100129 20070831 00129 NM 2007 8 31 2007UALA03311 1 20070821 A 5210 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD ENTRY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 FWD ENTRY DOOR AFT FRAME CRACKED AT NR 6 & 7 STOPS. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR ANGLES AT 6 & 7 STOP F ITTINGS ON THE AFT FRAME. 2 L 7 2 4F 4 F RT A16WE E21EU 2007083100132 20070831 00132 NM 2007 8 31 2007UALA03314 1 20070822 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA 25158 CABIN -C- ZONE LEFT SIDE EEL DIM. REPLACED BATTERY PACK, OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100135 20070831 00135 EU 2007 8 31 07FDEA03107 1 20070824 A 5330 A53773487 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 DENTED AND SCRATCHED FUSELAGE SKIN BETWEEN FRAME 19-21, STRG 47-48 RHS. REPAIR PERFORMED BY BLEND OUT SCRATCHES PER SRM 53-10-12 AND IS IN LIMIT IAW. DIAGRAMM 111/112, NDT FOUND NO CRACKS. REPAIR IS COVERED BY EA 6-5313-101263. 2 L 7 2 4F RT A35EU 2007083100136 20070831 00136 NM 2007 8 31 2007UALA03318 1 20070821 A 5753 FLAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RT WING SCRATCHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 A 2.75 INCH SCRATCH RIGHT I/B MID FLAP. LOCATED JUST BEHIND I/B PUSHROD APPROX 4 INCHES I/B OF 2ND FLAP TRACKS. REPLA CED ASSY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007083100138 20070831 00138 EU 2007 8 31 07FDEA03109 1 20070824 A 5313 A53974202226 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT CARGO PIT, STR 54L CORRODED BETWEEN FR 58 AND FR61 (STA X3143 AND STA X3302) CUT OUT CORRODED SECTION OF STR 54L FRO M STA X3143 TO STA X3302. FABRICATED AND SPLICED IN REPAIR SECTION IAW A310-200 SRM 53-10-14 FIG 201, 51-21-10 AND 51-2 3-10. 2 L 7 2 4F RT A35EU 2007083100139 20070831 00139 NM 2007 8 31 2007UALA03319 1 20070822 A 2432 WARNING SYSTEM BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE APU BATTERY ACTIVATED A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 793UA 26946 BATTERY CHARGER AND APU BATTERY MESSAGES DISPLACED ON STATUS PAGE. REPLACED BATTERY AND CHARGER PER MM24-31-05 & MM24- 31-06. OP CHECKS READY FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007083100141 20070831 00141 WP 2007 8 31 IXXA07SMN213S 1 20070817 A 5753 SKIN DOUG DC8 DC873F 302199F WP LT WING TE FLAP DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, LT WING INNER FLAP, UPPER SKIN SHOWS DENT BETWEEN STA XF 112.000 TO STA XF 120.000. 2 L 7 4 4F RT 4A25 2007083100147 20070831 00147 WP 2007 8 31 IXXA07SMN206S 1 20070813 A 5510 BULKHEAD DOUG DC8 DC873F 302199F WP BS 1766 S9-10L CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, AFT BULKHEAD.-TEE CAP OF LT SIDE PRESS WALL UPPER PART BETWEEN L-9L AND L-10L, STA 17 66.000 SHOWS CRACK 1". 2 L 7 4 4F RT 4A25 2007083100150 20070831 00150 WP 2007 8 31 IXXA07SMN208S 1 20070813 A 5512 SKIN DOUG DC8 DC873F 302199F WP BS 97-103 DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, HORIZ STABILIZER EMPENNAGE INBD L/E EXT SKIN SHOWS (01EA) DENTS AT STA XFS 97.500 AND STA XFS 103.000. 2 L 7 4 4F RT 4A25 2007083100151 20070831 00151 NM 2007 8 31 2007UALA03323 1 20070822 A 5320 SUPPORT ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 THRESHOLD WEB SUPPORT ANGLE CORRODED: STA 847 RBL 19-26. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED SUPPORT ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007083100152 20070831 00152 WP 2007 8 31 IXXA07SMN209S 1 20070813 A 5522 SKIN DOUG DC8 DC873F 302199F WP RT ELEVATOR DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, RT ELEVATOR OIL CANNING LOWER PANEL, PLATING AT STA XE 279.000 STA XE 306.000. 2 L 7 4 4F RT 4A25 2007083100153 20070831 00153 NM 2007 8 31 2007UALA03324 1 20070822 A 5241 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU R1 GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 R1 FWD GALLEY DOOR CRACK: AFT LOWER CORNER AFT SIDE O/B FASTENER HOLE CRACKED. MAJOR REPAIR ACCOMPLISHED: REPLACED C RACKED FRAME. 2 L 7 2 4F 4 F RT A16WE E21EU 2007083100154 20070831 00154 WP 2007 8 31 IXXA07SMN215S 1 20070817 A 5551 FITTING DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, RT HORIZ STABILIZER FITTING SHOWS CRACK 2" FRONT PART AT STA NFS 60.000. 2 L 7 4 4F RT 4A25 2007083100158 20070831 00158 NM 2007 8 31 2007UALA03327 1 20070822 A 5330 BEAR STRAP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA 25158 FOUND AFT CARGO DOOR CUTOUT FWD UPPER CORNER SKIN 7 BEARSTRAP CRACKED. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER ST ACK-UP PER SRM 53-60-01 REPAIR 3. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100161 20070831 00161 NM 2007 8 31 2007UALA03329 1 20070822 A 5230 STRUCTURE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE AFT CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA 25158 DURING REPAIR INSTALLATION AT AFT CARGO DOOR FWD UPPER CORNER, BRACKET FLANGE AT STR 27 INTERFERES WITH HI-LOK INSTALLAT ION. MAJOR REPAIR ACCOMPLISHED: TRIMMED BRACKET FLANGE & INSTALLED REINFORCING ANGLE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100164 20070831 00164 NM 2007 8 31 2007UALA03330 1 20070822 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 EXTERNAL FUSELAGE STA 1197+110 BETWEEN STR 39R AND 38L SKIN DENTED INSIDE OUT. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMA GE. HFEC INSPECTION TO VERIFY DAMAGE REMOVAL. NO CRACKS FOUND. FABRICATED & INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2007083100166 20070831 00166 NM 2007 8 31 2007UALA03331 1 20070822 A 5320 ATTACH BRACKET BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 FLOORBEAM INTERCOSTAL ATTACH BRACKET CRACKED AT STA 303, BL 0. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKED ANGLE. FABR ICATED & INSTALLED NEW ANGLE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007083100172 20070831 00172 NM 2007 8 31 2007UALA03333 1 20070822 A 5320 STIFFENER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 FLOORBEAM STA 246 VERTICAL STIFFENER CRACKED AT RBL 12 FWD SIDE. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKED STIFFENER. LOCATED, DRILLED & INSTALLED NEW STIFFENER. 2 L 7 2 4F 4 F RT A1NM E24NE 2007083100174 20070831 00174 NM 2007 8 31 2007UALA03334 1 20070822 A 5320 STIFFENER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 FLOORBEAM STA 246 VERTICAL STIFFENER CRACKED AT RBL 26 FWD SIDE. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKED STIFFENER. INSTALLED NEW STIFFENER. 2 L 7 2 4F 4 F RT A1NM E24NE 2007083100180 20070831 00180 NM 2007 8 31 2007UALA03336 1 20070822 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 674UA 29242 FWD GALLEY EEL STRIP IS INOPERATIVE. REPLACED EEL STRIP. CHECKS OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007083100185 20070831 00185 NM 2007 8 31 2007UALA03338 1 20070821 A 2400 CIRCUIT CARD BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SPEED CONTROL FAILED A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 768UA 26919 HYD PUMP DEM C1 MESSAGE. ACP FAILED GROUND TEST. REPLACED C1 LOGIC SPEED CONTROL CARD AND OPS TEST OK IAW AMM 29-11-1 5. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007083100186 20070831 00186 SO 2007 8 31 RAIA00708040 1 20070823 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 813HK 145044 PRE FLT 5488-IAD- RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE RESEATED THE CONNECTOR FOR THE SUBJECT L IGHT ASSEMBLY. 2 L 7 2 4T RT T00011AT 2007083100201 20070831 00201 NM 2007 8 31 UIEA200700300 1 20070726 A 5320 THRESHOLD BOEING 747 747271C 1384869 NM ZONE 200 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 CORROSION ON RIGHT AFT LOWER CORNER CUTOUT INNER SURFACE MED NR 3. REMOVED CORROSION AND BLENDED AREA20:1 MIN REMAINING MATERIAL .222". REMOVED CORNER DOUBLER. INSTALLED NEW DOUBLER. INSTALLED NEW THRESHOLD IAW SRM 51-10-01, 51-30-02, 5 1-30-04 BOEING MESSAGE NR 1-383704990-2. 2 L 7 4 4F A20WE 2007083100202 20070831 00202 SO 2007 8 31 RAIA00708036 1 20070821 A 3610 CLAMP EMB 145 EMB145EP 3260221 SO A/C BAY LOOSE A RAIA B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 827HK 145021 FLT 5535 - BNA - AIRCRAFT EXPERIENCED A RAPID DEPRESSURIZATION DURING FLIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND FO UND THAT THE BLEED DUCT TO THE MIXER/CONDITIONER HAD COME OFF. DUCT WAS RE-INSTALLED AND SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2007083100203 20070831 00203 NM 2007 8 31 UIEA200700301 1 20070726 A 5320 THRESHOLD BOEING 747 747271C 1384869 NM ZONE 200 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 CRACK NOTED AT SKIN 1.75" IN LENGTH. CRACK NOTED IN BEARSTRAP AT SAME LOCATION 1.75" IN LENGTH. CRACK TERMINATES AT FA STENER HOLE. REMOVED EXISTING DOUBLER AT CRACK TERMINATION HOLE. REAMED HOLE .100 OVERSIZED. FABRICATED AND INSTALLED FREEZE PLUG DRILLED UP AND INSTALLED LARGE STEEL DOUBLER WHICH IS PART OF KIT NR 65B25848-9 ALONG WITH NEW STAINLESS ST EEL THRESHOLD THEN REINSTALLED ALL PARTS IAW SB 747-53A2552. 2 L 7 4 4F A20WE 2007083100204 20070831 00204 NM 2007 8 31 SWAA074170 1 20070823 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 465WN 33829 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007083100206 20070831 00206 NM 2007 8 31 UIEA200700302 1 20070727 A 5330 65B15410603 SKIN BOEING 747 747271C 1384869 NM BS 1250 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 CORROSION LEFT FWD UPPER CORNER CUTOUT INNER SURFACE MED NR 3L. REMOVED CORROSION ON INNER SURFACE OF L-3 DOOR CUTOUT I AW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW BOEING MSG SR-1384850927-4. FABRICATED REPLACEMENT TAB FROM .080 2 024-T3 PER SAME BOEING MESSAGE. REPLACED SKIN WITH P/N 65B15410-603 IAW BOEING MESSAGE NUMBER SR-1-38450927-2. 2 L 7 4 4F A20WE 2007083100207 20070831 00207 NM 2007 8 31 UIEA200700303 1 20070727 A 5320 WEB BOEING 747 747271C 1384869 NM CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 .50 LENGTH HORIZONTAL CRACK RIGHT SIDE PANEL/WEB AT WL 170 STA 313 NOSE WHEEL WELL AREA. ACCOMPLISHED NOSE WHEEL WELL R EPAIR AT WL 170 FROM STA 309 TO 317 IAW SRM 53-10-04. 2 L 7 4 4F A20WE 2007083100209 20070831 00209 NM 2007 8 31 SWAA074181 1 20070823 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 793SA 27888 EEPLS COVER LOOSE AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007083100210 20070831 00210 NM 2007 8 31 SWAA074164 1 20070823 A 3350 417A5703 CAP BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 214WN 32486 EEPLS END CAP MISSING AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007082900076 20070829 00076 SO 2007 8 29 C2XA07SH045 1 20070815 A 5751 14573900419 SHROUD EMB 145 EMB145LR 3260212 SO LT AILERON DEBONDED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26545 145558 SHV - DURING C-CHECK MAINTENANCE FOUND LEFT LWR AILERON SHROUD WITH BAD BONDING ON OUTBOARD END. MAINTENANCE REPAIRED L EFT LWR AILERON SHROUD IAW EC 5750-01315 REV D. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007082900080 20070829 00080 SO 2007 8 29 C2XA07TY044 1 20070817 A 5342 MS2113406020 ATTACH FITTING EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14959 145091 TYS - DURING A CURRENT C-CHECK INSPECTION, THE VERTICAL STAB ATTACH FITTING AT FRAME 75 WAS FOUND FRETTING. MAINTENANCE REMOVED AND REPLACED THE VERTICAL STAB FITTING AT FRAME 75 IAW EC5310-01317. ALL WORK WAS ACCOMPLISHED AND WILL BE REL EASED AT THE END OF THE CHECK. 2 L 7 2 4T RT T00011AT 2007082900085 20070829 00085 NM 2007 8 29 ASAA0741979 1 20070817 A 5753 6546430189 SKIN BOEING 737 737490 1384715 NM FORE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 LEFT INBOARD FORE FLAP UPPER CAMBER HAS APPROX 12 X 15 INCHES DENT AT RSS 264 276. REPAIRED FLAP IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007082900087 20070829 00087 EU 2007 8 29 ASAA0741980 2 20070819 A 7200 LUBRICATION BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU NR 2 ENGINE ODOR A ASAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 02 765AS 25102 ODOR IN COCKPIT, FLT ATTENDANTS REPORTED ODOR AND HAZE IN FWD GALLEY PAX PORTION AND IN AFT GALLEY. FAN LUB ACCOMPLISHE D ON NR 2 ENG JUST PRIOR TO THIS FLIGHT. FOUND RESIDUAL LUBE MATERIAL ON FAN BLADES BOOSTER COMP AND IGV'S. CLEANED OF F EXCESS LUBRICANT. ACCOMPLISHED CABIN ODOR TROUBLESHOOTING PER ASA MM 05-60-00 AND BURN OUT PROCEDURE PER AMM 21 00 01 . 2 L 7 2 4F 4 F RT A16WE E21EU 2007082900092 20070829 00092 EU 2007 8 29 07FDEA02872 1 20070814 A 7830 32142368 SHUTOFF VALVE AIRBUS 310 A310222 3930315 EU THRUST REVERSER INOPERATIVE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 449FE 217 AFTER LIFTOFF(KATL) ENG1 THRUST REVERSER SHOWED "UNLOCKED". ON T/O ROLL, LIGHT FLICKERED MOMENTARILY THEN WENT OUT. FOLLOWED QRH AND ECAM PROC AND DECLARED EMERGENCY MEL 14AUG07. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGOR Y: C EXP: 17AUG07 "MEL 78-30-01-C: ENGINE (IDENTIFY 1 OR 2) 1 THRUST REVERSER, INOP. THRUST REV IS DEACT IN FWD THRUST POSITION." REPLACED NR 1 THRUST REVERSER PRESSURE REGULATOR/SHUTOFF VALVE PER A310-200 AMM 78-31-05-4 03 AND VALVE CO NNECTOR DH9 PER AIRBUS ESPM. NR 1 REVESER OPS CHECKS GOOD. 2 L 7 2 4F RT A35EU 2007082900093 20070829 00093 NM 2007 8 29 UPS07650456 1 20070816 A 3020 ANTI-ICE VALVE BOEING 767 76734AF 1385212 NM RT ENGINE MALFUNCTIONED A IPXA K NONE J WARNING INDICATION UK UNKNOWN 1 SO 01 309UP 27740 INSPECTION TYPE:ETOP EICAS MESSAGE RIGHT ENGINE ANTI-ICE DISPLAYED AND VALVE LIGHT REMAINED ILLUMINATED WITH SWITCH ON. EXTINGUISHED WHEN POWER INCREASED AFTER SEVERAL ATTEMPTS. REMOVED AND REPLACED RIGHT ANTI-ICE VALVE, OPS CHECK GOOD PE R 30-21-03-0. 2 L 7 2 4F RT A1NM 2007082900096 20070829 00096 WP 2007 8 29 UPS07850463 1 20070806 A 5240 WEB DOUG DC8 DC873F 302199F WP SERVICE DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 HOLE DRILLED THROUGH FASTENER AND INTO FWD CENTER WEB OF RIGHT FWD SERVICE DOOR INTERIOR. CUT OUT DA MAGED AREA FROM CENTER WEB ON RIGHT FWD SERVICE DOOR IAW SRM 52-02-00 FIG 4. FABRICATED AND INSTALLED REPAIR DOUBLER ON CENTER WEB OF THE RIGHT FWD SERVICE DOOR IAW SRM 52-03-01 FIG 3 AND SRM 52-02-00 FIG 4. 2 L 7 4 4F RT 4A25 2007082900108 20070829 00108 CE 2007 8 29 S2YA07004 1 20070429 A 5711 SPAR CAP BEECH 1900 1900D 1154162 CE RT WING CRACKED A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 85SK UE85 ON 04/29/07 DURING INSPECTION REQUIRED BY AD 2006-18-51 SKYWAY MAINTENANCE FOUND A CRACK ON RIGHT WING AFT SPAR, LOWER S PAR CAP AFT FLANGE AT WING STATION 117 INCHES. THE CRACK RAN FROM THE AFT EDGE TO A RIVET HOLE. THE DAMAGE WAS REPAIRE D IAW RAYTHEON AIRCRAFT CO. RDO FIELD REPAIR FR-CO-01527 BY EMERY AIR IN ROCKFORD AND AN FAA FORM 337 WAS FILLED OUT ON 05/07/07. 2 L 7 2 4T RT A24CE 2007082900110 20070829 00110 CE 2007 8 29 106CG081707 1 20070817 A 2197 MS3106R10SL3S CONNECTOR BEECH MU300 400BEECH CE CABIN PRESSURE SEPARATED E UVCA B EMER. DESCENT O OTHER CR CRUISE 1 CE 03 106CG 6202 108 RJ12 PRESSURIZATION WENT TO EMERGENCY CONFIGURATION AT 41,000 FLIGHT LEVEL. CREW PERFORMED AN DESCENT TO 13,000 FT AND PROCE EDED TO DESTINATION WITH NO OTHER PROBLEMS. 2 H 7 2 4F RT A16SW 2007082900112 20070829 00112 CE 2007 8 29 ERAA200700003 1 20070817 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE CABIN ODOR A ERAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 AL 03 972EA UE389 STRONG BURNING SMELL AT FL190 AND LIGHT SMOKE OBSERVED BY CREW & PAX. RETURNED TO ANC. VISUALLY INSPECTED WIRING & CON NECTIONS AT WINDSHIELD PANELS, CB PANELS, OVERHEAD SWITCH PANELS. NO DEFECTS NOTED. UNABLE TO DUPLICATE DISCREPANCY AT EXTENSIVE GROUND RUN SIMULATING FLIGHT CONDITIONS. A/C DISPATCHED FOR OPERATIONAL TEST FLT ONLY. 2 L 7 2 4T RT A24CE 2007082900117 20070829 00117 NM 2007 8 29 KCSA071322 1 20070821 A 5313 STRINGER BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 FUSELAGE STR 39L CORRODED BETWEEN BS 660 AND 680. 2 L 7 4 4F RT A20WE 2007082900121 20070829 00121 EA 2007 8 29 TRAX200701200 1 20070816 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 752EV 10166 SEVERAL LEFT SIDE SEAT RAILS HAVE MINOR CORROSION FS 379.00 TO FS 977.00. REMOVED CORROSION FROM SEAT RAILS FROM VARIOU S SPOTS BETWEEN LEFT FS 379.00 TO FS 977.00. BRUSHED REWORKED AREAS WITH ALODINE. ALL DIMENSIONS WITHIN ALLOWABLE LIMI TS. EACH REWORKED SEAT RAIL IDENTIFIED WITH THE WORDS REO 670-53-00-013. ALL WORK DONE IN REFERENCE TO CRJ 700 SRM 53-21-49. ALL WORK DONE IAW CRJ 700 SRM 51-12-00, 51-21-06, 51-21-16, AND 53-21-49. JOB COMPLETE. SUPPLEMENTAL - SDR CLOSED 08/21/07. 2 L 7 2 4F RT A21EA 2007082900143 20070829 00143 WP 2007 8 29 ABXA070262 1 20070815 A 5311 99578605 FRAME DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 WHILE COMPLYING WITH EA 53300036, FOUND CRACKED FRAME, REF AD 2002-21-09. REPLACED FRAME IAW DC9 SRM 51-30-02 AND 51-30 -05. 2 L 7 2 4F A6WE 2007082900145 20070829 00145 EA 2007 8 29 TRAX200701195 1 20070816 A 5320 BEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 752EV 10166 LEFT FS 280 TRANSVERSE BEAM CORRODED. WORK ACCOMPLISHED IAW REO 670-53-11-052. SUPPLEMENTAL - SDR CLOSED 08/22/07. 2 L 7 2 4F RT A21EA 2007082900158 20070829 00158 WP 2007 8 29 ASAA0781992 1 20070817 A 5230 5910419 DOOR FRAME DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 943AS 53018 AFT CARGO BAY DOOR FRAME CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 52-05. 2 L 7 2 4F RT A6WE 2007082900162 20070829 00162 2007 8 29 UPS07250476 4 20070817 A 2565 SLIDE BOEING 727 727185C 138406N NM EMERGENCY EXIT OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE:N/A CREW ENTRY ESCAPE SLIDE FELL OUT OF CASE. REPLACED ESCAPE SLIDE AS NEEDED. OKAY FOR SERVICE REF MM 25-60-14-2. 2 L 7 3 4F A3WE 2007082900164 20070829 00164 NM 2007 8 29 UPS07650468 1 20070819 A 5247 WARNING SYSTEM BOEING 767 76734AF 1385212 NM APU DOOR MALFUNCTIONED A IPXA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 332UP 32843 INSPECTION TYPE:ETOP BTB - APU DOOR STATUS MESSAGE ILLUMINATED ON TAXI M356945. DMP 49-15-1-2 RESET, DMI M356945 CLOSED . 2 L 7 2 4F RT A1NM 2007082900169 20070829 00169 WP 2007 8 29 UPS07850474 1 20070724 A 5320 SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 L36 SPLICE BETWEEN STA 1260 AND 1280 CRACKED. REMOVED AND REPLACED FITTING IAW SAA EA 008-5310-01-A0 987. 2 L 7 4 4F RT 4A25 2007082900173 20070829 00173 NM 2007 8 29 PIDA07041 1 20070816 A 3350 POWER SUPPLY BOEING 737 737228 13844AG NM CABIN DISCHARGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 252TR 23001 EMERGENCY EXIT LIGHT - CENTER AISLE STATION 617 IS INOP. REMOVED AND REPLACED POWER SUPPLY. SYSTEM OPS CHECKS GOOD IAW B737 M/M 33-51. 2 L 7 2 4F RT A16WE 2007082900176 20070829 00176 EU 2007 8 29 SA07052 1 20070820 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU CABIN FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 753US 15336 1326 CLT - AFT L EPSU BATTERY FAULT DURING EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED AFT L EMERGENCY POWER SUPPLY UNIT. O PERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007082900185 20070829 00185 NM 2007 8 29 ABXA070272 1 20070724 A 5230 140T26033 BEAM BOEING 767 767232 1385132 NM CARGO DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 739AX 22216 FORWARD LOWER CARGO DOOR BEAM WAS CORRODED AROUND FORWARD 3 NUT PLATES. REMOVED AND REPLACED BEAM IAW B767 SRM 51-40-1. 2 L 7 2 4F RT A1NM 2007082900198 20070829 00198 EA 2007 8 29 TRAX200701232 1 20070823 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 390CA 10106 LEFT EXTERNAL, 2ND FROM AFT, EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007082900206 20070829 00206 NM 2007 8 29 SWAA074147 1 20070822 A 2121 215201 GASPER FAN BOEING 737 7377H4 1384404 NM E&E BAY MALFUNCTIONED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 775SW 30590 ELECTRICAL SMELL EMITTING FROM GASPER VENTS. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2007082900222 20070829 00222 NM 2007 8 29 SWAA074159 1 20070822 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007082900224 20070829 00224 NM 2007 8 29 SWAA074157 1 20070822 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 18R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007083000009 20070830 00009 CE 2007 8 30 DXTA200702407 1 20070815 A 2760 UNKNOWN BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE SPEED BRAKES UNKNOWN E DXTA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 07 140QS RK406 DURING DESCENT WHEN SPEED BRAKES WERE EXTENDED, THE AIRPLANE ROLLED TO THE RT. WHEN THE SPEED BRAKES WERE EXTENDED IN L EVEL FLIGHT, NO ROLL CHANGES WERE NOTED. C/W SPEED BRAKE SYSTEMS, OPS CHECKS. CHECKED RIGGING & CABLE TENSIONS ALL CHEC KS GOOD. IAW 400XP MM 27-60-00 2 H 7 2 4F 4 F RT A16SW E25EA 2007083000021 20070830 00021 NM 2007 8 30 07FDEA03123 1 20070825 A 5753 SKATE ANGLE BOEING 727 727233 138408A NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LT WING IB TE NR 3 FLAP TRACK FWD FRG IB SKATE ANGLE IS CRACKED AT 2 WING SKIN FASTENERS WBL 199, 3" FWD AND AFT OF SPAR . REPAIRED NR 3 FLAP TRACK SKATE ANGLE IAW B 272-200 SRM 51-40-3 AND 51-30-2. ALL LEAK CK'S GOOD. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007083100018 20070831 00018 NM 2007 8 31 MWEA070187 1 20070822 A 7931 42D1091A PRESSURE SWITCH DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE ENGINE MALFUNCTIONED A MWEA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 13 601ME 49762 OIL STRAINER CLOGGING LIGHT CAME ON, OIL TEMPERATURE WENT TO 120 THEN DECREASED OIL PRESSURE AT 45 EPR. REMOVED AND REP LACED OIL DIFFERENTIAL PRESSURE SWITCH. 2 L 7 2 4F 4 F RT A6WE E9NE 2007083100024 20070831 00024 NM 2007 8 31 SB07071 1 20070822 A 3234 A42006028305 SOLENOID BOEING 737 7373B7 1384580 NM COCKPIT FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 506AU 23381 CLT - AFTER TAKEOFF FROM CLT, DURING GEAR RETRACTION FROM UP TO OFF, CREW RECEIVED TWO MAIN LANDING GEAR RED LIGHTS AND A LEFT MAIN LANDING GEAR GREEN LIGHT. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR LEVER LATCH SOLENOID. ALSO, REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPLO CK ACTUATOR PER MM 32-32-41-4. PERFORMED RETRACTION TEST PER MM 32-32-00-501. OPERATIONAL TEST GOOD. 2 L 7 2 4F RT A16WE 2007083100038 20070831 00038 WP 2007 8 31 070150 1 20070816 A 7711 PROBE DOUG DC9 DC983 3022083 WP PT 2 OBSTRUCTED A WX0A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 19 893GA 53051 DURING TAKEOFF ROLL, NORMAL ENGINE SPOOL TO 1.4 EPR AND AUTO THROTTLE ENGAGED. LEFT ENGINE EPR FLUCTUATED AND DISENGAGED AUTO THROTTLES. LEFT EPR CONTINUED TO FLUCTUATE 1.0 TO 2.4. DISCONTINUED TAKEOFF AND AIRCRAFT RETURNED TO THE GATE. MA INTENANCE DEPARTMENT PERSONNEL INSPECTED AND FOUND PT2 PROBE OBSTRUCTED WITH DEBRIS, CLEARED OBSTRUCTION IAW M/M 73-11-0 3 AND PERFORMED GROUND OPERATIONAL CHECK IAW 71-00-00. OPERATIONAL CHECK NORMAL, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007083100040 20070831 00040 WP 2007 8 31 UPS07850483 1 20070806 A 5311 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 STA 1060 FRAME FITTING IS GOUGED. REMOVED FRAME FITTING AT STA 1060 IAW SRM 51-3-0. LOCATED, DRILLE D UP AND INSTALLED NEW FRAME FITTING AT STA 1060 IAW SRM 51-03-02 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007083100085 20070831 00085 NM 2007 8 31 2007UALA03269 1 20070820 A 3397 CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN CUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA 25158 SEAT EEL CABLE CUT AT SEAT 39HJK. 08-31-07 REPLACED CONNECTOR, OP CHECKED OK . 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100086 20070831 00086 NM 2007 8 31 2007UALA03270 1 20070820 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 GALLEY G1A LEFT SIDE, EEL INOP. 08-31-07 REPLACED EEL CABLE, OP CHECKED OK 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100089 20070831 00089 NM 2007 8 31 2007UALA03273 1 20070820 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 LEFT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP, 3RD FROM FWD LIGHT ASSY. 08-31-07 REPLACED LIGHT ASSY. OPS. CK. NOR MAL 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100090 20070831 00090 NM 2007 8 31 2007UALA03274 1 20070819 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EEL 4J AFT & 39 LEFT ARE INOPERATIVE. RELAMPED EEL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100091 20070831 00091 NM 2007 8 31 2007UALA03275 1 20070819 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY CEILING LIGHT INOP ROW 13. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100092 20070831 00092 NM 2007 8 31 2007UALA03276 1 20070819 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EEL 33 LEFT INOP. 08-31-07 SECURED CONNECTOR TO LAMP. OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100095 20070831 00095 NM 2007 8 31 2007UALA03279 1 20070820 A 2751 INDICATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 659UA 27114 FLAP INDICATOR NEEDLES OUT OF LIMITS FOR FLAPS 5, 15 & 20. CHECKED FLAP POSITION TRANSMITTER NR 1 AND NR 8 RIGGING FOU ND OK. CLEANED TRANSMITTER CANNON PLUGS. EXTENDED AND RETRACTED FLAPS SEVERAL TIMES USING NORMAL AND ALTERNATE MODES. B OTH IND. NEEDLES FOLLOWING THE RELATED FLAP LEVER DETENT POSITION WITHOUT DISAGREE. UNABLE TO DUPLICATE PROBLEM. 2 L 7 2 4F 4 F RT A1NM E24NE 2007083100096 20070831 00096 NM 2007 8 31 2007UALA03280 1 20070820 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 773UA 26929 AFT PROX EEL LIGHT AT SEAT 3F IS INOP. 08-31-07 REPLACED LIGHT ASSY. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007083100105 20070831 00105 NM 2007 8 31 2007UALA03286 1 20070820 A 5514 LUG BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU STABILIZER CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 LEFT STAB CORRODED: CENTER SECTION, REAR SPAR, AFT LOWER CLEVIS HAS CORROSION. REMOVED BUSHINGS FWD & AFT LUGS. SPOT FACE FWD FACE OF AFT LUG. REAMED FWD AND AFT BORES, HFEC, ROTO PEENED, TREAT & PRIMED. FAB OVERSIZED BUSHINGS, FPI, CA D PLATE AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007083100117 20070831 00117 NM 2007 8 31 2007UALA03297 1 20070820 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EEL LIGHT INOP AT SEAT 4E FWD LIGHT ASSY. REPLACED THE LAMP, CHECKED OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100130 20070831 00130 NM 2007 8 31 2007UALA03312 1 20070821 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 CREASE BEAM CORRODED: RT SIDE 1 INCH - 3 INCHES FWD OF STA 727E WL 208.5 STR 17R. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED CREASE BEAM WEB FROM STA 727D TO 727E RT SIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007083100131 20070831 00131 NM 2007 8 31 2007UALA03313 1 20070821 A 2432 WARNING SYSTEM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE APU BATTERY ACTIVATED A UALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 117UA 28810 TAXI INBOUND APU BATTERY STATUS MESSAGE. REPLACED APU BATTERY AND APU BATTERY CHARGER, CHARGING SYSTEM GROUND OPS NOR MALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100140 20070831 00140 NM 2007 8 31 2007UALA03320 1 20070822 A 7830 CONTROL MODULE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE THRUST REVERSER MALFUNCTIONED A UALA O OTHER J K WARNING INDICATION FLUID LOSS NR NOT REPORTED 1 WP 29 506UA 24627 EMERGENCY DECLARED DUE TO LOW QUANTITY ON THE LEFT HYDRAULIC SYSTEM FLUID LEVEL. SERVICED RIGHT HYDRAULIC SYSTEM TO FU LL AND NO LEAKS FOUND. FOUND CRACK IN NR 1 ENGINE THRUST REVERSER CONTROL MODULE. REPLACED DIRECTIONAL FLOW CONTROL VA LVE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007083100142 20070831 00142 WP 2007 8 31 IXXA07SMN219S 1 20070817 A 5711 SPAR DOUG DC8 DC873F 302199F WP RT WING CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, NR 1 MAIN TANK, CTR SPAR LWR CAP, CRACKED 3" AT STA XRS 255.000 BETWEEN S-61 AND S-62 . 2 L 7 4 4F RT 4A25 2007083100148 20070831 00148 WP 2007 8 31 IXXA07SMN207S 1 20070813 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 180 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, FWD BELLY PIT UPPER FLANGE OF FLOORBEAM, CRACKED AT STA BS 180.000, RBL 46". 2 L 7 4 4F RT 4A25 2007083100208 20070831 00208 NM 2007 8 31 SWAA074165 1 20070823 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 RIGHT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007083100211 20070831 00211 NM 2007 8 31 UIEA200700304 1 20070727 A 5343 TRUNNION BOEING 747 747271C 1384869 NM BS 1480 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 LEFT BODY GEAR INBOARD TRUNNION FITTING HAS CORROSION AROUND THE UPPER FACE OF 3 BOLT HOLES (INBOARD FWD, OUTBOARD FWD, AND OUTBOARD AFT). LOCALLY BLENDED OUT ALL PITTING CORROSION AREAS. HFEC AND 10X VISUAL INSPECTION PLUS DYE PENETRANT INSPECTION ACCOMPLISHED. SPOT FACED WASHER BEARING SURFACE AREA. HFEC AND 10X VISUAL INSPECTION OF BOLT HOLES ACCOMPLI SHED, FLAP PEENED REWORKED AREA. TREATED AND PRIMED AREA. AREA WITH IN LIMITS PER BOEING MESSAGE NR 1-381511269. 2 L 7 4 4F A20WE 2007083100212 20070831 00212 NM 2007 8 31 UIEA200700305 1 20070727 A 5511 SPAR CAP BOEING 747 747271C 1384869 NM HORIZONTAL STAB DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 HORIZONTAL STAB RT UPPER AFT DAMAGED HOLE AT RT VERTICAL SPAR CAP. INBD OF RBL 43.5 INBD UPPER AND LOWER FASTENER HOLE (CENTER SECTION) WAS NOTED DURING OPEN HOLE HFEC INSPECTION (NDT). COULD NOT ACQUIRE GOOD HFEC INDICATION DUE TO HOLE D AMAGE. REAMED DAMAGED HOLES TO 2ND OVERSIZE (.403-.406) IAW SB 747-55A2050 NDT FINDS NO DEFECTS BOLTS INSTALLED ON CARD 8010 / 8011. 2 L 7 4 4F A20WE 2007083100213 20070831 00213 NM 2007 8 31 UIEA200700306 1 20070727 A 5510 SPLICE PLATE BOEING 747 747271C 1384869 NM ZONE 300 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 HORIZONTAL STAB UPPER AFT CRACK INDICATION HOLE/HOLE DAMAGE AT LT SPLICE PLATE UPPER PLATE UPPER INBOARD OF LBL 45.3. AF T OF T/E AFT OUTBOARD FASTENER HOLE (CENTER SECTION). WAS NOTED DURING OPEN HOLE HFEC (NDT) COULD NOT ACQUIRE GOOD HFEC INDICATION DUE TO DAMAGED HOLE. REAMED DAMAGED HOLE TO FIRST OVERSIZE (.388-.391) IAW SB 747-55A2050. NDT FINDS NO DE FECTS. BOLTS INSTALLED ON CARD 8010 / 8011. 2 L 7 4 4F A20WE 2007083100214 20070831 00214 NM 2007 8 31 UIEA200700307 1 20070727 A 5511 SPAR CAP BOEING 747 747271C 1384869 NM ZONE 300 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 HORIZONTAL STAB RT AFT CRACK INDICATION/HOLE DAMAGED AT RT HORIZ SPAR CAP INBD OF 43.5 O/B AFT HOLE. REAMED DAMAGED HOL E TO FIRST OVERSIZE (.450-.453) IAW SB 747-55A2050. NDT FINDS NO DEFECTS. BOLTS INSTALLED ON CARD 8010 / 8011. 2 L 7 4 4F A20WE 2007083100215 20070831 00215 NM 2007 8 31 UIEA200700308 1 20070727 A 5511 SPAR CAP BOEING 747 747271C 1384869 NM ZONE 300 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 HORIZONTAL STAB RT AFT CRACK INDICATION/HOLE DAMAGED AT RT HORIZ SPAR CAP INBD OF 43.5 INBD AFT HOLE. REAMED DAMAGED HO LE TO FIRST OVERSIZE (.450-.453) IAW SB 747-55A2050. NDT FINDS NO DEFECTS. BOLTS INSTALLED ON CARD 8010 / 8011. 2 L 7 4 4F A20WE 2007083100216 20070831 00216 NM 2007 8 31 UIEA200700309 1 20070727 A 5511 SPAR CAP BOEING 747 747271C 1384869 NM ZONE 300 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 HORIZONTAL STAB RT AFT CRACK INDICATION/HOLE DAMAGED AT RT HORIZ SPAR CAP RT SIDE OTBD OF 43.5 INBD FWD HOLE. REAMED DA MAGED HOLE TO FIRST OVERSIZE (.450-.453) IAW SB 747-55A2050. NDT FINDS NO DEFECTS. BOLTS INSTALLED ON CARD 8010 / 8011 . 2 L 7 4 4F A20WE 2007083100217 20070831 00217 NM 2007 8 31 UIEA200700322 1 20070817 A 5320 WEB BOEING 747 747243B 1384830 NM ZONE 100 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 AFT CARGO COMPARTMENT FLOOR WEB STA 1900 LBL 49 HAS SMALL CRACK. DAMAGED AREA OF WEB CUT OUT AND DOUBLER INSTALLED IAW SRM 53-10-04 FIG 71. 2 L 7 4 4F A20WE 2007083100218 20070831 00218 2007 8 31 SWAA074172 4 20070823 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 465WN 33829 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007083100219 20070831 00219 2007 8 31 SWAA074171 4 20070823 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 465WN 33829 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007083100222 20070831 00222 NM 2007 8 31 UIEA200700324 1 20070824 A 5730 SKIN BOEING 747 747228F 1384895 NM ZONE 500 DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 LT WING UPPER SURFACE TRAILING EDGE FIXED PANEL AT STATION 1224 HAS AN AREA OF 2.0 INCH LONG BY 15.0 INCH WIDE AREA OF D ELAMINATION. PERMANENT REPAIR OF AREA WAS ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 2, SHEETS 4 & 5. 2 L 7 4 4F A20WE 2007083100223 20070831 00223 NM 2007 8 31 UIEA200700317 1 20070814 A 5754 STRUCTURE BOEING 747 7472D7B 1384803 NM KRUGER FLAP DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 527MC 22471 ON WALK AROUND FOUND NR 12 L/E KRUGER FLAP DAMAGED. PERFORMED INTERIM REPAIR IAW XEO 57-081307. PERM REPAIR TO BE ACCO MPLISHED AT NEXT "A' CHECK 20 AUG 07. 2 L 7 4 4F RT A20WE 2007083100224 20070831 00224 NM 2007 8 31 UIEA200700312 1 20070801 A 8011 38402251 STARTER BOEING 747 747341 13848AM NM NR 2 ENGINE FAILED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 BLOCK TURN BACK, NR 2 ENGINE STARTER WOULD NOT GIVE INDICATION OF ROTATION. THE PYLON BLEED VALVE AND STARTER VALVE LIG HT WERE ON. REPLACED STARTER, OPS CHECKED OKAY. 2 L 7 4 4F RT A20WE 2007083100225 20070831 00225 NM 2007 8 31 UIEA200700319 1 20070814 A 5347 SEAT TRACK BOEING 747 74747UF 1384812 NM BS 1550 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 412MC 30559 MAIN DECK CARGO CTR PALLET LOCK AT STA 1550 UNABLE TO USE LOCK IN POSITION UNTIL FLOOR AND SEAT TRACK REPAIR. SEAT TRAC K REPAIRED AT STA 1550 RBL 10 IAW SRM 53-00-52 AND XEO 53-081107-1 AND FLOOR BOARD AT STA 1550 RBL REPAIRED PER SRM 51-7 0-07. 2 L 7 4 4F RT A20WE 2007083100226 20070831 00226 NM 2007 8 31 UIEA200700318 1 20070814 A 5347 SEAT TRACK BOEING 747 74747UF 1384812 NM ZONE 500 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 412MC 30559 LWR AFT CARGO COMPARTMENT SEAT TRACK CROWN DAMAGED AT STA 1880 RBL 25. DAMAGED SEAT TRACK SECTION REMOVED AND REPLACED PER SRM 53-00-53 REPAIR NR 7 AND 10 AND XEO 53-081107. 2 L 7 4 4F RT A20WE 2007083100227 20070831 00227 NM 2007 8 31 UIEA200700321 1 20070817 A 5347 SEAT TRACK BOEING 747 747243B 1384830 NM BS 1872-1881 BROKEN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 AFT CARGO COMPARTMENT HAS SEAT TRACK CROWN BROKEN BETWEEN STA 1872 AND STA 1881 LBL 47. REPAIRED SEAT TRACK IAW SRM 53- 10-05. 2 L 7 4 4F A20WE 2007083100228 20070831 00228 NM 2007 8 31 UIEA200700310 1 20070727 A 5511 SPAR CAP BOEING 747 747271C 1384869 NM ZONE 300 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 SEVERAL BOLT HOLES DAMAGED IN LEFT HORIZ STAB SPAR CAP IN THE AREA OF LBL 43.5. REF NON ROUTINES 18389-18392. REAMED DA MAGED HOLE TO FIRST OVERSIZE (.450-.453) IAW SB 747-55A2050. NDT FINDS NO DEFECTS. BOLTS INSTALLED ON CARD 8010 / 8011 . 2 L 7 4 4F A20WE 2007083100229 20070831 00229 NM 2007 8 31 UIEA200700323 1 20070821 A 2750 65B1565110 PUSHROD BOEING 747 7472D7B 1384803 NM TE FLAP SHEARED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 ON WALK AROUND FOUND NR 5 FLAP TRACK MOVABLE CANOE FAIRING AFT PUSH ROD SHEARED AND BENT AND FORWARD LINK SUPPORT BENT. INBOARD SIDE OF FAIRING SEAL RETAINER WAS DAMAGED AND A 20 INCH SECTION OF COMPOSITE SKIN UNDER THE RETAINER WAS CRACKE D.ROD AND LINK WAS REMOVED AND REPLACED AS PER 747-200 MM 27-51-39 AND FAIRING WAS REMOVED FROM AIRCRAFT AS PER CDL 27-5 1-2, REFERENCE ATLAS DMI M07 242. 2 L 7 4 4F RT A20WE 2007083100230 20070831 00230 NM 2007 8 31 SWAA074180 1 20070823 A 5311 6545874 FRAME BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 736SA 27868 DURING SCHEDULED 8Y CHECK, FOUND L2 DOOR LOWER STUB FRAME CRACKED AT BS 296. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007083100231 20070831 00231 NM 2007 8 31 UIEA200700313 1 20070808 A 5320 WEB BOEING 747 74747UF 1384812 NM ZONE 100 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 499MC 29260 TOP OF FLOOR WEB DAMAGED AT STA 1660-1680 IN AFT LOWER CARGO COMPARTMENT. REPAIRED PER XEO 53-080707 AND PER BOEING SRM 51-70-13 FIG 201 REPAIR 1. 2 L 7 4 4F RT A20WE 2007083100238 20070831 00238 NM 2007 8 31 SWAA074166 1 20070823 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007083100239 20070831 00239 NM 2007 8 31 SWAA074177 1 20070823 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 710SW 27844 DURING SCHEDULED MV1 CHECK, FOUND LEFT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007083100240 20070831 00240 NM 2007 8 31 SWAA074174 1 20070823 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 465WN 33829 DURING SCHEDULED HC1 CHECK, RIGHT OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK P ER MM. 2 L 7 2 4F RT A16WE 2007083100241 20070831 00241 NM 2007 8 31 SWAA074175 1 20070823 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 465WN 33829 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2007083100242 20070831 00242 NM 2007 8 31 SWAA074169 1 20070823 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 428WN 29844 DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007083100243 20070831 00243 NM 2007 8 31 SWAA074173 1 20070823 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 465WN 33829 DURING SCHEDULED HC1 CHECK, RIGHT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007083100253 20070831 00253 NM 2007 8 31 USAA070664 1 20070824 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 23381 STA 727D + 17" TO +19", .5 INCH ABOVE STR 22L CENTER LINE HAS CRACK. DOUBLER REPAIR FROM .050 2024-TS INSTALLED PER SRM 53-00-01, REP 31, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007083100264 20070831 00264 NM 2007 8 31 KCSA071325 1 20070826 A 5330 SKIN BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FUSELAGE SKIN CRACKED AT BS 344, STR 5R. 2 L 7 4 4F RT A20WE 2007083100280 20070831 00280 2007 8 31 UPS07150495 4 20070825 A 2565 GAUGE AIRBUS A300 A300F4622R 3930360 EU EVAC SLIDE NOT SEATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 125UP 0809 INSPECTION TYPE:N/A PRESSURE GAUGE IN SLIDE HARD TO READ. RESEATED THE GAUGE IAW 25-60-00. 2 L 7 2 4F RT A35EU 2007083100283 20070831 00283 EU 2007 8 31 UPS07150496 1 20070824 A 5321 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU MAIN CARGO BAY PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 138UP 0821 INSPECTION TYPE:N/A MAIN CARGO DECK FLOOR PANEL BETWEEN 10R AT 11R PUNCTURED 1 INCH. ACCOMPLISHED PERMANENT REPAIR PER SRM 53-10-20. OPS CHECK OK. 2 L 7 2 4F RT A35EU 2007083100286 20070831 00286 NM 2007 8 31 UPS07450491 1 20070809 A 5280 65B12435601 SUPPORT FITTING BOEING 747 747200 1384847 NM RT BLG WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C RIGHT BLG I/B WHEEL WELL DOOR FWD INTERIOR DOOR SUPPORT FITTING FOUND WORN. RIGHT BLG I/B WHEEL WELL DOOR FWD INTERIOR DOOR SUPPORT FITTING REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F RT A20WE 2007083100293 20070831 00293 NM 2007 8 31 UPS07450493 1 20070814 A 5420 65B913143 FITTING BOEING 747 747200 1384847 NM NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C NR 1 PYLON REAR ENGINE MOUNT BULKHEAD UPPER LINK BEAM ATTACHMENT BATH FITTING FOUND CRACKED (CRACK LEN GTH .375 INCH). NR 1 PYLON REAR ENGINE MOUNT BULKHEAD UPPER LINK BEAM ATTACHMENT BATH FITTING REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F RT A20WE 2007083100297 20070831 00297 NM 2007 8 31 UPS07550498 1 20070825 A 5534 STRUCTURE BOEING 757 75724APF 1384969 NM VERTICAL STAB DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 407UP 23729 DELAMINATION VERTICAL STAB 2FT X 3FT. A/C FERRIED TO BFM D35760 ASSIGNED. REPAIR PER EO B757-5530-27491A. REMOVED VER TICAL STAB PANEL AND INSTALLED NEW PANEL IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007083100301 20070831 00301 NM 2007 8 31 UPS07650480 1 20070822 A 2432 BATTERY BOEING 767 76734AF 1385212 NM APU DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 334UP INSPECTION TYPE:ETOP BTB - APU AIR INOP. REMOVED AND REPLACED APU BATTERY PER MM 24-31-04-4. 2 L 7 2 4F RT A1NM 2007083100304 20070831 00304 2007 8 31 UPS07650489 4 20070823 A 3442 TRANSCEIVER BOEING 767 76734AF 1385212 NM WEATHER RADAR MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 312UP 27763 INSPECTION TYPE:ETOP WEATHER RADAR WOULD NOT TEST. REMOVED AND REPLACED R/T UNIT. OPS TEST OK PER MM 34-43-01-4. 2 L 7 2 4F RT A1NM 2007083100306 20070831 00306 WP 2007 8 31 UPS07850497 1 20070825 A 3350 LIGHT DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:N/A FRONT FWD ENTRANCE EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT, OPS CHECK OK PER MM 33-50-02. 2 L 7 4 4F RT 4A25 2007083100315 20070831 00315 NM 2007 8 31 ASAA0741996 1 20070826 A 5753 65C2637035 SKIN BOEING 737 737490 1384715 NM MID FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 28887 LEFT O/B MID FLAP HAS 3 EACH DENTS ON TOP SURFACE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED SKIN FILLER AND DOUBL ER IAW SRM 51-70-10 REPAIR 2. 2 L 7 2 4F RT A16WE 2007083100326 20070831 00326 NM 2007 8 31 ASAA0741999 1 20070826 A 5330 65C357882 SKIN BOEING 737 737490 1384715 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 28887 TWO DENTS ON FUSELAGE SKIN, DENTS IN ADJACENT BAYS. CUT OUT DAMAGED SECTIONS OF SKIN, FABRICATED AND INSTALLED REPAIR D OUBLERS AND FILLERS IAW ASA EA 5330 02231. 2 L 7 2 4F RT A16WE 2007083100328 20070831 00328 NM 2007 8 31 PIDR07003 1 20070824 A 5313 STRINGER BOEING 737 737297 1384480 NM FUSELAGE DAMAGED B RYNA K NONE O OTHER IN INSP/MAINT 1 SO 05 147AW 22630 STRINGER 16 RT AT BS 727B HAS A DAMAGED FASTENER HOLE. REPAIRED IN ACCORDANCE WITH SRM 53-10-3 FIGURE 2. 2 L 7 2 4F A16WE 2007083100330 20070831 00330 NM 2007 8 31 QXEA200701355 1 20070825 A 2120 UNKNOWN DHAV DHC8 DHC8202 2809007 NM COCKPIT ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 346PH 477 SEA - BURNING ELECTRICAL ODOR IN FLIGHT DECK. CAPTAIN MAP LIGHT IS WIRED BACKWARDS WHEN FIRST TURNED ON GOES FULL BRIGHT AND WHEN TURNED TO THE RIGHT GOES OFF. MAP LIGHT PUT ON MEL. INSPECTED FLIGHT DOOR AREA FOR ELECTRICAL PROBLEMS ASSOC IATED WITH ELECTRICAL SMELL. NO PROBLEMS NOTED. INVERTERS CHECKED GOOD. AVIONICS BAY CHECKED GOOD, ALL CRT BREAKERS I N. AIRCRAFT VERY DIRTY THROUGHOUT AND DID HAVE AN ASSOCIATED BAD ODOR UPON ENTERING CABIN. SERVICED LAV, CLEANED OUT G ALLEY TRASH AREA AND REMOVED ALL TRASH FROM AIRCRAFT ODOR DISAPPEARED. NO PARTS REPLACED. AIRCRAFT OK FOR CONTINUED SE RVICE. 2 H 7 2 4T RT A13NM 2007083100331 20070831 00331 NM 2007 8 31 PIDR07002 1 20070824 A 5330 SKIN BOEING 737 737297 1384480 NM FUSELAGE CRACKED B RYNA K NONE O OTHER NR NOT REPORTED 1 SO 05 147AW 22630 CRACK IN FUSELAGE SKIN AT BS 727A+14.5 AT STR 17 LT WAS REPAIRED BY REPLACING SECTION OF SKIN FROM BS 727A +8 TO BS 767 FROM STR 16 LT TO STR 18 LT DUE TO PROXIMITY OF ADJACENT REPAIRS. REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH PACE AIRLI NES REPAIR PROCEDURE REPORT EA 53-231 DATED 8/18/07 WITH FAA DER APPROVED 8110-3 DATED 08/23/2007. 2 L 7 2 4F A16WE 2007083100332 20070831 00332 NM 2007 8 31 PIDR07001 1 20070824 A 5330 SKIN BOEING 737 737297 1384480 NM FUSELAGE CRACKED B RYNA K NONE O OTHER NR NOT REPORTED 1 SO 05 147AW 22630 CRACK IN THE FUSELAGE SKIN AT BS 727B+4 AT STR 17 RT WAS REPAIRED BY REPLACING THE DAMAGED SECTION OF SKIN FROM BS 727 T O BS 757 FROM STR 14 RT TO STR 20 RT DUE PROXIMITY OF ADJACENT REPAIRS. REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH PACE AIRLINES REPAIR PROCEDURE REPORT EA 53-231 DATED 8/18/07 WITH FAA DER APPROVED 8110-3 DATED 08/23/2007. 2 L 7 2 4F A16WE 2007083100333 20070831 00333 NM 2007 8 31 QXEA200701351 1 20070824 A 2750 CONTROL SYSTEM BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 405QX 4047 SMF FLIGHT NR 2410: FLAP POWER CAUTION LIGHT ILLUMINATED ON PUSH BACK. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE CLEARED FLAP NVM. RESET FLAP CONTROL SYSTEM. NO FURTHER FAULTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007083100335 20070831 00335 NM 2007 8 31 QXEA200701352 1 20070825 A 2721 8DK4075001 CONTROL PANEL BOMBDR DHC8 DHC8402 1390042 NM RUDDER TRIM MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 405QX 4047 PDX FLIGHT NR 2415: RUDDER TRIM INOP. AIRCRAFT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED AILERON/RUDDER TRIM PANEL IAW Q400 AMM TASK 27-13-16-000-801 AND 27-13-16-400-801. OPS CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT RETURNED T O SERVICE. 2 H 7 2 4T RT A13NM 2007083100338 20070831 00338 2007 8 31 ZZDA2007263 4 20070825 A 2565 D29982225 SLIDE BOEING 717 717200 1383700 NM R1 DOOR UNWANTED DEPLOY A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 970AT 55031 R1 DOOR SLIDE ACCIDENTALLY DEPLOYED. INSTALLED SERVICEABLE R1 DOOR SLIDE PER MM 25-61. P/N OFF D29982-225, S/N OFF 263 8, P/N ON D29982-225, S/N ON 2644. 2 L 7 2 4F TR A6WE 2007083100339 20070831 00339 NM 2007 8 31 CALA0700453 1 20070824 A 5320 6555872 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A .75 INCH CRACK IN UPPER WEB FORWARD OF L-2 DOOR AT STA 947 AFT OF S11L. REPAIRED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007083100340 20070831 00340 NM 2007 8 31 CALA0700454 1 20070824 A 5320 654656411 FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND SKIN CLIP CORRODED AT STA 986.5 BETWEEN S24R AND S25R. THE SKIN CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007083100341 20070831 00341 NM 2007 8 31 CALA0700455 1 20070824 A 5313 6545776 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND S27L CORRODED AT STA 957. THE STRINGER WAS REPAIRED IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 2007083100343 20070831 00343 NM 2007 8 31 CALA0700457 1 20070826 A 5347 151W62031 SEAT TRACK BOEING 777 777224 1385225 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 79011 29859 INSPECTION FOUND SEAT TRACK CORRODED AT STA 1508-1540, LBL 74. THE SEAT TRACK SECTION WAS REPLACED IAW SRM 53-00-52, FI GURE 202, REPAIR 3. 2 L 7 2 4F RT T00001SE 2007083100345 20070831 00345 NM 2007 8 31 SWAA074185 1 20070824 A 3350 1619 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED MV2 CHECK, FOUND RIGHT FWD FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BUL B PER MM. 2 L 7 2 4F RT A16WE 2007083100346 20070831 00346 NM 2007 8 31 SWAA074182 1 20070824 A 3350 311500 LENS BOEING 737 7373Y0 1384671 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 BULL NOSE EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 20 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007083100348 20070831 00348 2007 8 31 SWAA074183 4 20070824 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 473WN 33832 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007083100349 20070831 00349 NM 2007 8 31 SWAA074200 1 20070824 A 5312 6545819 PRESSURE PANEL BOEING 737 737317 138447P NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT LBL 7.75. REPAIRED CEILING PANEL PER ACO. 2 L 7 2 4F RT A16WE 2007083100350 20070831 00350 NM 2007 8 31 SWAA074199 1 20070824 A 5312 6545819 PRESSURE PANEL BOEING 737 737317 138447P NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT RBL 7.75. REPAIRED CEILING PANEL PER ACO. 2 L 7 2 4F RT A16WE 2007083100351 20070831 00351 NM 2007 8 31 SWAA074208 1 20070825 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007083100352 20070831 00352 NM 2007 8 31 QXEA200701353 1 20070824 A 2160 8209601 SENSOR BOMBDR DHC8 DHC8402 1390042 NM CABIN TEMP MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 400QX 16155 16155 4030 LAX - MFR FLIGHT NR 2424: FLIGHT COMPARTMENT PACK HOT CAUTION LIGHT AND CABIN DUCT HOT CAUTION LIGHT. FLIGHT DIVERTED T O SMF. MAINTENANCE INTERROGATED CDS AND FOUND FAULT 3D09-CAB OLT MISCMP. REMOVED AND REPLACED CABIN ZONE SUPPLY TEMP S ENSOR (P/N 820907-3) IAW Q400 AMM TASK 21-61-11-000-801 AND 21-61-11-400-801. REMOVED AND REPLACED LT COMPRESSOR OUTLET TEMP SENSOR IAW Q400 AMM TASKS 21-51-91-000-801 AND 21-51-91-400-801. OPERATED BOTH AIR CONDITIONING PACKS. NO DEFECT S NOTED. CLEARED ECS FAULTS IN CDS. GROUND RAN AIRCRAFT. NO DEFECTS NOTED. INTERROGATE ECS SYSTEM IN CDS WITH NO CUR RENT FAULTS FOUND. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007083100353 20070831 00353 EA 2007 8 31 A6WA200740464 1 20070713 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 419AW 7633 FOUND CORROSION ON SKIN CUT OUT OF MAIN AVIONIC DOOR SURROUND. MAINTENANCE PERFORMED BOMBARDIER MODSUM 601R53210045 TO COMPLY WITH REO 601R-53-21-781. (M) 2 L 7 2 4F RT A21EA 2007083100354 20070831 00354 EA 2007 8 31 A6WA200740465 1 20070713 A 5242 SKIN CNDAIR CL600 CL6002B19 1900309 EA E/E BAY DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 419AW 7633 FOUND CORROSION ON AVIONIC DOOR INNER SKIN AT FS 364 BTW STRINGER 25L TO STRINGER 25R. MAINTENANCE PERFORMED REPAIR TO AVIONIC DOOR APERTURE INNER DOUBLER FS 364 TO FS 379 STRINGER 27 TO STRINGER 25R IAW REO 601R-53-21-781. (M) 2 L 7 2 4F RT A21EA 2007083100355 20070831 00355 EA 2007 8 31 A6WA200740463 1 20070713 A 5242 RETAINER CNDAIR CL600 CL6002B19 1900309 EA E/E BAY DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 419AW 7633 CORROSION FOUND ON FORWARD SEAL RETAINER OF THE MAIN AVIONICS COMPARTMENT DOOR. SEAL RETAINER P/N 601R14533-41, CC670-3 86743 AND CC 670-38663-5 REPLACED IAW SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007083100356 20070831 00356 EA 2007 8 31 A6WA200740371 1 20070706 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 461AW 7870 LEFT INBOARD 280 CLIP IS CRACKED APPROX .25 INCH L AT LBL 9. MAINTENANCE REMOVED DAMAGED LEFT INBOARD 280 CLIP AT LBL 9 AND INSTALLED NEW SERVICEABLE CLIP AT LBL IAW BSC REPAIR 601R-53-0057A. (M) 2 L 7 2 4F RT A21EA 2007083100357 20070831 00357 EA 2007 8 31 A6WA200740370 1 20070706 A 5340 601R311358 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA FS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 461AW 7870 RIGHT INBOARD AND OUTBOARD 280 CLIPS ARE CRACKED APPROX .25 INCH AT RBL 9. MAINTENANCE REMOVED RIGHT INBOARD AND OUTBOA RD 280 CLIPS AT RBL 9 AND INSTALLED 2 NEW SERVICEABLE 280 CLIPS IAW BSC REPAIR 601R-53-0037A. (M) 2 L 7 2 4F RT A21EA 2007083100358 20070831 00358 EA 2007 8 31 A6WA200740359 1 20070703 A 5320 6013501252 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 409AW 7447 RIGHT FS 621 TO 625 OBLIQUE ANGLE IS CRACKED 1.5 INCH LONG IN AFT RADIUS. MAINTENANCE REMOVED CRACKED ANGLE AND INSTALL ED NEW ANGLE P/N 601-35012-52 IAW CRJ SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007083100359 20070831 00359 EA 2007 8 31 A6WA200740360 1 20070707 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 461 DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 409AW 7447 TOP RIVET IS MISSING FROM INTERCOSTAL FLANGE AT FS 461, LBL 9. MAINTENANCE INSTALLED RIVET IAW CRJ SRM 51-45-06. (M) 2 L 7 2 4F RT A21EA 2007083100360 20070831 00360 EA 2007 8 31 A6WA200740474 1 20070820 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 467AW 7900 FOUND FS 484 RBL 36 INTERCOSTAL CRACKED IN RADIUS. MAINTENANCE REPAIRED INTERCOSTAL AT FS 484 RBL 36 IAW BOMBARDIER REO 601R-53-41-059 AND BSC STANDARD REPAIR 601R-53-0030A. (M) 2 L 7 2 4F RT A21EA 2007083100361 20070831 00361 EA 2007 8 31 A6WA200740476 1 20070822 A 5320 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA LT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 467AW 7900 LT MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER HAT CHANNEL IS CRACKED AT INBOARD LEGS APPROX .20 INCH LONG. MAINTENANCE R EMOVED AND REPLACED HAT CHANNEL P/N 601R75262-159 IAW CRJ SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007083100362 20070831 00362 EA 2007 8 31 A6WA200740472 1 20070820 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 467AW 7900 FOUND FS 484, LBL 27 INTERCOSTAL CRACKED. MAINTENANCE REPAIRED INTERCOSTAL AT FS 484 LBL 27 IAW REO 601R-53-41-059 AND BSC STANDARD REPAIR 601R-53-0029B. (M) 2 L 7 2 4F RT A21EA 2007083100364 20070831 00364 NM 2007 8 31 CHQA200700042 1 20070826 A 4990 38004883 APU BOMBDR CL600 CL6002D15 NM GE CF34 CF343B1 NE APU BAY OVERSERVICED A CHQA O OTHER W M J INADEQUATE Q C OVER TEMP WARNING INDICATION AP APPROACH 1 GL 11 642BR 6477 7356 GEE872617 SDF TO IAH - DURING APPROACH INTO IAH, CREW RECEIVED "APU OVERTEMP" AURAL WARNING AND MESSAGE AFTER SWITCHING BLEEDS TO APU. CREW OBSERVED THE TEMPERATURE REACHED 999 DEGREES CELSIUS. COMPLETED THE QRH FOR APU OVERTEMP MSG. EGT WAS SUSTA INED AT 999 DEGREES AND CREW DECLARED AN EMERGENCY. MAINTENANCE INSPECTED APU AND FOUND THE APU OIL OVERSERVICED. MAIN TENANCE SERVICED OIL TO THE PROPER LEVEL AND OPS CHECKED THE APU. APU OPERATED NORMALLY AFTER SERVICING. 2 L 7 2 4F 4 F RT A21EA E15NE 2007083100366 20070831 00366 NM 2007 8 31 AWXA200701020 1 20070815 A 5322 SHEAR TIE BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5987943, CRACK FOUND ON R1 DOOR SURROUND SKIN ANGLE, BS 280 - BS290, S-13R. REPLAC ED R1 DOOR SURROUND SKIN ANGLE, BS 280 - BS290, S-13R IAW B737-300 SRM 51-40-02-0G, FIG 3, 8, AND FIG 12. 2 L 7 2 4F RT A16WE 2007083100367 20070831 00367 NM 2007 8 31 AWXA200701021 1 20070818 A 5322 140N2002344 SHEAR TIE BOEING 757 7572S7 1384962 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 MCN - MAJOR REPAIR - C-11 CHECK - NR 5988360, CRACK ON FUSELAGE FRAME SHEAR TIE, BS 1459, S-29R - S-30R. REPLACED FUSEL AGE FRAME SHEAR TIE, BS 1459, S-29R - S-30R IAW BOEING DWG 140N2002 AND B757-200 SRM 51-30-01-06, FIG 3, 7, 8, AND 9. 2 L 7 2 4F RT A2NM 2007083100368 20070831 00368 NM 2007 8 31 AWXA200701022 1 20070818 A 5322 140N2002345 SHEAR TIE BOEING 757 7572S7 1384962 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 MCN- MAJOR REPAIR - C-11 CHECK - NR 5988361, CRACK ON FUSELAGE FRAME SHEAR TIE, BS 1459, S-28R - S-29R. REPLACED FUSELA GE FRAME SHEAR TIE, BS 1459, S-28R - S-29R IAW BOEING DWG 140N2002 AND B757-200 SRM 51-30-01-06, FIG 3, 7, 8, 9. 2 L 7 2 4F RT A2NM 2007083100369 20070831 00369 NM 2007 8 31 AWXA200701023 1 20070822 A 5340 143N52601 ATTACH ANGLE BOEING 757 7572S7 1384962 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 MCN- MAJOR REPAIR - C-11 CHECK - NR 5988573, CRACK ON INTERCOSTAL ATTACHED ANGLE, BS 540 - BS 560, BL 0. REPLACED INTER COSTAL ATTACHED ANGLE, BS 540 - BS 560, BL 0 IAW B757-200 SRM 51-40-02-0G, PAR 4B, FIG 3 AND 8. 2 L 7 2 4F RT A2NM 2007083100370 20070831 00370 NM 2007 8 31 AWXA200701024 1 20070822 A 5340 412N202221 BRACKET BOEING 757 7572S7 1384962 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 MCN - MAJOR REPAIR - C-11 CHECK - NR 5988668, CRACK ON INTERCOSTAL SUPPORT CLIP, BS 1600, S-6L. REPLACED INTERCOSTAL S UPPORT CLIP, BS 1600, S-6L IAW B757-200 SRM 51-40-02-0G, FIG 8 AND 12. 2 L 7 2 4F RT A2NM 2007083100371 20070831 00371 NM 2007 8 31 AWXA200701025 1 20070814 A 5311 6546525 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5987890, CRACK ON FORWARD FUSELAGE FRAME, BS 380, S-16R. REPAIRED FORWARD FUSELAGE FRAME, BS 380, S-16R IAW B737-300 SRM 53-00-07-2R, REPAIR 8, FIG 201. 2 L 7 2 4F RT A16WE 2007083100372 20070831 00372 NM 2007 8 31 AWXA200701026 1 20070813 A 5340 69374024 ATTACH ANGLE BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5987942, CRACK ON R1 DOOR SURROUND ATTACH ANGLE, BS 294.5, S-17R. REPLACED R1 DOOR SURROUND ATTACH ANGLE, BS 294.5, S-17R IAW B737-300 SRM 51-40-02-0G, FIG 3, 8, AND 12. 2 L 7 2 4F RT A16WE 2007083100373 20070831 00373 WP 2007 8 31 AALA20071472 1 20070809 A 2822 PUMP DOUG DC9 DC982 3022082 WP FUEL BOOST INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 407AA 49318 STL INFLIGHT T616/08AUG DFW TO DTW - FORWARD CENTER FUEL BOOST PUMP CIRCUIT BREAKER POPPED. FUEL STOPPED FEEDING FROM C ENTER TANK. LANDED STL WITHOUT INCIDENT. REPLACED CENTER FUEL TANK FORWARD FUEL BOOST PUMP. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F A6WE 2007083100374 20070831 00374 NM 2007 8 31 AALA20071478 1 20070809 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 DFW - EXTERIOR EMERGENCY LIGHT AT RIGHT OVERWING EXIT INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RIGHT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007083100375 20070831 00375 NM 2007 8 31 AALA20071481 1 20070810 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 937AN 30082 MIA - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007083100376 20070831 00376 NM 2007 8 31 AALA20071479 1 20070809 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 DFW - EXTERIOR EMERGENCY LIGHT AT LEFT OVERWING EXIT INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT OV ERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007083100381 20070831 00381 WP 2007 8 31 AALA20071474 1 20070809 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9681B 53631 BOS - EMERGENCY LIGHT AT OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007083100382 20070831 00382 NM 2007 8 31 AALA20071475 1 20070809 A 3232 ACTUATOR BOEING 757 757223 1384957 NM RT MLG DOOR INOPERATIVE A AALA O OTHER J WARNING INDICATION LD LANDING 1 SW 21 656AA 24614 SEA INFLIGHT T1603/09AUG - RIGHT MAIN GEAR DOOR REMAINED OPEN ON GEAR EXTENSION. DOOR WARNING AND GEAR DOOR EICAS MESSA GE ILLUMINATED. LANDED SEA WITHOUT INCIDENT. REPLACED RIGHT MAIN GEAR DOWN LOCK ACTUATOR LINE AND HYDRAULIC EXTENSION AND RETRACTOR FUSES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007083100383 20070831 00383 WP 2007 8 31 AALA20071468 1 20070808 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 562AA 49344 LGA - EMERGENCY LIGHTS AT SEAT ROWS 25 TO 29 INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 29DEF FOR EMERGENCY LIGHTS AT SEAT ROWS 25 TO 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007083100384 20070831 00384 NM 2007 8 31 AALA20071469 1 20070808 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 349AN 33088 SFO - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOO R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007083100385 20070831 00385 NM 2007 8 31 AALA20071470 1 20070809 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 788AN 30011 DFW - EMERGENCY LIGHT LENS AT RIGHT MID GALLEY PARTITION MISSING. REPLACED LENS FOR EMERGENCY LIGHT AT RIGHT MID GALLEY PARTITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007083100386 20070831 00386 NM 2007 8 31 AALA20071471 1 20070809 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 788AN 30011 DFW EMERGENCY LIGHT AT OVERHEAD AISLE LEFT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEA D AISLE LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007083100387 20070831 00387 NM 2007 8 31 AALA20071473 1 20070809 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT SEAT 23C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007083100389 20070831 00389 NM 2007 8 31 SWAA074207 1 20070825 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007083100390 20070831 00390 NM 2007 8 31 SWAA074187 1 20070826 A 5311 6546552 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007083100391 20070831 00391 NM 2007 8 31 SWAA074205 1 20070825 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007083100392 20070831 00392 NM 2007 8 31 SWAA074206 1 20070825 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007082900187 20070829 00187 EA 2007 8 29 TRAX200701219 1 20070811 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 839AS 7284 FLOOR EMERGENCY LIGHT BULLET CONNECTOR MISSING AT AFT RIGHT OVERWING EXIT. 2 L 7 2 4F RT A21EA 2007082900188 20070829 00188 EA 2007 8 29 TRAX200701220 1 20070814 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 839AS 7284 LEFT BONDED SKIN DOUBLER AT 640 FRAME CRACKED. 2 L 7 2 4F RT A21EA 2007082900211 20070829 00211 NM 2007 8 29 SWAA074151 1 20070822 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 402, STR 5L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007082900213 20070829 00213 NM 2007 8 29 SWAA074143 1 20070822 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007082900216 20070829 00216 NM 2007 8 29 SWAA074153 1 20070822 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007082900218 20070829 00218 NM 2007 8 29 SWAA074139 1 20070822 A 3234 6554219 HANDLE BOEING 737 7373H4 1384600 NM COCKPIT DIRTY A SWAA K NONE J WARNING INDICATION AP APPROACH 1 SW 29 304SW 22944 LANDING GEAR EXTENDED 3 GREEN LIGHTS ILLUMINATED, 3 RED LIGHTS DID NOT EXTINGUISH. CYCLED LANDING GEAR ALL INDICATIONS NORMAL. INSPECTED AND FOUND LANDING GEAR HANDLE STAYS OUT. LUBED AND CLEANED LANDING GEAR HANDLE PER MM. 2 L 7 2 4F RT A16WE 2007082900219 20070829 00219 NM 2007 8 29 SWAA074140 1 20070822 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM R2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2007082900220 20070829 00220 NM 2007 8 29 SWAA074142 1 20070822 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM L2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2007082900229 20070829 00229 2007 8 29 SWAA074141 4 20070822 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007082900242 20070829 00242 CE 2007 8 29 DXTA200702400 1 20070813 A 3297 6508012201 WIRE HARNESS CESSNA 500 560CESSNA 2076750 CE BRAKES WORN E DXTA O OTHER O OTHER LD LANDING 1 GL 07 336QS 11057 5600336 AFTER APPLYING BRAKE PRESSURE THE BRAKES GRAB AND THEN QUICKLY RELEASE. THET THEN GRAB AGAIN IN A JERKY FASHION. BLED A/ C BRAKES. REMOVED AND REPLACED THE LEFT ANTI SKID HARNESS P/N 6508012-201 AND THE RIGHT ANTI SKID HARNESS P/N 8508012-20 2. OPS CHECK GOOD. I/A/W CE-560 MM 32-42-07, 32-42-00 AND WIRING PRINTS 32-40-01. 2 L 7 2 4F RT A22CE 2007083100013 20070831 00013 NM 2007 8 31 USAA070653 1 20070823 A 5320 6517684638 INTERCOSTAL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 517AU 23703 BS 294.5, S-12L, WEB INTERCOSTAL HAS CRACK. REPLACED INTERCOSTAL IAW SRM 51-10-02, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007083100014 20070831 00014 NM 2007 8 31 USAA070652 1 20070823 A 5320 6517684 INTERCOSTAL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 517AU 23703 BS 294.5 & S76 HAS CRACK. REPLACED INTERCOSTAL IAW 51-10-02, DEFECT SIZE: .0625 INCH. 2 L 7 2 4F RT A16WE 2007083100022 20070831 00022 2007 8 31 SWIA200718616 4 20070814 A 3417 8220372436 COMPUTER CNDAIR CL600 CL6002C10 1390015 EA NR 1 ADC MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 774SK 1764 1764 10240 FLIGHT DISPLAY NR 1 IS MISSING ALTITUDE AND SPEED INFORMATION, FLIGHT NR 1001. REPLACED NR 1 ADC IAW MM 34-13-01. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007083100030 20070831 00030 SO 2007 8 31 SWIA200718620 1 20070822 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO CABIN ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 229SW 120305 PASSENGERS AND FLIGHT ATTENDANT COMPLAINED OF SMOKE IN THE CABIN WITH AN ELECTRICAL BURNING ODOR, FLIGHT NR 5727. RAN R IGHT PACK WITH APU AIR FOR 30 MIN. RAN EACH ENGINE WITH PACKS ON AT 30 MIN EACH. NO BURNING OR OVERHEAT ODOR NOTED AT THIS TIME. 2 L 7 2 4T RT A31SO 2007083100035 20070831 00035 NE 2007 8 31 QXEA200701348 2 20070817 A 7320 4120T00P37 FADEC CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE LT ENGINE FAULTED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 604QX 3374 1055 10019 BOI - RECEIVED A LEFT ENGINE DEGRADE CAUTION MESSAGE IN FLIGHT. RETURNED TO THE FIELD. MAINTENANCE FOUND THE LEFT FADE C HAD A INTERNAL FAULT AND REPLACED THE FADEC. AS A PRECAUTION ALSO REPLACED THE K19 AND K21 RELAYS AS A PRECAUTION. O PERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007083100037 20070831 00037 WP 2007 8 31 UPS07850481 1 20070811 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 FLOORBEAM AT STA 240 BL-0 HAS CORROSION OUT OF LIMITS. CUT OUT DAMAGED AREA OF FLOORBEAM AT STA 240 BL 0 IAW SRM 53-02-00 FIG 001. FABRICATED AND INSTALLED REPAIR ANGLES AND STRAP AT STA 240 BL 0 IAW SRM 53-02-00 FIG 00 1. 2 L 7 4 4F RT 4A25 2007083100049 20070831 00049 WP 2007 8 31 MWEA070186 1 20070821 A 2597 0202952001 CONNECTOR DOUG DC9 DC981 3022081 WP CABIN DISCONNECTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 812ME 48006 SEAT 6 A/B OXYGEN MASK DOOR DID NOT OPEN WHEN THE OXYGEN SYSTEM SWITCH WAS ACTIVATED. CONNECTED PSU CONNECTOR. 2 L 7 2 4F A6WE 2007083100053 20070831 00053 EU 2007 8 31 07FDEA03066 1 20070823 A 5753 A57970650002 VANE AIRBUS 310 A310324 3930206 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 OLD REPAIR ON FLAP VANE OF INBOARD FLAP LT REPAIR PERFORMED WITH HFEC INSPECTION THAT DENTED AREA IS FREE OF CRACKS, CUT OUT ON LOWER SKIN IS FILLED WITH RESIN AS PER SRM 57-53-12/FIG 206 AND INSTALLING AN EXTERNAL DOUBLER AS PER PRINCIPLES GIVEN IN SRM 57-53-12/FIG 207. REPAIR COVERED IN EA 6-5752-101278 AND RAS/DABRE/7006846/2006 ISS "B". 2 L 7 2 4F RT A35EU 2007083100054 20070831 00054 NM 2007 8 31 07FDEA03081 1 20070824 A 5710 PANEL DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 RIGHT WING REFUELING PANEL CUT OUT INBOARD CORNER FOUND WITH CRACK. 09-04-07 RT WING REFUELLING PANEL CUT OUT INBOARD CORNER REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 21 VOL. I. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007083100063 20070831 00063 EU 2007 8 31 07FDEA03087 1 20070824 A 5311 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CRACK FOUND IN FRAME 43 LT, STR 26-27 LT REPAIR PERFORMED BY REPLACEMENT OF FITTING IAW SRM 53-15-18/FIG 1 AND EA 6-5315 -03255. 2 L 7 2 4F RT A35EU 2007083100070 20070831 00070 NM 2007 8 31 07FDEA03093 1 20070824 A 5347 BAC1520792 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 MAIN CABIN FLOOR SEAT TRACK IS CORRODED AT STA 1090, RBL 24 BLENDED CORROSION. ORIGINAL "T" .090", REMOVED .025" OUT OF LIMITS REF SRM 51-10-1 PG 15. FABRICATED REPLACEMENT SEAT TRACK, FABRICATED SPLICE REPAIR PARTS, TREATED AND PRIMED SE AT TRACK AND REPAIR PARTS. INSTALLED SEAT TRACK AND REPAIR PARTS REF SRM 53-10-5 FIG 1. INSTALLED 3 U- CHANNELS REF SRM 51-30-2, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007083100071 20070831 00071 NM 2007 8 31 07FDEA03094 1 20070824 A 5320 651960414 WEB BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT UPPER MAIN DECK, CORROSION ON UPPER SHEAR DECK, UNDER FLOORBOARDS, STA 1166 PLUS 8", RBL 17" TO RBL 36" (BETTER VIEW FROM LWR AFT PIT) REMOVED SEAT TRACK AT STA 1128 - 1178, RBL 25 AND 45. REMOVED ATTACHING STRUCTURE FOR SHEAR WEB RE MOVAL. REMOVED SHEAR WEB. DRILLED UP SHEAR WEB. INSTALLED REMOVED STRUCTURE, SEAT TRACK, RBL 25-45 AND SHEAR WEB REF. 51-30-2, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007083100075 20070831 00075 NM 2007 8 31 2007UALA02940 1 20070730 A 2810 114001109 HOUSING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 DRIP STICK LEAKING A UALA O OTHER K FLUID LOSS CR CRUISE 1 WP 29 659UA 27114 CREW REPORT: FUEL BALANCE EXCEEDED 1400 LBS DURING 4 HOUR FLIGHT. TURNED ON ALL FUEL PUMPS & CHECKED FUEL TANK QTY AFT ER 1 HOUR. NO LEAKS OR UNWANTED FUEL TRANSFER NOTED. CHECKED PER MM 28-11-95. LOCATED LEAK NEAR RT CTR AUX FUEL DRIP STICK NR 1 HOUSING. REPLACED NR 1 STICK HOUSING. LEAK CHECKED OK. NO ADD'L UNWANTED FUEL X-FER REPORTED IN PAST 21 DA YS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007083100076 20070831 00076 NM 2007 8 31 07FDEA03098 1 20070824 A 5313 655623622 STRINGER BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD CARGO AREA, STA 700 TO 705, STR 28R, AT RBL 4 TO RBL 7, STRINGER IS CORRODED REMOVED CORRODED SECTION OF STRINGER F ROM STA 680 TO STA 720 AND INSTALLED NEW SECTION REF SRM 51-30-2, AND BOEING DOCUMENT NUMBER 65-54577, ID NR 0004/FRAME NR 1. 2 L 7 3 4F RT A3WE 2007083100077 20070831 00077 NM 2007 8 31 07FDEA03099 1 20070824 A 5320 69648411 ANGLE BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD LOWER CARGO BAY REINFORCING ANGLE DOUBLER AT AT BS 740 BULKHEAD STR S-27R IS CORRODED REMOVED CORRODED REINFORCING A NGLE. REMOVED CORROSION AND ANGLE WAS OUT OF LIMITS. FABRICATED NEW REINFORCING ANGLE ON SNRM NR N01045, 8130 FORM TRA CKING 2007-06-143. INSTALLED REINFORCING ANGLE REF BOEING DOCUMENT NR 69-64841, ID NR 0001/FRAME NR 1, THIS IS CLASSIFI ED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007083100078 20070831 00078 NM 2007 8 31 2007UALA03262 1 20070818 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 301UA 23642 RIGHT AFT EMERGENCY EXIT IND LIGHT INOP. REPLACED LIGHT ASSY REF:WD M33-51-15. 2 L 7 2 4F 4 F RT A16WE E21EU 2007083100079 20070831 00079 NM 2007 8 31 2007UALA03263 1 20070818 A 3350 INVERTER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 301UA 23642 LEFT EMERGENCY EXIT IND LIGHT INOP, NEEDS INVERTER. REPLACED LT MID EMERGENCY EXIT INVERTER. OPS NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007083100093 20070831 00093 NM 2007 8 31 2007UALA03277 1 20070819 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 DOOR 4R FWD SILL EMERGENCY LIGHT INOPERATIVE. 08-31-07 RELAMPED. OP CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100097 20070831 00097 NM 2007 8 31 2007UALA03281 1 20070820 A 3350 32142410 EPSU AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 848UA 1647 EMERGENCY LIGHT SYS FAILS 3SVC CHECK WITH MESSAGE EPSU UNIT EMER L. REPLACED LEFT EPSU. 2 L 7 2 4F 4 F RT A28NM E40NE 2007083100127 20070831 00127 NM 2007 8 31 2007UALA03309 1 20070821 A 5311 FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 913UA 25291 CABIN FLOOR CREASE BEAM REQUIRES TO BE CUT FOR ACCESS TO REPAIR FRAME BS 446 - 466 STR 17R. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED CREASE BEAM REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007083100133 20070831 00133 NM 2007 8 31 2007UALA03315 1 20070821 A 3350 582240 POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 652UA 25390 EMERGENCY EEL LIGHT INOP FROM SEAT 31HJ TO 39 HJ. REPLACED BATTERY POWER SUPPLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007083100134 20070831 00134 NM 2007 8 31 2007UALA03316 1 20070821 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 774UA 26936 SEAT 11F EEL LIGHT INOPERATIVE. RELAMPED, OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007083100143 20070831 00143 EU 2007 8 31 2007UALA03321 1 20070822 A 3350 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 449UA 851 EPSU BATT EMER L FOUND WHEN TESTED. FOUND FAULTY BATTERY PACK. REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007083100155 20070831 00155 NM 2007 8 31 2007UALA03325 1 20070822 A 5241 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU R1 GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 1R FWD GALLEY DOOR CRACKED: FWD LOWER CORNER FWD SIDE 2 EA O/B FASTENER HOLES CRACKED. MAJOR REPAIR ACCOMPLISHED: SPL ICED REPAIR KIT FRAME. 2 L 7 2 4F 4 F RT A16WE E21EU 2007083100157 20070831 00157 WP 2007 8 31 IXXA07SMN217S 1 20070817 A 5340 4705419U502 FITTING DOUG DC8 DC873F 302199F WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 95905 1791 46044 DURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT AFT FITTING SHOWS CRACK 2" BETWEEN STA 1220.000 AND L-19R. REPLACED CRACKED FITTING WITH NEW FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007083100159 20070831 00159 NM 2007 8 31 2007UALA03328 1 20070822 A 5315 FLOORBEAM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA 25158 MAIN PRESS DECK WEB & FLOORBEAM LOWER TEE CORRODED, BS 1440-1480 LBL 0 TO LBL 25. REMOVED CORRODED MATERIAL. INSTALL ED FLOORBEAM TEE SPLICE & NEW PRESSURE DECK WEB SECTION. AIRCRAFT OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100160 20070831 00160 WP 2007 8 31 IXXA07SMN218S 1 20070817 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 759 L18L CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT AFT FITTING SHOWS CRACK 2" AT STA 759.000 AND L-18.8L. 2 L 7 4 4F RT 4A25 2007083100162 20070831 00162 WP 2007 8 31 IXXA07SMN216S 1 20070817 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 1152 L20R CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT FWD FITTING SHOWS CRACK 1" BETWEEN STA 1152.000 AND L-20R. 2 L 7 4 4F RT 4A25 2007083100163 20070831 00163 WP 2007 8 31 IXXA07SMN214S 1 20070817 A 5512 SKIN DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, LT HORIZONTAL STABILIZER, POINTS OF CORROSION ON UPPER SKIN FROM STA XE 28.843 TO STA XE 30.000. 2 L 7 4 4F RT 4A25 2007083100165 20070831 00165 WP 2007 8 31 IXXA07SMN221S 1 20070817 A 5711 SPAR CAP DOUG DC8 DC873F 302199F WP WING CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, NR 2 MAIN TANK LOWER CAP OF CENTER SPAR 3" CRACKED AT STA ZRS 172.000 BETWEEN S-61 AN D S-62. 2 L 7 4 4F RT 4A25 2007083100167 20070831 00167 WP 2007 8 31 IXXA07SMN194S 1 20070808 A 5753 SKIN DOUG DC8 DC873F 302199F WP LT WING TE FLAP DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, LT WING INBD FLAP UPPER FWD PLATING SHOWS DENT BETWEEN STA XW 28.000 TO STA XW 91.000 . 2 L 7 4 4F RT 4A25 2007083100168 20070831 00168 WP 2007 8 31 IXXA07SMN196S 1 20070808 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT WING TE FLAP DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, RT WING OTBD FLAP AFT PANEL PLATING LWR SKIN SHOWS (04EA) DENTS BETWEEN STA XF 415.00 0 AND STA XF 453.000. 2 L 7 4 4F RT 4A25 2007083100170 20070831 00170 WP 2007 8 31 IXXA07SMN195S 1 20070808 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT WING TE FLAP DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, RT WING OTBD FLAP AFT PANEL LWR SKIN SHOWS (03EA) DENTS BETWEEN STA XF 375.000 AND ST A XF 405.000. 2 L 7 4 4F RT 4A25 2007083100171 20070831 00171 WP 2007 8 31 IXXA07SMN197S 1 20070808 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT WING TE FLAP MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, RT WING INB FLAP PANEL LWR SKIN SHOWS (03EA) NON STANDARD REPAIR FROM STA XW 2.000 TO STA XW 92.000. 2 L 7 4 4F RT 4A25 2007083100173 20070831 00173 WP 2007 8 31 IXXA07SMN198S 1 20070808 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT WING TE FLAP MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, RT WING INBD FLAP UPPER SKIN SHOWS NON STANDARD REPAIR AND DENT BETWEEN STA XW 2.000 AND STA XW 92.000. 2 L 7 4 4F RT 4A25 2007083100175 20070831 00175 WP 2007 8 31 IXXA07SMN202S 1 20070809 A 5542 SKIN DOUG DC8 DC873F 302199F WP RUDDER CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, RUDDER EXT SKIN WITH CORROSION AT STA ZR -162.000 RT SIDE. 2 L 7 4 4F RT 4A25 2007083100176 20070831 00176 WP 2007 8 31 IXXA07SMN203S 1 20070809 A 5542 SKIN DOUG DC8 DC873F 302199F WP RUDDER CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, RUDDER EXT SKIN WITH CORROSION AT STA ZR -253.000 RT SIDE. 2 L 7 4 4F RT 4A25 2007083100177 20070831 00177 WP 2007 8 31 IXXA07SMN204S 1 20070809 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 980 DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, EXT FUSELAGE UPPER SKIN WITH DENT AT STA FS 980.000 AND L-7 LT. 2 L 7 4 4F RT 4A25 2007083100178 20070831 00178 WP 2007 8 31 IXXA07SMN200S 1 20070809 A 5730 SKIN DOUG DC8 DC873F 302199F WP LWS 247 DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, LT WING NON STANDARD REPAIR ON INBD SLOT VANE AT STA XS 247.000. 2 L 7 4 4F RT 4A25 2007083100179 20070831 00179 NM 2007 8 31 2007UALA03335 1 20070822 A 5320 FASTENER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE IMPROPER PART A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 REPAIR AT BS 294-303 AT STR 27L FOUND WITH BLIND FASTENERS. REMOVED BLIND FASTENERS AND REPLACED WITH SOLID FASTENERS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007083100181 20070831 00181 WP 2007 8 31 IXXA07SMN211S 1 20070817 A 5313 LONGERON SPLICE DOUG DC8 DC873F 302199F WP BS 1690 L36 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT LONGERON SPLICE FITTING CRACKED AT STA 1690.000 L-36. 2 L 7 4 4F RT 4A25 2007083100183 20070831 00183 WP 2007 8 31 IXXA07SMN212S 1 20070817 A 5753 SKIN DOUG DC8 DC873F 302199F WP LT WING TE FLAP DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, LT WING INBD FLAP UPPER SKIN SHOWS DENT AT XW 88.000. 2 L 7 4 4F RT 4A25 2007083100184 20070831 00184 WP 2007 8 31 IXXA07SMN199S 1 20070809 A 5753 SKIN DOUG DC8 DC873F 302199F WP LT WING TE FLAP DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, LT WING OTBD FLAP LWR SKIN PANEL SHOWS (04EA) DENTS BETWEEN STA XF 415.000 AND STA XF 453.000. 2 L 7 4 4F RT 4A25 2007083100187 20070831 00187 SO 2007 8 31 RAIA00708038 1 20070822 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 813HK 145044 PRE FLT 5526 - STL - EMERGENCY AT ROW 3 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007083100188 20070831 00188 WP 2007 8 31 IXXA07SMN225S 1 20070821 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1367 L30L MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, FS 1367, LONGERON 30.5 LEFT, DOUBLER BELOW AND AFT OF AFT EMERGENCY EXIT DOOR. REPAI R NUMBER 606AL-R37. PROBLEM: SIDE 2 ENDS ON LONGERON WITHOUT FINGER DOUBLER. DISPOSITION: UPGRADE IAW SRM. 2 L 7 4 4F RT 4A25 2007083100190 20070831 00190 WP 2007 8 31 IXXA07SMN223S 1 20070821 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 80 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, MAIN CARGO LT CUSP EXTRUSION, FITTING WITH CORROSION AT STA 80.000, L-21L. 2 L 7 4 4F RT 4A25 2007083100191 20070831 00191 SO 2007 8 31 RAIA00708037 1 20070821 A 3350 LIGHT EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 826HK 145016 PRE FLT 5586 - STL - FORWARD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT. OPS CH ECKED GOOD. 2 L 7 2 4F RT T00011AT 2007083100193 20070831 00193 WP 2007 8 31 IXXA07SMN224S 1 20070821 A 5310 STRUCTURE DOUG DC8 DC873F 302199F WP BS 1345 L30L MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, FS 1345, LONGERON 30.5 LEFT. DOUBLER BELOW AND AFT OF AFT EMERGENCY EXIT DOOR. REPA IR NUMBER 606 AL-R36. PROBLEM: SIDE 2, 2ND ROW EXCEEDS MAS RIVET SPACING. DISPOSITION: ADD RIVETS TO BRING INTO LIMITS OR UPGRADE. 2 L 7 4 4F RT 4A25 2007083100194 20070831 00194 EA 2007 8 31 SIMA200723604 1 20070820 A 5320 S61444 BRACKET CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 505AE 11594 5000 10053 RIGHT TEE BRACKET AT FS 280 WAS CRACKED. REPAIRED DEFECT IAW BOMBARDIER AEROSPACE REPAIR ENGINEERING ORDER 670-53-11-04 5. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007083100195 20070831 00195 SO 2007 8 31 SIMA200723602 1 20070823 A 2460 14529739401 CONTROL PANEL EMB 135 EMB135KL 3260302 SO COCKPIT SMOKE A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 807AE 14370 145506 AFTER GPU CONNECTED ELECTRICAL SMOKE COMING FROM OVER HEAD PANEL, POST INSPECTION REVEALED ELECTRIC PUMP CIRCUIT BREAKER HAD BURNING ODOR. REMOVED AND REPLACED HYDRAULIC CONTROL PANEL IAW EMB AMM 20-13-10. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007083100196 20070831 00196 SO 2007 8 31 SIMA200723603 1 20070823 A 3350 78812 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 647AE 17173 145222 EMERGENCY FLOOR LIGHT STRIP ROW 7 THROUGH 12 INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLOOR PROXIMITY STRIP LIGHT IA W EMB AMM 33-50-12. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007083100197 20070831 00197 SO 2007 8 31 CHQA200700041 1 20070821 A 3320 BR900022 BALLAST EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL SEAT 18A BURNED OUT A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 575RP 145847 CAE312676 JFK TO IND JUST AFTER LIFT OFF RECEIVED THE "LAV SMOKE" WARNING. FA CHECKED FOR SMOKE OR FIRE AND NOTICED A HOT ELECTRI CAL BURNING SMELL IN THE REAR OF THE CABIN. THE SMELL QUICKLY DISSIPATED. FLIGHT CREW DECLARED AN EMERGENCY AND RAN TH ROUGH THE APPROPRIATE CHECK LISTS. RETURN LAND AT JFK NORMAL AND CLEARED RUNWAY, TAXIED BACK TO GATE AND SHUT DOWN AIRC RAFT. MAINTENANCE RAN ENGINES AND DID NOT SEE OR SMELL SMOKE DURING ENGINE RUNS, INSPECTED AIRCRAFT AND FOUND BALLAST F OR CEILING LIGHTS OVER SEAT 18A BURNT OUT. MAINTENANCE REPLACED BALLAST, NO FURTHER DEFECTS NOTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007083100198 20070831 00198 NM 2007 8 31 UIEA200700297 1 20070726 A 5315 FLOORBEAM BOEING 747 747271C 1384869 NM BS 440 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 CRACK INDICATION IN RIGHT SIDE OF UPPER DECK FLOORBEAM FUSELAGE STA 440 3RD AND 4TH HOLES FROM THE OUTBOARD TOP ROW OF F ASTENERS STRAP AREA OF UPPER CORD REF S/B 747-53A2449 FIG 2 STEP 2. DISASSEMBLED AREA AT STA 440 DISCOVERED CRACKS IN F RAME WEB AND CRACKED SPLICE DOUBLER. INSTALLED NEW SECTION IAW SRM 51-20-01 AND SRM 51-30-02. 2 L 7 4 4F A20WE 2007083100199 20070831 00199 NM 2007 8 31 UIEA200700298 1 20070726 A 5315 FLOORBEAM BOEING 747 747271C 1384869 NM ZONE 200 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 CRACK INDICATION IN LEFT SIDE OF UPPER DECK FLOORBEAM FUSELAGE STA 360 5TH AND 8TH HOLES FROM THE OUTBOARD STRAP AREA OF UPPER CORD REF S/B 747-53A24201 FIG 2 STEP 2. INSTALLED FRAME WEB REPAIR REPLACEMENT PARTS IAW SRM 53-10-04 FIG 103 DE TAIL 2. 2 L 7 4 4F A20WE 2007083100200 20070831 00200 NM 2007 8 31 UIEA200700299 1 20070726 A 5315 FLOORBEAM BOEING 747 747271C 1384869 NM ZONE 200 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 CRACK INDICATION IN LEFT SIDE OF UPPER DECK FLOORBEAM FUSELAGE 6, 7 AND 8TH HOLES FROM OUTBOARD TOP ROW OF FASTENERS STR AP AREA OF UPPER CHORD REF S/B 747-53A24201 FIG 2 STEP 2. REMOVED CRACKED CHORD SECTION REMOVED CRACKED WEB SECTION FAB RICATED AND INSTALLED NEW WEB SECTION AND REPAIR DOUBLER . FIT AND INSTALLED CHORD REPAIR KIT 141U0044-115 REINSTALLED PARTS REMOVED FOR REPAIR INCLUDING STIFFENERS ON FWD SIDE OF FLOORBEAMS COVERED BY BOEING MESSAGE 1-404648834-7 REF S/B 747-53A2429R1 AND DRAWING NR 141U0044 SHEET 4. 2 L 7 4 4F A20WE 2007083100221 20070831 00221 NM 2007 8 31 SWAA074168 1 20070823 A 5330 6545866 SKIN BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 20Y CHECK, FOUND KEEL BEAM SKIN CRACKED BETWEEN BS 695 AND BS 705, LBL 6.5. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007083100244 20070831 00244 EU 2007 8 31 TRBA2007071 1 20070820 A 3350 3011210 LIGHT AEROSP ATR72 ATR72212 8680945 EU CABIN FAILED A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 434AT 434 PAX DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY IAW CMM NR 33-51-26. PERFORMED OP CK. 2 H 7 2 4T RT A53EU 2007083100245 20070831 00245 NM 2007 8 31 AWXA200701010 1 20070822 A 5314 6562125 KEELBEAM BOEING 737 7373S3 1384711 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 PHX - MAJOR REPAIR - CORROSION ON KEEL BEAM CHORD, BS 500C - BS 500D, S28R. REPAIRED KEEL BEAM CHORD, BS 500C - BS 500D , S28R PER US AIRWAYS EA 120167. 2 L 7 2 4F RT A16WE 2007083100247 20070831 00247 NM 2007 8 31 QXEA200701350 1 20070824 A 3150 WARNING LIGHT DHAV DHC8 DHC8202 2809007 NM FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 345PH 476 SEA FLIGHT NR 2145 - AFTER PERFORMING THE "TO WARNING TEST" NR 1 ENGINE MANUAL CAUTION LIGHT ILLUMINATED. COMPLIED WITH BETA LOCKOUT RESET PER AMM 76-10-16. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007083100248 20070831 00248 NM 2007 8 31 AWXA200701011 1 20070822 A 2611 RAI2800M0706 CONTROL BOX AIRBUS A319 A319132 3930340 NM SMOKE DETECTION FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 839AW 26097 26097 2669 PHX - OTH - MX REPORTED LAV CRG DET FAULT MESSAGE ILLUMINATED. MX REPLACED THE SMOKE DETECTOR SMOKE UNIT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007083100249 20070831 00249 WP 2007 8 31 IXXA07SMN222S 1 20070817 A 5711 SPAR DOUG DC8 DC873F 302199F WP WING CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, NR 2 MAIN TANK WEB OF CENTRAL SPAR (LWR SIDE) CRACKED 2 1/2" AT STA XRS 172.000 BETWE EN S-61 AND S-62. 2 L 7 4 4F RT 4A25 2007083100250 20070831 00250 NM 2007 8 31 NWAA072915508 1 20070823 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 508US 23197 DURING OVERNIGHT CHECK, FOUND RIGHT PASSENGER DOOR 1 SLIDE LIGHT WAS INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPL Y. OPERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007083100251 20070831 00251 NM 2007 8 31 AALA20071465 1 20070808 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 779AN 29955 MIA - EMERGENCY LIGHT AT SEAT 9D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT T00001SE 2007083100252 20070831 00252 NM 2007 8 31 AALA20071459 1 20070720 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 758AN 32637 AFW - EMERGENCY LIGHT IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007083100254 20070831 00254 NM 2007 8 31 AALA20071466 1 20070808 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 779AN 29955 TUL - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 37C TO AFT OF CABIN INOPERATIVE. REPLACED BATTERY PACK AT LEFT NUMBER THRE E DOOR FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 37C TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007083100255 20070831 00255 NM 2007 8 31 AALA20071467 1 20070808 A 2510 MASK BOEING 777 777223 1385213 NM COCKPIT LEAKING A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 770AN 29578 ANC INFLIGHT T169/08AUG - CREW FOUND OXYGEN TEST BUTTON STUCK. CREW OXYGEN BOTTLE HAS LOW PRESSURE. LANDED ANC WITHOU T INCIDENT. FOUND FIRST OBSERVER MASK LEAK. REPLACED FIRST OBSERVER MASK ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERA TION. 2 L 7 2 4F RT T00001SE 2007083100256 20070831 00256 NM 2007 8 31 AALA20071462 1 20070723 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 931AN 30079 TUL - EMERGENCY LIGHT AT LEFT AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT AFT GALLEY. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007083100257 20070831 00257 NM 2007 8 31 AALA20071463 1 20070724 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 931AN 30078 TUL EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD ENTRY DOOR . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007083100258 20070831 00258 NM 2007 8 31 AALA20071458 1 20070718 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 940AN 30598 TUL - EMERGENCY LIGHT IN COACH CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN COACH CABIN. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007083100260 20070831 00260 2007 8 31 AALA20071464 4 20070806 A 2565 69B14855Y1 GIRT BAR BOEING 757 757223 1384957 NM ESCAPE SLIDE MISLOCATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 698AN 26980 MEX - FOUND LEFT NUMBER ONE ESCAPE SLIDE GIRT BAR OUT OF PLACE. REPOSITIONED LEAF SPRING AT DOOR FOR LEFT NUMBER ONE E SCAPE SLIDE GIRT BAR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007083100261 20070831 00261 NM 2007 8 31 AALA20071460 1 20070720 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 758AN 32637 AFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIGHT NUMBER O NE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007083100262 20070831 00262 NM 2007 8 31 AALA20071461 1 20070720 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 758AN 32637 AFW - EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIGHT NUMBER T WO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007083100263 20070831 00263 NM 2007 8 31 AWXA200701013 1 20070814 A 5754 65C2679414 SKIN BOEING 737 7373G7 1384595 NM ZONE 600 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - CRACKS FOUND ON NR 5 SLAT BOTTOM SKIN, SLAT STA 213 - SLAT STA 217. REPAIRED NR 5 SLA T BOTTOM SKIN SLAT STA 213 - SLAT STA 217 IAW B737-300 SRM 57-43-01-2, REPAIR 6. 2 L 7 2 4F RT A16WE 2007083100265 20070831 00265 NM 2007 8 31 AWXA200701014 1 20070815 A 5340 69366002 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5987939, CRACK FOUND AT L1 DOOR SURROUND STRINGER CLIP, BS 277, S-10L. REPLACED L1 DOOR SURROUND STRINGER CLIP, BS 277, S-10L IAW B737-300 SRM 51-40-02-0G, FIG 8 AND FIG 12. 2 L 7 2 4F RT A16WE 2007083100266 20070831 00266 NM 2007 8 31 AWXA200701015 1 20070815 A 5340 69489856 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5987940, CRACK FOUND AT L1 DOOR SURROUND STRINGER CLIP, BS 360, S-11L. REPLACED L1 DOOR SURROUND STRINGER CLIP, BS 360, S-11L IAW B737-300 SRM 51-40-02-0G, FIG 8 AND FIG 12. 2 L 7 2 4F RT A16WE 2007083100267 20070831 00267 NM 2007 8 31 AWXA200701016 1 20070814 A 5754 65C2679310 SKIN BOEING 737 7373G7 1384595 NM ZONE 600 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5987798, CRACKS FOUND ON NR 4 SLAT BOTTOM SKIN, SLAT STA 55 - SLAT STA 87. REPAIRE D NR 4 SLAT BOTTOM SKIN, SLAT STA 55 - SLAT STA 87 IAW B737-300 SRM 57-43-01-2, REPAIR 6, FIG 201. 2 L 7 2 4F RT A16WE 2007083100268 20070831 00268 NM 2007 8 31 AWXA200701017 1 20070814 A 5311 6558280511 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5987891, CRACK FOUND AT FUSELAGE FRAME, BS 360, S-14R - S-15R. REPAIRED FUSELAGE F RAME, BS 360, S-14R - S-15R IAW 737-300 SRM 53-00-07-2, REPAIR 7, FIG 201. 2 L 7 2 4F RT A16WE 2007083100269 20070831 00269 NM 2007 8 31 AWXA200701018 1 20070816 A 5315 65528941 FLOORBEAM BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - CRACK FOUND ON CABIN FLOOR SUPPORT CHANNEL ASSEMBLY, BS 540, LBL 25. REPLACED CABIN F LOOR SUPPORT CHANNEL ASSEMBLY, BS 540, LBL 25 IAW B737-300 SRM 51-40-04-0G, FIG 1. 2 L 7 2 4F RT A16WE 2007083100270 20070831 00270 WP 2007 8 31 07FDEA03077 1 20070823 A 3230 S4913807AT01728 CABLE DOUG MD10 MD1010F 3022112 WP MLG BROKEN A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 562FE 46947 AFTER TAKEOFF, RIGHT MAIN GEAR INDICATED UNSAFE ON BOTH PRIMARY AND SECONDARY WITH GEAR HANDLE UP. FOLLOWED QRH PROCEDU RES AND PUT GEAR HANDLE DOWN AND HAD GOOD DOWN AND LOCKED INDICATIONS. FOUND RIGHT MAIN GEAR FOLLOW UP GEAR UP CABLE RU N BROKEN. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOOR FOLLOW UP CABLE. PERFORMED GEAR SWING FOR OPERATIONAL CHEC K OF RIGHT MAIN LANDING GEAR DOOR. 2 L 7 3 4F RT A22WE 2007083100271 20070831 00271 WP 2007 8 31 07FDEA03110 1 20070824 A 5753 ARC24441 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 399FE 48262 LEFT WING INBOARD FLAP LOWER SKIN HAS SIX DENTS IN SAME AREA XORS299-372. REMOVED AND REPLACED SKIN SECTION AND DOUBLER ON WEDGE IAW MD/DC 10SRM 57-10-00 VOL I FIG 3, AND 51-35-01 VOL II. ALODINED AND PRIMERED IAW MD/DC10 SRM 51-21-01 VOL II. 2 L 7 3 4F RT A22WE 2007083100272 20070831 00272 NM 2007 8 31 07FDEA03111 1 20070824 A 5310 655457712 ANGLE BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD PIT BILGE BODY SKIN STIFFENER IS BUCKLED/CRACKED, BS 720B PLUS 13" 5", IB OF STR 28R, WL 148. REMOVED DAMAGE SUPPOR T ANGLE AND INSTALLED NEW SUPPORT ANGLE, REF BOEING DWG NR 65-54577 AND SRM 51-30-2, THIS IS CLASSIFIED AS A MAJOR REPAI R. 2 L 7 3 4F RT A3WE 2007083100273 20070831 00273 NM 2007 8 31 07FDEA03112 1 20070824 A 5340 69456281 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K O NONE OTHER O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD LWR CARGO PIT BILGE STRINGER TIE, ON PRESSURE BULKHEAD HAS CORROSION, STA 740, STR 27R. REMOVED CORRODED STRINGER T IES, FABRICATED NEW STRINGER TIES, AND INSTALLED. REF BOEING DRAWING NR 69-45628 AND SRM 51-30-02. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007083100311 20070831 00311 NM 2007 8 31 UPS07M50486 1 20070823 A 3020 WARNING SYSTEM DOUG MD11 MD11F 3023600 NM ANTI-ICE SYSTEM MALFUNCTIONED A IPXA K NONE N FALSE WARNING TO TAKEOFF 1 SO 01 278UP 48577 INSPECTION TYPE:N/A ATB - NR 2 ENGINE ANTI-ICE DUCT FAIL MESSAGE (CREW SHUT DOWN ENGINE). T/S PERFORMED IAW FIM 30-11-0 0-1. NO FAULTS FOUND. SYSTEM OK. 2 L 7 3 4F RT A22WE 2007083100342 20070831 00342 NM 2007 8 31 CALA0700456 1 20070825 A 5312 6545409 PRESSURE PANEL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A 1 INCH CRACK IN UPPER PRESSURE DECK IN MLG WHEEL WELL AT STA 664, RBL 38. REPAIRED IAW SRM 53-60-51, FIGURE 201. 2 L 7 2 4F RT A16WE 2007083100365 20070831 00365 EU 2007 8 31 AWXA200701019 1 20070810 A 5280 D5337062220400 FITTING AIRBUS 320 A320231 3930325 EU LT MLG DOOR WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 SAL - MAJOR REPAIR - C-06 CHECK - NR 5985453, WEAR ON FORWARD SUPPORT FITTING OF LT MAIN LANDING GEAR DOOR, BS 1869/FR 4 2, S-41L. REPLACED FORWARD SUPPORT FITTING OF LT MAIN LANDING GEAR DOOR, BS 1869/FR 42, S-41L IAW A320 SRM 51-72-11, PA GE 1. 2 L 7 2 4F RT A28NM 2007083100380 20070831 00380 NM 2007 8 31 SWAA074189 1 20070824 A 5322 6546529 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500C, STR 23L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007083100393 20070831 00393 NM 2007 8 31 SWAA074209 1 20070825 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007083100400 20070831 00400 NM 2007 8 31 SWAA074214 1 20070826 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 2007083100401 20070831 00401 NM 2007 8 31 SWAA074197 1 20070824 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007083100402 20070831 00402 NM 2007 8 31 SWAA074216 1 20070826 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007083100404 20070831 00404 NM 2007 8 31 SWAA074210 1 20070826 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007083100406 20070831 00406 NM 2007 8 31 SWAA074198 1 20070824 A 5322 69353656 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 380, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007083100408 20070831 00408 NM 2007 8 31 SWAA074211 1 20070826 A 3350 B21506 FUSE BOEING 737 7377H4 1384404 NM BATTERY CHARGER FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 749SW 29801 DURING SCHEDULED 8Y CHECK, FOUND FWD CABIN EMERGENCY EXIT BATTERY CHARGER INOP. REMOVED AND REPLACED BATTERY CHARGER FU SES PER MM. 2 L 7 2 4F RT A16WE 2007083100409 20070831 00409 NM 2007 8 31 SWAA074196 1 20070824 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER 20R CORRODED AT BS 500C. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007083100410 20070831 00410 NM 2007 8 31 SWAA074188 1 20070824 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER 21L CORRODED AT BS 500A. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007083100411 20070831 00411 NM 2007 8 31 SWAA074195 1 20070824 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER 25R CORRODED AT BS 350. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007083100412 20070831 00412 NM 2007 8 31 SWAA074194 1 20070824 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER 21L CORRODED AT BS 370. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007083100413 20070831 00413 2007 8 31 SWAA074186 4 20070826 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 1/2D THRU CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007083100414 20070831 00414 NM 2007 8 31 SWAA074201 1 20070825 A 3297 D4536P CONNECTOR BOEING 737 7373H4 1384600 NM MLG W/W FAULTY A SWAA K NONE N FALSE WARNING NR NOT REPORTED 1 SW 29 318SW 23339 RIGHT MLG RED LIGHT ILLUMINATED INTERMITTENTLY DURING FLIGHT. REMOVED AND REPLACED UPLOCK SENSOR AND CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2007083100415 20070831 00415 NM 2007 8 31 SWAA074212 1 20070826 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 749SW 29801 DURING SCHEDULED 8Y CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007083100417 20070831 00417 SO 2007 8 31 SWIA200718622 1 20070820 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DAMAGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 227SW 120304 EMERGENCY EXIT LIGHT ON OVERHEAD BIN AT ROW 9 IS INOP, FLIGHT NR 5639. INSTALLED A NEW WIRE SPLICE. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007083100418 20070831 00418 NE 2007 8 31 COMA0760529 2 20070815 A 7200 CF343A1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE RIGHT LEAKING A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 969CA 19034 7141 807552 FLIGHT 9432 - RECEIVED RIGHT ENGINE OIL PRESSURE WARNING MESSAGE. DIVERTED TO PIT, LANDED WITHOUT INCIDENT. REPLACED R IGHT ENGINE. NO FURTHER DEFECTS. 2 L 7 2 4F 4 F RT A21EA E15NE 2007083100419 20070831 00419 EA 2007 8 31 SWIA200718623 1 20070812 A 2150 GG670950091 ACM CNDAIR CL600 CL6002C10 1390015 EA RIGHT SEIZED A SWIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 709SK 10159 ON TAXI OUT, THE FLIGHT ATTENDANT CALLED WITH SMOKE IN THE CABIN. CREW GOT A RIGHT PACK AUTO FAIL, FLIGHT NR 5947. REP LACED RIGHT ACM IAW AMM 21-51-08. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007083100421 20070831 00421 2007 8 31 SWIA200718625 4 20070822 A 2210 6229815704 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 924SW 7681 UNCOMMANDED RUDDER MOVEMENT IN CLIMBOUT WITH AUTO PILOT ON, FLIGHT NR 5838. REPLACED FCC NR 2 IAW 22-12-14. OPS CK GOO D. 2 L 7 2 4F RT A21EA 2007083100422 20070831 00422 EA 2007 8 31 SWIA200718626 1 20070822 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA MLG OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 958SW 7833 NOSE GEAR DISAGREE AFTER SELECTING GEAR UP AFTER TAKEOFF. RETURNED TO FIELD, FLIGHT NR 6378. ADJUSTED NOSE GEAR PROX S ENSOR BRACKET AND PERFORMED NOSE GEAR SWING. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007083100423 20070831 00423 EA 2007 8 31 SWIA200718627 1 20070820 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 913EV 7731 FORWARD CEILING EMERGENCY LIGHT INOP, FLIGHT NR 3845. RELAMPED FORWARD CEILING EMERGENCY LIGHT. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007083100424 20070831 00424 SO 2007 8 31 SWIA200718628 1 20070823 A 3350 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS BURNED OUT A SWIA O OTHER L NO TEST UK UNKNOWN 1 NM 07 234SW 120308 RIGHT OVERWING EMERGENCY EXIT SIGN IS NOT ILLUMINATING, FLIGHT NR 5737. RELAMPED EMERGENCY EXIT SIGN. OPS CHECKED GOOD . 2 L 7 2 4T RT A31SO 2007083100425 20070831 00425 EA 2007 8 31 A6WA200740470 1 20070820 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 467AW 7900 LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 54.897 (540BB, HOLE NR 1) HAS FRETTING DAMAGE AT INBOARD AND OU TBOARD ENDS. INBOARD END MEASURES APPROX 9.5 INCH BY .30 INCH BY .004 INCH DEEP. OUTBOARD END MEASURES APPROX 4.5 INCH BY .30 INCH BY .004 INCH DEEP IN NON-CRITICAL AREA. MAINTENANCE REPAIRED FRETTING DAMAGE IAW REO 601R-57-21-030 REV F . (M) 2 L 7 2 4F RT A21EA 2007083100426 20070831 00426 EA 2007 8 31 A6WA200740471 1 20070820 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 467AW 7900 RIGHT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 54.897 9640BB, HOLE NR 1) HAS FRETTING DAMAGE AT INBOARD AND O UTBOARD ENDS OF CUTOUT IN NON-CRITICAL AREA. INBOARD AREA MEASURES APPROX 6 INCH LENGTH BY .30 INCH WIDE BY .005 INCH D EEP. OUTBOARD AREA MEASURE APPROX 5.5 INCH LONG BY .30 INCH WIDE BY .005 INCH DEEP. OUTBOARD AREA MEASURE APPROX 5.5 I NCHES LONG BY .30 INCHES WIDE BY .005 INCHES DEEP. MAINTENANCE REPAIRED CORRODED (FRETTING) DAMAGE AREAS IAW REO 601R-5 7-21-030 REV F. (M) 2 L 7 2 4F RT A21EA 2007083100427 20070831 00427 EA 2007 8 31 A6WA200740473 1 20070820 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 467AW 7900 FOUND LT FS 621 FLOORBEAM ANGLE CRACKED. MAINTENANCE REPAIRED LT FS 621 FLOORBEAM ANGLE BY CUTTING AWAY DAMAGE AREA AND INSTALLING REPAIR PARTS IAW BOMBARDIER REO 601R-53-61-117 REV C. (M) 2 L 7 2 4F RT A21EA 2007083100428 20070831 00428 EA 2007 8 31 A6WA200740469 1 20070820 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 467AW 7900 LT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 12.245 (510AB, HOLE NR 2) HAS FRETTING DAMAGE AROUND ENTIRE CIRCU MFERENCE OF HOLE, IN CRITICAL AREA, APPROX .30 INCH WIDE BY .006 INCH DEEP. MAINTENANCE REPAIRED DAMAGED AREA IAW REO 601R-57-21-030 REV F. (M) 2 L 7 2 4F RT A21EA 2007083100429 20070831 00429 EA 2007 8 31 A6WA200740477 1 20070821 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 424AW 7656 FOUND FS 280 INBOARD AND OUTBOARD STRINGER CLIP AT LBL 9 ARE CRACKED. MAINTENANCE REMOVED AND REPLACED 280 STRINGER CLI P IAW CRJ 200 SRM 51-42-21 AND 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007083100430 20070831 00430 EA 2007 8 31 A6WA200740480 1 20070822 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 424AW 7656 FOUND FS 484 FLOOR SUPPORT BEAM INTERCOSTAL ANGLE AT RBL 36 IS CRACKED. MAINTENANCE REPAIRED CRACKED ANGLE BY REMOVING CRACKED ANGLE AND FABRICATED NEW ANGLE AND INSTALLED SERVICEABLE ANGLE IAW BSC STANDARD REPAIR 601R-53-0030A AND REO 60 1R-53-41-059 REV A. (M) 2 L 7 2 4F RT A21EA 2007083100431 20070831 00431 EA 2007 8 31 A6WA200740481 1 20070822 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 460 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 424AW 7656 FOUND FS 460 FLOORBEAM ANGLE AT RBL 9 IS CRACKED. MAINTENANCE REPAIRED FS 460 FLOORBEAM ANGLE AT RBL 9 BY REMOVING DAMA GED ANGLE AND INSTALLING NEW ANGLE IAW CRJ 200 SRM 51-42-06, 51-42-20, 51-42-21 AND BSC EO 601R-53-12916. (M) 2 L 7 2 4F RT A21EA 2007083100432 20070831 00432 EA 2007 8 31 A6WA200740478 1 20070821 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 424AW 7656 FOUND FS 280 INBOARD AND OUTBOARD CLIPS AT RBL 9.0 ARE CRACKED. MAINTENANCE REMOVED AND REPLACED TWO 280 CLIPS IAW CRJ 200 SRM 51-42-21 AND 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007090400001 20070904 00001 CE 2007 9 4 DXTA200702412 1 20070819 A 3260 S33682 BULB CESSNA 500 560CESSNA 2076750 CE COCKPIT BURNED OUT E DXTA A UNSCHED LANDING P NO WARNING INDICATION DE DESCENT 1 GL 07 820QS 2960 5600650 LEFT MAIN GEAR LIGHT DID NOT ILLUMINATE. PRESSURE BOTTLE WAS USED TO BLOW DOWN GEAR.REPLACED BAD BULB- OPS CHECK GOOD IA W CE560 MM 32-60-00. BLED HYD SYSTEM & SERVICED BLOW DOWN BOTTLE IAW CE560 MM 12-13-01. 2 L 7 2 4F RT A22CE 2007090400002 20070904 00002 CE 2007 9 4 DXTA200702413 1 20070820 A 3222 STRUT CESSNA 750 750 2076810 CE NLG UNDERSERVICED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 945QS 7500029 ON TAKE OFF GEAR WOULD NOT RETRACT. PERFORMED SEVERAL SATISFACTORY GEAR SWINGS. CHECKED RIGGING OF SQUAT SWITCHES CHECK ED GOOD. CHECKED GEAR HANDLE SOLENOID . CHECKED GOOD. CHECKED NWS CENTERING AND CHECKED GOOD. FOUND NOSE STRUT SERVICE L OW PERHAPS CAUSING NLG SQUAT SWITCH TO MAKE. SERVICED IAW CH 12-10-38 OF THE CE-750 M/M. 2 L 7 2 4J RT T00007WI 2007090400003 20070904 00003 CE 2007 9 4 DXTA200702415 1 20070821 A 4990 7547512 BYPASS VALVE CESSNA 750 750 2076810 CE AFT SERVICE BAY INOPERATIVE E DXTA O OTHER K W B FLUID LOSS INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 908QS 7262 7500108 AN EXCESSIVE ODOR OF BURNING OIL IS PRESENT THROUGHOUT CABIN. FOUND APU OIL OVER SERVICED. REMOVED 0.5 CAPS OIL TO BRING APU OIL TO SERVICEABLE LEVEL. INSPECTED AND CLEANED AIR DELIVERY LINES FROM WATER SEPERATOR LEFT SIDE TO THE PERSSURE B ULKHEAD. REPLACED FWD ECU BYPASS VALVE CONTROLLER (ANTI-ICE) WITH REPAIRED UNIT. OPS CHECK GOOD AND NO ODOR OF BURNING O IL PRESENT AT THIS TIME. DONE IN REF- TO CE-750 MM 21-51-00 AND 21-52-00. 2 L 7 2 4J RT T00007WI 2007090400004 20070904 00004 CE 2007 9 4 DXTA200702416 1 20070822 A 2700 7002800901 ACTUATOR CESSNA 750 750 2076810 CE YAW DAMPER INOPERATIVE E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 944QS 6779 7500144 DURING TAKEOFF ROLL APPROXIMATELY 80 KTS, YAW DAMP OFF LOWER B CAS MESSAGE. REMOVED FAILED NR 2 LINEAR ACTUATOR, INSTALL ED REPAIRED NR 2 LINEAR ACTUATOR, IAW CESSNA 750 MM 27-24-00 08/23 OPPS CHECK GOOD. 2 L 7 2 4J RT T00007WI 2007090400005 20070904 00005 CE 2007 9 4 DXTA200702414 1 20070820 A 2150 73838433 ACM CESSNA 750 750 2076810 CE AFT SERVICE BAY LEAKING E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 905QS 4671 4671 7500105 COCKPIT AND CABIN FILLED WITH BLUE/BLACK SMOKE. REMOVED AND REPLACED FORWARD ACM AND COALESCERS AND ORING FOR L/H AND R/ H SEPARATOR. OPS CHECK AND LEAK CHECK GOOD. ALL WORK DONE IAW 21-51-00 OF THE CE750 M/M. 2 L 7 2 4J RT T00007WI 2007090400008 20070904 00008 EU 2007 9 4 MALA070104 1 20070823 A 2120 UNKNOWN SAAB SF340 340B 7860101 EU COCKPIT ODOR A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 426XJ 340B426 CREW REPORTED IN FLIGHT BURNING ODOR IN FLIGHT DECK AT HIGH POWER SETTINGS. COMPLETED OPERATIONAL CHECK OF AUTO AND MAN UAL TEMP CONTROL IAW TASK CARD 2150-301. RAN IN FULL HOT AND FULL COLD FOR SEVERAL MINUTES. COULD NOT DUPLICATE. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2007090400010 20070904 00010 EU 2007 9 4 SIMA200723903 1 20070826 A 2750 FLAP SYSTEM SAAB SF340 340B 7860101 EU TE FLAPS OUT OF RIG A SIMA L ABORTED APPROACH F FLT CONT AFFECTED DE DESCENT 1 SW 21 250AE 340B250 SELECT FLAPS TO 15 DEGREES WITH NO MOVEMENT, ABORTED APPROACH, SELECTED FLAPS TO 15 DEGREES ON SECOND APPROACH WITH MOVE MENT. FOUND FLAPS ELECTRICALLY OUT OF RIG. PERFORMED ELECTRICAL RIGGING OF FLAPS IAW SAAB AMM. OPERATIONAL CHECK GOOD . RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007090400011 20070904 00011 GL 2007 9 4 SIMA200723901 2 20070824 A 7200 AE3007A13 ENGINE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL ZONE 400 FAILED A SIMA B E EMER. DESCENT ENGINE SHUTDOWN B G J SMOKE/FUMES/ODORS/SPARKS MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 SW 21 853AE 10869 4110 145742 CAE312297 UNCOMMAND ENGINE 2 SHUTDOWN WITH E2 OUT EICAS MESSAGE FOLLOWED BY PUFF OF SMOKE ON FLIGHT DECK AND CABIN WITH LOSS OF P RESSURIZATION, POST INSPECTION FOUND ENGINE QUILL SHAFT SHEARED. REMOVED AND REPLACED NUMBER 2 ENGINE IAW AMERICAN EAGL E WORK CARD. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007090400012 20070904 00012 SO 2007 9 4 SIMA200723904 1 20070826 A 2121 FAN EMB 135 EMB135KL 3260302 SO OBSTRUCTED A SIMA O OTHER M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 826AE 145592 ACID BURNING ODOR ON FLIGHT DECK AND CABIN ON TAXI IN, NO VISIBLE SMOKE. FOUND INSULATION SUCKED INTO BOTH COOLING FANS . REPAIRED INSULATION IAW EMB AMM 25-81-01. PERFORMED GROUND ENGINE RUNS WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007090400013 20070904 00013 EU 2007 9 4 SIMA200723902 1 20070824 A 3240 426833 CONTROL BOX SAAB SF340 340B 7860101 EU BRAKES FAILED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 238AE 19289 7822 340B238 ANTI-SKID INOPERATIVE MESSAGE, ABORTED TAKEOFF. REMOVED AND REPLACED BRAKE CONTROL BOX IAW SAAB AMM 32-43-85. OPERATIO NAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007083100048 20070831 00048 WP 2007 8 31 WX0A070147 1 20070817 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS NO TEST A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 860GA 49786 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007083100051 20070831 00051 EU 2007 8 31 07FDEA03065 1 20070823 A 5753 RIB AIRBUS 310 A310324 3930206 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 SEVERAL OLD REPAIRS ON LT INBOARD FLAP, AT T/E AND RIB 9 AND 10 POSITION. REPAIRS PERFORMED BY REPLACEMENT OF TRAILING EDGE, REPAIR OF DAMAGED RIB FLANGE IAW SRM 57-52-11/FIG 202 AND REPAIR OF FLAP CENTER WING BOX DAMAGE WITH EXTERNAL DOUB LER IAW SRM 57-52-12/FIG 205. REPAIRS COVERED IN EA 6-5752-101278 AND RAS/DABRE/7006846/2006 ISS "B". 2 L 7 2 4F RT A35EU 2007083100057 20070831 00057 SO 2007 8 31 C2XA07CL072 1 20070823 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 16918 145397 CLE FLIGHT 2221 - THE CREW REPORTED IN FLIGHT THE F/A AND PASSENGER SMELLED SOMETHING BURNING IN THE MAIN CABIN. NO BUR NING SMELL WAS NOTED IN THE COCKPIT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE PACK SYSTEM IAW 21-51-00 AND PERFO RMED OPERATIONAL CHECK OF THE ANTI-ICE SYSTEM. NO DEFECTS WERE FOUND. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007083100084 20070831 00084 NM 2007 8 31 2007UALA03268 1 20070820 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN IMPROPER PART A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 179UA 25158 SEAT EEL LIGHTS WRONG PART INSTALL AT SEAT 1J (AFT) 1A (FWD) AND 3A (AFT). 08-31-07 RELAMPED WITH CORRECT EEL LAMP, TWO POSITIONS. OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100088 20070831 00088 NM 2007 8 31 2007UALA03272 1 20070820 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EEL LIGHT ASSY INOP AT SEATS 22AB THRU 26AB. REPLACED BATTERY ASSY. EEL LIGHTS OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100094 20070831 00094 NM 2007 8 31 2007UALA03278 1 20070820 A 3350 STRIP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 672UA 30027 SEATS 2L & 3R ARE MISSING THE AFT EEL STRIP SECTION. INSTALLED LAMP ASSEMBLY IN BOTH SEAT POSITIONS. OP CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007083100104 20070831 00104 EU 2007 8 31 07FDEA03103 1 20070824 A 5340 A5377364420600 FITTING AIRBUS 310 A310203 3930313 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 FWD PIT, FRAME FITTING CRACKED, FR 36, (STA. X1976) BL 60L (Y1520). 09-04-07 REMOVED AND REPLACED FRAME FITTING IAW A 310-200 SRM51-40-21, PART 6 & 7. 2 L 7 2 4F RT A35EU 2007083100108 20070831 00108 NM 2007 8 31 2007UALA03289 1 20070820 A 2612 CONNECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FIRE WARNING SYS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 304UA 23665 A-LOOP INOP ON FIRE TEST ON NR 2 ENGINE. REPLACED THE FAN LOWER FIRE LOOP AND CONNECTOR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007083100118 20070831 00118 NM 2007 8 31 2007UALA03298 1 20070820 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 UPPER DECK EMERGENCY EXIT CEILING LIGHT INOP BETWEEN ROW 15 AND 16. REPLACED THE LAMP, CHECKED OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100137 20070831 00137 EU 2007 8 31 07FDEA03108 1 20070824 A 5313 A53974202226 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT CARGO PIT, STR 45R CORRODED, FR 54.2 TO FR 54.3 (X3037 TO X3090) CUT OUT CORRODED SECTION OF STRINGER 45R, FROM STA X2984 TO X 3090, FABRICATED AND SPLICED IN REPAIR SECTION, IAW A310-200 SRM 53-10-14 FIG 201, 51-71-30 FIG 202, 51-40-2 1 PAR 6, 51-21-10 AND 51-23-10. 2 L 7 2 4F RT A35EU 2007083100144 20070831 00144 WP 2007 8 31 IXXA07SMN220S 1 20070817 A 5711 SPAR DOUG DC8 DC873F 302199F WP RT WING CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, NR 1 MAIN TANK CTR SPAR WEB LWR SIDE, CRACK 4" AT STA XRS 255.000 BETWEEN S-61 AND S- 62. 2 L 7 4 4F RT 4A25 2007083100145 20070831 00145 WP 2007 8 31 IXXA07SMN210S 1 20070813 A 5310 BEAM DOUG DC8 DC873F 302199F WP BS 50 DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, ACCESS CMPT CORROSION ON BEAM AT STA 50.000 AND RBL 35". 2 L 7 4 4F RT 4A25 2007083100146 20070831 00146 WP 2007 8 31 IXXA07SMN205S 1 20070813 A 5280 STRUCTURE DOUG DC8 DC873F 302199F WP NLG DOOR CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 46044 DURING ROUTINE C CHECK INSPECTION, RT AFT NLG DOOR, AFT DOOR STRUCTURE ATTACH ARM HAS CRACK FWD UPPER AREA (CRACKS IN FI LLER PNL NOT DOOR HINGE) FILLER PNL REMOVED. 2 L 7 4 4F RT 4A25 2007083100156 20070831 00156 NM 2007 8 31 2007UALA03326 1 20070822 A 3210 PLATE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RT MLG CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 RIGHT MLG SWING LINK BOLT THROUGH PLATE IS CORRODED AROUND BOLT HOLES. INSPECTED LEFT MLG BEAM FITTING RETAINING PIN LUGS FOR CRACKS, FOUND UPPER AND LOWER BOLT HOLES ELONGATED. REMOVED & REPLACED LEFT MLG FITTING AND SWING LINK ASSEM BLY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007083100169 20070831 00169 NM 2007 8 31 2007UALA03332 1 20070822 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 FLOORBEAM STA 246 T-CAP ANGLE CRACKED AT LBL 12, AFT SIDE. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKED SECTION OF CAP A NGLE. FABRICATED & INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 2007083100182 20070831 00182 NM 2007 8 31 2007UALA03337 1 20070822 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 674UA 29242 SEAT 31AB EEL LIGHT IS INOPERATIVE. REPLACED SEAT EEL WIRING. OP CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007083100189 20070831 00189 SO 2007 8 31 RAIA00708035 1 20070820 A 3350 RPSB1 POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 847HK 14500857 PRE FLT 8087 - STL - EMERGENCY LIGHT AT THE RIGHTHAND OVERWING EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE E MERGENCY LIGHT POWER SUPPLY. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007083100192 20070831 00192 SO 2007 8 31 RAIA00708039 1 20070823 A 2460 SWITCH EMB 145 EMB145LR 3260212 SO NR 1 AVIONICS DIRTY A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 829HK 145281 FLT 3508 - PIT - CREW REPORTED THAT WHILE PASSING THROUGH 100FL, CLICKING WAS HEARD FOLLOWED BY THE NR 1 AVIONICS MASTER SWITCH BUTTON POPPED OUT. MAINTENANCE CLEANED THE NR 1 AVIONICS SWITCH AND SYSTEM OPS CHECKED GOOD AS PER EMB145 AMM 2 4-62-00. 2 L 7 2 4T RT T00011AT 2007083100205 20070831 00205 NM 2007 8 31 SWAA074167 1 20070823 A 3350 1010745 SIGN BOEING 737 7373K2 13844BA NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 20Y CHECK, FOUND AFT CABIN EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM. 2 L 7 2 4F RT A16WE 2007083100233 20070831 00233 NM 2007 8 31 SWAA074178 1 20070823 A 5313 6551698 STRINGER SPLICE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 22L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007083100234 20070831 00234 NM 2007 8 31 SWAA074179 1 20070823 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007083100235 20070831 00235 NM 2007 8 31 UIEA200700320 1 20070816 A 5410 DOOR BOEING 747 747243B 1384830 NM NR 1 NACELLE PUNCTURED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 NR 1 PYLON OUTBOARD TRAILING EDGE DOOR INNER FACE PUNCTURED BY HOLD OPEN ROD WHEN DOORS ARE CLOSED 1.5 BY 1.5. PERM REP AIR CARRIED OUT IAW SRM 51-40-20 PAGE 1 250 DEGREES F. 2 L 7 4 4F A20WE 2007083100236 20070831 00236 NM 2007 8 31 P5CA0701530 1 20070819 A 3150 WARNING LIGHT BOEING 747 74746NF 13848BT NM GENERATORS FALSE ACTIVATION A P5CA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 15 453PA 30811 ELECT GEN 1, ELECT GEN 2, ELECT GEN 3 MESSAGES AFTER ENGINE START. RETURNED TO BLOCKS. PERFORMED GROUND TEST PER MM 24 -23-00. OPERATIONS NORMAL. 2 L 7 4 4F RT A20WE 2007083100237 20070831 00237 NM 2007 8 31 GTIA200700018 1 20070823 A 3350 321430 BATTERY PACK AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 505NK 5925 2485 ON CHECK, EMERG LIGHTS FAIL 11WL POSITION. REMOVED AND REPLACED 11WL BATTERY PACK. 2 L 7 2 4F RT A28NM 2007083100259 20070831 00259 NM 2007 8 31 KCSA071324 1 20070826 A 5330 SKIN BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FUSELAGE SKIN CRACKED AT 6 FASTENER HOLES BETWEEN BS 341 AND BS 344, STR 5L TO STR 5AL. 2 L 7 4 4F RT A20WE 2007083100323 20070831 00323 NM 2007 8 31 ASAA0741998 1 20070826 A 5242 6555830131 SKIN BOEING 737 737490 1384715 NM E&E BAY DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 28887 E&E COMPARTMENT DOOR DENTED ON RRIGHT EDGE. REMOVED DENTED SKIN, FABRICATED AND INSTALLED REPLACEMENT SKIN IAW SRM 51-3 0-01, 51-40-01 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007083100334 20070831 00334 NM 2007 8 31 ZZDA2007260 1 20070824 A 3350 8039251 BATTERY BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 939AT 55099 EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSY B5-118 REF WDM 33-51-14 AND OPS CHECK EMERGENCY LIGHTS REF AMM 33-51. 2 L 7 2 4F TR A6WE 2007083100336 20070831 00336 NM 2007 8 31 ZZDA2007261 1 20070824 A 3244 2613042 TIRE BOEING 717 717200 1383700 NM NR 3 FAILED A ZZDA O OTHER O OTHER LD LANDING 1 SO 37 955AT 55139 NR 3 TIRE FAILED. REMOVED AND REPLACED NR 3 MAIN TIRE AND WHEEL ASSY REF AMM 32-41. 2 L 7 2 4F TR A6WE 2007083100344 20070831 00344 NM 2007 8 31 SWAA074203 1 20070825 A 3350 101073 LENS BOEING 737 7377AD 1384502 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 798SW 28436 L1 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007083100363 20070831 00363 EA 2007 8 31 A6WA200740475 1 20070820 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 467AW 7900 RT FS 621 FLOOR SUPPORT ANGLE CRACKED. MAINTENANCE REPAIRED AREA IAW REO 601R-53-61-117 REV C. (M) 2 L 7 2 4F RT A21EA 2007083100394 20070831 00394 NM 2007 8 31 07FDEA03154 1 20070827 A 5754 SKIN DOUG MD11 MD11F 3023600 NM NR 5 SLAT DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 LEFT WING, NR 5 SLAT LEADING EDGE AREA FOUND WITH DENT. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 5 VOL.I. REPAIR C LASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007083100395 20070831 00395 NM 2007 8 31 SWAA074190 1 20070824 A 5313 6551698 STRINGER SPLICE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 25R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007083100396 20070831 00396 NM 2007 8 31 07FDEA03155 1 20070827 A 5711 SPAR CAP DOUG MD11 MD11F 3023600 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 LEFT WING, TRAILING EDGE REAR SPAR UPPER CAP AT STATION XORS 1042 FOUND CORRODED. COMPLIED WITH FEDEX E.A. 1-5710-1 15175, CLASSIFIED AS A MINOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007083100397 20070831 00397 NM 2007 8 31 SWAA074192 1 20070824 A 5313 6551698 STRINGER SPLICE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 26R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007083100398 20070831 00398 NM 2007 8 31 SWAA074193 1 20070824 A 5313 6551698 STRINGER SPLICE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 23L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007083100399 20070831 00399 NM 2007 8 31 SWAA074213 1 20070826 A 5314 6562125 KEELBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND LEFT KEEL BEAM CORRODED AT BS 488B, LBL 6.50. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2007083100407 20070831 00407 NM 2007 8 31 SWAA074202 1 20070825 A 3397 8100022607 CONNECTOR BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 486WN 33852 EEPLS INOP BETWEEN ROW 1 ABC AND ROW 3 ABC. SECURED LOOSE CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2007083100420 20070831 00420 EA 2007 8 31 SWIA200718624 1 20070821 A 2721 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA RUDDER TRIM STUCK A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 924SW 7681 RUDDER TRIM KNOB STICKS. WILL NOT RECENTER AFTER USE, FLIGHT NR 6085. REPLACED RUDDER/AILERON TRIM CONTROL PANEL IAW C RJ AMM CHAP 27-11-10. 2 L 7 2 4F RT A21EA 2007090400007 20070904 00007 EU 2007 9 4 MALA070103 1 20070821 A 3240 BRAKE SAAB SF340 340B 7860101 EU MLG UNKNOWN A MALA K NONE O OTHER LD LANDING 1 GL 15 427XJ 340B427 DURING BRAKING ON THE LANDING ROLL AND TAXI TO GATE THE AIRCRAFT PULLS HARD LEFT. FOUND LEFT BRAKE INBOARD TIRE WITH RA TTLE. REMOVED AND REPLACED WHEEL AND BRAKE ASSEMBLY. BRAKE PN: 5012589-3, SN ON: JUL87-0032. TIRE ASSEMBLY PN 5010488 -2, SN ON: JUL98-2696. ALL CHECKS GOOD. SEE WORK CARDS 3240-302, 3240-301 FOR DETAILS. 2 L 7 2 4T RT A52EU 2007090400009 20070904 00009 WP 2007 9 4 ARWA20070803 1 20070822 A 3097 CONNECTOR DOUG DC10 DC1010 3022110 WP HEATER CONTROL DAMAGED A ARWA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 19 68041 46900 LEFT STATIC PORT HEAT AND RIGHT STATIC PORT HEAT AND LEFT ANGLE OF ATTACK C/B`S POPPED WITH LIGHT SMOKE FROM AROUND THE FIRE HANDLES. REMOVED AND REPLACED CONNECTOR FROM HEATER CONTROLLER IN ACCORDANCE WITH M/M 20-30-02, AND REMOVED AND RE PLACED HEATER CONTROLLER MONITOR IN ACCORDANCE WITH M/M 30-35-01. OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH M/M 30-30 -00. 2 L 7 3 4F A22WE 2007090400015 20070904 00015 EA 2007 9 4 SIMA200724003 1 20070827 A 3240 BRAKE ASSY CNDAIR CL600 CL6002C10 1390015 EA NR 1 SEIZED A SIMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 21 506AE 10056 BRAKES LOCKED UP ON TAXI. BLEED NR 1 MAIN BRAKE IAW CRJ AMM. PERFORMED SYSTEM OPERATIONAL CHECK WITH NO DEFECTS, RETUR NED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007090400016 20070904 00016 SO 2007 9 4 SIMA200724001 1 20070826 A 3230 355022002 CONTROL UNIT EMB 145 EMB145LR 3260212 SO MLG FAILED A SIMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 21 674RJ 14500801 LANDING GEAR AURAL WARNING WITH GEAR DOWN, FLAPS 22 AT 1680 FEET. REMOVED AND REPLACED LANDING GEAR ELECTRONIC CONTROL UNIT IAW EMB AMM 32-33-01. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007090400017 20070904 00017 EU 2007 9 4 TRBA2007072 1 20070825 A 3397 WIRE AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT BROKEN A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 429AT 429 EMERGENCY EXIT LIGHT UNDER SERVICE DOOR INOP. REPAIRED BROKEN WIRE AT EMERGENCY LIGHT ASSY, AS PER STANDARDS PRACTICES 20-20-00, OP CHECK FOUND OK. 2 H 7 2 4T RT A53EU 2007090400018 20070904 00018 NM 2007 9 4 DHL2007785006 1 20070825 A 5350 10010021 RADOME BOEING 727 727214 138407R NM BS 178 CRACKED A DHLA D RETURN TO BLOCK W INADEQUATE Q C TX TAXI/GRND HDL 1 SO 01 785AT 21691 AT COMPLETION OF PUSH BACK, GROUND CREW UNABLE TO REMOVE TOW BAR. WHEN TOW BAR RELEASED, WITH PARKING BRAKE SET, ACFT M OVED FORWARD. VISIBLE DAMAGE NOTED TO RADOME ASSY. 2 L 7 3 4F A3WE 2007090400019 20070904 00019 CE 2007 9 4 N88833 1 20070822 A 3213 AXLE CESSNA 402 402C 207590R CE RT MLG CRACKED E HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 88833 402C0265 THE RT AXLE OF N88833 CRACKED DURING LANDING. THE LOWER STRUT LEG WAS REPLACED WITH SERVICEABLE ASSY AND A/C RETURNED T O SERVICE. 1 L 7 2 3O A7CE 2007090400020 20070904 00020 NM 2007 9 4 C1HA200792002 1 20070824 A 3297 CONNECTOR BOEING 727 727212 138407G NM MLG BROKEN A C1HA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 292AS 21458 AFTER GEAR RETRACTION RED GEAR LIGHT FOR NOSE GEAR REMAINED ILLUMINATED REFORMED COM 2.32.22 LIGHT REMAINED ON. REPLACE D BOTH NOSE GEAR DOWN LOCK AND GEAR POSITION SWITCHES SWING NOSE GEAR OPS CK NORMAL MM 32-61-71 MM 7-11-00 MM 32-61-01. CONNECTOR D298 NLG LOCK BROKEN. REPLACED WITH NEW CONNECTOR, OPS CK IS REQUIRED NOSE GEAR WARNING SYSTEM REQUIRES OPS CK NOSE GEAR WARNING SYSTEM. OPS CK GOOD REF MM 32-61-01, 7-11-00. 2 L 7 3 4F A3WE 2007090400021 20070904 00021 NM 2007 9 4 AWXA200701027 1 20070815 A 5311 65458076 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR#5987941, CRACK ON R1 DOOR SURROUND FORWARD UPPER STUB FRAME, BS 296, WL 265, RBL 5 0. REPLACED R1 DOOR SURROUND FORWARD UPPER STUB FRAME, BS 296, WL 265, RBL 50 IAW B737-300 SRM 51-40-02-0G PAR 4B, 7B, AND FIG 3, 8, 12. 2 L 7 2 4F RT A16WE 2007090400064 20070904 00064 EA 2007 9 4 A6WA200740444 1 20070810 A 2997 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM DIRTY A A6WA O OTHER J WARNING INDICATION CL CLIMB 1 GL 31 422AW 7341 DURING CLIMB, HYDRAULIC NR 3 LOW PRESSURE MESSAGE APPEARED AND 0 PSI WAS INDICATED. FOUND 3A PUMP CIRCUIT BREAKER 2G15 POPPED, RESET ONCE, LOW PRESSURE MESSAGE CLEARED. ON GROUND, FOUND CB2N12 TO BE POPPED (HYD SYSTEM IND 3) TRIED ONE RES ET C/B WOULD NOT RESET. CLEANED CONNECTOR ON HYD PRESSURE TRANSDUCER NR 3, RESET CB 2N12. OPS CHECK GOOD IAW AMM 29-10 -00. NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F RT A21EA 2007090400065 20070904 00065 EA 2007 9 4 A6WA200740445 1 20070810 A 2910 O-RING CNDAIR CL600 CL6002B19 1900309 EA HYD PUMP FAILED A A6WA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 31 466AW 7899 DURING CLIMB AT 25,000 FT, LT ENGINE LOW OIL PRESSURE WARNING ILLUMINATED 23 PSI 2-3 SECONDS AS PER QRH REDUCED THRUST L EVER, OIL PRESSURE STAYED BETWEEN 30-40 PSI LOW OIL PRESSURE ILLUMINATED. REMOVED AND REPLACED ENGINE NR 1 HYD ENGINE D RIVEN PUMP O-RINGS AT ENGINE NR 1 HYD EDP AXIS F CARBON SEAL AND MATING RING, OPS AND LEAK CHECK GOOD, IAW AMM 72-60-00, SUPP 05-018A. (M) 2 L 7 2 4F RT A21EA 2007090400066 20070904 00066 EA 2007 9 4 A6WA200740442 1 20070809 A 2613 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA LT PYLON MALFUNCTIONED A A6WA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 GL 31 453AW 7838 LT 14TH DUCT MESSAGE INTERMITTENT, INFLIGHT. COMPLIED WITH QRH. REMOVED AND REPLACED LEFT PYLON SENSING ELEMENT IAW AM M 36-21-04. TEST GOOD AT THIS TIME. (M) 2 L 7 2 4F RT A21EA 2007090400067 20070904 00067 EA 2007 9 4 A6WA200740443 1 20070723 A 5220 HANDLE CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH DIRTY A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 CREW ESCAPE HATCH EXTERNAL HANDLE WILL NOT DEPLOY. CLEANED AND LUBRICATED HANDLE IAW CRJ200 AMM 12-20-52-640-803. OPER ATES NORMAL. (M) 2 L 7 2 4F RT A21EA 2007090400068 20070904 00068 EA 2007 9 4 A6WA200740433 1 20070806 A 2740 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A A6WA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 31 407AW 7424 STAB TRIM/MACH TRIM CAUTION MESSAGE IN FLIGHT. STAB TRIM STUCK AT 4.4 DEGREES. FLAPS AT 20 WHEN FAILURE OCCURRED, BOTH CHANNELS. REMOVED AND REPLACED STAB/MACH TRIM PANEL ASSEMBLY IAW AMM 27-40-00. (M) 2 L 7 2 4F RT A21EA 2007090400069 20070904 00069 EA 2007 9 4 A6WA200740432 1 20070731 A 2760 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILERS MALFUNCTIONED A A6WA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 31 434AW 7322 ON CLIMB-OUT, MOMENTARILY UNCOMMANDED ROLL TO RIGHT OCCURRED FOLLOWED BY SPOILERON FAULT STATUS MESSAGE. FLIGHT CONTROL PAGE INDICATES RIGHT SPOILERON WHITE. REMOVED AND REPLACED RT OUTBOARD SPOILERON PCU IAW AMM 27-62-02-943-004. (M) 2 L 7 2 4F RT A21EA 2007090400070 20070904 00070 EA 2007 9 4 A6WA200740461 1 20070819 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX LACK OF LUBE A A6WA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 433AW 7289 UNABLE TO OPEN MAIN PASSENGER DOOR. AFTER MULTIPLE ATTEMPTS, DOOR OPENED. OPERATED DOOR SEVERAL TIMES. DOOR APPEARS T O OPERATE NORMALLY. PLACED ON MEL. REF LOG 177995/2 CLEANED AND LUBED PASSENGER DOOR. PERFORMED OPS CHECK OF PASSENGE R DOOR SEVERAL TIMES. OPS CHECK GOOD IAW 52-11-00. (M) 2 L 7 2 4F RT A21EA 2007090400071 20070904 00071 EA 2007 9 4 A6WA200740446 1 20070815 A 2740 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A A6WA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 31 458AW 7861 HIGH SPEED ABORT DUE TO RED WARNING STAB CONFIGURATION. AIRCRAFT WEIGHT 47200 SPEED 120 KNOTS BRAKE TEMPS AFT 5 MINUTES 10, 8, 8, 8 (STAB CHANNEL 1 INOP). REMOVED AND REPLACED MOTOR CONTROL UNIT, HORIZONTAL STAB TRIM ACTUATOR, AND HORIZON TAL STAB TRIM CONTROL UNIT IAW AMM 27-40, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007090400072 20070904 00072 EA 2007 9 4 A6WA200740462 1 20070820 A 2731 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA PITCH FEEL MALFUNCTIONED A A6WA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 GL 31 450AW 7823 WITH FLAPS AT ZERO, PITCH CONTROL FORCE UNUSUALLY HIGH, FLAPS OUT TO ZERO HAS NORMAL CONTROL FORCE. REMOVED AND REPLAC ED BOTH PITCH FEEL SIMULATOR UNITS PER AMM TASK 27-31-20-000-801. PERFORMED CONTROL COLUMN FEEL FORCE AND CENTERING CHE CK PER AMM TASK 27-31-00-220-807 AND FUNCTIONAL CHECK OF THE PITCH FEEL SYSTEM. FOUND OK. (M) 2 L 7 2 4F RT A21EA 2007090400073 20070904 00073 EA 2007 9 4 A6WA200740453 1 20070812 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 464AW 7890 FOUND FS 280 LBL 9 INBOARD AND OUTBOARD FLOOR SUPPORT CLIPS ARE CRACKED. 10-04-07 MAINTENANCE REPLACED CLIPS IAW BSC S TANDARD REPAIR 601R-53-0057A AND CRJ 200 SRM 51-42-13 AND 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007090400074 20070904 00074 EA 2007 9 4 A6WA200740458 1 20070812 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 464AW 7890 THE RT WING LOWER PLANK ACCESS HOLE FOR PANEL 640BB HAS PITTING APPROX .005 INCH DEEP AT THE INBOARD AND OUTBOARD RADIUS . 10-04-07 MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV F. (M) 2 L 7 2 4F RT A21EA 2007090400075 20070904 00075 NM 2007 9 4 AWXA200701030 1 20070825 A 2611 RAI2800M0706 CONTROL BOX AIRBUS A319 A319132 3930340 NM SMOKE DETECTION FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 816AW 6744 6744 1254 1350 PHX - OTH - CREW REPORTED SMOKE LAVATORY DET FAULT. MX REPLACED THE SMOKE DETECTOR AND THE CONTROL UNIT. OPERATIONAL C HECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007090400076 20070904 00076 EA 2007 9 4 A6WA200740450 1 20070811 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 464AW 7890 FOUND RIGHT FS 621 FLOOR SUPPORT ANGLE CRACKED APPROX .3 INCH LONG. 10-04-07 MAINTENANCE REPLACED ANGLE IAW BOMBARDIER REO 601R-53-61-117. (M) 2 L 7 2 4F RT A21EA 2007090400077 20070904 00077 EA 2007 9 4 A6WA20074055 1 20070812 A 5310 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 464AW 7890 FOUND CARGO DOOR TRACK SUPPORT BEAM ANGLE AT FS 621 IS CRACKED AT BOTTOM ANGLE. (M) 2 L 7 2 4F RT A21EA 2007090400078 20070904 00078 EA 2007 9 4 A6WA200740454 1 20070812 A 5340 NUT CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 464AW 7890 FOUND FS 280 RBL 9 INBOARD AND OUTBOARD FLOOR SUPPORT CLIPS ARE CRACKED. 10-04-07 MAINTENANCE REPLACED CLIPS IAW BSC STANDARD REPAIR 601R-53-0057A AND CRJ 200 SRM 51-42-13 AND 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007090400079 20070904 00079 EA 2007 9 4 A6WA200740456 1 20070812 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 464AW 7890 THE LEFT WING LOWER PLANK ACCESS HOLE FOR PANEL 540BB AT WS 54.897 HAS PITTING APPROX .005 INCH DEEP AT THE INBOUND AND OUTBOARD RADIUS. 10-04-07 MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV F. (M) 2 L 7 2 4F RT A21EA 2007090400080 20070904 00080 EA 2007 9 4 A6WA200740447 1 20070811 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 464AW 7890 FOUND RIGHT FS 621-625 INTERCOSTAL ANGLE, P/N 601-35012-52 CRACKED APPROX .2 INCH LONG. 10-04-07 MAINTENANCE REPLACE D ANGLE IAW BOMBARDIER REO 601R-53-61-422 AND CRJ 200 SRM 51-42-06 AND 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007090400081 20070904 00081 EA 2007 9 4 A6WA200740457 1 20070812 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 464AW 7890 THE LEFT WING LOWER PLANK ACCESS HOLE FOR PANEL 510AB AT WS 12.245 HAS PITTING APPROX .007 INCH DEEP. 10-04-07 MAINTEN ANCE C/W REPAIR OF LT WING LOWER PLANK ACCESS HOLE PANEL 510AB IAW REO 601R-57-20-030 REV F. (M) 2 L 7 2 4F RT A21EA 2007090400082 20070904 00082 EA 2007 9 4 A6WA200740448 1 20070811 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 464AW 7890 LT FS 621-625 INTERCOSTAL ANGLE, P/N 601-35012-51, CRACKED APPROX .2 INCH LONG. 07-04-07 MAINTENANCE REPLACED ANGLE IAW BOMBARDIER REO 601R-53-61-422 AND CRJ 200 SRM 51-42-06 AND 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007090400083 20070904 00083 EA 2007 9 4 A6WA200740452 1 20070811 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 464AW 7890 ANGLE CRACKED IN FLOOR SUPPORT STRUCTURE AT FS 484 LBL 27, WL 73.50. 10-04-07 MAINTENANCE REPLACED ANGLE IAW BOMBARDIE R REO 601R-53-41-059 AND BSC STANDARD REPAIR 601R-53-0029B. (M) 2 L 7 2 4F RT A21EA 2007090400084 20070904 00084 EA 2007 9 4 A6WA200740449 1 20070811 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 464AW 7890 FOUND LEFT FS 621 FLOOR SUPPORT ANGLE CRACKED APPROX .3 INCH LONG. 10-04-07 MAINTENANCE REPLACED ANGLE IAW BOMBARDIER REO 601R-53-61-117. (M) 2 L 7 2 4F RT A21EA 2007090400085 20070904 00085 EA 2007 9 4 A6WA200740451 1 20070811 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 464AW 7890 ANGLE CRACKED IN FLOOR SUPPORT STRUCTURE AT FS 484 RBL 27, WL 73.50. 10-04-07 MAINTENANCE REPLACED ANGLE IAW BOMBARDI ER REO 601R-53-41-059 AND BSC STANDARD REPAIR 601R-53-0029B. (M) 2 L 7 2 4F RT A21EA 2007090400086 20070904 00086 NM 2007 9 4 HALA0700356 1 20070828 A 2911 211C223520 PRESSURE SWITCH BOEING 767 767322 1385200 NM HYD SYSTEM FAILED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 HA598 23278 ADP AUTO FUNCTION INOP, OPERATES NORMAL IN ON POSITION. ACCOMPLISHED FIM 29-11-00, FIGURE 109. REPLACED ADP CONTROL PR ESSURE SWITCH S29 PER AMM 29-11-19. GROUND OPS AND LEAK CHECK OK. REMOVED PLACARD. CLEARED MIC SHEET. MOC NOTIFIED. 2 L 7 2 4F RT A1NM 2007090400087 20070904 00087 2007 9 4 HALA0700357 2 20070829 A 7597 TERMINAL BOEING 767 767322 1385200 NM BLEED VALVE BROKEN A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 598HA 23278 RIGHT ENGINE BLEED VALVE EICAS MESSAGE. REPAIRED BROKEN TERMINAL WIRES ON RIGHT HPSOV AS REQUIRED. HPSOV VALVE REMAINS LOCKED CLOSED. DMI REQUIREMENTS MET DMI CONTINUES. 2 L 7 2 4F RT A1NM 2007090400088 20070904 00088 NE 2007 9 4 HALA0700355 2 20070827 A 7200 7202388 ENGINE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE LEFT SURGES A HALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 13 HA485 4963 55130 13318 RIGHT AT TAKEOFF POWER, HEARD A BIG BOOM FOLLOWED WITH AN OVERTEMP ON THE LEFT ENGINE. FOUND RIGHT ENGINE WITH NO DEFEC TS. FOUND LEFT ENGINE FAILED CONFIRMED BY HEAVY METAL DEBRIS IN TAILPIPE. VERIFIED W/PPOE LEFT ENGINE EXCEEDANCE. NO REPORT ON RIGHT ENGINE. SEE L/P 197559/16 FOR ENGINE REMOVAL. REPLACED LEFT ENGINE. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007090400089 20070904 00089 NM 2007 9 4 AALA20071483 1 20070810 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 777AN 29585 DFW - EMERGENCY LIGHT AT SEAT ROW 40C IS INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 40C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007090400090 20070904 00090 NM 2007 9 4 AALA20071490 1 20070810 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 777AN 29585 DFW - EMERGENCY LIGHT AT SEAT ROW 38C IS INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 38C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007090400091 20070904 00091 WP 2007 9 4 AALA20071497 1 20070811 A 3397 WIRE HARNESS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7538A 49992 DFW - EMERGENCY LIGHT AT SEAT 8D IS INOPERATIVE. REPAIRED WIRE FROM SIDEWALL AREA TO SEAT FOR EMERGENCY LIGHT AT SEAT 8 D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007090400092 20070904 00092 2007 9 4 AALA20071501 4 20070811 A 2565 HOOK AND LOOP DOUG DC9 DC982 3022082 WP SERVICE DOOR FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7538A 49992 DFW - EMERGENCY SLIDE AT AFT SERVICE DOOR HANDLE HOOK AND LOOP INOPERATIVE. REPLACED EMERGENCY SLIDE AT AFT SERVICE DOO R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007090400093 20070904 00093 WP 2007 9 4 AALA20071515 1 20070812 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 582AA 53159 DFW - EMERGENCY LIGHT AT SEAT ROW 24D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007090400094 20070904 00094 EU 2007 9 4 AALA20071506 1 20070812 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80058 466 MIA - EMERGENCY LIGHT AT SEAT ROW 32G IS INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 32G. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007090400095 20070904 00095 EU 2007 9 4 AALA20071507 1 20070812 A 3350 LENS AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 80058 466 MIA - EMERGENCY LIGHT AT SEAT ROW 2D HAD BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 2D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007090400096 20070904 00096 EU 2007 9 4 AALA20071509 1 20070812 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80058 466 MIA - EMERGENCY LIGHT AT SEAT ROW 30C IS INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 30C. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007090400097 20070904 00097 WP 2007 9 4 AALA20071510 1 20070812 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 582AA 53159 DFW - EMERGENCY LIGHT AT SEAT ROW 8D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 8D. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007090400098 20070904 00098 WP 2007 9 4 AALA20071511 1 20070812 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 582AA 53159 DFW - EMERGENCY LIGHT AT SEAT ROW 16D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 16D. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007090400099 20070904 00099 NM 2007 9 4 AALA20071492 1 20070810 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 908AN 29510 MIA - EMERGENCY LIGHT AT OVERHEAD BIN 22ABC INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD BIN 22ABC. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007090400100 20070904 00100 NM 2007 9 4 AALA20071493 1 20070810 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 908AN 29510 MIA - EMERGENCY LIGHT AT OVERHEAD BIN 25ABC IS INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD BIN 25ABC. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007090400101 20070904 00101 NM 2007 9 4 AALA20071531 1 20070813 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 909AN 29511 EMERGENCY LIGHT AT FORWARD LEFT OVERWING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT FORWARD LEFT OVERWING. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007090400102 20070904 00102 2007 9 4 AALA20071530 4 20070813 A 2565 100504205 SLIDE DOUG DC9 DC982 3022082 WP DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7520A 49897 MSP - EMERGENCY SLIDE GIRT BAR VELCRO INOPERATIVE AND MANUAL DEPLOY HANDLE RING CORRODED AT RIGHT NUMBER ONE DOOR. REPL ACED EMERGENCY SLIDE AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007090400103 20070904 00103 WP 2007 9 4 AALA20071527 1 20070813 A 2130 39613011 VALVE DOUG DC9 DC982 3022082 WP FLOW CONTROL INOPERATIVE A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 447AA 49473 ORD INFLIGHT T1189/13AUG CREW REPORTED UNABLE TO MAINTAIN CABIN PRESSURE. DESCENDED BELOW 10000 FEET. LANDED ORD WITH OUT INCIDENT. REPLACED RIGHT HAND FLOW CONTROL VALVE AND LEFT AIR CYCLE MACHINE. SYSTEM GROUND CHECKED NORMAL OPERATIO N. 2 L 7 2 4F A6WE 2007090400104 20070904 00104 NM 2007 9 4 AALA20071528 1 20070813 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 391AA 27451 JFK - EMERGENCY LIGHT AT AFT GALLEY MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT AFT GALLEY. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007090400105 20070904 00105 NM 2007 9 4 AALA20071529 1 20070813 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 391AA 27451 JFK - EMERGENCY LIGHT AT AFT GALLEY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT AFT GALLEY. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007090400106 20070904 00106 NM 2007 9 4 AALA20071526 1 20070812 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 789AN 30252 DFW - EMERGENCY LIGHT AT SEAT ROW 21G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 21G. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007090400107 20070904 00107 WP 2007 9 4 AALA20071516 1 20070812 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 582AA 53159 DFW - EMERGENCY LIGHT AT SEAT ROW 19D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 19D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007090400108 20070904 00108 WP 2007 9 4 AALA20071498 1 20070811 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7538A 49992 DFW - EMERGENCY LIGHT AT RIGHT EXTERIOR OVERWING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT EXTERIOR OVERW ING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007090400109 20070904 00109 NM 2007 9 4 AALA20071522 1 20070812 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 789AN 30252 DFW - EMERGENCY LIGHT AT SEAT ROW 36G HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 36G. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007090400110 20070904 00110 NM 2007 9 4 AALA20071523 1 20070812 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 789AN 30252 DFW - EMERGENCY LIGHT AT SEAT ROW 36G HAS MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 36G. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007090400111 20070904 00111 NE 2007 9 4 AALA20071503 2 20070807 A 7250 BLADE BOEING 737 737823 13844BZ NM GE CFM56 CFM56* 13802 NE LT ENGINE DAMAGED A AALA A UNSCHED LANDING M E J OVER TEMP VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 21 926AN 29527 88923 MEM INFLIGHT T1227/07AUG BNA TO DFW - CREW REPORTED NUMBER ONE ENGINE VIBRATIONS AND ENGINE GAS TEMPERATURE INTO RED. R EDUCED ENGINE TO IDLE AND LANDED MEM WITHOUT INCIDENT. FOUND NUMBER ONE ENGINE SUSTAINED HEAT DAMAGE. REPLACED NR 1 EN GINE ON 07 AUG AT MEM. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A16WE E2GL 2007090400112 20070904 00112 NM 2007 9 4 AALA20071489 1 20070810 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 777AN 29585 DFW - EMERGENCY LIGHT AT SEAT ROW 26C IS INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 26C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007090400113 20070904 00113 WP 2007 9 4 AALA20071512 1 20070812 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 582AA 53159 DFW - EMERGENCY LIGHT AT SEAT ROW 18D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 18D. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007090400114 20070904 00114 WP 2007 9 4 AALA20071518 1 20070812 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 582AA 53159 DFW - EMERGENCY LIGHT AT EXTERIOR OVERWING INOPERATIVE. REPLACED BATTERY PACK B5 49 FOR EMERGENCY LIGHT AT EXTERIOR OVE RWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007090400115 20070904 00115 NM 2007 9 4 AALA20071484 1 20070810 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 777AN 29585 DFW - EMERGENCY LIGHT AT SEAT ROW 25G IS INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 25G. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007090400116 20070904 00116 WP 2007 9 4 AALA20071499 1 20070811 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7538A 49992 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 12AB IS INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROW 12AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007090400117 20070904 00117 WP 2007 9 4 AALA20071500 1 20070811 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7538A 49992 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 13AB IS INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROW 13AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007090400118 20070904 00118 WP 2007 9 4 AALA20071495 1 20070811 A 2500 LIGHT DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7538A 49992 DFW - PORTABLE EMERGENCY LIGHT AT FORWARD CABIN IS INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT AT FORWARD CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007090400119 20070904 00119 NM 2007 9 4 AALA20071491 1 20070810 A 2500 PLACARD BOEING 767 767323 1385205 NM CABIN MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 348AN 33087 DFW - EMERGENCY EXIT PLACARD AT LEFT NUMBER FOUR DOOR MISSING. REPLACED PLACARD FOR EMERGENCY EXIT AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007090400120 20070904 00120 NM 2007 9 4 AALA20071487 1 20070810 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 777AN 29585 DFW - EMERGENCY LIGHT AT SEAT ROW 22C IS INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT ROW 22C. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007090400121 20070904 00121 NM 2007 9 4 AALA20071502 1 20070810 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 937AN 30082 MIA - EMERGENCY LIGHT AT LEFT EXTERIOR NUMBER TWO DOOR INOPERATIVE. 2 L 7 2 4F RT A16WE 2007090400122 20070904 00122 WP 2007 9 4 AALA20071517 1 20070812 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 582AA 53159 DFW - EMERGENCY EXIT SIGN LIGHT AT FORWARD LEFT OVERWING INOPERATIVE. REPLACED FORWARD LAMP FOR EMERGENCY EXIT SIGN LIG HT AT FORWARD LEFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007090400123 20070904 00123 WP 2007 9 4 AALA20071494 1 20070811 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7538A 49992 DFW - EMERGENCY LIGHT AT SEAT ROW 18D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 18D. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007090400124 20070904 00124 NM 2007 9 4 AALA20071519 1 20070812 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 789AN 30252 DFW - EMERGENCY LIGHT AT SEAT ROW 20C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 20C. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007090400125 20070904 00125 NM 2007 9 4 AALA20071520 1 20070812 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 789AN 30252 DFW - EMERGENCY LIGHT AT SEAT ROW 36C INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 36C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007090400126 20070904 00126 NM 2007 9 4 AALA20071521 1 20070812 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 789AN 30252 DFW - EMERGENCY LIGHT AT SEAT ROW 37C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 37C. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007090400127 20070904 00127 NM 2007 9 4 AALA20071524 1 20070812 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 789AN 30252 DFW - EMERGENCY LIGHT AT SEAT ROW 24G HAS MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 24G. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007090400128 20070904 00128 NM 2007 9 4 AALA20071525 1 20070812 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 789AN 30252 DFW - EMERGENCY LIGHT AT SEAT ROW 23G INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT ROW 23G. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007090400129 20070904 00129 EU 2007 9 4 AALA20071508 1 20070812 A 3350 LENS AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 80058 466 MIA - EMERGENCY LIGHT AT SEAT ROW 5G HAD BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 5G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007090400130 20070904 00130 WP 2007 9 4 AALA20071513 1 20070812 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 582AA 53159 DFW - EMERGENCY LIGHT AT SEAT ROW 20D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 20D. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007090500001 20070905 00001 NM 2007 9 5 07FDEA03160 1 20070827 A 5753 STRAP DOUG MD11 MD11F 3023600 NM TE FLAP HINGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 LEFT WING, OUTBOARD FLAP INBOARD HINGE TENSION STRAP FOUND CRACKED. 09-12-07 REMOVED AND REPLACED AS PER FEDEX E.O. 1- 5750-7-5004 PT1, REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007090500002 20070905 00002 EU 2007 9 5 07FDEA03163 1 20070828 A 5311 A53985135205 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORRSOSION IN UPPER CORNER FITTING AT FRAME 88, STRG 15-17 RHS. REPAIR PERFORMED BY CUTTING AND INSTALLING DOUBLER IAW EA 6-5319-103257. 2 L 7 2 4F RT A35EU 2007090500008 20070905 00008 EU 2007 9 5 07FDEA03170 1 20070828 A 5340 FRAME AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 TOO SMALL EDGE MARGIN AT TEE-FITTING, CABIN FLOOR STRUCTURE FRAME 18, Y-2462. REPAIR PERFORMED BY REPLACING TEE-FITTING IAW SRM 51-75-10. 2 L 7 2 4F RT A35EU 2007090500009 20070905 00009 EU 2007 9 5 07FDEA03172 1 20070828 A 5311 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 OLD MISDRILLED MARK ON THE CONNECTION SECTION FRAME 64-65, STRG 37 RT. REMAINING THICKNESS AFTER REMOVING OUT OF LIMIT. REPLACEMENT OF CONNECTING SECTION IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007090500012 20070905 00012 NM 2007 9 5 07FDEA03175 1 20070828 A 5313 651594014 STRINGER BOEING 727 727233 138408A NM ZONE 100 DAMAGED A FDEA K O NONE OTHER O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 BS 740, VERTICAL ANGLE AND BULKHEAD SKIN, ABOVE STR S-28 HAS 2 EA PLUG RIVETS THROUGH ALL PARTS (PREVIOUS DAMAGE) ACCO MPLISHED WORK INSTRUCTION ON EA NR 7-5310-11068 FOR REPAIR OF 2 (EA) PLUG RIVETS THROUGH VERTICAL ANGLE, AND BULKHEAD. 2 L 7 3 4F RT A3WE 2007090500013 20070905 00013 EU 2007 9 5 07FDEA03176 1 20070828 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 HEAVY CORROSION FOUND ON FRAME 92 AT SEVERAL ANGLE SECTIONS, STRG 14 RT TO 17 LT. REPAIR PERFORMED BY REPLACEMENT OF PA RTS IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007090500021 20070905 00021 EU 2007 9 5 07FDEA03184 1 20070828 A 5313 A53811368202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION AT STRG 49, BETWEEN FRAME 39-44 LH. REMAINING THICKNESS OUT OF LIMIT, STRINGER REPAIR PERFORMED WITH PRINCI PLE DESCRIBED IN SRM 53-10-14/FIG 201A, APPROVED BY EA 6-5315-103260 AND RAS/046453/012/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007090500023 20070905 00023 EU 2007 9 5 07FDEA03186 1 20070828 A 5313 A53811307 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION AT STRG 40-41, BETWEEN FRAME 40-45 RT. REMAINING THICKNESS OUT OF LIMIT. STRINGER REPAIR PERFORMED WITH PRIN CIPLE DESCRIBED IN SRM 53-10-14/FIG 201A, APPROVED BY EA 6-5315-103260 AND RAS/046453/012/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007090500024 20070905 00024 EU 2007 9 5 07FDEA03187 1 20070828 A 5313 A53811374203 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION AT STRG 44, BETWEEN FRAME 40-45 RT. REMAINING THICKNESS OUT OF LIMIT. STRINGER REPAIR PERFORMED WITH PRINC IPLE DESCRIBED IN SRM 53-10-14/FIG 201A, APPROVED BY EA 6-5315-103260 AND RAS/046453/012/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007090500027 20070905 00027 EU 2007 9 5 07FDEA03189 1 20070828 A 5313 A53811406202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION AT STRG 47, BETWEEN FRAME 39-42 RT. REMAINING THICKNESS OUT OF LIMIT. STRINGER REPAIR PERFORMED WITH PRINC IPLE DESCRIBED IN SRM 53-10-14/FIG 201A, APPROVED BY EA 6-5315-103260 AND RAS/046453/012/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007090500028 20070905 00028 EU 2007 9 5 07FDEA03190 1 20070828 A 5313 A53811360203 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION AT STRG 48, BETWEEN FRAME 40-44 RT. REMAINING THICKNESS OUT OF LIMIT. STRINGER REPAIR PERFORMED WITH PRINC IPLE DESCRIBED IN SRM 53-10-14/FIG 201A, APPROVED BY EA 6-5315-103260 AND RAS/046453/012/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007090500030 20070905 00030 EU 2007 9 5 07FDEA03191 1 20070828 A 5313 A53811369202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION AT STRG 50, BETWEEN FRAME 39-43 RT. REMAINING THICKNESS OUT OF LIMIT. STRINGER REPAIR PERFORMED WITH PRINC IPLE DESCRIBED IN SRM 53-10-14/FIG 201A, APPROVED BY EA 6-5315-103260 AND RAS/046453/012/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007090500032 20070905 00032 EU 2007 9 5 07FDEA03193 1 20070828 A 5330 A53778160204 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 FOUND OLD PLUGGING RIVET CLOSE TO HOIST POINT ON RT KARMAN STRUCTURE, EXTERNAL SKIN C36-37, P31-32 RT. REPAIR PERFORM ED BY REMOVE THE DOUBLE HOLE AND REAM UP AND INSTALLING A BUSH IAW EA 6-5314-103261 AND RAS/DABRE/7006900/2006 ISS A. 2 L 7 2 4F RT A35EU 2007090500036 20070905 00036 EU 2007 9 5 07FDEA03199 1 20070828 A 5330 A53978157200 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA K NONE W W W INADEQUATE Q C INADEQUATE Q C INADEQUATE Q C IN INSP/MAINT 1 SO 25 811FD 457 DURING REMOVAL OF OLD DOUBLER FRAME 69-70, STRG 41-42 RHS, FOUND AN OLD MISDRILLED HOLE BETWEEN OUTER SKIN AND INNER CLI P. REPAIR PERFORMED BY REMOVE THE AFFECTED CLIP, PERFORM COUNTERSINKING OF AFFECTED HOLE IN THE SKIN, REWORK OF CLIP OU TER FLANGE AND REINSTALLATION OF CLIP IAW EA 6-5317-103328 AND RAS/DAHAM/4021214/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007090500047 20070905 00047 NM 2007 9 5 CALA0700462 1 20070827 A 3350 ADD71701100 BATTERY BOEING 737 737824 13844BZ NM CABIN DISCHARGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18220 28929 THE EMERGENCY LIGHT BATTERY PACKS ABOVE AFT GALLEY BOTH LEFT AND RIGHT WOULD NOT HOLD CHARGE. BOTH BATTERY PACKS WERE R EMOVED AND REPLACED. 2 L 7 2 4F RT A16WE 2007090500048 20070905 00048 NM 2007 9 5 USAA200708004 1 20070825 A 5320 FLOOR SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 A 6 INCH CRACK FOUND - FLOOR SUPPORT CRACKED IN HALF AT AFT CARGO DOOR UPLOCK AT STA 787-807 RBL 19.5. DEFECTIVE PART R EPLACED WITH IDENTICAL PART PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007090500049 20070905 00049 NM 2007 9 5 USAA200708005 1 20070825 A 5320 STRAP BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 23380 A 1 X 1 INCH CORRODED AREA AT STA 795 I/B OF STR 25R. REPLACED STRAP PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007090500050 20070905 00050 EA 2007 9 5 TRAX200701236 1 20070811 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 839AS 7284 FLOOR EMERGENCY LIGHT BULLET CONNECTOR MISSING AT SERVICE DOOR ENTRY POSITION. 2 L 7 2 4F RT A21EA 2007090500051 20070905 00051 EA 2007 9 5 TRAX200701237 1 20070811 A 5514 FITTING CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 839AS 7284 HORIZONTAL STAB ANTI-ROTATION FITTING CORRODED. 2 L 7 2 4F RT A21EA 2007090500052 20070905 00052 EA 2007 9 5 TRAX200701238 1 20070816 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 881AS 7496 EMERGENCY ESCAPE HATCH NEEDS THE FOLLOWING EXTERIOR PLACARDS EMERGENCY EXIT (INSTRUCTION PLACARD), OPEN PLACARD, ARROW I NDICATION PLACARD AND CLOSED PLACARD. 2 L 7 2 4F RT A21EA 2007090500053 20070905 00053 NM 2007 9 5 QXEA200701354 1 20070820 A 3010 4100S00502 VALVE BOMBDR DHC8 DHC8402 1390042 NM DE ICE SYSTEM INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 6665 2394 4048 SEA - DEICE PRESSURE CAUTION LIGHT ILLUMINATED. RUNNING THE CHECKLIST, NOTICED THE LEFT OUTBOARD BOOT LIGHT DIDN'T ILLU MINATE. THE DEICE PRESSURE IS NORMAL THROUGH ALL CYCLES. MAINTENANCE REMOVED AND REPLACED THE NR 5 DDV. OPERATIONAL C HECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007090500055 20070905 00055 EA 2007 9 5 TRAX200701239 1 20070824 A 3260 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 834AS 7254 NLG GEAR DISAGREE MSG AFTER GEAR HANDLE SELECTED UP. A/C RETURNED TO AVL AFTER T/O. EMERGENCY DECLARED. (LANDING GEAR RETRACTION SYSTEM) 2 L 7 2 4F RT A21EA 2007083100232 20070831 00232 NM 2007 8 31 SWAA074176 1 20070823 A 5755 654645268A HINGE BOEING 737 7373G7 1384595 NM NR 5 SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED C2 CHECK, FOUND RIGHT WING NR 5 GROUND SPOILER OUTBOARD HINGE CRACKED. REMOVED AND REPLACED NR 5 SPOIL ER PER MM. 2 L 7 2 4F RT A16WE 2007083100246 20070831 00246 NM 2007 8 31 USAA070665 1 20070824 A 5210 507945178 DOOR FRAME BOEING 737 7373B7 1384580 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 FWD PASSENGER DOOR FRAME CRACKED AT 37 STOP PIN CUTOUT, L1 DOOR, FWD ENTRY DOOR. INSTALLED DOUBLER REPAIR PER EA 98819, DEFECT SIZE: .125 INCH. 2 L 7 2 4F RT A16WE 2007083100274 20070831 00274 NM 2007 8 31 07FDEA03113 1 20070824 A 5340 69456281 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FUSELAGE, BS 740, S-27L, 2 STR CLIPS CORRODED REMOVED CLIPS, REMOVED CORROSION AND CLIPS ARE OUT OF LIMITS. FABRICATED NEW CLIPS, TREATED AND PRIMED AND INSTALLED. REF BOEING DOCUMENT DRAWING NR 69-45628/ID NR 0001/FRAME NR 1 CLASSIFIED A S A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007083100275 20070831 00275 NM 2007 8 31 07FDEA03114 1 20070824 A 5320 BAC15201485 FLOOR SUPPORT BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD CARGO AREA, STA 718, STR 29L, ABOUT LBL 2, FLOOR SUPPORT IS CORRODED ON REPAIR ANGLE REMOVED DAMAGE. FABRICATION REPAIR PART, TREATED AND PRIMED REPAIR PARTS AND INSTALLED. THIS REPAIR IS CLASSIFIED AS MINOR. 2 L 7 3 4F RT A3WE 2007083100276 20070831 00276 NM 2007 8 31 07FDEA03115 1 20070824 A 5313 655458318 STRINGER SPLICE BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT PIT BILGE BODY FRAME STR SPLICE IS CORRODED, BS 1008-1012, STR 29L, WL 140. REMOVED STRINGER SPLICE, CLEANED DAMAGE HOLE, HFEC STRINGER, FABRICATED STRINGER SPLICE. FABRICATED STRINGER CLIPS, TREATED AND PRIMED PARTS, PERFORMED HIDDEN DAMAGE INSPECTION. INSTALLED STRINGER SPLICE AND STRINGER CLIP REF EA NR 7-5310-113077. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007083100277 20070831 00277 EU 2007 8 31 UPS07150494 1 20070824 A 2597 CONNECTOR AIRBUS A300 A300F4622R 3930360 EU EVAC SLIDE DIRTY A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 128UP 0812 INSPECTION TYPE:N/A EVACUATION SLIDE WARNING LIGHT INOP. CLEANED & RESEATED CONNECTOR ON THE AUTONOMOUS STANDBY POWER S UPPLY UNIT 70WN AS REQUIRED. WARNING LIGHT OPS CHECKS GOOD PER AMM 52-73-11-04. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2007083100278 20070831 00278 NM 2007 8 31 07FDEA03116 1 20070825 A 5330 651786331 SKIN BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD ENTRY DOOR CUTOUT, LOWER HINGE REPAIR, 3 HOLES ARE CRACKED. NEED ENGINEERING EVALUATION PER WIC 53308429 ITEM 5. HOLES CIRCLE IN BLACK, ALSO ON NR00077 LT FUSELAGE SKIN IS CRACKED OUT OF THE MAIN ENTRY DOOR CUTOUT LWR HINGE CUTOUT. REPAIR OF LOWER HINGE CUTOUT ACCOMPLISHED ON EO NR 7-5330-7-2345 P2. BOTH DISCREPANCIES NR00077 AND NN00500 ARE REPAIRE D ON THIS EO. 2 L 7 3 4F RT A3WE 2007083100279 20070831 00279 NM 2007 8 31 07FDEA03117 1 20070825 A 5330 651768331 SKIN BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD ENTRY DOOR CUTOUT, UPPER HINGE CUTOUT REPAIR, 5 HOLES ARE CRACKED NEED EVALUATION PER WIC 53308429 ITEM 5, HOLES ARE CIRCLED IN BLACK. ALSO FUSELAGE SKIN IS CRACKED OUT OF THE MAIN ENTRY DOOR CUTOUT UPPER HINGE ON WO NR 36352/N00076 CO MPLIED WITH EA NR 7-5330-113939. WORKED IN CONJUCTION WITH WO NR 36352/ N00076 AND N00499. UPPER HINGE CUTOUT DOUBLER AND TRIPLER. 2 L 7 3 4F RT A3WE 2007083100281 20070831 00281 NM 2007 8 31 07FDEA03118 1 20070825 A 5347 BAC1520752 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 SEAT TRACK CORRODED, STA 386-390, LBL 44-45 AREA AT STA 386-390, LBL 44-45, BLENDED AND MAPPED, REF SRM 53-10-1. NDT, F OUND NO DEFECTS. AREA ROTO PEENED REF SOPM 20-10-03, TREATED AND PRIMED REF SRM 51-10-2 REF EA NR 7-5310-113091, LEVEL 1 CORROSION. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007083100282 20070831 00282 NM 2007 8 31 07FDEA03119 1 20070825 A 5347 BAC1520752 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 SEAT TRACK CORRODED FROM STA 363-372, LBL 24-25 AREA AT STA 363-372, LBL 24-25 BLENDED AND MAPPED, REF SRM 53-10-1. ND T, FOUND NO DEFECTS. AREA ROTO - PEENED REF REF SOPM 20-10-03. TREATED AND PRIMED REF SRM 51-10-2. REF EA NR 7-5310-1 13091, CORROSION IS LEVEL 1, THIS IS CLASSIFIED A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007083100284 20070831 00284 NM 2007 8 31 07FDEA03120 1 20070825 A 5311 BAC150510043 FRAME BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LWR FUSELAGE RT SIDE STA 743, RBL 7", SUPPORT FRAME AT IB SIDE OF ACCESS DOOR 3449R IS CORRODED OB SIDE REMOVED BEACON, REMOVED PANELS 3449R AND 3346. CORROSION THROUGH SUPPORT FRAME. REMOVED SUPPORT FRAME. FABRICATED NEW PARTS, ASSEMBLE D NEW FRAME. INSTALLED NEW PARTS, REF SRM 51-40-02. TREATED AND PRIMED PARTS REF SRM 51-10-2. REINSTALLED PANELS 3449 R AND 3346 REF SRM 51-30-2. INSTALLED BEACON AND OPS CHECKED (GOOD) REF SWPM 20-30-12 PG 88-89. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007083100285 20070831 00285 NM 2007 8 31 07FDEA03121 1 20070825 A 5313 BAC1493515 STRINGER BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LWR FWD CARGO PIT FUSELAGE STRINGER UPPER O/B FLANGE HAS CRACK, STA 720 PLUS 14.5" STR 25R. REMOVED DAMAGE REF SRM 53-1 0-3. FABRICATED REPAIR REF SRM 53-10-3 FIG 2, SHEET 2. INSTALLED REPAIR REF 51-30-2 PG 1, PG 1-3, THIS IS CLASSIFIED A S A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007083100287 20070831 00287 NM 2007 8 31 07FDEA03122 1 20070825 A 5311 69436951 FRAME BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD PIT BILGE, BODY FRAME CHORD IS CORRODED, BS 740, STR 27L- 28L, WL149 REMOVED AND REPLACED CHORD ANGLE REF B727 SRM 5 1-30-02 PG 2 DUE TO CORROSION BEING OUT OF LIMITS REF SRM 727 SRM 51-10-1, CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007083100288 20070831 00288 NM 2007 8 31 07FDEA03124 1 20070825 A 5330 6554574 SKIN BOEING 727 727233 138408A NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FOUND DOUBLE DRILLED HOLE AT STA 720F PLUS 5", STR 27R IN NEW SKIN. REMOVED DAMAGE, FABRICATED REPAIR FILLER, STRUCTURA L FILLER AND REPAIR DOUBLER. TREATED AND PRIMED ALL REPAIR PARTS. INSTALLED ALL REPAIR PARTS. REF SRM 53-30-3/FIG NR 3/PAGES 12-14, CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007083100289 20070831 00289 NM 2007 8 31 UPS07450492 1 20070814 A 5420 65B913143 FITTING BOEING 747 747200 1384847 NM NR 4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C NR 4 PYLON REAR ENG MOUNT BULKHEAD UPPER LINK BEAM ATTACHMENT BATH FITTING FOUND CRACKED. CRACK LENGT H .3125 INCH APPROX. NR 4 PYLON REAR ENGINE MOUNT BULKHEAD UPPER LINK BEAM ATTACHMENT BATH FITTING REPLACED AND INSTALL ED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F RT A20WE 2007083100290 20070831 00290 NM 2007 8 31 07FDEA03125 1 20070825 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RIGHT WING LEADING EDGE CAVITY STRINGER AT XOS 667 FOUND CRACKED. COMPLIED WITH FEDEX E.A. 1-5710-115147, CLASSIFIED A S MINOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007083100291 20070831 00291 NM 2007 8 31 07FDEA03126 1 20070825 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RIGHT WING LEADING EDGE CAVITY STRINGER AT XOS 789 FOUND CRACKED. COMPLIED WITH FEDEX E.A. 1-5710-115149, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007083100292 20070831 00292 NM 2007 8 31 07FDEA03127 1 20070825 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 NOSE LANDING GEAR LEFT TRUNNION FITTING FOUND CRACKED. 09-11-07 NOSE LANDING GEAR LEFT HAND TRUNNION FITTING REPAIR CA RRIED OUT AS PER SRM 53-40- 00 FIG. 23 VOL I. REPETITIVE INSPECTION REQUIRED FOR CRACK GROWTH AT NOT TO EXCEED 1500 L ANDING INTERVALS. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007083100294 20070831 00294 NM 2007 8 31 07FDEA03128 1 20070825 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM NLG BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 NOSE LANDING GEAR RIGHT TRUNNION FITTING SUSPECT CRACKED. 09-11-07 NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING REP AIR CARRIED OUT AS PER SRM 53- 40-00 FIG. 23 VOL I. REPETITIVE INSPECTION REQUIRED FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007083100295 20070831 00295 NM 2007 8 31 07FDEA03129 1 20070825 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 LEFT WING LEADING EDGE CAVITY AREA STRINGER AT STATION XOS 790 FOUND CRACKED. 09-11-07 COMPLIED WITH FEDEX EA. 1-5 710-115148, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007083100296 20070831 00296 NM 2007 8 31 07FDEA03130 1 20070825 A 5754 SLAT TRACK DOUG MD11 MD11F 3023600 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 LEFT WING, FIXED LEADING EDGE NR 10 SLAT TRACK CUTOUT INBOARD CORNER FOUND CRACKED. 09-11-07 REPAIR CARRIED OUT AT LEFT HAND WING : FIXED LEADING EDGE NR 10 SLAT TRACK CUTOUT INBOARD CORNER AREA AS PER SRM 57-10-00 FIG. 21 VOL I. CLA SSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007083100298 20070831 00298 EU 2007 8 31 07FDEA03131 1 20070826 A 5347 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 200 SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 446FE 224 MAIN CABIN RIGHT SEAT TRACK Y-1959 AT FRAME 47 LUGS ARE BROKE OUT. 2 L 7 2 4F RT A35EU 2007083100299 20070831 00299 EU 2007 8 31 07FDEA03132 1 20070826 A 5315 102519ITL FLOORBEAM AIRBUS 310 A310203 3930313 EU CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT PIT FRAME 58 T CAP LEFT SIDE ABOVE STRINGER 50L NUT PLATE CORRODED REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, RE MOVED CROSS BEAM AND SPLICE, FABBED CROSSBEAM T-CAP AND SPLICE ANGLES. TREATED REPAIR PARTS AND INSTALLED, IAW A31-200 SRM 51-74-10, 53-10-15 FIG 207, 51-21-10, 51-23-10 PARA 3, 51-40-21 PARA 5 AND 6. 2 L 7 2 4F RT A35EU 2007083100300 20070831 00300 NM 2007 8 31 07FDEA03133 1 20070826 A 5330 DOUBLER DOUG MD11 MD11F 3023600 NM BS 1341 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 CENTER LANDING GEAR STATION 1341.0 LEFT DOUBLER FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007083100302 20070831 00302 NM 2007 8 31 07FDEA03134 1 20070826 A 5330 DOUBLER DOUG MD11 MD11F 3023600 NM BS 1341 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 CENTER LANDING GEAR STATION 1341.0 RIGHT DOUBLER FOUND CRACKED. 09-12-07 REMOVED AND REPLACED AS PER SRM 51-33-01 V OL.II. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007083100303 20070831 00303 NM 2007 8 31 07FDEA03135 1 20070827 A 5754 FITTING DOUG MD11 MD11F 3023600 NM LT WING LE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 LEFT WING, OUTBOARD FLAP LEADING EDGE STOP BOLT FITTING FOUND CRACKED. 09-12-07 REMOVED AND REPLACED AS PER SRM 51- 33-01 VOL. II. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007083100305 20070831 00305 NM 2007 8 31 07FDEA03136 1 20070827 A 5753 HINGE DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 RIGHT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING SUPPORT 1 FASTENER HOLE FOUND CORROSION. 09-04-07 COMPLIED WITH FE DEX E.A. 1-5750-115156, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007083100307 20070831 00307 NM 2007 8 31 07FDEA03137 1 20070827 A 5753 STRUT DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 RIGHT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING STRUT 1 FASTENER HOLE FOUND CORROSION. 09-04-07 COMPLIED WITH F EDEX E.A. 1-5750-115157, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007083100308 20070831 00308 NM 2007 8 31 07FDEA03138 1 20070827 A 5753 STRUT DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 RIGHT WING, OUTBOARD FLAP OUTBOARD HINGE AFT FAIRING STRUT 1 FASTENER HOLE FOUND CORROSION. 09-04-07 COMPLIED WITH FE DEX E.A. 1-5750-115158, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007083100309 20070831 00309 EU 2007 8 31 07FDEA03139 1 20070827 A 5240 A52378078200 STRUCTURE AIRBUS 310 A310324 3930206 EU ZONE 800 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 DAMAGED LATERAL PART ON BULK CARGO DOOR, THE HOLES FROM LOCKING BOLT ARE WORN OUT. REPLACEMENT OF PART IAW SRM 51-52-10 . 2 L 7 2 4F RT A35EU 2007083100310 20070831 00310 EU 2007 8 31 07FDEA03140 1 20070827 A 5240 A52378078200 STRUCTURE AIRBUS 310 A310324 3930206 EU ZONE 800 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 DAMAGED LATERAL PART ON BULK CARGO DOOR, THE HOLES FROM LOCKING BOLT ARE WORN OUT. REPLACEMENT OF PART IAW SRM 51-52-10 . 2 L 7 2 4F RT A35EU 2007083100312 20070831 00312 NM 2007 8 31 07FDEA03141 1 20070827 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 FORWARD CARGO COMPARTMENT, MAIN DECK CARGO SEAT TRACK LBL 47.5 FOUND CRACK. 09-04-07 MAIN DECK CARGO SEAT TRACK FROM STA 625 TO STA 665 LBL 47.5 REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007083100313 20070831 00313 WP 2007 8 31 07FDEA03142 1 20070827 A 5712 RIB DOUG DC10 DC1010F 3022111 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 LT WING INT L/E ON UPPER RIB FOUND CRACK 0.60" LONG. REPAIRED RIB IAW SRM 57-20-00 VOL 1 FIG 1. 2 L 7 3 4F A22WE 2007083100314 20070831 00314 WP 2007 8 31 07FDEA03143 1 20070827 A 5712 RIB DOUG DC10 DC1010F 3022111 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 LT WING INTERNAL L/E ON UPPER RIB FOUND CRACK 0.70" LONG. REPAIRED RIB IAW SRM 57-20-00 FIG 1 VOL I. 2 L 7 3 4F A22WE 2007083100316 20070831 00316 EU 2007 8 31 07FDEA03144 1 20070827 A 5340 A53974321000 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 DEEP CORROSION AT FITTING FRAME 63, STRG 43 LHS. REPLACEMENT OF FITTING IAW. SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007083100317 20070831 00317 WP 2007 8 31 07FDEA03145 1 20070827 A 5720 INTERCOSTAL DOUG DC10 DC1010F 3022111 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 LT WING L/E INTERNAL CRACK LONG 0.50" ON INTERCOSTAL. 10-10-07 REPAIRED INTERCOSTAL IAW SRM 57-00-01 VOL I FIG 10. 2 L 7 3 4F A22WE 2007083100318 20070831 00318 WP 2007 8 31 07FDEA03146 1 20070827 A 5720 INTERCOSTAL DOUG DC10 DC1010F 3022111 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 LT WING L/E CRACK ON INTERNAL INTERCOSTAL. REPAIRED INTERCOSTAL IAW SRM 57-00-01 VOL I FIG 10. 2 L 7 3 4F A22WE 2007083100319 20070831 00319 NM 2007 8 31 ASAA0741997 1 20070826 A 5753 6546430190 SKIN BOEING 737 737490 1384715 NM FORE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 28887 SEVERAL DENTS ON LOWER SURFACE OF RIGHT I/B FORE FLAP. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED SKIN FILLER AND D OUBLER IAW SRM 51-70-10 REPAIR 2. 2 L 7 2 4F RT A16WE 2007083100320 20070831 00320 EU 2007 8 31 07FDEA03147 1 20070827 A 5313 A53980877 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION FOUND ON STRG 56 LT AND RT OUTER FLANGE BETWEEN FRAME 76-77. REPAIR PERFORMED BY CUT STRINGER OUTER FLANGES P 56 LT, ROTO TEST OF OPEN FASTENER HOLES, CORROSION REMOVAL ON SKIN, FLAP PEENING AT SKIN REWORKED AREAS AND INSTALLING R EPAIR ANGLE IAW EA 6-5318-103256 AND RAS/DAHAM/4021169. 2 L 7 2 4F RT A35EU 2007083100321 20070831 00321 EU 2007 8 31 07FDEA03148 1 20070827 A 5313 A53980852204 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION ON STRG 55 LHS BETWEEN FRAME 75-76, REMAINING THICKNESS OUT OF LIMIT. STRINGER SPLICE REPAIR PERFORMED IAW SR M 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007083100322 20070831 00322 EU 2007 8 31 07FDEA03149 1 20070827 A 5313 A53980852202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION ON STRG 56 LHS BETWEEN FRAME 72-73, REMAINING THICKNESS OUT OF LIMIT. STRINGER SPLICE REPAIR PERFORMED IAW S RM 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007083100324 20070831 00324 EU 2007 8 31 07FDEA03150 1 20070827 A 5311 A53974482 FRAME SPLICE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION ON CONNECTION SECTION FRAME 69-70 BETWEEN STRG 45-48 LT, REMAINING THICKNESS IS OUT OF LIMIT. REPAIR PERFORME D BY REPLACEMENT OF AFFECTED PARTS IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007083100325 20070831 00325 EU 2007 8 31 07FDEA03151 1 20070827 A 5330 A53974481210 DOUBLER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION ON INTERNAL WASTE PANEL DOUBLER BETWEEN FRAME 71-72 AND STRG 47-48 RHS. REPAIR PERFORMED BY SMOOTH BLEND OUT AND FLAP PEENING IAW EA-5317-101267 AND RAS/DATLS/0003300/2006. 2 L 7 2 4F RT A35EU 2007083100327 20070831 00327 EU 2007 8 31 07FDEA03152 1 20070827 A 5313 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION ON STRG 59 BETWEEN FRAME 55/58-59, REMAINING THICKNESS OUT OF LIMIT. CONNECTING SECTION REPAIRED IAW SRM 53-1 0-14/FIG 201. 2 L 7 2 4F RT A35EU 2007083100329 20070831 00329 EU 2007 8 31 07FDEA03153 1 20070827 A 5340 A53773644206 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 ENLARGED HOLE IN CORNER FITTING AT FRAME 34,38 AND 38.1 LHS BETWEEM STRG 40-41. REPAIR PERFORMED BY REPLACMENT OF CORNE R FITTINGS IAW. SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007083100337 20070831 00337 NM 2007 8 31 ZZDA2007262 1 20070822 A 5320 PAN BOEING 717 717200 1383700 NM CARGO BAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 930AT 55072 FWD CARGO COMP LOWER PAN HAS CORROSION. INSTALLED LOWER PAN SPLICE REPAIR PER SRM 53-20-15 FIG 201. 2 L 7 2 4F TR A6WE 2007083100347 20070831 00347 NM 2007 8 31 SWAA074204 1 20070825 A 3350 311500 LENS BOEING 737 7373K2 13844BA NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED 20Y CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007083100377 20070831 00377 NM 2007 8 31 AALA20071476 1 20070809 A 3350 MODULE BOEING 767 767223 1385123 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 335AA 22333 JFK - EMERGENCY LIGHTS AT LEFT AND RIGHT NUMBER ONE DOORS INOPERATIVE. REPLACED CONTROL MODULE FOR EMERGENCY LIGHTS AT LEFT AND RIGHT NUMBER ONE DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007083100378 20070831 00378 NM 2007 8 31 AALA20071480 1 20070810 A 2797 RELAY BOEING 737 737823 13844BZ NM STAB TRIM INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 923AN 29524 YYZ INFLIGHT T1084/10AUG - SPEED TRIM FAIL LIGHT ILLUMINATED DURING CLIMB IN CONJUNCTION WITH THE STABILIZER TRIM INOPER ATIVE. LANDED YYZ WITHOUT INCIDENT. REPLACED STABILIZER TRIM CUTOUT RELAY R64 AND ACCOMPLISHED STABILIZER TRIM CUTOUT TEST. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007083100379 20070831 00379 NM 2007 8 31 AALA20071477 1 20070809 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 DFW - EMERGENCY LIGHTS AT SEAT MOUNTED LEFT SEAT ROWS 10 TO 17 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT MOUNTED LEFT SEAT ROWS 10 TO 17. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007083100388 20070831 00388 NM 2007 8 31 SWAA074191 1 20070824 A 5322 6546529 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 23R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007083100416 20070831 00416 NM 2007 8 31 07FDEA03156 1 20070827 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 HFEC INSPECTION CARRIED OUT FOUND 01 EACH LOWER FASTENER HOLE ON THE LONGERON WITH CRACK INDICATION LOCATED NEAR THE L EFT NOSE LANDING GEAR TRUNNION FITTING, APPROX TOTAL LENGTH OF 1/2 INCH LENGTH. 09-12-07 COMPLIED WITH FEDEX E.A. 1 -5310-115173, REPAIR AND SRM 51-31-01 VOL.II. CLASSIFIED AS A MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007090400006 20070904 00006 CE 2007 9 4 DXTA200702417 1 20070822 A 2130 671847711 CONTROL MODULE CESSNA 750 750 2076810 CE CABIN PRESSURE INOPERATIVE E DXTA G O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 GL 07 926QS 9410 7500026 RED CAS MESSAGE " CABIN ALTITUDE" ILLUMINATED AT CRUISE ALTITUDE. PERFORMED CHECKLIST AND LANDED WITHOUT INCIDENT. PAX OXY MASK WERE DROPPED IN MANUAL MODE. REMOVED AND REPLACED CABIN ALTITUDE MODULES IAW CE750 MM. CHAPTER 45-45-03. OPERA TIONAL CHECK GOOD. 2 L 7 2 4J RT T00007WI 2007090400022 20070904 00022 NM 2007 9 4 07FDEA03157 1 20070827 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM FUSLEAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 HFEC INSPECTION CARRIED OUT FOUND 01 EACH LOWER FASTENER HOLE ON THE LONGERON WITH CRACK INDICATION LOCATED NEAR THE R IGHT NOSE LANDING GEAR TRUNNION FITTING, APPROX TOTAL LENGTH OF 3/8 INCH LENGTH. 09-12-07 LONGERON LOCATED NEAR THE RI GHT HAND NOSE LANDING GEAR TRUNNION FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJO R REPAIR AS PER FEDEX GMM 6 -2-100. 2 L 7 3 4F RT A22WE 2007090400023 20070904 00023 NM 2007 9 4 07FDEA03158 1 20070827 A 5710 STRUCTURE DOUG MD11 MD11F 3023600 NM RT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RIGHT WING FIXED LEADING EDGE XOS 717 TO XOS 774 FOUND CHAFED MARK. 09-11-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG.15 VOL. I.REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007090400024 20070904 00024 NM 2007 9 4 07FDEA03159 1 20070827 A 5710 STRUCTURE DOUG MD11 MD11F 3023600 NM RT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT WING FIXED LEADING EDGE BETWEEN XOS 680 TO XOS 717 FOUND CHAFING MARK. 09-11-07 REPAIR CARRIED OUT AS PER SRM 57-1 0-00 FIG.15 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007090400025 20070904 00025 NM 2007 9 4 HALA0700353 1 20070825 A 3610 LUG BOEING 767 767332 1382001 NM TERMINAL BROKEN A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 598HA 23278 RIGHT ENGINE BLEED LIGHT CAME ON DURING CLIMB-OUT. REPLACED BROKEN LUG AT HPSOV TERMINAL ACCOMPLISHED AIR SUPPLY SYSTEM BITE TEST PER AMM 36-23-00. NO FAULTS NOTED CLEARED MIC SHEET. PLACARD REMOVED. 2 L 7 2 4F RT A1NM 2007090400026 20070904 00026 NM 2007 9 4 HALA0700354 1 20070826 A 5520 BOLT BOEING 767 767332 1382001 NM RT ELEVATOR MISSING A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 598HA 23278 RIGHT ELEVATOR, MID ELEVATOR PCA FORWARD ATTACH BOLT NUT NOT INSTALLED. ATTACHED RIGHT ELEVATOR, MID ELEVATOR PCA ATTAC H BOLT, WASHERS, BUSHING, AND NUT INSTALLED PER AMM 27-31-05. 2 L 7 2 4F RT A1NM 2007090400027 20070904 00027 NM 2007 9 4 EIA2007052 1 20070310 A 5313 STRINGER BOEING 747 747212B 1384886 NM BS 460 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 485EV 20712 BS 460 STRINGER 14R EXISTING DOUBLER REMOVED FOR OPEN HOLE HFEC OF REPAIR. REMOVED AND REPLACED DOUBLER AT BS 460 STRIN GER 14R PER ECRA 485-53-185-2. 2 L 7 4 4F A20WE 2007090400028 20070904 00028 EA 2007 9 4 A6WA200740479 1 20070822 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 424AW 7656 FOUND FS 484 FLOORBEAM ANGLE AT LBL 36 IS CRACKED. MAINTENANCE REPAIRED ANGLE BY REMOVING CRACKED ANGLE, FABRICATING NEW ANGLE AND INSTALLING SERVICEABLE ANGLE IAW BSC STANDARD REPAIR 601R-53-0030A AND REO 601R-53-41-059 REV A. (M) 2 L 7 2 4F RT A21EA 2007090400029 20070904 00029 EA 2007 9 4 A6WA200740468 1 20070807 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 466AW 7899 LEFT FUEL TANK ACCESS CUTOUT 540BB AT WS 54.897 HAS CORROSION IN NON-CRITICAL AREA MEASURING 3.5 INCH BY .35 NCH BY .004 INCH DEEP ALONG INBOARD LIP LANDING. MAINTENANCE BLENDED CORROSION ON LEFT FUEL TANK ACCESS CUTOUT 540BB AT WS 54.897 IAW BOMBARDIER REO 601R-57-21-030 REV F. (M) 2 L 7 2 4F RT A21EA 2007090400030 20070904 00030 SO 2007 9 4 SIMA200724101 1 20070828 A 3350 110049 POWER SUPPLY EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHTS FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 806AE 10230 1160 145503 EMERGENCY CEILING LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY SUPPLY IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007090400031 20070904 00031 EU 2007 9 4 N14834CA 1 20070823 A 5711 SPAR AEROSP ATR42 ATR42320 8680930 EU RT WING CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 29747 193 CORROSION ON RIGHT WING REAR SPAR LOWER HORIZONTAL FLANGE BETWEEN THE WING RIBS 16 AND 19. 2 H 7 2 4T RT A53EU 2007090400032 20070904 00032 EA 2007 9 4 A6WA200740466 1 20070721 A 5310 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 FS 280 RBL 9 CLIP P/N 601R31113-58 (OUTBD) IS CRACKED .25 INCH. MAINTENANCE REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-42-13 AND BSC SR 601R-53-0057A. (M) 2 L 7 2 4F RT A21EA 2007090400033 20070904 00033 NM 2007 9 4 DL76S071064 1 20070813 A 5311 FRAME BOEING 767 767332 1382001 NM BS 1809.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 129DL 24079 DURING HMV, STA 1809.5 BULKHEAD OUTER CHORD WAS FOUND CRACKED BETWEEN S-7R AND S-8R. CHORD WAS REPAIRED PER BOEING INST RUCTIONS. 2 L 7 2 4F RT A1NM 2007090400034 20070904 00034 NM 2007 9 4 DL76S071065 1 20070813 A 5420 311T1231 FITTING BOEING 767 767332 1382001 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 129DL 24079 DURING HMV, ONE HOLE IN THE NR 2 PYLON BULKHEAD FITTING COMMON TO THE UPPER SPAR FITTING WAS FOUND CRACKED. CRACK WAS R EPAIRED PER INSTRUCTIONS APPROVED BY BOEING. 2 L 7 2 4F RT A1NM 2007090400035 20070904 00035 NM 2007 9 4 DL757071130 1 20070822 A 5620 PA65457911 WINDOW BOEING 757 757232 1384965 NM PAX CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 662DN 24991 ON MECHANICS PREDEPARTURE CHECK, FOUND A CRACKED OUTER PANE ON PASSENGER WINDOW 31ABC. ON FURTHER INSPECTION, FOUND WIN DOW AT 30 ABC ALSO CRACKED. REPLACED BOTH OUTER PANES. 2 L 7 2 4F RT A2NM 2007090400036 20070904 00036 NM 2007 9 4 DL76L071131 1 20070821 A 5311 145T138212 FRAME BOEING 767 767332 1382001 NM BS 903 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 180DN 25985 RT FS 903.5 LOWER INNER CHORD FOUND CRACKED IN LOWER END RADIUS. REPAIR INSTALLED. SUBJECT AD 2003-18-10 APPLIES. 2 L 7 2 4F RT A1NM 2007090400037 20070904 00037 NM 2007 9 4 DL738071132 1 20070822 A 2611 4739551 CONTROL PANEL BOEING 737 737832 13844CF NM SMOKE A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 394DA 30562 CARGO DET PANEL BEGAN TO SMOKE ON PREFLIGHT. REPLACED CARGO DET/PANEL, OPS NORMAL. 2 L 7 2 4F RT A16WE 2007090400038 20070904 00038 NE 2007 9 4 DL76G071137 2 20070823 A 7200 CF680C2B6F ENGINE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 1 UNKNOWN A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 1613B 29938 32776 706318 L ENG OIL FILTER EICAS MSG, REMOVED AND REPLACED LT ENG SCAVENGE OIL FILTER ELEMENT AND REMOVED AND REPLACED LT ENG OIL FILTER DIFFERENTIAL PRESSURE SWITCH. CHECK ALL CHIP DETECT, NO DEFECT NOTED. PERFORM HIGH POWER RUN FOR 10 MIN ALL IND ICATIONS NORMAL. 2 L 7 2 4F 4 F RT A1NM E13NE 2007090400039 20070904 00039 NM 2007 9 4 DL75E071138 1 20070823 A 5710 STRUCTURE BOEING 757 7572Q8 1384972 NM RT WING DAMAGED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 703TW 27620 DURING THE INSTALLATION OF THE APB BLENDED WINGLET, THERE WAS AN INSTALLATION ERROR WHILE TRIMMING THE SHEAR TIE AT THE RT WING BETWEEN S-11 AND S-12 ON RIB 18 AT WING STATION 565.50. THE HORIZONTAL LEG OF THE 112N5176-6 CHORD UPPER SHEAR TIE SURFACE WAS BLENDED RESULTING IN AN AREA OF REDUCED MATERIAL THICKNESS NEAR THE RADIUS OF THE CHORD. APB WAS CONTAC TED AND PROVIDED AN APPROVED REPAIR CONSISTING OF TRIMMING OUT A PORTION OF THE CHORD, AND LETTING SOME OF THE BLENDS RE MAIN. PLEASE REFER TO 462999-14. 2 L 7 2 4F RT A2NM 2007090400041 20070904 00041 NM 2007 9 4 DLM88071145 1 20070825 A 2910 B-NUT DOUG MD88 MD88 3023688 NM HYD SYSTEM LOOSE A DALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 27 950DL 49881 HYD LOSS ON TOP OF DESCENT DURING FLAP EXTENSION. TIGHTENED B-NUT IN RT WHEEL WELL. SERVICED HYD FAN MOTORS A HYD PUMP S LK CKS GOOD. CYCLED FLIGHT CONTROLS CKS OK. 2 L 7 2 4F RT A6WE 2007090400042 20070904 00042 NM 2007 9 4 DLM88071146 1 20070826 A 3222 STRUT DOUG MD88 MD88 3023688 NM NLG UNDERSERVICED A DALA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 SO 27 905DE 53410 AT GEAR RETRACTION, THERE WAS AN ABNORMAL CLUNK FOLLOWED BY A NOSE GEAR RED UNSAFE LIGHT. NO EVIDENCE OF NLG CONTACT IN NOSE W/W, JACKED AC RAN NLG DISCONNECTED FWD DOORS SHOOK ALL GEAR WIRING NO UNSAFE INDICATION. CHECKED NLG STRUT SVC, FOUND SVC LOW SERVICED NLG STRUT PER MM. RECONNECTED FWD DOORS OPERATED NLG, OPS NORMAL CHECKED SENSORS PROX BOX CKS GO OD. 2 L 7 2 4F RT A6WE 2007090500003 20070905 00003 EU 2007 9 5 07FDEA03164 1 20070828 A 5311 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORRSOSION IN UPPER CORNER FITTING AT FRAME 88, STRG 15-17 RHS. REPAIR PERFORMED BY CUTTING AND INSTALLING DOUBLER IAW EA 6-5319-103257. 2 L 7 2 4F RT A35EU 2007090500010 20070905 00010 EU 2007 9 5 07FDEA03173 1 20070828 A 5311 A53773488200 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 TOOLING MARK (DENT) IN SKIN 240MM BEHIND FRAME 26/32 BETWEEN STRG 50-51 LHS. DENT REPAIR PERFORMED WITH SKIN REPAIR BUS H PER SRM 53-10-12/FIG 221/SH 1 AND 2. 2 L 7 2 4F RT A35EU 2007090500015 20070905 00015 EU 2007 9 5 07FDEA03179 1 20070828 A 5313 A53811373200 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION AT STRG 45, BETWEEN FRAME 39-42 LT. REMAINING THICKNESS OUT OF LIMIT. STRINGER REPAIR PERFORMED WITH PRINC IPLE DESCRIBED IN SRM 53-10-14/FIG 201A, APPROVED BY EA 6-5315-103260 AND RAS/046453/012/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007090500058 20070905 00058 NM 2007 9 5 SWAA074234 1 20070827 A 5315 417A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 749SW 29801 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 986, LBL 32. REPAIRED FLOORBEAM CHORD PER SRM. 2 L 7 2 4F RT A16WE 2007090500060 20070905 00060 NM 2007 9 5 SWAA074226 1 20070827 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 489WN 33855 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007090500062 20070905 00062 NM 2007 9 5 SWAA074218 1 20070827 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 463WN 32467 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 3 ABC AND ROW 8 ABC. REMOVED AND REPLACED COVER PER M M. 2 L 7 2 4F RT A16WE 2007090500063 20070905 00063 NM 2007 9 5 SWAA074219 1 20070827 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 463WN 32467 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 10 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007090500064 20070905 00064 EU 2007 9 5 F3LA200700206 1 20070827 A 5320 D5347112420000 SHEAR PLATE AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED RT SHEAR PLATE BETWEEN FR 69 AND FR 70 CORRODED. REMOVED AND REPLACED SHEAR PLA TE IAW A319 SRM 51-42-11, PARA 6.B. 2 L 7 2 4F RT A28NM 2007090500065 20070905 00065 NM 2007 9 5 SWAA074220 1 20070827 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 463WN 32467 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 19 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007090500068 20070905 00068 EU 2007 9 5 07FDEA03192 1 20070828 A 5330 A5377805020000 SKIN AIRBUS 310 A310324 3930206 EU DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 SKIN DIMPLED FRAME 38, LT SIDE STR 35L AROUND 3 FASTENERS. ACCOMPLISHED HFEC INSPECTION ON 3 EACH DENTS IAW A310 NTM 51 -10-03 WITH NO DEFECTS NOTED. DRESSED OUT TWO DENTS AT STR 39 AND STR 40 IAW A310 SRM 51-73-10. BOTH DENTS FOUND TO BE WITHIN LIMITS IAW A310 SRM 53-10-12 FIG 110 AND DIAGRAM 109. 3RD DENT AT STR 41 FOUND TO BE OUT OF LIMITS IAW A310 S RM 53-10-12 FIG 110 AND DIAGRAM 109. CUT OUT DAMAGE AND TRIMMED 3RD DENT AND INSTALLED SKIN DOUBLER IAW FED EX A310 SRM 53-10-12. 2 L 7 2 4F RT A35EU 2007090500069 20070905 00069 NM 2007 9 5 07FDEA03200 1 20070828 A 5310 BEAM BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 469FE 21581 HORIZONTAL WALKWAY BEAM R/SIDE STATION 320 HAS EVIDENCE OF CORROSION. REMOVED CORROSION ON TOP OF RT WALKWAY BEAM FROM STA 328 TO STATION 336 AND ACCOMPLISHED ULTRASOUND THICKNESS TEST (ACCEPTABLE) REFERENCE 727-200 SRM 53- 10-4 FIG 7. 2 L 7 3 4F A3WE 2007090500070 20070905 00070 NM 2007 9 5 07FDEA03202 1 20070828 A 2120 UNKNOWN DOUG MD11 MD11F 3023600 NM COCKPIT ODOR A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 599FE 48598 PASSING 9000FT AFTER T/O CAPT NOTICED FAINT BURNT PAPER ODOR. NO OTHER INDICATIONS, F/O WENT TO COURIER AREA NO FUMES BUT NOTICED EMERGENCY LIGHT ON. CAPT MADE DECISION TO RETURN TO HKG. DECLARED EMERGENCY, UNEVENTFUL LANDING. PANELED SHUTDOWN ENGS TO REMOVE PWR FROM A/C. REPLACED NR 2B TRANSFORMER RECTIFIER. REMOVED ALL DU, AFS PANELS AND FLIGHT CONT ROL PANELS, NO FAULTS. OVERHEAD CB PANEL INSP'D AND CKD OK. REMOVED AND REPLACED EPCU. REPLACED ALL 3 COALESCER BAGS INSP THE COCKPIT WINDSHIELD HEAT ELECTRICAL WIRE, THE AV COMPT AND LWR FWD CARGO TEMP CONTROL VALVE RT SIDE. EMERG LIG HTS CKD OK. 2 L 7 3 4F RT A22WE 2007090500078 20070905 00078 EU 2007 9 5 07FDEA03208 1 20070829 A 5313 A53974267202 STRINGER AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 FOUND CORROSION ON STRG 56 LT, FRAME 57.3-61. REPAIR PERFORMED BY REMOVAL OF CORROSION AND ROTO TEST IAW EA 6-5317-1125 11 AND RAS/DATLS/003803/2007 ISS "A". 2 L 7 2 4F RT A35EU 2007090500079 20070905 00079 EU 2007 9 5 07FDEA03209 1 20070829 A 5313 A53974267203 STRINGER AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 FOUND CORROSION ON STRG 56 RT, FRAME 57.3-61. REPAIR PERFORMED BY REMOVAL OF CORROSION AND ROTO TEST IAW EA 6-5317-1125 11 AND RAS/DATLS/003803/2007 ISS "A". 2 L 7 2 4F RT A35EU 2007090500080 20070905 00080 EU 2007 9 5 07FDEA03210 1 20070829 A 5754 A57864057205 SKIN AIRBUS 300 A300B4605R 3930308 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 ABRASION FOUND NOSE SKIN OF RT SLAT NR 2 RIB 21-22. REPAIR PERFORMED BY BLEND OUT AND NDT INSPECTION FOR CRACK FREE IAW EA 6-5743-112508 AND RAS/FOK/189/2007 ISS "A". 2 L 7 2 4F RT A35EU 2007090500094 20070905 00094 EU 2007 9 5 SA07054 1 20070827 A 3232 2271500002 ACTUATOR AIRBUS 320 A320214 3930316 EU NLG DOOR FAULTY A USAA O OTHER E VIBRATION/BUFFET CL CLIMB 1 EA 19 111US 20610 1114 LAS FLT 883 EN ROUTE FLL TO LAS. AIRCRAFT EXPERIENCED A VERY LOUD NOISE AND A MILD VIBRATION IN THE COCKPIT DURING CLI MB, WITH ALL INDICATIONS NORMAL. AFTER LEVEL OFF, THE NOSE GEAR DOORS HAD XX-XX INDICATION. THE FLIGHT DESCENDED TO FL 240 AND RECYCLED THE GEAR. THE XX-XX INDICATION WENT AWAY AND THE FLIGHT PROCEEDED TO LAS WITHOUT FURTHER INCIDENT. M AINTENANCE REPLACED THE NOSE LANDING GEAR DOOR ACTUATOR. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007090500095 20070905 00095 NM 2007 9 5 USAA070679 1 20070828 A 5754 65C26601180 SKIN BOEING 737 7373B7 1384580 NM L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 NR 6 SLAT, LOWER T/E AT OUTBOARD END, CRACKED AT RIVET HOLES. INSTALLED FILLER/DOUBLER REPAIR PER SRM 57-43-01, DEFECT SIZE: .125 INCH. 2 L 7 2 4F RT A16WE 2007090500096 20070905 00096 NM 2007 9 5 USAA070667 1 20070828 A 5210 507945178 DOOR FRAME BOEING 737 7373B7 1384580 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 FWD PAX DOOR FRAME CRACKED AT NR 7 STOP PIN CUTOUT. INSTALLED DOUBLER REPAIR PER EA 98819, DEFECT SIZE: .125 INCH. 2 L 7 2 4F RT A16WE 2007090500097 20070905 00097 NM 2007 9 5 USAA070668 1 20070828 A 5210 507945178 DOOR FRAME BOEING 737 7373B7 1384580 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 FWD PAX DOOR FRAME CRACKED AT NR 5 STOP PIN CUTOUT. INSTALLED DOUBLER REPAIR PER EA 98819, DEFECT SIZE: .125 INCH. 2 L 7 2 4F RT A16WE 2007090500098 20070905 00098 NM 2007 9 5 USAA070669 1 20070828 A 5210 507945178 DOOR FRAME BOEING 737 7373B7 1384580 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 FWD PAX DOOR FRAME CRACKED AT NR 6 STOP PIN CUTOUT. INSTALLED DOUBLER REPAIR PER EA 98819, DEFECT SIZE: .125 INCH. 2 L 7 2 4F RT A16WE 2007090500099 20070905 00099 NM 2007 9 5 USAA070670 1 20070828 A 5320 STRUCTURE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 THE 500A AND 500B AT STR 26L AT LIGHTENING HOLE HAS CRACK. MANUFACTURED NEW PART PER SRM 53-30-04, 51-10-02, DEFECT SIZ E: .375 INCH. 2 L 7 2 4F RT A16WE 2007090500100 20070905 00100 NM 2007 9 5 USAA070671 1 20070828 A 5313 6561777505 STRINGER SPLICE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 STA 360 S14L, STRINGER SPLICE HAS CRACK. DRILLED UP NEW PART & INSTALLED PER SRM 51-40-02, DEFECT SIZE: .500 INCH. 2 L 7 2 4F RT A16WE 2007090500102 20070905 00102 WP 2007 9 5 07FDEA03213 1 20070829 A 5230 AFA38063 PAN DOUG DC10 DC1010F 3022111 WP ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 CTR LOWER CARGO DOOR CRACK ON FWD JAMB DOOR PAN. REPAIRED AREA IAW SRM 52-00-01 FIG 7 SHT 2 VOL 1. 2 L 7 3 4F A22WE 2007090500105 20070905 00105 WP 2007 9 5 07FDEA03217 1 20070829 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 FWD CARGO COMPT BILGE AREA FOUND SEVERE CORROSION ON LONGERON. REPAIRED LONGERON IAW SRM 53-10-00 VOL I FIG 1& 2. 2 L 7 3 4F A22WE 2007090500106 20070905 00106 NM 2007 9 5 USAA070672 1 20070828 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 STA 867 AT I/B FASTENER FOR A/C SUPPORT BRACKET, BETWEEN STR 8 & 9R HAS CRACK. INSTALLED TYPICAL FRAME REPAIR DOUBLER P ARTS PER TR 53-10-20E, DEFECT SIZE: .125 INCH. 2 L 7 2 4F RT A16WE 2007090500107 20070905 00107 NM 2007 9 5 USAA070673 1 20070828 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 BS 500 BENEATH RIGHT TRANSITION ANGLE, INTERCOSTAL BAFFLE HAS CRACK. FABRICATED NEW INTERCOSTAL BAFFLE DEFECT SIZE: .375 INCH. 2 L 7 2 4F RT A16WE 2007090500108 20070905 00108 EU 2007 9 5 07FDEA03218 1 20070829 A 5750 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 MISREPAIRED A FDEA K NONE W W W INADEQUATE Q C INADEQUATE Q C INADEQUATE Q C IN INSP/MAINT 1 SO 25 725FD 572 OLD FLUSH DOUBLER REPAIR FOUND ON LT SLAT NR 1 AT UPPER SURFACE BETWEEN RIB 8-10. INVALID REPAIR AS PER SRM 57-42-11/FI G 202 WHICH IS ONLY VALID FOR INBOARD OF RIB 19, STRG 1.3 AND 1.4. REPAIR PERFORMED IAW TD FOK/055/2008 ISSUE: D, APPRO VED BY EA 6-5742-99145A AND RAS/FOK/055/2006 ISSUE: B. 2 L 7 2 4F RT A35EU 2007090500109 20070905 00109 EU 2007 9 5 07FDEA03219 1 20070829 A 5313 A539742022300 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT PIT STRINGER 55L BETWEEN FRAMES 54.2 AND 54.3 CORRODED LEFT SIDE COMPLIED WITH EA 6-5310-112955 FUSELAGE AFT PIT STR INGERS P52L, P54L, P55L REPAIR. 2 L 7 2 4F RT A35EU 2007090500112 20070905 00112 NM 2007 9 5 QXEA200701360 1 20070829 A 2750 FLAP SYSTEM BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 410QX 4053 SEA FLIGHT NR 2465: FLAP POWER CAUTION LIGHT ILLUMINATED. CHECKLIST PROCEDURE COMPLIED WITH. AIRCRAFT RETURNED TO BLOC K. MAINTENANCE RESET FLAP POWER FAULT PER SL D8-400-SL-27-002A. C/W THE OPS TEST OF THE WING FLAPS PER Q400 AMM TASK 2 7-50-00-710-801. OPS CHECK GOOD. NO OTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007090500114 20070905 00114 NM 2007 9 5 KCSA071326 1 20070828 A 5411 FRAME BOEING 747 747209F 1384800 NM NR 4 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 NR 4 PYLON I/B FRAME CRACKED APPROX 10 INCHES ABOVE LOWER SPAR AT NAC STA 236. 2 L 7 4 4F RT A20WE 2007090500115 20070905 00115 EA 2007 9 5 TRAX200701214 1 20070816 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 752EV 10166 PAX DOOR SILL AND FLOOR SUPPORT HAS CORROSION DAMAGE FS 310.00 TO FS 349.00. REMOVED PAX DOOR SILL AND FLOOR SUPPORT AN GLE BLENDED AREAS UNDERNEATH ANGLE FOR CORRISION WITHIN LIMITS. PRIMED AND PAINTED AREAS IAW CRJ 700 SRM 51-12-00 AND 5 1-42-06 CB7015474. INSTALLED NEW PAX DOOR SILL AND FLOOR SUPPORT ANGLE IAW CRJ 700 SRM 51-42-06 CB7015474. INSTALLED P AX DOOR MICRO SWITCH (PROX SWITCH) OPS CHECK GOOD IAW CRJ700 AMM 52-70-04 DH17539. SUPPLEMENTAL - SDR CLOSED 08/28/07. 2 L 7 2 4F RT A21EA 2007090500116 20070905 00116 NM 2007 9 5 QXEA200701362 1 20070829 A 2430 GENERATOR BOMBDR DHC8 DHC8402 1390042 NM NR 2 MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 431QX 4164 PDX FLIGHT NR 2326: ON START UP FOR TAXI, NR 2 DC GEN WOULD NOT COME ON-LINE. RAN CHECKLIST. NO HELP PER CHECKLIST. L EFT NR 2 DC GEN SWITCH OFF. MAINTENANCE CYCLED BUSS FAULT. RESET SWITCH AND C/W OPS TEST OF DC GEN SYSTEM IAW Q400 AMM TASK 24-31-00-710-802. NO DEFECTS NOTED. COULD NOT DUPLICATE DISCREPANCY. NO PARTS REPLACED. AIRCRAFT RETURNED TO S ERVICE. 2 H 7 2 4T RT A13NM 2007090500119 20070905 00119 EU 2007 9 5 F3LA200700209 1 20070829 A 5730 D5725130000200 PANEL AIRBUS A319 A319112 3930323 EU WING CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON ATTACHMENT HOLES ON PANEL 540JB. REPLACED PANEL IAW A319 WORKCARD CP757-2 2 L 7 2 4F RT A28NM 2007090500120 20070905 00120 NM 2007 9 5 NWAA072935516 1 20070829 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 516US 23204 DURING OVERNIGHT CHECK, FOUND DOOR 2 RIGHT EMERGENCY EXTERIOR LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BATTERY SUPP LY. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007090500122 20070905 00122 NM 2007 9 5 KPVA200711 1 20070824 A 4997 AJA4N176 RELAY DHAV DHC8 DHC8103 1386005 NM APU BURNED A KPVA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 13 979HA 373 (PIREP) SMOKE IN COCKPIT AND IN CABIN WHILE BOARDING DOOR OPEN ON GROUND IN JHM. (MX) DETERMINED APU CONTROL RELAY LEFT SIDE NOSE COMPARTMENT MALFUNCTIONED. MEL 49-1 CAT D. (MX) REMOVED & REPLACED RELAY 2449-K62 IAW DHC WD 24-33-03 SHEET 2 PG 1. REMOVED AND REPLACED APU DC STARTER/GENERATOR IAW DHC-8 MM 49-10-01 PG 204-205. CLEARED MEL 49-1. 2 H 7 2 4T RT A13NM 2007090500124 20070905 00124 NM 2007 9 5 AALA20071485 1 20070810 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 777AN 29585 DFW - EMERGENCY LIGHT AT SEAT ROW 20C IS INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 20C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007090500125 20070905 00125 NM 2007 9 5 AALA20071486 1 20070810 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 777AN 29585 DFW - EMERGENCY LIGHT AT SEAT ROW 21C IS INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 21C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007090500126 20070905 00126 NM 2007 9 5 AALA20071504 1 20070811 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 387AM 27184 DFW - EMERGENCY LIGHTS AT SEAT ROWS 32AB TO 41AB INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 3 2AB TO 41AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007090500128 20070905 00128 NM 2007 9 5 WRLA2007088 1 20070823 A 5730 ARB2890502 SKIN DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE RT WING CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 275WA 48631 DURING 3C+12A CHECK, EGAT MECHANIC FOUND CRACK ON RIGHT HAND WING FIXED LEADING EDGE NOSE SKIN AT STA XOS=906. 09-26-0 7 PERFORM NDT/ET FOR REWORK AREA REF JC 0032337. REPAIR CRACK AREA PER MD-11 SRM 57-10-00 FIG.41 VOL.1 REV.40. 2 L 7 3 4F 4 F RT A22WE E24NE 2007090500129 20070905 00129 WP 2007 9 5 AALA20071505 1 20070812 A 2897 CIRCUIT BREAKER DOUG DC9 DC982 3022082 WP FUEL PUMP TRIPPED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7540A 49994 DFW INFLIGHT T2334/12AUG - CREW REPORTED UNABLE TO GET FUEL FLOW FROM CENTER TANK. RETURNED TO DFW AND LANDED WITHOUT I NCIDENT. FOUND CENTER TANK FUEL PUMP CIRCUIT BREAKER POPPED. RESET CENTER TANK FUEL PUMP CIRCUIT BREAKER. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007090500130 20070905 00130 NM 2007 9 5 AALA2071482 1 20070810 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 777AN 29585 DFW - EMERGENCY LIGHT AT SEAT ROW 36C HAS MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 36C. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007090500134 20070905 00134 EU 2007 9 5 AWXA200701034 1 20070823 A 5320 D53472188202 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980124, CORROSION ON CABIN FLOORBEAM, BS 3207/FR67 - BS 3310/FR 69, -Y1162. REPL ACED CABIN FLOORBEAM, BS 3207/ FR67 - BS 3310 / FR 69, -Y1162 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007090500135 20070905 00135 EU 2007 9 5 AWXA200701035 1 20070823 A 5322 D53471124200 SHEAR PLATE AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980127, CORROSION ON LEFT SIDE CABIN SHEAR PLATE, BS 3310/FR69 - BS 3366/FR 70. R EPLACED LEFT SIDE CABIN SHEAR PLATE, BS 3310/FR69 - BS 3366/FR 70 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007090500136 20070905 00136 EU 2007 9 5 AWXA200701036 1 20070823 A 5320 D53472190203 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980149, CORROSION ON CABIN FLOORBEAM, BS 3043/FR64 - BS 3158+5"/FR 66+5", -Y765. REPLACED CABIN FLOORBEAM, BS 3043/FR64, BS 3158+5"/ FR 66+5", -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007090500141 20070905 00141 EU 2007 9 5 AWXA200701041 1 20070826 A 5315 D53472098006 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980123, CORROSION ON CABIN FLOORBEAM, BS 3101/FR 65 - BS 3207/FR 67, +Y919. REPLA CED CABIN FLOORBEAM, BS 3101/FR 65 - BS 3207/FR 67, +Y919 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007090500142 20070905 00142 EU 2007 9 5 AWXA200701042 1 20070826 A 5321 D5361060500100 FLOOR PANEL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK- NR 5980137, CORROSION ON RIGHT CABIN FLOORBOARD 222FF, BS 709/FR 16 - BS 808/FR 20. RE PLACED RIGHT CABIN FLOOR BOARD 222FF, BS 709/FR 16 - BS 808/FR 20 IAW A320 SRM 52-72-11. 2 L 7 2 4F RT A28NM 2007090500143 20070905 00143 EU 2007 9 5 AWXA200701043 1 20070827 A 5320 D53472197200 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980121, CORROSION ON CABIN FLOORBEAM, BS 3257/FR 68 - BS 3366/FR70, -Y470. REPLA CED CABIN FLOORBEAM, BS 3257/FR 68 - BS 3366/FR70, -Y470 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007090500145 20070905 00145 EU 2007 9 5 AWXA200701045 1 20070828 A 5320 D53472192200 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980125, CORROSION ON CABIN FLOORBEAM, BS 3158/FR 66 - BS 3366/FR 70, +Y765. REPLA CED CABIN FLOORBEAM, BS 3158/FR 66 - BS 3366/FR 70, +Y765 IAW A320 SRM 51-72-11 AND 51-42-11. 2 L 7 2 4F RT A28NM 2007090500146 20070905 00146 EU 2007 9 5 AWXA200701047 1 20070825 A 5320 D53112827201 DUMMY RAIL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980106, CORROSION ON CABIN RAIL DUMMY, BS 605/FR12 - BS 709/FR 16, +Y503.2. REPLA CED CABIN RAIL DUMMY, BS 605/FR12 - BS 709/FR 16, +Y503.2 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007090500147 20070905 00147 NM 2007 9 5 QXEA200701363 1 20070830 A 2110 7786953 REGULATOR VALVE DHAV DHC8 DHC8202 2809007 NM A/C PACK MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 369PH 3032 513 SEA FLIGHT NR 2063 - AIR CONDITIONING PACK HOT LIGHT CYCLED ON AND OFF DURING CLIMB-OUT THROUGH 8000 FEET. RAN CHECKLIS T, MANUALLY WARMED THE TEMPERATURE, CAUTION LIGHT EXTINGUISHED. REPLACED PRESSURE REGULATING VALVE IAW AMM TASK. OPERAT IONAL CHECK AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007090500151 20070905 00151 EA 2007 9 5 QXEA200701365 1 20070829 A 3610 GG670800027 SHUTOFF VALVE CNDAIR CL600 CL6002C10 1390015 EA ENGINE BLEED FAILED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 611QX 7363 228 10041 SEA- FLIGHT 2503, RECEIVED A LEFT BLEED CAUTION MESSAGE, RETURNED TO THE GATE. MAINTENANCE PLACED THE SYSTEM ON MEL 36- 11-2 AND RETURNED THE AIRCRAFT TO SERVICE. IN PDX ON 8/30/07, MAINTENANCE REPLACED THE NR 1 ENGINE PRSOV. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007090500152 20070905 00152 EA 2007 9 5 QXEA200701364 1 20070829 A 3610 GG670950023 SHUTOFF VALVE CNDAIR CL600 CL6002C10 1390015 EA ENGINE BLEED FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 609QX 8052 10031 PDX - FLIGHT 2551 (PDX-SBA) ON CLIMB RECEIVED A LEFT BLEED DUCT WARNING MESSAGE FOLLOWED BY A LEFT BLEED DUCT CAUTION. RETURNED TO THE FIELD AND ACCOMPLISHED A OVERWEIGHT LANDING. MAINTENANCE PERFORMED A OVERWEIGHT LANDING INSPECTION AND FOUND THAT DESCENT RATE AND WEIGHT DID NOT MEET OVERWEIGHT LANDING CRITERIA, NO DEFECTS NOTED. REPLACED THE LEFT PACK H OT AIR SHUTOFF VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007090500153 20070905 00153 EA 2007 9 5 QXEA200701366 1 20070830 A 3310 LIGHT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT SPARKS A QXEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 601QX 10009 LIT- FLIGHT 4321, F/O'S MAP LIGHT SHORTED AND SPARKED, THEN THE CIRCUIT BREAKER POPPED. MAINTENANCE DEACTIVATED THE SYST EM BY PLACING A COLLAR OVER THE CIRCUIT BREAKER AND PLACED THE SYSTEM ON MEL 33-11-1. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007090500154 20070905 00154 EU 2007 9 5 DHL2007367502 1 20070807 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH 265 PASSENGER SEAT ATTACHMENT FITTING AT FR 54.2 BEAM NO RT-4 NO 14 MEASURED .041 IS OUT OF LIMITS. REMOVED SEAT TRACK ATTA CH FLOOR SUPPORT AT MAIN CABIN FRAME 54.2 LBL 47 IAW A300 SRM 51-30-00. MEASURE SEAT TRACK ATTACH FITTING .041 FOUND TO BE OUT OF LIMITS IAW A300 SB 94FS494-53-12. INSTALLED SEAT TRACK ATTACHMENT FITTING AT FR 54.2 RT-4 NR 14 IAW A300 SRM 51-30-00 AN SB 94FS494-53-12. 2 L 7 2 4F RT A35EU 2007090500156 20070905 00156 NM 2007 9 5 DHL2007746522 1 20070809 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 950F-970 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 WHILE AT FLIGHTSTAR FOR A "C' CHECK, AFT CARGO COMPT BS 950F-970 STR 28L HAS CORROSION O/B SIDE. CUTOUT DAMAGED AREA DI M 36" IAW B727 SRM 53-10-03 FIG 1, FAB STR REPAIR DIM. 36" MAT. USED BAC1498-145 7075-T6 PO NR 9004219. FAB 3 SPLICE M AT USED BAC1498-131 7075-T6 PO NR 7232174 DIM 3EACH 14.3/4" IAW B727 SRM 53-10-02 FIG 9 AND 53-10-03 FIG 1. TREATED AND PRIMED IAW B727 SRM 51-10-02. INSTALLED STR REPAIR IAW B727 SRM 53-10-03 FIG 1. 2 L 7 3 4F A3WE 2007090500164 20070905 00164 NM 2007 9 5 DHL2007746513 1 20070809 A 5311 FRAME BOEING 727 727224 1384076 NM BS 580 S17R DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 WHILE AT FLIGHTSTAR FOR A "C" CHECK, DENT ON FUSELAGE FRAME BS 580 ABOVE STR 17R. CUT OUT DAMAGE AREA DIM 1" BY 1" IAW B727 SRM 51-40-03. FAB DOUBLER ANGLE REPAIR DIM 9" BY 4" FROM 7075-T6 .050 PO NR 9003230 IAW B727 SRM 51-40-03 FIG 1 AN D LOCATED DRILL IAW B727 SRM 51-30-05. TREATED AND PRIMED AREA IAW B727 SRM 51-10-02. INSTALLED DOUBLER ANGLE REPAIR A T BS 580 IAW B 727 SRM 51-30-02 AND 51-40-03. 2 L 7 3 4F A3WE 2007090500169 20070905 00169 NM 2007 9 5 07FDEA03201 1 20070828 A 2923 MS9391130ZE4C MOTOR BOEING 727 727233 138408A NM HYD PUMP FAILED A FDEA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 25 223FE 20935 LOST SYS "A" HYD QUANTITY. "A" PUMPS WERE OFF FOR LESS THAN 15 MINUTES. QUANTITY REMAINED JUST ABOVE ZERO AFTER COMPLE TE QRH PROCEDURES THEREFORE DID NOT TURN OFF FLUID SHUTOFF. REMOVED AND REPLACED LT AND RT FLAP PWR UNIT HYD MOTORS PER MM 27-51-062-4. OPS AND LEAK CKS GOOD. 2 L 7 3 4F RT A3WE 2007090500170 20070905 00170 NM 2007 9 5 DHL2007746514 1 20070809 A 5311 FRAME BOEING 727 727224 1384076 NM BS 600 S16-17R DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 WHILE AT FLIGHTSTAR FOR A "C" CHECK, DENT ON FUSELAGE FRAME BS 600 BETWEEN STR 16R-17R. CUT OUT DAMAGE AREA, DIM 1" BY 1" IAW B727 SRM 51-40-03 FIG 6. FAB DOUBLER ANGLE REPAIR FROM 7075-T6 .050 PO NR 9003230 DIM 9" BY 4" IAW B727 SRM 51-4 0-03 FIG 1. LEATED DRILL IAW B727 SRM 51-30-05. TREATED AND PRIMED AREA IAW B727 SRM 51-10-02. INSTALLED DOUBLER ANGL E REPAIR AT BS 600 IAW B727 SRM 51-30-02 & 51-40-03. 2 L 7 3 4F A3WE 2007090500172 20070905 00172 NM 2007 9 5 DHL2007746511 1 20070813 A 5311 FRAME BOEING 727 727224 1384076 NM BS 303 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 WHILE AT FLIGHTSTAR FOR A "C" CHECK, FUSE BS 303.9 FRAME AT LT WALKWAY BEAM HAS EXFOLIATED CORROSION WL 143. CUT OUT DA MAGED AREA OF FRAME AT LT WALKWAY BEAM NWW AREA BS 303.9 WL 143 IAW B727 SRM 51-10-4 FIG 5. FABRICATED AND INSTALLED DO UBLER REPAIRS IAW B727 SRM 53-10-2 FIG 1, 53-10-4 FIG 5. MAT USED .063 7075-T6 9.5" BY 4.5" PO NR 9005314 AND .050 7075 -0 7" BY 5" BY 1" PO NR 7229266 HT TREATED TO T6 CONDITION IAW FAS ENG REPORT NR 2-37153-801 REV A (DAMAGE CUTOUT 7" BY 5" BY 1"). ALL PARTS AND AREA TREATED AND PRIMED IAW B727 SRM 51-10-02. 2 L 7 3 4F A3WE 2007090500174 20070905 00174 WP 2007 9 5 DHL2007804513 1 20070724 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 MAIN CARGO COMPT FLOOR PANEL SUPPORT ANGLE CORRODED (STA 8.000 - 70.000, RBL 8" TO 46"). REMOVED CORROSION IAW SRM 51-1 -8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT CORRODED SECTION OF ANGLE AND FABRICATED REINFORCING AN GLE (EXTRUSION P/N S2701008) AND FILLER (ALCLAD 7075T6 0.063") IAW SRM 53-2-0 PG 1. CLEANED, TREATED AND PRIMED AREA AN D REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007090500179 20070905 00179 WP 2007 9 5 DHL2007804516 1 20070807 A 5730 5611013502 PANEL DOUG DC8 DC873F 302199F WP RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 RT WING T/E LWR PANEL DELAMINATED (STA XW 97.000 - XRS 162.000). REMOVED AND REPLACED RT WING T/E LWR PANEL (STA XW 97. 000 - XRS 162.000) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007090500180 20070905 00180 WP 2007 9 5 DHL2007804517 1 20070807 A 5730 PANEL DOUG DC8 DC873F 302199F WP RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 RT WING T/E LWR PANEL DELAMINATED (STA XW 0.0000 - 47.000). REMOVED AND REPLACED DELAMINATED RT WING T/E LWR PANEL (STA XW 0.000 - 47.000) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007090500181 20070905 00181 WP 2007 9 5 DHL2007804518 1 20070807 A 5730 PANEL DOUG DC8 DC873F 302199F WP RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 RT WING T/E LWR PANEL DELAMINATED (STA XRS 162.000 - XF 219.000). REMOVED AND REPLACED DELAMINATED RT WING T/E LWR PANE L (STA XRS 162.000 - XF 219.000) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007083100403 20070831 00403 NM 2007 8 31 SWAA074215 1 20070826 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007083100405 20070831 00405 NM 2007 8 31 SWAA074184 1 20070824 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505C, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007090500183 20070905 00183 WP 2007 9 5 DHL2007804520 1 20070807 A 5730 56488952 PANEL DOUG DC8 DC873F 302199F WP RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 RT WING T/E UPPER PANEL DELAMINATED (STA XA 566.000 - 613.000). REMOVED AND REPLACED DELAMINATED RT WING T/E UPPER PANE L (STA XA 566.000 - 613.000) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007090500187 20070905 00187 NM 2007 9 5 USAA070681 1 20070828 A 5522 65C25746132 SKIN BOEING 737 7373B7 1384580 NM RT ELEVATOR DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 RIGHT ELEV UPPER SKIN, UPPER SURFACE LOCATED 12 INCHES FWD OF T/E & 16 INCHES INBOARD T/E TIP HAS DAMAGE. REPAIR INSTAL LED CONFORMS TO SRM 55-20-01 REPAIR 1, DEFECT SIZE: 8 INCH DIA. 2 L 7 2 4F RT A16WE 2007090500189 20070905 00189 WP 2007 9 5 DHL2007804525 1 20070807 A 5753 5652288506 SKIN DOUG DC8 DC873F 302199F WP TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 NR 2 RT FLAP VANE LWR SKIN DELAMINATED. REMOVED AND REPLACED NR 2 RT FLAP VANE IAW MM 27-51-14 PG 201-202. REFER TO NR 060653 FOR OPS CHECK. 2 L 7 4 4F RT 4A25 2007090500195 20070905 00195 NM 2007 9 5 USAA070682 1 20070828 A 5522 65C25746132 SKIN BOEING 737 7373B7 1384580 NM ELEVATOR DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 UPPER SURFACE, LOCATED 19.5 INCHES FWD OF ELEV TAB T/E & 37 INCHES OUTBOARD OF INBOARD T/E TIP HAS DAMAGE. REPAIR INSTA LLED CONFORMS TO SRM 55-20-01 REPAIR 1, DEFECT SIZE: 5 INCH DIA. 2 L 7 2 4F RT A16WE 2007090500196 20070905 00196 NM 2007 9 5 USAA070683 1 20070828 A 5754 65C26602217 SKIN BOEING 737 7373B7 1384580 NM NR 2 SLAT GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 NR 2 SLAT O/B END UPPER SURFACE, SLAT WEDGE SKIN, GROOVE/GOUGE. INSTALLED NEW CORE FILLER & NEW UPPER SURFACE BONDED DO UBLER PER SRM 57-43-01, 51-70-10, DEFECT SIZE: 1.25 X .250 INCH. 2 L 7 2 4F RT A16WE 2007090500199 20070905 00199 EU 2007 9 5 DHL2007367501 1 20070807 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH 265 PASSENGER SEAT TRACK ATTACHMENT FITTING AT FR 54.2 BEAM NR RH-4 NO 14 MEASURED ,041 IS OUT OF LIMITS. REMOVED SEAT TRAC K ATTACH FLOOR SUPPORT MAIN CABIN FRAME LBL 47IAW IAW A300 SRM 51-30-00. MEASURED SEAT TRACK ATTACH FITTING .041 FOUND TO BE OUT OF LIMITS IAW A300 SB 94FS494-53-12. INSTALLED SEAT TRACK ATTACHMENT FITTING AT FR 54.2 NR RT 4 NR 14 IAW A30 0 SRM 51-30-00 AN SB 94FS494-53-12. 2 L 7 2 4F RT A35EU 2007090500200 20070905 00200 NM 2007 9 5 USAA070685 1 20070828 A 5754 65C26603158M SKIN BOEING 737 7373B7 1384580 NM NR 4 L/E SLAT DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 NR 4 SLAT T/E WEDGE HAS ERODED SKIN & DISBOND ON LOWER SURFACE I/B SIDE OF SLAT. REMOVED DISBONDED AREA, INSTALLED REPA IR PARTS PER TR 57-42-03, SRM 51-70-10, DEFECT SIZE: 2 X 3 INCHES. 2 L 7 2 4F RT A16WE 2007090500203 20070905 00203 NM 2007 9 5 DHL2007746509 1 20070806 A 5751 TAB BOEING 727 727224 1384076 NM AILERON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 DURING AN "C" CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT OUTBD AILERON BALANCE TAB, LEADING EDGE CENTER HAS A CRA CK. REF NR 099154, REMOVED DAMAGED SECTION OF LT O/B AILERON BALANCE TAB L/E CENTER IAW B727 SRM 51-30-2. FABRICATED A ND INSTALLED NEW SECTION IAW B727 SRM 57-50-2,51-30-2 MAT`L USED .016 2024 T3 10" BY 1.75" PO NR 9003189 MAT`L SUBSTITUT ION B727 SRM 51-20-1 USED 2024 T3 INSTEAD OF 5052-H34. TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. 2 L 7 3 4F A3WE 2007090500204 20070905 00204 NM 2007 9 5 USAA070686 1 20070828 A 5754 WEDGE BOEING 737 7373B7 1384580 NM NR 3 L/E SLAT DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 NR 3 SLAT UPPER OUTBOARD WEDGE DISBONDED. INSTALLED REPAIR PARTS PER SRM 51-70-17, 51-70-10, DEFECT SIZE: 1.5 X 2 INCH ES. 2 L 7 2 4F RT A16WE 2007090500205 20070905 00205 EU 2007 9 5 DHL2007367505 1 20070807 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH 265 PASSENGER SEAT ATTACHMENT FITTING AT FR 54.2 BEAM NUMBER RH-3 NR 15 MEASURED .035 IS OUT OF LIMITS. REMOVED SEAT TRACK ATTACH FLOOR SUPPORT AT MAIN CABIN FR 54.2 LBR 38 IAW A300 SRM 51-30-00. MEASURED SEAT TRACK ATTACHMENT FITTING .035 FO UND TO BE OUT OF LIMITS IAW A300 SB 94FS494-53-121R. INSTALLED SEAT TRACK ATTACHMENT FITTING AT 54.2 BEAM RH3 NR 15 IAW A300 SRM 51-30-00 AN SB 94FS494-53-121R. 2 L 7 2 4F RT A35EU 2007090500206 20070905 00206 NM 2007 9 5 USAA070687 1 20070828 A 5730 SKIN BOEING 737 7373B7 1384580 NM RT WING DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 THREE WORKING FASTENER RIGHT WING TO CENTER SECTION Z-ANGLE AT WS 72, AFT 3 FASTENERS ELONGATED. OVERSIZED FIRST OVER, COLD WORKED HOLES & INSTALLED NEW FASTENERS PER SRM 51-40-02, 51-40-03, 51-40-, DEFECT SIZE: .125 INCH 2 L 7 2 4F RT A16WE 2007090500207 20070905 00207 NM 2007 9 5 USAA070688 1 20070828 A 5730 SKIN BOEING 737 7373B7 1384580 NM RT WING DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 WS 72, RIGHT WING, LOWER SURF, Z-ANGLE 3 FWD ATTACH FASTENERS ELONGATED. REMOVED FASTENERS, OVERSIZE & COLD WORK HOLES, & INSTALLED FIRST-OVER FASTENERS PER SRM 51-40-02, 51-40, DEFECT SIZE: .125 INCHES. 2 L 7 2 4F RT A16WE 2007090500208 20070905 00208 NM 2007 9 5 USAA070689 1 20070828 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 532AU 24479 SKIN AT BS 727E + 13 INCHES JUST BELOW S-23L HAS CRACK. FAB'D & INSTALLED DOUBLER PER SRM 53-00-01, REP 31, DEFECT SIZE : 0.2 INCH. 2 L 7 2 4F RT A16WE 2007090500209 20070905 00209 NM 2007 9 5 USAA070690 1 20070828 A 5414 PANEL BOEING 737 7373B7 1384580 NM RT PYLLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 532AU 24479 TOP OF RT ENGINE PYLON AT PANEL 5828R OPENING HAS CRACK. INSTALLED DOUBLER PER TYP REP 54-30-07, DEFECT SIZE: .75 INCH . 2 L 7 2 4F RT A16WE 2007090500210 20070905 00210 NM 2007 9 5 USAA070677 1 20070828 A 5414 SKIN BOEING 737 7373B7 1384580 NM NR 2 PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 PYLON ABOVE NR 2 ENGINE O/B SIDE OF LOAD FITTING PIN HAS CRACK. REMOVED REPAIR, CLEANED AREA, INSTALLED REPAIR WET WITH SEALANT PER TR 57-41-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007090500211 20070905 00211 NM 2007 9 5 2007UALA03339 1 20070823 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 FOUND EMERGENCY LIGHT INOP AT ROW 36 RT & SEAT ROW 34ABC. RELAMPED EMERGENCY LIGHT. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090500213 20070905 00213 NM 2007 9 5 2007UALA03341 1 20070823 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 FOUND UPPER OVERWING EMERGENCY LIGHT INOP LEFT SIDE. REPLACED FUSE. LIGHT OP CHECKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090500214 20070905 00214 NM 2007 9 5 2007UALA03342 1 20070822 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 117UA 28810 EMERGENCY LIGHT STRIP ON UPPER DECK STAIRS IS FALLING OFF. RESECURED LIGHT STRIP ON UPPER DECK STAIRS, OP CHECKS OK . 2 L 7 4 4F 4 F RT A20WE E24NE 2007090500215 20070905 00215 NM 2007 9 5 2007UALA03343 1 20070822 A 3397 CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA 25158 EEL CABLE BROKEN, UPPER DECK FWD END. REPLACED UPPER DECK FWD EEL CABLE, OP CHE CKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090500216 20070905 00216 NM 2007 9 5 2007UALA03345 1 20070823 A 2432 BATTERY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE MAIN FAULTY A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 780UA 26944 MAIN BATTERY + BATTERY CHARGER MAIN STATUS MSG WITH MAIN BATTERY DISCHARGE EICAS. REPLACED MAIN BATTERY AND MAIN BATT ERY CHARGER PER MM24-31-02 AND 24-31-01. BOTH CHECK OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007090500217 20070905 00217 EU 2007 9 5 2007UALA03346 1 20070824 A 3350 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 407UA 456 EMERGENCY LIGHT TEST FAILED. MESSAGE: EPSU BATTERY EMER L. FOUND EPSU BATTERY FAILURE. REPLACED BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007090500218 20070905 00218 NM 2007 9 5 2007UALA03347 1 20070823 A 5310 6547959U78 DOOR FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 913UA 25291 AFT CARGO DOOR CUTOUT, FWD FRAME IS CRACKED AT LWR STOP FITTING. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED FWD FRA ME BS 794. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090500219 20070905 00219 NM 2007 9 5 2007UALA03348 1 20070823 A 5310 6520703066 DOOR FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 913UA 25291 FWD CARGO DOORWAY CUTOUT, AFT FRAME IS CRACKED AT LWR STOP FITTING. MAJOR REPAIR ACCOMPLISHED: REMOVED & INSTALLED NEW FRAME. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090500220 20070905 00220 NM 2007 9 5 2007UALA03349 1 20070823 A 5241 TORQUE TUBE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT GALLEY DOOR EXCESS PLAY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 AFT GALLEY DOOR CUTOUT TORQUE TUBE HAS MOVEMENT BEYOND .003. REMOVED TORQUE TUBE ASSY, UPPER & LOWER LINKS, RADIUS LINK , GUIDE PLATE & STOP PLATE. REPLACED BEARINGS & REINSTALLED PLATES WITH LINKS & REPAIRED TORQUE TUBE ASSY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090500221 20070905 00221 NM 2007 9 5 2007UALA03350 1 20070823 A 5320 ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 PASSENGER CABIN STA 290 JUST ABOVE & BELOW STR 13R ANGLE CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED ANGLE. DRILLED U P & INSTALLED NEW ANGLES. DINOLED AREA. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090500246 20070905 00246 NM 2007 9 5 2007UALA03369 1 20070824 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 EMERGENCY EXIT LIGHT INOP AT AFT CREW REST STAIRS. ONE BULB INOP. RELAMPED. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090500247 20070905 00247 NM 2007 9 5 2007UALA03370 1 20070824 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 EMERGENCY EEL LIGHT INOP AT DOOR 4L GALLEY LOWER WALL CROSSAISLE. SECURED CONNECTOR. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090500248 20070905 00248 NM 2007 9 5 2007UALA03371 1 20070824 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 UPPER DECK EMERGENCY EXIT CEILING LIGHT INOP AT ROWS 12 & 17 & BETWEEN ROWS 15 & 16. RELAMPED EEL IN ALL THREE POSITION S. ALL OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090500249 20070905 00249 NM 2007 9 5 2007UALA03372 1 20070824 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 EMERGENCY EEL LIGHT INOP AT SEAT 4J FWD LIGHT ASSY. REPLACED LAMP. OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090500250 20070905 00250 NM 2007 9 5 2007UALA03374 1 20070821 A 5730 SKIN PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT WING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 LEFT WING IS DAMAGED. REMOVED UNDERWING SKIN PANEL FOR REPLACEMENT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007090500251 20070905 00251 NM 2007 9 5 USAA920070802 1 20070827 A 5320 141N516641 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 942UW 27807 BFM - MAJOR REPAIR - C-04 CHECK - CORROSION FOUND ON FLOOR SUPPORT WEB, BS 395, RBL 27 - RBL 44. REPLACED FLOOR SUPPORT WEB, BS 395, RBL 27 - RBL 44 IAW B757-200 SRM 51-10-02, 53-00-51 AND 51-20-01. 2 L 7 2 4F RT A2NM 2007090500252 20070905 00252 NM 2007 9 5 CALA0700463 1 20070828 A 5311 BAC14902807 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND FRAME CORRODED AT STA 947, S26R TO S27R. THE FRAME WAS REPAIRED IAW SRM 53-00-07. 2 L 7 2 4F RT A16WE 2007090500253 20070905 00253 2007 9 5 COMA0770045 4 20070820 A 3416 ALTIMETER CNDAIR CL600 CL6002C10 1390015 EA COCKPIT ERRATIC A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 391CA 10108 FLIGHT 5257 - AFTER TAKEOFF RADAR ALTIMETER BECAME ERRATIC, FLUCTUATING FROM 300 TO 3000 FT. A TERRAIN ALERT WAS ALSO R ECEIVED AT ABOUT 2000 FT. AIRCRAFT LANDED SAFELY BACK AT CVG. COULD NOT DUPLICATE ON GROUND. OHMED AND MEGGED CABLES, NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007090500254 20070905 00254 EA 2007 9 5 COMA0760534 1 20070820 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 712CA 7244 FLIGHT 5425 - EMERGENCY LIGHT ON CEILING BY LAV INOP. REMOVED AND REPLACED LAMP. 2 L 7 2 4F RT A21EA 2007090500257 20070905 00257 NM 2007 9 5 UPS07650507 1 20070827 A 2150 A/C PACK BOEING 767 76734AF 1385212 NM LEFT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 309UP 27740 INSPECTION TYPE:ETOP RIGHT SYSTEM DUCT PSI LOW, IN FLIGHT AT FL 290 RIGHT DUCT PSI WAS 10 LEFT PACK OFF AIRCRAFT WAS NOT MAINTAINING CABIN ALTITUDE. RECONNECTED HPC ELECTRICAL CONNECTOR. REF MM 36-11-00-5. REPLACED PRSOV PER MM 36-11-09-2. OPS CHECKED SYSTEM, CHECKS OK OPS CHECKED VALVE, CHECKS OK. 2 L 7 2 4F RT A1NM 2007090500323 20070905 00323 2007 9 5 BB07069 4 20070828 A 3140 19314090003 COMPUTER BOEING 757 7572B7 1384964 NM EICAS FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 206UW 27808 FLIGHT 739, LIS-PHL: AFTER TAKEOFF, BOTH EICAS COMPUTERS FAILED. RETURNED TO LIS. MAINTENANCE REPLACED BOTH EICAS COM PUTERS. 2 L 7 2 4F RT A2NM 2007090500324 20070905 00324 NM 2007 9 5 SB07073 1 20070829 A 3350 3004321 LIGHT BOEING 737 7374B7 1384702 NM EXTERIOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 445US 24863 BDL - MAINTENANCE REPORTED THE FORWARD ESCAPE SLIDE EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE LIGHT ASSEMBLY/HOUSING. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007090500325 20070905 00325 NM 2007 9 5 SB07074 1 20070829 A 3230 BACR13CG2AB RELAY BOEING 737 7373B7 1384580 NM LANDING GEAR FAULTY A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 505AU 23380 CLT - FLT 1979 AFTER TAKEOFF FROM CLT, EN ROUTE TO EWR, CREW COULD NOT RAISE THE LANDING GEAR HANDLE. CREW ACCOMPLISH ED QUICK REFERENCE HANDBOOK PROCEDURES AND WAS ABLE TO RAISE GEAR HANDLE USING THE OVERRIDE TRIGGER. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE R27 6 AIR SENSING RELAY ALONG WITH THE GROUND SPOILER TELEFLEX CABLE. OPERATIONAL CHECK GOOD PER MM 32-09-01. 2 L 7 2 4F RT A16WE 2007090500345 20070905 00345 NM 2007 9 5 USAA070694 1 20070830 A 5320 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 STA 344 - 312 FWD ENTRY WAY, LT SIDE HAS CORROSION. REPLACED DAMAGED Z-ANGLE WITH NEW PER SRM 51-10-02, 51-40-03; CORR TASK C53-107-02, DEFECT SIZE: .750 INCH. 2 L 7 2 4F RT A16WE 2007090500346 20070905 00346 NM 2007 9 5 USAA070695 1 20070830 A 5320 65317875 CHANNEL BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 STA 344 - 312, FWD ENTRY WAY, SHORT U-CHANNEL BEAM HAS CORROSION. REMOVED & REPLACED WITH NEW CHANNEL PER SRM 51-10-02, 51-40-03; CORR TASK C53-107-02, DEFECT SIZE: .750 INCH. 2 L 7 2 4F RT A16WE 2007090500349 20070905 00349 NM 2007 9 5 USAA070698 1 20070830 A 2560 FITTING BOEING 737 7373B7 1384580 NM AFT GIRT BAR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 MED AFT GIRT BAR ATTACH POINTS, CORROSION AROUND ATTACH HOLE. REMOVED & REPLACED GIRT BAR BASE FITTING PER SRM 51-20-00 ; COR TASK C53-107-02, DEFECT SIZE: .250 INCH. 2 L 7 2 4F RT A16WE 2007090500350 20070905 00350 NM 2007 9 5 USAA070699 1 20070830 A 5753 65C26603158M SLAT BOEING 737 7373B7 1384580 NM T/E FLAP ERODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 ERODED SKIN & DISBOND, NR 4 SLAT T/E WEDGE, LOWER SURFACE I/B SIDE OF SLAT. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER SRM 51-70-10; TR 57-42-03, DEFECT SIZE: 2 X 3 INCHES. 2 L 7 2 4F RT A16WE 2007090500351 20070905 00351 NM 2007 9 5 USAA070692 1 20070830 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 STA 328, BL 0 HAS CORROSION. REMOVED DAMAGE ON T-CAP, INSTALLED FILLER/ANGLE REPAIR PARTS PER SRM 53-10-51; CORR TASK C 53-107-02; DEFECT SIZE: 3 INCHES. 2 L 7 2 4F RT A16WE 2007090500352 20070905 00352 NM 2007 9 5 USAA070701 1 20070830 A 5320 651768U165 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 BS 312 - 360 LBL 55, CHORD ANGLE HAS CORROSION. REMOVED DAMAGED PARTS & INSTALLED NEW PARTS PER SRM 51-20-01; 51-20-00; CORR TASK C53-107-02, DEFECT SIZE: 3 X 36 INCHES. 2 L 7 2 4F RT A16WE 2007090500353 20070905 00353 EU 2007 9 5 USAA070710 1 20070830 A 5320 D5347218820400 BEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 185UW 1666 Y1292 BEAM BETWEEN FR C68 & 69 HAS CORROSION. 2 L 7 2 4F RT A28NM 2007090500354 20070905 00354 NM 2007 9 5 USAA070704 1 20070830 A 5320 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 FLOOR SUPPORT STA 312 LBL 10 CORRODED. REMOVED DAMAGED AREA & REPLACED WITH NEW FLOOR SUPPORT PER SRM 51-01-02; CORR TS K C53-107-02, DEFECT SIZE: 6 INCHES. 2 L 7 2 4F RT A16WE 2007090500355 20070905 00355 NM 2007 9 5 USAA070705 1 20070830 A 5320 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 STA 312, RBL 12 HAS CORROSION. REMOVED & REPLACED WITH NEW PART PER SRM 51-10-02; CORR TASK C53-107-02, DEFECT SIZE: 6 INCHES. 2 L 7 2 4F RT A16WE 2007090500356 20070905 00356 NM 2007 9 5 USAA070706 1 20070830 A 5340 STRINGER CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 STA 747 S28L, STRINGER TIE CLIP HAS CORROSION. REMOVED & REPLACED STRINGER TIE CLIP PER SRM 51-20-01, 51-10-02; CORR TA SK C53-202-01, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007090600010 20070906 00010 NM 2007 9 6 TAMF20070019S 1 20070825 A 5330 SKIN BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE BS 1536 S36L DENTED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 768QT 23803 DURING INSPECTION OF (C2) CHECK WAS FOUND A DENT A/Y=40 ON LAP SKIN STA 1536 STR 36 - LT. DAMAGED AREA WAS REPAIRED IA W EWO 767-53-049 AND SRM 53-00-01 REPAIR 12. THIS REPAIR CONSTITUTES A MAJOR REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007090600011 20070906 00011 NM 2007 9 6 TAMF20070022S 1 20070822 A 5330 SKIN BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE BS 212 S30R DENTED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 768QT 23803 DURING INSPECTION OF C2 CHECK WAS FOUND A DENT ON LAP SKIN STA 212.5, STR 30-RT. DENT ON LIMITS IAW EWO 767-53-051 AND MFG SERVICE REQUEST 1-526586182. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007090600013 20070906 00013 NM 2007 9 6 TAMF20070015S 1 20070825 A 5330 SKIN BOEING 767 767200 1385120 NM PWA PT6 PT6A114A 52043 NE BS 676-698 DENTED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 768QT 23803 DURING INSPECTION OF (C2) CHECK WAS FOUND A DENT OVER REPAIR DOUBLER AT SKIN STA 676-698 STRINGER 37-38 - RT. THE DOUBL ER NEEDS TO BE REPLACE. DAMAGED AREA WAS REPAIRED IAW EWO 767 53-047 AND SRM 53-00-01 REPAIR 14. THIS REPAIR CONSTITUTE S A MAJOR REPAIR. 2 L 7 2 4F 3 T RT A1NM E4EA 2007090600014 20070906 00014 NM 2007 9 6 TAMF20070020S 1 20070825 A 5751 RIB BOEING 767 767200 1385120 NM PWA PT6 PT6A114A 52043 NE RT AILERON CHAFED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 768QT 23803 DURING C-CHECK INSPECTION WAS FOUND A WEAR OUT OF LIMITS ON IB AILERON RT - OB CLOSURE RIB WEB.DAMAGED AREA WAS REPAIRED IAW EWO 767 57-026 AND SERVICE REQUEST 1-525478883. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 3 T RT A1NM E4EA 2007090600015 20070906 00015 CE 2007 9 6 GLBA20060990 1 20070824 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 228 CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 251GL UE251 UPON ROUTINE INSPECTION MAINTENANCE FOUND CORROSION ON RT SIDE OF BELLY AT FS 228.25 FROM BUTTLINE 2.25 RT TO BUTTLINE 5 .0 RT APPROXIMATELY 1 INCH WIDE. MAINTENANCE REMOVED APPROXIMATELY 6 INCH BY 12 INCH AREA OF SKIN AT FS 228.25 TO REMOV E CORROSION AND INSTALLED INSERTION REPAIR IAW SRM 51-70. RII COMPLIED IAW TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007090600018 20070906 00018 SO 2007 9 6 N93A12082007 1 20070812 A 3250 1159SCH4023 VALVE GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU NLG STEERING FAILED E N93A O OTHER O OTHER TX TAXI/GRND HDL 1 SO 13 408QS 1308 NOSE WHEEL STEERING FAILURE DURING START UP. 2 L 7 2 4F 4 F RT A12EA E25NE 2007090600024 20070906 00024 NE 2007 9 6 DJFA2007096 2 20070819 A 7200 ENGINE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE LEFT FAILED E DJFA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 EA 23 715TA RK189 PCEJA0236 DURING CLIMB 34,000 TO 40,000 HEARD A LOUD BANG & NOTICED LT ENGINE SPOOLING DOWN. DECLARED AN EMERGENCY & DIVERTED. RE START ATTEMPT FAILED. 1 ENGINE LANDING NORMAL, NO PROBLEMS. MX FOUND SEVERE DAMAGE IN AFT PORTION OF ENGINE INCLUDING DAMAGED TURBINE BLADES. INLET SECTION SHOWED NO EVIDENCE OF DAMAGE. ENGINE SEIZED. MX REPLACED ENGINE. 2 H 7 2 4F 4 F RT A16SW E25EA 2007090600027 20070906 00027 CE 2007 9 6 DJFA2007095 1 20070820 A 5510 673207411 STIFFENER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 708LX 5216 7500109 DURING A PHASE 34 INSPECTION MX FOUND THE LT HORIZONTAL STABILIZER TE STIFFENER (P/N 6732074-11) DENTED AND CRACKED, CAU SE WAS FOUND TO BE INTERFERENCE FROM AN INSTALLED LOANER ELEVATOR. THERE ARE NO PROVISIONS IN THE SRM FOR A REPAIR SO MX WILL REPLACE THE DAMAGED PARTS. TO BE UPDATED UPON COMPLETION OF TASK. MX REPLACED THE LT HORIZONTAL STAB STIFFENER P N 6732774-11 WITH NEW STIFFENER (P/N 6732774-11). 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007090600028 20070906 00028 CE 2007 9 6 AMWA25033F 1 20070822 A 5311 1294400681 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 438 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 159YV UE159 FUSELAGE FRAME HAD FRICTION CHAFING. REPAIRED IAW ENGINEERING REPORT 6829-1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007090600031 20070906 00031 CE 2007 9 6 DELA200700006 1 20070820 A 3260 DOWNLOCK SENSOR LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP MLG FALSE INDICATION E DELA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 CE 03 431AS 431 ON APPROACH, LOWERED LANDING GEAR AND HAD RED LIGHT ON RT MLG. RECYCLED GEAR, SAME RESULT. PERFORMED ELECTRICAL MALFUN CTION ALTERNATE GEAR EXTENSION, SAME RESULT. CHANGED LANDING LOCATION; LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED MA LFUNCTIONING RT MLG DOWNLOCK SWITCH. REPLACED SWITCH, PN 1EN1-8. PERFORMED GEAR SWING, OPS CHECK GOOD. 2 L 7 2 4F 4 F A10CE E6WE 2007090600033 20070906 00033 NM 2007 9 6 TIPR200736008 1 20070813 A 5230 SKIN BOEING 767 767222 1385122 NM PWA JT9 JT9D* NE CARGO DOOR DENTED B K NONE O OTHER IN INSP/MAINT 1 SO 05 609UA 21870 BULK CARGO DOOR EXTERIOR SURFACE DENTED NUMEROUS PLACES. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 52-30-01 F IG 101. REFERENCE SERVICE ORDER- 599125 OPERATION-23372. 2 L 7 2 4F 4 F RT A1NM E20EA 2007090600034 20070906 00034 CE 2007 9 6 GUUA08190701 1 20070819 A 3230 UNKNOWN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LANDING GEAR UNKNOWN A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 29 69549 UE194 DURING APPROACH LANDING, GEAR WOULD NOT EXTEND WHEN GEAR HANDLE SELECTED DOWN, DIVERTED. MANUALLY EXTENDED LANDING GEAR . LANDED WITHOUT INCIDENT. TROUBLESHOT SYSTEM COULD NOT DUPLICATE OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007090600037 20070906 00037 EU 2007 9 6 4145081607 1 20070816 A 2110 59008 COMPRESSOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE A/C PACK BINDING E QMLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 125LN 4145 19062 DURING MEDICAL FLIGHT, CREW ENCOUNTERED FUMES AND SLIGHT SMOKE IN THE COCKPIT. PILOT SHUTDOWN A/C THEN ALL ELECTRICAL PO WER IAW CHECKLIST. CREW DEVIATED, APPROXIMATELY 10 MILES DISTANCE. AIRCRAFT LANDED AND SHUTDOWN WITHOUT INCIDENT. SUBSEQ UENT MAINTENANCE EVALUATION SHOWED THE A/C COMPRESSOR WAS SEIZING. NEW COMPRESSOR ORDERED. NO OTHER DAMAGE TO AIRCRAFT N OR HARM TO CREW. 1 G 7 1 3U 3 U H9EU E19EU 2007090600040 20070906 00040 CE 2007 9 6 AMWA86756BC 1 20070817 A 2432 121013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FALSE ACTIVATION A AMWA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 163YV 25794 120 UE163 BATTERY CHARGE ANNUNCIATOR ILLUMINATED WHEN GEAR WAS EXTENDED AND THEN EXTINGUISHED. AC LANDED WITH NO FURTHER INCIDENT . THIS BATTERY CHARGE ANNUNCIATOR WRITEUP IS A NUISANCE WRITEUP AND DISTRACTION TO THE CREW. COULD NOT DUPLICATE ON GR OUND, OPS CHECKS NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007090600044 20070906 00044 CE 2007 9 6 AMWA25033H 1 20070822 A 5311 456129440035 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FS 456 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 159YV UE159 FUSELAGE FRAME HAD FRICTION CHAFING. REPAIRED IAW ENGINEERING REPORT 6829-2. 2 L 7 2 4T 4 T RT A24CE E26NE 2007090600046 20070906 00046 NE 2007 9 6 HEEA116825 1 20070807 A 3260 824037 PROXIMITY SWITCH SKRSKY S76 S76C 8143008 NE MLG OUT OF ADJUST D HEEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 03 781P 760630 RAISED GEAR AFTER TAKEOFF, RED GEAR LIGHT AND NOSE CENTERED LIGHT ILLUMINATED, EXTENDED GEAR, RED LIGHT OUT, CENTERING L IGHT STILL ON. RETURNED TO BASE. MAINTENANCE ADJUSTED CENTERING SWITCH. 1 G 7 2 3U NC H1NE 2007090600047 20070906 00047 NE 2007 9 6 HEEA116826 1 20070808 A 7931 9550170040 PRESSURE SWITCH SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL2S2 60036 NE ENGINE OIL MALFUNCTIONED D HEEA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 03 745P 760619 NR 1 ENGINE OIL PRESSURE LIGHT CAME ON IN FLIGHT. MAINTENANCE REPLACED THE OIL PRESSURE SWITCH. 1 G 7 2 3U 4 U NC H1NE E00054EN 2007090600051 20070906 00051 2007 9 6 HEEA116943 4 20070820 A 2200 CONTROL SWITCH SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL1S1 60030 NE TRIM MALFUNCTIONED E HEEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 03 761P 760588 DURING TAKEOFF, AFTER RELEASING THE FORCE TRIM BUTTON AT (4), CYCLIC WOULD COME AFT. MAINTENANCE INSPECTED THE AIRCRAF T, CONNECTED A HYDRAULIC MULE AND WORKED ALL CONTROLS. THEY WERE UNABLE TO DUPLICATE THE DISCREPANCY. 1 G 7 2 3U 3 U NC H1NE E19EU 2007090600054 20070906 00054 NM 2007 9 6 2007F00045 1 20070825 A 2497 TERMINAL BLOCK BOEING 777 777 UTILUSE NM GE GE90 GE9092B 30036 NE ELECTRICAL SYS BURNED W ZCQF D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 29 A6EBR 5563 WD608 906227228 A/C RETURNED TO STAND DUE TO ACRID BURNING ODOR AND SMOKE IN FLT DECK AFTER SECOND ENG START. CABIN CREW AT L1 ALSO REP ORTED STRONG ODOR AND HEARD A NOISE FROM THE FWD E/E BAY BELOW HER JUMP SEAT. P110 PANEL SHOWED BURN MARKS, MONITOR CA RD M24518 BURNED. TERMINAL BLOCK ATTACHED TO ABOVE ALSO BURNED. SHORT LENGTH OF WIRES BURNED AND BLACKENING OF WIRES N EARBY NOTED. 2 L 7 2 4F 4 F RT T00001SE E00049EN 2007090600062 20070906 00062 CE 2007 9 6 GLBA20060987 1 20070813 A 5313 STRINGER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 163 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 208GL UE208 FRAME CRACKED AT STRINGER 9R RELIEF HOLE ON FRAME AT F.S. 163.975. MAINTENANCE REPAIRED THE AFFECTED AREA AT FS 163.975 IAW SRM 51-70. REPAIR APPROXIMATELY 5 INCH BY 2INCH. RII INSPECTION COMPLIED WITH IAW TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007090600067 20070906 00067 2007 9 6 0097614 3 20070718 A 6110 BEARING RACE HAMSTD EMB 120 EMB120 3260201 SO PROPELLER CORRODED B EY2R K NONE O OTHER IN INSP/MAINT 1 GL 03 BEARING RACE CORROSION. 2 L 7 2 4T RT A31SO 2007090600069 20070906 00069 2007 9 6 0097442 3 20070706 A 6110 7901822 DOME EMB 120 EMB120 3260201 SO PROPELLER CORRODED B EY2R K NONE O OTHER IN INSP/MAINT 1 GL 03 DOME CORRODED. 2 L 7 2 4T RT A31SO 2007090600077 20070906 00077 CE 2007 9 6 GLBA20060983 1 20070814 A 5313 STRINGER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 451 S10R CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 208GL UE208 (2) CRACKS FOUND ON STRINGER 10R AT F.S. 451.0. FORWARD CRACK .5625 INCH LONG AFT CRACK .2500 INCH LONG. MAINTENANCE RE PAIRED CRACKS ON STRINGER 10R AT F.S. 451.0 IAW SRM 51-70. REPAIR APPROXIMATELY 9 INCHES LONG. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007090600081 20070906 00081 CE 2007 9 6 AMWA25033I 1 20070822 A 5311 4681294400364 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FS 468 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 159YV UE159 FUSELAGE FRAME DAMAGED BY CHAFING. REPAIRED IAW ENGINEERING REPORT 6829-2, REV 1R DATED AUG 1, 2007. 2 L 7 2 4T 4 T RT A24CE E26NE 2007090600086 20070906 00086 NM 2007 9 6 EVA96001 1 20070730 A 5753 65B1706478 FLAP TRACK BOEING 747 74745E 1384947 NM NR 5 TE FLAP FRACTURED W QOCF K NONE O OTHER IN INSP/MAINT 1 WP 03 16407 61718 27899 B-16407. DURING C01 CHECK, FRACTURE WAS DETECTED ON NR 5 FLAP TRACK (PN 65B17064-78) FWD END CLEVIS. THE FLAP TRACK HAD PERFORMED THE AD 2003-14-15 REQUIRED SB 747-57-2307 ACTION. THE DAMAGE PART HAD SENT TO MFG FOR ANALYSIS. 2 L 7 4 4F RT A20WE 2007090600092 20070906 00092 EU 2007 9 6 07FDEA03271 1 20070831 A 5313 A53772135 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DEBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 DEBONDED STRINGER ON P36-40, FRAME 20-24 LT. REPAIR PERFORMED BY INSTALLING RIVETS IAW SRM 53-10-14 / FIG 202. 2 L 7 2 4F RT A35EU 2007090600093 20070906 00093 EU 2007 9 6 07FDEA03273 1 20070831 A 5320 A53771417206 SILL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 CORROSION AT FWD CARGO DOOR SILL BEAM, BETWEEN FRAME 20A-25A, STRG 43-44 RT REPAIR PERFORMED BY CUT THE UPPER FLANGE OF CORNER FITTING AT C24 AND INSTALLING REPAIR ANGLE IAW EA 6-5313-99224 AND RAS/DABRE/7006397/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600097 20070906 00097 EU 2007 9 6 07FDEA03277 1 20070831 A 5740 A53510218201 BRACKET AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 FOUND HEAVY CORRODED BRACKET ON RT WING IN KRUEGER FLAP AREA, FRAME 38-39. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 57-45-11. 2 L 7 2 4F RT A35EU 2007090600098 20070906 00098 EU 2007 9 6 07FDEA03278 1 20070831 A 5740 A53510217201 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 FOUND HEAVY CORRODED FITTING ON RT WING IN KRUEGER FLAP AREA, FRAME 38-39. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 57-45-11. 2 L 7 2 4F RT A35EU 2007090600099 20070906 00099 EU 2007 9 6 07FDEA03279 1 20070831 A 5710 A53510216203 BEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 FOUND HEAVY CORRODED BEAM ON RT WING IN KRUEGER FLAP AREA, FRAME 38-39. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 57-45-11. 2 L 7 2 4F RT A35EU 2007090600102 20070906 00102 EU 2007 9 6 07FDEA03282 1 20070831 A 5330 A53978157200 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 DENT FOUND AT FRAME 65, STRG 41-42 RT. REPAIR PERFORMED BY REMOVAL OF AFFECTED FASTENERS, ROTO-TEST INSPECTION WITH NIL FINDINGS, EDDY CURRENT INSPECTION OF SKIN, INTERNAL BONDED DOUBLER AND INTERNAL BUTT STRAP WITH NIL FINDINGS AND INSTAL LATION OF NEW FASTENERS IAW EA 6-5317-99143 AND RAS/DAHAM/4020579/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600105 20070906 00105 EU 2007 9 6 07FDEA03285 1 20070831 A 5730 A57340087 SKIN PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 ELONGATED HOLES ON PYLON NR 2 SUPPORT BRACKET AND LOWER WING SKIN, RIB 7-8 RT. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLATION OF FREEZE PLUGS IAW EA 6-2900-106507 AND RAS/BAE/1005210/2007 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600106 20070906 00106 EU 2007 9 6 07FDEA03286 1 20070831 A 5730 A57340087 SKIN PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 ELONGATED HOLES ON PYLON NR 1 SUPPORT BRACKET AND LOWER WING SKIN, RIB 7-8 LT. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLATION OF FREEZE PLUGS IAW EA 6-2900-106507 AND RAS/BAE/1005210/2007 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600108 20070906 00108 EU 2007 9 6 07FDEA03288 1 20070831 A 5730 A57340086 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 600 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 OLD REPAIR DOUBLER PLATES ON BOTTOM WING SKIN PANEL NR 1 BOTH RHS AND LHS, BETWEEN RIB 8 AND TRACK 4 FWD OF FRONT SPAR A RE NOT PERFORMED IAW DRW R572- 40179/PG 9 (SB A300-57-6019). IN ADDITION THE INSTALLED HI-LOCKS ARE IN BAD CONDITION. REPAIR RENEWED BY INSTALLING CRACK STOP PLUGS AT HOLES NR 7 AND NR 9 (LHS ONLY) AND INSTALLING AFT LANDING PLATES ON BO TH SIDES IAW DRW R572-40179 SHEET 9 AND 10. APPROVED BY EA 6-5710-101323 AND RAS/BAE/1002496/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600109 20070906 00109 EU 2007 9 6 07FDEA03289 1 20070831 A 5320 A53980071 FLOOR SUPPORT AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 AFTER REMOVAL OF OLD GROOVES AT LONGITUDINAL BEAMS (LT & RT) FRAME 73A-75A, THE REMAINING THICKNESS IS OUT OF LIMIT. BO TH PARTS REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007090600112 20070906 00112 EU 2007 9 6 07FDEA03292 1 20070831 A 5340 A53973613200 ATTACH FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 DAMAGED FITTING AT FRAME 63A BETWEEN STRG 42-46, RHS, ATTACH FITTING REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007090600113 20070906 00113 EU 2007 9 6 07FDEA03293 1 20070831 A 5751 A57240497000 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 FOUND AT ALL SPEED AILERON HINGE RIBS LT/RT DEEP CHAFING MARKS. ON THE INTERMEDIATE RIBS WIAX21-9 POSITIONS ON BOTH W INGS, DAMAGE WAS ALSO FOUND AT THE INTERMEDIATE RIB WIAX13-9 ON THE RT WING. REPAIR PERFORMED BY BLENDING AND REPROTECT ION AT POSITIONS RIB WIAX13-9, WITH THE INSTALLATION OF A DOUBLER AT POSITIONS WIAX21-9 AS PER TD/J1/S1/0234/2006 ISSUE B. APPROVED BY EA 6-5751-99137 AND RAS/BAE/1002354/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600114 20070906 00114 EU 2007 9 6 07FDEA03294 1 20070831 A 5751 A57240497000 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 FOUND AT ALL SPEED AILERON HINGE RIBS LT/RT DEEP CHAFING MARKS. ON THE INTERMEDIATE RIBS WIAX21-9 POSITIONS ON BOTH W INGS, DAMAGE WAS ALSO FOUND AT THE INTERMEDIATE RIB WIAX13-9 ON THE RT WING. REPAIR PERFORMED BY BLENDING AND REPROTECT ION AT POSITIONS RIB WIAX13-9, WITH THE INSTALLATION OF A DOUBLER AT POSITIONS WIAX21-9 AS PER TD/J1/S1/0234/2006 ISSUE B. APPROVED BY EA 6-5751-99137 AND RAS/BAE/1002354/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600116 20070906 00116 EU 2007 9 6 07FDEA03296 1 20070831 A 5320 A53612201201 FLOOR SUPPORT AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 Z-SECTION ANGLE ( X3892, Y730 ) OF LAVATORY FLOOR STRUCTURE IS CRACKED BY DAMAGE UNDER THE FITTING ( Z-174, Y925 ). REP AIR PERFORMED IAW SRM 51-71-40/FIG 201. 2 L 7 2 4F RT A35EU 2007090600117 20070906 00117 WP 2007 9 6 07FDEA01450 1 20070411 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP BS 1561 MISREPAIRED A FDEA K NONE W W W INADEQUATE Q C INADEQUATE Q C INADEQUATE Q C IN INSP/MAINT 1 SO 25 397FE 46631 MD10-10 ACF MODIFICATION AND REPAIR ASSESTMENT DURING INSPECTION FOUND EXISTING REPAIR WITH MISSING SEALANT STA 1561 B/T L51 LT TO L 51 RT. REPAIR HAS BEEN ACCOMPLISHED IN COMPLIANCE WITH SRM 53-30-00 FIG 8. NO ACTION REQUIRED. REPAIRED SEALANT IAW SRM 51-41-01 VOL II. 2 L 7 3 4F RT A22WE 2007090600123 20070906 00123 EU 2007 9 6 07FDEA03302 1 20070902 A 5320 A53771417202 SILL AIRBUS 310 A310203 3930313 EU FWD PIT FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 FWD LOWER CARGO PIT ANGLE REPAIR AT FR 24 STRINGER 43R AT DOOR SILL JAMB. EVALUATED AND FOUND TO NOT MEET APPROVED FAA REQUIREMENTS. REMOVED AND REPLACED REPAIR ANGLE AT FR 24 STRINGER 43R IAW FEDEX EA NR 6-5310-112957 FUSELAGE FWD CARGO D OOR LOWER SILL INCOMING REPAIR. 2 L 7 2 4F RT A35EU 2007090600131 20070906 00131 EU 2007 9 6 07FDEA03312 1 20070903 A 5320 A53610986201 ANGLE AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 NUMEROUS FASTENERS WERE FOUND TO BE NON CONFORMING AND ELONGATED ON FITTING FRAME 12A, FRAME 12A AND CORNERS RT AND LT SIDES. REPAIR PERFORMED BY DETAILED VISUAL AND ROTO TEST INSPECTIONS IN DAMAGED HOLES, REPLACMENT OF FITTING, CORN ER SPLICE AND CORNER ANGLE WITH INSTALLATION OF NEW SPLICE UNDER STRG 26. INSTALLING REPAIR BUSHES IN FRAME 12A WEB RT SIDE ONLY AND OVERSIZED FASTENERS IAW TD 942.043937/012/2006. APPROVED BY EA 6-5312-99226 AND RAS/AS/0047/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600133 20070906 00133 EU 2007 9 6 07FDEA03314 1 20070903 A 5311 A53610319211 FRAME AIRBUS 300 A300B4622R 3930312 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 TOOLING MARKS WERE FOUND AT FRAME 12A BETWEEN STRG 26-27 RT. REPAIR PERFORMED BY REMOVING FASTENERS, SMOOTH BLEND OUTS, FOR ELIMINATE THE DEEPEST MARK A 13MM SKIN HOLE DIA WAS PERFORMED, ROTO TEST AND HFEC INSPECTION WITH NIL FINDINGS AN D ONE 13MM DIAMETER SHOULDERED BUSH WAS INSTALLED AS PER SRM 53-10-12/FIG 221 WITH A ASNA2019-40 FASTENER. REPAIR IAW E A 6-5312-101254 AND RAS 044514/014/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600134 20070906 00134 EU 2007 9 6 07FDEA03315 1 20070903 A 5712 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 CRACK DAMAGE ON LT WING LEADING EDGE CLOSING RIB WOFX-277.9. REPAIR PERFORMED BY TRIMMING OUT THE DAMAGED AREA, LOCALLY MANUFACTURING AND INSTALLING AN INFILL PACKER AND REPAIR ANGLE USING EXISTING AND NEW FASTENER POSITIONS IAW TD/J1/02 572/2006 ISSUE A APPROVED BY EA 6-5741-99184 AND RAS/BAEE/1002572/2008 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600135 20070906 00135 WP 2007 9 6 07FDEA03318 1 20070903 A 5320 ADA37741 PAN DOUG DC10 DC1010F 3022111 WP DOOR FRAME CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 LOWER CENTER CARGO DOOR CRACK LONG .250" AND DEFORMATION ON LWR FORWARD CORNER. 11-07-07 REPAIRED AREA IAW SRM 52-1 0-00 FIG 17 VOL I. 2 L 7 3 4F A22WE 2007090600137 20070906 00137 EU 2007 9 6 07FDEA03323 1 20070903 A 5340 A53973613200 ATTACH FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 CRACKED FITTING AT FRAME 63 OF SILL BEAM. REPLACEMENT OF FITTING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007090600138 20070906 00138 EU 2007 9 6 07FDEA03324 1 20070903 A 5310 A53810876 BEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 AFTER HFEC INSPECTION FOUND 18MM LONG CRACKS IN GANTRY BEAM 3 LT AND RT AT FRAME 49 LOWER INBOARD FLANGE. CRACK REPAIR PERFORMED ON FRAME 49 GANTRY 3 LT AND 3 RT PER DRW R538-10426 WITH ENLARGED DIAPHRAGM WORK AREA WHILE MAINTAINING AN EDG E DISTANCE OF 1.5 RIVET DIAMETER IAW EA 6-5315-99180 AND RAS 044008/013/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600139 20070906 00139 EU 2007 9 6 07FDEA03325 1 20070903 A 5754 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 OLD FLUSH DOUBLER REPAIR FOUND ON SLAT NR 2 RT THAT REQUIRES REWORKING. REPAIR RENEWED IAW TD FOK/065/2006 ISSUE C, APP ROVED BY EA 6-5740-99182A AND RAS/FOK/065/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600140 20070906 00140 EU 2007 9 6 07FDEA03326 1 20070903 A 5100 SKIN AIRBUS 300 A300B4622R 3930312 EU RUDDER MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 WASHERS USED BY OLD REPAIR ON RUDDER ARE NOT CONFORM TO SRM 55-41-12/PB 201/FIG 216. DELAMINATION, CORRODED AND TOO SHO RT FASTENERS. DELAMINATION OF GFRP FITTING CONNECTION REPAIR PERFORMED AT ALL HINGE FITTINGS IAW SRM 55-41-12/FIG 216. 2 L 7 2 4F RT A35EU 2007090600142 20070906 00142 EU 2007 9 6 07FDEA03328 1 20070903 A 5330 A53985240204 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 CORROSION SPOTS ON EXTERNAL SKIN PANEL BETWEEN FRAME 78-88, STRG 5 LT TO 5 RT. REPAIR PERFORMED BY SMOOTH BLEND OUT, HF EC AND ROTO TEST INSPECTION, INSTALLING AN EXTERNAL REPAIR DOUBLER AND FLAP PEENING IAW TD/K4/S1/20147/2005/A APPROVED B Y EA 6-5319-92222 AND RAS/DAHAM/4020147/2005. 2 L 7 2 4F RT A35EU 2007090600143 20070906 00143 EU 2007 9 6 07FDEA03259 1 20070831 A 5210 A5211010401211 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 800 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 725FD 572 FOUND OLD DOUBLER REPAIR ON FWD RT PAX DOOR LOWER FWD CORNER NOT CONFORM TO SRM REPAIR RENEWED IAW SRM 52-10-00 FIG 204. 2 L 7 2 4F RT A35EU 2007090600150 20070906 00150 EU 2007 9 6 07FDEA03266 1 20070831 A 5311 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 CORROSION FOUND ON FWD FACE OF FRAME 92 ON DOUBLER. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007090600152 20070906 00152 EU 2007 9 6 07FDEA03268 1 20070831 A 5310 A53973085210 BEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 HEAVY CORROSION AT AFT CARGO DOOR SILL BEAM, BETWEEN FRAME 63-63A, STRG 42-43 RT REPAIR WAS PERFORMED IAW SRM 53-17-18/F IG 205. 2 L 7 2 4F RT A35EU 2007090600154 20070906 00154 WP 2007 9 6 07FDEA03229 1 20070829 A 5730 ARB0936 DOUBLER DOUG MD10 MD1010F 3022112 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 LT WING L/E CRACK 1" ON TEE ANGLE FIXED PANEL REPAIRED WING LOWER L/E STRINGER DOUBLER IAW SRM 57-10-00 FIG 49. 2 L 7 3 4F RT A22WE 2007090600156 20070906 00156 WP 2007 9 6 07FDEA03234 1 20070829 A 5347 S4929149 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 MAIN CABIN SEAT TRACK HAS CORROSION AT STA.720 AT LBL 107. REMOVED, FABRICATED AND INSTALLED SPLICED PLATE, SPLICE HAT AND SEAT TRACK IAW MD/DC10 SRM 53-70-00 VOL I PGE 3-4,51-31-01 VOL II PGE 1-10,53-70-00 PG E51 VOL I AND PART MARKED IAW FED EX GMM 7-0-1000. MAJOR REPAIR MECH 111258 QC 348. 2 L 7 3 4F RT A22WE 2007090600157 20070906 00157 NE 2007 9 6 07FDEA03235 2 20070829 A 7200 ENGINE BOEING 727 727277 138408S NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAILED A FDEA E B A ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 25 242FE 21178 685599 FL350, FELT VIOLENT SHUDDER, NR 2 EGT MAXED OUT, OIL PRESS DROPPED TO APPROX 15 PSI. SHUTDOWN ENG AND EGT DROPPED. NO FIRE INDICATIONS. REMOVED AND REPLACED NR 2 ENG PER FEDEX ENG CHANGE W/C. OPS AND LEAK CHECK OK RII:226917. 2 L 7 3 4F 4 F RT A3WE E2EA 2007090600158 20070906 00158 EU 2007 9 6 07FDEA03236 1 20070830 A 5730 A57340087 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 FOUND THE HYDRAULIC FITTING HOLES IN PYLON SUPPORT BRACKET IN LOWER SKIN PANEL OF THE LT AND RT WING ELONGATED. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLATION OF REPAIR BUSHES IAW R571-50532 ISSUE: A APPROVED BY EA 6-5720-99183 AND RAS/BAE/1002415/2006 ISSUE: A. 2 L 7 2 4F RT A35EU 2007090600161 20070906 00161 NM 2007 9 6 07FDEA03239 1 20070830 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM WING TO BODY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RIGHT WING TO FUSELAGE BODY FAIRING LONGERON 27, STA 1305 FOUND WITH CORROSION. 09-11-07 RIGHT HAND WING TO FUSELA GE BODY FAIRING LONGERON REMOVED & REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6- 2-100. 2 L 7 3 4F RT A22WE 2007090600162 20070906 00162 EU 2007 9 6 07FDEA03240 1 20070830 A 5311 A53810787 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 FOUND DEVIATIONS BETWEEN RAS/AS/212/2003A AND A/C CONDITION AND DEVIATIONS TO SB 53-6125 ON FRAME 45, STRG 26-28 RHS AND LHS. REPAIR: HOLES H1 RT AND LT AND H2 FRAME 45 LT: COLD WORKING, BUSH INSTALLATION IN FRAME AND DOUBLER, NEW NOMINAL FASTENER NSA5351V4 INSTALLATION. HOLE H4 FRAME 45 LH: COLD WORKING, 2ND OVERSIZED FASTENER NSA5359-9 INSTALLATION. REP AIR APPROVED AND IAW EA 6-5315-99181 AND RAS/018565/049/2002 ISSUE: A WHICH SUPERSEDES RAS/AS/212/2003 ISSUE: A. 2 L 7 2 4F RT A35EU 2007090600165 20070906 00165 EU 2007 9 6 07FDEA03243 1 20070830 A 5313 A53610567 STRINGER AIRBUS A300 A300F4622R 3930360 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 CORROSION FOUND AT STRG 44 LT BETWEEN FRAME 16A-17. STRUCTURE REPAIR PERFORMED IAW SRM 53-12-14 / FIG 201. 2 L 7 2 4F RT A35EU 2007090600166 20070906 00166 EU 2007 9 6 07FDEA03244 1 20070830 A 5320 A53974259200 PROFILE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 DEFORMED LONGITUDINAL PROFILE BETWEEN FRAME 65-66 LHS OF AD OF FLOOR SUPPORT STRUCTURE. REPAIR PERFORMED BY REPLACEMENT OF LONGITUDINAL PROFILE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007090600167 20070906 00167 EU 2007 9 6 07FDEA03245 1 20070830 A 5320 A53974263202 PROFILE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 DEFORMED LONGITUDINAL PROFILE BETWEEN FRAME 65-66 RHS OF AD OF FLOOR SUPPORT STRUCTURE. REPAIR PERFORMED BY REPLACEMENT OF LONGITUDINAL PROFILE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007090600168 20070906 00168 NM 2007 9 6 07FDEA03246 1 20070830 A 5315 6520827 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FRAME 680 FLOORBEAM LBL 4", CORRODED ON UNDERSIDE OF SCREW HOLE. REMOVED CORROSION, MEASURED MATERIAL. ORG MATERIAL THI CKNESS .125". REMOVED .035" REMAINING .090" FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AREA. FABRICATED REPAIR ANGLES AND FILLER. TREATED AND PRIMED REPAIR PARTS. INSTALLED REPAIR PARTS. ANGLES WERE HEAT TREATED TO TH1050 CONDITION THEN CAD PLATED PER REF 51-10-2 PG 7 SRM 51-30-02, PG 2, FED EX DWG SR 27-53-034 REPAIR NR 1, REV F, SRM 53-10-1 FIG 5, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007090600170 20070906 00170 EU 2007 9 6 07FDEA03248 1 20070830 A 5730 A57241132201 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 CHAFING MARK IN SKIN OF LEADING EDGE RT WING, BETWEEN TRACK 3 AND 4. REPAIR PERFORMED BY REPLACEMENT OF SKIN PANEL IAW SRM 51-72-10 (SRM 57-41-12/ FIG 6/ITEM 5). 2 L 7 2 4F RT A35EU 2007090600173 20070906 00173 EU 2007 9 6 07FDEA03251 1 20070830 A 5315 A53974322214 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 HEAVY CORROSION ON TOP CAP BEAM FRAME 63, BETWEEN Y805 TO Y1470. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 / FIG 207. 2 L 7 2 4F RT A35EU 2007090600176 20070906 00176 EU 2007 9 6 07FDEA03254 1 20070830 A 5751 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 DELAMINATION AT OUTBOARD TRAILING EDGE AREA, RIB 18 OF ALL SPEED AILERON RHS. REPAIR PERFORMED IAW TD FOK/051/2006, APP ROVED BY EA 6-5760-99146 AND RAS/FOK/051/2006 ISSUE B. 2 L 7 2 4F RT A35EU 2007090600181 20070906 00181 EU 2007 9 6 07FDEA03333 1 20070904 A 5710 A57111092203 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 FOUND CRACK IN HOLE G/T OF ANGLE FITTING IN CENTER WING BOX AT FRAME 47 LT DURING SB A300-57-6086, -6050, AND -6049. REPAIR PERFORMED BY OVERSIZING THE HOLES IN ALL LAYERS ON A STEP BY STEP BASIS, ROTO TEST INSPECTION AT EACH STEP AND IN STALLING OVERSIZED FASTENERS IAW EA 6-5710-92223 AND RAS/AS/0297/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600182 20070906 00182 EU 2007 9 6 07FDEA03334 1 20070904 A 5710 A57111092202 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 FOUND CRACK IN HOLES H, G, Q, S AND T OF ANGLE FITTING IN CENTER WING BOX AT FRAME 47 RT DURING SB A300-57-6086, -6050, AND -6049. REPAIR PERFORMED BY OVERSIZING THE HOLES IN ALL LAYERS ON A STEP BY STEP BASIS, ROTO TEST INSPECTION AT EACH STEP AND INSTALLING OVERSIZED FASTENERS, 3 BUSHES INSTALLED IN EACH HOLE OF Q/S IAW EA 6-5710-92223 AND RAS/AS/0297/2 005 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600187 20070906 00187 2007 9 6 07FDEA03258 4 20070830 A 2220 56024004 ACTUATOR BOEING 727 727233 138408A NM STAB TRIM FAILED A FDEA O OTHER O OTHER CL CLIMB 1 SO 25 282FE 22349 CLIMBING THRU FL190 A/P CRUSE TRIM WOULD NOT WORK IN EITHER DIRECTION, NOR WOULD THE MAIN ELC TRIM WORK IN THE NOSE DOWN DIRECTION. RECYCLED THE CUTOUT SWITCHES, BUT STILL DIDN'T WORK. NO STAB TRIM C/B'S WERE POPPED ON THE DESCENT THE TR IM STARTED TO WORK NORMALLY. REMOVED AND REPLACED AUTO PILOT STAB TRIM SERVO IAW MM 22-11-021-2 AND REMOVED AND REPLA CED MAIN ELECTRIC STABILIZER TRIM ACTUATOR PER MM 27040-031-2. 2 L 7 3 4F RT A3WE 2007090600189 20070906 00189 NM 2007 9 6 DHL200774650 1 20070809 A 5313 STINGER BOEING 727 727224 1384076 NM BS 680 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 DURING A "C" CHECK AT FLIGHTSTAR, THE FOLLOWING DISCREPANCIES WERE NOTED REF NR 099305, FWD CARGO COMPT STA 685 STR 27R HAS CORROSION IN CENTER OF SPLICE. REMOVED STRINGER SPLICE AT STR 27R STA 680 IAW B727 SRM 51-30-2 FIG 1. FAB NEW SPLI CE FROM BAC 1498-131,7075 T6 PO NR 7232174, DIM 12" IAW B727 SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9. TREATED AND PRIMED IA W B727 SRM 51-10-2. STRINGER SPLICE INSTALLED AT STR 28R STA 680 IAW SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2007090600191 20070906 00191 EU 2007 9 6 DHL2007367506 1 20070807 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH 265 PASSENGER SEAT ATTACHMENT FITTING AT FR. 54.2 BEAM NUMBER LH-5 NUMBER 21 MEASURED .038 AN IS OUT OF LIMITS. REMOVED SEA T TRACK ATTACHMENT FITTING AT FR 54.2 NR LH-5 NR 21 IAW A300 SRM 51-30-00 AN SB 94FS494-53-12 R1. MEASURED SEAT TRACK A TTACHMENT FITTING .038 FOUND OUT OF LIMITS PER SB 94FS494-53-12 R1. INSTALLED SEAT TRACK ATTACHMENT FITTING AT FR 54.2 BEAM NR LH5 NR 21 IAW A300 SRM 51-30-00 AN SB 94FS494-53-12 R1. 2 L 7 2 4F RT A35EU 2007090600192 20070906 00192 NM 2007 9 6 DHL2007746515 1 20070809 A 5311 FRAME BOEING 727 727224 1384076 NM BS 480 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 WHILE AT FLIGHTSTAR FOR A "C" CHECK, DENT ON FUSELAGE FRAME BS 480 ABOVE STR 17R. CUT OUT DAMAGE AREA DIM 1" BY 1" IAW B727 SRM 51-40-03 FIG 1. FAB DOUBLER ANGLE. REPAIR FROM 7075-T6 .050 PO NR 9003230 DIM 9" BY 4" IAW B727 SRM 51-40-03 FIG 1. LOCATED DRILL IAW B727 SRM 51-30-05. TREATED AND PRIME IAW B727 SRM 51-10-02. INSTALLED DOUBLER ANGLE REPAIR I AW B727 51-30-02 & 51-40-03. 2 L 7 3 4F A3WE 2007090400014 20070904 00014 EU 2007 9 4 SIMA200724002 1 20070826 A 3350 330151 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 393AE 18474 67 340B393 LEFT EMERGENCY EXIT LIGHT ON CEILING INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHTING POWER SUPPLY 23LN IAW SAAB AM M 33-50-04. OPERATIONAL TEST GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007090400043 20070904 00043 NM 2007 9 4 DLM88071147 1 20070826 A 5330 593666751 SKIN DOUG MD88 MD88 3023688 NM FS 1211 L28R DENTED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 920DL 49644 AIRCRAFT STRUCK BY GROUND EQUIPMENT AT C-3 DOOR CUTOUT. LOWER SKIN AND DOUBLERS DENTED. DAMAGE CUTOUT AND DOUBLERS INS TALLED 2 L 7 2 4F RT A6WE 2007090400044 20070904 00044 NM 2007 9 4 DL764071149 1 20070827 A 2121 732591F FAN BOEING 767 767432ER 1385134 NM EQUIP COOLING OVERHEATED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 825MH 29696 ELEC ODOR IN COCKPIT AT FLT 350 AND .80 MACH WITH EQUIP COOLING FAN STATUS MSG. REPLACED FWD EQUIP COOLING EXHAUST FAN PER M/M. MCO/PLAC RMVD. 2 L 7 2 4F RT A1NM 2007090400045 20070904 00045 NM 2007 9 4 DL76S071150 1 20070827 A 2120 UNKNOWN BOEING 767 767332 1382001 NM COCKPIT ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 126DL 24076 NOTICED BURNING ODOR DISCOVERED C/B G-26 FLT CONT ELEC 2R POPPED. NO OTHER ABNORMAL INDICATIONS. REPLACED CSEU PER AM M, OPS NML. 2 L 7 2 4F RT A1NM 2007090400046 20070904 00046 2007 9 4 DL764071151 4 20070828 A 3460 COMPUTER BOEING 767 767432ER 1385134 NM E/E MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 832MH 29704 DIVERT DUE TO LOSS OF BOTH FMS COMPUTERS AND AUTO-PILOT. REPLACED BOTH FMS COMPUTERS AND MODE CONTROL PANEL. 2 L 7 2 4F RT A1NM 2007090400047 20070904 00047 WP 2007 9 4 DHL2007804500 1 20070716 A 5712 RIB DOUG DC8 DC873F 302199F WP NR 1 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 NR 1 STUB WING RIB JOINT ANGLE CRACKED 0.750", STA XFS 529.000. REMOVED CRACKED ANGLE IAW SRM 51-1-21. FABRICATED NEW ANGLE (AL7075"0" 0.080") IAW DWG NR 9753297. HEAT TREATED FROM AL7075"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED AREA AND NEW ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007090400048 20070904 00048 WP 2007 9 4 DHL2007804501 1 20070714 A 5711 FRAME DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 RT OUTERWING INBD L/E CRACKED 0.500" AT LWR FORMER STA XFS 635.000. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE AND FABRICATED (2EA) ANGLE DOUBLER (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-20D, SRM 51-3-1 PG 2 (TORQUE). 2 L 7 4 4F RT 4A25 2007090400049 20070904 00049 WP 2007 9 4 DHL2007804526 1 20070813 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 230 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 PERFORMED DETAILED VISUAL INSPECTION OF REPAIR AND FOUND IT TO BE NOT IN ACCORDANCE WITH SRM. PERFORMED MAJOR REPAIR IA W FAA FORM 8110-3 DATED 08-13-07, ASTAR EVA D853-00013-001-D REV IR DATED 08-08-07. REMOVED NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. VISUALLY INSPECTED L-23L AND FOUND 3/4 INCH CRACK. CUT OUT LONGERON DAMAGED SEGMENT P/N 270487 7 AND FABRICATED NEW SEGMENT (EXTRUSION 7075T651, P/N S264145ST) AND SPLICES P/N 2641454 IAW SRM 53-4-0 FIG 28 SHEET 1 I TEM "J" SRM 51-2-0 FIG 50 (SHEET 70), SRM 53-2-2 FIG 10, TR NR 53-153 DATED 12-10-02. FABRICATED REPAIR DOUBLER (AL7075 T6 0.090") AND FILLER (AL7075T6 0.080") IAW ASTAR EVA D853-00013, DWG ASTAR ES D853-00013-001-D. PERFORMED NDT INSPECTI 2 L 7 4 4F RT 4A25 2007090400050 20070904 00050 WP 2007 9 4 DHL2007804527 1 20070813 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 160 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 PERFORMED DETAILED VISUAL INSPECTION OF REPAIR AND FOUND IT TO BE NOT IN ACCORDANCE WITH SRM. PERFORMED MAJOR REPAIR IA W FAA FORM 8110-3 DATED 08-13-07, EVA D853-00014 REV IR DATED 08-07-07. DRAWING AD79-23-104 REV IR DATED 08-03-07. REM OVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICATED (2EA) FILLERS ( AL7075T6 0.071") AND DOUBLER (AL7075T6 0.080") IAW EVA D853-00014 REV IR, COTNEY DWG AD79-53-104 REV IR. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 08-00-02 TO 07. NO CRACK FOUND. ENCLOSED SMN FORM 242-4. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW EVA D853-00014 REV IR, COTNEY DWG AD79-53-104 REV IR, 2 L 7 4 4F RT 4A25 2007090400051 20070904 00051 WP 2007 9 4 DHL2007804528 1 20070813 A 5320 STRUCTURE DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 FUSELAGE EXTERIOR PRIMARY HEAT EXCHANGER AFT UPPER CORNER ACS MODIFICATION DOUBLER 0.375" CRACK STA -12.000 L-24L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 08-13-07, ASTAR EVA D853-00007 DATED 07-10-07, ASTAR DWG ES D853-00007-001 DATED 08-06-07. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED (2EA) REPAIR FILLERS (AL2024T3 0.100") AND REPAIR DOUBLER (AL2024T3 0.050") AND REPAIR TRIPLER (AL2024T3 0.063") IAW EVA D853-0007, A STAR DWG ES D853-00007-001. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 08-00-02 TO 07. ENCLOSED SMN FORM 242-4. CL EANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW EVA D853-0007, ASTAR DWG ES 2 L 7 4 4F RT 4A25 2007090400052 20070904 00052 WP 2007 9 4 DHL2007804529 1 20070715 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT TE FLAP MISREPAIRED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 RT OUTBD FLAP T/E UPPER PANEL HAS A NON-STANDARD REPAIR AT STA XF 375.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW BO EING MSG NR 1-405802434-2 DATED 06-07-07. REMOVED PANEL PLATING WITH EXISTING NON-STANDARD REPAIR IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PANEL PLATING (AL2024T3 0.025") AND BONDED FINGER DOUBLER (AL2024T3 0.020") IAW BOEING MSG NR 1-405802434-2, DOUGLAS DWG NR 5654759. BONDED BOTH PARTS WITH HYSOL IAW SRM 51-1-9, SRM 51-1-9A, DPS 1.950 REV AR R- 1. CLEANED, TREATED AND PRIMED AREA AND PANEL PLATING INNER FACE IAW SRM 51-1-8B. INSTALLED PANEL PLATING IAW BOEING M SG NR 1-405802434-2, SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE) REFER TO JC EC-00454-001 (WO 1616) FOR 2 L 7 4 4F RT 4A25 2007090400053 20070904 00053 WP 2007 9 4 DHL2007804502 1 20070714 A 5711 FRAME DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 RT OUTER WING INBD L/E UPPER FORMER CRACKED 0.500" STA XFS 691.250. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE AND FABRICATED (2EA) ANGLE DOUBLER (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOU BLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007090400054 20070904 00054 WP 2007 9 4 DHL2007804503 1 20070726 A 5320 565122114 CHANNEL DOUG DC8 DC873F 302199F WP MLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 RT MLG, ZEE CHANNEL OF FAIRING CRACKED 4", STA XW 3.125. REMOVED CRACKED ZEE CHANNEL IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED ZEE CHANNEL (P/N 5651221-14SP) IAW SRM 51-1-21. REFER TO JC EC-00426-001 ( WO 1616) FOR FABRICATION. 2 L 7 4 4F RT 4A25 2007090400055 20070904 00055 WP 2007 9 4 DHL2007804504 1 20070728 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 LT OUTER WING INBD L/E SKIN HOLES ELONGATED, STA XFS 710.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-25-07 , DWG NR AD79-57-101 REV IR DATED 07-13-07. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAM AGED SECTION IAW DWG NR AD79-57-101 REV IR. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 08-00-02 TO 07. NO CRACK NOR CORROSION FOUND. ENCLOSED SMN FORM 242-4. FABRICATED REPAIR DOUBLER (AL7075T6 0.063") AND FILLER (AL7075T6 0.050") IA W DWG NR AD79-57-101 REV IR. CLEANED, TREATED AND PRIMED AREA, FILLER AND INNER FACE OF REPAIR DOUBLER IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DWG NR AD79-57-101 REV IR, SRM 51-1-11, SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D, SRM 51-3-1 ( 2 L 7 4 4F RT 4A25 2007090400056 20070904 00056 WP 2007 9 4 DHL2007804505 1 20070801 A 5730 PANEL DOUG DC8 DC873F 302199F WP LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 LT WING T/E UPPER SURFACE PANEL CORRODED, STA XRS 74.000. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMI TS IAW SRM 57-2-0 PG 16. REMOVED CORRODED PANEL ASSY IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PANEL ASSY IAW SRM 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007090400057 20070904 00057 WP 2007 9 4 DHL2007804506 1 20070803 A 5310 STRUCTURE DOUG DC8 DC873F 302199F WP MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 804DH 85412 46124 PPERFORMED DETAILED VISUAL INSPECTION AND FOUND A PREVIOUS REPAIR NOT IN ACCORDANCE WITH SRM. PERFORMED MAJOR REPAIR IA W SRM 53-2-1 FIG 7 SHEET 1, 4. REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED REPAIR D OUBLER (AL7075T6 0.063") (2EA) INTERNAL FINGER DOUBLER (AL7075T6 0.032") IAW SRM 53-2-1 FIG 7 SHEET 1, 4, SRM 53-3-3 FIG 1 ITEM A. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 53-2-1 FI G 7 SHEET 1, 4, SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE). THIS IS A CLASS 1 REPAIR: INITIAL 4.000, REPETITIVE 4.000, REPLACEMENT N/A IAW SRM 53-2-1 FIG 5, TR NR 53-190 DATED 09-20-03. REINSPECT DUE AT 34.822 LANDING. 2 L 7 4 4F RT 4A25 2007090400058 20070904 00058 WP 2007 9 4 DHL2007804507 1 20070803 A 5310 STRUCTURE DOUG DC8 DC873F 302199F WP BS 1730 MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 804DH 85412 46124 PERFORMED DETAILED VISUAL INSPECTION AND FOUND PREVIOUS REPAIR NOT IN ACCORDANCE WITH SRM. PERFORMED MAJOR REPAIR IAW S RM 53-2-1 FIG 7 SHEET 1-5. REMOVED EXISTING NON-STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER (AL7075T6 0.050") IAW SRM 53-2-1 FIG 7 SHEET 1, 5, SRM 53-5-3 FIG 1 ITEM "E". CLEANED, T REATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 53-2-1 FIG 7 SHEET 1, 5, SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D, SRM 51- 3-1 (TORQUE). THIS IS A CLASS 1 TYPE REPAIR, INITIAL 4.000, REPETITIVE 4.000, REPLACEMENT N/A IAW SRM 53-2-1 FIG 5, TR NR 53-190 DATED 09-20-03. REINSPECT DUE AT 34.822 CYCLES LANDING. 2 L 7 4 4F RT 4A25 2007090400059 20070904 00059 WP 2007 9 4 DHL2007804508 1 20070803 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 RT WING UPPER SKIN CRACKED 1 1/4" AT STA XCW 69.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 20 SHEET 1. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW SRM 57-2-1 FIG 20 SHEET 1. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 08-00-01 TO 07. NO CRACK NOR CORROSION FOUND. ENCLOSED SMN FORM 242-4. FABRICATED REPAIR DOUBLER (AL7075T6 0.160") REPAIR TRIPLER (AL7075T6 0.125") AND FILLER (AL7075"0" 0.312") IAW SRM 57-3-3 FIG 13 I TEM "L", SRM 57-2-1 FIG 20 SHEET 1, SRM 51-1-4. HEAT TREATED FILLER FROM 7075"0" TO 7075T651 IAW SRM 51-1-1 PG 1, 13, 1 7. CLEANED AREA AND APPLIED POLYURETHANE TOP COATING AND REPAIR PARTS IAW SRM 51-1-12. INSTALLED REPAIR PARTS IAW SRM 2 L 7 4 4F RT 4A25 2007090400060 20070904 00060 WP 2007 9 4 DHL2007804509 1 20070801 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP BS 521 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 "B" CARGO DOOR FWD LWR JAMB CORNER CRACKED 1/2" STA 521.000 L-31R TO L-32R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW F AA FORM 8100-9 DATED 07-20-07, BOEING MSG NR 1-425040944-2 DATED 07-20-07, AD2005-18-07, DOUGLAS DWG NR 57507776, ASTAR EVAD852-00012 REV IR DATED 03-18-07, DWG SEMAN ED-4580 DATED 07-09-07. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-1-20B. CUT OUT DAMAGED SECTION IAW SEMAN DWG ED-4580. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 08-00-02-0 7. NO CRACK NOR CORROSION FOUND. ENCLOSED SMN FORM 242-4. FABRICATED REPAIR DOUBLER (AL7075T6 0.090") (2EA) FILLER (A L7075T6 0.071") AND REPAIR TRIPLER (AL7075T6 0.125") IAW SMN DWG ED-4580. CLEANED, TREATED AND PRIMED AREA AND REPAIR P 2 L 7 4 4F RT 4A25 2007090400061 20070904 00061 WP 2007 9 4 DHL2007804510 1 20070803 A 5310 STRUCTURE DOUG DC8 DC873F 302199F WP BS 1710 MISREPAIRED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 PERFORMED DETAILED VISUAL INSPECTION AND FOUND PREVIOUS REPAIR NOT IN ACCORDANCE WITH SRM. PERFORMED MAJOR REPAIR IAW S RM 53-2-1 FIG 7 SHEET 1, 5. REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTIO N AND FABRICATED REPAIR DOUBLER (AL7075T6 0.063") INTERNAL FINGER DOUBLER (AL7075T6 0.032") AND FILLER (AL7075T6 0.050") IAW SRM 53-2-1 FIG 7 SHEET 1, 5, SRM 53-5-3 FIG 1 ITEM "E". CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 53-2-1 FIG 7 SHEET 1, 5, SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TO RQUE). THIS IS A CLASS 1 TYPE REPAIR: INITIAL 4.000, REPETITIVE 4.000, REPLACEMENT N/A IAW SRM 53-2-1 FIG 5, TR NR 53-1 2 L 7 4 4F RT 4A25 2007090400062 20070904 00062 NM 2007 9 4 UIEA 1 20070828 A 5753 PANEL BOEING 747 74747UF 1384812 NM TE FLAP DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 492 29253 RT IB T/E AFT FLAP IMPACT DAMAGE 195" FROM IB END AND 4" FROM TE OF LE PANEL 3.5" OF DELAMINATION AND 2" BY 1" CRACK. 2 L 7 4 4F RT A20WE 2007090400063 20070904 00063 EA 2007 9 4 A6WA200740467 1 20070721 A 5315 601R3111358 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 FOUND FS 280 RBL 9 INBOARD CLIP, P/N 601R31113-58 IS CRACKED. MAINTENANCE REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51 -42-13 ABD BSC SR 601R-53-0057A. (M) 2 L 7 2 4F RT A21EA 2007090500004 20070905 00004 EU 2007 9 5 07FDEA03165 1 20070828 A 5311 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORRSOSION IN UPPER CORNER FITTING AT FRAME 88, STRG 15-17 RHS. REPAIR PERFORMED BY CUTTING AND INSTALLING DOUBLER IAW EA 6-5319-103257. 2 L 7 2 4F RT A35EU 2007090500005 20070905 00005 NM 2007 9 5 07FDEA03167 1 20070828 A 5753 VANE DOUG MD11 MD11F 3023600 NM TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 LEFT WING, OUTBOARD FLAP VANE INSIDE OF LEADING EDGE ACCESS HOLE FOUND CORRODED. 09-11-07 REMOVED AND REPLACED AS PER AMM 27-50-32-4. ADJUSTMENT CARRIED OUT AS PER AMM 27-50-32-5 FOUND SATISFACTORY. LH WING OUTBOARD FLAP OPERATION CHECK CARRIED OUT AS PER AMM 27-50-00-2 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007090500006 20070905 00006 EU 2007 9 5 07FDEA03168 1 20070828 A 5720 PANEL AIRBUS 310 A310324 3930206 EU ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 DELAMINATION FOUND ALONG THE EDGE LANDING OF L/E PANEL A572-46071, BETWEEN TRACK 7-8 ON RT WING. REPAIR PERFORMED BY REMOVING THE DAMAGED LAYERS AND PERFORMING A HOT BOND REPAIR AND RESTORING THE ALUMINIUM LAYER ON THE INTERNAL SURFACE I AW EA 6-5741-103258 AND RAS/BAE/1003272/2008 ISS "A". 2 L 7 2 4F RT A35EU 2007090500007 20070905 00007 EU 2007 9 5 07FDEA03169 1 20070828 A 5311 A53988624207 FRAME AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION ON CROSS STRUT FRAME 86, STRG 15 RHS. REMAINING THICKNESS OUT OF LIMIT. CROSS STRUT REPLACED IAW SRM 51-72-1 0. 2 L 7 2 4F RT A35EU 2007090500011 20070905 00011 EU 2007 9 5 07FDEA03174 1 20070828 A 5330 A53978468200 BUTTSTRAP AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 DRILLING MARK FOUND ON BUTT STRAP AT FRAME 65, STRG 37 RHS. REPAIR PERFORMED BY CUT OUT DAMAGE AND INSTALLING NEW BUTT STRAP PORTION IAW EA 6-5317-103259 AND RAS/DAHAM/4021137/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007090500014 20070905 00014 EU 2007 9 5 07FDEA03178 1 20070828 A 5313 A53811374202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION AT STRG 44, BETWEEN FRAME 39-44 LT. REMAINING THICKNESS OUT OF LIMIT. STRINGER REPAIR PERFORMED WITH PRINC IPLE DESCRIBED IN SRM 53-10-14/FIG 201A, APPROVED BY EA 6-5315-103260 AND RAS/046453/012/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007090500016 20070905 00016 EU 2007 9 5 07FDEA03180 1 20070828 A 5313 A53811372200 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION AT STRG 46, BETWEEN FRAME 39-42 LT. REMAINING THICKNESS OUT OF LIMIT. STRINGER REPAIR PERFORMED WITH PRINC IPLE DESCRIBED IN SRM 53-10-14/FIG 201A, APPROVED BY EA 6-5315-103260 AND RAS/046453/012/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007090500017 20070905 00017 EA 2007 9 5 TRAX200701234 1 20070823 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 FWD ASD ANCHOR FITTING CORRODED. 2 L 7 2 4F RT A21EA 2007090500018 20070905 00018 EU 2007 9 5 07FDEA03181 1 20070828 A 5313 A53811306202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION AT STRG 46 AND 50, BETWEEN FRAME 39-42 LT. REMAINING THICKNESS OUT OF LIMIT. STRINGER REPAIR PERFORMED WITH PRINCIPLE DESCRIBED IN SRM 53-10-14/FIG 201A, APPROVED BY EA 6-5315-103260 AND RAS/046453/012/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007090500019 20070905 00019 EU 2007 9 5 07FDEA03182 1 20070828 A 5313 A53811362200 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION AT STRG 48, BETWEEN FRAME 39-42 LT. REMAINING THICKNESS OUT OF LIMIT. STRINGER REPAIR PERFORMED WITH PRINC IPLE DESCRIBED IN SRM 53-10-14/FIG 201A, APPROVED BY EA 6-5315-103260 AND RAS/046453/012/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007090500020 20070905 00020 EU 2007 9 5 07FDEA03183 1 20070828 A 5313 A53811368202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION AT STRG 49, BETWEEN FRAME 39-44 LT. REMAINING THICKNESS OUT OF LIMIT. STRINGER REPAIR PERFORMED WITH PRINC IPLE DESCRIBED IN SRM 53-10-14/FIG 201A, APPROVED BY EA 6-5315-103260 AND RAS/046453/012/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007090500022 20070905 00022 EU 2007 9 5 07FDEA03185 1 20070828 A 5313 A53811371202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION AT STRG 50, BETWEEN FRAME 46-47 LT. REMAINING THICKNESS OUT OF LIMIT. STRINGER REPAIR PERFORMED WITH PRINC IPLE DESCRIBED IN SRM 53-10-14/FIG 201A, APPROVED BY EA 6-5315-103260 AND RAS/046453/012/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007090500025 20070905 00025 EU 2007 9 5 07FDEA03188 1 20070828 A 5313 A53811376200 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORROSION AT STRG 46, BETWEEN FRAME 39-42 RT. REMAINING THICKNESS OUT OF LIMIT. STRINGER REPAIR PERFORMED WITH PRINC IPLE DESCRIBED IN SRM 53-10-14/FIG 201A, APPROVED BY EA 6-5315-103260 AND RAS/046453/012/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007090500026 20070905 00026 EA 2007 9 5 TRAX200701235 1 20070823 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 833AS 7246 F/A REPORTED MAIN CABIN DOOR HARD TO CLOSE AND OPEN. 2 L 7 2 4F RT A21EA 2007090500029 20070905 00029 NM 2007 9 5 USAA920070801 1 20070821 A 5320 141N517031 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 942UW 27807 BFM - MAJOR REPAIR - C-04 CHECK - CORROSION FOUND ON LT HAND TUNNEL ABOVE NLG FLOOR SUPPORT WEB, BS 310 - BS 324, LBL 20 . REPLACED LT HAND TUNNEL ABOVE NLG FLOOR SUPPORT WEB, BS 310 - BS 324, LBL 20 IAW 757-200 SRM 51-40-02, SRM 51-42-08, AND SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007090500031 20070905 00031 NM 2007 9 5 USAA920070803 1 20070822 A 5320 141N517030 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 942UW 27807 BFM - MAJOR REPAIR - C-04 CHECK - CORROSION FOUND ON FLOOR SUPPORT WEB, BS 324 - BS 345, LBL 20. REPLACED FLOOR SUPPORT WEB, BS 324 - BS 345, LBL 20 IAW 757-200 SRM 51-40-02, SDR 51-42-02. 2 L 7 2 4F RT A2NM 2007090500033 20070905 00033 EA 2007 9 5 COMA0760528 1 20070815 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION CL CLIMB 1 SO 01 957CA 7109 FLIGHT 4946 - RECEIVED FLAP FAIL MESSAGE DURING RETRACTION AFTER TAKEOFF. DECLARED EMERGENCY UPON LANDING AT CVG. LAND ED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1 , 2, 3 (A,B,C) FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2007090500034 20070905 00034 EU 2007 9 5 07FDEA03195 1 20070828 A 5311 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 FOUND 3 DRILLING MARKS AT FRAME 12 LH OF NLG-WELL. REPAIR PERFORMED BY SMOOTH REWORK OF DRILLING MARKS IAW EA 6-5312-10 1328 AND RAS/046631/007/2006 ISS A. 2 L 7 2 4F RT A35EU 2007090500035 20070905 00035 EU 2007 9 5 07FDEA03198 1 20070828 A 5330 A53974208200 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA K NONE W W W INADEQUATE Q C INADEQUATE Q C INADEQUATE Q C IN INSP/MAINT 1 SO 25 811FD 457 OLD REPAIR DOUBLER FOUND AT FRAME 69-70, STRG 47-48 LHS WITH MISDRILLED LOWER RIVET ROW. DOUBLER REPAIR WAS RENEWED IAW EA 6-5317-103313 ISS "A" AND RAS/DAHAM/4021212/2006 ISS "B". 2 L 7 2 4F RT A35EU 2007090500037 20070905 00037 NE 2007 9 5 COMA0760530 2 20070815 A 7261 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE RT ENGINE OVERSERVICED A COMA A UNSCHED LANDING M W OVER TEMP INADEQUATE Q C CR CRUISE 1 SO 01 779CA 7309 FLIGHT 5158 - DURING CLIMB NOTED HIGH OIL TEMP ON RIGHT ENGINE. DIVERTED TO JFK. DECLARED EMERGENCY, LANDED WITHOUT IN CIDENT. FOUND ENGINE OIL OVERSERVICED. DRAINED EXCESS OIL. RAN ENGINE, NO FURTHER DEFECTS. 2 L 7 2 4F 4 F RT A21EA E15NE 2007090500038 20070905 00038 NM 2007 9 5 MWEA070188 1 20070826 A 7830 7150923REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 925ME 55191 LEFT THRUST REVERSER UPPER OUTBOARD AT STATION 26 FRAME IS CRACKED. FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F TR A6WE 2007090500039 20070905 00039 NM 2007 9 5 MWEA070189 1 20070826 A 7830 7150923REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 925ME 55191 LEFT THURST REVERSER OUTBOARD AT STATION 26, FRAME IS CRACKED. FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F TR A6WE 2007090500040 20070905 00040 NM 2007 9 5 MWEA070190 1 20070827 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 925ME 55191 LEFT THURST REVERSER BOTTOM BUCKET, INBOARD AT STATION 25, FRAME IS CRACKED. FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F TR A6WE 2007090500041 20070905 00041 NM 2007 9 5 MWEA070191 1 20070827 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 925ME 55191 LEFT THRUST REVERSER TOP BRACKET OUTBAORD AT STATION 25, FRAME IS CRACKED. FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F TR A6WE 2007090500042 20070905 00042 EA 2007 9 5 COMA0760531 1 20070816 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA LANDING GEAR FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 710CA 3628 7241 FLIGHT 5376 - NOSE GEAR WOULD NOT EXTEND. CYCLED GEAR, ON SECOND ATTEMPT GEAR EXTENDED NORMALLY. LANDED WITHOUT INCIDE NT. REPLACED MAIN AND NOSE LANDEING GEAR PRIORITY VALVES. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007090500043 20070905 00043 NM 2007 9 5 CALA0700458 1 20070826 A 5347 151W62031 SEAT TRACK BOEING 777 777224 1385225 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 79011 29859 INSPECTION FOUND SEAT TRACK CORRODED AT STA 1504-1545, RBL 74. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52, FIGURE 202 , REPAIR 3. 2 L 7 2 4F RT T00001SE 2007090500044 20070905 00044 NM 2007 9 5 CALA0700459 1 20070827 A 5310 65C352436 DOOR FRAME BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33608 27321 INSPECTION FOUND C-2 DOOR CUTOUT CORRODED AT LOWER AFT CORNER ON BELTFRAME AT STA 847, S25R TO S26R. THE FRAME WAS REPL ACED IAW ECRA 5310-04652. 2 L 7 2 4F RT A16WE 2007090500045 20070905 00045 NM 2007 9 5 CALA0700460 1 20070828 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17328 23458 INSPECTION FOUND MAIN CABIN SEAT TRACK CORRODED AT STA 480-540, RBL 25. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-40-00. 2 L 7 2 4F RT A16WE 2007090500046 20070905 00046 NM 2007 9 5 CALA0700461 1 20070828 A 5313 BAC1498157 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND STRINGER 26R CORRODED AT STA 986.5. A STRINGER SPLICE WAS INSTALLED IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 2007090500054 20070905 00054 NM 2007 9 5 QXEA200701357 1 20070828 A 2997 CONTACT BOMBDR DHC8 DHC8402 1390042 NM RELAY DIRTY A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 426QX 4154 BTM - ON FLIGHT 2381, RETURNED TO GATE, WHEN TAXING OUT THE NR 3 HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED. MAINTENANCE CLEANED PL-4 RELAY CONTACTS AFTER REMOVING. REINSTALLED RELAY, COMPLIED WITH PRESSURIZATION CHECK OF THE NR 3 HYDRAULIC SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007090500056 20070905 00056 NM 2007 9 5 NWAA072926624 1 20070828 A 3350 POWERPACK BOEING 747 747251B 1384892 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 624US 21706 DURING OVERNIGHT CHECK, "A" ZONE EMERGENCY PATH LIGHTS DO NOT ILLUMINATE AT TEST. MAINTENANCE REMOVED AND REPLACED POWE R PACK. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F A20WE 2007090500057 20070905 00057 EU 2007 9 5 F3LA200700203 1 20070827 A 5315 D5347219220000 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON UPPER SURFACE OF LT FLOORBEAM Y765 AT FR68. FLOORBEAM FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14, PG 106. REMOVED AND REPLACED FLOORBEAM AT FRAME 68-70 IAW A318 SRM 53-00-14, SRM 5 1-42-11, DRAWING D53472815 AND DRAWING D53472780. 2 L 7 2 4F RT A28NM 2007090500059 20070905 00059 EU 2007 9 5 F3LA200700204 1 20070827 A 5320 PROFILE AIRBUS A319 A319112 3930323 EU CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION AROUND FWD CARGO COMPARTMENT AFT FLOOR PROFILE FASTENER HOLES. REMOVE D AND REPLACED PROFILE IAW A319 SRM 51-42-11 AND 53-21-14. 2 L 7 2 4F RT A28NM 2007090500061 20070905 00061 EU 2007 9 5 F3LA200700205 1 20070827 A 5320 D5311282720200 DUMMY RAIL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED CABIN FLOOR LT DUMMY RAIL AT FR12 TO FR16 CORRODED. REMOVED AND REPLACED DUMMY RAIL IAW A319 SRM 51-42-11. 2 L 7 2 4F RT A28NM 2007090500066 20070905 00066 WP 2007 9 5 DHL2007804511 1 20070803 A 5310 STRUCTURE DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A DHLA K NONE W W W INADEQUATE Q C INADEQUATE Q C INADEQUATE Q C IN INSP/MAINT 1 SO 01 804DH 85412 46124 PERFORMED DETAILED VISUAL INSPECTION AND FOUND PREVIOUS REPAIR NOT IN ACCORDANCE WITH SRM. PERFORMED MAJOR REPAIR IAW S RM 53-2-1 FIG 7 SHEET 1, 3. REMOVED NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FAB RICATED REPAIR DOUBLER (AL7075T6 0.071") (2EA) INTERNAL FINGER DOUBLER (AL7075T6 0.040") IAW SRM 53-2-1 FIG 7 SHEET 1, 3 , SRM 53-4-1 FIG 5C ITEM "B". CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PART S IAW SRM 53-2-1 FIG 7 SHEET 1, 3, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE). THIS IS A CLASS 1 TYPE REPAIR: INITI AL 4.000, REPETITIVE 4.000, REPLACEMENT N/A IAW SRM 53-2-1 FIG 5, TR NR 53-190 DATED 9-20-03. REINSPECT DUE AT 34.822 C 2 L 7 4 4F RT 4A25 2007090500067 20070905 00067 EU 2007 9 5 07FDEA03166 1 20070828 A 5330 A52410178202 DOUBLER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CORRODED INTERNAL DOUBLER AT GROUND CONNECTING DOOR 121DL, FRAME 18-19, STRG 54 LH - 54 RH. REPAIR PERFORMED BY FABRICA TING AND INSTALLATION OF NEW DOUBLER ACCORDING TO DRW A524-10178. 2 L 7 2 4F RT A35EU 2007090500071 20070905 00071 EU 2007 9 5 07FDEA03203 1 20070829 A 5312 PRESSURE PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 A CRACK WAS FOUND AT NLG ROOF PANEL AT STIFFENER C-5 IN AREA OF FRAME 14. REPAIR PERFORMED BY BLENDING OUT THE CRACKED STIFFENER AND INSTALLING REINFORCED ANGLES AND SHIMS IAW EA 6-5312-103289 AND RAS/AS/139/2006 ISS A. 2 L 7 2 4F RT A35EU 2007090500072 20070905 00072 NM 2007 9 5 SWAA074223 1 20070827 A 3230 65448106 UPLOCK ACTUATOR BOEING 737 7373H4 1384600 NM LT MLG FAULTY A SWAA K NONE J WARNING INDICATION CL CLIMB 1 SW 29 326SW 23690 CLIMBING OUT OF GEG LEFT MLG RED LIGHT STAYED ILLUMINATED. CYCLED GEAR, LIGHT WENT OUT. REMOVED AND REPLACED LEFT MLG UPLOCK ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2007090500073 20070905 00073 EU 2007 9 5 07FDEA03204 1 20070829 A 5330 A53980664 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA K NONE W W W INADEQUATE Q C INADEQUATE Q C INADEQUATE Q C IN INSP/MAINT 1 SO 25 811FD 457 FOUND OLD REPAIR DOUBLER AT FRAME 74-75, STRG 38-39 LT. THE REPAIR DOES NOT CONFORM TO SRM 53-10-12/FIG 205, AS IT ENDS ON THE STRINGER. DOUBLER REPAIR RENEWED IAW SRM 53-10-12/FIG 225 APPROVED BY EA 6-5318-103343. 2 L 7 2 4F RT A35EU 2007090500074 20070905 00074 NM 2007 9 5 SWAA074221 1 20070827 A 5330 6545768 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 374, STR 26R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007090500075 20070905 00075 EU 2007 9 5 07FDEA03205 1 20070829 A 5750 A57710096002 SKIN AIRBUS 300 A300B4622R 3930312 EU SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 FOUND TWO DELAMINATED AREAS ON BOTTOM SKIN TRAILING EDGE OF LT SPOILER NR 1. DELAMINATION REPAIRS PERFORMED IAW SRM 57- 71-11/PG 201/PARA 10, APPROVED BY EA 6-5770-101551. 2 L 7 2 4F RT A35EU 2007090500076 20070905 00076 EU 2007 9 5 07FDEA03206 1 20070829 A 5714 A55171914202 SKIN AIRBUS 300 A300B4605R 3930308 EU ZONE 300 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 FOUND DEEP CHAFING MARKS IN LOWER SKIN OF TRIM TANK CENTER BOX UNDER THE WATER DRAIN INTAKE, INSIDE THE CENTER BOX. R EPAIR PERFORMED BY BLEND OUT IAW EA 6-5511-112507 AND RAS/CASA/5733/2007 ISS "A". 2 L 7 2 4F RT A35EU 2007090500077 20070905 00077 EU 2007 9 5 07FDEA03207 1 20070829 A 5313 A53974267202 STRINGER AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 FOUND CORROSION ON STRG. 56 LT, FRAME 57.3-61. REPAIR PERFORMED BY REMOVAL OF CORROSION AND ROTO TEST IAW EA 6-5317-112 511 AND RAS/DATLS/003803/2007 ISS "A". 2 L 7 2 4F RT A35EU 2007090500081 20070905 00081 NM 2007 9 5 SWAA074217 1 20070827 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007090500082 20070905 00082 NM 2007 9 5 SWAA074222 1 20070827 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 289, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007090500083 20070905 00083 NM 2007 9 5 SWAA074231 1 20070827 A 5311 6546526 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007090500084 20070905 00084 NM 2007 9 5 SWAA074232 1 20070827 A 5311 6546548 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007090500085 20070905 00085 NM 2007 9 5 SWAA074228 1 20070827 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007090500086 20070905 00086 NM 2007 9 5 SWAA074233 1 20070827 A 5311 6546550 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007090500087 20070905 00087 NM 2007 9 5 SWAA074229 1 20070827 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007090500088 20070905 00088 NM 2007 9 5 SWAA074227 1 20070827 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007090500089 20070905 00089 NM 2007 9 5 SWAA074225 1 20070827 A 5311 65C2529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007090500090 20070905 00090 NM 2007 9 5 SWAA074224 1 20070827 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007090500091 20070905 00091 NM 2007 9 5 SWAA074235 1 20070827 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007090500092 20070905 00092 2007 9 5 SWAA074230 4 20070827 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM L1 DOOR UNWANTED DEPLOY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007090500093 20070905 00093 2007 9 5 SA07053 4 20070827 A 2565 D30665109 SLIDE AIRBUS 320 A320214 3930316 EU L2 DOOR LEAKING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 110UW 8752 279 1112 TPA - THE L2 DOOR SLIDE PRESSURE WAS FOUND OUT OF GREEN BAND. MAINTENANCE REPLACED THE L2 DOOR ESCAPE SLIDE ASSEMBLY. INSPECTED OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2007090500101 20070905 00101 WP 2007 9 5 07FDEA03212 1 20070829 A 5230 ADA37741 SKIN DOUG DC10 DC1010 3022110 WP ZONE 800 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 CTR LWR CARGO DOOR, LWR FWD CORNER OF SKIN DEFORMED. REPAIRED AREA IAW SRM 52-10-00 FIG 17 VOL 1. 2 L 7 3 4F A22WE 2007090500103 20070905 00103 WP 2007 9 5 07FDEA03215 1 20070829 A 5312 BULKHEAD DOUG DC10 DC1010F 3022111 WP ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 CTR W/W SPACE CRACK ON VERTICAL BULKHEAD. PERFORMED REPAIR IAW SRM 53-00-01 VOL I FIG 4. 2 L 7 3 4F A22WE 2007090500104 20070905 00104 WP 2007 9 5 07FDEA03216 1 20070829 A 5312 BULKHEAD DOUG DC10 DC1010F 3022111 WP ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 RT W/W CRACK 0.5" LONG ON VERTICAL BULKHEAD. REPAIRED BULKHEAD IAW SRM 53-00-01 VOL I FIG 10. 2 L 7 3 4F A22WE 2007090500110 20070905 00110 NM 2007 9 5 QXEA200701358 1 20070828 A 3620 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM NR 2 BLEED FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING AP APPROACH 1 NM 09 407QX 4049 BOI FLIGHT NR 2326: ON APPROACH, RECEIVED THE NR 2 BLEED HOT CAUTION LIGHT. C/W THE CHECKLIST AND THE CAUTION LIGHT WEN T OUT WHEN THE NR 2 BLEED WAS SWITCHED OFF. MAINTENANCE C/W FIM PROCEDURE 36-20-00-810-802. FOUND CDS RELATED MESSAGE "R ANA WING LEAK". ERASED THE DATA FROM THE CDS AND C/W OPS CHECK OF THE BLEED AIR SYSTEM IAW FIM. NO NR 2 BLEED HOT C AUTION LIGHT ILLUMINATED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007090500111 20070905 00111 NM 2007 9 5 QXEA200701359 1 20070828 A 3060 DEICE SYSTEM BOMBDR DHC8 DHC8402 1390042 NM PROPELLER MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 401QX 4031 BOI FLIGHT NR 2406: AFTER START-UP, PROP DEICE LIGHT REMAINED ON (PROP DEICE SYSTEM INOP). MAINTENANCE FOUND NO FAULTS UPON INTERROGATION OF EMU, NO RECENT HISTORY OF PROP DEICE CAUTION. PERFORMED FUNCTIONAL TEST OF PROP DEICING SYSTEM PE R Q400 AMM TASK 30-61-11-720-801. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007090500113 20070905 00113 NM 2007 9 5 QXEA200701361 1 20070829 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM AFT PAX STUCK A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 417QX 4086 SEA FLIGHT NR 2393: FA WAS UNABLE TO OPEN REAR PAX DOOR. MAINTENANCE DISLODGED DOOR. CHECKED FOR DAMAGE WITH NO DAMAGE NOTED. CYCLED DOOR SEVERAL TIMES WITH NO DEFECTS NOTED. RESET DOOR PER SERVICE LETTER DH8-400-SL-52-003A. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007090500117 20070905 00117 EU 2007 9 5 F3LA200700207 1 20070830 A 5311 D5347112320300 FRAME AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED RT SUPPORT FRAME BETWEEN FR69 AND FR70 CORRODED. REMOVED AND REPLACED SUPPORT F RAME IAW A319 SRM 51-42-11. 2 L 7 2 4F RT A28NM 2007090500118 20070905 00118 EU 2007 9 5 F3LA200700208 1 20070830 A 5340 D5323131920000 BRACKET AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED FWD CARGO DOOR BOTTOM FRAME ALONG STR 38, JUST FWD OF FR26 FITTING BETWEEN 2ND A ND 3RD LOCKING ROLLERS, CORRODED AT OTBD DOME NUT HOLE. REMOVED AND REPLACED FITTING AT FWD CARGO DOOR BOTTOM FRAME 26, STR 38, IAW A319 SRM 51-42-11 AND 51-72-11. 2 L 7 2 4F RT A28NM 2007090500121 20070905 00121 WP 2007 9 5 AALA20071514 1 20070812 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 582AA 53159 DFW - EMERGENCY LIGHT AT SEAT ROW 28D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 28D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007090500123 20070905 00123 NM 2007 9 5 AALA20071488 1 20070810 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 777AN 29585 DFW - EMERGENCY LIGHT AT SEAT ROW 22C IS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 22C. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007090500127 20070905 00127 WP 2007 9 5 AALA20071496 1 20070811 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7538A 49992 DFW - EMERGENCY LIGHTS AT FORWARD CABIN CEILING FLIGHT DECK, FORWARD ENTRY AND GALLEY INOPERATIVE. REPLACED BATTERY PAC K B5 23 FOR EMERGENCY LIGHTS AT FORWARD CABIN CEILING FLIGHT DECK, FORWARD ENTRY AND GALLEY. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F A6WE 2007090500131 20070905 00131 NM 2007 9 5 AWXA200701031 1 20070816 A 5313 6545800771 STRINGER BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5988018, CRACK FOUND ON FUSELAGE STRING S-10R, BS 277. REPAIRED FUSELAGE STRINGER S-10R, BS 277 IAW B737-300 SRM 53-00-03-2 R3 FIG 201. 2 L 7 2 4F RT A16WE 2007090500132 20070905 00132 EU 2007 9 5 AWXA200701032 1 20070823 A 5315 D53472197200 FLOORBEAM AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980114, CORROSION ON CABIN FLOORBEAM, BS 3257/FR68 - BS 3366/FR 70, -Y765. REPLA CED CABIN FLOORBEAM, BS 3257/FR68 - BS 3366/FR 70, -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007090500133 20070905 00133 EU 2007 9 5 AWXA200701033 1 20070823 A 5320 D534722840008 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980119, CORROSION ON CABIN FLOORBEAM, BS 3043/FR64 - BS 3207/FR 67, -Y470. REPLAC ED CABIN FLOORBEAM, BS 3043/FR64 - BS 3207 / FR 67, -Y470 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007090500137 20070905 00137 EU 2007 9 5 AWXA200701037 1 20070823 A 5322 D53471124201 SHEAR PLATE AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980150, CORROSION ON RIGHT SIDE CABIN SHEAR PLATE, BS 3310/FR69 - BS 3366/FR 70. REPLACED RIGHT SIDE CABIN SHEAR PLATE, BS 3310/FR69 - BS 3366/FR 70 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007090500138 20070905 00138 EU 2007 9 5 AWXA200701038 1 20070825 A 5347 D5342815200 SEAT TRACK AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980105, CORROSION ON CABIN SEAT TRACK, BS 605/FR 12 - BS 950/FR 24, +Y765. REPLAC ED CABIN SEAT TRACK, BS 605/FR 12 - BS 950/FR 24, +Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007090500139 20070905 00139 EU 2007 9 5 AWXA200701039 1 20070825 A 5320 D53472189202 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980116, CORROSION ON CABIN FLOORBEAM, BS 3257/FR 68- BS 3366/FR 70, -Y1292. REPL ACED CABIN FLOORBEAM, BS 3257/FR 68 - BS 3366/FR 70, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007090500140 20070905 00140 EU 2007 9 5 AWXA200701040 1 20070825 A 5320 D53472172201 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980118, CORROSION ON CABIN FLOORBEAM, BS 3158/FR 66- BS 3207/FR 67, -Y1292. REPL ACED CABIN FLOORBEAM, BS 3158/FR 66 - BS 3207/FR 67, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007090500144 20070905 00144 EU 2007 9 5 AWXA200701044 1 20070827 A 5320 D53472190205 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980132, CORROSION ON CABIN FLOORBEAM, BS 3043/FR 64 - BS 3158/FR 66, -Y1292. REP LACED CABIN FLOORBEAM, BS 3043/FR 64 - BS 3158/FR 66, -Y1292 IAW A320 SRM 51-72-11 AND 51-42-11. 2 L 7 2 4F RT A28NM 2007090500148 20070905 00148 NM 2007 9 5 NWAA072946719 1 20070830 A 3350 BATTERY PACK BOEING 747 747251F 1384898 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING OVERNIGHT CHECK, FOUND UPPER DECK DOOR THRESHOLD EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F A20WE 2007090500149 20070905 00149 NM 2007 9 5 NWAA072955520 1 20070830 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 520US 23208 DURING OVERNIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS IN FIRST CLASS INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007090500150 20070905 00150 EA 2007 9 5 QXEA200701356 1 20070824 A 3610 GG670950283 SHUTOFF VALVE CNDAIR CL600 CL6002C10 1390015 EA ENGINE BLEED FAILED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 601QX 15094 10009 DEN - FLIGHT 4330, RECEIVED A RIGHT ENGINE BLEED CAUTION MESSAGE. MAINTENANCE REPLACED THE HIGH PRESSURE SHUTOFF VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007090500155 20070905 00155 EU 2007 9 5 DHL2007367504 1 20070807 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH 265 PASSENGER SEAT ATTACHMENT FITTING AT FR 54.2 BEAM NR RH-4 NUMBER 16 MEASURED .084 IS OUT OF LIMITS. REMOVED SEAT TRACK ATTACH FLOOR SUPPORT AT MAIN CABIN FR 54.2 LBR 19 IAW A300 SB 94FS494-53-12 AND SRM 51-30-00. MEASURED SEAT TRACK ATTAC H FITTING .034 FOUND OUT OF LIMITS IAW SB 94FS494-52-12. INSTALLED SEAT TRACK ATTACHMENT FITTING AT FR 54.2 RT NR 16 IA W A300 SRM 51-30-00 AN A300 SB 94FS494-53-12. 2 L 7 2 4F RT A35EU 2007090500157 20070905 00157 NM 2007 9 5 WRLA2007089 1 20070823 A 5713 ARB293311 DOUBLER DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE RT WING CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 275WA 48631 DURING 3C+12A CHECK, EGAT MECHANIC FOUND CRACK ON RIGHT HAND WING FIXED LOWER LEADING EDGE STRINGER DOUBLER AT STA XOS 9 06. 09-26-07 REPAIRED PER MD-11 SRM 57-10-00 FIG.18 VOL.1 REV.40. 2 L 7 3 4F 4 F RT A22WE E24NE 2007090500158 20070905 00158 NM 2007 9 5 WRLA2007087 1 20070823 A 5753 ARC2443501 SKIN DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE T/E FLAP DAMAGED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 275WA 48631 DURING 3C+12A, EGAT MECHANIC FOUND CRACK ON INBOARD FLAP SKIN AT STA XIFH 198, YIFH 40 ON LEFT HAND WING. 09-26-07 P ERFORM NDT/ET FOR CUTOUT AREA REF JC31896, NO CRACK FOUND. REPAIR CRACK AREA PER MD11 SRM VOL.157-10-00 REV.40 2 L 7 3 4F 4 F RT A22WE E24NE 2007090500159 20070905 00159 NM 2007 9 5 USAA070674 1 20070828 A 5320 651768455 WEB BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 STA 294.5, S7L HAS CRACK. FABRICATED NEW WEB AND INSTALLED PER BOEING DWG 65-17684, DEFECT SIZE: .350 INCH. 2 L 7 2 4F RT A16WE 2007090500160 20070905 00160 NM 2007 9 5 USAA070675 1 20070828 A 5310 DOOR FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 BS 492.4 STR 24R FWD CARGO DOOR FRAME HAS CRACK. DEFECTIVE PART REPLACED WITH IDENTICAL PART; INSTALLED NEW FRAME PER S RM 5-40-00, 53-00-53, DEFECT SIZE: .75 INCH. 2 L 7 2 4F RT A16WE 2007090500161 20070905 00161 NM 2007 9 5 USAA070676 1 20070828 A 5320 654580733 STIFFENER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 STA 294 BETWEEN STR S10R & S11R, ANGLE STIFFENER HAS CRACK. REMOVED & REPLACED ANGLE STIFFENER WITH NEW PART PER SRM 51 -10-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007090500162 20070905 00162 NM 2007 9 5 DHL2007746521 1 20070818 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 740 S26L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 WHILE AT FLIGHTSTAR FOR A "C" CHECK, FWD CARGO COMPT STR 26L IS CORRODED AT STA 740. CUT OUT DAMAGE SECTION OF STR 26LT AT STA 740 IAW B727 SRM 53-10-03, 5" LONG FAB AND INSTALLED STRINGER REPAIR IAW B727 SRM 53-10-03 FIG 1, MAT USED STRIN GER BAC1498-147 7075-T6 5" LONG SPLICE BAC 1498-131 9.5/8" LONG PO NR 724567 & 723214. TREATED AND PRIMED PARTS AND ARE A IAW B727 SRM 51-10-02. 2 L 7 3 4F A3WE 2007090500163 20070905 00163 NM 2007 9 5 USAA070666 1 20070828 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 BS 727D AT S23L HAS CRACK. REMOVED DAMAGE, INSTALLED DOUBLER PER TR 53-60-03A, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007090500165 20070905 00165 EU 2007 9 5 DHL2007367503 1 20070812 A 5340 FITTING AIRBUS 300 A300B4203 3930306 EU EMERGENCY EXIT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH 265 CRACK IN AFT LWR CORNER FITTING OF THE LT EMERGENCY EXIT DOOR CUTOUT. REMOVED FLOOR PANEL FOR ACC. REMOVED CRACKED FIT TING AT AFT LWR CORNER OF THE LT EMERG EXIT DOOR CUT OUT AREA AS PER A300 SRM 51-30-29. INSTALLED NEW FITTING IN AREA A S PER A300 SRM 53-16-00 AN 51-30-29. INSTALLED FLOOR PANEL AS PER A300 SRM 51-30-29. 2 L 7 2 4F RT A35EU 2007090500166 20070905 00166 NM 2007 9 5 DHL2007746508 1 20070809 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 685 S27L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 DURING A "C" CHECK AT FLIGHTSTAR, THE FOLLOWING DISCREPANCIES WERE NOTED; REF NR 099303, FWD CARGO COMPT STA 685 STR. S PLICE HAS CORROSION IN CENTER OF SPLICE STR 27L. ALSO CRACK INDICATION. REMOVED STRINGER SPLICE AT STR 27L STA 680 IAW B727 SRM 51-30-2 FIG 1. FAB NEW SPLICE FROM BAC1498-131,7075 T6 PO NR 7232174 DIM 12" IAW B727 SRM 53-10-3 FIG 1 AND 5 3-10-2 FIG 9. TREATED AND PRIMED IAW B727 SRM 51-10-2, STRINGER SPLICE INSTALLED AT STR.27L STA 680 IAW B727 SRM 53-10- 3 FIG 1. 2 L 7 3 4F A3WE 2007090500167 20070905 00167 EU 2007 9 5 07FDEA03233 1 20070829 A 5347 A5361164020000 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 683FE 801 MDCC SEAT TRACK 3 RT FR15B-FR19 5 SQ IN CORROSION REF A300-600 AMM 53-10-16-6-02 ZONE 220. REMOVED CORROSION ON SEAT TR ACK IAW A300 SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW A300 SRM 53-10-16 FIG 102. REMOVED AND REPLACED SEAT TRACK IA W A300 SRM 53-40-21. 2 L 7 2 4F RT A35EU 2007090500168 20070905 00168 NM 2007 9 5 USAA070678 1 20070828 A 5730 SKIN BOEING 737 7373B7 1384580 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 LEFT WING FIXED LEADING EDGE LOWER SKIN PANEL AT SLAT STA 3.25 HAS CRACK. REMOVED DAMAGE, FAB'D & INSTALLED REPAIR PART S PER BOEING TR 57-41-02, DEFECT SIZE: .75 INCH. 2 L 7 2 4F RT A16WE 2007090500171 20070905 00171 NM 2007 9 5 DHL2007746516 1 20070809 A 5311 FRAME BOEING 727 727224 1384076 NM BS 500 S17R DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 WHILE AT FLIGHTSTAR FOR A "C" CHECK, DENT ON FUSELAGE FRAME BS 500 ABOVE STR 17R. CUT OUT DAMAGE AREA DIM 1" BY 1" IAW B727 SRM 51-40-03 FIG 1, FAB DOUBLER ANGLE. REPAIR FROM 7075-T6 .050 PO NR 9003230 DIM 9" BY 4" IAW B727 SRM 51-40-03 F IG 1. LOCATED DRILL IAW B727 SRM 51-30-05. TREATED AND PRIMED IAW B727 SRM 51-10-02. INSTALLED DOUBLER ANGLE REPAIR I AW B727 51-30-02 AND 51-40-03. 2 L 7 3 4F A3WE 2007090500173 20070905 00173 NM 2007 9 5 DHL2007746510 1 20070803 A 5410 COWLING BOEING 727 727224 1384076 NM NR 1 NACELLE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 DURING AN "C" CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED, REF NR 098958 NR 1 ENG NOSE COWL EXTERIOR SKIN AT 9 O'CLOCK POSITION HAS 3 INCH CRACK FROM RIVET HEAD FWD. CUT OUT DAMAGED AREA ON NR 1 ENG NOSE COWL EXTERIOR SKIN 9 O`CLOCK POSI TION 3" BY 2" IAW B727 SRM 54-30-3 FIG 3A. FABRICATED AND INSTALLED DOUBLER REPAIR IAW B727 SRM 54-30-3 FIG A MAT`L USE D DOUBLER .050 2024 T3 PO NR 9005554 6.5" BY 6.75", SPACER PLATE (SHIM) .063 2024 T3 PO NR 9005138 6.5" BY 6.75", FILLER .040 2024 T3 PO NR 9005098 2" BY 3", ALL PARTS ALODINED AND PRIMED IAW B727 SRM 51-10-2. 2 L 7 3 4F A3WE 2007090500175 20070905 00175 WP 2007 9 5 DHL2007804514 1 20070712 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 MAIN CARGO COMPT FLOOR PANEL NR 8 UPPER SKIN CORRODED (STA 8.000 - 70.000). REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FLOOR PANEL SKIN IAW SRM 51-1-21. FABRICATED NEW FLOOR PAN EL SKIN (AL7075T6 0.090") AND CHANNEL (EXTRUSION S1059661) IAW SRM 57-7-3 PG 2A/2B. CLEANED, TREATED AND PRIMED AREA AN D REPAIR PARTS IAW SRM 51-1-8B. INSTALLED CHANNEL AND FLOOR PANEL SKIN IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007090500176 20070905 00176 NM 2007 9 5 USAA070691 1 20070828 A 5414 PANEL BOEING 737 7373B7 1384580 NM NR 2 PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 532AU 24479 TOP OF PYLON 2 PANEL 5727L OPENING HAS CRACK. INSTALLED DOUBLER PER TR 54-30-07, DEFECT SIZE: .5. 2 L 7 2 4F RT A16WE 2007090500177 20070905 00177 WP 2007 9 5 DHL2007804515 1 20070714 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSLEAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 MAIN CARGO COMPT FLOOR PANEL SUPPORT ANGLE CORRODED, STA 25.000 RBL 26 TO 42. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18 . FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT CORRODED ANGLE SEGMENT IAW SRM 53-2-0 PG 1. FABRICATED REINFORCIN G ANGLE (AL7075T6 0.063") AND FILLER (AL7075T6 0.050") IAW SRM 53-2-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 51-1-21, SRM 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007090500178 20070905 00178 NM 2007 9 5 USAA070680 1 20070828 A 5347 SEAT TRACK BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 STA 727B RBL 24.75 HAS CRACK. INSTALLED FABRICATED REPAIR PARTS PER EA 98824, DEFECT SIZE: 3 INCH. 2 L 7 2 4F RT A16WE 2007090500182 20070905 00182 WP 2007 9 5 DHL2007804519 1 20070807 A 5730 56110111 PANEL DOUG DC8 DC873F 302199F WP LT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 LT WING T/E LWR PANEL DELAMINATED (STA XW 0.000 - 90.000). REMOVED AND REPLACED DELAMINATED LT WING T/E LWR PANEL (STA XW 0.000 - 90.000) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007090500184 20070905 00184 WP 2007 9 5 DHL2007804521 1 20070804 A 5330 4646945 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 FWD CARGO COMPT INNER DOUBLER CORRODED STA 70.000 L-36 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW JC EC-00423 (WO 1616) , DWG DOUGLAS NR 4646945. REMOVED CORROSION IAW SRM 51-1-8B PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOV ED CORRODED DOUBLER IAW SRM 53-1-0 PG 1, SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED DOUB LER IAW SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D, SRM 51-3-1 (TORQUE). REFER TO JC EC-00423-001 (WO NR 1616) FOR DOUBLER F ABRICATION. 2 L 7 4 4F RT 4A25 2007090500186 20070905 00186 WP 2007 9 5 DHL2007804523 1 20070806 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 RT OUTER WING INBD L/E HOLES ELONGATED STA XW 485.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 08-02-07, EVA D 857-0009 REV IR DATED 06-13-07, DWG AD79-57-102 REV IR DATED 07-13-07. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0, S RM 51-1-20D. CUT OUT DAMAGED SECTION IAW DWG NR AD79-57-102 REV IR. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 08-00 -02 TO 07. NO CRACK NOR CORROSION FOUND. ENCLOSED SMN FORM 242-4. FABRICATED REPAIR DOUBLER (AL7075T6 0.063") AND FIL LER (AL7075T6 0.050") IAW DWG AD79-57-102 REV IR. CLEANED, TREATED AND PRIMED AREA, FILLER AND INNER FACE OF REPAIR DOU BLER IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DWG AD79-57-102 REV IR, SRM 51-1-11, SRM 51-1-21, SRM 51-3-0, SRM 51-1 2 L 7 4 4F RT 4A25 2007090500188 20070905 00188 WP 2007 9 5 DHL2007804524 1 20070806 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 LWR FUSELAGE EXTERNAL SKIN HAS TWO CRACKS OF 0.250" AND 0.500", STA 60.000 L-35.8R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 08-02-07, EVA D853-00011 REV IR DATED 03-18-07, DWG AD79-53-103 REV IR DATED 07-19-07. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION IAW DWG AD79-53-103 REV IR. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 08- 00-02 TO 07. NO CRACK NOR CORROSION FOUND AFTER CUT OUT. ENCLOSED SMN FORM 242-4. FABRICATED REPAIR DOUBLER (AL7075T6 0.063") FILLER (AL7075T6 0.050") AND INTERNAL FINGER DOUBLER (AL7075T6 0.032") IAW DWG AD79-53-103 REV IR. CLEANED, TR EATED AND PRIMED AREA, FILLER, FINGER DOUBLER AND INNER FACE OF REPAIR DOUBLER IAW SRM 51-1-8B. INSTALLED REPAIR PARTS 2 L 7 4 4F RT 4A25 2007090500190 20070905 00190 EU 2007 9 5 07FDEA03220 1 20070829 A 5310 STRUCTURE AIRBUS 310 A310203 3930313 EU CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT PIT BETWEEN FRAMES 66 AND 65 T CAP NUT PLATE JUST FWD OF FRAME 66 ABOVE STRINGER 45R CORRODED UNDERNEATH. REMOVED T -CAP IAW A310 SRM 51-40-21, RECEIVED NEW PROFILE P/N A5397426020451 PO J80248.1. INSTALLED NEW PROFILE IAW A310 SRM 51- 40-21 PARA 7 AND PARA 13. 2 L 7 2 4F RT A35EU 2007090500192 20070905 00192 EU 2007 9 5 07FDEA03223 1 20070829 A 5311 A53970781 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 GOUGES FOUND AT FRAME 55 LHS AND RHS, BETWEEN STRG 14-15. REPAIR PERFORMED BY SMOOTH BLENDING AND NDT INSPECTION IAW EA 6-5316-99140 AND RAS/DATLS/0003069/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007090500193 20070905 00193 EU 2007 9 5 07FDEA03224 1 20070829 A 5313 LONGERON AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 HEAVY CORRODED LONGERON BETWEEN FRAME 11-15A, CABIN FLOOR STRUCTURE. INSTALLATION OF NEW LONGERON IAW SRM 53-12-15 / FI G 207. 2 L 7 2 4F RT A35EU 2007090500194 20070905 00194 EU 2007 9 5 07FDEA03225 1 20070829 A 5510 A55176100265 WEB AIRBUS 300 A300B4622R 3930312 EU ZONE 300 DAMAGED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 725FD 572 FOUND MISMATCHED HOLES IN WEB OF RT HORIZONTAL STABILIZER TIP. REPAIR PERFORMED BY REPLACEMENT OF AFFECTED WEB AND CHAN GING SOLID RIVETS BY HI-LOK FASTENERS AT SOME LOCATIONS IAW EA 6-5514-99141 AND RAS/CASA/4583/2006 ISSUE: A. 2 L 7 2 4F RT A35EU 2007090500197 20070905 00197 NM 2007 9 5 DHL2007746518 1 20070809 A 5311 FRAME BOEING 727 727224 1384076 NM BS 540 S17R DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 WHILE AT FLIGHTSTAR FOR A "C" CHECK, DENT ON FUSELAGE FRAME BS 540 ABOVE STR 17R. CUT OUT DAMAGE AREA DIM 1" BY 1" IAW B727 SRM 51-40-03 FIG 1. FAB DOUBLER ANGLE. REPAIR FROM 7075-T6 .050 PO NR 9003230 DIM 9" BY 4" IAW B727 SRM 51-40-03 FIG 1. LOCATED DRILL IAW B727 SRM 51-30-05. TREATED AND PRIMED IAW B727 SRM 51-10-02. INSTALLED DOUBLER ANGLE REPAIR IAW B727 51-30-02 AND 51-40-03. 2 L 7 3 4F A3WE 2007090500198 20070905 00198 EU 2007 9 5 DHL2007367500 1 20070807 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH 265 PASSENGER SEAT ATTACHMENT FITTING AT FR 54.2 BEAM NUMBER LH4-20 MEASURED .055 OUT OF LIMITS. REMOVED PASSENGER SEAT TRA CK ATTACHMENT FITTING AT FR. 54.2 LH4-20 IAW A300 SB 94FS494-53-12. MEASURED SEAT TRACK ATTACHMENT FITTING .055 FOUND O UT OF LIMITS IAW SB 94FS494-53-12R1. INSTALLED NEW SEAT TRACK ATTACHMENT FITTING AT FRAME 54.2 BEAM LH4-20 IAW A300 SRM 51-30-00 AN A300 SB 94FS494-53-12. 2 L 7 2 4F RT A35EU 2007090500202 20070905 00202 NM 2007 9 5 07FDEA03232 1 20070829 A 5414 311N504632 SKIN BOEING BOEING 757 7572B7 1384964 NM ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 NR 2 STRUT, RIGHT SIDE SKIN AT APPROXIMATE PP STA 182 HAS CORROSION ON SKIN AND UNDER LOWER FRAME. CORROSION WAS REMO VED FROM SKIN, AND FOUND OUT OF LIMITS PER SRM 54-50-01. CONTACTED ENGINEERING AND WAS PRESENTED EA NR F-5450-110764A F OR CORRECTIVE ACTION. FABRICATED FILLER, FABRICATED DOUBLER & INSTALLED REPAIR PARTS IAW EA NR F-5450-110764A. REPAIR IS CLASSIFIED AS A MAJOR REPAIR PER GMM 6-2-100. 2 L 7 2 4F RT A2NM 2007090500222 20070905 00222 NM 2007 9 5 2007UALA03351 1 20070823 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 FWD ENTRY DOOR AFT FRAME STOP SIXTH STOP FITTING CUTOUT HOLE FRAME CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACK. INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090500223 20070905 00223 NM 2007 9 5 2007UALA03352 1 20070823 A 5320 CROSSBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 AFT LAV AREA RIGHT CROSSBEAM CORRODED AT BS 1006 TO BS 1016 BL 4R TO 10R WL 208. MAJOR REPAIR ACCOMPLISHED: REPLACED C ROSSBEAM. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090500224 20070905 00224 NM 2007 9 5 2007UALA03353 1 20070823 A 5230 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 AFT CARGO DOOR FWD LOWER CORNER IS DAMAGED. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW DOUBLER & FILLER AFTER SKIN REPLA CEMENT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090500225 20070905 00225 NM 2007 9 5 2007UALA03354 1 20070823 A 5320 FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 CABIN BODY FRAME INTERCOSTAL CLIP IS CRACKED BS 295 STR 11L. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED NEW ANG LE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090500226 20070905 00226 NM 2007 9 5 2007UALA03355 1 20070823 A 5311 ATTACH ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 PASSENGER CABIN STA 294 STR 12L FRAME ATTACH ANGLE CRACKED ON LOWER SIDE. MAJOR REPAIR ACCOMPLISHED: REMOVED, FABRICAT ED & INSTALLED INTERCOSTAL WEB. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090500227 20070905 00227 NM 2007 9 5 2007UALA03356 1 20070823 A 5320 CROSSBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUESLAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 AFT LAV AREA LEFT CROSSBEAM CORRODED AT BS 1006 TO BS 1016 AT BL 4L TO 10L WL 208. MAJOR REPAIR ACCOMPLISHED: REPLACED CROSSBEAM. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090500228 20070905 00228 NM 2007 9 5 2007UALA03357 1 20070823 A 5320 ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 AFT LAV AREA SMALL WALL ANGLE CORRODED AT BS 1013 TO BS 1016 BL 4L TO 6L AT WL 208. MAJOR REPAIR ACCOMPLISHED: FABRICA TED & INSTALLED AFT LAV WALL ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090500229 20070905 00229 NM 2007 9 5 2007UALA03358 1 20070823 A 5320 ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 ANGLE CRACKED STA 616, CABIN RIGHT SIDE AT SIDE WALL. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF INBOARD CH ORD. FABRICATED & INSTALLED ANGLE REPAIR. REMOVED DAMAGED WEB. FABRCIATED & INSTALLED REPLACEMENT WEB. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090500185 20070905 00185 WP 2007 9 5 DHL2007804522 1 20070806 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT TE FLAP WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 85412 46124 RT OUTBD FLAP UPPER SKIN WORN 1/2", STA XF 226.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 08- 02-07, ASTAR EV D853-00008 REV IR DATED 07-10-07, REV IR, COTNEY DOC EDW27-5, RELEASE DATE 07-21-04 REV IR, DWG NR W27-R 05 IR DATE 07-21-04. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED SPLICE STRAP (AL2024T3 0.080") AND NEW SKIN SEGMENT (AL2024T3 0.071") IAW ED-W27-R05. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 08-00-02 T O 07. NO CRACK NOR CORROSION FOUND. ENCLOSED SMN FORM 242-4. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SR M 51-1-8B. INSTALLED REPAIR PARTS IAW ED-W27-5, DWG NR W27-R05, SRM 51-1-11, SRM 51-1-21, SRM 51-3-0, SRM 51-3-1 (TORQU 2 L 7 4 4F RT 4A25 2007090500191 20070905 00191 EU 2007 9 5 07FDEA03221 1 20070829 A 5754 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 OLD FLUSH DOUBLER REPAIR ON SLAT NR 3 LT, UPPER SKIN, BETWEEN RIB 44-46. BLIND RIVETS WITHOUT PIN, RIB 46 IS MISDRILLED AND RIVETS FORM IS NOT ADHERED. REWORK PER TD FOK/233/2005 ISSUE: C, APPROVED BY EA 6-5744-99139A AND RAS/FOK/2332005 ISSUE: A. 2 L 7 2 4F RT A35EU 2007090500201 20070905 00201 NM 2007 9 5 07FDEA03231 1 20070829 A 5315 6516338283 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT UPPER MAIN DECK, CORROSION ON UPPER SURFACE OF UPPER T- CAP ON FLOOR BEAM, STA 950, LBL 10.5 AND LBL 21". REMOVED C ORROSION FROM SURFACE ON UPPER T-CAP REF SRM 51-10-01. REMOVED SEAT TRACK SRM 51-30-2. REMOVED WEB SUPPORT AND BRACKET AT 950. REMOVED TWO STRAPS BS 950 UNDER T- CAP, LBL 22-63. FAB REPAIR ANGLE, FAB UPPER T-CHORD, HEAT TREATED AND PRIM ED, INSTALLED UPPER T-CHORD, BS 950, RBL 13 TO LBL 62. WORK ACCOMPLISHED ON EA NR 7-5310-113054. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007090500230 20070905 00230 NM 2007 9 5 2007UALA03359 1 20070823 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 CREASE BEAM INNER CHORD AND WEB CRACKED AT BS 616R RBL 64. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF INBOA RD CHORD. FABRICATED & INSTALLED ANGLE REPAIR. REMOVED DAMAGED WEB. FABRICATED & INSTALLED REPLACEMENT WEB. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090500231 20070905 00231 NM 2007 9 5 2007UALA03360 1 20070822 A 5210 DOOR FRAME BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE PAX DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA 25158 NR 1 LEFT MAIN ENTRY DOOR FRAME CRACKED AT GATE HINGE ATTACH HOLES. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR ANGLE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090500232 20070905 00232 2007 9 5 2007UALA03361 4 20070823 A 2565 HARNESS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE FRAYED A UALA O OTHER L NO TEST IN INSP/MAINT 1 WP 29 519UA 24872 R-2 DOOR SLIDE HARNESS WEBBING FRAYED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007090500233 20070905 00233 NM 2007 9 5 2007UALA03362 1 20070823 A 3510 HOSE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT DEFECTIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 596UA 28749 OXYGEN MASK HOSE DEFECTIVE AT 2 (1=CAPT, 2=1ST OF, 3= 1ST OBS). 2 L 7 2 4F 4 F RT A2NM E17NE 2007090500234 20070905 00234 NM 2007 9 5 2007UALA03363 1 20070824 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 214UA 30220 EXTERIOR EMERGENCY LIGHTS AT DOORS 4L AND 4R ARE INOP. RELAMPED LT AND RT EXT EMERGENCY LIGHTS AT DOOR 4 RT AND LT PER MM 33-51-00. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007090500235 20070905 00235 NM 2007 9 5 DHL2007746505 1 20070809 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 680 S28R CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 DURING A "C" CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED, REF NR 099305. FWD CARGO COMPT STA 685 STR 27R HAS CORROSIO N IN CENTER OF SPLICE. REMOVED STRINGER SPLICE AT STR 27R STA 680 IAW B727 SRM 51-30-2 FIG 1. FAB NEW SPLICE FROM BAC 1498-131,7075 T6 PO NR 7232174. DIM 12 INCH IAW B727 SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9. TREATED AND PRIMED IAW B727 SRM 51-10-2. STRINGER SPLICE INSTALLED AT STR 28R STA 680 IAW SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2007090500236 20070905 00236 NM 2007 9 5 DHL2007746506 1 20070810 A 5320 INTERCOSTAL BOEING 727 727224 1384076 NM BS 950A-950B CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 DURING A "C" CHECK AT FLIGHTSTAR, THE FOLLOWING DISCREPANCIES WERE NOTED, REF NR 099407, AFT CARGO COMPT AT BS 950A OB O F STR 28R INTERCOSTAL LWR FLANGE HAS EXFOLIATED CORROSION. REMOVED AFT BODY PANEL NR 3522 IAW B727 SRM 51-30-2. REMOVE D INTERCOSTAL AT AFT CARGO COMPT 950A AND 950B OB. OF STR 28R IAW B727 SRM 51-30-2. FABRICATED NEW INTERCOSTAL.MATERIAL USED 7075 T6 .040 PO NR 9005551 DIMENSION 20"BY 7" IAW B727 SRM 53-10-2 FIG 5 AND 51-10-3,51-30-5. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED NEW INTERCOSTAL IAW B727 SRM 51-30-2. INSTALLED BODY PANEL NR 3522 IAW B727 SRM 51-30- 2. 2 L 7 3 4F A3WE 2007090500237 20070905 00237 NM 2007 9 5 2007UALA03364 1 20070823 A 2560 COVER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE R4 DOOR MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 768UA 26919 DOOR 4R AFT GIRT BAR DOESN'T SHOW ARMED. FOUND AFT GIRT BAR POSITION INDICATOR PLASTIC COVER IN UPSIDE DOWN POSITION . REINSTALLED COVER. GIRT BAR SHOWS ARMED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007090500238 20070905 00238 EU 2007 9 5 07FDEA03171 1 20070828 A 5320 A53989395234 SUPPORT AIRBUS 310 A310324 3930206 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 THE SUPPORT ANGLE AT FRAME 101, BETWEEN STRG 15 RT TO STRG 15 LT IS DEFORMED AND CRACKED. REPLACEMENT OF SUPPORT ANGLE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007090500239 20070905 00239 CE 2007 9 5 DXTA200702418 1 20070821 A 2120 UNKNOWN CESSNA 500 560CESSNA 2076750 CE COCKPIT ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 351QS 5600451 ON DESCENT SMELLED ELECTRICAL BURNING IN COCKPIT. COMPLIED WITH A THOROUGH INSPECTION OF THE COCKPIT AND CABIN AREA WITH NO DISCREPANCY NOTED AT THIS TIME. WE ALSO COMPLIED IWTH AN ENGINE RUN TO INCLUDE OPERATION OF AIR CONDITIONING AND AVI ONICS SYS WITH NO DISCREPANCY NOTED AT THIS TIME. 2 L 7 2 4F RT A22CE 2007090500240 20070905 00240 CE 2007 9 5 DXTA200702419 1 20070724 A 3234 CONTROL HANDLE CESSNA 750 750 2076810 CE MLG INTERMITTENT E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 979QS 7500079 LANDING GEAR HANDLE WOULD NOT MOVE AFTER TAKEOFF TO RETRACT GEAR. JACKED A/C, HOOKED UP HYD. SERVICE CART, CYCLED LANDI NG GEAR FOUND GEAR HANDLE OPERATION INTERMITTENT, REMOVED + REPLACED GEAR HANDLE MODULE, OPERATED GEAR HANDLE SEVERAL TI MES OPS CHECK GOOD. WORK DONE IAW 750 M/M CH 32-30-01, 52-80-20 2 L 7 2 4J RT T00007WI 2007090500241 20070905 00241 NM 2007 9 5 DXTA200702420 1 20070726 A 5610 SPSF2M322 WINDSHIELD AMD FALC50 FALCON2000 2730170 NM COCKPIT FAILED E DXTA B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 259QS 5711 159 AT FL430 AFTER APPOX. 4 HOURS OF FLT TIME, THE COPILOT'S FRONT WINDSCREEN SHATTERED BUT DID NOT BREAK AWAY COMPLETELY. N O PRESSURIZATION WAS LOST. REPLACED CO-PILOT'S FRONT WINDSCREEN PANEL WITH A NEW PANEL PER F2000 MM 56-102. OPS CHECK W INDSHIELD HEAT GOOD LEAK CHECKED GOOD. 2 K 7 2 4F RT A50NM 2007090500243 20070905 00243 EU 2007 9 5 07FDEA03194 1 20070828 A 5740 A57112205 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 FOUND SEVERAL HOLES WITH CRACKS AT C47 REAR SPAR INTERNAL ANGLE FITTING. REPAIR PERFORMED BY REAM UP THE HOLES UNTIL CR ACK REMOVAL, INSTALLING BUSHINGS AND CUT OUT THE LT INTERNAL ANGLE FITTING IN AREA OF HOLE NR 1 LT IAW EA 6-5710-101281 AND RAS/046699/025/2006 ISS A. 2 L 7 2 4F RT A35EU 2007090500244 20070905 00244 NM 2007 9 5 2007UALA03368 1 20070824 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 EMERGENCY EXIT LIGHT INOP AT DOOR 1 RIGHT CEILING ENTRY. RELAMPED. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090500245 20070905 00245 EU 2007 9 5 07FDEA03196 1 20070828 A 5311 A57150802202 SPAR AIRBUS 310 A310324 3930206 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 FOUND CRACKS AT HOLE H NR 11 AND H NR 24 IN REAR SPAR AT SPOILER NO:NR 3 LT ACTUATOR FITTING. REPAIR PERFORMED BY REAM UP UNTIL CRACK REMOVAL OF HOLES IAW EA 6-5720-103316 AND RAS/BAE/1003422/2006 ISS "A". 2 L 7 2 4F RT A35EU 2007090500255 20070905 00255 EA 2007 9 5 COMA0760535 1 20070820 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 659BR 7509 FLIGHT 5688 - FLAPS FAIL CAUTION MESSAGE AT 30 DEGREES. ABORTED FIRST APPROACH AND LANDED SAFELY ON SECOND APPROACH IN CAK. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C) . FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007090500256 20070905 00256 EA 2007 9 5 COMA0760536 1 20070821 A 3234 555405 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 587SW 29414 7062 FLIGHT 4984 - GEAR DOWN DISAGREE AND NOSE DOOR WARNING MESSAGES RECEIVED ON APPROACH. PERFORMED QRH, NOSE GEAR EXTENDED . DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR SELECTOR VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007090500258 20070905 00258 EA 2007 9 5 COMA0760537 1 20070821 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 587SW 1 7062 FLIGHT 4984- GEAR DOWN DISAGREE AND NOSE DOOR WARNING MESSAGES RECEIVED ON APPROACH. PERFORMED QRH, NOSE GEAR EXTENDED. DECLARED EMRGENCY AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2007090500259 20070905 00259 EA 2007 9 5 COMA0760538 1 20070821 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 999CA 23284 7230 FLIGHT 5672 - CAPTAIN'S LEFT WINDSHIELD CRACKED AT CRUISE. DIVERTED TO CVG AND LANDED WITHOUT INCIDENT. REPLACED CAPTA IN'S LEFT WINDSHIELD. 2 L 7 2 4F RT A21EA 2007090500260 20070905 00260 EA 2007 9 5 COMA0760539 1 20070821 A 3234 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 710CA 16082 7241 FLIGHT 5258 - DURING LANDING GEAR EXTENSION, RECEIVED GEAR DISAGREE MESSAGE. NOSE GEAR DID NOT COME DOWN. REPLACED NOS E GEAR SELECTOR VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007090500261 20070905 00261 EA 2007 9 5 COMA0760540 1 20070821 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 416CA 17421 7450 FLIGHT 5452 - FLAP FAIL MESSAGE RECEIVED ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LEFT BPSU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007090500262 20070905 00262 EA 2007 9 5 COMA0760541 1 20070824 A 3230 SWITCH CNDAIR CL600 CL6002B19 1900309 EA NLG OUT OF POSITION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 966CA 7132 FLIGHT 4961 - RECEIVED NOSE DOOR WARNING MESSAGE. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. FOUND NOSE DOOR MAIN TENANCE SWITCH IN OPEN POSITION. RETURNED TO FLIGHT NORMAL. SWUNG, GEAR NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007090500263 20070905 00263 NE 2007 9 5 COMA0760542 2 20070826 A 7261 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE NR 1 ENGINE OVERSERVICED A COMA E ENGINE SHUTDOWN W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 SO 01 805CA 7354 FLIGHT 5363 - RECEIVED HIGH OIL TEMPERATURE MESSAGE FOR NR 1 ENGINE. SHUTDOWN NR 1 ENGINE, DECLARED EMERGENCY, LANDED W ITHOUT INCIDENT. FOUND ENGINE OVERSERVICED BY 2 QTS. REMOVED EXCESS OIL. RAN ENGINE, NO FURTHER DEFECTS. 2 L 7 2 4F 4 F RT A21EA E15NE 2007090500264 20070905 00264 EA 2007 9 5 COMA0760543 1 20070826 A 2710 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA AILERON MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 812CA 7381 FLIGHT 5113 - ON CLIMB, BOX A ON PFD FLASHED 2-3 SECONDS, FOLLOWED BY AUTO-PILOT DISCONNECT. NOTICED STIFFNESS IN CONTR OLS WHEN TURNING LEFT. RETURNED TO ATL. LANDED WITHOUT INCIDENT. PERFORMED EO-27-075, AILERON CONTROL PATH INSPECTION . NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007090500265 20070905 00265 CE 2007 9 5 DXTA200702423 1 20070727 A 2110 11344001 A/C PACK BEECH MU300 400A 1155402 CE AFT SERVICE BAY INOPERATIVE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 122QS 842 RK467 REFRIG COMPR CIRUIT BREAKER POPPED ON GROUND, ACCOPANIED BY A HOT ELECTRICAL ODER MOST NOTICABLE IN THE CARGO COMPARTMEN T AND AT THE REAR OF THE A/C. INSTALLED OVERHAULED COMPRESSOR CONDENSER MODULE ASSEMBLY OPS CHECK GOOD IAW 21-51-00 OF THE H-400XP MM 2 H 7 2 4F RT A16SW 2007090500266 20070905 00266 EA 2007 9 5 COMA0760544 1 20070826 A 2750 7455001 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 427CA 17280 7460 FLIGHT 5618 - RECEIVED FLAP FAIL CAUTION MESSAGE AFTER LANDING. REPLACED FLAP CONTROL HANDLE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007090500267 20070905 00267 EA 2007 9 5 COMA0760545 1 20070827 A 2916 601R751113 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA MLG WW LEAKING A COMA L ABORTED APPROACH K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 01 587SW 29434 7062 FLIGHT 5579 - RECEIVED GEAR DISAGREE MESSAGE, MAINS DOWN, NOSE UP, PERFORMED QRH, GEAR EXTENDED AFTER 2B AND 3B PUMPS AC TIVATED. REPLACED NR 3 HYDRAULIC RESERVOIR. 2 L 7 2 4F RT A21EA 2007090500268 20070905 00268 CE 2007 9 5 DXTA200702421 1 20070727 A 2910 AS11606K0166 HOSE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL HYD SYSTEM RUPTURED E DXTA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 07 978QS 5713 7500187 IMMEDIATELY AFTER RAISING, THE LANDING GEAR HANDLE AFTER TAKEOFF, ALL (A) SYSTEM HYDRAULIC PRESSURE WAS LOST AND THE EIC AS INDICATED 4 PERCENT HYDRAULIC FLIUD REMAINING. THE MAIN LANDING GEAR RETRACTED AND THE NOSE GEAR REMAINED DOWN. FOU ND "NWS" CETERING HYD LINE RUPTURED. REPLACED LINE WITH NEW. REPLACED THE REMAINING 3 HOSES PN'S: AS116-06K0166 PER RE QUEST. INSPECTED ALL OTHERS CHECK GOOD. REPLACED AUX PUMP CASE DRAIN FILTER PN: CPD750-29-1. PERFORMED BLEED, LEAK, A ND OPERATIONAL TESTS OF ALL RELATED SYSTEMS ALL CHECKS SATISFACTORY. REF 750 MM CH'S 12-10-15, 29-20-04, 29-10-02, AND 32-42-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007090500269 20070905 00269 EA 2007 9 5 COMA0760546 1 20070827 A 3230 46193 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG WW FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 587SW 9608 7062 FLIGHT 5579 - RECEIVED GEAR DISAGREE MESSAGE, MAINS DOWN, NOSE UP, PERFORMED QRH, GEAR EXTENDED AFTER 2B AND 3B PUMPS AC TIVATED. REPLACED MAIN GEAR PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2007090500270 20070905 00270 CE 2007 9 5 DXTA200702422 1 20070727 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 316QS 5600516 LT BRAKE PEDAL PRESSURE ON F/O SIDE IS LOW. NEEDS TO BE PUMPED UP MANUALLY. PREFORMED BRAKE BLEEDING PROCEDURE IAW CES SNA 560 MM 32-42-00. OPS AND LEAK CHECK GOOD AT THIS TIME. 2 L 7 2 4F 4 F RT A22CE E25EA 2007090500271 20070905 00271 EA 2007 9 5 COMA0760547 1 20070827 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 587SW 34239 7062 FLIGHT 5579 - RECEIVED GEAR DISAGREE MESSAGE, MAINS DOWN, NOSE UP, PERFORMED QRH, GEAR EXTENDED AFTER 2B AND 3B PUMPS AC TIVATED. REPLACED NOSE GEAR PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2007090500272 20070905 00272 EA 2007 9 5 TRAX200701240 1 20070814 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH DETERIORATED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 874AS 7551 ALL PLACARDS O CREW ESCAPE HATCH ARE DETERIORATED. 2 L 7 2 4F RT A21EA 2007090500273 20070905 00273 EA 2007 9 5 TRAX200701241 1 20070817 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 903EV 7621 PASSENGER IN SEAT 8A REPORTED AN ELECTRICAL SMOKE SMELL ON APPROACH. FLT 4914 DEL 26 MINS. 2 L 7 2 4F RT A21EA 2007090500274 20070905 00274 EA 2007 9 5 TRAX200701242 1 20070825 A 5210 BRACKET CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 902EV 7620 ASD AFT CABLE COUNTER BALANCE ANCHOR BRACKET CRACKED. 2 L 7 2 4F RT A21EA 2007090500275 20070905 00275 EA 2007 9 5 TRAX200701243 1 20070825 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 874AS 7551 RIGHT OUTBOARD 480 CLIP IS CRACKED. 2 L 7 2 4F RT A21EA 2007090500276 20070905 00276 NM 2007 9 5 KCSA071327 1 20070829 A 5330 SKIN BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 FUSELAGE SKIN CRACKED AT BS 750, STR 16L. 2 L 7 4 4F RT A20WE 2007090500277 20070905 00277 EA 2007 9 5 TRAX200701244 1 20070825 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 MAIN CABIN DOOR WILL NOT OPEN. FLT 4728 DEL 70 MINS. 2 L 7 2 4F RT A21EA 2007090500278 20070905 00278 EA 2007 9 5 TRAX200701245 1 20070825 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 835AS 7258 SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. FLT 4605 DEL 91 MINS. 2 L 7 2 4F RT A21EA 2007090500279 20070905 00279 NM 2007 9 5 UPS07450499 1 20070809 A 5280 65B1148314 RIB BOEING 747 747200 1384847 NM RT BLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C RIGHT BLG I/B WHEEL WELL DOOR FWD AREA FOUND BULGE AS MARKED. RIGHT BLG I/B WHEEL WELL DOOR FWD SUPPO RT RIB REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F RT A20WE 2007090500280 20070905 00280 NM 2007 9 5 UPS07450500 1 20070809 A 5320 ANGLE BOEING 747 747200 1384847 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C RIGHT W/G WHEEL WELL STA 1319 VERTICAL ANGLE ATTACHED TO LONGERON FOUND CORROSION AS MARKED. CORROSIO N BLEND OUT 0.065" X .5" X 4" , HAS EXCEEDED SRM 53-10-01 FIG 1 LIMITS, RIGHT W/G WHEEL WHEEL BS 1319 VERTICAL ANGLE REP AIRED AS PER SRM 51-40-04 FIG 1. 2 L 7 4 4F RT A20WE 2007090500281 20070905 00281 NM 2007 9 5 UPS07450501 1 20070813 A 5280 65B12435601 FITTING BOEING 747 747200 1384847 NM RT BLG DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C RIGHT BLG WHEEL WELL DOOR FWD SIDE INTERNAL FITTING FOUND CORROSION. CORROSION BLEND OUT 0.045" X 1" X 3" RIGHT B/G WHEEL WELL DOOR FWD SIDE INTERNAL FITTING REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F RT A20WE 2007090500282 20070905 00282 NM 2007 9 5 UPS07450511 1 20070814 A 5420 65B913143 FITTING BOEING 747 747200 1384847 NM NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C NR 3 PYLON REAR ENG MOUNT BULKHEAD UPPER LINK BEAM ATTACHMENT BATH FITTING FOUND SUSPECTED CRACK. CRA CK LENGTH .3125 INCH. NR 3 PYLON REAR ENG MOUNT BULKHEAD UPPER LINK BEAM ATTACHMENT BATH FITTING REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F RT A20WE 2007090500283 20070905 00283 NM 2007 9 5 UPS07450512 1 20070809 A 5313 LONGERON BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C RIGHT W/G WHEEL WELL STA 1248 LONGERON CRACK APPROX 0.850 INCH AS MARKED. RIGHT W/G WHEEL WELL BETWEE N BS 1244 TO BS 1270 O/B LONGERON REPAIRED AS PER SRM 51-40-04 FIG 3. 2 L 7 4 4F RT A20WE 2007090500284 20070905 00284 NM 2007 9 5 UPS07450513 1 20070811 A 5320 65B11751606 FITTING BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D R3 DOOR CUTOUT FWD LWR CORNER FITTING CRACKED. CRACK LENGTH .5 INCH. M/D R3 DOOR CUTOUT FWD LWR CORNER FITTING REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F RT A20WE 2007090500285 20070905 00285 NM 2007 9 5 UPS07450514 1 20070807 A 5330 SKIN BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C U/D RIGHT BS 340 - 360 S6R LAP JOINT TOP ROW FASTENER ROW 1EA HOLE FOUND CRACK AT FX SKIN RUNNING AFT APPROX .125 INCH BEYOND RIVET HEAD. FX STR 6R BETWEEN BS 340-392 LAP JOINT SKIN REPAIRED AS PER SRM 53-30-03 FIG 26 AND UPS EO B747-5330-0209 APP B AND TAR S/N 127776 WITHOUT ZERO TIMING AT CRITICAL ROW FASTENERS. REPEAT INSPECTION IS REQ UIRED AS PER SRM 53-30-03 FIG 26 AND UPS ASSIGNED MPI P19377. 2 L 7 4 4F RT A20WE 2007090500286 20070905 00286 2007 9 5 DXTA200702411 4 20070819 A 2210 7022090901 COMPUTER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL FWD AVIONICS BAY MALFUNCTIONED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 942QS 2019 7500024 UPPER RUDDER B IN CRUISE AT FL240 WENT LT 4 TIMES IN 5 MIN CAUSING AIRCRAFT TO YAW WITH A HARD BUMP. REMOVED AND REPLAC ED YSAC-B COMPUTER WITH UNIT INSPECTED BY HONEYWELL. OPERATIONAL AND RIG CHECK NORMAL. WORK IAW CESSNA 750 MM CHAPT 27-2 4-01 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007090500287 20070905 00287 NM 2007 9 5 UPS07450515 1 20070807 A 5320 CHANNEL BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D RIGHT BS 900 TENSION TIE TO FRAME CONNECTION FOUND NR 5, 13, 14 HOLE CRACK AT FWD CHANNEL. CRACK LENGTH 0.030", 0.040", 0.060". M/D RIGHT BS 900 TENSION TIE FWD CHANNEL REPAIRED AS PER SRM 53-10-11 FIG 2. REPEAT INS PECTION IS REQUIRED AS PER SRM 53-10-11 FIG 2 TABLE 4 AND UPS ASSIGNED MPI P19384. 2 L 7 4 4F RT A20WE 2007090500288 20070905 00288 NM 2007 9 5 UPS07450516 1 20070807 A 5320 CHANNEL BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D LEFT BS 900 TENSION TIE TO FRAME CONNECTION FOUND NR 5 AND 13 HOLE CRACK AT FWD CHANNEL. CRACK LE NGTH 0.030" AND 0.040". M/D LEFT BS 900 TENSION TIE FWD CHANNEL REPAIRED AS PER SRM 53-10-11 FIG 2. REPEAT INSPECTION IS REQUIRED AS PER SRM 53-10-11 FIG 2 TABLE 4 AND UPS ASSIGNED MPI P19385. 2 L 7 4 4F RT A20WE 2007090500289 20070905 00289 NM 2007 9 5 UPS07450517 1 20070806 A 5320 CHANNEL BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D LEFT BS 840 TENSION TIE TO FRAME CONNECTION FOUND NR 4 HOLE CRACK AT FWD CHANNEL RUNNING UP AND DO WN. CRACK LENGTH 0.040 INCH. M/D LEFT BS 840 TENSION TIE FWD CHANNEL REPAIRED AS PER SRM 53-10-11 FIG 2. REPEAT INSPE CTION IS REQUIRED AS PER SRM 53-10-11 FIG 2 TABLE 4 AND UPS ASSIGNED MPI P19389. 2 L 7 4 4F RT A20WE 2007090500290 20070905 00290 NM 2007 9 5 UPS07450518 1 20070807 A 5311 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D RIGHT BS 820 TENSION TIE TO FRAME CONNECTION FOUND NR 10 HOLE CRACK AT FRAME WEB. CRACK LENGTH .0 625 INCH APPROX. M/D RIGHT BS 820 TENSION TIE ATTACH FRAME BETWEEN STR 8R TO STR 12R AREA REPAIRED AS PER SRM 53-10-04 FIG 132. 2 L 7 4 4F RT A20WE 2007090500291 20070905 00291 NM 2007 9 5 UPS07450519 1 20070806 A 5320 CHANNEL BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D LEFT BS 880 TENSION TIE TO FRAME CONNECTION FOUND NR 6, 7, 16 HOLE CRACK AT AFT CHANNEL. CRACK LE NGTH 0.030 INCH. M/D LEFT BS 880 TENSION TIE AFT CHANNEL REPAIRED AS PER SRM 53-10-11 FIG 2. REPEAT INSPECTION IS REQU IRED AS PER SRM 53-10-11 FIG 2 TABLE 4 AND UPS ASSIGNED MPI P19386. 2 L 7 4 4F RT A20WE 2007090500292 20070905 00292 NM 2007 9 5 UPS07450520 1 20070807 A 5320 CHANNEL BOEING 747 747200 1384847 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D RIGHT BS 820 TENSION TIE TO FRAME CONNECTION FOUND NR 23 AND 24 HOLE WITH PILOT HOLE. M/D RIGHT B S 820 TENSION TIE TO FRAME AFT CHANNEL NR 23 AND 24 HOLES OVERSIZED IN STACK UP TO 0.278 INCH DIA BY INCREMENT AS PER EO B747-5310-23715 APP D. FASTENER INSTALLED AS PER EO B747-5310-23715 APP C AFTER HFEC INSPECTED PER NTM PART 6 51-00-00 FIG 16. 2 L 7 4 4F RT A20WE 2007090500293 20070905 00293 NM 2007 9 5 UPS07450521 1 20070807 A 5320 CHANNEL BOEING 747 747200 1384847 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D RIGHT BS 940 TENSION TIE TO FRAME CONNECTION FOUND NR 4 HOLE CRACK AT FWD CHANNEL RUNNING DOWN. C RACK LENGTH 0.060 INCH. M/D RIGHT BS 940 TENSION TIE TO FRAME FWD CHANNEL NR 4 HOLE OVERSIZED IN STACK UP TO 0.309 INCH DIA BY INCREMENT AS PER EO B747-5310-23715 APP D. FASTENER INSTALLED AS PER EO B747-5310-23715 APP C AFTER HFEC INSPEC TED PER NTM PART 6 51-00-00 FIG 16. 2 L 7 4 4F RT A20WE 2007090500294 20070905 00294 NM 2007 9 5 UPS07450522 1 20070806 A 5320 65B38600113 FITTING BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D RIGHT BS 880 TENSION TIE TO FRAME CONNECTION FOUND NR 10 HOLE CRACK AT TIE CLIP RUNNING UP AND DOW N. CRACK LENGTH 0.040 INCH. M/D RIGHT BS 880 STR 9R FRAME ATTACH TIE CLIP REPLACED AND INSTALLED AS PER SRM 51-10-01 P G 9 AND 51-30-02. 2 L 7 4 4F RT A20WE 2007090500295 20070905 00295 NM 2007 9 5 UPS07450523 1 20070806 A 5320 65B38600113 FITTING BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D LEFT BS 880 TENSION TIE TO FRAME CONNECTION FOUND NR 10 HOLE CRACK AT TIE CLIP RUNNING DOWN. CRAC K LENGTH 0.040 INCH. M/D LEFT BS 880 STR 9L AREA FRAME ATTACH TIE CLIP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F RT A20WE 2007090500296 20070905 00296 NM 2007 9 5 UPS07450524 1 20070806 A 5311 FAILSAFE BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D LEFT BS 880 TENSION TIE TO FRAME CONNECTION FOUND NR 10 HOLE CRACK AT FAILSAFE CHORD RUNNING UP. CRACK LENGTH 0.040 INCH. M/D LEFT BS 880 BETWEEN STR 8L TO STR 12L AREA FAILSAFE CHORD REPAIRED AS PER SRM 51-40-03 FIG 2. 2 L 7 4 4F RT A20WE 2007090500297 20070905 00297 NM 2007 9 5 UPS07450525 1 20070806 A 5320 65B01735124 DOUBLER BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D RIGHT BS 840 TENSION TIE TO FRAME CONNECTION FOUND NR 3 HOLE CRACK AT FRAME WEB DOUBLER RUNNING UP . CRACK LENGTH 0.030 INCH. M/D RIGHT BS 840 TENSION TIE TO FRAME ATTACH DOUBLER REPLACED AND INSTALLED BETWEEN STR 9R TO STR 12R AREA AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F RT A20WE 2007090500298 20070905 00298 2007 9 5 DXTA200702410 4 20070817 A 2210 8220327508 COMPUTER AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE AVIONICS BAY MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 258QS 5610 158 AP TRIM FAIL ILLUMINATED WITH (E) DISPLAYED ON PFD. OCCURRED IN CLIMB THROUGH FL400. REPLACED LEFT AND RIGHT FCC-4002 FLIGHT CTRL COMPUTERS I/A/W F2000 MM 34-003. PERFORMED A/P FUNCTIONAL TEST W/ NO DISCREPANCIES NOTED, I/A/W F2000 MM 22 -100. 2 K 7 2 4F 4 F RT A50NM E44NE 2007090500299 20070905 00299 NM 2007 9 5 UPS07450526 1 20070806 A 5320 CHANNEL BOEING 747 747200 1384847 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D RIGHT BS 880 TENSION TIE TO FRAME CONNECTION FOUND NR 20 HOLE OVAL AT AFT CHANNEL. M/D RIGHT BS 8 40 TENSION TIE TO FRAME AFT CHANNEL NR 20 HOLE OVERSIZED IN STACK UP TO 0.309 INCH DIA BY INCREMENT AS PER EO B747-5310- 23715 APP D. FASTENER INSTALLED AS PER EO B747-5310-23715 APP C, AFTER HFEC INSPECTED PER NTM PART 6 51-00-00 FIG 16. 2 L 7 4 4F RT A20WE 2007090500300 20070905 00300 NM 2007 9 5 UPS07450527 1 20070810 A 5320 DOUBLER BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D RIGHT BS 820 TENSION TIE TO FRAME CONNECTION FOUND 1 EA HOLE CRACK AT WEB DOUBLER AT STR 11R LOCAT ION. M/D RIGHT BS 820 TENSION TIE TO FRAME ATTACH DOUBLER REPLACED BETWEEN STR 9R TO 12R AREA AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F RT A20WE 2007090500301 20070905 00301 NM 2007 9 5 UPS07450528 1 20070807 A 5320 CHANNEL BOEING 747 747200 1384847 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D LEFT BS 820 TENSION TIE TO FRAME CONNECTION FOUND NR 20, 23, 24 HOLE WITH PILOT HOLE AT AFT CHANNE L. M/D LEFT BS 820 TENSION TIE TO FRAME ATTACH TENSION TIE AFT CHANNEL NR 20, 23, 24 HOLES OVERSIZED IN STACK UP TO 0.2 78 INCH DIA BY INCREMENT AS PER EO B747-5310-23715 APP D. FASTENERS INSTALLED AS PER EO B747-5310-23715 APP C, AFTER HF EC INSPECTED PER NTM PART 6 51-00-00 FIG 16. 2 L 7 4 4F RT A20WE 2007090500302 20070905 00302 CE 2007 9 5 DXTA200702425 1 20070727 A 2612 FIRE LOOP CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE NR 2 NACELLE LOOSE E DXTA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 658QS 5605665 THE NR 2 ENGINE FIRE LIGHT WOULD FAINTLY GLOW AND FLICKER DURING FLIGHT WHEN WE WERE IN FROZEN PRECIP AND CONTINUOUS CHO P TURBULENCE. THE ENG/WING ANTI ICE WAS ON, BUT ALL ENGINE PARAMETERS APPEARED NORMAL. EXITING THE WEATHER CONDITIONS TH E INDICATION WENT A AWAY. INSPECTED RT ENGINE FIRE CABLE FOUND CABLE UNSAFETY AND VERY LOOSE AT CONNECTING POINT. ALSO FOUND 3 CLAMPS MISSING RECONNECTED AND SAFETIED. INSTALLED 3 NEW CLAMP. INSPECTED RT ENGINE FOR BLEED LEAKS NONE NOTED. PERFORMED ENGINE FIRE TEST CHECK GOOD. RAN ENGINE ALL INDICATIONS GOOD ALL WORK IAW CE560XLS M/M CH 26-11-01 2 L 7 2 4F 4 F RT A22CE E00059EN 2007090500303 20070905 00303 NM 2007 9 5 UPS07450529 1 20070807 A 5320 DOUBLER BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D LEFT BS 820 TENSION TIE TO FRAME CONNECTION FOUND NR 12 HOLE CRACK AT FRAME WEB DOUBLER. M/D LEFT BS 820 TENSION TIE TO FRAME ATTACH DOUBLER AT HOLE NR 12 OVERSIZED IN STACK UP TO 0.247 INCH DIA BY INCREMENT AS PER EO B747-5310-23715 APP D. FASTENER INSTALLED AS PER EO B747-5310-23715 APP C, AFTER HFEC INSPECTED PER NTM PART 6 51-00-0 0 FIG 16. 2 L 7 4 4F RT A20WE 2007090500304 20070905 00304 NM 2007 9 5 UPS07450530 1 20070808 A 5320 65B0966114 SHEAR WEB BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D BETWEEN TENSION TIE RIGHT SLOPING SHEAR WEB CRACKED AT BS 820. CRACK LENGTH 1.5 INCH. M/D BETWEE N BS 820 TO BS 840 TENSION TIE RIGHT SLOPING SHEAR WEB REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F RT A20WE 2007090500305 20070905 00305 NM 2007 9 5 UPS07450531 1 20070809 A 5311 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C AFT CARGO COMPT STA 1540 FRAME FOUND CRACKED ADJACENT TO SIDE GUIDE SUPPORT BRACKET AREA AT S39R. CRA CK LENGTH .25 INCH. AFT CARGO COMPT BS 1540 STR 39R AREA FRAME REPAIRED AS PER SRM 51-40-03 FIG 1. 2 L 7 4 4F RT A20WE 2007090500306 20070905 00306 NM 2007 9 5 UPS07450532 1 20070809 A 5311 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C AFT CARGO COMPT STA 1560 FRAME FOUND CRACKED ADJACENT TO SIDE GUIDE SUPPORT BRACKET AREA AT STR 39R. CRACK LENGTH .3125 INCH. AFT CARGO COMPT BS 1560 STR 39R AREA FRAME REPAIRED AS PER SRM 51-40-03 FIG 1. 2 L 7 4 4F RT A20WE 2007090500307 20070905 00307 NM 2007 9 5 UPS07450533 1 20070809 A 5311 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C AFT CARGO COMPT STA 1600 FRAME FOUND CRACKED ADJACENT TO SIDE GUIDE SUPPORT BRACKET AREA STR 39R. CRA CK LENGTH .375 INCH. AFT CARGO COMPT BS 1600 FRAME AT STR 39R AREA REPAIRED AS PER SRM 51-40-03 FIG 1. 2 L 7 4 4F RT A20WE 2007090500308 20070905 00308 NM 2007 9 5 UPS07450534 1 20070809 A 5311 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C AFT CARGO COMPT STA 1580 FRAME FOUND CRACK ADJACENT TO SIDE GUIDE SUPPORT BRACKET AT S39R. CRACK LEGN TH .25 INCH. AFT CARGO COMPT BS 1580 STR 39R AREA FRAME REPAIRED AS PER SRM 51-40-03 FIG 1. 2 L 7 4 4F RT A20WE 2007090500309 20070905 00309 NM 2007 9 5 UPS07650508 1 20070827 A 3620 CIRCUIT CARD BOEING 767 76734AF 1385212 NM BLEED AIR SYS FAULTY A IPXA A UNSCHED LANDING N FALSE WARNING UK UNKNOWN 1 SO 01 327UP 27753 INSPECTION TYPE:ETOP L DUCT LEAK LIGHT ILLUMINATED. EICAS MESSAGE: L/BLEED DUCT LEAK DISPLAYED. LIGHT EXITING APPROXI MATELY 5 MINUTES AFTER MESSAGE BLEED AIR SUPPLY & ISOLATION VALVES CLOSED. ACCOMPLISHED FIM PROC 26-18-00, FIGURE 104, NO FAULTS FOUND. MEASURED DUCT LEAK DETECTOR CENTER CONDUCTOR TO GROUND RESISTANCE = 3.1 MEGOHM. REPLACED DUCT LEAK CA RD M691 IAW 26-10-01-4. RAN ENGINE, NO DUCT LEAK INDICATION OCCURRED. 2 L 7 2 4F RT A1NM 2007090500310 20070905 00310 WP 2007 9 5 UPS07850503 1 20070808 A 5330 56153741 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 MAJOR CORROSION BETWEEN STA 1620 - 1640 L31L - L31R, BETWEEN SKIN AND INTERNAL DOUBLER, CORROSION ARO UND OUTFLOW VALVE. REMOVED AND REPLACED BELLY SKIN FROM STA 1490 - 1690 L31L - L31R IAW SRM 51-1-20D AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007090500311 20070905 00311 WP 2007 9 5 UPS07850504 1 20070809 A 5313 564932959 LONGERON SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 .25 INCH CRACK LWR ROW STA 1749 ON L28R SPLICE AND EXISTING REPAIR THAT IS NOT PER SRO8530032. REMOV ED EXISTING REPAIR AND CUT OUT DAMAGED AREA OF L28R SPLICE AT STA 1749 IAW SRO8530032. FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS AT STA 1749 L28R IAW SAA EA 008-5330-01-A1044, UPS EO DC8- 5330-27492-A, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007090500312 20070905 00312 WP 2007 9 5 UPS07850506 1 20070804 A 5347 6015176 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 SEAT TRACK GOUGED OUT OF LIMITS AT STA 240 BL 0. REMOVED AND REPLACED SEAT TRACK SECTION FROM STA 23 0-250 BL 0 IAW SRM 53-02-03-0 FIG 014, 53-07-03 FIG 2B, AND DWG S2400463. 2 L 7 4 4F RT 4A25 2007090500313 20070905 00313 2007 9 5 UPS07850509 4 20070828 A 2565 SLIDE DOUG DC8 DC871F 302199D WP EMERGENCY EXIT OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:N/A ESCAPE SLIDE FELL OUT WHEN DOOR WAS OPENED. RESECURED SLIDE. OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2007090500314 20070905 00314 WP 2007 9 5 UPS07850535 1 20070829 A 3350 LIGHT DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 EMERGENCY LIGHTS ON AT POWER TRANSFER, WOULD NOT GO OUT. 09-07-07 RESET DC EMERGENCY BREAKER. SYTEM OPS CKS OK REF M M 33-50-00-0. 2 L 7 4 4F RT 4A25 2007090500315 20070905 00315 CE 2007 9 5 DXTA200702424 1 20070727 A 3243 9536718 MASTER CYLINDER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE BRAKES LEAKING E DXTA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 331QS 4013 5600331 COPILOTS RT BRAKE PEDAL GOES TO FLOOR WITHOUT BRAKES. PEDAL PUMPS UP NORMALLY AND THEN BRAKE CATCHES. PERFORMED OPS CH ECK OF CO-PILOTS R/H BRAKE PEDAL IAW CESSNA 560MM 32-42-02. FOUND CO-PILOTS R/H BRAKE MASTER CYLINDER LEAKING FROM LOWE R JAM NUT REMOVED AND REPLACED CO-PILOTS R/H MASTER CYLINDER AND PILOTS R/H MASTER CYLINDER IAW CESSNA 560 MM 32-42-02 BRAKE SYSTEM BLED IAW CESSNA 560 MM 32-42-00 OPS & LEAK CK GOOD 2 L 7 2 4F 4 F RT A22CE E25EA 2007090500316 20070905 00316 NM 2007 9 5 UPS07M50502 1 20070727 A 5320 STRUCTURE DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C AFT CARGO COMPT, RIGHT SIDE AFT VENT CUTOUT SURROUNDING AREA FOUND WITH CORROSION. CORROSION REMOVED FOUND EXCEEDED LIMIT PER SRM 53-00-01 FIG 1A VI R38. CORRODED INNER DOUBLER REMOVED PER SRM 51-35-01VII R38. NEW DOUBL ER FAB PER DOC DWG: AGA8013 MAT'L USED 707576-0.160". NEW DOUBLER FASTENER HOLES PICKED UP, REPROTECTED & PRIMER TOUCHE D UP. NEW DOUBLER INSTALLED PER SRM 51-31-01 VI R38. REWORKED AREA PAINTED PER SRM 51-21-02 VII R38. 2 L 7 3 4F RT A22WE 2007090500317 20070905 00317 2007 9 5 UPS07M50505 4 20070825 A 2565 SWITCH DOUG MD11 MD11F 3023600 NM EMERGENCY EXIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 252UP 48768 INSPECTION TYPE:N/A FLIGHT CREW PRE DEPT CK - L1 DOOR EVACUATION SLIDE PRESS PUSH TO TEST INOP, M357419. PFM T/S FOUND LAMPS MISSING PTT SWITCH CONTACT WAS NO GOOD. REPLACED 2EA LAMPS & ADJUSTED PTT SWITCH & PFM OPERATION TEST. CONDITION BACK TO SATISFACTORY AS PER AMM 25-61-04, MEL 25-61-2 & DEFERRAL M357419 IS CLOSED. 2 L 7 3 4F RT A22WE 2007090500318 20070905 00318 CE 2007 9 5 DXTA200702426 1 20070728 A 3243 MASTER CYLINDER RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP BRAKES UNDERSERVICED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 838QS 258338 MAIN BRAKES FEEL SOFT, MORE PRESSURE THAN NORMAL NEEDED TO STOP AIRCRAFT. CHECKED ALL BRAKE WEAR INDICATORS CHECKED GO OD. SERVICED MASTER CYLENDERS AND BLED BRAKES IAW HAWKER 800XP AMM 32-40-00. SERVICED HYD RESERVOIR IAW HAWKER 800XP M /M 12-29-00 2 L 7 2 4F 4 F RT A3EU E6WE 2007090500319 20070905 00319 NM 2007 9 5 KPVA200712 1 20070828 A 2131 1305221 CONTROL PANEL DHAV DHC8 DHC8103 1386005 NM COCKPIT DEFECTIVE A KPVA I B A CABIN DEPRESSURIZATION EMER. DESCENT UNSCHED LANDING O OTHER CL CLIMB 1 WP 13 829EX 168 146 (PIREP) EN ROUTE TO LIH AT APPROX 12,700 FT CLIMBING, HEARD A LOUD RUSHING NOISE IN COCKPIT. PRESSURE RATE WAS PEGGED A T 2000 FPM CLIMB. CABIN DEPRESSURIZED TO 9,000 FT DIFFERENTIAL DROPPED TO ZERO. RAN CHECKLIST BUT PRESSURE NEVER RETUR NED. (MX) REMOVED AND REPLACED CABIN AIR PRESSURE SELECTOR PANEL IAW DHC MM 21-30-07 PG 201-202. OPS CHECK IAW DHC MM 21-30-00 PG 201-203. OPS CHECK GOOD. POST MAINTENANCE CHECK FLIGHT SATISFACTORY. 2 H 7 2 4T RT A13NM 2007090500320 20070905 00320 CE 2007 9 5 DXTA200702427 1 20070729 A 2910 O-RING CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE HYD SYSTEM CUT E DXTA O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 619QS 5605562 WITH AIR COMING OUT OF SIDE VENTS. UPPER DUCTS A BURNED ACRID SMELL AND BLUE-ISH SMOKE LIKE HAZE WAS OBSERVED IN CABIN (APU RUNNING, ENGINES OFF) FOUND HYD RESERVOIR LEAKING AT FWD UNION REPLACED CUT O-RING AND SVCD HYDRAULIC SYS. I/A/ W CE560XL AMM 29-11-01 CLEANED OIL RESIDUE IN SUPPLY DUCT TO COALESCER BAG AND WASHED COALESCER BAG I/A/W CE560XL AMM 12 -19-02. OPERATED ENVIROMENTAL CONTROL SYS. NO DEFECTS NOTED. INSP APU AND BOTH ENG PNEUMATIC DUCTS FOR OIL RESIDUE. NONE FOUND 2 L 7 2 4F 4 F RT A22CE E00059EN 2007090500321 20070905 00321 NM 2007 9 5 USAA920070804 1 20070826 A 5320 141N516625 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 942UW 27807 BFM - MAJOR REPAIR - C-04 CHECK - CORROSION FOUND ON FLOOR SUPPORT, BS 395, RBL 46 - RBL 60. REPLACED FLOOR SUPPORT, BS 395, RBL 46 - RBL 60 IAW B757-200 SRM 53-00-51, 51-10-01 AND 51-40-02. 2 L 7 2 4F RT A2NM 2007090500322 20070905 00322 NM 2007 9 5 USAA920070805 1 20070828 A 5320 141N51911 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 942UW 27807 BFM - MAJOR REPAIR - C-04 CHECK - CORROSION FOUND ON FLOOR SUPPORT, BS 324 - BS 418, BL 0. REPLACED FLOOR SUPPORT, BS 3 24 - BS 418 IAW B757-200 SRM 51-40-02, 51-10-02, AND 51-40-05. 2 L 7 2 4F RT A2NM 2007090500326 20070905 00326 EU 2007 9 5 SA07055 1 20070827 A 3232 2271500002 ACTUATOR AIRBUS 320 A320214 3930316 EU MLG DOOR OUT OF ADJUST A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 111US 1114 TPA FLT 774 EN ROUTE LAS TO TPA. DURING FINAL APPROACH, THE CREW RECEIVED A NOSE GEAR DOOR ECAM MESSAGE. THE GEAR W AS EXTENDED USING THE ALTERNATE EXTENSION METHOD. AFTER LANDING, THE AIRCRAFT WAS TOWED TO THE GATE WITHOUT FURTHER INC IDENT. MAINTENANCE ADJUSTED THE NOSE LANDING GEAR DOOR ACTUATOR. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007090500327 20070905 00327 NM 2007 9 5 07FDEA03161 1 20070828 A 5710 ARC199114 BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) FORWARD SUPPORT INBOARD AFT BORE EXISTING DIAMETER = 0.5INCH. COM PLIED WITH FEDEX EA 1-5750-115159. 2 L 7 3 4F RT A22WE 2007090500328 20070905 00328 EA 2007 9 5 TRAX200701246 1 20070826 A 3260 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 834AS 7254 NOSE GEAR DISAGREE WARNING MESSAGE AND STEERING INOP CAUTION MESSAGE WHEN RETRACTING GEAR. A/C RETURNED TO ATL AFTER T/ O. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007090500329 20070905 00329 EA 2007 9 5 TRAX200701247 1 20070826 A 3260 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 834AS 7254 ON T/O RETRACTED GEAR AND RECEIVED -STEERING INOP- EICAS CAUTION FOLLOWED BY GEAR DISAGREE MANUALLY LOWERED GEAR. REAR DISAGREE MESSAGE OUT. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. FLTS 4729, 4700 CX. 2 L 7 2 4F RT A21EA 2007090500330 20070905 00330 EA 2007 9 5 TRAX200701248 1 20070826 A 2613 OVERHEAT SYS CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 904EV 7628 LT JETPIPE OVERHEAT WARNING MSG. EN ROUTE TO ICT A/C DIVERTED TO HSV DUE TO MTC. EMERGENCY DECLARED. FLTS 4124 CX. 2 L 7 2 4F RT A21EA 2007090500331 20070905 00331 NM 2007 9 5 CALA0700464 1 20070829 A 5311 6546551 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A .75 INCH CRACK AROUND RIVET IN FRAME AT STA 807 ABOVE S9L. REPAIR PARTS WERE INSTALLED IAW ECRA 5310 -04650. 2 L 7 2 4F RT A16WE 2007090500332 20070905 00332 NM 2007 9 5 CALA0700465 1 20070829 A 5311 6546555 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A .75 INCH CRACK AROUND RIVET IN FRAME AT STA 867 ABOVE S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-0465 0. 2 L 7 2 4F RT A16WE 2007090500333 20070905 00333 NM 2007 9 5 CALA0700466 1 20070829 A 5311 6546552 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A .75 INCH CRACK AROUND RIVET IN FRAME AT STA 827 ABOVE S9L. THE FRAME WAS REPAIRED IAW ECRA 5310-0465 0. 2 L 7 2 4F RT A16WE 2007090500334 20070905 00334 NM 2007 9 5 CALA0700467 1 20070829 A 5311 6546557 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A .75 INCH CRACK AROUND RIVET IN FRAME AT STA 887 ABOVE S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-0465 0. 2 L 7 2 4F RT A16WE 2007090500335 20070905 00335 NM 2007 9 5 CALA0700468 1 20070829 A 5311 6546552 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A .75 INCH CRACK AROUND RIVET IN FRAME AT STA 827 ABOVE S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-0465 0. 2 L 7 2 4F RT A16WE 2007090500336 20070905 00336 EU 2007 9 5 07FDEA03162 1 20070828 A 5414 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 811FD 457 CRACKED HOLE ON PYLON NR 2 AT RIB 8 UPPER SPAR. REPAIR PERFORMED IAW SRM 54-51-31/FIG 20. INSPECTION PROGRAM IAW EA 6- 5451-103288. 2 L 7 2 4F RT A35EU 2007090500337 20070905 00337 NM 2007 9 5 CALA0700469 1 20070829 A 5311 6546525 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 380 BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04650. 2 L 7 2 4F RT A16WE 2007090500338 20070905 00338 NM 2007 9 5 CALA0700470 1 20070829 A 5311 6546526 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 400 BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04650. 2 L 7 2 4F RT A16WE 2007090500339 20070905 00339 NM 2007 9 5 CALA0700471 1 20070829 A 5311 6546555 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A .5 INCH CRACK AROUND RIVET IN FRAME AT STA 867 ABOVE S9L STRINGER TIE. THE FRAME WAS REPAIRED IAW EC RA 5310-04650. 2 L 7 2 4F RT A16WE 2007090500340 20070905 00340 NM 2007 9 5 CALA0700472 1 20070829 A 5311 6546557 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A .5 INCH CRACK AROUND RIVET IN FRAME AT STA 887 ABOVE S9L STRINGER TIE. THE FRAME WAS REPAIRED IAW EC RA 5310-04650. 2 L 7 2 4F RT A16WE 2007090500341 20070905 00341 NM 2007 9 5 CALA0700473 1 20070830 A 5230 6546921 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A .25 INCH CRACK IN C-1 CARGO DOOR SKIN AT HANDLE CUTOUT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00 -01. 2 L 7 2 4F RT A16WE 2007090500342 20070905 00342 NM 2007 9 5 CALA0700474 1 20070830 A 5311 65C22909 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 500D ONE INCH ABOVE S13R. THE FRAME WAS REPAIRED IAW SRM 53-00-07. 2 L 7 2 4F RT A16WE 2007090500343 20070905 00343 NM 2007 9 5 USAA070702 1 20070830 A 5340 STRINGER CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 STA 767, S26L, STRINGER TIE CLIP HAS CORROSION. REPLACED STRINGER TIE CLIP PER SRM 51-20-01, 51-10-02; CORR TASK C53-20 2-01, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007090500344 20070905 00344 NM 2007 9 5 USAA070693 1 20070830 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 STA 727E, LBBL 8 ON FRAME WHERE IT ATTACHES TO SKIN EXFOLIATED. FABRICATED REPAIR PART & INSTALLED PER SRM 53-60-07; CO RR TASK C53-208-01, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007090500347 20070905 00347 NM 2007 9 5 USAA070696 1 20070830 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 STA 986.5, LBL 32 THRU RBL 34 HAS CORROSION. INSTALLED FILLER & DOUBLER PER TYP 51-70-12; CORR TASK C53-107-02, DEFECT SIZE: 2 X 2 INCHES. 2 L 7 2 4F RT A16WE 2007090500348 20070905 00348 NM 2007 9 5 USAA070697 1 20070830 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 STA 328, BL 50, FLOORBEAM T-CAP HAS CORROSION. REMOVED PREVIOUS REPAIR & INSTALLED/SPLICED IN NEW T-CAP PER SRM 53-10-5 0 FIG 201; CORR TASK C53-107, DEFECT SIZE: 24 INCHES. 2 L 7 2 4F RT A16WE 2007090500357 20070905 00357 EU 2007 9 5 USAA070707 1 20070830 A 5330 SKIN AIRBUS A321 A321211 3930370 EU FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 185UW 1666 FR 76 - 77 BETWEEN STRINGERS R36-37 HAS CREASE. CUT OUT DAMAGE & INSTALLED DOUBLER PER SRM 53-00-11 FIG 203, DEFECT SIZ E: 2.5" X 1" X .125". 2 L 7 2 4F RT A28NM 2007090600004 20070906 00004 NM 2007 9 6 TAMF20070018S 1 20070825 A 5330 SKIN BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE BS 1506 S31-32L DENTED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 768QT 23803 DURING INSPECTION OF (C2) CHECK WAS FOUND A DENT A/Y=20 ON FUSELAGE SKIN AT STA 1506, STR 31-32 -LT. DAMAGED AREA WAS R EPAIRED IAW EWO 767-53-048 AND SRM 53-00-01 REPAIR 6. THIS REPAIR CONSTITUTES A MAJOR REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007090600005 20070906 00005 GL 2007 9 6 HEEA116968 2 20070816 A 7250 6898663 TURBINE WHEEL BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE FAILED E HEEA R AUTOROTATION R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 03 433PH 1905 53679 CAE847233 APPROXIMATELY 5 MINUTES AFTER TAKEOFF, THE ENGINE FAILED AND AUTOROTATION WAS COMPLETED TO THE WATER. ENGINE WAS REMOVE D DUE TO ENGINE SHUTDOWN. SUSPECT 3RD STAGE WHEEL FAILURE, 3RD STAGE WHEEL FOUND WITH ALL BLADES FRACTURED AT ROOT. TU RBINE WAS SHIPPED TO MFG FOR FAILURE ANALYSIS. 1 G 7 1 3U 3 U O H2SW E1GL 2007090600006 20070906 00006 SW 2007 9 6 HEEA116969 1 20070819 A 7931 222375077113 TRANSDUCER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE FAILED E HEEA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 03 612PH 53199 10 MINUTES OUT, THE ENGINE OIL PRESSURE DROPPED TO ZERO, NO TORQUE FLUCTUATION, TEMP STABLE, NO CAUTION LIGHTS. LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE OIL PRESSURE TRANSDUCER PN 222-375-077-113, SN 6073-3A-70 AND THE ENG INE OIL TEMP-PRESS INDICATOR PN 407-375-004-103, SN 0842. 1 G 7 1 3U 3 U O H2SW E1GL 2007090600007 20070906 00007 2007 9 6 HEEA116970 4 20070818 A 3414 7660021007041 DETECTOR SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL2S2 60036 NE LOW SPEED MALFUNCTIONED E HEEA O OTHER J WARNING INDICATION CR CRUISE 1 SW 03 779P 329 760655 IN CRUISE, NR 1 CRT LIGHT ILLUMINATED. MAINTENANCE REPLACED THE LOW SPEED DETECTOR. 1 G 7 2 3U 4 U NC H1NE E00054EN 2007090600008 20070906 00008 2007 9 6 HEEA116982 4 20070821 A 2215 7690001802106 ACTUATOR SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL2S2 60036 NE MALFUNCTIONED E HEEA O OTHER J WARNING INDICATION CL CLIMB 1 SW 03 784P 760634 DURING CLIMB, AIRCRAFT YAWED NOTICEABLY AND WAS ACCOMPANIED BY AN IE27 YAW FAILURE CAUTION LIGHT. RESET BOTH AP1 AND AP 2 SWITCHES AND CAUTION LIGHT EXTINGUISHED. COLLECTIVE YAW CIRCUIT BREAKER WAS THEN FOUND TO BE TRIPPED. RESET CIRCUIT BREAKER. DURING DESCENT, A VERTICAL SPEED WAS ESTABLISED AT 400 FPM. AIRCRAFT THEN NOSED OVER AND REACHED A RATE OF 1 100 FPM BEFORE PILOT DECOUPLED AP AND HAND FLEW AIRCRAFT TO LANDING. NOSE OVER WAS ACCOMPANIED BY AN IE40 ERROR. REPLA CED NR 1 PITCH LINEAR ACTUATOR. 1 G 7 2 3U 4 U NC H1NE E00054EN 2007090600009 20070906 00009 2007 9 6 HEEA116983 4 20070821 A 2200 AUTOPILOT SYS SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL2S1 60057 NE UNKNOWN E HEEA O OTHER J WARNING INDICATION HO HOVERING 1 SW 03 767P 760599 DURING HOVER FOR TAKEOFF, AFCS KICKED HARD. LANDED AIRCRAFT GROUND TAXIED TO PARKING. MAINTENANCE INSPECTED THE AIRCRA FT, CONNECTED A HYDRAULIC MULE AND WORKED ALL CONTROLS. THEY WERE UNABLE TO DUPLICATE THE DISCREPANCY. 1 G 7 2 3U 4 U NC H1NE E00054EN 2007090600017 20070906 00017 NM 2007 9 6 TAMF20070017S 1 20070826 A 5710 BEAM BOEING 767 767200 1385120 NM PWA PT6 PT6A114A 52043 NE WING LE CRACKED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 768QT 23803 DURING C-CHECKS INSPECTION WAS FOUND A CRACK ON FIXED LEADING EDGE NOSE BEAM WEB STA OSS 644.58-694.55 - RT. DAMAGED AR EA WAS REPAIRED IAW EWO 767-57-025 AND SRM 57-41-13 REPAIR 1-2. THIS REPAIR CONSTITUTES A MAJOR REPAIR. 2 L 7 2 4F 3 T RT A1NM E4EA 2007090600019 20070906 00019 EU 2007 9 6 75408212007 1 20070821 A 2120 UNKNOWN BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C28B 03013 GL UNKNOWN ODOR E QMLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 485EC S754 FUEL ODOR NOTICEABLE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO BASE. MAINTENANCE INSPECTED BELLY, SUMP DRAINS, AND DRAIN PORTS, FOUND NO EVIDENCE OF LEAKS. ALSO, THE MECHANIC INSPECTED BOTH ENGINES FOR EVIDENCE OF FUEL LEAKS, FOUND NONE. MAINTENANCE OPERATIONAL CHECK SHOWED NO LEAKS DURING OPERATION OR ODORS DURING FLIGHT. 1 G 7 2 3U 3 U H3EU E1GL 2007090600023 20070906 00023 NM 2007 9 6 ASMF200708005 1 20070820 A 5330 SKIN BOEING 737 737* NM CFMINT CFM567 CFM567B22 13802 NE BS 941 S23L DENTED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 842AM 32842 DURING TRANSIT CHECK WAS DETECTED A DENT OF 0.225 INCH DEPTH AND 3.0 INCH WIDTH OUT OF LIMITS ON THE FUSELAGE LT SIDE, B ELOW LT SERVICE DOOR AT STATION 941 AND S-23 LT. AIRCRAFT WAS SENT TO THE HANGAR AND PERMANENT REPAIR WAS PERFORMED IAW MSG 1-522571883-2. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007090600025 20070906 00025 CE 2007 9 6 AMWA25033D 1 20070822 A 5311 12943003623 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 363 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 159YV UE159 FUSELAGE FRAME HAD FRICTION CHAFING. REPAIRED IAW ENGINEERING REPORT 6829-1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007090600026 20070906 00026 CE 2007 9 6 AMWA25033E 1 20070822 A 5311 1294300311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 378 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 159YV UE159 FUSELAGE FRAME HAD FRICTION CHAFING. REPAIRED IAW ENGINEERING REPORT 6829-1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007090600029 20070906 00029 CE 2007 9 6 AMWA25033G 1 20070822 A 5311 1294400681 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 438 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 159YV UE159 FUSELAGE FRAME HAD FRICTION CHAFING. REPAIRED IAW ENGINEERING REPORT 6829-1 2 L 7 2 4T 4 T RT A24CE E26NE 2007090600032 20070906 00032 WP 2007 9 6 ASMF200708007 1 20070825 A 7830 0711346003 CONTROL VALVE DOUG DC8 DC821 3021906 WP PWA JT8 JT8D217A 52053 NE THRUST REVERSER LEAKING W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 501AM 10130 9942 49188 DURING TRANSIT CHECK WAS DETECTED A HYDRAULIC LEAK IN THE LT ENGINE REVERSE CONTROL VALVE. THE VALVE WAS REPLACED IAW MM 78-31-04, TESTED CORRECT AND 6/4 OF HYDRAULIC FLUID WERE REPLENISHED IAW MM 12-13-82. 2 L 7 4 4J 4 F 4A25 E9NE 2007090600039 20070906 00039 NE 2007 9 6 704208212007 2 20070821 A 7310 418159001 TUBE BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE NR 2 ENGINE CHAFED E QMLA K NONE K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 NM 03 217LN 7042 LE45987 AFTER COMPLETING A SCENE FLIGHT PILOT REPOSITIONED TO WAIT ON MED CREW AND REFUEL. AFTER SHUTTING DOWN, PILOT PERFORMED A WALK AROUND AND NOTICED FUEL COMING FROM NR 2 SIDE ENGINE COWLINGS. MECHANIC FOUND CHAFED TUBE FROM FUEL PUMP TO FUEL FILTER ON NR 2 ENGINE. 1 G 7 2 3U 3 U H13EU E5NE10 2007090600041 20070906 00041 CE 2007 9 6 DXTA200702393 1 20070809 A 5210 DOOR CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE MAIN PAX OUT OF ALIGNMENT E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 808QS 5600619 DURING T/O ROIL MAIN CABIN DOOR ANNUNCIATOR CAME ON, UPON INSPECTION PRIOR TO OPENING DOOR NOTICED ALLIGNMENT MARKS TO B E OUT OF ALIGNMENT APROX .1250 INCH. 2 L 7 2 4F 4 F RT A22CE E00053EN 2007090600043 20070906 00043 CE 2007 9 6 AMWA25033B 1 20070822 A 5311 1294300311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 273 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 159YV UE159 FUSELAGE FRAME HAS FRICTION CHAFING. REPAIRED IAW ENGINEERING REPORT 6829-1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007090600045 20070906 00045 NE 2007 9 6 HEEA116823 1 20070728 A 7714 7690001821104 TRANSDUCER SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL2S1 60057 NE NR 2 ENGINE FLUCTUATES D HEEA O OTHER J WARNING INDICATION CR CRUISE 1 SW 03 761P 760588 IN CRUISE FLIGHT AT 5000 FT IFR NR 2 ENGINE DECELLED THEN CAME BACK TO NORMAL. ENGINE OUT LIGHT, AUDIO BOTH CAME ON FOR ABOUT 1 SECOND DURATION. ENGINE RECOVERED. AFTER DESCENDING TO 2000 FT TO START APPROACH, AFTER ABOUT 20 SEC LEVEL A T 2000 FT. N1 ON NR 2 ENGINE AGAIN DROPPED 30, T5, TORQUE FLUCTUATED FOR ABOUT 5 SECONDS THEN STABILIZED AND REMAINED S TABLE TILL LANDING. MAINTENANCE REPLACED TRANSDUCER. 1 G 7 2 3U 4 U NC H1NE E00054EN 2007090600052 20070906 00052 GL 2007 9 6 HEEA116944 2 20070820 A 7230 NA COMPRESSOR BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ENGINE STALLED E HEEA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 03 6160Y 51609 PILOT REPOSITIONED THE AIRCRAFT FROM THE AIRFIELD TO A HELIPAD AT CUSTOMER'S LOCATION. DURING TAKEOFF TO A HOVER AT THA T LOCATION, PILOT HEARD A LOUD POPPING NOISE AND THE AIRCRAFT LOST SOME POWER. PILOT SUSPECTED COMPRESSOR STALL, SHUTDO WN. MAINTENANCE INSPECTED AIRCRAFT AND FOUND A FROG HAD BEEN INGESTED BY THE ENGINE. NO DAMAGE WAS NOTED. COMPLIED WITH A COMPRESSOR RINSE AND RELEASE AIRCRAFT. 1 G 7 1 3U 3 U H2SW E1GL 2007090600072 20070906 00072 WP 2007 9 6 AMTA200700392 1 20070817 A 3244 TIRE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211535E4 54555 NE NLG FAILED A AMTA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 11 164AT 1238 ON LANDING BOTH NOSE TIRES BLOWN. REMOVED AND REPLACED BOTH NLG TIRES IAW L1011, MM 32-42-01. REF VAL WO 0317-15-0026. (K) 2 L 7 3 4F 4 F A23WE E12EU 2007090600089 20070906 00089 2007 9 6 UH02007F00002 2 20070402 A 7414 GEAR SKRSKY S58 S58J 8141814 NE MAGNETO FAILED E UH0A O OTHER O OTHER NR NOT REPORTED 1 SW 03 58HU 06442M 581575 DURING CRUISE FLIGHT (2,500 ER PM AND 37 MAP) ENGINE BACKFIRED AND FAILED. AIRCRAFT WAS LANDED W/O FURTHER INCIDENT OR DAMAGE. INSPECTION REVEALED FAILURE OF PHENOLIC GEAR INSIDE MAGNETO. GEAR IS LUBRICATED DURING O/H BUT WAS DRY. RECO MMENDED EVALUATION OF TYPE OIL USED DURING O/H LUBRICATION AND PROCEDURE FOR RE-LUBRICATING IN THE FIELD. (K) 2 G 7 1 4R 1H11 2007090600094 20070906 00094 EU 2007 9 6 07FDEA03274 1 20070831 A 5740 A53510223200 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 FOUND HEAVY CORRODED FITTING ON LT WING IN KRUEGER FLAP AREA, FRAME 38-39. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 57-45-11. 2 L 7 2 4F RT A35EU 2007090600095 20070906 00095 EU 2007 9 6 07FDEA03275 1 20070831 A 5740 A53510218202 BRACKET AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 FOUND HEAVY CORRODED BRACKET ON LT WING IN KRUEGER FLAP AREA, FRAME 38-39. REPAIR PERFORMED BY REPLACEMENT OF PART IAW S RM 57-45-11. 2 L 7 2 4F RT A35EU 2007090600096 20070906 00096 EU 2007 9 6 07FDEA03276 1 20070831 A 5740 A53510218201 BRACKET AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 FOUND HEAVY CORRODED BRACKET ON RT WING IN KRUEGER FLAP AREA, FRAME 38-39. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 57-45-11. 2 L 7 2 4F RT A35EU 2007090600111 20070906 00111 EU 2007 9 6 07FDEA03291 1 20070831 A 5311 A5377537020000 FRAME AIRBUS 310 A310203 3930313 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 FRAME 38 CRACKED WHERE FRAME LEG ATTACHES TO FUSELAGE SKIN, BETWEEN STR 41L AND STR 42L. TRIMMED CRACKED FLANGE, FABRIC ATED AND INSTALLED REPAIR FALSE FLANGE IAW EA 6-5310-109195, FUSELAGE FRAME, FRAME 38 BETWEEN STRINGER 41 AND 42 CRACKED FLANGE, REPAIR. 2 L 7 2 4F RT A35EU 2007090600120 20070906 00120 EU 2007 9 6 07FDEA03299 1 20070901 A 5753 SKIN AIRBUS 300 A300F4605R 3930327 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 683FE 801 RT CTR FLAP UPPER SURFACE HAS 6 EA WEAR MARKS FROM CONTACT WITH NR 5 SPOILER IB SUPPORT ARM RIVETS. DEPTH RANGES FROM . 005 TO .009" DEEP. AREA FOUND TO BE OUT OF LIMITS IAW A300 SRM 57-50-00 FIG 101, SH 5. REPAIRED AREA IAW A300 SRM 57-5 0-00 PARA E, FIG 205. 2 L 7 2 4F RT A35EU 2007090600121 20070906 00121 NM 2007 9 6 07FDEA03300 1 20070901 A 5347 BAC1520792 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 SEAT TRACK FROM STA 560 - 572, LBL 24 - 25 CORRODED REMOVED CORRODED SEAT TRACK, MANUFACTURED NEW SEAT TRACK AND INSTALL ED REF SRM 51-30-02 FOR REMOVAL, AND SRM 5-30-02 FOR INSTALL. SEAT TRACK WAS REPLACED FROM STA 480 TO 689, LBL 24. THI S IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007090600122 20070906 00122 EU 2007 9 6 07FDEA03301 1 20070902 A 5313 A5397420228 STRINGER AIRBUS 310 A310203 3930313 EU AFT PIT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT PIT STRINGER 55L REQUIRES REPLACEMENT FROM FR 58 TO 63. STRINGER HAS HEAVY CORROSION REMOVED SHEAR TIES AT STATION 59, 60, 61. CUT OUT STRINGER 55L FROM FRAME 58 TO 63 IAW A310 SRM FIG 20. FABBED STRINGER AND COUPLINGS IAW A310 SRM 5 3-10-14 FIG 201. ALODINED PRIMED AND PAINTED REPAIR PARTS IAW A310 SRM 51-21-10 PARA 2, 51-23-10 PARA 3. PART MARKED A ND INSTALLED REPAIR PARTS IAW A310 SRM 51-40-21 PARA 6 AND 7. REINSTALLED SHEAR TIES AT STRINGER 55L IAW A31 SRM 51-40 -21 PARA 6 AND 7. 2 L 7 2 4F RT A35EU 2007090600125 20070906 00125 EU 2007 9 6 07FDEA03304 1 20070902 A 7830 FLANGE AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 683FE 801 A 1.5" AND A .5 INCH CRACK EXIST AT NR 2 ENGINE O/B T/R UPPER L/E FLANGE REF 78-31-00-6 REMOVED AND REPLACED NR 2 ENG O/ B T/R IAW A300-600 AMM 71-13-03-4-05 OPS CHECK GOOD IAW A300-600 AMM 71-03-4-05. 2 L 7 2 4F RT A35EU 2007090600126 20070906 00126 EU 2007 9 6 07FDEA03305 1 20070902 A 7830 BRACKET AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 683FE 801 A 3.5" INCH CRACK EXIST AT NR 2 ENGINE T/R I/B L/E UPPER POSITION LOCATED ON BRACKET SUPPORT FLANGE REF 78-31-00-6. REM OVED AND REPLACED NR 2 ENG I/B T/R IAW A300-600 AMM71-13-03-4-05, OPS CHECKED GOOD IAW A300-600 AMM 71-13-03-4-05. 2 L 7 2 4F RT A35EU 2007090600128 20070906 00128 EU 2007 9 6 07FDEA03309 1 20070903 A 5340 A53610996201 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 NUMEROUS FASTENERS WERE FOUND TO BE NON CONFORMING AND ELONGATED ON FITTING FRAME 12A, FRAME 12A AND CORNERS RT AND LT SIDES. REPAIR PERFORMED BY DETAILED VISUAL AND ROTO TEST INSPECTIONS IN DAMAGED HOLES, REPLACEMENT OF FITTING, CORNER SPLICE AND CORNER ANGLE WITH INSTALLATION OF NEW SPLICE UNDER STRG 26. INSTALLING REPAIR BUSHES IN FRAME 12A WEB RT SID E ONLY AND OVERSIZED FASTENERS IAW TD 942.043937/012/2006. APPROVED BY EA 6-5312-99226 AND RAS/AS/0047/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600141 20070906 00141 EU 2007 9 6 07FDEA03327 1 20070903 A 5320 A53981972200 COUPLING AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 727FD 579 THE COUPLING BETWEEN LT FWD AND AFT DORSAL FIN CONNECTING STRIPS IS CORRODED. REPLACEMENT OF LHS AREA CONNECT STRIPS CO UPL, C76, IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007090600149 20070906 00149 EU 2007 9 6 07FDEA03265 1 20070831 A 5311 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 CORROSION FOUND ON FWD FACE OF FRAME 92 ON SEVERAL ANGLES. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007090600151 20070906 00151 EU 2007 9 6 07FDEA03267 1 20070831 A 5315 A53778807202 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 TOP CAP BEAM FOUND WITH HEAVY CORROSION ON C27 RT CARGO FLOOR STRUCTURE. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 / FIG 207. 2 L 7 2 4F RT A35EU 2007090600159 20070906 00159 NM 2007 9 6 07FDEA03237 1 20070830 A 5730 SKIN DOUG MD11 MD11F 3023600 NM LT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 AFTER LEFT WING UPPER FUELTANK PANEL NR 531AT CUTOUT RUBSTRIP REMOVED. FOUND SKIN CUTOUT WITH 02 EACH DOUBLE HOLES. 09 -11-07 COMPLIED WITH FEDEX E.A. 1-5710-115177, CLASSIFIED AS A MINOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007090600160 20070906 00160 EU 2007 9 6 07FDEA03238 1 20070830 A 5330 A53812189201 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 EXTERNAL CORROSION ON SKIN PANEL RHS AT TWO PLACES BETWEEN FRAME 39-40, STRG 28-29 AND BETWEEN FRAME 39-40, STRG 27-28, BOTH PLACES OUT OF LIMIT. REPAIR PERFORMED BY INSTALLATION OF WEDGED SHIMS ON BOTH SIDES AS WELL AS ONE INTERNAL DOUBLE R AND TWO EXTERNAL DOUBLER AS PER DRW, R538-10623 AND R538-10603 AND TD 942-043210/011/2006 ISSUE: A. APPROVED BY EA 6-5 315-99185 AND RAS/AS/035/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600163 20070906 00163 NM 2007 9 6 07FDEA03241 1 20070830 A 5347 6520840 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 UPPER MAIN DECK FLOOR STRUCTURE, UPPER BEAM CAP HAS MULTIPLE DRILL HOLES UNDER REMOVED SEAT TRACK STA 1166, RBL 25. I NSTALLED TWO FREEZE PLUGS IN 1166 FLOORBEAM. PLUG TWO HOLES IN 1166 FLOORBEAM. DRILLED TWO HOLES IN 1166 FLOORBEAM. DRILLED TWO TO BLUE PRINT SIZE IN FREEZE PLUG. IN REF TO EA 7-5310-113070. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007090600169 20070906 00169 EU 2007 9 6 07FDEA03247 1 20070830 A 5315 A53974322238 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 CORROSION AT TOP CAP BEAM FRAME 66, Y600 LHS, CARGO COMP FLOOR STRUCTURE. SPLICE REPAIR PERFORMED IAW SRM 53-10-15/FIG 207. 2 L 7 2 4F RT A35EU 2007090600171 20070906 00171 EU 2007 9 6 07FDEA03249 1 20070830 A 5315 A53974268200 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 HEAVY CORROSION ON TOP CAP BEAM FRAME 56, BETWEEN Y805 TO Y1470. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 / FIG 207. 2 L 7 2 4F RT A35EU 2007090600174 20070906 00174 NM 2007 9 6 07FDEA03252 1 20070830 A 5753 SKIN BOEING 727 727233 138408A NM ZONE 500 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 LT WING, O/B FORE FLAP, HAS A DEEP GOUGE ON UPPER SKIN, APPROX 70" IN FROM I/B END AND 6 INCH LONG. REMOVED DAMAGE AND BONDED FILLER AND DOUBLER, REF 51-40-20 PARA'S 6, 7, 14, 15, 18, 20, 21, 22. PRIMED AND PAINTED REF MM 51-20-151-7, TH IS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007090600175 20070906 00175 EU 2007 9 6 07FDEA03253 1 20070830 A 5714 A57111092203 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 DAMAGE FOUND IN ALL LAYERS OF HOLE (APPEARED TO BE TOOL MARKS) INSIDE CENTER WING BOX, FRAME 47 LHS LOWER CORNER ANGLE F ITTING. REPAIR PERFORMED BY OVERSIZING HOLE AND INSTALLING FASTENER NSA5351-10 WITH TRANSITION FIT IAW EA 6-5710-9914 4 AND RAS/043285/014/2006. 2 L 7 2 4F RT A35EU 2007090600177 20070906 00177 EU 2007 9 6 07FDEA03329 1 20070903 A 5530 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU VERTICAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 UPPER HOIST POINT OF DORSAL FIN IS DAMAGED BY EROSION. SURFACE REPAIRED AS PER GUIDELINES OF SRM 51-77-11 PARA 3 A., US ING PASTE ADHESIVE AS PER SRM 51-77-10 PARA 5 B (1) IAW. EA 6-5318-92211 AND RAS/DAHAM/4020086/2005 ISS A. 2 L 7 2 4F RT A35EU 2007090600178 20070906 00178 WP 2007 9 6 07FDEA03330 1 20070903 A 5730 NRB6019 SKIN DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 RT WING UPPER SURFACE FOUND 1 CRACK REPAIR SKIN IAW SRM 57-10-00 VOL1 FIG 68 SHT 1, 2. 2 L 7 3 4F A22WE 2007090600179 20070906 00179 WP 2007 9 6 07FDEA03331 1 20070903 A 5321 FLOOR SKIN DOUG DC10 DC1010 3022110 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 FOUND SEVERE CORROSION ON 2 COCKPIT MEMBRANES 1 WEB REPAIRED IAW SRM 53-00-01 FIG 10 VOL 1. THE OTHER WEB IS WITHIN LIM ITS AFTER CORROSION REMOVAL IAW SRM 53-00-01 FIG1 VOL1:TREATED AREA IAW SRM 51-21-01. 2 L 7 3 4F A22WE 2007090600180 20070906 00180 EU 2007 9 6 07FDEA03332 1 20070904 A 5320 A53612214200 FLOOR SUPPORT AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 STRONG CORROSION ON LONGERON (CABIN FLOOR STRUCTURE) BETWEEN FRAME 11 AND 14, Y730 LHS. REPAIR PERFORMED BY INSTALLING PROFILES IAW SRM 53-12-15 / FIG 207. 2 L 7 2 4F RT A35EU 2007090600183 20070906 00183 WP 2007 9 6 07FDEA03335 1 20070904 A 5312 NCA624627 BULKHEAD DOUG DC10 DC1010F 3022111 WP ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 NLG W/W FOUND CRACK ON LT VERTICAL BULKHEAD. REPAIRED WEB IAW SRM 53-40-00 FIG 34 VOL I. 2 L 7 3 4F A22WE 2007090600186 20070906 00186 NM 2007 9 6 07FDEA03257 1 20070830 A 5315 6520827 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 262FE 21624 PREVIOUS REPAIR STA 720A, RBL 29-42, CORRODED ON UNDERSIDE FROM NO TREATING OR PRIMING REPAIR FLOORBEAM 720A, RBL 29-42 REF. FED EX DRAWING SR-53-034 REV F, SRM 53-10-1, 51-10-2 51-30-2. REMOVED AND REINSTALLED SEAT RAIL HARDWARE, RBL 24, STA 690 TO 720B AND STIFFENER RBL 24, STA 720A REF SRM 51-30-2, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007090600188 20070906 00188 NM 2007 9 6 DHL2007746512 1 20070807 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 720B CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 WHILE AT FLIGHTSTAR FOR A "C" CHECK, STRINGER 15L CRACKED AT BS 720B+15. STRIPPED PAINT FROM AREA IAW B727 MM 51-20-01, CUT OUT DAMAGE AREA DIM 13" IAW B727 SRM 53-10-03 FIG 1. AFTER NOT VERIFIED CRACK FAB STRINGER FROM BAC2798-143 7075-T 6 PO NR 7267138 DIM 14 3/8" BY 4" AND SPLICE FROM BAC1492-132 P0 NR 7268204 DIM 14 1/8" BY 4 IAW B727 SRM 53-10-03 FIG 1 . TREATED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-02. INSTALLED REPAIR PARTS IAW B727 SRM 53-10-03 FIG 1 AND 51-30- 02. 2 L 7 3 4F A3WE 2007090600190 20070906 00190 NM 2007 9 6 DHL2007746507 1 20070815 A 5330 SKIN BOEING 727 727224 1384076 NM BS 720D CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 DURING A "C" CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED: SURFACE CORROSION ON BS 720D STR 27R ON SKIN. CUT OUT DAMAG ED AREA ON SKIN AT STA 720D STR 27R IAW B727 SRM 53-30-3 FIG 3 4 3/4 BY 4". FABRICATED AND INSTALLED REPAIR DOUBLER IAW B727 SRM 53-30-3 FIG 3 MATERIAL USED DBIR .125 2024 T3 14.5 BY 12.5 PO NR 9005400, FILLERS .100 2024 T3 4" BY 1" .75 BY 2.0 PO NR 9005138 ALL PARTS AND AREA TREATED AND PRIMED IAW B727 SRM 51-10-2. 2 L 7 3 4F A3WE 2007090600195 20070906 00195 NM 2007 9 6 DHL2007746520 1 20070809 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 685 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 WHILE AT FLIGHTSTAR FOR A "C" CHECK, FWD CARGO COMPT, STA 685 STR SPLICE HAS CORROSION IN CENTER OF SPLICE STR 28LT. RE MOVED STRINGER SPLICE AT STR 28 LT STA 680 IAW B-727 SRM 51-30-2 FIG-1. FABRICATED NEW SPLICE FROM BAC 1498-131 7075T6, PO NR 7232174 DIM 12", IAW B-727 SRM 53-10-3, FIG-1 AND 53-10-2, FIG-9. TREATED AND PRIMED IAW:B-727, SRM, 51-10-2, ST RINGER SPLICE INSTALLED AT STR 28 RT, STA 680, IAW B-727 SRM 53-10-3, FIG-1. 2 L 7 3 4F A3WE 2007090600196 20070906 00196 SO 2007 9 6 C2XA07TY047 1 20070828 A 3397 CONNECTOR EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18120 145681 EMERGENCY ROW EXIT SIGN NOT ILLUMINATING ON AFT FACE. VERIFIED CONNECTIONS AND OPS CHECKED GOOD IAW EMB 145 AMM 33-50-1 5. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT 2007090600197 20070906 00197 EA 2007 9 6 TRAX200701249 1 20070827 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 THE 2ND FROM FRONT CEILING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007090600199 20070906 00199 EA 2007 9 6 TRAX200701252 1 20070829 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 920EV 7810 PAX DOOR BOTTOM STEP IS BROKEN. 2 L 7 2 4F RT A21EA 2007090700004 20070907 00004 NM 2007 9 7 SWAA074304 1 20070830 A 3213 654611644 CYLINDER BOEING 737 7373L9 1384470 NM LT MLG AXLE FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 LEFT MLG NR 1 AXLE INNER CYLINDER DAMAGED DUE TO NR 1 WHEEL BEARING FAILURE. REMOVED AND REPLACED INNER CYLINDER PER MM . 2 L 7 2 4F RT A16WE 2007090700008 20070907 00008 EA 2007 9 7 TRAX200701256 1 20070829 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 855AS 7395 ON PREFLIGHT INSPECTION F/A FOUND FLASHLIGHT ON F/A AREA DEAD. 2 L 7 2 4F RT A21EA 2007090700009 20070907 00009 EA 2007 9 7 TRAX200701257 1 20070830 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 971EV 7528 CAPTAIN'S FLASHLIGHT IS INOP. 2 L 7 2 4F RT A21EA 2007090700010 20070907 00010 EA 2007 9 7 TRAX200701258 1 20070830 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 977EV 7720 EMERGENCY LIGHTS FAIL TO ILLUMINATE DURING TEST OR WHEN SWITCHED ON. 2 L 7 2 4F RT A21EA 2007090700013 20070907 00013 EA 2007 9 7 TRAX200701261 1 20070830 A 3210 LANDING GEAR CNDAIR CL600 CL6002C10 1390015 EA MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 752EV 10166 GEAR WOULD NOT RETRACT WITH GEAR DOWN. ABNORMAL WIND NOISES COMING FROM NOSE GEAR AREA. A/C LANDED OVERWEIGHT AS PER F LT CONTROL AND MAINT. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007090700014 20070907 00014 SO 2007 9 7 C2XA07SH058 1 20070829 A 5751 14574000405 PANEL EMB 145 EMB145XR 3260214 SO AILERONS CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11106 145650 SHV - DURING C-CHECK MAINTENANCE FOUND RIGHT TOP AILERON SHROUD WITH CORROSION AT BONDING PLATES. MAINTENANCE REPAIRED RIGHT TOP AILERON SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007090700018 20070907 00018 SO 2007 9 7 C2XA07SH052 1 20070829 A 5310 14538924402 PANEL EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11106 145650 SHV - DURING C-CHECK MAINTENANCE FOUND PANEL 197CL HAS CORRODED BONDING PLATES. MAINTENANCE REPAIRED PANEL 197CL IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007090700019 20070907 00019 SO 2007 9 7 C2XA07SH059 1 20070829 A 5322 14525480603 SHEAR TIE EMB 145 EMB145XR 3260214 SO CARGO BAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11106 145650 SHV - DURING C-CHECK MAINTENANCE FOUND SHEAR CLIP AT FRAME 65 & CARGO DOOR CUTOUT LOWER BEAM WITH CORROSION. MAINTENANC E REPAIRED SHEAR CLIP AT FRAME 65 IAW EC 5330-01458 & REMOVED AND REPLACED CARGO DOOR CUTOUT SILL IAW EMB 145XR SRM 51-4 0-00. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007090700025 20070907 00025 NM 2007 9 7 2007UALA03379 1 20070824 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 FWD ENTRY DOOR UPPER HINGE CUTOUT ONE EACH FASTENER HOLE HAS CRACK INDICATION AT FWD END OF HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700026 20070907 00026 NM 2007 9 7 2007UALA03380 1 20070825 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN BODY FRAME CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 CABIN BODY FRAME INTERCOSTAL OUTBOARD CHORD IS CRACKED BS 301 STR 13L. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALL ED INTERCOSTAL & RELATED PARTS PER AAR EA-I070550 ON NR12432-2500-0014. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700027 20070907 00027 NM 2007 9 7 2007UALA03381 1 20070825 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN BODY FRAME CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 CABIN BODY FRAME INTERCOSTAL OUTBOARD CHORD IS CRACKED BS 301.1 INCH ABOVE STR 10L. MAJOR REPAIR ACCOMPLISHED: FABRICA TED & INSTALLED REPLACEMENT INTERCOSTAL & REPLACED PARTS PER AAR EA-I070596. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700029 20070907 00029 NM 2007 9 7 2007UALA03383 1 20070825 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 942 S24L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 EXTERNAL FUSELAGE SKIN HAS A CRACK JUST FORWARD OF POTABLE WATER SERVICE PANEL BS 942 STR 24L. MAJOR REPAIR ACCOMPLISHE D: FABRICATED & INSTALLED EXTERNAL FUSELAGE DOUBLER & INTERNAL TEAR STRAP DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700031 20070907 00031 2007 9 7 2007UALA03385 4 20070825 A 2565 LATCH BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU SLIDE UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 AFT ENTRY DOOR EVACUATION SLIDE LATCH CHAIN ASSEMBLY UNHOOKED. RESECURED LATCH/CHAIN. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700033 20070907 00033 NM 2007 9 7 2007UALA03387 1 20070826 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 727A S20R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 AFT PIT, STRINGER CLIP HAS DEEP TOOLING MARK, CRACKED BS 727A STR 20R. REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700034 20070907 00034 NM 2007 9 7 2007UALA03388 1 20070825 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 279 S5L GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 APPROX F-STATION 279.5 STR 5L AND 6L FUSELAGE SKIN EXTERNAL DEEP GOUGES EXIST. MAJOR REPAIR ACCOMPLISHED PER SRM 53-00 -01. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700037 20070907 00037 NM 2007 9 7 2007UALA03391 1 20070826 A 5512 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZONTAL STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 315UA 23947 RIGHT HORIZONTAL STABILIZER HAS DENT IN LEADING EDGE AT APPROX STA 176, 14 FT OUTBOARD OF FUSELAGE. REPAIRED DENT, PER FORMED EDDY CURRENT - NO CRACKS PRESENT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700038 20070907 00038 2007 9 7 2007UALA03392 4 20070826 A 2565 SLEEVE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU GIRT BAR TORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 FWD ENTRY DOOR EVAC SLIDE GIRT BAR NYLON SLEEVE TORN. REMOVED & REPLACED SLIDE ASSEMBLY. REMOVED SAFETY PIN FROM BOTT LE AND STOWED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700039 20070907 00039 2007 9 7 2007UALA03393 4 20070826 A 2565 GIRT BAR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT GALLEY DOOR FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 335UA 24230 AFT GALLEY DOOR EVAC SLIDE GIRT BAR HANGING DOWN TOO FAR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700042 20070907 00042 NM 2007 9 7 2007UALA03396 1 20070826 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 340 S23R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 STA 340 STRINGER 23R IS DAMAGED. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007090700043 20070907 00043 NM 2007 9 7 2007UALA03397 1 20070823 A 5420 SKATE ANGLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 NACELLE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 NR 1 PYLON AFT SKATE ANGLE CRACKED OUT OF OUTBOARD ATTACH FASTENER AFT OF AFT ENG MOUNT. MAJOR REPAIR ACCOMPLISHED: FA BRICATED & INSTALLED NEW SKATE ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007090700044 20070907 00044 NM 2007 9 7 2007UALA03398 1 20070824 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 L-2 DOOR INSTALL REPAIR DOUBLER AT UPPER HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007090700046 20070907 00046 NM 2007 9 7 2007UALA03400 1 20070825 A 3210 LANDING GEAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MALFUNCTIONED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 564UA 26666 GEAR DOWN AND LANDING GEAR ALTN EXTEND C/B (F5) ON P6 PANEL TRIPPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007090700047 20070907 00047 NM 2007 9 7 2007UALA03401 1 20070826 A 2420 GENERATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU FAULTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 APU GENERATOR FAULTY & RT BUSS DROPPING OFF. 2 L 7 2 4F 4 F RT A2NM E17NE 2007090700048 20070907 00048 EU 2007 9 7 2007UALA03402 1 20070827 A 2750 FLAP SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE TE FLAPS MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 440UA 702 RTFL DUE TO FLAPS LOCKED INDICATION. 2 L 7 2 4F 4 F RT A28NM E40NE 2007090700050 20070907 00050 2007 9 7 2007UALA03404 4 20070824 A 2565 PIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ESCAPE SLIDE UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 415UA 475 LEFT OVERWING ESCAPE SLIDE SHOWS NOT ARMED ON ECAM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007090700053 20070907 00053 EA 2007 9 7 TRAX200701268 1 20070831 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 972EV 7534 F/A REPORTS SERVICE DOOR HARD TO OPERATE. 2 L 7 2 4F RT A21EA 2007090700054 20070907 00054 NM 2007 9 7 KCSA071328 1 20070831 A 5310 DOOR FRAME BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 MAIN DECK DOOR R-1 HAS STOP DRILL ON VERTICAL CHORD LOCATED AT FWD LOWER CORNER FROM PREVIOUS REPAIR THAT HAS .25 INCH L ONG CRACK PAST STOP DRILL HOLE. 2 L 7 4 4F RT A20WE 2007090700055 20070907 00055 NM 2007 9 7 KPVA200713 1 20070831 A 2120 UNKNOWN DHAV DHC8 DHC8103 1386005 NM CABIN ODOR A KPVA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 13 809WP 146 (PIREP) FLIGHT ATTENDANT REPORTED BURNING ODOR IN CABIN AFTER LANDING. (MX) INSPECTED FOR BURNING ODOR IN CABIN, LAV CO MPARTMENTS. NO SMELL NOTED. 2 H 7 2 4T RT A13NM 2007090700057 20070907 00057 SO 2007 9 7 C2XA07IA186 1 20070827 A 3222 2233A000001 LEG ASSY EMB 145 EMB145XR 3260214 SO NLG UNDERSERVICED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14148 11548 11548 145751 IAH - FLIGHT 3095, THE CREW REPORTED AN AIR/GROUND FAILURE DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED W ITHOUT INCIDENT. MAINTENANCE SERVICED THE NLG STRUT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007090700059 20070907 00059 NM 2007 9 7 2007UALA03501 1 20070831 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SEAT 1E BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 222UA 30553 SEAT 1E HAS ONE EEL LIGHT BROKEN. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007090700060 20070907 00060 NM 2007 9 7 2007UALA03502 1 20070828 A 3246 WHEEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NLG VIBRATES A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 568UA 26674 NOSE WHEEL VIBRATES AT GEAR RETRACTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007090700066 20070907 00066 NM 2007 9 7 2007UALA03161 1 20070811 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 DOOR 5 RIGHT FWD SILL EMERGENCY LIGHT IS INOP. *S/D* RELAMPED DOOR 5L EEL. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700069 20070907 00069 NM 2007 9 7 2007UALA03181 1 20070814 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 DOOR 2R SILL FWD EMERGENCY LIGHT IS INOPERATIVE. *S/D* RELAMPED EMERGENCY LIGHT, OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700070 20070907 00070 NM 2007 9 7 2007UALA03182 1 20070814 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 UPPER DECK CEILING 2 EACH EMERGENCY LIGHT IS INOP. *S/D* RELAMPED BOTH LIGHTS. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700071 20070907 00071 NM 2007 9 7 2007UALA03183 1 20070815 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHT ROW 4A INOPERATIVE. *S/D* RESECURED EMERGENCY LIGHT CONNECTION. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700072 20070907 00072 NM 2007 9 7 2007UALA03184 1 20070815 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHT ROWS 40 ABC, 59 CB & 61 RIGHT ARE INOPERATIVE. *S/D* RESECURED EMERGENCY LIGHTS IN ALL THREE POSITIONS . ALL EEL OP CHECK NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700074 20070907 00074 SO 2007 9 7 C2XA07SH056 1 20070829 A 5751 14573900411 PANEL EMB 145 EMB145XR 3260214 SO AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11106 145650 SHV - DURING C-CHECK MAINTENANCE FOUND RIGHT LOWER AILERON SHROUD WITH CORROSION AT BONDING PLATES. MAINTENANCE REPAIRE D RIGHT LOWER AILERON SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007090700077 20070907 00077 NM 2007 9 7 2007UALA03188 1 20070815 A 3350 276005 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 OVERWING EMERGENCY LIGHT LEFT 1ST & 2ND LIGHT INOP. *S/D* REPLACED FUSE ON BATTERY CHARGER. OP CHECK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700078 20070907 00078 NM 2007 9 7 2007UALA03197 1 20070816 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY LIGHT INOP: DOORS 1L & 5R SLIDE ILLUM. *S/D* REPLACED LAMP, OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700081 20070907 00081 NM 2007 9 7 2007UALA03200 1 20070816 A 3350 78671 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 SEAT EEL INOP: ROWS 55LT & 59LT. *S/D* REPLACED LAMPS IN BOTH SEAT POSITIONS. OP CHECKS READY FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700090 20070907 00090 NM 2007 9 7 SWAA074238 1 20070828 A 3260 121909018 LOGIC CARD BOEING 737 7375H4 138449D NM NLG INDICATOR FAULTY A SWAA O OTHER N FALSE WARNING CR CRUISE 1 SW 29 509SW 24186 THIRTY MINUTES PRIOR TO DESCENT NLG RED LIGHT ILLUMINATED. WHEN GEAR HANDLE SELECTED TO DOWN POSITION NLG INDICATED UNS AFE. CYCLED GEAR TWICE BEFORE SAFE INDICATION. REMOVED AND REPLACED NLG M983 LOGIC CARD PER MM. 2 L 7 2 4F RT A16WE 2007090700091 20070907 00091 NM 2007 9 7 SWAA074263 1 20070828 A 5315 147A5505 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 736SA 27868 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 11 TO RBL 10. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007090700093 20070907 00093 NM 2007 9 7 SWAA074237 1 20070828 A 3350 417N521331SP LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 489WN 33855 EEPLS LIGHT STRIP LOOSE AT ROW 1 ABC. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007090700094 20070907 00094 NM 2007 9 7 SWAA074252 1 20070828 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM BS 188 S17-17LR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L AND STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007090700095 20070907 00095 NM 2007 9 7 SWAA074240 1 20070828 A 5330 6545774 SKIN BOEING 737 737317 138447P NM BS 787 S18R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787 STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007090700096 20070907 00096 NM 2007 9 7 SWAA074253 1 20070828 A 5315 6545833 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 194 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 194, STR 17R AND STR 17L. REPAIRED FLOORBEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2007090700097 20070907 00097 NM 2007 9 7 SWAA074261 1 20070828 A 5753 6546435 SKIN BOEING 737 737317 138447P NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND LEFT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007090700098 20070907 00098 NM 2007 9 7 SWAA074241 1 20070828 A 5753 6546486156 SKIN BOEING 737 737317 138447P NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING INBOARD MID FLAP DELAMINATED. REMOVED AND REPLACED MID FLAP PER MM. 2 L 7 2 4F RT A16WE 2007090700099 20070907 00099 NM 2007 9 7 SWAA074257 1 20070828 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007090700100 20070907 00100 NM 2007 9 7 SWAA074245 1 20070828 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007090700101 20070907 00101 NM 2007 9 7 SWAA074251 1 20070828 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM BS 520 S8-8LR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007090700102 20070907 00102 NM 2007 9 7 SWAA074248 1 20070828 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM BS 559 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007090700103 20070907 00103 NM 2007 9 7 SWAA074262 1 20070828 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 767 S25R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 25R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007090700105 20070907 00105 NM 2007 9 7 2007UALA03411 1 20070826 A 2730 COMPUTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ELEVATOR FEEL MALFUNCTIONED A UALA O OTHER O OTHER AP APPROACH 1 WP 29 576UA 26690 CREW REPORTS ON APPROACH AT APPROX 20 FT EXCESSIVE FORCE REQUIRED TO FLAIR ELEVATOR. REQUIRED THREE TIMES THE FORCE THA N NORMAL. ACCOMPLISHED ELEVATOR FEEL SYSTEM FORCE TEST AND FOUND FEEL COMPUTER LEAKING AND FORCES NOTICEABLY DIFFE RENT WITH LEFT AND RIGHT SYSTEM PRESSURIZED. REMOVED AND REPLACED THE ELEVATOR FEEL COMPUTER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007090700106 20070907 00106 NM 2007 9 7 2007UALA03412 1 20070824 A 3510 OXYGEN MASK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 CAPTAIN'S OXYGEN MASK HEAD STRAPS LEAKS AIR WHEN INFLATED. REPLACED MASK PER MM 35-11 -51.CKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007090700107 20070907 00107 NM 2007 9 7 2007UALA03413 1 20070824 A 3350 767 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 552UA 26641 EXTERIOR EMERGENCY EXIT LIGHT AT DOOR 4R INOPERATIVE. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007090700109 20070907 00109 NM 2007 9 7 2007UALA03415 1 20070826 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 661UA 27158 EEL STRIP CROSS AISLE AT 1R INOP. FIRST EEL STRIP AFT OF 1R INOP. FOUND PINS BROKEN OFF AT CONNECTION. NEEDS NEW EEL S TRIP, OR SPLICE IN NEW PLUG. INSTALLED NEW EEL STRIP AT 1R, OPS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007090700110 20070907 00110 NM 2007 9 7 2007UALA03416 1 20070827 A 2497 WIRE HARNESS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT IDG DAMAGED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 544UA 25322 RTFL DUE TO LEFT GENERATOR DISCONNECTION. ACCOMPLISHED TROUBLESHOOTING OF EICAS MESSAGE DISPLAY AND GENERATOR DRIVE L IGHT ILLUMUNATION. DISCONNECTED GENERATOR DRIVE. REPLACED AND SERVICED IDG. FOUND BACK SIDE WIRE HARNESS ELECTRICAL PLUG FOR LT IDG CAME APART. REPLACED D5132 CONNECTOR FOR LT ENGINE IDG. 2 L 7 2 4F 4 F RT A2NM E17NE 2007090700116 20070907 00116 NM 2007 9 7 2007UALA03422 1 20070826 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 EMERGENCY EXIT EEL LIGHTS INOP AT SEATS 3J AFT & 5E AFT. REPLACED LAMPS IN EEL FOR BOTH SEAT POSITIONS. BOTH CHECK OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700118 20070907 00118 EA 2007 9 7 TRAX200701262 1 20070829 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 PAX DOOR INNER HANDLE CRACKED. NEW PAX DOOR INNER HANDLE INSTALL IAW SRM 51-41-04. 2 L 7 2 4F RT A21EA 2007090700119 20070907 00119 EA 2007 9 7 TRAX200701263 1 20070829 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 599 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 CORROSION FOUND ON LEFT FLOOR SILL BETWEEN FS 599 + 80 AND FS 559 + 112 RBL 45. REMOVED CORROSION AS PER IAW SRM 51-21-0 6 APLY FINISH CODE AS PER IAW SRM 51-21-16 MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.002 WITHIN LIMITS AS PER S RM: 53-00-00 2 L 7 2 4F RT A21EA 2007090700125 20070907 00125 NM 2007 9 7 2007UALA03425 1 20070826 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 32ABC INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 32 ABC. REPLACED LIGHT ASSY. OPERATES NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700126 20070907 00126 NM 2007 9 7 2007UALA03426 1 20070826 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 EMERGENCY EXIT EEL LIGHT INOP AT DOOR 4 LEFT, BOTH LOWER WALL AISLE AND LOWER WALL CROSS AISLE. FOUND LOOSE CONNECTION. SECURED CONNECTOR. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700131 20070907 00131 NM 2007 9 7 2007UALA03431 1 20070827 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY LIGHT ROW 33 LEFT INOP. RESECURED EMERGENCY LIGHT CONNECTION. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700134 20070907 00134 EU 2007 9 7 2007UALA03434 1 20070827 A 3250 CONTROL SERVO AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG STEERING FAULTED A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 426UA 510 AIRCRAFT PULLS TO THE RIGHT WHILE TAXIING. FOUND NOSE WHEEL STEERING CONTROL FAULTY. REPLACED NOSE WHEEL STEERING C ONTROL SERVO 2 L 7 2 4F 4 F RT A28NM E40NE 2007090700135 20070907 00135 NM 2007 9 7 2007UALA03435 1 20070827 A 3510 B-NUT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CREW OXYGEN SYS LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 306UA 23667 CREW COMMENTS: CREW OXYGEN PSI DROPPED FROM 1900 TO 1600 PSI IN 2 HOURS. LEAKING O2 AT B-NUT. TIGHTENED B-NUT, REPLA CED COCKPIT GAUGE AND RESTOWED ALL THREE MASKS PROPERLY. NO REPEATS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700136 20070907 00136 NM 2007 9 7 2007UALA03436 1 20070827 A 3350 BR9279318 SIGN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 848UA 1647 EMERGENCY EXIT SIGN JUST FWD OF DOOR 1R BROKEN UNSECURE. REPLACED LIGHT ASSY. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007090700137 20070907 00137 NM 2007 9 7 SWAA074258 1 20070828 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM BS 747 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007090700138 20070907 00138 EU 2007 9 7 2007UALA03437 1 20070827 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 429UA 539 FOUND UPON ARRIVAL LEFT FUSELAGE SKIN WAS DENTED AND GOUGED AT FRAME 14 APPROX 10 INCHES BELOW FLOOR LINE AND APPROX 18 INCHES FWD OF DOOR 1LT. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007090700141 20070907 00141 2007 9 7 2007UALA03440 4 20070827 A 2565 D30656126 ASPIRATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR SLIDE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 588UA 26717 DOOR SLIDE HAS A DAMAGED ASPIRATOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007090700142 20070907 00142 NM 2007 9 7 2007UALA03441 1 20070828 A 3350 LAMP AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE RT FWD OVERWING BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 829UA 1211 RIGHT FWD OVERWING LIGHT INOPERATIVE. FOUND LAMP BURNED OUT. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007090700145 20070907 00145 NM 2007 9 7 2007UALA03444 1 20070828 A 5743 SUPPORT FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RT MLG CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 RIGHT MLG AFT SUPPORT BEAM FITTING IS CRACKED AT THE 12:00 AT THE 3:00 AND AT THE 6:00 O'CLOCK POSITIONS AT THE REAR SPA R ATTACHMENT. MAJOR REPAIR ACCOMPLISHED: REPLACED RIGHT MLG SUPPORT FITTING. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700146 20070907 00146 NM 2007 9 7 2007UALA03445 1 20070828 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 639 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 LONGITUDINAL FLOORBEAM CRACKED AT BS 639R RBL 45-47, MID CABIN AREA. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED SEC TION OF LONGITUDINAL FLOORBEAM FROM BS 540 TO BS 727B AT RBL 45. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700148 20070907 00148 NM 2007 9 7 2007UALA03447 1 20070828 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1485 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 AFT PIT CORROSION ON FLOORBEAM AT STA 1485, RBL 9. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION & REMAINING MATERIAL O UT OF LIMITS. FABRICATED & INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007090700149 20070907 00149 NM 2007 9 7 2007UALA03448 1 20070828 A 5101 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1682 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 STA 1682 RIGHT SIDE AT FLOOR LEVEL IS DAMAGED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED & INSTALLED A NE W REPAIR ANGLE & STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007090700153 20070907 00153 NM 2007 9 7 SWAA074255 1 20070828 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787 S8L AND S8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007090700154 20070907 00154 NM 2007 9 7 SWAA074360 1 20070904 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 727C S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007090700155 20070907 00155 NM 2007 9 7 SWAA074303 1 20070830 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007090700156 20070907 00156 NM 2007 9 7 SWAA074296 1 20070830 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S14R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 14R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007091000001 20070910 00001 NM 2007 9 10 SWAA074301 1 20070830 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 727B CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091000002 20070910 00002 NM 2007 9 10 SWAA074300 1 20070830 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091000003 20070910 00003 NM 2007 9 10 SWAA074299 1 20070830 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 727C S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091000004 20070910 00004 NM 2007 9 10 SWAA074295 1 20070830 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500A S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007091000006 20070910 00006 NM 2007 9 10 SWAA074359 1 20070904 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 907 S2R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091000009 20070910 00009 NM 2007 9 10 SWAA074317 1 20070831 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 770 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 737JW 27869 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 770, LBL 3 AND RBL 7.5. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007091000011 20070910 00011 2007 9 10 SWAA074315 4 20070831 A 2565 D31354 SLIDE BOEING 737 7373L9 1384470 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007091000012 20070910 00012 2007 9 10 SWAA074354 4 20070901 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007091000014 20070910 00014 NM 2007 9 10 SWAA074294 1 20070830 A 3233 65C310992 ACTUATOR BOEING 737 7373H4 1384600 NM MLG FAULTY A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 302SW 22942 AIR TURNBACK. CLIMBING OUT OF TUS WITH LANDING GEAR HANDLE IN UP POSITION NLG UNSAFE LIGHT ILLUMINATED. CYCLED GEAR SE VERAL TIMES THEN GOT THREE GREEN LIGHTS. REMOVED AND REPLACED NLG RETRACT ACTUATOR AND FUSE PER MM. 2 L 7 2 4F RT A16WE 2007091000016 20070910 00016 NM 2007 9 10 SWAA074292 1 20070830 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 251WN 32510 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP BETWEEN ROW 18 ABC AND ROW 20 ABC. REMOVED AND REPLACED BATTERY PACK PER M M. 2 L 7 2 4F RT A16WE 2007091000019 20070910 00019 NM 2007 9 10 SWAA074412 1 20070905 A 5315 147A5558 FLOOR SUPPORT BOEING 737 7377H4 1384404 NM BS 1010-1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 737JW 27869 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM WEB CRACKED BETWEEN BS 1010 AND BS 1016, RBL 37. REMOVED AND REPLACED FLOORB EAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2007090600060 20070906 00060 CE 2007 9 6 AMWA25032 1 20070822 A 5711 11810001953 SPAR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT WING DAMAGED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 159YV UE159 RT MAIN SPAR FASTENERS NEAR BL 114.250 AND WS 124.588 HAD (2) OVERSIZED FASTENERS. REPAIRED IAW REPAIR DRAWING 1900UE 159-1 REV 1R, DATED AUGUST 14, 2007. 2 L 7 2 4T 4 T RT A24CE E26NE 2007090600063 20070906 00063 CE 2007 9 6 AMWA25033A 1 20070822 A 5311 1294300311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 213 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 159YV UE159 FUSELAGE FRAME HAD FRICTION CHAFING. REPAIRED IAW ENGINEERING REPORT 6829-1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007090600064 20070906 00064 CE 2007 9 6 AMWA25033C 1 20070822 A 5311 12943003719 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FS 303 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 159YV UE159 FUSELAGE FRAME HAD FRICTION CHAFING. REPAIRED IAW ENGINEERING REPORT 6829-1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007090600083 20070906 00083 NM 2007 9 6 TIPR200736006 1 20070806 A 5330 SKIN BOEING 767 767222 1385122 NM PWA JT9 JT9D* NE BS 1540 S39R CORRODED B K NONE O OTHER IN INSP/MAINT 1 SO 05 609UA 21870 AFT PIT STA 1540 HAS CORROSION UNDER STRINGER 39R. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-00-01 FIG 201 . REFERENCE SERVICE ORDER-599125 OPERATION 26209. 2 L 7 2 4F 4 F RT A1NM E20EA 2007090600084 20070906 00084 EU 2007 9 6 2007F00049 1 20070810 A 7922 727029 BYPASS VALVE STWARNER AGUSTA A109 A119 0261102 EU PWA PT6 PT6* 52043 EA OIL COOLER MALFUNCTIONED D A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 11 911AM 1221 176 14054 0069 ON A FLIGHT, AC EXPERIENCED AN ENGINE OIL HOT LIGHT, THE EMERGENCY PROCEDURE IN THE AFM IS TO LAND AS SOON AS POSSIBLE. THE AIRCRAFT WAS LANDED IN A FIELD WITHOUT INCIDENT. FAA POI, WAS NOTIFIED. UPON INVESTIGATION IT WAS DETERMINED THA T THE OIL COOLER BYPASS VALVE HAD FAILED AND THE OIL WAS BYPASSING THE OIL COOLER. THE AIRCRAFTS IDS SYSTEM NOTED THAT THE OIL TEMP REACHED 117C (115C LIMIT). THE VALVE ,P/N 727029 WAS REPLACED, AN AIRWORTHINESS CHECK PERFORMED, THE AIRC RAFT WAS LEAK CHECKED AND A POWER ASSURANCE CHECK WAS PERFORMED. AIRCRAFT WAS FLOWN WITHOUT INCIDENT. 1 G 7 2 3U 3 T H7EU E2NE 2007090600091 20070906 00091 EU 2007 9 6 07FDEA03270 1 20070831 A 5720 A57140202 PLATE AIRBUS 300 A300B4622R 3930312 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 DAMAGED CORNER SECTION AT LT PYLON AFT MOUNT FITTING REPAIR PERFORMED BY BLEND OUT TO SMOOTH PROFILE AND NDT INSPECTION FOR CRACK FREE IAW EA 6-5720-99222 AND RAS/BAE/1002436/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600100 20070906 00100 EU 2007 9 6 07FDEA03280 1 20070831 A 5710 A53510216203 BEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 FOUND HEAVY CORRODED BEAM ON RT WING IN KRUEGER FLAP AREA, FRAME 38-39. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 57-45-11. 2 L 7 2 4F RT A35EU 2007090600101 20070906 00101 EU 2007 9 6 07FDEA03281 1 20070831 A 5320 A53810966200 DIAPHRAGM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 TOOLING MARKS AT GANTRY DIAPHRAGM BETWEEN FRAME 51-52 NEAR BEAM 5 RT. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5315-99148 AND RAS 043415/014/2006. 2 L 7 2 4F RT A35EU 2007090600103 20070906 00103 EU 2007 9 6 07FDEA03283 1 20070831 A 5311 A53831217200 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 MISDRILLED HOLE IN AFT FITTING FRAME 47 LT, STRG 24 NEAR HOLE G OF SB 53-61-23. REPAIR PERFORMED BY SPOTFACING THE MISDR ILLED HOLE, OVERSIZING HOLE G AND INSTALLING FASTENER NSA5357-4 IAW EA 6-5315-99153 AND RAS 0453451/012/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600115 20070906 00115 EU 2007 9 6 07FDEA03295 1 20070831 A 5712 A57240880000 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 FOUND AT ALL SPEED AILERON HINGE RIBS LT/RT DEEP CHAFING MARKS, ON THE INTERMEDIATE RIB 6A POSITIONS ON BOTH WINGS. R EPAIR PERFORMED BY BLENDING AND REPROTECTION AT POSITIONS RIB 6A AS PER TD/J1/S1/0234/2006 ISSUE B APPROVED BY EA 6-5751 -99137 AND RAS/BAE/1002354/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600127 20070906 00127 NM 2007 9 6 07FDEA03308 1 20070902 A 7330 INDICATOR BOEING 727 7272S2F 1384O81 NM FUEL INDICATOR SHORTED A FDEA J DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 25 210FE 22932 DURING CLIMB-OUT OF FL220, NR 2 FUEL ICING LIGHT CAME ON. RAN QRH PROCEDURE, FUEL TEMP WAS 40 DEGREES, RETURNED TO MEMP HIS, DUMPED FUEL AND FUEL ICING LIGHT REMAINED ON THROUGH LANDING, WENT OUT WHILE WAITING TO PARK. FOUND BULB ASSY BENT CAUSING BULB TO SHORT OUT AND COME ON WHEN VIBRATION OCCURRED. RELAMPED WITH NEW BULB PER 727-200 MM SHAKING LIGHT A SSY BEFORE RELAMPING, LIGHT STAYED ON. LIGHT TEST GOOD, NR 2 FUEL HEAT VALVE OPS CHECK GOOD. ALL INDICATIONS FOR FUEL HEAT VALVES OPS CHECK. 2 L 7 3 4F A3WE 2007090600132 20070906 00132 EU 2007 9 6 07FDEA03313 1 20070903 A 5311 A53610319 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 NUMEROUS FASTENERS WERE FOUND TO BE NON CONFORMING AND ELONGATED ON FITTING FRAME 12A, FRAME 12A AND CORNERS RT AND LT SIDES. REPAIR PERFORMED BY DETAILED VISUAL AND ROTO TEST INSPECTIONS IN DAMAGED HOLES. REPLACMENT OF FITTING, CORNER SPLICE AND CORNER ANGLE WITH INSTALLATION OF NEW SPLICE UNDER STRG 26. INSTALLING REPAIR BUSHES IN FRAME 12A WEB RT SID E ONLY AND OVERSIZED FASTENERS IAW TD 942.043937/012/2006. APPROVED BY EA 6-5312-99226 AND RAS/AS/0047/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600136 20070906 00136 EU 2007 9 6 07FDEA03320 1 20070903 A 5340 A53974321000 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 HEAVY CORROSION AT ASSY FITTING FRAME 63, STRG 45 LHS. REPLACEMENT OF FITTING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007090600148 20070906 00148 EU 2007 9 6 07FDEA03264 1 20070831 A 5311 A53989317206 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 CORROSION FOUND ON FWD FACE OF FRAME 92 ON T-SECTION. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007090600153 20070906 00153 EU 2007 9 6 07FDEA03269 1 20070831 A 5410 A57140202 PLATE AIRBUS 300 A300B4622R 3930312 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 DAMAGED CORNER SECTION AT RT PYLON AFT MOUNT FITTING REPAIR PERFORMED BY BLEND OUT TO SMOOTH PROFILE AND NDT INSPECTION FOR CRACK FREE IAW EA 6-5720-99222 AND RAS/BAE/1002436/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600155 20070906 00155 WP 2007 9 6 07FDEA03230 1 20070829 A 5730 ARB09372 SKIN DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 RT WING LWR SURFACE FOUND 1 CRACK 2" LONG ON SKIN. REPAIRED CRACK IAW SRM 57-10-00 FIG 68 SHT 1 VOL 1. 2 L 7 3 4F A22WE 2007090600164 20070906 00164 EU 2007 9 6 07FDEA03242 1 20070830 A 5313 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 CORRODED STRINGER COUPLING BETWEEN FRAME 74-75, STRG 30 RHS. REPAIR PERFORMED BY REPLACEMENT OF CONNECTING SECTION IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007090600172 20070906 00172 EU 2007 9 6 07FDEA03250 1 20070830 A 5315 A53974268200 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 HEAVY CORROSION ON TOP CAP BEAM FRAME 56, BETWEEN Y805 TO Y1470. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 / FIG 207. 2 L 7 2 4F RT A35EU 2007090600184 20070906 00184 NM 2007 9 6 07FDEA03255 1 20070830 A 5522 6572795 SKIN BOEING 727 727233 138408A NM RT ELEVATOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 RT HORIZONTAL STAB ELEVATOR, OB MOST UPPER SURFACE STATIC WICK. CORROSION ON SKIN SURFACE, AROUND AND UNDER STATIC WICK BASE, AND ON WICK BASE ALSO REMOVED CORROSION ON UPPER RT OUTBOARD ELEVATOR STATIC WICK, FOUND TO BE OUT OF LIMITS BY N DT. MATERIAL LOSS OF .008". REPAIRED AREA IN REF TO SRM 55-20-3 PG 2-3, SRM 55-20-1 DETAIL 1, MM 23-61-00-6 PG 1, MM 51-20-151-7 PG 1-3. THIS IS CLASSIFIED MINOR REPAIR, LEVEL 1 CORROSION. 2 L 7 3 4F RT A3WE 2007090600193 20070906 00193 NM 2007 9 6 DHL2007746517 1 20070809 A 5311 FRAME BOEING 727 727224 1384076 NM BS 520 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 WHILE AT FLIGHTSTAR FOR A "C" CHECK, DENT ON FUSELAGE FRAME BS 520 ABOVE STR 17R. CUT OUT DAMAGE AREA DIM 1" BY 1" IAW B727 SRM 51-40-03 FIG 1. FAB DOUBLER ANGLE. REPAIR FROM 7075-T6 .050 PO NR 9003230 DIM 9" BY 4" IAW B727 SRM 51-40-03 FIG 1. LOCATED DRILL IAW B727 SRM 51-30-05. TREATED AND PRIMED IAW B727 SRM 51-10-02. INSTALLED DOUBLER ANGLE REPAIR IAW B727 51-30-02 AND 51-40-03. 2 L 7 3 4F A3WE 2007090600198 20070906 00198 EA 2007 9 6 TRAX200701251 1 20070828 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 851AS 7360 LEFT AFT EXTERIOR EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007090700001 20070907 00001 NM 2007 9 7 SWAA074297 1 20070830 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 430WN 33659 EEPLS COVER MISSING AT ROW 5 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007090700006 20070907 00006 EA 2007 9 7 TRAX200701254 1 20070829 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 PRESSURE FLOOR FS 484.00 RIGHT BOTH ANGLE OF INTERCOSTAL FOUND CRACKED. REPAIRED AS PER REO 601R-53-41-059-REV-A 2 L 7 2 4F RT A21EA 2007090700015 20070907 00015 SO 2007 9 7 C2XA07SH055 1 20070829 A 5310 14552235401 PANEL EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11106 145650 SHV - DURING C-CHECK MAINTENANCE FOUND PANEL 193 AAB WITH BAD BONDING PLATES. MAINTENANCE REPAIRED PANEL 193 AAB IAW EM B 145 EC 5750-01315. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007090700020 20070907 00020 SO 2007 9 7 C2XA07SH057 1 20070829 A 5751 14574000405 PANEL EMB 145 EMB145XR 3260214 SO LT AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11106 145650 SHV - DURING C-CHECK MAINTENANCE FOUND LT AILERON UPPER SHROUD WITH CORRODED BONDING PLATES. MAINTENANCE REPAIRED LEFT AILERON UPPER SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007090700021 20070907 00021 NM 2007 9 7 2007UALA03375 1 20070823 A 2410 CSD BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 2 OVERSERVICED A UALA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION LD LANDING 1 WP 29 302UA 23643 723255 CREW REPORT: AFTER LANDING NR 2 HI OIL TEMP CSD LIGHT CAME ON. ENG SHUT DOWN AND LIGHT WENT OUT AFTER 5 MINUTES. FOU ND OVERSERVICE OF CSD. DRAINED CSD OIL AND RESERVICED TO PROPER LEVEL. PERFORMED ENGINE RUNS WITH DEFECTS OR ABNORMAL ITIES NOTED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700023 20070907 00023 EU 2007 9 7 2007UALA03377 1 20070827 A 2130 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN PRESSURE UNKNOWN A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 434UA 592 RTFL DUE TO PROBLEM WITH PRESSURIZATION. 2 L 7 2 4F 4 F RT A28NM E40NE 2007090700028 20070907 00028 NM 2007 9 7 2007UALA03382 1 20070825 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 FWD GALLEY DOOR LOWER HINGE CUTOUT FASTENER HOLE CRACKED. MAJOR REPAIR ACCOMPLISHED: FABRICATED EXTERNAL FUSELAGE DOUB LER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700030 20070907 00030 NM 2007 9 7 2007UALA03384 1 20070824 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 727B S20R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 AFT PIT STR CLIP HAS DEEP TOOLING MARK AT STA 727B STR 20R. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700032 20070907 00032 NM 2007 9 7 2007UALA03386 1 20070825 A 5241 BEARING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 FWD GALLEY DOOR CUTOUT TORQUE TUBE HAS MOVEMENT BEYOND .003. REPLACED UPPER & LOWER BEARINGS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700041 20070907 00041 NM 2007 9 7 2007UALA03395 1 20070824 A 3350 POWER SUPPLY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 513UA 24810 ESCAPE PATH LIGHTING INOP ROWS 25 TO 30. 2 L 7 2 4F 4 F RT A2NM E17NE 2007090700084 20070907 00084 SO 2007 9 7 C2XA07SH051 1 20070821 A 5320 14524196001 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12166 14500831 SHV - DURING C-CHECK MAINTENANCE FOUND RIGHT OMEGA BEAM NUT PLATE HOLE AFT OF FRM 23 HAS CORROSION. MAINTENANCE REPAIRE D RIGHT OMEGA BEAM AT FRM 23 IAW EC 5320-01228. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007090700085 20070907 00085 NM 2007 9 7 ABXA070274 1 20070826 A 2120 UNKNOWN BOEING 767 767232 1385132 NM CABIN ODOR A ABXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 746AX 22223 SMELLED SMOKE IN FLIGHT AFTER TAKEOFF. SUSPECT HIGH PRESSURE VALVE STAYED OPEN WHEN COMMANDED TO CLOSE. VERIFIED ALL C IRCUIT BREAKERS TO BE NORMAL (NOT POPPED OUT). RAN ENGINE UP, NO ODOR PRESENT AS PER B767 AMM 71-00-00. 2 L 7 2 4F RT A1NM 2007090700092 20070907 00092 NM 2007 9 7 SWAA074242 1 20070828 A 2432 279202 CHARGER BOEING 737 7377H4 1384404 NM MASTER BATTERY OVERHEATED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 29 288WN 36611 DIVERSION / DECLARED EMERGENCY. CLIMBING OUT OF SAN AT 23000, CREW SMELLED AN ACRID / ELECTRICAL ODOR. TURNED RECIRC A ND GASPER FAN OFF, ODOR DISSIPATED. FOUND AIRCRAFT BATTERY CHARGER OVERHEATING, REMOVED AND REPLACED BATTERY CHARGER AN D BATTERY PER MM. 2 L 7 2 4F RT A16WE 2007090700113 20070907 00113 EU 2007 9 7 2007UALA03419 1 20070825 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SEAT 17 BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 404UA 450 AISLE EMERGENCY LIGHT PATH HAS LIGHT BROKEN AT SEAT 17. UNKNOWN DAMAGE TO LIGHT ASSY. REPLACED LIGHT ASSY AT SEAT 17. 2 L 7 2 4F 4 F RT A28NM E40NE 2007090700114 20070907 00114 EU 2007 9 7 2007UALA03420 1 20070825 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ROW 18, INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 404UA 450 AISLE EMERGENCY LIGHT PATH HAS LIGHTS OUT AT ROW 18, 19, 21. FOUND LAMPS FAULTY. RELAMPED EMERGENCY LIGHTS AT ROW 18 ,19,21. 2 L 7 2 4F 4 F RT A28NM E40NE 2007090700127 20070907 00127 NM 2007 9 7 2007UALA03427 1 20070826 A 3350 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 371UA 24540 RIGHT OFF WING (AFT OF TRAILING EDGE) EMERGENCY EXIT LIGHT INOP. FAILED LAMP. RELAMPED- OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700128 20070907 00128 NM 2007 9 7 2007UALA03428 1 20070825 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 DOOR 1R SIDE SILL LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700140 20070907 00140 NM 2007 9 7 2007UALA03439 1 20070827 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 507UA 24743 CREW REPORTED EMERGENCY LIGHT ABOVE SEATS 22 ABC IS OUT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007090700144 20070907 00144 EU 2007 9 7 2007UALA03443 1 20070828 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 429UA 539 FOUND ON ARRIVAL DENT AND SCUFF MARKS APPROX 3 FT BELOW DOOR 1L. DAMAGE IS AFT OF E&E DOOR AND FWD OF E&E FAN INTAKE VL V. LOCATION IS FROM FR18 TO FR 21 - BETWEEN STR33L & STR34L. BETWEEN FR18 AND FR19 DENT APPROX 6IN X 2IN X .046IN. BE TWEEN FR19 & FR20 DENT APPROX 4IN X 2IN X .031IN. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007090700150 20070907 00150 NM 2007 9 7 2007UALA03449 1 20070828 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 565UA 26669 EXTERIOR EMERGENCY LIGHT INOP AT DOORS 1L & 4R. RELAMPED EXTERIOR EMERGENCY LIGHT AT DOOR 1L & 4R. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091000005 20070910 00005 NM 2007 9 10 SWAA074358 1 20070904 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 747 S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091000015 20070910 00015 NM 2007 9 10 SWAA074306 1 20070830 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM BS 350 S25R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND STRINGER 25R CORRODED AT BS 350. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007091000027 20070910 00027 NM 2007 9 10 SWAA074368 1 20070901 A 5330 6545766 SKIN BOEING 737 7373T5 1384608 NM BS 970 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 696SW 23064 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000029 20070910 00029 NM 2007 9 10 SWAA074389 1 20070905 A 5311 6545812 FRAME BOEING 737 7375H4 138449D NM BS 328 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000032 20070910 00032 NM 2007 9 10 SWAA074415 1 20070905 A 5755 ATTACH FITTING BOEING 737 7373H4 1384600 NM NR 4 SPOILER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED SERVICE CHECK, FOUND LEFT WING NR 4 SPOILER ATTACH LUG BROKEN. REMOVED AND REPLACED NR 4 SPOILER PER M M. 2 L 7 2 4F RT A16WE 2007091000033 20070910 00033 NM 2007 9 10 SWAA074379 1 20070905 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000034 20070910 00034 NM 2007 9 10 SWAA074414 1 20070905 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000038 20070910 00038 NM 2007 9 10 SWAA074388 1 20070905 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000042 20070910 00042 NM 2007 9 10 SWAA074381 1 20070905 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000043 20070910 00043 NM 2007 9 10 SWAA074387 1 20070905 A 5311 6546552 FRAME BOEING 737 7375H4 138449D NM BS 827 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000044 20070910 00044 NM 2007 9 10 SWAA074390 1 20070905 A 5311 6546552 FRAME BOEING 737 7375H4 138449D NM BS 827 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 9R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000046 20070910 00046 NM 2007 9 10 SWAA074404 1 20070905 A 5310 6546818 CREASE BEAM BOEING 737 7373A4 1384585 NM BS 747-767 S17L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 747 AND BS 767, STR 17L. REMOVED AND REPLACED CRE ASE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2007091000048 20070910 00048 NM 2007 9 10 SWAA074405 1 20070905 A 5313 6551698 STRINGER SPLICE BOEING 737 7373A4 1384585 NM BS 907 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER S RM. 2 L 7 2 4F RT A16WE 2007091000050 20070910 00050 NM 2007 9 10 SWAA074378 1 20070905 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM BS 360 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000051 20070910 00051 NM 2007 9 10 SWAA074420 1 20070905 A 5314 6562125 KEELBEAM BOEING 737 7373H4 1384600 NM BS 500C-500D CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND LEFT KEEL BEAM CORRODED AT BS 500C TO BS 500D, LBL 6.5. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2007091000053 20070910 00053 NM 2007 9 10 SWAA074417 1 20070905 A 5754 65C26686 SKIN BOEING 737 7373H4 1384600 NM NR 2 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 14Y CHECK, FOUND LEFT WING NR 2 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED L/E SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007091000054 20070910 00054 NM 2007 9 10 SWAA074370 1 20070904 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007091000055 20070910 00055 NM 2007 9 10 SWAA074377 1 20070904 A 5313 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 727C S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091000058 20070910 00058 NM 2007 9 10 SWAA074343 1 20070903 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 249WN 34951 L2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007091000060 20070910 00060 NM 2007 9 10 SWAA074311 1 20070831 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 454WN 29851 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 5 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007091000061 20070910 00061 NM 2007 9 10 SWAA074309 1 20070831 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 2 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007091000063 20070910 00063 NM 2007 9 10 SWAA074342 1 20070903 A 5315 417A5503 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 927 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 737JW 27869 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 927, LBL 3. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007091000064 20070910 00064 NM 2007 9 10 SWAA074307 1 20070831 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 278WN 36441 EEPLS LENS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007091000065 20070910 00065 NM 2007 9 10 SWAA074310 1 20070831 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 454WN 29851 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 19 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007091000067 20070910 00067 NM 2007 9 10 SWAA074312 1 20070831 A 3350 417A5703 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 466WN 30677 EEPLS ASSY LOOSE AT ROW 3 ABC. SECURED EEPLS ASSY PER MM. 2 L 7 2 4F RT A16WE 2007091000068 20070910 00068 2007 9 10 SWAA074364 4 20070901 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 734SA 27866 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007091000069 20070910 00069 NM 2007 9 10 SWAA074316 1 20070831 A 3233 65448105 ACTUATOR BOEING 737 7373Q8 1384670 NM RT MLG FAULTY A SWAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 29 695SW 23506 WITH THE GEAR HANDLE IN THE OFF POSITION AND AIRBORNE THE RIGHT MLG EXTENDED. RETRACTED NORMALLY AND STAYED STOWED FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED RIGHT MLG UPLOCK ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2007091000074 20070910 00074 NM 2007 9 10 SWAA074246 1 20070828 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000075 20070910 00075 NM 2007 9 10 SWAA074243 1 20070828 A 5315 6546809 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CHORD CRACKED AT BS 947, LBL 55. REPAIRED FLOORBEAM CHORD PER ER. 2 L 7 2 4F RT A16WE 2007091000076 20070910 00076 NM 2007 9 10 SWAA074244 1 20070828 A 5551 CLEVIS BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND RIGHT AND LEFT HORIZONTAL STABILIZER CLEVIS LUG FACES CORRODED. REPAIRED HORIZONTAL S TABILIZER PER SRM. 2 L 7 2 4F RT A16WE 2007091000077 20070910 00077 NM 2007 9 10 SWAA074260 1 20070828 A 3350 6556633 LIGHT BOEING 737 737317 138447P NM EMERGENCY EXIT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 LEFT OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007091000085 20070910 00085 NM 2007 9 10 2007UALA03453 1 20070829 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 171UA 24322 EEL LIGHT AISLE STRIPS AT ROWS 6-8 TURN OFF AND ON AT RANDOM. SECURED STRIPS CONNECTOR & CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007091000086 20070910 00086 NM 2007 9 10 2007UALA03454 1 20070829 A 3350 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY LIGHTS INOP: LEFT OVERWING 2 FWD ASSY'S. REPLACED FUSE IN EMERGENCY POWER SUPPLY UNIT, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007091000089 20070910 00089 NM 2007 9 10 2007UALA03457 1 20070829 A 2612 LOOP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CARGO BAY FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EXISTING ACTIVE FAULT: FWD CARGO 1 LOOP A FAIL. MNT MSG 26160. RESET SYST, RETEST OF CMC GROUND TEST. SYSTEM PA SSED. NO EXISTING FAULTS, NO STATUS MSG, FIRE TEST OK 2 L 7 4 4F 4 F RT A20WE E24NE 2007091000090 20070910 00090 NM 2007 9 10 2007UALA03458 1 20070828 A 3210 LANDING GEAR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 371UA 24540 ONCE AIRBORNE LANDING GEAR WOULD NOT RETRACT. GEAR FINALLY RETRACTED AFTER RUNNING THRU CHECKLIST. 10-11-07 FOUND A IR SAFETY SENSOR S106 GAP TO BIG. REPLACED SENSOR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091000091 20070910 00091 EU 2007 9 10 2007UALA03459 1 20070828 A 2750 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE TE FLAPS UNKNOWN A UALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 WP 29 403UA 442 FLIGHT DIVERTED DUE TO FLAPS LOCKED MESSAGE DISPLAYED. PERFORMED WTB PROCEDURE PER TSM AND FLAPS RESET AND PERFORMED N ORMALLY. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007091000092 20070910 00092 NM 2007 9 10 2007UALA03460 1 20070829 A 5610 WINDSHIELD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 589UA 28707 RTFL DUE TO SHATTERING OF PILOT'S WINDSHIELD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091000093 20070910 00093 NM 2007 9 10 2007UALA03461 1 20070829 A 2730 COMPUTER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FLT CONTROLS MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 816UA 871 ELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN, - F-CTL. AIRCRAFT STARTED UNCOMMANDED FLIGHT MOVEMENT IN A DOWN PITCH BEFO RE ECAM AND AFTER FAULT NO FURTHER UNCOMMANDED MOVEMENT. RESET ELAC2 AND PERFORMED GROUND SCAN- NO PROBLEMS NOTED, NO REPEATS SINCE ORIGINAL 2 L 7 2 4F 4 F RT A28NM E40NE 2007091000096 20070910 00096 NM 2007 9 10 SWAA074236 1 20070828 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM BS 500C S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000097 20070910 00097 NM 2007 9 10 SWAA074254 1 20070828 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED 18Y CHECK, FOUND STRINGER 15L CRACKED AT BS 380. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007091000098 20070910 00098 NM 2007 9 10 SWAA074239 1 20070828 A 2560 PH22300L GLOWSTRIP BOEING 737 737317 138447P NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIPS WORN BETWEEN ROW 1 DEF AND ROW 5 DEF. REMOVED AND REPLAC ED STRIPS PER MM. 2 L 7 2 4F RT A16WE 2007091000099 20070910 00099 NM 2007 9 10 2007UALA03463 1 20070829 A 5320 ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 530 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 ANGLE CRACKED, C1 LEFT LOWER FUSELAGE JUST ABOVE AC PACK RAM AIR DUCT APPROX STA 530, SUPPORT ANGLE. MAJOR REPAIR ACCOM PLISHED: FABRICATED & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091000100 20070910 00100 NM 2007 9 10 2007UALA03464 1 20070829 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 616 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 FRAME CRACKED BS 616R RBL 62-64 OVERWING BODY FRAME INNER CHORD. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED REP AIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091000101 20070910 00101 NM 2007 9 10 2007UALA03465 1 20070829 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 FUSELAGE SKIN CRACKED AROUND GROUND AIR SERVICE DOOR AT 11:00 POSITION. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FA BRICATED & INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091000102 20070910 00102 NM 2007 9 10 2007UALA03466 1 20070829 A 5320 ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 300 S10L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 CABIN BS 300, INTERCOSTAL ABOVE STRINGER S10L OUTER ATTACH ANGLE IS CRACKED. MAJOR REPAIR ACCOMPLISHED: REPLACED DAMAG ED ATTACH ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091000103 20070910 00103 NM 2007 9 10 2007UALA03467 1 20070829 A 5412 BULKHEAD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 NACELLE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 NR 1 PYLON, GOUGED BULKHEAD FITTING AT NAC STA 237.39. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA. CUT OUT PREVI OUSLY TRIMMED FLANGE FROM BULKHEAD (P/N 311T3281). FABRICATED A REPAIR ANGLE & A REPLACEMENT BRACKET (272T0082-28) & A REPLACEMENT CLIP (313T3310-469). 2 L 7 2 4F 4 F RT A1NM E24NE 2007091000104 20070910 00104 NM 2007 9 10 2007UALA03468 1 20070829 A 5754 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 9 SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 NR 9 SLAT OUTBOARD EDGE DELAM ON UPPER AND LOWER SURFACE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007091000105 20070910 00105 NM 2007 9 10 2007UALA03469 1 20070829 A 4960 BATTERY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 APU BATTERY NOT CHARGING. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007091000107 20070910 00107 NM 2007 9 10 2007UALA03471 1 20070829 A 2425 GENERATOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 775UA 26947 RIGHT BACKUP GENERATOR FAILED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007091000108 20070910 00108 EU 2007 9 10 2007UALA03472 1 20070829 A 2731 ROD END AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ELEVATOR OUT OF ADJUST A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 491UA 1741 LIGHT AIRFRAME VIBRATION IN CLIMB. VIBRATION STOPPED AT FL250. FOUND ELEVATOR SERVO CONTROL ROD ENDS OUT OF ADJUSTM ENT. ADJUSTED INBD AND OTBD ELEV SERVO CONTROL ROD ENDS. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007091000109 20070910 00109 NM 2007 9 10 2007UALA03473 1 20070829 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SMOKE A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 87UA 26713 F/A REPORTS ODOR OF SMOKE IN VIDEO COMPARTMENT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091000114 20070910 00114 NM 2007 9 10 2007UALA03478 1 20070829 A 5551 CLEVIS BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZONTAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 RIGHT HORIZ STAB CORRODED: CENTER SECTION AFT UPPER CLEVIS AFT LUG EMITTING CORROSION. REMOVED BUSHINGS (FWD AND AFT LUGS), REAMED BORES OF LUGS, HFEC INSPECTED WITH NO DAMAGE FOUND, ROTO-PEENED, TREATED AND PRIMED LUGS, FABRICATED OVER SIZED BUSHINGS-INSTALLED ASSY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091000115 20070910 00115 NM 2007 9 10 2007UALA03479 1 20070829 A 5551 LUG BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZONTAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 RIGHT HORIZ STAB FWD UPPER LUG CORRODED AND BUSHINGS HAVE MIGRATED. REMOVED FWD & AFT BUSHING & SLEEVE AND REMOVED COR ROSION ON FWD FACE OF LUG. FABRICATED & INSTALLED OVERSIZED BUSHING & SLEEVE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091000116 20070910 00116 2007 9 10 2007UALA03480 4 20070829 A 2565 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE 5R DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26877 DOOR 5 RIGHT SLIDE CAME APART. DID NOT DEPLOYED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007091000118 20070910 00118 NM 2007 9 10 2007UALA03482 1 20070829 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ROW 13ABC UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 558UA 26654 EMERGENCY LIGHT STRIP ON FLOOR AT ROW 13ABC STICKS UP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091000121 20070910 00121 NM 2007 9 10 2007UALA03485 1 20070829 A 5220 HANDLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ESCAPE HATCH OBSTRUCTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 641UA 25091 RIGHT AFT EMERGENCY ESCAPE HATCH AUTO ARM AND AUTO FIVE SWITCHES DID NOT MOVE TO THE (UP) POSITION, DURING TEST. 2 L 7 2 4F 4 F RT A1NM E24NE 2007091000122 20070910 00122 NM 2007 9 10 2007UALA03486 1 20070829 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SEAT 2AB MISSING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 673UA 29241 EEL LIGHT MISSING AT SEAT 2AB. REPLACED LIGHT ASSY, CHECKS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007091000123 20070910 00123 2007 9 10 2007UALA03487 4 20070828 A 2565 D30656126U1 SWIVEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR SLIDE UNSERVICEABLE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 590UA 28708 DAMAGED INFLATION HOSE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091000125 20070910 00125 2007 9 10 2007UALA03489 4 20070829 A 2565 DISK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR SLIDE RUPTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 LOW BOTTLE PRESSURE. FOUND RUPTURE DISC LEAKING. REPLACED RUPTURE DISK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091000127 20070910 00127 NM 2007 9 10 KCSA071329 1 20070831 A 3350 LIGHT BOEING 747 747122 1384872 NM EMERGENCY EXIT INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 716CK 19753 EMERGENCY EXIT SIGN ABOVE UPPER DECK RIGHT ESCAPE DOOR INOP. 2 L 7 4 4F A20WE 2007091000128 20070910 00128 SO 2007 9 10 C2XA07TY046 1 20070829 A 3350 1317 BULB EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17108 145655 EMERGENCY LIGHT IN CEILING BY ROW 17A INOP. REPLACED LIGHT BULB IAW EMB 145 AMM 33-50-04, OPS CHECK GOOD. AIRCRAFT REL EASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT 2007091000133 20070910 00133 NM 2007 9 10 USAA070703 1 20070830 A 5340 MOUNT BOEING 737 7373B7 1384580 NM STA 986.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 STA 986.5 + 7, S17L & S17R, LT & RT INBOARD & OUTBOARD AFT LAV MOUNTS CORRODED. REMOVED & REPLACED MOUNTS PER SRM 51-20 -01, 51-10-02; CORR TASK C53-107-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007091000135 20070910 00135 NM 2007 9 10 SWAA074285 1 20070829 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 408WN 27895 DURING SCHEDULED 6Y CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.9. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007091000140 20070910 00140 NM 2007 9 10 SWAA074270 1 20070829 A 5311 6546526 FRAME BOEING 737 7373A4 1384585 NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000142 20070910 00142 NM 2007 9 10 SWAA074272 1 20070829 A 5311 6546548 FRAME BOEING 737 7373A4 1384585 NM BS 747 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000144 20070910 00144 NM 2007 9 10 SWAA074273 1 20070829 A 5311 6546554 FRAME BOEING 737 7373A4 1384585 NM BS 847 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000146 20070910 00146 NM 2007 9 10 SWAA074282 1 20070829 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM BS 360 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000149 20070910 00149 NM 2007 9 10 SWAA074267 1 20070829 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM BS 500C S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000153 20070910 00153 NM 2007 9 10 2007UALA03493 1 20070830 A 3350 LAMP BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 921UA 25388 OUTSIDE LEFT OVERWING EMERGENCY LIGHT BURNED OUT. RELAMPED ASSY, OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091000154 20070910 00154 NM 2007 9 10 2007UALA03494 1 20070830 A 3350 BULB BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 ONE EEL LIGHT NOT WORKING AT SEAT ROW 7. SECURED LAMP IN ASSY, RECHECKED LIGHT SYS-NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091000155 20070910 00155 NM 2007 9 10 2007UALA03495 1 20070830 A 3350 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 347UA 24251 RIGHT AFT FUSELAGE SLIDE EEL LIGHT IS INOPERATIVE. LAMP BURNED OUT. RELAMPED LIGHT ASSY, OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091000156 20070910 00156 NM 2007 9 10 2007UALA03496 1 20070830 A 3397 FEEDER CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 347UA 24251 FLOOR EEL LIGHTS ARE INOP FROM SEAT ROW 10 AFT. BROKEN LEAD, FEEDER CABLE. REPLACED LEAD ON THE MIDDLE SECTION, FOUN D INVERTER AND FEEDER CABLE BAD.REPLACED INVERTER AND FEEDER CABLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091000159 20070910 00159 NM 2007 9 10 SWAA074286 1 20070829 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM BS 727D S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000161 20070910 00161 NM 2007 9 10 SWAA074289 1 20070829 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 294 S11L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091000163 20070910 00163 NM 2007 9 10 SWAA074274 1 20070829 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 727E S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091000164 20070910 00164 NM 2007 9 10 SWAA074275 1 20070829 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 727D S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091000166 20070910 00166 NM 2007 9 10 SWAA074277 1 20070829 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 706 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091000167 20070910 00167 NM 2007 9 10 SWAA074290 1 20070829 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 277 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091000169 20070910 00169 EU 2007 9 10 USAA070708 1 20070830 A 5320 D5347112420100 SHEAR PLATE AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 185UW 1666 RIGHT LATERAL SHEAR PLATE BETWEEN FR 69 & 70 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART; CORR TASK JA-2 60-53500, DEFECT SIZE: 2" X 3". 2 L 7 2 4F RT A28NM 2007091000171 20070910 00171 NM 2007 9 10 USAA070700 1 20070830 A 5320 6545834256 STIFFENER BOEING 737 7373B7 1384580 NM STA 328 LBL 10 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 STA 328, LBL 10, FLOOR SUPPORT STIFFENER HAS CORROSION. REMOVED & REPLACED WITH NEW STIFFENER PER SRM 51-10-02; CORR TA SK C53-107-02, DEFECT SIZE: 2" X 12". 2 L 7 2 4F RT A16WE 2007091000172 20070910 00172 NM 2007 9 10 NOCA15007 1 20070827 A 2610 2156606 DETECTOR BOEING 767 767306 1385148 NM CARGO BAY UNKNOWN A NOCA K NONE N FALSE WARNING IN INSP/MAINT 1 EA 15 765NA 28098 FWD CARGO DET 1 ON STATUS PAGE ACTION T/S SYSTEM PER FIM 26-16-00 FIG 104 &108. FOUND FWD CARGO DET M324 AT FAULT. REM OVED & REPLACED PER MM 26-16-01, OPS CHECK OK. 2 L 7 2 4F RT A1NM 2007091000173 20070910 00173 NM 2007 9 10 USAA920070806 1 20070816 A 5320 SUPPORT ANGLE BOEING 757 757225 1384959 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 923UW 22203 PIT - MAJOR REPAIR - C-04 CHECK, CRACK ON AFT CARGO SUPPORT ANGLE, BS 1300. MANUFACTURED AND REPLACED AFT CARGO SUPPORT ANGLE, BS 1300 PER US AIRWAYS TR 53-10-01. 2 L 7 2 4F RT A2NM 2007091000178 20070910 00178 NM 2007 9 10 SWAA074344 1 20070901 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM BS 347 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT 347, STR 15R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007091000179 20070910 00179 NM 2007 9 10 SWAA074335 1 20070902 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM BS 765 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 765, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007091000180 20070910 00180 NM 2007 9 10 SWAA074321 1 20070901 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 739 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007091000182 20070910 00182 NM 2007 9 10 SWAA074320 1 20070901 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 921 S24R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 921, STR 24R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000185 20070910 00185 NM 2007 9 10 SWAA074352 1 20070903 A 5311 6546525 FRAME BOEING 737 7375H4 138449D NM BS 380 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007091000186 20070910 00186 NM 2007 9 10 SWAA074355 1 20070903 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007090600061 20070906 00061 CE 2007 9 6 GLBA20060985 1 20070814 A 5230 1294400491 HINGE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CARGO DOOR CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 208GL UE208 MAINTENANCE DISCOVERED BOTH CARGO DOOR HINGES CRACKED. MAINTENANCE REMOVED AND REPLACED CARGO DOOR HINGES IAW EO 05-02 . DOOR HINGE PN 129-440049-1. FUSELAGE PN 129-440049-3. 2 L 7 2 4T 4 T RT A24CE E26NE 2007090600065 20070906 00065 CE 2007 9 6 DJFA2007097 1 20070820 A 5540 673104025 HINGE FITTING CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RUDDER CHAFED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 708LX 5216 7500109 MX DISCOVERED CHAFING DAMAGE ON THE FOLLOWING PARTS DURING A SCHEDULED/ REFURB MX EVENT( 6731046-7 UPPER HINGE ASSY, 673 1040-25 LOWER HINGE ASSEMBLY, AND THE 6733126-2 SPAR FOR THE 6733120-1 UPPER RUDDER). DAMAGE TO THE 6733126-2 SPAR WAS A PPROXIMATELY 0.005 IN. DEEP ON THE UPPER HINGE LOWER LUG, AND 0.010 IN. DEEP ON THE LOWER HINGE UPPER LUG. THE CAUSE OF THE DAMAGE WAS IDENTIFIED AS APPROXIMATELY 0.063 IN. OF MISMATCH BETWEEN SPACING OF THE VERTICAL FIN HINGES AND THE LUG S ON THE RUDDER SPAR WHICH CAUSED A PRELOAD AND CHAFING CONDITION. MX REPLACED ALL REQUIRED ATTACH HDWR 2) UPPER RUDDE R (A) UPPER AND LOWER HINGES (ATTACH PTS ON UPPER RUDDER) WERE REPAIRED AND NDT WAS C/W IAW STRUCTURES. REPAIR DEFINITIO 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007090600074 20070906 00074 EU 2007 9 6 350608222007 1 20070822 A 2110 S3036EC1 COMPRESSOR UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE AIR CONDITIONER SEIZED E QMLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 130LN 3506 AIR CONDITIONER BELT HAD BEEN REPLACE. AC RELEASED FOR FLIGHT. AT ABOUT THE SAME TIME WE WERE TONED FOR A SCENE CALL. AB OUT 30 SECONDS AFTER TAKEOFF, SMELLED SMOKE, AIR CONDITIONER WAS TURNED OFF BUT THE SMELL OF SMOKE GOT WORSE SO A 180 TU RN WAS MADE AND RETURNED TO THE AIRPORT. WHEN THE MECHANIC INSPECTED THE AIR CONDITIONER UNIT, THE COMPRESSOR HAD SEIZED . AIRCRAFT WAS GROUNDED AND PARTS REPLACED. 1 G 7 2 3U 3 U H9EU E00054EN 2007090600080 20070906 00080 CE 2007 9 6 AMWA86724BC 1 20070817 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FALSE INDICATION A AMWA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 133YV 22639 585 UE133 DURING A FERRY FLIGHT, THE BATTERY CHARGE ANNUNCIATOR ILLUM IN FLT. ACFT LANDED WITH NO FURTHER INCIDENT. THIS IS A NU ISANCE WRITEUP AND DISTRACTION TO THE AIR CREW. RAN ACFT, SYSTEM OPS CHECKED NORMAL, COULD NOT DUPLICATE. 2 L 7 2 4T 4 T RT A24CE E26NE 2007090600104 20070906 00104 EU 2007 9 6 07FDEA03284 1 20070831 A 5730 A57340087 SKIN PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 ELONGATED HOLES ON PYLON NR 2 SUPPORT BRACKET AND LOWER WING SKIN, RIB 7-8 RT. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLATION OF FREEZE PLUGS IAW EA 6-2900-106507 AND RAS/BAE/1005210/2007 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600107 20070906 00107 EU 2007 9 6 07FDEA03287 1 20070831 A 5330 A53610317 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 DENT WITH SCRATCH IN SKIN BETWEEN FRAME 14A-15 CLOSE TO STRG 30-32 LT. REPAIR PERFORMED BY BLEND OUT SCRATCH, HFEC INSP ECTION OF SKIN WITH NIL FINDINGS AND INSTALLATION OF OVERSIZED FASTENERS IN ROTOTESTED HOLES OF ADJACENT STRINGER IAW EA 6-5312-99150 AND RAS 043534/005/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600110 20070906 00110 EU 2007 9 6 07FDEA03290 1 20070831 A 5310 A53973085210 BEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 CORROSION ON AFT CARGO DOOR SILL BEAM AT FRAME 59A AND NEAR FRAME 60, OUT OF LIMIT REPAIR PERFORMED BY EXTEND THE T-SECT ION AND INSTALLING FILLER/SHIM AS PER TD/K4/S1/20580/2006. ALL OTHER REQUIREMENTS AS PER SRM 53-17-18 / FIG 204. APPRO VED BY EA 6-5317-99225 AND RAS/DAHAM/4020580/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600118 20070906 00118 NM 2007 9 6 07FDEA03297 1 20070901 A 5412 AUB7525501 BULKHEAD DOUG MD11 MD11F 3023600 NM ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 595FE 48553 REFERENCE TO SNRM N00486, CORROSION WAS DETECTED AFTER REMOVAL OF NR 3 PYLON AFT MOUNTING BEARING. COMPLIED WITH FEDEX EA NR 1-5410-112388, TITLE: NACELLES AND PYLONS, NR 3 PYLON AFT MOUNT BEARING HOUSING BORE, INTERIM (24 MONTHS) REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007090600119 20070906 00119 EU 2007 9 6 07FDEA03298 1 20070901 A 5753 SKIN AIRBUS 300 A300F4605R 3930327 EU RT FLAP DENTED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 683FE 801 RT INBD FLAP TOP SURFACE 2 IN OTBD OF RIB 6 10 IN AFT OF FRONT SPAR IS A DENT 1.4 BY .020 INCH WITH A GOUGE .6 IN BY .1 IN BY .002 IN REF A300/600 SRM 57-50-00 AREA FOUND TO BE OUT OF LIMITS IAW A300 SRM 57-50-00 FIG 101, SH5. REPAIRED AR EA IAW A300 FREIGHTER SRM 57-50-00 PARAGRAPH E FIG 205, ALONG WITH A300 SRM 51-75-10. 2 L 7 2 4F RT A35EU 2007090600124 20070906 00124 EU 2007 9 6 07FDEA03303 1 20070902 A 7830 FLANGE AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 683FE 801 A 1.5" AND A .5 INCH CRACK EXIST AT NR 2 ENGINE O/B T/R UPPER L/E FLANGE REF 78-31-00-6. REMOVED AND REPLACED NR 2 ENG O/B T/R IAW A300-600 AMM 71-13-03-4-05 OPS CHECK GOOD IAW A300-600 AMM 71-03-4-05. 2 L 7 2 4F RT A35EU 2007090600129 20070906 00129 EU 2007 9 6 07FDEA03310 1 20070903 A 5310 A53610994203 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 725FD 572 NUMEROUS FASTENERS WERE FOUND TO BE NON CONFORMING AND ELONGATED ON FITTING FRAME 12A, FRAME 12A AND CORNERS RT AND LT S IDES. REPAIR PERFORMED BY DETAILED VISUAL AND ROTO TEST INSPECTIONS IN DAMAGED HOLES, REPLACEMENT OF FITTING, CORNER SP LICE AND CORNER ANGLE WITH INSTALLATION OF NEW SPLICE UNDER STRG 26. INSTALLING REPAIR BUSHES IN FRAME 12A WEB RT SIDE ONLY AND OVERSIZED FASTENERS IAW TD 942.043937/012/2006. APPROVED BY EA 6-5312-99226 AND RAS/AS/0047/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600130 20070906 00130 EU 2007 9 6 07FDEA03311 1 20070903 A 5310 A53610994203 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 725FD 572 NUMEROUS FASTENERS WERE FOUND TO BE NON CONFORMING AND ELONGATED ON FITTING FRAME 12A, FRAME 12A AND CORNERS RT AND LT SIDES. REPAIR PERFORMED BY DETAILED VISUAL AND ROTO TEST INSPECTIONS IN DAMAGED HOLES, REPLACEMENT OF FITTING, CORNE R SPLICE AND CORNER ANGLE WITH INSTALLATION OF NEW SPLICE UNDER STRG 26. INSTALLING REPAIR BUSHES IN FRAME 12A WEB RT S IDE ONLY AND OVERSIZED FASTENERS IAW TD 942.043937/012/2006. APPROVED BY EA 6-5312-99226 AND RAS/AS/0047/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007090600144 20070906 00144 EU 2007 9 6 07FDEA03260 1 20070831 A 5313 A53778025 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 CORROSION FOUND ON STRINGER 33 AND 34 LT, FRAME 35-36. SPLICE REPAIR PERORMED IAW PRINCIPLE OF SRM 53-10-14 FIG 201, AP PROVED BY EA 6-5314-99178 AND RAS/DABRE/2006 ISS A. 2 L 7 2 4F RT A35EU 2007090600145 20070906 00145 NM 2007 9 6 07FDEA03227 1 20070829 A 5310 65198615 BEAM BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 469FE 21581 HORIZONTAL WALKWAY BEAM L/SIDE HAS EVIDENCE OF CORROSION AT APPROX STA 320. REMOVED CORROSION ON TOP OF LT WALKWAY BEAM FROM STA 320 TO STATION 330 AND ACCOMPLISHED ULTRASOUND THICKNESS TEST (ACCEPTABLE) IAW 727 200 SRM 53-10-4 FIG 7. MEC HANICS WROTE ITEM AS BEING A WALKWAY BEAM AND STRUCTURES MECHANICS SIGNED THE REPAIR OFF AS A WALKWAY BEAM. THE BOEING SRM REFERS TO THE ITEM AS A WALKWAY BEAM CORD AND THE BOEING DRAWING 65-18415 PL REFERS TO IT AS A CORD. 2 L 7 3 4F A3WE 2007090600146 20070906 00146 EU 2007 9 6 07FDEA03261 1 20070831 A 5730 A57340087 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 FOUND THE HYDRAULIC FITTING HOLES IN PYLON SUPPORT BRACKET IN LOWER SKIN PANEL OF THE RT WING ELONGATED. REPAIR PERFORM ED BY OVERSIZING HOLES AND INSTALLATION OF REPAIR BUSHES IAW R571-50532 ISSUE: A APPROVED BY EA 6-5720-99183 AND RAS/BAE /1002415/2006 ISSUE: A. 2 L 7 2 4F RT A35EU 2007090600147 20070906 00147 EU 2007 9 6 07FDEA03262 1 20070831 A 5310 A53773644203 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 725FD 572 CORNER FITTING AT FRAME 30 RT IS CRACKED. REPAIR WAS PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007090600185 20070906 00185 EU 2007 9 6 07FDEA03256 1 20070829 A 3260 PROXIMITY SENSOR AIRBUS 300 A300B4622R 3930312 EU MLG MALFUNCTIONED A FDEA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 25 723FD 543 ON TAKEOFF TRIED TO RAISE GEAR WITH NR 1 SYS WOULD NOT COME UP SWITCHED TO SYS 2 GEAR CAME UP. WHILE GEAR WAS RETRACTIN G NR 1 PITCH TRIM BOTH ATS LEVERS NR 1 CABIN PRESS REGULATOR KICKED OFF OVERWEIGHT LANDING AT 312K AND DECLARED EMERGENC Y. FOUND LT UPPER NOSE GEAR HARNESS DAMAGED. REPLACED THE HARNESS P/N D22296010 AS A PRECAUTION REF A300 SUPP M/M 32-2 1-43-4. COMPLIED WITH PHASE 1 INSPECTION OF THE OVERWEIGHT INSPECTION NO DEFECTS NOTED AT THIS TIME A-300-600 MM 05-51 -11-0. REMOVED AND REPLACED SENSORS 80 AND 81GB. REMOVED AND REPLACED 65GB, NO HELP REFA300-600ASM 32-31-00. REMOVED AND REPLACED 9GA, 8GA AND 64 GB SYSTEM 1 PROX DETECTORS REFA300-600 MM 32-00-00-4. SWUNG GEAR, CKD OK. 2 L 7 2 4F RT A35EU 2007090600194 20070906 00194 NM 2007 9 6 DHL2007746519 1 20070809 A 5311 FRAME BOEING 727 727224 1384076 NM BS 640 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 WHILE AT FLIGHTSTAR FOR A "C" CHECK, FUSELAGE FRAME DENTED BS 640 BETWEEN 16R-17R. CUT OUT DAMAGE AREA DIM 1.5" AND 1" BY 1" IAW B727 SRM 51-40-03 FIG 1. FAB ANGLE REPAIR FROM 7075-T6 .050 PO NR 9005138 IAW B727 SRM 53-10-02 AND 51-40-03 FIG 1, LOCATED AND DRILLED IAW B 727 SRM 51-30-05. ALODINE AND PRIMED ANGLE AND AREA IAW B 727 SRM 51-10-02. INSTALLED ANGLE REPAIR IAW B727 SRM 51-30-02 AND 51-40-03 FIG 1. 2 L 7 3 4F A3WE 2007090600200 20070906 00200 EA 2007 9 6 TRAX200701253 1 20070829 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 855AS 7395 NR 6, 7, 8 FLOOR TRACK LIGHTS AND RIGHT OVERWING FLOOR EXIT LIGHT INOP. 2 L 7 2 4F RT A21EA 2007090700002 20070907 00002 2007 9 7 SWAA074298 4 20070830 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 466WN 30677 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007090700003 20070907 00003 2007 9 7 SWAA074293 4 20070830 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 241WN 32504 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007090700005 20070907 00005 NM 2007 9 7 SWAA074302 1 20070830 A 5753 6546481 CARRIAGE BOEING 737 7373H4 1384600 NM RT WING TE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND LEFT WING NR 1 T/E FLAP CARRIAGE CORRODED. REMOVED AND REPLACED CARRIAGE PER MM. 2 L 7 2 4F RT A16WE 2007090700011 20070907 00011 EA 2007 9 7 TRAX200701259 1 20070830 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 857AS 7411 EMERGENCY LIGHTS 6 THROUGH 9 WILL NOT ILLUMINATE. 2 L 7 2 4F RT A21EA 2007090700016 20070907 00016 SO 2007 9 7 C2XA07SH053 1 20070829 A 5310 14538922401 PANEL EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11106 145650 SHV - DURING C-CHECK MAINTENANCE FOUND PANEL 197 DR HAS CORRODED BONDING PLATES. MAINTENANCE REPAIRED PANEL 197 DR IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007090700017 20070907 00017 SO 2007 9 7 C2XA07SH054 1 20070829 A 5310 14551154601 PANEL EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11106 145650 SHV - DURING C-CHECK MAINTENANCE FOUND PANEL 197 AB HAS CORRODED BONDING PLATES. MAINTENANCE REPAIRED PANEL 197 AB IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007090700024 20070907 00024 NM 2007 9 7 2007UALA03378 1 20070824 A 5312 BULKHEAD BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LT MLG WW CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 LEFT MLG WHEEL WELL HORIZONTAL BULKHEAD WEB IS CRACKED BS 672, LBL 42, WL 202; BS 665, LBL 39, WL 202 AND BS 665, LBL 32 , WL 202. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED WEB REPLACEMENTS, DOUBLERS AND TRIPLER REPAIRS AT BOTH LBL 42 AND LBL 39. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700036 20070907 00036 NM 2007 9 7 2007UALA03390 1 20070824 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 938 S25L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 308UA 23669 FUSELAGE SKIN CRACKED AT STA 938 AND 1FT ABOVE STRINGER 25L. CRACK STARTS FROM SKIN RADIUS AND EXTENDS BEYOND RIVET HOL E. APPROX LOCATION IS 1FT FWD OF WATER SERVICE PANEL. CRACK IS 1.5 INCH LONG. MAJOR REPAIR ACCOMPLISHED: MFG DOUBLER S. LAYED OUT & PILOT DRILLED TWO STRUCTURAL FILLERS, A DOUBLER AND TRIPLER. FINAL DRILLED AND TRIMMED ALL PIECES. INS TALLED SHIMS, TEAR STRIPS & INSTALLED RIVETS. COMPLETED DAMAGED AREA REF SRM 53-00-01, REPAIR 31, DETAILS 6,18, AND 28. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700049 20070907 00049 NE 2007 9 7 2007UALA03403 2 20070827 A 7230 COMPRESSOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 2 ENGINE STALLED A UALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 664UA 29236 724371 NR 2 ENG HAD A MODERATE TO LARGE COMPRESSOR STALL-BOOM AT STEADY STATE POWER SETTING OF 1.30 EPR. WIND 290-1 4 KTS. EI CAS STATUS MSG GENERATED -R SURGE DET- MSG. NR 2 ENGINE SURGED REPEATEDLY ON GROUND RUNS. HPC BORESCOPE NOTED NO DEFEC TS. ENGINE REPLACED AT SFO PRIOR TO FURTHER FLIGHT. SHOP TROUBLESHOOTING DID NOT DISCLOSE ANY CONCLUSIVE FINDINGS. ENG INE CONVERTED TO RING CASE CONFIGURATION (RCC) IAW AD 2003-19-15. 2 L 7 2 4F 4 F RT A1NM E24NE 2007090700051 20070907 00051 EU 2007 9 7 2007UALA03405 1 20070827 A 5101 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSLEAGE VIBRATION A UALA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 WP 29 488UA 1680 LIGHT LATERAL AIRFRAME VIBRATION IN COCKPIT AND AFT GALLEY DURING CLIMB FL248-270. 2 L 7 2 4F 4 F RT A28NM E40NE 2007090700058 20070907 00058 NM 2007 9 7 2007UALA03500 1 20070830 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE MID GALLEY & AFT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 670UA 29240 MID GALLEY EEL STRIP & AFT GALLEY LARGE EEL STRIP ARE INOPERABLE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007090700068 20070907 00068 NM 2007 9 7 2007UALA03180 1 20070814 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 ZONE-D LEFT CEILING EMERGENCY LIGHT IS INOP. *S/D* RELAMPED CEILING LIGHT, CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700075 20070907 00075 NM 2007 9 7 2007UALA03186 1 20070815 A 3350 78671 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHT ROW 44 HJK INOP. *S/D* RELAMPED EMERGENCY LIGHT. OP CHECK NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700082 20070907 00082 SO 2007 9 7 C2XA07IA188 1 20070828 A 3260 355022002 ELECTRONIC UNIT EMB 145 EMB145XR 3260214 SO MLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 21154 12191 1786 145772 TUS - FLIGHT 3150, THE CREW REPORTED AN AIR/GRND FAILURE INDICATION AFTER TAKEOFF. THE AIRCRAFT RETURNED TO TUS WHERE I T LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS INSPECTED FOR THE PURPOSES OF A FERRY FLIGHT, AND WAS FERRIED IAH WHERE MAI NTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007090700083 20070907 00083 SO 2007 9 7 C2XA07SH050 1 20070821 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12166 14500831 SHV - DURING C-CHECK MAINTENANCE FOUND GALLEY CTR OMEGA BEAM AT FRAME 17 TO FRAME 24 WITH CORROSION. MAINTENANCE REMOVE D & REPLACED CENTER OMEGA BEAM AT FRAME 17 TO FRAME 24 IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED TO RETURN TO SER VICE. 2 L 7 2 4F RT 2007090700104 20070907 00104 NM 2007 9 7 2007UALA03410 1 20070824 A 2622 WARNING LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU EXTINGUISHER ILLUMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 APU BOTTLE DISCHARGE LIGHT IS ILLUMINATED. ACCOMPLISHED TROUBLESHOOTING ON ONE OF THE THREE LARGE CONNECTORS AFT LEFT SIDE OF GEAR TO CHECK FOR ANY SHORTING OF PIN 2-3; RECHECKED VOLTAGE AT SQUIB ON APU BOTTLE. THE PROGNOSIS IS ON A BAD CONNECTOR WITH A BAD PIN-SOCKET. REPLACED CONNECTOR AND CHECKED VOLTAGE AT THE CONNECTOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007090700108 20070907 00108 NM 2007 9 7 2007UALA03414 1 20070824 A 3397 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 586UA 26710 ESCAPE PATH LIGHTING INOPERATIVE FROM ROW 9 TO 13. SECURED EEL CONNECTION AT 13A. NO COMPONENTS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007090700111 20070907 00111 NM 2007 9 7 2007UALA03417 1 20070825 A 3397 FEEDER CABLE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 937UA 26668 EEL LIGHTS ARE INOP FROM ROW 15 TO THE BACK OF THE PLANE. EEL CABLE FAULTY. REPLACED EEL CABLE FROM FEED IN. NO R EPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700120 20070907 00120 EA 2007 9 7 TRAX200701264 1 20070830 A 5220 STOP PIN CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 CORROSION ON COCKPIT ROOF CREW ESCAPE HATCH HINGE ARM STOP PINS. STOP PINS REMOVED IAW SRM 51-21-06 PINS STEEL SERVIC ABAE. 2 L 7 2 4F RT A21EA 2007090700129 20070907 00129 NM 2007 9 7 2007UALA03429 1 20070825 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 58LH INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 SEAT 58 LEFT SIDE EMERGENCY INOPERATIVE. REPLACED EMERGENCY LIGHT. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700133 20070907 00133 NM 2007 9 7 2007UALA03433 1 20070827 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY LIGHT AFT GALLEY RIGHT WALL INOP. RELAMPED EMERGENCY LIGHT. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700139 20070907 00139 NM 2007 9 7 2007UALA03438 1 20070827 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 569UA 26677 INTERIOR EMERGENCY LIGHTS ON (DOORS 3 RT & LT INTERMITTENT EXIT PATH) WITHOUT MANUAL ACTIVATION. REPLACED INBOARD BAT TERY PACK AT STATION 1680. 2 L 7 2 4F 4 F RT A2NM E17NE 2007090700143 20070907 00143 EU 2007 9 7 2007UALA03442 1 20070828 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 429UA 539 LEFT FUSELAGE HAD 2 EA PREVIOUSLY ARCHIVED DENTS IN ADJACENT FRAME BAYS BETWEEN FR 18 - 20 AND STR 32L & 33L. MAJOR REP AIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007090700152 20070907 00152 NM 2007 9 7 SWAA074247 1 20070828 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM BS 747 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747 S8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007090700157 20070907 00157 NM 2007 9 7 SWAA074305 1 20070830 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 907 S2R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091000010 20070910 00010 2007 9 10 SWAA074334 4 20070902 A 2565 D31354 SLIDE BOEING 737 7373K2 13844BA NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007091000013 20070910 00013 NM 2007 9 10 SWAA074332 1 20070901 A 3350 MS155721 LAMP BOEING 737 7373T5 1384608 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 696SW 23064 DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007091000017 20070910 00017 NM 2007 9 10 SWAA074400 1 20070905 A 3350 10107451 SIGN BOEING 737 7375H4 138449D NM EMERGENCY EXIT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 AFT CABIN EMERGENCY EXIT SIGN MISSING. INSTALLED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007091000018 20070910 00018 NM 2007 9 10 SWAA074371 1 20070904 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 738CB 27870 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 35.5. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007091000025 20070910 00025 NM 2007 9 10 SWAA074419 1 20070905 A 5311 6516352 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 2 DOOR STOP. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007091000028 20070910 00028 NM 2007 9 10 SWAA074367 1 20070901 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 740 S19R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740, STR 19R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000030 20070910 00030 NM 2007 9 10 SWAA074424 1 20070905 A 5330 6545857 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007091000035 20070910 00035 NM 2007 9 10 SWAA074382 1 20070905 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM BS 277 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 277, STR 9L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007091000040 20070910 00040 NM 2007 9 10 SWAA074374 1 20070904 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM BS 747 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000052 20070910 00052 NM 2007 9 10 SWAA074418 1 20070905 A 5311 65C22910 FRAME BOEING 737 7373A4 1384585 NM BS 500D S13R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 13R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000056 20070910 00056 NM 2007 9 10 SWAA074384 1 20070905 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 328 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091000059 20070910 00059 NM 2007 9 10 SWAA074353 1 20070901 A 3350 10107451 SIGN BOEING 737 7375H4 138449D NM EMERGENCY EXIT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 FWD CABIN EMERGENCY EXIT SIGN ASSY LOOSE. SECURED SIGN ASSY PER MM. 2 L 7 2 4F RT A16WE 2007091000066 20070910 00066 NM 2007 9 10 SWAA074365 1 20070901 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 466WN 30677 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007091000079 20070910 00079 NM 2007 9 10 SWAA074266 1 20070828 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 294 S11L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER S RM. 2 L 7 2 4F RT A16WE 2007091000087 20070910 00087 NM 2007 9 10 2007UALA03455 1 20070829 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 17L MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 177UA 24384 EEL INOP: ROW 17L 1EA MISSING. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007091000088 20070910 00088 NM 2007 9 10 2007UALA03456 1 20070829 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 44 HJK INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EEL INOP: SEAT 44 HJK. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007091000110 20070910 00110 NM 2007 9 10 2007UALA03474 1 20070829 A 3350 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 825UA 980 EMERGENCY LIGHTS FAIL TEST AT CIDS PANEL. FOUND LEFT EPSU BATTERY FAILURE. REPLACED LT EPSU BATTERY. OPS CHECKED GOO D. 2 L 7 2 4F 4 F RT A28NM E40NE 2007091000119 20070910 00119 2007 9 10 2007UALA03483 4 20070829 A 2565 LATCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE OVERWING SLIDE OUT OF TOLERANCE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 641UA 25091 LEFT OVERWING SLIDE DOOR LATCHES NR 1, 2, 3 & 4 FAIL EDGE MARGIN TEST. 2 L 7 2 4F 4 F RT A1NM E24NE 2007091000120 20070910 00120 2007 9 10 2007UALA03484 4 20070829 A 2565 MECHANISM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE OVERWING SLIDE OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 641UA 25091 LEFT OVERWING SLIDE INFLATION CYLINDER PULL FORCE MECHANISM BALL IS IN THE WRONG POSITION, BALL IS IN FRONT OF THE RETAI NER SPRING, NOT BEHIND IT AS REQUIRED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007091000129 20070910 00129 SO 2007 9 10 C2XA07TY045 1 20070828 A 2612 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO CARGO BAY MALFUNCTIONED A C2XA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 27 11121 145683 TYS ECIAS SHOWED BAGGAGE SMOKE INDICATION DURING FIRE DETECTION TEST AND BAGGAGE LIGHT NOT ILLUMINATED. MAINTENANCE REM OVED AND REPLACED NR 1 BAGGAGE DETECTOR IAW EMB 145 AMM 26-15-01. ALL OPS CHECKS WERE GOOD AND RELEASED TO SERVICE. 2 L 7 2 4F RT 2007091000130 20070910 00130 EU 2007 9 10 200708271 1 20070826 A 2150 10018582 HEAT EXCHANGER EMB ERJ170 ERJ170100SE 3260406 EU RT PACK DIRTY A UHLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 869RW 17000133 DFW TO JFK FLIGHT 6496 AT CRUISE THE A FLIGHT ATTENDANT INFORMED THE FLIGHT DECK THAT THERE WAS A STRONG BURNING SMELL I N THE FORWARD PART OF THE CABIN. AT THE SAME MOMENT THE CREW NOTICE A BURNING SMELL AS WELL. CREW DECLARED AN EMERGENC Y AND DIVERTED TO IND. THE SMELL SLOWLY STARTED TO DISSIPATE AFTER LANDING. MAINTENANCE REPLACED THE NR 2 DUEL HEAT EX CHANGER AND CLEANED COFFEE RESIDUE FROM ACM. 2 L 7 2 4F RT A56NM 2007091000131 20070910 00131 WP 2007 9 10 ABXA070275 1 20070825 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP EMERGENCY LIGHTS DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING PRE-DEPARTURE CHECK, EMERGENCY LIGHTS FOUND INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00-8. 2 L 7 2 4F A6WE 2007091000132 20070910 00132 SO 2007 9 10 C2XA07CL075 1 20070905 A 2750 3631101007 SELECTOR EMB 145 EMB145XR 3260214 SO TE FLAPS FAULTY A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 26141 12225 145733 CLE FLIGHT 2197 THE CREW REPORTED AFTER TAKEOFF THE GEAR RETRACTED NORMALLY BUT RECEIVED A LANDING GEAR WARNING CONTINUO USLY. MAINTENANCE INSPECTED AND REPLACED THE FLAP SELECTOR CONTROL ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2007091000137 20070910 00137 NM 2007 9 10 SWAA074278 1 20070829 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 245WN 32506 EEPLS LENS BROKEN AT ROW 3 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007091000143 20070910 00143 NM 2007 9 10 SWAA074281 1 20070829 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000147 20070910 00147 NM 2007 9 10 SWAA074268 1 20070829 A 3211 65605795 DRAG BRACE BOEING 737 7373L9 1384470 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED SERVICE CHECK, FOUND LEFT MLG LOWER DRAG BRACE BUSHING AND TEE FITTING CORRODED. REMOVED AND REPLACED DRAG BRACE PER MM. 2 L 7 2 4F RT A16WE 2007091000151 20070910 00151 NM 2007 9 10 2007UALA03491 1 20070830 A 7931 UNKNOWN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE ENG OIL PRESSURE UNKNOWN A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 787UA 26939 ENG OIL PRESS L LEFT ENGINE OIL PRESSURE BELOW THE RED LINE LIMIT WITH ENGINE RUNNING. ENGINE REPLACED AT ORD. SHOP TE ARDOWN REVEALED A FAILURE OF THE NR 2 BALL BEARING. A 2.5" CIRCUMFERENTIAL X 1" WIDE CHUNK WAS BROKEN OFF OF THE OUTER RACE. THE BEARING HAS BEEN RETURNED TO MANUFACTURER FOR MORE IN DEPTH ANALYSIS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007091000152 20070910 00152 NM 2007 9 10 2007UALA03492 1 20070830 A 3350 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 845UA 1585 CABIN EMERGENCY LIGHT FAULT EPSU INTERNAL LOAD RIGHT. REPLACED EPSU. 2 L 7 2 4F 4 F RT A28NM E40NE 2007091000158 20070910 00158 NM 2007 9 10 2007UALA03498 1 20070830 A 3510 OXYGEN SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 COCKPIT OXYGEN PRESSURE 1130 PSI. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091000160 20070910 00160 NM 2007 9 10 SWAA074283 1 20070829 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500A S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007091000165 20070910 00165 NM 2007 9 10 SWAA074276 1 20070829 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 578 S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091000168 20070910 00168 NM 2007 9 10 SWAA074280 1 20070829 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 360 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND STRINGER 15L CRACKED AT BS 360. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007091000174 20070910 00174 NM 2007 9 10 PIDA07042 1 20070823 A 3350 LIGHT BOEING 737 737228 13844AG NM CABIN MALFUNCTIONED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 252TR 23001 ABOVE L2 DOOR EMERGENCY LIGHT COMES ON WHEN AIRCRAFT POWER IS REMOVED. REPLACED LIGHT ASSEMBLY. SYSTEM OPS CHECKS GOOD IAW M/M 33-51-11. 2 L 7 2 4F RT A16WE 2007091000176 20070910 00176 NM 2007 9 10 SWAA074308 1 20070831 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 350 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 350, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000177 20070910 00177 NM 2007 9 10 SWAA074319 1 20070901 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 740 S19R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740, STR 19R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000184 20070910 00184 NM 2007 9 10 SWAA074314 1 20070831 A 5311 6545810 FRAME BOEING 737 7373H4 1384600 NM BS 312 S6L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 312, STR 6L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007091000187 20070910 00187 NM 2007 9 10 SWAA074326 1 20070901 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000189 20070910 00189 NM 2007 9 10 SWAA074341 1 20070903 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM BS 482A S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED MV3 CHECK, FOUND SHEAR TIE CRACKED AT BS 482A, STR 10L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007091000190 20070910 00190 NE 2007 9 10 MASA200700500 2 20070812 A 7230 COMPRESSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 ENGINE SEIZED A MASA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 07 650ML 7137 872140 ASH 7433 MHT-IAD ABORTED T/O DUE TO A NR 2 TR DISAGREE, AND POSSIBLE COMPRESSOR STALL. MX INSPECTED THE ENGINE, AND FOU ND IT TO BE SEIZED. MX IS CURRENTLY TROUBLESHOOTING. 2 L 7 2 4F 4 F RT A21EA E15NE 2007091000192 20070910 00192 SO 2007 9 10 C2XA07CL074 1 20070904 A 3397 WIRE EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHTS LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17928 145007 DURING ROUTINE MAINTENANCE THE RIGHT EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND RECONNECTED THE WIRE AT THE EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2007091000193 20070910 00193 NM 2007 9 10 SWAA074357 1 20070903 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000194 20070910 00194 NM 2007 9 10 SWAA074337 1 20070902 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000195 20070910 00195 NM 2007 9 10 SWAA074313 1 20070831 A 5311 6546530 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000197 20070910 00197 NM 2007 9 10 SWAA074345 1 20070901 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000199 20070910 00199 NM 2007 9 10 SWAA074347 1 20070901 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM BS 520 S8RL CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000201 20070910 00201 NM 2007 9 10 SWAA074351 1 20070901 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM BS 747 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000204 20070910 00204 NM 2007 9 10 SWAA074348 1 20070901 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000207 20070910 00207 NM 2007 9 10 SWAA074327 1 20070901 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000209 20070910 00209 NM 2007 9 10 SWAA074336 1 20070902 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM BS 727D S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000211 20070910 00211 NM 2007 9 10 SWAA074340 1 20070903 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 482A S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 482A, STR 10L. REMOVED AND REPLACED STRINGER CLI P PER SRM. 2 L 7 2 4F RT A16WE 2007091000212 20070910 00212 NM 2007 9 10 SWAA074361 1 20070904 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 727C S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091000213 20070910 00213 WP 2007 9 10 UPS07850536 1 20070801 A 5511 RIB DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 LT HORIZ STAB L/E RIB CRACKED, AFT LWR, STA XFS 140. REPAIRED CRACKED RIB ON L/H HORIZ. STAB L/E AT STA XFS 140 BY INSTALLING DOUBLER IAW SRM 55-02-00, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007091000218 20070910 00218 SO 2007 9 10 SIMA200724304 1 20070829 A 3260 852701 PROXIMITY SENSOR EMB 135 EMB135KL 3260302 SO ZONE 200 FAILED A SIMA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SW 21 821AE 13344 145577 ABNORMALLY LOUD SQUEAL FROM FRONT OF AIRCRAFT, POST INSPECTION FOUND NOSE LANDING GEAR DOOR SEQUENCE PROXIMITY SHOWED IN CLOSE POSITION. REMOVED AND REPLACED NOSE LANDING GEAR DOOR SEQUENCE PROXIMITY SENSOR IAW EMB 32-63-03. OPERATIONAL C HECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007091000219 20070910 00219 EU 2007 9 10 CPCP20070089 1 20070730 A 5320 DOUBLER AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 4AE 244 LT FR 36 STR 14 DOUBLER CORRODED. LT FR 36 STR 14 DOUBLER REPLACED AS PER SRM 51-25-01 AND SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007091000221 20070910 00221 WP 2007 9 10 UPS07850537 1 20070822 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FS 1766 L28R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 STA 1766 L28R CORROSION OUT OF LIMITS. REMOVED L28R FROM STA 1690-1766 IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT LONGERON L28R AT STA 1690-1766 IAW SRM 53-05-03 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007091000222 20070910 00222 WP 2007 9 10 UPS07850538 1 20070821 A 5310 DOUBLER DOUG DC8 DC873F 302199F WP FS 1720 L28R FAILED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 FOUND INTERNAL DOUBLER CUT IN TWO PLACES L28R, STA 1720. REMOVED INTERNAL DOUBLER AT STA 1720, L28R IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR INTERNAL DOUBLER AT STA 1720 L28R IAW DWG 5649328, AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007091000223 20070910 00223 WP 2007 9 10 UPS07850539 1 20070814 A 5530 STIFFENER DOUG DC8 DC873F 302199F WP VERTICAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 SMALL HORIZ STIFFENER CORRODED/EXFOLIATED INSIDE VERT STAB REAR SPAR, THROUGH ACCESS PNL 55. REMOVED DAMAGED STIFFENER ON VERT STAB INSIDE ACCESS PNL 55 IAW SRM 51-01-21. FABRICATED AND INSTALLED REPAIR STIFFENER IAW SR M 51-01-21 AND DWG 5611400. 2 L 7 4 4F RT 4A25 2007091000224 20070910 00224 WP 2007 9 10 UPS07850551 1 20070829 A 3350 LIGHT DOUG DC8 DC873F 302199F WP COCKPIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01-2 AND CHECKS GOOD PER SAME. 2 L 7 4 4F RT 4A25 2007091000225 20070910 00225 WP 2007 9 10 UPS07850552 1 20070726 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FS 1220-1260 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 L-35R CORRODED FROM STA 1220-1260 ON INBD LONGERON. REMOVED AND REPLACED LONGERON AND BATHTUB FITTIN GS FROM STA 1210 TO 12 0 IAW SRM 53-2-0 AND DWG 5750322. 2 L 7 4 4F RT 4A25 2007091000226 20070910 00226 NM 2007 9 10 UPS07M50561 1 20070710 A 5753 HINGE DOUG MD11 MD11F 3023600 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C RT O/B FLAP I/B HINGE (WING MOUNTED) LOWER ATTACHMENT LUG O/B FOUND BORE AND SPOT FACES CORROSION AS M ARKED. BORE AND SPOTFACE CORROSION REMOVED, EXCEED LIMIT CMM 57-44-08 PG 602-607 R58. ORG DIA 0.644" THK 0.461" FINAL D IA 0.706" THK 0.435" MATL REMOVED 0.026" MAX ALLOW DIA 0.709" MIN ALLOW THK 0.720". FPI C/O AND FOUND NO CRACK EVIDENT. FLAP PEENING C/O ON REWORKED AREA BSOPM20-11-01R58. BUSHING FAB CMM57-44-08 R58. BUSHING INSTL PER CMM57-44-08R58. 2 L 7 3 4F RT A22WE 2007091000227 20070910 00227 NM 2007 9 10 UPS07M50562 1 20070710 A 5753 HINGE DOUG MD11 MD11F 3023600 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C RT O/B FLAP I/B HINGE (WING MOUNTED) LOWER ATTACHMENT LUG I/B FOUND BORE AND SPOT FACES CORROSION AS M ARKED. BORE AND SPOTFACE CORROSION REMOVED, EXCEED LIMIT CMM 57-44-08 PG 602-607 R58 ORG DIA 0.644" THK 0.460" FINAL DI A 0.707" THK 0.441" MATL REMOVED 0.019" MAX ALLOW DIA 0.709" MIN ALLOW THK 0.720". FPI C/O AND FOUND NO CORROSION AND C RACK EVIDENT. FLAP PEENING C/O BSOPM20-11-01 R58. BUSHING FAB CMM57-44-08R58. BUSHING INSTL PER CMM 57-44-08R58. 2 L 7 3 4F RT A22WE 2007091000229 20070910 00229 SO 2007 9 10 SIMA200724701 1 20070831 A 3320 BR900022 BALLAST EMB 135 EMB135LR 3260305 SO ZONE 200 BURNED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 727AE 15947 145326 BURNED SMOKE ODOR IN CABIN. REMOVED AND REPLACED ROW 3A LIGHTING BALLAST IAW EMB AMM 33-21-03. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007091000231 20070910 00231 2007 9 10 RU3A0707 4 20070808 A 3497 WIRE BEECH 300 300BEECH 1152930 CE DISPLAY SHORTED E RU3A O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 15 72 FF7 PILOT DU1 POPPED CB, CREW COULD DETECT BURNING EQUIPMENT ODOR. FOUND SHORTED WIRE AT CONNECTOR ON DISPLAY UNIT. 2 L 7 2 4T A24CE 2007091000232 20070910 00232 NM 2007 9 10 AWXA200701046 1 20070829 A 3350 321454 POWER SUPPLY BOEING 737 73733A 1384673 NM EMERGENCY LIGHTS FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 164AW 23625 PHX - EEL - LOG NR 4159565 - MX REPORTED ROWS 19-23 LEFT EMERGENCY SEAT LIGHTS INOP. MX REPLACED AFT BATTERY POWER SUPP LY. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2007091000233 20070910 00233 NM 2007 9 10 AWXA200701051 1 20070831 A 2611 RAI2800M0706 CONTROL UNIT AIRBUS A319 A319132 3930340 NM SMOKE DETECTION FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 820AW 19924 2321 1397 PHX - OTH - LOG NR 7809886 - MX REPORTED SMOKE LAV AND CARGO DET FAULT ON ECAM. MX REPLACED THE SDCU, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007091000234 20070910 00234 EU 2007 9 10 AWXA200701028 1 20070826 A 3350 321454 POWER UNIT AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHTS FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 627AW 52823 1336 66 LAS - EEL - NR 4138710 - MX REPORTED AFT EPSU FAILS EMERG LIGHT TEST AND SELF-TEST. MX REPLACED THE AFT EPSU AND BATTER Y. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007091000235 20070910 00235 NM 2007 9 10 AWXA200701029 1 20070827 A 2560 P2070001214 FLASHLIGHT BOEING 737 7373G7 1384595 NM CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 307AW 24634 LAS - EEL - LOG NR 7824838 - FWD EMERGENCY FLASHLIGHT INOP. MX REPLACED FLASHLIGHT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2007091000236 20070910 00236 EU 2007 9 10 AWXA200701048 1 20070816 A 5340 D53112198201 FITTING AIRBUS 320 A320231 3930325 EU ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 SAL - MAJOR REPAIR - C-06 CHECK - NR 5985459, CORROSION ON CENTER FITTING IN R1 DOOR THRESHOLD SILL AREA, BS 709/FR16 - BS 808/FR 20, -Z 520. REPLACED CENTER FITTING IN R1 DOOR THRESHOLD SILL AREA, BS 709/FR16 - BS 808/FR 20, -Z 520 IAW A3 20 ARM 51-72-11. 2 L 7 2 4F RT A28NM 2007091000237 20070910 00237 EU 2007 9 10 AWXA200701049 1 20070829 A 5347 D53472190209 SEAT TRACK AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980131, CORROSION ON CABIN PASSENGER SEAT RAIL BEAM, BS 3043/FR 64 - BS 3158+5" / FR 66+3", -Y1292. REPLACED CABIN PASSENGER SEAT RAIL BEAM, BS 3043 / FR 64 - BS 3158+5" / FR 66+3", -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007091000240 20070910 00240 CE 2007 9 10 GUUA08220702 1 20070822 A 5540 10164001423 BRACKET BEECH 1900 1900D 1154162 CE RUDDER CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 38537 25044 UE158 AT SCHEDULED INSPECTION DISCOVERED LOWER RUDDER ATTACH BRACKET EXFOLIATED. REPLACED LOWER RUDDER BRACKET. 2 L 7 2 4T RT A24CE 2007091000243 20070910 00243 NM 2007 9 10 UIEA200700340 1 20070831 A 5510 HINGE FITTING BOEING 747 7472D7B 1384803 NM HORIZONTAL STAB CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 BS 2598 H/S RT RBL 40" REAR SPAR UPPER I/B OF HINGE FITTING OPEN HOLE. OVERSIZE TO 0.403", USED BACB30 US6K21Y BOLT. C ARRIED OUT NDT TEST OF THE OPEN OVERSIZE HOLE FOUND SATISFACTORY. 2 L 7 4 4F RT A20WE 2007091000244 20070910 00244 NM 2007 9 10 UIEA200700334 1 20070831 A 2510 PAN BOEING 747 7472D7B 1384803 NM COCKPIT SEAT CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 COCKPIT 2ND OBSERVER SEAT PAN CRACKED. REPAIRED IAW BOEING MESSAGE NR 1-497681686-1. 2 L 7 4 4F RT A20WE 2007091000249 20070910 00249 NM 2007 9 10 CALA0700481 1 20070831 A 5230 65C36231Y2 SKIN BOEING 737 7373T0 1384582 NM C2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A 1/2 INCH CRACK IN C-2 DOOR OUTER SKIN AT DOOR HANDLE CUTOUT. A DOUBLER WAS INSTALLED IAW SRM 52-00-0 1, REPAIR 2. 2 L 7 2 4F RT A16WE 2007091000250 20070910 00250 NM 2007 9 10 ASAA0742010 1 20070830 A 5210 NAS110413 BOLT BOEING 737 7374Q8 138447Q NM R1 DOOR LOOSE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 R 1 DOOR WILL NOT OPEN. UPON INSPECTION, FOUND BOLT TO ROD END NOT ATTACHED, NUT MISSING. REATTACHED ROD END INSIDE DO OR, TESTED PER AMM 52 41 00. 2 L 7 2 4F RT A16WE 2007091000251 20070910 00251 NE 2007 9 10 AMTA200700396 2 20070820 A 7200 ENGINE BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE NR 1 UNKNOWN A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 314TZ 30640 NR 1 ENGINE CONTROL LIGHT ON. PERFORMED FIM PROCEDURE 73-06-00-810-801 NO FAULTS NOTED OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A16WE E2GL 2007091000252 20070910 00252 NM 2007 9 10 AALA20071538 1 20070814 A 3350 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 787AL 30010 JFK - EMERGENCY LIGHT AT SEAT ROW 12 INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 12. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091000253 20070910 00253 NM 2007 9 10 AALA20071539 1 20070814 A 3350 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 787AL 30010 JFK - EMERGENCY LIGHT AT SEAT ROW 13 INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 13. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091000254 20070910 00254 NM 2007 9 10 AALA20071540 1 20070814 A 3350 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 787AL 30010 JFK - EMERGENCY LIGHT AT SEAT ROW 26G INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 26G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091000255 20070910 00255 NM 2007 9 10 AALA20071541 1 20070813 A 3350 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 767AJ 33539 DFW - EMERGENCY LIGHT AT SEAT ROW 13D INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091000257 20070910 00257 NM 2007 9 10 AALA20071537 1 20070814 A 3397 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 787AL 30010 JFK - EMERGENCY LIGHT AT SEAT ROW 11 INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 11. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091000258 20070910 00258 2007 9 10 AALA20071543 4 20070814 A 2565 HOOK AND LOOP DOUG DC9 DC982 3022082 WP L2 DOOR SLIDE INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 MSP - EMERGENCY DOOR SLIDE AT LEFT NUMBER TWO DOOR GIRT BAR HOOK AND LOOP INOPERATIVE. REPLACED EMERGENCY DOOR SLIDE AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007091000260 20070910 00260 NM 2007 9 10 HALA0700358 1 20070831 A 2410 60B40161 IDG BOEING 767 7673CB 1385187 NM LEFT FAILED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 590HA 8075 33467 LEFT IDG DRIVE LIGHT AND EICAS ON STEADY. COMPLIED WITH QRH AND DISCONNECTED LEFT GENERATOR. REMOVED AND INSPECTED LEF T IDG OIL FILTER, NO CONTAMINTATION FOUND. REMOVED AND REPLACED LEFT IDG PER AMM 24-11-01-004 AND 24-11-01-404. LEFT I DG, OPS CHECK OK AND LEAK CHECK OK. 2 L 7 2 4F RT A1NM 2007091000262 20070910 00262 NM 2007 9 10 HALA0700361 1 20070902 A 3697 CONNECTOR BOEING 767 767332 1382001 NM HP CONTROLLER SHORTED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 594HA 23275 RT ENG BLEED AIR VALVE OFF LIGHT ILLUM WITH SWITCH 'ON' AND ENGINE RUNNING. DUCT PRESSURE WAS ZERO, ENG WAS STARTED AND DUCT PRESSURE WAS VERIFYED OK, DMI#75140. OK TO CONTINUE PER C 36-11-2. INSTALL SHORTING CONNECTOR PLUG ON THE HP CON TROLLER. 2 L 7 2 4F RT A1NM 2007091000264 20070910 00264 NM 2007 9 10 AMTA200700378 1 20070808 A 7500 1074925 REGULATOR BOEING 737 73783N 13844HI NM NR 1 BLEED SYS UNSERVICEABLE A AMTA O OTHER O OTHER NR NOT REPORTED 1 GL 11 310TZ 28243 DUCT PRESSURE SPLIT ON CLIMB AT 10,000 FT L14/ R34 20K, L13 R32, 30K, L13, R24, AT CRUISE 380K L16/R23. REMOVED AND REP LACED NR 1 ENG BLEED AIR REGULATOR IAW 36-11-03-4. 2 L 7 2 4F RT A16WE 2007091000265 20070910 00265 NM 2007 9 10 AMTA200700385 1 20070812 A 5320 INTERCOSTAL BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE BS 330-340 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 STA 330-340, LBL 21, FLOORBEAM INTERCOSTAL LARGE AREA OF CORROSION AND 4 EA DRILLED OUT FASTENERS. REMOVED CORROSION AT LBL 21, STA 330-360, AREA FOUND WITHIN LIMIT, ORG MAT .125, REMOVED .006 IAW SRM 53-00-01 TREATED AND PRIMED IAW SRM 51 -20-01, REMOVED 4 EA FASTENERS IAW SRM 51-40-02. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007091000266 20070910 00266 NE 2007 9 10 AMTA200700391 2 20070810 A 7310 163521538 LINE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE UNSERVICEABLE A AMTA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 560TZ 33525 FUEL LINE LEAKING RT ENGINE. INLET LINE TO GEAR DRIVEN FUEL PUMP. REMOVED AND REPLACED RT ENGINE INLET TO GEAR DRIVEN FUEL PUMP IAW MM 73-11-06-4. RAN ENGINE OPS CK GOOD. NO LEAKS IAW MM 77-00-00. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007091000267 20070910 00267 NM 2007 9 10 AWXA200701052 1 20070815 A 5340 69366002 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5987960, CRACKED STRINGER TIE CLIP, BS 277, S10R. REPLACED STRINGER TIE CLIP, S10R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007091000269 20070910 00269 NM 2007 9 10 AWXA200701054 1 20070814 A 5754 65C2679912 SKIN BOEING 737 7373G7 1384595 NM NR 6 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5987801, RIGHT WING NR 6 SLAT LOWER SURFACE HAS 3 CRACKS, SS 292 - SS 327. REPAIRE D RIGHT WING NR 6 SLAT LOWER SURFACE, SS 292 - SS 327 IAW B737-300 SRM 57-43-01-2R6, FIGURE 201. 2 L 7 2 4F RT A16WE 2007090700007 20070907 00007 EA 2007 9 7 TRAX200701255 1 20070829 A 5220 SHAFT CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 CREW ESCAPE HATCH OUTER HANDLE SHAFT CORRODED. CREW ESCAPE HATCH REMOVED AND REPLACED AS PER CMM 52-22-03 - CREW ESCA PE HATCH HANDLE OPS TEST C/O IAW 52-22-03. 2 L 7 2 4F RT A21EA 2007090700012 20070907 00012 EA 2007 9 7 TRAX200701260 1 20070830 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 F/A FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007090700045 20070907 00045 NM 2007 9 7 2007UALA03399 1 20070826 A 2611 SMOKE DETECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CARGO BAY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 528UA 25018 NR 2 FORWARD CARGO COMPARTMENT SMOKE DETECTOR INOPERATIVE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007090700052 20070907 00052 EA 2007 9 7 TRAX200701267 1 20070831 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 839AS 7284 MAIN ASD JAMMED SHUT. 2 L 7 2 4F RT A21EA 2007090700062 20070907 00062 NM 2007 9 7 2007UALA03157 1 20070813 A 3350 59192 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 STAIRS TO UPPER DECK EMERGENCY LIGHTS INOP. *S/D* SECURED EEL LIGHTING CONNECTOR AT TOP OF STAIRS. EMERGENCY LIGHTING CHECKD NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700063 20070907 00063 NM 2007 9 7 2007UALA03158 1 20070811 A 3350 20131A CHARGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 RIGHT OVERWING AFT TWO EMERGENCY LIGHTS ARE INOP. *S/D* REPLACED BATTERY CHARGER. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700067 20070907 00067 NM 2007 9 7 2007UALA03179 1 20070814 A 3350 78671 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 SEATS 5J FWD, 48ABC & 54HJK EMERGENCY LIGHTS ARE INOPERATIVE. *S/D* REPLACED LAMPS IN THREE SEAT POSITIONS. EEL TESTE D READY FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700079 20070907 00079 NM 2007 9 7 2007UALA03198 1 20070816 A 3350 7945243 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 WALL EEL INOP: BETWEEN MID LAVS & DOOR 5L CROSS AISLE. *S/D* FOUND LOOSE CONNECTION AND SECURED, OP CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700080 20070907 00080 NM 2007 9 7 2007UALA03199 1 20070816 A 3350 GE1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 WALL EEL INOP: LEFT SIDE MID GALLEY. *S/D* REPLACED LAMP, OP CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700086 20070907 00086 EU 2007 9 7 2007UALA03406 1 20070826 A 3500 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE OXYGEN SYSTEM LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 420UA 489 CREW REPORT: CREW O2 APPEARS TO LEAK. SHOWS 40 PSI AND AA REG LOW PR WARNING. 2 L 7 2 4F 4 F RT A28NM E40NE 2007090700087 20070907 00087 2007 9 7 2007UALA03407 4 20070825 A 2565 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 DOOR 1L SLIDE CAME OFF DOOR. REPLACED DOOR SLIDE 1L AS A PRECAUTION. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700088 20070907 00088 NM 2007 9 7 2007UALA03408 1 20070825 A 3397 FEEDER CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 365UA 24534 TRACK LIGHTING ON FLOOR BETWEEN 15-21 AND AFT GALLEY INOPERATIVE. POWER FEEDER CABLE LOOSE. RE-SECURED POWER FEEDE R CABLE-OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700089 20070907 00089 NM 2007 9 7 2007UALA03409 1 20070827 A 5753 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU TE FLAP GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 RIGHT HAND OUTBOARD FORE FLAP HAS A 1.250 INCH GOUGE ON LEADING EDGE 13.250 INCHES FROM OUTBOARD EDGE. REPLACED RT FOR EFLAP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700112 20070907 00112 NM 2007 9 7 2007UALA03418 1 20070825 A 3350 LIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN DETACHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 937UA 26668 AFT GALLEY ESCAPE PATH LIGHTS TOTALLY DETACHED FROM FLOOR. REPAIRED AND SECURED AFT GALLEY EEL LIGHTS. OPS CHECK GOOD , NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700117 20070907 00117 SO 2007 9 7 C2XA07ON019 1 20070828 A 2432 32845001 BATTERY EMB 145 EMB145XR 3260214 SO ZONE 100 OVERHEATED A C2XA B EMER. DESCENT M OVER TEMP CR CRUISE 1 SW 27 12569 9133 1914 145630 FLIGHT 7770 - OAK TO LAX - FLIGHT CREW DECLARED EMERGENCY IN FLIGHT DUE TO BATTERY NR 2 OVERHEAT TO 80 DEGREES F. CREW LANDED IN LAX WITHOUT INCIDENT. MX PERSONNEL REMOVED AND REPLACED NR 2 MAIN BATTERY OPERATIONALLY CHECKED WITH NO DEFEC TS AND A/C WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2007090700121 20070907 00121 EA 2007 9 7 TRAX200701265 1 20070830 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA BS 364 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 CORROSION FOUND ON TOP OF SEAT RAIL BETWEEN FS 364 AND 15.409 + 128 AT RBL 9 AND LBL 9. REMOVED CORROSION ON TOP OF SEA T RAIL BTW FS 364 & 409 + 128 AT RBL 9 & CBL 9 AS PER SRM 51-21-06 ALODINE APPLIED AS PER 51-21-11 2 L 7 2 4F RT A21EA 2007090700122 20070907 00122 EA 2007 9 7 TRAX200701266 1 20070831 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 976EV 7601 CABIN EMERGENCY TRACK LIGHTING AT SEAT 10CD HAS A SEGMENT INOP. (ELECTROLUMINESCENT FLOOR PROXIMITY EMERGENCY ESCAPE PA TH MARKING SYSTEM) 2 L 7 2 4F RT A21EA 2007090700123 20070907 00123 NM 2007 9 7 2007UALA03423 1 20070826 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 2A BOTH LIGHT ASSY'S. REPAIRED WIRES AT CONNECTOR. OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700124 20070907 00124 NM 2007 9 7 2007UALA03424 1 20070826 A 3350 582240 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 RIGHT HAND EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP 2 EA FWD LIGHT ASSY'S. REPLACED POWER SUPPLY. OP CHECKS NORMALL Y. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700147 20070907 00147 NM 2007 9 7 2007UALA03446 1 20070828 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 616 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 LONGITUDINAL FLOORBEAM CRACKED AT BS 616 RBL 45-47, MID CABIN AREA. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED LONG ITUDINAL FLOORBEAM SECTION. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091000007 20070910 00007 NM 2007 9 10 SWAA074323 1 20070901 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 313 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER 4R CRACKED AT BS 313. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007091000008 20070910 00008 NM 2007 9 10 SWAA074322 1 20070901 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 380 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER 15R CRACKED AT BS 380. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007091000023 20070910 00023 2007 9 10 SWAA074393 4 20070905 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 208WN 29856 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007091000024 20070910 00024 2007 9 10 SWAA074413 4 20070905 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 762SW 27876 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007091000026 20070910 00026 NM 2007 9 10 SWAA074401 1 20070905 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM BS 885 S24-25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 885, BETWEEN STR 24R TO STR 25R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000031 20070910 00031 NM 2007 9 10 SWAA074421 1 20070905 A 5753 SKIN BOEING 737 737317 138447P NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND LEFT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER END. REPAIRED FLAP PER SR M. 2 L 7 2 4F RT A16WE 2007091000037 20070910 00037 NM 2007 9 10 SWAA074383 1 20070905 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM BS 277 S11L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 277, STR 11L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007091000039 20070910 00039 NM 2007 9 10 SWAA074372 1 20070904 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM BS 616 S17R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 616, STR 17R. REMOVED AND REPLACED FRAME CHORD PER MM. 2 L 7 2 4F RT A16WE 2007091000041 20070910 00041 NM 2007 9 10 SWAA074380 1 20070905 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM BS 747 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000047 20070910 00047 NM 2007 9 10 SWAA074406 1 20070905 A 5310 6546958 CREASE BEAM BOEING 737 7373A4 1384585 NM BS 492 S17R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 492, STR 17R. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2007091000083 20070910 00083 NM 2007 9 10 2007UALA03451 1 20070828 A 5522 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ELEVATOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 LEADING EDGE OF LEFT OUTBOARD ELEVATOR UPPER SURFACE IS CHIPPED ABOVE HINGE AT 240. 2 L 7 2 4F 4 F RT A1NM E24NE 2007091000095 20070910 00095 SO 2007 9 10 C2XA07IA187 1 20070824 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11544 835 835 145557 MCI - FLIGHT 621, DURING POST-FLIGHT INSPECTION THE LEFT HAND OVERWING EMERGENCY EXIT IDENTIFIER WAS FOUND TO BE INOPERA TIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY, OPERATIONAL CHECKED WITH NO DEFECTS, A ND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007091000112 20070910 00112 EU 2007 9 10 2007UALA03476 1 20070830 A 5754 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 5 SLAT DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 470UA 1427 SLAT NR 4 & 5 ARE DAMAGED ON LEADING EDGE. REMOVED NR 4 SLAT AND INSTALLED REPAIRED UNIT. REWORKED DENT ON NR 5 LE SLA T AND FIXED LE WING DAMAGE REPAIRED AND INSPECTED FOR CRACKS. ALL ITEMS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007091000126 20070910 00126 NE 2007 9 10 NOCA14907 2 20070829 A 7230 COMPRESSOR BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535* NE RT ENGINE STALLED A NOCA A UNSCHED LANDING R M J PARTIAL RPM/PWR LOSS OVER TEMP WARNING INDICATION CL CLIMB 1 EA 15 754NA 29381 RIGHT ENGINE MULTIPLE COMPRESSOR STALLS AFTER POWER REDUCTION AT 1000 FT TEMP AT TAKEOFF WAS 845 DEG MAX AFTER POWER RED UCTION THE TEMP DROPPED NORMALLY, THEN STARTED STALLING MAX TEMP WAS 991 DEG C. ITEM REMAINS OPEN. 2 L 7 2 4F 4 F RT A2NM E12EU 2007091000134 20070910 00134 SO 2007 9 10 C2XA07CL073 1 20070828 A 3350 744436 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15973 145159 DURING ROUTINE MAINTENANCE THE EXIT SIGN AT THE RIGHT AFT DOOR WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EXIT SIG N. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007091000136 20070910 00136 NM 2007 9 10 SWAA074284 1 20070829 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 408WN 27895 DURING SCHEDULED 6Y CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STA 101.9 AND STA 129.50. REPAIR ED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007091000141 20070910 00141 NM 2007 9 10 SWAA074287 1 20070829 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000157 20070910 00157 2007 9 10 2007UALA03497 4 20070830 A 2565 FITTING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 1R GIRT BAR OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 DOOR 1R DOES NOT HAVE ARM LIGHT WHEN DOOR IS ARMED AND CREW STATES THAT DOOR DOES NOT FEEL NORMAL WHEN ARM SELECTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091000196 20070910 00196 NM 2007 9 10 SWAA074338 1 20070902 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000198 20070910 00198 NM 2007 9 10 SWAA074356 1 20070903 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM BS 520 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000202 20070910 00202 NM 2007 9 10 SWAA074329 1 20070901 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM BS 747 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000208 20070910 00208 NM 2007 9 10 SWAA074363 1 20070904 A 5311 6546595 FRAME BOEING 737 737317 138447P NM BS 727A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000215 20070910 00215 EU 2007 9 10 SIMA200724301 1 20070828 A 2750 708372 ACTUATOR SAAB SF340 340B 7860101 EU ZONE 600 FAILED A SIMA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SW 21 250AE 22458 15151 340B250 FLAPS SELECTED TO 15 DEGREES, NO MOVEMENT. AFTER 10 SECONDS MOVE FLAP TO ZERO, AFTER 30 SECONDS THE FLAP CYCLED TO 7 DE GREE THEN TO ZERO. REMOVED AND REPLACED RIGHT FLAP ACTUATOR IAW SAAB AMM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED T O SERVICE. 2 L 7 2 4T RT A52EU 2007091000217 20070910 00217 SO 2007 9 10 SIMA200724302 1 20070829 A 3220 UNKNOWN EMB 145 EMB145LR 3260212 SO NLG UNKNOWN A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 654AE 145437 RECEIVED LANDING GEAR AIR/GROUND FAIL MESSAGE, RETURNED TO DFW. RESERVICED NOSE LANDING GEAR IAW EMB AMM 32-20-01. OPE RATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007091000228 20070910 00228 CE 2007 9 10 HYIA070902001 1 20070901 A 2400 CN358950 MASTER SWITCH CESSNA 402 402C 207590R CE COCKPIT INOPERATIVE E HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 2714B 875 875 402C0210 AVIONIC MASTER SWITCH INOPERATIVE DATE CODE 0633. REMOVED AND REPLACED INOPERATIVE SWITCH WITH NEW SWITCH DATE CODED 06 33. 1 L 7 2 3O A7CE 2007091000238 20070910 00238 NM 2007 9 10 AWXA200701050 1 20070830 A 5730 SKIN BOEING 737 7373G7 1384595 NM ZONE 600 DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 PIT - MAJOR REPAIR, TEAR AND DELAMINATION ON RIGHT WING LEADING EDGE SKIN, WS 538. REPAIRED RIGHT WING LEADING EDGE SKI N, WS 538 PER US AIRWAYS EA (ENGINEERING AUTHORIZATION). 2 L 7 2 4F RT A16WE 2007091000242 20070910 00242 NM 2007 9 10 UIEA200700330 1 20070831 A 5753 PANEL BOEING 747 7472D7B 1384803 NM ZONE 200 CONTAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 LT WING T/E I/B PANEL FOUND WATER. REPLACE LHW T/E I/B FIXED PAL AS PER SRM 51-10-01 AND SRM 51-30-02, AND PANEL REPAIR IAW BOEING MESSAGE 31-516595696-1 TO 1-516595696-4. 2 L 7 4 4F RT A20WE 2007091000245 20070910 00245 NM 2007 9 10 UIEA200700339 1 20070831 A 5330 SKIN BOEING 747 7472D7B 1384803 NM BS 780 DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 FX EXTERIOR SKIN DENT AS MARKED APPR, 1" SQ IN AT BS 780 S47-R. REINSTALLED A REPAIRED DOUBLER AS PER SRM 53-30-03 DETA ILS AS PER SWS SHOWN. 2 L 7 4 4F RT A20WE 2007091000247 20070910 00247 NM 2007 9 10 UIEA200700331 1 20070831 A 5522 SKIN BOEING 747 7472D7B 1384803 NM RT ELEVATOR DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 HORIZONTAL STAB RT I/B ELEVATOR L/E UPPER SKIN DENTED. REPAIRED IAW BOEING MESSAGE SR 1-514407012. 2 L 7 4 4F RT A20WE 2007091000259 20070910 00259 NM 2007 9 10 AALA20071546 1 20070814 A 3397 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 MIA - EMERGENCY LIGHT AT SEAT ROWS 3DG AND 4DG INOPERATIVE. SECURED LOOSE CONNECTOR AT SEAT 3D FOR EMERGENCY LIGHT AT S EAT ROWS 3DG AND 4DG. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091000271 20070910 00271 NM 2007 9 10 AWXA200701056 1 20070814 A 5313 6545767120 STRINGER BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5987893, STRINGER CRACKED AT EXISTING REPAIR, BS 500C, S16L. REPAIRED STRINGER, BS 500C, S16L IAW AWA ER 03-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2007091000272 20070910 00272 NM 2007 9 10 AWXA200701057 1 20070816 A 5320 654795711 STRAP BOEING 737 7373G7 1384595 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5988011, CORROSION ON AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL WEB INNER CHORD STRAP, BS 793 - BS 847, S25R. REPLACED AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL WEB INNER CHORD STRAP, BS 793 - B S 847, S25R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007091000274 20070910 00274 NM 2007 9 10 AWXA200701059 1 20070822 A 5340 146N674818 STRINGER CLIP BOEING 757 7572S7 1384962 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 MCN - MAJOR REPAIR - C-11 CHECK - NR 5988669, CRACKED DOOR CUT OUT SURROUND STRUCTURE "T" CLIP, BS 1681.8, S11R. REPLAC ED DOOR CUT OUT SURROUND STRUCTURE "T" CLIP, BS 1681.8, S11R IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007091000275 20070910 00275 EU 2007 9 10 AWXA200701060 1 20070823 A 5321 D5367180500200 FLOOR PANEL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980147, CORROSION ON CABIN FLOORBOARD 261FF, BS 3158/FR 66 - BS 3257/FR 68, +Y1292 TO +Y1732. REPLACED CABIN FLOORBOARD 261FF, BS 3158/FR 66 - BS 3257/FR 68, +Y1292 TO +Y1732 IAW AWA TASK CARD C1D25318 . 2 L 7 2 4F RT A28NM 2007091000277 20070910 00277 EU 2007 9 10 AWXA200701062 1 20070823 A 5320 D53472190202 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980129, CORROSION ON CABIN FLOORBEAM, BS 3101/FR 65, +Y765. REPLACED CABIN FLOORB EAM, BS 2883/FR 60 TO BS 3158/FR 66, +Y765 I/A/W A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007091000278 20070910 00278 EU 2007 9 10 AWXA200701063 1 20070823 A 5320 D5347212202 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980122, CORROSION ON CABIN FLOORBEAM, BS 3158/FR 66 - BS 3207 / FR 67, +Y1292. RE PLACED CABIN FLOOR BEAM, BS 3158/FR 66 - BS 3207/FR 67, +Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007091000279 20070910 00279 EU 2007 9 10 AWXA200701064 1 20070822 A 5347 D570147203 SEAT TRACK AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5986011, CORROSION ON CABIN SEAT TRACK, BS 1725/FR 39 - BS 1810/FR 41, -Y1292. REP LACED CABIN SEAT TRACK, BS 1590/FR 36 - BS 1810/FR 41, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007091000280 20070910 00280 NM 2007 9 10 HALA0700362 1 20070822 A 5320 145T86293 FLOOR SUPPORT BOEING 767 76733A 1385209 NM FUSELAGE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 PANEL SUPPORT TEE P/N 145T8629-3 CORRODED. PART REPLACED WITH NEW ITEM. CPC APPLIED. 2 L 7 2 4F RT A1NM 2007091000281 20070910 00281 NM 2007 9 10 HALA0700363 1 20070827 A 5314 KEELBEAM BOEING 767 76733A 1385209 NM BS 960-1006 MISREPAIRED A HALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 13 580HA 28140 CORROSION AROUND RIVNUT INSTALLATION ON KEELBEAM FAIRING PANEL FLANGES, BOTH LEFT AND RIGHT FLANGES FROM STA 960 AND 100 6. REMOVED RIVNUTS REPLACED BY SRM REPAIR ANCHOR NUT PLATES AFTER CORROSION REMOVAL SRM 53-05-12. THOROUGH APPLICATION OF CPC ON THE KEEL BEAM INCLUDING BOTH SIDES OF FAIRING PANEL FLANGES PRIOR TO FAIRING PANEL INSTALLATION. 2 L 7 2 4F RT A1NM 2007091000282 20070910 00282 NM 2007 9 10 HALA0700364 1 20070904 A 5347 143T521711 SEAT TRACK BOEING 767 76733A 1385209 NM BS 592 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 SECTION 43 SEAT TRACK CORROSION RBL 88.50 STN 592 CORROSION BEYOND SRM LIMITS, REPAIRED BE SEAT TRACK REPLACEMENT. REPL ACEMENT P/N 143T5217-11. 2 L 7 2 4F RT A1NM 2007091000283 20070910 00283 NM 2007 9 10 HALA0700366 1 20070904 A 5347 143T521711 SEAT TRACK BOEING 767 76733A 1385209 NM BS 560 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 SECTION 43 SEAT TRACK CORROSION RBL 88.50 STN 560 CORROSION BEYOND SRM LIMITS, REPAIRED BE SEAT TRACK REPLACEMENT. REPL ACEMENT P/N 143T5217-11. 2 L 7 2 4F RT A1NM 2007091000284 20070910 00284 NM 2007 9 10 HALA0700365 1 20070904 A 5347 143T521711 SEAT TRACK BOEING 767 76733A 1385209 NM BS 560 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 SECTION 43 SEAT TRACK CORROSION RBL 88.50 STN 560.5, CORROSION BEYOND SRM LIMITS, REPAIRED BE SEAT TRACK REPLACEMENT. R EPLACEMENT P/N 143T5217-11. 2 L 7 2 4F RT A1NM 2007091000285 20070910 00285 NM 2007 9 10 HALA0700367 1 20070904 A 5347 143T521711 SEAT TRACK BOEING 767 76733A 1385209 NM BS 597 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 SECTION 43 SEAT TRACK CORROSION LBL 11 STN 597.5. CORROSION BEYOND SRM LIMITS, REPAIRED BE SEAT TRACK REPLACEMENT. REP LACEMENT P/N 143T5217-11. 2 L 7 2 4F RT A1NM 2007091000286 20070910 00286 NM 2007 9 10 HALA0700368 1 20070904 A 5347 143T521711 SEAT TRACK BOEING 767 76733A 1385209 NM BS 565 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 SECTION 43 SEAT TRACK CORROSION LBL 11 STN 565. CORROSION BEYOND SRM LIMITS, REPAIRED BE SEAT TRACK REPLACEMENT. REPLA CEMENT P/N 143T5217-11. 2 L 7 2 4F RT A1NM 2007091000287 20070910 00287 NM 2007 9 10 HALA0700369 1 20070904 A 5347 143T521711 SEAT TRACK BOEING 767 76733A 1385209 NM BS 592 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 SECTION 43 SEAT TRACK CORROSION RBL 88.50 STN 592 CORROSION BEYOND SRM LIMITS, REPAIRED BE SEAT TRACK REPLACEMENT. REPL ACEMENT P/N 143T5217-11. 2 L 7 2 4F RT A1NM 2007091000288 20070910 00288 EU 2007 9 10 CPCP20070087 1 20070730 A 5320 FLOOR SUPPORT AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 4AE 244 RT FR 36-38 FLOOR SUPPORT CORRODED. RT FRAME 36-38 FLOOR SUPPORT REPLACED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007091100001 20070911 00001 NM 2007 9 11 UIEA200700351 1 20070905 A 7810 NOZZLE BOEING 747 7472D7B 1384803 NM EXHAUST DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 NR 4 ENGINE EXHAUST NOZZLE EXTERIOR SKIN DENTED AT 0700 TO 0900. NDT CHECKED NIL CRACK DENT AREA WITHIN LIMIT AMM 78-11 -01 PAGE 601. 2 L 7 4 4F RT A20WE 2007091100005 20070911 00005 CE 2007 9 11 GUUA05150701 1 20070515 A 5220 NAS76A3107P BUSHING BEECH 1900 1900D 1154162 CE EMERGENCY EXIT FROZEN A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 87551 UE206 AT SCHEDULED FLEET CAMPAIGN INSPECTION: LEFT EMERGENCY EXIT DOOR INTERNAL BEARING BUSHING AT HANDLE FROZEN. REPLACED B USHING. 2 L 7 2 4T RT A24CE 2007091100006 20070911 00006 CE 2007 9 11 GUUA04300702 1 20070430 A 5210 MS166241075 RETAINER BEECH BEECH 1900 1900D 1154162 CE HANDLE ASSY LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 81556 UE239 CABIN DOOR HANDLE BROKEN. RESECURED CABIN DOOR OUTER HANDLE. 2 L 7 2 4T RT A24CE 2007091100007 20070911 00007 CE 2007 9 11 GUUA04090701 1 20070409 A 5260 1295140591 CABLE ASSY BEECH BEECH 1900 1900D 1154162 CE AIRSTAIR DOOR BROKEN A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 87551 UE206 CAMS ON FWD PASSENGER DOOR WILL NOT TURN. REPLACED AIRSTAIR DOOR FORWARD LOWER CABLE ASSEMBLY. 2 L 7 2 4T RT A24CE 2007091100008 20070911 00008 NM 2007 9 11 QXEA200701371 1 20070903 A 2931 APT1750004000SW INDICATOR DHAV DHC8 DHC8202 2809007 NM HYD PRESSURE MALFUNCTIONED A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 367PH 22318 511 SEA - ON AFTERSTART CHECKSLIST STANDBY HYDRAULIC PRESSURE NR 1 AND NR 2. NR 2 STANDBY HYDRAULIC PRESSURE INDICATING 260 0/2700 PSI AFTERSTART. REPLACED NR 2 STANDBY PRESSURE TRANSMITTER. NO HELP NOTED. REPLACED DUAL HYDRAULIC PRESSURE IN DICATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091100010 20070911 00010 NM 2007 9 11 QXEA200701374 1 20070831 A 5270 INDICATION SYS BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 408QX 4050 RNO FLIGHT NR 2256: RT REAR FUSELAGE DOOR MASTER WARNING. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE DOOR A ND C/W TEST OF THE AFT DOOR WITH NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091100011 20070911 00011 NM 2007 9 11 QXEA200701376 1 20070903 A 2760 3958001005 DUMP VALVE BOMBDR DHC8 DHC8402 1390042 NM SPOILERS MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 408QX 9544 9544 4050 SEA FLIGHT NR 2438: SELECTING FLIGHT TAXI TO FLIGHT, INBD LIGHTS DO NOT ILLUMINATE OR EXTEND. FOLLOWED CHECKLIST, COULD NOT CLEAR FAULT. ROLL INBD SPOILERS ON RIGHT SIDE DOES NOT EXTEND FOR A SECOND, THEN RETRACTS LEAVING ONLY OUTBD SPOIL ERS EXTENDED. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE REMOVED AND REPLACED BOTH OF THE LIFT DUMP VALVES FOR THE INBOAR D ROLL SPOILERS IAW Q400 AMM 27-62-01, PGS 401-407. PERFORMED OPS CHECK OF GROUND SPOILER SYSTEM IAW TASK 27-62-00-710- 801. OPS CHECKS GOOD. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091100015 20070911 00015 NM 2007 9 11 UIEA200700337 1 20070831 A 5245 ACCESS PANEL BOEING 747 7472D7B 1384803 NM ZONE 100 DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 AIR COND, BAY ACCESS PANEL 192HR EXT SURFACE FOUND SKIN DELAMINATION. AIR COND BAY ACCESS PANEL 192HR REPAIRED WITH PRE -PRED FABRIC AS PER MESSAGE NR 1-497468248-2. 2 L 7 4 4F RT A20WE 2007091100016 20070911 00016 NM 2007 9 11 UIEA200700329 1 20070831 A 5311 FRAME BOEING 747 7472D7B 1384803 NM BS 800 S17L CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 BS 800 S17 LT ONE FASTENER HOLE FOUND CRACK ON FWD INNER CHORD ANGLE. REPLACEMENT PER BOEING CONTROL NO PO24708. 2 L 7 4 4F RT A20WE 2007091100019 20070911 00019 NM 2007 9 11 UIEA200700328 1 20070830 A 7830 STRUCTURE BOEING 747 747243B 1384830 NM THRUST REVERSER DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 NR 2 ENGINE OUTBOARD REVERSER EXTERIOR SKIN HAS A 7.5 INCH BY 6.0 INCH DENT IN UPPER AREA OF TRANSLATING COWL. PERMANEN T REPAIR ACCOMPLISHED AS PER GE CF6-50 ENGINE MANUAL 78-32-01, REPAIR 003. ALSO, REFERENCE ATLAS AIR XEO NR 78-082907. 2 L 7 4 4F A20WE 2007091100020 20070911 00020 NM 2007 9 11 UIEA200700327 1 20070830 A 5280 STRUCTURE BOEING 747 747243B 1384830 NM LT MLG DOOR DEBONDED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 LT WING GEAR LOWER STRUT DOOR, AFT LOWER END, PREVIOUS REPAIR, EDGE IS SEPARATING. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 12 SHEET 1, 2 AND 3. ALSO, REFERENCE ATLAS AIR XEO NR 52-082907. 2 L 7 4 4F A20WE 2007091100021 20070911 00021 2007 9 11 QXEA200701372 2 20070831 A 7261 ENGINE BOMBDR DHC8 DHC8402 1390042 NM OVERSERVICED A QXEA O OTHER W B J INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 NM 09 401QX 4031 PDX FLIGHT: ON DESCENT THROUGH 11,000 FT, FA REPORTED PUNGENT 'BURNING TIRE' ODOR MOST EVIDENT BETWEEN ROWS 2 AND 5. TH E CREW COULD SLIGHTLY DETECT AN ODOR ON THE FLIGHT DECK. NO CB'S POPPED AND ALL ENGINE INDICATIONS APPEAR NORMAL. MAIN TENANCE FOUND THE ENGINES TO BE OVERSERVICED. DE-SERVICED TO APPROPRIATE LEVELS. BOROSCOPE NR 1 ENGINE. NO DEFECTS. GROUND RAN BLEEDS ON AT VARIOUS POWER SETTINGS FOR 20 MINUTES. NO BURNING TIRE ODOR NOTED. NO PARTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091100023 20070911 00023 EA 2007 9 11 QXEA200701368 1 20070901 A 5270 895001 PROXIMITY SENSOR CNDAIR CL600 CL6002C10 1390015 EA CARGO DOOR OUT OF ADJUST A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 600QX 10005 PDX - FLIGHT 2565 (PDX-ONT), AFTER TAKEOFF DURING CLIMB, RECEIVED A AFT CARGO DOOR WARNING MESSAGE. NO LOSS OF CABIN PR ESSURE. CIRCLED FOR 30 MINUTES TO BURN OFF FUEL AND RETURNED TO PDX AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE ADJUSTED THE PX-102 PROX SENSOR IAW AMM 52-70-02-400-802-A02. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007091100024 20070911 00024 SO 2007 9 11 GUUA08160703 1 20070816 A 3350 1013073 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A GUUA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 29 285AS 120265 FLIGHT: 9287 FLL/GGT DURING PREFLIGHT, DISCOVERED ONE WHITE EMERGENCY LIGHT ON THE FLOOR INOPERATIVE. REPLACED AISLE MA RKER LIGHT. 2 L 7 2 4T RT A31SO 2007091100026 20070911 00026 NM 2007 9 11 AMTA200700395 1 20070820 A 3150 INDICATION SYS BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE ENGINE MALFUNCTIONED A AMTA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 314TZ 30640 AFTER LANDING, ENGINE CONTROL LIGHT ILLUMINATED ON NR 1 ENGINE. PERFORMED BITE CHECK IAW FIM 73-06-00-810-801 CHECKED E EC HARNESS FOR SECRUITY RAN ENG NO DEFECTS NOTED OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A16WE E2GL 2007091100027 20070911 00027 NM 2007 9 11 AMTA200700370 1 20070730 A 4900 425404 CHARGER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE APU UNSERVICEABLE A AMTA K NONE J WARNING INDICATION IN INSP/MAINT 1 GL 11 522AT 29330 EICAS MESSAGE (APU BTY CHARGER). REMOVED AND REPLACED (APU BATTERY CHARGER) IAW MM CH 24-31-04, OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007091100029 20070911 00029 NM 2007 9 11 AMTA200700408 1 20070827 A 3350 D71701100 BATTERY PACK BOEING 757 757* NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHTS INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 552TZ 32586 EXTERIOR EMERGENCY EXIT LIGHT JUST AFT OF R-4 DOOR IS INOPERATIVE. REMOVED AND REPLACED RT AFT EMERGENCY BATTERY PACK I AW AMM 33-51-07-2. OPS CHECKS GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007091100030 20070911 00030 NM 2007 9 11 QXEA200701389 1 20070904 A 2420 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM AC BUSS UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 408QX 4050 SEA FLIGHT 2312: AFTER PUSHBACK, RT AC BUSS CAUTION LIGHT REMAINED ON. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE TROUBLE SHOT PER FIM 24-20-00-810-806. PERFORMED OPS TEST OF AC VARIABLE FREQUENCY GENERATOR SYSTEM IAW AMM 24-21-00-710-801. OPS TEST GOOD, NO DEFECTS NOTED. RT AC BUSS CAUTION LIGHT DID NOT ILLUMINATE. NO PARTS REPLACED. AIRCRAFT RETURNED T O SERVICE. 2 H 7 2 4T RT A13NM 2007091100032 20070911 00032 EU 2007 9 11 AWXA200701066 1 20070823 A 5320 D53480043202 SILL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980130, CORROSION ON THE L2 DOOR CUT OUT LOWER SILL, BS 3158/FR 66, +Y1465. REPAI RED THE L2 DOOR CUT OUT LOWER SILL, BS 3158/FR 66, +Y1465 IAW A320 SRM 53-41-14 FIGURE 201. 2 L 7 2 4F RT A28NM 2007091100033 20070911 00033 NM 2007 9 11 QXEA200701382 1 20070829 A 2100 UNKNOWN DHAV DHC8 DHC8202 2809007 NM A/C PACK N UNKNOWN A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 369PH 513 PDX FLIGHT NR 2142 AIR CONDITIONING PACK HOT LIGHT DURING CRUISE WITH CABIN/FLIGHT COMPARTMENT IN AUTO MODE. FOLLOWED C HECKLIST AND LIGHT EXTINGUISHED. C/W FUNCTIONAL TEST OF THE TEMP CONTROL SYSTEM IAW AMM 21-60-00-720-801. OPERATION CH ECK GOOD. COULD NOT DUPLICATE PROBLEM. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091100034 20070911 00034 NM 2007 9 11 QXEA200701379 1 20070704 A 2900 CIRCUIT BREAKER DHAV DHC8 DHC8202 2809007 NM HYD SYSTEM TRIPPED A QXEA O OTHER O OTHER AP APPROACH 1 NM 09 353PH 496 SEA - WHEN SELECTING NR 1 STANDBY HYDRAULIC PRESSURE ON DURING APPROACH CHECKLIST NR 1 STANDBY HYDRAULIC PRESSURE INDICA TED ZERO. AFTER FLAP SELECTION INDICATOR STILL READ ZERO. MAIN PRESSURE INDICATED NORMALLY AND NO LIGHTS ILLUMINATED. ALL COCKPIT BREAKERS NORMAL. MAINTENANCE INSPECTED AND FOUND CIRCUIT BREAKER 2931 IN THE RIGHT AC CONTRACTOR BOX POPPE D. RESET PER GMM 5-18-0. C/W SPU OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091100035 20070911 00035 NM 2007 9 11 QXEA200701380 1 20070806 A 3150 INDICATION SYS DHAV DHC8 DHC8202 2809007 NM NR 2 ENGINE MALFUNCTIONED A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 347PH 480 SEA - DURING FLIGHT THERE IS A POWER LEVER SPLIT OF APPROXIMATELY 1", THROUGHOUT THE ENTIRE RANGE OF MOVEMENT. NR 2 POW ER LEVER LEADS NR 1. DURING START NR 2 ENGINE MANUAL CAUTION LIGHT ILLUMINATED WHICH WAS RESET PER THE EMERGENCY ABNORM AL CHECKLIST. INSPECTED ENGINE CONDITION PANEL AND FOUND NR 2 ECU FLAGGES. RESET ENGINE CONDITION PANEL, VERIFIED NR 1 AND NR 2 ENGINE RIGGING. NO ADJUSTMENT MADE. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVIC E. 2 H 7 2 4T RT A13NM 2007091100036 20070911 00036 NM 2007 9 11 QXEA200701381 1 20070813 A 2930 SENSOR DHAV DHC8 DHC8202 2809007 NM PUMP TEMP MALFUNCTIONED A QXEA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 358PH 506 SEA FLIGHT NR 2189, WHEN NR 1 STANDBY HYDRAULIC PUMP PRESSURE TURNED ON NR 1 STANDBY HYDRAULIC PUMP HOT CAUTION LIGHT. WHEN PUMP TURNED OFF PER CHECKLIST, LIGHT REMAINED ILLUMINATED. SWAPPED STANDBY PUMP TEMP SENSOR TO SPARE IAW AMM 29-11 -17, PAGE 501. OPERATIONAL CHECK GOOD. PLACED ON RSI. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091100039 20070911 00039 NM 2007 9 11 QXEA200701391 1 20070904 A 2997 SOCKET BOMBDR DHC8 DHC8402 1390042 NM PRESSURE SWITCH DAMAGED A QXEA O OTHER J WARNING INDICATION TO TAKEOFF 1 NM 09 407QX 4049 SEA FLIGHT NR 2262: ELEVATOR PRESSURE CAUTION ILLUMINATED AT ROTATION ON TAKEOFF. C/W EMERGENCY ABNORMAL CHECKLIST. CA UTION LIGHT EXTINGUISHED ON TOUCHDOWN. MAINTENANCE REPAIRED SOCKET FOR NR 1 SYSTEM PRESS SWITCH. C/W FUNCTIONAL TEST O F NR 3 SYSTEM. HYD OPS TEST GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091100040 20070911 00040 NM 2007 9 11 QXEA200701392 1 20070731 A 3350 LIGHT BOMBDR DHC8 DHC8402 1390042 NM CABIN MALFUNCTIONED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 421QX 4149 PDX FLIGHT NR 2359: DURING BOARDING, EMERGENCY LIGHTS ACTIVATED AND REMAINED ON AFTER SWITCH WAS CYCLED. MAINTENANCE PE RFORMED OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM IAW TASK 33-51-00-710-801. OPS CHECK NORMAL. NO PARTS REPLACED . AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091100041 20070911 00041 WP 2007 9 11 07FDEA03336 1 20070904 A 5712 RIB DOUG DC10 DC1010F 3022111 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 RT WING TIP CRACKS, 1.5" LONG ON EXTERNAL SKIN XW 928, YW 799. CONTINUED CRACK ON INT OLD REPAIR ON FRAME XW 928, YW 79 9. REPAIRED AREA IAW SRM 57-00-01 FIG 10 VOL I. 2 L 7 3 4F A22WE 2007091100044 20070911 00044 EU 2007 9 11 07FDEA03339 1 20070904 A 5311 A53970781200 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 CORROSION ON FRAME 57 INNER FLANGE AT STR 14 RT. REPAIR PERFORMED BY REWORK IAW EA 6-5316-92212 AND RAS/DAHAM/4020097/2 005 ISS B. 2 L 7 2 4F RT A35EU 2007091100045 20070911 00045 EU 2007 9 11 07FDEA03340 1 20070904 A 5320 COVER AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 CORROSION ON TORSION BOX COVER PLATE AT FRAME 57, STRG 15 RT. REPAIR PERFORMED BY REWORK AND FLAP PEENING IAW EA 6-5316 -92212 AND RAS/DAHAM/4020097/2005 ISS B. 2 L 7 2 4F RT A35EU 2007091100047 20070911 00047 EU 2007 9 11 07FDEA03342 1 20070904 A 5730 A57340085 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 FOUND CORROSION ON TOP SKIN PANEL NR 3 LT, NEAR RIB 25-28 AT T/E, OUT OF SRM LIMIT. REPAIR PERFORMED BY BLEND OUT, REPL ACEMENT OF AFFECTED FASTENERS AND FLAP PEENING IAW EA 6-5720-92224 AND RAS/BAE/1001906/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091100049 20070911 00049 EU 2007 9 11 07FDEA03344 1 20070904 A 5320 A53981113 SHEAR PLATE AIRBUS A300 A300F4622R 3930360 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 CRACKED SHEAR PLATE AT FRAME 79, STRG 26 LT AND RT. REPAIR PERFORMED BY INSTALLATION OF NEW PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091100056 20070911 00056 NM 2007 9 11 CALA0700476 1 20070830 A 5330 6545774 SKIN BOEING 737 7373T0 1384582 NM BS 727E CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A 1" CRACK IN SKIN JUST AFT OF STA 727E, S24L. A DOUBLER AND TRIPLER WERE INSTALLED IAW SRM 53-00-01, FIGURE 201, REPAIR 31. 2 L 7 2 4F RT A16WE 2007091100062 20070911 00062 EA 2007 9 11 SWIA200718629 1 20070827 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 408SW 7055 CAPTAINS SIDE WINDOW CRACKED WHILE AIRCRAFT WAS SITTING AT THE GATE. FLIGHT NR 3995, REPLACED LEFT SIDE WINDOW IAW MM 5 6-12-01. 2 L 7 2 4F RT A21EA 2007091100063 20070911 00063 EA 2007 9 11 SWIA200718630 1 20070827 A 2913 887055 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 NM 07 408SW 10710 3945 7055 HYDRAULIC SYSTEM 2 RESERVOIR INDICATES EMPTY. FLIGHT NR 3995, REPLACED NR 2 EDP. 2 L 7 2 4F RT A21EA 2007091100065 20070911 00065 EA 2007 9 11 SWIA200718632 1 20070823 A 2497 TERMINAL BLOCK CNDAIR CL600 CL6002B19 1900309 EA COCKPIT SHORTED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 07 416SW 7089 ELECTRICAL SMOKE FROM THE FIRST OFFICER'S CB PANEL DURING DESCENT INTO SLC. FLIGHT NR 3922, REPLACED TERMINAL BLOCK NR 12 AND TERMINAL ENDS IAW AMM 20-00-00. 2 L 7 2 4F RT A21EA 2007091100066 20070911 00066 SO 2007 9 11 SWIA200718633 1 20070823 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN BROKEN A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 296SW 120325 FLIGHT NR 3697, EMERGENCY EXIT LIGHT AT ROW 9 IS BROKEN. REPLACED EMERGENCY EXIT SIGN WITH A SERVICEABLE LIGHT. OPS CH ECK GOOD. 2 L 7 2 4T RT A31SO 2007091100068 20070911 00068 EA 2007 9 11 SWIA200718635 1 20070713 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 719SK 10188 STA 280 FLOORBEAM SUPPORT IS CRACKED AT LBL9, FOUND AT C-CHECK. INSTALLED REPAIR PARTS AND BEAM AT STA 280 PER CRJ7/9 S RM 51-42-06-001-001 AND REO:670-53-11-242. 2 L 7 2 4F RT A21EA 2007091100069 20070911 00069 EA 2007 9 11 SWIA200718636 1 20070702 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SW 7034 STA 280 FLOOR SUPPORT IS CRACKED ON LT SIDE AND HAS INTERGRANULAR CORROSION, FOUND AT C-CHECK. REPLACED STA 280 FLOOR S UPPORT AT LBL9 TO RBL 9 PER CRJ200 SRM 51-42-07 PGS 12 AND 13. 2 L 7 2 4F RT A21EA 2007091100071 20070911 00071 EA 2007 9 11 SWIA200718638 1 20070702 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SW 7034 FS 280 LBL 9 UPPER FLOOR SUPPORT ANGLE HAS CRACK AT RADIUS. FOUND AT C-CHECK, REPLACED AFT FLOOR ANGLE PER CRJ REO:601R -53-11-137 AND 138. 2 L 7 2 4F RT A21EA 2007091100073 20070911 00073 NM 2007 9 11 QXEA200701390 1 20070905 A 3150 LIGHT BOMBDR DHC8 DHC8402 1390042 NM MASTER CAUTION INTERMITTENT A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 416QX 4083 PDX FLIGHT NR 2463: MASTER CAUTION LIGHT INOP. MAINTENANCE COULD NOT DUPLICATE. MASTER CAUTION LIGHT WORKS NORMALLY. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091100074 20070911 00074 EA 2007 9 11 SWIA200718641 1 20070702 A 5755 BOLT CNDAIR CL600 CL6002B19 1900309 EA RT WING SPOILER CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SW 7034 RIGHT WING SPOILERON HAS CORRODED BOLTS ON SPOILERON HINGE, FOUND AT C-CHECK. REPLACED CORRODED BOLTS ON FLIGHT SPOILER ON HINGE PER AMM 20-21-00-910-801. 2 L 7 2 4F RT A21EA 2007091100076 20070911 00076 CE 2007 9 11 GUUA09050701 1 20070905 A 3260 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE LT MLG OUT OF ADJUST A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 29 190YV UE190 FLIGHT: 9243 NAS/FLL, DURING FLIGHT LANDING GEAR RED UNSAFE LIGHT FLICKERED SEVERAL TIMES. ADJUSTED LEFT LANDING GEAR U PLOCK SWITCH. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 2007091100078 20070911 00078 EA 2007 9 11 SWIA200718643 1 20070702 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SW 7034 RIGHT FORWARD ENGINE MOUNT YOKE BEARING IS CORRODED, FOUND AT C-CHECK. REPLACED RIGHT ENGINE MOUNT BEARING, P/N 601-370 15-8 S/N RJ/SLC/121806. 2 L 7 2 4F RT A21EA 2007091100079 20070911 00079 EA 2007 9 11 SWIA200718644 1 20070702 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA COCKPIT WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SW 7034 PILOT SEAT TRACKS HAVE ELONGATED HOLES AND ARE WORN, FOUND AT C-CHECK. REPLACED PILOT SEAT TRACK PER CRJ200 SRM 51-42-2 1 PG 17-19. 2 L 7 2 4F RT A21EA 2007091100082 20070911 00082 SO 2007 9 11 GUUA08180701 1 20070818 A 3260 SENSOR EMB 120 EMB120ER 3260203 SO MLG DIRTY A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 29 268AS 120202 FLIGHT: 9166 NAS/FLL, DURING FLIGHT LANDING GEAR RED "A" GEAR LIGHTS FLASH ON. CLEANED LEFT AND RIGHT MAIN LANDING GEAR SENSORS. LANDING GEAR OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A31SO 2007091100084 20070911 00084 EU 2007 9 11 COEA0707902 1 20070815 A 2130 UNKNOWN AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE CABIN PRESSURE UNKNOWN A COEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 13 902FX 175 DURING CLIMB OUT AT CPR ON FLIGHT NR 8788 THE PILOT NOTICED THAT THE CABIN WAS NOT PRESSURIZING AT 1000 FT. THE CREW RE CEIVED THE MASTER WARNING. THE CREW ELECTED TO RETURN TO DEPARTURE. NO EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED WI THOUT INCIDENT. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007091100085 20070911 00085 NM 2007 9 11 AMTA200700374 1 20070804 A 2560 BATTERY BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE FLASHLIGHT DISCHARGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 305TZ 30706 F/A AFT RIGHT J/S FLASHLIGHT BATTERY LOW. REMOVED AND REPLACED BATTERY AS REQUIRED. OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A16WE E2GL 2007091100086 20070911 00086 EU 2007 9 11 COEA0703901 1 20070730 A 5753 S5751014800200 GUIDE AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE LT WING TE FLAP CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 901FX 172 CORROSION FOUND DURING HEAVY CHECK. LT WING OB FLAP CAM GUIDE NR 4 AT RIB 16 HAS AREA OF LEVEL 2 CORROSION. REMOVED AN D REPLACED FLAP CAM GUIDE NR 4 AT RIB 16. FABRICATED REPAIR SCHEME IAW SRM 57-53-20. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007091100088 20070911 00088 EU 2007 9 11 CPCP20070090 1 20070730 A 5320 THRESHOLD AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 4AE 244 LT BETWEEN FRAME 36-39 THRESHOLD CORRODED. THRESHOLD LT BETWEEN FRAME 36-39 REPLACED AS PER SRM 51-25-03 THRESHOLD FABR ICATED ON NRWC 181406. 2 H 7 2 4T RT A53EU 2007091100090 20070911 00090 EU 2007 9 11 COEA0705901 1 20070730 A 5740 S57210609200 MOUNT FITTING AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE LT WING AILERON DAMAGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 901FX 172 DAMAGE FOUND DURING HEAVY CHECK. LT WING AILERON HINGE FITTING AT RIB 24 ACCIDENTAL DAMAGE AT IB AND OB LUGS. DAMAGE B LENDED OUT IAW ATR/SRI DO/TS-3041/07-8984 WITH REFERENCE TO SRAS DO/ TS-3041/07 4181. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007091100097 20070911 00097 2007 9 11 AMTA200700375 4 20070803 A 3422 312BS1011 CHARGER BOEING 737 73783N 13844HI NM UNSERVICEABLE A AMTA O OTHER O OTHER CL CLIMB 1 GL 11 310TZ 14589 28243 ISFD DISPLAY BLANK. REMOVED AND REPLACED THE DBC IAW 34-24-00, ISFD. OPS CHECKS GOOD. OK FOR SERVICE. (K) 2 L 7 2 4F RT A16WE 2007091100098 20070911 00098 CE 2007 9 11 GUUA08140701 1 20070814 A 5540 10164001415 ATTACH BRACKET BEECH 1900 1900D 1154162 CE RUDDER CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81538 23458 UE199 AT SCHEDULED INSPECTION DISCOVERED TOP RUDDER ATTACH BRACKET EXFOLIATED. REPLACED TOP RUDDER BRACKET. 2 L 7 2 4T RT A24CE 2007091100099 20070911 00099 CE 2007 9 11 GUUA08210701 1 20070821 A 3200 UNKNOWN BEECH 1900 1900D 1154162 CE MLG UNKNOWN A GUUA O OTHER O OTHER AP APPROACH 1 SO 29 81538 UE199 FLIGHT: 9142 MIA/EYW DURING APPROACH, LANDING GEAR CIRCUIT BREAKER POPPED WHEN GEAR HANDLE MOVED TO THE DOWN POSITION. CONTINUED TO EYW LANDED WITHOUT INCIDENT. PERFORMED LANDING GEAR OPERATIONAL CHECK SEVERAL TIMES UNABLE TO DUPLICATE. 2 L 7 2 4T RT A24CE 2007091100101 20070911 00101 CE 2007 9 11 GUUA08240701 1 20070824 A 3260 UNKNOWN BEECH 1900 1900D 1154162 CE MLG HANDLE UNKNOWN A GUUA O OTHER N FALSE WARNING CL CLIMB 1 SO 29 87554 UE227 FLIGHT: 9136 FLL/EYW AFTER TAKEOFF, THE LANDING GEAR HANDLE LIGHT REMAINED ILLUMINATED WITH THE LANDING GEAR RETRACTED. RETURNED TO FLL. LANDED WITHOUT INCIDENT. PERFORMED LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECKS NORMAL. 2 L 7 2 4T RT A24CE 2007091100103 20070911 00103 NM 2007 9 11 AMTA200700379 1 20070807 A 2150 A/C PACK BOEING 737 73783N 13844HI NM RIGHT UNKNOWN A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 314TZ 30640 RT PACK OVERHEAT LIGHT ON OVERHEAD WILL NOT RESET. PERFORMED PACK/ZONE TEMP. CONTR. BITE IAW MM 21-51-00-5. CONTRL NR 1 NO FAULTS. CONTR 2 SHOWS TCV. RESET CONTROLLER, OPS CHECK NORMAL. (K) 2 L 7 2 4F RT A16WE 2007091100104 20070911 00104 NM 2007 9 11 AMTA200700380 1 20070809 A 3350 LIGHT BOEING 737 73783N 13844HI NM GALLEY BROKEN A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 317TZ 28246 FWD GALLEY EGRESS WINDSCREEN PROX LIGHT ASSY BROKEN IN PIECES. REMOVED AND REPLACED LIGHT ASSY FOR FWD GALLEY EGRESS WI NDSCREEN PROX. OPS CHECKS NORMAL. (K) 2 L 7 2 4F RT A16WE 2007091100106 20070911 00106 NM 2007 9 11 UPS07450541 1 20070807 A 5322 SHEAR TIE BOEING 747 747212B 1384886 NM BS 900 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D BS 900 RT TENSION TIE STEEL PLATE FOUND SEM. M/DECK BS 900 RT TENSION TIE ATTACH STEEL PLATE REPA IRED. AS PER HX RS NR R53-25-35847 REPEAT INSPECTION IS REQUIRED AS PER UPS EO NR B747-5310-27440. 2 L 7 4 4F A20WE 2007091100110 20070911 00110 NM 2007 9 11 UPS07450545 1 20070808 A 5320 65B01837319 REVEAL BOEING 747 747212B 1384886 NM L1 DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D L1 DOOR FWD CUTOUT REVEAL NR 9 STOP FTG DOUBLER BULGED UP. M/D L1 DOOR FWD CUTOUT REVEAL NR 9 STO P FTG AREA SPLICE DOUBLER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007091100111 20070911 00111 NM 2007 9 11 UPS07450546 1 20070811 A 5311 FRAME BOEING 747 747212B 1384886 NM BS 400 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C E/E COMPT STA400 FRAME INNER CHORD FOUND CRACKED AT S44L, CRACK LENGTH 5/8". E/E COMPT BS 400 FRAME I NNER CHORD AT ABOVE STR 44L AREA REPAIRED AS PER SRM 51-40-04 FIG 3. 2 L 7 4 4F A20WE 2007091100117 20070911 00117 EU 2007 9 11 07FDEA03354 1 20070905 A 5320 STIFFENER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 FOUND CORROSION ON T-SECTION BETWEEN STRG 50-55 LT AT FRAME 39. ON PRESSURE BULKHEAD, SMALL CRACKS HAVE BEEN FOUND. TH E REPAIR CONSISTS IN CUTTING OUT THE TEE AND INSTALLING A NEW TEE WITH AN ANGLE AND A STRAP. A SPECIFIC REPAIR HAS BEEN INSTALLED FOLLOWING PRINCIPLES AS PER SRM 53-15-17/FIG 201. 2 L 7 2 4F RT A35EU 2007091100118 20070911 00118 EU 2007 9 11 07FDEA03355 1 20070905 A 5320 A53810948200 TEE FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 FOUND CORROSION ON T-SECTION BETWEEN STRG 50-55 LT AT FRAME 39. ON PRESSURE BULKHEAD, SMALL CRACKS HAVE BEEN FOUND. TH E REPAIR CONSISTS IN CUTTING OUT THE TEE AND INSTALLING A NEW TEE WITH AN ANGLE AND A STRAP. A SPECIFIC REPAIR HAS BEEN INSTALLED FOLLOWING PRINCIPLES AS PER SRM 53-15-17/FIG 201. ALL IAW EA 6-5315-92213 AND RAS/AS/0268/2005 ISSUE C. 2 L 7 2 4F RT A35EU 2007091100124 20070911 00124 2007 9 11 AMTA200700399 4 20070820 A 2565 SLIDE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE R1 DOOR UNWANTED DEPLOY A AMTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 11 519AT 27975 R-1 DOOR SLIDE INFLATED IN FWD GALLEY. REPLACED DOOR SLIDE IAW W/C 222R2505. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007091100125 20070911 00125 NM 2007 9 11 AMTA200700394 1 20070817 A 2560 BATTERY BOEING 737 73783N 13844HI NM FLASHLIGHT INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 315TZ 28245 REAR GALLEY LT SIDE FLASHLIGHT DID NOT BLINK. REMOVED AND REPLACED GALLEY FLASHLIGHT BATTERY, OPS CHECK GOOD. (K) 2 L 7 2 4F RT A16WE 2007091100126 20070911 00126 EA 2007 9 11 SWIA200718647 1 20070829 A 5610 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 367CA 10069 LEFT WINDSHIELD CRACKED ON CLIMB OUT, FLIGHT NR 4003. REPLACED LEFT WINDSHIELD IAW AMM 56-11-01, P/N NP-139321-13, S/N OFF 02122H5460. 2 L 7 2 4F RT A21EA 2007091100127 20070911 00127 EA 2007 9 11 SWIA200718648 1 20070903 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER DE DESCENT 1 NM 07 507CA 7796 FLT 2871, ON DESCENT, THE RIGHT COCKPIT WINDOW CRACKED. REPLACED SIDE WINDOW PER AMM 56-12-01, P/N OFF 601R33033-12, S/ N OFF 03106H2074. 2 L 7 2 4F RT A21EA 2007091100129 20070911 00129 EA 2007 9 11 SWIA200718650 1 20070828 A 3350 COVER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT MISSING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 702SK 10136 FLT 5821, "EMERGENCY EXIT" COVER IN GALLEY IS MISSING. REPLACED LENS COVER. 2 L 7 2 4F RT A21EA 2007091100130 20070911 00130 EA 2007 9 11 SWIA200718651 1 20070831 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA LEFT ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 494CA 7765 FLT 2805, BURNING ODOR WHEN LEFT PACK IS SELECTED. REPLACED LEFT AIR CYCLE MACHINE IAW AMM 21-51-10. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007091100131 20070911 00131 EA 2007 9 11 SWIA200718652 1 20070827 A 2530 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 962SW 7859 FLT 5860 - FLIGHT ATTENDANT REPORTS BURNING SMELL IN GALLEY. INSPECTED GALLEY HEAT, FAN, LIGHTS AND POTABLE WATER SYSTE M. COULD NOT DUPLICATE BURNING SMELL. 2 L 7 2 4F RT A21EA 2007091000020 20070910 00020 NM 2007 9 10 SWAA074366 1 20070902 A 5310 149A5510 CREASE BEAM BOEING 737 7377H4 1384404 NM BS 328-344 S17R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 737JW 27869 DURING SCHEDULED 8Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 328 AND BS 344, STR 17R. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007091000021 20070910 00021 NM 2007 9 10 SWAA074376 1 20070904 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 490WN 32476 EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007091000022 20070910 00022 NM 2007 9 10 SWAA074416 1 20070905 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 415WN 29836 EEPLS COVER LOOSE AT ROW 5 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007091000036 20070910 00036 NM 2007 9 10 SWAA074403 1 20070905 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM BS 500A S27L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007091000045 20070910 00045 NM 2007 9 10 SWAA074422 1 20070905 A 5320 6546568 STIFFENER BOEING 737 737317 138447P NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CORRODED AT BS 1016, BL 0. REMOVED AND REPLACED STIFF ENER PER SRM. 2 L 7 2 4F RT A16WE 2007091000049 20070910 00049 NM 2007 9 10 SWAA074391 1 20070905 A 3350 6556633 SIGN BOEING 737 7373H4 1384600 NM EMERGENCY EXIT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 LEFT OVERWING EMERGENCY EXIT SIGN MISSING. INSTALLED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007091000057 20070910 00057 NM 2007 9 10 SWAA074331 1 20070901 A 3350 101073 LENS BOEING 737 7373G7 1384595 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 FWD CABIN EMERGENCY EXIT SIGN MISSING LENS. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007091000062 20070910 00062 NM 2007 9 10 SWAA074324 1 20070901 A 3350 311500 LENS BOEING 737 7375H4 138449D NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 L2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007091000070 20070910 00070 NM 2007 9 10 SWAA074333 1 20070901 A 5330 6545765 SKIN BOEING 737 7377H4 1384404 NM BS 505-511 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 737JW 27869 DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE SKIN CORRODED BETWEEN BS 505 AND BS 511, RBL 3 AND LBL 3. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 2007091000071 20070910 00071 NM 2007 9 10 SWAA074250 1 20070828 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8LR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000072 20070910 00072 NM 2007 9 10 SWAA074259 1 20070828 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000073 20070910 00073 NM 2007 9 10 SWAA074249 1 20070828 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000078 20070910 00078 NM 2007 9 10 SWAA074256 1 20070828 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM BS 360 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000080 20070910 00080 NM 2007 9 10 SWAA074264 1 20070828 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 867 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007091000081 20070910 00081 NM 2007 9 10 SWAA074265 1 20070828 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 727B S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007091000084 20070910 00084 NM 2007 9 10 2007UALA03452 1 20070828 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEATS 1E & 2E UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 775UA 26947 EMERGENCY LIGHT STRIP AT SEATS 1E AND 2E COMING LOOSE. SECURED EEL STRIP AT ASSOCIATED SEATS. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007091000094 20070910 00094 NM 2007 9 10 2007UALA03462 1 20070829 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 290 GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 EXT FUSE SKIN GOUGED: STA 290 BETWEEN STR 3L & 4L, 3 EA GOUGES. MAJOR REPAIR ACCOMPLISHED: BLENDED GOUGES. FABRICATE D & INSTALLED EXTERNAL DOUBLER, TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091000106 20070910 00106 NM 2007 9 10 2007UALA03470 1 20070829 A 4920 ENGINE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 775UA 26947 CREW REPORTS APU AUTO SHUTDOWN WHILE AT THE GATE. AFTER TROUBLESHOOTING & DURING RESTART OF APU HAD A TAIL PIPE FIRE, S HUTDOWN APU. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007091000117 20070910 00117 2007 9 10 2007UALA03481 4 20070829 A 2565 BOTTLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE 5R DOOR SLIDE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26877 DOOR 5 RIGHT SLIDE CAME OFF. DOOR ASSIST BOTTLE NEEDS REPLACEMENT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007091000124 20070910 00124 2007 9 10 2007UALA03488 4 20070828 A 2565 HOSE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE ASPIRATOR FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 590UA 5353 28708 ASPIRATOR LEAKS. ON TROUBLESHOOTING FOUND DAMAGED INFLATION HOSE, WHICH SUPPOSEDLY HAPPENED DURING PACKING THEREBY INA CTIVATING . REPLACED HOSE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091000138 20070910 00138 NM 2007 9 10 SWAA074288 1 20070829 A 5753 6546486 WEDGE BOEING 737 7373A4 1384585 NM TE FLAPS DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD MID FLAP LOWER T/E WEDGE DISBONDED. REPAIRED WEDGE PER SRM. 2 L 7 2 4F RT A16WE 2007091000139 20070910 00139 NM 2007 9 10 SWAA074271 1 20070829 A 5311 6546525 FRAME BOEING 737 7373A4 1384585 NM BS 380 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000145 20070910 00145 NM 2007 9 10 SWAA074269 1 20070829 A 5311 6546593 FRAME BOEING 737 7373A4 1384585 NM BS 500A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000148 20070910 00148 2007 9 10 SWAA074279 4 20070829 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM R1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. REMOVED AND REPLACED GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2007091000150 20070910 00150 NM 2007 9 10 2007UALA03490 1 20070830 A 2900 UNKNOWN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE HYD SYTEM UNKNOWN A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 777UA 26916 CREW COMMENTS: RIGHT HYDRAULIC QTY DROPPED TO .40 IN FLT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007091000162 20070910 00162 NM 2007 9 10 SWAA074291 1 20070829 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 294 S12L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007091000170 20070910 00170 EU 2007 9 10 USAA070709 1 20070830 A 5310 BEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 185UW 1666 THE 1162/1292 BEAM SEGMENT BETWEEN FR C66 & 68 HAS CORROSION. PART REPLACED WITH LIKE PART PER SRM 53-41-14; CORR TASK JA-260-53500, DEFECT SIZE: 1 INCH SQ (2 EA). 2 L 7 2 4F RT A28NM 2007091000175 20070910 00175 NM 2007 9 10 SWAA074339 1 20070903 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM BS 497B S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 497B, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000181 20070910 00181 NM 2007 9 10 SWAA074318 1 20070901 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 804-813 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 804 AND BS 813, STR 19L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000183 20070910 00183 NM 2007 9 10 SWAA074325 1 20070901 A 5310 65458075 DOOR FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED MV4 CHECK, FOUND R1 DOOR CUTOUT FWD FRAME CENTER STUB FRAME CRACKED. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000205 20070910 00205 NM 2007 9 10 SWAA074349 1 20070901 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000214 20070910 00214 EU 2007 9 10 TRBA2007073 1 20070901 A 5610 NP1588014 WINDSHIELD AEROSP ATR72 ATR72212 8680945 EU COCKPIT CRACKED A TRBA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 29 440AM 440 DEVELOPED CRACK IN F/O'S WINDSHIELD DURING DEPARTURE CLIMBING (FROM SXM) THROUGH 4,000 FT FOR 10,000 FT. REMOVED AND RE PLACED F/O WINDSHIELD AS PER JIC NR 56-11-00. 2 H 7 2 4T RT A53EU 2007091000220 20070910 00220 NM 2007 9 10 TSAA0729047 1 20070823 A 2997 BACC45FT105S CONNECTOR BOEING 737 737210C 1384459 NM PRESSURE SWITCH FAILED A TSAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 834AL 20917 NON-ETOPTS CARGO FLIGHT 928 HNL-OGG, ON TAKE OFF, AFTER THE CREW RETRACTED THE LANDING GEAR, THE CREW NOTED HYDRAULIC QU ANTITY INDICATION DROPPED TO 2 GALLONS. AFTER FLAPS WERE RETRACTED, THE QUANTITY DROPPED DOWN TO 1.5 GALLONS AND THE CR EW ELECTED TO RETURN TO HNL. THE CREW LANDED IN HNL WITHOUT FURTHER INCIDENT. MAINTENANCE ADDED 1.5 GALLONS OF HYDRAUL IC FLUID TO THE RESERVOIR, OPERATED THE HYDRAULIC SYSTEM AND CHECKED FOR LEAKS. NO LEAKS WERE NOTED. MAINTENANCE ALSO FOUND THE NR 2 B SYSTEM PUMP LOW PRESSURE LIGHT INOPERATIVE AND RELEASED THE AIRCRAFT TO SERVICE PER MEL 29-5. THE AIRC RAFT WAS RETURNED TO SERVICE. THE MEL WAS CLEARED BY REPLACING THE LOW PRESSURE SWITCH CONNECTOR IAW AMM 29-12-31. 2 L 7 2 4F A16WE 2007091000230 20070910 00230 EA 2007 9 10 SIMA200724702 1 20070901 A 3250 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA NLG STEERING UNKNOWN A SIMA O OTHER J WARNING INDICATION CL CLIMB 1 SW 21 519AE 10131 RECEIVED STEERING INOPERATIVE MESSAGE ON EICAS, DECLARED EMERGENCY. 2 L 7 2 4F RT A21EA 2007091000241 20070910 00241 CE 2007 9 10 GUUA08200701 1 20070820 A 3260 H111541 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE MLG OUT OF ADJUST A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 29 81546 UE187 FLIGHT:9197 TPA/FLL - DURING FLIGHT, LANDING GEAR HANDLE LIGHT FLICKERS ON AND OFF. ADJUSTED LEFT MAIN LANDING GEAR UPL OCK SWITCH OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 2007091000246 20070910 00246 NM 2007 9 10 UIEA200700333 1 20070831 A 5315 FLOORBEAM BOEING 747 7472D7B 1384803 NM ZONE 200 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 FLOOR STRUCTURE BEAM WEB CRACKED. REPAIRED IAW BOEING MESSAGE NR 1-497681686-1. 2 L 7 4 4F RT A20WE 2007091000248 20070910 00248 NM 2007 9 10 UIEA200700338 1 20070831 A 3220 TORQUE LINK BOEING 747 7472D7B 1384803 NM NLG CHAFED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 NLG LOWER TORSION LINK FOUND CHAFING. BLEND OUT THE CHAFING AREA WITH MIN 20-1 BLEND-RATIO. 2 L 7 4 4F RT A20WE 2007091000256 20070910 00256 NM 2007 9 10 AALA20071542 1 20070814 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 796AN 30796 DFW - EMERGENCY LIGHT AT OVERHEAD LEFT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD LEF T NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091000270 20070910 00270 NM 2007 9 10 AWXA200701055 1 20070816 A 5311 6546541504 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5988022 & 5988023, FRAME CHORD CRACKED, BS 663.75, S3L AND S3R. REPAIRED FRAME CHO RD, BS 663.75, S3L AND S3R IAW B737-300 SRM 53-00-07-2R9, FIGURE 201. 2 L 7 2 4F RT A16WE 2007091100009 20070911 00009 NM 2007 9 11 QXEA200701373 1 20070831 A 3600 INDICATOR BOMBDR DHC8 DHC8402 1390042 NM BLEED SYS MALFUNCTIONED A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 413QX 4060 SJC FLIGHT NR 2404: ON PUSHBACK AS APU BLEED WAS TURNED OFF, OPEN LIGHT WILL NOT EXTINGUISH. AIRCRAFT RETURNED TO BLOCK . MAINTENANCE PERFORMED TEST OF THE APU BLEED AIR SYSTEM WITH NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091100012 20070911 00012 SO 2007 9 11 GUUA08160702 1 20070816 A 3231 DOOR EMB 120 EMB120ER 3260203 SO RT MLG UNSECURE A GUUA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 29 266AS 120188 FLIGHT:9259 AFTER TAKEOFF, PUTTING LANDING GEAR UP. RIGHT LANDING GEAR RED INDICATOR LIGHT STAYED ON. SECURED AFT INBO ARD LANDING GEAR DOOR. 2 L 7 2 4T RT A31SO 2007091100013 20070911 00013 NM 2007 9 11 UIEA200700332 1 20070831 A 5315 FLOORBEAM BOEING 747 7472D7B 1384803 NM BS 1220 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 FLOOR STRUCTURE BEAM WEB CRACKED. C/OUT AS PER BOEING MESSAGE NR 1-497681686-1. 2 L 7 4 4F RT A20WE 2007091100052 20070911 00052 EU 2007 9 11 07FDEA03348 1 20070904 A 5315 A53974554006 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 727FD 579 OLD REPAIR AT CROSSBEAM FRAME 63 IS NOT PERFORMED IAW SRM 53-10-15/FIG 207. SPLICE REPAIR RENEWED IAW SRM 53-10-15/FIG 207. 2 L 7 2 4F RT A35EU 2007091100060 20070911 00060 NM 2007 9 11 CALA0700480 1 20070830 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 767-907 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17328 23458 INSPECTION FOUND LT I/B SEAT TRACK CORRODED FROM STA 767-907, LBL 25. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 5 3-00-52. 2 L 7 2 4F RT A16WE 2007091100075 20070911 00075 SO 2007 9 11 GUUA09040701 1 20070904 A 3350 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 266AS 120188 FLIGHT: 9166 NAS/FLL, AFTER LANDING DISCOVERED THREE EMERGENCY LIGHTS NOT WORKING. ADJUSTED THREE EMERGENCY FLOOR LAMPS . 2 L 7 2 4T RT A31SO 2007091100089 20070911 00089 EU 2007 9 11 COEA0704901 1 20070730 A 5740 S57210615201 MOUNT FITTING AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE LT WING AILERON CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 901FX 172 DAMAGE TO LT WING REAR SPAR AILERON CENTER MOUNT LUG FOUND DURING HEAVY CHECK IN COE. REMOVED MOUNT AND BLENDED DAMAGE, FOUND BLENDED AREA TO BE OUT OF LIMITS. NEW FITTING WAS FABRICATED AND INSTALLED IAW ATR42 SRM. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007091100092 20070911 00092 SO 2007 9 11 RAIA00708043 1 20070826 A 2130 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN PRESSURE UNKNOWN A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 831HK 145232 FLT NR 8026 - EWR - AIRCRAFT CABIN PRESSURIZATION STARTED TO CLIMB WITH BOTH PACKS IN COLD. MAINTENANCE INSPECTED THE P ACK AND PRESSURIZATION SYSTEMS AND COULD FIND NO DEFECTS WITH EITHER SYSTEM. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007091100093 20070911 00093 SO 2007 9 11 RAIA00708041 1 20070824 A 2760 RELAY EMB 145 EMB145 3260210 SO SPOILERS FAULTY A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 805HK 145096 FLT NR 3506 - BDL - SPOILER FAIL MESSAGE ON TAXI. MAINTENANCE REMOVED AND REPLACED RELAY NR K0021. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2007091100107 20070911 00107 NM 2007 9 11 UPS07450542 1 20070807 A 5322 65B0961415 SHEAR TIE BOEING 747 747212B 1384886 NM BS 900 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D BS 900 LT TENSION TIE STEEL PLATE FOUND SEM. M/D LT BS 900 TENSION TIE STEEL PLATE REPAIRED AS PE R HX RS NR R53-25-35847 AND REPEAT INSPECTION IS REQUIRED AS PER UPS EO NR B747-5310-27440. 2 L 7 4 4F A20WE 2007091100121 20070911 00121 EU 2007 9 11 07FDEA03358 1 20070905 A 5310 A52170269200 DOOR FRAME AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 CRACKED FRAME SEGMENT ON BEAM 8 OF AFT CREW DOOR RT. REPAIR PERFORMED BY REPLACEMENT OF FRAME SEGMENT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091100128 20070911 00128 EA 2007 9 11 SWIA200718649 1 20070830 A 2150 GG670950093 ACM CNDAIR CL600 CL6002C10 1390015 EA RIGHT SMOKE A SWIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 762SK 10226 FLT 6056 - FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. REPLACED RIGHT ACM IAW CRJ MM 21-51-08. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007091100132 20070911 00132 EA 2007 9 11 SWIA200718653 1 20070830 A 3350 BATTERY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCHARGED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 964SW 7868 FLT 6617, FLOOR LEVER EMERGENCY FLOODLIGHTS ARE INOP. REPLACED NR 2 EMERGENCY BATTERY POWER SUPPLY IAW 33-80-00. 2 L 7 2 4F RT A21EA 2007091100133 20070911 00133 EA 2007 9 11 SWIA200718654 1 20070828 A 3350 SIGN CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT MISSING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 732SK 10194 FLT 6478 - FLOOR LEVEL GALLEY EMERGENCY EXIT SIGN IS MISSING COVER. INSTALLED NEW COVER. 2 L 7 2 4F RT A21EA 2007091100140 20070911 00140 EU 2007 9 11 MALA070105 1 20070828 A 2121 FAN SAAB SF340 340B 7860101 EU CABIN SMOKE A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 444XJ 340B444 NOTED ELECTRICAL BURNING ODOR JUST BEFORE START. ALSO, NOTED POSSIBLE SMOKE FROM THE SEAT ROW 1 AREA. SHUTDOWN AND CAL LED CFR. EVACUATED THE AIRCRAFT. ODOR AND SMOKE NEAR SEAT 1D, ALLS FANS, SUPP A/C AND POWER WAS TURNED OFF, SMOKE STOP PED. REPLACED LEFT RECIRC FAN. 2 L 7 2 4T RT A52EU 2007091100141 20070911 00141 SO 2007 9 11 RAIA00708048 1 20070830 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 833HK 145240 PRE FLT NR 8015 - ORD - EMERGENCY LIGHT LEFT OVERWING EXIT IDENTIFIER IS OUT. MAINTENANCE RE-SEATED BATTERY CONNECTOR E MERGENCY LIGHTS TEST OK. 2 L 7 2 4T RT T00011AT 2007091100143 20070911 00143 SO 2007 9 11 RAIA00708047 1 20070830 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 833HK 145240 PRE FLT NR 8011 - MLI - EMERGENCY LIGHT AT LEFT WING EXIT INOP. MAINTENANCE SECURED CONNECTOR CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2007091100145 20070911 00145 NM 2007 9 11 QXEA200701393 1 20070831 A 3350 LIGHT BOMBDR DHC8 DHC8402 1390042 NM CABIN MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 421QX 4149 SEA FLIGHT NR 2332: EMERGENCY LIGHTS COME ON IN THE ARMED POSITION. MAINTENANCE CYCLED AIRCRAFT POWER OFF THEN ON. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091100146 20070911 00146 2007 9 11 QXEA200701394 4 20070827 A 2310 CDU3933AE04 DISPLAY BOMBDR DHC8 DHC8402 1390042 NM COCKPIT FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 409QX 5925 5925 4051 SEA FLIGHT NR 2477: NR 1 ARCDU FAILED. RAN THE CHECKLIST AND RECYCLED ON-OFF SWITCH. NR 1 ARCDU FAILED MESSAGE REAPPEA RED 3 MINUTES LATER. MAINTENANCE REMOVED AND REPLACED CAPTAIN'S ARCDU. OPS CHECK GOOD IAW MTC 6238101. HGS OPERATIONA L TEST FAILED. AIRCRAFT DOWNGRADED TO CAT I. PLACARD REFLECTS THE SAME. MTX CONTROL NOTIFIED. AIRCRAFT RETURNED TO S ERVICE. 2 H 7 2 4T RT A13NM 2007091100149 20070911 00149 NM 2007 9 11 ASAA0742002 1 20070830 A 5753 SKIN BOEING 737 737490 1384715 NM FORE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 2272 28887 LT IB FORE FLAP HAS MULTIPLE DENTS ON LOWER SURFACE OB OF MIDDLE TRACK. REMOVED DAMAGED AREA FABRICATED AND INSTALLED R EPAIR FILLER AND DOUBLER IAW SRM 51 70 10 PG 201. 2 L 7 2 4F RT A16WE 2007091100150 20070911 00150 NM 2007 9 11 ASAA0742003 1 20070830 A 5753 SKIN BOEING 737 737490 1384715 NM FORE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 28887 LT IB FORE FLAP HAS MULTIPLE DENTS ON LOWER SURFACE JUST OB OF IB TRACK. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND SKIN IAW SRM 51 70 10 PG 201. 2 L 7 2 4F RT A16WE 2007091100152 20070911 00152 NM 2007 9 11 ASAA0742005 1 20070830 A 5320 652072629 WEB BOEING 737 737490 1384715 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 28887 FWD CARGO DOOR LOWER SILL WEB IS CRACKED. REMOVED CRACKED WEB FABRICATED AND INSTALLED REPLACEMENT WEB IAW SRM 51 40 2 AND 51 20 01. 2 L 7 2 4F RT A16WE 2007091100153 20070911 00153 NM 2007 9 11 ASAA0742007 1 20070830 A 5753 SKIN BOEING 737 737490 1384715 NM AFT FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 2442 28887 RT OB AFT FLAP HAS 2 EACH DENTS AT OB END OF UPPER SURFACE. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2007091100156 20070911 00156 EU 2007 9 11 07FDEA03359 1 20070905 A 5730 A57340087 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 ELONGATED HOLES IN LT PYLON SUPPORT BRACKET AND BOTTOM WING SKIN, RIB 8. REPAIR PERFORMED BY REAM UP THE HOLES AND INST ALLING BUSHES IAW DRW, R571- 50532, APPROVED BY EA 6-5720-95853 AND RAS/BAE/1002114/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091100158 20070911 00158 SO 2007 9 11 RAIA00708049 1 20070831 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 817HK 145058 PRE FLT NR 5584 - STL - AFT CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR TO THE SUBJECT LIG HT ASSEMBLY. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007091100159 20070911 00159 SO 2007 9 11 RAIA00709001 1 20070901 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 820HK 145064 PRE FLT NR 5535 - STL - LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT. OP ERATIONAL CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007091100160 20070911 00160 EU 2007 9 11 07FDEA03360 1 20070905 A 5754 A57864200169 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 2 SLAT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 ON OLD REPAIR ON NOSE SKIN, INNER RIB 7-9 OF SLAT NR 2 FOUND MISDRILLED HOLE. AFTER REMOVAL OF SKIN INSERT FOUND THREE RIBS DAMAGED. FLUSH SKIN REPAIR RENEWED IAW EA 6-5740-95837 AND RAS/FOK/267/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091100161 20070911 00161 EU 2007 9 11 07FDEA03361 1 20070905 A 5753 A57960000002 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 TEMPORARY REPAIR FOUND ON LT INNER FLAP, UPPER SKIN AT RIB 27, STRG 2.1-2.2 (RAS/FOK/146/2005 ISS A, WITH 5 FC). DOUB LER REPAIR RENEWED IAW EA 6-5750-95842 AND RAS/FOK/260/2005 ISSUE C. 2 L 7 2 4F RT A35EU 2007091100165 20070911 00165 WP 2007 9 11 07FDEA03365 1 20070905 A 5330 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 371FE 46609 EXTERNAL FUSELAGE SKIN EXISTING DOUBLER. NOT PER SRM. REPAIRED SKIN IAW SRM 53-20-00 FIG 6 VOL I. 2 L 7 3 4F A22WE 2007091100168 20070911 00168 EU 2007 9 11 07FDEA03368 1 20070905 A 5754 A57863031201 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 FOUND TWO OLD REPAIRS ON RT SLAT NR 1 IN BAD CONDITION, BETWEEN RIB 10-13, L/E AREA. ONE FLUSH DOUBLER REPAIR BETWEEN R IB 10-13 PERFORMED IAW EA 6-5740-95838 AND RAS/FOK/265/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091100171 20070911 00171 NM 2007 9 11 AMTA200700371 1 20070804 A 3040 6240665 CONTROLLER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE WINDOW HEAT MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 11 520AT 27976 RT WINDOW HEAT INOP LIGHT ILLUMINATED SEVERAL TIMES DURING CLIMB. REMOVED AND REPLACED WINDOW HEAT CONTROLER IAW MM 30- 41-01-4, OPS CK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007091100172 20070911 00172 2007 9 11 AMTA200700377 4 20070809 A 3460 4077880908 CONTROL PANEL BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT UNSERVICEABLE A AMTA O OTHER L NO TEST TX TAXI/GRND HDL 1 GL 11 561TZ 33526 DURING PREFLIGHT, LT CDU WOULD NOT TURN ON. STAYED BLANK. REMOVED AND REPLACED LT CDU IAW MM 34-61-02. OPS CHECK OK. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007091100173 20070911 00173 EU 2007 9 11 07FDEA03371 1 20070905 A 5753 A57960331201 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 727FD 579 FOUND OLD REPAIR ON NOSE SKIN OF RT CENTER FLAP, RIB 18-20, NOT CONFORM TO SRM 57- 50-00/FIG 208 (ONE RIVET ROW ON EACH SIDE MISSING). REPAIR RENEWED IAW SRM 57-50-00/PB 200 / FIG 208. 2 L 7 2 4F RT A35EU 2007091100174 20070911 00174 WP 2007 9 11 07FDEA03372 1 20070905 A 5754 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 SLAT NR 5 RT : INSTALLING EXTEND CABLE ASSY FOUND NUT PLATE OF BOLT ASSY TRACK CABLE RETAINER ON TRACK SLAT, MISSING. R EPAIRED SLAT SKIN IAW SRM 57-00-01 VOL I FIG 4 SHT 2. 2 L 7 3 4F A22WE 2007091100175 20070911 00175 EU 2007 9 11 07FDEA03373 1 20070905 A 5754 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 727FD 579 FOUND OLD FLUSH REPAIR ON LT SLAT NR 2 LOWER SKIN, BETWEEN TRACK 5-6 WITH POOR EDGE MARGIN. FLUSH DOUBLER REPAIR PERFOR MED IAW EA 6-5743-95844 AND RAS/FOK/264/2005 ISSUE C. 2 L 7 2 4F RT A35EU 2007091100176 20070911 00176 NM 2007 9 11 AALA20071544 1 20070814 A 3350 8200008731 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39364 24045 ORD - EMERGENCY LIGHT DOOR HANDLE SPOT LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGEN CY LIGHT DOOR HANDLE SPOT LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007091100178 20070911 00178 NM 2007 9 11 AALA20071532 1 20070813 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 683A 25340 JFK - EMERGENCY LIGHT AT SEAT ROWS 16D TO 25D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROWS 16D T O 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007091100179 20070911 00179 NM 2007 9 11 AALA20071533 1 20070813 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 913AN 29514 LAX - EMERGENCY LIGHT AT SEAT ROW 9D INOPERATIVE. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 9D. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007091100180 20070911 00180 NM 2007 9 11 AALA20071534 1 20070813 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 913AN 29514 LAX - EMERGENCY LIGHT AT SEAT ROW 9D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 9D. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007091100181 20070911 00181 WP 2007 9 11 AALA20071535 1 20070814 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 283AA 49296 LGA - EMERGENCY LIGHT AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT FORWARD GALLEY CEILING FOR EMERGENCY LIGHT AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007091100182 20070911 00182 EU 2007 9 11 AALA20071536 1 20070814 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7082A 643 MIA - EMERGENCY LIGHTS AT SEAT ROWS 6G TO 18G INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 6G T O 18G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007091100184 20070911 00184 EU 2007 9 11 CPCP20070088 1 20070730 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 4AE 244 FR 39 FLOORBEAM CORRODED. FR 39 FLOORBEAM REPAIRED TRANSFER ON W/C 181274. 2 H 7 2 4T RT A53EU 2007091100185 20070911 00185 NM 2007 9 11 UPS07450559 1 20070810 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D LT NR 3 MED CUTOUT FWD LOWER CORNER FOUND SKIN AND BEAR STRAP CRACK, CRACK LENGTH 0.040" TO 3/4". M/D LT NR 3 MED CUTOUT FWD LOWER CORNER SKIN AND BEARSTRAP REPAIRED AS PER UPS EO NR B747-5330-24674 APPX 'M'. 2 L 7 4 4F A20WE 2007091100186 20070911 00186 NM 2007 9 11 UPS07450560 1 20070810 A 5330 BEAR STRAP BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D RT NR 3 MED CUTOUT FWD LOWER CORNER FOUND SKIN CRACK AND BEARSTRAP CORROSION, CRACK LENGTH 1/16 IN CH APPROX. M/D RT NR 3 MED CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER UPS EO B747-5330-24674 APPENDIX 'N', BEAR STRAP CORROSION REMOVED AND REPROTECTED AS PER SRM 51-10-01 AND 51-10-02 ORI, 0.120" BLEND OUT DEPTH 0.010" BY 1/2" BY 6" WITHIN SRM 53-30-01 FIG 1 LIMIT (REF HX RS NR R53-41-35852, AND UPS EO B747-5330-27528) 2 L 7 4 4F A20WE 2007091100188 20070911 00188 NM 2007 9 11 UPS07450564 1 20070808 A 5320 SUPPORT BOEING 747 747212B 1384886 NM A/C BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C FX AIR CONDITIONING BAY PANEL SUPPORT FRAME FOUND CORROSION AT STA 1018 TO STA 1045 LBL 58, CORROSION BLEND OUT 0.045" BY 1" BY 1" EXCEED SRM 53-10-01 FIG 1 LIMITS, FX BS 987 TO BS 1060 LBL 58" FAIRING SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 1. 2 L 7 4 4F A20WE 2007091100190 20070911 00190 NM 2007 9 11 UPS07450566 1 20070809 A 5320 65B01837377 REVEAL BOEING 747 747212F 1384851 NM L1 DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D L1 DOOR FWD CUTOUT REVEAL CRACKED AT LATCH CAM FTG, CRACK LENGTH 3/8" APPROX. M/D L1 DOOR FWD CUT OUT REVEAL PANEL REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F RT A20WE 2007091100191 20070911 00191 NM 2007 9 11 UPS07450567 1 20070807 A 5330 SKIN BOEING 747 747212B 1384886 NM BS 340-360 S5L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C U/D LT BS 340-360 S5L LOCATION FOUND 1 HOLE CRACK AT FX SKIN RUNNING FWD AND AFT APPROX 1/8" BEYOND RI VET HEAD FX BS 340-360 STR 5L AREA SKIN REPAIRED WITH OUT ZERO TIMING AT CRITICAL ROW FASTENER AS PER SRM 53-30-03 FIG 1 AND UPS EO B747-5330-26295 APPENDIX A AND HX TAR NR 127778 REPEAT INSPECTION IS REQUIRED AS PER SRM 53-30-03 FIG 1. 2 L 7 4 4F A20WE 2007091100194 20070911 00194 2007 9 11 AMTA200700386 4 20070810 A 2310 9640452012 TRANSCEIVER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT HF SYS UNSERVICEABLE A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 519AT 27975 RT HF TRANSMISSION AND RECEPTION INOPERATIVE. AT ALL CREW STATIONS. REMOVED AND REPLACED RT HF TRANSCEIVER IAW AMM 23- 11-03-401. OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007091100195 20070911 00195 NM 2007 9 11 AMTA200700389 1 20070813 A 3150 WARNING LIGHT BOEING 737 73783N 13844HI NM MASTER CAUTION MALFUNCTIONED A AMTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 323TZ 30033 MASTER CAUTION AND ENG LIGHT SETTING STD THRUST. THROTTLES TO IDLE AND EXITED RUNWAY. ACCOMPLISHED EEC BIT IAW AMM 73- 00-00-810-801 NO FAULTS NOTED. ALSO, RESET CB MASTER CAUTION AND CHECKED NR1 AND NR2 EEC CONTACTORS, OK FOR SERVICE. ( K) 2 L 7 2 4F RT A16WE 2007091100197 20070911 00197 NM 2007 9 11 UPS07550554 1 20070803 A 5311 146N10055 FRAME BOEING 757 75724APF 1384969 NM BS 1280 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 415UP 23855 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1280, APPROX BET S25R AND S26R. ACCOMPLISHED PER FINAL EA NR 757 -5362-27-A1723 AND UPS EO NR B757-5310- 27514-A. 2 L 7 2 4F RT A2NM 2007091100200 20070911 00200 NE 2007 9 11 NWAA072986743 2 20070902 A 7200 ENGINE BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 4 FLAMED OUT A NWAA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 01 643NW 22245 702171 DURING CRUISE, THE NR 4 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. PER THE COM THE ENGINE WAS OPERATED AT REDUCED THRU ST. THE ENGINE SUBSEQUENTLY EXPERIENCED A FLAME-OUT. A RESTART ATTEMPT WAS UNSUCCESSFUL. THE FLIGHT CONTINUED TO NRT AND LANDED WITHOUT FURTHER INCIDENT. THE NR 4 ENGINE WAS REPLACED. 2 L 7 4 4F 4 F A20WE E3NE 2007091100201 20070911 00201 NM 2007 9 11 NWAA073005808 1 20070908 A 3350 BATTERY PACK BOEING 757 757351 1384991 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 588NW 32988 DURING OVER NIGHT CHECK, EMERGENCY BATTERY PACKS BOTH FORWARD AND MID DID NOT ILLUMINATE THEIR GROUPS OF LIGHTS FOR 15 M INUTES. MAINTENANCE REMOVED AND REPLACED BATTERY PACKS. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007091100202 20070911 00202 WP 2007 9 11 002 2 20070905 A 7200 31021802 ENGINE MTSBSI MU2 MU2B60 5780460 CE GARRTT TPE331 TPE331* 01514 WP ZONE 600 SHUTDOWN E BKAA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 13 610CA 7341 1330 788SA P36192C RT ENGINE SHUT DOWN IN FLIGHT. APPEARS TO BE A GEARBOX FAILURE OF SOME TYPE 1 H 7 2 3T 3 T RT A10SW E2WE 2007091100203 20070911 00203 CE 2007 9 11 BKAA200710001 1 20070827 A 2150 6831601 ACM MTSBSI MU2 MU2B35 5780411 CE ACM BAY SEIZED E BKAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 13 334EB 10675 568 AIR CYCLE MACHINE TURBINE SEIZED UP CAUSING SMOKE IN THE COCKPIT. THE AIR CYCLE MACHINE REQUIRED REPLACEMENT. 1 H 7 2 3T RT A10SW 2007091100204 20070911 00204 WP 2007 9 11 BKAA070905102 2 20070905 A 7200 31021802 ENGINE MTSBSI MU2 MU2B60 5780460 CE GARRTT TPE331 TPE331* 01514 WP ZONE 600 SHUTDOWN E BKAA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 SO 13 610CA 7341 1330 788SA P36192C RT ENGINE SHUT DOWN IN FLIGHT. APPEARS TO BE A GEARBOX FAILURE OF SOME TYPE 1 H 7 2 3T 3 T RT A10SW E2WE 2007091200001 20070912 00001 NM 2007 9 12 ASMF200709002 1 20070904 A 5350 RADOME BOEING 737 737* NM CFMINT CFM567 CFM567B22 13802 NE FUSELAGE DAMAGED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 850AM 33786 AIRCRAFT WAS HIT BY A STAIR THAT GOT MOVED BY A STRONG WIND DURING A STORM, RESULTING DAMAGE ON RADOME RT FRONT SIDE OF 23 INCH LENGTH WITH 5 PERFORATIONS (2 IN LOWER EXTREME AND 3 IN UPPER EXTREME) AND EXPOSITION OF COMPOUND MATERIAL. THE DETAILS OF THE REPAIR WILL BE SUBMITTED AS SOON AS WORKS WILL BE CONCLUDED. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007091200016 20070912 00016 2007 9 12 ASMF200709003 4 20070905 A 2230 POWERPLANT DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE RIGHT OVERSPEED W ASMF O OTHER J WARNING INDICATION AP APPROACH 1 SW 23 803ML 42025 2137 49726 725884 CAPTAIN REPORTED WINDSHEAR DURING APPROACH AND ATS DISCONNECTED, SPEED DECREASED, SO AUTOTHOTTLES WERE SET TO THE MAXIM UM POWER. AT PLATFORM, MAINTENANCE PERSONNEL DOWNLOAD THE ENGINES INFORMATION FROM THE MINIQAR DETECTING THAT THE RT ENG INE HAD VALUES OF N1 103.4 WITH AN EPR OF 2.16, OUT OF LIMITS IAW MM 72-00-00. RT ENGINE WAS REPLACED IAW MPCM 71-00-02 AND OPERATIONAL TEST WAS PERFORMED IAW MPCM 71-00-01, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007091200068 20070912 00068 EU 2007 9 12 07FDEA03473 1 20070910 A 5730 A57247017002 PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 500 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 FOUND ON OUTBOARD T/E PANEL, LHS, DELAMINATION REPAIR PERFORMED BY REMOVING THE DELAMINATION AND INSTALLING NEW PLIES IA W EA 6-5751-95858 AND RAS /BAE/1002007/2005 ISS A. 2 L 7 2 4F RT A35EU 2007091200069 20070912 00069 EU 2007 9 12 07FDEA03475 1 20070910 A 5320 A57111092 ANGLE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 DURING SB57-6086 AND SB57-6049, HOLES H, G, RT AND G, I , N, T ON LT HAVE BEEN FOUND CRACKED IN CENTER WING BOX, FRAME 47. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLATION OF NEW FASTENERS IAW EA 6-5710-95836 AND RAS/AS/0016/2006 IS SUE A. 2 L 7 2 4F RT A35EU 2007091200071 20070912 00071 EU 2007 9 12 07FDEA03401 1 20070906 A 5315 A53974268200 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORROSION ON CARGO FLOOR CROSSBEAM FRAME 56 AND 58, Y-800, RHS. CROSSBEAM SPLICE REPAIR PERFORMED IAW SRM 53-10-15/FIG 207. 2 L 7 2 4F RT A35EU 2007091000188 20070910 00188 NM 2007 9 10 SWAA074362 1 20070904 A 5311 6546526 FRAME BOEING 737 737317 138447P NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000191 20070910 00191 NE 2007 9 10 MASA200700419 2 20070713 A 7200 CF343B1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 VIBRATION A MASA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SW 07 77286 25122 7286 872583 ASH 2772 LAS. EN ROUTE TO MYR PILOT DIVERTED TO BFL DUE TO NR 2 ENG VIBRATION AND LOUD NOISE. NR 2 ENGINE WAS SHUT DOW N IN FLIGHT. PILOT DECLARED AN EMERGENCY AND LANDING WAS UNEVENTFUL CONTRACT MAINTENANCE FOUND THE EXHAUST TURBINE BLAD ES DAMAGED. MX REPLACED ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007091000200 20070910 00200 NM 2007 9 10 SWAA074350 1 20070901 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM BS 559 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000203 20070910 00203 NM 2007 9 10 SWAA074328 1 20070901 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000206 20070910 00206 NM 2007 9 10 SWAA074346 1 20070901 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091000210 20070910 00210 NM 2007 9 10 SWAA074330 1 20070901 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 294 S11L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091000216 20070910 00216 EU 2007 9 10 SIMA200724303 1 20070829 A 3246 510488 WHEEL SAAB SF340 340B 7860101 EU ZONE 700 SEPARATED A SIMA O OTHER D INFLIGHT SEPARATION TX TAXI/GRND HDL 1 SW 21 394AE 340B394 NUMBER TWO MAIN WHEEL/TIRE ASSEMBLY DISCOVERED TO BE MISSING FROM MAIN LANDING GEAR AXLE. REMOVED AND REPLACED LEFT LOW ER STRUT ASSEMBLY IAW SAAB AMM 32-11-27 AND REMOVED AND REPLACED NUMBER 2 TIRE ASSEMBLY IAW AMERICAN EAGLE WORK CARD 32- 71-23. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007091000239 20070910 00239 CE 2007 9 10 GUUA08220701 1 20070822 A 5540 10164001415 BRACKET BEECH 1900 1900D 1154162 CE RUDDER CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 38537 25044 UE158 AT SCHEDULED INSPECTION DISCOVERED UPPER RUDDER ATTACH BRACKET EXFOLIATED. REPLACED UPPER RUDDER BRACKET. 2 L 7 2 4T RT A24CE 2007091000261 20070910 00261 NM 2007 9 10 HALA0700360 1 20070902 A 4920 106170756D EXCITER BOEING 767 767332 1382001 NM APU ENGINE FAILED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 594HA 19555 19555 23275 ATBH: APU FAILED TO START, FAULT LGT ILLUM. AND EICAS MSG APU FAULT DISPLAYED 4904554 012353 000819 001 02. DID BITE OF ECU PER FIM 49-11-00 SHOWS NO LIGHT. REPLACED IGNITER PLUG AND LEAD NO HELP. REPLACED EXCITER BOX WITH LOANER BOX FRO M UAL. APU STARTS NORMALLY APU OPERATION NORMAL. 2 L 7 2 4F RT A1NM 2007091000263 20070910 00263 NM 2007 9 10 HALA0700359 1 20070902 A 4900 UNKNOWN BOEING 767 767332 1382001 NM UNKNOWN A HALA O OTHER O OTHER CR CRUISE 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, APU INFLIGHT START, OAT - 44 DEG C, TIME 44 SEC (FROM START TILL FAULT LIGHT), FL 350. 3RD ATT EMPT UNSUCCESSFUL. TROUBLESHOT PER FIM 49-11-00 FIG 104, 103, 107. BITE ECU NO MINI FLAGS FAULTY LRU "SEE MAINT MAN" W ITH REASON "NO LIGHT OFF" T/S FIG 107 BLK 4/5 BOTH OIL PUMP SHAFT AND DRIVE SHAFT FOR OIL PUMP CHECKS NORMAL. CLEARED E CU, RAN APU, IGNITION AUDIBLE CHECK NORMAL APU START 1 MIN 3 SEC RESTART APU 3 TIME WITH NO EICAS MESSAGE. VERIFICATION FLIGHT REQUIRED. 2 L 7 2 4F RT A1NM 2007091000268 20070910 00268 NM 2007 9 10 AWXA200701053 1 20070812 A 5311 6546921116 FRAME BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5987597, FORWARD CARGO COMPARTMENT DOOR CUT OUT FORWARD FRAME CRACKED, BS 445, S25R - S26R. REPLACED FORWARD CARGO COMPARTMENT DOOR CUT OUT FORWARD FRAME, BS 445, S25R - S26R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007091000273 20070910 00273 NM 2007 9 10 AWXA200701058 1 20070903 A 5320 140N250547 ANGLE BOEING 757 7572S7 1384962 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 MCN - MAJOR REPAIR - C-11 CHECK - NR 5988833, CRACKED CABIN INTERCOSTAL ANGLE, BS 180 - BS 1600, RBL 45.5, WL 208. REPL ACED CABIN INTERCOSTAL ANGLE, BS 180 - BS 1600, RBL 45.5, WL 208 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007091100002 20070911 00002 CE 2007 9 11 GUUA06090703 1 20070609 A 5220 NAS76A107P BUSHING BEECH 1900 1900D 1154162 CE ZONE 800 FROZEN A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 45AR UE12 AT SCHEDULED FLEET CAMPAIGN INSPECTION, LT FWD EMERGENCY EXIT WILL NOT OPEN FROM INSIDE. REPLACED BUSHING. 2 L 7 2 4T RT A24CE 2007091100003 20070911 00003 CE 2007 9 11 GUUA04300701 1 20070430 A 5220 1295140841 PIN BEECH 1900 1900D 1154162 CE EMERGENCY DOOR DIRTY A GUUA K NONE L NO TEST IN INSP/MAINT 1 SO 17 53545 UE185 ON PRE-FLIGHT INSPECTION, 6A EMERGENCY EXIT DOES NOT FUNCTION PROPERLY LOCKED AND WILL NOT OPEN. LUBED AND ADJUSTED LOC K PINS. 2 L 7 2 4T RT A24CE 2007091100004 20070911 00004 CE 2007 9 11 GUUA05080702 1 20070508 A 5220 1295140361 HANDLE BEECH 1900 1900D 1154162 CE EMERGENCY EXIT OUT OF ALIGNMENT A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 49543 UE181 AT SCHEDULED FLEET CAMPAIGN INSPECTION: SEAT 6F HATCH COVER NEEDS ADJUSTMENT CATCHING ON SIDEWALL. ADJUSTED SEAT 6F EM ERGENCY HATCH COVER. 2 L 7 2 4T RT A24CE 2007091100014 20070911 00014 NM 2007 9 11 UIEA200700335 1 20070831 A 5245 ACCESS PANEL BOEING 747 7472D7B 1384803 NM A/C BAY ERODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 AIR COND, BAY ACCESS PANEL 191HL EXT SURFACE FOUND ERODED. AIR COND BAY ACCESS PANEL 191HL REPAIRED WITH PRE-PRED FABRI C AS PER MESSAGE NR 1-497468248-2. 2 L 7 4 4F RT A20WE 2007091100017 20070911 00017 NM 2007 9 11 UIEA200700325 1 20070827 A 5754 SKIN BOEING 747 747341 13848AM NM LE FLAP DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 ON WALKAROUND AFTER FLIGHT OF GT5421, FOUND NR 11 L/E DEVISE DELAMINATED AT AFT I/B CORNER. PERFORMED INTERIM REPAIR PE R XEO57-082707. REPETITIVE INSPECTIONS FOR CONDITION AND SECURITY TO BE ACCOMPLISHED EVERY OTHER FLIGHT CYCLE UNTIL PER MANENT REPAIR OR PART REPLACEMENT ACCOMPLISHED. 2 L 7 4 4F RT A20WE 2007091100018 20070911 00018 NM 2007 9 11 UIEA200700336 1 20070831 A 5245 ACCESS PANEL BOEING 747 7472D7B 1384803 NM A/C BAY ELONGATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 AIR COND, BAY ACCESS PANEL 192ER EXT SURFACE FOUND SKIN ELONGATION. AIR COND BAY ACCESS PANEL 192ER REPAIRED WITH PRE-P RED FABRIC AS PER MESSAGE NR 1-497468248-2. 2 L 7 4 4F RT A20WE 2007091100031 20070911 00031 EU 2007 9 11 AWXA200701065 1 20070822 A 5347 D57130147200 SEAT TRACK AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5986012, CORROSION ON CABIN SEAT TRACK, BS 1590/FR 36 - BS 1810/FR 41, -Y765. REPL ACED CABIN SEAT TRACK, BS 1590/FR 36 - BS 1810/FR 41, -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007091100038 20070911 00038 NM 2007 9 11 QXEA200701388 1 20070906 A 3010 4100S01806 TMU BOMBDR DHC8 DHC8402 1390042 NM DEICE SYSTEM MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 402QX 8348 364 4032 SEA FLIGHT NR 2488: DEICER TIMER AND DEICE CAUTION WILL NOT EXTINGUISH. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE REMOVE D AND REPLACED THE TIMER AND MONITOR UNIT IAW Q400 MM 30-11-01 PGS 401-405. OPS CHECK GOOD. NO OTHER DEFECTS NOTED. A IRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091100043 20070911 00043 EU 2007 9 11 07FDEA03338 1 20070904 A 5330 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 727FD 579 FOUND OLD INTERNAL DOUBLER WITH CUT OUT ACC SRM IN OUTER SKIN AT FRAME 19, STRG 17 RHS. INNER DOUBLER IS NOT COMPATIBLE WITH PTOF CONVERSION. REPAIR PERFORMED BY RENEWING INTERNAL DOUBLER BY AN EXTERNAL ONE IAW DWG BEA 14095229-02 AND RA S/DABRE/70059934/2005. 2 L 7 2 4F RT A35EU 2007091100048 20070911 00048 EU 2007 9 11 07FDEA03343 1 20070904 A 5730 A57340085 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU RT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 FOUND CHAFING MARK ON INTERNAL SURFACE OF RT WING TOP SKIN PANEL NR 3 BETWEEN RIB 27-28 NEAR FRONT SPAR. REPAIR PERFO RMED BY BLEND OUT, HFEC INSPECTION FOR CRACK FREE AND FLAP PEENING IAW EA 6-5720-95843 AND RAS/BAE/1001878/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091100050 20070911 00050 EU 2007 9 11 07FDEA03345 1 20070904 A 5315 A53974268 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 CORROSION AT TOP CAP BEAM FRAME 58 LT AND RT. SPLICE REPAIR ON TOP CAP BEAM FRAME 58 LT AND RT PERFORMED IAW SRM 53-10- 15/FIG 207. 2 L 7 2 4F RT A35EU 2007091100054 20070911 00054 EU 2007 9 11 07FDEA03350 1 20070904 A 5315 A53978267208 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 CORROSION ON CROSSBEAM FRAME 67 RT, OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF CROSSBEAM IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091100067 20070911 00067 SO 2007 9 11 SWIA200718634 1 20070823 A 5730 ACCESS PANEL EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 582SW 120350 LOWER FORWARD STRINGER IN LEFT WING ACCESS PANEL INBOARD OF NACELLE IS CRACKED. FOUND AT C-CHECK, REPAIRED LEFT WING ST RINGER IAW SRM 57-20-103 PG 203. 2 L 7 2 4T RT A31SO 2007091100070 20070911 00070 EA 2007 9 11 SWIA200718637 1 20070713 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 719SK 10188 AFT COCKPIT FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. REPLACED COCKPIT FLOOR SUPPORT PER SB670-53-026. 2 L 7 2 4F RT A21EA 2007091100072 20070911 00072 EA 2007 9 11 SWIA200718640 1 20070702 A 5755 BOLT CNDAIR CL600 CL6002B19 1900309 EA SPOILER HINGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SW 7034 RIGHT WING STATION 213.08 HAS CORRODED FLIGHT SPOILER OUTBOARD HINGE BOLT. FOUND AT C-CHECK, REPLACED CORRODED BOLT ON FLIGHT SPOILER HINGE. 2 L 7 2 4F RT A21EA 2007091100077 20070911 00077 EA 2007 9 11 SWIA200718642 1 20070702 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA BS 484-499 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SW 7034 RIGHT SIDE SEAT RAIL HAS SURFACE CORROSION AT STA 484 TO 499. FOUND AT C-CHECK, REPLACED CORRODED SEAT TRACK SECTIONS A T RT OTBD FS 444.02 TO 495.98 PER REO 601R 53-00-055 AND CRJ200 AMM 53-01-11-420-001. 2 L 7 2 4F RT A21EA 2007091100081 20070911 00081 EA 2007 9 11 SWIA200718646 1 20070702 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA CABIN CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SW 7034 PAX SEAT TRACK HAS SURFACE CORROSION IN SEVERAL PLACES, FOUND AT C-CHECK. REPLACED CORRODED SEAT TRACKS WITH SERVICABLE TRACK. 2 L 7 2 4F RT A21EA 2007091100087 20070911 00087 EU 2007 9 11 COEA0706901 1 20070730 A 5230 S52176207228 INTERCOSTAL AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE AFT CARGO DOOR CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 901FX 172 CORROSION FOUND DURING HEAVY CHECK, LEVEL 2 CORROSION FOUND ON AFT CARGO DOOR INTERCOSTAL. REMOVED DOOR INTERCOSTAL AND INSTALLED NEWLY FABRICATED INTERCOSTAL. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007091100100 20070911 00100 SO 2007 9 11 GUUA08160701 1 20070816 A 3213 STRUT EMB 120 EMB120ER 3260203 SO MLG UNDERSERVICED A GUUA O OTHER O OTHER LD LANDING 1 SO 29 285AS 120265 FLIGHT:9287 FLL/GGT AFTER TAKEOFF IDLE 1 UNLOCK LIGHT AND CABIN ALTITUDE LIGHT ILLUMINATED. RETURNED TO FLL. AFTER LAND ING SLOWING THROUGH 80 KTS ON LANDING ROLL OUT BRAKES FAILED WITH ANTI-SKID ON. TURNED THE ANTI-SKID OFF AND REGAINED N ORMAL BRAKING. INSPECTED PROXIMITY SWITCHES, CLEANED STRUTS, CHECKED STRUT FLUID, SERVICED STRUTS WITH NITROGEN. PERFO RMED TAXI CHECKS. SYSTEM OPERATES NORMAL. 2 L 7 2 4T RT A31SO 2007091100102 20070911 00102 EU 2007 9 11 CPCP20070091 1 20070730 A 5340 BRACKET AEROSP ATR72 ATR72212 8680945 EU STEP CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 4AE 244 LT BETWEEN FRAME 36-39 FWD-AFT FOLDING STEP BRACKETS CORRODED. LT BETWEEN FRAME 36-39 FWD AND AFT FOLDING STEP BRACKETS REPLACED AS PER SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007091100108 20070911 00108 NM 2007 9 11 UPS07450543 1 20070807 A 5322 SHEAR TIE BOEING 747 747212B 1384886 NM BS 940 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D BS 940 LT TENSION TIE STEEL PLATE FOUND SEM. M/D BS 940 LT TENSION TIE ATTACH STEEL PLATE REPLACE D AND INSTALLED AS PER HX RS NR R53-25-35850 CONTINUE INSPECTION ARE REQUIRED AS PER UPS EO B747-5310-27442. 2 L 7 4 4F A20WE 2007091100112 20070911 00112 NM 2007 9 11 UPS07450548 1 20070812 A 5753 65B085323 SPAR BOEING 747 747212B 1384886 NM LT WING TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C LHW O/B MID FLAP REAR SPAR O/B UPPER CHORD FOUND CRACKED, CRACK LENGTH 18" APPROX. LHW O/B MID FLAP R EAR SPAR O/B UPPER CHORD BETWEEN WBL 801 TO MOST O/B AREA REPAIRED AS PER HX RS NR R57-58-35853 AND UPS ENGINEERING FILE NR 747-57-20148. 2 L 7 4 4F A20WE 2007091100114 20070911 00114 EU 2007 9 11 07FDEA03351 1 20070905 A 5320 A53974321004 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 CORROSION ON CORNER FITTING AT FRAME 63, STRG 44 LT, OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF FITTING IAW SRM 5 1-72-10. 2 L 7 2 4F RT A35EU 2007091100115 20070911 00115 EU 2007 9 11 07FDEA03352 1 20070905 A 5320 A53970710 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 CORROSION ON CORNER FITTINGS AT FRAME 58, STRG 44 LT AND RT, OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF BOTH FITT INGS LT AND RT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091100120 20070911 00120 EU 2007 9 11 07FDEA03357 1 20070905 A 5311 A53776575203 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 FOUND WEAR MARK ON INNER FLANGE OF FRAME 38.1 BETWEEN STRG 14-15 RT. REPAIR PERFORMED BY INSTALLING INTERNAL ANGLE AND ADDITIONAL SHIM AS PER PRINCIPLES GIVEN IN SRM 53-10-13/FIG 202, APPROVED EA 6-5314-95855 AND RAS/DABRE/7005992/2005. 2 L 7 2 4F RT A35EU 2007091100122 20070911 00122 NM 2007 9 11 AMTA200700388 1 20070811 A 7720 SENSOR BOEING 737 73783N 13844HI NM ENGINE TEMP MALFUNCTIONED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 310TZ 28243 INITIAL CLIMB DUCT PRESSURE L-15, R42 PSI, AT 16,000, N1 96.3, L 13, R 32 PSI, AT 27,000, L13, R 26, N1 98.7 IN CRUISE A T 370, L18, R 28. ON DESCENT BOTH MATCH UP. REMOVED AND REPLACED NR 1 ENG 450 TEMP SENSOR IAW MM 36-11-05-4. (K) 2 L 7 2 4F RT A16WE 2007091100134 20070911 00134 EA 2007 9 11 SWIA200718655 1 20070829 A 5297 WIRE HARNESS CNDAIR CL600 CL6002C10 1390015 EA CARGO DOOR CHAFED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 718SK 10184 FLT 6372 - "PROX SYS FAULT 2" STATUS MESSAGE APPEARED. REPAIRED CHAFED WIRING IN FORWARD CARGO DOOR HARNESS IAW CRJ MM 24-00-01. 2 L 7 2 4F RT A21EA 2007091100135 20070911 00135 EA 2007 9 11 SWIA200718656 1 20070827 A 3350 LENS CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS MISSING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 701SK 10133 FLT 6564 - WHITE LENS COVER MISSING AT CENTER CABIN EMERGENCY EXIT SIGN. REPLACED LENS COVER. 2 L 7 2 4F RT A21EA 2007091100136 20070911 00136 EA 2007 9 11 SWIA200718657 1 20070830 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 507CA 7796 FLT 2653 - THE FLAPS DEPLOYED TO 5° WITHOUT ANY PILOT INPUT, THEY THEN RETRACTED AND REDEPLOYED TO 3° AND RETRACTED ON CE AGAIN. REPLACED FECU IAW AMM 27-51-05. RIGGED, TESTED AND OPS CHECKED OK. 2 L 7 2 4F RT A21EA 2007091100137 20070911 00137 EU 2007 9 11 TRBA2007075 1 20070903 A 3350 7012210 LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS INOPERATIVE A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 342AT 345 PAX DOOR EMERGENCY STAIR LIGHT INOPERATIVE. ADJUSTED LAMP AND PERFORMED OP CHECK IAW JIC NR 33-50-00 AND FOUND WORKING PROPERLY. 2 H 7 2 4T RT A53EU 2007091100138 20070911 00138 NM 2007 9 11 QXEA200701377 1 20070903 A 2730 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM PITCH TRIM UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 403QX 4037 SEA FLIGHT NR 2328: PITCH TRIM CAUTION ON TAXI OUT. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE INTERROGATED CDS AND FOUND 'FCECU FAILURE 7C AND 67'. CLEARED FAULTS IAW Q400 FIM TASK 27-30-00-810-803. C/W OPS CHECK OF ELEVATOR PITCH TRIM SY STEM IAW Q400 AMM TASK 27-32-00-710-802. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091100139 20070911 00139 NM 2007 9 11 QXEA200701378 1 20070903 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS ILLUMINATED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 403QX 4037 SEA FLIGHT NR 2328: FLAP POWER CAUTION LIGHT ON TAXI. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE CLEARED FLAP POWER CAUTI ON LIGHT IAW SERVICE LETTER DH8-400-SL-27-002A AND C/W OPS CHECK OF FLAPS IAW Q400 AMM TASK 27-50-00-710-801. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091100151 20070911 00151 NM 2007 9 11 ASAA0742004 1 20070830 A 5753 SKIN BOEING 737 737490 1384715 NM FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 28887 DENT ON TOP SURFACE OF RT IB AFT FLAP. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND SKIN IAW SRM 51 70 10 PG 201. 2 L 7 2 4F RT A16WE 2007091100154 20070911 00154 NM 2007 9 11 ASAA072009 1 20070827 A 5710 STRUCTURE BOEING 737 737890 1384527 NM WING DAMAGED A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 0104 35103 LT WINGLET DAMAGED DUE CONTACT WITH AIRCRAFT N784 AT GATE. REMOVED AND REPLACED WINGLET ASSY PER AMM 57 20 21 2 L 7 2 4F RT A16WE 2007091100162 20070911 00162 WP 2007 9 11 07FDEA03362 1 20070905 A 5330 DOUBLER DOUG DC10 DC1010F 3022111 WP ZONE 100 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 EXTERNAL FUSELAGE EXISTING EXTERNAL DOUBLER. REPAIRED AREA IAW SRM 53-20-00 FIG 6 VOL I. 2 L 7 3 4F A22WE 2007091100164 20070911 00164 WP 2007 9 11 07FDEA03364 1 20070905 A 5330 ACA76831 DOUBLER DOUG DC10 DC1010F 3022111 WP ZONE 100 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 EXISTING DOUBLER ON EXTERNAL FUSELAGE. REPAIRED AREA IAW SRM 53-20-00 FIG 6 VOL I. 2 L 7 3 4F A22WE 2007091100187 20070911 00187 NM 2007 9 11 UPS07450563 1 20070813 A 5411 RIB BOEING 747 747212B 1384886 NM NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C NR 1 PYLON DRY BAY UPPER LINK STRUT BEAM O/B SIDE ATTACHMENT RIB ANGLE FOUND CRACKED AS MARKED NAC STA 223 (AFT SIDE) , CRACK LENGTH 5/8" APPROX NR 1 PYLON DRY BAY UPPER LINK STRUT BEAM O/B SIDE ATTACHMENT RIB ANGLE REPAIR ED AS PER HX RS NR R54-51-35856 AND UPS EO NR B747-5410-27512, DETAIL REPEAT INSPECTION OF THE SUBJECT REPAIRED AREA IS REQ. AT EVERY 'C' CHK OR 18 MONTHS PER HX RS NR R54-51-35856 AND UPS EO NR B747-5410-27512. 2 L 7 4 4F A20WE 2007091100192 20070911 00192 EU 2007 9 11 CPCP20070092 1 20070730 A 5310 STRUCTURE AEROSP ATR72 ATR72212 8680945 EU FUSELAGE DAMAGED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 4AE 244 FRAME 28B BETWEEN STR LT 21-20 CORROSION FOUND. FRAME 28B CENTER SEGMENT REPLACED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007091100196 20070911 00196 NM 2007 9 11 UPS07550553 1 20070803 A 5311 7075T651 FRAME BOEING 757 75724APF 1384969 NM BS 1320 S25R DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 415UP 23855 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1320,S25R. REPAIRED FRAME IAW SRM 53-00-07 TR 53-09. 2 L 7 2 4F RT A2NM 2007091100198 20070911 00198 NM 2007 9 11 UPS07550555 1 20070803 A 5311 70750063C FRAME BOEING 757 75724APF 1384969 NM BS 1580 S26L DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 415UP 23855 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1580, S26L. FRAME REPAIR AT STA 1580 S26L HAS BEEN ACCOMPLISHED IAW SRM 53-00-07, (TR 53-09) THIS REPAIR IS A CATEGORY B REPAIR AND REQUIRES REINSPECTION PER DETAIL V, TABLE 11 ZONE 3 FIG 201. 2 L 7 2 4F RT A2NM 2007091200065 20070912 00065 NM 2007 9 12 07FDEA03470 1 20070909 A 5330 SKIN DOUG MD11 MD11F 3023600 NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 FUSELAGE EXTERIOR, FORWARD CARGO DOOR CUTOUT AFT LOWER AREA FOUND CHAFED. 09-21-07 FUSELAGE EXTERIOR, FORWARD CARGO DOOR CUTOUT AFT LOWER CHAFFED AREA REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER SRM 53-50-00 F IGURE 17 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007091200067 20070912 00067 EU 2007 9 12 07FDEA03472 1 20070910 A 5712 A57141280200 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 FOUND CRACK (3MM) ON MLG RIB 5, LHS, AT HOLE 47 (RAS/BAE/1001321/2005 GIVES A LIMIT OF 10 FC). REPAIR PERFORMED BY REAM UP UNTIL CRACK REMOVAL IAW EA 6-5710-92236 AND RAS/BAE/1001952/2005 ISS B. 2 L 7 2 4F RT A35EU 2007091200073 20070912 00073 WP 2007 9 12 07FDEA03403 1 20070906 A 5315 NJC6040175 FLOORBEAM DOUG MD10 MD1010F 3022112 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 AFT CABIN BULKHEAD FLOOR TEE ANGLE SUPPORT CORRODED UNDER FLOOR PANEL SUPPORT AT RBL 20 REMOVED CORROSION IAW MD10 SRM 53-40-00 VOL1 FIG 18. ORIGINAL THICKNESS .125 IAW MD10 SRM 53-40-00 VOL 1 FIG 18, REMAINING .094 MATERIAL REMOVED .031 . REPAIRED IAW MD10 SRM 53-40-00 FIG 16 VOL 1 AT AFT PRESSURE BULKHEAD STA 2007 RBL 10-30. 2 L 7 3 4F RT A22WE 2007091200074 20070912 00074 EU 2007 9 12 07FDEA03404 1 20070906 A 5330 A53611171202 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 808FD 439 FOUND AN OLD EXTERNAL DOUBLER REPAIR ON FRAME 0-1, STRG 27 LHS, NOT CONFORM TO REPAIR INSTRUCTION AS PER SRM 53-11-12/FI G 201 (ONE RIVET ROW IS MISSING). REPAIR RENEWED WITH DEVIATIONS BY INSTALLING NEW FASTENERS IN OLD HOLES IAW EA 6-5311 -95927 AND RAS 042577/018/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091200081 20070912 00081 EU 2007 9 12 07FDEA03413 1 20070906 A 5210 SKIN AIRBUS 310 A310324 3930206 EU ZONE 800 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 808FD 439 FOUND OLD EXTERNAL DOUBLER REPAIR ON RT AFT PAX DOOR LOWER AFT CORNER WITHOUT ANY DOCUMENTATION. THE REPAIR WAS NOT C ONFORM TO SRM 52-10-00/FIG 203 (RIVET ROW MISSING). REPAIR PERFORMED BY INSTALLING THE MISSING FASTENER ROW (MS20426-DD 5) TO THE EXISTING REPAIR, APPROVED BY EA 6-5213-95906 AND RAS/DAHAM/4020451/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091200082 20070912 00082 EU 2007 9 12 07FDEA03414 1 20070906 A 5753 A57970100011 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 FOUND OLD DOUBLER REPAIR WITH NEW DAMAGED CORE ON RT INBOARD FLAP T/E, RIB 1, LOWER SURFACE. REPAIR PERFORMED IAW SRM 5 7-53-12 / FIG 208, APPROVED BY EA 6-5752-95905 AND RAS/DABRE/7006189/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091200083 20070912 00083 EU 2007 9 12 07FDEA03415 1 20070906 A 5101 NONE AIRBUS 310 A310324 3930206 EU NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 FOUND OLD EXTERNAL RIVETED DOUBLER ON RT INBOARD FLAP, OUTBOARD EDGE RIB 21, WITHOUT ANY RECORD. REPAIR RENEWED BY CUT OUT TO A REGULAR SHAPE AND INSTALLING A NEW DOUBLER, APPROVED BY EA 6-5752-95905 AND RAS/DABRE/7006189/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091200085 20070912 00085 EU 2007 9 12 07FDEA03417 1 20070906 A 5753 SKIN AIRBUS 310 A310324 3930206 EU TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 FOUND DENT ON RT INBOARD FLAP, BETWEEN RIB 15 AND TRACK 2, STRG 13-14, LOWER SKIN. DOUBLER REPAIR PERFORMED IAW EA 6-57 52-95905 AND RAS/DABRE/7006189/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091200086 20070912 00086 EU 2007 9 12 07FDEA03418 1 20070906 A 5311 FRAME AIRBUS 310 A310324 3930206 EU ZONE 300 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 FOUND OLD REPAIR AT APU COMPARTMENT, FRAME 101 WITH AN ADDITIONAL DAMAGE (BENDED) ON SUPPORT ANGLE AND THE DOUBLER. R EPAIR PERFORMED BY DRESS BACK THE BENDED FLANGE OF THE L-SECTION IAW EA 6-5339-95908 AND RAS/DAHAM/4020455/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091200088 20070912 00088 EU 2007 9 12 07FDEA03420 1 20070906 A 5311 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 FOUND OLD REPAIRS AT MANHOLE FITTING FRAME 38.1-38.2 (MORE THAN FOUR ADJACENT POCKETS AFFECTED), NOT ALLOWED IAW SRM 53- 14-12/PG 228. REPAIR PERFORMED BY REPLACEMENT OF MANHOLE FITTING BETWEEN FRAME 38.1-38.2 IAW DRW R537-06164 ISSUE D, AP PROVED BY EA 6-5310-99167A AND RAS/DABRE/7006403/2006 ISSUE B. 2 L 7 2 4F RT A35EU 2007091200089 20070912 00089 EU 2007 9 12 07FDEA03421 1 20070906 A 5310 FRAME AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 808FD 439 FOUND TWO OLD MISDRILLED HOLES IN SHEAT WEB FRAME 75A-76, STRG 26 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 5 1-72-10. 2 L 7 2 4F RT A35EU 2007091200090 20070912 00090 EU 2007 9 12 07FDEA03423 1 20070905 A 2934 642500052 TRANSMITTER AIRBUS 310 A310203 3930313 EU HYD SYSTEM MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 411FE 359 DURING CRUISE, GREEN HYDRAULICS SHOWED "0" PRESSURE AND "LO RSVR QUANTITY" ON ECAM. QUANTITY CONFIRMED ON OVERHEAD PANE L. DIVERTED TO ATL. DURING MANUAL GEAR EXTENSION, QUANTITY RETURNED TO GREEN BAND (BELOW TOP HAT). INSTALLED ALL THRE E GEAR PINS IN AIRCRAFT. FOUND HYD PRESSURE TRANMITTER IN LT WHEEL WELL LEAKING. REMOVED AND REPLACED LT PRESSURE TR ANMITTER (GREEN SYS). RESERVICED GREEN SYSTEM AND WORKED AIR OUT OF SYSTEM A300-200 M/M 29-32-13-4. SDR PREVIOUSLY SUB MITTED UNDER TRACKING #07-3392. DISREGARD THIS SDR-ADMINISTRATOR. 2 L 7 2 4F RT A35EU 2007091200091 20070912 00091 EU 2007 9 12 07FDEA03424 1 20070906 A 5310 A53974299208 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 FOUND CORROSION ON SHEAR PLATE FRAME 68-69, STRG 47-48 LHS. REPAIR WAS PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-1 0. 2 L 7 2 4F RT A35EU 2007091200092 20070912 00092 EU 2007 9 12 07FDEA03425 1 20070906 A 5320 A53773667202 BRACKET AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 FOUND CORROSION ON BRACKET RING BETWEEN FRAME 24-25 AND STRG 54 LT TO 54 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IA W SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091200093 20070912 00093 EU 2007 9 12 07FDEA03426 1 20070906 A 5310 A53770977202 COUPLING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 FOUND CORROSION ON COUPLING AT FRAME 26/32, STRG 44 LHS. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091200094 20070912 00094 NM 2007 9 12 QXEA200701401 1 20070907 A 5240 DOOR BOMBDR DHC8 DHC8402 1390042 NM AFT SERVICE OUT OF ADJUST A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 420QX 4147 SEA FLIGHT NR 2498: FA REPORTS LOUD SQUEAL COMING FROM AFT SERVICE DOOR (R2) AFTER ENGINE START WITH BLEEDS SELECTED ON. MAINTENANCE RE-ADJUSTED AFT SERVICE DOOR SEAL AND CLEANED DOOR SEAL. PRESSURIZED AIRCRAFT FOR MAINTENANCE IAW AMM 21- 00-00-863-801 AND 54-41-00-820-801 SUB TASK 54-41-00-820-059. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091200095 20070912 00095 NM 2007 9 12 QXEA200701402 1 20070910 A 3350 58401A2B5C5F4L30 SWITCH BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY LIGHTS MALFUNCTIONED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 421QX 4149 SEA FLIGHT NR 2316: EMERGENCY LIGHTS REMAIN ON IN THE ARM POSITION. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHTS, NORMAL/ON SWITCH ON FWD BULKHEAD ASSY. PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHT SYSTEM IAW Q400 AMM TASK 33-51 -00-710-801. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091200096 20070912 00096 EU 2007 9 12 07FDEA03428 1 20070906 A 5310 A53610027 WINDOW FRAME AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 FOUND CORROSION AT WINDSHIELD FRAMEWORK BETWEEN FRAME 7-10, LT/RT. REPAIR WAS PERFORMED BY BLEND OUT THE CORROSION IAW EA 6-5311-95933 AND RAS 042711/019/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091200098 20070912 00098 EU 2007 9 12 07FDEA03392 1 20070905 A 2934 642500052 TRANSMITTER AIRBUS 310 A310203 3930313 EU HYD SYSTEM LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 411FE 348 348 359 DURING CRUISE, GREEN HYDRAULICS SHOWED "0" PRESSURE AND "LO RSVR QUANTITY" ON ECAM. QUANTITY CONFIRMED ON OVERHEAD PANE L. DURING MANUAL GEAR EXTENSION, QUANTITY RETURNED TO GREEN BAND (BELOW TOP HAT). FOUND HYD PRESSURE TRANSMITTER IN LT WHEEL WELL LEAKING. REMOVED AND REPLACED LT PRESSURE TRANSMITTER (GREEN SYS). RESERVICED GREEN SYSTEM AND WORKED AIR OUT OF SYSTEM. RESTORATION TO NORMAL CONFIGURATION CHECKS GOOD. 2 L 7 2 4F RT A35EU 2007091200100 20070912 00100 EU 2007 9 12 07FDEA03394 1 20070906 A 5320 A53612214201 FLOOR SUPPORT AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 HEAVY CORRODED LONGERON BETWEEN FRAME 12A-14, CABIN FLOOR STRUCTURE, OUT OF LIMIT AS PER SRM 53-10-00. REPAIR PERFORMED IAW SRM 53-12-15/FIG 207. 2 L 7 2 4F RT A35EU 2007091200101 20070912 00101 EU 2007 9 12 07FDEA03395 1 20070906 A 5320 A53612214201 FLOOR SUPPORT AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 HEAVY CORRODED LONGERON BETWEEN FRAME 12A-14, CABIN FLOOR STRUCTURE, OUT OF LIMIT AS PER SRM 53-10-00. REPAIR PERFORMED IAW SRM 53-12-15/FIG 207. 2 L 7 2 4F RT A35EU 2007091200105 20070912 00105 EU 2007 9 12 07FDEA03399 1 20070906 A 5315 A53974219220 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORROSION ON CARGO FLOOR CROSSBEAM FRAME 63, Y-500 TO Y-800, RHS. CROSSBEAM SPLICE REPAIR PERFORMED IAW SRM 53-10-15/FI G 207. 2 L 7 2 4F RT A35EU 2007091200107 20070912 00107 NM 2007 9 12 07FDEA03430 1 20070906 A 5315 6520827218 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FWD CARGO PIT, FLOORBEAM LOWER FOWARD FLANGE UPPER SURFACE HAS CORROSION AT NUTPLATE HOLES, BS 720, RBL 3-34. REMOVED C ORRODED LOWER FLANGE FROM RBL 3-34. FABRICATED NEW FLANGE, FILLERS AND 4 REPAIRS ANGLES, AND HEAT TREATED 4 REPAIR ANGL ES REF DWG SR 27-53-034 SHEET 8. TREATED AND PRIMED REF 727 SRM 53-10-1 AND INSTALLED REF 727 SRM 51-30-2. THIS IS CLA SSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007091200110 20070912 00110 EU 2007 9 12 07FDEA03433 1 20070907 A 5330 A53611171202 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 DENT ON LOWER SKIN PANEL BETWEEN FRAME 1-2 WAS REPAIRED IN YEAR 1995 BY CUTTING OUT AREA AND INSTALLING AN INTERNAL DOUB LER. IN FEBRUARY 2006, REPAIR FOUND INSTALLED BETWEEN FRAME 0-1 AS PER REPAIR DRAWING AND THE DOUBLER MATERIAL WAS NOT IAW. DOCUMENTATION, MEASURED BY NDT. REPAIR RENEWED BY REINSTALLATION OF NEW DOUBLER WITH OVERSIZED FASTENERS AS PER D RW 12F53025A, APPROVED BY EA 6-5311-95926 AND RAS/AS/031/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091200111 20070912 00111 EU 2007 9 12 07FDEA03434 1 20070907 A 5330 A53778160200 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 FOUND EXISTING SKIN REWORK IN POOR CONDITION AT FRAME 37, STRG 32, LHS. REPAIR AREA POLISHED, NDT INSPECTED WITH NIL FI NDINGS AND FLAP PEENED IAW EA 6-5314-95918 AND RAS/DABRE/7005252/2006 ISSUE A (NOMINAL THICKNESS 1, 6 MM, REMAINING THIC KNESS 1,01 MM). 2 L 7 2 4F RT A35EU 2007091200113 20070912 00113 EU 2007 9 12 07FDEA03436 1 20070907 A 5320 A53980376226 SUPPORT AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 CRACKED SUPPORT STRUT BETWEEN FRAME 77-78, STRG 45. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091200114 20070912 00114 EU 2007 9 12 07FDEA03437 1 20070907 A 5320 A53575557200 WEB AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 808FD 439 DAMAGED WEB AT FRAME 59 BETWEEN STRG 29-36 RHS, OUTBOARD. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091200115 20070912 00115 EU 2007 9 12 07FDEA03438 1 20070907 A 5714 A57310051 PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 FOUND WRONG INSTALLED FASTENERS AT CENTER WING BOX, FRAME 40-47. REPAIR PERFORMED BY INSTALLING NEW OVERSIZED BULL NOSE FASTENERS IAW EA 6-5710- 95919 AND RAS/042817/015/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091200119 20070912 00119 EU 2007 9 12 07FDEA03442 1 20070907 A 5420 A57350138201 PLATE AIRBUS 310 A310324 3930206 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 CHAFING DAMAGE (10 BY 1.5 MM) ON PYLON REINFORCING PLATE, RT WING AT FWD OUTBOARD EDGE, RIB 9. REPAIR PERFORMED BY BLEN D OUT AND NDT INSPECTION IAW EA 6-5720-95909 AND RAS/BAE/1002261/2006. 2 L 7 2 4F RT A35EU 2007091200124 20070912 00124 EU 2007 9 12 07FDEA03447 1 20070907 A 5313 A53974203578 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 CORROSION ON STRINGER 54 LT, BETWEEN FRAME 65-66, OUT OF LIMIT AS PER SRM 53-10-00. STRINGER SPLICE REPAIR PERFORMED IA W SRM 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007091200126 20070912 00126 EU 2007 9 12 07FDEA03449 1 20070907 A 5313 A53980877 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 FOUND CORRODED AREAS ON FUSELAGE STRINGER OUTER FLANGE BETWEEN FRAME 76-77, STRG 56 RT AND 56 LT. REPAIR PERFORMED BY R EWORK CORROSION FOLLOWING ROTO- AND HFEC INSPECTION OF AREAS AND ADJACENT HOLES WITH NIL FINDINGS IAW EA 6-5318-95920 AN D RAS/DATLS/0003029/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091200128 20070912 00128 EU 2007 9 12 200708221 1 20070820 A 2150 A/C PACK EMB ERJ170 ERJ170100SE 3260406 EU NR 1 FAILED A UHLA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 11 649RW 17000070 DEN TO YYZ FLIGHT 7546 DURING TAKEOFF ROLL THE CREW SMELLED SMOKE. THE CREW EXECUTED A REJECTED TAKEOFF AT APPROX 100KT S THEN RECEIVED A PACK-1 FAIL EICAS MESSAGE. THE SMOKE SMELL DIMINISHED AT THIS TIME. AIRCRAFT RETURNED TO THE GATE. M AINTENANCE PLACED THE NR 1 AIR CONDITIONING PACK ON MEL. REMAINS ON MEL. NO COMPONENTS CHANGED AS OF THIS DATE. WILL UP DATE WHEN CORRECTIVE ACTION IS ACCOMPLISHED. 2 L 7 2 4F RT A56NM 2007091200129 20070912 00129 EU 2007 9 12 TRAX200701250 1 20070827 A 5710 ANGLE AEROSP ATR72 ATR72 EU WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 A/C OPERATION WITH CRACKED WINGS PRESSURE DECK ANGLES EO 72-53-0168 COMPLY WITH. PERFORMED AMO 46-90 IAW EO 72-53-0168. CRACKS IN ANGLE DO NOT EXTEND BEYOND EXISTING MEASUREMENTS. ADDITIONAL CRACKS FOUND ON LT & RT ANGLES FROM UPPER EDGE OF ANGLE PROPAGATING DOWN NOT EXTENDING BEYOND FIRST FASTENER TASK COMPLIED IAW EO 72-53-0168 2 H 7 2 4T RT 2007091300001 20070913 00001 2007 9 13 WGEA200700002 4 20070822 A 3160 700000079103 DISPLAY ECLIPS EA500 ECLIPSEEA500 3350000 SW COCKPIT MALFUNCTIONED E WGEA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 131DJ 15 000033 DURING TAXI FOR TAKEOFF, SMELLED SMOKE, MFD STARTED TO DIM, SMOKE BEGAN TO POUR OUT FROM UNDER PANEL, SHUT DOWN ENGINE A ND TURNED OFF ALL ELECTRICS. SUP REMOVED AND REPLACED MFD WITH A NEW UNIT PER EA 500 AMM 31-10-15. INSPECTED ALL AREAS FORWARD OF MFD AND PFD'S TO INCLUDE HARNESSESS AND CONNECTORS NO DEFECTS OR DAMAGE NOTED. PERFORMED ALL FUNCTIONAL CHE CKS IAW AMM 31-10-00. ALL CHECKS GOOD. 1 L 7 2 4J RT A00002AC 2007091300004 20070913 00004 SW 2007 9 13 WGEA200700003 1 20070829 A 3411 1004353940 PROBE ECLIPS EA500 ECLIPSEEA500 3350000 SW PITOT/STATIC SYS OBSTRUCTED E WGEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 130DJ 42 000023 ON INITIAL LEVEL OFF AT 4000 FT ACCELERATING TO 220 KEAS HAD AIRSPEED DISAGREE, YAW DAMP FAIL AND AUTO PILOT FAIL CAS ME SSAGE. AUTO PILOT DISENGAGE, AIRSPEED 224 LEFT 216 RIGHT. SUP CLEANED PILOTS AND COPILOTS PITOT PROBES. PERFORMED PIT OT/STATIC VERIFICATION TEST. SYSTEM OP'S CHECK GOOD, AIRSPEED/ALTITUDE MATCHED PERFECTLY IAW EA 500 AMM 34-10-00. 1 L 7 2 4J RT A00002AC 2007091300005 20070913 00005 NM 2007 9 13 SCNA07010 1 20070830 A 3350 BATTERY PACK BOEING 737 7378Q8 13844BX NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 806SY 28215 DURING A FUNCTIONAL TEST OF THE EMERGENCY LIGHTS, MAINTENANCE FOUND LEFT REAR BIN EMERGENCY EXIT LIGHTS & L2 DOOR EXTERI OR EMERGENCY EXIT LIGHT BATTERY PACK FAILS THE FUNCTIONAL TEST. MAINTENANCE REMOVED & REPLACED THE BATTERY PACK FOR THE LEFT AFT BIN EMERGENCY LIGHTS & L2 EXTERIOR DOOR. 2 L 7 2 4F RT A16WE 2007091300006 20070913 00006 NM 2007 9 13 BB07070 1 20070901 A 2721 CONTROL PANEL BOEING 757 7572B7 1384964 NM RUDDER TRIM MALFUNCTIONED A USAA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 EA 19 200UU 27809 FLIGHT 750, PHL-BRU: RUDDER TRIM INOPERATIVE WOULD NOT TRIM TO THE RIGHT. FLIGHT RETURNED TO PHL. MAINTENANCE REPLACE D THE P8 TRIM CONTROL PANEL. NO FURTHER FAULTS. 2 L 7 2 4F RT A2NM 2007091300007 20070913 00007 NM 2007 9 13 BB07071 1 20070902 A 3412 PROBE BOEING 757 7572B7 1384964 NM TAT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 206UW 27808 FLIGHT 724, PHL-SNN: TAT PROBE HEAT FAILED. RETURNED TO PHL. MAINTENANCE REPLACED THE TAT PROBE. NO FURTHER FAULTS. 2 L 7 2 4F RT A2NM 2007091300008 20070913 00008 NM 2007 9 13 BB07072 1 20070901 A 3350 2012 POWER SUPPLY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 929UW 27144 MAINTENANCE FOUND EMERGENCY LIGHTS AT R3 AND R4 DOORS INOPERATIVE. REPLACED POWER SUPPLY. NO FURTHER FAULTS. 2 L 7 2 4F RT A2NM 2007091300009 20070913 00009 EU 2007 9 13 BA07013 1 20070831 A 3350 32146210 POWER SUPPLY AIRBUS 330 A330323 3930335 EU CABIN FAULTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 272AY 0333 MAINTENANCE FOUND THE 3R EMERGENCY LIGHT POWER SUPPLY FAULTED. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A46NM 2007091300010 20070913 00010 NM 2007 9 13 MWEA070193 1 20070902 A 7830 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 904ME 55168 LEFT THRUST REVERSER UPPER BUCKET STATION 26 ZEE FRAME CRACKED ON INBOARD END. 2 L 7 2 4F TR A6WE 2007091300012 20070913 00012 NM 2007 9 13 MWEA070195 1 20070902 A 7830 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 904ME 55168 LEFT HAND THRUST REVERSER LOWER BUCKET STATION 26 FRAME IS CRACKED AT OUTBOARD END. 2 L 7 2 4F TR A6WE 2007091300013 20070913 00013 NM 2007 9 13 MWEA070196 1 20070902 A 7830 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 904ME 55168 LEFT THRUST REVERSER LOWER BUCKET STATION 26 ZEE FRAME IS CRACKED AT ONBOARD END. 2 L 7 2 4F TR A6WE 2007091300014 20070913 00014 NM 2007 9 13 MWEA070197 1 20070902 A 7830 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 904ME 55168 LEFT THRUST REVERSER LOWER BUCKET STATION 35 ZEE FRAME IS CRACKED AT OUTBOARD END. 2 L 7 2 4F TR A6WE 2007091300015 20070913 00015 NM 2007 9 13 MWEA070198 1 20070902 A 7830 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 904ME 55168 RIGHT THRUST REVERSER UPPER BUCKET STATION 26 ZEE FRAME IS CRACKED AT OUTBAORD END. 2 L 7 2 4F TR A6WE 2007091300019 20070913 00019 WP 2007 9 13 MWEA070202 1 20070830 A 5350 49182411 PANEL DOUG DC9 DC981 3022081 WP TAIL CONE INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 813ME 48007 TAIL CONE EXIT DOOR ARM/DISARM PANEL DOES NOT STAY IN DISARMED POSTION OR DOES NOT LATCH PROPERLY. RESECURED PANEL. 2 L 7 2 4F A6WE 2007091300026 20070913 00026 NM 2007 9 13 UPS07450579 1 20070814 A 5420 ANGLE BOEING 747 747200 1384847 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C NR 2 PYLON REAR ENG MOUNT BULKHEAD ATTACHMENT UPPER LINK BEAM AFT SIDE O/B ANGLE CRACKED AS MARKED (CR ACK LENGTH .75 INCH). NR 2 PYLON REAR ENG MOUNT BULKHEAD ATTACHMENT UPPER LINK BEAM AFT SIDE O/B ANGLE REPAIRED AS PER SRM 54-14-03 FIG B & REFER NRC ALW51195 FOR WORKING DETAIL. 2 L 7 4 4F RT A20WE 2007091300027 20070913 00027 NM 2007 9 13 UPS07450580 1 20070813 A 5411 RIB BOEING 747 747200 1384847 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C NR 2 PYLON REAR ENG MOUNT BULKHEAD ATTACHMENT UPPER LINK BEAM O/B AND I/B SIDE RIB ANGLE FOUND CRACKED (NAC STA 277-4) FWD SIDE (CRACK LENGTH 1 INCH APPROX). NR 2 PYLON REAR ENG MOUNT BULKHEAD ATTACHMENT UPPER LINK BEAM O /B AND I/B SIDE RIB ANGLE REPAIRED AS PER SRM 54-14-03 FIG 13. 2 L 7 4 4F RT A20WE 2007091300028 20070913 00028 NM 2007 9 13 UPS07450581 1 20070813 A 5411 RIB BOEING 747 747200 1384847 NM NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C NR 3 PYLON REAR ENG MOUNT BULKHEAD ATTACHMENT ENG MOUNT BULKHEAD ATTACHMENT UPPER LINK BEAM O/B & I/B SIDE RIB ANGLE FOUND CRACKED (NAC STA 227.4) FWD SIDE (CRACK LENGTH .375 INCH & 1 INCH). NR 3 PYLON REAR ENG MOUNT BULK HEAD ATTACHMENT ENG MOUNT BULKHEAD UPPER LINK BEAM O/B SIDE RIB ANGLE REPAIRED AS PER SRM 54-14-03 FIG 13 AND O/B SIDE R IB ANGLE REPAIRED AS PER HX RS R54-51-35857 REPEAT INSP IS REQUIRED PER HX RS R54-51-35857 AND UPS EO B747-5410-27513. 2 L 7 4 4F RT A20WE 2007091300030 20070913 00030 NM 2007 9 13 UPS07550569 1 20070804 A 5311 143N102530 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 415UP 23855 INSPECTION TYPE:C DENTS IN FWD CARGO FUSELAGE FRAME STA 180, APPROX S23R AND S24R (2EA). ACCOMPLISHED REPAIR PER FINAL EA 757-5332-27-A1728 AND UPS EO B757-5310-27479-A. 2 L 7 2 4F RT A2NM 2007091300031 20070913 00031 NM 2007 9 13 UPS07550571 1 20070804 A 5311 143N102530 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 415UP 23855 INSPECTION TYPE:C DENTS IN FWD CARGO FUSELAGE FRAME STA 780, APPROX S23R AND S24R (2EA). ACCOMPLISHED REPAIR PER FINAL EA 757-5332-27-A1728 AND UPS EO B757-5310-27479-A. 2 L 7 2 4F RT A2NM 2007091300033 20070913 00033 NM 2007 9 13 UPS07550591 1 20070803 A 5311 70750090C FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 415UP 23855 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1340, S26R. FRAME REPAIR AT STA 1340, S26R WAS ACCOMPLISHED IAW SRM 53-00-07 (TR53- 9) AND REQUIRES REINSPECTION AS STATED IN STEP 14 OF ECA 112685. 2 L 7 2 4F RT A2NM 2007091300036 20070913 00036 WP 2007 9 13 UPS07850575 1 20070821 A 5522 SKIN DOUG DC8 DC873F 302199F WP LT ELEVATOR DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 4 DENTS ON LEFT ELEV UPPER SKIN BETWEEN STA XE 36 AND XE 57. DRILLED OUT DENTS ON LEFT ELEV UPPER SK IN AT STA XE 35 AND XE 36 IAW SRM 55-02-00. FABRICATED AND INSTALLED REPAIR DOUBLER AT LEFT ELEV STA XE 35-XE 36 IAW SR M 55-02-01-0 FIG 010, AND SRM 51-01-21-0. 2 L 7 4 4F RT 4A25 2007091300038 20070913 00038 WP 2007 9 13 UPS07850582 1 20070821 A 5320 FINGER DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 COCKPIT SUBFLOOR FINGER DOUBLER CORRODED OUT OF LIMITS AT STA -80. REMOVED COCKPIT SUBFLOOR FINGER D OUBLER AT STA -80 IAW SRM 51-01-21. FABRICATED AND INSTALLED REPAIR FINGER DOUBLER AT STA -80 IAW DWG 5612298, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007091300039 20070913 00039 WP 2007 9 13 UPS07850583 1 20070821 A 5522 SKIN DOUG DC8 DC873F 302199F WP LT ELEVATOR CUT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 LEFT ELEV UPPER SKIN CUT AT T/E NEAR STA XE 147. CUT OUT DAMAGED AREA AT LEFT ELEV UPPER SKIN STA XE 147 IAW SRM 55- 02-01. FABRICATED AND INSTALLED REPAIR DOUBLER AT LEFT ELEV UPPER SKIN STA XE 147 IAW SRM 55-04-01, AN D SRM 55-02-01. 2 L 7 4 4F RT 4A25 2007091300041 20070913 00041 WP 2007 9 13 07FDEA03306 1 20070902 A 5347 4929405 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREA AT F/S 1380-1530 LBL8. REMOVED DAMAGED SEAT TRACK. FABRICATED AND INSTALLE D NEW SEAT TRACK AND HAT SPLICES. 2 L 7 3 4F RT A22WE 2007091300042 20070913 00042 WP 2007 9 13 07FDEA03307 1 20070902 A 5347 4929149 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREA AT F/S 1039-1059 LBL 107. REMOVED DAMAGED SEAT TRACK AND FABRICATED AND INS TALL NEW SEAT TRACK AND HAT SPLICES. 2 L 7 3 4F RT A22WE 2007091300043 20070913 00043 WP 2007 9 13 UPS07850585 1 20070813 A 5753 37759071 FLAP TRACK DOUG DC8 DC873F 302199F WP T/E FLAP DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 FLAP TRACK CHROME MISSING LEFT FLAP STA 410 O/B. REMOVED AND REPLACED LEFT STA 410 FLAP TRACK IAW AM M DC8 27-51-03-2. 2 L 7 4 4F RT 4A25 2007091300045 20070913 00045 WP 2007 9 13 UPS07850588 1 20070817 A 5313 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 CRACK ON L17L END FITTING, 60 COMPT STA 1772. REMOVED AND REPLACED LONGERON END FITTING AT STA 1772 L17L IAW SRM 51-01-20D, 51-03-02-0, AND SRM 51-1-11. 2 L 7 4 4F RT 4A25 2007091300047 20070913 00047 WP 2007 9 13 UPS07850590 1 20070821 A 5347 36575031 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 COCKPIT 1ST OBSERVERS SEAT TRACK HOLES ARE ELONGATED AT STA -32. REMOVED AND REPLACED 1ST OBSERVERS SEAT TRACK AT STA -32 IAW SRM 51-03-00, AND SRM 51-01-24. 2 L 7 4 4F RT 4A25 2007091300049 20070913 00049 NM 2007 9 13 CALA0700483 1 20070831 A 5320 69353525 FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A .5 INCH CRACK IN FRAME TO STRINGER CLIP AT STA 847, S27L, LBL 3. A NEW CLIP WAS INSTALLED IAW SRM 51 -10-02. 2 L 7 2 4F RT A16WE 2007091300050 20070913 00050 NM 2007 9 13 CALA0700484 1 20070902 A 5230 65C8073525 STRUCTURE BOEING 737 7373T0 1384582 NM C2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A .5 INCH CRACK AT FORWARD AND AFT CORNERS OF C-2 DOOR LOWER T-CHORD. THE T-CHORD WAS REMOVED AND REPL ACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007091300053 20070913 00053 NM 2007 9 13 CALA0700487 1 20070902 A 5311 654655138 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND FRAME CORRODED AT STA 807 BETWEEN S27L AND S27R, LBL 6 TO RBL 6. THE FRAME WAS REMOVED AND REPLACED IA W SRM 51-40-02 AND 51-10-02. 2 L 7 2 4F RT A16WE 2007091300054 20070913 00054 NM 2007 9 13 CALA0700488 1 20070902 A 3350 20121 CHARGER BOEING 737 7373T0 1384582 NM AFT GALLEY INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14325 23455 INSPECTION FOUND THE LAST 4 SEAT MOUNTED EMERGENCY LIGHTS OUT. THREE BATTERY CHARGERS IN THE AFT GALLEY WERE REMOVED AN D REPLACED IAW AMM 33-51-51. THE EMERGENCY LIGHTS NOW OPERATE NORMALLY. 2 L 7 2 4F RT A16WE 2007091300061 20070913 00061 NM 2007 9 13 ASAA0742011 1 20070901 A 5512 65C274824565C274 SKIN BOEING 737 7374Q8 138447Q NM HORIZ STAB DAMAGED A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 784AS 28199 DAMAGE TO LEFT HORIZONTAL STABILIZER TIP DUE TO CONTACT FROM AC PUSHING BACK. REFERENCE SDR ASAA0742008. TEMPORARY REPA IR TO LEFT HAND HORIZONAL STAB TIP REPAIRED IAW CASCADE ERO 7152 AND EA 5510 01304. PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 6 MONTHS. 2 L 7 2 4F RT A16WE 2007091300065 20070913 00065 EA 2007 9 13 TRAX200701269 1 20070901 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA LT WING INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 922EV 7822 LEFT WING EMERGENCY LIGHT IS INOP. 2 L 7 2 4F RT A21EA 2007091300066 20070913 00066 EA 2007 9 13 TRAX200701270 1 20070901 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 684BR 7708 EMERGENCY EXIT SIGN AT ASD IS INOP. 2 L 7 2 4F RT A21EA 2007091300067 20070913 00067 EA 2007 9 13 TRAX200701271 1 20070831 A 2913 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYS FAILED A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 877AS 7579 THE 3B PUMP FAILED IN FLT. EN ROUTE TO ATL A/C DIVERTED TO AVL DUE TO MTC. RELATED TO DEFECT 352241-2. EMERGENCY DECL ARED. FLT 4812 CX. 2 L 7 2 4F RT A21EA 2007091300068 20070913 00068 EU 2007 9 13 UPS07150573 1 20070831 A 3244 A300MN TIRE AIRBUS A300 A300F4622R 3930360 EU LT MLG FAILED A IPXA K NONE O OTHER LD LANDING 1 SO 01 152UP 0835 INSPECTION TYPE:N/A ON ARRIVAL/LANDING NR 1, 2 AND 5 TIRES THERMALLED. REMOVED NR 1 TIRE. INSPECTED PER MM 05-51-16-00 CHECK OK. INSTALLED NEW T&W PER MM 12-37-32-00. S/N OFF 17914. REMOVED AND REPLACED NR 2 T/W ASSY PER MM 12-37-32-00, INSPECTED PER MM 05-51-16-00 CHECK OK. S/N OFF 18495. REMOVED AND REPLACED NR 5 MLG T/W ASSY PER MM 12-37-32-00. INS PECTED PER MM 05-51-16-00 CHECKS OK. S/N OFF 29295. 2 L 7 2 4F RT A35EU 2007091300069 20070913 00069 NM 2007 9 13 UPS07550601 1 20070803 A 5311 146N102859 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 415UP 23855 INSPECTION TYPE:C DENTS IN AFT CARGO FUSELAGE FRAME STA 1300, APPROX BETWEEN S25L AND TO S27L (3EA). REPAIR ACCOMPLISHE D PER PRELIM NR 2 AND FINAL EA 757-5362-27-A1727 AND UPS EO B757-5310-27523-A. 2 L 7 2 4F RT A2NM 2007091300070 20070913 00070 NM 2007 9 13 UPS07550602 1 20070803 A 5311 146N102818 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 415UP 23855 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1260, S26R. ACCOMPLISHED PER FINAL EA 757-5362-27-A1732 AND UP E O B757-5310- 27532-A. 2 L 7 2 4F RT A2NM 2007091300071 20070913 00071 NM 2007 9 13 UPS07550606 1 20070904 A 3350 LIGHT BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 407UP 23729 INSPECTION TYPE:N/A EMERGENCY LIGHT ASSY HAS SIX LAMPS INOP. RELAMPED EMERGENCY LIGHT ASSY PER MM 33-51-01-2. OPS CHEC K GOOD. 2 L 7 2 4F RT A2NM 2007091300076 20070913 00076 WP 2007 9 13 UPS07850603 1 20070830 A 5522 SKIN DOUG DC8 DC873F 302199F WP LT ELEVATOR PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 LEFT ELEV LWR SKIN PUNCTURED VERY INBOARD SIDE. DRILLED OUT DAMAGED AREA FOR REPAIR IAW SRM 55-02-00 FIG 006. PLUGGED HOLE ON LEFT ELEV SKIN IAW SRM 55-02-00 FIG 006. 2 L 7 4 4F RT 4A25 2007091000276 20070910 00276 EU 2007 9 10 AWXA200701061 1 20070823 A 5320 D53472193200 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980115, CORROSION ON CABIN FLOORBEAM, BS 3158/FR 66, -Y765. REPLACED CABIN FLOORB EAM, BS 3158/FR 66 TO BS 3366/FR 70, -Y765 I/A/W A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007091100022 20070911 00022 NM 2007 9 11 QXEA200701375 1 20070901 A 5230 HANDLE BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR UNSECURE A QXEA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 NM 09 425QX 4039 SEA TO BZN FLIGHT NR 2478: FUSELAGE DOORS MASTER CAUTION WARNING IN FLIGHT, DOOR PAGE SHOWED BAG DOOR UNSAFE. FLIGHT WA S DIVERTED TO GEG. MAINTENANCE INSPECTED AND FOUND AFT BAGGAGE DOOR HANDLE IN UNLOCKED POSITION. C/W H/S NR 05-0001. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091100028 20070911 00028 NM 2007 9 11 AMTA200700400 1 20070822 A 2130 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN PRESSURE UNKNOWN A AMTA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 GL 11 401TZ 24663 CABIN ALTITUDE WARNING HORN SOUNDED WHILE CLIMBING THROUGH FL 360. DONNED OX MASK, REQUESTED DESCENT AND WHILE PERFORMI NG CHECK LIST THE CABIN BEGAN TO DESCEND AND PRESSURIZATION WAS RESTORED. VISUALLY INSPECTED AFT PRESSURE BULKHEAD SEAL , NO DEFECTS NOTED. PERFORMED PRESS CONTROL SYS OPERATIONAL TEST IAW MM 21-31-00, PGS 201-205. OPS CHECK STATIS OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2007091100037 20070911 00037 NM 2007 9 11 QXEA200701383 1 20070829 A 2150 78279018 ACM DHAV DHC8 DHC8202 2809007 NM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 369PH 15921 230 513 PSC - PASSING THROUGH APPROXIMATELY 15000' AIR CONDITION PACK HOT CAUTION LIGHT ILLUMINATED FOR 1 MINUTE. RAN CHECKLIST WENT TO MANUAL ON CABIN A BUMPED UP TEMP. LIGHT FLICKERED AND WENT OUT. DUCT TEMP INDICATED APPROXIMATELY 20C WHEN LI GHT CAME ON. REPLACED THE ACM IAW D8-200 AMM TASK 21-50-11-000-801 AND 21-50-11-400-801. OPERATIONAL CHECK GOOD AIRCRA FT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091100042 20070911 00042 EU 2007 9 11 07FDEA03337 1 20070904 A 5754 RIB AIRBUS 300 A300B4622R 3930312 EU NR 1 SLAT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 LT SLAT 1 TRAILING EDGE LOWER SKIN DAMAGE AT INNERRIB 23, AREA AT T/E PROFILE. REPAIR IS PERFORMED WITH SKIN INSERT AND REPAIR PATCH IAW TD FOK/262/2005 ISSUE B. 2 L 7 2 4F RT A35EU 2007091100046 20070911 00046 EU 2007 9 11 07FDEA03341 1 20070904 A 5754 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 1 SLAT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 DENT WITH A CHAFING MARK WAS FOUND ON THE RT SLAT NR 1, LOWER SKIN T/E HONEYCOMB TAIL, NEAR RIB 21-23. REPAIR PERFORM ED BY SKIN INSERT AND REPAIR PATCH IAW TD FOK/273/2005 ISS B, APPROVED BY EA 6-5742-95845 AND RAS/FOK/237/2005 ISS. B. 2 L 7 2 4F RT A35EU 2007091100051 20070911 00051 EU 2007 9 11 07FDEA03347 1 20070904 A 5315 A53978267202 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 CORROSION ON TOP CAP BEAM FRAME 66 RHS, OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT IAW SRM 51-74-10. 2 L 7 2 4F RT A35EU 2007091100053 20070911 00053 EU 2007 9 11 07FDEA03349 1 20070904 A 5340 A53773644208 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 DENTED MILLED CORNER FITTING AT C 25, STRG 41-43 LT, OUT OF LIMIT IAW SRM 53-10-00. REPAIR PERFORMED BY REPLACEMENT OF CORNER FITTING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091100055 20070911 00055 NM 2007 9 11 CALA0700475 1 20070830 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 767-907 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17328 23458 INSPECTION FOUND LT O/B SEAT TRACK CORRODED FROM STA 767-907, LBL 45. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52, PAG E 201. 2 L 7 2 4F RT A16WE 2007091100057 20070911 00057 NM 2007 9 11 CALA0700477 1 20070830 A 5322 6546549 SHEAR TIE BOEING 737 7373T0 1384582 NM BS 767 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT STA 767 JUST I/B OF S27L, LBL 8. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 53-00-07. 2 L 7 2 4F RT A16WE 2007091100058 20070911 00058 NM 2007 9 11 CALA0700478 1 20070830 A 5415 310A10502 FITTING BOEING 737 7373T0 1384582 NM NR 2 NACELLE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND NR 2 ENGINE RT MIDSPAR ATTACH FITTING CORRODED. REPAIRED IAW ECRA 5410-01629. 2 L 7 2 4F RT A16WE 2007091100059 20070911 00059 NM 2007 9 11 CALA0700479 1 20070830 A 5415 310A10502 FITTING BOEING 737 7373T0 1384582 NM NR 2 NACELLE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND NR 2 ENGINE LT MIDSPAR ATTACH FITTING CORRODED. REPAIRED IAW ECRA 5410-01629. 2 L 7 2 4F RT A16WE 2007091100061 20070911 00061 NM 2007 9 11 AMTA200700397 1 20070822 A 4900 APU BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE INOPERATIVE A AMTA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 323TZ 30033 APU DOES NOT START. FAULT LIGHT ON. BITE APU, STARTED APU OPS CHECK GOOD REM 49-00-00. (K) 2 L 7 2 4F 4 F RT A16WE E2GL 2007091100064 20070911 00064 EA 2007 9 11 SWIA200718631 1 20070828 A 3231 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG DOOR MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 919SW 7657 GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGES APPEARED, FLIGHT NR 6208. REPLACED NOSE LANDING GEAR SELECTOR VALVE. OPS CHECK GOOD PER CRJ MM 32-33-00, PN: 750006000, SN ON: 0584T SN OFF: 1949. 2 L 7 2 4F RT A21EA 2007091100080 20070911 00080 EA 2007 9 11 SWIA200718645 1 20070702 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA COCKPIT WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SW 7034 CO-PILOT SEAT TRACKS HAVE ELONGATED HOLES AND ARE WORN, FOUND AT C-CHECK. REPLACED COPILOT SEAT TRACK PER CRJ200 SRM 51 -42-21 PG 19. 2 L 7 2 4F RT A21EA 2007091100083 20070911 00083 EU 2007 9 11 COEA0707901 1 20070730 A 5230 SKIN AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE AFT CARGO DOOR CRACKED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 901FX 172 SKIN CRACKED, FOUND DURING HEAVY CHECK, FOUND CARGO DOOR INNER SKIN AND UNDERLYING STRUCTURE BENT JUST AFT OF ACTUATOR M OUNT. FOUND SKIN REPAIR TO BE CRACKED DUE TO IMPROPERLY FABRICATED INTERCOSTAL. INSTALLED NEW INTERCOSTAL AND FABRICAT ED NEW SKIN REPAIR IAW SRM. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007091100091 20070911 00091 SO 2007 9 11 RAIA00708044 1 20070828 A 5340 14566156404 BRACKET EMB 145 EMB145LR 3260212 SO FUSELAGE BROKEN A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 814HK 145046 FLT NR 5495 - STL - HEADING 2 FAIL WITH INDICATION BEING 100 DEGREES OFF FROM THE NR 1 HEADING. MAINTENANCE INSPECTED T HE AIRCRAFT AND FOUND THE RT FLUX VALVE BRACKET TO BE BROKEN. BRACKET WAS REMOVED AND REPLACED AND FLUX VALVE COMPENSAT ION WAS PERFORMED. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007091100094 20070911 00094 SO 2007 9 11 RAIA00708045 1 20070828 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 817HK 145058 PRE FLT NR 5461 - STL - EMERGENCY LIGHT INOPERATIVE IN THE CABIN. MAINTENANCE RESECURED THE CONNECTOR TO THE AFFECTED L IGHT ASSEMBLY. 2 L 7 2 4T RT T00011AT 2007091100095 20070911 00095 SO 2007 9 11 RAIA00708042 1 20070825 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 817HK 145058 PRE FLT NR 5584 - RIC - OVERHEAD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR TO THE AFFECTED LIGHT . OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007091100096 20070911 00096 NM 2007 9 11 QXEA200701396 1 20070814 A 2430 11521102 TRU BOMBDR DHC8 DHC8402 1390042 NM SMOKE A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 402QX 15997 15597 4032 PDX FLIGHT NR 2296: AFTER ENGINE START, FO NOTICED PUFF OF SMOKE BY NOSE AREA. ELECTRICAL PAGE SHOWED NO LOAD ON NR 1 T RU WITH .25 LOAD ON NR 2 TRU AND .5 LOAD ON BOTH DC GENERATORS. MAINTENANCE REMOVED AND REPLACED NR 1 TRU IAW AMM 24-31 -21. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091100105 20070911 00105 NM 2007 9 11 UPS07450540 1 20070806 A 5320 CHANNEL BOEING 747 747212B 1384886 NM BS 840 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D RT BS 840 TENSION TIE TO FRAME CONNECTION FOUND NR 8 HOLE CRACK AND NR 20 HOLE OVAL AT FWD CHANNEL .(CRACK LENGTH 0.040"). M/D RT BS 840 TENSION TIE FWD CHANNEL REPAIRED AS PER SRM 53-10-11 FIG 2 REPEAT INSPECTION IS R EQUIRED AS PER SRM 53-10-11 FIG 2 TABLE IV AND UPS ASSIGNED MPI NR P19388. 2 L 7 4 4F A20WE 2007091100109 20070911 00109 NM 2007 9 11 UPS07450544 1 20070806 A 5320 PLATE BOEING 747 747212B 1384886 NM BS 920 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D BS 920 RHS TENSION TIE TO FRAME STEEL PLATE 2EA HOLE FOUND SEM AT MOST O/B AS MARKED. M/D BS 920 RT TENSION TIE ATTACH STEEL PLATE REPLACED AND INSTALLED AS PER HX RS NR R53-25-35848 AND REPEAT INSPECTION IS REQUIRED AS PER UPS EO NR B747-5310-27452. 2 L 7 4 4F A20WE 2007091100113 20070911 00113 NM 2007 9 11 UPS07450558 1 20070807 A 5330 SKIN BOEING 747 747212B 1384886 NM BS 340-360 S5R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C U/D RT BS 340-360 S5R LOCATION FOUND 1 HOLE CRACK AT FX SKIN RUNNING FWD AND AFT APPROX 1/8" BEYOND RI VET HEAD. FX BS340-360 STR5R AREA SKIN REPAIRED WITHOUT ZERO TIMING AT CRITICAL ROW FASTENER AS PER SRM 53-30-03 FIG 1 AND UPS EO B747-5330-26295 APP B AND TAR 127777. REPEAT INSPECTION IS REQUIRED AS PER SRM 53-30-03 FIG 1 AND UPS ASSIGN ED MPI NR P19375. 2 L 7 4 4F A20WE 2007091100116 20070911 00116 EU 2007 9 11 07FDEA03353 1 20070905 A 5320 SILL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 CORROSION, MISDRILLED HOLES AND CRACKS ON THE UPPER FLANGE OF THE FWD CARGO DOOR SILL BEAM BETWEEN FRAME 20-26. REPAIR PERFORMED BY REPLACEMENT OF FWD CARGO DOOR SILL BEAM UPPER FLANGE PER DRW R537-06091 ISSUE B WITH DEVIATIONS NOTED IN RA S/DABRE/7005974/2005 ISSUE A AND EA 6-5313-92214. 2 L 7 2 4F RT A35EU 2007091100142 20070911 00142 SO 2007 9 11 RAIA00708046 1 20070830 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 839HK 14500829 POST FLT NR 8003 - RIC - EMERGENCY EXIT FLOOR PROXIMITY LIGHT LOOSE. MAINTENANCE SECURED LIGHT STRIP, CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2007091100144 20070911 00144 2007 9 11 SWIA200718658 3 20070829 A 6140 SENSOR EMB 120 EMB120ER 3260203 SO FAULTY A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 562SW 120336 FLT 5768 - AFTER ROTATION RIGHT NP FLUCTUATED ON BOTH ANALOG AND DIGITAL INDICATIONS. REPLACED NP SENSOR IAW MM 27-12-0 0. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007091100147 20070911 00147 NM 2007 9 11 QXEA200701395 1 20070725 A 3620 8209074 SWITCH BOMBDR DHC8 DHC8402 1390042 NM NR 2 BLEED SYS MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 409QX 770 770 4051 SJC FLIGHT NR 2453: NR 2 BLEED HOT CAUTION LIGHT CAME ON DURING APPROACH. CHECKLIST C/W. LIGHT STAYED ON. LIGHT STAYE D ON AFTER ENGINE SHUTDOWN. MAINTENANCE INTERROGATED CDS, FAULT CODES PG 2-7005 R BLD ANA, 3BNO DIST DAMPER, 1701 R BLD TEMP SW. REMOVED AND REPLACED NR 2 OVERTEMP SWITCH IAW AMM TASK 36-11-16-400-801. C/W FIM TASK 36-20-00-810-802. OPS TEST OF BLEED AIR SYSTEM CHECKS GOOD. NO OTHER FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091100148 20070911 00148 NM 2007 9 11 ASAA0742001 1 20070830 A 5755 SKIN BOEING 737 737490 1384715 NM SPOILER PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS MA5884 28887 NR 4 GROUND SPOILER HAS HOLE NEAR THE TRAILING EDGE. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR FILLER AND SKIN IAW SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2007091100157 20070911 00157 SO 2007 9 11 RAIA00709003 1 20070903 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 807HK 145119 PRE FLT NR 3574 - STL - SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR TO THE LIGHT ASSEMBLY. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2007091100166 20070911 00166 WP 2007 9 11 07FDEA03366 1 20070905 A 5330 SKIN DOUG DC10 DC1010 3022110 WP ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 371FE 46609 FOUND EXTERNAL FUSELAGE SKIN EXISTING DOUBLER. NOT PER SRM. REPAIRED SKIN IAW SRM 53-20-00 VOL I FIG 6. 2 L 7 3 4F A22WE 2007091100169 20070911 00169 WP 2007 9 11 07FDEA03369 1 20070905 A 5321 ABA72031 FLOOR PANEL DOUG DC10 DC1010F 3022111 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 PERFORMED INSPECTION AFTER REMOVAL FLOOR PANEL IN COCKPIT WITH OAN J/C SP10530208-2JR, FOUND SEVERE CORROSION WITH EXFOL IATION (OUT OF LIMIT) ON MEMBRANE AND CRACK. REPLACED WEB SECTION IAW SRM 53-00-01 FIG 10 VOL I. 2 L 7 3 4F A22WE 2007091100193 20070911 00193 NM 2007 9 11 MWEA070192 1 20070827 A 3510 SWITCH BOEING 717 717200 1383700 NM OXYGEN MASK STICKING A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 906ME 55170 CAPTAIN'S OXYGEN MASK TEST/RESET SWITCH IS STICKY. REMOVED AND REPLACED OXYGEN MASK STORAGE BOX. 2 L 7 2 4F TR A6WE 2007091100199 20070911 00199 NM 2007 9 11 UPS07550556 1 20070808 A 5412 311N3271 BULKHEAD BOEING 757 75724APF 1384969 NM NR 1 NACELLE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 415UP 23855 INSPECTION TYPE:C NR 1 PYLON AFT BULKHEAD OUTBD SIDE LOWER CORNER CHAFED. BULKHEAD MILL WAS DONE ON TRAV NR T7/696069 P ER PRELIMINARY 1 EA 757- 5453-27-A1725 STEP 1. HFEC WAS DONE ON TRAV NR T7/696069 PER PRELIMINARY EA 757-5453-27-A1725 STEP 2. BLEND IS 2.1 L BY 1.25W BY .080D PER PRELIMINARY 1 EA 757-5453-27-A175 STEP 3. REMAINING THICKNESS ON FLANGE IS .120 PER PRELIMINARY 1 EA 757-5453-27-A1725 STEP 4. 2 L 7 2 4F RT A2NM 2007091200066 20070912 00066 EU 2007 9 12 07FDEA03471 1 20070910 A 3297 CONNECTOR AIRBUS 300 A300F4605R 3930327 EU SELECTOR VALVE CONTAMINATED A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 662FE 761 ON APPR INTO KONT, PUT LDG GEAR HANDLE DOWN AND IT WAS STRANGELY QUIET, GEAR DID NOT COME DOWN. TRIED SYS 2 WITH SAME R ESULT. EXECUTED GA AND MANUALLY EXTENDED GEAR. UPON LANDING/ENGINE SHUTDOWN, ECAM SHOWED C/B MONITOR OPEN, "LDG GEAR E XTEND CONTROL" C/B HAD POPPED. FOUND CONNECTOR ON LANDING GEAR SELECTOR VALVE 3GA-A FOULED WITH HYDRAULIC RESIDUE. CLE ANED, REPLACED 3 AMP CIRCUIT BREAKER 1GA REFERENCE WIRING DIAGRAM 32-31-01 PAGE 1, AND CHAPTER 20-16-00-2. PERFORMED O PERATIONAL TEST OF SYSTEM 4 TIMES, ALL CHECKS GOOD, NO FAULTS AND ON EACH TEST THE CIRCUIT BREAKER REMAINED IN, PER MM 32-31-12-6. 2 L 7 2 4F RT A35EU 2007091200072 20070912 00072 EU 2007 9 12 07FDEA03402 1 20070906 A 5315 A53973490200 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 FOUND CORROSION ON CARGO FLOOR STRUCTURE ANGLE SECTION FRAME 60, Y-1470, RHS. REPAIR PERFORMED BY REPLACEMENT OF PART I AW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091200076 20070912 00076 WP 2007 9 12 07FDEA03408 1 20070906 A 5730 ARB1075504 SKIN DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 RT WING LWR SURFACE FOUND CRACK ON SKIN. REPAIRED CRACK IAW SRM 57-10-00 FIG 68 SHT 1 VOL I. 2 L 7 3 4F A22WE 2007091200079 20070912 00079 EU 2007 9 12 07FDEA03411 1 20070906 A 5311 A53610265204 FRAME AIRBUS 310 A310324 3930206 EU ZONE 300 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 808FD 439 FOUND OLD EXTERNAL DOUBLER REPAIR ON FRAME 10 LH, Z-336, NOT FULLY CONFORM TO RAS/AS/359/95 ISSUE A AND OLD DELTA AIRLIN ES RECORD 297854-14 (WRONG RIVETS INSTALLED: HLT411-6 INSTEAD OF HL109-6). REPAIR PERFORMED BY REMOVING WRONG FASTENERS , NDT INSPECTION FOR CRACK FREE CONDITION AND INSTALLING ASNA2026V3, APPROVED BY EA 6-5312-95928 AND RAS/042710/022/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091200087 20070912 00087 EU 2007 9 12 07FDEA03419 1 20070906 A 5311 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 FOUND OLD REPAIRS AT MANHOLE FITTING FRAME 23-24 (MORE THAN FOUR ADJACENT POCKETS AFFECTED), NOT ALLOWED IAW SRM 53-13-1 2/PG 220. REPAIR PERFORMED BY REPLACMENT OF MANHOLE FITTING BETWEEN FRAME 23-24 IAW DRW, R537-06163 ISSUE B, APPROVED B Y EA 6-5310-95923A AND RAS/DABRE/7006402/2006 ISSUE B. 2 L 7 2 4F RT A35EU 2007091200104 20070912 00104 EU 2007 9 12 07FDEA03398 1 20070906 A 5730 A57241132201 SKIN AIRBUS 300 A300B4605R 3930308 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CHAFING MARK (18 BY 17 MM) FOUND AT WING L/E SKIN RT BETWEEN TRACK 3 AND WOFX-48.9. REPAIR PERFORMED BY BLEND OUT TO SM OOTH PROFILE IAW EA 6-5741-112506 AND RAS/BAE/1005353/2007 ISSUE A. 2 L 7 2 4F RT A35EU 2007091200106 20070912 00106 NM 2007 9 12 ERAA200700004 1 20070826 A 3350 BATTERY PACK DHAV DHC8 DHC8103 1386005 NM EMERGENCY LIGHTS MALFUNCTIONED A ERAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 882EA 098 CENTER AISLE EMERG EXIT LIGHT GOES OUT SHORTLY AFTER SWITCH IS TURNED ON. REMOVED AND REPLACED EMERG EXIT LIGHT BATTERY PACKS AS REQUIRED. OPS CKS GOOD. 2 H 7 2 4T RT A13NM 2007091200116 20070912 00116 EU 2007 9 12 07FDEA03439 1 20070907 A 5730 A57310052 PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 MISPINNED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 808FD 439 FOUND WRONG INSTALLED FASTENERS AT CENTER WING BOX, FRAME 40-47. REPAIR PERFORMED BY INSTALLING NEW OVERSIZED BULL NOSE FASTENERS IAW EA 6-5710- 95919 AND RAS/042817/015/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091200120 20070912 00120 EU 2007 9 12 07FDEA03443 1 20070907 A 5313 A53773636206 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 CORROSION AT STRG 51, BETWEEN FRAME 20-21 LHS, OUT OF LIMIT. SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007091200127 20070912 00127 EU 2007 9 12 07FDEA03450 1 20070907 A 5313 A53980852204 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 CORROSION ON STRINGER 54 LT BETWEEN C76-77, OUT OF LIMIT AS PER SRM 53-10-00. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14. 2 L 7 2 4F RT A35EU 2007080200162 20070802 00162 NM 2007 8 2 SWAA073683 1 20070726 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM BS 727D S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200167 20070802 00167 NM 2007 8 2 SWAA073675 1 20070726 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 380 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER 15R CRACKED AT BS 380. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007080200184 20070802 00184 NM 2007 8 2 SWAA073659 1 20070725 A 5311 6546558 FRAME BOEING 737 7373K2 13844BA NM BS 907 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200191 20070802 00191 WP 2007 8 2 ASAA0781911 1 20070726 A 5320 993053867 CUSP WEB DOUG DC9 DC983 3022083 WP BS 218-237 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 CUSP WEB CRACKED. REPLACED WEB PER SRM 51-10-4 AMD 51-30-2. 2 L 7 2 4F RT A6WE 2007080200192 20070802 00192 WP 2007 8 2 ASAA0781898 1 20070726 A 5320 99365343 WEB DOUG DC9 DC983 3022083 WP BS 170-199 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 CABIN FLOOR MEMBRANE CORRODED. CUT OUT DAMAGED AREA AND INSTALLED REPLACEMENT WEB PER SRM 51-70-4 AND 51-30-2. 2 L 7 2 4F RT A6WE 2007080200200 20070802 00200 WP 2007 8 2 UPS07850216 1 20070710 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FS 1140 L34R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 LONGERON ATTACH FITTING CRACKED AT STA 1140 L34R. REMOVED END FITTING AT STA 1140 L34R IAW SRM 51-1- 20D. FABRICATED AND INSTALLED REPLACEMENT END FITTING AT STA 1140 L34R IAW SRM 51-1-20D, AND DWG 475814. 2 L 7 4 4F RT 4A25 2007080300008 20070803 00008 NM 2007 8 3 UPS07450295 1 20070703 A 5311 65B01734102 FRAME BOEING 747 747212B 1384886 NM BS 820 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C RT BS 820 TENSION TIE TO FRAME CONNECTION AREA FOUND HOLE NR 4 CRACK AT FRAME WEB DOUBLER APPROX 0.040 ". M/ BS 820 RT TENSION TIE TO FRAME WEB ATTACH DOUBLER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND EO B747-531 0-23715-C AND SRM 51-30-02. 2 L 7 4 4F A20WE 2007080300010 20070803 00010 NM 2007 8 3 UPS07450297 1 20070703 A 5320 CHANNEL BOEING 747 747212B 1384886 NM BS 860 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C RT BS 860 TENSION TIE TO FRAME CONNECTION AREA FOUND HOLE NR 5 CRACK AT FWD CHANNEL APPROX 0.030". M/ D BS 860 RT TENSION TIE FWD CHANNEL REPAIRED AS PER RS R53-25-35820 AND UPS EO B747-5310-27253. CONTINUED INSPECTIONS A RE REQUIRED AS PER RS R53-25-35820 AND UPS EO B747-5310-27253. 2 L 7 4 4F A20WE 2007080300013 20070803 00013 NM 2007 8 3 UPS07450300 1 20070703 A 5311 65B0174069 FRAME BOEING 747 747212B 1384886 NM BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C LT BS 940 TENSION TIE NR 1 FASTENER HOLE FOUND CRACK AT WEB DOUBLER RUNNING 5 O/C POSITION APPROX 1/16 " IN LENGTH. M/D BS 940 LT SIDE FRAME DOUBLER THROUGH FRAME TENSION TIE, STEEL PLATE AND FAIL/SAFE CHORD HOLE OVERSIZED AND FASTENER INSTALLED AS PER UPS EO B747-5310-23715 APP D AND C. 2 L 7 4 4F A20WE 2007080300016 20070803 00016 NM 2007 8 3 UPS07450304 1 20070702 A 5311 65B0173534 FRAME BOEING 747 747212B 1384886 NM BS 840 S10R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C CRACK FOUND AT BS 840 RT SIDE S10R TENSION TIE ATTACHED FRAME CRACK LOCATED AT NR 4 FASTENER HOLE 0.03 0" APPROX RUNNING O/B DIRECTION. M/D BS 840 BETWEEN STR 8R TO STR 12R FRAME REPAIRED AS PER RS R53-25-35818 AND UPS EO B747-5310-27272-A. CONTINUED INSPECTIONS ARE REQUIRED AS PER RS R53-25-35818 AND UPS EO B747-5310-27272. 2 L 7 4 4F A20WE 2007080300025 20070803 00025 NM 2007 8 3 UPS07450310 1 20070702 A 5310 CHANNEL BOEING 747 747212B 1384886 NM BS 880 S9R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C CRACK FOUND AT BS 880 RT SIDE S9R TENSION TIE ATTACH FWD CHANNEL CRACK LOCATED AT NR 9 FASTENER HOLE 0 .030" APPROX. RUNNING UPWARD DIRECTION, M/D BS880 TENSION TIE FWD CHANNEL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALL ED AS PER UPS EO B747-5310-23715-C AND SRM 51-30-02 REFER NRC 50073 FOR WORKING DETAIL. 2 L 7 4 4F A20WE 2007080300038 20070803 00038 NM 2007 8 3 UPS07450321 1 20070703 A 5320 CHANNEL BOEING 747 747212B 1384886 NM BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C RT BS940 TENSION TIE TO FRAME CONNECTION AREA FOUND 2 FASTENER HOLES CRACKED AND 3 FASTENER HOLES OVAL AT AFT CHANNEL. M/D BS 940 RT TENSION TIE AFT CHANNEL LT TO RT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51- 30-02 AND EO B747-5310-23715-C. 2 L 7 4 4F A20WE 2007080300040 20070803 00040 NM 2007 8 3 UPS07550238 1 20070629 A 5420 313N305039 FAIRING BOEING 757 75724APF 1384969 NM NR 2 PYLON DEBONDED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 402UP 23724 INSPECTION TYPE:C NR 2 PYLON AFT FAIRING INBD AND OUTBD SKIN FORWARD END UPPER CORNER DISBONDED AND WORN SURFACE (PANEL RACK). REPAIRS ACCOMPLISHED PER FINAL EA NR 757-5451-27-A1704 AND UPS FILE NUMBER 757-54-20083, REPAIR WAS IDENTIFIED P ER STEP NR 11 OF FINAL EA. 2 L 7 2 4F RT A2NM 2007080300042 20070803 00042 NM 2007 8 3 UPS07550241 1 20070628 A 5412 311N3271 BULKHEAD BOEING 757 75724APF 1384969 NM NR 1 PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 402UP 23724 INSPECTION TYPE:C NR 1 PYLON, AFT BULKHEAD (LT) LOWER, INNER AND OUTER SURFACE HAS A CHAFED/GOUGES. MILL AND NDT WERE D ONE ON TRAV NR T7/689684. HFEC WAS DONE ON TRAV NR T7/689684. MILLED AREA 1.25W BY 2.1L BY .080 REMOVED ORIGINAL THICK NESS SHOT PEENED AREA PER SOPM 20-10-03 REF EA NR 757-5451-27-A1703 PRELIMINARY 1. 2 L 7 2 4F RT A2NM 2007080300050 20070803 00050 SO 2007 8 3 C2XA07IA176 1 20070726 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14972 145151 MTY - FLIGHT 2702, THE CREW REPORTED A LG AIR/GRD FAIL AFTER T/O MSG WENT AWAY. WE WERE ABLE TO USE DOWN LOCK REL TO RA ISE GEAR. THE AIRCRAFT RETURNED TO MTY WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NOSE PROX SW ITCH AND CONNECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007080300053 20070803 00053 NM 2007 8 3 CALA0700379 1 20070708 A 5730 65C25204 SKIN BOEING 737 7373T0 1384582 NM LT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND LT WING SKIN CORRODED ON TOP SURFACE AT APPROX WS 175 JUST FORWARD OF TRAPEZOIDAL PANEL NEAR CENTER LIN E. LOCATED ABOUT 17 FASTENERS I/B OF O/B TIP OF TRAPEZOIDAL PANEL FORWARD OF NR 4 SPOILER. REPAIRED IAW ECRA 5720-0202 2. 2 L 7 2 4F RT A16WE 2007080300073 20070803 00073 EA 2007 8 3 QXEA200701190 1 20070722 A 5230 HANDLE CNDAIR CL600 CL6002C10 1390015 EA CARGO DOOR UNSECURE A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 618QX 10205 PDX - FLIGHT 2521- AFTER TAKEOFF RECEIVED A AFT CARGO DOOR CAUTION MESSAGE, RETURNED TO THE FIELD AND ACCOMPLISHED A UNE VENTFUL LANDING. MAINTENANCE FOUND THE HANDLE POPPED OUT. CHECKED DOOR AND SECURED HANDLE WITH NO DEFECTS NOTED. AIRC RAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007080300074 20070803 00074 EA 2007 8 3 QXEA200701191 1 20070721 A 2150 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA RT PACK UNKNOWN A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 603QX 10011 PDX- FLIGHT 2551- RIGHT PACK CAUTION MESSAGE AFTER ENGINE START, RETURNED TO THE GATE. MAINTENANCE CHECKED THE SYSTEM W ITH NO DEFECTS NOTED, COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007080300081 20070803 00081 WP 2007 8 3 IXXA07SMN185S 1 20070630 A 5340 3750497U2 FITTING DOUG DC8 DC873F 302199F WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND IN MIDSHIP ACCESSORY COMPARTMENT A FITTING CRACKED STATION 660.000 LONGERON 36. REMOVED CRACKED FITTING. INSTALLED NEW FITTING. IAW DC8 SRM 51-1-20D, AND SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007080300084 20070803 00084 2007 8 3 HALA0700306 4 20070726 A 3416 6225048381 CONTROL PANEL BOEING 767 76733A 1385209 NM RADAR MALFUNCTIONED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM, PREFLIGHT, COPILOTS RADAR ALT DH REF INDICATOR WILL NOT RESET. REPLACED F/O'S EFIS CONTROL PN L. GND OPS CHK OK IAW 34-22-02. NO FAULTS NOTED. A/C OK TO REMAIN AT LAND 3 STATUS. 2 L 7 2 4F RT A1NM 2007080300085 20070803 00085 SO 2007 8 3 SIMA200721301 1 20070725 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS FAILED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 628AE 11433 41 145124 FORWARD EXIT SIGN ABOVE FLIGHT ATTENDANT SEAT WILL NOT ILLUMINATE. REMOVED AND REPLACED NR 1 EMERGENCY BATTERY IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007080300090 20070803 00090 2007 8 3 HNAA0700158 4 20070728 A 3442 82200015003 RADAR DHAV DHC8 DHC8102 2809003 NM WX SYSTEM FAILED A HNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 07 941HA 161 WHILE EN ROUTE GSO-DCA WEATHER RADAR STOPPED PAINTING WEATHER. CREW SHUT THE WX RADAR DOWN FOR 5 MINUTES THEN RESTARTED AND THAT DID NOT FIX IT. WITH THUNDERSTORMS AHEAD THE CREW CALLED DISPATCHER AND THEY BOTH DECIDED TO DIVERT TO ROA AW AY FROM THE THUNDERSTORMS TO A MAINTENANCE BASE. TO GET THE AIRCRAFT REPAIRED. 2 H 7 2 4T RT A13NM 2007080300104 20070803 00104 NM 2007 8 3 DHL2007784535 1 20070722 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 FUSELAGE INTERIOR SEAT TRACK FROM BS 760 TO BS 850, LBL 45.50, WL 208.5 IS CORRODED. REMOVED SEAT TRACK OUT OF LIMITS S TA 760 TO 850 IAW B727 SRM 51-30-2. FABRICATED NEW SEAT TRACK FROM P/N BAC1520-841-7178T6, DIM 94.875 IAW B727 SRM 53-1 0-5, FIG 2. TREATED, PRIMED AND INSTALLED SEAT TRACK IAW B727 SRM 51-10-2 AND 53-10-5, FIG 2. 2 L 7 3 4F A3WE 2007080300105 20070803 00105 NM 2007 8 3 UPS07450245 1 20070705 A 5313 STRINGER BOEING 747 747212B 1384886 NM BS 485 DEFORMED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C FWD CARGO COMPT S38L STRINGER FOUND DEFORM AT STA 485, FWD CARGO COMPT BS 484 TO BS 496 STR38L STRINGE R REPAIRED AS PER SRM 53-10-03 FIG 3. 2 L 7 4 4F A20WE 2007080300109 20070803 00109 NE 2007 8 3 MWEA070162 2 20070727 A 7321 114E7842G120 EEC BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE LT ENGINE INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 922ME 55184 13414 LEFT ENGINE SYSTEM FAIL ALERT AND ENGINE POWER BEGAN TO DECREASE. REMOVED AND REPLACED LEFT ENGINE EEC. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007080300121 20070803 00121 NM 2007 8 3 HALA0700310 1 20070729 A 2410 734284F GCU BOEING 767 7673G5 1385126 NM RIGHT FAILED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM, RT GENERATOR FIELD OFF LIGHT ON, WILL NOT RESET. REPLACE RT GCU OPS CK OKAY PER AMM 24-22-02- 404-010, NO FAULTS NOTED. 2 L 7 2 4F RT A1NM 2007080700076 20070807 00076 NM 2007 8 7 UPS07450283 1 20070703 A 5320 PLATE BOEING 747 747212B 1384886 NM BS 900 MISINSTALLED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D BS 900 RT TENSION TIE FWD ATT STEEL PLATE UPPER ROW NR 5 FASTENER HOLE (COUNT FROM I/B) FOUND SHOR T EDGE MARGIN. M/DECK BS 900 RT TENSION TIE FWD ATTACH STEEL PLATE REPAIRED AS PER HX RS NR R53-25-35819 CONTINUE INSPE CTION IS REQUIRED AS PER UPS EO NR B747-5310-27294. 2 L 7 4 4F A20WE 2007080700079 20070807 00079 WP 2007 8 7 IXXA07SMN181S 1 20070630 A 5340 4772397U FITTING DOUG DC8 DC873F 302199F WP ZONE 200 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE FITTING CRACKED AT LONGERON 17 RIGHT AT STATION 1768.000. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, 51-3-0, 51-3-1, DC8 SRM 51-1-21, 51-3-0, AND SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007080700080 20070807 00080 EU 2007 8 7 TRBA2007057 1 20070724 A 3350 7012210 LAMP AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHTS INOPERATIVE A TRBA O OTHER O OTHER NR NOT REPORTED 1 SO 29 529AM 529 PAX DOOR EMERGENCY STAIR LIGHT INOPERATIVE. REPOSITIONED LAMP IAW MM NR 33-51-24. OP CK IAW JIC 33-50-00. 2 H 7 2 4T RT A53EU 2007080700081 20070807 00081 NM 2007 8 7 DHL2007784518 1 20070719 A 5520 ANGLE BOEING 727 727227 1384078 NM RT ELEVATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 SUSPECT CRACKED ANGLE AT RT ELEVATOR INBD AFT END, R ELEV STA 36.91 TO 53.91. OPENED END CAP ON RT ELEVATOR INBD SIDE F OUND ANGLE CRACKED AND OPENED ELEVATOR SKIN PANEL. CUT OUT DAMAGED AREA OF ANGLE, REAR SPAR 1 BY 2 IAW B727 SRM 51-40-3 . FABRICATED REPAIR DOUBLER FROM 2024T3, .032, 10.75 BY 3 AND FILLER FROM 2024T3, .032, 2 BY 1 IAW B727 SRM 55-20-2, FI G 4 AND 51-40-3. TREATED, PRIMED, INSTALLED PARTS AND CLOSED SKIN PANEL IAW B727 SRM 51-10-2, 51-30-2, 51-40-3. RECALC ULATED MOMENT IS 134.4 AND WITHIN LIMITS OF 120+-20 IAW B727 SRM 51-80-7, PARA 2. Y=31 WEIGHT CHANGE =.2, M=6.2. NEW MO NENT ETCHED ON ELEVATOR PLACARD. NO FURTHER ACTION REQUIRED. 2 L 7 3 4F A3WE 2007080700084 20070807 00084 SO 2007 8 7 N93A26072007 1 20070726 A 3250 POTENTIOMETER GULSTM G1159 GIV 3980115 SO NLG STEERING MALFUNCTIONED E N93A K NONE O OTHER TX TAXI/GRND HDL 1 SO 13 441QS 1341 DURING TAXI, NOSE WHEEL STEERING MOVES LEFT AND RIGHT UNCOMMANDED. 2 L 7 2 4F RT A12EA 2007080700086 20070807 00086 NE 2007 8 7 BSAASDR0722 2 20070722 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWC PT6 PT6A67AG 52211 NE RIGHT SURGES A BSAA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 NM 05 132YV UE132 114105 DURING CLIMB AND CRUISE THE RT ENGINE SURGED SEVERAL TIMES. ENGINE SHUT DOWN ON FINAL. INSPECTED PROP GOV, AND OVERSPE ED GOV DUMP VALVE WIRING AND CONNECTOR. REINSTALLED CONNECTORS IN RESPECTIVE POSITIONS. GROUND CHECK NORMAL, WITH NO F URTHER DISCREPANCIES. PT6A-67D NOT LISTED FOR REPORT. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080700088 20070807 00088 EA 2007 8 7 MASA200700304 1 20070605 A 3350 RELAY CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 932LR 15032 ASH RON PHX - PILOT REPORTED EMERGENCY LIGHTS CYCLING ON AND OFF. MAINTENANCE REPLACED (K135) RELAY, OPS CHECK GOOD. A IRCRAFT CONTINUED OPERATIONS. 2 L 7 2 4F RT A21EA 2007080700092 20070807 00092 EA 2007 8 7 MASA200700315 1 20070609 A 3350 CONTROL PANEL CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT SMOKE A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 910FJ 15010 ASH 2917 ELP - CAPTAIN REPORTED ON POWER UP OF AIRCRAFT, THERE WAS SMOKE COMING OUT FROM BEHIND THE FO'S LIGHTING PANEL. MX CHANGED FLOOD LIGHT. 2 L 7 2 4F RT A21EA 2007080700093 20070807 00093 EA 2007 8 7 MASA200700317 1 20070610 A 3350 LENS CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77302 7302 ASH 7185 AVP - CREW REPORTED THE MID CABIN EMERGENCY CALL LIGHT RED LENS IS MISSING. AIRCRAFT WAS BEING PREPARED TO FER RY TO ORD WHERE THE PART IS AT TIME OF REPORT TO HAVE THE LENS INSTALLED. MX REMOVED AND REPLACED LENS. 2 L 7 2 4F RT A21EA 2007080700097 20070807 00097 EA 2007 8 7 MASA200700325 1 20070612 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN CONTAMINATED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37228 7228 ASH 2752 PHX - FWD HALF OF EMERGENCY FLOOR PROXIMITY LIGHTING INOP. MX CLEANED WATER FROM THE LIGHT STRIP ASSEMBLIES AN D THE OP CHECK WAS GOOD. 2 L 7 2 4F RT A21EA 2007080700100 20070807 00100 EA 2007 8 7 MASA200700332 1 20070617 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77278 7278 ASH 2704 PHX - EMERGENCY PATH LIGHTING INOP (FIRST 3 STRIPS). REMOVED AND REPLACED EMERG FLOOR STRIPS. 2 L 7 2 4F RT A21EA 2007080700106 20070807 00106 WP 2007 8 7 IXXA07SMN183S 1 20070630 A 5340 4772397U1 FITTING DOUG DC8 DC873F 302199F WP ZONE 200 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 1760.000 TO 1766.000 LONGERON 10 RIGHT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, 51-3-1. 2 L 7 4 4F RT 4A25 2007080700111 20070807 00111 EU 2007 8 7 07FDEA02653 1 20070728 A 5315 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 653FE 736 FLOORBEAM FRAME 31 BETWEEN SEAT TRACKS NR L4 AND NR 5L HAS A .5 INCH CRACK AT STIFFENER. CUT OUT CRACKED SECTION OF FLO ORBEAM IAW A300-600 FREIGHTER SRM 53-10-15. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW A 300-600 FREIGHTER SR M 53-10-15. ALODINED FLOORBEAM, REPAIR ANGLE AND FILLER IAW A300-SRM 51-21-10. PRIMED ALL PARTS IAW A300 SRM 51-75-10. TOPCOATED REPAIR IAW A300 SRM 51-75-10. 2 L 7 2 4F RT A35EU 2007080700112 20070807 00112 EU 2007 8 7 07FDEA02654 1 20070728 A 5320 20240080 ANGLE AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 653FE 736 MDCC AT FR 24 BETWEEN STG 11R AND 15R HAS 4 EA GOUGES APPROX 4 " ZONE 230 REF A300- 600 SRM 51-10-00. BLENDED GOUGES ( 4EA) FR 24 BETWEEN STR 11R AND 15R IAW A300 SRM 51-73-10 1 EA AREA OUT OF LIMITS IAW A300 SRM 53-10-00 PG 101 B=.63 A=0. 50 L= .013. FABRICATED REPAIR ANGLE IAW A300-600 FREIGHTER SRM 53-10-13 FIG 202. ALODINED REPAIR IAW A300 SRM 51-21-10 . PRIMED REPAIR IAW A300 SRM 51-75-10. INSTALLED REPAIR IAW A300-600 FREIGHTER SRM 53-10-13 FIG 202. 2 L 7 2 4F RT A35EU 2007080700113 20070807 00113 EU 2007 8 7 07FDEA02661 1 20070729 A 5210 PANEL AIRBUS 300 A300F4605R 3930327 EU PAX DOOR MISALIGNED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 667FE 771 FL 390 LEFT MAIN CABIN DOOR ALARM AND LIGHT FLASHING, ADV BY JUMPSEAT, RT INDICATOR BETWEEN LOCK AND UNLOCK. DOOR ALARM OFF IN DESCENT BELOW FL 200/PRESSURE DIF.6.7 CABIN AT 3300' NO ECAM INDICATIONS FOR THE LEFT CABIN UNLOCKED. FOUND CO VER PANEL OF DOOR (INTERIOR) MISALIGNED CAUSING HANDLE NOT TO ENGAGE PROPERLY, REALIGNED AND SECURED DOOR PANELS PER SMP 20-00, DOOR OPS CKS NORMAL AT THIS TIME. 2 L 7 2 4F RT A35EU 2007080700114 20070807 00114 WP 2007 8 7 07FDEA02666 1 20070730 A 5313 LONGERON DOUG DC10 DC1010F 3022111 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 FWD CARGO COMPT BILGE ON LONGERON LT SIDE FOUND CRACKS. REPAIRED LONGERON IAW SRM 53-10-00 VOL 1 FIG 5 SHT 1. 2 L 7 3 4F A22WE 2007080700116 20070807 00116 EU 2007 8 7 07FDEA02676 1 20070730 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 FOUND ALC STR 51L CORRODED BETWEEN FR 58 AND FR 61. [08-20-07] REMOVED AND REPLACED STRINGER 51L BETWEEN FRAMES 58 AN D 65 IAW SRM 51-40-21 PG1 AND 53-10-14. 2 L 7 2 4F RT A35EU 2007080700119 20070807 00119 SO 2007 8 7 SIMA200721102 1 20070726 A 3350 20131A BATTERY PACK EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHT FAILED A SIMA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SW 21 846AE 8315 1848 145692 EMERGENCY LIGHTS NO TEST. REMOVED AND REPLACED ALL FOUR BATTEY PACKS IAW EMB AMM. OPERATIONAL CHECK GOOD. RETURNED AI RCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007080700121 20070807 00121 NM 2007 8 7 AWXA200700909 1 20070706 A 5320 654695812 CUSP WEB BOEING 737 7373G7 1384595 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5962202, CORROSION ON CUSP SHEAR WEB, BS 486 - BS 500, S17R. REPLACED CUSP SHEAR W EB, BS 486 - BS 500, S17R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007080700122 20070807 00122 NM 2007 8 7 AWXA200700910 1 20070705 A 5320 65479765 CUSP WEB BOEING 737 7373G7 1384595 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5962161, CORROSION ON CUSP SHEAR WEB, BS 807 - BS 827, S17R. REPLACED CUSP SHEAR W EB, BS 807 - BS 827, S17R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007080700125 20070807 00125 NM 2007 8 7 AWXA200700913 1 20070705 A 5311 90526911 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961287, CRACKED FRAME, BS 500A, S9R. REPAIRED FRAME, BS 500A, S9R IAW USAIRWAYS E A 120121. 2 L 7 2 4F RT A16WE 2007080700126 20070807 00126 NM 2007 8 7 AWXA200700914 1 20070704 A 5311 90526911 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5981842, CRACKED FRAME, BS 807, S9L. REPAIRED FRAME, BS 807, S9L IAW USAIRWAYS EA 120121. 2 L 7 2 4F RT A16WE 2007080700128 20070807 00128 NM 2007 8 7 AWXA200700916 1 20070704 A 5311 90526911 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5981848, CRACKED FRAME, BS 767, S9R. REPAIRED FRAME, BS 767, S9R IAW USAIRWAYS EA 120121. 2 L 7 2 4F RT A16WE 2007080700130 20070807 00130 NM 2007 8 7 AWXA200700918 1 20070705 A 5311 65465302 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MAJOR REPAIR - C-20 CHECK - NR 5961289, CRACKED FRAME, BS 440, S9R. REPAIRED FRAME, BS 440, S9R IAW USAIRWAYS EA 120121 . 2 L 7 2 4F RT A16WE 2007080700133 20070807 00133 NM 2007 8 7 AWXA200700921 1 20070704 A 5311 65465548 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5981844, CRACKED FRAME, BS 867, S9L. REPAIRED FRAME, BS 867, S9L IAW USAIRWAYS EA 120121. 2 L 7 2 4F RT A16WE 2007080700134 20070807 00134 NM 2007 8 7 AWXA200700922 1 20070705 A 5311 90526911 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961279 AND 5961288, CRACKED FRAME, BS 480, S9L AND S9R. REPAIRED FRAME, BS 480, S 9L AND S9R IAW USAIRWAYS EA 120121. 2 L 7 2 4F RT A16WE 2007080700135 20070807 00135 NM 2007 8 7 AWXA200700923 1 20070704 A 5311 65465588 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5981845 AND 5981452, CRACKED FRAME, BS 907, S9L AND S9R. REPAIRED FRAME, BS 907, S 9L AND S9R IAW USAIRWAYS EA 120121. 2 L 7 2 4F RT A16WE 2007080700136 20070807 00136 NM 2007 8 7 AWXA200700924 1 20070704 A 5311 654655211 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5981843 AND 5981849, CRACKED FRAME, BS 827, S9L AND S9R. REPAIRED FRAME, BS 827, S 9L AND S9R IAW USAIRWAYS EA 120121. 2 L 7 2 4F RT A16WE 2007080700137 20070807 00137 NM 2007 8 7 AWXA200700925 1 20070704 A 5311 654655734 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5981451, CRACKED FRAME, BS 887, S9R. REPAIRED FRAME, BS 887, S9R IAW USAIRWAYS EA 120121. 2 L 7 2 4F RT A16WE 2007080700139 20070807 00139 NM 2007 8 7 QXEA200701222 1 20070729 A 2430 RELAY DHAV DHC8 DHC8202 2809007 NM INOPERATIVE A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 346PH 477 PDX FLIGHT NR 2098 - UPON PUSHBACK AUX INVERTER CAUTION LIGHT ILLUMINATED. MAINTENANCE REPLACED RELAY 24-22-K3. OPERAT IONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007080700144 20070807 00144 EA 2007 8 7 TIPR200705001 1 20070711 A 5313 BAC1498200 STRINGER FRCHLD 24 24W41A 3370620 EA CONT R670 W670* 17016 SO BS 412-434 CORRODED C K NONE O OTHER IN INSP/MAINT 1 SO 05 609 W41104 DEFECT CORROSION ALONG STRINGER 38L, BS 412 TO 434 UNDER DOME SEALANT. SPLICED IN STRINGER SECTION IAW SRM. 1 H 7 1 3R 3 R A707 E162 2007080700147 20070807 00147 NE 2007 8 7 HEEA116405 1 20070711 A 5340 BRACKET SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL PROX SWITCH LOOSE B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 762P 760060 LANDING GEAR WOULD NOT RETRACT. FOUND NOSE WHEEL CENTERING PROXIMITY SWITCH BRACKET LOOSE. TIGHTENED BRACKET AND CHECK ED AND ADJUSTED SWITCH GAP. 1 G 7 2 3U 3 U H1NE E1GL 2007080700153 20070807 00153 NM 2007 8 7 DU4R2007149 1 20070702 A 5311 FRAME BOEING 757 757 UTILUSE NM PWA 2037 PW2037 NE BS 1500 DENTED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 638DL 23761 NR 291043, NR 22882 - FOUND DENT ON MAIN FRAME UPPER CAP IN AFT PIT BS 1500 BETWEEN STRINGERS S25-R AND S-26R. REPAIRED BY CUTTING DENTED AREA, HFEC CUT OUT IAW D6-34N301, PT. 6 51-00-19, NO RELEVANT INDICATIONS. FABRICATED AND INSTALLED REPAIR 19.2500 X 2.7500 X 1.5 FROM 7075-T6 .063 IAW SRM 51-20-01, DPS 900-2 NR 3, 53-00-07, 51-20-01 AND 51-40-02. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080700157 20070807 00157 EA 2007 8 7 O2G2007F00001 1 20070627 A 2820 9648V470081 SOLENOID VALVE CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF34* NE FUEL VENT LINE FAILED E O2GA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 EA 63 601BE 5103 FUEL VENTING FROM LT VENT. REMOVED AND REPLACED VENT SOLENOID VALVE. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007080700166 20070807 00166 CE 2007 8 7 AMWA15036A 1 20070710 A 5311 12944000681 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA BS 438 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 155ZV UE155 FUSELAGE FRAME AT FS 438.25 LT HAD CHAFFING. REPAIRED IAW ACFT ENGINEERING REPORT NR 6772-2 REV 1R. 2 L 7 2 4T 3 T RT A24CE E2NE 2007080700177 20070807 00177 2007 8 7 WNH2007F00000 4 20070522 A 3416 2871101 ALTIMETER BEECH 90 C90A 1152911 CE PWA PT6 PT6* 52043 EA COCKPIT MALFUNCTIONED E WNHA O OTHER O OTHER NR NOT REPORTED 1 WP 25 73PG 26 LJ1607 ENCODING ALTIMETER DISPLAY FADES IN AND OUT TO THE POINT THAT THE INFORMATION DISPLAYED IS ILLEGIBLE TO THE PILOT. (K) 1 L 7 2 3T 3 T RT 3A20 E2NE 2007080700179 20070807 00179 EU 2007 8 7 PG9A115822 1 20070511 A 2913 PUMP UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE HYD SYSTEM WORN B PG9A O OTHER J WARNING INDICATION CR CRUISE 1 WP 19 131GC 3638 3691 PILOT REPORTED A SERVO AND HYD LIGHT ILLUMINATION DURING FLIGHT. UPON INSPECTION IT WAS FOUND, THAT THE SPLINES OF THE B ELT DRIVEN HYD PUMP DRIVE COUPLING HAD WORN TO THE POINT THEY WERE SLIPPING. REPLACED HYD PUMP AND DRIVE COUPLING. 1 G 7 2 3U 3 U H9EU E00054EN 2007080700180 20070807 00180 NM 2007 8 7 AMTA200700331 1 20070710 A 4930 AV16E1209D VALVE BOEING 737 73783N 13844HI NM APU UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 304TZ 30675 APU FAILED TO LIGHT OFF ROTATION AND IGNITION. OK, NO FUEL FLOW. TROUBLESHOT SYSTEM IAW FIM 49-31-00-810-808. FOUND A PU FUEL SHUTOFF VALVE WOULD NOT OPEN. REMOVED AND REPLACED VALVE IAW AMM 28-25-02-4. OPS CHECK GOOD. (K) 2 L 7 2 4F RT A16WE 2007080700183 20070807 00183 2007 8 7 AMTA200700333 4 20070710 A 2210 FEEL UNIT LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE PITCH TRIM OUT OF RIG A AMTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 164AT 1238 IN FLIGHT ABOVE 20,000 FT, WHEN AUTOPILOT ENGAGED PITCH TRIM MOVES FULL NOSE DOWN AND AC LEAVES ASSIGNED TRIM MOVES FULL NOSE DOWN AND AC LEAVES ASSIGNED ALTITUDE. AP LIMIT FLAG DISPLAYS. RIGGED MECHANICAL PITCH FEEL IAW MM 27-41-17. OPS CHECK NORMAL. (K) 2 L 7 3 4F 4 F A23WE E12EU 2007080800003 20070808 00003 NM 2007 8 8 AMTA200700338 1 20070711 A 2150 UNKNOWN BOEING 737 73783N 13844HI NM RT A/C PACK WARNING MESSAGE A AMTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 11 323TZ 30033 DURING CLIMB OUT, RT PACK LIGHT ILLUMINATED MASTER CAUTION AND AIR COND LIGHT DID NOT ILLUMINATE. PERFORMED RT PACK TEM P/ZONE CONTROLLER BITE IAW FIM 21-62-00-810-801, FLT FAULT WOULD NOT VERIFY, REF 2100/117, AND PERFORMED MASTER CAUTION FIN 31-52-00-810-801, NO FAULTS NOTED. (K) 2 L 7 2 4F RT A16WE 2007080800004 20070808 00004 NM 2007 8 8 AMTA200700339 1 20070711 A 2150 UNKNOWN BOEING 737 73783N 13844HI NM RT A/C PACK WARNING MESSAGE A AMTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 11 323TZ 30033 RT PACK LIGHT ILLUMINATED ON CLIMB OUT, PACK LIGHT EXTINGUISHED AFTER RESETTING MASTER CAUTION. PERFORMED RT PACK ZONE/ TEMP CONTROLLER BITE IAW FIM 21-62-00-810-801, FOUND FLT FAULT TCV. RESET FAULT, FAULT WOULD NOT VERIFY, RT PACK BITE T EST OK. INTERMITTENT FAULT. 30 DAY HISTORY, NO FAULTS. 2 L 7 2 4F RT A16WE 2007080800005 20070808 00005 2007 8 8 AMTA200700340 4 20070714 A 2310 TRANSCEIVER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT HF SYSTEM INOPERATIVE A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 518AT 27974 RT HF RADIO INOPERATIVE. UNREADABLE ON ALL FREQUENCIES. RT HF CKD GOOD ON GROUND. CONTACTED SFO, TRANSMIT AND RECEIVE GOOD. OPS CK IAW MM 23-11-00-5. SWAPPED TRANSCEIVERS FOR T/S. LT NOW PN 0964-0452-022, SN 0326. RT NOW 0964-0452-01 2, SN XK516D1-01235. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007080800020 20070808 00020 CE 2007 8 8 DJFA2007073 1 20070716 A 5411 675132010 RIB CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RT PYLON CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 707LX 5370 7500078 DURING A SCHEDULED INSPECTION, MAINTENANCE DISCOVERED A RIB IN THE RT PYLON, CRACKED. THE RIB WAS CRACKED AT THE UPPER AND LOWER FLANGES. BOTH CRACKS WERE APPROX 2 INCHES LONG. THE RIB WAS REPLACED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007080800021 20070808 00021 CE 2007 8 8 DJFA2007075 1 20070718 A 2170 M832481033 COALESCER BAG CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CABIN AIR DIRTY E DJFA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 706LX 5549 7500073 TRIP NR 1204364- DURING CRUISE, CREW NOTICED A BURNING SMELL FROM THE AIR DISTRIBUTION SYSTEM. CREW ISOLATED PROBLEM TO THE NR 1 PACK. THE PACK WAS SHUT DOWN AND THE FLIGHT CONTINUED TO ITS DESTINATION. MAINTENANCE FOUND THE COALESCER BA G DIRTY; IT WAS CLEANED AND REINSTALLED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007080800024 20070808 00024 WP 2007 8 8 ASMF200707013 1 20070716 A 2820 AV16B1736D VALVE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUEL SYSTEM UNSERVICEABLE W ASMF K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SW 23 583MD 18775 49659 DURING TRANSIT CHECK A FUEL SPILLAGE OCCURRED AT PLATFORM. SPILLAGE STARTED WHEN THE AIRCRAFT WAS BEING REFUELED AND FUE L WAS TRANSFERRED FROM CENTRAL TANK TO LT TANK. MAINTENANCE PERSONNEL REPLACE THE LT FUEL FILL VALVE IAW MM 28-20-02 AND PERFORMED AN INDICATION TEST FUEL IAW MM 28-40-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007080800030 20070808 00030 NM 2007 8 8 TIPR200736001 1 20070723 A 5315 146T1206 FLOORBEAM BOEING 767 767222 1385122 NM PWA JT9 JT9D* NE BS 1197 CORRODED B K NONE O OTHER IN INSP/MAINT 1 SO 23 609UA 21870 AFT PIT FLOORBEAM UPPER T-CAP AT UPPER AND LOWER SURFACES HAS CORROSION AT BS1197 BETWEEN RBL 22 TO RBL 44. REMOVED COR ROSION IAW MM 51-00-53. FOUND TO BE BEYOND LIMITS IAW SRM 53-00-07. MATERIAL ID IS BAC1506-3123 IAW DRAWING 146T1206. F ABRICATED NEW T-CAP IAW DRAWING 146T1206. ALODINED, PRIMED AND PAINTED IAW SRM 51-20-01. INSTALLED NEW T-CAP IAW SRM 51- 40-02. REMOVED AND REINSTALLED AUX GUIDES IAW SRM 51-40-02. REFERENCE SO 599125 OPERATION 25191. 2 L 7 2 4F 4 F RT A1NM E20EA 2007080800032 20070808 00032 CE 2007 8 8 DJFA2007079 1 20070721 A 7830 20200081 IDLER LINK BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE THRUST REVERSER BROKEN E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 731TA 6125 RK273 ON POST FLIGHT, CREW NOTICED DAMAGE TO THE RT THRUST REVERSER (TR). MAINTENANCE FOUND THE IDLER ARM ROD END BROKEN. T HE BREAK BISECTED THE ROD END PERPENDICULAR TO THE ARM. THE BUSHING REMAINED ATTACHED TO THE DOOR ASSEMBLY. THE BROKEN ARM INDUCED ADDITIONAL DAMAGE INTO THE ADJACENT STRUCTURE. THE (TR) WAS REMOVED AND REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007080800033 20070808 00033 CE 2007 8 8 GLBA20060963 1 20070720 A 2150 ACM BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CABIN AIR CONTAMINATED A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 170GL UE170 PILOTS REPORTED A STRONG EXHAUST ODOR IN CABIN WITH HEAT TURNED ON. MAINTENANCE REMOVED EXCESS WATER IN ACM AND CLEANED OBSTRUCTION IN WATER NOZZLE ASSEMBLY. OPERATIONAL CHECK OF THE SYSTEM IAW 21-40-00 AND 21-50-00 WAS GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080800037 20070808 00037 CE 2007 8 8 DXTA200702342 1 20070717 A 2170 7464513 COALESCER BAG CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL AFT SERVICE BAY DIRTY E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 983QS 7870 7500083 THE CABIN PAC TEMP IS UNCONTROLLABLE AND ALSO PRODUCING AN OILY SMELL IN THE CABIN. INSPECTED ACM, OIL, AND SERVICED, R EPLACED COALESCER SOCKS PERFORMED APU AND ENGINE RUNS, NO OIL SMELL PRESENT. PERFORMED OPS CHECK OF CABIN TEMP CONTROLE R WITH APU AND ENGINE WITH NO FAULTS NOTED. CONTROLS TEMP IN MANUAL AND AUTO REF CE 750 M/M 12-10-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007080800040 20070808 00040 CE 2007 8 8 DXTA200702346 1 20070718 A 2120 UNKNOWN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE CABIN ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 335QS 5600335 STRONG BURNING ODOR ENCOUNTERED IN FLIGHT. TURNED OFF AIR CONDITIONER AND ODOR DISSIPATED. INSPECTED FWD AND AFT AIR CO NDITIONING EVAPORATOR UNITS FOR BURNING SMALL AND SIGNS OF DAMAGE. CHECKED RESISTANCE OF FAN SPEED RESISTORS, BOTH READ 1.8 OHM NO SIGNS OF BORING ODOR OR DAMAGE NOTED. INSPECTED TAIL CONE ACM AND FREON COMPRESSOR UNITS AND DRIVE BELT. NO S IGNS OF DAMAGE NOTED. APPLIED ELECTRICAL LOADS TO AVIONICS SYSTEMS, RADIOS, LIGHTS, MFD, PFD'S, AIR CONDITIONING SYSTEMS , ETC. WITH ENGINES RUNNING FOR MORE THEN 20 MINUTES. NO SIGNS OF BURNING ODOR WAS NOTED. 2 L 7 2 4F 4 F RT A22CE E25EA 2007080800041 20070808 00041 CE 2007 8 8 DXTA200702347 1 20070719 A 3097 WIRE CESSNA 680 680CE 2076811 CE ANTI ICE SYSTEM BROKEN E DXTA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 350QS 6800036 INFLIGHT AT APPROX FL 300 THE AMBER LT IB WING ANTI-ICE MSG ILLUMINATED FOLLOWED BY THE LT OB WING ANTI-ICE AND THE LT W ING SUPPLY BLEED LEAK CAS MSGS. WE READ THE MFG CHECKLIST FOLLOWED THE PROCEDURE AND WERE UNABLE TO EXTINGUISH ANY OF T HE AMBER CAS MSGS. FOUND CUFF PANEL (LT) TEMPERATURE SENSOR WIRES BROKEN. REPAIRED WIRING IAW MODEL 680 WDM. 20-10-03. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RC T00012WI 2007091100155 20070911 00155 NM 2007 9 11 TSAA0753048 1 20070828 A 5330 SKIN BOEING 737 737210C 1384459 NM BS 908 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 834AL 20917 WHILE ACCOMPLISHING VISUAL INSPECTIONS TO COMPLY WITH AD 92-25-09, CORROSION WAS DISCOVERED AT BS 908 BETWEEN STR 17L AN D STR 24L. THE CORROSION WAS REPAIRED IAW SRM 53-3-03 FIG 48. 2 L 7 2 4F A16WE 2007091100163 20070911 00163 WP 2007 9 11 07FDEA03363 1 20070905 A 5310 ACA72261 DOOR FRAME DOUG DC10 DC1010F 3022111 WP ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 UPPER MAIN CARGO DOOR FOUND DEEP INTERGRANULAR CORROSION ON TOP OF LOWER DOOR JAMB, UNDER SPOOL FITTING NR 6. ACCOMPLI SHED EA NR 8-5310-111456. 2 L 7 3 4F A22WE 2007091100167 20070911 00167 EU 2007 9 11 07FDEA03367 1 20070905 A 5754 A57864038238 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 UNKNOWN REPAIR FOUND AT LT SLAT NR 2 NEAR JACKSCREW NR 3 ATTACH FITTING. REPAIR WAS RENEWED WITH DOUBLER IAW EA 6-5743- 92228 AND RAS/FOK/279/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091100170 20070911 00170 EU 2007 9 11 07FDEA03370 1 20070905 A 2750 4909505 COMPUTER AIRBUS 300 A300F4605R 3930327 EU TE FLAPS FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 692FE 878 ON TAKEOFF, THE FLAPS WOULD NOT RAISE PAST 20. RECYCLED SEVERAL TIMES NO CHANGE. ON APPROACH, THE FLAPS WOULD NOT GO P AST 20. ON LANDING, THE FLAPS RETURNED TO 0 DURING AFTER LANDING CHECK BOTH SFCC'S REPLACED. RAN ENGINES, OPERATED FLA PS FULL TRAVEL SEVERAL TIMES WITH NO FAULTS ON EITHER SFCC. CHECKED ALL FLAP JACKSCREWS FOR ABNORMALITIES. NONE NOTED. GREASE PRESENT AT ALL ROLLERS AND BEARINGS AND BALLNUTS. TORQUE LIMITER INDICATORS NOT POPPED. 2 L 7 2 4F RT A35EU 2007091100177 20070911 00177 WP 2007 9 11 AALA20071545 1 20070814 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 954U 49426 LGA - EMERGENCY LIGHTS AT AFT SEAT ROW INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT SEAT ROW. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007091100183 20070911 00183 EU 2007 9 11 TRBA2007074 1 20070902 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS FAILED A TRBA O OTHER O OTHER NR NOT REPORTED 1 SO 29 426AT 426 EMERGENCY FLOOR LIGHTS WILL NOT GO OUT. REMOVED AND REPLACED BATTERY PACK AT EMERGENCY POWER SUPPLY 61WL IAW JIC NR 33- 50-10. PERFORMED OPS CK IAW JIC NR 33-50-00 AND FOUND WORKING PROPERLY. 2 H 7 2 4T RT A53EU 2007091100189 20070911 00189 NM 2007 9 11 UPS07450565 1 20070813 A 5411 RIB BOEING 747 747212B 1384886 NM NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C NR 1 PYLON REAR ENG MOUNT BULKHEAD ATTACHMENT UPPER LINK BEAM O/B SIDE RIB ANGLE FOUND CRACKED FWD SID E, CRACK LENGTH 1" BY 1/2". NR 1 PYLON REAR ENG MOUNT BULKHEAD ATTACHMENT UPPER LINK BEAM O/B SIDE RIB ANGLE REPAIRED AS PER HX RS NR R54-51-35856 AND UPS EO NR B747-5410-27512, DETAIL REPEAT INSP OF THE SUBJECT REPAIRED AREA IS REQUIRED AT EVERY 'C' CHK OR 18 MONTHS PER HX RS NR R54-51-35856 AND UPS EO NR B747-5410-27512. 2 L 7 4 4F A20WE 2007091200070 20070912 00070 EU 2007 9 12 07FDEA03400 1 20070906 A 5315 A53970091216 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORROSION ON CARGO FLOOR CROSSBEAM FRAME 62, AD TO Y800, LHS. CROSSBEAM SPLICE REPAIR PERFORMED IAW SRM 53-10-15/ FIG 207. 2 L 7 2 4F RT A35EU 2007091200077 20070912 00077 EU 2007 9 12 07FDEA03409 1 20070906 A 5730 A57340087 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 ELONGATED HOLES CAUSED BY CHAFING OF HYDRAULIC LINES IN WING PYLON AFT SUPPORT BRACKET AND BOTTOM SKIN, RIB 8. REPAIR P ERFORMED BY OVERSIZING HOLES AND INSTALLING ECCENTRIC BUSHES IAW R572- 49184 ISSUE C, APPROVED B EA 6-5720-95912 AND RAS /BAE/1002263/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091200078 20070912 00078 EU 2007 9 12 07FDEA03410 1 20070906 A 5730 A57340087 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 ELONGATED HOLES CAUSED BY CHAFING OF HYDRAULIC LINES IN WING PYLON AFT SUPPORT BRACKET AND BOTTOM SKIN, RIB 8. REPAIR P ERFORMED BY OVERSIZING HOLES AND INSTALLING ECCENTRIC BUSHES IAW R572- 49184 ISSUE C, APPROVED B EA 6-5720-95912 AND RAS /BAE/1002263/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091200084 20070912 00084 EU 2007 9 12 07FDEA03416 1 20070906 A 5100 NONE AIRBUS 310 A310324 3930206 EU NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 FOUND OLD BONDED DOUBLER ON RT INBOARD FLAP, RIB 15-17, LOWER SKIN T/E, WITHOUT ANY RECORD. REPAIR RENEWED IAW SRM 57 -53-12/FIG 208, APPROVED BY EA 6-5752-95905 AND RAS/DABRE/7006189/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091200099 20070912 00099 EU 2007 9 12 07FDEA03393 1 20070906 A 5320 A53778807202 SUPPORT AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 FWD PIT LT SIDE PANEL SUPPORT HAS CORROSION ON LOWER SURFACE AT FR 36 LBL 50 REMOVED NUTPLATES AND CORROSION IAW FEDEX A 310 SRM 51-40-21 AND 51-74-10. FOUND TO BE OUT OF LIMITS IAW FEDEX A310 SRM 53-10-00. REMOVED AND REINSTALLED LT SLANT PANELS CARGO GUIDE RAILS, TRANSITION PANELS, MOUNTS AND ROLLER TRAYS FROM FR 23-38.2 IAW FEDEX A310 AMM 25-54-10-2. FA BRICATED T-CAP AND SPLICE ANGLE IAW FEDEX A310 SRM 53-10-15 ALODINED IAW FEDEX A310 SRM 51-21-10. PRIMED AND PAINTED IA W A310 SRM 51-23-10. INSTALLED T-CAP AND SPLICE ANGLE IAW FEDEX A310 SRM 53-10-15 AND 51-40-21. PDU OPS GOOD IAW FEDEX A310 AMM 25-52-26-4, MINOR REPAIR. 2 L 7 2 4F RT A35EU 2007091200102 20070912 00102 EU 2007 9 12 07FDEA03396 1 20070906 A 5320 A53612214201 FLOOR SUPPORT AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 HEAVY CORRODED LONGERON BETWEEN FRAME 12A-14, CABIN FLOOR STRUCTURE, OUT OF LIMIT AS PER SRM 53-10-00. REPAIR PERFORMED IAW SRM 53-12-15/FIG 207. 2 L 7 2 4F RT A35EU 2007091200112 20070912 00112 EU 2007 9 12 07FDEA03435 1 20070907 A 5310 A53981113 SHEAR PLATE AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 CRACKED SHEAR PLATES IN ZONE 170, FRAME 79, STRG 26 LHS AND RHS. REPAIR PERFORMED BY REPLACEMENT OF PARTS IAW SRM 51-72 -10. 2 L 7 2 4F RT A35EU 2007091200117 20070912 00117 EU 2007 9 12 07FDEA03440 1 20070907 A 5310 A53973085210 BEAM AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 808FD 439 OLD REPAIR ON AFT CARGO COMPARTMENT DOOR SILL BEAM BETWEEN FRAME 62-63, PLATE MATERIAL IS NOT CONFORM TO SRM 53-17-18/F IG 201. REPAIR RENEWED BY INSTALLING A CORRECT PLATE IAW SRM 53-17-18/FIG 201. 2 L 7 2 4F RT A35EU 2007091200118 20070912 00118 EU 2007 9 12 07FDEA03441 1 20070907 A 5753 A57970650003 VANE AIRBUS 310 A310324 3930206 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 DENT (15 BY 30 MM) WITH CHAFING MARK FOUND AT NOSE SKIN OF INBOARD FLAP VANE RT, BETWEEN RIB 21 AND RIB 22. REPAIR PERF ORMED BY SMOOTH BLEND OUT OF CHAFING AND NDT INSPECTION FOR CRACK FREE IAW EA 6-5752-95917 AND RAS/DABRE/7006243/2006 IS SUE A. 2 L 7 2 4F RT A35EU 2007091200122 20070912 00122 EU 2007 9 12 07FDEA03445 1 20070907 A 5313 A53974203220 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 CORROSION ON STRINGER 52, BETWEEN FRAME 65-66, OUT OF LIMIT AS PER SRM 53-10-00, STRINGER SPLICE REPAIR PERFORMED IAW SR M 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007091200123 20070912 00123 EU 2007 9 12 07FDEA03446 1 20070907 A 5313 A53974203576 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 CORROSION ON STRINGER 53 LT, BETWEEN FRAME 65-66, OUT OF LIMIT AS PER SRM 53-10-00. STRINGER SPLICE REPAIR PERFORMED IA W SRM 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007080800044 20070808 00044 EU 2007 8 8 2007F00039 1 20070724 A 2150 80K197537401 DRAIN PAN PIAGIO P180 P180 6960204 EU WARPED E K NONE O OTHER IN INSP/MAINT 1 SO 14 DUE TO THE HEAT IN THIS AREA, THIS DRAIN PAN IS CRACKING AND WARPING, WHICH IN TURN IS CAUSING THE WATER FROM THE EVAPOR ATOR TO SPILL INTO THE BELLY OF THE AIRCRAFT. THE RESOLUTION HAS BEEN TO REWORK THE PAN, REFORMING THE PAN FROM ALUMINUM STOCK, USING ORIGINAL DRAIN MAST. SEVERAL OF THESE HAVE BEEN FOUND ON OUR FLEET OF 36 AIRCRAFT. 1 H 7 2 3O RT A59EU 2007080800055 20070808 00055 CE 2007 8 8 COEA0702899 1 20070712 A 7330 99103388 INDICATOR CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE FUEL FLOW ERRATIC A COEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 13 899FE 433 208B0235 19163 AIR TURN BACK PDT: FUEL FLOW INDICATING ERRATIC ON CLIMB OUT. TORQUE ITT AND NG DID NOT FOLLOW FUEL FLOW CHANGES. AS A PERCAUTION PILOT ELECTED TO RETURN TO BASE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FUEL FLOW INDICATOR. AIRCRAFT RETURNED TO SERVICE. (K) 1 H 7 1 3T 3 T A37CE E4EA 2007080800060 20070808 00060 SO 2007 8 8 GBB2007F00000 1 20070627 A 5610 45099013 WINDOW PIPER PA31T PA31T 7103124 SO COCKPIT BROKEN E GBBA O OTHER O OTHER NR NOT REPORTED 1 NM 11 22DT 10361 31T8020057 ON JUNE 27, 2007 AT APPROXIMATELY 6:25 PM, WHILE ON A MEDICAL FLIGHT, WAS CLIMBING THRU 20,000 FT FOR 22,000 FT, THE LT NR 2 CABIN SIDE WINDOW SUFFERED AN UNFORESEEN CATASTROPHIC FAILURE. AN EMERGENCY WAS DECLARED TO AIR TRAFFIC CONTROL AN D THE AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENT. THE INCIDENT WAS REPORTED IMMEDIATELY TO THE FAA. THE BROKEN WI NDOW WAS REPLACED WITH APPROVED REPLACEMENT WINDOW. THE AIRCRAFT PASSED ALL SUBSEQUENT POST MAINTENANCE AND FLIGHT TEST S AND WAS RETURNED TO SERVICE. THE BROKEN WINDOW WAS GIVEN TO THE FAA. (K) 1 L 7 2 3T A8EA 2007080800062 20070808 00062 CE 2007 8 8 AJC2007F00000 1 20070703 A 2612 24403915 SENSOR LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE FIRE DETECTION SHORTED E AJCA O OTHER N FALSE WARNING AP APPROACH 1 EA 25 43NR 4526 043 PCE305199 WHILE ON 10 MILE FINAL, THE ENGINE FIRE LIGHT ILLUMINATED FOR APPROXIMATELY 10 SECONDS. AFTER FOLLOWING THE CHECK LIST, THE FIRE LIGHT EXTINGUSHED. WHILE PERFORMING POST FLIGHT, THE FIRE DETECTION SYSTEM DID NOT PASS. NR 1 ENGINE SPECIFIC PART CAUSING PROBLEM. (K) 2 L 7 2 4F 4 F RT A10CE E35NE 2007080800070 20070808 00070 CE 2007 8 8 AMWA06032I 1 20070725 A 5311 12943003717 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 363 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080800074 20070808 00074 CE 2007 8 8 AMWA06032L 1 20070725 A 5311 1294300311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 408 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080800077 20070808 00077 CE 2007 8 8 AMWA06032P 1 20070725 A 5311 12942003625 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 258 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080800080 20070808 00080 CE 2007 8 8 AMWA06032R 1 20070725 A 5311 12943003621 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 303 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080800084 20070808 00084 CE 2007 8 8 AMWA06032V 1 20070725 A 5311 1294400671 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 438 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080800087 20070808 00087 CE 2007 8 8 AMWA06032G 1 20070725 A 5311 12943003719 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 303 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING INC. REPORT 6799-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080800092 20070808 00092 CE 2007 8 8 AMWA06032E 1 20070725 A 5311 1294300311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 243 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080800094 20070808 00094 EA 2007 8 8 S9BA1207 1 20070724 A 5753 C6WFM110934 HINGE FITTING DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA TE FLAP CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 573 RT FWD FLAP IB HINGE ARM HAS CORROSION ON IT. REMOVED AND REPLACED HINGE ARM. 1 H 7 2 3T 4 T RT A9EA E4EA 2007080800095 20070808 00095 EA 2007 8 8 S9BA1307 1 20070724 A 5753 C6WFL20629 HINGE FITTING DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA ZONE 600 CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 573 OB HINGE ARM ON RT FLAP CORRODED, REMOVED AND REPLACED HINGE ARM. 1 H 7 2 3T 4 T RT A9EA E4EA 2007080800097 20070808 00097 EU 2007 8 8 TRBA2007058 1 20070725 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU PWA PW120 PW127 NE EMERGENCY LIGHTS FAILED A TRBA O OTHER L NO TEST NR NOT REPORTED 1 SO 29 545AT 545 EMERGENCY LIGHT AT 10AB INOPERATIVE. RAR BATTERY PACK AT FIN NR 73WL IAW JIC NR 33-51-21. OPT CK IAW JIC NR 33-50-00. 2 H 7 2 4T 4 T RT A53EU E20NE 2007080800098 20070808 00098 EU 2007 8 8 200706092204 1 20070609 A 6420 BEARING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE TAIL ROTOR BINDING E RMXA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 SW 05 112LL 7038 PILOT EXPERIENCED BINDING IN THE T/R CONTROLS. DIRT WAS FOUND IN T/R GRIP BEARINGS CAUSING BINDING IN CONTROL. 1 G 7 2 3U 3 U H13EU E5NE 2007080800099 20070808 00099 NM 2007 8 8 ANCF200700019 1 20070726 A 2611 FIRE LOOP BOEING 757 757236 1384971 NM RROYCE RB211 RB211* 54555 NE NR 1 NACELLE MALFUNCTIONED W ANCF F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 23 522NA 25133 PILOT REPORT: RT ENGINE FIRE AT MDE THE FAULT WAS PRESENTED AFTER 5 MIN OF DEPARTURE. BOTTLE NR 1 WAS DISCHARGED AND RET URNED TO MDE WITH NORMAL LANDING FLIGHT TIME WITH SINGLE ENG +/- 13 MTS. INSPECTED RT ENGINE IAW AMM 71-00-00 PAGE 604. NO FIRE EVIDENCE FOUND. REPLACED FIRE LOOP HARNESS BETWEEN DETECTOR N 3 AND 4. CVR REPLACED IN ACCORDANCE WITH AMM 23- 71-01 INSTALLATION TEST OK FDR REPLACED IAW AMM 31-31-01 INSTALLATION TEST OKREPLACED N.1 ENGINE FIRE EXTINGUISHER BOTTL E IAW AMM 26-21-01 PAGE 401. 2 L 7 2 4F 4 F RT A2NM A12EU 2007080800104 20070808 00104 EU 2007 8 8 UPS07150347 1 20070621 A 5321 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU PWA 4158 PW4158 NE FUSELAGE PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 127UP 0811 INSPECTION TYPE: N/A (2) PUNCTURES IN FLOOR BOARD AS POSITION 1. REPAIRED (2) HOLES IAW SRM 53-10-20. 2 L 7 2 4F 4 F RT A35EU E24NE 2007080800105 20070808 00105 2007 8 8 UPS07650333 4 20070727 A 3421 6227998003 ADI BOEING 767 767300 1385204 NM GE CF6 CF680C2B7 NE COCKPIT FAILED A IPXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 334UP INSPECTION TYPE: ETOP ATB - CAPT EADI FLICKERED; HAD STRANGE DISPLAY THEN WENT OUT. THERE WAS A FISHY/PLASTIC ODOR. NO VISIBLE SMOKE. OXYGEN MASKS DONNED AS A PRECAUTION. VERIFIED EADI FAILURE IAW ADJ AND TEST, REMOVED AND REPLACED CAPTA IN'S EADI IAW MM 34-22-03-4. EADI NOW TESTS NORMAL. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E13NE 2007080800107 20070808 00107 NE 2007 8 8 ASMF200707017 2 20070727 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LEFT VIBRATION W ASMF A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 23 501AM 53371 4655 49188 P709834 CAPTAIN REPORTED THAT DURING TAKE OFF AND INITIAL CLIMB, LT ENGINE WITH STRONG VIBRATION. MAINTENANCE PERFORMED AN ENGI NE RUN CONFIRMING VIBRATION OUT OF LIMITS, THE ENGINE WAS REPLACED IAW MPCM 71-00-02 AND OPERATIONAL TEST WAS PERFORMED IAW MPCM 71-00-01, ALL CORRECT. 2 L 7 2 4F 4 F A6WE E9NE 2007080800112 20070808 00112 CE 2007 8 8 COEA0701897 1 20070723 A 2610 C20050R BUTTON CESSNA 208 208B 2073701 CE PWA PT6 PT6A114 52043 NE COCKPIT LOOSE A COEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 13 897FE 208B0227 JUST AFTER TAKEOFF, ON FLIGHT NR 7797 THE PILOT RECEIVED A FIRE WARNING. HE DECLARED AND EMERGECY AND RETURNED. AIRCRA FT LANDED WITHOUT INCIDENT. MAINTENANCE DISCOVERED THE FIRE WARNING TEST BUTTON HAD FALLEN OFF CAUSING A FALSE WARNING. MAINTENANCE REINSTALLED THE FIRE WARNING TEST BUTTON. FOUND FIRE TEST BUTTON LOOSE. MAINTENANCE THEN REMOVED AND REP LACED THE FIRE TEST BUTTON. AIRCRAFT RETURNED TO SERVICE. (K) 1 H 7 1 3T 3 T A37CE E4EA 2007080200053 20070802 00053 EA 2007 8 2 SWIA200718526 1 20070531 A 5751 BEARING CNDAIR CL600 CL6002B19 1900309 EA PCU LINK CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 973SW 7949 LEFT AILERON PCU LINK BEARINGS AND AFT ATTACH BOLTS ARE CORRODED, DISCOVERED AT C-CHECK. INSTALLED NEW LEFT AILERON PCU OUTPUT LINKS PER CRJ200 AMM 27-14-015-400-801. 2 L 7 2 4F RT A21EA 2007080200056 20070802 00056 EA 2007 8 2 SWIA200718529 1 20070619 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 713SK 10174 FORWARD WEB OF PAX DOOR IS CRACKED BETWEEN 2ND AND 3RD STEPS, DISCOVERED AT C-CHECK. REPAIRED AND ASSEMBLED PARTS FOR P AX DOOR PER REO 670-52-11-104. 2 L 7 2 4F RT A21EA 2007080200064 20070802 00064 NM 2007 8 2 NWAA072636312 1 20070725 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 672US 30267 DURING OVERNIGHT LINE CHECK, CEILING EMERGENCY LIGHT IN AFT CREW BUNK WAS INOP. MAINTENANCE REMOVED AND REPLACCED POWER PACK. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007080200065 20070802 00065 WP 2007 8 2 070140 1 20070723 A 3350 408822101 BATTERY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 875GA 53468 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENC Y EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BA TTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007080200069 20070802 00069 EU 2007 8 2 07FDEA02639 1 20070629 A 5315 A53781842 FLOORBEAM AIRBUS 310 A310222 3930315 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 FWD CARGO COMPARTMENT, CABIN FLOORBEAM CRACKED AT FRAME 36 BETWEEN Y450 AND Y953. IT WAS REPAIRED IAW SRM SUPP 53-10-15 FIG 201 SHEET 2. 2 L 7 2 4F RT A35EU 2007080200085 20070802 00085 NM 2007 8 2 2007UALA02805 1 20070723 A 2800 UNKNOWN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE UNKNOWN A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 787UA 26939 CENTER FUEL QUANTITY INOPERATIVE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007080200094 20070802 00094 NM 2007 8 2 2007UALA02814 1 20070724 A 3350 20121 POWER SUPPLY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 564UA 26666 INTERIOR OVERWING EEL LIGHTS INOPERATIVE, ONE ON EACH SIDE OF A-C. REPLACED EEL PWR SUPPLY. OP CK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080200098 20070802 00098 NM 2007 8 2 2007UALA02818 1 20070724 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SEAT 2E MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 EEL LIGHT MISSING BY SEAT 2E. INSTALLED LIGHT. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080200101 20070802 00101 EA 2007 8 2 VNAA0707012 1 20070719 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE DAMAGED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 250PS 7929 CREW REPORTED A LIGHTNING STRIKE. MAINTENANCE COMPLIED WITH A DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE FOUND BURN MARKS ON BOTH LEFT AND RIGHT WINGLET TIPS AND BURNED RIVETS ON THE BOTTOM SIDE OF THE RADOME. MAINTENANCE REMOVED AND REPLACED THE RADOME ALONG WITH REPAIRING ALL DAMAGE. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007080200115 20070802 00115 NM 2007 8 2 ZZDA2007232 1 20070608 A 5320 INTERCOSTAL BOEING 717 717200 1383700 NM BS 946-954 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 INTERCOSTAL BETWEEN STA 946 AND 954 AND BETWEEN STR 30R - 29R IS CORRODED AND CRACKED. INSTALLED NEW INTERCOSTAL BETWEE N STA 946 TO STA 954 AND STR 30R AND 29R IAW B717 SRM 54-41-02 AND SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007080200119 20070802 00119 NM 2007 8 2 ZZDA2007234 1 20070610 A 5313 STRINGER SPLICE BOEING 717 717200 1383700 NM BS 898.5 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 BS 898.5 LONGERON 29L STRINGER SPLICE IS CORRODED. INSTALLED SPLICE ON LONGERON 29L ON BS 898.5 PER B717 SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007080200122 20070802 00122 NM 2007 8 2 ZZDA2007236 1 20070610 A 5313 STRINGER SPLICE BOEING 717 717200 1383700 NM BS 898.5 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 BS 898.5 LONGERON 27L STRINGER SPLICE IS CORRODED. INSTALLED SPLICE ON LONGERON 27L ON BS 898.5 PER B717 SRM 53-00-05. 2 L 7 2 4F TR A6WE 2007080200126 20070802 00126 NM 2007 8 2 ZZDA2007240 1 20070610 A 5313 LONGERON SPLICE BOEING 717 717200 1383700 NM BS 1002-1022 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 SPLICE ON L-22L BETWEEN STA 1002 AND 1022 IS CORRODED OUT OF LIMITS. INSTALLED SPLICE ON L-22L BETWEEN STA 1002 AND STA 1022 IAW B717 SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007080200130 20070802 00130 NM 2007 8 2 ZZDA2007248 1 20070605 A 5322 SHEAR TIE BOEING 717 717200 1383700 NM BS 1002 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT BS 1002 SHEAR TIE BETWEEN LONGERON 30 AND LONGERON 22L. INSTALLED NEW SHEAR TIE AT S TA 1002 BETWEEN LONGERON 30L AND 22L PER B717 SRM 51-41-02 AND SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007080200135 20070802 00135 WP 2007 8 2 ABXA070249 1 20070716 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP MAIN CABIN DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-02-4-0001. 2 L 7 2 4F A6WE 2007080200136 20070802 00136 WP 2007 8 2 ABXA070250 1 20070724 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP EMERGENCY LIGHT DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 ON PRE-FLIGHT, EMERGENCY LIGHTS WOULD NOT COME ON IN THE -ON- POSITION. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-02-4-0001. 2 L 7 2 4F A6WE 2007080200139 20070802 00139 NM 2007 8 2 USAA070581 1 20070727 A 5310 DOOR FRAME BOEING 737 7374B7 1384702 NM BS 440 S24R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 BS 440 & S-24R HAS CRACK. INSTALLED DOUBLER PER EA 98810, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007080200140 20070802 00140 NM 2007 8 2 SWAA073707 1 20070726 A 5322 6546546 SHEAR TIE BOEING 737 7373Y0 1384671 NM BS 847 S27R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 847, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007080200178 20070802 00178 NM 2007 8 2 SWAA073654 1 20070725 A 5322 6546546 SHEAR TIE BOEING 737 7373Y0 1384671 NM BS 787 S27R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007080200179 20070802 00179 NM 2007 8 2 SWAA073658 1 20070725 A 5311 6546550 FRAME BOEING 737 7373K2 13844BA NM BS 787 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200180 20070802 00180 NM 2007 8 2 SWAA073651 1 20070725 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200187 20070802 00187 NM 2007 8 2 SWAA073664 1 20070725 A 5314 6562125 KEELBEAM BOEING 737 7375H4 138449D NM BS 487B S28R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, FOUND KEEL BEAM CORRODED AT BS 487B, STR 28R. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2007080200194 20070802 00194 WP 2007 8 2 ASAA0781902 1 20070726 A 5321 993654759 FLOOR PANEL DOUG DC9 DC983 3022083 WP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-24-0 AND 53-05. 2 L 7 2 4F RT A6WE 2007080200199 20070802 00199 WP 2007 8 2 UPS07850212 1 20070626 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FS 340 RBL 60 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 CRACKED FLOORBEAM SUPPORT FITTING FS 340 RBL 60 A-PIT DOOR UPPER CUTOUT L21 CUSP AREA. REMOVED AND R EPLACED FLOORBEAM SUPPORT FITTING AT STA 340 RBL 60 IAW SRM 51-01-20D, DWG 9754022, AND SRM 51-3-2. 2 L 7 4 4F RT 4A25 2007080300001 20070803 00001 EA 2007 8 3 COMA0760493 1 20070721 A 2910 AE7120312 LINE CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYS FAILED A COMA L ABORTED APPROACH K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 01 988CA 7204 FLIGHT 5228 - HYDRAULIC LOW PRESS CAUTION MESSAGE WITH 0 PRESS AND 0 QTY. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED NR 2 HYD SYS LINE. 2 L 7 2 4F RT A21EA 2007080300006 20070803 00006 NM 2007 8 3 UPS07450293 1 20070705 A 5710 SUPPORT BOEING 747 747212B 1384886 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C RT WING WS500 L/E MOST FWD INTERIOR LOWER SUPPORT CHORD BULGED AS MARK. CORROSION BLEND OUT EXFOLIATI ON THROUGH WHOLE THICKNESS EXCEED SRM LIMIT. RHW WS 492 TO WS 508 L/E MOST FWD INTERIOR LOWER SUPPORT REPAIRED AS PER S RM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 2007080300011 20070803 00011 NM 2007 8 3 UPS07450298 1 20070702 A 5320 PLATE BOEING 747 747212B 1384886 NM BS 920 MISINSTALLED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D BS 920 RT TENSION TIE FWD ATT STEEL PLATE TOP ROW NR 5 FASTENER HOLE (COUNT FROM I/B) FOUND SHORT EDGE MARGIN. M/D BS 920 RT TENSION TIE FWD ATTACH STEEL PLATE REPAIRED AS PER RS R53-25-35821 AND UPS EO B747-5310-2726 8. CONTINUED INSPECTION IS REQUIRED AS PER RS R53-25-35821 AND UPS EO B747-5310-27268. 2 L 7 4 4F A20WE 2007080300017 20070803 00017 EA 2007 8 3 SWIA200718547 1 20070726 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 432SW 7548 THIRD AFT CEILING LEVEL EMERGENCY FLOODLIGHT IS NOT WORKING. REPLACED LAMP. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007080300027 20070803 00027 NM 2007 8 3 UPS07450312 1 20070702 A 5320 CHANNEL BOEING 747 747212B 1384886 NM BS 880 S9R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C CRACK FOUND AT BS 880 RT SIDE S9R TENSION TIE ATTACHED FWD CHANNEL CRACK LOCATED AT NR 14 FASTENER HOL E 0.030" APPROX RUNNING DOWNWARD DIRECTION. M/D BS 880 TENSION TIE FWD CHANNEL REPLACED AS PER SRM 51-10-01 PG 9 AND IN STALLED AS PER UPS EO B747-5310-23715-C AND SRM 51-30-02. 2 L 7 4 4F A20WE 2007080300029 20070803 00029 NM 2007 8 3 UPS07450314 1 20070702 A 5320 CHANNEL BOEING 747 747212B 1384886 NM BS 880 S9R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C CRACK FOUND AT BS 880 RT SIDE S9R TENSION TIE ATTACHED AFT CHANNEL CRACK LOCATED AT NR 6 FASTENER HOLE 0.040" APPROX RUNNING UPWARD DIRECTION. M/D BS 880 TENSION TIE AFT CHANNEL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTA LLED AS PER UPS EO B747-5310-2371-C AND SRM 51-30-02. 2 L 7 4 4F A20WE 2007080300032 20070803 00032 NM 2007 8 3 UPS07450317 1 20070705 A 5720 65B108911 STIFFENER BOEING 747 747212B 1384886 NM RT MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C RT W/G W/W STIFFENER APPEAR CORRODED AT STA1241 RBL 63. RT W/G W/W AT BS 1241 RBL63 VERTICAL STIFFENE R REPLACED AND INSTALLED AS PER SRM 51-10-10 PG 9 AN 51-30-02. 2 L 7 4 4F A20WE 2007080300044 20070803 00044 NM 2007 8 3 UPS07550243 1 20070627 A 5311 146N103038 FRAME BOEING 757 75724APF 1384969 NM BS 1540 S25-26L DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 402UP 23724 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1540, BET S25L AND S26L. DENT REPAIR AT STA 1540, S25L TO S26L W AS ACCOMPLISHED PER FINAL EA NR 757-5362-27-A1702. 2 L 7 2 4F RT A2NM 2007080300052 20070803 00052 NM 2007 8 3 CALA0700378 1 20070727 A 5320 141A54103 INTERCOSTAL BOEING 737 737824 13844BZ NM BS 277-294.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 36207 30579 INSPECTION FOUND A 1.5" CRACK IN INTERCOSTAL AT STA 277-294.5, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 5 1-40-02. 2 L 7 2 4F RT A16WE 2007080300063 20070803 00063 NM 2007 8 3 UPS07M50284 1 20070525 A 5730 SKIN DOUG MD11 MD11 3023602 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C LT FIXED LE LWR COMPT UPPER SKIN DOUBLER SUSPECTED CRACK AT STA XORS 535. HFEC INSP CARRIED OUT PER D AC NDTSPM R.13 PART 06-10-01-001 FOUND CRACK AS MARKED. REPAIR ANGLES FAB AND CRACK AREA TRIM OFF PER EN1375-07. REPAI R ANGLES HEAT TREATED PER DPS7.00-1 AND HARDNESS VALUES 86.1 PER DPS1.05-3 REP PARTS HOLE PICK UP PER EN1375-07 AND PROT ECTED PER SRM 51-21-01V.2R.38. REPAIR PARTS INSTALLED PER EN1375-07. 2 L 7 3 4F RT A22WE 2007080300067 20070803 00067 NM 2007 8 3 UPS07M50324 1 20070725 A 5610 WINDOW DOUG MD11 MD11F 3023600 NM COCKPIT STUCK A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 CAPTAIN'S WINDOW WILL NOT OPEN ALL THE WAY. SUNSHADE INTERFERES. RESECURED VISOR. WINDOW OPS CK OK. 2 L 7 3 4F RT A22WE 2007080300071 20070803 00071 2007 8 3 HNAA0700157 4 20070727 A 3442 82200015003 RADAR DHAV DHC8 DHC8102 2809003 NM WX SYSTEM FAILED A HNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 07 980HA 376 JUST AFTER TAKEOFF CREW NOTICED WX RADAR WAS NOT PAINTING ANY STORMS THEN RED DOTS BEGAN TO DISPLAY ON THE RADAR. AFTER TALKING WITH DISPATCH WITH DISPATCH AND WITH THUNDERSTORMS ON THEIR ROUTE OF FLIGHT, RETURNED TO LGA. 2 H 7 2 4T RT A13NM 2007080300087 20070803 00087 NM 2007 8 3 AWXA200700936 1 20070706 A 5510 183N13261 BEAM BOEING 757 757225 1384959 NM ZONE 300 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - NR 5956472, CORROSION ON THE LEFT HORIZONTAL REAR AFT BEAM, STABILIZER STATION 224 - 3 66. REPAIRED THE LEFT HORIZONTAL REAR AFT BEAM, STABILIZER STATION 224 - 366 IAW USAIRWAYS EA 120102 . 2 L 7 2 4F RT A2NM 2007080300092 20070803 00092 EA 2007 8 3 QXEA200701199 1 20070724 A 2840 73811813 COMPUTER CNDAIR CL600 CL6002C10 1390015 EA FUEL QTY CONTAMINATED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 611QX 10326 10041 ABQ - FLIGHT 4334- RECEIVED A FUEL CHANNEL 1/2 FAIL MESSAGE. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDIN G. MAINTENANCE REPLACED THE FUEL QUANTITY GAUGING COMPUTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007080300094 20070803 00094 EA 2007 8 3 QXEA200701189 1 20070723 A 2612 47388904 CONTROL PANEL CNDAIR CL600 CL6002C10 1390015 EA FIRE DETECTION MALFUNCTIONED A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 618QX 10647 10205 ONT - FLIGHT 2561- RECEIVED A FIRE SYSTEM FAULT MESSAGE EN ROUTE. MAINTENANCE PLACED THE SYSTEM ON MEL 26-00-1. MEL CL EARED BY REPLACING THE FIDEX CONTROL PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007080300095 20070803 00095 NM 2007 8 3 DHL2007784529 1 20070710 A 5322 SHEAR TIE BOEING 727 727227 1384078 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 AFT CARGO COMPARTMENT BS 1166, STR 29L TO 27L, FRAME SHEAR TIE HAS CORROSION ON BOTH SIDES OF FRAME. REMOVED DAMAGED SH EAR TIE DIM 13.5 BY 2.75 IAW B727 SRM 53-10-4, FIG 13. FABRICATED SHEAR TIE REPAIR, FROM 7075T0 .071, 13.25 BY 7.5 AND ONE EACH FILLER ANGLE FROM 7075T0 .071, 13.50 BY 2.75 IAW B727 SRM 53-10-4, FIG 13 AND HEAT TREATED PARTS TO T6 IAW FLIG HTSTAR AIRCRAFT SERVICES ENGINEERING REPORT 2-37153-801 REV.A. TREATED, PRIMED AND INSTALLED PARTS IAW B727 SRM 51-10-2 , 51-30-2 AND 53-10-4, FIG 13. 2 L 7 3 4F A3WE 2007080300099 20070803 00099 NM 2007 8 3 DHL2007784531 1 20070710 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 MAIN CARGO GOUGES AND CORROSION ON SEAT TRACK LBL 45, BS 480 TO BS 690, WL 208.5 ON ENTIRE TRACK. REMOVED FLOOR BOARDS AT MAIN CABIN ROW A, STA 480 TO 720C AND SEAT TRACK STA 480 TO BS 690 IAW B727 SRM 51-30-2. FABRICATED TWO EACH SEAT TR ACKS FROM P/N BAC1520-792-7178T6511, DIM. 100 AND 109.5 LONG, TWO EACH ANGLES FROM BAC 1503-100122-7178T6, DIM. 14 BY 2. 50 AND ONE STRAP FROM 7075T6, .250, DIM. 7.50 BY 2.5 IAW B727 SRM 53-10-5, FIG 1. TREATED, PRIMED AND INSTALLED SEAT TR ACK IAW B727 SRM 51-10-2 AND 51-30-2. INSTALLED FLOOR BOARDS IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007080300101 20070803 00101 NM 2007 8 3 DHL2007784523 1 20070708 A 5330 SKIN BOEING 727 727227 1384078 NM ZONE 100 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 EXTERNAL FUSELAGE BS 680 AT STR 7R HAS SKIN BUTT JOINT WITH A LIGHTING STRIKE BURN. BLENDED OUT AREA OF LIGHTNING STRIK E IAW B727 SRM 53-30-3, FIG 20. MATERIAL LOSS OVER 30 PERCENT AND LIGHTNING STRIKE STILL PRESENT AND OUT OF LIMITS IAW B727 SRM 53-30-1. CUT OUT DAMAGED SKIN AREA DIM 5.75 BY 5.75 IAW B727 SRM 53-30-3, FIG 3A. HFEC COMPLIED WITH IN CUT O UT AREA, NO CRACKS NOTED IAW B727 NDTM PT.6 51-00-00, FIG 23. FABRICATED DOUBLER REPAIR FROM 2024T3, .080, DIM 8.75 BY 11 AND FILLER FROM 2024T3, .040, DIM 4 BY 5.75 IAW B727 SRM 53-30-3, FIG 3A. TREATED, PRIMED AND INSTALLED REPAIR IAW B 727 SRM 51-10-2, 51-30-2 AND 53-30-3, FIG 3. 2 L 7 3 4F A3WE 2007080300107 20070803 00107 NM 2007 8 3 UPS07450248 1 20070706 A 5320 65B079413 INTERCOSTAL BOEING 747 747212B 1384886 NM BS 290 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C NWW TOP PANEL LBL20 INTERCOSTAL FOUND CRACK AT 1 FASTENER LOCATION AT BS290 AS MARKED, CRACK LENGTH 1/ 2". NWW TOP PANEL AT BS 290 LBL20 INTERCOSTAL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007080300111 20070803 00111 EU 2007 8 3 NWAA072653228 1 20070729 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320211 3930320 EU EMERGENCY LIGHTS FAILED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 328NW 2605 1061 298 DURING EMERGENCY ESCAPE LIGHTING CHECK, FORWARD POWER SUPPLY UNIT FAILED. REPLACED FORWARD EPSU 10WL, CHECKS OK. 2 L 7 2 4F RT A28NM 2007080300114 20070803 00114 EU 2007 8 3 07FDEA02646 1 20070728 A 5311 A53773644201 FRAME AIRBUS 310 A310203 3930313 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 FRAME FITTING C38 (STA 2082) IS CRACKED AT RBL 69 (-Y1520) FWD PIT, FLOOR LEVEL. [08-06-07] REMOVED AND REPLACED FRAM E FITTING AT C38 IAW A310-200 SRM 51-40-20. 2 L 7 2 4F RT A35EU 2007080300118 20070803 00118 EA 2007 8 3 QXEA200701223 1 20070717 A 3213 AXLE CNDAIR CL600 CL6002C10 1390015 EA LT MLG CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - LEFT MAIN LANDING GEAR AXLE HAS LIGHT CORROSION. REMOVED CORROSION IAW SCR 046-07. 2 L 7 2 4F RT A21EA 2007080600023 20070806 00023 NM 2007 8 6 2007UALA02772 1 20070722 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE AFT GALLEY LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 TRIM LOOSE AFT GALLEY EMERGENCY EXIT LIGHT. REPLACED MISSING END CAP AND BROKEN LENS COVER ON EEL STRIP AT LAST SECTION NEAR AFT LAVATORY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080600032 20070806 00032 NM 2007 8 6 2007UALA02782 1 20070722 A 3350 LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 775UA 26947 THE 9F FWD, 24C & 39G EEL LIGHTS ARE INOPERATIVE. [08-14-07] RELAMPED, AS PER MM33-51- 05, OPS CHECKED. SYS OPS NORMA L, RETURNED AIRCRAFT FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007080600050 20070806 00050 NM 2007 8 6 CALA0700371 1 20070721 A 5347 BAC15207927178T6 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 328-360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND THE FORWARD ENTRY RIGHT O/B SEAT TRACK CORRODED BETWEEN STA 328 AND 360, RBL 36. THE SEAT TRACK WAS RE MOVED AND REPLACED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 2007080600051 20070806 00051 NM 2007 8 6 CALA0700372 1 20070723 A 5320 6517685 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 357 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A .75 INCH CRACK IN INTERCOSTAL WEB AT STA 357, S16L. REPAIR PARTS WERE INSTALLED IAW SRM 53-10-04. 2 L 7 2 4F RT A16WE 2007080600055 20070806 00055 EU 2007 8 6 USAA070577 1 20070724 A 5320 D5311281820401 FLOOR SUPPORT AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 183UW 1539 FLOOR SUPPORT Y254 AT CROSSBEAM C23 HAS CORROSION. INSTALLED DOUBLER IAW SRM 53-00-14; CORR TASK JA-220-53500, DEFECT S IZE: .5 INCH DIA. 2 L 7 2 4F RT A28NM 2007080600060 20070806 00060 NM 2007 8 6 ASAA0741875 1 20070719 A 5754 65C26606302 SKIN BOEING 737 7374Q8 138447Q NM NR 5 SLAT DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 NR 5 SLAT TRAILING EDGE DELAMINATED ON O/B END. NR 5 SLAT TRAILING EDGE DELAMINATION AT O/B END REPAIRED IAW SRM 51-70- 10. 2 L 7 2 4F RT A16WE 2007080600068 20070806 00068 NM 2007 8 6 SWAA073624 1 20070724 A 5210 6545871 BEAM BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR CRACKED AT LOWER BEAM WEB. REMOVED AND REPLACED R1 DOOR ASSY PER MM. 2 L 7 2 4F RT A16WE 2007080600071 20070806 00071 NM 2007 8 6 SWAA073626 1 20070724 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080600072 20070806 00072 NM 2007 8 6 SWAA073642 1 20070724 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080600077 20070806 00077 NM 2007 8 6 SWAA073641 1 20070724 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM BS 747 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080600078 20070806 00078 NM 2007 8 6 SWAA073638 1 20070724 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080600080 20070806 00080 NM 2007 8 6 SWAA073639 1 20070724 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM BS 360 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080600094 20070806 00094 2007 8 6 SWAA073613 4 20070722 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007080600104 20070806 00104 WP 2007 8 6 ASAA0781880 1 20070724 A 5330 5920323249 SKIN DOUG DC9 DC983 3022083 WP BS 460-470 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 FUSELAGE SKIN CREASED OVER SHEAR TIE. REMOVED DAMAGED AREA. INSTALLED FILLER AND DOUBLER PER SRM 53-04. 2 L 7 2 4F RT A6WE 2007080600111 20070806 00111 WP 2007 8 6 ASAA0781897 1 20070725 A 5330 5920323249 SKIN DOUG DC9 DC983 3022083 WP BS 579-599 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 FUSELAGE SKIN DENTED. REPAIR PER SRM 53-04. 2 L 7 2 4F RT A6WE 2007091200075 20070912 00075 EU 2007 9 12 07FDEA03406 1 20070906 A 5330 A53918255 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 808FD 439 OLD EXTERNAL DOUBLER REPAIR FOUND BETWEEN FRAME 72-73, STRG 26-27 LHS. DOUBLER THICKNESS NOT CONFORM TO SRM. DOUBLER R EPAIR RENEWED IAW SRM 53-10-12/FIG 225, APPROVED BY EA 6-5318-99164. 2 L 7 2 4F RT A35EU 2007091200080 20070912 00080 EU 2007 9 12 07FDEA03412 1 20070906 A 5753 SKIN AIRBUS 310 A310324 3930206 EU ZONE 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 FOUND OLD REPAIR WITH NEW DAMAGED CORE AND DENTS ON LT INBOARD FLAP LOWER SURFACE AT T/E BETWEEN RIB 13-14. REPAIR RENE WED IAW SRM 57-53-12/FIG 208, APPROVED BY EA 6-5752-95904 AND RAS/DABRE/7006107/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091200103 20070912 00103 EU 2007 9 12 07FDEA03397 1 20070906 A 5320 A53612213203 FLOOR SUPPORT AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 HEAVY CORRODED LONGERON BETWEEN FRAME 12A-14, Y-450, CABIN FLOOR STRUCTURE RT, OUT OF LIMIT AS PER SRM 53-10-00. REPAIR PERFORMED IAW SRM 53-12-15/FIG 207. 2 L 7 2 4F RT A35EU 2007091200108 20070912 00108 EU 2007 9 12 07FDEA03431 1 20070907 A 5521 RIB AIRBUS 310 A310324 3930206 EU ZONE 300 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 RT ELEVATOR TIP SKIN PLATE AND RIBS DEFORMED. FOUND CRACKS (20 AND 30 MM) IN LOWER SKIN AT T/E PROFILE. REAR UPPER ANC HOR NUT OF ELEVATOR RIB ER41 CRACKED. REPAIR PERFORMED BY TRIM OUT TO REMOVE THE CRACKED AND DENTED AREA. INSTALLATION OF REPAIR ANGLE AND FILLER, REINSTALLATION OF ANCHOR NUT AND REPLACEMENT OF TIP IAW EA 6-5524-95911 AND RAS/CASA/4555/2 006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091200109 20070912 00109 EU 2007 9 12 07FDEA03432 1 20070907 A 5730 A57247239004 PANEL AIRBUS 310 A310324 3930206 EU ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 DELAMINATION FOUND ON OUTER SHROUD BOX ON RT WING, LOWER SKIN NEAR RIB 31 AND CORROSION OF ALUMINIUM EXTRUSION ON RT WIN G OUTER TRAILING EDGE PANEL. REPAIR PERFORMED BY REMOVING AND REPLACING ALL DAMAGED LAYERS WITH WET LAY UP. REPLACING T HE ALUMINUM T/E SECTION AND AFFECTED RIVETS IAW EA 6-5751-95922 AND RAS/BAE/1002265/2006. 2 L 7 2 4F RT A35EU 2007091200125 20070912 00125 EU 2007 9 12 07FDEA03448 1 20070907 A 5313 A53974267202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 CORROSION ON STRINGER 56 LT, BETWEEN FRAME 65-66, OUT OF LIMIT AS PER SRM 53-10-00. STRINGER SPLICE REPAIR PERFORMED IA W SRM 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007080600121 20070806 00121 NM 2007 8 6 ZZDA2007216 1 20070605 A 5311 FRAME BOEING 717 717200 1383700 NM BS 1002 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT BS 1002 FRAME BETWEEN LONGERON 30 AND LONGERON 22L. INSTALLED NEW FRAME AT STA 1002 BETWEEN LONGERON 30L AND 22L PER B717 SRM 51-41-02 AND SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007080600123 20070806 00123 NM 2007 8 6 ZZDA2007218 1 20070612 A 5310 STRUCTURE BOEING 717 717200 1383700 NM BS 1053 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 JACKPAD FITTING BARREL NUT HOLE IS CORRODED. INSTALLED NEW END TIE FITTING LONGERON 30 AT AFT CARGO COMPARTMENT STA 105 3 IAW B717 SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007080600125 20070806 00125 NM 2007 8 6 ZZDA2007220 1 20070605 A 5313 LONGERON BOEING 717 717200 1383700 NM BS 1053 L28L CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT (WASTE TANK AREA) AT LONGERON 28L END TIE FITTING. INSTALLED NEW END TIE FITTING LON GERON 28L AT AFT CARGO COMPARTMENT STA 1053 IAW B717 SRM 51-41-02 AND SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007080600146 20070806 00146 NM 2007 8 6 SWAA073655 1 20070725 A 5313 BAC1498 STRINGER BOEING 737 7373Y0 1384671 NM BS 867 S26R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 26R CORRODED AT BS 867. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007080600147 20070806 00147 2007 8 6 SWAA073645 4 20070725 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007080600155 20070806 00155 NM 2007 8 6 CALA0700375 1 20070726 A 5330 6552988 SKIN BOEING 737 7373T0 1384582 NM BS 947 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN ABOVE L-2 DOOR UPPER HINGE, STA 947.5, S11L T0 14L. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-60-01. 2 L 7 2 4F RT A16WE 2007080600166 20070806 00166 NM 2007 8 6 2007UALA02794 1 20070723 A 3397 7945243 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 193UA 26890 SEAT EEL INOP: 47 HJK & 48 HJK. *S/D* REPAIRED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080600167 20070806 00167 EU 2007 8 6 YENA2007066 1 20070726 A 2910 HYDRAULIC SYSTEM AIRBUS 320 A320232 3930326 EU YELLOW SYSTEM OVERSERVICED A YENA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 EA 15 517JB 1327 FLT 24, TPA TO JFK, AIR RETURN TO TPA. HYD YELLOW RESERVOIR OVERHEAT ECAM ON CLIMBOUT. PERFORMED TSM TASK 29-13-00-810 -802. FOUND YELLOW RESERVOIR OVERSERVICED AT 17L. DRAINED AND SERVICED YELLOW RESERVOIR. SYSTEM NOW CHECKS GOOD DURIN G ENG RUN, TAXI AND FLIGHT CONTROL CK. 2 L 7 2 4F RT A28NM 2007080600173 20070806 00173 EA 2007 8 6 TRAX200701047 1 20070724 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 903EV 7621 CREW REPORTS CAPTAIN`S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007080600175 20070806 00175 EA 2007 8 6 TRAX200701050 1 20070725 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA BS 559 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 873AS 7549 CORROSION ON SEAT RAILS AT VARIOUS ATTACH SCREWS AT FS 559 RBL 9.00. 2 L 7 2 4F RT A21EA 2007080600176 20070806 00176 NM 2007 8 6 HNAA0700154 1 20070718 A 7500 310848501 VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE AIR SWITCH MALFUNCTIONED A HNAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 07 980HA 376 120911 UPON DESCENT INTO TYS POWER LEVERS AT FLT IDLE FLT DECK/CABIN STARTED TO FILL WITH SMOKE WITH BOTH BLEEDS ON. TURNED OF F ENGINE BLEEDS AND SMOKE STARTED TO DISSIPATE. F/A REPORTED THAT THE CABIN GOT VERY WARM AT THIS TIME. INSPECTED NR 1 ENGINE FOR OIL OTY AND FOR LEAKS, OIL QTY BETWEEN 1 QT AND FULL, FOUND OIL LEAK TO BE LEAKING IN DEFUSER TUBE AREA. GR OUND RAN A/C WITH CREW, SEE FERRY PERMIT FOR LIMITS (MECHANIC SHOT SINGED). REMOVED AND REPLACED O-RINGS TO BEARING CAV ITY AND REMOVED AND REPLACED AIR SWITCHING VALVE NR 1 OPS AND LEAK CHECK GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2007080600178 20070806 00178 EA 2007 8 6 TRAX200701054 1 20070725 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 833AS 7246 THE 280 AFT ANGLE COMMON TO THE EMERGENCY RELEASE CABLE O/B OF LBL 9 IS CRACKED. 2 L 7 2 4F RT A21EA 2007080600181 20070806 00181 EA 2007 8 6 TRAX200701059 1 20070725 A 5270 LIGHT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR HANDLE NO TEST A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 854AS 7382 PAX DOOR HANDLE -EXIT PULL- BETA LIGHT FAILED TEST. 2 L 7 2 4F RT A21EA 2007080600182 20070806 00182 EA 2007 8 6 TRAX200701060 1 20070725 A 2560 MEGAPHONE CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 730EV 10141 MEGAPHONE INOP. 2 L 7 2 4F RT A21EA 2007080600186 20070806 00186 EU 2007 8 6 WRNA200700046 1 20070727 A 2780 CHA1061005A JACKSCREW AIRBUS 300 A300B4203 3930306 EU SLATS LOCKED A WRNA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 505TA 271 SLATS FAILED TO RETRACT AFTER TAKEOFF. DUMPED FUEL AND RETURNED TO FIELD FOR A SAFE LANDING. FOUND NR 4 AND 5 SLAT JAC K SCREWS LOCKED OUT AND RT FRICTION BRAKE FAILED TORQUE CHECK. REPLACED NR 4 JACK SCREW IAW 27-81-27 PG 401, NR 5 SLAT JACK SCREW IAW 27-81-28 PG 401 AND RT FRICTION BRAKE IAW 27-81-47 PG 401. A/C RETURNED TO SERVICE. 2 L 7 2 4F RT A35EU 2007080600189 20070806 00189 SO 2007 8 6 RAIA00707040 1 20070723 A 3350 RPSB1 POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DISCHARGED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 844HK 14500838 PRE FLT 7947 - STL - VARIOUS EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER S UPPLY. 2 L 7 2 4T RT T00011AT 2007080600191 20070806 00191 NM 2007 8 6 SWAA073708 1 20070726 A 3350 101331 LENS BOEING 737 7375H4 138449D NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007080600192 20070806 00192 NM 2007 8 6 SWAA073679 1 20070726 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007080600193 20070806 00193 NM 2007 8 6 SWAA073673 1 20070726 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 402WN 29814 EEPLS COVER MISSING AT ROW 11 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007080600194 20070806 00194 NM 2007 8 6 SWAA073690 1 20070726 A 2730 6545166 PUSHROD BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL PUSHROD AND BEARING PER MM . 2 L 7 2 4F RT A16WE 2007080600195 20070806 00195 NM 2007 8 6 SWAA073689 1 20070726 A 2730 6545166 PUSHROD BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL PUSHROD AND BEARING PER MM . 2 L 7 2 4F RT A16WE 2007080600196 20070806 00196 NM 2007 8 6 SWAA073687 1 20070726 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM BS 380 S28L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 618WN 28034 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380 BETWEEN BL 0 AND STR 28L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007080600197 20070806 00197 NM 2007 8 6 SWAA073699 1 20070726 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080600199 20070806 00199 NM 2007 8 6 SWAA073694 1 20070726 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080600200 20070806 00200 NM 2007 8 6 SWAA073680 1 20070726 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080600203 20070806 00203 WP 2007 8 6 ASAA0781905 1 20070726 A 5321 993655211 FLOOR PANEL DOUG DC9 DC983 3022083 WP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007080600205 20070806 00205 WP 2007 8 6 ASAA0781907 1 20070726 A 5320 99366405 FLOOR PANEL DOUG DC9 DC983 3022083 WP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND DAC DWG 9936640. 2 L 7 2 4F RT A6WE 2007080600206 20070806 00206 WP 2007 8 6 ASAA0781908 1 20070726 A 5330 593666751 SKIN DOUG DC9 DC983 3022083 WP BS 1253-1263 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 FUSELAGE SKIN CREASED AT PRIOR REPAIR. REMOVED EXISTING REPAIR DOUBLER RECONTOURED SKIN AND INSTALLED REPLACEMENT DOUBL ER PER SRM 53-04. 2 L 7 2 4F RT A6WE 2007080600207 20070806 00207 WP 2007 8 6 ASAA0781909 1 20070726 A 5330 593666751 SKIN DOUG DC9 DC983 3022083 WP BS 1266-1278 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 FUSELAGE SKIN DENTED AT PREVIOUS REPAIR. REPLACED DAMAGED SECTION AND PREVIOUS REPAIR DOUBLER PER SRM 53-04. 2 L 7 2 4F RT A6WE 2007080600209 20070806 00209 WP 2007 8 6 ASAA0781913 1 20070726 A 5754 5930496507 VANE DOUG DC9 DC983 3022083 WP TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 LEFTHAND WING OUTBOARD FLAP INBOARD VANE TRAILING EDGE IS CHAFED. REPAIRED DAMAGED AREA WITH BONDED FILLER AND DOUBLER PER SRM 51-70-2. 2 L 7 2 4F RT A6WE 2007080600211 20070806 00211 NM 2007 8 6 KCSA071261 1 20070727 A 5311 FRAME BOEING 747 7472B4B 138481B NM BS 460 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 FUSELAGE FRAME FLANGE IS CRACKED AT STA 460, BETWEEN STR 26R AND 30R. 2 L 7 4 4F RT A20WE 2007080600213 20070806 00213 EA 2007 8 6 COMA0760492 1 20070721 A 2910 AE7137631 HOSE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM FAILED A COMA L ABORTED APPROACH K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 01 988CA 7204 FLIGHT 5228 - HYDRAULIC 2 LOW PRESS CAUTION MESSAGE WITH 0 PRESS AND 0 QTY. AIRCRAFT LANDED SAFELY. REMOVED AND REPLAC ED NR 2 HYD SYS HOSE. 2 L 7 2 4F RT A21EA 2007080600214 20070806 00214 EA 2007 8 6 COMA0760495 1 20070721 A 3230 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA MLG FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 708CA 20990 7235 FLIGHT 6433 - GEAR DISAGREE MESSAGE AFTER TAKEOFF QRH FOLLOWED GEAR EXTENDED, AIRCRAFT RETURNED TO CVG AND LANDED SAFELY . REMOVED AND REPLACED PSEU. 2 L 7 2 4F RT A21EA 2007080600215 20070806 00215 EA 2007 8 6 COMA0760496 1 20070723 A 7830 THRUST REVERSER CNDAIR CL600 CL6002B19 1900309 EA LEFT UNKNOWN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 926CA 7027 FLIGHT 5541 - AFTER TAKEOFF RECEIVED LEFT REV UNLOCK CAUTION MESSAGE. AIRCRAFT RETURNED BACK TO CMH AND LANDED SAFELY. TRANSFERRED TO DMI LIST PER 78-30-01. 2 L 7 2 4F RT A21EA 2007080700001 20070807 00001 NM 2007 8 7 2007UALA02821 1 20070724 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 EEL LEAD WIRE BROKEN. REMOVED AND REPLACED EEL LIGHT BARS PER MM 33-51-10 AND OPS CHECK GOOD PER MM 33-51-00 ON N-R 256 92. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080700002 20070807 00002 NE 2007 8 7 2007UALA02822 2 20070724 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 2 STALLED A UALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 WP 29 676UA 30028 729015 NR 2 ENG APPEARED TO SUSTAIN A STALL DURING WAKE TURB ENCOUNTER. ALL ENG PARAMETERS REMAINED NORMAL AND ENG CONTINUED T O OPERATE NORMALLY. [08-14-07] BORESCOPE OF HPC PER AMM 72-00-00 SHOWED NO DAMAGE. BLEED SYSTEM CHECKED NORMAL. ALL OTHER CHECKS WERE WITHIN LIMITS. AS THE SURGE OCCURRED BELOW 15,000 FT, AND EPR WAS ABOVE 1.25 FOR MORE THAN 30 SECOND S, BUT BELOW 1.45, ACCOMPLISHMENT OF TEST-21 PER AD 2003-19-15 IS NOT REQUIRED PER INDUSTRY AMOC DATED 04/17/07 FROM FAA ECO. ENGINE OK TO CONTINUE IN SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080700003 20070807 00003 2007 8 7 2007UALA02823 4 20070721 A 2565 ARMING LEVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR SLIDE OBSTRUCTED A UALA K NONE C F.O.D. IN INSP/MAINT 1 WP 29 551UA 25399 UNABLE TO ARM 1R SLIDE. FOUND AN OVEN TIMER KNOB LODGED IN AND OBSTRUCTING ARMING OF SLIDE. REMOVED OBJECT AND DOOR 1 R SLIDE ARMS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080700007 20070807 00007 NM 2007 8 7 2007UALA02828 1 20070725 A 5210 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE PAX DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 FWD ENTRY DOOR SN 229 INNER SKIN AND AFT FRAME CRACKED AT AFT SIDE NR 7 STOP FITTING CUTOUT. MAJOR REPAIR ACCOMPLISHED : FABRICATED & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080700008 20070807 00008 NM 2007 8 7 2007UALA02829 1 20070725 A 5210 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE PAX DOOR GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 FWD ENTRY DOOR SN 229 WEB ANGLES AT BOTH UPPER AND LOWER TORQUE TUBE BUSHINGS ARE GOUGED FROM TORQUE TUBE CONTACT. MAJ OR REPAIR ACCOMPLISHED: INSTALLED NEW INTERCOSTALS ADJACENT TO HINGE ARM CASTINGS. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080700009 20070807 00009 EU 2007 8 7 2007UALA02830 1 20070725 A 5210 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R1 DOOR ASSIST DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 445UA 826 DOOR 1R ASSIST BOTTLE HAS ZERO PRESSURE. PRESSURE DISK FAILURE ON DOOR ASSIST BOTTLE. REPLACED THE R1 DOOR BOTTLE PRESSURE DIAPHRAGM AND SERVICED BOTTLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080700011 20070807 00011 EU 2007 8 7 2007UALA02832 1 20070725 A 3250 STEERING SYS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG INOPERATIVE A UALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 29 457UA 1146 PER FLT CREW: NOSE GEAR STEERING INOP. NOSE LANDING GEAR STEERING SERVO CONTROL UNIT INTERNAL GROUND SHORTED. REP LACED NLG SERVO CONTROL UNIT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080700014 20070807 00014 NM 2007 8 7 2007UALA02835 1 20070725 A 5754 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 SLAT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 NR 1 SLAT DAMAGED ABOVE INBD GUIDE OUT OF LIMITS. REMOVED NR 1 SLAT AND REPAIRED, REINSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080700016 20070807 00016 EU 2007 8 7 2007UALA02837 1 20070726 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ROWS 9 & 18 NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 409UA 462 EMERGENCY AISLE LIGHTS AT SEAT ROWS 9&18 NOT ILLUMINATING ON TEST. DISCONNECTED CONNECTOR UNDER SEAT 9A. SECURED CON NECTOR AND RELAMPED THE LIGHT FIXTURE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080700020 20070807 00020 NM 2007 8 7 2007UALA02841 1 20070725 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SEATS 20AB TO 23 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 EMERGENCY EEL LIGHTS AT SEATS 20AB TO 23AB INOP, EMERGENCY EXIT DOORS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080700021 20070807 00021 NM 2007 8 7 2007UALA02842 1 20070725 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SEATS 2AB & 38HJ INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 FWD EEL LIGHT AT SEAT 2AB AND LIGHT AT SEATS 38HJ ARE INOPERATIVE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080700025 20070807 00025 NM 2007 8 7 2007UALA02846 1 20070726 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 CEILING EMERGENCY LIGHTS INOP AT COCKPIT, ROW 16, ROW 18 AND ROW 32. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080700026 20070807 00026 NM 2007 8 7 2007UALA02847 1 20070726 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EEL INOP:SEATS 5E FWD AND 5J AFT SECTIONS. RELAMPED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080700027 20070807 00027 NM 2007 8 7 2007UALA02848 1 20070726 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EMERGENCY LIGHT INOPERATIVE: DOORS 2R AND 5L SLIDE ILLUM. RELAMPED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080700029 20070807 00029 NM 2007 8 7 2007UALA02850 1 20070726 A 3397 80603 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EMERGENCY LIGHT INOP, DOOR 5R CROSS AISLE. BAD RIBBON CABLE. REPLACED RIBBON CABLE. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080700030 20070807 00030 NM 2007 8 7 DHL2007784519 1 20070719 A 5522 SKIN BOEING 727 727227 1384078 NM RT ELEVATOR DISTORTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 RT ELEVATOR, LWR SKIN IS OIL CANNING ON INBD DRAIN HOLE SKIN, 11 FWD OF ELEVATOR T/E, R ELEV STA 17.20. REMOVED DAMAGED AREA DIM .5 BY .75 IAW B727 SRM 55-20-3, FIG 1. FABRICATED DOUBLER REPAIR, MATERIAL USED 2024T3, 032, 5 BY 5 IAW B727 SRM 55-20-3, FIG 1. TREATED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 51-10-2 AND 55-20-3, FIG 1. 2 L 7 3 4F A3WE 2007080700031 20070807 00031 NM 2007 8 7 DHL2007784520 1 20070708 A 5754 RIB BOEING 727 727227 1384078 NM NR 5 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 RT WING STA 233.5, NR 5 SLAT INBD ACTUATOR ATTACH RIB CRACKED. REMOVED 2 DAMAGED RIBS IAW B727 SRM 51-30-5. FABRICATED NEW RIB SUPPORTS FROM 7075T6, .071, 12 BY 2.50 IAW B727 SRM 57-50-2, FIG 2 AND 51-20-1. TREATED, PRIMED AND INSTALLED RIB SUPPORTS IAW B727 SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 2007080700034 20070807 00034 NM 2007 8 7 DHL2007784522 1 20070710 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM BS 740-868 GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 MAIN CARGO COMPARTMENT NICKS, GOUGES AND CORROSION ON SEAT TRACK RBL 24 BS 740 TO BS 868, WL 208.5 ON UPPER AND LOWER TR ACK SURFACES. REMOVED DAMAGED SEAT TRACK STA 760 TO BS 850 IAW B727 SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK P/ N BAC1520-841-7178T6, DIM. 99.25 LONG IAW B727 SRM 53-10-2, FIG 8 AND 51-30-5. TREATED, PRIMED AND INSTALLED SEAT TRACK IAW B727 SRM 51-10-2 AND 51-30-2, FIG 1. 2 L 7 3 4F A3WE 2007080700035 20070807 00035 NM 2007 8 7 DHL2007784524 1 20070708 A 5330 SKIN BOEING 727 727227 1384078 NM ZONE 100 BURNED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 EXTERNAL FUSELAGE BS 259.5 AT STR 12R HAS A LIGHTING STRIKE BURN. BLENDED OUT AREA OF LIGHTNING STRIKE IAW B727 SRM 53- 30-3, FIG 20. MATERIAL LOSS OVER 30 PERCENT, LIGHTNING STRIKE STILL PRESENT AND OUT OF LIMITS IAW B727 SRM 53-30-1. CUT OUT DAMAGED SKIN AREA DIM 1 BY 2 IAW B727 SRM 53-30-3, FIG 3. HFEC COMPLIED WITH IN CUT OUT AREA, NO CRACKS NOTED IAW B727 NDTM PT.6 51-00-00, FIG 23. FABRICATED DOUBLER REPAIR FROM 2024T3, .071”, DIM 8 BY 6.5 AND FILLER FROM 2024T3, .06 3, DIM 2 BY 1 IAW B727 SRM 53-30-3, FIG 3. TREATED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 51-10-2, 51-30-2 AND 53-30 -3, FIG 3. 2 L 7 3 4F A3WE 2007080700037 20070807 00037 NM 2007 8 7 DHL2007784526 1 20070708 A 5330 SKIN BOEING 727 727227 1384078 NM ZONE 200 BURNED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 EXTERNAL FUSELAGE BS 188 BELOW STR 13R HAS A LIGHTNING STRIKE BURN. BLENDED OUT AREA OF LIGHTNING STRIKE IAW B727 SRM 5 3-30-3, FIG 20. MATERIAL LOSS OVER 30 PERCENT OUT OF LIMITS IAW B727 SRM 53-30-1. CUT OUT DAMAGED SKIN AREA DIM. 2.5 B Y 2 IAW B727 SRM 53-30-3, FIG 3. HFEC COMPLIED WITH IN CUT OUT AREA, NO CRACKS NOTED IAW B727 NDTM PT.6 51-00-00, FIG 2 3. FABRICATED DOUBLER AND FILLER FROM 2024T3, .071, DIM 10.5 BY 8 AND FILLER FROM 2024T3, .063”, DIM 2.5 BY 2 IAW B727 SRM 53-30-2, FIG 1. TREATED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 51-10-2, 53-30-2, FIG 2 AND 53-30-3. 2 L 7 3 4F A3WE 2007080700039 20070807 00039 GL 2007 8 7 J4PA200702558 1 20070726 A 2420 646843 ALTERNATOR CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO HARTZL HCJ3Y PHCJ3YF1 GL ENGINE OPEN E J4PA O OTHER J WARNING INDICATION CR CRUISE 1 SO 13 675CD 7 1708 688944 FP3777B AIRCRAFT DEPARTED KCAE TO KHXD WITH 1 PASSENGER. DURING CRUISE NR 1 ALT FAIL LIGHT ILLUMINATED. PILOT RETURNED TO KCAE WITHOUT INCIDENT. MAINTENANCE DROVE TO KCAE, REMOVED AND REPLACED THE NR 1 ALTERNATOR AND NR 1 FIELD CONTROL MODULE. 1 L 7 1 3O 3 O NT A00009CH E3SO 5 C P36EA 2007080700041 20070807 00041 WP 2007 8 7 IXXA07SMN178S 1 20070630 A 5522 SKIN DOUG DC8 DC873F 302199F WP ZONE 300 DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND LT ELEVATOR LOWER SKIN SHOWS DENT AT STATION XE 55.062. REMOVED FASTENER AS NE EDED TO PERFORM REPAIR AND DAMAGED AREA. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS FROM STATION XAR 0 TO STATION XE 132.000. PERFORMED BALANCE TO LT ELEVATOR IAW DC8 SRM 51-4-4 PAGES 1-2. FOUND WITHIN ALLOWABLE TOLERANCE LIMITS. MOMENT 1450.87 IN LBSDC8 SRM 55-4-1 FIGURE 1 SHEETS 1 AND 2, DC8 SRM 55-1-0 FIGURE 1, DC8 SRM 51-1-21, DC8 SRM 55-4-1 FIGURE 1 SHEETS 1 AND 2 IT EM "E" AND "F", DRAWING DOUGLAS NR 5654970-5, DC8 SRM 51-1-9, DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007080700045 20070807 00045 NM 2007 8 7 UPS07450252 1 20070705 A 5313 STRINGER BOEING 747 747212B 1384886 NM BS 550 S30L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C FWD CARGO COMPT S30L STRINGER FOUND DAMAGED AT STA 550, CRACK LENGTH 7/16". FWD CARGO COMPT BS 550 ST R 30L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 2. REPEAT INSPECTION IS REQUIRED AS PER SRM 53-10-03 FIG 2 SHEET 4 TABL E 3. UPS MPI NR P109303 RAISED. 2 L 7 4 4F A20WE 2007080700046 20070807 00046 NM 2007 8 7 UPS07450253 1 20070706 A 5320 65B0765265 INTERCOSTAL BOEING 747 747212B 1384886 NM BS 340-350 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C LT FUSELAGE SKIN AREA AT BS 340-350 STR 5A 1 FASTENER HOLE FOUND CRACKED AT INTERCOSTAL. (1ST LAYER FR OM I/B) RUNNING DOWNWARD APP 0.030" IN LENGTH (REFER SKETCH FOR DETAIL). LT FUSELAGE SKIN BS 340-360 STR 5A ATTACHED IN TERCOSTAL REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007080700047 20070807 00047 NM 2007 8 7 UPS07450254 1 20070706 A 5340 STRINGER CLIP BOEING 747 747212B 1384886 NM AFT CARGO CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C AFT CARGO COMPT S33L STRINGER CLIP FOUND CRACKED AT STA 1760, CRACK LENGTH 5/16". AFT CARGO COMPT BS 1760 STR 33L STRINGER CLIP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007080700048 20070807 00048 NM 2007 8 7 UPS07450255 1 20070705 A 5320 PANEL SUPPORT BOEING 747 747212B 1384886 NM BS 1540 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C AFT CARGO COMPT SLOPE PANEL LT SIDE UPPER SUPPORT FOUND CRACKED AT STA 1540, CRACK LENGTH 1/2". AFT C ARGO COMPT BS 1530 TO BS 1550 LT SIDE SLOPE PANEL UPPER SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 2. 2 L 7 4 4F A20WE 2007080700050 20070807 00050 NM 2007 8 7 UPS07450257 1 20070705 A 5340 65B386001007 STRINGER CLIP BOEING 747 747212B 1384886 NM BS 1680 S33L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C AFT CARGO COMPT S33L STRINGER CLIP FOUND CRACKED AT STA1680, CRACK LENGTH 3/8". AFT CARGO COMPT BS 16 80 STR33L STRINGER CLIP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007080700051 20070807 00051 NM 2007 8 7 UPS07450258 1 20070705 A 5310 65B3848822 CREASE BEAM BOEING 747 747212B 1384886 NM BS 960-980 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C RT FX CROWN BS 960-980 UPPER CREASE BEAM FWD FRAME ATTACH ANGLE RADIUS FOUND CRACK APPROX 1/2" LONG. FX CROWN BS 960-980 RT UPPER CREASE BEAM FWD FRAME ATTACH ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-3 0-02. 2 L 7 4 4F A20WE 2007080700053 20070807 00053 NM 2007 8 7 UPS07450260 1 20070705 A 5310 65B3848863 CREASE BEAM BOEING 747 747212B 1384886 NM BS 940-960 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C FX CROWN BS 940-960 LOWER CREASE BEAM FWD FLANGE RADIUS FOUND CRACK APPROX 3/8" LONG. FX CROWN BS 940 -960 LOWER CREASE BEAM REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007080700054 20070807 00054 NM 2007 8 7 UPS07450261 1 20070705 A 5310 65B3848866 CREASE BEAM BOEING 747 747212B 1384886 NM BS 960-980 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C RT FX CROWN BS960-980 LOWER CREASE BEAM FWD FLANGE FOUND CRACK APPROX 1/2" LONG. FX CROWN BS 960-980 RT LOWER CREASE BEAM REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007080700055 20070807 00055 NM 2007 8 7 UPS07450262 1 20070702 A 5320 PLATE BOEING 747 747212B 1384886 NM BS 920 MISINSTALLED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D BS 920 LT TENSION TIE FWD ATT STEEL PLATE LOWER ROW MOST O/B FASTENER HOLE FOUND SHORT EDGE MARGIN , M/D BS 920 LT TENSION TIE FWD ATTACH STEEL PLATE REPAIRED AS PER RS R53-25-35821 AND UPS EO B747-5310-27268. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35821 AND UPS EO B747-5310-27268. 2 L 7 4 4F A20WE 2007080700056 20070807 00056 NM 2007 8 7 UPS07450263 1 20070708 A 5322 69B036301 SHEAR TIE BOEING 747 747212B 1384886 NM BS 2200 S42-34L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C AFT OF BULK CARGO COMPT SKIN ATT ANGLE FOUND BULGE AT STA 2200 BTN S42L AND S37L. CORROSION BLEND OUT EXFOLIATION THROUGH WHOLE THICKNESS. AFT OF BULK CARGO COMPT BS 2200 STR 37L TO STR 42L FRAME ATTACH SUPPORT ANGLE REP LACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007080700057 20070807 00057 NM 2007 8 7 UPS07450264 1 20070706 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C NR 3L MED CUTOUT AFT UPPER CORNER FOUND SKIN AND BEARSTRAP EDGE FOUND CRACKED, CRACK LENGTH 1/8" APPRO X. NR 3L MED CUTOUT AFT UPPER CORNER AND BEARSTRAP REPAIRED AS PER UPS EO B747-5330-24674 APP I AND O. 2 L 7 4 4F A20WE 2007080700058 20070807 00058 NM 2007 8 7 UPS07450265 1 20070707 A 5320 65B11751605 REVEAL BOEING 747 747212B 1384886 NM DOOR FRAME CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D L3 DOOR FWD CUTOUT LWR CORNER REVEAL FTG FOUND CRACK, CRACK LENGTH 3/4" APPROX. M/D L3 DOOR FWD C UTOUT LWR CORNER REVEAL FTG REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007080700059 20070807 00059 NM 2007 8 7 UPS07450266 1 20070714 A 5320 SUPPORT BOEING 747 747212B 1384886 NM BS 920-940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D BS920-940 RBL30 TENSION TIE SUPPORT FOUND CRACK, CRACK LENGTH 5/16". M/D BS 920-940 RBL30 TENSION TIE SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007080700060 20070807 00060 NM 2007 8 7 UPS07450267 1 20070714 A 5320 SUPPORT BOEING 747 747212B 1384886 NM BS 930-940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D BS 930-940 LBL30 TENSION TIE SUPPORT FOUND CRACK, CRACK LENGTH 3/8". M/D BS 920-940 LBL30 TENSION TIE SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007080700068 20070807 00068 NM 2007 8 7 UPS07450275 1 20070705 A 5315 FLOORBEAM BOEING 747 747212B 1384886 NM BS 2360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D BS 2360 LBL 55 FLOORBEAM UPPER CHORD FOUND CORROSION. CORROSION BLEND OUT 0.047" BY 1" BY 2" EXCE ED SRM LIMIT. M/D BS 2360 LBL25 TO LT MOST O/B AREA FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 1. 2 L 7 4 4F A20WE 2007080700069 20070807 00069 NM 2007 8 7 UPS07450276 1 20070705 A 5320 69B030061 FLOOR SUPPORT BOEING 747 747212B 1384886 NM BS 2300-2320 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D STA2300-2320 LBL34 FLOOR SUPPORT FOUND SEVERAL CORROSION. CORROSION BLEND OUT 0.023" BY 1" BY 4" EXCEED SRM LIMIT. M/D BS 2300-2320 LBL34 FLOOR SUPPORT REPLACED AND INSTALED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007080700071 20070807 00071 NM 2007 8 7 UPS07450278 1 20070705 A 5710 SHEAR TIE BOEING 747 747212B 1384886 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C RT W/G REAR SPAR WS 375 UPPER FIXED PANEL SUPPORT APPEARED CORRODED. CORROSION BLEND OUT EXFOLIATION THROUGH WHOLE THICKNESS 2" BY 3/4" EXCEED SRM LIMIT. RT W/G REAR SPAR WS375 UPPER FIXED PANEL SUPPORT REPAIRED AS PER S RM 51-40-04 FIG 2. 2 L 7 4 4F A20WE 2007080700072 20070807 00072 NM 2007 8 7 UPS07450279 1 20070705 A 5320 65B106718 STIFFENER BOEING 747 747212B 1384886 NM BS 1241 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C RT W/G W/W STIFFENER CORROSION AT STA 1241 RBL 85, CORROSION BLEND OUT 0.105" BY 2" BY 4" EXCEED SRM 5 7-10-01 FIG 1 LIMITS. RT W/G W/W AT BS 1241 RBL 85" VERT STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007080700074 20070807 00074 NM 2007 8 7 UPS07450281 1 20070705 A 5320 SUPPORT ANGLE BOEING 747 747212B 1384886 NM BS 1000 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C FWD CARGO COMPT STA 1000 BULKHEAD 1 SUPPORT ANGLE FOUND CRACKED AT LBL 100 WL 155, CRACK LENGTH 1/2". FWD CARGO COMPT BS 1000 BULKHEAD AT LBL 100 WL 155 SUPPORT ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51 -30-02. 2 L 7 4 4F A20WE 2007080700075 20070807 00075 NM 2007 8 7 UPS07450282 1 20070703 A 5320 PLATE BOEING 747 747212B 1384886 NM BS 900 MISINSTALLED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D BS 900 LT TENSION TIE FWD ATT STEEL PLATE UPPER ROW MOST O/B FASTENER HOLE FOUND SHORT EDGE MARGIN . M/DECK BS 900 LT TENSION TIE FWD ATTACH STEEL PLATE REPAIRED AS PER HX RS NR R53-25-35819 AND CONTINUE INSPECTION IS REQUIRED AS PER UPS EO NR B747-5310-27294. 2 L 7 4 4F A20WE 2007080100107 20070801 00107 EA 2007 8 1 MASA200700098 1 20070212 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 27172 7172 ASH 7348 IAD. AIRCRAFT RETURNED TO THE FIELD WHEN CREW REPORTED A PAX DOOR WARNING MESSAGE IN FLIGHT. MX LUBED THE OU TER DOOR HANDLE MECHANISM AND PERFORMED PRESSURIZATION CHECKS WITH NO FAULTS FOUND. 2 L 7 2 4F RT A21EA 2007080100130 20070801 00130 EA 2007 8 1 MASA200700086 1 20070209 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE STICKING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37342 7342 ASH 7202 ORD - SERVICE DOOR WOULD NOT OPEN. MX FOUND THE DOOR STICKING DUE TO THE COLD AND FREED IT UP AND OP CHECKED G OOD. 2 L 7 2 4F RT A21EA 2007080100134 20070801 00134 EA 2007 8 1 MASA200700091 1 20070210 A 5240 LATCH CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR LACK OF LUBE A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 37342 7342 ASH 7181 DSM - CREW REPORTED THE SERVICE DOOR WAS DIFFICULT TO OPEN. MX LUBED THE HINGE AND LATCH MECHANISMS AND THE DO OR, OP CHECKED GOOD. 2 L 7 2 4F RT A21EA 2007080100137 20070801 00137 EA 2007 8 1 MASA200700282 1 20070523 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX OUT OF RIG A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 593ML 7465 ASH 7256 ORD - PAX DOOR W/NOT CLOSE. MX IS IN THE PROCESS OF RIGGING THE DOOR. 2 L 7 2 4F RT A21EA 2007080100138 20070801 00138 EA 2007 8 1 MASA200700257 1 20070510 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX NONE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7264V 7264 ASH 2750 PHX - CREW UNABLE TO OPEN MAIN CABIN DOOR FROM INSIDE. MX OPENED DOOR AND FOUND NO FAULTS. OPS CHECKED NORMAL . 2 L 7 2 4F RT A21EA 2007080100145 20070801 00145 2007 8 1 MASA200700158 4 20070321 A 2561 P0640101 LIFE VEST CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 655BR 1154 7457 ASH 1032 HNL - TWO INFANT LIFE VEST WERE MISSING. MX INSTALLED 2 NEW LIFE VESTS. 2 L 7 2 4F RT A21EA 2007080100164 20070801 00164 EA 2007 8 1 MASA200700106 1 20070215 A 1100 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27172 7172 ASH 7133 IAD - EMERGENCY EXIT SIGN MISSING FROM PAX DOOR. MX RESECURED. 2 L 7 2 4F RT A21EA 2007080100170 20070801 00170 EA 2007 8 1 MASA200700012 1 20070103 A 2750 WARNING MESSAGE CNDAIR CL600 CL6002D24 1390016 EA TE FLAPS FALSE ACTIVATION A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 939LR 15039 ASH 2687 DTW - FLAP 1/2 SPEED STATUS MESSAGE. MX RESET SYSTEM AND FAULT CLEARED. SYSTEM OPS CHECK NORMALLY WITH NO DEF ECTS NOTED. 2 L 7 2 4F RT A21EA 2007080100172 20070801 00172 EA 2007 8 1 MASA200700230 1 20070430 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY NO TEST A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 17358 7358 ASH 2985 PHX - LAV SMOKE DETECTOR WOULD NOT TEST. MX RESECURED THE SMOKE DETECTOR HARDWARE AND THE SYSTEM TEST WAS GOO D. 2 L 7 2 4F RT A21EA 2007080100180 20070801 00180 EA 2007 8 1 MASA200700261 1 20070511 A 2560 TUBE CNDAIR CL600 CL6002B19 1900309 EA PSU STRETCHED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17358 17358 ASH 2832 LAS - ROW 11 D/F PSU FELL DOWN. MX FOUND THE TUBING WAS STRETCHED AND REINSTALLED THE TUBING. 2 L 7 2 4F RT A21EA 2007080100185 20070801 00185 EA 2007 8 1 MASA200700014 1 20070103 A 2751 5913163 SENSOR CNDAIR CL600 CL6002D24 1390016 EA TE FLAPS MALFUNCTIONED A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 939LR 3987 15039 ASH 2618 CLT - FLAPS 1/2 SPEED STATUS. MX REPLACED BOTH RT INBD SKEW SENSORS. 2 L 7 2 4F RT A21EA 2007080100197 20070801 00197 EA 2007 8 1 MASA200700045 1 20070122 A 5220 SEAL CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT DIRTY A MASA O OTHER O OTHER CR CRUISE 1 SW 07 17175 7175 ASH 7364 ORD - PILOT REPORTED LEFT EMERGENCY DOOR CAUTION IN FLIGHT. MX WAS CALLED OUT AND REMOVED THE DOOR, INSPECTED AND CLEANED SEAL AND SWITCH AND PERFORMED OPS CHECK. THE OPS CHECK WAS GOOD. 2 L 7 2 4F RT A21EA 2007080200017 20070802 00017 EA 2007 8 2 MASA200700302 1 20070604 A 3350 RELAY CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 932LR 15032 ASH 2726 LAS - CAPTAIN REPORTED THE EMERGENCY LIGHTS WERE CYCLING ON AND OFF ON THE GROUND ON GPU AND APU GEN POWER. MX CHANGED RELAY K135 ON PCBC 5 IN JB11. 2 L 7 2 4F RT A21EA 2007080200030 20070802 00030 NM 2007 8 2 UIEA200700294 1 20070725 A 5753 STRUCTURE BOEING 747 747271C 1384869 NM ZONE 600 PUNCTURED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 PUNCTURE IN COMPOSITE ON RIGHT OUTBOARD T/E FLAP CARRIAGE NR 6 ON RT INBOARD FLAP. REMOVED DAMAGED FABRICATED DOUBLER O UT OF 2024 T3 IAW SRM 51-40-20. 2 L 7 4 4F A20WE 2007080200034 20070802 00034 NE 2007 8 2 UIEA200700293 2 20070721 A 7200 ENGINE BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE NR 3 FAILED A UIEA E ENGINE SHUTDOWN E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 15 527MC 22471 530276 NR 3 ENGINE SHUT DOWN DUE TO A LOUD BANG, N1 STARTED TO DECREASED, VISUAL INSPECTION SHOWED NO OPEN T/R BUT ENGINE WAS S WINGING EXCESSIVELY COMPARED TO NR 4 ENGINE WAS NOT SWINGING OR MOVING SMOOTH AIR SHUT DOWN IAW FHB SEC 3. 2 L 7 4 4F 4 F RT A20WE E23EA 2007080200043 20070802 00043 NM 2007 8 2 DL76P070953 1 20070724 A 3620 CIRCUIT CARD BOEING 767 767332 1382001 NM NR 2 ENGINE DEFECTIVE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 144DA 1654 27584 1654 RIGHT DUCT LEAK LIGHT INFLIGHT CLIMBING THRU FL210. CHECKED ALL DUCTS FROM RT ENGINE TO THE RT ISOL VALVE. REPLACED WH EEL WELL OVHT ECS DUCT LEAK DETECTION SYS CONTROL CARD. RAN ENGINES AT IDLE FOR 30 MINUTES, T/O POWER FOR 10 MINUTES AN D 15 MINUTES AT CLIMB POWER. NO TROUBLE NOTED. 2 L 7 2 4F RT A1NM 2007080200050 20070802 00050 EA 2007 8 2 SWIA200718523 1 20070531 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 973SW 7949 FS280 FLOOR SUPPORT BEAM IS CRACKED AT LOWER LBL9, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS AT FS 280 FLOOR SUPPOR T LOWER LBL9 PER REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 2007080200052 20070802 00052 EA 2007 8 2 SWIA200718525 1 20070531 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 973SW 7949 FLOOR SUPPORT STRUCTURE ATTACHED TO BULKHEAD AT STA 621 IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS PER C RJ200 REO 601R 53-61-117 REV A. 2 L 7 2 4F RT A21EA 2007080200059 20070802 00059 SO 2007 8 2 SWIA200718532 1 20070723 A 2910 LINE EMB 120 EMB120ER 3260203 SO HYD SYSTEM LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 294SW 120321 FLT 2945 - IN FLIGHT AT CRUISE, BLUE HYDRAULIC SYSTEM FLUID WAS LEAKING. PERFORMED PERMANENT HARDLINE REPAIR AT RIGHT E NGINE OUTBOARD NACELLE IAW MM 20-10-04. LEAK CHECK GOOD. 2 L 7 2 4T RT A31SO 2007080200066 20070802 00066 WP 2007 8 2 070141 1 20070708 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 892GA 49826 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENC Y EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BA TTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007080200068 20070802 00068 NM 2007 8 2 07FDEA02638 1 20070727 A 5753 652163475 SKIN BOEING 727 7272S2F 1384O81 NM LT WING TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 212FE 22934 LT WING IB AFT FLAP DISBONDED AT IB END REMOVED AND REPLACED FLAP ASSY IAW MM 27-51-002-4. 2 L 7 3 4F A3WE 2007080200076 20070802 00076 NM 2007 8 2 QXEA200701212 1 20070722 A 2420 31708001A GENERATOR DHAV DHC8 DHC8202 2809007 NM NR 2 AC INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 1254 1254 512 SEA - RIGHT STALL WARNING CAUTION LIGHT FOLLOWED 5 SECONDS LATER BY NR 2 AC GENERATOR CAUTION LIGHT. RAN CHECKLIST, ALL CAUTION LIGHTS OUT. SHORTLY THEREAFTER RIGHT STALL WARNING CAUTION LIGHT FOLLOWED BY NR 2 AC GENERATOR CAUTION. NR 2 AC GENERATOR SWITCH TURNED OFF. MAINTENANCE REMOVED AND REPLACED NR 2 AC GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007080200079 20070802 00079 NM 2007 8 2 2007UALA02799 1 20070723 A 3350 60243 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 202UA 24717 EEL LIGHT INOPERATIVE AT AFT LAV. REPLACED EEL LIGHT STRIP IN FLOOR AT AFT FWD GALLEY AREA. OPS CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080200082 20070802 00082 NM 2007 8 2 2007UALA02802 1 20070723 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294-328 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 CABIN FLOOR CREASE BEAM INBD OR DOOR 1R CORRODED BS 294- 328. INSTALLED REPLACEMENT CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080200083 20070802 00083 NM 2007 8 2 2007UALA02803 1 20070723 A 3350 767 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 540UA 25252 FWD OVERWING EMERGENCY SLIDE LIGHT INOP AT LEFT OVERWING HATCH. RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080200086 20070802 00086 NM 2007 8 2 2007UALA02806 1 20070722 A 5753 STRUCTURE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE TE FLAPS CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26877 TWO CRACKS IN LT INBD MID TRAILING EDGE FLAP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080200087 20070802 00087 NM 2007 8 2 2007UALA02807 1 20070724 A 2897 WIRE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 2 FUEL FLOW DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 910UA 25254 CENTER FQI INOP, NR 2 ENG FUEL FLOW INDICATOR INOP. FOUND CENTER CONDUCTOR WIRE PULLED OUT OF D800 IN COCKPIT. CONNEC TOR REPLACED AND CTR TANK DCTU CALIBRATED. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080200089 20070802 00089 EU 2007 8 2 2007UALA02809 1 20070724 A 2622 EXTINGUISHER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 416UA 479 FIRE EXTINGUISHER PSI IN COCKPIT LOW. LOSS OF PRESSURE IN BOTTLE (FIREXT) REPLACED HALON FIRE EXT IN COCKPIT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080200097 20070802 00097 NM 2007 8 2 2007UALA02817 1 20070724 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE AFT GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 647UA 25284 LARGE AFT GALLEY EEL STRIP IS INOPERATIVE. REPLACED EEL STRIP. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080200127 20070802 00127 NM 2007 8 2 ZZDA2007241 1 20070615 A 5320 INTERCOSTAL BOEING 717 717200 1383700 NM BS 1002-1022 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 INTERCOSTAL AT BS 1002 - 1022 AND BETWEEN LONG 26L AND 27L. INSTALLED INTERCOSTAL BETWEEN STA 1002 AND STA 1022 AND BET WEEN LONGERON 26L AND 27L IAW B717 SRM 51-41-02. 2 L 7 2 4F TR A6WE 2007080200145 20070802 00145 NM 2007 8 2 SWAA073712 1 20070726 A 5311 6546552 FRAME BOEING 737 7373K2 13844BA NM BS 827 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200154 20070802 00154 NE 2007 8 2 JBGA200700012 2 20070726 A 7597 WIRE HARNESS LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE BLEED VALVE MALFUNCTIONED E BSYA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 07 529KF 064 PCE305248 ON TAKEOFF OUT OF LUK TO TSY AT 4000 FT RIGHT ENGINE STARTED SURGING FROM FULL POWER TO IDLE, PILOT REDUCED POWER TO 85 PERCENT THEN 10 SECONDS ENGINE STARTED TO SURGE FROM 85 PERCENT TO IDLE, PILOT THEN SHUT ENGINE DOWN AND RETURNED TO LUK NO PROBLEM. CAUSE FOR THIS PROBLEM NOT KNOWN AT THIS TIME 7-27-2007. ENGINE REPAIRED BY REPLACING BLEED AIR VALVES AN D ENGINE WIRE HARNESS. AIDS RECORD SUBMITTED ON 8/1/2007 2 L 7 2 4F 4 F RT A10CE E35NE 2007080200163 20070802 00163 NM 2007 8 2 SWAA073688 1 20070726 A 5522 65C25746 SKIN BOEING 737 7373H4 1384600 NM LT ELEVATOR DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 618WN 28034 DURING SCHEDULED C1 CHECK, FOUND LT ELEVATOR DELAMINATED AT LOWER OUTBOARD END. REMOVED AND REPLACED ELEVATOR PER MM. 2 L 7 2 4F RT A16WE 2007080200165 20070802 00165 NM 2007 8 2 SWAA073686 1 20070726 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 400 S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080200170 20070802 00170 2007 8 2 SWAA073677 4 20070726 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007080200172 20070802 00172 NM 2007 8 2 KCSA071255 1 20070725 A 5330 SKIN BOEING 747 7472B4B 138481B NM BS 2198 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 FUSELAGE SKIN CRACKED AT BS 2198 BETWEEN STR-46R AND STR-44R. 2 L 7 4 4F RT A20WE 2007080200175 20070802 00175 NM 2007 8 2 SWAA073646 1 20070725 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 230WN 34592 EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007080200195 20070802 00195 WP 2007 8 2 ASAA0781903 1 20070726 A 5321 993655113 FLOOR PANEL DOUG DC9 DC983 3022083 WP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-24-0 AND 53-05. 2 L 7 2 4F RT A6WE 2007080200196 20070802 00196 WP 2007 8 2 ASAA0781904 1 20070726 A 5321 99365465 FLOOR PANEL DOUG DC9 DC983 3022083 WP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-24-0 AND 53-05. 2 L 7 2 4F RT A6WE 2007080300007 20070803 00007 NM 2007 8 3 UPS07450294 1 20070703 A 5320 PLATE BOEING 747 747212B 1384886 NM BS 820 MISINSTALLED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D BS 820 RT TENSION TIE FWD ATT STEEL PLATE LOWER ROW MOST O/B FASTENER HOLE FOUND SHORT EDGE MARGIN . M/D BS820 RT TENSION TIE FWD ATTACH STEEL PLATE REPAIRED AS PER RS R53-25-35817 AND UPS EO B747-5310-27264. CONTINUE D INSPECTION IS REQUIRED AS PER RS R53-25-35817 AND UPS EO B747-5310-27264. 2 L 7 4 4F A20WE 2007080300019 20070803 00019 WP 2007 8 3 IXXA07SMN188S 1 20070630 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 660 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND THE MID ACCESSORY COMPARTMENT FITTING CRACKED BETWEEN STATION 660.000 LONGERO N 36 LT. REMOVED CRACKED FITTING. FABRICATED FITTING. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED FITTING IAW DC8 SRM 51-1-20D AND 51-3-1, REPAIR SPECIFICATION NUMBER 2003-05, DOUGLAS DRAWING N UMBER 3750497, NDT SPM PART 08-00-02 TO 07, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007080300022 20070803 00022 NM 2007 8 3 UPS07450307 1 20070703 A 5314 65B150746 KEELBEAM BOEING 747 747212B 1384886 NM BS 1445-1448 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C FX KEEL BEAM RT LOWER CHORD UPPER SURFACE FOUND CORROSION AT STA 1445-1448 RBL8. CORROSION BLEND OUT 0.091" BY 2" BY 3" EXCEED SRM LIMIT. FX KEEL BEAM RT LOWER CHORD BS 1445-1448 RBL8 LWR FLANGE UPPER SURFACE CORROSION R EMOVED AND REPROTECTED AS PER SRM 51-10-01 AND 51-10-02 AN RS R53-49-35827 AND UPS ENGINEERING FILE NR 747-53-20424. 2 L 7 4 4F A20WE 2007080300028 20070803 00028 NM 2007 8 3 UPS07450313 1 20070703 A 5320 CHANNEL BOEING 747 747212B 1384886 NM BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C RT BS 940 TENSION TIE TO FRAME CONNECTION AREA FOUND 1 FASTENER HOLE CRACKED AND 3 FASTENER HOLES OVAL AT FWD CHANNEL, CRACK LENGTH 0.090" APPROX. M/D BS 940 RT TENSION TIE FWD CHANNEL LT TO RT REPLACED AND INSTALLED AS P ER SRM 51-10-01 PG 9 AND 51-30-02 AND EO B747-5310-23715-C. 2 L 7 4 4F A20WE 2007080300034 20070803 00034 NM 2007 8 3 UPS07450319 1 20070706 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C NR 3R MED CUTOUT FWD LOWER CORNER FOUND SKIN AND BEARSTRAP EDGE CRACKED. NR 3R MED CUTOUT FWD LOWER C ORNER SKIN AND BEARSTRAP REPAIRED AS PER UPS EO B747-5310-24674 APP N. 2 L 7 4 4F A20WE 2007080300039 20070803 00039 NM 2007 8 3 UPS07450322 1 20070703 A 5320 CHANNEL BOEING 747 747212B 1384886 NM BS 880 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C LT BS 880 TENSION TIE NR 6 HOLE FOUND CRACK AT AFT CHANNEL APPROX 0.040" RUNNING UP. M/D BS 880 TENSI ON TIE AFT CHANNEL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER UPS EO B747-5310-23715-C AND SRM 51-30-02 REFE R NRC 50076 FOR WORKING DETAIL. 2 L 7 4 4F A20WE 2007080300047 20070803 00047 2007 8 3 UPS07650325 2 20070710 A 7532 SHUTOFF VALVE BOEING 767 76734AF 1385212 NM RT ENGINE MALFUNCTIONED A IPXA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 327UP 27753 INSPECTION TYPE:ETOP RT ENGINE HPSOV DISPLAYED. R ENG BLEED LEFT ILLUMINATED STEADY AT HIGH THRUST. DUCT PRESS NORMAL. REMOVED AND REPLACED HPSOV RT ENG IAW 36-11-07-4. PERFORMED TEST IAW 36-11-07-5 RUN ENGINES ALL CHECK OK. 2 L 7 2 4F RT A1NM 2007080300058 20070803 00058 NM 2007 8 3 UPS07650328 1 20070723 A 4920 ENGINE BOEING 767 76734AF 1385212 NM APU INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 312UP 27763 INSPECTION TYPE:ETOP APU WILL NOT START. T/S PER FIM 49-11-00 FIG 104. RESET APU ECU POWER, APU RUN UP OPS CHECK NORMA L. 2 L 7 2 4F RT A1NM 2007080300064 20070803 00064 NM 2007 8 3 UPS07M50285 1 20070605 A 5311 FRAME DOUG MD11 MD11 3023602 NM BS 1841 L44 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C AFT CGO STA 1841 APPROX LONGERON 44 AREA, FRAME FOUND WITH CORROSION AS MARKED. DAMAGED FRAME REMOVED PER SRM 51-31-01 V.2R.38. NEW FRAME FASTENER HOLES PICKED UP PER SRM51-31-01 V.2R.38. NEW FRAME REPROTECTED AND PAINT TOUCHED UP PER SRM 51-21-01 V.2R.38. NEW FRAME INSPECTED OK TO INSTALL. NEW FRAME INSTALLED PER SRM 51-31-01 V.2R.38. PAINT TOUCH UP ON REWORK AREA PER SRM51-21-01 V.2R.38. 2 L 7 3 4F RT A22WE 2007080300076 20070803 00076 WP 2007 8 3 G41A2007002 2 20070726 A 7200 UNKNOWN LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP NR 2 ENGINE UNKNOWN E G41A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 01 46MF 377 WAS ON AN AIR AMBULANCE TRIP FROM ABQ TO LAS WHEN ON ROLL OUT THE CAPTAIN NOTICED THE NR 2 ENGINE N1 INDICATION WAS 4 PE RCENT LOWER THAN THE NR 1 ENGINE INDICATION. THE CREW REPORTED THE SITUATION AND WERE INSTRUCTED TO CHANGE AIRCRAFT. O N THE MORNING OF THE 27TH THE AIRCRAFT WAS RUN UP FOR MAX POWER CHECK AND THE PROBLEM COULD NOT BE DUPLICATED. THE FUEL COMPUTERS (DEECS) WERE DOWNLOADED ON THE 27TH AND THE INFO FORWARDED TO REPAIR STATION FOR EVALUATION. THE AIRCRAFT WI LL BE CONSIDERED OUT OF SERVICE UNTIL CONTACTED BY REPAIR STATION. 2 L 7 2 4F 4 F A10CE E6WE 2007080300078 20070803 00078 EA 2007 8 3 QXEA200701196 1 20070709 A 3240 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA BRAKE OVERHEAT UNKNOWN A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 609QX 10031 YYC - ON CLIMB RECEIVED A BRAKE OVERHEAT MESSAGE. CLEARED THE WARNING BY CHECKLIST. MAINTENANCE INSPECTED THE BRAKES AN D SYSTEM WITH NO DEFECTS. PERFORMED A OPERATIONAL CHECK IAW TASK 32-46-00-720-801-A01. CHECKS GOOD WITH NO DEFECTS NOT ED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007080300082 20070803 00082 2007 8 3 HALA0700305 4 20070726 A 2310 9640452012 TRANSCEIVER BOEING 767 76733A 1385209 NM NR 2 HF SYSTEM INOPERATIVE A HALA O OTHER O OTHER CR CRUISE 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM, NR 2 HF INOP. NO TRANSMIT, RECEIVE, SIDETONE, DATALINK. REMOVED AND REPLACED NR 2 HF XCVR. GND CHK OK PER AMM 23-11-03. 2 L 7 2 4F RT A1NM 2007080300086 20070803 00086 NM 2007 8 3 AWXA200700935 1 20070706 A 5510 183N13055 STRUCTURE BOEING 757 757225 1384959 NM ZONE 300 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - NR 5956477, CORROSION ON THE LEFT HORIZONTAL TRAILING EDGE WEB UPPER CHORD, STABILIZER STATION 318.9. REPLACED THE LEFT HORIZONTAL TRAILING EDGE WEB UPPER CHORD, STABILIZER STATION 318.9 IAW B757-200 SRM 5 1-40-02. 2 L 7 2 4F RT A2NM 2007080300093 20070803 00093 EA 2007 8 3 QXEA200701194 1 20070723 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002C10 1390015 EA LT MLG OUT OF ADJUST A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 602QX 10010 PDX - FLIGHT 2506 ON TAKEOFF, DOWNLOCK OVERRIDE REQUIRED TO RETRACT GEAR. RECEIVED A GEAR DISAGREE MESSAGE AND GEAR DID NOT RETRACT. RECEIVED A PROX SYSTEM 1 FAULT. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANC E ADJUSTED THE MAIN GEAR PROX SENSORS FOR THE LEFT GEAR IAW 32-61-05-820-803-A01. CHECKS GOOD. AIRCRAFT RETURNED TO SE RVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007080300097 20070803 00097 NM 2007 8 3 DHL2007784530 1 20070710 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 MAIN CARGO GOUGES AND CORROSION ON SEAT TRACK LBL 24, BS 480 TO BS 690, WL 208.5 ON ENTIRE TRACK. REMOVED FLOORBOARDS A T MAIN CABIN ROW B AND C, STA 480 TO 720C AND SEAT TRACK OUT OF LIMITS STA 740 TO BS 720B PLUS 10 IAW B727 SRM 51-30-2. FABRICATED THREE EACH SEAT TRACKS FROM P/N BAC1520-792-7178T6511, DIM 110.50, 100 AND 79.50 LONG, TWO EACH SPLICES, FOU R EACH ANGLES FROM BAC 1503-100122-7178T6, DIM 12.50 BY 2.50 AND TWO EACH STRAPS FROM 7075T6, .250, DIM. 7.50 BY 2 IAW B 727 SRM 53-10-5, FIG 5. TREATED, PRIMED AND INSTALLED SEAT TRACK IAW B727 SRM 51-10-2 AND 51-30-2. INSTALLED FLOORBOAR DS IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007080300098 20070803 00098 NM 2007 8 3 DHL2007784528 1 20070708 A 5310 MS20001167200 DOOR FRAME BOEING 727 727227 1384078 NM ZONE 200 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 MCD HINGE AFT SEGMENT (FUSELAGE SIDE) HAC ONE LOBE CRACKED STA 620, WL 291, LBL 29. REMOVED DAMAGED MCD AFT HINGE SEGME NT IAW B727 SRM 51-30-2. DRILLED UP NEW HINGE SEGMENT PARTS IAW B727 SRM 51-30-5 AND AEI AMM CH. 52, FIG 5210, P/N MS20 001-16-7200. TREATED, PRIMED PARTS, AREA AND INSTALLED REPAIR PARTS IAW B727 SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 2007080300100 20070803 00100 NM 2007 8 3 QXEA200701227 1 20070730 A 7930 CONNECTOR BOMBDR DHC8 DHC8402 1390042 NM NR 2 ENGINE OIL DIRTY A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 407QX 4049 SEA FLIGHT NR 2458: NR 2 ENGINE OIL GAUGE NOT REGISTERING. AIRCRAFT WAS DIVERTED. MAINTENANCE CLEANED AND REINSTALLED CONNECTOR P16 ON MOT ITT SENSOR IAW Q400 AMM 70-00-15-400-801 NR 2 ENGINE. GROUND RAN NR 2 ENGINE. NR 2 OIL TEMP REGIS TERING WITHIN NORMAL LIMITS. OPS CHECK GOOD. ITT READS NORMAL (WITHIN LIMITS). NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007080300102 20070803 00102 NM 2007 8 3 DHL2007784532 1 20070710 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM BS 540-689 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 MAIN CARGO NICKS AND GOUGES ON SEAT TRACK BOTTOM SURFACE, BS 540 TO BS 689, LBL 45, WL 208.5 AS MARKED. REMOVED SEAT TR ACK STA 550 TO BS 690 IAW B727 SRM 51-30-2. FABRICATED NEW SEAT TRACK FROM P/N BAC1520-792-7170T6511, DIM 11’8 AND TWO EACH ANGLES FROM BAC 1503-100122-7178T6511, DIM 15 AND 12 AND ONE STRAP FROM 7075T6, .250, DIM. 8 BY 2 IAW B727 SRM 53-1 0-5, FIG 1. TREATED, PRIMED AND INSTALLED SEAT TRACK IAW B727 SRM 51-10-2 AND 53-10-5, FIG 1. 2 L 7 3 4F A3WE 2007080300115 20070803 00115 EU 2007 8 3 07FDEA02647 1 20070728 A 5311 A53773644201 FRAME AIRBUS 310 A310203 3930313 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 FRAME FITTING C36 (STA 1976) IS CRACKED AT RBL 60 (-Y 15200) FWD PIT FLOOR LEVEL. [08-09-07] REMOVED AND REPLACED FRAM E FITTING IAW A310-200 SRM 51-40-21 PAR 6. 2 L 7 2 4F RT A35EU 2007080600007 20070806 00007 NM 2007 8 6 2007UALA02746 1 20070719 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 648UA 25285 EEL INOP IN AISLE AFT OF MED 1L. REPAIRED FLOOR-MOUNTED EEL PER MM 33-51-10. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080600008 20070806 00008 2007 8 6 2007UALA02747 4 20070719 A 2397 CONNECTOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE ENTERTAIN SYS MISPINNED A UALA K NONE W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 218UA 30222 FWD BUSINESS CLASS CABIN HAS STRONG ELECTRICAL ODOR. [08-14-07] SUSPECT ONE OF ELEC UNIT UNDER SEAT ROW 9FED CREATED THE ODOR. DEACTIVATED ALL ELEC. UNIT AT THIS SEAT ROW. RECONNECTED VIDEO CONNECTIONS UNDER SEATS 8 DE&F, 9 DE&F, OPS CH ECKED SYSTEM FOR ABOUT 4 HRS. NO NOTICEABLE ELECTRICAL ODOR NOTED, EVEN IN CARGO COMPT. AIRPLANE RETURNED TO SERVICE. S USPECT CONNECTORS WERE SOURCE OF HIGH CURRENT/ ELECTRICAL ODOR. RECONNECTING ELIMINATED ODOR SOURCE AND NO REPEAT IN 21 DAYS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007080600010 20070806 00010 NM 2007 8 6 2007UALA02751 1 20070719 A 2611 SMOKE DETECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT LAVATORY FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 AFT LAVATORY SMOKE DETECTOR ALARM ON BEFORE BOARDING. [08-17-07] REPLACED SMOKE DETECTOR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007080600015 20070806 00015 EU 2007 8 6 2007UALA02756 1 20070719 A 3251 STEERING SYS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG INOPERATIVE A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 445UA 826 LOST NOSE WHEEL STEERING. REPLACED BOTH NWS GEARBOXES, TILLER AND SERVO CONTROL. NO REPEATS SINCE 7/19/07. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080600016 20070806 00016 EU 2007 8 6 2007UALA02757 1 20070720 A 2820 FUEL FEED AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE INOPERATIVE A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 413UA 470 AUTO FUEL FEED SYSTEM INOPERATIVE. FAULTY LOW LEVEL FUEL SENSORS IN RT WING TANK CAUSING LOGIC FAULT IN FQIC. REPLACE D TWO LOW LEVEL SENSORS IN RT WING TANK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080600018 20070806 00018 NM 2007 8 6 2007UALA02760 1 20070720 A 2910 HYDRAULIC SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 829UA 1211 FLIGHT DIVERTED DUE TO LOSS OF BLUE HYDRAULIC SYSTEM. LOSS OF HYDRAULIC FLUID DUE TO LEAK AT MOUNTING POINT FLANGE OF THE ELECTRIC HYD PUMP. REPLACED BLUE ELECTRIC HYDRAULIC PUMP, SERVICED SYSTEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080600019 20070806 00019 EU 2007 8 6 2007UALA02761 1 20070721 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 456UA 1128 EMERGENCY LIGHT TEST FAILED EPSU UNIT AFT LEFT. REPAIRED SHORTED WIRES IN EEL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080600020 20070806 00020 2007 8 6 2007UALA02762 4 20070722 A 2565 DIAPHRAGM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R1 DOOR SLIDE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 462UA 1272 DOOR 1L SLIDE BOTTLE PRESSURE LOW. LOSS OF PRESSURE DUE TO DIAPHRAGM RUPTURED AND STRIKER PIN BROKEN. REPLACED DIAPH RAGM AND STRIKER PIN AND RECHARGED BOTTLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080600021 20070806 00021 EU 2007 8 6 2007UALA02763 1 20070722 A 3350 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 447UA 836 EMERGENCY LIGHT TEST FAULTED LEFT EMERGENCY LIGHT. FAULTY BATTERY PACK. REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080600022 20070806 00022 EU 2007 8 6 2007UALA02764 1 20070720 A 3510 OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CAPTAIN'S NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 479UA 1538 CAPTS O2 MASK WILL NOT TEST. FOUND FAULTY MASK & LEAKING HARNESS. REPLACED MASK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080600024 20070806 00024 NM 2007 8 6 2007UALA02773 1 20070721 A 3397 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 550UA 25398 FLOOR MOUNTED EMERGENCY ESCAPE PATH LIGHT INOP AT AFT LAV. RESECURED CONNECTOR FROM LIGHT STRIP TO POWER CABLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080600025 20070806 00025 NM 2007 8 6 2007UALA02775 1 20070721 A 3897 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE AFT LAVATORY BURNED A UALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 29 554UA 26644 ACFT RTBL WITH DOOR 3L AFT LAVATORY BURNING ODOR DUE TO A BURNED WIRE. 09-14-07 ON TROUBLESHOOTING FOUND TOILET TANK FILL LINE SHUTOFF VALVE CONNECTOR HAS BURNED WIRES. CAPPED WIRES & TIED BACK. CONNECTOR SECURED AT AREA FOR RE-USE. L AVATORY TO SERVICE FROM INSIDE OR MANUALLY OPEN SHUTOFF VALVE FOR SERVICING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080600026 20070806 00026 NM 2007 8 6 2007UALA02776 1 20070721 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 644UA 25094 FLOOR EEL STRIP AT DOOR 1L CLOSET HAS BEEN DAMAGED AND IS INOP. [08-14-07] REPAIRED EEL STRIP AT DOOR 1L CLOSET. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080600027 20070806 00027 NM 2007 8 6 2007UALA02777 1 20070722 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 648UA 25285 THE 27A EMERGENCY FLOOR LIGHTS INOPERATIVE. [08-14-07] FOUND CUT IN CABLE ASSY. SPLICED CUT STRIP. TESTS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080600035 20070806 00035 NM 2007 8 6 2007UALA02787 1 20070720 A 5240 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR LWR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 L-2 DOOR LWR GATE HAS CORROSION AND FOUND MISDRILLED HOLES AT RUB STRIP AND EDGES. REPLACED LOWER DOOR GATE 2 L 7 2 4F 4 F RT A2NM E17NE 2007080600036 20070806 00036 NM 2007 8 6 2007UALA02795 1 20070720 A 2612 CONTROL MODULE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU APU MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 RIGHT FIRE TEST SQUIB LIGHT INOP IN BOTH NR 1 AND 2 POSITION. FIRE PANEL SQUIB TEST SHOWS L & APU WHEN IN NR 2 POSITION . SHOWS APU ONLY IN NR 1 POSITION. REPLACED ENG AND APU FIRE CONTROL MODULE, 2 L 7 2 4F 4 F RT A16WE E21EU 2007080600037 20070806 00037 NM 2007 8 6 2007UALA02796 1 20070721 A 7931 TRANSMITTER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE ENGINE OIL MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 675UA 29243 L ENG OIL PRESSURE IS RED 0. [08-07-07] REPLACED OIL PRESSURE TRANSMITTER PER AMM 79-32-01. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080600042 20070806 00042 EU 2007 8 6 YENA2007065 1 20070721 A 2120 17055785401 DUCT EMB ERJ190 ERJ190100IGW 3260408 EU RT A/C PACK TORN A YENA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 15 206JB 19000025 FLT 585, HPN TO FLL DIVERTED TO JFK, DURING CLIMB THRU 17,000 FT, FLT ATTENNDANT REPORTED SQUEALING NOISE NEAR R1 DOOR T HEN CLIMBING THRU 320, CAB ALT SHOWED 8200" (EICAS INDICATION TURNED AMBER) AND WAS STILL CLIMBING AT 400FT/MIN. DESCEN DED TO 17,000FT AND CABIN ALT RETURNED TO NORMAL RANGE. PERFORMED VISUAL INSPECTION OF THE R1 DOOR. NO DEFECT NOTED. INSPECTED LT & RT PACK DUCTS. FOUND RT PACK OUTLET DUCT BELLOW TORN. REMOVED AND REPLACED RT PACK OUTLET DUCT BELLOW. LEAK CHECK GOOD. REF AMM 21-51-21. PERFORMED CABIN PRESSURIZATION LEAKAGE FUNCTIONAL TEST. NO DEFECT NOTED. OPS CHE CK GOOD REF AMM 21-31-00. 2 L 7 2 4F RT A57NM 2007080600044 20070806 00044 NM 2007 8 6 TIPR200736003 1 20070724 A 5330 SKIN BOEING 767 767222 1385122 NM BS 1320 CORRODED B K NONE O OTHER IN INSP/MAINT 1 WP 29 609UA 21870 AFT PIT STA 1320 BETWEEN STRINGER 36L TO STRINGER 37L SKIN HAS CORROSION. REMOVED CORROSION IN ACCORDANCE WITH B767MM51 -00-53. ORIGINAL MATERIAL THICKNESS .056 MATERIAL REMOVED .019 MATERIAL REMAINING .037. FOUND TO BE BEYOND LIMITS IN A CCORDANCE WITH B767 SRM 53-00-01. FABRICATED AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH B767 SRM 53-00-01. REFERE NCE SERVICE ORDER 599125 OPERATION 25254. 2 L 7 2 4F RT A1NM 2007080600046 20070806 00046 EU 2007 8 6 TRAX200701030 1 20070720 A 3350 SIGN AEROSP ATR72 ATR72 EU EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 AFT LOWER EMERGENCY EXIT SIGN BY PAX DOOR INOP. 2 H 7 2 4T RT 2007080600047 20070806 00047 EA 2007 8 6 TRAX200701031 1 20070720 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 926EV 7843 SERVICE DOOR WILL NOT OPEN FROM THE OUTSIDE. 2 L 7 2 4F RT A21EA 2007080600052 20070806 00052 NM 2007 8 6 USAA070580 1 20070724 A 5343 BEAM BOEING 737 7373B7 1384580 NM BS 259.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 23700 STA 259.5 AT NOSE W/W CEILING WL 192.5, BL 0, RADIUS OF NOSE GEAR ACT BEAM. REPLACED GUSSET PER SRM 51-10-02, DEFECT SI ZE: .75 INCH. 2 L 7 2 4F RT A16WE 2007080600056 20070806 00056 EU 2007 8 6 USAA070576 1 20070724 A 5315 D53472075001 FLOORBEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 183UW 1539 DOOR R4 SILL BEAM FWD END ABOVE FRAME 66; CORRODED TASK JA-260-53500. CUT OUT AREA, FAB'D & INSTALLED FILLER & SPLICE A NGLES PER SRM 53-41-14, DEFECT SIZE: .5 X .5 INCH. 2 L 7 2 4F RT A28NM 2007080600058 20070806 00058 WP 2007 8 6 ASAA0781873 1 20070723 A 5230 59101573 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 MID CARGO DOOR SKIN IS DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FAIRING AND DOUBLER PER SRM 52-05. 2 L 7 2 4F RT A6WE 2007080600059 20070806 00059 WP 2007 8 6 ASAA0781874 1 20070723 A 5321 995252179 FLOOR PANEL DOUG DC9 DC983 3022083 WP BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 CABIN FLOOR PANEL HAS BROKEN END. PREPARED DAMAGED AREA. RE-BONDED PER MM 25-00-00. 2 L 7 2 4F RT A6WE 2007080600063 20070806 00063 SO 2007 8 6 C2XA07SH042 1 20070715 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16541 145542 SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 23-25. MAINTENANCE REMOVED THE DAMAG ED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-00-10, ITEM 4, FIG 203 AND EMB 145 CPM 51-21-06. THE AIRC RAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007080600065 20070806 00065 SO 2007 8 6 C2XA07IA171 1 20070720 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO CABIN ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 13123 145688 IAH - FLIGHT 2901, THE CREW REPORTED A ODOR OF FUEL AND/OR BURNED RUBBER DURING AND IMMEDIATELY AFTER TAKEOFF. THE AIRC RAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND PERFORMED HIGH POWER EN GINE RUNS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007080600066 20070806 00066 2007 8 6 C2XA07IA172 4 20070723 A 3100 14530503403 MODULE EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL COCKPIT INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14153 10401 10401 145761 IAH - DURING MAINTENANCE INSPECTION, IT WAS NOTED THAT THE TAKEOFF DATA HAD UNCONTROLLABLE COMMANDS. MAINTENANCE REMOVE D AND REPLACED THE POWER PLANT CONTROL MODULE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. 2 L 7 2 4F 4 F RT TE6CH 2007080600067 20070806 00067 SO 2007 8 6 C2XA07IA169 1 20070709 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13975 56 56 145163 BAN - DURING MAINTENANCE INSPECTION THE NUMBER 4 EMERGENCY LIGHT BATTERY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS A PPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007080600070 20070806 00070 NM 2007 8 6 SWAA073625 1 20070724 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM BS 380 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080600073 20070806 00073 NM 2007 8 6 SWAA073627 1 20070724 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080600074 20070806 00074 NM 2007 8 6 SWAA073640 1 20070724 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM BS 520 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080600075 20070806 00075 NM 2007 8 6 SWAA073635 1 20070724 A 5311 6546534 FRAME BOEING 737 737317 138447P NM BS 520 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080600076 20070806 00076 NM 2007 8 6 SWAA073644 1 20070724 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM BS 616 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, STR 18L. REPAIRED FRAME PER SB. 2 L 7 2 4F RT A16WE 2007080600079 20070806 00079 NM 2007 8 6 SWAA073636 1 20070724 A 5311 6546552 FRAME BOEING 737 737317 138447P NM BS 827 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080600082 20070806 00082 NM 2007 8 6 SWAA073643 1 20070724 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM BS 500C S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080600083 20070806 00083 NM 2007 8 6 SWAA073611 1 20070722 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM L2 DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 L2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007080600084 20070806 00084 NM 2007 8 6 SWAA073632 1 20070724 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 706 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080600088 20070806 00088 NM 2007 8 6 SWAA073628 1 20070724 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727D S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080600090 20070806 00090 2007 8 6 SWAA073634 4 20070724 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED 10Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2007080600091 20070806 00091 NM 2007 8 6 SWAA073615 1 20070723 A 3350 8200037741 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 247WN 32508 DURING SCHEDULED MV3 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007080600092 20070806 00092 2007 8 6 SWAA073621 4 20070724 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007080600095 20070806 00095 2007 8 6 SWAA073622 4 20070724 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007080600096 20070806 00096 2007 8 6 SWAA073610 4 20070722 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007080600098 20070806 00098 WP 2007 8 6 ASAA0781890 1 20070725 A 5311 99236303 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 FRAME ON FRONT LEFTHAND SIDE OF CANT CRACKED AT RADIUS. REPAIRED FRAME PER SRM 51-30-5. 2 L 7 2 4F RT A6WE 2007080600099 20070806 00099 WP 2007 8 6 ASAA0781891 1 20070725 A 5311 9911842111 FRAME DOUG DC9 DC983 3022083 WP FUSLEAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 CANT REPAIR (WEB STIFFENER) CRACKED AS FASTENER HOLES. REPLACED WEB STIFFENER PER SRM 51-30-5. 2 L 7 2 4F RT A6WE 2007080600101 20070806 00101 WP 2007 8 6 ASAA0781893 1 20070725 A 5320 991184237 WEB DOUG DC9 DC983 3022083 WP CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 WEB IS CRACKED AT FASTENER HOLE. INSTALLED REPLACEMENT FRAME SECTION AND REPAIR DOUBLERS PER SRM 53 01. 2 L 7 2 4F RT A6WE 2007080600102 20070806 00102 WP 2007 8 6 ASAA0781896 1 20070725 A 5320 9930601285 CUSP WEB DOUG DC9 DC983 3022083 WP CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 CUSP WEB CRACKED. REMOVED DAMAGED SECTION AND INSTALLED FILLER AND DOUBLER PER SRM 51-70-4. 2 L 7 2 4F RT A6WE 2007080600103 20070806 00103 WP 2007 8 6 ASAA0781879 1 20070724 A 5321 99365841 FLOOR PANEL DOUG DC9 DC983 3022083 WP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 CABIN FLOORBOARD CORRODED AT FASTENER HOLES. REPLACED FLOOR PANEL PER SRM 41-30 AND MM 53-20-01. 2 L 7 2 4F RT A6WE 2007080600105 20070806 00105 WP 2007 8 6 ASAA0781885 1 20070724 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 607 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 RADIO ALTIMETER ANTENNA CUTOUT AT FLANGE IS CORRODED. REMOVED DAMAGED PIECE. INSTALLED DOUBLER PER SRM 53-04, 51-30-02 AND 51-30-05. 2 L 7 2 4F RT A6WE 2007080600109 20070806 00109 WP 2007 8 6 ASAA0781894 1 20070725 A 5330 593666751 SKIN DOUG DC9 DC983 3022083 WP BS 1190-1210 BULGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 FUSELAGE SKIN HAS BULGES. REPLACED PREVIOUSLY INSTALLED EXTERNAL DOUBLER PER ASA EA 5330 02221. 2 L 7 2 4F RT A6WE 2007080600115 20070806 00115 WP 2007 8 6 ASAA0781884 1 20070724 A 5753 5930495507 VANE DOUG DC9 DC983 3022083 WP TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 LEFTHAND INBOARD FLAP OUTBOARD VANE HAS DENTS ON LOWER SURFACE. REMOVED DAMAGED SECTION. INSTALLED REPAIR SKIN AND DOU BLER PER SRM 51-70-2. 2 L 7 2 4F RT A6WE 2007080600116 20070806 00116 NM 2007 8 6 ZZDA2007211 1 20070605 A 5313 LONGERON BOEING 717 717200 1383700 NM BS 889-1053 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION SPOTS ON AFT CARGO COMPARTMENT ON LONGERON 28L BETWEEN BS 889 AND BS 1053. INSTALLED LONGERON 28L AT AFT CARG O COMPARTMENT BETWEEN STA 889 AND STA 1053 AS PER B717 SRM 51-41-02 AND SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007080600119 20070806 00119 NM 2007 8 6 ZZDA2007214 1 20070605 A 5313 LONGERON BOEING 717 717200 1383700 NM BS 898.5-1053 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION SPOTS ON AFT CARGO COMPARTMENT LONGERON 29L BETWEEN BS 898.5 AND BS 1053. INSTALLED LONGERON 29L AT AFT CARGO COMPARTMENT BETWEEN STA 898.5 AND STA 1053 AS PER B717 SRM 51-41-02. 2 L 7 2 4F TR A6WE 2007080600120 20070806 00120 NM 2007 8 6 ZZDA2007215 1 20070605 A 5313 LONGERON BOEING 717 717200 1383700 NM STA 898.5 - 1053 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT LONGERON 30 BETWEEN BS 898.5 AND BS 1053. INSTALLED LONGERON 30L AT AFT CARGO COMPAR TMENT BETWEEN STA 898.5 AND STA 1053 AS PER B717 SRM 51-41-02. 2 L 7 2 4F TR A6WE 2007080600126 20070806 00126 NM 2007 8 6 ZZDA2007221 1 20070605 A 5313 LONGERON BOEING 717 717200 1383700 NM BS 1053 L27L CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT (WASTE TANK AREA) AT LONGERON 27L END TIE FITTING. INSTALLED NEW END TIE FITTING LON GERON 27L AT AFT CARGO COMPARTMENT STA 1053 IAW B717 SRM 51-41-02 AND SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007080600130 20070806 00130 NM 2007 8 6 ABXA070246 1 20070708 A 5330 141T3330 SKIN BOEING 767 767200 1385120 NM L1 DOOR CUTOUT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AX 23432 L1 DOOR CUTOUT, LOWER AFT CORNER CRACKED. REPAIRED AREA IAW REA B653-56023-MR. 2 L 7 2 4F RT A1NM 2007080600131 20070806 00131 NM 2007 8 6 ABXA070248 1 20070706 A 5510 180T00093 PIN BOEING 767 767200 1385120 NM HORIZONTAL STAB DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AX 23432 RIGHT OUTER PIVET PIN OF HORIZONTAL STABILIZER SHOWS INDICATION OF LINEAR DEFECT ON INNER SURFACE. REMOVED AND REPLACED RIGHT OUTER PIVOT PIN ON JOB CARD 7302001 IAW B767 SRM. 2 L 7 2 4F RT A1NM 2007080600132 20070806 00132 WP 2007 8 6 ABXA070244 1 20070705 A 5312 59101303 BULKHEAD DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 AFT PRESSURE BULKHEAD LEFT DOOR CORNER SKIN HAD RADIAL CRACK OF UNKNOWN LENGTH IN LOWER INBOARD PORTION ONLY. NO PREVIO US REPAIRS INSTALLED. REPAIRED LEFT LOWER CORNER DOOR OF AFT PRESSURE BULKHEAD IAW DWG J060088-525. 2 L 7 2 4F A6WE 2007080600135 20070806 00135 CE 2007 8 6 MAC070705 1 20070723 A 2120 UNKNOWN CESSNA 208 208 2073702 CE COCKPIT SMOKE A MTNA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 33 801FE 1855 20800009 SMELLED SMOKE FROM RADIO, COCKPIT, RADIO HOT TO TOUCH. 1 H 7 1 3T NT A37CE 2007080600137 20070806 00137 2007 8 6 SWAA073670 4 20070725 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM L1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM. 2 L 7 2 4F RT A16WE 2007080600139 20070806 00139 NM 2007 8 6 SWAA073649 1 20070725 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM BS 727D S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080600140 20070806 00140 NM 2007 8 6 SWAA073662 1 20070725 A 5340 65C27314 STRINGER CLIP BOEING 737 7373K2 13844BA NM BS 927 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007080600145 20070806 00145 NM 2007 8 6 SWAA073667 1 20070725 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 540 S27R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CORRODED AT BS 540, STR 27R. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 2007080600148 20070806 00148 NM 2007 8 6 SWAA073657 1 20070725 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 787SA 29812 DURING SCHEDULED MV2 CHECK, FOUND LEFT MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007080600150 20070806 00150 NM 2007 8 6 KCSA071256 1 20070726 A 5311 BULKHEAD BOEING 747 7472B4B 138481B NM BS 1475 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA-1475 CENTER BULKHEAD AFT CORNER HAS CORROSION. 2 L 7 4 4F RT A20WE 2007080600152 20070806 00152 NM 2007 8 6 KCSA071258 1 20070726 A 5414 SKIN BOEING 747 7472B4B 138481B NM NR 4 NACELLE CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NR 4 PYLON STA 180-265 AFT LOWER SPAR O/B SKIRT CHAFED AT KNIFE EDGE. 2 L 7 4 4F RT A20WE 2007080600156 20070806 00156 NM 2007 8 6 CALA0700376 1 20070726 A 5311 65C352436 FRAME BOEING 737 7373T0 1384582 NM BS 847 S26R CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND FRAME CORRODED AT STA 847, S25R TO S26R. THE FRAME WAS REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007080600158 20070806 00158 NM 2007 8 6 2007UALA02784 1 20070720 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU ROW 21 UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 307UA 23668 EMERGENCY LIGHTING STRIP ON ROW 21 IS OFF. SECURED EEL LIGHTING STRIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007080600160 20070806 00160 NM 2007 8 6 2007UALA02788 1 20070722 A 3397 794640 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EMERGENCY LIGHT ROWS 36 ABC & 53 HJK ARE INOPERATIVE. RESECURED EMERGENCY LIGHT CONNECTOR. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080600162 20070806 00162 NM 2007 8 6 2007UALA02790 1 20070722 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EMERGENCY SILL LIGHT DOOR 5 RT INOP. RELAMPED SILL LIGHT. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080600163 20070806 00163 NM 2007 8 6 2007UALA02791 1 20070723 A 3397 794640 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 WALL EEL INOP: AFT GALLEY FWD WALL, LT WALL & DOOR 5L CROSS AISLE. *S/D* REPLACED FEEDER CABLE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080600164 20070806 00164 NM 2007 8 6 2007UALA02792 1 20070723 A 3350 582240 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 DOOR 4L EXIT EEL SIGN INOP FWD OF DOOR. REPLACED POWER SUPPLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100196 20070731 00196 NM 2007 7 31 2007UALA02282 1 20070628 A 2121 6054578 FAN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY FAULTY A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 662UA 27159 AFT EQ EXH FAN 2 STATUS MSG AFTER AIRCRAFT PWR UP. SOME HOT SMELLING ODOR. REPLACED EXHAUST FAN PER MM 21-26-01. ODOR GONE AND OP CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007073100197 20070731 00197 NM 2007 7 31 2007UALA02283 1 20070628 A 2120 212T311813 DUCT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CARGO BAY CRACKED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 673UA 29241 EXTREMELY HOT AIR AT ROW 30. EVERYWHERE ELSE IN CABIN IS COOL. FLOW STOPPED WHEN AFT CARGO HEAT TURNED OFF, INOPED AFT CARGO HEAT SYS. REACTIVATED CARGO HEAT SYS VLV NOT THE PROBLEM. FOUND CRACKED DISTRIBUTION DUCT. REPLACED PNEUMATIC DUCT IN AFT PIT LT SIDE. LEAKED CHECKED SATISFACTORILY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007073100201 20070731 00201 NM 2007 7 31 KCSA071248 1 20070724 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 UPPER DECK SEAT TRACK CORRODED AT LBL-65, BS 519. 2 L 7 4 4F RT A20WE 2007073100203 20070731 00203 NM 2007 7 31 KCSA071252 1 20070725 A 5411 FRAME BOEING 747 7472B4B 138481B NM NR 4 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NR 4 PYLON NAC STA 221 BULKHEAD I/B FRAME CRACKED. 2 L 7 4 4F RT A20WE 2007073100205 20070731 00205 NM 2007 7 31 KCSA071254 1 20070725 A 5315 FLOORBEAM BOEING 747 7472B4B 138481B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 MAIN DECK FLOORBEAM WEB DAMAGED AT BS 460, LBL-99. 2 L 7 4 4F RT A20WE 2007073100207 20070731 00207 EA 2007 7 31 COMA0770040 1 20070718 A 3252 498003 SHIMMY DAMPENER CNDAIR CL600 CL6002C10 1390015 EA RT MLG WORN A COMA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 378CA 8326 10097 MLG SHIMMY ON TAKEOFF AND GEAR RETRACTION. AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED RIGHT MLG SHIMMY DAMPENER. 2 L 7 2 4F RT A21EA 2007073100213 20070731 00213 EA 2007 7 31 TRAX200701033 1 20070721 A 5320 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 754EV 10173 RIGHT FS 280 CROSSBEAM CRACKED ON UPPER FLANGE O/B OF RBL 9.0. [07-31-07] REPAIRED IAW MODSUM IS67053110026. 2 L 7 2 4F RT A21EA 2007073100220 20070731 00220 EA 2007 7 31 TRAX200701040 1 20070721 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA RT WING INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 882AS 7503 RIGHT WING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007073100232 20070731 00232 NM 2007 7 31 UPS07M50220 1 20070521 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C CTR CARGO STA 1701 LONGERON L43 FOUND WITH CORROSION AS MARKED. LONG STA 1091-1751 REMOVED & TRIMMED OFF PER SRM 53-10-01 V1 R38. HFEC INSP CARRIED OUT PER DAC NDTSPM R13 FOUND NO CRACK EVIDENT. REPAIR LONG & SPLICE FAB & FASTENER HOLES PICK UP PER SRM 51-31-01V2 R38 & SRM 53-10-00 V1 R38. REPAIR LONG & SPLICE REPROTECTED & PAINT TOUCHE D UP PER SRM 51-21-01 V2 R38. REP LONG & SPLICE INSTALLED PER SRM 51-31-01 V2 R38. 2 L 7 3 4F RT A22WE 2007073100236 20070731 00236 NM 2007 7 31 UPS07M50229 1 20070525 A 5720 STRUCTURE DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C RIGHT FIXED L/E STRUCTURE FOUND CRACKS ON UPPER DOOR CUTOUT AREA NR 3 SLAT TELESCOPIC DUCT VICINITY. DAMAGE AREA TRIM OFF PER ADV EN1356-07. HFEC INSP CARRIED OUT PER DAC NDTSPM R13 06-10-01.001 FOUND NO CRACK EVIDENT. REPAIR PARTS FAB, HOLES PICK UP & PROTECTED PER ADV EN1356-07. RIGHT WING NR 3 SLAT INSTALLED PER AMM 27-80-30 R55. RI GHT WING NR 3 SLAT OPERATIONAL TEST CARRIED OUT, REFER TO TC 8313. 2 L 7 3 4F RT A22WE 2007073100244 20070731 00244 NM 2007 7 31 SWAA073609 1 20070721 A 3350 311500 LENS BOEING 737 7373G7 1384595 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED SERVICE CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 2 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007073100246 20070731 00246 2007 7 31 SWAA073616 4 20070723 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 737JW 27869 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007080100019 20070801 00019 EA 2007 8 1 MASA200700232 1 20070408 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27173 7173 FWD PRESSURE BULKHEAD CRACKED. REPAIRED FWD PRESSURE BULKHEAD. 2 L 7 2 4F RT A21EA 2007080100020 20070801 00020 EA 2007 8 1 MASA200700296 1 20070601 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA EXTINGUISHER LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75998 7336 ASH 7214 IAD - FIRE EXT BRACKET LOOSE. MX RESECURED BRACKET. 2 L 7 2 4F RT A21EA 2007080100037 20070801 00037 EA 2007 8 1 MASA200700072 1 20070202 A 5241 DOOR CNDAIR CL600 CL6002D24 1390016 EA GALLEY LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 924FJ 15024 ASH 2885 PHX - CREW REPORTED THE GALLEY DOOR HARD TO OPEN. MX LUBED GALLEY SERVICE DOOR AND IT OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2007080100043 20070801 00043 EA 2007 8 1 MASA200700238 1 20070424 A 5420 ANGLE CNDAIR CL600 CL6002B19 1900309 EA NACELLE DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17337 7337 LT PYLON WAS DAMAGED BY ENGINE FAILURE. REMOVED AND REPLACED PYLON ANGLES 601-37051-3 AND 601-37051-7. 2 L 7 2 4F RT A21EA 2007080100053 20070801 00053 EA 2007 8 1 MASA200700251 1 20070508 A 5210 COVER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MISALIGNED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75999 7471 ASH 7227 ORD - PAX DOOR WOULD NOT OPEN. CREW REPORTED THE DOOR WOULD OPEN ABOUT 8 INCHES AND STOP. MX FOUND THE DOOR A SSIST SWITCH COVER WAS MISALIGNED AND APPLYING PRESSURE TO THE SWITCH. MX REALIGNED THE COVER TO THE PROPER POSITION AN D THE DOOR ASSIST SYSTEM, OP CHECKED GOOD. 2 L 7 2 4F RT A21EA 2007080100058 20070801 00058 EA 2007 8 1 MASA200700074 1 20070202 A 1100 PLACARD CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 906FJ 15006 ASH 2670 CLT - EMERGENCY EXIT ARROWS ROW 16AC ARE COMING OFF. MX SECURED. 2 L 7 2 4F RT A21EA 2007080100085 20070801 00085 EA 2007 8 1 MASA200700190 1 20070407 A 7830 COWLING CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER DAMAGED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 77278 7278 ASH 2752 TUS - AIRCRAFT DIVERTED TO TUS EN ROUTE TO PHX FROM ELP. CREW REPORTED RT REVERSER UNLOCK CAUTION IN FLIGHT, A TTEMPTED TO STOW AND THEN SHUT DOWN THE ENGINE. DECLARED AN EMERGENCY. MX DEFERRED THE REVERSER AND FOUND 2 COWL FASTE NERS MISSING. MX REPLACED THE FASTENERS. 2 L 7 2 4F RT A21EA 2007080100087 20070801 00087 EA 2007 8 1 MASA200700181 1 20070402 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 571ML 7209 ASH 7366 PIT - FWD CEILING EMERGENCY LIGHT INOP. MX RELAMPED 2 L 7 2 4F RT A21EA 2007080100094 20070801 00094 EA 2007 8 1 MASA200700277 1 20070518 A 3520 DOOR CNDAIR CL600 CL6002D24 1390016 EA OXYGEN UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 914FJ 15014 ASH 2627 CLT - AFT LAV OXYGEN DOOR CAME OPEN. MX REPACKED AND SECURED. 2 L 7 2 4F RT A21EA 2007080100108 20070801 00108 EA 2007 8 1 MASA200700222 1 20070421 A 5210 ROD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR GATE DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 47239 7239 ASH 7379 IAD - AIRCRAFT RETURNED TO FIELD FOR PAX DOOR OUTER HANDLE CAUTION MESSAGE. MX REPLACED PAX DOOR PRESSURIZATIO N FLAPPER DOOR ROD. 2 L 7 2 4F RT A21EA 2007080100116 20070801 00116 2007 8 1 MASA200700246 2 20070504 A 7261 755469E IDG CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17175 18215 7175 ASH 7174 BHM - PILOT REPORTED A LT ENG OIL PRESS WARNING MESSAGE, PRESS HAD DROPPED TO 25PSI, PILOT SHUT DOWN THE NR 1 E NGINE AND AN EMERGENCY WAS DECLARED. MX REMOVED AND REPLACED IDG. 2 L 7 2 4F RT A21EA 2007080100117 20070801 00117 EA 2007 8 1 MASA200700133 1 20070303 A 2150 DRAIN LINE CNDAIR CL600 CL6002B19 1900309 EA LT A/C PACK TORN A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 655BR 7457 ASH 1017 HNL - PILOT REPORTED THE LEFT PACK OVERTEMP ACCOMPANIED BY SMOKE IN THE COCKPIT. DECLARED AN EMERGENCY AND RET URNED TO THE FIELD. MX FOUND A SECTION OF THE OB DRAIN LINE TORN AND REPLACED THE DRAIN LINE. ALSO, FOUND THE ACM NOT PROPERLY SERVICED AND SERVICED. OPS NORMAL. 2 L 7 2 4F RT A21EA 2007080100118 20070801 00118 EA 2007 8 1 MASA200700143 1 20070310 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA LEFT ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 37178 5997 7178 ASH 2802 PHX - STRONG BURNING SMELL FROM PACKS. MX T/S TO LT PACK. MX REMOVED AND REPLACED ACM. 2 L 7 2 4F RT A21EA 2007080100149 20070801 00149 EA 2007 8 1 MASA200700109 1 20070220 A 4920 APU CNDAIR CL600 CL6002B19 1900309 EA CONTAMINATED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 17175 7175 ASH 7108 BHM - CREW REPORTED A BURNED ODOR IN COCKPIT AFTER BLEED SOURCE WAS TRANSFERRED TO THE APU. MX INSPECTED AND F OUND GLYCOL RESIDUE IN SYSTEM. CLEARED SYSTEM OF GLYCOL, ODOR GONE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007080100162 20070801 00162 EA 2007 8 1 MASA200700067 1 20070201 A 2751 855D1009 SENSOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A MASA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 37218 15689 7218 ASH 2752 PHX.- CREW REPORTED DECLARING AN EMERGENCY DUE TO FLAPS FAIL CAUTION AT 2 DEGREES ON APPROACH. MX C/W PART A A ND B, MX REPLACED THE PDU AND RT BPSU. 2 L 7 2 4F RT A21EA 2007080100175 20070801 00175 EA 2007 8 1 MASA200700124 1 20070227 A 5220 DOOR CNDAIR CL600 CL6002D24 1390016 EA DOOR TRIM OBSTRUCTED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 924FJ 15024 ASH 2712 LAS - SERVICE DOOR WILL NOT SWING OPEN ALL THE WAY. MX REPOSIONED TRIM. 2 L 7 2 4F RT A21EA 2007080100176 20070801 00176 EA 2007 8 1 MASA200700235 1 20070421 A 5330 601R35004423 SKIN CNDAIR CL600 CL6002B19 1900309 EA FS 559-640 UNSERVICEABLE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17337 7337 FUSELAGE SKIN HAS SEVERE DISTORTIONS, PUNCTURES AND GOUGES FROM FS 559+112 TO FS 640 BETWEEN STRINGERS 6L TO 20L. REMOV ED AND REPLACED FUSELAGE SKIN. 2 L 7 2 4F RT A21EA 2007080100190 20070801 00190 EA 2007 8 1 MASA200700205 1 20070414 A 5270 SENSOR CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT MALFUNCTIONED A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 942LR 15042 ASH 2643 CLT - CAPTAIN REPORTED LT AFT OVERWING EMERGENCY EXIT INDICATES OPEN WHEN CLOSED. MX ADJUSTED SENSOR. 2 L 7 2 4F RT A21EA 2007080100193 20070801 00193 EA 2007 8 1 MASA200700052 1 20070125 A 2697 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA SMOKE DETECTOR LOOSE A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 17358 7358 ASH 2894 LGB - CREW REPORTED AN INTERMITTENT CARGO SMOKE WARNING. MX RESEATED A CONNECTOR ON THE NR 1 CARGO SMOKE DETEC TOR AND COULD NOT DUPLICATE THE DISCREPANCY. 2 L 7 2 4F RT A21EA 2007080200004 20070802 00004 EA 2007 8 2 MASA200700287 1 20070530 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37178 7178 ASH 2849 PHX - PILOT REPORTED THE CEILING LEVEL EMERGENCY LIGHT ABOVE ROW 2 INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2007080200005 20070802 00005 EA 2007 8 2 MASA200700288 1 20070530 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 927LR 15027 ASH 2892 TUS ROW 3 CEILING LEVEL EMERGENCY FLOOD LIGHT INOP. MX RE-LAMPED. 2 L 7 2 4F RT A21EA 2007080200007 20070802 00007 EA 2007 8 2 MASA200700253 1 20070509 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27185 7185 ASH 7351 IAD - MID CABIN EMERGENCY CALL LIGHT WAS INOP. MX RELAMPED THE LIGHT, OP CHECK GOOD. 2 L 7 2 4F RT A21EA 2007080200015 20070802 00015 EA 2007 8 2 MASA200700300 1 20070603 A 4900 12684221 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA APU MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37228 13014 7228 ASH 2844 PHX - APU OVERTEMP, FOLLOWED BY APU FIRE, CREW FOLLOWED CFM CHECKLIST, APU FIRE CHANGED TO APU FAULT. REMOVED AND REPLACED DIFFUSER CG ACTUATOR. 2 L 7 2 4F RT A21EA 2007080200032 20070802 00032 NM 2007 8 2 UIEA200700295 1 20070725 A 5753 SUPPORT BRACKET BOEING 747 747271C 1384869 NM ZONE 600 DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 RIGHT INBOARD MIDFLAP MOST OUTBOARD UNDERSIDE SUPPORT BRACKET AREA ON FLAP PREVIOUS REPAIR DISBONDED. REMOVED DISBONDED REPAIR AND INSTALLED NEW REPAIR ON RIGHT INBOARD MIDFLAP MOST OUTBOARD UNDERSIDE SUPPORT BRACKET AREA IAW SRM 51-40-12. 2 L 7 4 4F A20WE 2007080200033 20070802 00033 NM 2007 8 2 UIEA200700292 1 20070721 A 5710 STRUCTURE BOEING 747 747243B 1384830 NM LT WING DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 AFTER LANDING LEFT WING UPPER SURFACE, INBOARD OF NR 2 ENG JUST AFT OF LEADING EDGE, PATCH MISSING. EXPOSED DAMAGE HONEY COMB, MATERIAL EXPOSED WITH PORTIONS OF HONEY COMB MISSING AND BULGED UP FROM SURFACE AREA. INTERIM REPAIR WAS ACCOMPLI SHED IAW XEO NR 57-072207 22 JUL 07. ATLAS AIR PART 1 INTERIM REPAIR. PART 2, 3, 4 AND 5. 2 L 7 4 4F A20WE 2007080200055 20070802 00055 EA 2007 8 2 SWIA200718528 1 20070619 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 713SK 10174 COCKPIT FLOORBEAM IS CRACKED AT BUTTLINE 9, DISCOVERED AT C-CHECK. INSTALLED REPLACEMENT FLOOR SUPPORT PARTS PER MM 51- 42-06. 2 L 7 2 4F RT A21EA 2007080200060 20070802 00060 SO 2007 8 2 SWIA200718533 1 20070722 A 5330 SKIN EMB 120 EMB120ER 3260203 SO FUSELAGE DENTED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 576SW 120345 FUSELAGE LOWER SECTION HAS A DENT AT STATION 18B AREA. APPLIED STRINGER REPAIR AT STRINGER 20L JUST FORWARD OF FRAME 19 PER SRM 53-00-03. 2 L 7 2 4T RT A31SO 2007080200071 20070802 00071 EU 2007 8 2 07FDEA02641 1 20070710 A 5330 A53981540200 SKIN AIRBUS 310 A310222 3930315 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 420FE 339 LOWER FUSELAGE, PREVIOUS REPAIR FOUND LOCATED ON FR 74/75 AND STR 41/44 LT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM R EPAIR. NEW REPAIR WAS ACCOMPLISHED PER SRM 53-10-12 FIG 225 SHEET 1. 2 L 7 2 4F RT A35EU 2007080200073 20070802 00073 EU 2007 8 2 07FDEA02643 1 20070629 A 5315 A53781841200 FLOORBEAM AIRBUS 310 A310222 3930315 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 FWD CARGO COMPARTMENT, CABIN FLOORBEAM CRACKED AT FR 37 BETWEEN Y1456 AND Y1959. IT WAS REPAIRED IAW FEDEX EA 6-5310-11 2431. 2 L 7 2 4F RT A35EU 2007080200075 20070802 00075 NM 2007 8 2 QXEA200701211 1 20070721 A 2420 UNKNOWN DHAV DHC8 DHC8202 2809007 NM UNKNOWN A QXEA O OTHER O OTHER CL CLIMB 1 NM 09 350PH 488 PSC - DURING INITIAL CLIMB NR 1 AC GENERATOR CAUTION ILLUMINATED. FOLLOWING THE CHECKLIST, THE LIGHT EXTINGUSHED. 90 SE CONDS LATER, THE LIGHT RE-ILLUMINATED. A SECOND RESET WAS NOT ATTEMPTED. NR 2 AC GENERATOR LOADS WERE MONITORED AND NO LIMITATIONS WERE EXCEEDED. MAINTENANCE COMPLIED WITH FUNCTIONAL TEST OF AC GENERATOR SYSTEM. TEST OK. RAN PROP HEAT DURING GROUND RUN TO CHECK LOAD CARRING ABILITY, CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007080200077 20070802 00077 WP 2007 8 2 IXXA07SMN173S 1 20070630 A 5753 VANE DOUG DC8 DC873F 302199F WP ZONE 600 MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INTERIM HAD IMPROPER REPAIR AT OUTBOARD VANE SLOT XOLDO 067 AT STATI ON XFS 566.250. REMOVED EXISTING REPAIR. CUT DAMAGED AREA.PERFORMED NDT INSPECTION. NO CRACK OR CORROSION AFTER CUT. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA, AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW FAA FORM 8110 -3 NUMBER 07330 DATED 07-18-07, SEMAN DRAWING NUMBER ED 4576 DATED 06-29-07. DC8 SRM 51-1-21, 51-3-0, DC8 NDT SPM PART 0 6-10-01-001, SMN 242-2, DC8 SRM 51-1-8B, 51-1-20D, AND SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007080200081 20070802 00081 NM 2007 8 2 2007UALA02801 1 20070723 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 S14-15L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 FUSELAGE FRAME SHEAR TIE CRACKED BS 360 BTWN STR'S 14L-15L. INSTALLED REPLACEMENT FRAME SHEAR TIE SECTION. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080200088 20070802 00088 NM 2007 8 2 2007UALA02808 1 20070724 A 2612 FIRE WARNING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2 NACELLE FALSE ACTIVATION A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 NR 2 ENG FIRE LOOP 'A' EICAS STATUS MESSAGE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080200095 20070802 00095 NM 2007 8 2 2007UALA02815 1 20070724 A 3350 362624 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 545UA 25323 DOOR R2 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED. OPS CHECK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080200096 20070802 00096 NM 2007 8 2 2007UALA02816 1 20070724 A 3350 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 647UA 25284 FWD LEFT AND MID LEFT LAV FLOOR EEL STRIPS ARE INOPERATIVE. SECURED CONNECTOR. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080200103 20070802 00103 GL 2007 8 2 C2XA07ON013 2 20070722 A 7261 23054499 LINE EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL ENGINE OIL CHAFED A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 27 14179 6687 6687 145896 CAE312763 FLT 7679 - MMLM TO LAX - DURING FLIGHT CREW REPORTED E1 OIL PRESSURE FELL - DROPPED SUDDENLY TO 2 QUARTS. E1 WAS SECURE D IN FLIGHT. A/C LANDED IN LAX WITHOUT INCIDENTS WITH A SINGLE ENGINE APPROACH. MX COMPLIED WITH TROUBLESHOOTING AND F OUND OIL PRESSURE LINE FROM ACCESSORY GEAR BOX TO REGULATING VALVE CHAFED. MX REMOVED AND REPLACED E1 OIL PRESSURE LINE , OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F 4 F RT TE6CH 2007080200113 20070802 00113 NM 2007 8 2 ZZDA2007230 1 20070607 A 5330 DOUBLER BOEING 717 717200 1383700 NM BS 1040 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT DRAIN DOUBLER LOCATED BETWEEN LONGERON 30L AND LONGERON 29L AT BS 1040. INSTALLED NE W DOUBLER BETWEEN LONGERON 30L AND LONGERON 29L IAW B717 SRM 51-41-02. MATERIAL USED 0.063 7075T6; SIZE 3.0 X 4.25 INCH ES. 2 L 7 2 4F TR A6WE 2007080200114 20070802 00114 NM 2007 8 2 ZZDA2007231 1 20070607 A 5320 SPLICE BOEING 717 717200 1383700 NM STA 898.5 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 AFT CARGO COMP STA 898.5 INNER SPLICE CORRODED FROM LONG 26L AND 26R. REPLACED INNER SPLICE FROM LONGERON 26 LT TO 26 R T ON STA 898.5 IAW B717 SRM 51-41-05. MATERIAL USED 7075 T6 0.080" X 60." X 3.50". 2 L 7 2 4F TR A6WE 2007080200116 20070802 00116 NM 2007 8 2 ZZDA2007233 1 20070610 A 5313 STRINGER SPLICE BOEING 717 717200 1383700 NM BS 898.5 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 BS 898.5 LONGERON 30L STRINGER SPLICE IS CORRODED. INSTALLED SPLICE ON LONGERON 30L ON BS 898.5 PER B717 SRM 51-41-02 A ND SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007080200120 20070802 00120 NM 2007 8 2 SWAA073697 1 20070726 A 5311 6546538 FRAME BOEING 737 7373H4 1384600 NM BS 597 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200161 20070802 00161 NM 2007 8 2 SWAA073711 1 20070726 A 5311 65C25228 FRAME BOEING 737 7373K2 13844BA NM BS 727C S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200164 20070802 00164 NM 2007 8 2 SWAA073715 1 20070726 A 5340 65C27314 STRINGER CLIP BOEING 737 7373K2 13844BA NM BS 663 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007080200166 20070802 00166 NM 2007 8 2 SWAA073714 1 20070726 A 5340 65C27314 STRINGER CLIP BOEING 737 7373K2 13844BA NM BS 500A S3R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007080200168 20070802 00168 NM 2007 8 2 SWAA073674 1 20070726 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 1006-1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER 26R CORRODED BETWEEN BS 1006 AND BS 1016. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007080200169 20070802 00169 2007 8 2 SWAA073678 4 20070726 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007080200171 20070802 00171 EU 2007 8 2 USAA0000000 1 20070706 A 5330 ASNA2051DKS SKIN AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED G USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 183UW 22021 1539 CORRODED RIVET TAILS WERE FOUND IN FUSELAGE CARGO COMPARTMENT BETWEEN FRAME 24 TO 35.6 STRINGER 38R TO 38L. APPROXIMATE LY 1350 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD THE PAINT FL AKING OFF THE RIVET TAILS THAT WERE CLEANED AND HAD PRIMER AND PAINT REAPPLIED. AIRCRAFT WAS MANUFACTURED JULY 17, 2001 . 2 L 7 2 4F RT A28NM 2007080200173 20070802 00173 NM 2007 8 2 SWAA073709 1 20070726 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED HC1 CHECK, LT OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007080200174 20070802 00174 NM 2007 8 2 SWAA073665 1 20070725 A 5330 141A3702 SKIN BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 732SW 27864 DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE SKIN CRACKED AT EXTERNAL POWER RECEPTACLE CUTOUT AFT END. REPAIRED SKIN PER S WA EA. 2 L 7 2 4F RT A16WE 2007080200176 20070802 00176 NM 2007 8 2 SWAA073647 1 20070725 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200177 20070802 00177 NM 2007 8 2 SWAA073650 1 20070725 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200181 20070802 00181 NM 2007 8 2 SWAA073656 1 20070725 A 5310 6546554 DOOR FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME WEB CRACKED AT LOWER OUTBOARD CORNER. REMOVED AND REP LACED FRAME WEB PER ACO. 2 L 7 2 4F RT A16WE 2007080200182 20070802 00182 NM 2007 8 2 SWAA073653 1 20070725 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM BS 867 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200183 20070802 00183 NM 2007 8 2 SWAA073652 1 20070725 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200185 20070802 00185 NM 2007 8 2 SWAA073666 1 20070725 A 5311 6546564 FRAME BOEING 737 7375H4 138449D NM BS 992 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 992, RBL 46. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2007080200186 20070802 00186 NM 2007 8 2 SWAA073648 1 20070725 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200188 20070802 00188 NM 2007 8 2 2007UALA02736 1 20070719 A 3200 UNKNOWN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE MLG UNKNOWN A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 195UA 26899 GEAR DISAGREE CAUTION MESSAGE WITH GEAR DOOR ADVISORY MESSAGE & GEAR MONITOR MESSAGE DISPLAYED AFTER GEAR RETRACTION. A LL NORMAL WITH GEAR LEVER NOW IN THE UP POSITION. [08-14-07] PERFORM NLG WHEEL WELL AREA CONDITION CHECK DUE TO FOREI GN OBJECT (STOWAWAY) FOUND IN WHEEL WELL AREA. ACCOMPLISHED NOSE LANDNG GEAR WHEEL WELL CHECK. NO ADDITIONAL DAMAGE FOU ND. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080200189 20070802 00189 NM 2007 8 2 ASAA0771914 1 20070726 A 2170 602978200 COALESCER BAG BOEING 737 737790 13844CN NM RT ACM CONTAMINATED A ASAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 02 611AS 29753 F/A REPORTED ELECTRICAL SMOKE ORIGINATING FROM REAR OF ACFT IMMEDIATELY AFTER T/O, ACCOMPLISHED CHECKLIST. SMOKE DISSIP ATED AFTER RIGHT PACK TURNED OFF. REMOVED WATER SEPARATOR BAG. FOUND OIL CONTAMINATION ON BAG. PERFORMED FIM 2100 TAS K 801. NO VISIBLE SMOKE OR ODOR DETECTED. RIGHT WATER SEPARATOR COALESCER BAG REPLACED REF MM 21-51-05. RETURNED TO S ERVICE. 2 L 7 2 4F RT A16WE 2007080200190 20070802 00190 WP 2007 8 2 ASAA0781910 1 20070726 A 5210 591140659 SKIN DOUG DC9 DC983 3022083 WP PAX DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 FORWARD ENTRY DOOR IS DENTED. RECONTOURED DOOR SKIN AND INSTALLED INTERNAL DOUBLER PER SRM 53-04. 2 L 7 2 4F RT A6WE 2007080200193 20070802 00193 WP 2007 8 2 ASAA0781899 1 20070726 A 5321 993654511 FLOOR PANEL DOUG DC9 DC983 3022083 WP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-24-0 AND 53-5. 2 L 7 2 4F RT A6WE 2007080200197 20070802 00197 NM 2007 8 2 UPS07650197 1 20070627 A 5420 FITTING BOEING 767 76734AF 1385212 NM LT PYLON MISINSTALLED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 309UP 27740 INSPECTION TYPE:SIP LEFT PYLON AFT PITCH LOAD FITTING HAS SHORT EDGE MARGIN. FABBED RADIUS FILLER FROM 7075-T7351. LOC ATED, DRILLED & REAMED TO FINAL SIZE. VERIFIED RADIUS FILLER LIES FLAT AS BACKUP FITTING. ALODINED & PRIMED RADIUS FIL LER PER ER 07-2696. C/W ALL REQUIREMENTS OF ER 07-2696 CUSTOMER AUTHORIZATION EO B767-5740-27262-A. 2 L 7 2 4F RT A1NM 2007080200198 20070802 00198 WP 2007 8 2 UPS07850211 1 20070621 A 5315 37746061 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 INTERCOSTAL CORRODED AROUND AND UNDER NUT PLATE AT FS 50 AND RBL 30. REPAIRED INTERCOSTAL AND FLOORB EAM AT STA 55 RBL 10 TO RBL 28 IAW SAA EA 008-5310-01-A0946, UPS RAA DC8-53-20638, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007080200201 20070802 00201 WP 2007 8 2 UPS07850225 1 20070714 A 5210 DOOR FRAME DOUG DC8 DC873F 302199F WP L1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 L-1 DOOR FRAME SEGMENT CRACKED IN BAYONETTE AREA. STOP DRILLED CRACK IN FRAME SEGMENT AT L-1 DOOR IA W SRM 52-2-0. FABRICATED AND INSTALLED REPAIR DOUBLER ON L-1 DOOR FRAME SEGMENT IAW SRM 52-02-02 FIG 007. 2 L 7 4 4F RT 4A25 2007080200202 20070802 00202 WP 2007 8 2 UPS07850227 1 20070711 A 5340 3755854502 FITTING DOUG DC8 DC873F 302199F WP FS 1180 L27L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 STA 1180 L27L BANANA FITTING IS CRACKED. REMOVED AND REPLACED BANANA FITTING AT STA 1180 L27L IAW SR M 51-01-20D, AND SRM 51-3-2. 2 L 7 4 4F RT 4A25 2007080300002 20070803 00002 EA 2007 8 3 COMA0760494 1 20070721 A 3234 7179015 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA MLG FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 708CA 23279 7235 FLIGHT 6433 - GEAR DISAGREE MESSAGE AFTER TAKEOFF QRH FOLLOWED GEAR EXTENDED, AIRCRAFT RETURNED TO CVG AND LANDED SAFELY . REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE. 2 L 7 2 4F RT A21EA 2007080300003 20070803 00003 NM 2007 8 3 SWAA073766 1 20070729 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007080300004 20070803 00004 NM 2007 8 3 SWAA073770 1 20070730 A 5330 417A3110 SKIN BOEING 737 7377H4 1384404 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 264LV 32521 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CREASED AT BS 963, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007080300005 20070803 00005 NM 2007 8 3 UPS07450290 1 20070705 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C AFT CARGO DOOR CUTOUT FWD UPPER CORNER SKIN REPAIRED AS PER HX RS NR R53-61-35822, CRACK LENGTH 0.030" AND 0.090"). AFT CARGO DOOR CUTOUT FWD UPPER CORNER SKIN REPAIRED AS PER HX RS NR R53-61-35822. CONTINUE INSPECTION A RE REQUIRED AS PER HX RS NR R53-61-35822 AND UPS EO NR B747-5330-27287. 2 L 7 4 4F A20WE 2007080300009 20070803 00009 NM 2007 8 3 UPS07450296 1 20070702 A 5311 FRAME BOEING 747 747212B 1384886 NM BS 840 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C CRACK FOUND AT BS 840 RT SIDE S10R TENSION TIE ATTACHED FRAME DOUBLER CRACK LOCATED AT NO.4 FASTENER H OLE THROUGH THICKNESS RUNNING O/B DIRECTION, CRACK LENGTH 0.060" APPROX. M/D BS 840 RT SIDE FRAME DOUBLER THROUGH FRAME TENSION TIE AND STEEL PLATE HOLE OVERSIZED AT FASTENER INSTALLED AS PER UPS EO B747-5310-23715 APP D AND C. 2 L 7 4 4F A20WE 2007080300012 20070803 00012 NM 2007 8 3 UPS07450299 1 20070703 A 5311 FRAME BOEING 747 747212B 1384886 NM BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C LT BS 940 TENSION TIE NR 1 FASTENER HOLE FOUND CRACK AT FRAME RUNNING 7 O/C POSITION APPROX 0.040" IN LENGTH (LOOKING AFT). M/D BS 940 LT SIDE FRAME THROUGH FRAME DOUBLER, TENSION TIE, STEEL PLATE AND FAIL/SAFE CHORD HOLE OVERSIZED AND FASTENER INSTALLED AS PER UPS EO B747-5310-23715 APP D AND C. 2 L 7 4 4F A20WE 2007080300014 20070803 00014 NM 2007 8 3 UPS07450301 1 20070705 A 5315 FLOORBEAM BOEING 747 747212B 1384886 NM BS 2340 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D BS2340 LBL40-59 FLOORBEAM UPPER CHORD FOUND SEVERAL AREAS OF CORROSION. CORROSION BLEND OUT 0.040 " BY 1" BY 3" EXCEED SRM LIMIT. M/D BS 2340 LBL 25 TO LT MOST O/B FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FI G 1. 2 L 7 4 4F A20WE 2007080300015 20070803 00015 NM 2007 8 3 UPS07450303 1 20070703 A 5320 CHANNEL BOEING 747 747212B 1384886 NM BS 820 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C LT BS 820 TENSION TIE NR 4 FASTENER HOLE FOUND CRACK AT FWD CHANNEL APPROX 1/16" IN LENGTH RUNNING UP. M/D BS 820 TENSION TIE FWD CHANNEL REPAIRED AS PER RS R53-25-35817 AND UPS EO B747-5310-27264-A. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35817 AND UPS EO B747-5310-27264. 2 L 7 4 4F A20WE 2007080300018 20070803 00018 NM 2007 8 3 UPS07450305 1 20070702 A 5340 65B38600113 STRINGER CLIP BOEING 747 747212B 1384886 NM BS 880 S9R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C CRACK FOUND AT BS 880 RT SIDE S9R TENSION TIE ATTACHED STRINGER CLIP CRACK LOCATED AT NR 10 FASTENER H OLE 0.030" APPROX RUNNING UPWARD DIRECTION. M/D BS 880 RT SIDE STR 9R TENSION TIE ATTACHED STRINGER CLIP REPLACED AND I NSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02 AND EO B747-5310-23715-C. 2 L 7 4 4F A20WE 2007080300020 20070803 00020 WP 2007 8 3 IXXA07SMN186S 1 20070630 A 5340 3755843U501 FITTING DOUG DC8 DC873F 302199F WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND AFT LOWER CARGO COMPARTMENT A CRACKED FITTING AT STATION 1180.000 LONGERON 34 R IGHT, AND LONGERON 35 RIGHT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, AND SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007080300021 20070803 00021 NM 2007 8 3 UPS07450306 1 20070706 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C NR 3L MED CUTOUT FWD LOWER CORNER FOUND SKIN AND BEARSTRAP EDGE CRACKED, CRACK LENGTH 1/16" TO 5/8" RE SP. NR 3L MED CUTOUT FWD LOWER CORNER SKIN AND BEARSTRAP REPAIRED AS PER UPS EO B747-5330-24674 APP M. 2 L 7 4 4F A20WE 2007080300023 20070803 00023 NM 2007 8 3 UPS07450308 1 20070705 A 5340 65B38600116 STRINGER CLIP BOEING 747 747212B 1384886 NM BS 780 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C FWD CARGO COMPT S33L STRINGER CLIP FOUND CRACKED AT STA780, CRACK LENGTH 1/4". FWD CARGO COMPT BS 780 STR 33L STRINGER CLIP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 3 AND 51-30-02. 2 L 7 4 4F A20WE 2007080300024 20070803 00024 NM 2007 8 3 UPS07450309 1 20070703 A 5314 KEELBEAM BOEING 747 747212B 1384886 NM BS 1460 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C FX KEEL BEAM BOX LOWER EXTERNAL PANEL SUPPORT ATT SHIM FOUND CORROSION AT STA 1460 LBL4 TO LBL5 AND RB L4 TO RBL5 UPPER SURFACE TO STIFFENER AREA AS MARKED. CORROSION BLEND OUT 0.065" BY 3/4" BY 1 1/4" EXCEED SRM LIMIT. F X KEEL BEAM BOX LOWER EXTERNAL PANEL SUPPORT ATT SHIM REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007080300026 20070803 00026 NM 2007 8 3 UPS07450311 1 20070702 A 5320 CHANNEL BOEING 747 747212B 1384886 NM BS 880 S9R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C CRACK FOUND AT BS 880 RT SIDE S9R TENSION TIE ATTACHED FWD CHANNEL CRACK LOCATED AT NR 16 FASTENER HOL E 0.040" APPROX RUNNING UPWARD DIRECTION. M/D BS 880 TENSION TIE FWD CHANNEL REPLACED AS PER SRM 51-10-01 PG 9 AND INST ALLED AS PER UPS EO B747-5310-23715-C AND SRM 51-30-02 REFER NRC 50073 FOR WORKING DETAIL. 2 L 7 4 4F A20WE 2007080300030 20070803 00030 NM 2007 8 3 UPS07450315 1 20070704 A 5330 SKIN BOEING 747 747212B 1384886 NM BS 340 S5-5AR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C U/D FX SKIN AT BS 340 S5-5A FOUND CRACK AT 1 FASTENER HOLE CRACK LENGTH 1/16". FX BS 340 BETWEEN STR 5R TO 5 AR SKIN REPAIRED WITHOUT ZERO TIMING AT CRITICAL ROW FASTENERS AS PER SRM 53-30-03 FIG 1 AND TAR S/N 127808 REV A REPEAT INSP IS REQUIRED AS PER SRM 53-30-03 FIG 1. UPS MPI NR P19299 RAISED FOR CONTINUE REPEAT INSP AND MPI NR P19300 RAISED FOR PERM REPAIR. 2 L 7 4 4F A20WE 2007080300031 20070803 00031 NM 2007 8 3 UPS07450316 1 20070703 A 5320 65B0961429 PLATE BOEING 747 747212B 1384886 NM BS 940 MISINSTALLED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/ BS940 LT TENSION TIE FWD ATT STEEL PLATE UPPER ROW MOST I/B FASTENER HOLE FOUND SHORT EDGE MARGIN. M/D BS 940 LT TENSION TIE FWD ATTACH STEEL PLATE REPLACED AND INSTALLED AS PER RS R53-25-35824 AND EO B747-5310-23715-C . CONTINUED INSPECTIONS ARE REQUIRED AS PER RS R53-25-35824 AND UPS EO B747-5310-27295. 2 L 7 4 4F A20WE 2007080300033 20070803 00033 NM 2007 8 3 UPS07450318 1 20070705 A 5313 65B0442122 STRINGER SPLICE BOEING 747 747212B 1384886 NM BS 738 S31R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C FWD CARGO COMPT S31R STRINGER SPLICE FOUND CRACKED AT STA738. CRACK LENGTH 1/4". FWD CARGO COMPT BS 7 38 STR 31R STRINGER SPLICE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG9 AND 51-30-02. 2 L 7 4 4F A20WE 2007080300035 20070803 00035 SO 2007 8 3 CHQA200700040 1 20070730 A 2150 C1431236 CONTROL VALVE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 AC PACK INOPERATIVE A CHQA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 11 264SK 6064 2190 221 CAE311337 ON CLIMB-OUT FROM CLE WITH PACK 2 DEFERRED WERE UNABLE TO MAINTAIN COMFORTABLE CABIN/COCKPIT TEMPERATURE. TEMPERATURE R EACHED 38 DEGREES C IN COCKPIT. WE SMELLED SOMETHING BURNING. FA REPORTED HEARING A LOUD POP. WE COULD FEEL IT GETTIN G WARMER QUITE RAPIDLY. THEN PUT OXYGEN MASKS ON AND MADE A RAPID DESCENT TO 10,000FT AND SHUT PACK OFF AND MADE PRECAU TIONARY LANDING AT CMH. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007080300036 20070803 00036 NM 2007 8 3 DHL2007741516 1 20070726 A 5320 SUPPORT BOEING 727 7272Q9 138448M NM BS 720C S26L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 FOUND STR 26L TO BS 720C FRAME SUPPORT CLIP CORRODED. REMOVED STRINGER CLIP, FABRICATED NEW CLIP FROM 2024-T3, .040" BY 4" BY 3.25", PO NR 9005138, PER B727 SRM 53-10-2 FIG 3 AND 51-10-3. TREATED, PRIMED, AND INSTALLED STRINGER CLIP PER B 727 SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007080300037 20070803 00037 NM 2007 8 3 UPS07450320 1 20070704 A 5330 SKIN BOEING 747 747212B 1384886 NM BS 340-350 S5-5A CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C U/D FX SKIN AT BS340-350 S5-5A FOUND CRACKS AT 3 FASTENER HOLES, CRACK LENGTH 1/16, 1/2 AND 9/16". FX BS 340 TO 350 STR5L SKIN REPAIRED WITHOUT ZERO TIMING AT CRITICAL ROW FASTENERS AS PER SRM 53-30-03 FIG 1 AND TAR S/N 1 27807 REV A REPEAT INSP IS REQUIRED AS PER SRM 53-30-03 FIG 1. UPS MPI#P19298 RAISED FOR CONTINUE REPEAT INSPECTION. 2 L 7 4 4F A20WE 2007080300041 20070803 00041 NM 2007 8 3 UPS07550240 1 20070628 A 5412 311N3271 BULKHEAD BOEING 757 75724APF 1384969 NM NR 2 PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 402UP 23724 INSPECTION TYPE:C NR 2 PYLON AFT BULKHEAD RT LOWER/OUTBD SURFACE HAS IS CHAFED. BULKHEAD MILL AND NDT WERE DONE ON TRAV T7/689654. HFEC WAS DONE ON TRAV NR T7/689654. MILLED AREA 1.25W" BY 2.1W BY .040 REMOVED, ORIGINAL THICKNESS .200 RE MAINING .160. SHOT PEENED AREA PER SOPM 20-10-03, REF EA NR 757-5451-27-A1703 PRELIMINARY 1. 2 L 7 2 4F RT A2NM 2007080300043 20070803 00043 NM 2007 8 3 UPS07550242 1 20070628 A 5412 311N3271 BULKHEAD BOEING 757 75724APF 1384969 NM NR 2 PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 402UP 23724 INSPECTION TYPE:C NR 2 PYLON AFT BULKHEAD LT LOWER/OUTER SURFACE HAS A CHAFED. BULKHEAD MILL AND NDT WERE DONE ON TRAV T7/689654. HFEC WAS DONE ON TR TRAV NR T7/689654. MILLED AREA 1.25W BY 2.1L BY .050 REMOVED ORIGINAL THICKNESS .200, . 150 REMAINING. SHOT PEENED AREA PER SOPM 20-10-03, REF EA NR 757-5451-27-A1703 PRELIMINARY 1. 2 L 7 2 4F RT A2NM 2007080300045 20070803 00045 NM 2007 8 3 UPS07550292 1 20070726 A 2910 271N61191 LINE BOEING 757 75724APF 1384969 NM HYDRAULIC SYSTEM LEAKING A IPXA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 01 468UP 25484 ON APPROACH INTO PHX ,THE LEFT HYDRAULIC SYSTEM WENT TO ZERO. CREW LANDED AIRCRAFT WITHOUT INCIDENT. FOUND HOLE IN LMG DOWNLOCK ACTUATOR FLEX LINE. HOLE WASN'T CAUSED BY CONTACT W/ANYTHING. THE HOLE APPEARS TO BE FROM FATIGUE NEAR A SWA GED FTG. FLEX LINE REPLACED. REPLACED CASE DRAIN AND PRESSURE FILTERS NO METAL FOUND REF MM 29-11-17-4. REPLACED ACMP CASE DRAIN AND PRESSURE FILTERS PER AMM 29-11-18-4. ALL LEAK CHECKS GOOD. 2 L 7 2 4F RT A2NM 2007080300046 20070803 00046 2007 8 3 UPS07650323 4 20070726 A 3420 H150AKM1 INDICATOR BOEING 767 76734AF 1385212 NM STANDBY ATTITUDE INOPERATIVE A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 312UP 27763 INSPECTION TYPE:ETOP STAND BY ATTITUDE INDICATOR IS ABNORMAL IN ROLL MODE. GYRO FLAG RETRACTED. REMOVED AND REPLACED S AI PER AMM 34-24-01-2. 2 L 7 2 4F RT A1NM 2007080300048 20070803 00048 NM 2007 8 3 UPS07650326 1 20070720 A 2751 TRANSMITTER BOEING 767 76734AF 1385212 NM TE FLAPS INOPERATIVE A IPXA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 319UP 27758 INSPECTION TYPE:ETOP CLEARING THE RUNWAY FLAP ASSY MESSAGE DISPLAYED FOR 3-4 SECONDS THEN CLEARED. REMOVED AND REPLACE D NR 1 T/E FLAP POSITION TRANSMITTER IAW MM 27-51-45-2. OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2007080300049 20070803 00049 SO 2007 8 3 C2XA07IA175 1 20070726 A 3350 78241 INVERTER EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 29515 145309 IAH -FLIGHT 2487, DURING CREW INSPECTION THE RT EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE NUMBER 5 EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007080300051 20070803 00051 NM 2007 8 3 CALA0700377 1 20070727 A 5313 BAC1498156 STRINGER BOEING 737 7373T0 1384582 NM BS 1006 S25L CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND STRINGER 25L CORRODED AT REPAIR CUTOUT AFT OF STA 1006. THE CORRODED SECTION OF STRINGER WAS REMOVED AN D REPLACED IAW SRM 53-00-03, FIGURE 201, REPAIR 1. 2 L 7 2 4F RT A16WE 2007080300054 20070803 00054 NM 2007 8 3 CALA0700380 1 20070708 A 5730 65C25204 SKIN BOEING 737 7373T0 1384582 NM LT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND LT WING SKIN CORRODED FORWARD OF NR 3 SPOILER, I/B HINGE POINTS, APPROX WS 311.37. REPAIRED IAW ECRA 5 720-02022. 2 L 7 2 4F RT A16WE 2007080300055 20070803 00055 NM 2007 8 3 CALA0700381 1 20070729 A 5311 6546567 FRAME BOEING 737 7373T0 1384582 NM BS 1006 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND FRAME CORRODED AT STA 1006 FROM S25R TO 26L. THE CORRODED SECTION OF FRAME WAS CUT OUT AND A REPAIR DO UBLER WAS INSTALLED IAW SRM 53-00-07, FIGURE 201, REPAIR 1. 2 L 7 2 4F RT A16WE 2007080300056 20070803 00056 NM 2007 8 3 CALA0700382 1 20070730 A 5320 6545801512 STRUCTURE BOEING 737 7373T0 1384582 NM BS 227.8 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND LOWER FUSELAGE O/B CHORD CORRODED AT STA 227.8, LBL5.7 TO RBL 5.7. REPAIRED IAW ECRA 5311-01345. 2 L 7 2 4F RT A16WE 2007080300057 20070803 00057 NM 2007 8 3 UPS07650327 1 20070720 A 3020 2790583108 ANTI-ICE VALVE BOEING 767 76734AF 1385212 NM ENGINE INOPERATIVE A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 329UP 27755 INSPECTION TYPE:ETOP EICAS MESSAGE ANTI-ICE DISPLAYED AND ENGINE ANTI-ICE VALVE LIGHT REMAINED ILLUMINATED WITH SWITCH S ELECTED ON TO OFF. REMOVED AND REPLACED ANTI-ICE VALVE. OPS CHK WITH ENG RUNNING AND LEAK CHK DONE SATISFACTORY. NO L EAK REF B767 AMM 30-21-03/401. 2 L 7 2 4F RT A1NM 2007080300059 20070803 00059 NM 2007 8 3 UPS07650329 1 20070722 A 2432 CHARGER BOEING 767 76734AF 1385212 NM MAIN BATTERY INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 331UP 27757 INSPECTION TYPE:ETOP MAIN BATTERY CHARGER STATUS MESSAGE DISPLAYED. REMOVED AND REPLACED MAIN BATTERY CHARGER IAW MM 24 -31-02-4 AND MAIN BATTERY IAW MM 24-30-01-4 SYSTEM CHECKS GOOD IAW BOTH. 2 L 7 2 4F RT A1NM 2007080300060 20070803 00060 NM 2007 8 3 UPS07650331 1 20070713 A 2432 CHARGER BOEING 767 76734AF 1385212 NM MAIN BATTERY UNKNOWN A IPXA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 01 324UP 27750 INSPECTION TYPE:ETOP AT ENG SHUTDOWN RECEIVED ADVISORY LEVEL EICAS MESSAGE "MAIN BAT CHGR". ACCOMPLISHED FIM PROCEDURE 31-41-00/101 SYSTEM CHECKS OK. 2 L 7 2 4F RT A1NM 2007080300061 20070803 00061 NM 2007 8 3 UPS07650332 1 20070714 A 2797 CONNECTOR BOEING 767 76734AF 1385212 NM TE FLAP XMITER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 319UP 27758 INSPECTION TYPE:ETOP BLOCK TURN BACK DUE TO EICAS MSG FLAP/SLAT ELEC DISPLAYED. BITE CHECK FSEU-FAULT-1 LT O/B TRANSMIT TER. FOUND CORROSION IN CONNECTOR. CLEANED. OPS CHECK PER MM 27-58-00-5. CHECKED OK. 2 L 7 2 4F RT A1NM 2007080300062 20070803 00062 WP 2007 8 3 UPS07850244 1 20070725 A 3350 6012235 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:SP EMERGENCY LIGHTING FAILED OPS CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK IAW DC8 AM M 33-50-01-2. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2007080300065 20070803 00065 NM 2007 8 3 UPS07M50286 1 20070608 A 5313 LONGERON SPLICE DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C CTR CGO STA 5-113 LONGERON 47 LONGERON SPLICE FITTING FOUND CRACKED AS MARKED NEW SPLICE FITTING FABRI CATED PER DWG A5A7114 MATL USED:1D11047. FPI CARRIED OUT PER DPS4.707 REV AW AND FOUND NO CRACK EVIDENT. NEW SPLICE FA STENER HOLES PICK UP PER SRM51-31-01 V.2R.38. NEW SPLICE REPROTECTED AND PAINT TOUCH UP PER SRM 51-21-01 V.2R.38. NEW SPLICE INSTALLED PER SRM 51-31-01 V.2R.38. 2 L 7 3 4F RT A22WE 2007080300066 20070803 00066 NM 2007 8 3 UPS07M50302 1 20070521 A 5313 LONGERON DOUG MD11 MD11 3023602 NM BS1661 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C CTR CARGO THRU STATION 1661, LONGERON R48 FOUND WITH CORROSION AS MARKED. CORROSION REMOVED FOUND EXC EEDS PER SRM 53-00-01V.1R.38. REPAIR ANGLES FAB AND FASTENER HOLES PICK UP PER EN1355-07. REP ANGLES 02EA AND REWORK A REA REPROTECTED AND PAINT TOUCH UP PER SRM 51-21-01V.2R.38. REPAIR ANGLES 02 EA INSTALLED AS PER EN1355-07. 2 L 7 3 4F RT A22WE 2007080300068 20070803 00068 2007 8 3 QXEA200701218 2 20070726 A 7323 699018002 CONTROLLER BOMBDR DHC8 DHC8402 1390042 NM ENGINE MALFUNCTIONED A QXEA A O UNSCHED LANDING OTHER J WARNING INDICATION CL CLIMB 1 NM 09 407QX 4074 4071 4049 SEA FLIGHT NR 2341: POWER PLANT MESSAGE ON ED AFTER ROTATION. NO OTHER CAUTIONS OR WARNING LIGHTS WERE OBSERVED. ALL E NGINE INDICATIONS WERE NORMAL. POWER LEVERS WERE ALSO MATCHED THROUGHOUT THE FLIGHT. AIRCRAFT RETURNED TO FIELD. MAIN TENANCE INTERROGATED ED'S AND FOUND FAULT CODE 84 ON THE NR 1 ENGINE. REMOVED AND REPLACED PEC IAW Q400 AMM 61-20-36 PA GES 401-407. PERFORMED POWER ASSURANCE RUN PER QX MTC 6710005. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007080300069 20070803 00069 NM 2007 8 3 QXEA200701219 1 20070726 A 3150 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM PITCH TRIM UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 403QX 4037 SEA FLIGHT NR 2289: PITCH TRIM CAUTION. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE C/W FIM TASK 27-30-00-810-803. PITCH TRIM CAUTION LIGHT EXTINGUISHED. CHECKED CDS. NO FAULTS PRESENT. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007080300070 20070803 00070 NM 2007 8 3 QXEA200701220 1 20070728 A 3150 HOSE BOMBDR DHC8 DHC8402 1390042 NM AVIONICS COOLING DISCONNECTED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 419QX 4145 SEA FLIGHT NR 2286: ON TAXI OUT, AVIONICS CAUTION MESSAGE WITH ASSOCIATED HOT ED MESSAGE. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE REMOVED ED AND FOUND AVIONICS AIR COOLING HOSES DISCONNECTED FROM UNIT. RECONNECTED HOSES AND REINSTALLED E D IAW Q400 AMM TASKS 31-61-01-000-801 AND 31-61-01-400-801. PERFORMED OPS TEST OF THE ENGINE DISPLAY IAW Q400 AMM TASK 31-61-01-710-803. TEST IS GOOD WITH NO REOCCURRENCE OF CAUTION OR ED MESSAGES. NO PARTS REPLACED. AIRCRAFT RETURNED T O SERVICE. 2 H 7 2 4T RT A13NM 2007080300072 20070803 00072 EU 2007 8 3 MALA070092 1 20070726 A 3211 PIN SAAB SF340 340B 7860101 EU MLG FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 429XJ 340B429 AFTER TAKEOFF FROM MSP, THERE WAS A LOUD CLUNK IN THE NOSE GEAR AREA AND THE INTRANSIT LIGHT REMAINED ILLUMINATED. CREW FOLLOWED THE QRH AND RETURNED TO MSP. REPLACING NOSE LANDING GEAR ACTUATOR RETRACT PIN, PN: AIR127298. 2 L 7 2 4T RT A52EU 2007080300075 20070803 00075 EA 2007 8 3 QXEA200701157 1 20070716 A 5210 ROD CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR BENT A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 604QX 10019 DEN - MAIN CABIN DOOR HARD TO OPEN. MAINTENANCE REPLACED THE AFT ANCHOR SWIVEL LEVER AND THE BENT AFT UPPER CABLE ASSEM BLY ROD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007080300077 20070803 00077 NE 2007 8 3 QXEA200701195 2 20070708 A 7200 FAN BLADE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE ENGINE DAMAGED A QXEA O OTHER O OTHER CL CLIMB 1 NM 09 602QX 10010 BOI- FLIGHT 4277- ON CLIMB, THE NR 2 ENGINE FAN VIBRATIONS REACHED 1.9. AFTER COMPLETING THE CHECKLIST AND REDUCING POWE R, THE VIBRATION DIMINISHED INTO THE GREEN AREA. MAINTENANCE C/W A TANG LUBE OF THE FAN BLADES IAW 72-21-02-640-801-A01 AND REPLACED THE FAN BLADE PINS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007080300079 20070803 00079 NM 2007 8 3 DHL2007784527 1 20070706 A 5311 FRAME SPLICE BOEING 727 727227 1384078 NM ZONE 100 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 MAIN CABIN FRAME BS 783.95, LBL 70, WL 204 IS CRACKED LWR END OF WEB AREA, CRACK ABOUT 1.5 NDT FINDING. REMOVED FASTENE RS AT MAIN CABIN FRAME AT LWR END IAW B727 SRM 51-30-2. STOP DRILLED CRACK .250 IAW B727 SRM 51-10-1. HFEC VERIFIED ST OP DRILL IAW B727 NDTM PT.6 51-00-00. DRILLED UP REPAIR PARTS IAW B727 S/B 727-53-0197 AND DWG 65C36280. TREATED, PRIM ED AND INSTALLED REPAIR PARTS IAW B727 SRM 51-10-2, B727 S/B 727-53-0197 AND DWG 65C36280. 2 L 7 3 4F A3WE 2007080300080 20070803 00080 NM 2007 8 3 DHL2007741517 1 20070726 A 5311 SUPPORT BOEING 727 7272Q9 138448M NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 STRINGER 26R TO BS 720C FRAME SUPPORT CLIP CORRODED. REMOVED CLIP, FABRICATED NEW CLIP FROM 2024-T3, .040" BY 4" BY 3.2 5", PO NR 9005138, PER B727 SRM 53-10-2 FIG 3, 51-10-3, AND 51-20-1. TREATED, PRIMED, AND INSTALLED STRINGER CLIP PER B 727 SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007080300083 20070803 00083 NM 2007 8 3 HALA0700304 1 20070726 A 2612 89873202 CIRCUIT CARD BOEING 767 76733A 1385209 NM FIRE DETECTION MALFUNCTIONED A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM, DURING ETOPS 1 CHECK FOUND L ENG FIRE LP 1 EICAS MESSAGE ILLUMINATED. REPLACED LT ENG FIRE DE T CARD (M681), OPS CHECK OK IAW AMM 26-12-000. 2 L 7 2 4F RT A1NM 2007080300088 20070803 00088 NM 2007 8 3 AWXA200700937 1 20070706 A 5511 182N11011 SPAR BOEING 757 757225 1384959 NM ZONE 300 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - NR 5956471, CORROSION ON THE LEFT HORIZONTAL REAR AFT SPAR, STABILIZER STATION 224 - 3 66. REPAIRED THE LEFT HORIZONTAL REAR AFT SPAR, STABILIZER STATION 224 - 366 IAW USAIRWAYS EA 120107. 2 L 7 2 4F RT A2NM 2007080300089 20070803 00089 NM 2007 8 3 KCSA071265 1 20070730 A 5330 SKIN BOEING 747 7472B4B 138481B NM BS 1710 S40L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 FUSELAGE SKIN CRACKED AT BS 1710, STR-40L. 2 L 7 4 4F RT A20WE 2007080300091 20070803 00091 EU 2007 8 3 F3LA200700186 1 20070726 A 5610 SPSA320922 WINDOW AIRBUS A319 A319112 3930323 EU COCKPIT UNKNOWN A F3LA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 909FR 1 1761 DIVERSION AT FL 370, FLIGHT CREW HEARD A LOUD POP AND HISSING SOUND FROM THE CAPTAIN'S AFT SIDE WINDOW. AIRCRAFT DESCEN DED TO 14000 RA AND LANDED AT KMCI. REPLACED CAPTAIN'S FIXED WINDOW AS A PRECAUTIONARY MEASURE IAW AMM 56-11-12. PERFO RMED OPS TEST OF ANTI-ICE AND DEFOGGING SYSTEM AND CHECKED GOOD IAW AMM 30-42-00-7/0001. 2 L 7 2 4F RT A28NM 2007080300096 20070803 00096 EA 2007 8 3 QXEA200701197 1 20070712 A 2612 22802675 ELEMENT CNDAIR CL600 CL6002C10 1390015 EA FIRE LOOP SHORTED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 618QX 10205 PDX- FLIGHT 2571- FIRE SYSTEM FAULT MESSAGE CAME ON AFTER FIRE SYSTEM TEST. MAINTENANCE FOUND FIRE LOOP A (LT) SHORTED, PLACED ON MEL 26-00-1. CLEARED ON 7/19 BY REPLACING THE LOOP. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007080300103 20070803 00103 NM 2007 8 3 DHL2007784534 1 20070711 A 5311 FRAME BOEING 727 727227 1384078 NM BS 990 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 AFT CARGO COMPARTMENT BS 990, FWD AND AFT SIDES OF FRAME STR 29L-28L HAS WEB AND FRAME SURFACE CORROSION. CUT OUT DAMAG ED SHEAR TIE AREA DIM 7 BY 1 IAW B727 SRM 53-10-4, FIG 13. FABRICATED NEW SHEAR TIE FROM 7075T0 .071 DIM 8 BY 4.25 IAW B727 SRM 53-10-4, FIG 13 AND 53-10-2, FIG 5. HEAT TREATED PART TO T6 IAW FLIGHTSTAR AIRCRAFT SERVICES ENGINEERING REPOR T 2-37153-801 REV A. TREATED, PRIMED AND INSTALLED NEW SHEAR TIE AT BS 990 BETWEEN STR 28L AND 29L IAW B727 SRM 51-10-2 AND 51-30-2, FIG 1. 2 L 7 3 4F A3WE 2007080300106 20070803 00106 NM 2007 8 3 UPS07450246 1 20070704 A 5330 SKIN BOEING 747 747212B 1384886 NM BS 2725 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C EMP LT TAIL CONE SKIN FOUND DENT MARK AT STA 2725 BTN S0L AND S1L. EMP LT TAIL CONE SKIN AT BS2725 BT N STR 0 AND STR 1L SKIN REPAIRED AS PER SRM 53-30-03 FIG 1A. 2 L 7 4 4F A20WE 2007080300108 20070803 00108 NM 2007 8 3 UPS07450249 1 20070708 A 5320 SILL BOEING 747 747212B 1384886 NM BS 434-440 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D RT BS434 TO BS 440 FLOOR SILL WEB CORROSION CRACK REVEALED, CRACK LENGTH 1" APPROX. M/D BS 434 TO BS 440 DOOR 1R SILL WEB REPAIRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2007080300110 20070803 00110 EA 2007 8 3 MASA200700334 1 20070617 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA LAVATORY MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 515MJ 10117 ASH 7436 IAD - LAV EMER CALL LIGHT REMAINS ON. MAINTENANCE RESET CB M5 ON PNL 2, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007080300113 20070803 00113 EU 2007 8 3 07FDEA02645 1 20070728 A 5330 2024OCLAD063 SKIN AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 657FE 748 MDCC FR 22 5 IN UP FROM STR 13 R IS A GOUGE .5 IN BY .5 IN BY .020 IN IN THE FRAME - ZONE 230 REF A300 AMM 53-13-11. FA BRICATED NEW COUPLING IAW EA6-5310-113301. CUT OUT DAMAGE AREA IAW EA6-5310-113301. INSTALLED NEW COUPLING IAW EA6-531 0-11330. REPROTECTED ALL AREAS IAW A300-600 SRM 51-75-10. 2 L 7 2 4F RT A35EU 2007080300116 20070803 00116 NM 2007 8 3 07FDEA02637 1 20070727 A 2910 BACH8A08NN0360T HOSE BOEING 727 727233 138408A NM HYD SYSTEM FAILED A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 265FE 21671 UPON GEAR RETRACTION AFTER T/O SYS A FLUID QTY WENT TO ZERO. LT MAIN GEAR REMAINED EXTENDED. SYS A PUMPS AND FLUID SHU TOFF SWITCH WERE TURNED OFF FOR APPROX 25 MINS WITH ENGINES RUNNING. GEAR MANUALLY EXTENDED. FOUND RETRACT LINE BLOWN ON LEFT GEAR. REMOVED AND REPLACED NR 1 ENG HYD PUMP PER M/M 29-11-033-4, NR 1/2 CASE DRAIN FILTERS PER M/M 29-11-041-2 , THE RT GEAR RETRACT HOSE TO THE ACTUATOR. THE NR 2 ENG HYD PUMP PER M/M 29-11-033-4,29-11-033-4. RAN ENGS PER JRH, C YCLED ALL FLIGHT CONTROLS TO REMOVE AIR FROM SYS. REMOVED AND REPLACED "A"SYSTEM PRESSURE FILTERS PER MM 29-11-062-3. LEAK CHECKS OK. 2 L 7 3 4F RT A3WE 2007080300117 20070803 00117 EU 2007 8 3 07FDEA02648 1 20070728 A 5710 A5726021320700 BEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 657FE 748 RT WING TIP INBD T/E UPPER SURFACE STATIC BASE HAS 1.5 SQ IN AREA OF CORROSION EXTENDING UNDER BASE BETWEEN BASE AND SKI N SURFACE REF A300 AMM 57-00-00. REMOVED AND REINSTALLED WING TIP IAW A300-600 AMM 57-30-11-4. REMOVED AND REPLACED UP PER BEAM ON WING TIP IAW A300-600 AMM 57-30-11-4. REMOVED AND REPLACED STATIC WICK IAW A300-600 AMM 23-61-21-4, RESISTA NCE CHECK GOOD NAV PARK LIGHTS GOOD IAW A300-600 AMM 33-41-31. 2 L 7 2 4F RT A35EU 2007080300119 20070803 00119 EA 2007 8 3 QXEA200701224 1 20070717 A 3213 AXLE CNDAIR CL600 CL6002C10 1390015 EA RT MLG CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - RIGHT MAIN LANDING GEAR AXLE HAS LIGHT CORROSION. REMOVED CORROSION IAW SCR 046-07. 2 L 7 2 4F RT A21EA 2007080300120 20070803 00120 2007 8 3 HALA0700311 4 20070728 A 3414 UNKNOWN BOEING 767 767332 1382001 NM UNKNOWN A HALA O OTHER O OTHER CR CRUISE 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM, ON F/O'S AIRSPEED TAPE SPD LIM FLAG IN VIEW AND VMO TAPE NOT IN VIEW. PREVIOUS ITEM NR 83. NO TE: STATUS MSG WARN ELEX CAME ON WHEN SPD LIM FLAG APPEARED FIM CODE 3412XC02. T/S PER FIM 34-12-00 FIG 108A AND FIG 10 9. DID ADC BITE PER FIM 34-12-00. NO FAULTS. DID AIR DATA TEST ON P-61 PNL. TESTS OK. DID MCDP TEST 30. ALL TESTS OK. ACFT REMAINS IN LAND 3 STATUS. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007080600003 20070806 00003 NE 2007 8 6 2007UALA02742 2 20070720 A 7261 OIL SYSTEM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 ENGINE LOW A UALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 177UA 24384 724353 RTFL DUE TO NR 4 ENGINE OIL QUANTITY LOW & PRESSURE DECREASING. [08-14-07] GROUND CHECK FOUND OIL LEAKING AT NR 4 BEA RING PRESSURE TUBE HOUSING. REPLACED TUBE AND HOUSING PER MM 72-54-02. ACP'D ENG IDLE RUNNING LEAKS CHECK PER AMM 71-00- 00 -501 TEST NR 3. NO LEAKS FOUND. OIL PRESS SHOWS 113 AND OIL TEMP SHOWS 102 AFTER ENG RUNNING AT IDLE FOR 10 MINUTES. APPLIED WINDMILLING CHECKS. AIRPLANE RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080600006 20070806 00006 NM 2007 8 6 2007UALA02745 1 20070719 A 5315 STIFFENER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 246 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 CABIN FLOORBEAM STA 246 VERTICAL STIFFENER AT FWD FACE, RBL 11, CRACKED AT BEND RADIUS. [08-14-07] REMOVED AND REPLAC ED VERTICAL STIFFENER PER SRM 53-10-51, PARAGRAPH 3. AIRPLANE READY FOR SERVICE. SUSPECT FATIGUE EXACERBATED BY ASSEMBL Y PRE-LOAD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007073100068 20070731 00068 NM 2007 7 31 2007UALA02688 1 20070716 A 5230 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE AFT CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 581UA 26701 FOUND DAMAGE ON AFT CARGO DOOR ON LOWER AFT CORNER. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE. INSTALLED DOUBLER REPA IR & PERFORMED FILLET SEAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007073100081 20070731 00081 EU 2007 7 31 2007UALA02695 1 20070717 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 436UA 638 EXTERNAL FUSELAGE SKIN DENT 7 INCHES FWD OF FRAME 28 STR 42R. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER & TRIPLER AT SKIN LAP. 2 L 7 2 4F 4 F RT A28NM E40NE 2007073100082 20070731 00082 EU 2007 7 31 2007UALA02696 1 20070717 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 436UA 638 STR 42L HAS CORROSION AT FRAME 57. MAJOR REPAIR ACCOMPLISHED: INSTALLED STRINGER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007073100087 20070731 00087 NM 2007 7 31 2007UALA02702 1 20070717 A 5210 STRAP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 2R LOOSE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 R2 DOOR WILL NOT ARM. [08-17-07] REMOVED BUSTLE, TIGHTENED STRAPS AND OPS CHECKED OKAY. REINSTALLED BUSTLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007073100089 20070731 00089 NM 2007 7 31 2007UALA02704 1 20070717 A 2560 SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GIRT BAR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 L-2 DOOR SLIDE, CENTER GIRT BAR ATTACH SUPPORT, ON SLIDE ASSY, IS CORRODED. [08-17-07] REPLACED SUPPORT PLATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007073100090 20070731 00090 NM 2007 7 31 2007UALA02705 1 20070717 A 2560 SCREW BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GIRT BAR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 R-1 DOOR SLIDE, CENTER GIRT BAR SUPPORT, 2 EACH SCREWS CORRODED. [08-17-07] REPLACED SUPPORT PLATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007073100096 20070731 00096 2007 7 31 2007UALA02717 4 20070718 A 2565 SLEEVE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EVAC SLIDE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 927UA 26649 CABIN DOOR 2R ESCAPE SLIDE PACK GIRT BAR PROTECTIVE SLEEVE IS TORN AND MISSING AT RELEASE CABLE EYELET. [08-17-07] FOUND TO BE WORN. REPLACED SLIDE PACK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007073100105 20070731 00105 NM 2007 7 31 2007UALA02731 1 20070715 A 5753 FLAP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LT WING DAMAGED A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 175UA 24382 LEFT OUTBOARD MID TRAILING EDGE FLAP HAS A DEFLECTION IN ITS TRAILING EDGE OF 1 INCH OVER A LENGTH OF 38 INCHES. [08-1 4-07] EXISTING FLAP IS NOT DELAMINATED AND IS STRUCTURALLY SOUND. HOWEVER, REPLACED THE LT OUTBOARD FLAP PER MM-27-51- 04. AIRCRAFT TEST FLOWN AFTER FLIGHT CONTROL CHANGE. TEST WENT WELL. AIRPLANE RETURNED TO SERVICE. SUSPECT OB MID-TRAI LING EDGE FLAP CONTACTED BY GROUND EQUIPMENT & DEFORMED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100118 20070731 00118 NM 2007 7 31 SWAA073567 1 20070719 A 5523 65C2638420M FITTING BOEING 737 7373Y0 1384671 NM ELEVATOR TAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND RT ELEVATOR TAB INBOARD FITTING CRACKED. REMOVED AND REPLACED ELEVATOR TAB PER SWA E A. 2 L 7 2 4F RT A16WE 2007073100120 20070731 00120 2007 7 31 SWAA073565 4 20070718 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007073100121 20070731 00121 SO 2007 7 31 LR7A07058 1 20070715 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 544 4606 DURING CARGO LOADING OPERATION, FUSELAGE SKIN AND FRAME WERE DAMAGED AT FS 773E, WL 280, LBL 40 AND RBL 40. INTERIM REP AIR PERFORMED AT RQI IAW EO5330-417-ERA, AIRCRAFT FERRIED TO ANC FOR PERMANENT REPAIR OF SKIN AND FRAMES IAW LAC MEA 382 -53-07-050 . 2 H 7 4 4T A1SO 2007073100125 20070731 00125 NM 2007 7 31 UPS07550198 1 20070708 A 5230 SKIN BOEING 757 75724APF 1384969 NM AFT CARGO DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 465UP 28269 INSPECTION TYPE:C AFT LWR CARGO DOOR SKIN DENTED AND CREASED 12 INCHES AFT OF DOOR HANDLE. DENT/CREASE OUT OF LIMITS, P ERFORMED REPAIR PER SRM 52-30-01-224, SRM 52-30-01-1A. 2 L 7 2 4F RT A2NM 2007073100133 20070731 00133 NM 2007 7 31 UPS07M50204 1 20070514 A 5712 RIB DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C RIGHT SLAT TRACK 16 STRUCTURE I/B RIB CRACKED. CRACKED RIB 16 AT RIGHT WING REMOVED PER SRM 51-31-01 V2 R38. ATTACHMENT HOLES XFERRED ONTO NEW RIB PER DOUGLAS DWG ARB2873. FASTENER HOLES PICKED UP PER SRM 51-31-01 V2 R3 8. REWORKED AREA REPROTECTED PER SRM 51-31-01 V2 R38. RIB 16 INSTALLED PER SRM 51-31-01 V2 R38. OPERATIONAL TEST CARR IED OUT REFER TO TC 1177. 2 L 7 3 4F RT A22WE 2007073100136 20070731 00136 NM 2007 7 31 UPS07M50214 1 20070720 A 3350 6044115 BATTERY DOUG MD11 MD11F 3023600 NM COCKPIT DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP 48576 INSPECTION TYPE:N/A UPON TEST EMERGENCY LT BATT 1 LO ANNUNCIATED. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY 1 PER AM M 33-51-01-4. OPS TEST PASS PER AMM 33-51-01-5. 2 L 7 3 4F RT A22WE 2007073100137 20070731 00137 NM 2007 7 31 ZZDA2007202 1 20070618 A 5313 STRAP BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 INTERNAL TIE STRAP ON LONG 25L HAS CORROSION FROM STA 1002 - 1033. INSTALLED INTERNAL TIE STRAP ON LONGERON 25L FROM ST A 1002 TO STA 1003 IAW B717 SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007073100150 20070731 00150 SO 2007 7 31 RAIA00707034 1 20070719 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 813HK 145044 PRE FLT NR MX - RIC - EMERGENCY LIGHT SERVICE DOOR EXIT IDENTIFIER, SERVICE DOOR EXIT MARKER AND FLOOR PROXIMITY LIGHT I S INOP. MAINTENANCE REMOVED AND REPLACED NR 2 EMERGENCY LIGHT INVERTER CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007073100158 20070731 00158 SO 2007 7 31 RAIA00707035 1 20070721 A 3350 CONTACT EMB 145 EMB145LR 3260212 SO EXIT LIGHT DIRTY A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 833HK 145240 PRE FLT 7979 - OMA - LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE CLEANED THE CONTACTS AT THE SUBJECT LI GHT. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007073100167 20070731 00167 NM 2007 7 31 SWAA073598 1 20070720 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED RON, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007073100172 20070731 00172 NM 2007 7 31 SWAA073581 1 20070719 A 5330 655774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 790, STR 20L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007073100173 20070731 00173 NM 2007 7 31 SWAA073579 1 20070720 A 2560 6567380 WINDOW BOEING 737 7377H4 1384404 NM EVAC SLIDE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 737JW 27869 L1 DOOR SLIDE PRESSURE IND VIEWING WINDOW LOOSE. SECURED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2007073100178 20070731 00178 NM 2007 7 31 SWAA073584 1 20070719 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 727A, STR 10L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007073100182 20070731 00182 NM 2007 7 31 SWAA073589 1 20070719 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 727A, STR 7L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007073100186 20070731 00186 NM 2007 7 31 SWAA073595 1 20070719 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 500D, STR 8R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007073100195 20070731 00195 2007 7 31 2007UALA02281 4 20070627 A 2330 176421CY767 MODULE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN MALFUNCTIONED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 647UA 25284 SMOKE REPORTED COMING FROM SEAT 5D UPON DEPLANING. COCKPIT CONFIRMED SMELL. FOUND VDB FAILED, SOME INTERNAL COMPONENTS OVERHEATED. NO OTHER DAMAGE TO WIRING OR OTHER COMPONENTS. REPLACED SEAT 5CD VIDEO DISTRIBUTION BOX. SYSTEM OP CHECK ED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007073100209 20070731 00209 EA 2007 7 31 COMA0760491 1 20070721 A 5297 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CONTAMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 917CA 7017 PAX DOOR CAUTION MESSAGE ON CLIMBOUT. AIRCRAFT RETURNED TO ORF AND LANDED SAFELY. INSPECTED PAX DOOR CONNECTOR AND FOU ND TO BE CONTAMINATED. CLEANED CONNECTOR AND PERFORMED, OPS CHECK OF SYSTEM. 2 L 7 2 4F RT A21EA 2007073100217 20070731 00217 EA 2007 7 31 TRAX200701037 1 20070721 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA RT WING INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 860AS 7433 RIGHT WING EMERGENCY LIGHT IS INOP. 2 L 7 2 4F RT A21EA 2007073100221 20070731 00221 NM 2007 7 31 CALA0700373 1 20070724 A 5315 BAC1518338 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AROUND FASTENER HOLE AT STA 360, BL 0. THE CORRODED AREA WAS CUT OUT AND REPAIR ANGLES WERE INSTALLED IAW SRM 53-30-51, FIGURE 201, REPAIR 2. 2 L 7 2 4F RT A16WE 2007073100226 20070731 00226 NM 2007 7 31 UPS07650196 1 20070626 A 5414 SKIN BOEING 767 76734AF 1385212 NM LT PYLON GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 309UP 27740 INSPECTION TYPE:2C LEFT ENGINE PYLON SKIN GOUGED. BLENDED BOTH GOUGES. BOTH BLENDS OUT OF LIMIT. HFEC INSPECTION BLEN DED AREAS, NO CRACKS FOUND. DRILLED DOUBLER PER SRM 54-52-01-2. ALODINED & PRIMED DOUBLER & BLENDED AREAS. INSTALLED DOUBLER. INSTALLED FASTENERS PER SRM 54-52-01-29. REC'D FINAL ENG ER 07-2748 CUSTOMER AUTHORIZATION UPS RAA 767-54-201 57. 2 L 7 2 4F RT A1NM 2007073100234 20070731 00234 NM 2007 7 31 UPS07M50222 1 20070521 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C CTR CARGO STA 5-110 THRU 5-119 LONGERON R46 FOUND WITH CORROSION AS MARKED. CTR CARGO STA 5-110 THRU 5-119 DAMAGED LONG TRIMMED OFF PER SRM 53-10-00 V1 R38. HFEC INSP CARRIED OUT PER DAC NDTSPM R13 06-10-01.001 FOUND NO CRACK EVIDENT. REP LONG & SPLICE FAB & FASTENER HOLES PICKED UP PER SRM 53-10-00 V1 R38. LONGERON AND SPLICE INSTALLED PER SRM 51-31-01 V1 R38. 2 L 7 3 4F RT A22WE 2007080100002 20070801 00002 NM 2007 8 1 QXEA200701137 1 20070705 A 5340 STRINGER CLIP DHAV DHC8 DHC8202 2809007 NM BS 483 S24L CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - STRINGER 24L TIE CLIP CORRODED BETWEEN STATION X483.00 TO X491.00. REPAIRED IAW SRM 51-20-11, 51-40-11. 2 H 7 2 4T RT A13NM 2007080100005 20070801 00005 NM 2007 8 1 QXEA200701141 1 20070707 A 5310 SUPPORT BEAM DHAV DHC8 DHC8202 2809007 NM BS 196 S31L CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - VERTICAL AFT SUPPORT BEAM FOR AVIONICS CLOSET HAS CORROSION ON INBOARD SURFACE BEHIND INTERCOSTAL 31L AT STATIO N 196.0. REPAIRED IAW SRM 51-20-11, 51-20-36. 2 H 7 2 4T RT A13NM 2007080100007 20070801 00007 NM 2007 8 1 QXEA200701139 1 20070708 A 5340 STRINGER CLIP DHAV DHC8 DHC8202 2809007 NM BS 355 S24L CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - CORROSION ON FRAME CLIP ON STRINGER 24L STATION X355.950. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-20-36, AND 5 1-40-11. 2 H 7 2 4T RT A13NM 2007080100018 20070801 00018 EA 2007 8 1 MASA200700011 1 20070103 A 2780 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA SLATS UNKNOWN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 519LR 10260 ASH 7290 IAD - SLATS 1/2 SPEED. MX PERFORMED OPS CHECK AND OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2007080100025 20070801 00025 EA 2007 8 1 MASA200700053 1 20070125 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY MALFUNCTIONED A MASA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 07 17358 5009 7358 ASH 2894 PHX - CREW DISCHARGED THE CARGO FIRE BOTTLE, DECLARED AN EMERGENCY AND RETURNED TO THE FIELD DUE TO A CARGO SMO KE WARNING. MX REPLACED BOTH CARGO FIRE BOTTLES AND BOTH CARGO SMOKE DETECTORS. 2 L 7 2 4F RT A21EA 2007080100030 20070801 00030 2007 8 1 MASA200700117 2 20070223 A 7261 GARLOCK SEAL CNDAIR CL600 CL6002D24 1390016 EA NR 1 ENGINE LEAKING A MASA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 921FJ 15021 ASH 9390 BWI - THE A/C DIVERTED TO IAD DUE TO THE NR 1 ENGINE OIL LOW. ENGINE SHUT DOWN DURING FLIGHT. MX REMOVED AND REPLACED EDP GARLOCK SEAL O-RING. 2 L 7 2 4F RT A21EA 2007080100040 20070801 00040 EA 2007 8 1 MASA200700004 1 20070101 A 7830 THRUST REVERSER CNDAIR CL600 CL6002C10 1390015 EA RIGHT UNKNOWN A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 519LR 10260 ASH 7281 IAD - CREW ABORTED TAKEOFF DUE TO RT T/R UNSAFE CAUTION MESSAGE ON T/O ROLL. MX MEL'D T/R. 2 L 7 2 4F RT A21EA 2007080100042 20070801 00042 EA 2007 8 1 MASA200700267 1 20070513 A 5210 CAM ROLLER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37228 7228 ASH 2748 PHX - MAIN PAX DOOR WILL NOT OPEN OR CLOSE. MX FOUND CAM ROLLER CRACKED AND CHANGED OUT. 2 L 7 2 4F RT A21EA 2007080100049 20070801 00049 EA 2007 8 1 MASA200700210 1 20070416 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS UNKNOWN A MASA O OTHER J WARNING INDICATION LD LANDING 1 SW 07 27172 7172 ASH 7206 ORD - CREW DECLARED AN EMERGENCY AND LANDED WITH FLAPS AT ZERO DUE TO A FLAPS FAIL. MX COMPLIED WITH THE FLAP FAIL INSPECTION PART "A" AND COULD NOT DUPLICATE THE PROBLEM. 2 L 7 2 4F RT A21EA 2007080100051 20070801 00051 EA 2007 8 1 MASA200700178 1 20070401 A 2560 P2070011100 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27185 7185 ASH 7117 IAD - CREW REPORTED THE FWD FA FLASHLIGHT INDICATOR WAS NOT FLASHING. MX REMOVED AND REPLACED FLASHLIGHT. 2 L 7 2 4F RT A21EA 2007080100060 20070801 00060 EA 2007 8 1 MASA200700077 1 20070204 A 5240 SEAL CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17231 7231 ASH 2925 MYR - SERVICE DOOR STIFF TO OPEN. MX LUBED DOOR SEAL, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2007080100061 20070801 00061 EA 2007 8 1 MASA200700058 1 20070126 A 3230 533407 SELECTOR VALVE CNDAIR CL600 CL6002C10 1390015 EA MLG UNKNOWN A MASA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 515MJ 737 10117 ASH 7464 ORD - GEAR DISAGREE MASTER WARNING ON DEPARTURE. MX REMOVED AND REPLACED MLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2007080100063 20070801 00063 EA 2007 8 1 MASA200700188 1 20070405 A 5210 VENT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77278 7278 ASH 2923 SBA - THE PAX DOOR VENT FLAP BROKEN. FERRIED THE PLANE TO PHX WHERE MX REPLACED THE VENT DOOR HINGE ASSY. 2 L 7 2 4F RT A21EA 2007080100065 20070801 00065 EA 2007 8 1 MASA200700157 1 20070322 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG UNKNOWN A MASA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 653ML 6689 7039 ASH 7475 ORD - REPORTED A GEAR DISAGREE AFTER TAKEOFF. FERRIED THE PLANE TO IAD WHERE MAINTENANCE REMOVED AND REPLACED NLG SELECTOR VALVE.. 2 L 7 2 4F RT A21EA 2007080100069 20070801 00069 EA 2007 8 1 MASA200700208 1 20070415 A 5220 SEAL CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 932LR 15032 ASH 2690 CLT - LT FORWARD EMERGENCY EXIT DOOR SQUEALS. MX INSPECTED AND LUBED SEAL. 2 L 7 2 4F RT A21EA 2007080100082 20070801 00082 2007 8 1 MASA200700283 4 20070525 A 3100 CC670511491 CONTROL UNIT CNDAIR CL600 CL6002D24 1390016 EA MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 907FJ 9760 15007 ASH 2881 PHX - PILOT REPORTED THAT THE EICAS DCU1 CIRCUIT BREAKER HAD POPPED AND WOULD NOT RESET. ALSO REPORTED A "FUNN Y" SMELL IN THE COCKPIT. MX REMOVED AND REPLACED DCU PANEL. 2 L 7 2 4F RT A21EA 2007080100083 20070801 00083 EA 2007 8 1 MASA200700148 1 20070316 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA CABIN AIR DIRTY A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 653ML 7039 ASH 7211 IAD - AIRCRAFT RETURNED TO THE GATE FOR BURNING ODOR IN COCKPIT/FWD CABIN AREA. MX FOUND WATER SEPARATOR SCK D IRTY, REPLACED, OP GOOD. 2 L 7 2 4F RT A21EA 2007080100095 20070801 00095 EA 2007 8 1 MASA200700242 1 20070503 A 5100 NONE CNDAIR CL600 CL6002B19 1900309 EA NONE NONE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7264V 7264 ASH 2843 PHX - EMERG EXIT LIGHTS AT PAX AND SERVICE DOORS INOP. NO DEFFECT NOTED, LIGHT WAS GLOW TYPE. 2 L 7 2 4F RT A21EA 2007080100099 20070801 00099 2007 8 1 MASA200700262 4 20070511 A 2561 P0640101 LIFE VEST CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 651BR 7139 ASH 1018 HNL - INFANT LIFE VEST WAS MISSING. MX INSTALLED A NEW LIFE VEST. 2 L 7 2 4F RT A21EA 2007080100122 20070801 00122 EA 2007 8 1 MASA200700165 1 20070326 A 5220 ESCAPE ROPE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75999 7471 ASH 7185 IAD - EMERG DOOR ESCAPE ROPE COVER LOOSE. RESECURED. 2 L 7 2 4F RT A21EA 2007080100128 20070801 00128 EA 2007 8 1 MASA200700009 1 20070103 A 2760 SENSOR CNDAIR CL600 CL6002B19 1900309 EA SPOILERS DIRTY A MASA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 570ML 7206 ASH 7191 CLT - AIRCRAFT ABORTED TAKEOFF DUE TO SPOILER CONFIG MESSAGE. MX CLEANED SENSOR. 2 L 7 2 4F RT A21EA 2007080100136 20070801 00136 EA 2007 8 1 MASA200700281 1 20070523 A 2611 47359719 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY NO TEST A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 27314 7314 ASH 7307 BMI - PILOT REPORTED THE CARGO FIRE-EXT TEST 1 INOP. MX REMOVED AND REPLACED NR 1 DETECTOR. 2 L 7 2 4F RT A21EA 2007080100139 20070801 00139 EA 2007 8 1 MASA200700057 1 20070126 A 5270 SENSOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT FALSE ACTIVATION A MASA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 17175 7175 ASH 7450 ORD - LT EMERGENCY EXIT DOOR CAUTION IN FLIGHT. MX CLEANED SENSORS OP CHECK GOOD. 2 L 7 2 4F RT A21EA 2007080100152 20070801 00152 EA 2007 8 1 MASA200700090 1 20070210 A 2611 NONE CNDAIR CL600 CL6002B19 1900309 EA SMOKE DETECTOR NONE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17358 7358 ASH 7358 PHX - LAV SMOKE DETECTOR WOULD NOT TEST. MX PERFORMED THE TEST WITH NO FAULTS NOTED. OPS TEST GOOD. 2 L 7 2 4F RT A21EA 2007080100154 20070801 00154 EA 2007 8 1 MASA200700174 1 20070331 A 2520 OXYGEN MASK CNDAIR CL600 CL6002B19 1900309 EA CABIN UNWANTED DEPLOY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 571ML 7209 ASH 7227 DSM - ROW 5 D/F PAX O2 MASK FELL DOWN. MX RESECURED THE O2 MASKS. 2 L 7 2 4F RT A21EA 2007080100156 20070801 00156 2007 8 1 MASA200700172 4 20070330 A 2561 P0640101 LIFE VEST CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 646BR 826 7392 ASH 1019 HNL - ONE INFANT LIFE VEST WAS MISSING AND ANOTHER INFANT LIFE VEST SEAL BROKEN. MX INSTALLED AND REPLACED THE INFANT LIFE VESTS. 2 L 7 2 4F RT A21EA 2007080100158 20070801 00158 EA 2007 8 1 MASA200700286 1 20070529 A 3260 16600103 UPLOCK ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77195 7195 ASH 7172 GSP - CREW REPORTED A GEAR DISAGREE WARNING (NOSE GEAR). MX REMOVED AND REPLACED UPLOCK. 2 L 7 2 4F RT A21EA 2007080100171 20070801 00171 EA 2007 8 1 MASA200700108 1 20070220 A 5260 RING CNDAIR CL600 CL6002B19 1900309 EA ESCAPE ROPE MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75999 7471 ASH 7367 IAD - RT OVERWING EXIT ESCAPE ROPE D-RING MISSING. MX REINSTALLED D-RING. 2 L 7 2 4F RT A21EA 2007080100177 20070801 00177 EA 2007 8 1 MASA200700236 1 20070423 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77195 7195 PRESSURE BULKHEAD WEB FS 621 THAT SURROUNDS THE LINTEL ATTACHMENT FITTING IS CRACKED. REPAIRED. 2 L 7 2 4F RT A21EA 2007080100182 20070801 00182 EA 2007 8 1 MASA200700115 1 20070207 A 2910 601R7528661 LINE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM DAMAGED A MASA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 7291Z 7291 ASH 2771 ICT - PILOT RETURNED TO FIELD AND DECLARED AN EMERGENCY FOR HYDRAULIC 1 LOW PRESS MESSAGE. MX REPAIRED PRESSUR E LINE AND SUPPLY LINE. 2 L 7 2 4F RT A21EA 2007080100184 20070801 00184 EA 2007 8 1 MASA200700013 1 20070103 A 2780 SLAT SYSTEM CNDAIR CL600 CL6002C10 1390015 EA OUT OF RIG A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 502MJ 10050 ASH 7224 ORD - SLAT FAIL CAUTION MESSAGE. MX REATTACHED RT NR 4 OB ACTUATOR TORQUE TUBE AND RE-RIGGED SLATS. 2 L 7 2 4F RT A21EA 2007080100196 20070801 00196 EA 2007 8 1 MASA200700044 1 20070121 A 3230 533407 SELECTOR VALVE CNDAIR CL600 CL6002D24 1390016 EA MLG MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 939LR 3925 15039 ASH 2908 PHX - MLG DID NOT RETRACT. MX REMOVED AND REPLACED MLG SELECTOR VALVE. NO FURTHER DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007080200003 20070802 00003 EA 2007 8 2 MASA200700198 1 20070408 A 2560 A1181030 STRAP CNDAIR CL600 CL6002C10 1390015 EA FLASHLIGHT BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 513MJ 10111 ASH 7320 IAD - FORWARD F/A EMERGENCY FLASHLIGHT STRAP BROKEN. REMOVED AND REPLACED THE STRAP. 2 L 7 2 4F RT A21EA 2007080200006 20070802 00006 EA 2007 8 2 MASA200700291 1 20070513 A 5753 RIB CNDAIR CL600 CL6002B19 1900309 EA TE FLAP DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27191 7191 DAMAGE TO RT I/B FLAP RIB FLAP. REPAIRED LT I/B FLAP RIB FLAP. 2 L 7 2 4F RT A21EA 2007080200012 20070802 00012 EA 2007 8 2 MASA200700293 1 20070601 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCONNECTED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 154SF 7154 ASH 2923 IAD - FWD ISLE EXIT LIGHT STRIP INOP. MX RECONNECTED FWD STRIP. OP CK GOOD. 2 L 7 2 4F RT A21EA 2007080200013 20070802 00013 EA 2007 8 2 MASA200700295 1 20070601 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA EXTINGUISHER OPEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17275 7275 ASH 2923 PHX - FWD CABIN FIRE EXT BRACKET WILL NOT LATCH. MX RESECURED BRACKET. 2 L 7 2 4F RT A21EA 2007080200016 20070802 00016 EA 2007 8 2 MASA200700301 1 20070603 A 3350 LENS CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27318 7318 ASH 2782 LAS - MID CABIN FA EMERGENCY CALL LIGHT RED LENS COVER WAS MISSING. MX INSTALLED A NEW LENS COVER. 2 L 7 2 4F RT A21EA 2007080200028 20070802 00028 NM 2007 8 2 UIEA200700289 1 20070725 A 5313 STRINGER BOEING 747 747271C 1384869 NM BS 1220 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 CORROSION ON STRINGER S-15 RIGHT AT BS 1220 4 EACH RIVETS HEADS POPPED WITH CORROSION NOTED UNDER THE RIVET. PRIMER LOO SE AND FLAKING OFF THE STRINGER AT SAME AREA. REMOVED FASTENER AND STRAP IAW SRM 51-30-02. CLEANED STRINGER 15R AT BS 1220 IAW MM 20-11-14. TREATED AND PRIMED AREA AND INSTALLED NEW FASTENERS IAW SRM 51-30-02. NO CORROSION NOTED ON STRI NGER. 2 L 7 4 4F A20WE 2007080200035 20070802 00035 NM 2007 8 2 UIEA200700296 1 20070725 A 5315 FLOORBEAM BOEING 747 747271C 1384869 NM BS 330 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 CRACK ON FORWARD FACE OF FLOORBEAM WEB (UPPER DECK) STA 330 LEFT SIDE AT FRAME TO FLOORBEAM ATTACHMENT. REPAIRED CRACKE D FLOORBEAM WEB AT STA 330 LEFT PER SB 747-53-2272 DRAWING NR 65B28068 SRM 51-30-02 AND SRM 51-10-01. AREA CHECKED FOR FOD. 2 L 7 4 4F A20WE 2007080200036 20070802 00036 EU 2007 8 2 F3LA200700182 1 20070724 A 5340 D5347112420000 SKATE ANGLE AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 803FR 5201 2017 DURING C-3 CHECK, INSPECTION REPORTED MODERATE CORROSION IN NUT PLATE MOUNT HOLES OF SKATE ANGLE AFT OF L2 DOOR GIRT BAR CUT OUTS. REMOVED AND REPLACED SKATE ANGLE IAW A318 SRM 51-42-11, PARA. 5, 6 AND 13. 2 L 7 2 4F RT 2007080200037 20070802 00037 EU 2007 8 2 F3LA200700183 1 20070724 A 5340 D5347112420100 SKATE ANGLE AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 803FR 5201 2017 DURING C-3 CHECK, INSPECTION REPORTED MODERATE CORROSION IN NUT PLATE MOUNT HOLES OF SKATE ANGLE AFT OF R2 DOOR GIRT BAR CUTOUTS. REMOVED AND REPLACED SKATE ANGLE IAW A318 SRM 51-42-11, STEPS B AND D. 2 L 7 2 4F RT 2007080200038 20070802 00038 EU 2007 8 2 F3LA200700184 1 20070724 A 5310 PLATE AIRBUS A318 A318111 3940019 EU FLOORBEAM DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 803FR 5201 2017 DURING C-3 CHECK, INSPECTION REPORTED HOLES ON JOINT PLATE COMMON TO FLOORBEAM AT -Y1292 BETWEEN FR68 AND FR69 DAMAGED. FABRICATED AND INSTALLED REPLACEMENT JOINT PLATE IAW A318 SRM 53-41-14, FIG 17, AND 51-42-11, STEP 7B. 2 L 7 2 4F RT 2007080200054 20070802 00054 EA 2007 8 2 SWIA200718527 1 20070619 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 713SK 10174 STA 280 FLOORBEAM CRACKED AT BUTTLINE 9, DISCOVERED AT C-CHECK. INSTALLED REPLACEMENT STA 280 FLOORBEAM, DOUBLERS AND " T" BRACKETS AT BUTTLINE 9 PER SB670BA-53-026. 2 L 7 2 4F RT A21EA 2007080200057 20070802 00057 EA 2007 8 2 SWIA200718530 1 20070619 A 5210 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 713SK 10174 AFT DRAG ANGLE OF PAX DOOR IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS PER REO:670-52-11-072. 2 L 7 2 4F RT A21EA 2007080200058 20070802 00058 EA 2007 8 2 SWIA200718531 1 20070619 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 1098 DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 713SK 10174 FOUND ONE RIVET DAMAGED BY LIGHTNING AT FS 1098.2 JUST FORWARD OF THE EQUIPTMENT BAY DOOR, DISCOVERED AT C-CHECK. REMOV ED AND INSTALLED NEW RIVET IAW CRJ700/900 SRM 51-42-06-001-001-A01. 2 L 7 2 4F RT A21EA 2007080200061 20070802 00061 EA 2007 8 2 SWIA200718534 1 20070714 A 2780 TORQUE TUBE CNDAIR CL600 CL6002C10 1390015 EA NR 1 SLAT DISCONNECTED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 609SK 10020 FOUND "SLATS FAIL" CAUTION MESSAGE. RECONNECTED INBOARD TORQUE TUBE TO NR 1 SLAT ACTUATOR ON RIGHT WING PER AMM 27-81-0 1. 2 L 7 2 4F RT A21EA 2007080200062 20070802 00062 EA 2007 8 2 SWIA200718535 1 20070725 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BROKEN A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 932SW 7714 FLT 6530 - EMERGENCY EXIT SIGN AT MAIN CABIN DOOR IS INOP. REPAIRED A BROKEN WIRE TO EXIT SIGN. OPS CHECK GOOD IAW WM 20-00-00. 2 L 7 2 4F RT A21EA 2007080200063 20070802 00063 EA 2007 8 2 SWIA200718536 1 20070714 A 7830 32725706 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 411SW 6981 6981 7067 RIGHT THRUST REVERSER UNLOCK CAUTION MESSAGE ILLUMINATED IN FLIGHT. RETURNED TO FIELD. REPLACED RIGHT LOWER INBOARD THR UST REVERSER BALLSCREW ACTUATOR IAW MM 78-32-01. 2 L 7 2 4F RT A21EA 2007080200067 20070802 00067 WP 2007 8 2 IXXA07SMN169S 1 20070630 A 5330 SKIN DOUG DC8 DC873F 302199F WP ZONE 100 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND CORROSION AT FLIGHT STATION 1510 LONGERON 27 TO 31 RIGHT, DOUBLER AFT FUSELAGE SIDE, AFT OF D-PIT DOOR. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PA RTS. APPLIED SEALANT TO FAYING SURFACE. INSTALLED REPAIR PARTS AND NEW FATNERS IAW SRM 53-2-1 FIGURE 7 SHEET 1, FAA FO RM 8110-3 NR 07284 DATED 06-27-07 SEMAN DRAWING NUMBER ED-4052 REV "1" DATED 06-23-07, DC8 SRM 51-1-21, SRM 51-1-20D, DC 8 SRM 51-1-8B, DC8 SRM 51-1-11, AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007080200070 20070802 00070 EU 2007 8 2 07FDEA02640 1 20070709 A 5330 A53978149 SKIN AIRBUS 310 A310222 3930315 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 420FE 339 LOWER FUSELAGE: PREVIOUS REPAIR FOUND LOCATED ON LT FR360/61 AND STGR 42/43. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF WAS ACCOMPLISHED USING FAA APPROVAL. THE EXISTING REPAIR WAS EVALUATED AND FOUND NOT TO CONFORM T O AN EXISTING SRM REPAIR. NEW REPAIR WAS ACCOMPLISHED PER SRM 53-10-12 FIG 225 SHEET1. 2 L 7 2 4F RT A35EU 2007080200072 20070802 00072 EU 2007 8 2 07FDEA02642 1 20070629 A 5330 SKIN AIRBUS 310 A310222 3930315 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 FUSELAGE, RT FUSELAGE SKIN SURFACE WITH MISSING MATERIAL BETWEEN FR 25 AND 26/32 AT STR 29 RT AN APPROVAL FOR THE MISSIN G MATERIAL WAS OBTAINED. FEDEX EA 6-5330-113154 WAS ACCOMPLISHED. 2 L 7 2 4F RT A35EU 2007080200074 20070802 00074 WP 2007 8 2 IXXA07SMN172S 1 20070630 A 5310 STRUCTURE DOUG DC8 DC873F 302199F WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT FUSELAGE NOSE SECTION ACS MODIFICATION DOUBLER HEAT EXCHANGER COMPARTMENT LOWER AFT IAMB CORNER CRACKED AT FLIGHT STATION 12.000 LONGERON 27 RIGHT. REMOVED FASTENER AS NEEDED TO PERFORMED REPA IR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION AFTER DAMAGED REMOVED. FABRICATED REPAIR PA RTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW FAA FORM 8110-3 N UMBER 07330 DATED 07-18-07, SEMAN DRAWING NUMBER ED-4575, DC8 SRM 51-1-21, DC8 NDT SPM PART 06-10-01-001, SRN 242-2, DC8 SRM 51-1-2B, SRM 51-1-8B, SRM 51-1-11, 51-1-20D, AND SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007080200078 20070802 00078 NM 2007 8 2 2007UALA02280 1 20070627 A 3350 767 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR SLIDE INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 554UA 26644 DOOR 1R SLIDE ARM LIGHT NOT ON WITH DOOR ARMED. CLEANED CONTACTS ON PROX SWITCH AND REPLACED LED LAMP. CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080200080 20070802 00080 NM 2007 8 2 2007UALA02800 1 20070723 A 3397 58781 FEEDER CABLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 202UA 24717 EEL LIGHTS INOP FROM ROW 12-15. REPLACED EEL LIGHT CABLE FROM ROW 12 TO 15. OPS CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080200084 20070802 00084 NM 2007 8 2 2007UALA02804 1 20070723 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 540UA 25252 EEL LIGHT INOP AT FWD CLOSET. REPLACED LAMP, TRACK BASE, HOUSING COVER AND END CAPS. OP CKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080200090 20070802 00090 NM 2007 8 2 2007UALA02810 1 20070724 A 5754 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT WING SLAT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 LEFT WING NR 1 L/E SLAT LOWER SKIN CRACK THREE INCHES LONG INBOARD OF ACTUATOR. FABRICATED AND INSTALLED EXTERNAL DOUBL ER-FILLER REPAIR PER SRM 57-43-01, REPAIR NR 6. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080200092 20070802 00092 NM 2007 8 2 2007UALA02812 1 20070724 A 3510 OXYGEN MASK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 CAPT OXYGEN MASK LEAKING. MASK DOES NOT LEAK WHEN STOWED, ONLY LEAKS WHEN HOSE PRESSURIZED. REPLACED OXYGEN MASK AND S ERVICED OXYGEN SYSTEM TO FULL. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080200093 20070802 00093 NM 2007 8 2 2007UALA02813 1 20070724 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 890-892 S10R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 338UA 24242 EXTERNAL FUSELAGE SKIN CRACKED AT CHEM-MILLED STEP, AT STR 10R, FROM STA 890-892. FABRICATED AND INSTALLED EXTERNAL DOU BLER-FILLER REPAIR PER MM 53-31-96 FIGURE 602. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080200099 20070802 00099 NM 2007 8 2 2007UALA02819 1 20070724 A 3350 CAP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 F/A REPORTS AISLE LIGHT AT SEAT 1B END CAP IS COMING OFF. INSTALLED CAP AND SECURED CONNECTOR AND EEL CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080200100 20070802 00100 NM 2007 8 2 2007UALA02820 1 20070724 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 649UA 25286 RIGHT SIDE EXTERNAL OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. TROUBLESHOT AND FOUND BAD LAMP. REMOVED AND REPLACED LAMP. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080200102 20070802 00102 NM 2007 8 2 HNAA0700140 1 20070707 A 5313 85300291101 STRINGER DHAV DHC8 DHC8102 2809003 NM BS 467 S29R CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 839EX 226 LIGHT CORROSION AT STR 29 AND X467.00. 2 H 7 2 4T RT A13NM 2007080200104 20070802 00104 NM 2007 8 2 HNAA0700155 1 20070725 A 2910 87950010207 LINE DHAV DHC8 DHC8102 2809003 NM HYDRAULIC SYS LEAKING A HNAA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 07 906HA 009 HYD LEAK IN NR 2 GEAR WELL LEFT SIDE ABOVE JET PIPE. ROA MX CANNOT REACH LEAK, CREW WILL TAKE A/C TO HANGAR, LOOKING TO TAKE A/C 980 AS A SPARE WILL HAVE TO USE LOWER COWL FOR 980. SWAP 980 AND TAKING LOWER COWL OFF OF 906. FOUND RIGHT L IFT DUMP SPOILER HYD LINE LEAKING. INSTALLED TEMP FLEX LINE. LEAK CHECK GOOD. 2 H 7 2 4T RT A13NM 2007080200105 20070802 00105 NM 2007 8 2 ZZDA2007222 1 20070605 A 5313 LONGERON BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT (WASTE TANK AREA) AT LONGERON 26L END TIE FITTING. INSTALLED NEW END TIE FITTING LON GERON 26L AT AFT CARGO COMPARTMENT IAW B717 SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007080200106 20070802 00106 NM 2007 8 2 ZZDA2007223 1 20070605 A 5313 LONGERON BOEING 717 717200 1383700 NM BS 1053 L25L CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT (WASTE TANK AREA) AT LONGERON 25L END TIE FITTING. INSTALLED NEW END TIE FITTING LON GERON 25L AT AFT CARGO COMPARTMENT STA 1053 IAW B717 SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007080200107 20070802 00107 NM 2007 8 2 ZZDA2007224 1 20070605 A 5313 LONGERON BOEING 717 717200 1383700 NM BS 1037-1053 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT (WASTE TANK AREA) AT LONGERON 24LT END TIE FITTING. INSTALLED NEW END TIE FITTING LO NGERON 24L AT AFT CARGO COMPARTMENT STA 1037 TO STA IAW B717 SRM 51-41-02 AND SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007080200109 20070802 00109 NM 2007 8 2 ZZDA2007226 1 20070605 A 5313 LONGERON BOEING 717 717200 1383700 NM BS 1053 L22L CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT (WASTE TANK AREA) AT LONGERON 22L END TIE FITTING. INSTALLED NEW END TIE FITTING LON GERON 22L AT AFT CARGO COMPARTMENT STA 1053 IAW B717 SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007080200111 20070802 00111 NM 2007 8 2 ZZDA2007228 1 20070607 A 5313 LONGERON BOEING 717 717200 1383700 NM BS 813-832 L26L CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 FS 813 - 832 L AND LONG 26L, EXTERNAL LONGERON HAS CORROSION AT FWD AND AFT ENDS. INSTALLED EXTERNAL LONGERON AT STA 81 3 TO 832 IAW B717 SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007080200112 20070802 00112 NM 2007 8 2 ZZDA2007229 1 20070607 A 5330 SKIN BOEING 717 717200 1383700 NM BS 898.5-1053 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 AFT CARGO COMPARTMENT REAR SKIN PANEL CORROSION ON LT EDGE FINGER DOULBER FROM BS 898.5 TO BS 1053. INSTALLED NEW FINGE R DOUBLER FROM BS 898.5 TO BS 1053 LT PER B717 SRM 51-41-02. 2 L 7 2 4F TR A6WE 2007080200117 20070802 00117 NM 2007 8 2 KCSA071249 1 20070724 A 5320 SUPPORT FITTING BOEING 747 7472B4B 138481B NM BS 947 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NR 3 MED NR 6 STOP SUPPORT FITTING CRACKED AT I/B AFT AREA. 2 L 7 4 4F RT A20WE 2007080200118 20070802 00118 NM 2007 8 2 KCSA071250 1 20070724 A 5310 STOP FITTING BOEING 747 7472B4B 138481B NM DOOR FRAME CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NR 3R MED, NR 6 STOP SUPPORT FITTING IS CRACKED AT I/B AFT AREA OF FITTING. 2 L 7 4 4F RT A20WE 2007080200121 20070802 00121 NM 2007 8 2 ZZDA2007235 1 20070610 A 5313 STRINGER SPLICE BOEING 717 717200 1383700 NM BS 898.5 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 BS 898.5 LONGERON 28L STRINGER SPLICE IS CORRODED. INSTALLED SPLICE ON LONGERON 28L ON BS 898.5 PER B717 SRM 51-41-01 A ND SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007080200123 20070802 00123 NM 2007 8 2 ZZDA2007237 1 20070610 A 5313 STRINGER SPLICE BOEING 717 717200 1383700 NM BS 898.5 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 BS 898.5 LONGERON 26L STRINGER SPLICE IS CORRODED. INSTALLED SPLICE AT AFT CARGO COMPARTMEN AT STA 898.5 LONGERON 26L A S PER B717 SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007080200124 20070802 00124 NM 2007 8 2 ZZDA2007238 1 20070616 A 5320 INTERCOSTAL BOEING 717 717200 1383700 NM BS 927-946 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 BS 927 LONGERON 29R FUSELAGE FRAME HAS CORROSION. INSTALLED INTERCOSTAL AT STA 927 TO STA 946 STR 29R AS PER B717 SRM 5 1-41-02 AND SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007080200125 20070802 00125 NM 2007 8 2 ZZDA2007239 1 20070610 A 5312 BULKHEAD BOEING 717 717200 1383700 NM BS 1053 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 AFT PRESSURE BULKHEAD LOWER CHORD DOUBLER IS CORRODED STA 1053 BETWEEN L-29L TO 29R. INSTALLED LOWER CHORD ANGLE DOUBLE R AT AFT PRESSURE BULKHEAD STA 1053 BETWEEN L-29L TO 29R AS PER B717 SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007080200128 20070802 00128 NM 2007 8 2 ZZDA2007242 1 20070612 A 5310 RIB BOEING 717 717200 1383700 NM STA 851 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 LEFT FUSELAGE STA 851, FAIRING SUPPORT RIB HAS CORROSION ON LOWER END. INSTALLED NEW FAIRING SUPPORT RIB AT LT STA 851 IAW B717 SRM 51-41-02. 2 L 7 2 4F TR A6WE 2007080200129 20070802 00129 NM 2007 8 2 ZZDA2007243 1 20070612 A 5310 RIB BOEING 717 717200 1383700 NM BS 832 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 LEFT FUS FAIRING SUPPORT RIB AT STA 832 IS CORRODED. INSTALLED NEW FAIRING SUPPORT RIB AT LEFT STA 832 IAW B717 SRM 51- 41-02 AND SRM 51-41-056. 2 L 7 2 4F TR A6WE 2007080200131 20070802 00131 2007 8 2 ZZDA2007249 4 20070725 A 2565 D29982225 SLIDE BOEING 717 717200 1383700 NM L1 DOOR LOOSE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 899AT 55049 L1 EMERGENCY SLIDE APPEARS LOOSE. REMOVED AND REPLACED L1 DOOR SLIDE REF AMM 25-61. 2 L 7 2 4F TR A6WE 2007080200132 20070802 00132 2007 8 2 VNAA0707013 4 20070722 A 3418 C16258AA AOA CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE RIGHT FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 718PS 6597 10175 CREW REPORTED A STALL FAIL CAS MESSAGE ON CLIMBOUT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REMO VED AND REPLACED THE ANGLE OF ATTACK IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007080200133 20070802 00133 NM 2007 8 2 HNAA070156 1 20070726 A 2120 7786848 MIXER BOX DHAV DHC8 DHC8102 2809003 NM CONDENSOR WORN A HNAA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 EA 07 982HA 18862 5247 380 CABIN GOT VERY HOT AFTER TAKEOFF, FLIGHT DECK COLD. AFTER SEVERAL PAX GOT SICK, F/A INFORMED CREW THAT THE CABIN WAS TO O HOT TO CONTINUE. ACFT WAS APPROX 20 MILES OUT OF LGA, ACFT RETURNED TO FIELD. CONTACTED LGA MX. ACFT HAS BEEN WRITT EN UP TWICE BEFORE. DUCTING UNDER FLOOR APPEARS TO BE IN GOOD SHAPE. FLIGHT DECK IS COLD WITH GOOD DUCTING TEMP. LGA HAS SEVERAL BROKE ACFT WILL FERRY TO MDT. CLAMP UNDER DORSAL FIN LOOSE, TIGHTENED AND REMOVED AND REPLACED CONDENSER MI XER. 2 H 7 2 4T RT A13NM 2007080200134 20070802 00134 NM 2007 8 2 KCSA071262 1 20070727 A 5315 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 460 DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 MAIN DECK FLOORBEAM WEB IS DENTED AT STA 460, RBL 103, WL 189 TO 199. 2 L 7 4 4F RT A20WE 2007080200137 20070802 00137 NM 2007 8 2 USAA070583 1 20070727 A 5313 STRINGER BOEING 737 7374B7 1384702 NM BS 360 S15L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 STR 15L AT STA 360, STRINGER EXTENSION HAS CRACK. INSTALLED NEW STRINGER EXTENSION PER SRM 51-40-02, DEFECT SIZE: 1 IN CH. 2 L 7 2 4F RT A16WE 2007080200138 20070802 00138 NM 2007 8 2 USAA070582 1 20070727 A 5310 DOOR FRAME BOEING 737 7374B7 1384702 NM BS 492.4 S24R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 BS 492.4 & S-24R HAS CRACK. INSTALLED DOUBLER PER EA 98809, DEFECT SIZE: .4 INCH. 2 L 7 2 4F RT A16WE 2007080200141 20070802 00141 NM 2007 8 2 SWAA073706 1 20070726 A 5322 6546546 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 727A, STR 22L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007080200142 20070802 00142 NM 2007 8 2 SWAA073702 1 20070726 A 5311 6546547 FRAME BOEING 737 7373H4 1384600 NM BS 727D S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200143 20070802 00143 NM 2007 8 2 SWAA073703 1 20070726 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM BS 747 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200144 20070802 00144 NM 2007 8 2 SWAA073691 1 20070726 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200146 20070802 00146 NM 2007 8 2 SWAA073692 1 20070726 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200147 20070802 00147 NM 2007 8 2 SWAA073704 1 20070726 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM BS 867 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200148 20070802 00148 NM 2007 8 2 SWAA073713 1 20070726 A 5311 6546555 FRAME BOEING 737 7373K2 13844BA NM BS 867 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200149 20070802 00149 NM 2007 8 2 SWAA073710 1 20070726 A 5311 6546557 FRAME BOEING 737 7373K2 13844BA NM BS 887 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200150 20070802 00150 NM 2007 8 2 SWAA073685 1 20070726 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200151 20070802 00151 NM 2007 8 2 SWAA073684 1 20070726 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200152 20070802 00152 NM 2007 8 2 SWAA073701 1 20070726 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200153 20070802 00153 NM 2007 8 2 KCSA071263 1 20070727 A 5313 LONGERON BOEING 747 7472B4B 138481B NM BS 1371 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 LEFT WHEEL WELL OVERWING LONGERON WEB IS CORRODED AT STA 1371, WL 150, LBL 122. 2 L 7 4 4F RT A20WE 2007080200155 20070802 00155 2007 8 2 SWAA073676 4 20070726 A 2565 6557463 GIRT BAR BOEING 737 7373H4 1384600 NM FUSELAGE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER MM. 2 L 7 2 4F RT A16WE 2007080200156 20070802 00156 NM 2007 8 2 SWAA073693 1 20070726 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM BS 360 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200157 20070802 00157 NM 2007 8 2 SWAA073698 1 20070726 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM BS 360 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200158 20070802 00158 NM 2007 8 2 SWAA073705 1 20070726 A 5520 656531012 TORQUE TUBE BOEING 737 7373Y0 1384671 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, RIGHT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR OUTPUT TORQUE TUBE PE R MM. 2 L 7 2 4F RT A16WE 2007080200159 20070802 00159 NM 2007 8 2 SWAA073681 1 20070726 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM BS 500C S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007080200160 20070802 00160 NM 2007 8 2 SWAA073695 1 20070726 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM BS 500C S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007073000152 20070730 00152 NM 2007 7 30 AWXA200700883 1 20070711 A 5554 D5537131800200 HINGE FITTING AIRBUS A319 A319132 3930340 NM ZONE 300 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5964295, NR 3 RUDDER HINGE BEARING HAS EXCESSIVE PLAY, VERTICLE STABILZER STATION 2 279/RIB 5. REPLACED NR 3 RUDDER HINGE FITTING, VERTICLE STABILZER STATION 2279/RIB 5 IAW A319 AMM 55-36-41. 2 L 7 2 4F RT A28NM 2007073000153 20070730 00153 NM 2007 7 30 NWAA072543101 1 20070721 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319114 3930350 NM EMERGENCY LIGHTS MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 301NB 17231 1058 DURING OVERNIGHT LINE CHECK OF EMERGENCY ESCAPE LIGHT SYSTEM, EPSU INT LOAD AFT L FAULT MESSAGE DISPLAYED. REPLACED AFT 13WL EMERGENCY LIGHT POWER SUPPLY UNIT, CHECKS OK. 2 L 7 2 4F RT A28NM 2007073000164 20070730 00164 NM 2007 7 30 DL76S070937 1 20070608 A 5315 BAC15063116 FLOORBEAM BOEING 767 767332 1382001 NM BS 287 RBL 26 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 130DL 24080 DURING HMV3 AT MOBILE AEROSPACE ENGINEERING, FOUND MAIN CABIN FLOORBEAM T-CAP EXFOLIATED AT RBL 26, STA 287. REMOVED DA MAGED SECTION OF T-CAP AND REPAIRED PER SRM 53-00-51D. 2 L 7 2 4F RT A1NM 2007073000172 20070730 00172 NM 2007 7 30 NWAA072515533 1 20070714 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 533US 24264 EMERGENCY ESCAPE LIGHTS AT 4B AND 13D INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATTERY AT STA 369, CHECKS OK. 2 L 7 2 4F RT A2NM 2007073000175 20070730 00175 NM 2007 7 30 DHL2007741501 1 20070702 A 5330 SKIN BOEING 727 7272Q9 138448M NM BS 720C-720D DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 FUSELAGE SKIN HAS DRILL DAMAGE AT STR 20R BETWEEN BS 720C AND BS 720D AND DRILLED OFF SCREWS. CUTOUT DAMAGED AREA (DIME NSION 3.5" BY 4.5"). FABRICATED REPAIR DOUBLER FROM 2024-T3 0.071" PO NR 9005314 (DIMENSION 13.5" BY 8") AND 1 EA FILLE R FROM 2024-T3 0.063 PO NR 9005089 (DIMENSION 4.5 BY 3.5") IAW B-727 SRM 53-30-2 FIGURE 2 AND 53-30-3 FIGURE 4. TREATED AND PRIMED PARTS AND AREA IAW B-727 SRM 51-10-2 AND INSTALLED REPAIR PARTS AND FUSELAGE SKIN STRINGER 20R BETWEEN BS 72 0C AND BS 720D IAW B-727 SRM 53-30-3 FIG 4 AND 51-30-2. REMOVED DRILLED OFF SCREWS IAW B-727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007101800009 20071018 00009 2007 10 18 U30A200700003 4 20070713 A 2565 D30665309 SLIDE AIRBUS 320 A320214 3930316 EU PAX DOOR PARTIAL INFLATE A U30A K NONE O OTHER IN INSP/MAINT 1 EA 17 262AV 9525 9525 1725 AIRCRAFT IN MAINTENANCE. MPD TASK 25624104, "OPERATIONAL TEST OF THE ESCAPE-SLIDE DEPLOYMENT, FWD/AFT PASSENGER/CREW DOO R" WAS BEING PERFORMED ON THE L2 PAX/CREW DOOR SLIDE/RAFT. THE SLIDE/RAFT FAILED TO DEPLOY PROPERLY. THE PACK OPENED UP & THE BOTTLE DROPPED DOWN BELOW THE DOOR, BUT DID NOT START INFLATING THE SLIDE/RAFT ASSY. ONLY AFTER COAXING BY THE MAI NTENANCE PERSONNEL IN THE CABIN, DID THE BOTTLE PRESSURE RELEASE & START TO INFLATE. MAINTENANCE R&R THE SLIDE/RAFT ASSY PER AMM 25-62-44-400-007 & REPLACED THE DIAPHRAGM IN THE DOOR DAMPER/EMERGENCY CYLINDER & SERVICED PER AMM 52-10-00-610 -001. AIRCRAFT RETURNED TO SERVICE. UPDATE AMMENDMENT: AFTER DETAILED REVIEW, THE L2 PAX/CREW APPEARED NOT TO OPEN FULLY 2 L 7 2 4F RT A28NM 2007073000197 20070730 00197 EU 2007 7 30 AWXA200700890 1 20070714 A 5554 D5537131800200 HINGE FITTING AIRBUS 320 A320232 3930326 EU ZONE 300 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 654AW 1050 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5898133, NR 4 RUDDER HINGE FITTING WORN, VERTICAL STABILIZER STATION 2632/RIB 6. R EPLACED NR 4 RUDDER HINGE FITTING, VERTICAL STABILIZER STATION 2632/RIB 6 IAW A320 AMM 55-36-41. 2 L 7 2 4F RT A28NM 2007073000206 20070730 00206 CE 2007 7 30 DXTA200702355 1 20070721 A 7930 OIL SYSTEM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LT ENGINE MALFUNCTIONED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 956QS 7500156 ON THE TAKEOFF ROLL WITH POWER (N1) INCREASING THROUGH 86 PERCENT OIL PRESSURE ON THE LT ENGINE ROSE TO 120 PSI AND STAY ED THERE. AFTER REJECTING TAKEOFF THE ENGINE WAS RUN UP THROUGH 86 PERCENT TWICE AND BOTH TIMES PRESSURE INCREASED TO A BOVE 120 PSI. RAN AIRCRAFT ENGINES THROUGH 86% N1 ENGINE OIL PRESSURES STABILIZED AT 83 PSI (BOTH LT & RT). BOTH OIL TE MPERATURES ALSO CHECKED GOOD AT TAKE OFF SETTINGS. ALL VISUAL INSPECTIONS OF OIL PRESSURE TRANSDUCER AND WIRING GOOD, N O DEFECTS NOTED, ALL ENGINE PARAMETERS GOOD. WORK PERFORMED IAW CESSNA CE-750 MAINT MANUAL 79-30-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007073000207 20070730 00207 CE 2007 7 30 DXTA200702353 1 20070720 A 3213 67420861 PACKING CESSNA 750 750 2076810 CE NOSE STRUT OUT OF TOLERANCE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 906QS 4515 7500206 GEAR WOULD NOT RETRACT AFTER T.O. GEAR HANDLE LOCKED DOWN. HAD BEEN ACTING UP ON PRIOR FLIGHTS, NOT ALLOWING US TO RETRA CT IMMEDIATELY. DISASSEMBLED LOWER NOSE STRUT, REPLACED PACKINGS AND REASSEMBLED, SERVICED PER 750 C/M/M 32-20-02. REPLA CED NOSE STRUT ORIFICE PER 750 C/M/M 32-20-02, GEAR SWING CLEARANCE CHECKS GOOD, TAXI CHECK GOOD. 2 L 7 2 4J RT T00007WI 2007073000208 20070730 00208 CE 2007 7 30 DXTA200702354 1 20070720 A 2913 MP50B1 MOTOR CESSNA 560 560XL 2076702 CE HYD PUMP INOPERATIVE E DXTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 670QS 6134 5605170 AFTER LANDING AND 2 MINUTES INTO OUR TAXI THE "LOW BRK PRESS" AND "ANTI SKID" CAUTION LIGHT ILLUMINATED. 45 SECONDS LATE R BRAKES FAILED AND WE ACTUATED THE EMERGENCY BRAKE SYSTEM. R&R ANTI-SKID HYDRAULIC PUMP MOTOR IAW CE560XL MM 32-42-00. OPS CHECK GOOD. R&R'D MOTOR POWER RELAY IAW CE560XL MM 32-42-00. OPS CHECK GOOD. BLED ANTI SKID BRAKE SYSTEM IAW CE560XL MM 32-42-00. OPS CHECK GOOD 2 L 7 2 4F RT A22CE 2007073000209 20070730 00209 NM 2007 7 30 DXTA200702351 1 20070719 A 2530 OVEN AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE GALLEY ODOR E DXTA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 290QS 190 WHITE ODORLESS SMOKE POURS OUT OF THE GALLEY CONVECTIVE OVEN WHEN OPERATING. CLEANED OUT INSIDE OF OVEN. OPERATED AT H IGHEST TEMPERATURE SETTING FOR 15 MINUTES. VERY MINIMAL SMOKE NOTED AFTER CLEANING. IAW F2000 M/M 20-314 2 K 7 2 4F 4 F RT A50NM E44NE 2007073100005 20070731 00005 NM 2007 7 31 CALA0700366 1 20070719 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT STA 344, LBL 17 TO RBL 12. THE FLOORBEAM WAS REPAIRED IAW SRM 5 3-10-51. 2 L 7 2 4F RT A16WE 2007073100015 20070731 00015 NM 2007 7 31 2007UALA02227 1 20070625 A 2530 UNKNOWN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE GALLEY ODOR A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 WP 29 217UA 30550 BURNING SMELL IN CABIN ON ARRIVAL. INBOARD CABIN CREW REPORTED BURNING SMELL IN AFT SIDE CABIN AFTER LANDING. CHECKED NO CIRCUIT BREAKERS POPPED IN AFT GALLEY. ALSO CHECKED AFT CABIN AREA WITH CEILING PANEL REMOVED, CONDITION NORMAL. CA BIN AND LAV LIGHTING SYS, IN-FLIGHT ENTERTAINMENT SYS OK. NO REPEAT OF BURNING SMELL. SUSPECT FOOD-FOULED FOIL CAUGHT IN GALLEY OVEN. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007073100045 20070731 00045 NM 2007 7 31 2007UALA02292 1 20070625 A 2810 TANK BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUEL SYSTEM LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 924UA 26645 FUEL SEEP NOTED AT WING ROOT. LEAK FOUND ON OUTSIDE OF NR 1 TANK LOWER INBOARD AFT CORNER. SEALED THE LEAK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007073100088 20070731 00088 NM 2007 7 31 2007UALA02703 1 20070717 A 2560 SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GIRT BAR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 R-4 DOOR SLIDE, CENTER GIRT BAR SUPPORT IS CORRODED. [08-17-07] REMOVED AND REPLACED SUPPORT PLATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007073100092 20070731 00092 NM 2007 7 31 2007UALA02707 1 20070717 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 DENTED FRAME STA 1500, STR 25L IN AFT PIT. [08-17-07] MAJOR REPAIR ACCOMPLISHED. REPAIRED PER UA ENGINEERING SPECIF ICATIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007073100093 20070731 00093 NM 2007 7 31 2007UALA02708 1 20070718 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 AT BS 680 STRINGER 14L FWD OF L2 DOOR THERE IS A STRESS CRACK AT THE INTERCOSTAL STRUCTURE. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED INTERCOSTAL & STRINGER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007073100098 20070731 00098 NM 2007 7 31 2007UALA02719 1 20070718 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 648UA 25285 FLOOR MOUNTED EEL LIGHTS INOP RIGHT SIDE IN F-C. FLOOR MOUNTED CONNECTOR HAS BEEN DAMAGED. [08-14-07] FLOOR MOUNTED C ONNECTOR HAS BEEN DAMAGE BY CLEANERS. -RPR-:REPAIRED FLOOR-MOUNTED EEL PER MM 33-51-10. 2 L 7 2 4F 4 F RT A1NM E24NE 2007073100100 20070731 00100 NM 2007 7 31 2007UALA02721 1 20070718 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 MAIN CABIN FLOORBEAM STA 365 RBL 20 TO RBL 50 HAS SURFACE CORROSION. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED T-CAP, RBL 20 TO CUSP. FABRICATED T-CAP. INSTALLED ANGLE DOUBLER & STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007073100109 20070731 00109 NM 2007 7 31 UPS07450189 1 20070704 A 5350 SKIN BOEING 747 747200 1384847 NM TAILCONE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C EMP RIGHT TAIL CONE SKIN SURFACE FOUND A DENT MARK AT STA 2755 BETWEEN 17R & 18R. EMP RIGHT TAIL CONE SKIN BS 2750 TO 2762 STR 17R - 18R AREA REPAIRED AS PER SRM 53-30-03 FIG 1A. 2 L 7 4 4F RT A20WE 2007073100131 20070731 00131 NM 2007 7 31 UPS07M50202 1 20070518 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C CTR CARGO STA 5-113 THRU 1541, LONGERON L48 FOUND WITH CORROSION AS MARKED. CTR CARGO STA 5-119 L48 S PLICE REMOVED PER SRM 51-33-01 V2 R38. DAMAGED LONGERON STA 5-113 THRU 1551 TRIMMED PER SRM 53-10-00 V1 FIG 2 R38, STA 5-119 L48 SPLICE & STA 1551 L48 REPAIR LONG & SPLICE FASTENER HOLES PICKED UP PER SRM 51-31-01 V2 R38. REPAIR PARTS & S PLICE INSP OK TO INSTALL. CTR CARGO L48 & STA 1551 INSTALLED PER SRM 51-33-01 VOL 2 R38. 2 L 7 3 4F RT A22WE 2007073100134 20070731 00134 NM 2007 7 31 UPS07M50207 1 20070517 A 5730 SKIN DOUG MD11 MD11F 3023600 NM LT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C LEFT WING I/B FLAP LOWER SURFACE I/B SEGMENT SKIN TO BE REPLACED. NEW SKIN FAB PER BOEING DWG ARC2736 R.B. NEW SKIN HOLES PICKED UP PER SRM 51-31-01 V2 R38. NEW SKIN PROTECTED PER SRM 51-21-01 V2 R38. NEW SKIN INSTALLE D PER SRM 51-31-01 V2 R38. LEFT WING I/B FLAP I/B SEGMENT INSTALLED PER AMM 20-50-02 R55. 2 L 7 3 4F RT A22WE 2007073100139 20070731 00139 NM 2007 7 31 ZZDA2007204 1 20070626 A 5313 STRINGER SPLICE BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 STA 898.5 LONG 25L SPLICE CORRODED. INSTALLED SPLICE AT BS 898.5 LONGERON 25L IAW B717 SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007073100143 20070731 00143 NM 2007 7 31 ZZDA2007208 1 20070605 A 5322 SHEAR TIE BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT BS 927 STRINGER TIE BETWEEN LONG 29R AND 22L. REPLACED SHEAR TIE BS 927 BETWEEN LONG ERON 29R AND LONGERON 22L IAW SRM 51-41-02. 2 L 7 2 4F TR A6WE 2007073100151 20070731 00151 GL 2007 7 31 RAIA00707028 2 20070714 A 7261 42520192 SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 ENGINE WORN A RAIA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 CE 03 833HK 145240 FLT NR 7916 - ORD - E2 LOW OIL PRESSURE MESSAGE- QTY AT 3 QTS. MAINTENANCE REPLACED SEAL AT STARTER. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007073100155 20070731 00155 SO 2007 7 31 RAIA00707033 1 20070719 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 811HK 145256 PRE FLT NR 5493 - STL - PAX DOOR HANDRAIL EMERGENCY LIGHT OUT. MAINTENANCE REPAIRED A BROKEN WIRE TO THE SUBJECT LIGHT. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007073100160 20070731 00160 SO 2007 7 31 RAIA00707036 1 20070722 A 2120 CLAMP EMB 145 EMB145LR 3260212 SO NR 2 PACK LOOSE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 834HK 145269 FLT 8037 - EWR - PACK NR 1 INOPERATIVE MESSAGE ON THE EICAS FOLLOWED BY PACK NR 2 APPROXIMATELY ONE MINUTE LATER. BOTH PACKS RESET AND WORKED FINE ON THE GROUND. MAINTENANCE PERFORMED AN INSPECTION AND FOUND THAT THE NR 2 PACK CLAMP CAME OFF FROM THE DUCT. REINSTALLED THE DUCT AND OPS CHECKED SYSTEM WITH NO OTHER DEFECTS/FAULTS NOTED. 2 L 7 2 4T RT T00011AT 2007073100171 20070731 00171 NM 2007 7 31 SWAA073582 1 20070719 A 5330 655772 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 770, STR 14L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007073100185 20070731 00185 NM 2007 7 31 SWAA073594 1 20070719 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 500C, STR 7R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007073100188 20070731 00188 NM 2007 7 31 SWAA073597 1 20070719 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 727E, STR 9R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007073100202 20070731 00202 NM 2007 7 31 KCSA071251 1 20070725 A 5311 ATTACH BRACKET BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 BS 1372 FUSELAGE FRAME ATTACHMENT BRACKET CORRODED ABOVE RIGHT OVERWING LONGERON. 2 L 7 4 4F RT A20WE 2007073100212 20070731 00212 EA 2007 7 31 TRAX200701032 1 20070721 A 5320 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 754EV 10173 LEFT FS 280 CROSSBEAM CRACKED ON UPPER FLANGE O/B OF LBL 9.0. COMPLIED WITH E.O. 700-53-0058 REV A. 2 L 7 2 4F RT A21EA 2007073100219 20070731 00219 EA 2007 7 31 TRAX200701039 1 20070721 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 914EV 7752 ON APPROACH AFTER FLAPS STABILIZED AT 30 DEG RECEIVED FLAPS FAIL CAUTION MSG, C/W QRH PROCEDURES, FLAPS REMAINED AT 30 D EG FOR LANDING. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007073100222 20070731 00222 NM 2007 7 31 CALA0700374 1 20070724 A 5320 654797321 SHEAR WEB BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND A 2.5 INCH CRACK IN LEFT SHEAR WEB FORWARD OF STA 639 FUSELAGE FRAME, LBL 50. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007073100225 20070731 00225 NM 2007 7 31 UPS07550235 1 20070724 A 3350 LIGHT BOEING 757 75724APF 1384969 NM CABIN ACTIVATED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 411UP 23851 INSPECTION TYPE:N/A EMERGENCY LIGHT HAS SEVERAL LAMPS INOP. RELAMPED SEVEN LAMPS IN THE EMERGENCY LIGHT ASSEMBLY PER MM 33-51-01-2, OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2007073100227 20070731 00227 WP 2007 7 31 UPS07850234 1 20070618 A 5730 561134017 SKIN DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 LEFT WING UPPER FRONT SPAR SKIN CRACKED 2 INCHES LONG AT XRS -36.000. REPAIRED LEFT WING UPPER FRONT SPAR SKIN AT STA XRS -36.000 IAW SAA EA 008-5730-01-A0937, UPS EO DC8-5730-27267-A, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007073100230 20070731 00230 NM 2007 7 31 UPS07M50217 1 20070518 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C CTR CARGO STA 5-113 LONGERON L43 FOUND WITH CORROSION AS MARKED. DAMAGED LONG L43 TRIMMED OFF PER SRM 53-10-00 V1 R38. HFEC CARRIED OUT PER DAC NDTSPM R13 FOUND NO CRACK EVIDENT. REPAIR LONG & SPLICE FAB AND FASTENER HO LES PICK UP PER SRM 53-10-00 V1 R38 & SRM 51-31-01 V2 R38. REPAIR LONGERON & SPLICE INSTALLED PER SRM 51-31-01 V2 R38. PAINT TOUCHED UP ON REWORKED AREA PER SRM 51-21-01 V1 R38. 2 L 7 3 4F RT A22WE 2007073100245 20070731 00245 NM 2007 7 31 SWAA073608 1 20070721 A 3350 6042221 LIGHT BOEING 737 7373G7 1384595 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY P ER MM. 2 L 7 2 4F RT A16WE 2007080100008 20070801 00008 NM 2007 8 1 QXEA200701140 1 20070709 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 202 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - CORROSION ON STRAPS UNDER STRINGER 31L AND OUTBOARD OF 31L FORWARD OF LOWER FRAME AT STATION 202.75. REPAIRED IAW SRM 51-20-11, 51-40-11, 51-20-16, 51-20-36, AND 51-20-26. 2 H 7 2 4T RT A13NM 2007080100011 20070801 00011 EA 2007 8 1 MASA200700051 1 20070124 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A MASA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 SW 07 653ML 7039 ASH 7133 CLT - CREW REPORTED SMOKE TOILET MESSAGE FOR ABOUT 6 SECONDS AND A SMOKE ODOR IN THE CABIN OCCURRING AT THE GAT E. MX REMOVED AND REPLACED COALESCERS, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007080100024 20070801 00024 EA 2007 8 1 MASA200700233 1 20070414 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FS 621 CRACKED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17358 7358 FLOOR SUPPORT ANGLE AT FS 621 RT IS CRACKED. REPAIRED ANGLE. 2 L 7 2 4F RT A21EA 2007080100027 20070801 00027 EA 2007 8 1 MASA200700075 1 20070203 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA ICED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37342 7342 ASH 7300 ORD - SERVICE DOOR WILL NOT OPEN FROM THE INSIDE OR OUTSIDE. MX DEICED THE SERVICE DOOR AND THE OPS CK WAS GOO D. 2 L 7 2 4F RT A21EA 2007080100032 20070801 00032 EA 2007 8 1 MASA200700234 1 20070415 A 5330 601R3500369 SKIN CNDAIR CL600 CL6002B19 1900309 EA FS 559-640 DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17337 7337 FUSELAGE SKIN BETWEEN FS 559-640 STRINGER 6R-6L WAS DAMAGED BY ENGINE FAILURE. MX C/W MAJOR REPAIR. 2 L 7 2 4F RT A21EA 2007080100041 20070801 00041 EA 2007 8 1 MASA200700020 1 20070107 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG UNKNOWN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7264V 8276 7264 ASH 2777 PHX - GEAR UP DISAGREE WARNING AND NOSE LANDING GEAR DOOR WARNING. MX REMOVED AND REPLACED NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2007080100044 20070801 00044 EA 2007 8 1 MASA200700152 1 20070319 A 3210 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A MASA O OTHER O OTHER LD LANDING 1 SW 07 87353 7353 ASH 2816 PHX - WHEN LANDING GEAR SELECTED, GEAR WOULD NOT DEPLOY. PERFORMED GEAR SWINGS, OP GOOD. 2 L 7 2 4F RT A21EA 2007080100045 20070801 00045 EA 2007 8 1 MASA200700153 1 20070320 A 5210 CAM CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR OUT OF ADJUST A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 905J 15005 ASH 2730 DSM - PAX DOOR WILL NOT OPEN. MX ADJUSTED FWD AND AFT SPIGOTS AND CLEARANCE CAMS. 2 L 7 2 4F RT A21EA 2007080100046 20070801 00046 EA 2007 8 1 MASA200700272 1 20070517 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX OUT OF RIG A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7264V 7264 ASH 2832 LAS - PAX DOOR WOULD NOT OPEN. REPEAT PROBLEM. AIRCRAFT FERRIED TO PHX WHERE MX RIGGED AND LUBED THE DOOR. 2 L 7 2 4F RT A21EA 2007080100052 20070801 00052 EA 2007 8 1 MASA200700054 1 20070125 A 5220 COVER CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 907FJ 15007 ASH 2910 GDL. - ROW 15A OVERWING EMERGENCY EXIT HANDLE INTERIOR COVER LOOSE. MX RESECURED COVER. 2 L 7 2 4F RT A21EA 2007080100055 20070801 00055 EA 2007 8 1 MASA200700279 1 20070521 A 2150 GG670950095 ACM CNDAIR CL600 CL6002D24 1390016 EA SMOKE A MASA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 910FJ 15010 ASH 2658 ALT - CREW RETURNED TO THE GATE WITH SMOKE IN THE CABIN. CREW REPORTED THEY WERE TAXING ON 1 ENGINE WITH APU A ND PACKS OPERATING. MX REMOVED AND REPLACED ACM. 2 L 7 2 4F RT A21EA 2007080100064 20070801 00064 EA 2007 8 1 MASA200700060 1 20070127 A 5220 SEAL CNDAIR CL600 CL6002B19 1900309 EA OVERWING EXIT OUT OF POSITION A MASA O OTHER O OTHER CR CRUISE 1 SW 07 17175 7175 ASH 7245 IAD - LT EMERGENCY OVERWING DOOR CAUTION IN FLIGHT. MX REPOSITIONED THE SEAL. 2 L 7 2 4F RT A21EA 2007080100070 20070801 00070 EA 2007 8 1 MASA200700256 1 20070510 A 5210 COUNTERBALANCE CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR OUT OF ADJUST A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 935LR 15035 ASH 2627 CLT - PAX DOOR HARD TO OPEN. ADJUSTED COUNTER BALANCE. 2 L 7 2 4F RT A21EA 2007080100071 20070801 00071 EA 2007 8 1 MASA200700278 1 20070518 A 2520 PSU CNDAIR CL600 CL6002B19 1900309 EA ROW 10 DISLODGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77195 7195 ASH 7218 MYR - PSU AT ROW 10 A/C FELL DOWN. MX CHANGED PSU TUBING. 2 L 7 2 4F RT A21EA 2007080100074 20070801 00074 EA 2007 8 1 MASA200700110 1 20070221 A 2520 COFFEEMAKER CNDAIR CL600 CL6002B19 1900309 EA GALLEY ODOR A MASA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SW 07 17175 7175 ASH 7160 IAD - CREW REPORTED A BURNED ODOR FROM GALLEY AREA. MX FOUND A COFFEE BAG INSIDE POT AND BURNER LEFT ON. 2 L 7 2 4F RT A21EA 2007080100079 20070801 00079 EA 2007 8 1 MASA200700273 1 20070517 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 903FJ 7103 15003 ASH 2678 CLT - DURING PRE-FLIGHT, FOUND ALL EMERGENCY LIGHTS COME ON AND THEN GOES OUT. MX REMOVED AND REPLACED ALL EME RGENCY BATTERY PACKS AND INVERTER. 2 L 7 2 4F RT A21EA 2007080100086 20070801 00086 EA 2007 8 1 MASA200700245 1 20070504 A 2750 601R931057 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS OUT OF RIG A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH 2777 PHX - PILOT REPORTED A FLAPS FAIL CAUTION WITH THE FLAPS AT ZERO. SHE RETURNED TO THE FIELD, AN EMERGENCY WAS DECLARED, THE LANDING WAS UNEVENTFUL. MX RIGGED FLAPS AND REMOVED AND REPLACED BPSU. 2 L 7 2 4F RT A21EA 2007080100097 20070801 00097 EA 2007 8 1 MASA200700259 1 20070511 A 2150 35002300003 CHECK VALVE CNDAIR CL600 CL6002B19 1900309 EA RT A/C PACK MALFUNCTIONED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 17337 16027 7337 ASH 2701 PHX - ON TAXI INTO PHX, LAV SMOKE CAUTION ACCOMPANIED BY VISIBLE SMOKE IN THE COCKPIT AND CABIN. MX REMOVED AN D REPLACED RT PACK HIGH TEMP SW AND BYPASS CHECK VALVE. 2 L 7 2 4F RT A21EA 2007080100114 20070801 00114 EA 2007 8 1 MASA200700097 1 20070209 A 5210 DOOR ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA POWER ASSIST INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37208 7208 ASH 7255 ORD - REPORTED A PAX DOOR POWER ASSIST INOP. MX COULD NOT DUPLICATE THE DISCREPANCY. 2 L 7 2 4F RT A21EA 2007080100115 20070801 00115 EA 2007 8 1 MASA200700207 1 20070415 A 2560 BATTERY CNDAIR CL600 CL6002B19 1900309 EA FLASHLIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 653ML 7039 ASH 7340 IAD - FWD FA EMERGENCY FLASHLIGHT INOP. MX REPLACED BATTERY. 2 L 7 2 4F RT A21EA 2007080100119 20070801 00119 EA 2007 8 1 MASA200700227 1 20070429 A 2612 FIRE WARNING CNDAIR CL600 CL6002B19 1900309 EA APU FALSE ACTIVATION A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 37208 7208 ASH 7108 BHM - APU AUTO SHUTDOWN ON THE GROUND DIE TO A FALSE FIRE WARNING. CONTRACT MX COULD NOT FIND ANY EVIDENCE OF A FIRE AND MEL'D THE APU. 2 L 7 2 4F RT A21EA 2007080100125 20070801 00125 2007 8 1 MASA200700194 4 20070407 A 2561 P01074201 LIFE VEST CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 655BR 1786 7457 ASH 1016 HNL - TWO INFANT LIFE VEST WERE MISSING. MX INSTALLED 2 NEW LIFE VESTS. 2 L 7 2 4F RT A21EA 2007080100126 20070801 00126 EA 2007 8 1 MASA200700185 1 20070404 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA LAVATORY ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 507MJ 10077 ASH 7209 DEN - BURNING ODOR IN LAV. MX PERFORMED NUMEROUS ENGINE RUNS AND OPERATIONAL CHECKS OF ALL LAV AND ACM SYSTEMS . NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007080100127 20070801 00127 EA 2007 8 1 MASA200700410 1 20070711 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 37178 1036 7178 ASH 2914 SBA-PHX, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD DUE TO A GEAR DISAGREE ON TAKEOFF. AIRCRAFT FERR IED TO PHX WHERE MX REMOVED AND REPLACED THE GEAR SELECTOR VALVE AND ADJUSTED THE UPLOCK OPS CK GOOD. 2 L 7 2 4F RT A21EA 2007080100129 20070801 00129 EA 2007 8 1 MASA200700085 1 20070209 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 27172 7172 ASH 7143 IAD - CREW REPORTED PAX DOOR WARNING IN FLIGHT WITH AN OUTER HANDLE CAUTION. MX INSPECTED THE DOOR AND LUBED T HE OUTER HANDLE. OP AND PRESSURIZATION CHECKS WERE GOOD. 2 L 7 2 4F RT A21EA 2007080100131 20070801 00131 EA 2007 8 1 MASA200700015 1 20070103 A 2721 UNKNOWN CNDAIR CL600 CL6002D24 1390016 EA RUDDER TRIM UNKNOWN A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 905J 15005 ASH 2693 CLT - TAKEOFF CONFIGURATION ADVISORY MESSAGE WHEN TAKING RUNWAY. UPON ARRIVAL AT GATE CREW NOTICED THE RUDDER TRIM OUT OF THE GREEN. MX PERFORMED AN OPERATIONAL CHECK OF THE RUDDER AND PERFORMED TAKE OFF CONFIGURATION CHECK WITH RUDDER IN GREEN. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007080100132 20070801 00132 EA 2007 8 1 MASA200700016 1 20070103 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA ILLUMINATED A MASA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 07 591ML 7388 ASH 7309 ORD - CREW REPORTED STALL FAIL FOLLOWED BY A TAKEOFF CONFIG WARNING ON TAKEOFF ROLL. MX CURRENTLY TROUBLESHOOT ING. 2 L 7 2 4F RT A21EA 2007080100133 20070801 00133 EA 2007 8 1 MASA200700221 1 20070422 A 5210 SPRING CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR HANDLE BINDING A MASA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 503MJ 10058 ASH 7155 ROC - RETURNED TO THE FIELD DUE TO PASSENGER DOOR WARNING MESSAGE IN FLIGHT. MX INSPECTED, FOUND DOOR LOCK HAN DLE DETENT CAM SPRING BINDING. CLEANED AND LUBED, OPS CHECKED GOOD 2 L 7 2 4F RT A21EA 2007080100135 20070801 00135 EA 2007 8 1 MASA200700206 1 20070414 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT ILLUMINATED A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 97325 7325 ASH 2703 LAX - RT OVERWING EMERGENCY EXIT DOOR INDICATED OPEN. MX CONTROL DEFERRED THE DOOR INDICATION SYSTEM WITH THE CREW. 2 L 7 2 4F RT A21EA 2007080100140 20070801 00140 EA 2007 8 1 MASA200700066 1 20070130 A 2150 A/C PACK CNDAIR CL600 CL6002D24 1390016 EA RIGHT FAILED A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 912FJ 15012 ASH 2995 PHX - AFT LAV SMOKER WARNING W/RT PACK FAIL. MX FOUND SMOKE CAUSE BY RT PACK FAILURE. PACK DEFERRED. 2 L 7 2 4F RT A21EA 2007080100141 20070801 00141 EA 2007 8 1 MASA200700126 1 20070227 A 5210 DOOR ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA POWER ASSIST INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37208 7208 ASH 7176 ORD - CREW REPORTED THE PAX DOOR POWER ASSIST WAS INOP. MX RESET POWER TO THE SYSTEM AND IT WORKED NORMALLY. 2 L 7 2 4F RT A21EA 2007080100142 20070801 00142 EA 2007 8 1 MASA200700138 1 20070302 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM MALFUNCTIONED A MASA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 75996 14031 7357 ASH 7454 ORD - AIRCRAFT RETURNED TO THE FIELD FOR A GEAR DISAGREE/NOSE DOOR OPEN WARNING. MX REMOVED AND REPLACED 3A AN D 3B PUMP. 2 L 7 2 4F RT A21EA 2007080100143 20070801 00143 EA 2007 8 1 MASA200700107 1 20070220 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA LEFT ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 17175 7175 ASH 7105 ORD - CREW REPORTED A BURNING ODOR IN COCKPIT. MX PLACED LEFT PACK ON MEL (REF MASA200700109). 2 L 7 2 4F RT A21EA 2007080100144 20070801 00144 EA 2007 8 1 MASA200700122 1 20070226 A 5240 DOOR CNDAIR CL600 CL6002D24 1390016 EA SERVICE LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 924FJ 15024 ASH 2985 PHX - CAPTAIN REPORTED THE SERVICE DOOR EXTREMELY HARD TO OPEN. MX LUBED. 2 L 7 2 4F RT A21EA 2007080100146 20070801 00146 EA 2007 8 1 MASA200700159 1 20070322 A 2731 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 47202 7202 ASH 7202 IAD - REPORTED STAB CHANNEL NR 1 W/ NOT ENGAGE. MX REMOVED AND REINSTALLED THE HSTCU, AND COULD NOT DUPLICATE THE PROBLEM. 2 L 7 2 4F RT A21EA 2007080100148 20070801 00148 2007 8 1 MASA200700144 2 20070313 A 7230 FAN CNDAIR CL600 CL6002C10 1390015 EA ENGINE DAMAGED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 505MJ 10070 ASH 7302 IAD - BURNING ODOR IN CABIN AFTER BIRD STRIKE. MX COMPLIED WITH REPAIR TO THE FAN CASE AND COWLING. 2 L 7 2 4F RT A21EA 2007080100150 20070801 00150 EA 2007 8 1 MASA200700220 1 20070422 A 5220 SEAL CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT DIRTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 932LR 15032 ASH 2806 PHX - SEAT 16A EMERGENCY EXIT SQUEALS. MX CLEANED AND INSPECTED SEAL, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2007080100151 20070801 00151 EA 2007 8 1 MASA200700218 1 20070422 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT STUCK A MASA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SW 07 651ML 7139 ASH 7102 CAE - RT OVERWING EMERGENCY EXIT WILL NOT OPEN. MX FOUND IT TO BE STICKING PAINT, CLEANED AND OPS CHECKED GOOD . 2 L 7 2 4F RT A21EA 2007080100153 20070801 00153 EA 2007 8 1 MASA200700139 1 20070307 A 5220 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA OVERWING DOOR DIRTY A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 650ML 7137 ASH 7227 DSM - RT EMERGENCY OVERWING DOOR CAUTION IN FLIGHT. MX CLEANED THE DOOR PROX SENSORS AND THE MESSAGE CLEARED. 2 L 7 2 4F RT A21EA 2007080100155 20070801 00155 2007 8 1 MASA200700179 4 20070401 A 2561 LIFE VEST CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 651BR 7426 ASH 1018 HNL. - SEATS 12A AND 12C MISSING THE LIFE VESTS. MX INSTALLED NEW LIFE VESTS. 2 L 7 2 4F RT A21EA 2007080100157 20070801 00157 EA 2007 8 1 MASA200700269 1 20070515 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA NONE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 97325 7325 ASH 2721 PHX - REPORTED HAVING TROUBLE OPENING THEIR PAX DOOR. MX OPENED THE DOOR NORMAL AND COULD NOT DUPLICATE THE DI SCREPANCY. 2 L 7 2 4F RT A21EA 2007080100159 20070801 00159 EA 2007 8 1 MASA200700031 1 20070115 A 7700 829599 SENSOR CNDAIR CL600 CL6002D24 1390016 EA RT ENGINE MALFUNCTIONED A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 902FJ 655 15002 ASH 2941 TUS - RT ENGINE FLAMED OUT DURING TAXI. MX REMOVED AND REPLACED THE N2 SENSOR AND NO DEFECTS NOTED ON BORESCOP E. 2 L 7 2 4F RT A21EA 2007080100160 20070801 00160 EA 2007 8 1 MASA200700176 1 20070401 A 2621 EXTINGUISHER CNDAIR CL600 CL6002C10 1390015 EA APU BAY LOW A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 505MJ 10070 ASH 7110 ORD - APU BOTTLE LOW CAUTION MESSAGE AND APU SQUIB CAUTION MESSAGE. MX DEFERED THE APU FIRE EXTINGUISHING SYST EM AND APU. 2 L 7 2 4F RT A21EA 2007080100161 20070801 00161 EA 2007 8 1 MASA200700161 1 20070322 A 2731 70623 MCU CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75999 9656 7471 ASH 7340 BOS - STAB CHANNEL NR 1/2 WILL NOT ENGAGE. CONTRACT MX WAS UNABLE TO RESET AND ENGAGE THE STAB. MX REPLACED M OTOR CONTROL UNIT. 2 L 7 2 4F RT A21EA 2007080100163 20070801 00163 EA 2007 8 1 MASA200700068 1 20070202 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA MLG OUT OF RIG A MASA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 592ML 7209 ASH 7367 IAD - CREW RETURNED TO THE FIELD AND REPORTED A GEAR DISAGREE AND NLG DOOR OPEN AFTER TAKE OFF. MX RIGGED PROX SENSOR. 2 L 7 2 4F RT A21EA 2007080100165 20070801 00165 EA 2007 8 1 MASA200700247 1 20070504 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77302 7302 ASH 7168 IAD - LT OVERWING EMERGENCY EXIT LIGHT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2007080100166 20070801 00166 2007 8 1 MASA200700248 4 20070508 A 2561 P0640101 LIFE VEST CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 651BR 7426 ASH 1006 HNL. - MX REPORTED AN INFANT LIFE VEST WAS MISSING. MX INSTALLED A NEW LIFE VEST. 2 L 7 2 4F RT A21EA 2007080100167 20070801 00167 2007 8 1 MASA200700249 4 20070508 A 2561 P0640101 LIFE VEST CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 655BR 7457 ASH 1034 HNL. - MX FOUND 3 INFANT LIFE VEST MISSING. MX REPLACED THE LIFE VESTS. 2 L 7 2 4F RT A21EA 2007080100168 20070801 00168 EA 2007 8 1 MASA200700099 1 20070212 A 2120 UNKNOWN CNDAIR CL600 CL6002D24 1390016 EA CABIN SMOKE A MASA C ABORTED TAKEOFF B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 SW 07 914FJ 15014 ASH 2908 PHX. - ABORTED TAKEOFF DUE TO LAV SMOKE WARNING AND ODOR OF SMOKE IN CABIN. MX PERFORMED ENGINE RUNS. NO DEFE CTS NOTED. 2 L 7 2 4F RT A21EA 2007080100169 20070801 00169 EA 2007 8 1 MASA200700070 1 20070202 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA OVERWING EXIT OUT OF ADJUST A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 17175 7175 ASH 7238 BNA - LT WING OVERWING EMERGENCY DOOR CAUTION IN FLIGHT. MX ADJUSTED PROX SWITCH. 2 L 7 2 4F RT A21EA 2007080100173 20070801 00173 EA 2007 8 1 MASA200700239 1 20070424 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FS 640, WL 119 CRACKED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17337 7337 ENGINE SUPPORT BEAM IS CRACKED AT AFT WEB FIVE FASTENERS TO THE RIGHT OF BL 0. REPAIRED ENGINE SUPPORT BEAM. 2 L 7 2 4F RT A21EA 2007080100174 20070801 00174 EA 2007 8 1 MASA200700116 1 20070223 A 2150 GG670950095 ACM CNDAIR CL600 CL6002D24 1390016 EA RIGHT ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 924FJ 7548 15024 ASH 2835 AUS - PRIOR TO BOARDING THE FLIGHT CREW DETECTED A BURNING ODOR IN THE CABIN. THE RT AC PACK HAD OVERHEATED AN D FAILED. CONTRACT MX INSPECTED THE EQUIPMENT BAY FOR ANY OTHER DEFECTS, MX REMOVED AND REPLACED ACM. 2 L 7 2 4F RT A21EA 2007080100178 20070801 00178 EA 2007 8 1 MASA200700131 1 20070303 A 2150 GG670950091 ACM CNDAIR CL600 CL6002C10 1390015 EA SMOKE A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 515MJ 9149 10117 ASH 7197 ORD - CREW REPORTED SMOKE IN THE CABIN AT THE GATE. MX REPLACED THE ACM. 2 L 7 2 4F RT A21EA 2007080100179 20070801 00179 EA 2007 8 1 MASA200700290 1 20070508 A 5210 601R31902 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77195 7195 PAX DOOR OUTER SKIN HAS A TEMPORARY REPAIR PERFORMED TO THE LOWER AFT CORNER OUTER SKIN. PERFORMED A PERMANENT REPAIR B Y REMOVING DAMAGE AND INSTALLING A FLUSH REPAIR. 2 L 7 2 4F RT A21EA 2007080100181 20070801 00181 EA 2007 8 1 MASA200700215 1 20070417 A 5220 HANDLE CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT SEPARATED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 902FJ 15002 ASH 2946 RNO - 16DF EMERGENCY EXIT HANDLE COVER CAME OFF. MX REPAIRED HANDLE. 2 L 7 2 4F RT A21EA 2007080100183 20070801 00183 EA 2007 8 1 MASA200700010 1 20070103 A 5210 GATE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR NOT CLOSED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 27172 7172 ASH 7156 GSP - EN ROUTE TO ORD, AIRCRAFT DIVERTED TO BNA FOR A PAX DOOR WARNING IN FLIGHT. MX FOUND DOOR FLAPPER VENT N OT CLOSING PROPERLY. MX ADJUSTED FLAPPER PUSHROD. OP CHECK NORMAL. 2 L 7 2 4F RT A21EA 2007080100188 20070801 00188 EA 2007 8 1 MASA200700289 1 20070530 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75983 7481 ASH 7367 IAD - AFT UPPER CEILING EMERG LIGHT INOP, MX RELAMPED. 2 L 7 2 4F RT A21EA 2007080100189 20070801 00189 EA 2007 8 1 MASA200700150 1 20070319 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A MASA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 87353 17103 7353 ASH 2944 DSM - PILOT REPORTED WHEN THE GEAR WAS SELECTED TO THE DOWN POSITION, THE NOSE GEAR FAILED TO COME DOWN. SWITC HED THE HYDRAULIC 3B PUMP TO THE "ON" POSITION AND RECYCLED THE GEAR. MX REMOVED AND REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2007080100191 20070801 00191 EA 2007 8 1 MASA200700127 1 20070227 A 5250 DOOR CNDAIR CL600 CL6002B19 1900309 EA COCKPIT OBSTRUCTED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77302 7302 ASH 7302 SBP - CREW REPORTED THE FLT DECK DOOR WAS TAKEN OFF THE HINGES DUE TO A STORAGE CABINET DOOR TRIM PIECE OR SLID ER BLOCKING THE DOOR FROM OPENING. RESECURED DOOR HINGE. 2 L 7 2 4F RT A21EA 2007080100192 20070801 00192 EA 2007 8 1 MASA200700141 1 20070308 A 3320 SOCKET CNDAIR CL600 CL6002B19 1900309 EA GALLEY BURNED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 77302 7302 ASH 2800 BUR - AIRCRAFT DIVERTED WAS EN ROUTE FROM BUR TO LAS WHEN THE SMOKE FORMED IN THE COCKPIT. MX FOUND GALLEY LIG HT SOCKET BURNED AND PLACED ON DEFERRAL. CREW PULLED CVR AND FDR CIRCUIT BREAKERS. 2 L 7 2 4F RT A21EA 2007080100194 20070801 00194 EA 2007 8 1 MASA200700119 1 20070226 A 4940 STARTER CNDAIR CL600 CL6002B19 1900309 EA APU BURNED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27191 7191 ASH 7367 IAD - CREW REPORTED APU SHUT DOWN WITH BURNING SMELL AND SMOKE. MX REPORTED THE STARTER BURNT UP CAUSING THE S MELL. MX REPORTS THE APU START CONTACTOR IN JB-5 IS BAD AND THE STARTER IS BURNED BECAUSE OF THE CONTACTOR. MX DISABLE D THE START CONTACTOR AND DEFERRED THE APU. 2 L 7 2 4F RT A21EA 2007080100195 20070801 00195 EA 2007 8 1 MASA200700228 1 20070427 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 926LR 15026 ASH 2604 IAH - TWO CEILING EMERG LIGHTS INOP. MX PLACED ITEM ON MEL. 2 L 7 2 4F RT A21EA 2007080100198 20070801 00198 EA 2007 8 1 MASA200700002 1 20070101 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STUCK A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 97325 7325 ASH 2704 PHX - PAX DOOR WILL NOT OPEN FORM THE OUTSIDE. MX INSPECTED THE DOOR BUT WERE UNABLE TO DUPLICATE THE PROBLEM. 2 L 7 2 4F RT A21EA 2007080100199 20070801 00199 EA 2007 8 1 MASA200700177 1 20070401 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT MALFUNCTIONED A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 923FJ 15023 ASH 2672 CHS - AFT LT EMERGENCY DOOR INDICATES OPEN WHEN CLOSED AND LOCKED. MAINTENANCE RESECURED THE DOOR. 2 L 7 2 4F RT A21EA 2007080200001 20070802 00001 EA 2007 8 2 MASA200700196 1 20070407 A 7830 THRUST REVERSER CNDAIR CL600 CL6002B19 1900309 EA LEFT DEPARTED A MASA O OTHER D J INFLIGHT SEPARATION WARNING INDICATION CR CRUISE 1 SW 07 77181 7181 ASH 7193 ORD - CREW DECLARED AN EMERGENCY EN ROUTE TO ORD FROM LAN. CREW REPORTED A LT REVERSER UNLOCK CAUTION IN FLIGH T AND ALSO REPORTED COMPONENTS MISSING FROM THE REVERSER. MX REPORTS IT IS THE ENTIRE REVERSER IS MISSING AND LT ELEVAT OR, RUDDER AND VERTICAL STAB IS DAMAGED. AWAITING NTSB RESPONSE AND PULLING CVR AND FDR BREAKERS AT TIME OF THIS REPORT . 2 L 7 2 4F RT A21EA 2007080200002 20070802 00002 EA 2007 8 2 MASA200700197 1 20070408 A 7830 THRUST REVERSER CNDAIR CL600 CL6002B19 1900309 EA NR 2 OUT OF RIG A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 77278 7278 ASH 2914 PHX. - ABORTED T/O DUE TO A NR 2 TR CAUTION. MX RIGGED STOW AND DEPLOY SWITCHES. 2 L 7 2 4F RT A21EA 2007080200008 20070802 00008 EA 2007 8 2 MASA200700254 1 20070509 A 3397 CONNECTOR CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 927LR 15027 ASH RON TUC - FLOOR LEVEL EMERGENCY LIGHT INOP ON AFT SERVICE DOOR. RESECURED CONNECTOR. 2 L 7 2 4F RT A21EA 2007080200011 20070802 00011 EA 2007 8 2 MASA200700292 1 20070531 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH 2728 PHX - THE CREW REPORTED ONE CELING FLOOD LIGHT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2007080200014 20070802 00014 EA 2007 8 2 MASA200700299 1 20070603 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 933LR 15033 ASH 2972 LAS - PILOT REPORTED THE SECOND EMERGENCY FLOOD LIGHT INOP. MX REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 2007080200018 20070802 00018 NM 2007 8 2 UIEA200700279 1 20070724 A 5343 TRUNNION BOEING 747 747271C 1384869 NM ZONE 700 DAMAGED A UIEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 15 537MC 22403 NOSE GEAR LEFT TRUNNION BEARING LOWER CAP TOOLING DAMAGE ON BOTTOM MATING SURFACE. BLENDED OUT DAMAGE MIN .250"R , HFEC AND 10X VISUAL INSPECTION TREATED AND PRIMED. REF BOEING 8100-9 MESSAGE 1-384920112-1. 2 L 7 4 4F A20WE 2007080200019 20070802 00019 NM 2007 8 2 UIEA200700280 1 20070724 A 5511 SPAR BOEING 747 747271C 1384869 NM HORIZONTAL STAB GOUGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 RT HORIZ STAB AUX SPAR FWD FACE HAS 7 EACH GOUGES BETWEEN STAB STATIONS 210 - 240 ABOVE LOWER RIVET PATTERN. FOUND GOUG ES OUT OF LIMITS, IAW 747 SRM 55-10-01. CUT OUT DAMAGE, FABRICATED FILLER AND DOUBLER IAW B747 SRM 51-10-02. INSTALLED FILLER AND DOUBLER IAW SRM 55-10-05. 2 L 7 4 4F A20WE 2007080200020 20070802 00020 NM 2007 8 2 UIEA200700281 1 20070724 A 5753 SKIN BOEING 747 747271C 1384869 NM TE FLAP PUNCTURED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 3 SMALL PUNCTURES IN UPPER SURFACE OF LEFT INBOARD MID FLAP. CAUSED BY DROPPED TOOL. CLEANED AREA OF DAMAGE PREPPED AR EA FOR REPAIRS IAW 747 SRM 51-40-12 REPAIRS 4C AND 4D. APPLIED CONDUCTIVE COATING IAW 747AMM 51-24-03 PRIMED AND TOP CO ATED IAW AMM 51-24-03. 2 L 7 4 4F A20WE 2007080200021 20070802 00021 NM 2007 8 2 UIEA200700282 1 20070724 A 5343 TRUNNION BOEING 747 747271C 1384869 NM BS 1480 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 CORROSION ON UPPER SURFACE OF RIGHT BODY GEAR OUTBOARD TRUNNION UPPER CAP AROUND THE FORWARD BOLT HOLE. LOCALLY BLENDED PITTING CORRODED AREA. HFEC AND 10X VISUAL INSPECTION PLUS DYE PENETRANT INSPECTED. SPOT FACED WASHER BEARING SURFACE AREA SHOT PEENED BLEND. REWORKED AREA. HFEC CHECKED BOLT HOLES. TREATED ,PRIMED AREA PER BOEING 8100-9. 2 L 7 4 4F A20WE 2007080200022 20070802 00022 NM 2007 8 2 UIEA200700283 1 20070724 A 5330 SKIN BOEING 747 747271C 1384869 NM BS 1271.5 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 RIGHT SIDE STA 1271.5 WL 200 CRACK NOTED ON SKIN 1" IN LENGTH AND TERMINATES JUST AFT OF FASTENER HOLE. DOES NOT GO IN TO HOLE. REMOVED EXISTING DOUBLER ACCOMPLISHED TRIM OUT ON SKIN AND BEAR STRAP. INSTALLED NEW DOUBLER AND FILLER FOR T RIMMED OUT AREA IAW SB 747-53A2512. 2 L 7 4 4F A20WE 2007080200023 20070802 00023 NM 2007 8 2 UIEA200700284 1 20070724 A 5512 PANEL BOEING 747 747271C 1384869 NM HORIZONTAL STAB GOUGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 PANEL 341BR RIGHT HORIZ STAB LEADING EDGE TOOLING MARKS AND GOUGES. REPAIRED TOOLING MARKS ON RIGHT LEADING EDGE OF HOR IZ STAB IAW SRM 55-10-03. 2 L 7 4 4F A20WE 2007080200024 20070802 00024 NM 2007 8 2 UIEA200700285 1 20070724 A 5753 SKIN BOEING 747 747271C 1384869 NM TE FLAP PUNCTURED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 PUNCTURE ON LOWER AFT SURFACE OF RT INBOARD T/E FORE FLAP AT WBL 235.2. PUNCTURE ON LOWER AFT SURFACE OF RIGHT I/B T/E FOREFLAP AT WBL 235.2 CLEANED AND PREPPED AREA FOR REPAIR IAW SRM 51-40-12. APPLIED REPAIR IAW SRM 51-40-12 PARA 4A AND PAINTED IAW MM 51-40-12. REINSTALLED PHONOLIC RUB STRIP IAW 51-50-00 PARA 3. 2 L 7 4 4F A20WE 2007080200025 20070802 00025 NM 2007 8 2 UIEA200700286 1 20070725 A 5753 SKIN BOEING 747 747271C 1384869 NM TE FLAP PUNCTURED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 LT OUTBOARD MID FLAP HAS A PUNCTURE IN THE UPPER SURFACE 112" FROM INBOARD EDGE AND 8" FROM T/E. REPAIRED LT OUTBOARD M IDFLAP IAW SRM 51-40-15 PARA 4C. APPLIED CONDUCTIVE COATING IAW SRM 51-24-03 APPLIED PRIMER AND TOP COAT PER 51-21-02. 2 L 7 4 4F A20WE 2007080200026 20070802 00026 NM 2007 8 2 UIEA200700287 1 20070725 A 5347 SEAT TRACK BOEING 747 747271C 1384869 NM BS 480-520 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 CORROSION ON SEAT TRACK UPPER DECK GALLEY STA 480 TO 520 LBL 40. REMOVED UPPER DECK GALLEY SEAT TRACK STA 480-530 LBL 4 0. FABRICATED NEW SECTION OF SEAT TRACK FROM BAC1520-1567 7178-T6511 PO NR 1114517 IAW SRM 53-10-05. INSTALLED NEW SEC TION OF SEAT TRACK FOD CHECKED AREA AS REQUIRED. 2 L 7 4 4F A20WE 2007080200027 20070802 00027 NM 2007 8 2 UIEA200700288 1 20070725 A 5347 SEAT TRACK BOEING 747 747271C 1384869 NM ZONE 900 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 CORROSION ON SEAT TRACK UPPER DECK GALLEY STA 480 TO 520 LBL 60. REMOVED UPPER DECK GALLEY SEAT TRACK STA 480-590 LBL 6 0. FABRICATED NEW SECTION OF SEAT TRACK FROM BAC1520-1567 7178-T6511 PO NR 1114517 IAW SRM 53-10-05. INSTALLED NEW SEC TION OF SEAT TRACK FOD CHECKED AREA AS REQUIRED. 2 L 7 4 4F A20WE 2007080200029 20070802 00029 NM 2007 8 2 UIEA200700290 1 20070725 A 5753 STRUCTURE BOEING 747 747271C 1384869 NM TE FLAP DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 NICK AND GOUGE DAMAGE TO COMPOSITE ON RT OUTBOARD MID FLAP. CLEANED AND PREPPED AREA. APPLIED REPAIR PER SRM 51-40-15P ARA 4L. 2 L 7 4 4F A20WE 2007080200031 20070802 00031 NM 2007 8 2 UIEA200700291 1 20070723 A 2613 UNKNOWN BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE NACELLE TEMP UNKNOWN A UIEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 15 517MC 23300 455793 RTO: T/O + 15 MINUTES NR 2 ENGINE NACELLE TEMPS WENT TO 9.2 "A" LOOP AND 8.1 "B" LOOP FAULT LIGHT CAME ON. FAULT LIGHT ON FWD PANEL WAS ON. ACCOMPLISHED FWB PROCEDURES. TOOK 20 MINUTES FOR OVERHEAT TO COOL AFTER NR 2 THROTTLE TO IDLE. 2 L 7 4 4F 4 F A20WE E23EA 2007080200039 20070802 00039 EU 2007 8 2 F3LA200700185 1 20070724 A 3210 TORQUE LINK AIRBUS A318 A318111 3940019 EU MLG CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 803FR 5201 2017 DURING C-3 CHECK, INSPECTION REPORTED PITTING AND CORROSION ON NLG UPPER TORQUE LINK ATTACH POINT. REMOVED PITS AND COR ROSION AND CADMIUM PLATED INNER BORE IAW EA A8-23R-12046. 2 L 7 2 4F RT 2007080200040 20070802 00040 2007 8 2 DL76L070950 4 20070723 A 3454 6225222102 RECEIVER BOEING 767 767332 1382001 NM ADF ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 192DN 28449 ADFL CAUTION MSG ON HSI. LEFT ADF INOP-LEFT ADF C/B. POPPED AND SMOKE ODOR, ELECTRICAL FOR APPROX 10 MIN AFTER CB POPP ED. VERIFIED LEFT ADF-REC. INOP AND UNIT SMELLS ELECTRICAL SMOKE. REPLACED LT ADF REC - CHECKED AND CLEANED LT ADF RE C SHELF CONNECTOR. LEFT ADF CB STAYS IN AND NO ELECT SMOKE DETECTED. PERFORMED L ADF GRD CHECK ALL OPS AND IND NORMAL PER M/M. 2 L 7 2 4F RT A1NM 2007080200041 20070802 00041 NM 2007 8 2 DL76S070951 1 20070723 A 2120 UNKNOWN BOEING 767 767332 1382001 NM CABIN ODOR A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 138DL 25409 F/ATTENDS SMELL BURNT ODOR THROUGHOUT AIRPLANE. CHKD CABIN AND GALLEY AREAS, NO NOTICEABLE ODORS FOUND. NO REPORT BY INBOUND CREW. SUSPECT ODOR INTRODUCED BY GROUND A CONDITIONING. NO TROUBLE FOUND. 2 L 7 2 4F RT A1NM 2007080200044 20070802 00044 NM 2007 8 2 DL757070955 1 20070724 A 2420 IDG BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE INOPERATIVE A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 662DN 24991 727053 ON TAKEOFF, AROUND 60 KTS RT ENG GEN DRIVE LIGHT ON WITH EICAS MSG. ABORTED T/O. REPLACED RT ENG IDG AND GCU. NO FAUL TS ON BPCU. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080200045 20070802 00045 NM 2007 8 2 DL757070956 1 20070724 A 2120 DUCT BOEING 757 757232 1384965 NM RT A/C PACK BLOWN A DALA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 SO 27 616DL 22823 LEFT DUCT LEAK THEN RIGHT DUCT LEAK, LOST REMAINING RT PACK AUTO PRESS 1 AND 2 FAIL MSGS. LOST CABIN PRESS, EMERGENCY D ESCENT TO 10,000 FT. FOUND DUCT IN RT SIDE BLOWN BLOWING HOT AIR INTO THE RT AND LT A/C BAYS GIVING DUCT LEAK MSGS. D UCT BLOWN WAS THE REHEATER DUCT FOR THE RT PACK. REPLACED SAME. LEFT PACK WAS ALREADY ON MCO. 2 L 7 2 4F RT A2NM 2007080200046 20070802 00046 SO 2007 8 2 CHQA200700038 1 20070724 A 2810 UNKNOWN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUEL SYSTEM UNKNOWN A CHQA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 11 571RP 827 CAE312629 FLT 6328 - RDU TO MCO - AFTER TAKEOFF FROM RDU ON CLIMB-OUT, PAX NOTICED FUEL LEAKING FROM RT WING AROUND AILERON AREA. FLT ATTENDANT NOTIFIED OF LEAK & THEN PROCEEDED TO NOTIFY FLT CREW. TANK 2 INDICATION SHOWED A FUEL USAGE OF APPROX 30 0 LBS MORE THAN TANK 1 AFTER REACHING 8,000 FT ON CLIMB OUT FROM RDU. FUEL QTY ON MFD TANK 2 INDICATION NOTICED DECREAS ING AT AN IRREGULARLY FAST RATE, APPROX 10 LBS EVERY 5 SECONDS. DECISION MADE OUT OF SAFETY OF FLT TO RETURN TO RDU DUE TO FUEL LEAKAGE. AN EMERGENCY DECLARED & A NORMAL LANDING EXECUTED. AIRCRAFT WAS REFUELED AND OPERATION OF VENT VALV E VERIFIED AS OPERATING PROPERLY. INSPECTED ALL RT FUEL ACCESS PANELS AND RIGHT REAR SPAR WITH NO LEAKS NOTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007080200047 20070802 00047 EA 2007 8 2 SWIA200718520 1 20070531 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BRAKE TRANSDUCER CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 973SW 7949 RIGHT BRAKE TRANSDUCER BRACKET IS CRACKED IN 2 PLACES, DISCOVERED AT C-CHECK. REPLACED BRAKE TRANSDUCER BRACKET IAW CRJ 200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007080200048 20070802 00048 EA 2007 8 2 SWIA200718521 1 20070531 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BRAKE TRANSDUCER CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 973SW 7949 LEFT BRAKE TRANSDUCER BRACKET IS CRACKED, DISCOVERED AT C-CHECK. REPLACED BRAKE TRANSDUCER BRACKET IAW CRJ200 SRM 51-42 -06. 2 L 7 2 4F RT A21EA 2007080200049 20070802 00049 EA 2007 8 2 SWIA200718522 1 20070531 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 973SW 7949 FS280 FLOOR SUPPORT BEAM UPPER LBL9 IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS AT FS 280 FLOOR SUPPORT B EAM UPPER LBL9 PER REO 601R-53-11-138. 2 L 7 2 4F RT A21EA 2007073000065 20070730 00065 NM 2007 7 30 07FDEA02607 1 20070725 A 5311 6556131 FRAME BOEING 727 727233 138408A NM BS 1090 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT PIT FRAME STA 1090 CORRODED FWD FACE, OTBD RADIUS BETWEEN STR 19-20R. REMOVED CORROSION PER EA NRI070450 STEP 1, RO TO PEENED AREA PER EA I070450 STEP 3. ALODINED AND PRIMED PER EA NR I070450 STEP 4, THIS IS CLASSIFIED AS A MINOR REPAI R. 2 L 7 3 4F RT A3WE 2007073000068 20070730 00068 EU 2007 7 30 07FDEA02610 1 20070725 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT PIT STRINGER 49L BETWEEN FRAME 58 AND 54.3 CORRODED. [08-06-07] REMOVED AND REPLACED AFT PIT STRINGER 49L BETWWEN FRAME 54.3 AND 58 IAW A310 SRM 53-10-14 FIG. 201, PG 203/204. 2 L 7 2 4F RT A35EU 2007073000092 20070730 00092 EU 2007 7 30 07FDEA02632 1 20070726 A 5311 FRAME AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 T-CAP IS CORRODED ON END AT FRAME 38.2 RBL60. [08-17-07] FABBED AND REMOVED AND REPLACED T-CAP, A310-22-00 SRM 53-10 -00, 53-10-15, 51-74-10. 2 L 7 2 4F RT A35EU 2007073000097 20070730 00097 NM 2007 7 30 QXEA200701175 1 20070712 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - SCRATCH ABOVE PANEL 121AL FORWARD UPPER LEFT CORNER ON AIRFRAME. REPAIRED IAW SRM 51-20-11, 51-20-26. 2 H 7 2 4T RT A13NM 2007073000102 20070730 00102 NM 2007 7 30 QXEA200701180 1 20070706 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 4 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - LEFT NR 4 FLAP TRACK, TOP SURFACE HAS TWO DIVOTS. REPAIRED IAW RD8/4-57-988. 2 H 7 2 4T RT A13NM 2007073000110 20070730 00110 SO 2007 7 30 SIMA200720421 1 20070610 A 5210 14533404403 BRACKET EMB 135 EMB135KL 3260302 SO PAX DOOR CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 819AE 13303 5000 145566 MAIN ENTRANCE DOOR INNER HANDLE BRACKET CRACKED. STOPPED DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW EMB IC 200 7-145/30894, PARAGRAPH ONE AND IC2007-145/6600A. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000124 20070730 00124 SO 2007 7 30 SIMA200720502 1 20070712 A 5320 14522459003 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 858AE 9542 5000 145754 FLOOR SUPPORT CENTER HAT BEAM AT FRAME 20 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000127 20070730 00127 SO 2007 7 30 SIMA200720509 1 20070626 A 5311 14522178005 FRAME EMB 135 EMB135LR 3260305 SO ZONE 100 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 722AE 15882 5000 145287 FRAME 68 WEB BETWEEN STRINGERS 10L AND 11L DENTED AND CHAFED. FABRICATED AND INSTALLED DOUBLER IAW EMB IC2007-145/04209 , PARAGRAPH 2, DATED JUNE 21,2007. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000128 20070730 00128 SO 2007 7 30 SIMA200720501 1 20070708 A 5320 14522460007 CHANNEL EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 816AE 13301 5000 145552 GUSSET OVER CENTER HAT BEAM BETWEEN FRAMES 19 AND 23 CORRODED. REMOVED AND REPLACED GUSSET IAW EMB SRM 51-40-02. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000129 20070730 00129 SO 2007 7 30 SIMA200720505 1 20070712 A 5320 14522178005 SILL EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 858AE 9542 5000 145754 SERVICE DOOR CENTER SILL CORRODED. REMOVED AND REPLACED IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000141 20070730 00141 2007 7 30 AWXA200700872 4 20070718 A 2565 2LA00546900 CONTROL PANEL AIRBUS 320 A320232 3930326 EU R2 DOOR SLIDE INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 654AW 1050 SAL - EES -BC-6 CHECK - NR 5948566, R2 DOOR SLIDE ARMED INDICATOR LIGHT DOES N0T COME ON. REPLACED AND OPERATIONAL CHEC KED THE R2 DOOR SLIDE ARMED INDICATOR PANEL IAW A320 AMM 52-73-21 AND 52-73-00. 2 L 7 2 4F RT A28NM 2007073000155 20070730 00155 WP 2007 7 30 NWAA072559855 1 20070721 A 2160 CONTROLLER DOUG DC9 DC951 3022051 WP CABIN TEMP MALFUNCTIONED A NWAA A UNSCHED LANDING M B J OVER TEMP SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 01 764NC 47717 AFTER ROTATION AT TAKEOFF THE SMOKE DETECTORS SOUNDED AND THE FLIGHT ATTENDANT REPORTED SIGNIFICANT HEAT IN THE CABIN. THE RIGHT PACK WAS PEGGED AT FULL HOT AND MANUAL CONTROL COULD NOT CORRECT IT. THE FLIGHT RETURNED TO AN UNEVENTFUL LAN DING BACK AT STL. MAINTENANCE WAS NOT ABLE TO PRODUCE ANY SMOKE OR FUMES. BOTH COALESCER BAGS WERE CHANGED AFTER BURN- OUT PROCEDURES WERE COMPLIED WITH. THE CABIN TEMPERATURE CONTROLLER WAS REPLACED AFTER THE AIRCRAFT ARRIVED IN MSP. TH E AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007073000157 20070730 00157 NM 2007 7 30 DL76L070921 1 20070715 A 3610 77328911 CONTROLLER BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE LT ENGINE MALFUNCTIONED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 1201P 28458 723834 L HPSOV CAUTION ON TAKEOFF ROLL. ABORTED T/O AT 10KTS. REPEAT GRIPE FWD TO MCO AND PLACARD PER MEL 36-11-02. VALVE LOC KED IN CLOSED POSITION. BITE OF AIR SUPPLY MODULE SHOWS L HPC. TESTED SYS AND REPLACED LT HPC PER M/M VERIFY BLEED SHI FT AT ENG RUN. RAN ENG BLEED SHIFT CHECKED GOOD SHIFT AROUND 54-55 PERCENT N1 MCO AND PLACARD REMOVED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007073000165 20070730 00165 NM 2007 7 30 NWAA072616729 1 20070720 A 5312 PRESSURE PANEL BOEING 747 747251F 1384898 NM NLG WW CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 629US 22388 DURING "L" CHECK, FOUND CRACKS IN LT NOSE WHEEL WELL WEB BS 320-340 WL 150. REPAIRED PER EA 67-209735. 2 L 7 4 4F A20WE 2007073000167 20070730 00167 NM 2007 7 30 NWAA072586729 1 20070719 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 940 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 629US 22388 DURING "L CHECK FOUND FRAME DOUBLER FASTENER HOLE WITH PLUG INSTALLED AND FRAME WEB WITH FASTENER HOLE CRACKED AT BS 940 . REPAIRED PER EA 67-209730. 2 L 7 4 4F A20WE 2007073000168 20070730 00168 NM 2007 7 30 NWAA072576729 1 20070718 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 820 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 629US 22388 DURING "L" CHECK, FOUND CRACKS IN FRAME WEB AND TENSION TIE FORWARD CHANNEL FASTENER HOLES AT BS 820. REPAIRED PER EA 6 7-209727. 2 L 7 4 4F A20WE 2007073000179 20070730 00179 NM 2007 7 30 DL76S070938 1 20070609 A 5315 BAC15063123 FLOORBEAM BOEING 767 767332 1382001 NM BS 1219 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 130DL 24080 DURING HMV3 FOUND AFT PIT STA 1219 UPPER CHORD CORRODED OUT OF LIMITS AT LBL 23 TO LBL 30. REMOVED DAMAGE SECTION AND RE PAIRED PER SRM 53-00-07 REPAIR NR 4. 2 L 7 2 4F RT A1NM 2007073000183 20070730 00183 NM 2007 7 30 DLM88070942 1 20070719 A 5330 5910142525 SKIN DOUG MD88 MD88 3023688 NM BS 427-465 DAMAGED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 978DL 53259 THE AIRCRAFT SUSTAINED GROUND DAMAGE TO THE FUSELAGE SKIN, C1 DOOR CUTOUT SURROUND DOUBLER, LONGERON, AND FRAME AFT OF T HE FWD CARGO DOOR CUTOUT BETWEEN STA 427 - STA 465 AND L-19R- L20R. SPLICED A NEW SECTION OF FUSELAGE SKIN BETWEEN STA 394 AND STA 494, FROM L-18R TO L-26R. THE FRAME AND LONGERON REPAIR WAS ACCOMPLISHED PER SRM. AN EXTERNAL REPAIR WAS I NSTALLED AT THE UPPER AFT CORNER OF THE C1 DOOR CUTOUT TO REPAIR THE SURROUND DOUBLER. 2 L 7 2 4F RT A6WE 2007073000185 20070730 00185 2007 7 30 DL764070944 4 20070718 A 2565 SLIDE BOEING 767 767432ER 1385134 NM EMERGENCY EXIT BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 832MH 29704 FOUND DURING HMV-1 IN GSO ON TIMCO OPERATION 20951, RT EMERGENCY EXIT DOOR SLIDE FWD LOWER PACK TRAY SAFETY LANYARD AT B OTTOM PIN HOLE SAFETY STRONG FISHING LINE BROKEN AND HAS ONR STRAND HOLDING PIN. 2 L 7 2 4F RT A1NM 2007073000187 20070730 00187 NM 2007 7 30 DHL2007741511 1 20070718 A 5710 BAC1506860 BEAM BOEING 727 7272Q9 138448M NM ZONE 600 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 RT WING T/E UPPER "I" BEAM IS CRACKED FWD OF NR 7 SPOILER SUPPORT AT RWBL 118. REMOVED "I" BEAM, FABRICATED NEW "I" BEA M FROM BAC1506-860, 71" LONG, PO NR 7232109, PER B727 SRM 57-20-2 FIG 2 AND 51-20-1. TREATED, PRIMED, AND INSTALLED NEW "I" BEAM, RWBL 70.5 TO 141.5, PER B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007073000204 20070730 00204 NM 2007 7 30 QXEA200701142 1 20070707 A 5320 SUPPORT BEAM DHAV DHC8 DHC8202 2809007 NM BS 184 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - VERTICAL FORWARD SUPPORT BEAM FOR AVIONICS CLOSET HAS CORROSION ON INBOARD SURFACE BEHIND INTERCOSTAL 31L AT ST ATION 184.0. REPAIRED IAW SRM 51-20-11, 51-20-36. 2 H 7 2 4T RT A13NM 2007073100020 20070731 00020 NM 2007 7 31 2007UALA02229 1 20070625 A 2121 6054578 FAN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN MALFUNCTIONED A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 187UA 26877 SMOKE ODOR IN CABIN BETWEEN ROWS 37+44. TURNED OFF UPPER RECIRC FAN AND SMELL WENT AWAY. REPLACED UPPER RECIRC FAN 1 P ER MM 21-25-01. OPS NORMAL & CIRCUIT BREAKER STAYS IN. AIRCRAFT OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100070 20070731 00070 NM 2007 7 31 2007UALA02689 1 20070716 A 4920 APU BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SHUTDOWN A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 APU AUTO SHUTDOWN. [08-17-07] RESET APU ENGINE CONTROL UNIT. APU CK'S OK. AIRPLANE RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007073100072 20070731 00072 NM 2007 7 31 2007UALA02691 1 20070717 A 5320 THRESHOLD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 561UA 26661 CENTER OF LOWER THRESHOLD FOR FWD CARGO DOOR CUTOUT HAS A 1 INCH DENT WITH A CRACK. [08-17-07] MAJOR REPAIR NEEDED AT THE DOORWAY SCUFF PLATE. TWO CRACKS HAVE BEEN STOP DRILLED, EACH BEING LESS THAN 1.5" LONG, REMOVED DENTED SCUFF PLAT E. INSTALLED SCUFF PLATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007073100073 20070731 00073 NM 2007 7 31 2007UALA02692 1 20070718 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 561UA 26661 NR 2 RT MED CRACKED AT UPPER HINGE CUTOUT. [08-17-07] NR 2 RT MED CRACKED AT UPPER HINGE CUT OUT. INSTALLED DOUBLER REPAIR PER UA ENGINEERING SPECIFICATIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007073100078 20070731 00078 NM 2007 7 31 2007UALA02768 1 20070722 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 FWD CARGO DOOR CUTOUT, UPPER SILL STUB FRAME CORRODED AT AFT DOOR SNUBBER HINGE MOUNT. MAJOR REPAIR: REPLACED FRAME AND SNUBBER HINGE MOUNT PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2007073100079 20070731 00079 NM 2007 7 31 2007UALA02769 1 20070722 A 5310 65C807351 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 986 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 CREASE BEAM CORRODED ADJACENT TO MED 2R BS 986. MAJOR REPAIR: REPLACED CREASE BEAM PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2007073100080 20070731 00080 NM 2007 7 31 2007UALA02770 1 20070722 A 5312 PRESSURE PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 665 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 CABIN BELOW FLOOR LEVEL APPROX STA 665 LBL 32 WL 302 PRESSURE DECK CRACKED 2 EA PLACES. MAJOR REPAIR: FABRICATED AND IN STALLED DOUBLER REPAIR PER SRM 53-21-98 FIGURE 802. 2 L 7 2 4F 4 F RT A16WE E21EU 2007073100084 20070731 00084 NM 2007 7 31 2007UALA02771 1 20070720 A 3510 OXYGEN SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CREW READS LOW A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 376UA 24641 CREW OXYGEN IS BELOW 1250 PSI. SERVICED TO 1900 PSI. 2 L 7 2 4F 4 F RT A16WE E21EU 2007073100086 20070731 00086 EU 2007 7 31 N93A25072007 2 20070725 A 7200 ENGINE GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU SHUTDOWN E N93A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 13 486QS 1386 AFTER TAKEOFF CREW RECEIVED LP EXCEEDANCE CAS MESSAGE WHEN THROTTLES WERE RETARDED ENGINE DID NOT RESPOND TO MOVEMENT. C REW SHUTDOWN ENGINE AND RETURNED TO DEPARTURE AIRPORT. 2 L 7 2 4F 4 F RT A12EA E25NE 2007073100091 20070731 00091 NM 2007 7 31 2007UALA02706 1 20070717 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 DENTED FRAME STA 1580 BETWEEN STR 25-26L IN AFT PIT. [08-17-07] MAJOR REPAIR ACCOMPLISHED. REPAIRED PER UA ENGINEER ING SPECIFICATIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007073100099 20070731 00099 NM 2007 7 31 2007UALA02720 1 20070718 A 5321 FLOOR PANEL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FWD CARGO BAY GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 FWD CARGO PIT TORQUE FLOOR GOUGED FWD AND AFT OF PDU 8C, RBL 5, STA 560. [08-14-07] FOUND OUT OF LIMITS. FABRICATED N EW PANEL PER BAC DWR 451T2504. INSTALLED NEW PANEL PER SRM51-40-02. AIRPLANE RETURNED TO SERVICE READY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007073100101 20070731 00101 NM 2007 7 31 2007UALA02722 1 20070719 A 3530 PBE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN TORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 595UA 28748 PBE ON FWD WALL ON LEFT AFT CABIN LAV STORAGE BAG IS TORN. 09-07-07 FOUND A FAULTY PERSONAL BREATHING EQUIPMENT. RE PLACED PBE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007073100124 20070731 00124 EU 2007 7 31 UPS07150210 1 20070721 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 144UP 0827 INSPECTION TYPE:N/A EMERGENCY LIGHTS TEST FAILED. REMOVED AND REPLACED 1864 BULB AT POSTION 91LE AND PERFORMED SUCCESSF UL OPS TEST IAW METHODS CARD 050000-01-1-999. 2 L 7 2 4F RT A35EU 2007073100129 20070731 00129 NM 2007 7 31 UPS07M50200 1 20070517 A 5730 SKIN DOUG MD11 MD11F 3023600 NM LT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C LEFT WING - I/B FLAP, LWR SURFACE O/B SEGMENT SKIN TO BE REPLACED. SKIN REMOVED PER SRM 51-31-01V2R38 . NEW SKIN FAB PER SRM 51-31-01V2R3 8. NEW SKIN HOLE P/UP PER 51-31-01V2R38. NEW SKIN PROTECTED PER SRM 51- 31-01V2R3 8. NEW SKIN PAINTED PER SRM 51-21-01V2R38. INSTALL NEW SKIN. NEW SKIN INSTALLED PER SRM 51-31-01 V2R38. LEFT WING I/ B FLAP O/B SEGMENT INSTALLED PER AMM20-50-02.R55. 2 L 7 3 4F RT A22WE 2007073100140 20070731 00140 NM 2007 7 31 ZZDA2007205 1 20070626 A 5313 STRINGER SPLICE BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 STA 878.5 LONG 23L SPLICE CORRODED. INSTALLED NEW SPLICE AT BS 878.5 LONGERON 23L IAW B717 SRM 41-41-05. 2 L 7 2 4F TR A6WE 2007073100142 20070731 00142 NM 2007 7 31 ZZDA2007207 1 20070605 A 5322 SHEAR TIE BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT BS 908 STRINGER TIE BETWEEN LONG 28R AND 22L. REPLACED SHEAR TIE BS 908 BETWEEN LONG ERON 28R AND LONGERON 22L IAW SRM 51-41-02. 2 L 7 2 4F TR A6WE 2007073100145 20070731 00145 NM 2007 7 31 ZZDA2007210 1 20070605 A 5313 LONGERON BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 SPOTS OF CORROSION ON AFT CARGO COMPARTMENT LONGERON 27L BETWEEN BODY STATION 889 AND BODY STATION 1053. INSTALLED LONG ERON 27L AT AFT CARGO COMPARTMENT BETWEEN STA 889 AND STA 1053 AS PER B717 SRM 51-41-02 AND SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007073100146 20070731 00146 NM 2007 7 31 ZZDA2007244 1 20070605 A 5311 FRAME BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT BS 908 FRAME BETWEEN LONG 28R AND 22L. REPLACED FRAME BS 908 BETWEEN LONGERON 28R AN D LONGERON 22L IAW SRM 51-41-02. 2 L 7 2 4F TR A6WE 2007073100152 20070731 00152 SO 2007 7 31 RAIA00707030 1 20070714 A 3350 316 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 824HK 145498 PRE FLT NR 5515 - STL - HANDRAIL EMERGENCY LIGHT IS INOP. MAINTENANCE RELAMPED LIGHT AS REQUIRED, OPS TEST GOOD. 2 L 7 2 4T RT T00011AT 2007073100161 20070731 00161 NM 2007 7 31 WRNA200700045 1 20070720 A 2751 18158612 TRANSMITTER BOEING 747 747212B 1384886 NM T/E FLAP MALFUNCTIONED A WRNA K NONE N FALSE WARNING AP APPROACH 1 SO 05 526UP 21937 ON APPROACH TO ANC, OUTBOARD TRAILING EDGE FLAP HAD AN ASYMMETRICAL TRIP AND NR 2 LT LEADING EDGE FLAP DID NOT EXTEND. CONTINUED APPROACH AND MADE A SAFE LANDING. REPLACED FLAP POSITION TRANSMITTER IAW MM 27-58-01 PAGE 401, SYSTEM CHECKED NORMAL AND LEADING EDGE FLAPS OPERATED PROPERLY. AIRCRAFT RELEASED TO SERVICE. 2 L 7 4 4F A20WE 2007073100176 20070731 00176 NM 2007 7 31 SWAA073587 1 20070719 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 727A, STR 5L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007073100184 20070731 00184 NM 2007 7 31 SWAA073592 1 20070719 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 727C, STR 5L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007073100187 20070731 00187 NM 2007 7 31 SWAA073596 1 20070719 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 520, STR 7R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007073100189 20070731 00189 NM 2007 7 31 SWAA073591 1 20070719 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 727C, STR 4L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007073100190 20070731 00190 GL 2007 7 31 SWAA073578 2 20070719 A 7321 7086005 MEC BOEING 737 7373H4 1384600 NM CFMINT CFM56 CFM563B1US GL NR 2 ENGINE ERRATIC A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 29 328SW 23692 DIVERSION / DECLARED EMERGENCY, NR 2 ENG N1 ROLLBACK IND. REMOVED AND REPLACED NR 2 ENG MEC. 2 L 7 2 4F 4 F RT A16WE E2GL 2007073100191 20070731 00191 NM 2007 7 31 SWAA073607 1 20070720 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 632SW 27707 DURING MV2 CHECK, FOUND FWD EEPLS INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2007073100192 20070731 00192 NM 2007 7 31 SWAA073602 1 20070721 A 3397 BR2013 WIRE BOEING 737 7377H4 1384404 NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 413WN 29819 EEPLS INOP AT FWD END. REPAIRED LOOSE WIRES PER MM. 2 L 7 2 4F RT A16WE 2007073100193 20070731 00193 EU 2007 7 31 2007UALA01502 1 20070514 A 3520 D3521430 OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN WRONG PART A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 454UA 1104 CABIN SEAT 6ABC OXYGEN MASKS (4 EA) HAVE WRONG PART NUMBERS ON THEM. INSTALLED 4 EA CORRECT MASKS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007073100194 20070731 00194 NM 2007 7 31 2007UALA02243 1 20070624 A 2432 BATTERY BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU E&E BAY DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 337UA 24241 CREW REPORT: AC FOUND WITH BATTERY DEAD AND BATTERY C/B POPPED. RESET AND POPPED AGAIN. FOUND FAULTY BATTERY AND BATT ERY CHARGER. REPLACED BATTERY AND BATTERY CHARGER. NO FAULTS FOUND ON BOTH THE BATTERY AND BATTERY CHARGER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007073100198 20070731 00198 2007 7 31 2007UALA02293 4 20070628 A 2565 680146904 O-RING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EVAC SLIDE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 196UA G1159 28715 LOW BOTTLE PRESSURE. PIN HOLE LEAK AROUND O-RING ON PRESSURE GAUGE. REPLACED O-RING, RECHECKED, NO LEAKS FOUND, REPLAC ED WITH STOCK BOTTLE. SLIDE PROBLEM ROOT CAUSE: O-RING HARDENED DUE TO HEAT & OXIDATION & LOST ELASTICITY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100199 20070731 00199 NM 2007 7 31 NOCA14307 1 20070723 A 2560 P207003001 FLASHLIGHT BOEING 757 75728A 1384976 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 752NA 28174 DOOR R4 FLIGHT ATTENDANT FLASHLIGHT IS INOP. REMOVED AND REPLACED FLASHLIGHT ASSY AT DOOR 4R. 2 L 7 2 4F RT A2NM 2007073100200 20070731 00200 NM 2007 7 31 KCSA071247 1 20070724 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 UPPER DECK SEAT TRACK CORRODED AT LBL-65 BETWEEN BS 580 AND 700. 2 L 7 4 4F RT A20WE 2007073100204 20070731 00204 NM 2007 7 31 KCSA071253 1 20070725 A 5411 FRAME BOEING 747 7472B4B 138481B NM NR 4 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NR 4 PYLON NAC STA 221 BULKHEAD O/B FRAME CRACKED. 2 L 7 4 4F RT A20WE 2007073100206 20070731 00206 EA 2007 7 31 COMA0770039 1 20070718 A 3252 498003 SHIMMY DAMPENER CNDAIR CL600 CL6002C10 1390015 EA LT MLG WORN A COMA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 378CA 10457 10097 FLIGHT 5058 - MLG SHIMMY ON TAKEOFF AND GEAR RETRACTION. AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED LEFT MLG SHIMMY DAMPENER. 2 L 7 2 4F RT A21EA 2007073100208 20070731 00208 EA 2007 7 31 COMA0760490 1 20070719 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 918CA 7018 PERMANENT REPAIR REQUIRED ON PREVIOUSLY APPLIED TEMP REPAIR TO FS 621.00 REAR PRESS BULKHEAD FRAME AT WEB BL 0.00 WL 111 .09. APPLIED PERMANENT REPAIR ANGLE ON FS 621.00 BULKHEAD IAW BOMBARDIER REO 601R-53-61-1285. 2 L 7 2 4F RT A21EA 2007073100210 20070731 00210 WP 2007 7 31 MWEA070161 1 20070724 A 2432 30475002 BATTERY DOUG DC9 DC981 3022081 WP E&E BAY MALFUNCTIONED A MWEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 13 803ME 48029 AFTER LANDING, SMELLED ELECTRICAL ODOR, CREW NOTICED SMOKE COMING OUT NEAR E&E DOOR. REMOVED AND REPLACED LEFT & RIGHT MAIN BATTERIES. 2 L 7 2 4F A6WE 2007073100211 20070731 00211 NM 2007 7 31 TIPR200736004 1 20070725 A 5330 SKIN BOEING 767 767222 1385122 NM FUSELAGE GOUGED B TIPR K NONE O OTHER IN INSP/MAINT 1 SO 05 609UA 21870 FUSELAGE EXTERIOR SKIN GOUGED BS 1197 STRINGER 36L TO 37L. REMOVED FASTENERS TO FACILITATE OTHER MAINTENANCE IN ACCORDA NCE WITH B767 SRM 51-40-02. REMOVED DAMAGE FOUND TO BE BEYOND LIMITS PER THE Z DIMENSION MEASUREMENT IN ACCORDANCE WITH B767 SRM 53-00-01. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IN ACCORDANCE WITH B767 SRM 53-00-01 FIG 201. R EFERENCE SERVICE ORDER 599125 OPERATION 23109. 2 L 7 2 4F RT A1NM 2007073100214 20070731 00214 EA 2007 7 31 TRAX200701034 1 20070721 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 754EV 10173 FS 280 FWD CENTER FLOOR SUPPORT ANGLE CRACKED. COMPLIED WITH INSPECTION OF THE PRESSURIZATION SYSTEM MANUAL MADE MORTO R AND ALTITUDE LIMITATION IAW PART A OF BOMBARDIER ALERT SERVICE BULLETIN A670BA-21-022. NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2007073100215 20070731 00215 EA 2007 7 31 TRAX200701035 1 20070721 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 754EV 10173 LEFT LOWER FS 280 WEB HAS CORROSION. [07-31-07] CORROSION FOUND TO BE OUT OF LIMITS, REPLACED OF LT LOWER FS 280 WEB PER REO 670-53-11-052. 2 L 7 2 4F RT A21EA 2007073100216 20070731 00216 EA 2007 7 31 TRAX200701036 1 20070721 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 754EV 10173 RIGHT LOWER FS 280 WEB HAS CORROSION. [07-31-07] CORROSION FOUND TO BE OUT OF LIMITS PER: REO 670-53-11-052, REPAIRE D IAW THE SAME EO. 2 L 7 2 4F RT A21EA 2007073100218 20070731 00218 EA 2007 7 31 TRAX200701038 1 20070721 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR BINDS A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 PAX DOOR HANDLE HARD TO OPEN/CLOSE PAX DOOR. FLT 4407 DEL 147 MINS. 2 L 7 2 4F RT A21EA 2007073100223 20070731 00223 NM 2007 7 31 BB07057 1 20070726 A 2160 11518681 CONTROLLER BOEING 757 7572B7 1384964 NM CABIN TEMP FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 201UU 17879 93 27810 FLIGHT 724, PHL-SNN: TWENTY MINUTES INTO FLIGHT, COCKPIT TEMPERATURE BEGAN TO RISE. WHEN TEMPERATURE REACHED 97F, THE CAPTAIN ELECTED TO PHL. MAINTENANCE REPLACED THE ZONE TEMP CONTROLLER. 2 L 7 2 4F RT A2NM 2007073100224 20070731 00224 EU 2007 7 31 UPS07150226 1 20070723 A 5321 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU CARGO BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 171UP 0005 INSPECTION TYPE:N/A BULK CARGO COMPARTMENT FLOOR PANEL JUST FWD OFF BCC DOOR CUTOUT HAS A .5 INCH DIAMETER HOLE THROUGH UPPER SKIN, 12 INCHES FROM RIGHT SIDE OF PANEL, 4.5 INCHES FORWARD OF AF PANEL EDGE. ACCOMPLISHED REPAIR PER SRM 53-10- 20 PERM REPAIR WITHIN 350 HOURS. PERM REPAIR IS DEFERRED UNDER D355018. 2 L 7 2 4F RT A35EU 2007073100228 20070731 00228 WP 2007 7 31 UPS07850236 1 20070724 A 3397 CONNECTOR DOUG DC8 DC871F 302199D WP CABIN DISCONNECTED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTING INOP. RE-ATTACHED POWER SUPPLY CONNECTOR. OPS CHECK GOOD REF DC8 MM 38-50- 01-2. 2 L 7 4 4F RT 4A25 2007073100229 20070731 00229 WP 2007 7 31 UPS07850237 1 20070719 A 3350 BATTERY DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS WILL NOT COME ON DURING BATTERY CHECK. REMOVED AND REPLACED EMERGENCY LIGHTIN G BATTERY IAW MM 33-50-01-2. 2 L 7 4 4F RT 4A25 2007073100231 20070731 00231 NM 2007 7 31 UPS07M50219 1 20070521 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C CTR CARGO STA 1561 LONGERON R43 FOUND WITH CORROSION AS MARKED. DAMAGED LONG REMOVED & TRIMMED OFF PE R SRM 53-10-00 V1 R38. HFEC INSP CARRIED OUT PER DAC NDTSPM R13 06-10-01.001 FOUND NO CRACK EVIDENT. REPAIR SPLICE FAB PER SRM 53-10-00 V1 R38. REP LONG & SPLICE FASTENER HOLES PICK UP PER SRM 51-31-01V2 R38. REPAIR LONG & SPLICE INSTAL LED PER SRM 51-31-01 V2 R38. 2 L 7 3 4F RT A22WE 2007073100233 20070731 00233 NM 2007 7 31 UPS07M50221 1 20070521 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C CTR CARGO STA 5-113, LONGERON R43 FOUND WITH CORROSION AS MARKED. CTR CARGO STA 5-99 TO 5-119 DAMAGED LONG TRIMMED OFF PER SRM 53-10-00 V1 R38. HFEC INSP CARRIED OUT PER DAC NDTSPM R13 06-10-01.001 FOUND NO CRACK EVIDENT . REP LONG & SPLICE FABRICATED & FASTENER HOLES PICK UP PER SRM 53-10-01 V1 & SRM 51-31-01 V2 R38. REPAIR LONG & SPLIC E INSTALLED PER SRM 51-31-01 V2 R38. 2 L 7 3 4F RT A22WE 2007073100235 20070731 00235 NM 2007 7 31 UPS07M50228 1 20070523 A 5320 BRACKET DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C CTR CARGO BETWEEN STA 1541-1561 BETWEEN LONGERON L42 & L43 PARTITION BRACKET FOUND WITH CORROSION AS M ARKED. CORROSION REMOVED PER SRM 51-21-01 V1 R38. MATL TK:0.063" TK RMV:0.036" THK REM:0.027" FOUND EXCEEDED LIMIT PER SRM 53-00-01 V2 FIG 1A R38. NEW BRACKET FAB PER DOC DWG ACA7049 MATL USED 7075-0-0.063". BRACKET HEAT TREATED PER DPS 7.00-1 & HARDNESS VALUES HRB88.8 PER DPS1-05.3. BRACKET FASTENER HOLES PICK UP & INSTALLED PER SRM 051-31-01 V1 R38. 2 L 7 3 4F RT A22WE 2007073100237 20070731 00237 NM 2007 7 31 UPS07M50230 1 20070529 A 5313 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C AFT CARGO STA 1853-1871 LONGERON R48 FOUND LONGERON SPLICE WITH CORROSION AS MARKED. NEW SPLICE FAB P ER DOC DWG: AGA7438. FPI CARRIED OUT IAW BOEING DPS 4.707 & FOUND NO CRACK EVIDENT. NEW SPLICE FASTENER HOLES PICK UP PER SRM 51-31-01 V2 R38. NEW SPLICE REPROTECTED & PRIMER TOUCHED UP PER SRM 51-21-01 V2 R38. NEW SPLICE 02EA INSTALLE D PER SRM 51-31-01 V2 R38. 2 L 7 3 4F RT A22WE 2007073100238 20070731 00238 NM 2007 7 31 UPS07M50231 1 20070529 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C AFT CARGO STA 1960 LONGERON R40 FOUND WITH CORROSION AS MARKED. AFT CARGO STA 1950 TO 1960 LONG R40 R EMOVED & TRIMMED OFF PER SRM 53-10-01 V1 R38. HFEC INSP CARRIED OUT PER DAC NDTSPM R.13 06-10-01.001 & FOUND NO CRACK E VIDENT. REP LONG & SPLICE FAB & FASTENER HOLES PICK UP PER SRM 53-10-00 V1 R38 & SRM 51-31-01 V2 R38. REPAIR LONG & SP LICE INSTALLED & ACCESS FRAME & SHEAR CLIP INSTALLED PER SRM 51-31-01 V2 R38. 2 L 7 3 4F RT A22WE 2007073100239 20070731 00239 NM 2007 7 31 UPS07M50232 1 20070530 A 5754 SKIN DOUG MD11 MD11F 3023600 NM L/E SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C LEFT DROOP L/E UPPER O/B SKIN FOUND CRACK AS MARKED. REPAIR DOUBLER FAB PER SRM 57-10-00 FIG 26 V1 R3 8. HFEC INSP CARRIED OUT PER DAC NDTSPM R.13 06-10-01.001 FOUND CRACK APPROX 1.5 INCH. DOUBLER HEAT TREATED PER DPS5.0 0-2 & HARDNESS VALUES 41.8 PER DPS1.05-5. HOLES & NEW DOUBLER PICKED UP PER SRM 51-21-01 V2 R38. THE DROOP L/E INSTALL ED PER AMM27-80-10R.55. OPERATIONAL TEST CARRIED OUT REFER TO TC 1175. 2 L 7 3 4F RT A22WE 2007073100240 20070731 00240 SO 2007 7 31 C2XA07IA173 1 20070724 A 3350 78241 INVERTER EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15941 145035 IAH - FLIGHT 2533, DURING POSTFLIGHT INSPECTION THE RIGHT HAND EMERGENCY EXIT MARKER LIGHT WAS FOUND TO BE INOP. MAINTE NANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED. 2 L 7 2 4F RT T00011AT 2007073100241 20070731 00241 SO 2007 7 31 C2XA07IA174 1 20070721 A 3350 744436 SIGN EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12142 145735 AUS - DURING SERVICE CHECK THE UPPER EMERGENCY EXIT LIGHT ON THE RIGHT HAND SIDE WAS FOUND TO BE INOPERATIVE. MAINTENAN CE REMOVED AND REPLACED THE AFFECTED SIGN, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. 2 L 7 2 4F RT 2007073100242 20070731 00242 NM 2007 7 31 SWAA073637 1 20070724 A 3350 0371BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 221WN 34259 DURING SCHEDULED HC1 CHECK, FOUND EEPLS LIGHT INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007073100243 20070731 00243 NM 2007 7 31 SWAA073612 1 20070722 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED MV2 CHECK, FOUND AFT CABIN LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007073100247 20070731 00247 NM 2007 7 31 SWAA073620 1 20070724 A 5330 6545766 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740D, STR 21R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007073100248 20070731 00248 NM 2007 7 31 SWAA073619 1 20070724 A 5311 6545812 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328, STR 21R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007080100001 20070801 00001 NM 2007 8 1 QXEA200701138 1 20070708 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 491 S24L CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 SUPPORT FRAME CORRODED STATION X491.00 JUST ABOVE STRINGER 24L. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-20-36, AND 51-4 0-11. 2 H 7 2 4T RT A13NM 2007080100003 20070801 00003 NM 2007 8 1 QXEA200701143 1 20070708 A 5340 ATTACH FITTING DHAV DHC8 DHC8202 2809007 NM BS 488 S23-25L CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - FRAME CLIP BETWEEN STRINGERS 25L AND 23L AT FRAME 488.5 HAS LIGHT SURFACE CORROSION. REPAIRED IAW SRM 51-20-16 , 51-20-36, AND 51-40-11. 2 H 7 2 4T RT A13NM 2007080100004 20070801 00004 NM 2007 8 1 QXEA200701144 1 20070709 A 5260 SKIN DHAV DHC8 DHC8202 2809007 NM AIRSTAIR DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - INNER SKIN OF PAX AIRSTAIR DOOR SHELL AROUND 4 NUTPLATES USED TO MOUNT DOOR SHELL HAS BARE METAL AND LIGHT SURF ACE CORROSION. REPAIRED IAW SRM 51-20-11. 2 H 7 2 4T RT A13NM 2007080100006 20070801 00006 NM 2007 8 1 QXEA200701135 1 20070705 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 467 S30-31R CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - MAINTENANCE REQUEST, CORROSION ON FRAME X467.00 BETWEEN STRINGERS 30R AND 31R. REPAIRED IAW SRM 51-20-16, 51-4 0-11, 51-20-36, 51-20-26. 2 H 7 2 4T RT A13NM 2007080100009 20070801 00009 NM 2007 8 1 QXEA200701136 1 20070705 A 5753 DOUBLER DHAV DHC8 DHC8202 2809007 NM TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - LEFT OUTBOARD FLAP HAS CHAFE DAMAGE ON INBOARD UPPER SIDE ON THE DOUBLER. REPAIRED IAW RD8/4-57-1022. 2 H 7 2 4T RT A13NM 2007080100012 20070801 00012 2007 8 1 MASA200700244 4 20070503 A 2561 P01074201 LIFE VEST CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 655BR 1786 7457 ASH 001 HNL - FOUND SEAT 2A LIFE VEST MISSING. INSTALLED LIFE VEST. 2 L 7 2 4F RT A21EA 2007080100013 20070801 00013 EA 2007 8 1 MASA200700229 1 20070430 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17358 7358 ASH 2985 PHX - FWD EMERGENCY FLOOR LIGHT STRIP WAS LOOSE. MX RESECURED THE LIGHT STRIP, OP CHECK WAS GOOD. 2 L 7 2 4F RT A21EA 2007080100015 20070801 00015 EA 2007 8 1 MASA200700212 1 20070416 A 2750 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS WARNING LIGHT A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 650ML 7137 ASH 7193 ROC - FLAPS FAIL CAUTION IN FLT AT ZERO IN CRUISE. CREW DECLARED AN EMERGENCY BUT HAD AN UNEVENTFUL LANDING. CONTRACT MX COMPLIED WITH THE FLAPS FAIL PART A PROCEDURE WITH THE RESET OF THE SYSTEM OP CHECKING GOOD. 2 L 7 2 4F RT A21EA 2007080100016 20070801 00016 EA 2007 8 1 MASA200700168 1 20070328 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS OUT OF RIG A MASA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SW 07 27172 7172 ASH 7452 BNA - AIRCRAFT HAD A FLAPS FAIL IN CRUISE WITH THE FLAP HANDLE AT ZERO. CAPT DECLARED A EMERGENCY ON APPROACH. COMPLIED WITH PART A/B, RERIGGED 2 BPSU'S. 2 L 7 2 4F RT A21EA 2007080100017 20070801 00017 EA 2007 8 1 MASA200700270 1 20070516 A 5210 LATCH CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 97325 7325 ASH 2864 PHX - PAX DOOR WOULD NOT OPEN. MX REMOVED DRIED LUBE FROM THE MECHANISM AND CLEANED THE LATCHES AND RELUBED. 2 L 7 2 4F RT A21EA 2007080100021 20070801 00021 EA 2007 8 1 MASA200700055 1 20070125 A 5220 COVER CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 902FJ 15002 ASH 2892 TUS - ROW 15D/F OVERWING EMERGENCY EXIT HANDLE INTERIOR COVER LOOSE. MX RESECURED COVER. 2 L 7 2 4F RT A21EA 2007080100023 20070801 00023 EA 2007 8 1 MASA200700213 1 20070417 A 2150 A/C PACK CNDAIR CL600 CL6002D24 1390016 EA NR 2 SMOKE A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 911FJ 15011 ASH 2632 CLT - NR 2 PACK UNCONTROLLABLE/SMOKING. MX DEFERRED PACK. 2 L 7 2 4F RT A21EA 2007080100026 20070801 00026 EA 2007 8 1 MASA200700276 1 20070518 A 5210 HANDLE CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR STUCK A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 926LR 15026 ASH 2611 CLT - PASSENGER DOOR OUTER HANDLE IS NOT FULLY CLOSING. MX UNSTUCK THE HANDLE. 2 L 7 2 4F RT A21EA 2007080100028 20070801 00028 EA 2007 8 1 MASA200700032 1 20070116 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG UNKNOWN A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 77195 9473 7195 ASH 7334 CHS - NOSE GEAR DOOR WARNING AND NOSE GEAR DISAGREE AFTER TAKEOFF. CONTRACT MX INSPECTED THE NOSE GEAR AREA AN D FOUND NO DAMAGE OR LEAKS. MX REMOVED AND REPLACED NLG PRIORITY VALVE AND SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2007080100029 20070801 00029 EA 2007 8 1 MASA200700033 1 20070116 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA LAVATORY SMOKE A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 154SF 7154 ASH 7376 GSO - CREW REPORTED TOILET SMOKE WARNING MESSAGE AND FA REPORTED SMOKE IN THE LAV. CONTRACT MX INSPECTED THE L AV COMPONENTS AND FOUND NO SIGN OF FIRE OR OVERHEATING. CONTRACT MX WITH THE CREW PERFORMED POWER ENGINE RUNS WITH THE PACKS ON AND COULD NOT GET ANYMORE SMOKE IN THE LAV. 2 L 7 2 4F RT A21EA 2007080100031 20070801 00031 EA 2007 8 1 MASA200700125 1 20070227 A 7830 THRUST REVERSER CNDAIR CL600 CL6002B19 1900309 EA LEFT UNKNOWN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7264V 7264 ASH 2869 GJT - CAPT DECLARED AN EMERGENCY DUE TO A LT REV UNLOCK CAUTION IN FLIGHT. LANDING WAS UNEVENTFUL. MX PLACED THE REV ON MEL. 2 L 7 2 4F RT A21EA 2007080100033 20070801 00033 EA 2007 8 1 MASA200700093 1 20070211 A 3213 STRUT CNDAIR CL600 CL6002C10 1390015 EA NLG UNKNOWN A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 506MJ 10073 ASH 7488 PIT - AIRCRAFT RETURNED TO THE FIELD FOR THE NLG WILL NOT RETRACT. MX SERVICED NOSE STRUT. 2 L 7 2 4F RT A21EA 2007080100034 20070801 00034 EA 2007 8 1 MASA200700149 1 20070318 A 4940 OIL COOLER CNDAIR CL600 CL6002B19 1900309 EA APU DIRTY A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 37342 7342 ASH 7424 IAD - APU FIRE WARNING WITH APU FAULT AND DOOR INHIBIT. MX CLEANED OIL COOLER AND REPAIRED LOOPS. 2 L 7 2 4F RT A21EA 2007080100035 20070801 00035 EA 2007 8 1 MASA200700275 1 20070518 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27318 7318 ASH 2872 PHX. REPORTED THE LT OVERWING EMERGENCY EXIT LT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2007080100036 20070801 00036 EA 2007 8 1 MASA200700271 1 20070516 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 97325 7325 ASH 2721 PHX - CREW REPORTED TROUBLE HAVING PROBLEM OPENING PAX DOOR. MX CLEANED AND LUBED DOOR. 2 L 7 2 4F RT A21EA 2007080100038 20070801 00038 EA 2007 8 1 MASA200700073 1 20070202 A 5220 COVER CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 902FJ 15002 ASH 2829 PHX - CREW REPORTED THE OVERWING EMERGENCY EXIT DOOR AT 15A THE DOOR HANDLE COVER AS LOOSE. MX REPLACED THE VE LCRO AND RESECURED COVER. 2 L 7 2 4F RT A21EA 2007080100048 20070801 00048 2007 8 1 MASA200700005 4 20070102 A 3418 NONE CNDAIR CL600 CL6002B19 1900309 EA NONE NONE A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 77181 7181 ASH 7283 ORD - STALL FAIL CAUTION. MX TROUBLESHOT AND SYSTEM, OPS CK NORMAL. 2 L 7 2 4F RT A21EA 2007080100050 20070801 00050 EA 2007 8 1 MASA200700211 1 20070416 A 2560 ESCAPE ROPE CNDAIR CL600 CL6002B19 1900309 EA RT CABIN DISLODGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75999 7471 ASH 7160 IAD - RT CABIN EMERGENCY ROPE FELL DOWN. MX RESECURED ROPE. 2 L 7 2 4F RT A21EA 2007080100054 20070801 00054 EA 2007 8 1 MASA200700252 1 20070508 A 2611 47359719 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY MALFUNCTIONED A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 17231 8017 7231 ASH 2777 PHX - CARGO SMOKE WARNING AND CARGO FAN FAIL CAUTION ON GROUND. MX REPLACED THE CARGO SMOKE DETECTOR AND THE F AN, OP CHECKED GOOD. 2 L 7 2 4F RT A21EA 2007080100056 20070801 00056 EA 2007 8 1 MASA200700156 1 20070321 A 3230 46193 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG UNKNOWN A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 87353 6768 7353 ASH 2709 ICT - WHILE ON APPROACH INTO PHX, THE CREW REPORTED A GEAR DISAGREE FAULT DURING EXTENSION. REMOVED AND REPLAC ED MLG AND NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2007080100057 20070801 00057 EA 2007 8 1 MASA200700118 1 20070226 A 5210 INDICATOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR STEP OUT OF POSITION A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75998 7336 ASH 7365 LGA - PAX DOOR CLOSED INDICATION IN STEP NOT VISIBLE WHEN DOOR CLOSED AND LOCKED. MX REPOSITIONED INDICATOR AN D OP CK GOOD. 2 L 7 2 4F RT A21EA 2007080100059 20070801 00059 EA 2007 8 1 MASA200700231 1 20070404 A 5312 601R36008205 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FS 621.00 CRACKED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7264V 7264 FS 621.00 PRESSURE BULKHEAD WEB HAS A .50 CRACK A LBL 18.0 WL 113. REPAIRED PRESSURE BULKHEAD WEB. 2 L 7 2 4F RT A21EA 2007080100062 20070801 00062 EA 2007 8 1 MASA200700059 1 20070127 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT LOOSE A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 17175 7175 ASH 7294 CLT - LT EMERG DOOR CAUTION IN FLIGHT. MX RESECURED DOOR, NO MESSAGES NOTED. 2 L 7 2 4F RT A21EA 2007080100066 20070801 00066 EA 2007 8 1 MASA200700024 1 20070110 A 3240 158863 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA PARKING BRAKE MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27173 16995 7173 ASH 7276 ORD - CREW REPORTED THE NLG WOULD NOT RETRACT WITH AN ASSOCIATED NLG DOOR WARNING AND GEAR DISAGREE MESSAGE. M X REPLACED PARKING BRAKE SOV GEAR SWINGS GOOD. 2 L 7 2 4F RT A21EA 2007080100067 20070801 00067 EA 2007 8 1 MASA200700030 1 20070114 A 5340 SH670314161 STRIKER CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR BENT A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 504MJ 10066 ASH 7229 CAE - SERVICE DOOR AFT CORNER SEAL STRIKER BENT. MX FOUND CRACK IN RADIUS OF AFT CORNER SEAL STRIKER. MX REPA IRED SEAL STRIKER. 2 L 7 2 4F RT A21EA 2007080100068 20070801 00068 EA 2007 8 1 MASA200700284 1 20070528 A 3397 FEEDER CABLE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17358 7358 ASH 2864 PHX - PILOT REPORTED THAT THE AISLE EMERGENCY LIGHTS FROM ROW 6 TO 8 AND THE RIGHT LOWER OVERWING EMERGENCY EXI T SIGN WERE INOP. MX REPLACED THE POWER STRIP. 2 L 7 2 4F RT A21EA 2007080100072 20070801 00072 EA 2007 8 1 MASA200700240 1 20070502 A 5220 PROXIMITY SENSOR CNDAIR CL600 CL6002D24 1390016 EA OVERWING EXIT DIRTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 923FJ 15023 ASH 2918 SBA - LT AFT OVERWING EMERGENCY EXIT DOOR CAUTION MESSAGE. MX INSPECTED, CLEANED PROXIMITY SENSOR AND IT OPS G OOD. 2 L 7 2 4F RT A21EA 2007080100073 20070801 00073 EA 2007 8 1 MASA200700250 1 20070508 A 5100 NONE CNDAIR CL600 CL6002B19 1900309 EA NONE NONE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 571ML 7209 ASH 7220 ROC - PORTABLE O2 BOTTLE USED FOR MEDICAL EMERGENCY. CONTRACT MX SERVICED AND CLEANED THE MASK ON THE PORTABLE O2 BOTTLE. 2 L 7 2 4F RT A21EA 2007080100075 20070801 00075 EA 2007 8 1 MASA200700040 1 20070120 A 5280 600330441001 DOOR CNDAIR CL600 CL6002B19 1900309 EA NLG DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 649BR 14013 7414 ASH 7163 IAD - CRACK IN NLG SPADE DOOR, LOWER RT CORNER. DAMAGE WAS CAUSED BY RT NOSE TIRE SHREDDED. AIRCRAFT FERRIED TO CAE WHERE MX REMOVED AND REPLACED NOSE DOOR. 2 L 7 2 4F RT A21EA 2007080100076 20070801 00076 EA 2007 8 1 MASA200700041 1 20070121 A 2697 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA SMOKE DETECTOR DIRTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 591ML 7388 ASH 7178 CLT - CREW REPORTED A LAV SMOKE CTN MSG. MX CLEANED SMOKE DETECTOR CONNECTIONS. OPS CHECKED NORMAL 2 L 7 2 4F RT A21EA 2007080100077 20070801 00077 EA 2007 8 1 MASA200700043 1 20070121 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 915FJ 15015 ASH 2688 CLT - CEILING EMERGENCY FLOOD LIGHT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2007080100078 20070801 00078 EA 2007 8 1 MASA200700096 1 20070211 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE FROZEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37342 7342 ASH 7352 ORD - CREW UNABLE TO OPEN SERVICE DOOR FROM INSIDE AND RAMP UNABLE TO OPEN SERVICE DOOR FROM OUTSIDE. MX FOUND THE DOOR FROZEN SHUT AND THAWED THE DOOR OUT, OPS CK GOOD. 2 L 7 2 4F RT A21EA 2007080100080 20070801 00080 EA 2007 8 1 MASA200700285 1 20070528 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 77195 7195 ASH 7429 LAN - GEAR DISAGREE ON RETRACTION. WILL FERRY PLANE TO ORD. MX REMOVED AND REPLACED PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2007080100081 20070801 00081 EA 2007 8 1 MASA200700189 1 20070406 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT UNSECURE A MASA O OTHER O OTHER CR CRUISE 1 SW 07 97325 7325 ASH 2984 PHX - RT EMERGENCY DOOR CAUTION IN FLIGHT. MX RESEATED RT EMERG DOOR. 2 L 7 2 4F RT A21EA 2007080100084 20070801 00084 EA 2007 8 1 MASA200700095 1 20070211 A 3260 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 592ML 7410 ASH 7133 IAD - CREW RETURNED TO FIELD DUE TO LANDING GEAR WOULD NOT RETRACT. MX ADJUSTED THE PROX SWITCH. 2 L 7 2 4F RT A21EA 2007080100088 20070801 00088 EA 2007 8 1 MASA200700104 1 20070218 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT UNSECURE A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 650ML 7137 ASH 7118 PWM - RT OVER WING EMERGENCY DOOR CAUTION IN FLIGHT. NO PRESSURIZATION ISSUES WERE REPORTED. MX RESEATED THE DOOR. 2 L 7 2 4F RT A21EA 2007080100089 20070801 00089 EA 2007 8 1 MASA200700241 1 20070503 A 5220 STRIKER CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT OUT OF ADJUST A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 923FJ 15023 ASH 2885 PHX. - LT AFT OVERWING EMERGENCY EXIT DOOR CAUTION MESSAGE. MX ADJUSTED STRIKER. 2 L 7 2 4F RT A21EA 2007080100090 20070801 00090 EA 2007 8 1 MASA200700243 1 20070503 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 915FJ 15015 ASH 2779 MEM - 2 CEILING EMERGENCY FLOOD LIGHTS INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2007080100091 20070801 00091 EA 2007 8 1 MASA200700145 1 20070314 A 3240 UNKNOWN CNDAIR CL600 CL6002D24 1390016 EA LT BRAKES UNKNOWN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 956LR 15056 ASH 2651 ILM - LEFT MLG BRAKE EICAS READOUT READS 7 AND 8, WITH BRAKES SMOKING. COOLED BRAKE, RAN BRAKE TEST, NO DEFECT S FOUND. 2 L 7 2 4F RT A21EA 2007080100092 20070801 00092 EA 2007 8 1 MASA200700266 1 20070513 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 918FJ 15018 ASH 2730 PHX - AFT CEILING EMERGENCY LIGHT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2007080100093 20070801 00093 EA 2007 8 1 MASA200700223 1 20070423 A 5100 NONE CNDAIR CL600 CL6002B19 1900309 EA NONE NONE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 592ML 7410 ASH 7463 ROC - FWD CABIN PBE VSI WAS PROTRUDING AND PACKAGE FELT SPONGY. MX FOUND GOOD TO FLY FOR 36 HOURS AND AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 2007080100096 20070801 00096 EA 2007 8 1 MASA200700162 1 20070326 A 3260 601R8500291 UPLOCK CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 87353 20342 7353 ASH 2922 PHX - NOSE GEAR DISAGREE, GEAR WOULD NOT EXTEND. CYCLED HANDLE AND GOT GEAR TO EXTEND. REMOVED AND REPLACED N LG UPLOCK ASSY. 2 L 7 2 4F RT A21EA 2007080100098 20070801 00098 EA 2007 8 1 FDKA200700260 1 20070511 A 5100 NONE CNDAIR CL600 CL6002B19 1900309 EA NONE NONE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17275 7275 ASH 2864 PHX - FWD FA LIFEVEST INSPECTION EXPIRED. MX INSPECTED THE LIFEVEST AND APPLIED A NEW INSPECTION LABEL. 2 L 7 2 4F RT A21EA 2007080100100 20070801 00100 EA 2007 8 1 MASA200700263 1 20070511 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 925FJ 15025 ASH 2887 PHX - EMERGENCY CALL LIGHT ON EXIT SIGN INOP. SECURED WIRING AND RELAMPED. 2 L 7 2 4F RT A21EA 2007080100101 20070801 00101 EA 2007 8 1 MASA200700264 1 20070511 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 907FJ 15007 ASH 2730 PHX - 15F EMERGENCY EXIT SIGN INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2007080100102 20070801 00102 EA 2007 8 1 MASA200700274 1 20070518 A 2520 PSU CNDAIR CL600 CL6002B19 1900309 EA ROW 2 AC DISLODGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7264V 7264 ASH 2866 LAS - PSU AT ROW 2AC FELL DOWN. MX RESECURED THE PSU. 2 L 7 2 4F RT A21EA 2007080100103 20070801 00103 EA 2007 8 1 MASA200700201 1 20070413 A 5210 ROLLER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75994 7367 ASH 7130 IAD - CREW REPORTED THE PAX DOOR HARD TO OPEN. MX REPLACED A BROKEN ROLLER ON THE DOOR ASSEMBLY. 2 L 7 2 4F RT A21EA 2007080100104 20070801 00104 EA 2007 8 1 MASA200700203 1 20070413 A 5220 DOOR CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT NONE A MASA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SW 07 923FJ 15023 ASH 7497 ORD - LT AFT EMERG DOOR WAS OPENED BY FLIGHT ATTENDANT. MX CLOSED DOOR AS REQUIRED. 2 L 7 2 4F RT A21EA 2007080100105 20070801 00105 EA 2007 8 1 MASA200700182 1 20070403 A 5220 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA DOOR WARNING UNKNOWN A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 571ML 7209 ASH 7172 GSP - LT EMERG DOOR CTN IN FLIGHT. MX COULD NOT DUPLICATE. 2 L 7 2 4F RT A21EA 2007080100106 20070801 00106 EA 2007 8 1 MASA200700226 1 20070429 A 2611 47359719 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY MALFUNCTIONED A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 77260 5773 7260 ASH 2766 PHX - CARGO SMOKE WARNING MESSAGE WITH THE DOOR OPEN. MX REPLACED THE FAILED SMOKE DETECTOR. 2 L 7 2 4F RT A21EA 2007072700026 20070727 00026 NM 2007 7 27 DU4R2007153 1 20070719 A 5753 113N20012 TORQUE TUBE BOEING BOEING 757 757232 1384965 NM TE FLAPS CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 639DL 000211 23993 FOUND RT I/B FLAP I/B TORQUE TUBE CORRODED. REPAIRED BY REMOVING AND REPLACING TUBE WITH P/N 113N2108-1 AND 113N2105-2 IAW B757 AMM 27-51-05 AND DELTA EA 06-097981-14 REV A. 2 L 7 2 4F RT A2NM 2007072700029 20070727 00029 NM 2007 7 27 DU4R2007156 1 20070719 A 5321 FLOOR PANEL BOEING 757 757232 1384965 NM BS 1713-1717 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 639DL 23993 FOUND AFT DECK PLATE BS 1713 TO BS 1717 RBL 6 TO RBL 26 CORRODED. REPAIRED BY FABRICATING AND INSTALLING DOUBLER REPAIR 7-3/8 BY 6-3/4 FROM 2024-T3 .063 IAW B757 SRM 53-30-51 FIG 201, 51-40-02 AND 51-20-01. 2 L 7 2 4F RT A2NM 2007072700033 20070727 00033 NM 2007 7 27 DU4R2007161 1 20070716 A 5340 FITTING BOEING 757 757232 1384965 NM BS 1440 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 639DL 23993 FOUND FITTING AT C-2 DOOR CORRODED (AT NUTPLATES) THRESHOLD BS 1440 S-27R. REPAIRED BY REMOVING FITTING AND INSTALLING P/N 69-45578-7 IAW B757 SRM 51-40-02 AND 51-10-02. 2 L 7 2 4F RT A2NM 2007072700034 20070727 00034 NM 2007 7 27 DU4R2007159 1 20070711 A 5321 146N5318 FLOOR PANEL BOEING 757 757232 1384965 NM BS 1681-1682 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 639DL 23993 FOUND CORRODED AFT DECK PLATE BS 1681.8 FROM LBL 14 TO LBL 29. REPAIRED BY CUTTING OUT CORRODED SHEAR SKIN AT B/L 25L A ND SECTION OF FLOORBEAM. FABRICATED AND INSTALLED REPAIR DOUBLER 17 BY 4 FROM 2024-T3 .080, REPAIR STRAPS 24 BY 1 FROM 7075-T6 .040. REPAIR ANGLES 24 BY 3 BY 1 FROM 7075-T6 .040 IAW B757 SRM 53-00-51 AND 51-10-01. 2 L 7 2 4F RT A2NM 2007072700038 20070727 00038 NM 2007 7 27 HALA0700301 1 20070722 A 2612 CONNECTOR BOEING 767 76733A 1385209 NM FIRE DETECTIONS LOOSE A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM, EICAS STATUS MESSAGE " LEFT FIRE LP2 " DISPLAYED. FOUND LOOSE CONNECTOR ON LOWER AFT DETECTOR ASSY. CONNECTOR NR TS 682B/2. PER FIM 26-11-00 SYSTEM TEST NORMAL. 2 L 7 2 4F RT A1NM 2007072700068 20070727 00068 EU 2007 7 27 07FDEA02602 1 20070724 A 5347 ASNA24737075T651 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 657FE 748 MDCC SEAT TRACK 3RH FR 45 - FR 54 20 SQ INCH CORROSION REF A300-600 AMM 53-10-16-6-02 ZONE 200. REMOVED CORROSION IAW A 300-600 SRM 51-74-10. CHECKED LIMIT FOUND TO BE OUT OF LIMIT IAW A300-600 SRM 53-10-16 FIG 101. FAB`D SEAT TRACK IAW A 300-600 DWG NR A53274005. PROTECTED SEAT TRACK IAW A300-600 SRM 51-21-10 AND 51-23-10 (ALODINE, PRIMED, TOPCOATED). IN STALLED SEAT TRACK IAW A300-600 SRM 51-40-21, 18 FOOT SECTION OF SEAT TRACK INSTALLED. 2 L 7 2 4F RT A35EU 2007072700069 20070727 00069 EU 2007 7 27 TRBA2007054 1 20070721 A 2120 UNKNOWN AEROSP ATR72 ATR72212A 8680902 EU CABIN ODOR A TRBA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 29 550LL 550 F/A REPORTED BURNING ODOR AROUND AFT GALLEY AREA AS A/C PARKED. ODOR DISSIPATED WHEN CABIN DOOR OPENED. PERFORMED DVI OF ALL LIGHTS IN THE BACK OF THE A/C FOR DAMAGE ON LIGHT FIXTURES. NO DAMAGE FOUND. PERFORMED OPT CK OF PAX COMPARTMEN T LIGHTING IAW JIC NR 33-20-00 AND FOUND WORKING PROPERLY. 2 H 7 2 4T RT A53EU 2007072700078 20070727 00078 SO 2007 7 27 SWIA200718487 1 20070709 A 2710 GA2201A RVDT EMB 120 EMB120ER 3260203 SO AILERONS BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 580SW 46 46 120348 ON TAXI CHECK, YOKE ONLY DEFLECTS APPROX 1/3 OF THE WAY TO FULL RIGHT AILERON. REPLACED NR 1 AILERON RVDT AND ALIGNED I AW MM 31-30-00. 2 L 7 2 4T RT A31SO 2007072700080 20070727 00080 NM 2007 7 27 07FDEA02534 1 20070720 A 5320 6567231 ANGLE BOEING 727 727233 138408A NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD LWR CARGO PIT CLOSEOUT WEB SUPPORT L-ANGLE AT STA 555 RT SIDE IS CRACKED MANY LOCATIONS. REMOVED AND REPLACED WITH NEW FABRICATED L-ANGLE PER BOEING DRAWING 65-67231 AND SRM 51-30-2 PG 2 AND 3. 2 L 7 3 4F RT A3WE 2007072700087 20070727 00087 NM 2007 7 27 07FDEA02541 1 20070720 A 5753 652163586 SKIN BOEING 727 727233 138408A NM ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 RT OB FLAP, TRAILING EDGE DAMAGED ON AFT FLAP. REMOVED DAMAGE AND PREPPED FOR REPAIR REF SRM 51-40-20 PARA 7 BONDED ON REPAIR DOUBLER REF SRM 51-40-20 PARA 14, 15, 19, 20, 21, 22. PRIMED AND PAINTED REF M/M 51-20-151-7. 2 L 7 3 4F RT A3WE 2007072700092 20070727 00092 NM 2007 7 27 07FDEA02546 1 20070720 A 5315 6520832 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FOUND REPAIR LOCATED AT BS 1050 FLOORBEAM UPPER CHORD FROM LBL 18" TO 22". REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR D ETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED OLD REPAIR. REPLACED REPAIR WITH NEW REPAIR. REF FEDEX DWG SR 27-53-034 REV F REPAIR 2. 2 L 7 3 4F RT A3WE 2007072700101 20070727 00101 WP 2007 7 27 07FDEA02554 1 20070720 A 3244 TIRE DOUG MD10 MD1010F 3022112 WP MLG FAILED A FDEA J A DUMP FUEL UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SO 25 396FE 4021 4021 46630 PDIS: NOTIFIED BY DEPT CONTROL TOWER AFTER T/O THAT PROBABLY HAD A TIRE FAILURE AT OR APPROACHING ROTATION. SLT VIBRA TION FELT-LIKE FROM NOSE TIRES. GEAR RETRACTED NORMALLY. DUMPED-15K FUEL. RTN TO MEM, LDG 18C W/FLAPS 50. STOPPED O N RWY. FAILED TIRE RT TRK. FOUND NR 3 TIRE BLOWN. REMOVED AND REPLACED NR 3 TIRE PER MD10-10 AMM. REPAIRED DAMAGE. 2 L 7 3 4F RT A22WE 2007072700106 20070727 00106 SO 2007 7 27 SIMA200720411 1 20070605 A 5320 14521413605 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 855AE 9744 5000 145747 LEFT OMEGA BEAM CORRODED AT FRAME 27. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007072700107 20070727 00107 SO 2007 7 27 SIMA200720419 1 20070609 A 5320 14525480603 SILL EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 819AE 13303 5000 145566 BAGGAGE DOOR LOWER SILL CORRODED. REMOVED AND REPLACED LOWER DOOR SILL IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERV ICE. 2 L 7 2 4F RT T00011AT 2007072700108 20070727 00108 SO 2007 7 27 SIMA200720414 1 20070607 A 5320 14521700007 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 855AE 9744 5000 145747 LEFT OMEGA BEAM CORRODED AT FRAME 20. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10 AND 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007072700109 20070727 00109 SO 2007 7 27 SIMA200720413 1 20070607 A 5320 14521413605 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 855AE 9744 5000 145747 CENTER OMEGA BEAM CORRODED AT FRAME 24 AND 25. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10, FIGURE 203. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007072700111 20070727 00111 EA 2007 7 27 SIMA200720109 1 20070526 A 5315 CC670341757 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 521AE 7880 3977 10142 STATION 280 FLOORBEAM CORRODED ALONG TOP FLANGE FROM BL 24L TO BL42R. SPLICED IN FRAME 280 AND EXTENSION MOUNTS IAW AM ERICAN EAGLE ENGINEERING ORDER CR-53MR-119. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007072700116 20070727 00116 NM 2007 7 27 QXEA200701172 1 20070709 A 5320 INTERCOSTAL DHAV DHC8 DHC8202 2809007 NM BS 182-202 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - EXFOLIATION CORROSION AT STATION 202.75 NEAR STRINGER 31L ON INTERCOSTAL THAT ATTACHES AT STATION 202.75 TO 182 .00. REPAIRED IAW SRM 51-40-11, 51-20-26. 2 H 7 2 4T RT A13NM 2007072700117 20070727 00117 NM 2007 7 27 QXEA200701173 1 20070714 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 370 S32L CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - FRAME ANGLE HAS CORROSION AT STATION 370.80 STRINGER 32L TO THE LEFT AND UNDERNEATH THE ATTENUATOR. REPAIRED I AW SRM 5120-11, 51-20-36, 51-20-00, 51-40-11. 2 H 7 2 4T RT A13NM 2007073000004 20070730 00004 NM 2007 7 30 DHL2007741515 1 20070720 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 680 S23-24L DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 FWD PIT, 1 DENT IN RADIUS OF FRAME AT BS 680, STR 23L TO 24L. CUT OUT DAMAGED AREA 1.5" BY 1", FABRICATED REPAIR DOUBLE R FROM 7075-T0, .071" BY 12" BY 4" BY 1", PO NR 9004690, PER B727 SRM 53-10-2 FIG 3, AND 51-40-3 FIG 1. HEAT TREATED RE PAIR PART TO 7075-T6 PER FAS.I. ER 2-37153-801 REV A. TREATED, PRIMED, AND INSTALLED REPAIR DOUBLER PER B727 SRM 51-40- 3 FIG 1, AND 51-10-2. 2 L 7 3 4F RT A3WE 2007073000007 20070730 00007 NM 2007 7 30 AWXA200700904 1 20070705 A 5311 6558280511 FRAME BOEING 737 7373G7 1384595 NM BS 360 S14-15R CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961268, CRACKED FRAME FOOT, BS 360 S14R - S15R. REPAIRED FRAME FOOT, BS 360 S14R - S15R IAW B737-300 SRM 53-00-07-2R3. 2 L 7 2 4F RT A16WE 2007073000012 20070730 00012 EU 2007 7 30 07FDEA02621 1 20070629 A 5315 A53781302202 FLOORBEAM AIRBUS 310 A310222 3930315 EU BS 1711 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 FWD CARGO COMPARTMENT, CABIN FLOOR CROSS-BEAM CRACKED AT FRAME 25 BETWEEN Y- 450 AND Y-953. IT WAS REPAIRED IN ACCORDAN CE WITH SRM SUPP 53-10-15 FIG 201 SHEET 4A. 2 L 7 2 4F RT A35EU 2007073000014 20070730 00014 EU 2007 7 30 07FDEA02623 1 20070629 A 5315 A53781840200 FLOORBEAM AIRBUS 310 A310222 3930315 EU BS 1817 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 FWD CARGO COMPARTMENT, CABIN FLOOR CROSSBEAM CRACKED AT FR 33 BETWEEN Y-450 AND Y-953. IT WAS REPAIRED IN ACCORDANCE WI TH SRM SUPP 53-10-15 FIG 201 SHEET 4A. 2 L 7 2 4F RT A35EU 2007073000016 20070730 00016 EU 2007 7 30 07FDEA02625 1 20070726 A 5313 A5397330320000 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 ALC UNDER FLOOR CORROSION ON S49L BETWEEN FRAME 64 AND 65. REMOVED CORRODED SPLICE IAW A310 SRM 51-40-21 PG 23. INSTAL LED NEW SPLICE IAW A310 SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007073000017 20070730 00017 EU 2007 7 30 07FDEA02626 1 20070726 A 5313 DAN50B05 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT PIT FRAME 68 TO 65 STRINGER 56 RIGHT CORRODED. REMOVED CORRODED STRINGER IAW A310 SRM 51-40-21. INSTALLED NEW STRI NGER IAW A310 SRM 53-10-14 PG 203. 2 L 7 2 4F RT A35EU 2007073000024 20070730 00024 EU 2007 7 30 AWXA200700898 1 20070724 A 3350 321454 POWER SUPPLY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 642AW 34978 34978 584 PHX - EEL - LOG NR 4136271 - MX REPORTED EMERGENCY ESCAPE PATH LIGHTING ROW 1AB, 2AB DIM. MX REPLACED EMERGENCY LIGHT POWER SUPPLY, L FWD IAW MM 33-52, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007073000025 20070730 00025 WP 2007 7 30 IXXA07SMN189S 1 20070630 A 5542 SKIN DOUG DC8 DC873F 302199F WP RUDDER MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON RUDDER RIGHT SIDE OUTER SKIN FROM STATION ZR 293.938, TO ZV 315.000 AND ZV 330.250. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL CLEAN ED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS AND NEW FASTE NER AT STATION ZR 271.000 TO ZR 335.260. PERFORMED RUDDER BALANCE FOUND WITHIN LIMITS (MOMENT= 2484.8 IN-LBS) IAW DC8 S RM 55-6-1 FIGURE 1, DC8 SRM 55-1-0 PAGE 1 AND SRM 51-1-21, DC8 SRM 51-1-9 TR NUMBER 51-142 AND SRM 51-1-9A TR NUMBER 51- 141, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND DC8 SRM 51-4-6 PAGES 1 AND 3. 2 L 7 4 4F RT 4A25 2007073000045 20070730 00045 SO 2007 7 30 SIMA200720702 1 20070710 A 5320 14525480603 SILL EMB 135 EMB135LR 3260305 SO ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 723AE 13150 5000 145288 BAGGAGE DOOR CUTOUT LOWER SILL CORRODED. REMOVED AND REPLACED SILL IAW EMB SRM 51-20-01, 51-20-03, 51-40-02, 51-40-04 A ND 51-40-06. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000049 20070730 00049 EA 2007 7 30 SIMA200720712 1 20070719 A 5315 CC670341757 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 511AE 10680 4000 10107 CROSS BEAM AT FRAME 280 CORRODED. REMOVED AND REPLACED CROSS BEAM IAW CRJ REPAIR STATEMENT REO670-53-11-47. AIRCRAFT R ETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007073000053 20070730 00053 EA 2007 7 30 SIMA200720715 1 20070714 A 5315 CC670341757 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 524AE 8230 5000 10154 FLOORBEAM AT STATION 280 CORRODED BETWEEN BL24L AND BL42R. SPLICED IN FRAME 280 AND EXTENTION MOUNTS IAW AMERICAN EAGLE ENGINEERING ORDER CR-53MR-119. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007073000055 20070730 00055 SO 2007 7 30 SIMA200720704 1 20070710 A 5320 14521713005 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 723AE 13150 5000 145288 GALLEY FLOOR CENTER HAT BEAM CORRODED. REMOVED AND REPLACED BEAM IAW EMB SRM 51-20-01, 51-20-03, 51-40-02 AND 51-40-04. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000060 20070730 00060 NM 2007 7 30 DHL2007741512 1 20070719 A 5320 SUPPORT BRACKET BOEING 727 7272Q9 138448M NM BS 1183 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AFT PIT RT, BS 1183, RBL 55, MAIN CABIN AFT BULKHEAD BOTTOM WEB SUPPORT BRACKET CRACKED. REMOVED CRACKED BRACKET, FABRI CATED NEW BRACKET FROM 2024-T3, .032" BY 13.75" BY 1" BY 1", PO NR 9002406, PER B727 SRM 53-10-2 FIG 5 AND 51-20-1. TRE ATED, PRIMED, AND INSTALLED NEW BRACKET PER B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007073000062 20070730 00062 WP 2007 7 30 IXXA07SMN176S 1 20070630 A 5522 SKIN DOUG DC8 DC873F 302199F WP LT ELEVATOR DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND DENTS ON LEFT ELEVATOR UPPER SKIN BETWEEN STATION XE 161.375 AND STATION XE 176 .156. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PR IMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACE. INSTALLED REPAIR PARTS AND NEW FASTENERS FROM STATION X E 132.000 TO STATION XE 246.000. PERFORMED BALANCE TO LEFT ELEVATOR FOUND WITHIN ALLOWABLE TOLERANCE LIMITS MOMENT 1450 .87 IN LBS IAW DC8 SRM 55-4-1 FIGURE 1 SHEETS1, 2, ITEM "E" AND "F", DC8 SRM 57-1-0 PAGE 1 AND DC8 SRM 51-1-21, DC8 SRM 51-1-9, T/R 51-141, SRM 51-142 DATED 04-03-06 AND 04-05-06, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND DC8 SRM 51-4-4 PAGES 1 2 L 7 4 4F RT 4A25 2007073000075 20070730 00075 EU 2007 7 30 SIMA200720605 1 20070715 A 5347 7253742407 SEAT TRACK SAAB SF340 340B 7860101 EU ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 250AE 24107 5000 340B250 SEAT TRACK AT BL36L FOUND CORRODED. REMOOVED AND REPLACED SEAT TRACK IAW SAAB SRM 51-40-21 AND 51-40-22. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007073000081 20070730 00081 EU 2007 7 30 SIMA200720606 1 20070712 A 5347 7253725191 SEAT TRACK SAAB SF340 340B 7860101 EU ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 250AE 24107 5000 340B250 SEAT TRACK AT BL0.0 FOUND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SAAB AMM 53-70-60. AIRCRAFT RETURNED TO SERVIC E. 2 L 7 2 4T RT A52EU 2007073000082 20070730 00082 EU 2007 7 30 SIMA200720608 1 20070703 A 5347 7253742409 SEAT TRACK SAAB SF340 340B 7860101 EU ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 250AE 24107 5000 340B250 SEAT TRACK AT BL36.0R FOUND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SAAB AMM 51-40-21, 51-40-22 AND 51-40-25. AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007073000088 20070730 00088 NM 2007 7 30 UIEA200700276 1 20070724 A 5511 SPAR CAP BOEING 747 747271C 1384869 NM HORIZONTAL STAB CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 HORIZONTAL STABILIZER UPPER AFT CRAFT INDICATION/HOLE DAMAGE AT LT HORIZONTAL SPAR CAP INBD OF LBL 43.5 INBD AFT HOLE. REAMED DAMAGED HOLE TO FIRST OVERSIZE (.450-.453) IAW SB 747-55A2050. NDT FINDS NO DEFECTS. BOLTS INSTALLED ON CARDS N R 8010/8011. 2 L 7 4 4F A20WE 2007073000089 20070730 00089 NM 2007 7 30 UIEA200700277 1 20070724 A 5343 TRUNNION BOEING 747 747271C 1384869 NM BS 1480 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 LT BODY GEAR OUTBOARD TRUNNION FITTING HAS CORROSION AROUND THE UPPER FACE OF THE FWD BOLT HOLE. LOCALLY BLENDED CORROS ION AREAS AND THEN SPOT FACING AROUND THE FORWARD BOLT HOLE REMOVE ALL BLEND OUTS WITHIN THE BEARING SURFACE. REF BOEI NG 8100-9. 2 L 7 4 4F A20WE 2007073000093 20070730 00093 EU 2007 7 30 07FDEA02633 1 20070726 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 FWD PIT FLOORBEAM UPPER TEE CORRODED FR 34 AT RBL 60. [08-14-07] REMOVED AND REPLACED UPPER TEE AND SPLICE PER A310- 200 SRM 53-10-15 PG 241/242 2 L 7 2 4F RT A35EU 2007073000095 20070730 00095 NM 2007 7 30 QXEA200701165 1 20070718 A 2120 NONE DHAV DHC8 DHC8202 2809007 NM NONE NONE A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 NM 09 353PH 496 PDX - FOUL ODOR THROUGHOUT CABIN AND FLIGHT DECK WORSE DURING TIMES PARKED AT GATE AND ALSO DURING APPROACH AND LANDING. CLEANED REFUSE AND SPILLED BEVERAGES FROM GALLEY WASTE CAN AREA. CLEANED FLOOR. NO FURTHER ODORS NOTED. NO PARTS RE PLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007073000104 20070730 00104 NM 2007 7 30 QXEA200701182 1 20070710 A 5310 STOP DHAV DHC8 DHC8202 2809007 NM DOOR FRAME WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - RIGHT FORWARD EMERGENCY EXIT STOPS ON FUSELAGE ARE WORN. REPAIRED IAW RD8/4-53-126. 2 H 7 2 4T RT A13NM 2007073000105 20070730 00105 NM 2007 7 30 QXEA200701183 1 20070713 A 5310 STOP DHAV DHC8 DHC8202 2809007 NM DOOR FRAME WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - LEFT CENTER EMERGENCY EXIT DOOR STOPS ON FUSELAGE HAVE LIGHT WEAR. REPAIRED IAW RD8/4-53-126. 2 H 7 2 4T RT A13NM 2007073000114 20070730 00114 SO 2007 7 30 SIMA200720426 1 20070621 A 5320 14000466401 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 811AE 13526 5000 145529 CENTER OMEGA BEAM CORRODED BETWEEN FRAMES 57 AND 59. REPAIRED DAMAGED AREA IAW IC2007-145/03984. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000115 20070730 00115 SO 2007 7 30 SIMA200720427 1 20070621 A 5320 14521725403 SILL EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 811AE 13526 5000 145529 FORWARD SERVICE DOOR SILL CORRODED BETWEEN FRAMES 18 AND 20. REMOVED AND REPLACED DOOR SILL IAW EMB SRM 51-40-02. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000117 20070730 00117 SO 2007 7 30 SIMA200720429 1 20070623 A 5311 14523512411 FRAME EMB 145 EMB145LR 3260212 SO ZONE 100 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 642AE 17161 5000 145193 DAMAGE BETWEEN FRAME 67 AND STRINGERS 15R AND 16R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB IC2007 -145/04150. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007073000120 20070730 00120 SO 2007 7 30 SIMA200720431 1 20070708 A 5340 14524131005 ATTACH ANGLE EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 816AE 13301 5000 145552 PASSENGER DOOR THRESHOLD FORWARD ATTACH ANGLE CORRODED. REMOVED AND REPLACED ATTACH ANGLE IAW EMB SRM 51-40-02. AIRCRA FT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000132 20070730 00132 NM 2007 7 30 QXEA200701159 1 20070717 A 2930 LAMP DHAV DHC8 DHC8202 2809007 NM HYD PUMP INDI NO TEST A QXEA D RETURN TO BLOCK P NO WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 358PH 506 SEA FLIGHT NR 2633, NR 2 ENGINE HYDRAULIC PUMP CAUTION LIGHT WILL NOT TEST. RELAMPED NR 2 ENGINE HYDRAULIC CAUTION LIGH T. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007073000151 20070730 00151 NM 2007 7 30 AWXA200700882 1 20070711 A 5554 D5537131800000 HINGE FITTING AIRBUS A319 A319132 3930340 NM ZONE 300 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5964296, NR 2 RUDDER HINGE BEARING HAS EXCESSIVE PLAY, VERTICLE STABILZER STATION 1926/RIB 4. REPLACED NR 2 RUDDER HINGE FITTING, VERTICLE STABILZER STATION 1926/RIB 4 IAW A319 AMM 55-36-41. 2 L 7 2 4F RT A28NM 2007073000154 20070730 00154 EU 2007 7 30 MALA070091 1 20070722 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU LAVATORY MALFUNCTIONED A MALA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 426XJ 340B426 LAVATORY SMOKE LIGHT ILLUMINATED ON MASTER WARNING IN FLIGHT. COMPLETED QRH. NO EVIDENCE OF SMOKE OR FIRE FOUND IN LAV ATORY. LIGHT REMAINED ON UNTIL SHUTDOWN. REMOVED AND REPLACED LAVATORY SMOKE DETECTOR IAW SAAB MM 26-13-10, PN 72-1112 11-000; SN OFF: A2707, SN ON: A2067. 2 L 7 2 4T RT A52EU 2007073000162 20070730 00162 NM 2007 7 30 DLM88070934 1 20070717 A 2797 BUSS CABLE DOUG MD88 MD88 3023688 NM AILERONS BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DL 49538 MOVING RT AILERON HAD NO EFFECT ON LT AILERON. FOUND AILERON BUSS CABLE BROKEN IN RT W/W. FOUND AILERON BOSS CABLE 36B BROKEN. REPLACED SAME ADJ/TEST AMM 460188. RII DEPT 625 B/O INSTALLATION AND ADJUSTMENT OF CABLE PER M/M 1506. 2 L 7 2 4F RT A6WE 2007073000177 20070730 00177 NM 2007 7 30 DHL2007741503 1 20070711 A 5320 WEB BOEING 727 7272Q9 138448M NM BS 304-312 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 NOSE LANDING GEAR LT WEB HAS CORROSION SPOTS BETWEEN BS 304 AND BS 312 (WHERE NLG TRUNNION FITTING WAS REMOVED). REMOVE D CORROSION IAW B727 SRM 51-10-6, FOUND OUT OF LIMITS IAW B727 SRM 53-10-1 FIGURE 1. CUT OUT DAMAGED AREA (DIM. 2.75" B Y 2.25"). FABRICATED REPAIR DOUBLER FROM 7075-T6 0.090" PO NR 9005216 (DIM 7" BY 4.75") AND REPAIR FILLER FROM 7075-T6 0.080" PO NR 9004670 (DIM 2.75" BY 2.25") IAW B727 53-10-2 FIGURE 2 AND 51-40-2 FIGURE 1. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2 AND INSTALLED REPAIR PARTS AT NLG LT WEB IAW B727 SRM 51-40-2 FIGURE 1 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007073000194 20070730 00194 EU 2007 7 30 AWXA200700887 1 20070714 A 5554 D5537131800000 HINGE FITTING AIRBUS 320 A320232 3930326 EU ZONE 300 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 654AW 1050 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5898129, NR 1 RUDDER HINGE FITTING WORN, VERTICLE STABILZER STATION 780/RIB 2. REP LACED NR 1 RUDDER HINGE FITTING, VERTICLE STABILZER STATION 780/RIB 2 IAW A320 AMM 55-36-41. 2 L 7 2 4F RT A28NM 2007073000196 20070730 00196 EU 2007 7 30 AWXA200700889 1 20070714 A 5554 D5537134800200 HINGE FITTING AIRBUS 320 A320232 3930326 EU ZONE 300 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 654AW 1050 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5898132, NR 3 RUDDER HINGE FITTING WORN, VERTICAL STABILIZER STATION 2279/RIB 5. R EPLACED NR 3 RUDDER HINGE FITTING, VERTICAL STABILIZER STATION 2279/RIB 5 IAW A320 AM 55-36-41. 2 L 7 2 4F RT A28NM 2007073000198 20070730 00198 EU 2007 7 30 AWXA200700891 1 20070714 A 5554 D5537131800000 HINGE FITTING AIRBUS 320 A320232 3930326 EU ZONE 300 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 654AW 1050 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5898134, NR 5 RUDDER HINGE FITTING WORN, VERTICAL STABILIZER STATION 2985/RIB 7. REPLACED NR 5 RUDDER HINGE FITTING, VERTICAL STABILIZER STATION 2985/RIB 7 IAW A320 AMM 55-36-41. 2 L 7 2 4F RT A28NM 2007073000201 20070730 00201 NM 2007 7 30 AWXA200700894 1 20070705 A 5320 65479769 CUSP WEB BOEING 737 7373G7 1384595 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5962159, CORROSION ON CUSP WEB, BS 847 - BS 867, S17L. REPLACED CUSP WEB, BS 847 - BS 867, S17L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007073100002 20070731 00002 CE 2007 7 31 DXTA200702357 1 20070722 A 3260 MS243311 DOWNLOCK SWITCH BEECH MU300 400A 1155402 CE MLG INOPERATIVE E DXTA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 136QS 1240 RK414 WHEN LANDING GEAR WAS EXTENDED THE RIGHT MAIN GEAR DID NOT INDICATE DOWNLOCK. LIGHT BULB TESTED OK. FOLLOWED CHECKLIST P ROCEDURE. ALL GEAR DETERMINED DOWN.LANDING NORMAL. RIGHT MAIN LIGHT NEVER ILLUMINATED AFTER LANDING. REMOVED AND REPLACE D R/H DOWN AND LOCK INDICATION SWITCH AND ADJUSTED IAW HAWKER 400A MM 32-60-00, 32-10-00 AND W/M 32-61-01 32-31-02 OSP C HECK GOOD, NO DISC NOTED. 2 H 7 2 4F RT A16SW 2007073100003 20070731 00003 CE 2007 7 31 DXTA200702358 1 20070722 A 3260 387 LAMP CESSNA 560 560XL 2076702 CE NLG INDICATOR BURNED OUT E DXTA A UNSCHED LANDING P NO WARNING INDICATION AP APPROACH 1 GL 07 615QS 3963 5605360 THE TOP LIGHT IN THE NOSE GEAR INDICATOR IS OUT.REPLACED LAMP WITH NEW IAW CE560XL MM CH-33-10-06, OPS CHECK GOOD. 2 L 7 2 4F RT A22CE 2007073100004 20070731 00004 CE 2007 7 31 DXTA200702356 1 20070722 A 3244 315381 TIRE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG OUT OF ROUND E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 916QS 543 543 7500116 DURING TAKE-OFF ROLL WE EXPERINCED A VIOLENT NOSE WHEEL SHIMMY BELOW 70 KNTS INDICATED. FOUND BOTH (LT & RT) NOSE TIRE S OUT OF ROUND AND FLAT SPOTTED. BOTH NOSE WHEELS ALSO UNDER TORQUE SPECS. REMOVED LT & RT NOSE WHEEL ASSY. INSTALLED NE W L/H & R/H NOSE WHEEL ASSY. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007073100007 20070731 00007 NM 2007 7 31 CALA0700368 1 20070719 A 5330 6545800 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A 1 INCH CRACK AT AFT LOWER CORNER OF R-1 DOOR CUTOUT OUTER SKIN, STA 344-360, S16R TO S17R. THE SKIN WAS REPAIRED IAW SRM 53-10-01. 2 L 7 2 4F RT A16WE 2007073100012 20070731 00012 NM 2007 7 31 2007UALA02221 1 20070625 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 RIGHT AFT LOWER FUSELAGE HAS A DENT APPROX 13 INCHES LONG BELOW AFT CARGO DOOR CUTOUT, 2 INCHES INBOARD OF STR 25R SKIN LAP BETWEEN BS 827-847. MAJOR REPAIR: CUT OUT DAMAGED SKIN AND CORRODED BEAR STRAP. INSTALLED EXTERNAL SKIN DOUBLER - TRIPLER AND STRUCTURAL FILLER PER AAR EA-I070402. 2 L 7 2 4F 4 F RT A16WE E21EU 2007073100044 20070731 00044 NM 2007 7 31 2007UALA02714 1 20070718 A 3397 80603 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EEL AT DOOR 5R XAISLE INOP. REPLACED FLOOR RIBBON CABLE AT DOOR 5 RIGHT. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100047 20070731 00047 EU 2007 7 31 2007UALA02716 1 20070715 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 467UA 1359 BURNING SMELL IN FWD GALLEY FOR SHORT TIME THEN NOTICED AUDIO INOP WITH C/B-PBS MUSIC LT POPPED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007073100052 20070731 00052 NM 2007 7 31 2007UALA02725 1 20070719 A 3397 7945243 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 SEAT 4F EEL INOP. REPLACED WITH NEW CABLE ASSEMBLY AND OP CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100054 20070731 00054 NM 2007 7 31 2007UALA02726 1 20070719 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEATS 1A, FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 SEATS 1A, 36HJK & 52HJK EEL ARE FAULTY. REPLACED WITH NEW LIGHT AND OP CHECKED GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100058 20070731 00058 NM 2007 7 31 2007UALA02727 1 20070719 A 3397 7945243 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EEL CABLE PIN BROKEN, SEAT 34HJK. REPLACED WITH NEW LIGHT CABLES AND OP' CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100060 20070731 00060 NM 2007 7 31 2007UALA02728 1 20070719 A 3397 60286 PIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 FLOOR EEL PIN BROKEN AT SEAT 34ABC. REPLACED WITH NEW COVER CABLE AND THE NON GRD OP' CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100063 20070731 00063 NM 2007 7 31 2007UALA02683 1 20070716 A 2440 RECEPTACLE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EXTERNAL POWER FIRE A UALA K NONE A FLAME/FIRE IN INSP/MAINT 1 WP 29 204UA 28713 FIRE AT EXTERNAL POWER RECEPTICLE WHILE EXTERNAL POWER CORD HOOKED UP. [08-17-07] REPLACED PRI EXTERNAL RECEPTACLE PE R MM24-41-04, OP CHK WITH GROUND POWER, OP CHECKS GOOD. GROUND POWER CABLE HAD HIGH CURRENT SHORT WHERE RUBBER INSULATIO N HAD BROKEN DOWN AND CAUSED HIGH TEMP. NOT A PROBLEM WITH AIRPLANE ALTHOUGH AIRPLANE WAS DAMAGED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007073100064 20070731 00064 NM 2007 7 31 2007UALA02684 1 20070717 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 EMERGENCY LIGHT INOP: CEILING ROW 12, 16, 17 & COCKPIT. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100066 20070731 00066 NM 2007 7 31 2007UALA02687 1 20070716 A 2121 33638 BLOWER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CARGO DETECTOR FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 549UA 25397 STATUS MESSAGE AFT CARGO DETECTOR 1. [08-17-07] FOUND BLOWER NOT OPERATING PROPERLY. REPLACED BLOWER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007073100067 20070731 00067 EU 2007 7 31 2007UALA02738 1 20070719 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS WRONG PART A UALA K NONE L W NO TEST INADEQUATE Q C IN INSP/MAINT 1 WP 29 447UA 836 ROWS 1, 2, 3 & 5 HAVE NO EEL LIGHTS. INSTALLED NEW PWR SUPPLY IN FWD POSITION WITH BORROWED PART FROM US AIRWAYS P/N 32 14-54-10, S/N 2016, AND OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007073100069 20070731 00069 NM 2007 7 31 2007UALA02741 1 20070719 A 3350 362624 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 326UA 23958 EEL LIGHTS INOP FROM SEAT 15 TO BACK OF CABIN. REPLACED TO FLEXIBLE LAMPS PER MM 33-51-90. TEST OK 33-51-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2007073100071 20070731 00071 NM 2007 7 31 2007UALA02750 1 20070719 A 3350 58674 INVERTER BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C 13802 EU EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 937UA 26668 FLOOR EEL LIGHTS INOP FROM SEAT 14C AFT TO GALLEY. REPLACED INVERTER AND CORRECTED WIRING. 2 L 7 2 4F 4 F RT A16WE E21EU 2007073100074 20070731 00074 NM 2007 7 31 2007UALA02765 1 20070720 A 5310 DOOR FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 927UA 26649 AFT CARGO PIT DOOR CUTOUT, FWD FRAME WEB CRACKED AT LOWER STOP PAD, LOWER OUTBOARD CORNER. MAJOR REPAIR: REMOVED AND IN STALLED NEW FRAME PER SRM 51-40-02, PG 1-40. 2 L 7 2 4F 4 F RT A16WE E21EU 2007073100075 20070731 00075 NM 2007 7 31 2007UALA02693 1 20070718 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 561UA 26661 FUSELAGE SKIN STA 600 - 650 STR 17L - 18L IS DAMAGED. [08-17-07] MAJOR REPAIR ACCOMPLISHED. DENT MEETS ALL LIMITS SHOWN IN SRM EXCEPT DEPTH & A-Y RATIO. ACCOMPLISHED INTERIOR INSPECTION, NO STRINGER OF FRAME DAMAGE NOTED. REMOVED DA MAGE, HFEC OPEN HOLES AND CUTOUT AND INSTALLED REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007073100076 20070731 00076 NM 2007 7 31 2007UALA02766 1 20070722 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 LEFT UPPER FUSELAGE AFT ENTRY DOOR 2L BODY TORQUE TUBE UPPER HINGE CUTOUT FWD CORNER SKIN CRACKED. MAJOR REPAIR: FABRIC ATED AND INSTALLED EXTERNAL SKIN DOUBLER REPAIR PER SRM 53-60-01 REPAIR #5 AND DRAWING 65-46561. 2 L 7 2 4F 4 F RT A16WE E21EU 2007073100077 20070731 00077 NM 2007 7 31 2007UALA02767 1 20070722 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 RIGHT UPPER FUSELAGE AFT GALLEY DOOR 2R BODY TORQUE TUBE LOWER HINGE CUTOUT FWD CORNER SKIN IS CRACKED. MAJOR REPAIR: F ABRICATED AND INSTALLED EXTERNAL SKIN DOUBLER-TRIPLER REPAIR PER SRM 53-60-01 REPAIR NR 7. 2 L 7 2 4F 4 F RT A16WE E21EU 2007073100083 20070731 00083 NM 2007 7 31 2007UALA02697 1 20070717 A 2611 SMOKE DETECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT LAVATORY FALSE ACTIVATION A UALA O OTHER W N INADEQUATE Q C FALSE WARNING IN INSP/MAINT 1 WP 29 377UA 24642 AFT LAV SMOKE DETECTOR FALSELY ACTIVATED. [08-17-07] REPLACED SMOKE DETECTOR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007073100085 20070731 00085 2007 7 31 2007UALA02700 4 20070717 A 3442 RADAR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE WEATHER RADAR SMOKE A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 779UA 26941 FLIGHT CREW REPORTED SMOKE IN COCKPIT COMING FROM WX RADAR. PULLED C/B'S AND SMOKE DISSIPATED. [08-17-07] REPLACED WX RADAR CONTROL PANEL, BITE TEST OK. AIRPLANE RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007073100095 20070731 00095 EU 2007 7 31 2007UALA02715 1 20070718 A 4920 PRESSURE VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE APU FAILED A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 471UA 1432 APU WENT INTO AUTO SHUTDOWN AND MESSAGE LP VALVE ON EICAS. APU FUEL LOW PRESSURE VALVE FAILURE. REPLACED APU FUEL LOW PRESSURE VALVE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007073100097 20070731 00097 NM 2007 7 31 2007UALA02718 1 20070718 A 3350 CAP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 F/A REPORTS AISLE LIGHT AT SEAT 1B END CAP IS COMING OFF. [08-14-07] SHORT EEL STRIP IN FRONT OF END CAP HAS BROKEN END PINS AND DOES NOT ILLUMINATE. REPLACED EEL STRIP. AIRPLANE OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007073100102 20070731 00102 NM 2007 7 31 2007UALA02723 1 20070718 A 3397 59191 CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 87UA 26713 EEL LIGHTS INOP ROWS 9-13. REPLACED JUMPER CABLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007073100103 20070731 00103 NM 2007 7 31 2007UALA02729 1 20070719 A 5415 STRUCTURE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 PYLON CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 107UA 26900 CORROSION FOUND ON NR 4 PYLON DSB OUTBOARD WING FITTING, 4 EACH ECCENTRIC BUSHINGS AROUND SURFACE, & 4 EACH DSB BEARINGS . [08-14-07] CORROSION FOUND ON NR 4 PYLON DUAL SIDE BRACE OTBD WING FTNG, 4 EACH ECCENTRIC BUSHINGS AROUND SURFACE, & 4 EACH DSB BEARINGS. CORROSION REMOVED REF MM 54-45-98. MODIFICATION ACCOMPLISHED TO CORRECT CORROSION PROBLEM. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100104 20070731 00104 NM 2007 7 31 2007UALA02730 1 20070719 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 107UA 26900 EXTERNAL FUSELAGE SKIN CORRODED AT BS 820-840 STR 46L TO 47R. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE, INSTALLED EXT ERNAL DOUBLER REPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100106 20070731 00106 EU 2007 7 31 2007UALA02732 1 20070718 A 2910 HYDRAULIC SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE YELLOW SYS LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 429UA 539 FLIGHT DIVERTED DUE TO YELLOW RSVR LOW LEVEL DISPLAYED ON UPPER ECAM. GREEN SYSTEM DROPPING TOO. FOUND PTU SUPPLY CHECK VALVE LEAKING. REPLACED PTU SUPPLY CHECK VALVE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007073100107 20070731 00107 NM 2007 7 31 2007UALA02734 1 20070718 A 3250 STEERING SYS AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NLG FAILED A UALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 29 844UA 1581 NOSE WHEEL STEERING FAILED ON TAXI OUT. FOUND SERVO 6GC FAILURE. REPLACED SERVO 6GC. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007073100108 20070731 00108 NM 2007 7 31 2007UALA02735 1 20070718 A 5330 65B1055422 PANEL BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LT A/C BAY MISSING A UALA K NONE D INFLIGHT SEPARATION NR NOT REPORTED 1 WP 29 187UA 26877 LEFT AC BAY PANEL DEPARTED ACFT. [08-14-07] A-C SERVICE DOOR MISSING FROM AIRCRAFT. FOUND ALSO HOLD OPEN ROD BROKE N OFF AND DOOR HINGES DAMAGED.DURING FURTHER INSP. FOUND PANEL ABOVE MISSING DOOR PNL PUNCTURED FROM MISSING DOOR PANEL LATCHES. INSTALLED NEW ACCESS PANEL FOR NR 2 PACK. CORRECTED OR DEFERRED ALL OTHER DAMAGE DESCRIBED. SUSPECT PANEL IM PROPERLY LATCHED & CAUGHT AIRSTREAM DURING FLIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100110 20070731 00110 WP 2007 7 31 UPS07850184 1 20070707 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 HEAVY CORROSION ON TOP OF FLOORBEAM IN C-PIT TUNNEL AT STA 1300 LBL 51. REMOVED CORROSION FROM FLOOR BEAM, FOUND TO BE OUT OF LIMITS IAW SRM 53-2-00. FABRICATED AND INSTALLED REPAIR ANGLES AT STA 1300 LBL 51 FLOORBEAM IA W SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 2007073100111 20070731 00111 WP 2007 7 31 UPS07850185 1 20070710 A 5313 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 LONGERON ATTACH FITTING CRACKED AT STA 1140 L33R. REMOVED LONGERON END FITTING AT STA 1140 L33R IAW SRM 51-1-20D. LOCATED, DRILLED UP, AND INSTALLED LONGERON END FITTING AT STA 1140 L33R IAW SRM 51-3-2, AND SRM 51-1-20D . 2 L 7 4 4F RT 4A25 2007073100112 20070731 00112 WP 2007 7 31 UPS07850191 1 20070710 A 5313 3758496U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 LONGERON END FITTING CRACKED AT STA 1140 L35L. REMOVED L35L END FITTING AT STA 1140 IAW SRM 51-1-20D . LOCATED, DRILLED UP, AND INSTALLED L35L END FITTING AT STA 1140 IAW SRM 51-3-2, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007073100113 20070731 00113 WP 2007 7 31 UPS07850192 1 20070708 A 5542 SKIN DOUG DC8 DC873F 302199F WP RUDDER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 LEFT SIDE OF RUDDER SKIN ZR 251 HAS CORROSION. REMOVED SKIN PANEL ON LEFT SIDE OF RUDDER STA ZR 251 IAW SRM 51-1-21. FABRICATED AND INSTALLED LEFT RUDDER SKIN PANEL AT STA ZR 251 IAW SRM 51-3-2, SRM 51-1-9A, AND DWG 565 5077. 2 L 7 4 4F RT 4A25 2007073100114 20070731 00114 WP 2007 7 31 UPS07850195 1 20070622 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE UPPER RIB CRACKED AT XFS 697. STOP DRILLED CRACK AT XFS 697 RIGHT WING I AW SRM 51-1-21. INSTALLED DOUBLER IAW SRM 57-03-01 AND 57-02-00. 2 L 7 4 4F RT 4A25 2007073100115 20070731 00115 NM 2007 7 31 SWAA073570 1 20070719 A 5313 6551698 STRINGER SPLICE BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007073100116 20070731 00116 NM 2007 7 31 SWAA073569 1 20070719 A 2560 6557463 FITTING BOEING 737 7373Y0 1384671 NM L1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FIT TING PER SRM. 2 L 7 2 4F RT A16WE 2007073100117 20070731 00117 NM 2007 7 31 SWAA073568 1 20070719 A 2560 6557463 FITTING BOEING 737 7373Y0 1384671 NM L1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FIT TING PER SRM. 2 L 7 2 4F RT A16WE 2007073100119 20070731 00119 NM 2007 7 31 SWAA073559 1 20070719 A 3350 8200448401 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 403WN 29815 L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007073100122 20070731 00122 SO 2007 7 31 LR7A07059 1 20070719 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE PUNCTURED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 556 4606 DURING POST FLIGHT INSPECTION, MAINTENANCE NOTED FUSELAGE SKIN PUNCTURED AND BULKHEAD DAMAGED AT FS 800E TO FS 817E, WL 126, LBL 15 TO RBL 15. INTERIM REPAIR PERFORMED AT ANC IAW EO5330-419-ERA, AIRCRAFT FERRIED TO WSAP FOR PERMANENT REPAI R OF SKIN AND BULKHEAD. 2 H 7 4 4T A1SO 2007073100123 20070731 00123 EU 2007 7 31 UPS07150193 1 20070717 A 5297 CONNECTOR AIRBUS A300 A300F4622R 3930360 EU WARNING SYS MALFUNCTIONED A IPXA K NONE L NO TEST UK UNKNOWN 1 SO 01 127UP 0811 INSPECTION TYPE:N/A ESCAPE SLIDE WARNING LIGHT FOUND INOP ON PREFLIGHT. DEFER PER MEL 52-73-01-1. *SUPPLEMENTAL SDR* RESET CONNECTOR ON ASPSU. PERFORMED SUCCESSFUL OPERATIONAL TEST IAW AMM 52-73-00-05. THIS CLEARS DEFERRAL M354613. PL ACARD REMOVED. 2 L 7 2 4F RT A35EU 2007073100127 20070731 00127 WP 2007 7 31 UPS07850194 1 20070718 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP CARGO BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:N/A HOLE IN CARGO COMPT 33 FLOOR, APPROX LOCATION FS 1069, LBL 40. PERFORMED INTERIM REPAIR IAW EO DC8- 5320-8724. ENTERED IN DEFERRED ITEM LOG CONTROL NR D354723. PERFORMED PERMANENT REPAIR PER EO DC8-5320-8724-APP C. T HIS CLEARS D354723. CLOSING LP 820362. 2 L 7 4 4F RT 4A25 2007073100128 20070731 00128 NM 2007 7 31 UPS07M50199 1 20070629 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C CORROSION ON SEAT TRACK CROWN & FLANGE AT STA 815-865 X=-8. CABIN SEAT TRACK X=-8 STA 815-865 CORROSI ON REMOVED & REPROTECTED SRM 512101VIIR38 . CHNNL ORG THK 0.100" MATL REMN 0.075" MATL REMV 0.025". EXCEEDS LIMIT. CORR ODED SEAT TRACK CUTOFF FRM STA 799-909 & REMOVED SRM 53-70-00VIF1R38. HFEC INSP C/O DAC NDTSPM R13 06-10-01.001 ON CUTO FF AREA, NO CRACK EVIDENT. NEW SEAT TRACK, SPLICE HAT & PLATE FAB & INSTALLED. 2 L 7 3 4F RT A22WE 2007073100130 20070731 00130 NM 2007 7 31 UPS07M50201 1 20070517 A 5730 SKIN DOUG MD11 MD11F 3023600 NM RT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C RIGHT WING - I/B FLAP LWR SURFACE O/B SEGMENT SKIN TO BE REPLACED. SKIN REMOVED PER SRM 51-31-01 V2R3 8. NEW SKIN FAB USING MATL 2024T3-0. 040" TK PER DWGARB2444. NEW SKIN HOLES DRILLED & REPROTECTED PER SRM 51-21-01V2R3 8. OK TO INSTALL NEW SKIN. NEW SKIN INSTALLED PER SRM 51-31-0 1V2R38. RIGHT WING I/B FLAP O/B SEGMENT INSTALLED PER A MM20-50-02 R.55. 2 L 7 3 4F RT A22WE 2007073100132 20070731 00132 NM 2007 7 31 UPS07M50203 1 20070514 A 5712 RIB DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C LEFT SLAT TRACK 16 STRUCTURE I/B RIB CRACKED. CRACKED RIB 16 AT LEFT WING REMOVED PER SRM 51-31-01 V2 . ATTACHMENT HOLES T XFERRED ONTO NEW RIB PER DOUGLAS DWG ARB2873. FASTENER HOLES PICKED UP PER SRM 51-31-01 V2 R38. REWORKED AREA REPROTECTED PER SRM 51-21-01 V2 R38. OK TO INSTALL. RIB 16 LEFT INSTALLED PER SRM 51-31-01 V2 R38, OPERA TIONAL TEST CARRIED OUT. 2 L 7 3 4F RT A22WE 2007073100135 20070731 00135 NM 2007 7 31 UPS07M50208 1 20070518 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C CTR CARGO STA 5-113 THRU 1541 LONGERON L47 FOUND WITH CORROSION AS MARKED. CTR CARGO STA 5-113 THRU 1 551 DAMAGED LONG TRIMMED OFF PER SRM 53-10-00 V1 R38. HFEC CARRIED OUT PER DAC NDTSPM R13 06-10-01.001 ON TRIMMED OFF A REA & FOUND NO CRACK EVIDENT. REP LONG & SPLICE FAB & HOLES PICK UP PER SRM 53-10-00 & 51-31-01 V1 R38. REP LONG & SPL ICE REPROTECTED PER SRM 51-21-01 V1 R38. REP LONG & SPLICE INSTALLED SRM 51-31-01 V1 R38. 2 L 7 3 4F RT A22WE 2007073100138 20070731 00138 NM 2007 7 31 ZZDA2007203 1 20070618 A 5313 STRAP BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 INTERNAL TIE STRAP ON LONG 23L HAS CORROSION FROM STA 1002 - 1033. INSTALLED INTERNAL TIE STRAP ON LONGERON 23L FROM ST A 1002 TO STA 1003 IAW B717 SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007073100141 20070731 00141 NM 2007 7 31 ZZDA2007206 1 20070627 A 5350 STRAP BOEING 717 717200 1383700 NM FAIRING CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 STRAP ON FAIRING SUPPORT STA 851 RT SIDE CORRODED. INSTALLED STRAP ON FAIRING SUPPORT STA 851 RT SIDE IAW B717 SRM 51-4 1-02. MATERIAL USED 7075-T6 100" SIZE 6'.3" X 2". 2 L 7 2 4F TR A6WE 2007073100144 20070731 00144 NM 2007 7 31 ZZDA2007209 1 20070605 A 5322 SHEAR TIE BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT BS 974 SHEAR TIE BETWEEN LONG 29R AND 21L. REPLACED SHEAR TIE BS 974 BETWEEN LONGERO N 29R AND LONGERON 21L IAW SRM 51-41-02. 2 L 7 2 4F TR A6WE 2007073100147 20070731 00147 NM 2007 7 31 ZZDA2007245 1 20070605 A 5311 FRAME BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT BS 927 FRAME BETWEEN LONG 29R AND 22L. REPLACED FRAME BS 927 BETWEEN LONGERON 29R AN D LONGERON 22L IAW SRM 51-41-02. 2 L 7 2 4F TR A6WE 2007073100148 20070731 00148 NM 2007 7 31 ZZDA2007246 1 20070605 A 5311 FRAME BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT BS 974 FRAME BETWEEN LONG 29R AND 21L. REPLACED FRAME BS 974 BETWEEN LONGERON 29R AN D LONGERON 21L IAW SRM 51-41-02. 2 L 7 2 4F TR A6WE 2007073100149 20070731 00149 2007 7 31 ZZDA2007247 4 20070718 A 2565 D29982225 SLIDE BOEING 717 717200 1383700 NM R1 DOOR LOW PRESSURE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 896AT 55048 R1 DOOR SLIDE PACK QUESTIONABLE PRESSURE. REPLACED R1 DOOR EVAC SLIDE ASSY PER AMM 25-60. 2 L 7 2 4F TR A6WE 2007073100153 20070731 00153 SO 2007 7 31 RAIA00707029 1 20070714 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 819HK 145062 POST FLT NR 5461 - STL - EMERGENCY LIGHT MAIN DOOR FLOOD LIGHT AND MAIN DOOR EXIT MARKER ARE OUT. MAINTENANCE RESECURED CONNECTOR TO LIGHTS, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007073100154 20070731 00154 SO 2007 7 31 RAIA00707031 1 20070716 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 810HK 145231 PRE FLT NR 8043 - RIC - RIGHTHAND OVERWING EXIT EMERGENCY LIGHT OUT. MAINTENANCE REMOVED AND REPLACED RIGHTHAND OVERWIN G EMERGENCY EXIT SIGN INVERTER, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007073100156 20070731 00156 SO 2007 7 31 RAIA00707032 1 20070718 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 833HK 145240 POST FLT NR 8025 - IAD - CEILING LIGHT INOP, EMERGENCY LIGHT AT ROW 16A. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007073100157 20070731 00157 SO 2007 7 31 RAIA00707038 1 20070721 A 2170 HOSE EMB 145 EMB145ER 3260211 SO WATER SEPARATOR LOOSE A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 808HK 145157 FLT 3532 - STL - NR 1 PACK CAUSING BURNING SMELL WITH SMOKE IN THE COCKPIT. MAINTENANCE INSPECTED THE NR 1 PACK SYSTEM AND FOUND THE WATER SEPARATOR HOSE LOOSE AND LEAKING. RE-SECURED HOSE, PERFORMED OPS CHECK OF THE BLEED SYSTEM WITH FUR THER DEFECTS NOTED. 2 L 7 2 4F RT T00011AT 2007073100159 20070731 00159 SO 2007 7 31 RAIA00707037 1 20070722 A 2450 860CC01 CONTACTOR EMB 145 EMB145LR 3260212 SO ELECTRICAL SYS INOPERATIVE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 830HK 145313 FLT NR 5521 - STL - AFTER TAKEOFF, CREW RECEIVED AN ELECTRICAL EMERGENCY ABNORMAL INDICATION ON THE EICAS. MAINTENANCE R EMOVED AND REPLACED THE ESSENTIAL BUS CONTACTOR. 2 L 7 2 4T RT T00011AT 2007073100162 20070731 00162 NM 2007 7 31 SWAA073601 1 20070721 A 3350 079123 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 219WN 32490 FWD EEPLS COVER CRACKED. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007073100163 20070731 00163 NM 2007 7 31 SWAA073605 1 20070720 A 5330 6545768 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 405.5, STR 17L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007073100164 20070731 00164 NM 2007 7 31 SWAA073603 1 20070721 A 5330 6545773 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 794, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007073100165 20070731 00165 NM 2007 7 31 SWAA073606 1 20070720 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT, BS 291, WL 233. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007073100166 20070731 00166 NM 2007 7 31 SWAA073604 1 20070721 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SPV CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED FLAP ASSY PER SRM. 2 L 7 2 4F RT A16WE 2007073100169 20070731 00169 NM 2007 7 31 SWAA073600 1 20070720 A 5315 6546804 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED RON, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 986.5, RBL 44. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2007073100170 20070731 00170 NM 2007 7 31 SWAA073580 1 20070719 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007073100174 20070731 00174 NM 2007 7 31 SWAA073577 1 20070719 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 L1 DOOR EVACUATION SLIDE GIRT BAR STOW HOOKS LOOSE. SECURED HOOKS PER MM. 2 L 7 2 4F RT A16WE 2007073100175 20070731 00175 NM 2007 7 31 SWAA073593 1 20070719 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007073100177 20070731 00177 NM 2007 7 31 SWAA073583 1 20070719 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 727A, STR 9L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007073100179 20070731 00179 NM 2007 7 31 SWAA073585 1 20070719 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 500, STR 7L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007073100180 20070731 00180 NM 2007 7 31 SWAA073586 1 20070719 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 727A, STR 3L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007073100181 20070731 00181 NM 2007 7 31 SWAA073588 1 20070719 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 727A, STR 6L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007073100183 20070731 00183 NM 2007 7 31 SWAA073590 1 20070719 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED RON, FOUND FUSELAGE STR CLIP CRACKED AT BS 727B, STR 6L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007072500165 20070725 00165 NM 2007 7 25 DHL2007784510 1 20070711 A 5313 BAC14981317075T6 STRINGER SPLICE BOEING 727 727227 1384078 NM AFT CARGO BAY CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 AFT CARGO COMPARTMENT BS 1010, STR 28R, DOUBLER HAS SURFACE CORROSION.CORRECTIVE ACTION: REMOVED AFT CARGO COMPARTMENT S TR 28R DOUBLER IAW B727 SRM 51-30-2. FABRICATED NEW DOUBLER, MATERIAL USED BAC 1498-131-7075T6, DIM 12 LONG IAW B727 SR M 53-10-2, FIG 9 AND 53-10-3, FIG 1. TREATED, PRIMED AND INSTALLED STRINGER DOUBLER IAW B727 SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 2007072500167 20070725 00167 SO 2007 7 25 SIMA200720103 1 20070518 A 5330 14520556001 SKIN EMB 135 EMB135KL 3260302 SO ZONE 200 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 854AE 9759 5000 145743 RIGHT CENTER FUSELAGE II SKIN DENTED. CUT OUT DAMAGED AREA. FABRICATED DOUBLER AND FILLER. INSTALLED IAW EMB SRM 53-2 2-01, FIGURE 201, SHEET 1. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007072500170 20070725 00170 SO 2007 7 25 SIMA200720104 1 20070521 A 5320 14521713005 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 802AE 13511 5000 145471 GALLEY CENTER HAT BEAM CORRODED. REMOVED AND REPLACED HAT BEAM IAW EMB SRM 51-40-02 AND 51-40-04. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007072500177 20070725 00177 NM 2007 7 25 QXEA200701126 1 20070705 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 488 S32R CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - CORROSION AT RIGHT STRINGER 32 STATION X488.5. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-40-11, 51-20-36, AND 51 -20-26. 2 H 7 2 4T RT A13NM 2007072500181 20070725 00181 NM 2007 7 25 QXEA200701130 1 20070710 A 5414 SKIN DHAV DHC8 DHC8202 2809007 NM NR 1 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - NR 1 NACELLE HAS A CRACK IN THE NACELLE SKIN AT THE FORWARD OUTBOARD CUTOUT RADIUS FOR THE FORWARD GEAR DOOR. REPAIRED IAW RD8/4-54-873. 2 H 7 2 4T RT A13NM 2007072500182 20070725 00182 NM 2007 7 25 QXEA200701133 1 20070705 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 488 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - MAINTENANCE REQUEST, CORROSION ON FRAME X488.500, BETWEEN STRINGERS 29R AND 31R. REPAIRED IAW SRM 51-40-11, 51 -20-36, 51-20-26. 2 H 7 2 4T RT A13NM 2007072500189 20070725 00189 SO 2007 7 25 SIMA200720001 1 20070718 A 3350 20131A BATTERY PACK EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHT FAILED A SIMA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 839AE 9665 105 145653 ESCAPE PATH LIGHTING AT EXIT ROW WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK IAW EMB AMM 33-50-04. OPERATIO NAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007072500192 20070725 00192 SO 2007 7 25 SIMA200719901 1 20070717 A 8000 DOOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL STARTER OPEN A SIMA O OTHER E G VIBRATION/BUFFET MULTIPLE FAILURE CL CLIMB 1 SW 21 630AE 145132 CAE BUFFET FELT FIVE MINUTES AFTER CLIMB-OUT AT APPROXIMATELY 12,000 FEET, AT CRUISE AIRCRAFT ACCELERATED ONLY TO 232 KNOTS AT 33,000 FEET. RIGHT ENGINE PARAMETERS HIGHER THAN LEFT ENGINE, POST FLIGHT INSPECTION REVEALED AIR TURBINE STARTER DO OR OPEN AND OUTER BYPASS DUCT ACCESS PANEL MISSING ON THE NUMBER ONE ENGINE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007072500199 20070725 00199 WP 2007 7 25 07FDEA02526 1 20070719 A 5322 SHEAR TIE DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CLG WHEEL WELL CAVITY, CORROSION ON SHEAR TIE/LONGERON AT STA 15012 LONGERON 50L. REMOVED, FABRICATED AND INSTALLED NEW SHEAR-TIE/ FRAME IAW MD/DC10 SRM51-33-01 VOL II , 53-00-01 FIG 1B VOLI , 51-35-01 VOLII AND DWG AEA0273 REV G. 2 L 7 3 4F RT A22WE 2007072500200 20070725 00200 SO 2007 7 25 SIMA200720420 1 20070609 A 5320 14522178005 SILL EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 819AE 13303 5000 145566 SERVICE DOOR SILL FOUND CORRODED. BLENDED CORROSION AREA, FILLED WITH HYSOL EA934NA RESIN, APPLIED ALODINE, PRIMER AND TOP COAT TO BLENDED AREA AND INSTALLED DOULBER IAW EMB SRM 53-21-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007072500207 20070725 00207 SO 2007 7 25 SIMA200720403 1 20070603 A 5320 14530642401 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 806AE 13290 5000 145503 LEFT OMEGA BEAM CORRODED AT FRAMES 24 AND 25. REPAIRED OMEGA BEAM IAW EMB IC2007-145/03695. AIRCRAFT RETURNED TO SERVI CE. 2 L 7 2 4F RT T00011AT 2007072500215 20070725 00215 NM 2007 7 25 DHL2007741508 1 20070719 A 5320 INTERCOSTAL BOEING 727 7272Q9 138448M NM BS 950A CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AFT PIT RT BS 950A PLUS 4" INTERCOSTAL WEB CRACKED, CORRODED AT AREA UNDERNEATH SIDE WALL PANEL BETWEEN STR-26R AND STR- 27R. REMOVED CRACKED ANGLE IAW B727 SRM 51-30-2. FABRICATED NEW ANGLE FROM 2024-T3 0.063" PO NR 9004940 (DIM 18 1/8" B Y 1 1/2") IAW B727 SRM 53-10-2 FIG 5 AND 51-10-3 AND 51-20-1. TREATED AND PRIMED AREA AND NEW ANGLE W B727 SRM 51-10-2 AND INSTALLED NEW ANGLE AT AFT PIT RT BS 950A PLUS 4" INTERCOSTAL WEB IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007072500219 20070725 00219 NM 2007 7 25 QXEA200701169 1 20070718 A 2160 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM A/C PACK UNKNOWN A QXEA O OTHER O OTHER CR CRUISE 1 NM 09 428QX 4160 SEA - ON FLIGHT 2267, CABIN PACK HOT CAUTION LIGHT ILLUMINATED DURING CRUISE FLIGHT. AFTER RUNNING CHECKLIST, CAUTION L IGHT WENT OUT. MAINTENANCE INTERRAGATED CDS FOUND 3A02-CABTSOV IN FAULT HISTORY, COMPLIE WITH FIM. CABIN PACK HOT CAUT ION CT DID NOT ILLUMINATE, COMPLIED WITH FIM. FOR THE ECS, RAN THE ECS AND CAB PACKS FULL HOT/COLD SEVERAL TIMES WITHOU T DEFECTS. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007072500220 20070725 00220 NM 2007 7 25 QXEA200701168 1 20070715 A 3010 BOOT BOMBDR DHC8 DHC8402 1390042 NM DE ICE SYSTEM DAMAGED A QXEA O OTHER O OTHER CR CRUISE 1 NM 09 403QX 4037 SJC - ON FLIGHT 2453, AFTER SELECTING BOOT DE-ICE TO SLOW, RECEIVED A DE-ICE PRESSURE CAUTION LIGHT. AFTER RUNNING CHEC KLIST AND RE-SELECTING BOOTS ON, CAUTION LIGHT REAPPEARED AND ONE LIGHT ON OUTBOARD LEADING EDGE ON RIGHT SIDE DID NOT L IGHT ON FIRST CYCLE, BUT DID ON THE SECOND CYCLE. MAINTENANCE INSTALLED PATCH ON BOOT. LEAK CHECK GOOD. AIRCRAFT RETU RNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007072600001 20070726 00001 NM 2007 7 26 QXEA200701162 1 20070717 A 5210 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR UNKNOWN A QXEA C ABORTED TAKEOFF J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 400QX 4030 FCA - ON FLIGHT 2285 ABORTED TAKEOFF, ON START OF TAKEOFF ROLL, RECEIVED A MASTER WARNING WITH FUSELAGE DOOR, AFT PASSEN GER DOOR. MAINTENANCE PERFORMED OPS TEST OF THE AFT PAX DOOR IAW AMM TASK 52-12-00-710-802, PG 504-506 PAR 1-4. OPS CHE CK GOOD. INTERROGATED PSEU. NO PRESENTS FAULTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007072600089 20070726 00089 NM 2007 7 26 QXEA200701206 1 20070722 A 2730 3985001007 CONTROL UNIT BOMBDR DHC8 DHC8402 1390042 NM ELEVATORS MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 422QX 984 984 4150 EUG FLIGHT NR 2330: WHEN CONDUCTION T/O WARNING TEST PRIOR TO T/O, WARNING HORN SOUNDS WITH ELEVATOR TRIM INDICATOR IN N U HALF OF THE RANGE. WARNING HORN DOES NOT SOUND WITH INDICATOR IN ND AREA OUTSIDE OF T/O RANGE. ELEVATOR TRIM TEST OP ERATES NORMAL. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE REMOVED AND REPLACED PCECU 8 IAW Q400 AMM TASKS 27-00-01-000-80 2 AND 27-00-01-400-802. OPS CHECK AND FUNCTIONAL TEST GOOD. ALSO, PERFORMED FUNCTIONAL TEST OF THE TAKEOFF WARNING SYS TEM IAW TASK 31-52-00-720-801. FUNCTIONAL TEST PASSED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007072600090 20070726 00090 EU 2007 7 26 F3LA200700179 1 20070724 A 5315 D5347217220400 FLOORBEAM AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 803FR 5201 2017 DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM INBD OF L2 DOOR GIRT BAR CUTOUTS HAD LIGHT TO MODERATE CORROSION AT ALL NUT PLATE ATTACH POINTS. REPLACED FLOORBEAM IAW A318 SRM 51-42-11, PARA 5-7. 2 L 7 2 4F RT 2007072600091 20070726 00091 NM 2007 7 26 QXEA200701208 1 20070722 A 6120 697072004 GOVERNOR BOMBDR DHC8 DHC8402 1390042 NM NR 2 PROPELLER MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 430QX 13 13 4163 BOI FLIGHT NR 2237: NR 2 PROP FAILED TO COME OUT OF FEATHER FOR APPROXIMATELY 5 MINUTES AFTER ENGINE START. AIRCRAFT RE TURNED TO BLOCK. MAINTENANCE REMOVED AND REPLACED NR 2 PROP OVER SPEED GOVERNOR WITH SERVICEABLE UNIT IAW Q400 TASK 61- 20-26-000-801 FOR REMOVAL AND TASK 61-20-26-400-801 FOR INSTALLATION. C/W OPS CHECK OF THE OSG IAW TASK 61-20-00-710-80 3 OF Q400 AMM. OPS TEST GOOD. C/W FUNCTIONAL TEST OF THE PROP TIME TO UNFEATHER IAW Q400 MM TASK 61-20-00-720-801. OP S CHECK GOOD. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007072600092 20070726 00092 NM 2007 7 26 QXEA200701203 1 20070721 A 2120 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM GALLEY ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 403QX 4037 PDX FLIGHT NR 2416: FA REPORTS ELECTRICAL SMELL IN GALLEY AREA. MAINTENANCE PERFORMED A GVI OF THE AFT GALLEY, MAPCOS A ND FA CONTROL PANELS. NO DEFECTS WERE NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007072600093 20070726 00093 NM 2007 7 26 QXEA200701170 1 20070718 A 3350 6138001 POWER SUPPLY BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY LIGHTS INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 15850 15850 4030 SEA-WHILE PERFORMING CHECK OF THE EMERGENCY LIGHTS, FOUND VERY AFT LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REP LACED POWER SUPPLY UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007072600094 20070726 00094 NM 2007 7 26 07FDEA02530 1 20070720 A 5310 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 CENTER ACCESSORY COMPARTMENT BILGE AREA AT LONGERON 51R BETWEEN STA 1139 AND STA 1159, FOUND CORROSION. [08-06-07] R EMOVED AND REPLACED WITH NEW LONGERON AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007072600095 20070726 00095 NM 2007 7 26 07FDEA02531 1 20070720 A 5730 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 CRACK INDICATIONS REVEALED IN 04 EACH FASTENER HOLES TOWARDS EDGE OF ACCESS CUTOUT IN LEFT WING LOWER SKIN ACCESS DOOR C UTOUT BETWEEN XORS = 683.4 AND XORS = 713.6. [08-06-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-112359, REPAIR CLAS SIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007072600096 20070726 00096 NM 2007 7 26 07FDEA02532 1 20070720 A 5730 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 CRACK INDICATIONS REVEALED IN 04 FASTENER HOLES TOWARDS EDGE OF ACCESS, CUTOUT IN RIGHT WING LOWER SKIN ACCESS DOOR CUTO UT BETWEEN XORS = 683.4 AND XORS = 713.6. [08-06-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-112360, REPAIR CLASS IFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007072700008 20070727 00008 EU 2007 7 27 07FDEA02567 1 20070723 A 5322 A5397421621590 SHEAR TIE AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 A L C AT FR 61 SHEAR TIE CORRODED BETWEEN S52R AND S53R. SHEAR TIE CORROSION OUT OF LIMITS IAW A310 SRM 53-10-00 TABLE 102. REMOVED AND REPLACED SHEAR TIE IAW A310 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007072700014 20070727 00014 NM 2007 7 27 07FDEA02581 1 20070723 A 5730 SKIN DOUG MD11 MD11F 3023600 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 603FE 48459 CRACK INDICATIONS REVEALED IN FASTENER HOLE TOWARDS EDGE OF ACCESS CUTOUT IN LEFT WING LOWER SKIN ACCESS DOOR CUTOUT (PA NEL 536AB). [08-09-07] REPAIR CARRIED OUT IN FASTENER HOLE TOWADS EDGE OF ACCESS CUTOUT IN LT WING LOWER SKIN ACCESS D OOR CUTOUT (PANEL 536AB) AS PER FEDEX EA 1-5710-112365, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007072700023 20070727 00023 NM 2007 7 27 HALA0700294 1 20070720 A 7830 STRUCTURE BOEING 767 767332 1382001 NM THRUST REVERSER PUNCTURED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 598HA 23278 ETOPS SIGNIFICANT SYSTEM, ON WALKAROUND FOUND DAMAGE ON LEFT INBOARD T/R COWL, 3/4 INCH PUNCTURE 18-1/2 INCH AFT OF LEAD ING EDGE AND 7-1/2 INCH BELOW MID ACCESS DOOR. ACCOMPLISHED TEMP REPAIR PER HAL-M105 FILE NR 598054. REINSP SPEED TAPE AT A-CK. PERMANENT REPAIR AT C-CK XCRIBED TO DPM FILE NR P187357-40. SILVER DOT INSTALLED. 2 L 7 2 4F RT A1NM 2007072700037 20070727 00037 2007 7 27 HALA0700299 4 20070722 A 3442 DISPLAY BOEING 767 76733A 1385209 NM WX RADAR SYSTEM MALFUNCTIONED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 581HA 28141 ETOPS SIGNIFICANT SYSTEM, L. RADAR SYS WILL NOT DISPLAY ON EITHER HSI. SWITCHED TO R RADAR SYS DISPLAY APPEARS NORMAL. RESET LEFT WX RADAR SYS C/B OPS CHK OK PER MM 34-43-00. 2 L 7 2 4F RT A1NM 2007072700043 20070727 00043 NE 2007 7 27 DL76L070948 2 20070723 A 7261 CARBON SEAL BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 175DN 69944 24803 724144 LEFT ENG OIL LOSS IN 2 HOURS INDICATION WENT FROM 11 DOWN TO3. ABOUT 20 MINS LATER DROPPED TO 2. CHANGING THROTTLE SET TING AND EICAS COMPUTERS, NO HELP. RETURNING TO JFK. OPENED NR 1 ENG PRESSURIZED GEARBOX THROUGH BREATHER. FOUND LEAK ING FROM IDG CARBON SEAL NEEDS NEW CARBON SEAL. REMOVED AND REPLACED IDG CARBON SEAL PER AMM. RAN ENG AT T/O PWR. PERF ORMED ENG LEAK CK. NO LEAKS FOUND. IDG OPS OK. CHIP DETECTORS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072700047 20070727 00047 EU 2007 7 27 07FDEA02584 1 20070723 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT PIT, STR 54L FRAME 68 TO 70 CORRODED. [08-07-07] REMOVE AND REPLACED STRINGER 54L FRAME 68 TO 70 IAW SRM 53-10-1 4 PG 203/204. 09-04-07 2 L 7 2 4F RT A35EU 2007072700052 20070727 00052 EU 2007 7 27 07FDEA02575 1 20070723 A 5313 DAN2001T79511 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 FWD PIT LEFT SIDE S45L HAS CORROSION BETWEEN FRAME 38.1 AND FRAME 38.2. REMOVED AND REPLACED S45L IAW A310-200 SRM 53-1 0-14 PG 203/204. 2 L 7 2 4F RT A35EU 2007072700053 20070727 00053 EU 2007 7 27 TRBA2007055 1 20070721 A 3350 7012210 LAMP AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHTS INOPERATIVE A TRBA O OTHER O OTHER NR NOT REPORTED 1 SO 29 540AM 540 EMERGENCY LIGHT ON MAIN PAX DOOR INOPERATIVE. REMOVED AND REPLACED LAMP IAW JIC NR 33-51-00. PERFORMED OPT CK OF EMERG ENCY LIGHTING IAW JIC NR 33-50-00 AND FOUND WORKING PROPERLY. 2 H 7 2 4T RT A53EU 2007072700066 20070727 00066 EU 2007 7 27 07FDEA02600 1 20070724 A 5347 ASNA24727075T65 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 657FE 748 MDCC SEAT TRACK 2RT FR45-FR54 8 SQ INCH CORROSION REF A300-600 AMM 53-10-16-6. REMOVED OLD SEAT PER A300-600 SRM 51-40- 21. FABRICATED NEW SEAT TRACK PER AIRBUS DRAWING 532-74005. REPROTECTED SURFACE USING ALODINE, PRIMER, TOPCOAT PER A30 0-600 SRM 51-75-10. INSTALLED NEW SEAT TRACK PER A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007072700067 20070727 00067 NM 2007 7 27 07FDEA02601 1 20070724 A 3260 656021123 ACCESSORY UNIT BOEING 727 727233 138408A NM MLG FAILED A FDEA O OTHER J WARNING INDICATION LD LANDING 1 SO 25 275FE 17397 1016 22040 AFTER LOWERING LANDING GEAR, DID NOT GET LEFT OR RIGHT GEAR DOWN LIGHTS. COMPLIED WITH QRH PROCEDURES TO VERIFY GEAR DO WN AND LOCKED. NORMAL LANDING ACCOMPLISHED. REMOVED AND REPLACED LANDING GEAR POSITION/WARNING ACCESSORY UNIT IAW 727- 200 AMM 32-09-122-5. PREMATURE REMOVAL/INSTALLATION OFF MFG 65-60211-23, POS ONL, SRL R00587, TAG 0828A5 O N MFG 65-60211-23, SRL D00020,TAG 19B559. 2 L 7 3 4F RT A3WE 2007072700072 20070727 00072 GL 2007 7 27 J4PA200701772 1 20070121 A 2421 14605010 CONTROL MODULE CIRRUS MCU130 CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO HARTZL HCJ3Y PHCJ3YF1 GL FAILED E J4PA O OTHER J WARNING INDICATION CR CRUISE 1 SO 13 121SR 751 UNK 1885 689148 FP4481B FLIGHT FROM BGF TO JZI AT 7000, 30 TO 45 MINUTES INTO FLIGHT, ALT NR 2 FAIL LIGHT CAME ON AND BATT NR 2 CB POPPED. TRIE D TO RESET BUT WOULD NOT RESET. CONTINUED ONTO JZI WITH NO OTHER PROBLEMS. DID NOT LOOSE ANY OTHER SYSTEMS. TROUBLE SH OT DISCREPANCY AND FOUND THE NR 2 FIELD CONTROL MODULE INOP. REPLACED CONTROL AND SYSTEM CHECK SATISFACTORY. 1 L 7 1 3O 3 O NT A00009CH E3SO 5 C P36EA 2007072700075 20070727 00075 EU 2007 7 27 07FDEA02606 1 20070725 A 5313 A5327400500053 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 MAIN DECK CARGO COMPT SEAT TRACK FLANGE CORRODED AT FRAME 50/51 STA 2733 Y1446. REMOVED CORROSION AND FOUND TO BE O UT OF LIMITS IAW A310 SRM 53-10-16 PG 101. FABRICATED SPLICES AND REPLACEMENT SEAT TRACK SECTION IAW A310 SRM 51-10-16 PG 201. INSTALLED SEAT TRACK REPAIR IAW A310 SRM 53-10-16. 2 L 7 2 4F RT A35EU 2007072700079 20070727 00079 NM 2007 7 27 07FDEA02533 1 20070720 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 MAIN DECK CARGO ALONG CENTER STA 1521 TO 5-93 SEAT TRACK AROUND FASTENER HOLE AREA FOUND WITH CORROSION. [08-02-07] CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 6 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007072700081 20070727 00081 NM 2007 7 27 07FDEA02535 1 20070720 A 5320 658069034 WEB BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 CABIN FLOOR WEB UPPER SURFACE HAS CORROSION AROUND FASTENERS BS 720 - 720A RBL 48. REMOVED CORROSION, FOUND WEB OUT OF LIMITS REF SRM 53-10-1, REMOVED WEB, VERIFIED MATERIAL 7075 T6-.063 A91989. FABRICATED NEW WEB REF SRM 53-10-2. TREATE D AND PRIMED REF SRM 51-10-2. INSTALLED NEW WEB REF SRM 53-10-2. 2 L 7 3 4F RT A3WE 2007072700083 20070727 00083 NM 2007 7 27 07FDEA02537 1 20070720 A 5315 652082761 FLOORBEAM BOEING 727 727233 138408A NM BS 560 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 CABIN BS 560 FLOORBEAM UPPER CHORD HAS CORROSION ON UPPER SURFACE BETWEEN LBL12 AND LBL 20. REMOVED DAMAGE IAW SRM 51-1 0-1 MAT WAS .125 REMOVED .005 -.120 REMAINS FOUND TO BE WITHIN LIMITS PERFORMED NDT FOR CRACKS, NEGATIVE RESULTS. ROTO- PEENED IAW SOPM 20-10-03 PG 16. TREATED AND PRIMED IAW SRM 51-10-2 PG 1 EA NR 7-5310713046. 2 L 7 3 4F RT A3WE 2007072700118 20070727 00118 NM 2007 7 27 QXEA200701176 1 20070704 A 5320 SILL DHAV DHC8 DHC8202 2809007 NM BS 242-247 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - CORROSION NEXT TO NUTPLATES UNDERNEATH MAIN CABIN DOOR SILL PLATE AT STATION X242.200 AND X247.00. REPAIRED IA W SRM 51-20-11, 51-40-11. 2 H 7 2 4T RT A13NM 2007073000027 20070730 00027 EU 2007 7 30 07FDEA02614 1 20070726 A 5330 SKIN AIRBUS 300 A300B4605R 3930308 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 CRACKS AT DIFFERENT HOLES AT CIRCUMFERENTIAL JOINT AT C13, AREA P9 AND BEAM 2, BOTH LT AND RT SIDE. REPAIR PERFORMED BY OVERSIZING HOLES IAW RAS 053024/026/2007 AND EA 6-5312-106506. 2 L 7 2 4F RT A35EU 2007073000028 20070730 00028 NM 2007 7 30 07FDEA02615 1 20070726 A 5347 BAC1520792 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 MAIN CABIN FLOOR SEAT TRACK IS CORRODED AT STA 1090 RBL 45 REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, .090" REMOVED. VERIFIED MATERIAL BAC1520-792 7178T6511, FABRICATED NEW SEAT TRACK, TREATED AND PRIMED NEW SEAT TRACK. INSTALLED NE W SEAT TRACK REF 27 SRM 51-30-2 PG 4. 2 L 7 3 4F RT A3WE 2007073000029 20070730 00029 NM 2007 7 30 07FDEA02616 1 20070726 A 5230 52FX15381 DOOR FRAME BOEING 727 727233 138408A NM CARGO DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 UPPER MAIN CARGO DOOR, AFT SIDE FRAME, HAS DEEP GOUGE IN PRIOR REPAIR DOUBLER, 19" UP FROME BOTTOM EDGE REMOVED OLD DO UBLER REF SRM 51-30-2, VERIFIED MATERIAL AS 7075-0-.090, FABRICATED REPAIR DOUBLER REF. PF SRM 52-30-2, HEAT TREATED T O 7075-T6, FIT AND DRILLED DOUBLER REF PFSRM52-30-2, TREATED AND PRIMED REF SRM51-10-2, INSTALLED REPAIR DOUBLER R EF. PF SRM 52-30-2 2 L 7 3 4F RT A3WE 2007073000031 20070730 00031 NM 2007 7 30 07FDEA02618 1 20070726 A 5720 652255527 SPLICE BOEING 727 727233 138408A NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LEFT WING LEADING EDGE OVER WING PANEL 3342, FORWARD SPLICE ANGLE HAS LOOSE/WORKING RIVETS AND IS CRACKED IN HALF. REPL ACED FASTENERS AND FAB SPLICE ANGLE REF 51-30-2, GMM 7-0-1001, DWG 65-22555. 2 L 7 3 4F RT A3WE 2007073000033 20070730 00033 NM 2007 7 30 07FDEA02620 1 20070726 A 5315 65649503 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 STA 848 FLOORBOARD SUPPORT BET BL 0 AND LBL 24, HAS LIGHT CORROSION AT NUTPLATE HOLES, UPPER AND LOWER FLANGES SURFACES REMOVED FLOOR SUPPORT AND INSTALLED NEW FLOORBOARD SUPPORT BL 0 TO LBL 24 NAD INSTALLED INBD AND OTBD SEAT TRACK FLANGE, STA 780 - 850 FER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007073000034 20070730 00034 EU 2007 7 30 07FDEA02635 1 20070726 A 5311 FRAME AIRBUS 310 A310203 3930313 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 FRAME FITTING C33 IS CRACKED AT RBL 60 FWD PIT FLOOR LEVEL. 08-30-07 REMOVED SLANTE PANEL 132JW, XY GUIDE, RAILS, TRA NSITION PANEL TO FOM. REMOVED FITTING, RECEIVED NEW FITTING A5377364420100 PO 582198.2. LOCATED AND DRILLED FITTING IAW A310 SRM 51-40-40, INSTALLED FITTING IAW A310 SRM 51-40-21 PARA 7, INSTALLED TRANSITION PANEL IAW A310 SRM 51-40-2 1 PARA 7. INSTALLED LATCH XY GUIDE AND RAILS IAW A310 AMM 25-52-44-4 AND 25-52-48-4. INSTALLED SLANTE PANEL 132JW IAW FEDEX A310 AMM 52-54-10-2 PART 2 B1. 2 L 7 2 4F RT A35EU 2007073000035 20070730 00035 EU 2007 7 30 07FDEA02595 1 20070724 A 5313 DAN50805 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT PIT BETWEEN FRAME 66 AND FRAME 65 STRINGER 49L CORRODED REMOVED CORRODED STRINGER 49L BETWEEN FRAME 65-66 IAW A310-2 00 SRM 51-40-21 PG 23. INSTALLED NEW STRINGER IAW A310-200 SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007073000072 20070730 00072 WP 2007 7 30 IXXA07SMN193S 1 20070704 A 5753 PANEL DOUG DC8 DC873F 302199F WP TE FLAP DEFORMED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION; FOUND RIGHT WING INBOARD FLAP LEADING EDGE UPPER PANEL DEFORMED BETWEEN STATION XW 12 3.000 AND STATION XW 136.000. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 57-7-1 FIGURE 1 PAGE 2 ITEM "F", DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-8B, AND DC8 51-1-11. 2 L 7 4 4F RT 4A25 2007073000073 20070730 00073 WP 2007 7 30 IXXA07SMN190S 1 20070630 A 5522 SKIN DOUG DC8 DC873F 302199F WP ZONE 300 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR HAS A NON STANDARD REPAIR AT UPPER SKIN AT STATION XE 187.000. R EMOVED DAMAGED AREA. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED A REA AND REPAIR PART. APPLIED SEALANT TO FAYING SURFACE. INSTALLED REPAIR PARTS AND NEW FASTENERS FROM STATION XE 132.0 00 TO STATION XE 246.000. PERFORMED BALANCE TO LEFT ELEVATOR FOUND WITHIN ALLOWABLE TOLERANCE LIMITS MOMENT 1450.87 IN LBS IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 55-4-1 FIGURE 1 SHEETS 1 AND 2 ITEM "E" AND "F", DC8 SRM 51-1-9 , T/R 51-141 AND SRM 51-142 DATED 04-03-06 AND 04-05-06, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-4-4 PAGES 1 AND 2. 2 L 7 4 4F RT 4A25 2007073000076 20070730 00076 SO 2007 7 30 SIMA200720609 1 20070716 A 5347 14530637006 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 723AE 13150 5000 145288 RIGHT NUMBER 5 SEAT TRACK SUPPORT CORRODED. CUTOUT CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB IC2007-145/ 04757A, DATED JULY 13, 2007. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000078 20070730 00078 EA 2007 7 30 SIMA200720603 1 20070707 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 504AE 11750 4000 10044 RIGHT FLIGHT DECK BULKHEAD WEB FOUND CORRODED. REPAIRED WEB IAW CRJ REPAIR STATEMENT REO0670-53-11-240, ITEMS 1 THROUGH 8. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007073000079 20070730 00079 EA 2007 7 30 SIMA200720604 1 20070707 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 504AE 11750 4000 10044 STATION 280 FLOORBEAM CRACKED AND CORRODED. REMOVED AND REPLACED FLOOR BEAM IAW CRJ REO 670-53-11-240. AIRCRAFT RETURN ED TO SERVICE. 2 L 7 2 4F RT A21EA 2007073000083 20070730 00083 EU 2007 7 30 SIMA200720607 1 20070707 A 5347 7253725193 SEAT TRACK SAAB SF340 340B 7860101 EU ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 250AE 24107 5000 340B250 SEAT TRACK AT BL18.3L FOUND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SAAB AMM 53-70-60. AIRCRAFT RETURNED TO SERV ICE. 2 L 7 2 4T RT A52EU 2007073000099 20070730 00099 NM 2007 7 30 QXEA200701177 1 20070705 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT TE FLAPS WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - LEFT INBOARD FLAP OUTBOARD LOWER TRACK HAS SEVERAL AREAS OF WEAR ON UPPER CONTACT SURFACE AT 8" AND 20" AFT OF FORWARD END. REPAIRED IAW RD8/4-57-986. 2 H 7 2 4T RT A13NM 2007073000107 20070730 00107 NM 2007 7 30 QXEA200701185 1 20070712 A 5320 SUPPORT BRACKET DHAV DHC8 DHC8202 2809007 NM PAX DOOR HINGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - CRACKED SUPPORT BRACKET AT STATION X240.50 OUTBOARD OF PASSENGER DOOR HINGE. REPAIRED IAW SRM 51-40-11, 52-10- 11. 2 H 7 2 4T RT A13NM 2007073000121 20070730 00121 EU 2007 7 30 F3LA200700181 1 20070724 A 5315 D5347218920400 FLOORBEAM AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 803FR 5201 2017 DURING C-3 CHECK, INSPECTION REPORTED AFT GALLEY RT FLOORBEAM -Y1292, FR 68 TO FR69 CORRODED AT NUT PLATE FASTENER LOCAT IONS. 2 L 7 2 4F RT 2007073000125 20070730 00125 SO 2007 7 30 SIMA200720503 1 20070712 A 5320 14521700007 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 858AE 9542 5000 145754 LEFT OMEGA BEAM CORRODED AT FRAME 20. REPAIRED BEAM IAW EMB SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000126 20070730 00126 SO 2007 7 30 SIMA200720507 1 20070712 A 5340 14524131011 ATTACH ANGLE EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 858AE 9542 5000 145754 PASSENGER DOOR THRESHOLD ATTACH ANGLE CORRODED. REMOVED AND REPLACED ATTACH ANGLE IAW EMB SRM 51-40-02. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000138 20070730 00138 NM 2007 7 30 07FDEA02503 1 20070717 A 5712 65C3722112 RIB BOEING 727 727227 1384078 NM ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 COMPLY WITH EA 7-5710-110753, RT SIDE ONLY, WINGS- (AD 90-06-09 AND AD 94-07-08) MAIN FRAME, RIB UPPER CHORD REPAIR EO 7 -5710-7-2308 PART 2. COMPLIED WITH EA 7-5710-110753 RT SIDE IAW SB 727-57-0112. 2 L 7 3 4F A3WE 2007073000142 20070730 00142 NM 2007 7 30 AWXA200700873 1 20070713 A 5347 D57130147202 SEAT TRACK AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5971952, CORROSION ON CABIN SEAT TRACK, +Y1292, BS 1430/FR 36 TO BS 1650/FR 41. RE PLACED CABIN SEAT TRACK, +Y1292, BS 1430/FR 36 TO BS 1650/ FR 41 I/A/W A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007073000143 20070730 00143 NM 2007 7 30 AWXA200700874 1 20070713 A 5347 D53371110012 SEAT TRACK AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5971953, CORROSION ON CABIN SEAT TRACK, +Y1292, BS 1650/FR 41 TO BS 1976/FR 47. RE PLACED CABIN SEAT TRACK, +Y1292, BS 1650/FR 41 TO BS 1976/FR 47 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007073000147 20070730 00147 NM 2007 7 30 AWXA200700878 1 20070707 A 5321 D5361060500000 FLOOR PANEL AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5972035, CORROSION ON FLOOR PANEL 221FF, BS 709/FR 16 - BS 808/FR 20, +Y1292 TO +Y1 732. REPLACED FLOOR PANEL 221FF, BS 709/FR 16 - BS 808/FR 20, +Y1292 TO +Y1732 IAW AWA TASK CARD C1C53302. 2 L 7 2 4F RT A28NM 2007073000150 20070730 00150 NM 2007 7 30 AWXA200700881 1 20070711 A 5554 D5537131800000 HINGE FITTING AIRBUS A319 A319132 3930340 NM ZONE 300 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5964297, NR 1 RUDDER HINGE BEARING HAS EXCESSIVE PLAY, VERTICLE STABILZER STATION 780/RIB 2. REPLACED NR 1 RUDDER HINGE FITTING, VERTICLE STABILZER STATION 780/RIB 2 IAW A319 AMM 55-36-41. 2 L 7 2 4F RT A28NM 2007073000156 20070730 00156 NE 2007 7 30 DL757070913 2 20070713 A 7200 PW2037RTC ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 DAMAGED A DALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 640DL 22070 728772 23994 728772 IRR:ON SELECTION OF TAKEOFF POWER, AT 31 DERATE-LEFT ENGINE EMITTED LOUD BANG. POWER-EPR/N1-DETERIORATED AND TAKEOFF WA S ABORTED-LESS THAN 10 KTS. MOMENTARY PUFF OF SMOKE. OTHER AIRCRAFT REPORTED FLASH AND SPARKS FROM TAILPIPE. ENGINE E GT AND OIL PRESSURE WENT RED. PERFORMED ENGINE SEVERE DAMAGE CHECKLIST AND SHUT DOWN ENGINE. FOUND METAL IN TAILP IPE. ENGINE CHANGE IN PROGRESS. REMOVED AND REPLACED NR 1 ENGINE PER TRANSMITTAL 6T103 UP T PREFLIGHT 605239. PREFLIG HT COMPLETE CK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007073000158 20070730 00158 NM 2007 7 30 DLM90070929 1 20070628 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 655 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 SEAT TRACK STA. 655.760 LBL 24 FOUND CORRODED OUT OF LIMITS. REPAIRED PER SRM 53-40-01 REF AAR N/R 2700-0146. 2 L 7 2 4F RT A6WE 2007073000159 20070730 00159 NM 2007 7 30 DLM90070930 1 20070714 A 5320 ANGLE DOUG MD90 MD9030 3023690 NM RT MLG WW CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 RT MLG WHEEL WELL O/B AFT CORNER ANGLE CRACKED, REPAIRED PER SRM 53-60-02D REF AAR N/R 1000-0296. 2 L 7 2 4F RT A6WE 2007073000160 20070730 00160 NM 2007 7 30 DL76S070931 1 20070717 A 5312 148T2610217 BULKHEAD BOEING 767 767332 1382001 NM BS 1528 PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 130DL 24080 DURING HMV AT MOE, THE AFT PRESSURE BULKHEAD SUSTAINED TOOLING DAMAGE WHICH RESULTED IN A PUNCTURE IN THE WEB. 2 L 7 2 4F RT A1NM 2007073000161 20070730 00161 NM 2007 7 30 DL764070933 1 20070716 A 2150 111975 DETECTOR BOEING 767 767432ER 1385134 NM AIRFLOW MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 840MH 29717 AT 240 INTO FLT FWD EQ OVHT EICAS ILLUMINATED WENT TO STDBY PER QRH. AFTER 5 MIN THE OVHT LT RE-ILLUM. WENT TO OVRD PE R QRH. FWD EQ COOLING LT ILLUM ON OVRD ON SHORT FINAL INSP CONICAL SCREEN AT EQ COOLING SUPPLY FAN. NO DEFECTS NOTED. REMOVED TS104 FLOW DETECTOR. STRONG AIRFLOW IN AUTO AND STDBY. REPLACED TS104 FLOW DETECTOR. ALSO, REPLACED EQ COOLI NG IND CARD M867. CKS OK. 2 L 7 2 4F RT A1NM 2007073000163 20070730 00163 NM 2007 7 30 DL76S070936 1 20070605 A 5330 146T3330 SKIN BOEING 767 767332 1382001 NM BS 1562 S26L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 130DL 24080 DURING HMV3 AT MOBILE AEROSPACE ENGINEERING, FOUND LWR FUSELAGE HAS DENT WITH OVER BURNISHED FASTENERS AT S26L STA 1562. REMOVED DAMAGE AND REPAIRED PER SRM 53-00-01 LAP SPLICE REPAIR. 2 L 7 2 4F RT A1NM 2007073000166 20070730 00166 NM 2007 7 30 NWAA072626729 1 20070719 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 900 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 629US 22388 DURING "L" CHECK, FOUND CRACK IN FRAME AND FORWARD CHANNEL FASTENER HOLE IN TENSION TIE AREA AT BS 900 LT. REPAIRED PER EA 67-209733. 2 L 7 4 4F A20WE 2007073000169 20070730 00169 NM 2007 7 30 NWAA072596729 1 20070720 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 840 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 629US 22388 DURING "L" CHECK, FOUND CRACKS IN FRAME FASTENER HOLES AND SHORT EDGE MARGIN IN TENSION TIE AREA AT BS 840. REPAIRED PE R EA 67-209728. 2 L 7 4 4F A20WE 2007073000170 20070730 00170 NM 2007 7 30 NWAA072606729 1 20070719 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 800 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 629US 22388 DURING "L" CHECK, FOUND CRACKS IN FRAME AT TENSION TIE AREA AND LT AFT AND LT FORWARD CHANNEL AT BS 800. REPAIRED PER E A 67-209731. 2 L 7 4 4F A20WE 2007073000171 20070730 00171 NM 2007 7 30 DHL2007741513 1 20070720 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 720A DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 FWD PIT, BS 720A, DENT IN RADIUS OF FRAME BETWEEN STR 24L AND 25L. CUT OUT DMG, 1" BY 1", FABRICATED REPAIR ANGLE FROM 7075-T0, .071" BY 10" BY 4" BY 1", PO NR 9004690, PER B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1. HEAT TREATED REPAIR ANG LE TO 7075-T6 PER FASI. ER NR 2-37153-801 REV A. TREATED, PRIMED, AND INSTALLED REPAIR ANGLE PER B727 SRM 51-10-2, AND 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2007073000173 20070730 00173 NM 2007 7 30 QXEA200701164 1 20070717 A 5270 PROXIMITY SENSOR BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR OUT OF ADJUST A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 409QX 4051 SJC - ON FLIGHT 2404 ABORTED TAKEOFF, ON TAKEOFF ROLL, PUSHER SYSTEM FAIL ILLUMINATED BETWEEN 90-100 KTS. FUSELAGE DOOR WARNING ILLUMINATED, RESET AT 40 KTS, THEN REILLUMINATED IMMEDIATELY THEREAFTER PUSHER SYSTEM FAIL CAUTION CLEARED AFTE R CLEARING RUNWAY, FUSELAGE DOOR WARNING CONTINUED TO CYCLE. MAINTENANCE ADJUSTED AFT PASSENGER DOOR PROX SENSORS. OPE RATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007073000174 20070730 00174 NM 2007 7 30 QXEA200701155 1 20070716 A 2822 956A15B662362 PUMP BOMBDR DHC8 DHC8402 1390042 NM FUEL INOPERATIVE A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 421QX 4149 SEA - ON FLIGHT 2288 RETURNED TO GATE, NR 2 TANK AUXILIARY PUMP SWITCH LIGHT INOPERABLE. REMOVED AND REPLACED NR 2 AUXI LIARY PUMP SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007073000176 20070730 00176 NM 2007 7 30 DHL2007741502 1 20070705 A 5310 STRUCTURE BOEING 727 7272Q9 138448M NM BS 730D GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 BS 720D PLUS 10 STR 19L PREVIOUS REPAIR GOUGED. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-02, FABRICATED NEW DOUBLER F ROM 2024-T3 0.090" PO NR 9004940 (DIM. 12" BY 8") IAW B727 SRM 53-30-2 FIG 2 AND 53-30-3 FIG 14. TREATED AND PRIMED PAR T AND AREA IAW B727 SRM 51-10-2. INSTALLED NEW REPAIR DOUBLER IAW B727 SRM 53-30-3 FIG 14 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007073000178 20070730 00178 NM 2007 7 30 DHL2007741504 1 20070629 A 5753 SKIN BOEING 727 7272Q9 138448M NM TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 L/WING O/B AFT FLAP DELAM ON UPPER/LOWER SURFACE WBL 442. REMOVED DELAMINATED AREAS APPROX (LOWER SKIN) 17" BY 9", (UPP ER SKIN) 20" BY 9" AND COVE 17" BY 9", CLEANED AND PREPPED DAMAGED AREA TO BE REPAIRED, FABRICATED SKINS LOWER 17" BY 9" AND TWO DOUBLERS 3" BY 9" FROM .016" 2024-T3 PO NR 9004174, UPPER SKIN 20" BY 9" AND TWO DOUBLERS (3" BY 9") FROM .016" 7075-T6 PO NR 9003988 AND REPAIR COVE PLUG (17" BY 9") FROM PED 3.1 3/16 5052N4 PO NR 6261123; ANODIZED, PRIMED AND APP LIED ADHESIVE IAW B727 SRM 51-40-20 PAR 7, 8, FIG 3 AND 51-40-24 FIG 3 AND 57-50-2 FIG 4; INSTALLED REPAIRED PARTS, CURE D AND FINISHED REPAIR AREAS IAW B727 SRM 51-40-20 AND 51-40-24. 2 L 7 3 4F RT A3WE 2007073000180 20070730 00180 2007 7 30 DL757070939 4 20070718 A 3160 4038170905 DISPLAY BOEING 757 757232 1384965 NM COCKPIT UNSERVICEABLE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 655DL 24395 AT 13000 FT GOT ODOR OF ELEC SMOKE THEN SAW SMOKE BILLOWING UP FROM COPILOTS LT LEG. RETURNED TO LAS. FOUND EVIDENCE O F F/O'S FMS MCDU BURNT. ASSOCIATED FMC MSG MCDU BLANK. INSPECTED AREA AND ASSOCIATED HARNESSES FROM FWD E AND E COMPT AND PEDESTAL. REPLACED F/O MCDU. ALL CHECKS NORMAL. 2 L 7 2 4F RT A2NM 2007073000181 20070730 00181 NM 2007 7 30 DLM90070940 1 20070715 A 3240 STATOR DOUG MD90 MD9030 3023690 NM NR 2 BRAKE BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 NR 2 BRAKE IS LEAKING AT FWD BOTTOM PLUG. FOUND BRAKE ROTORS AND STATOR BROKEN. REMOVED AND REPLACED NR 2 BRAKE IAW MD -90 M/M 32-47-01. 2 L 7 2 4F RT A6WE 2007073000182 20070730 00182 NM 2007 7 30 DL757070941 1 20070719 A 5330 413N33203 SKIN BOEING 757 757232 1384965 NM FS 635 S17L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 639DL 23993 DURING HMV, INSPECTION NOTED 2 DENTS AND AN EXISTING EXTERNAL DOUBLER ON THE FUSELAGE SKIN, LEFT SIDE. THE TWO DENTS WE RE CUTOUT, AND THE EXISTING REPAIR WAS REMOVED. THE EXISTING REPAIR WAS ALSO CUT OUT, REMOVING ALL EXISTING HOLES, AND THREE BOEING APPROVED REPAIRS WERE INSTALLED PER 461667-14 2 L 7 2 4F RT A2NM 2007073000184 20070730 00184 2007 7 30 DL764070943 4 20070718 A 2565 SLIDE BOEING 767 767432ER 1385134 NM EMERGENCY EXIT FRAYED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 832MH 29704 LT EMERGENCY EXIT DOOR SLIDE CENTER PACK TRAY CENTER LACING FRAYED AND DRY ROTTING, FOUND DURING HMV-1. SLIDE REPLACED ON TIMCO OPERATION 20950. 2 L 7 2 4F RT A1NM 2007073000186 20070730 00186 NM 2007 7 30 DL764070945 1 20070718 A 5330 SKIN BOEING 767 767432ER 1385134 NM BS 1560 S13R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 832MH 29704 FUSELAGE SKIN HAS CRACK STA 1560 S13R, FOUND DURING HMV AT TIMCO. REPAIRED PER B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007073000188 20070730 00188 NM 2007 7 30 AWXA200700899 1 20070723 A 5740 D57259162000 FITTING AIRBUS A319 A319132 3930340 NM ZONE 500 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 SAL - MAJOR REPAIR- BC-6 CHECK - NR 5964268, 5964269, 5964270 AND 5964344, CORROSION FOUND ON HOLE 52, 53, AND 54 OF LT MAIN LANDING GEAR ANCHORAGE FITTING ON LT WING INNER REAR SPAR BETWEEN RIB 2 TO RIB 5. CORROSION REMOVED FROM HOLE 52, 53, AND 54 OF LT MAIN LANDING GEAR ANCHORAGE FITTING ON LT WING INNER REAR SPAR BETWEEN RIB 2 TO RIB 5 IAW US AIRWAYS E A NR 120115 AND MONITORED BY NR 5946344. 2 L 7 2 4F RT A28NM 2007073000189 20070730 00189 NM 2007 7 30 AWXA200700900 1 20070723 A 5711 D57252520006 SPAR AIRBUS A319 A319132 3930340 NM ZONE 500 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5964268, 5964269, 5964270, AND 5964344, CORROSION FOUND ON LT WING REAR INNER SPAR, RIB 2 - RIB 5, AREA ON HOLE 52, 53 AND 54 OF MAIN LANDING GEAR ANCHORAGE FITTING. CORROSION REMOVED ON LT WING REAR IN NER SPAR, RIB 2 - RIB 5 IAW US AIRWAYS EA NR 120115 AND MONITORED BY NR 5946344. 2 L 7 2 4F RT A28NM 2007073000190 20070730 00190 NM 2007 7 30 AWXA200700902 1 20070712 A 5522 D55281232000 SKIN AIRBUS A319 A319132 3930340 NM ZONE 300 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 SAL - MAJOR REPAIR - BC - 6 CHECK, NR 5963167, CRACK ON LT ELEVATOR EXTERNAL UPPER SKIN LOCATED BETWEEN HORIZONTAL STAB LIZER RIB 4 TO RIB 5, AT 14" FROM UPPER EDGE AND 23" FROM INBOARD EDGE. CRACK WAS REPAIRED AT AT LT ELEVATOR EXTERNAL UPPER SKIN LOCATED BETWEEN HORIZONTAL STABLIZER RIB 4 TO RIB 5, AT 14" FROM UPPER EDGE AND 23" FROM INBOARD EDGE PER A3 19 SRM 51-77-13, FIG 14. 2 L 7 2 4F RT A28NM 2007073000191 20070730 00191 NM 2007 7 30 AWXA200700884 1 20070711 A 5554 D5537131800200 HINGE FITTING AIRBUS A319 A319132 3930340 NM ZONE 300 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5964249, NR 4 RUDDER HINGE BEARING HAS EXCESSIVE PLAY, VERTICLE STABILZER STATION 2632/RIB 6. REPLACED NR 4 RUDDER HINGE FITTING, VERTICLE STABILZER STATION 2632/RIB 6 IAW A319 AMM 55-36-41. 2 L 7 2 4F RT A28NM 2007073000192 20070730 00192 NM 2007 7 30 AWXA200700885 1 20070711 A 5554 D5537131800000 HINGE FITTING AIRBUS A319 A319132 3930340 NM ZONE 300 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5964298, NR 5 RUDDER HINGE BEARING HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 2985/RIB 7. REPLACED NR 5 RUDDER HINGE FITTING, VERTICAL STABILIZER STATION 2985/RIB 7 IAW A319 AM 55-36-41. 2 L 7 2 4F RT A28NM 2007073000193 20070730 00193 EU 2007 7 30 AWXA200700886 1 20070714 A 5554 D5537131800400 HINGE FITTING AIRBUS 320 A320232 3930326 EU ZONE 300 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 654AW 1050 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5898135, NR 7 RUDDER HINGE FITTING WORN, VERTICLE STABILZER STATION 5605/RIB 11. R EPLACED NR 7 RUDDER HINGE FITTING, VERTICLE STABILZER STATION 5605/RIB 11 IAW A320 AMM 55-36-41. 2 L 7 2 4F RT A28NM 2007073000195 20070730 00195 EU 2007 7 30 AWXA200700888 1 20070714 A 5554 D5537131800000 HINGE FITTING AIRBUS 320 A320232 3930326 EU ZONE 300 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 654AW 1050 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5898131, NR 2 RUDDER HINGE FITTING WORN, VERTICAL STABILIZER STATION 1926/RIB 4. R EPLACED NR 2 RUDDER HINGE FITTING, VERTICAL STABILIZER STATION 1926/RIB 4 IAW A20 AMM 55-36-41. 2 L 7 2 4F RT A28NM 2007073000199 20070730 00199 NM 2007 7 30 AWXA200700892 1 20070705 A 5320 65479761 CUSP WEB BOEING 737 7373G7 1384595 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5962157, CORROSION ON CUSP WEB, BS 787 - BS 807, S17L. REPLACED CUSP WEB, BS 787 - BS 807, S17L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007073000200 20070730 00200 NM 2007 7 30 AWXA200700893 1 20070705 A 5320 654797611 CUSP WEB BOEING 737 7373G7 1384595 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5962154, CORROSION ON CUSP WEB, BS 867 - BS 887, S17L. REPLACED CUSP WEB, BS 767 - BS 887, S17L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007073000202 20070730 00202 NM 2007 7 30 QXEA200701207 1 20070721 A 2420 1150924 GCU BOMBDR DHC8 DHC8402 1390042 NM NR 2 AC GEN MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 430QX 166 166 4163 SEA FLIGHT NR 2348: NR 2 AC GEN WOULD NOT COME ON LINE AFTER START. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE PERFORMED RETRIEVAL OF DATA FROM EPCU. FOUND CODE 28 2AC GCU. REMOVED AND INSTALLED SERVICEABLE NR 2 AC GEN GCU IAW Q400 AMM 24- 21-06-000-801 AND 24-21-06-400-801. PERFORMED OPS TEST IAW Q400 AMM 24-21-00-710-801. OPS TEST GOOD. NR 2 AC GEN COME S ON LINE AS REQUIRED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007073000203 20070730 00203 NM 2007 7 30 QXEA200701210 1 20070721 A 2420 1150924 GCU BOMBDR DHC8 DHC8402 1390042 NM NR 1 AC GEN MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 408QX 15534 15534 4050 SEA FLIGHT: NR 1 AC GEN CAUTION ILLUMINATED. RAN ABNORMAL CHECKLIST. LIGHT REMAINED ILLUMINATED. MAINTENANCE REMOVED AND REPLACED NR 1 AC GCU IAW AMM 24-21-06 PAGES 401-405. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007073000205 20070730 00205 2007 7 30 DXTA200702352 4 20070720 A 3410 701700098803 SYMBOL GENERATOR CESSNA 560 560XL 2076702 CE FWD AVIONCS BAY INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 603QS 5875 5605203 RED (PIC) "X" ON PFD/MFD [SYMBOL GENERATOR FAILURE SINGLE]. POST FLIGHT INSPECTION PERFORMED REVEALED NO CIRCUIT BREAKER S POPPED. REMOVED AND INSTALLED I.A.C- -615 IAW CESSNA M.M, 34-25-01. OPS CHECKS GOOD I/A/W CE560 M.M. 34-25-02. 2 L 7 2 4F RT A22CE 2007073000211 20070730 00211 2007 7 30 DXTA200702345 4 20070718 A 2210 4006719910 SERVO RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP ELEVATORS INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 862QS 599 258362 BOTH AUTOPILOTS FAILED IN FLIGHT AND WOULD NOT RE-ENGAGE. REMOVED AND REPLACED ELEVATOR SERVO, PERFORMED FUNCTIONAL TES T OF FLIGHT GUIDANCE / AUTO PILOT SYSTEMS WITH NO DISCREPANCIES NOTED. WORK PERFORMED IAW HAWKER SPZ-8000 M.M. 22-14-00 2 L 7 2 4F 4 F RT A3EU E6WE 2007073100006 20070731 00006 NM 2007 7 31 CALA0700367 1 20070719 A 5315 BAC1505100247 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED THE ENTIRE LENGTH, AT STA 328, LBL 45 TO RBL 45. THE FLOORBEAM WAS REPA IRED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2007073100008 20070731 00008 NM 2007 7 31 PIDA07036 1 20070716 A 3350 BATTERY PACK BOEING 737 7372K5 138448X NM CABIN DISCHARGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 249TR 22598 OVERHEAD AISLE EMERGENCY EXIT LIGHT AT ROW 2 INOP. RELEASED FOR FLIGHT PER MEL 33-15-3 CONTROL NUMBER 0716003. CHARGED EMERGENCY BATTERY PACK. CLEARED MEL. 2 L 7 2 4F RT A16WE 2007073100009 20070731 00009 2007 7 31 UPS07M50209 4 20070721 A 3197 WIRE DOUG MD11 MD11F 3023600 NM NR 3 MCDU BROKEN A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 286UP 48453 DUE TO MCDU NR 2 FAILURE DEFERRED PER MEL 31-65-1. DEF 354944 & 355043. ON T/S FOUND WIRE BROKEN AT PIN 41 OF P1-1026A . REPAIRED IAW SWP AND WEDM 34-63-22. R&R NR 3 MCDU IAW AMM 31-65-01-4. OPS TEST IAW AMM 31-65-01-5 NOW NORMAL. DMI CLOS ED, PLACARD REMOVED. 2 L 7 3 4F RT A22WE 2007073100011 20070731 00011 NM 2007 7 31 2007UALA02659 1 20070713 A 3350 8100133801 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SEAT 1E MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 206UA 30212 EXIT PATH LIGHT COVER 1E NOT ATTACHED. EEL STRIP MISSING. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007073100013 20070731 00013 NM 2007 7 31 2007UALA02661 1 20070714 A 3350 AML76C10T01P003 SPRING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LIGHT SWITCH BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 121UA 29167 SPRING ON EMERGENCY EXIT LIGHT SWITCH BROKEN ON OVERHEAD PANEL. INSTALLED NEW SPRING ON SWITCH GUARD. OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100014 20070731 00014 NM 2007 7 31 2007UALA02663 1 20070714 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY SILL LIGHT AFT ON DOOR 1L INOPERATIVE. RELAMPED SILL LIGHT. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100016 20070731 00016 NM 2007 7 31 2007UALA02664 1 20070714 A 3397 794640 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY LIGHTS FWD GALLEY BOTTOM OF LT WALL & FWD OF LAV 100 LT BOTTOM OF WALL AFT DOOR 1 ARE INOPERATIVE. RESECURED EMERGENCY LIGHT CONNECTOR. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100017 20070731 00017 NM 2007 7 31 2007UALA02228 1 20070625 A 3350 BACS16X3A SOCKET BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN ARCED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 177UA 24384 UPPER DECK COVE LIGHT ASSY AT ROW 17AB ARCING AND HAS ELECTRICAL ODOR. *S/D* REPLACED SOCKET ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100018 20070731 00018 NM 2007 7 31 2007UALA02666 1 20070714 A 3350 9F19948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 1A DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 SEAT 1A EMERGENCY LIGHT STRIP DAMAGED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100019 20070731 00019 NM 2007 7 31 2007UALA02667 1 20070715 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 EEL INOP: SEATS 2A & 4E AFT SECTIONS. ALSO SEAT 22 RT & ROW 34 LT. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100021 20070731 00021 NM 2007 7 31 2007UALA02245 1 20070624 A 2421 745329C IDG BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE LT ENGINE FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 673UA 29241 LEFT GEN DRIVE LIGHT NOT ILLUMINATED W-ENGINE SHUTDOWN. REPLACED IDG PER MM 24-11-01. ELECT GEN AND POWER CHECKS GOOD DURING RUN. NO LEAKS NOTED. OUTBOUND CREW CONDUCTED VERIFICATION FLIGHT AND IDG RAN FLAWLESSLY. OK FOR CONTINUED ETOP S. 2 L 7 2 4F 4 F RT A1NM E24NE 2007073100022 20070731 00022 NM 2007 7 31 2007UALA02668 1 20070715 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE WALL: AISLE ACRO DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 WALL EEL INOP: AISLE ACROSS LAV 100. REPAIRED FEEDER WIRE 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100023 20070731 00023 NM 2007 7 31 2007UALA02669 1 20070715 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 EMERGENCY LIGHT INOP: DOOR 3R SLIDE ILLUM. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100024 20070731 00024 NM 2007 7 31 2007UALA02670 1 20070715 A 3397 794640 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 WALL EEL INOP: CROSS AISLE DOOR 5R. FOUND LOOSE CONNECTION, SECURED, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100025 20070731 00025 NM 2007 7 31 2007UALA02671 1 20070715 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 EMERGENCY LIGHT INOP: CEILING ROW 24 RT. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100026 20070731 00026 NM 2007 7 31 2007UALA02672 1 20070716 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY LIGHTS ROWS 3A & 39ABC ARE INOPERATIVE. RELAMPED EMERGENCY LIGHTS. OP CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100027 20070731 00027 NM 2007 7 31 2007UALA02251 1 20070625 A 5523 65C257458 TAB BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RT ELEVATOR FAILED A UALA O OTHER F FLT CONT AFFECTED IN INSP/MAINT 1 WP 29 376UA 24641 LT AND RT ELEVATOR TABS ARE NOT WITHIN .010 OF EACH OTHER. *S/D* RIGHT HAND TAB HARDWARE FAILED CHECK. REPLACED RIGHT HAND ELEVATOR TAB. 2 L 7 2 4F 4 F RT A16WE E21EU 2007073100028 20070731 00028 NM 2007 7 31 2007UALA02673 1 20070716 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY SILL LIGHT DOOR 1R FWD INOPERATIVE. RELAMPED. OP CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100029 20070731 00029 NM 2007 7 31 2007UALA02674 1 20070716 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY CEILING LIGHT ABOVE ROW 48ABC INOPERATIVE. RELAMPED EMERGENCY LIGHT. OP CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100030 20070731 00030 NM 2007 7 31 2007UALA02257 1 20070626 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 UPPER EXTERNAL FUSE SKIN HAS CHAFING WEAR AT DORSAL FIN LANDING FROM BS 860 - 907 BL 0 - LBL 8. MAJOR REPAIR: BLENDED CROWN SKIN WEAR. APPLIED .020 WEAR STRIPS PER SRM 53-60-01 REPAIR 10 PARAGRAPH 5. 2 L 7 2 4F 4 F RT A16WE E21EU 2007073100031 20070731 00031 NM 2007 7 31 2007UALA02681 1 20070716 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 674UA 29242 MID GALLEY EEL FLOOR STRIP IS INOPERATIVE. REPLACED EEL STRIP CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007073100032 20070731 00032 NM 2007 7 31 2007UALA02686 1 20070717 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE 4L DOOR SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 EMERGENCY LIGHT INOP: DOOR 4L SLIDE ILLUM. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100033 20070731 00033 2007 7 31 2007UALA02259 4 20070626 A 2565 680150904 O-RING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EVAC SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 180UA G433 25224 SLIDE PRESSURE AT DOOR 5 LEFT LOW. THERE WAS A SMALL LEAK AROUND O-RING ON THE GAUGE ELBOW ASSEMBLY GOING INTO VALVE. REPLACED O-RING, WATER TESTED FOR 15 MINUTES, NO LEAK FOUND. REPLACED BOTTLE WITH STOCK BOTTLE. REPLACED SLIDE RAFT AS SEMBLY. SLIDE PROBLEM ROOT CAUSE: O'RING HARDENED & LOST ELASTICITY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100034 20070731 00034 NM 2007 7 31 2007UALA02698 1 20070718 A 3397 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 774UA 26936 AFT EMERGENCY EXIT LIGHT ON SEAT 2E INOP. SECURED CONNECTOR. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007073100035 20070731 00035 NM 2007 7 31 2007UALA02265 1 20070626 A 5270 284T04841 SENSOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY EXIT OUT OF ADJUST A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 642UA 25092 EMERGENCY DOORS LIGHT ILLUM WITH EICAS MSG POS 11 (05=L EMER DR , 06=R EMER DR, 11=L WING SLIDE, 12=R WING SLIDE). *S/D * FOUND SENSOR FOR DOOR CLOSED, S218 OUT OF ADJUSTMENT. SHIMMED AND ADJUSTED SENSOR PER MM 52-71-00. REACTIVATED DOOR PER MM 25-65-00. OP CHECKED OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007073100036 20070731 00036 NM 2007 7 31 2007UALA02699 1 20070718 A 3350 8100133801 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 33G INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 774UA 26936 EEL LIGHT AT SEAT 33G IS INOPERATIVE. REPLACED LIGHT ASSY. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007073100037 20070731 00037 NM 2007 7 31 2007UALA02266 1 20070626 A 3297 M102D2372A WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE MLG CROSSED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 658UA 27113 SPINNING NR 8 ANTISKID TRANSDUCER CAUSES THE NR 3 WHEEL BRAKE TO RELEASE, SHOULD RELEASE NR 4. STOPPING THE NR 8 TRANSD UCER CAUSES NR 7 BRAKE TO RELEASE, SHOULD RELEASE NR 8. FOUND WIRES TO TRANSDUCER CROSSED BETWEEN TRANSDUCER NR 7 AND N R 8. REINSTALLED WIRES REF WDM 32-42-11. TRANSDUCER SPIN TEST REF MM 32-42-00. NO FAULTS ON EICAS. TEST PASSED. AIR CRAFT OK FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007073100039 20070731 00039 NM 2007 7 31 2007UALA02709 1 20070717 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 119UA 28812 SEAT 2A, AFT EEL LIGHT MISSING. REPLACED EEL LAMP, OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100040 20070731 00040 NM 2007 7 31 2007UALA02711 1 20070718 A 3350 582240 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY LIGHT INOP AT DOOR 5L FWD & AFT SILL. REPLACED POWER SUPPLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100041 20070731 00041 NM 2007 7 31 2007UALA02269 1 20070627 A 2910 MS21907W10 ELBOW BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE HYDRAULIC SYS CRACKED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 792UA 26934 FLIGHT DIVERTED DUE TO A HYDRAULIC INDICATION PROBLEM. HYD LEAK ON NR 1 PYLON. FOUND CRACKED ELBOW MS21907W10, NON STO CK PART AVAILABLE AT BOEING. REPLACED ELBOW. SERVICED HYD SYSTEM. LEAK CHECK OK WITH ENG MOTORING, NO LEAKS NOTED. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007073100042 20070731 00042 NM 2007 7 31 2007UALA02712 1 20070718 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EEL AT 5E AFT & 52ABC ARE INOPERATIVE. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100043 20070731 00043 NM 2007 7 31 2007UALA02713 1 20070718 A 3350 FU305 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE POWER SUPPLY BLOWN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY LIGHTS INOP RIGHT OVERWING BODY FAIRING TWO AFT ASSEMBLIES. REPLACED FUSE IN POWER SUPPLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100046 20070731 00046 NM 2007 7 31 2007UALA02658 1 20070714 A 2697 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FIRE LOOP LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 777UA 26916 FIRE LOOP 2 APU. [08-07-07] FOUND CONNECTOR AT LUG LOOSE. SECURED LUG AFTER MEGGER OF ELEMENT. M26009. FIRE DET. TES T CHECKS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007073100048 20070731 00048 NM 2007 7 31 2007UALA02660 1 20070715 A 3320 BALLAST BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN LIGHTS OVERHEATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 783UA 26950 LAV 100 MIRROR LIGHT ASSY SHOWED SIGNS OF OVERHEATING. [08-07-07] REPLACED LIGHT ASSY AND BALLAST. OP CK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007073100049 20070731 00049 NM 2007 7 31 2007UALA02662 1 20070714 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY LIGHT ROW 3A AFT INOP. REPLACED EMERGENCY LIGHT. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100051 20070731 00051 NM 2007 7 31 2007UALA02665 1 20070714 A 3350 1317 A/C PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY CEILING LIGHT ABOVE ROW 44 LT INOP. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100053 20070731 00053 2007 7 31 2007UALA02675 4 20070716 A 2565 RESERVOIR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY EXIT UNKNOWN A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 417UA 483 CIDS CAUTION LIGHT ON AT THE F-AS PANEL. REPLACED LT OVERWING RESERVOIR AS PRECAUTION. NO CIDS CAUTION LIGHT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007073100055 20070731 00055 EU 2007 7 31 2007UALA02676 1 20070716 A 3520 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 425UA 508 TWENTY SIX EA O2 COMPT DOORS DID NOT DEPLOY DURING TEST: FWD FLIGHT ATTENDANT, AFT FLIGHT ATTENDANT, LT SEAT ROWS (6, 9 , 11, 13, 15) AND RT SEAT ROWS (1, 2, 3, 6, 9, 11, 13, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26). RESET BREAKERS AND RETESTED. ALL RELEASED PROPERLY 2ND TIME. 2 L 7 2 4F 4 F RT A28NM E40NE 2007073100056 20070731 00056 EU 2007 7 31 2007UALA02677 1 20070717 A 3510 HOSE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE O2 MASK BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 451UA 865 CAPTAIN`S O2 MASK WEB WILL NOT INFLATE INNER HOSE BROKEN. INNER HOSE BROKEN ON CAPTAINS O2 MASK. REPLACED MASK ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072400197 20070724 00197 NM 2007 7 24 2007UALA02631 1 20070714 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GALLEY ODOR A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 558UA 26654 ACFT RETURN TO BLOCK DUE TO BURNING ODOR FROM AFT GALLEY AREA. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072500021 20070725 00021 NM 2007 7 25 SWAA073534 1 20070718 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM BS 784 S20L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 784, STR 20L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007072500028 20070725 00028 NM 2007 7 25 USAA070556 1 20070718 A 5730 SKIN BOEING 737 737401 1384701 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 LEADING EDGE JUST O/B OF LEFT PYLON WING STA 157 HAS CRACK. STOP DRILLED CRACK, INSTALLED DOUBLER PER TR 57-41-02, DEFE CT SIZE: 0.5 INCH. 2 L 7 2 4F RT A16WE 2007072500042 20070725 00042 NM 2007 7 25 USAA070571 1 20070719 A 5730 ACCESS PANEL BOEING 737 737401 1384701 NM RT WING CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 RIGHT OUTER WING AT FUEL SHUTOFF VALVE ACCESS PANEL HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER IPC 28-22-11; CORR TASK C57-300-01, DEFECT SIZE: .1875 INCH. 2 L 7 2 4F RT A16WE 2007072500048 20070725 00048 NM 2007 7 25 SWAA073553 1 20070718 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM BS 440 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007072500063 20070725 00063 NM 2007 7 25 KCSA071244 1 20070719 A 5313 STRINGER BOEING 747 7472B4B 138481B NM BS 585 S47R CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA 585 STRINGER 47R CORROSION FWD OF SPLICE. 2 L 7 4 4F RT A20WE 2007072500064 20070725 00064 NM 2007 7 25 SWAA073543 1 20070718 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 706 S2L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007072500067 20070725 00067 NM 2007 7 25 SWAA073548 1 20070718 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 344 S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007072500074 20070725 00074 NM 2007 7 25 BB07055 1 20070722 A 3350 3016692 SOCKET BOEING 757 7572B7 1384964 NM EMERGENCY LIGHTS INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 937UW 27245 MAINTENANCE FOUND THE FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LIGHT SOCKET. NO FURTHER DIFFICULTIES. 2 L 7 2 4F RT A2NM 2007072500078 20070725 00078 NM 2007 7 25 SWAA073561 1 20070719 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007072500084 20070725 00084 NM 2007 7 25 SWAA073566 1 20070719 A 5315 6545834 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CRACKED AT BS 312. BL 0. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007072500092 20070725 00092 NM 2007 7 25 MASA200700307 1 20070607 A 3397 WIRE DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHT BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 434YV 434 ASH FLT 7064 GJT - EMERGENCY LIGHTS WILL NOT TEST FROM FLIGHT ATTENDANT STATION. MX REPAIRED BROKEN WIRE. 2 H 7 2 4T RT A13NM 2007072500096 20070725 00096 EU 2007 7 25 2007UALA02637 1 20070713 A 2400 ELECTRONIC UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN ODOR A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 467UA 1359 BURNING ODOR IN FWD GALLEY FOR SHORT TIME THEN NOTICED AUDIO INOPERATIVE W-CB-PBS MUSIC LT POPPED. REPLACED SEU UNDER SEAT 2ABC, MULTIPLEX BOX AT 3ABC AND CB 23MK. AS PRECAUTIONARY. ODOR WAS INTERMITTMENT AND POSSIBLY UNRELATED TO THE MTX PREFORMED. ODOR HAS NOT RETURNED SINCE 7/13/07. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072500097 20070725 00097 EA 2007 7 25 TRAX200701005 1 20070716 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 718EV 10095 ASD EXIT PLACARD WORN. 2 L 7 2 4F RT A21EA 2007072500100 20070725 00100 EA 2007 7 25 TRAX200701008 1 20070716 A 5260 ATTACH BRACKET CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 718EV 10095 ASD INTERCOSTAL ATTACH BRACKET AT LOWER FWD CORNER HAS POSSIBLE CRACK. 2 L 7 2 4F RT A21EA 2007072500121 20070725 00121 NM 2007 7 25 2007UALA02656 1 20070714 A 4990 OIL COOLER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE APU FAILED A UALA O OTHER M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 677UA 30029 APU FAILED DURING TAXI OUT WITH FAIL LIGHT ILLUMINATED. [08-17-07] REPLACED OIL COOLER RAN APU WITH FULL LOAD 35 MIN, AND NO AUTO SHUTDOWN. OPS CHECK NORMAL AT THIS TIME 2 L 7 2 4F 4 F RT A1NM E24NE 2007072500122 20070725 00122 NM 2007 7 25 BB07054 1 20070719 A 3350 LIGHT BOEING 757 7572B7 1384964 NM R4 DOOR BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 933UW 27199 MAINTENANCE FOUND THE R4 DOOR EMERGENCY LIGHT BROKEN. REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F RT A2NM 2007072500123 20070725 00123 SO 2007 7 25 C2XA07RI059 1 20070711 A 3350 78241 INVERTER EMB 135 EMB135ER 3260203 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15509 145192 DURING A ROUTINE MX INSPECTION, NR 1 EMERGENCY SIDE MARKER LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D NR 4 INVERTER WITH OPERATIONAL CHECK GOOD. A/C APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007072500137 20070725 00137 NM 2007 7 25 QXEA200701147 1 20070712 A 7312 7269094 VALVE BOMBDR DHC8 DHC8402 1390042 NM FUEL HEATER MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 416QX 4083 SEA - ON FLIGHT 2286, DURING CRUISE FUEL INLET TEMP NR 2 WENT TO +75, RAN CHECKLIST AND TEMP CAME DOWN TO +71. ON GROUN D TEMP CLIMBED TO +75 DURING TAI WITH FUEL PUMP ON. MAINTENANCE REMOVED AND REPLACED FUEL HEATER THERMAL ACTUATOR VALVE . RAN AIRCRAFT AND PERFORMED LEAK CHECK. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007072500140 20070725 00140 NM 2007 7 25 QXEA200701163 1 20070717 A 7700 WARNING MESSAGE BOMBDR DHC8 DHC8402 1390042 NM ENGINE FALSE ACTIVATION A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 402QX 4032 SEA - ON FLIGHT 2294, RETURNED TO GATE, POWER PLANT MESSAGE ON ED. MAINTENANCE FOUND FAULT CODE 796 A/B ON THE NR 1 ENG INE. REMOVED AND RE-INSTALLED SAME FADEC ON THE NR 1 ENGINE TO PERFORM INSPECTION ON THE PINS AND APPLY PIN ENHANCEMENT . ALSO, INSPECTED ALL CONNECTION ON FADEC HARNESS. NO DEFECTS FOUND. NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007072500144 20070725 00144 NM 2007 7 25 UIEA200700272 1 20070718 A 7830 COWLING BOEING 747 74747UF 1384812 NM THRUST REVERSER CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 492 29253 NR 2 LT T/R COWL DELAMINATED ON OUTSIDE WIRE MESH AND INSIDE SKIN WITH 2 ASSOCIATED CRACKS. 2 L 7 4 4F RT A20WE 2007072500145 20070725 00145 NM 2007 7 25 07FDEA02506 1 20070717 A 5330 SKIN DOUG MD11 MD11F 3023600 NM BS 1851 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 WITH REFERENCE TO WORK CARD NR T1-5310-96612 PT2, DENT FOUND IN FUSELAGE AT STA 1851 BETWEEN LONGERON 35R AND LONGERON 3 6R. [08-06-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-114762, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007072500160 20070725 00160 NM 2007 7 25 UIEA200700269 1 20070718 A 7830 BULLNOSE BOEING 747 74747UF 1384812 NM THRUST REVERSER DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 492 29253 IMPACT DAMAGE NR 3 ENG LT T/R UPPER FILLET BULLNOSE LEADING EDGE FAIRING. 2 L 7 4 4F RT A20WE 2007072500176 20070725 00176 NM 2007 7 25 QXEA200701125 1 20070705 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 461-467 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 530 C4 PDX - SUSPECTED CORROSION BETWEEN RIGHT STRINGER 32 AND 33 AND STATION X461.0 AND X467.0. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-40-11. 2 H 7 2 4T RT A13NM 2007072500188 20070725 00188 SO 2007 7 25 SIMA200720006 1 20070517 A 5340 14529834405 ATTACH FITTING EMB 145 EMB145LR 3260212 SO CARGO AREA DRILLED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 942LL 4931 14500930 MISDRILLED FASTENERS ON FORWARD CARGO NET FITTING BETWEEN FRAME 63, FRAME 64, STRINGER 11L AND STRINGER 12L. REAMED HOL ES AND INSTALLED OVERSIZE FASTENERS IAW EMB, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007072500194 20070725 00194 EU 2007 7 25 07FDEA02521 1 20070719 A 5347 A5327901220000 SEAT TRACK AIRBUS 310 A310203 3930313 EU BS 3888-3938 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 RIGHT AFT MAIN DECK CARGO COMPARTMENT SEAT TRACK UPPER SURFACE HAS CORROSION BETWEEN C72-C73 BL 00 REMOVED FLOOR PANEL 2 52/251WH TO GAIN ACCESS TO DAMAGED SEAT TRACK GOT MATERIAL FOR SEAT TRACK AND U SECTION. LOCATED AND DRILLED SEAT TRACK AND U SECTION. INSTALLED SEAT TRACK AND U SECTION IAW AIR BUS 310/200 SRM 51-40-21 MATERIAL ID SEAT TRACK (PO NR 57776 3-1) PART NR FOR U SECTION (R5327049020000). 2 L 7 2 4F RT A35EU 2007072500195 20070725 00195 WP 2007 7 25 07FDEA02522 1 20070719 A 5347 AGA38555 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CORRODED SEAT TRACK AT LBL 54 AFT BULK PIT AT STA 1801 TO1840. REMOVED, FABRICATED AND INSTALLED SEAT TRACK IAW MD/DC10 SRM 51-31-01 VOLII AND 51-21-01 VOLII AND DWG AGA3855. 2 L 7 3 4F RT A22WE 2007072500198 20070725 00198 WP 2007 7 25 07FDEA02525 1 20070719 A 5311 AEA00181 FRAME DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CLG WHEEL WELL CAVITY CORROSION ON CIRCUMFERENTIAL ANGLE AT FWD OF STA 15121, BETWEEN LONGERON 51L AND 52. REMOVED, RE PLACED AND INSTALLED 2 EACH ANGLES AT 51L TO 52 AT FS 1521 IAW MD/DC10 SRM 51-33-01 VOL II PAGE 1. 2 L 7 3 4F RT A22WE 2007072500201 20070725 00201 SO 2007 7 25 SIMA200720412 1 20070606 A 5322 14525175001 SHEAR TIE EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 855AE 9744 5000 145747 SHEAR TIE AT FRAME 65 CORRODED. REMOVED AND REPLACED SHEAR TIE IAW EMB IC2007-145-03768, PARGRAPH ONE. RETURNED AIRCRA FT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007072500203 20070725 00203 SO 2007 7 25 SIMA200720404 1 20070603 A 5320 14524128403 SUPPORT FITTING EMB 135 EMB135KL 3260302 SO ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 806AE 13290 5000 145503 PASSENGER DOOR THRESHOLD FORWARD SUPPORT CORRODED. REMOVED AND REPLACED PASSENGER DOOR THRESHOLD SUPPORT IAW EMB SRM 51 -40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007072500205 20070725 00205 SO 2007 7 25 SIMA200720416 1 20070608 A 5320 14525480603 SILL EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 855AE 9744 5000 145747 BAGGAGE DOOR LOWER SILL FOUND CORRODED. REMOVED AND REPLACED LOWER SILL IAW EMB SRM 51-20-01, 51-20-03, 51-40-02, 51-40 -04 AND 51-40-06. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007072500213 20070725 00213 NM 2007 7 25 DHL2007784508 1 20070713 A 5347 BAC15201467170 CARGO TRACK BOEING 727 727227 1384078 NM MAIN CARGO BAY CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 MAIN CARGO, NICKS, GOUGES AND CORROSION ON SEAT TRACK, RBL 24, BS 850 TO BS 870. REMOVED DAMAGED SEAT TRACK SECTION IAW B727 SRM 51-30-2 AND B727 AMM 53-10-1. FABRICATED NEW SEAT TRACK, MATERIAL USED BAC1520-146-7178T6511, DIM. 17 LONG IA W B727 SRM 53-10-2, FIG.7 AND 51-30-5. TREATED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 2007072500216 20070725 00216 NM 2007 7 25 07FDEA02528 1 20070720 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 603FE 48459 CENTER LANDING GEAR LEFT MOUNTING TRUNNION FITTING CENTER GUIDE HOLE FOUND WITH CORROSION. [08-06-07] REPAIR CAR RIED OUT AS PER FEDEX EA 1-5310-112364, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007072600054 20070726 00054 NM 2007 7 26 QXEA200701200 1 20070723 A 5210 SEAL BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR DIRTY A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 406QX 4048 PDX FLIGHT NR 2454: AFT PASSENGER DOOR HARD TO OPEN. MAINTENANCE CLEANED THE DOOR SEAL. OPS CHECK WAS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007072600055 20070726 00055 NM 2007 7 26 QXEA200701201 1 20070724 A 6120 AUTOFEATHER SYS BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 421QX 4149 SEA FLIGHT NR 2287: AUTOFEATHER FAILED TO ARM ON TAKEOFF ROLL. REJECTED TAKEOFF AT 65 KIAS. PERFORMED REJECTED T/O CHE CKLIST. MAINTENANCE INTERROGATED CDS. NO FAULTS POSTED. PERFORMED OPS TEST OF AUTOFEATHER SYSTEM. BOTH ENGINES START ED AND RUNNING IAW AMM TASK 61-20-00-710-801. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007072600056 20070726 00056 NM 2007 7 26 QXEA200701204 1 20070722 A 5230 HANDLE BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR UNSECURE A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 401QX 4031 STS FLIGHT NR 2467: FUSELAGE DOOR WARNING LIGHT ILLUMINATED ON T/O. AFT BAGGAGE DOOR INDICATES OPEN. AIRCRAFT RETURNED TO THE FIELD. MAINTENANCE FOUND THE AFT BAGGAGE DOOR HANDLE POPPED. VISUALLY INSPECTED AFT CARGO DOOR. NO DEFECTS NO TED. C/W Q400 AMM OPS TEST OF AFT CARGO DOOR TASK 52-31-00-710-801. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RE TURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007072600057 20070726 00057 2007 7 26 753002 4 20070718 A 3450 7890860011 INU BOEING 747 747228F 1384895 NM ZONE 100 FAILED A Q2SA C ABORTED TAKEOFF G J MULTIPLE FAILURE WARNING INDICATION TO TAKEOFF 1 EA 63 753SA 21787 TAKEOFF REJECTED AT 120 KNOTS AT RKSI, DUE TO NR 1 INS FAIL WARNING AND CAPTAIN'S ATTITUDE INSTRUMENT FAIL WARNING. REM OVED AND REPLACED NR 1 INU IN ACCORDANCE WITH AMM 34-41-03. OPERATIONAL CHECK NORMAL ON GROUND. ACCOMPLISHED HIGH ENER GY STOP/HEAT DAMAGE CONDITION INSPECTION IN ACCORDANCE WITH AMM 05-51-10. NO DISCREPANCIES FOUND. 2 L 7 4 4F A20WE 2007072600058 20070726 00058 NM 2007 7 26 QXEA200701202 1 20070720 A 2910 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM HYD SYSTEM UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 419QX 4145 SEA FLIGHT NR 2294: DURING AFTER START FLOW, FO REPORTS NR 3 HYD PRESSURE DROPS BELOW 1000 PSI DURING CONTROL CHECK. AI RCRAFT RETURNED TO BLOCK. MAINTENANCE BLED THE NR 3 HYDRAULIC SYSTEMS IAW AMM TASK 29-10-00-870-803. PERFORMED OPERATI ONAL TEST OF THE NR 3 HYDRAULIC SYSTEM IAW TASK 29-12-01-710-801. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNE D TO SERVICE. 2 H 7 2 4T RT A13NM 2007072600059 20070726 00059 NM 2007 7 26 QXEA200701205 1 20070721 A 2131 92146A010401 CONTROLLER BOMBDR DHC8 DHC8402 1390042 NM CABIN PRESSURE MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 410QX 12148 12148 4053 RNO FLIGHT NR 2258: CABIN PRESSURIZATION WARNING AND PARTIAL LOSS OF PRESSURIZATION. PRESSURE HELD 3.0 INCHES IN AUTO. MAINTENANCE REMOVED AND REPLACED CONTROLLER. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007072600060 20070726 00060 NM 2007 7 26 DHLA200700035 1 20070720 A 2612 FIRE WARNING BOEING 727 727247 138408F NM ILLUMINATED A DHLA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. M A J OVER TEMP FLAME/FIRE WARNING INDICATION TX TAXI/GRND HDL 1 GL 05 793DH 21393 ENG NR 1 NO LIGHT OFF, PERF ABNORMAL PROC MOTORED ENG AND ON RESTART ENG DID NOT LIGHT, JUST BEFORE IDLE CUTOFF ENG LIT AND OVERTEMPED 580 DEG MOMENTARALLY GROUND CREW ADVISED ENG NR 1, TAILPIPE FIRE. PULLED FIRE HANDLE AND DISCHARGED 1 FI REBOTTLE AT MX REQUEST. 2 L 7 3 4F A3WE 2007072600061 20070726 00061 NM 2007 7 26 DU4R2007146 1 20070702 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM BS 365 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 638DL 23761 FOUND CORROSION ON UPPER T-CAP OF CABIN FLOORBEAM AT BS 365, B/L 3-R TO B/L 32R. REPAIRED BY FABRICATING AND INSTALLING T-CAP REPAIR 52 BY 2.5 FROM 7075-T6 .071, SUPPORT ANGLE 11 BY 1.75 FROM 7075-T6 .063, SUPPORT ANGLE 8.5 BY 1.75 7075-T6 .090, RADIUS FILLER 7 BY 1 FROM 7075-T6 .125, STRAP 10.25 BY 1 FROM 7075-T6 .063 AND STRAP 7 BY 1 FROM 7075-T6 .090 IAW B757 SRM 53-00-51 FIG 201. 2 L 7 2 4F RT A2NM 2007072600062 20070726 00062 NM 2007 7 26 DU4R2007145 1 20070702 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM BS 345 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 638DL 23761 FOUND CORROSION ON UPPER T-CAP OF CABIN FLOORBEAM AT BS 345 B/L 48R. REPAIRED BY FABRICATING AND INSTALLING T-CAP PAN 7 5-3/4 FROM BAC 1505-100617, SPLICES 12 BY 2 BY ¾ FROM 7075-T6 .050 AND 8 BY 2 BY ¾ FROM 075-T6 .063”, STRIPS 11-1/2, 1 BY 6 BY 1 AND 10 BY 2 BY ¾ , 6-3/4 BY 2 BY ¾, 9-3/4 BY 1 AND 6 BY 1 FROM 7075-T6 .063 IAW B757 SRM 53-00-51 FIG 201. 2 L 7 2 4F RT A2NM 2007072600063 20070726 00063 NM 2007 7 26 DU4R2007151 1 20070714 A 5311 FRAME BOEING 757 757232 1384965 NM BS 1480 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 638DL 23761 FOUND CORROSION IN AFT PIT ON MAIN FRAME BS 1480 UPPER AND FWD AREA BETWEEN S-26, S-27 RT. REPAIRED BY FABRICATING AND INSTALLING DOUBLER REPAIR 20 BY 4.0 FROM 7075-T6 .063 IAW B757 SRM 53-00-57, 53-60-07, 51-20-01 AND 51-40-02. 2 L 7 2 4F RT A2NM 2007072600064 20070726 00064 NM 2007 7 26 QXEA200701209 1 20070724 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY MALFUNCTIONED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 368PH 18204 5945 512 PDX FLIGHT NR 2149 SMOKE WARNING LIGHT ILLUMINATED DURING CLIMB-OUT. RETURNED TO FIELD AS PER EMERGENCY V-LIST. C/W OP S CHECK OF BAG SMOKE DETCTORS. COULD NOT DUPLICATE ON GROUND. VISUAL OF BAGGAGE COMPARTMENT DETECTORS NR 1 SMOKE DETEC TOR ON CEILING DID NOT HAVE COPPER GROUNDING TAPE INSTALLED. REPLACED NR 1 SMOKE DETECTOR. OPERATIONAL CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007072600065 20070726 00065 EU 2007 7 26 F3LA200700180 1 20070724 A 5315 D5347217220500 FLOORBEAM AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 803FR 5201 2017 DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM INBD OF R2 DOOR GIRT BAR CUTOUTS HAD LIGHT TO MODERATE CORROSION AT ALL NUT PLATE ATTACH POINTS. REPLACED FLOORBEAM IAW A318 SRM 51-42-11, STEP 7B. 2 L 7 2 4F RT 2007072600066 20070726 00066 NM 2007 7 26 DHL2007741509 1 20070717 A 5321 PRESSURE PANEL BOEING 727 7272Q9 138448M NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 WHILE IN "C" CHECK REF ASTAR NR 127407, AFT PIT RT BS 1176 TO 1183 BETWEEN RBL45 AND RBL 55 PRESSURE WEB IS CRACKED (WL2 08). REMOVED CRACKED WEB IAW B727 SRM 51-30-2. FABRICATED NEW WEB IAW B727 SRM 53-10-2 FIG 5 AND 51-20-1 FROM 2024T3 . 032 PO NR 9002406 (DIM.16 5/8" BY 6"). TREATED AND PRIMED NEW WEB IAW B727 SRM 51-10-2 AND INSTALLED NEW WEB AT AFT PIT WL208 RT BETWEEN BS 1176 AND 1183 IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007072600067 20070726 00067 EU 2007 7 26 MALA070088 1 20070714 A 5220 SKIN SAAB SF340 340B 7860101 EU ESCAPE HATCH DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 444XJ 340B444 DURING 4K CHECK, 5 DENTS WERE FOUND IN THE OUTER SKIN OF THE PILOT EMERGENCY DOOR (CREW HATCH) RANGING IN DEPTH FROM 0.0 02 TO 0.018 INCH DEEP. ONE DENT IS ON THE CHEM MILLED STEP, AND ANOTHER HAS A SLIGHT CREASE WITH EVIDENCE OF DISBOND. PER SAAB REPAIR STATEMENT 340SDS012750 DATED 07/09/2007, THE DISBONDED DENT MUST BE REPAIRED. REPAIRED DISBONDED DENT P ER EO NR S52076. 2 L 7 2 4T RT A52EU 2007072600068 20070726 00068 EU 2007 7 26 MALA070089 1 20070714 A 5320 STRUCTURE SAAB SF340 340B 7860101 EU BS 288 UNKNOWN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 444XJ 340B444 BOTTOM FRAME REINFORCEMENT STA 288-294. REPAIRED BOTTOM FRAME REINFORCEMENT IAW EO NR S53362 AND SRM 53-70-30 SPECIAL R EPAIR PARAGRAPH 7. 2 L 7 2 4T RT A52EU 2007072600069 20070726 00069 EU 2007 7 26 MALA070090 1 20070714 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 444XJ 340B444 CORROSION DAMAGE ON THE LOWER FLANGE AND WEB OF A SEAT TRACK IN THE CABIN PER SRM 53-70-60 PARAGRAPH 8. THIS REPAIR MUS T BE ACCOMPLISHED IF REMAINING LOWER FLANGE THICKNESS IS 80 PERCENT OR LESS OF ORIGINAL THICKNESS, AFTER REMOVAL OF THE CORROSION DAMAGE. CABIN SEAT TRACK LOWER FLANGE AND WEB CORROSION FOUND DURING 4K CHECK. REPAIRED PER EO NR S53342 AND SRM 53-70-60. 2 L 7 2 4T RT A52EU 2007072600070 20070726 00070 EU 2007 7 26 AWXA200700862 1 20070709 A 5347 D571301472004 SEAT TRACK AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 654AW 1050 SAL - MAJOR REPAIR - CORROSION ON CABIN SEAT TRACK, BS 1590/FR 36 + 1", -Y765. REPLACED CABIN SEAT TRACK, BS 1590/FR 36 - BS 1810/FR 41, -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007072600071 20070726 00071 EU 2007 7 26 AWXA200700863 1 20070709 A 5321 D5361060500100 FLOOR PANEL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 654AW 1050 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5962604, CORROSION ON CABIN FLOORBOARD 222FF, BS 709/FR 16 - BS 808/FR 20, -Y1292 T O -Y1732. REPLACED CABIN SEAT TRACK, BS 1430/FR 36 - BS 1650/FR 41, -Y765 IAW AWA TASK CARD C1C53302. 2 L 7 2 4F RT A28NM 2007072600072 20070726 00072 EU 2007 7 26 AWXA200700864 1 20070709 A 5347 D57130147203 SEAT TRACK AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 654AW 1050 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5948791, CORROSION ON CABIN SEAT TRACK, BS 1590/FR 36 + 1" AND BS 1753/FR 40 + 14" , -Y1292. REPLACED CABIN SEAT TRACK, BS 1590/FR 36 - BS 1810/FR 41, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007072600073 20070726 00073 EU 2007 7 26 AWXA200700865 1 20070710 A 5315 D5347218820400 FLOORBEAM AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 654AW 1050 SAL - MAJOR REPAIR - BC-6 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3257/FR 68 + 2" , +Y1162. REPLACED CABIN FLOORBEAM, BS 3207/FR 67 - BS 3310/FR 69, +Y1162 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007072600074 20070726 00074 EU 2007 7 26 AWXA200700866 1 20070710 A 5320 D5347218902 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 654AW 1050 SAL - MAJOR REPAIR - BC-6 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3257/FR 68 + 2" , -Y1162. REPLACED CABIN FLOORBEAM, BS 3257/FR 68 - BS 3310/FR 69, -Y1162 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007072600075 20070726 00075 EU 2007 7 26 AWXA200700867 1 20070709 A 5320 D53475765200 SILL AIRBUS 320 A320232 3930326 EU ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 654AW 1050 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5948930, CORROSION ON BULK CARGO COMPARTMENT DOOR CUT OUT LOWER SILL, BS 2883/FR 61 + 19" , -Y630. REPAIRED BULK CARGO COMPARTMENT DOOR CUT OUT LOWER SILL, BS 2883/FR 61 + 19", -Y630 IAW A320 SRM 53-41 -49. 2 L 7 2 4F RT A28NM 2007072600076 20070726 00076 EU 2007 7 26 AWXA200700868 1 20070711 A 5322 D5347112420100 SHEAR TIE AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 654AW 1050 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5962700, CORROSION ON SHEAR PLATE, BS 3510 FR 69, -Y1732. REPLACED SHEAR PLATE, BS 3510 FR 69 - BS 3366/FR 70, -Y1732 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007072600077 20070726 00077 2007 7 26 TSAA0734041 4 20070718 A 3422 7771083002 HSI BOEING 737 7372X6C 1384552 NM NR 1 FAILED A TSAA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 13 816AL 23122 CARGO FLIGHT 944 HNL-KOA - DURING CLIMB, THE CAPTAIN NOTED THE NR 1 HORIZONTAL SITUATION INDICATOR HAD THE COMPASS FLAG IN VIEW. THE CAPTAIN ATTEMPTED TO TRANSFER THE COMPASS INDICATION TO BOTH ON NR 2 BUT THE FLAG REMAINED IN VIEW. THE C REW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 HSI AND OPS CHECKED PER AMM 34-26-21. AIRC RAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007072600078 20070726 00078 NM 2007 7 26 07FDEA02527 1 20070719 A 3610 652244419 DUCT BOEING 727 727233 138408A NM NR 1 ENGINE LEAKING A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 277FE 22042 NR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON AT 6000' DURING CLIMB, RAN QRH PROCEDURE AND WERE ABLE TO MAKE THE LIGHT GO OUT WITH REDUCING POWER. ADVANCING POWER CAUSED THE LIGHT TO COME ON AGAIN. REDUCED NR 1 ENGINE TO IDLE POWER AND RETURN TO MEMPHIS. MEM R AT HIGH PWR SETTING FOUND 8TH STAGE AIR DUCT BLOWING AIR TOWARDS SENSOR LOOP. REPLACED DUCT AND RE POSITIONED CLAMPS. RAN ENG PER JRH, REINSTALLED PANELS AND OPS GOOD. 2 L 7 3 4F RT A3WE 2007072600079 20070726 00079 SO 2007 7 26 SWIA200718486 1 20070716 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN BROKEN A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 295SW 120322 FLT 5547 - FRONT LEFT FLOOR EMERGENCY LIGHT IS BROKEN. INSTALLED NEW LENS ASSEMBLY. 2 L 7 2 4T RT A31SO 2007072600080 20070726 00080 2007 7 26 SWIA200718488 2 20070713 A 7200 ENGINE CNDAIR CL600 CL6002C10 1390015 EA LEFT VIBRATES A SWIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 07 753SK 10214 FLT 6685 - LEFT VIB GAUGE WENT TO 1.8 AS WE CLIMBED OUT. RETURNED TO FIELD. PERFORMED ENGINE FAN BLADE LUBE IAW ST 900 -1016 ON THE LEFT ENGINE. ALL VIB CHECKS WITHIN LIMITS. 2 L 7 2 4F RT A21EA 2007072600081 20070726 00081 EA 2007 7 26 SWIA200718489 1 20070714 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 919SW 7657 FLT 5937 - LEFT SIDE WINDOW CRACKED AT FL340. REPLACED LEFT WINDOW AS REQUIRED IAW CRJ 200 MM 56-12-01, PN ON NP-13932 2-5, SN OFF, 02056H9385. 2 L 7 2 4F RT A21EA 2007072600082 20070726 00082 EA 2007 7 26 SWIA200718490 1 20070601 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 710SK 10170 STA 280 FLOORBEAM IS CRACKED AND CORRODED, DISCOVERED AT C-CHECK. INSTALLED NEW FLOOR BEAM, U CHANNELS AND INTERCOSTALS PER REO:670-53-11-047. 2 L 7 2 4F RT A21EA 2007072600083 20070726 00083 EA 2007 7 26 SWIA200718491 1 20070601 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 710SK PAX DOOR FORWARD WEB IS CRACKED AT 2ND STEP, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS PER REO 670-52-11-104. 2 L 7 2 4F RT A21EA 2007072600084 20070726 00084 EA 2007 7 26 SWIA200718492 1 20070601 A 5210 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 710SK 10170 PAX DOOR AFT DRAG ANGLE IS CRACKED, DISCOVERED AT C-CHECK. COMPLIED WITH STEPS 1-13 ON REO 670-52-11-072 FOR REPAIR ON PAX DOOR DRAG ANGLE ON AFT SIDE. 2 L 7 2 4F RT A21EA 2007072600085 20070726 00085 EA 2007 7 26 SWIA200718493 1 20070601 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 710SK 10170 PAX DOOR AFT WEB IS CRACKED BETWEEN 2ND AND 3RD STEP, DISCOVERED AT C-CHECK. COMPLIED WITH STEPS 1-17 OF REO 670-52-11- 104 FOR DOOR REPAIR. 2 L 7 2 4F RT A21EA 2007072600086 20070726 00086 EA 2007 7 26 SWIA200718494 1 20070601 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 710SK 10170 AFT COCKPIT FLOOR SUPPORT IS CORRODED, DISCOVERED AT C-CHECK. REPAIRED DAMAGED COCKPIT FLOOR SUPPORT PER CRJ7/9 SRM 51- 42-06-001-001-A01. 2 L 7 2 4F RT A21EA 2007072600087 20070726 00087 EA 2007 7 26 SWIA200718495 1 20070715 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 703SK 10139 OVERHEAD EMERGENCY LIGHT AT ROW 16 IS OUT. RELAMPED OVERHEAD EMERGENCY LIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007072600088 20070726 00088 EA 2007 7 26 SWIA200718496 1 20070714 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 442SW 7609 THIRD CEILING EMERGENCY LIGHT FROM THE FRONT IS INOP. REPLACED EMERGENCY LAMP. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007072700001 20070727 00001 EU 2007 7 27 07FDEA02559 1 20070719 A 3230 BDM3003 PROXIMITY SENSOR AIRBUS 310 A310324 3930206 EU ZONE 700 FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 801FD 15023 335 539 ON DEPARTURE EDDF RWY 18 LDG GEAR WOULD NOT RETRACT. RETURNED TO LAND 10,000 BELOW MLW. NO FURTHER PROBLEMS. JACK A/C PER MM 07-11-00-0. REMOVED AND REPLACED BOGIE BEAN PROX DETECTOR 8GA PER MM 32-00-00-4. WHILE REPLACING 8GA PROX DETE CTOR FOUND 12GA PROX DETECTOR ADJUSTMENT NOT WITHIN MM LIMITS. ADJUSTED SAME AS PER MM 32-00-00-4. SWUNG GEAR ON BOTH SYS 1 AND SYS 2 ALL GEARS AND DOORS WORKED NORMAL ON BOTH SYSTEM. 2 L 7 2 4F RT A35EU 2007072700006 20070727 00006 EU 2007 7 27 07FDEA02564 1 20070723 A 5754 SEE4A FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 CORROSION ON FITTING AND DAMAGED REINFORCING ANGLE IN KRUEGER FLAP AREA RT. REPAIR WAS PERFORMED BY REPLACEMENT OF FITT ING IAW SRM 57-45-11 AND REINFORCEMENT ANGLE IAW SRM 57-41-11. 2 L 7 2 4F RT A35EU 2007072700009 20070727 00009 EU 2007 7 27 07FDEA02568 1 20070723 A 5330 A53812225 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 TWO SIMILAR DEFORMATIONS ON SKIN PANEL (BOTH RHS AND LHS) BETWEEN C51 AND C52, P39-40. REPAIR PERFORMED BY DRESSING BAC K THE DENTS, PERFORMING ROTOTEST AND HFEC AND INSTALLING HL11VF5 FASTENERS IAW EA 6-53-15-103318 AND RAS 046898/014/2006 . 2 L 7 2 4F RT A35EU 2007072700010 20070727 00010 EU 2007 7 27 07FDEA02570 1 20070723 A 5320 STIFFENER AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 657FE 748 FWD CARGO COMPARTMENT FWD SIDE OF FLOORBEAM C32 VERTICAL STIFFENER OUTBD SEAT TRACK 4L HAS .25" LONG CRACK IAW A300-600 AMM 53-13-11-6. CUT OUT DAMAGED AREA IAW A300-600 SRM 53-10-15 PG 254. NDT SHOWS NO CRACK REMAINS PER NTM 51-10-02. FABRICATED REPAIR PARTS PER A300-600 SRM 53-10-15 PG 311/312. INSTALLED REPAIR PER A300-600 SRM 53-10-15. RESTORED SURF ACE PROTECTION (ALODINE, PRIME, AND TOPCOAT) IAW A300-600 SRM'S 51-21-10 AND 51-75-10. 2 L 7 2 4F RT A35EU 2007072700011 20070727 00011 NM 2007 7 27 07FDEA02578 1 20070723 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 603FE 48459 CENTER LANDING GEAR RIGHT TRUNNION FITTING FOUND WITH CORROSION. [08-03-07] REPAIR CARRIED OUT AT CENTER LANDING GEAR RIGHT HAND TRUNNION FITTING AS PER SRM 53-40-00 FIGURE 16 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007072700012 20070727 00012 NM 2007 7 27 07FDEA02579 1 20070723 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 603FE 48459 CENTER LANDING GEAR MOUNTING LEFT TRUNNION FITTING FOUND WITH CORROSION. [08-03-07] REPAIR CARRIED OUT AT CENTER LAN DING GEAR MOUNTING LEFT HAND TRUNNION FITTING AS PER SRM 53-40-00 FIGURE 16 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007072700013 20070727 00013 NM 2007 7 27 07FDEA02580 1 20070723 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 603FE 48459 CENTER LANDING GEAR LEFT MOUNTING TRUNNION FITTING BOTTOM SURFACE FOUND WITH CHAFED MARK. [08-03-07] REPAIR CARRIED OUT AT CENTER LANDING GEAR LEFT HAND MOUNTING TRUNNION FITTING BOTTOM SURFACE AS PER SRM 53-40-00 FIGURE 16 VOLUME I. R EPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007072700016 20070727 00016 EU 2007 7 27 07FDEA02572 1 20070723 A 5347 A5361252420 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 657FE 748 MDCC SEAT TRACK 3L FR15 HAS 1 SQ IN AREA OF CORROSION EXTENDING ON AND UNDER SCALLOPS ZONE 220 REF A300-600 AMM 53-10-16 . REMOVED CORROSION AT 3L FR15 SEAT TRACK. FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-16. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-40-21. REPROTECED SEAT TRACK IAW A300-600 SRM 51-23-10. 2 L 7 2 4F RT A35EU 2007072700022 20070727 00022 NM 2007 7 27 HALA0700295 1 20070721 A 2797 CABLE BOEING 767 767300 1385204 NM BROKEN A HALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 13 486HA 55131 DURING FLAP RETRACTION AFTER LANDING FLAP/SLAT DISAGREE ALERT ILLUMINATED. FOUND FLAP BUSS CABLE RUN 33B AND 34A BROKEN . REVD CABLES, FABRICATED CABLES 33B AND 34A PER AMM 91-10-05 AND AMM 20-00-03. INSTALLED AND ADJUSTED PER AMM 27-50-0 0. OPS CHK OK. (CHECK OUT THIS MODEL, I THINK IT MIGHT REALLY BE A 717200, OR WRONG N#). 2 L 7 2 4F RT A1NM 2007072700027 20070727 00027 NM 2007 7 27 DU4R2007154 1 20070719 A 5330 SKIN BOEING 757 757232 1384965 NM BS 660 GOUGED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 639DL 23993 FOUND GOUGE IN FUSELAGE SKIN AT PREVIOUS REPAIR ON LT SIDE BS 660, S-17L. REPAIRED BY FABRICATING AND INSTALLING DOUBLE R REPAIR 13 BY 10 BY 11-3/8 BY 8-1/2 AND TRIPLER 12 BY 8 BY 9-1/4 BY 7-3/4 FROM 2024-T3 .063, DOUBLER AND FILLER 11.25 B Y 8 AND 21 BY 18.50” FROM 2024-T3 .063” IAW DELTA ERA NR 461667-14 REV ORIG DATED 07-19-2007, FAA FORM 8100-9. REPAIR P ERMANENT PER PS 900-51, NR 4. 2 L 7 2 4F RT A2NM 2007072700045 20070727 00045 NM 2007 7 27 07FDEA02582 1 20070723 A 5730 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 603FE 48459 CRACK INDICATIONS REVEALED IN FASTENER HOLE TOWARDS EDGE OF ACCESS CUTOUT IN RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT (P ANEL 636AB). [08-09-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-112366, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2 -100. 2 L 7 3 4F RT A22WE 2007072700060 20070727 00060 EU 2007 7 27 07FDEA02593 1 20070724 A 5320 SR531799A00500 SILL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 HEAVY CORROSION ON UPPER FLANGE OF THE AFT CARGO DOOR SILL BEAM BTW C59-64 RT. REPAIR PERFORMED BY REPLACEMENT OF UPPER FLANGE IAW EA 6-5317-103276 AND RAS/DATLS/0003386/2006. 2 L 7 2 4F RT A35EU 2007072700074 20070727 00074 NM 2007 7 27 07FDEA02605 1 20070725 A 5330 6518385 SKIN BOEING 727 727233 138408A NM ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 RT LWR AFT FUSELAGE EXTERIOR SKIN CHAFED AT AFT CARGO PIT FWD DOOR CUTOUT FWD UPPER CORNER. REMOVED CHAFED DAMAGE IAW S RM 51-10-1, NDT FOR MATERIAL LOSS, IAW NDT MANUAL PART 4 51-00-00 FIG 2, OUT OF LIMITS PER SRM 53-30-1 PG 2C FIG 2, VERI FIED MATERIAL 2024- T3, .050 PER EA NR I070418 P1, STEP 4A. REMOVED FASTENERS FOR NDT INSPECTION OF HOLES, NO DEFECTS NOTED OF HOLES, FAB`D DOUBLER. INSTALLED IAW EA I070418 AT RT AFT FUSELAGE SKIN AT FWD UPPER CORNER OF AFT CARGO PIT DO OR. PRIMED AND TOP COATED AREA OF INSTALLATION IAW EA NR I070418. 2 L 7 3 4F RT A3WE 2007072700084 20070727 00084 NM 2007 7 27 07FDEA02538 1 20070720 A 5315 652082761 FLOORBEAM BOEING 727 727233 138408A NM BS 560 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 CABIN BS 560 FLOORBEAM UPPER CHORD HAS CORROSION ON UPPER SURFACE BETWEEN LBL 12 AND LBL 20. REMOVED DAMAGE IAW SRM 51- 10-1 MAT WAS .125. REMOVED .005 -.120 REMAINS FOUND TO BE WITHIN LIMITS. PERFORMED NDT FOR CRACKS, NEGATIVE RESULTS. ROTO- PEENED IAW SOPM 20-10-03 PG 16. TREATED AND PRIMED IAW SRM 51-10-2 PG 1 EA NR 7-5310713046. 2 L 7 3 4F RT A3WE 2007072700098 20070727 00098 NM 2007 7 27 07FDEA02552 1 20070720 A 5411 65175551621 RIB BOEING 727 727233 138408A NM ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LT AFT FUSELAGE UNDER REMOVED CENTER ENG SUPPORT EXT SKIN PANEL, TRIANGULAR RIB WEB IS CRACKED AT UPP IB CORNER ATTACHED TO OB SIDE OF VERT STAB SKIN BS 1360. (MKD) REMOVED RIB ASSEMBLY, DISASSEMBLED, FABRICATED AND HEAT TREATED NEW WEB, D RILLED UP NEW WEB, ASSEMBLED RIB ASSEMBLY AND INSTALLED REF BAC DRAWING 65-17555 AND SRM 51-30-02. 2 L 7 3 4F RT A3WE 2007072700100 20070727 00100 NM 2007 7 27 DHL2007784513 1 20070708 A 5330 SKIN BOEING 727 727227 1384078 NM BS 475 SCRATCHED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 EXTERNAL FUSELAGE BS 475 AT STR 8R HAS A LIGHTNING BURN ON A FASTENER. BLENDED OUT AREA OF LIGHTNING STRIKE IAW B727 SR M 53-30-3, FIG 20. MATERIAL LOSS OVER 30 PERCENT AND LIGHTNING STRIKE STILL PRESENT AND OUT OF LIMITS IAW B727 SRM 53-3 0-1. CUT OUT DAMAGED AREA DIM 1.5 BY 1.25 IAW B727 SRM 53-30-3, FIG 3. HFEC COMPLIED WITH IN CUT OUT AREA, NO CRACKS N OTED IAW B727 NDTM PT.6 51-00-00, FIG 23. FABRICATED DOUBLER REPAIR FROM .050, 2024T3, DIM 9 BY 6.50 AND FILLER FROM .0 40, 2024T3, DIM 1.5 BY 1.25 IAW B727 SRM 53-30-2, FIG 2 AND 53-30-3, FIG 3. TREATED, PRIMED AND INSTALLED REPAIR IAW B7 27 SRM 51-10-2, 51-30-2 AND 53-30-3, FIG 3. 2 L 7 3 4F A3WE 2007072700104 20070727 00104 WP 2007 7 27 07FDEA02557 1 20070720 A 3220 ACG70111 LUG DOUG DC10 DC1030F 3023504 WP NLG STEERING DAMAGED A FDEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 25 307FE 49980 8073 48291 PDIS: CAPT DOES NOT HAVE FULL NOSE WHEEL AUTHORITY TURNING TO THE RIGHT. RETURNED TO RAMP. FOUND NOSE WHEEL STEERING C OLLAR RT LUG DAMAGED. REMOVED PISTON AND REMOVED AND REPLACED STEERING COLLAR. REPACKED PISTON AND REINSTALLED PISTON, REF DC-10-30MM 32-21-01-8. REMOVED AND REPLACED RT STEERING CYLINDER REF DC-10-30 MM 32-52-01-2. SERVICED NOSE GEAR S TRUT REF DC-10-30 MM 32-21-01-9 2, LEAK CHECKS GOOD. COMPLETED OPS AND LK CK OF STEERING CYLINDER CK'S GOOD REF AMM DC1 0-32-52-01-2. COMPLETED STEERING CABLE ADJUSTMENT AND SAFETY. COMPLETED STEERING SYSTEM OPS CK, NOW CK'S GOOD WITH TIL LER AND RUDDER. 2 L 7 3 4F RT A22WE 2007072700115 20070727 00115 NM 2007 7 27 QXEA200701188 1 20070712 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - WARDROBE SUPPORT CHANNEL IS CORRODED AT WARDROBE FLOOR AFT OUTBOARD ATTACH AT X220, Y32L AND Z100. REPAIRED IA W SRM 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 2007073000005 20070730 00005 NM 2007 7 30 AWXA200700901 1 20070707 A 3397 D9299200900200 WIRE HARNESS AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS DAMAGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 806AW 1056 SAL - EEL - BC-6 CHECK - NR 5971751, DURING OPERATIONAL TEST OF EMERGENCY LIGHTS THE FOLLOWING MESSAGE WAS FOUND "ESPU E XT LOAD EMER L" "EPSU COMM FWD L"ON PTP PANEL. REPLACED AND OPERATIONAL CHECKED WIRE HARNESS AT SEAT 1A IAW A319 AMM 33 -51-19 AND 33-51-00. 2 L 7 2 4F RT A28NM 2007073000010 20070730 00010 NM 2007 7 30 AWXA200700907 1 20070627 A 5320 146N5391107 PANEL BOEING 757 757225 1384959 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - NR 5950875, CORROSION ON AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL SIDE PLATE PANE L, BS 1310 - BS 1377, RBL 25, WL 156.80. REPLACED AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL SIDE PLATE PANEL, BS 13 10 - BS 1377, RBL 25, WL 156.80 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007073000019 20070730 00019 EU 2007 7 30 07FDEA02628 1 20070726 A 5315 7075T7 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 653FE 736 FWD CARGO COMPT CEILING, CABIN FLOORBEAM C-27 HAS A CRACK ON FWD FACE VERTICAL FORMED SECTION, BETWEEN RT SEAT TRACK 2-3 WITH APPROX 0.25 IN LONG REF A300-600 SRM 51-10-10. CLEAN OUT CRACK IN FLOORBEAM IAW A300-600 SRM 53-10-15. FAB`D REP AIR ANGLE AND FILLER IAW A300-600 SRM 51-10-15. ALODINE PARTS IAW A300-600 SRM 51-53-00. PRIME IAW A300-600 SRM 51-23- 00. TOPCOAT IAW A300-600 SRM 51-23-00. INSTALLED REPAIR PART IAW A300-600 SRM 51-10-15 FIG 212. 2 L 7 2 4F RT A35EU 2007073000023 20070730 00023 NM 2007 7 30 AWXA200700897 1 20070724 A 2560 P2070001214 FLASHLIGHT BOEING 737 7373G7 1384595 NM FWD GALLEY FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 309AW 24711 PHX - EEL - LOG 4157208 - MX REPORTED FLASHLIGHT IN FWD GALLEY HAS A DEAD BATTERY. MX REPLACED THE FWD GALLEY FLASHLIGH T. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2007073000046 20070730 00046 SO 2007 7 30 SIMA200720708 1 20070710 A 5310 14521713003 BEAM EMB 135 EMB135KL 3260302 SO ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 818AE 13149 5000 145561 GALLEY HAT BEAM FOUND CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-21-10. AIRCRAF T RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000058 20070730 00058 NM 2007 7 30 DHL2007741510 1 20070721 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 700 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 FWD PIT HAS 1 EA DENT IN RADIUS OF FRAME AT BS 700 BETWEEN STR 23L AND 24L. CUT OUT DAMAGED AREA 1.5" BY 1.25", FABRICA TED REPAIR DOUBLER FROM 7075-T0, .071" BY 9.75" BY 3.75", PO NR 9004690, PER B727 SRM 51-40-3 FIG 1. HEAT TREATED REPAI R PART TO 7075-T6 PER FASI. ER 2-37153-801 REV A. TREATED, PRIMED, AND INSTALLED REPAIR DOUBLER PER B727 SRM 51-40-3 FI G 1, 51-10-2, AND 51-30-2. 2 L 7 3 4F RT A3WE 2007073000067 20070730 00067 EU 2007 7 30 07FDEA02609 1 20070725 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT PIT STRINGER 51L BETWEEN FRAMES 58 AND 54.3 CORRODED. [08-06-07] REMOVED AND REPLACED AFT PIT STRINGER 51L BETWE EN FR 54.3 AND FR 58 IAW A310 SRM 53-10-14 FIG 201 PG 203/204 2 L 7 2 4F RT A35EU 2007073000069 20070730 00069 NM 2007 7 30 07FDEA02611 1 20070725 A 5720 691859016 BRACKET BOEING 727 727233 138408A NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 RT WING FWD NAV LIGHT BRACKET CRACKED. REPLACED RT WING FWD NAV LIGHT BRACKET, REF SRM 51-30-02 P.13. 2 L 7 3 4F RT A3WE 2007073000070 20070730 00070 NM 2007 7 30 07FDEA02612 1 20070725 A 5315 6520832 FLOORBEAM BOEING 727 727233 138408A NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 CABIN FLOORBEAM AT STA 950 HAS CORROSION ON UPPER SURFACE BET RBL 24 RBL 45 REMOVED CORROSION FROM FLOORBEAM AT STA 950 RBL 24 TO RBL 45 IAW B727 SRM 51-10-1, ORIGINAL .125", REMAINING .120", HFEC. NO DEFECTS NOTED, ROTO PEENED, TREATED AN D PRIMED IAW EA NR 7-5310-113055. 2 L 7 3 4F RT A3WE 2007073000071 20070730 00071 CE 2007 7 30 Y2PA200700024 1 20070724 A 3260 6838 BULB LEAR 35 35A 5170602 CE MLG INDICATOR BURNED OUT A Y2PA A UNSCHED LANDING P NO WARNING INDICATION AP APPROACH 1 GL 23 135DE 667 AIR WAS ENTERING DOWNWIND LEG AT AMA, AT APPROPRIATE TIME GEAR DOWN WAS CALLED FOR. LANDING GEAR SELECTED DOWN, LEFT MA IN DID NOT INDICATE DOWN "NO GREEN". LANDING GEAR WAS CYCLED BACK UP THEN BACK DOWN. UPON 2ND GEAR DOWN ATTEMPT ONLY T HE NOSE WHEEL INDICATED DOWN. AT GEAR DOWN ATTEMPT FO REPORTED "POP". CREW REQUESTED FLYBY OF AMA TOWER. TOWER REPORT ED RIGHT GEAR APPEARED DOWN HOWEVER AN AMERICAN EAGLE FLIGHT ON LEFT SIDE OF AIRCRAFT REPORTED THAT LEFT GEAR DID NOT AP PEAR TO BE DOWN AND LOCKED. GEAR WAS RETRACTED AND CAPTAIN ELECTED TO RETURN TO ABQ. NORMAL FLIGHT BACK TO ABQ. DECLA RED EMERGENCY WITH ABQ APPROACH, EXTEND GEAR NORMALLY REQUESTED FLYBY OF TOWER AND MAINTENANCE. AFTER GEAR WAS REPORTED 2 L 7 2 4F A10CE 2007073000074 20070730 00074 WP 2007 7 30 IXXA07SMN192S 1 20070630 A 5751 SKIN DOUG DC8 DC873F 302199F WP ZONE 500 DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND DENTS LEFT WING OUTBOARD AILERON LEADING EDGE SKIN BETWEEN STATION 680.000 AND XA 674.000. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND DOUBLERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS . APPLIED SEALANT TO FAYING SURFACE. INSTALLED REPAIR PARTS FROM STATION XA 674.000 TO XW 698.000. PERFORMED BALANCE TO OTBD AILERON FOUND WITHIN ALLOWABLE TOLERANCE LIMITS. MOMENT: 3341.7 IN LBS IAW DC8 SRM 57-8-1 FIGURE 4, DC8 57-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 57-8-1 FIGURE 4 ITEM "H", DC8 SRM 51-1-8B,DC8 SRM 51-1-11, DC8 SRM 51-4-3. 2 L 7 4 4F RT 4A25 2007073000077 20070730 00077 EA 2007 7 30 SIMA200720602 1 20070707 A 5315 S61444 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 504AE 11750 4000 10044 LEFT CENTER FLOORBEAM T-FITTING AT STATION 280 CRACKED. REPAIRED IAW CRJ REPAIR STATEMENT REO 670-53-11-045. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007073000080 20070730 00080 SO 2007 7 30 SIMA200720601 1 20070724 A 2913 971808MODA PUMP EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LT ENGINE FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 648AE 16309 1071 145225 CAE312612 "SUP" LANDING GEAR DISAGREE, NOSE LANDING GEAR INDICATOR SHOWED GREEN, BOTH MAIN INDICATOR SHOWED RED, CYCLED GEAR AND I T EXTENDED NORMALLY. DECLARED EMERGENCY, RETURNED TO EVV. REMOVED AND REPLACED NUMBER ONE HYDRAULIC ENGINE DRIVEN PUMP IAW EMB AMM 29-10-03. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007073000084 20070730 00084 SO 2007 7 30 SIMA200720610 1 20070716 A 5347 14530637004 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 723AE 13150 5000 145288 RIGHT NUMBER 4 UPPER SEAT TRACK SUPPORT CORRODED. CUTOUT CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB IC200 7-145/04757A, DATED JULY 13, 2007. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000085 20070730 00085 NM 2007 7 30 UIEA200700273 1 20070720 A 5280 65B1166947 DOOR BOEING 747 747341 13848AM NM MLG DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 MATERIAL SEPARATING ON FORWARD EDGE OF LT WING GEAR INBOARD DOOR. AREA IS 15.0 INCH LONG BY 1.0 INCH WIDE. PERMANENT R EPAIR ACCOMPLISHED AS PER B747-300 SRM 51-40-09, FIG 12, SHEETS 1, 2, AND 3, TABLE II, 250*F CURE AND SRM 51-40-12, REFE RENCE ATLAS AIR XEO NR 52-071907. 2 L 7 4 4F RT A20WE 2007073000086 20070730 00086 NM 2007 7 30 UIEA200700274 1 20070719 A 5280 65B1166974 FAIRING BOEING 747 747341 13848AM NM MLG DOOR CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 RT WING GEAR INBOARD STRUT DOOR FAIRING HAS A COMPOSITE CRACK AT AFT SIDE TOP SKIN AND CHAFE STRIP DAMAGED. PERMANENT R EPAIR ACCOMPLISHED AS PER B747-300 SRM 51-40-09, FIG 12, SHEETS 1, 2, AND 3, TABLE I, 250*F CURE AND SRM 51-40-12, CHAFE STRIP REPLACED AS PER B747-300 SRM 51-30-02, REFERENCE ATLAS AIR XEO NR 52-071907. 2 L 7 4 4F RT A20WE 2007073000087 20070730 00087 NM 2007 7 30 UIEA200700275 1 20070724 A 5311 FRAME BOEING 747 747271C 1384869 NM BS 1310 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 CORROSION ON RIGHT AFT UPPER AND LOWER CORNER INBOARD SIDE OF THE R3 DOOR CUT OUT. XEO-53-072007 ACCOMPLISHED TO REMOVE EXFOLIATION CORROSION. TO BE REINSPECTED EVERY 3000 FLIGHT CYCLES PER PART 2 OF XEO 53-072007. NDT AND VISUAL INSPECT ION ACCOMPLISHED REF BOEING MESSAGE 1-383704990-2 AND SRM 53-30-03 FIG 44. 2 L 7 4 4F A20WE 2007073000090 20070730 00090 NM 2007 7 30 UIEA200700278 1 20070724 A 5343 TRUNNION BOEING 747 747271C 1384869 NM BS 1480 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 LT BODY GEAR OUTBOARD TRUNNION BEARING SUPPORT FITTING FACE HAS PITTING. BORE FACE AND SIDE FACES WERE MACHINED TO REMO VE DAMAGED AREAS ID= 10.826", IB SIDE FACE = 0.017 REMOVED. OB SIDE FACE = 0.025 REMOVED. REPAIR REF B747 SRM 53-10-08 FIG 2. 2 L 7 4 4F A20WE 2007073000091 20070730 00091 NM 2007 7 30 07FDEA00631 1 20070303 A 2910 HYDRAULIC SYSTEM BOEING 727 727233 138408A NM A SYSTEM DISCHARGED A FDEA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 25 218FE 21101 HYD "A" SYSTEM DEPLETED W/FLAPS SELECTED TO 2 ON APPROACH ON 27 MEM. NR 2 "A" PUMP LIGHTS ON FOR 2-3 MINS, FLUID SHUTO FF SWITCHES OF 2-3 MINS. 2 L 7 3 4F RT A3WE 2007073000094 20070730 00094 EU 2007 7 30 07FDEA02634 1 20070726 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 FLOORBEAM UPPER TEE CORRODED ON LOWER SIDE AT FRAME 36 RBL 60. [08-08-07] REMOVED CORROSION FOUND OUT OF LIMITS IAW A310-200 SRM 53-10-00, REMOVED CORRODED SECTION AND REPLACED WITH NEW UPPER TEE IAW A310-200 SRM 53-10-15 PG241/242 2 L 7 2 4F RT A35EU 2007073000096 20070730 00096 2007 7 30 QXEA200701167 4 20070718 A 3421 H321ALM1 INDICATOR DHAV DHC8 DHC8202 2809007 NM COCKPIT MALFUNCTIONED A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 366PH 3012 510 SEA FLIGHT NR 2070 - DURING CLIMB, THE STANDBY ATTITUDE INDICATOR ROLLER OVER. REPLACED STANDBY ATTITUDE INDICATOR IAW D8 200 AMM 34-23-00-000-801 AND 24-33-00-400-801. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007073000098 20070730 00098 NM 2007 7 30 QXEA200701174 1 20070709 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM BS 600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - CORROSION AT STATION 600 ON LOWER FACE OF AFT CARGO STEP JUST AFT OF CARGO DOOR CUTOUT. REPAIRED IAW SRM 51-20 -11, 51-20-16, 51-20-36. 2 H 7 2 4T RT A13NM 2007073000100 20070730 00100 NM 2007 7 30 QXEA200701178 1 20070705 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT TE FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - LEFT INBOARD FLAP INBOARD UPPER TRACK HAS AREA OF WEAR ON LOWER CONTACT SURFACE AT 10" AFT OF FORWARD END. REP AIRED IAW RD8/4-57-985. 2 H 7 2 4T RT A13NM 2007073000101 20070730 00101 NM 2007 7 30 QXEA200701179 1 20070705 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT TE FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - LEFT INBOARD FLAP INBOARD LOWER TRACK HAS SEVERAL AREAS OF WEAR ON UPPER CONTACT SURFACE AT 4", 8", AND 20" AFT OF FORWARD END. REPAIRED IAW RD8/4-57-985. 2 H 7 2 4T RT A13NM 2007073000103 20070730 00103 NM 2007 7 30 QXEA200701181 1 20070706 A 5753 STRUCTURE DHAV DHC8 DHC8202 2809007 NM NR 4 FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - LEFT NR4 FLAP, HAS TWO DIVOTS ON OUTBOARD CENTER SURFACE. REPAIRED IAW RD8/4-57-988. 2 H 7 2 4T RT A13NM 2007073000106 20070730 00106 NM 2007 7 30 QXEA200701184 1 20070713 A 5310 STOP DHAV DHC8 DHC8202 2809007 NM DOOR FRAME WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - RIGHT CENTER EMERGENCY EXIT DOOR STOPS ON FUSELAGE HAVE LIGHT WEAR. REPAIRED IAW RD8/4-53-126. 2 H 7 2 4T RT A13NM 2007073000108 20070730 00108 NM 2007 7 30 QXEA200701186 1 20070706 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 4 FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX -LEFT WING NR 4 FLAP TRACK UPPER SURFACE OF OUTBOARD LOWER TRACK HAS PITTING AT FORWARD END. REPAIRED IAW RD8/4 -57-988. 2 H 7 2 4T RT A13NM 2007073000109 20070730 00109 SO 2007 7 30 SIMA200720422 1 20070610 A 5315 14521413605 FLOORBEAM EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 819AE 13303 5000 145566 CENTER OMEGA BEAM CORRODED AT FRAME 25. REMOVED CORROSION, CLEANED, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 5 3-00-10 AND 51-40-02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000111 20070730 00111 SO 2007 7 30 SIMA200720424 1 20070620 A 5320 14522178005 SILL EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 720AE 15781 5000 145279 SERVICE DOOR SILL FOUND CORRODED. REMOVED AND REPLACED SILL IAW EMB SRM 51-40-02 AND 51-40-04. RETURNED AIRCRAFT TO SE RVICE. 2 L 7 2 4F RT T00011AT 2007073000112 20070730 00112 SO 2007 7 30 SIMA200720425 1 20070621 A 5310 14522461011 DOUBLER EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 811AE 13526 5000 145529 DOUBLER PLATE AT FRAME 20 CORRODED. REMOVED AND REPLACED DOUBLER IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000113 20070730 00113 SO 2007 7 30 SIMA200720432 1 20070708 A 5320 14522178005 SILL EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 816AE 13301 5000 145552 SERVICE DOOR MIDDLE SILL CORRODED. REMOVED AND REPLACED SILL IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000116 20070730 00116 SO 2007 7 30 SIMA200720423 1 20070620 A 5320 14521700007 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 720AE 13303 5000 145279 LEFT OMEGA BEAM CORRODED BETWEEN 24 AND 25. CUT OUT CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00- 10, FIGURE 202. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000118 20070730 00118 SO 2007 7 30 SIMA200720430 1 20070627 A 5310 14525480603 BEAM EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 722AE 15882 5000 145287 CARGO DOOR LOWER BEAM CORRODED. REMOVED AND REPLACED BEAM IAW EMB SRM 51-40-02, 51-20-03 AND 51-40-06. AIRCRAFT RETURN ED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000119 20070730 00119 SO 2007 7 30 SIMA200720428 1 20070622 A 5310 14521413605 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 720AE 15781 5000 145279 RIGHT OMEGA BEAM CORRODED BETWEEN FRAMES 24 AND 25. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10, FIGURE 203. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000122 20070730 00122 SO 2007 7 30 SIMA200720506 1 20070712 A 5340 14524131009 ATTACH ANGLE EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 858AE 9542 5000 145754 PASSENGER DOOR THRESHOLD ATTACH ANGLE CORRODED. REMOVED AND REPLACED ATTACH ANGLE IAW EMB SRM 51-40-02. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000123 20070730 00123 SO 2007 7 30 SIMA200720508 1 20070702 A 5322 14524014001 SHEAR TIE EMB 135 EMB135LR 3260305 SO ZONE 100 CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 721HS 15764 5000 145283 FOUND SHEAR CLIP AT FRAME 15 CHAFED. REMOVED 26 INCH SECTION, FABRICATED AND INSTALLED NEW SHEAR CLIP IAW EMB IC2007-14 5/04376, DATED JUNE 28, 2007. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000130 20070730 00130 SO 2007 7 30 SIMA200720504 1 20070712 A 5320 14000421001 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 858AE 9542 5000 145754 LEFT OMEGA BEAM CORRODED BETWEEN FRAMES 24 AND 25. REPAIRED OMEGA BEAM IAW EMB SRM 53-00-10. AIRCRAFT RETURNED TO SERV ICE. 2 L 7 2 4F RT T00011AT 2007073000131 20070730 00131 NM 2007 7 30 DHLA200700036 1 20070723 A 3350 BATTERY PACK BOEING 727 7272B7 138407L NM EMERGENCY LIGHTS DISCHARGED A DHLA O OTHER O OTHER NR NOT REPORTED 1 GL 05 770AT 21953 EMERGENCY EXIT LIGHTS (BOTH) WOULD NOT WORK DURING STBY TEST. REMOVED AND REPLACED BATTERIES IAW B727 MM 33-50-71, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2007073000133 20070730 00133 NM 2007 7 30 QXEA200701160 1 20070717 A 2150 78279018 ACM DHAV DHC8 DHC8202 2809007 NM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 369PH 2747 512 PDX - UNABLE TO CONTROL CABIN TEMP AT ALL IN AUTO OR MANUAL. ROSE ON CLIMB TO DUCT TEMP 50 DEGREES. STAYED THERE DESPI TE CHECKLIST UNLATCH PROCEDURES. INVESTIGATED AND FOUND THE COMPRESSOR FAN OF THE ACM FROZEN-NO MOVEMENT. REPLACED THE ACM PER -200 AMM 21-50-11-00-801 AND 21-50-11-400-801. 2 H 7 2 4T RT A13NM 2007073000134 20070730 00134 NM 2007 7 30 07FDEA02499 1 20070717 A 5320 WEB BOEING 727 727227 1384078 NM BS 1165-1166 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 MAIN DECK FLOOR SHEAR WEB AT BS 1165-1166 RBL 48" TO 49" WL 208 HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION AND N DT AREA. REMOVED DAMAGED AREA INSTALLED DOUBLER AND FILLER PER SRM 51-40-02 FIGURE NR 1. REINSTALLED DISTURBED AREA PE R MM 53-20-012-4, SRM 51-30-2 PG 13. MATERIAL VERIFIED PER SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 2007073000135 20070730 00135 NM 2007 7 30 07FDEA02500 1 20070717 A 5320 6519606 WEB BOEING 727 727227 1384078 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 MAIN DECK FLOOR SHEAR WEB AT BS 1165-1166 RBL 48" TO 49" WL 208 HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION AND N DT AREA. REMOVED DAMAGED AREA INSTALLED DOUBLER AND FILLER PER SRM 51-40-02 FIGURE NR 1. REINSTALLED DISTURBED AREA PE R MM 53-20-012-4, SRM 51-30-2 PG 13. MATERIAL VERIFIED PER SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 2007073000136 20070730 00136 NM 2007 7 30 07FDEA02501 1 20070717 A 5712 65C3722112 RIB BOEING 727 727227 1384078 NM ZONE 600 MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 WING RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS EA NR 7-5710-110754. COMPLIED WITH EA NR 7-5710-110754 WING, AD 90-06-0 9: 94-07-08: 98-11-03) RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS. 2 L 7 3 4F A3WE 2007073000137 20070730 00137 NM 2007 7 30 07FDEA02502 1 20070717 A 5712 RIB BOEING 727 727227 1384078 NM ZONE 600 MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 COMPLY WITH EA NR 7-5710-110754 WING, (AD 90-06-09: 94-07-08: 98-11-03) RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS. COM PLIED WITH EA NR 7-5710-110754 WING, (AD 90-06-09: 94-07-08: 98-11-03) RBL 70.5 RIB UPPER REPAIR DEVIATIONS. 2 L 7 3 4F A3WE 2007073000139 20070730 00139 NM 2007 7 30 07FDEA02504 1 20070717 A 5754 SLAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 FOUND CRACK, RIGHT WING SLAT TRACK NR 14 CUTOUT. [07-30-07] REPAIRED AS PER SRM 57-10-00. REPAIR CLASSIFIED AS M AJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007073000140 20070730 00140 NM 2007 7 30 AWXA200700871 1 20070719 A 5320 D53480043205 SILL AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5971972, CORROSION ON R2 DOOR CUT OUT LOWER SILL, BS 2838 / FR 67 + 19.5", -Y1265. REPAIRED R2 DOOR CUT OUT LOWER SILL, BS 2838/FR 67 + 19.5", -Y1265 IAW A319 SRM 53-41-14. 2 L 7 2 4F RT A28NM 2007073000144 20070730 00144 NM 2007 7 30 AWXA200700875 1 20070713 A 5320 D5367227420000 SILL AIRBUS A319 A319132 3930340 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5972146, CORROSION ON AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL PLATE, BS 2350/ FR 58 + 5", -Y705. REPLACED AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL PLATE, BS 2350/FR 58 + 5", -Y705 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007073000145 20070730 00145 NM 2007 7 30 AWXA200700876 1 20070711 A 5753 6546486129 SKIN BOEING 737 7373G7 1384595 NM TE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961981, LEFT WING MID FLAP OUTBOARD END DELAMINATED, WS 184.275, INSIDE PANEL 722D . REPAIRED LEFT WING MID FLAP OUT BOARD END, WS 184.275, INSIDE PANEL 722D IAW B737-300 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 2007073000146 20070730 00146 NM 2007 7 30 AWXA200700877 1 20070707 A 5321 D5367060500100 FLOOR PANEL AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5972146, CORROSION ON FLOOR PANEL 222FF, BS 709/FR 16 - BS 808/FR 20, -Y1292 TO -Y1 732. REPLACED FLOOR PANEL 222FF, BS 709/FR 16 - BS 808/FR 20, -Y1292 TO -Y1732 IAW AWA TASK CARD C1C53302. 2 L 7 2 4F RT A28NM 2007073000148 20070730 00148 NM 2007 7 30 AWXA200700879 1 20070703 A 5755 65464516SP SKIN BOEING 737 7373G7 1384595 NM ZONE 500 DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961251, LEFT WING SPOILER NR 1 LOWER SURFACE HAS AREA OF DISBOND, WS 384 - WS 390 . REPAIRED LEFT WING SPOILER NR 1 LOWER SURFACE, WS 384 - WS 390 IAW B737-300 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 2007072400100 20070724 00100 WP 2007 7 24 AALA20071279 1 20070710 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 441AA 49460 DFW - EMERGENCY LIGHT AT SEAT ROW 21 HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 21. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400130 20070724 00130 NM 2007 7 24 KCSA071241 1 20070719 A 5312 BULKHEAD BOEING 747 7472B4B 138481B NM BS 2360 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 CORROSION IN BS 2360 BULKHEAD HOLE RT142. 2 L 7 4 4F RT A20WE 2007072400153 20070724 00153 NM 2007 7 24 2007UALA02588 1 20070712 A 5330 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU BS 400 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 902UA 25002 EXTERIOR SKIN DENTED AND GOUGED AT STA 400 UPPER FWD CARGO CUTOUT. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKS & ACCOMPL ISHED A DOUBLER/TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007072400168 20070724 00168 NM 2007 7 24 2007UALA02602 1 20070713 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 WALL EEL EXIT SIGN INOP: DOOR 1R. [07-27-07] SECURED CONNECTOR AT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072400187 20070724 00187 NM 2007 7 24 2007UALA02622 1 20070713 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 U-D EMERGENCY LIGHTS ON INTERMITTENTLY IN FLT. EMERGENCY EXIT SWITCH AUTO. [07-27-07] REPLACED BATTERY PACK & BAT TERY TRAY BETWEEN U-D DOORS FWD ASSY. U-D EMER EXIT LTS CK GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072400194 20070724 00194 EU 2007 7 24 2007UALA02628 1 20070714 A 5322 SHEAR TIE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE STR 42L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 436UA 638 SHEAR TIE AT FR 57 STR 42L IS DAMAGED. MAJOR REPAIR ACCOMPLISHED: REMOVED SHEAR TIE. FABRICATED & INSTALLED NEW SHEAR TIE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072400202 20070724 00202 EU 2007 7 24 2007UALA02636 1 20070715 A 5310 STRUCTURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 436UA 638 FWD PIT HAS NUMEROUS CORRODED FASTENERS FROM FRAME 24B THROUGH FRAME 34 AND BETWEEN STR 38R & 38L. AREA WAS REPAIRED 2 L 7 2 4F 4 F RT A28NM E40NE 2007072500011 20070725 00011 NM 2007 7 25 MASA200700088 1 20070210 A 3230 574205A SELECTOR VALVE DHAV DHC8 DHC8202 2809007 NM MLG MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 448YV 13199 448 ASH 7044 COS - CREW HAD A GEAR SHUDDER ONCE THE A/C ARRIVED IN DEN. MX REMOVED AND REPLACED SELECTOR VALVE & RELAYS. 2 H 7 2 4T RT A13NM 2007072500022 20070725 00022 NM 2007 7 25 SWAA073530 1 20070718 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 801 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 801, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007072500055 20070725 00055 NM 2007 7 25 SWAA073539 1 20070718 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 616 S3R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007072500056 20070725 00056 NM 2007 7 25 SWAA073536 1 20070718 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500D S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007072500060 20070725 00060 NM 2007 7 25 SWAA073542 1 20070718 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 685 S2L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007072500071 20070725 00071 NM 2007 7 25 SWAA073533 1 20070718 A 5330 65C381921 SKIN BOEING 737 7373A4 1384585 NM BS 385 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 385, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007072500086 20070725 00086 NM 2007 7 25 SWAA073573 1 20070719 A 5312 6546568 BULKHEAD BOEING 737 7375H4 138449D NM BS 1016 S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 7L. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007072500089 20070725 00089 NM 2007 7 25 KCSA071245 1 20070720 A 5313 STRINGER BOEING 747 7472B4B 138481B NM BS 755 S39R CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA 755 STR 39R HAS CORROSION AT DOME NUT. 2 L 7 4 4F RT A20WE 2007072500090 20070725 00090 NM 2007 7 25 KCSA071246 1 20070720 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 690-720 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 UPPER DECK SEAT TRACK AT LBL 46 IS CORRODED AT STA 690 TO 720. 2 L 7 4 4F RT A20WE 2007072500093 20070725 00093 NM 2007 7 25 MASA200700312 1 20070608 A 3350 CONTROL UNIT DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHT MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 436YV 436 ASH 7106 DEN - EMERGENCY EXIT LIGHTS WILL NOT TURN ON FROM F/A'S PANEL. MX REPLACED THE PANEL CONTROL UNIT. 2 H 7 2 4T RT A13NM 2007072500099 20070725 00099 EA 2007 7 25 TRAX200701007 1 20070716 A 5260 SKIN CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 718EV 10095 ASD INNER SKIN CRACKED AT AFT CORNER UNDER UPPER STEP. 2 L 7 2 4F RT A21EA 2007072500107 20070725 00107 NM 2007 7 25 2007UALA02643 1 20070716 A 5312 PRESSURE PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1681-1697 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 DURING HMV CORROSION DAMAGE REPAIRS WERE ACP AT AFT PRESS DECK BS 1681 BETWEEN RBL 8.75 - 10.25 & BS 1697 RBL 50.25. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072500112 20070725 00112 NM 2007 7 25 2007UALA02648 1 20070713 A 3150 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE UNKNOWN WARNING MESSAGE A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 573UA 26685 STATUS MESSAGE NOSE A-G DISAGREE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072500117 20070725 00117 NM 2007 7 25 2007UALA02652 1 20070715 A 2497 WIRE HARNESS BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 ELECTRICAL BURNING ODOR WITH SMOKE FROM MID GALLEY (416) AFT COUNTER HOTPLATE AREA. C/B FOR HOTPLATE H41 HAS BEEN PULLE D AND BURNING ODOR AND SMOKE HAS DISSIPATED. HOTPLATE WAS NOT HOT BUT AREA AROUND HOTPLATE WAS HOT, POSSIBLE DAMAGED WI RING HARNESS. [08-17-07] REMOVED AND INSPECTED THE BACK OF HOTPLATE FOR ANY BURNED WIRING OR ODOR. NOTHING FOUND. RT PLATE HAD A LOT OF PLASTIC BURNED ON TOP OF IT. CLEANED IT. HOTPLATE INOPERATIVE FOR THREE DAYS. WHEN DOMESTIC AGAIN , OPERATED HOTPLATE. NO ADDITIONAL ODOR. HOT PLATE & AIRPLANE RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072500119 20070725 00119 NM 2007 7 25 2007UALA02654 1 20070714 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 664UA 29236 EEL STRIP AT DOOR 1L AFT LAV INOP. [07-27-07] SECURED LOOSE CONNECTOR, OPS CK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072500132 20070725 00132 2007 7 25 BB07056 4 20070720 A 2310 6225272001 TRANSCEIVER BOEING 767 767201 1385125 NM HF SYSTEM MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 246AY 64812 13 23898 FLIGHT 742, PHL-BCN: FLIGHT RETURNED TO PHL DUE TO AN INOPERATIVE NR 2 HF RADIO. MAINTENANCE REPLACED BOTH HF COUPLERS AND BOTH TRANSCEIVERS. NO FURTHER DIFFICULTIES. 2 L 7 2 4F RT A1NM 2007072500135 20070725 00135 2007 7 25 ABXA070242 4 20070713 A 3421 6227998003 INDICATOR BOEING 767 767200 1385120 NM COCKPIT BURNED A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 798AX 3481 23431 STA: JFK, MAINTENANCE SMELLED ELECTRICAL SMOKE IN COCKPIT. CO-PILOT EADI BLANK. INSPECTED AND FOUND F/O'S EADI DAMAGE D. REMOVED AND REPLACED F/O'S EADI IAW B767 AMM 34-22-34. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2007072500147 20070725 00147 NM 2007 7 25 07FDEA02508 1 20070716 A 5313 STRINGER BOEING 757 7572B7 1384964 NM BS 1660 S26R DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 AFT PIT, BS 1660, S26R DAMAGED. BLENDED DAMAGE ON STRINGER IAW SRM 53-00-03. FOUND TO BE OUT OF LIMITS PER SRM 53-00-0 3, FIG 101. REMOVED DAMAGED SECTION OF STRINGER IAW SRM 53-00-03. FABRICATED REPAIR STRINGER. FABRICATED FILLER IAW S RM 53-00-03, FIG 201. TREATED AND PRIMED STRINGER AND FILLER IAW SRM 51-20-01. INSTALLED STRINGER REPAIR AND FILLER IA W SRM 53-00-03, FIG 201 AND SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007072500162 20070725 00162 NM 2007 7 25 DHL2007741505 1 20070708 A 5313 STRINGER BOEING 727 7272Q9 138448M NM BS 720C S20R DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 FUSELAGE STR 20R HAS DRILLED OFF SCREWS AT BS 720C PLUS 10". CUTOUT DAMAGED AREA OF STRINGER, FABRICATED HAT CHANNELS F ROM BACH1498-143 (2 EA.) 7075-T6 PO NR 7207138 (DIMENSIONS 10" AND 12.5"), STRINGER FILLER FROM BAC 1498-147 PO NR 71781 78 ( DIM 20" LONG) AND 2 EA FILLERS FROM 2024-T3 0.071" PO NR 9005314 (DIMS 11" BY 1" AND 5.5" BY 1") IAW B727 SRM 53-10 -2 FIG 9 AND 53-10-3 FIG 1. TREATED AND PRIMED AREA IAW B727 SRM 51-10-2 AND INSTALLED REPAIR PARTS AT FUSELAGE STRINGE R 20R BS 720C PLUS 10 IAW B727 SRM 53-10-3 FIG 1 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007072500164 20070725 00164 NM 2007 7 25 DHL2007784509 1 20070713 A 5347 CARGO TRACK BOEING 727 727227 1384078 NM BS 850-870 GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 MAIN CARGO NICKS AND GOUGES ON SEAT TRACK, RBL 45, BS 850 TO BS 870. REMOVED SEAT TRACK IAW B727 SRM 51-30-2 AND B727 A MM 53-10-1. FABRICATED NEW SEAT TRACK, MATERIAL USED BAC1520-146-7178T6511, DIM 17 LONG IAW B727 SRM 53-10-2, FIG 7 AND 51-30-5. TREATED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 2007072500166 20070725 00166 NM 2007 7 25 DHL2007784512 1 20070708 A 5330 SKIN BOEING 727 727227 1384078 NM BS 520 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 EXTERNAL FUSELAGE BS 520 AT STR 8R HAS A LIGHTNING BURN. BLENDED OUT AREA OF LIGHTNING STRIKE IAW B727 SRM 53-30-3, FIG 20. MATERIAL LOSS OVER 30 PERCENT AND LIGHTNING STRIKE STILL PRESENT AND OUT OF LIMITS IAW B727 SRM 53-30-1. CUT OUT DAMAGED AREA DIM. 4 BY 2 IAW B727 SRM 53-30-3, FIG.3. HFEC COMPLIED WITH IN CUT OUT AREA, NO CRACKS NOTED IAW B727 NDTM PT.6 51-00-00, FIG.23. FABRICATED DOUBLER REPAIR FROM .050, 2024T3, DIM 11.75 BY 2.25” AND FILLER FROM .040, 2024T3, DIM 4 BY 1.75 IAW B727 SRM 53-30-2, FIG.2 AND 53-30-3, FIG.3. TREATED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 51-10-2, 51 -30-2 AND 53-30-3, FIG 3. 2 L 7 3 4F A3WE 2007072500179 20070725 00179 NM 2007 7 25 QXEA200701127 1 20070709 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 222 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - NR 7 SEAT TRACK HAS PITTING CORROSION AROUND TIE DOWN FASTENER AROUND STATION 222. REPAIRED IAW RD8/4-53-4473 AND RD8/4-53-1102. 2 H 7 2 4T RT A13NM 2007072500184 20070725 00184 NM 2007 7 25 QXEA200701134 1 20070705 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 488 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - MAINTENANCE REQUEST, CORROSION ON FRAME X488.500 BETWEEN STRINGER 25R AND 28R. REPAIRED IAW SRM 51-40-11, 51-2 0-36, 51-20-36. 2 H 7 2 4T RT A13NM 2007072500202 20070725 00202 SO 2007 7 25 SIMA200720409 1 20070603 A 5320 14521713003 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 806AE 13290 5000 145503 LEFT OMEGA BEAM CORRODED AT FRAME 20. REPAIRED OMEGA BEAM IAW EMB SRM 53-00-10. AIRCARFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007072500210 20070725 00210 SO 2007 7 25 SIMA200720418 1 20070608 A 5330 PE11001F4 SKIN EMB 145 EMB145LR 3260212 SO ZONE 200 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 690AE 6752 14500858 LEFT LOWER FUSELAGE SKIN DAMAGED BETWEEN FRAMES 63 AND 65 AT STRINGER 19L, 20L AND 21L. CUT OUT DAMAGED AREA, FABRICATE D AND INSTALLED REPAIR PARTS IAW EMB IC2004-145/03857A, IC2007-145-03878 AND IC2007-145/03912. AIRCRAFT RETURNED TO SER VICE. 2 L 7 2 4T RT T00011AT 2007072500217 20070725 00217 NM 2007 7 25 07FDEA02529 1 20070720 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 MAIN DECK CARGO ALONG CENTER STA 1501 TO 1521 SEAT TRACK AROUND FASTENER HOLE AREA FOUND WITH CORROSION. [07-30-07] CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 6 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007072600006 20070726 00006 2007 7 26 SIMA200720402 4 20070722 A 3416 SH67059305003 CABLE CNDAIR CL600 CL6002C10 1390015 EA ALTIMETER FAILED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 510AE 10567 10105 APPROXIMATELY 1500 FEET RECEIVED GROUND PROXIMITY AURAL DESCENT/SINK WARNING, RETURNED TO DFW. REMOVED AND REPLACED ALT IMETER CABLE IAW CRJ 34-44-00. OPERATIONAL CHECK GOOD - AIRCRAFT RETURNED TO SERVICES. 2 L 7 2 4F RT A21EA 2007072600049 20070726 00049 EA 2007 7 26 SWIA200718515 1 20070603 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 715SK 10179 FS 280 FLOORBEAM IS CRACKED AT LBL9, DISCOVERED AT C-CHECK. NEW BEAM INSTALLED PER REO 670-53-11-047. 2 L 7 2 4F RT A21EA 2007072600050 20070726 00050 EA 2007 7 26 SWIA200718516 1 20070603 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 715SK 10179 COCKPIT FLOOR SUPPORT ANGLE IS CRACKED AT LBL9. (DISCOVERED AT C-CHECK)INSTALLED NEW COCKPIT FLOOR SUPPORT ANGLES IAW C RJ7/9 SRM 51-42-06-001-001-A01. 2 L 7 2 4F RT A21EA 2007072600051 20070726 00051 EA 2007 7 26 SWIA200718517 1 20070603 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 715SK 10179 PAX DOOR AFT WEB IS CRACKED AT UPPER STEP, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLES, DOUBLERS, AND SHIMS PER REO5 2-11-104. 2 L 7 2 4F RT A21EA 2007072600052 20070726 00052 EA 2007 7 26 SWIA200718518 1 20070603 A 5210 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 715SK 10179 PAX DOOR AFT DRAG ANGLE IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLES AND SPLICES PER REO:670-52-11-072. 2 L 7 2 4F RT A21EA 2007072600053 20070726 00053 EA 2007 7 26 SWIA200718519 1 20070603 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 715SK 10179 RIGHT SIDE OF STA 280 WEB IS CORRODED, DISCOVERED AT C-CHECK. REPLACED RIGHT WEB PER REO 670-53-11-05-2. 2 L 7 2 4F RT A21EA 2007072700002 20070727 00002 EU 2007 7 27 07FDEA02560 1 20070719 A 3260 BDM3003 PROXIMITY SENSOR AIRBUS 310 A310324 3930206 EU ZONE 700 FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 801FD 15023 335 539 ON DEPARTURE EDDF RWY 18 LDG GEAR WOULD NOT RETRACT. RETURNED TO LAND 10,000 BELOW MLW. NO FUTHER PROBLEMS. JACK A/C PER MM 07-11-00-0. REMOVED AND REPLACED BOGIE BEAN PROX DETECTOR 8GA PER MM 32-00-00 -4. WHILE REPLACING 8GA PROX DET ECTOR FOUND 12GA PROX DETECTOR ADJUSTMENT NOT WITHIN MM LIMITS. ADJUSTED SAME AS PER MM 32-00-00-4. SWUNG GEAR ON BOT H SYS 1 AND SYS 2 ALL GEARS AND DOORS WORKED NORMAL ON BOTH SYSTEM. 2 L 7 2 4F RT A35EU 2007072700003 20070727 00003 WP 2007 7 27 07FDEA02561 1 20070721 A 5320 AFA390711 CHANNEL DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 398FE 46634 STA 1787 LOWER "J" CHANNEL AT FRAME TO LONGERON CRACKED. FABBED NEW "J" SECTION FROM LONGERON 43R-49R IAW DAC DWG AFA 3907 REV C. ALODINED AND PRIMERED IAW MD/DC 10 SRM 51-21-01 VOL.II. INSTALLATION ON SNRM N00581 (SEE SDR NR 07-2225) 2 L 7 3 4F RT A22WE 2007072700004 20070727 00004 2007 7 27 07FDEA02562 4 20070720 A 2210 AUTOPILOT SYS AIRBUS 310 A310222 3930315 EU UNKNOWN A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 454FE 278 CLOSE R AP 1 AND 2 DO NOT ENGAGE. MTP FAULT REVIEW FOUND FCC 1/ FCC 2/FCU/TORQUE LIMIT RESET A/P 1 AND 2 BOTH FCC AND F CU. PERFORMED AFS/LAND ENGAGE TEST AS PER AMM 22-10-00-5 BOTH A/P CAN BE ENGAGED. A/C RETURNED TO SERVICE. MTP FAULT REVIEW FOUND FCC1/FCC2/FCU/TORQUE LIMITER, RESET A/P1 AND A/P2 BOTH FCC'S AND FCU, PERFORMED AFS/LAND ENGINE TEST AS PER AMM 22-10-00-5, BOTH A/P CAN BE ENGAGED, A/C RTN TO SERVICE. MTP FAULT REVIEW FOUND FCC1/FCC2/FCU/TORQUE LIMITER, RES ET A/P1 AND A/P2 BOTH FCC'S AND FCU, PERFORMED AFS/LAND ENGINE TEST AS PER AMM 22-10-00-5, BOTH A/P CAN BE ENGAGED, A/C RTN TO SERVICE. 2 L 7 2 4F RT A35EU 2007072700005 20070727 00005 EU 2007 7 27 07FDEA02563 1 20070723 A 5754 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU DRUEGER FLAPS CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 HEAVY CORROSION IN KRUEGER FLAP AREA LT ON FITTING P/N: A535-10217-200 RIBLET (P/N A572-41993-200) IS CRACKED. REPAIR W AS PERFORMED BY REPLACEMENT OF FITTING IAW SRM 57-45-11 AND CHANGE RIBLET IAW SRM 57-41-11/FIG 1. 2 L 7 2 4F RT A35EU 2007072700015 20070727 00015 EU 2007 7 27 07FDEA02571 1 20070723 A 5320 STIFFENER AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 657FE 748 FWD CARGO COMPARTMENT FWD SIDE OF FLOORBEAM C23 VERTICAL STIFFENER OUTBD SEAT TRACK 2R HAS .25" LONG CRACK IAW A300-600 AMM 53-13-11-6. CUT OUT DAMAGED AREA PER A300-600 SRM 53-10-15 PG 254. NDT SHOWS NO CRACK REMAINS PER NTM 51-10-08. F ABRICATED REPAIR PARTS PER A300-600 SRM 53-10-15 PG 311/312. INSTALLED REPAIR PER A300-600 SRM 53-10-15. RESTORED SURF ACE PROTECTION USING ALODINE, PRIME, AND TOPCOAT PER A300-600 SRM 51-75-10. 2 L 7 2 4F RT A35EU 2007072700018 20070727 00018 EU 2007 7 27 07FDEA02574 1 20070723 A 5347 A53274005 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 657FE 748 THREE 4.5 SQ INCH AREAS OF CORROSION EXIST AT MDCC SEAT TRACK R-3 BETWEEN FRAMES 40 THRU 45 REF 53-10-16-06 ZONE 200 IAW A300-600 AMM. BLENDED CORROSION IAW A300-600 SRM 51-74-10. CHECKED LIMIT IAW A300-600 SRM 53-10-16, FOUND TO BE OUT O F LIMIT. FAB`D SEAT TRACK IAW DRAWING NR A53832020. REPROTECTED SEAT TRACK IAW A300-600 SRM'S 51-21-10 AND 51-75-10. INSTALLED SEAT TRACK IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007072700019 20070727 00019 EU 2007 7 27 07FDEA02576 1 20070723 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 FWD PIT LEFT SIDE BILGE AREA S53L HAS CORROSION BETWEEN FRAME 35 AND 36. [08-29-07] REMOVED CORROSION IAW A310-200 SR M 51-74-10 PAGE 201. FOUND TO BE OUT OF LIMITS A310-200 SRM 53-14-14. REMOVED STR. 53L FROMFRAME 35 TO 37 IAW A310-200 SRM 51-40-21 PARA. 5. FABRICATED IAW A310-200 SRM 53-10-14 FIG. 201. INSTALLED IAW A310-200 SRM 51-40-21 PARA. 7. L EAK CHECK GOOD IAW A310-200 MM 21-51-00-5. 2 L 7 2 4F RT A35EU 2007072700020 20070727 00020 EU 2007 7 27 07FDEA02577 1 20070723 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 FWD PIT LEFT SIDE BILGE AREA S53L HAS CORROSION BETWEEN FRAME 36 TO FRAME 37. [08-29-07] ALL WORK ACCOMPLISHED ON FED EX N/R N00610. 2 L 7 2 4F RT A35EU 2007072700024 20070727 00024 NM 2007 7 27 HALA0700296 1 20070721 A 8011 70R065 HOUSING BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE STARTER GBOX CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 ETOPS SIGNIFICANT SYSTEM, NR 2 STARTER GEAR BOX HOUSING ASSEMBLY CRACKED. REPLACED NR 2 HOUSING ASSY. LEAK CHECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072700025 20070727 00025 NM 2007 7 27 DU4R2007152 1 20070719 A 5753 113N21051 TORQUE TUBE BOEING BOEING 757 757232 1384965 NM TE FLAPS CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 639DL 000212 23993 FOUND LT I/B FLAP I/B TORQUE TUBE CORRODED. REPAIRED BY REMOVING AND REPLACING TUBE WITH P/N’S 113N2105-1 AND 113N2108- 1 IAW B757 AMM 27-51-05 AND DELTA EA 06-097981-14 REV A. 2 L 7 2 4F RT A2NM 2007072700028 20070727 00028 NM 2007 7 27 DU4R2007155 1 20070719 A 5320 SILL BOEING 757 757232 1384965 NM BS 1390-1440 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 639DL 23993 FOUND AFT CARGO LWR DOOR SILL CORRODED FROM BS 1390 TO BS 1440 S-27R. REPAIRED BY REMOVING DOOR SILL AND INSTALLING P/N 146N8522-52 IAW B757 SRM 51-40-02, 53-60-15, 51-40-04 AND 51-40-06. 2 L 7 2 4F RT A2NM 2007072700030 20070727 00030 NM 2007 7 27 DU4R2007157 1 20070703 A 5321 FLOOR PANEL BOEING 757 757232 1384965 NM BS 1381 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 639DL 23993 FOUND CORRODED AFT DECK PLATE BS 1681.8 FROM LBL 1 TO LBL 14. REPAIRED BY FABRICATING AND INSTALLING REPAIR DOUBLER 6-1 /2 BY 14 FROM 2024-T3 .063 IAW B757 SRM 53-60-51 PG 201/204 AND 51-10-01. 2 L 7 2 4F RT A2NM 2007072700031 20070727 00031 NM 2007 7 27 DU4R2007158 1 20070703 A 5321 FLOOR PANEL BOEING 757 757232 1384965 NM BS 1681 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 639DL 23993 FOUND CORRODED AFT DECK PLATE BS 1681.8 FROM LBL 1 TO LBL 14. REPAIRED BY FABRICATING AND INSTALLING REPAIR DOUBLER 6-1 /2 BY 14 FROM 2024-T3 .063 IAW B757 SRM 53-60-51 PG 201/204 AND 51-10-01. 2 L 7 2 4F RT A2NM 2007072700032 20070727 00032 NM 2007 7 27 DU4R2007160 1 20070716 A 5753 RIB BOEING BOEING 757 757232 1384965 NM TE FLAP CRACKED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 639DL 23993 FOUND LT INBB FLAP MAIN FLAP RIB (3RD FROM I/B END) CRACKED. REPAIRED BY REMOVING RIB AND INSTALLING RIB FABRICATED (ON N/R 25000)16.780 BY 8.550 FROM 7050-T7457 IAW B757 SRM 51-40-02, BOEING DWG NR 113N2352 REV C, AND B757 SRM 51-20-01. 2 L 7 2 4F RT A2NM 2007072700035 20070727 00035 NM 2007 7 27 HALA0700302 1 20070723 A 4900 APU BOEING 767 7673CB 1385187 NM UNKNOWN A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 592HA 33468 ETOPS SIGNIFICANT SYSTEM, APU AUTO SHUTDOWN AFTER START. PERFORMED BITE PROCEDURE ON ECU PER FIM 49-11-00 FIG 103. UND ERSPEED MESSAGE RESET PER FIM 49-11-00. APU OPS NORMAL. NO MESSAGES ON ECU. 2 L 7 2 4F RT A1NM 2007072700036 20070727 00036 NM 2007 7 27 HALA0700303 1 20070721 A 7931 8D1494 PRESSURE SWITCH BOEING 767 7673CB 1385187 NM PWA 4060 PW4060 52119 NE ENGINE OIL MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 592HA 33468 ETOPS SIGNIFICANT SYSTEM, R ENG OIL PRESS LIGHT DID NOT ILLUMINATE ON ENG SHUTDOWN. REMOVED AND REPLACED RIGHT ENGINE L OW OIL PRESSURE SWITCH PER AMM 79-33-01. LEAK AND OPS CHK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072700039 20070727 00039 NM 2007 7 27 HALA0700298 1 20070723 A 8011 S332T00117 STARTER BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE NR 1 MALFUNCTIONED A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 591HA 5919 5919 33423 ETOPS SIGNIFICANT SYSTEM - BTB - WHILE STARTING LT ENG N2 REACHED 23 PERCENT AND THEN DECREASED TO 0. REMOVED AND REPLA CED NR 1 STARTER IAW 80-11-01 AND SERVICED, DRIED MOTORED ENG IAW AMM-71-00-00-201, ALL OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072700040 20070727 00040 NM 2007 7 27 DL764070748 1 20070618 A 2897 CN1156701 WIRE HARNESS BOEING 767 767432ER 1385134 NM FUEL QTY DAMAGED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 832MH 29704 RIGHT MAIN AND TOTAL FUEL QTY BLANKED AFTER ENGINE START. MTC IN PROGRESS. TRANSFERRED TO TIMCO OP 6002 AT HMV1, REPLA CED RT MAIN FUEL T HARNESS IAW B767 MM 28-41-09. PERFORMED FUEL QUANTITY BITE CH IAW B767 MM 28-41-00-715-001. OPS CHE CK GOOD. PERFORMED 1 2 ENGINE START IAW B767-400 PREFLIGHT CHECKLIST. NO DEFECTS NOTED. 2 L 7 2 4F RT A1NM 2007072700041 20070727 00041 NM 2007 7 27 DL738070878 1 20070706 A 3150 UNKNOWN BOEING 737 737832 13844CF NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE UNKNOWN A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 3749D 19384 30490 888402 NR 1 ENG ON CLIMB-OUT 3000-4000FT MSL ENG OIL BYPASS LIGHT ILLUMINATED AND EXTINGUISHED AFTER 30 SEC NO POWER CHANGE. T HEN AFTER 1 MIN OIL BYPASS LIGHT ILLUMINATED EXECUTED QRH PROCEDURE PULLED POWER BACK LIGHT WENT OUT BELOW 70 N1. ALL O THER ENG INDICATIONS NORMAL. RTB LAX , BITE ECC 1 AND 1A FOR FAULTS PER FIM NO MSG-NO FILTER MSG. TROUBLE SHOOT PER FI M 79-05-00-810-817. FOUND NON METALLIC PARTICLES IN AFT SCAVENGE CHIP DETECTOR. REMOVED FOR LAB ANALYSIS. RAN ENG NR 1 TO 70 PERC N1 FOR 10 MIN. REINSPECT CHIP DETECTORS, NO PARTICLES FOUND MCO PLACARD REMOVED. 2 L 7 2 4F 4 F RT A16WE E2GL 2007072700044 20070727 00044 EU 2007 7 27 07FDEA02569 1 20070723 A 5320 ANGLE AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 657FE 748 FWD CARGO COMPARTMENT FWD SIDE OF FLOORBEAM C27 VERTICAL STIFFENER OUTBD SEATRACK 2R HAS .25" LONG CRACK IAW A300-600 AM M 53-13-11-6. REPAIRED FLOORBEAM IN FWD CARGO COMPARTMENT C27 OUTBD SEATRACK 2R IAW A300-600 SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 2007072700046 20070727 00046 EU 2007 7 27 07FDEA02583 1 20070723 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 ALC STR 50 L CORRODED BETWEEN FR 63 AND FR 64. 09-04-07 REMOVED CORROSION FROM STRINGER FOUND TO BE OUT OF LIMITS, R EMOVED STRINGER 50L FROM FRAME 62 TO 65, RECEIVED NEW STRINGER , LOCATED DRILLED TREATED PRIMED AND INSTALLED NEW ST RINGER. IAW 51-40-11, 53-17-14, 51-40-21, DAN50-04, 53-21-14 AND 53- 10-14 2 L 7 2 4F RT A35EU 2007072700048 20070727 00048 EU 2007 7 27 07FDEA02585 1 20070723 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT PIT FRAME 67, STRINGER 54R CORRODED. REMOVED AND REPLACED STRINGER 54R FR 67 IAW A310 SRM 53-10-14 PG 203/204 FIG 2 01. 2 L 7 2 4F RT A35EU 2007072700049 20070727 00049 EU 2007 7 27 07FDEA02586 1 20070723 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT PIT STRINGER 52L BETWEEN FRAMES 61 AND 62 CORROSION IN WORK. [08-06-07] REMOVED AND REPLACED STRINGER 52L BETWEE N FR 61-63 IAW A310 SRM 53-10-14 PAGE 203/204. 2 L 7 2 4F RT A35EU 2007072700050 20070727 00050 EU 2007 7 27 07FDEA02587 1 20070723 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 ALC STR 50 L CORRODED BETWEEN FR 58 AND FR 60. [08-14-07] REPLACED STRINGER IAW A310 SRM 53-10-14, FIG 201, PG 203/ 204 2 L 7 2 4F RT A35EU 2007072700051 20070727 00051 EU 2007 7 27 07FDEA02588 1 20070723 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT PIT FR 67 STRINGER 53 L CORRODED. [08-07-07] REMOVED CORROSION REF A310 SRM 51-74-10, OUT OF LIMITS. ORG MAT THICK NESS .078, MAT LOSS .028 REMANING .050. REMOVED AND FABRICATED NEW STRINGER AND SPLICE PER A310 SRM 53-10-14. ALODIN ED, PRIMED AND TOPCOATED REF A310 SRM 51-21-10 AND 51-23-10. INSTALLED NEW STRINGER AND SPLICE REF A310 SRM 53-11-14, AND 51-40-21 2 L 7 2 4F RT A35EU 2007072700054 20070727 00054 EU 2007 7 27 TRBA2007056 1 20070725 A 3231 1005383400 SELECTOR VALVE AEROSP ATR72 ATR72212 8680945 EU MLG FAILED A TRBA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 29 414WF 414 AFTER T/O AND GEAR HANDLE SELECTED UP, L/G TOOK APPROXIMATELY 1.5 MIN TO FULLY RETRACT. BOTH RED AND GREEN INDICATION O N PANEL. L/G WAS CYCLED AS PER MOC REQUEST. UPON SECOND RETRACTION, SAME RESULTS OCCURED. REMOVED AND REPLACED L/G SE LECTOR VALVE IAW JIC NR 32-31-51 RAI 10000. L/G INDICATION ALL NORMAL. 2 H 7 2 4T RT A53EU 2007072700055 20070727 00055 GL 2007 7 27 02541 1 20070723 A 2420 646843 ALTERNATOR CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO HARTZL HCJ3Y PHCJ3YF1 GL ENGINE OPEN E J4PA O OTHER J WARNING INDICATION DE DESCENT 1 SO 13 675CD 89 1708 688944 FP3777B DURING DESCENT INTO KPDK FROM KJZI, WITH ONE PASSENGER THE NR 1 ALT WARNING LIGHT COME ON. TRIED RESETTING THE SYSTEM D ID NOT HELP. PERFORMED LOAD SHEDDING AND LANDED WITHOUT INCIDENT. FOUND NR 1 ALT HAD AN OPEN FIELD IN THE ALTERNATOR I TSELF. 1 L 7 1 3O 3 O NT A00009CH E3SO 5 C P36EA 2007072700056 20070727 00056 EU 2007 7 27 07FDEA02589 1 20070723 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 BULK CARGO BAY STR 55 L CORRODED BETWEEN FR 64 AND 65. REMOVED CORROSION IAW A310 SRM 51-74-10 STRINGER 55L CONNECTING SECTION AT FR 65 OUT OF LIMITS IAW A 310 SRM 53-17-14 PG101. REMOVED CONNECTING SECTION IAW A310 51-40-21 FIG 8 INS TALLED NEW CONNECTING SECTION PN A5397422820090 IAW A310 SRM 53- 10-14 FIG 201 2 L 7 2 4F RT A35EU 2007072700057 20070727 00057 EU 2007 7 27 07FDEA02590 1 20070723 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT PIT STRINGER 54 R AT FRAME 70 CORRODED. [08-20-07] REMOVED AND REPLACED STRINGER 54R AT FR 70 PER A310 SRM 53-10-1 4 PG 203/204 FIG 201 2 L 7 2 4F RT A35EU 2007072700058 20070727 00058 EU 2007 7 27 07FDEA02591 1 20070724 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 ALC STRINGER 52 R CORRODED BETWEEN FR 58 AND FR 61. [08-06-07] REMOVED AND REPLACED STRINGER SECTION FR 59 TO FR 61 S TR 52 R IAW A310 SRM 53-10- 14 PG 203 2 L 7 2 4F RT A35EU 2007072700059 20070727 00059 EU 2007 7 27 07FDEA02592 1 20070724 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 ALC STR 55 L CORRODED BETWEEN FR 59 AND FR 61 IN WORK. ALL WORK WAS ACCOMPLISHED ON THIS N/R. CUT OUT STRINGER 55L B ETWEEN FRAME 58 AND FRAME 63 IAW A310 SRM 53-10-44 FIG 201. FABRICATED STRINGERCOUPLINGS IAW A310 SRM 53-10-14 FIG 201 , ALODINED, PRIMED AND PAINTED REPAIR PARTS IAW A310 SRM 51-21-10 PAR3, PART MARKED INSTALLED STRINGER 55L IAW A310 SRM 51-40-21 PARA 6 AND7, INSTALLED SHEAR TIE FRAME 59,60,61 IAW A310 SRM 51-40-21PARA 6 AND 7. 2 L 7 2 4F RT A35EU 2007072700061 20070727 00061 EU 2007 7 27 07FDEA02594 1 20070724 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 ALC STR 56 R CORRODED BETWEEN FR 58 AND FR 61. REMOVED CORROSION IAW FEDEX A310 51-74-10 PG 204, FOUND TO BE OUT OF LIM ITS IAW FEDEX SRM 51-74-10, REMOVED DAMGED PORTIONS OF STRINGER 56R FROM FROM FR58- FR64 IAW FEDEX SRM A310 SRM 51-40 -21 PG 23 AND 24, FABRICATED AND INSTALLED REPAIR PARTS FOR STRINGER 56R FROM FRAME 58 TO FRAME 64 IAW FEDEX SRM A310 SRM 53-10-14 2 L 7 2 4F RT A35EU 2007072700062 20070727 00062 EU 2007 7 27 07FDEA02596 1 20070724 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 ALC UNDER FLOOR CORROSION ON STR 49 L BETWEEN FR 64 AND 65 IN WORK. 09-04-07 REMOVED CORRODED STRINGER IAW A310 SRM 51-40-21 PG 23, LOCATED DRILLED AND INSTALLED STRINGER AND SPLICE IAW A310 SRM 53-10-14 PG 201, 51-40-40. 2 L 7 2 4F RT A35EU 2007072700063 20070727 00063 EU 2007 7 27 07FDEA02597 1 20070724 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 ALC STR 56L CORRODED BETWEEN FR 63 AND FR 64 IN WORK. 09-04-07 FOUND TO BE OUT OF LIMITS IAW FED EX A310 SRM 51-74 1-10. REMOVED DAMAGED SECTION OF STRINGER 56L FROM FR 58- 64 IAW FED EX A310 SRM 51-40-21 PG 23-24. FABRICATED AND INST ALLED REPAIR PARTS FOR STR 56L FROM FR 58-64 IAW FED EX A310 SRM 53-10-14 MAJOR REPAIR 2 L 7 2 4F RT A35EU 2007072700064 20070727 00064 EU 2007 7 27 07FDEA02598 1 20070724 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 ALC STR 51 L CORRODED BETWEEN FR 58 AND FR 61 IN WORK. 09-04-07 FABRICATED NEW STRINGER SECTION IAW SRM 51-40-44, LO CATED DRILLED AND TREATED PRIMED AND PAINTED REPAIR PARTS IAW A310 SRM 51-40-44, 51-21-10,51-23-10, INSTALLED STRINGER 51L AND SPLICE IAW A310 SRM 51-40-21 AND 53-10-14 FIG 210. 2 L 7 2 4F RT A35EU 2007072700065 20070727 00065 EU 2007 7 27 07FDEA02599 1 20070724 A 5330 A53778736202 SKIN PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 CORROSION ON SKIN PANEL AROUND DME 2 ANTENNA, BETWEEN FRAME 30 -31, P54 LT/P54 RT. REPAIR PERFORMED BY CORROSION REMOVA L AND INSTALLING AN EXTERNAL DOUBLER BASED ON SRM 53-10-12 / FIG 225, COVERED BY EA 6-5314-106493. 2 L 7 2 4F RT A35EU 2007072700070 20070727 00070 WP 2007 7 27 NWAA072569864 1 20070722 A 2161 CONTROLLER DOUG DC9 DC951 3022051 WP CABIN TEMP MALFUNCTIONED A NWAA A UNSCHED LANDING M B J OVER TEMP SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 01 773NC 47775 SHORTLY AFTER TAKEOFF, THE FLIGHT ATTENDANT REPORTED VERY HOT TEMPERATURES AND SMOKE IN THE CABIN. THE FLIGHT CREW COU LD SMELL SMOKE AND OIL FUMES ALSO. NO MENTION OF COM COMPLIANCE BUT CREW DID SAY THAT ALL PACK INDICATIONS WERE NORMAL. THE FLIGHT RETURNED TO A SUCCESSFUL BUT OVERWEIGHT LANDING BACK AT LAN AND WAS ABLE TO TAXI TO THE GATE UNDER ITS OWN POWER. MAINTENANCE DID FIND OIL RESIDUE IN THE LEFT COALESCER BAG AND REPLACED IT. SOURCE OF OIL WAS NOT IDENTIFIED. COMPLETE PACK BURNOUT PROCEDURES WERE ACCOMPLISHED AND THE COCKPIT TEMPERATURE CONTROLLER WAS REPLACED. THE AIRCRAFT HA S RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007072700073 20070727 00073 NM 2007 7 27 07FDEA02604 1 20070725 A 5347 BAC1520792 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 UPPER MAIN DECK SEAT TRACK HAS CORROSION AT BL- 0, STA 930 LT SEAT TRACK FLANGE. REMOVED OLD SEAT TRACK, FABRICATED NEW TRACK. INSTALLED NEW TRACK AT BS 930 BL 0, REF SRM 51-30-02. 2 L 7 3 4F RT A3WE 2007072700076 20070727 00076 WP 2007 7 27 NWAA072529954 1 20070718 A 2131 CONTROLLER DOUG DC9 DC931 3022065 WP CABIN PRESSURE MALFUNCTIONED A NWAA G B A O2 MASK DEPLOYED EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 921RW 47164 WHILE MANEUVERING THROUGH A LINE OF THUNDERSTORMS AND CLEARED TO FL340 THE FLIGHT CREW NOTICED THE RED "CABIN PRESS" WAR NING LIGHT ILLUMINATED AND THAT THE CABIN ALTITUDE WAS CLIMBING. COM PROCEDURES WERE COMPLIED WITH INCLUDING THE RED BO RDER CHECKLIST AND AN EMERGENCY DESCENT WAS PERFORMED. THE PASSENGER MASK DID DEPLOY AUTOMATICALLY BUT THE VESSEL DID N OT EXPERIENCE A RAPID DECOMPRESSION. THE CREW DIVERTED TO A NORMAL AND SAFE LANDING AT IND. MAINTENANCE DID PERFORM BI TE BUT NO FAULT RESULTED. BOTH CABIN PRESSURE CONTROLLERS, TEMPERATURE CONTROL VALVES, AND COALESCER BAGS WERE ALL REPL ACED. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007072700077 20070727 00077 WP 2007 7 27 07FDEA01675 1 20070430 A 5330 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 309FE 48298 AIRCRAFT HAS DAMAGE TO SKIN P/N ACA3109-1 AT STA 603 BETWEEN LONGERONS 47 AND 48 AND P/N ACA3039-513 CLIP AND NCA 6313-1 7 LONGERON 47, AS A RESULT OF A FIRE OF THE EXTERNAL POWER WIRING. EXTERNAL POWER WIRING ALSO HAS DAMAGE. REF N/R 004 , CUT OUT DAMAGED AREA AND FABRICATED REPAIR PER SRM 53-20-00. REF N/R 005, CUT OUT DAMAGED STRINGER DRILLED NEW STRING ER PER SRM 51-00-01. REF N/R 006, DRILLED NEW CLIP PER SRM 51-00-01. REF N/R 007. FABRICATED AND INSTALLED NEW STRING ER PER SRM 53-10-00. REF N/R 008, FABRICATED AND INSTALLED NEW BRACKET PER SERVICE BULLETIN 24-11 PG 7. REF. N/R 009, CLEANED POWER FEEDER CABLES PER SMP ISSUED EA NR 8-2440-112390. REF W/O 37161 2 L 7 3 4F RT A22WE 2007072700082 20070727 00082 EU 2007 7 27 07FDEA02536 1 20070720 A 5330 SEE4A SKIN AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 CORROSION SPOTS ON FUSELAGE SKIN PANEL AT C39, P55 LT (P/N SPLICE A538-12119-200, SKIN PANEL A538-10775-200). REPAIR PE RFORMED BY BLEND OUT THE CORROSION AND INSTALLING OVERSIZE FASTENER IAW EA 6-5315-106500 AND RAS 053011/010/2007 ISS A. 2 L 7 2 4F RT A35EU 2007072700085 20070727 00085 NM 2007 7 27 07FDEA02539 1 20070720 A 5313 652241919 STRINGER BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LT WW ABOVE UPLOCK TORQUE TUBE, STR 18 HAS CORROSION ON UPPER SURFACE BETWEEN STA 930 AND 940. REMOVED CORROSION AT L T W/W, STR 18 ON UPPER SURFACE BETWEEN STA 930 TO 940. FOUND OUT OF LIMITS IAW B727 SRM 53-10-1 PG 2A. CUTOUT DAMAGED AREA. FABRICATED REPAIR DOUBLER AND FILLER IAW B727 SRM 51-40-2 PG 1. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER IAW B727SRM 51-10-2, 51-40-2 51-30-2. 2 L 7 3 4F RT A3WE 2007072700086 20070727 00086 NM 2007 7 27 07FDEA02540 1 20070720 A 5312 65255505 BULKHEAD BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LOWER EDGE OF RIGHT WHEEL WELL AFT BULKHEAD HAS CORROSION BETWEEN FRAME AND FAIRING. CORROSION STARTS AT RBL 11 AND CON TINUES OUTBOARD. THIS AREA IS LOCATED AT THE FWD EDGE OF THE WING TO BODY FAIRING 3622. FABRICATED NEW FRAME ASSY IAW DWG 65-25550 ON LOWER EDGE OF RIGHT WHEEL WELL, AFT BULKHEAD, TREATED, PRIMED AND INSTALLED IAW B727 SRM 51-10-2, 51-30- 2. 2 L 7 3 4F RT A3WE 2007072700088 20070727 00088 EU 2007 7 27 07FDEA02542 1 20070720 A 5320 A53773644202 FITTING AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CORNER FITTING C 27 LT CORRODED REPAIR PERFORMED BY REPLACING THE PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007072700089 20070727 00089 NM 2007 7 27 07FDEA02543 1 20070720 A 5311 6520827 FRAME BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD LWR. CARGO PIT BILGE, FRAME HAS CORROSION ON FWD SIDE ON SKIN ATTACH FLANGE AND UP VERTICAL SIDE 2", STA 720E BETWEE N STR 27R AND 28R. REMOVED DAMAGED SECTION BS 720E BETWEEN STR 27R - 28R. FABRICATED REPAIR PART, SHEAR TIE PER SRM 53 -10-4 PG 43-45. 2 L 7 3 4F RT A3WE 2007072700090 20070727 00090 EU 2007 7 27 07FDEA02544 1 20070720 A 5320 A53610996 STIFFENER AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 CRACK FINDING (4MM) AT FRAME C12A LT MODIFATION IAW SB A300-53-6137 PERFORMED, APPROVED BY EO 6-5340-7-5002 PT 5. 2 L 7 2 4F RT A35EU 2007072700091 20070727 00091 EU 2007 7 27 07FDEA02545 1 20070720 A 5313 A53611667200 STRINGER SPLICE AIRBUS 300 A300B4605R 3930308 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 MISDRILLED HOLE IN STRINGER SPLICE AT C19, P43 RT REPAIR PERFORMED BY REPLACING THE PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007072700093 20070727 00093 NM 2007 7 27 07FDEA02547 1 20070720 A 5347 6523638 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 CABIN BL 0 SEAT TRACK LEFT FLANGE UPPER SURFACE HAS CORROSION BETWEEN BS 500 AND 580. REMOVED SEAT TRACK AND FABRICATED NEW TRACK FROM BAC1520-792. TREATED PRIMED AND INSTALLED SEAT TRACK REF SRM 51-30-02 P1. 2 L 7 3 4F RT A3WE 2007072700094 20070727 00094 EU 2007 7 27 07FDEA02548 1 20070720 A 5310 A53973100200 BEAM AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 CORROSION ON BEAM BULK CARGO DOOR CUT OUT REPAIR PERFORMED BY REPLACING THE PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007072700095 20070727 00095 NM 2007 7 27 07FDEA02549 1 20070720 A 5311 6556114 FRAME BOEING 727 727233 138408A NM ZONE 100 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 REWORK: BUCKLE IN BODY FRAME SHEAR TIE WAS STRAIGHTENED USING SRM 51-40-1 (FUSELAGE SKIN) REMOVED SHEAR TIE, FAB NEW S HEAR TIE AND 2 FILLERS, AND INSTALLED AT STA 720B, STRINGER 28 TO STRINGER 28 WL 148 IAW BOEING 727 SRM 53-10-4, PGS 46, 47, 48, 49. 2 L 7 3 4F RT A3WE 2007072700096 20070727 00096 NM 2007 7 27 07FDEA02550 1 20070720 A 5320 6559896 INTERCOSTAL BOEING 727 727233 138408A NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 MAIN CABIN FLOOR STRUCTURE STA 560 TO STA 580 BL 0 INTERCOSTAL WEB UPPER FLANGE HAS 21 HOLES THAT WERE PREVIOUSLY ELONGA TED. REMOVED INTERCOSTAL WEB AND T-ANGLES. FABRICATED NEW INTERCOSTAL AND HEAT TREATED. SEE WORK ORDER 00036352. FAB RICATED T-ANGLE AS PER DRAWING 65-59896. INSTALLED AS PER 51-30-2. 2 L 7 3 4F RT A3WE 2007072700097 20070727 00097 NM 2007 7 27 07FDEA02551 1 20070720 A 5347 6519602 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 RBL 24 SEAT TRACK BETWEEN STA 804 TO 848 HAS LIGHT CORROSION AROUND NUT PLATE HOLES ON UPPER AND LWR FLANGE SURFACES (DO T 15) REPLACED T-CAP IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007072700099 20070727 00099 NM 2007 7 27 07FDEA02553 1 20070720 A 5315 6520827218 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 CABIN MAIN DECK FLOORBEAM AT BS 720 RBL 48" HAS A DOUBLE DRILLED HOLE IN FWD FLANGE OF THE UPPER CHORD. REMOVED DAMAG E AREA'S. FAB 2EA REPAIR ANGLES FAB 3EA SHIMS, FAB CHORD, FAB WEB, FAB T-CHORD PN 65-80690 IAW B727 SRM 51-30-2 FIG NR 8. INSTALLED FAB PARTS AND FASTENERS IAW B727 SRM 51-30-2 PG 5 ALSO REF SRM 53-10-8. 2 L 7 3 4F RT A3WE 2007072700103 20070727 00103 WP 2007 7 27 07FDEA02556 1 20070720 A 5230 VENT DOUG DC10 DC1030F 3023504 WP CARGO DOOR MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 304FE 46992 PDIS: RCVD CABIN RATE ON DEPARTURE. A/C WOULD NOT PRESSURIZE. CHANGED CONTROLLER TO MANUAL NO CHANGE. OUTFLOW VALVE INDICATED CLOSED ENTIRE TIME ON SYNOPTIC PAGE AND ON PNL. ON SYNOPTIC "CLOSED" INDICATOR IN AMBER BUT VALVE INDICATOR WAS CLOSED. RETURNED TO MEM. FOUND HARDWARE MISSING IN CENTER CARGO DOOR VENT DOOR LINKAGE. REPLACED HARDWARE IAW MD- 10-30 SMP. OPS CHECKED DOOR IAW MD-10-30 MM 52-32-00-5. PRESSURIZED A/C PER MD-10-30 MM 21-00-00-5 CHECKED GOOD. 2 L 7 3 4F RT A22WE 2007072700105 20070727 00105 WP 2007 7 27 07FDEA02558 1 20070720 A 5312 AEA00181 BULKHEAD DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CLG WHEEL WELL CAVITY, CORROSION ON BULKHEAD LOWER CIRCUMFERENCIAL ANGLE AT STA 1521 LONGERON 50R TO 49R. REMOVED CORRO SION ON T-CHORD IAW MD/DC10 SRM 51-21-01 VOL II PAGE 1, DAC DWG AEA 0018,ORIG. THICKNESS .200 REMAINING THICKNESS .177, .023 REMOVED. REMOVAL LIMITS OF T- CHORD ARE GOOD IAW EA 8-5310-112948. REMOVED AND REPLACED 4 END FITTINGS IAW MD/DC1 0 SRM 51-33-01 PAGE 1 VOL II AN 51-35-01 PGE 1 VOLII. 2 L 7 3 4F RT A22WE 2007072700110 20070727 00110 SO 2007 7 27 SIMA200720415 1 20070608 A 5320 14521700007 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 855AE 9744 5000 145747 LEFT OMEGA BEAM CORRODED AT FRAME 27. CUT OUT DAMAGE, FABRICATED AND INSTALLED REAPAIR PARTS IAW EMB SRM 53-00-10, FIGU RE 202. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT T00011AT 2007072700112 20070727 00112 SO 2007 7 27 SIMA200720401 1 20070720 A 3231 22250100003 SOLENOID EMB 135 EMB135KL 3260302 SO ZONE 700 FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 823AE 12992 145582 NOISE AND RUMBLE FROM NOSE LANDING GEAR AREA, EICAS INDICATED GEAR UP POSITIONS, RETURNED TO LGA. FOUND NOSE LANDING GE AR DOOR WOULD NOT CLOSE AFTER RETRACTION. REMOVED AND REPLACED NOSE GEAR DOOR SOLENOID VALVE IAW EMB AMM 32-33-02 AND E XTENSION AND RETRACTION CHECKS IAW EMB AMM 32-30-00 WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007072700113 20070727 00113 SO 2007 7 27 SIMA200720110 1 20070601 A 5710 STRUCTURE EMB 135 EMB135LR 3260305 SO ZONE 500 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 716AE 15935 5000 145264 LEFT NUMBER ONE LEADING EDGE DENTED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 57-40-00. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007072700114 20070727 00114 NM 2007 7 27 QXEA200701187 1 20070710 A 5330 SUPPORT BEAM DHAV DHC8 DHC8202 2809007 NM BS 202 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - CORROSION AT STATION 202.75 STRINGER 31L ON SEAT TRACK SUPPORT BEAM AROUND ATTACH BOLT. REPAIRED IAW SRM 51-20 -26, 51-40-11. 2 H 7 2 4T RT A13NM 2007072700119 20070727 00119 NM 2007 7 27 QXEA200701166 1 20070718 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM INOPERATIVE A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 354PH 498 SEA FLIGHT NR 2064, NR 1 ENGINE START SMOKE MASTER WARNING ILLUMINATED. NR 2 SMOKE DETECTOR INOP. PLACED ON MEL 372270. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007073000001 20070730 00001 SO 2007 7 30 SIMA200720706 1 20070627 A 5315 14521700007 FLOORBEAM EMB 135 EMB135LR 3260305 SO ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 722AE 15852 5000 145287 LEFT OMEGA BEAM AT FRAME 21 CORRODED. BLENDED OUT CORROSION AND RESTORE FINISH IAW EMB SRM 51-40-02, 51-20-03, 51-40-06 AND EMB IC2007-145/04209, DATED JUNE 21, 2007. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000002 20070730 00002 SO 2007 7 30 SIMA200720703 1 20070710 A 5320 14521713005 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 723AE 13150 5000 145288 LEFT OMEGA BEAM AT FRAME 20 CORRODED. REPAIRED BEAM IAW EMB SRM 53-00-10 AND 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000003 20070730 00003 WP 2007 7 30 IXXA07SMN168S 1 20070630 A 5313 LONGERON DOUG DC8 DC873F 302199F WP ZONE 100 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT FLIGHT STATION 680 LONGERON 33 RIGHT DOUBLER, RIGHT FORWARD FUSELAGE AT WING TO BODY FAIRING ATTACH SCREWS. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTI ON. NO CRACKS OR CORROSION FOUND. FABRICATED NEW SKINS EXTERNAL DOUBLER AND INTERNAL DOUBLER. CLEANED, TREATED AND PR IMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACE. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW FAA FORM 8 110-3 DATED 07-05-07 SEMAN DRAWING ED 4572 DATED 06-27-07, DC8 SRM 51-1-20D, SRM 51-3-0, NDT SPM PART 06-10-01-001, FORM SMN 242-2,DC8 SRM 51-1-8B,DC8 SRM 51-1-11, DC8 SRM 51-1-21, AND SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007073000006 20070730 00006 NM 2007 7 30 AWXA200700903 1 20070718 A 5320 146N539139 FLOOR SUPPORT BOEING 757 757225 1384959 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - NR 5998957, CORROSION ON AFT CARGO COMPARTMENT DOOR SILL FLOOR SUPPORT "Z" ANGLE BS 13 80 - BS 1440, RBL 22, S27R, WL 156.80. REPLACED AFT CARGO COMPARTMENT DOOR SILL FLOOR SUPPORT "Z" ANGLE BS 1380 - BS 14 40, RBL 22, S27R, WL 156.80 IAW 757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007073000008 20070730 00008 NM 2007 7 30 AWXA200700905 1 20070628 A 5320 146N852230 THRESHOLD BOEING 757 757225 1384959 NM BS 1380-1440 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - NR 5978998, CORROSION ON AFT CARGO COMPARTMENT DOOR THRESHOLD "T" CAP, BS 1380 - BS 14 40, RBL 22, S27R, WL 156.80. REPLACED AFT CARGO COMPARTMENT DOOR THRESHOLD "T" CAP, BS 1380 - BS 1440, RBL 22, S27R, W L 156.80 IAW 757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007073000009 20070730 00009 NM 2007 7 30 AWXA200700906 1 20070726 A 5313 143N83377 STRINGER BOEING 757 757225 1384959 NM BS 655 S16L CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - NR 5961743, CRACKED STRINGER, BS 655, S16L. REPAIRED STRINGER, BS 655, S16L IAW USAIR WAYS EA120101. 2 L 7 2 4F RT A2NM 2007073000011 20070730 00011 NM 2007 7 30 AWXA200700908 1 20070702 A 5310 65458715 DOOR FRAME BOEING 737 7373G7 1384595 NM BS 328 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5981344 AND 5981345, R1 DOOR AFT FRAME CRACKED, BS 328, WL 250 AT THE 3RD AND 4TH S TOP FITTING. REPAIRED R1 DOOR AFT FRAME, BS 328, WL 250 AT THE 3RD AND 4TH STOP FITTING IAW USAIRWAYS EA120112. 2 L 7 2 4F RT A16WE 2007073000013 20070730 00013 NM 2007 7 30 07FDEA02622 1 20070726 A 5315 BAC14902773 FLOORBEAM BOEING 727 727233 138408A NM BS 643 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD CARGO AREA, STA 643 AT STR 28R ABOUT RBL 12, FLOOR SUPPORT CORRODED UNDER NUT PLATE. REMOVED CORROSION BY CUTTING O UT DAMAGED AREA, SRM 51-40 -4 PG 1. FABRICATED REPAIR PARTS SRM 51-40-4 PG 1-5. DRILLED FASTENER HOLES SRM 51-40-4 AND 51-30-2 PG 1- 12. TREATED AND PRIMED REPAIR PARTS SRM 51-10-2 PG 1. INSTALLED REPAIR PARTS SRM 51-40-4, PG 1-5. 2 L 7 3 4F RT A3WE 2007073000015 20070730 00015 NM 2007 7 30 07FDEA02624 1 20070726 A 5754 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 603FE 48459 RIGHT WING, NR 1 LEADING EDGE SLAT INBOARD EDGE FILLET ASSEMBLY ALIGNMENT PIN HOLE FOUND CRACK. [08-17-07] REPAIR CA RRIED OUT AS PER FEDEX EA 1-5710-114770, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007073000018 20070730 00018 NM 2007 7 30 07FDEA02627 1 20070726 A 5330 6554577 SKIN BOEING 727 727233 138408A NM ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT LWR EXTERNAL BELLY SKIN HAS NUMEROUS NICKS, FROM STA 950D BACK TO 1050, STR 26L TO 26R BLENDED BELLY SKINS FOR NICKS AND REMOVED CORROSION, SRM 51-10-1, ORIGINAL METAL .075", METAL REMOVED .010 AND METAL REMAINING .065" THIS IS CLASSIFI ED AS A MINOR REPAIR. TREATED AREA, SRM 51-20-21-7. 2 L 7 3 4F RT A3WE 2007073000021 20070730 00021 EU 2007 7 30 07FDEA02630 1 20070726 A 5347 60224577075T7 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 653FE 736 FUSELAGE MAIN DECK SEAT TRACK 2L GOUGED ON I/B FLANGE, AROUND 6 FASTENER HOLES BETWEEN FRAMES 47-51 (ZONE 240) REF A300- 600 SRM 51-10-00 TOTAL AREA GOUGED 6 INCHES APPROX. BY .010 DEEP. BLENDED DAMAGE PER A300-600 SRM 51-73-10 AND FOUND T O BE OUT OF LIMITS PER A300-600 SRM 53-10-16 PB 101. REMOVED DAMAGED SEAT TRACK SECTION PER A300-600 SRM 51-72-10. FAB RICATED NEW SEAT TRACK SECTION PER A300-600 SRM 53-15-16 AND DRAWING A53812915. ALODINED, PRIMED AND TOP COATED SEAT TRACK SECTION PER A300-600 SRM 51-21-10 AND 51-75-10. INSTALLED SEAT TRACK SECTION ASSY PER A300-600 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007073000022 20070730 00022 EU 2007 7 30 07FDEA02631 1 20070726 A 5347 60224577075T76 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 653FE 736 COURIER AREA FR 16A- FR 18 SEAT TRACK 3L 20 SQ IN CORROSION REF A300-600 AMM 53-12-00-6 ZONE 230. REMOVED CORROSION ON L3 SEAT TRACK. WENT OUT OF LIMITS IAW A300-600 SRM 53-10-16. REPAIR SEAT TRACK IAW A300-600 SRM 53-12-16. PRIMED AND TREATED PARTS IAW A300-600 SRM 51-75-10. INSTALLED REPAIR IAW A300-600 SRM 53-12-16 FIG 201. 2 L 7 2 4F RT A35EU 2007073000026 20070730 00026 NM 2007 7 30 07FDEA02613 1 20070725 A 5720 65217963 FAIRING BOEING 727 727233 138408A NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 RT WING OB TE NR 8 JACKSCREW FAIRING, CRACK COMING OUT OF FASTENER HOLE AT FWD END. REMOVED DAMAGE AREA REF SRM 57-20-4 FIG 1 PG 5. FAB`D REPAIR PARTS REF SRM 51-30- 05 AND 57-20-4 FIG, 1 PG 5. INSTALLED REPAIR PARTS REF SRM 51-30-02 PG 1 AND REF SRM 57-20-04 FIG 1 PG 5. VERIFIED METAL AS 6061-T4 .050" 2 L 7 3 4F RT A3WE 2007073000030 20070730 00030 EU 2007 7 30 07FDEA02617 1 20070710 A 5414 A54611752504 PANEL AIRBUS 310 A310222 3930315 EU ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 PYLON NR 2, RIB 8 LT WITH CRACK AT UPPER AREA. IT WAS REPAIRED IN ACCORDANCE WITH SRM 54-51-31 FIG 201. 2 L 7 2 4F RT A35EU 2007073000032 20070730 00032 EU 2007 7 30 07FDEA02619 1 20070629 A 5315 A53781300202 FLOORBEAM AIRBUS 310 A310222 3930315 EU BS 1499 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 FWD CARGO COMPARTMENT, CABIN FLOOR CROSS-BEAM CRACKED AT FR21, BETWEEN Y-450 AND Y-953. IT WAS REPAIRED IN ACCORDANCE W ITH SRM SUPP 53-10-15 FIG 201 SHEET 2. 2 L 7 2 4F RT A35EU 2007073000036 20070730 00036 WP 2007 7 30 IXXA07SMN171S 1 20070630 A 5751 SKIN DOUG DC8 DC873F 302199F WP ZONE 500 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON LEFT WING INBOARD AILERON LOWER SKIN FROM STATION XA 542.000 TO STATION XA 603.000. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN AND DOUBLER. BONDED BOTH PARTS AS NEEDED WITH HY SOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACE. INSTALLED REPAIR PARTS AND NEW FASTENERS FROM STA XW 563.000 TO STA XA 542.000. PERFORMED BALANCE TO INBOARD AILERON FOUND WITHIN ALLOWABLE TOLE RANCE LIMITS MOMENT 3323.3 IN LBS IAW DC8 SRM 57-8-1 FIGURE 1 ITEM "B" AND "K", DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-9 T/R 51-141, SRM 51-142 DATED 04-03-06 AND 04-05-06, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND DC8 SRM 51-4-1. 2 L 7 4 4F RT 4A25 2007073000037 20070730 00037 NM 2007 7 30 07FDEA02636 1 20070726 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 620 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 286FE 22623 ON AGING A/C INSP, FOUND EXISTING REPAIR LOCATED AT BS 620 FLOORBEAM UPPER CHORD FROM LBL 3" TO 19". EVALUATED AND DETE RMINED REPAIR NOT TO CONFORM TO FED EX DWG SR27-53-034. REMOVED EXISTING REPAIR, FABRICATED NEW REPAIR ANGLE FROM 17-7 PH .063", HEAT TREATED TO 180-200 KSI , TH 1050 CAD PLATED, PRIMED. [07-30-07] PRIMED AND INSTALLED REPAIR ANGEL AT B S 620 LBL 3" TO 9" . REF. FED EX DWG. SR27-53-034 2 L 7 3 4F RT A3WE 2007073000038 20070730 00038 WP 2007 7 30 IXXA07SMN165S 1 20070630 A 5330 SKIN DOUG DC8 DC873F 302199F WP ZONE 100 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT FLIGHT STATION 341 LONGERON 33LEFT DOUBLER FORWARD LOWER FUS ELAGE LEFT SIDE ACROSS FROM A-PIT DOOR OPENING SIDE 1 AND 3 FORWARD AND AFT. REMOVED FASTENERS AND EXISTING REPAIR. FA BRICATED NEW SKIN, EXTERNAL DOUBLER AND INTERNAL DOUBLER. CLEANED,TREATED, AND PRIMED AREA AND REPAIR PARTS. APPLIED S EALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW DC8 SRM 53-2-1 FIGURE 7 SHEET 1 AND 3, DC8 SRM 51-1-21, SRM 53-4-1 FIGURE 4 ITEM "C", SRM 51-9-0 FIGURE 68A, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, 51-1-20D AND 51-3-1, 2 L 7 4 4F RT 4A25 2007073000039 20070730 00039 WP 2007 7 30 IXXA07SMN167S 1 20070630 A 5330 SKIN DOUG DC8 DC873F 302199F WP ZONE 100 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT FLIGHT STATION 511 LONGERON 36 DOUBLER, FORWARD LOWER FUSELA GE BELLY FORWARD OF B-PIT DOOR. REMOVED EXISTING REPAIR. FABRICATED NEW SKINS, INTERNAL FINGER DOUBLER. CLEANED, TREA TED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW FAA FORM 8110 NUMBER 07284 DATED 06-27-07, SEMAN DRAWING NUMBER ED-4050 REVISION "I" DATED 06-22-07,DC8 SRM 51-1-20D, D C8 SRM 51-1-8B, SRM 51-1-21, AND 51-3-1. 2 L 7 4 4F RT 4A25 2007073000040 20070730 00040 WP 2007 7 30 IXXA07SMN164S 1 20070630 A 5330 SKIN DOUG DC8 DC873F 302199F WP ZONE 100 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT FLIGHT STATION 160 LONGERON 32.5 LEFT DOUBLER FORWARD LOWER FUSELAGE LEFT SIDE OF BELLY ADF ANTENNAS REPAIR SIDE 2 AND 4 EXCEED MAXIMUM FASTENER SPACING. REMOVED FASTENERS. REMOV ED DAMAGED AREA. FABRICATED EXTERNAL DOUBLER AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW DC8 SRM 53-2-1 FIGURE 7 SHEETS 1, 3, A ND 5, DC8 SRM 51-1-21, SRM 53-4-1 FIGURE 4 ITEM A, SRM 51-9-0 FIGURE 68A, DC8 SRM 51-1-8B, DC8 51-1-11, 51-1-20D, AND 5 1-3-1. 2 L 7 4 4F RT 4A25 2007073000041 20070730 00041 2007 7 30 HALA0700300 4 20070721 A 3442 RADAR BOEING 767 76733A 1385209 NM WX SYSTEM FAILED A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, RIGHT WEATHER RADAR FAIL. TROUBLESHOOT SYS PER FIM 34-41-00 ALL SETTINGS NORMAL, SYSTEM OK FO R SERVICE. 2 L 7 2 4F RT A1NM 2007073000042 20070730 00042 WP 2007 7 30 IXXA07SMN177S 1 20070630 A 5522 SKIN DOUG DC8 DC873F 302199F WP ZONE 300 DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION; FOUND DENTS ON LEFT ELEVATOR UPPER SKIN AT STATION EX. 135.750. REMOVED DAMAGED AREA . FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSON. CLEANED, TREATED AND PRIMED AREA AND REPAIR PAR T. APPLIED SEALANT TO FAYING SURFACE INSTALLED REPAIR PARTS FROM STATION EX. 132.000 TO STATION EX. 246.000. PERFORMED BALANCE TO LEFT ELEVATOR FOUND WITHIN ALLOWABLE TOLERANCE LIMITS MOMENT 1450.87 IN LBS IAW DC8 SRM 55-4-1 FIGURE 1 SHEE TS 1 AND 2, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 55-4-1 FIGURE 1 SHEETS 1 AND 2 ITEM "E" AND "F", DC8 SRM 51- 1-9, T/R 51-141, SRM 51-142 DATED 04-03-06 AND 04-05-06, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND DC8 SRM 51-4-4 PAGES 1 AN 2 L 7 4 4F RT 4A25 2007073000043 20070730 00043 NM 2007 7 30 DHL2007784517 1 20070709 A 5240 6557140514 SKIN BOEING 727 727227 1384078 NM SERVICE DOOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 C-1 DOOR SKIN HAS DENT AT AFT UPPER CORNER, STA 610-618, W/L 183. CUT OUT DAMAGED SKIN 3” BY 2.5 IAW B727 SRM 52-00-3, FIG 3. FABRICATED REPAIR DOUBLER, FROM 2024T3, 080, 8” BY 8.50 IAW B727 SRM 52-00-3, FIG.3 AND 52-30-1, FIG 7. TREATED , PRIMED AND INSTALLED REPAIR DOUBLER IAW B727 SRM 51-10-2 AND 51-30-2, FIG 1. C-1 CARGO DOOR P/N 65-57140-514, S/N 942 . 2 L 7 3 4F A3WE 2007073000044 20070730 00044 SO 2007 7 30 SIMA200720707 1 20070707 A 5315 14521413605 FLOORBEAM EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 818AE 13149 5000 145561 LEFT OMEGA BEAM FRAME 20 CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000047 20070730 00047 SO 2007 7 30 SIMA200720709 1 20070707 A 5320 14522178005 SILL EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 818AE 13149 5000 145561 SERVICE DOOR SILL FOUND CORRODED. REMOVED AND REPLACED SILL IAW EMB SRM 51-40-06, 51-20-03 AND 51-40-02. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000048 20070730 00048 SO 2007 7 30 SIMA200720711 1 20070716 A 5312 14572078021 BULKHEAD EMB 135 EMB135KL 3260302 SO ZONE 700 CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 815AE 13239 5000 145545 LEFT MAIN LANDING GEAR WHEEL WELL AFT WALL CRACKED. STOPPED DRILLED CRACK AND INSTALLED DOUBLER IAW EMB IC2007-145/0469 4. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000050 20070730 00050 EA 2007 7 30 SIMA200720714 1 20070719 A 5315 67053110453 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 511AE 10680 4000 10107 CROSSBEAM AT FRAME 280 CORRODED. REMOVED CORROSION AND INSTALLED NEW SECTION IAW CRJ REPAIR STATEMENT REO 670-53-11-045 . AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007073000051 20070730 00051 SO 2007 7 30 SIMA200720710 1 20070707 A 5315 14521413605 FLOORBEAM EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 818AE 13149 5000 145561 LEFT OMEGA BEAM FRAME 20 CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000052 20070730 00052 EA 2007 7 30 SIMA200720713 1 20070719 A 5340 S61444 TEE FITTING CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 511AE 10680 5000 10107 LEFT TEE FITTING CRACKED AT FRAME 280. REMOVED DAMAGED AREA AND INSTALLED NEW TEE FITTING IAW CRJ REO 670-53-045. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007073000054 20070730 00054 EA 2007 7 30 SIMA200720716 1 20070714 A 5320 67053110522 WEB CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 524AE 8230 5000 10154 WEB AT STATION 280 RIGHT SIDE FOUND CORRODED AT FLOORBEAM MATING AREA. REMOVED AND REPLACED WEB IAW CRJ SRM 51-78-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007073000056 20070730 00056 SO 2007 7 30 SIMA200720705 1 20070707 A 5320 14522178005 SILL EMB 135 EMB135LR 3260305 SO ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 723AE * 5000 145288 SERVICE DOOR CENTER SILL CORRODED. REMOVED AND REPLACED SILL IAW EMB SRM 51-20-01, 51-20-03, 51-40-02, 51-40-04 AND 51- 40-06. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000057 20070730 00057 SO 2007 7 30 SIMA200720701 1 20070710 A 5313 12020333048 STRINGER EMB 135 EMB135LR 3260305 SO ZONE 100 CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 723AE 13150 5000 145288 PREVIOUS REPAIR ON STRINGER 19L CHAFED AT FRAME 54. REPAIRED STRINGER 19L IAW EMB SRM 53-24-02, FIGURE 201. RETURNED A IRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007073000059 20070730 00059 NM 2007 7 30 DHL2007741514 1 20070723 A 5330 SKIN BOEING 727 7272Q9 138448M NM BS 178-300 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 LIGHTNING STRIKE MARKS, 4 PLACES ALONG RIGHT SIDE FUSELAGE BETWEEN BS 178 TO BS 300, STR 17R TO 18R. DAMAGE AT BS 190, 259, AND 276: BLEND OUT'S WITHIN SERV LIMITS PER B727 SRM 53-30-2 FIG 1 AND 51-10-1. HFEC INSP INDICATED CRACKS AT BS 190 AND BS 276 BLEND OUT'S: REPAIRED DAMAGE PER INSTRUCTIONS IN B727 SRM 53-30-3 FIG 20, ITM 2 (.187" HOLE SIZE/FASTENE R). REPAIRED DMG AT BS 277 PER B727 SRM 53-30-3 FIG 20 ITM 2 (.187" HOLE SIZE/FASTENER). NO FURTHER ACTION REQUIRED. 2 L 7 3 4F RT A3WE 2007073000061 20070730 00061 WP 2007 7 30 IXXA07SMN170S 1 20070630 A 5751 SKIN DOUG DC8 DC873F 302199F WP ZONE 500 MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 98143 3336 46003 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON LEFT WING OUTBOARD AILERON LOWER SKIN FROM STATION XW 546.00 0 TO STATION XA 630.000. REMOVED SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN, EXTERNAL DOUBLER, AND INTERNAL DO UBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYIN G SURFACE. INSTALLED REPAIR PARTS AND NEW FASTENER. AT STATION XW546.000 AND STATION XA 630.000. PERFORMED BALANCE TO OUTBOARD AILERON. FOUND WITHIN ALLOWABLE TOLERANCE LIMITS MOMENT 3341.7 IN LBS IAW DC8 SRM 57-8-1 FIGURE 4, DC8 SRM 57 -1-0 PAGE 1, SRM 51-1-21, DC8 SRM 57-8-1 FIGURE 4 ITEM "E" AND "L", DC8 SRM 51-1-9 T/R 51-141, SRM 51-142 DATED 04-03-06 2 L 7 4 4F RT 4A25 2007072300083 20070723 00083 NM 2007 7 23 HNAA0700144 1 20070712 A 7120 LM431SA4 MOUNT DHAV DHC8 DHC8101 2809002 NM PWA 120 PW120 NE NR 2 ENGINE BROKEN A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 942HA 25995 12584 163 120042 ENGINE REMOVED FROM A/C 942 HA IN MDT ON 7-3-07 RECEIVED AT SBY MAINTANCE SHOP. FOUND TORQUE MOUNT END BROKEN OFF. ENG S/N 12-42. 2 H 7 2 4T 4 T RT A13NM E20NE 2007072300089 20070723 00089 NM 2007 7 23 2007UALA02585 1 20070711 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 549UA 25397 STBY INVERTER STATUS MESSAGE FOLLOWED ABOUT 4 MINS LATER WITH A REPORT FROM THE F/A'S OF A PLASTIC OVERHEATING TYPE OF O DOR IN THE CABIN. CREW TURNED UTILITY BUSSES AND RECIRC FANS OFF AND ODOR DISSIPATED. NO SMOKE OBSERVED PER CREW. RE PLACED STATIC INVERTER AS A RESOLUTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072300090 20070723 00090 NM 2007 7 23 2007UALA02586 1 20070711 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 947 DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 351UA 24319 ACFT WAS HIT BY VEHICLE AT APPROX STA 947. 5, AREA BELOW LAST CABIN WINDOW ON THE SKIN LAP JOINT LOWEST TO BOTTOM OF ACF T LT SIDE. [07-27-07] ACCOMPLISHED REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007072300091 20070723 00091 SO 2007 7 23 FDKA200706308 1 20070628 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 FDM 6004 ATL, 4 OVERWING EMERGENCY LIGHTS AND ONE FLOOR EMERGENCY STRIP INOP. MX RESET SYSTEM, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007072300092 20070723 00092 SO 2007 7 23 FDKA200707319 1 20070701 A 3350 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6043 JFK (1009 PHX LCL). BOTH ROW 12 EMERGENCY LOCATOR SIGNS INOP. MX RESET EMERGENCY LIGHTS, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007072300093 20070723 00093 SO 2007 7 23 FDKA200707322 1 20070703 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FDM 6166 PWM-JFK (0900 PHX LCL). EMERGENCY AILSE CEILING LIGHT PLACARD AT ROW 12 INOP. MX RE-SECURED LIGHT CONNECTOR. OPS GOOD. 2 L 7 2 4T RT T00011AT 2007072300094 20070723 00094 SO 2007 7 23 FDKA200707326 1 20070706 A 3350 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6152 FLL-MCO (1209 PHX LCL). EMERGENCY LIGHT AT ROW 12 INOP. MX OPS CHECKED LIGHT GOOD, NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2007072300095 20070723 00095 SO 2007 7 23 FDKA200707329 1 20070707 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 10898 145416 FDM 6037 CLT-CVG (1032 PHX LCL). ALL EMERGENCY LIGHTS INOP. MX REMOVED AND REPLACED ALL FOUR BATTERY PACKS, OPS CHECKE D GOOD. 2 L 7 2 4T RT T00011AT 2007072300096 20070723 00096 SO 2007 7 23 FDKA200707330 1 20070707 A 3350 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DISLODGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6137 ATL (0839 PHX LCL). EXIT ROW SIGN FALLING FROM CEILING ROW 12. MX RE-SECURED EXIT ROW SIGN. 2 L 7 2 4T RT T00011AT 2007072300097 20070723 00097 WP 2007 7 23 G6OA200700002 1 20070710 A 2910 976085521 HOSE DOUG DC10 DC1030F 3023504 WP NR 1 HYD SYSTEM CHAFED A G6OA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 27 604GC 47924 NR 1 ENGINE RIGHT HYDRAULIC PUMP MAIN SUPPLY LINE CHAFED THROUGH CAUSING RAPID LOSS OF NR 1 SYSTEM HYDRAULICS. 2 L 7 3 4F RT A22WE 2007072300098 20070723 00098 SO 2007 7 23 C2XA07IA164 1 20070711 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13958 2028 2028 145085 DAY - FLIGHT 2770, DURING PREFLIGHT INSPECTION THE CREW REPORTED THE OVERWING INTERIOR EXIT LIGHT AND AISLE PATH LIGHTIN G TO BE INOP. CONTRACT MAINTENANCE CHARGED THE AFFECTED EMERGENCY LIGHT BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007072400001 20070724 00001 NM 2007 7 24 HALA0700291 1 20070716 A 2910 30591037 ACCUMULATOR BOEING 717 717200 1383700 NM RT HYD SYSTEM RUPTURED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 480HA 55125 RT HYDRAULIC SYSTEM ACCUMULATOR RUPTURED. REPLACED RT HYDRAULIC SYSTEM ACCUMULATOR PER AMM 29-12-05. LEAK CK CK. 2 L 7 2 4F TR A6WE 2007072400002 20070724 00002 NM 2007 7 24 HALA0700287 1 20070717 A 2612 472566 FIRE DETECTOR BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE LT NACELLE MALFUNCTIONED A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM, EICAS STATUS MESSAGES "LEFT FIRE LP1" AND L ENG FIRE LP2". REMOVED, CLEANED, AND REINSTALLED PYLON CONNECTORS J1, J2, J3, J4, AND J5. PER FIM REPLACED LOWER AFT DETECTOR ASSY PER AMM 26-11-02. LEFT ENGINE FIRE DETECTION SYSTEM NOW TESTS OK. NO MESSAGES. NO FAULTS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072400012 20070724 00012 NM 2007 7 24 AALA20071211 1 20070629 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 780AN 29956 MIA EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F RT T00001SE 2007072400018 20070724 00018 NM 2007 7 24 AWXA200700837 1 20070710 A 5321 D5367180500400 FLOOR PANEL AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5963182, CORROSION ON CABIN FLOOR PANEL 261FF, BS 2786 - BS 2884/FR 66 - FR68, +Y12 92 TO +Y1732. REPLACED CABIN FLOOR PANEL 261FF, BS 2786 - BS 2884 / FR 66 - FR68, +Y1292 TO +Y1732 IAW A319 SRM 51-72-1 1. 2 L 7 2 4F RT A28NM 2007072400020 20070724 00020 NM 2007 7 24 AWXA200700839 1 20070705 A 5340 6623574501 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961277, CRACKED STRINGER TIE CLIP, BS 706, S11L. REPLACED STRINGER TIE CLIP, BS 7 06, S11L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007072400031 20070724 00031 WP 2007 7 24 IXXA070034O 1 20070717 A 5210 DOOR DOUG DC8 DC862F 3021972 WP ZONE 800 UNLOCKED A IXXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 11 71CX 70600 597 45961 DURING TAKEOFF FROM WSAP AT SIXTY KNOTS, THE DOOR WARNING LIGHT (MASTER WARNING) ILLUMINATED. THE CREW ABORTED TAKEOFF WITHOUT INCIDENT AND RETURNED TO BLOCKS. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND R-2 DOOR UNLOCKED. MAINTENANCE R ESECURED THE DOOR AND WARNING LIGHT WENT OUT. MAINTENANCE PERFORMED UNSCHEDULED MAINTENANCE INSPECTION FOR REJECTED TAK EOFF IAW DC8 MAINTENANCE MANUAL 13.01-5. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2007072400032 20070724 00032 NM 2007 7 24 DL757070906 1 20070713 A 3230 LINE BOEING 757 757232 1384965 NM RT DOWNLOCK ACT LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 27 635DL 23762 JUST PRIOR TO LANDING, LOST LEFT HYDRAULIC FLUID. FOUND PRESS HYD LINE FOR RT GEAR DOWN LOCK ACTUATOR LEAKING. REPLACE D LINE AND SERVICED HYD QTY . 2 L 7 2 4F RT A2NM 2007072400043 20070724 00043 WP 2007 7 24 NWAA072469929 1 20070705 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8923E 45838 DURING "H" CHECK FOUND CRACK IN RT FUSELAGE SKIN AT UPPER LEFT CORNER OF FORWARD CARGO DOOR JAMB. REPAIRED PER EA 99-20 9597 SECT I SECT II TO BE ACCOMPLISHED ON OR BEFORE TWO YEARS OR 3000 CYCLES AFTER SECTION I ACCOMPLISHMENT. 2 L 7 2 4F A6WE 2007072400044 20070724 00044 WP 2007 7 24 NWAA072479929 1 20070705 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8923E 45838 DURING "H" CHECK FOUND CRACK IN RT FUSELAGE SKIN AT FORWARD UPPER CORNER OF THE FORWARD CARGO DOOR JAMB. REPAIRED PER E A 99-209598 SECTION I SECTION II TO BE ACCOMPLISHED ON OR BEFORE 2 YEARS OR 3000 CYCLES AFTER SECTION I ACCOMPLISHMENT. 2 L 7 2 4F A6WE 2007072400055 20070724 00055 NM 2007 7 24 DL76P070926 1 20070716 A 3610 77328810 SHUTOFF VALVE BOEING 767 767332 1382001 NM LT ENGINE INOPERATIVE A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 140LL 25988 LEFT ENG BLEED VALVE WOULD NOT OPEN. REPLACED LEFT PRSOV IAW AMM. LEFT ENG PRSOV OPS CKS GOOD. 2 L 7 2 4F RT A1NM 2007072400076 20070724 00076 WP 2007 7 24 AALA20071264 1 20070707 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 417AA 49328 LGA - EMERGENCY LIGHTS AT SEAT ROWS 1 TO 19 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 1 TO 1 9. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400078 20070724 00078 NM 2007 7 24 AWXA200700847 1 20070628 A 5751 113N710028 SKIN BOEING 757 757225 1384959 NM AILERON DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - NR 5950929, RIGHT WING AILERON INBOARD LOWER SURFACE IS DELAMINATED, WS 667 - WS 668. REPAIRED RIGHT WING AILERON INBOARD LOWER SURFACE, WS 667 - WS 668 IAW B757-200 SRM 51-70-04. 2 L 7 2 4F RT A2NM 2007072400079 20070724 00079 NM 2007 7 24 DHL2007784504 1 20070709 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 1050-1054 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 BULGE IN FUSELAGE SKIN AT STA 1050 PLUS 4 AND STR 27R. REMOVED INTERCOSTAL BETWEEN STA 950 TO 970, IAW B727 SRM 51-30-2 . CUT OUT DAMAGED STRINGER DIM 16 LONG IAW B727 SRM 53-10-3, FIG 1. FABRICATED FILLER, MATERIAL USED BAC 1498-145-7075 T6, DIM 16 LONG AND TWO SPLICES, MATERIAL USED BAC 1498-131-7075T6, DIM 12 LONG IAW B727 SRM 53-10-2, FIG 2. AND 53-10-3 , FIG 1. TREATED, PRIMED AND INSTALLED STRINGER REPAIR, INTERCOSTAL IAW B727 SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 2007072400081 20070724 00081 NM 2007 7 24 NWAA072456309 1 20070712 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 DURING OVERNIGHT CHECK, FOUND FORWARD UPPER DECK EMERGENCY PATH LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED BATTERY A ND POWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007072400089 20070724 00089 WP 2007 7 24 AALA20071283 1 20070712 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 450AA 49476 LGA - EMERGENCY LIGHT AT AFT OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT OVERWING. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400096 20070724 00096 NM 2007 7 24 AALA20071275 1 20070708 A 7500 CLAMP BOEING 757 757223 1384957 NM LEFT ENGINE LOOSE A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 185AN 32379 LAX INFLIGHT T192/08JUL - ON CLIMB, RECEIVED LEFT ENGINE OVERHEAT INDICATION AND EICAS MESSAGE. RETURNED TO LAX AND LAN DED WITHOUT INCIDENT. FOUND CLAMPS ON HIGH STAGE BLEED VALVE ON NUMBER ONE ENGINE LOOSE AND LEAKING. RETIGHTENED CLAMP S AND ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007072400101 20070724 00101 WP 2007 7 24 AALA20071280 1 20070710 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 441AA 49460 DFW - EMERGENCY LIGHT AT SEAT ROW 23 HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 23. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400105 20070724 00105 NM 2007 7 24 AALA20071286 1 20070712 A 2560 FLASHLIGHT DOUG MD80 MD83 3023681 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9420D 49824 DFW - EMERGENCY FLASHLIGHT IN CABIN INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2007072400121 20070724 00121 SO 2007 7 24 C2XA07IA168 1 20070718 A 3350 SG9632 LIGHT EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17108 145655 IAH - FLIGHT 2713, DURING PREFLIGHT INSPECTION, THE GALLEY EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENAN CE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE. 2 L 7 2 4F RT 2007072400122 20070724 00122 SO 2007 7 24 C2XA07TY038 1 20070718 A 5530 14540881001 HINGE BRACKET EMB 145 EMB145LR 3260212 SO VERTICAL STAB OUT OF LIMITS A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11535 145518 TYS - DURING A CURRENT C-CHECK INSPECTION THE VERTICAL STAB HINGE FITTING SPHERICAL BEARING HOUSING ON THE LT AND RT WER E OUT OF LIMITS. MAINTENANCE REAMED BOTH SIDES OF VERTICAL STAB AND REPLACED NEW BUSHINGS IAW EMB 145 SRM 55-30-02. AL L WORK WAS ACCOMPLISHED AND WAS RELEASED AT THE END OF THE CHECK. 2 L 7 2 4T RT T00011AT 2007072400123 20070724 00123 NM 2007 7 24 KCSA071234 1 20070718 A 5315 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 1220 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA 1220 RBL 113 AFT SIDE OF LOWER FLOORBEAM WEB CRACKED 1 INCH. 2 L 7 4 4F RT A20WE 2007072400128 20070724 00128 NM 2007 7 24 KCSA071239 1 20070719 A 5313 STRINGER BOEING 747 7472B4B 138481B NM BS 1840 S38L CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STR 38L IS CORRODED AT STA 1840. 2 L 7 4 4F RT A20WE 2007072400146 20070724 00146 NM 2007 7 24 USAA070547 1 20070717 A 5320 SUPPORT BRACKET BOEING 737 737401 1384701 NM BS 500E S20L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 FWD CARGO SIDEALL SUPPORT BRACKET STA 500E STR 20L CRACKED. FABRICATED NEW BRACKET PER BOEING DWG 65C32055 & 65C32625, DEFECT SIZE: .250 INCH. 2 L 7 2 4F RT A16WE 2007072400154 20070724 00154 NM 2007 7 24 2007UALA02589 1 20070712 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 625 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 LEFT EXTERNAL FUSELAGE AT EXISTING REPAIR DOUBLER, FOUND STR 16L AT STA 625 HAS AN ENLARGED HOLE. MAJOR REPAIR ACCOMPLI SHED: REMOVED DAMAGE SECTION OF STRINGER. FABRICATED & INSTALLED A STRINGER SECTION & SPLICE ANGLES. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072400158 20070724 00158 NM 2007 7 24 2007UALA02593 1 20070712 A 2560 BATTERY BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FLASHLIGHT FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 934UA 26662 AFT OUTBOARD EMERGENCY FLASHLIGHT DOES NOT BLINK. [08-08-07] FAILED BATTERY. REPLACED BATTERY AND FLASHLIGHT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007072400174 20070724 00174 NM 2007 7 24 2007UALA02608 1 20070712 A 2150 CONTROL VALVE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU A/C PACK MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 378UA 24653 FLIGHT DIVERTED DUE TO PACK PROBLEM. REPLACED RAM AIR ACTUATOR AND PACK CONTROL VALVE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007072400177 20070724 00177 NM 2007 7 24 2007UALA02611 1 20070712 A 3040 CONTROLLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WINDOW HEAT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 540UA 25252 WINDOW EICAS MSG DISPLAYED, POSITION 4.(1=L FWD, 2=L SIDE, 3=R FWD, 4=R SIDE) INOP LIGHT ILLUM. INOP LIGHT DID NOT EXTI NGUISH WHEN SWITCH WAS RECYCLED TO OFF THEN ON. CREW COMMENTS: IT HAPPENED AGAIN. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072400201 20070724 00201 EU 2007 7 24 2007UALA02635 1 20070713 A 3520 OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE 6 DEF UNWANTED DEPLOY A UALA O OTHER W INADEQUATE Q C LD LANDING 1 WP 29 406UA 454 OXYGEN MASKS DEPLOYED 7DEF ON LANDING. BROKEN O2 LATCH AT ROW 7DEF. REPLACED O2 CONTAINER ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072500001 20070725 00001 NM 2007 7 25 715200701 1 20070715 A 2611 302842 SMOKE DETECTOR BOEING 727 7272K5 138004P NM FALSE ACTIVATION A PCSA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 17 909PG 21852 SMOKE DETECTOR WARNING LIGHT CAME ON DURING TAXI. 2 L 7 3 4F RT A3WE 2007072500007 20070725 00007 SO 2007 7 25 MASA200700305 1 20070606 A 3350 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 ASH 7145 IAD - THE 12A EMERGENCY DOOR LOCATOR SIGN INOP. MX RESET SYSTEM, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007072500025 20070725 00025 NM 2007 7 25 SWAA073531 1 20070718 A 5753 654643127 SKIN BOEING 737 7373A4 1384585 NM LT WING TE FLAPS DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED A1 CHECK, FOUND LEFT WING OUTBOARD FORE FLAP T/E DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2007072500040 20070725 00040 NM 2007 7 25 USAA070569 1 20070719 A 5754 65C26602203 WEDGE BOEING 737 737401 1384701 NM SLAT DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 OUTBOARD END, WEDGE - TOP SURFACE DISBOND. INSTALLED NEW CORE SKIN & DOUBLER PER SRM 51-71-10, 51-70-09, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007072500044 20070725 00044 NM 2007 7 25 USAA070573 1 20070719 A 5510 BEAM BOEING 737 737401 1384701 NM HORZONTAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 CORRODED AT NUT PLATE HOLE, HORZ STAB UNDER PANEL 9109L HAS CORROSION. INSTALLED DOUBLER/ANGLE REPAIR PER EA 98870, DEF ECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007072500045 20070725 00045 NM 2007 7 25 USAA070574 1 20070719 A 5512 65548212 SKIN BOEING 737 737401 1384701 NM HORIZONTAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 RIGHT STAB L/E, LOWER O/B SURF, 43 INCHES FROM O/B END, ELONGATED & CRACKED HOLES. INSTALLED FREEZE PLUG & REPAIR DOUBL ER PER EA 98762, DEFECT SIZE: 5 INCHES. 2 L 7 2 4F RT A16WE 2007072500049 20070725 00049 NM 2007 7 25 SWAA073556 1 20070718 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BL 0. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007072500053 20070725 00053 NM 2007 7 25 SWAA073550 1 20070718 A 5310 6547976 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 956-982 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 956 AND BS 982, RBL 70. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2007072500054 20070725 00054 NM 2007 7 25 SWAA073554 1 20070718 A 5753 6573732 SKIN BOEING 737 7373K2 13844BA NM LT WING TE FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND LEFT WING OUTBOARD MID FLAP CRACKED AT NR 2 CARRIAGE CUTOUT. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007072500072 20070725 00072 NM 2007 7 25 SWAA073528 1 20070718 A 3350 767 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 705SW 27839 DURING SCHEDULED MV1 CHECK, FOUND RIGHT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BUL B PER MM. 2 L 7 2 4F RT A16WE 2007072500077 20070725 00077 NM 2007 7 25 SWAA073557 1 20070716 A 7933 162BL804A INDICATOR BOEING 737 7373H4 1384600 NM OIL TEMP FAULTY A SWAA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 SW 29 399WN 27693 INFLIGHT SHUTDOWN / DECLARED EMERGENCY. NR 2 ENGINE SHUTDOWN IN FLIGHT DUE TO HIGH OIL TEMP INDICATION. REMOVED AND RE PLACED OIL TEMP BULB AND INDICATOR PER MM. 2 L 7 2 4F RT A16WE 2007072500082 20070725 00082 NM 2007 7 25 SWAA073564 1 20070719 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 517D, STR 12R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007072500101 20070725 00101 EA 2007 7 25 TRAX200701009 1 20070716 A 5260 INTERCOSTAL CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 718EV 10095 ASD INTERCOSTAL AT LOWER AFT CORNER HAS POSSIBLE CRACK. 2 L 7 2 4F RT A21EA 2007072500102 20070725 00102 EA 2007 7 25 TRAX200701010 1 20070716 A 3350 COVER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 706EV 10054 EXIT LIGHT/SIGN COVER MISSING AT GALLEY 2. FLT 4097 DEL 61 MINS. 2 L 7 2 4F RT A21EA 2007072500105 20070725 00105 NM 2007 7 25 2007UALA02640 1 20070715 A 3350 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 340UA 24244 RIGHT OVERWING EEL LIGHT INOPERATIVE. [07-27-07] RELAMPED, CK OK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007072500106 20070725 00106 2007 7 25 2007UALA02642 4 20070713 A 2565 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR SLIDE LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 449UA 851 EMERGENCY SLIDE HAS LOW BOTTLE PRESSURE. REPLACED SLIDE ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072500118 20070725 00118 NM 2007 7 25 2007UALA02653 1 20070714 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 664UA 29236 FWD EEL LIGHT AT SEAT 1HJ AND LIGHTS AT SEATS 12AB & 29AB ARE INOPERATIVE. [07-27-07] REPLACED EEL STRIP, OPS CK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072500120 20070725 00120 NM 2007 7 25 2007UALA02655 1 20070714 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 664UA 29236 FWD GALLEY CROSS AISLE EEL STRIP INOP. [08-17-07] REPAIRED BROKEN EEL EXTENSION, OPS CK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072500125 20070725 00125 EU 2007 7 25 SA07009 1 20070207 A 3260 PROXIMITY SENSOR AIRBUS 320 A320214 3930316 EU MLG OUT OF ADJUST A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 119US 1268 PHX - FLT 1161 EN ROUTE MSP TO PHX. AFTER TAKEOFF, THE GEAR HANDLE WOULD NOT RAISE. AFTER A SECOND ATTEMPT, THE GEAR H ANDLE DID GO UP, BUT THE GEAR DID NOT COME UP FOR ABOUT A MINUTE. AFTERWARDS, THE GEAR CAME UP AND ALL SYSTEMS WERE NOR MAL FOR THE REST OF THE FLIGHT. MAINTENANCE ADJUSTED NOSE PROXIMITY SENSORS 24GA AND 25GA. EXTENSION AND RETRACTION TE ST OF NOSE GEAR CHECKS NORMAL. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2007072500127 20070725 00127 NM 2007 7 25 MWEA070159 1 20070719 A 5230 STRUCTURE BOEING 717 717200 1383700 NM CARGO DOOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 918ME 55180 RAMP MADE CONTACT WITH AIRCRAFT BY A BAGGAGE CART, MADE HOLE IN AIRCRAFT`S BAGGAGE DOOR. REMOVED AND REPLACED BAGGAGE D OOR. 2 L 7 2 4F TR A6WE 2007072500134 20070725 00134 NM 2007 7 25 CALA0700365 1 20070718 A 5330 6545778 SKIN BOEING 737 7373T0 1384582 NM BS 947.5-967 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN BELOW R-2 DOOR LOWER HINGE AT STA 947.5-967, S13R TO S14R. 2 L 7 2 4F RT A16WE 2007072500141 20070725 00141 EA 2007 7 25 QXEA200701151 2 20070713 A 7200 312162701 ENGINE BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA NR 1 MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 425QX 2840 2840 4039 LAX - ON FLIGHT 2469, AT FL250 MASTER WARNING NR 1 OIL PRESSURE LIGHT CAME ON. SECURED ENGINE PER E/A CHECKLIST. MAINT ENANCE REMOVED AND REPLACED NR 1 ENGINE, NR 1 PROP ASSY, NR 1 AC GENERATOR, NR 1 OIL COOLER. ALL OPERATIONAL AND LEAK C HECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2007072500143 20070725 00143 NM 2007 7 25 UIEA200700270 1 20070718 A 5753 SKIN BOEING 747 74747UF 1384812 NM TE FLAP CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 492 29253 SMALL AREA OF CHAFING/CRACK AND DELAMINATION TO RT O/B FOREFLAP. 2 L 7 4 4F RT A20WE 2007072500148 20070725 00148 NM 2007 7 25 07FDEA02509 1 20070718 A 5313 BAC1408204 STRINGER BOEING 757 7572B7 1384964 NM BS 1660 DAMAGED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 901FD 27122 AFT PIT, STATION 1660 AT STRINGER 27R, HAS TOOLING MARKS ON STRINGER. BLENDED TOOL MARKS FROM STRINGER IAW SRM 53-00-03. FOUND TO BE OUT OF LIMITS PER SRM 53-00-03, FIG 101. REMOVED DAMAGED SECTION OF STRINGER IAW SRM 53-00-03, FIG 201. FABRICATED REPAIR STRINGER. FABRICATED FILLER, IAW SRM 53-00-03, FIG 201. TREATED AND PRIMED STRINGER REPAIR AND FILLE R IAW SRM 51-20-01. INSTALLED REPAIR PARTS IAW SRM 53-00-03, FIG 201. 2 L 7 2 4F RT A2NM 2007072500149 20070725 00149 NM 2007 7 25 07FDEA02510 1 20070718 A 2780 H1010271 SWITCH BOEING 727 7272S2F 1384O81 NM NR 5 SLAT FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 210FE 22932 UPON FLAP RETRACTION TO 2 THE NR 5 SLAT REMAINED EXTENDED WITH AMBER LIGHT ON FORWARD LED INDICATOR PANEL. S/O LED INDI CATOR PANEL SHOWED NR 5 SLAT EXTENDED. QRH WAS FOLLOWED WITH ALL PROCEDURES COMPLIED WITH. RETURNED TO MEM FOR UNEVENT FUL LANDING. REMOVED AND REPLACED NR 5 SLAT SWITCH (REF 27-82-011-4). OP CHECKED GOOD (REF 27-82-011-4). 2 L 7 3 4F A3WE 2007072500156 20070725 00156 NM 2007 7 25 KNNA200700034 1 20070509 A 5315 FLOORBEAM BOEING 737 7372Q8 138448K NM PWA JT8 JT8D217 52053 NE BS 941 CORRODED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 413JG 23148 PASSENGER CABIN/CORRODED UPPER SURFACE ON FLOORBEAM BS 941.5 AND LBL-16 TO RBL-7ACO NR 075378 REV. 0 PROVIDE INSTRUCTION ON REPAIR OF FLOOR BEAM AT BS-947.5, LBL 36-RBL 12, SRM 53-10-9 FIGURE 9. 2 L 7 2 4F 4 F RT A16WE E9NE 2007072500157 20070725 00157 NM 2007 7 25 UIEA200700271 1 20070718 A 2750 65B8157347 TORQUE TUBE BOEING 747 74747UF 1384812 NM TE FLAP WORN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 492 29253 NR 5 T/E FLAP TRANSMISSION TORQUE TUBE HAS WEAR OUT OF LIMITS 5/8" WIDTH 0.017" DEEP. 2 L 7 4 4F RT A20WE 2007072500158 20070725 00158 NM 2007 7 25 07FDEA02518 1 20070718 A 5313 140N1530 STRINGER BOEING 757 7572B7 1384964 NM BS 1640 S27L DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 AFT PIT - BS 1640 S27L, DRILL MARKS IN STRINGER (4 EACH HOLES) BLENDED DRILL MARKS ON STRINGER 27L IAW SRM 53-00-03. FO UND TO BE OUT OF LIMITS IAW SRM 53-00-03, FIG 101, SHEET 1. NO HOLES ALLOWED. REMOVED DAMAGE IAW SRM 53-00-03, FIG 201 . FABRICATED REPAIR HAT SECTION. FABRICATED FILLER IAW SRM 53-00-03, FIG 201. TREATED AND PRIMED REPAIR HAT AND FILLE R IAW SRM 51-20-01. INSTALLED REPAIR HAT AND FILLER ON S27L AT BS 1640 IAW SRM 53-00-03, FIG 201. 2 L 7 2 4F RT A2NM 2007072500159 20070725 00159 WP 2007 7 25 07FDEA02519 1 20070718 A 5410 AUB70877 STIFFENER DOUG MD10 MD1010F 3022112 WP ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 NR 1 PYLON HAS 6" CRACK VERTICAL STRUCTURE SUPPORT ON OUTBOARD BULKHEAD. VIEWED THROUGH ACCESS PANEL AUB7025-3 APPROXIMA TE 4 FEET FWD PYLON STATION YN=358. [08-24-07] REMOVED AND REPLACED STIFFENER BRACKET AS REQUIRED, REF. DAC DRAWING AU B 7087. 09-04-07 NR 1 ENGINE AND PYLON WERE REMOVED FOR ACCESS THE REPAIR. 2 L 7 3 4F RT A22WE 2007072500161 20070725 00161 NM 2007 7 25 DHL2007741507 1 20070719 A 5320 INTERCOSTAL BOEING 727 7272Q9 138448M NM BS 950A-950B DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AFT PIT LT 950A-950B AT STR-25L AND 24L INTERCOSTAL WEB ARE DENTED AT TOP AREA. FOUND BOTH INTERCOSTAL WEBS (STR 24L AN D 25L) CRACKED AT DENTED AREA IAW B727 SRM 51-10-1. STOP DRILLED CRACKS (0.0250" DIAMETER) IAW B727 SRM 51-10-1. FABRI CATED 2EA ANGLE REPAIRS FROM 2024-T3 0.050" PO NR 9002463 (DIM 4 BY 2.5) IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1. TREATED AND PRIMED AREA AND ANGLES IAW B727 SRM 51-10-2 AND INSTALLED REPAIR ANGLES AT AFT PIT LT BS 950A-950B AT STRS 2 4L AND 25L INTERCOSTAL WEBS TOP AFT AREA IAW B727 SRM 51-40-3 FIG 1 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007072500163 20070725 00163 NM 2007 7 25 DHL2007784511 1 20070708 A 5753 SKIN BOEING 727 727227 1384078 NM TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 RT INBD MID FLAP, OUTBD T/E DELAMINATED UPPER AND LOWER SURFACE, RWBL 239 TO 243.93. REMOVED DAMAGED AREA 3.5 BY 3.6, C LEANED AND PREPPED AREA TO BE REPAIRED IAW B727 SRM 51-40-20, PARA 7, FIG 3. FABRICATED FILLER 3.5 BY 3.6 AND DOUBLER 6 .5 BY 5.1 FROM .012, 7075-T6. ANODIZED, PRIMED AND APPLIED ADHESIVE FILM IAW B727 SRM 51-40-20, 51-40-24, FIG 1 AND 57- 50-2, FIG 3. INSTALLED REPAIR PARTS, CURED AND FINISHED REPAIR AREA IAW B727 SRM 51-40-20, PARA 20, 22 AND 51-40-24, FI G 1. RT INBD MID FLAP P/N 65-2132-62, S/N BN 50. 2 L 7 3 4F A3WE 2007072500168 20070725 00168 SO 2007 7 25 SIMA200720101 1 20070719 A 2701 YOKE EMB 145 EMB145LR 3260212 SO CONTROL COLUMN STICKING A SIMA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SW 21 918AE 14500902 CONTROL YOKE FEELS LIKE IT IS JAMMING WHEN MOVING LEFT AILERON. 2 L 7 2 4T RT T00011AT 2007072500169 20070725 00169 SO 2007 7 25 SIMA200720102 1 20070517 A 5320 14525480603 SILL EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 854AE 9759 5000 145743 CARGO DOOR SILL FOUND CORRODED. REMOVED AND REPLACED DOOR SILL IAW EMB SRM 51-20-03 AND 51-40-06. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007072500171 20070725 00171 SO 2007 7 25 SIMA200720105 1 20070522 A 5320 14522459003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 15926 5000 145224 FORWARD FLOOR SUPPORT AT FRAME 20 FOUND CORRODED. REMOVED AND REPLACED FLOOR SUPPPORT IAW EMB SRM 51-40-02. AIRCRAFT R ETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007072500172 20070725 00172 SO 2007 7 25 SIMA200720107 1 20070525 A 5330 14527605005 SKIN EMB 135 EMB135KL 3260302 SO ZONE 100 CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 802AE 13511 5000 145471 CRACK DEVELOPED DURING DAMAGE CONTOUR. CUT OUT DAMAGE AREA. FABRICATED DOUBLER AND FILLER. INSTALLED IAW EMB IC 2007- 145/03554A, PARAGRAPH 1. 2 L 7 2 4F RT T00011AT 2007072500173 20070725 00173 SO 2007 7 25 SIMA200720106 1 20070524 A 5320 14525480603 SILL EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 802AE 13511 5000 145471 CARGO DOOR LOWER SILL FOUND CORRODED. REMOVED AND REPLACED LOWER SILL IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVI CE. 2 L 7 2 4F RT T00011AT 2007072500174 20070725 00174 EA 2007 7 25 SIMA200720108 1 20070526 A 5320 67053110522 WEB CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 521AE 7880 4000 10142 WEB AT STA 280 CORRODED AT FLOORBEAM MATTING AREA. SPLICED IN NEW WEB IAW AMERICAN EAGLE ENGINEERING ORDER CR-53MR-124. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007072500175 20070725 00175 NM 2007 7 25 QXEA200701131 1 20070709 A 5340 STRINGER CLIP DHAV DHC8 DHC8202 2809007 NM BS 424 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - STRINGER ATTACH CLIP HAS CORROSION AROUND RIVET HEAD AND ON BOTTOM SIDE OF STRINGER 24R STATION X424.124 FORWAR D SIDE OF REAR SPAR FRAME. REPAIRED IAW SRM 51-20-16, 51-20-36. 2 H 7 2 4T RT A13NM 2007072500178 20070725 00178 NM 2007 7 25 QXEA200701132 1 20070705 A 5320 ATTACH FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - WEB ATTACH CLIP HAS MINOR SURFACE CORROSION AT STRINGER 23R STATION X488.500. REPAIRED IAW SRM 51-20-16, 51-20 -36, 51-20-26. 2 H 7 2 4T RT A13NM 2007072500180 20070725 00180 NM 2007 7 25 QXEA200701129 1 20070709 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 242 S23R CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - CORROSION AROUND RIVET ON FRAME AT STATION 242.200 JUST ABOVE STRINGER 23R. REPAIRED IAW SRM 51-20-11, 51-20-4 1. 2 H 7 2 4T RT A13NM 2007072500183 20070725 00183 NM 2007 7 25 QXEA200701128 1 20070707 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 242 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 379PH 520 C4 PDX - NR 4 SEAT TRACK AT STATION 242 HAS PITTING CORROSION ON FLANGE AND VERTICAL SIDE OF RAIL. REPAIRED IW RD8/4-53 -4698 AND RD8/4-53-1102. 2 H 7 2 4T RT A13NM 2007072500185 20070725 00185 NM 2007 7 25 DHL2007741506 1 20070719 A 5322 SHEAR TIE BOEING 727 7272Q9 138448M NM BS 1070 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AFT PIT LT BS 1070 MAIN FRAME CORRODED, CRACKED AT AREA UNDER SIDE PANEL O/B OF STR-27L (SHEAR TIE). REMOVED CRACKED SH EAR TIE IAW B727 SRM 51-30-2, FABRICATED NEW SHEAR TIE FROM BAC1505-10210 7075-T73 POX NR 7161380 (DIM 5.50" BY 2.25") I AW B727 SRM 53-10-2 FIGURE 5 AND 51-20-1. INSTALLED NEW SHEAR TIE AT AFT PIT LT BS 1070 MAIN FRAME O/B OF STIR 27L AFTE R TREATING AND PRIMING NEW SHEAR TIE IAW B727 SRM 51-10-2. INSTALLATION PERFORMED IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007072500186 20070725 00186 SO 2007 7 25 SIMA200720005 1 20070517 A 5311 14523050401 FRAME EMB 145 EMB145LR 3260212 SO ZONE 100 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 942LL 4931 4931 14500930 THREE FASTENER HOLES MISDRILLED ON FRAME 64AT STRINGER 11R. REAMED HOLES AND INSTALLED OVERSIZE FASTENERS IAW EMB. RET URNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007072500187 20070725 00187 SO 2007 7 25 SIMA200720004 1 20070507 A 5322 14525175001 SHEAR TIE EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 854AE 9758 5000 145743 SHEAR CLIP AT FRAME 65 LOWER SECTION CORRODED. REMOVED AND REPLACED SHEAR CLIP IAW EMB IC2207-145/03294A. RETURNED AIRC RAFT TO SERVICE 2 L 7 2 4F RT T00011AT 2007072500190 20070725 00190 SO 2007 7 25 SIMA200720002 1 20070718 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 620AE 8929 6216 145102 EMERGENCY LIGHTS INOPERATIVE DUE TO SWITCH LEFT IN ARM POSITION. REMOVED AND REPLACED BATTERY PACKS 1 THRU 4 IAW EMB AM M 33-50-04. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007072500191 20070725 00191 SO 2007 7 25 SIMA200720003 1 20070507 A 5322 14525175003 SHEAR TIE EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 854AE 9758 5000 145743 SHEAR CLIP AT FRAME 68 LOWER SECTION FOUND CORRODED. REMOVED AND REPLACED SHEAR CLIP IAW EMB IC2007-145/03294A. RETURN ED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007072500193 20070725 00193 NM 2007 7 25 07FDEA02520 1 20070719 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 MAIN DECK CARGO CENTER STA 635 BETWEEN FLOOR PANELS NR 232FF AND NR 233GF, FOUND SEAT TRACK CROWN AREA CHIPPED OFF. CAR RIED OUT REPAIR ON DAMAGED SEAT TRACK AT STA 625 TO STA 645 AS PER SRM 53-70-00 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007072500196 20070725 00196 WP 2007 7 25 07FDEA02523 1 20070719 A 5330 ADA31391 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 AFT SKIN DENTED AT APPROXIMATELY THE 5:00 POSITION ON FRAME AND IS 18 INCHES OF RVSM (CENTER PLATE). THIS SDR REPLACES (SDR#07-2123) REPAIRED SKIN IAW EA 8-55330-112937 FUSELAGE-SKIN REPAIR AT STA 851-913 L36R-L48R. 2 L 7 3 4F RT A22WE 2007072500197 20070725 00197 WP 2007 7 25 07FDEA02524 1 20070719 A 5311 AEA00181 FRAME DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CLG WHEEL WELL CAVITY, CORROSION ON BULKHEAD LOWER CIRCUMFERENTIAL ANGLE AT STA 152 LONGERON 50R TO 49R. REMOVED, FABRI CATED AND INSTALLED 4 EACH ANGLES 49R TO 50R IAW MD/DC10 SRM 51-33-01 VOLII AND 51-35-01 VOLII PAGE 1. 2 L 7 3 4F RT A22WE 2007072500204 20070725 00204 SO 2007 7 25 SIMA200720405 1 20070603 A 5320 13500469403 PROFILE EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 15957 5000 145235 Z PROFILE CORRODED AT FRAME 22. REMOVED AND REPLACED PROFILE IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007072500206 20070725 00206 SO 2007 7 25 SIMA20720408 1 20070603 A 5320 14524128403 SUPPORT FITTING EMB 135 EMB135KL 3260302 SO ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 806AE 13290 5000 145503 PASSENGER DOOR THRESHOLD AFT SUPPORT CORRODED. REMOVED AND REPLACED PASSENGER DOOR THRESHOLD SUPPORT IAW EMB SRM 51-40- 02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007072500208 20070725 00208 SO 2007 7 25 SIMA200720407 1 20070603 A 5320 13500429401 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 15967 5000 145235 CENTER OMEGA BEAM CORRODED ON INBOARD SIDE OF CROSSBEAM AT FRAME 32. REPAIRED OMEGA BEAM IAW EMB IC2007-145-0348 AND EM B SRM 53-10-03. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007072500209 20070725 00209 SO 2007 7 25 SIMA200720417 1 20070609 A 5330 14564091001 SKIN EMB 145 EMB145LR 3260212 SO ZONE 200 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 941LT 4929 14500926 DENT AT FRAMES 66 AND 67 AT STRINGER 14R. REPAIRED DENT IAW AMERICAN EAGLE ENGINEERING ORDER EM-53MR-785. RETURNED AIR CRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007072500211 20070725 00211 SO 2007 7 25 SIMA200720410 1 20070605 A 5320 14521700007 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 855AE 9744 5000 145747 LEFT OMEGA BEAM CORRODED AT FRAME 24 AND 25. CUT OUT DAMAGED, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-1 0, FIGURE 202. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007072500212 20070725 00212 SO 2007 7 25 SIMA200720406 1 20070603 A 5320 14521713005 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 15967 5000 145235 LEFT OMEGA BEAM CORRODED AT FRAME 20. REPAIRED OMEGA BEAM IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007072500214 20070725 00214 NM 2007 7 25 NWAA072536303 1 20070715 A 3350 SIGN BOEING 747 747451 1384940 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 663US 23818 DURING OVERNIGHT LINE CHECK, EMERGENCY EXIT SIGN INOP. MAINTENANCE REMOVED AND REPLACED EXIT SIGN, POWER SUPPLY AND BAT TERY. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007072500218 20070725 00218 2007 7 25 QXEA200701171 2 20070719 A 7200 ENGINE BOMBDR DHC8 DHC8402 1390042 NM NR1 SMOKE A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 426QX 4154 SEA - ON FLIGHT 2338, NR 1 ENGINE START ABORT. ENGINE SPOOLED UP NORMALLY FOR ABOUT 10 SECONDS THEN TUG OPERATOR REPORT ED EXCESSIVE SMOKE, NL=0 ABORTED START. MAINTENANCE INTERRAGATED CDS, NO FAULTS, COMPLIED WITH 2 CONSECUTIVE STARTS ON NR 1 ENGINE WITH NO DEFECTS NOTED. ALL ENGINE PARAMETERS NORMAL. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007072600002 20070726 00002 EA 2007 7 26 TRAX200701011 1 20070717 A 5350 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA TAILCONE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 718EV 10095 LT VERT STAB AND FUSELAGE ATTACHMENT ANGLE CRACKED ON T/E, ABOVE THE FWD OF TAIL CONE. REMOVED AND REPLACED LT VERT STA B DRAG ANGLE IAW REO 670-55-31-018 2 L 7 2 4F RT A21EA 2007072600003 20070726 00003 EA 2007 7 26 TRAX200701012 1 20070717 A 5350 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA TAILCONE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 718EV 10095 RHS VERT STAB AND FUSELAGE ATTACHMENT ANGLE CRACKED ON T/E, ABOVE THE FWD OF TAIL CONE. REMOVED AND REPLACED RS VERT ST AB DRAG ANGLE PER REO 670-55-31-018 2 L 7 2 4F RT A21EA 2007072600004 20070726 00004 EA 2007 7 26 TRAX200701019 1 20070718 A 5320 SILL CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 718EV 10095 RT FLOOR SILL AT RBL 45 FS 280 IS CORRODED OUT OF LIMITS. REPAIRED RT FLOOR SILL AT RBL 45 FS280 IAW REO 670-53-21-139 2 L 7 2 4F RT A21EA 2007072600005 20070726 00005 EA 2007 7 26 TRAX200701028 1 20070719 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA BS 310 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 718EV 10095 CORROSION DAMAGE FS 310.00 FRAME BETWEEN STR 27 AND 26 RT IN MAIN AVIONICS BAY (MARKED). FOUND BLENDED AREA WITHIN LIMI TS IAW CRJ 700 SRM 53-21-00 ONLY .002 MATERIAL REMOVED ALLOWED UP TO .005. ALODINES PRIMED AND PAINTED BLENDED AREA. I NSTALLED FOUR REMOVED RIVETS IN WORKED AREA IAW CRJ 700 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007072600016 20070726 00016 NM 2007 7 26 AWXA200700850 1 20070707 A 5753 WEDGE BOEING 737 7373G7 1384595 NM ZONE 600 DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5962306, RIGHT WING INBOARD MID FLAP TRAILING EDGE WEDGE LOWER SURFACE HAS AREA OF DISBOND, WS 161.5 - WS 167.5. REPAIRED RIGHT WING INBOARD MID FLAP TRAILING EDGE WEDGE LOWER SURFACE, WS 161.5 - WS 167 .5 IAW B737-300 SRM 51-70-10-2R4, FIGURE 203. 2 L 7 2 4F RT A16WE 2007072600017 20070726 00017 NM 2007 7 26 AWXA200700851 1 20070705 A 5320 146N852217 WEB BOEING 757 757225 1384959 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - NR 5950598, CORROSION ON WEB, BS 1360 - BS 1380, S27R. REPLACED WEB, BS 1360 - BS 138 0, S27R IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007072600018 20070726 00018 NM 2007 7 26 AWXA200700852 1 20070703 A 5322 146N542111 SHEAR TIE BOEING 757 757225 1384959 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - NR 5950591, CORROSION ON SHEAR TIE, BS 1360 + 16", RBL 26, WL 158. REPLACED SHEAR TIE , BS 1360 + 16", RBL 26, WL 158 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007072600019 20070726 00019 NM 2007 7 26 DHL2007784516 1 20070711 A 5534 SUPPORT ANGLE BOEING 727 727227 1384078 NM ZONE 300 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 CRACK AT BS 1342 WEB AND LT SUPPORT ANGLE INSIDE VERT STAB PANEL 9504. REMOVED CRACKED SUPPORT ANGLE INSIDE VERT STAB P ANEL 9504 IAW B727 SRM 51-30-2. FABRICATED NEW SUPPORT ANGLE FROM .040, 7075T6, DIM. 3.75 BY 8.25 IAW B727 SRM 51-10-2. TREATED, PRIMED AND INSTALLED SUPPORT ANGLE IAW B727 SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 2007072600020 20070726 00020 NM 2007 7 26 AWXA200700853 1 20070628 A 5322 146N542644 SHEAR TIE BOEING 757 757225 1384959 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - NR 5979000, CORROSION ON AFT CARGO COMPARTMENT SHEAR CLIP, BS 1420, RBL 21, WL 156.80. REPLACED AFT CARGO COMPARTMENT SHEAR CLIP, BS 1420, RBL 21, WL 156.80 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007072600021 20070726 00021 NM 2007 7 26 AWXA200700854 1 20070628 A 5320 146N54012 WEB BOEING 757 757225 1384959 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - CORROSION ON AFT CARGO COMPARTMENT WEB, BS 1400 - BS 1420, RBL 21, WL 156.80. REPLACE D AFT CARGO COMPARTMENT WEB, BS 1400 - BS 1420, RBL 21, WL 156.80 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007072600022 20070726 00022 NM 2007 7 26 AWXA200700855 1 20070705 A 5320 146N54279 INTERCOSTAL BOEING 757 757225 1384959 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - NR 5950599, CORROSION ON INTERCOSTAL, BS 1360 - BS 1380, S26R - S27R. REPLACED INTERC OSTAL, BS 1360 - BS 1380, S26R - S27R IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007072600023 20070726 00023 NM 2007 7 26 AWXA200700856 1 20070713 A 5340 146N542113 ATTACH ANGLE BOEING 757 757225 1384959 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - NR 5950589, CORROSION ON ATTACH ANGLE, BS 1360 +16", RBL 24. REPLACED ATTACH ANGLE, B S 1360 +16", RBL 24 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007072600024 20070726 00024 NM 2007 7 26 AWXA200700857 1 20070712 A 5320 146N542510 INTERCOSTAL BOEING 757 757225 1384959 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - NR 5979102, CORROSION ON INTERCOSTAL, BS 1435 - BS 1440, S27R - S28R. REPLACED INTERC OSTAL, BS 1435 - BS 1440, S27R - S28R IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007072600025 20070726 00025 NM 2007 7 26 AWXA200700858 1 20070703 A 5340 140N2006210 ATTACH ANGLE BOEING 757 757225 1384959 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - FOUND CORROSION ON ATTACH ANGLE, BS 1400, S26R - S27R. REPLACED ATTACH ANGLE, BS 1400 , S26R - S27R IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007072600026 20070726 00026 NM 2007 7 26 P5CA0701527 1 20070718 A 3150 UNKNOWN BOEING 747 74747UF 1384812 NM UNKNOWN A P5CA O OTHER J WARNING INDICATION CL CLIMB 1 EA 15 416MC 32838 ON CLIMB-OUT, BLEED HP ENG 4, ENG 4 LOW IDLE, NAI ENG 4 MESSAGES. DEFERRED BLEED HP ENG 4 PER MEL 36-11-3 AND 78-31-1A. DEFERRED NAI 4 MESSAGE PER MEL 30-21-1B 2 L 7 4 4F RT A20WE 2007072600027 20070726 00027 NM 2007 7 26 AWXA200700895 1 20070712 A 5320 65557572 STIFFENER BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - CORROSION ON FORWARD LAVATORY HOUSING HAT SECTION STIFFENER, BS 271, RBL 65, WL 183.0. REPLACED FORWARD LAVATORY HOUSING HAT SECTION STIFFENER, BS 271, RBL 65, WL 183.0 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007072600028 20070726 00028 2007 7 26 AWXA200700896 2 20070723 A 7320 8249722016 EEC AIRBUS 320 A320232 3930326 EU RT ENGINE FAILED A AWXA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 WP 28 673AW 24173 9574 2312 LAS - IFSD - CREW REPORTED ECAM MESSAGE, "ENG 2 FAIL" ON SHORT FINAL, ENGINE SHUT DOWN WITH ABNORMAL ENGINE INDICATIONS. MX REPLACED NR 2 ENGINE EEC NR 2 ENG PER R5M73302 AND ALSO REPLACED NR 2 ENGINE FMU PER AMM 73-22-52-000-010-A AMM 73- 22-52-400-010-A LEAK TEST OK C/W A- 5 HIGH POWER ASSURANCE TEST PER F5M71312. NO FAULTS NOTED. 2 L 7 2 4F RT A28NM 2007072600029 20070726 00029 NM 2007 7 26 QXEA200701192 1 20070720 A 3150 NONE DHAV DHC8 DHC8202 2809007 NM BATTERY FALSE INDICATION A QXEA O OTHER N FALSE WARNING AP APPROACH 1 NM 09 366PH 510 LMT FLIGHT NR 2093 ON APPROACH, MAIN BATTERY HOT WARNING LIGHT ILLUMINATED. TEMP SENSOR INDICATED NORMAL. RAN CHECKLIS T. MONITORED AND REMAINED ILLUMINATED UNTIL POWER DOWN AT GATE. PERFORMED OPERATIONAL TEST OF BATTERY TEMP MONITOR SYS TEM IAW AMM TASK 24-34-00-710-801. OPERATIONAL TEST GOOD. POWERED DOWN AIRCRAFT INSPECTED MAIN BATTERY AND MAIN BATTER Y TEMP CONNECTOR, NO DEFECTS NOTED. BATTERY WAS COOL TO TOUCH. POWERED AIRCRAFT UP BATTERY TEMP SYSTEMS NORMAL. NO PA RTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007072600030 20070726 00030 NM 2007 7 26 QXEA200701193 1 20070723 A 2133 10306814 OUTFLOW VALVE DHAV DHC8 DHC8202 2809007 NM CABIN PRESSURE MALFUNCTIONED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 346PH 10913 477 PDX - WITH ONLY GROUND FAN ON, ELECTRICAL SMELL COMING FROM AIR DUCT VENTS. DID NOT SMELL IT WITH RECIRC FAN. MAINTENAN CE REPLACED OUTFLOW VALVE. OPERATION CHECK GOOD. 2 H 7 2 4T RT A13NM 2007072600031 20070726 00031 SO 2007 7 26 SWIA200718497 1 20070722 A 5753 STRUCTURE EMB 120 EMB120ER 3260203 SO NACELLE FLAP CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 216SW 120285 FOUND CRACK ON LEFT SIDEWALL OF NACELLE FLAP. REPLACED LEFT NACELLE FLAP IAW 27-50-00, P/N - 120-37299-009. 2 L 7 2 4T RT A31SO 2007072600032 20070726 00032 EA 2007 7 26 SWIA200718498 1 20070717 A 5751 601R130002 AILERON CNDAIR CL600 CL6002B19 1900309 EA WING WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 427SW 17262 17262 7497 REPLACE RIGHT AILERON DUE TO EXCESSIVE BACKLASH. REPLACED RIGHT AILERON WITH A SERVICEABLE UNIT IAW 27-15-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007072600033 20070726 00033 SO 2007 7 26 SWIA200718499 1 20070719 A 3350 SIGN EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 251YV 120251 FLT 5708 - F/A REPORTS "EXIT" SIGN BY JUMPSEAT IS CRACKED. REPLACED "EXIT" SIGN. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007072600034 20070726 00034 EA 2007 7 26 SWIA200718500 1 20070720 A 5753 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 913EV 7731 LEFT INBOARD FLAP IS DAMAGED FROM BIRDSTRIKE. REPLACED LEFT INBOARD FLAP IAW 27-54-01, PN: 601R14002-1, SN OFF: SB/RJ/7 59. 2 L 7 2 4F RT A21EA 2007072600035 20070726 00035 EA 2007 7 26 SWIA200718501 1 20070720 A 5210 STRUT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 410SW 7066 FLT 3865 - MAIN CABIN DOOR DOES NOT OPEN FREELY. REPLACED AFT PAX DOOR STRUT IAW AMM 52-11-17, PN: 601R31911-9. 2 L 7 2 4F RT A21EA 2007072600036 20070726 00036 EA 2007 7 26 SWIA200718502 1 20070719 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS LOOSE A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 408SW 7055 FLT 3850 - EMERGENCY LIGHTS IN THE GALLEY DO NOT WORK. RESECURED LOOSE CONNECTIONS IN THE GALLEY CLOSET. OPS CHECK GOO D. 2 L 7 2 4F RT A21EA 2007072600037 20070726 00037 EA 2007 7 26 SWIA200718503 1 20070716 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 951SW 7795 FLT 6688 - LEFT SIDE EXTERIOR EMERGENCY EXIT LIGHT IS INOP. RELAMPED LEFT AFT EMERGENCY LIGHT BULB IAW MM 33-51-00. OP CHECK GOOD. 2 L 7 2 4F RT A21EA 2007072600038 20070726 00038 EA 2007 7 26 SWIA200718504 1 20070716 A 3230 UPLOCK CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA O OTHER O OTHER AP APPROACH 1 NM 07 919SW 7657 FLT 6533 - WHEN THE GEAR WAS SELECTED DOWN, THE NOSE GEAR DID NOT EXTEND. AFTER PULLING THE LANDING GEAR MANUAL RELEASE HANDLE, THE NOSE GEAR EXTENDED AND INDICATED DOWN AND LOCKED. REPLACED THE NOSE GEAR UPLOCK ASSY IAW MM 32-33-05. OPS CHECK GOOD, PN 11600-103, SN/OFF NGL/0673/02. 2 L 7 2 4F RT A21EA 2007072600039 20070726 00039 EA 2007 7 26 SWIA200718505 1 20070615 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 712SK 10172 FLOOR SUPPORT 280 CRACKED AT LBL 9, DISCOVERED AT C-CHECK. REPLACED FS 280 FLOOR SUPPORT BEAM SECTIONS, DOUBLERS, AND R ADIUS PLATE PER REO:670-53-11-047 REV (D). 2 L 7 2 4F RT A21EA 2007072600040 20070726 00040 EA 2007 7 26 SWIA200718506 1 20070615 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 712SK 10172 AFT COCKPIT FLOOR SUPPORT CRACKED IN 2 PLACES, DISCOVERED AT C-CHECK. REPLACED COCKPIT FLOOR SUPPORT PER CRJ700/900 SRM 51-42-06-001-001-A01. 2 L 7 2 4F RT A21EA 2007072600041 20070726 00041 EA 2007 7 26 SWIA200718507 1 20070615 A 5210 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 712SK 10172 PASSENGER DOOR AFT DRAG ANGLE IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED FILLER AND SPLICE ANGLES PER REO 670-52-11-0 72. 2 L 7 2 4F RT A21EA 2007072600042 20070726 00042 EA 2007 7 26 SWIA200718508 1 20070524 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA MLG WW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 427SW 7497 RIGHT BRAKE TRANSDUCER BRACKET IS CRACKED AT 3 PLACES, DISCOVERED AT C-CHECK. INSTALLED NEW BRACKET PER CRJ200 SRM 51-4 2-06. 2 L 7 2 4F RT A21EA 2007072600043 20070726 00043 EA 2007 7 26 SWIA200718509 1 20070524 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 427SW 7497 FOUND STA 280 RBL9 LOWER ANGLE IS CRACKED, DISCOVERED AT C-CHECK. PERFORMED REPAIR IAW REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 2007072600044 20070726 00044 EA 2007 7 26 SWIA200718510 1 20070524 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 427SW 7497 FOUND FS 280 FLOORBEAM IS CRACKED AT LBL9 UPPER ANGLE, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLES IAW REO:601R-53-1 1-138. 2 L 7 2 4F RT A21EA 2007072600045 20070726 00045 EA 2007 7 26 SWIA200718511 1 20070524 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 427SW 7497 COCKPIT FLOORBOARD SUPPORT ANGLE AT STA 280 LBL9/RBL9 IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED NEW REPAIR ANGLES AT STN 280, LBL9.0-RBL9.0 IAW CRJ200 SRM CH 51-42-06, SECTION 9, PG 11. 2 L 7 2 4F RT A21EA 2007072600046 20070726 00046 EA 2007 7 26 SWIA200718512 1 20070524 A 5310 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 427SW 7497 PAX DOOR FRAME IS CRACKED AT LOWER AFT CORNER RADIUS, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLE AND FILLER PER CRJ 200 REO 601R-52-11-279 REV NC 10-18-01. 2 L 7 2 4F RT A21EA 2007072600047 20070726 00047 EA 2007 7 26 SWIA200718513 1 20070524 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 342 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 427SW 7497 MAIN CABIN FS342.0 LBL41 HAS CORROSION, DISCOVERED AT C-CHECK. REPLACED SUPPORT BRACKET ASSEMBLY IAW CRJ200 SRM 51-42-0 6. 2 L 7 2 4F RT A21EA 2007072600048 20070726 00048 EA 2007 7 26 SWIA200718514 1 20070603 A 5320 SUPPORT BEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 715SK 10179 FS 280 SUPPORT BEAM IS CRACKED AT LBL9, DISCOVERED AT C-CHECK. INSTALLED SPLICE DOUBLERS PER REO 670-53-11-047 REV D. 2 L 7 2 4F RT A21EA 2007072000146 20070720 00146 2007 7 20 2007UALA02487 4 20070709 A 2300 CONTROL PANEL BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 182UA 25279 DOOR 5R FLIGHT ATTENNDANT STATION EMERGENCY EVAC SIGNAL IS CONTINUOUS, SHOULD BE INTERMITTENT. [08-08-07] REPLACED EM ERGENCY EVACUATION SIGNAL PANEL. OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072000154 20070720 00154 NM 2007 7 20 2007UALA02495 1 20070708 A 2150 CONTROL VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN COOLING MALFUNCTIONED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 520UA 24890 UNABLE TO COOL CABIN. TEMP IN CABIN ABOVE 85 DEGREES. TRIED ALL CONFIGURATIONS. TRIM AIR OFF, STDBY COLD, ONE PACK AT A TIME, BOOSTING ENGINE BLEEDS, ALL NO HELP. [08-08-07] DURING PACK OPERATIONAL TEST FOUND LEFT PACK TEMP CONTROL VA LVE FAULT ON BITE BOX. REPLACED PACK, NOW OPERATES NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072000157 20070720 00157 NM 2007 7 20 2007UALA02498 1 20070707 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 589UA 28707 EXTERIOR EMERGENCY EXIT LIGHT INOP AT DOOR 1R. [07-27-07] RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072000169 20070720 00169 NM 2007 7 20 2007UALA02510 1 20070707 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 AFT LEFT & AFT RIGHT DOOR EXTERNAL EEL LIGHTS ARE INOP. [07-27-07] RELAMPED. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072000171 20070720 00171 SO 2007 7 20 C2XA07RI057 1 20070713 A 3231 22250100003 SOLENOID VALVE EMB 145 EMB145XR 3260214 SO MLG INOPERATIVE A C2XA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 27 13118 12923 12923 145675 DURING CLIMB, CREW REPORTED LOUD NOISE AND VIBRATION FROM NOSE AREA AND UNABLE TO CYCLE NOSE GEAR IN AIR. AFTER AIR RET URN, MX MAINTENANCE DISCOVERED THE NOSE LANDING GEAR DOOR SOLENOID VALVE TO BE THE CAUSE. MX REMOVED AND REPLACED NLG D OOR SOLENOID VALVE WITH OPERATIONAL AND LEAK CHECKS GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007072000182 20070720 00182 2007 7 20 2007UALA02522 4 20070708 A 2565 MECHANISM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE ARMING FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 555UA 26647 BOTH AFT DOORS ARMING MECHANISM FELT DIFFERENT. [08-08-07] 4 LT LUBED AND ADJUSTED CAM PLATE 4 RT REMOVED BEARING PLAT E AND REPLACED BEARING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072300010 20070723 00010 NM 2007 7 23 2007UALA02531 1 20070710 A 2612 FIRE DETECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FWD CARGO BAY FAULTY A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 642UA 25092 FWD CARGO DETECTOR NR 2 AND GROUND PROXIMITY SYS STATUS WILL NOT CLEAR. [08-08-07] RESTARTED SYSTEM. FWD CARGO "DET 2" MSG CLEARED. GROUND PROX SYSTEM MESSAGE STILL PRESENT. RESET GLIDESLOPE DISCRETE PER MM34-46-00 MESSAGE CLEARED. MESSAGE REPEATED 8 DAYS LATER. ACCOMPLISHED TEST OF SMOKE DETECTION SYSTEM PER MM 26-16-00 P105. ALL TESTS WERE NORMAL, NO EICAS OR STATUS MESSAGES DISPLAYED. NO HARDWARE CHANGED OR IMPLICAED. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072300036 20070723 00036 EU 2007 7 23 2007UALA02554 1 20070710 A 3250 SERVO CONTROL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG STEERING INOPERATIVE A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 401UA 435 NOSE WHEEL STEERING INOPERATIVE. FAULTY NOSE WHEEL STEERING CONTROL SERVO 6GC. REPLACED NOSE WHEEL STEERING SERVO C ONTROL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072300054 20070723 00054 EA 2007 7 23 TRAX200700947 1 20070706 A 5260 HANDLE CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 ASD INNER VERTICLE RELEASE HANDLE CRACKED SEVERAL SPOT NEAR READ BALL. RIGGING ADJUSTMENT CHECKED GOOD. SUPPLEMENTAL - SDR CLOSED 07/16/07. 2 L 7 2 4F RT A21EA 2007072300055 20070723 00055 EA 2007 7 23 TRAX200700958 1 20070706 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 349 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 FRAME AT FS 349.00 HAS CORROSION ON FWD FRAME DOUBLER AND AFT SIDE OF FRAME AT STR 27. REMOVED UPPER RIVETS AT STA 349 TOP OF FRAME AT FRAME DOUBLER AND REMOVED LT AND RT INTERCOSTAL SPLICES AT STA 364 FRAME TOP SIDE PER SRM 51-42-06, 51-4 2-20. REMOVED 4 EA INTERCOSTALS BETWEEN LBL 9 AND RBL 9 CONTINUED REMOVING RIVETS FROM FS 349 FRAME IAW CRJ 200 SRM 51- 42-06 MS 7022223. REMOVED FRAME 349, REMOVED VERT FLOOR SUPPORT BEAM ON LT SIDE AT 349, PER SRM 51-42-06. RI 17912. RE MOVED FRAME SUPPORT ANGLE. DRILLED UP NEW FRAME. WORK DONE IAW 51-42-00. STARTED INSTALLATION OF 349 FRAME ALL WORK P ER CRJ200, SRM 51-40-00. FINISHED INSTALLATION OF 349 FRAME, PRIME AND PAINTED, STILL NEEDS DYNTROL APPLIED AND DOOR S 2 L 7 2 4F RT A21EA 2007072300057 20070723 00057 NM 2007 7 23 2007UALA02568 1 20070710 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 SEAT 2A FWD EMERGENCY LIGHT IS INOP. [07-27-07] RELAMPED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072300074 20070723 00074 NM 2007 7 23 BB07052 1 20070712 A 2842 0779406 PROBE BOEING 757 75723N 1384973 NM FUEL QTY INTERMITTENT A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 204UW 30886 FLIGHT 724, PHL-SNN: AFTER TAKEOFF, CREW REPORTED THAT THE RIGHT FUEL QUANTITY GAUGE WAS INOPERATIVE AND RECEIVED AN IN TERMITTANT FUEL QUANTITY STATUS MESSAGE. FLIGHT RETURNED TO PHL. MAINTENANCE FOUND THE RIGHT FUEL COMPENSATOR PROBE IN TERMITTANT. REPLACED PROBE. NO FURTHER FAULTS. 2 L 7 2 4F RT A2NM 2007072300075 20070723 00075 2007 7 23 2007UALA02583 4 20070711 A 2565 BEARING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ARMING MECHANISM DRY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 DOOR 4R WILL NOT ARM. ARMING MECHANISM HAS DRY BEARINGS, FOUND MOVEMENT STIFF. REMOVED DOOR LINING AND SLIDE. LUBED ARMING MECHANISM AND PERFORMED A SATISFACTORY OPERATIONAL CHECK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072300079 20070723 00079 EU 2007 7 23 TRAX200701001 1 20070715 A 5210 DOOR AEROSP ATR72 ATR72 EU MAIN PAX STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 PAX DOOR HARD TO OPEN FROM INSIDE. 2 H 7 2 4T RT 2007072300084 20070723 00084 NE 2007 7 23 2007UALA02532 2 20070709 A 7230 51A045002 SPINNER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FAN DELAMINATED A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 116UA 25547 9508 26908 727595 CREW REPORTS ON CLIMBOUT HEARD BANG FROM NR 2 ENGINE. ALL ENGINE PARAMETERS FLUCTUATED, FLT ATTENDANTS REPORTED BANG, CR EW REPORTED ENG2 VIB INDICATION AT 5.0 BUT NOT FELT. THE FAN SPINNER CONE HAD DELAMINATION AT THE TRAILING EDGE (T/E ) SKIRT, WITH MULTIPLE KEVLAR AREAS UNRAVELED. AREAS AT THE T/E SHOWED BOTH SIGNS OF DISBONDING, AS WELL AS AREAS WHERE RESIN WAS EITHER ABSENT OR COMPROMISED. SEVERAL INTACT AREAS FAILED THE "TAP" TEST. BLACKLIGHT INSPECTION SHOWED NO SIG N OF BIRD REMAINS. THIS SPINNER CONE HAD BEEN MODIFIED PER SB PW4ENG 72-629. THIS SB ADDS ADDITIONAL PLIES AT THE REARMO ST PORTION OF THE INLET CONE TO PRECLUDE T/E DELAMINATION. IT APPEARS THAT THIS MODIFICATION WAS NOT ACCOMPLISHED PROPER 2 L 7 4 4F 4 F RT A20WE E24NE 2007072300085 20070723 00085 NE 2007 7 23 2007UALA02553 2 20070710 A 7310 LINE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUEL SYSTEM LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 783UA 14457 26950 NR 2 ENGINE HAS FIRE DAMAGE FROM FUEL LEAKING AT THE MAIN FUEL SUPPLY HOSE AT THE NACELLE DISCONNECT PANEL. FIRE NOT CO NFIRMED. ECM DATA SHOWED UNDER COWL TEMPERATURES TO BE NORMAL. HOWEVER, THERE WAS DAMAGE DUE TO A FUEL LEAK IN THE ARE A. DAMAGE WAS FOUND DURING A ROUTINE C-CHECK. WHAT WAS DESCRIBED AS "SCORCHING" WAS FOUND IN THE AREA UNDER THE HOSE P ANEL. THE FUEL SUPPLY LINE (BOEING IPC REF. 73-11-08-01-050) WAS LEAKING FROM THE UPPER CONNECTION AT THE NACELLE DISCO NNECT PANEL. NO PLASTIC MATERIALS (HOSES, CLAMPS, HARNESSES) APPEARED TO HAVE MELTED. THE FUEL SUPPLY LINE WAS REPLACE D. ENGINE TIME SINCE INSTALLATION 14457 HOURS (2085 CYCLES). 2 L 7 2 4F 4 F RT T0001SE E46NE 2007072400004 20070724 00004 NM 2007 7 24 HALA0700290 1 20070717 A 3397 CONNECTOR BOEING 767 76733A 1385209 NM EMERGENCY LIGHT UNSECURE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 583HA 25531 EMERGENCY ESCAPE PATH LIGHTS INOP LT SIDE ROWS 31-38 ON OVERNIGHT CHECK. RESECURED STRIP CONNECTOR, SYSTEM NOW CHECKS N ORMAL PER B767 AMM 33-51-10-402. 2 L 7 2 4F RT A1NM 2007072400010 20070724 00010 NM 2007 7 24 AALA20071209 1 20070629 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 344AN 33083 MIA EMERGENCY LIGHT AT RIGHT SECOND ROW FROM LAST INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT CABIN SECOND ROW FROM LAST. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007072400011 20070724 00011 NM 2007 7 24 AALA20071210 1 20070629 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 780AN 29956 MIA EMERGENCY LIGHT AT SEAT 20C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F RT T00001SE 2007072400035 20070724 00035 2007 7 24 DL764070910 4 20070714 A 3417 311040007 COMPUTER BOEING 767 767432ER 1385134 NM AIR DATA MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 838MH 29711 F/O AIR DATA INOP. R DPC MESSAGE. MTC IN PROGRESS. THIS IS FOR FLT 108/13. SECOND MRR DUE TO ATB. INSTALLED NEW SER VICEABLE DPC R RETURNED ADIRU SOURCE SELECT BACK TO NML RAN IRMP TEST NO FAULTS DPC NEEDS SOFTWARE VERIFICATION S/W LOAD ED. RETERMINATED WIRE W173-234R-24 AT 3163 UA33 WDM 34-21-83 SH 2. CKS GOOD PER AMM. 2 L 7 2 4F RT A1NM 2007072400068 20070724 00068 WP 2007 7 24 AALA20071296 1 20070713 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 208AA 49159 DFW - EMERGENCY LIGHT AT SEAT ROW 10D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 10D. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400073 20070724 00073 NM 2007 7 24 AALA20071260 1 20070706 A 3350 CAP BOEING 757 7572Q8 1384972 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 707TW 27625 DFW - EMERGENCY FLOOR LIGHT IN FIRST CLASS MISSING BOTH END CAPS. REPLACED BOTH END CAPS FOR EMERGENCY FLOOR LIGHT IN F IRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007072400075 20070724 00075 WP 2007 7 24 AALA20071263 1 20070707 A 2612 FIRE LOOP DOUG DC9 DC982 3022082 WP APU BAY FAULTY A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 419AA 49331 DFW INFLIGHT T2368/07JUL - DURING CLIMB CREW REPORTED APU FIRE WARNING INDICATION. BOTH FIRE BOTTLES WERE DISCHARGED A ND AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. INSPECTION FOUND NO FIRE. WARNING WAS STILL ON FOR LOOP NUMBE R ONE. REPLACED LEFT FIRE LOOP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400083 20070724 00083 NM 2007 7 24 AALA20071266 1 20070707 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 183AN 29593 SFO - OVERHEAD EMERGENCY LIGHT AT SEAT 31C INOPERATIVE. RELAMPED OVERHEAD EMERGENCY LIGHT AT SEAT 31C. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007072400086 20070724 00086 WP 2007 7 24 AALA20071271 1 20070708 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 400AA 49311 LGA - EMERGENCY LIGHTS AT FORWARD GALLEY CEILING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD GAL LEY CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400109 20070724 00109 EA 2007 7 24 TRAX200701002 1 20070715 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STICKING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 PAX DOOR HARD TO CLOSE. 2 L 7 2 4F RT A21EA 2007072400117 20070724 00117 NM 2007 7 24 HNAA070144 1 20070712 A 7120 LM431SA4 MOUNT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE NR 2 ENGINE BROKEN A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 942HA 25995 12584 163 120042 ENGINE WAS REMOVED FROM A/C IN MDT ON 7-3-07. RECEIVED IN SBY MAINTENANCE SHOP FOUND TORQUE MOUNT END BROKE OFF. ENGIN E S/N 120042. 2 H 7 2 4T 4 T RT A13NM E20NE 2007072400119 20070724 00119 EU 2007 7 24 USA2007F00010 1 20070613 A 5310 STRUCTURE AIRBUS A321 A321211 3930370 EU CFMINT CFM56 CFM565B3P 13006 NE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 181UW 21870 1531 CORRODED RIVET TAILS WERE FOUND IN FUSELAGE CARGO COMPARTMENT BETWEEN FRAME 25 TO 35.6 STRINGER 31L TO 31R. APPROXIMATE LY A TOTAL OF 600 RIVETS WERE REPLACED. 7 RIVETS WERE REPLACED AT S31L AND 3 S32L FOR A TOTAL OF 22 RIVETS THAT WERE RE PLACED ABOVE STRINGER 38. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD THE PAINT FLAKI NG OFF THE RIVET TAILS THAT WERE CLEANED AND HAD PRIMER AND PAINT REAPPLIED. AIRCRAFT WAS MFG JULY 6, 2001. 2 L 7 2 4F 4 F RT A28NM E37NE 2007072400120 20070724 00120 SO 2007 7 24 C2XA07IA167 1 20070712 A 3350 110049 POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13553 145585 MCI - FLIGHT 530, DURING POST-FLIGHT INSPECTION THE EXTERIOR UPPER OVERWING EMERGENCY LIGHT AND FWD SIDE CEILING OVERWIN G EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT P OWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007072400129 20070724 00129 NM 2007 7 24 KCSA071240 1 20070719 A 5412 BULKHEAD BOEING 747 7472B4B 138481B NM NR 3 NACELLE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NR 3 PYLON FWD BULKHEAD FRAME AT NAC STA 221 O/B SIDE IS CRACKED 2 INCHES. 2 L 7 4 4F RT A20WE 2007072400132 20070724 00132 EA 2007 7 24 TRAX200701000 1 20070712 A 7830 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 LEFT T/R SWITCH SUPPORT FWD BRACKET (ANGLE) CRACKED AT TOP HOLE. 2 L 7 2 4F RT A21EA 2007072400133 20070724 00133 NM 2007 7 24 2007UALA02685 1 20070717 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 MAIN STAIRS EEL INOPERATIVE. [07-27-07] SECURED CONNECTOR AT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072400134 20070724 00134 EA 2007 7 24 TRAX200701014 1 20070717 A 5240 HANDLE CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR LOOSE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 713EV 10081 SERVICE DOOR RELEASE HANDLE LOOSE WN LET OPEN. 2 L 7 2 4F RT A21EA 2007072400145 20070724 00145 EU 2007 7 24 TRAX200701021 1 20070718 A 3350 COVER AEROSP ATR72 ATR72 EU EMERGENCY LIGHT MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 FWD LEFT EMERGENCY EXIT LIGHT COVER MISSING. 2 H 7 2 4T RT 2007072400147 20070724 00147 WP 2007 7 24 MWEA070157 1 20070719 A 5101 NONE DOUG DC9 DC981 3022081 WP NONE NONE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 805ME 48031 SM 2673 SOILD FASTENERS NEED TO BE INSTALLED PER ETA 0602B STEP 1 BETWEEN CENTER & FIRST OFFICER`S WINDOW AT THE NEXT HE AVY CHECK. INSTALLED FASTENERS. 2 L 7 2 4F A6WE 2007072400150 20070724 00150 NM 2007 7 24 SB07057 1 20070717 A 5610 5893543109 WINDSHIELD BOEING 737 7373B7 1384580 NM COCKPIT CRACKED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 511AU 15590 15590 23594 JAX - FLT 983 - ON DESCENT INTO JAX, THE CAPTAIN'S NR 1 WINDSHIELD ARCED AND THEN CRACKED. FLIGHT LANDED WITHOUT FURTHE R INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S NR 1 WINDSHIELD PER JOB CARD J356-11-01. ALSO, REMOVED AND REPLACED WINDOW HEAT CONTROL UNIT AS PRECAUTIONARY PER MM 30-41-11-4. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007072400159 20070724 00159 NM 2007 7 24 SB07056 1 20070715 A 5610 5893543139 WINDSHIELD BOEING 737 737301 1384611 NM COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 592US 23937 CHS - FLT - 1575 DURING CRUISE, EN ROUTE FROM DCA TO JAX, THE CAPTAIN'S NR 1 WINDSHIELD OUTER PANE CRACKED. CREW COMPLI ED WITH QUICK REFERENCE HANDBOOK PROCEDURES AND DIVERTED TO CHS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S NR 1 WINDSHIELD PER JOB CARD J356-11-01. ALSO, REPLACED T HE WINDOW HEAT CONTROL UNIT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007112100132 20071121 00132 NM 2007 11 21 WRLA2007125 1 20071107 A 5312 TEE FITTING DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE BULKHEAD CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING C-CHECK INSPECTION, CORROSION FOUND ON BULKHEAD TEE CHORD STA Y=2007 X=27.5. REPLACED DAMAGE TEE CHORD PER MD11 SRM VOL.II 51-35-01 REV.40 REF EGAT NRC U05014. 2 L 7 3 4F 4 F RT A22WE E24NE 2007072400183 20070724 00183 2007 7 24 2007UALA02618 4 20070713 A 3442 RADAR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE WX SYS INOPERATIVE A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 479UA 1538 RTFL DUE TO INOPERATIVE WEATHER RADAR. [08-24-07] REPLACED WX RADAR PN 622-5137-601. NO REPEATS SINCE 7/16/07. 2 L 7 2 4F 4 F RT A28NM E40NE 2007083100044 20070831 00044 WP 2007 8 31 070153 1 20070822 A 3241 PIN DOUG DC9 DC983 3022083 WP TRANSDUCER BROKEN A WX0A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 19 864GA 49912 DURING TAKEOFF ROLL THE WHEEL NOT TURNING LIGHT ILLUMINATED, TAKEOFF ABORTED AND AIRCRAFT RETURNED TO THE GATE IN LAS VE GAS. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED THE AIRCRAFT AND FOUND THE NR 1 WHEEL TRANSDUCER PINS LAYING IN THE HUB CAP. TRANSDUCER PINS REINSTALLED AND OPERATIONAL CHECK PERFORMED NORMAL IAW M/M 32-43-02. AIRCRAFT RETURNED TO SERVIC E. 2 L 7 2 4F RT A6WE 2007072400195 20070724 00195 NM 2007 7 24 2007UALA02629 1 20070714 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 MED 2R UPPER HINGE CUTOUT CRACKED. MAJOR REPAIR ACCOMPLISHED: INSURANCE CUT & INSTALLED A DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072400198 20070724 00198 2007 7 24 2007UALA02632 4 20070714 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR SLIDE OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 GIRT BAR WILL NOT ENGAGE DOOR 1R. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072400199 20070724 00199 NM 2007 7 24 2007UALA02633 1 20070715 A 5600 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN PRESSURE UNKNOWN A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 548UA 25396 RTFL DUE TO A PRESSURIZATION PROBLEM. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072400200 20070724 00200 NM 2007 7 24 2007UALA02634 1 20070715 A 2120 UNKNOWN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN ODOR A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 844UA 1581 FLIGHT ATTENDANT REPORTING ELECTRICAL ODOR AROUND ROW 20, COOLED DOWN THE TEMP AND SHUT OFF LIGHTS AND ODOR IS DISSIPATI NG. INSPECTION DONE OF AREA, TURNING OFF AND ON LIGHTS AND AIR. NO ODORS NOTED. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072500002 20070725 00002 NM 2007 7 25 USAA200707003 1 20070716 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 531AU 24478 A .375 INCH LONG CRACK AT RT REAR SERVICE DOOR UPPER HINGE CUTOUT. INSTALLED DOUBLER REPAIR PER SRM 53-60-01 FIG 201. 2 L 7 2 4F RT A16WE 2007072500003 20070725 00003 NM 2007 7 25 MASA200700082 1 20070207 A 3230 692101 SEQUENCE VALVE DHAV DHC8 DHC8202 2809007 NM MLG VIBRATION A MASA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 SW 07 448YV 13185 448 ASH 7067 DEN. UPON GEAR RETRACTION LOUD GRINDING AND VIBRATION & NOSE GEAR DOOR CTN MSG. MX REMOVED AND REPLACED MECHA NICAL SEQUENCE VALVE AND GEAR SWINGS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2007072500004 20070725 00004 GL 2007 7 25 MASA200700192 2 20070407 A 7200 AE3007A1 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 UNKNOWN A MASA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SW 07 856MJ 14560 145626 CAE311538 ASH 7374 IAD. AIRCRAFT DIVERTED TO CLT DUE TO NR 2 ENGINE AUTO SHUTDOWN. MX REMOVED AND REPLACED ENGINE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007072500005 20070725 00005 SO 2007 7 25 MASA200700268 1 20070513 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 858MJ 145767 ASH 7144 IAD - MAIN DOOR HANDLE DIFFICULT TO OPERATE. MX LUBED DOOR ROLLERS AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2007072500006 20070725 00006 SO 2007 7 25 MASA200700297 1 20070602 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 ASH 7144 IAD - EMERGENCY EXIT LIGHT INOP AT LEFT OVERWING EXIT. MX REPAIRED THE WIRING AND OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2007072500008 20070725 00008 SO 2007 7 25 MASA200700343 1 20070620 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 ASH 7406 GSP-IAD, LEFT EMERGENCY LIGHT INOP. MX RESECURED CONNECTOR AT LIGHT ASSY, OPS GOOD. 2 L 7 2 4T RT T00011AT 2007072500009 20070725 00009 SO 2007 7 25 MASA200700123 1 20070227 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX STUCK A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 ASH 7249 PIT - PAX DOOR WOULD NOT OPEN. MX TROUBLESHOOTING. 2 L 7 2 4T RT T00011AT 2007072500010 20070725 00010 NE 2007 7 25 MASA200700173 2 20070330 A 7200 BETA SWITCH DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 2 ENGINE OUT OF ADJUST A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 454YV 454 PCEAG0005 ASH 9704 DEN - NR 2 ENGINE SHUTDOWN DUE TO/AT FLIGHT IDLE NR 2 ENGINE PROP RPM DROPS OFF AT POWER. ADJUSTED BETA SWITCH AND REMOVED AND REPLACED INTER COMPRESSOR VALVE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007072500012 20070725 00012 NM 2007 7 25 MASA200700100 1 20070213 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY FALSE ACTIVATION A MASA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SW 07 436YV 436 ASH 7059 DEN - BAGGAGE COMPARTMENT SMOKE LIGHT ILLUMINATED ON GROUND. MX REMOVED AND REPLACED FWD SMOKE DETECTOR. 2 H 7 2 4T RT A13NM 2007072500013 20070725 00013 NM 2007 7 25 USAA070567 1 20070719 A 5512 SKIN BOEING 737 737401 1384701 NM HORIZONTAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 RIGHT HORIZONTAL STAB, LOWER SKIN AT REAR SPAR 86 INCHES FROM INBOARD END OF STAB HAS CRACK. FAB'D & INSTALLED PERMANEN T REPAIR DOUBLER PER TR 57-10-07, DEFECT SIZE: 1.5 INCH. 2 L 7 2 4F RT A16WE 2007072500015 20070725 00015 EU 2007 7 25 SWAA073521 2 20070718 A 7200 332A10000 ENGINE BOEING 737 7373H4 1384600 NM CFMINT CFM56 CFM563C 13802 EU RIGHT FAILED A SWAA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 SW 29 361SW 26572 721642 INFLIGHT SHUTDOWN / DECLARED EMERGENCY. NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED INTERMITTENTLY. NR 2 ENGINE OI L QUANTITY WENT TO ZERO. PER QRH SHUTDOWN NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007072500016 20070725 00016 NM 2007 7 25 SWAA073523 1 20070718 A 3350 417A5600 LIGHT BOEING 737 7377H4 1384404 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 240WN 32503 DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007072500017 20070725 00017 NM 2007 7 25 SWAA073525 1 20070718 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 451WN 32495 EEPLS COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007072500018 20070725 00018 2007 7 25 SWAA073524 4 20070718 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 421LV 32452 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007072500019 20070725 00019 2007 7 25 SWAA073529 4 20070718 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 727SW 27859 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007072500020 20070725 00020 NM 2007 7 25 SWAA073532 1 20070718 A 5330 6545766 SKIN BOEING 737 7373A4 1384585 NM BS 534D S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 534D, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007072500023 20070725 00023 NM 2007 7 25 SWAA073527 1 20070718 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM 780 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007072500024 20070725 00024 NM 2007 7 25 SWAA073526 1 20070718 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 945 S25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 945, STR 25R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007072500026 20070725 00026 NM 2007 7 25 SWAA073552 1 20070718 A 5311 6546525 FRAME BOEING 737 7375H4 138449D NM BS 380 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007072500027 20070725 00027 NM 2007 7 25 SWAA073535 1 20070718 A 5311 6546525 FRAME BOEING 737 7373A4 1384585 NM BS 380 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 15R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007072500029 20070725 00029 NM 2007 7 25 USAA070566 1 20070719 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 380 S26L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 STA 380, STR 26L HAS CRACK. INSTALLED FABRICATED REPAIR PART PER SRM 51-10-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007072500030 20070725 00030 NM 2007 7 25 USAA070557 1 20070719 A 5210 507945264 SKIN BOEING 737 737401 1384701 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 NR 4 STOP PIN ACCESS HOLE IS CRACKED AT EDGE OF DOOR INTERIOR SKIN. REPAIRED PER EA 98739, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007072500031 20070725 00031 NM 2007 7 25 USAA070558 1 20070719 A 5311 FRAME BOEING 737 737401 1384701 NM BS 1138 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 IN FRAME STRAP, LEFT STA 1138 LT STAB HINGE FUSELAGE LOWER CUTOUT CRACKED. STOP DRILLED CRACK & INSTALLED DOUBLER PER S RM 53-00-01 FIG 201, DEFECT SIZE: 2.25 INCH. 2 L 7 2 4F RT A16WE 2007072500032 20070725 00032 NM 2007 7 25 USAA070559 1 20070719 A 5311 FRAME BOEING 737 737401 1384701 NM BS 1138 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 RIGHT STA 1138 AT RIGHT STAB HINGE FUSELAGE LOWER CUTOUT HAS CRACK. STOP DRILLED CRACKS & INSTALLED DOUBLER REPAIR PER SRM 53-00-01 FIG 201, SRM 51-10-02, DEFECT SIZE: 1.8 INCH. 2 L 7 2 4F RT A16WE 2007072500033 20070725 00033 NM 2007 7 25 USAA070560 1 20070719 A 5311 507945264 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 NR 4, 5, 6 & 7 STOP IN ACCESS HOLES AT EDGE OF INTERIOR SKIN 0.5 INCH, AFT FRAME HAS CRACK. FAB'D DOUBLERS & INSTALLED; INNER SKIN DOUBLER, DOOR STOP DOUBLER (4 EA) ON AFT FRAME PER EA 98739, DEFECT SIZE: 0.5 INCH. 2 L 7 2 4F RT A16WE 2007072500034 20070725 00034 NM 2007 7 25 USAA070561 1 20070719 A 5311 FRAME BOEING 737 737401 1384701 NM BS 727D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 STA 727D, RBL 2 AND LBL 2 HAS CRACK. INSTALLED REPAIR DOUBLER PER SRM 51-70-11, DEFECT SIZE: .25 INCH CRACK. 2 L 7 2 4F RT A16WE 2007072500035 20070725 00035 NM 2007 7 25 USAA070562 1 20070719 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM BS 295 S7L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 STR 7L INTERCOSTAL WEB CRACKED AT STA 295 HAS CRACK. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 10-15-01-1, DE FECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007072500036 20070725 00036 NM 2007 7 25 USAA070563 1 20070719 A 5414 SKIN BOEING 737 737401 1384701 NM LT NACELLE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 AT ACCESS PANEL OPENING 5727 LEFT ENGINE PYLON HAS CRACK. INSTALLED DOUBLER PER TR 54-30-07, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007072500037 20070725 00037 NM 2007 7 25 USAA070565 1 20070719 A 5313 STRINGER BOEING 737 737401 1384701 NM BS 359 S14L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 STR 14L AT STA 359, STRINGER/SPLICE HAS CRACK. REMOVED & REPLACED STRINGER SPLICE PR SRM 51-10-02, 51-40-03 DEFECT SI ZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007072500038 20070725 00038 NM 2007 7 25 USAA070575 1 20070719 A 5510 STRUCTURE BOEING 737 737401 1384701 NM HORIZONTAL STAB DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 RIGHT STAB, L/E UPPER I/B END, ELONGATED HOLES. INSTALLED HOLE FILLER & DOUBLER REPAIR PER EA 98762, DEFECT SIZE: 20 I NCHES. 2 L 7 2 4F RT A16WE 2007072500039 20070725 00039 NM 2007 7 25 USAA070568 1 20070719 A 5313 STRINGER BOEING 737 737401 1384701 NM BS 907 S4L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 STA 907 STR 4L, STRINGER SPLICE HAS CRACK. INSTALLED REPAIR PARTS PER SRM 51-10-02, DEFECT SIZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007072500041 20070725 00041 NM 2007 7 25 USAA070570 1 20070719 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 1123 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 APU COMPT STA 1123, S13-15R, TEE ANGLE CORRODED. REMOVED & REPLACED ANGLES, VERT STIFFENERS, TORQUE BOX SKIN, PER SRM 5 1-40-02, 51-70-12; DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007072500043 20070725 00043 NM 2007 7 25 USAA070572 1 20070719 A 5320 TRACK BOEING 737 737401 1384701 NM BS 943 LBL 17 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 STA 943 LBBL 17.20 HAS CORROSION. INSTALLED NEW SECTION OF TRACK PER SRM 53-00-53, FIG 201; CORR TASK C53-202-01, DEFEC T SIZE: .5 X 1.5 INCH. 2 L 7 2 4F RT A16WE 2007072500046 20070725 00046 NM 2007 7 25 USAA070564 1 20070719 A 5340 ATTACH ANGLE BOEING 737 737401 1384701 NM BS 380 S26L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 STA 380, STR 26L, FRAME ATTACH ANGLE HAS CRACK. INSTALLED FABRICATED REPAIR PART PER SRM 51-10-02, DEFECT SIZE: 1 INCH . 2 L 7 2 4F RT A16WE 2007072500047 20070725 00047 NM 2007 7 25 USAA200707004 1 20070718 A 5310 DOOR FRAME BOEING 737 7374B7 1384702 NM BS 492 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 441US 24812 A .5 INCH CRACK AT FWD CARGO DOOR OPENING, AFT FRAME BS 492, LOWER DOOR STOP FITTING, S-24R. CUT OUT DAMAGED AREA, FABR ICATED & INSTALLED REPAIR FILLER & ANGLES PER EA 98795. 2 L 7 2 4F RT A16WE 2007072500050 20070725 00050 NM 2007 7 25 SWAA073546 1 20070718 A 5311 6546538 FRAME BOEING 737 7373H4 1384600 NM BS 597 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007072500051 20070725 00051 NM 2007 7 25 SWAA073545 1 20070718 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007072500052 20070725 00052 NM 2007 7 25 SWAA073551 1 20070718 A 5311 6546564 FRAME BOEING 737 7375H4 138449D NM BS 986 S20R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 986, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007072500057 20070725 00057 NM 2007 7 25 SWAA073538 1 20070718 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 597 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007072500058 20070725 00058 NM 2007 7 25 SWAA073540 1 20070718 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 639 S3L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007072500059 20070725 00059 NM 2007 7 25 SWAA073541 1 20070718 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 685 S3L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007072500061 20070725 00061 NM 2007 7 25 KCSA071242 1 20070719 A 5311 FRAME BOEING 747 7472B4B 138481B NM BS 1315 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 R3 DOOR CUT CRACKED IN UPPER AFT CORNER STA 1315 WL 275, 2 INCHES. 2 L 7 4 4F RT A20WE 2007072500062 20070725 00062 NM 2007 7 25 KCSA071243 1 20070719 A 5315 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 460 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 UPPER TEE CHORD CORRODED UPPER DECK FLOORBEAM STA 460 RBL 45 WL 308. 2 L 7 4 4F RT A20WE 2007072500065 20070725 00065 NM 2007 7 25 SWAA073544 1 20070718 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 706 S3L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007072500066 20070725 00066 NM 2007 7 25 SWAA073547 1 20070718 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 277 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007072500068 20070725 00068 NM 2007 7 25 SWAA073549 1 20070718 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500A S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007072500069 20070725 00069 NM 2007 7 25 SWAA073555 1 20070718 A 5340 65C27314 STRINGER CLIP BOEING 737 7373K2 13844BA NM BS 727B S3R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007072500070 20070725 00070 NM 2007 7 25 SWAA073537 1 20070718 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 597 S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007072500073 20070725 00073 NM 2007 7 25 MASA20070076 1 20070203 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY FALSE ACTIVATION A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 987HA 425 ASH 2993 PHX - CREW REPORTED NUMEROUS FALSE LAV SMOKE WARNINGS WITH ENGINES RUNNING. MX REPLACED SMOKE DETECTOR. 2 H 7 2 4T RT A13NM 2007072500075 20070725 00075 NM 2007 7 25 SWAA073558 1 20070719 A 3350 10107451 SIGN BOEING 737 7373Q8 1384670 NM EMERGENCY LIGHTS DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 LEFT OVERWING EMERGENCY EXIT SIGN FELL OFF. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2007072500076 20070725 00076 NM 2007 7 25 SWAA073575 1 20070719 A 5315 147A5502 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 903 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 732SW 27864 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 903, RBL 8. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007072500079 20070725 00079 NM 2007 7 25 SWAA073562 1 20070719 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007072500080 20070725 00080 NM 2007 7 25 SWAA073560 1 20070719 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 464WN 32468 EEPLS COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007072500081 20070725 00081 NM 2007 7 25 SWAA073576 1 20070719 A 5311 6517684 FRAME BOEING 737 7373H4 1384600 NM BS 303 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 16L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007072500083 20070725 00083 NM 2007 7 25 SWAA073574 1 20070719 A 5311 6545808 FRAME BOEING 737 7375H4 138449D NM BS 296 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND STUB FRAME CRACKED AT BS 296, STR 16R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007072500085 20070725 00085 NM 2007 7 25 SWAA073563 1 20070719 A 5210 6545877 SKIN BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007072500087 20070725 00087 NM 2007 7 25 SWAA073571 1 20070719 A 5312 6546568 BULKHEAD BOEING 737 7373Y0 1384671 NM BS 1016 S23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 23L. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007072500088 20070725 00088 NM 2007 7 25 SWAA073572 1 20070719 A 5310 6547959 DOOR FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED NR 5 DOOR STOP. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007072500091 20070725 00091 NM 2007 7 25 MASA200700255 1 20070509 A 5210 85210240007 STRUT DHAV DHC8 DHC8202 2809007 NM PAX DOOR BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 987HA 425 ASH 2897 DRO - PASSENGER DOOR AFT STRUT BROKEN. REMOVED & REPLACED AFT UPPER STRUT. 2 H 7 2 4T RT A13NM 2007072500094 20070725 00094 NM 2007 7 25 MASA200700339 1 20070619 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY MALFUNCTIONED A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 446YV 446 ASH 7089 CPR - DIVERTED TO CYS DUE TO SMOKE WARNING LIGHT ILLUMINATED IN FLIGHT FOR SEVERAL SECONDS. MAINTENANCE CHANGE D FORWARD CARGO SMOKE DETECTOR. 2 H 7 2 4T RT A13NM 2007072500095 20070725 00095 NM 2007 7 25 MASA200700408 1 20070710 A 3350 BULB DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 988HA 426 ASH 2894 PHX - REPORTED ONE BULB ON A FLOOR PATH LIGHT STRIP INOP. MEL'ED WITH THE CREW. 2 H 7 2 4T RT A13NM 2007072500098 20070725 00098 EA 2007 7 25 TRAX200701006 1 20070716 A 5260 SKIN CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 718EV 10095 ASD INNER SKIN CRACKED AT FWD CORNER UNDER UPPER STEP. [07-26-07] REPLACED UPPER EDGE MEMBER PER CRJ 700 SRM 51-42- 06. 2 L 7 2 4F RT A21EA 2007072500103 20070725 00103 EA 2007 7 25 TRAX200701013 1 20070717 A 5320 ANGLE CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 718EV 10095 COCKPIT FWD 280 ANGLE (LAND) CORRODED. 2 L 7 2 4F RT A21EA 2007072500104 20070725 00104 NM 2007 7 25 2007UALA02639 1 20070714 A 3397 FEEDER CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 303UA 23644 EMERGENCY FLOOR LIGHTS SEAT 15-21 INOPERATIVE. [07-27-07] REPLACED EEL CABLE, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007083100046 20070831 00046 WP 2007 8 31 070148 1 20070810 A 3241 42807 CONTROL BOX DOUG DC9 DC983 3022083 WP ANTI SKID SYSTEM MALFUNCTIONED A WX0A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 19 865GA 49998 DURING TAKEOFF ROLL WHEEL NOT TURNING LIGHT ILLUMINATED AT 70 KNOTS. NO DRAG FROM WHEELS WAS NOTED. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE AT LAS VEGAS. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED AND REPLACED ANTI-SKID CONT ROL BOX IAW M/M 32-43-00. OPERATIONAL CHECK NORMAL IAW MM 32-43-02, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007072500109 20070725 00109 2007 7 25 2007UALA02645 4 20070713 A 2565 LEVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR SLIDE STIFF A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 THE 1L ARMING LEVER IS VERY STIFF. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072500110 20070725 00110 NM 2007 7 25 2007UALA02646 1 20070715 A 2121 FAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN ODOR A UALA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 29 568UA 26674 OILY ODOR ON TAKEOFF AND CLIMB. PRETTY STRONG ODOR. TURNED THE RT RECIRCULATION FAN OFF. LESSENED THE ODOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072500111 20070725 00111 NM 2007 7 25 2007UALA02647 1 20070714 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 570UA 26678 EXTERIOR EMERGENCY LIGHT INOP AT DOOR 2R AND RT AFT OVERWING. [07-27-07] RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072500113 20070725 00113 NM 2007 7 25 2007UALA02649 1 20070714 A 3150 WARNING MESSAGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MLG UNKNOWN A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 543UA 25698 GEAR DISAGREE EICAS MSG AND LIGHT ILLUMINATED UPON SELECTING GEAR HANDLE DOWN. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072500114 20070725 00114 NM 2007 7 25 2007UALA02650 1 20070714 A 3350 POWER SUPPLY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 508UA 24744 MED 2R UPPER EMERGENCY EXIT SIGN INOP ALONG WITH EEL LIGHTING AT SEATS 2AB, 3AB, 9AB, 10AB & 11AB. [07-27-07] REPL ACED POWER SUPPLY. CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072500116 20070725 00116 NM 2007 7 25 2007UALA02651 1 20070715 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 652UA 25390 EXTERNAL EEL LIGHT JUST AFT OF LEFT WING IS INOP. [07-27-07] RELAMPED AND LIGHT CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072500124 20070725 00124 2007 7 25 MASA200700028 2 20070114 A 7261 TRANSFER TUBE DHAV DHC8 DHC8202 2809007 NM ENGINE OIL LEAKING A MASA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 448YV 448 ASH 7085 DEN - IN FLIGHT THE NR 1 ENGINE OIL PRESSURE WAS FLUCTUATING. THE FLIGHT CREW SHUT THE ENGINE DOWN IN FLIGHT A ND DECLARED AN EMERGENCY. MX FOUND AN OIL LEAK FROM THE STARTER TRANSFER TUBE. MX REMOVED AND REPLACED O-RINGS ON AGB TRANSFER TUBE. 2 H 7 2 4T RT A13NM 2007072500126 20070725 00126 SO 2007 7 25 C2XA07RI058 1 20070717 A 3350 110049 CHARGER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11548 145565 DURING A ROUTINE MX INSPECTION, IT WAS FOUND THAT THE AFT AISLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED NR 4 EMERGENCY BATTERY CHARGER. OPERATIONAL CHECK GOOD. A/C APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007072500128 20070725 00128 NM 2007 7 25 MWEA070160 1 20070720 A 2710 846D1007 MOTOR BOEING 717 717200 1383700 NM PRIMARY TRIM INOPERATIVE A MWEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 13 916ME 55178 PRIMARY TRIM IS WORKING INTERMITTENTLY. REMOVED AND REPLACED PRIMARY TRIM MOTOR. 2 L 7 2 4F TR A6WE 2007072500129 20070725 00129 NM 2007 7 25 KCSA071233 1 20070718 A 5412 BULKHEAD BOEING 747 7472B4B 138481B NM NACELLE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 APPROX 3 INCHES CRACK ON NAC STA 221 BULKHEAD WEB LT SIDE APPROX 12 INCHES ABOVE LOWER SPAR. 2 L 7 4 4F RT A20WE 2007072500130 20070725 00130 NM 2007 7 25 MWEA070155 1 20070713 A 3350 41B004AD07G3 BATTERY DOUG MD88 MD88 3023688 NM EMERGENCY LIGHTS INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 701ME 49760 COCKPIT EMERGENCY LIGHTS DO NOT ILLUMINATE WHEN SWITCHED TO ON. REMOVED AND REPLACED BATTERY. 2 L 7 2 4F RT A6WE 2007072500131 20070725 00131 NM 2007 7 25 MWEA070156 1 20070716 A 5220 2274640 HANDLE BOEING 717 717200 1383700 NM TAILCONE FAILED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 922ME 55184 AFT ENTRY DOOR EMERGENCY HANDLE FAILED TO DEPLOY DURING TEST. CLEANED TAIL CONE HANDLE RELEASE CLIPS. 2 L 7 2 4F TR A6WE 2007072500133 20070725 00133 NM 2007 7 25 CALA0700364 1 20070717 A 5340 ATTACH FITTING BOEING 737 7373T0 1384582 NM BS 312 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND A .5 INCH CRACK IN H-STRAP ON FUSELAGE STRUCTURE STA 312 L-1 DOOR LOWER HINGE ATTACH FITTING. A REPAIR WAS INSTALLED IAW ECRA 5311-01342. 2 L 7 2 4F RT A16WE 2007072500136 20070725 00136 NM 2007 7 25 ABXA070241 1 20070713 A 5630 140124135 WINDOW BOEING 767 767281 1385109 NM EMERGENCY EXIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 790AX 23140 STA: SJC, MAINTENANCE FOUND LEFT OVERWING EMERGENCY EXIT WINDOW OUTER WINDOW DAMAGED /CRACKED /MISSING. REMOVED AND RE PLACED LEFT OVERWING EXIT DOOR WINDOW IAW B767 MM 56-21-01-4. GROUND PRESSURE CHECK GOOD. 2 L 7 2 4F RT A1NM 2007072500138 20070725 00138 2007 7 25 QXEA200701158 4 20070716 A 3416 8220615312 TRANSCEIVER BOMBDR DHC8 DHC8402 1390042 NM ALTIMETER INOPERATIVE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 401QX 9585 9585 4031 LAX - ON FLIGHT 2442 RETURNED TO GATE, RADIO ALTIMETER NR 1 FAIL MESSAGE ON ED. MAINTENANCE REMOVED AND REPLACED NR 1 R ADIO ALTIMETER TRANSCEIVER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007072500139 20070725 00139 NM 2007 7 25 QXEA200701161 1 20070716 A 2150 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM A/C PACK UNKNOWN A QXEA O OTHER O OTHER CR CRUISE 1 NM 09 428QX 4160 MSO-ON FLIGHT 2340, CABIN PACK HOT CAUTION ILLUMINATED IN CRUISE FLIGHT. PERFORMED ABNORMAL CHECKLIST, LIGHT WENT OUT W HEN CABIN PACK WAS SELECTED OFF. MAINTENANCE COMPLIED WITH FIM TASK 21-60-00-810-801, NO FAULT FOUND. OPERATIONAL TEST ECS TEMP CONTROL. SYSTEM OPERATES NORMAL. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007072500142 20070725 00142 NM 2007 7 25 07FDEA02505 1 20070717 A 5753 VANE DOUG MD11 MD11F 3023600 NM TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 RIGHT WING OUTBOARD FLAP VANE UPPER SURFACE FOUND DELAMINATED. [07-30-07] COMPLIED WITH FEDEX E.A. 1-5750-112356. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007072500146 20070725 00146 NM 2007 7 25 07FDEA02507 1 20070718 A 5330 SKIN BOEING 757 7572B7 1384964 NM BS 1507 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 EXTERNAL FUSELAGE HAS A LARGE DENT AT STATION 1507 ON STRINGER 2R. FOUND TO BE OUT OF LIMITS PER SRM 53-00-01, FIG 101. CUT OUT DAMAGE ON SKIN PER SRM 53-00-01, FIG 201. FABRICATED REPAIR DOUBLER. TREATED AND PRIMED DOUBLER IAW SRM 51-2 0-01. 2 L 7 2 4F RT A2NM 2007072500150 20070725 00150 NM 2007 7 25 07FDEA02511 1 20070718 A 5311 6515922 FRAME BOEING 727 727227 1384078 NM ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 43378 21463 GALLEY DOOR (R-1) CUTOUT UPPER FWD SIDE STATION 380 FRAME CRACKED ON FORWARD SIDE BETWEEN STR 7R AND 8R. REMOVED FASTEN ERS IN DAMAGED AREA, CUTOUT DAMAGE, NDT VERIFIED NO DEFECTS. FABRICATED STRAP AND FILLER, TREATED, PRIMED REPAIR PARTS. INSTALLED REPAIR PARTS REF EA NR 7-5310-113937, SRM 51-30-2. 2 L 7 3 4F A3WE 2007072500151 20070725 00151 EU 2007 7 25 07FDEA02512 1 20070718 A 7830 THRUST REVERSER AIRBUS 300 A300B4622 3930401 EU NR 1 UNKNOWN A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 719FD 388 ON POWER-UP FOR TAKEOFF, NR 1 REVERSE UNLOCK LIGHT ILLUMINATED. EXTINGUISHED AFTER RETURNING THROTTLES TO IDLE. RETUR NED TO GATE. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 28JUL07 "MEL 78-30-01-C: ENGINE (IDEN TIFY 1 OR 2. NR 1 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION." [07-27-07] R & R RESSURE REGULATING AND SHUT OFF VALVE PER MM 78-31-05-4. REACTUATED TR PER MM 78-31-00-9. OP'S CHECKS NORMAL PER MM 78-31-00-5 AND PER A300. OKAY FOR SERVICE. 2 L 7 2 4F RT A35EU 2007072500152 20070725 00152 WP 2007 7 25 07FDEA02514 1 20070718 A 5313 LONGERON DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CLG WHEEL WELL CAVITY, CORROSION ON LONGERON END FITTING AT STA 1501 TO 1521, LONGERON 51L. REMOVED, FABRICATED AND INS TALLED NEW END FITTINGS IAW MD/DC10 SRM51-33-01 VOLII. 2 L 7 3 4F RT A22WE 2007072500153 20070725 00153 NM 2007 7 25 07FDEA02515 1 20070718 A 5322 SHEAR TIE BOEING 727 727227 1384078 NM BS 1010 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 AFT PIT STA 1010 BUTT JOINT SPLICE SHEAR TIE CORRODED BETWEEN STR 27-28R BLENDED CORROSION, ORIGINAL MATERIAL THICKNESS WAS .075" BETWEEN 0.001" AND 0.017 IS THE MATERIAL LOSS. OUT OF LIMITS REF SRM 53-30-01 FIG 1. FABRICATED AND INSTALLE D FILLER AND DOUBLER REF EA NR 7-5330-113263. 2 L 7 3 4F A3WE 2007072500154 20070725 00154 WP 2007 7 25 07FDEA02516 1 20070718 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP BS 1501-1521 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CLG WHEEL WELL CAVITY, CORROSION ON SKIN INTERIOR BETWEEN LONGERON 50R AND 49R, STA 1501 TO 1520. REMOVED AND REPLACED L51R END FITTINGS IAW MD/DC10 SRM 51-35-01 VOLII. SKIN REPLACED ON N/R N00616 EA8-5330-112939 (FUSELAGE SKIN REPAIR AT STA 1381- 1531, L48L-L48R REPAIR) W/O 36633,"SDR" 07-2147. 2 L 7 3 4F RT A22WE 2007072500155 20070725 00155 NM 2007 7 25 07FDEA02517 1 20070718 A 5330 146N3531 SKIN BOEING 757 7572B7 1384964 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 BULK CARGO - BILGE AREA, BS 1580, BETWEEN S27R AND 28R, SHEAR TIE AND SKIN EXFOLIATED. REMOVED AND REPLACED SHEAR TIE A S IT HAD 100 PERCENT MATERIAL LOSS IAW SRM 51-40-02. SHEAR TIE WAS FABRICATED ON MAE TRAVELER T7/689492 IAW SRM 51-10-0 1. REMOVED CORROSION FROM SKIN IAW SRM 53- 00-01. ORIGINAL MATERIAL THICKNESS 0.053, AFTER REWORK, 0.037. FOUND TO B E OUT OF LIMITS PER SRM 53- 00- 01, FIG 101. CUT OUT DAMAGED AREA AT STATION 1580 IAW SRM 53-00-01, FIG.201. FABRICA TED REPAIR DOUBLER FROM 2024 T3, 0.063, BATCH NR 1271859, IAW SRM 53-00-01, FIG 201 OF REPAIR NR 16. 2 L 7 2 4F RT A2NM 2007072000017 20070720 00017 2007 7 20 SWAA073455 4 20070713 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 768SW 30587 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007072000020 20070720 00020 NM 2007 7 20 SWAA073492 1 20070715 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM BS 383-391 S19R DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 606SW 27926 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CREASED BETWEEN BS 383 AND BS 391, STR 19R. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2007072000022 20070720 00022 NM 2007 7 20 SWAA073462 1 20070715 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 752 S24R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 752, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007072000023 20070720 00023 NM 2007 7 20 SWAA073458 1 20070714 A 5330 6545774 SKIN BOEING 737 7373T5 1384608 NM BS 740E S18R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 696SW 23064 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740E, STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007072000035 20070720 00035 NM 2007 7 20 USAA070533 1 20070716 A 5315 65C333671 FLOORBEAM BOEING 737 737401 1384701 NM BS 949, LBL 50 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 BS 949, LBL 50 AT FASTENER HOLES HAVE CORROSION. REMOVED & REPLACED WITH NEW PART PER SRM 51-10-02; CORR TASK C53-107-0 2; LEVEL 2, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007072000039 20070720 00039 NM 2007 7 20 USAA070529 1 20070716 A 5320 THRESHOLD BOEING 737 737401 1384701 NM BS 328-294 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 BS 328-BS 294 RT THRESHOLD HAS CORROSION. REMOVED DAMAGE, INSTALLED NEW PART PER SR 53-60-15 FIG 101; CORR LEVEL 2; TAS K C53-107-02, DEFECT SIZE: 12 INCHES. 2 L 7 2 4F RT A16WE 2007072000041 20070720 00041 NM 2007 7 20 UPS07450171 1 20070715 A 5321 FLOOR PANEL BOEING 747 747200 1384847 NM CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 3.5 INCH CRACK IN BULK CARGO COMPARTMENT FLOOR BETWEEN OBI BOXES. REPAIRED IAW SRM 51-40-02 FIG 1. 2 L 7 4 4F RT A20WE 2007072000048 20070720 00048 NM 2007 7 20 SWAA073481 1 20070715 A 5311 6546549 FRAME BOEING 737 7373H4 1384600 NM BS 767 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007072000056 20070720 00056 2007 7 20 SWAA073461 4 20070715 A 2565 65C16820 HOOK BOEING 737 7377H4 1384404 NM L1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 751SW 29803 L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2007072000065 20070720 00065 NM 2007 7 20 CALA0700358 1 20070715 A 5320 6545801512 STRUCTURE BOEING 737 7373T0 1384582 NM BS 227.8 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND CHORD CORRODED AT STA 227.8, RBL 9 TO LBL 9. A LOWER O/B CHORD REPAIR WAS INSTALLED IAW ECRA 5311-0134 0. 2 L 7 2 4F RT A16WE 2007072000070 20070720 00070 NM 2007 7 20 SWAA073482 1 20070715 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 639 S3R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007072000074 20070720 00074 NM 2007 7 20 SWAA073484 1 20070715 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 385 S2R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007072000076 20070720 00076 NM 2007 7 20 SWAA073452 1 20070713 A 3350 8100022704 CONNECTOR BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 253WN 32511 EEPLS INOP BETWEEN ROW 8 ABC AND ROW 12 ABC. FOUND LOOSE CONNECTOR, SECURED CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2007072000080 20070720 00080 EA 2007 7 20 VNAA0707003 1 20070707 A 5100 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE UNKNOWN DAMAGED A VNAA O OTHER O OTHER CL CLIMB 1 GL 05 226JS 7895 CREW REPORTED A LIGHTNING STRIKE ON CLIMBOUT OF CLT. CREW CONTINUED ON TO PHF WITHOUT INCIDENT. MAINTENANCE COMPLIED W ITH A VISUAL AND EN ROUTE LIGHTNING STRIKE INSPECTION IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 05-51-05-210-80 1 AND GENERAL MAINTENANCE MANUAL 2-5-18-C. MAINTENANCE COMPLIED WITH A DETAILED LIGHTNING STRIKE INSPECTION IN ACCORDAN CE WITH THE AIRCRAFT MAINTENANCE MANUAL 05-51-05-220-802. MAINTENANCE REPAIRED ALL DAMAGE. AIRCRAFT WAS RELEASED FOR S ERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007072000085 20070720 00085 EA 2007 7 20 COMA0760477 1 20070715 A 2420 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 1 MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 811CA 7380 FLIGHT 5609 - DURING TAKEOFF ROLL RECEIVED AN IDG NR 1 CAUTION. ABORTED TAKEOFF AND RETURNED TO THE GATE. DEFERRED NR 1 IDG PER MEL 24-11-01-1. 2 L 7 2 4F RT A21EA 2007072000088 20070720 00088 NM 2007 7 20 SWAA073501 1 20070715 A 3350 300432 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 420WN 29825 DURING SCHEDULED MV2 CHECK, FOUND LT FWD EXTERIOR EMERGENCY LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2007072000104 20070720 00104 NM 2007 7 20 SWAA073498 1 20070715 A 5710 BAC1505100545T6 SHEAR TIE BOEING 737 7373H4 1384600 NM RT WING BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED SPV CHECK, FOUND RT WING SHEAR TIE BROKEN AT RIB 505, FWD SPAR. REMOVED AND REPLACED SHEAR TIE PER BAC DRAWING. 2 L 7 2 4F RT A16WE 2007072000110 20070720 00110 NM 2007 7 20 SWAA073509 1 20070716 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 719SW 27853 DURING SCHEDULED HC2 CHECK, CENTER CABIN EMERGENCY LIGHTS BATTERY PACK FAILED THE CAPACITY TEST. REMOVED AND REPLACED B ATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007072000111 20070720 00111 NM 2007 7 20 SWAA073510 1 20070716 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 719SW 27853 DURING SCHEDULED HC2 CHECK, FWD CABIN EMERGENCY EXIT LIGHTS BATTERY PACK FAILED THE CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007072000116 20070720 00116 NM 2007 7 20 USAA070555 1 20070717 A 5511 RIB BOEING 737 737401 1384701 NM RT STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 RIGHT STAB L/E NOSE RIB CUTOUT, 139 INCHES FROM I/B END. BLENDED OUT DAMAGE & RE-INSTALLED RIB PER SRM 55-10-09, FIG 10 1, DEFECT SIZE: .080 INCH. 2 L 7 2 4F RT A16WE 2007072000117 20070720 00117 NM 2007 7 20 USAA070554 1 20070717 A 5512 RIB BOEING 737 737401 1384701 NM RT STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 RIGHT STAB L/E, NOSE RIB FWD CUTOUT, 167 INCHES FROM I/B END. BLENDED DAMAGE & RE-INSTALLED PART PER SRM 55-10-09, FIG 101, DEFECT SIZE: .063 INCH. 2 L 7 2 4F RT A16WE 2007072000126 20070720 00126 NM 2007 7 20 UPS07550187 1 20070718 A 2750 FLAP SYSTEM BOEING 757 75724APF 1384969 NM TE FLAPS INOPERATIVE A IPXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 411UP 23851 DURING THE APPROACH FLAPS WERE AT 20 DEGREES. WHEN F/O CALLED FOR FLAPS 30, THE T/E FLAP DISAGREE LIGHT ILLUMINATED & T HE FLAPS WOULD NOT EXTEND BEYOND 20. [07-20-07] REMOVED AND REPLACED FLAP/SLAT ELECTRONIC UNIT IN REF TO M/M 27-51- 01-2. OPS CHECKS GOOD. NO FURTHER FAULTS NOTED. 2 L 7 2 4F RT A2NM 2007072000130 20070720 00130 NM 2007 7 20 USAA070550 1 20070717 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 540 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 FLOOR SUPPORT, STA 540, LBL 0 TO LBL 25 HAS CRACK. REPLACED FLOOR SUPPORT PER SRM 51-10-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007072000131 20070720 00131 NM 2007 7 20 USAA070549 1 20070717 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 328 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 STA 328 RBL 47 FLOORBEAM CRACKED. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-10-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007072000136 20070720 00136 EA 2007 7 20 COMA0760488 1 20070716 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FS 202.75 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 965CA 27846 7131 FORWARD PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE. REPAIRED IAW REO 601R-53-11-563. 2 L 7 2 4F RT A21EA 2007072000139 20070720 00139 EA 2007 7 20 COMA0770038 1 20070715 A 2730 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA PITCH FEEL MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 371CA 10082 FLIGHT 5881 - EN ROUTE ATL-MDW RECEIVED A PITCH FEEL CAUTION MESSAGE. FLIGHT DIVERTED TO ORD. PERFORMED RESET OF SSCU 1 AND 2, PERFORMED AN OPERATIONAL CHECK OF PITCH FEEL UNITS, NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2007072000144 20070720 00144 NM 2007 7 20 2007UALA02485 1 20070709 A 5270 WARNING HORN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L3 DOOR FALSE ACTIVATION A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 182UA 25279 DOOR 3L EMERGENCY EVAC HORN SOUND IS CONTINUOUS DURING OP CHECK, SHOULD BE INTERMITTENT. [08-08-07] REPAIRED, CLEAN ED CONNECTIONS AND REMOUNTED EEC PANEL AT DOOR 3L. OP CHECKED OK . 2 L 7 4 4F 4 F RT A20WE E24NE 2007072000151 20070720 00151 NM 2007 7 20 2007UALA02492 1 20070709 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 DOOR 2R EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED, OP CHECKED OK REF MM 33-51-10. [07-27-07] RELAMPED, OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072000160 20070720 00160 NM 2007 7 20 2007UALA02501 1 20070708 A 2741 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE STAB TRIM UNKNOWN A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 512UA 24809 STAB TRIM WILL NOT TRIM IN NOSE DOWN DIRECTION WITH CENTER STAB TRIM CUTOUT SWITCH IN NORMAL AND RIGHT STAB TRIM SWITCH IN CUTOUT POSITION. TRIMS NORMALLY WITH TRIM LEVERS. [08-08-07] STABILIZER NOSE DOWN OPERATION STARTED WORKING OK AY AFTER CYCLING STABILIZER WITH ALTERNATE LEVERS. IN THE ALTERNATE ELECTRIC STAB TRIM MODE, THE UP LIMIT IS RESTRICTED TO APPROX.+3.85 DEGREES. PASSED MCDP TEST 65. REPLACED STAB TRAVEL LIMIT AND POSITION TRANSMITTER MODULE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072000165 20070720 00165 NM 2007 7 20 2007UALA02506 1 20070707 A 3350 SWITCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 EMERGENCY LIGHTING TEST SWITCH AT 1L AND 2R DOES NOT SWITCH ON FLOOR LIGHTING. [08-08-07] OPERATED EMERGENCY LIGHTIN G TEST SWITCH AT 1L AND 2R. OPS CK OK. CANNOT DUPLICATE PROBLEM. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072000173 20070720 00173 NM 2007 7 20 2007UALA02513 1 20070706 A 5313 STRINGER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE BS 793 S33R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 781UA 26945 DAMAGE REPORTED BY CATERING TRUCK ADJACENT TO R2 DOOR. DAMAGE IS AT STA 793, ON STRINGER S-33R. [08-08-07] DOUBLER INSTALLED & INSPECTED. AIRCRAFT OK FOR SERVICE. DAMAGE CAUSED BY CONTACT WITH CATERING TRUCK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007072000176 20070720 00176 NM 2007 7 20 2007UALA02516 1 20070707 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 WALL EXIT EEL SIGN INOP AT DOOR 1R. REPLACED BATTERY PACK, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072000185 20070720 00185 NM 2007 7 20 2007UALA02525 1 20070710 A 2841 INDICATOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUEL QTY INOPERATIVE A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 774UA 26936 FUEL QTY INDICATOR BLANKING. [08-08-07] ACCOMPLISHED TANK ENTRY & REPLACED FUEL PROBES. NR 3 RT CENTER AND NR 3 LT C ENTER. RT MAIN NR 19 AND 20. AND LT MAIN NR 19 AND NR 20 PE. CHECKED VALUES AFTER INSTALLATION AND ALL ACCEPTABLE. AIR CRAFT READY FOR SERVICE. SEVERAL PROBES WERE REPLACED IN ORDER TO SOLVE BLANKING. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007072300007 20070723 00007 NM 2007 7 23 2007UALA02527 1 20070711 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 905 S21L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 351UA 24319 EXT SKIN STA 905 FWD OF BUTT JOINT 3EA HOLES ELONGATED JUST ABOVE STR 21L. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR DOUBLER & TRIPLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007072300027 20070723 00027 NM 2007 7 23 2007UALA02547 1 20070710 A 2432 CHARGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MAIN BATTERY INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 567UA 26673 MAIN BATTERY CHARGER WILL NOT ERASE ON ECS MSG. [08-08-07] REPLACED MAIN BATTERY AND MAIN BATTERY CHARGER 2 L 7 2 4F 4 F RT A2NM E17NE 2007072300035 20070723 00035 NM 2007 7 23 UPS07M50179 1 20070717 A 3350 SWITCH DOUG MD11 MD11F 3023600 NM EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP 48576 INSPECTION TYPE:N/A EMERGENCY LIGHT BATTERY 1 LOW ALERT ON EMERGENCY LIGHTS TEST. RESET EMERGENCY LIGHT SWITCH. OPS CH ECK OK. REF 33-50-00. 2 L 7 3 4F RT A22WE 2007072300038 20070723 00038 NM 2007 7 23 2007UALA02556 1 20070111 A 5523 D55982020202203 TAB AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE RT ELEVATOR BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 834UA 1420 LOWER ANTI-ROTATION TAB AT THE RT ELEVATOR HINGE FITTING III WAS FOUND BROKEN OFF. THE UPPER TAB IS INTACT. L-ANGLE FA BRICATED AND INSTALLED TO REPLACE A DAMAGED ANTI-ROTATION TAB. INSPECTION OF THE REWORKED AREA SHOWED NO CRACK INDICATI ONS. MAJOR REPAIR ACCOMPLISHED PER EVA-70021. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072300043 20070723 00043 NM 2007 7 23 2007UALA02561 1 20070710 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 780UA 26944 EEL LIGHT ON SIDE OF SEAT 1E MISSING. [07-27-07] REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007072300062 20070723 00062 NM 2007 7 23 2007UALA02573 1 20070711 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 20UAÊ 29166 EMERGENCY LIGHT INOP AT 5E AFT. [07-27-07] SECURED CONNECTOR AT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072300065 20070723 00065 EU 2007 7 23 2007UALA02576 1 20070712 A 5340 ATTACH ANGLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 424UA 506 LEFTHAND & RIGHTHAND WHEEL WELL AREAS, BELLY FAIRING SUPPORT BRACKET UPPER ATTACH ANGLE IS CRACKED AT FRAME 46. MAJOR R EPAIR ACCOMPLISHED: REPLACED ANGLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072300068 20070723 00068 EU 2007 7 23 2007UALA02579 1 20070711 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 490UA 1728 CREW OXYGEN LOW. SERVICED O2 SYSTEM, NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072300087 20070723 00087 NM 2007 7 23 07FDEA02498 1 20070717 A 3260 656021123 ACCESSORY UNIT BOEING 727 727233 138408A NM MLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 223FE 20935 DURING NORMAL CLIMB-OUT, THE LANDING GEAR LEVER WAS RAISED TO THE UP POSITION AFTER GEAR UP THE RIGHT MAIN GEAR INDICATE D GREEN AND RED LIGHTS FIRST OFFICER WAS FLYING AND CONFIRMED THAT THERE WAS SIGNIFICANT DRAG ON THE RIGHT SIDE OF THE A IRCRAFT. REPLACED LANDING GEAR ACCESSORY UNIT, AND THE TEST WAS REPEATED, WITH POSITIVE RESULTS. JACKED A/C REF 727-20 0 MM 07-11-000-2, RETRACTED AND EXTENDED LANDING GEAR MULTI. TIMES WITH NO FAULT, SYSTEM OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2007072300088 20070723 00088 NM 2007 7 23 UPS07M50186 1 20070717 A 3350 LIGHT DOUG MD11 MD11F 3023600 NM EMERGENCY EXIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP 48576 INSPECTION TYPE:N/A EMERGENCY LIGHTS TEST FAILED D354644 ASSIGNED. T/S PER FIM 33-51-02-00 & WDM 33-51-01, RESEATED & RE SECURED R2-5700 (RELAY) & PERFORMED EMERGENCY LIGHT SYSTEM TEST. PASSED PER MM 33-50-00-5. THIS CLEARS M354644 AND PLACA RD REMOVED. 2 L 7 3 4F RT A22WE 2007072300099 20070723 00099 NM 2007 7 23 HNAA0700146 1 20070706 A 5320 85310346104 SUPPORT ANGLE DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 839EX 226 HORIZONTAL ANGLE AT TOP OF RIGHT NLG WELL TRUNNION WEB IS CRACKED WHERE IT ATTACHES BETWEEN THE WEB AND VERT TRUNNION MO UNT BEAM. 2 H 7 2 4T RT A13NM 2007072300100 20070723 00100 EA 2007 7 23 TRAX200700957 1 20070706 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 333 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 FRAME AT FS 333.00 HAS CORROSION AT STR 27. 2 L 7 2 4F RT A21EA 2007072300101 20070723 00101 EA 2007 7 23 TRAX200700975 1 20070709 A 5310 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA BS 472 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 832AS 7243 SUSPECTED CRACK ON THE UPPER I/B RADIUS OF BOTH TAB FITTINGS AT FS 472 RBL 9. PERFORMED LPI ON THE FS 472 RBL 9 UPPER R ADIUS OF BOTH I/B AND O/B TAB FITTINGS IAW NDTM 51-20-08. FS 472 RBL 9 UPPER RADIUS OF BOTH I/B AND O/B TAB FITTINGS, A PPROX .5 INCH. STARTED REMOVING HI-LOKS IAW CRJ SRM 51-42-21. REMOVED BOTH BATH TUB FITTINGS FROM RBL 9. LOCATED BOTH BATH TUB FITTINGS AT FS 472 RBL 9. OK TO INSTALL I/B FITTING. STARTED INSTALLING I/B FITTING IAW CRJ 200 SRM 51-42-21 . STARTED INSTALLING I/B FITTING IAW CRJ 200 SRM 51-42-21. COMPLETED INSTALLATION OF I/B FITTING IAW CRJ 200 SRM 51-42 -21. INSTALLED O/B FITTING IAW CRJ 200 SRM 51-42-21. SUPPLEMENTAL - SDR CLOSED 07/16/07. 2 L 7 2 4F RT A21EA 2007072300102 20070723 00102 NM 2007 7 23 HNAA0700149 1 20070712 A 2910 65960 VALVE DHAV DHC8 DHC8102 2809003 NM HYD SYSTEM MALFUNCTIONED A HNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 07 933HA 134 AT 20 MILES OUT OF MHT, THE FLIGHT CREW SAW THE NUMBER TWO HYDRAULIC QUANTITY DROP TO TWO QUARTS. ALSO, NOTICED THE NUM BER ONE HYDRAULIC QUANTITY DROP TO ONE AND ONE HALF QUARTS. THE NUMBER TWO HYDRAULIC QUANTITIES THEN STARTED DROPPING B ELOW TWO QUARTS AMOUNT. THE CREW SLOWED THE AIRCRAFT DOWN AND LOWERED THE LANDINTG GEAR AND FLAPS. AN EMERGENCY WAS DE CLARED AND DIVERTED IN TO BDL. THE FLIGHT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED UNLOADING VALVE FOR OUTBOARD R IGHT. SPOILER OPS AND LEAK CHECK GOOD. 2 H 7 2 4T RT A13NM 2007072300103 20070723 00103 SO 2007 7 23 C2XA07RI056 1 20070712 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO CARGO BAY NO TEST A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17138 6134 23 145727 DURING ROUTINE INSPECTION, MX DISCOVERED FWD BAGGAGE SMOKE DETECTOR TO NOT TEST PROPERLY. MAINTENANCE REMOVED AND REPLA CED FWD BAGGAGE SMOKE DETECTOR. OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007072300104 20070723 00104 NM 2007 7 23 HNAA0700150 1 20070715 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM CARGO BAY FALSE ACTIVATION A HNAA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 EA 07 812EX 312 SMOKE WARN LIGHT ILLUMINATED IN FLT & ON APPROACH INTO LANCASTER GOING ON & OFF INTERMITTENTLY, WITH ASSC MASTER WARN LI GHT. INSP BAG BAY, NO FIRE OR SMOKE DETECTED. REMOVED AND REPLACED FWD AND AFT CEILING BAG BAY SMOKE DET'S AS REQUIRED . 2 H 7 2 4T RT A13NM 2007072300105 20070723 00105 EA 2007 7 23 TRAX200700992 1 20070706 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 559-621 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 ALL CARGO FLOOR TRACKS AND TIE DOWNS ARE CORRODED BETWEEN FS 559.00 AND FS 621 AT LBL 9 AND LBL 27. 2 L 7 2 4F RT A21EA 2007072300106 20070723 00106 EA 2007 7 23 TRAX200700993 1 20070712 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA SPOILERS ILLUMINATED A ASOA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 908EV 7654 EN ROUTE RECEIVED SPOILERON AND FLT SPOILER CAUTION MSG FOLLOWED QRH. EMERGENCY DECLARED BY TOWER. EMERGENCY EQUIPMENT ON STANDBY. 2 L 7 2 4F RT A21EA 2007072300107 20070723 00107 EU 2007 7 23 TRAX200700994 1 20070713 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 ASD EMERGENCY LIGHT IS INOP. 2 H 7 2 4T RT 2007072300108 20070723 00108 EA 2007 7 23 TRAX200700995 1 20070713 A 3350 BATTERY CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS WEAK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 753EV 10169 NR 1 EMERGENCY BATTERY IS WEAK. 2 L 7 2 4F RT A21EA 2007072300109 20070723 00109 EA 2007 7 23 TRAX200700996 1 20070713 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 FWD F/A FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007072300110 20070723 00110 EA 2007 7 23 TRAX200700997 1 20070713 A 5260 DOOR CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 880AS 7606 ASD HARD TO CLOSE. 2 L 7 2 4F RT A21EA 2007072300111 20070723 00111 EA 2007 7 23 TRAX200700998 1 20070713 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA SPOILERS ILLUMINATED A ASOA O OTHER J WARNING INDICATION DE DESCENT 1 SO 27 908EV 7654 IN FLIGHT RECEIVED SPOILERS AND FLIGHT SPOILERS CAUTION MSG. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007072300112 20070723 00112 EA 2007 7 23 TRAX200700999 1 20070710 A 5310 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 338 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 832AS 7243 PAX DOOR AFT FRAME MEMBER AT FS 338.90 IS CRACKED. REF REO 601R-52-11-402 FOR POSSIBLE REPAIR. [07-26-07] REPAIRED I AW ALL SRMS AND EO`S. 2 L 7 2 4F RT A21EA 2007072300115 20070723 00115 SO 2007 7 23 RAIA00707024 1 20070711 A 3350 1317 BULB EMB 145 EMB145 3260210 SO EMERGENCY LIGHT BURNED OUT A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 804HK 145082 PRE FLT NR 3542 - STL - EMERGENCY LIGHT MAIN DOOR FLOOD LIGHT INOP. MAINTENANCE RELAMPED BULB, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007072400016 20070724 00016 WP 2007 7 24 AALA20071215 1 20070629 A 4990 OIL SYSTEM DOUG DC9 DC982 3022082 WP APU LEAKING A AALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 481AA 49656 DFW - INFLIGHT T848/29JUN - CREW REPORTED SMOKE IN CABIN. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND AUXILIAR Y POWER UNIT (APU) LEAKING OIL. REPLACED APU ON 01 JUL 2007 AT DFW. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400025 20070724 00025 EU 2007 7 24 AWXA200700844 1 20070713 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHTS FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 636AW 54176 7273 098 LAS - EEL - LOG NR 7811308 - CREW REPORTED EMERGENCY EXIT SIGNS, LEFT OVERWING AND MID CABIN OVERHEAD ARE INOP. MX REPL ACED THE POWER SUPPLY UNIT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007072400027 20070724 00027 NM 2007 7 24 DHL2007753001 1 20070715 A 5753 SKIN BOEING 727 727223 1384074 NM TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 57923 22468 SMALL AREA OF DELAMINATION ON RT I/B MID FLAP T/E. CUT OUT DELAMINATED AREA ON RT I/B MID FLAP, APPROX 4 1/4" BY 5". FABBED FILLER APPROX 4 1/4" BY 5" AND DOUBLER APPROX 3" BY 4 1/4" FROM 7075-T6 .016" PO NR 9003988. CLEANED, PREPPED, P RIMED, BONDED, CLEANED, TREATED, PRIMED AND SEALED EDGES IAW B727 SRM 57-50-2 FIG 3 AND 51-40-24 FIG 3. 2 L 7 3 4F A3WE 2007072400033 20070724 00033 NM 2007 7 24 DL757070907 1 20070713 A 5330 143N347111 SKIN BOEING 757 757232 1384965 NM BS 528 S26L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 696DA 29728 FUSELAGE SKIN HAS A DENT/GOUGE AT STA 528 BETWEEN S-26L AND S-27L. THE DAMAGED FUSELAGE SKIN WAS CUTOUT AND AN EXTERNAL DOUBLER WAS INSTALLED. 2 L 7 2 4F RT A2NM 2007072400034 20070724 00034 2007 7 24 DL764070908 4 20070713 A 3444 HG2050AC07 ADIRU BOEING 767 767432ER 1385134 NM RIGHT INOPERATIVE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 838MH 29711 RIGHT AIR DATA FAILED. REPLACED RT ADIRU. ALL DATA BACK AND NORMAL. 2 L 7 2 4F RT A1NM 2007072400045 20070724 00045 WP 2007 7 24 NWAA072489929 1 20070706 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8923E 45838 DURING "H" CHECK, FOUND CRACK IN FUSELAGE SKIN AT AFT UPPER CORNER OF FORWARD SERVICE DOOR JAMB . REPAIRED PER EA 99-20 9601 SECTION I SECTION II TO BE ACCOMPLISHED ON OR BEFORE TWO YEARS OR 3,000 CYCLES AFTER SECTION I ACCOMPLISHMENT. 2 L 7 2 4F A6WE 2007072400049 20070724 00049 NM 2007 7 24 HALA0700284 1 20070714 A 2420 IDG BOEING 767 76733A 1385209 NM RIGHT INOPERATIVE A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 581HA 28141 ETOPS SIGNIFICANT SYSTEM, RIGHT IDG OUT AND RISE TEMPERATURES VARY RAPIDLY AND ERRATICALLY FROM 0 TO 140. SERVICED RT I DG TO PROPER LEVEL. NO MSG ON BPCU. RAN ENG, OPS NML PER FIM 24-20-00. 2 L 7 2 4F RT A1NM 2007072400057 20070724 00057 NM 2007 7 24 DHL2007784503 1 20070708 A 5320 WEB BOEING 727 727227 1384078 NM BS 1243 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 BS 1243, WL 196, RBL 21, RT TORQUE BOX UPPER HOLE CRACKED AT 12 O`CLOCK POSITION. CUT OUT DAMAGED AREA DIM .25 BY .25 I AW B727 SRM 51-40-2, FIG 1. FABRICATED DOUBLER REPAIR, MATERIAL USED 7075T6, 040, 3.8 BY 3 IAW B727 SRM 51-40-2, FIG 1 AND 53-10-2, FIG 6. TREATED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 51-10-2, 51-40-2, FIG 1 AND 53-30-2. 2 L 7 3 4F A3WE 2007072400058 20070724 00058 NM 2007 7 24 HALA0700292 1 20070718 A 3244 416K421 TIRE BOEING 717 717200 1383700 NM NR 1 DAMAGED A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 479HA 747 747 55124 RIGHT AT RETRACTION IN HNL, NOTICED A SLIGHT NOISE AT LIFT OFF, NO OTHER INDICATION NOTICED. AFTER PARKING IN LIHUE RAM P NOTICED THE NR 1 TIRE SHREDDED. LOOKS LIKE IT WENT THRU THE NR 1 ENGINE. REPLACED NR 1 MAIN TIRE BORESCOPE INSP OF N R 1 AND 3 LP COMP BLADES, NO DAMAGE NOTED. 2 L 7 2 4F TR A6WE 2007072400062 20070724 00062 NM 2007 7 24 DHL2007784502 1 20070708 A 5753 652163479 SKIN BOEING 727 727227 1384078 NM LEFT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 LT INBD AFT FLAP LE CRACKED AT NR 3 TRACK CUTOUT, LWBL 112. STOP DRILLED CRACK AT LT INBD AFT FLAP AT NR 3 TRACK CUTOUT , LWBL 112 IAW B727 SRM 57-50-4, FIG 1. HFEC VERIFIED CRACK STOPPED IAW B727 NDTM 51-00-00 PT 6, FIG 23. FABRICATED RE PAIR DOUBLER, MATERIAL USED 7075T6, 050, 3 BY 4 IAW B727 SRM 57-50-4, FIG 1 AND 57-20-2, FIG 3. TREATED, PRIMED AND INS TALLED REPAIR IAW B727 SRM 51-10-2, 51-30-2 AND 57-50-4, FIG 1. 2 L 7 3 4F A3WE 2007072400063 20070724 00063 NM 2007 7 24 DHL2007784501 1 20070708 A 5330 SKIN BOEING 727 727227 1384078 NM BS 720 S19R GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 FUSELAGE SKIN GOUGED AT BS 720 PLUS 15, STR 19R. REMOVED GOUGED FILLER AT FUSELAGE SKIN AT PREVIOUS REPAIR. FILLER DIM . 5.5 BY 2.75 IAW B727 SRM 53-30-3, FIG 14. FABRICATED NEW FILLER, MATERIAL USED 2024T3, 063, 5.5 BY 2.75 IAW B727 SRM 53-30-3, FIG 14 AND 53-30-2, FIG 2. TREATED, PRIMED AND INSTALLED FILLER IAW B727 SRM 51-10-2, 53-30-3, FIG 14 AND 53- 30-2. 2 L 7 3 4F A3WE 2007072400066 20070724 00066 WP 2007 7 24 AALA20071297 1 20070713 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7547A 53029 LGA - EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400071 20070724 00071 NM 2007 7 24 AALA20071259 1 20070706 A 2613 ELEMENT BOEING 737 737823 13844BZ NM OVERHEAT INOPERATIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 390AN 29529 DFW INFLIGHT T282/06JUL - CREW REPORTED WING TO BODY OVERHEAT INDICATION DURING CLIMB. RETURNED TO DFW AND LANDED WITHO UT INCIDENT. REPLACED LEFT WING LEADING EDGE OUTBOARD OVERHEAT ELEMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007072400080 20070724 00080 NM 2007 7 24 AWXA200700845 1 20070710 A 5511 183N150322 RIB BOEING 757 757225 1384959 NM HORIZONTAL STAB CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - NR 5956488, CRACKED LEFT HORIZONTAL STABILIZER TRAILING EDGE RIB WEB, STABILIZER STATI ON 244.501. REPLACED LEFT HORIZONTAL STABILIZER TRAILING EDGE RIB WEB, STABILIZER STATION 244.501 IAW B757-200 SRM 51-4 0-02. 2 L 7 2 4F RT A2NM 2007072400092 20070724 00092 WP 2007 7 24 AALA20071288 1 20070713 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 208AA 49159 DFW - EMERGENCY LIGHT AT SEAT ROW 18D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400098 20070724 00098 NE 2007 7 24 AALA20071277 2 20070710 A 7320 EEC BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4 54555 NE LEFT ENGINE FAILED A AALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SW 21 692AA 26972 31118 ORD INFLIGHT T9653/10JUL - ON TAKE OFF LEFT BLEED, LEFT ELECTRONIC ENGINE CONTROL, AND LEFT ELECTRICAL LOAD CONTROL FAIL ED. LEFT ENGINE FAILED ON APPROACH. LANDED ORD WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE ON 12 JUL AT ORD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2007072400103 20070724 00103 NM 2007 7 24 AALA20071284 1 20070712 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 369AA 25196 JFK - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 21C. RELAMPED EMERGENCY LIGHT AT OVERHEAD SEAT ROW 21C. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007072400104 20070724 00104 NM 2007 7 24 AALA20071285 1 20070712 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 936AN 29532 DFW - EMERGENCY EXIT FLOOD LIGHT AT SEAT ROW 14A INOPERATIVE. RELAMPED EMERGENCY EXIT FLOOD LIGHT AT SEAT ROW 14A. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007072400106 20070724 00106 WP 2007 7 24 AALA20071293 1 20070713 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 208AA 49159 DFW - EMERGENCY LIGHT AT SEAT ROW 15D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400107 20070724 00107 WP 2007 7 24 AALA20071291 1 20070713 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 208AA 49159 DFW - EMERGENCY LIGHT AT SEAT ROW 8D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 8D. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400108 20070724 00108 WP 2007 7 24 AALA20071292 1 20070713 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 208AA 49159 DFW - EMERGENCY LIGHT AT SEAT ROW 9D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 9D. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400110 20070724 00110 EU 2007 7 24 TRAX200701003 1 20070715 A 3350 SIGN AEROSP ATR72 ATR72 EU EMERGENCY LIGHT MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 EMERGENCYY EXIT SIGN MISSING THAT GOES TO THE LEFT OF THE SERVICE DOOR IS MISSING. 2 H 7 2 4T RT 2007072400111 20070724 00111 2007 7 24 NOCA14207 4 20070718 A 2565 D30654122 SLIDE BOEING 757 75728A 1384976 NM L1 DOOR UNWANTED DEPLOY A NOCA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 EA 15 750NA 26277 L1 SLIDE DEPLOYED ON GROUND. REMOVED AND REPLACED L1 SLIDE AS PER MM 52-11-33 SYSTEM CHECK OK ACCOMPLISHED EO 757-25-19 9. 2 L 7 2 4F RT A2NM 2007072400112 20070724 00112 NM 2007 7 24 NOCA13907 1 20070718 A 3350 767 BULB BOEING 757 75728A 1384976 NM EMERGENCY LIGHT INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 755NA 30043 EXTERIOR DOOR L4 AND R4 EMERGENCY LIGHTS ARE INOP. RELAMPED EMERGENCY LIGHTS. 2 L 7 2 4F RT A2NM 2007072400113 20070724 00113 NM 2007 7 24 NOCA13807 1 20070712 A 3350 399783000 SIGN BOEING 757 75728A 1384976 NM EMERGENCY LIGHT BROKEN A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 752NA 28174 EMERGENCY EXIT SIGN AT L1 DOOR IS BROKEN. REPLACED EMERGENCY EXIT SIGN AT L1 DOOR. 2 L 7 2 4F RT A2NM 2007072400114 20070724 00114 NM 2007 7 24 NOCA14007 1 20070717 A 3350 767 BULB BOEING 767 767304 NM EMERGENCY LIGHT INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 769NA 28039 L4 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED L4 EMERGENCY LIGHT, OPS NORMAL. 2 L 7 2 4F RT A1NM 2007072400115 20070724 00115 NM 2007 7 24 NOCA14107 1 20070716 A 2612 285T03856 MODULE BOEING 767 76739H 1385311 NM FIRE DETECTION MALFUNCTIONED A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 760NA 26257 FIRE WARNING BELL INOP DURING WHEEL WELL TEST AND FIRE/OVERHEAT TEST. REMOVED AND REPLACED MASTER WARNING AND BELL/CHIM E CARD MODULES PER MM 31-51-04, OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 2007072400116 20070724 00116 SO 2007 7 24 C2XA07TY039 1 20070718 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14116 145672 EMERGENCY LIGHT ABOVE SERVICE DOOR INOP. REMOVED AND REPLACED NR 3 INVERTER IAW EMB 145 XR AMM 33-50-00, OPS CHECK GOOD . AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT 2007072400118 20070724 00118 NM 2007 7 24 SCNA07007 1 20070717 A 2560 SEAL BOEING 737 7378Q8 13844BX NM BREATING EQUIP BROKEN A SCNA O OTHER O OTHER NR NOT REPORTED 1 GL 15 805SY 30032 FLIGHT ATTENDANT FOUND THE AFT PROTECTIVE BREATHING EQUIPMENT SEAL BROKEN. THE PBE WAS NOT USED AND MAINTENANCE INSPECT ED AND REPLACED THE SEAL ON THE PBE. 2 L 7 2 4F RT A16WE 2007072400124 20070724 00124 NM 2007 7 24 KCSA071235 1 20070718 A 5313 STRINGER BOEING 747 7472B4B 138481B NM BS 600-620 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA 600 TO 620 STR 44R HAS CORROSION. 2 L 7 4 4F RT A20WE 2007072400125 20070724 00125 NM 2007 7 24 KCSA071236 1 20070718 A 5313 STRINGER SPLICE BOEING 747 7472B4B 138481B NM BS 585 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA 585 STR 45R HAS CORROSION ON SPLICE. 2 L 7 4 4F RT A20WE 2007072400126 20070724 00126 NM 2007 7 24 KCSA071237 1 20070718 A 5313 STRINGER BOEING 747 7472B4B 138481B NM BS 790 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA 790 STR 43L CORRODED. 2 L 7 4 4F RT A20WE 2007072400127 20070724 00127 NM 2007 7 24 KCSA071238 1 20070719 A 5330 SKIN BOEING 747 7472B4B 138481B NM BS 740 BULGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA 740 BUTT SPLICE STR 44R LAP SEAM HAS SKIN PILLOWING. 2 L 7 4 4F RT A20WE 2007072400131 20070724 00131 2007 7 24 BB07053 4 20070717 A 3442 20414440401 ANTENNA BOEING 757 757225 1384959 NM WX RADAR SYS FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 916UW 51730 139 22192 FLIGHT 807, CLT-CUN: FLIGHT RETURNED TO CLT DUE TO INOPERATIVE WEATHER RADAR FAILURE. MAINTENANCE REPLACED THE WEATHER RADAR ANTENNA. NO FURTHER FAULTS. 2 L 7 2 4F RT A2NM 2007072400135 20070724 00135 EA 2007 7 24 TRAX200701015 1 20070717 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 858AS 7417 CAPT'S, F/O'S, AND F/A'S FLASHLIGHT INOP AND DIM. 2 L 7 2 4F RT A21EA 2007072400136 20070724 00136 EA 2007 7 24 TRAX200701016 1 20070717 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 979EV 7737 F/A'S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007072400137 20070724 00137 SO 2007 7 24 C2XA07ON012 1 20070712 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NLG MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16546 01037 145562 FLT 096 - ONT TO ONT - DURING CLIMB FLIGHT CREW HAD A MESSAGE ON EICAS STATING LANDING GEAR AIR/GND FAIL. THE AIRCRAFT RETURNED TO ONT WHERE IT LANDED WITH OUT INCIDENT. MX REMOVED AND REPLACED RIGHT AIR GROUND WOW SWITCH AND HARNESS, CLE ANED NOSE PROX SWITCHES OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED TO RETURNED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007072400138 20070724 00138 EA 2007 7 24 TRAX200701022 1 20070718 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002C10 1390015 EA FIRE BOTTLE ILLUMINATED A ASOA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 27 750EV 10161 NR 1 AND 2 ENG FIRE BOTTLE LOW CAUTION MSGS. 2 L 7 2 4F RT A21EA 2007072400139 20070724 00139 EA 2007 7 24 TRAX200701023 1 20070718 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 F/A FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007072400140 20070724 00140 EA 2007 7 24 TRAX200701024 1 20070718 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 928EV 8006 F/A'S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007072400141 20070724 00141 EU 2007 7 24 TRAX200701025 1 20070718 A 2910 HYDRAULIC SYSTEM AEROSP ATR72 ATR72 EU LOW A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 633AS 344 AFTER TAKEOFF OUT OF ATL GOT A BLUE HYDRAULIC SYSTEM LOW LEVEL. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. EM ERGENCY EQUIPMENT ON STANDBY. FLT 4437 DEL 15 MINS. FLTS 4697, 4837(X2), 4181, 4624, 4536 CX. 2 H 7 2 4T RT 2007072400142 20070724 00142 EA 2007 7 24 TRAX200701026 1 20070718 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 916EV 7757 CAPTAIN`S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007072400143 20070724 00143 EA 2007 7 24 TRAX200701027 1 20070719 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 682BR 7691 LEFT FUSELAGE FWD EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007072400144 20070724 00144 EU 2007 7 24 TRAX200701020 1 20070718 A 2560 FLASHLIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 FWD F/A'S FLASHLIGHT IS INOP. 2 H 7 2 4T RT 2007072400148 20070724 00148 WP 2007 7 24 MWEA070158 1 20070720 A 5754 SKIN DOUG DC9 DC981 3022081 WP LT SLAT DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 805ME 48031 LEFT SLAT INBOARD LEADING EDGE AT INBOARD WING TO BODY LOCATION DAMAGED AT STATION XFS 12.290. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2007072400149 20070724 00149 SO 2007 7 24 C2XA07RI060 1 20070718 A 2697 WIRE EMB 145 EMB145LR 3260212 SO FIRE DETECTION DAMAGED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 11535 145518 ON CLIMB, 5 MINUTES AFTER T/O, CREW RECEIVED A STEADY E2 FIRE DETECTION FAIL MSG AND THEN IT WENT INTERMITTENT. AIR-RET URNED. MAINTENANCE REPAIRED WIRES W407-14-20 AND W407-13-20 IAW EMB 145 SPWM 20-21-00 WITH REF TO EMB 145 MM 36-11-51. OPERATIONAL CHECK GOOD 26-10-00. A/C WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007072400151 20070724 00151 EU 2007 7 24 USA2007F00008 1 20070607 A 5320 STRUCTURE AIRBUS A321 A321211 3930370 EU CFMINT CFM56 CFM565B3P 13006 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 180US 22044 1525 CORRODED RIVET TAILS WERE FOUND IN FUSELAGE CARGO COMPARTMENT BETWEEN FRAME 24 TO 35.7 STRINGER 38L TO 39R OB (UPPER). APPROXIMATELY A TOTAL OF 2,500 RIVETS WERE REPLACED. APPROXIMATELY 700 WERE REPLACED ON OB (UPPER) SIDE OF STRINGER 38. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD THE PAINT FLAKING OFF THE RIVET TAILS THA T WERE CLEANED AND HAD PRIMER AND PAINT REAPPLIED. AIRCRAFT WAS MFG JUN 27, 2001. (K) 2 L 7 2 4F 4 F RT A28NM E37NE 2007072400152 20070724 00152 NM 2007 7 24 2007UALA02587 1 20070712 A 5310 DOOR FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FWD CARGO BAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 902UA 25002 FWD CARGO DOOR CUTOUT AFT FRAME IS CRACKED IN 3 PLACES, 2 CRACKS ON FWD SIDE OF THE FRAME AT OUTBOARD LOWER CORNER AND I NBOARD UPPER CORNER OF BOTTOM STOP FITTING AND THE THIRD CRACK IS ON AFT SIDE OF FRAME IN RADIOUS ADJACENT TO INBOARD UP PER CORNER OF BOTTOM STOP FITTING. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKS & ACCOMPLISHED ANGLE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007072400155 20070724 00155 EU 2007 7 24 2007UALA02590 1 20070712 A 2611 SMOKE DETECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LAVATORY FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 479UA 1538 LAV SMOKE DETECTOR FAULT. LAV SMOKE DETECTOR FAULTY. REPLACED LAV SMOKE DETECTOR. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072400156 20070724 00156 2007 7 24 2007UALA02591 4 20070712 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RIGHT FWD ENTRY OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 588UA 26717 FWD RT ENTRY DOOR WILL NOT ARM. [08-08-07] RESECURED LANYARD CORD INTERFERRING WITH GIRT BAR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072400157 20070724 00157 NM 2007 7 24 2007UALA02592 1 20070712 A 2611 PPA120100 SMOKE DETECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FWD LAVATORY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 802UA 690 FWD LAV SMOKE DETECTOR INOP (TEST INOP). REPLACED FWD LAVATORY SMOKE DETECTOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072400160 20070724 00160 NM 2007 7 24 2007UALA02594 1 20070712 A 3510 OXYGEN MASK BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FIRST OFFICER LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 941UA 26676 FIRST OFFICER'S O2 MASK HEAD BAND HAS AIR LEAK. [08-08-07] MASK FOUND WORN. REPLACED OXYGEN MASK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007072400161 20070724 00161 NM 2007 7 24 2007UALA02595 1 20070712 A 3350 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 314UA 23675 EMERGENCY LIGHT AT SEAT POSITION 5 ABC INOP. [07-27-07] RELAMPED EMERGENCY AISLE L AMP, OPS CHECK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007072400162 20070724 00162 NM 2007 7 24 2007UALA02596 1 20070712 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 SEATS 2J AFT, 3A AFT & 55 HJK EMERGENCY LIGHTS ARE INOPERATIVE. RELAMPED EMERGENCY LIGHT, CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072400163 20070724 00163 NM 2007 7 24 2007UALA02597 1 20070712 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 DOOR 2L FWD AND AFT SILL EMERGENCY LIGHT IS INOP. [07-27-07] RELAMPED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072400164 20070724 00164 NM 2007 7 24 2007UALA02598 1 20070712 A 3350 CHARGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 RIGHT OVERWING FWD TWO EMERGENCY LIGHT ASSY IS INOP. [07-27-07] REPLACED BATTERY CHARGER UNIT. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072400166 20070724 00166 NM 2007 7 24 2007UALA02600 1 20070713 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 ALL SEAT EEL INOP RIGHT OUTBOARD FIRST CLASS. [07-27-07] SECURED BATTERY CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072400167 20070724 00167 NM 2007 7 24 2007UALA02601 1 20070713 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 WALL EEL INOP: DOOR 5L CROSS AISLE. [07-27-07] SECURED LOOSE CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072400170 20070724 00170 NM 2007 7 24 2007UALA02604 1 20070713 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 EMERGENCY LIGHT INOP: DOOR 2 RT SLIDE ILLUM. [07-27-07] RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072400171 20070724 00171 NM 2007 7 24 2007UALA02605 1 20070713 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 SEAT EEL INOP: 2A AFT SECTION. [07-27-07] RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072400172 20070724 00172 NM 2007 7 24 2007UALA02606 1 20070713 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 EMERGENCY LIGHT INOP: AFT CREW REST STAIRS ILLUM. [07-27-07] RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072400173 20070724 00173 NM 2007 7 24 2007UALA02607 1 20070713 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 25RH INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 EEL INOP SEAT 25 RT. [07-27-07] REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072400175 20070724 00175 NE 2007 7 24 2007UALA02609 2 20070711 A 7397 61B43506044 WIRE HARNESS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUEL CONTROL SHORTED A UALA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION NR NOT REPORTED 1 WP 29 193UA 9261 26890 727742 ENG 4 DID SHUTDOWN AFTER FUEL CONTROL SWITCH PLACED IN CUTOFF POSITION. ENG 4 SHUTDOWN AFTER 45 SECONDS & FUEL CONT VAL VE - ENG 4 C/B L13 POPPED ON P6-2 PANEL. *S/D* SFOMM FOUND WIRE W3506-460-18 CHAFED AND SHORTED TO GROUND. THIS WIRE IS LOCATED IN THE W3506 WIRING HARNESS (BOEING 747 IPC 71-50-00-03-200; BOEING P/N 61B43506-044. REPAIRED & SECURED TH E WIRE HARNESS. SUBSEQUENT ENGINE RUN AND SHUTDOWN WERE NORMAL; C/B DID NOT POP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072400176 20070724 00176 NM 2007 7 24 2007UALA02610 1 20070712 A 3520 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MAIN CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 THE O2 MASKS DID NOT DROP DURING OPS CHECK IN MAIN CABIN AT ROWS 6AB, 4AB, 4CD, 10ABC, 27ABC & FWD F/A SEAT. [08-17-07] ELECTRICAL OPS CHECK TURNED OUT TO BE SUCCESSFUL. RELOCATED GREEN LANYARD AND RESET PLUNGER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072400179 20070724 00179 NM 2007 7 24 2007UALA02613 1 20070712 A 3150 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT GENERATOR ILLUMINATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 651UA 25389 LEFT GEN DRIVE LIGHT ILLUMINATED WITH ASSOCIATED EICAS L GEN DRIVE DISC MSG. [08-07-07] REPLACED LT IDG AS PER MM 24 -11-01, FINAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072400180 20070724 00180 NM 2007 7 24 2007UALA02614 1 20070713 A 5414 PANEL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 1 NACELLE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 829UA 1211 NR 1 ENGINE FWD PYLON CANTILEVER PANEL IS DAMAGED. REPAIRED FAIRING. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072400181 20070724 00181 EU 2007 7 24 2007UALA02615 1 20070713 A 5280 DOOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT MLG DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 411UA 464 RIGHT MLG MAIN DOOR & UPPER SIDE DOOR FOUND DAMAGED UPON ARRIVAL. REPLACED RT MLG FIXED AND SECONDARY HINGED FAIRINGS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072400182 20070724 00182 NE 2007 7 24 2007UALA02616 2 20070713 A 7250 BLADE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE FRACTURED A UALA E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 WP 29 653UA 25391 727815 CREW SHUTDOWN THE NR 1 ENGINE DUE TO VIBRATION. LANDED UNDER AMBER ALERT. [08-14-07] ENGINE REPLACED AT IAD. SHOP TEARDOWN FOUND ONE STAGE-2 HPT BLADE FRACTURED AT THE PLATFORM. THIS CAUSED AN UNBALANCE THAT PRODUCED HEAVY VIBRATION. FAILURE RESULT OF UNDER PLATFORM STRESS CORROSION CRACKING. A NEW CONFIGURATION BLADE, WITH IMPROVED UNDER PLATFORM COATING TO ELIMINATE STRESS CORROSION CRACKING IS AVAILABLE. THIS NEW CONFIGURATION BLADE IS BEING INCORPORATED INTO UN ITED'S FLEET AT HPT BUILD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072400184 20070724 00184 NM 2007 7 24 2007UALA02619 1 20070713 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 520-660 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 LEFT EXTERNAL FUSELAGE AT EXISTING REPAIR DOUBLERS STA 520-660, STR 14L-20L, SKIN HAS NUMEROUS DENTS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072400185 20070724 00185 NM 2007 7 24 2007UALA02620 1 20070713 A 5742 FITTING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT WING GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 RIGHT WING (PYLON) FITTING (SIDE LINK) FASTNER HOLE AT LOCATION F ON WING HAS INTERNAL GOUGE DAMAGE. 09-07-07 MAJOR REPAIR ACCOMPLISHED. PANEL ON PYLON 432AR UPPER RIGHT HAS DELAMINATION DUE TO HEAT. REPAIRED PANEL PER UA ENGINEERING SPECIFICATIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072400186 20070724 00186 NM 2007 7 24 2007UALA02621 1 20070713 A 4900 CHARGER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE APU BATTERY FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 796UA 26931 EICAS STATUS MESSAGES, APU BATTERY, APU BATTERY CHARGER. [08-07-07] REPLACED APU BATTERY AND APU CHARGER. AIRCRAFT R EADY FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007072400188 20070724 00188 NM 2007 7 24 2007UALA02179 1 20070623 A 2822 60B924015 VALVE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LT FUEL PUMP LEAKING A UALA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 29 204UA 28713 UNWANTED FUEL TRANSFER FROM CENTER TANK TO RIGHT MAIN TANK. *S/D* AFTER EXTENSIVE TROUBLESHOOTING AND REPLACEMENT OF L EFT REFILL VALVE CONTROLLER DIDN'T SOLVE PROBLEM. REPLACED LEFT MAIN AFT PUMP DISCHARGE CK VALVE PER MM 28-22-08. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007072400189 20070724 00189 SO 2007 7 24 C2XA07TY040 1 20070723 A 5551 14521939005 HINGE FITTING EMB 145 EMB145LR 3260212 SO HORIZONTAL STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13994 145291 HORZ STAB LT HINGE PIN SAFETY PIN STRUCTRAL FITTING BROKEN ON LT ROOT FITTING. REMOVED AND REPLACED LT OUTBOARD SIDE HO RZ STAB HINGE FITTING. REAMED LT OUTBOARD & INBOARD FITTING TO FIRST OVERSIZE IAW EMB 145 SRM 51-40-02, 51-00-03, 55-10 -02, EMB 145 AMM 20-10-03, 55-16-00. AIRCRAFT STILL IN C-CHECK. 2 L 7 2 4T RT T00011AT 2007072400191 20070724 00191 NM 2007 7 24 2007UALA02625 1 20070713 A 2721 TRIM SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RUDDER FAILED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 556UA 26650 RUDDER TRIM FAILED TO TRIM IN EITHER DIRECTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072400193 20070724 00193 NM 2007 7 24 2007UALA02627 1 20070714 A 2750 TRANSFORMER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE TE FLAPS OUT OF RIG A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 662UA 27159 CAPTAIN REPORTED, T/E FLAP DISAGREE ON FINAL. [08-17-07] FSEU BITE CARRIED OUT WITH FLAP HANDLE SET FOR 30 AND READ OUT SHOWING 20. THIS CONFIG RESULTED FROM THE FLAP LEVER ROTARY VARIABLE DIFFERENTIAL TRANSFORMER BEING IN MISRIGGED CO NFIGURATION & OUTBD SLAT PEDISTAL FLAP CONTROL ROTARY TRANSFORMER ALSO BEING MISRIGGED. SYSTEM RESET BY CYCLING ARMING S W'S, LIGHTS SHOWN AFTER THE BITE CHECK. L, C, R BITE - ALL OK,THEN FLAP OPERATION NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072400196 20070724 00196 NM 2007 7 24 2007UALA02630 1 20070714 A 3350 SIGN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 301UA 23642 EMERGENCY EXIT MARKER INOP AT SEAT 9B. [07-27-07] SECURED CONNECTOR OPS CKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071900284 20070719 00284 EA 2007 7 19 S9BA1007 1 20070713 A 2121 SZ470032A FAN DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6* 52043 EA CABIN ODOR A S9BA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 29 888PV 467 620 ODOR OF BURNING WIRES IN AIRCRAFT. SHUTDOWN AIR CONDITIONING AND CABIN FANS. ODOR SUBSIDED. REMOVED AND REPLACED LT AND RT CABIN BLOWER FANS. (SZ57-003-2A) 1 H 7 2 3T 3 T RT A9EA E2NE 2007071900286 20070719 00286 EA 2007 7 19 S9BA1107 1 20070710 A 2750 C6WFM111127 WASHER DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA TE FLAPS WORN A S9BA O OTHER E VIBRATION/BUFFET DE DESCENT 1 SO 29 573SA 674 AFTER COMMENCING DESCENT, FUSELAGE VIBRATION FELT PRIMARILY ON LT SIDE OF AIRCRAFT AT 185 KNOTS. FOUND PLAY IN THE IB FL AP FUSELAGE MOUNTING POINT. REPLACED SPECIAL WASHER. PN C6WFM1111-27. CHECK FLIGHT OK. 1 H 7 2 3T 4 T RT A9EA E4EA 2007071900288 20070719 00288 NM 2007 7 19 2007UALA02478 1 20070706 A 5210 BEARING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU STOP PAD LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 FWD ENTRY DOOR CUTOUT HAS AN AFT STOP PAD LOOSE. [07-20-07] REMOVED AND REPLACED BEARING STOP PAD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071900290 20070719 00290 NM 2007 7 19 2007UALA02479 1 20070706 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 FWD PIT DOORWAY CUTOUT FWD FRAME IS CRACKED AT LWR DOOR STOP FITTING. [07-27-07] MAJOR REPAIR: REMOVED CRACK AND A CCOMPLISHED ANGLE REPAIR PER MM 53-30-75. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071900291 20070719 00291 NM 2007 7 19 2007UALA02480 1 20070706 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 EXTERNAL CROWN SKIN HAS WEAR DAMAGE UNDER DORSAL LANDING ON LEFT SIDE FROM BS 908-965. [07-27-07] MAJOR REPAIR: IN STALLED DOUBLER, TEAR STRAP DOUBLER, AND TAPE RED FILLER. REFERENCE AAR EA I0700457 IR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071900294 20070719 00294 NM 2007 7 19 2007UALA02481 1 20070707 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 369UA 24538 RIGHT LOWER AFT FUSELAGE EMERGENCY EXIT LIGHT IS INOP. [07-27-07] RELAMPED RT LOWER AFT FUSELAGE EMERGENCY 2 L 7 2 4F 4 F RT A16WE E21EU 2007071900295 20070719 00295 NM 2007 7 19 2007UALA02482 1 20070707 A 5314 KEELBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 WEAR ON UPPER KEEL BEAM RIGHT HAND FROM 2 PANEL FASTENER RBL 7 STA 720-722. [07-27-07] MAJOR REPAIR: INSTALLED AN ANGLE, CUTOUT FILLER AND REPAIR FILLER. ACCOMPLISHED PER AAR EA REV IR, EAI070461 IR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071900296 20070719 00296 EA 2007 7 19 TRAX200700988 1 20070710 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 885AS 7521 CAPTAIN'S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007071900297 20070719 00297 EA 2007 7 19 TRAX200700989 1 20070711 A 2560 MEGAPHONE CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 738EV 10146 MEGAPHONE INOP. 2 L 7 2 4F RT A21EA 2007071900298 20070719 00298 EA 2007 7 19 TRAX200700990 1 20070711 A 3260 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ILLUMINATED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 970EV 7527 MAIN GEAR DISAGREE ON APPROACH. EMERGENCY DECLARED. EMERGENCY EQUIPMENT ON STANDBY. 2 L 7 2 4F RT A21EA 2007071900299 20070719 00299 EA 2007 7 19 TRAX200700991 1 20070711 A 2560 MEGAPHONE CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 723EV 10132 MEGAPHONE NOT OPERATING. 2 L 7 2 4F RT A21EA 2007071900300 20070719 00300 NM 2007 7 19 CALA0700347 1 20070711 A 5313 BAC1498156 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND STRINGER 26R CORRODED ON FORWARD END BETWEEN STA 1006-1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071900301 20070719 00301 NM 2007 7 19 CALA0700348 1 20070707 A 5753 65C35615 FLAP TRACK BOEING 737 7373T0 1384582 NM T/E FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND CORROSION INSIDE THE AFT TRANSMISSION MOUNT HOLE OF THE NR 8 FLAP TRACK, RT WING, WS 289-511. THE CORR OSION IN THE BORE WAS REAMED, SHOT PEENED, PLATED AND A SLEEVE BUSHING WAS INSTALLED IAW CMM 57-53-15, PAGE 16, FIGURE 6 AND SOPM 20-42-10 AND 20-42-03. 2 L 7 2 4F RT A16WE 2007071900302 20070719 00302 NM 2007 7 19 CALA0700349 1 20070712 A 5320 6517684638 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL WEB AT RIVET LOCATED AT STA 294.5, S12L. THE INTERCOSTAL WEB WAS REMOVED AND REPLACED IAW ECRA 5311-01339. 2 L 7 2 4F RT A16WE 2007071900303 20070719 00303 NM 2007 7 19 CALA0700350 1 20070712 A 5320 69489854 ATTACH FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND A 1.5 INCH CRACK AT I/B CORNER OF ATTACHMENT CLIP, STA 360, S10L. THE CLIP WAS REMOVED AND REPLACED IA W ECRA 5311-01339. 2 L 7 2 4F RT A16WE 2007071900304 20070719 00304 NM 2007 7 19 CALA0700351 1 20070712 A 5320 65558722 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND A 1 INCH CRACK IN WEB JUST FORWARD OF L-2 DOOR AT STA 942, S11L. THE CLOSE OUT WEB WAS REMOVED AND REP LACED IAW ECRA 5311-01335. 2 L 7 2 4F RT A16WE 2007071900305 20070719 00305 NM 2007 7 19 CALA0700352 1 20070712 A 5311 65528747 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND A .75 INCH CRACK IN STUB FRAME FOR L-2 DOOR UPPER HINGE AREA, STA 947.5, S11L. THE FRAME WAS REPAIRED IAW ECRA 5311-01335. 2 L 7 2 4F RT A16WE 2007071900306 20070719 00306 NM 2007 7 19 CALA0700353 1 20070712 A 5320 9078224 STRAP BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND A .5 INCH CRACK IN H-STRAP AT THE UPPER L-1 DOOR HINGE ATTACH FITTING, STA 312. THE H-STRAP WAS REPLAC ED IAW ECRA 5311-01337. 2 L 7 2 4F RT A16WE 2007071900307 20070719 00307 NM 2007 7 19 CALA0700354 1 20070712 A 5320 50794662 ATTACH FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND A .5 INCH CRACK AT AFT END OF ATTACHMENT CLIP, STA 294-309, S10L. THE CLIP WAS REPLACED IAW ECRA 5311- 01337. 2 L 7 2 4F RT A16WE 2007071900308 20070719 00308 SO 2007 7 19 C2XA07CL061 1 20070711 A 3350 SG963 STRIP EMB 145 EMB145XR 3260214 SO CABIN LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11150 145756 CLE FLIGHT 2322 - THE CREW REPORTED THE AISLE PATH LIGHT STRIP WAS LOOSE ON THE FLOOR. MAINTENANCE INSPECTED AND RE-ATT ACHED THE AISLE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2007071900309 20070719 00309 NM 2007 7 19 SWAA073427 1 20070712 A 5755 6544851 SPOILER BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED C3 CHECK, FOUND RIGHT WING NR 5 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED NR 5 SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007071900310 20070719 00310 NM 2007 7 19 SWAA073426 1 20070712 A 5755 CASTING BOEING 737 7373H4 1384600 NM NR 4 SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED C3 CHECK, FOUND LEFT WING NR 4 GROUND SPOILER INBOARD ACTUATOR ATTACH CASTING CRACKED. REMOVED AND REP LACED NR 4 SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007071900319 20070719 00319 SO 2007 7 19 SWIA200718462 1 20070618 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 LEFT SIDEWALL FORWARD SEAT TRACK IS CORRODED, DISCOVERED AT C-CHECK. REPLACED THE LEFT SIDEWALL SEAT TRACK IAW EMB SERV ICE LETTER EST-186/96 AND MM 20-10-03. 2 L 7 2 4T RT A31SO 2007071900321 20070719 00321 SO 2007 7 19 SWIA200718464 1 20070618 A 5230 FRAME EMB 120 EMB120ER 3260203 SO CARGO DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 CARGO DOOR FORWARD SIDE FRAME HAS CRACK ON TOP CORNER, DISCOVERED AT C-CHECK. REPLACED FRAME IAW SRM 51-10-02. 2 L 7 2 4T RT A31SO 2007071900325 20070719 00325 GL 2007 7 19 2502 1 20070714 A 2400 14610002 MODULE CIRRUS 100 CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO HARTZL HCJ3Y PHCJ3YF1 GL MCU BROKEN E J4PA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 13 695CD 02332 1372 688086 FP3486B AT 0900, DURING CLIMB OUT FROM GMU TO 60J THE ALT, NR 1 AND NR 2 FAIL LIGHT CAME ON. RETURNED TO GMU WITH OUT INCIDENT. HAD ONE PASSENGER ONBOARD. GROUND RAN AIRCRAFT COULD NOT DUPLICATED PROBLEM. PERFORM A AROUND THE PATTERN FLIGHT AND PROBLEM CAME BACK. AFTER FURTHER TROUBLESHOOTING FOUND THE LOGIC MODULE INSIDE THE MCU TO HAVE A BROKEN CONNECTION PIN . REMOVED AND REPLACED MCU. 1 L 7 1 3O 3 O NT A00009CH E3SO 5 C P36EA 2007071900331 20070719 00331 NM 2007 7 19 SWAA073429 1 20070712 A 5755 ATTACH FITTING BOEING 737 7373H4 1384600 NM NR 5 SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED C1 CHECK, FOUND RIGHT WING NR 5 GROUND SPOILER INBOARD ACTUATOR FWD ATTACH LUG CRACKED. REMOVED AND RE PLACED NR 4 SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007071900332 20070719 00332 NM 2007 7 19 SWAA073428 1 20070712 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007071900334 20070719 00334 NM 2007 7 19 SWAA073432 1 20070712 A 5330 6545766 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730B, STR 14R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007071900335 20070719 00335 NM 2007 7 19 SWAA073433 1 20070712 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 406, RBL 1. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007071900336 20070719 00336 NM 2007 7 19 SWAA073442 1 20070712 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 482A, BL 0, WL 148. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007071900338 20070719 00338 NM 2007 7 19 SWAA073438 1 20070712 A 5311 6546534 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071900339 20070719 00339 NM 2007 7 19 SWAA073430 1 20070712 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007071900341 20070719 00341 NM 2007 7 19 SWAA073448 1 20070712 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071900342 20070719 00342 NM 2007 7 19 SWAA073441 1 20070712 A 5311 6546550 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071900343 20070719 00343 NM 2007 7 19 SWAA073436 1 20070712 A 5322 6546569 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007071900344 20070719 00344 NM 2007 7 19 SWAA073439 1 20070712 A 5311 6546596 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071900345 20070719 00345 NM 2007 7 19 SWAA073451 1 20070712 A 5315 6546811 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 747SA 29799 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 27. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2007071900356 20070719 00356 2007 7 19 SWIA200718480 4 20070710 A 2210 AUTOPILOT SYS CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 447SW 7677 FLT 3900 - PRE-SELECTED ALTITUDE CHANGES SPONTANEOUSLY AFTER BEING SET CAUSING THE AUTOPILOT TO OVERSHOOT ASSIGNED ALTIT UDES. FCC DIAGNOSTICS HAD NO FAULTS LOGGED. ALTITUDE SELECT FUNCTIONS NORMALLY. NO DISCREPANCY NOTED. 2 L 7 2 4F RT A21EA 2007071900369 20070719 00369 EU 2007 7 19 TRBA2007049 1 20070718 A 5751 46797648010 INDICATOR AEROSP ATR72 ATR72212A 8680902 EU COCKPIT FAILED A TRBA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 29 494AE 494 FLAP UNLOCK INDICATION ON APPROACH. DECLARED EMERGENCY AND ABORTED APPROACH. LANDED WITH ZERO FLAPS. PERFORMED OP CK OF FLAP VALVE BLOCK IAW JIC NR 27-54-71. REMOVED AND REPLACED FLAP POSITION INDICATOR IAW JIC NR 27-55-81. PERFORMED OP CK OF FLAP SYSTEM IAW JIC NR 27-27-51-00 AND FOUND WORKING PROPERLY. 2 H 7 2 4T RT A53EU 2007071900370 20070719 00370 NM 2007 7 19 F3LA200700172 1 20070707 A 5320 PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 933FR 5232 2260 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT TRANSITION PANELS 151BE, 151UG, 161BF, AND 161CF DAMAGED. R EPAIRED TRANSITION PANELS IAW SRM 53-02-00, FIG 204. 2 L 7 2 4F RT A28NM 2007071900386 20070719 00386 NM 2007 7 19 KCSA071224 1 20070715 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 865 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 CORROSION ON SEAT TRACK I/B RADIUS AT STA 865 RBL 12 WL 199. 2 L 7 4 4F RT A20WE 2007071900387 20070719 00387 NM 2007 7 19 KCSA071225 1 20070715 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 520-560 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA 520 TO 560 RBL 11 SEAT TRACK UPPER I/B FLANGE HAS CORROSION. 2 L 7 4 4F RT A20WE 2007072000006 20070720 00006 NE 2007 7 20 HNAA0700148 2 20070710 A 7200 PW120A ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 MALFUNCTIONED A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 810EX 308 PCE120876 NR 1 ENGINE TQ AND WF FLUX PLUS OR MINUS 15 PERCENT. PROP RPM FOLLOWED. NO MANUAL LIGHT. CREW DID NOT CONTACT MX BEFO RE RETURN TO FIELD. REMOVED AND REPLACED NR 1 ENGINE, OPS CHECK ALL SYSTEMS ON RUN CHECK, CHECK GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2007072000007 20070720 00007 EA 2007 7 20 VNAA0706016 1 20070629 A 2840 73811813 COMPUTER CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE FUEL QTY FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 703PS 5320 10137 CREW REPORTED A FUEL CHANNEL 1/2 CAUTION MESSAGE SHORTLY AFTR TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FUEL QUANTITY COMPUTER IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANU AL 28-41-22-400-801. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007072000029 20070720 00029 NM 2007 7 20 USAA070539 1 20070716 A 5340 ATTACH BRACKET BOEING 737 737401 1384701 NM BS 400 S9L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 BS 400 S-9L, A/C ATTACH BRACKET FRAME HAS CRACK. INSTALLED DOUBLER PER SRM TR 53-10-20E, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007072000032 20070720 00032 NM 2007 7 20 USAA070536 1 20070716 A 5320 SUPPORT BOEING 737 737401 1384701 NM BS 328-344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 SUPPORT STA 328 - 344 LBL 12 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-10-51, 5-10-02; CORR TASK C53-107-02, DEFECT SIZE: 5 INCHES. 2 L 7 2 4F RT A16WE 2007072000053 20070720 00053 NM 2007 7 20 SWAA073467 1 20070715 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM BS 360 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007072000057 20070720 00057 NM 2007 7 20 SWAA073490 1 20070715 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 747 S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007072000066 20070720 00066 NM 2007 7 20 CALA0700359 1 20070715 A 5420 65C2630812 FITTING BOEING 737 7373T0 1384582 NM NR 2 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND A 1 INCH CRACK IN NR 2 ENGINE PYLON AFT HORSE COLLAR (FITTING). THE FITTING WAS REMOVED AND REPLACED I AW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007072000068 20070720 00068 NM 2007 7 20 SWAA073485 1 20070715 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 706 S2R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007072000069 20070720 00069 NM 2007 7 20 SWAA073483 1 20070715 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 685 S3R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007072000073 20070720 00073 NM 2007 7 20 SWAA073468 1 20070715 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 706 S11-11R/L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L AND STR 11R. REMOVED AND REPLACED STRINGER C LIP PER SRM. 2 L 7 2 4F RT A16WE 2007072000079 20070720 00079 EA 2007 7 20 VNAA0707001 1 20070704 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT WING DAMAGED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 248PS 7925 CREW REPORTED A LIGHTNING STRIKE WHEN THE AIRCRAFT TERMINATED IN CLT. MAINTENANCE INSPECTED AND FOUND LIGHTNING STRIKE DAMAGE TO THE LEFT HAND WINGLET TIP. MAINTENANCE COMPLIED WITH A DETAILED LIGHTNING STRIKE INSPECTION FOR DAMAGE IN ACC ORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 05-51-05-220-801 AND 05-51-220-803. MAINTENANCE COMPLIED WITH TEMP REPAIR IN ACCORDANCE WITH REO 601R-57-30-001. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007072000081 20070720 00081 EA 2007 7 20 VNAA0705012 1 20070502 A 5311 CC670341757 FRAME CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE BS 280 CORRODED A VNAA K NONE O OTHER IN INSP/MAINT 1 GL 05 702PS 7582 10135 FS 280 FRAME, AT WL 73 IS CORRODED FROM LBL 45 TO RBL 9. MAINTENANCE REMOVED AND REPLACED FRAME AT WL 73 FS 280 AS REQU IRED IN ACCORDANCE WITH THE AIRCRAFT STRUCTURE REPAIR MANUAL 51-42-06-001-001-A01. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007072000089 20070720 00089 2007 7 20 SWAA073494 4 20070715 A 2565 416A2200 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 701GS 27836 R1 DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2007072000093 20070720 00093 NM 2007 7 20 SWAA073514 1 20070716 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM BS 706 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007072000097 20070720 00097 NM 2007 7 20 SWAA073512 1 20070716 A 5311 65C22910 FRAME BOEING 737 7373H4 1384600 NM BS 500D S14R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 14R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007072000103 20070720 00103 NM 2007 7 20 SWAA073502 1 20070714 A 5311 65C25230 FRAME BOEING 737 7373H4 1384600 NM BS 727E S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007072000124 20070720 00124 WP 2007 7 20 UPS07850168 1 20070623 A 5754 DOUBLER DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 LT/WING OUTBOARD L/E INNER DOUBLER CRACKED AT STA XFS 597. REMOVED CRACKED INNER DOUBLER AT LT/WING OUTBOARD L/E AT STA XFS 597. FABRICATED AND INSTALLED REPAIR DOUBLER AT LT/WING OUTBOARD L/E STA XFS 597 IAW SRM 51-1-2 1, 51-1-4, AND DWG 576900. 2 L 7 4 4F RT 4A25 2007072000135 20070720 00135 NM 2007 7 20 USAA070543 1 20070717 A 5240 654571124 DOOR FRAME BOEING 737 737401 1384701 NM CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FWD SERVICE DOOR FRAME AFT SIDE AT APEX OF OPENING FOR DOOR STOPS. REMOVED DAMAGED AREAS & INTALLED REPAIR DOUBLERS PER EA 98738, DEFECT SIZE: .125 INCH. 2 L 7 2 4F RT A16WE 2007072000150 20070720 00150 NM 2007 7 20 2007UALA02491 1 20070709 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 AFT CREW REST AREA ENTRY WALL EMERGENCY EXIT LIGHT INOP. RELAMPED, OP CHECKED OK, REF MM 33-51-00. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072000163 20070720 00163 NM 2007 7 20 2007UALA02504 1 20070706 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 FWD GALLEY FLOOR AREA, STA 246 AT RBL 72 AREA, BULKHEAD WALL, LOWER FLOOR CHORD CORRODED UNDER SHEAR WEBBING, FWD EDGE. REMOVED DAMAGED SECTION OF CHORD, RBL 49 TO RBL 72. FABRICATED & INSTALLED SPLICE & REPAIR ANGLES. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072300014 20070723 00014 NM 2007 7 23 2007UALA02536 1 20070710 A 5330 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU BS 277 S3L GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 902UA 25002 UPPER FUSELAGE EXTERNAL SKIN IS GOUGED AT STA 277 STR 3L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. INSTALLED DOUBLE R/TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007072300016 20070723 00016 NM 2007 7 23 2007UALA02538 1 20070710 A 3320 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FIRE A UALA K NONE A FLAME/FIRE IN INSP/MAINT 1 WP 29 174UA 24381 SMOKE ODOR DOWNSTAIRS AND THEN FIRE FORWARD OF UPPER DECK GALLEY IN THE CEILING. ONE HALON EXTINGUISHER FIRED. [08-08 -07] FOUND FLUORESCENT LITE SOCKETS WITH HEAT DAMAGE. REPLACED UPPER DECK CEILING FLUORESCENT LIGHT SOCKETS. ALSO RE PLACED BALLAST. ALL CKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072300021 20070723 00021 NM 2007 7 23 2007UALA02540 1 20070711 A 4900 APU BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU UNKNOWN A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 924UA 26645 APU POWER PROBLEMS. [08-08-07] REPLACED APU GENERATOR TRANSFORMER T2 AS A PRECAUTION. OPERATIONAL CHECKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007072300034 20070723 00034 NM 2007 7 23 UPS07M50177 1 20070716 A 3350 BATTERY PACK DOUG MD11 MD11F 3023600 NM EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS WILL NOT EXTINGUISH IN OFF POSITION. REMOVED AND REPLACED BATTERY POWER SUPPL Y. CLEARED & RE-BONDED ENHANCEMENT GOOD. WDM 33-51-01 PER SWPM 20-50-01 & TESTED EMERGENCY LIGHTS OK. 2 L 7 3 4F RT A22WE 2007072300040 20070723 00040 NM 2007 7 23 2007UALA02558 1 20070710 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 575UA 26689 FOUR EEL LIGHTING END CAPS MISSING THROUGHOUT CABIN. [08-17-07] REPLACED MISSING END CAPS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072300042 20070723 00042 NM 2007 7 23 2007UALA02560 1 20070711 A 5320 COVER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 24D DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 COVER AT 24D HAS SHARP EDGE AT PAX FEET. [08-08-07] REPOSITIONED COVER PLATE AT SEAT 24D. NO LONGER HAS SHARP EDGE AT CONTACT POINT. OPERATES SATISFACTORIALLY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007072300046 20070723 00046 2007 7 23 2007UALA02564 4 20070709 A 2565 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE DOOR 3R FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 181UA 25278 AFTER POWER UP THE ACFT FOUND DOOR 3R INDICATOR SHOW DOOR OPENED. AFTER CHECK FOUND SLIDE RAFT WAS LAID DOWN ON THE FLO OR NEAR BY DOOR 3R. [08-07-07] REPLACED 3R SLIDE RAFT ASSY PER MM 25-65-16. CHKD OK. -INSPECTED INSTALLATION OF DR-3 R SLIDE RAFT ASSY PER MM 25-65-16. NO DEFECTS NOTED. AFTER INSTALLATION, DISCOVERED AFT RELEASE HANDLE OF RAFT COVER CA ME OFF. MADE INTERIM REPAIR BY BOLTING INTO HINGE OF BUSSLE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072300050 20070723 00050 EA 2007 7 23 TRAX200700942 1 20070705 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 872AS 7542 FS 280 FLOORBEAM ANGLE AT RBL 9.0 I/B CRACKED. REMOVED DAMAGED FLOORBEAM ANGLE, DUPLICATED PART FROM 2024-T3 .050, PO 9 50029 AND INSTALLED NEW SERVICEABLE ANGLE, IAW CRJ SRM 51-24-16 AND 51-42-21. 07/12/07 DUPLICATED PART, IAW AND IN CON JUNCTION WITH REO 601R-53-11-926 B. SUPPLEMENTAL - SDR CLOSED 07/16/07. 2 L 7 2 4F RT A21EA 2007072300051 20070723 00051 EA 2007 7 23 TRAX200700943 1 20070705 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 872AS 7542 FS 280 FLOORBEAM ANGLE AT LBL 9.0 I/B CRACKED. REMOVED DAMAGED FLOORBEAM ANGLE, DUPLICATED PART FROM 2024-T3 .050, PO 9 50029 AND INSTALLED NEW SERVICEABLE ANGLE, IAW CRJ SRM 51-24-16 AND 51-42-21. 07/12/07 DUPLICATED PART, IAW AND IN CON JUNCTION WITH REO 601R-53-11-926 B. SUPPLEMENTAL - SDR CLOSED 07/16/07. 2 L 7 2 4F RT A21EA 2007072300071 20070723 00071 NM 2007 7 23 ABXA070238 1 20070713 A 3260 BULB BOEING 767 767231 1385131 NM MLG INDICATOR INOPERATIVE A ABXA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 GL 23 708AX 22571 ABORTED APPROACH AT MHR. NOSE GEAR FAILED TO ILLUMINATE ON GEAR SELECT DOWN, NO LIGHT IN GEAR INDICATION LIGHT TEST. D ID ALT GEAR EXTEND PROCEDURE AND HAD TOWER CONFIRM NOSE GEAR DOWN. VERIFIED NOSE GEAR ANNUNCIATOR DID NOT ILLUMINATE ON LIGHTS TEST. REPLACED BOTH BULBS IAW ABX 767 AMM 33-16-02, OPS CHECKED GOOD. NOSE GEAR WAS DOWN AND LOCKED AND INDICA TION AGREED. 2 L 7 2 4F RT A1NM 2007072300077 20070723 00077 EA 2007 7 23 TRAX200700945 1 20070705 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA BS280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 872AS 7542 FS 280 WEB HAS CORROSION NEAR BL 0.0. REPAIRED DAMAGE TO 280 WEB, IAW ASA REO 601R-53-11-926. INSTALLED ALL FASTENERS, EXCEPT 8 JO-BOLTS IN -1 AND -2 WEB SPLICES. 07/12/07 INSTALLED REMAINING 8 JO-BOLTS, 4 AT LBL 9.00 FS 280.00 AND 4 AT RBL 9.00 FS 280.00. INSTALLATION OF JO-BOLTS, IAW CRJ 200 SERIES SRM 51-23-00 AND 51-42-22. SUPPLEMENTAL - SDR CLOSED 07/17/07. 2 L 7 2 4F RT A21EA 2007072300113 20070723 00113 SO 2007 7 23 RAIA00707027 1 20070713 A 3397 CONNECTOR EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHTS UNSECURE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 826HK 145016 PRE FLT NR 5452 - IND - EMERGENCY LIGHT COCKPIT STEP EXIT IDENTIFIER AND FWD CEILING EXIT LOCATOR ARE OUT. MAINTENANCE RESECURED CONNECTOR AT COCKPIT STEP LIGHT, OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT T00011AT 2007072300114 20070723 00114 SO 2007 7 23 RAIA00707026 1 20070712 A 3350 66364 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 821HK 145068 POST FLT NR FLMX - STL - EMERGENCY LIGHT INOP AT FLOOR PROXIMITY LIGHT. MAINTENANCE REMOVED AND REPLACED LIGHT STRIP. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007072300116 20070723 00116 SO 2007 7 23 RAIA00707025 1 20070711 A 3350 78241 INVERTER EMB 145 EMB145 3260210 SO EMERGENCY LIGHT NO TEST A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 809HK 145187 POST FLT NR 5561 - STL - EMERGENCY LIGHT LEFTHAND OVERWING EXIT MARKER INOP. MAINTENANCE REMOVED AND REPLACED NR 5 EMER GENCY INVERTER, SYSTEM CHECKS GOOD. 2 L 7 2 4F RT T00011AT 2007072400003 20070724 00003 NM 2007 7 24 HALA0700289 1 20070715 A 3600 UNKNOWN BOEING 767 76733A 1385209 NM PNEUMATIC PRESS UNKNOWN A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 ETOPS SIGNIFICANT SYSTEM, PNEUMATIC PRESSURE DRIPS EXCESSIVELY WHEN USING APU AIR FOR ENGINE STARTS. OPS CHECKED APU BL EED AIR PEC AMM 49-11-00-802, OPS CHECKED GOOD ALSO CHECKED FIM 36-10-00 FIG 118. NO FAULTS NOTED. 2 L 7 2 4F RT A1NM 2007072400005 20070724 00005 NM 2007 7 24 HALA0700288 1 20070716 A 4900 UNKNOWN BOEING 767 76733A 1385209 NM APU UNKNOWN A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 ETOPS SIGNIFICANT SYSTEM, APU AUTO SHUT DOWN AT GATE. PERFORMED ECU BITE PER FIM 40-11-00-1. NO FAULTS NOTED. RESTART ED APU, OPS CK NORMAL WITH NO FAULTS. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007072400006 20070724 00006 NM 2007 7 24 DHL2007753500 1 20070714 A 5753 STRUCTURE BOEING 727 727223 1384074 NM RT WING TE FLAP CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 RIGHT WING INBD FORE FLAP HAS O/B OF L/E DEEP CHAFE. REMOVED RT INBD FORE FLAP TO FOM IAW B727 MM 27-51-1. CUT OUT DAM AGED AREA I/B FORE FLAP R/WING. DIM CUT OUT 3/4" BY 3/4" AS REQUIRED IAW B727 SRM 57-50-4 FIG 1. FABBED DOUBLER REPAIR FROM P/N 2024-T3 .063" APPROX DIM 4" BY 4" IAW B727 SRM 57-10-4 FIG 1. TREATED AN PRIMED PART AND AREA IAW B727 SRM 5 1-10-2. INSTALLED DOUBLER REPAIR AT R/WING INB FORE FLAP L/E IAW B727 SRM 57-40-4 FIG 1 AND 51-30-2. INSTALLED RT I/B FORE FLAP IAW B727 MM 27-51-1. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2007072400007 20070724 00007 NM 2007 7 24 AWXA200700848 1 20070705 A 5340 69353521 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961321, CRACKED STRINGER CLIP, BS 727B, S23R. REPLACED STRINGER CLIP, BS 727B, S2 3R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007072400008 20070724 00008 NE 2007 7 24 NWAA072509875 2 20070714 A 7314 SHAFT DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE FUEL PUMP SHEARED A NWAA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 01 784NC 48109 688760 DURING CRUISE FLIGHT ENGINE NR 2 FLAMED OUT. FLIGHT CREW SECURED ENGINE NR 2 AND LANDED AT DESTINATION. MAINTENANCE FO UND THE FUEL PUMP SHAFT SHEARED, REPLACED FUEL CONTROL UNIT AND FUEL PUMP. 2 L 7 2 4F 4 F RT A6WE E2EA 2007072400009 20070724 00009 NM 2007 7 24 AALA20071213 1 20070629 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 780AN 29956 MIA EMERGENCY LIGHT AT SEAT 24C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT T00001SE 2007072400013 20070724 00013 WP 2007 7 24 AALA20071216 1 20070630 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70401 49312 LGA EMERGENCY LIGHTS AT SEAT ROWS 28 TO AFT OF CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT RO WS 28 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400014 20070724 00014 WP 2007 7 24 AALA20071217 1 20070630 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 599AA 53289 SFO EMERGENCY LIGHTS AT SEAT ROWS 27 TO 30 INOPERATIVE. CLEANED CONTACTS FOR EMERGENCY LIGHTS AT SEAT ROWS 27 TO 30. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007072400015 20070724 00015 WP 2007 7 24 AALA20071208 1 20070628 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 214AA 49162 DFW - OVERHEAD EMERGENCY LIGHTS AT SEAT ROWS 18 TO 21 INOPERATIVE. REPLACED BATTERY PACK B5 104 FOR EMERGENCY LIGHTS AT SEAT ROWS 18 TO 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400017 20070724 00017 NM 2007 7 24 AALA20071229 1 20070703 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 789AN 30252 JFK - EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT T00001SE 2007072400019 20070724 00019 NM 2007 7 24 AWXA200700838 1 20070710 A 5320 D534800149216 COVER AIRBUS A319 A319132 3930340 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5962429, CRACKED CABIN FLOOR COVER SHEET, BS 2884 / FR68, +Y1235. REPLACED CABIN F LOOR COVER SHEET, BS 2884 / FR68, +Y1235. I/A/W A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007072400021 20070724 00021 NM 2007 7 24 AWXA200700840 1 20070705 A 5340 693535221 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961325, CRACKED STRINGER TIE CLIP, BS 787, S21R. REPLACED STRINGER TIE CLIP, BS 7 87, S21R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007072400022 20070724 00022 NM 2007 7 24 AWXA200700841 1 20070705 A 5320 65479737 SHEAR WEB BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961270, CRACKED CREASE BEAM WEB, BS 559 - BS 578, S17L, WL 208. REPLACED CREASE B EAM WEB, BS 559 - BS 578, S17L, WL 208 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007072400023 20070724 00023 NM 2007 7 24 AWXA200700842 1 20070629 A 5310 146N8512 DOOR FRAME BOEING 757 757225 1384959 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - NR 5950466, AFT CARGO DOOR CUT OUT WEB CRACKED, BS 1440, S25R - S26R AT THE NR 6 STOP UPPER INBOARD HOLE. REPAIRED AFT CARGO DOOR CUT OUT WEB, BS 1440, S25R - S26R AT THE NR 6 STOP UPPER INBOARD HOLE IAW B 757-200 SRM 53-00-07. 2 L 7 2 4F RT A2NM 2007072400024 20070724 00024 NM 2007 7 24 AWXA200700843 1 20070714 A 2611 RAL2800M0706 CONTROL UNIT AIRBUS A319 A319132 3930340 NM SMOKE DETECTOR FAILED A AWXA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 28 816AW 16572 10944 1350 PHX - EE - LOG NR 7752699 - CREW REPORTED SDCU FAULT. MX REPLACED THE SMOKE DETECTOR CONTROL UNIT. OPERATIONAL CHECK W AS GOOD. 2 L 7 2 4F RT A28NM 2007072400026 20070724 00026 NM 2007 7 24 NWAA072496743 1 20070712 A 2133 7242821 OUTFLOW VALVE BOEING 747 747249F 1384849 NM CABIN PRESSURE MALFUNCTIONED A NWAA B J A EMER. DESCENT DUMP FUEL UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 643NW 70037 22927 22245 CLIMBING THROUGH 20,000 FEET, CABIN ALTITUDE WARNING HORN SOUNDED, CABIN ALTITUDE WAS AT 12,000 FEET. COM PROCEDURES FO LLOWED WITH DESCENT TO 10,000 FEET. FUEL WAS DUMPED AND AIRCRAFT LANDED UNEVENTFULLY. AT TIME OF EVENT, 3 PACS WERE OP ERATING, BLEEDS OPEN, ISOLATION VALVE OPEN, OUTFLOW VALVES SHOWED CLOSED AND AUTO CONTROLLER WAS IN AUTO. ALTITUDE CONT ROLLER WAS SET AT 34,000 FEET, BARO SET AT 29.92. ON TAXI IN OUTFLOW VALVES OPENED MANUALLY. THERE WERE NO DOOR OPEN LI GHTS ILLUMINATED. NO GROUND SAFE RELAY LIGHT ON DURING DESCENT. AT 10,000 FEET CABIN ALTITUDE WAS 7,000. REPLACED RIGH T OUTFLOW VALVE. 2 L 7 4 4F A20WE 2007072400028 20070724 00028 NM 2007 7 24 DLM88070903 1 20070711 A 2530 50459 OVEN DOUG MD88 MD88 3023688 NM FWD GALLEY UNSERVICEABLE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 995DL 53362 SMOKE FUMES NOTICED IN FWD CABIN/COCKPIT. SECURED OVEN AND FUMES DISSIPATED. DIVERTED TO KRIC. REPLACED FIRST CLASS G ALLEY OVEN. OPN CKS NML. REMOVED MCO AND PLCD. 2 L 7 2 4F RT A6WE 2007072400029 20070724 00029 EA 2007 7 24 DATA200700006 2 20070711 A 7200 ENGINE STBROS SD3 SD360 8100606 EU PWA PT6 PT6A65R 52043 EA SURGES E DATA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 13 151CA 23775 4327 SH3653 PCE97173 THE CREW WAS DEPARTING CHARLESTON, SC, THE PILOT SMOOTHLY ADVANCED THE THROTTLES TO ALLOW THE PROPS TO SPIN UP TO MAX R PM, BEFORE SETTING TAKEOFF POWER. THE LEFT ENGINE STARTED SURGING AND BACKFIRING WHILE THE PILOT ADVANCED THE THROTTLES . THE COPILOT CALLED TO ABORT THE TAKEOFF. PILOT PROMPTLY REACTED AND BROUGHT THE AIRPLANE TO A COMPLETE STOP. THE AI RCRAFT WAS TAXIED TO THE FOB AND MAINTENANCE AND DISPATCH WERE CALLED. 2 H 7 2 4T 4 T A41EU E4EA 2007072400030 20070724 00030 NM 2007 7 24 DHL2007784507 1 20070708 A 5753 652163479 SKIN BOEING 727 727227 1384078 NM TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 LT INBD AFT FLAP LE CRACKED AT NR 2 TRACK CUTOUT PREVIOUS DOUBLER, LWBL 60. REMOVED PREVIOUS REPAIR DOUBLER IAW B727 SR M 51-10-2, 51-30-2. HFEC IAW B727 NDTM PT.6 51-00-00, FIG.23, NO CRACKS INDICATED. FABRICATED REPAIR DOUBLER, MATERIAL USED 7075T6, 050, 3 BY 4 IAW B727 SRM 57-54-4. TREATED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 51-10-2, 51-30-2 AND 57-54-4. 2 L 7 3 4F A3WE 2007072400036 20070724 00036 NM 2007 7 24 DL764070911 1 20070713 A 2160 211040032 CONTROLLER BOEING 767 767432ER 1385134 NM CABIN TEMP INOPERATIVE A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 834MH 29707 L TRIM AIR OFF LIGHT ILLUMINATED WITH FWD AND AFT CABIN TEMP CONTROLLER INOP LIGHTS ILLUM. ATTEMPTED TO AND RESET C/B`S , NO HELP. FWD TO MCO AND PLACARD PER MEL 21-61-03. TRIM AIR VALVE LOCKED CLOSED. C/P REMOVED AND STOWED. NO TROUBLE FOUND. OPERATED PACKS NO ABNORMALITIES AFTER REACTIVATING VALVE. TRIM AIR VALVE HAS NORMAL OPERATION. DUE TO HI STORY REMOVED AND REPLACED LT CTC. GROUND TEST GOOD. PACK VAL OPS NML. MCO AND PLACARD REMOVED. 2 L 7 2 4F RT A1NM 2007072400037 20070724 00037 NM 2007 7 24 DL764070912 1 20070714 A 2910 MANIFOLD BOEING 767 767432ER 1385134 NM HYD SYSTEM LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 841MH 29714 LT HYD FLUID LOSS, HYDRAULIC MANIFOLD LEAKING SECT 72 VERTICAL STAB SEALS REPLACED LEAK CHK OK. IPC REF 27-21-56-01. 2 L 7 2 4F RT A1NM 2007072400038 20070724 00038 NM 2007 7 24 DLM90070914 1 20070703 A 5311 FRAME DOUG MD90 MD9030 3023690 NM BS 446 L28L DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 STA 446 LONGERON 28L HAS DOUBLE DRILLED HOLES. FABBED NEW FORMER PER DRAWING. INST PER SRM 53-10-02D, REF N/R 1000-032 0. 2 L 7 2 4F RT A6WE 2007072400039 20070724 00039 NM 2007 7 24 DL76S070915 1 20070714 A 3520 9700C2CF20D BOTTLE BOEING 767 767332 1382001 NM PAX OXYGEN MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 133DN 24982 2 PAX 02 BOTTLES WOULD NOT FLOW. REPLACED BOTTLES W/ SVCBL BOTTLES FROM STOCK. 2 L 7 2 4F RT A1NM 2007072400040 20070724 00040 2007 7 24 DL777070916 4 20070714 A 3442 6225132633 CONTROL PANEL BOEING 777 777232 1385232 NM WX RADAR FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 864DA 29736 AFTER T/O WX RADAR FAIL MESSAGE. TRIED RECYCLING C/B FOR WX RADAR AND OTHER PROCEDURES. ALL NO HELP. RETURNED TO ATL. MTC IN PROGRESS TROUBLESHOOTING SYS. REPLACED WX RADAR CONTROL PANEL AND TRANSCEIVER XCVR P/N O 622-5132-633 LRU SYST EM AND OPS CHECK ALL NORMAL. 2 L 7 2 4F RT T00001SE 2007072400041 20070724 00041 NM 2007 7 24 DL757070917 1 20070713 A 2120 UNKNOWN BOEING 757 757232 1384965 NM CABIN ODOR A DALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 6709 30481 FLT 597/13 JFK-SEA DIVERTED TO ORD FOR ELECTRICAL ODOR AND SLIGHT HAZE IN AFT CABIN NEAR THE AFT GALLEY. FLT CREW DECLA RED AN EMERGENCY AND LANDED OVERWEIGHT. DURING DESCENT FLT CREW TURNED OFF BOTH UTILITY BUSSES, ODOR AND HAZE BEGAN TO DISSIPATE. MTC COMPLETED OVERWEIGHT INSP AND ALSO INSPECTED SEVERAL THINGS WHICH MAY HAVE CAUSED THE PROBLEM BUT COULD NOT DUPLICATE THE PROBLEM. 2 L 7 2 4F RT A2NM 2007072400042 20070724 00042 NM 2007 7 24 DLM90070923 1 20070716 A 5330 SKIN DOUG MD90 MD9030 3023690 NM BS 474-588 DEFORMED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 DEFORMATION SKIN STA 474 TO 588 STR L-29R TO L27R. REMOVED FASTENERS AND SHIMMED ERA 462055-14 REV ORIG DATED 7-13-07 R EF AAR OKC N/R 1000-0317. 2 L 7 2 4F RT A6WE 2007072400046 20070724 00046 NM 2007 7 24 HALA0700285 1 20070712 A 5100 UNKNOWN BOEING 767 76733A 1385209 NM UNKNOWN UNKNOWN A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 581HA 28141 ETOPS SIGNIFICANT SYSTEM, REQUIRES 2 UNITS LT YOKE DISPLACEMENT FOR WINGS LVL.//INFO NOTED WITHIN LIMITS PER AMM27-01-00 . OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007072400047 20070724 00047 2007 7 24 HALA0700282 4 20070714 A 3416 4039892904 ALTIMETER BOEING 767 7673G5 1385126 NM COCKPIT INOPERATIVE A HALA O OTHER O OTHER CR CRUISE 1 WP 13 584HA 24258 ETOPS SIGNIFICANT SYSTEM, OFF FLAG IN VIEW F/O ALTIMETER WITH BOTH NORM AND ALTN SELECTED NOTE: AFTER LANDING FLAG DISAP PEARED. REPLACED F/O ELECTRIC ALTIMETER. OPS CHECK OK PER MM 34-13-00. 2 L 7 2 4F RT A1NM 2007072400048 20070724 00048 2007 7 24 HALA0700280 4 20070707 A 2565 101656305 SLIDE BOEING 767 76733A 1385209 NM LT OVERWING UNWANTED DEPLOY A HALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 13 591HA 1219 1219 33423 LT OVERWING SLIDE DEPLOYED DURING RT OVERWING SLIDE REPLACEMENT. REMOVED AND REPLACED LEFT OVERWING SLIDE ASSY PER AMM 25-65-01 AND 767-3-195002. 2 L 7 2 4F RT A1NM 2007072400050 20070724 00050 NM 2007 7 24 HALA0700281 1 20070706 A 5414 SKIN BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 NACELLE BENT A HALA O OTHER O OTHER CR CRUISE 1 WP 13 597HA 23277 PER INBD CREW, F/A REPORTS METAL STICKING UP ON NR 2 ENGINE. FOUND OUTBD FAN COWL TOP FWD CORNER DAMAGE APPROX 1-1/2" B Y 1/2" AND FWD OUTBD. ON PYLON EXTENSION LIFTED APPROX 4" (APPROX 1/2" LIFTED UP). ACCOMPLISHED HAL-M105 FILE #597063 AND 597064. CONDITION AND SECURITY CK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072400051 20070724 00051 NM 2007 7 24 HALA0700286 1 20070714 A 2420 FITTING BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE IDG LEAKING A HALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, R GEN DRIVE LIGHT CAME ON APPROACH, TURNED ON APU. PERFOMED BPCU BITE PER FIM 24-20-00. ALL ELECTRICAL SYSTEMS CHECK GOOD. NO FAULTS. FOUND IDG OVERFLOW SERVICE FITTING LEAKING. REPLACED SERVICE AND OVERFLOW S ERVICE ADAPTERS PER AMM 24-11-03. SERVICED RIGHT IDG. RAN NR 2 ENGINE, OPS AND LEAK CHECK GOOD. NR 2 GEN OPS CHECK GO OD. SECURED NR 2 ENG COWL. NO EICAS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072400052 20070724 00052 NM 2007 7 24 HALA0700283 1 20070712 A 2913 PUMP BOEING 767 76733A 1385209 NM HYD SYSTEM INOPERATIVE A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 593HA 33424 ETOPS SIGNIFICANT SYSTEM, RIGHT ELEC DEMAND PUMP INOP. ACCOMPLISHED FIM 29-11-00 FIG 104A, OPS CHECK NORMAL NOW. 2 L 7 2 4F RT A1NM 2007072400053 20070724 00053 NM 2007 7 24 DLM90070924 1 20070716 A 5330 SKIN DOUG MD90 MD9030 3023690 NM BS 229-475.5 BUCKLED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 LOWER FUSE SKIN BULGED AND WRINKLED STA 229-395 LONGERON 28-30 RT. REMOVED AND REPLACED SKIN FROM STA 229 TO 475.5 LONG ERON 26L TO 26R PER ERA 462055-14 REV ORIG DATED 07-13-07. 2 L 7 2 4F RT A6WE 2007072400054 20070724 00054 NM 2007 7 24 DL76S070925 1 20070716 A 5311 145T10017 FRAME BOEING 767 767332 1382001 NM BS 903.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 130DL 24080 DURING HMV3, THE LT BS 903.5 INBOARD CHORD WAS FOUND CRACKED AT WL 190. 2 L 7 2 4F RT A1NM 2007072400056 20070724 00056 NM 2007 7 24 DL76L070927 1 20070716 A 3397 WIRE BOEING 767 767332 1382001 NM EMERGENCY LIGHTS DISCONNECTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 171DN 24759 ON DRC, FOUND 31 A AND 19F E-PATH LIGHTS INOP. RECONNECTED WIRES TO LIGHTS ALL OPS OK. 2 L 7 2 4F RT A1NM 2007072400059 20070724 00059 NM 2007 7 24 HALA0700293 1 20070718 A 8011 35054367 STARTER BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE FAILED A HALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 13 580HA 15037 15037 28140 ETOPS SIGNIFICANT SYSTEM - BTB - RETURNED TO GATE, ON STARTING ENGINE NR 2 GND PERSONAL REPORT SPARKS FROM RT ENG PRIOR TO FUEL INTRO START TERMINATED, STARTER CUTOFF LIGHT AND RT ENG VALVE LIGHT REMAINED ON. RIGHT ENGINE REPLACED STARTER PER AMM 80-11-01. LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072400060 20070724 00060 NM 2007 7 24 DHL2007784505 1 20070711 A 5740 SUPPORT BOEING 727 727227 1384078 NM FLAP ACTUATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 NR 6 K-FLAP ACTUATOR SUPPORT IS CRACKED AT INBD CORNERS, W/S 304. REMOVED NR 6 K-FLAP ACTUATOR TRUNNION SUPPORT ANGLES INBD AND OUTBD IAW B727 SRM 51-30-2. FABRICATED SUPPORT ANGLES FROM 7075T6, .071, 8.25 BY 6.25 IAW B727 SRM 57-20-2, FI G 1 AND 51-20-1, FIG 7. TREATED, PRIMED AND INSTALLED PARTS IAW B727 SRM 51-10-2, 51-30-2 AND 57-20-2, FIG 1. 2 L 7 3 4F A3WE 2007072400061 20070724 00061 NM 2007 7 24 DHL2007784506 1 20070709 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 960C S28L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 AFT CARGO CORROSION ON STRINGER 28L, BS 960C. CUT OUT DAMAGED STR 28L STA 950C PLUS 10 AS REQUIRED IAW B727 SRM 53-10-3 , FIG 1, DET I. FABRICATED REPAIR PARTS, 1 EACH FILLER MATERIAL USED BAC1498-147-7075T6, .090, 5 LONG AND 1 EACH SPLIC E, MATERIAL USED BAC1498-131-7075T6, DIM 18.25 LONG IAW B727 SRM 53-10-2, FIG 9 AND 53-10-3, FIG 1. TREATED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 51-10-2 AND 53-10-3, FIG 1. 2 L 7 3 4F A3WE 2007072400064 20070724 00064 WP 2007 7 24 AALA20071294 1 20070713 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 208AA 49159 DFW - EMERGENCY LIGHT AT SEAT ROW 17D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400065 20070724 00065 WP 2007 7 24 AALA20071295 1 20070713 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 208AA 49159 DFW - EMERGENCY LIGHT AT SEAT ROW 10D HAS MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 10D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400067 20070724 00067 WP 2007 7 24 AALA20071298 1 20070713 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7547A 53029 LGA - EMERGENCY LIGHT AT SEAT ROW 14DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 14DEF. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400069 20070724 00069 NM 2007 7 24 AALA20071274 1 20070708 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 351AA 24032 JFK - EMERGENCY EXIT SIGN LIGHTS AT LEFT AND RIGHT AFT DOOR M10722 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXI T SIGN LIGHTS AT LEFT AND RIGHT AFT DOOR M10722. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007072400070 20070724 00070 NM 2007 7 24 AALA20071268 1 20070708 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 184AN 29594 MIA - EMERGENCY LIGHT EXIT SIGN AT RIGHT NUMBER FOUR DOOR HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT EXIT SIGN AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007072400072 20070724 00072 NM 2007 7 24 AALA20071262 1 20070707 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 798AN 30797 MIA - EMERGENCY SEAT MOUNTED LIGHT AT FORWARD GALLEY COMPARTMENT 371 RIGHT OUTBOARD FRAME MISSING. REPLACED LIGHT ASSEM BLY FOR EMERGENCY SEAT MOUNTED LIGHT AT FORWARD GALLEY COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007072400074 20070724 00074 NM 2007 7 24 AALA20071261 1 20070706 A 3350 LENS BOEING 757 7572Q8 1384972 NM EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 707TW 27625 DFW - EMERGENCY FLOOR LIGHT IN FIRST CLASS HAS DAMAGED LENS. REPLACED LENS FOR EMERGENCY FLOOR LIGHT IN FIRST CLASS. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007072400077 20070724 00077 NM 2007 7 24 AWXA200700846 1 20070703 A 5320 65479734 SHEAR WEB BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5982112, CRACKED CUSP SHEAR WEB, BS 540 - BS 559, S17R. REPLACED CUSP SHEAR WEB, B S 540 - BS 559, S17R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007072400084 20070724 00084 NM 2007 7 24 AALA20071269 1 20070708 A 4920 351A10001 APU BOEING 737 737823 13844BZ NM FAILED A AALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 942AN 30084 LGA - ON GROUND T1084/08JUL - AS PASSENGERS WERE DEPLANING WHEN LIGHTS FLICKERED AND WARNING LIGHTS WENT OFF IN COCKPIT. A FLIGHT ATTENDANT REPORTED SMELLING AN ODOR AND SEEING SMOKE OUTSIDE THE AFT RIGHT GALLEY DOOR. DISCHARGED FIRE BOTT LE. EVACUATED REMAINING PASSENGERS USING FORWARD ENTRY DOOR. ENGINEERING REQUESTED FLIGHT DATA RECORDER DOWNLOAD. REP LACED AUXILIARY POWER UNIT (APU) AND APU FIRE BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007072400085 20070724 00085 WP 2007 7 24 AALA20071270 1 20070708 A 3397 WIRE HARNESS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 400AA 49311 LGA - EMERGENCY LIGHTS AT AFT CATWALK INOPERATIVE. REPAIRED OVERHEAD BROKEN WIRE AT CONNECTOR FOR EMERGENCY LIGHTS AT A FT CATWALK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400087 20070724 00087 EU 2007 7 24 AALA20071272 1 20070708 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 90070 513 MIA - EMERGENCY LIGHTS AT SEAT ROWS 19C TO 28C INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 19C TO 28C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007072400088 20070724 00088 WP 2007 7 24 AALA20071282 1 20070712 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 484AA 49677 LGA - EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD CENTER AISLE FOR EMERGENC Y LIGHTS AT OVERHEAD FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400090 20070724 00090 EU 2007 7 24 AALA20071273 1 20070708 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 34078 615 MIA - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROW 7C INOPERATIVE. REPLACED CONNECTOR FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROW 7C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007072400091 20070724 00091 WP 2007 7 24 AALA20071287 1 20070713 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 208AA 49159 DFW - EMERGENCY LIGHT AT SEAT ROW 8D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 8D. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400093 20070724 00093 WP 2007 7 24 AALA20071289 1 20070713 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 208AA 49159 DFW - EMERGENCY SLIDE FLOOD LIGHT AT MIDDLE POSITION TAIL COMPARTMENT INOPERATIVE. RELAMPED EMERGENCY SLIDE FLOOD LIGHT AT MIDDLE POSITION TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400094 20070724 00094 WP 2007 7 24 AALA20071281 1 20070711 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 488AA 49681 LGA - EMERGENCY LIGHT AT OVERHEAD FORWARD MAIN ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVE RHEAD FORWARD MAIN ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400095 20070724 00095 WP 2007 7 24 AALA20071267 1 20070707 A 7830 CONTROL VALVE DOUG DC9 DC983 3022083 WP THRUST REVERSER LEAKING A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 9627R 53597 SFO ON GROUND T1951/07JUL - AFTER LANDING FLIGHT ATTENDANTS REPORTED SMOKE IN CABIN. TURNED OFF APU BLEED AIR AND SMOKE BEGAN TO DISSIPATE. FOUND THRUST REVERSER HYDRAULIC LEAK AT CONTROL VALVE B NUT. TIGHTENED NUT AND NO LEAKS FOUND. R EPLACED APU DUE TO HYDRAULIC FLUID INGESTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007072400097 20070724 00097 WP 2007 7 24 AALA20071276 1 20070709 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 259AA 49289 LGA - OVERHEAD EMERGENCY LIGHTS AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT FIRS T CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007072400099 20070724 00099 WP 2007 7 24 AALA20071278 1 20070710 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 441AA 49460 DFW - EMERGENCY LIGHT AT SEAT ROW 12 HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 12. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071900121 20070719 00121 EA 2007 7 19 TRAX200700970 1 20070707 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 MAIN PAX DOOR DIFFICULT TO OPEN. 2 L 7 2 4F RT A21EA 2007071900128 20070719 00128 2007 7 19 DXTA200702336 4 20070714 A 2210 AUTOPILOT SYS RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP LEFT MALFUNCTIONED E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 833QS 258433 DURING LEVEL FLIGHT AT FL340 ON THE LT AUTOPILOT, THE AIRCRAFT STARTED A STEEP CLIMB WITH NO INPUTS REQUESTED. AFTER REC OVERING AND SWITCHING TO THE RT AUTOPILOT (WHICH WORKED FINE AND NORMALLY) THE COMMAND BARS ON THE LT SIDE MADE ERRATIC MOVES UP AND DOWN. [07-23-07] PERFORMED GROUND MAINTENANCE TEST SEVERAL TIMES WITH NO FAILURES. OPERATIONAL CHECKED AUTOPILOT SEVERAL TIMES WITH NO FAILURES. NO DEFECTS NOTED. ALL OPERATIONAL TESTS GOOD. I.A.W. H800XP A.M.M. CH. 34- 22-05. 2 L 7 2 4F 4 F RT A3EU E6WE 2007071900134 20070719 00134 NM 2007 7 19 KCSA071210 1 20070712 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 UPPER DECK SEAT TRACK CORRODED BETWEEN BS 560 AND 580 AT LBL 46.45. 2 L 7 4 4F RT A20WE 2007071900137 20070719 00137 2007 7 19 ABXA070237 4 20070710 A 3160 6225046101 DISPLAY BOEING 767 767232 1385132 NM COCKPIT FAILED A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 745AX 4958 22222 STA: ILN, ON CREW PREFLIGHT, SMOKE DETECTED IN COCKPIT. ALSO EICAS SCREEN AND LEFT FMC BLANK. REMOVED UPPER EICAS DIS PLAY UNIT AND LEFT FMC DISPLAY UNIT. INSPECTED WIRING AND CONNECTORS, NO DEFECTS NOTED. REMOVED AND REPLACED EICAS DIS PLAY UNIT AND LEFT FMC. BOTH UNITS CHECK GOOD IAW B767 MM. LEFT FMC REMOVED: P/N: 4038170-905, S/N: 84040157, TSSV: 1 001, CSSV: 243. 2 L 7 2 4F RT A1NM 2007071900139 20070719 00139 SO 2007 7 19 RAIA00707008 1 20070706 A 3350 ML316 LIGHT EMB 145 EMB145LR 3260212 SO EXTERIOR INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 838HK 145321 PRE FLT NR 7981 - ROA - MAIN DOOR EXTERNAL EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED AIRSTAIR EMERGENCY LIGHT. OPS CH ECKS GOOD. 2 L 7 2 4T RT T00011AT 2007071900156 20070719 00156 CE 2007 7 19 DXTA200702318 1 20070705 A 3246 315381 WHEEL CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG OUT OF ROUND E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 906QS 587 587 7500206 EXTREMELY NOTICABLE NOSEWHEEL SHIMMY DURING TAKEOFF ROLL BETWEEN 60-70 KNOTS. FOUND NOSE TIRES OUT OF ROUND REMOVED AND REPLACED NOSE WHEEL/ TIRE ASSY'S WITH AN O/H WHEEL AND NEW TIRE IAW MM 32-41-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071900158 20070719 00158 SO 2007 7 19 RAIA00707022 1 20070709 A 3411 0851HU3 SENSOR EMB 145 EMB145LR 3260212 SO PITOT/STATIC SYS MALFUNCTIONED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 816HK 21646 40 145055 FLT NR 5529 - STL - PITOT 2 INOP MESSAGE. MAINTENANCE REMOVED AND REPLACED PITOT NR 2 SENSOR. OPS AND LEAK CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007071900163 20070719 00163 EA 2007 7 19 TRAX200700923 1 20070703 A 5320 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 717EV 10088 LEFT FS 280 CROSSBEAM HAS CORROSION ON UPPER FLANGE. REMOVED LEFT FS 280 CROSS BEAM IAW CRJ SRM 51-42-06 AND 51-42-21. LOCATED LEFT SECTION OF FS 280.00, CROSSBEAM FROM SERVICEABLE CROSSBEAM P/N CC670-34175-7 IAW BOMBARDIER REO 670-53-11- 032. INSTALLED ALL FASTENERS IN LEFT BEAM EXCEPT CENTER SPLICE IAW REO IS 67053110026. INSTALLED OUTER SPLICE AND FAST ENERS. TOP COATED IAW CRJ SRM 51-25-16. SUPPLEMENTAL - SDR CLOSED 07/12/07. 2 L 7 2 4F RT A21EA 2007071900180 20070719 00180 NM 2007 7 19 SWAA073383 1 20070710 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 222WN 34290 EEPLS COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007071900186 20070719 00186 NM 2007 7 19 SWAA073396 1 20070711 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 759, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007071900187 20070719 00187 NM 2007 7 19 SWAA073409 1 20070711 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 847, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007071900189 20070719 00189 NM 2007 7 19 SWAA073400 1 20070711 A 5330 6545877 BEAR STRAP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT L1 DOOR LOWER HINGE CUTOUT LOWER CORNER. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007071900196 20070719 00196 SO 2007 7 19 SIMA200719717 1 20070708 A 5347 14530658007 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 816AE 13301 5000 145552 RIGHT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900199 20070719 00199 NM 2007 7 19 SWAA073421 1 20070711 A 5311 6546529 BELTFRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 500B, STR 20L. REPAIRED BELTFRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071900204 20070719 00204 NM 2007 7 19 SWAA073404 1 20070711 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM R2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007071900213 20070719 00213 SO 2007 7 19 SIMA200719804 1 20070522 A 5320 13500469403 PROFILE EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 15926 5000 145224 UPPER FLOORBEAM AT FRAME 22 CORRODED. REMOVED AND REPLACED FLOORBEAM IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVIC E. 2 L 7 2 4F RT T00011AT 2007071900214 20070719 00214 NM 2007 7 19 SWAA073389 1 20070710 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED SERVICE CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071900224 20070719 00224 NM 2007 7 19 07FDEA02456 1 20070713 A 5314 6518636 KEELBEAM BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 AFT PIT KEEL BEAM CHORD/STR 29L CORRODED STA 990-1010 REMOVED CORROSION. FOUND TO BE OUT OF LIMITS TREATED AND PRIMED B LENDED AREA REF SRM 51-10-2. FABBED REPAIR STRAP REF DWG SR 27-53-023. TREATED AND PRIMED REF SRM 51-10-2. INSTALLED REPAIR REF DWG SR 27-53-023. 2 L 7 3 4F A3WE 2007071900226 20070719 00226 WP 2007 7 19 07FDEA02458 1 20070713 A 5322 SHEAR TIE DOUG DC10 DC1010F 3022111 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 CTR CARGO COMPT TUNNEL ON SHEAR CLIP NR 2 CRACKS. REPAIRED SHEAR CLIP IAW SRM 53-30-00 FIG 10 VOL 1. 2 L 7 3 4F A22WE 2007071900229 20070719 00229 SO 2007 7 19 CHQA200700036 1 20070714 A 3260 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO MLG DIRTY A CHQA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 GL 11 275SK 145345 FLIGHT 3420 - IAH-BTR - DURING DESCENT BETWEEN 9,000 AND 10,000 FEET, THE FLAPS WERE SET TO 9 DEGREES AND THE LANDING GE AR WAS SELECTED DOWN. AFTER THREE GREEN WITH DOWN INDICATIONS, EICAS MESSAGE LG AIR/GND FAIL APPEARED. COMPLETED QRH. DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED THE WOW PROX SENSORS AND RESET THE SYSTEM. 2 L 7 2 4T RT T00011AT 2007071900241 20070719 00241 NM 2007 7 19 SWAA073416 1 20070711 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 460WN 32464 DURING SCHEDULED HC1 CHECK, LEFT OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2007071900246 20070719 00246 NM 2007 7 19 SWAA073395 1 20070711 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED SPV CHECK, FOUND AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2007071900257 20070719 00257 WP 2007 7 19 UPS07850160 1 20070711 A 3350 LIGHT DOUG DC8 DC871F 302199D WP COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:N/A EMERGENCY EXIT DISARM LIGHT ON OVERHEAD PANEL IS INOP. RELAMPED EMERGENCY EXIT DISARM LIGHT ON OVER HEAD PANEL PER MM 33-13-00-2. 2 L 7 4 4F RT 4A25 2007071900322 20070719 00322 SO 2007 7 19 SWIA200718465 1 20070618 A 5210 STRUCTURE EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 PAX DOOR INTERNAL STRUCTURE CRACKED AT FORWARD NR 4 STOP, DISCOVERED AT C-CHECK. REPAIRED INTERNAL PAX DOOR STRUCTURED STOP IAW SRM 52-10-02 FIG 203 PG 208. 2 L 7 2 4T RT A31SO 2007071900324 20070719 00324 EA 2007 7 19 SWIA200718467 1 20070708 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 452SW 7716 EMERGENCY LIGHT POD IN CEILING BY LAVATORY IS BURNED OUT, FLIGHT NR 3954. RELAMPED EMERGENCY LIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007071900328 20070719 00328 EA 2007 7 19 SWIA200718473 1 20070701 A 5512 SKIN CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB DENTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 903SW 7425 LEFT HORIZONTAL STABILIZER HAS LEADING EDGE DENT AT SECTION 10.91.DAMAGE FOUND TO BE A MAJOR REPAIR. C/W REO 601R-55-12 -349. OK FOR SERVICE. 2 L 7 2 4F RT A21EA 2007071900360 20070719 00360 EU 2007 7 19 TRBA2007050 1 20070715 A 3350 COVER AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT LOOSE A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 369AT 369 EMERGENCY FLOOR LIGHT AT PASSENGER SEAT 8B HAS BEEN PULLED OUT FROM ITS PROTECTIVE PLASTIC STRIP GUARD COVER. MAINTENAN CE PERSONNEL REPOSITIONED PROTECTIVE PLASTIC STRIP GUARD COVER ON EMERGENCY LIGHT BULB AT ROW 8B AS PER STANDARD PRACTIC E. PERFORMED OPERATIONAL CHECK AS PER ATR 72-AMM 33-51-00. 2 H 7 2 4T RT A53EU 2007071900371 20070719 00371 NM 2007 7 19 F3LA200700173 1 20070707 A 5321 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 933FR 5232 2260 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR PANEL 151VE DAMAGED. REPAIRED FLOOR PANEL 151VE IAW S RM 53-02-00. 2 L 7 2 4F RT A28NM 2007071900378 20070719 00378 SO 2007 7 19 C2XA07IA165 1 20070709 A 3350 20131A BATTERY PACK EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 23139 5814 2512 145731 MCI - FLIGHT 3118, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE OVERWING EMERGENCY EXIT LIGHTS TO BE INOP. MAINT ENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007071900383 20070719 00383 NM 2007 7 19 SWAA073520 1 20070716 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 294 S13L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND STR CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071900384 20070719 00384 NM 2007 7 19 SWAA073516 1 20070716 A 2910 6937317 MODULE BOEING 737 7373Q8 1384670 NM HYD SYSTEM FAULTY A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 317WN 24068 DIVERSION / DECLARED EMERGENCY. HYD A-SYS OVERHEAT LIGHT ILLUMINATED, DIM -TEST C/B TRIPPED AND MASTER CAUTION SYS LOSS . REMOVED AND REPLACED HYD A-SYS PUMP & OVERHEAD HYD CONTROL MODULE PER MM. 2 L 7 2 4F RT A16WE 2007071900392 20070719 00392 NM 2007 7 19 KCSA071213 1 20070715 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1890-1950 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 CORROSION ON MAIN DECK SEAT TRACK BETWEEN BS 1890 AND 1950 AT LBL 76, WL 199. 2 L 7 4 4F RT A20WE 2007071900408 20070719 00408 NM 2007 7 19 SWAA073443 1 20070712 A 5322 69353656 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007072000001 20070720 00001 NM 2007 7 20 SB07055 1 20070716 A 3350 036000570010 FUSE BOEING 737 7374B7 1384702 NM EMERGENCY LIGHTS BLOWN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 454UW 24996 FLL - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 24ABC, 25ABC AND THE R2 DOOR ESCAPE SLIDE EMERGENC Y LIGHT WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FUSES IN THE OVERHEAD CHARGER ASSEMBLIES. OPERATIONAL C HECK GOOD. 2 L 7 2 4F RT A16WE 2007072000010 20070720 00010 EA 2007 7 20 VNAA0705011 1 20070502 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE BS 280 CORRODED A VNAA K NONE O OTHER IN INSP/MAINT 1 GL 05 702PS 10135 RIGHT HAND LOWER WEB (AFT) AT FS 280 IS CORRODED IN MULTIPLE AREAS BEYOND REPAIRABLE LIMITS AND REQUIRES REPLACEMENT. M AINTENANCE PERFORMED REPAIR TO LOWER RIGHT HAND BULKHEAD FS 280 IN ACCORDANCE WITH REO 670-53-11-052. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007072000013 20070720 00013 WP 2007 7 20 ABXR070240 1 20070616 A 5740 5919289521N ATTACH FITTING DOUG DC9 DC932 3022066 WP RIGHT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 697BJ 47799 FORWARD AND AFT SURFACE OF FIXED BRACE ATTACH LUG ON RIGHT TRUNNION WAS CORRODED. REPLACED TRUNNION ON JOB CARD 0317 AN D EA 57430026. 2 L 7 2 4F A6WE 2007072000031 20070720 00031 NM 2007 7 20 USAA070537 1 20070716 A 5340 MOUNT BOEING 737 737401 1384701 NM AFT GIRT BAR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 AFT GIRT BAR SUPPORT MOUNT HAS CORROSION. REMOVED & REPLACED WITH NEW PART PER SRM 51-10-02; CORR TASK C53-107-02; LEVE L 2, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007072000043 20070720 00043 NM 2007 7 20 KCSA071230 1 20070716 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 2030-2150 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 MAIN DECK SEAT TRACK CORRODED BETWEEN BS 2030 AND 2150, LBL 98. 2 L 7 4 4F RT A20WE 2007072000044 20070720 00044 NM 2007 7 20 KCSA071231 1 20070716 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1910-2030 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 MAIN DECK SEAT TRACK CORRODED BETWEEN BS 1910 AND 2030, LBL 98, WL 199. 2 L 7 4 4F RT A20WE 2007072000047 20070720 00047 NM 2007 7 20 SWAA073480 1 20070715 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM BS 520 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007072000060 20070720 00060 NM 2007 7 20 SWAA073487 1 20070715 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 706 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007072000061 20070720 00061 NM 2007 7 20 HNAA0700151 1 20070715 A 2150 78279010 ACM DHAV DHC8 DHC8102 2809003 NM ACM BAY LEAKING A HNAA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 07 812EX 312 ,ACM LEAKING OIL. MECH FOUND ACM LEAKING OIL, BAG BAY SMOKE DET'S REMOVED AND REPLACED. 2 H 7 2 4T RT A13NM 2007072000062 20070720 00062 NM 2007 7 20 CALA0700355 1 20070713 A 5315 BAC1506210 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, S17R TO 17L. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03851. 2 L 7 2 4F RT A16WE 2007072000063 20070720 00063 NM 2007 7 20 CALA0700356 1 20070714 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 867-947 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 867-947, LBL 40. A NEW SEAT TRACK SECTION WAS INSTALLED IAW SRM 53 -00-52, REPAIR 3, FIGURE 201. 2 L 7 2 4F RT A16WE 2007072000067 20070720 00067 NM 2007 7 20 SWAA073486 1 20070715 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 706 S3R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007072000086 20070720 00086 NM 2007 7 20 SWAA073496 1 20070715 A 3350 079123 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 461WN 32465 EEPLS LENS AFT COVER MISSING. INSTALLED COVER ASSY PER MM. 2 L 7 2 4F RT A16WE 2007072000087 20070720 00087 NE 2007 7 20 SWAA073493 2 20070715 A 7230 1663M24P01AP BLADE BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE WARPED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 721347 NR 2 ENG FAN BLADES NR 6 & NR 7 WARPED. REMOVED AND REPLACED BOTH NR 2 ENG FAN BLADES PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2007072000094 20070720 00094 NM 2007 7 20 SWAA073503 1 20070714 A 5311 6546549 FRAME BOEING 737 7373H4 1384600 NM BS 767 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007072000112 20070720 00112 SO 2007 7 20 C2XA07SH041 1 20070713 A 5320 14530643401 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15986 145254 SHV - DURING C-CHECK MAINTENANCE FOUND CENTER OMEGA BEAM WITH CORROSION BETWEEN FRAMES 23 & 25. MAINTENANCE REPAIRED DA MAGE AREA ON CENTER OMEGA BEAM AT FRAME 23 & 25 IAW EMB 145 SRM 53-00-10 FIG 203. AIRCRAFT WAS APPROVED TO RETURN TO SE RVICE. 2 L 7 2 4T RT T00011AT 2007072000113 20070720 00113 SO 2007 7 20 C2XA07SH040 1 20070713 A 5320 14522215411 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15986 145254 SHV - DURING C-CHECK MAINTENANCE FOUND CENTER OMEGA BEAM AT FRAME 60 WITH CORROSION AROUND NUT PLATE. MAINTENANCE REPAI RED CENTER OMEGA BEAM AT FRAME 60 AROUND NUT PLATE USING REPAIR PROCEDURES DESCRIBED ON THE EMB 145 SRM 53-21-10 ITEM 3 FIG 202 IAW EC 5320-01373 REV ORIG. AIRCRAFT APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007072000118 20070720 00118 NM 2007 7 20 USAA070553 1 20070717 A 5313 STRINGER BOEING 737 737401 1384701 NM BS 257 S10L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 STR 10L AT STA 257 HAS CRACK. CUT OUT DAMAGED AREA, FAB'D & INSTALLED REPAIR ANGLE PER SRM 53-10-03, 51-70-11, DEFECT S IZE: .33 INCH. 2 L 7 2 4F RT A16WE 2007072000125 20070720 00125 NM 2007 7 20 UPS07450174 1 20070705 A 7830 SKIN BOEING 747 747200 1384847 NM THRUST REVERSER CHIPPED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C NR 3 ENGINE AFT EXHAUST SLEEVE EXTERNAL SKIN FWD EDGE CHIPPED AT 5 O`CLOCK POSITION. CRACK LENGTH .18 75 INCH. NR 3 ENGINE AFT EXHAUST SLEEVE EXTERNAL SKIN FWD EDGE AT 5 O`CLOCK POS REPAIRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F RT A20WE 2007072000133 20070720 00133 NM 2007 7 20 USAA070545 1 20070717 A 5320 69374024 ANGLE BOEING 737 737401 1384701 NM BS 291 S17 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 APPROX BS 291 STR 17 HAS CRACK. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-10-02, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007072000143 20070720 00143 NM 2007 7 20 2007UALA02484 1 20070708 A 3350 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY LIGHT ROW 4J AFT INOP. RESECURED EMERGENCY LIGHT CONNECTOR. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072000145 20070720 00145 NM 2007 7 20 2007UALA02486 1 20070709 A 3350 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 CABIN E-ZONE LEFT FWD EEL CABLE BROKEN. REPLACED EEL CABLE, OP CHECKED OK REF MM 33-51-12 BY MECH 9602880 & INSP KAL90. [07-27-07] REPLACED EEL CABLE, OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072000147 20070720 00147 NM 2007 7 20 2007UALA02488 1 20070709 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 LEFT OVERWING EMERGENCY LIGHTS INOP, 3RD & 4TH FROM FWD & RIGHT OVERWING EMERGENCY EXIT, 2ND & 3RD FROM FWD. DEFECT IS ACTUALLY 3RD & 4TH LIGHTS FROM FWD. RELAMPED & REPLACED FUSES, OP CHECKED OK REF MM 33-51-03. [07-27-07] DEFECT I S ACTUALLY 3RD & 4TH LIGHTS FROM FWD. RELAMPED & REPLACED FUSES, OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072000148 20070720 00148 NM 2007 7 20 2007UALA02489 1 20070709 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 SEAT 38ABC EEL PLUG BROKEN. REPLACED CONNECTOR, OP CHECKED OK REF MM 33-51-12. [07-27-07] REPLACED CONNECTOR, OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072000149 20070720 00149 NM 2007 7 20 2007UALA02490 1 20070709 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 UPPER DECK CEILING EMERGENCY EXIT LIGHTS INOP, 2ND & 4TH FROM FWD END & UPPER DECK CEILING FWD EMERGENCY EXIT LIGHT ARE INOPERATIVE. RELAMPED, OP CHECKED OK REF MM 33-51-07. [07-27-07] RELAMPED, OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072000152 20070720 00152 NM 2007 7 20 2007UALA02493 1 20070707 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 ALL FIRST CLASS EEL INOP AT RT INBOARD & OUTBOARD SEATS. REPLACED BATTERY PACK,CHECKS OK. [07-27-07] REPLACED BAT TERY PACK. CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072000153 20070720 00153 2007 7 20 2007UALA02494 4 20070707 A 2565 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 4R CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 R-4 DOOR, GIRT BAR RESTRAINT PLATE CORRODED. [08-08-07] REPLACED GIRT BAR RESTRAINT FITTING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072000155 20070720 00155 2007 7 20 2007UALA02496 4 20070709 A 3442 RADAR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU WX SYSTEM INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 372UA 24637 FLIGHT DIVERTED DUE TO LOSS OF WEATHER RADAR. [07-27-07] WEATHER RADAR TRANSCEIVER FAILED. REPLACED THE WEATHE R RADAR TRANSCEIVER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007072000156 20070720 00156 2007 7 20 2007UALA02497 4 20070709 A 2565 HOSE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ESCAPE SLIDE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 RIGHT OFF WING ESCAPE SLIDE INFLATION HOSE FROM INFLATION CYLINDER IS CONTAMINATED WITH HYDRAULIC FLUID AND IS DETERIORA TED. [08-08-07] HOSE IS DETERIORATED AND WALLS HAVE COLLAPSED FROM LONG TERM CONTACT WITH HYDRAULIC FLUID. REPLACE D HOSE ASSY. SLIDE AND AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072000159 20070720 00159 2007 7 20 2007UALA02500 4 20070707 A 2565 TRACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 3L ARMING DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 586UA 26710 F/A REPORTED DOOR 3L WAS HARD TO ARM, ARMING LEVER VERY STIFF. [08-08-07] REMOVED DEBRIS FROM ARMING TRACK. OPERATI ON IMPROVED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072000161 20070720 00161 NM 2007 7 20 2007UALA02502 1 20070707 A 5754 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 3 SLAT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 LEFT WING NR 6 LEADING EDGE SLAT HAS A FOUR INCH LONG BY THREE QUARTER INCH DEEP PIECE OF FIBERGLASS MISSING FROM THE LO WER EDGE CLOSE OUT PANEL. [08-08-07] REPAIRED BY BACKSHOP 273 MECHANIC. REPAIRED PER SHOP MM AND INSPECTED. RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072000164 20070720 00164 NM 2007 7 20 2007UALA02505 1 20070707 A 2597 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY CART FAULTY A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 653UA 25391 ACRID ELECTRICAL ODOR IN AFT GALLEY AREA REPORTED AFTER TAKEOFF, NO SMOKE NOTED. [08-08-07] FOUND GALLEY CART CONNEC TOR WITH PINS DIRTY AND PINS BENT. STRAIGHTENED PINS AND CLEANED CONNECTORS ON BOTH AIRCRAFT AND CART SIDES OF CONNECTIO N. LEFT CART WORKING FOR HALF HOUR NOW OK . AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072000166 20070720 00166 NM 2007 7 20 2007UALA02507 1 20070706 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 661UA 27158 EEL STRIP LIGHTS INOP AT SEATS 8HJ-10HJ. [07-27-07] SECURED CONNECTOR, OPS CK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072000167 20070720 00167 NM 2007 7 20 2007UALA02508 1 20070706 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 661UA 27158 EEL LIGHTS INOP AT SEATS 20HJ-23HJ. [07-27-07] SECURED CONNECTOR, OPS CK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072000168 20070720 00168 NM 2007 7 20 2007UALA02509 1 20070707 A 3397 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 AFT GALLEY LONG EEL STRIP IS INOP. [07-27-07] SECURED FEEDER CABLE. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072000170 20070720 00170 NM 2007 7 20 2007UALA02511 1 20070707 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 LEFT SIDE EXTERNAL EEL LIGHT JUST AFT OF WING IS INOP. [07-27-07] RELAMPED. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072000172 20070720 00172 NM 2007 7 20 2007UALA02512 1 20070706 A 3350 78941 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SEAT 2B INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 672UA 30027 EMERGENCY EXIT LGHT INOP ON SEAT 2B. REPLACED LIGHT ASSY, TEST OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072000174 20070720 00174 NM 2007 7 20 2007UALA02514 1 20070708 A 3510 OXYGEN BOTTLE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 781UA 26945 CREW O2 LOW 300 PSI. [08-08-07] REMOVED AND REPLACED CREW O2 BOTTLE, LEAK CHK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007072000175 20070720 00175 NM 2007 7 20 2007UALA02515 1 20070707 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 ONE EMERGENCY LIGHT INOP AT FWD STAIR. RELAMPED, OPS CHECKS NORMAL. [07-27-07] RELAMPED. OPS. CKS. NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072000177 20070720 00177 NM 2007 7 20 2007UALA02517 1 20070707 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 WALL EEL INOP, RIGHT SIDE FWD GALLEY. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072000178 20070720 00178 NM 2007 7 20 2007UALA02518 1 20070707 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 5E DISLODGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 196UA 28715 SEAT 5E EEL LIGHT IS DISLODGED FROM SEAT. REPAIRED TEAR, ALSO REPLACED BROKEN EXIT EEL LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072000179 20070720 00179 NM 2007 7 20 2007UALA02519 1 20070709 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EXIT LIGHTS 5J AFT, 24 ABC, 38 ABC & 41 HJK ARE INOPERATIVE. RELAMPED EXIT LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072000180 20070720 00180 NM 2007 7 20 2007UALA02520 1 20070709 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EEL AT LAV 110 XAISLE INOPERATIVE. SECURED LAMP CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072000183 20070720 00183 NM 2007 7 20 2007UALA02523 1 20070710 A 2913 PUMP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE HYD SYSTEM INOPERATIVE A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 671UA 30026 LOST LEFT ENGINE DRIVEN HYD PUMP. [08-08-07] REPLACED LEFT HYD ENG PUMP PER MM 29-11-05. OPS CKS OK. NO LEAKS AFTE R SHUTDOWN. AFTER LT HYDRAULIC EDP CHANGE FOUND PUMP LOW PRESSURE LIGHT AND EICAS MSG REPLACED EDP PRESSURE SWITCH. ALSO, REPLACED CONNECTOR ON LT ENGINE HYDRAULIC PUMP DEPRESSURATION VALVE. CHECKS GOOD DURING AND AFTER ENG RUN. NO LEAK S AFTER SHUTDOWN. AIRCRAFT RECEIVED VERIFICATION FLIGHT CHECK AND SYSTEMS OK FOR ETOPS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072000184 20070720 00184 NM 2007 7 20 2007UALA02524 1 20070710 A 2910 LINE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HYD SYSTEM LEAKING A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 398UA 24673 NLG STEERING LOCKS IN BOTH LT & RT TURNS WITH GRINDING NOISE AND VIBRATION. [07-31-07] FOUND HYDRAULIC LINE TO NOSE S TEERING METERING UNIT LEAKING. ROOT CAUSE UNKNOWN. FABRICATED REPLACEMENT HYDRAULIC LINE AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007072300001 20070723 00001 EA 2007 7 23 TRAX200700941 1 20070705 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 872AS 7542 FS 280 FLOORBEAM ANGLE AT RBL 9.0 O/B CRACKED. REMOVED DAMAGED FLOORBEAM ANGLE, DUPLICATED PART FROM 2024-T3 .050, PO 9 50029 AND INSTALLED NEW SERVICEABLE ANGLE, IAW CRJ SRM 51-24-16 AND 51-42-21. 07-12-07. DUPLICATED PART, IAW AND IN CO NJUNCTION WITH REO 601R-53-11-926-B. SUPPLEMENTAL - SDR CLOSED 07/16/07. 2 L 7 2 4F RT A21EA 2007072300002 20070723 00002 WP 2007 7 23 UPS07850180 1 20070713 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK ASSEMBLY IAW MM 33-50-02-2. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2007072300003 20070723 00003 WP 2007 7 23 UPS07850181 1 20070716 A 3397 CONNECTOR DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. SEATED CONNECTOR ON BATTERY PACK & LIGHTS TESTED NORMAL PER 33-50-01 -2 . 2 L 7 4 4F RT 4A25 2007072300004 20070723 00004 WP 2007 7 23 UPS07850182 1 20070713 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:N/A EMERGENCY LIGHTS ARE VERY DIM. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK OK. 2 L 7 4 4F RT 4A25 2007072300005 20070723 00005 NM 2007 7 23 KCSA071232 1 20070716 A 5343 FITTING BOEING 747 747146 1384905 NM MLG TRUNNION CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 CORROSION ON LT BODY LANDING GEAR TRUNNION SUPPORT FITTING IN BEARING BORE AND ON SIDE FACES BS 1470. 2 L 7 4 4F RT A20WE 2007072300006 20070723 00006 NM 2007 7 23 2007UALA02526 1 20070711 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 900 S20L GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 351UA 24319 EXTERNAL FUSELAGE SKIN STA 900 AT SKIN LAP STR 20L IS GOUGED. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR DOUBLER & TR IPLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007072300008 20070723 00008 NM 2007 7 23 2007UALA02528 1 20070709 A 2612 CIRCUIT CARD BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FIRE DETECTION FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 781UA 26945 FIRE LOOP 2 ENG R STATUS MESSAGE. REPLACED CIRCUIT CARD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007072300011 20070723 00011 NM 2007 7 23 2007UALA02533 1 20070710 A 3830 DRAIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LAVATORY TANK CLOGGED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 643UA 25093 RTFL DUE TO AFT LAV TANK INOP LIGHT ILLUMINATED. CREW REPORTED LAVS FULL AND OVERFLOWING. RETURNED TO FIELD DUE TO NO FUNCTIONING LAVS. FOUND DRAINS CLOGGED. UNPLUGGED DRAINS. FOUND 9 CLOTH NAPKINS, 2 RUBBER LAV DOOR SEAL, AND 2 PIEC ES OF POLYURETHANIC SEALS. REMOVED POINT LEVEL SENSORS, INSPECTED INSIDE BOTH WASTE TANKS. TANKS ARE EMPTY. RE-INSTAL LED SENSORS IAW AMM38-33-01. ALL LAV WORKS OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072300012 20070723 00012 NM 2007 7 23 2007UALA02534 1 20070710 A 5310 DOOR FRAME BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE AFT CARGO CUTOUT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 182UA 25279 AFT CARGO CUTOUT FWD UPPER CORNER, BS 1810 STR 27R THE UPPER MAIN SILL FRAME TO SILL CLIP INTERFERES WITH FASTENER INSTA LLATION. MAJOR REPAIR ACCOMPLISHED: TRIMMED CLIP. INSTALLED REPAIR ANGLE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072300013 20070723 00013 NM 2007 7 23 2007UALA02535 1 20070710 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 182UA 25279 AFT CARGO DOOR CUTOUT FWD UPPER CORNER FUSELAGE SKIN CRACKED. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR DOUBLERS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072300015 20070723 00015 2007 7 23 2007UALA02537 4 20070710 A 3160 DISPLAY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT MALFUNCTIONED A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 478UA 1533 LAV AND CARGO DETECTOR FAULT DISPLAYED ON UPPER ECAM SCREEN, SMOKE. REPLACED SCDU. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072300017 20070723 00017 NM 2007 7 23 USAA070542 1 20070717 A 5754 65C26601284 SKIN BOEING 737 737401 1384701 NM NR 6 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 AT 34.5 INCHES FROM I/B END TO 53 INCHES FROM I/B END OF SLAT AT I/B AUX TRACK NR 6 SLAT HAS CRACK. REMOVED DAMAGE & IN STALLED DOUBLER & FILLER PER SRM 57-43-01, REP 6, 51-20-01, DEFECT SIZE: 8 INCHES. 2 L 7 2 4F RT A16WE 2007072300018 20070723 00018 NM 2007 7 23 2007UALA02539 1 20070710 A 3397 WIRE HARNESS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 178UA 24385 DOOR 5R SLIDE EMERGENCY LIGHT FLICKERS ON WHEN DOOR IS CLOSED AND LOCKED. FOUND WIRE HARNESS FAULTY. [08-08-07] FOUN D WIRES W2088-004-20 & W2088-005-20 BROKEN IN FLEX CONDUIT BETWEEN CONNECTOR DX323 & TB214, REF WDM 33-51-61 PG.1 SH.1. REPLACED HARNESS AND GRD CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072300019 20070723 00019 NM 2007 7 23 USAA070541 1 20070717 A 5311 FRAME BOEING 737 737401 1384701 NM BS 440 S9R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 BS 440 S-9R, ATTACH BRACKET FRAME HAS CRACK. INSTALLED DOUBLER PER TR 53-10-20E, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007072300020 20070723 00020 SO 2007 7 23 C2XA07ON011 1 20070715 A 2824 2810051102 VALVE EMB 145 EMB145LR 3260212 SO FUEL SYSTEM LEAKING A C2XA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 27 15555 145594 FLT 403 - BOI TO BOI - AFTER TAKEOFF FROM BOI TOWER ADVISED FUEL LEAKING FROM LEFT WING, RETURNED TO BOI. FUEL FOUND ON UPPER AND LOWER SURFACE OF LEFT WING. MX DISPATCHED MX CREW TO BOI AND INSPECTED AND FOUND LEFT VENT VALVE LEAKING. M X REMOVED AND REPLACED LEFT WING VENT VALVE IAW EMB 145 AMM 28-23-06 AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. THE A/C WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007072300022 20070723 00022 NM 2007 7 23 2007UALA02541 1 20070710 A 3297 TERMINAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU MLG LOOSE A UALA O OTHER N FALSE WARNING DE DESCENT 1 WP 29 369UA 24538 GEAR WARNING HORN SOUNDS WITH THROTTLES IN IDLE AND FLAPS UP. FOUND GROUND GD2858 DC LOOSE AT TERMINAL STUD SECURED LU G, 2 L 7 2 4F 4 F RT A16WE E21EU 2007072300023 20070723 00023 NM 2007 7 23 2007UALA02542 1 20070710 A 2720 INDICATOR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU RUDDER TRIM OUT OF ALIGNMENT A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 938UA 26671 RUDDER TRIM INDICATOR INOPERATIVE. REPLACED RUDDER TRIM INDICATOR. UNIT OFF ALIGNMENT. REPAIRED CONNECTOR PINS AND ALI GNED INDICATOR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007072300024 20070723 00024 NM 2007 7 23 2007UALA02543 1 20070710 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE OVERWING EXIT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 673UA 29241 MULTIPLE EXIT LIGHTS OUT BY FWD OVERWING EXIT. REPLACED BATTERY PACK 2 L 7 2 4F 4 F RT A1NM E24NE 2007080300122 20070803 00122 NM 2007 8 3 2007UALA02545 1 20070710 A 3350 582233 BATTERY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 673UA 29241 EXIT LIGHTS INOP BY 2L. SUPPLEMENTAL DATA UPDATE -REPLACED BATTERY AND LIGHTS TURN ON. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072300028 20070723 00028 NM 2007 7 23 2007UALA02548 1 20070710 A 2432 CHARGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MAIN BATTERY INOPERATIVE A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 561UA 26661 MAIN BATTERY CHARGER DISPLAYED. [08-08-07] REPLACED MAIN BATTERY CHARGER WITH APU BATTERY CHARGER 2 L 7 2 4F 4 F RT A2NM E17NE 2007072300029 20070723 00029 2007 7 23 2007UALA02549 4 20070710 A 2565 SLIDE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LT OVERWING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 836UA 1460 RAMP REPORTS LT OVERWING SLIDE PACK DOOR HAS A VERTICAL CRACK ON AFT EDGE. REPLACED SLIDE ASSY 2 L 7 2 4F 4 F RT A28NM E40NE 2007072300030 20070723 00030 NM 2007 7 23 2007UALA02550 1 20070709 A 3397 CONNECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU ROW 17 FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 337UA 24241 EEL FLOOR LIGHTING INOP FROM ROW 17 ON BACK. [07-27-07] FOUND CONNECTIONS FOR EEL LIGHTS WET. CLEANED AND DRIED CON NECTIONS. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007072300031 20070723 00031 NM 2007 7 23 2007UALA02551 1 20070709 A 2560 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FLASHLIGHT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 641UA 25091 EMERGENCY FLASH LIGHT BETWEEN 1L & 1R FLIGHT ATTENDANT SEAT DOES NOT BLINK. [08-08-07] REPLACED BATTERY AND SEAL. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072300032 20070723 00032 NM 2007 7 23 2007UALA02552 1 20070709 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 661UA 27158 EMERGENCY LIGHT STRIP FOUND TORN UP IN LEFT AISLE ADJACENT TO BUSINESS CLASS GALLEY. [07-27-07] REPLACED EEL LAMP AS SY OPS NORMAL 2 L 7 2 4F 4 F RT A1NM E24NE 2007072300033 20070723 00033 NM 2007 7 23 UPS07M50175 1 20070716 A 3350 BATTERY PACK DOUG MD11 MD11F 3023600 NM EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP 48745 ON PRE-DEPARTURE CHECK EMERGENCY LIGHT TEST SHOWS EMERGENCY LIGHT BATTERY 1 LOW. PER FIM 33-51-00-1. REMOVED AND REPLA CED EMERGENCY LIGHTING BATTERY POWER SUPPLY PER MM 33-51-01-4. OPS CHECK GOOD. 2 L 7 3 4F RT A22WE 2007072300037 20070723 00037 NE 2007 7 23 2007UALA02555 2 20070710 A 7200 SOLENOID AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE 7TH STAGE FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 470UA 1427 CREW REPORTS DURING ENG 1 START GOT START FAULT, ENG STALL, EGT OVERLIMIT FAULT, ENG AUTO CRANKED & S- DOWN, NO EGT LIMI TS EXCEEDED. FOUND 7TH STAGE "A" CONTROL SOLENOID FAILED. REPLACED 7TH STAGE "A" CONTROL SOLENIOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072300039 20070723 00039 NM 2007 7 23 2007UALA02557 1 20070709 A 3510 OXYGEN SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 COCKPIT O2 IS LOW AT 1200 PSI. [07-31-07] SERVICE O2 TO CORRECT LEVEL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007072300041 20070723 00041 2007 7 23 2007UALA02559 4 20070710 A 2565 LATCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE OVERWING SLIDE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 RIGHTHAND OVERWING SLIDE COMPARTMENT DOOR NR 3 LATCH WORN. REMOVED & REPLACED LATCH AND KEEPER. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072300044 20070723 00044 NM 2007 7 23 2007UALA02562 1 20070710 A 2613 OVERHEAT LOOP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 1 FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 219UA 30551 BLEED LOOP 1 WING R FAILURE OF RIGHT WING DUCT LEAK DETECTION LOOP OR CENTER DUCT LEAK OVERHEAT DETECTION SYSTEM (DLODS) CARD. [08-08-07] CHECKED FOR DUCT LEAK RH AC PACK-BAY AREA. ALSO CHKED FOR DAMAGE OF SENSOR ELEMENTS. ALL SENSORS ARE OK. UNABLE TO DUPLICATE DEFECT. NO MSG FOUND. OVER HEAT FIRE DET TEST PASSED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007072300045 20070723 00045 NM 2007 7 23 2007UALA02563 1 20070710 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 797UA 26924 BOTH EEL LIGHTS AT SEAT 1E ARE INOP. [07-27-07] REPLACED BOTH EEL STRIPS, OPS CK OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007072300047 20070723 00047 NM 2007 7 23 2007UALA02565 1 20070710 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 DOOR 3R FWD SILL EMERGENCY LIGHT IS INOP. [07-27-07] RELAMPED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072300048 20070723 00048 NM 2007 7 23 2007UALA02566 1 20070710 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 UPPER DECK CEILING 2 EA EMERGENCY LIGHT IS INOP. [07-27-07] RELAMPED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072300049 20070723 00049 NM 2007 7 23 2007UALA02567 1 20070710 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LT OVERWING INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 FWD ASSY FWD EMERGENCY LIGHT IS INOP. [07-27-07] RELAMPED LEFT OVERWING EMERGENCY LIGHT ASSY. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072300052 20070723 00052 EA 2007 7 23 TRAX200700944 1 20070705 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 872AS 7542 COCKPIT FLOORBOARD SUPPORT ANGLE AT FS 280 HAS CORROSION. UPON FURTHER INVESTIGATION OF COCKPIT FLOORBOARD SUPPORT ANGL E AT FS 280 HAS MINOR SURFACE CORROSION. REMOVED MINOR CORROSION FROM ANGLE, IAW CRJ SRM 51-21-06. ALODINED, PRIMED AN D TOPCOATED, IAW CRJ SRM 51-21-16. REMOVED COCKPIT FLOORBOARD SUPPORT ANGLE AT FS 280, TO PERFORM THE ABOVE CORRECTIVE ACTION. 07/05/07 INSTALLED COCKPIT FLOORBOARD SUPPORT, IAW CRJ SRM 51-42-06. 07/12/07 MINOR SURFACE CORROSION WITHIN SERVICEBLE LIMITS, IAW CRJ SRM 53-11-43. 07/12/07 SUPPLEMENTAL - SDR CLOSED 07/16/07. 2 L 7 2 4F RT A21EA 2007072300053 20070723 00053 EA 2007 7 23 TRAX200700946 1 20070705 A 5310 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA BS 605 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 CORROSION AT FS 605 BELOW FLOOR IN CARGO BAY. REFER TO WO 63655 N/R-00150 AND 00160 FOR CORRECTIVE ACTION. SUPPLEMENTA L SDR - CLOSED 07/16/07. 2 L 7 2 4F RT A21EA 2007072300056 20070723 00056 EA 2007 7 23 TRAX200700960 1 20070706 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 310-349 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 SERVICE DOOR FLOOR SUPPORT STRINGER CORRODED BETWEEN FS 310-349. REMOVED UPPER -239 ATTACH ANGLE. REMOVED CORRODED -25 3 ANGLE, STRINGER AND 2EA FWD & AFT ATTACH BRACKETS. REMOVED 3EA CENTER CLIPS. DRILLED, REAMED NEW -253 ANGLE IAW CRJ 200 SRM 51-40-11. 07/12/2007 INSTALLED NEW -253 ANGLE IAW CRJ200 SRM 51-42-06. INSTALLED -253 ANGLE CLIPS AND APPLIED CORROSION INHIBITOR PER CRJ200 SRM 51-42-20. APPLIED CIC AT SERVICE DOOR -253 ANGLE. SUPPLEMENTAL - SDR CLOSED 07/16/ 07. 2 L 7 2 4F RT A21EA 2007072300058 20070723 00058 NM 2007 7 23 2007UALA02569 1 20070709 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE DOOR MOUNTED DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 DOOR MOUNTED EMERGENCY LIGHT QUICK DISCHARGE AT DOOR 1L. [08-07-07] REPLACED WITH SERVICEABLE EMERGENCY LIGHT. SY STEM OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072300059 20070723 00059 NM 2007 7 23 2007UALA02570 1 20070710 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 LEFT UPPER DECK EMERGENCY EXIT LIGHT INOP. [07-27-07] RELAMPED, OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072300060 20070723 00060 NM 2007 7 23 2007UALA02571 1 20070709 A 3350 SWITCH BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY LIGHTS COME ON WITH THE SWITCH IN THE ON AND OFF POSITION. [07-27-07] RESET AND SECURED EMERGENCY LIGHTS S WITCH AT 1L. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072300061 20070723 00061 NM 2007 7 23 2007UALA02572 1 20070709 A 2600 LOOP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CARGO BAY UNKNOWN A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 198UA 28716 FWD CARGO 1 LOOP -B- EICAS STATUS MESSAGE DISPLAYED. [08-07-07] REPLACED SMOKE DETECTOR 1 LOOP B. PERFORMED FIRE T EST. TEST PASS. MSG CLEARED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072300063 20070723 00063 NM 2007 7 23 2007UALA02574 1 20070711 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHT INOP AT 1A AFT. [08-07-07] REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072300066 20070723 00066 EU 2007 7 23 2007UALA02577 1 20070711 A 5322 SHEAR TIE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 436UA 638 SHEAR TIE CLIP CORRODED AT FRAME 31 BETWEEN STR 40R - 41R. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED SHEAR TIE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072300067 20070723 00067 EU 2007 7 23 2007UALA02578 1 20070712 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 436UA 638 LEFT FUSELAGE SKIN IS DENTED 6 INCHES ABOVE AND 18 INCHES AFT OF STATIC PORT, LOCATED WITHIN RVSM AREA. MAJOR REPAIR AC COMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072300069 20070723 00069 EU 2007 7 23 2007UALA02580 1 20070711 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 491UA 1741 EMERGENCY LIGHT SYSTEM FAILS TEST, FAULTS PWR SUPPLY ABOVE DOOR 1L. [07-27-07] REPLACED BATTERY AND UNIT NOW CHECKS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072300070 20070723 00070 2007 7 23 2007UALA02581 4 20070711 A 2565 HOLDER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU DOOR 1L GIRT BAR BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 330UA 24191 GIRT BAR HOLDER ON SLIDE PACK AT DOOR 1L BROKE OFF. [08-08-07] REPLACED SLIDE PACK AND GIRT BAR CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007072300072 20070723 00072 EU 2007 7 23 YENA2007064 1 20070717 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU CABIN ODOR A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 594JB 2284 FLT 411, BOS TO SAN. PRIOR TO DESCENT, F/A NOTIFIED OF A RUBBER, ELECTRICAL ODOR OUT OF THE A/C AFT GALLEY LT SIDE EYEB ALL VENT. ODOR WENT AWAY QUICKLY. ACCOMPLISHED TSM TASK 24-00-00-801-823, NO DEFECTS NOTED. UNABLE TO DUPLICATE ODOR, MEL 25-22-03-6-D APPLIED PRECAUTIONARY. INOP AFT GALLEY COFFEEMAKERS. [07-24-07] REMOVED AND REPLACED NR 3 AFT GAL LEY COFFEE MAKER PER MM 25-30-01.OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 2007072300076 20070723 00076 NM 2007 7 23 2007UALA02584 1 20070711 A 2150 A/C PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 590UA 28708 FOUL ODOR IN AIR COND SYSTEM DURING DESCENT AT IDLE. MAINT TEXT: CREW REPORTED, OIL BURNING ODOR IN COCKPIT & FWD CABI N. CREW SUSPECT ODOR IS FROM LT PACK. ODOR - OIL BURNING ODOR WAS DETECTED ON GROUND WITH PACKS ON. [08-08-07] CRE W SUSPECT ODOR IS FROM LT PACK.. OIL BURNING ODOR WAS DETECTED ON GRD WITH PACKS ON. AFTER PERFORMED TROUBLESHOOTING , FOUND RT HYDRAULIC SYSTEM OVERSERVICED. DRAINED RT SYSTEM TO APPROPRIATE LEVEL AND RAN ENGINES. NO MORE ODOR DETECTE D. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072300078 20070723 00078 EA 2007 7 23 TRAX200700949 1 20070706 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 872AS 7542 RIGHT FS 484 INTERCOSTAL ANGLE CRACKED AT RBL 36.0. REMOVED CRACKED ANGLE AT RBL 36.0 FS RIGHT 484. DUPLICATED ANGLE F ROM 2024-T3, .063 IAW REO 601R-53-41-059. ALODINED, PRIMED, AND PAINTED ANGLE AND INSTALLED ANGLE IAW REO 601R-53-41-05 9. PERFORMED PRESSURIZATION LEAK CHECK IAW CRJ AMM 21-31-00. NO DEFECTS NOTED. SUPPLEMENTAL - SDR CLOSED 07/17/07. 2 L 7 2 4F RT A21EA 2007072300080 20070723 00080 NM 2007 7 23 UPS07550126 1 20070706 A 2150 A/C PACK BOEING 757 75724APF 1384969 NM RIGHT INOPERATIVE A IPXA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 01 445UP 27390 INSPECTION TYPE:N/A DIVERSION - RIGHT PACK WOULD NOT HOLD CABIN PRESSURE. SMOKE IN THE COCKPIT. EMERGENCY WAS DECLARED . FLIGHT LANDED IN PIT WITHOUT FURTHER INCIDENT, CREW EVACUATED THROUGH COCKPIT WINDOWS. *S/D* REMOVED AND REPLACED O UTFLOW VALVE ACTUATOR. SYSTEM OPS NORMAL PER MM 21-31-04-4. PRESSURE CHECKED A/C WITH BOTH ENGINES AND APU. NO FAULTS WITH PACK SYSTEM. OPS NORMAL. A/C OK CHECK WAS GOOD. ALL SYSTEMS TIGHT. 2 L 7 2 4F RT A2NM 2007072300081 20070723 00081 EA 2007 7 23 TRAX200700962 1 20070706 A 5310 BEAM CNDAIR CL600 CL6002B19 1900309 EA BS 349 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 STA 349 CORRODED AT SERVICE DOOR TRANSVERSE BEAM RBL 45. BEAM RBL 45. WORK COMPLETED IN ACCORDANCE WITH: SRM 51-21-0 6, 53-00-00, 51-42-16, REO 601R-53-21-782, 51-20-06, 51-42-06, AND 20-21-00. 2 L 7 2 4F RT A21EA 2007072300082 20070723 00082 NE 2007 7 23 SA07048 2 20070712 A 7320 3380599510 SENSE LINE AIRBUS A321 A321211 3930370 EU GE CFM56 CFM56* 13802 NE ZONE 400 CRACKED A USAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 19 172US 1472 FLIGHT 1522, SFO-CLT: AFTER TAKEOFF, POWER ON NUMBER 1 ENGINE ROLLED BACK. NO SHUTDOWN OCCURRED. FLIGHT RETURNED TO S FO. MAINTENANCE REPLACED THE NUMBER ONE ENGINE HMU AND FUEL PUMP - NO HELP. FOUND THE NUMBER ONE ENGINE PS3 SENSE LINE DAMAGED. REPLACED THE PS3 LINE TO THE NUMBER ONE ENGINE. 2 L 7 2 4F 4 F RT A28NM E2GL 2007071800395 20070718 00395 EU 2007 7 18 MALA070073 1 20070704 A 5101 STRUCTURE SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A MALA E ENGINE SHUTDOWN W INADEQUATE Q C TX TAXI/GRND HDL 1 GL 15 437XJ 340B437 AIRCRAFT HAD ARRIVED TO MSP AFTER LANDING FLIGHT 2788 WITH PASSENGERS ON BOARD. AIRCRAFT TAXIED TO GATE AREA AND WAS WA ITING AT CIRCLE 95. AIRCRAFT 8896 WAS PUSHED BACK AND LEAVING FROM B14 WHEN JET BLAST FROM THE CRJ PUSHED BAG CARTS FR OM THE GOPHER AREA. ONE CART MADE CONTACT WITH THE RT SIDE OF N437XJ BELOW FO'S SIDE WINDOW. ENGINE WAS SHUTDOWN BY CR EW TO AVOID A POSSIBLE PROP STRIKE WITH BAG CART. INSTALLED FLUSH REPAIR TO DAMAGE ON RT SIDE OF A/C JUST BELOW AND A F EW FEET BEHIND FO'S WINDOW IAW EO NR S53044. 2 L 7 2 4T RT A52EU 2007071900003 20070719 00003 NM 2007 7 19 07FDEA02475 1 20070713 A 5320 655835222 FLOOR SUPPORT BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD CARGO AREA, STA 718, STR 27R ABOUT RBL 12, FLOOR SUPPORT ANGLE IS CORRODED ON REPAIR ANGLE. REMOVED AND INSTALLED N EW REPAIR ANGLE IAW SRM 51-40-3. 2 L 7 3 4F RT A3WE 2007071900022 20070719 00022 EA 2007 7 19 TRAX200700933 1 20070705 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 753EV 10169 CORROSION AT FS 280 FRAME TO FS 295 FRAME BETWEEN STRINGERS 26L AND 26R BL 0 (MARKED). REMOVED CORROSION FROM FS 295 L OWER FRAME. DAMAGE FOUND TO BE WITHIN LIMITS IAW CRJ 700 SRM 53-21-06. REMOVED AND REPLACED FOUR SOLID RIVETS ON FS 29 5 FRAME ON RT SIDE OF BL 0. RESTORED FINISH TO SURFACE. WORK DONE IAW CRJ 700 SRM 51-00-00. SUPPLEMENTAL - SDR CLOSED 07/10/07. 2 L 7 2 4F RT A21EA 2007071900038 20070719 00038 EA 2007 7 19 TRAX200700920 1 20070703 A 5210 BRACKET CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 753EV 10169 ASD LOWER SIDE WALL ANGLE BRACKET CRACKED (MARK). REMOVED FASTENERS, MOTOR PULLEY BRACKET AND DID CUT-OUT IAW BOMBARDIE R REO 670-52-11-072. EDDY CURRENT INSPECTED, NO CRACKS NOTED PER NDTM 51-20-06. FABRICATED PARTS AND INSTALLED IAW BOM BARDIER REO 670-52-072. SUPPLEMENTAL - SDR CLOSED 07/10/07. 2 L 7 2 4F RT A21EA 2007071900046 20070719 00046 WP 2007 7 19 07FDEA02484 1 20070713 A 5313 LONGERON DOUG MD10 MD1010F 3022112 WP BS 1501-1521 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CLG WHEEL WELL CAVITY, CORROSION ON LONGERON END FITTING AT STA 1501 TO 1521, LONGERON 49L REMOVED CORROSION ON LONGERON END FITTING AND FOUND TO BE WITHIN LIMITS IAW DC/MD10-10 SRM53-00-01 FIG 1B VOL 1. ORIGINAL THICKNESS 0.130" MATERIAL LOSS 0.007", MATERIAL REMAINING 0.123". ALODINED PRIMED AND PAINTED FITTING IAW DC/MD10-10 SRM 51-21-01 VOL 2. 2 L 7 3 4F RT A22WE 2007071900047 20070719 00047 EU 2007 7 19 0627070144 1 20070627 A 6720 L673M40A1003 ACTUATOR UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1A NE TAIL SERVO LEAKING E E3MA K NONE O OTHER AA AIR AMBULANCE 1 EA 03 522ME 40 40 0144 LEAKING FLUID FROM HOUSING BEYOND SERVICEABLE LIMITS. 1 G 7 2 3U 3 U H88EU E34NE 2007071900053 20070719 00053 NM 2007 7 19 07FDEA02445 1 20070712 A 5311 6515932 FRAME BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD CARGO AREA, STA 718, STR 28R, RBL 8 FLOOR SUPPORT CORRODED ON REPAIR ANGLE. REMOVED CORRODED REPAIR ANGLE, VERIFIED MATERIAL AS BAC1517-1507 7075-T6. FABRICATED NEW REPAIR ANGLE, INSTALLED NEW REPAIR ANGLE, TREATED AND PRIMED NEW REPAI R ANGLE. INSTALLED NEW REPAIR ANGLE REF SRM 51-40-3 FIG 1 SHT 3. 2 L 7 3 4F RT A3WE 2007071900059 20070719 00059 NM 2007 7 19 07FDEA02495 1 20070716 A 5720 STOP FITTING DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 LEFT WING OUTBOARD FLAP SECONDARY UP STOP FITTING FOUND CRACKED. [08-02-07] REMOVED CRACKED FITTING AND INSTALLED NEW FITTING AT LT WING OUTBOARD FLAP AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007071900063 20070719 00063 EU 2007 7 19 SIMA200719401 1 20070711 A 3350 35916451 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 263AE 26698 340B263 EXIT SIGN AT ROW 8 NOT ILLUMINATING. REMOVED AND REPLACED EMERGENCY LIGHT IAW SAAB AMM 33-50-00. OPERATIONAL CHECK GOO D, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007071900073 20070719 00073 SO 2007 7 19 SIMA200719409 1 20070621 A 5347 14000486005 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 811AE 13526 5000 145529 LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 23 TO 28. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERAT IONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900074 20070719 00074 NM 2007 7 19 UPS07550148 1 20070615 A 5412 311N3271 BULKHEAD BOEING 757 75724APF 1384969 NM NR 1 PYLON DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 420UP 23907 INSPECTION TYPE:C GOUGE AT NR 1 LEFT AFT LOWER BULKHEAD (PANEL RACK). BULKHEAD MILL AND NDT WERE DONE ON TRAV T7/682612 . FILLER WAS FABED REF TRAV T7/687613 PRELIMINARY 1 EA 757-5453-27-A1688. SHOT PEEN REWORK AREA PER SOPM 20-10-03 AND PRELIMINARY 1 EA 757-5453-27-A1688. 2 L 7 2 4F RT A2NM 2007071900094 20070719 00094 SO 2007 7 19 SIMA200719415 1 20070705 A 5347 14532605015 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 717AE 15889 5000 145272 LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 36 TO 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERA TIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900099 20070719 00099 SO 2007 7 19 SIMA200719416 1 20070705 A 5347 13500434005 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 717AE 15889 5000 145272 LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 17 TO 23. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERA TIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900118 20070719 00118 CE 2007 7 19 DXTA200702333 1 20070713 A 3222 STRUT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG UNDERSERVICED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 982QS 7500182 COULD NOT RETRACT GEAR AFTER DEPARTURE. GEAR HANDLE WAS LOCKED IN THE DOWN POSITION AND COULD NOT BE MOVED. JACKED A/C, FOUND NLG STRUT DID NOT EXTEND. SERVICED STRUT AND OLEO IAW MM CH 12-10-38. PERFORMED GEAR SWING IAW MM CH 32-30-00. NO DEFECTS NOTED. DOWN JACKED A/C AND SERVICED HYD RES IAW MM CH. 12-10-15. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071900119 20070719 00119 EA 2007 7 19 TRAX200700969 1 20070707 A 7603 POWER LEVER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT STUCK A ASOA K NONE O OTHER CL CLIMB 1 SO 27 907EV 7648 ON DEPARTURE THE LEFT THRUST LEVER WAS STUCK AT TAKEOFF POWER AND WOULD NOT COME BACK. THE N1 WAS SET AT T/O POWER FOR ABOUT 25 MINUTES. AFTER APPROX 20 MINUTES, GOT IT TO COME BACK TO CRUISE POWER. EMERGENCY DECLARED. FLT 4534 DEL 20 M INS. 2 L 7 2 4F RT A21EA 2007071900122 20070719 00122 CE 2007 7 19 DXTA200702328 1 20070710 A 5100 NONE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE NONE NONE E DXTA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 312QS 5600312 DURING THE TAKEOFF ROLL AT APPROXIMATELY 65 KTS, WE HIT A FLOCK OF BIRDS AND ABORTED THE TAKEOFF. (M2B) COMPLIED WITH F OD INSPECTIONS IAW MM. CHAPTER 05-50 MM. CHAPTER 72-00, AND NJA CE-560 AAIP. NO DISCREPANCIES NOTED. 2 L 7 2 4F 4 F RT A22CE E25EA 2007071900133 20070719 00133 SO 2007 7 19 C2XA07RI053 1 20070709 A 4950 4504113 APU EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 15985 7983 145248 FLT 2445 - EWR - CREW REPORTED APU BLEED PRODUCING SMOKE IN CABIN AND COCKPIT. EWR MX PERFORMED OPERATIONAL CHECK AND C OULD NOT DUPLICATE THE PROBLEM. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007071900140 20070719 00140 CE 2007 7 19 DXTA200702340 1 20070716 A 3260 INDICATION SYS CESSNA 680 680CE 2076811 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 307QS 6800130 UPON GEAR RETRACTION RED (UNLOCK) STAYED ON. CYCLE GEAR DOWN (3) GREEN, LANDING UNEVENTFUL. [07-23-07] PERFORMED FU NCTIONAL TEST OF MASTER WARNING SYSYTEM IAW HAWKER 800XP MM. 31-50-00. FUNCTIONAL CHECKS NORMAL NO DEFECTS NOTED. 2 L 7 2 4F 4 F RC T00012WI E25EA 2007071900145 20070719 00145 EU 2007 7 19 HAEA002002007 1 20070717 A 5341 ATTACH FITTING AMD FALC20 FALCONE 2720305 EU GE CF700 CF7002D2 30010 NE FUSELAGE CORRODED E HAEA K NONE O OTHER IN INSP/MAINT 1 SW 05 285TW 22773 285 DURING TANK AND PLANK INSPECTION THE LT AND RT WING TO FUSELAGE ATTACH FITTINGS WERE DISCOVERED TO HAVE MINOR CORROSION ON THE LOWER OB SURFACE. THE WINGS WERE DEMATED TO INSURE THAT CORROSION HAD NOT MIGRATED TO BETWEEN THE WING TO FUSELA GE ATTACH FITTINGS. CORROSION WAS EVALUATED BY ENGINEERING AND AN ENGINEERING INSTRUCTION WAS ISSUED. CORROSION WAS WOR KED IAW THE ENGINEERING INSTRUCTION. NO FURTHER ACTION REQUIRED. [CLOSED] 2 L 7 2 4F 4 F A7EU E7EA 2007071900151 20070719 00151 SO 2007 7 19 RAIA00707015 1 20070708 A 2913 971808 PUMP EMB 145 EMB145LR 3260212 SO NR 1 ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 CE 03 819HK 15278 9019 145062 FLT NR 5532 - STL - NR 1 HYDRAULIC SYSTEM OVERHEAT MESSAGE. MAINTENANCE GROUND RAN ENGINE. REMOVED AND REPLACED NR 1 E NGINE HYDRAULIC PUMP AND NR 1 TEMP SWITCH. OPS CHECK GOOD, NO RELATED CMC MESSAGES. 2 L 7 2 4T RT T00011AT 2007071900155 20070719 00155 SO 2007 7 19 RAIA00707020 1 20070709 A 3350 SIGN EMB 145 EMB145LR 3260212 SO CABIN UNSECURE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 815HK 145048 POST FLT NR 5586 - STL - EMERGENCY EXIT SIGN FALLING DOWN AT EMERGENCY EXIT. MAINTENANCE RESECURED SIGN. 2 L 7 2 4T RT T00011AT 2007071900161 20070719 00161 EA 2007 7 19 COMA0760463 1 20070701 A 2797 WIRE CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP NICKED A COMA K NONE J WARNING INDICATION CR CRUISE 1 SO 01 914CA 7012 FLIGHT 5589 - FLAP FAIL MESSAGE RECEIVED. DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. REPAIRED NICKED WIRE (SHORTING ) AT PRESSURE BULKHEAD AFT OF WHEEL WELL. 2 L 7 2 4F RT A21EA 2007071900162 20070719 00162 EA 2007 7 19 COMA0760464 1 20070702 A 3297 140153 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA LT MLG DAMAGED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 929CA 29623 7035 FLIGHT 5300 - ABORTED TAKEOFF APPROX 105 - 110 KTS DUE TO ANTI-SKID CAUTION MESSAGE. REPLACED LEFT OUTBOARD LOWER MLG H ARNESS ASSEMBLY. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007071900166 20070719 00166 EA 2007 7 19 COMA0760466 1 20070703 A 2750 855D100 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 735CA 2041 7267 FLIGHT 5175 - RECEIVED FLAP FAIL MESSAGE AFTER TAKEOFF. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MEGGED LEFT AN D RIGHT BPSU HARNESSES AND BPSU'S. REPLACED LEFT AND RIGHT BPSU'S. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007071900167 20070719 00167 EA 2007 7 19 COMA0760467 1 20070703 A 2421 755469E IDG CNDAIR CL600 CL6002B19 1900309 EA RIGHT ENGINE FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 810CA 4418 7370 FLIGHT 5356 - REJECTED TAKEOFF AT 60 KTS. RECEIVED GEN 2 CAUTION MESSAGE. REPLACED NR 2 IDG AND TEMP BULB. 2 L 7 2 4F RT A21EA 2007071900168 20070719 00168 EA 2007 7 19 COMA0760468 1 20070705 A 2760 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 1900309 EA SPOILER SYS TRIPPED A COMA K NONE J WARNING INDICATION DE DESCENT 1 SO 01 735CA 7267 FLIGHT 5298 - FLIGHT SPOILERS AND SPOILERON CAUTION MESSAGE DISPLAYED. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. RE SET CIRCUIT BREAKER. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007071900169 20070719 00169 EA 2007 7 19 COMA0760469 1 20070706 A 5210 601R386493 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA FAULTY A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 967CA 7134 FLIGHT 5134 - AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE AND A LOUD NOISE CAME FROM THE MAIN CABIN DOOR. AIRCRAFT RET URNED TO AIRPORT, LANDED WITHOUT INCIDENT. REPLACED PRESSURE FLAP CONTROL PANEL. 2 L 7 2 4F RT A21EA 2007071900190 20070719 00190 NM 2007 7 19 SWAA073399 1 20070711 A 5330 6545877 BEAR STRAP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT L1 DOOR UPPER HINGE CUTOUT LOWER CORNER. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007071900191 20070719 00191 SO 2007 7 19 SIMA200719709 1 20070705 A 5347 13500439001 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 717AE 15889 5000 145272 LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 23 TO 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRA FT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900200 20070719 00200 SO 2007 7 19 SIMA200719714 1 20070708 A 5347 14000486007 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 816AE 13301 5000 145552 LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 28 TO 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900202 20070719 00202 SO 2007 7 19 SIMA200719805 1 20070522 A 5320 14524131009 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 15926 5000 145224 FORWARD CABIN FLOOR U-SHAPE AT FRAME 17 AND STRINGER 16 LEFT SIDE CORRODED. REMOVED AND REPLACED BRACKET IAW EMB SRM 51 -40-02. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900215 20070719 00215 NM 2007 7 19 SWAA073415 1 20070711 A 3397 8100022602 CONNECTOR BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 245WN 32506 EEPLS INOP AT ROW 1 ABC. SECURED LOOSE CONNECTOR AT LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007071900230 20070719 00230 NM 2007 7 19 KCSA071212 1 20070712 A 5314 KEEL FITTING BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 TEMPORARY REPAIR INSTALLED AT LEFT DRAG STRUT/KEEL BEAM ATTACHMENT FITTING AND THE SUPPORT BRACKET IS CRACKED AT STA 141 6. 2 L 7 4 4F RT A20WE 2007071900231 20070719 00231 SO 2007 7 19 C2XA07TY036 1 20070712 A 3350 8232 SIGN EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11140 145732 TYS - DURING A SCHEDULED MAINTENANCE CHECK THE AISLE HEADLINER EMERGENCY EXIT SIGN WAS FOUND INOP. THE SIGN WAS REMOVED AND REPLACED IAW EMB 145XR AMM 33-50-15 AND OPS CHECKED GOOD. 2 L 7 2 4F RT 2007071900235 20070719 00235 EA 2007 7 19 TRAX200700961 1 20070706 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 ASD FLOOR SUPPORT ANGLE ABOVE STRINGER CORRODED 310-349. BLENDED CORROSION ON ASD FLOOR SUPPORT ANGLE ABOVE STRINGER, W ITHIN LIMITS. REMOVED CLIPS PRIMED ANGLE IAW CRJ 200 SRM 51-21-06. SUPPLEMENTAL - SDR CLOSED 07/13/07. 2 L 7 2 4F RT A21EA 2007071900244 20070719 00244 NM 2007 7 19 SWAA073412 1 20070709 A 3350 MS155721 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 242WN 32505 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007071900245 20070719 00245 NM 2007 7 19 SWAA073397 1 20070711 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED A1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007071900255 20070719 00255 NM 2007 7 19 UPS07550164 1 20070712 A 5321 FLOOR PANEL BOEING 757 75724APF 1384969 NM MAIN DECK CARGO PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 469UP 25485 INSPECTION TYPE:N/A MAIN DECK CARGO FLOOR PANEL NEXT TO LEFT SIDEWALL AT POS 7-8 5 X 5 INCH AREA HAS PUNCTURE AND GOUGES (PUNCTURES AFFECTING SKIN). TEMPORARY REPAIR PER EO B757-5320-18249 (4) PUNCTURES AFFECTING UPPER SKIN AND HONEYCOMB C ORE (C) PAGE 6. 2 L 7 2 4F RT A2NM 2007071900285 20070719 00285 NM 2007 7 19 2007UALA02476 1 20070706 A 3350 LIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 912UA 25290 FLOOR EEL LIGHTS INOPERATIVE FROM SEAT 9B TO 15A. [07-27-07] SECURED EEL LIGHTS FEEDER CABLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071900289 20070719 00289 EU 2007 7 19 TRBA2007047 1 20070711 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHTS INOPERATIVE A TRBA O OTHER O OTHER NR NOT REPORTED 1 SO 29 550LL 550 WITH BATTERY POWER OFF, EMERGENCY EXIT LIGHT INOPERATIVE AT FWD OVERHEAD AND WINDOW EXIT LIGHT. REMOVED AND REPLACED EM ERGENCY BATTERY PACK AT 43WL IAW JIC NR33-51-71. OP CK OK. 2 H 7 2 4T RT A53EU 2007071900314 20070719 00314 EA 2007 7 19 SWIA200718457 1 20070710 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 979SW 7954 FLT 5911 - FLT 5911 - MAIN CABIN DOOR WOULD NOT OPEN AFTER FLIGHT. CYCLED DOOR MANY TIMES. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007071900315 20070719 00315 SO 2007 7 19 SWIA200718458 1 20070618 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 RIGHT FORWARD STRINGER IN NR 1 FUEL BAY OF RIGHT WING IS CRACKED, DISCOVERED AT C-CHECK. REPAIRED RIGHT FORWARD STRINGE R IN NR 1 FUEL BAY IAW EMB 120 SRM 57-20-03 FIG 202. 2 L 7 2 4T RT A31SO 2007071900320 20070719 00320 SO 2007 7 19 SWIA200718463 1 20070618 A 2710 COUNTERWEIGHT EMB 120 EMB120ER 3260203 SO LT AILERON MIGRATED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 LEFT AILERON OUTBOARD LEAD WEIGHT HAS MIGRATED OUT DUE TO CORROSION AND IS RUBBING ON BEARING SUPPORT, DISCOVERED AT C-C HECK. REPLACED LEFT AILERON LEAD WEIGHT IAW EMB 120 MM 27-00-00 AND 51-61-01. 2 L 7 2 4T RT A31SO 2007071900346 20070719 00346 NM 2007 7 19 SWAA073434 1 20070712 A 5553 6546872 FITTING BOEING 737 7375H4 138449D NM VERTICAL FIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND VERTICAL FIN PRIMARY FITTING CLEVIS LUGS CORRODED. REPAIRED FITTING CLEVIS LUGS PER E R. 2 L 7 2 4F RT A16WE 2007071900347 20070719 00347 NM 2007 7 19 SWAA073450 1 20070712 A 5310 6547955 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT LOWER FWD CORNER. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007071900348 20070719 00348 NM 2007 7 19 SWAA073431 1 20070712 A 5313 6551698 STRINGER SPLICE BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER ER. 2 L 7 2 4F RT A16WE 2007071900349 20070719 00349 NM 2007 7 19 SWAA073435 1 20070712 A 5313 6551698 STRINGER SPLICE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 16L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007071900350 20070719 00350 NM 2007 7 19 SWAA073449 1 20070712 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071900351 20070719 00351 NM 2007 7 19 SWAA073425 1 20070712 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED C3 CHECK, FOUND RIGHT WING NR 4 L/E SLAT CRACKED AT AFT INBOARD END. REPAIRED SLAT PER SWA EA. 2 L 7 2 4F RT A16WE 2007071900352 20070719 00352 NM 2007 7 19 SWAA073437 1 20070712 A 5754 65C26602 SLAT BOEING 737 7375H4 138449D NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, FOUND LRFT WING NR 2 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007071900353 20070719 00353 NM 2007 7 19 SWAA073444 1 20070712 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071900354 20070719 00354 NM 2007 7 19 SWAA073440 1 20070712 A 5311 65C33509 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071900355 20070719 00355 EA 2007 7 19 SWIA200718479 1 20070711 A 2701 SHAFT CNDAIR CL600 CL6002C10 1390015 EA CONTROL COLUMN LOOSE A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 766SK 10232 FLT 6757 - WHILE ON FINAL, FIRST OFFICER REPORTS THAT THE AILERONS FELT STIFF AND STICKY. RETORQUED FORWARD AND AFT NUT S ON CONTROL YOKE SHAFT IAW AMM 27-31-01. 2 L 7 2 4F RT A21EA 2007071900361 20070719 00361 EU 2007 7 19 TRBA2007052 1 20070714 A 3240 ANTI-SKID SYS AEROSP ATR72 ATR72212 8680945 EU MLG MALFUNCTIONED A TRBA O OTHER O OTHER LD LANDING 1 SO 29 417AT 417 NUMBER 2 MAIN TIRE LOCK-UP DURING LANDING. TIRE NEEDS TO BE CHANGED. MAINTENANCE REPLACED NUMBER 2 MAIN WHEEL ASSY IAW ATR 72-JIC-12-37-32-RAI-10000-001. PERFORMED ANTI-SKID OPERATIONAL TEST IAW ATR-72-AMM32-42-00-FUT-10000-001. 2 H 7 2 4T RT A53EU 2007071900380 20070719 00380 NM 2007 7 19 SWAA073517 1 20070716 A 5330 6545774 SKIN BOEING 737 737317 138447P NM BS 780 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULE SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007071900389 20070719 00389 NM 2007 7 19 KCSA071227 1 20070715 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 850-880 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 CORROSION ON SEAT TRACK I/B RADIUS STA 850 TO 880 LBL 12 WL 199. 2 L 7 4 4F RT A20WE 2007071900391 20070719 00391 NM 2007 7 19 KCSA071229 1 20070715 A 5315 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 1220 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA 1220 LBL 113 AFT SIDE LOWER FLOORBEAM WEB IS CRACKED 1.5 INCH. 2 L 7 4 4F RT A20WE 2007071900394 20070719 00394 NM 2007 7 19 KCSA071215 1 20070715 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1950-1990 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 CORROSION ON MAIN DECK SEAT TRACK I/B RADIUS FROM BS 1950 TO 1990, RBL 12, WL 199. 2 L 7 4 4F RT A20WE 2007071900395 20070719 00395 WP 2007 7 19 ASAA0781867 1 20070711 A 5311 991960563 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 AFT CARGO BAY FRAME CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPLACEMENT SECTION PER SRM 51-10-4, 51-30-2 AND DAC DWG 9919605. 2 L 7 2 4F RT A6WE 2007071900396 20070719 00396 NM 2007 7 19 KCSA071216 1 20070715 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1720 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 CORROSION ON MAIN DECK SEAT TRACK O/B RADIUS AT BS 1720, LBL 76, WL 199. 2 L 7 4 4F RT A20WE 2007071900402 20070719 00402 NM 2007 7 19 KCSA071222 1 20070715 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1620-1720 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 CORROSION ON MAIN DECK SEAT TRACK I/B RADIUS FROM BS 1620 TO 1720, RBL 12, WL 199. 2 L 7 4 4F RT A20WE 2007072000009 20070720 00009 EA 2007 7 20 VNAA0705010 1 20070502 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE BS 280 CORRODED A VNAA K NONE O OTHER IN INSP/MAINT 1 GL 05 702PS 10135 LEFT HAND LOWER WEB AT BULKHEAD FS 280, WL 73 IS CORRODED AT VARIOUS AREAS; THE BIGGEST BEING 4"L X 1.5"W. MAINTENANCE PERFORMED REPAIR TO LOWER LEFT HAND BULKHEAD FS 280 IN ACCORDANCE WITH REO 670-53-11-052. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007072000011 20070720 00011 EA 2007 7 20 COMA0760489 1 20070716 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FS 621.00 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 965CA 27846 7131 REAR PRESSURE BULKHEAD CRACKED AROUND LINTEL FITTING. PERFORMED PERMANENT REPAIR TO AFT PRESSURE BULKHEAD IAW REO 601R- 53-11-563. 2 L 7 2 4F RT A21EA 2007072000015 20070720 00015 2007 7 20 SWAA073456 4 20070714 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 445WN 29841 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007072000016 20070720 00016 2007 7 20 SWAA073453 4 20070713 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 267WN 32525 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007072000018 20070720 00018 NM 2007 7 20 SWAA073463 1 20070715 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 519 S12L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 519, STR 12L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007072000019 20070720 00019 NM 2007 7 20 SWAA073491 1 20070715 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM BS 361-372 S19R DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 606SW 27926 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CREASED BETWEEN BS 361 AND BS 372, STR 19R. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2007072000021 20070720 00021 NM 2007 7 20 SWAA073464 1 20070715 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 784 S26R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 784, STR 26R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007072000024 20070720 00024 NM 2007 7 20 SWAA073459 1 20070714 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM BS 930 S25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007072000025 20070720 00025 NM 2007 7 20 SWAA073473 1 20070715 A 5311 6545815 FRAME BOEING 737 7373H4 1384600 NM BS 342 S6L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 342, STR 6L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007072000026 20070720 00026 NM 2007 7 20 SWAA073478 1 20070715 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007072000027 20070720 00027 NM 2007 7 20 SWAA073469 1 20070715 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007072000028 20070720 00028 NM 2007 7 20 USAA070540 1 20070716 A 5340 ATTACH BRACKET BOEING 737 737401 1384701 NM BS 380 S9L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 BS 380 S-9L, A/C ATTACH BRACKET FRAME HAS CRACK. INSTALLED DOUBLER PER TR 53-10-20E, DEFECT SIZE: .25 INCH. 2 L 7 2 4F RT A16WE 2007072000030 20070720 00030 NM 2007 7 20 USAA070538 1 20070716 A 5340 ATTACH BRACKET BOEING 737 737401 1384701 NM BS 400 S9R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 BS 400 S-9R, ATTACH BRACKET FRAME HAS CRACK. INSTALLED DOUBLER PER TR 53-10-20E, DEFECT SIZE: .5 INCH. 2 L 7 2 4F RT A16WE 2007072000033 20070720 00033 NM 2007 7 20 USAA070535 1 20070716 A 5320 SUPPORT ANGLE BOEING 737 737401 1384701 NM BS 883 LBL 38 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 BS 883 LBL 38, WEB Z-SUPPORT ANGLE HAS CORROSION. REMOVED & FAB'D NEW Z-WEB PER SRM 51-20-01, 51-10-02; CORR TASK C53-1 07-02; LEVEL 2, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007072000034 20070720 00034 NM 2007 7 20 USAA070534 1 20070716 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 949 LBL 47 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 BS 949 LBL 47 HAS CORROSION. REMOVED & REPLACED WITH NEW PART PER SRM 51-10-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007072000036 20070720 00036 NM 2007 7 20 USAA070532 1 20070716 A 5315 BAC14902734 FLOORBEAM BOEING 737 737401 1384701 NM BS 344 LBL 15 & CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 STA 344 LBL 15 & BL 0 HAS CORROSION. REMOVED DAMAGED PART & INSTALLED MODIFIED PRT PER SRM 53-10-51 REPAIR 5; CORR TASK C53-107-02, DEFECT SIZE: 15 X 1 INCH. 2 L 7 2 4F RT A16WE 2007072000037 20070720 00037 NM 2007 7 20 USAA070531 1 20070716 A 5315 BAC1505100246 FLOORBEAM BOEING 737 737401 1384701 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 STA 328 BL 0 - LBL 65 HAS CORROSION. INSTALLED REPAIR PARTS PER TR 53-15-01; CORR TASK C53-107-01; LEVEL 2, DEFECT SIZE : 36 X .5 INCH. 2 L 7 2 4F RT A16WE 2007072000038 20070720 00038 NM 2007 7 20 USAA070530 1 20070716 A 5320 6517688U165 ANGLE BOEING 737 737401 1384701 NM BS 277-360 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 STA 277 TO 360 RBL 60 ST 17R HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-10-02; CORR LEVEL 2; TASK C53-107-02, DEFECT SIZE: 10 INCHES. 2 L 7 2 4F RT A16WE 2007072000040 20070720 00040 NM 2007 7 20 USAA070528 1 20070716 A 5320 6516788U165 ANGLE BOEING 737 737401 1384701 NM BS 259-360 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 BS 259-360 RT THRESHOLD AREA, EACH FASTENER HAS CORROSION. REMOVED & REPLACED ZEE ANGLE PER SRM 51-10-02; CORR LEVEL 2; TASK C53-107-02, DEFECT SIZE: 1 INCH. 2 L 7 2 4F RT A16WE 2007072000042 20070720 00042 NM 2007 7 20 UPS07550173 1 20070713 A 3350 LAMP BOEING 757 75724APF 1384969 NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 457UP 25478 EXTERIOR EMERGENCY EGRESS LIGHT INOP. RELAMPED PER AMM 33-51-06-2, OPS CHECK NORMAL. 2 L 7 2 4F RT A2NM 2007072000045 20070720 00045 EU 2007 7 20 USAABA07010 1 20070714 A 3244 31596 TIRE AIRBUS 330 A330323 3930335 EU MLG LEAKING A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 276AY 12313 3148 0375 FLIGHT 718, PHL-FCO: DURING FLIGHT, CREW NOTICED THE LEFT NOSE TIRE PRESSURE SLOWLY DROPPING. FLIGHT DIVERTED TO BOS. MAINTENANCE REPLACED BOTH NOSE TIRES. 2 L 7 2 4F RT A46NM 2007072000046 20070720 00046 NM 2007 7 20 SWAA073476 1 20070715 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007072000049 20070720 00049 NM 2007 7 20 SWAA073479 1 20070715 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007072000050 20070720 00050 NM 2007 7 20 SWAA073475 1 20070715 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007072000051 20070720 00051 NM 2007 7 20 SWAA073472 1 20070715 A 5310 6546959 CREASE BEAM BOEING 737 7373K2 13844BA NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM CRACKED AT BS 520, RBL 70. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2007072000052 20070720 00052 NM 2007 7 20 SWAA073470 1 20070715 A 5312 6549574 BULKHEAD BOEING 737 7373K2 13844BA NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD CORRODED AT BS 1016, LBL 1. REPAIRED BULKHEAD PER SRM AND BOEI NG DRAWING. 2 L 7 2 4F RT A16WE 2007072000054 20070720 00054 NM 2007 7 20 SWAA073474 1 20070715 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM BS 360 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007072000055 20070720 00055 NM 2007 7 20 SWAA073477 1 20070715 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM BS 360 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007072000058 20070720 00058 NM 2007 7 20 SWAA073489 1 20070715 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727E S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007072000059 20070720 00059 NM 2007 7 20 SWAA073488 1 20070715 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727B S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007072000064 20070720 00064 NM 2007 7 20 CALA0700357 1 20070715 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 887-927 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 887-927, RBL 20. A REPAIR SPLICE SEAT TRACK WAS INSTALLED IAW SRM 53-00-52, REPAIR 3, FIGURE 201. 2 L 7 2 4F RT A16WE 2007072000071 20070720 00071 NM 2007 7 20 SWAA073465 1 20070715 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 420 S28L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007072000072 20070720 00072 NM 2007 7 20 SWAA073466 1 20070715 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 380 S25L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007072000075 20070720 00075 NM 2007 7 20 SWAA073457 1 20070714 A 3397 8100022704 CONNECTOR BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 470WN 33860 EEPLS INOP BETWEEN ROW 13 ABC AND ROW 17 ABC. FOUND LOOSE CONNECTOR, SECURED CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2007072000077 20070720 00077 NM 2007 7 20 SWAA073471 1 20070715 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373K2 13844BA NM BS 773 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 773, RBL 3. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007072000078 20070720 00078 NM 2007 7 20 SWAA073460 1 20070714 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 776WN 30591 DURING SCHEDULED MV2 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007072000082 20070720 00082 EA 2007 7 20 VNAA0705013 1 20070502 A 5310 CC670341757 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE BS 280 CORRODED A VNAA K NONE O OTHER IN INSP/MAINT 1 GL 05 702PS 7582 10135 FS 280 FRAME, AT WL 73 IS CRACKED BETWEEN RBL 9 AND RBL 18 APPROXIMATELY .5 INCH L, AT UPPER AFT CHANNEL. MAINTENANCE R EMOVED AND REPLACED FRAME AT WL 73 FS 280 AS REQUIRED IN ACCORDANCE WITH THE AIRCRAFT STRUCTURE REPAIR MANUAL 51-42-06- 001-001-A01. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007072000083 20070720 00083 NM 2007 7 20 SB07054 1 20070717 A 3397 WIRE BOEING 737 737401 1384701 NM EMERGENCY LIGHTS PINCHED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 BDL - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 24 AND 25, LEFT-HAND SIDE, WERE INOPERATIVE. MAINT ENANCE FOUND SEAT ROW 25 HAD PINCHED WIRES. REWIRED AND REROUTED WIRES. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007072000084 20070720 00084 EA 2007 7 20 COMA0760473 1 20070711 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 735CA 7267 FLIGHT 5512 - RECEIVED NOSE GEAR DISAGREE AFTER TAKEOFF. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. FOUND NLG CEN TERED/EXTENDED PROXIMITY SENSOR OUT OF ADJUSTMENT. ADJUSTED SENSOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007072000090 20070720 00090 2007 7 20 SWAA073497 4 20070715 A 2565 416A2205 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 747SA 29799 L1 DOOR EVAC SLIDE LOOSE. SECURED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2007072000091 20070720 00091 NM 2007 7 20 SWAA073500 1 20070713 A 5311 6545808 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT STR 4L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007072000092 20070720 00092 NM 2007 7 20 SWAA073513 1 20070716 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM BS 520 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007072000095 20070720 00095 2007 7 20 SWAA073495 4 20070715 A 2565 6557463 HOOK BOEING 737 7373H4 1384600 NM L1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 L1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED GIRT BAR HOOKS PER MM. 2 L 7 2 4F RT A16WE 2007072000096 20070720 00096 NM 2007 7 20 SWAA073499 1 20070713 A 5523 6573799 TAB BOEING 737 7373H4 1384600 NM RT ELEVATOR DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 DURING SCHEDULED BRDG CHECK, FOUND RT ELEV TAB DELAMINATED AT OUTBOARD L/E. REPAIRED ELEV TAB PER SRM. 2 L 7 2 4F RT A16WE 2007072000098 20070720 00098 NM 2007 7 20 CALA0700361 1 20070716 A 5330 65516242 SKIN BOEING 737 7373T0 1384582 NM BS 1006 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND SKIN STRAP CORRODED AT STA 1006, S27R, BL 0 TO RBL 8. THE CORRODED SECTION OF SKIN STRAP WAS REMOVED A ND A DOUBLER AND TRIPLER WERE INSTALLED IAW ECRA 5331-01327. 2 L 7 2 4F RT A16WE 2007072000099 20070720 00099 NM 2007 7 20 CALA0700362 1 20070716 A 5315 6546812 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016, LBL 26 TO RBL 30. THE FLOORBEAM UPPER CHORD WAS REPLACED IAW ECRA 5310 -03851. 2 L 7 2 4F RT A16WE 2007072000100 20070720 00100 NM 2007 7 20 CALA0700363 1 20070716 A 5311 65C25723 FRAME BOEING 737 7373T0 1384582 NM BS 616 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A .25 INCH CRACK IN MAIN FRAME AT STA 616, LBL 55. A REPAIR WAS INSTALLED IAW ECRA 5311-01158. 2 L 7 2 4F RT A16WE 2007072000101 20070720 00101 SO 2007 7 20 C2XA07CL062 1 20070713 A 3230 23092900001 UPLOCK EMB 135 EMB135ER 3260203 SO RT MLG FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 17507 19579 145215 ABE FLIGHT 2054 - THE CREW REPORTED A LANDING GEAR LEVER DISAGREE MESSAGE UPON GEAR RETRACTION. THE AIRCRAFT RETURNED T O ABE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT MAIN GEAR UPLOCK BOX. OPERATIONAL CHEC KS WERE GOOD. 2 L 7 2 4F RT T00011AT 2007072000102 20070720 00102 NM 2007 7 20 SWAA073511 1 20070716 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM BS 727D S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007072000105 20070720 00105 NM 2007 7 20 SWAA073505 1 20070716 A 5313 BAC1798 STRINGER BOEING 737 7373H4 1384600 NM BS 500B-510A DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE STRINGER 9R DAMAGED BETWEEN BS 500B TO BS 510A. REPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 2007072000106 20070720 00106 NM 2007 7 20 SWAA073504 1 20070716 A 5313 BAC1798 STRINGER BOEING 737 7373H4 1384600 NM BS 360-460 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE STRINGER 9L DAMAGED BETWEEN BS 360 TO BS 460. REPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 2007072000107 20070720 00107 2007 7 20 SWAA073506 4 20070716 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2007072000108 20070720 00108 2007 7 20 SWAA073507 4 20070716 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2007072000109 20070720 00109 NM 2007 7 20 SWAA073508 1 20070716 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 719SW 27853 DURING SCHEDULED HC2 CHECK, AFT EMERGENCY EXIT LIGHTS BATTERY PACK FAILED THE CAPACITY TEST. REMOVED AND REPLACED BATTE RY PACK PER MM. 2 L 7 2 4F RT A16WE 2007072000114 20070720 00114 SO 2007 7 20 C2XA07RI055 1 20070712 A 3350 110049 CHARGER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13964 145123 CREW REPORTED OVERWING EMERGENCY LIGHT INOP. MX MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGER. OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007072000115 20070720 00115 EU 2007 7 20 YENA2007063 1 20070711 A 3350 32145410 EPSU AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS NO TEST A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 568JB 16700 2063 EMERGENCY LIGHTS AT OVERWING EXITS INOP. REMOVED AND REPLACED 12WL EPSU AS PER AMM 33-51-38. OPS CHECK OK. 2 L 7 2 4F RT A28NM 2007072000119 20070720 00119 NM 2007 7 20 USAA070552 1 20070717 A 5340 6548657U126 ATTACH FITTING BOEING 737 737401 1384701 NM FAIRING WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 RT SIDE AFT FAIRING ATTACH POINT WORN. DEFECTIVE PART REPLACED WITH IDENTICAL PART, DEFECT SIZE: 2 X 2 INCHES. 2 L 7 2 4F RT A16WE 2007072000120 20070720 00120 NM 2007 7 20 USAA070551 1 20070717 A 5531 RIB BOEING 737 737401 1384701 NM VERTICAL FIN CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 VERTICAL FIN FWD RIB BOTTOM LEFT & RIGHT SIDE AT STA 1007.55 CHAFED. REMOVED DAMAGED AREA, INSTALLED DOUBLER PER SRM 53 -30-09, 51-70-11; EA 98755, DEFECT SIZE: 8 AND 12 INCHES. 2 L 7 2 4F RT A16WE 2007072000121 20070720 00121 NE 2007 7 20 UPS07650169 2 20070715 A 7230 COMPRESSOR BOEING 767 76734AF 1385212 NM GE CF6 CF680C2B7 NE LT ENGINE STALLED A IPXA J A DUMP FUEL UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 01 334UP 32844 INSPECTION TYPE:ETOP ATB - RT ENGINE COMPRESSOR STALL. ENGINE CHANGE IN PROGRESS. TAT - 19043; TAC - 5073; TET - 239 23; TEC - 7253; TSR/4647. [07-23-07] REMOVED AND REPLACED NR 2 ENGINE IAW TC 6002. VERIFIED OPS AND LEAK CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E13NE 2007072000122 20070720 00122 NE 2007 7 20 UPS07650170 2 20070716 A 7261 OIL SYSTEM BOEING 767 76734AF 1385212 NM GE CF6 CF680C2B7 NE LT ENGINE OVERTEMP A IPXA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 01 326UP 27752 INSPECTION TYPE:ETOP IFSD - LT ENGINE HIGH OIL TEMP IN AMBER A/C IS OOS TAC = 25693; TAT = 5073; ET = 22841; TEC = 6814; TSLV/TSR = 1123. [07-25-07] ALL CHECKS FOUND NORMAL. R & R LT ENG EEC PER AMM 72-21-15-4. ACCOMPLISHED LT ENGINE AD JUSTMENT IAW 71-00-00-2. 2 L 7 2 4F 4 F RT A1NM E13NE 2007072000123 20070720 00123 WP 2007 7 20 UPS07850166 1 20070705 A 5280 SKIN DOUG DC8 DC873F 302199F WP NLG DOOR DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 DENTS ON NLG RT/STRUT DOOR EXTERIOR SKIN. CUT OUT DAMAGED AREA ON RT/NLG STRUT DOOR IAW SRM 52-02-00 FIG 4. FABRICATED AND INSTALLED REPAIR DOUBLER ON RT/NLG STRUT DOOR IAW SRM 52-02-00 FIG 004. 2 L 7 4 4F RT 4A25 2007072000127 20070720 00127 NM 2007 7 20 UPS07550188 1 20070717 A 5610 WINDOW BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 459UP 25480 PREFLIGHT ESCAPE WINDOW WILL NOT OPEN (WINDOW JAMS). CAPTAIN'S NR 2 WINDOW OPS CHECK NORMAL IAW 757 AMM 56-10-04-4. 2 L 7 2 4F RT A2NM 2007072000128 20070720 00128 WP 2007 7 20 UPS07850172 1 20070703 A 5330 SKIN DOUG DC8 DC873F 302199F WP FS 1740 L19R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 CRACK ON EXTERIOR FUSE SKIN AT STA 1740 L19R. CUT OUT DAMAGED AREA ON FUSELAGE SKIN AT STA 1740 L19R IAW SRM 53-02-01 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER, FINGER DOUBLER, AND FILLER AT STA 1740 L19R IAW SRM 5 3-02-01 FIG 7. 2 L 7 4 4F RT 4A25 2007072000129 20070720 00129 WP 2007 7 20 UPS07850178 1 20070708 A 5542 SKIN DOUG DC8 DC873F 302199F WP RUDDER CANNING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C2 RIGHT SIDE OF RUDDER SKIN ZR 271 HAS OIL CANNING. REMOVED SKIN PANEL ON RT/SIDE OF RUDDER AT ZR 271 IAW SRM 51-1-21. FABRICATED AND INSTALLED RUDDER SKIN PANEL ON RT/SIDE OF RUDDER STA ZR 271 IAW SRM 51-1-21, AND DWG 56 555077. 2 L 7 4 4F RT 4A25 2007072000132 20070720 00132 NM 2007 7 20 USAA070546 1 20070717 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM BS 351-360 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 STRINGER 16L INTERCOSTAL, BS 351 HAS CRACK. FABRICATED INTERCOSTAL & REPLACED WEB AND STRAP PER SRM 53-10-04, DEFECT SI ZE: .375 INCH. 2 L 7 2 4F RT A16WE 2007072000134 20070720 00134 NM 2007 7 20 USAA070544 1 20070717 A 5313 65516989 STRINGER SPLICE BOEING 737 737401 1384701 NM BS 907 S4R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 BS 907 S-4R HAS CRACK. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-10-02, DEFECT SIZE: .75 INCH. 2 L 7 2 4F RT A16WE 2007072000138 20070720 00138 NM 2007 7 20 2007UALA02483 1 20070708 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY LIGHT ROW 1J AFT INOP. RELAMPED EMERGENCY LIGHT. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072000140 20070720 00140 EA 2007 7 20 COMA0760474 1 20070711 A 2750 860D10018 ECU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 528CA 9721 7481 FLIGHT 5011 - FLAP FAIL CAUTION RECEIVED ON TAXI OUT. RETURNED TO GATE. REPLACED FECU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007072000141 20070720 00141 2007 7 20 COMA0760475 4 20070712 A 2212 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 588SW 7069 FLIGHT 5482 - FAILED TO GET CONFIG MESSAGE ON TAKEOFF. IAPS DEGRADED MESSAGE FOLLOWED. TAKEOFF WAS ABORTED. CHECKED M DC FOR IAPS DEGRADED FAULT HISTORY, WITH NO FAULT CODES DISPLAYED. OPS CHECK OF IAPS GOOD. 2 L 7 2 4F RT A21EA 2007072000142 20070720 00142 EA 2007 7 20 COMA0760476 1 20070712 A 5210 601R318723 SEAL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR FAILED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 443CA 7539 FLIGHT 5169 - LOUD NOISE AT MAIN PAX DOOR. AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED PAX D OOR SEAL. 2 L 7 2 4F RT A21EA 2007071800254 20070718 00254 SO 2007 7 18 GM07003 1 20070710 A 5321 FON2323333193 FLOORBOARD GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE BS 426 CORRODED E UG8A K NONE O OTHER IN INSP/MAINT 1 GL 23 5101 5623 550 CORROSION DISCOVERED ON ALL FLOORBOARD INSERTS AFT OF FS 426.5. 2 L 7 2 4F 4 F RT A12EA E00057EN 2007071800261 20070718 00261 NE 2007 7 18 2007UALA02416 2 20070704 A 7261 MANIFOLD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OIL BREATHER CRACKED A UALA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 WP 29 559UA 26657 726560 NR 2 ENGINE EGT EXCEEDED 645 DEGREES, NOT DURING SURGE. PEAK EGT WAS 664. CREW COMMENTS, AT TAKEOFF WITH FULL THRUST F OR WEATHER LASTED FOR 6 MINUTES. TEMP WAS 664C. 10-05-07 FOUND BREATHER MANIFOLD CRACKED AND CLAMP BROKEN. 10 QTS O F OIL WAS ADDED AFTER BREATHER MANIFOLD WAS REPLACED. CHECKED C-D, NO DEBRIS FOUND. REMOVED AND REPLACED THE ANGLE GEA RBOX RADIAL DRIVE LOWER SHAFT AND OIL DUCT PER SHOP JOB CARDS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071800265 20070718 00265 NM 2007 7 18 2007UALA02420 1 20070705 A 2432 LIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 910UA 25254 AIRCRAFT FAILS STANDBY POWER TEST. STANDBY POWER LIGHT DOES NOT ILLUMINATE WHEN STANDBY POWER IS TURNED OFF, AC POWER R EMAINS ON. [07-27-07] FAULTY STANDBY POWER RELAY AND STANDBY AC VOLTAGE SENSOR. REPLACED THE STANDBY POWER RELAY (R238) AND STANDBY AC VOLTAGE SENSOR (M562). 2 L 7 2 4F 4 F RT A16WE E21EU 2007071800267 20070718 00267 EA 2007 7 18 N6WA00707001 1 20070711 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE CABIN INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 162 10254 CABIN CEILING LEVEL EMERGENCY LIGHT OUT. DEFERRED CEILING LEVEL EMERGENCY LIGHT IAW MEL 35-01-2A. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007071800302 20070718 00302 NM 2007 7 18 2007UALA02431 1 20070706 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY LIGHT ON DOOR 1R FWD SILL LIGHT INOP. [07-24-07] RELAMPED EMERGENCY LIGHT. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071800313 20070718 00313 EU 2007 7 18 2007UALA02442 1 20070706 A 2620 EXTINGUISHER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE AFT LAVATORY UNSERVICEABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 490UA 1728 F/A REPORTS FIRE EXTINGUISHER IN AFT LAV SHOWS PRESSURE ON RED BAND. REMOVED AND REPLACED AFT LAV FIREXT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071800315 20070718 00315 EU 2007 7 18 2007UALA02446 1 20070706 A 5270 TARGET AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR OUT OF ADJUST A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 427UA 512 FLIGHT DIVERTED DUE TO DOOR 2L OPEN INDICATION. NO LOSS OF CABIN PRESSURIZATION. PROX TARGET OUT OF ADJUSTMENT. CLEA NED AND ADJUSTED TARGET. INDICATION NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071800322 20070718 00322 CE 2007 7 18 DXTA200702302 1 20070627 A 2497 RH5068OHM RESISTOR RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP ZONE 100 OVERHEATED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 871QS 917 258763 VISUALLY SAW SMOKE IN THE VICINITY OF THE APU PANEL ALONG WITH A STRONG SMELL OF ELECTRICAL FIRE. NOTE-NO FIRE WAS SEEN OR INDICATED. REMOVED OVERHEATED RESISTOR PN RH50-68 OHM AND INSTALLED NEW RESISTOR PN RH50-68OHM IN STALL VANE HEAT O N (DR) PANEL. PERFORM OPERATIONAL CHECK OF THE SYSTEM, FOUND NO DISCREPANCY AT THIS TIME. WORK PERFORMED IAW MM CHAPTER 31-20-05. 2 L 7 2 4F 4 F RT A3EU E6WE 2007071800348 20070718 00348 EU 2007 7 18 2007UALA02462 1 20070708 A 3350 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 456UA 1128 EPSU INT LOAD FWD L MESSAGE ON EMERGENCY LIGHT TEST. [07-27-07] RESET BATTERY EMERGENCY TEST OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071800355 20070718 00355 NM 2007 7 18 2007UALA02467 1 20070706 A 5240 TORQUE TUBE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT GALLEY DOOR EXCESS PLAY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 AFT GALLEY DOOR CUTOUT TORQUE TUBE HAS MOVEMENT BEYOND .003. [07-31-07] REMOVED TORQUE TUBE, SPIGOT, AND BOTH GUIDE PLATES WITH BEARINGS. REINSTALLED BOTH GUIDE PLATES WITH NEW BEARINGS AND INSTALLED NEW TORQUE TUBE AND SPIGOTS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071800358 20070718 00358 NM 2007 7 18 2007UALA02470 1 20070706 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 AFT PIT STA 807 BETWEEN STR 27R AND 27L AT BL 0, SHEAR TIE IS CRACKED IN RADIUS AT OUTER SKIN. [07-27-07] MAJOR RE PAIR: ACCOMPLISHED SHEAR TIE REPLACEMENT AT STA 807 STR 27R TO STR 27L. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071800359 20070718 00359 NM 2007 7 18 2007UALA02471 1 20070706 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 LWR AFT FUSELAGE BELLY SKIN, BS 807 BL 0 BETWEEN STRINGERS 27L-27R HAS LARGE DENT ADJACENT TO FRAME CAUSING FASTENER PRO TRUSION. [07-27-07] MAJOR REPAIR: REMOVED DAMAGE AND REPAIRED THE SKIN BY INSTALLING A DOUBLER. REFERENCE SRM 53-0 0-01 REPAIR 13. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071800361 20070718 00361 NM 2007 7 18 2007UALA02473 1 20070706 A 2710 CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RT AILERON MISROUTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 369UA 24538 RIGHT AILERON CABLE MISROUTED ABOVE CONTROL QUADRANT CASTING DAMAGE TO CABLE AND AILERON QUADRANT ATTACH HARDWARE. [07 -31-07] REMOVED AND REPLACED MISROUTED CABLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071800375 20070718 00375 NM 2007 7 18 SWAA073367 1 20070709 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 434WN 32454 EEPLS COVER LOOSE AT ROW 2 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007071800377 20070718 00377 2007 7 18 SWAA073381 4 20070708 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 459WN 32497 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071800378 20070718 00378 NM 2007 7 18 SWAA073361 1 20070708 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 390, STR 27L. REPAIRED SKI N PER SB. 2 L 7 2 4F RT A16WE 2007071800385 20070718 00385 WP 2007 7 18 07FDEA02462 1 20070713 A 5730 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 500 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 EXISTING REPAIR LT WING I/B FLAP LOWER SKIN. REPAIRED IAW SRM 57-00-01 VOL 1 FIG 1A SHT 2. 2 L 7 3 4F A22WE 2007071800387 20070718 00387 WP 2007 7 18 07FDEA02464 1 20070713 A 5310 BEAM DOUG DC10 DC1010F 3022111 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 FWD CARGO COMPT ON BEAM FOUND CRACK. REPAIRED BEAM IAW SRM 53-00-01 VOL 1 FIG 9 SHT 7. 2 L 7 3 4F A22WE 2007071800402 20070718 00402 NM 2007 7 18 SWAA073379 1 20070709 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071800412 20070718 00412 NM 2007 7 18 SWAA073377 1 20070709 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071900002 20070719 00002 WP 2007 7 19 07FDEA02474 1 20070713 A 5311 FRAME DOUG DC10 DC1010F 3022111 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 AVIONIC COMPT ON FRAME FOUND CRACKS. REPAIRED AREA IAW SRM 53-30-00 VOL 1 FIG 11. 2 L 7 3 4F A22WE 2007071900023 20070719 00023 WP 2007 7 19 07FDEA02483 1 20070713 A 5313 LONGERON DOUG MD10 MD1010F 3022112 WP BS 1501-1521 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 LONGERON 51L IN CLG AREA BETWEEN STA 1501 AND 1521 CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW MD10-10 S RM 53-00-01 VOL 1 FIG 1A. REMOVED AND REPLACED LONGERON SECTION IAW MD10-10 SRM 53-00-01 FIG 9, VOL 1, AND 51-35-01 VOL 2. FABRICATED LONGERON SECTION AND REPAIR SPLICES IAW MD10-10 SRM 53-00-01 FIG 9 VOL 1, AND 51-21-01 VOL 2. 2 L 7 3 4F RT A22WE 2007071900042 20070719 00042 SO 2007 7 19 SIMA200719405 1 20070621 A 5347 14530658007 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 811AE 13526 5000 145529 RIGHT INBORAD SEAT TRACK CORRODED BETWEEN FRAMES 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERA TIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900043 20070719 00043 SO 2007 7 19 SIMA200719406 1 20070621 A 5347 13500439007 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 811AE 13526 5000 145529 LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 19 TO 23. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERAT IONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900056 20070719 00056 WP 2007 7 19 070138 1 20070705 A 2613 10200012 BULB DOUG DC9 DC983 3022083 WP LT CSD MALFUNCTIONED A WX0A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 19 863GA 49911 AIRCRAFT 863 FLIGHT 706 CREW REPORTED LEFT CSD TEMP GAUGE RED LINED WITH APPROXIMATELY 15 DEGREE RISE. PERFORMED QRH AN D DISCONNECTED CSD. THE LEFT CSD WAS DEFERRED BY ALLEGIANT AIR MTX CONTROL. FLIGHT 781 CREW REPORTED APU DROPPED OFF L INE, AIRCRAFT DIVERTED TO MEMPHIS, TN. ALLEGIANT AIR MTX PERSONNEL WERE DISPATCHED FROM SANFORD, FLORIDA TO MEMPHIS,TN TO INSPECT AND REPAIR, CSD MEL AND APU DISCREPANCY. THE APU OIL LEVEL WAS VERIFIED AND APU OPERATIONAL CHECK PERFORMED AT FULL LOAD AND OPERATION WAS NORMAL. THE LEFT CSD OUTLET TEMP BULB WAS REPLACED AND OPERATIONAL LOAD CHECK PERFORMED N ORMAL. CSD MEL WAS CLEARED AND THE APU DISCREPANCY CORRECTED. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007071900057 20070719 00057 WP 2007 7 19 070139 1 20070709 A 3510 4714037517 LINE DOUG DC9 DC987 3022087 WP OXYGEN SYS LEAKING A WX0A B EMER. DESCENT O OTHER CR CRUISE 1 WP 19 949MA 49779 APPROXIMATELY ONE HOUR INTO CRUISE FLIGHT COCKPIT OXYGEN BOTTLE STARTED LEAKING. DESCENDED TO FLIGHT LEVEL 250 AND SHUT OXYGEN VALVE PER MAINTENANCE CONTROL. LEAK CONTINUED UNTIL APPROXIMATELY 5000 FEET. ON CALL MAINTENANCE REMOVED AND R EPLACED THE OXYGEN DISCHARGE LINE IAW MM 35-10-01. NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007071900060 20070719 00060 NM 2007 7 19 07FDEA02496 1 20070716 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM NLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 NOSE LANDING GEAR LEFT TRUNNION FITTING FOUND CRACKED. [08-03-07] CARRIED OUT REPAIR AS PER SRM 53-40- 00 FIGURE 23 VOLUME I. REPETITIVE INSPECTION TO BE CARRIED OUT NOT EXCEEDING 1,500 LANDING INTERVALS. REPAIR CLASSIFIED AS MAJOR P ER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007071900061 20070719 00061 EU 2007 7 19 SIMA200719403 1 20070712 A 3350 6013200 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 324AE 604 168 340B324 TWO CONSECUTIVE EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AT 20LN IAW SAAB AMM 33-50-10. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007071900069 20070719 00069 NM 2007 7 19 UPS07550145 1 20070615 A 5412 311N3271 BULKHEAD BOEING 757 75724APF 1384969 NM NR 2 PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 420UP 23907 INSPECTION TYPE:C NR 2 PYLON AFT BULKHEAD LEFT LOWER OUTBOARD HAS A CHAFED. BULKHEAD MILL AND NDT WERE DONE ON TRAV T7/ 687615. FILLER WAS FABED REF TRAV T7/687616 PER PRELIMINARY 1 EA 757-5453-27-A1688. SHOT PEEN REWORKED AREA PER PER SO PM 20-10-03 AND PRELIMINARY 1 EA 757-5453-27 -A1688. 2 L 7 2 4F RT A2NM 2007071900077 20070719 00077 WP 2007 7 19 ARWA20070610 1 20070615 A 5730 ACCESS DOOR DOUG DC8 DC863F 302198F WP RT WING CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING "C" CHECK INSPECTIONS, THE FOLLOWING WAS FOUND; RT WING UPPER SURFACE MAIN FUEL TANK ACCESS DOOR NR 505E CUT OUT WITH CRACK. REPAIRED RT WING UPPER SURFACE MAIN FUEL TANK ACC DOOR NR 505E CUT OUT IN ACCORDANCE WITH DRAWING NR AIPSAC -N661AV-02/07 RD, SHEETS 1 TO 4, DATED 01-12-2007. LEAK CHECK IN ACCORDANCE WITH DC-8 M/M 28-00, NO LEAKS NOTED. 2 L 7 4 4F 4A25 2007071900095 20070719 00095 SO 2007 7 19 SIMA200719420 1 20070705 A 5347 14530658005 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 717AE 15889 5000 145272 RIGHT INBORAD SEAT TRACK CORRODED BETWEEN FRAMES 36 TO 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERA TIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900105 20070719 00105 SO 2007 7 19 SIMA200719708 1 20070705 A 5347 13500412001 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 717AE 15889 5000 145272 RIGHT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 53 TO 55. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900108 20070719 00108 SO 2007 7 19 SIMA200719707 1 20070705 A 5347 14530659007 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 717AE 15889 5000 145272 LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRA FT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900114 20070719 00114 NM 2007 7 19 UPS07M50144 1 20070416 A 5730 SKIN DOUG MD11 MD11F 3023600 NM RT WING DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C RIGHT WING UPPER SURFACE FIXED L/E STRUCTURE FOUND DEEP DENT AT STA XORS 593 AREA. RIGHT WING L/E COM PT RIBS 4EA REMOVED. RIGHT WING L/E DAMAGED SKIN TRIMMED PER EN12 63-07. HFEC INSP CUT OUT ON TRIMMED OFF AREA, FOUND NO CRACK. REPAIR SKIN & DOUBLER FAB PER EN1263-07. REPAIR SKIN HEAT TREATED, FASTENER HOLES PICKED UP & REWORKED, REPR OTECTED & PAINTED. REPAIR PARTS & SKIN INSTALLED. REWORK AREA PAINTED. 2 L 7 3 4F RT A22WE 2007071900131 20070719 00131 CE 2007 7 19 DXTA200702337 1 20070715 A 3260 LIGHT CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG INDICATOR INOPERATIVE E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 334QS 5600434 ON APP TO BTV ER PUT THE GEAR HANDLE DOWN AND ONLY GOT 2 GREEN AND NO RED. DISCONTINUED THE APP WENT OVER THE LAKE, RAN THE CHECKLIST. DID THE ROTARY TEST NO LIGHT. NO HORN BELOW 150 KTS FLAP PAST 15 DEG. DECLARED THE EMERGENCY, DID A FL YBY OF THE TOWER CAME BACK AND LANDED. [07-23-07] R & R LDG SAFE & UNLOCK LIGHTS P/N 327 IAW CE560 MM 32-60-00. OPS CHECK GOOD. OPS CHECKED THE LANDING GEAR IAW TASK 32-01-00-711 2 L 7 2 4F 4 F RT A22CE E25EA 2007071900132 20070719 00132 NM 2007 7 19 USAA070522 1 20070711 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 23379 FWD OF STA 727E & 3 INCHES AFT OF EXISTING REPAIR DOUBLER AT S-24L HAS CRACK. FABRICATED DOUBLERS & INSTALLED PER SRM 5 3-00-01, DEFECT SIZE: 1.25 INCH. 2 L 7 2 4F RT A16WE 2007071900135 20070719 00135 SO 2007 7 19 C2XA07RI054 1 20070708 A 3397 CONNECTOR EMB 145 EMB145EP 3260221 SO CABIN UNSECURE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 14937 145026 FLT 2534 - EWR - CREW REPORTED EMERGENCY LIGHT ON EXIT ROW INOP. MX MAINTENANCE RE-SECURED CONNECTOR BEHIND EMERGENCY L IGHT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900143 20070719 00143 SO 2007 7 19 RAIA00707012 1 20070707 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR DIRTY A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 843HK 14500822 POST FLT NR 8000 - IAD - PAX DOOR HARD TO OPEN. MAINTENANCE CLEANED AND LUBRICATED PAX DOOR ROLLER MECHANISM. 2 L 7 2 4T RT T00011AT 2007071900147 20070719 00147 CE 2007 7 19 DXTA200702321 1 20070705 A 3310 387 BULB RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP COCKPIT BURNED OUT E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 861QS 7568 258361 CLIMBING THROUGH ABOUT FL300 A BURNING ODOR WAS IN THE COCKPIT (PAX COULD NOT ODOR SMOKE IN CABIN). M2B- INSPECTED BEHI ND INSTRUMENT PANELS AND UNDER GLARESHIELD PANELS WITH NO FAULTS NOTED. RAN AIRCRAFT FOR .5 HRS WITH NO SMELL OF SMOKE. TALKED WITH TECH REPS AND WAS TOLD TO CHECK FOR BURNED OUT BULBS IN ANNUNCIATOR PANEL DUE TO HISTORY OF SMOKY ODOR WHEN BULBS BURN OUT. FOUND 4 INDIVIDUAL BULBS OUT IN THE UPPER AC POWER ANNUNCIATOR PANEL. REPLACED BULBS WITH NEW AND RAN A IRCRAFT FOR .5 HRS WITH NO SMELL OF SMOKE NOTED. WORK DONE IAW MM CHP 33-10-00. 2 L 7 2 4F 4 F RT A3EU E6WE 2007071900160 20070719 00160 EA 2007 7 19 COMA0760462 1 20070701 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A COMA K NONE J WARNING INDICATION CR CRUISE 1 SO 01 914CA 7012 FLIGHT 5589 - FLAP FAIL MESSAGE RECEIVED. DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. REPLACED RIGHT BPSU. 2 L 7 2 4F RT A21EA 2007071900164 20070719 00164 EA 2007 7 19 TRAX200700924 1 20070703 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 717EV 10088 LEFT LOWER FS 280 WEB HAS CORROSION. REMOVED LOWER LEFT FS 280 WEB, DUPLICATED ALODINED AND PRIMED IAW BOMBARDIER REO 6 70-53-11-052. DRILLED OUT FASTENERS IN UPPER WEB AND PEELED UP FOR ACCESS TO LOWER WEB. OK TO RE-INSTALL UPPER WEB. I NSTALLED ALL FASTENERS IN LEFT LOWER WEB EXCEPT O/B HI-LITES IAW REO 670-53-11-052. INSTALLED O/B HI-LITES IN LEFT WEB IAW CRJ SRM 51-42-21. TOP COATED IAW CRJ SRM 51-25-16. RE-INSTALLED UPPER WEB IAW CRJ REO 670-53-11-052. SUPPLEMENTAL - SDR CLOSED 07/12/07. 2 L 7 2 4F RT A21EA 2007071900176 20070719 00176 EA 2007 7 19 TRAX200700973 1 20070708 A 2740 TRIM SYSTEM CNDAIR CL600 CL6002B19 1900309 EA STABILIZER MALFUNCTIONED A ASOA K NONE J WARNING INDICATION CL CLIMB 1 SO 27 916EV 7757 STAB TRIM / MOC TRIM WOULD NOT ENGAGE. EMERGENCY DECLARED. RELATED TO DEFECT NR 362863A-1. 2 L 7 2 4F RT A21EA 2007071900177 20070719 00177 EA 2007 7 19 TRAX200700974 1 20070708 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOOR MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 848AS 7339 EXIT STICKER MISSING ON AIRSTAIR DOOR. FLT 4744 DEL 55 MINS. 2 L 7 2 4F RT A21EA 2007071900183 20070719 00183 NM 2007 7 19 SWAA073408 1 20070711 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 390, LBL 3.5. REPAIRED SKI N PER EA. 2 L 7 2 4F RT A16WE 2007071900185 20070719 00185 NM 2007 7 19 SWAA073388 1 20070710 A 5330 6545768208 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515D, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007071900188 20070719 00188 SO 2007 7 19 SIMA200719704 1 20070716 A 3397 7287503617 WIRE HARNESS EMB 135 EMB135LR 3260305 SO CABIN LIGHTS BURNED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 731BE 15037 145356 BURNING ODOR IN AFT CABIN. REMOVED AND REPLACED RIGHT AFT WALL LIGHT HARNESS ASSEMBLY IAW EMB AMM 33-21-05. OPERATIONA L CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900194 20070719 00194 NM 2007 7 19 SWAA073386 1 20070710 A 5753 6546435277 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED C3 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007071900198 20070719 00198 SO 2007 7 19 SIMA200719713 1 20070708 A 5347 13500439005 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 816AE 13301 5000 145552 LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 19 TO 23. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900201 20070719 00201 NM 2007 7 19 SWAA073422 1 20070711 A 5311 6546529 BELTFRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 500B, STR 20R. REPAIRED BELTFRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071900212 20070719 00212 SO 2007 7 19 SIMA200719803 1 20070716 A 3230 LANDING GEAR EMB 135 EMB135LR 3260305 SO INOPERATIVE A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 722AE 145287 LANDING GEAR WOULD NOT RETRACT, GEAR LEVER WOULD NOT MOVE. RETURNED TO LGA. 2 L 7 2 4F RT T00011AT 2007071900217 20070719 00217 NM 2007 7 19 SWAA073403 1 20070711 A 5320 907822 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR UPPER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007071900223 20070719 00223 SO 2007 7 19 SIMA200719702 1 20070713 A 2701 CONTROL COLUMN EMB 145 EMB145LR 3260212 SO COCKPIT STUCK A SIMA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SW 21 918AE 14500902 DURING TAXI CHECK, FLIGHT CONTROL JAMMED WHEN MOVING LEFT AILERON CONTROL COLUMN UN-JAMMED AFTER FEW MINUTES. RETURNED TO THE BLOCK. 2 L 7 2 4T RT T00011AT 2007071900233 20070719 00233 EA 2007 7 19 TRAX200700934 1 20070705 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 FS 473.15 FRAME IS CORRODED ON RT SIDE INBOARD JUST ABOVE FLOOR LEVEL. BLENDED CORROSION AT FS 473.15 IAW CRJ 200 SRM 5 3-00-00, FOUND TO BE IN LIMIT. ALODINED, PRIMED AND PAINTED. SUPPLEMENTAL - SDR CLOSED 07/13/07. 2 L 7 2 4F RT A21EA 2007071900236 20070719 00236 SO 2007 7 19 CHQA200700034 1 20070711 A 2621 337000271 EXTINGUISHER EMB 145 EMB145LR 3260212 SO CARGO BAY INOPERATIVE A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 298SK 13243 374 145508 FLIGHT 3052 - SAV-LGA - WHILE AT FL370, THE BAGGAGE FIRE EXTINGUISHER BUTTON LIT UP, NO EICAS OR AWU WARNING/MESSAGES DI SPLAYED. UPON PRESSING THE BAGGAGE FIRE EXTINGUISHER BUTTON, THE BAGG SMOKE EICAS MESSAGE APPEARED BRIEFLY THEN DISAPPE ARED 15-20 SECONDS LATER. FIRE BOTTLE INOP MESSAGE APPEARED, NO AWU WARNINGS AT ANY POINT. DECLARED AN EMERGENCY AND C OMPLIED WITH QRH. LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HIGH RATE BOTTLE AND METERING BOTTLE I AW MM 26-23-01. 2 L 7 2 4T RT T00011AT 2007071900238 20070719 00238 EA 2007 7 19 TRAX200700966 1 20070706 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 INTERCOSTAL AT FS 484.00 BETWEEN RBL 27 INBOARD CLIP IS CRACKED. FINISHED INSTALLING INBOARD CLIP AT FS 484 BETWEEN RBL 27 AND 36 IAW CRJ 200 SRM 51-42-21. SUPPLEMENTAL - SDR CLOSED 07/13/07. 2 L 7 2 4F RT A21EA 2007071900256 20070719 00256 WP 2007 7 19 UPS07850159 1 20070614 A 5720 FITTING DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 STRINGER END FITTING TO FRONT SPAR CRACKED BETWEEN XRS 463 TO XRS 450 NR 1 ALT TANK REMOVED STRIN GER END FITTING FROM FWD SPAR BETWEEN XRS 463 TO XRS 450 IAW SRM 51-01-20D, FABRICATED AND INSTALLED STRINGER END FITTIN G AT WING STA XRS 463 TO XRS 450 IAW DWG 3644046, AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 2007071900267 20070719 00267 EA 2007 7 19 TRAX200700979 1 20070709 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 832AS 7243 LEFT FUSELAGE 280 LBL 9 I/B CLIP CRACKED. 2 L 7 2 4F RT A21EA 2007071900268 20070719 00268 CE 2007 7 19 DXTA200702308 1 20070629 A 3243 991205017 MASTER CYLINDER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE BRAKES LEAKING E DXTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 335QS 1091 1091 5600335 DURING AIRCRAFT TAXI, CAPTAINS AND F/O RT BRAKE PEDAL LOSSES PRESSURE WHEN APPLYING BRAKES. WHEN LOSING PRESSURE F/O PE DAL WENT TO THE FLOOR CAPTAINS SIDE WENT DOWN 2-3 INCHES. T/S AND FOUND RT CO-PILOTS MASTER CYLINDER LEAKING INTERNALLY REMOVED AND REPLACED CO-PILOTS LT AND RT MASTER CYLINDER TO BLED AND LEAK CHECKS WERE GOOD IAW MM 32-42-02. 2 L 7 2 4F 4 F RT A22CE E25EA 2007071900269 20070719 00269 EA 2007 7 19 TRAX200700980 1 20070709 A 2560 MEGAPHONE CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 718EV 10095 F/A REPORTS MEGAPHONE IS DEAD. 2 L 7 2 4F RT A21EA 2007071900270 20070719 00270 EA 2007 7 19 TRAX200700981 1 20070709 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 930EV 8014 EMERGENCY LIGHTS WN COME ON. FLT 4914 DEL 16 MINS. 2 L 7 2 4F RT A21EA 2007071900271 20070719 00271 CE 2007 7 19 DXTA200702309 1 20070629 A 2760 LEVER CESSNA 680 680CE 2076811 CE SPEED BRAKE OUT OF ADJUST E DXTA O OTHER O OTHER CR CRUISE 1 GL 07 308QS 6800116 SPEED BRAKE LEVER DOES NOT STAY IN THE FULLY DEPLOYED DETENT, IT TENDS TO (SPRING) BACK TO A HALF DEPLOYED POSTION. ADJ USTED SPEED BRAKE LEVER DETENT. OPERATIONAL CHECK NORMAL IAW MM 76-10-00. 2 L 7 2 4F RC T00012WI 2007071900272 20070719 00272 NM 2007 7 19 DXTA200702311 1 20070630 A 2797 2415501 CIRCUIT BOARD AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE TE FLAPS INOPERATIVE E DXTA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 268QS 5301 168 IN FLIGHT AT FL 430, MASTER CAUTION LIGHT ILLUMINATED, ACCOMPANIED BY AUDIBLE GONG. (FLAP ASYSTEMMETRY) CAUTION LIGHT IL LUMINATED (5) SECONDS LATER FLAP CONTROL CIRCUIT BREAKER IN OVERHEAD C/B PANEL POPPED. LANDED NO FLAP. REPLACED PCB CAR D (50WW) WITH A NEW UNIT IN ACCORDANCE WITH F2000 MM 27-509 AND F2000 SPM 20-000. PERFORMED A SATISFACTORY TEST OF THE F LAP ASYMMETRY IAW F2000 MM 27-502. OPERATIONAL TEST OF FLAPS CONTROL AND INDICATING SYSTEM GOOD. 2 K 7 2 4F 4 F RT A50NM E44NE 2007071900273 20070719 00273 EA 2007 7 19 TRAX200700982 1 20070709 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 ON COCKPIT CHECK, EMERGENCY LIGHTS WOULD NOT INDICATE ON STATUS. 2 L 7 2 4F RT A21EA 2007071900274 20070719 00274 CE 2007 7 19 DXTA200702312 1 20070701 A 2150 73838433 ACM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL AFT SERVICE BAY LEAKING E DXTA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 913QS 2176 2176 7500113 EXTREME SULPHUR FUMES IN COCKPIT AND CABIN AT FL390, BOTH PACS IN NORM, BOTH TEMP SELECT IN AUTO, ENROUTE TIME 60 MINUTE S. FUMES DISIPATED DURING DESCENT. DECLARED AN EMERGENCY. NORMAL APPROACH AND LANDING. REMOVED AND REPLACED AFT ACM IAW MM 21-51-00. OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071900275 20070719 00275 CE 2007 7 19 DXTA200702307 1 20070629 A 2720 67604461 BUNGEE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL ZONE 300 INOPERATIVE E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 987QS 1101 7500087 LT RUDDER TRIM EXCESSIVE IN DIFFERENT PHASES OF FLIGHT. IN CLIMB OUT LT RUDDER TRIM INSIDE OF T ON TRIM INDICATOR, WITH AUTO PILOT ON AND DESCENDING THRU 20,500 AT 300 KTS, THE AIRPLANE SWERVED/SMALL JOLT AND IT IMMEDIATELY SHOWED MORE RUDD ER TRIM REQUIRED. THIS TOOK LT RUDDER TRIM OUTSIDE OF T ON INDICATOR. AS WE CLIMBED TO FL 410 AND INCREASED SPEED MORE LT RUDDER WAS NEEDED. AC LEVELED OFF AT FL430, SWITCHED FGC'S AND RUDDER CHANNELS WITH NO CHANGE OCCURRING TO TRIM. TRI M REMAINED OUTSIDE OF T ON INDICATOR DURING DESCENT. ACCOMPLISHED SUMMING LINK INSPECTION IAW MM CHAPTER 27-20-00. NO DEFECTS NOTED REMOVED AND REPLACED RUDDER COMMAND BUNGEE IAW MM CHAPTER 27-20-00. OPS RIG AND TRAVEL CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071900276 20070719 00276 EA 2007 7 19 TRAX200700983 1 20070710 A 5330 STRAP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 832AS 7243 LEFT SKIN BUTT JOINT STRAP AT FS 640 BETWEEN STR 10 AND STR 11 IS CRACKED; REQUIRES REO 601R 53-61-506. [07-26-07] R EPAIRED LT SKIN BUTT JOINT STRAP FS 640 BETWEEN STR 10 AND STR 11 IAW REO 601R 53-61-506. 2 L 7 2 4F RT A21EA 2007071900277 20070719 00277 CE 2007 7 19 DXTA200702310 1 20070629 A 3246 315381 WHEEL CESSNA 750 750 2076810 CE NLG OUT OF BALANCE E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 960QS 274 274 7500160 APPROXIMATELY 70 KNTS, HAD STRONG NOSE WHEEL VIBRATION AND YD OFF LOWER CAS MESSAGE. ABORTED TAKEOFF AND MESSAGE DISAPP EARED. ONLY DEFECT NOTED WAS LOWER TORQUE LINK HARDWARE WAS VERY LOOSE, ALLOWING SOME PLAY IN LOWER LINK. RETIGHTENED H ARDWARE IAW MM AND INSTALLED NEW TIRE ASSEMBLIES. ALL WORK PERFORMED IAW MM 52-41-01 AND 32-20-00. 2 L 7 2 4J RT T00007WI 2007071900278 20070719 00278 EA 2007 7 19 TRAX200700984 1 20070710 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA STAIRS CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 FOUND BOTTOM STEP BROKE DURING CAM LATCH RIGGING. 2 L 7 2 4F RT A21EA 2007071900279 20070719 00279 EA 2007 7 19 TRAX200700985 1 20070710 A 3350 COVER CNDAIR CL600 CL6002C10 1390015 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 709EV 10068 SERVICE DOOR EMERGENCY EXIT SIGN COVER MISSING. 2 L 7 2 4F RT A21EA 2007071900280 20070719 00280 EA 2007 7 19 TRAX200700986 1 20070710 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 929EV 8007 EMERGENCY LIGHTS -OFF- LIGHT HAS A LIGHT BULB INOP INSIDE COCKPIT. 2 L 7 2 4F RT A21EA 2007071900281 20070719 00281 EA 2007 7 19 TRAX200700987 1 20070710 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 AIRSTAIR DOOR VERY HARD TO OPEN. 2 L 7 2 4F RT A21EA 2007071900282 20070719 00282 NM 2007 7 19 2007UALA01715 1 20070526 A 2560 AC450012 SWITCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMEGENCY EXIT OUT OF ADJUST A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 LEFT FWD AUTO FIRE SWITCH THREADS TOUCHING ARMING LEVER FOR OVERWING SLIDE HATCH. ADJ SWITCHES PER MM 25-65-15. ARMING TO BE ACCOMP ON JIC E8320-60-10. FIRE SWITCH TOGGLE NUTS TIGHTENED SO THAT SWITCHES ARE CLEAR OF ARMING LEVER. AIRCRA FT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071900283 20070719 00283 2007 7 19 2007UALA02475 4 20070709 A 3440 DISPLAY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 FAULTED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 439UA 683 ADR 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. FOUND ADIRU MISALIGNED. CYCLED CB'S C2 AND F6. ALIGNED ADIRU'S AND FAULT LI TE EXTINGUISHED. PERFORMED BITE CK OF ADR1 AND NO FAULTS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071900292 20070719 00292 GL 2007 7 19 CHQA200700037 2 20070716 A 7200 AE3007A13 ENGINE EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL NR 1 ODOR A CHQA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 841RP 14523 1309 145737 CAE311866 FLIGHT 6242 - MSY-CVG - CLIMBING THROUGH FL310, A FAINT HAZE AND ODOR OF SMOKE ENTERED COCKPIT FOLLOWED BY LAV SMOKE EIC AS WARNING. PERFORMED QRH. VERIFIED FA ALSO SMELLED SMOKE AND RECEIVED LAV SMOKE ALARM IN GALLEY. DECLARED AN EMERGE NCY. SMOKE BEGAN TO DISSIPATE DURING DESCENT. LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS MAINTENANCE FERRIED TO SDF WH ERE THE NR 1 ENGINE WAS REPLACED. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007071900293 20070719 00293 EA 2007 7 19 SWIA200718468 1 20070715 A 3230 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 408SW 7055 FLT 3897 - GEAR DISAGREE WARNING WITH NOSE GEAR UP INDICATION ON FINAL. WHEN 3B WAS SELECTED, NOSE GEAR DOWN INDICATION GIVEN. REPLACED PRIORITY VALVE AND CYCLED GEAR UP AND DOWN SEVERAL TIMES. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2007071900311 20070719 00311 EA 2007 7 19 SWIA200718469 1 20070715 A 3020 5399001 VALVE CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE DISCONNECTED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 454SW 9923 9923 7749 FLT 3845 - RIGHT COWL ANTI-ICE CAUTION MESSAGE CAME ON DURING CLIMB-OUT. RETURNED TO FIELD. FOUND BLEED SOURCE LINE ON THRUST REVERSER PDU DISCONNECTED. RECONNECTED LINE IAW MM 78-32-03. REPLACED RIGHT LOWER COWLING, COWL ANTI-ICE PRESSU RE SWITCH, AND COWL ANTI-ICE VALVE IAW MM 30-22-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007071900312 20070719 00312 EA 2007 7 19 SWIA200718470 1 20070714 A 3310 SWITCH CNDAIR CL600 CL6002C10 1390015 EA COCKPIT LIGHT SHORTED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 774SK 10240 CAPTAIN'S DOME LIGHT SWITCH IS HARD TO OPERATE AND APPEARS TO BE SHORTING. REPLACED CAPTAIN'S DOME LIGHT SWITCH AS REQU IRED BY AMM 33-13-09. 2 L 7 2 4F RT A21EA 2007071900313 20070719 00313 EA 2007 7 19 SWIA200718456 1 20070708 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 740SK 10196 EMERGENCY EXIT LIGHT NEAR SERVICE DOOR IS BROKE OFF. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY WITH A SERVICABLE UNIT. O PS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007071900316 20070719 00316 SO 2007 7 19 SWIA200718459 1 20070618 A 5210 DOOR FRAME EMB 120 EMB120ER 3260203 SO CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 PAX DOOR FORWARD SIDE OF INTERNAL FRAME IS CRACKED, DISCOVERED AT C-CHECK. REPAIRED PAX DOOR INTERNAL FRAME IAW SRM 52- 10-02 FIG 203 PG 208. 2 L 7 2 4T RT A31SO 2007071900317 20070719 00317 SO 2007 7 19 SWIA200718460 1 20070618 A 5210 TORQUE TUBE EMB 120 EMB120ER 3260203 SO MAIN PAX CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 PAX DOOR INTERCONNECT TORQUE TUBE INBOARD BEARING BOSS IS CORRODED, DISCOVERED AT C-CHECK. REPLACED PAX DOOR INTERCONNE CT TORQUE TUBE BEARING BOSS IAW EMB 120 MM 52-11-00. 2 L 7 2 4T RT A31SO 2007071900318 20070719 00318 SO 2007 7 19 SWIA200718461 1 20070618 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 RIGHT SIDEWALL FORWARD SEAT TRACK IS CORRODED, DISCOVERED AT C-CHECK. SPLICED IN A NEW SECTION OF TRACK IAW EMB SERVICE LETTER EST-186/96 AND MM 20-10-03. 2 L 7 2 4T RT A31SO 2007071900323 20070719 00323 SO 2007 7 19 SWIA200718466 1 20070618 A 5311 FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 FUSELAGE FRAME IS CRACKED FORWARD OF INSTRUMENT PANEL BELOW CAPTAINS WINDSCREEN, DISCOVERED AT C-CHECK. REPLACED FUSELA GE FRAME BELOW CAPTAINS WINDSCREEN IAW SRM 120 51-10-02 PG 3 SEC 3A. 2 L 7 2 4T RT A31SO 2007071900326 20070719 00326 EA 2007 7 19 SWIA200718471 1 20070701 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA BS 202 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 903SW 7425 FOUND POSSIBLE CRACK ON UPPER NOSE AREA AT FS 202.75.DAMAGE FOUND TO BE A MAJOR REPAIR. REPAIRED FUSELAGE SKIN IN ACCOR DANCE WITH CRJ REO 601R-53-11-1212. 2 L 7 2 4F RT A21EA 2007071900327 20070719 00327 EA 2007 7 19 SWIA200718472 1 20070701 A 5510 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 903SW 7425 RIGHT HORIZONTAL STABILIZER HAS A DENT ON THE LEADING EDGE AT SECTION 10.91. DAMAGE FOUND TO BE A MAJOR REPAIR. C/W RE O 601R-55-12-348. OK FOR SERVICE. 2 L 7 2 4F RT A21EA 2007071900329 20070719 00329 EA 2007 7 19 SWIA200718474 1 20070701 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA BS 169-210 DENTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 903SW 7425 UPPER FORWARD FUSELAGE BETWEEN FS 169.00 AND FS 210.00 HAS SEVERAL DENTS. DAMAGE FOUND TO BE A MAJOR REPAIR. REPLACED FUSELAGE SKIN BETWEEN FS 169.00 AND FS 193 IAW CRJ SRM 51-42-06 AND REO 601R-53-11-1207. 2 L 7 2 4F RT A21EA 2007071900330 20070719 00330 SO 2007 7 19 SWIA200718475 1 20070712 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO EMERGENCY EXIT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 566SW 120341 EMERGENCY EXIT LIGHT AT ROW 6 IS BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007071900333 20070719 00333 SO 2007 7 19 SWIA200718476 1 20070706 A 2530 COFFEEMAKER EMB 120 EMB120ER 3260203 SO GALLEY OVERHEATED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 308SW 120326 F/A REPORTS COFFEE POT OVERHEATED WITH A BURNING ODOR. REPLACED COFFEE POT WITH SERVICEABLE UNIT. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007071900337 20070719 00337 EA 2007 7 19 SWIA200718477 1 20070712 A 3350 BATTERY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 923SW 7664 FLT 6108 - MULTIPLE EMERGENCY EXIT LIGHTS ARE INOP. REPLACED TB105-1 AND NR 2 BATT AND CHARGER ASSEMBLY. OPS CHECK GOO D, P/N 1-2013-1A, S/N ON - 57038, S/N OFF - 68998, P/N 2 - N549-3156. 2 L 7 2 4F RT A21EA 2007071900340 20070719 00340 SO 2007 7 19 SWIA200718478 1 20070709 A 5210 STOP FITTING EMB 120 EMB120ER 3260203 SO PAX DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 271YV 120271 FLT 5477 - MAIN CABIN DOOR WILL NOT OPEN. REPLACED TOP AFT STOP BOLT. 2 L 7 2 4T RT A31SO 2007071900357 20070719 00357 EU 2007 7 19 TRBA2007046 1 20070711 A 3350 3013000 POWER SUPPLY AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHT INOPERATIVE A TRBA O OTHER O OTHER NR NOT REPORTED 1 SO 29 533AT 533 FWD EXIT EMERGENCY LIGHT INOPERATIVE WITH BATTERY OFF. REMOVED AND REPLACED POWER SUPPLY 63WL IAW JIC #33-51-71. OP CK OK. 2 H 7 2 4T RT A53EU 2007071900358 20070719 00358 EU 2007 7 19 TRBA2007051 1 20070715 A 3350 WIRE AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT BROKEN A TRBA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 29 447AM 447 EXIT SIGN OVER THE AFT F/A SEAT DOES NOT COME ON WHEN EMERGENCY LIGHT SWITCH IS TURN INTO THE ON POSITION. MAINTENANCE REPAIRED WIRE AS PER ATR-72-AMM-20-27-17 AT EXIT SIGN LOCATED BY AFT F/A SEAT. PERFORMED OPERATIONAL CHECK AS PER ATR-7 2-JIC-33-50-00. 2 H 7 2 4T RT A53EU 2007071900359 20070719 00359 WP 2007 7 19 ASAA0781868 1 20070710 A 5313 S27779223 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE C F.O.D. IN INSP/MAINT 1 NM 02 969AS 53063 FUSELAGE DENTED. REPAIR FUSELAGE SKIN AND LONGERON PER SRM 53-02. 2 L 7 2 4F RT A6WE 2007071900362 20070719 00362 EU 2007 7 19 TRBA2007048 1 20070713 A 2120 UNKNOWN AEROSP ATR72 ATR72212 8680945 EU CABIN ODOR A TRBA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 29 407AT 407 BOTH F/A REPORTED SMELLING ELECTRIC BURN AT PAX SEAT 15B WHILE SERVICING. NO ODOR AFTER READING AND LATERAL LIGHTS WERE TURNED OFF. WITH DC AND AC POWER ON PERFORMED AN INSPECTION LOOKING FOR BURNING ODOR, BUT FOUND NORMAL AS PER JIC #33- 20-00. 2 H 7 2 4T RT A53EU 2007071900363 20070719 00363 EU 2007 7 19 TRBA2007053 1 20070713 A 3350 7012210 LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT INOPERATIVE A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 322AC 320 F/A REPORTED EMERGENCY EXIT FORWARD TOP LIGHT INOPERATIVE WHEN ACTIVATED THE SYSTEM AND BATTERY POWER WAS OFF. MAINTENA NCE RE-LAMPED LIGHT AND PERFORMED OPERATIONAL CHECK AS PER ATR 72- AMM-33-50-00. 2 H 7 2 4T RT A53EU 2007071900364 20070719 00364 EA 2007 7 19 SWIA200718481 1 20070522 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 928SW 7701 ENGINE SUPPORT BEAM LOWER WEB IS CRACKED AT FORWARD INBOARD CORNER OF RIGHT ACCESS OPENING, DISCOVERED AT C-CHECK. INST ALLED REPAIR PARTS PER CRJ REO 601R 53-61-258 REV A. 2 L 7 2 4F RT A21EA 2007071900365 20070719 00365 EA 2007 7 19 SWIA200718482 1 20070522 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 928SW 7701 ENGINE SUPPORT BEAM LOWER WEB IS CRACKED AT FORWARD, INBOARD CORNER OF LEFT ACCESS OPENING, DISCOVERED AT C-CHECK. INST ALLED REPAIR DOUBLER, WEB FILLER, SHIMS, STRAP AND ANGLE PER CRJ200 REO 601R 53-61-358. 2 L 7 2 4F RT A21EA 2007071900366 20070719 00366 EA 2007 7 19 SWIA200718483 1 20070522 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BRAKE TRANDUCER CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 928SW 7701 BRAKE TRANSDUCER BRACKET IN LEFT WHEEL WELL IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED NEW LEFT TRANSDUCER BRACKET PE R CRJ200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007071900367 20070719 00367 EA 2007 7 19 SWIA200718484 1 20070522 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 928SW 7701 RIGHT WING ANTI-ICE BRACKETS ARE CRACKED UNDER PANEL 620AT, DISCOVERED AT C-CHECK. REPLACED RIGHT WING ANTI-ICE BRACKET S UNDER PANEL 620AT PER CRJ200 AMM 30-11-41-000-801. 2 L 7 2 4F RT A21EA 2007071900368 20070719 00368 EA 2007 7 19 SWIA200718485 1 20070522 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 928SW 7701 FOUND THE ENGINE SUPPORT BEAM UPPER ANGLE TO BE CRACKED, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLE PER CRJ200 SRM 5 1-42-21 PG 17. 2 L 7 2 4F RT A21EA 2007071900372 20070719 00372 EU 2007 7 19 F3LA200700175 1 20070712 A 5320 PANEL AIRBUS A318 A318111 3940019 EU FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 807FR 5281 2276 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT TRANSITION PANELS 151FH, 151HH, AND 162SF DAMAGED. REPAIRED PUNCTURES IN PANELS IAW A318 SRM 53-20-00, PB 201, PARA 8C, FIG 204. 2 L 7 2 4F RT 2007071900373 20070719 00373 EU 2007 7 19 F3LA200700176 1 20070712 A 5321 FLOOR PANEL AIRBUS A318 A318111 3940019 EU FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 807FR 5281 2276 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR PANEL 161QF DAMAGED. REPAIRED FLOOR PANEL 161QF IAW A 318 SRM 53-02-00, FIG 204. 2 L 7 2 4F RT 2007071900374 20070719 00374 NM 2007 7 19 F3LA200700171 1 20070707 A 5320 PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 933FR 5232 2260 DURING C-2 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT TRANSITION PANEL 131CF DAMAGED. REPAIRED ONE SKIN PENETRATI ON IAW SRM 53-02-00, PAGE 204, 205, PARA 2-E, FIG. 201, AND AMM 25-00-00-370-001. 2 L 7 2 4F RT A28NM 2007071900375 20070719 00375 EU 2007 7 19 F3LA200700174 1 20070712 A 5320 PANEL AIRBUS A318 A318111 3940019 EU FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 807FR 5281 2276 DURING C-2 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT TRANSITION PANEL 131BF DAMAGED. REPAIRED PUNCTURE IAW A318 SRM 53-20-00, PB 201, PARA 8.C., FIG. 204. 2 L 7 2 4F RT 2007071900377 20070719 00377 NM 2007 7 19 ASAA0771866 1 20070709 A 3520 E7174000 OXYGEN GEN BOEING 737 737790 13844CN NM CABIN ACTIVATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 FOUND 1 EACH OXYGEN GENERATOR SPENT VIA BAND BLACK AT ROW 13DEF DURING WORKCARD INSPECTION OF OXYGEN GENERATORS TC 78035 00. REMOVED SPENT GENERATOR. NEW O2 GENERATOR FAILED INSTALLATION BY INADVERTENT ACTIVATION OF PIN. 2 L 7 2 4F RT A16WE 2007071900379 20070719 00379 NM 2007 7 19 SWAA073515 1 20070716 A 3210 6544825 ACTUATOR BOEING 737 7373A4 1384585 NM RT MLG WEAK A SWAA O OTHER J WARNING INDICATION CL CLIMB 1 SW 29 680AA 23505 RT MLG UNSAFE LIGHT IND CYCLED GEAR HANDLE AND LIGHT IND WENT AWAY. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2007071900381 20070719 00381 NM 2007 7 19 SWAA073519 1 20070716 A 5322 6552880 SHEAR TIE BOEING 737 7373K2 13844BA NM BS 357 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 357, RBL 1 TO RBL 4. REPAIRED SHEAR TIE PER SWA EA. 2 L 7 2 4F RT A16WE 2007071900382 20070719 00382 2007 7 19 SWAA073518 4 20070716 A 2565 6557463 LATCH BOEING 737 7377H4 1384404 NM L1 DOOR SLIDE INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 479WN 33990 DURING SCHEDULE MV2 CHECK, FOUND L1 DOOR EVAC SLIDE LATCH INOP. REMOVED AND REPLACED EVAC SLIDE LATCH PER MM. 2 L 7 2 4F RT A16WE 2007071900385 20070719 00385 NM 2007 7 19 KCSA071223 1 20070715 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 710-760 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA 760 TO 710 AT LBL 99 SEAT TRACK UPPER I/B FLANGE HAS CORROSION. 2 L 7 4 4F RT A20WE 2007071900388 20070719 00388 NM 2007 7 19 KCSA071226 1 20070715 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 460 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA 460 LBL 64 LOWER SIDE OF SEAT TRACK HAS CORROSION. 2 L 7 4 4F RT A20WE 2007071900390 20070719 00390 NM 2007 7 19 KCSA071228 1 20070715 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1010 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA 1010 RBL 99 SEAT TRACK DAMAGED. 2 L 7 4 4F RT A20WE 2007071900393 20070719 00393 NM 2007 7 19 KCSA071214 1 20070715 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1900 BROKEN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 MAIN DECK SEAT TRACK FLANGE BROKEN AT BS 1900, LBL 99. 2 L 7 4 4F RT A20WE 2007071900397 20070719 00397 NM 2007 7 19 KCSA071217 1 20070715 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1660-1670 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 CORROSION ON MAIN DECK SEAT TRACK I/B AND O/B RADIUS FROM BS 1660 TO 1670, LBL 98, WL 199. 2 L 7 4 4F RT A20WE 2007071900398 20070719 00398 NM 2007 7 19 KCSA071218 1 20070715 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1650-1760 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 CORROSION ON MAIN DECK SEAT TRACK I/B AND O/B RADIUS FROM BS 1650 TO 1760, RBL 98, WL 199. 2 L 7 4 4F RT A20WE 2007071900399 20070719 00399 NM 2007 7 19 KCSA071219 1 20070715 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1655-1735 GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 MAIN DECK SEAT TRACK GOUGED AT BS 1655, 1705 AND 1735, LBL 35. 2 L 7 4 4F RT A20WE 2007071900400 20070719 00400 NM 2007 7 19 KCSA071220 1 20070715 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1780-1830 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 CORROSION ON MAIN DECK SEAT TRACK I/B RADIUS FROM BS 1780 TO 1830, LBL 12, WL 199. 2 L 7 4 4F RT A20WE 2007071900401 20070719 00401 NM 2007 7 19 KCSA071221 1 20070715 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 2000-2020 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 CORROSION ON MAIN DECK SEAT TRACK I/B RADIUS FROM BS 2000 TO 2020, LBL 12, WL 199. 2 L 7 4 4F RT A20WE 2007071900403 20070719 00403 WP 2007 7 19 ASAA0781870 1 20070713 A 5320 9936534177 MEMBRANE DOUG DC9 DC983 3022083 WP CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 FORWARD WET AREA MEMBRANE IS CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER PER SRM 53-01. 2 L 7 2 4F RT A6WE 2007071900404 20070719 00404 WP 2007 7 19 ASAA0781871 1 20070713 A 5320 9936534177 MEMBRANE DOUG DC9 DC983 3022083 WP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 FORWARD WEB AREA MEMBRANE IS CORRODED ON UPPER SURFACE. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER PER SRM 53-0 1. 2 L 7 2 4F RT A6WE 2007071900405 20070719 00405 WP 2007 7 19 ASAA0781872 1 20070713 A 5321 99365445 FLOOR PANEL DOUG DC9 DC983 3022083 WP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05 DAC DWG 9936585 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007071900406 20070719 00406 2007 7 19 HNAA0700145 4 20070705 A 2216 7003032612 SERVO DHAV DHC8 DHC8102 2809003 NM ELEVATOR MALFUNCTIONED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 911HA 034 AFTER TAKEOFF THE ELEVATOR WAS SLOW TO MOVE. PITCH WAS VERY SLOW AS WELL. THE CREW DECLARED AN EMERGENCY AND RETURNED TO LGA. THE FLIGHT LANDED AND TAXIED WITHOUT INCIDENT. REMOVED AND REPLACED ELEVATOR SERVO, EVALUATION FLIGHT CHECK S ATISFACTORY. 2 H 7 2 4T RT A13NM 2007071900407 20070719 00407 WP 2007 7 19 ASAA0781869 1 20070713 A 5320 9936534177 MEMBRANE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 FORWARD WET AREA MEMBRANE IS CORRODED ON UPPER SURFACE. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER P ER SRM 53-01. 2 L 7 2 4F RT A6WE 2007071900409 20070719 00409 NM 2007 7 19 SWAA073424 1 20070712 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 726SW 27858 DURING SCHEDULED MV3 CHECK, FOUND AFT LEFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007071900410 20070719 00410 NM 2007 7 19 SWAA073447 1 20070712 A 3397 8100022702 CONNECTOR BOEING 737 73776Q 13845AA NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 550WN 30279 DURING SCHEDULED MV3 CHECK, FOUND EEPLS INOP BETWEEN ROW 4 ABC AND ROW 7 ABC. FOUND LOOSE CONNECTOR, RECONNECTED PER MM . 2 L 7 2 4F RT A16WE 2007071900411 20070719 00411 NM 2007 7 19 SWAA073445 1 20070712 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, FOUND STRINGER 27R CORRODED AT BS 540. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007071900412 20070719 00412 NM 2007 7 19 SWAA073446 1 20070712 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 435WN 32455 DURING SCHEDULED HC1 CHECK, FWD CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007071900413 20070719 00413 NM 2007 7 19 USAA220707001 1 20070711 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 501UW 23231 A 2.5 INCH CRACK FOUND AT STA 867 + 4 STRINGER 24R. INSTALLED EXT FUSELAGE SKIN REPAIR PER SRM 53-0-01, REPAIR 31. 2 L 7 2 4F RT A16WE 2007071900414 20070719 00414 NM 2007 7 19 USAA200707002 1 20070710 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 591US 23936 A 1.7 INCH CRACK AT STA 500D + 5 STRINGER 15L. INSTALLED EXT FUSELAGE SKIN REPAIR PER EA 98787. 2 L 7 2 4F RT A16WE 2007072000002 20070720 00002 NM 2007 7 20 CALA0700360 1 20070714 A 2560 61020 BATTERY BOEING 767 767424ER 1385270 NM R-4 FLASHLIGHT INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59053 29448 THE R-4 DOOR FWD EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. THE FLASHLIGHT BATTERY WAS REPLACED. 2 L 7 2 4F RT A1NM 2007072000003 20070720 00003 SO 2007 7 20 C2XA07IA166 1 20070711 A 3397 WIRE EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHTS DAMAGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15926 145005 IAH - DURING A-CHECK INSPECTION THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED A DEFECTIVE WIRE SPLICE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. 2 L 7 2 4F RT T00011AT 2007072000004 20070720 00004 SO 2007 7 20 C2XA07TY037 1 20070714 A 5313 14521687008 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11535 145518 DENT ON FUSELAGE AT FRAME 15 AND STRINGER 20L. CUT OUT DAMAGED SECTION OF STRINGER, DRILLED AND INSTALLED REPAIR IAW EM B SRM 53-00-03 AND 51-40-02. AIRCRAFT STILL IN C-CHECK. 2 L 7 2 4T RT T00011AT 2007072000005 20070720 00005 NM 2007 7 20 HNAA0700147 1 20070706 A 2913 6305405 PUMP DHAV DHC8 DHC8102 2809003 NM HYDRAULIC SYS BROKEN A HNAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 07 930HA 126 IN FLT NR 1 HYD ISO VALVE, ROLL SPOILER INBOARD DYD, NR 1 RUD HYD CAUTION LIGHT ILLUMINATED FOLLOW BY LOSS OF NR 1 HYD Q TY. REMOVED AND REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP. NO CONTAMINATION IN CASE DRAIN FILTER, OPS & LEAK CHECK GO OD. 2 H 7 2 4T RT A13NM 2007072000008 20070720 00008 EA 2007 7 20 VNAA0706017 1 20070630 A 2150 504225 SLEEVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT A/C PACK WORN A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 05 259PS 7945 CREW REPORTED A CARGO BOTTLE LOW CAUTION MESSAGE IN CRUISE. CREW FOLLOWED THE QRH AND DIVERTED TO ATL. CREW LANDED WIT HOUT INCIDENT IN ATL. MAINTENANCE INSPECTED AND DEFERRED THE CARGO COMPARTMENT FIRE EXTINGUISHING SYSTEM PER MEL 26-25- 01 CODE C. MAINTENANCE LEAK TESTED THE PACK SYSTEM AND FOUND THE LEFT HAND PACK TO BE LEAKING FROM THE DISCHARGE CLAMP. MAINTENANCE REMOVED AND REPLACED THE SLEEVE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 21-51-15-400-801. OPER ATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007072000012 20070720 00012 WP 2007 7 20 ABXR070239 1 20070616 A 5740 5919289521N ATTACH FITTING DOUG DC9 DC932 3022066 WP LEFT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 697BJ 47799 FORWARD AND AFT SURFACE OF FIXED BRACE LUG ON LEFT TRUNNION WAS CORRODED. REPLACED TRUNNION ON JOB CARD 0317 AND EA 574 30025. 2 L 7 2 4F A6WE 2007072000014 20070720 00014 NM 2007 7 20 SWAA073454 1 20070713 A 3350 417A5701 COVER BOEING 737 737705 13844SC NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 270WN 29089 EEPLS COVER LOOSE AT ROW 21 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007071800118 20070718 00118 NM 2007 7 18 AALA20071203 1 20070628 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 949AN 29537 MIA - EMERGENCY LIGHT AT SEAT 16D INOPERATIVE. RELAMPED EMERGENCY LIGHT SAT SEAT ROW 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007071800128 20070718 00128 NM 2007 7 18 QXEA200701153 1 20070714 A 2910 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM HYD IND C/B UNKNOWN A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 418QX 4143 EUG - ON FLIGHT 2421, RETURNED TO GATE, STANDBY HYDRAULIC INOP. FOUND STANDBY HYDRAULIC PRESSURE INDICATOR 1 CIRCUIT BR EAKER POPPED. MAINTENANCE RESET CIRCUIT BREAKER, PERFORMED OPERATIONAL TEST OF POWER UNIT. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007071800130 20070718 00130 WP 2007 7 18 ASAA0781853 1 20070704 A 5322 995823885 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 AFT CARGO SHEAR TIE CORRODED AT BS 1322 BETWEEN LONG 29R AND LONG 29L. REMOVED DAMAGED SECTION OF SHEAR TIE, FABRICATED , LOCATED, DRILLED AND INSTALLED SHEAR TIE AND REPAIR SPLICES IAW SRM 53-03 PG 4M FIG 3 SRM 51-60-0 PG 5 FIG 1 SHEET 1. 2 L 7 2 4F RT A6WE 2007071800133 20070718 00133 NM 2007 7 18 SWAA073349 1 20070706 A 3350 101114 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 247WN 32508 MID CABIN OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007071800136 20070718 00136 NM 2007 7 18 SWAA073356 1 20070706 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SKIN CORRODED AT RADIO ALTIMETER ANTENNA CUTOUT BS 439, STR 28R. REPAIRED SK IN PER ACO. 2 L 7 2 4F RT A16WE 2007071800137 20070718 00137 NM 2007 7 18 QXEA200701148 1 20070712 A 7921 800600M02 ACTUATOR BOMBDR DHC8 DHC8402 1390042 NM OIL COOLER INOPERATIVE A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 405QX 15214 15214 4047 SEA - ON FLIGHT 2328, NR 1 OIL TEMP 105 DEGREES ON CLIMB-OUT, C/W CHECKLIST. TEMP STARTED TO COOL, IT STABILIZED AT 85 DEGREES. MAINTENANCE FOUND NR 1 ENGINE OIL COOLER AIR OUTLET FLAP ACTUATOR TO BE STICKING. REPLACED ACTUATOR. AIRCRAF T RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071800139 20070718 00139 NM 2007 7 18 SWAA073352 1 20070706 A 5753 6546430122 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED MV1 CHECK, FOUND RIGHT WING INBOARD FORE FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FORE F LAP PER MM. 2 L 7 2 4F RT A16WE 2007071800146 20070718 00146 EA 2007 7 18 QXEA200701118 1 20070617 A 5300 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 C3 OKC - FS 280 AT RBL 9 AFT SIDE HAS CORROSION. REPAIRED IAW SRM 51-42-06, 51-42-21. 2 L 7 2 4F RT A21EA 2007071800157 20070718 00157 NM 2007 7 18 KCSA071205 1 20070710 A 5320 STIFFENER BOEING 747 7472B4B 138481B NM NLG WW CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NOSE WHEEL WELL TOP PANEL STIFFENER CRACKED AT BS 310, LBL 11. 2 L 7 4 4F RT A20WE 2007071800162 20070718 00162 NM 2007 7 18 KCSA071208 1 20070710 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 MAIN DECK SEAT TRACK CORRODED AT BS 200, RBL 48. 2 L 7 4 4F RT A20WE 2007071800163 20070718 00163 NM 2007 7 18 QXEA200701124 1 20070711 A 6100 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM PROP ASSY UNKNOWN A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 426QX 562 562 DAP0346 4154 PDX FLIGHT NR 2466: DURING CLIMB, NR 2 PROP DROPPED TO 890 WHILE NR 1 REMAINED AT 900. PILOT TAPPED NR 2 CONDITION LEVE R IN DETENT AND RPM RETURNED TO 900. ONE MINUTE LATER, NR 2 RPM JUMPED TO 910 RPM AND POWER PLANT MESSAGE APPEARED ON E D. MESSAGE REMAINED ON DURING THE REST OF THE FLIGHT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED NR 2 PROPELLER IAW MTC 6610003 AND MTC 6610004. OPS CHECKS GOOD. NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071800172 20070718 00172 EA 2007 7 18 QXEA200701103 1 20070612 A 5753 PANEL CNDAIR CL600 CL6002C10 1390015 EA RT TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 C3 OKC - RIGHT FLAP LEADING EDGE PANEL 684LB CHAFED AT CUTOUT. REPAIRED IAW SRM51-12-00, 57-52-01, 51-25-06. 2 L 7 2 4F RT A21EA 2007071800173 20070718 00173 NM 2007 7 18 ZZDA070605194 1 20070605 A 5313 LONGERON BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT LONG 26 LT BETWEEN BS 813 AND BS 1053. INSTALLED NEW LONGERON 26L AND SPLCE FROM STA 813 TO 1053 AND NEW FINGER DOUBLER AS PER B717 SRM 51-41-02 AND 51-41-05. 2 L 7 2 4F TR A6WE 2007071800181 20070718 00181 WP 2007 7 18 AALA20071200 1 20070628 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISLODGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 441AA 49460 LGA - EMERGENCY LIGHTS AT OVERHEAD TAIL CATWALK INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY LIGHTS A OVERHEAD TAIL CATWALK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071800184 20070718 00184 WP 2007 7 18 AALA20071204 1 20070628 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 458AA 49563 SFO - EMERGENCY LIGHTS AT SEAT ROWS 17 TO 21 INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 20 FOR EMERGENCY LIGHTS AT SEAT ROWS 17 TO 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071800185 20070718 00185 EU 2007 7 18 AALA20071205 1 20070628 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 MIA - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007071800198 20070718 00198 NM 2007 7 18 ZZDA070611199 1 20070611 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 AFT CARGO COMPARTMENT FUSELAGE SKIN INNER SURFACE IS CORRODED FROM STA 1002 TO 1053 BETWEEN L-26L TO 21L. INSTALLED SKI N AND DOUBLER AT AFT CARGO COMPARTMENT FROM STA 895.5 TO STA 1053, LONGERON 21L TO LONGERON 26L AS PER B717 SRM 51-41-02 AND SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007071800242 20070718 00242 CE 2007 7 18 GUUA07090701 1 20070709 A 3230 571302 POWERPACK BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG DEFECTIVE A GUUA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 231YV UE231 FLIGHT: 9174, AFTER TAKEOFF, LANDING GEAR WILL NOT RETRACT. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. REPLACED L ANDING GEAR POWER PACK MOTOR. LANDING GEAR OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007071800256 20070718 00256 WP 2007 7 18 ASAA0781863 1 20070708 A 5320 993061287 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 RIGHT CUSP WEB CORRODED. REMOVED DAMAGED SECTION OF WEB, LOCATED, DRILLED AND INSTALLED A REPLACEMENT CUSP WEB IAW SRM 51-30-2, 51-10-4 AND 51-30-5. 2 L 7 2 4F RT A6WE 2007071800271 20070718 00271 CE 2007 7 18 DXTA200702305 1 20070628 A 2720 H517A POSITION SENSOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RUDDER OUT OF ADJUST E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 921QS 534 7500241 RUDDER OSCILLATED IN CRUISE FLIGHT (FL270 - 340KTS IAS) FOR APPROX 10 SECS FOLLOWED BY BLUE YD FAIL - B MSG FOLLOWED APP ROX 20 SECS LATER BY YELLOW (YD FAIL - AB) MSG OSCILLATIONS. UPPER RUDDER POSITION SENSORS FOUND TO BE OUT OF ADJUSTMEN T, AND RUDDER PEDAL (A) SENSOR TO BE NON ADJUSTABLE TO BRING INTO +.5 INCH TOLERANCE. ADJUSTED UPPER RUDDER A+B SENSORS , AND REPLACED (A) RUDDER PEDAL POSITION SENSOR AND ADJUSTED IAW 27-24-01 OF MM. OPS CHECK GOOD. OLD P/N: H517A. OLD S/ N: H7594. NEW P/N: H517A. NEW S/N: K4546. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071800283 20070718 00283 NM 2007 7 18 UIEA200700261 1 20070710 A 2750 5700824 BALL SCREW BOEING 747 74747UF 1384812 NM FLAP DRIVE WORN A UIEA O OTHER O OTHER DE DESCENT 1 EA 15 499MC 29260 FLAP DRIVE MESSAGE. OUTBOARDS AT 30 INBOARDS 25. LE ALL GREEN. RT INBOARD FLAPS INDICATES EXTENDED MORE THAN LEFT INB OARDS. FOUND NR 4, 5 AND 6 JACKSCREWS/BALLSCREWS HAD PLAY AND WERE WORN REMOVED AND REPLACED ALL 3 UNITS OPS CHECKED OK AY. 2 L 7 4 4F RT A20WE 2007071800290 20070718 00290 WP 2007 7 18 AALA20071224 1 20070701 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14551 53033 DFW - EMERGENCY LIGHT AT SEAT 12D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071800298 20070718 00298 NM 2007 7 18 2007UALA02429 1 20070706 A 3350 20131A BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 OVERWING LEFT EMERGENCY LIGHT 2ND FROM BOTTOM INOP. REPLACED BATTERY PACK. OP CHECK'S SYSTEM & ALL CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071800300 20070718 00300 NM 2007 7 18 2007UALA02430 1 20070706 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY CEILING LIGHT ABOVE ROW 17 INOPERATIVE. RELAMPED EMERGENCY LIGHT. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071800310 20070718 00310 NM 2007 7 18 2007UALA02437 1 20070706 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS BROKEN A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 182UA 25279 CABIN UPPER DECK FWD & AFT EEL CABLES ARE BROKEN. [07-27-07] REPLACED EEL CABLES, OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072600014 20070726 00014 NM 2007 7 26 DHL2007784514 1 20070708 A 5330 SKIN BOEING 727 727227 1384078 NM BS 660 BURNED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 EXTERNAL FUSELAGE BS 660 AT STR 7R HAS A LIGHTNING BURN. BLENDED OUT AREA OF LIGHTNING STRIKE IAW B727 SRM 53-30-3, FIG 20. MATERIAL LOSS OVER 30 PERCENT AND LIGHTNING STRIKE STILL PRESENT AND OUT OF LIMITS IAW B727 SRM 53-30-1. CUT OUT DAMAGED AREA DIM 4.5 BY 2.5 IAW B727 SRM 53-30-3, FIG 3. HFEC COMPLIED WITH IN CUT OUT AREA, NO CRACKS NOTED IAW B727 N DTM PT.6 51-00-00, FIG 23. FABRICATED DOUBLER REPAIR FROM .050, 2024T3, DIM 12 BY 7.50 AND FILLER FROM .040, 2024T3, DI M 4.5 BY 2.25 IAW B727 SRM 53-30-2, FIG 2 AND 53-30-3, FIG 3. TREATED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 51-10-2 , 51-30-2 AND 53-30-3, FIG 3. 2 L 7 3 4F A3WE 2007071800317 20070718 00317 NM 2007 7 18 2007UALA02448 1 20070707 A 5610 WINDOW BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT CRACKED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 310UA 23671 FLIGHT DIVERTED DUE TO SHATTERED F/O EYE BROW WINDOW. INNER AND OUTER PANES INTACT, ONLY INTERLAYER IS DAMAGED. UNIT HA S BEEN ON A/C FOR EXTENDED PERIOD OF TIME (10 YEARS). ALSO, FOUND WINDOW HEAT WIRE BROKEN OFF. REPLACED EYEBROW WINDOW . 2 L 7 2 4F 4 F RT A16WE E21EU 2007071800323 20070718 00323 CE 2007 7 18 DXTA200702303 1 20070626 A 3240 99121631 PRESSURE SWITCH CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE BRAKES INOPERATIVE E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 334QS 8843 5600434 ON LANDING BRAKE PRESS LOW AND ANTISKID INOP LIGHTS ILLUMINATED WITH NO BRAKES. LIGHTS WENT OUT AND NORMAL BRAKING RETU RNED AFTER PUMPING BRAKES. TESTED ANTISKID SYSTEM WITH NO FAULTS. REPLACED KNOO2 RELAY P/N: M83536/9-024 + LOW PRESSUR E SWITCH. CHECKED SYSTEM + BLED BRAKES. OPERATIONAL CHECKS GOOD IAW MM CH. 32-42-00. OLD P/N: 9912163-1. OLD S/N: 2279. NEW P/N: 9912163-1. NEW S/N: 3285. CORRECTED BY: (DK). DATE CORRECTED: 6/29/07. CERT. TYPE AND NR: CNQ8918C. 2 L 7 2 4F 4 F RT A22CE E25EA 2007071800325 20070718 00325 SO 2007 7 18 N93A13072007 1 20070713 A 2530 MT4078SPB OVEN GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU GALLEY DEFECTIVE E N93A I CABIN DEPRESSURIZATION B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 13 462QS 1262 MICROWAVE OVEN DEFECTIVE. 2 L 7 2 4F 4 F RT A12EA E25NE 2007071800331 20070718 00331 CE 2007 7 18 DXTA200702314 1 20070702 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG WEAK E DXTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 319QS 5600519 CO-PILOTS BRAKE PEDALS ARE SPONGY. REQUIRES THE BRAKE PEDALS TO BE PUMPED (2) TO (3) TIMES TO BUILD PRESSURE. BLED BRAK ES. LT AND RT SIDE, TAXI CHECKED FOR BRAKE OPERATIONS. OPS CHECK GOOD. LEAK CHECK GOOD. IAW MM 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007071800332 20070718 00332 NM 2007 7 18 2007UALA02455 1 20070708 A 2740 PITCH CONTROL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 807UA 798 AIRCRAFT HAS CONSTANT TRIM PITCH UP AND PITCH DOWN CONDITION. CONDITION SAME WITH EITHER AUTOPILOT ENGAGED. REPLACED A CCELEROMETER 12CE3 PER TSM 27-30-00-810-853.PERFORMED MCDU TEST OF EPCS1.NO FAILURE MSSGS NOTED. REPLACED ACCEL 12CE4 AND THS POSITION TXDCR ACP AFS TEST ECFS1 AND ECFS2 TEST ALL OK CK THS RIG PIN STAB AT 0 RIG PIN OK ()ASSISTED AND CONFI RMED MCDU CHECKS GOOD. FLT TEST OK 2 L 7 2 4F 4 F RT A28NM E40NE 2007071800340 20070718 00340 NM 2007 7 18 2007UALA02459 1 20070708 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 838UA 1477 CABIN EMERGENCY LIGHTS FAILED TEST. [07-24-07] OPS CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071800343 20070718 00343 CE 2007 7 18 DXTA200702322 1 20070707 A 2150 73838433 ACM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL AFT SERVICE BAY FAILED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 944QS 4722 7500144 DESCENDING TROUGH FL310 CREW HEARD A VERY LOUD POP SOUND FOLLOWED IMMEDIATELY BY A STRONG SMOKE SMELL. NO SMOKE WAS OBS ERVED, THE POP SOUND SEEMED TO COME FROM CABIN AREA. T/S FOUND AFT (COCKPIT) ACM INOP. GAINED ACCESS TO ACM. REMOVED A CM AND INSTALLED A REPAIRED ACM. REINSTALLED ACCESS ITEMS. OPS AND LEAK CHECK CHECKS GOOD. WORK DONE IAW MM 21-51-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071800350 20070718 00350 CE 2007 7 18 DXTA200702327 1 20070710 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG WEAK E DXTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 371QS 5600471 BRAKES ARE VERY SPONGY USING BOTH SETS OF RUDDER PEDALS. INSPECTED AND BLEED BOTH LT AND RT BRAKE ASSY. NO DEFECTS FOUND , OPS CK GOOD IAW MM CH 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007071800357 20070718 00357 NM 2007 7 18 2007UALA02469 1 20070706 A 5320 SUPPORT ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 369UA 24538 AFT PIT STA 807, BETWEEN STR 26R AND 25R LOWER DOOR SILL SUPPORT ANGLE IS CRACKED. [07-27-07] MAJOR REPAIR: REPLA CED SUPPORT ANGLE AT STA 807 BETWEEN STR 26R AND 25R. REFERENCE SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071800362 20070718 00362 NM 2007 7 18 2007UALA02474 1 20070706 A 5310 BEARING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU STOP PAD LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 FWD ENTRY DOOR CUTOUT FWD & AFT STOP PADS ARE LOOSE. [07-20-07] REMOVED & REPLACED BEARING STOP PAD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071800365 20070718 00365 EA 2007 7 18 TRAX200700940 1 20070705 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 PUSH IN TO EXIT PLACARD WORN ON RT EMERGENCY EXIT DOOR (EXTERIOR). 2 L 7 2 4F RT A21EA 2007071800369 20070718 00369 EA 2007 7 18 TRAX200700952 1 20070706 A 5312 FLOOR SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 LT SIDE PRESSURE FLOOR SKIN AND DOUBLERS ARE CORRODED AT SEVERAL LOCATION BETWEEN FS 409.00 + 128 AND FS 559.00 BETWEEN LBL 36 AND 45 AT WL 73.50. WORK COMPLETED IN ACCORDANCE WITH: SRM 51-21-06, NDTM 51-20-04, REO6 601R-53-41-554, ND TM 51-20-06, AND SP 607. 2 L 7 2 4F RT A21EA 2007071800370 20070718 00370 EA 2007 7 18 TRAX200700954 1 20070706 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 AFT POTABLE WATER DRAIN MAST SKIN DOUBLER UNDER FLOOR IS CORRODED. 2 L 7 2 4F RT A21EA 2007071800388 20070718 00388 WP 2007 7 18 07FDEA02466 1 20070713 A 5312 BULKHEAD DOUG DC10 DC1010F 3022111 WP ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 CLG WHEEL WELL AREA CRACK ON VERTICAL BULKHEAD. REPAIRED AREA IAW SRM 53-00-01 FIG 10 VOL 1. 2 L 7 3 4F A22WE 2007071800392 20070718 00392 EA 2007 7 18 QXEA200701116 1 20070615 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 C3 OKC - LOWER TCAS MOUNT SKIN HAS LIGHT CORROSION. REPAIRED IAW SRM 51-21-06, 53-00-01. 2 L 7 2 4F RT A21EA 2007071900004 20070719 00004 NM 2007 7 19 07FDEA02476 1 20070713 A 5320 655835222 FLOOR SUPPORT BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD CARGO AREA, STA 718, STR 27R ABOUT RBL 12, FLOOR SUPPORT ANGLE IS CORRODED ON REPAIR ANGLE. REMOVED AND INSTALLED N EW REPAIR ANGLE IAW SRM 51-40-3. 2 L 7 3 4F RT A3WE 2007071900007 20070719 00007 WP 2007 7 19 07FDEA02479 1 20070713 A 5730 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 LT WING L/E ON EXTERNAL SKIN DROPPED FOUND DEEP WEAR. REPAIRED AREA IAW SRM 57-10-00 FIG 39 VOL 1. 2 L 7 3 4F A22WE 2007071900033 20070719 00033 NM 2007 7 19 CALA0700344 1 20070703 A 5313 6549914542 FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND STRINGER 17R END FITTING CORRODED JUST BELOW FLOOR LINE AT STA 1016. THE FITTING WAS REMOVED AND REPLA CED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071900044 20070719 00044 SO 2007 7 19 SIMA200719402 1 20070711 A 3350 2013A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 636AE 678 90 145160 FIRST 5 ROWS OF EMERGENCY LIGHT WILL NOT EXTINGUISH. REMOVED AND REPLACED NUMBER TWO BATTERY AND CHARGER IAW EMB AMM. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007071900045 20070719 00045 EU 2007 7 19 0703070144 1 20070703 A 6720 L673M40A1003 ACTUATOR UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1A NE LEAKING E E3MA K NONE O OTHER AA AIR AMBULANCE 1 EA 03 522ME 20 20 0144 LEAKING FLUID FROM WEEP HOLE. 1 G 7 2 3U 3 U H88EU E34NE 2007071900064 20070719 00064 SO 2007 7 19 SIMA200719419 1 20070705 A 5347 13500438003 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 717AE 15889 5000 145272 RIGHT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 23 TO 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPER ATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900078 20070719 00078 WP 2007 7 19 ARWA20070611 1 20070615 A 5730 ACCESS DOOR DOUG DC8 DC863F 302198F WP RT WING CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; RT WING UPPER SURFACE MAIN FUEL TANK ACC DOOR NR 505C WT OUT WITH 02 CRACKS. REPAIR ACC DOOR NR 505C OF RT WING UPPER SURFACE MAIN FUEL TANK IN ACCORDANCE WITH DRAWING NR AIPSAC - N661A V-02/07, DATED 01-12-07, SHEETS 1, 3, AND 4. LEAK CHECK IN ACCORDANCE WITH DC8 M/M 28-00, NO LEAKS NOTED. 2 L 7 4 4F 4A25 2007071900080 20070719 00080 WP 2007 7 19 ARWA20070704 1 20070710 A 3244 TIRE DOUG DC10 DC1030F 3023504 WP NR 7 FAILED A ARWA O OTHER O OTHER LD LANDING 1 SO 19 450ML 47831 NR 7 TIRE BLEW DURING LANDING AT SEGU. REMOVED AND REPLACED NR 7 MAIN WHEEL ASSEMBLY AND BRAKE ASSEMBLY AS PER M/M 32-4 1-03 AND 32-43-01; ALSO NR 8 TIRE INSPECTED AND FOUND SERVICEABLE TO BE DISPATCHED IN ACCORDANCE WITH ARROW AIR GMM 5-23 -7, SECTION "C". 2 L 7 3 4F RT A22WE 2007071900082 20070719 00082 NM 2007 7 19 07FDEA02449 1 20070713 A 5320 694488012 INTERCOSTAL BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 AFT PIT STA 970 STR 27R-28R INTERCOSTAL. REMOVED INTERCOSTAL REF SRM 51-30-2, REMOVED STIFFENERS REF SRM 51-30-2. FABR ICATED AND HEAT TREATED NEW INTERCOSTAL REF WO 2007-07-027 PN 69-44880-12. TREATED AND PRIMED INTERCOSTAL REF SRM 51-10 -2. INSTALLED NEW INTERCOSTAL REF SRM 51-30-2. 2 L 7 3 4F A3WE 2007071900098 20070719 00098 SO 2007 7 19 SIMA200719414 1 20070705 A 5347 1350412005 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 717AE 15889 5000 145272 LEFT OUTBORAD SEAT TRACK CORRODED BETWEEN FRAMES 53 TO 55. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERA TIONAL CHECK GOOD - RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900102 20070719 00102 SO 2007 7 19 SIMA200719705 1 20070705 A 5347 13500439003 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 717AE 15889 5000 145272 LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 23 TO 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900103 20070719 00103 SO 2007 7 19 SIMA200719711 1 20070708 A 5347 14000486005 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 816AE 13301 5000 145552 LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 23 TO 28. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRA FT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900109 20070719 00109 SO 2007 7 19 SIMA200719721 1 20070708 A 5347 14530659007 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 816AE 13301 5000 145552 LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRA FT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900110 20070719 00110 SO 2007 7 19 SIMA200719722 1 20070708 A 5347 14000486009 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 816AE 13301 5000 145552 RIGHT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 24 TO 28. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900112 20070719 00112 SO 2007 7 19 SIMA200719724 1 20070708 A 5347 14000486005 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 816AE 13301 5000 145552 LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 23 TO 28. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900115 20070719 00115 EA 2007 7 19 TRAX200700967 1 20070707 A 5230 BRACKET CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 857AS 7411 CARGO DOOR AFT RAIL SUPPORT BEAM BRACKET CRACKED. 2 L 7 2 4F RT A21EA 2007071900116 20070719 00116 EA 2007 7 19 TRAX200700968 1 20070707 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 758EV 10210 F/A FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007071900123 20070719 00123 NM 2007 7 19 USAA070527 1 20070711 A 5320 FLOOR SUPPORT BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 STA 312-328 LBL 12 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER 51-10-02; CORR TASK C53-107-02; LEVEL 1, DEFECT SIZE: 1 X 8 INCH. 2 L 7 2 4F RT A16WE 2007071900124 20070719 00124 2007 7 19 DXTA200702329 4 20070710 A 2210 7011702929 CONTROLLER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL AUTOPILOT INOPERATIVE E DXTA O OTHER O OTHER CR CRUISE 1 GL 07 947QS 4320 7500047 IN CRUISE ALTITUDE OF FL200 MACH NR APPEARED. SELECTED C/O BUTTON ON AUTOPILOT PANEL AND THE BUTTON REMAINED IN THE DEP RESSED POSITION. NO OTHER MODES WERE ALLOWED TO BE SELECTED AND AUTO PILOT WOULD NOT RE ENGAGE. REMOVED AND REPLACED F LIGHT CONTROLLER GC-810 OPPS CHECKS GOOD, REF MM CH 22-10-03. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071900126 20070719 00126 NM 2007 7 19 USAA070526 1 20070711 A 5210 6545871124 DOOR FRAME BOEING 737 737401 1384701 NM CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 DOOR FRAME AFT SIDE 4 INCHES BELOW CENTERING GUIDE ROLLER BEARING AT STOP FITTING CUTOUT HAS CRACK. REMOVED DAMAGED PAR TS & INSTALLED REPAIR PARTS PER TR 52-10-11, DEFECT SIZE: .125 INCH. 2 L 7 2 4F RT A16WE 2007071900127 20070719 00127 NM 2007 7 19 USAA070525 1 20070711 A 5320 TRACK BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 STA 767 + 5 RBL 8.10 HAS CORROSION. INSTALLED REPAIR KIT PER TYP REP 53-10-06B; CORR TASK C53-202-01; LEVEL 2, DEFECT S IZE: 2 INCHES. 2 L 7 2 4F RT A16WE 2007071900129 20070719 00129 NM 2007 7 19 USAA070524 1 20070711 A 5320 WEB BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 23379 FUSELAGE WEB AT DOOR SKIN, STA 847-867 AFT OF AFT CARGO DOOR HAS CORROSION. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER EA 97955A, DEFECT SIZE: 20 INCHES. 2 L 7 2 4F RT A16WE 2007071900130 20070719 00130 NM 2007 7 19 USAA070523 1 20070711 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 24893 BETWEEN BS 727E & 727F S-25R HAS CRACK. INSTALLED DOUBLER PER SRM 53-00-01, DEFECT SIZE: 3 INCHES. 2 L 7 2 4F RT A16WE 2007071900136 20070719 00136 CE 2007 7 19 DXTA200702338 1 20070715 A 2910 O-RING CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE BRAKE PUMP LEAKING E DXTA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 671QS 5605071 BLUE GEAR FLUID LEAKING OUT OF NOSE GEAR AND A HALF CUP OF FLUID HAS POOLED IN LT AVIONICS BAY. STARTED SMOKING WITH BAT TERY SWITCH ON. PULLED CIRCUIT BREAKERS. [07-23-07] FOUND BRAKE PUMP FILTER BOWL O-RING BLOWN & SMOKING WAS A SKYDR OL MIST COMING FROM BOWL WHEN UNDER PRESSURE. REPLACED O-RING & BLED BRAKES IAW CE560XL M/M CHAP 32-42-00. OPS CHECK & L EAK CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007071900138 20070719 00138 2007 7 19 DXTA200702339 4 20070715 A 2210 AUTOPILOT SYS BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE MALFUNCTIONED E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 145QS RK421 WITH AUTOPILOT CONNECTED RED (AP PITCH TRIM FAIL) ANNUNICTOR ILLUMINATED. WITH AP ON WE HEARD AN INTERMITTENT CLICK ( LI KE WHEN A CB POPS) BUT ALL CB'S ARE IN. [07-23-07] COMPLETED COMPLETE TRIM SYSTEM OPERATIONAL CHECK IN NORMAL EMERGE NCY AND AUTO-PILOT. ACCESSED PITCH TRIM ACTUATOR CLEANED, LUBED AND OEPRATED ACTUATOR NO DEFECT NOTED AT THIS TIME ALL W ORK IAW 400XP 27-40-00 & 12-20-00. 2 H 7 2 4F 4 F RT A16SW E25EA 2007071900141 20070719 00141 SO 2007 7 19 RAIA00707014 1 20070707 A 5210 STOP FITTING EMB 145 EMB145LR 3260212 SO PAX DOOR OUT OF ADJUST A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 843HK 14500822 POST FLT NR FLMX - STL - PAX DOOR HARD TO OPEN. MAINTENANCE PERFORMED RIG CHECK OF PAX DOOR AND ADJUSTED DOOR STOP SHIM S. DOOR OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT T00011AT 2007071900146 20070719 00146 CE 2007 7 19 DXTA200702320 1 20070705 A 3240 6633622021 CONTROL CABLE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL BRAKES STICKING E DXTA O OTHER O OTHER LD LANDING 1 GL 07 900QS 7056 7500123 AFTER LANDING AND STRONG BREAKING, AIRCRAFT BRAKES FEEL LIKE THEY HAVE NOT RELEASED. BRAKES FINALLY RELEASED WHEN PEDA LS WERE QUICKLY PUSHED AS HARD AS POSSIBLE AND THEN RELEASED. REMOVED AND REPLACED BOTH BRAKE CABLES WITH NEW IAW MM 32 -42-02 GROUND OPS CHECKED GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071900153 20070719 00153 SO 2007 7 19 RAIA00707018 1 20070709 A 2910 3535701001 MANIFOLD EMB 145 EMB145LR 3260212 SO AILERON LEAKING A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 819HK 21861 21861 145062 FLT NR 5505 - STL - DURING FLIGHT -EICAS MESSAGE- NR 1 HYDRAULIC OVERHEAT MESSAGE, RAN CHECKLIST TURNED NR 1 SYSTEM OFF DURING DESCENT INTO STL. TURNED SYSTEM BACK ON AS PER CHECKLIST AND GOT A NR 1 SYSTEM FAIL-E1 HYD PUMP FAIL HYD NR 1 SO V CLOSED ON FINAL APPROACH THE PUMP STARTED. MAINTENANCE PERFORMED FAULT ISOLATION PROCEDURES, FOUND AILERON MANIFOLD A SSY LEAKING AND REMOVED AND REPLACED MANIFOLD. OPS AND LEAK CHECK GOOD. COULD NOT DUPLICATE PROBLEM WITH LANDING GEAR UP AND PUMPS RUNNING FOR 45 MIN. 2 L 7 2 4T RT T00011AT 2007071900157 20070719 00157 CE 2007 7 19 DXTA200702330 1 20070711 A 3234 HANDLE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG STUCK E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 915QS 7500015 AFTER TAKEOFF LANDING GEAR HANDLE WAS STUCK IN THE DOWN POSITION. [07-23-07] REMOVED AND REPLACED NOSE LANDING GEAR ASSY WITH SERVICABLE UNIT FROM CESSNA ICT RS CNQR918C PER CESSNA 750 MM 32-20-00. GROUND OP'S CHECKED GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071900159 20070719 00159 NM 2007 7 19 SB07053 1 20070711 A 3350 20131ASMI BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 511AU 23594 PIT - MAINTENANCE REPORTED THE AFT GALLEY EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LE FT BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007071900165 20070719 00165 EA 2007 7 19 COMA0760465 1 20070703 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 735CA 11507 7267 FLIGHT 5175 - RECEIVED FLAP FAIL MESSAGE AFTER TAKEOFF. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MEGGED LEFT AN D RIGHT HARNESSES AND BPSU'S. REPLACED LEFT AND RIGHT BPSU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007071900170 20070719 00170 NM 2007 7 19 WRLA2007079 1 20070709 A 2530 831620405 OVEN DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE FWD GALLEY MALFUNCTIONED A WRLA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 801DE 48472 KBWI/LIMC FWD GALLEY OVENS MADE POPPING SOUND FOLLOWED BY ELECTRICAL SMELL WHILE COOKING. REMOVED POWER FROM OVENS BY P ULLING C/B'S. RAN BOTH OVENS FOR ONE HOUR, BOTH OPERATED AS NORMAL IAW MM 25-31-50. 2 L 7 3 4F 4 F RT A22WE E24NE 2007071900171 20070719 00171 EA 2007 7 19 COMA0760470 1 20070706 A 2760 4916405 SECU CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 477CA 1560 7670 FLIGHT 5264 - ON DESCENT, RECEIVED SPOILERON CAUTION MESSAGE, FOLLOWED IN 15 SECONDS BY FLIGHT SPOILER CAUTION AS WELL A S O/B AND I/B GROUND SPOILER FAULT. ABORTED APPROACH, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND CODES 1F AND 15 FOR SECU'S. REPLACED NR 2 SECU. NO FURTHER DEFEFCTS. 2 L 7 2 4F RT A21EA 2007071900172 20070719 00172 EA 2007 7 19 COMA0760471 1 20070706 A 2760 4916405 SECU CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 477CA 16274 7670 FLIGHT 5264 - ON DESCENT, RECEIVED SPOILERON CAUTION MESSAGE, FOLLOWED IN 15 SECONDS BY FLIGHT SPOILER CAUTION AS WELL A S O/B AND I/B GROUND SPOILER FAULT. ABORTED APPROACH, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. FOUND CODES 1F A ND 15 FOR SECU'S. REPLACED NR 1 SECU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007071900173 20070719 00173 EA 2007 7 19 COMA0760472 1 20070709 A 5320 601R311135758 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 510CA 10926 7802 FLOOR SUPPORT STRUCTURE CRACKED AT FS 280.00 RBL 9. REMOVED AND REPLACED INBOARD AND OUTBOARD CLIPS AT RBL 9 FS 280.0 I AW CRJ SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007071900174 20070719 00174 EA 2007 7 19 TRAX200700971 1 20070708 A 3260 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 900EV 7608 AFTER DEPARTING BTR, RECEIVED -GEAR DISAGREE, WOW INPUT GEAR UNSAFE, NOSE WHEEL STEERING INOP- MSG. IN THE COCKPIT VERI FIED THROUGH NOISE AND VIBRATION THAT THE NOSE GEAR WAS NOT UP AND LOCKED. COMPLIED WITH QRH. A/C RETURNED TO BTR AFTE R T/O. EMERGENCY DECLARED. RELATED TO DEFECT NR 317576-2. FLT 4703 CX. 2 L 7 2 4F RT A21EA 2007071900175 20070719 00175 EA 2007 7 19 TRAX200700972 1 20070708 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 925EV 7831 RIGHT WING EMERGENCY LIGHT IS INOP. 2 L 7 2 4F RT A21EA 2007071900178 20070719 00178 NM 2007 7 19 SWAA073387 1 20070710 A 5523 18A80101 BOLT BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED C3 CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BOLT AND BUSHING PER MM. 2 L 7 2 4F RT A16WE 2007071900179 20070719 00179 NM 2007 7 19 SWAA073393 1 20070709 A 3350 3071BPEGPL LAMP BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT LOWER LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007071900181 20070719 00181 NM 2007 7 19 SWAA073384 1 20070709 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 245WN 32506 EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007071900182 20070719 00182 NM 2007 7 19 SWAA073402 1 20070711 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, STR 28R. REPAIRED SKI N PER SWA EA. 2 L 7 2 4F RT A16WE 2007071900184 20070719 00184 SO 2007 7 19 SIMA200719703 1 20070714 A 2720 985051579310 PRESSURE SENSOR EMB 145 EMB145LR 3260212 SO RUDDER FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 663AR 9015 145778 RECEIVED RUDDER 1-2 INOPERATIVE MESSAGE ABOVE FL 220 WITH AUTO PILOT ON - FOLLOWED AOM PROCEDURES. DIVERTED TO SGF. RE MOVED AND REPLACED RUDDER PRESSURE SWITCH IAW EMB AMM 27-23-04. OPERATIONAL CHECK GOOD IAW EMB AMM 27-23-00-700-804A, S TEP J, SECTION 2. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007071900192 20070719 00192 SO 2007 7 19 SIMA200719710 1 20070708 A 5347 14532605015 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 816AE 13301 5000 145552 LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 36 TO 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900193 20070719 00193 SO 2007 7 19 SIMA200719712 1 20070708 A 5347 14000486003 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 816AE 13301 5000 145552 RIGHT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 28 TO 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900195 20070719 00195 SO 2007 7 19 SIMA200719716 1 20070708 A 5347 14000486017 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 816AE 13301 5000 145552 RIGHT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 23 TO 28. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900197 20070719 00197 SO 2007 7 19 SIMA200719718 1 20070708 A 5347 13500439007 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 816AE 13301 5000 145552 LEFT FORWARD INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 18 TO 23. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900203 20070719 00203 NM 2007 7 19 SWAA073423 1 20070711 A 5311 6546529 BELTFRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 500C, STR 20R. REPAIRED BELTFRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071900205 20070719 00205 NM 2007 7 19 SWAA073411 1 20070711 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM R2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 14Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007071900206 20070719 00206 SO 2007 7 19 SIMA200719801 1 20070715 A 2400 UNKNOWN EMB 135 EMB135KL 3260302 SO WARNING MESSAGE UNKNOWN A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 838AE 145651 RECEIVED ELECTRICAL EMERGENCY ABNORMAL MESSAGE, DIVERTED TO BUF, MESSAGE CLEARED ITSELF. NO CMC MESSAGE NOTED, RESET EL ECTRICAL POWER PER EMB FAULT ISOLATION MANUAL TASK 24-60-00-810-820A. 2 L 7 2 4F RT T00011AT 2007071900207 20070719 00207 SO 2007 7 19 SIMA200719806 1 20070522 A 5320 14521725001 SILL EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 15926 5000 145224 FORWARD CABIN FLOOR SILL LEFT SIDE CORRODED. REMOVED AND REPLACED FLOOR SILL IAW EMB SRM 51-40-02. RETURNED AIRCRAFT T O SERVICE. 2 L 7 2 4F RT T00011AT 2007071900208 20070719 00208 NM 2007 7 19 SWAA073420 1 20070711 A 5314 6562125 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND KEEL BEAM CORRODED AT BS 540, RBL 6.50. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2007071900209 20070719 00209 NM 2007 7 19 SWAA073413 1 20070711 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED C4 CHECK, FOUND LEFT WING NR 2 L/E SLAT CRACKED AT FWD INBOARD END. REPAIRED SLAT PER SWA EA. 2 L 7 2 4F RT A16WE 2007071900210 20070719 00210 EA 2007 7 19 SIMA200719802 1 20070715 A 2780 SLAT SYSTEM CNDAIR CL600 CL6002C10 1390015 EA UNKNOWN A SIMA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 21 506AE 10056 SLAT FAIL CAUTION AND SLAT ACT SYSTEM FAILED MECHANICAL JAM MESSAGE. RESET SLAT ACTUATOR, TRIP INDICATORS; LEFT SIDE WS 48.00, WS327.00, WS423.00 AND RIGHT SIDE WS48.00, WS327.00, WS353.00, WS423.00 IAW CRJ AMM 27-81-09. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007071900211 20070719 00211 NM 2007 7 19 SWAA073407 1 20070711 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007071900216 20070719 00216 NM 2007 7 19 SWAA073392 1 20070708 A 3397 8100022701 CONNECTOR BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 266WN 32523 EEPLS INOP BETWEEN ROW 5 ABC AND ROW 7 ABC. FOUND LOOSE CONNECTOR, RECONNECTED PER MM. 2 L 7 2 4F RT A16WE 2007071900218 20070719 00218 NM 2007 7 19 SWAA073401 1 20070711 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND STRINGER 23R CRACKED AT BS 494. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007071900219 20070719 00219 2007 7 19 SWAA073414 4 20070711 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 L2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071900220 20070719 00220 2007 7 19 SWAA073390 4 20070710 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071900221 20070719 00221 2007 7 19 SWAA073410 4 20070711 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 14Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071900222 20070719 00222 NM 2007 7 19 SWAA073419 1 20070711 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 460WN 32464 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2007071900225 20070719 00225 WP 2007 7 19 07FDEA02457 1 20070713 A 5322 SHEAR TIE DOUG DC10 DC1010F 3022111 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 CTR CARGO COMPT TUNNEL ON SHEAR CLIP FOUND CRACK 0.50" LONG. REPAIRED SHEAR CLIP IAW SRM 53-30-00 VOL 1 FIG 10. 2 L 7 3 4F A22WE 2007071900227 20070719 00227 NM 2007 7 19 KCSA071211 1 20070712 A 5320 SHEAR WEB BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 TENSION TIE SHEAR WEB O/B WEB CRACKED BETWEEN STA 820 AND 840 LT SIDE. 2 L 7 4 4F RT A20WE 2007071900228 20070719 00228 EA 2007 7 19 CHQA200700035 1 20070714 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS INOPERATIVE A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 638BR 7311 FLIGHT 3203 - CMH-IAH - AT FL360, EXPERIENCED AN UNCOMMANDED FLAP DEPLOYMENT OF UP TO 8 DEGREES IN FLIGHT WITH THE FLAP SELECTOR IN THE 0 DEGREE POSITION. IMMEDIATELY REDUCED AIRSPEED AND INITIATED A DESCENT TO 15,000 FEET. IN DESCENT, TH E FLAPS CONTINUED TO OSCILLATE BETWEEN 3-8 DEGREES EXTENSION. THE FLAP DISPLAY WAS WHITE IN COLOR INDICATING A POSSIBLE ASSYMETRIC CONDITIONS, HOWEVER THAT FLIGHT CHARACTERISTIC WAS NOT NOTED. DECLARED AN EMERGENCY AND LANDED WITHOUT INCI DENT. MAINTENANCE REMOVED AND REPLACED THE PDU. 2 L 7 2 4F RT A21EA 2007071900232 20070719 00232 EA 2007 7 19 TRAX200700928 1 20070704 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 AFT ANGLE FS 280 BETWEEN RBL 9 AND LBL 9 CORRODED. APPLIED CORROSION INHIBITOR AND SEALANT TO BULKHEAD PER REO601R-53-1 1-956. SUPPLEMENTAL - SDR CLOSED 07/13/07. 2 L 7 2 4F RT A21EA 2007071900234 20070719 00234 EA 2007 7 19 TRAX200700953 1 20070706 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 INTERCOSTAL AT FS 484.00 BETWEEN LBL 27 AND 36 INBOARD CLIP IS CRACKED. FINISHED INSTALLING INBOARD CLIP AT FS 484 BETW EEN LBL 27 AND 36 IAW CRJ 200 SRM 51-42-21 SG20421. SDR CLOSED 07/13/07. 2 L 7 2 4F RT A21EA 2007071900237 20070719 00237 EA 2007 7 19 TRAX200700963 1 20070706 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 SERVICE DOOR ANGLE CORRODED AT FS 31- 349 AT SERVICE DOOR SEAL. FOR CORROSION TO SERVICE DOOR SILL ANGLE, REFER TO WO 6 3655 N/R-00166. BLENDED CORROSION ON ANGLE P/N 601R38303-255 AS PER CRJ 200 SRM 51-21-06 AND WITHIN LIMITS OF CRJ200 SR M 53-00-00. ALODINED, PRIMED, AND PAINTED IAW CRJ200 SRM 51-25-00. JOB COMPLETE, SUPPLEMENTAL - SDR CLOSED 07/13/07. 2 L 7 2 4F RT A21EA 2007071900239 20070719 00239 EU 2007 7 19 UPS07150161 1 20070712 A 5321 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 127UP 0811 INSPECTION TYPE:N/A IN BULK COMPARTMENT LOAD CREW REPORTED SMALL HOLE IN FLOOR FOUND TO BE DENT 1.75 INCH WITH .75 INCH TEAR AT BOTTOM LOCATED 31.5 INCHES IN FROM BULK DOOR AND 3.5 INCHES FROM TIE DOWN FITTING FOR NET. PERFORMED TEMP REPAI R TO DAMAGE W/ REF TO SRM 53-10-20 FIG 110. ITEM TO BE PERMANENTLY REPAIRED WITHIN 350 FLIGHT HOURS ASSIGNED ON DEFERRA L D-354335. 2 L 7 2 4F RT A35EU 2007071900240 20070719 00240 NM 2007 7 19 SWAA073418 1 20070711 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 460WN 32464 DURING SCHEDULED HC1 CHECK, RIGHT AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007071900242 20070719 00242 NM 2007 7 19 SWAA073417 1 20070711 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 460WN 32464 DURING SCHEDULED HC1 CHECK, LEFT AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK P ER MM. 2 L 7 2 4F RT A16WE 2007071900243 20070719 00243 NM 2007 7 19 SWAA073398 1 20070711 A 3350 MS155721 LAMP BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007071900247 20070719 00247 NM 2007 7 19 SWAA073385 1 20070710 A 2560 PL22300LH GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 703SW 27837 EEPLS PHOTOLUMINESCENT STRIP LOOSE AT RIGHT OVERWING EMERGENCY EXIT ROW. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007071900248 20070719 00248 NM 2007 7 19 SWAA073391 1 20070710 A 5523 REP4HE8 BEARING BOEING 737 7375H4 138449D NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED C4 CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL PUSHROD BEARING PER MM. 2 L 7 2 4F RT A16WE 2007071900249 20070719 00249 NM 2007 7 19 SWAA073405 1 20070711 A 5523 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 14Y CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BUSHING AND TOR QUE TUBE BEARING PER MM. 2 L 7 2 4F RT A16WE 2007071900250 20070719 00250 NM 2007 7 19 SWAA073406 1 20070711 A 5523 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM LT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 14Y CHECK, LEFT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BUSHING AND TORQ UE TUBE BEARING PER MM. 2 L 7 2 4F RT A16WE 2007071900251 20070719 00251 NM 2007 7 19 SWAA073394 1 20070709 A 3397 W13411522 WIRE BOEING 737 7373H4 1384600 NM CABIN FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED MV2 CHECK, INTERIOR EMERGENCY EXIT LIGHTS ILLUMINATED INTERMITTENTLY. FOUND FRAYED WIRE AT AFT FLIGHT ATTENDANT SWITCH. REPAIRED WIRE PER MM. 2 L 7 2 4F RT A16WE 2007071900252 20070719 00252 NM 2007 7 19 R61A20070012 1 20070609 A 2840 WARNING SYSTEM EMB ERJ170 ERJ170100SU 3260403 NM FUEL SYSTEM MALFUNCTIONED A R61A O OTHER N FALSE WARNING CL CLIMB 1 GL 11 818MD 17000039 CREW REPORTED THAT DURING CLIMBOUT RECEIVED A FUEL FEED 1 FAULT WARNING ON EICAS. RETURNED TO THE FIELD. MAINTENANCE W AS DISPATCHED, TROUBLESHOT SYSTEM, DID NOT FIND ANY DEFECTS. COMPLETED AN OPERATIONAL CHECK OF THE SYSTEM, OPERATIONAL CHECK GOOD. MAINTENANCE RETURNED THE A/C TO SERVICE. 2 L 7 2 4F RT A56NM 2007071900253 20070719 00253 EU 2007 7 19 UPS07150162 1 20070711 A 2910 FLEX LINE AIRBUS A300 A300F4622R 3930360 EU HYDRAULIC SYS LEAKING A IPXA K NONE K FLUID LOSS AP APPROACH 1 SO 01 135UP 0818 INSPECTION TYPE:N/A PILOT REPORTED HYDRAULIC FLUID LOSS DURING SHORT FINAL. PER MM REPLACE NR 2 ENG DRIVEN HYDRAULIC PU MP, YELLOW SYS MM 29-11-32-04. FOUND YELLOW SYS FLEX LINE LEAKING JUST AFT OF RIGHT WING MLG STRUT. REPLACED BOTH PRES S & RETURN FLEX LINES FOR RIGHT WING AILERON. LEAK CHECK GOOD. REMOVED AND REPLACED NR 2 ENG DRIVEN HYDRAULIC PUMP, YE LLOW SYS PER MM 29-11-32-04. 2 L 7 2 4F RT A35EU 2007071900254 20070719 00254 NM 2007 7 19 UPS07550158 1 20070613 A 5311 143N102569 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 420UP 23907 INSPECTION TYPE:C DENTS IN FWD CARGO FUSELAGE FRAME STA 760, BETWEEN S23L TO S25L. ACCOMPLISHED ON FINAL EA 757-5330-27 -A1697 AND UPS EO B757-5310- 27210-A. 2 L 7 2 4F RT A2NM 2007071900258 20070719 00258 2007 7 19 UPS07850163 4 20070711 A 2565 SLIDE DOUG DC8 DC873F 302199F WP COCKPIT OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:N/A RESTOW ESCAPE SLIDE. RESTOWED ESCAPE SLIDE IAW MM 25-60-01-2. 2 L 7 4 4F RT 4A25 2007071900259 20070719 00259 NM 2007 7 19 UPS07M50154 1 20070409 A 5347 AFA7789547 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C AFT CABIN - CORROSION ON SEAT TRACK CROWN & FLANGE AT STA 1966 X=107. CURVE SEAT TRACK ATTACHMENT & A TTACHED PARTS AT STA 1831-2007 X=107 LEFT REMOVED PER SRM 51-31-01 V.II R.39. CLEAN UP REWORKED AREA PER SRM 51-21- 01 V.II R.39. NEW SEAT TRACK AFA7789-547, 1EA LOCATED PER SRM 53-70-00 V. V.I FIG 8.R.39. NEW SEAT TRACK INSTALLED PER SR M 51-31-01 V.II R.39. HFEC INSP C/O ON REWORKED AREA FOUND NO CRACK ON REWORKED AREA. 2 L 7 3 4F RT A22WE 2007071900260 20070719 00260 NM 2007 7 19 UPS07M50155 1 20070529 A 5720 WEB DOUG MD11 MD11F 3023600 NM RT WINGLET CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C RIGHT WINGTIP LOWER WINGLET LOWER STRUCTURAL BORE FOUND CRACK. WEB CRACK END STOP HOLE DRILLED PER EN 1350-07. CRACK BOLT HOLE REAMED PER EN 1350-07. REP BUSHING FAB & INSTALLED PER EN 1350-07. FPI CARRIED OUT AS PER D PS 4.707 REV AW ON FABRICATED PART AND FOUND NO CRACK EVIDENT. 2 L 7 3 4F RT A22WE 2007071900261 20070719 00261 NM 2007 7 19 UPS07M50156 1 20070409 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C MID CABIN - CORROSION ON SEAT TRACK CROWN AT STA 909 X=-75.0. CABIN STA 909 X=-75 SEAT TRACK BASE COR ROSION REMOVED & REPROTECTED PER SRM 53-70-00 FIG 3 V.I R.39 & SRM 51-21-01 V.II R.39. CABIN STA 909.6 X =-75 SEAT TRAC K CROWN CORROSION REMOVED 0.072", REMAIN THICKNESS 0.073" & FOUND WITHIN LIMIT. NEW REPAIR SEAT TRACK, REPAIR SPLICE, N EW FAB CLIP & BRACKET INSTALLED PER EN 1363-07. 2 L 7 3 4F RT A22WE 2007071900262 20070719 00262 NM 2007 7 19 UPS07M50157 1 20070425 A 5730 DOUBLER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C RIGHT WING L/E COMPARTMENT AT STA XORS 550 APPROX FOUND UPPER SKIN DOUBLER CRACKED AS MARKED. DAMAGED AREA AT RIGHT WING L/E COMPT AT STA XORS 550 APPROX, UPPER SKIN DOUBLER AREA TRIMMED OUT AS PER SRM 57-10-00 V.I FIG 27 IAW EN 1294-07. HFEC IN INSP C/O PER DAC NDTSPM R.13 06-10-01.001 ON TRIMMED OUT AREA, FOUND NO CRACK EVIDENT. NEW RE PAIR FILLER DOUBLER & REPAIR ANGLES FAB & INSTALLED PER EN 1294-07. 2 L 7 3 4F RT A22WE 2007071900263 20070719 00263 EA 2007 7 19 TRAX200700976 1 20070709 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 832AS 7243 SUSPECTED CRACK ON INTERCOSTAL UPPER RADIUS AT FS 484 LBL 27 O/B. 2 L 7 2 4F RT A21EA 2007071900264 20070719 00264 WP 2007 7 19 DXTA200702331 2 20070711 A 7314 306071016 PUMP RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP RT ENGINE LOW PRESSURE E DXTA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 GL 07 842QS 7143 258542 AT CRUISE, TRANSFERRING FUEL AS RT PUMP WAS TURNED OFF AIRCRAFT SHUDDERED WITH LOUD BANG NOISE. ELECTED TO STOP THE TRA NSFER: AS PUMP WAS TURNED ON AGAIN AIRCRAFT AGAIN SHOOK WITH BANG NOISE. ALSO, NOTED A DROP IN FUEL FLOW TO RT ENG. IN SPECTED RT WING BOOST PUMP-NO DEFECTS NOTED. DRAINED SMALL AMOUNT OF WATER FROM BOTH WING TANKS - OPS TESTED RT BOOST P UMP, OPS TEST OK. INSTALLED A REPAIRED CONDITION FUEL PUMP ON THE NR 2 ENGINE. PERFORMED OPS CHECK IAW LMM 72-00-00. ( NO DEFECTS NOTED) 2 L 7 2 4F 4 F RT A3EU E6WE 2007071900265 20070719 00265 EA 2007 7 19 TRAX200700977 1 20070709 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 832AS 7243 SUSPECTED CRACK ON INTERCOSTAL UPPER RADIUS AT FS 484 RBL 27 O/B. LPI WAS PERFORMED ON THE CLIP UPPER RADIUS AT FS 484 RBL 27, O/B IAW NDTM 51-20-08 AND FOUND TO BE CRACKED IN THE UPPER RADIUS, APPROX 1/4". REMOVED DAMAGED CLIP AT FS 484 RBL 27 O/B AND DUPLICATED PART FROM PRE-FORMED STOCK P/N S-6144-3 FROM PO 950007 IAW CRJ 200 SRM 51-40-06, 51-40-11 AND BOMBARDIER DWG NR S6144. OK TO TREAT AND PRIME. ALODINED AND PRIMED IAW CRJ 200 SRM 51-21-11 AND 51-25-06. OK TO INSTA LL. INSTALLED DUPLICATED CLIP AT FS 484 RBL 27 O/B IAW CRJ 200 SRM 51-42-21. SUPPLEMENTAL - SDR CLOSED 07/18/07 2 L 7 2 4F RT A21EA 2007071800010 20070718 00010 EA 2007 7 18 TRAX200700936 1 20070705 A 3350 STRIP CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 970EV 7527 AFT EMERGENCY LIGHTING FLOOR STRIP MISSING. 2 L 7 2 4F RT A21EA 2007071800011 20070718 00011 NM 2007 7 18 DLM88070884 1 20070706 A 5311 FRAME DOUG MD88 MD88 3023688 NM BS 905 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948DL 49879 CRACK ON FORMER STA Y=905 X=-58. DOUBLER MANUFACTURED PER SRM 51-70-5 FIG 1 ON N/R T0060286 HMV-3. 2 L 7 2 4F RT A6WE 2007071800035 20070718 00035 EU 2007 7 18 SA07046 1 20070708 A 3260 LAMP AIRBUS A319 A319112 3930323 EU NLG OUT OF POSITION A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 708UW 0972 FLIGHT 1026, TPA-CLT: AFTER TAKEOFF, CREW RECEIVED A NOSE LANDING GEAR SHOCK ABSORBER WARNING. RETURNED TO TPA. MAINT ENANCE REMOVED A LAMP FROM THE NOSE GEAR ASSEMBLY. 2 L 7 2 4F RT A28NM 2007071800040 20070718 00040 SO 2007 7 18 RAIA00707004 1 20070703 A 3350 74448 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 810HK 145231 PRE FLT 7901 - ORD - EMERGENCY EXIT LIGHT AT RIGHT HAND OVERWING EXIT IDENTIFIER INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. 2 L 7 2 4T RT T00011AT 2007071800052 20070718 00052 NM 2007 7 18 CALA0700339 1 20070706 A 5310 652072371 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR CUTOUT AFT FRAME AT LOWER DOOR STOP FITTING, STA 440, S17R TO 24R. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071800053 20070718 00053 NM 2007 7 18 CALA0700340 1 20070706 A 5330 65C33930 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14346 23584 INSPECTION FOUND A .5 INCH CRACK IN SKIN AT SCREW HOLE, STA 380, S28L TO 28R. REPAIRED IAW ECRA 5330-02894. 2 L 7 2 4F RT A16WE 2007071800054 20070718 00054 NM 2007 7 18 CALA0700341 1 20070707 A 5320 6545819U45 GUSSET BOEING 737 7373T0 1384582 NM NLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND A 2 INCH CRACK IN NOSE WHEEL WELL GUSSET AT END OF NLG DRAG BRACE. THE GUSSET WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071800065 20070718 00065 NM 2007 7 18 UPS07550140 1 20070708 A 5210 DOOR BOEING 757 75724APF 1384969 NM ENTRY DOOR STICKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 454UP 25475 INSPECTION TYPE:N/A CABIN ENTRY DOOR STICKS AND DIFFICULT TO OPEN AND CLOSE. PER AMM 12-21-20 LUBRICATED CABIN ENTRY DO OR HANDLE CAM. OPERATION CHECK OK. 2 L 7 2 4F RT A2NM 2007071800072 20070718 00072 2007 7 18 DL76P070905 2 20070711 A 7320 7705401 RELAY BOEING 767 767332 1382001 NM RT ENGINE INOPERATIVE A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 1402A 25989 P1076 RT ENG EEC MODE MESSAGE, RETURN TO BLOCK. T/S PER FIM REPLACED RELAYS K403 AND K670 RAN ENG MESSAGE ERASED. 2 L 7 2 4F RT A1NM 2007071800073 20070718 00073 NM 2007 7 18 AALA20071212 1 20070629 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 780AN 29956 MIA - EMERGENCY LIGHT AT SEAT 24C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT T00001SE 2007071800076 20070718 00076 WP 2007 7 18 AALA20071226 1 20070701 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 419AA 49331 LGA - AFT OVERHEAD EMERGENCY LIGHTS AT RIGHT LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR AFT OVERHEAD EMERGENCY LIG HT AT RIGHT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071800077 20070718 00077 NM 2007 7 18 AALA20071227 1 20070702 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 369AA 25196 JFK - EMERGENCY EXIT SIGN LIGHTS AT LEFT AND RIGHT NUMBER FOUR DOORS INOPERATIVE. REPLACED BATTERY PACK AT LEFT NUMBER FOUR DOOR FOR EMERGENCY EXIT SIGN LIGHTS AT LEFT AND RIGHT NUMBER FOUR DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007071800099 20070718 00099 WP 2007 7 18 ASAA0781849 1 20070704 A 5311 991960431 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 AFT CARGO FRAME CORRODED AT STA 1250 BETWEEN LONG 29L AND LONG 29R. REMOVED DAMAGED SECTION OF FRAME, LOCATED DRILLED A ND INSTALLED A REPLACEMENT FRAME IAW SRM 51-03 FIG 2A AND 51-30-5 PG 12 AND 13. 2 L 7 2 4F RT A6WE 2007071800115 20070718 00115 NM 2007 7 18 AALA20071254 1 20070706 A 3350 8039001 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9412W 53187 LGA - OVERHEAD EMERGENCY LIGHTS AT SEAT ROW 8 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROW 8. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2007071800125 20070718 00125 NM 2007 7 18 QXEA200701156 1 20070715 A 3060 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM PROP DEICE UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 424QX 4006 SEA - ON FLIGHT 2394, RETURNED TO GATE, PROP DEICE CAUTION AFTER START UP. MAINTENANCE PERFORMED OPERATIONAL CHECK, OPE RATIONAL CHECK GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007071800135 20070718 00135 NM 2007 7 18 SWAA073347 1 20070706 A 2612 FIRE WARNING BOEING 737 7373H4 1384600 NM COCKPIT MALFUNCTIONED A SWAA F ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 SW 29 373SW 26581 DECLARED EMERGENCY. DESCENDING INTO SEA FWD CARGO FIRE LIGHT ILLUMINATED, DISCHARGED FIRE BOTTLES. NO EVIDENCE OF FIRE . REMOVED AND REPLACED FIRE BOTTLES AND SQUIBS PER MM. 2 L 7 2 4F RT A16WE 2007071800142 20070718 00142 NM 2007 7 18 SWAA073357 1 20070706 A 5531 6547428 RIB BOEING 737 7373H4 1384600 NM VERTICAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND VERTICAL STABILIZER RIB CRACKED AT STA 292.70. REMOVED AND REPLACED RIB PER SRM. 2 L 7 2 4F RT A16WE 2007071800144 20070718 00144 NM 2007 7 18 SWAA073350 1 20070706 A 5511 6547517 RIB BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 14Y CHECK, FOUND LEFT HORIZONTAL STAB RIB CRACKED AT STA 212.30. REMOVED AND REPLACED RIB PER SRM. 2 L 7 2 4F RT A16WE 2007071800145 20070718 00145 EA 2007 7 18 QXEA200701117 1 20070628 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 C3 OKC - FLIGHT DECK CENTER FLOORBOARD AFT SUPPORT ANGLE HAS CORROSION ON LOWER SURFACE. REPAIRED IAW SRM 51-40-00, 51- 42-06. 2 L 7 2 4F RT A21EA 2007071800147 20070718 00147 NM 2007 7 18 SWAA073355 1 20070706 A 5743 6582764 BEAM BOEING 737 7373H4 1384600 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND RIGHT MLG STABILIZER BEAM CORRODED. REMOVED AND REPLACED MLG BEAM PER MM. 2 L 7 2 4F RT A16WE 2007071800154 20070718 00154 NM 2007 7 18 SWAA073353 1 20070706 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED MV4 CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2007071800164 20070718 00164 EA 2007 7 18 QXEA200701108 1 20070613 A 5730 PANEL CNDAIR CL600 CL6002C10 1390015 EA LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 C3 OKC - LEFT WING PANEL 584GB CHAFED. REPAIRED IAW SRM 51-12-00, 51-25-06, 57-52-01. 2 L 7 2 4F RT A21EA 2007071800168 20070718 00168 NM 2007 7 18 SB07050 1 20070704 A 3350 20131ASMI BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 511AU 23594 DCA - MAINTENANCE REPORTED THE AFT CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BOTH THE AFT LE FT AND AFT RIGHT BATTERY PACKS. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007071800171 20070718 00171 EA 2007 7 18 HNAA0700122 1 20070626 A 7931 APT761000100D TRANSMITTER DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 2 ENGINE FAULTY A HNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 07 328EN 281 123154 NR 2 ENGINE OIL PRESSURE WENT TO ZERO ON TAKEOFF ROLL, ALL OTHER ENGINE PERIMETERS NORMAL, NO CAUTION LIGHTS. CHECKED O IL LEVEL FOUND TO ABOVE ADD 1 QT. CLEANED C/P'S ON OIL PRESSURE S/W AND TRANSMITTER NO FIX. SWAPPED OIL PRESSURE GAUGE IN FLT DECK NO FIX. INSTALLED BACK IN ORIGINAL POSITION. (MECHANIC IN SYR SHORT SINGED AT THE LOG BOOK AT THIS POINT) REMOVED AND REPLACED PRESSURE TRANSMITTER GROUND RAN A/C OPS CHECK AND LEAK CHECK GOOD IAW 71-00-02. PART NUMBER TO F OLLOW. 2 H 7 2 4T 4 T RT A13NM E20NE 2007071800179 20070718 00179 NM 2007 7 18 AALA20071238 1 20070704 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 387AM 27184 MIA - OVERHEAD EMERGENCY LIGHTS AT SEATS 37H AND 39H INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS A T SEATS 37H TO 39H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007071800186 20070718 00186 NM 2007 7 18 ZZDA070605196 1 20070605 A 5322 SHEAR TIE BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT BS 1022 SHEAR TIE. INSTALLED SHEAR TIE ON STA 1022 BETWEEN L 30 AND 26L AS PER B717 SRM 51-41-02 AND SRM 51-41-05. MATERIAL USED 7075-T6 .050 AND 7075-T6 0.071. 2 L 7 2 4F TR A6WE 2007071800206 20070718 00206 SO 2007 7 18 GUUA06280701 1 20070628 A 3350 BULB EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE EMERGENCY LIGHT BROKEN A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 280AS 722 120231 AT SCHEDULED MAINTENANCE, DISCOVERED LT AFT EMERGENCY LIGHT BULB BROKEN OFF IN SOCKET. REPLACED LT AFT EMERGENCY LIGHT ASSEMBLY. 2 L 7 2 4T 4 T RT A31SO E20NE 2007071800216 20070718 00216 NM 2007 7 18 ZZDA070619191 1 20070619 A 5330 DOUBLER BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 AFT CARGO COMPARTMENT REAR LAVATORY DUMP DOUBLER CORROSION ON LT LOWER EDGE FROM STA 1022 TO 1037 AND BETWEEN LONGERON 2 3 TO LONGERON 25. INSTALLED REAR LAVATORY DUMP DOUBLER AT AFT CARGO COMPARTMENT STA 1022 TO 1037 AND BETWEEN LONGERON 2 3L AND LONGERON 25L AS PER B717 SRM 51-41-02 AND EA 17-53-00534 IR. MATERIAL USED 2024-T3 .090. 2 L 7 2 4F TR A6WE 2007071800245 20070718 00245 CE 2007 7 18 AMWA15036C 1 20070710 A 5730 1181100152 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT WING CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 155ZV UE155 FRICTION CHAFFING CREATED WORN SEGMENTS ON THE RT ENGINE NACELLES. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SH APE. DEPTH VARIED AS INDICATED ON THE REPAIR AUTHORIZATION. REPAIRED IAW ENGINEERING REPORT NR 6772-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007071800248 20070718 00248 WP 2007 7 18 CNMA20070002 1 20070107 A 2697 WIRE HARNESS DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 ENGINE DAMAGED A CNMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 49082 47927 ENG NR 3 FIRE WARNING LOOP A AND B ILLUMINATED AFTER TAKE OFF. EXTINGUISHED AT THRUST REDUCTION. REPLACED WIRE HARNESS IN NR 3 ENG IAW MM 20-30. OPS CK NORM. C/W INSP OF NR 3 ENG IAW 07-005 ENG RUN UP, OPS CHECK NORMAL IAW JRH. 2 L 7 3 4F 4 F A22WE E23EA 2007071800251 20070718 00251 WP 2007 7 18 CNMA20070011 1 20070612 A 5210 L3082511 MOTOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE L2 DOOR BYPASSING A CNMA K NONE L NO TEST IN INSP/MAINT 1 SW 07 630AX 46596 L-2 DOOR AIR MOTOR IS BYPASSING AIR INTERNALLY DURING OPS CHECK. 2 L 7 3 4F 4 F A22WE E23EA 2007071800258 20070718 00258 WP 2007 7 18 ASAA0781865 1 20070708 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 MID PIT BILGE DRAIN AREA SKIN CORRODED. REMOVED DAMAGED AREA OF SKIN. FABRICATED DOUBLER AND FILLER, INSTALLED IAW SRM 51-10-3 PG 24 AND ASA EA 5330 02220. 2 L 7 2 4F RT A6WE 2007071800259 20070718 00259 NM 2007 7 18 2007UALA01936 1 20070610 A 2163 2202450 SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN TEMP STUCK A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 550UA 25398 CABIN TEMPERATURE DIFFICULT TO CONTROL, CANNOT WARM UP THE CABIN & COCKPIT. INSPECTED AND CLEANED CABIN AND FLT DECK TE MP SENSORS AND EVALUATE TEMP CONTROL SYSTEM AS REQUIRED. REPAIRED LARGE AIR LEAK AT JOINT BETWEEN ACM AND PREHEATER IN LT PACK. REPLACED RT PACK AC COMP OUT SENSOR AND RT PACK TEMP SENSOR PACK OUT TEMPS NOW WITHIN LIMITS. DURING T/S FOUN D RT PACK STUCK IN LOW FLOW. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071800276 20070718 00276 NM 2007 7 18 UIEA200700268 1 20070715 A 3250 CONNECTOR BOEING 747 74747UF 1384812 NM NLG STEERING DISCONNECTED A UIEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 412MC 30559 RTO EICAS MSG "CONFIG GEAR STR" WITH HORN AND LIGHTS. SUSPECT WARNING IS DUE TO BODY GEAR STEERING SYS MSG MEL 32-53-2 APPLIES. MAINTENANCE PROCEDURE CARRIED OUT. ELECTRICAL CONNECTORS OF BOTH STEERING ACTUATORS ON RT BODY GEAR DISCONNEC TED AND STOWED. ITEM DEFERRED. 2 L 7 4 4F RT A20WE 2007071800281 20070718 00281 NM 2007 7 18 2007UALA02422 1 20070705 A 5320 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 FWD ENTRY DOOR CUTOUT, UPPER AND LOWER HINGE CUTOUTS CRACKED OUT OF FASTENER HOLES. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. MFG'D & INSTALLED 2EA STRUCTURAL FILLER & DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071800305 20070718 00305 EA 2007 7 18 QXEA200701111 1 20070622 A 5410 FRAME CNDAIR CL600 CL6002C10 1390015 EA RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 C3 OKC - RIGHT LOWER TRANS COWL CENTER FRAME CRACKED ON OUTBOARD SIDE. REPAIRED IAW REO670-54-21-814. 2 L 7 2 4F RT A21EA 2007071800308 20070718 00308 NM 2007 7 18 2007UALA02435 1 20070706 A 3350 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 OVERWING RIGHT EMERGENCY LIGHT 2ND FROM BOTTOM 1 BULB INOP. [07-27-07] REPLACED FUSE ON BATTERY CHARGER. OP CK NOR MAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071800314 20070718 00314 NM 2007 7 18 2007UALA02444 1 20070706 A 4920 APU BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SHUTDOWN A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 674UA 29242 APU AUTO SHUTDOWN 3 TIME AT GATE. [07-27-07] REPLACED APU BATTERY PRECAUTIONARY DUE TO BAT VOLTS NOTED AT 16VDC DU RING CRANKING. INSTALLED A NEW ENGINE CONTROL UNIT DUE TO ORIG BOX DOES NOT RECORD OR CAPTURE FAULTS OF AUTOSHUTDOWN. ALSO, REPLACED OIL COOLER AND BY-PASS VALVE PER MM. FOUND GEARBOX SHUTOFF VALVE PNEU LINE LOOSE. APU OPS CHKS GOOD D URING CREW VERIFICATION FLT. APU STARTED AND OPS CHKS NORMAL AT FLT LEVEL 370 ON TWO DIFFERENT FLIGHTS. AIRCRAFT OK FO R SERVICE AND RETURNED TO ETOPS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071800328 20070718 00328 NM 2007 7 18 2007UALA02454 1 20070706 A 2730 ELEVATOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE RIGHT FAILED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 845UA 1585 RIGHT ELEVATOR FAILED ELEVATOR DAMPING TEST. REPLACED ELEV ACTUATOR 34CE2, RETEST- TESTED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071800329 20070718 00329 SO 2007 7 18 N93A07072007A 1 20070707 A 2842 057024001 PROBE GULSTM GIVX GIVXG450 3980205 SO RROYCE TAY TAY65154 EU FUEL QTY FAULTED E N93A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 13 440QS 4025 LOW FUEL INDICATION AFTER TAKEOFF. REMOVED AND REPLACED FUEL LEVEL LOW SENSOR PROBE. 2 L 7 2 4F 4 F RT A12EA E25NE 2007071800335 20070718 00335 CE 2007 7 18 DXTA200702316 1 20070704 A 3260 327 BULB CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE MLG INDICATOR INOPERATIVE E DXTA A UNSCHED LANDING P NO WARNING INDICATION LD LANDING 1 GL 07 644QS 1948 5605582 WHEN LOWERING GEAR FOR LANDING, NOSE LIGHT DIDN'T ILLUMINATE. RED UNSAFE LIGHT WAS OUT AND BOTH MAIN LIGHT ILLUMINATED. PERFORMED CHECKLIST PROC. AND ACTIVATED BLOW DOWN SYSTEM. REMOVED AND REPLACED BOTH LIGHT BULBS FOR NOSE LIGHT INDICATI ON. OPS CHECKS GOOD. BLED LANDING GEAR SYSTEM AND RESAFTIED BOTTLE, SERVICED BOTTLE IAW MM 32-30-00, 33-10-02, 12-13-01. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007071800337 20070718 00337 EU 2007 7 18 2007UALA02457 1 20070708 A 3350 32145410321431 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 421UA 500 EMERGENCY LIGHTS TEST FAILS, -EPSU EXT LOADS EMER L- MESSAGE DISPLAYED. REPLACED POWER SUPPLY AND BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071800338 20070718 00338 CE 2007 7 18 452037052807 1 20070528 A 7797 30607572 WIRE HARNESS LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE7312 01518 WP ITT INDICATOR UNKNOWN E J7SA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 05 611FX 2037 P116646C PILOT REPORTED THAT THE LT ITT EXCEEDED 1014 DEGREES TWICE AND THE PILOT PERFORMED AN IN-FLIGHT SHUTDOWN. BOTH N1 INDICA TIONS WERE MATCHED. BOTH FF INDICATIONS WERE MATCHED. PILOT FURTHER REPORTED THAT THE LT ITT INDICATION FOLLOWING ENGINE SHUTDOWN WAS 940 DEGREES AND REMAINED SO UNTIL TOUCHDOWN. MX REVIEWED THE ECTM DOWNLOAD AND THE DEEC SAW THE ITT OUT OF RANGE. HE RECOMMENDS REPLACING THE ENGINE HARNESS PN 3060757-1 OR -2. ENGINE HARNESS REPLACED AND GROUND POWER RUNS PE RFORMED. NO FURTHER DEFECTS NOTED. 2 L 7 2 4F 4 F RT T00008WI E6WE 2007072600009 20070726 00009 NM 2007 7 26 AWXA200700860 1 20070718 A 2100 CIRCUIT BOARD BOEING 757 7572S7 1384962 NM COOLING SYSTEM FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 905AW 23567 PHX - OTHER - LOG NR 7809150 - CREW REPORTED EQUIPMENT SMOKE TEST STATUS MESSAGE ILLUMINATED. MX REPLACED THE EQUIPMENT COOLING CARD M10650 IAW MM 21-58-20-4. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2007071800360 20070718 00360 NM 2007 7 18 2007UALA02472 1 20070706 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 UPPER FUSELAGE ATC ANTENNA HAD A DEEP SCRIBE IN SKIN FOUND AFTER ANTENNA REMOVED. [07-27-07] MAJOR REPAIR: INSTALLE D A DOUBLER PER EA 1070451 REV IR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071800363 20070718 00363 EA 2007 7 18 TRAX200700938 1 20070628 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 870AS 7530 PAX DOOR FOLDING STEP, HALF IS CORRODED. 2 L 7 2 4F RT A21EA 2007071800372 20070718 00372 EA 2007 7 18 TRAX200700956 1 20070706 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 FLOOR SUPPORT BEAM UPPER CAP BETWEEN FS 589.00 AND FS 621 AT LBL-27 IS CORRODED AT NUT PLATE HOLES. 2 L 7 2 4F RT A21EA 2007071800374 20070718 00374 NM 2007 7 18 SWAA073368 1 20070709 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 441WN 29837 EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007071800394 20070718 00394 NM 2007 7 18 QXEA200701121 1 20070711 A 2741 CONTROL UNIT BOMBDR DHC8 DHC8402 1390042 NM PITCH TRIM FAULTED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 425QX 4039 PDX FLIGHT NR 2356: PITCH TRIM CAUTION MESSAGE. AIRCRAFT RETURNED TO GATE. MAINTENANCE FOUND CDS REPORTS FCECU FAILURE NR 67. PERFORMED FAULT CONFIRMATION IAW FIM 37-30-00-810-803. FAULT CLEARED. NO FURTHER DEFECTS FOUND. NO PARTS REPL ACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071800396 20070718 00396 WP 2007 7 18 07FDEA02468 1 20070713 A 5322 SHEAR TIE DOUG DC10 DC1010F 3022111 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 CTR CARGO COMPT TUNNEL ON SHEAR CLIP FOUND CRACK 0.75" LONG. REPAIRED SHEAR CLIP IAW SRM 53-30-00 FIG 10 VOL 1. 2 L 7 3 4F A22WE 2007071800397 20070718 00397 WP 2007 7 18 07FDEA02469 1 20070713 A 5730 SKIN DOUG DC10 DC1010 3022110 WP ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 RT WING SLATS DEEP WEAR ON EXT SKIN ON DROOPED L/E OUTBOARD SIDE. REPAIRED AREA IAW SRM 57-10-00 VOL 1 PAG 39. 2 L 7 3 4F A22WE 2007071800398 20070718 00398 WP 2007 7 18 07FDEA02470 1 20070713 A 5101 STRUCTURE DOUG DC10 DC1010F 3022111 WP ZONE 100 UNKNOWN A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 68052 47806 EXISTING DOUBLER EXTERNAL FUSELAGE. REPAIRED AREA IAW SRM 53-20-00 FIG 6 VOL 1. 2 L 7 3 4F A22WE 2007071800399 20070718 00399 NM 2007 7 18 07FDEA02471 1 20070713 A 5315 65187451 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 STA 870 FLOORBEAM HAS CORROSION ON UPPER SURFACE AT RBL12 DOT 17. REMOVED CORROSION, ORIGINAL THICKNESS .690, REMAINING .630 REMOVED .060 TOOL NR IN17-1458 DUE 4-24-08 IAW SRM 51-10-1, FOUND TO BE IN LIMITS, ROTO PEENED, CHECKED FOR CRACK S, TREATED, PRIMED, APPLIED BMS 3-23 CORROSION INHIBITOR REF FEDEX EA 7-5310-113048, SRM 51-10-2 AND SOPM 20-10-03. REM OVED AND INSTALLED A FASTENERS THROUGH PULLEY BRACKET IAW SRM 51-03-2. INSTALLED 2 EA NUT PLATES IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007071800401 20070718 00401 WP 2007 7 18 07FDEA02473 1 20070713 A 5347 WSP04145 SEAT TRACK DOUG DC10 DC1010F 3022111 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 MAIN CABIN SEVERE EXFOLIATION CORROSION ON SEAT TRACK. INSTALLED NEW TRACK AND SPLICE IAW SRM 53-70-00 FIG 1 VOL 1. 2 L 7 3 4F A22WE 2007071800403 20070718 00403 NM 2007 7 18 SWAA073374 1 20070709 A 5315 6545410145 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 662, LBL 0.07. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007071800404 20070718 00404 NM 2007 7 18 SWAA073364 1 20070708 A 5330 6545765 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 516D, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007071800405 20070718 00405 NM 2007 7 18 SWAA073382 1 20070708 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 FUSELAGE SKIN CRACKED AT BS 520, STR 8L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007071800406 20070718 00406 NM 2007 7 18 SWAA073362 1 20070708 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT COOLING DUCT EXHAUST BS 378. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2007071800407 20070718 00407 NM 2007 7 18 SWAA073363 1 20070708 A 5330 6545772 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CHAFED BETWEEN BS 860 AND BS 887, STR 1. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2007071800408 20070718 00408 NM 2007 7 18 SWAA073373 1 20070709 A 5311 6545805 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007071800409 20070718 00409 NM 2007 7 18 SWAA073365 1 20070708 A 5322 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 16R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007071800410 20070718 00410 NM 2007 7 18 SWAA073372 1 20070709 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007071800411 20070718 00411 NM 2007 7 18 SWAA073376 1 20070709 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071900001 20070719 00001 EA 2007 7 19 TRAX200700921 1 20070703 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 RIGHT O/B FUSELAGE STA 280 CLIP IS CRACKED. REMOVED 1EA CRACKED ANGLE CLIP AT FUSELAGE STA 280 RBL 9. WORK DONE IAW CR J 200 SRM 51-42-21. SUPPLEMENTAL - SDR CLOSED 07/10/07. 2 L 7 2 4F RT A21EA 2007071900005 20070719 00005 WP 2007 7 19 07FDEA02477 1 20070713 A 5720 ARB43135 STIFFENER DOUG DC10 DC1010F 3022111 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 DURING PERFORM OF OAN J/C 0600B620-2JR, FOUND NR 2 CRACKS 0.50" LONG ON STIFFENERS OF L/E ACCESS PANEL 617CT. REPAIRED STIFFENERS IAW SRM 57-10-00 VOL 1 FIG 10. 2 L 7 3 4F A22WE 2007071900006 20070719 00006 WP 2007 7 19 07FDEA02478 1 20070713 A 5311 FRAME DOUG DC10 DC1010F 3022111 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 AVIONIC COMPT ON FRAME FOUND SEVERE CORROSION WITH EXFOLIATION. REPAIRED FRAME IAW SRM 53-30-00 PAGE 13 FIG 4 VOL 1. 2 L 7 3 4F A22WE 2007071900008 20070719 00008 WP 2007 7 19 07FDEA02480 1 20070713 A 5311 FRAME DOUG DC10 DC1010F 3022111 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 AVIONIC COMPT ON FRAME RT SIDE FOUND CRACK. REPAIRED FRAME IAW SRM 53-30-00 VOL 1 FIG 5. 2 L 7 3 4F A22WE 2007071900009 20070719 00009 WP 2007 7 19 07FDEA02481 1 20070713 A 5313 LONGERON DOUG DC10 DC1010F 3022111 WP BS 1501-1521 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 LONGERON 51L IN CLG AREA BETWEEN STA 1501 AND 1521 CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW MD10-10 S RM 53-00-01 VOL 1 FIG 1A. REMOVED AND REPLACED LONGERON SECTION IAW MD10-10 SRM 53-00-01 FIG 9 VOL 1, AND 51-35-01 VOL 2. FABRICATED LONGERON SECTION AND REPAIR SPLICES IAW MD10-10 SRM 53-00-010 FIG 9 VOL 1 AND 51-21-01 VOL 2. 2 L 7 3 4F A22WE 2007071900010 20070719 00010 WP 2007 7 19 07FDEA02488 1 20070716 A 5730 ARC1113501 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 UPON REMOVAL OF LOWER SKIN ON LT AILERON FOUND TOP SKIN TO BE CORRODED UNDER FINGER DOUBLERS AND T/E WEDGE. REMOVED AND REPLACED SKIN IAW DC-10/MD-10 SRM 51-35-01 VOL II AND 51-35-02 VOL II. 2 L 7 3 4F A22WE 2007071900011 20070719 00011 WP 2007 7 19 07FDEA02489 1 20070716 A 5730 ARC1113501 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 500 CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 UPON REMOVAL OF LOWER SKIN ON LT AILERON FOUND TOP SKIN TO BE CORRODED UNDER FINGER DOUBLERS AND T/E WEDGE. REMOVED AND REPLACED SKIN IAW DC-10/MD-10 SRM 51-35-01 VOL II AND 51-35-02 VOL II. 2 L 7 3 4F A22WE 2007071900012 20070719 00012 WP 2007 7 19 07FDEA02490 1 20070716 A 5313 AYB70201 LONGERON DOUG DC10 DC1010F 3022111 WP ZONE 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CORROSION ON LONGERON END FITTING AT STA 1521, L48R CLG WHEEL/WELL. REMOVED AND REPLACED LONGERON END FITTINGS L48R IAW DC-10/MD-10 SRM 51-35-01 VOL. II. 2 L 7 3 4F A22WE 2007071900013 20070719 00013 WP 2007 7 19 07FDEA02491 1 20070716 A 5330 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 700 CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CLG WHEEL WELL CAVITY, CORROSION ON FUSELAGE SKIN INTERIOR BETWEEN LONGERON 50R AND 49R, STA 1501 TO 1520. REMOVED AND REPLACED L51R END FITTINGS IAW DC-10/MD-10 SRM 51-35-01 VOL II. 2 L 7 3 4F A22WE 2007071900014 20070719 00014 WP 2007 7 19 07FDEA02492 1 20070716 A 5320 AEA02763 INTERCOSTAL DOUG MD10 MD1010F 3022112 WP BS 1381-1401 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CLG WHEEL WELL CAVITY CORROSION ON INTERCOSTAL ABOVE LONGERON 52 R STA 1381 TO 1401. REMOVED AND REPLACED INTERCOSTAL I AW DC/MD-10 SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2007071900015 20070719 00015 WP 2007 7 19 07FDEA02493 1 20070716 A 5313 AYB70201 LONGERON DOUG MD10 MD1010F 3022112 WP ZONE 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 CLG WHEEL WELL CAVITY CORROSION ON LONGERON END FITTING STA 1501 TO STA 1521 LONGERON 51L TO 52L REMOVED AND REPLACED LO NGERON END FITTING L52R IAW DC/MD-10 SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2007071900016 20070719 00016 WP 2007 7 19 07FDEA02494 1 20070716 A 5313 LONGERON DOUG MD10 MD1010F 3022112 WP ZONE 700 CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 FOUND CORROSION ON LONG END FITTINGS AT STA 1521 LONG 48L CLG WHEEL WELL. REMOVED AND REPLACED L48L END FITTINGS IAW DC /MD-10 SRM 51-33-01 VOL. II. 2 L 7 3 4F RT A22WE 2007071900017 20070719 00017 EA 2007 7 19 TRAX200700926 1 20070704 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 FWD CENTER FLOORBOARD ANGLE JUST FWD OF STA 280 CROSSBEAM HAS SURFACE CORROSION PER MTC. 2 L 7 2 4F RT A21EA 2007071900018 20070719 00018 SO 2007 7 19 SIMA200719404 1 20070712 A 5320 12315660401 HOLDER EMB 135 EMB135KL 3260302 SO COCKPIT BURNED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 830AE 12229 145615 CAPTAIN CHART HOLDER SMOKES WITH A VISIBLE GLOW. REMOVED AND REPLACED CHART HOLDER IAW EMB 25-15-11. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900019 20070719 00019 SO 2007 7 19 SIMA200719417 1 20070705 A 5347 14532606017 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 717AE 15889 5000 145272 LEFT OUTBORAD SEAT TRACK CORRODED BETWEEN FRAMES 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERA TIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900020 20070719 00020 SO 2007 7 19 SIMA200719418 1 20070705 A 5347 14532606015 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 717AE 15889 5000 145272 LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 36 TO 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERA TIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE 2 L 7 2 4F RT T00011AT 2007071900021 20070719 00021 WP 2007 7 19 07FDEA02482 1 20070713 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 362FE 48261 CORROSION POSSIBLE ON FUSELAGE SKIN CORROSION LIMITED TO LONGERON DAMAGE WHICH WAS REPAIRED PER 53-10-00 VOL 1 OF MD10-1 0. 2 L 7 3 4F RT A22WE 2007071900024 20070719 00024 EA 2007 7 19 TRAX200700964 1 20070706 A 5220 ESCAPE HATCH CNDAIR CL600 CL6002B19 1900309 EA CREW ESCAPE FAILED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 832AS 7243 CREW ESCAPE HATCH FAILS OPEN AND CLOSE FUNCTIONAL TEST. [07-26-07] REMOVED HATCH, LUBED WITH, D.C. 33. REPLACED AND PERFORMED FUNCTIONAL TEST. NO DECREPANCIES FOUND AT THIS TIME, IAW CRJ 200 AMM . 2 L 7 2 4F RT A21EA 2007071900025 20070719 00025 EA 2007 7 19 TRAX200700965 1 20070706 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 FLOOR SUPPORT BEAM UPPER CAP BETWEEN FS 589.00 AND FS 621 AT RBL 27 IS CORRODED AT NUT PLATE HOLES. [07-20-07] COMPLI ED WITH EC/TC REO 601R-53-00-214. 2 L 7 2 4F RT A21EA 2007071900026 20070719 00026 NM 2007 7 19 SWAA073370 1 20070709 A 5312 665458197 PRESSURE PANEL BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND LEFT NLG W/W PRESSURE WEB CRACKED AT BS 246, WL 170. REPAIRED PRESSURE WEB PER SWA E A. 2 L 7 2 4F RT A16WE 2007071900027 20070719 00027 2007 7 19 SWAA073380 4 20070709 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071900028 20070719 00028 GL 2007 7 19 SWAA073369 2 20070708 A 7200 GE7482 ENGINE BOEING 737 7373Q8 1384670 NM CFMINT CFM56 CFM563B1US GL RIGHT VIBRATION A SWAA E ENGINE SHUTDOWN E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 29 662SW 23255 858645 INFLIGHT SHUTDOWN/DIVERSION. NR 2 ENGINE EXPERIENCED COMPRESSOR STALLS AND EXCESSIVE VIBRATION. SHUTDOWN NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071900029 20070719 00029 NM 2007 7 19 SWAA073366 1 20070709 A 3350 PH22300L STRIP BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 13 ABC. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007071900030 20070719 00030 NM 2007 7 19 KCSA071209 1 20070710 A 5730 SKIN BOEING 747 747146 1384905 NM RT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 LOWER RIGHT WING SKIN FWD OF FRONT SPAR WS 1308.00 IS CORRODED AT STIFFENER PAD. 2 L 7 4 4F RT A20WE 2007071900031 20070719 00031 NM 2007 7 19 BB07051 1 20070710 A 3350 LIGHT BOEING 757 7572B7 1384964 NM CABIN MISSING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934UW 27200 MAINTENANCE FOUND THE L4 DOOR EMERGENCY LIGHT MISSING. REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F RT A2NM 2007071900032 20070719 00032 NM 2007 7 19 CALA0700343 1 20070710 A 5322 65465677 SHEAR TIE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND SHEAR TIE CORRODED AT STA 1006, S27R. THE SHEAR TIE WAS REMOVED AND REPLACED IAW MM 51-40-02. 2 L 7 2 4F RT A16WE 2007071900034 20070719 00034 NM 2007 7 19 CALA0700345 1 20070709 A 5347 151W6203 SEAT TRACK BOEING 777 777224 1385225 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76010 29480 INSPECTION FOUND SEAT TRACK CORRODED AT STA 1460-1535, LBL 74. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52, REPAIR 3, FIGURE 202. 2 L 7 2 4F RT T00001SE 2007071900035 20070719 00035 NM 2007 7 19 CALA0700346 1 20070711 A 5230 6546921530 SKIN 6546921528 BOEING 737 7373T0 1384582 NM FWD CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59302 1059 23353 INSPECTION FOUND A CRACK AT LIGHTENING HOLE IN THE INNER SKIN OF THE FORWARD CARGO DOOR. THE DOOR SKIN WAS REPAIRED IAW ECRA 5230-01797. 2 L 7 2 4F RT A16WE 2007071900036 20070719 00036 NM 2007 7 19 NOCA13707 1 20070705 A 2750 285N001140 FSEU BOEING 757 75728A 1384976 NM NR 2 FAULTY A NOCA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 754NA 29381 FLAP/SLAT ELEC EICAS MESSAGE ON STATUS PAGE. FOUND NR 2 FSEU AT FAULT. REMOVED AND REPLACED NR 2 FSEU AS PER MM 27-51- 01, OPS CHECK OK. 2 L 7 2 4F RT A2NM 2007071900037 20070719 00037 EA 2007 7 19 TRAX200700919 1 20070703 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 753EV 10169 ASD EXTERIOR HANDLE CRACKED. REMOVED AND REPLACED EXTERIOR HANDLE IAW 700 AMM 52-11-03. SUPPLEMENTAL - SDR CLOSED 07/1 1/07. 2 L 7 2 4F RT A21EA 2007071900039 20070719 00039 NE 2007 7 19 ARWA20070703 2 20070710 A 7532 563883 BLEED VALVE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 3 ENGINE MALFUNCTIONED A ARWA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 19 661AV * 1361 45969 671063 ABORTED TAKE-OFF AT 118 KTS, UNABLE TO MAINTAIN TAKEOFF POWER WITHOUT EXCEEDING NR 3 ENGINE EGT LIMIT. REMOVED NR 3 ENG INE SURGE VALVE IN ACCORDANCE WITH M/M 75-30-3. INSTALLED NEW COMPRESSOR BLEED VALVE AND CONTROL IN ACCORDANCE WITH M/M 75-30-3. OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH M/M 71-00-00. 2 L 7 4 4F 4 F 4A25 1E8 2007071900040 20070719 00040 SO 2007 7 19 SIMA200719408 1 20070621 A 5347 14000486009 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 811AE 13526 5000 145529 RIGHT INBORAD SEAT TRACK CORRODED BETWEEN FRAMES 23 TO 28. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERA TIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900041 20070719 00041 SO 2007 7 19 SIMA200719411 1 20070621 A 5347 14530658005 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 811AE 13526 5000 145529 RIGHT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 36 TO 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERA TIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900048 20070719 00048 NM 2007 7 19 07FDEA02485 1 20070716 A 5311 6516339 FRAME BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 AFT PIT STA 970 SHEAR TIE CORRODED BETWEEN STRINGER 25R-26R RBL 17-22 REMOVED CORRRODED SHEAR TIE. FAB`D REPAIR SHEAR T IE AND INSTALLED PER SRM 53-10- 4 FIG 11 PAGE 43 THR 45. 2 L 7 3 4F A3WE 2007071900049 20070719 00049 NM 2007 7 19 07FDEA02486 1 20070716 A 5730 6521657254 PANEL BOEING 727 727227 1384078 NM ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 RT WING OB TE PANEL 8855, LWR SKIN HAS LARGE AREA OF DISBOND IN CENTER OF PANEL. INSTALLED NEW PANEL IAW SRM 51-30-02 P G 1 AND PG 13-14. 2 L 7 3 4F A3WE 2007071900050 20070719 00050 NM 2007 7 19 07FDEA02487 1 20070716 A 5230 DEPRESSOR BOEING 727 727227 1384078 NM CARGO DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 FWD LWR CARGO DOOR LOWER EDGE SEAL DEPRESSOR I/B SURFACE IS GOUGED IN 2 PLACES 26" AND 33" FROM AFT END OF DOOR. REPLAC ED SEAL DEPRESSOR IAW SRM 52-30-1. 2 L 7 3 4F A3WE 2007071900051 20070719 00051 GL 2007 7 19 07FDEA02439 2 20070710 A 7320 MEC DOUG MD10 MD1010F 3022112 WP GE CF6 CF66D 30020 GL NR 1 ENGINE FAILED A FDEA D RETURN TO BLOCK X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 377FE 56674 56674 47965 451553 NR 1 ENGINE FLAMED OUT ON ROLLOUT. FIRST INDICATION WAS GEN 1 OFF FOLLOWED BY AIR SYS 1 LOW PRESS. REMOVED AND REPLACE D FUEL PUMP AND MEC. 2 L 7 3 4F 4 F RT A22WE E23EA 2007071900052 20070719 00052 NM 2007 7 19 07FDEA02444 1 20070712 A 5315 651594065 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 STA 740 FLOOR SUPPORT BET BL 0 AND RBL 24 HAS CORROSION AT NUTPLATES HOLES, AND CORROSION BETWEEN BEAM AND FLOOR SUPPORT PLATE AND ALSO A SCRIBE LINE ON TOP SURFACE. REMOVED AND REPLACED FLOOR SUPPORT STRIP REF 51-30-2. 2 L 7 3 4F RT A3WE 2007071900054 20070719 00054 NM 2007 7 19 07FDEA02446 1 20070712 A 5313 655623622 STRINGER BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD CARGO AREA, STA 650 TO 655, AT STR 28L ABOUT LBL7 STRINGER 28L IS CORRODED. STRINGER SECTION STA 640 11" TO 680 REP LACED ON SNRM N00598. REMOVED STRINGER SECTION FROM STA 680-STA 720 AND INSTALLED NEW SECTION. THE CORRODED STRINGER S ECTION WAS OUT OF LIMITS. REF SRM53-10-3/PAGES 1-4B/FIGURE NR 1. 2 L 7 3 4F RT A3WE 2007071900055 20070719 00055 NM 2007 7 19 07FDEA02447 1 20070712 A 5313 655623632 STRINGER BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD CARGO AREA, STA 665 TO 675, STR 28L ABOUT LBL 7, STRINGER IS CORRODED REMOVED STRINGER SECTION FROM STA 640 11" TO S TA 680 / STR 28L. THE SECTION REMOVED WAS OUT OF LIMITS. INSTALLED NEW SECTION REF SRM 53-10-3/FIGURE NR 1/ PAGES 1- 4B. 2 L 7 3 4F RT A3WE 2007071900058 20070719 00058 2007 7 19 07FDEA02390 2 20070707 A 7261 MANIFOLD AIRBUS 310 A310203 3930313 EU NR 1 BEARING FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 414FE 400 WHILE CLIMBING OUT OF MEM AT APPROX 35,000 AN ODOR RESEMBLING PAINT THINNER WAS DETECTED IN THE COCKPIT. NO ODOR WAS DE TECTED IN THE CABIN BUT ALMOST IMMEDIATELY THE MID 2 LOOP B CARGO DETECTOR FAULTED FOLLOWED BY A MID 2 SMOKE INDICATION. AN EMERGENCY WAS DECLARED FOLLOWED BY A RETURN TO MEM. FOUND OIL LEAKING AT FAN BLADES AND HUB INDICATIVE OF A FAILED NR 1 BEARING MANIFOLD ASSEMBLY SEAL. REMOVED SPINNER AND MANIFOLD ASSEMBLY AND FOUND REAR SEAL OF MANIFOLD DEFECTIVE. REMOVED AND REPLACED NR 1 BEARING MANIFOLD ASSEMBLY FWD AND AFT SEALS IN REF TO A310-200 AMM 72-21-00-8 04. RAN NR 1 E NG AT 40 PERCENT N1 FOR APPROXIMATELY 20 MIN IN REF TO JRH W/NO LEAKS NOTED. 2 L 7 2 4F RT A35EU 2007071900062 20070719 00062 NM 2007 7 19 07FDEA02497 1 20070716 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM NLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 NOSE LANDING GEAR RIGHT TRUNNION FITTING FOUND CRACKED. [08-03-07] CARRIED OUT REPAIR AS PER SRM 53-40 -00 FIGURE 23 VOLUME I. REPETITIVE INSPECTION TO BE CARRIED OUT NOT EXCEEDING 1,500 LANDING INTERVALS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007071900065 20070719 00065 2007 7 19 200707111 4 20070709 A 3100 70244401901 POWER SUPPLY EMB ERJ170 ERJ170100SE 3260406 EU MAU FAILED A UHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 644RW 17000061 FLIGHT 7638 MSY TO ORD WHILE ON CLIMBOUT THE CREW ENCOUNTERED SOME LIGHT TURBULENCE AND RECEIVED -CRG AFT SMOKE- WARNING , -AVNX MAU 3B FAIL-, -SPOILER FAULT- CAUTIONS, AND -CMF1 FAIL- ADVISORY EICAS MESSAGES SIMULTANEOUSLY. THE CREW RAN TH E QRH FOR AFT CARGO SMOKE. THE AFT CARGO SMOKE LIGHT EXTINGUISHED. NO UNUSUAL SMELLS AND NO SMOKE NOTED IN THE CABIN. THE CREW RETURNED TO THE MSY, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE MAU3 NR 1 PO WER SUPPLY. 2 L 7 2 4F RT A56NM 2007071900066 20070719 00066 2007 7 19 UPS07150141 4 20070710 A 2565 WARNING SYSTEM AIRBUS A300 A300F4622R 3930360 EU EVAC SLIDE MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 130UP 0814 INSPECTION TYPE:N/A WHEN DISARMING SLIDE UPON BLOCK IN, THE HORN DID NOT WORK WHEN BUTTON PRESSED. LIGHT DID NOT OPERAT E. PERFORMED ADJ/TEST OF ESCAPE SLIDE WARNING SYSTEM. COULD NOT DUPLICATE. SYSTEM OPS NORMAL PER MM 52-73-00-5. 2 L 7 2 4F RT A35EU 2007071900067 20070719 00067 NM 2007 7 19 UPS07450142 1 20070710 A 3251 O-RING BOEING 747 747200 1384847 NM STEERING SYS CUT A IPXA H DEACTIVATE SYST/CIRCUITS K FLUID LOSS AP APPROACH 1 SO 01 521UP 21944 INSPECTION TYPE:N/A HYDRAULIC SYSTEM NR 1 FLUID LOSS IN FLIGHT. FOUND CUT O-RING ON LEFT NOSE WHEEL STEERING ACT TRANSF ER TUBE. REPLACED SEALS IAW 32-51-05. OPS AND LEAK CHECKS GOOD DUE TO HYD FLUID LOSS. NR 1 EDP REMOVED AND REPLACED I AW MM 29-11-05. OPS AND LEAK CHECKS GOOD. CASE DRAIN AND PRESS FILTERS REPLACED. OPS AND LEAKS CHECK GOOD. 2 L 7 4 4F RT A20WE 2007071900068 20070719 00068 NM 2007 7 19 UPS07550143 1 20070709 A 2560 ESCAPE REEL BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 445UP 27390 INSPECTION TYPE:N/A 2 ESCAPE REELS HAVE TAMPER RESISTANT TAPE LOOSE. BOTH OBSERVERS SEATS INOP PER DMP. REELS IN PFM. REPLACED MISSING INTERTIAL ESCAPE REELS 2EA, REMOVED AND REPLACED IAW MM 25-61-02-2. REMOVED UNITS PREVIOUSLY STORED I N PFM. 2 L 7 2 4F RT A2NM 2007071900070 20070719 00070 NM 2007 7 19 UPS07550146 1 20070612 A 5311 146N10307 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 420UP 23907 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1520, BETWEEN S25L TO S27L. REMOVED TRANSITION PNL FOR ACCESS FR OM STA 1410-1530 LEFT AFT CARGO IAW SRM 51-40-02. PART REMOVED FLOOR PNLS FROM STA 1400-1560 IAW SRM 51-40-02. ACCOMPL ISHED ON FINAL EA 757-5360-27-A1696 AND UPS EO B757-5310-27208-A. 2 L 7 2 4F RT A2NM 2007071900071 20070719 00071 NM 2007 7 19 UPS07550147 1 20070613 A 5311 143N102471 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 420UP 23907 INSPECTION TYPE:C DENTS IN FWD CARGO FUSELAGE FRAME STA 820, BETWEEN S23L TO S25L (3EA). ACCOMPLISHED ON FINAL EA 757-5 332-27-A1689. 2 L 7 2 4F RT A2NM 2007071900072 20070719 00072 SO 2007 7 19 SIMA200719407 1 20070621 A 5347 14530659005 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 811AE 13526 5000 145529 LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 36 TO 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERAT IONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900075 20070719 00075 WP 2007 7 19 ARWA20070608 1 20070615 A 5512 SKIN DOUG DC8 DC863F 302198F WP HORIZONTAL STAB DENTED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND LT HORIZONTAL STABILIZER XH 285.00 L/E LOWER SURFACE WITH DENT. RE PAIRED L/E PLATING OF LT HORIZONTAL STABILIZER BETWEEN XFS 263 AND XH 285 IN ACCORDANCE WITH AIPSAC DRAWING NR AIPSAC-N6 61AVE-03/07, SHEET 1 TO 4, DRAWING DATE 01/08/2007. 2 L 7 4 4F 4A25 2007071900076 20070719 00076 WP 2007 7 19 ARWA20070609 1 20070615 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 260 S21L CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; FUSELAGE EXTERIOR STATION 260 L-21L SKIN WITH CORROSION. REPAIRED FUSELAGE EXTERIOR SKIN ATW FS 200 AND FS 350 AND BETWEEN L-18L AND L-24L IN ACCORDANCE WITH DRAWING NR AIPSAC-N661AV-01 /06, REVISION 0, SHEET 1 M4, DATED 01/12/2007. 2 L 7 4 4F 4A25 2007071900079 20070719 00079 NM 2007 7 19 UPS07550151 1 20070710 A 5610 WINDOW BOEING 757 75724APF 1384969 NM COCKPIT LACK OF LUBE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 413UP 23853 INSPECTION TYPE:N/A L-2 WINDOW WILL NOT CLOSE. CLEAN AND LUBE DOOR (WINDOW ASSY). CYCLE SEVERAL TIMES, OPS CHECKS NORM AL. 2 L 7 2 4F RT A2NM 2007071900081 20070719 00081 NM 2007 7 19 07FDEA02448 1 20070713 A 5315 AFA78087 FLOORBEAM DOUG MD11 MD11F 3023600 NM BS 1761 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CENTER CARGO COMPT: DOORWAY CEILING AREA MAIN DECK CARGO FLOORBEAM LOWER FLANGE AT STA 1761, X = -100 FOUND DENTED. [ 07-25-07] REPAIRED AS PER EA 1-5310-112358. 2 L 7 3 4F RT A22WE 2007071900083 20070719 00083 NM 2007 7 19 07FDEA02450 1 20070713 A 5730 6521657254 PANEL BOEING 727 727227 1384078 NM RT WING DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 RT WING O/B T/E PANEL 8855, LWR SKIN HAS LARGE AREA OF DISBOND IN CENTER OF PANEL. INSTALLED NEW PANEL IAW SRM 51-30-2 PG 1 & PG 13-14. 2 L 7 3 4F A3WE 2007071900084 20070719 00084 NM 2007 7 19 07FDEA02451 1 20070713 A 5320 65295672 PANEL BOEING 727 727227 1384078 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 UPPER MAIN DECK STA. 1176-1183 RBL 27", ARCHED FLOOR WEB CLOSURE, INBD ANGLE IS DAMAGED. REMOVED DAMAGED ANGLE, FABRICA TED NEW AND SENT FOR HEAT TREAT. TREATED AND PRIMED REF M/M 51-20-151-7. INSTALLED NEW ANGLE REF SRM 51-30-02. 2 L 7 3 4F A3WE 2007071900085 20070719 00085 NM 2007 7 19 07FDEA02452 1 20070713 A 5320 65295672 PANEL BOEING 727 727227 1384078 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 MAIN DECK ARCHED WEB BETWEEN BS 1176-1183 RBL 36" TO 47" HAS SEVERAL CRACKS AND SEPARATED COMPOSITE PATCH. REMOVED DAMA GED PART AND FABRICATED NEW FROM 2024-O .032 MATERIAL AND SENT FOR HEAT TREAT. TREATED AND PRIMED REF M/M 51-20-151-7. INSTALLED NEW PARTS REF SRM 51-30-2. 2 L 7 3 4F A3WE 2007071900086 20070719 00086 NM 2007 7 19 UPS07550153 1 20070706 A 2560 LATCH BOEING 757 75724APF 1384969 NM ESCAPE ROPE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 433UP 25464 INSPECTION TYPE:N/A COCKPIT ENTRY DOOR EMERGENCY ESCAPE ROPE POCKET DOOR LATCH BROKEN. REPLACED LATCH ASSY PER STANDARD SRM PRACTICE AND RE-INSTALLED EMERGENCY ESCAPE ROPE PER MM 25-61-04. 2 L 7 2 4F RT A2NM 2007071900087 20070719 00087 NM 2007 7 19 07FDEA02453 1 20070713 A 5311 53FX1350 FRAME BOEING 727 727227 1384078 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 FWD CARGO PIT LT SIDE BS 600 STR 21L FRAME EXTENSION CRACKED ON O/B EDGE ABOVE STR 21L. REMOVED FRAME SPLICE REF SRM 51 -30-02. FORMED NEW FRAME SPLICE USING .063 7075-O A 66693 PO NR 1008655 REF DWG 53FX1350 REV A. RECEIVED HEAT TREATED REPAIR SPLICE REF FORM 8130-3 FORM NR 2007-07-031 AND SNRM N00633. LOCATED DRILLED AND DEBURRED HOLES IN REPAIR PART RE F SRM 51-30-02. INSTALLED REPAIR SPLICE IAW SRM 51-30-02 AND DWG NR 53FX1350. 2 L 7 3 4F A3WE 2007071900088 20070719 00088 NM 2007 7 19 07FDEA02454 1 20070713 A 5320 6529567 WEB BOEING 727 727227 1384078 NM BS 1180 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 MAIN DECK ARCHED WEB AND ANGLE AT BS 1180 LBL38" WL 208 IS CRACKED. ABOVE SNRM WAS SOILED. FABRICATED NEW WEB, ANGLES AT BS 1180 LBL 38" WL 208 IAW B727 DWG 65-29567. TREATED AND PRIMED, INSTALLED IAW B727 SRM 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 2007071900089 20070719 00089 WP 2007 7 19 UPS07850149 1 20070621 A 5320 CUSP WEB DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 L21L UPPER CUSP BETWEEN STA 1160-1140 CRACKED. CUT OUT CRACKED CUSP SEGMENT AT STA 1130-1160 L21L IA W SRM 53-02-05 FIG 15A. FABRICATED AND INSTALLED REPAIR CUSP SEGMENT, DOUBLERS AND FILLERS AT STA 1130-1160 L21L IAW SR M 53-02-05 FIG 15A. 2 L 7 4 4F RT 4A25 2007071900090 20070719 00090 NM 2007 7 19 07FDEA02455 1 20070713 A 5230 SKIN BOEING 727 727227 1384078 NM CARGO DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 FWD LWR CARGO DOOR INNER SKIN IS GOUGED 2 " FROM TOP 19 " FROM AFT EDGE. BLENDED DAMAGE PER SRM 51-10-1 PG 3-4 IT WAS O UT OF LIMITS PER SRM 52-00-2 PG 1 STEP 1B, REMOVED DOUBLER AND MANUFACTURED NEW DOUBLER OUT OF 7075-T6 .050. INSTALLED ON DOOR AND INSTALLED FIELD FASTENERS AROUND DAMAGED AREA PER SRM 52-00-3 FIG 3 AND SRM 51-30-2. TREATED AND PRIMED DO UBLER PER SRM 51-10-2 DOOR WAS REMOVED AND INSTALLED ON SNRM N00361. 2 L 7 3 4F A3WE 2007071900091 20070719 00091 WP 2007 7 19 UPS07850152 1 20070711 A 2560 CASE DOUG DC8 DC871F 302199D WP EVAC SLIDE SEPARATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:N/A EMERGENCY ESCAPE SLIDE CASE IS SEPARATED. CLOSED SLIDE COVER AND RE-INSTALLED PIN PER MM 25-60-01-2 . 2 L 7 4 4F RT 4A25 2007071900092 20070719 00092 NM 2007 7 19 UPS07M50103 1 20070615 A 5330 SKIN DOUG MD11 MD11F 3023600 NM FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 282UP 48452 INSPECTION TYPE:C FUSELAGE SKIN CENTER CARGO DOOR AFT JAMB GOUGE REPAIR. REF DMI# D350923. CUT OUT DAMAGED AREA, FABRI CATED, AND INSTALLED REPAIR DOUBLER, TRIPLER, AND FILLER IAW MD-11 SRM 53-50-00 FIG 17. REPAIRED ON NRC 082034. 2 L 7 3 4F RT A22WE 2007071900093 20070719 00093 SO 2007 7 19 SIMA200719413 1 20070705 A 5347 14530658007 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 717AE 15889 5000 145272 RIGHT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERA TIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900096 20070719 00096 SO 2007 7 19 SIMA200719410 1 20070621 A 5347 14530659007 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 811AE 13526 5000 145529 LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERAT IONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900097 20070719 00097 SO 2007 7 19 SIMA200719412 1 20070621 A 5347 14530659007 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 811AE 13526 5000 145529 LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. OPERAT IONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900100 20070719 00100 EU 2007 7 19 SIMA200719701 1 20070713 A 7921 5034T31P02 OIL COOLER SAAB SF340 340B 7860101 EU ENGINE FAILED A SIMA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 384AE 7216 1294 340B384 RIGHT ENGINE OIL TEMPERATURE INDICATION IN RED, DURING TAXI OIL PRESSURE INDICATION ERRATIC WITH ENGINE SHUTDOWN. RETUR NED TO LFT. REMOVED AND REPLACED OIL SAVAGE PUMP, OIL BYPASS VALVE AND OIL COOLER IAW SAAB AMM. OPERATIONAL CHECK GOOD . RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007071900101 20070719 00101 SO 2007 7 19 SIMA200719715 1 20070708 A 5347 14532605015 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 816AE 13301 5000 145552 RIGHT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 36 TO 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900104 20070719 00104 SO 2007 7 19 SIMA200719706 1 20070705 A 5347 14530659005 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 717AE 15889 5000 145272 LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 36 TO 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRA FT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900106 20070719 00106 SO 2007 7 19 SIMA200719719 1 20070708 A 5347 14532605017 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 816AE 13301 5000 145552 RIGHT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900107 20070719 00107 SO 2007 7 19 SIMA200719720 1 20070708 A 5347 14530658005 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 816AE 13301 5000 145552 LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 36 TO 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRA FT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900111 20070719 00111 SO 2007 7 19 SIMA200719723 1 20070708 A 5347 14532606017 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 816AE 13301 5000 145552 LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071900113 20070719 00113 NM 2007 7 19 UPS07M50120 1 20070703 A 3610 SENSOR DOUG MD11 MD11F 3023600 NM NR 2 MANIFOLD MALFUNCTIONED A IPXA J A DUMP FUEL UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 254UP 48406 INSPECTION TYPE:N/A ATB - NR 2 MANIFOLD FAIL MESSAGE. FUEL IMBALANCE, DUMPED 55.0 LBS OF FUEL TO LAND. DEFERRED UNDER M353851. AFTER CLEARING WAN 136845 REPLACED ALL 6 ZONE SENSORS NR 2 ENG ESC OP CHECKS NORMAL IN AUTO AND MANUAL MODE. ESC PASSES RTS TEST MM 21-08-01. OPERATED APU AIR IN MANUAL AND AUTO MODE. OPS CHECKS NORMAL. THIS CLEARS DEF 353851. PLACARD REMOVED. 2 L 7 3 4F RT A22WE 2007071700061 20070717 00061 EA 2007 7 17 A6WA200740349 1 20070625 A 5340 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AW 7878 FS 484.0 LT LBL 27.0, WL 71.0 TO 73.5 ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED CRACKED ANGLE AT FS 484.00, LBL 2 7.0 IAW REO 601R53-41-059. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700065 20070717 00065 2007 7 17 AMTA200700330 4 20070709 A 3442 20414440402 DRIVE UNIT BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE WX RADAR INOPERATIVE A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 550TZ 32584 STATUS CODE (WXR SYS) DISPLAYED. REMOVED AND REPLACED WXR DRIVE UNIT IAW MM34-43-05, OPS CHECK NORMAL, MSG EXTINGUISHED , OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007071700070 20070717 00070 NM 2007 7 17 AMTA200700316 1 20070630 A 3040 HEATER BOEING 737 73783N 13844HI NM COCKPIT UNKNOWN A AMTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 11 304TZ 30675 RT SIDE WINDOW HEAT CAME ON DURING DECENT THROUGH 9,000. REMOVED AND REPLACED RT SIDE OPENABLE WINDOW IAW AMM 56-12-11- 4, OPS AND SECURED OK. NO LEAK. (K) 2 L 7 2 4F RT A16WE 2007071700080 20070717 00080 NM 2007 7 17 DL76L070838 1 20070630 A 4900 UNKNOWN BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE APU UNKNOWN A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 1200K 42216 28457 P154 APU FAULT AND SHUTDOWN ON ENGINE START. BITE CHECK OF APU ECU SHOWS NO FAULTS, APU SHUTDOWN OCCURRED ON ENGINE START WI TH AIR DEMAND. FWD APU PNEU TO MCO PER MEL49-11-01C. ECU SHOWS NO FAULTS. REPLACED SCV AS PREVENTIVE MEASURE PE M/M. MOTORED ENG 2 TIMES CKS OK MCO AND PLACARD REMOVED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071700081 20070717 00081 NE 2007 7 17 DL76L070840 2 20070701 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 FLAMED OUT A DALA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 27 195DN 38635 28452 727774 DIV DUE NR 2 ENGINE FLAME OUT. PERFORM FADEC BITE. FAULTS P5 LINE FAIL. REF ITEM 006. REMOVED AND REPLACED E FUEL PU MP AND FMU PER AMM. REF ITEM 005 FOR FUEL BOOST PUMP REPLACEMENT. PERFORM TEST 2, 3 AND 4 PER AMM 71-00-00 PG 501 ENG OPERATION AND ALL INDICATIONS NML. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071700082 20070717 00082 NM 2007 7 17 DL76L070842 1 20070627 A 4920 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE APU MALFUNCTIONED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 175DN 34465 24803 P1073 APU SHUTDOWN DURING ENG START. RESTARTED APU ELECT OK. REPLACED APU ASSY PER AMM. OP AND LK CKS GOOD. REMOVED MCO/PL AC. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071700084 20070717 00084 NM 2007 7 17 DL757070844 1 20070703 A 2530 OVEN BOEING 757 757232 1384965 NM MID GALLEY OVERHEATED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 658DL 24420 SMOKEY SMELL IN MID GALLEY. LT BREAKER POPPED ON AFT SECTION OF MID GALLEY M301. VENT ON FWD PART OF MID GALLEY WAS W ARM TO TOUCH EVEN AFTER TURNING OFF BOTH UTILITY BUSES. FOUND AFT OVEN MID GALLEY INOP. FWD TO MCO 25-20-01E. REPLAC ED OVEN IN MID, OVEN OPS NORMAL. MCO AND PLACARD REMOVED. 2 L 7 2 4F RT A2NM 2007071700085 20070717 00085 NM 2007 7 17 DLM88070845 1 20070703 A 5730 59304953 SKIN DOUG MD88 MD88 3023688 NM LT WING DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948DL 49879 THE LT INBOARD FLAP OUTBOARD GUIDE VANE WAS FOUND DELAMINATED AT HMV. THE DAMAGE WAS REPAIRED PER ER/A 462557-14 AND AP PROVED PER BOEING MESSAGE 1-387586211-3, DATED JUNE 25, 2007. 2 L 7 2 4F RT A6WE 2007071700086 20070717 00086 NM 2007 7 17 DLM88070846 1 20070703 A 5330 59670632 SKIN DOUG MD88 MD88 3023688 NM BS 1437 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948DL 49879 TWO CRACKS (.500" AND .750") WERE FOUND IN THE FUSELAGE SKIN AT FS 1437 BETWEEN RT L-1 AND L-4. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ER/A 462554-14 AND APPROVED BY BOEING MESSAGE 1-385059352-2. 2 L 7 2 4F RT A6WE 2007071700103 20070717 00103 NM 2007 7 17 DLM90070864 1 20070625 A 5320 9930538412 CUSP WEB DOUG MD90 MD9030 3023690 NM IAE V2525 V2525D5 NE BS 579-598 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 V20105 RIGHT CUSP WEB STA 579-598 CORRODED OUT OF LIMITS. REMOVED DAMAGED CUSP WEB AND REPLACED WITH A SERVICEABLE WEB IAW THE MD 90 SRM 51-30-02, 51-30-01, 51-10-05 AND 51-30-05 2 L 7 2 4F 4 F RT A6WE A40NE 2007071700106 20070717 00106 NM 2007 7 17 DLM90070868 1 20070617 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 564-550 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 LT CUSP WEB AT FS 564 AND 550 OUT OF LIMITS CORROSION. REPAIRED CUSP WEB IAW MD80 SRM 53-05D FIG 827D. 2 L 7 2 4F RT A6WE 2007071700113 20070717 00113 NM 2007 7 17 QXEA200701060 1 20070625 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 201 S31L CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - CABIN UNDER FLOOR LEFT AT FRAME X201.300 AND AT STRINGER 31L, STRINGER FITTING TO LEFT SEAT TRACK LOWER CHANNEL SUPPORT HAS CORROSION AT FASTENERS. REPAIRED IAW SRM 51-20-11, 51-40-11, 51-20-36. 2 H 7 2 4T RT A13NM 2007071700118 20070717 00118 NM 2007 7 17 QXEA200701062 1 20070625 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 467 S30-31L CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX-CABIN UNDER FLOOR LEFT AT FRAME X467.00 AND BETWEEN STRINGER 30L AND 31L, FRAME CASTELLATION HAS CORROSION AT FAS TENERS. REPAIRED IAW SRM 51-20-11, 51-40-11, 51-30-26. 2 H 7 2 4T RT A13NM 2007071700119 20070717 00119 NM 2007 7 17 QXEA200701066 1 20070627 A 5230 UNKNOWN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR UNKNOWN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - CARGO DOOR UPPER FORWARD FIBERGLASS CORNER PIECE HAS REINFORCEMENT STRAP INSTALLED EXTERNALLY. REPAIRED IAW SR M 51-40-11. 2 H 7 2 4T RT A13NM 2007071700124 20070717 00124 NM 2007 7 17 QXEA200701086 1 20070628 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - THE TOP CENTER CARGO DOOR SKIN HAS A GOUGE 3.5" LONG FROM THE EDGE DOWN. REPAIRED IAW RD8/4-52-029. 2 H 7 2 4T RT A13NM 2007071700130 20070717 00130 NM 2007 7 17 AWXA200700811 1 20070703 A 5340 694511562 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - CRACKED STRINGER CLIP, BS 578, S11R. REPLACED STRINGER CLIP, BS 578, S11R IAW B737-300 SRM 51-40-0 2. 2 L 7 2 4F RT A16WE 2007071700132 20070717 00132 EU 2007 7 17 AWXA200700815 1 20070707 A 2150 SENSOR AIRBUS 320 A320232 3930326 EU NR 1 A/C PACK FAILED A AWXA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 WP 28 663AW 1419 CREW REPORTED DURING CRUISE AT 280FL PACK 1 OVERHEAT. NR 2 PACK WAS ON MEL. CREW DESCENDED TO 10K. CREW RESET NR 1 PA CK, PACK OPERATED NORMAL. CREW DECIDED TO DIVERT TO DEN. LANDING WAS UNEVENTFUL. MX REPLACED THE 10HB PRESSURE SENSOR IAW AMM 21-51-11-400- 001. OPERATIONAL CHECK WAS GOOD. THE A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2007071700137 20070717 00137 NM 2007 7 17 AWXA200700817 1 20070705 A 5340 69387901 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - CRACKED STRINGER CLIP, BS 578, S10L. REPLACED STRINGER CLIP, BS 578, S10L IAW B737-30 0 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071700140 20070717 00140 NM 2007 7 17 AWXA200700820 1 20070703 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5982103, CRACKED STRINGER CLIP, BS 639, S2L. REPLACED STRINGER CLIP, BS 639, S2L I AW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071700145 20070717 00145 NM 2007 7 17 AWXA200700806 1 20070709 A 5310 6555074 GUSSET BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 PHX - MAJOR REPAIR - CRACK AT FIRST OFFICERS NR 1 WINDOW POST GUSSET UPPER RIGHT CORNER, BS 196.5 - BS 203.8, S9R - S10 R. REPAIRED FIRST OFFICERS NR 1 WINDOW POST GUSSET UPPER RIGHT CORNER, BS 196.5 - BS 203.8, S9R - S10R IAW B737-300 SRM 53-10-01-2R. 2 L 7 2 4F RT A16WE 2007071700149 20070717 00149 NM 2007 7 17 AWXA200700827 1 20070705 A 5340 69353502 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR# 5961290, CRACKED STRINGER CLIP, BS 520, S16L. REPLACED STRINGER CLIP, BS 520, S16 L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071700158 20070717 00158 NM 2007 7 17 AWXA200700834 1 20070711 A 5347 D53233436200 SEAT TRACK AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5964132, CORROSION ON CABIN SEAT TRACK, -Y765, BS 1323 / FR 34. REPAIRED CABIN SEA T TRACK, -Y765, BS 1323/FR 34 IAW A319 SRM 53-00-15. 2 L 7 2 4F RT A28NM 2007071700171 20070717 00171 NM 2007 7 17 ASAA0751826 1 20070628 A 3320 417A5200205 LIGHT BOEING 737 737800* NM CABIN ODOR A ASAA H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 NM 02 581AS 35188 ELECTRICAL TYPE SMELL IN CABIN DURING FLIGHT. F/A'S REPORT MOST NOTICEABLE AT ROWS 9, 11 AND NEAR AFT GALLEY VENT. SLI GHTLY NOTICEABLE IN COCKPIT. TURNED OFF CABIN LIGHTING AND SMELL DISSIPATED. CHECKED AFT GALLEY OVENS COFFEEMAKERS HOT PLATES FOR DEBRIS NONE NOTED. CYCLED SAME, NO ODOR PRESENT. TURNED ON ALL CABIN LIGHTS & READING LIGHTS IN AREAS, IND ICATED NO ODORS NOTICED. RAN PACKS, NO ODORS. 2 L 7 2 4F RT A16WE 2007071700172 20070717 00172 WP 2007 7 17 ASAA0781827 1 20070702 A 5340 4911383504 ATTACH FITTING DOUG DC9 DC983 3022083 WP BS 1271 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 FRAME ATTACH FITTING HAS EXFOLIATION (CORROSION). REPLACED FITTING PER SRM 51-10-4 AND 51-30-5. 2 L 7 2 4F RT A6WE 2007071700178 20070717 00178 WP 2007 7 17 ASAA0781833 1 20070702 A 5320 59568791 TORQUE BOX DOUG DC9 DC983 3022083 WP BS 209-213 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 L1 DOOR CUTOUT TORQUE BOX WEB CRACKED AT AFT SIDE OF LONGERON. INSTALLED DOUBLER AND FILLER PER DWG 65956879 SRM 51-70- 4 AND 51-10-3. 2 L 7 2 4F RT A6WE 2007071700180 20070717 00180 WP 2007 7 17 ASAA0781836 1 20070702 A 5321 9936547505 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 CABIN FLOORBOARD PUNCTURED. REPLACED FLOOR PANEL PER SRM 53-05 AND DAC DWG 99366549. 2 L 7 2 4F RT A6WE 2007071700197 20070717 00197 EA 2007 7 17 TRAX200700917 1 20070702 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX OBSTRUCTED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 858AS 7417 PAX DOOR WILL NOT CLOSE, IT GETS 18 INCHES FROM AIRFRAME AND STOPS. 2 L 7 2 4F RT A21EA 2007071700198 20070717 00198 EA 2007 7 17 TRAX200700918 1 20070703 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 WARDROBE EMERGENCY EXIT LIGHT STRIP INOP. 2 L 7 2 4F RT A21EA 2007071700199 20070717 00199 EA 2007 7 17 TRAX200700922 1 20070703 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 LEFT WING PLANK APPEARS CRACKED AT WS 148.019 LEFT, NEEDS NDT TO VERIFY CRACK. COMPLETED IN ACCORDANCE WITH REO 601R-57 21-130. 2 L 7 2 4F RT A21EA 2007071700201 20070717 00201 EA 2007 7 17 TRAX200700929 1 20070704 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 753EV 10169 LEFT AND RIGHT WEBS AT FS 280 RBL 9 TO OUTBOARD WALL AND LBL 9 TO OUTBOARD WALL CORRODED (PER MTC). 2 L 7 2 4F RT A21EA 2007071800005 20070718 00005 EA 2007 7 18 TRAX200700932 1 20070704 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 917EV 7769 FLAPS FAILED AT 8 DEG WHEN 20 DEG WAS SELECTED. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007071800015 20070718 00015 NM 2007 7 18 DL76L070885 1 20070706 A 2420 HOUSING BOEING 767 767332 1382001 NM AC GENERATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 176DN 2107 25061 APU A/C GENERATOR HOUSING CRACKED, LEAKING OIL FROM 12 O`CLOCK POS. REPLACED APU A/C GEN PER MM, SYSTEM TEST OK PER MM MFG P/N727810B. 2 L 7 2 4F RT A1NM 2007071800018 20070718 00018 NM 2007 7 18 DLM88070887 1 20070706 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 663 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948DL 49879 CORROSION ON RT CUSP WEB AT STA Y=663, TASK 58-53313. REPAIRED PER ERA 398191-14MA ON N/R T0060304 AT HMV. 2 L 7 2 4F RT A6WE 2007071800032 20070718 00032 NM 2007 7 18 HNAA0700142 1 20070707 A 5320 STRAP DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 839EX 226 LITE CORROSION BETWEEN X510.00 AND X531.500 ON STR 29 STRAP. 2 H 7 2 4T RT A13NM 2007071800060 20070718 00060 NM 2007 7 18 UPS07550134 1 20070613 A 5311 143N1024138 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 420UP 23907 INSPECTION TYPE:C DENT IN FWD CARGO FUSELAGE FRAME STA 660, BETWEEN S24R AND S25R. ACCOMPLISHED ON FINAL EA 757-5332-27 -A1690 AND UPS EO B757-5310-27178. 2 L 7 2 4F RT A2NM 2007071800069 20070718 00069 NM 2007 7 18 DL757070900 1 20070709 A 2150 211080107 A/C PACK BOEING 757 757232 1384965 NM GE CF6 CF680C2* GL RIGHT MALFUNCTIONED A DALA B EMER. DESCENT S AFFECT SYSTEMS CR CRUISE 1 SO 27 605DL 22812 706288 IN FLIGHT, THE RIGHT PACK WAS UNABLE TO PRESSURIZE A/C. THE LT PACK WAS ON MCO. CHECKED NR 1 AND NR 2 CABIN PRESSURE C ONTROLLER BOTH CK GOOD. CHECKED ALL DOOR SEALS AND OUTFLOW VALVE. AFTER LT ACM CHANGE PRESSURIZED A/C TO 5 PSID WITH A PU NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A2NM E23EA 2007071800095 20070718 00095 WP 2007 7 18 ASAA0781845 1 20070702 A 5347 593054768 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 SEAT TRACK HAS DOUBLE DRILLED HOLES. REMOVED DAMAGED SECTION OF TRACK, LOCATED, DRILLED AND INSTALLED A REPLACEMENT TRA CK IAW SRM 53-05 PG 11 FIG 4H, 51-10-4 PG 1 AND 51-30-5 PG 1 AND 51-30-1 PG 1. 2 L 7 2 4F RT A6WE 2007071800120 20070718 00120 NM 2007 7 18 AALA20071214 1 20070629 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 780AN 29956 MIA - EMERGENCY LIGHT AT SEAT 26C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007071800122 20070718 00122 WP 2007 7 18 ASAA0781856 1 20070704 A 5753 5910043510 SKIN DOUG DC9 DC983 3022083 WP T/E FLAP VANE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 RIGHT WING O/B FLAP O/B VANE GOUGED ON UPPER SURFACE 68 INCHES FROM O/B END. PREPAIRED DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED IAW SRM 51-70-2 PG 23 PARA 18B AND 51-70-2 FIG 12. 2 L 7 2 4F RT A6WE 2007071800131 20070718 00131 NM 2007 7 18 QXEA200701150 1 20070713 A 2510 LOCK PIN BOMBDR DHC8 DHC8402 1390042 NM COCKPIT SEAT DIRTY A QXEA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 NM 09 414QX 4061 SEA - ON FLIGHT 2490, RETURNED TO FIELD CAPTAINS SEAT WILL NOT LOCK IN PLACE. MAINTENANCE CLEANED AND LUBED SEAT LOCKIN G PINS. OPERATIONAL CHECK GOOD, NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007071800132 20070718 00132 NM 2007 7 18 MWEA070154 1 20070706 A 5753 59121553 STRUCTURE BOEING 717 717200 1383700 NM T/E FLAP DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 905ME 55169 LEFT WING FLAP TRAILING EDGE FIBER SHAPE IS DAMAGED. REMOVED AND REPLACED REPAIR SEGMENT. 2 L 7 2 4F TR A6WE 2007071800149 20070718 00149 NM 2007 7 18 SWAA073351 1 20070706 A 5523 65C26384 TAB BOEING 737 7373H4 1384600 NM RT ELEVATOR DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 14Y CHECK, FOUND RIGHT ELEVATOR TAB DELAMINATED AT NR 1 HINGE CUTOUT. REPAIRED TAB PER SRM. 2 L 7 2 4F RT A16WE 2007071800158 20070718 00158 NM 2007 7 18 KCSA071206 1 20070710 A 5320 STIFFENER BOEING 747 7472B4B 138481B NM NLG WW CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NOSE WHEEL WELL TOP PANEL STIFFENER CRACKED AT BS 310, RBL 11. 2 L 7 4 4F RT A20WE 2007071800167 20070718 00167 SO 2007 7 18 C2XA07TY035 1 20070706 A 5751 14569009410 BRACKET EMB 145 EMB145LR 3260212 SO RT AILERON WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13995 145295 RIGHT AILERON PCA ATTACH FITTING I/B MOST LUG WORN AND HAS CORROSION INSIDE BORE. REMOVED AND REPLACED PCA BRACKET IAW EC 5750-01177. AIRCRAFT IS STILL IN C-CHECK. 2 L 7 2 4T RT T00011AT 2007071800183 20070718 00183 WP 2007 7 18 AALA20071202 1 20070628 A 3350 8029001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 441AA 49460 LGA - EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS CABI N. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071800222 20070718 00222 CE 2007 7 18 DJFA2007070 1 20070708 A 3297 WIRE HARNESS RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG INDICATOR DAMAGED E DJFA O OTHER P NO WARNING INDICATION AP APPROACH 1 EA 23 720TA 258320 ON APPROACH, THE CREW RECEIVED NO GEAR INDICATION (TRANSIT OR DOWN AND LOCKED) WHEN SELECTING THE GEAR TO THE DOWN POSIT ION. THE GEAR INDICATOR LIGHT CIRCUIT BREAKER HAD POPPED IN FLIGHT. THE SECONDARY INDICATORS DID INDICATE THE GEAR WAS DOWN. AN EMERGENCY WAS DECLARED. THE LANDING WAS UNEVENTFUL. DURING TROUBLESHOOTING MAINTENANCE FOUND THE NOSE GEAR WIRE HARNESS CONTACTING THE MANUAL DOOR RELEASE STRUT DURING EXTENSION AND RETRACTION. THE WIRES WERE INSPECTED, WRAPP ED AND REROUTED. OPS CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A3EU E6WE 2007071800244 20070718 00244 CE 2007 7 18 AMWA15036B 1 20070710 A 5730 11811001541 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT WING CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 155ZV UE155 FRICTION CHAFFING CREATED WORN SEGMENTS ON THE LT AND RT ENGINE NACELLES. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NAC ELLE SHAPE. DEPTH VARIED AS INDICATED ON THE REPAIR AUTHORIZATION. REPAIRED IAW ENGINEERING REPORT NR 677201 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007071800249 20070718 00249 WP 2007 7 18 ASAA0781860 1 20070708 A 5321 S4932106 FLOORBOARD DOUG DC9 DC983 3022083 WP CABIN CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 FLOORBOARD CORRODED AT STA 256 X 22 TO X 44. FABRICATED REPLACEMENT FLOORBOARD IAW SRM 53-05 DWG S4932106. 2 L 7 2 4F RT A6WE 2007071800250 20070718 00250 NM 2007 7 18 CNMA20070006 1 20070318 A 5320 CHANNEL DOUG DC10 DC10 N/A-SDR NM GE CF6 CF650C2 30018 NE BS 2007 CORRODED A CNMA K NONE O OTHER IN INSP/MAINT 1 SW 07 270AX 48318 BS 2007, RBL 20-23, CORROSION ON CHANNEL SUPPORT UNDERNEATH GALLEY. CORRODED PORTION REMOVED NEW FABRICATED M/F S2920883 -12000 AND INSTALLED WITH EXISTING FASTNERS IAW SRM VOL 2 51-31-01 AND CHERRY-MAX MS 2885/6-4/08. 2 L 7 3 4F 4 F RT A22WE E23EA 2007071800252 20070718 00252 WP 2007 7 18 ASAA0781861 1 20070710 A 5321 99365441 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 CABIN FLOOR PANEL HAS DAMAGED INSERTS. FABRICATED AND INSTALLED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PG 122B THRU 12 7 SECTION 44 FIGS 40 THRU 50. 2 L 7 2 4F RT A6WE 2007071800253 20070718 00253 SO 2007 7 18 GM07004 1 20070710 A 5347 1159B5127413 SEAT TRACK GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE BS 426 CORRODED E UG8A K NONE O OTHER IN INSP/MAINT 1 GL 23 5101 5623 550 CORROSION DISCOVERED ON ALL SEAT TRACKS AFT OF FS 426.5. 2 L 7 2 4F 4 F RT A12EA E00057EN 2007071800255 20070718 00255 WP 2007 7 18 ASAA0781862 1 20070704 A 5753 5930496508 SKIN DOUG DC9 DC983 3022083 WP T/E FLAP VANE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 RIGHT WING O/B FLAP I/B VANE GOUGED ON L/E 7 INCHES FROM I/B END. PREPARED DAMAGED AREA. FABRICATED DOUBLER AND INSTAL LED IAW SRM 51-70-2 PG 59. 2 L 7 2 4F RT A6WE 2007071800257 20070718 00257 WP 2007 7 18 ASAA0781864 1 20070708 A 5311 991960443 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 AFT CARGO FORMER CORRODED. REMOVED DAMAGED AREA OF FORMER FABRICATED, LOCATED, DRILLED AND INSTALLED A REPLACEMENT FORM ER IAW SRM 51-10-3 PG 24. 2 L 7 2 4F RT A6WE 2007071800260 20070718 00260 NM 2007 7 18 2007UALA02415 1 20070705 A 3097 TERMINAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WINDSHIELD HEAT FAILED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 572UA 26682 WINDOW 1R OUTER PANE SHATTERED WITH ARCING IN 3 DIFFERENT SPOTS AT BOTTOM OF WINDSCREEN. [08-08-07] PROBABLE CAUSE I S LOOSE TERMINAL CONNECTION CAUSED BY INCORRECT TORQUE OF SCREW OR AN INCORRECTLY INSTALLED SCREW. REPLACED 1R WINDSHIE LD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071800262 20070718 00262 NM 2007 7 18 2007UALA02417 1 20070704 A 2420 IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 538UA 25222 EICAS MSG LT GEN DRIVE DISPLAYED. GEN DRIVE LIGHT ILLUM. GEN DRIVE DISCONNECTED. [08-08-07] RED DPI POPPED ON I DG. APU OIL SVC'D TO FULL. REPLACED NR 1 ENG IDG. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071800264 20070718 00264 NM 2007 7 18 2007UALA02419 1 20070705 A 3350 MR33512 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 821UA 944 EMERGENCY LIGHTS FAIL TEST PER 3SVC FOR AFT LEFT BATTERY. REPLACED AFT ESPU BATTERY FOR A SECOND TIME, SYSTEM PASSED TE ST. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071800266 20070718 00266 NM 2007 7 18 2007UALA02421 1 20070705 A 5313 STRINGER SPLICE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 FUSELAGE STRINGER SPLICE IS CRACKED AT LOWER FLANGE AND UPPER FLANGE BS360 STR 15L. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED STRINGER SPLICE 15L AT STA 360. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071800268 20070718 00268 SW 2007 7 18 AC2A116357 1 20070706 A 5410 3P7118A00132 COWLING AGUSTA AB139 AB139 0260110 SW PWA PT6 PT6* 52043 EA NACELLE BURNED B AC2A K NONE O OTHER IN INSP/MAINT 1 SW 31 139FW 773 31022 COWLING WAS FOUND BURNED DURING EXHAUST BRACKET REPLACEMENT. BURNED AREA WAS APPROXIMATELY (2) INCHES BY (3) INCHES. C OWLING WAS REPAIRED AND RETURNED TO SERVICE. ALL OTHER AIRCRAFT IN FLEET WERE INSPECTED AND FOUND OK PHOTO OF COWLING H AS BEEN SENT TO FSDO. 2 G 7 2 4U 3 T R00002RD E2NE 2007071800269 20070718 00269 CE 2007 7 18 DXTA200702332 1 20070712 A 3260 INDICATOR CESSNA 500 560CESSNA 2076750 CE PWA 545 PW545A NE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 844QS 5600629 LT MAIN LANDING GEAR INDICATOR WOULD NOT EXTINGUISH AFTER GEAR WAS BROUGHT UP. CYCLED GEAR 3 TIMES, INDICATOR STAYED ON EACH TIME. [07-23-07] JACKED A/C IAW CESSNA AIRCRAFT TO MODEL 560 MAINTENANCE MANUAL 7-10-11. SWING LANDING GEAR TH ROUGH 5 CYCLES, COULD NOT DUPLICATE LANDING GEAR INDICATOR PROBLEM. PERFORMED HYDRALIC ACT DOWNLOAD SWITCH ADJUSTMENT IA W CITATION 560MM 32-31-04 PG 207. CYCLED GEAR TWICE COULD NOT DUPLICATE PROBLEM. OPS CHECK GOOD IAW CITATION 560 MM CHAP TER 32-01-00. LOWERED A/C VERIFICATION OF GEAR LOCKED. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007071800272 20070718 00272 CE 2007 7 18 DXTA200702306 1 20070628 A 2700 CONTROL PANEL RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP FLT CONTROLS SHORTED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 861QS 258361 10 MIN INTO FLT AT NIGHT, 12000 MSL, IN AND OUT OF CLOUDS AND RAIN, AREA ABOVE RT- SIDE FLT CONTROL PANEL SPARKED W/POPP ING NOISE AND BRIEF BURNED SMELL ACCOMPAINIED BY BOTH MASTER WARNING LTS FLASHING. RAN A/C APU AND ENGINES TO VERIFY DI SCREPANCY, COULD NOT DUPLICATE SPARKING SMELL OR WIRING ACTUATION. PERFORMED GENERAL INSPECTION OF COCKPIT FLIGHT CONTR OL PANELS AND PILOT AND CO-PILOT WINDSHIELDS. FOUND 4 STATIC DISCHARGE DRAINS NOT SECURED. REPAIRED STATIC DRAIN WEDGES IAW SRM CHAPTER 56-10-11. 2 L 7 2 4F 4 F RT A3EU E6WE 2007071800273 20070718 00273 CE 2007 7 18 DXTA200702304 1 20070628 A 3240 216011 BRAKE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG STUCK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 627QS 556 5605227 LT BRAKE IS STICKING CAUSING CONTROL ISSUES WHILE TAXIING. INSTALLED AN OVERHAULED BRAKE IN LT POSITION IAW MM CH 32-42 . INSTALLED AN OVERHAULED METERING VALVE IN LT POSITION IAW THE MM CH 32-42. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007071800274 20070718 00274 NM 2007 7 18 DXTA200702334 1 20070713 A 3240 BRAKE AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE MLG MALFUNCTIONED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 284QS 185 WHEN MAIN A/C BRAKES ARE APPLIED BRAKES WILL GRAB THEN RELEASE, THEN GRAB WHILE BRAKES ARE APPLIED SMOOTHLY. [07-23-07 ] PERFORMED BRAKE PRESSURE CHECKS AND FOUND NO ABNORMAL PRESSURES. IAW F2000 MM 32-412. FOUND FAULT CODES FOR BSCU N R 1 AND 2 AND FOUND CODE 335 AND 435. REMOVED (DEFECTIVE) 4 EACH WHEEL GENERATOR SLEEVES P/N A35005, INSTALLED 4 EACH N EW GENERATOR SLEEVES P/N A35005 IAW 32-415 OPERATIONAL CHECK GOOD. 2 K 7 2 4F 4 F RT A50NM E44NE 2007071800275 20070718 00275 NM 2007 7 18 UIEA200700267 1 20070713 A 5414 SKIN BOEING 747 7472D7B 1384803 NM NR 3 NACELLE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 NR 3 ENGINE LT CORE COWL NR 437, AFT LOWER CORNER LONGERON STRUCTURE AND OUTER COWL SKIN HAS A CRACK AND LOOSE RIVETS. PERMANENT REPAIR ACCOMPLISHED AS PER 747 SRM 54-31-03 FIG 3 AND ATLAS EO4771A026 AND FAA 8110-3 FORM (REF: FIG. 1 AND 2) AND ATLAS AIR XEO NR 54-071307. 2 L 7 4 4F RT A20WE 2007071800277 20070718 00277 NM 2007 7 18 UIEA200700265 1 20070713 A 5410 DOOR BOEING 747 7472D7B 1384803 NM FAIRING DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 NR 1 ENGINE RT STRUT TRAILING EDGE FAIRING DOOR, PANEL NR 454AR, FORWARD LOWER CORNER HAS AN AREA OF 7.0 INCH BY 10.0 IN CH AREA OF DELAMINATION. ACCOMPLISHED PERMANENT REPAIR AS PER 747-200 SRM 51-40-06 FIG 4, SHEET 1 AND 747-200 SRM 51-40 -20. ALSO, REF: ATLAS AIR XEO NR 54-071207. 2 L 7 4 4F RT A20WE 2007071800278 20070718 00278 NM 2007 7 18 UIEA200700263 1 20070713 A 5347 BAC15201566 SEAT TRACK BOEING 747 7472D7B 1384803 NM BS 1906 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 MAIN DECK SEAT TRACK AT BS1906, LBL 99 HAS CROWN LUGS CRACKED. PERMANENT REPAIR WAS ACCOMPLISHED AS PER 747-200 SRM 53- 10-05 FIG 1A AND 747-200 SRM 51-10-08. ALSO, REF: ATLAS AIR XEO NR 53-071307. 2 L 7 4 4F RT A20WE 2007071800279 20070718 00279 NM 2007 7 18 UIEA200700264 1 20070713 A 5730 PANEL BOEING 747 7472D7B 1384803 NM RT WING DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 RT WING FUELING BAY ACCESS PANEL NR 621BB, INNER SKIN HAS 2 EACH AREAS OF DELAMINATION. PERMANENT REPAIR WAS ACCOMPLISH ED AS PER 747-200 SRM 51-40-09 FIG 18, SHEET 1, 3, AND 5, TABLE 1, PREPEG 250* F CURE. ALSO, REFERENCE ATLAS AIR XEO NR 57-071207. 2 L 7 4 4F RT A20WE 2007071800280 20070718 00280 NM 2007 7 18 UIEA200700266 1 20070713 A 5350 FAIRING BOEING 747 7472D7B 1384803 NM WING TO BODY PUNCTURED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 LOWER BODY FAIRING PANELS 194C AND 194B HAVE A PUNCTURED HOLE. PANEL 194B AREA OF PUNCTURE IS 2.750 BY .750 INCHES AND 194C IS 1.250 BY .750 INCHES. PERMANENT REPAIR WAS ACCOMPLISHED AS PER 747-200 SRM 51-40-09 FIG 11 AND 747-200 SRM 51-4 0-12. ALSO, REF: ATLAS AIR XEO NR 53-071107. 2 L 7 4 4F RT A20WE 2007071800282 20070718 00282 NM 2007 7 18 UIEA200700260 1 20070708 A 2120 UNKNOWN BOEING 747 7472D7B 1384803 NM COCKPIT ODOR A UIEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 15 528MC 22472 AT DEPARTURE SMOKE AND BURNING ODOR IN COCKPIT, ELECTRICAL ODOR. PULLED C/BS FOR T/R UNITS, SMOKE AND ODOR STOPPED. WI RE BUNDLES AND AREA BELOW F/E PANEL (4) INSPECTED NO SIGN OF SHORTING OR CHAFING FOUND. PULLED T/R UNITS, PULLED AND IN SPECTED FOUND NR 1 T/R UNIT VERY HOT AND WITH BURNED ODOR. NR 1 T/R TRANSFERRED TO DMI M07-134 IAW MEL 24-8. DDPG MAIN T STEPS C/W ALL TEST PASS. 2 L 7 4 4F RT A20WE 2007071800284 20070718 00284 NE 2007 7 18 UIEA200700262 2 20070707 A 7314 8062899 VALVE BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE FUEL PUMP SHUTDOWN A UIEA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 EA 15 524MC 52771 2938 CGW11191 21784 517658 AT CRUISE ALT 38000 AFTER APPROX 50 MIN INTO THE TRIP NR 2 ENGINE SLOWLY ROLLED BACK THEN SHUTDOWN ALL OTHER INDICATIONS NORMAL. OIL PRESS TEMP OIL QTY AND FUEL FLOW IND WERE NORMAL. AFTER ENGINE NR 2 SHUTDOWN ENGINE INDICATED APPROX 1000 KGS BURN PER HOUR. NO FUEL LEAK NOTED WAS DETERMINED. ACCOMPLISHED THE APPROP FWB CHECKLIST. CHECKED ENGINE INLET/EXH AUST, MASTER CHIP DETECTOR, CDP LINE, VSV FEEDBACK CABLE, FUEL FILTER, FUEL S/O ACTUATOR, SPAR VALVE. NO DEFECTS NOTED. REMOVED AND REPLACED MEC IAW MM 73-2101. REMOVED AND REPLACED ENG FUEL PUMP IAW MM 73-11-01. CARRIED OUT ENG NR 2 RU N AFTER MEC AND FUEL PUMP REPLACEMENT AS PER MM 71-00-00. TEST 5 AND SATISFIED. 2 L 7 4 4F 4 F RT A20WE E23EA 2007071800286 20070718 00286 NM 2007 7 18 2007UALA02424 1 20070705 A 5210 TORQUE TUBE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD ENTRY DOOR EXCESS PLAY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 FWD ENTRY DOOR CUTOUT TORQUE TUBE HAS MOVEMENT BEYOND .003. REMOVED & REPLACED BODY TORQUE TUBE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071800287 20070718 00287 NM 2007 7 18 UIEA200700259 1 20070703 A 5610 SEAL BOEING 747 7472D7B 1384803 NM L3 WINDOW LOOSE A UIEA O OTHER O OTHER CR CRUISE 1 EA 15 528MC 22472 L-3 WINDOW SEAL LIFTING IN THE WIND WITH EXCESSIVE COCKPIT NOISE. ALSO, DURING LEVEL FLIGHT APPROX TIME 1335Z FL 31.0 T EMP -09 TAT HEARD BANG AIRCRAFT SHOOK, POSSIBLE ENGINE STALL. AUTO THROTTLES TRIPPED OFF SEVERAL TIMES IN FLIGHT. RES ECURED WINDOW SEAL IAW 56-11-00. INSPECTED INTAKES AND EXHAUST OF ALL ENGINES WITH NO FINDINGS. INSPECTED FUSELAGE IAW 5-51-00, NO FINDINGS. 2 L 7 4 4F RT A20WE 2007071800288 20070718 00288 WP 2007 7 18 AALA20071223 1 20070701 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14551 53033 DFW - EMERGENCY LIGHT AT SEAT 9D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071800289 20070718 00289 NM 2007 7 18 2007UALA02425 1 20070705 A 5514 BUSHING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZ STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 LEFT HORIZONTAL STAB, UPPER FRONT SPAR TO CTR SECTION ATTACH LUG HAS CORROSION EMITTING FROM BUSHING. MAJOR REPAIR ACCO MPLISHED: REMOVED CORROSION. MANUFACTURED & INSTALLED BUSHING. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071800291 20070718 00291 NM 2007 7 18 2007UALA02426 1 20070705 A 5514 BUSHING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZ STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 LEFT HORIZONTAL STAB FWD SPAR UPPER LUG AFT FACE 8 - 11 O'CLOCK POS HAS CORROSION OUTSIDE OF THE SPOT FACE. MAJOR REPAI R ACCOMPLISHED: REMOVED CORROSION. MANUFACTURED & INSTALLED BUSHING. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071800292 20070718 00292 EU 2007 7 18 MALA070074 1 20070708 A 3610 HOSE SAAB SF340 340B 7860101 EU RT ENGINE BLEED LEAKING A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 422XJ 340B422 DURING CLIMB-OUT, THE RT ENGINE BLEED LEAK LIGHT ILLUMINATED. THE CREW RETURNED AND LANDED WITHOUT FURTHER INCIDENT. F OUND RT WING ROOT HOSE LEAKING. REMOVED AND REPLACED BLEED HOSE PN: 9303688-100. REF AMM 36-11-35-04. OPS CHECK GOOD . 2 L 7 2 4T RT A52EU 2007071800293 20070718 00293 EA 2007 7 18 A6WA200740237 1 20070503 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 455AW 7848 FOUND LEFT FS 621 FLOOR SUPPORT ANGLE IS CRACKED 1.25 INCH LONG IN OUTBOARD RADIUS. MAINTENANCE CUT OUT DAMAGED AREA AN D INSTALLED REPAIR IAW BOMBARDIER REO 601R-53-61-117. (M) 2 L 7 2 4F RT A21EA 2007071800294 20070718 00294 NM 2007 7 18 2007UALA02427 1 20070705 A 3350 1317 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 AFT CREW REST CEILING EMERGENCY LIGHT IS INOP. REPLACED ASSY. CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071800295 20070718 00295 2007 7 18 MALA070075 4 20070710 A 3100 DISPLAY SAAB SF340 340B 7860101 EU COCKPIT INOPERATIVE A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 430XJ 340B430 JUST AFTER TAKEOFF, FO TUBES WENT BLANK, LOST WX RADAR, TCAS, GPS, NAV, COM 2. LOOKED UP AT PANEL AND NOTED R MAIN AND R ESS BUSS LIGHTS ILLUMINATED. CREW DECLARED AN EMERGENCY AND RETURNED TO MEM WITHOUT FURTHER INCIDENT. CREW CYCLED CI RCUIT BREAKER "R ESS R MAIN" AFTER LANDING AND OPS RETURNED TO NORMAL. CYCLED A/C POWER AND TESTED ELECTRICAL SYSTEM RE F AMM 24-30-00-05 AND 24-20-00-05. INSPECTED RT PDU AREA AND REPLACED TRANSIENT SUPPRESSOR RDI 56P1CR1 PN: 7239790-501 FOR PRECAUTIONARY REASONS. RAN A/C AGAIN AND VERIFIED NORMAL OPS. ALL CIRCUIT BREAKERS REMAINED IN THROUGHOUT TESTING AND TROUBLESHOOTING. 2 L 7 2 4T RT A52EU 2007071800296 20070718 00296 NM 2007 7 18 2007UALA02428 1 20070705 A 3350 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 SEATS 3J & 32ABC EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED LAMP ASSY. CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071800297 20070718 00297 NM 2007 7 18 QXEA200701120 1 20070710 A 6120 AUTOFEATHER SYS BOMBDR DHC8 DHC8402 1390042 NM FAULTED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 400QX 4030 MFR FLIGHT NR 2458: AUTO FEATHER DID NOT APPEAR ON ED WITH A/F SELECT. PUSHED AFTER RETURNING TO GATE, A/F PASSED. MAI NTENANCE FOUND FAULT CODE 64B BOTH SIDES. C/W F/M FAS 61-20-02-810-834. CLEARED FAULTS, UNABLE TO DUPLICATE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071800299 20070718 00299 2007 7 18 MALA070076 2 20070710 A 7261 B-NUT SAAB SF340 340B 7860101 EU ENGINE OIL LOOSE A MALA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 GL 15 434XJ 340B434 CREW REPORTED THE LEFT ENGINE OIL PRESSURE LIGHT ILLUMINATED AND THE GAUGE WAS FLUCTUATING. SHUT DOWN THE ENGINE INFLIGH T TO MSL. FOUND DELTA P REF TUBE B-NUT LOOSE AT FITTING. TIGHTENED B-NUT AND NO FURTHER LEAKS NOTED. PERFORMED GE SPE CIAL PROCEDURES PARA 3C BY INSPECTING POWER UNIT SCAVENGE SCREENS AND CHIP DETECTOR. NO DEFECTS NOTED. DID OIL CONSUMPT ION RUNS. NO FURTHER LEAKS NOTED. CLEANED OIL. 2 L 7 2 4T RT A52EU 2007071800301 20070718 00301 2007 7 18 C1HA200797002 4 20070708 A 3414 INDICATOR BOEING 727 727270 138408P NM CAPT AIRSPEED INACCURATE A C1HA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 697CA 23052 ON CLIMB-OUT, CAPTAIN'S AIRSPEED INDICATOR INDICATED ERRONEOUS AIRSPEED AND MACH. COMPLIED WITH COM 2.31.8.9.10.11.12 " FLIGHT WITH UNRELIABLE AIRSPEED/MACH" IVSI INDICATED INTERMITTENTLY VERTICAL SPEED INFORMATION ONLY. CLIMB STOPPED AT F L 280. ALL CIRCUIT B, REPLACED CAPT A/S IND. PERFORMED OPS CK ON A/S IND AND ADC IAW M/M 34-12-00 AND SUPP M/M 34-12-1 1. INSP CAPT PITOT TUBE FOUND CONTAMINATED WITH DEBRIS. REMOVED DEBRIS. OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 2007071800303 20070718 00303 2007 7 18 C1HA200797003 4 20070710 A 3414 2083081 INDICATOR BOEING 727 727270 138408P NM COCKPIT MALFUNCTIONED A C1HA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 697CA 23052 DURING CLIMB-OUT CAPTAINS AIRSPEED INDICATOR .95 ON CAPTAINS SIDE/COPILOTS MACH INDICATOR .76 MACH AIRSPEED CLACKER SOUN DED UNCONTROLLABLE COMPLIED WITH COM 2.31.8 LANDED AT DFW CONFIRMED FAULT OF NR 1 MACH IND. REMOVED AND REPLACED IND SY STEM CHECK GOOD IAW MM 34-12-00 CHECKED MACH IND AT .5, .6, .7 AND .75 MACH ALL IND NORMAL AND AGREED WITH BARFIELD DPS3 50 TEST BOX 2 L 7 3 4F RT A3WE 2007071800306 20070718 00306 NM 2007 7 18 2007UALA02433 1 20070706 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY LIGHT ROW 58 ABC INOPERATIVE. [07-24-07] RESECURED EMERGENCY LIGHT LAMP CONNECTOR. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071800307 20070718 00307 NM 2007 7 18 2007UALA02434 1 20070706 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY LIGHT MID GALLEY BOTTOM WALL LEFT INOPERATIVE. [07-24-07] RELAMPED MID GALLEY EMERGENCY LIGHT. OP CK NORMA L. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071800309 20070718 00309 NM 2007 7 18 2007UALA02436 1 20070706 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 182UA 25279 CABIN -E- ZONE RIGHT & LEFT AFT EEL CABLES ARE BROKEN. [07-27-07] REPLACED CABLES, OP CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071800311 20070718 00311 NM 2007 7 18 2007UALA02438 1 20070705 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 579UA 26697 EXTERIOR EMERGENCY LIGHT AT 1R, 4R & 4L ARE INOPERATIVE. [07-27-07] RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071800312 20070718 00312 NM 2007 7 18 2007UALA02440 1 20070705 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 FOUND GALLEY MID LEFT & MID RIGHT EMERGENCY LIGHT STRIPS INOP. [07-27-07] REPLACED MID LEFT TOILET EMERGENCY LIGHT STRIP. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071800316 20070718 00316 NM 2007 7 18 2007UALA02447 1 20070706 A 2740 TRIM SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE STABILIZER MALFUNCTIONED A UALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 29 527UA 24995 FLIGHT DIVERTED WITH STABILIZER TRIM PROBLEM. [08-08-70] REPLACED STAB TRIM LIMIT SWITCH AND POSTION TRANSMITTER M ODULE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071800318 20070718 00318 2007 7 18 2007UALA02449 4 20070705 A 2565 SLIDE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE L4 DOOR DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 219UA 30551 LARGE SLIT DOWN BOTTOM TUBE APPROXIMATELY 2 TO 2.5 FEET IN LENGTH. [08-08-07] OPERATIONALLY CHECKED EMERGENCY ESCA PE SLIDE AT DOOR 4L 649-9016 MR25718 PER MM 25-66-00, PAGE SERIES 501. AFTER COMPLETION, SIGN-OFF USING NR DATA. SLIDE DID NOT DEPLOY PROPERLY. HAD LARGE SLIT 30" LONG IN LOWER TUBE. APPEARS TO BE DAMAGE INTRODUCED DURING SHIPPING TO UN ITED. NR 4 LT DOOR SLIDE RAFT REMOVED & SERVICABLE SLIDE INSTALLED, AIRCRAFT READY FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007071800320 20070718 00320 2007 7 18 2007UALA02451 4 20070706 A 2565 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU R2 DOOR OUT OF POSITION A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 386UA 24661 CREW REPORTS, DOOR 2R SLIDE PACK HAS SHIFTED AND DROPPED SO FAR THAT THE PULL TAB IS EXPOSED. [07-27-07] REROUTED SLIDE LATCH LANYARD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071800321 20070718 00321 NM 2007 7 18 2007UALA02452 1 20070706 A 5270 PROXIMITY SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L3 DOOR FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 556UA 26650 CREW REPORT, 3L SLIDE ARM LIGHT DOES NOT ILLUMINATE. [08-08-07] SUSPECT FLOOR MOUNTED PROX SWITCHES MIGHT BE BAD. REPLACED AND TESTED OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071800324 20070718 00324 CE 2007 7 18 DXTA200702335 1 20070713 A 2720 RUDDER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL OUT OF TRIM E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 923QS 7500023 RT ELEVATOR ON EICAS SHOWS .3333 DEFLECTION DOWN IN CRUISE FLIGHT. AC YAWS AND THEN EXCESSIVE RUDDER IS NEEDED TO TRIM L EVEL. [07-23-07] ACCOMPLISHED BLEEDING OF HYD. SYSTEM TO ENSURE PROPER OPERATION OF FLIGHT CONTROLS. AFTER BLEEDING & SERVICING OF SYSTEM ALL FLIGHT CONTROLS OPERATED WITHIN SPEC. I/A/W CE750 27-30-00 & SERVICING I/AW/ CE750 MM 12-10-15 . 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071800326 20070718 00326 NM 2007 7 18 2007UALA02453 1 20070706 A 3250 SENSOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NLG STEERING MALFUNCTIONED A UALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 29 844UA 1581 NO NOSE WHEEL STEERING ON TAXI OUT. PROXIMITY SENSOR 28GA FAILURE. REPLACED PROXIMITY SENSOR 28GA. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071800330 20070718 00330 CE 2007 7 18 DXTA200702313 1 20070702 A 2131 21198623 CONTROLLER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CABIN PRESSURE MALFUNCTIONED E DXTA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 07 966QS 6210 7500166 AT FL450 LOST CABIN PRESSURE. CABIN CLIMB RATE +5500 FPM. AMBER CABIN ALT FO SAW CABIN AT 9500. INDICATED EMERGENCY DE SCENT. DIVERTED INTO KNEW. CABIN OXYGEN MASKS USED. VISUALLY INSPECTED INSIDE TAIL COMPT FOR ANY LOOSE DUCTS, BLOWN D UCTS, LOOSE COUPLINGS ETC, NONE FOUND. REMOVED CABIN PRESSURE CONTROLLER AND INSTALLED REPAIRED UNIT. COMPLIED WITH MANU AL CABIN PRESSURE CONTROL SYSTEM OPS CHECK AND BAGGAGE COMPT. ISOLATION SYSTEM FUNCTIONAL CHECK REF MM 21-30-00 WITH NO FAULTS FOUND. REPACKED O2 MASK'S AS REQUIRED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071800333 20070718 00333 CE 2007 7 18 DXTA200702315 1 20070703 A 2150 73838433 ACM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LEAKING E DXTA D RETURN TO BLOCK K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 998QS 1143 1143 7500198 STRONG ODOR OF SOMETHING BURNING IN COCKPIT. REMOVED BOTH COALESCER SOCKS P/N 746451-3 AND INSTALLED 2 NEW SOCKS P/N 74 6451-3. REMOVED THE COCKPIT (AFT) ACM P/N 738384-33 S/N 9808193 AND INSTALLED A REPAIRED UNIT P/N 738384-33 S/N 2002070 59. PERFORMED AN OPS/LEAK CHECK WITH NO DEFECTS NOTED. ALL WORK WAS PERFORMED IAW THE MM 21-51-00 AND 12-10-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071800334 20070718 00334 2007 7 18 2007UALA02456 4 20070708 A 2565 HOSE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE OVERWING SLIDE CONTAMINATED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 654UA 25392 RIGHT OFF WING ESCAPE SLIDE INFLATION HOSE FROM INFLATION CYLINDER IS CONTAMINATED HYDRAULIC FLUID, AREA OF CONTAMINATIO N IS ADJACENT TO THE HYD SYSTEM SERVICING SELECTOR. PRESSURIZED HYD SYSTEMS AND NO LEAKS DETECTED. PIPE IS SPONGY AND WALLS HAVE COLLAPSED FROM LONG TERM CONTAMINATION BY HYD FLUID. REPLACED PIPE ASSY. SLIDE AND AIRCRAFT OK FOR SERVICE . 2 L 7 2 4F 4 F RT A1NM E24NE 2007071800339 20070718 00339 WP 2007 7 18 452051071207 2 20070712 A 7261 30609642 LINE LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE7312 01518 WP ENGINE OIL LEAKING E J7SA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 05 615FX 2051 P116719C LOW OIL PRESSURE IN FLIGHT ON LT ENGINE. AIR DIVERSION, IFE DECLARED BY CONTROL TOWER. LANDING AND TAXI UNEVENTFUL. GA INED ACCESS AND RESEALED NR 6 BEARING (N1 COVER) WITH NEW GASKET. REPLACED NR 6 BEARING PRESSURE LINE WITH NEW LINE. SE RVICED OIL AND PERFORMED ENGINE RUNS AND LEAK CHECKS. 2 L 7 2 4F 4 F RT T00008WI E6WE 2007071800341 20070718 00341 EU 2007 7 18 2007UALA02460 1 20070707 A 5320 BRACKET AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 423UA 504 LEFT BELLY FAIRING SUPPORT BRACKET Y127 IS CRACKED AT FRAME 46 JUST BELOW KEEL BEAM. MAJOR REPAIR ACCOMPLISHED: REPLAC ED ANGLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071800344 20070718 00344 CE 2007 7 18 DXTA200702323 1 20070707 A 3233 99125374 ACTUATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG INOPERATIVE E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 641QS 619 619 5605295 DURING LANDING GEAR EXTENSION THE RT MAIN GEAR WOULD NOT EXTEND AND THE (HYD PRESS) ANNUNCIATOR ILLUMINATED CONTINUOUSLY . THE LANDING GEAR EXTENDED AFTER COMPLETING THE LANDING GEAR WILL NOT EXTEND CHECKLIST. REMOVED AND REPLACED RT MAIN L ANDING GEAR ACTUATOR. CAMBER CHECKS GOOD. OPERATIONAL AND LEAK CHECKS GOOD. WORK DONE IAW MM 32-01-00. RENTAL ACTUAT OR WITH 1421 CYCLES. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007071800345 20070718 00345 2007 7 18 DXTA200702324 4 20070708 A 2210 7000622901 VERTICAL GYRO CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE COCKPIT FAULTY E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 325QS 8363 5600425 AUTOPILOT MALFUNCTION - LEVEL AT 41000 MSL, THE AUTOPILOT AGGRESSIVELY PITCHED UP TO OVER 1000 FPM. THE AUTOPILOT WAS DISCONNECTED. AFTER 1 MINUTE, THE AUTOPILOT WAS RECONNECTED AND PROBLEM REOCURRED. REMOVED FAULTY LT SIDE PITOT STATIC PORT HOSE AND NR 1 VERTICAL GYRO (FAULTY) INSTALLED NEW HOSE AND REPAIRED VG. PERFORMED PITOT STATIC SYSTEM LEAK TEST GOOD. PERFORMED OPERATIONAL CHECK GOOD 2 L 7 2 4F 4 F RT A22CE E25EA 2007071800346 20070718 00346 2007 7 18 DXTA200702325 4 20070710 A 2210 4006719903 ROLL SERVO CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL INOPERATIVE E DXTA O OTHER O OTHER CR CRUISE 1 GL 07 962QS 6662 7500126 AT CRUISE FL 450 WOULD FAIL TRANSFER TO FGB-B AND RESET WITHIN 30 SECONDS THEN FGC B WOULD FAIL TRANSFER TO FGC-A THEN R ESET WITHIN 30 SECONDS. THE AUTOPILOT WOULD DISCONNECT SOMETIMES. GAINED ACCESS TO IMT PAGE. INSPECTED AND FOUND FAULT CODE NR 1250 IAC/AILERON SERVO INTERPAGE ERROR. REQS AFCS TEST ON AILERON SERVO, NOTED AILERON SERVO BREAK OUT. AMPERAG E EXCESSIVE HIGH. REPLACED AILERON SERVO WITH REPAIRED UNIT. OPS CHECK GOOD. WORK DONE IAW MM CHAPTER 22-10-01. OLD P/N : 400-6719-903. OLD S/N: 000-130-65. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071800347 20070718 00347 EU 2007 7 18 2007UALA02461 1 20070707 A 5320 ANGLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 423UA 504 AT C-CHECK FOUND RIGHT BELLY FAIRING SUPPORT BRACKET Y127 UPPER ANGLE IS CRACKED AT FRAME 46 JUST BELOW KEELBEAM. REPLA CED BRACKET Y127 AT C CHECK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071800349 20070718 00349 CE 2007 7 18 DXTA200702326 1 20070710 A 3222 STRUT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG OVERSERVICED E DXTA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 GL 07 915QS 7500015 AFTER TAKEOFF LANDING GEAR HANDLE WOULD NOT MOVE TO ALLOW RETRACTION OF GEAR, ABOUT 40 SECONDS LATER A SMALL THUMP OCCUR RED AND WE WERE ABLE TO RETRACT. JACKED AIRCRAFT, FOUND NOSE STRUT TO EXTEND TO FULL LENGTH. PERFORMED GEAR SWINGS. NO DISCREPANCY NOTED. RESERVICED NOSE STRUT WITH NITROGEN AND FLUID, IAW MM CH 12-10-38. FINAL GEAR SWING OPERATIONAL CHEC K GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071800351 20070718 00351 EU 2007 7 18 2007UALA02463 1 20070707 A 2797 WIRE HARNESS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RUDDER FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 482UA 1584 RUDDER TRAVEL LIM MESSAGE RECEIVED. FOUND A BROKEN WIRE IN STA2456-FR53. REPAIRED WIRE IN BUNDLE AND REPLACED RUDDER T RAVEL LIMITATION UNIT AS PRECAUTION. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071800353 20070718 00353 NM 2007 7 18 2007UALA02465 1 20070706 A 5310 DOOR FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 924UA 26645 FWD CARGO DOOR CUTOUT, AFT FRAME IS CRACKED ON AFT SIDE OF FRAME IN RADIUS ADJACENT TO UPPER I/B CORNER OF LOWER BOTTOM STOP FITTING. [07-27-07] MAJOR REPAIR: -REMOVED CRACK AND ACCOMPLISHED ANGLE REPAIR PER MM 53-30-75. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071800354 20070718 00354 NM 2007 7 18 2007UALA02466 1 20070706 A 5210 TORQUE TUBE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT ENTRY DOOR EXCESS PLAY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 AFT ENTRY DOOR CUTOUT TORQUE TUBE HAS MOVEMENT BEYOND .003 INCH. [07-31-07] REMOVED TORQUE TUBE, SPIGOT, AND BOTH GUID E PLATES WITH BEARINGS. REINSTALLED BOTH GUIDE PLATES WITH NEW BEARINGS AND INSTALLED NEW TORQUE TUBE AND SPIGOTS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071800356 20070718 00356 NM 2007 7 18 2007UALA02468 1 20070706 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 FUSELAGE SKIN DENTED AT STA 870 STR 28R TO STR 28L. [07-27-07] MAJOR REPAIR: REMOVED DAMAGE. ACCOMPLISHED A DOUBLE R REPAIR. ALSO REPLACED THE CRACKED SHEAR TIE IN THE AFT PIT. REFERENCE SRM 53-00-07 REPAIR 4. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071800364 20070718 00364 EA 2007 7 18 TRAX200700939 1 20070705 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH FADED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 ALL CREW ESCAPE HATCH EXTERNAL PLACARDS ARE FADED. 2 L 7 2 4F RT A21EA 2007071800366 20070718 00366 EA 2007 7 18 TRAX200700948 1 20070706 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 STA 605 FRAME HAS CORROSION BETWEEN STR 27 AND 26 LEFT. COMPLIED WITH EC/TC REO 601R-53-61-2260. 2 L 7 2 4F RT A21EA 2007071800367 20070718 00367 EA 2007 7 18 TRAX200700950 1 20070706 A 2520 RAIL CNDAIR CL600 CL6002C10 1390015 EA CABIN SEAT CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 753EV 10169 CORROSION ON LEFT SIDE CABIN SEAT SIDE RAIL FS 677.00 TO 708.00. 2 L 7 2 4F RT A21EA 2007071800368 20070718 00368 EA 2007 7 18 TRAX200700951 1 20070706 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 753EV 10169 CORROSION ON RT SIDE CABIN FLOOR RAIL FS 349.00 TO 485.00. 2 L 7 2 4F RT A21EA 2007071800371 20070718 00371 EA 2007 7 18 TRAX200700955 1 20070706 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 FLOOR SUPPORT BEAM TO AFT PRESSURE BULKHEAD ATTACH FITTING AT LBL 27 HAS CORROSION. 2 L 7 2 4F RT A21EA 2007071800373 20070718 00373 EA 2007 7 18 TRAX200700959 1 20070706 A 5313 STRINGER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 ASD FLOOR SUPPORT STRINGER CORRODED BETWEEN FS 310-349. WORK COMPLETED IN ACCORDANCE WITH: SRM`S 51-42-21, 51-40-11, & 51-42-06, AMM 52-70-04, & 52-70-04 NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007071800376 20070718 00376 NM 2007 7 18 SWAA073360 1 20070708 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 249WN 34951 MID CABIN EEPLS COVER LOOSE. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007071800379 20070718 00379 NM 2007 7 18 SWAA073371 1 20070709 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 827, STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007071800380 20070718 00380 NM 2007 7 18 SWAA073375 1 20070709 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071800381 20070718 00381 NM 2007 7 18 SWAA073378 1 20070709 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071800382 20070718 00382 WP 2007 7 18 07FDEA02459 1 20070713 A 5322 SHEAR TIE DOUG DC10 DC1010 3022110 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 CTR CARGO COMPT TUNNEL ON SHEAR CLIP FOUND CRACK. REPAIRED SHEAR CLIP IAW SRM 53-30-00 VOL1 FIG 10. 2 L 7 3 4F A22WE 2007071800383 20070718 00383 WP 2007 7 18 07FDEA02460 1 20070713 A 5330 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 100 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 EXISTING DOUBLER EXTERNAL SKIN. REPAIRED AREA IAW SRM 53-20-00 FIG 6 VOL 1, SRM 51-00-01 VOL 1 AND DWG NCA6012. 2 L 7 3 4F A22WE 2007071800384 20070718 00384 WP 2007 7 18 07FDEA02461 1 20070713 A 5347 SEAT TRACK DOUG DC10 DC1010F 3022111 WP ZONE 200 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 EXISTING SEAT TRACK SPLICE REPAIR MAIN CABIN. REPAIRED AREA IAW SRM 53-70-00 FIG 1 VOL 1 AND SRM 51-31-00 VOL 2 PAR 6. 2 L 7 3 4F A22WE 2007071800386 20070718 00386 WP 2007 7 18 07FDEA02463 1 20070713 A 5512 SB1055001615 PANEL DOUG DC10 DC1010F 3022111 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 DURING INSPECTION OF UPPER INTERIOR SKIN PANELS OF STB HORIZONTAL SECTION FOUND 1 PANEL P/N 7207-1 WITH CRACK. ACCOMP LISHED EA NR 8-5510-96123. 2 L 7 3 4F A22WE 2007071800389 20070718 00389 NM 2007 7 18 07FDEA02467 1 20070713 A 5753 RIB BOEING 727 727233 138408A NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LEFT OB MID FLAP OB END RIB WEDGE CLIP AND SEAL RETAINER ANGLE ALL CRACKED AT AFT REAR CORNER OF FLAP. REMOVED LT, O/B MIDFLAP, REPLACED WITH SERVICABLE UNIT, REINSTALLED ON NON-ROUTINE #N00234. 2 L 7 3 4F RT A3WE 2007071800390 20070718 00390 EA 2007 7 18 QXEA200701109 1 20070613 A 5730 PANEL CNDAIR CL600 CL6002C10 1390015 EA LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 C3 OKC - LEFT WING PANEL 584ET CHAFED. REPAIRED IAW SRM 51-12-00, 57-52-01, 51-21-11. 2 L 7 2 4F RT A21EA 2007071800391 20070718 00391 EA 2007 7 18 QXEA200701115 1 20070618 A 5320 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 C3 OKC - FS 280 AT LBL 9 IS CRACKED. REPAIRED IAW REO670-53-11-045. 2 L 7 2 4F RT A21EA 2007071800393 20070718 00393 NM 2007 7 18 QXEA200701119 1 20070710 A 2150 SWITCH DHAV DHC8 DHC8202 2809007 NM OVERTEMP UNKNOWN A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 369PH 513 PDX FLIGHT NR 2140 WHILE IN CRUISE FLIGHT, RECEIVED MASTER CAUTION "AIR CONDITION PACK HOT" WE FOLLOWED APPROPRIATE ABNO RMAL CHECKLIST PROCEDURES. PACK HOT CAUTION CONTINUED TO CYCLE THROUGHOUT DESCENT. MAINTENANCE GROUND RAN COULD NOT DU PLICATE, NO PACK HOT CAUTION LIGHT. REPLACED PACK COMPRESSOR DISCHARGE OVERTEMP SWITCH AS A PRECAUTIONARY MEASURE, IAW D-8-200 MM 21-50-31, PAGE 401-405. GROUND RAN LEAK CHECK OK. NO PACK HOT CAUTIONS NOTED. AIRCRAFT RETURNED TO SERVICE . 2 H 7 2 4T RT A13NM 2007071600023 20070716 00023 EU 2007 7 16 07FDEA02391 1 20070707 A 3243 BRAKE ASSY AIRBUS 300 A300B4622R 3930312 EU MLG MALFUNCTIONED A FDEA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 SO 25 729FD 657 A/C POSITIONED AT THE HOLD SHORT LINE WITH PARKING BRAKE SET. RELEASED BRAKE AND ATTEMPTED TO TAXI FOR TAKEOFF A/C WOUL D NOT MOVE. PARKING BRAKE RESET GOT PERMISSION FROM TOWER TO POWER UP. RELEASED PARKING AGAIN. POWERED UP TO 45 PERC ENT N1 WITH NO MOVEMENT OF A/C. TOWED AIRCRAFT BACK TO GATE WITH NO PROBLEMS. I.E. PARKING BRAKE RELEASED NORMALLY. P ARKING BRAKE ADJUSTMENT TEST IN PROGRESS. TOWED AIRCRAFT BACK TO GATE WITH NO PROBLEMS. I.E. TOWED A/C BACK TO GATE. PARK BRAKE FUNCTIONED NORMALLY, AFTER RE-CYCLING BRAKE HANDLE SEVERAL TIMES ON GATE CARRIED OUT PARKING BRAKE/ULTIMATE EMERGENCY BRAKING OPERATIONAL TEST PER AM 32-45-00- 5. NO FAULTS FOUND, CHECKS SERVICEABLE. 2 L 7 2 4F RT A35EU 2007071600030 20070716 00030 NM 2007 7 16 07FDEA02399 1 20070709 A 5320 65672505 ANGLE BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LWR AFT CARGO PIT, STA 1166 BULKHEAD WALL STRUCTURE. UPPER HORIZONTAL L-ANGLE, JUST BELOW FLOORBEAM, 3 FASTENER HOLES H AVE CORROSION ON BACK SIDE. REMOVED ANGLE REF SRM 51-30-2. FABRICATED NEW ANGLE REF DWG 65-67250-2 AND SRM 51-30-5. I NSTALLED NEW L-ANGLE REF SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007071600031 20070716 00031 NM 2007 7 16 07FDEA02400 1 20070709 A 5322 69436833 SHEAR TIE BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD PIT BILGE BODY FRAME SHEAR TIE IS CRACKED BS 720C, STR 25L- 26L, WL 152 (MKD). REMOVED SHEAR TIE BS 720C STR 25L-26 L IAW SRM 51-30-2. INSTALLED NEW SHEAR TIE P/N 69-43683-3 A TAG NR A49331 IAW SRM 51-30-2 PAGE 2 AND SRM 51-20-4 PAGE 1 . 2 L 7 3 4F RT A3WE 2007071600033 20070716 00033 NM 2007 7 16 07FDEA02408 1 20070709 A 5347 6586245 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 AFT UPPER MAIN DECK, CORROSION ON LWR O/B FLANGE OF SEAT TRACK STA 950 10" TO 950B 10" RBL 47". REMOVED CORROSION REF SR M 51-10-6 AFTER BLEND. ORIGINAL MATERIAL "T" .081 AFTER BLEND MATERIAL REMAINING .052 FOR A MATERIAL LOSS OF .029 AND W AS OUT OF LIMITS REF SRM 53-10-1 FIG 3. REMOVED TRACK REF SRM 51-30-2. FABRICATED NEW TRACK REF IAW SRM 53-10-5 AND D WG 65-86245. INSTALLED NEW TRACK REF SRM 51-30-2 AND DWG 65-86245 2 L 7 3 4F RT A3WE 2007071600035 20070716 00035 EU 2007 7 16 TRBA2007040 1 20070707 A 3350 7012210 LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS BURNED OUT A TRBA O OTHER O OTHER NR NOT REPORTED 1 SO 29 348AE 349 INTERIOR EMERGENCY EXIT LIGHT (UNDER LT EMERGENCY EXIT WINDOW) BURNED OUT. REMOVED AND REPLACED LAMPS AS PER MM NR 33-5 1-00 AND FOUND WORKING PROPERLY AT THIS TIME. 2 H 7 2 4T RT A53EU 2007071600044 20070716 00044 NM 2007 7 16 07FDEA02425 1 20070711 A 5322 65561156 SHEAR TIE BOEING 727 727233 138408A NM BS 720C CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD PIT BILGE BODY FRAME SHEAR TIE IS CORRODED BS 720C, STR 28L- 28R WL 148. REMOVED SHEAR TIE DOUBLER, REMOVED CORROS ION FROM SHEAR TIE AND DOUBLER. TREATED AND PRIMED SHEAR TIE. INSTALLED NEW SHEAR TIE DOUBLER. NDT FOUND SHEAR TIE WI THIN LIMITS, FOUND SHEAR TIE DOUBLER OUT OF LIMITS REF 51-10-2 PG 7, SRM 51-30-2 PG 2,3 SRM 51-10-6, SRM 53-10-1. SHEAR TIE ORIGINAL MATERIAL THICKNESS IS .063", MATERIAL REMAINING IS .057". 2 L 7 3 4F RT A3WE 2007071600047 20070716 00047 EU 2007 7 16 07FDEA02427 1 20070711 A 5315 A53773558 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 TOP CAP BEAM C30 LT IS CORRODED TOP CAP BEAM SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207 AND SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007071600048 20070716 00048 NM 2007 7 16 07FDEA02428 1 20070711 A 5320 69477072 BRACKET BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 A/C DISTRIBUTION BAY BS 740 LBL 6" A/C DUCT SUPPORT BRACKET IS CRACKED ON BULKHEAD ATTACH FLANGE. REMOVED CRACKED SUP PORT BRACKET. VERIFIED MATERIAL AND FABRICATED NEW BRACKET. TREATED, PRIMED, AND INSTALLED NEW BRACKET REF SRM 51-30-2 ,PG 13-14/ SRM 51-10-2,PG 1, BOEING DRAWING NR 69-47707. 2 L 7 3 4F RT A3WE 2007071600061 20070716 00061 NM 2007 7 16 QXEA200701095 1 20070706 A 2133 88060B010003 OUTFLOW VALVE BOMBDR DHC8 DHC8402 1390042 NM CABIN PRESSURE MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 428QX 114 3 4160 SEA FLIGHT NR 2381: ON THE CLIMB-OUT OF BZN, OUT OF 8000 FT, NOTICED THE FAULT LIGHT ON THE PRESS PANEL. FOLLOWED THE C HECKLIST. RAN IT ON MANUAL. NO FURTHER PROBLEMS. MAINTENANCE FOUND CDS REPORTED AFT OUTFLOW VALVE FAIL. REPLACED AFT OUTFLOW VALVE PER Q400 AMM 21-31-16-000-801 AND 21-31-16-400-801. TESTS GOOD. ALSO, PERFORMED VISUAL INSPECTION OF PAX AND AFT CARGO DOOR SEALS. SEALS REMAINED INFLATED ON RESERVOIR AIR ALONE. NO LEAKS AT THIS TIME. ALSO, PERFORMED OPS CHECK OF AUTO PRESSURIZATION CONTROL PER Q400 AMM 21-31-00-710-802. TESTS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071600068 20070716 00068 NM 2007 7 16 07FDEA02412 1 20070710 A 5320 65586001 ANGLE BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 AFT PIT FWD BULKHEAD BRACKET AT STA 950 WL 146 RBL 21-24 CORRODED. REPLACED ANGLE IAW SRM 53-10-1 THIS IS CLASSIFIED AS A MINOR REPAIR REF BAC65-58600, SRM 51-30-2. 2 L 7 3 4F A3WE 2007071600073 20070716 00073 NM 2007 7 16 QXEA200701092 1 20070708 A 6120 RELAY DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS MALFUNCTIONED A QXEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 09 361PH 516 SEA FLIGHT NR 2033 - ON TAKEOFF ROLL OUT OF SEA, AUTOFEATHER FAILED TO ARM, TAKEOFF WAS ABORTED AT APPROXIMATELY 65 KTS. COMPLIED WITH AUTO FEATHER ARMING POTENTIOMETER ADJUSTMENT/TEST. NO ADJUSTMENT OF POTENTIOMETERS REQUIRED. REPLACED 6121-K5 RELAY/COMPLIED WITH FUNCITON CHECK OF THE AUTO FEATHER SYSTEM. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071600076 20070716 00076 NM 2007 7 16 QXEA200701055 1 20070625 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 467 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - CORROSION AT FORWARD LOWER FLANGE OF FRAME X467.00 JUST OUTBOARD OF LEFT STRINGER 25. REPAIRED IAW SRM 51-20- 11, 51-40-11, 51-30-26, AND 51-20-51. 2 H 7 2 4T RT A13NM 2007071600079 20070716 00079 NM 2007 7 16 QXEA200701058 1 20070626 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 333 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX-CABIN UNDER FLOOR LEFT AT FRAME X333.300 AND BETWEN STRINGER 29L AND 30L, AFT SIDE, FRAME CASTELLATION HAS CORROS ION AT FASTENERS. REPAIRED IAW SRM 51-20-11, 51-40-11, 51-20-26. 2 H 7 2 4T RT A13NM 2007071600080 20070716 00080 NM 2007 7 16 QXEA200701059 1 20070624 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 270 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX-CABIN UNDER FLOOR LEFT AT FRAME X270.500 AND BETWEEN STRINGER 30L AND 31L, FRAME CASTELLATION CORROSION AT FASTEN ERS. REPAIRED IAW SRM 51-20-11, 51-40-11, AND 51-20-26. 2 H 7 2 4T RT A13NM 2007071600087 20070716 00087 NM 2007 7 16 07FDEA02438 1 20070712 A 5713 ARB75151 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 LT WING FUEL TANK AT STRINGER 15 FOUND CRACKED. [07-24-07] SLOTTED OUT AND REPAIRED AS PER SRM 57-20-00, FIG 11, V OL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007071700007 20070717 00007 CE 2007 7 17 GLBA20060960 1 20070701 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA BS 423 DAMAGED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 247GL UE247 HOLE IN FUSELAGE ON THE RT SIDE FORWARD OF FS 423.25 AND 2 INCHES ABOVE STRINGER 12R. APPROXIMATELY 1 INCH V SHAPE HOLE/ CUT. MAINTENANCE REPAIRED AFFECTED AREA WITH A FLUSH REPAIR IAW MFG SRM 51-70. RII COMPLIED WITH IAW TASKCARD 8.2.1. HOL E CUTOUT SIZE 1.3 INCH X 1.3 INCH. 2 L 7 2 4T 3 T RT A24CE E2NE 2007071700022 20070717 00022 EA 2007 7 17 A6WA200740352 1 20070624 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AW 7878 PAX DOOR AFT DRAG ANGLE CRACKED APROX .7 INCH LONG IN AREA OF PULLEY BRACKET. MAINTENANCE CUT AWAY CRACKED SECTION OF D RAG ANGLE AND INSTALLED REPAIR ANGLE IAW REO 601R52-11-513, REV A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700025 20070717 00025 EA 2007 7 17 A6WA200740308 1 20070612 A 3230 46193 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE MLG INOPERATIVE A A6WA O OTHER S AFFECT SYSTEMS DE DESCENT 1 GL 31 438AW 10532 7748 GOT GEAR DISAGREE WHEN LOWERING GEAR FOR LANDING. CYCLED GEAR UP AND DISAGREE WITH GEAR UP ALSO. COMPLIED WITH DISAGRE E CHECKLIST AND HAD NORMAL INDICATION. REMOVED AND REPLACED MLG PRIORITY VALVE IAW AMM 32-32-15. OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700031 20070717 00031 EA 2007 7 17 A6WA200740315 1 20070614 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SILL CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 434AW 7322 LOWER SILL JOINT BRACKET (PN 601R38335-1) CORRODED AT FS 318.70, RBL 36, WL 73. MAINTENANCE REMOVED AND REPLACED BRACKE T (PN 601R38335-1) IAW CRJ 200 SRM 51-42-21. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700035 20070717 00035 EA 2007 7 17 A6WA200740319 1 20070618 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 460AW 7867 FLOOR SUPPORT ANGLE AT FS 621, WL 73, RBL 27 - 45 IS CRACKED .5 INCH LONG. MAINTENANCE REPAIRED FS 621 ANGLE IAW REO 6 01R-53-61-117, REV C. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700037 20070717 00037 EA 2007 7 17 A6WA200740321 1 20070621 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 31 418AW 7618 FLAP FAIL CAS CAUTION MESSAGE IN CRUISE FLIGHT. FLAPS FAILED AT ZERO. QRH COMPLIED WITH. BRAKE TEMPS INDICATE 4,4,5,6 , COMPLIED WITH RESET PROCEDURE IAW SUPP 98-018B, STEPS 1.3 AND 1.4. FLAP SYSTEM RESET, OK. REMOVED AND REPLACED LT BP SU, OPS CHECK GOOD IAW AMM 27-51-00. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700050 20070717 00050 EA 2007 7 17 A6WA200740336 1 20070623 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 462AW 7875 LT FS 625 OBLIQUE ANGLE IS CRACKED APPROX 1 INCH L. MAINTENANCE REMOVED AND REPLACED ANGLE IAW SRM 51-42-06, 51-42-21 A ND REO 601R-53-61-422. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700051 20070717 00051 EA 2007 7 17 A6WA200740337 1 20070623 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 432AW 7875 RT FS 625 OBLIQUE ANGLE IS CRACKED APPROX 1 INCH L. MAINTENANCE REMOVED AND REPLACED ANGLE IAW SRM 51-42-21 AND REO 60 1R-53-61-422. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700066 20070717 00066 NM 2007 7 17 AMTA200700320 1 20070703 A 2841 INDICATOR BOEING 737 73783N 13844HI NM FUEL QTY INOPERATIVE A AMTA O OTHER P NO WARNING INDICATION CR CRUISE 1 GL 11 310TZ 28243 CENTER TANK QUANITY INDICATOR BLANK, NOT SHOWING ANY QUANITY. PERFORMED FQIS BITE PROCEDURE IAW FIM 28-41-00-810-810. NO FAULTS DETECTED. OK FOR SERVICE. (K) 2 L 7 2 4F RT A16WE 2007071700117 20070717 00117 NM 2007 7 17 QXEA200701061 1 20070624 A 5313 STRINGER DHAV DHC8 DHC8202 2809007 NM BS 201 S31L CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - CABIN UNDER FLOOR LEFT FORWARD OF FRAME X201.300 AND OUTBOARD OF STRINGER 31L, STRINGER HAS CORROSION AT FASTEN ERS. REPAIRED IAW SRM 51-20-11, 51-20-26, 51-20-36. 2 H 7 2 4T RT A13NM 2007071700123 20070717 00123 NM 2007 7 17 QXEA200701068 1 20070627 A 5313 STRINGER DHAV DHC8 DHC8202 2809007 NM BS 488 S24 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX-CORROSION FOUND AT STRINGER 24 FRAME 488, REF NON ROUTINE 00234 FOR WORK PERFORMED IN ERROR AT THIS STRINGER AND FRAME LOCATION. THIS CARD IS REWORK. REPAIRED IAW SRM 51-20-11, 51-40-11, AND 51-20-26. 2 H 7 2 4T RT A13NM 2007071700135 20070717 00135 NM 2007 7 17 AWXA200700814 1 20070703 A 5340 69560374 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - CRACKED STRINGER CLIP, BS 616, S5R. REPLACED STRINGER CLIP, BS 616, S5R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071700144 20070717 00144 NM 2007 7 17 AWXA200700804 1 20070709 A 5330 6518420 SKIN BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 PHX - MAJOR REPAIR - NR 3927251, CRACK AT FIRST OFFICERS NR 1 WINDOW POST SKIN UPPER RIGHT CORNER, BS 196.5 - BS 203.8, S9R - S10R. REPAIRED FIRST OFFICERS NR 1 WINDOW POST SKIN UPPER RIGHT CORNER, BS 196.5 - BS 203.8, S9R - S10R IAW B737 -300 SRM 53-10-01-2R. 2 L 7 2 4F RT A16WE 2007071700146 20070717 00146 NM 2007 7 17 AWXA200700824 1 20070707 A 5347 D571347200 SEAT TRACK AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5971950, CORROSION ON CABIN SEAT TRACK, FR 36/BS 1430 - FR 41/1650, +Y765. REPLACE D CABIN SEAT TRACK, FR 36/BS 1430 - FR 41/1650, +Y765 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007071700148 20070717 00148 NM 2007 7 17 AWXA200700826 1 20070707 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR# 5962280, CRACKED STRINGER CLIP, BS 578, S4R. REPLACED STRINGER CLIP, BS 578, S4R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071700150 20070717 00150 NM 2007 7 17 AWXA200700828 1 20070703 A 5340 50794873 ATTACH FITTING BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5982114, CRACKED INTERCOSTAL TO FRAME ATTACH CLIP ( CHANNEL), BS 360, S6L. REPLACE D INTERCOSTAL TO FRAME ATTACH CLIP ( CHANNEL), BS 360, S6L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071700151 20070717 00151 NM 2007 7 17 AWXA200700829 1 20070706 A 5320 6545834525 INTERCOSTAL BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5962209, CRACKED INTERCOSTAL, BS 344 - BS 360, BL 0, WL 208.1. REPLACED INTERCOSTA L, BS 344 - BS 360, BL 0, WL 208.1 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071700154 20070717 00154 NM 2007 7 17 AWXA200700832 1 20070628 A 5320 143N851112 WEB BOEING 757 757225 1384959 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - NR 5978954, FORWARD CARGO COMPARTMENT DOOR CUT OUT WEB CRACKED, BS 560, S19R - S21R. REPLACED FORWARD CARGO COMPARTMENT DOOR CUT OUT WEB, BS 560, S19R - S21R IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007071700163 20070717 00163 SO 2007 7 17 RAIA00706042 1 20070630 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 816HK 145055 PRE FLT 5584 - STL - EMERGENCY LIGHT AT ROW 16 INOP. MAINTENANCE REMOVED AND REPLACED THE BULB. 2 L 7 2 4T RT T00011AT 2007071700166 20070717 00166 SO 2007 7 17 RAIA00707002 1 20070701 A 3350 RPS1B BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DISCHARGED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 825HK 145510 PRE FLT 5587 - STL - EMERGENCY LIGHTS INOP THROUGHOUT THE CABIN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT B ATTERY PACK. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007071700189 20070717 00189 SO 2007 7 17 C2XA07IA156 1 20070628 A 3260 355022002 ELECTRONIC UNIT EMB 145 EMB145LR 3260212 SO MLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13989 4849 4849 145271 OMA - FLIGHT 2748, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL INDICATION ON CLIMB. THE AIRCRAFT RETURNED TO OMA W HERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND IT WAS FERRIED TO MCI WHERE MAINTENANCE REMOVED AND REPLACED THE LGEU, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . 2 L 7 2 4T RT T00011AT 2007071700194 20070717 00194 NM 2007 7 17 UPS07M50125 1 20070418 A 5712 ARB2850506 RIB DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C RIGHT WING L/E SLAT TRACK NR 16 I/B SUPPORT RIB FOUND CRACK. RIGHT WING L/E SLAT TRACK NR 16 ATTACHIN G PARTS & WIRE HARNESS REMOVED. NR 16 CRACK I/B SUPPORT RIB REMOVED. HOLES TRANSFERRED TO NEW NR 16 RIB ASSY. RIGHT W ING L/E SLAT TRACK NR 16 I/B NEW RIB P/N: ARB2850-506 & RELATED PARTS & WIRE HARNESS INSTALLED. CABLE ADJUSTMENT & RIG HT SLAT OPERATION CHECK C/OUT FOUND SATIS. 2 L 7 3 4F RT A22WE 2007071800004 20070718 00004 NM 2007 7 18 DLM88070880 1 20070708 A 3260 TARGET DOUG MD88 MD88 3023688 NM LT MLG OUT OF ADJUST A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 909DL 49540 LEFT MAIN GEAR UNSAFE RED LIGHT ON WITH GEAR UP AFTER. TAKEOFF CYCLING GEAR NO HELP. LANDING GEAR MTC IN PROGRESS. FO UND TARGET FAR ON PROX BOX F16. ADJUSTED PROX SENSOR WITH LIMITS PER AMM. JACKED A/C AND CYCLED LANDING GEAR. CHECKS GOOD ON GEAR SWING AND AT PROX BOX. 2 L 7 2 4F RT A6WE 2007071800033 20070718 00033 NM 2007 7 18 HNAA0700064 1 20070409 A 3350 6013211 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN FAULTY A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 827EX 30539 30539 390 EMERGENCY LIGHTS (FRONT TWO) GLOWED AFTER EMERGENCY LIGHT SWITCH IS TURNED OFF. REPLACED EMERGENCY BATTERY PACK AT ROW 8 LEFT. 2 H 7 2 4T RT A13NM 2007071800034 20070718 00034 NM 2007 7 18 HNAA0700143 1 20070707 A 5313 STRINGER DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 839EX 226 LITE CORROSION ON STR 29 BETWEEN X488.500 AND X510.00. 2 H 7 2 4T RT A13NM 2007071800036 20070718 00036 NM 2007 7 18 NOCA13607 1 20070709 A 3397 WIRE BOEING 757 75728A 1384976 NM CABIN BROKEN A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 750NA 26277 SECTION OF E-PATH LIGHTING INOP AT L3 DOOR. FOUND BROKEN WIRE IN A FEW SPOTS AND RE-SPLICED WIRE, OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2007071800037 20070718 00037 EU 2007 7 18 SA07047 1 20070708 A 3260 TARGET AIRBUS A319 A319112 3930323 EU NLG OUT OF ADJUST A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 708UW 0972 FLIGHT 1026, TPA-CLT: AFTER TAKEOFF, CREW RECEIVED A NOSE LANDING GEAR SHOCK ABSORBER FAULT. RETURNED TO TPA. MAINTEN ANCE ADJUSTED THE NOSE GEAR PROX SENSOR TARGETS. 2 L 7 2 4F RT A28NM 2007071800041 20070718 00041 SO 2007 7 18 RAIA00707007 1 20070705 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 810HK 145231 PRE FLT 5495 - STL - EMERGENCY EXIT LIGHT AT LEFT OVERWING EXIT IDENTIFIER INOP. MAINTENANCE RESECURED A LOOSE CONNECTI ON TO THE LIGHT ASSEMBLY. 2 L 7 2 4T RT T00011AT 2007071800042 20070718 00042 SO 2007 7 18 RAIA00707006 1 20070704 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 838HK 145321 PRE FLT 8038 - IAD - EMERGENCY LIGHT AT LEFT HAND OVERWING EXIT INOP. MAINTENANCE SECURED A LOOSE CONNECTION TO THE LIG HT ASSEMBLY. 2 L 7 2 4T RT T00011AT 2007071800064 20070718 00064 NM 2007 7 18 UPS07550138 1 20070613 A 5311 143N102490 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 420UP 23907 INSPECTION TYPE:C DENT IN FWD CARGO FUSELAGE FRAME STA 800, S23R TO S24R. ACCOMPLISHED FINAL REPAIR AT STA 800, S23R - S24R, PER FINAL EA 757-5332-27-A1691 AND UPS EO B757-5310-27128-A, NO DEVIATIONS. 2 L 7 2 4F RT A2NM 2007071800066 20070718 00066 WP 2007 7 18 UPS07850129 1 20070617 A 5522 SKIN DOUG DC8 DC871F 302199D WP LT ELEVATOR DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 LEFT ELEVATOR LWR INBOARD SKIN HAS DEEP DENT. CUT OUT DAMAGED AREA ON L/ELEV INBOARD SKIN IAW SRM 55 -02-01 FIG 010, FABRICATED AND INSTALLED REPAIR DOUBLER ON L/ELEV INBOARD LWR SKIN IAW SRM 55-02-01 FIG 010. 2 L 7 4 4F RT 4A25 2007071800067 20070718 00067 NM 2007 7 18 DLM90070867 1 20070617 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 602-601 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 LT CUSP WEB AT FS 602 AND 621 OUT OF LIMITS. CORROSION REPAIRED CUSP WEB IAW MD-80 SRM 53-05D FIG 827D. 2 L 7 2 4F RT A6WE 2007071800071 20070718 00071 NM 2007 7 18 UPS07M50127 1 20070706 A 2560 INDICATOR DOUG MD11 MD11F 3023600 NM RT EVAC SLIDE NOT SEATED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 274UP 48575 INSPECTION TYPE:N/A FOUND RIGHT DOOR EVACUATION SLIDE REMOTE PRESS-TO-TEST SWITCH FAILED. DEFERRED M353996. *S/D* RE- SEATED THE PRESSURE INDICATOR ASSY PER AMM 25-61-04-4. C/W OPS TEST PER AMM 25-61-04-5. RESULT NORMAL. THIS CLOSES WA N 1257616 AND DI M 353996. PLACARD REMOVED. 2 L 7 3 4F RT A22WE 2007071800078 20070718 00078 NM 2007 7 18 AALA20071230 1 20070703 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 789AN 30252 JFK - EMERGENCY LIGHT AT SEAT 21C HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007071800082 20070718 00082 WP 2007 7 18 AALA20071240 1 20070704 A 2611 855020 SMOKE DETECTOR DOUG DC9 DC982 3022082 WP CARGO BAY INOPERATIVE A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 7543A 53025 LIT - PHL TO DFW - AFT CARGO FIRE WARNING LIGHT ILLUMINATED. EMERGENCY DECLARED AND LANDED LIT WITHOUT INCIDENT. AIRC RAFT INSPECTED AND CONFIRMED NO FIRE. REPLACED CARGO COMPARTMENT SMOKE DETECTOR. SYSTEM GROUND CHECKED NORMAL OPERATIO N. 2 L 7 2 4F A6WE 2007071800083 20070718 00083 WP 2007 7 18 AALA20071256 1 20070706 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 475AA 49650 LGA - EMERGENCY EXIT LIGHTS AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS AT RI GHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071800084 20070718 00084 NM 2007 7 18 UPS07M50128 1 20070705 A 3350 6044115 BATTERY DOUG MD11 MD11F 3023600 NM CABIN DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 281UP 48538 INSPECTION TYPE:N/A EMERGENCY LIGHT BATTERY LOW ALERT ILLUMINATED DURING EMERGENCY LIGHT TEST. DEF NR 353905. T/S C/O IAW FIM 33-51-01-00. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY IAW MM 33-51-01-4. OPS CHECKED SATISFAC TORY. THIS CLOSES DMI. 2 L 7 3 4F RT A22WE 2007071800085 20070718 00085 WP 2007 7 18 AALA20071233 1 20070704 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70425 49337 LGA - OVERHEAD EMERGENCY LIGHTS AT SEATS 6B TO 7B INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT S EATS 6B TO 7B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071800086 20070718 00086 NM 2007 7 18 AALA20071236 1 20070704 A 3397 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 792AN 30253 ORD - EMERGENCY LIGHTS AT SEAT ROWS 35 TO AFT OF CABIN INOPERATIVE. FOUND LOOSE CONNECTOR AT SEAT 35. REINSTALLED CON NECTOR FOR EMERGENCY LIGHTS AT SEAT ROWS 35 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007071800100 20070718 00100 WP 2007 7 18 ASAA0781850 1 20070704 A 5311 9957739511 FRAHM DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 AFT CARGO FRAME CORRODED AT BS 1287 BETWEEN LONG 29L AND LONG 29R. REMOVED DAMAGED SECTION OF FRAME, LOCATED, DRILLED A REPLACEMENT FRAME IAW SRM 53-3 FIG 2A AND DAC DWG 9957739. 2 L 7 2 4F RT A6WE 2007071800101 20070718 00101 WP 2007 7 18 ASAA0781854 1 20070704 A 5753 5910042511 SKIN DOUG DC9 DC983 3022083 WP T/E FLAP VANE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 LT WING I/B FLAP I/B VANE DENTED ON LWR SURFACE NEXT TO PREVIOUS REPAIR EDGE. REMOVED EXISTING REPAIR, PREPAIRED SURFAC E, FABRICATED DOUBLER AND INSTALLED IAW SRM 57-03 FIG 9A AND 51-70-2 FIG 12. 2 L 7 2 4F RT A6WE 2007071800119 20070718 00119 WP 2007 7 18 AALA20071199 1 20070628 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 441AA 49460 LGA - EMERGENCY LIGHTS IN CEILING FROM SEAT ROWS 23 TO 27 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN CE ILING FROM SET ROWS 23 TO 27. SYSTEM ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071800121 20070718 00121 NM 2007 7 18 AALA20071218 1 20070630 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 605AA 27056 PHL - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 9 TO 18 LEFT ON OVERNIGHT AND INOPERATIVE. REPLACED BATTERY PACK FOR E MERGENCY LIGHTS AT SEAT ROWS 9 TO 18. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071800123 20070718 00123 NM 2007 7 18 AALA20071237 1 20070704 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 387AM 27184 MIA - SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT 32H TO 41H INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT 32H TO 41H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007071800124 20070718 00124 WP 2007 7 18 ASAA0781857 1 20070706 A 5347 5936663501 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 AFT CARGO RT CARGO TRACK IS CORRODED BETWEEN STA 1148 AND 1155. REMOVED DAMAGED SECTION OF CARGO TRACK, LOCATED, DRILLE D AND INSTALLED A REPLACEMENT TRACK SECTION IAW SRM 51-30-1 PG 13 AND 51-30-5 PG 3. 2 L 7 2 4F RT A6WE 2007071800126 20070718 00126 WP 2007 7 18 ASAA0781851 1 20070704 A 5311 995823879 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 AFT CARGO FRAME CORRODED AT BS 1322 BETWEEN LONG 29R AND LONG 29L. REMOVED DAMAGED AREA OF FRAME, LOCATED, DRILLED AND INSTALLED A REPLACEMENT FRAME AND SPLICE PARTS IAW SRM 53-03 FIG 2A, 51-30-2 PG 1 AND 51-30-5 PG 1. 2 L 7 2 4F RT A6WE 2007071800127 20070718 00127 2007 7 18 QXEA200701154 4 20070715 A 3418 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM STICK PUSHER UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 424QX 4006 SEA - ON FLIGHT 2369, RETURNED TO GATE, ON PUSH BACK DURING ENGINE START MASTER CAUTION "PUSHER SYSTEM FAIL". MAINTENAN CE CYCLED NR 1 AND NR 2 SPM CIRCUIT BREAKERS. PERFORMED OPERATIONAL CHECK OF THE ELEVATOR CONTROL STICK PUSHER SYSTEM. OPERATIONAL CHECK GOOD. NO FAULT REPORTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007071800129 20070718 00129 WP 2007 7 18 ASAA0781852 1 20070704 A 5322 995823885 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 AFT CARGO SHEAR TIE CORRODED AT BS 1322 BETWEEN LONG 26R AND 25R. REMOVED DAMAGED SECTION OF SHEAR TIE, FABRICATED, LOC ATED, DRILLED AND INSTALLED SHEAR TIE AND REPAIR SPLICES IAW SRM 53-03 PG 4M FIG 3, 51-60-0 PG 5 FIG 1 SH 1. 2 L 7 2 4F RT A6WE 2007071800134 20070718 00134 NM 2007 7 18 QXEA200701149 1 20070712 A 3060 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM PROP DEICE SYS UNKNOWN A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 408QX 4050 PDX - ON FLIGHT 2260, PROP DEICE CAUTION ILLUMINATED, UNABLE TO REMEDY VIA E/A CHECKLIST. MAINTENANCE INTERROGATED CDS, NO FAULTS FOUND. C/W VISUAL INSPECTION OF NR 1 AND NR 2 BLADE BOOTS, NO DEFECTS NOTED. REMOVED NR 1 AND NR 2 PROP SPI NNERS AND C/W VISUAL INSPECTION OF WIRE LEADS TO BOOTS, NO DEFECTS NOTED. REINSTALLED BOTH SPINNERS AND C/W TASK 30-61- 00-72-801 FOR PROP DEICE SYSTEM. OPERATIONAL CHECK GOOD. NO DEFECTS FOUND. AIRCRAFT RETURNED TO SERVICE. NO PARTS RE PLACED. 2 H 7 2 4T RT A13NM 2007071800138 20070718 00138 NM 2007 7 18 SWAA073354 1 20070706 A 5310 654584 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 291 TO BS 332, STR 17R. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2007071800140 20070718 00140 NM 2007 7 18 QXEA200701145 1 20070713 A 3150 BULB DHAV DHC8 DHC8202 2809007 NM WARNING LIGHT INOPERATIVE A QXEA D RETURN TO BLOCK P NO WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 358PH 506 PDX FLIGHT NR 2149 - NR 1 AUX FUEL TANK PUMP ADVISORY LIGHT DID NOT LIGHT UP PRESS TO TEST INDCATES A BAD BULB. REPLACE D BULB COMPLIED WITH OPERATIONAL CHECK. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071800141 20070718 00141 NM 2007 7 18 SWAA073358 1 20070706 A 5753 6546486 WEDGE BOEING 737 7375H4 138449D NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, FOUND RIGHT WING INBOARD MID FLAP T/E WEDGE DELAMINATED AT OUTBOARD LOWER SURFACE. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007071800143 20070718 00143 2007 7 18 QXEA200701146 3 20070716 A 6197 CONNECTOR DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS MISALIGNED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 349PH 486 SEA FLIGHT NR 2104 - DURING TAKEOFF ROLL AUTO FEATHER FAILED TO ARM THROUGH 80 PERCENT. TORQUE ON BOTH NR 1 AND NR 2. FOUND CONNECTOR 6121-P9 TO BE ASKEW. RESEATED CONNECTOR 6121-P9. FUNCTIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071800148 20070718 00148 EA 2007 7 18 QXEA200701114 1 20070621 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSLEAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 C3 OKC - FORWARD LOWER FUSELAGE SKIN UNDER LOWER ADF ANTENNA AROUND RIGHT AFT MOUNT HOLE THERE IS CORROSION. REPAIRED I AW SRM 51-21-06, 53-22-21, 51-21-11. 2 L 7 2 4F RT A21EA 2007071800150 20070718 00150 EA 2007 7 18 QXEA200701113 1 20070624 A 5320 STIFFENER CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 C3 OKC - FS 280 STIFFENER AT RBL 21 CRACKED AT BOTTOM RIVET. REPAIRED IAW SRM 51-42-06, 51-25-06. 2 L 7 2 4F RT A21EA 2007071800151 20070718 00151 NM 2007 7 18 SWAA073359 1 20070706 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, FOUND STRINGER 7L CRACKED AT BS 1011. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007071800152 20070718 00152 EA 2007 7 18 QXEA200701110 1 20070629 A 7830 LATCH CNDAIR CL600 CL6002C10 1390015 EA THRUST REVERSER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 C3 OKC - NR 2 ENGINE LOWER TRANSCOWL CENTER LATCH CUTOUT CORNER IS CRACKED. REPAIRED IAW SRM 51-42-06, 51-42-13, 51-21- 11. 2 L 7 2 4F RT A21EA 2007071800153 20070718 00153 EA 2007 7 18 QXEA200701112 1 20070621 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 C3 OKC - REPAIR DENT IN FUSELAGE SKIN PER REO 670-53-11-228. REPAIRED IAW REO 670-53-11-228. 2 L 7 2 4F RT A21EA 2007071800155 20070718 00155 NM 2007 7 18 QXEA200701122 1 20070711 A 5210 TRACK BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR LACK OF LUBE A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 408QX 4050 SEA FLIGHT NR 2436: AFT PAX DOOR HARD TO OPEN. MAINTENANCE CLEANED AND LUBED AFT PAX DOOR ROLLER TRACKS. OPS CHECK GOO D. NO FURTHER PROBLEM NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071800156 20070718 00156 NM 2007 7 18 SWAA073348 1 20070707 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 607SW 27927 EEPLS PHOTOLUMINESCENT STRIP CRACKED BETWEEN ROW 8 DEF AND ROW 10 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007071800159 20070718 00159 NM 2007 7 18 QXEA200701123 1 20070711 A 3620 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM NR 2 BLEED CAUT UNKNOWN A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 418QX 4143 SEA FLIGHT NR 2361: NR 2 BLEED HOT CAUTION ILLUMINATED EN ROUTE. PERFORMED CHECKLIST. VERIFIED LIGHT WAS STILL ILLUMIN ATED UPON MTX ARRIVAL TO AIRCRAFT. MAINTENANCE FOUND RT BLEED OVERTEMP MESSAGE IN CDS. DURING TROUBLE SHOOTING, CAUTIO N AND FAULT MESSAGES EXTINGUISHED. GROUND RAN ENGINES FOR 15 MINUTES WITH BLEED ON MAX. NO FURTHER FAULTS NOTED. UNAB LE TO INDUCE FAULTS. CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071800160 20070718 00160 NM 2007 7 18 KCSA071207 1 20070710 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 MAIN DECK SEAT TRACK CRACKED AT BS 900, RBL 33. 2 L 7 4 4F RT A20WE 2007071800161 20070718 00161 NM 2007 7 18 QXEA200701089 1 20070627 A 5340 STRINGER CLIP DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - CORROSION FOUND ON END CLIP FOR STRINGER 25 FORWARD OF FRAME 424.124. REPAIRED IAW SRM 51-40-11, 51-20-26. 2 H 7 2 4T RT A13NM 2007071800165 20070718 00165 EA 2007 7 18 QXEA200701101 1 20070614 A 5210 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 C3 OKC - PASSENGER DOOR LOWER EDGE MEMBER CRACKED ON FORWARD AND AFT EDGE. REPAIRED IAW REO 601R-52-11-279. 2 L 7 2 4F RT A21EA 2007071800166 20070718 00166 SO 2007 7 18 C2XA07TY 1 20070706 A 5751 14569009410 BRACKET EMB 145 EMB145LR 3260212 SO RT AILERON WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13995 145295 RIGHT AILERON PCA ATTACH FITTING I/B MOST LUG WORN AND HAS CORROSION INSIDE BORE. REMOVED AND REPLACED PCA BRACKET IAW EC 5750-01177. AIRCRAFT IS STILL IN C-CHECK. 2 L 7 2 4T RT T00011AT 2007071800169 20070718 00169 NM 2007 7 18 HNAA0700125 1 20070626 A 5240 DOUBLER DHAV DHC8 DHC8102 2809003 NM LAVATORY SERVICE DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 912HA 040 CORROSION FOUND IN VARIOUS PLACES IN LAV SERVICE PANEL. LAVATORY MACHINED SERVICE DOOR DOUBLER REPAIRED AS PER 8-53-07- 3235 AND INSTALLED WITH SOLID RIVETS AS PER SRM 51-40-00, HFEC CUT OUT NO CRACKS. 2 H 7 2 4T RT A13NM 2007071800170 20070718 00170 EA 2007 7 18 QXEA200701104 1 20070614 A 5753 PANEL CNDAIR CL600 CL6002C10 1390015 EA RT TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 C3 OKC - RIGHT FLAP LEADING EDGE PANEL 684JB CHAFED AT CUTOUT. REPAIRED IAW SRM 51-12-00, 51-21-11, 51-25-06, 57-52-01. 2 L 7 2 4F RT A21EA 2007071800174 20070718 00174 EA 2007 7 18 QXEA200701106 1 20070614 A 5753 PANEL CNDAIR CL600 CL6002C10 1390015 EA RT TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 C3 OKC - RIGHT FLAP LEADING EDGE 684GB CHAFED AT CUTOUT. REPAIRED IAW SRM 51-12-00, 51-21-11, 57-52-01. 2 L 7 2 4F RT A21EA 2007071800175 20070718 00175 EA 2007 7 18 QXEA200701107 1 20070613 A 5730 PANEL CNDAIR CL600 CL6002C10 1390015 EA LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 C3 OKC - LEFT WING PANEL 584JB CHAFED. REPAIRED IAW SRM 51-12-00, 57-52-01, 51-21-11. 2 L 7 2 4F RT A21EA 2007071800176 20070718 00176 EA 2007 7 18 QXEA200701105 1 20070614 A 5753 SKIN CNDAIR CL600 CL6002C10 1390015 EA RT TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 C3 OKC - RIGHT FLAP LEADING EDGE 684EB CHAFED AT CUTOUT. REPAIRED IAW SRM 51-12-00, 51-21-11, 51-25-06, 57-52-01. 2 L 7 2 4F RT A21EA 2007071800177 20070718 00177 EA 2007 7 18 QXEA200701102 1 20070616 A 5210 SKIN CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 C3 OKC - PASSENGER DOOR EXTERNAL SKIN FORWARD UPPER CORNER HAS SEVERAL DEEP SCRATCHES. REPAIRED IAW SRM 51-12-00, 51-21 -11. 2 L 7 2 4F RT A21EA 2007071800178 20070718 00178 NM 2007 7 18 ZZDA070605195 1 20070605 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION SPOTS ON AFT CARGO COMPARTMENT SKIN INNER SURFACE BETWEEN BS 898.5 AND BS 1053 AND FROM LONG 26 LT TO LONG 29 RT. INSTALLED LOWER SKIN BETWEEN STA 895.5 TO STA 1053 AND BETWEEN LONGERON 26L TO LONGERON 26R PER B717 SRM 51-41-02 S RM 51-41-05. 2 L 7 2 4F TR A6WE 2007071800180 20070718 00180 NM 2007 7 18 AALA20071239 1 20070704 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 387AM 27184 MIA - EMERGENCY EXIT LIGHT COVER IN COCKPIT FELL OFF LIGHT ASSEMBLY. SECURED LENS FOR EMERGENCY EXIT LIGHT ASSEMBLY IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007071800182 20070718 00182 WP 2007 7 18 AALA20071201 1 20070628 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 441AA 49460 LGA - EMERGENCY LIGHTS AT SEAT ROW 26 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROW 26. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071800187 20070718 00187 EU 2007 7 18 AALA20071206 1 20070628 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 MIA EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT NUMBER TWO D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007071800188 20070718 00188 NM 2007 7 18 ZZDA070605197 1 20070605 A 5322 SHEAR TIE BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT BS 1037 ON SHEAR TIE. INSTALLED SHEAR TIE ON STA 1037 BETWEEN LONGERON 25L TO 20L AS PER B717 SRM 51-41-02 AND SRM 51-41-05. MATERIAL USED 7075-T6 .063 AND 7075-T6 0.071. 2 L 7 2 4F TR A6WE 2007071800189 20070718 00189 EU 2007 7 18 AALA20071207 1 20070628 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 MIA - EMERGENCY LIGHTS AT SEAT ROWS 1D TO 18C INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 1D T O 18C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007071800190 20070718 00190 NM 2007 7 18 ZZDA070605200 1 20070605 A 5311 FRAME BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT FRAME BETWEEN LONG 30 AND LONG 22L. INSTALLED FRAME SPLICE AT STA 1022 FROM LONGERON 25L TO 23L AS PER B717 SRM 51-41-02 AND SRM 51-41-05. MATERIAL USED 7075-T6 .050 AND 7075-T6 0.071. 2 L 7 2 4F TR A6WE 2007071800191 20070718 00191 2007 7 18 AALA20071242 4 20070705 A 2565 D30656126 SLIDE BOEING 757 757223 1384957 NM R4 DOOR LOW PRESSURE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 647AM 24605 DFW - RIGHT NUMBER FOUR SLIDE PRESSURE LOW. REPLACED SLIDE TO RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F RT A2NM 2007071800192 20070718 00192 WP 2007 7 18 AALA20071219 1 20070701 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14551 53033 DFW - EMERGENCY LIGHT AT LEFT AFT OVERWING EMERGENCY EXIT SIGN COVER IS CRACKED. REPLACED COVER FOR EMERGENCY LIGHT AT LEFT AFT OVERWING EMERGENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071800193 20070718 00193 WP 2007 7 18 AALA20071220 1 20070701 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14551 53033 DFW - EMERGENCY LIGHTS AT FORWARD CABIN CEILING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD CABI N CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071800194 20070718 00194 NM 2007 7 18 ZZDA070605201 1 20070605 A 5311 FRAME BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT BS 1037 ON FRAME BETWEEN LONGERON 29R AND LONG 21L. INSTALLED NEW FRAME SECTION STA STA 1037 FROM LONGERON 29R TO 18L AS PER B717 SRM 51-41-02 AND SRM 51-41-05. MATERIAL USED 7075-T6 .063 AND 7075-T6 0.0 71. 2 L 7 2 4F TR A6WE 2007071800195 20070718 00195 WP 2007 7 18 AALA20071221 1 20070701 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14551 53033 DFW - EMERGENCY LIGHTS AT MID CABIN CEILING INOPERATIVE. REPLACED BATTERY PACK B5 104 FOR EMERGENCY LIGHTS AT MID CABIN CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071800196 20070718 00196 WP 2007 7 18 AALA20071222 1 20070701 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14551 53033 DFW - EMERGENCY LIGHTS AT CEILING TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK AT B5 28 FOR EMERGENCY LIGHTS AT CEILING TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071800197 20070718 00197 NM 2007 7 18 ZZDA070606198 1 20070606 A 5312 STRAP BOEING 717 717200 1383700 NM BULKHEAD CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 AFT PRESSURE DOME FWD FACE AT 6 O'CLOCK POSITION STRAP HAS CORROSION (9-010). INSTALLED WEB AND DOUBLER 2 EACH AT AFT P RESSURE BULKHEAD IAW B717 SRM 51-41-05 AND SRM 51-41-02. MATERIAL USED ON WEB 7075-T6 0.040 SIZE 33.5 X 9.25 INCHES AND 38 X 9.25 INCHES, DOUBLER 7075-T6 0.050 SIZES 9.3125 X 4.25 INCHES AND 10 X 4.25 INCHES. 2 L 7 2 4F TR A6WE 2007071800199 20070718 00199 SW 2007 7 18 BAQQ200700024 1 20070628 A 6240 0861110066 SPEED SWITCH BOLKMS 117 BK117C2 5626002 SW MAIN ROTOR DIRTY E BAQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 03 906GL 174 9089 DURING FLIGHT TO PICKUP PATIENT, ROTOR TACH NEEDLE INDICATED ZERO. ABORTED FLIGHT AND NOTIFIED MECHANIC. RETURNED TO BAS E FOR MAINTENANCE. DURING TROUBLESHOOTING, MECHANIC CLEANED CONNECTIONS AT THE MAG PICKUP AND THE TRIPLE TACH. OPERATION AL CHECK AND GROUND RUN SUCCESSFUL. NO DEFECTS NOTED. 1 G 7 2 3U H13EU 2007071800200 20070718 00200 CE 2007 7 18 GUUA06270702 1 20070627 A 3260 WARNING HORN BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A GUUA O OTHER N FALSE WARNING AP APPROACH 1 SO 29 38537 UE158 FLIGHT: 9259 DURING APPROACH LANDING GEAR WARNING HORN SOUNDS WHEN POWER IS PULLED BACK, WHILE SILENCING THE HORN SILE NCE BUTTON NOT WORKING. PERFORMED LANDING GEAR OPERATIONAL CHECK NO DEFECTS NOTED. 2 L 7 2 4T RT A24CE 2007071800201 20070718 00201 NM 2007 7 18 ZZDA070613188 1 20070613 A 5312 STIFFENER BOEING 717 717200 1383700 NM BULKHEAD CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 AFT CARGO COMPARTMENT, FWD BULKHEAD, VERTICAL STIFFENER LBL 48, LWR SECTION IS CORRODED. INSTALLED EXTRUDED REPAIR ON V ERTICAL STIFFENER AFT CARGO, FWD BULKHEAD LBL 48 LOWER SECTION PER SRM 51-70-11 FIG 201. 2 L 7 2 4F TR A6WE 2007071800202 20070718 00202 CE 2007 7 18 GUUA06270701 1 20070627 A 3233 ROD BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG ACTUATOR BENT A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 29 87551 UE206 FLIGHT: 5407, DURING APPROACH NOSE LANDING GEAR WOULD NOT COME DOWN ON THE FIRST TRY RECYCLED, LANDING GEAR EXTENDED N ORMALLY. REPLACED NOSE LANDING GEAR ACTUATOR, OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007071800203 20070718 00203 CE 2007 7 18 GLBA20060961 1 20070702 A 7712 1143800653 TORQUEMETER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LEFT MALFUNCTIONED A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 03 154GL UE154 ABORTED TAKEOFF, FLIGHT 5063, UPON TAKEOFF PILOTS REPORTED THAT THE LT TORQUE INDICATOR STUCK AND WOULD NOT WORK CORRECT LY. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE LT TORQUE GAUGE IAW MM 33-10. OPERATIONAL CHECK OF THE SYSTEM GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2007071800204 20070718 00204 NM 2007 7 18 ZZDA070618189 1 20070618 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 AFT CARGO COMPARTMENT, INNER SURFACE OF SKIN HAS CORROSION BETWEEN STA 813 AND 898.5 AND L 26L TO 25L LAP SEAM AREA. IN STALLED DOUBLER AND TRIPLER REPAIR AT AFT CARGO COMPARTMENT, INNER SURFACE SKIN BETWEEN STA 813 AND 898.5 AND L-26L AND L-25L IAW BOEING MESSAGE NUMBER 1-383755005-4 DATED 20-JUN-2007 AND AIRTRAN EA 17-53-00541 IR. MATERIAL USED FOR DOUBLE R AND TRIPLER 7075-T6 .080. SIZE 1.0 X 19.0 INCHES. 2 L 7 2 4F TR A6WE 2007071800205 20070718 00205 NE 2007 7 18 GUUA06240702 2 20070624 A 7200 310470001 ENGINE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE NR 1 FAILED A GUUA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 261AS 39735 7175 120141 115008 FLIGHT: 9287, DURING CLIMB, NR 1 ENGINE FAILED. SHUTDOWN NR 1 ENGINE. RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. REPLACED NR (1) ENGINE. 2 L 7 2 4T 4 T RT A31SO E20NE 2007071800207 20070718 00207 NE 2007 7 18 GUUA06290701 2 20070629 A 7200 ENGINE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE LEFT FLAMED OUT A GUUA B A EMER. DESCENT UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 29 266AS 120188 FLIGHT: 9287, DURING FLIGHT, LT ENGINE FAILED. DIVERTED, LANDED WITHOUT INCIDENT. PERFORMED DETAIL INSPECTION OF LT EN GINE, REFUELED LT WING, PERFORMED ENGINE RUN. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 2007071800208 20070718 00208 CE 2007 7 18 2007F00038 1 20070705 A 5610 10150413S WINDSHIELD BEECH 200 B200 1152922 CE PWA PT6 PT6* 52043 EA COCKPIT CRACKED E O OTHER O OTHER DE DESCENT 1 SW 09 177LA 7118 BB1203 AIRCRAFT DEPARTED, ENROUTE, ABOUT 45 MINUTES INTO FLIGHT, CREW REPORTED THEY WERE AROUND FL220 AND STARTED THEIR DESCENT , WHEN AT FL190 THE PILOT'S WINDSHIELD CRACKED AND SPIDER WEBBED ACROSS THE ENTIRE WINDSHIELD. CREW LANDED THE AIRCRAFT WITHOUT ANY OTHER ISSUES. REPLACED WINDSHIELD AS REQUIRED IAW MM. 1 L 7 2 4T 3 T A24CE E2NE 2007071800209 20070718 00209 CE 2007 7 18 AMWA28032 1 20070705 A 5711 11810001825 SPAR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE WING SHEARED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 126YV UE126 SHEARED AND STRETCHED RIVETS AT LT AND RT WS 114.25. REPAIRED IAW ER NR 6699-2 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007071800210 20070718 00210 NM 2007 7 18 SPAA0700093 1 20070630 A 3350 110049 POWER SUPPLY BOEING 737 7372T4 1384492 NM PWA JT8 JT8D17 52049 NE EMERGENCY LIGHTS INOPERATIVE A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 07 703S 22529 AFT EXIT AND FLOOR PROXIMITY EMERGENCY LIGHTING DOES NOT ILLUMINATE WHEN TURNED ON. REPLACED CHARGER AND BATTERY PACK I AW AMM 33-51-81,SYSTEM OPS TEST NORMAL IAW AMM 33-51-11. 2 L 7 2 4F 4 F A16WE E2EA 2007071800211 20070718 00211 NM 2007 7 18 SPAA0700094 1 20070630 A 3350 110049 POWER SUPPLY BOEING 737 7372T4 1384492 NM PWA JT8 JT8D17 52049 NE EMERGENCY LIGHTS INOPERATIVE A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 28 703S 22529 AFT EXIT AND FLOOR PROXIMITY EMERGENCY LIGHTING DOES NOT ILLUMINATE WHEN TURNED ON. REPLACED CHARGER AND BATTERY PACK IA W AMM 33-51-81,SYSTEM OPS TEST NORMAL IAW AMM 33-51-11. 2 L 7 2 4F 4 F A16WE E2EA 2007071800212 20070718 00212 NM 2007 7 18 SPAA0700095 1 20070630 A 3350 110049 POWER SUPPLY BOEING 737 7372T4 1384492 NM PWA JT8 JT8D17 52049 NE EMERGENCY LIGHTS INOPERATIVE A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 28 703S 22529 AFT EXIT AND FLOOR PROXIMITY EMERGENCY LIGHTING DOES NOT ILLUMINATE WHEN TURNED ON. REPLACED CHARGER AND BATTERY PACK IA W AMM 33-51-81,SYSTEM OPS TEST NORMAL IAW AMM 33-51-11. 2 L 7 2 4F 4 F A16WE E2EA 2007071800214 20070718 00214 NM 2007 7 18 ZZDA070618190 1 20070618 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 AFT CARGO COMPARTMENT AREA FUSELAGE SKIN, EXTERNAL SURFACE HAS CORROSION BETWEEN STA 860 AND 880 AND L-29L TO 27L. INST ALLED DOUBLER REPAIR AT AFT CARGO COMPARTMENT BETWEEN STA 851 AND STA 874 AS PER AIRTRAN EA 1753-00542 IR. MATERIAL USE D .063 7075T6, 7.0 X 17.0 INCHES AND .025 2024T3 FOR FINGER DOUBLER. 2 L 7 2 4F TR A6WE 2007071800213 20070718 00213 CE 2007 7 18 FCPR20070006 1 20070518 A 2752 991405457 BALLSCREW CESSNA 650 650 2076802 CE FLAP ACTUATOR FAILED B FCPR K NONE O OTHER IN INSP/MAINT 1 NM 09 651CV 4086 6500036 FLAP ACTUATOR DRIVE CARRIAGE BALLSCREW NUT FAILED. FLAPS WOULD NOT MOVE. 2 L 7 2 4F A9NM 2007071800215 20070718 00215 2007 7 18 5083 4 20070516 A 3418 SLZ7695 COMPUTER CESSNA 500 S550 2076607 CE STICK SHAKER DEFECTIVE E T17A O OTHER O OTHER CL CLIMB 1 GL 17 408CT 6392 S5500055 STICK SHAKER DID NOT ACTIVATE WHEN DOING STALL RECOGNITION/RECOVERY TRAINING. 1 L 7 2 4F RT A22CE 2007071800217 20070718 00217 NM 2007 7 18 ZZDA070627192 1 20070627 A 5311 FRAME BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 AFT CARGO COMPARTMENT AT STA 832 AND LONGERON 26 LEFT FRAME LOWER FLANGE IS DAMAGED. INSTALLED FRAME REPAIR SPLICE ON S TA 832 AND LONGERON 26L IAW B717 SRM 53-20-07 F-201. MATERIAL USED .063, 7075-0, TREATED TO T6 SIZE 11 X 2.75 INCHES. 2 L 7 2 4F TR A6WE 2007071800218 20070718 00218 NM 2007 7 18 ZZDA070629193 1 20070629 A 5312 STIFFENER BOEING 717 717200 1383700 NM CARGO BAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 AFT CARGO, FWD BULKHEAD VERTICAL STIFFENER LBL 34 LOWER SECTION CORRODED. INSTALLED REPAIR AT AFT CARGO COMPARTMENT LBL 34 FWD BULKHEAD VERTICAL STIFFENER. 2 L 7 2 4F TR A6WE 2007071800223 20070718 00223 SO 2007 7 18 C2XA07IA159 1 20070707 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO CARGO BAY MALFUNCTIONED A C2XA F ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 SW 27 17138 11830 11830 145727 IAH - FLIGHT 3089 - THE CREW REPORTED THAT ON ARRIVAL TO IAH HAD A BAGGAGE SMOKE WARNING IN EICAS, AND A BAGGAGE WARNING LIGHT ON. THE CREW DISCHARGED THE CARGO FIRE BOTTLES AS A PRECAUTION, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE FORWARD CARGO COMPARTMENT SMOKE DETECTOR & FIRE BOTTL ES, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007071800224 20070718 00224 CE 2007 7 18 DJFA2007071 1 20070709 A 2120 UNKNOWN BEECH MU300 400A 1155402 CE CABIN SMOKE E DJFA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 23 471LX RK506 DURING CLIMB, THE CREW NOTICED SMOKE IN THE CABIN. POWER WAS REDUCED AND THE AFT BLOWER WAS TURNED OFF. THE AIRCRAFT R ETURNED TO THE BASE OF DEPARTURE. IT WAS NOTICED THAT THE RT CABIN SIDEWALL WAS VERY HOT WITH THE TEMPERATURE SET FULL COLD. TROUBLESHOOTING FOUND THE MANUAL TEMPERATURE CONTROL SYSTEM DEFECTIVE CAUSING HIGH TEMPERATURE BLEED AIR TO ENTER THE CABIN AIR DISTRIBUTION SYSTEM. THE AUTO TEMPERATURE CONTROL SYSTEM WAS VERIFIED TO OPERATE NORMALLY. THE MANUAL T EMPERATURE CONTROL SYSTEM WAS MEL'D AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4F RT A16SW 2007071800226 20070718 00226 SO 2007 7 18 C2XA07IA160 1 20070707 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO CARGO BAY MALFUNCTIONED A C2XA B F EMER. DESCENT ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 SW 27 17138 11830 11830 145727 IAH - FLIGHT 3089 - THE CREW REPORTED THAT ON ARRIVAL TO IAH HAD A BAGGAGE SMOKE WARNING IN EICAS, AND A BAGGAGE WARNING LIGHT ON. THE CREW DISCHARGED THE CARGO FIRE BOTTLES AS A PRECAUTION, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE AFT CARGO COMPARTMENT SMOKE DETECTOR & FIRE BOTTLES, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007071800227 20070718 00227 SO 2007 7 18 C2XA07RI052 1 20070703 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 14953 145071 FLT 2774 - DAY - CREW REPORTED MAIN CABIN DOOR EMERGENCY LIGHT INOPERATIVE. DAY MX RECYCLED BATTERY SWITCHES AND PERFOR MED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007071800228 20070718 00228 SO 2007 7 18 C2XA07IA161 1 20070706 A 3350 20131A BATTERY PACK EMB 135 EMB135LR 3260305 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12528 12408 1044 145504 IAH - DURING A-CHECK INSPECTION THE LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS AND SEVERAL CABIN EMERGENCY EXIT LIGHT S WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 4 EMERGENCY EXIT LIGHT BATTERY PACK, OPERAT IONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071800229 20070718 00229 SO 2007 7 18 C2XA07IA162 1 20070705 A 3231 852701 PROXIMITY SWITCH EMB 145 EMB145XR 3260214 SO NLG INOPERATIVE A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 11109 145657 IAH - FLIGHT 2771, THE CREW REPORTED A LOUD WIND NOISE FROM THE FRONT GEAR DOOR AREA BEGINNING AT CRUISE AT 35,000 FEET. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NLG DOOR SEQUENCE PROXIMITY SWI TCH, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007071800230 20070718 00230 NE 2007 7 18 706200701 2 20070706 A 7200 JT8D17 ENGINE BOEING 727 7272F9 138407D NM PWA JT8 JT8D17 52049 NE NR 3 DAMAGED A PCSA A UNSCHED LANDING E X J VIBRATION/BUFFET ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SO 17 199AJ 58977 1291 21426 688045 FLIGHT 743 DEPARTED, WHEN THE CREW REPORTED, DURING CLIMBOUT, THE NR 3 ENGINE STARTED TO VIBRATE ABOUT FL340, ENGINE IND ICATIONS WERE ERRATIC, NR 3 FUEL QTY GAUGE SHOWED 1700 LBS. DIFFERENCE WITH NR 1 FUEL TANK, THEN NR 3 ENGINE FLAMED OUT. THE CREW ACCOMPLISHED A RESTART OF THE NR 3 ENGINE AND LANDED WITHOUT FURTHER INCIDENT. UPON VISUAL INSPECTION OF THE N R 3 ENGINE INLET, BLADE DAMAGE WAS NOTED TO THE C-1 AND C-2 COMPRESSOR SECTIONS OF THE NR 3 ENGINE. THE AIRCRAFT WAS FER RIED ON A (2) ENGINE FERRY PERMIT AND LANDED WITHOUT FURTHER INCIDENT. THE DAMAGED C-1 BLADES HAVE BEEN DRESSED AND THE C-2 COMPRESSOR ASSEMBLY IS BEING REPLACED. 2 L 7 3 4F 4 F RT A3WE E2EA 2007071800231 20070718 00231 EU 2007 7 18 070207 1 20070702 A 6720 L673M40A1003 ACTUATOR UROCOP EC135 EC135T1 5620026 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAIL ROTOR WRONG PART E E3MA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 EA 03 308ME 283 283 0502 AIRCRAFT REQUIRED EXCESSIVE LT PEDAL IN A HOVER. CHANGED TAIL ROTOR SERVO. NOTE: UNDER MODEL THERE IS NOT THE OPTION FOR EC-135 T2 AND FOR THE ENGINE THERE IS NO OPTION FOR ARRIEL 2B2. UNDER MANUFACTURE NAME FOR THE PART THERE IS NOT A LIST ING FOR THE COMPANY. 1 G 7 2 3U 3 U H88EU E00054EN 2007071800232 20070718 00232 EU 2007 7 18 0621070132 1 20070610 A 6720 BEARING UROCOP EC135 EC135T1 5620026 EU TMECA ARRIEL ARRIEL2B1 60056 NE ACTUATOR WORN E E3MA K NONE O OTHER IN INSP/MAINT 1 EA 03 533ME 395 395 00451 0132 SPHERICAL BEARING WORN ON INPUT SHAFT. 1 G 7 2 3U 3 U H88EU E00054EN 2007071800233 20070718 00233 EU 2007 7 18 0524070157 1 20070524 A 6720 BEARING UROCOP EC135 EC135T1 5620026 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAIL SERVO WORN E E3MA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 03 575ME 1276 1276 00419 0157 SPHERICAL BEARING WORN AND LEAKING FLUID. 1 G 7 2 3U 3 U H88EU E00054EN 2007071800234 20070718 00234 SO 2007 7 18 C2XA07IA163 1 20070705 A 3231 852701 PROXIMITY SWITCH EMB 135 EMB135LR 3260305 SO NLG INOPERATIVE A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 12519 145366 IAH - FLIGHT 2799, THE CREW REPORTED THAT ON TAKEOFF, HEARD A LOUD NOISE CONSISTENT WITH GEAR DOWN NOISE. ANOTHER AIRCR AFT VERIFIED THAT THE NOSE LANDING GEAR DOORS WERE OPEN, AND THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDE NT. MAINTENANCE REMOVED AND REPLACED THE NLG DOOR SEQUENCE PROXIMITY SWITCH, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071800236 20070718 00236 WP 2007 7 18 ASAA0781859 1 20070708 A 5321 99365465 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 CABIN FLOOR PANEL HAS HOLES IN PANEL. REMOVED FLOOR PANEL, FABRICATED AND INSTALLED FLOOR PANEL IAW SRM 53-05 AND DWG 9 936585. 2 L 7 2 4F RT A6WE 2007071800240 20070718 00240 EU 2007 7 18 0613070144 1 20070613 A 6720 BEARING UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1A NE TAIL SERVO WORN E E3MA K NONE O OTHER IN INSP/MAINT 1 EA 03 522ME 683 683 00067 0144 SPHERICAL BEARING ON INPUT SHAFT, WORN. 1 G 7 2 3U 3 U H88EU E34NE 2007071800241 20070718 00241 SO 2007 7 18 N93A04072007 1 20070704 A 3250 716483 TILLER GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE NLG STEERING UNKNOWN E N93A O OTHER O OTHER NR NOT REPORTED 1 SO 13 506QS 623 NOSE STEERING INOPERATIVE. 2 L 7 2 4F 4 F RT A12EA E00057EN 2007071800243 20070718 00243 CE 2007 7 18 AMWA15036 1 20070709 A 5711 118100001825 SPAR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT WING CORRODED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 155ZV UE155 CORROSION LT AND AFT MAIN SPAR FLANGE. REPAIRED IAW ENGINEERING REPORT NR 6772-3 REV A DATED JUN 25, 2007. 2 L 7 2 4T 4 T RT A24CE E26NE 2007071300289 20070713 00289 SO 2007 7 13 SIMA200719209 1 20070617 A 5347 13500439005 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 812AE 13442 5000 145531 LEFT FOWARD OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 17 AND 23. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 . AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300290 20070713 00290 SO 2007 7 13 SIMA200719210 1 20070621 A 5347 14532606015 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 811AE 13526 5000 145529 LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 36 AND 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300292 20070713 00292 SO 2007 7 13 SIMA200719205 1 20070617 A 5347 14532605015 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 817AE 13442 5000 145554 RIGHT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 28 AND 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300296 20070713 00296 2007 7 13 2007UALA02379 4 20070702 A 2565 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU R2 DOOR MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 340UA 24244 F/A REPORTS DOOR 2 RIGHT SLIDE DIFFICULT TO ARM & APPEARS TO BE VELCROED INCORRECTLY. [07-27-07] RE-POSITIONED VELCR O. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071300297 20070713 00297 SO 2007 7 13 SIMA200719207 1 20070617 A 5347 14532606015 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 812AE 13442 5000 145531 LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 36 AND 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300311 20070713 00311 NM 2007 7 13 2007UALA02392 1 20070704 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 307UA 23668 EMERGENCY EXIT LIGHT AT LEFT OVERWING EXIT SIDE WALL INOP. [07-27-07] REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081500371 20070815 00371 NM 2007 8 15 USAA070611 1 20070807 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CANNING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 RIGHT SIDE OF 178 BULKHEAD, LEFT OF BOTTOM RIGHT INSPECTION HOLE HAS OIL CANNING. FAB'D NEW DOUBLERS, FILLERS & INSTALL ED PER SRM 53-10-08 FIG 201 REPAIR 9, DEFECT SIZE: 18 X 12 INCHES. 2 L 7 2 4F RT A16WE 2007071300331 20070713 00331 NM 2007 7 13 2007UALA02407 1 20070704 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 543UA 25698 DOORS 1R AND 3R DIFFICULT TO DISARM. [08-08-07] REMOVED DEBRIS FROM 1R, 3R DOOR GIRT BARS & LUBED GIRT BAR FITTINGS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071300349 20070713 00349 NM 2007 7 13 QXEA200701090 1 20070705 A 7312 10879C FUEL HEATER BOMBDR DHC8 DHC8402 1390042 NM NR 1 ENGINE MALFUNCTIONED A QXEA O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 09 407QX 15363 6 4049 PDX FLIGHT NR 2308: ON CLIMB-OUT, NR 1 FUEL TEMP WENT TO 74 DEG C AS PER CHECKLIST, TURNED ON NR 1 AUX PUMP. THE TEMP D ROPPED TO 71 DEG C AND THEN LOWERED. AS PER CHECKLIST, THE PUMP WAS TURNED OFF. THE TEMP CLIMBED BACK UP. THE PUMP WA S THEN TURNED BACK ON AND THE TEMP DROPPED. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE FUEL HEATER IAW Q400 AMM 7 3-11-01-000-801 AND 73-11-01-400-801. OPS AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071300350 20070713 00350 EU 2007 7 13 07FDEA02375 1 20070705 A 2450 F11QY3714 RECTIFIER AIRBUS 310 A310222 3930315 EU NR 1 FAILED A FDEA D RETURN TO BLOCK J S G WARNING INDICATION AFFECT SYSTEMS MULTIPLE FAILURE CL CLIMB 1 SO 25 449FE 217 FOUND NR 1 TRANSFORMER RECTIFIER FAULTED ON MAINT PANE (MULTIPLE FAULTS IN FLT- TRANSPONDER, AUTO-THROTTLE, PITCH TRIM). REMOVED AND REPLACED NR 1 TRANSFORMER RECTIFIER IAW AIRBUS M/M 24-32-11-4. OPS CHECKED NORMAL PER AIRBUS M/M 24-32-00 -5. ALL OTHER FAULTED SYSTEMS TESTED OK. THIS BUSS PROBLEM APPEARED TO BE THE ROOT CAUSE, SEE 34-54/9169 (TRANSPONDER) , 22-10/9170 (PITCH TRIM) AND 22-30/9171 (AUTO-THROTTLE). 2 L 7 2 4F RT A35EU 2007071300358 20070713 00358 EA 2007 7 13 QXEA200701084 1 20070703 A 2612 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA FIRE WARNING UNKNOWN A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 618QX 10205 DEN - FLIGHT 4311 - INTERMITTENT FIRE SYSTEM FAULT MESSAGE. MAINTENANCE PLACED THE SYSTEM ON MEL 26-00-1. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007071300364 20070713 00364 2007 7 13 HEEA116156 4 20070627 A 2211 7015480903 COMPUTER SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL2B1 60056 NE FLT CONTROL MALFUNCTIONED B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 766P 760594 IN FLIGHT TRIM FAILURE WITH CODE 23-20. COMPLIED WITH EMERGENCY PROCEDURE BUT FAILURE OCCURRED TWICE MORE. EACH TIME R ESET AP NR 2 AND TRIM LIGHT WENT OUT. MAINTENANCE REPLACED FLIGHT CONTROL COMPUTER. 1 G 7 2 3U 3 U NC H1NE E00054EN 2007071300366 20070713 00366 2007 7 13 HEEA116160 4 20070629 A 3197 WIRE SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL2S1 60057 NE CHAFED B HEEA K NONE O OTHER IN INSP/MAINT 1 SW 05 767P 760599 TRIM FAIL AND MASTER CAUTION LIGHT BLINK IN HOVER. SYSTEM OPERATES NORMALLY. MAINTENANCE REPAIRED CHAFED WIRING IN CEN TER CONSOLE TO CONTROL PANEL. 1 G 7 2 3U 4 U NC H1NE E00054EN 2007071300368 20070713 00368 NE 2007 7 13 HEEA116165 1 20070628 A 3231 DOOR SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL MLG OBSTRUCTED B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 5435V 760158 AFTER LOWERING THE GEAR HANDLE, IT TOOK MORE THAN (4) MINUTES FOR THE LT MAIN GEAR GREEN LIGHT TO COME ON. MAINTENANCE FOUND THE FLOAT LINE NOT LETTING THE GEAR DOOR CLOSE PROPERLY. REPOSITIONED LINE AND SYSTEM CHECKED GOOD. 1 G 7 2 3U 3 U H1NE E1GL 2007071300370 20070713 00370 EU 2007 7 13 HEEA116216 1 20070705 A 6397 CONNECTOR UROCOP EC135 EC135P2 5620027 EU OIL PRESS XMITER CONTAMINATED B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 343PH 0456 THE MAIN TRANSMISSION OIL PRESSURE DROPPED TO ZERO, TURNED AROUND TO RETURN AND THE PRESSURE CAME BACK TO NORMAL. NO OT HER INDICATIONS OF A PROBLEM. MAINTENANCE CLEANED MOISTURE FROM THE CONNECTOR TO THE OIL PRESSURE TRANSMITTER. 1 G 7 2 3U H88EU 2007071300372 20070713 00372 2007 7 13 F3LA200700165 4 20070627 A 2565 RELEASE CABLE AIRBUS A319 A319111 3930336 NM ESCAPE SLIDE OUT OF ADJUST A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED OPERATIONAL TESTS OF BOTH OVERWING RELEASE SLIDE CABLES FAILED. ADJUSTED LT AND R T EMERGENCY SLIDE EXIT RELEASE CABLES IAW AMM 25-62-43-820-050 AND CHECKED GOOD. 2 L 7 2 4F RT A28NM 2007071300379 20070713 00379 2007 7 13 F3LA200700169 4 20070702 A 2565 D31516317 SLIDE AIRBUS A319 A319111 3930336 NM L1 DOOR LOOSE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED L1 DOOR SLIDE CAME UNPACKED. REPLACED L1 DOOR SLIDE IAW AMM 25-62-44-000-002. OP ERATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 2007071300394 20070713 00394 NM 2007 7 13 UPS07M50113 1 20070521 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C RT HORIZONTAL STABILIZER BARREL NUT HOLE NR 22 BORE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMO VED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTT OM PERIPHERY RADIUSED SMOOTHENED AND PROTECTED. FAB AND PROTECTED REPAIR SLEEVE BUSHING, PR1422 B1/2 SEALANT APPLIED AT BLEND OUT VOID AND REPAIR SLEEVE BUSHING INSTALLED. REWORK AREA PAINTED. 2 L 7 3 4F RT A22WE 2007071300396 20070713 00396 NM 2007 7 13 UPS07M50115 1 20070528 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C LT HORIZONTAL STABILIZER BARREL NUT NR 25 BORE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS AND BOTTOM P ERIPHERY RADIUSED SMOOTHENED AND PROTECTED. REPAIR SLEEVE BUSHING FAB AND PROTECTED. PR1422 B1/2 SEALANT APPLIED AT BL END OUT VOIDS AND REPAIR SLEEVE BUSHING INSTALLED. REWORK AREA PAINTED. 2 L 7 3 4F RT A22WE 2007071300405 20070713 00405 NM 2007 7 13 SWAA073336 1 20070705 A 5311 6546595 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071300408 20070713 00408 NM 2007 7 13 SWAA073326 1 20070705 A 5754 65C26602218A SLAT BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED C2 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT UPPER OUTBOARD END. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 2007071300416 20070713 00416 2007 7 13 SWAA073325 4 20070705 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 730SW 27862 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071300420 20070713 00420 2007 7 13 2007UALA02411 4 20070704 A 2565 COVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 412UA 465 DOOR 2R SLIDE COVER OFF. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071600028 20070716 00028 EU 2007 7 16 07FDEA02396 1 20070707 A 5320 A53810318 ANGLE AIRBUS 310 A310203 3930313 EU ZONE 100 NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FS 40 LT PICKUP ANGLE EFFECTIVITY NOT CONSISTENT WITH SB ANGLE REQUIRES EXCESS MATERIAL TO BE TRIMMED OFF PER EA 6-5310- 110489 PG NR 2 COMPLIED WITH EA 6-5310-110489 PG NR 2. TRIMMED EXCESSIVE MATERIAL OFF OF PN A53810318. 2 L 7 2 4F RT A35EU 2007071600032 20070716 00032 NM 2007 7 16 07FDEA02401 1 20070709 A 5313 655623620 STRINGER BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD LWR CARGO PIT BILGE STRINGER HAS CORROSION AT END STA 740 STR 27R AT PRESSURE BULKHD TIE. REMOVED SECTION OF STRI NGER REF SRM 51-30-2 PG 2, VERIFIED MATERIAL FOR REPAIR. FABRICATED REPAIR PARTS REF SRM 53-10-3 FIG 1. TREATED AND PR IMED REPAIR PARTS REF SRM 51-10-2 PG 2. INSTALLED REPAIR PARTS REF SRM 53-10-3 FIG 1 AND SRM 53-10-2 PG 2. 2 L 7 3 4F RT A3WE 2007071600034 20070716 00034 NM 2007 7 16 07FDEA02409 1 20070709 A 5311 65561161 FRAME BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD PIT BILGE BODY FRAME SHEAR TIE IS CORRODED BS 720D, 2-5" IB OF STR 28L, WL 148 (MKD). REMOVED CORROSION, FOUND TO B E BEYOND LIMITS REF SRM 53-10-1 PG 1&2. REMOVED SHEAR TIE. FABRICATED AND HEAT TREATED SHEAR TIE. INSTALLED NEWLY FAB RICATED SHEAR TIE BS 720D IB STR 28L IAW SRM 53-10-4 FIG 15 STEP 12 PG 58. 2 L 7 3 4F RT A3WE 2007071600039 20070716 00039 EU 2007 7 16 07FDEA02419 1 20070711 A 5340 A53613846 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND 2 CRACKS (13MM AND 6MM,LT SIDE) AND 1 CRACK (5MM RT SIDE) ON C 12 A STIFFENER FITTING. REPAIR PERFORMED BY MODIFI CATION OF STRUCTURE IAW SB A300-53-6137, APPROVED BY EO 6-5340-7-5002 PART 5600. 2 L 7 2 4F RT A35EU 2007071600043 20070716 00043 NM 2007 7 16 07FDEA02424 1 20070711 A 5320 655617522 PLATE BOEING 727 727227 1384078 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 AFT CARGO PIT THRESHOLD PLATE IS CRACKED BY WELD. REPAIR ACCOMPLISHED ON N/R N00477, PER SR 27-53-025C. 2 L 7 3 4F A3WE 2007071600046 20070716 00046 EU 2007 7 16 TRBA2007043 1 20070710 A 3350 5211309111B LIGHT AEROSP ATR72 ATR72212 8680945 EU GALLEY FLOOR BROKEN A TRBA O OTHER O OTHER NR NOT REPORTED 1 SO 29 288AM 288 GALLEY AFT FLOOR ESCAPE EMERGENCY LIGHT BROKEN. REMOVED AND REPLACED LIGHTING STRIP ASSEMBLY IAW JIC NR 33-51-24. OP C K OK. 2 H 7 2 4T RT A53EU 2007071600063 20070716 00063 NM 2007 7 16 QXEA200701097 1 20070706 A 5610 17180005 WINDOW BOMBDR DHC8 DHC8402 1390042 NM COCKPIT FAILED A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 417QX 8864 8864 4086 SEA FLIGHT NR 2286: ON CLIMB-OUT, NOTICED A POPPING SOUND COMING FROM THE CAPTAINS SIDE WINDOW. AS CONTINUED TO PRESSUR IZE IN THE CABIN, THE POPPING CONTINUED. ALSO, NOTICED THE SAME IN DESCENT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE R EPLACED CAPTAIN'S SIDE WINDOW IAW Q400 AMM 56-10-06-000-801 AND TR 56-017 AND 56-10-06-400-801. OPS AND LEAK CHECK GOOD . NO POPPING SOUND NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071600071 20070716 00071 NM 2007 7 16 QXEA200701099 1 20070709 A 6120 311835404 TSCU DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS MALFUNCTIONED A QXEA C ABORTED TAKEOFF O OTHER TX TAXI/GRND HDL 1 NM 09 361PH 6333 516 YVR FLIGHT NR 2151 - AUTO FEATHER FAILED TO ARM. REPLACED TSCU'S ON NR 1 AND NR 2 ENGINES. OPERATIONAL CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071600072 20070716 00072 NM 2007 7 16 QXEA200701100 1 20070710 A 3150 UNKNOWN DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 2 ENGINE UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 353PH 496 PDX FLIGHT NR 2164, NR 2 ENGINE MANUAL CAUTION LIGHT ILLUMINATED ON TAXI OUT. CYCLED ENGINE MANUAL CIRCUIT BREAKER. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007071600077 20070716 00077 NM 2007 7 16 QXEA200701056 1 20070625 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 467 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX-CORROSION AT LOWER FORWARD FLANGE X467.00, JUST OUTBOARD OF LEFT STRINGER 26. REPAIRED IAW SRM 51-20-11, 51-40-1 1, 51-30-26, AND 51-20-51. 2 H 7 2 4T RT A13NM 2007071600085 20070716 00085 2007 7 16 07FDEA02436 4 20070705 A 3441 46300161300413 INU DOUG DC10 DC1010 3022110 WP ZONE 100 FAILED A FDEA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 68058 14697 711 46705 NR 1 INU FAILED AFTER PUSH BACK. REPLACED NR 1 INU GRD, OPS CK NORMAL MM 34-43-04-2, OFF MFG 463001-6130-0413, POS 1 SR L 0341, TAG 0357A9, ON MFG 463001-6130-0413, SRL 2223, TAG 572A32. 2 L 7 3 4F A22WE 2007071700004 20070717 00004 EA 2007 7 17 N6WA00706002 1 20070625 A 3350 RPSIB POWER SUPPLY CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE EMERGENCY LIGHTS INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 161GJ 10253 OVERHEAD CENTER EMERGENCY LIGHT INOPERATIVE. REPLACED EMERCENCY POWER SUPPLY PACK. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007071700006 20070717 00006 SO 2007 7 17 GLBA20060959 1 20070629 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE COCKPIT SMOKE A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 297UX 120297 SMOKE-SMELL : FLIGHT 5120: PILOTS REPORTED SMOKE IN COCKPIT WITH IDLE UNLOCK LIGHTS ILLUMINATED AND ELECTRICAL LIGHT ILL UMINATED ON PANEL. MAINTENANCE PERFORMED HIGH POWER RUN-UP AND TAXI OF AIRCRAFT AND PERFORMED OPERATIONAL CHECKS OF FLI GHT IDLE SOLENOID SYSTEM IAW EMB-120 76-13-00 AND PERFORMED SYSTEM CHECKS OF ELECTRICAL SYSTEMS IAW 24-30-00. ALL CHECK S GOOD WITH NO FAULTS FOUND. 2 L 7 2 4T 4 T RT A31SO E20NE 2007071700008 20070717 00008 EU 2007 7 17 BAQA200700023 1 20070629 A 2697 0301057890 WIRE HARNESS AEROSP AS365 AS365N2 8680815 EU TMECA ARRIEL ARRIEL1C 60030 NE NR 1 FIRE DETECT DEFECTIVE E BAQA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 03 293SV 739 6408 12064 DURING LEVEL FLIGHT NR 1 ENGINE FIRE LIGHT ILLUMINATED. AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENT. AFTER MECHANIC I NVESTIGATED FOR CAUSE FOUND ENGINE WIRING HARNESS TO BE DEFECTIVE. 1 G 7 2 3U 3 U RT H10EU E19EU 2007071700029 20070717 00029 EA 2007 7 17 A6WA200740313 1 20070614 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FLOORBEAM CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 434AW 7322 RT FLOORBEAM ATTACH CLIPS ARE CRACKED AT IB AND OB SIDES FS 280, RBL 9, WL 72. (K) [07-31-07] MAINTENANCE REPAIRED IAW BSC STANDARD REPAIR 601R53-0057A, AND CRJ 200, SRM 51-42-13 AND 51-42-21. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700034 20070717 00034 EA 2007 7 17 A6WA200740318 1 20070616 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 434AW 7322 LT WING STR 53.60 BATTERY RIB IS CRACKED 1.0 INCH ON UPPER AFT CORNER. MAINTENANCE REPAIRED IAW REO 601R-57-51-046. (K ) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700043 20070717 00043 EA 2007 7 17 A6WA200740327 1 20070619 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 460AW 7867 AFTER REMOVING PAX DOOR TOP STEP 832DT FOR ACCESS FWD PAX DOOR FWD SIDE SKIN CRACKED APPROX .750 INCH L LOWER CORNER OF NR 2 STEP IN RADIUS. MAINTENANCE CUT AWAY DAMAGE FABBED REPAIR PARTS AND INSTALLED IAW REO 601R52-11-702, STEPS 1 THRU 12. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700054 20070717 00054 EA 2007 7 17 A6WA200740340 1 20070624 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 462AW 7875 RT FS 484 ANGLE IS CRACKED AT RBL 27 AND 36 APPROX 1.4 INCH L. MAINTENANCE REPAIRED RT FS 484 ANGLES AT RBL 27 AND RBL 36 IAW REO 601R-53-41-059 AND BSC STANDARD REPAIR 601R-53-0030A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700058 20070717 00058 EA 2007 7 17 A6WA200740345 1 20070625 A 5340 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 462AW 7875 HYDRAULIC PRESSURE TRANSDUCER HAT CHANNEL (PN 601R75262-159) CRACKED APPROX .2 INCH LONG IN LT MLG WHEEL WELL CEILING. M AINTENANCE REMOVED AND REPLACED CHANNEL PN 601R75262-159 IAW SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700060 20070717 00060 NM 2007 7 17 ASMF200707008 1 20070711 A 2780 SLAT SYSTEM BOEING 777 777* UTILUSE NM GE GE90 GE9092B 30036 NE MALFUNCTIONED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 774AM 28689 AIRCRAFT RETURNED TO PLATFORM, EICAS SHOWS SLATS PRIMARY FAIL MESSAGE. MAINTENANCE PERSONNEL CHECKED THE MAT AND IT SHO WED THE FAILURE CODE 27-20962 (LATCHED); SO FIM 27-82 PROCEDURE TASK 804 WAS PERFORMED, TESTED CORRECT. 2 L 7 2 4F 4 F RT T00001SE E00049EN 2007071700068 20070717 00068 NM 2007 7 17 AMTA200700322 1 20070704 A 2841 3012803 PROCESSOR BOEING 737 73783N 13844HI NM CENTER UNSERVICEABLE A AMTA O OTHER P NO WARNING INDICATION CR CRUISE 1 GL 11 310TZ 28243 CENTER FUEL TANK QTY BLANKS INTERMITTENTLY. (K) REMOVED AND REPLACED FUEL QTY PROCESSOR UNIT, C/W OPS CHECK, OPS CHECK GOOD. NO FAULTS NOTED AT THIS TIME IAW AMM 28-41-81. (K) 2 L 7 2 4F RT A16WE 2007071700072 20070717 00072 2007 7 17 AMTA200700318 4 20070629 A 3442 20414440401 DRIVE UNIT BOEING 737 73783N 13844HI NM WX RADAR SYSTEM INOPERATIVE A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 314TZ 30640 WITH RADAR TILT SET AT (0) DEGREE, THE GROUND IS PAINTED. TILT MUST BE SET AT +2.5 DEGREE TO REMOVE GOURND RETURN, SEE LOG PAGE 800323. (K) 2 L 7 2 4F RT A16WE 2007071700089 20070717 00089 NM 2007 7 17 DL76S070849 1 20070703 A 5712 7075T600631N RIB BOEING 767 767332 1382001 NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 RT WING LES 688 AREA RIB SUPPORT FWD END CRACKED. RT WING LES 688 AREA RIB SUPPORT REPAIRED PER SRM 57-41-01 FIGURE 201 REPAIR 4. 2 L 7 2 4F RT A1NM 2007071700104 20070717 00104 NM 2007 7 17 DLM90070865 1 20070625 A 5320 9930538412 CUSP WEB DOUG MD90 MD9030 3023690 NM IAE V2525 V2525D5 NE BS 503-579 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 V20105 RIGHT CUSP WEB STA 503-579 CORRODED OUT OF LIMITS. REMOVED DAMAGED CUSP WEB AND REPLACED WITH A SERVICEABLE WEB IAW THE MD90 SRM 51-30-02, 51-30-01, 51-10-05, AND 51-30-05. 2 L 7 2 4F 4 F RT A6WE A40NE 2007071700112 20070717 00112 NM 2007 7 17 DLM90070874 1 20070603 A 5520 5940489501 ELEVATOR DOUG MD90 MD9030 3023690 NM RIGHT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 RT ELEVATOR O/B T/E HAS COMPOSITE DAMAGE. REPAIRED ELEVATOR O/B T/E DAMAGED IAW MD-90 SRM 51-10-04D PAR 8J. 2 L 7 2 4F RT A6WE 2007071700120 20070717 00120 NM 2007 7 17 QXEA200701065 1 20070625 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 201 S31L CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - CORROSION UNDER FLOOR AT STATION 201 AT STRINGER 31L FITTING CASTING ON VERTICAL FRAME. REPAIRED IAW SRM 51-40 -11. 2 H 7 2 4T RT A13NM 2007071700125 20070717 00125 NM 2007 7 17 QXEA200701087 1 20070625 A 5320 SILL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - MAIN CABIN DOOR LOWER SILL PLATE BOTTOM SIDE HAS CORROSION. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007071700136 20070717 00136 NM 2007 7 17 AWXA200700816 1 20070705 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR# 5961269, CRACKED STRINGER CLIP, BS 380, S1. REPLACED STRINGER CLIP, BS 380, S1 I AW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071700142 20070717 00142 NM 2007 7 17 AWXA200700822 1 20070629 A 5340 140N20018 STRINGER CLIP BOEING 757 757225 1384959 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - NR 5950483, CRACKED STRINGER CLIP, BS 840, S25L. REPLACED STRINGER CLIP, BS 840, S25L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007071700153 20070717 00153 NM 2007 7 17 AWXA200700831 1 20070628 A 5754 114N4003126 SKIN BOEING 757 757225 1384959 NM ZONE 600 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - NR 5950909, RIGHT WING NR 9 SLAT COVE SKIN CRACKED, WS 677.5 - WS 705.5. REPLACED RIG HT WING NR 9 SLAT COVE SKIN, WS 677.5 - WS 705.5 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007071700177 20070717 00177 WP 2007 7 17 ASAA0781832 1 20070702 A 5311 59360759 FRAME DOUG DC9 DC983 3022083 WP BS 1219 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 AFT CARGO BAY STUB FRAME FORMER CORRODED ON FORWARD AND AFT SIDES. REPLACED FORMER PER SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F RT A6WE 2007071700181 20070717 00181 WP 2007 7 17 ASAA0781837 1 20070702 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 CABIN FLOOR PANEL HAS DAMAGED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND DAC DWGS 9936549 AND 4932106. 2 L 7 2 4F RT A6WE 2007071700196 20070717 00196 EA 2007 7 17 TRAX200700916 1 20070702 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 922EV 7822 PAX DOOR BOTTOM STEP BROKEN. 2 L 7 2 4F RT A21EA 2007071800001 20070718 00001 NM 2007 7 18 DLM90070875 1 20070621 A 5100 NONE DOUG MD900 MD900 3027375 NM NONE NONE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 TEMP REPAIR INSTALLED ON FUSELAGE SKIN AT RT CANT FRAME STA 1531 APPROX 16 IN UP FROM DOOR CUT OUT. REMOVED TEMP REPAIR AND INSTALLED PERM. REPAIR IAW MD90 SRM 53-00-01 FIG 4 VOL I. 1 G 7 2 3U NC H19NM 2007071800002 20070718 00002 NM 2007 7 18 DLM90070876 1 20070621 A 5330 SKIN DOUG MD90 MD9030 3023690 NM BS 220 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 FOUND FUSELAGE SKIN DENTED AT LONG 17 LT STA 220 ON LONGERON. REPAIRED SKIN IAW MD90 SRM 51-30-01 FIG 5 VOL I. 2 L 7 2 4F RT A6WE 2007071800003 20070718 00003 NM 2007 7 18 DLM90070877 1 20070624 A 5730 SKIN DOUG MD90 MD9030 3023690 NM LT WING GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 LT WING FIXED L/E BETWEEN SLAT TRACK NR 8 AND 7 SKIN HAS GOUGES. REPAIRED DAMAGE TO WING L/E IAW MD-90 SRM 57-20-01 FIG 11 VOL 1. 2 L 7 2 4F RT A6WE 2007071800006 20070718 00006 NM 2007 7 18 DLM88070881 1 20070707 A 5330 593600419 SKIN DOUG MD88 MD88 3023688 NM BS 693-712 S29R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 925DL 49712 CORROSION IN SKIN AND CARGO DOOR SURROUND DOUBLER AT FS 693-712 NEAR L-29R. CUTOUT DAMAGE AND INSTALLED DOUBLER AND TR IPLER. 2 L 7 2 4F RT A6WE 2007071800007 20070718 00007 NM 2007 7 18 DLM88070882 1 20070706 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948DL 49879 SKIN DENT BELOW R-1 SERVICE DOOR,FOUND TO BE WITH IN LIMITS PER SRM 53-04D TABLE C. REPAIRED PER SRM 53-04D FIG 38 COND 1B VIEW E ON N/R T0060082 HMV-3. 2 L 7 2 4F RT A6WE 2007071800008 20070718 00008 EA 2007 7 18 TRAX200700935 1 20070705 A 5312 PRESSURE PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 AREAS OF CORROSION ON WING BOX PRESSURE FLOOR UPPER SURFACE SKIN AND DOUBLERS SPANNING BETWEEN FS 424.00 AND FS 559.00 + 16 BETWEEN RBL 45 AND 36. WORK COMPLETED IN ACCORDANCE WITH: CRJ 200 NDTM 51-20-04, REO6 601R-53-41-554, CRJ 200 NDT M 51-20-06, AND SP607. 2 L 7 2 4F RT A21EA 2007071800009 20070718 00009 NM 2007 7 18 DLM88070883 1 20070706 A 5720 ANGLE DOUG MD88 MD88 3023688 NM LT WING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948DL 49879 EXFOLIATION CORROSION ON LT TRAPAZOIDAL PANEL UPPER ANGLE. ANGLE WAS REPLACED PER DWG 5930515 ON N/R TOO60106 HMV-3. 2 L 7 2 4F RT A6WE 2007071800012 20070718 00012 NM 2007 7 18 KCSA071202 1 20070706 A 3350 LIGHT BOEING 747 7472B4B 138481B NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 710CK 21097 UPPER DECK EGRESS/ESCAPE DOOR EMERGENCY LIGHT INOP. 2 L 7 4 4F RT A20WE 2007071800013 20070718 00013 NM 2007 7 18 KCSA071203 1 20070706 A 3350 LIGHT BOEING 747 7472B4B 138481B NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 710CK 21097 CEILING EMERGENCY LIGHT LEFT STA 560 IS INOP. 2 L 7 4 4F RT A20WE 2007071800014 20070718 00014 NM 2007 7 18 KCSA071201 1 20070706 A 3350 LIGHT BOEING 747 7472B4B 138481B NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 710CK 21097 L-5 DOOR EMERGENCY LIGHT INOP. 2 L 7 4 4F RT A20WE 2007071800016 20070718 00016 NM 2007 7 18 KCSA071204 1 20070706 A 5320 SHEAR WEB BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 SLOPING SHEAR WEB CRACKED AT BS 840 RIGHT SIDE BETWEEN STR 10R AND STR 11R. CRACK LENGTH 1 INCH. 2 L 7 4 4F RT A20WE 2007071800017 20070718 00017 NM 2007 7 18 DLM88070886 1 20070706 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 1174-1193 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948DL 49879 FOUND CORROSION ON LEFT CUSP WEB BETWEEN STA Y=1174 AND 1193, TASK 58-533313. REPAIRED PER SRM 51-70-4 ON N/R TOO60302 AT HMV. 2 L 7 2 4F RT A6WE 2007071800019 20070718 00019 NM 2007 7 18 DLM88070888 1 20070705 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 840 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948DL 49879 FOUND CRACK ON RT CUSP WEB AT STATION Y=840, REPAIRED PER ERA 398191-14MA ON N/R T0060308 AT HMV. 2 L 7 2 4F RT A6WE 2007071800020 20070718 00020 NM 2007 7 18 DLM88070889 1 20070706 A 5320 WEB DOUG MD88 MD88 3023688 NM STA 1463 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948DL 49879 FOUND CRACKED WEB AT STA 1463 BETWEEN LONGERON 21-23 LT. REPAIRED PER SRM 53-01 FIG 2 ON N/R T0060676 AT HMV. 2 L 7 2 4F RT A6WE 2007071800021 20070718 00021 NM 2007 7 18 DLM88070890 1 20070706 A 5320 STIFFENER DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948DL 49879 FOUND CRACK ON STIFFENER AT STA Y=1338 LONGERON 01, TASK 58-53309. REPLACED PER DWG 9915562 ON N/R T0060516 AT HMV. 2 L 7 2 4F RT A6WE 2007071800022 20070718 00022 SO 2007 7 18 C2XA07SH038 1 20070707 A 5320 14521700003 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27962 145110 SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 20. MX REPAIRED LT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 2007071800023 20070718 00023 SO 2007 7 18 C2XA07SH039 1 20070707 A 5320 14532637401 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27962 145110 SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION BETWEEN FR 24-25. MX REPAIRED LT OMEGA BEAM BETWEEN FR 24-25 IAW EMB 1 45 SRM 53-00-01 FIG 202. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 2007071800024 20070718 00024 NM 2007 7 18 DLM88070891 1 20070706 A 5313 LONGERON DOUG MD88 MD88 3023688 NM BS 160 S2L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948DL 49879 FOUND CRACK ON LONGERON 2 LT AT STA 160. REPAIRED PER 53-02 FIG 18 ON NR T0060398. 2 L 7 2 4F RT A6WE 2007071800025 20070718 00025 NM 2007 7 18 DLM88070892 1 20070706 A 5313 LONGERON DOUG MD88 MD88 3023688 NM BS 160 L3L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948DL 49879 FOUND CRACK ON LONGERON 3 LT AT STA 160. REPAIRED PER SRM 53-02 FIG 18 ON N/R T0060396 AT HMV. 2 L 7 2 4F RT A6WE 2007071800026 20070718 00026 NM 2007 7 18 DLM88070893 1 20070705 A 5313 LONGERON DOUG MD88 MD88 3023688 NM BS 160 L4L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948DL 49879 FOUND CRACK ON LONGERON 4 LT AT STA 160. REPAIRED PER SRM 53-02 FIG 18 ON N/R T0060397 AT HMV. 2 L 7 2 4F RT A6WE 2007071800027 20070718 00027 NM 2007 7 18 DLM88070894 1 20070706 A 5320 INTERCOSTAL DOUG MD88 MD88 3023688 NM BS 1380-1401 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948DL 49879 EXFOLIATION CORROSION ON INTERCOSTALS BETWEEN FRAME 1380 AND 1401 IN AFT FUSELAGE LOWER SECTION. REPLACED INTERCOSTAL R EF DWG BOEING 9919661 ON NR T0060687 AT HMV GDL. 2 L 7 2 4F RT A6WE 2007071800028 20070718 00028 NM 2007 7 18 HNAA0700141 1 20070707 A 5320 STRAP DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 839EX 226 LITE CORROSION AT STR 29 STRAP BETWEEN STA X467 AND X488.500. 2 H 7 2 4T RT A13NM 2007071800029 20070718 00029 NM 2007 7 18 DLM88070896 1 20070706 A 5311 FRAME DOUG MD88 MD88 3023688 NM BS 1309 L27R-28L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948DL 49879 FOUND CORROSION ON FRAME AT STA. Y=1309 LONGERON 27 RT-28 LT, TASK 57-53300. REPAIRED PER SRM 53-01 FIG 1 ON N/R T00611 08 AT HMV. 2 L 7 2 4F RT A6WE 2007071800030 20070718 00030 NM 2007 7 18 DLM88070897 1 20070709 A 3244 TIRE DOUG MD88 MD88 3023688 NM NR 1 MLG FAILED A DALA O OTHER O OTHER LD LANDING 1 SO 27 969DL 53172 A/C ARRIVED AT GATE E-7, NR 1 MLG TIRE SHREDDED DAMAGING NR 2 AFT BRAKE LINE, LT STRUT CLAMP, SPLASH GUARD, LT INBOAD FL AP (DENT), LT FUSELAGE (MARK), NR 1 ENG NOSE COWL (UNDERSIDE - MARK). 2 L 7 2 4F RT A6WE 2007071800031 20070718 00031 NM 2007 7 18 HNAA0700152 1 20070707 A 5320 STRAP DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 839EX 226 LIGHT CORROSION BETWEEN X510.00 AND X531.500 ON STR 29 STRAP. 2 H 7 2 4T RT A13NM 2007071800038 20070718 00038 EA 2007 7 18 COMA0760460 1 20070630 A 2797 WIRE CNDAIR CL600 CL6002B19 1900309 EA MLG WW NICKED A COMA K NONE N FALSE WARNING CR CRUISE 1 SO 01 914CA 7012 FLIGHT 5169 - FLAP FAIL MESSAGE RECEIVED. LANDED WITHOUT INCIDENT. REPAIRED NICKED WIRE (SHORTING) AT PRESSURE BULKHEA D AFT OF WHEEL WELL. 2 L 7 2 4F RT A21EA 2007071800039 20070718 00039 EA 2007 7 18 COMA0760461 1 20070630 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE N FALSE WARNING CR CRUISE 1 SO 01 914CA 11926 7012 FLIGHT 5169 - FLAP FAIL MESSAGE RECEIVED. LANDED WITHOUT INCIDENT. REPLACED RIGHT BPSU. 2 L 7 2 4F RT A21EA 2007071800043 20070718 00043 SO 2007 7 18 RAIA00707005 1 20070704 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 818HK 145059 PRE FLT 5574 - STL - EMERGENCY LIGHTS AT COCKPIT AND FORWARD AISLE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PO WER SUPPLY. 2 L 7 2 4T RT T00011AT 2007071800044 20070718 00044 NM 2007 7 18 BB07050 1 20070708 A 3350 2012 CHARGER BOEING 767 7672B7 1385107 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 253AY 24894 MAINTENANCE FOUND FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE ON CABIN LEFT SIDE, ROW 18 AND AFT. REPLACED BATTERY CHARGER . NO FURTHER FAULTS. 2 L 7 2 4F RT A1NM 2007071800045 20070718 00045 NM 2007 7 18 CALA0700337 1 20070707 A 3350 BR964411 LIGHT BOEING 737 737500 138449E NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14652 28913 EMERGENCY EXIT LIGHT AT SEAT 19C WAS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT AT SEAT 19C REF AMM 33-51-81. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2007071800046 20070718 00046 EU 2007 7 18 BA07009 1 20070708 A 3350 32146210 POWER SUPPLY AIRBUS 330 A330323 3930335 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 275AY 0370 L1 DOOR EMERGENCY LIGHTS FOUND INOPERATIVE. MAINTENANCE REPLACED THE L1 POWER SUPPLY. 2 L 7 2 4F RT A46NM 2007071800047 20070718 00047 NM 2007 7 18 DL76L070837 1 20070630 A 2930 291702048 TRANSMITTER BOEING 767 767332 1382001 NM HYD SYSTEM INTERMITTENT A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 193DN 28450 CENTER HYD QTY DROPPED TO ZERO 3X ON TAXI OUT. RESERVOIR LIGHT CAME ON OVERHEAD ALSO. FWD TO MCO AND PLACARD PER MEL 2 9-33-02. CTR HYD QTY INDICATION INOP. PERFORM REP CK. REPLACED CENTER RESERVOIR QTY TRANSMITTER PER M/M REMOVE D MCO A PLAC LEAK CHECK OK. 2 L 7 2 4F RT A1NM 2007071800048 20070718 00048 NM 2007 7 18 SB07052 1 20070708 A 3233 69355005 UPLOCK ACTUATOR BOEING 737 7374B7 1384702 NM RT MLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 455UW 44400 44400 24997 CLT FLT919 ON CLIMBOUT FROM CLT, CREW RECEIVED A RIGHT MAIN LANDING GEAR RED AND GREEN LIGHT WHEN PLACING THE GEAR HANDL E FROM UP TO OFF. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND RETURNED TO FIELD AT CLT. FLIGHT LANDED WI THOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR UPLOCK ACTUATOR PER MM 32-32-41-4. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007071800049 20070718 00049 SO 2007 7 18 C2XA07ON009 1 20070625 A 3350 BA50900901 BATTERY PACK EMB 145 EMB145XR 3260214 SO CABIN DISCHARGED A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 12167 145834 SCHEDULE MX - SVC/RTN - ONT - DURING OVERNIGHT INSPECTION MX PERSONNEL FOUND EXIT LIGHT BY LEFT EXIT WINDOW WON'T LIGHT UP. MX PERSONNEL REMOVED AND REPLACED AFT FLOOR EMERGENCY BATTERY PACK AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. THE A/C WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2007071800050 20070718 00050 SO 2007 7 18 C2XA07CL059 1 20070708 A 3234 7455503 CONTROL LEVER EMB 145 EMB145LR 3260212 SO COCKPIT FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13914 14506 6972 145430 BNA FLIGHT 2634 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM BNA. THE AIRCRAFT RETURNED TO B NA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007071800051 20070718 00051 NM 2007 7 18 CALA0700338 1 20070706 A 5210 604468 PAN BOEING 737 7373T0 1384582 NM L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND A .5 INCH CRACK (THREE EACH) IN L-1 DOOR AFT PAN AT NR 5, NR 6, AND NR 7 STOP FITTING ADJUSTMENT ACCESS HOLES. A DOUBLER REPAIR WAS INSTALLED AT EACH CRACK LOCATION IAW ECRA 5210-01941. 2 L 7 2 4F RT A16WE 2007071800055 20070718 00055 NM 2007 7 18 CALA0700342 1 20070708 A 5314 656212526 KEELBEAM BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14613 27326 INSPECTION FOUND CENTER KEEL BEAM AT RIGHT SIDE OF MLG WHEEL WELL BEAM EDGE CORRODED AT THE LOWER SURFACE AROUND FASTENE R HOLES, STA 700-727, RBL 7. THE KEEL BEAM WAS REPAIRED IAW ECRA 5311-01336. 2 L 7 2 4F RT A16WE 2007071800056 20070718 00056 2007 7 18 UPS07250122 4 20070705 A 2565 SLIDE BOEING 727 72722C 138400F NM COCKPIT OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:N/A EMERGENCY SLIDE TORN OFF CABIN/COCK PIT ENTRY DOOR, UNABLE TO REINSTALL. DEF YBDER N353884. INSTALL ED EVAC SLIDE MAIN CABIN DOOR PER MM CHAP 25-60-14-2. 2 L 7 3 4F A3WE 2007071800057 20070718 00057 NM 2007 7 18 UPS07550130 1 20070613 A 5311 143N1024118 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 420UP 23907 INSPECTION TYPE:C DENT IN FWD CARGO FUSELAGE FRAME STA 780, APPROX S24R TO S25R. ACCOMPLISHED ON FINAL EA 757-5453-27-A 1693 AND UPS EO B757-5310-27142-A. 2 L 7 2 4F RT A2NM 2007071800058 20070718 00058 NM 2007 7 18 UPS07550132 1 20070613 A 5311 143N1024116 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 420UP 23907 INSPECTION TYPE:C DENTS IN FWD CARGO FUSELAGE FRAME STA 680, BETWEEN S23R TO S25R, 2EA. ACCOMPLISHED ON FINAL EA 757-53 32-A1694 AND UPS EO B757-5310-27161-A. 2 L 7 2 4F RT A2NM 2007071800059 20070718 00059 NM 2007 7 18 UPS07550133 1 20070612 A 5311 146N103074 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 420UP 23907 INSPECTION TYPE:N/A DENT IN AFT CARGO FUSELAGE FRAME STA 1580, BETWEEN S25L AND S26L. ACCOMPLISHED ON FINAL EA 757-5362 -27-A1687 AND UPS EO B757-5310-27132-A. 2 L 7 2 4F RT A2NM 2007071800061 20070718 00061 NM 2007 7 18 UPS07550135 1 20070612 A 5311 146N102911 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 420UP 23907 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1460 APPROX S26L. ACCOMPLISHED ON FINAL EA 757-5362-27-A1699 AND UPS EO B757-5310-27182-A. 2 L 7 2 4F RT A2NM 2007071800062 20070718 00062 NM 2007 7 18 UPS07550136 1 20070613 A 5311 146N10249 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 420UP 23907 INSPECTION TYPE:C DENT IN FWD CARGO FUSELAGE FRAME STA 700, APPROX S24L. ACCOMPLISHED ON FINAL EA 757-5453-27-A1692 AND UPS EO B757-5310-27138-A. 2 L 7 2 4F RT A2NM 2007071800063 20070718 00063 NM 2007 7 18 UPS07550137 1 20070612 A 5311 146N102886 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 420UP 23907 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1340, APPROX S26L. ACCOMPLISHED ON FINAL EA 757-5362-27-A1686 AN D UPS EO B757-5310-27141-A. 2 L 7 2 4F RT A2NM 2007071800068 20070718 00068 WP 2007 7 18 UPS07850131 1 20070629 A 5312 BULKHEAD DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 MAIN CABIN AFT PRESS BULKHEAD CRACKED 2 INCHES LONG AT STA 1766 BETWEEN L10L AND L11L, LBL 30. CUT O UT DAMAGED AREA OF PRESS BULKHEAD STA 1766 L10L AND L11L IAW SRM 53-02-05 FIG 14A. FABRICATED AND INSTALLED REPAIR DOUB LER, FINGER DOUBLER, AND FILLER AT STA 1766 PRESS BULKHEAD BETWEEN L10L AND L11L IAW SRM 53-02-05 FIG 1A, SRM 53-02-05 F IG 14A. 2 L 7 4 4F RT 4A25 2007071800070 20070718 00070 NM 2007 7 18 DL76G070904 1 20070703 A 4900 UNKNOWN BOEING 767 7673P6 1385105 NM APU UNKNOWN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 152DL 19928 24984 AFTER STARTING APU DUCT PRESS NEVER ROSE ABOVE 10 PSI WITH PACKS OFF. SHUT DOWN AND RESTARTED WITH NO SUCCESS. REPLA CED TOTAL PRESSURE SENSOR, NO HELP. APU EGT AT 522 DEG C. IN DUCT PRESSURIZATION MODE. PER FIM AND APU SHOP 500 DEG C MAX NEEDS APU. REMOVED APU PN 3800298-1-5 SN P-1706 PER MM. INSTALLED APU PER MM 49-11-01. NO HELP. REPLACED ECU N O HELP. REINSTALLED ORIGINAL REPLACED SURGE VALVE CHECKS GOOD MCO AND PLAC REMOVED MFG P/N 979806-12. 2 L 7 2 4F RT A1NM 2007071800074 20070718 00074 NE 2007 7 18 AALA20071228 2 20070702 A 7261 BEARING AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C2A5 NE RT ENGINE LEAKING A AALA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 19059 469 695222 MIA - IMMEDIATELY AFTER TAKEOFF SMOKE ALARMS SOUNDED AND SMOKE REPORTED IN THE CABIN. RETURNED TO MIA AND LANDED WITHOU T INCIDENT. ACCOMPLISHED RIGHT ENGINE CHANGE DUE TO OIL LEAK AT NUMBER ONE BEARING. SYSTEM GROUND CHECKED NORMAL OPERA TION. 2 L 7 2 4F 4 F RT A35EU E13NE 2007071800075 20070718 00075 WP 2007 7 18 AALA20071225 1 20070701 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 419AA 49331 LGA - EMERGENCY LIGHTS AT BOTH OVERWING EXIT SIGNS IN AFT CABIN INOPERATIVE. CLEANED CORROSION ON BATTERY PACK FOR EMER GENCY LIGHTS AT OVERWING EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071800079 20070718 00079 NM 2007 7 18 AALA20071231 1 20070703 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 789AN 30252 JFK - EMERGENCY LIGHT AT SEAT 36C INOPERATIVE. REPLACED BULB FOR EMERGENCY LIGHT AT SEAT 36C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007071800080 20070718 00080 NM 2007 7 18 AALA20071232 1 20070703 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 789AN 30252 JFK - EMERGENCY LIGHT AT SEAT 36C HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 36C. SYSTEM GROUND CHECK ED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT T00001SE 2007071800081 20070718 00081 NM 2007 7 18 AALA20071235 1 20070703 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 620AA 24578 JFK - EMERGENCY LIGHT AT AFT DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT DOOR. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071800087 20070718 00087 WP 2007 7 18 AALA20071234 1 20070703 A 3350 SHROUD DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9407R 49400 DFW - EMERGENCY LIGHT AT SEAT 17D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007071800088 20070718 00088 EU 2007 7 18 AALA20071241 1 20070705 A 2420 GCU AIRBUS 300 A300B4605R 3930308 EU LT GENERATOR FAULTED A AALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 SW 21 11060 470 JFK - LEFT GENERATOR FAILED IN FLIGHT. AUXILLIARY POWER UNIT WOULD NOT START. LANDED JFK WITHOUT INCIDENT. FLIGHT WAS OVERWEIGHT. REPLACED GENERATOR CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007071800089 20070718 00089 NM 2007 7 18 UPS07M50139 1 20070424 A 5720 DOUBLER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C LEFT LEADING EDGE LWR COMPT 519CB (PRESSURE REFUEL) FOUND STIFFENER DOUBLER SUSPECTED CRACK AS MARKED. HFEC INSP CUTOUT FOUND CRACK APPROX .25 INCH. LEFT WING LEADING EDGE LWR COMPT 519CB (PRESS REFUEL) RIBS REMOVED. CR ACK AREA TRIMMED OUT. HFEC CUTOUT ON TRIMMED EDGE FOUND NO CRACK. NEW REPAIR FILLERS 02EA, DOUBLER & ANGLES 06EA FAB, HEAT TREATED & HOLES DRILLED. REPAIRED PARTS & TRIMMED AREA REPROTECTED & PAINTED. REPAIR PARTS INSTALLED. 2 L 7 3 4F RT A22WE 2007071800090 20070718 00090 SO 2007 7 18 C2XA07CL060 1 20070708 A 3350 3104404 FUSE EMB 145 EMB145EP 3260221 SO CABIN BLOWN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13935 145022 DURING ROUTINE MAINTENANCE THE AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE AT ROW 3 THRU 7. ALSO THE EXIT LIGHT AT ROW 2 AND THE EMERGENCY LIGHT ON THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND FOUND THE FUSE BLOWN ON THE N R 2 EMERGENCY LIGHT BATTERY CHARGER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2007071800091 20070718 00091 EA 2007 7 18 TRAX200700937 1 20070705 A 5350 COVER CNDAIR CL600 CL6002B19 1900309 EA TAILCONE MISSING A ASOA K NONE D INFLIGHT SEPARATION CR CRUISE 1 SO 27 680BR 7679 RIGHT ENG MISSING INSPECTION COVER ON TOP LEFT SIDE OF TAIL CONE. FLTS 4672, 4713 CX. 2 L 7 2 4F RT A21EA 2007071800092 20070718 00092 NM 2007 7 18 ZZDA070602186 1 20070602 A 5310 DOOR FRAME BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 FWD CARGO COMPARTMENT DOOR CUTOUT LOWER SECTION HAS SPOTS OF CORROSION. INSTALLED DOOR JAMB LOWER SECTION AT FWD CARGO COMPARTMENT DOOR CUTOUT AS PER B717 SRM 53-20-115. 2 L 7 2 4F TR A6WE 2007071800093 20070718 00093 NM 2007 7 18 ZZDA070603187 1 20070603 A 5320 PAN BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 AFT CARGO COMPARTMENT DOOR CUTOUT LOWER SECTION HAS SPOTS OF CORROSION. ROUT OUT DAMAGED AREAS AND INSTALLED (2 EA) DOU BLERS REPAIRS, FABRICATED FROM 7075-0 .063 AND HEAT TREATED TO T-6. DIMENSION 4.5 X 4.25 INCHES AND 4.5 X 4.5 INCHES AS PER MESSAGE 1-383694435-1 AND AIRTRAN EA 17-53-00526IR. 2 L 7 2 4F TR A6WE 2007071800094 20070718 00094 NM 2007 7 18 ZZDA070704185 1 20070704 A 3397 WIRE BOEING 717 717200 1383700 NM CABIN BROKEN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 987AT 55088 ROW 17 DEF EMERGENCY EXIT LIGHT INOP (E-PATH). REPAIRED BROKEN WIRE AT SEAT DISCONNECT IAW SWPM 20-10-01, OPS CHECK NOR MAL IAW AMM 33-51-00. 2 L 7 2 4F TR A6WE 2007071800096 20070718 00096 WP 2007 7 18 ASAA0781846 1 20070702 A 5320 9930538 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 CABIN RIGHT CUSP WEB CORRODED BETWEEN BS 503 AND BS 541. REMOVED DAMAGED CUSP WEB, LOCATED DRILLED AND INSTALLED A REPL ACEMENT WEB IAW SRM 51-10-4 PG 1, 51-30-2 PG 1 AND 51-30-5 PG 1. 2 L 7 2 4F RT A6WE 2007071800097 20070718 00097 WP 2007 7 18 ASAA0781847 1 20070704 A 5320 5936660167 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 AFT CARGO RIGHT ZEE ANGLE CORRODED. REMOVED DAMAGED SECTION OF ZEE, LOCATED DRILLED AND INSTALLED A REPLACEMENT SECTION IAW SRM 51-30-5 PG 3 21 AND 51-30-1 PG 13. 2 L 7 2 4F RT A6WE 2007071800098 20070718 00098 WP 2007 7 18 ASAA0781848 1 20070704 A 5347 593056671 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 CABIN SEAT TRACK CORRODED. REMOVED DAMAGED AREA OF TRACK, LOCATED, DRILLED AND INSTALLED A REPLACEMENT SECTION IAW SRM 53-05 FIG 4A PG 8C AND 8D. 2 L 7 2 4F RT A6WE 2007071800102 20070718 00102 WP 2007 7 18 ASAA0781855 1 20070704 A 5753 5930496508 SKIN DOUG DC9 DC983 3022083 WP T/E FLAP VANE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 RIGHT WING O/B FLAP I/B VANE GOUGED ON LEADING EDGE 7 INCHES FROM I/B END. PREPAIRED DAMAGED AREA, FABRICATED DOUBLER A ND INSTALLED IAW SRM 51-70-2 PG 59. 2 L 7 2 4F RT A6WE 2007071800103 20070718 00103 NM 2007 7 18 AALA20071243 1 20070705 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 685AA 25342 MIA- LEFT NUMBER ONE DOOR EMERGENCY LIGHT SWITCH LEFT ON. EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATT ERY PACK AT STATION 400 FOR EMERGENCY LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071800104 20070718 00104 NM 2007 7 18 AALA20071244 1 20070705 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 685AA 25342 MIA - LEFT NUMBER ONE EMERGENCY LIGHT SWITCH LEFT ON. EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT STATION 700 FOR EMERGENCY LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071800105 20070718 00105 NM 2007 7 18 AALA20071245 1 20070705 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 685AA 25342 MIA - LEFT NUMBER ONE DOOR EMERGENCY LIGHT SWITCH LEFT ON. EMERGENCY LIGHTS IN MID CABIN INOPERATIVE. REPLACED BATTERY PACK AT STATION 1050 FOR EMERGENCY LIGHTS IN MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071800106 20070718 00106 NM 2007 7 18 AALA20071246 1 20070705 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 685AA 25342 MIA - LEFT NUMBER ONE DOOR EMERGENCY LIGHTS SWITCH LEFT ON. EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTER Y PACK AT STATION 1635 FOR EMERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071800107 20070718 00107 NM 2007 7 18 AALA20071257 1 20070706 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 664AA 25298 MIA - EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071800108 20070718 00108 NM 2007 7 18 AALA20071247 1 20070705 A 3350 PBS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 685AA 25342 MIA - LEFT NUMBER ONE DOOR EMERGENCY LIGHTS SWITCH LEFT ON. EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BA TTERY PACK AT STATION 345 FOR EMERGENCY LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071800109 20070718 00109 NM 2007 7 18 AALA20071248 1 20070705 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 685AA 25342 MIA - LEFT NUMBER ONE DOOR EMERGENCY LIGHTS SWITCH LEFT ON. EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BA TTERY PACK AT STATION 365 FOR EMERGENCY LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071800110 20070718 00110 NM 2007 7 18 AALA20071249 1 20070705 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 685AA 25342 MIA - LEFT NUMBER ONE DOOR EMERGENCY LIGHTS SWITCH LEFT ON. EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BA TTERY PACK AT STATION 710 FOR EMERGENCY LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071800111 20070718 00111 NM 2007 7 18 AALA20071250 1 20070705 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 685AA 25342 MIA - LEFT NUMBER ONE DOOR EMERGENCY LIGHTS SWITCH LEFT ON. EMERGENCY LIGHTS IN MID CABIN INOPERATIVE. REPLACED BATTER Y PACK AT STATION 985 FOR EMERGENCY LIGHTS IN MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071800112 20070718 00112 NM 2007 7 18 AALA20071251 1 20070705 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 685AA 25342 MIA - LEFT NUMBER ONE DOOR EMERGENCY LIGHTS SWITCH LEFT ON. EMERGENCY LIGHTS IN MID CABIN INOPERATIVE. REPLACED BATTER Y PACK AT STATION 1095 FOR EMERGENCY LIGHTS IN MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071800113 20070718 00113 NM 2007 7 18 AALA20071252 1 20070705 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 685AA 25342 MIA - LEFT NUMBER ONE DOOR EMERGENCY LIGHTS SWITCH LEFT ON. EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTER Y PACK AT STATION 1240 FOR EMERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071800114 20070718 00114 NM 2007 7 18 AALA20071253 1 20070705 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 685AA 25342 MIA - LEFT NUMBER ONE DOOR EMERGENCY LIGHTS SWITCH LEFT ON. EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTER Y PACK AT STATION 1665 FOR EMERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071800116 20070718 00116 NM 2007 7 18 AALA20071255 1 20070706 A 3350 8039001 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9412W 53187 LGA - EMERGENCY LIGHTS AT FIRST CLASS GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS GAL LEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2007071800117 20070718 00117 NM 2007 7 18 AALA20071258 1 20070706 A 3397 WIRE HARNESS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 395AN 29432 LGA - SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 41HJ INOPERATIVE. REPAIRED HARNESS FOR EMERGENCY LIGHTS AT SEATS 41HJ. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007071300179 20070713 00179 EA 2007 7 13 COMA0770036 1 20070628 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002C10 1390015 EA LAVATORY ACTIVATED A COMA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 01 655CA 10134 FLIGHT 4933 - AFTER TAKEOFF AIRCRAFT DIVERTED BACK TO GSO FOR LAV FIRE WARNING. AIRCRAFT LANDED SAFELY. PERFORMED ENGI NE RUN WITH BLEEDS ON, ALL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007071300187 20070713 00187 EA 2007 7 13 TRAX200700904 1 20070627 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 870AS 7530 CRACK FOUND ON FLOOR SUPPORT FITTING FS 460 RBL 9 O/B. REMOVED AND REPLACED FLOOR SUPPORT FITTING IAW SRM 51-41-43. SU PPLEMENTAL - SDR CLOSED 07/05/07. 2 L 7 2 4F RT A21EA 2007071300195 20070713 00195 NM 2007 7 13 SWAA073291 1 20070703 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007071300198 20070713 00198 NM 2007 7 13 SWAA073294 1 20070703 A 5311 6546525 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071300203 20070713 00203 NM 2007 7 13 SWAA073321 1 20070704 A 5230 6547953 SKIN BOEING 737 7375H4 138449D NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR HANDLE CUTOUT CRACKED AT AFT UPPER RADIUS. REPAIRED DOOR PER SWA EA. 2 L 7 2 4F RT A16WE 2007071300230 20070713 00230 NM 2007 7 13 SWAA073307 1 20070703 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071300235 20070713 00235 NM 2007 7 13 SWAA073312 1 20070703 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 710SW 27844 DURING SCHEDULED MV2 CHECK, FOUND RT AFT FUSELAGE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007071300237 20070713 00237 NM 2007 7 13 SWAA073311 1 20070703 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 710SW 27844 DURING SCHEDULED MV2 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007071300238 20070713 00238 NM 2007 7 13 HALA0700276 1 20070705 A 2910 RELAY BOEING 767 76733A 1385209 NM HYD SYSTEM MALFUNCTIONED A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 580HA 28140 ETOPS SIGNIFICANT SYSTEM, EICAS MSG "C HYD SYS MAINT" DISPLAYED HYD PRESS NORMAL. REPLACED HYD GEN ADP CMD RELAY K865 & SYS 1 AIR/GROUND RELAY K1788 PERFORMED OPERATIONAL TEST PER M/M 29-11-00-715-896. OPS CKS NORMAL. 2 L 7 2 4F RT A1NM 2007071300245 20070713 00245 2007 7 13 SWAA073320 4 20070704 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071300249 20070713 00249 NM 2007 7 13 SWAA073313 1 20070704 A 3234 MS253831 SWITCH BOEING 737 7373H4 1384600 NM COCKPIT FAULTY A SWAA K NONE N FALSE WARNING AP APPROACH 1 SW 29 653SW 28398 ON FINAL APPROACH LANDING GEAR SELECTED DOWN. THREE GREEN AND THREE RED LIGHTS ILLUMINATED. CYCLED GEAR HANDLE, THREE GREEN LIGHTS ILLUMINATED. REMOVED AND REPLACED LANDING GEAR LEVER SWITCH PER MM. 2 L 7 2 4F RT A16WE 2007071300261 20070713 00261 SO 2007 7 13 SIMA200719107 1 20070522 A 5347 14530659005 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 15926 5000 145224 LEFT INBOARD SEAT TRACK BETWEEN FRAME 36 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMER ICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R2. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300264 20070713 00264 SO 2007 7 13 SIMA200719109 1 20070522 A 5347 13500438003 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 15926 5000 145224 RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 24 AND 36 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETU RNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300281 20070713 00281 2007 7 13 2007UALA02374 4 20070702 A 2565 COVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 SLIDE LOOSE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 444UA 824 THE 2R SLIDE COVER COMING OFF. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071300286 20070713 00286 SO 2007 7 13 SIMA200719001 1 20070706 A 5250 A411259 LOCK EMB 135 EMB135KL 3260302 SO ZONE 200 BROKEN A SIMA O OTHER O OTHER CR CRUISE 1 SW 21 823AE 12898 145582 LAVATORY DOOR LOCKS AND WILL NOT UNLOCK, TRAPPED PASSENGER INSIDE LAVATORY, EITHER NORMAL OR ALTERNATE RELEASE PROCEDURE S WORK. REMOVED AND REPLACED LAVATORY DOOR LOCK IAW EMB AMM 25-40-02. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SE RVICE. 2 L 7 2 4F RT T00011AT 2007071300291 20070713 00291 SO 2007 7 13 SIMA200719203 1 20070603 A 5347 13500438001 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 15957 5000 145235 RIGHT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 21 AND 24. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300299 20070713 00299 SO 2007 7 13 SIMA200719211 1 20070621 A 5347 14532605015 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 811AE 13526 5000 145529 LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 36 AND 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300302 20070713 00302 NM 2007 7 13 2007UALA02382 1 20070703 A 3350 BR964421 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 813UA 858 SEAT EEL LIGHT ASSY HAS ONE BULB INOP. LIGHT ASSY DAMAGED. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071300304 20070713 00304 2007 7 13 2007UALA02384 4 20070703 A 2565 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R1 DOOR LOW PRESSURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 473UA 1469 DOOR 1R PRESSURE IS LOW. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071300320 20070713 00320 NM 2007 7 13 C77A200700002 1 20070517 A 2760 270007 PCU BOMBDR CL600 CL6002D15 NM SPOILERS MISRIGGED A C77A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 601XJ 17057 2 8044 ON TAKEOFF ROLL, CONFIGURATION, SPOILERS MESSAGE APPEARED. ABORTED TAKEOFF. FOUND LT INBOARD SPOILER PCU SLIGHTLY OUT OF RIG, ADJUSTED SPOILER IAW AMM. 2 L 7 2 4F RT A21EA 2007071300329 20070713 00329 NM 2007 7 13 2007UALA02405 1 20070703 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 MAIN STAIRS EEL LIGHTS INOPERATIVE. [07-24-07] SECURED CONNECTOR. OPS. NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071300332 20070713 00332 NM 2007 7 13 2007UALA02408 1 20070704 A 2121 FAN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 198UA 28716 EXPERIENCED ODOR OF SMOKE. SUSPECT COOLING FAN. FLIGHT CONTINUED TO DESTINATION. [07-27-07] REPLACED RECIRCULAT ION FAN LT PER MM 21-25-07, OPS CHECK NORMAL, NO FURTHER MSG DISPLAYED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071300344 20070713 00344 NM 2007 7 13 QXEA200701044 1 20070620 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - THERE IS A DENT AND SCRATCH ON THE TOP OF FUSELAGE AFT OF X222 APPROXIMATELY 3" BETWEEN STRINGERS 5R AND 6R. R EPAIRED IAW DHC 8 SRM 51-20-16 AND 1-20-41. 2 H 7 2 4T RT A13NM 2007071300351 20070713 00351 NM 2007 7 13 07FDEA02376 1 20070705 A 5313 69436659 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD LWR CARGO PIT BILGE, FRAME ATTACH ANGLE LWR END HAS CORROSION, STA. 720E OB SIDE AT KEEL BEAM EXTENSION STR 28R REMO VED FRAME ATTACH ANGLE SRM 51-30-2. FABRICATED NEW FRAME ATTACH ANGLE REF BOEING DWG 69-43665-1/1. TREATED AND PRIMED NEW ANGLE, SRM 51-10-2. INSTALLED FRAME ATTACH ANGLE SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007071300357 20070713 00357 EA 2007 7 13 QXEA200701083 1 20070703 A 2820 L92B13602 CARTRIDGE CNDAIR CL600 CL6002C10 1390015 EA FUEL UNKNOWN A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 601QX 10009 DEN - ON CLIMB-OUT, RECEIVED A LEFT XFER SOV FUEL CAUTION. AFTER CHECKLIST PERFORMED, NO FURTHER PROBLEMS. RETURNED TO THE FIELD. MAINTENANCE REPLACED THE LEFT FUEL TRANSFER SOV CARTRIDGE. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007071300359 20070713 00359 EA 2007 7 13 QXEA200701085 1 20070703 A 7930 4120T17P02 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA ENGINE OIL MALFUNCTIONED A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 609QX 10031 DEN - ON TAXI OUT, RECEIVED A LEFT ENGINE OIL PRESSURE WARNING. RETURNED TO THE GATE. MAINTENANCE REPLACED THE ENGINE OIL PRESSURE SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007071300361 20070713 00361 NM 2007 7 13 SWAA073327 1 20070705 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 20R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007071300363 20070713 00363 NE 2007 7 13 HEEA116155 1 20070627 A 2422 SPC38G INVERTER SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL1S1 60030 NE INOPERATIVE B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 761P 760588 APPROX 7 MILES EAST, AIRCRAFT HAD A COLLECTIVE TRIM FAILURE, THE FUEL ON THE NR 1 SIDE WENT TO ZERO AND THE IDS DISPLAY ON THE NR 1 SIDE FAILED, ALONG WITH A YELLOW FUEL LIGHT INDICATING ONLY 210 POUNDS OF FUEL ON BOARD. THE OAT GAUGE ON T HE NR 2 IIDS DISPLAY TURNED AMBER. MAINTENANCE REPLACED INVERTER AND RADU -76450-01098-106. 1 G 7 2 3U 3 U NC H1NE E19EU 2007071300380 20070713 00380 NM 2007 7 13 F3LA200700170 1 20070702 A 3240 351H51002 MONITOR AIRBUS A319 A319111 3930336 NM BRAKE TEMP INOPERATIVE A F3LA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 918FR 1553 1943 AFTER TAKEOFF FROM KDCA, RECEIVED ECAM FOR HOT BRAKES. LOWERED GEAR AND NR 2 BRAKE INDICATED 980 DEG C. SHORTLY AFTER, NR 2 BRAKE INDICATOR WENT TO 2 AMBER XX FOR TEMP INDICATOR. FLIGHT CREW DECLARED AN EMERGENCY AND DIVERTED TO KIAD. A IRCRAFT LANDED WITHOUT INCIDENT AND TAXI WAS NORMAL. ITEM WAS TRANSFERRED TO MEL REF 32-47-01A, CONTROL NR 1028764. PU LLED AND COLLARED C/B 37 PER MEL. UPON ARRIVAL IN DEN, REPLACED THE BRAKE TEMP MONITORING UNIT IAW AMM 32-47-18-400-001 AND OPS CHECKED GOOD. 2 L 7 2 4F RT A28NM 2007071300384 20070713 00384 NM 2007 7 13 UPS07M50101 1 20070507 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C EMPENNAGE/LT HORIZONTAL STABILIZER BARREL NUT NR 24 LT FOUND BORE CORRODED. CORROSION AT BARREL NUT B ORE REMOVED, BOTTOM REMAINING BLEND OUT EXCEEDS LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS AND BOTTOM PERIPHERY RADIUSED SMOOTHENED AND PROTECTED. REPAIR SLEEVE BUSHING FAB AND PROTECTED, PR1422 B1/2 SEALANT AP PLIED AT BLEND OUT VOIDS AND REPAIR SLEEVE BUSHING INSTALLED. REWORK AREA PAINTED. 2 L 7 3 4F RT A22WE 2007071300389 20070713 00389 NM 2007 7 13 UPS07M50108 1 20070522 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C RT HORIZONTAL STABILIZER BARREL NUT HOLE NR 16 BORE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMO VED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTT OM PERIPHERY RADIUSED SMOOTHENED AND PROTECTED. REPAIR SLEEVE BUSHING FAB AND PROTECTED, PR1422 B1/2 SEALANT APPLIED AT BLEND OUT VOID AND REPAIR SLEEVE BUSHING INSTALLED. REWORK AREA PAINTED. 2 L 7 3 4F RT A22WE 2007071300392 20070713 00392 NM 2007 7 13 UPS07M50111 1 20070510 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C RT HORIZONTAL STABILIZER BARREL NUT NR 23 FOUND BORE CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTTOM PE RIPHERY RADIUSED SMOOTHENED AND PROTECTED. REPAIR SLEEVE BUSHING FAB AND PROTECTED, PR1422 B1/2 SEALANT APPLIED AT BLEN D OUT VOID AND REPAIR SLEEVE BUSHING INSTALLED. REWORK AREA PAINTED. 2 L 7 3 4F RT A22WE 2007071300409 20070713 00409 NM 2007 7 13 SWAA073344 1 20070705 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 2007071600003 20070716 00003 EU 2007 7 16 CPCP20070052 1 20070511 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 260AE 263 FOUND FLOORBEAM AT FRAME 38 IS CORRODED. FLOORBEAM AT FRAME 38 REPLACED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007071600009 20070716 00009 NM 2007 7 16 07FDEA02382 1 20070706 A 5320 66167701 CHANNEL BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LEFT GEAR BODY DOOR AFT STOP FITTING SUPPORT CHANNEL IS CRACKED AND BROKEN AT LWR ATTACH FLANGES AND STRAP. FABRICATED REPAIR CHANNEL AND ANGLES IAW B727 SRM 51-40-3. ALODINE, AND PRIME REPAIR PARTS IAW B-727 SRM 51-10-2. INSTALL FASTENE RS IAW B-727 SRM 51-30-2. INSTALLED REPAIR PARTS IAW B-727 SRM51-40-3 PG 1. THIS REPAIR IS CLASSIFIED AS MINOR. 2 L 7 3 4F RT A3WE 2007071600016 20070716 00016 NM 2007 7 16 07FDEA02344 1 20070629 A 5311 AFA00283 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 MAIN DECK CARGO, RIGHT FRAME 1681 AT STRINGER L12 FOUND DENT. REPAIR CARRIED OUT AT MAIN DECK CARGO, RIGHT FRAME 1681 A T STRINGER L12 AS PER SRM 53-30-00 FIGURE I VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007071600025 20070716 00025 NM 2007 7 16 07FDEA02393 1 20070707 A 5330 6554574 SKIN BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 FWD CARGO BAY INNER SKIN HAS CORROSION, BS 720C TO 720C 6 ", LBL 205" TO 5" WL 148.5. CUT OUT DAMAGE SKIN AT BS 720C TO 726C IAW B727 SRM 53-30-3. 2 L 7 3 4F A3WE 2007071600027 20070716 00027 NM 2007 7 16 07FDEA02395 1 20070707 A 5313 65562491 STRINGER BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 AFT PIT STRINGER 27R CORRODED FROM STA 1030-1060, BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED SHEAR TIE A ND DAMAGED SECTION OF STRINGER. FABRICATED STRINGER REPAIR PARTS AND DRILLED TO FIT. TREATED AND PRIMED REPAIR PARTS. INSTALLED STRINGER REPAIR AT STA 1030-1060 STRINGER 27L AND REINSTALLED SHEAR TIE, REF SRM 53-10-1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2007071600037 20070716 00037 WP 2007 7 16 07FDEA02417 1 20070710 A 5347 S4929405 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 MAIN CABIN SEAT TRACK AT LBL - 8 BETWEEN STA 1681 AND 1701 IS GOUGED BLENDED SEAT TRACK AND OUT OF LIMITS. REMOVED AND INSTALLED NEW SEAT TRACK IAW DC/MD 10 SRM 53- 70-00 VOL I PG 3. FABED SEAT TRACK AND 2 SPLICE HAT AND 2 PLATES IAW DC/ MD 10 SRM 53-70-00 VOL I PG 3. 2 L 7 3 4F RT A22WE 2007071600040 20070716 00040 EU 2007 7 16 07FDEA02421 1 20070711 A 5320 A534974321000 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 CORROSION DETECTED ON CORNER FITTING AT C63 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007071600041 20070716 00041 EU 2007 7 16 07FDEA02422 1 20070711 A 5313 A53986219 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 OLD REPAIR ON P37, C54.3 RT NOT CONFORM TO SRM. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007071600049 20070716 00049 EU 2007 7 16 07FDEA02429 1 20070711 A 5315 A53970197 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 749FD 536 OLD TOP CAP BEAM REPAIR ON C55 NOT CONFORM TO SRM. TOP CAP BEAM REPAIR RENEWED IAW SRM 53-10-15 FIG 208. 2 L 7 2 4F RT A35EU 2007071600054 20070716 00054 NM 2007 7 16 07FDEA02403 1 20070709 A 5100 651593810 FRAME BOEING 727 727233 138408A NM ZONE 100 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FOUND REPAIR LOCATED AT BS 700 ON FRAME BETWEEN STR S-20R AND S-23R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMI NATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING REPAIR REF SRM 51-30-2. FABRICATED INNER CHORD REF DWG 65-82614. INSTALLED REPAIR ANGLES REF DWG 65-15938 AND DWG 65-82614 AND SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007071600064 20070716 00064 NM 2007 7 16 QXEA200701098 1 20070708 A 2131 92146A010401 CONTROLLER BOMBDR DHC8 DHC8402 1390042 NM CABIN PRESSURE MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 423QX 14089 14089 4153 SEA FLIGHT NR 2292: CABIN AUTO PRESSURIZATION CONTROL INOP. FAULT LIGHT ILLUMINATED IN AUTO MODE. FAULT LIGHT EXTINGUI SHED IN MANUAL MODE PER A/C EMERGENCY CHECKLIST. ABLE TO CONTROL PRESSURIZATION MANUALLY. MAINTENANCE REMOVED AND REPL ACED CABIN PRESSURIZATION CONTROLLER IAW AMM Q400 TASK 21-31-06-000-801 AND 21-31-06-400-801. OPS CHECK GOOD. NO FURTH ER DEFECTS NOTED. PLACARD REMOVED FROM LOG BOOK AND CABIN PRESSURE CONTROL PANEL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071600069 20070716 00069 NM 2007 7 16 07FDEA02413 1 20070710 A 5313 655623663 STRINGER BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 FWD CARGO BAY STR S-28R I/B UPPER FLANGE IS CORRODED AT BS 530. REMOVED CORROSION. ORIGINAL MATERIAL THICKNESS WAS .06 3". REMAINING MATERIAL IS OUT OF LIMITS AT .043". FABBED, TREATED, AND PRIMED REPAIR PART, P/N BAC1498-132. INSTALLED REPAIR PART AND NUT SPACERS AFTER DAMAGE WAS REMOVED, REF SRM 51-10-6 AND SRM 53-10-3, PG 3-4B. 2 L 7 3 4F A3WE 2007071600078 20070716 00078 NM 2007 7 16 QXEA200701063 1 20070625 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 467 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX-CABIN UNDER FLOOR LEFT AT FRAME X467.00 AND BETWEEN STRINGER 29L AND 30L, FRAME CASTELLATION HAS CORROSION AT FAS TENERS. REPAIRED IAW SRM 51-20-11, 51-40-11, AND 51-20-51. 2 H 7 2 4T RT A13NM 2007071700030 20070717 00030 EA 2007 7 17 A6WA200740314 1 20070614 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FLOORBEAM CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 434AW 7322 LT FLOORBEAM ATTACH CLIPS ARE CRACKED AT IB AND OB SIDES FS 280, LBL 9, WL 72. (K) [07-31-07] MAINTENANCE REPAIRED IAW CRJ 200 SRM 51-42-13 AND 51-42-21 AND BSC STANDARD REPAIR NR 601R-53-0057A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700044 20070717 00044 EA 2007 7 17 A6WA200740328 1 20070614 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 460AW 7867 UNDERFLOOR SUPPORT INTERCOSTAL HAS A CRACKED FLANGE AT IB SIDE OF LBL 36, FS 484, WL 72.5. MAINTENANCE CUT OFF CRACKED F LANGE AND INSTALLED REPAIR ANGLE IAW REO 601R53-41-059. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700056 20070717 00056 EA 2007 7 17 A6WA200740343 1 20070625 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 462AW 7875 HYDRAULIC LINE Z-BRACKET (PN 601R75262-153) CRACKED APPROX .1 INCH LONG IN RT MLG WHEEL WELL. MAINTENANCE REMOVED AND R EPLACED BRACKET (PN 601R75262-153) IAW SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700057 20070717 00057 EA 2007 7 17 A6WA200740344 1 20070624 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 462AW 7875 PAX DOOR AFT DRAG ANGLE CRACKED JUST ABOVE ASSIST MOTOR PULLEY BRACKET. MAINTENANCE CUT OUT DAMAGED AREA AND INSTALLED REPAIR ANGLE IAW REO 601R-52-11-513. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700059 20070717 00059 WP 2007 7 17 ASMF200707006 1 20070709 A 5511 5930602515 SPAR CAP DOUG DC9 DC983 3022083 WP HORIZONTAL STAB CRACKED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 583MD 49659 COMPLEMENTING THE REPORT ASMF200707004 DATED ON JULY 5, 2007 WHICH INDICATES THAT (DURING THE INSPECTION OF THE HORIZONT AL STABILIZER REAR SPAR UPPER CAPS), REQUIRED BY THE AD 2007-10-04, DETECTED A CRACK OF (2) INCHES LONG AT STATION XH = 6.5 INCHES. MAINTENANCE REPLACED THE HORIZONTAL STABILIZER IAW MM 27-40-00, TESTED CORRECT. 2 L 7 2 4F RT A6WE 2007071700062 20070717 00062 NM 2007 7 17 AMTA200700314 1 20070627 A 2150 3989083 VALVE BOEING 737 73783N 13844HI NM RT A/C PACK UNSERVICEABLE A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 318TZ 28247 GAT RETURN, DUE TO RT PACK LT ON, WOULD NOT RESET IAW QRH. REMOVED AND REPLACED PACK TEMPERATURE CONTROL VALVE IAW AMM 21-51-10-4. OPS AND LEAK CHECK GOOD. (K) 2 L 7 2 4F RT A16WE 2007071700063 20070717 00063 2007 7 17 AMTA200700325 4 20070708 A 2310 9640453011 COUPLER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE HF SYSTEM INOPERATIVE A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 522AT 29330 HF TRANSMISSION INOPERATIVE AT ALL CREW STATIONS. REMOVED AND REPLACED LT HF COUPLER, OPS CHECK GOOD IAW AMM 23-11-01-4 . (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007071700064 20070717 00064 NM 2007 7 17 AMTA200700326 1 20070706 A 2612 UNKNOWN BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE FIRE DETECTION UNKNOWN A AMTA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 518AT 27974 PILOT REPORTS EICAS MSG (L ENG. LOOP 1 ). PERFORMED TROUBLESHOOTING IAW FIM 26-11-00. CLEARED MSG AC OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007071700067 20070717 00067 NM 2007 7 17 AMTA200700321 1 20070704 A 2841 INDICATOR BOEING 737 73783N 13844HI NM FUEL QTY INOPERATIVE A AMTA O OTHER P NO WARNING INDICATION CR CRUISE 1 GL 11 310TZ 28243 CENTER TANK FUEL QUANTITY INDICATION BLANK. PERFORMED FQIS BITE IAW FIM 28-41-00-810-801, INDICATION NORMAL. (K) 2 L 7 2 4F RT A16WE 2007071700069 20070717 00069 NM 2007 7 17 AMTA200700315 1 20070629 A 3040 HEATER BOEING 737 73783N 13844HI NM WINDSHIELD INOPERATIVE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 304TZ 30675 WINDOW HEAT RT SIDE (NR 2) OFF LIGHT ILLUMINATED IN FLIGHT. RESET AND LIGHT WOULD ILLUMINATE AGAIN. RERACKED WHCU M320 . PERFORMED WINDOW HEAT FAULT ISLN IAW FIM 30-41-00-810-814 AND OPS CHECK IAW MM 30-41-00-710-801 NO FAULT FOUND. BITE C/W IAW FIM 30-41-00-810-801 NO MSG ON WHCU PANEL. OK FOR SERVICE. (K) 2 L 7 2 4F RT A16WE 2007071700071 20070717 00071 2007 7 17 AMTA200700317 4 20070629 A 3442 20414440401 DRIVE UNIT BOEING 737 73783N 13844HI NM WX RADAR SYS MALFUNCTIONED A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 314TZ 30640 WEATHER RADAR SWEEPS VERY LOW ON THE RT SIDE OF DISPLAY. SHOULD BE AN EVEN RETURN ON BOTH SIDES OF DISPLAY, SEE LOG PG 800323. REMOVED AND REPLACED ANTENNA DRIVE IAW 34-43-11-4. (K) 2 L 7 2 4F RT A16WE 2007071700073 20070717 00073 2007 7 17 AMTA200700319 4 20070701 A 3160 4052506955 COMPUTER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE FLT MANAGE INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 519AT 27975 RT FMC INOPERATIVE. (CDU`S OPS NORMAL). REMOVED AND REPLACED RT FMC. OPS CKD GOOD, IAW AMM 34-60-00. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007071700074 20070717 00074 NM 2007 7 17 ASMF200707009 1 20070713 A 3220 LANDING GEAR BOEING 757 7572Q8 1384972 NM NOSE INOPERATIVE W ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 805AM 26272 AIRCRAFT RETURNED, NOSE LANDING GEAR DID NOT RETRACT. DURING CHECK, TECH DETECTED THE LOCK PIN OF THE NOSE LANDING GEAR INSTALLED, SO IT WAS REMOVED AND AIRCRAFT WAS DISPATCHED. OVERWEIGHT LANDING INSPECTION WAS NOT NECESSARY, AIRCRAFT LAND ED WITH 73900 POUNDS AND THE MAXIMUM LIMIT IS 139,500 POUNDS. 2 L 7 2 4F RT A2NM 2007071700075 20070717 00075 NM 2007 7 17 ASMF200707010 1 20070714 A 5330 SKIN DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE BS 271 CRACKED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 169PL 53175 DURING TRANSIT CHECK, THE AIRCRAFT WAS HIT BY A GATEWAY PROMOTING A CRACK OF 3 INCHES LONG IN FUSELAGE SKIN LOCATED AT S TA 271, BETWEEN LONGERONS 17 AND 18 LEFT SIDE. THE NON ROUTINE CARD A0116633 WAS ISSUED, TO REPAIR DAMAGE. REPAIR DETAIL S WILL BE SENT AS A SUPPLEMENT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007071700076 20070717 00076 NM 2007 7 17 P5CA0701526 1 20070705 A 2612 UNKNOWN BOEING 747 74746NF 13848BT NM FIRE DETECTION UNKNOWN A P5CA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 15 452PA 30810 MASTER WARNING AND FIRE BELL INTERMITTENT ON TAXI IN. AFTER ENGINE SHUTDOWN AND APU POWER ONLINE THE PROBLEM CEASED. P ERFORMED FIRE WARNING SYSTEM OPERATIONAL CHECKS WITH NO DEFECTS NOTED. 2 L 7 4 4F RT A20WE 2007071700077 20070717 00077 NE 2007 7 17 07100701 2 20070706 A 7321 77333322 FUEL CONTROL BOEING 767 767269 1385103 NM PWA JT9 JT9D7R4E 52054 NE LT ENGINE FAULTY A L43A A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 EA 27 251MY 43 23280 716808 CLIMBING BETWEEN FL 370 AND 390, LEFT ENGINE RETARDED JUST ABOVE FLIGHT IDLE AND WOULD NOT RESPOND TO ANY THROTTLE MOVEM ENT. AFTER DESCENT PASSING THROUGH FL 340 LEFT ENGINE RESPONDED THEN FROZE UP AGAIN. THE FLIGHT DIVERTED INTO CYQX. A MAINTENANCE TEAM WAS SENT TO CTQX AND TROUBLESHOT SYSTEM TO FUEL CONTROL. THE FUEL CONTROL WAS REPLACED ALONG WITH THE FUEL PUMP AND THE ENGINE TRIMMED PER THE MAINTENANCE MANUAL. PLEASE NOTE THAT AFFECTED ENGINE IS JT9D7R4E4 WHICH IS NO T AVAILABLE AS AN OPTION IN BLOCK (C) OF THIS DATABASE. 2 L 7 2 4F 4 F RT A1NM E3NE 2007071700078 20070717 00078 NM 2007 7 17 AWXA200700805 1 20070707 A 5320 BRACKET AIRBUS A319 A319132 3930340 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 660AW 1234 PHX - MAJOR REPAIR - NR 7770898, KEEL BEAM AFT INBOARD CORNER BRACKET (CONNECTION SECTION) CRACKED, FR 40/BS 1753, S42R INSIDE YELLOW HYDRAULIC BAY. REPLACED KEEL BEAM AFT INBOARD CORNER BRACKET (CONNECTION SECTION), FR 40/BS 1753, S42R I NSIDE YELLOW HYDRAULIC BAY IAW A320 SRM 51-31-00. 2 L 7 2 4F RT A28NM 2007071700079 20070717 00079 NM 2007 7 17 DL76S070824 1 20070622 A 5743 113T11105 SWIVEL FITTING BOEING 767 767332 1382001 NM MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 CORROSION WAS FOUND INSIDE THE LUG BORES AND ON THE BUSHINGS OF THE LT AND RT MLG SIDE STRUT SWIVEL FITTINGS. REPAIRED PER ERA 01-462303-14 REV ORG. 2 L 7 2 4F RT A1NM 2007071700083 20070717 00083 NM 2007 7 17 DL76L070843 1 20070702 A 3244 TIRE BOEING 767 767332 1382001 NM MLG FAILED A DALA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 SO 27 197DN 28454 DURING T/O ROLL NOTICED VIBRATION FROM LEFT SIDE. ABORTED T/O AND PULLED OF ACTIVE RNWY 22R ONTO RNWY 31L. ABORT SPEED LESS THAN 105 KTS. FOUND BOTH 5 AND 6 MAIN TIRES BLOWN. ACFT SITTING ON RIMS (5 AND 6). BRAKE TEMPS LESS THAN 2 ON AL L WHEELS. REPLACED NR 5 AND 6 MAIN WHEEL ASSY AND BRAKE ASSY PER AMM. 2 L 7 2 4F RT A1NM 2007071700087 20070717 00087 NE 2007 7 17 DLM88070847 2 20070703 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 UNKNOWN A DALA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 SO 27 905DE 34543 53410 726865 NR 2 ENGINE ROLLED BACK ON LEVEL OUT AT 4000 FT ON APPROACH. OIL PRESS WENT TO ZERO. ENGINE WAS MANUALLY SHUT DOWN. R EPLACED NR 2 ENG OIL FILTER, NO METAL FOUND CHECKED CHIP DETECTOR NO METAL FOUND NEEDS LEAK CK REMOVED FUEL CONTROL P M/ M. REPLACED FUEL PUMP AND FUEL CONTROL PER M/M NEEDS OPS CHECK. OP CHECKS GOOD PER M/M. 2 L 7 2 4F 4 F RT A6WE E9NE 2007071700088 20070717 00088 NM 2007 7 17 DL764070848 1 20070703 A 2910 UNKNOWN BOEING 767 767432ER 1385134 NM HYD SYSTEM UNKNOWN A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 843MH 29716 DURING PREFLIGHT, RIGHT HYD .89, AFTER ENGINE START W/ FLAPS EXTENDED TO 5 RIGHT QTY DROPPED TO .66 THEN .61 W/ RF SIGN AT SAME TIME CENTER. HYD INCREASED TO 1.30, DRAINED C HYD SYS REFILLED R SYS TO FULL RAN BOTH ENGS OPERATED BRAKES, FLAPS COULD NOT DUPLICATE PROBLEM. OK FOR SVC. 2 L 7 2 4F RT A1NM 2007071700090 20070717 00090 NM 2007 7 17 DL76S070850 1 20070703 A 5711 BACB30YL10K24X SPAR BOEING 767 767332 1382001 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 LT WING FRONT SPAR AT NR 8 RIB POST FOUND 1 FASTENER HOLE CRACKED AT RIB POST. LT WING FRONT SPAR NR 8 RIB AREA REWORKE D AND FASTENER INSTALLED PER ERA 461699-14AD REV ORG. 2 L 7 2 4F RT A1NM 2007071700091 20070717 00091 NM 2007 7 17 DL76S070851 1 20070703 A 5230 140T298210 CHANNEL BOEING 767 767332 1382001 NM FWD CARGO DOOR NICKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 FWD CARGO DR LWR EDGE FWD REPAIRED PATCH NICKED. FWD CARGO DOOR LOWER EDGE CHANNEL REPLACED SRM 51-10-02 PAGE 8. 2 L 7 2 4F RT A1NM 2007071700092 20070717 00092 NM 2007 7 17 DL76S070852 1 20070703 A 5320 7075T6BAR01001N ANGLE BOEING 767 767332 1382001 NM BS 1417 WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 FS 1417 LEFT FLOOR SUPPORT ANGLE HAS AN ELONGATED FASTENER HOLE. BULK CARGO COMPT, BS1417, STR 36L AREA FLOOR SUPPORT A NGLES ELONGATED HOLE REPAIRED IAW ERA 462310-14AD REV ORG. 2 L 7 2 4F RT A1NM 2007071700093 20070717 00093 NM 2007 7 17 DL76G070853 1 20070704 A 3240 BRAKE BOEING 767 7673P6 1385105 NM MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 154DL 25241 RETURNED TO GATE, PARKING BRAKE LIGHT AND EICAS MSG WHEN PARKING BRAKES ARE RELEASED. REPLACED PARKING BRAKE SWITCH S4 59. CHECKS GOOD. 2 L 7 2 4F RT A1NM 2007071700094 20070717 00094 NM 2007 7 17 DLM90070854 1 20070628 A 5310 DOOR FRAME DOUG MD90 MD9030 3023690 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 MID - PIT LWR DOOR JAMB BEAM HAS MULITPLE AREAS OF CORROSION. REPAIRED JAMB BEAM IAW MD-80 SRM 5308 FIG 63. 2 L 7 2 4F RT A6WE 2007071700095 20070717 00095 NM 2007 7 17 DLM90070855 1 20070702 A 5320 52777976 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 1231-1276 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 RT CUSP WEB STA 1231-1276 CORRODED OUT OF LIMITS BETWEEN STA 1231 AND 1250. REPAIRED RT CUSP WEB STA 1231-1250 IAW DELT A ERA 398191-14MA DATED 9-18-02. 2 L 7 2 4F RT A6WE 2007071700096 20070717 00096 NM 2007 7 17 DLM90070856 1 20070603 A 5322 995823825 SHEAR TIE DOUG MD90 MD9030 3023690 NM BS 1379 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 AFT CARGO STA 1379 AFT SIDE OF SHEAR TIE FROM L-29R TO L-28L IS CORRODED. REMOVED AND REPLACED WITH NEW SHEAR TIE AT ST A 1379 FROM L-29R TO L-26L IAW MD-90 SRM 51-10-05, 51-30-02 AND 51-30-05. 2 L 7 2 4F RT A6WE 2007071700097 20070717 00097 NM 2007 7 17 DLM90070857 1 20070702 A 5320 52777976 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 1231-1276 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 RT CUSP WEB STA 1231-1276 CORRODED OUT OF LIMITS BETWEEN STA 1231 AND 1250. REPAIRED RT CUSP WEB STA 1231-1250 IAW DELT A ERA 398191-14MA DATED 9-18-02. 2 L 7 2 4F RT A6WE 2007071700098 20070717 00098 NM 2007 7 17 DLM90070859 1 20070603 A 5320 9930612U23 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 1174 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 RT CUSP WEB STA 1174-1231 CORRODED OUT OF LIMITS BETWEEN STA 1174 TO 1193. REMOVED DAMAGED CUSP WEB, LOCATED AND DRILLE D NEW CUSP WEB AND INSTALLED IAW MD-90 SRM 51-30-2 AND 51-30-05. 2 L 7 2 4F RT A6WE 2007071700099 20070717 00099 NM 2007 7 17 DLM90070860 1 20070628 A 5313 LONGERON DOUG MD90 MD9030 3023690 NM BS 315 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 LONGERON 28 LT HAS A SMALL DENT AT STA 315. REMOVED AND REPLACED LONGERON 28 LT IAW MD-90 SRM 53-10-02 FIG 2. 2 L 7 2 4F RT A6WE 2007071700100 20070717 00100 NM 2007 7 17 DLM90070861 1 20070628 A 7830 FLANGE DOUG MD90 MD9030 3023690 NM IAE V2525 V2525D5 NE THRUST REVERSER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 33033 V20105 53386 V20105 NR 2 ENGINE AFT LOWER INBOARD SECTION OF THRUST REVERSER V SEAL FLANGE HAS 16 INCH CRACK. REPLACED ENGINE. INSTALLATIO N TO BE COMPLIED WITH ON 1002751, 4000-0103, OPN 7004AD CARD 986. 2 L 7 2 4F 4 F RT A6WE A40NE 2007071700101 20070717 00101 NM 2007 7 17 DLM90070862 1 20070626 A 5730 SKIN DOUG MD90 MD9030 3023690 NM IAE V2525 V2525D5 NE LT WING GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 V20105 LT WING FIXED L/E JUST I/B OF SLAT TRACK NR 9 SKIN IS GOUGED REPAIRED LT WING L/E IAW MD-90 SRM 57-20-01 FIG 11 VOL I. 2 L 7 2 4F 4 F RT A6WE A40NE 2007071700105 20070717 00105 NM 2007 7 17 DLM90070866 1 20070621 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 655-674 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 V20105 LT CUSP WEB AT FS 655-674 OUT OF LIMITS, CORROSION. REPAIRED CUSP WEB IAW ERA 398191-14MA DATED 5/15/07. 2 L 7 2 4F RT A6WE 2007071700107 20070717 00107 NM 2007 7 17 DLM90070869 1 20070622 A 5320 52777976 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 484-503 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 FWD PIT RT CUSP WEB CORRODED AROUND LIGHTENING HOLES STA 484-503 LOWER SURFACE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW EA 413196-14MA REV ORG ISSUED 5/13/03. 2 L 7 2 4F RT A6WE 2007071700108 20070717 00108 NM 2007 7 17 DLM90070870 1 20070628 A 5320 5940441 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 617-636 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 RIGHT CUSP WEB STA 617-636 CORRODED OUT OF LIMITS. FABRICATED REPLACEMENT CUSP WEB FROM .020 7075-T6 AND INSTALLED IAW MD90 SRM 51-10-05 VOL 2 AND 51-30-02. 2 L 7 2 4F RT A6WE 2007071700109 20070717 00109 NM 2007 7 17 DLM90070871 1 20070621 A 5347 593054790 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 579 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 SEAT TRACK CORRODED OUT OF LIMITS RBL 22 AND STA 579. FABRICATED AND REPLACED SEAT TRACK STA 522-579 AT RBL 22 IAW MD90 SRM 53-40-01 FIG 6. 2 L 7 2 4F RT A6WE 2007071700110 20070717 00110 NM 2007 7 17 DLM90070872 1 20070702 A 5347 593054792 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 850 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 SEAT TRACK RBL 22 BLENDED OUT OF LIMITS AT FS 850. REMOVED DAMAGED SECTION OF TRACK BETWEEN FS 722-850. SPLICED IN NEW SECTION IAW MD90 SRM 53-40-01 FIG 6. 2 L 7 2 4F RT A6WE 2007071700111 20070717 00111 NM 2007 7 17 DLM90070873 1 20070628 A 5347 593054792 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 655-760 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 SEAT TRACK FS 655-760 LBL 24 FOUND TO BE CORRODED OUT OF LIMITS. REPAIRED SEAT TRACK IAW MD-90 SRM 53-40-01. 2 L 7 2 4F RT A6WE 2007071700114 20070717 00114 NM 2007 7 17 QXEA200701053 1 20070626 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 436 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - CORROSION AT LOWER FLANGE OF FRAME X436.50, BETWEEN LEFT STRINGER 24 AND 25. REPAIRED IAW SRM 51-20-11, 51-40- 11, 51-20-26. 2 H 7 2 4T RT A13NM 2007071700115 20070717 00115 NM 2007 7 17 QXEA200701054 1 20070625 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 467 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - CORROSION AT FORWARD LOWER FLANGE OF FRAME X467.00, JUST OUTBOARD OF LEFT STRINGER 24. REPAIRED IAW SRM 51-20- 11, 51-40-11, 51-30-26, AND 51-20-51. 2 H 7 2 4T RT A13NM 2007071700116 20070717 00116 NM 2007 7 17 QXEA200701057 1 20070625 A 5320 INTERCOSTAL DHAV DHC8 DHC8202 2809007 NM BS 424 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - CORROSION AT INTERCOSTAL WHICH ATTACHED TO LEFT STRINGER 23, AFT OF FRAME X424.124. REPAIRED IAW SRM 51-20-11, 51-40-11, 51-20-26. 2 H 7 2 4T RT A13NM 2007071700121 20070717 00121 NM 2007 7 17 QXEA200701064 1 20070624 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 201 S31R CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - CORROSION UNDER FLOOR AT STATION 201 AT STRINGER 31R FITTING CASTING ON VERTICAL FRAME. REPAIRED IAW SRM 51-40 -11. 2 H 7 2 4T RT A13NM 2007071700122 20070717 00122 NM 2007 7 17 QXEA200701067 1 20070627 A 5340 STRINGER CLIP DHAV DHC8 DHC8202 2809007 NM BS 424 S24L CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - REF NON ROUTINE 00234 CORROSION NOTED AT LEFT STRINGER 24 ATTACH CLIP AREA, FORWARD OF FRAME 424.124. REPAIRED IAW SRM 51-20-11, 51-20-26, 51-20-51. 2 H 7 2 4T RT A13NM 2007071700126 20070717 00126 NM 2007 7 17 QXEA200701088 1 20070628 A 5230 STRUCTURE DHAV DHC8 DHC8202 2809007 NM CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - CARGO DOOR UPPER AFT FIBERGLASS CORNER PIECE HAS REINFORCEMENT STRAP INSTALLED EXTERNALLY. REPAIRED IAW SRM 51 -40-11. 2 H 7 2 4T RT A13NM 2007071700127 20070717 00127 NM 2007 7 17 AWXA200700808 1 20070703 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5982109, CRACKED STRINGER CLIP, BS 639, S4R. REPLACED STRINGER CLIP, BS 639, S4R I AW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071700128 20070717 00128 NM 2007 7 17 AWXA200700809 1 20070629 A 5340 453N182018 ATTACH ANGLE BOEING 757 757225 1384959 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 MCN - MAJOR REPAIR - C-12 CHECK - NR 5950465, FORWARD CARGO COMPARTMENT DOOR CUT OUT FRAME CHORD ATTACH ANGLE CRACKED, B S 560, S20R. REPLACED FORWARD CARGO COMPARTMENT DOOR CUT OUT FRAME CHORD ATTACH ANGLE, BS 560. S20R IAW B757-200 SRM 51 -40-02. 2 L 7 2 4F RT A2NM 2007071700129 20070717 00129 NM 2007 7 17 AWXA200700810 1 20070705 A 5340 69451561 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5961271, CRACKED STRINGER CLIP, BS 578, S11L. REPLACED STRINGER CLIP, BS 578, S11L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071700131 20070717 00131 NM 2007 7 17 AWXA200700801 1 20070707 A 3233 65448105 ACTUATOR BOEING 737 7373S3 1384711 NM RT MLG FAILED A AWXA O OTHER J WARNING INDICATION AP APPROACH 1 WP 28 313AW 27146 234 23712 MKE - PHX - EL - LOG# 7746754 - CREW SELECTED GEAR DOWN, RIGHT MAIN RED LANDING GEAR LIGHT REMAINED ILLUMINATED, GREEN L IGHT ON NOSE AND LEFT MAIN. TOWER CONFIRMED RIGHT GEAR WAS UP. THE CREW DECLARED AN EMERGENCY AND PERFORMED GEAR LIGHT DISAGREEMENT CHECKLIST. CREW PERFORMED MANUAL GEAR EXTENSION, 3 GREEN LIGHTS. THE CABIN WAS PREPARED FOR AN EMERGENCY LANDING. THE LANDING WAS UNEVENTFUL. THE A/C TAXIED TO THE GATE. MX PERFORMED GEAR SWING OF RIGHT MLG. MX FOUND GEA R WOULD NOT DROP WHEN SELECTING GEAR HANDLE FROM OFF TO DOWN. OPS NORMAL WHEN GEAR HANDLE MOVED FROM UP DIRECTLY TO DOW N. MX REMOVED AND REPLACED RT MLG UP LOCK ACTUATOR, RT TRANSFER CYLINDER AND RT MLG MODULAR PACKAGE IAW REF R4M32010, M 2 L 7 2 4F RT A16WE 2007071700133 20070717 00133 NM 2007 7 17 AWXA200700812 1 20070703 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - CRACKED STRINGER CLIP, BS 706, S2R. REPLACED STRINGER CLIP, BS 706, S2R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071700134 20070717 00134 NM 2007 7 17 AWXA200700813 1 20070705 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - CRACKED STRINGER CLIP, BS 578, S9L. REPLACED STRINGER CLIP, BS 578, S9L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071700138 20070717 00138 NM 2007 7 17 AWXA200700818 1 20070705 A 5340 69414372 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - CRACKED STRINGER CLIP, BS 663, S10L. REPLACED STRINGER CLIP, BS 663, S10L IAW B737-30 0 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071700139 20070717 00139 NM 2007 7 17 AWXA200700819 1 20070703 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - CRACKED STRINGER CLIP, BS 639, S4L. REPLACED STRINGER CLIP, BS 639, S4L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071700141 20070717 00141 NM 2007 7 17 AWXA200700821 1 20070703 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5982105, CRACKED STRINGER CLIP, BS 685, S2L. REPLACED STRINGER CLIP, BS 685, S2L I AW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071700143 20070717 00143 NM 2007 7 17 AWXA200700823 1 20070707 A 5320 D53480043204 SILL AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5971971, CORROSION ON THE L2 DOOR CUT OUT LOWER SILL, FR 67 + 18.5"/BS 2835, +Y1265 . REPAIRED THE L2 DOOR CUT OUT LOWER SILL, FR 67 + 18.5"/BS 2835, +Y1265 IAW A319 SRM 53-41-14. 2 L 7 2 4F RT A28NM 2007071700147 20070717 00147 NM 2007 7 17 AWXA200700825 1 20070707 A 5315 D53472172205 FLOORBEAM AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 SAL - MAJOR REPAIR - BC-6 CHECK - CORROSION ON CABIN FLOORBEAM, FR 66/BS 2786 - FR 68 / 2884, -Y1165. REPLACED CABIN F LOORBEAM, FR 66/BS 2786 - FR 68/2884, -Y1165 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007071700152 20070717 00152 NM 2007 7 17 AWXA200700830 1 20070703 A 5322 69482042 SHEAR TIE BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - C-20 CHECK - NR 5982117, CRACKED SHEAR TIE, BS 360, S14L - S15L. REPLACED SHEAR TIE, BS 360, S14L - S15L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007071700155 20070717 00155 NM 2007 7 17 AWXA200700802 1 20070706 A 2611 RAI2800M0706 SMOKE DETECTOR AIRBUS A319 A319132 3930340 NM E/E BAY FAILED A AWXA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 28 827AW 33409 33409 1547 PHX - EES - LOG NR 7848154 - CREW REPORTED SMOKE LAV AND CRG DET FAULT. MX REMOVED AND REPLACED SDCU IAW AMM 26-17-34, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007071700156 20070717 00156 EU 2007 7 17 AWXA200700807 1 20070710 A 2560 P2070001214 FLASHLIGHT AIRBUS 320 A320231 3930325 EU AFT CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 631AW 077 PHX - EEL - LOG NR 7826626 - CREW REPORTED EMERGENCY FLASHLIGHT IN AFT CABIN INOP. MX REPLACED THE AFT EMERGENCY FLASHL IGHT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007071700157 20070717 00157 NM 2007 7 17 AWXA200700833 1 20070711 A 5320 D53480043204 SILL AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5964045, CORROSION ON L2 DOOR CUT OUT LOWER SILL, +Y1265, FR 67 + 18.5"/ BS 2835. REPAIRED L2 DOOR CUT OUT LOWER SILL, +Y1265, FR. 67 + 18.5"/ BS 2835 IAW A319 SRM 53-41-14. 2 L 7 2 4F RT A28NM 2007071700159 20070717 00159 EU 2007 7 17 AWXA200700835 1 20070711 A 5320 D53480019216 PLATE AIRBUS 320 A320232 3930326 EU ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 654AW 1050 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5962701, CRACKED CABIN PLATE/TRAY, BS 3257/FR 68, +Y1732. REPLACED CABIN PLATE/TRA Y, BS 3257/FR 68 TO BS 3510/FR 69, +Y1732 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007071700160 20070717 00160 NM 2007 7 17 AWXA200700836 1 20070710 A 5321 D5367180500500 FLOOR PANEL AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5963181, CORROSION ON CABIN FLOOR PANEL 262FF, BS 2786 - BS 2884/FR 66 - FR68, -Y12 92 TO -Y1732. REPLACED CABIN FLOOR PANEL 262FF, BS 2786 - BS 2884 / FR 66 - FR68, -Y1292 TO -Y1732 IAW A319 SRM 51-72-1 1. 2 L 7 2 4F RT A28NM 2007071700161 20070717 00161 WP 2007 7 17 MWEA070152 1 20070628 A 7830 STRUCTURE DOUG DC9 DC981 3022081 WP THRUST REVERSER DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 LIGHTNING STRIKE AT THRUST REVERSER AT MID POINT. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2007071700162 20070717 00162 NM 2007 7 17 MWEA070153 1 20070701 A 7830 7150920507 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 914ME 55177 STATION 35.669 CRACKED IN ZEE FRAME INBOARD END. FABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007071700164 20070717 00164 SO 2007 7 17 RAIA00706041 1 20070630 A 3230 3555022002MOD CONTROL UNIT EMB 145 EMB145LR 3260212 SO MLG MALFUNCTIONED A RAIA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 CE 03 829HK 19101 910 145281 FLT 7996 - STL - CREW REPORTED RED LANDING GEAR DISAGREE MESSAGE WITH ALL BEAR DOWN & LOCKED INDICATIONS. MAINTENANCE R EMOVED AND REPLACED THE LGECU. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007071700165 20070717 00165 SO 2007 7 17 RAIA00707001 1 20070701 A 3350 78241 INVERTER EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 802HK 145066 PRE FLT 3564 - RIC - EMERGENCY LIGHT AT SERVICE DOOR EXIT MARKER INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 INVERTER. 2 L 7 2 4F RT T00011AT 2007071700167 20070717 00167 SO 2007 7 17 RAIA00707003 1 20070702 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 813HK 145044 PRE FLT 5534 - STL - EMERGENCY EXIT LIGHT AT LEFT OVERWING EXIT INOP. MAINTENANCE RESECURED WIRING TO THE EMERGECNY LIG HT. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007071700168 20070717 00168 NM 2007 7 17 ZZDA070624183 1 20070624 A 5230 SKIN BOEING 717 717200 1383700 NM FWD CARGO DOOR DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 943AT 55006 BAG CART HIT FORWARD CARGO DOOR OPENING. CUT OUT DAMAGE AREA IN SKIN, DOUBLER AND TITANIUM DOUBLER IAW B717 SRM 53-20-1 5 FIG 201. INSTALLED DOUBLER IAW B717 SRM 53-20-150 FIG 201. REPAIRED SEAL DEPRESSOR IAW B717 SRM 53-20-15. 2 L 7 2 4F TR A6WE 2007071700169 20070717 00169 NM 2007 7 17 ZZDA070628184 1 20070628 A 5310 DOOR FRAME BOEING 737 7377BD 1384511 NM FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 316AT 33928 FORWARD LWR CORNER AT AFT CARGO DOOR FRAME CRACKED. HFEC INSPECTED AREA - CUT OUT DAMAGE, FABRICATED REPAIR IAW 737 SRM 53-00-01. INSTALLED SAME PER SRM 51-20-01. 2 L 7 2 4F RT A16WE 2007071700170 20070717 00170 SO 2007 7 17 C2XA07TY033 1 20070627 A 3260 DOWNLOCK SWITCH EMB 145 EMB145XR 3260214 SO MLG MISALIGNED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 11140 145732 TYS - AIRCRAFT WAS DIVERTED FROM CLT TO TYS WHEN ON CLIMBOUT, A WARNING INDICATION OF THE NOSE LANDING GEAR DOOR WOULDN' T RETRACT. MAINTENANCE ADJUSTED THE DOOR SWITCHES AND CYCLED GEAR. OPS CHECKS WERE GOOD AND RELEASED BACK TO SERVICE. 2 L 7 2 4F RT 2007071700173 20070717 00173 WP 2007 7 17 ASAA0781828 1 20070702 A 5320 993053811 CUSP WEB DOUG DC9 DC983 3022083 WP BS 505-508 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 FORWARD CARGO BAY LEFTHAND CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER PER SRM 53-01 AND 51-1 0-3. 2 L 7 2 4F RT A6WE 2007071700174 20070717 00174 WP 2007 7 17 ASAA0781829 1 20070702 A 5320 993653473 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 FLOOR TRACK HAS DOUBLE DRILLED HOLES. REPLACED FLOOR TRACK PER SRM 51-10-4 AND 51-30-1. 2 L 7 2 4F RT A6WE 2007071700175 20070717 00175 WP 2007 7 17 ASAA0781830 1 20070702 A 5320 9936534139 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 FLOOR TRACK HAS DOUBLE DRILLED HOLES. REPLACED FLOOR TRACK PER SRM 51-10-4 AND 51-30-1. 2 L 7 2 4F RT A6WE 2007071700176 20070717 00176 WP 2007 7 17 ASAA0781831 1 20070702 A 5313 593666713 LONGERON DOUG DC9 DC983 3022083 WP BS 1237-1295 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 LONGERON 30 CORRODED INSIDE OF CHANNEL. REPLACED DAMAGED SECTION PER SRM 51-10-4, 51-10-3, 51-30-2 AND 51-30-5. 2 L 7 2 4F RT A6WE 2007071700179 20070717 00179 WP 2007 7 17 ASAA0781835 1 20070702 A 5320 99367183 INTERCOSTAL DOUG DC9 DC983 3022083 WP BS 1307-1322 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 AFT CARGO BAY INTERCOSTAL CORRODED. REPLACED INTERCOSTAL PER SRM 57-30-2 AND 51-30-5. 2 L 7 2 4F RT A6WE 2007071700182 20070717 00182 WP 2007 7 17 ASAA0781838 1 20070702 A 5543 595545503 TAB DOUG DC9 DC983 3022083 WP RUDDER DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 RUDDER TAB DELAMINATED AT TRAILING EDGE. REPAIRED WITH GLASS CLOTH AND ASTROSTICKE PER SRM 51-70-1A. 2 L 7 2 4F RT A6WE 2007071700183 20070717 00183 WP 2007 7 17 ASAA0781839 1 20070702 A 5347 593054765 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 200-247 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 CABIN SEAT TRACK CORRODED. REPLACED DAMAGED SECTION OF TRACK PER SRM 51-10-4, 53-05 AND 51-30-5. 2 L 7 2 4F RT A6WE 2007071700184 20070717 00184 WP 2007 7 17 ASAA0781842 1 20070702 A 5321 993658211 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 946-1003 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 CABIN FLOOR PANEL HAS DAMAGED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05. 2 L 7 2 4F RT A6WE 2007071700185 20070717 00185 WP 2007 7 17 ASAA0781843 1 20070702 A 5321 99365393 FLOOR PANEL DOUG DC9 DC983 3022083 WP PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 975AS 53451 COCKPIT FLOOR PANEL PUNCTURED. REPLACED FLOOR PANEL PER SRM 53-05. 2 L 7 2 4F RT A6WE 2007071700186 20070717 00186 NM 2007 7 17 ASAA0771844 1 20070701 A 3320 SOCKET BOEING 737 737790 13844CN NM NIGHT LIGHT MELTED A ASAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 02 613AS 30163 BURNING SMELL AT ROW 21 RT SIDE OF AIRCRAFT WITH NIGHT LIGHT TURNED ON. SMELL NO LONGER PRESENT WITH NIGHT LIGHT TURNED OFF. FOUND NIGHT LIGHT SOCKET MELTED AT ROW 21R. REPLACED SOCKET ASSY. SYSTEM OPS OK. 2 L 7 2 4F RT A16WE 2007071700187 20070717 00187 2007 7 17 C2XA07ON010 4 20070701 A 2340 PA SYSTEM EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA O OTHER L NO TEST NR NOT REPORTED 1 SW 27 11193 1450938 CABIN CALL/ CABIN EMERGENCY AND PA SYSTEM NOT WORKING. VERIFIED NORMAL OPERATION CABIN EMERGENCY PA SYSTEM. NO SYTEMS FAULT FOUND. 2 L 7 2 4F RT 2007071700188 20070717 00188 SO 2007 7 17 C2XA07SH037 1 20070702 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11536 145520 SHV - DURING C-CHECK MAINTENANCE FOUND CENTER OMEGA BEAM WITH CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED C ENTER OMEGA BEAM FROM FRAMES 18 TO 24 IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007071700190 20070717 00190 NM 2007 7 17 NOCA13407 1 20070621 A 2597 WIRE BOEING 767 767324 1385203 NM COFFEEMAKER DAMAGED A NOCA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 767NA 27569 CABIN CREW AND FLIGHT CREW NOTED AN ELECTRICAL SPARK AND OBSERVED SMOKE FROM THE FORWARD GALLEY, ABOVE THE COFFEEMAKERS. INSPECTED AS PER AMM 20-60-03 AND BY SHAKING THE WIRE BUNDLE ON CONNECTOR D10932 W0222 AND TOUCHING THE GALLEY TRIM A SPARK WAS NOTED AND DISCOVERED ONE OF THE FOUR WIRES WAS CHAFING. TAPED THE CHAFING WIRE WITH ELECTRICAL TAPE AS PER TH E SWPM. AFTER CONSULTING THE WDM 25-31-11 AND 25-31-01 WHICH SHOWS THE GALLEY POWER FOR G4 CIRCUIT BREAKER. CB C007 WA S PULLED AND COLLARD, MX CONFIRMED NO SPARK BY SHAKING THE WIRE BUNDLE AGAIN AFTER C/B WAS PULLED. THE FORWARD GALLEY G 4 POWER HAS BEEN DEACTIVATED WHICH WILL ALSO EFFECT THE 3 COFFEEMAKERS AND WARMERS AND THE WORK AREA LIGHT. THIS ITEM H 2 L 7 2 4F RT A1NM 2007071700191 20070717 00191 NM 2007 7 17 NOCA13507 1 20070619 A 2612 FIRE LOOP BOEING 767 767304 NM RT NACELLE MALFUNCTIONED A NOCA O OTHER N FALSE WARNING CR CRUISE 1 EA 15 769NA 28039 THE -R ENG FIRE LOOP 1- STATUS MESSAGE ILLUMINATED IN FLIGHT. IN RMS OPENED CI 26-03. PERFORMED FIM TASK 26-11-00, NO FAULTS NOTED ACP ENGINE RUN UP CHECKS OK. NO EICAS MSG, CLEARED CI WITH MCC HOUSTON. 2 L 7 2 4F RT A1NM 2007071700192 20070717 00192 WP 2007 7 17 UPS07850124 1 20070617 A 5522 SKIN DOUG DC8 DC871F 302199D WP LT ELEVATOR CANNING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 L/ELEVATOR UPPER MIDDLE SKIN HAS OIL CANNING ON O/B SIDE. CUT OUT DAMAGED SKIN SECTION FROM L/ELEVAT OR, UPPER MIDDLE STA 219 - 234 IAW SRM 55-02-01 FIG 008. FABRICATED AND INSTALLED SKIN SEGMENT ON L/ELEVATOR STA 219 - 234.5 IAW DWG 5654970, AND SRM 55-02-01 FIG 008. 2 L 7 4 4F RT 4A25 2007071700193 20070717 00193 2007 7 17 UPS07M50102 4 20070703 A 2565 PRESSURE SWITCH DOUG MD11 MD11F 3023600 NM ESCAPE SLIDE INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 251UP 48744 INSPECTION TYPE:N/A R1 EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATING SYSTEM INOP. RELAMPED, NO HELP. BATTE RIES CHECKED OK. SUSPECTED THE PRESS-TO-TEST LIGHT ASSY. REPLACED RIGHT EMERGENCY ESCAPE SLIDE PRESSURE SWITCH INDICAT OR. OPS CHECKS GOOD. CLOSED DEFERRAL ON M353756. 2 L 7 3 4F RT A22WE 2007071700195 20070717 00195 EU 2007 7 17 TRAX200700915 1 20070702 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 SEVERAL CABIN EMERGENCY LIGHTS INOP. 2 H 7 2 4T RT 2007071700200 20070717 00200 EA 2007 7 17 TRAX200700925 1 20070703 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT NO TEST A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 852AS 7369 LEFT EMERGENCY EXIT FAILED BETA LIGHT TEST. 2 L 7 2 4F RT A21EA 2007071700202 20070717 00202 EA 2007 7 17 TRAX200700930 1 20070704 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 931EV 8015 PAX DOOR LOWER STEP CRACKED. 2 L 7 2 4F RT A21EA 2007071300044 20070713 00044 NM 2007 7 13 HNAA0700128 1 20070628 A 5720 DOUBLER DHAV DHC8 DHC8102 2809003 NM LT WING CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 912HA 040 LEFT AUX BOOST PUMP (FUEL) WING DOUBLER FOUND CORRODED INSIDE AND OUTSIDE FUEL TANK. LEFT AUX BOOST PUMP (FUEL) WING DO UBLER INSIDE AND OUTSIDE OF FUEL TANK CORROSION REMOVED IAW RD8-57-3679 (MATERIAL REMAINING .415") S/B 8-57-28 PREVIOUSL Y COMPLIED WITH. HFEC AND DISBOND C/O, NO DEFECTS FOUND. 2 H 7 2 4T RT A13NM 2007071300045 20070713 00045 NM 2007 7 13 AALA20071177 1 20070626 A 3350 LIGHT BOEING 757 757231 1384950 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 717TW 28485 DFW - EMERGENCY LIGHT AT SEAT 24D INOP WITH TRACK LIGHT END PLUG MISSING. REPLACED PATH FLOOR EMERGENCY LIGHTING AT SEA T 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071300064 20070713 00064 NM 2007 7 13 AALA20071192 1 20070627 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT SEAT 20C HAS DAMAGED LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007071300066 20070713 00066 NM 2007 7 13 AALA20071195 1 20070628 A 3397 WIRE HARNESS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 363AA 24044 ORD - EMERGENCY LIGHT AT SEAT ROW 12HJ INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHT AT SEAT ROW 12HJ. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007071300072 20070713 00072 SO 2007 7 13 SWIA200718429 1 20070323 A 5210 BOSS EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 569SW 120344 PAX DOOR HAS CRACKED LOCKING MECHANISM BOSS BETWEEN FRAMES 4 AND 5, DISCOVERED AT C-CHECK. REPLACED LOCKING MECHANISM B OSS IAW 52-11-03. 2 L 7 2 4T RT A31SO 2007071300074 20070713 00074 NE 2007 7 13 QXEA200701022 2 20070623 A 7320 4120T35P02 MANIFOLD CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE RT ENG FUEL LEAKING A QXEA O OTHER K FLUID LOSS NR NOT REPORTED 1 NM 09 290RB 10029 PDX - FLIGHT 2509 - BOTTOM SIDE OF RIGHT SIDE ENGINE HAS A FUEL LEAK. MAINTENANCE REPLACED THE FUEL CONTROL MANIFOLD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007071300108 20070713 00108 EA 2007 7 13 QXEA200701076 1 20070629 A 3241 6007302 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA ANTI SKID SYS MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 614QX 27998 10049 PDX - LEFT BRAKES SEEM MUSHY AND SEEM TO GET HOT QUICKLY. MAINTENANCE REPLACED THE ANTI-SKID CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007071300118 20070713 00118 WP 2007 7 13 UPS07850096 1 20070622 A 5754 DOUBLER DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 R/WING CENTER L/E INNER DOUBLER CRACKED AT DRAIN HOLE AT STA XFS 334. REMOVED CRACKED INNER DOUBLER AT R/WING STA XFS 334 IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT DOUBLER AT R/WING L/E STA XFS 334 IAW SRM 5 7-03-01-0 FIG 004. 2 L 7 4 4F RT 4A25 2007071300128 20070713 00128 NM 2007 7 13 USAA070519 1 20070703 A 5311 652072328 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 444US 24862 BS 492.4, S-24R HAS CRACK. REMOVED DAMAGE, FABRICATED & INSTALLED FILLER & REPAIR ANGLES PER EA 98762, DEFECT SIZE: .8 INCH. 2 L 7 2 4F RT A16WE 2007071300131 20070713 00131 EA 2007 7 13 HNAA0700131 1 20070628 A 3244 314802 TIRE DHAV DHC8 DHC8311 1386006 EA LANDING GEAR FLAT A HNAA O OTHER O OTHER LD LANDING 1 EA 07 336EN 336 CREW STOPPED THE AIRCRAFT ON THE TAXIWAY AND REPORTED TO TOWER THAT AIRCRAFT HAD A FLAT TIRE. THE AIRPORT AUTHORITY SEN T OVER A VEHICLE AND VERIFIED THAT PLANE HAS TWO FLAT TIRES. PASSENGERS WERE DEPLANED WITH GROUND TRANSPORT. REMOVED A ND REPLACED NR 1 TIRE AND NR 2 MWA, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007071300133 20070713 00133 SO 2007 7 13 SIMA200719004 1 20070708 A 2750 FLAP SYSTEM EMB 135 EMB135LR 3260305 SO TE FLAPS STUCK A SIMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 721HS 145283 FLAPS SELECTED TO THE UP POSITION FOLLOWED BY FLAP FAIL AND SPS ADVANCE MESSAGE, FLAPS STUCK AT 9 DEGREES. 2 L 7 2 4F RT T00011AT 2007071300148 20070713 00148 EA 2007 7 13 SWIA200718430 1 20070705 A 3350 BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INOPERATIVE A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 728SK 10192 FLT 6444 - EMERGENCY LIGHTS NOT WORKING. REPLACED NR 1, NR 2, AND NR 3 BATTERY PACKS IAW CRJ 700 AMM 33-51-07. OPS CHE CK GOOD AT THIS TIME, P/N AD-2013-1A NR 1 S/N OFF 33006, NR 2 S/N OFF 66789, NR 3 S/N OFF 69316. 2 L 7 2 4F RT A21EA 2007071300149 20070713 00149 EA 2007 7 13 SWIA200718431 1 20070702 A 2421 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA AUTO DEPLOY MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 907SW 7511 FLT 6020 - ON ROTATION AND WEIGHT OFF WHEELS, THE ADG DEPLOYED. REPLACED ADG AUTO DEPLOY CONTROLLER IAW MM 24-23-15, P/ N 82046-5 S/N OFF 1149. 2 L 7 2 4F RT A21EA 2007071300152 20070713 00152 SO 2007 7 13 SWIA200718433 1 20070706 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS INOPERATIVE A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 284YV 120284 EMERGENCY LIGHTS AFT OF ROW 6 ARE INOPERATIVE. REPLACED AFT ELBP PER MM 33-50-02, OPS CHECK GOOD, P/N - D366-04-001, S /N OFF - 1252. 2 L 7 2 4T RT A31SO 2007071300166 20070713 00166 SO 2007 7 13 SWIA200718444 1 20070505 A 5411 RIB EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 216SW 120285 RIGHT NACELLE FLAP INNER RIB IS CRACKED, DISCOVERED AT C-CHECK. REPAIRED NACELLE FLAP INNER RIB IAW SRM 51-70-05. 2 L 7 2 4T RT A31SO 2007071300174 20070713 00174 SO 2007 7 13 SWIA200718448 1 20070323 A 5320 SUPPORT BRACKET EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 569SW 120344 LEFT DV WINDOW HORIZONTAL SUPPORT BRACKET IS CRACKED, DISCOVERED AT C-CHECK. REPLACED SUPPORT BRACKET BEHIND LEFT DV WI NDOW IAW EMB 120 SRM 51-10-02/51-40-02. 2 L 7 2 4T RT A31SO 2007071300175 20070713 00175 NM 2007 7 13 BB07048 1 20070703 A 2781 TARGET BOEING 767 7672B7 1385107 NM L/E SLAT LOOSE A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 255AY 25257 FLIGHT 710, PHL-ZRH: DURING CRUISE, RECEIVED -LE SLAT ASYM- MESSAGE. FLIGHT RETURNED TO PHL AND LANDED WITH NO DIFFICU LTIES. MAINTENANCE FOUND THE NUMBER 8 SLAT RETRACT TARGET LOOSE AND OUT OF ADJUSTMENT. RE-ADJUSTED TARGET PER AMM. NO FURTHER FAULTS. 2 L 7 2 4F RT A1NM 2007071300188 20070713 00188 WP 2007 7 13 NWAA072449953 1 20070710 A 2130 UNKNOWN DOUG DC9 DC931 3022065 WP CABIN PRESSURE UNKNOWN A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 918RW 47158 CABIN CREW REPORTED A PRESSURE LEAK TYPE SQUEAL COMING FROM THE AFT EMERGENCY ESCAPE HATCH. WHEN FLIGHT CREW REDUCED TH RUST THE CABIN ALTITUDE CLIMBED UNCONTROLLABLY. THE PILOT PERFORMED A RAPID DESCENT TO A LOWER ALTITUDE AND CONTINUED T O SCHEDULED DESTINATION. THE PASSENGER OXYGEN MASKS DID NOT DEPLOY. THE LANDING AT VPS WAS WITHOUT FURTHER INCIDENT. MAINTENANCE RESEATED THE AFT TAIL COMPARTMENT PLUG DOOR AND PRESSURE CHECKED THE AIRCRAFT. THEY ALSO DID PERFORM BITE O N THE PRESSURE CONTROLLERS. ALL CHECKS WERE GOOD AND THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007071300191 20070713 00191 NM 2007 7 13 SWAA073309 1 20070703 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 414WN 29820 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 129.50. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007071300193 20070713 00193 NM 2007 7 13 SWAA073324 1 20070704 A 5523 6545166 ROD END BOEING 737 7375H4 138449D NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR TAB CONTROL ROD TO ELEVATOR TAB MAST FITTING EXCESSIVE PLAY. REMOVED AND R EPLACED TAB CONTROL ROD ENDS PER MM. 2 L 7 2 4F RT A16WE 2007071300202 20070713 00202 NM 2007 7 13 HALA0700271 1 20070627 A 2700 UNKNOWN BOEING 767 76733A 1385209 NM UNKNOWN A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 587HA 33421 ETOPS SIGNIFICANT SYSTEM, AIRCRAFT REQUIRES 4 UNITS OF LEFT RUDDER TRIM TO KEEP THE AILERON TRIM INDICATOR AT ZERO ONLY DURING CLIMB AND DESCENT. AT CRUISE, ALL TRIM SETTINGS ARE NORMAL. T/S PER FIM 27-21-00. OPERATED RUDDER TRIM FULL LT AND RT. RUDDER TRIM SYSTEM OPERATION NORMAL INFORMATION NOTED AND RECORDED. 2 L 7 2 4F RT A1NM 2007071300206 20070713 00206 NM 2007 7 13 SWAA073299 1 20070703 A 5313 6551698 STRINGER SPLICE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER S RM. 2 L 7 2 4F RT A16WE 2007071300210 20070713 00210 EU 2007 7 13 07FDEA02368 1 20070703 A 2131 82010B040901 CONTROLLER AIRBUS 310 A310203 3930313 EU CABIN PRESSURE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 409FE 273 ATB AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. ECAM MAN PRESS VALVE INDICATED OPEN. EMERGENCY VALVE INDICATION IN CO CKPIT NEAR HANDLE INDICATED CLOSED AND VALVE LOOKED CLOSED ON PREFLIGHT. PERFORMED CABIN PRESSURE CONTROL AND MONITORIN G TEST PER AMM 21-31-00-5. ALL TESTS CHECKED OK PER AMM. WHEN A/C CAME BACK TO GATE SYS NR 2 CONTROLLER WAS IN COMMAND . REPLACED NR 2 CABIN PRESSURE CONTROLLER AS PER AMM A310-200 21-31-11-4. OPS CK PER 21-31-00-5. 2 L 7 2 4F RT A35EU 2007071300214 20070713 00214 NM 2007 7 13 07FDEA02374 1 20070705 A 5720 6521657155 SEAL DEPRESSOR BOEING 727 727227 1384078 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 LT WING TE PNL 8155 SEAL DEPRESSOR IS FRETTED, CRACKED ALONG INBD EDGE. REPLACED SEAL DEPRESSOR IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2007071300220 20070713 00220 NM 2007 7 13 SWAA073323 1 20070704 A 5523 65C25798 HINGE BOEING 737 7375H4 138449D NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REPAIRED NR 1 HINGE PER SWA EA. 2 L 7 2 4F RT A16WE 2007071300231 20070713 00231 NM 2007 7 13 SWAA073308 1 20070703 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071300240 20070713 00240 NM 2007 7 13 SWAA073318 1 20070704 A 3350 BR9442 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED C2 CHECK, FOUND RT FWD CABIN EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER M M. 2 L 7 2 4F RT A16WE 2007071300244 20070713 00244 2007 7 13 SWAA073288 4 20070703 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071300251 20070713 00251 NM 2007 7 13 AWXA200700799 1 20070708 A 5330 6518420 SKIN BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 PHX - MAJOR REPAIR - CRACK AT FIRST OFFICERS NR 1 WINDOW POST SKIN UPPER OUTBOARD CORNER, BS 196.5 - BS 203.8, S9R - S1 0R. REPAIRED FIRST OFFICERS NR 1 WINDOW POST SKIN UPPER OUTBOARD CORNER, BS 196.5 - BS 203.8, S9R - S10R IAW B737-300 S RM 53-10-01-2R. 2 L 7 2 4F RT A16WE 2007071300257 20070713 00257 EA 2007 7 13 TRAX200700914 1 20070702 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 973EV 7575 F/O SIDE FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007071300259 20070713 00259 SO 2007 7 13 SIMA200719104 1 20070522 A 5347 14532606015 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 15926 5000 145224 LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 36 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETUR NED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300260 20070713 00260 SO 2007 7 13 SIMA200719106 1 20070522 A 5347 14532606017 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 15926 5000 145224 LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AME RICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R2. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300263 20070713 00263 SO 2007 7 13 SIMA200719102 1 20070522 A 5347 13500412003 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 15926 5000 145224 LEFT INBOARD SEAT TRACK BETWEEN FRAME 53 AND 55 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMER ICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R2. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300265 20070713 00265 SO 2007 7 13 SIMA200719110 1 20070522 A 5347 14530658 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 15926 5000 145224 RIGHT INBOARD SEAT TRACK BETWEEN FRAME 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETUR NED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300266 20070713 00266 SO 2007 7 13 SIMA200719111 1 20070522 A 5347 13500439005 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 15926 5000 145224 LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 17 AND 23 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETUR NED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300269 20070713 00269 NM 2007 7 13 2007UALA02362 1 20070701 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 220UA 30223 THE 2E AFT & 35C EEL LIGHTS ARE INOPERATIVE. [07-27-07] RELAMPED. SYS OPS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007071300270 20070713 00270 NM 2007 7 13 2007UALA02363 1 20070701 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 220UA 30223 EXTERIOR EMERGENCY LIGHT AT DOOR 1R IS OUT. [07-27-07] RELAMPED. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007071300279 20070713 00279 NM 2007 7 13 2007UALA02372 1 20070702 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EMERGENCY EXIT LIGHT INOP AT DOOR 2 RIGHT ENTRY CEILING. FOUND BATTERY PACK LOOSE, SECURED. CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071300293 20070713 00293 SO 2007 7 13 SIMA200719206 1 20070617 A 5347 14532605017 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 812AE 13442 5000 145531 RIGHT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 36 AND 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIR CRAFT RETURNED TO SERVICE 2 L 7 2 4F RT T00011AT 2007071300301 20070713 00301 NM 2007 7 13 2007UALA02381 1 20070701 A 2612 LENS BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FIRE WARNING INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 657UA 27112 RED FIRE WARNING LIGHT DOES NOT ILLUMINATE WHEN TESTED. [07-27-07] REPLACED FIRE ANNUNICATOR LENS ASSY. OP CHECKS NORMALLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071300305 20070713 00305 EU 2007 7 13 2007UALA02385 1 20070703 A 3350 32145410 EPSU AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 432UA 587 SEVERAL EMERGENCY LIGHTS STAY ON WITH POWER OFF NEAR CENTER OF ACFT. REPLACED EPSU. CHECKS OKAY AT THIS TIME. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071300312 20070713 00312 NM 2007 7 13 2007UALA02393 1 20070704 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 307UA 23668 EMERGENCY EXIT LIGHT LOWER RIGHT SLIDE LIGHT INOP. [07-27-07] REPLACED LIGHT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071300317 20070713 00317 SO 2007 7 13 SIMA200719006 1 20070709 A 2750 3632701001 TRANSDUCER EMB 145 EMB145LR 3260212 SO ZONE 100 FAILED A SIMA K NONE F FLT CONT AFFECTED AP APPROACH 1 SW 21 615AE 19271 145087 FLAPS FAILED AT NINE DEGREE ON APPROACH. REMOVED AND REPLACED FLAP POSITION TRANSDUCER AND RIGHT VELOCITY SENSOR IAW EM B AMM 27-51-12. OPERATIONAL CHECK GODD WITH NO DEFECTS. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007071300325 20070713 00325 NM 2007 7 13 2007UALA02401 1 20070703 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 121UA 29167 SEAT 2J AFT EEL STRIP LIGHT ADRIFT FROM ARMREST. [07-24-07] SECURED LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071300340 20070713 00340 NM 2007 7 13 QXEA200701049 1 20070620 A 5410 COWL DOOR DHAV DHC8 DHC8202 2809007 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 - PDX NR 2 RIGHT SIDE ENGINE FORWARD INBOARD SIDE COWL DOOR 423AL HAS A CRACK ON THE UPPER STIFFENER FOR THE OIL ACCE SS DOOR. REPLACED IAW DHC-8-200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007071300355 20070713 00355 NM 2007 7 13 07FDEA02380 1 20070706 A 5330 6554583 SKIN BOEING 727 727227 1384078 NM ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 AFT FUSELAGE EXT SKIN BS 1208 STR S-23R SKIN IS GOUGED. INSTALLED REPAIR ON EXT SKIN, AFT FUSELAGE STA 1208 STR 23R R EF B727 SRM 53-30-3, PG 6 FIG 1. 2 L 7 3 4F A3WE 2007071300360 20070713 00360 NM 2007 7 13 TSAA0729040 1 20070707 A 2910 AE2464162E0192 HOSE BOEING 737 7372Y5 1384554 NM HYD SYSTEM FAILED A TSAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 13 810AL 24031 FLIGHT 26 HNL-OGG - AFTER TAKEOFF FROM HNL, CREW NOTED LOSS OF SYSTEM A HYDRAULIC PRESSURE. CREW RETURNED TO HNL WITHOU T FURTHER INCIDENT. MAINTENANCE TOWED THE AIRCRAFT TO THE GATE AND REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR HYDR AULIC SURGE RELIEF LINE. ALL HYDRAULIC PRESSURE AND LEAK CHECKS OK. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4U RT A16WE 2007071300365 20070713 00365 NE 2007 7 13 HEEA116157 1 20070627 A 3297 7655200904044 WIRE HARNESS SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL2S1 60057 NE MLG DAMAGED B HEEA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SW 03 767P 760599 RAISED GEAR. ALL (3) GREEN LIGHTS AND RED LIGHTS WENT OUT. RT MAIN GREEN LIGHT THEN CAME ON. LOWERED GEAR. RETURNED TO BASE. MAINTENANCE REPLACED RT MAIN PROXIMITY SWITCH HARNESS. 1 G 7 2 3U 4 U NC H1NE E00054EN 2007071300369 20070713 00369 SW 2007 7 13 HEEA116166 1 20070701 A 7921 BEARING BELL 412 412 1182202 SW PWA PT6 PT6* 52043 EA COOLER BLOWER FAILED B HEEA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SW 03 412SM 51009731602 33197 IN CRUISE FLIGHT THE AIRCRAFT EXPERIENCED A RHYTHMIC BUT INTERMITTENT VIBRATION. MAINTENANCE FOUND ONE OIL COOLER BLOWE R TO HAVE BAD BEARINGS AND CHIPPED BLADES. REPLACED OIL COOLER BLOWER. 1 G 7 2 4U 3 T H4SW E2NE 2007071300374 20070713 00374 NM 2007 7 13 F3LA200700163 1 20070627 A 5320 TRANSITION PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED HOLES IN AFT CARGO COMPARTMENT LT UPPER TRANSITION PANEL 151UG. REPLACED TRANSITI ON PANEL 151UG IAW AMM 53-42-14-000-001. 2 L 7 2 4F RT A28NM 2007071300388 20070713 00388 NM 2007 7 13 UPS07M50107 1 20070522 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C RT HORIZONTAL STABILIZER BARREL NUT HOLE NR 7 BORE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOV ED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTTO M PERIPHERY RADIUSED SMOOTHENED AND PROTECTED. REPAIR SLEEVE BUSHING FAB AND PROTECTED, PR1422 B1/2 SEALANT APPLIED AT BLEND OUT VOID AND REPAIR SLEEVE BUSHING INSTALLED. REWORK AREA PAINTED. 2 L 7 3 4F RT A22WE 2007071300390 20070713 00390 NM 2007 7 13 UPS07M50109 1 20070506 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C RT HORIZONTAL STABILIZER BARREL NUT NR 2 RT FOUND BORE CORRODED. CORROSION AT BARREL NUT BORE REMOVED , REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT AND BOTTOM PERIP HERY RADIUSED SMOOTHENED AND PROTECTED. REPAIR SLEEVE BUSHING FAB AND PROTECTED. PR1422 B1/2 SEALANT APPLIED AT BLEND OUT VOID AND REPAIR SLEEVE BUSHING INSTALLED. REWORK AREA PAINTED. 2 L 7 3 4F RT A22WE 2007071300397 20070713 00397 NM 2007 7 13 UPS07M50116 1 20070424 A 5753 HINGE DOUG MD11 MD11 3023602 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C RT O/B FLAP I/B AFT HINGE LOWER BORE (02EA) FOUND RUSTY. RT AFT O/B FLAP I/B HINGE PIVOT I/B AND O/B BORE BUSHING REMOVED. SPOT FACE CORROSION REMOVED FOUND EXCEED LIMIT. FPI C/OUT ON REWORK AREA FOUND NO CORROSION AND NO CRACK. REWORK AREA ETCH, FLAP PEENING, CADMIUM PLATING AND PAINTED. BUSHINGS (02EA) FAB, HEAT TREATED, MPI FOUND NO CRACK, CADMIUM PLATED AND INSTALLED. 2 L 7 3 4F RT A22WE 2007071300398 20070713 00398 NM 2007 7 13 UPS07M50117 1 20070424 A 5720 STIFFENER DOUG MD11 MD11 3023602 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C LT LE LWR COMPT ACCESS NR 519DB FOUND STIFFENER DOUBLER SUSPECTED CRACK AS MARKED, JUST O/B OF REFUEL PNL NR 519CB. HFEC INSP C/OUT FOUND CRACK APPROX 1/4". LT LE LWR COMPT ACCESS NR 51 9DB CLAMPS REMOVED. DAMAGED AREA AT LT LE LWR COMPT NR 519DB JUST O/B OF REFUEL PNL NR 519CB TRIMMED OUT. HFEC INSP C/OUT ON TRIMMED OUT AREA FOUND NO C RACK. REPAIR DOUBLER, FILLER AND ANGLES FAB, HOLES PICKED UP, HEAT TREATED, REPROTECTED, PAINTED AND INSTALLED. NR 519 DB CLAMPS INSTALL. 2 L 7 3 4F RT A22WE 2007071300399 20070713 00399 EA 2007 7 13 TRAX200700913 1 20070627 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 870AS 7530 CREW ESCAPE HATCH PLACARDS MISSING AND FADED. PAINTED CREW ESCAPE HATCH PLACARDS IAW SRM 51 25 00 2 L 7 2 4F RT A21EA 2007071300410 20070713 00410 NM 2007 7 13 SWAA073335 1 20070705 A 5311 65C33511 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071300412 20070713 00412 NM 2007 7 13 SWAA073331 1 20070705 A 5210 BACB10A201G BEARING BOEING 737 7373H4 1384600 NM R2 DOOR EXCESS PLAY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR TORQUE TUBE BEARINGS HAVE RADIAL PLAY. REMOVED AND REPLACED TORQUE TUBE BEARI NGS PER MM. 2 L 7 2 4F RT A16WE 2007071600007 20070716 00007 EU 2007 7 16 CPCP20070057 1 20070514 A 5320 ANGLE AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 260AE 263 FOUND FORWARD AND AFT HOLDING ANGLE FOR SIDE PANEL 222 CW AND 222A AW CORRODED. FORWARD AND AFT HOLDING ANGLE FOR SIDE PANEL 222CW AND 222AW REPLACED AS PER 51-25-01. 2 H 7 2 4T RT A53EU 2007071600008 20070716 00008 EU 2007 7 16 CPCP20070056 1 20070514 A 5330 SKIN AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 260AE 263 CORROSION FOUND ON EXTERNAL SURFACEOF LT GUTTER BETWEEN GUTTER BETWEEN FRAME 14 TO 17. FORWARD CARGO ENTRY GUTTER REPLA CED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007071600010 20070716 00010 NM 2007 7 16 07FDEA02383 1 20070706 A 5312 6518745 PANEL BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LT MLG WHEEL WELL, AFT LOWER WEB FAIRING ENCLOSURE, AFT SIDE HAS 2 FASTENER HOLES CRACKED LBL40-42, STATION JUST AFT OF 950 WL 147. REMOVED DAMAGED AREA'S IAW B727 SRM 51-10-1. FAB REPAIR FILLER AND DOUBLER IAW B727 SRM 51-40-3. INSTALLE D-FAB FILLER AND DOUBLER, IAW B727 SRM 51-40-3. THIS REPAIR IS CLASSIFIED AS MINOR. 2 L 7 3 4F RT A3WE 2007071600011 20070716 00011 NM 2007 7 16 07FDEA02384 1 20070706 A 5320 6523555108 BRACKET BOEING 727 727233 138408A NM ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD PIT STRUCTURE, BS 740, AT FWD END OF DELTA BEAM, "T" BRACKET, WL 150, RBL 5", IS GOUGED IN FWD RADIUS AREA. REMOVE D "T" BRACKET REF SRM 51-30-2. INSTALLED NEW "T" BRACKET AND FASTENERS REF SRM 51-30-02. 2 L 7 3 4F RT A3WE 2007071600012 20070716 00012 NM 2007 7 16 07FDEA02385 1 20070706 A 5314 655642210 KEELBEAM BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LWR FUSELAGE RT SIDE STA 740, RBL 7,KEEL BEAM CORRODED BETWEEN T-CAP FITTING AND SKIN. REMOVED FASTENERS FROM KEEL BEAM , REMOVED KEEL BEAM, DRILLED HOLES IN NEW KEEL BEAM ON SHOP NON ROUTINE NR N01206. INSTALLED BOLTS AT STA 740 IN KEEL B EAM USING TOOL S/N NR 030763468 DUE DATE 3-5-08 REF. DWG 65-2355. INSTALLED FASTENERS IN KEEL BEAM. 2 L 7 3 4F RT A3WE 2007071600013 20070716 00013 NM 2007 7 16 07FDEA02386 1 20070706 A 5322 691487112 SHEAR TIE BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD PIT BILGE BODY FRAME SHEAR TIE IS CRACKED/CORRODED BS 700, STR 28L-28R, WL 148 (MKD) REF SNRM N01157. REMOVED SHEAR TIE, BLENDED CORROSION ON FRAME, NDT FOR CRACKS, FABED NEW SHEAR TIE REF DRWG 69-14871-12. HEAT TREATED PART REF WO N0 1217. TREATED AND PRIMED REF SRM 51-10-2. INSTALLED SHEAR TIE REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007071600014 20070716 00014 NM 2007 7 16 07FDEA02342 1 20070629 A 5311 AFA00263 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 MAIN DECK CARGO, RIGHT FRAME 1641 AT STRINGER L12 FOUND DENT. REPAIR CARRIED OUT AT MAIN DECK CARGO, RIGHT FRAME 1641 A T STRINGER L12 AS PER SRM 53-30-00 FIGURE I VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007071600015 20070716 00015 NM 2007 7 16 07FDEA02343 1 20070629 A 5311 AFA00273 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 MAIN DECK CARGO, RIGHT FRAME 1661 AT STRINGER L12 FOUND DENT. REPAIR CARRIED OUT AT MAIN DECK CARGO, RIGHT FRAME 1661 A T STRINGER L12 AS PER SRM 53-30-00 FIGURE I VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007071600017 20070716 00017 NM 2007 7 16 07FDEA02345 1 20070629 A 5311 AFA00283 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 MAIN DECK CARGO, RIGHT FRAME 1701 AT STRINGER L12 FOUND DENT. REPAIR CARRIED OUT AT MAIN DECK CARGO, RIGHT FRAME 1701 A T STRINGER L12 AS PER SRM 53-30-00 FIGURE I VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007071600018 20070716 00018 WP 2007 7 16 07FDEA02369 1 20070703 A 5311 AFA00403 FRAME DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 398FE 46634 LOWER CENTER CARGO COMPARTMENT, FLOORBEAM AT FRAME 1741 CRACKED AT LBL 1"-5" AND RBL 2.5"-4" ON UPPER FLANGE. REPAIRED BY CUTTING OUT DAMAGE AND FABRICATING AND INSTALLING FILLER AND REPAIR ANGLES IAW MD/DC 10 SRM 53-00-01 FIG 9 VOL I. A LODINED AND PRIMERED AREA AND PARTS IAW MD/DC 10 SRM 51-21-01 VOL II. THIS IS A MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2007071600019 20070716 00019 NM 2007 7 16 07FDEA02371 1 20070704 A 5753 SKIN DOUG MD11 MD11F 3023600 NM TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 RIGHT WING I/B FLAP LOWER SURFACE FOUND DENT. REPAIR CARRIED OUT AT RIGHT HAND WING I/B FLAP LOWER SURFACE AS PER SRM 5 7-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007071600020 20070716 00020 WP 2007 7 16 07FDEA02387 1 20070706 A 2913 1489951 PUMP DOUG DC10 DC1030 3023501 WP HYD SYSTEM MALFUNCTIONED A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 309FE 15094 2891 48298 PDIS: CLIMBING THRU 7000MSL HYD NR 3 PRESSURE CUE LIGHT ILLUMINATED COMPLIED WITH QRH RETURNED TO MEM WHEN THE HYD PUMPS WERE TURNED OFF HYD QTY RETURNED TO 5.7 GALS. WHILE RUNNING QRH CHECKLIST PUMPS WERE TURNED ON HYD QTY DECREASED AND H YD PRESS CUE LIGHT ILLUMINATED. SHUT DOWN HYD SYS 3 QTY SHOWED 6.2 GALS. ALT GEAR HANDLE WAS USED TO EXTEND LANDING GE AR. FOUND HYD FLUID ON TAIL OF A/C FOGGING OUT OF THE DOOR RAN NR 3 HYD SYS AND FOUND SYS 3 HYD S/O VLV MOTOR LEAKING F ROM BETWEEN VLV HOUSING AND MOTOR. A GAP CAN BE SEEN BETWEEN VLV MOTOR AND HOUSING. REMOVED AND REPLACED 3-2 NON REVER SIBLE MOTOR PUMP SHUTOFF VALVE. RESET MANUAL EXT HANDLE. CHECKED ENG PUMP AND NR 3 CASE DRAIN FILTER DP INDICATORS. A 2 L 7 3 4F A22WE 2007071600021 20070716 00021 WP 2007 7 16 07FDEA02388 1 20070706 A 2620 HEAD DOUG MD10 MD1010F 3022112 WP FIRE BOTTLE SHEARED A FDEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 568FE 6192 53 41393EC 47827 MDIS: PER FLIGHT CREW, ON PREFLIGHT FOUND EAD ALERT NR 2 ENG NR 1 FIRE BOTTLE PRESSURE LOW ALERT AND OVERHEAD DISCHARGE LIGHT ON. WHILE T/S CONFIRMED NR 2 ENG NR 1 FIRE BOTTLE IS DISCHARGED. FOUND ON ENG SIDE OF BOTTLE DISCHARGE HEAD ASSY TO BE SHEARED IN HALF, SEPARATING IT FROM DISCHARGE LINE. REMOVED AND INSTALLED NR 2 ENGINE/APU FIRE EXTINGUISHER CONT AINER. INSTALLED DEPLOYMENT LINE AND DISCHARGE CARTRIDGES, A/C OK TO CONTINUE. 2 L 7 3 4F RT A22WE 2007071600022 20070716 00022 NM 2007 7 16 07FDEA02389 1 20070707 A 5343 ACA7017501 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 NOSE LANDING GEAR LT TRUNNION FOUND CRACKED. [07-24-07] REPAIR CARRIED OUT AS PER SRM 53-40-00 VOL.I. FIG. 23. C LASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007071600024 20070716 00024 EU 2007 7 16 07FDEA02392 1 20070707 A 3243 BRAKE ASSY AIRBUS 300 A300B4622R 3930312 EU MLG MALFUNCTIONED A FDEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 25 729FD 657 A/C POS AT (TAXIWAY A/RWY34) HOLD SHORT LINE WITH PKG BRK SET. RELEASED BRK, ATTEMPTED TO TAXI FOR T/O A/C WON'T MOVE. PKG BRK RESET GOT PERMISSION FROM TOWER TO POWER UP. RELEASED PKG AGAIN. POWERED UP TO 45 PERCENT N1/NO MOVEMENT OF A/C. (MX)TOWED A/C BACK TO GATE, NO PROBLEMS. IE PKG BRK RELEASED NORM. PKG BRK ADJ/TEST C/W. TOWED BACK TO GATE. P KG BRK FUNCTIONAL NORM, AFTER RE-CYCLING BRK HANDLE SEVERAL TIMES ON GATE CARRIED OUT PKG BRK/ULTIMATE EMERG BRAKING. O PS TEST PER MM 32-45-00-5. NO FAULTS FOUND, CHECKS SERVICEABLE. CYYC AIRPORT OPS SENT MX INSPECTOR TO CK FOR SOFT AREA (CONCRETE BASE/ASPHALT OVERLAY). NO DAMAGE. 2 L 7 2 4F RT A35EU 2007071600026 20070716 00026 NM 2007 7 16 07FDEA02394 1 20070707 A 5322 65561241 SHEAR TIE BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 AFT PIT SHEAR TIE CORRODED STA 950F BETWEEN STR 27 R-28R RBL 17 - 22 REMOVED CORROSION AT STA 950F, STR 27-28R, RBL 1 7-22, IAW SRM 53-10-1 PG 2, NDT FOR MATERIAL LOSS, ORIGINAL THICKNESS .063". REMAINING THICKNESS IS .058" . WITHIN 10 % LIMIT IAW SRM 53-10-1 PG 1. TREATED AND PRIMED AFFECTED AREA SRM 51-10-2. 2 L 7 3 4F A3WE 2007071600029 20070716 00029 NM 2007 7 16 07FDEA02398 1 20070709 A 5315 AFA7169U4006 FLOORBEAM DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CTR CARGO COMPT, FLOORBEAM STA 1781 FWD FLANGE AT X = -50 CRACKED. [07-24-07] REPAIRED AS PER FEDEX EA 1-5310-11235 4. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007071600036 20070716 00036 WP 2007 7 16 07FDEA02416 1 20070710 A 5347 S4929405 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 MAIN CABIN SEAT TRACK AT RBL-27, AT STA 1059 IS GOUGED. BLENDED SEAT TRACK AND OUT OF LIMITS. REMOVED AND INSTALLED NE W SEAT TRACK IAW DC/MD 10 SRM 53- 70-00 VOL I PGS 1-6A AND DC/MD 10 SRM 51-21-01 VOL II PGS 1-46. 2 L 7 3 4F RT A22WE 2007071600038 20070716 00038 WP 2007 7 16 07FDEA02418 1 20070710 A 5347 S4929147 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 556FE 46710 MAIN CABIN SEAT TRACK AT RBL - 8 AT STA 1199 IS GOUGED. BLENDED SEAT TRACK AND OUT OF LIMITS. FABRICATED SEAT TRACK AN D SPLICE REPAIR IAW DC/MD 10 SRM 53- 70-00 VOL I FIG 5. INSTALLED IAW DC/MD 10 SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2007071600042 20070716 00042 EU 2007 7 16 07FDEA02423 1 20070711 A 5313 A53986212 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 CORROSION FOUND ON STRINGER P55, C70-71, RT/LT STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007071600045 20070716 00045 EU 2007 7 16 07FDEA02426 1 20070711 A 5315 A53773558 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 749FD 536 OLD TOP CAP BEAM REPAIR NOT CONFORM TO SRM, AFT CARGO COMPARTMENT, C57 LT TOP CAP BEAM REPAIR RENEWED IAW SRM 53-10-15 F IG 208. 2 L 7 2 4F RT A35EU 2007071600050 20070716 00050 EU 2007 7 16 07FDEA02430 1 20070711 A 5320 A53970710202 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 HEAVY CORROSION ON C58 LT CORNER FITTING. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007071600051 20070716 00051 EU 2007 7 16 07FDEA02432 1 20070711 A 5310 SEE4A CROSSBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 HEAVY CORROSION ON CROSSBEAMS, C 61 RT (P/N A539-78476-200), C60 LT (A539-73599), C58 LT (P/N A539-74268). CROSSBEAM RE PAIR PERFORMED ON C58 LT AND C60 LT IAW SRM 53-10-15 FIG 207 AND REPLACEMENT OF PART ON C61 . 2 L 7 2 4F RT A35EU 2007071600052 20070716 00052 EU 2007 7 16 07FDEA02433 1 20070710 A 7830 32142368 REGULATOR VALVE AIRBUS 310 A310222 3930315 EU THRUST REVERSER FAILED A FDEA F C ACTIVATE FIRE EXT. ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 418FE 343 ENG 1 REV UNLOCK LIGHTS ILLUMINATED ON T/O ROLL LESS THAN 80KTS. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C 11JUL SFS. REMOVED AND REPLACED ENG 1 PRSOV, PERFORMED OPERATIONAL TEST, NORMAL PER MM 78-32-11-4 AND MM78-32-11-5. 2 L 7 2 4F RT A35EU 2007071600053 20070716 00053 NM 2007 7 16 07FDEA02402 1 20070709 A 5720 652165832 CHANNEL BOEING 727 727233 138408A NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 LT WING OB TE FLAP WELL LWR FIXED PNL SPPT CHANNEL IS CRACKED AT STRUT ATTACH POINT RSS 501 IB SIDE (MKD). REMOVED AND REPLACED CHANNEL ON LT WING OB TE FLAP P/N 65-21658 USE P/O 1013862, FX 0993 IAW B 727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007071600055 20070716 00055 NM 2007 7 16 07FDEA02404 1 20070709 A 5322 6943668 SHEAR TIE BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD PIT BILGE BODY FRAME SHEAR TIE IS BUCKLED/CRACKED BS 720E, 2 "OB OF STR 26L, WL 151 (MKD). REMOVED SHEAR TIE, FORME D, HEAT TREATED, TREATED, PRIMED AND MATCH DRILLED NEW SHEAR TIE. INSTALLED SHEAR TIE REF SRM 51-30-2, REF DRAWING 69-4 3668, SRM 51-10-2. 2 L 7 3 4F RT A3WE 2007071600056 20070716 00056 NM 2007 7 16 07FDEA02405 1 20070709 A 5730 SKIN BOEING 727 727233 138408A NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 RT WING LEADING EDGE CUTOUT IS CRACKED AT NR 6 SLAT INBD TRACK CUTOUT. INSTALLED DOUBLER REPAIR ON R/ WING LEADING EDGE CUTOUT AT NR 6 SLAT I/B TRACK CUTOUT. REF B727 SRM 51-30-02 PG2 57-30-4 PG 33 FIG II. 2 L 7 3 4F RT A3WE 2007071600057 20070716 00057 NM 2007 7 16 07FDEA02406 1 20070709 A 5320 65589896 ANGLE BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD PIT BILGE BODY FRAME INTERCOSTAL LWR CHORD IS BROKEN/CRACKED BS 720C 19, WL 148. REMOVED CHORD ANGLE REF SRM 51-30- 2 PG 2, VERIFIED MATERIAL AS BAC1505-100052. FABRICATED NEW CHORD ANGLE REF BOEING DWG NR 65-58989 ITEM -6. TREATED AN D PRIMED REF SRM 51-10-2 PG 2. INSTALLED CHORD ANGLE REF SRM 51-30-2 PG 2. 2 L 7 3 4F RT A3WE 2007071600058 20070716 00058 NM 2007 7 16 07FDEA02407 1 20070709 A 5411 6519645199 FRAME BOEING 727 727233 138408A NM ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 NR 2 ENG FWD LT COWL FWD END LWR CORNER CLOSURE COVER ANGLE CRACKED AT OUTER RADIUS. REMOVED DAMAGED CLOSURE COVER AN GLE REF SRM 51-30-2. FABRICATED NEW CLOSURE COVER ANGLE REF SRM 51-30-2 AND DWG 65-19645-199 AND INSTALLED NEW PART REF SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007071600059 20070716 00059 EU 2007 7 16 TRBA2007041 1 20070708 A 3350 3012701 LIGHT AEROSP ATR72 ATR72212A 8680902 EU CABIN FAILED A TRBA O OTHER O OTHER NR NOT REPORTED 1 SO 29 545AT 545 EMERGENCY LIGHT ON PAX DOOR ENTRY STAIR INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AS PER JIC NR 33-51- 24 AND FOUND WORKING PROPERLY. 2 H 7 2 4T RT A53EU 2007071600060 20070716 00060 NM 2007 7 16 QXEA200701094 1 20070708 A 2900 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM HYD SYSTEM UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 430QX 4163 SEA FLIGHT NR 2459: NR 2 RUD HYD CAUTION AND NR 2 HYD PRESS BLANK. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE INSPECTED A ND FOUND NR 2 HYD CIRCUIT BREAKER POPPED. RESET BREAKER AND GROUND RAN NR 2 ENGINE. NR 2 HYD CAUTION LIGHT EXTINGUISHE D. OPS CHECK OF NR 2 HYD PRESSURE INDICATION AND OPERATION IS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071600062 20070716 00062 NM 2007 7 16 QXEA200701096 1 20070708 A 6120 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM AUTOFEATHER SYS UNKNOWN A QXEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 09 406QX 4048 SEA FIGHT NR 2394: TAKEOFF ABORTED DUE TO NO AUTO FEATHER ARM. AIRCRAFT RETURNED TO GATE. MAINTENANCE INTERROGATED CDS FOR FAULTS. FOUND FAULT CODE 71 ON NR 2 PEC. CLEARED FAULT PER Q400 FIM 61-20-02-810-835. C/W OPS CHECK OF THE A/F A ND UPTRIM SYSTEM IAW Q400 AMM 61-20-00-710-801. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071600065 20070716 00065 EU 2007 7 16 TRBA2007042 1 20070707 A 3320 E038711 LIGHT AEROSP ATR72 ATR72212A 8680902 EU CABIN BURNED OUT A TRBA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 29 499AT 499 DURING DEPLANING THE LAST PAX AND F/O SAW AND SMELLED SMOKE ABOVE THE OVERHEAD BIN AT PAX SEAT 7AB. THE BURN MARKS ARE VISIBLE ON THE UPPER PART OF THE OVERHEAD BIN DOOR. REMOVED FLUORESCENT TUBE AT ROW 7AB IAW JIC NR 33-21-23 AND ITEM DE FERRED ON MEL 33-02 AUTH NR 070046-C. MEL DUE AT 07-18-2007. 2 H 7 2 4T RT A53EU 2007071600066 20070716 00066 NM 2007 7 16 07FDEA02410 1 20070709 A 5311 651593920 FRAME BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD PIT BILGE BODY FRAME SHEAR TIE IS CORRODED BS 720, STR 28L- 28R, WL 148 (MKD). REMOVED DAMAGED SHEAR TIE IAW 727 SRM 53-10-4 AND 51-30-2. FAB NEW SHEAR TIE IAW 53-10- 4. INSTALLED NEW SHEAR TIE IAW SRM 53-10-4 AND 51-30-2. 2 L 7 3 4F RT A3WE 2007071600067 20070716 00067 EU 2007 7 16 07FDEA02411 1 20070710 A 7830 UNKNOWN AIRBUS 310 A310222 3930315 EU THRUST REVERSER UNKNOWN A FDEA G O2 MASK DEPLOYED J WARNING INDICATION TO TAKEOFF 1 SO 25 418FE 343 UNLOCK LIGHTS ILLUMINATED ON T/O ROLL, LESS THAN 80KTS. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIR ATION: 20JUL07 "MEL 78-30-01-C: ENGINE (IDENTIFY 1 OR 2) NR 1 THRUST REVERSER, INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION." 2 L 7 2 4F RT A35EU 2007071600070 20070716 00070 NM 2007 7 16 07FDEA02414 1 20070710 A 5311 53FX1350 FRAME BOEING 727 727227 1384078 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 FWD CARGO PIT LT SIDE BS 600 STR 21L FRAME EXTENSION CRACKED ON O/B EDGE ABOVE STR 21L. REMOVED FRAME SPLICE REF SRM 51 -30-2. FORMED NEW FRAME SPLICE USING .063 7075-O A66693 PO NR 1008655 REF DWG 53FX1350 REV A. RECEIVED HEAT TREATED RE PAIR SPLICE REF FORM 8130-3 FORM NR 2007-07-031 AND SNRM N00633. LOCATED, DRILLED AND DEBURRED HOLES IN REPAIR PART REF SRM 51-30-02. INSTALLED REPAIR SPLICE IAW SRM 51-30-02 AND DWG # 53FX1350. 2 L 7 3 4F A3WE 2007071600074 20070716 00074 NM 2007 7 16 QXEA200701093 1 20070709 A 3150 UNKNOWN DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 1 ENGINE UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 358PH 506 SEA FLIGHT NR 2182, ENGINE 1 AND ENGINE 2 MANUAL CAUTION LIGHTS ILLUMINATED ON TAXI DURING BETA BACK UP TEST. RESET BET A BACK UP SYSTEM. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007071600075 20070716 00075 NM 2007 7 16 QXEA200701091 1 20070705 A 3244 4151171 TIRE BOMBDR DHC8 DHC8402 1390042 NM MLG FAILED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 402QX 4032 YVR FLIGHT NR 2279: DURING TAXI THERE WAS A LOUD POP. INSPECTION REVEALED LARGE HOLE IN SIDE OF RT INBOARD TIRE. MAINT ENANCE REPLACED 33 AND NR 4 MLG WHEEL ASSY'S IAW MTC 6324101. C/W TIRE EXPLOSION CHECK IAW Q400 AMM TASK 05-50-61-210-8 01. NO DEFECTS FOUND. CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071600081 20070716 00081 EU 2007 7 16 TRBA2007044 1 20070710 A 3350 3012701 LIGHT AEROSP ATR72 ATR72212A 8680902 EU CABIN INOPERATIVE A TRBA O OTHER O OTHER NR NOT REPORTED 1 SO 29 529AM 529 MAIN PAX DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED PAX DOOR EMERGENCY LIGHT ASSEMBLY IAW JIC NR 33-51-24. OP CK IAW JIC #33-50-00. 2 H 7 2 4T RT A53EU 2007071600082 20070716 00082 NM 2007 7 16 07FDEA02397 1 20070708 A 3233 ROD END BOEING BOEING 727 7272S2F 1384O81 NM ACTUATOR SHEARED A FDEA R AUTOROTATION J WARNING INDICATION LD LANDING 1 SO 25 215FE 18437 18437 864 22936 LANDING AT GTF, THE NOSE GEAR WOULD NOT EXTEND. RAN THE QRH EXTENDED THE GEAR MANUALLY. FOUND LOCK ACTUATOR RODEND SHE ARED OFF. REPLACED NOSE GEAR LOCK ACTUATOR PER MM 32-33-011-4. OPS CHECKS NORMAL. PREMATURE REMOVAL/INSTALLATION OFF MFG 65-40467-6, SRL 864, TAG 6795B5, ON MFG 65-40467-6 SRL 797, TAG 697142. 2 L 7 3 4F A3WE 2007071600083 20070716 00083 2007 7 16 07FDEA02434 4 20070711 A 3414 4045053914 ADC AIRBUS 300 A300F4605R 3930327 EU NR 2 FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 671FE 778 DIVERTED TO IAD, CLIMBING THRU 16,000', GOT APPROX 25 KT DIFFERENCE IN AIR SPEED IND. SECONDARY GEAR IND INOP. ENG N-1 MODE FAULT. BLOWING OUT NR 2 SYS, REMOVED AND REPLACED ADC NR 2 PER MM 34-11-34-4. REMOVED AND REPLACED PROX BOX PER MM 32-31-71-4. ACN RELEASED FOR SERVICE PER MEL/CDL: 73-23-01-05-1. 2 L 7 2 4F RT A35EU 2007071600084 20070716 00084 NE 2007 7 16 07FDEA02435 2 20070711 A 7261 MAIN BEARING AIRBUS 310 A310203 3930313 EU GE CF6 CF680A3 30025 NE NR 1 ENGINE LEAKING A FDEA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 25 414FE 400 585145 DIVERTED - PIT AT FL340 NOTICED A FAINT BURN ODOR. THIS WAS FOLLOWED BY A ECAM [MAIN DECK CARGO LOOP FAULT] W/ASSOCIATE D LOOP "A" LIGHT AFT. 15-20 SECONDS LIGHT EXTINGUISHED. NEXT LOOP "A/B" LIGHTS ILLUMINATED W/RED SMOKE (AFT) ILLUMINAT ED FOLLOWED BY LOOP "A" /LOOP "B" LIGHTS W/MID 2 SMOKE LIGHT ILLUMINATED. ECAM CALLED FOR LAND ASAP/MAIN DECK SMOKE/OXY GEN MASKS SMOKE DET SYS CHECKED OK. SLIGHT HAZE IN CABIN, NOTICED OIL LEAKING FROM NR 1 ENGINE REVERSER HALFS. NR 1 MA IN BEARING LEAK, REPEAT DETERMINED TO BE ENGINE CHANGE FOR OIL LEAK. 2 L 7 2 4F 4 F RT A35EU E13NE 2007071600086 20070716 00086 EU 2007 7 16 07FDEA02437 1 20070711 A 2800 UNKNOWN AIRBUS 310 A310203 3930313 EU FUEL SYS UNKNOWN A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 431FE 316 IN CRUISE FLT, LT INNER FUEL GAUGE READ 5 K LESS THAN RT. RAN CK LIST RESET SYSTEM C/B'S IAW QRH STILL SHOWED IMBALANCE. DIVERTED DUE TO SUSPECTED LEAK. WING DIPPED ON FINAL AS IF RIGHT WING WAS HEAVY. GAUGES SHOWED 6000 LB LOSS IN LEFT INNER IN CHOCKS. CK'D STICKS ON LT AND RT INNER LT INNER APPROX 5000 LESS THAN RT. TESTED FUEL QTY SYS PER M/M 28-42 -00-05 FAULTS LA,111,122 ,952. FUELED A/C TO 40000 WHILE TAKING READING LT INNER JUMPED 5000 HIGHER WITH NO FUEL BEING ADDED AND TOTALIZER SHOWED 45000 TRANSFERRED FUEL OUT OF LT INNER AND FUELED LT INNER TO KNOWN QTY FROM RT INNER. RAN ALL PUMPS AND CK'D FOR MIGRATION NONE NOTED FUELED LT INNER TO 26000 AND CK'D FOR LEAKS. NONE NOTED. 2 L 7 2 4F RT A35EU 2007071600088 20070716 00088 EU 2007 7 16 07FDEA02440 1 20070712 A 5311 SEE4B FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 IN THE AREA OF FWD AND AFT SIDE OF FRAME 932 SOME AREAS WITH CORROSION REPAIR PERFORMED BY REPLACEMENT OF THE FOLLOWING PARTS IAW SRM 51-72-10. T-SECTION A539-89317-206, ANGLE SECTION A539-89317-228, A539-893127-229, A539-89317-224, A539-8 9317-225, A538-89317-222, A539-89317-223, A539-89579-201, A539-89579-203 2 L 7 2 4F RT A35EU 2007071600090 20070716 00090 NM 2007 7 16 07FDEA02443 1 20070712 A 5347 BAC1520792 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 CABIN LBL 25 SEAT TRACK IB AND OB FLANGES UPPER SURFACES HAVE CORROSION BETWEEN BS 560 AND BS 620. REMOVED CORROSION, C HECK FOR MATERIAL LOSS, OUT OF LIMITS. REMOVED SEAT TRACK STA 480-690 LBL 25, FAB NEW SEAT TRACK MATERIAL VERIFIED A-TA G NR A44280 P/O 1023241 BAC1520-792 7178T651. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED NUTPLATES AND RADIUS BLOCK S INSTALLED NEW SEAT TRACK STA 480-690 LBL 25 REF SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007071600091 20070716 00091 EU 2007 7 16 TRBA2007045 1 20070710 A 2497 WIRE AEROSP ATR72 ATR72212 8680945 EU COCKPIT SHORTED A TRBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 29 342AT 345 CAPT RETURNED TO SXM WITH ELECTRICAL SHORT AND FUMES IN COCKPIT. EMERGENCY DECLARED. WIRES SPLICING ON WIRING BUNDLE 2 M AT 120VU IN PROGRESS. NEED TO PERFORM OP CKS. 2 H 7 2 4T RT A53EU 2007071700001 20070717 00001 2007 7 17 BAQA200700019 4 20070626 A 2330 01121036158 TRANSCEIVER UROCOP EC135 EC135P2 5620027 EU FM RADIO BURNED OUT E BAQA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 03 138MH 1379 79 0417 JUST AFTER LEVEL OFF TO CRUISE FLIGHT, MULTIBAND TRANSCEIVER (FM RADIO) DISPLAY SCREEN WENT BLACK, ACCOMPANIED BY ELECT RICAL BURNING SMELL. RETURNED TO BASE AND MADE A NORMAL LANDING WITH NO FURTHER INCIDENT. 1 G 7 2 3U H88EU 2007071700002 20070717 00002 CE 2007 7 17 GUUA06260701 1 20070626 A 3260 DOWNLOCK SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NLG DAMAGED A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 29 87551 UE206 FLIGHT: 9244 FLL/GGT DURING APPROACH THE LANDING GEAR IN TRANSIT LIGHT REMAINED ILLUMINATED WITH THE GEAR HANDLE IN THE DOWN POSITION. NOSE GEAR INDICATED UNSAFE CONDITION. RECYCLED LANDING GEAR OBTAINED GOOD INDICATIONS. REPLACED NOSE G EAR DOWNLOCK SWITCH AND ADJUSTED. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007071700003 20070717 00003 SO 2007 7 17 GUUA06210701 1 20070621 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN INOPERATIVE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 261AS 120141 FLIGHT: 253, RT TOP EMERGENCY LIGHT BY THE RT PACK BURNED OUT. FOUND RT TOP EMERGENCY LIGHT WORKING, OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2007071700005 20070717 00005 CE 2007 7 17 DJFA2007069 1 20070625 A 5511 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 447LX RK248 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER IB RIB AND BRACKET ASSEMBLIES, THE RT AND LT IB ROLLER BRACKETS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIO NS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE NR 70. MAINTENANCE REOMVED AND REPLACED THE RIBS. 2 H 7 2 4F 4 F RT A16SW E25EA 2007071700010 20070717 00010 SO 2007 7 17 HSYA20070701 1 20070629 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN FUMES E HSYA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 05 210AS 120006 DURING TAXI, CREW REPORTED HAZE IN THE COCKPIT CAUSING EYE AND NOSE IRRITATION. THE AIRCRAFT RETURNED TO THE PARKING ARE A/RAMP WITHOUT INCIDENT. MX COULD NOT DUPLICATE THE DISCREPANCY AFTER PERFORMING A VISUAL INSPECTION OF THE AVIONICS S YSTEMS COMPONENTS AND WIRING, ENGINE RUNS AND AIR CONDITIONING CHECKS WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2007071700020 20070717 00020 EA 2007 7 17 A6WA200740350 1 20070623 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AW 7878 RT SIDE FS 621.00 TO 625.30 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. MAINTENANCE REMOVED AND REPLACED RT SIDE FS621.00 TO 625..00 INTERCOSTAL AT STR 14 R IAW CRJ 200 SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700021 20070717 00021 EA 2007 7 17 A6WA200740351 1 20070623 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AW 7878 LT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. MAINTENANCE REMOVED AND REPLACED LT SIDE FS 621.00 TO 625.00 INTERCOSTAL AT STR 14L IAW CRJ 200, SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700023 20070717 00023 EA 2007 7 17 A6WA200740353 1 20070625 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AW 7878 RT FLOOR SUPPORT STRUCTURE IS CRACKED AT FS 621.00. MAINTENANCE REPAIRED RT FS 621 IAW REO 601R53-61-117 REV C. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700024 20070717 00024 EA 2007 7 17 A6WA200740354 1 20070625 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AW 7878 LT FLOOR SUPPORT STRUCTURE IS CRACKED AT FS 621.00. MAINTENANCE REPAIRED FLOOR SUPPORT BY CUTTING OUT DAMAGED ANGLE, FAB BING REPAIR PARTS AND INSTALLING IAW REO 601R53-61-717, REV C AND BSC EO 601R-53-12256. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700026 20070717 00026 EA 2007 7 17 A6WA200740309 1 20070616 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LAVATORY ODOR A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 31 433AW 7289 LAV SMOKE TOILET MESSAGE APPEARED ON FINAL APPROACH. F/A REPORTED SMOKE AND STRONG ELECTRICAL ODOR COMING FROM CENTER O VERHEAD. APU AND PACKS ON. SMOKE DISSIPATED 3-5 MINUTES AFTER INDICATION. REMOVED CEILING PANELS. INSPECTED LIGHT FI XTURES AND WIRING. FOUND NO EVIDENCE OF BURNING OR ARCING IAW AMM 20-10-00. RAN AC PACKS FOR (2) HOURS. NO ODOR/ SMOK E NOTED. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700027 20070717 00027 EA 2007 7 17 A6WA200740310 1 20070616 A 4900 38004883 APU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AFT SMOKE A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 31 433AW 19596 7289 AFTER TRANSFERRING BLEEDS TO APU, THERE WAS A FAINT ODOR IN THE COCKPIT, ENGINES AT IDLE, (SMOKE TOILET) MESSAGE ON ED 1 . MESSAGE CLEARED ON RUNWAY. FA REPORTS SMOKE AT CEILING AT ROW 11 AND 12. REPORTS SMOKE AT CEILING AT ROW 11 AND 12 REMOVED AND REPLACED APU ASSEMBLY IAW 49-10-00. OPS LEAK CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700028 20070717 00028 EA 2007 7 17 A6WA200740312 1 20070618 A 5210 PUSH-PULL ROD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR OUT OF POSITION A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 431AW 7256 PASSENGER DOOR WILL NOT OPEN/CLOSE FROM OUTSIDE. OPCV NORMAL FROM INSIDE. PLACARDED AND PLACED ON MEL. REPOSITIONED O UTER DOOR HANDLE PUSHPULL TUBES IAW CMM. OPS CHECK GOOD. REMOVED FROM MEL. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700032 20070717 00032 EA 2007 7 17 A6WA200740316 1 20070615 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 434AW 7322 LT FS 484 INTERCOSTAL ANGLE CRACKED APPROX .2 INCH LONG LBL 27 AT FLOORBEAM. MAINTENANCE REPAIRED IAW CRJ 200 SRM 51-42 -21 AND BSC STANDARD REPAIR NR 601R-53-0029B. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700033 20070717 00033 EA 2007 7 17 A6WA200740317 1 20070616 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 434AW 7322 RT WING STR 53.60 BATT RIB IS CRACKED 1.0 INCH ON UPPER AFT CORNER. MAINTENANCE REPAIRED IAW REO 601R-57-51-046. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700038 20070717 00038 EA 2007 7 17 A6WA200740322 1 20070624 A 5210 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR UNKNOWN A A6WA O OTHER S AFFECT SYSTEMS NR NOT REPORTED 1 GL 31 470ZW 7927 PASSENGER DOOR WILL NOT OPEN. (DISCOVERED AT GATE, WHEN TRYING TO DEPLANE PASSENGERS). PERFORMED OPERATIONAL CHECK OF PASSENGER DOOR, COULD NOT DUPLICATE MALFUNCTION IAW AMM 52-11-00. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700039 20070717 00039 EA 2007 7 17 A6WA200740323 1 20070618 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 434AW 7322 NLG AFT DOOR CUTOUT CRACKED IN LT AND RT RADIUS .5 INCH EACH SIDE. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700040 20070717 00040 EA 2007 7 17 A6WA200740324 1 20070622 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 434AW 7322 REAR PRESSURE BULKHEAD WEB AT RBL 9.5 NL 85.5 HAS AN INDICATION NOTED APPROX .5 INCHES IN LENGTH IN VERTICAL DIRECTION F AILED NDT INSPECTION. [07-31-07] MAINT REPAIRED REAR PRESSURE BULKHEAD WEB AT RBL 9.5, WL 85..5 BY CUTTING AWAY DAMAG E, FABBIN REPAIR PARTS AND INSTALLING IAW REO 601-53-61-1285. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700041 20070717 00041 EA 2007 7 17 A6WA200740325 1 20070619 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 460AW 7867 PAX DOOR AFT DRAG ANGLE HAS A CRACK APPROX 1 INCH LONG AT UPPER EDGE OF CABLE PULLEY BRACKET. [07-31-07] MAINTENANCE REPAIRED IAW REO 601R-52-11-513, STEPS 1-10. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700042 20070717 00042 EA 2007 7 17 A6WA200740326 1 20070619 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 460AW 7867 PAX DOOR AFT DRAG ANGLE HAS A CRACK APPROX .5 INCH LONG AT LOWER CORNER OF NR 2 STEP. MAINT REPAIRED IAW REO 601R-52-1 1-702. REV A STEPS 1 THRU 12. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700045 20070717 00045 EA 2007 7 17 A6WA200740329 1 20070617 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 460AW 7867 RT FS 621 TO FS 625 UPPER INTERCOSTAL (OBLIQUE) ANGLE IS CRACKED 1.5 INCH LONG. MAINTENANCE REMOVED CRACKED ANGLE AND I NSTALLED A NEW ANGLE (PN 601-35012-52 IAW SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700046 20070717 00046 EA 2007 7 17 A6WA200740330 1 20070617 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 460AW 7867 LT FS 621 TO FS 625 UPPER INTERCOSTAL (OBLIQUE) ANGLE IS CRACKED 1..5 INCH LONG. MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED A NEW ANGLE PN 601-35012-51 IAW CRJ SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700048 20070717 00048 EA 2007 7 17 A6WA200740334 1 20070625 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 462AW 7875 RT FS 621 FLOOR SUPPORT ANGLE APPROX .2 INCH LONG. MAINTENANCE REMOVED DAMAGED AREA AND INSTALLED REPAIR ANGLE IAW REO 601R-53-61-117. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700049 20070717 00049 EA 2007 7 17 A6WA200740335 1 20070625 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 462AW 7875 LT FS 621 FLOOR SUPPORT ANGLE CRACKED APPROX .2 INCH LONG. MAINTENANCE CUT OUT DAMAGED AREA AND INSTALLED REPAIR ANGLE IAW REO 601R-53-61-117. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700052 20070717 00052 EA 2007 7 17 A6WA200740338 1 20070624 A 5230 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CARGO DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 462AW 7875 CARGO DOOR FWD TRACK C-CHANNEL HAS A .5 INCH LONG CRACK WL. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700053 20070717 00053 EA 2007 7 17 A6WA200740339 1 20070624 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 462AW 7875 LT FS 484 ANGLE IS CRACKED AT LBL 36 AND 27 APPROX 1.4 INCH L. MAINTENANCE REPAIRED LT FS 484 IAW REO AND SRM. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071200098 20070712 00098 NM 2007 7 12 F3LA200700152 1 20070627 A 5320 TRANSITION PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED HOLES IN AFT CARGO COMPARTMENT TRANSITION PANEL 162CF. REPAIRED TRANSITION PANEL 162CF IAW SRM 53-02-00, FIG. 204. 2 L 7 2 4F RT A28NM 2007071200103 20070712 00103 NM 2007 7 12 F3LA200700154 1 20070627 A 5321 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED HOLES IN TOP SURFACE OF AFT CARGO COMPARTMENT FLOOR PANEL 161PF. REPAIRED HOLES I N FLOOR PANEL 161PF IAW SRM 53-02-00, FIG. 204. 2 L 7 2 4F RT A28NM 2007071200107 20070712 00107 NM 2007 7 12 F3LA200700157 1 20070627 A 5321 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED HOLES IN TOP SURFACE OF AFT CARGO COMPARTMENT FLOOR PANEL 151PE. REPAIRED HOLES I N FLOOR PANEL 151PE IAW SRM 53-02-00, PB201, PARA 8 C., FIG 204. 2 L 7 2 4F RT A28NM 2007071200108 20070712 00108 NM 2007 7 12 F3LA200700158 1 20070627 A 5321 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED TOP SKIN PUNCTURED ON AFT CARGO COMPARTMENT FLOOR PANEL 161NF. REPAIRED PUNCTURES ON FLOOR PANEL 161NF IAW SRM 53-02-00, PB 201, PARA 8 C., FIG 204. 2 L 7 2 4F RT A28NM 2007071200109 20070712 00109 NM 2007 7 12 F3LA200700159 1 20070627 A 5320 TRANSITION PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT TRANSITION PANEL 151AE DAMAGED. REPAIRED PUNCTURES IN TRANS ITION PANEL 151AE IAW SRM 53-02-00, PB 201, PARA 8 C., FIG 204. 2 L 7 2 4F RT A28NM 2007071200116 20070712 00116 NE 2007 7 12 HEEA115976 1 20070615 A 2910 7665104001082 LINE SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL1S1 60030 NE HYD SYSTEM CHAFED B HEEA O OTHER J WARNING INDICATION LD LANDING 1 SW 03 761P 760588 DURING SHORT FINAL LANDING AT VK989, NR 1 HYDRAULIC LIGHT CAME ON. COMPLETED LANDING SAFELY ON DECK, SHUTDOWN. MAINTEN ANCE FOUND HYDRAULIC TUBE BELOW TAIL ROTOR GEARBOX TO HAVE A HOLE CHAFED IN IT. REPLACED TUBE ASSY. 1 G 7 2 3U 3 U NC H1NE E19EU 2007071200117 20070712 00117 NE 2007 7 12 HEEA115977 1 20070617 A 3212 7625100702043 LINK SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30 03013 GL MLG SHEARED B HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 776P 760275 AFTER DEPARTURE, THE RED GEAR UNSAFE LIGHT STAYED ILLUMINATED WHEN THE GEAR HANDLE WAS PLACED IN THE UP POSITION. MAINT ENANCE FOUND THE SHEAR PIN IN ONE EXPLOSIVE LINK SHEARED. REPLACED LINK ASSY. 1 G 7 2 3U 3 U H1NE E1GL 2007071200118 20070712 00118 2007 7 12 HEEA115978 4 20070618 A 3100 B19030MD03 INDICATOR SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B 60037 NE FAILED B HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 350LG 3690 RETURNED TO BASE, WHEN LANE 2 OF VEMD FAILED TO ILLUMINATE. REPLACEMENT OF VEMD CURED PROBLEM. 1 G 7 1 3U 3 U H9EU E00054EN 2007071200137 20070712 00137 2007 7 12 UPS07250056 4 20070626 A 2565 SLIDE BOEING 727 72722C 138400F NM EMERGENCY EXIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 ESCAPE SLIDE IS OUT OF PACK. REINSTALLED EVACUATION SLIDE IAW AMM 25-60-14-2. 2 L 7 3 4F A3WE 2007071200146 20070712 00146 NM 2007 7 12 UPS07450041 1 20070528 A 5320 65B0961410 PLATE BOEING 747 747212B 1384886 NM BS 840 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C M/D BS 840 RT TENSION TIE ATTACH STEEL PLATE SHORT EDGE MARGIN FOUND AT UPPER ROW NR 4 COUNT FROM O/B. M/D BS 840 RT TENSION TIE ATTACH S/STEEL PLATE REPLACED AND INSTALLED AS PER RS R53-25-35808. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35808 AND UPS EO B747-5310-26949. 2 L 7 4 4F A20WE 2007071200147 20070712 00147 NM 2007 7 12 UPS07450042 1 20070530 A 5320 FILLER BOEING 747 747212B 1384886 NM BS 820 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C CRACK FOUND AT FILLER AT LT SIDE OF BS 820 STR 10A ATTACHED TENSION TIE NR 12 HOLE AT 4 AND 7 O/C POSI TION. CRACK LENGTH 3/32" AND 1/16". M/D BS 820 LT STR 10A TENSION TIE ATTACH FILLER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND UPS EO B747-5310-23715-C. 2 L 7 4 4F A20WE 2007071200153 20070712 00153 NM 2007 7 12 UPS07550063 1 20070627 A 2560 ESCAPE ROPE BOEING 757 75724APF 1384969 NM EMERGENCY EXIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 456UP 25477 CAPT SIDE EMERGENCY ESCAPE ROPE ACCESS DOOR WILL NOT STAY IN PLACE. REPLACED BROKEN LATCH ON UPPER LT SIDE PANEL. CAPT 'S EMERGENCY ESCAPE ROPE ACCESS DOOR NOW SECURED. 2 L 7 2 4F RT A2NM 2007071200158 20070712 00158 WP 2007 7 12 UPS07850054 1 20070607 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FS 320 L21L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 L21L AT STA 320 CRACKED. CUT OUT DAMAGED CUSP AT STA 275 - 330 L21L IAW SRM 53-02-05 FIG 15. FABRIC ATED AND INSTALLED REPAIR DOUBLERS, FILLERS AND CUSP SECTION AT STA 275 - 330 L21L IAW SRM 53-02-05 FIG 15. 2 L 7 4 4F RT 4A25 2007071200162 20070712 00162 NM 2007 7 12 UPS07M50060 1 20070406 A 5313 LONGERON DOUG MD11 MD11 3023602 NM STA 5-128 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C CTR CARGO COMPT AT STA 5-128 LONGERON 45 RT FOUND SUSPECTED CRACKED ON DOUBLER AREA. HFEC INSP C/OUT PER DAC NDT SPM REV 13 PART 06-10-01-001 ON DOUBLER FOUND CRACK. CRACK LONGERON SPLICE AT CTR CGO STA 5-128 L45R REMOV ED. NEW SPLICE P/N A5A7116-509 FAB PER DWG A5A7116. FPI C/OUT ON NEW SPLICE, FOUND NO CRACK. NEW SPLICE FASTENER HOLE S PICKED UP, REPROTECTED PAINTED AND INSTALLED. REWORK AREA PAINTED PER SRM 51-21-02 VOLII REV 39. 2 L 7 3 4F RT A22WE 2007071200175 20070712 00175 WP 2007 7 12 UPS07850080 1 20070622 A 5720 CHANNEL DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 R/WING CENTER L/E OUTBD T CHANNEL IS CRACKED. STOP DRILLED CRACKED T CHANNEL AT R/WING STA X 501 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR ANGLE ON T CHANNEL IAW SRM 57-02-00 FIG 002. 2 L 7 4 4F RT 4A25 2007071200190 20070712 00190 NM 2007 7 12 UPS07M50094 1 20070518 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 889-919 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C CABIN-SEAT TRACK BETWEEN STA889-919 RBL=107 FOUND CORRODED. REMOVAL C/OUT ON SEAT TRACK AREA TO EXECU TE REPAIR AS NECESSARY. REPAIRED S/TRACK SPLICE HAT AND SPLICE PLATE FAB PER SRM 53-70-00.V2.R 38. PICKED UP HOLES FOR FAB PARTS PER SRM 51-31-01.V2.R38. FAB PARTS ALODINE AND PAINTED PER SRM 51-21-01.R38. FAB PARTS OK TO INSTALL. SEA T TRACK INSTALLED PER SRM 51-31-01V2.R38, FOUND SATIS. 2 L 7 3 4F RT A22WE 2007071300036 20070713 00036 NM 2007 7 13 USAA070516 1 20070629 A 5320 CHANNEL BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 BETWEEN BS 500 & BS 400, STR 28L & 28R UNDER CHANNEL HAS CORROSION. REPAIRED PER BOEING DWG 65-45783, SRM 51-10-02; COR R TASK C53-208-01, DEFECT SIZE: 4 X 6 INCHES. 2 L 7 2 4F RT A16WE 2007071300057 20070713 00057 NM 2007 7 13 AALA20071193 1 20070628 A 3397 WIRE HARNESS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 363AA 24044 ORD - EMERGENCY LIGHT AT SEAT ROW 10HJ INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHT AT SEAT ROW 10HJ. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007071300060 20070713 00060 NM 2007 7 13 BB07046 1 20070629 A 3350 20131 CHARGER BOEING 767 7672B7 1385107 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 251AY 24764 MAINTENANCE FOUND EMERGENCY EXIT SIGN AT POSITION R2 INOPERATIVE. REPAIRED WIRING AND REPLACED BATTERY CHARGER. NO FUR THER FAULTS. 2 L 7 2 4F RT A1NM 2007071300061 20070713 00061 NM 2007 7 13 AALA20071197 1 20070628 A 3397 WIRE HARNESS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 363AA 24044 ORD - EMERGENCY LIGHT AT SEAT ROW 17HJ INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHT AT SEAT ROW 17HJ. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007071300067 20070713 00067 NM 2007 7 13 AALA20071198 1 20070628 A 3397 WIRE HARNESS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 363AA 24044 ORD - EMERGENCY LIGHTS AT BULKHEAD FORWARD OF SEAT ROW 20CEG INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHTS AT BULKH EAD FORWARD OF SEAT ROW 20CEG. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007071300073 20070713 00073 NE 2007 7 13 QXEA200701028 2 20070625 A 7200 4114T15P02 BLADES CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE NR 2 ENGINE WORN A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 609QX 1157 10031 DEN- TAXI FOR FLIGHT 4275, NR 2 ENGINE FAN VIBRATIONS. RETURNED TO THE GATE. MAINTENANCE INSPECTED THE BLADES AND PLACE D THEM ON RSI FOR 10 HOURS. MAINTENANCE REPLACED THE FAN BLADES. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVIC E. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007071300091 20070713 00091 NM 2007 7 13 SWAA073267 1 20070629 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071300092 20070713 00092 NM 2007 7 13 SWAA073265 1 20070629 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071300094 20070713 00094 NM 2007 7 13 SWAA073280 1 20070701 A 5754 65C26602 SKIN BOEING 737 7373H4 1384600 NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND RT WING NR 4 L/E SLAT LOWER SKIN CRACKED AT OUTBOARD AUX TRACK. REPAIRED SLAT PER SRM . 2 L 7 2 4F RT A16WE 2007071300095 20070713 00095 NM 2007 7 13 SWAA073264 1 20070629 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071300096 20070713 00096 NM 2007 7 13 SWAA073273 1 20070701 A 3350 8100022602 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 404WN 27892 MID CABIN EEPLS ASSY LOOSE. SECURED ASSY PER MM. 2 L 7 2 4F RT A16WE 2007071300099 20070713 00099 EA 2007 7 13 QXEA200701026 1 20070621 A 5241 SEAL CNDAIR CL600 CL6002C10 1390015 EA GALLEY DOOR DIRTY A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 602QX 10010 PDX- FLIGHT ATTENDANT REPORTS THE GALLEY SERVICE DOOR IS HARD TO OPEN. MAINTENANCE CLEANED AND LUBRICATED THE DOOR SEAL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE, NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007071300103 20070713 00103 EA 2007 7 13 QXEA200701023 1 20070622 A 2150 GG670950023 SHUTOFF VALVE CNDAIR CL600 CL6002C10 1390015 EA A/C PACK MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 606QX 10023 DEN - FLIGHT 4339, ON LIFT OFF, A RIGHT PACK TEMPERATURE CAUTION MESSAGE WAS RECEIVED. RETURNED TO THE FIELD AND ACCOMP LISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE HOT AIR SHUT OFF VALVE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007071300105 20070713 00105 NM 2007 7 13 SWAA073268 1 20070629 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 432WN 33715 DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007071300107 20070713 00107 NM 2007 7 13 KPVA20078 1 20070701 A 3260 814005 PSEU DHAV DHC8 DHC8103 1386005 NM MALFUNCTIONED A KPVA D RETURN TO BLOCK N FALSE WARNING CL CLIMB 1 WP 13 829EX 146 (PIREP) AFTER TAKEOFF, THE AMBER AND RED LIGHTS ON THE NOSE GEAR INTERMITTENTLY CAME ON TWICE. (MX) REMOVED AND REPLACE D THE PSEU. BITE TEST AND TARGET TEST IAW DHC-8 MM 32-61-50 PG 201-204. NO DEFECTS NOTED. 2 H 7 2 4T RT A13NM 2007071300112 20070713 00112 WP 2007 7 13 NWAA072409979 1 20070630 A 5310 STRUCTURE DOUG DC9 DC931 3022065 WP FUSELAGE DAMAGED A NWAA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 GL 01 9343 47439 DURING GROUND OPERATIONS AIRCRAFT WAS DAMAGED BY SERVICE VEHICLE AT BS 299 S24L. STRINGER 24L AND BUTT SPLICE STRAP WER E BOTH SEVERED. FUSELAGE SKIN FORWARD AND AFT OF BS 229 WAS DAMAGED. THE FUSELAGE SKIN AND STRINGER WILL BE REPAIRED P ER SRM. THE BUTT SPLICE STRAP REPAIR WILL BE ACCOMPLISHED BY EA 99-209308 SECT I. SECTION IV REPAIR TO BE ACCOMPLISHED 8000 CYCLES AFTER SECT I. 2 L 7 2 4F A6WE 2007071300114 20070713 00114 EA 2007 7 13 TRAX200700895 1 20070625 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 871AS 7537 FS 280 FLOOR SUPPORT ANGLE IS CRACKED, JUST O/B OF THE LBL 27.0. UPON REMOVAL OF DAMAGED SECTION OF SUPPORT ANGLE THE 2 80 WEB WAS FOUND TO HAVE MINOR SURFACE CORROSION. REMOVED MINOR SURFACE CORROSION AT 280 WEB PER: CRJ SRM 53-00-00. AP PLIED CORROSION PROTECTION PER: CRJ SRM 51-21-11. APPLIED FR7 PRIMER PER: CRJ SRM 51-25-06. REPAIRED FS 280 SUPPORT AN GLE, IAW REO 601R-53-11-136. 06/28/07 REQUIRES TOPCOAT TO FASTENERS AND CIC. 06/28/07 REPAIRED J-ANGLE ON THE PILOTS B ULKHEAD AT FS 280 LT BL 9.0, IAW EO 600-53-0091. SUPPLEMENTAL - SDR CLOSED 07/03/07. 2 L 7 2 4F RT A21EA 2007071300122 20070713 00122 NM 2007 7 13 USAA920070792 1 20070624 A 5315 141N5112 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 939UW 27303 BFM - MAJOR REPAIR - C-4 CHECK - NR 6000701, CORROSION ON CABIN FLOORBEAM, BS 365, RBL 20 - RBL 25, WL 208. REPAIRED CA BIN FLOORBEAM, BS 365, RBL 20 - RBL 25, WL 208 IAW USAIRWAYS TYPICAL REPAIR 53-15-01. 2 L 7 2 4F RT A2NM 2007071300124 20070713 00124 SO 2007 7 13 SIMA200719002 1 20070708 A 2611 SMOKE WARNING EMB 135 EMB135KL 3260302 SO CARGO BAY FALSE ACTIVATION A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 830AE 145615 BAGGAGE SMOKE INDICATION LIGHT ILLUMINATED INFLIGHT WITH NO AURAL WARNING, RETURNED TO LAW. POST INSPECTION REVEALED NO EVIDENCE OF SMOKE. PERFORMED OPERATIONAL CHECK OF SYSTEM IAW EMB AMM WITH NO DEFECTS, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300130 20070713 00130 NM 2007 7 13 SWAA073283 1 20070702 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED C3 CHECK, FOUND RT FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007071300132 20070713 00132 EA 2007 7 13 SIMA200719003 1 20070708 A 2710 C13045BA04 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA PITCH FEEL FAILED A SIMA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 21 500AE 8552 3316 10025 CAUTION PITCH FEEL MESSAGE, DECLARED EMERGENCY. REMOVED AND REPLACED SPOILER STABILIZER CONTROL UNIT IAW CRJ AMM 27-61- 05. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 2007071300144 20070713 00144 SO 2007 7 13 SIMA200719103 1 20070522 A 5347 13500412005 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 15926 5000 145224 LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 53 AND 55 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETUR NED AIRCRAFT TO SERVICE 2 L 7 2 4F RT T00011AT 2007071300150 20070713 00150 EA 2007 7 13 SWIA200718432 1 20070704 A 3350 CHARGER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 923SW EMERGENCY LIGHT OVER EXIT ROW INOP. REPLACED THE NR 2 AND NR 3 BATTERY CHARGERS AND DIODE ASSEMBLY IAW AMM 33-51-05. O PS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007071300151 20070713 00151 NM 2007 7 13 KCSA071200 1 20070703 A 3350 LIGHT BOEING 747 747122 1384872 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 716CK 19753 EMERGENCY LIGHT ABOVE UPPER DECK EXIT DOOR INOP. 2 L 7 4 4F A20WE 2007071300168 20070713 00168 NM 2007 7 13 HNAA0700138 1 20070509 A 5320 DOUBLER DHAV DHC8 DHC8102 2809003 NM FUSELAGE DEBONDED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 937HA 148 DOUBLER UNDER STR 28S IS DISBONDED IN FRAME BAYS X424 TO X434. 2 H 7 2 4T RT A13NM 2007071300170 20070713 00170 SO 2007 7 13 SWIA200718446 1 20070505 A 5310 FRAME EMB 120 EMB120 3260201 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 216SW 120285 FRAME 23 BETWEEN STRINGERS 20L AND 20R IS CORRODING OUTBOARD OF STRINGER 21L, DISCOVERED AT C-CHECK. COMPLIED WITH REPA IR OF FUSELAGE SKIN AT FRAME 23 BETWEEN STRINGERS 20L AND 20R PER EMBRAER APPROVED REPAIR #1C2007-120/03354. 2 L 7 2 4T RT A31SO 2007071300186 20070713 00186 EA 2007 7 13 COMA0760458 1 20070628 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 518CA 7816 FLIGHT 5286 - FLAP FAIL CAUTION AT 38 DEGREES ON SHORT FINAL. PERFORMED GO AROUND AND AIRCRAFT LANDED SAFELY. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007071300190 20070713 00190 NM 2007 7 13 SWAA073314 1 20070704 A 3350 101073 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 206WN 34011 R2 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT COVER PER MM. 2 L 7 2 4F RT A16WE 2007071300197 20070713 00197 NM 2007 7 13 SWAA073290 1 20070703 A 5330 6545777 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT LOWER LT SIDE. REPAIRED SKIN PER S WA EA. 2 L 7 2 4F RT A16WE 2007071300201 20070713 00201 NM 2007 7 13 SWAA073297 1 20070703 A 5311 6546596 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071300205 20070713 00205 NM 2007 7 13 SWAA073300 1 20070703 A 5313 6551698 STRINGER SPLICE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER S RM. 2 L 7 2 4F RT A16WE 2007071300207 20070713 00207 NM 2007 7 13 SWAA073316 1 20070704 A 2560 6567380 LENS BOEING 737 7377H4 1384404 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 765SW 29805 L1 DOOR EMERGENCY EVAC SLIDE VIEWING LENS LOOSE. SECURED SLIDE LENS PER MM. 2 L 7 2 4F RT A16WE 2007071300219 20070713 00219 NM 2007 7 13 2007UALA02359 1 20070629 A 5754 SLAT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT WING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 213UA 30219 RIGHT WING MOST OUTBOARD L/E SLAT 14 IS DAMAGED. [07-27-07] REMOVED NR 14 SLAT AND INSTALLED SERVICABLE SURFACE PER 27-81-15. ACCOMPLISHED TEST FLIGHT. AIRCRAFT TESTS OK & IS READY FOR SERVICE. SUSPECT SLAT IMPACTED BY GROUND EQUIP MENT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007071300241 20070713 00241 2007 7 13 SWAA073286 4 20070703 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071300242 20070713 00242 2007 7 13 SWAA073287 4 20070703 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071300254 20070713 00254 NM 2007 7 13 BB07049 1 20070705 A 3397 WIRE HARNESS BOEING 767 767201 1385125 NM CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 250AY 23902 MAINTENANCE FOUND FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE AT MID CABIN, RIGHT SIDE. FOUND WIRING DISCONNECTED. RE-CON NECTED WIRING, NO FURTHER FAULTS. 2 L 7 2 4F RT A1NM 2007071300267 20070713 00267 SO 2007 7 13 SIMA200719112 1 20070522 A 5347 14530658005 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 15926 5000 145224 RIGHT INBOARD SEAT TRACK BETWEEN FRAME 36 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETUR NED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300271 20070713 00271 NM 2007 7 13 2007UALA02364 1 20070701 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 SEATS 4A AFT & 58ABC EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY LAMPS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071300277 20070713 00277 NM 2007 7 13 2007UALA02370 1 20070702 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EMERGENCY EEL LIGHT INOP FWD OF LAV 102 BELOW CLOSET. [07-24-07] REPLACED LIGHT ASSY. OPS. CKS. NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071300294 20070713 00294 SO 2007 7 13 SIMA200719208 1 20070617 A 5347 14532606017 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 812AE 13442 5000 145531 LEFT AFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 47 AND 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300295 20070713 00295 SO 2007 7 13 SIMA200719201 1 20070603 A 5347 13500412003 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 15957 5000 145235 LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 53 AND 55. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300298 20070713 00298 SO 2007 7 13 SIMA200719213 1 20070621 A 5347 14532606017 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 811AE 13526 5000 145529 LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 47 AND 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300300 20070713 00300 NM 2007 7 13 2007UALA02380 1 20070629 A 4940 1HE49 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 APU WOULD NOT START. STARTED APU BY PULLING THE REMOTE FIRE INDICATION. [08-08-07] REPLACED APU FIRE SHUT DOWN SWITC H. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071300303 20070713 00303 EU 2007 7 13 2007UALA02383 1 20070703 A 3350 321431 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 407UA 456 EMERGENCY LIGHTS FAIL TEST PER 3 SVC. SHOWS BATTERY FWD LEFT. REPLACED FWD LEFT BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071300306 20070713 00306 EU 2007 7 13 2007UALA02386 1 20070704 A 5210 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 438UA 678 DOOR ASSIST BOTTLE AT DOOR 1L IS LOW - 1300 PSI. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072700017 20070727 00017 EU 2007 7 27 07FDEA02573 1 20070723 A 5347 60224577075T56 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 657FE 748 A 5 SQ INCH AREA OF CORROSION EXIST AT MDCC SEAT TRACK L-2 FRAME 42 REF. 53-10-16-06 IAW A300-600 AMM. REMOVED CORROSIO N IAW A300-600 SRM 51-74-10. MAT LOSS IS FOUND TO BE OUT LIMITS. REMOVED SEAT TRACK L-2 FR 40 THRU FR 45 IAW A300-600 SRM 51-40-21. FABRICATED SEAT TRACK IAW A300-600 SRM 53-15-16. REPROTECTED SEAT TRACK IAW A300-600 SRM 51-75-10. INST ALLED SEAT TRACK L-2 FR40-45 IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007071300307 20070713 00307 EU 2007 7 13 2007UALA02388 1 20070704 A 3350 321431 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 491UA 1741 FOUND EMERGENCY LIGHTING BATTERIES LOW ON CHARGE AT FWD LEFT AND MID LEFT. REPLACED BATTERY & PERFORMED SUCCESSFUL CIDS TEST. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071300308 20070713 00308 NM 2007 7 13 2007UALA02389 1 20070704 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 FLIGHT CANCELLED DUE TO FAILED EMERGENCY EXIT LIGHTS. [07-27-07] EMERGENCY LIGHT UNPLUGGED AT 27AB, TESTED EMERG L IGHT, 27AB SHOWS OK 2 L 7 2 4F 4 F RT A1NM E24NE 2007071300309 20070713 00309 NM 2007 7 13 2007UALA02390 1 20070703 A 5230 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 FWD CARGO DOOR S/N 1783 EXTERNAL SKIN HAS LARGE AREA OF DAMAGE CREASED 9 INCHES FROM FWD TO 9 INCHES FROM AFT AND 18 INC HES FROM TOP TO 27 INCHES FROM TOP. REMOVED DAMAGE AREA. REPLACED WITH NEW CARGO DOOR SKIN. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071300310 20070713 00310 NM 2007 7 13 2007UALA02391 1 20070703 A 5230 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 AFT CARGO HAS DENT 9 INCHES FROM UPPER AFT CORNER AND 8 INCHES DOWN FROM TOP. REMOVED DAMAGE. INSTALLED DOUBLER REPAIR . 2 L 7 2 4F 4 F RT A16WE E21EU 2007071300314 20070713 00314 NM 2007 7 13 2007UALA02395 1 20070704 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY LIGHTS INOPERATIVE AT 6AB FWD & 41 HJK. REPLACED LIGHT ASSEMBLIES. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071300315 20070713 00315 SO 2007 7 13 SIMA200719212 1 20070621 A 5347 14532506017 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 811AE 13526 5000 145529 RIGHT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 47 AND 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300316 20070713 00316 SO 2007 7 13 SIMA200719005 1 20070708 A 2751 3633501003 POSITION SENSOR EMB 135 EMB135LR 3260305 SO ZONE 200 FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 721HS 15777 145283 "SUP" FLAPS SELECTED TO THE UP POSITION FOLLOWED BY FLAP FAIL AND SPS ADVANCE MESSAGE, FLAPS STUCK AT 9 DEGREES, RETURNE D TO DFW. REMOVED AND REPLACED LEFT FLAP SPEED SENSOR AND FLAP BRAKE IAW EMB AMM. OPERATIONAL CHECK GOOD. RETURNED AI RCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300318 20070713 00318 NM 2007 7 13 HALA0700279 1 20070708 A 3810 288239 COMPRESSOR BOEING 767 76733A 1385209 NM POTABLE WATER OVERHEATED A HALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 13 582HA 20232 20232 28139 F/A REPORTED SMELLING AN ELECTRICAL ODOR IN THE AFT RIGHT CABIN LAST 5 ROWS ON THE RIGHT SIDE, ALL GALLEY EQUIPMENT WAS OFF. INSP CABIN AREA AROUND SEATS 39-43 H/J INCLUDING UNDER SEATS, OVERHEAD BINS, AFT GALLEY AND AFT LAVS CHECKED FWD, AFT AND BULK CARGO COMPTS. NO UNUSUAL ODOR OR FAULTS NOTED, NO ABNORMAL COCKPIT INDICATION. OK TO CONTINUE. 2 L 7 2 4F RT A1NM 2007071300319 20070713 00319 GL 2007 7 13 HEEA116033 2 20070619 A 7321 0164548300 FUEL CONTROL SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL ENGINE MALFUNCTIONED B HEEA O OTHER J WARNING INDICATION CR CRUISE 1 SW 03 1545X 5599 760050 DURING CRUISE FLIGHT NR 2 ENGINE TORQUE UNCOMMANDED WENT TO 105 AND N1 WENT 100. BROUGHT ENGINE UNDER CONTROL WITH THRO TTLE. 5 MINUTES AFTER THAT THE NR 1 ENGINE OIL PRESSURE GAUGE WENT TO ZERO WITH NO OTHER INDICATIONS. IT STAYED THERE 5 MINUTES AND CAME BACK UP NORMAL. MAINTENANCE REPLACED FUEL CONTROL. 1 G 7 2 3U 3 U H1NE E1GL 2007071300321 20070713 00321 NM 2007 7 13 2007UALA02396 1 20070704 A 3350 STRIP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 BOTH CROSSAISLE EEL STRIPS AT DOOR 4L ARE FAULTY. [07-24-07] REPLACED CROSS AISLE EMERGENCY LAMP. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071300322 20070713 00322 NM 2007 7 13 2007UALA02397 1 20070703 A 3040 THERMOSTAT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE R3 WINDOW LOOSE A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 118UA 28811 WINDOW 3R HEAT FAIL MESSAGE PRESENT IN FAULT HISTORY FOR LAST SEVERAL LEGS. [07-27-07] FOUND NR 3R WINDOW THERMOSTA T LOOSE. RESECURED AND CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071300323 20070713 00323 NM 2007 7 13 2007UALA02399 1 20070704 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 671UA 30026 EEL LIGHT AT SEAT 30AB IS INOPERATIVE. RELAMPED EMERGENCY LIGHT CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071300324 20070713 00324 NM 2007 7 13 2007UALA02400 1 20070704 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 671UA 30026 EEL LIGHTING INOP SEATS 26HJ THROUGH 36HJ. [07-27-07] SECURED EEL CABLE'S CONNECTOR AT 35H, OP CK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071300326 20070713 00326 NM 2007 7 13 2007UALA02402 1 20070703 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY LIGHTS INOP, ALL 4 RIGHT OVERWING LIGHT ASSEMBLIES. [07-27-07] REPLACED 2 EA FUSES IN EPSU, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071300327 20070713 00327 NM 2007 7 13 2007UALA02403 1 20070703 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY LIGHT INOP, LEFT OVERWING 2ND FROM AFT 1 BULB. [07-27-07] REPLACED LAMPS. CHKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071300328 20070713 00328 NM 2007 7 13 2007UALA02404 1 20070703 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY LIGHT INOP AT TOP OF STAIRS. [07-24-07] RELAMPED. OPS. NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071300330 20070713 00330 NM 2007 7 13 2007UALA02406 1 20070703 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 WALL EEL INOP, DOORS 1R & 5L CROSS AISLE. [07-24-07] SECURED CONNECTOR. OPS. CKS. NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071300333 20070713 00333 NM 2007 7 13 2007UALA02409 1 20070704 A 2121 COOLING FAN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN DIRTY A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 792UA 26934 EXPERIENCED ODOR OF SMOKE. SOURCE DETERMINED TO BE FAILED COOLING FAN. CONTINUED TO DESTINATION. [07-27-07] REPL ACED EQUIPMENT COOLING FAN AND RESTORED P210 ELMS CARD. OPS CHECKED NORMAL. SUSPECT DIRT ACCUMULATED IN STATOR & SHORTE D THE MOTOR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007071300334 20070713 00334 NM 2007 7 13 2007UALA02410 1 20070704 A 2425 IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 MALFUNCTIONED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 512UA 24809 EICAS MESSAGE LEFT GENERATOR DRIVE DISPLAYED. [08-08-07] ON CLIMB OUT CREW GOT LEFT GENERATOR DRIVE INDICATION. CRE W DISCONNECTED LEFT GENERATOR DRIVE AND STARTED APU. RAN FUEL BURN FOR APU ENROUTE. REPLACED NR 1 IDG AND ENG FUEL-OIL EXCHANGER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072700021 20070727 00021 NM 2007 7 27 HALA0700297 1 20070721 A 3244 3910797513 TIRE BOEING 717 717200 1383700 NM NR 3 FAILED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 478HA 55123 AFTER LANDING IN HNL, RAMP NOTICED THE NR 3 MAIN TIRE CAME APART AND WENT THROUGH THE NR 2 ENG. REPLACED NR 3 TIRE PER AMM32-41-01. PERFORMED FOD INSP PER 717 AMM TASK 72-00-01 FROM 2A THR 2D (2)(A)(2). LP NR 2 AND NR 3 STAGE BLADES NO I NDICATION OF DAMAGES (NOTED). 2 L 7 2 4F TR A6WE 2007071300335 20070713 00335 NM 2007 7 13 QXEA200701080 1 20070629 A 7930 D2887355C VALVE BOMBDR DHC8 DHC8402 1390042 NM NR 1 ENGINE MALFUNCTIONED A QXEA O OTHER M OVER TEMP CL CLIMB 1 NM 09 406QX 4048 SEA FLIGHT NR 2318: NR 1 ENGINE OIL TEMP IN RED AT 110 DEGREES C ON CLIMB THROUGH 8000-9000 FT. CLOSED NR 1 ENGINE INTA KE BYPASS DOOR PER CHECKLIST. NR 1 OIL TEMP DECREASED INTO GREEN ARC TEMPS. REMAINED IN RED ARC 3-4 MINUTES. MAINTENA NCE REMOVED AND REPLACED THE NR 1 ENGINE BYPASS VALVE AND PERFORMED LEAK AND OPS CHECK ON NR 1 ENGINE OIL TEMP SYSTEM. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071300336 20070713 00336 NM 2007 7 13 QXEA200701081 1 20070703 A 3150 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 411QX 4055 SEA FLIGHT NR 2292: FLAP POWER CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE CLEARED FAULT AND TE STED IAW Q400 FIM TASK 27-50-00-810-802. CHECKS GOOD WITH NO FURTHER FAULTS. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071300337 20070713 00337 NM 2007 7 13 QXEA200701082 1 20070703 A 2130 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN A QXEA A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CR CRUISE 1 NM 09 428QX 4160 SEA - FCA FLIGHT NR 2282: FAULT LIGHT ILLUMINATED ON CABIN ALT CONT. A/C WOULD NOT PRESSURIZE IN AUTO MODE. MANUAL MOD E PRESSURIZED NORMALLY. CDS FAULT 'AFT OUTFLOW ONLINE FAIL' MESSAGE. AIRCRAFT WAS DIVERTED TO GEG. MAINTENANCE C/W TE ST OF PRESSURIZATION CONTROL SYSTEM IAW AMM 21-31-00-720-801. FUNCTIONAL CHECK GOOD WITH NO FAULT CODES IN CDS. NO PAR TS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071300338 20070713 00338 NM 2007 7 13 QXEA200701047 1 20070620 A 5340 STRINGER CLIP DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 - PDX CABIN UNDER FLOOR CENTER AT FRAME X488.50 AND STRINGER 32R THERE IS CORROSION ON THE STRINGER CLIP SPLICE. REP AIRED IAW DHC8 SRM 51-20-11, 51-20-26 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007071300339 20070713 00339 NM 2007 7 13 QXEA200701048 1 20070620 A 5320 INTERCOSTAL DHAV DHC8 DHC8202 2809007 NM STRINGER 25L CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 - PDX CORROSION AT OUTBOARD SIDE OF LEFT INTERCOSTAL (LEFT STRINGER 25) AROUND PNEUMATIC TUB FITTING FOR MAIN CABIN D OOR SEAL, JUST INBOARD OF MAIN CABIN DOOR LAYSHAFT FORWARD SECTION. REPAIRED IAW DHC-8-200 SRM 51-20-26 AND 51-20-36. 2 H 7 2 4T RT A13NM 2007071300341 20070713 00341 NM 2007 7 13 QXEA200701050 1 20070620 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 - PDX CORROSION AT FRAME FORWARD FLANGE APPROXIMATELY X545.00 JUST OUTBOARD OF RIGHT STRINGER 31. REPAIRED IAW DHC-8 -200 SRM 51-20-11, 51-20-16, 51-00-01 AND SRM 51-20-51. 2 H 7 2 4T RT A13NM 2007071300342 20070713 00342 NM 2007 7 13 QXEA200701051 1 20070626 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - CORROSION AT LOWER FLANGE OF FRAME X445.50 BETWEEN RIGHT STRINGER 30 AND 31. REPAIRED IAW DHC-8-200 SRM 51-20- 11, 51-40-11 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2007071300343 20070713 00343 NM 2007 7 13 QXEA200701043 1 20070620 A 5313 STRINGER DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - CORROSION AT TOP OF LEFT STRINGER 25 JUST AFT OF FRAME X355.950. REPAIRED IAW SRM 51-20-11 AND 51-20-26. 2 H 7 2 4T RT A13NM 2007071300345 20070713 00345 NM 2007 7 13 QXEA200701045 1 20070620 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - CABIN UNDER FLOOR CENTER AT FRAME X510.00 AND BETWEEN STRINGER 31R NAD 32R THERE IS CORROSION ON THE FRAME CAST ELLATION. REPAIRED IAW DHC-8 SRM 51-40-11, 51-20-36 AND SRM 51-20-51. 2 H 7 2 4T RT A13NM 2007071300346 20070713 00346 NM 2007 7 13 QXEA200701046 1 20070620 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - CABIN UNDER FLOOR CENTER AT FRAME X531.50 AND STRINGER 32R THERE IS CORROSION ON THE STRINGER ATTACH CLIP SPLIC E. REPAIRED IAW SRM 51-40-11, 51-20-36 AND 51-20-51. 2 H 7 2 4T RT A13NM 2007071300347 20070713 00347 NM 2007 7 13 QXEA200701052 1 20070625 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 374PH 528 C4 PDX - CORROSION AT INNER FUSELAGE SKIN JOINT STRAP AROUND RIVETS TAILS JUST AFT OF FRAME X424.00 AND INBOARD OF LEFT HAND STRINGER 24. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-40-11 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2007071300348 20070713 00348 NM 2007 7 13 TSAA0752039 1 20070629 A 5270 189915 PROXIMITY SENSOR BOEING 737 7372X6C 1384552 NM PAX DOOR DIRTY A TSAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 13 816AL 23122 FLIGHT 940 HNL-KOA - ON TAKEOFF ROLL, CREW NOTED THE DOOR ANNUNCIATOR LIGHT ILLUMINATED AND ABORTED THE TAKEOFF AT 110 K NOTS INDICATED AIRSPEED. CREW RETURNED TO THE CARGO RAMP WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED AND OPS CHECKED THE FORWARD ENTRY DOOR PROXIMITY SENSOR PER AMM 52-71-0 PAGE 501. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007071300352 20070713 00352 NM 2007 7 13 07FDEA02377 1 20070705 A 5322 65561151 SHEAR TIE BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD PIT BILGE BODY FRAME SHEAR TIE IS CRACKED/BROKEN BS 720C, STR 27R-28R, WL 148. REPAIRED SHEAR TIE FLOOR SUPPORT AND SHIMS REFERENCING SRM 53-10-4 FIG 11, 51-10- 2, AND 53-10-2, AND BOEING DRAWING 69-43676. TREATED AND PRIMED ALL REPAI R PARTS REF SRM 51-10-2. 2 L 7 3 4F RT A3WE 2007071300353 20070713 00353 NM 2007 7 13 07FDEA02378 1 20070705 A 3260 NONE BOEING 727 727233 138408A NM MLG DOOR UNKNOWN A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 274FE 22039 ON TAKEOFF, RT MAIN GEAR DOOR LIGHT REMAINED ILLUMINATED. COMPLIED WITH QRH, RECYCLED GEAR AND LIGHT EXTINGUISHED. CON TINUED FLIGHT. INSPECTED GEAR DOOR SWITCHES CK GOOD, CYCLE DOOR OPEN CLOSED SEVERAL TIME. OPS CHECKS NORMAL IAW AMM 32 -62-011-5. 2 L 7 3 4F RT A3WE 2007071300354 20070713 00354 NM 2007 7 13 07FDEA02379 1 20070706 A 7810 652784613 LINER BOEING 727 727227 1384078 NM HUSH KIT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 NR 1 ENGINE HUSH KIT INNER LINER DISBONDED AND CRACKED AT 9 O'CLOCK POS. VERIFIED MATERIAL (INCONEL) REF. 78 -38-41 PR EP FOR WELD REF 78-38-41, WELD WITH AMS 5837, A29984 INSPECT REF 78-38-41. 2 L 7 3 4F A3WE 2007071300356 20070713 00356 EU 2007 7 13 07FDEA02381 1 20070706 A 5315 A53970091 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 749FD 536 OLD TOP CAP BEAM REPAIR , C62, LT, ARE NOT CONFORM TO SRM. REPAIR RENEWED IAW SRM 53-10-15 FIG 208. 2 L 7 2 4F RT A35EU 2007071300362 20070713 00362 NM 2007 7 13 SWAA073328 1 20070705 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED BS 520, STR 28R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007071300367 20070713 00367 NE 2007 7 13 HEEA116164 1 20070630 A 2435 7655009006108 STARTER GEN SKRSKY S76 S76C 8143008 NE NR 2 FAILED B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 781P * 760630 NR 2 ENGINE GENERATOR FAILED IN FLIGHT. MAINTENANCE REPLACED THE STARTER GENERATOR. 1 G 7 2 3U NC H1NE 2007071300371 20070713 00371 EU 2007 7 13 U0GA116272 1 20070710 A 6220 350A31191600 STARFLEX AEROSP AS355 AS355* EU TMECA ARRIEL ARRIEL1 60030 NE MAIN ROTOR SHEARED E U0GA O OTHER O OTHER NR NOT REPORTED 1 SW 03 147BH 482 1273 STARFLEX BLUE ARM SHEARED AT APPROXIMATELY 14 MM FROM OB END. AIRCRAFT WAS AT 100 NR FLAT PITCH WHEN THIS OCCURRED. ST ARFLEX WAS REMOVED FOR FURTHER INSPECTION. 1 G 7 2 3U 3 U H11EU E19EU 2007071300373 20070713 00373 NM 2007 7 13 F3LA200700164 1 20070627 A 5320 TRANSITION PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED HOLES IN AFT CARGO COMPARTMENT FWD RT LOWER TRANSITION PANEL 152WG. REPLACED TRAN SITION PANEL 152WG IAW AMM 53-42-14-400-001. 2 L 7 2 4F RT A28NM 2007071300375 20070713 00375 NM 2007 7 13 F3LA200700166 1 20070627 A 5320 TRANSITION PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT TRANSITION PANEL 161BF PUNCTURED ON TOP SKIN. REPLACED TRAN SITION PANEL 161BF IAW AMM 53-42-14-400-001. 2 L 7 2 4F RT A28NM 2007071300376 20070713 00376 WP 2007 7 13 UPS07850123 1 20070623 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP FS 1677 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 DOUBLE DRILLED HOLES IN WEB AT LWR AFT CORNER OF L2 DOOR JAMB STA 1667. TRIMMED OUT DAMAGED AREA OF WEB AND FRAME SEGMENT OF L2 DOOR LWR AFT CORNER DOOR JAMB IAW DWG DC8-53A-011. FABRICATED AND INSTALLED "J" ANGLE DOUBL ER AT L2 DOOR LWR AFT DOOR JAMB CORNER IAW SRM 53-02- 00 FIG 23 AND DWG DC8-53A-011. 2 L 7 4 4F RT 4A25 2007071300377 20070713 00377 NM 2007 7 13 F3LA200700167 1 20070627 A 5321 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR PANEL 151CE DAMAGED. REPLACED FLOOR PANEL 151CE IAW A MM 53-42-11-400-001. 2 L 7 2 4F RT A28NM 2007071300381 20070713 00381 NM 2007 7 13 UPS07M50098 1 20070506 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C EMPENNAGE/RT HORIZONTAL STABILIZER BARREL NUT NR 15 RT FOUND BORE C CORRODED. CORROSION AT BARREL NUT BORE REMOVED, BOTTOM SURFACE REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BOR E BLEND OUT, BOTTOM PERIPHERY RADIUSED SMOOTHENED AND PROTECTED. REPAIR SLEEVE BUSHING FAB AND PROTECTED, PR1422 B1/2 S EALANT APPLIED. REWORK AREA PAINTED. 2 L 7 3 4F RT A22WE 2007071300382 20070713 00382 NM 2007 7 13 UPS07M50099 1 20070507 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C EMPENNAGE/LT HORIZONTAL STABILIZER BARREL NUT NR 9 LT FOUND BORE CORRODED. CORROSION AT BARREL NUT BO RE REMOVED, BOTTOM REMAINING BLENDED OUT EXCEEDS LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTTOM PERIPHERY RADIUSED SMOOTHENED AND PROTECTED. REPAIR SLEEVE BUSHING FAB AND PROTECTED. PR144 B1/2 SEALANT AP PLIED AT BLEND OUT VOIDS AND REPAIR SLEEVE BUSHING INSTALLED. REWORK AREA PAINTED. 2 L 7 3 4F RT A22WE 2007071300383 20070713 00383 NM 2007 7 13 UPS07M50100 1 20070507 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C EMPENNAGE/LT HORIZONTAL STABILIZER BARREL NUT NR 15 LT FOUND BORE CORRODED. CORROSION AT BARREL NUT B ORE REMOVED, BOTTOM REMAINING BLENDED OUT EXCEEDS LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUTS AND BOTTOM PERIPHERY RADIUSED SMOOTHENED AND PROTECTED. REPAIR SLEEVE BUSHING FAB AND PROTECTED PR1422 B1/2 SEALANT APPLIE D AT BLEND OUT VOIDS AND REPAIR SLEEVE BUSHING INSTALLED. REWORK AREA PAINTED. 2 L 7 3 4F RT A22WE 2007071300385 20070713 00385 NM 2007 7 13 UPS07M50104 1 20070510 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C RT HORIZONTAL STABILIZER BARREL NUT NR 20 FOUND BORE CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTTOM PE RIPHERY RADIUSED SMOOTHENED AND PROTECTED. REPAIR SLEEVE BUSHING FAB AND PROTECTED. PR1422 B1/2 SEALANT APPLIED AT BLE ND OUT VOID AND REPAIR SLEEVE BUSHING INSTALLED. REWORK AREA PAINTED. 2 L 7 3 4F RT A22WE 2007071300386 20070713 00386 NM 2007 7 13 UPS07M50105 1 20070511 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C LT HORIZONTAL STABILIZER BARREL NUT HOLE NR 36 FOUND CORRODED. ACCESS CUT AT UPPER TORQUE BOX WEB. C ORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEED LIMITS. DVI C/OUT FOUND NO CORROSION. REPAIR SLE EVE BUSHING, DOUBLER AND FILLERS FAB AND PROTECTED AND INSTALLED. PR1422 B1/2 SEALANT APPLIED AT BLEND OUT VOIDS. REWO RK AREA PAINTED. 2 L 7 3 4F RT A22WE 2007071300387 20070713 00387 NM 2007 7 13 UPS07M50106 1 20070521 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C RT HORIZONTAL STABILIZER BARREL NUT HOLE NR 19 BORE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMO VED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTT OM PERIPHERY RADIUSED SMOOTHENED AND PROTECTED. REPAIR SLEEVE BUSHING FAB AND PROTECTED. PR1422 B1/2 SEALANT APPLIED A T BLEND OUT VOID AND REPAIR SLEEVE BUSHING INSTALLED. REWORK AREA PAINTED. 2 L 7 3 4F RT A22WE 2007071300391 20070713 00391 NM 2007 7 13 UPS07M50110 1 20070510 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C LT HORIZONTAL STABILIZER BARREL NUT NR 30 FOUND BORE CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS AND BOTTOM P ERIPHERY RADIUSED SMOOTHENED AND PROTECTED. REPAIR SLEEVE BUSHING FAB AND PROTECTED, PR1422 B1/2 SEALANT APPLIED AT BLE ND OUT VOIDS AND REPAIR SLEEVE BUSHING INSTALLED. REWORK AREA PAINTED. 2 L 7 3 4F RT A22WE 2007071300393 20070713 00393 NM 2007 7 13 UPS07M50112 1 20070515 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C LT HORIZONTAL STABILIZER BARREL NUT HOLE NR 23 BORE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMO VED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTT OM PERIPHERY RADIUSED SMOOTHENED AND PROTECTED. REPAIR SLEEVE BUSHING FAB AND PROTECTED, PR1422 B1/2 SEALANT APPLIED AT BLEND OUT VOID AND REPAIR SLEEVE BUSHING INSTALLED. REWORK AREA PAINTED. 2 L 7 3 4F RT A22WE 2007071300395 20070713 00395 NM 2007 7 13 UPS07M50114 1 20070528 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C LT HORIZONTAL STABILIZER BARREL NUT HOLE NR 22 BORE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMO VED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS AND BOT TOM PERIPHERY RADIUSED SMOOTHENED AND PROTECTED. REPAIR SLEEVE BUSHING FAB AND PROTECTED. PR1422 B1/2 SEALANT APPLIED AT BLEND OUT VOID AND REPAIR SLEEVE BUSHING INSTALLED. REWORK AREA PAINTED. 2 L 7 3 4F RT A22WE 2007071300400 20070713 00400 NM 2007 7 13 SWAA073346 1 20070705 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 808, BL 0. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007071300401 20070713 00401 NM 2007 7 13 SWAA073334 1 20070705 A 5310 6545834 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED SERVICE CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 295, RBL 60, WL 208. REMOVED AND REPLACED WEB PER S RM. 2 L 7 2 4F RT A16WE 2007071300402 20070713 00402 NM 2007 7 13 SWAA073338 1 20070705 A 5311 6546548 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071300403 20070713 00403 NM 2007 7 13 SWAA073339 1 20070705 A 5311 6546555 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071300404 20070713 00404 NM 2007 7 13 SWAA073340 1 20070705 A 5311 6546558 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071300406 20070713 00406 NM 2007 7 13 SWAA073337 1 20070705 A 5311 6546596 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071300407 20070713 00407 NM 2007 7 13 SWAA073345 1 20070705 A 5311 65C229081 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071300411 20070713 00411 NM 2007 7 13 SWAA073333 1 20070705 A 2711 6943491 ROD END BOEING 737 7373H4 1384600 NM RT MLG WW CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED SERVICE CHECK, FOUND AILERON ROD END CORRODED IN RT MLG W/W. REMOVED AND REPLACED ROD END PER MM. 2 L 7 2 4F RT A16WE 2007071300413 20070713 00413 NM 2007 7 13 SWAA073342 1 20070705 A 2560 PL22300LH GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 790SW 30604 DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 9 ABC. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007071300414 20070713 00414 NM 2007 7 13 SWAA073332 1 20070705 A 3397 W146006220 GROUND WIRE BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED GROUND WIRE W1460-062-20 PER WDM. 2 L 7 2 4F RT A16WE 2007071300415 20070713 00415 NM 2007 7 13 SWAA073341 1 20070705 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 409WN 27896 DURING SCHEDULED MV3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007071300417 20070713 00417 2007 7 13 SWAA073343 4 20070705 A 2565 LENS BOEING 737 7377H4 1384404 NM EVAC SLIDE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 790SW 0246A 30604 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE LENS CRACKED. REMOVED AND REPLACED EVAC S LIDE PER MM. 2 L 7 2 4F RT A16WE 2007071300418 20070713 00418 NM 2007 7 13 SWAA073329 1 20070705 A 2730 6545187 TORQUE TUBE BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TORQUE TUBE, HORN BEARING AND BOLTS PER MM. 2 L 7 2 4F RT A16WE 2007071300419 20070713 00419 NM 2007 7 13 SWAA073330 1 20070705 A 2730 6545187 TORQUE TUBE BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 10Y CHECK, RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TORQUE TUBE AND HORN BEAR ING PER MM. 2 L 7 2 4F RT A16WE 2007071600001 20070716 00001 EU 2007 7 16 CPCP20070050 1 20070511 A 5320 FLOOR SUPPORT AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 260AE 263 LT FLOOR SUPPORT BETWEEN FRAME 39 AND FRAME 40 IS CORRODED. LT FLOOR SUPPORT BETWEEN FRAME 39 AND FRAME 40 REPLACED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007071600004 20070716 00004 EU 2007 7 16 CPCP20070053 1 20070511 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 260AE 263 FOUND FLOORBEAM AT FRAME 40 IS CORRODED. NEW FLOORBEAM INSTALLED IAW SRM 51-25-01 AND 51-25-04. 2 H 7 2 4T RT A53EU 2007071600005 20070716 00005 EU 2007 7 16 CPCP20070054 1 20070511 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 260AE 263 FOUND FLOORBEAM AT FRAME 36 IS CORRODED. FLOORBEAM AT 36 REPLACED AS PER SRM 51-25-01 AND 51-25-04. 2 H 7 2 4T RT A53EU 2007071600006 20070716 00006 EU 2007 7 16 CPCP20070055 1 20070514 A 5230 LATCH AEROSP ATR72 ATR72212 8680945 EU CARGO DOOR CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 260AE 263 CARGO DOOR ENTRY CORROSION FOUND NEAR AFT DOOR LATCH FITTING. CARGO DOOR ENTRY REPAIRED AS PER SRM 53-00-00 FIG 402. 2 H 7 2 4T RT A53EU 2007071100256 20070711 00256 NM 2007 7 11 2007UALA02218 1 20070624 A 2600 SQUIB BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2 ENGINE NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 NR 2 ENG, A CHANNEL SQUIB TEST FAILED. [07-20-07] NR 2 ENG, PRESS TO TEST IS OK, B CHANNEL TEST OK. NOTE: THIS IS A RECURRENT MAL FUNCTION. REPLACED CHANNEL A SQUIP. PERFORMED TEST. PASSED, LIGHTS WORKING. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071100261 20070711 00261 EU 2007 7 11 CPCP20070048 1 20070511 A 5320 THRESHOLD AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 260AE 263 LT THRESHOLD BETWEEN FRAME 36 AND FRAME 39 IS CORRODED. LT THRESHOLD BETWEEN FRAME 36 AND FRAME 39 REPLACED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007071100262 20070711 00262 EU 2007 7 11 CPCP20070049 1 20070511 A 5320 THRESHOLD AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 260AE 263 RT THRESHOLD PLATE AT FRAME 36 IS CORRODED. RT THRESHOLD PLATE AT FRAME 36 REPLACED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007071100269 20070711 00269 EU 2007 7 11 AWXA200700785 1 20070620 A 5320 D53475758000 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 667AW 1710 SAL - MAJOR REPAIR - BC-4 CHECK - NR# 5948226, 5948227, 594828, 5948229 AND 5948180, CORROSION ON BULK CARGO DOOR CUT OU T LOWER SILL, FR 60 + 11" AT -Y660, FR 61 AT -Y650, FR 61 + 10" AT -Y630, FR 61 + 19" AT -Y630 AND FR 62 + 2" AT -Y960. REPAIRED BULK CARGO DOOR CUT OUT LOWER SILL, FR 60 + 11" AT -Y660, FR 61 AT-Y650, FR 61 + 10" AT -Y630, FR 61 + 19" AT -Y630 AND FR 62 + 2" AT -Y960 IAW A320 SRM 53-41-49. 2 L 7 2 4F RT A28NM 2007071100291 20070711 00291 NM 2007 7 11 070131 1 20070624 A 3350 408822101 BATTERY PACK DOUG MD80 MD83 3023681 NM CABIN DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 874GA 49643 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT 2007071100301 20070711 00301 NM 2007 7 11 SWAA073237 1 20070628 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071100303 20070711 00303 NM 2007 7 11 SWAA073241 1 20070628 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071100310 20070711 00310 NM 2007 7 11 SWAA073258 1 20070628 A 5754 65C26602 SLAT BOEING 737 7377H4 1384404 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 406WN 27894 DURING SCHEDULED 6Y CHECK, FOUND LT WING NR 2 L/E SLAT CRACKED. R&R SLAT PER MM. 2 L 7 2 4F RT A16WE 2007071100311 20070711 00311 NM 2007 7 11 SWAA073246 1 20070628 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071100313 20070711 00313 2007 7 11 SWAA073224 4 20070626 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071100327 20070711 00327 NM 2007 7 11 2007UALA02174 1 20070621 A 3350 1619 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 309UA 23670 LEFT OVERWING EXTERIOR EMEGENCY LIGHT INOP. RELAMPED OPS CHK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071100333 20070711 00333 NM 2007 7 11 2007UALA02203 1 20070623 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 573UA 26685 OUTSIDE EMERGENCY LIGHTS INOP DOORS 2L, 3L, 3R, 1R. RELAMPED LIGHTS. OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071100336 20070711 00336 NM 2007 7 11 2007UALA02211 1 20070623 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 EXIT PATH LIGHTS OUT AT SEATS 2B AND 5B. REPLACED BOTH LAMP ASSEMBLIES. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071100350 20070711 00350 2007 7 11 2007UALA02350 4 20070701 A 2565 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 518UA 24871 R EMERGENCY ESCAPE SLIDE SQUIB LIGHT FAILED TO ILLUMINATE. [08-08-07] SECURED LOOSE LAMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071200006 20070712 00006 NM 2007 7 12 USAA070493 1 20070628 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 294 S11L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND CRACK BS 294.5, S-11L. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-40-03, BOEING DWG 65-17684, DEFECT SIZE: 1". 2 L 7 2 4F RT A16WE 2007071200007 20070712 00007 NM 2007 7 12 USAA070494 1 20070628 A 5340 STRINGER CLIP BOEING 737 737401 1384701 NM BS 344 S11R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND STA 344 STRINGER 11R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-02, DEFECT SIZE: 1/2". 2 L 7 2 4F RT A16WE 2007071200020 20070712 00020 NM 2007 7 12 USAA070505 1 20070629 A 5320 SUPPORT ANGLE BOEING 737 737401 1384701 NM CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 TWO NUTS CORRODED ON FASTENERS THRU SKIN SUPPORT ANGLE DOOR CABLE TENSIONER. REMOVED AND REPLACED FASTENERS, NUTS AND W ASHERS PER STANDARD PRACTICE; CORROSION TASK C53-202-01; LEVEL 2, DEFECT SIZE: .250" BY .175". 2 L 7 2 4F RT A16WE 2007071200022 20070712 00022 NM 2007 7 12 USAA070498 1 20070629 A 5230 6546921132XE SKIN BOEING 737 737401 1384701 NM FWD CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND FWD CARGO DOOR SKIN AT UPPER AFT CORNER OF DOOR HANDLE CUTOUT. CUT OUT DAMAGE AND INSTALLED DOUBLERS PER EA 98744 , DEFECT SIZE: 3/8". 2 L 7 2 4F RT A16WE 2007071200026 20070712 00026 NM 2007 7 12 USAA070511 1 20070629 A 5320 65C340597 INTERCOSTAL BOEING 737 737401 1384701 NM BS 947-967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND RBL 17, BETWEEN BS 947 AND 967, MULTIPLE AREAS OF FLOORBOARD ATTACH CLIPNUT. REMOVED AND REPLACED WITH IDENTICAL PART PER SRM 51-10-02; CORROSION TASK C53-107-02, DEFECT SIZE: 1.250" BY 1.250". 2 L 7 2 4F RT A16WE 2007071200032 20070712 00032 SO 2007 7 12 SIMA200718402 1 20070630 A 3350 78241 INVERTER EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHTS FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 735TS 14299 145386 LEFT AND RIGHT EMERGENCY DOOR, LOWER EXIT LIGHTS EMERGENCY EXIT FLOOR LIGHTING INOPERATIVE. REMOVED AND REPLACED NR 5 I NVERTER IAW EMB AMM. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071200033 20070712 00033 NM 2007 7 12 AALA20071165 1 20070625 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 919AN 29520 DFW - EMERGENCY EXIT IDENTIFIER LIGHT AT RIGHT AFT CABIN DOOR L1191 HAS BROKEN BASE. REPLACED EMERGENCY EXIT LIGHT ASSE MBLY L1191 FOR EMERGENCY LIGHT AT RIGHT AFT CABIN DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007071200044 20070712 00044 NM 2007 7 12 AALA20071160 1 20070625 A 3350 POWER SUPPLY BOEING 737 737823 13844BZ NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 937AN 30082 MIA - EMERGENCY LIGHTS FROM SEAT ROWS 22 TO AFT OF CABIN INOPERATIVE. RECHARGED POWER SUPPLY FOR EMERGENCY LIGHTS FROM SEAT ROWS 22 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007071200047 20070712 00047 NM 2007 7 12 AALA20071172 1 20070625 A 3350 SHROUD BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 919AN 29520 DFW - EMERGENCY LIGHT AT SEAT 16D HAS BROKEN SHROUD. REPLACED SHROUD EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007071200053 20070712 00053 SO 2007 7 12 SWIA200718409 1 20070628 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DISCONNECTED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 233SW 120307 FLT 5792 - EMERGENCY "EXIT" SIGN ABOVE ROW 9 DOES NOT ILLUMINATE RECONNECTED WIRE ON EXIT SIGN. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007071200054 20070712 00054 EA 2007 7 12 SWIA200718410 1 20070630 A 3520 OXYGEN MASK CNDAIR CL600 CL6002C10 1390015 EA LAVATORY UNWANTED DEPLOY A SWIA G O2 MASK DEPLOYED O OTHER CR CRUISE 1 NM 07 766SK 10232 FLT 5943 - O2 MASK IN LAV DEPLOYED INFLIGHT. INSPECTED AND STOWED O2 MASK ASSEMBLY. 2 L 7 2 4F RT A21EA 2007071200056 20070712 00056 EA 2007 7 12 SWIA200718412 1 20070628 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 954SW 7815 FLT 5853 - EMERGENCY LIGHTS INOP. REPLACED NR 1, NR 2, NR 3 AND NR 4 EMERGENCY LIGHT BATTERY PACKS IAW AMM 33-51-04. O PS CHECK GOOD, P/N 1 - AD-2013-1A, S/N OFF - 50465, P/N 2 - AD-2013-1A, S/N OFF 66819, P/N 3 - AD-2013-1A, S/N OFF - 747 49, P/N 4 - AD-2013-1A, S/N OFF - 64816. 2 L 7 2 4F RT A21EA 2007071200061 20070712 00061 SO 2007 7 12 SWIA200718417 1 20070501 A 5712 RIB EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 234SW 120308 RIGHT INBOARD LEADING EDGE RIB IS CRACKED, DISCOVERED AT C-CHECK. REPLACED RIB IAW EMB 120 SRM 51-10-02 PG 2 SECT 2B AN D 51-40-02. 2 L 7 2 4T RT A31SO 2007071200062 20070712 00062 SO 2007 7 12 SWIA200718418 1 20070501 A 5712 RIB EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 234SW 120308 LEFT INBOARD LEADING EDGE RIB IS CRACKED, DISCOVERED AT C-CHECK. REPLACED RIB IAW EMB 120 SRM 51-10-02 PG 2 SECT 2B AND 51-40-02. 2 L 7 2 4T RT A31SO 2007071200065 20070712 00065 SO 2007 7 12 SWIA200718421 1 20070416 A 2730 ROD END EMB 120 EMB120ER 3260203 SO RT ELEVATOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 233SW 120307 RIGHT LOWER ROD END BEARING ON THE ELEVATOR QUADRANT IS CORRODED, DISCOVERED AT C-CHECK. REPLACED RIGHT LOWER ROD END O N ELEVATOR QUADRANT IAW EMB 120 MM 27-31-04, PN RA4MK7-J. 2 L 7 2 4T RT A31SO 2007071200068 20070712 00068 SO 2007 7 12 SWIA200718424 1 20070416 A 5310 CROSSBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 233SW 120307 EXFOLIATING CORROSION FOUND ON PROFILE OF RIGHT SIDE CROSSBEAM MEMBER FORWARD OF CARGO DOOR, DISCOVERED AT C-CHECK. REP AIRED RIGHT SIDE OF CROSSBEAM IAW EMB 120 SRM 51-10-02 PG 3 SEC 3A, P/N 120-04449-001. 2 L 7 2 4T RT A31SO 2007071200076 20070712 00076 CE 2007 7 12 RU3A0705 1 20070702 A 2150 1013841353 MOTOR BEECH 300 300BEECH 1152930 CE BLOWER FAILED E RU3A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 15 75 26 FF10 WHILE OUTBOUND IN A "FLIGHT INSPECTION HOLDING PATTERN" THE MISSION SPECIALIST REPORTED SOMETHING WAS ON FIRE IN THE REA R CABIN, BOTH PILOTS VISUALLY CONFIRMED SMOKE IN THE AFT CABIN AREA. DECLARED AN EMERGENCY WITH INTENTION TO LAND AT WI LEY POST, CREW DONNED OXYGEN MASKS AND PREPARED FOR IMMEDIATE LANDING. UPON LANDING IMMEDIATELY CLEARED THE RUNWAY, SHU T DOWN AND EVACUATED THE AIRCRAFT. AFTER SHUTTING DOWN NO FURTHER INDICATIONS OF ANY SMOKE OR FUMES. 2 L 7 2 4T A24CE 2007071200114 20070712 00114 EU 2007 7 12 AWXA200700797 1 20070702 A 2150 PLENUM AIRBUS 320 A320231 3930325 EU A/C PACK UNKNOWN A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 632AW 81 PHX - LAS - EL - NR 7752072 - CREW REPORTED DURING CLIMB-OUT, PACK NR 2 TRIPPED OFF AND WOULD NOT RESET. THE NR 1 PACK WAS ON MEL. THE CREW DECLARED AN EMERGENCY AND RETURNED TO PHX. REMOVED AND REPLACED PLENUM PER AMM 21-52-22, PACK OPE RATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007071200119 20070712 00119 NE 2007 7 12 HEEA116019 1 20070620 A 2612 9231004802103 DETECTOR SKRSKY S92 S92A NE NR 2 MALFUNCTIONED B HEEA O OTHER N FALSE WARNING CL CLIMB 1 SW 03 892PH 334 920038 NR 2 ENGINE FIRE LIGHT ILLUMINATED FOR APPROX 2 SECONDS DURING IFR CLIMBOUT FIVE MINUTES AFTER TAKEOFF. REPLACED FLAME DETECTOR AND ALSO REPLACED HARNESS 92552-04112-041. 2 G 7 2 4U R00024BO 2007071200124 20070712 00124 WP 2007 7 12 ASMF200707002 1 20070701 A 2120 A/C PACK DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE LEAKING W ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 214AM 49585 718133 AIR TURNED BACK DUE TO HIGH TEMPERATURE IN TAIL CONE, LIGHT TURNED ON AND RT ENGINE WITH LOW ACCELERATION. MAINTENANCE CORRECTED PNEUMATIC LEAKS IN THE LT AND RT AIR-CONDITIONED SYSTEMS IAW MM 36-20-02 AND MPCM 21-10-00; ADDITIONALLY, THE ACCELERATION CAMS AND THE BLEED VALVES WERE LUBRICATED IAW MM 73-20-01 AND MM 75-31-05, TESTED CORRECT IAW 71-00-00. AIR CRAFT LANDED WITH 57000 KILOGRAMS, SO IT WAS NOT NECESSARY AN OVERWEIGHT LANDING INSPECTION IAW MM 05-51-04. 2 L 7 2 4F 4 F RT A6WE E9NE 2007071200136 20070712 00136 EU 2007 7 12 UPS07150062 1 20070626 A 5321 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 134UP 0817 AS REPORTED BY UNLOAD CREW, HOLE IN THE FLOOR OF A/B SECTION, MARKED WITH A RED STICKY. HOLE 1.5" 34" FROM FWD OF BULK PIT, 4' IN FROM FWD DOOR FRAME. DEFERRED IAW SRM 53-10-20 FIG 110. PERMANENT REPAIR IN 359 FLIGHT HOURS. 2 L 7 2 4F RT A35EU 2007071200157 20070712 00157 WP 2007 7 12 UPS07850053 1 20070623 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 L/WING OUTBD LEADING EDGE AT STA XFS 641 IS CRACKED. STOP DRILLED CRACK AT STA XFS 641 L/WING LEADIN G EDGE IAW SRM 57-2- 0 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER AT L/WING LEADING EDGE STA XFS 641 IAW SRM 57-03 -01 FIG 006. 2 L 7 4 4F RT 4A25 2007071200159 20070712 00159 NM 2007 7 12 UPS07M50046 1 20070328 A 5753 SKIN DOUG MD11 MD11 3023602 NM TE FLAPS DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C LTW, INBD FLAP LOWER AFT INBD AND OUTBD SEGMENTS NEED RE-SKIN. LHW I/B FLAP LWR AFT I/B AND O/B SEGME NTS REMOVED. DAMAGED SKIN REMOVED. NEW SKIN FAB PER DWG ARC2736. NEW SKIN PROTECTED, PAINTED AND INSTALLED. LHW I/B FLAP O/B SEGMENT FAB PER DWG ARC2444. NEW SEGMENT PRO TECTED, PAINTED AND INSTALLED. REWORKED AREA PAINTED TOP COAT PE R SRM51 -21-02 VOL II REV 39. 2 L 7 3 4F RT A22WE 2007071200166 20070712 00166 WP 2007 7 12 UPS07850065 1 20070609 A 5320 FITTING DOUG DC8 DC873F 302199F WP FS 922 L21R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 END FITTING CRACKED AT STA 922 L21R. REMOVED END FITTING AT STA 922 L21R IAW SRM 51-1-20D. LOCATED, DRILLED AND INSTALLED REPAIR END FITTING AT STA 922 L21R IAW SRM 51-1-24, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007071200167 20070712 00167 WP 2007 7 12 UPS07850066 1 20070609 A 5313 DC853B00939 LONGERON DOUG DC8 DC873F 302199F WP FS 1721 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 L15R AT STA 1720 CRACKED. REMOVED DAMAGED LONGERON SECTION AT STA 1721 TO 1766 L15R IAW SRM 51-01-21 -0. FABRICATED AND INSTALLED LONGERON SPLICE SECTION AT STA 1721 TO 1766 L15R IAW SRM 53-02-02-0 FIG 10. 2 L 7 4 4F RT 4A25 2007071200168 20070712 00168 WP 2007 7 12 UPS07850067 1 20070612 A 5330 564932731 SKIN DOUG DC8 DC873F 302199F WP FS 1720 L15L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 FUSELAGE EXTERIOR SKIN CRACKED IN 3 EA AREAS AT STA 1720 L15L. REPAIRED FUSELAGE SKIN AT STA 1720 L1 5L IAW SAA EA NR 008-5330-01-A 0923, UPS EO DC8-5330-27108-A, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007071200172 20070712 00172 WP 2007 7 12 UPS07850077 1 20070622 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 L/WING OUTBD L/E LWR RIB CRACKED AT STA XFS 734. STOPPED DRILLED CRACKED RIB AT L/WING LE STA XFS 73 4 IAW SRM 57-02- 0 FIG 2. FABRICATED AND INSTALLED REPAIR DOUBLER AT L/WING LE STA XFS 734 IAW SRM 57-03-03-0 FIG 7. 2 L 7 4 4F RT 4A25 2007071200186 20070712 00186 NM 2007 7 12 UPS07M50072 1 20070414 A 5320 WEB DOUG MD11 MD11 3023602 NM BS 2015 RBL 25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C AFT FUSELAGE COMPARTMENT HAS UPPER TORQUE BOX WEB CRACKED AT STA 2015 APPROX RBL 25 AT MAN HOLE ACCESS CUTOUT STICKER 8344. AFT FX COMPT STA2015 APPROX RBL 25 UPP TORQUE BOX WEB CRACK AREA ATTACHING PARTS REMOVED. HFEC I NSP C/OUT FOUND CRACK APPROX 1/2". UPP TORQUE BOX WEB CRACK END STOP DRILLED. HFEC INSP C/OUT ON REWORK AREA FOUND NO CRACK IN STOP DRILL HOLE. REPAIR DOUBLER AND SHIM FAB PER SRM 53-40-00 FIG 23 VOLI REV 38, REPROTECTED, PAINTED AND INS TALLED. 2 L 7 3 4F RT A22WE 2007071300026 20070713 00026 EA 2007 7 13 TRAX200700906 1 20070627 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 906EV 7642 F/A STATION FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007071300038 20070713 00038 NM 2007 7 13 QXEA200701078 1 20070702 A 7600 UNKNOWN DHAV DHC8 DHC8202 2809007 NM UNKNOWN A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 347PH 480 YVR FLIGHT NR 2039 - AFTER SINGLE ENGINE TAXI, WHEN BRINGING NR 1 CL FROM START/FEATHER TO MAX FOR TAKEOFF TORQUE INDICA TION SPIKED AT APPROXIMATELY 125 PERCENT. POWER LEVER WAS BELOW FLIGHT IDLE AND TAKEOFF WHEN TEST WAS NOT BEING PUSHED. PERFORMED OVER TORQUE INSPECTION PER PW 213 AMM 05-10-00. NO DEFECTS FOUND. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071300049 20070713 00049 NM 2007 7 13 AALA20071183 1 20070627 A 3350 SWITCH BOEING 777 777223 1385213 NM EMERGENCY LIGHT OBSTRUCTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 796AN 30796 LHR INFLIGHT T108/27JUN - EMERGENCY LIGHTS CAME ON IN FLIGHT AND COULD NOT BE EXTINGUISHED. REMOVED STICKY TAPE FROM TE ST SWITCH AT LT NR 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007071300054 20070713 00054 NM 2007 7 13 AALA20071185 1 20070607 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 394AN 29431 DFW - EMERGENCY LIGHT AT SEAT 11C IS LOOSE. SECURED LOOSE EMERGENCY LIGHT ASSEMBLY AT SEAT 11C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007071300055 20070713 00055 NM 2007 7 13 AALA20071186 1 20070607 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 394AN 29431 DFW - EMERGENCY LIGHT AT SEAT 26H INOPERATIVE. REPLAMPED EMERGENCY LIGHT AT SEAT 26H. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F RT A1NM 2007071300058 20070713 00058 WP 2007 7 13 AALA20071190 1 20070627 A 3397 WIRE HARNESS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 573AA 53092 SFO - EMERGENCY LIGHT AT SEAT 23 INOPERATIVE. REPAIRED HARNESS FOR EMERGENCY LIGHT AT SEAT ROW 23. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071300068 20070713 00068 SO 2007 7 13 SWIA200718425 1 20070325 A 5210 RIB EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 232SW 120306 PAX DOOR TORQUE TUBE FORWARD ATTACH RIB IS CRACKED, DISCOVERED AT C-CHECK. REPLACED CRACKED RIB PER SRM 51-40-02. 2 L 7 2 4T RT A31SO 2007071300075 20070713 00075 EA 2007 7 13 QXEA200701024 1 20070622 A 5320 PANEL CNDAIR CL600 CL6002C10 1390015 EA CABIN LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 DEN- TAXI FOR FLIGHT 4331 THE PLASTIC OVERHEAD PANEL IN CABIN WAS LOOSE. RETURNED TO THE GATE. MAINTENANCE SECURED THE PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007071300076 20070713 00076 EU 2007 7 13 MAC070201 1 20070626 A 5751 TEE FITTING AEROSP AEROSP ATR42 ATR42300 8680920 EU AILERON CORRODED A MTNA K NONE O OTHER IN INSP/MAINT 1 SO 33 916FX 1257 314 DURING INSPECTION, LEVEL 2 CORROSION WAS FOUND ON A T-FITTING IN THE AILERON S/N 1257, P/N S57610250-001, MFG DATE 08/92 . THE T-REPLACED HAD EXFOLIATION CORROSION ALONG THE FITTING EDGES. LOCATED AT THE CENTER OUTBOARD SECTION. REF ATR42 SRM 57-61-10 FIG 101. REASON FOR INSPECTION: MRB 576108-01 (8 YEAR INTERVAL). 2 H 7 2 4T RT A53EU 2007071300082 20070713 00082 NM 2007 7 13 SWAA073278 1 20070701 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 482WN 29852 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007071300104 20070713 00104 2007 7 13 SWAA073269 4 20070630 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071300106 20070713 00106 NM 2007 7 13 KPVA20077 1 20070630 A 3230 5352011 CONTROL UNIT DHAV DHC8 DHC8103 1386005 NM LANDING GEAR INOPERATIVE A KPVA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 WP 13 809WP 032 (PIREP) PLACED GEAR HANDLE DOWN, GOT 3 RED INDICATIONS ONLY. GEAR CAME DOWN ON IT'S OWN AFTER GO AROUND WITH CLIMB TO 3 000 FT. ALTERNATE GEAR EXTENSION LIGHTS SHOWED 3 DOWN. ANTI-SKID TESTED OK. (MX) REMOVED AND REPLACED LANDING GEAR CO NTROL UNIT IAW DHC-8MM 32-30-05 PG 201-203. FUNCTIONAL GEAR RETRACTION CHECK GOOD IAW DHC-8 MM 32-30-00 PG 203-204. 2 H 7 2 4T RT A13NM 2007071300111 20070713 00111 EA 2007 7 13 QXEA200701077 1 20070702 A 2760 5120011 PCU CNDAIR CL600 CL6002C10 1390015 EA SPOILERS MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 616QX 9940 10128 DEN - RECEIVED A INBOARD SPOILER CAUTION ON TAXI OUT. RETURNED TO THE GATE. MAINTENANCE REPLACED THE RIGHT INBOARD PCU . OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007071300113 20070713 00113 NM 2007 7 13 NWAA072416311 1 20070703 A 3397 WIRE BOEING 747 747451 1384940 NM BATTERY PACK SHORTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 671US 26477 DURING OVERNIGHT LINE CHECK, FOUND EMERGENCY FLOOR LIGHTS FROM SEAT 64C TO DOOR 4 LEFT STARTED DIMMING. MAINTENANCE FOU ND SHORTED WIRES. MAINTENANCE REPAIRED SHORTED WIRES AND REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECKED GOOD A ND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007071300119 20070713 00119 EA 2007 7 13 TRAX200700894 1 20070625 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 871AS 7537 FS 280 FLOOR SUPPORT ANGLE IS CRACKED, JUST O/B OF THE LBL 27.0. FABRICATED NEW O/B CLIP LBL 9, AND LOCATED HOLES, IAW CRJ SRM 51-24-26 AND 51-40-11. 06/28/07 INSTALLED CLIP, IAW CRJ SRM 51-42-06 AND 51-42-21. 06/28/07, AT FS 280 LBL 9. SUPPLEMENTAL - SDR CLOSED 07/03/07. 2 L 7 2 4F RT A21EA 2007071300123 20070713 00123 WP 2007 7 13 UPS07850119 1 20070606 A 5532 564779637 SKIN DOUG DC8 DC873F 302199F WP VERTICAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 RIGHT SIDE OF VERTICAL STAB UPPER SKIN HAS 5 SHEARED FASTENERS AND POSSIBLE CORROSION UNDER SKIN. RE MOVED PANEL NR 5647796-37 AND REMOVED CORROSION THAT WENT OUT OF LIMITS IAW SRM 51-03-00-0. REPLACED SKIN PANEL NR 5647 796-37 IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007071300127 20070713 00127 EU 2007 7 13 USAA070520 1 20070703 A 5320 D53472986000 FLOOR SUPPORT AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 182UW 1536 TOPSIDE OF FLOOR SUPPORT Y1732 AT NUT PLATE HOLE HAS CORROSION. ACCOMPLISHED BATH TUB REPAIR PER SRM 53-41-14; CORR TAS K JA-260-53500; LEVEL 1, DEFECT SIZE: 1 X 1 INCH. 2 L 7 2 4F RT A28NM 2007071300138 20070713 00138 SO 2007 7 13 SIMA200719101 1 20070522 A 5347 13500412001 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 15956 5000 145224 RIGHT AFT INBOARD SEAT TRACK BETWEEN FRAME 53 AND 57 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R2. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300139 20070713 00139 SO 2007 7 13 SIMA200719105 1 20070522 A 5347 14532605017 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 15926 5000 145224 RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AM ERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R2. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300142 20070713 00142 SO 2007 7 13 SIMA200719114 1 20070522 A 5347 14530659007 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 15926 5000 145224 LEFT INBOARD SEAT TRACK BETWEEN FRAME 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURN ED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300153 20070713 00153 EA 2007 7 13 SWIA200718434 1 20070707 A 3397 CONTACT CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS CONTAMINATED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 442SW 7609 FLT 3890 - EMERGENCY FLOOR LIGHTS AT ROWS 1 THRU 5 ARE NOT ILLUMINATING. CLEANED MOISTURE FROM THE CONTACT AREA. OPS C HECKS GOOD. 2 L 7 2 4F RT A21EA 2007071300156 20070713 00156 NM 2007 7 13 HNAA0700133 1 20070601 A 3830 85320980105 DRAIN LINE DHAV DHC8 DHC8102 2809003 NM CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 912HA 040 CORROSION FOUND ON LAV DRAIN TUBE FLANGE. 2 H 7 2 4T RT A13NM 2007071300157 20070713 00157 SO 2007 7 13 SWIA200718437 1 20070519 A 5210 BRACKET EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 235SW 120310 PAX DOOR HAS A CRACK AT THE AFT LOWER RADIUS AREA, DISCOVERED AT C-CHECK. REPLACED CRACKED BRACKET IAW EMB SRM 51-40-02 . 2 L 7 2 4T RT A31SO 2007071300161 20070713 00161 SO 2007 7 13 SWIA200718440 1 20070519 A 5310 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 235SW 120310 CORROSION AT CENTER BUTT STRAP BETWEEN FRAMES 37 AND 38, DISCOVERED AT C-CHECK. REPLACED CENTER BUTT STRAP IAW EMB SRM 51-10-02 PG 3 SECT 3A. 2 L 7 2 4T RT A31SO 2007071300162 20070713 00162 SO 2007 7 13 SWIA200718441 1 20070519 A 5310 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 235SW 120310 CORROSION AT RIGHT BUTT STRAP BETWEEN FRAMES 38 AND 40, DISCOVERED AT C-CHECK. REPLACED RIGHT BUTT STRAP IAW SRM 120 51 -10-02 PG 3 SEC 3A. 2 L 7 2 4T RT A31SO 2007071300177 20070713 00177 SO 2007 7 13 SWIA200718450 1 20070323 A 5210 FRAME EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 569SW 120344 PAX DOOR IS CRACKED AT FRAME 5 ON THE AFT SIDE, DISCOVERED AT C-CHECK. NEW FRAME INSTALLED IAW SRM 120 51-10-02 PG 3, S EC 3 A. 2 L 7 2 4T RT A31SO 2007071300178 20070713 00178 SO 2007 7 13 SWIA200718451 1 20070323 A 5210 BRACKET EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 569SW 120344 PAX DOOR IS CRACKED AT AFT LOWER CORNER, DISCOVERED AT C-CHECK. REPLACED CRACKED BRACKET ON PAX DOOR AFT LOWER CORNER I AW EMB 120 SRM 51-10-02 AND 51-40-02. 2 L 7 2 4T RT A31SO 2007071300180 20070713 00180 SO 2007 7 13 SWIA200718452 1 20070323 A 5210 FRAME EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 569SW 120344 PAX DOOR IS CRACKED AT FRAME NR 3 DISCOVERED AT C-CHECK. DOUBLER INSTALLED IAW SRM 120 52-10-02. 2 L 7 2 4T RT A31SO 2007071300181 20070713 00181 EA 2007 7 13 SWIA200718453 1 20070708 A 3350 POWER SUPPLY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCHARGED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 963SW 7865 FLT 6107 - FORWARD OVERHEAD WING EXIT SIGN AND TWO EXTERIOR EMERGENCY LIGHTS ARE INOP. REPLACED NR 2 EMERGENCY BATTERY PER AMM 33-51-04. OPS CHECK GOOD, P/N: AD-2013-1A S/N OFF: 29652. 2 L 7 2 4F RT A21EA 2007071300182 20070713 00182 2007 7 13 COMA0760456 4 20070628 A 3417 8220372445 ADC CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAULTY A COMA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 796CA 8488 7338 FLIGHT 9496 - ON FINAL APPROACH WHEN FLAPS SELECTED TO 45 DEGREES, THE OVERSPEED CLACKER CAME ON AND DID NOT GO OFF. PE RFORMED GO AROUND, CLACKER WENT OFF WHEN FLAPS CAME UP TO 30 DEGREES, AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED NR 2 ADC. 2 L 7 2 4F RT A21EA 2007071300183 20070713 00183 SO 2007 7 13 SWIA200718454 1 20070702 A 3397 CONNECTOR EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DISCONNECTED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 567SW 120342 EMERGENCY EXIT SIGN AT ROW 9 IS NOT LIGHTING UP. REPAIRED BAD SPLICE CONNECTORS. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007071300184 20070713 00184 NM 2007 7 13 NWAA072436716 1 20070622 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 360 S24L CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 616US 21120 DURING "L" CHECK, FOUND CRACK IN FUSELAGE FRAME AND DOUBLER AT BS 360 S24L. REPAIRED PER EA 67-209717. 2 L 7 4 4F A20WE 2007071300185 20070713 00185 EA 2007 7 13 COMA0760457 1 20070628 A 2421 755469E IDG CNDAIR CL600 CL6002B19 1900309 EA NR 2 ENGINE FAILED A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 443CA 3527 7539 FLIGHT 5045 - ABORTED TAKEOFF FOR NR 2 GEN FAIL ON TAKEOFF. REMOVED AND REPLACED NR 2 IDG. 2 L 7 2 4F RT A21EA 2007071300189 20070713 00189 EA 2007 7 13 TRAX200700899 1 20070627 A 5753 ANGLE CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 870AS 7530 RIGHT SIDE O/B FLAP HINGE ARM W/S 264 I/B SIDE ANGLE CRACKED. ANGLE FABRICATED IAW SRM 51-24-16. ALODINED, PRIMED AND PAINTED IAW SRM. ANGLE ON RIGHT O/B HINGE ARE REMOVED AND REPLACED IAW SRM 51-42-13. SUPPLEMENTAL - SDR CLOSED 07/05/0 7. 2 L 7 2 4F RT A21EA 2007071300192 20070713 00192 NM 2007 7 13 HALA0700269 1 20070627 A 2613 89873202 CIRCUIT CARD BOEING 767 7673G5 1385126 NM PWA 4060 PW4060 52119 NE OVERHEAT LOOP MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM, RT ENG OVHT LOOP 1 STATUS MSG. T/S PER FIM 26-11-00 SWAPPED LT AND RT AFOLTS CARDS MSG FOLLOW CARD. RTN GOOD CARD TO ORIGINAL POS. REPLACED RT ENG CARD M689 MSG CLEARED. FIRE AND OVHT FOR LT AND RT ENG TEST NOR MAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071300194 20070713 00194 NM 2007 7 13 HALA0700270 1 20070628 A 2710 UNKNOWN BOEING 767 76733A 1385209 NM UNKNOWN A HALA O OTHER F FLT CONT AFFECTED CL CLIMB 1 WP 13 587HA 33421 ETOPS SIGNIFICANT SYSTEM, ON CLIMB-OUT RT I/B AILERON APPEARED ON STATUS PAGE TO BE IN EXTENDED UP POSITION THIS CAUSED LEFT RUDDER TRIM USE OF 4 UNITS. IN CRUISE LOOK AT BOTH I/B AIL BOTH APPEARED TO BE BELOW NORMAL WHILE STATUS PG DEPICT ED THEM ABOVE NORMAL POSITION RUDDER CENTERED. ON YOKE DEGREE MARKINGS FOUND AILERONS TRIMED 1 UNIT LT PER FIM 27-18-00 AIL INDICATION POINTER TRAVEL FIG 107 CHECK OK. ALSO, PERFORMED FIM 27-18-00 FIG 106 AND PASSED CK OK. ALSO, PERFORME D FIM 27-18-00 FIG 105 PASSED CK OK AND PERFORMED AMM 27-18-00-715-003. CK GOOD AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007071300196 20070713 00196 NM 2007 7 13 SWAA073292 1 20070703 A 5330 6545777 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT LOWER END. REPAIRED SKIN PER SWA E A. 2 L 7 2 4F RT A16WE 2007071300199 20070713 00199 NM 2007 7 13 SWAA073298 1 20070703 A 5311 6546552 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071300200 20070713 00200 NM 2007 7 13 HALA0700272 1 20070629 A 4990 OIL SYSTEM BOEING 767 76733A 1385209 NM APU FLUCTUATES A HALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, APU OIL QTY FLUCTUATES BETWEEN .50 AND FULL. SHUT DOWN APU AND CHECKED OIL LEVEL. ADDED 1/2 PINT OIL. STARTED APU NO OIL LEAKS NOTED. EICAS READS FULL. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007071300204 20070713 00204 2007 7 13 HALA0700273 4 20070630 A 3442 RADAR BOEING 767 7673G5 1385126 NM WX SYSTEM INOPERATIVE A HALA O OTHER O OTHER CR CRUISE 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM, RIGHT WX RADAR R/T INOP, DISPLAYS INOP ON CRT, ALSO WINDSHEAR FAIL ILLUMINATED. SWITCHED TO L EFT RT, SYS OKAY. PERFORMED FIM 34-43-00-1 TEST PASS, OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007071300208 20070713 00208 WP 2007 7 13 07FDEA02341 1 20070629 A 3620 UNKNOWN DOUG MD10 MD1010F 3022112 WP UNKNOWN A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 68050 47804 EN ROUTE TO SEA, NOTICED ON PNEUMATIC PNL RED MANF NR 3 LIGHT AND AMBER BLEED OFF LIGHT. PNEUMATIC SYNOPTIC PG SHOWED N R 3 PNEU MANF IN THE RED AND PRESS IN MANF SLOWLY DROPPING. 2 MIN LATER RECEIVED LVL 3 ALERT "AIR MANF 3 FAIL". C/W QR H AND DIVERTED TO BOI. PERFORMED PNEUMATIC SYSTEM PRESSURE DECAY TEST ON NR 3 SYST TEST PASSED MANUALLY CLOSED AND LOCK ED RT WING ANTI-ICE VALVE PER MEL 30-11-01. T/S REF FIM, REACTIVATED WING ANTI ICE. EXTENDED LEADING EDGE SLATS, PERFO RMED LEAK CHECK ON ANTI ICE DUCTING ON RT WING. NO LEAKS FOUND. PNEUMATIC MANIFOLD RT WING PRESSURE SWITCH FAULT BALL SHOWING. RESET FAULT BALL. REPLACED FAIL DETECTION PRESSURE SWITCH. 2 L 7 3 4F RT A22WE 2007071300209 20070713 00209 NM 2007 7 13 07FDEA02367 1 20070703 A 2841 53307312 CONTROL KNOB BOEING 727 727233 138408A NM CROSSFEED VALVE MISALIGNED A FDEA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 SO 25 270FE 22035 CLIMBING THRU 10,000' NOTICED NR 3 FUEL TANK SHOWED HAVING ALL IT'S FUEL AND NR 2 SHOWED HAVING BURNED TWICE THE AMOUNT IT SHOULD HAVE. AFTER FURTHER ANALYSIS CONCLUDED THE NR 3 CROSSFEED VALVE WAS NOT OPERATING AS THE INDICATOR SWITCH WAS SHOWING. WHEN THE CROSSFEED SHOWED OPEN BELIEVED IT WAS ACTUALLY CLOSED. DIVERTED TO EWR. VISUALLY VERIFIED, AT THE VALVE POSITION INDICATOR, THAT THE NR 3 XFEED KNOB INDEX DISAGREES WITH THE ACTUAL POSITION OF THE NR 3 XFEED VALVE. R EPLACED NR 3 XFEED VALVE CONTROL KNOB. SYSTEM OPS CHECKS GOOD PER 727-200 AMM 28-22-111-2. 2 L 7 3 4F RT A3WE 2007071300211 20070713 00211 WP 2007 7 13 07FDEA02370 1 20070703 A 5230 ANB74371 ACCESS PANEL DOUG DC10 DC1030F 3023504 WP CARGO DOOR MISSING A FDEA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 SO 25 316FE 48314 CTR CARGO DOOR ACCESS PANEL FOR VENT DOOR MISSING ON ARRIVAL INTO PDX. OIL: NO RESTRICTION LOWER CENTER CARGO DOOR VENT DOOR MISSING. (OK PER EA 8-5230-113246), (CK AFTER EA FLT) INSPECTED SCRATCH PER SMP 51-80-01 AND DOOR ALL WITHIN LIMITS. COMPLIED WITH PART 1 EA-8-5230-113246. INSTALLED PANEL PER MM. OPS CK OK. 2 L 7 3 4F RT A22WE 2007071300212 20070713 00212 NM 2007 7 13 07FDEA02372 1 20070705 A 5531 6572187 RIB BOEING 727 727227 1384078 NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 VERTICAL STABLIZER RIB NUMBER 2 LT OTBD CHORD CRACKED AT STRINGER 7. REMOVED DAMAGE, FABRICATED REPAIR PARTS, SENT TO H EAT TREAT, TRACKING NR 2007-06-203, DRILLED, TREATED, AND PRIMED REPAIR PARTS. INSTALLED REPAIR PARTS REF SRM 55-30-5 F IG 1. 2 L 7 3 4F A3WE 2007071300213 20070713 00213 NM 2007 7 13 07FDEA02373 1 20070705 A 5720 652811616 SKATE ANGLE BOEING 727 727227 1384078 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 481FE 21463 RT WING AT NR 6 FLAP TRACK FWD FAIRING, I/B SKATE ANGLE IS CRACKED. REMOVED DAMAGE, FABRICATED NEW 2 REPAIR ANGLE AND I NSTALLED 2 REF. REPAIR ANGLES, REF SRM 51-40-3 PG 1-6. 2 L 7 3 4F A3WE 2007071300215 20070713 00215 NM 2007 7 13 HALA0700274 1 20070703 A 2710 TRANSMITTER BOEING 767 767332 1382001 NM AILERONS OUT OF ADJUST A HALA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM, BTB, INBOARD AILERON DISPLAY ON EICAS DOES NOT SHOW CORRECT CONTROL CHECK. ON ARRIVAL BACK IN TO GATE FOUND RT IB AILERON NOT FAIRING. ADJUSTED INBOARD AILERON TRANSMITTER PER AMM 27-18-00-501 AND ADJUSTED INBOARD AILERON PCA INPUT ROD PER AMM 27-11-48-422-040. AILERON OPS CHECK OKAY. 2 L 7 2 4F RT A1NM 2007071300216 20070713 00216 NM 2007 7 13 HALA0700275 1 20070705 A 2911 RELIEF VALVE BOEING 767 76733A 1385209 NM ADP FILTER LEAKING A HALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM, C HYD FLUID QUANTITY DECREASED TO .47. FOUND PACKING ON PRESSURE RELIEF VALVE OF ADP FILTER M ODULE LEAKING. REPLACED PACKING ON RELIEF VALVE PER TASK 29-11-19-004-001. LEAK CK'S OK. SERVICED CENTER HYD SYSTEM T O FULL. 2 L 7 2 4F RT A1NM 2007071300217 20070713 00217 2007 7 13 2007UALA02357 4 20070629 A 3436 WINDSHEAR SYS BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT INOPERATIVE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 774UA 26936 WXR SYS WXR DISPLAY IS NOT PRESENT WHEN WXR SELECTED ON EFIS CONTROL PANEL. WINDSHEAR SYS EITHER PREDICTIVE OR REACTIVE WINDSHEAR ALERTING FUNCTIONS ARE FAILED SUCH THAT WINDSHEAR ALERTING CAPABILITY IS REDUCED OR NOT AVAILABLE. A REACTIV E WINDSHEAR FAILURE WILL ONLY SET THE MESSAGE WITH THE REACTIVE WINDSHEAR OPTION ACTIVE. [07-27-07] UNABLE TO DUPLI CATE FAULT. AFTER CONSIDERABLE TROUBLESHOOTING, REPLACED WX RADAR CONTROL PANEL AND ANTENNA DRIVE ASSY. WINDSHEAR ALER TING CAPABILITY RETURNED TO NORMAL. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007071300218 20070713 00218 NM 2007 7 13 2007UALA02358 1 20070629 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 778UA 26940 THE 8D FWD, 11F FWD, 12F FWD, 19G AND 34C EEL LIGHTS ARE INOPERATIVE. RELAMPED EMERGENCY LIGHTS. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007071300221 20070713 00221 NM 2007 7 13 SWAA073322 1 20070704 A 5523 65C2638415M TAB BOEING 737 7375H4 138449D NM LT ELEVATOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED C4 CHECK, FOUND LT ELEVATOR TAB CRACKED AT UPPER OUTBOARD END. REMOVED AND REPLACED ELEVATOR TAB PER M M. 2 L 7 2 4F RT A16WE 2007071300222 20070713 00222 NM 2007 7 13 SWAA073289 1 20070703 A 5754 65C266011 SLAT BOEING 737 7375H4 138449D NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 18Y CHECK, FOUND LT WING NR 1 LEADING EDGE SLAT LOWER TRAILING EDGE CRACKED AT INBOARD AUX TRACK. REPA IRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007071300223 20070713 00223 NM 2007 7 13 SWAA073315 1 20070704 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 725SW 27857 R2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007071300224 20070713 00224 NM 2007 7 13 SWAA073302 1 20070703 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071300225 20070713 00225 NM 2007 7 13 SWAA073301 1 20070703 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071300226 20070713 00226 NM 2007 7 13 SWAA073305 1 20070703 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071300227 20070713 00227 NM 2007 7 13 SWAA073293 1 20070703 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071300228 20070713 00228 NM 2007 7 13 SWAA073304 1 20070703 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071300229 20070713 00229 NM 2007 7 13 SWAA073306 1 20070703 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071300232 20070713 00232 NM 2007 7 13 SWAA073303 1 20070703 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007071300233 20070713 00233 NM 2007 7 13 SWAA073295 1 20070703 A 5311 65C34355 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071300234 20070713 00234 NM 2007 7 13 SWAA073296 1 20070703 A 5311 65C34356 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071300236 20070713 00236 NM 2007 7 13 SWAA073310 1 20070703 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 710SW 27844 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007071300239 20070713 00239 NM 2007 7 13 HALA0700277 1 20070704 A 5754 SKIN BOEING 767 767332 1382001 NM LE SLAT DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 I/B SLAT T/E LEFT WING, AND PANEL 511CB DAMAGED (INTERM REPAIR) 2 CYCLES. INTERIM REPAIR PER HAL M105 FILE NR 596020 OK FOR SERVICE, OK TO CONTINUE PER HAL M105 FILE NR 596020 TRANSCRIBE TO MIC SHEET. 2 L 7 2 4F RT A1NM 2007071300243 20070713 00243 NM 2007 7 13 HALA0700278 1 20070605 A 3600 79275514 CONTROLLER BOEING 767 7673G5 1385126 NM PWA 4060 PW4060 52119 NE MALFUNCTIONED A HALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 13 586HA 3024 3024 24259 ATO - DUE TO HPSOV AND PRV EICAS MSG ILLUMINATING AS THROTTLE WERE ADVANCED FOR TAKE OFF ROLL. REPLACED PRV CONTROLLER PER AMM 36-11-19, OPS CK LK CK OK. LOCKED OUT HPSOV PER MEL 36-11-2 ENTERED IN MIC SHT PLAC. INSTALLED PER MEL SHORTIN G CONNECTOR PLUG INSTALLED ON HP CONTROLLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071300246 20070713 00246 2007 7 13 SWAA073319 4 20070704 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071300247 20070713 00247 2007 7 13 SWAA073317 4 20070704 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE COVER BROKEN. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071300248 20070713 00248 NM 2007 7 13 SWAA073285 1 20070703 A 3350 MS15772 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED MV1 CHECK, FOUND FWD LAV EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007071300252 20070713 00252 NM 2007 7 13 AWXA200700800 1 20070708 A 5755 113N550142 SKIN BOEING 757 7572S7 1384962 NM SPOILER DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - MAJOR REPAIR - RIGHT WING NR 10 SPOILER, UPPER SURFACE DELAMINATED, WS 459.50 - WS 510.00. REPAIRED, RE-INSTALLED AND OPERATIONAL CHECKED RIGHT WING NR 10 SPOILER IAW B757-200 SRM 27-61-01. 2 L 7 2 4F RT A2NM 2007071300253 20070713 00253 NM 2007 7 13 SWAA073284 1 20070703 A 3350 OL3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 396SW 27690 BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 3 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007071300255 20070713 00255 EA 2007 7 13 COMA0770037 1 20070628 A 3610 GG670950021 SHUTOFF VALVE CNDAIR CL600 CL6002C10 1390015 EA BLEED AIR SYS LEAKING A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 625CA 10486 10113 FLIGHT 5230 - RECEIVED RIGHT BLEED AIR DUCT WARNING. RIGHT AND LEFT PACK SHUT DOWN. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND RIGHT HOT AIR SOV LEAKING FROM REGULATOR. REPLACED RIGHT SOV. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007071300256 20070713 00256 EA 2007 7 13 COMA0760459 1 20070629 A 3260 TARGET CNDAIR CL600 CL6002B19 1900309 EA RT MLG LOOSE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 962CA 7123 FLIGHT 5531 - RECEIVED GEAR DISAGREE MESSAGE UPON GEAR RETRACTION. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND RIGHT MLG UPLOCK TARGET LOOSE. SECURED TARGET, ADJUSTED PROX SENSOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007071300262 20070713 00262 SO 2007 7 13 SIMA200719115 1 20070522 A 5347 14532605 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 15926 5000 145224 RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 36 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETU RNED AIRCRAFT TO SERVICE 2 L 7 2 4F RT T00011AT 2007071300268 20070713 00268 NE 2007 7 13 2007UALA02360 2 20070702 A 7200 ENGINE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 OVERTEMP A UALA O OTHER M OVER TEMP NR NOT REPORTED 1 WP 29 815UA 867 V10511 NR 2 ENGINE OVERTEMP ON START 717 DEG, 30 SEC. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071300272 20070713 00272 NM 2007 7 13 2007UALA02365 1 20070701 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 DOOR 4 RIGHT AFT SILL EMERGENCY LIGHT IS INOP. [07-24-07] RELAMPED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071300273 20070713 00273 NM 2007 7 13 2007UALA02366 1 20070701 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 ZONE-B RIGHTSIDE CEILING (2EA) & UPPER DECK CEILING (1EA) EMERGENCY LIGHTS ARE INOP. RELAMPED EMERGENCY LIGHTS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071300275 20070713 00275 NM 2007 7 13 2007UALA02368 1 20070630 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY EXIT LIGHT INOP AT DOOR 2 GALLEY CEILING LIGHT. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071300276 20070713 00276 NM 2007 7 13 2007UALA02369 1 20070702 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 UPPER DECK EMERGENCY LIGHT INOP AT DOORS FWD CEILING LIGHT. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071300280 20070713 00280 NM 2007 7 13 2007UALA02373 1 20070701 A 3350 COVER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 178UA 24385 EEL COVER BROKEN ZONE 614 BEHIND SEAT 47H. [07-24-07] REPLACED EEL LIGHT AT SEAT 47H. LIGHT OPERATES NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071300282 20070713 00282 NM 2007 7 13 2007UALA02375 1 20070702 A 3260 WARNING SYSTEM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 121UA 29167 TOO LOW GEAR WARNING ON APPROACH, GO AROUND PERFORMED. GEAR INDICATIONS WERE NORMAL WITH NO EICAS MESSAGES. [07-27-07 ] CLEANED & LUBED LANDING GEAR HANDLE. STILL HAD BODY GEAR STEERING MESSAGE. REPLACED LT BODY GEAR PRIMARY LOCK ACTU ATOR SWITCH AS PER MM 32-53-16 PG 401 & OPS CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071300283 20070713 00283 NM 2007 7 13 2007UALA02376 1 20070702 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 581UA 26701 DOOR NR 2 LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. [07-27-07] RELAMPED EMERGENCY LIGHT AT DOOR NR 2 LEFT, OPS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071300284 20070713 00284 NM 2007 7 13 2007UALA02377 1 20070702 A 2530 OVEN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE GALLEY FUMES A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 209UA 30215 FLIGHT DIVERTED DUE TO FUMES COMING FROM A BUSINESS CLASS OVEN. [07-27-07] FOUND ODOR TO BE STRONGEST IN MID GALLEY AREA. APPEARED TO BE ACIDY SMELL. WHEN WARMING OVEN W33 WAS OPENED, ODOR BECAME MUCH STRONGER. FOUND PAPER TOWEL AND RES IDUE OF MELTED PLASTIC ALONG WITH ROLL BAGS. REMOVED ALL MATERIAL AND INOPED WARMING OVEN. NO ODOR NOTED AFTER ITEMS RE MOVED FROM AC. AFTER FURTHER TROUBLESHOOTING, REPLACED LEFT HAND GALLEY CEILING LIGHT BALLAST, DR 2 CROSS AISLE 2 L 7 2 4F 4 F RT T0001SE E46NE 2007071300285 20070713 00285 NM 2007 7 13 2007UALA02378 1 20070702 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EMERGENCY EXIT LIGHTS INOPERATIVE AT DOOR 2R FWD AND AFT SILL LIGHTS. ALSO, EMERGENCY EXIT SIGN INOP AT ROW 22 RIGHT. FOUND BATTERY PACKS LOOSE; SECURED. CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071300287 20070713 00287 SO 2007 7 13 SIMA200719202 1 20070603 A 5347 13500439007 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 15957 5000 145235 LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 21 AND 24. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300288 20070713 00288 SO 2007 7 13 SIMA200719204 1 20070603 A 5347 13500439007 SEAT TRACK EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 806AE 13290 5000 145503 LEFT FORWARD INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 20 AND 21. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 . AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071100068 20070711 00068 EA 2007 7 11 UH02007F00000 1 20070601 A 5100 NONE SCWZER 269 269D 8059501 EA ALLSN 250C 250C20 03013 GL NONE NONE E UH0A O OTHER O OTHER NR NOT REPORTED 1 SW 03 411HU 0040 DURING PRACTICE AUTOROTATION, ENGINE SHUTDOWN DUE TO THROTTLE INADVERTENTLY CLOSING INTO FUEL CUTOFF POSITION. STUDENT` S LEG CONTACTED IDLE, IDLE RELEASE BUTTON ON COLLECTIVE STICK HEAD AND THIS ALLOWED THROTTLE TO ROTATE BEYOND IDLE POSIT ION. HAVE CONTACTED THE AIRCRAFT MFG PREVIOUSLY DUE TO PRIOR SHUTDOWNS. (2 TIMES) (1ST SHUTDOWN TODAY) (K) 1 G 7 1 3U 3 U 0 4H12 E4CE 2007071100079 20070711 00079 NE 2007 7 11 DXTA200702293 2 20070624 A 7200 ENGINE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE UNKNOWN E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 640QS 5605240 UPON ADDING TAKEOFF POWER, CREW HEARD VERY LOUD EXPLOSIVE SOUND. CREW ABORTED TAKEOFF AND AS WE TAXIIED OFF OF RUNWAY, C REW HEARD EXTREMELLY LOUD FLUTTER BANGS THAT WERE CONSTANT. CREW SHUTDOWN RIGHT ENGINE. [07-12-07] RAN ENGINE AND NOIS E STOPPED. RAN BOTH ENGINES AND TURNED CABIN FLOW OFF AND NO BANG. TURNED ON AND 2-3 MINS GOT BANG AT 28% N1. DOWNLOAD ED BOTH EEC'S AND SENT FILE TO PRATT & WHITNEY, NO DEFECTS OR FAULTS NOTED. INSPECTED INLETS AND EXHAUSTS OF BOTH ENGIN ES WITH NO DEFECTS NOTED. INSPECTED PLUMBING FOR ENVIRONMENTAL SYSTEM IN TAILCONE WITH NO DEFECTS NOTED. FOUND WATER S EPERATOR FULL OF WATER & CONDENSER DIRTY. REMOVED SEPERATOR AND CLEANED. REMOVED AND REPLACED CONDENSER WITH NEW. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007071100081 20070711 00081 CE 2007 7 11 DXTA200702295 1 20070625 A 2150 A/C PACK CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CABIN ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 900QS 7500123 UPON LANDING, CABIN A/C PACK BEGAN PRODUCING AN OILY ODOR AND HAZE. [07-12-07] REMOVED AND REPLACED COCKPIT PAC. ACM L EAK CHECK AND OPS CHECK GOOD IAW CE750 M/M 21-51-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071100097 20070711 00097 NM 2007 7 11 ABXA070209 1 20070523 A 3213 015T150476 CYLINDER BOEING 767 767200 1385120 NM RT MLG CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 797AX 23147 RIGHT MAIN LANDING GEAR HAD A LARGE CRACK AT CASTING ON UPPER CENTER AFT END. REPLACED RIGHT MAIN LANDING GEAR ON JOB C ARD 32-045-01-2 IAW BOEING SRM. 2 L 7 2 4F RT A1NM 2007071100102 20070711 00102 WP 2007 7 11 ABXA070219 1 20070608 A 5312 591013085 BULKHEAD DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 AFT PRESSURE BULKHEAD DOOR CUTOUT AFT LOWER LEFT CORNER HAD 2 EACH CRACKS. ONE CRACK WAS 1.250 INCH AND ONE WAS .75 INC H. ONE IN ORIGINAL DOUBLER P/N: 5910130-87 AND ONE IN ORIGINAL DOUBLER P/N: 5910130-85. ALSO AFT PRESSURE BULKHEAD SKI N LOWER TAB HAD DRILL START. REPAIRED BOTH LEFT AND RIGHT AFT PRESSURE BULKHEAD CUTOUT LOWER IAW DC9 SRM. 2 L 7 2 4F A6WE 2007071100103 20070711 00103 WP 2007 7 11 ABXA070220 1 20070608 A 5312 591013085 BULKHEAD DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 AFT PRESSURE BULKHEAD DOOR CUTOUT AFT LOWER RIGHT CORNER HAD 2 EACH CRACKS. ONE CRACK WAS 2 INCHES AND ONE WAS 1.25 INC H. ONE IN ORIGINAL DOUBLER P/N: 5910130-85 AND ONE IN LOWER TAB PORTION OF AFT PRESSURE BULKHEAD SKIN P/N: 5910130-5. REPAIRED LOWER LEFT AND RIGHT AFT PRESSURE BULKHEAD DOOR CORNERS IAW DC9 DWG J060088. 2 L 7 2 4F A6WE 2007071100112 20070711 00112 NM 2007 7 11 ABXA070215 1 20070525 A 5712 114T220918 RIB BOEING 767 767200 1385120 NM RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 797AX 23147 CORROSION WS 564, RIGHT WING LEADING EDGE PANEL SUPPORT/RIB. REPLACED STRUT RIB IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007071100117 20070711 00117 EU 2007 7 11 HSYA20070601 1 20070622 A 3260 176191 PROXIMITY SWITCH STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA RT MLG OUT OF ADJUST E HSYA L A ABORTED APPROACH UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 NM 05 330SB SH3013 FLT 120-DURING APPROACH, CREW REPORTED RT MLG UNLOCK INDICATION AFTER SELECTING GEAR HANDLE TO THE DOWN POSITION. THE AI RCRAFT WAS DIVERTED, ATC DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MX FOUND THE RT MLG DOWNLOCK PR OXIMITY SWITCH OUT OF ADJUSMENT. MX PERFORMED ADJUSTMENT AND OPERATIONAL CHECK OF THE SWITCH AND THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. 2 H 7 2 4T 4 T A41EU E4EA 2007071100124 20070711 00124 NM 2007 7 11 CALA0700336 1 20070703 A 5714 VAPOR BARRIER BOEING 737 737824 13844BZ NM MLG W/W CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 73259 30803 INSPECTION FOUND MLG WHEEL WELL LEFT FORWARD BULKHEAD HAD A CRACK ON VAPOR BARRIER, REAR SPAR CENTER SECTION, LT SIDE TH AT HAD MIGRATED BEYOND A STOP DRILL. THE CRACK WAS NOW 18 INCHES LONG. A TEMPORARY REPAIR HAD BEEN PERFORMED PREVIOUSL Y A FEW MONTHS PRIOR. A PERMANENT REPAIR WAS PERFORMED IAW SRM 57-10-10 TO BAYS 5, 7 AND 8. 2 L 7 2 4F RT A16WE 2007071100126 20070711 00126 WP 2007 7 11 ABXA070229 1 20070613 A 5322 99577397 SHEAR TIE DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 SHEAR TIE CRACKED -945 RIGHT, JUST ABOVE LONGERON 16 RIGHT. REMOVED AND REPLACED SHEAR TIE STA 945 IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2007071100205 20070711 00205 NM 2007 7 11 2007UALA02170 1 20070621 A 5210 BOTTLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R1 DOOR LOW A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 831UA 1291 DOOR 1R DOOR PRESSURE LOW. SERVICED DOOR ASSIST SYSTEM. NO REPEATS SINCE ORIGINAL.. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100213 20070711 00213 EU 2007 7 11 2007UALA02177 1 20070620 A 3250 STEERING SYS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG MALFUNCTIONED A UALA C ABORTED TAKEOFF O OTHER TX TAXI/GRND HDL 1 WP 29 442UA 780 LOST NOSE WHEEL STEERING ON TAXI OUT. THERE WAS A RECURRENCE OF THIS EVENT ON FLIGHTS 0816-27 & 1612-29 DURING LANDIN G PHASE. FOUND BSCU FAILED. REPLACED BSCU AND SERVO 6GC. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100229 20070711 00229 2007 7 11 2007UALA02188 4 20070623 A 2565 HOOK AND LOOP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 408UA 457 DOOR 2L SLIDE-RAFT LANYARD HOOK AND LOOP STRIP DOES NOT STICK TOGETHER. FOUND WORN HOOK AND LOOP STRIP. REPLACED DOOR SLIDE 2L. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100242 20070711 00242 NM 2007 7 11 2007UALA02201 1 20070623 A 3350 767 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 516UA 24860 EMERGENCY SLIDE LIGHT ON EXTERIOR OF ACFT AFT OF LT WING TRAILING EDGE INOP. RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071100260 20070711 00260 EU 2007 7 11 07FDEA02360 1 20070702 A 5730 A57340086 SKIN AIRBUS 300 A300B4605R 3930308 EU LT WING WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 ELONGATED HOLE ON PYLON NR 1 TO BOTTOM WING SKIN REPAIR PERFORMED BY OVERSIZING THE HOLES AND INSTALLING FREEZE PLUGS IA W DRAWING R 571-50532 REV A. APPROVED BY EA 6-5720-106472 REV A AND RAS/BAE/1004873/2007 ISS A. 2 L 7 2 4F RT A35EU 2007071100263 20070711 00263 NM 2007 7 11 NWAA072356301 1 20070630 A 3350 FUSE BOEING 747 747451 1384940 NM CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23719 DURING OVERNIGHT CHECK, FOUND EMERGENCY LIGHT RIGHT SIDE INOP BOTTOM 2 LIGHTS. MAINTENANCE REMOVED AND REPLACED FUSES. OPERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007071100271 20070711 00271 EU 2007 7 11 AWXA200700788 1 20070621 A 5743 D57252921000 ANCHOR FITTING AIRBUS 320 A320231 3930325 EU LT WING CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 SAL - MAJOR REPAIR - C6 CHECK - NR# 5978208, CORROSION ON LEFT WING MAIN LANDING GEAR ANCHORAGE FITTING LUG UPPER FACE A ND INSIDE THE LUG BORE, RIB 2 - RIB 3. REPAIRED LEFT WING MAIN LANDING GEAR ANCHORAGE FITTING LUG UPPER FACE AND INSIDE THE LUG BORE, RIB 2 - RIB 3 IAW USAIRWAYS EA 120074. 2 L 7 2 4F RT A28NM 2007071100293 20070711 00293 WP 2007 7 11 070132 1 20070620 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 862GA 49556 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENC Y EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BA TTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007071100308 20070711 00308 NM 2007 7 11 SWAA073243 1 20070628 A 2560 65C16820 HOOK BOEING 737 7375H4 138449D NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM. 2 L 7 2 4F RT A16WE 2007071100324 20070711 00324 NM 2007 7 11 F3LA200700143 1 20070627 A 5321 TRANSITION PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT TRANSITION PANEL 132EG DAMAGED. REPAIRED TRANSITION PANEL 1 32EG IAW SRM 53-02-00, FIG. 204. 2 L 7 2 4F RT A28NM 2007071100329 20070711 00329 NM 2007 7 11 2007UALA02175 1 20070621 A 3350 1619 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 309UA 23670 LEFT AFT BODY FAIRING EXTERIOR EMERGENCY LIGHT INOP. RELAMPED OPS CHK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071100331 20070711 00331 NM 2007 7 11 2007UALA02199 1 20070622 A 3350 58781 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 341UA 24245 CREW REPORTS EEL LIGHTS COMING OFF THE LAST THREE FEET. LIGHTS INOP FROM ROW 16 BACK. REPLACE EEL AFT STRIP OPS CKS OK . 2 L 7 2 4F 4 F RT A16WE E2GL 2007071100347 20070711 00347 NM 2007 7 11 2007UALA02346 1 20070701 A 3350 20131A BATTERY PACK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 351UA 24319 EEL AT DOORS 1L AND 1R AND FLOOR LIGHTS BETWEEN FWD GALLEY AND ROW 2 INOPERATIVE. REPLACED M1132 BATT PACK AND M1503 IN VERTER. OPS CK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071100352 20070711 00352 NM 2007 7 11 2007UALA02352 1 20070630 A 3397 60444 POWER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 643UA 25093 LIGHT STRIP NR 5 INOP. REPAIRED POWER CABLE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071100356 20070711 00356 EU 2007 7 11 AWXA200700791 1 20070701 A 3397 WIRE AIRBUS 320 A320231 3930325 EU CABIN DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 SAL - EEL - C-06 CHECK - NR# 5970863, DAMAGED EMERGENCY EXIT LIGHT WIRE AT CABIN PARTITION 1 LEFT. REPAIRED AND OPERAT IONAL CHECKED EMERGENCY EXIT LIGHT WIRE AT CABIN PARTITION 1 LEFT IAW AIRBUS ESPM 20-53-21. 2 L 7 2 4F RT A28NM 2007071100357 20070711 00357 EU 2007 7 11 AWXA200700794 1 20070627 A 5744 D5755104120000 PIN AIRBUS 320 A320232 3930326 EU NR 1 SPOILER CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 667AW 1710 SAL - MAJOR REPAIR - BC-4 CHECK - NR# 5948352, CORROSION ON LEFT WING SPOILER NR 1 HINGE PIN, WS 306 - WS 407. REPLACED LEFT WING SPOILER NR 1 HINGE PIN, WS 306 - WS 407 IAW A320 AMM 27-64-41. 2 L 7 2 4F RT A28NM 2007071200001 20070712 00001 NM 2007 7 12 USAA070482 1 20070627 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 INBD FASTENER HOLE FOR A/C RAIL ATTACH BRACKET, BS 400 STR 8R AND 9R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLERS PER 53-10-20E, DEFECT SIZE: 1/8". 2 L 7 2 4F RT A16WE 2007071200010 20070712 00010 NM 2007 7 12 USAA070489 1 20070628 A 5311 FRAME BOEING 737 737401 1384701 NM BS 500C S8-9L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND CRACK STA 500C BETWEEN STR 8L AND 9L. INSTALLED DOUBLER PER T/R 53-10-20E, DEFECT SIZE: 1". 2 L 7 2 4F RT A16WE 2007071200011 20070712 00011 NM 2007 7 12 USAA070422 1 20070605 A 5310 BEAM BOEING 737 737401 1384701 NM BS 291 S10-11R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 FOUND CRACK STA 291RT, BETWEEN STR 10R AND 11R STUB BEAM. REMOVED DAMAGE AND INSTALLED REPAIR PARTS PER SRM 51-10-02, D EFECT SIZE: 1". 2 L 7 2 4F RT A16WE 2007071200012 20070712 00012 EU 2007 7 12 SA07045 1 20070628 A 3350 LIGHT AIRBUS A321 A321211 3930370 EU INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 183UW 1539 TPA - THE EMERGENCY BATTERY TEST LIGHTS WAS FOUND INOPERATIVE AT THE CIDS PANEL. 2 L 7 2 4F RT A28NM 2007071200015 20070712 00015 NM 2007 7 12 USAA070500 1 20070629 A 5414 SKIN BOEING 737 737401 1384701 NM NR 2 NACELLE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND CRACK AT 2 PYLON PANEL NR 5828R BENEATH LONGERON. STOP DRILLED END OF CRACK AND INSTALLED REPAIR DOUBLER PER TR 5 4-30-07, DEFECT SIZE: .250". 2 L 7 2 4F RT A16WE 2007071200019 20070712 00019 NM 2007 7 12 USAA070504 1 20070629 A 5320 FLOOR SUPPORT BOEING 737 737401 1384701 NM BS 328-344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND CORROSION BETWEEN BS 328 AND 344, LBL 11 FLOOR SUPPORT. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-10-02; CORR OSION TASK C53-107-01; LEVEL 2 DEFECT SIZE: 16". 2 L 7 2 4F RT A16WE 2007071200021 20070712 00021 NM 2007 7 12 USAA070506 1 20070629 A 5320 6545834260 FLOOR SUPPORT BOEING 737 737401 1384701 NM BS 312-328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND FLOOR SUPPORT CORRODED, STA 312-328 LBL-11. REMOVED AND REINSTALLED NEW FLOOR SUPPORT PER SRM 51-10-02; CORROSION TASK C53-107-01; LEVEL 2 DEFECT SIZE: 12". 2 L 7 2 4F RT A16WE 2007071200027 20070712 00027 NM 2007 7 12 USAA070512 1 20070629 A 5340 STOP FITTING BOEING 737 737401 1384701 NM BS 440 S24R CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND PITTING STA 440 S24R DOOR STOP ON FWD DOOR FRAME, LOWEST STOP. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER ST ANDARD PRACTICE MANUAL; CORROSION TASK C53-100-01, DEFECT SIZE: 1/16" BY 1/16". 2 L 7 2 4F RT A16WE 2007071200028 20070712 00028 NM 2007 7 12 USAA070513 1 20070629 A 5340 655287U97 ANGLE BOEING 737 737401 1384701 NM BS 965-986 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND CORROSION Z ANGLE AFT ENTRY DOOR BS 965-986 LBL49. REMOVED Z ANGLE AND REPLACLED WITH NEW PER SRM 51-40-02, 51-20 -01; CORR TASK C53-107-01, DEFECT SIZE: 24" BY 3.5". 2 L 7 2 4F RT A16WE 2007071200029 20070712 00029 SO 2007 7 12 SIMA200718001 1 20070628 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 21 674RJ 14500801 BURNED ODOR NOTICED IN GALLEY AND ROW THREE, NO SMOKE NOTICED. INSPECTED AIRCRAFT IN STANDARD OPERATIONAL CONFIGURATION WITH ALL PACKS ON RECERT FANS, LIGHTS AND AMENITIES OPERATING WITH NO DEFECTS NOTED. PERFORMED FUNCTIONAL C CHECK FLIG HT WITH NO DISCREPANCIES. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007071200052 20070712 00052 NM 2007 7 12 AALA20071180 1 20070626 A 3397 FEEDER CABLE BOEING 757 757231 1384950 NM EMERGENCY LIGHT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 717TW 28485 DFW - EMERGENCY LIGHTS AT SEAT ROWS 7 TO AFT OF LAVATORY D DOOR INOP. REPLACED PATH FLOOR EMERGENCY LIGHTING CABLE FEED AT SEAT ROW 24 FOR EMERGENCY LIGHTING AT SEAT ROWS 7 TO AFT OF LAVATORY D DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION . 2 L 7 2 4F RT A2NM 2007071200058 20070712 00058 SO 2007 7 12 SWIA200718414 1 20070501 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 234SW 120308 RIGHT SIDEWALL SEAT TRACK IS CORRODED IN SEVERAL AREAS, DISCOVERED AT C-CHECK. REPLACED RIGHT SIDEWALL SEAT TRACK ASSEM BLY, P/N 120-15997-603. 2 L 7 2 4T RT A31SO 2007071200067 20070712 00067 SO 2007 7 12 SWIA200718423 1 20070416 A 5210 RIB EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 233SW 120307 PAX DOOR MID SECTION FORWARD INTERNAL RIB IS CRACKED. REPLACED PAX DOOR INTERNAL RIB IAW SRM 120 51-10-02 PG 3 SEC 3A. 2 L 7 2 4T RT A31SO 2007071200082 20070712 00082 2007 7 12 748001 4 20070704 A 2565 SLIDE BOEING 747 747206B 1384856 NM UNWANTED DEPLOY A Q2SA O OTHER O OTHER NR NOT REPORTED 1 EA 63 748SA 21110 INADVERTENTLY DEPLOYED RIGHT SIDE UPPER DECK SLIDE WHILE AIRCRAFT WAS PARKED AT KMIA. REMOVED SLIDE IN ACCORDANCE WITH AMM 25-68-07. TRANSFERRED TO DI LOG #12408 IN ACCORDANCE WITH MEL 25-11. PLACARD INSTALLED. SLIDE DEPLOYED WITHOUT AN Y MALFUNCTION. 2 L 7 4 4F RT A20WE 2007071200083 20070712 00083 SO 2007 7 12 C2XA07RI050 1 20070603 A 3350 110049 CHARGER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SW 27 16571 145633 FLT 2550 - EWR - CREW REPORTED NR 2 EMERGENCY CEILING PANEL LIGHT AND RT OVERWING EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED BATTERY CHARGER ASSY NR 2 IAW EMB AMM 33-50-04 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007071200093 20070712 00093 NM 2007 7 12 F3LA200700147 1 20070627 A 5320 TRANSITION PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT TRANSITION PANEL 131CF DAMAGED. REPAIRED TRANSITION PANEL 1 31CF IAW SRM 53-02-00, FIG 204. 2 L 7 2 4F RT A28NM 2007071200112 20070712 00112 NM 2007 7 12 F3LA200700162 1 20070628 A 5320 TRANSITION PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT TRANSITION PANEL 161CF DAMAGED. REPAIRED PUNCTURES IN TRANS ITION PANEL 161CF IAW SRM 53-02-00, PB 201, PARA 8 C., FIG 204. 2 L 7 2 4F RT A28NM 2007071200115 20070712 00115 WP 2007 7 12 ARWA20070701 1 20070704 A 3242 26014120 BRAKE ASSY DOUG DC8 DC863F 302198F WP MLG LOCKED A ARWA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 19 441J 45988 AFTER LANDING, ON TAXI TO RAMP, BRAKES "LOCKED UP". REMOVED AND REPLACED BRAKE ASSEMBLY NR 2 IN ACCORDANCE WITH DC-8 M/ M 32-42-1. OPERATIONAL CHECK FOR LEAKS OK. 2 L 7 4 4F 4A25 2007072300086 20070723 00086 WP 2007 7 23 ARWA20070702 1 20070705 A 3240 26014122 BRAKE ASSY DOUG DC8 DC863F 302198F WP MLG DAMAGED A ARWA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 19 441J 45988 WHILE TAXING TO RAMP, AFTER LANDING, BRAKES LOCKED UP. NR 5 BRAKE ASSEMBLY LOCKED UP ON TAXI WAY. REMOVED AND REPLACED NR 5 ANTI-SKID WHEEL SPEED TRANSDUCER IAW MM 32-43-2. NR 5 MAIN WHEEL ANTI-SKID TRANSDUCER DAMAGED. REMOVED AND REPLACED NR 5 BRAKE ASSEMBLY IAW MM 32-42-1; PERFORMED BLEEDING AND SERVICED IAW DC8 MM 32-42-1 PERFORMED OPERATIONAL CHECK IAW MM 32-43-0, FOUND NORMAL. 2 L 7 4 4F 4A25 2007071200139 20070712 00139 NM 2007 7 12 UPS07450034 1 20070601 A 5311 FRAME BOEING 747 747212B 1384886 NM BS 800 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C BS 800 RT SIDE AT STR16 INNER CHORD 1 HOLE FOUND CRACKED AT 9 O/C POSITION WITH LENGTH 0.125" LENGTH. M/D BS 800 RT SIDE FRAME FWD INNER CHORD AND STRAP REPAIRED AT BETWEEN STR 15R TO STR 18R AREA AS PER RS R53-21-35812. POST REPAIR INSPECTION ARE REQUIRED AS PER RS R53-21-35812 AND UPS EO B747-5310-27072. 2 L 7 4 4F A20WE 2007071200140 20070712 00140 NM 2007 7 12 UPS07450035 1 20070602 A 5311 FRAME BOEING 747 747212B 1384886 NM BS 800 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C NR 2 DOOR FWD FRAME AT BS 800 RT SIDE FOUND CRACKED AT NR 5 AND NR 6 FAST HOLE BELOW STR 16 BOTH HOLE CRACKED AT STRAP WITH LENGTH 0.040" RUNNING AFTWARD. BS 800 RT SIDE FRAME FWD INNER CHORD AND STRAP REPAIRED AT BTN STR 15T TO STR 18R AREA AS PER RS R53-21-35812. POST REPAIR INSPECTION ARE REQUIRED AS PER RS R53-21-35812. WORKING DETAI L REFER NRC50958 AND REFER UPS EO B747-5310-27072. 2 L 7 4 4F A20WE 2007071200142 20070712 00142 NM 2007 7 12 UPS07450037 1 20070601 A 5313 STRINGER BOEING 747 747212B 1384886 NM BS 740 S36L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C FWD CARGO COMPT S36L STRINGER FOUND CORROSION AT STA 740. CORROSION BLEND OUT 0.045" BY 1/2" BY 2" EX CEED SRM LIMIT. FWD CARGO COMPT BS 740 TO BS 770 STR 36L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 2007071200144 20070712 00144 NM 2007 7 12 UPS07450039 1 20070529 A 5320 FILLER BOEING 747 747212B 1384886 NM BS 940 S8L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C CRACK FOUND AT BS 940 S8L TENSION TIE AT HOLE NR 11 THE CRACK WAS FOUND THROUGH THICKNESS AT THE FILLE R. CRACK LENGTH 3/8". M/D BS 940 LT FRAME TENSION TIE ATTACH FILLER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AN D UPS EO B747-5310-23715-C. 2 L 7 4 4F A20WE 2007071200151 20070712 00151 NM 2007 7 12 UPS07450049 1 20070626 A 2170 WATER SEPARATOR BOEING 747 747123 1384873 NM NR 3 PACK CRACKED A IPXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 672UP 20324 ATB - AFTER T/O, NR 3 PACK WOULD NOT OPERATE. ZERO AIRFLOW. NO FUNCTION. SWITCHES AND C/B'S RECYCLED. TRIED IN MAN/AU TO. NO HELP. NOTE: ISOLATION A BLEED VALVES OPEN WITH NORMAL DUCT PRESSURE. T/S PERFORMED. FOUND NR 3 PACK WATER SEP ARATOR FROZEN UP. WATER BAG CLEANED AND RE-INSTALLED. F/C NR 3 PACK AS PER MM 21-50-00. FOUND NR 3 WATER SEPARATOR DR AIN LINE WITH SMALL CRACK. DRAIN LINE TEMP REPAIR PERFORMED. DEFERRED UNDER D353304. 2 L 7 4 4F A20WE 2007071200154 20070712 00154 WP 2007 7 12 UPS07850050 1 20070623 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 C3 L/WING LEADING EDGE OUTBD LWR RIB CRACKED AT STA XFS 772. STOP DRILLED CRACK ON RIB AT STA XFS 772 L/WING LEADING ED GE IAW SRM 57-02-00 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER AT STA XFS 772 L/WING LEADING EDGE IAW SRM 57-03-0 1-0 FIG 007. 2 L 7 4 4F RT 4A25 2007071200161 20070712 00161 NM 2007 7 12 UPS07M50059 1 20070416 A 5313 LONGERON DOUG MD11 MD11 3023602 NM BS 5-128 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C CTR CARGO COMPT AT STATION 5-128 LONGERON 43 RT FOUND SUSPECTED CRACK ON DOUBLER AREA AS MARKED. HFEC INSP C/OUT PER DAC NDT SPM REV 13 PART 06-10-01-001 ON DOUBLER FOUND CRACK. CRACK LONGERON SPLICE AT CTR CGO STA5-128 L43RH REMOVED. NEW SPLICE P/N A5A7114.535 FAB PER DWG A5A7114. FPI C/OUT ON NEW SPLICE FOUND NO CRACK. NEW SPLICE FAS TENER HOLES PICKED UP, REPROTECTED AND PAINTED. NEW FAB SPLICE INSTALLED AND REWORK AREA PAINTED. 2 L 7 3 4F RT A22WE 2007071200174 20070712 00174 WP 2007 7 12 UPS07850079 1 20070622 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 R/WING CENTER L/E UPPER RIB CRACKED AT STA XFS 360. STOPPED DRILLED CRACKED RIB AT R/WING L/E STA XF S 360 IAW SRM 57-03 -03-0 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER AT R/WING STA XFS360 IAW SRM 57-03-03-0 FIG 2. 2 L 7 4 4F RT 4A25 2007071200176 20070712 00176 WP 2007 7 12 UPS07850081 1 20070622 A 5710 DOUBLER DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 R/WING OUTBD L/E UPPER AND LWR INNER DOUBLER CRACKED AT STA XW 761. REMOVED CRACKED DOUBLERS AT R/WI ND L/E STA XW 761 IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR DOUBLERS AT R/WING L/E STA XW 761 IAW SRM 51-01-20D, AND DWG 5769545. 2 L 7 4 4F RT 4A25 2007071200187 20070712 00187 NM 2007 7 12 UPS07M50073 1 20070508 A 5310 WEB DOUG MD11 MD11 3023602 NM COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C COCKPIT, 1ST OBSERVER SEAT SUPPORT WEB FOUND CRACKED. COCKPIT 1ST OBS SEAT SUPPORT WEB CRACKED AREA T RIMMED OFF PER SRM 53-00-01 VOLI REV 39. HFEC INSP C/OUT ON TRIMMED OFF AREA, NO CRACK REINFORCED DOUBLER FAB PER SRM 5 3-00-01 VOLI FIG 6 REV 39. FASTENER HOLES PICKED UP AND ALODINE C/OUT ON FAB DOUBLER. FAB DOUBLER INSTALLED PER SRM 53 -00-01 VOL I REV 39 AND SRM 51-35-01 VOLII REV 39. 2 L 7 3 4F RT A22WE 2007071200188 20070712 00188 NM 2007 7 12 UPS07M50074 1 20070418 A 5712 RIB DOUG MD11 MD11 3023602 NM RT WING 657-714 DEFORMED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C RT WING LOWER SURFACE FIXED L/E COMPARTMENT BETWEEN STA XOS 657 AND XO S 714 APPROX FOUND 04 SUPPORT R IB DEFORMED. 4 SUPPORT DEFORMED RIBS REMOVED. NEW SUPPORT RIBS FAB PER DWG ARB2924-8, ARB2924-6, ARB2924-4 AND ARB2930 -16. RIBS HEAT TREATED AND HARNESS VALUES TO T6 COND. NEW RIBS FASTENER HOLES P/U, REPROTECT AND PAINTED. NEW RIBS 04 INSTALLED PER SRM 51-31-01 VOLII REV 38 AND DWG ARB2924 AND ARB2930. 2 L 7 3 4F RT A22WE 2007071200192 20070712 00192 SO 2007 7 12 SIMA200718602 1 20070701 A 2130 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN PRESSURE UNKNOWN A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 674RJ 14500801 AUTO PRESSURE CONTROL INOPERATIVE, DIVERTED TO ACT. PERFORMED OPERATIONAL OF PRESSURE CONTROL SYSTEM IN AUTO MODE IAW E MB AMM 21-31-00 WITH NO DEFECTS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007071200193 20070712 00193 SO 2007 7 12 SIMA200718701 1 20070704 A 3297 D3899926KA98 CONNECTOR EMB 135 EMB135KL 3260302 SO ZONE 700 DAMAGED A SIMA O OTHER O OTHER LD LANDING 1 SW 21 827AE 12658 145602 CLUNK SOUND HEARD JUST BEFORE TOUCHDOWN FOLLOWED BY LOUD BANGING NOISE DURING TAXI. INSPECTED GROUND CONNECTOR P0040 FO UND UNSERVICEABLE. REMOVED AND REPLACED CONNECTOR IAW EMB SPWM 20-50-00 AND EMB 32-63-05. OPERATIONAL CHECK GOOD, RETU RNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300011 20070713 00011 EA 2007 7 13 COMA0760453 1 20070625 A 3350 362624 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 720SW 7297 FLIGHT 5523 - EMERGENCY FLOOR LIGHTING INOP BETWEEN SEATS 6 AND 8. REMOVED AND REPLACED EMERGENCY LIGHTING LAMP STRIP. 2 L 7 2 4F RT A21EA 2007071300023 20070713 00023 EA 2007 7 13 TRAX200700902 1 20070627 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 870AS 7530 CORROSION FOUND ON LOWER SILL OF PAX DOOR FS 319 AND FS 335. 2 L 7 2 4F RT A21EA 2007071300030 20070713 00030 NM 2007 7 13 ASAA0791825 1 20070621 A 5330 147A31101 SKIN BOEING 737 737990 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 FUSELAGE SKIN GOUGED 22 INCHES AFT OF L2 DOOR 18 INCHES UP FROM BOTTOM OF L2 DOOR CUTOUT. TEMP REPAIR INSTALLED PER ASA EA 5330 02215. 2 L 7 4 4F RT A16WE 2007071300039 20070713 00039 NM 2007 7 13 USAA070507 1 20070629 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 BS 312 AT LBL 7 TO RBL 8, TOP CHORD OF FLOORBEAM HAS CORROSION. REMOVED DAMAGED T-CAP & REPLACED WITH NEW PART PER SRM 53-51-51, 51-20-01; CORR TASK C53-107-02; DEFECT SIZE: 15 INCHES. 2 L 7 2 4F RT A16WE 2007071300041 20070713 00041 NM 2007 7 13 QXEA200701079 1 20070702 A 6120 30005000056 TSCU DHAV DHC8 DHC8202 2809007 NM NR 2 MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 369PH 513 EUG FLIGHT NR 2118 AUTO FEATHER ARM LIGHT FAILED TO ILLUMINATE DURING TAKEOFF ROLL (AUTO FEATHER SYSTEM INOP). REPLACED THE NR 2 TSCU IAW P/W MM 72-01-10, PAGE 420-424, PARAGRAPH 7. GROUND RUNS COMPLIED WITH. OPERATIONAL CHECK GOOD. AIR CRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071300042 20070713 00042 NM 2007 7 13 AALA20071175 1 20070626 A 3350 LIGHT BOEING 757 757231 1384950 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 717TW 28485 DFW - EMERGENCY LIGHT AT LAVATORY D INOP WITH BOTH ENDS TRACK LIGHT MISSING. REPLACED PATH FLOOR EMERGENCY LIGHTING AT L AVATORY D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071300043 20070713 00043 NM 2007 7 13 AALA20071176 1 20070626 A 3350 LIGHT BOEING 757 757231 1384950 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 717TW 28485 DFW - EMERGENCY LIGHT AT SEAT 7D INOP WITH TRACK LIGHT END PLUG MISSING. REPLACED PATH FLOOR EMERGENCY LIGHTING AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071300046 20070713 00046 NM 2007 7 13 AALA20071181 1 20070626 A 2760 CABLE BOEING 737 737823 13844BZ NM GROUND SPOILERS BROKEN A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 957AN 29541 RDU INFLIGHT T1541/26JUN - RECEIVED LANDING GEAR WARNING AND MANUAL OVERRIDE OF GEAR HANDLE FOR RETRACTION. LANDED RDU WITHOUT INCIDENT. REPLACED BROKEN GROUND SPOILER LOCKOUT VALVE CABLE. 2 L 7 2 4F RT A16WE 2007071300047 20070713 00047 WP 2007 7 13 AALA20071182 1 20070626 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7549A 53031 LGA - EMERGENCY CEILING LIGHTS AT TAIL COMPARTMENT AFT LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY CEILIN G LIGHTS AT TAIL COMPARTMENT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071300048 20070713 00048 NM 2007 7 13 HNAA0700130 1 20070628 A 3234 CONTROL HANDLE DHAV DHC8 DHC8102 2809003 NM COCKPIT FAULTY A HNAA A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 EA 07 838EX 220 CREW SELECTED GEAR DOWN AND GOT THREE RED LIGHTS. DIVERTED THE LANDING AND TRIED THE ALTERNATE GEAR EXTENSION, WHICH BR OUGHT THE LANDING GEAR DOWN WITH 3 GREEN LIGHT. INSP INHIBIT SWITCH, L/G SELECTOR VALVE C/P AND WIRING, NO DEFECTS NOTE D. REMOVED AND REPLACED L/G SELECTOR HANDLE. CYCLED GEAR TEN TIMES. CHECKED MEMORY ON PSEU, NO FAULTS. OPS CHECK GOO D. 2 H 7 2 4T RT A13NM 2007071300050 20070713 00050 WP 2007 7 13 AALA20071188 1 20070627 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 573AA 53092 SFO - EMERGENCY LIGHTS AT SEAT ROWS 21D TO 32D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 21D TO 32D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071300051 20070713 00051 EU 2007 7 13 BA07008 1 20070628 A 2910 O-RING AIRBUS 330 A330323 3930335 EU HYDRAULIC SYS DAMAGED A USAA K NONE K FLUID LOSS CR CRUISE 1 EA 19 271AY 0323 FLIGHT 731, LGW-PHL: DURING CRUISE, GREEN HYDRAULIC SYSTEM QUANTITY BEGAN DROPPING. CAPTAIN DECLARED EMERGENCY INBOUND TO PHL. FLIGHT LANDED WITH NO DIFFICULTIES. MAINTENANCE REPLACED AN O-RING ON THE GREEN SYSTEM HIGH PRESSURE FILTER M ODULE. 2 L 7 2 4F RT A46NM 2007071300052 20070713 00052 WP 2007 7 13 AALA20071189 1 20070627 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 573AA 53092 SFO - EMERGENCY LIGHT AT AFT AIR STAIRS INOPERATIVE. REPLACED BATTERY PACK AT AFT SERVICE DOOR FOR EMERGENCY LIGHT AT A FT AIR STAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007071300053 20070713 00053 NM 2007 7 13 AALA20071184 1 20070627 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 666A 25300 LAX - EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. SECURED LOOSE CONNECTION FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007071300056 20070713 00056 NM 2007 7 13 AALA20071187 1 20070607 A 3397 PIN BOEING 767 767323 1385205 NM EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 394AN 29431 DFW - EMERGENCY LIGHT AT SEAT 37H INOPERATIVE. SECURED LOOSE CONNECTION FOR EMERGENCY LIGHT AT SEAT 37H. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007071300059 20070713 00059 NM 2007 7 13 AALA20071196 1 20070628 A 3397 WIRE HARNESS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 363AA 24044 ORD - EMERGENCY LIGHT AT SEAT ROW 13HJ INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHT AT SEAT ROW 13HJ. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007071300062 20070713 00062 NM 2007 7 13 BB07047 1 20070629 A 3350 20121 CHARGER BOEING 767 7672B7 1385107 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 256AY 26847 FLOOR LEVEL EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. NO FURTHER FAULTS. 2 L 7 2 4F RT A1NM 2007071300063 20070713 00063 NM 2007 7 13 AALA20071191 1 20070627 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT SEAT 20C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT T00001SE 2007071300065 20070713 00065 NM 2007 7 13 AALA20071194 1 20070628 A 3350 WIRE HARNESS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 363AA 24044 ORD - EMERGENCY LIGHT AT SEAT ROW 11HJ INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHT AT SEAT ROW 11HJ. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007071300069 20070713 00069 SO 2007 7 13 SWIA200718426 1 20070628 A 2710 BELLCRANK EMB 120 EMB120ER 3260203 SO AILERON CONTROL WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 295SW 120322 FLT 5788 - THE YOKE FEELS AS THOUGH IT FALLS INTO A DETENT IN THE CENTER POSITION. REPLACED LEFT AILERON BELLCRANK AND AILERON SPIGOT BEARING IAW EMB 120 MM 27-11-05. 2 L 7 2 4T RT A31SO 2007071300070 20070713 00070 SO 2007 7 13 SWIA200718427 1 20070323 A 5620 WINDOW EMB 120 EMB120ER 3260203 SO CABIN SCRATCHED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 569SW 120344 PAX WINDOW 11BC HAS TWO HEAVY SCRATCHES ON THE OUTER PANE, DISCOVERED AT C-CHECK. REPLACED PAX WINDOW AT 11BC IAW AMM 5 6-20-00. 2 L 7 2 4T RT A31SO 2007071300071 20070713 00071 SO 2007 7 13 SWIA200718428 1 20070323 A 5210 ATTACH FITTING EMB 120 EMB120ER 3260203 SO PAX DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 569SW 120344 PAX DOOR FORWARD AND AFT CAM LINK ATTACH HARDWARE IS CORRODED, DISCOVERED AT C-CHECK. REPLACED HARDWARE AT PAX DOOR CAM LINKS AND BUSHINGS IAW 52-11-03. 2 L 7 2 4T RT A31SO 2007071300077 20070713 00077 EU 2007 7 13 MAC070702 1 20070626 A 5751 TEE FITTING AEROSP AEROSP ATR42 ATR42300 8680920 EU AILERON CORRODED A MTNA K NONE O OTHER IN INSP/MAINT 1 SO 33 916FX 1257 314 DURING INSPECTION, LEVEL 2 CORROSION WAS FOUND ON A T-FITTING IN THE AILERON S/N 1257 P/N S57610250-001, MFG DATE 08/92. THE -T- REPLACED HAD EXFOLIATION CORROSION ALONG THE FITTING EDGES. LOCATED AT THE CENTER OUTBOARD SECTION. REF ATR4 2 SRM 57-61-10 FIG 101. REASON FOR INSPECTION: MRB 576108-01 (8 YEAR INTERVAL). 2 H 7 2 4T RT A53EU 2007071300078 20070713 00078 NM 2007 7 13 SWAA073271 1 20070630 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 DURING SCHEDULED MV3 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007071300079 20070713 00079 NM 2007 7 13 SWAA073261 1 20070629 A 3350 101114 COVER BOEING 737 7373A4 1384585 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 FWD CABIN EMERGENCY EXIT SIGN COVER LOOSE. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007071300080 20070713 00080 NM 2007 7 13 SWAA073277 1 20070701 A 3350 1619 LAMP BOEING 737 7373K2 13844BA NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007071300081 20070713 00081 NM 2007 7 13 SWAA073263 1 20070629 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED MV1 CHECK, FOUND LT AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007071300083 20070713 00083 NM 2007 7 13 SWAA073262 1 20070629 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007071300084 20070713 00084 NM 2007 7 13 SWAA073275 1 20070701 A 3350 311500 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 714CB 27848 L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007071300085 20070713 00085 NM 2007 7 13 SWAA073272 1 20070630 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 237WN 34632 EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007071300086 20070713 00086 2007 7 13 SWAA073274 4 20070701 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 458WN 33857 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071300087 20070713 00087 2007 7 13 SWAA073276 4 20070701 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 736SA 27868 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071300088 20070713 00088 2007 7 13 SWAA073260 4 20070629 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 245WN 32506 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007071300089 20070713 00089 NM 2007 7 13 SWAA073279 1 20070701 A 5320 6546547 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 727, LBL 19. REMOVED AND REPLACED VERTICAL STIFFENE R PER SRM. 2 L 7 2 4F RT A16WE 2007071300090 20070713 00090 NM 2007 7 13 SWAA073266 1 20070629 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071300093 20070713 00093 NM 2007 7 13 SWAA073281 1 20070701 A 5754 65C26601 SKIN BOEING 737 7373H4 1384600 NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED SPV CHECK, FOUND LT WING NR 1 L/E SLAT LOWER SKIN CRACKED AT OUTBOARD AUX TRACK. REPAIRED SLAT PER SRM . 2 L 7 2 4F RT A16WE 2007071300097 20070713 00097 NE 2007 7 13 SWAA073270 2 20070630 A 7230 COMPRESSOR CFMINT BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B22 13802 NE NR 1 ENGINE STALLED A SWAA K NONE R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 29 766SW 874112 29806 874112 ON CLIMBOUT OF MCO NR 1 ENGINE EXPERIENCED COMPRESSOR STALL. ENGINE PARAMETERS NORMAL. REMOVED AND REPLACED NR 1 ENGIN E PER MT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007071300098 20070713 00098 EA 2007 7 13 QXEA200701025 1 20070623 A 4990 38824961 FILTER CNDAIR CL600 CL6002C10 1390015 EA APU FUEL UNKNOWN A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 612QX 10042 PDX - AFTER TAKEOFF ON FLIGHT 2527, THE APU FAULT CAUTION ILLUMINATED ALONG WITH AUTO SHUTDOWN OF THE APU. DUE TO ONE I DG ALREADY BEING ON MEL, RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE APU FUEL FILTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007071300100 20070713 00100 EA 2007 7 13 QXEA200701034 1 20070626 A 3240 60072934 VALVE CNDAIR CL600 CL6002C10 1390015 EA RT BRAKE MALFUNCTIONED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 614QX 19445 10049 PDX - RIGHT BRAKE WEAK. MAINTENANCE REPLACED THE ANTI-SKID CONTROL VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007071300101 20070713 00101 EA 2007 7 13 QXEA200701069 1 20070627 A 4900 P760A154E002 RELAY CNDAIR CL600 CL6002C10 1390015 EA APU BATTERY MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 604QX 10019 PDX - FLIGHT 2575, RETURNED TO THE GATE FOR THE APU BATTERY POPPED THE CIRCUIT BREAKER AFTER ENGINE START. MAINTENANCE REPLACED THE K101 RELAY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007071300102 20070713 00102 EA 2007 7 13 QXEA200701027 1 20070625 A 2613 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA BRAKE OVERHEAT UNKNOWN A QXEA O OTHER O OTHER AP APPROACH 1 NM 09 609QX 10031 DEN - ON APPROACH, THE BRAKE OVERHEAT MESSAGE ILLUMINATED, COMPLIED WITH THE CHECKLISTS AND THE MESSAGE WENT OUT AND DID NOT RETURN. MESSAGE WAS FOR THE RIGHT OUTBOARD BRAKE. MAINTENANCE PERFORMED A OPERATIONAL TEST WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007071300109 20070713 00109 EA 2007 7 13 QXEA200701075 1 20070629 A 2610 47388904 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA FIRE WARNING MALFUNCTIONED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 618QX 7030 10205 DEN - RECEIVED A INTERMITTENT FIRE SYSTEM WARNING FAULT MESSAGE. MAINTENANCE REPLACED THE FIDEX CONTROL UNIT. OPERATION AL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007071300110 20070713 00110 EA 2007 7 13 TRAX200700893 1 20070625 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 871AS 7537 FS 280 FLOORBEAM ATTACHMENT CLIP ON I/B SIDE OF RBL 27.0 IS CRACKED. REMOVED DAMAGED ANGLE & FS 280 RBL 9.0 I/B SIDE DU PLICATED SERVICEABLE ANGLE FROM 2024-T3 .050 PO10404 LOCATED AND DEBURRED IAW CRJ SRM 53-21-43. ALODINED AND PRIMED SER VICEABLE ANGLE IAW CRJ SRM 51-25-06. TOP COATED AND INSTALLED SERVICEABLE ANGLE WITH HST 10AG-5, HILITES AND KFM 586-08 NUTS IAW CRJ SRM 51-42-21. SUPPLEMENTAL - SDR CLOSED 07/03/07. 2 L 7 2 4F RT A21EA 2007071300116 20070713 00116 NM 2007 7 13 UPS07550121 1 20070704 A 3350 LAMP BOEING 757 75724APF 1384969 NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 457UP 25478 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED, OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2007071300117 20070713 00117 WP 2007 7 13 UPS07850095 1 20070619 A 5330 SKIN DOUG DC8 DC871F 302199D WP FS 1742 L17L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 FUSELAGE EXTERIOR SKIN CRACKED AT STA 1742 L17L. CUT OUT DAMAGED AREA OF FUSELAGE SKIN AT STA 1742 L 17L IAW SRM 53-02-01-0 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER, FINGER DOUBLER, AND FILLERS AT STA 1742 L17L IAW SRM 53-03-02-0 FIG 7. 2 L 7 4 4F RT 4A25 2007071300120 20070713 00120 EA 2007 7 13 TRAX200700900 1 20070627 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 870AS 7530 CRACK FOUND ON CLIP FS 280 LBL 9 AND RBL 9. NEW CLIP INSTALLED AS PER SRM 51-42-20. SUPPLEMENATAL- SDR CLOSED 07/03/07 . 2 L 7 2 4F RT A21EA 2007071300121 20070713 00121 WP 2007 7 13 UPS07850097 1 20070622 A 5313 FITTING DOUG DC8 DC871F 302199D WP FS 1770 L10R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 LONGERON END FITTING AT STA 1770 L10R IS CRACKED. REMOVED CRACKED END FITTING AT STA 1770 L10R IAW S RM 51-1-21. LOCATED, DRILLED-UP, AND INSTALLED LONGERON END FITTING AT STA 1770 L10R IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007071300125 20070713 00125 NM 2007 7 13 USAA920070793 1 20070628 A 5754 114N4003 SKIN BOEING 757 7572B7 1384964 NM L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 939UW 27303 BMH - MAJOR REPAIR - C-4 CHECK - NR 6000784, RIGHT WING LEADING EDGE SLAT NR 9 INNER SKIN CRACKED, WS 623.5. REPLACED R IGHT WING LEADING EDGE SLAT NR 9 INNER SKIN CRACKED, WS 623.5 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007071300126 20070713 00126 EU 2007 7 13 USAA070521 1 20070703 A 5320 D5348004320501 BEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 182UW 1536 FWD END OF RIGHT (R4) SILL BEAM ABOVE FR C66. DAMAGED AREA CUTOUT AND REPAIRED PER SRM REPAIR, SRM 53-41-14; CORR TASK JA-260-53500, LEVEL 1, DEFECT SIZE: 1 X 1.25 INCH. 2 L 7 2 4F RT A28NM 2007071300129 20070713 00129 NM 2007 7 13 SWAA073282 1 20070702 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 416WN 32453 EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007071300134 20070713 00134 NM 2007 7 13 NWAA072425519 1 20070707 A 5414 SKIN BOEING 757 757251 1384970 NM NR 2 NACELLE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 519US 23207 DURING SCHEDULED NR 2 ENGINE CHANGE FOUND CRACK IN PYLON SIDE SKIN AT NAC STA 128. REPAIRED PER EA 55-210070 SECTION I, SECTION II TO BE ACCOMPLISHED WITHIN 24 MONTHS OF SECTION I. 2 L 7 2 4F RT A2NM 2007071300135 20070713 00135 SO 2007 7 13 SIMA200719117 1 20070522 A 5347 13500439007 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 15926 5000 145224 LEFT INBOARD SEAT TRACK BETWEEN FRAME 17 AND 23 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURN ED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300136 20070713 00136 SO 2007 7 13 SIMA200719119 1 20070603 A 5347 14530658007 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 15957 145235 RIGHT INBOARD SEAT TRACK BETWEEN FRAME 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETUR NED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300137 20070713 00137 SO 2007 7 13 SIMA200719118 1 20070603 A 5347 14530659007 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 15957 5000 145235 LEFT INBOARD SEAT TRACK BETWEEN FRAME 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETURN ED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300140 20070713 00140 SO 2007 7 13 SIMA200719108 1 20070522 A 5347 13500439011 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 15926 5000 145224 LEFT INBOARD SEAT TRACK BETWEEN FRAME 24 AND 36 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND AMER ICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-110R2. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300141 20070713 00141 SO 2007 7 13 SIMA200719113 1 20070522 A 5347 13500439003 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 15926 5000 145224 LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 24 AND 36 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETUR NED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300143 20070713 00143 SO 2007 7 13 SIMA200719116 1 20070522 A 5347 13500438001 SEAT TRACK EMB 135 EMB135LR 3260305 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TB 15926 5000 145224 RIGHT INBOARD SEAT TRACK BETWEEN FRAME 24 AND 36 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. RETUR NED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071300145 20070713 00145 2007 7 13 HNAA0700129 4 20070628 A 3418 C809072 TRANSDUCER DHAV DHC8 DHC8102 2809003 NM STALL WARNING MALFUNCTIONED A HNAA D RETURN TO BLOCK N FALSE WARNING CL CLIMB 1 EA 07 906HA 9 JUST AFTER ROTATION FROM LGA, THE STICK SHAKER WENT OFF. CAPTAIN QUICKLY RETURNED TO THE FIELD. CAPTAIN'S STALL WARNIN G HAS A PROBLEM. REMOVED AND REPLACED NR 1 STALL WARNING TRANSDUCER. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007071300146 20070713 00146 NM 2007 7 13 2007UALA02356 1 20070629 A 3350 BATTERY PACK BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE L2 DOOR UNRELIABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 DOOR 2L EPAS BATTERY PACK -DATE LAST SERVICED OR MFG- IS UN-READABLE. [07-27-07] REPLACED DOOR 2L EPAS BATTERY PACK. AIRCRAFT READY FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007071300147 20070713 00147 NM 2007 7 13 HNAA0700132 1 20070529 A 5330 SKIN PANEL DHAV DHC8 DHC8102 2809003 NM FUSELAGE DEBONDED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 912HA 040 DISBOND DETECTED ON LEFT FUSELAGE SKIN PANEL BETWEEN FUSELAGE STA 488.50 AND STA 510.00 AND BETWEEN STR 23 AND STR 24. 2 H 7 2 4T RT A13NM 2007071300154 20070713 00154 SO 2007 7 13 SWIA200718435 1 20070602 A 5210 FRAME EMB 120 EMB120ER 3260203 SO PAX DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 579SW 120347 PAX DOOR FORWARD UPPER CORNER FRAME IS CORRODED, DISCOVERED AT C-CHECK. REPLACED FORWARD CORNER FRAME WITH NEW PART IAW EMB 120 SRM 51-40-02, P/N 120-26550-001. 2 L 7 2 4T RT A31SO 2007071300155 20070713 00155 SO 2007 7 13 SWIA200718436 1 20070602 A 5210 FRAME EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 579SW 120347 PAX DOOR CENTER FORWARD FRAME IS CRACKED, DISCOVERED AT C-CHECK. REPLACED CENTER FORWARD FRAME IAW SRM 51-40-02, PN 120 -21058-003. 2 L 7 2 4T RT A31SO 2007071300158 20070713 00158 SO 2007 7 13 SWIA200718438 1 20070519 A 5210 FRAME EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 235SW 120310 PAX DOOR HAS CRACK ON FORWARD SIDE AT FRAME 3, DISCOVERED AT C-CHECK. REPAIRED CRACKED BRACKET IAW EMB SRM 52-10-02 FIG 203. 2 L 7 2 4T RT A31SO 2007071300159 20070713 00159 SO 2007 7 13 SWIA200718439 1 20070519 A 5210 FRAME EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 235SW 120310 PAX DOOR HAS A CRACK NEAR FRAME 5 ON FORWARD SIDE, DISCOVERED AT C-CHECK. NEW FRAME INSTALLED IAW SRM 120 51-10-02 PG 3 SEC 3A. 2 L 7 2 4T RT A31SO 2007071300160 20070713 00160 NM 2007 7 13 HNAA0700134 1 20070606 A 5521 15520140005 FAILSAFE DHAV DHC8 DHC8102 2809003 NM RT ELEVATOR CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 912HA 040 RIGHT ELEV O/B HINGE FAIL SAFE CORRODED. 2 H 7 2 4T RT A13NM 2007071300164 20070713 00164 NM 2007 7 13 HNAA0700135 1 20070508 A 5320 DOUBLER DHAV DHC8 DHC8102 2809003 NM FUSELAGE DEBONDED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 937HA 148 DOUBLER UNDER STR 25 IS DISBONDED IN FRAME BAYS X424 TO X467. 2 H 7 2 4T RT A13NM 2007071300167 20070713 00167 NM 2007 7 13 HNAA00138 1 20070509 A 5320 DOUBLER DHAV DHC8 DHC8102 2809003 NM FUSELAGE DEBONDED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 937HA 148 DOUBLER UNDER STR 28S IS DISBONDED IN FRAME BAYS X424 TO X434. 2 H 7 2 4T RT A13NM 2007071300169 20070713 00169 SO 2007 7 13 SWIA200718445 1 20070505 A 5620 TRACK EMB 120 EMB120 3260201 SO LT DV WINDOW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 216SW 120285 LEFT DV WINDOW SUPPORT BRACKET UNDER FORWARD TRACK IS CRACKED IN TWO AREAS, DISCOVERED AT C-CHECK. SPLICED REPLACEMENT SECTION AFT OF STRINGER 9L TO WINDOW SILL AND REPLACED END CLIPS PER EMB SRM 53-10-04 AND 51-40-02. 2 L 7 2 4T RT A31SO 2007071300171 20070713 00171 EA 2007 7 13 HNAA0700136 1 20070504 A 5320 DOUBLER DHAV DHC7 DHC7102 2802708 EA FUSELAGE DEBONDED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 937HA 148 DOUBLER UNDER STR 28 IS DISBONDED IN FRAME BAYS X424 TO X434. 2 H 7 4 4T A20EA 2007071300172 20070713 00172 EA 2007 7 13 SWIA200718447 1 20070702 A 2150 GG670950095 ACM CNDAIR CL600 CL6002C10 1390015 EA RIGHT SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 706SK 2559 2559 10149 FLT 6694 - EXPERIENCED WHITE SMOKE FROM ENVIRONMENTAL DUCTS FOLLOWED BY A RIGHT PACK AUTO FAIL MESSAGE. REPLACED THE RI GHT AIR CYCLE MACHINE IAW MM 21-51-08. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007071300173 20070713 00173 NM 2007 7 13 HNAA0700137 1 20070504 A 5320 DOUBLER DHAV DHC8 DHC8102 2809003 NM FUSELAGE DEBONDED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 937HA 148 DOUBLER UNDER STR 26S IS DISBONDED IN FRAME BAYS X424 TO X445. 2 H 7 2 4T RT A13NM 2007071100057 20070711 00057 EU 2007 7 11 07FDEA02358 1 20070702 A 5755 FASTENER AIRBUS AIRBUS 300 A300B4605R 3930308 EU NR 5 SPOILER WRONG PART A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 731FD TS0863 709 FOUND FASTENER WRONG INSTALLED ON SPOILER NR 5 RT, P/N 577-71000-004, S/N TS0863 IAW SB A300-57-6082. REPAIR PERFORMED BY INSTALLING THE ORIGINAL FASTENER AND FILLOUT THE MISDRILLED HOLE IAW EA 6-5770-106475 AND RAS/DABRE/7007745/2007 ISS A. 2 L 7 2 4F RT A35EU 2007071100065 20070711 00065 NM 2007 7 11 2007UALA02325 1 20070701 A 5241 TORQUE TUBE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR EXCESS PLAY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 FWD GALLEY DOOR UPPER AND LOWER LATCH TORQUE TUBE HAVE EXCESSIVE LATERAL PLAY. INSTALLED SHIMS AT BOTH UPPER & LOWER LA TCH TORQUE TUBES. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071100066 20070711 00066 CE 2007 7 11 DXTA200702287 1 20070622 A 3150 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MASTER WARNING UNKNOWN E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 933QS 7500133 MASTER WARNING ILLUMINATED DURING TAKEOFF ROLL JUST ABOVE 80 KTS. [07-12-07] REPLACED LOWER YAW DAMP "B" ACTUATOR AND OPS CHECKED IAW 750 M/M 27-24-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071100070 20070711 00070 2007 7 11 2007UALA02328 4 20070630 A 2565 FLANGE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE ESCAPE SLIDE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 831UA 1291 LEFT OFFWING ESCAPE SLIDE HAS A CRACK IN VERTICAL AFT FLANGE LOWER END. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100072 20070711 00072 NM 2007 7 11 2007UALA02329 1 20070630 A 5210 BOTTLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 847UA 1627 DOOR 2L DOOR ASSIST BOTTLE DIAPHRAGM BLOWN. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100084 20070711 00084 EU 2007 7 11 2007UALA02331 1 20070701 A 2611 SMOKE DETECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FWD CARGO BAY FAULTY A UALA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 29 428UA 523 FWD CARGO COMPT SMOKE DETECTOR FAULT MESSAGE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100089 20070711 00089 EU 2007 7 11 2007UALA02336 1 20070629 A 3350 PANEL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 445UA 826 EMERGENCY EXIT LIGHT SWITCH AT REAR FLIGHT ATTENDANT PANEL IS INOP. REPLACED PANEL AND OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100095 20070711 00095 WP 2007 7 11 ABXA070217 1 20070621 A 5610 CAM FOLLOWER DOUG DC9 DC941 302207N WP CLEARVIEW WINDOW OUT OF POSITION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 FIRST OFFICER'S CLEAR VIEW WINDOW WOULD NOT OPEN. FOUND UPPER ACTUATING BAR, CAM FOLLOWER, NOT IN CAM SLOT. REINDEXED AND CYCLED WINDOW SEVERAL TIMES. OPS CHECK GOOD IAW DC9 MM 56-10-03-5-0002. 2 L 7 2 4F A6WE 2007071100110 20070711 00110 NM 2007 7 11 ABXA070213 1 20070524 A 5551 180T00092 PIN BOEING 767 767200 1385120 NM RT HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 797AX 23147 RIGHT HORIZONTAL STABILIZER PIVOT PIN HAD CORRODED PITTING IN THREADS. REPLACED PIVOT PIN IAW JOB CARD 7302001. 2 L 7 2 4F RT A1NM 2007071100111 20070711 00111 NM 2007 7 11 ABXA070214 1 20070525 A 5712 114T22152 RIB BOEING 767 767200 1385120 NM RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 797AX 23147 CORROSION WS 720, RIGHT WING LEADING EDGE LOWER PANEL SUPPORT/RIB. REPLACED STRUT RIB IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007071100118 20070711 00118 CE 2007 7 11 DJFA2007068 1 20070624 A 2611 473054 SMOKE DETECTOR RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP LAVATORY FALSE INDICATION E DJFA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 23 813CW 8226 258413 TRIP NR 1191218 CREW REPORTED BAGGAGE FIRE INDICATION ILLUMINATED IN FLIGHT. AIRCRAFT DIVERTED; NO SMOKE WAS SEEN OR SM ELLED. MAINTENANCE FOUND THE LAV SMOKE DETECTOR INOPERATIVE AND REPLACED IT. 2 L 7 2 4F 4 F RT A3EU E6WE 2007071100120 20070711 00120 CE 2007 7 11 GUUA06250701 1 20070625 A 5340 1148200773 BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE DOWNLOCK BENT A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 29 87551 UE206 FLIGHT: 9224, DURING FINAL APPROACH NOSE GEAR DID NOT INDICATE DOWN AND LOCK UNTIL FIVE TO TEN SECONDS AFTER SELECTED DO WN POSITION. REPLACED NOSE LANDING GEAR DOWNLOCK BRACKET. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007071100160 20070711 00160 WP 2007 7 11 ABXA070222 1 20070611 A 5320 39164091 ATTACH ANGLE DOUG DC9 DC931 3022065 WP LT MLG WW CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 ATTACH ANGLE LEFT WHEEL WELL, STA 699, LEFT BUTT LINE 54, ADJACENT TO SLANT PANEL HAD EVIDENCE OF CORROSION. REMOVED AN D REPLACED ATTACH ANGLE IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2007071100173 20070711 00173 NM 2007 7 11 2007UALA02158 1 20070622 A 2432 CHARGER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE MAIN BATTERY FAILED A UALA O OTHER L NO TEST IN INSP/MAINT 1 WP 29 227UA 30555 MAIN BATTERY MAIN BATTERY CHARGER FAILURE. [07-17-07] REPLACED MAIN BATTERY AND ELMS CARD. OP CHECKED OK FOR SERVICE . 2 L 7 2 4F 4 F RT T0001SE E46NE 2007071100200 20070711 00200 NM 2007 7 11 2007UALA02167 1 20070621 A 3150 WARNING SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT ACTIVATED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 366UA 24535 ABORTED TAKEOFF AT 140 KNOTS DUE TO WINDSHEAR ALERT. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071100206 20070711 00206 2007 7 11 2007UALA02171 4 20070621 A 2562 ELT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FWD FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 433UA 589 FWD ELT MAKING A BUZZING NOISE. REPLACED ELT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100207 20070711 00207 EU 2007 7 11 2007UALA02172 1 20070622 A 5210 CYLINDER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R1 DOOR UNRELIABLE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 439UA 683 FOUND DOOR 1R EMERGENCY CYLINDER IN THE UNARMED POSITION AND NOT SAFETIED. ARMED EMERGENCY CYLINDER AND SAFETIED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100208 20070711 00208 NM 2007 7 11 2007UALA02173 1 20070621 A 3500 TRANSDUCER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE O2 BOTTLE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 O2 GAUGE READS 1700. BOTTLE READS 2000. FOUND FAULTY TRANSDUCER. REPLACED TRANSDUCER. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071100211 20070711 00211 2007 7 11 2007UALA02176 4 20070621 A 2565 PROXIMITY SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 565UA 26669 DOOR 1R "SLIDE" LIGHT REMAINS DIMLY ILLUMINATED AT ALL TIMES. [08-08-07] REPLACED BOTH GIRT BAR PROXIMITY SWITCHES. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071100236 20070711 00236 NM 2007 7 11 2007UALA02194 1 20070623 A 5310 DOOR FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 923UA 26643 FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT OB LOWER CORNER OF LOWER BOTTOM DOOR STOP FITTING VERIFIED BY HFEC, NR (12166 -1400-0001). FABRICATED AND INSTALLED 2 EA ANGLE AND FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071100243 20070711 00243 NM 2007 7 11 2007UALA02205 1 20070622 A 2597 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 583UA 26705 GIRT BAR CB POPPED. [08-08-07] FOUND BAD SOCKETS AT DOOR 1L AND 1R FOR SLIDE LOCK INDICATOR LIGHTS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071100244 20070711 00244 NM 2007 7 11 2007UALA02207 1 20070624 A 3510 OXYGEN SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CREW LOW A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 512UA 24809 CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. [08-08-07] FOUND 02 SYSTEM AT 1150 PSI, SERVICED 02 TO 1800 PSI. RECORD PRESSURE PRIOR TO SERVICING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071100251 20070711 00251 NM 2007 7 11 2007UALA02210 1 20070624 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 FWD PIT CARGO FLOORBEAM FRAME WEB HAS GOUGES ON FWD FRAME AT STA 654 AND LBL29. REMOVED DAMAGED SECTION OF WEB. FABRIC ATED AND INSTALLED A REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071100252 20070711 00252 NM 2007 7 11 2007UALA02212 1 20070622 A 3350 78691 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 674UA 29242 SEAT 21H EXIT PATH LIGHTING LOOSE. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071100270 20070711 00270 2007 7 11 ASMF200707003 4 20070702 A 3410 PITOT HEAD BOEING 737 737705 13844SC NM CFMINT CFM567 CFM567B22 13802 NE DAMAGED W ASMF C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 SW 23 852AM 33787 AIRCRAFT REJECTED TAKEOFF AT 80 KTS DUE TO CREW DETECTED A DISCREPANCY BETWEEN READINGS IN CAPTAIN (45 KNOTS) AND FIRST OFFICER’S (80 KNOTS) VELOCIMETERS. MAINTENANCE PERSONNEL DETECTED FOD ON LT PITOT CAUSED BY A BIRD STRIKE. FLUSH TO THE LT PITOT AND TESTS WERE PERFORMED IAW MM 34-13-00, ALL CORRECT. ADDITIONALLY, RADOME BIRD/HAIL STRIKE INSPECTION WAS P ERFORMED IAW MM 05-51-18, NO DAMAGES WERE FOUND. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007071100272 20070711 00272 NM 2007 7 11 ASMF200707004 1 20070705 A 5511 5930602515 STABILIZER DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE HORIZONTAL STAB CRACKED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 583MD 49659 DURING THE INSPECTION OF THE HORIZONTAL STABILIZER REAR SPAR UPPER CAPS, REQUIRED BY THE AD 2007-10-04, DETECTED A CRACK OF (2) INCHES LONG AT STATION XH = 6.5. THE REPAIR IS IN PROCESS, DETAILED INFORMATION WILL BE SUBMITTED IN A SUPPLEME NT AS SOON AS ITS CONCLUSION. (ASMF) MAINTENANCE PERSONEL REPLACED THE HORIZONTAL STABILIZER IAW MM 27-40-00, TESTED COR RECT. (K) 2 L 7 2 4F 4 F RT E9NE 2007071100274 20070711 00274 NE 2007 7 11 ASMF200707005 2 20070705 A 7320 8G4411 SWITCH DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE FUEL PRESSURE FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 214AM 13843 49585 725634 AIRCRAFT RETURNED TO PLATFORM DUE TO CAPTAIN REPORTED THAT THE LT INLET FUEL LOW PRESSURE AND MASTER CAUTION LIGHTS TURN ED ON. REPORT WAS DEFERRED IAW MEL 73-3. DURING OVERNIGHT CHECK AT MEX, MAINTENANCE PERSONNEL REPLACED THE LOW FUEL PRES SURE CAUTION SWITCH AND PERFORMED OPERATIONAL TEST AND LEAKS CHECK IAW MM 73-33-01, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007071100292 20070711 00292 WP 2007 7 11 070134 1 20070618 A 3350 0106607001 LENS DOUG DC9 DC987 3022087 WP CABIN MISSING A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 948MA 49778 IT HAS BEEN REPORTED BY THE FLIGHT CREW THE EMERGENCY EVACUATION LIGHTING SYSTEM HAS BEEN FOUND TO BE DEFECTIVE. FLOOR PATH LIGHTING STRIP IS MISSING THE LENS COVER. MAINTENANCE DEPARTMENT PERSONNEL HAVE INSPECTED THE SYSTEM AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE . 2 L 7 2 4F RT A6WE 2007071100305 20070711 00305 NM 2007 7 11 SWAA073259 1 20070628 A 5315 6546811 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM UPPER TEE CAP CORRODED AT BS 986.5, RBL 14 TO LBL 44. R&R FLOORBEAM UPPER TEE CAP PER SRM. 2 L 7 2 4F RT A16WE 2007071100309 20070711 00309 NM 2007 7 11 SWAA073244 1 20070628 A 2560 65C16820 HOOK BOEING 737 7375H4 138449D NM R1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM. 2 L 7 2 4F RT A16WE 2007071100322 20070711 00322 NM 2007 7 11 USAA070485 1 20070627 A 5313 STRINGER SPLICE BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 FOUND CRACK BS 360 S-14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM 51-20-01, DEFECT SIZE: .500. 2 L 7 2 4F RT A16WE 2007071100332 20070711 00332 NM 2007 7 11 2007UALA02202 1 20070622 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 531UA 25042 EMERGENCY LIGHTS OUT AT DOOR 2L OUTSIDE. RELAMPED, OK 2 L 7 2 4F 4 F RT A2NM E17NE 2007071100344 20070711 00344 NM 2007 7 11 2007UALA02343 1 20070629 A 5210 BEARING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD ENTRY DOOR LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 FWD ENTERY DOOR, UPPER LATCH TORQUE TUBE FWD AND AFT BEARINGS ARE LOOSE. TIGHTENED ROLLER BEARINGS ON UPPER LATCH TORQU E TUBE AND SAFETIED. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071100348 20070711 00348 NM 2007 7 11 2007UALA02347 1 20070701 A 3350 20121 POWER SUPPLY BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 351UA 24319 DOOR 1L INTERIOR EMERGENCY EXIT LIGHT ABOVE DOOR INOP. REPLACED DOOR 1L POWER SUPPLY. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071100349 20070711 00349 NM 2007 7 11 2007UALA02348 1 20070701 A 3350 20131A CHARGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 RIGHT OVERWING AFT TWO EMERGENCY LIGHTS IS INOP. REPLACED BATTERY CHARGER UNIT AT DOOR 3 RIGHT. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071200030 20070712 00030 SO 2007 7 12 SIMA200718302 1 20070627 A 3210 355022002 CONTROL UNIT EMB 135 EMB135KL 3260302 SO COCKPIT FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 832AE 12305 145627 ON TAKEOFF RECEIVED LANDING GEAR/GROUND FAIL MESSAGE WITH ASSOCIATED AURAL WARNINGS REGARDING CONFIGURATION. PERFORM PR OCEDURES IN AOM1 - RETURNED TO CMH. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR WEIGHT ON WHEELS 1 AND 2 TARGETS. REM OVED AND REPLACED LANDING ELECTRONIC GEAR CONTROL UNIT IAW EMB AMM 32-32-01. PERFORMED OPERATIONAL CHECKS WITH NO DEFEC TS IAW AMERICAN EAGLE WORK CARD 32-700-16. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007071200063 20070712 00063 SO 2007 7 12 SWIA200718419 1 20070501 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 234SW 120308 RIGHT SIDE SEAT TRACK IS CORRODED IN SEVERAL AREAS, DISCOVERED AT C-CHECK. REPLACED RIGHT SIDE FORWARD SEAT TRACK WITH SERVICEABLE UNIT. 2 L 7 2 4T RT A31SO 2007071200064 20070712 00064 SO 2007 7 12 SWIA200718420 1 20070416 A 5210 TORQUE TUBE EMB 120 EMB120ER 3260203 SO PAX DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 233SW 120307 PAX DOOR TORQUE TUBE AFT BEARING BOSS HAS CORROSION, DISCOVERED AT C-CHECK. REPLACED PAX DOOR TORQUE TUBE AFT BEARING B OSS IAW EMB 120 MM 52-11-05. 2 L 7 2 4T RT A31SO 2007071200070 20070712 00070 2007 7 12 AWXA200700787 4 20070701 A 2565 D31517317 SLIDE AIRBUS 320 A320232 3930326 EU L2 DOOR FAILED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 663AW 27325 6613 1419 LAS - EES - LOG# 4149154 - MX REPORTED THE L2 DOOR EMERGENCY SLIDE BOTTLE PRESSURE LOW. MX REPLACED THE L2 DOOR SLIDE IAW TASK CARD R1C25305. 2 L 7 2 4F RT A28NM 2007071200084 20070712 00084 WP 2007 7 12 IXXA07SMN160S 1 20070411 A 5340 FITTING DOUG DC8 DC871F 302199D WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 86484 2988 45993 DURING ROUTINE C CHECK INSPECTION, FOUND AFT LOWER CARGO BILGE INTERIOR FITTING CRACKED AT STATION 1260.000 LONGERON 35 RIGHT. REMOVED CRACKED FITTING. FABRICATED FITTING PERFORMED NDT. NO CRACK OR CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-1-8B, ATI REPAIR SPECIFICATION NU MBER 2003-05, DOUGLAS DRAWING NUMBER 3750277, DC8 NDT SPM PART 08-00-02 TO 07, AND 51-3-1. 2 L 7 4 4F RT 4A25 2007071200092 20070712 00092 NM 2007 7 12 F3LA200700146 1 20070627 A 5320 TRANSITION PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT TRANSITION PANEL 131BF DAMAGED. REPAIRED TRANSITION PANEL 1 31BF IAW SRM 53-02-00, FIG 204. 2 L 7 2 4F RT A28NM 2007071200099 20070712 00099 SO 2007 7 12 C2XA07IA155 1 20070627 A 2750 163500111 SENSOR EMB 145 EMB145LR 3260212 SO TE FLAPS SHORTED A C2XA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 SW 27 48901 4956 4956 145501 IAH - FLIGHT 2852, THE CREW REPORTED A W/S 1 FAIL MESSAGE ON EICAS FOLLOWED BY LOUD CLICKING OF RELAYS AND A STRONG BURN ED ELECTRICAL ODOR. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE WINDSHIELD HEAT ON MEL 30-42-02 CAT C CTL#124320, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RE TURNED TO 06/28/07, WHERE MAINTENANCE SWAPPED THE SENSORS WIRES TO S3 AND S4. OPERATIONALLY CHECKED THE WINDSHIELD HEAT SYSTEM WITH NO DEFECTS. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007071200100 20070712 00100 SO 2007 7 12 C2XA07IA157 1 20070629 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO CABIN ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 13123 145688 IAH - FLIGHT 2281, THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT AFTER ROTATION THAT DISSIPATED AROUND 1000 TO 12 00 FEET AGL. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE GROUND RAN BOTH ENGINES AND APU, OPERATIONAL LY CHECKED THE PACKS SYSTEM WITH NO DEFECTS OR LEAKS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007071200101 20070712 00101 SO 2007 7 12 C2XA07IA158 1 20070701 A 3397 SOCKET EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHT BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 16927 145006 IAH FLIGHT 2637, THE CREW REPORTED A BURNING SMELL NEAR SEAT 1A. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE BULB S OCKET FOR BURNED. THE CABIN LIGHTING WAS PLACED ON MEL 33-20-00 CAT-C CTL NUMBER 124492, AND THE AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE.THE AIRCRAFT RETURNED TO IAH ON FLIGHT 3141 WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIG HT ASSEMBLY, OPERAQTIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. 2 L 7 2 4F RT T00011AT 2007071200105 20070712 00105 SO 2007 7 12 C2XA07TY034 1 20070705 A 5330 14565100407 SKIN EMB 145 EMB145EP 3260221 SO FUSELAGE CRUSHED A C2XA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 27 16944 145045 TYS - AIRCRAFT SUFFERED GROUND DAMAGE FROM A BAGGAGE CART TO THE FUSELAGE UNDER WINDOWS 4 AND 5. MAINTENANCE REMOVED AN D REPLACED STRINGERS 11L, 12L AND FRAME 27 AND 2 SHEAR CLIPS ON FRAME 29 AND 30. REPLACED SKIN PANEL FROM FRAME 23 TO F RAME 36. ALSO, REPLACED LT WING LEADING EDGE. ALL WORK WAS ACCOMPLISHED IAW EA5330-01104. STRINGER P/N-145-20559-005- S/N-145-21675-001. 2 L 7 2 4F RT T00011AT 2007071200106 20070712 00106 NM 2007 7 12 F3LA200700156 1 20070627 A 5321 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED HOLES IN TOP SURFACE OF AFT CARGO COMPARTMENT FLOOR PANEL 151VG. REPAIRED HOLES I N FLOOR PANEL 151VG IAW SRM 53-02-00, PB 201, PARA 8 C., FIG 204. 2 L 7 2 4F RT A28NM 2007071200110 20070712 00110 NM 2007 7 12 F3LA200700160 1 20070628 A 5320 TRANSITION PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT TRANSITION PANEL 151DE DAMAGED. REPAIRED PUNCTURES IN TRANS ITION PANEL 151DE IAW SRM 53-02-00, PB 201, PARA 8 C., FIG 204. 2 L 7 2 4F RT A28NM 2007071200111 20070712 00111 NM 2007 7 12 F3LA200700161 1 20070628 A 5320 TRANSITION PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT TRANSITION PANEL 151HE DAMAGED. REPAIRED PUNCTURES IN TRANS ITION PANEL 151HE IAW SRM 53-02-00, PB 201, PARA 8 C., FIG 204. 2 L 7 2 4F RT A28NM 2007071200113 20070712 00113 NM 2007 7 12 DU4R2007144 1 20070623 A 5320 146N852257 ANGLE BOEING 757 757232 1384965 NM BS 1480 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 638DL 23761 FOUND HEAVY CORROSION IN AFT PIT ON MAIN ANGLE AT BS 1480 STR 27 RT. REPAIRED BY REMOVING ANGLE. DRILLED UP, TREATED, PRIMED AND INSTALLED CHORD P/N 146N8522-57 IAW 51-40-05 PG 1, 51-40-02 AND 51-20-01. 2 L 7 2 4F RT A2NM 2007071200135 20070712 00135 EU 2007 7 12 UPS07150047 1 20070624 A 5310 STRINGER AIRBUS A300 A300F4622R 3930360 EU PUNCTURED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 164UP 005 AIRCRAFT SUSTAINED DAMAGE FROM RUNWAY CANS AT SECTION 130 FROM STATION 1817 FR 27-2241 FR 35. A/C HAS BEEN PUNCTURED AT THESE STATIONS. REMOVED DAMAGE PER A300 SRM 53-10-12. REPAIRED DAMAGE STRINGER L AFT OF FR IAW SRM 53-10-14. REPAIRE D DAMAGE AREA IAW SRM 53-10-12. 2 L 7 2 4F RT A35EU 2007071200138 20070712 00138 NM 2007 7 12 UPS07450033 1 20070529 A 5320 CHANNEL BOEING 747 747212B 1384886 NM BS 820 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C CRACK FOUND AT FWD CHANNEL AT BS820 S10AR TENSION TIE AT HOLE NR 4 THE CRACK WAS FOUND RUNNING AT 12 O /C POSITION WITH LENGTH 0.040" APPROX. BS 820 RT FRAME ATTACH TENSION TIE FWD CHANNEL REPAIRED AS PER RS R53-25-35809. SUPPLEMENTAL INSPECTION IS REQUIRED AS PER RS R53-25-35809 AND UPS EO B747-5310-26947. 2 L 7 4 4F A20WE 2007071200141 20070712 00141 NM 2007 7 12 UPS07450036 1 20070604 A 5311 65B01717515 FRAME BOEING 747 747212B 1384886 NM BS 480 S15L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C CABIN BS 480 S15L FRAME FOUND CRACK. CRACK LENGTH 2 1/4" CABIN BS 480 STR 13AL TO STR 16L FRAME REPLA CED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007071200143 20070712 00143 NM 2007 7 12 UPS07450038 1 20070529 A 5320 CHANNEL BOEING 747 747212B 1384886 NM BS 940 S8L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C CRACK FOUND AT AFT CHANNEL OF BS 940 S8L TENSION TIE AT HOLE NR 16, THE CRACK WAS FOUND IN FWD FACE WI TH LENGTH 0.030" APPROX. M/D BS 940 LT SIDE FRAME ATTACH TENSION TIE AFT CHANNEL REPAIRED AS PER RS R53-25-35811. SUPP LEMENTAL INSPECTIONS ARE REQUIRED AS PER RS R53-25-35811 AND UPS EO B747-5310-26946. 2 L 7 4 4F A20WE 2007071200145 20070712 00145 NM 2007 7 12 UPS07450040 1 20070529 A 5320 PLATE BOEING 747 747212B 1384886 NM BS 940 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C M/D BS 940 LT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN AT MOST O/B. M/D BS 940 LT TENSION TIE ATT STEEL PLATE REPLACE AND INSTALLED AS PER RS R53-25-35811 AND UPS EO B747-5310-23715-C. 2 L 7 4 4F A20WE 2007071200148 20070712 00148 NM 2007 7 12 UPS07450043 1 20070530 A 5310 65B01734101 DOUBLER BOEING 747 747212B 1384886 NM BS 820 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C CRACK FOUND AT DOUBLER AT LT SIDE OF BS 820 STR 10A ATTACHED TENSION TIE NR 4 HOLE CRACK LENGTH 3/16" APPROX AT 8 O/C POSITION. M/D BS 820 LT SIDE STR 10A FRAME ATTACH DOUBLER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2 L 7 4 4F A20WE 2007071200149 20070712 00149 NM 2007 7 12 UPS07450044 1 20070529 A 5320 CHANNEL BOEING 747 747212B 1384886 NM BS 860 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C CRACK FOUND AT FWD CHANNEL OF BS 860 RBL80 TENSION TIE AT HOLE NR 6, THE CRACK WAS FOUND RUNNING AT 5 O/C POSITION WITH LENGTH 0.0625" APPROX. BS 860 RT TENSION TIE FWD CHANNEL REPAIRED AS PER RS R53-25-35810 AND UPS EO B 747-5310-26948. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35810 AND UPS EO B747-5310-26948. 2 L 7 4 4F A20WE 2007071200150 20070712 00150 NM 2007 7 12 UPS07450045 1 20070607 A 5311 FRAME BOEING 747 747212B 1384886 NM BS 420 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C M/D BS 420 S14ER FRAME FOUND CRACKED AS MARKED. CRACK LENGTH 5.5". BS 420 BTN S13AR TO S17R FRAME RE PAIRED AS PER RS R53-12-35815. CONTINUED INSPECTIONS ARE REQUIRED AS PER RS R53-12-35815 AND UPS EO B747-5310-27050. 2 L 7 4 4F A20WE 2007071200152 20070712 00152 NM 2007 7 12 UPS07550057 1 20070626 A 2150 A/C PACK BOEING 757 75724APF 1384969 NM COCKPIT ODOR A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 DEAD BUG PARTS AND FOUL SMELL IN COCKPIT AND ALL DUCTS, FROM LOWER PANEL OF APU AIR INTAKE PLENUM. CLEANED AIR INTAKE S CREEN AND SURROUNDING AREAS, ALL FUNCTIONS OF APU OPERATE NORMAL. GOOD DUCT PRESSURE. ENGINE STARTS NORMAL. 2 L 7 2 4F RT A2NM 2007071200155 20070712 00155 WP 2007 7 12 UPS07850051 1 20070623 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 L/WING OUTBD LEADING EDGE UPPER RIB CRACKED AT XFS 678. STOP DRILLED CRACK AT STA XFS 678 L/WING LEA DING EDGE IAW SRM 57-02-00-0 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER AT STA XFS 678 L/WING LEADING EDGE IAW SR M 57-03-01-0 FIG 006. 2 L 7 4 4F RT 4A25 2007071200156 20070712 00156 WP 2007 7 12 UPS07850052 1 20070623 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 L/WING OUTBD LEADING EDGE RIB CRACKED AT STA XFS 672. STOP DRILLED CRACK AT STA XFS 672 L/WING LEADI NG EDGE IAW SRM 57-2- 0 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER AT STA XFS 672 L/WING LEADING EDGE IAW SRM 57- 03-01 FIG 006. 2 L 7 4 4F RT 4A25 2007071200160 20070712 00160 NM 2007 7 12 UPS07M50058 1 20070328 A 5753 SKIN DOUG MD11 MD11 3023602 NM TE FLAP DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C RHW, INBD FLAP LOWER AFT INBD AND OUTBD SEGMENTS NEED RE-SKIN. RHW I/B FLAP LWR AFT I/B AND O/B SEGME NTS REMOVED. RHW RELATED PARTS AND I/B FLAP I/B AND O/B SEGMENTS LWR SKINS REMOVED. NEW SKINS FAB PER DWG ARC2736 AND ARC2444. NEW SKINS REPROTECTED, PAINTED AND INSTALLED. RHW I/B FLAP I/B AND O/B SEGMENTS REINSTALLED. REWORK AREA PA INTED TOP CO AT PER SRM51-21-02 VOL II REV 39. 2 L 7 3 4F RT A22WE 2007071200163 20070712 00163 NM 2007 7 12 UPS07M50061 1 20070416 A 5313 LONGERON DOUG MD11 MD11 3023602 NM STA 5-128 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C CTR CARGO COMPT AT STATION 5-128 LONGERON 45 LT FOUND SUSPECTED CRACKED ON DOUBLER AREA AS MARK. HFEC INSP C/OUT PER DAC NDT SPM REV 13 PART 06-10-01-001 ON DOUBLER FOUND CRACK. CRACK LONGERON SPLICE AT CTR CARGO STA 5-1 28 L45 LT REMOVED. NEW SPLICE P/N A5A7116-503 FAB PER DWG A5A7116. FPI C/OUT ON NEW SPLICE FOUND NO CRACK. NEW SPLICE FASTENER HOLES PICKED UP, REPROTECT ED, PAINTED AND INSTALLED. REWORK AREA PAINTED. 2 L 7 3 4F RT A22WE 2007071200164 20070712 00164 2007 7 12 UPS07250083 4 20070627 A 2565 SLIDE BOEING 727 72722C 138400F NM ENTRY DOOR INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 CREW SLIDE FELL OUT OF CONTAINER WHEN THE ENTRY DOOR WAS OPENED. REINSTALLED EVACUATION SLIDE IN THE CONTAINER IAW MM 5 2-25-60-14-2. 2 L 7 3 4F A3WE 2007071200165 20070712 00165 WP 2007 7 12 UPS07850064 1 20070613 A 5720 ANGLE DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 R/WING CENTER LEADING EDGE SLOT INBD SIDE "L" ANGLE CRACKED. STOP DRILLED CRACK ON "L" ANGLE AT R/WI NG CENTER L/E SLOT DOOR IAW SRM 51-03-02. FABRICATED AND INSTALLED REPAIR ANGLE DOUBLER IAW SRM 57-02-00 FIG 002. 2 L 7 4 4F RT 4A25 2007071200169 20070712 00169 WP 2007 7 12 UPS07850068 1 20070608 A 5754 WEB DOUG DC8 DC873F 302199F WP LT WING PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 L/WING INBD LEADING EDGE (AUX TANK) VERY INBD WEB HAS A PUNCTURE. REPAIRED L/WING INBD LEADING EDGE (AUX TANK) VERY INBD WEB IAW SAA EA NR 008-5710-01-A0921, UPS RAA NR DC8-57-20224, AND FAA FORM 8100-9 2 L 7 4 4F RT 4A25 2007071200170 20070712 00170 WP 2007 7 12 UPS07850075 1 20070622 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 R/WING OUTBD L/E UPPER RIB CRACKED AT XFS 734. STOP DRILLED CRACK ON R/WING UPPER OUTBD L/E AT STA X FS 734 IAW SRM 57-03-03-0. FABRICATED AND INSTALLED REPAIR DOUBLER AT STA XFS 734 R/WING L/E IAW SRM 57-03-03-0 FIG 7. 2 L 7 4 4F RT 4A25 2007071200171 20070712 00171 WP 2007 7 12 UPS07850076 1 20070622 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 R/WING OUTBD L/E UPPER RIB CRACKED AT XFS 816. STOPPED DRILLED CRACK AT R/WING L/E STA XFS 816 IAW S RM 57-03-03-0. FABRICATED AND INSTALLED REPAIR DOUBLER AT R/WING L/E STA XFS 816 IAW SRM 57-03-03-0 FIG 7, AND SRM 57-0 2-00-0 FIG 2. 2 L 7 4 4F RT 4A25 2007071200173 20070712 00173 WP 2007 7 12 UPS07850078 1 20070622 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 R/WING CENTER L/E UPPER RIB CRACKED AT STA XFS 461 STOPPED DRILLED CRACK RIB AT STA XFS 461 IAW S RM 57-03-03-0 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER AT STA XFS 461 IAW SRM 57-03-0 3-0 FIG 7. 2 L 7 4 4F RT 4A25 2007071200177 20070712 00177 WP 2007 7 12 UPS07850082 1 20070619 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 R/WING INBD L/E (AUX TANK) INBD LWR CORNER CRACKED. CUT OUT DAMAGED AREA ON R/WING L/E AUX TANK IAW SRM 57-02-00 FIG 6. FABRICATED AND INSTALLED REPAIR DOUBLER ON R/WING INDB L/E AUX TANK IAW SRM 57-03-00 FIG 3, AND SRM 51-01-26. 2 L 7 4 4F RT 4A25 2007071200178 20070712 00178 WP 2007 7 12 UPS07850085 1 20070612 A 5310 5649028U DOUBLER DOUG DC8 DC873F 302199F WP FS45-48 L31R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 EXFOLIATION CORROSION IN A/C COMPT AT STA 45 - 48 AT L31R. REMOVED CORRODED DOUBLER AT STA 45 - 48 L 31R IAW SRM 51-1-20D LOCATED, DRILLED-UP, AND INSTALLED REPAIR DOUBLER AT STA 45 -48 L31R IAW SRM 51-3-2, AND SRM 51-1-2 0D. 2 L 7 4 4F RT 4A25 2007071200179 20070712 00179 WP 2007 7 12 UPS07850086 1 20070606 A 5510 BEAM DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 RT HORIZONTAL STAB UPPER AFT H-ANGLE CRACKED. REMOVED RT HORIZ STAB UPPER AFT H-ANGLE IAW SRM 51-03- 00-0. FABRICATED AND INSTALLED REPAIR H-BEAM ON RT HORIZ STAB IAW DWG 3702464, AND SRM 51-03-00-0. 2 L 7 4 4F RT 4A25 2007071200180 20070712 00180 WP 2007 7 12 UPS07850087 1 20070609 A 5313 DC853B00939 LONGERON DOUG DC8 DC873F 302199F WP FS 1766 L15L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C3 L15L WHERE VERTICAL STAB ATTACHES TO LONGERON IS CRACKED. REMOVED SHEAR TIE AND DAMAGED LONGERON 15L SECTION AT STA 1766 IAW SRM 51-01-21-0. FABRICATED AND INSTALLED LONGERON REPAIR SPLICE AND STRAPS AT L15L STA 1766 IA W SRM 53-02-02-0 FIG 10. 2 L 7 4 4F RT 4A25 2007071200181 20070712 00181 WP 2007 7 12 UPS07850088 1 20070623 A 5710 DOUBLER DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C3 L/WING OUTBD L/E UPPER INNER DOUBLER CRACKED AT STA XW 761. REMOVED INNER DOUBLER ON L/WING OUTBD L/ E AT STA XW 761 IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR DOUBLER ON L/WING OUTBD L/E AT STA XW 761 IAW SRM 51-3 -2, AND SRM 51-1-8. 2 L 7 4 4F RT 4A25 2007071200182 20070712 00182 WP 2007 7 12 UPS07850089 1 20070628 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHT NO TEST A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 703UP 45939 EMERGENCY EXIT LIGHT FAILS TO TEST. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK PER MM 33-50-01-2-4. OPS CHECK OK. 2 L 7 4 4F RT 4A25 2007071200183 20070712 00183 NM 2007 7 12 UPS07M50069 1 20070608 A 5320 INTERCOSTAL DOUG MD11 MD11 3023602 NM STA 1887-1902 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C CABIN - FLOOR SUPPORT STRUCTURE STA 1887 - 1902, LBL 18 INTERCOSTAL FOUND CRACKED. CRACK AREA TRIMMED OUT PER SRM 53-00-01 FIG 6 VOL I REV38. HFEC INSP C/OUT FOUND 2 CRACKS APPROX 1" EACH. CRACK AREAS TRIMMED OUT PER SR M 53 -00-01 FIG 6 VOL I REV 38. HFEC INSP C/OUT FOUND NO CRACK. NEW REPAIR DOUBLER FAB PER SRM 53-00-01 FIG 6 VOLI REV 38. FAB REPAIR DOUBLER HEAT TREATED, HOLES TRANSFERRED, REPROTECTED, PAINTED AND INSTALLED. 2 L 7 3 4F RT A22WE 2007071200184 20070712 00184 NM 2007 7 12 UPS07M50070 1 20070608 A 5320 AGA740827 FLOOR SUPPORT DOUG MD11 MD11F 3023600 NM STA 1887-1902 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C CABIN, FLOOR SUPPORT STRUCTURE STA 1887 - 1902, RBL 18 INTERCOSTAL FOUND CRACKED. CRACK INTERCOSTAL A T CABIN FLOOR SUPPORT STRUCTURE STA 1887 TO 1902 RBL 18 AREA REMOVED. NEW STRUCTURE P/N AGA7408-27 FAB PER DWG AGA7408 INTERCOSTAL WEB HEAT TREATED PER DPS 7.00-1 AND HARNESS VALUES HRB 83 .7 PER DPS 1.05-3. NEW STRUCTURE FASTENER HOLES P ICKED UP, PROTECTED AND PAINTED. NEW STRUCTURE INSTALLED PER DWG AGA7408 AND SRM 51-31-01VOLII. 2 L 7 3 4F RT A22WE 2007071200185 20070712 00185 NM 2007 7 12 UPS07M50071 1 20070505 A 5754 DOUBLER DOUG MD11 MD11 3023602 NM XOS 698 TO 703 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:C RT WING, FIXED L/E INTERIOR FOUND BEADED DOUBLER CRACKED BETWEEN XOS 698 TO XOS 703 AS MARKED. RIBS A T RHW FIXED L/E REPAIR AREA REMOVED. CRACK AREA TRIMMED OFF PER SRM 57-10-00 FIG 27 VOLI REV 39. HFEC INSP C/OUT ON TR IMMED OFF AREA FOUND NO CRACK. REPAIR FILLER, DOUBLER AND ANGLES 02EA FAB PER SRM 57-10 -00 FIG 27 VOLI REV39. REPAIR PARTS HEAT TREATED, HOLES PICKED UP, REPROTECTED, PAINTED AND INSTALLED. RIBS AT RHW L/E REPAIR AREA REINSTALLED. 2 L 7 3 4F RT A22WE 2007071200189 20070712 00189 NM 2007 7 12 UPS07M50093 1 20070606 A 5311 FRAME DOUG MD11 MD11 3023602 NM BULKHEAD CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:C AFT FUSELAGE, AFT PRESSURE BULKHEAD, AFT FACE STA 2007, RBL10', UPPER PORTION OF T CHORD FOUND WITH CR ACK AT EDGE AS MARKED. AFT FUSELAGE, AFT PRESSURE BULKHEAD, AFT FACE STA 2007 RBL UPP PORTION REMOVED FOR ACCESS REPAIR PER SRM 51-21-01V.R.38. THE FOLLOWING ITEMS WERE FAB(A) T CHORD REPAIR SECTION PER DWG NR AJC7050. SPLICE ANGLES FAB PER SRM 53-00-01F9.V1.R38. FILLERS WEB SUPT ANGLES FAB PER SRM 53-00-01 .F9.V9.R38. RE-ASSEMBLE C/OUT AFT FX, AFT PRES S BULKHEAD STA 2007, SATIS. 2 L 7 3 4F RT A22WE 2007071200191 20070712 00191 SO 2007 7 12 SIMA200714301 1 20070520 A 5320 14525422001 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 935AE 4909 14500920 LEFT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 60 AND 61 CORRODED. REPLACED FLOOR SUPPORT IN ACCORDANCE WITH EMB SRM, RETUR NED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2007071300001 20070713 00001 EU 2007 7 13 Y2PA200700023 1 20070622 A 2121 FN100B COOLING FAN AMD FALC20 FALCON 2720302 EU COCKPIT SEIZED A Y2PA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 23 827AA 298 AS AIRCRAFT APPROACHING DESTINATION AIRPORT AND ENTERING RIGHT DOWN WIND FOR RUNWAY 23L, CREW SAW AND SMELLED ELECTRICAL SMOKE COMING FROM TOP OF PANEL ON F/O'S SIDE. CREW DECLARED EMERGENCY AND LANDED ASAP, TAXIED AIRCRAFT OFF RUN WAY, SH UT DOWN AND EVACUATED THRU NORMAL EXIT. USA JET MAINTENANCE PERSONAL INSPECTED AIRCRAFT COCKPIT COMPONENTS, WIRING AND INSTRUMENTS. NO VISUALLY DAMAGE FOUND, MAINTENANCE PERFORMED ENGINE RUN UP OF BOTH ENGINE AND COULD NOT IDENTIFY ANY ABN ORMAL TROUBLES. DURING INSPECTION AND TROUBLE SHOOTING MAINTENANCE FOUND THE FMS 5000 GPS COOLING FAN MOTOR SEIZED. RE PLACED FAN MOTOR AND PERFORMED SYSTEM OP'S CHECKS WITH NO FAULTS FOUND AT THIS TIME. AIRCRAFT HAS BEEN RETURNED TO SERV 2 L 7 2 4F A7EU 2007071300002 20070713 00002 EA 2007 7 13 TRAX200700890 1 20070623 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 970EV 7527 LEFT WING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007071300003 20070713 00003 EA 2007 7 13 COMA0760447 1 20070620 A 5730 601R100462 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 954CA 29296 7100 RIGHT WING PLANK IS CRACKED AT WS 148.019. REPAIRED PER REO 601R-57-21-130. 2 L 7 2 4F RT A21EA 2007071300004 20070713 00004 NM 2007 7 13 07FDEA02364 1 20070703 A 5313 BAC1498131 STRINGER BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD PIT BILGE BODY SKIN STRINGER IS CORRODED BS 720F 17, STR 27L, WL 149 (MKD). REMOVED CORROSION, MEASURED MATERIAL L OSS OUT OF LIMITS, VERIFIED REPAIR MATERIAL. FABRICATED NEW PARTS REF SRM 53-10-3 FIG 1, TREATED AND PRIMED REF SRM 51- 10-2 PG 2. INSTALLED REPAIR PARTS REF SRM 51-30-2 PG 2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007071300005 20070713 00005 EA 2007 7 13 COMA0760448 1 20070620 A 5730 601R100461 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 954CA 29296 7100 LEFT WING PLANK IS CRACKED AT WS 148.019. REPAIRED PER REO 601R-57-21-130. 2 L 7 2 4F RT A21EA 2007071300006 20070713 00006 EA 2007 7 13 COMA0760449 1 20070621 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 735CA 7267 FLIGHT 5106 - DURING DESCENT FOR OTHER WARNING, RECEIVED FLAP FAIL WARNING. DECLARED EMERGENCY AND LANDED WITHOUT INCID ENT. COMPLIED WITH AD 2006-12-21. FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2007071300007 20070713 00007 EA 2007 7 13 COMA0760450 1 20070621 A 2751 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA LT WING OUT OF RIG A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 735CA 13921 7267 FLIGHT 5223 - RECEIVED FLAP CAUTION AT CRUISE, FLAPS AT 0. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. PERFORMED E O 27-046 AD. LEFT BPSU NOT HOLDING RIG. REPLACED BPSU, NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007071300008 20070713 00008 EA 2007 7 13 COMA0760451 1 20070622 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 591SW 28347 7079 DURING FS 409 INSPECTION FOUND CRACK AT LOWER END OF VERTICAL STIFFENER, FS 409, RBL 36, INBOARD SIDE. CUT OUT DAMAGE A ND INSTALLED DOUBLER IAW CRJ REO 601R-53-41-189. 2 L 7 2 4F RT A21EA 2007071300009 20070713 00009 EA 2007 7 13 COMA0760452 1 20070622 A 2910 601R7514785 HYDRAULIC LINE CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYS FAILED A COMA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 01 818CA 7408 FLIGHT 5298 - NR 1 HYD LOW PRESSURE CAUTION MESSAGE. HYD QTY FLUCTUATES BETWEEN 5 AND 30 PERCENT. AIRCRAFT RETURNED TO DSM AND LANDED SAFELY. REMOVED AND REPLACED NR 1 HYD SYS PRESSURE HOSE. 2 L 7 2 4F RT A21EA 2007071300010 20070713 00010 EU 2007 7 13 TRAX200700891 1 20070624 A 5270 LIGHT AEROSP ATR72 ATR72 EU COCKPIT ILLUMINATED A ASOA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 27 631AS 362 ASD LIGHT WILL NOT EXTINGUISH. 2 H 7 2 4T RT 2007071300012 20070713 00012 EA 2007 7 13 COMA0760454 1 20070626 A 2797 601R571161 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA RT WING SHORTED A COMA K NONE J WARNING INDICATION CR CRUISE 1 SO 01 914CA 7012 FLIGHT 9456 - FLAP FAIL MESSAGE RECEIVED AT CRUISE. DECLARED EMERGENCY. LANDED AT CVG WITHOUT INCIDENT. REPLACED RIGH T WING BPSU HARNESS. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007071300013 20070713 00013 NM 2007 7 13 07FDEA02365 1 20070703 A 5313 BAC1498131 STRINGER BOEING 727 727233 138408A NM ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 286FE 22623 FWD PIT BILGE BODY SKIN STRINGER HAS SEVERAL GOUGES BS 720D TO 720E 8, STR 26L, WL 151 (MKD). REMOVED GOUGES, NDT VERIF IED BLENDED AREA OUT OF LIMITS. REMOVED AND INSTALLED STRINGER SECTION FROM STA 720C 10 TO 740 STR 26L, REF SRM 53-10-3 PG 3-4B, SRM 51-30-2, SRM 51-10-2,THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007071300014 20070713 00014 EU 2007 7 13 07FDEA02366 1 20070703 A 5270 UNKNOWN AIRBUS 310 A310222 3930315 EU CARGO DOOR WARNING LIGHT A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 454FE 278 FWD CARGO DOOR UNLOCK INDICATION NUMEROUS TIMES AFTER TAKEOFF. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-71-01, CATEGORY : C EXPIRATION: 13JUL07. 2 L 7 2 4F RT A35EU 2007071300015 20070713 00015 EU 2007 7 13 NWAA072383257 1 20070702 A 3350 321454 POWER SUPPLY AIRBUS 320 A320212 3930322 EU EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 357NW 33914 3368 830 EMERGENCY ESCAPE LIGHTING EPSU 11WL INOP. REPLACED EPSU 11WL, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 2007071300016 20070713 00016 EA 2007 7 13 COMA0760455 1 20070627 A 5210 SEAL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNKNOWN A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 427CA 7460 FLIGHT 5638 - AIRCRAFT LOST PRESSURE, AND PAX DOOR HAS LOUD SQUEALING NOISE. DECLARED EMERGENCY, LANDED JAX WITHOUT INC IDENT. INSPECTED MAIN CABIN DOOR, NO DEFECTS. PRESSURIZED 2 AND CHECKED WITH BUBBLE SOLUTION, NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007071300017 20070713 00017 NM 2007 7 13 NWAA072256302 1 20070621 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK TEST FOUND UPPER DECK RT EMERGENCY DOOR POWER SUPPLY AND BATTERY PACK INOPERATIVE. MNL MAINTENANCE RE MOVED AND REPLACED POWER SUPPLY AND BATTERY PACK PER AMM 33-51-04. SECURED AND FUNCTIONAL TEST OK. 2 L 7 4 4F RT A20WE 2007071300018 20070713 00018 EA 2007 7 13 TRAX200700881 1 20070616 A 5753 PANEL CNDAIR CL600 CL6002C10 1390015 EA T/E FLAP CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 751EV 10163 FOUND EXFOLIATION CORROSION ON INTERNAL STRUCTURE OF LT OUTBOARD FLAP ASSY IAW TASKCARD 000-57-590-502. REMOVED AND REP LACED LT OUTBOARD FLAP PANEL IAW CRJ 700 AMM 27-52-29. RIG AND OP'S CHECK GOOD IAW CRJ 700 AMM 27-52-00. STARTED REMOV ING FLAP FAIRING PANEL BRACKETS FROM OLD FLAP ASSY AND REINSTALLING ON NEW LT FLAP ASSY AS REQUIRED PER CRJ 700 SRM 51-4 2-00. COMPLETED REMOVAL AND TRANSFER OF FLAP FAIRING BRACKETS IAW CRJ 700 SRM 51-42-00. 06/27/2007 JOB COMPLETE. C/W RII IAW SP 607 AND CRJ 700 AMM 27-52-00. SUPPLEMENTAL - SDR CLOSED 06/29/07. 2 L 7 2 4F RT A21EA 2007071300019 20070713 00019 EA 2007 7 13 TRAX200700892 1 20070625 A 5320 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 871AS 7537 FS 280 FLOORBEAM ATTACHMENT CLIP O/B OF RBL 27.0 IS CRACKED. 2 L 7 2 4F RT A21EA 2007071300020 20070713 00020 EA 2007 7 13 TRAX200700896 1 20070625 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 868AS 7474 AFT EMERGENCY LIGHT IS INOP ON RIGHT OF FUSELAGE. 2 L 7 2 4F RT A21EA 2007071300021 20070713 00021 EA 2007 7 13 TRAX200700897 1 20070626 A 5210 BRACKET CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 880AS 7606 ASD FWD ANCHOR BRACKET CRACKED. 2 L 7 2 4F RT A21EA 2007071300022 20070713 00022 EA 2007 7 13 TRAX200700901 1 20070627 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 870AS 7530 CRACK FOUND ON BRACKET TO INTERCOSTAL 484 RBL 27. 2 L 7 2 4F RT A21EA 2007071300024 20070713 00024 EA 2007 7 13 TRAX200700903 1 20070627 A 5220 HINGE FITTING CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 871AS 7537 CREW ESCAPE HATCH AFT RIGHT HINGE ARM CRACKED. 2 L 7 2 4F RT A21EA 2007071300025 20070713 00025 EA 2007 7 13 TRAX200700905 1 20070627 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 870AS 7530 ANGLE CRACKED ON AFT PRESSURE BULKHEAD AT BAGGAGE DOOR BEAM FS 621.00. 2 L 7 2 4F RT A21EA 2007071300027 20070713 00027 EA 2007 7 13 TRAX200700908 1 20070628 A 5320 FITTING CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 AFT PRESSURE BULKHEAD RT SIDE BATHTUB FITTING AT THE NR 2 HYD PRESSURE LINE IS CONFIRMED CRACKED. 2 L 7 2 4F RT A21EA 2007071300028 20070713 00028 EA 2007 7 13 TRAX200700909 1 20070628 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 977EV 7720 LEFT OVERWING EMERGENCY LIGHT IS INOP. 2 L 7 2 4F RT A21EA 2007071300029 20070713 00029 NM 2007 7 13 ASAA0791824 1 20070529 A 5330 14A323128 SKIN BOEING 737 737990 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 315AS 30019 DENT ON FUSELAGE SKIN. DENT CUT OUT AND DOUBLER INSTALLED PER ASA EA 5330 02213. 2 L 7 4 4F RT A16WE 2007071300031 20070713 00031 EA 2007 7 13 TRAX200700910 1 20070623 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 871AS 7537 CREW ESCAPE HATCH MISSING PLACARDS. 2 L 7 2 4F RT A21EA 2007071300032 20070713 00032 WP 2007 7 13 PNSA070607 2 20070613 A 7200 ENGINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LEFT SURGES A PNSA A UNSCHED LANDING O OTHER TO TAKEOFF 1 AL 03 2719H AC713B P44664 ON DEPARTURE ROLL PAST V THE LEFT ENGINE START SURGING. THE SURGING CONTINUED AND INCREASED AS THE AIRPLANE BECAME AIR BORNE. AT 400 FT PILOT ELECTED TO SHUTDOWN ENGINE TO GAIN MORE PERFORMANCE AND STOP THE SURGING. PILOT DECLARED EMERGE NCY RAN ALL APPROPRIATE CHECK LISTS LANDED WITHOUT FURTHER INCIDENT SINGLE ENGINE. 2 L 7 2 4T 4 T RT A8SW E4WE 2007071300033 20070713 00033 NM 2007 7 13 NWAA072395512 1 20070629 A 2530 COFFEEMAKER BOEING 757 757251 1384970 NM GALLEY SMOKE A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 01 512US 23200 FLIGHT ATTENDANT REPORTED SMOKE COMING FROM COFFEEMAKER 3-4 OR 3-5 IN GALLEY G4A. CIRCUIT BREAKERS WERE PULLED. MAINTE NANCE REMOVED AND REPLACED COFFEE MAKER. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007071300034 20070713 00034 NM 2007 7 13 USAA070514 1 20070629 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 STA 967 LBL 10 TO LBL 37, FLOORBEAM HAS CORROSION. REMOVED DAMAGE & INSTALLED REPAIR PER SRM 53-00-51 FIG 201; CORR TAS K C53-107-01, DEFECT SIZE: 27 INCHES. 2 L 7 2 4F RT A16WE 2007071300035 20070713 00035 NM 2007 7 13 USAA070515 1 20070629 A 5322 SHEAR TIE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 BS 500A - 500B, BETWEEN S27R & 28R HAS CORROSION. REMOVED, FABRICATED & INSTALLED NEW DOUBLER PER T/R 20-00-02; CORR TA SK C53-208-01. 2 L 7 2 4F RT A16WE 2007071300037 20070713 00037 NM 2007 7 13 USAA070517 1 20070629 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 BS 500A & 500B, BETWEEN STR 27R & 28R HAS CORROSION. REMOVED & INSTALLED NEW DOUBLER PER T/R 20-00-02; CORR TASK C53-20 8-01, DEFECT SIZE: 4 X 6 INCHES. 2 L 7 2 4F RT A16WE 2007071300040 20070713 00040 EA 2007 7 13 CHQA200700033 1 20070702 A 2610 355924400 LOOP CNDAIR CL600 CL6002B19 1900309 EA ENGINE INOPERATIVE A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 486CA 7707 FLIGHT 3288 - IAH-CHS - RECEIVED LT 14TH STAGE BLEED LEAK MESSAGE ON THE EICAS. DECLARED AN EMERGENCY. MAINTENANCE TRO UBLE SHOT AND FOUND A FAULTY 14TH STAGE BLEED LEAK SENSE LOOP IN THE LEFT HAND FORWARD PYLON. REMOVED AND REPLACED THE LOOP. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007091300018 20070913 00018 NM 2007 9 13 MWEA070201 1 20070902 A 7830 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 904ME 55168 LEFT HAND THRUST REVERSER UPPER BUCKET STATION 35 ZEE FRAME IS CRAKCED AT OUTBAORD END. 2 L 7 2 4F TR A6WE 2007091300021 20070913 00021 NM 2007 9 13 ZZDA2007265 1 20070830 A 2530 64769001005 COFFEEMAKER BOEING 717 717200 1383700 NM NR 3 DEFECTIVE A ZZDA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 37 957AT 55019 BOTH CABIN AND FLIGHT CREW SMELLED VERY STRONG ODOR THAT MIGHT HAVE BEEN SMOKE, WITHIN 15 SEC OF NOTICING THE SMELL IT H AD DISSIPATED. CREW STATED, SAW EMERGENCY LIGHTS FLASH AND HEARD A POP OR CLICK BY L1 DOOR WHEN ODOR WAS SMELLED. REMO VED AND REPLACED GALLEY CONTROL RELAY AS PRECAUTION IAW B717 WDM 25-31. INSPECTED WIRES AND COMPONENTS BEHIND F/A SEAT IN GALLEY, REMOVED AND REPLACED COFFEEMAKER NR 3 OPS CHECK NORMAL NO C/B POPPED. PERFORMED ENG RUNS AND LOAD CHECK OF E LECTRICAL SYSTEM. ALL SYSTEMS CHECK GOOD. NO DEFECTS FOUND A/C OK FOR CONTINUED SERVICE. OPS CHECK OF EMERGENCY LIGHT S NORMAL. 2 L 7 2 4F TR A6WE 2007091300029 20070913 00029 NM 2007 9 13 UPS07550568 1 20070803 A 5311 70750090C FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 415UP 23855 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1480, S26R. FRAME REPAIR AT STA 1480 S26R ACCOMPLISHED IAW SRM 5 3-00-07 TR53-09. 2 L 7 2 4F RT A2NM 2007091300034 20070913 00034 2007 9 13 UPS07650593 4 20070903 A 3442 6225132101 TRANSCEIVER BOEING 767 76734AF 1385212 NM WEATHER RADAR INOPERATIVE A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 329UP 27755 INSPECTION TYPE:ETOP ATB - WX RADAR FAIL DISPLAYED ON HSI W/BOTH SYSTEMS SELECTED. WXR TEST DISPLAYS WXR FAIL WEAK R/T ON HSI. ATB ACCOMPLISHED DUE TO NO WX RADAR AND THUNDERSTORMS ON PLANNED FLIGHT ROUTE. T/S PER FIM 34-43-00. FOUND WX R TRANSCEIVER INOP REMOVED AND REPLACED LEFT IRU & WXR TRANSCEIVER PER MM 34-43-01 & MM 34-21-01 & OPS CHECK NORMAL PER MM 34-43-00. IRU P/N OFF HG1050AE09. S/N OFF 9604132. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007091300035 20070913 00035 WP 2007 9 13 UPS07850574 1 20070731 A 5311 5754671501 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 HEAVY CORROSION ON LWR FLANGE OF FRAME AT STA 1240 L35R. CUT OUT CORRODED AREA OF LWR FLANGE ON FRAM E STA 1240 L35R PER SAA EA 008-5330-01-A0995. REPAIRED LWR FLANGE ON FRAME STA 1240 L35R PER SAA EA 008-5330-01-A0995, UPS RAA DC8-53-20650, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007091300037 20070913 00037 WP 2007 9 13 UPS07850577 1 20070901 A 8010 STARTER DOUG DC8 DC871F 302199D WP PWA JT3D JT3D3 52039 NE NR 1 ENGINE LEAKING A IPXA E ENGINE SHUTDOWN K FLUID LOSS CL CLIMB 1 SO 01 750UP 45950 692519 INSPECTION TYPE:N/A IFSD - NR 1 ENG SHUTDOWN IN CLIMB PASSING 25000 DUE TO OIL QTY GOING TO ZERO. OIL PRESSURE WAS 12 P SI. SERVICED OIL, RAN ENGINE, FOUND OIL LEAKING FROM STARTER. REMOVED AND REPLACED NR 1 ENGINE STARTER IAW MM 80-10-01 -2. OPS CHECK REQUIRED. RAN ENG NO LEAKS NOTED PER 80-10-01. 2 L 7 4 4F 4 F RT 4A25 1E8 2007091300040 20070913 00040 2007 9 13 UPS07850584 4 20070820 A 2565 51561004DG SLIDE DOUG DC8 DC873F 302199F WP L1 DOOR UNSERVICEABLE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 ESCAPE SLIDE HAS FRAYED AREAS ALONG GIRT BAR AND DUE DATE STICKER NOT READABLE. REMOVED AND REPLACED NEW EMERGENCY ESCAPE SLIDE. 2 L 7 4 4F RT 4A25 2007091300055 20070913 00055 NM 2007 9 13 CALA0700489 1 20070904 A 5313 BAC1498156 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 INSPECTION FOUND STRINGER 25L CORRODED FROM STA 967-986.5, LBL 17. A REPAIR WAS INSTALLED IAW SRM 53-00-03, PAGE 206, F IGURE 201. 2 L 7 2 4F RT A16WE 2007091300057 20070913 00057 WP 2007 9 13 MWEA070203 1 20070831 A 5320 2912727 STRUCTURE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 AFT CARGO COMPARTMENT AT STATION 1289 STR 24L WITH CORROSION ON VERTICAL WALLS. FABRICATED AND INSTALLED REPAIR DOUBLER S. 2 L 7 2 4F A6WE 2007091300058 20070913 00058 WP 2007 9 13 MWEA070204 1 20070901 A 5313 27779485 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 FOUND LONGERON 26 CRACKED AT STATION 160.00 IN E&E COMPARTMENT. CUT OUT LONGERON AND INSTALLED REPAIR SPLICE. 2 L 7 2 4F A6WE 2007091300060 20070913 00060 NM 2007 9 13 ASAA0742008 1 20070827 A 5512 65C274824745 SKIN BOEING 737 7374Q8 138447Q NM HORIZ STAB DAMAGED A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 784AS 28199 DAMAGE TO LEFT HORIZONAL STABILIZER TIP DUE TO CONTACT FROM AIRCRAFT PUSHING BACK INTO ALLEY. INTERM REPAIR PER EA 5510 01303 AIRCRAFT RELEASED FOR FERRY FLIGHT TO YXX. 2 L 7 2 4F RT A16WE 2007091300072 20070913 00072 WP 2007 9 13 UPS07850592 1 20070804 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 SEAT TRACK GOUGED AT STA 317 RBL 60. REMOVED DAMAGED SEAT TRACK AT STA 317 RBL 60 IAW EO DC8-5340-77 79. INSTALLED SEAT TRACK PLUG AT STA 317 RBL 60 IAW EO DC8-5340-7779 APPX A AND SRM 53-2-3 FIG 6D. 2 L 7 4 4F RT 4A25 2007091300074 20070913 00074 WP 2007 9 13 UPS07850595 1 20070821 A 5522 SKIN DOUG DC8 DC873F 302199F WP LT ELEVATOR DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 LEFT ELEV UPPER SKIN DENTED AT T/E STA XE200. CUT OUT DAMAGED AREA ON LEFT ELEV STA XE 200 IAW SRM 5 5-02-01 FIG 10. FABRICATED AND INSTALLED REPAIR DOUBLER AT LEFT ELEV STA XE 200 IAW SRM 55-02-01 FIG 10. CALCULATED WE IGHT AND BALANCE IAW SRM 51-04 -08-0 FIG 059R. 2 L 7 4 4F RT 4A25 2007091300078 20070913 00078 WP 2007 9 13 UPS07850607 1 20070904 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:N/A ON PREFLIGHT FOUND EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK AND REL AY UNIT PER MM 33-50-01-2. SYSTEM OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2007091300081 20070913 00081 NM 2007 9 13 ASAA0752012 1 20070831 A 5720 115A29531 SUPPORT BOEING 737 737890 1384527 NM LT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 546AS 30022 LEFT WING UPPER TRAILING EDGE PANEL (WS 278.5) RT AFT ANGLE SUPPORT CRACKED. REPLACED WITH FABRICATED PART. 2 L 7 2 4F RT A16WE 2007091300083 20070913 00083 NM 2007 9 13 ASAA0752014 1 20070901 A 5753 113A91602 FAIRING BOEING 737 737890 1384527 NM FLAP DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 546AS 30022 RIGHT OUTBOARD FLAP FAIRING HAS LIGHTNING STRIKE DAMAGE TO AFT FRAME AFT SIDE LT. REPAIRED IAW EA5750 02386. 2 L 7 2 4F RT A16WE 2007091300084 20070913 00084 NM 2007 9 13 SB07075 1 20070906 A 3350 1012721 LIGHT BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 432US 24554 BDL - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 11C AND 12C INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLIES AT SEATS 11C AND 12C. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007091300085 20070913 00085 NM 2007 9 13 USAA070712 1 20070906 A 5313 STRINGER SPLICE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 442US 24841 STR 15L, STA 360, STRINGER SPLICE CRACKED. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER SRM 51-40-02, DEFECT SIZE: .5 I NCHES. 2 L 7 2 4F RT A16WE 2007091300086 20070913 00086 NM 2007 9 13 USAA070711 1 20070906 A 5320 SILL BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 23380 STA 795 I/B OF STR 25R DOOR SILL HAS CORROSION. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER SRM 51-40-02, DEFECT SIZE: 1 X 1 INCH. 2 L 7 2 4F RT A16WE 2007091300088 20070913 00088 2007 9 13 ZZDA2007268 4 20070905 A 2565 LANYARD BOEING 717 717200 1383700 NM EVAC SLIDE PULLED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 943AT 55006 L1 DOOR SLIDE LANYARD IS PULLED. BOTH PINS ARE PULLED ON SLIDE PACK. REMOVED AND REPLACED L1 DOOR SLIDE PACK IAW B717 M/M 25-61. 2 L 7 2 4F TR A6WE 2007091300090 20070913 00090 EU 2007 9 13 TRAX200701274 1 20070830 A 5311 FRAME AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 ON FRAME 38 BETWEEN STRINGER 21 LEFT AND STRINGER 20 LEFT CORROSION FOUND. CORROSION REMOVED IAW SRM 51-21-42. 2 H 7 2 4T RT 2007091300091 20070913 00091 EU 2007 9 13 TRAX200701275 1 20070830 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 RIGHT SEAT TRACK BETWEEN FR 39-40 CORROSION FOUND. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42. 2 H 7 2 4T RT 2007091300096 20070913 00096 EU 2007 9 13 TRAX200701280 1 20070831 A 5320 STRUCTURE AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 ON RIGHT Z-FLOOR, BETWEEN FR 39 AND FR 41 CORROSION FOUND. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42. 2 H 7 2 4T RT 2007091300097 20070913 00097 EU 2007 9 13 TRAX200701281 1 20070831 A 5313 STRINGER AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 ON FR 37, RIGHT SIDE AT STRINGER 14 CORROSION FOUND. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42. 2 H 7 2 4T RT 2007091300098 20070913 00098 EU 2007 9 13 TRAX200701282 1 20070831 A 5320 NUT AEROSP ATR72 ATR72 EU CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 LEFT SEAT DOOR BETWEEN FR 41 AND 44 ANCHOR NUT FOUND BROKEN. REPLACED SRM 51-25-01 2 H 7 2 4T RT 2007091300099 20070913 00099 EU 2007 9 13 TRAX200701283 1 20070831 A 5311 FRAME AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 FR 38 CORRODED, FOUND OUT OF LIMIT ON W/C 100-44, NEEDS REPAIR. REPAIRED AS PER SRM 53-61-40 FIG 414. 2 H 7 2 4T RT 2007091300101 20070913 00101 EU 2007 9 13 TRAX200701285 1 20070831 A 5315 FLOORBEAM AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 ON FLOORBEAM AT FR 36 CORROSION FOUND. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42 2 H 7 2 4T RT 2007091300104 20070913 00104 NM 2007 9 13 USAA920070807 1 20070902 A 5330 6545765 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 23379 CTL - MAJOR REPAIR - NR 4214778 - CRACKED FUSELAGE SKIN, BS 520, S10L. REPAIRED FUSELAGE SKIN, BS 520, S10L IAW B737-30 0 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2007091300106 20070913 00106 NM 2007 9 13 USAA920070809 1 20070825 A 5320 141N5170 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 942UW 27807 BFM - MAJOR REPAIR - C-4 CHECK - NR 6003955, CORROSION ON FLOOR SUPPORT WEB, BS 324 - BS 345, LBL 32. REPLACED FLOOR SU PPORT WEB, BS 324 - BS 345, LBL 32 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007091300107 20070913 00107 NM 2007 9 13 USAA920070810 1 20070829 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 942UW 27807 BFM - MAJOR REPAIR - C-4 CHECK - NR 6003909, CORROSION ON FLOORBEAM, BS 377.7, LBL 59 - RBL 30. REPAIRED FLOORBEAM, BS 377.7, LBL 59 - RBL 30 IAW USAIRWAYS TYPICAL REPAIR 53-15-01. 2 L 7 2 4F RT A2NM 2007091300110 20070913 00110 NM 2007 9 13 USAA920070813 1 20070829 A 5320 141N51704 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 942UW 27807 BFM - MAJOR REPAIR - C-4 CHECK - NR 6003954, CORROSION ON FLOOR SUPPORT WEB, BS 340, LBL 21 - LBL 30. REPLACED FLOOR SU PPORT WEB, BS 340, LBL 21 - LBL 30 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007091300111 20070913 00111 NM 2007 9 13 SWAA074396 1 20070905 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091300112 20070913 00112 NM 2007 9 13 SWAA074407 1 20070905 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091300113 20070913 00113 NM 2007 9 13 SWAA074386 1 20070905 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 1010, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007091300114 20070913 00114 NM 2007 9 13 SWAA074411 1 20070905 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091300115 20070913 00115 NM 2007 9 13 SWAA074395 1 20070905 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007091300116 20070913 00116 NM 2007 9 13 USAA920070817 1 20070907 A 5330 6552988 SKIN BOEING 737 737301 1384611 NM ZONE 100 - FUSEL CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 501UW 23231 CTL - MAJOR REPAIR - NR 4217926, CRACKED FUSELAGE SKIN, BS 909, S23R. REPAIRED FUSELAGE SKIN, BS 909, S23R IAW B737-300 SRM 53-00-01 REPAIR 31. DURING THE REPAIR OF THE DISCREPANCY IN NR 4217926 A SECOND CRACK WAS IDENTIFIED AND DOCUMENT ED ON NR 4217924. THE REPAIR FOR THE SECOND CRACK WAS INCORPORATED INTO THE FIRST REPAIR. 2 L 7 2 4F RT A16WE 2007091300117 20070913 00117 NM 2007 9 13 SWAA074410 1 20070905 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091300118 20070913 00118 NM 2007 9 13 SWAA074397 1 20070905 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091300119 20070913 00119 NM 2007 9 13 SWAA074398 1 20070905 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091300120 20070913 00120 NM 2007 9 13 SWAA074399 1 20070905 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091300122 20070913 00122 NM 2007 9 13 SWAA074409 1 20070905 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091300123 20070913 00123 NM 2007 9 13 SWAA074408 1 20070905 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091300124 20070913 00124 NM 2007 9 13 SWAA074402 1 20070905 A 5330 65C337568 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007091300127 20070913 00127 NM 2007 9 13 SWAA074423 1 20070905 A 2750 69466493 TORQUE TUBE BOEING 737 7373Q8 1384670 NM T/E FLAP WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED BRDG CHECK, FOUND RIGHT OUTBOARD T/E FLAP TORQUE TUBE WORN. REMOVED AND REPLACED TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007091300131 20070913 00131 NM 2007 9 13 SWAA074375 1 20070904 A 2560 P4010021 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 436WN 32456 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2007091300132 20070913 00132 NM 2007 9 13 CALA0700491 1 20070906 A 5311 65465632 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 INSPECTION FOUND FRAME TO SKIN ATTACH POINT CORRODED AT BS 967 JUST I/B OF S27L. A REPAIR WAS INSTALLED IAW ECRA 5310-0 4654B. 2 L 7 2 4F RT A16WE 2007091300135 20070913 00135 NM 2007 9 13 CALA0700494 1 20070906 A 5311 6546552 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17328 23458 INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 827, S9L. REPAIR ANGLES WERE INSTALLED IAW ECRA 5310-04651. 2 L 7 2 4F RT A16WE 2007091300136 20070913 00136 NM 2007 9 13 CALA0700495 1 20070906 A 5311 6546555 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17328 23458 INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 867, S9L. A REPAIR WAS INSTALLED IAW ECRA 5310-04651. 2 L 7 2 4F RT A16WE 2007091300137 20070913 00137 NM 2007 9 13 CALA0700496 1 20070906 A 5311 6546558 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17328 23458 INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 907, S9L. REPAIRED IAW ECRA 5310-04651. 2 L 7 2 4F RT A16WE 2007091300143 20070913 00143 NM 2007 9 13 CALA0700502 1 20070906 A 5311 6546534 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A .5 INCH CRACK IN FRAME O/B OF LEFT KEEL BEAM AT STA 520, S27L TO S28L. THE CRACK WAS LOCATED AT THE SECOND FASTENER HOLE FROM THE BOTTOM. 2 L 7 2 4F RT A16WE 2007091300144 20070913 00144 NM 2007 9 13 CALA0700503 1 20070906 A 5313 6545776 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND AFT CARGO STRINGER 26L CORRODED AT STA 727E + 11 INCHES. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A REPAIR WAS SPLICED IN IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 2007091300145 20070913 00145 WP 2007 9 13 MWEA070205 1 20070906 A 2560 P4010021 BATTERY DOUG DC9 DC981 3022081 WP FLASHLIGHT DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 813ME 48007 EMERGENCY FLASHLIGHT AT FLIGHT ATTENDANT 1A NOT SHOWING FLASHING RED CHARGE INDICATION. REMOVED AND REPLACED BATTERY. 2 L 7 2 4F A6WE 2007091300150 20070913 00150 NM 2007 9 13 SWAA074430 1 20070906 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER SWA EA. 2 L 7 2 4F RT A16WE 2007091300153 20070913 00153 NM 2007 9 13 SWAA074431 1 20070906 A 5524 185A410017 HINGE BRACKET BOEING 737 7377H4 1384404 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 462WN 32466 DURING SCHEDULED HC1 CHECK, FOUND RIGHT ELEVATOR OUTBOARD HINGE PLATE WORN. REMOVED AND REPLACED HINGE PLATE PER MM. 2 L 7 2 4F RT A16WE 2007091300154 20070913 00154 NM 2007 9 13 SWAA074428 1 20070906 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 AFT CABIN EMERGENCY EXIT LIGHTS WILL NOT SHUT OFF. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007091300002 20070913 00002 EA 2007 9 13 SIMA200724703 1 20070903 A 5610 NP13932211 WINDOW CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 CRACKED A SIMA O OTHER O OTHER AP APPROACH 1 SW 21 508AE 11434 10072 CAPTAINS LEFT SIDE WINDOW CRACKED ON SHORT FINAL. REMOVED AND REPLACED CAPTAINS SIDE WINDOW IAW CRJ AMM 56-12-01. OPERA TIONAL CHECK GOOD - AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT A21EA 2007091300011 20070913 00011 NM 2007 9 13 MWEA070194 1 20070902 A 7830 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 904ME 55168 LEFT HAND REVERSER UPPER BUCKET STATION 26, ZEE FRAME IS CRACKED AT OUTBOARD END. 2 L 7 2 4F TR A6WE 2007091300017 20070913 00017 NM 2007 9 13 MWEA070200 1 20070902 A 7830 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 904ME 55168 RIGHT THRUST REVERSER UPPER BUCKET STATION 35 ZEE FRAME IS CRACKED AT OUTBOARD END. 2 L 7 2 4F TR A6WE 2007091300020 20070913 00020 NM 2007 9 13 ZZDA2007264 1 20070827 A 3350 AMC7265001GPC LIGHT BOEING 717 717200 1383700 NM CABIN MISSING A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 919AT 55084 E-PATH LAMPS & WHITE LENS MISSING AT ROW 10. INSTALLED LENS & LAMPS AS REQ'D. OPS CHECK NORMAL IAW AMM 33-51. 2 L 7 2 4F TR A6WE 2007091300022 20070913 00022 NM 2007 9 13 ZZDA2007266 1 20070830 A 5311 STRAP BOEING 717 717200 1383700 NM FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 977AT 55036 AFT FUSELAGE COMPARTMENT CANTE FRAME SUPPORT STRAP AT STA 1178, BETWEEN LONG 16 AND 17 RIGHT HAND CRACKED. INSTALLED FO RMED ANGLE REPAIR AT FUS 1178 BETWEEN LONG 16 AND 17 RIGHT HAND PER SRM 51-70-11 FIG 201. 2 L 7 2 4F TR A6WE 2007091300023 20070913 00023 NM 2007 9 13 ZZDA2007267 1 20070830 A 5311 STRAP BOEING 717 717200 1383700 NM FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 977AT 55036 AFT FUSELAGE COMPARTMENT CANTE FRAME SUPPORT STRAP AT STA 1178, BETWEEN LONG 16 AND 17 LEFT HAND CRACKED. INSTALLED FOR MED ANGLE REPAIR AT FUS 1178 BETWEEN LONG 16 AND 17 LEFT HAND PER SRM 51-70-11 FIG 201. 2 L 7 2 4F TR A6WE 2007091300024 20070913 00024 EU 2007 9 13 UPS07150557 1 20070830 A 7931 INDICATOR AIRBUS A300 A300F4622R 3930360 EU PWA 4158 PW4158 NE COCKPIT FLUCTUATES A IPXA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 01 138UP 0821 INSPECTION TYPE:N/A DURING CLIMBOUT RIGHT ENGINE OIL PRESSURE INDICATION WENT TO XX ON BOTH ECAM & GAUGE, AFTER A COUPLE OF MINUTES INDICATION CAME BACK BUT WAS FLUCUATING, CREW REDUCED ENGINE POWER BUT DID NOT SHUTDOWN ENGINE, ON DESCENT E VERYTHING RETURNED TO NORMAL. VERIFIED INTEGRITY OF WIRING FROM XMTR TO IND. REMOVED AND REPLACED PRESS XMTR IAW 79-33 -11-04. REMOVED AND REPLACED COCKPIT IND IAW 79-33-21-04 ON TECH SERVICE RECOMMENDATION PRECAUTIONARY. RAN ENG AT VARI OUS PWR SETTINGS. OIL PRESSURE IND ON DUAL INDICTOR & ECAM NORMAL. OK FOR CONTINUED SERVICE. 2 L 7 2 4F 4 F RT A35EU E24NE 2007091300025 20070913 00025 NM 2007 9 13 UPS07450578 1 20070817 A 5420 65B90362602 STIFFENER BOEING 747 747200 1384847 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C NR 2 PYLON RIGHT UPPER STIFFENER FOUND CRACKED JUST AFT OF FWD ENGINE MOUNT NR 13 HOLE AT INTERNAL ANG LE (1.125 INCH APPROX). NR 2 PYLON AFT OF RIGHT FWD ENGINE MOUNT NR 13 HOLE UPPER STIFFENER REPAIRED AS PER HX RS R54-5 0-35861 DETAIL VISUAL REPEAT INSPECTION IS REQUIRED TO THE SUBJECT REPAIR AREA EVERY C-CHECK OR 18 MONTHS WHICHEVER OCCU RS FIRST REF UPS EO B747-5410-27520. 2 L 7 4 4F RT A20WE 2007091300032 20070913 00032 NM 2007 9 13 UPS07550576 1 20070802 A 5330 202473040C SKIN BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 415UP 23855 INSPECTION TYPE:C DENT AT FUSELAGE INNER SURFACE APPROX STA 1574, BETWEEN S27R AND S28R. DENT FOUND TO BE OIL CANNING, REQUIRES SKIN REPAIR PER SRM 53-00-01. REMOVED DAMAGED AREA IAW SRM 53-00-01 2R FIG 201 SHEET 3 AND INSTALLED REPAIR DO UBLER AND FILLER IAW 53-00-01-2R FIG 201. NOTE: THIS IS A PERMANENT REPAIR. 2 L 7 2 4F RT A2NM 2007091300044 20070913 00044 WP 2007 9 13 UPS07850587 1 20070810 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 TRANSFERRED FROM LP 749931 ITEM 2: MINOR FUSELAGE SKIN DENT DMG AT STA 1867 L32R. CUT OUT DAMAGED A REA AT STA 1867 L32R IAW SRM 53-02-01 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AT STA 1867 L32R IAW SR M 53-05-03-0, AND 53-02-01 FIG 07. 2 L 7 4 4F RT 4A25 2007091300046 20070913 00046 WP 2007 9 13 UPS07850589 1 20070814 A 5532 SKIN DOUG DC8 DC873F 302199F WP VERTICAL STAB LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 OUTER SKIN LOOSE AROUND COUNTERSINKS AT TOP OF VERTICAL STAB L/E LWR SECTION. REMOVED EXISTING FASTE NERS AND FABRICATED AND INSTALLED REPAIR DOUBLER AT TOP OF VERT STAB L/E LWR SECTION IAW SRM 55-2-1 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007091300051 20070913 00051 NM 2007 9 13 CALA0700485 1 20070902 A 5230 65479520257 WEB BOEING 737 7373T0 1384582 NM C2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A .25 INCH CRACK IN C-2 DOOR LOWER BEAM NR 5 WEB. THE CRACK WAS AT A FASTENER HOLE NEAR FORWARD STOP F ITTING AND OUTER T-CHORD. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007091300052 20070913 00052 NM 2007 9 13 CALA0700486 1 20070902 A 5315 BAC1506210 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17328 23458 INSPECTION FOUND AFT ENTRY FLOORBEAM CORRODED AT STA 1016, RBL 6 TO RBL 20. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03 851. 2 L 7 2 4F RT A16WE 2007091300059 20070913 00059 EU 2007 9 13 USAA200708006 1 20070830 A 5753 FLAP AIRBUS A319 A319112 3930323 EU RT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 703UW 0904 A 25 X 11 INCH DELAMINATION AT RIGHT O/B FLAP T/E AREA. REPAIRED IN ACCORDANCE WITH SRM 57-53-00 & EA 84951 & SRM 57-53 -00. 2 L 7 2 4F RT A28NM 2007091300075 20070913 00075 WP 2007 9 13 UPS07850597 1 20070818 A 5514 DOUBLER DOUG DC8 DC873F 302199F WP HORIZ STAB CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 OVERSIZED HOLE, 2 SHEARED RIVETS IN CHAFE STRIP AND ATTACH FLANGE ON I/B END OF LEFT HORIZONTAL STAB L/E. REMOVED OUTER RUB STRIP DOUBLERS ON I/B END OF LEFT HORIZONTAL STAB L/E IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLER AT LEFT HORIZONTAL STAB L/E IAW SRM 51-1-21, AND DWG 5644330. 2 L 7 4 4F RT 4A25 2007091300077 20070913 00077 WP 2007 9 13 UPS07850604 1 20070830 A 5522 SKIN DOUG DC8 DC873F 302199F WP LT ELEVATOR GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 LEFT ELEV UPPER SKIN GOUGED VERY INBOARD SIDE. DRILLED UP DAMAGED AREA ON LEFT ELEV UPPER SKIN IAW S RM 55-02-00 FIG 006. PLUGGED HOLE IN LEFT ELEV UPPER SKIN IAW SRM 55-02-00 FIG 006. 2 L 7 4 4F RT 4A25 2007091300092 20070913 00092 EU 2007 9 13 TRAX200701276 1 20070830 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 LEFT SEAT TRACK BETWEEN FR 36-39 CORROSION FOUND. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42. 2 H 7 2 4T RT 2007091300093 20070913 00093 EU 2007 9 13 TRAX200701277 1 20070830 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 RIGHT SEAT TRACK BETWEEN FR 36-39 CORROSION FOUND. REPAIR ACCOMPLISHED IN ACCORDANCE WITH 51-21-42. 2 H 7 2 4T RT 2007091300095 20070913 00095 EU 2007 9 13 TRAX200701279 1 20070831 A 5347 NUT AEROSP ATR72 ATR72 EU SEAT TRACK BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 ON RIGHT SEAT TRACK BETWEEN FR 36 AND FR 39 ANCHOR NUT FOUND BROKEN. 2 H 7 2 4T RT 2007091300102 20070913 00102 EA 2007 9 13 TRAX200701286 1 20070902 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 845AS 7324 FWD CEILING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007091300108 20070913 00108 NM 2007 9 13 USAA920070811 1 20070829 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 942UW 28707 BFM - MAJOR REPAIR - C-4 CHECK - NR 6003741, CORROSION ON FLOORBEAM, BS 365.25, LBL 11.5 - RBL 50.5. REPAIRED FLOORBEAM , BS 365.25, LBL 11.5 - RBL 50.5 IAW USAIRWAYS TYPICAL REPAIR 53-15-01. 2 L 7 2 4F RT A2NM 2007091300109 20070913 00109 NM 2007 9 13 USAA920070812 1 20070830 A 5320 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 942UW 27807 BFM - MAJOR REPAIR - C-4 CHECK - NR 6003912, CORROSION ON FLOOR SUPPORT WEB, BS 340 - BS 395, RBL 14 - RBL 23. REPLACED FLOOR SUPPORT WEB, BS 340 - BS 395, RBL 14 - RBL 23 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007091300121 20070913 00121 NM 2007 9 13 SWAA074385 1 20070905 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091300129 20070913 00129 2007 9 13 SWAA074373 4 20070904 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007091300130 20070913 00130 2007 9 13 SWAA074394 4 20070905 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007091300134 20070913 00134 NM 2007 9 13 CALA0700493 1 20070902 A 5311 6546532 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17328 23458 INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 480 BETWEEN STRINGERS 8 AND 9R. A REPAIR WAS INSTALLED IAW ECRA 5310- 04651. 2 L 7 2 4F RT A16WE 2007091300141 20070913 00141 NM 2007 9 13 CALA0700500 1 20070906 A 5311 6546551 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17328 23458 INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 807, S9R. REPAIRED IAW ECRA 5310-04651. 2 L 7 2 4F RT A16WE 2007091300142 20070913 00142 NM 2007 9 13 CALA0700501 1 20070906 A 5311 6546554 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17328 23458 INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 847, S9L. REPAIRED IAW ECRA 5310-04651. 2 L 7 2 4F RT A16WE 2007091300157 20070913 00157 NM 2007 9 13 SWAA074451 1 20070906 A 5330 6545766 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 729E, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007091300158 20070913 00158 NM 2007 9 13 SWAA074433 1 20070906 A 5330 6545767 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510D, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007091300159 20070913 00159 NM 2007 9 13 SWAA074441 1 20070906 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 817, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007091300160 20070913 00160 NM 2007 9 13 SWAA074457 1 20070906 A 5310 6545833 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 188 AND BS 196.5, STR 17R. REMOVED AND REPLACED W EB PER SRM. 2 L 7 2 4F RT A16WE 2007091300166 20070913 00166 NM 2007 9 13 SWAA074429 1 20070906 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091300171 20070913 00171 NM 2007 9 13 SWAA074458 1 20070906 A 5330 6547955 BEAR STRAP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT BS 847, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007091300172 20070913 00172 NM 2007 9 13 SWAA074427 1 20070906 A 3350 6556633 LENS BOEING 737 7373K2 13844BA NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED MV2 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007091300173 20070913 00173 2007 9 13 SWAA074432 4 20070906 A 2565 6557463 BRACKET BOEING 737 7373H4 1384600 NM EVAC SLIDE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM. 2 L 7 2 4F RT A16WE 2007091300175 20070913 00175 NM 2007 9 13 SWAA074450 1 20070906 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28R AND STR 28L. REMOVED AND REPLACED STRINGER C LIP PER SRM. 2 L 7 2 4F RT A16WE 2007091300176 20070913 00176 NM 2007 9 13 SWAA074448 1 20070906 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091300177 20070913 00177 NM 2007 9 13 SWAA074444 1 20070906 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091300178 20070913 00178 NM 2007 9 13 SWAA074447 1 20070906 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091300179 20070913 00179 NM 2007 9 13 SWAA074452 1 20070906 A 5330 65C381921 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 513B, STR 17L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007091300180 20070913 00180 NM 2007 9 13 SWAA074455 1 20070906 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 738CB 27870 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, STR 17. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007091300184 20070913 00184 NM 2007 9 13 USAA920070816 1 20070905 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 501UW 23231 CTL - MAJOR REPAIR - NR 4217925, CRACKED FUSELAGE SKIN, BS 767, S22R - S23R. REPAIRED FUSELAGE SKIN, BS 767, S22R - S23 R IAW B737-300 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2007091300186 20070913 00186 NM 2007 9 13 CALA0700505 1 20070907 A 5330 6545800 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17328 23458 INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT AFT LOWER CORNER OF R-1 DOOR CUTOUT, STA 328-344, S16R TO S17R. T HE SKIN WAS REPAIRED IAW SRM 53-10-01. 2 L 7 2 4F RT A16WE 2007091300188 20070913 00188 NM 2007 9 13 CALA0700507 1 20070908 A 5313 65617775 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A 1 INCH CRACK IN STRINGER 16L AT STA 360. A STRINGER SPLICE WAS INSTALLED IAW ECRA 5311-01354. 2 L 7 2 4F RT A16WE 2007091300189 20070913 00189 NM 2007 9 13 CALA0700508 1 20070908 A 5330 6552988 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17328 23458 INSPECTION FOUND INNER SKIN CORRODED AT STA 970-990 UNDER S25L. THE SKIN WAS REPAIRED IAW SRM 53-00-01, FIGURE 201, PAG E 235, DETAIL XIII. 2 L 7 2 4F RT A16WE 2007091300192 20070913 00192 SO 2007 9 13 LR7A07083 1 20070905 A 5230 STIFFENER LKHEED 382 382G 526414U SO FS 1012 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2537 4698 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5212, FOUND CARGO DOOR BHD STIFFENER CRACKED AT FS1012 BL20L. STIFFENER FABRI CATED USING 7075T6 .050" AND REPLACED IAW SMP583 CHAPTER 51-60 & 51-70. 2 H 7 4 4T A1SO 2007091300223 20070913 00223 EU 2007 9 13 AWXA200701077 1 20070823 A 5554 D5537131800200 FITTING AIRBUS 320 A320232 3930326 EU ZONE 300 WORN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-07 CHECK - NR 5980025, RUDDER HINGE NR 4 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 2632/RIB 6. REPLACED RUDDER HINGE NR 4, VERTICAL STABILIZER STATION 2632/RIB 6 IAW A320 AMM 27-21-00 AND 55-36-41. 2 L 7 2 4F RT A28NM 2007091300224 20070913 00224 NM 2007 9 13 AWXA200701078 1 20070816 A 5311 65465525002 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5988035, CRACKED FRAME, BS 827, S9R. REPAIRED FRAME, BS 827, S9R IAW USAIRWAYS EA 120228. 2 L 7 2 4F RT A16WE 2007091300225 20070913 00225 NM 2007 9 13 AWXA200701079 1 20070816 A 5311 65465515002 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5988034, CRACKED FRAME, BS 807, S9R. REPAIRED FRAME, BS 807, S9R IAW USAIRWAYS EA 120228. 2 L 7 2 4F RT A16WE 2007091300226 20070913 00226 NM 2007 9 13 AWXA200701080 1 20070815 A 5311 65465575004 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5987971, CRACKED FRAME, BS 887, S9R. REPAIRED FRAME, BS 887, S9R IAW USAIRWAYS EA 120228. 2 L 7 2 4F RT A16WE 2007091300227 20070913 00227 NM 2007 9 13 AWXA200701081 1 20070815 A 5311 6546529 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5987969, CRACKED FRAME, BS 440, S9R. REPAIRED FRAME, BS 440, S9R IAW USAIRWAYS EA 120228. 2 L 7 2 4F RT A16WE 2007091300228 20070913 00228 NM 2007 9 13 AWXA200701082 1 20070815 A 5311 6546532 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5987972, CRACKED FRAME, BS 480, S9L. REPAIRED FRAME, BS 480, S9L IAW USAIRWAYS EA 120228. 2 L 7 2 4F RT A16WE 2007091300229 20070913 00229 NM 2007 9 13 AWXA200701083 1 20070815 A 5311 6546554 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5987975, CRACKED FRAME, BS 847, S9L. REPAIRED FRAME, BS 847, S9L IAW USAIRWAYS EA 120228. 2 L 7 2 4F RT A16WE 2007091300230 20070913 00230 SO 2007 9 13 LR7A07069 1 20070801 A 5312 339482 MANIFOLD LKHEED 382 382G 526414U SO FS 567 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 578 4606 DURING SCHEDULED B-1 CHECK PER HB5301, FOUND RT MAIN WHEEL WELL MANIFOLD CRACKED, FS567, WL140, RBL62. MANIFOLD REPLACE D IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007091300232 20070913 00232 WP 2007 9 13 MWEA070206 1 20070906 A 5711 59205035 SPAR DOUG DC9 DC981 3022081 WP WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 LOWER WING AND REAR SPAR HAS CORROSION, CRACK NOTED ABOUT XCW 18-21 OUTBOARD OF CENTER BELLY AREA LEFT SIDE. REMOVED CO RROSION AND FABRICATED AND INSTALLED FASTENER. 2 L 7 2 4F A6WE 2007091300235 20070913 00235 WP 2007 9 13 MWEA070209 1 20070910 A 5230 59101419 PAN DOUG DC9 DC981 3022081 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 LOWER CENTER CARGO DOOR FORWARD OUTER PAN HAS A CRACK BETWEEN STOP 1 & 2. FABRICATED AND INSTALLED PAN. 2 L 7 2 4F A6WE 2007091300245 20070913 00245 NM 2007 9 13 SWAA074478 1 20070907 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 464WN 32468 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVERS CRACKED BETWEEN ROW 11 ABC AND ROW 15 ABC. REMOVED AND REPLACED COVERS P ER MM. 2 L 7 2 4F RT A16WE 2007091300246 20070913 00246 NM 2007 9 13 SWAA074459 1 20070907 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 495WN 33869 EEPLS COVER LOOSE AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007091300247 20070913 00247 NM 2007 9 13 SWAA074482 1 20070908 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 409WN 27896 EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007091300248 20070913 00248 NM 2007 9 13 SWAA074475 1 20070909 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 417WN 29822 DURING SCHEDULED MV1 CHECK, FOUND EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007091300249 20070913 00249 NM 2007 9 13 SWAA074476 1 20070907 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 464WN 32468 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVERS CRACKED BETWEEN ROW 3 ABC AND ROW 4 ABC. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2007091300250 20070913 00250 NM 2007 9 13 SWAA074477 1 20070907 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 464WN 32468 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVERS CRACKED BETWEEN ROW 8 ABC AND ROW 9 ABC. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2007091300252 20070913 00252 NM 2007 9 13 SWAA074483 1 20070908 A 3350 417A5703 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 495WN 33869 EEPLS LIGHT ASSY BROKEN AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007091300253 20070913 00253 2007 9 13 SWAA074479 4 20070907 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 466WN 30677 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007091300254 20070913 00254 2007 9 13 SWAA074470 4 20070907 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 290WN 36632 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007091300256 20070913 00256 2007 9 13 SWAA074486 4 20070908 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 704SW 27838 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007091300257 20070913 00257 NM 2007 9 13 SWAA074462 1 20070907 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 762 AND BS 770, STR 19L AND STR 18L. REPAIRED SKIN PE R SWA EA. 2 L 7 2 4F RT A16WE 2007091300262 20070913 00262 NM 2007 9 13 SWAA074463 1 20070907 A 5330 6545877 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007091400002 20070914 00002 2007 9 14 SIMA200725601 4 20070912 A 3414 INDICATOR SAAB SF340 340B 7860101 EU AIRSPEED MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 340RC 340B340 CREW REPORTED ABORTED TAKE OFF DUE TO CAPTAIN AIRSPEED INDICATION SHOWING RED FLAGS AND AIR SPEED INDICATION CIRCUIT BRE AKER F15 POPPED. MTX INSPECTED AND RESET CB F15 AND PERFORMED OPERATIONAL CHECK ON AIR DATA AND SERVO INSTRUMENT SYS IA W SAAB 340B AMM 34-12-00-05. OPS CHECK GOOD AT THIS TIME, NO DEFECTS NOTED AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007091400003 20070914 00003 SO 2007 9 14 SIMA200725602 1 20070912 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 644AE 145204 NOTIFIED BY THE CREW VIA TELESIS. FORWARD EMERGENCY EXIT SIGN ACROSS FROM GALLEY INOP AND EMERGENCY EXIT LIGHT IN COCKP IT STEP INOP. REMOVED AND REPLACED BATTERY PACK AT POS NR 1 IAW AMM 33-50-04. OPS CK GOOD AIRCRAFT RETURNED TO SERVICE . 2 L 7 2 4T RT T00011AT 2007091400004 20070914 00004 2007 9 14 SIMA200725604 4 20070911 A 3417 ADC CNDAIR CL600 CL6002C10 1390015 EA NR 1 MALFUNCTIONED A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 522AE 10147 AFTER DEPARTURE, CAPT NOTICED FIRST OFFICERS LOW SPEED AWARENESS CUE 1KIAS ABOVE CLIMB OUT SPEED "CLEAN CONFIGURATION." ABOUT 20 KIAS REMAIN UNTIL INCREASED TO 320 KIAS AT 31000 FT. CREW ELECTED TO RETURN TO DFW. ON DESCENT GOT STALL FA IL CAUTION MSG TWICE AND IT WAS ABOVE IAS ABOUT 20 KIAS UNTIL FLAPS WERE DEPLOYED. LANDING WEIGHT WAS 2200 LBS OVER TOU CH DOWN LIMITS WITH A V/S OF LESS THAN 100 FPM. AIRCRAFT RETURNED SAFELY TO THE GATE. REMOVED AND REPLACED NR 1 AIR DA TA COMPUTER IAW AMM 34-13-01 BIT TEST GOOD LEAK CHECK GOOD AND PASSED FUNCTIONAL CHECK FLIGHT AIRCRAFT RETURNED TO SERVI CE. 2 L 7 2 4F RT A21EA 2007091400005 20070914 00005 SO 2007 9 14 SIMA200725603 1 20070912 A 2120 8151138 COUPLING EMB 135 EMB135KL 3260302 SO CABIN DIST BLOWN A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 843AE 145680 AFTER DEPARTURE, NR 1 PACK VALVE FAIL FOLLOWED SHORTLY BY NR 1 BLEED VALVE CLOSED FOLLOWED CHECKLIST AND AFTER RESET ONC E. FUMES APPEARED IN COCKPIT. RETURNED TO BOS NO OTHER ABNORMALITIES NOTED. NO FUMES IN CABIN. FUMES DISSIPATED AS S OON AS BLEED VALVE CLOSED. FOUND COUPLING BETWEEN DUAL TEMP CONTROL AND NR 1 ACM TUBE BLOWN REMOVED AND REPLACED COUPLI NG IAW EMB AMM 21-60-01. RUN PACK OPS CHECK GOOD IAW AMM 21-51-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007091400007 20070914 00007 NM 2007 9 14 AWXA200701096 1 20070815 A 5311 654655514 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5987976, CRACKED FRAME, BS 867, S9L. REPAIRED FRAME, BS 867, S9L IAW USAIRWAYS EA 120228. 2 L 7 2 4F RT A16WE 2007091400009 20070914 00009 EU 2007 9 14 DHLA200700042 1 20070807 A 3411 INDICATOR AIRBUS 300 A300B4203 3930306 EU COCKPIT INOPERATIVE A DHLA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 GL 05 366DH 249 REJECTED T/O NO CAPT A/S EITHER DIGITAL OR ANALOG. REJECTED AT 80 KTS, 273000 GTOW TEMP 25 DEGS C, NORMAL BREAK ENERGY. FLUSHED NR 1 PITOT SYSTEM AS PER MM 34-11-10. DEBRIS CLEARED FROM LINES. PERFORMED PITOT/STATIC LEAK TEST NO LEAKS N OTED SYSTEM CHECKS NORMAL IAW A300 MM 34-11-00 A/C IS RVSM COMPLIANT. 2 L 7 2 4F RT A35EU 2007091400010 20070914 00010 SO 2007 9 14 LR7A07071 1 20070905 A 5311 3390108R FRAME LKHEED 382 382G 526414U SO FS 132, RBL 50 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2537 4698 DURING SCHEDULED C-8 CHECK, PER JOB CARD HC5311, FOUND COCKPIT RT FRAME CRACKED (INTERCOSTAL RIB OUT/IN FOR ACCESS, AT F S 132 WL207-217 RBL50. RIB (FRAME) REPLACED IAW SMP583 CHAPTER 51-60 AND 51-70. INTERCOSTAL RIB REINSTALLED IAW SMP583 CHAPTER 51-70. 2 H 7 4 4T A1SO 2007091400012 20070914 00012 SO 2007 9 14 LR7A07073 1 20070905 A 5310 RIB LKHEED 382 382G 526414U SO FS 204-237 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2537 4698 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5312, FOUND UNDERDECK INTERCOSTAL RIB CRACKED AT FS 204 AND 237 WL204 BL56L. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-19. 2 H 7 4 4T A1SO 2007091400013 20070914 00013 SO 2007 9 14 LR7A07074 1 20070905 A 5310 34257820R RIB LKHEED 382 382G 526414U SO FS 792 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2537 4698 DURING SCHEDULED C-8 CHECK FOUND PER JOB CARD HC5313, FOUND RT FORMER INBD CAP BROKEN AT AFT FUSELAGE INTERIOR FS 792 WL 160 RBL75. REPAIR CARRIED OUT IAW SMP583 FIG 53-50-14. 2 H 7 4 4T A1SO 2007091400014 20070914 00014 SO 2007 9 14 LR7A07075 1 20070905 A 5310 7075T6040 WEB LKHEED 382 382G 526414U SO FS 880 LBL 65 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2537 4698 DURING SCHEDULED C-8 CHECK FOUND PER JOB CARD HC5313, FOUND AFT FUSELAGE INTERIOR LT BHD WEB CRACKED AT FS 880 WL200 BL6 5L. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-17. 2 H 7 4 4T A1SO 2007091400015 20070914 00015 SO 2007 9 14 LR7A07076 1 20070905 A 5310 35184033 GUSSET LKHEED 382 382G 526414U SO FS990, WL280 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2537 4698 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5313, FOUND AFT FUSELAGE INTERIOR UPPER BHD TO RT SIDE BHD GUSSET PLATE CRACKE D AT FS 990 WL280. GUSSET PLATE FABRICATED USING 7075T6 BY 0.160" AND REPLACED IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007091400017 20070914 00017 SO 2007 9 14 LR7A07078 1 20070905 A 5312 7075T6063 BULKHEAD LKHEED 382 382G 526414U SO FS 858 WL 185 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2537 4698 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5313, FOUND AFT FUSELAGE INTERIOR RT BHD CRACKED AT FS 924 WL206 BL63.5. WEB FABRICATED USING 7075T6 .063" AND REPLACED IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007091400018 20070914 00018 SO 2007 9 14 LR7A07079 1 20070905 A 5320 33138683 FITTING LKHEED 382 382G 526414U SO FS 477 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2537 4698 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5313, FOUND CARGO COMPT UPPER TENSION TIE FITTING FOUND CRACKED AT FS 477 WL25 8 RBL63. RT UPPER TENSION TIE FITTING REPLACED IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007091400019 20070914 00019 SO 2007 9 14 LR7A07080 1 20070905 A 5230 7075T6025 BULKHEAD LKHEED 382 382G 526414U SO CARGO DOOR CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2537 4698 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5212, FOUND CARGO DOOR REAR BHD WEB WITH MULTIPLE CRACKS AND REPAIR PATCHES A T FS1035 BL40L TO BL40R. WEB SKIN FABRICATED USING 7075-T6 .025 AND REPLACED IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007091400020 20070914 00020 SO 2007 9 14 LR7A07081 1 20070905 A 5310 339482 MANIFOLD LKHEED 382 382G 526414U SO BS 567 WL 146 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2537 4698 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5323 FOUND HEAT MANIFOLD CRACKED AT LT MLG WELL FS567 WL146. MANIFOLD REPLACE D IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007091400021 20070914 00021 NM 2007 9 14 AWXA200701098 1 20070815 A 5311 6546552 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5987974, CRACKED FRAME, BS 827, S9L. REPAIRED FRAME, BS 827, S9L IAW USAIRWAYS EA 120228. 2 L 7 2 4F RT A16WE 2007091400022 20070914 00022 EU 2007 9 14 F3LA200700216 1 20070902 A 5321 D5367180500400 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CABIN CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON LOWER SURFACE OF FLOOR PANEL 261FF. REMOVED REPLACED FLOOR PANEL I AW SRM 51-24-00 AND AMM 53-42-12-400-002. 2 L 7 2 4F RT A28NM 2007091400024 20070914 00024 EU 2007 9 14 F3LA200700218 1 20070905 A 5321 D5361087600000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR THRESHOLD PANEL 221FF CORRODED TO EDGE. REMOVED AND REPLACED THRESHOLD P ANEL 221FF IAW AMM 53-12-12 AND WORK CARD CP753-12. 2 L 7 2 4F RT A28NM 2007091400025 20070914 00025 EU 2007 9 14 F3LA200700215 1 20070902 A 5315 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED CABIN FLOOR CENTER SUPPORT AT Y254, FR16, CORRODED. REMOVED DAMAGED AREA OF FLO ORBEAM Y254 IAW SRM 53-00-14, FIG 204. REMOVED AND REPLACED FLOORBEAM AND ANGLES IAW SRM 51-42-11, EA NR A9-53R-12100 A ND EA NR AO-51T-11976. 2 L 7 2 4F RT A28NM 2007091400026 20070914 00026 NM 2007 9 14 AWXA200701084 1 20070823 A 5340 140N20012 STRINGER CLIP BOEING 757 7572S7 1384962 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 MCN - MAJOR REPAIR - C-11 CHECK - NR 5988676, CRACKED STRINGER CLIP, BS 1220, S9L. REPLACED STRINGER CLIP, BS 1220, S9L IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007091400027 20070914 00027 EU 2007 9 14 AWXA200701085 1 20070815 A 5320 D53475765200 SILL AIRBUS 320 A320231 3930325 EU ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 SAL - MAJOR REPAIR - C-06 CHECK - NR 5985310, CORROSION ON BULK CARGO DOOR LOWER SILL, BS 2830/FR 60 - BS 2936/FR 62, -Y 630 TO -Y680. REPAIRED BULK CARGO DOOR LOWER SILL, BS 2830/FR 60 - BS 2936/FR 62, -Y630 TO -Y680 IAW A320 SRM 53-41-49 FIGURE 203. 2 L 7 2 4F RT A28NM 2007091400028 20070914 00028 EU 2007 9 14 AWXA200701086 1 20070816 A 5554 D5537123500600 FITTING AIRBUS 320 A320231 3930325 EU ZONE 300 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 SAL - MAJOR REPAIR - C-06 CHECK - NR 5985591, RUDDER HINGE NR 2 FITTING HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 1926 / RIB 4. REPLACED RUDDER HINGE NR 2 FITTING, VERTICAL STABILIZER STATION 1926/RIB 4 IAW A320 AMM 55-36-41. 2 L 7 2 4F RT A28NM 2007091400029 20070914 00029 EU 2007 9 14 AWXA200701087 1 20070907 A 5340 D53112198200 FITTING AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 655AW 1075 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5991311, CORROSION ON THE L1 DOOR CUT OUT LOWER SILL CENTER FITTING, BS 709/FR 16 - BS 808/FR 20. REPLACED THE L1 DOOR CUT OUT LOWER SILL CENTER FITTING, BS 709/FR 16 - BS 808/FR 20 IAW A320 SRM 51-72-1 1. 2 L 7 2 4F RT A28NM 2007091400030 20070914 00030 EU 2007 9 14 AWXA200701088 1 20070906 A 5347 D53371110008 SEAT TRACK AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 655AW 1075 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5991192, CORROSION ON CABIN SEAT TRACK, BS 1810/FR 41 - BS 2136/FR 47, +Y765. REPL ACED CABIN SEAT TRACK, BS 1810/FR 41 - BS 2136/FR 47, +Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007091400031 20070914 00031 EU 2007 9 14 AWXA200701089 1 20070906 A 5340 D534800480003 FITTING AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 655AW 1075 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5991283, CORROSION ON THE L2 DOOR CUT OUT LOWER SILL CENTER FITTING, BS 3158/FR 66 - BS 3257/FR 68. REPLACED THE L1 DOOR CUT OUT LOWER SILL CENTER FITTING, BS 3158/FR 66 - BS 3257/FR 68 IAW A320 SRM 51- 72-11. 2 L 7 2 4F RT A28NM 2007091400032 20070914 00032 2007 9 14 IXXA070045O 2 20070906 A 7200 ENGINE DOUG DC8 DC873F 302199F WP NR 1 OVERTEMP A IXXA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 11 605AL 98044 1483 46106 DURING CLIMB-OUT FROM KTOL, THE CREW PERFORMED MAX POWER TAKEOFF TO COMPLY WITH SEVEN DAY REQUIREMENT. NR ONE EGT WENT TO 906 FOR 2 SECONDS AFTER ROTATION, (N1 POWER SET FOR MAX 91.5 AFTER ROTATION N1 INCREASED TO 93.0 AND EGT FOLLOWED). NUMBER 4 EGT WENT TO 911 AFTER ROTATION. N1 POWER SET FOR MAX AT 91.5, AFTER CLIMB N1 INCREASED TO 93.5 AND EGT FOLLOWE D EGT AT 911 JUST MOMENTARILY. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED PMC DROP C HECK ADJUSTED MECHANICAL POWER TRIM, PERFORMED MAX POWER RUN ALL PARAMETERS ARE WITH IN LIMITS OPERATIONAL CHECK WAS GOO D. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2007091400033 20070914 00033 SO 2007 9 14 SIMA200725609 1 20070906 A 5320 SILL EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 656AE 145740 DURING A HMBV INSPECTION, THE CARGO DOOR CUT OUT LOWER SILL WAS FOUND TO BE CORRODED. REPLACED LOWER SILL WITH PART NUM BER 145-25480-603 IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007091400041 20070914 00041 EU 2007 9 14 F3LA200700211 1 20070830 A 5210 SEAL AIRBUS A319 A319112 3930323 EU PAX DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED LT DOOR SEAL CORRODED AT NUT PLATE HOLE AT FR66. FABRICATED REPAIR ANGLE, FILLE RS AND DOUBLER IAW SRM 53-41-14. INSTALLED SPLICE ANGLE, DOUBLERS AND FILLER IAW SRM 53-41-11. 2 L 7 2 4F RT A28NM 2007091400042 20070914 00042 EU 2007 9 14 DHL2007367507 1 20070807 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH 265 PASSENGER SEAT ATTACHMENT FITTING AT FR 54.2 BEAM NUMBER LH2-18 MEASURED .032. REMOVED SEAT TRACK ATTACHMENT FITTING AT FR 54.2 BEAM NR LH2-18 IAW FSI SB 94FS494-53-12R1. MEASURED SEAT TRACK ATTACHMENT FITTING .032 FOUND OUT OF LIMITS. I NSTALLED SEAT TRACK ATTACHMENT FITTING AT FR 54.2 BEAM LH2-18 IAW A300 SRM 51-30-00 AN SB 94FS494-53-12R1. 2 L 7 2 4F RT A35EU 2007091400043 20070914 00043 SO 2007 9 14 SIMA200725402 1 20070905 A 5315 14000492403 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AE 145762 UPPER FLOORBEAM AT FRAME 23 CORRODED DURING MBV FOUND UPPER FLOORBEAM AT FRAME 23 CORRODED. REMOVED FLOORBEAM AND INSTA LLED NEW FLOORBEAM AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007091400045 20070914 00045 SO 2007 9 14 SIMA200725403 1 20070905 A 5320 14590070004 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AE 145762 DURING MBV INSPECTION, FOUND FORWARD SERVICE DOOR SILL BETWEEN FRAMES 17-20 CORRODED. REPAIRED SILL. AIRCRAFT WAS RETU RNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007091400047 20070914 00047 EU 2007 9 14 07FDEA03514 1 20070911 A 5311 A53970781 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 SCRATCHED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 FOUND SCRUBMARKS AT FRAME 55 LT & RT, BETWEEN STR 14-15. REPAIR PERFORMED BY REWORK AND INSTALLING REINFORCEMENT PLATE IAW TD/K4/S1/20292/2005/A AND SRM 53-10-13 / FIG 202, APPROVED BY EA 6-5316-95880 AND RAS/DAHAM/4020292/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091400048 20070914 00048 EU 2007 9 14 07FDEA03515 1 20070911 A 5210 A52111338200 BEAM AIRBUS 310 A310 EU PAX DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION ON FWD PAX DOOR 31 LT AT BEAM NR 1 OUT OF LIMIT REPAIR PERFORMED IAW SRM 52-11-00 FIG 213, APPROVED BY EA 6-52 10-79568. 2 L 7 2 4F RT A35EU 2007091400049 20070914 00049 EU 2007 9 14 07FDEA03517 1 20070911 A 5320 A53613847200 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 DAMAGED FITTING AT FRAME 12A, Z-177, STRG 26 LT. REPAIR PERFORMED BY REPLACEMENT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091400052 20070914 00052 EU 2007 9 14 07FDEA03521 1 20070911 A 5730 A57340087 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 ELONGATED HOLES AT PYLON SUPPORT BRACKET AND BOTTOM SKIN OF LT WING. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLIN G BUSHES IAW EA 6-5720-95870 AND RAS/BAE/1002289/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091400053 20070914 00053 EU 2007 9 14 07FDEA03523 1 20070911 A 5322 A53981113 SHEAR TIE AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 CRACKED SHEAR PLATES BETWEEN FRAME 79-80, STRG 26. REPAIR PERFORMED BY REPLACEMENT OF PART SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091400054 20070914 00054 EU 2007 9 14 07FDEA03525 1 20070911 A 5311 A53981205202 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 FOUND OVERSIZED HOLES AT CROSSBEAM, FRAME CONNECTION, FRAME 77 BETWEEN STRG 27-28 LHS. REPLACMENT OF FRAME SEGMENT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091400056 20070914 00056 EU 2007 9 14 07FDEA03451 1 20070907 A 5313 A53980669207 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 CORROSION ON STRINGER 54 RT BETWEEN C76-77, OUT OF LIMIT AS PER SRM 53-10-00. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007091400058 20070914 00058 EU 2007 9 14 07FDEA03535 1 20070911 A 5320 A53610694205 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 DAMAGED FITTING AT FRAME 13, STR 26 RT. REPAIR PERFORMED BY REPLACEMENT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091400062 20070914 00062 EU 2007 9 14 07FDEA03453 1 20070907 A 5730 A57243768 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 FOUND CORROSION ON LT WING TOP SKIN T/E AREA AT WORX439.75. REPAIR PERFORMED BY BLEND OUT THE CORROSION AND INSTALLING OVERSIZED FASTENERS IAW EA 6-5720-95931 AND RAS/BAE/1002360/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091400067 20070914 00067 EU 2007 9 14 07FDEA03459 1 20070907 A 5313 A53811371202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 FOUND CORROSION ON STRINGER 50 RT BETWEEN FRAME 46-47. REPAIR PERFORMED BY REPLACEMENT OF STRINGER IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091400068 20070914 00068 EU 2007 9 14 07FDEA03460 1 20070907 A 5522 A55276796200 SKIN AIRBUS 310 A310324 3930206 EU RT ELEVATOR DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 DELAMINATION ON RT ELEVATOR LOWER SURFACE T/E NEAR TO RIB 1. REPAIR PERFORMED BY TRIM OUT THE AFFECTED SKIN, REPLACE TH E CORE WHERE IT'S NECESSARY AND INSTALL A METALLIC STRAP IAW EA 6-5521-99198 AND RAS/CASA/4676/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091400069 20070914 00069 EU 2007 9 14 07FDEA03461 1 20070907 A 5313 A53810869201 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 FOUND CORROSION ON STRINGER 44 RT BETWEEN FRAME 47-48, OUT OF LIMIT. REPAIR PERFORMED BY BLEND OUT THE CORRODED A REAS IAW EA 6-5315-99192 AND RAS/043644/008/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091400070 20070914 00070 EU 2007 9 14 07FDEA03462 1 20070907 A 5313 A53810868201 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 FOUND CORROSION ON STRINGER 43 RT BETWEEN FRAME 47-48, OUT OF LIMIT. REPAIR PERFORMED BY BLEND OUT THE CORRODED AREAS I AW EA 6-5315-99192 AND RAS/043644/008/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091400072 20070914 00072 EU 2007 9 14 F3LA200700210 1 20070830 A 5320 SHIM AIRBUS A319 A319112 3930323 EU FUSLEAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED FWD FLOOR PROFILER IN FWD CARGO COMPARTMENT HAD CORROSION AROUND FASTENER HOLE. REMOVED CORROSION ON SHIM FROM AROUND FASTENER HOLE IAW SRM 51-73-00. BLENDED AREA WAS APPROX .5" BY .5" WITH MAX DEPT H OF .012". REMOVED, FABRICATED AND INSTALLED NEW SHIM IAW SRM 51-42-11, 53-21-14, FIG 3, 51-21-11, 51-75-12, AND AIRBU S DRAWING C2 D53913797. 2 L 7 2 4F RT A28NM 2007091400074 20070914 00074 WP 2007 9 14 07FDEA03465 1 20070907 A 5330 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 DIRECTLY INLINE WITH AFT CARGO COMPARTMENT DOOR FORWARD FRAME ON LOWER BELLY SKIN ARE 2 SCRATCHES/CREASED ACROSS BELLY S TRINGERS APR 4 1/2 FEET LONG LT TO RT. TERMINATING ACTION ACCOMPLISHED FOR SRM 53-20-00 AT 84,197:34 H 23,464 C, REMOV ED CLASS 2 DOUBLER IAW SRM 51-31-01. INSTALLED NEW DOUBLER AND TRIPLER IAW SRM 53-20-00 FIG 6 SH 5 VOL 1. FAB DOUBLER AND TRIPLER FROM 2024-T3 .050C BATCH NR 1323872. FAB FINGER DOUBLER FROM 2024- T3 .040 BATCH NR 0001198113 IAW SRM 5 3-20-00 FIG 6 SH 5. TREATED, PRIMED AND PAINTED IAW SRM 51-21-01 AND 51-21-02 VOL 2. REPAIR IS CLASSIFIED AS PERMANEN T MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2007091400075 20070914 00075 WP 2007 9 14 07FDEA03466 1 20070907 A 5313 LONGERON DOUG DC10 DC1030F 3023504 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 AFT CARGO COMPARTMENT BILGE FOUND CORRODED ON LONG 51L BETWEEN STA 1967 TO 1947. REMOVED LONGERON CAP, FRAME, SHEAR TIE AND INTERCOSTAL IAW SRM 51-31-01. FAB REPAIR PARTS ON MAE TRAVELERS NR T7/697762 AND T7/697769. INSTALLED PARTS IAW S RM 53-30-00 FIG 5 SHEET 1. PAINTED AREA IAW SRM 51-21-02. THIS REPAIR IS CLASSIFIED AS A CAT B MAJOR REPAIR. FOLLOW U P ACTION IS REQUIRED. INITIAL INSPECTION IS AT 12,000 CYCLES AND REPETITIVE INSPECTIONS AT EVERY 8,000 THERE AFTER. CU RRENT CYCLES ARE 23464. 2 L 7 3 4F RT A22WE 2007091400077 20070914 00077 NM 2007 9 14 07FDEA03468 1 20070907 A 5315 6520832 FLOORBEAM BOEING 727 727233 138408A NM ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FLOORBEAM IN THE MAIN CARGO COMPARTMENT HAS CORROSION AT BS 1010, RBL 10.5 (UPPER T CAP) REMOVED CORROSION ORIGINAL MAT. THICKNESS .125, REMOVED .032, .093 REMAINING, OUT OF LIMITS. REPAIRED FLOORBEAM USING .063 17-7 PH STEEL, .125 7075 T6 . REF SRM 51-10-18 PGS 3-4, 53-10-2 PGS 44, 44E, 53-10 PG 19 AND SR27-53-034 REV F REPAIR NR 1. 2 L 7 3 4F RT A3WE 2007091400078 20070914 00078 EU 2007 9 14 07FDEA03539 1 20070911 A 5311 A53610318392 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 DAMAGED FRAME 12A RT (BENT PARTITIONS, IMPACTS AT RIVET HOLES, OVERSIZED HOLES), STRG 24-27. REPAIR PERFORMED BY REPLAC EMENT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091400079 20070914 00079 EU 2007 9 14 07FDEA03540 1 20070911 A 5320 A26270471 BRACKET AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 FOUND TWO CRACKED BRACKETS BETWEEN CROSSBEAM FRAME 29-30 AND 30-31, Y-2462 RHS. REPAIR PERFORMED BY REPLACEMENT OF PART S IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091400080 20070914 00080 EU 2007 9 14 07FDEA03543 1 20070911 A 5320 A53410549000 FLANGE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 FOUND SEVERAL MISDRILLED HOLES AT FLANGE FOR AOA SENSOR BETWEEN FRAME 18-19 LHS (PTOF DRW. R537B1311). REPAIR PERFORMED BY REPLACEMENT OF FLANGE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091400081 20070914 00081 NM 2007 9 14 QXEA200701397 1 20070903 A 3230 468483 LINK BOMBDR DHC8 DHC8402 1390042 NM MLG DAMAGED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 425QX 4039 SJC FLIGHT NR 2406: CLIMBING THROUGH 6000 FT, BOTH LEFT AND RIGHT MAIN GEAR DOORS CYCLED. RIGHT GEAR DOOR LIGHT REMAINE D ILLUMINATED APPROX 5 SECONDS IAS <200 KTS. DOOR LIGHT EXTINGUISHED AND GEAR AND DOORS UP AND LOCKED IN DESCENT. LEFT AND RIGHT DOORS CYCLED AGAIN. MAINTENANCE REMOVED AND INSTALLED LT MLG DOOR MECHANISM LOCK LINK IAW -8 400 AMM 32-31-3 1. ALSO RIGGED PROX SENSOR TO LT MLG RETRACT MECHANISM IAW -8 400 TASK 32-61-06-830-801. ALL CHECKS GOOD. AIRCRAFT RE TURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091400084 20070914 00084 EU 2007 9 14 F3LA200700220 1 20070906 A 5321 NAS130422 BOLT AIRBUS A319 A319112 3930323 EU FLOOR MOUNT CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED THE FLOOR MOUNT BOLT ON THE AFT INBD CORNER OF THE AFT WALL OF LAV A WAS CORRODE D AND COULD NOT BE REMOVED WITH STANDARD WRENCHES. THE HEAD WAS CUT OFF FROM BELOW TO REMOVE THE LAV WALL. REMOVED AND REPLACED BOLT IAW AMM 25-41-00. 2 L 7 2 4F RT A28NM 2007091400086 20070914 00086 NM 2007 9 14 QXEA200701398 1 20070810 A 3350 XD4N RELAY BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY LIGHTS MALFUNCTIONED A QXEA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 421QX 4149 BOI FLIGHT NR 2360: DURING TAXI OUT FA REPORTS THE EMERGENCY LIGHTS REMAIN ON WHEN THE COCKPIT EM SWITCH IS IN THE ARM P OSITION. FA EMERGENCY SWITCH IS WHERE IT IS SUPPOSED TO BE, THE COCKPIT EM SWITCH IS PUT IN THE OFF POSITION, THE LIGH TS GO OFF. MAINTENANCE REMOVED AND REPLACED 3351-K2 RELAY IWA FIM 33-50-00. ALL OPS AND INDICATIONS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091400087 20070914 00087 NM 2007 9 14 AWXA200701067 1 20070824 A 5347 146N51304 SEAT TRACK BOEING 757 7572S7 1384962 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 MCN - MAJOR REPAIR - C-11 CHECK - NR 5988776, CRACKED CABIN SEAT TRACK, BS 1600, RBL 45.50, WL 208. REPLACED CABIN SEAT TRACK, BS 1600, RBL 45.50, WL 208 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007091400088 20070914 00088 EU 2007 9 14 AWXA200701068 1 20070823 A 5320 D53480043202 SILL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-7 CHECK - NR 5980128, CORROSION ON THE L2 DOOR CUT OUT LOWER SILL, BS 3207/FR 67 - BS 3257/FR 68. REPAIRED THE L2 DOOR CUT OUT LOWER SILL, BS 3207/FR 67 - BS 3257/FR 68 IAW USAIRWAYS EA 120203. 2 L 7 2 4F RT A28NM 2007091400089 20070914 00089 EU 2007 9 14 AWXA200701069 1 20070823 A 5320 D53480043205 SILL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-7 CHECK - NR 5980133, CORROSION ON THE R2 DOOR CUT OUT LOWER SILL, BS 3158/FR 66, -Y1465. REPAIR ED THE R2 DOOR CUT OUT LOWER SILL, BS 3158/FR 66, -Y1465 IAW A320 SRM 53-41-14. 2 L 7 2 4F RT A28NM 2007091400094 20070914 00094 EU 2007 9 14 AWXA200701075 1 20070909 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHTS FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 628AW 69 21 67 PHX - EEL - LOG 4160010 - FWD EMERGENCY LIGHT TEST FAILED. MX REPLACED THE 10W POWER SUPPLY AND BATTERY PACK. OPERATIO NAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007091400097 20070914 00097 EA 2007 9 14 SIMA200725307 1 20070907 A 2780 5912999 BPSU CNDAIR CL600 CL6002C10 1390015 EA SLATS MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 SW 21 522AE 10147 OVERSPEED WARNING CAME ON AT 230 KTS WITH GEAR AND SLATS RETRACTED AND INDICATIONS SHOWING ZERO. NO BARBER POLE RED WAR NINGS. CYCLED FLAPS ZERO TO ONE DEGREE BACK TO ZERO WITHOUT SUCCESS. LANDING WAS UNDER 67000 LBS AND WAS APPROX 100 FP M AT TOUCHDOWN. SMOOTH LANDING. REMOVED AND REPLACED RIGHT WING BRAKE POSITION SENSOR UNIT IAW AMM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007091400098 20070914 00098 EU 2007 9 14 SIMA200725308 1 20070908 A 3397 CONNECTOR SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS DAMAGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 240DS 340B240 EMERGENCY EXIT SIGN INOP AT ROW 8A. REMOVED AND REPLACED EPS 22, 23, AND 20LN IAW MM. PERFORMED OPERATIONAL CHECK AND FOUND WORKING PROPERLY. FOUND PINS PUSHED BACK IN CONNECTOR FOR THE SIGN. REINSTALLED PINS IN CONNECTOR. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007091400099 20070914 00099 EU 2007 9 14 SIMA200725309 1 20070908 A 2842 INDICATOR SAAB SF340 340B 7860101 EU FUEL QTY READS HIGH A SIMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 902AE 340B269 DURING CRUISE CREW OBSERVED A FUEL IMBALANCE OF 200 LBS WITH THE LT WING BEING LOW. WHEN CROSS FEED WAS SELECTED THE IM BALANCED INCREASED. CREW ELECTED TO DIVERT INTO TYR. AIRCRAFT LANDED AND TAXIED TO THE GATE WITH NO FURTHER INCIDENT. VERIFIED RT WING FUEL QUANTITY WAS READING 200 LBS HIGHER THAN THE DIP STICKS ISSUED MELS. REMOVED AND REPLACED NR 6 P ROBE ON RIGHT HAND TANK AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007091400100 20070914 00100 SO 2007 9 14 SIMA200725303 1 20070907 A 2720 15HW48PH SENSOR EMB 135 EMB135LR 3260305 SO RUDDER MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 705AE 145184 RUDDER SYSTEM 1/2 INOP MESSAGE A/C RETURNED TO DFW REMOVED AND REPLACED RUDDER SYSTEM 2 SENSOR IAM EMB MAINTENANCE MANUA L. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007091400103 20070914 00103 EU 2007 9 14 F3LA200700225 1 20070831 A 5315 FLOORBEAM AIRBUS A319 A319112 3930323 EU CORRODED CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON UNDERNEATH SIDE OF NUTPLATE HOLE AT FR66. REPLACED COUPLING IAW 51 -42-11. 2 L 7 2 4F RT A28NM 2007091400104 20070914 00104 NE 2007 9 14 DL76G071148 2 20070827 A 7200 CF680C2B6F ENGINE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 1 MALFUNCTIONED A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 177DZ 21853 29698 706131 CREW REPORTS VIBRATION IN CONTROL YOKE AFTER TAKEOFF PASSING THRU 250KTS. ALSO EXPERIENCED VIBES ON NR 1 ENG THAT VARIE D FROM 1.7-3.5 WITH A PEAK OF 5.0.ENGINE THROTTLES PULLED AND ENG VIBE DROPPED TO .8 BUT YOKE VIBRATION REMAINED. C/W B OROSCOPE OF NR 1 ENG BORO PLUGS B1-1/B1-12/B1-5, NO DAMAGE FOUND. CKED NR 1 COMPONENTS FOR SECURITY SHAKE CKED NO FAULT S FOUND. INSP CHIP DETECTORS. NO DEBRIS FOUND, DL ID 448555. REMOVED ENG OIL FILTER IN. INSPECTED SAME NO METAL FOUN D INSTALLED NEW FILTER LEAK CK OK. INSPECTED AND LUBED ROTOR BLADES. FOUND ALL OK PER AMM. 2 L 7 2 4F 4 F RT A1NM E13NE 2007091400107 20070914 00107 NM 2007 9 14 DL76S071154 1 20070829 A 5753 LINK BOEING 767 767332 1382001 NM TE FLAPS CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 132DN 24981 WORKING EA 01-073591-12 FOUND LEFT AND RIGHT INDBD AFT DRIVE LINK FLAP ATTACH BOLT HOLES CORRODED REPAIRED PER ERA089397 -14MA. 2 L 7 2 4F RT A1NM 2007091400108 20070914 00108 NM 2007 9 14 DL76S071155 1 20070829 A 5753 FITTING BOEING 767 767332 1382001 NM TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 132DN 24981 CORROSION IN BORE OF HOLES FOR NR 4 AND 5 FLAP SUPPORT ATTACHMENTS. BUSHINGS REPLACED. 2 L 7 2 4F RT A1NM 2007091400110 20070914 00110 NM 2007 9 14 DL76S071157 1 20070828 A 5753 113T1212 SUPPORT BEAM BOEING 767 767332 1382001 NM NR 4 FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 135DL 25145 FROM NR 185 PSV 15, NUMBER 4 FLAP SUPPORT BEAM HAS PITTING IN FORWARD MOUNT HOLES. REPAIRED PER ERA 089397-14MA REV O. 2 L 7 2 4F RT A1NM 2007091300003 20070913 00003 EU 2007 9 13 SA07056 1 20070831 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU CABIN MALFUNCTIONED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 722US 21459 18569 1097 PHL - THE EMERGENCY LIGHTS TEST INDICATED EMERGENCY BATTERY FAULT. MAINTENANCE REPLACED THE MID-CABIN, LEFT EMERGENCY P OWER SUPPLY UNIT. 2 L 7 2 4F RT A28NM 2007091300016 20070913 00016 NM 2007 9 13 MWEA070199 1 20070902 A 7830 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 904ME 55168 RIGHT THRUST REVERSER UPPER BUCKET STATION 35 ZEE FRAME IS CRACKED. 2 L 7 2 4F TR A6WE 2007091300048 20070913 00048 NM 2007 9 13 CALA0700482 1 20070831 A 5322 6546549 SHEAR TIE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT STA 767 BETWEEN STRINGER 26L AND 27L, LBL 5 TO LBL 15. THE SHEAR TIE WAS REPAIRED IAW SRM 53-00-07, FIGURE 201. 2 L 7 2 4F RT A16WE 2007091300056 20070913 00056 NM 2007 9 13 CALA0700490 1 20070820 A 2131 7638101 CONTROLLER BOEING 737 7373T0 1384582 NM CABIN PRESSURE INOPERATIVE A CALA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 69348 44963 23586 THE CREW RECEIVED A CABIN ALTITUDE WARNING CLIMBING THROUGH FL 270. THE QRH WAS FOLLOWED AND A RAPID DESCENT TO 13,000 FEET WAS ACCOMPLISHED. CABIN PRESSURE WAS RECOVERED VIA MANUAL DC. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WI THOUT FURTHER PROBLEM. A CABIN PRESSURE CONTROLLER WAS REMOVED AND REPLACED IAW MM 21-31-21, PAGE 401. OPERATIONAL CHE CKS WERE GOOD IAW MM 21-31-00, PAGE 201. 2 L 7 2 4F RT A16WE 2007091300073 20070913 00073 WP 2007 9 13 UPS07850594 1 20070821 A 5522 SKIN DOUG DC8 DC873F 302199F WP RT ELEVATOR DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 RIGHT ELEV UPPER SKIN DENTED AT STA XE 200. CUT OUT DAMAGED AREA ON RIGHT ELEV SKIN AT STA XE 200 IA W SRM 55-02-01, FABRICATED AND INSTALLED REPAIR DOUBLER AT STA XE 200 IAW SRM 55-02-01-0. CALCULATED WEIGHT AND BALANCE IAW SRM 51-04-08-0 FIG 059R. 2 L 7 4 4F RT 4A25 2007091300079 20070913 00079 WP 2007 9 13 UPS07850608 1 20070904 A 2560 ESCAPE ROPE DOUG DC8 DC871F 302199D WP COCKPIT OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:N/A CAPTAIN'S ESCAPE ROPE HAS FALLEN FROM ITS STORAGE AREA. REPACKED CAPTAIN'S ESCAPE ROPE PER AMM 25-6 0-2-2-2. 2 L 7 4 4F RT 4A25 2007091300080 20070913 00080 NM 2007 9 13 ASAA0752013 1 20070830 A 5320 141A85121B INTERCOSTAL BOEING 737 737890 1384527 NM FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 546AS 30022 E&E DOOR SURROUND LT INTERCOSTAL WEB IS CHAFED. REPLACED WEB WITH FABRICATED REPAIR PART. 2 L 7 2 4F RT A16WE 2007091300082 20070913 00082 NM 2007 9 13 ASAA0752015 1 20070831 A 5720 115A29532 SUPPORT BRACKET BOEING 737 737890 1384527 NM RT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 546AS 30022 RIGHT WING UPPER FIXED TRAILING EDGE PANEL RIG AFT ANGLE SUPPORT BRACKET CRACKED. REPLACED TRAILING EDGE PANEL WITH NEW PART. 2 L 7 2 4F RT A16WE 2007091300087 20070913 00087 EU 2007 9 13 SA07057 1 20070906 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 754UW 210 1328 BOS - DURING EMERGENCY LIGHT CHECK FOUND EMERGENCY EXIT SEAT ROW LIGHTS INOP. MAINTENANCE REPLACED MID CABIN RIGHT SIDE EMERGENCY POWER SUPPLY UNIT (FIN 12WL). 2 L 7 2 4F RT A28NM 2007091300100 20070913 00100 EU 2007 9 13 TRAX200701284 1 20070831 A 5315 FLOORBEAM AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 ON FLOORBEAM AT FR 38 CORROSION FOUND. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 53-00-00 FIG 450. 2 H 7 2 4T RT 2007091300103 20070913 00103 EU 2007 9 13 TRAX200701287 1 20070902 A 3397 WIRE AEROSP ATR72 ATR72 EU CABIN EXPOSED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 WIRING UNSHIELDED IN FLOOR EMERGENCY LIGHTING, SOME FLOOR LIGHTING INOP. 2 H 7 2 4T RT 2007091300105 20070913 00105 NM 2007 9 13 USAA920070808 1 20070822 A 5320 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 942UW 27807 BFM - MAJOR REPAIR - C-4 CHECK - NR 6003914, CORROSION ON FLOOR SUPPORT WEB, BS 377.7 - BS 395, RBL 12. REPLACED FLOOR SUPPORT WEB, BS 377.7 - BS 395, RBL 12 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007091300125 20070913 00125 NM 2007 9 13 SWAA074425 1 20070905 A 5753 65C34812 FLAP TRACK BOEING 737 7373H4 1384600 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED BRDG CHECK, FOUND LEFT WING NR 2 FLAP TRACK CORRODED AT REAR SPAR. REPAIRED FLAP TRACK PER SRM. 2 L 7 2 4F RT A16WE 2007091300126 20070913 00126 2007 9 13 SWAA074392 4 20070905 A 2565 69451434 WINDOW BOEING 737 7377H4 1384404 NM R2 DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 413WN 29819 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE VIEWING WINDOW MISSING. INSTALLED WINDOW PER MM . 2 L 7 2 4F RT A16WE 2007091300128 20070913 00128 NM 2007 9 13 SWAA074369 1 20070904 A 3397 8100022602 CONNECTOR BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 243WN 34863 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 18 ABC. FOUND LOOSE CONNECTOR, SECURED CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2007091300133 20070913 00133 NM 2007 9 13 CALA0700492 1 20070906 A 5311 65465592 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 INSPECTION FOUND CORROSION AT FRAME ATTACH POINT, STA 927 JUST I/B OF S27L, LBL 27 TO RBL 27. A REPAIR WAS INSTALLED IA W ECRA 5310-04655. 2 L 7 2 4F RT A16WE 2007091300139 20070913 00139 NM 2007 9 13 CALA0700498 1 20070906 A 5311 6546530 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17328 23458 INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 480 BETWEEN STRINGERS 8 AND 9L. REPAIRED IAW ECRA 5310-04651. 2 L 7 2 4F RT A16WE 2007091300167 20070913 00167 NM 2007 9 13 SWAA074436 1 20070906 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091300169 20070913 00169 NM 2007 9 13 SWAA074437 1 20070906 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091300170 20070913 00170 NM 2007 9 13 SWAA074449 1 20070906 A 5312 6546568 BULKHEAD BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD CORRODED AT BS 1016, BETWEEN STR 26L AND STR 26R. REPAIRED BULK HEAD PER ACO. 2 L 7 2 4F RT A16WE 2007091300193 20070913 00193 SO 2007 9 13 LR7A07084 1 20070905 A 5230 7075T6050 BRACKET LKHEED 382 382G 526414U SO FS 906 WL 230 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2537 4698 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5212, FOUND CARGO DOOR INTERIOR SUPPORT BRACKET ATTACHED TO LOWER SKIN CRACKED AT FS906 WL230 BL48L. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-20. 2 H 7 4 4T A1SO 2007091300194 20070913 00194 SO 2007 9 13 LR7A07085 1 20070905 A 5230 7075T6511090 SUPPORT LKHEED 382 382G 526414U SO CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2537 4698 DURING SCHEDULED C-8 CHECKPER JOB CARD HC5211, FOUND RAMP DOOR INTERIOR BHD SUPPORT FITTING CRACKED (2 PLACES) AT RS8, R BL10. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-22. 2 H 7 4 4T A1SO 2007091300195 20070913 00195 SO 2007 9 13 LR7A07086 1 20070905 A 5312 7075T6040 BULKHEAD LKHEED 382 382G 526414U SO FS 880, WL 208 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2537 4698 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5313, FOUND AFT FUSELAGE INTERIOR BHD WEB CRACKED AT FS 880 WL208 RT SIDE RBL6 5. WEB REPAIR CARRIED OUT IAW SMP583 CHAPTER 51-140-17. 2 H 7 4 4T A1SO 2007091300196 20070913 00196 SO 2007 9 13 LR7A07087 1 20070905 A 5320 3620115R DOUBLER LKHEED 382 382G 526414U SO FS 132, WL 270 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2537 4698 DURING SCHEDULED C-8 CHECK PER JOB CARD HC2411, FOUND FLIGHT DECK RT RIB FORMER REINFORCEMENT DOUBLER CRACKED AT FS 132 WL227. REINFORCEMENT DOUBLER FABRICATED AND REPLACED IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007091300197 20070913 00197 SO 2007 9 13 LR7A07088 1 20070905 A 5230 7075T6511 SUPPORT ANGLE LKHEED 382 382G 526414U SO FS 880 BL 60R CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2537 4698 DURING SCHEDULED C-8 CHECK, FOUND CARGO DOOR BHD LOWER ANGLE BROKEN DURING GUSSET PLATE REMOVED FOR REPLACEMENT AT FS880 BL60R. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-23. 2 H 7 4 4T A1SO 2007091300198 20070913 00198 SO 2007 9 13 LR7A07089 1 20070905 A 5230 7075T6050 STIFFENER LKHEED 382 382G 526414U SO FS 1012 BL0. CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2537 4698 DURING SCHEDULED C-8 CHECK PER JOB CARD HC3215, FOUND CARGO DOOR BHD STIFFENER AND REINFORCE CLIP CRACKED AT FS 1012 BL0 . STIFFENER AND CLIP AT BL0 FABRICATED AND REPLACED IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007091300199 20070913 00199 SO 2007 9 13 200725303 1 20070907 A 2720 15HW48PH SENSOR EMB 135 EMB135LR 3260305 SO RUDDER MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 705AE 145184 RUDDER SYSTEM 1/2 INOP MESSAGE A/C RETURNED TO DFW REMOVED AND REPLACED RUDDER SYSTEM 2 SENSOR IAW EMB MAINTENANCE MANUA L. 2 L 7 2 4F RT T00011AT 2007091300200 20070913 00200 SO 2007 9 13 200725302 1 20070907 A 5610 SEAL EMB 145 EMB145LR 3260212 SO COCKPIT WINDOW FAILED A SIMA C ABORTED TAKEOFF D INFLIGHT SEPARATION TO TAKEOFF 1 SW 21 625AE 145115 AFTER TAKEOFF CAPTS COCKPIT WINDOW SEAL BLEW OUT IN FLIGHT. 2 L 7 2 4T RT T00011AT 2007091300217 20070913 00217 SO 2007 9 13 SIMA200725002 1 20070905 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 691AE 14500860 STRONG BURNING RUBBER ODOR COMBINED WITH MUSKY DIRTY SOCK ODOR. BURNING ODOR WENT AWAY AFTER TWO MINUTES, BUT MUSKY ODO R PERSISTED. NO SMOKE NOTICED. LANDED AT ORD. NO EMER DECLARED. C/A-REMOVED AND REPLACED ENGINE 2 OPS & LEAK CHECKS G OOD AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007091300218 20070913 00218 EU 2007 9 13 SIMA200725004 1 20070904 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU ZONE 100 FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 329AE 23568 16261 340B329 AVIONIC SMOKE LIGHT INFLIGHT, WENT OUT AFTER 10 MINUTES FOLLOWING LEFT AND RIGHT AVIONIC SWITCHES SELECTED TO OFF. EMER GENCY DECLARED, RETURNED TO LAX. REMOVED AND REPLACED AVIONIC SMOKE DETECTOR IAW SAAB AMM 26-13-05. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007091300219 20070913 00219 SO 2007 9 13 SIMA200725001 1 20070904 A 3260 M8353616022M RELAY EMB 135 EMB135KL 3260302 SO ZONE 200 FAILED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 807AE 14454 145506 LG AIR/GND FAIL MESSAGE ON TAKEOFF, RETURNED TO SJC. SERVICED LEFT STRUT IAW EMB AMM 32-10-02. REMOVED AND REPLACED RE LAY K0453 AND K0353 IAW WMM 32-23-10. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007091300220 20070913 00220 EU 2007 9 13 SIMA200725006 1 20070905 A 3220 3830010102 SHIMMY DAMPENER SAAB SF340 340B 7860101 EU ZONE 700 FAILED A SIMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 21 218AE 23004 340B218 NOSE SHIMMY REPORTED AT 50 KNOTS, ABORTED TAKEOFF. REMOVED AND REPLACED NOSE WHEEL SHIMMY DAMPER IAW SAAB AMM. OPERATI ONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 2007091300221 20070913 00221 SO 2007 9 13 SIMA200725003 1 20070905 A 2460 14521325405 CONTROL PANEL EMB 135 EMB135KL 3260302 SO ZONE 200 FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 842AE 12077 145673 RECEIVED ELECTRICAL EMERGENCY ABNORMAL MESSAGE, RETURNED TO ORD. REMOVED AND REPLACED ELECTRICAL CONTROL PANEL IAW EMB 24-00-01. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007091300222 20070913 00222 NM 2007 9 13 AWXA200701074 1 20070909 A 5330 6545774 SKIN BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 PHX - MAJOR REPAIR - NR 4155161, FUSELAGE SKIN CRACKED BS 727, S22L. REPAIRED FUSELAGE SKIN, BS 727, S22L IAW B737-300 SRM 53-00-01-2R1 FIGURE 201. 2 L 7 2 4F RT A16WE 2007091300233 20070913 00233 WP 2007 9 13 MWEA070207 1 20070907 A 5730 59305036 SKIN DOUG DC9 DC981 3022081 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 CORROSION AT WING CENTER SECTION REAR SPAR LOWER SKIN AT APPROXIMATELY XCW = 50.000 RIGHT SIDE. REMOVED CORROSION, FABR ICATED AND INSTALLED FASTENERS. 2 L 7 2 4F A6WE 2007091300244 20070913 00244 NM 2007 9 13 SWAA074467 1 20070907 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 793SA 27888 DURING SCHEDULED HC1 CHECK, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007091300251 20070913 00251 NM 2007 9 13 SWAA074487 1 20070909 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 286WN 32471 EEPLS COVER LOOSE AT ROW 3 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007091300255 20070913 00255 2007 9 13 SWAA074490 4 20070909 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 287WN 32537 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007091300263 20070913 00263 NM 2007 9 13 AWXA200701090 1 20070814 A 5313 654988630 STRINGER BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5987892, CRACKED STRINGER, BS 500D, S16L. REPAIRED STRINGER, BS 500D, S16L IAW AWA ER 03-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2007091300264 20070913 00264 NM 2007 9 13 AWXA200701091 1 20070814 A 5311 652072270 FRAME BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5987853, FORWARD CARGO COMPARTMENT DOOR CUT OUT FORWARD FRAME CRACKED, BS 440, S24R . REPLACED FORWARD CARGO COMPARTMENT DOOR CUT OUT FORWARD FRAME, BS 440, S24R IAW USAIRWAYS EA 120223. 2 L 7 2 4F RT A16WE 2007091300265 20070913 00265 NM 2007 9 13 AWXA200701092 1 20070814 A 5311 652072354 FRAME BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5987852, FORWARD CARGO COMPARTMENT DOOR CUT OUT AFT FRAME CRACKED, BS 492.3, S24R. REPLACED FORWARD CARGO COMPARTMENT DOOR CUT OUT AFT FRAME, BS 492.3, S24R IAW USAIRWAYS EA 120222. 2 L 7 2 4F RT A16WE 2007091300266 20070913 00266 NM 2007 9 13 AWXA200701093 1 20070813 A 5210 5079454 SKIN BOEING 737 7373G7 1384595 NM ZONE 800 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5983692, L1 DOOR INNER SKIN CRACKED, BEAM 12 - BEAM 13. REPAIRED L1 DOOR INNER SKI N, BEAM 12 - BEAM 13 IAW USAIRWAYS EA 120231. 2 L 7 2 4F RT A16WE 2007091300267 20070913 00267 NM 2007 9 13 AWXA200701094 1 20070813 A 5210 507945 FRAME BOEING 737 7373G7 1384595 NM ZONE 800 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5983694, L1 DOOR AFT FRAME CRACKED, BEAM 12 - BEAM 13. REPAIRED L1 DOOR AFT FRAME, BEAM 12 - BEAM 13 IAW USAIRWAYS EA 120231. 2 L 7 2 4F RT A16WE 2007091400011 20070914 00011 SO 2007 9 14 LR7A07072 1 20070905 A 5311 3390108L FRAME LKHEED 382 382G 526414U SO FS 132, LBL 50 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2537 4698 DURING SCHEDULED C-8 CHECK, PER JOB CARD HC5311, FOUND COCKPIT LT FRAME CRACKED AT FS132 WL206 TO 216 LBL50. RIB (FRAME ) FS132 LT FABRICATED USING P/N:2024T3 .050", B/N:CK260281DC AND REPLACED IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007091400023 20070914 00023 EU 2007 9 14 F3LA200700217 1 20070905 A 5321 D5361060500100 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL THRESHOLD PANEL 222FF CORRODED TO EDGE. REMOVED AND REPLACED FLOOR THRESHOLD PANEL 222FF IAW AMM 53-12-12 AND WORK CARD CP753-12. 2 L 7 2 4F RT A28NM 2007091400036 20070914 00036 EU 2007 9 14 SIMA200725606 1 20070910 A 5347 7253742407 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 211NE 22399 340B211 DURING A HMBV INSPECTION, CORROSION WAS FOUND ON BL 36 LT. REPLACED THE SEAT TRACK USING PART NUMBER 7253742-407 IAW SA AB SRM 53-70-60 PARA 3. AIRCRAFT RETURED TO SERVICE. 2 L 7 2 4T RT A52EU 2007091400037 20070914 00037 NM 2007 9 14 DHL2007742013 1 20070904 A 5330 SKIN BOEING 727 727225 1384077 NM BS 303 S12-14L CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 L1 DOOR FORWARD LOWER HINGE CUTOUT IS CRACKED AT FORWARD EDGE BS 303 BETWEEN STR 12/14. CONTINUED ON N/R 138192. REMOV ED FASTENERS AT L1 DOOR LOWER HINGE CUTOUT IAW B727 SRM 51-30-2. FABRICATED REPAIR DOUBLER FROM 301 1/2 HARD .063 PO NR 9004843 APPROXIMATE DIMENSIONS 17 1/2 BY 6 1/4 IAW SB727-53A0198 FIG 4 REV 3. HFEC INSPECTED EXISTING HOLES, NO CRACKS NOTED IAW B727 NDT MANUAL PT6 51-00-00. REMOVED CRACKED AREA APPROXIMATE LENGTH 1.80" PER S/B727-53A0198 FIG 3 REV 3. C/W HFEC INSP IAW B727 NDTM PT6 51-00-00 FIG 23. NO CRACKS NOTED. FABRICATED FILLER FROM 2024 T3 .080" PO NR 7177117 DIMENSION APPROXIMTELY 2 1/2" BY 2 1/4" IAW SB727-53A0198 FIG 4 REV 3. TREATED AND PRIMED PARTS AND AREA IAW SB727-53A0 2 L 7 3 4F A3WE 2007091400039 20070914 00039 EU 2007 9 14 DHL2007367509 1 20070803 A 5753 SKIN AIRBUS 300 A300B4203 3930306 EU LT WING TE FLAP GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH 265 LT WING INNER FLAP O/B UPPER SURFACE SKIN HAS GOUGE. CUT OUT DAMAGED AREA 3/4" BY 2" IAW A300 SRM 57-50-00. REMOVED DO UBLER REPAIR AT LT WING INNER FLAP O/B UPPER SURFACE IAW A300 SRM 57-50-00. FABBED NEW DOUBLER REPAIR FROM 2024T3 .063" PO NR 043258 IAW A300 TD205/2007. PERFORMED HFEC INSP OF CUT OUT EDGES IAW A300 NDT 51-30-0 PART 5. NO CRACKS FOUND. OK TO INSTALL NEW REPAIR. INSTALLED NEW REPAIR IAW A300 SRM 57-50-00. 2 L 7 2 4F RT A35EU 2007091400040 20070914 00040 NE 2007 9 14 EIA2007154 2 20070829 A 7200 JT9D7A ENGINE BOEING 747 747SR46 1384816 NM PWA JT9 JT9D7A 52054 NE ZONE 400 OIL CONSUMPTION A EIAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 NM 09 477EV 71177 71177 20784 685897 PASSING THROUGH FL 200, NR 4 OIL QTY WENT TO "0", OIL TEMP REDLINED, OIL PRESSURE 5 PSI. ENGINE SHUT-DOWN AND RETURNED TO SUU STATION. AIRCRAFT FERRIED TO MZJ AND ENGINE REPLACED. 2 L 7 4 4F 4 F RT A20WE E20EA 2007091400055 20070914 00055 EU 2007 9 14 07FDEA03527 1 20070911 A 5320 A53981959200 SUPPORT AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 CRACKED SUPPORT AT FRAME 79-80, STRG 28 LHS. REPLACEMENT OF SUPPORT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091400063 20070914 00063 EU 2007 9 14 07FDEA03454 1 20070907 A 5320 A53986751206 PLATE AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 808FD 439 FOUND MISDRILLED HOLES AT WEB PLATE, FRAME 86-87, STRG 33 LHS. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10 . 2 L 7 2 4F RT A35EU 2007091400066 20070914 00066 NM 2007 9 14 07FDEA03458 1 20070907 A 5310 A53610655208 DOOR FRAME BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 467FE 21449 CORROSION FOUND BELOW LOWER DOOR STOP FITTING ON LT FWD DOOR, FRAME 14 LT, T1. REPAIR WAS PERFORMED BY SMOOTH BLEND OUT OF CORROSION IAW EA 6-5312-95915 AND RAS/043491/005/2006 ISSUE A. 2 L 7 3 4F A3WE 2007091400071 20070914 00071 EU 2007 9 14 07FDEA03463 1 20070907 A 5730 A57110204 SKIN PANEL AIRBUS 310 A310324 3930206 EU CENTER WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 HEAVY CORROSION FOUND ON CENTER WING BOX TOP SKIN AT TR5 AND TR6 RT/LT, FRAME 43-46.2. REPAIR PERFORMED IAW SRM 57-10-1 2/FIG 201 AND RAS/042817/015/2006 ISSUE A, EXCEPT FOR DAMAGES AT FRAME 44, BEAM 5 AND 6 LT AND RT, WHICH WAS REPAIRED BY DOUBLER IAW RAS/042972/012/2006 ISSUE A, APPROVED BY EA 6-5710-95921A. 2 L 7 2 4F RT A35EU 2007091400073 20070914 00073 WP 2007 9 14 07FDEA03464 1 20070907 A 5313 ADA80981 LONGERON DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 399FE 48262 FORWARD PIT BILGE STRINGER 52 HAS EXFOLIATED CORROSION IN UPPER CENTER CHANNEL AT BS 824. REMOVED CORRODED SECTION OF L ONGERON IAW MD/DC10-10, SRM 53-10-00 FIG 1 VOL 1. INSTALLED NEW SECTION OF LONGERON AND SPLICE REPAIR IAW MD/DC10-10 SR M 53-10-00 FIG, 1 VOL 1, MD/DC10-10 SRM 53-10-00 FIG 2 VOL 1, MD/DC10-10 SRM 51-33-01 PG 1 VOL 11 CAT B REPAIR IAW MD/D C10-10 SRM 53-10-00 FIG 1 AND FIG 2 VOL, 1. 2 L 7 3 4F RT A22WE 2007091400096 20070914 00096 EU 2007 9 14 SIAM200725306 1 20070907 A 3297 CONNECTOR SAAB SF340 340B 7860101 EU LT MLG INDICATOR DISCONNECTED A SIMA O OTHER P NO WARNING INDICATION LD LANDING 1 SW 21 250AE 340B250 LANDING GEAR LEVER SELECTED DOWN, LT MAIN GEAR INDICATOR LIGHT DID NOT ILLUMINATE. AIRCRAFT DECLARED EMERGENCY PERFORME D EMERGENCY LANDING PROCEED AND LANDED WITH OUT INCIDENTS FOUND CONNECTOR 5GA/P1 DISCONNECTED RECONNECT. OPS CHECK GOOD AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007091400111 20070914 00111 NE 2007 9 14 DL76G071158 2 20070830 A 7200 CF680C2B6 ENGINE BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6 30025 NE NR 1 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 154DL 57793 7181 25241 695339 NR 1 ENG FAILED BORO ENGINE CHANGE. 2 L 7 2 4F 4 F RT A1NM E13NE 2007091400112 20070914 00112 2007 9 14 DL76G071159 4 20070821 A 2565 BATTERY PACK BOEING 767 767332 1382001 NM ESCAPE SLIDE FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 176DZ 29697 RT EMERGENCY ESCAPE SLIDE SQUIB TEST FAILED. REPLACED BATTERY PACK 2013-1A IN POWER SUPPLY M962. CHECKS OK. 2 L 7 2 4F RT A1NM 2007091400113 20070914 00113 NM 2007 9 14 DL76L071160 1 20070901 A 3350 0205029001 LIGHT BOEING 767 767332 1382001 NM CABIN DESTROYED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 195DN 28452 EPATH LIGHTS INOP SEATS 6FG TO 20FG. FOUND LIGHT ASSEMBLY SMASHED AT SEAT 6FG. REPLACED BROKEN BULBS, LENSES AND BATTE RY PACK CHARGER MODULE M9011. ALL SEAT EPATH LIGHTS CK OK. 2 L 7 2 4F RT A1NM 2007091400114 20070914 00114 NE 2007 9 14 DL76G071161 2 20070901 A 7200 CF680C2B6 ENGINE BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6 30025 NE NR 1 MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 153DL 53263 24985 695334 DURING ENGINE START, LT ENGINE, AS THE L FUEL CONTROL SWITCH WAS PLACED ON, THESE INDICATIONS APPEARED - 1 EICAS L ENG F UEL VLV MSG 2 ENG VLV LIGHT ON PEDESTAL ENGINE WOULD NOT START NO EGT RISE FUEL CONTROL SWITCH WAS PLACED OFF APPROX 2 M INUTES LATER THE ABOVE EICAS MSG AND VLV LIGHT EXTINGUISHED. RESTARTED ENGINE, AT GATE CHKS GOOD. 2 L 7 2 4F 4 F RT A1NM E13NE 2007091400115 20070914 00115 NM 2007 9 14 DL777071162 1 20070901 A 2420 756603E GCU BOEING 777 777232 1385232 NM LEFT MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 864DA 29736 RTB DUE TO LT ENG GEN CONTROL OFF LIGHT ON GROUND. REPLACED LT GCU. 2 L 7 2 4F RT T00001SE 2007091400121 20070914 00121 EU 2007 9 14 F3LA200700228 1 20070908 A 5280 ATTACH FITTING AIRBUS A319 A319112 3930323 EU RT MLG DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED LWR FWD ATTACH FITTING ON RT MLG STRUT DOOR RUSTED. REMOVED AFFECTED PARTS AND INSTALLED LWR FWD ATTACH FITTING IAW MM 32-12-14-400-002. 2 L 7 2 4F RT A28NM 2007091400123 20070914 00123 NM 2007 9 14 DL76S071163 1 20070902 A 5330 148T312062 SKIN BOEING 767 767332 1382001 NM BS 1725 S7R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 135DL 25145 REPAIR REMOVED THAT WAS OUT OF SCOPE FOR AD2006-09-09. UNDERLYING CHORD FOUND CRACKED. DAMAGE WAS CUTOUT AND REPAIR DO UBLER AND TRIPLER WAS INSTALLED. 2 L 7 2 4F RT A1NM 2007091400124 20070914 00124 NM 2007 9 14 DL764071164 1 20070902 A 3610 361740001 SENSOR BOEING 767 767* NM NR 2 ENGINE MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 828MH 29699 RTB DUE TO R ENG BLEED OVERHEAT AND PRSOV STATUS MSG, T/S PER FIMM 36-20-00 FAULT 36-10510. REPLACED TM1 SENSOR OPS/LK CK GOOD RAN ENG. COULD NOT DUPLICATE. 2 L 7 2 4F RT A1NM 2007091400125 20070914 00125 NM 2007 9 14 DL757071166 1 20070903 A 2910 AS11508K032 HOSE BOEING 757 757232 1384965 NM HYD SYSTEM LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 616DL 22823 ON FINAL APPROACH AFTER SELECTING LANDING FLAPS LEFT HYD QTY STATUS MSG AND QTY LEVEL ZERO. FOUND OUTBOARD NOSE STEERIN G FLEX HYD LINE LEAKING IN AFT RT SIDE OF NOSE WHEEL WELL. INSTALLED TEMP HYD LINE TO FOM. REMOVED TEMP HYD LINE AND I NSTALLED NEW FLEX HYD L PER AMM. LEAK CK OK. 2 L 7 2 4F RT A2NM 2007091400126 20070914 00126 NM 2007 9 14 DL76L071168 1 20070902 A 4997 WIRE HARNESS BOEING 767 767332 1382001 NM APU BAY DAMAGED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 173DN 13558 P2440 24800 DURING DRC CHECK, FOUND APU EGT HARNESS BURNED WIRE INSULATION DAMAGED EXHAUST LEAK. REMOVED AND REPLACED APU PER OPN 6 051 AND OPN 7951. 2 L 7 2 4F RT A1NM 2007091400127 20070914 00127 NM 2007 9 14 DL76G071169 1 20070903 A 2822 PUMP BOEING 767 767324 1385203 NM CTR FUEL TANK INOPERATIVE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 394DL 27394 RTB - RT CTR FUEL PUMP IS INOP. RESET C/B`S AND RAN ENGINE. PUMP OPS NORMAL. 2 L 7 2 4F RT A1NM 2007091400129 20070914 00129 NM 2007 9 14 DL75E071171 1 20070904 A 3150 WARNING LIGHT BOEING 757 7572Q8 1384972 NM ILLUMINATED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 703TW 27620 RUDDER RATIO LIGHT ON DURING TAXI OUT A/C RTB RESET FAIL LIGHT ON LEFT AND RIGHT RUDDER RATIO BOX-ALL IS NORMAL. 2 L 7 2 4F RT A2NM 2007091400131 20070914 00131 NM 2007 9 14 DLM8K071173 1 20070903 A 2910 B-NUT DOUG MD88 MD88 3023688 NM HYD SYSTEM LOOSE A DALA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 912DE 49997 UPON CONFIGURING A/C FOR LANDING, LEFT HYD QUANTITY WENT TO 3 QUARTS AND REMAINED THERE. RAN QRH AND LANDED NORMALLY. DID NOT START APU AS PER QRH CHECKLIST. FOUND HYD LINE B NUT LOOSE ON LT ENG HYD CASE DRAIN FILTER OUTBOARD SIDE. RETO RQUED SAME PER AMM. PERFORMED LEAK CK. ALL NML. 2 L 7 2 4F RT A6WE 2007091400132 20070914 00132 NM 2007 9 14 DL76G071174 1 20070904 A 2120 UNKNOWN BOEING 767 767332 1382001 NM MID CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1612T 30575 INFLIGHT FLIGHT ATTENDANT REPORTS AN ELECTRICAL/BALLAST ODOR IN MID CABIN ON LEFT SIDE. CAN NOT DUPLICATE FAULT. RAN A LL ELECTRICAL EQUIPMENT IN MID GALLEY AND CHECKED FOR ANY LIGHT THAT WERE OUT OR FLICKERING. NO FAULT NOTED. DID NOT D ETECT ANY ODOR. 2 L 7 2 4F RT A1NM 2007091400134 20070914 00134 EU 2007 9 14 F3LA200700213 1 20070902 A 5321 D5367180500500 FLOOR PANEL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON LOWER SURFACE OF FLOOR PANEL 262FF. REMOVED AND REPLACED FLOOR PAN EL 262FF IAW AMM 53-42-12-400-002. 2 L 7 2 4F RT A28NM 2007091400139 20070914 00139 EU 2007 9 14 07FDEA03482 1 20070910 A 5313 A53612519200 LONGERON AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 HEAVY CORROSION AT LONGERON BETWEEN FRAME 11-15A, Y953, CABIN FLOOR STRUCTURE. REPAIR PERFORMED IAW SRM 53-12-15 / FIG. 207. 2 L 7 2 4F RT A35EU 2007091400140 20070914 00140 EU 2007 9 14 07FDEA03483 1 20070910 A 5730 A57340087 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND ON WING BOTTOM SKIN LT, RIB 8 AN OLD CORROSION REPAIR AROUND HOLE 585 (DRAWING R571-401410 ) WITHOUT ANY DOCUMENTA TION. REPAIR PERFORMED BY REWORK OF AREA AND FASTENER REPLACEMENT IAW EA 6-5720-106534 AND RAS/BAE/1005114/2007 ISS A. 2 L 7 2 4F RT A35EU 2007091400142 20070914 00142 WP 2007 9 14 07FDEA03486 1 20070910 A 5311 70750 FRAME DOUG MD10 MD1010F 3022112 WP BS 1421 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 399FE 48262 CENTER WHEEL WELL SPACE-STA 1421, L52L-L51L FRAME (LWR) CORROSION REMOVED CORROSION IAW MD/DC10-10 SRM 51-21-01 VOL 2, PG 28 FOUND TO BE OUT OF LIMITS IAW MD/DC10-10 SRM 53-00-01 VOL 1 FIG 1B. REPAIRED FRAME AT STA 1421 IAW MD/DC 10-10 , SRM 53-00-01 VOL 1 FIG 8. ORIGINAL THICKNESS .080 IAW MD/DC10-10 SRM AND 53- 00-01 ORIGINAL THICKNESS .080 IAW MD /DC SRM 53-14-01 VOL 3 FIG 11 REMOVED .029 REMAINING .051 2 L 7 3 4F RT A22WE 2007091400150 20070914 00150 EU 2007 9 14 07FDEA03377 1 20070905 A 5330 A53978155 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 727FD 579 OLD EXTERNAL REPAIR AT SKIN FRAME 65-66, STRG 33-34 RT, NOT CONFORM TO SRM 53-10-12/FIG 225. EXTERNAL DOUBLER REPAIR RE NEWED IAW SRM 53-10-12/FIG 225. 2 L 7 2 4F RT A35EU 2007091400151 20070914 00151 EU 2007 9 14 07FDEA03378 1 20070905 A 5414 A54611752504 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 1 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 CRACKED HOLES (ABOUT 8 MM) ON PYLON NR 1, RIB 8 OUTBOARD SIDEWALL. REPAIR PERFORMED IAW SRM 54-51-31/FIG 201. 2 L 7 2 4F RT A35EU 2007091400152 20070914 00152 EU 2007 9 14 07FDEA03379 1 20070905 A 5313 A53971006 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 MISDRILLED HOLE FOUND AT STRG 53 RT, FRAME 54.3. STRINGER REPAIR PERFORMED IAW SRM 53-10-14/FIG 201A. 2 L 7 2 4F RT A35EU 2007091400154 20070914 00154 EU 2007 9 14 07FDEA03491 1 20070910 A 5280 A52810125 DOOR AIRBUS 300 A300B4622R 3930312 EU ZONE 800 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 OLD EXISTING REPAIR AT LT NLG DOOR NOT CONFORM TO TD 942.045310/008/2006 (MATERIAL THICKNESS 1,3MM INSTEAD OF 1,6MM) R EPAIR RENEWED IAW EA 6-5282-106514 AND RAS 045310/014/2006. 2 L 7 2 4F RT A35EU 2007091400155 20070914 00155 EU 2007 9 14 07FDEA03492 1 20070910 A 5753 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 DURING ACCOMPLISHMENT OF EO 6-5750-7-500 FOUND AT LT INBOARD FLAP LOWER SKIN NUMEROUS HOLES WITH CRACK, TOOLING MARKS AN D MISDRILLED. REPAIR PERFORMED BY RAISING THE HOLES UNTIL REMOVAL OF DAMAGES IAW EA 6-5752- 106527 AND RAS/FOK/140/200 7 ISS A. 2 L 7 2 4F RT A35EU 2007091400156 20070914 00156 EU 2007 9 14 07FDEA03493 1 20070910 A 5414 A54612403 PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 FOUND WORN HOLES ON RIB 8 INBOARD AND OUTBOARD PANEL, PYLON NR 1 LHS. REPAIR PERFORMED IAW SRM 54-51-31/CONF 02/FIG 201 . 2 L 7 2 4F RT A35EU 2007091400157 20070914 00157 EU 2007 9 14 07FDEA03494 1 20070910 A 5753 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 DURING ACCOMPLISHMENT OF EO 6-5750-7-500 FOUND AT RT INBOARD FLAP LOWER SKIN NUMEROUS HOLES WITH CRACK, TOOLING MARKS AN D MISDRILLED. REPAIR PERFORMED BY RAISING THE HOLES UNTIL REMOVAL OF DAMAGES IAW EA 6-5752- 106527 AND RAS/FOK/141/200 7 ISS A. 2 L 7 2 4F RT A35EU 2007091400159 20070914 00159 EU 2007 9 14 07FDEA03496 1 20070910 A 5414 A54612403 PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 FOUND WORN HOLES ON RIB 8 INBOARD AND OUTBOARD PANEL, PYLON NR 2 RHS. REPAIR PERFORMED IAW SRM 54-51-31/CONF 02/FIG 201 . 2 L 7 2 4F RT A35EU 2007091400161 20070914 00161 EU 2007 9 14 07FDEA03498 1 20070910 A 5730 A57241132201 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 FOUND TWO CHAFE MARKS AND ONE IMPACT DAMAGE ON FIXED L/E 'D' NOSE SKIN BETWEEN TRACK 3-4 RT WING. REPAIR PERFORMED BY B LEND OUT OF CHAFING MARKS AND DRILLING 1/4INCH DIA HOLE WITH CSK AND INSTALLING A SOLID ALUMINUM RIVET IAW TD/J1/S1/0204 4/2005 ISSUE B, APPROVED BY RAS/BAE/1002044/2005 ISSUE A AND EA 6-5741-95871. 2 L 7 2 4F RT A35EU 2007091400165 20070914 00165 EU 2007 9 14 07FDEA03502 1 20070910 A 5320 A53810967200 DIAPHRAGM AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 FOUND SEVERAL DAMAGES AN DIAPHRAGM BETWEEN TRACK 4/5 RT AND LT, DENT-NICK- SCRATCHES AROUND FASTENERS. REPAIR PERFORME D BY BLEND OUT SCRATCHES AROUND FASTENERS, DRILLING HOLES FOR NICK (FULL FILLED WITH FASTENER), LETTING DENT IN STATE AN D HFEC/ROTOTEST/DVI. INSPECTION IN DAMAGED AREAS IAW EA 6-5315-95860 AND RAS 041901/013/200 5 ISSUE A. 2 L 7 2 4F RT A35EU 2007091400166 20070914 00166 NM 2007 9 14 DHLA200700041 1 20070831 A 3350 LIGHT BOEING 727 727264 138408M NM CABIN LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 765AT 23014 EMERGENCY LIGHT ILLUMINATED ON TAKEOFF. FOUND COCKPIT EMERGENCY LIGHT ASSY LOOSE. RESECURED IN PLACE PERFORMED GROUND TEST IAW M/M33-50-01,TEST OK 2 L 7 3 4F A3WE 2007091400167 20070914 00167 EU 2007 9 14 F3LA200700222 1 20070906 A 5510 PLATE AIRBUS A319 A319112 3930323 EU GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED THE TRIMMABLE HORIZONTAL STAB MECHANICAL LINKAGE INBD OF UPPER CHAIN SPROCKET DA MAGED. SWIVEL PLATE AND LINK PLATE GOUGED. REPLACED SWIVEL PLATE AND LINK PLATE IAW AMM 27-41-45-400-001. PERFORMED O PERATIONAL CHECK IAW AMM 27-41-00-720-001, SWIVEL PLATE P/N D2747003600000, LINK PLATE P/N D2747003700000. 2 L 7 2 4F RT A28NM 2007091400170 20070914 00170 EU 2007 9 14 07FDEA03381 1 20070905 A 5730 A57110203 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 FOUND ON CENTER WING BOX UPPER PANEL, UPPER SURFACE A NOTCH AT FRAME 47, BETWEEN TRACK 3-4 RT. REPAIR PERFORMED BY BL END OUT DAMAGE IAW EA 6-5710-95852 AND RAS/AS/0003/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091400173 20070914 00173 EU 2007 9 14 07FDEA03384 1 20070905 A 5320 A53612214205 WEB AIRBUS 300 A300B4622R 3930312 EU ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 727FD 579 FOUND OLD REPAIR AT WEB ON FLOOR STRUCTURE FRAME 13A-13B RT, Y-730, NOT CONFORM TO SRM (SPLICE MATERIAL). REPAIR RENE WED IAW SRM 53-12-15/FIG 207. 2 L 7 2 4F RT A35EU 2007091400176 20070914 00176 WP 2007 9 14 07FDEA03390 1 20070905 A 5347 FX510000M214 SEAT TRACK DOUG DC10 DC1030 3023501 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREAS AT F/S 1641-1781 LBL48 REMOVE, FABRICATED AND INSTALLED DAMAGED SEAT TRACK PER SRM. 2 L 7 3 4F A22WE 2007091400177 20070914 00177 EU 2007 9 14 07FDEA03503 1 20070910 A 5210 A52175325 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 800 CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 728FD 581 FOUND CRACKED FRAME SEGMENT ON RT AND LT AFT PAX DOOR (ZONE 843 / 833 ). FRAME SEGMENT REPLACED IAW SRM 52-13-00 AND SR M 51-72-10. 2 L 7 2 4F RT A35EU 2007091400178 20070914 00178 WP 2007 9 14 NWAA072999606 1 20070904 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 606NW 47225 TAIL COMPARTMENT PATH LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATION CHECKS GOOD. 2 L 7 2 4F A6WE 2007091400179 20070914 00179 WP 2007 9 14 07FDEA03504 1 20070910 A 5730 ARC1652 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 600 DAMAGED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 68052 47806 RT WING LWR SURFACE OUTBD FLAP FOUND 30 EA LOOSE RIVETS ON SKIN. REPAIRED AREA IAW SRM 57-20-00 VOL I FIG 11. 2 L 7 3 4F A22WE 2007091400183 20070914 00183 WP 2007 9 14 07FDEA03509 1 20070910 A 5320 AEA01613 WEB DOUG DC10 DC1010F 3022111 WP ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 LT MLG W/W FOUND CRACKS ON VERTICAL WEB. REPAIRED WEB IAW SRM 53-00-01 FIG 10 VOL I. 2 L 7 3 4F A22WE 2007091400184 20070914 00184 NM 2007 9 14 QXEA200701400 1 20070908 A 2432 BATTERY BOMBDR DHC8 DHC8402 1390042 NM MASTER MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 401QX 4031 LAX FLIGHT NR 2468: ON TAXI OUT, NR 1 TRU SHOWED NO LOAD. MAIN BATTERY SHOWED BETWEEN A CHARGE OF -18 TO A LOAD OF +15 WITHIN A 15 SECOND SPAN AND CONTINUED TO CYCLE. NO TRU CAUTION LIGHT. PULLED TRU C/B PER MTC AND RESET. NR 1 TRU LOAD SHOWED .01 THEN 0. MAIN BATTERY CONTINUED CHARGE/DISCHARGE CYCLE. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE REMOVED MA IN BATTERY FOR FOM. CLEANED CONTACTS ON SHUNTS 2431-R3, 2431-R4 AND 2431-R7. REINSTALLED MAIN BATTERY. GROUND RAN BOT H ENGINES. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007091400185 20070914 00185 NM 2007 9 14 AALA20071576 1 20070818 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 949AN 29537 MIA - EMERGENCY LIGHT AT SEAT ROW 17D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 17D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007091400186 20070914 00186 NM 2007 9 14 AALA20071568 1 20070813 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 AFW - EMERGENCY LIGHTS AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091400189 20070914 00189 NM 2007 9 14 AALA20071566 1 20070813 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 AFW - EMERGENCY LIGHTS AT LEFT NUMBER THREE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091400191 20070914 00191 SO 2007 9 14 SWIA200718660 1 20070903 A 3040 NP1513111 ELEMENT EMB 120 EMB120ER 3260203 SO WINDSHIELD HEAT INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 560SW 2873 2873 120334 FLT 3733 - CAPTAIN'S WINDSHIELD HEATING ELEMENT IS INOP. REPLACED WINDSHIELD ASSEMBLY IAW MM 56-10-01. 2 L 7 2 4T RT A31SO 2007091400192 20070914 00192 EA 2007 9 14 SWIA200718661 1 20070810 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA DAMAGED DAMAGED A SWIA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 NM 07 405SW 7029 LEFT LOWER FUSELAGE IS DAMAGED DUE TO CONTACT WITH GROUND EQUIPMENT WHILE PARKED ON RAMP. REPAIRED LOWER FUSELAGE PER R EO 601R-53-11-1230 AND REO 601R-53-11-1231. 2 L 7 2 4F RT A21EA 2007091400200 20070914 00200 EA 2007 9 14 SWIA200718669 1 20070909 A 4930 PRESSURE SWITCH CNDAIR CL600 CL6002B19 1900309 EA APU FUEL SYS LEAKING A SWIA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 412SW 7101 FLT 6562 - STRONG FUEL SMELL THROUGHOUT THE AIRCRAFT AFTER LANDING. REPLACED LEAKING APU FUEL PRESSURE SWITCH. 2 L 7 2 4F RT A21EA 2007091700004 20070917 00004 NM 2007 9 17 TAMF20070030S 1 20070824 A 5510 FAIRING BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE HORIZONTAL STAB CORRODED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 768QT 23803 DURING C CHECK INSPECTION WAS FOUND A CORROSION ON HORIZONTAL STABILIZER TIP LT NOSE IB - LT.DAMAGED AREA WAS REPAIRED I AW EWO 767-57-030 AND MFG SERVICE REQUEST 1-524791300. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FORM 8100-9 WAS ISSUED A PPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007091700009 20070917 00009 CE 2007 9 17 HSYA20070702 1 20070701 A 5260 1144000221 AIRSTAIR BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA CRACKED E HSYA O OTHER O OTHER NR NOT REPORTED 1 NM 05 122GL 26808 UC122 DURING PREFLIGHT INSPECTION, CREW REPORTED A CRACK ON THE AIRSTAIR DOOR NEAR THE HINGE. MX FOUND A CRACK ON THE INNER DO OR SKIN NEAR THE AFT END DOOR HINGE. UPON INITIATION OF A REPAIR TO AFFECTED AREA, MX FOUND CORROSION ON THE INNER DOOR SKIN, CLOSURE AND METAL HONEY COMB CORE COMPONENTS THAT EXCEEDED LIMITS. BASED ON INFORMATION PROVIDED TO THE AIRCRAFT M FR, MX REPAIRED THE DAMAGED AREA OF THE DOOR IAW FIELD REPAIR FR-CO-01572, REV. 2. ISSUED 8/6/07. 8/16/07 UPON INSTALLAT ION OF THE REPAIRED DOOR, IT WAS FOUND THAT THE REPAIR DEFORMED THE CONTOUR OF THE DOOR PREVENTING PROPER INSTALLATION. THE REPAIRED DOOR WAS DETERMINED TO BE BEYOND ECONOMICAL REPAIR. 8/28/07 A NEW AIRSTAIR DOOR ASSEMBLY WAS INSTALLED AFTE 2 L 7 2 4T 4 T RT A24CE E4EA 2007091700012 20070917 00012 NM 2007 9 17 TAMF20070033S 1 20070829 A 5330 SKIN BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE BS 1307-1329 DENTED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 768QT 23803 DURING INSPECTION OF (C2) CHECK WAS FOUND A DENT A/Y=25 ON SKIN STA 1307-1329 STR 32-33 - LT. DAMAGED AREA WAS REPAIRE D IAW EWO 767-53-052 AND SRM 53-00-01 REPAIR 6. THIS REPAIR CONSTITUTES A MAJOR REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007091700017 20070917 00017 NM 2007 9 17 TAMF20070028S 1 20070825 A 5330 SKIN BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE BS 1417-1436 DENTED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 768QT 23803 DURING INSPECTION OF (C2) CHECK WERE FOUND SEVERAL DENTS ON FUSELAGE SKIN STA 1417-1436 STRINGER 33 -36-LT. DAMAGED AR EAS WERE REPAIRED IAW EWO 767-53-055 AND SERVICE REQUEST 1-527218048. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FORM 8100 -9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007091700022 20070917 00022 NM 2007 9 17 TAMF20070023S 1 20070825 A 5410 2242301513 COWLING BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE NACELLE DAMAGED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 768QT 23803 DURING C CHECK INSPECTION WAS FOUND CORE COWL P/N: 224-2301-513 S/N: 0130 WITH ELONGATED HOLE AT FRAME STA NAC 294 - CF6 -80C2. DAMAGED AREA WAS REPAIRED IAW CV07-1781-01 AND EWO 767-54-020. THIS REPAIR CONSTITUTES A MAJOR REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007091700029 20070917 00029 NM 2007 9 17 TAMF20070036S 1 20070826 A 5330 SKIN BOEING 767 767200 1385120 NM GE CF6 CF680 30025 NE BS 582 CORRODED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 768QT 23803 DURING INSPECTION OF (C2) CHECK WAS FOUND A CORROSION ON PRESSURE SKIN STA 582 BETWEEN STRINGER 34-35 RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-058 AND SERVICE REQUEST 1-526668594. THIS REPAIR CONSTITUTES A MAJOR REPAIR, FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007091700038 20070917 00038 NM 2007 9 17 ASMF200709001 1 20070902 A 5542 SKIN BOEING 737 737* NM CFMINT CFM567 CFM567B22 13802 NE RUDDER DAMAGED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 850AM 33786 DURING OVERNIGHT CHECK, DETECTED EXPOSED AND DEFORMED COMPOSITE MATERIAL IN RUDDER TRAILING EDGE OF 1.5 INCH OF LENGTH A ND .6250 INCH DEEP AT STATION 235 AND BURNED SURFACE IN RUDDER TRAILING EDGE OF 2 INCH LENGTH AND .6250 INCH DEEP AT STA TION 240; ALL OF THIS DUE TO LIGHTNING STRIKE. THE DETAILS OF THE REPAIR WILL BE SUBMITTED AS SOON AS THEY WILL BE CONC LUDED. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007091700064 20070917 00064 SO 2007 9 17 N93A28082007 1 20070828 A 5553 1159B2154361 ATTACH FITTING GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU VERTICAL STAB CORRODED E N93A K NONE O OTHER IN INSP/MAINT 1 SO 13 495QS 1295 DURING 5000 LANDING INSPECTION FOUND 714 BULKHEAD VERTICAL STAB ATTACH FITTINGS CORRODED. 2 L 7 2 4F 4 F RT A12EA E25NE 2007091700066 20070917 00066 2007 9 17 721608242007 4 20070824 A 2211 7004206901 COMPUTER BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE SAS FAILED E QMLA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 330SL 7216 PATIENT FLIGHT, DURING THE FLIGHT THE MASTER CAUTION ILLUMINATED WITH ACCOMPANYING ROLL SAS CAUTION LIGHT, IMMEDIATELY FOLLOWED BY A STRONG ACRID BURNING ODOR IN THE COCKPIT. NO OTHER ADVERSE INDICATIONS WERE NOTED. SWITCHED OFF ALL SAS CHANNELS AND THE ODOR DECREASED. NOTIFIED DISPATCH OF THE INCIDENT AND ASKED FOR A MECHANIC TO BE INFORMED. FLIGHT CONT INUED TO DESTINATION WITHOUT FURTHER INCIDENT. SAS COMPUTER WAS CHANGED AND TESTED SATISFACTORILY AND RETURNED TO SERVI CE. DEFECTIVE SAS COMPUTER HAD A VERY STRONG BURNED SMELL COMING FROM IT. 1 G 7 2 3U 3 U H13EU E5NE10 2007091300089 20070913 00089 EA 2007 9 13 TRAX200701273 1 20070829 A 3250 STEERING SYS CNDAIR CL600 CL6002C10 1390015 EA NLG FAULTED A ASOA K NONE J WARNING INDICATION CL CLIMB 1 SO 27 760EV 10212 AFTER T/O FROM ATL NWS FAULTED. RESET SYSTEM C/B`S AFTER LANDING IN IAH. SYSTEM RESET. TOWER DECLARED EMERGENCY. 2 L 7 2 4F RT A21EA 2007091300094 20070913 00094 EU 2007 9 13 TRAX200701278 1 20070830 A 5313 STRINGER AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 ON FR 36, LEFT SIDE STRINGER 14 CORROSION FOUND. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42. 2 H 7 2 4T RT 2007091300138 20070913 00138 NM 2007 9 13 CALA0700497 1 20070906 A 5311 6546551 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17328 23458 INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 807, S9L. REPAIRED IAW ECRA 5310-04643. 2 L 7 2 4F RT A16WE 2007091300140 20070913 00140 NM 2007 9 13 CALA0700499 1 20070906 A 5311 6546533 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17328 23458 INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 500A BETWEEN STRINGERS 8 & 9R. REPAIRED IAW ECRA 5310-04651. 2 L 7 2 4F RT A16WE 2007091300151 20070913 00151 NM 2007 9 13 SWAA074456 1 20070906 A 5315 141A5180 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 750SA 29802 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, BETWEEN RBL 20 TO RBL 54. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007091300152 20070913 00152 NM 2007 9 13 SWAA074454 1 20070906 A 5512 182A40001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 730SW 27862 DURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138.7. REPAIRED SKIN PER SWA EA . 2 L 7 2 4F RT A16WE 2007091300156 20070913 00156 NM 2007 9 13 SWAA074442 1 20070906 A 2761 6544561 CASTING BOEING 737 7373H4 1384600 NM NR 5 SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 5 SPOILER INBOARD ACTUATOR CASTING CRACKED. REMOVED AND REPLACED ACTUATO R CASTING PER MM. 2 L 7 2 4F RT A16WE 2007091300162 20070913 00162 NM 2007 9 13 SWAA074440 1 20070906 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091300164 20070913 00164 NM 2007 9 13 SWAA074434 1 20070906 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091300165 20070913 00165 NM 2007 9 13 SWAA074439 1 20070906 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091300182 20070913 00182 NM 2007 9 13 SWAA074443 1 20070906 A 3397 W01300002 WIRE BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 488WN 33853 DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EEPLS INOP. FOUND BROKEN WIRE. REPAIRED WIRE PER MM. 2 L 7 2 4F RT A16WE 2007091300187 20070913 00187 NM 2007 9 13 CALA0700506 1 20070908 A 5322 6546560 SHEAR TIE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A .5 INCH CRACK IN SHEAR TIE AT STA 947 BELOW S25R. THE SHEAR TIE WAS REPAIRED IAW SRM 53-00-07. 2 L 7 2 4F RT A16WE 2007091300190 20070913 00190 NM 2007 9 13 CALA0700509 1 20070908 A 5313 655298845 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17328 23458 INSPECTION FOUND STRINGER 25L CORRODED AT STA 986.5. THE STRINGER WAS REPAIRED IAW SRM 53-00-03, FIGURE 201, PAGE 206. 2 L 7 2 4F RT A16WE 2007091300191 20070913 00191 SO 2007 9 13 LR7A07082 1 20070905 A 5100 339482 MANIFOLD LKHEED 382 382G 526414U SO HEAT TRANSFER CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2537 4698 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5324, FOUND RT MWW MANIFOLD CRACKED AT FS 533 WL146 BL63R. MANIFOLD REPLACED IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007091300236 20070913 00236 NM 2007 9 13 MWEA070210 1 20070910 A 3350 B5116 BATTERY BOEING 717 717200 1383700 NM TAIL CONE DISCHARGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 902ME 55166 TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHT AND TAILCONE RELEASE/SLIDE EMERGENCY LIGHTS GO OUT AFTER 25 SECONDS DURING OPE RATION CHECK. REMOVED AND REPLACED BATTERY. 2 L 7 2 4F TR A6WE 2007091300243 20070913 00243 NM 2007 9 13 SWAA074468 1 20070907 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 793SA 27888 DURING SCHEDULED HC1 CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007091300260 20070913 00260 NM 2007 9 13 SWAA074485 1 20070908 A 5330 6545776 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 969, STR 25R. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007091300261 20070913 00261 NM 2007 9 13 SWAA074466 1 20070907 A 5315 6545810 FLOORBEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 12. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2007091400008 20070914 00008 NM 2007 9 14 AWXA200701097 1 20070815 A 5311 65465588 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5987977, CRACKED FRAME, BS 907, S9L. REPAIRED FRAME, BS 907, S9L IAW USAIRWAYS EA 120228. 2 L 7 2 4F RT A16WE 2007091400016 20070914 00016 SO 2007 9 14 LR7A07077 1 20070905 A 5340 342593R TEE FITTING LKHEED 382 382G 526414U SO FS858 WL185 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2537 4698 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5313, FOUND TEE FITTING CRACKED AT FS 858 BHD TO SLOPING LONGERON AFT FUSELAGE INTERIOR AT FS858 WL185 RBL64. FITTING REPLACED IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007091400059 20070914 00059 EU 2007 9 14 07FDEA03537 1 20070911 A 5320 A53613848200 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 DAMAGED FITTING AT FRAME 12A, Z-177, STRG 26 RHS. REPAIR PERFORMED BY REPLACEMENT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091400060 20070914 00060 NM 2007 9 14 P5CA0701531 1 20070821 A 5720 SUPPORT BRACKET BOEING 747 74747UF 1384812 NM FUEL SERVICE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 416MC 32838 DURING WALK AROUND INSPECTION IN THE LEFT WING FUELING SERVICE PANEL BRACKET SUPPORT CRACK. PERFORMED PART 1 PER XEO 57 -082107 AND INTERIM REPAIR APPROVED. 2 L 7 4 4F RT A20WE 2007091400065 20070914 00065 EU 2007 9 14 07FDEA03456 1 20070907 A 5315 A53773651212 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 OLD CROSSBEAM REPAIR AT FRAME 33 LT, NOT CONFORM TO SRM 53-10-15/FIG 207 (SPLICE MATERIAL NOT CORRECT). SPLICE REPAIR R ENEWED IAW SRM 53-10-15/FIG 207. 2 L 7 2 4F RT A35EU 2007091400090 20070914 00090 EU 2007 9 14 AWXA200701070 1 20070823 A 5320 D53472094008 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-7 CHECK - NR 5980120, CORROSION ON CABIN FLOORBEAM, BS 3158/FR 66, +Y512. REPLACED CABIN FLOORBE AM, BS 3043/FR 64 - BS 3207/FR 67, +Y512 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007091400118 20070914 00118 EU 2007 9 14 DHL2007367508 1 20070807 A 5713 STRINGER AIRBUS 300 A300B4203 3930306 EU LT WING WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH 265 WHILE REMOVING L/WING PIPE FOUND WING STRINGER 17A TOP FLANGE WORN THRU BETWEEN RIB 27 AN 28. ROUTED OUT DAMAGE AT WING STRINGER 17A ON TOP FLANGE BETWEEN RIB 27 AN 28 IAW ASTAR ENG SKETCH 14001-005 REV A. ACCOMPLISHED VISUAL INSP PER AST AR ENG SKETCH 14001-005 REV A NO DEFECTS NOTED. TREATED AN PRIMED IAW A300 SRM 51-40-11. INSTALLED ANGLES IAW ASTAR EN G SKETCH 14001-005 REV A AN A300 SRM 51-40-11 AN 57-13-12. 2 L 7 2 4F RT A35EU 2007091400133 20070914 00133 EU 2007 9 14 F3LA200700214 1 20070902 A 5321 FLOOR PANEL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON TOP SURFACE OF FLOOR PLANEL 221EF AFT OTBD CONNECTING PLATE. REMOV ED AND REPLACED CONNECTING PLATE IAW AMM 53-12-12-400-001. 2 L 7 2 4F RT A28NM 2007091400141 20070914 00141 EU 2007 9 14 07FDEA03484 1 20070910 A 5330 A53778736 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 CORROSION ON FUSELAGE SKIN BETWEEN FRAME 30-31, STRG 54 LT TO RT. REPAIR PERFORMED BY BLEND OUT CORROSION, APPROVED BY EA 6-5314-95877 AND RAS/DABRE/7006101/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091400143 20070914 00143 WP 2007 9 14 07FDEA03487 1 20070910 A 5311 7075T6 FRAME DOUG MD10 MD1010F 3022112 WP BS 1401 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 399FE 48262 CENTER WHEEL WELL SPACE, STA 1401 FWD LWR SIDE OF FRAME FROM L51L - L51R CORROSION REMOVED CORROSION IAW MD/DC10-10 SRM 51-21-01 VOL 2 PG 28. FOUND TO BE OUT OF LIMITS IAW MD/DC10-10 SRM 53-00-01 VOL 1 FIG 1B. REPAIRED FRAME AT STA 1401 I AW MD/DC10-10 SRM 53-00-01 VOL 1 FIG 8. ORIGINAL THICKNESS .080 IAW MD/DC10-10 SRM 53-14-01 VOL 3 FIG 11. REMOVED .04 3 REMAINING .037. 2 L 7 3 4F RT A22WE 2007091400174 20070914 00174 EU 2007 9 14 07FDEA03385 1 20070905 A 5711 A57140885 SPAR AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 DURING ACCOMPLISHMENT OF EO 6-5710-7-3301 A2 PART 1 FOUND CORRODED HOLE 'D (SEE SB A300-57-6063). REPAIR PERFORMED BY R EAM UP AND OVERSIZING HOLE IAW EA 6-5710-95892 AND RAS/BAE/1002151/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091400175 20070914 00175 NM 2007 9 14 07FDEA03387 1 20070905 A 3610 652244419 DUCT BOEING 727 727225 1384077 NM 8TH STAGE DAMAGED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 464FE 21288 NR 1 ENG STRUT OVERHEAT LIGHT ILLUMINATED. PERFORMED QRH PROCEDURE AND LIGHT EXTINGUISHED. AFTER LIGHT EXTINGUISHED, N ORMAL POWER SETTINGS USED, LIGHT NEVER CAME BACK ON. REMOVED AND REPLACED 8TH STAGE DUCT DUE TO FLANGE AND NUT LEAKING. GROUND RAN NR 1 ENGINE PER JRH. ALL NORMAL, OK TO CONTINUE. 2 L 7 3 4F A3WE 2007091400182 20070914 00182 WP 2007 9 14 07FDEA03508 1 20070910 A 5313 ACA3353 LONGERON DOUG DC10 DC1010F 3022111 WP ZONE 100 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 AIR CONDITIONING COMPT LT SIDE ON LONGERON FOUND DEEP WEAR OUT OF LIMITS IAW SRM 53-10-00. REPAIRED AREA IAW SRM 53-10- 00 FIG 7 VOL I. 2 L 7 3 4F A22WE 2007091400188 20070914 00188 WP 2007 9 14 AALA20071589 1 20070819 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 412AA 49323 ATL - EMERGENCY LIGHT AT COCKPIT OVERHEAD PANEL INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT COCKPIT OVERHEAD PANE L. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007091400197 20070914 00197 EA 2007 9 14 SWIA200718666 1 20070903 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 448SW 7678 FOUND CRACK ON ENGINE SUPPORT BEAM TOP SIDE.CUT AWAY DAMAGED AREA OF UPPER PANEL OF BOX BEAM AND INSTALLED DOUBLERS IAW RII 53-900-1001 AND CRJ REO 601R-53-61-345 AND CRJ REO 601R-53-61-530. 2 L 7 2 4F RT A21EA 2007091700011 20070917 00011 NM 2007 9 17 TAMF20070032S 1 20070825 A 5330 SKIN BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE FUSELAGE CHAFED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 768QT 23803 DURING INSPECTION OF (C) CHECK WAS FOUND A WEAR ON RUB STRIPS SKIN STA 1725.50 STRINGER 22 - RT/LT. DAMAGED AREA WAS R EPAIRED IAW EWO 767-53-054 AND MFG SERVICE REQUEST 1-524791119. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007091700016 20070917 00016 NM 2007 9 17 TAMF20070029S 1 20070825 A 5320 SILL BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE BS 610 CORRODED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 768QT 23803 FWD CARGO COMPARTMENT LOWER MAIN SILL, THE UPPER EXTERIOR EXTRUDED SECTION HAS CORROSION AT STA 610. REMOVED AND REPLAC ED MAIN SILL IN FWD CARGO COMPARTMENT UPPER EXTERIOR EXTRUDED SECTION STA 610 IAW SRM 51-40-02 PAGE 2-3 AND SRM 51-40-02 PAGE 4-7. 2 L 7 2 4F 4 F RT A1NM E13NE 2007091700028 20070917 00028 NM 2007 9 17 TAMF20070034S 1 20070826 A 5320 SILL BOEING 767 767200 1385120 NM GE CF6 CF680 30025 NE FUSELAGE CORRODED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 768QT 23803 DURING INSPECTION OF (C2) CHECK WAS FOUND A CORROSION ON CARGO DOOR SURROUND STRUCTURE, MAIN SILL, OUTER CHORD STA 632 R T. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-059 AND SERVICE REQUEST 1-533874348. THIS REPAIR CONSTITUTES A MAJOR REPAIR , FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007091700030 20070917 00030 NM 2007 9 17 TAMF20070035S 1 20070826 A 5320 SILL BOEING 767 767200 1385120 NM GE CF6 CF680 30025 NE BS 569 CORRODED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 768QT 23803 DURING INSPECTION OF (C2) CHECK WAS FOUND A CORROSION ON CARGO DOOR SURROUND STRUCTURE, MAIN SILL, OUTER CHORD STA 569. 65 RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-056 AND SERVICE REQUEST 1-527218048. THIS REPAIR CONSTITUTES A MAJOR RE PAIR, FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007091700035 20070917 00035 NM 2007 9 17 TAMF20070031S 1 20070825 A 5754 SKIN BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE NR 2 SLAT WRINKLED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 768QT 23803 DURING (C) CHECKS INSPECTION WAS FOUND AN EXISTING REPAIR WRINKLED ON LEADING EDGE SLAT NR 2 UPPER SKIN. DAMAGED AREA W AS REPAIRED IAW EWO 767-57-029 AND MFG SERVICE REQUEST 1-527377149. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007091700039 20070917 00039 EU 2007 9 17 401108252007 1 20070825 A 2121 4900171 BLOWER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE A/C UNIT ARCED E QMLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 129LN 4011 IN LEVEL CRUISE FLIGHT AT 3500 MSL, CREW DETECTED STRONG ELECTRICAL BURNING ODOR. PILOT BEGAN DESCENT AND TURNED OFF AIR CONDITIONER. AFTER 10-15 SECONDS WITH A/C OFF SMELL WENT AWAY. AIRCRAFT WAS LANDED AT NEARBY AIRPORT. PATIENT WAS TRANS PORTED BY GROUND. MECHANIC AND ASM WERE CALLED. MECHANIC RELEASED AIRCRAFT TO RELIEF PILOT AFTER DETERMINATION THAT AFT BLOWER ON A/C UNIT HAD FAILED. 1 G 7 1 3U 3 U H9EU E19EU 2007091700076 20070917 00076 EA 2007 9 17 SWIA200718670 1 20070908 A 2913 887055 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA O OTHER K FLUID LOSS NR NOT REPORTED 1 NM 07 406SW 13101 13101 7030 FLT 5935 - FOUND HYDRAULIC FLUID DRAINING OUT OF THE AFT EQUIPMENT BAY. REPLACED RIGHT ENGINE DRIVEN HYDRAULIC PUMP IAW MM 29-11-00. 2 L 7 2 4F RT A21EA 2007091800001 20070918 00001 EU 2007 9 18 07FDEA03557 1 20070911 A 5330 A53776577 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 728FD 581 OLD DOUBLER REPAIR AT FRAME 36-37, STRG 29-30 LT. DISAGREEMENT IN SRM REFERENCE IN OUTER RIVET ROW IS IAW SRM 53-10-12/ FIG 207. REPAIR PERFORMED CONFORM TO VALID REFERENCE: SRM 53-10-12/FIG 225. 2 L 7 2 4F RT A35EU 2007091800003 20070918 00003 EU 2007 9 18 07FDEA03616 1 20070912 A 5730 A57246241203 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 FOUND SKIN BULGE (CORROSION) ON LEADING EDGE OF RT WING INBOARD FLAP, NEAR TO TRACK 1. REPLACEMENT OF L/E SKIN AT FLAP IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091800004 20070918 00004 EU 2007 9 18 07FDEA03632 1 20070913 A 5320 A93213455001 BRACKET AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 CRACKED BRACKET AT FRAME 19, STRG 46 LT. REPLACEMENT OF BRACKET IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091800005 20070918 00005 EU 2007 9 18 07FDEA03633 1 20070913 A 5320 A21214026200 BRACKET AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 CRACKED BRACKET AT FRAME 19, STRG 49 LT . REPLACEMENT OF BRACKET IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091800006 20070918 00006 EU 2007 9 18 07FDEA03634 1 20070913 A 5320 A21214126001 BRACKET AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 CRACKED BRACKET AT FRAME 19, STRG 50 LT. REPLACEMENT OF BRACKET IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091800007 20070918 00007 WP 2007 9 18 UPS07850611 1 20070809 A 5311 5751966503 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 MAIN CABIN FRAME FITTING HAS EXFOLIATION CORROSION AND CRACK AT STA 940 L21L. REPAIRED FRAME FITTING AT STA 940 L21L IAW SAA EA 008-5310-01-A1016 UPS RAA DC8-53-20651, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007091800008 20070918 00008 NM 2007 9 18 UPS07M50598 1 20070814 A 5320 INTERCOSTAL DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C CENTER CARGO COMPT ATTACHED INTERCOSTAL STRUCTURE BETWEEN LONGERONS 42L & 43L FOUND CRACKED AT STA 176 1. CRACKED INTERCOSTAL REMOVED PER SRM 51-31-01 VII R38. NEW INTERCOSTAL FAB PER DRAWING A5A7085. NEW INTERCOSTAL INS TALLED PER SRM 51-31-01 VII R38. 2 L 7 3 4F RT A22WE 2007091800017 20070918 00017 2007 9 18 COMA0760532 4 20070818 A 3442 RADAR CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 588SW 7069 FLIGHT 5312 - EN ROUTE FROM RDU TO MCO RADAR SHOWED RADAR NOT AT THIS RANGE AND ALL DISPLAY RANGES BOTH SIDES. AIRCRAFT DIVERTED TO SAV AND LANDED SAFELY. PERFORMED TEST OF WEATHER RADAR SYSTEM ON GROUND WITH CREW. RESET SYSTEM AND NO DE FECTS NOTED. 2 L 7 2 4F RT A21EA 2007091800018 20070918 00018 EA 2007 9 18 COMA0760533 1 20070819 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 523CA 7821 FLIGHT 5624 - FLAPS FAIL CAUTION MESSAGE AFTER FLIGHT COMPARTMENT SAFETY INSP CHECK LIST COMPLETED. COMPLIED WITH AD 20 06-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007091800020 20070918 00020 EA 2007 9 18 COMA0760548 1 20070829 A 3234 7179015 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 587SW 4101 7062 FLIGHT 5263 - GEAR DISAGREE. MAIN DOWN GREEN, NOSE GEAR UP. COMPLIED WITH QRH, GEAR CAME DOWN THREE GREEN, AND LANDED SAFELY. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE ASSEMBLY. 2 L 7 2 4F RT A21EA 2007091800022 20070918 00022 NM 2007 9 18 KCSA071331 1 20070906 A 5320 STIFFENER BOEING 747 747236B 1384804 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 RIGHT BODY GEAR WHEEL WELL UPPER PRESSURE WEB STIFFENER IS CRACKED AT STA 1423, RBL 8, WL 186.5. 2 L 7 4 4F A20WE 2007091800023 20070918 00023 GL 2007 9 18 C2XA07IA190 2 20070830 A 7200 AE3007A1P ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL RIGHT MALFUNCTIONED A C2XA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 27 13968 14376 8063 145138 CAE311435 ATL - FLIGHT 3067, THE CREW REPORTED LAV SMOKE WARNING & HAZE IN CABIN DURING FLIGHT. DIVERTED TO ATL WHERE IT LANDED W ITHOUT INCIDENT. MAINTENANCE OPS CHECK NR 1/ NR 2 PACKS IAW EMB 145 MM AMM 21-51-00. ALL OPS & INDICATIONS NORMAL. VI SUALLY INSPECTED, NO DEFECTS NOTED. PLACED LAV SMOKE DETECTOR ON MEL CAT C CONTROL 128344 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON FLIGHT 3067 FROM ATL THE CREW REPORTED LAV SMOKE WARNING AND SMOKE FROM UPPER DUCTS IN CABIN AFTER T/O, THE AIRCRAFT RETURNED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE RAN NR 1/ NR 2 ENGINES. FOUND N R 2 ENG BLEED SYSTEM TO BE CAUSING SMOKE IN CABIN. PLACED ON MEL IAW 36-11-05, CAT C CONTROL 128351. THE AIRCRAFT WAS 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007091800024 20070918 00024 SO 2007 9 18 C2XA07IA189 1 20070903 A 2120 UNKNOWN EMB 145 EMB145EP 3260221 SO COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 15941 145035 LFT - FLIGHT 2734, DURING PREFLIGHT INSPECTION, THE CREW REPORTED A BURNING SMELL IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT, AND FOUND THE ODOR TO BE COMING FROM THE PACKS WITH THE APU RUNNING. MAINTENANCE MEL'D THE APU 49-00-00 (C) CONTRO 128496, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 09/04/07, IAH MAINTENANCE RAN THE APU AND PA CKS WITH NO DEFECTS NOTED, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007091800025 20070918 00025 SO 2007 9 18 C2XA07IA191 1 20070831 A 3350 LIGHT EMB 145 EMB145EP 3260221 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 13936 145025 ICT - FLIGHT 2914, THE CREW REPORTED THAT THE EMERGENCY LIGHTS WERE INOP FROM THE FLIGHT ATTENDANT POSITION. MAINTENANC E RESET THE EMERGENCY LIGHT SYSTEM, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. 2 L 7 2 4F RT T00011AT 2007091800026 20070918 00026 SO 2007 9 18 C2XA07IA192 1 20070902 A 3320 BR90002 BALLAST EMB 145 EMB145LR 3260212 SO CABIN DEFECTIVE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 15973 145159 IAH - FLIGHT 2857, THE CREW REPORTED THAT THE BALLAST ABOVE SEAT 4A SMELLED BURNT. MAINTENANCE INSPECTED THE AIRCRAFT, AND PLACED THE LIGHTING IN MEL 33-210-00/1 CAT C CONTROL 128447, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. T HE AIRCRAFT RETURNED TO IAH ON FLIGHT 3145 WHERE MAINTENANCE REPLACED BALLAST, OPS CHECK GOOD. REMOVED FROM MEL, AND TH E AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007091800028 20070918 00028 SO 2007 9 18 C2XA07IA194 1 20070827 A 2432 38245001 BATTERY EMB 145 EMB145XR 3260214 SO NR 2 OVERTEMP A C2XA H DEACTIVATE SYST/CIRCUITS M J OVER TEMP WARNING INDICATION CR CRUISE 1 SW 27 16112 9276 1783 145660 TUL - FLIGHT 2403, THE CREW REPORTED A BATTERY 2 OVERTEMP INDICATION ON EICAS. THE CREW DEACTIVATED THE NUMBER TWO BATT ERY, AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO MAIN BATTERY, OPERATIONA LLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007091800030 20070918 00030 SO 2007 9 18 C2XA07RI072 1 20070827 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO CARGO BAY DEFECTIVE A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 17138 10534 458 145727 EWR - MX - BAG SMOKE LIGHT REMAINS ON IN EICAS. MX REMOVED AND REPLACED NR 2 BAGG SMOKE DETECTOR IAW EMB145 AMM AND PER FORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007091800032 20070918 00032 NM 2007 9 18 UPS07550612 1 20070905 A 3350 LIGHT BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 450UP 25472 INSPECTION TYPE:N/A EMERGENCY LIGHT ASSY HAS SEVEN INOP LAMPS. RELAMPED EMERGENCY LIGHT ASSY PER MM 33-51-01-2. 2 L 7 2 4F RT A2NM 2007091800034 20070918 00034 WP 2007 9 18 UPS07850613 1 20070724 A 5330 57503223975492 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C2 C-PIT STA 1240-1260 BETWEEN L36 AND L34R INTERNAL DOUBLER HAS CORROSION AND EXTENDS UNDER L35R. REPA IRED FUSELAGE SKIN AND INTERNAL DOUBLER AT STA 1242 L35R IAW SAA EA 008-5330-01-A0985, UPS RAA DC8-53-20644, AD FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007091800035 20070918 00035 WP 2007 9 18 UPS07850619 1 20070906 A 3350 LIGHT DOUG DC8 DC871F 302199D WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS (2 EACH) OVER MAIN ENTRY DOOR INOP. RELAMPED (2 EACH) EMERGENCY EXIT BULBS RE F MM 33-50-00. OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2007091800037 20070918 00037 EU 2007 9 18 TRAX200701294 1 20070827 A 5711 SPAR AEROSP ATR72 ATR72 EU WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 SDI - CRACK DETECT, FRONT SPAR LOWER SURFACE FLANGE AT RIB 12. 2 H 7 2 4T RT 2007091800038 20070918 00038 EU 2007 9 18 TRAX200701295 1 20070827 A 5711 SPAR AEROSP ATR72 ATR72 EU WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 SDI - CRACK DETECT, FRONT SPAR LOWER SURFACE FLANGE AT RIB 10. 2 H 7 2 4T RT 2007091800039 20070918 00039 EU 2007 9 18 TRAX200701297 1 20070828 A 1100 PLACARD AEROSP ATR72 ATR72 EU EXTERIOR MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 EXTERNAL PLACARDS MISSING. 10-18-07 EXTERNAL PLACARD ERPLACED IAW MM 11-00-00. 2 H 7 2 4T RT 2007091800040 20070918 00040 EA 2007 9 18 TRAX200701298 1 20070904 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 875AS 7559 AAR - CLIP CRACKED AT FS 484, RBL 36 INBOARD. 2 L 7 2 4F RT A21EA 2007091800042 20070918 00042 EA 2007 9 18 TRAX200701300 1 20070904 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 875AS 7559 AAR - CLIP CRACKED AT FS 484, LBL 36 INBOARD. 2 L 7 2 4F RT A21EA 2007091800043 20070918 00043 EA 2007 9 18 TRAX200701301 1 20070904 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 875AS 7559 AAR - BATH TUB FITTING CRACKED AT FS 472, RBL 9 OUTBOARD. REPAIRED IAW CRJ 200 SRM 51-40-11. 2 L 7 2 4F RT A21EA 2007091800044 20070918 00044 EA 2007 9 18 TRAX200701308 1 20070904 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR STICKS A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 839AS 7284 MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE, MAIN DOOR HANDLE IS STICKING. 2 L 7 2 4F RT A21EA 2007091800046 20070918 00046 EU 2007 9 18 TRAX200701310 1 20070904 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 631AS 362 EMERGENCY LIGHT OUT ON MAIN DOOR. 2 H 7 2 4T RT 2007091800047 20070918 00047 EA 2007 9 18 TRAX200701311 1 20070904 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 880AS 7606 GROUND PERSONNEL REPORTS THE SERVICE DOOR IS DIFFICULT TO OPEN. 2 L 7 2 4F RT A21EA 2007091800049 20070918 00049 EU 2007 9 18 YENA2007079 1 20070906 A 2797 19014967401 WIRE HARNESS EMB ERJ190 ERJ190100IGW 3260408 EU L/E SLAT DAMAGED A YENA B EMER. DESCENT F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 EA 15 238JB 3308 19000039 SLAT FAIL MESSAGE WHEN GOING FROM POSITION 0 TO 1. QRH COMPLIED WITH. SLAT FAIL REMAINED. PERFORMED TSM 27-81-00-810- 805A. FOUND SKEW SENSOR HARNESS LT WING OUTBOARD SLAT 3/4 DEFECTIVE HIGH MILLIVOLTS & CRIMPED AND CHAFING. REMOVED AND REPLACED LT OUTBOARD WING SLAT 3/4 SKEW SENSOR HARNESS PER AMM 27-83-07. OPS CHECK GOOD, PERFORMED OPERATIONAL TEST OF OUTBOARD SLAT SKEW SENSOR (3 & 4 SLAT) PER AMM 27-83-01. OPERATIONAL TEST OK. NO FURTHER FAULTS FOUND. NO CMC FAILUR ES PERTAINING TO SLAT FAIL MESSAGES. 2 L 7 2 4F RT A57NM 2007091800050 20070918 00050 EA 2007 9 18 TRAX200701318 1 20070906 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 744EV 10157 RIGHT 2ND FROM AFT EXTERNAL EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007091800051 20070918 00051 EA 2007 9 18 TRAX200701319 1 20070906 A 3350 LENS CNDAIR CL600 CL6002C10 1390015 EA CABIN CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 719EV 10099 CREW REPORTS OVERWING EMERGENCY EXIT LIGHT LENS IS CRACKED. 2 L 7 2 4F RT A21EA 2007091800052 20070918 00052 EA 2007 9 18 TRAX200701320 1 20070906 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 708EV 10060 EMERGENCY LIGHT INOP AT ROW 5 O/H. 2 L 7 2 4F RT A21EA 2007091800053 20070918 00053 EU 2007 9 18 200709061 1 20070903 A 2150 10018582 ACM EMB ERJ170 ERJ170100SE 3260406 EU A/C BAY FAILED A UHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 11 632RW 17000050 FLIGHT 7509 IAD TO ROC ON DESCENT THE CREW SMELLED A BURNING ODOR. FLIGHT ATTENDANTS CONFIRMED A BURNING ODOR IN THE CA BIN. CREW SHUT OFF THE RECIRCULATION FANS AND DECLARED AN EMERGENCY. SHORTLY AFTER THE RECIRCULATION FANS WERE SHUT OF F THE SMELL WENT AWAY FOLLOWED BY A -PACK 2 FAIL- EICAS MESSAGE A SHORT TIME LATER. CREW RAN THE QRH PROCEDURE AND TURN ED THE NR 2 PACK OFF. FLIGHT LANDED UNEVENTFULLY. MAINTENANCE REPLACED THE NR 2 PACK ACM AND HEAT EXCHANGER. 2 L 7 2 4F RT A56NM 2007091800054 20070918 00054 NM 2007 9 18 2007UALA03154 1 20070810 A 2781 284T084322 SENSOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE L/E SLAT OUT OF ADJUST A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 675UA 29243 RTFL DUE TO L/E SLAT DISAGREE INDICATION & LIGHT. ADJUSTED NR 11 OUTBOARD SENSOR AND OPS CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007091800055 20070918 00055 NM 2007 9 18 2007UALA03156 1 20070812 A 5280 146N3641 INDICATION SYS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT MALFUNCTIONED A UALA O OTHER B N SMOKE/FUMES/ODORS/SPARKS FALSE WARNING CL CLIMB 1 WP 29 596UA 28749 CREW REPORTED GEAR HANDLE TO OFF THEN EICAS DOORS & GEAR DISAGREE. ALSO HAD HOT RUBBER ODOR IN COCKPIT. PERFORMED TROU BLESHOOTING OF PSEU INPUTS AND TARGET TESTED OK. NO INBOARD STATUS MESSAGE. CREW CYCLED HANDLE AND SYSTEM OPERATED OK. NO PREVIOUS HISTORY ON RECORD. NO FLIGHT FAULTS. NO OTHER MAINTENANCE SYSTEM MESSAGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091800056 20070918 00056 NM 2007 9 18 2007UALA03174 1 20070813 A 2760 285T0012112 CONTROL MODULE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SPOILER SYS MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 567UA 26673 RTFL DUE TO SPOILERS LIGHT ON DURING CLIMB ON EICAS AND OVERHEAD. FOUND A MALFUNCTIONING SPOILER CONTROL MODULE. REPLA CED SCM PER UA EG SPECIFICATIONS. SYSTEM CHECKS GOOD. NO LIGHT OR MESSAGE PRESENT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091800057 20070918 00057 2007 9 18 2007UALA03175 4 20070815 A 2565 D30656126 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R3 DOOR LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 590UA 28708 DOOR 4 RT SLIDE PRESSURE LOW INDICATOR NEEDLE AT LOW END OF GREEN BAND. PRESSURE LOW. SLIDE REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091800058 20070918 00058 NM 2007 9 18 2007UALA03176 1 20070814 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 580UA 26698 JETWAY CONTACTED LEFT SIDE OF AIRCRAFT JUST 6 FT FWD OF DOOR 2L. MAJOR REPAIR ACCOMPLISHED. DOOR 2L, DENT IS 4 INCHES BY 2 INCHES BY QUARTER OF AN INCH DEEP ON A STRINGER; SOME METAL WAS REMOVED FROM THE SCRAPE. ACCOMPLISHED DOUBLER REPA IR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091800060 20070918 00060 NM 2007 9 18 2007UALA03196 1 20070815 A 2842 201280104 PROBE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT FUEL TANK FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 660UA 27115 RIGHT TANK FUEL QUANTITY GAUGE INOPERATIVE. REPLACED FUEL PROBES NR 7 AND NR 9 THRU NR 14 IN RT TANK. BITE AND OPS CHE CKED OK. PANELS LEAK CHECKED OK. REBALANCED FUEL. CHECKED TANK WIRING FROM CONNECTOR TO WING TIP, FOUND NO DEFECTS. AFTER VERIFICATION FLIGHT, AIRCRAFT RETURNED TO ETOPS SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007091800061 20070918 00061 NM 2007 9 18 2007UALA03201 1 20070816 A 5250 AR47041 STRIKER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT DOOR BURNED A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 177UA 24384 RAMP TURNBACK DUE TO BURNING SMELL AT COCKPIT DOOR AREA. REPLACED COCKPIT DOOR STRIKER ASSY. SMELL GONE, OP CHECKED NO RMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007091800062 20070918 00062 NM 2007 9 18 2007UALA03504 1 20070904 A 3350 505800057 GUARD AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE F/A PANEL MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 829UA 1211 EMERGENCY LIGHT SW GUARD ON THE AFT F/A PANEL IS MISSING. REPLACED EMERGENCY SWITCH LIGHT AT AFT GALLEY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007091800063 20070918 00063 NM 2007 9 18 2007UALA03505 1 20070901 A 2611 PPA120200 SMOKE DETECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LAVATORY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 831UA 1291 DOOR 2L FWD LAV SMOKE DETECTOR IS INOPERATIVE. REPLACED FWD AFT LAV SMOKE DETECTOR. TESTED OK ON SDCU. 2 L 7 2 4F 4 F RT A28NM E40NE 2007091800064 20070918 00064 NM 2007 9 18 2007UALA03506 1 20070831 A 5313 STRINGER SPLICE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 843UA 1573 AFT STRINGER SPLICE IS CORRODED AT FR 51 ON STR 43L. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER SPLICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007091800066 20070918 00066 NM 2007 9 18 2007UALA03508 1 20070904 A 5210 CYLINDER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R2 DOOR LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 852UA 1671 NR 2 RIGHT PASSENGER DOOR EMERGENCY CYL-ACCUM PRESSURE LOW. SERVICE DOOR ASSIST CYLINDER TO PROPER PRESSURE, 2 L 7 2 4F 4 F RT A28NM E40NE 2007091800067 20070918 00067 CE 2007 9 18 DJFA2007105 1 20070828 A 7160 INLET BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE NACELLE CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 445LX RK298 PCEJA0243 DURING A SCHEDULED MAINTENANCE EVENT MAINTENANCE FOUND A CRACK ON THE RT ENGINE INLET RING AT THE 7 O’CLOCK POSITION. T HE CRACK TRANSECTED THE SCREW HOLE FROM THE AFT EDGE OF THE RING. 10-9-07 MAINTENANCE REPLACE THE INLET ASSEMBLY. 2 H 7 2 4F 4 F RT A16SW E25EA 2007091800068 20070918 00068 CE 2007 9 18 DJFA2007104 1 20070828 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 445LX 4946 RK298 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER IB RIB AND BRACKET ASSEMBLIES, BOTH THE RT IB ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS O F THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. MAINTENANCE REPLACED THE CRACKED RIB AND PREVENTATIVELY REPLACED THE LT RIB USING THE IMPROVED RIB ASSEMBLY. 2 H 7 2 4F RT A16SW 2007091800069 20070918 00069 EU 2007 9 18 BAQA200700028 1 20070828 A 6330 L633M2010107 MOUNT UROCOP EC135 EC135T1 5620026 EU M/R GEARBOX OUT OF TOLERANCE E BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 135KY 1084 0444 DURING GROUND POWER CHECKS FOUND AIRCRAFT TO HAVE A LATERAL VIBRATION. INSPECTED Z-ARIS MOUNTS AND FOUND THE RT REAR Z-A RIS MOUNT OUT OF LIMITS. REMOVED AND REPLACED THE RT REAR Z-ARIS MOUNT. PERFORMED MAIN ROTOR TRACK AND BALANCE. NO FU RTHER DEFECTS NOTED. 1 G 7 2 3U H88EU 2007091800070 20070918 00070 EU 2007 9 18 BAQA200700030 1 20070910 A 6210 109010301115 BLADES AGUSTA A109 A109 0260109 EU MAIN ROTOR CRACKED E BAQA O OTHER E VIBRATION/BUFFET LD LANDING 1 EA 03 2MF 663 7277 WHILE PERFORMING MAINTENANCE, PILOT FELT AN USUALLY HIGH VIBRATION LEVEL DURING LANDING. A POST FLIGHT INSPTION REVEALED A CORDWISE CRACKS FROM THE TRAILING EDGE TO THE AFT SIDE OF THE SPAR ON THE TOP AND BOTTOM SKINS. THE BLADE WAS REPLACE D WITH P/N 109-0103-01-115 S/N P127. THE TRACK AND BALANCE AND OPERATIONAL CHECK FLIGHT WAS PERFORMED WITH NO DEFECTS NO TED. 1 G 7 2 3U H7EU 2007091800071 20070918 00071 2007 9 18 AMWA87352 4 20070911 A 3410 INDICATION SYS BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE COCKPIT SMOKE A AMWA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 07 155ZV UE155 ON TAXI OUT CAPT NOTED SMOKE AND ELECTRICAL ODOR WHICH APPEARED TO BE COMING FROM CAPT'S EFIS SYSTEM. CREW DECIDED TO R ETURN TO GATE WITH NO FURTHER INCIDENT. CND ON GROUND, SYSTEM OPS CHECKS NORMAL. REMOVED AND REPLACED CAPT EFIS SCREEN FOR PRECAUTIONARY MEASURES. 2 L 7 2 4T 4 T RT A24CE E26NE 2007091800072 20070918 00072 EU 2007 9 18 2007UALA03509 1 20070903 A 3350 MR33131 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 402UA 439 EMERGENCY LIGHT LEFT FWD UNIT FAULT. REPLACED FWD LEFT EPSU BATTERY. OPS CHECK GOOD. NO FAULTS RETURNED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007091800073 20070918 00073 CE 2007 9 18 DJFA2007106 1 20070830 A 3260 DOWNLOCK SWITCH CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG ACTUATOR INOPERATIVE E DJFA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 23 703LX 107 7500074 ON APPROACH TO LAND, CREW REPORTED A NOSE GEAR UNSAFE LIGHT. CREW UTILIZED THE EMERGENCY GEAR EXTENSION PROCEDURE AND L ANDED SAFELY. MAINTENANCE FOUND THE NOSE DOWNLOCK SWITCH INOPERATIVE AND REMOVED AND REPLACED THE NLG ACTUATOR. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007091800075 20070918 00075 SO 2007 9 18 DJFA2007100 1 20070824 A 2120 UNKNOWN EMB 135 EMB135BJ 3260306 SO ALLSN AE300 AE3007A GL COCKPIT ODOR E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 23 908LX E145528 DURING CLIMB, CREW REPORTED STRONG FUEL ODOR. ODOR DISBURSED QUICKLY AND DID NOT RETURN. MAINTENANCE PERFORMED NUMEROU S OPERATIONAL AND LEAK CHECKS BUT WAS UNABLE TO DUPLICATE THE PROBLEM AND FOUND NO EVIDENCE OF FUEL LEAKAGE. 2 L 7 2 4F 4 F RT TE6CH 2007091800076 20070918 00076 EU 2007 9 18 2007UALA03511 1 20070903 A 2612 FIRE LOOP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 422UA 503 ENG 2 FIRE LOOP -A- FAULT ECAM. NR 2 ENG PYLON LOOP A 3WD2 FAILS. REPLACED NR 2 ENG PYLON LOOP A 3WD2. 2 L 7 2 4F 4 F RT A28NM E40NE 2007091800077 20070918 00077 CE 2007 9 18 DJFA2007099 1 20070824 A 7120 30710704 MOUNT RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP NR 1 ENGINE CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 828LX 258461 DURING A SCHEDULED MAINTENANCE INSPECTION, TECH FOUND THE NR 1 ENGINE UPPER AFT ENGINE MOUNT CRACKED. THE MOUNT IS CRAC KED AT THE RADIUS AT BOTH ENDS ON THE AFT SIDE OF THE MOUNT. CRACKS ARE APPROXIMATELY .75 INCHES. MAINTENANCE REPLACED THE UPPER AFT MOUNT. 2 L 7 2 4F 4 F RT A3EU E6WE 2007091800079 20070918 00079 SW 2007 9 18 AC2A117123 1 20070827 A 6320 430040003109 TRANSMISSION BELL 430 430 1182150 SW ALLSN 250C 250C40B 03032 NE MAIN ROTOR MAKING METAL E AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 430CH 4646 49037 XMSN CHIP / CHP PLTRY GB ILLUMINATED IN FLIGHT 8 MINUTES AFTER DEPARTURE FROM ICY HELIPORT. AIRCRAFT RETURNED TO ICY WIT HOUT INCIDENT.SMALL AMOUNT OF METAL WAS FOUND ON TRANSMISSION PLANETARY CHIP DETECTOR. COMPLIED WITH SERVICEABILITY CHEC K OF TRANSMISSION. THE TRANSMISSION PASSED SERVICEABILITY CHECK AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 2 3U 3 U RT H9SW E1GL 2007091800080 20070918 00080 EU 2007 9 18 2007UALA03513 1 20070831 A 3350 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 413UA 470 FOUND FWD 1L BATTERY AT FAULT FOR EMERGENCY LIGHTS. FOUND FAULTY BATTERY. REPLACED DOOR 1L LIGHT BATTERY, 2 L 7 2 4F 4 F RT A28NM E40NE 2007091800082 20070918 00082 NM 2007 9 18 2007UALA03514 1 20070901 A 3220 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NLG VIBRATION A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 658UA 27113 RTFL UNDER AMBER ALERT DUE TO NOSE LANDING GEAR VIBRATION ON TAKEOFF. 2 L 7 2 4F 4 F RT A1NM E24NE 2007091800088 20070918 00088 NM 2007 9 18 2007UALA03520 1 20070831 A 3350 STRIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN MISSING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 366UA 24535 EMERGENCY LIGHT STRIP MISSING AT ROW 12. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800092 20070918 00092 NM 2007 9 18 2007UALA03522 1 20070831 A 5230 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 FWD CARGO DOOR OUTER SKIN 12 INCHES ABOVE HANDLE CUTOUT AND 21 INCHES FROM AFT EDGE DENT, NEXT TO REPAIR DOUBLER A=1.0 Y =0.101 AND A TO Y RATIO = 9.9. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800093 20070918 00093 SW 2007 9 18 AC2A117290 1 20070912 A 6320 206040044107 TRANSMISSION BELL 206 206L3 1182108 SW ALLSN 250C 250C30 03013 GL MAIN ROTOR WARNING LIGHT E AC2A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 07 53702 51249 A FEW MINUTES AFTER DEPARTING SP78B, THE TRANSMISSION CHIP LIGHT BRIEFLY ILLUMINATED AND THEN WENT OUT. COMPLETED A 180 DEGREE TURN TOWARDS SP78B AND THE LIGHT ILLUMINATED AND REMAINED, LANDED AND SHUTDOWN. 1 G 7 1 3U 3 U H2SW E1GL 2007091800094 20070918 00094 SW 2007 9 18 AC2A117321 1 20070910 A 6320 427040006107 TRANSMISSION BELL 427 427 1182207 SW PWC PW207 PW207D NE MAIN ROTOR MAKING METAL E AC2A O OTHER J WARNING INDICATION CR CRUISE 1 SO 07 427GT 56044 TRANSMISSION CHIP LIGHT ILLUMINATED. 1 VERY SMALL FLAKE AND 1 SMALL HAIR SLIVER ON LT TRANSMISSION CHIP DETECTOR. CHECKE D AND CLEANED PLUG, ALSO CHECKED THE OTHER (2) CHIP DETECTORS AND FOUND TO BE CLEAN. PENALTY RAN AIRCRAFT FOR 1 HOUR WIT H NO FURTHER CHIP LIGHTS. RECHECKED ALL CHIP PLUGS WITH NO MORE METAL NOTED. AIRCRAFT RELEASED FOR FURTHER FLIGHT. 1 G 7 1 3U 3 U R00001RC E42NE 2007091800095 20070918 00095 CE 2007 9 18 DJFA2007107 1 20070831 A 7160 45A35042003 INLET BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE RT ENGINE CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 476LX 2845 RK376 PCEJA0531 DURING A SCHEDULED INSPECTION, MAINTENANCE DISCOVERED A CRACK ON THE RT ENGINE INLET AT THE 12 O'CLOCK POSITION THAT EXT ENDED FWD AND AFT OF THE SCREW TRANSECTING THE SCREW HOLE. MAINTENANCE REPLACED THE INLET. 2 H 7 2 4F 4 F RT A16SW E25EA 2007091800099 20070918 00099 CE 2007 9 18 CIEA200700007 1 20070828 A 5230 BRACKET BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA CARGO DOOR LATCH BENT E CIEA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 520MC 45 BB43 DURING CRUISE FLT, CREW HEARD A NOISE & NOTICED THAT THE LT WING LOCKER HAD COME OPEN AND DOOR WAS TRAILING A FEW INCHES OPEN IN FLIGHT. ACFT APPROXIMATELY 25 MILES FORM A SUITABLE AIRPORT & CREW LANDED WITHOUT FURTHER INCIDENT. BAGGAGE F ROM WING LOCKERS REMOVED & PLACED IN BAGGAGE COMPARTMENT INSIDE ACFT. CREW INSPECTED WING LOCKING MECHANISM & DETERMINE D IT WAS LOCKING. LOCKER CLOSED & UNIT LOCKED WITH KEY LOCK. ACFT CONTINUED FLT TO ITS DESTINATION. UPON RETURN OF AC FT TO ITS HOME BASE, MX INSPECTED WING LOCKER & FOUND RT RECEIVER LOCK BRACKET SLIGHTLY BENT. RECEIVER LATCH STRAIGHTEN ED & INSPECTED FOR ANY CRACKS & NONE NOTED. ACFT CARRYING A SOFT SIDED TYPE OF DUFFLE BAG & IT MAY HAVE BEEN SUBJECTING 1 L 7 2 4T 4 T A24CE E4EA 2007091800100 20070918 00100 NM 2007 9 18 2007UALA03525 1 20070901 A 5514 LUG BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZ STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 RIGHT STAB LUG CORRODED: RT HORIZ STAB UPPER LUG FWD FACE CORRODED OUTSIDE OF ALLOWABLE DAMAGE AREA. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800101 20070918 00101 EU 2007 9 18 BAQA200700027 1 20070821 A 6330 L633M2010107 MOUNT UROCOP EC135 EC135T1 5620026 EU M/R GEARBOX OUT OF TOLERANCE E BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 235U 27 0548 PILOT REPORTED MAIN ROTOR VIBRATION IN FLIGHT. INSPECTED Z-ARIS MOUNTS AN FOUND THE LT REAR AND LT FORWARD, Z-ARIS MOU NTS IN UNSERVICABLE CONDITION. REMOVED AND REPLACED Z-ARIS MOUNTS. PERFORMED TRACK AND BALANCE OF MAIN ROTOR. NO FURT HER DEFECTS NOTED. 1 G 7 2 3U H88EU 2007091800103 20070918 00103 NM 2007 9 18 2007UALA03526 1 20070901 A 5514 LUG BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZ STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 LEFT HORIZONTAL STAB CENTER SECTION FWD UPPER ATTACH CLEVIS AFT LUG HAS CORROSION ON FACE AND BORE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800104 20070918 00104 CE 2007 9 18 CIEA200700006 1 20070825 A 3397 WIRE BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA EMERGENCY LIGHTS PINCHED E CIEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 520MC 12924 BB43 SHORTLY AFTER TAKEOFF THE PASSENGER NOTIFIED THE FLIGHT CREW THAT THEY HAD OBSERVED SMOKE FROM THE AREA OF THE NO SMOKIN G FASTEN SEAT BELT SIGN. THE FLIGHT CREW THAN OBSERVED THAT THE NO SMOKING FASTEN SEAT BELT SIGN CIRCUIT BREAKER HAD IN FACT POPPED. THE FLIGHT CREW RETURNED TO THE AIRPORT AND LANDED WITHOUT INCIDENT. MAINTENANCE DID A QUICK INSPECTION OF THE AIRCRAFT AND VERIFIED THAT THERE WAS NO POWER TO THE NO SMOKING AND FASTEN SEAT BELT SIGN, TY-RAPPED THE CIRCUIT BREAKER AND MEL’ED THE SIGN. THE MAINTENANCE DEPARTMENT LATER INSPECTED THE SYSTEM AND FOUND ONE OF THE POWER WIRES TO THE NO SMOKING AND FASTEN SEAT BELT SIGN TO BE PINCHED IN THE FRAMEWORK OF THE EMERGENCY EXIT. THE WIRING WAS REPAIRED 1 L 7 2 4T 4 T A24CE E4EA 2007091800105 20070918 00105 CE 2007 9 18 DJFA2007103 1 20070826 A 2170 21BC112 COALESCER BAG BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE DIRTY E DJFA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 408CW RK108 DURING CRUISE, PAX REPORTED AN ODOR OF BURNING RUBBER IN THE CABIN. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTEN ANCE FOUND THE COALESCER SOCK DIRTY AND REPLACED IT. 2 H 7 2 4F 4 F RT A16SW E25EA 2007091800108 20070918 00108 NM 2007 9 18 2007UALA03529 1 20070902 A 2612 FIRE WARNING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 351UA 24319 FIRE BELL INOPERATIVE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800109 20070918 00109 CE 2007 9 18 DJFA2007102 1 20070826 A 3213 259UN11A STRUT RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP NLG DETACHED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 803TA 7422 258455 DURING PREFLIGHT, THE CREW NOTED A BUSHING ON THE NLG ACTUATOR THAT APPEARED TO BE MIGRATING. MAINTENANCE DISCOVERED TH AT THE BUSHING HAD IN FACT MIGRATED AND WAS ON THE VERGE OF SLIPPING OUT COMPLETELY. MAINTENANCE REMOVED AND REPLACED T HE NOSE STRUT ASSEMBLY. 2 L 7 2 4F 4 F RT A3EU E6WE 2007091800111 20070918 00111 EU 2007 9 18 M7K2007F00000 1 20070806 A 5302 350A23404020 FRAME UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAILBOOM CRACKED A M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 803MH 4833 3735 DURING ROUTINE 100 HOUR INSPECTION THE CRACK WAS FOUND UTILIZING A BRIGHT LIGHT LOOKING AFT DOWN THE TAIL BOOM INTERIOR FROM THE TAILBOOM MOUNTED BATTER ACCESS DOOR. AS VIEWED FROM THE REAR, THE CRACK WAS LOCATED AT THE 9:00 POSITION OF TH E TAIL BOOM FRAME, STARTING FROM A HI-LOCK FASTENER DRILL HOLE AND PROCEEDING AROUND THE FLANGE RADIUS AND OFF THE EDGE OF THE FRAME FLANGE UNDER THE TAILBOOM SKIN. THE MFG SUBSIDIARY WAS CONTACTED AND REPAIR SCHEME ENGINEERED AND ISSUED W ITH FORM 8110-3 AND DETAILED INSTRUCTIONS WAS APPLIED TO THE CRACKED FRAME AS A MAJOR REPAIR WITH FORM 337 SUBMITTED FOR THE WORK PERFORMED. AS TO A CAUSE, POSSIBLY THE HI-LOC DRILLED HOLE HAD NOT BEEN DEBURRED ADEQUATELY DURING MFG AND DO 1 G 7 2 3U 3 U H9EU E00054EN 2007091800112 20070918 00112 NM 2007 9 18 2007UALA03531 1 20070831 A 5330 DOUBLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 520UA 24890 FUSELAGE SKIN DOUBLER REPAIR DENTED AT UPPER LT CORNER STA 750 BETWEEN STR 15L AND 16L. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091800113 20070918 00113 NM 2007 9 18 2007UALA03532 1 20070831 A 5322 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 520UA 24890 LEFT EXTERNAL FUSELAGE, STA 1180 BETWEEN STR 27L- 28L, SHEAR TIE HAS CRACK INDICATION INBOARD AREA AT RADIUS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091800114 20070918 00114 NM 2007 9 18 2007UALA03533 1 20070831 A 5322 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 520UA 24890 RIGHT EXTERNAL FUSELAGE STA 1180, BETWEEN STR 27R- 28R, STRINGER SHEAR TIE CRACKED, AFT SIDE OF RIGHT W/W. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091800115 20070918 00115 CE 2007 9 18 CIEA200700008 1 20070830 A 3240 MS28775228 PACKING BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA BRAKE ASSY DEFORMED E CIEA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 NM 03 428P 485 BB745 AFTER LANDING AND SLOWING TO TAXI SPEED, THE FLIGHT CREW WERE UNABLE TO MAKE A RT TURN TO EXIT THE RUNWAY DUE TO THE LOS S OF BRAKING ACTION OF THE RT BRAKE. THE AIRCRAFT WAS STOPPED AND THEN REMOVED FROM THE RUNWAY USING A TOW TRACTOR. MA INTENANCE INSPECTED THE AIRCRAFT AND FOUND BRAKE FLUID LEAKING FROM THE NR 3 AND NR 4 BRAKE HOUSINGS. THE UNITS WERE DI SASSEMBLED AND THE O-RINGS WERE FOUND TO BE IN AN EGG SHAPE. THE O-RINGS WERE REPLACED WITH NEW UNITS AND THE AIRCRAFT WAS ABLE TO BE RETURNED TO SERVICE. THE O-RINGS ARE SUSPECTED TO BECOME EGG SHAPED DUE TO EXCESSIVE HEAT BUILDUP, ONE S USPECTED CAUSE IS THE FLIGHT CREWS TAXING TO THE RAMP, SETTING THE PARKING BRAKE AND LEAVING IT SET. THIS DOES NOT ALLO 1 L 7 2 4T 4 T A24CE E4EA 2007091800116 20070918 00116 NM 2007 9 18 2007UALA03534 1 20070901 A 5754 WEDGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L/E SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 RIGHT WING, 10 SLAT T/E WEDGE IS DELAM ALONG TRAILING EDGE FOR APPROX 20 INCHES. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091800118 20070918 00118 NM 2007 9 18 2007UALA03536 1 20070831 A 2560 LATCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE RAFT BIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 578UA 26694 LATCH AND CATCH FOR RAFT BIN BROKE. RAFT AND ELT REMOVED FOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091800121 20070918 00121 WP 2007 9 18 AALA20071633 1 20070827 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 505AA 49799 LGA - EMERGENCY LIGHTS AT OVERHEAD MAIN ENTRY DOOR TO SEAT ROW 3 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT S AT OVERHEAD MAIN ENTRY DOOR TO SEAT ROW 3. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007091800122 20070918 00122 WP 2007 9 18 AALA20071630 1 20070826 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 578AA 53155 LGA - EMERGENCY LIGHTS AT AFT LAVATORY CEILING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT LAVATORY CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007091800123 20070918 00123 WP 2007 9 18 AALA20071632 1 20070827 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 505AA 49799 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 6 TO 10 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEA D SEAT ROWS 6 TO 10. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007091800124 20070918 00124 WP 2007 9 18 AALA20071631 1 20070827 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 293AA 49305 LGA - EMERGENCY LIGHTS IN COCKPIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN COCKPIT. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007091300155 20070913 00155 NM 2007 9 13 SWAA074426 1 20070906 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 278WN 36441 EEPLS COVER LOOSE AT ROW 2 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007091300161 20070913 00161 NM 2007 9 13 SWAA074435 1 20070906 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091300163 20070913 00163 NM 2007 9 13 SWAA074438 1 20070906 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091300168 20070913 00168 NM 2007 9 13 SWAA074445 1 20070906 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827 STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007091300174 20070913 00174 NM 2007 9 13 SWAA074446 1 20070906 A 2560 6557463 FITTING BOEING 737 7373Q8 1384670 NM EVAC SLIDE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIR T BAR FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007091300181 20070913 00181 2007 9 13 SWAA074453 4 20070906 A 2565 D31354 SLIDE BOEING 737 7373T5 1384608 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR PER MM. 2 L 7 2 4F RT A16WE 2007091300183 20070913 00183 NM 2007 9 13 USAA920070814 1 20070905 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 459UW 25023 CTL - MAJOR REPAIR, CRACKED BULKHEAD WEB, BS 178, LBL 15, WL 234. REPAIRED BULKHEAD WEB, BS 178, LBL 15, WL 234 IAW B73 7-400 SRM 53-10-08. 2 L 7 2 4F RT A16WE 2007091300185 20070913 00185 NM 2007 9 13 CALA0700504 1 20070907 A 5314 65C385021 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND LEFT KEEL BEAM CORRODED JUST AFT OF STA 540 ON THE O/B FACE. THE CORRODED SECTION OF THE KEEL BEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-60-12. 2 L 7 2 4F RT A16WE 2007091300201 20070913 00201 EU 2007 9 13 200725309 1 20070908 A 2841 INDICATOR SAAB SF340 340B 7860101 EU FUEL QTY READS HIGH A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 902AE 340B269 DURING CRUISE CREW OBSERVED A FUEL IMBALANCE OF 200 LBS WITH THE LT WING BEING LOW. WHEN CROSS FEED WAS SELECTED THE IM BALANCED INCREASED. CREW ELECTED TO DIVERT INTO TYR. AIRCRAFT LANDED AND TAXIED TO THE GATE WITH NO FURTHER INCIDENT. VERIFIED RT WING FUEL QUANTITY WAS READING 200 LBS HIGHER THAN THE DIP STICKS ISSUED MELS. REMOVED AND REPLACED NR 6 P ROBE ON RIGHT HAND TANK. 2 L 7 2 4T RT A52EU 2007091300202 20070913 00202 EA 2007 9 13 200725307 1 20070907 A 2760 5912999 BPSU CNDAIR CL600 CL6002C10 1390015 EA SPOILERS MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 SW 21 522AE 10147 OVERSPEED WARNING CAME ON AT 230 KTS WITH GEAR AND SLATS RETRACTED AND INDICATIONS SHOWING ZERO. NO BARBER POLE RED WAR NINGS. CYCLED FLAPS ZERO TO ONE DEGREE BACK TO ZERO WITH OUT SUCCESS. LANDING WAS UNDER 67000 LBS AND WAS APPROX 100 F PM AT TOUCHDOWN. SMOOTH LANDING. REMOVED AND REPLACED RIGHT WING BRAKE POSITION SENSOR UNIT IAW AMM. 2 L 7 2 4F RT A21EA 2007091300203 20070913 00203 SO 2007 9 13 200725301 1 20070905 A 5320 14521718007 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AE 145762 DURING MBV INSPECTION, FOUND FLOOR SUPPORT ANGLE ON LEFT OMEGA BEAM JUST FORWARD OF FRAME 20 CORRODED. REMOVED AND REPL ACED FLOOR SUPPORT IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007091300204 20070913 00204 EU 2007 9 13 200725306 1 20070907 A 3260 CONNECTOR SAAB SF340 340B 7860101 EU MLG INDICATOR DISCONNECTED A SIMA O OTHER P NO WARNING INDICATION LD LANDING 1 SW 21 250AE 340B250 LANDING GEAR LEVER SELECTED DOWN, LT MAIN GEAR INDICATOR LIGHT DID NOT ILLUMINATE. AIRCRAFT DECLARED EMERGENCY PERFORME D EMERGENCY LANDING PROCEED AND LANDED WITHOUT INCIDENTS FOUND CONNECTOR 5GA/P1, DISCONNECTED RECONNECT. OPS CHECK GOOD . 2 L 7 2 4T RT A52EU 2007091300205 20070913 00205 EU 2007 9 13 200725308 1 20070908 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS DAMAGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 240DS 340B240 EMERGENCY EXIT SIGN INOP AT ROW 8A. REMOVED AND REPLACED EPS 22, 23, AND 20LN IAW MM. PERFORMED OPERATIONAL CHECK AND FOUND WORKING PROPERLY. FOUND PINS PUSHED BACK IN CONNECTOR FOR THE SIGN. REINSTALLED PINS IN CONNECTOR. 2 L 7 2 4T RT A52EU 2007091300206 20070913 00206 SO 2007 9 13 200725304 1 20070907 A 2740 3622009015 ACTUATOR EMB 145 EMB145LR 3260212 SO PITCH TRIM MALFUNCTIONED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 659AE 145762 EN ROUTE RECEIVED PITCH TRIM MAIN INOP ON EICAS CUT OUT SYSTEM. 2 L 7 2 4T RT T00011AT 2007091300207 20070913 00207 SO 2007 9 13 200725305 1 20070907 A 3320 WW5113 BULB EMB 135 EMB135LR 3260305 SO CABIN LIGHTS ODOR A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 21 725AE 145312 ELECTRICAL BURNING ODOR AT ROWS 6 AND 7A. REMOVED AND REPLACED WINDOW SIDE LIGHT BULBS IAW AMM 33-20-00, OPS CHECK OK. 2 L 7 2 4F RT T00011AT 2007091300208 20070913 00208 SO 2007 9 13 200725405 1 20070905 A 5310 14522461011 PLATE EMB 145 EMB145LR 3260212 SO FUSLEAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AE 145762 DURING MBV INSPECTION FOUND INTERSECTING PLATE BETWEEN RIGHT HAT BEAM AND FLOORBEAM 22 IS CORRODED. REMOVED AND REPLACE D PLATE IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007091300209 20070913 00209 SO 2007 9 13 200725401 1 20070910 A 4990 OIL SYSTEM EMB 135 EMB135KL 3260302 SO APU LEAKING A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 856AE 145748 OIL ODOR WITH BLEEDS ON. FOUND APU LEAKING OIL AND PLACED THE APU ON MEL. 2 L 7 2 4F RT T00011AT 2007091300210 20070913 00210 SO 2007 9 13 200725402 1 20070905 A 5315 14000492403 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AE 145762 UPPER FLOORBEAM AT FRAME 23 CORRODED DURING MBV FOUND UPPER FLOORBEAM AT FRAME 23 CORRODED. REMOVED FLOORBEAM AND INSTA LLED NEW FLOORBEAM. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007091300211 20070913 00211 SO 2007 9 13 200725404 1 20070905 A 5315 14521721009 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AE 145762 DURING MBV INSPECTION, FOUND DIGITAL BEAM CORRODED AT FRAME 17. REPAIRED BEAM, A/C RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007091300212 20070913 00212 SO 2007 9 13 200725403 1 20070905 A 5320 14590070004 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AE 145762 DURING MBV INSPECTION, FOUND FORWARD SERVICE DOOR SILL BETWEEN FRAMES 17-20 CORRODED. REPAIRED SILL. AIRCRAFT WAS RETU RNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007091300213 20070913 00213 SO 2007 9 13 LR7A07066 1 20070801 A 5330 37525635 SKIN LKHEED 382 382G 526414U SO FS 787E DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 578 4606 DURING SCHEDULED B-1 CHECK BELLY SKIN FS787E TO 799E, BL20L TO 20R DAMAGED WITH TEMPORARY REPAIR. SKIN REPLACED IAW SMP 583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007091300214 20070913 00214 SO 2007 9 13 LR7A07067 1 20070801 A 5315 3759749 FLOORBEAM LKHEED 382 382G 526414U SO FS 797E BROKEN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 578 4606 DURING SCHEDULED B-1 CHECK PER HB5301, FOUND FLOORBEAM LOWER CAP BROKEN, FS 797E, LBL20-RBL20, WL132. LOWER CAP REPLACE D IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007091300215 20070913 00215 SO 2007 9 13 LR7A07068 1 20070801 A 5320 ANGLE LKHEED 382 382G 526414U SO BS 516 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 578 4606 DURING SCHEDULED B-1 CHECK PER HB5301, FOUND RT MAIN WHEEL WELL CHINE ANGLE CRACKED, FS 516, WL145, RBL62. REPAIR CARRI ED OUT IAW SMP583 FIG 53-40-27. 2 H 7 4 4T A1SO 2007091300216 20070913 00216 SO 2007 9 13 SIMA200725005 1 20070904 A 2910 211118 SHUTTLE VALVE EMB 145 EMB145LR 3260212 SO ZONE 200 FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 694AE 7246 14500869 HYDRAULIC SYSTEM ONE FAILURE MESSAGE, CFR CALLED. RETURNED TO DFW. REMOVED AND REPLACED NUMBER FOUR BRAKE SHUTTLE VALV E AND TIGHTENED RESERVOIR REFILL CHECK VALVE AND LINE IAW EMB AMM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVIC E. 2 L 7 2 4T RT T00011AT 2007091300231 20070913 00231 NM 2007 9 13 CALA0700510 1 20070904 A 5311 6546539 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17326 23456 INSPECTION FOUND A 1.2 INCH CRACK IN LOWER SECTION OF LEFT FRAME INNER CHORD AT STA 616, S17L TO S18L. THE FRAME CHORD WAS REPAIRED IAW ECRA 5311-01158. 2 L 7 2 4F RT A16WE 2007091300234 20070913 00234 WP 2007 9 13 MWEA070208 1 20070908 A 5730 59305035 SKIN DOUG DC9 DC981 3022081 WP WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 CENTER WING SKIN AND STRINGER HAS CORROSION, 17 XCW, INDICATOR NOTED AT LOWER AFT 9 FOOT SKIN PANEL 53 INCHES FROM CENTE R FASTENERS ROW 3. REMOVED CORROSION, FABRICATED AND INSTALLED FASTENERS. 2 L 7 2 4F A6WE 2007091300237 20070913 00237 SO 2007 9 13 LR7A07070 1 20070801 A 5742 3308216 FITTING LKHEED 382 382G 526414U SO NR 1 ENGINE DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 578 4606 DURING SCHEDULED B-1 CHECK, FOUND NR 1 ENGINE OUTBD TRUSS MOUNT RIB CAP ATTACH FITTINGS BOLT HOLES DIAMETER MEASUREMENTS OUT OF LIMITS. FITTING INBD-OUTBD REPLACED IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2007091300238 20070913 00238 SO 2007 9 13 SIMA200725301 1 20070905 A 5320 14521718007 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AE 145762 DURING MBV INSPECTION, FOUND FLOOR SUPPORT ANGLE ON LEFT OMEGA BEAM JUST FORWARD OF FRAME 20 CORRODED. REMOVED AND REPL ACED FLOOR SUPPORT IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007091300239 20070913 00239 SO 2007 9 13 SIMA200725302 1 20070907 A 5610 SEAL EMB 145 EMB145LR 3260212 SO COCKPIT WINDOW FAILED A SIMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 21 625AE 145115 AFTER TAKEOFF CAPTS COCKPIT WINDOW SEAL BLEW OUT IN FLIGHT. 2 L 7 2 4T RT T00011AT 2007091300240 20070913 00240 SO 2007 9 13 SIMA200725304 1 20070907 A 2740 3622009015 ACTUATOR EMB 145 EMB145LR 3260212 SO PITCH TRIM FAILED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 659AE 145762 EN ROUTE RECEIVED PTRIM MAIN INOP ON EICAS CUT OUT SYSTEM. 2 L 7 2 4T RT T00011AT 2007091300241 20070913 00241 SO 2007 9 13 SIMA200725305 1 20070907 A 3320 WW5113 BULB EMB 135 EMB135LR 3260305 SO CABIN LIGHTS ODOR A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 21 725AE 145312 ELECTRICAL BURNING SMELL AT ROWS 6 AND 7A. REMOVED AND REPLACED WINDOW SIDE LIGHT BULBS IAW AMM 33-20-00. OPS CHECK OK . AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007091300242 20070913 00242 EU 2007 9 13 DHL2007363500 1 20070908 A 5420 GUSSET AIRBUS 300 A300B4203 3930306 EU ZONE 400 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 NR 2 ENG PYLON AT COWL HINGE FITTING O/B SIDE HAS A CRACK APPROX 3/4" ABOVE T BRACKET AT RIB 4. REMOVED AN REPLACED GUS SET HINGE FITTING AN T BRACKET AT NR 2 ENG PYLON O/B SIDE RIB 4 IAW A300 SRM 51-30-30 AN A300 SB A300-54-068. 2 L 7 2 4F RT A35EU 2007091300258 20070913 00258 NM 2007 9 13 SWAA074464 1 20070907 A 5330 6545767 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT CRACKED BS 450, BL 0. REPAIRE D SKIN PER EA. 2 L 7 2 4F RT A16WE 2007091300259 20070913 00259 NM 2007 9 13 SWAA074472 1 20070907 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 376.5, STR 8L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007091400001 20070914 00001 SO 2007 9 14 SIMA200725605 1 20070911 A 3150 WARNING MESSAGE EMB 135 EMB135KL 3260302 SO COCKPIT ILLUMINATED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 840AE 145656 ABORTED T/O DUE TO ENG 1 BLEED VALVE FAIL MESSAGE. ISSUED MEL 36-01 BY CMTX. 2 L 7 2 4F RT T00011AT 2007091400006 20070914 00006 NM 2007 9 14 AWXA200701095 1 20070830 A 5340 146N876924 ATTACH FITTING BOEING 757 7572S7 1384962 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 MCN - MAJOR REPAIR - C-11 CHECK - NR 5988878, CORROSION ON THE L4 DOOR CUT LOWER SILL ATTACH CHANNEL CLIP, BS 1640, S17L , WL 208. REPLACED THE L4 DOOR CUT LOWER SILL ATTACH CHANNEL CLIP, BS 1640, S17L, WL 208 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007091400034 20070914 00034 EU 2007 9 14 SIMA200725607 1 20070909 A 5347 7253799457 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 211NE 22399 340B211 DURING A HMBV INSPECTION CORROSION WAS FOUND ON THE CARGO SECTION OF THE SEAT TRACK AT B/L. 0.0. REPLACED THE SECTION O F CORRODED SEAT TRACK USING PART NUMBER 7253799-457 IAW SAAB SRM 53-70-60 PARA 3. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007091400035 20070914 00035 SO 2007 9 14 SIMA200725608 1 20070901 A 5311 7253721493 FRAME EMB 135 EMB135KL 3260302 SO BS 258 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 838AE 18475 145651 DURING A HMBV INSPECTION, THE GALLEY FLOOR FRAME AT STA 258 WAS FOUND CORRODED. REPAIRED CORRODED AREA IAW SAAB SRM 53- 70-30 AND SRM 51-40-21. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007091400038 20070914 00038 EU 2007 9 14 F3LA200700221 1 20070909 A 3350 32143031 BATTERY AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHTS FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 909FR 1761 DURING C4/S1 CHECK, INSPECTION REPORTED "TEST EMERG LIGHT BAT" BATTERY CAPACITY CHECK FAILED. REMOVED AND REPLACED EMER GENCY EXIT BATTERIES IAW AMM 33-51-38-PB401. OPERATIONAL CHECK GOOD IAW 33-51-00-710-001, (S/N'S 26827, 24286, 26936, 0 42015). 2 L 7 2 4F RT A28NM 2007091400044 20070914 00044 SO 2007 9 14 SIMA200725404 1 20070905 A 5315 14521721009 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AE 145762 DURING MBV INSPECTION, FOUND DIGITAL BEAM CORRODED AT FRAME 17. REPAIRED BEAM. A/C RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007091400046 20070914 00046 NM 2007 9 14 07FDEA03512 1 20070910 A 5710 DUCT DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 588FE 48490 LEFT WING, LEADING EDGE TELESCOPING DUCT CUTOUT I/B AND O/B CORNERS FOUND CRACKS. 10-01-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-115191. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007091400050 20070914 00050 EU 2007 9 14 07FDEA03519 1 20070911 A 5320 A53610694204 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 DAMAGED FITTING AT FRAME 13, STRG 26 LHS. REPAIR PERFORMED BY REPLACEMENT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091400051 20070914 00051 EU 2007 9 14 07FDEA03520 1 20070911 A 5311 A53610318369 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 DAMAGED FRAME 12A LT (BENT PARTITIONS, IMPACTS AT RIVET HOLES, OVERSIZED HOLES), STRG 24-27. REPAIR PERFORMED BY REPLAC EMENT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091400057 20070914 00057 EU 2007 9 14 07FDEA03533 1 20070911 A 5330 A53772018202 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 FOUND DENT BETWEEN FRAME 19-20, STRG 36 LT, BELOW THE BUTT JOINT STRG 35. REPAIR PERFORMED BY CUT OUT AND INSTALLING EX TERNAL DOUBLER FOLLOWING SRM 53-10-12/FIG 224/SH 2, APPROVED BY EA 6-5313-95878 AND RAS/DABRE/7006162/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091400061 20070914 00061 EU 2007 9 14 07FDEA03452 1 20070907 A 5313 A53974267 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 CORROSION ON STRINGER 56 LT AND RT BETWEEN C55/58-61, OUT OF LIMIT AS PER SRM 53-10-00. STRINGER SPLICE REPAIR PERFORME D IAW SRM 53-10-14/FIG 201A. 2 L 7 2 4F RT A35EU 2007091400076 20070914 00076 EU 2007 9 14 07FDEA03467 1 20070824 A 5347 R53070088204 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 AFT MDCC - SEAT TRACK Y0 WITH CORROSION OUT OF VALUES BETWEEN FR74 AND FR75. SEAT TRACK REPAIRED IN ACCORDANCE WITH SRM SUPP 53-10-16 FIG 202 BETWEEN FR 72 AND FR 73. 2 L 7 2 4F RT A35EU 2007091400082 20070914 00082 EU 2007 9 14 F3LA200700219 1 20070907 A 3150 WARNING LIGHT AIRBUS A319 A319112 3930323 EU FALSE ACTIVATION A F3LA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 915FR 1851 AIR TURN BACK AT 1244, FLIGHT CREW REPORTED VENT EXTRACT FAULT. AIRCRAFT RETURNED TO KMDW AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND PERFORMED OPS SYSTEM TEST VIA MCDU. NO DISCREPANCIES NOTED. AIRCRAFT OKAY FOR SERV ICE IAW AMM 21-26-00-710-050. 2 L 7 2 4F RT A28NM 2007091400083 20070914 00083 EU 2007 9 14 DHL2007367510 1 20070820 A 5754 WEB AIRBUS 300 A300B4203 3930306 EU LT SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 367DH 265 LT SLAT FOLDING NOSE HAS WEB CRACK BY O/B MOUNT. REMOVED L/W SLAT FOLDING NOSE. OPS AND ADJUSTMENT TEST PERFORMED. NO DEFECTS NOTED IAW A300 MM 27-81-34 AN 27-81-33. 2 L 7 2 4F RT A35EU 2007091400085 20070914 00085 SO 2007 9 14 SIMA200725405 1 20070905 A 5320 14522461011 PLATE EMB 145 EMB145LR 3260212 SO CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AE 145762 DURING MBV INSPECTION, FOUND INTERSECTING PLATE BETWEEN RIGHT HAT BEAM AND FLOORBEAM 22 IS CORRODED. REMOVED AND REPLAC ED PLATE IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007091400091 20070914 00091 EU 2007 9 14 AWXA200701071 1 20070823 A 5554 D5537131800000 FITTING AIRBUS 320 A320232 3930326 EU ZONE 300 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-7 CHECK - NR 5980023, RUDDER HINGE NR 2 HAS PLAY, VERTICAL STABILIZER STATION 1926/RIB 4. REPLAC ED RUDDER HINGE NR 2, VERTICAL STABILIZER STATION 1926/RIB 4 IAW A320 AMM 27-21-00. 2 L 7 2 4F RT A28NM 2007091400092 20070914 00092 EU 2007 9 14 AWXA200701072 1 20070823 A 5554 D5537131800000 FITTING AIRBUS 320 A320232 3930326 EU ZONE 300 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 648AW 770 SAL - MAJOR REPAIR - C-7 CHECK - RUDDER HINGE NR 5 HAS PLAY, VERTICAL STABILIZER STATION 2985/RIB 7. REPLACED RUDDER HI NGE NR 5, VERTICAL STABILIZER STATION 2985/RIB 7 IAW A320 AMM 27-21-00. 2 L 7 2 4F RT A28NM 2007091400093 20070914 00093 NM 2007 9 14 AWXA200701073 1 20070906 A 5720 6545402153 STIFFENER BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 PHX - MAJOR REPAIR - NR 4118486, CRACKED CENTER WING REAR SPAR VERTICAL STIFFENER, BS 540, RBL 6, WL 158. REPAIRED CENT ER WING REAR SPAR VERTICAL STIFFENER, BS 540, RBL 6, WL 158 IAW AWA ER 03-5712-06054-BA1. 2 L 7 2 4F RT A16WE 2007091400095 20070914 00095 EU 2007 9 14 AWXA200701076 1 20070907 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHTS FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 628AW 56170 7694 67 PHX - EEL - LOG 4121217 - EMERGENCY EXIT LIGHT TEST FAILED. MX REPLACED THE LT EPSU. OPERATIONAL TEST WAS GOOD. 2 L 7 2 4F RT A28NM 2007091400102 20070914 00102 EU 2007 9 14 F3LA200700224 1 20070830 A 5320 D5347112420000 SHEAR PLATE AIRBUS A319 A319112 3930323 EU CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED SURFACE CORROSION AT AFT END OF LT SHEAR PLATE BETWEEN FR69 AND FR70. REMOVED A ND REPLACED SHEAR PLATE BETWEEN FR69 AND FR70 IAW SRM 51-72-11 AND 51-42-11. 2 L 7 2 4F RT A28NM 2007091400105 20070914 00105 NM 2007 9 14 DL76L071152 1 20070829 A 2611 SMOKE DETECTOR BOEING 767 767332 1382001 NM CABIN FALSE ACTIVATION A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 198DN 28455 AFTER T/O, HAD 3 SMOKE DETECTORS GO OFF HAD HAZE AND ODOR IN CABIN. RETURNING TO BHM FOR REPAIRS. RAN RT ENGINE AT IDL E FOR 20 MIN, THEN TO T/O POWER. NO SIGN SMOKE OR HAZE. RAN LT ENG TO T/O WITH NO SIGN OF SMOKE ALSO INST LT/RT ISOL V LV FOR SIGN OF OIL. NTF INSP RT ENG PRV FOR OIL. NTF. 2 L 7 2 4F RT A1NM 2007091400106 20070914 00106 NM 2007 9 14 DL76L071153 1 20070829 A 7930 791701426 TRANSMITTER BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE INACCURATE A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 188DN 27583 723843 AFTER STARTING RT ENG THE OIL QTY DROPPED TO 6QTS, AFTER ABOUT 10 MIN OF IDLE QTY WENT TO 7 AND CYCLED BACK AND FORTH TO 8 QTY WENT TO 9 QTS APPROCHING THE GATE. INSP ENG NO LEAKS NOTED VERIFIED OIL TANK IS FULL FWD RT IND TO MCO AND PLAC PER MEL 79-31-0. REPLACED OIL QUANTITY XMTR TESTED PER M/M CHECKS GOOD, REMOVE MCO AND PLACARD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007091400109 20070914 00109 2007 9 14 DL757071156 4 20070830 A 2330 RDAV2132 VIDEO MONITOR BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 665DN 25013 DURING PREFLIGHT, ELECTRICAL ODOR IN FIRST CLASS CABIN. FOUND FIRST CLASS RETRACTABLE VIDEO MONITOR BURNT UP. REMOVED MONITOR PER ERA AND FWD TO MCO/PLACARD. INSTALLED FWD VIDEO MONT. OPS CK GOOD. 2 L 7 2 4F RT A2NM 2007091400116 20070914 00116 EU 2007 9 14 F3LA200700223 1 20070903 A 5315 D5347217220290 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED LT FLOORBEAM Y1292 CORRODED ON BOTTOM OF NUTPLATE HOLE AT FR66. FLOORBEAM FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14, PAGE 106. REMOVED AND REPLACED DAMAGED FLOORBEAM Y1292 SECTION FROM FR64 TO FR66 IAW 51-42-11. 2 L 7 2 4F RT A28NM 2007091400122 20070914 00122 EU 2007 9 14 F3LA200700229 1 20070908 A 5730 D5725130000200 ACCESS PANEL AIRBUS A319 A319112 3930323 EU RT WING CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON FUEL PANEL 640JB ATTACHMENT HOLES. REMOVED AND REPLACED FUEL PANEL 640JB ON RT WING IAW AMM 57-27-11-400-002. PERFORMED LEAK CHECK IAW 57-27-11-400-002, NO LEAKS FOUND. 2 L 7 2 4F RT A28NM 2007091400128 20070914 00128 NM 2007 9 14 DL75E071170 1 20070903 A 3411 PROBE BOEING 757 7572Q8 1384972 NM PITOT STATIC INOPERATIVE A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 703TW 27620 AFTER ENGINE START F/O PITOT EICAS MESSAGE WILL NOT EXTINGUISH. F/O PITOT PROBE REPLACED PER M/M. 2 L 7 2 4F RT A2NM 2007091400136 20070914 00136 EU 2007 9 14 07FDEA03479 1 20070910 A 5330 A53610320201 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 FOUND TWO MISDRILLED HOLES AT CIRCUMFERENTIAL LAP JOINT, FRAME 13, STRG 9 LT. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLING BUSHES IAW EA 6-5312-95874 AND RAS/AS/0012/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007091400137 20070914 00137 EU 2007 9 14 07FDEA03480 1 20070910 A 5730 A57340087 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND ELONGATED HOLES ON BOTTOM SKIN LT OUTER WING RIB 8 REPAIR PERFORMED IAW R571-50532 (REAM UP AND BUSHING INSTALLATI ON), APPROVED BY EA 6-5720-106531 AND RAS/BAE/1005033/2007 ISS A. 2 L 7 2 4F RT A35EU 2007091400145 20070914 00145 EU 2007 9 14 07FDEA03489 1 20070910 A 5310 A53989317206 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 HEAVY CORROSION ON LOWER T-SECTION AT FRAME 92 BETWEEN STRG 21 LT TO STRG 21 RT. REPAIR PERFORMED CUT OUT T-SECTION AND INSTALLING NEW PORTION OF T-SECTION AND A REPAIR ANGLE IAW EA 6-5319-95861 AND RAS/DAHAM/4020299/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091400147 20070914 00147 EU 2007 9 14 07FDEA03374 1 20070905 A 5311 A53810967000 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 FOUND ON DIAPHRAGM FRAME 47-54 AT BEAM 4-5 LT AND RT NICKS AND IMPACT DAMAGES. REPAIR PERFORMED BY SMOOTH REWORK OF DAM AGED AREA ON BEAM 4-5 LT IAW EA 6-5315-95840 AND RAS 041406/011/2005 ISSUE A AND CUT OUT THE DIAPHRAGM AND INSTALLING A REPAIR SPLICE ON BEAM 4-5 RT IAW EA 6-5315-95841 RAS 041427/006/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091400148 20070914 00148 EU 2007 9 14 07FDEA03375 1 20070905 A 5310 A53973100200 BEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 CORROSION ON BEAM NR 10, FRAME 67-69, STRG 45-47 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091400149 20070914 00149 EU 2007 9 14 07FDEA03376 1 20070905 A 5320 A53981959200 SUPPORT AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 FOUND CRACKED SUPPORT BETWEEN FRAME 79-80, STRG 28 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091400158 20070914 00158 EU 2007 9 14 07FDEA03495 1 20070910 A 5210 A52110502206 GUSSET AIRBUS 300 A300B4622R 3930312 EU ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 FOUND CRACKED GUSSET ON FWD PAX DOOR LT (DOOR ZONE 831) AT FWD LOWER CORNER. REPAIR PERFORMED BY REPLACEMENT OF GUSSET IAW SRM 52-11-00-C1. 2 L 7 2 4F RT A35EU 2007091400163 20070914 00163 EU 2007 9 14 07FDEA03500 1 20070910 A 5313 A53773455286 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 CORROSION ON STRINGER 44 LT BETWEEN FRAME 16A-17. STRINGER REPAIR PERFORMED IAW SRM 53-12-14 / FIG 201. 2 L 7 2 4F RT A35EU 2007091400164 20070914 00164 EU 2007 9 14 07FDEA03501 1 20070910 A 5313 A53974321000 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 HEAVY CORROSION ON FITTING AT FRAME 63 LT, STRG 43-46. REPLACED FITTING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091400168 20070914 00168 NM 2007 9 14 NWAA072976313 1 20070901 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 673US 30268 DURING OVERNIGHT CHECK, FOUND UPPER DECK LEFT FRONT EMERGENCY EXIT SIGN INOP AT DOOR FRAME. MAINTENANCE REMOVED AND REP LACED POWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007091400172 20070914 00172 EU 2007 9 14 07FDEA03383 1 20070905 A 5320 A53611534200 WEB AIRBUS 300 A300B4622R 3930312 EU ZONE 200 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 FOUND OLD REPAIR AT WEB ON FLOOR STRUCTURE FRAME 14A-14B, Y0, NOT CONFORM TO SRM (SPLICE MATERIAL). REPAIR RENEWED IAW SRM 53-12-15/FIG 207. 2 L 7 2 4F RT A35EU 2007091400180 20070914 00180 WP 2007 9 14 07FDEA03506 1 20070910 A 5347 WSP0413509 SEAT TRACK DOUG DC10 DC1010F 3022111 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 SEAT TRACK BALLMAT AREA CRACK ON SEAT TRACK. REPAIREED AREA IAW SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F A22WE 2007091400198 20070914 00198 EA 2007 9 14 SWIA200718667 1 20070908 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER TO TAKEOFF 1 NM 07 869AS 7479 FLT 3836 - ON TAKEOFF, CAPTAIN'S FORWARD WINDSHIELD CRACKED. REPLACED LEFT WINDSHIELD IAW AMM 56-11-01, PN NPN-139321-1 3, SN OFF 00301H2214. 2 L 7 2 4F RT A21EA 2007091700015 20070917 00015 WP 2007 9 17 I5HA0758012 1 20070912 A 2913 66WA4001 PUMP CVAC 580 580 2422806 WP ALLSN 501D 501D13 03004 GL HYDRAULIC SYS CRACKED A I5HA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 585P DURING DEPARTURE, ENROUTE, THE CREW LOST HYDRAULIC PRESSURE AND RETURNED TO DEPARTURE. THE AIRCRAFT LANDED UNEVENTFULLY AND WAS TOWED TO A PARKING SPACE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE ENGINE DRIVEN HYDRAULIC PUMP HAD FAIL ED AND PUMPED ALL THE HYDRAULIC FLUID OVERBOARD. MAINTENANCE REMOVED THE DEFECTIVE PUMP, REPLACED THE FILTERS, PURGED T HE HYDRAULIC SYSTEM, AND IS WAITING FOR A REPLACEMENT PUMP TO ARRIVE. REPLACEMENT PART ARRIVED AND WAS INSTALLED BY MAI NTENANCE. THE HYDRAULIC SYSTEMS WAS BLED AND SERVICED AND THE AIRCRAFT WAS RETURNED TO SERVICE ON 14 SEPT 2007. 2 L 7 2 4T 4 T RT E282 2007091700031 20070917 00031 NM 2007 9 17 TAMF20070037S 1 20070827 A 5320 STRAP BOEING 767 767200 1385120 NM GE CF6 CF680 30025 NE BS 1351 CORRODED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 768QT 23803 DURING INSPECTION OF (C2) CHECK WAS FOUND A CORROSION ON CARGO DOOR SURROUND STRUCTURE, SAFE FAIL STRAP P/N 146T8048-3. REMOVED, FABRICATED AND INSTALLED A NEW FAIL SAFE STRAP P/N 146T8048-3 IAW EWO 767-53-057 AND SERVICE REQUEST 1-5572925 75. THIS REPAIR CONSTITUTES A MAJOR REPAIR, FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007091700037 20070917 00037 NM 2007 9 17 TAMF20070024S 1 20070828 A 5711 SPAR BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE WING DAMAGED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 768QT 23803 DURING C CHECK INSPECTION (TASK CARD 57-650-00) WAS FOUND LOOSE MATERIAL ON SPLICE PLATE AT FRONT SPAR STA ISS 864.92 8 73.13 RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-028 AND SERVICE REQUEST 1-527347746. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007091700058 20070917 00058 NM 2007 9 17 TAMF20070025S 1 20070827 A 5711 SPAR BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE LT WING DAMAGED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 768QT 23803 DURING C CHECK INSPECTION (TASK CARD 06-102-01-1) WAS FOUND A LOOSE MATERIAL ON SPLICE PLATE AT FRONT SPAR STA ISS 1009 - 1017 LT. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-027 AND SERVICE REQUEST 1-526643882. THIS REPAIR IS CONSIDERED A MA JOR REPAIR. FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007091800012 20070918 00012 2007 9 18 UPS07M50605 4 20070902 A 2565 LIGHT DOUG MD11 MD11F 3023600 NM R1 ENTRY DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 271UP 48572 INSPECTION TYPE:N/A R1 MAIN ENTRY DOOR SLIDE REMOTE PRESS IND TEST INOP. RELAMPED AND CHECKED NORMAL. 2 L 7 3 4F RT A22WE 2007091800016 20070918 00016 NM 2007 9 18 KCSA071330 1 20070906 A 3350 S1686B LIGHT BOEING 747 747209B 138489B NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 715CK 22447 UPPER DECK EMERGENCY LIGHT AT STA 610 OVERHEAD IS INOP. 2 L 7 4 4F RT A20WE 2007091800019 20070918 00019 EA 2007 9 18 COMA0770046 1 20070828 A 3350 6100976 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 379CA 10102 FLIGHT 5273 - EMERGENCY LIGHT AT ROW 13 INOP. RELAMPED EMERGENCY FLOOD LIGHT. 2 L 7 2 4F RT A21EA 2007091800027 20070918 00027 SO 2007 9 18 C2XA07IA193 1 20070902 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16951 145063 IAH - DURING MAINTENANCE INSPECTION, THE LEFT HAND EXIT HATCH AFT EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCR AFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007091800033 20070918 00033 NM 2007 9 18 UPS07550618 1 20070906 A 3350 LIGHT BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 453UP 25474 INSPECTION TYPE:N/A EMERGENCY LIGHTS -UNARMED- LIGHT ASSY BROKEN/INOP. REMOVED AND REPLACED EMERGENCY LIGHTS -UNARMED- LIGHT ASSY, OPS CHECKS NORMAL IAW AMM 33-50-10-00. 2 L 7 2 4F RT A2NM 2007091800041 20070918 00041 EA 2007 9 18 TRAX200701299 1 20070904 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 875AS 7559 AAR - CLIP CRACKED AT FS 484, RBL 27 OUTBOARD. 2 L 7 2 4F RT A21EA 2007091800059 20070918 00059 NM 2007 9 18 2007UALA03195 1 20070815 A 3397 794640 CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 ESCAPE PATH LIGHTING NEAR 14 A-B INOP. *S/D* RECONNECTED ESCAPE PATH LIGHTING AT 14 A, B. 2 L 7 2 4F 4 F RT A1NM E24NE 2007091800065 20070918 00065 NM 2007 9 18 2007UALA03507 1 20070901 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FWD CLOSET FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 849UA 1649 FWD CLOSET EMERGENCY LIGHT IS FAULTY. REPLACED FWD CLOSET EMERGENCY LIGHT ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007091800074 20070918 00074 NM 2007 9 18 2007UALA03510 1 20070901 A 5414 PANEL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 PYLON DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 849UA 1649 PANEL ON NR 2 PYLON IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER/FILLER REPAIR ON PANEL 424CR. INSTALLED PANEL ONTO NR 2 PYLON. 2 L 7 2 4F 4 F RT A28NM E40NE 2007091800078 20070918 00078 2007 9 18 2007UALA03512 4 20070902 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 428UA 523 DOOR 1L EMERGENCY SLIDE FAILS EMERGENCY LIGHT TEST. REPLACED DOOR 1L SLIDE PACK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007091800098 20070918 00098 NM 2007 9 18 2007UALA03524 1 20070831 A 5522 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RT ELEVATOR PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 RT ELEV SN 085, UPPER SURFACE HAS AREA OF POTTED PUNCTURE 29 INCHES FROM O/B EDGE AND 4 INCHES FROM T/E. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800120 20070918 00120 NM 2007 9 18 2007UALA03538 1 20070904 A 3150 WARNING SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 367UA 24536 CREW REPORT: PASSING 7000 FT AT CLIMB THRUST T/O WARNING HORN SOUNDED FOR 20 SECONDS. CABIN CLIMBING NORMAL, LANDING G EAR HANDLE OFF POSITION. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800133 20070918 00133 EU 2007 9 18 2007UALA03540 1 20070904 A 7830 THRUST REVERSER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 419UA 487 V10292 NR 2 T/R SLEEVE DAMAGED DUE TO CONTACT WITH FUELING TRUCK. REVERSER REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007091800134 20070918 00134 NM 2007 9 18 AALA20071626 1 20070825 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 362AA 24043 MIA - EMERGENCY LIGHT AT SEAT 3B OVERHEAD INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 3B. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007091800135 20070918 00135 NM 2007 9 18 AALA20071636 1 20070828 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 352AA 24033 JFK - EMERGENCY LIGHT AT SEATS 20AB INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEATS 20AB. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007091800136 20070918 00136 NM 2007 9 18 AALA20071635 1 20070828 A 3350 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 640A 24598 MIA - EMERGENCY LIGHT AT SEAT 3E INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 3E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007091800137 20070918 00137 WP 2007 9 18 AALA20071634 1 20070827 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 570AA 49352 ATL - EMERGENCY LIGHTS IN COCKPIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN COCKPIT. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007091800138 20070918 00138 WP 2007 9 18 AALA20071625 1 20070825 A 3350 LENS DOUG DC9 DC983 3022083 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 966TW 53616 DFW - EMERGENCY LIGHT AT AFT LEFT OVERWING EXIT SIGN HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT AFT LEFT OVE RWING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007091800139 20070918 00139 NM 2007 9 18 AALA20071638 1 20070828 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 640A 24598 MIA - EMERGENCY LIGHTS AT FORWARD TO MID COACH INOPERATIVE. REPLACED BATTERY PACK AT RIGHT NUBMER TWO DOOR FOR EMERGENC Y LIGHTS AT FORWARD TO MID COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007091800140 20070918 00140 NM 2007 9 18 AALA20071637 1 20070828 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 640A 24598 MIA - EMERGENCY LIGHTS AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007091800141 20070918 00141 NM 2007 9 18 AALA20071618 1 20070825 A 3397 GROUND WIRE BOEING 767 767323 1385205 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 373AA 25200 ORD - EMERGENCY LIGHTS AT RIGHT SIDE OF FIRST CLASS INOPERATIVE. SECURED TWO LOOSE GROUND WIRES GD90000DC AND GD900015 FOR EMERGENCY LIGHTS AT RIGHT SIDE OF FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007091800142 20070918 00142 NM 2007 9 18 AALA20071616 1 20070825 A 2750 FLAP SYSTEM BOEING 737 737823 13844BZ NM INOPERATIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 926AN 29527 MIA INFLIGHT T2104/25AUG - AIRCRAFT DID A FLY BY PRIOR TO LANDING AT MIA DUE TO FLAPS WOULD NOT EXTEND. TOWER CONFIRMED FLAPS WERE NOT EXTENDED. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. UNABLE TO DUPLICATE ON GROUND. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007091800143 20070918 00143 NM 2007 9 18 AALA20071617 1 20070825 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 378AN 25447 MIA - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 10GH INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROW 10G H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007091800144 20070918 00144 NM 2007 9 18 2007UALA03541 1 20070904 A 2780 SLAT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU WING MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 328UA 24148 SPLIT FLAP INDICATION BETWEEN POSITION 10-15. ON GO AROUND FLAPS OK WITHOUT MOVING HANDLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800145 20070918 00145 NM 2007 9 18 2007UALA03542 1 20070904 A 2612 FIRE LOOP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU APU FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 328UA 24148 APU DETECTOR INOP LIGHT ILLUMINATED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800146 20070918 00146 WP 2007 9 18 AALA20071624 1 20070825 A 3350 SHROUD DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 966TW 53616 DFW - EMERGENCY LIGHT AT SEAT 16D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007091800147 20070918 00147 WP 2007 9 18 AALA20071623 1 20070825 A 3350 SHROUD DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 966TW 53616 DFW - EMERGENCY LIGHT AT SEAT 9D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007091800148 20070918 00148 NM 2007 9 18 AALA20071615 1 20070825 A 3230 MODULE BOEING 737 737823 13844BZ NM MLG INOPERATIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 920AN 29521 DFW INFLIGHT T1767/25AUG - WITH LANDING GEAR SELECTED DOWN, ALL SIX RED AND GREEN LIGHTS ILLUMINATED. THE RED LIGHTS W OULD NOT EXTINGUISH ON THE FORWARD INSTRUMENT PANEL. OVERHEAD PANEL GEAR INDICATOR NORMAL. LANDED DFW WITHOUT INCIDENT . REPLACED LANDING GEAR CONTROL MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007091800149 20070918 00149 WP 2007 9 18 AALA20071622 1 20070825 A 3350 LENS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 966TW 53616 DFW - EMERGENCY LIGHT AT SEAT 9D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A6WE 2007091800150 20070918 00150 NM 2007 9 18 HALA0700377 1 20070912 A 3150 WARNING LIGHT BOEING 767 767332 1382001 NM APU ILLUMINATED A HALA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 598HA 23278 ETOPS SIGNIFICANT SYSTEM "APU FAULT" UPON APU START UP AFTER LANDING. ACCOMP EICAS ERASE PROCEDURES PER AMM31-40-00. 2 L 7 2 4F RT A1NM 2007091800151 20070918 00151 NM 2007 9 18 HALA0700375 1 20070912 A 2612 233T42464 CONTROL PANEL BOEING 767 767332 1382001 NM CARGO FIRE MALFUNCTIONED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 597HA 915 915 23277 SQUIB TEST FOR CARGO 1 TEST ONE DOES NOT ILLUMINATE CARGO 1 LIGHT TEST TWO OK. FOUND SQUIB TEST FOR CARGO 1 TEST ONE IN TERMITTENT. REMOVED AND REPLACED SQUIB TEST CONTROL PANEL ASSY. OPERATIONAL CHECK OK PER 767 AMM 26-23-00. 2 L 7 2 4F RT A1NM 2007091800152 20070918 00152 NM 2007 9 18 HALA0700376 1 20070912 A 3350 BPS73 BATTERY PACK BOEING 767 767332 1382001 NM EMERGENCY LIGHTS INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 598HA 23278 DURING OVERNIGHT CHECK FOUND RIGHT OVERHEAD EMERGENCY LIGHTS ROWS 1 THRU 18 INOP. T/S 50 PWR SUPPLY CCN 3302190. REPLA CED BATTERY POWER SUPPLY OPS CK OK PER AMM33-51-00. 2 L 7 2 4F RT A1NM 2007091800153 20070918 00153 NE 2007 9 18 HALA0700374 2 20070911 A 7200 BR700715A130 ENGINE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE RIGHT FAILED A HALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 13 477HA 55122 13218 ATO - RT ENGINE FAILED 110 KNOTS ON TAKEOFF. FOUND RT ENGINE BLOWN. REMOVED RT ENGINE ASSY PER AMM144. OPS CHECK AND L EAK CHECK GOOD. OK FOR SERVICE. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007091800154 20070918 00154 EU 2007 9 18 07FDEA03682 1 20070913 A 5753 A57970372200 SKIN AIRBUS 310 A310203 3930313 EU ZONE 500 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND ON LT INBOARD FLAP LOWER SKIN AT TRAILING EDGE, RIB 3-4, DELAMINATION. IN THIS AREA FOUND ON UPPER SKIN AN OLD D OUBLER INSTALLED. REPAIR PERFORMED BY REMOVAL OF THE OLD REPAIR ON UPPER SKIN AND RENEW THE REPAIR ON LOWER AND UPPER SURFACE IAW SRM 57-52-12 FIG 204. 2 L 7 2 4F RT A35EU 2007091800155 20070918 00155 EU 2007 9 18 07FDEA03681 1 20070913 A 5730 A57350100 SKIN AIRBUS 310 A310203 3930313 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 DURING REMOVAL OF BOLT 642, NOTED IN SB A310-57-2028 FOUND CORROSION INSIDE THE FITTING BORE, LT WING AREA OF RIB 5 REPA IR PERFORMED BY OVERSIZING THE HOLE IAW EA 6-5721-81050 AND RAS/BAE/0928/2004 ISS A. 2 L 7 2 4F RT A35EU 2007091800165 20070918 00165 NM 2007 9 18 2007UALA03545 1 20070905 A 3610 BLEED AIR SYS BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU RIGHT MALFUNCTIONED A UALA B EMER. DESCENT O OTHER CL CLIMB 1 WP 29 912UA 25290 DURING CLIMB ACFT LOST RT BLEED SUPPLY. CABIN PRESSURE REACHED 10,000 FT, RAPID DESCENT TO FL230 AND SITUATION STABILIZ ED. MASKS DID NOT DEPLOY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800174 20070918 00174 NM 2007 9 18 2007UALA03548 1 20070827 A 2781 WARNING SYSTEM BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 914UA 25381 NR 1 LEADING EDGE FLAP OVERHEAD INDICATED GREEN WITH AMBER LEADING EDGE FLAPS TRANSITION, FLAP HANDLE UP. RESTRICTION 2 30KIAS, FL200 AND .65MACH. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800175 20070918 00175 NM 2007 9 18 2007UALA03549 1 20070901 A 5320 ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 WEB ANGLE CRACKED, BS 639R RBL 46-48 BELOW SEAT TRACK, MID CABIN AREA. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800176 20070918 00176 NM 2007 9 18 2007UALA03550 1 20070901 A 2611 MR26162 SMOKE DETECTOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CARGO BAY INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 219UA 30551 AFT LOWER CARGO COMPARTMENT SMOKE DETECTION SYSTEM INOPERATIVE. REPLACED DETECTOR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007091800178 20070918 00178 NM 2007 9 18 2007UALA03552 1 20070901 A 5320 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 FWD ENTRY DOOR LOWER HINGE CUTOUT HAS 2 EA HOLES WITH CRACKS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800179 20070918 00179 NM 2007 9 18 2007UALA03553 1 20070901 A 5230 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 AFT CARGO DOOR CRACKED: LOWER AFT INNER CORNER T-CHORD CRACKED THROUGH FASTENER HOLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800180 20070918 00180 NM 2007 9 18 2007UALA03554 1 20070901 A 5230 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 AFT PIT DOOR DENT, EXT SKIN UPPER RIGHT CORNER HAS A DENT OUT OF LIMITS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800181 20070918 00181 NM 2007 9 18 2007UALA03556 1 20070901 A 5330 PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 KEEL BEAM PANEL CRACKED STA 698 LBL 4-5. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800182 20070918 00182 EU 2007 9 18 07FDEA03660 1 20070913 A 5315 A53978267 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION AT CROSSBEAM C 67, C66. CROSSBEAM REPAIR PERFORMED IAW SRM 53-10-15 FIG 207 . 2 L 7 2 4F RT A35EU 2007091800183 20070918 00183 EU 2007 9 18 07FDEA03659 1 20070913 A 5311 A53973031246 FRAME AIRBUS 310 A310324 3930206 EU ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 TOOL IMPACT CAUSES DENT IN FRAME 71, STRG 15 RHS. SPLICE REPAIR PERFORMED IAW SRM 53-10-13 / PG 210, 213 / FIG 203. 2 L 7 2 4F RT A35EU 2007091800184 20070918 00184 EU 2007 9 18 07FDEA03658 1 20070913 A 5311 A53973030240 FRAME AIRBUS 310 A310324 3930206 EU ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 TOOL IMPACT CAUSES DENT IN FRAME 70, STRG 15 RHS. SPLICE REPAIR PERFORMED IAW SRM 53-10-13 / PG 210, 213/FIG 203. 2 L 7 2 4F RT A35EU 2007091800185 20070918 00185 EU 2007 9 18 07FDEA03657 1 20070913 A 5313 A53981965202 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION ON STRINGER P50 AT C80, LT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007091800186 20070918 00186 NM 2007 9 18 2007UALA03557 1 20070904 A 3510 OXYGEN MASK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT DEFECTIVE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 OXYGEN MASK DEFECTIVE AT 2.(1=CAPT,2=1ST OFF,3=1ST OBS). CREW COMMENTS: O2 MASK INFLATABLE BAND BURST. 2 L 7 2 4F 4 F RT A1NM E24NE 2007091800187 20070918 00187 NM 2007 9 18 2007UALA03558 1 20070903 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 649UA 25286 EEL LIGHT INOP LOCATED MID ZONE LAVATORY LEFT & RIGHT AISLES. 2 L 7 2 4F 4 F RT A1NM E24NE 2007091400117 20070914 00117 EU 2007 9 14 F3LA200700226 1 20070901 A 5315 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT FLOORBEAM FROM STR 38R TO STR 38L CORRODED AROUND FASTENER HOLES. REMOVED AND REPLACED TRANSITION PLATE AT FR28 BETWEEN STR 38R THRU STR 38L IAW SRM 51-42-11. 2 L 7 2 4F RT A28NM 2007091400119 20070914 00119 2007 9 14 F3LA200700227 4 20070909 A 2565 D30664309 SLIDE AIRBUS A319 A319112 3930323 EU R1 DOOR FAULTED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED EMERGENCY LIGHT TEST SHOWED LEFT EPSU EXTERNAL FAULT. REPLACED R1 DOOR SLIDE IA W AMM 25-62-44-400-007. 2 L 7 2 4F RT A28NM 2007091400130 20070914 00130 2007 9 14 DL757071172 4 20070903 A 2565 TRIGGER BOEING 757 757232 1384965 NM L2 DOOR SLIDE BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 650DL 17604 24390 DURING OPN 6T129 SLIDE/RAFT SAMPLING PROGRAM 2L DOOR SLIDE DID NOT DEPLOY. FOUND 2L DOOR TRIGGER BROKEN REPLACED SAME P ER M/M. INSTALLATION ADJ GOOD (QC1503) C/W OPN 6T129, NO DEFECTS FOUND. 2 L 7 2 4F RT A2NM 2007091400135 20070914 00135 WP 2007 9 14 IXXA070048O 1 20070911 A 3411 PITOT TUBE DOUG DC8 DC862F 3021972 WP DAMAGED A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 71CX 70935 932 45961 DURING CLIMB-OUT FROM PHIK, THE CREW NOTICED THE PITOT HEATER INOP LIGHT ILLUMINATED, ZERO AMPS INDICATED ON THE FIRST O FFICER'S PITOT TUBE POSITION. THE CREW RETURNED TO PHIK, MADE 50 DEGREES FLAP EMERGENCY OVERWEIGHT LANDING AND LANDED W ITH OUT INCIDENT. MAINTENANCE REPLACED FIRST OFFICER'S PITOT TUBE PERFORMED LEAK CHECK WAS GOOD, AND PERFORMED A OVERWE IGHT LANDING INSPECTION IAW DACO DC8 MAINTENANCE MANUAL 34-12-0 AND ATI JOB CARD 13.01-5. AIRCRAFT WAS RETURNED TO SERV ICE. 2 L 7 4 4F 4A25 2007091400138 20070914 00138 EU 2007 9 14 07FDEA03481 1 20070910 A 5330 A53980666 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 FOUND EXTERNAL DOUBLER REPAIR AT FRAME 72-73 BETWEEN STRG 43-44 LT, NOT CONFORM TO SRM 53-10-12/FIG 203. REPAIR PERFO RMED BY INSTALLATION OF NEW DOUBLER IAW SRM 53-10-12/FIG 225. 2 L 7 2 4F RT A35EU 2007091400144 20070914 00144 EU 2007 9 14 07FDEA03488 1 20070910 A 5330 A53610567203 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION ON INNER SKIN DOUBLER C10A-11, P 54RH-54LH. REPAIR PERFORMED BY REMOVAL OF CORROSION, SMOOTH BLEND OUT AND INSTALLING OVERSIZE FASTENER IAW EA 6-5312-114837 AND RAS 053782/014/2007. 2 L 7 2 4F RT A35EU 2007091400146 20070914 00146 EU 2007 9 14 07FDEA03490 1 20070910 A 5750 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 LT ALL SPEED AILERON LOWER SKIN, DENTS IN TRAILING EDGE HONEYCOMB AREA. REPAIR PERFORMED BY CUT OUT DENTED SKIN AND APPL Y WITH EXTERNAL PATCHES IAW EA 6-5761-95884 AND RAS/FOK/199/2005 ISSUE B. 2 L 7 2 4F RT A35EU 2007091400153 20070914 00153 EU 2007 9 14 07FDEA03380 1 20070905 A 5330 A53611171202 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 OLD DOUBLER REPAIR ON SKIN AT FRAME 3 LT BELOW FLOOR LEVEL, NOT CONFORM TO RAS/AS/189/00 ISSUE A (SHIM IN THE CUT OUT IS MISSING). REPAIR RENEWED IAW. RAS/AS/189/00 ISSUE A. 2 L 7 2 4F RT A35EU 2007091400160 20070914 00160 EU 2007 9 14 07FDEA03497 1 20070910 A 5410 A54515063004 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 FOUND CRACKED PICK UP MEMBER ON PYLON NR 2. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 54-54-11. 2 L 7 2 4F RT A35EU 2007091400162 20070914 00162 EU 2007 9 14 07FDEA03499 1 20070910 A 5313 A53971007212 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 HEAVY CORROSION ON STRINGER 49 RT BETWEEN FRAME 57.3-58. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 / FIG 201. 2 L 7 2 4F RT A35EU 2007091400169 20070914 00169 NM 2007 9 14 NWAA072966310 1 20070831 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670US 24225 DURING OVERNIGHT CHECK, FOUND RIGHT SIDE EXIT EMERGENCY LIGHTS FORWARD 2 INOP. MAINTENANCE REMOVED AND REPLACED EMERGEN CY LIGHT POWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007091400171 20070914 00171 EU 2007 9 14 07FDEA03382 1 20070905 A 5414 A54611752505 PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 CRACKED HOLES (8 MM) FOUND ON PYLON NR 1, RIB 8 INBOARD SIDE. REPAIR PERFORMED IAW SRM 54-51-31/FIG 201. 2 L 7 2 4F RT A35EU 2007091400181 20070914 00181 WP 2007 9 14 07FDEA03507 1 20070910 A 5313 ACA3796 LONGERON DOUG DC10 DC1010F 3022111 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 AIR CONDITIONING COMPT LT SIDE FOUND SEVERE EXFOLIATION CORROSION. REPAIRED AREA IAW SRM 53-10-00 FIG 6 VOL I. 2 L 7 3 4F A22WE 2007091400187 20070914 00187 NM 2007 9 14 AALA20071567 1 20070813 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 AFW - EMERGENCY LIGHTS AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091400190 20070914 00190 SO 2007 9 14 SWIA200718659 1 20070907 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 288SW 120316 FLT 5720 - EXIT ROW EMERGENCY LIGHT ASSEMBLY IS BROKEN. REPLACED EXIT SIGN ASSEMBLY, P/N 10-1301-15. 2 L 7 2 4T RT A31SO 2007091400193 20070914 00193 EA 2007 9 14 SWIA200718662 1 20070905 A 5210 LATCH CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 806SK 15070 PAX DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE. CLEANED PAX DOOR LATCH PINS AND CAMS. RELUBRICATED PAX DOOR IAW MM 12-2 0-52. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007091400194 20070914 00194 EA 2007 9 14 SWIA200718663 1 20070903 A 2750 7455001 LEVER CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 969SW 7876 FLT 6726 - FLAPS SUDDENLY EXTENDED TO 8 DEGREES, THEN RETURNED TO 0 DEGREES. REPLACED FLAP CONTROL LEVER PER MM 27-51-0 1. 2 L 7 2 4F RT A21EA 2007091400195 20070914 00195 EA 2007 9 14 SWIA200718664 1 20070907 A 5610 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 340CA 10062 RIGHT WINDOW CRACKED WHILE AT ALTITUDE. REPLACED RIGHT SIDE WINDOW IAW 56-12-01. OPS CHECK GOOD, P/N OFF NP-139322-00 1, S/N 02070H1423. 2 L 7 2 4F RT A21EA 2007091400196 20070914 00196 EA 2007 9 14 SWIA200718665 1 20070903 A 2910 LINE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA O OTHER K FLUID LOSS AP APPROACH 1 NM 07 448SW 7678 FLT 3819 - LOST HYDRAULIC FLUID ON NR 2 SYSTEM. REPLACED THE NR 2 HYDRAULIC SYSTEM PRESSURE LINE AND THE CASE DRAIN LIN E IN THE AFT EQUIPMENT BAY IAW CRJ MM 29-11-01. 2 L 7 2 4F RT A21EA 2007091400199 20070914 00199 EA 2007 9 14 SWIA200718668 1 20070908 A 3230 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 941SW 7750 RECEIVED A NOSE GEAR DISAGREE WARNING WHEN SELECTED. CYCLED GEAR AND RECEIVED NORMAL INDICATIONS. REPLACED NLG SELECTO R VALVE IAW 32-34-01, PN: 601R75146-1, SN OFF: 00447. 2 L 7 2 4F RT A21EA 2007091700048 20070917 00048 CE 2007 9 17 082907N413CS1 1 20070829 A 2730 TRIM SYSTEM CESSNA 525 525 2076601 CE WILINT FJ44 FJ44 66000 GL OUT OF ADJUST E Z5FA A UNSCHED LANDING F S FLT CONT AFFECTED AFFECT SYSTEMS CR CRUISE 1 EA 63 413CS 525B0082 ENROUTE, AT CRUISE ALTITUDE OF 5000 FT AIRCRAFT STARTED TO TURN RT, DISENGAGED AUTO-PILOT, TURN STILL EXISTED. DIVERTED TO TOL AND LANDED WITHOUT INCIDENT. AIRCRAFT CURRENTLY IN MAINTENANCE. CAUSE UNKNOWN AT THIS TIME. 09-03-07 ALL CONTRO L RUDDER, AILERON AND FLAP TRAVELS CHECKED ALL CABLE RUNS AND TENSIONS CHECKED GOOD. STATIC RIGGING CHECKED GOOD, FIRST FLIGHT CHECK HAD SAME TURNING TO THE RIGHT ISSUE. CREW TRIMMED UP RUDDER AND AILERON FOR STRAIGHT AND LEVEL FLIGHT. MAIN TENANCE CREW RESET TRIM INDICATIONS FOR FLIGHT NEUTRAL, NEXT FLIGHT CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 4F 4 F RT A1WI E3GL 2007091700077 20070917 00077 EU 2007 9 17 07FDEA03391 1 20070905 A 2130 RELAY AIRBUS 310 A310203 3930313 EU MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 443FE 283 AFTER T/O REC'D MASTER CAUTION LIGHT W/LEFT ECAM WARNING CABIN PRESS MAN PRESS VALVE NOT CLOSED. REC'D RIGHT CORRESPON DING ECAM PAGE. REPEAT WRITE UP MANUAL VALVE WOULD NOT CLOSE. R & R 208HM,133HM, AND 131HM. RELAY139HM, REINSTALLED N R 1 & 2 CPC'S. OPS CHECK OF NR 1 AND 2 CPC'S OPS CHECKS NORMAL. 2 L 7 2 4F RT A35EU 2007091700078 20070917 00078 WP 2007 9 17 UPS07850620 1 20070906 A 3350 CONTROL PANEL DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:N/A F/E PANEL EMERGENCY CONTROL LIGHT PANEL HAS 4 OR 6 LIGHTS INOP. DEF 358150 ASSIGNED. *SDR FILED OP EN* DEFERRED F/E EMERGENCY ELECT CONTROL LIGHTING PANEL REF MEL 33-1 PART REQ A 847094. 2 L 7 4 4F RT 4A25 2007091700079 20070917 00079 EU 2007 9 17 07FDEA03389 1 20070905 A 2133 OUTFLOW VALVE AIRBUS 310 A310203 3930313 EU CABIN PRESSURE MALFUNCTIONED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 443FE 283 AFTER T/O REC'D MASTER CAUTION LIGHT W/LEFT ECAM WARNING CABIN PRESS MAN PRESS VALVE NOT CLOSED. REC'D RIGHT CORRESPON DING ECAM PAGE. REPEAT WRITE UP MANUAL VALVE WOULD NOT CLOSE. NR 1 CABIN PRESS, MEL 21-31-04-02-A, A/C TO MEM UNPRESS FLT. MEM REMOVED AND REPLACED SWITCHES 129 AND140 HM ON 432 VU PANEL. A/C FAILED TEST FLT, MEM-/08. REMOVED AND REPLA CED OUTFLOW VALVES. TEST FLT FAILED MEM/09. R&R OUTFLOW VALVES. TEST FLT FAILED MEM/09. (WIRE 2131-6301-CF22) HAS A HIGH MEG OHM TO GRD BETWEEN 39HM-A AND 817VC REF A310 AWM 21-31-07.-REPLACED WIRE FROM PLUG 39HM TO DISCONNECT 817VC . R & R'D THE FOLLOWING RELAYS: 208HM,133HM & 131HM& 139HM . TEST FLIGHT ACCOMPLISHED PER MOCC REQUEST. 2 GOOD LEGS 2 L 7 2 4F RT A35EU 2007091700080 20070917 00080 SO 2007 9 17 SIMA200725401 1 20070910 A 4990 4504113A APU EMB 135 EMB135KL 3260302 SO LEAKING A SIMA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 856AE 145748 OIL SMELL WITH BLEEDS ON. FOUND APU LEAKING OIL AND PLACED THE APU ON MEL. AIRCRAFT RETURNED TO SERVICE. REMOVED AND REPLACED APU IAW AE WORKCARD 49-800-05 MEL RESTORED 2 L 7 2 4F RT T00011AT 2007091700081 20070917 00081 EU 2007 9 17 07FDEA03516 1 20070911 A 5313 A53610797222 LONGERON AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 LONGERON BETWEEN C12A AND 15A, Y 1959 HEAVY CORRODED SPLICE REPAIR PERFORMED IAW SRM 53-12-15 FIG 207. 2 L 7 2 4F RT A35EU 2007091700082 20070917 00082 EU 2007 9 17 07FDEA03518 1 20070911 A 5347 A53611640212 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION FOUND AT SEATTRACK C15A0-19, Y 1959 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091700083 20070917 00083 EU 2007 9 17 07FDEA03522 1 20070911 A 5330 A53778050200 SKIN PANEL AIRBUS 310 A310203 3930313 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 OLD EXTERNAL SKIN DOUBLER C 33, P37-39 LT NOT COMPATIBLE WITH P TO F CONVERSION. REPAIR PERFORMED BY RENEWING THE DOUBL ER REPAIR IAW RAS/DABRE/7004007/2004 ISS A AND DRAWING R737B1150. 2 L 7 2 4F RT A35EU 2007091700084 20070917 00084 EU 2007 9 17 07FDEA03524 1 20070911 A 5313 A53610797222 LONGERON AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 LONGERON C12A-15A, Y-1959 HEAVY CORRODED REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091700085 20070917 00085 EU 2007 9 17 07FDEA03526 1 20070911 A 5347 A53611640212 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND SEAT TRACK C15-19 Y-1959 HEAVY CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091700086 20070917 00086 EU 2007 9 17 07FDEA03528 1 20070911 A 5313 A53610797231 LONGERON AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 LONGERON C11-15A, Y 1456 HEAVY CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091700087 20070917 00087 EU 2007 9 17 07FDEA03529 1 20070911 A 5347 A53610798202 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 SEAT TRACK C15A-19, Y-1552 HEAVY CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091700088 20070917 00088 EU 2007 9 17 07FDEA03531 1 20070911 A 5347 A53611640200 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND SEAT TRACK C15A-19, Y-953 HEAVY CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091700089 20070917 00089 EU 2007 9 17 07FDEA03532 1 20070911 A 5311 A53772531202 FRAME AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION AT FRAME 20A, P45 RT OUT OF LIMIT REPAIR PERORMED IAW SRM 53-13-13 FIG 202. 2 L 7 2 4F RT A35EU 2007091700090 20070917 00090 EU 2007 9 17 07FDEA03534 1 20070911 A 5315 A53974343200 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION ON FLOORBEAM C70 RT OUT OF LIMIT. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 2007091700091 20070917 00091 EU 2007 9 17 07FDEA03536 1 20070911 A 5313 A53974475202 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION FOUND ON STRINGER P 56, AT C68 OUT OF LIMIT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007091700092 20070917 00092 EU 2007 9 17 07FDEA03538 1 20070911 A 5313 A53974203229 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION FOUND AT P 56 RT, C 69 OUT OF LIMIT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007091700093 20070917 00093 EU 2007 9 17 07FDEA03541 1 20070911 A 5313 A53974203 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION ON STRINGER P52, 53, 55 RT, C 65-66 OUT OF LIMIT STRINGER REPAIR PERORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007091700094 20070917 00094 EU 2007 9 17 07FDEA03542 1 20070911 A 5313 A53974203 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION FOUND AT C67-69, P 56 AND P56 RT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007091800009 20070918 00009 NM 2007 9 18 UPS07M50599 1 20070722 A 5744 HINGE DOUG MD11 MD11F 3023600 NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C LEFT WING O/B FLAP I/B HINGE (WING MOUNTED), I/B LOWER ATTACHMENT SPOT FACES 02 EA FOUND CORROSION AS MARKED. AFFECTED AREA CORROSION REMOVED & FOUND EXCEED LIMIT PER CMM57-44-08 PG 602- 607 R58. ORG THK 0.530" REMN THK 0.523" MAT'L RMVD 0.007" MIN ALLOW TH K 0.720". FPI C/O DAC NDTSPM R13 PART 8 FOUND NO CORR & CRACK EVIDENT. LEFT I/B HOLE SPOTFACE THK 0.523" EVAL & FOUND ACCEPTED EN1510-07. REWORKED AREA ETCH INSPECT, FOUND SATISFACTORY FLAP PEENING C /O BSOPM20-11-01R58. 2 L 7 3 4F RT A22WE 2007091800021 20070918 00021 EA 2007 9 18 COMA0760549 1 20070830 A 3260 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAULTY A COMA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 587SW 19972 7062 FLIGHT 5688 - RECEIVED GEAR DISAGREE MESSAGE, PERFORMED QRH AND LANDED WITHOUT INCIDENT. REPLACED PSEU. NO FURTHER DEF ECTS. 2 L 7 2 4F RT A21EA 2007091800029 20070918 00029 NM 2007 9 18 KCSA071332 1 20070906 A 3350 3004075 LIGHT BOEING 747 747236B 1384804 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 701CK 21730 MAIN DECK AFT EMERGENCY LIGHT IN CEILING AT L1 DOOR IS INOP. 2 L 7 4 4F A20WE 2007091800036 20070918 00036 2007 9 18 UPS07850621 4 20070905 A 2565 SLIDE DOUG DC8 DC873F 302199F WP COCKPIT OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 ESCAPE SLIDE ON CAPTAIN'S SIDE FELL OUT. 10-8-07 REINSTALLED CAPTAIN'S ESCAPE TAPE (ROPE) AND LINING IAW DC8 MM 25-61 -13-04. 2 L 7 4 4F RT 4A25 2007091800045 20070918 00045 EA 2007 9 18 TRAX200701309 1 20070904 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 870AS 7530 F/A REPORT PAX BOARDING DOOR DIFFICULT TO OPEN, APPEARS TO BE CAUGHT ON SOMETHING. 2 L 7 2 4F RT A21EA 2007091800091 20070918 00091 NM 2007 9 18 2007UALA03521 1 20070901 A 3260 WARNING SYSTEM BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT MALFUNCTIONED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 941UA 26676 NLG RED LIGHT CONSTANTLY ON WITH GEAR HANDLE UP OR OFF. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800106 20070918 00106 NM 2007 9 18 2007UALA03527 1 20070831 A 3350 5878158807 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN CONTAMINATED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 303UA 23644 FLOOR MOUNTED EEL LIGHTS INOP FROM SEAT ROW 15 TO AFT GALLEY. REPLACED WET POWER STRIP & AFT GALLEY LIGHT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800119 20070918 00119 NM 2007 9 18 2007UALA03537 1 20070901 A 2781 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE L/E SLAT ACTIVATED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 29 641UA 25091 RTFL DUE TO L/E SLAT DISAGREE MESSAGE. EVENT RECURRED ON NEXT FLIGHT OUT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007091800189 20070918 00189 NM 2007 9 18 2007UALA03560 1 20070903 A 3350 BEZEL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 BEZEL IS MISSING FROM EEL LIGHT AT ROW 18 BC. 2 L 7 2 4F 4 F RT A1NM E24NE 2007091800191 20070918 00191 NM 2007 9 18 2007UALA03562 1 20070903 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 649UA 25286 EEL LIGHT INOP LOCATED AT FIRST CLASS ZONE LEFT AISLE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007091800192 20070918 00192 NM 2007 9 18 2007UALA03563 1 20070902 A 2421 IDG BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE LEFT MALFUNCTIONED A UALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 29 675UA 29243 LEFT IDG VOLTS FLUCTUATING. 2 L 7 2 4F 4 F RT A1NM E24NE 2007091800193 20070918 00193 NM 2007 9 18 2007UALA03564 1 20070903 A 5320 STRUCTURE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 776UA 26937 LIGHTNING STRIKE AT STA 496 RBL 1 & STA 613 STR 1L. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007091800198 20070918 00198 NM 2007 9 18 2007UALA03570 1 20070903 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 THE -D- ZONE EEL'S INOP LT ROW OF SEATS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007091800200 20070918 00200 NM 2007 9 18 2007UALA03572 1 20070904 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY EEL LIGHTS INOP AT SEATS 1J AFT & SEAT 55 ABC. 2 L 7 4 4F 4 F RT A20WE E24NE 2007091800203 20070918 00203 EU 2007 9 18 07FDEA03656 1 20070913 A 5311 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 812FD 467 HEAVY CORROSION FOUND ON THE T-SECTION AT FRAME 92, BETWEEN STRG 19-23 LT (TAILCONE). REPAIR PERFORMED BY CUT OUT THE T-SECTION AND INSTALLING NEW PORTION AND REPAIR ANGLES IAW EA 6-5319-92229 AND RAS/DAHAM/4020157/2005 ISSUE B. 2 L 7 2 4F RT A35EU 2007091800205 20070918 00205 EU 2007 9 18 07FDEA03654 1 20070913 A 5310 A53973085208 BEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION FOUND ON LOWER SILL BEAM OF AFT CARGO DOOR AT C59A. REPAIR PREFORMED BY TRIM OUT THE AFFECTED AREA AND FABRIC ATE A STRAP IAW EA 6-5310-79580 AND RAS/DATLS/0001970/2004 ISS A. 2 L 7 2 4F RT A35EU 2007091800206 20070918 00206 EU 2007 9 18 07FDEA03653 1 20070913 A 5320 A53612213212 FLOOR SUPPORT AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 HEAVY CORROSION ON FLOOR SUPPORT BETWEEN FRAME 14-17, STRINGER 26, Y-1959 RT. REPAIR PERFORMED BY REINFORCING WITH ANGL E IAW SRM 53-12-15/FIG 207. 2 L 7 2 4F RT A35EU 2007091800207 20070918 00207 EU 2007 9 18 07FDEA03652 1 20070913 A 5330 A53980664204 SKIN PANEL AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION FOUND ON SKIN PANEL C78/80, P 45-50 RT, IN SERVICE PANEL AREA. REPAIR PERFORMED BY BLEND OUT UNTIL CORROSION REMOVAL AND REPLACING THE TOILET SERVICE DOOR WITH COVER A539-809076-200 IAW EA 6-5330-79575 AND RAS/DATLS/0001961/200 4 ISS A. 2 L 7 2 4F RT A35EU 2007091800209 20070918 00209 EU 2007 9 18 07FDEA03651 1 20070913 A 5320 A53970709203 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 MISDRILLED HOLE IN CORNER FITTING FRAME 54.1 RT DUE TO FAILED INSTALLED ROLLERTRACK ON CARGO FLOOR STRUCTURE. REPLACE MENT OF CORNERFITTING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091800210 20070918 00210 EU 2007 9 18 07FDEA03650 1 20070913 A 5320 A53978048208 ANGLE AIRBUS 310 A310324 3930206 EU ZONE 200 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 LESS MARGIN AT ONE HOLE AT FRAME 59, STRG 26 LT. NEW SUPPORT CAN'T BE INSTALLED BETWEEN FRAME 59 AND SEAT TRACK AS PER DRW, R539H0112. REPAIR PERFORMED BY INSTALLING REINFORCING PLATE WHICH IS FIXED WITH HI-LOK'S DAN5-5 IAW, SRM 51-72-1 0 AND EFW DD-0467024 ISSUE AA. 2 L 7 2 4F RT A35EU 2007091800211 20070918 00211 EU 2007 9 18 07FDEA03649 1 20070913 A 5320 A53984658208 ANGLE AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION AFT PRESSURE BULKHEAD CIRCUMFERENTIAL STRAP, INNER RIM ANGLE AND FRAME COUPLING AT C80/82, P25LH TO 36RH . REPAIR PERFORMED BY CUT OUT OF DAMAGED PARTS, REINSTALLING NEW PARTS IAW DRAWING R539-70603, APPROVED BY 6-5318-79562 AND RAS/DAHAM/4018245/2004 ISS A. 2 L 7 2 4F RT A35EU 2007091800212 20070918 00212 EU 2007 9 18 07FDEA03648 1 20070913 A 5330 A53989352 SKIN AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 HEAVY CORROSION UNDER ANTI-CHAFING PLATE ON SKIN PANEL BETWEEN FRAME 92-94, STRG 9-13 LT AND RT, OUT OF LIMIT. REPLACEM ENT OF BOTH SKIN-PANELS (FABRICATED BY EFW-DRS) IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091800213 20070918 00213 EU 2007 9 18 07FDEA03647 1 20070913 A 5313 A53978157240 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 SEVERAL MISDRILLED HOLES ON STRINGER 33 RT BETWEEN FRAME 69-70. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 2 01 / SEC "C-C". 2 L 7 2 4F RT A35EU 2007091800214 20070918 00214 EU 2007 9 18 07FDEA03645 1 20070913 A 5522 A55276700 SKIN AIRBUS 310 A310324 3930206 EU LT ELEVATOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 DENT IN BOTTOM SKIN OF LT ELEVATOR TRAILING EDGE (30X30X1,5). REPAIR PERFORMED IAW SRM 55-21-11/CONFIG 1/PARA 5D/FIG 20 4. 2 L 7 2 4F RT A35EU 2007091800216 20070918 00216 EU 2007 9 18 07FDEA03643 1 20070913 A 5313 A53974203230 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION ON STRINGER P 57 LT, C 69-70 OUT OF LIMIT. STRINGER REPAIR PERFORMED SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007091800219 20070918 00219 NM 2007 9 18 2007UALA03584 1 20070905 A 5330 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 842UA 1569 EVIDENCE OF LIGHTNING STRIKE IN SKIN 8 INCHES FWD OF FRAME 30, .5 INCH BELOW STR 41L. MAJOR REPAIR OF SKIN, 8" FWD OF FRAME 30, .5 INCH BELOW STR 41L- EXTERNAL DOUBLER REPAIR AND INTERNAL STRINGER REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007091800223 20070918 00223 NM 2007 9 18 2007UALA03585 1 20070905 A 5313 STRINGER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 LEFT SIDE OF FUSELAGE HAS A CRACK APPROX 2 INCHES IN LENGTH BEHIND LEFT AFT WING TO BODY FAIRING. CRACK IS ON STRINGER JUST BELOW EMERGENCY EXIT LIGHT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800225 20070918 00225 NM 2007 9 18 2007UALA03586 1 20070905 A 3260 PSEU BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LANDING GEAR FAILED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 195UA 26899 CMC MSG -R BODY GEAR DOWN ALTERNATE PROX SWITCH TARGET FAIL- (PSEU) ON 3 OF LAST 5 LEGS WITH HARD FAULTS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007091800226 20070918 00226 NM 2007 9 18 2007UALA03587 1 20070905 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN TORN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 513UA 24810 EMERGENCY LIGHT STRIP AT ROW 28 TORN AND DOES NOT ILLUMINATE. REPLACED DAMAGED EEL STRIP AND SECURED IT AS PER SPECI FICATIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091800227 20070918 00227 NM 2007 9 18 2007UALA03588 1 20070905 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 520UA 24890 AFT PIT STA 1398 ABOVE 27R FLOOR SUPPORT CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION AND CHECKED LIMITS - MATERIAL THICKNESS FOUND 0.063. REMAINING MATERIAL 0.044 WAS OUT OF LIMITS OF SRM. REMOVED STRINGER AND FABRICATED N EW STRINGER, APPLIED ALODINE, PRIMED AND INSTALLED REPAIR PER SRM, PAINTED AND SANDED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091800228 20070918 00228 NM 2007 9 18 2007UALA03589 1 20070905 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 224UA 30225 EEL LIGHT AT SEAT 37G IS INOP. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007091800229 20070918 00229 NM 2007 9 18 2007UALA03590 1 20070905 A 3520 MASK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 819UA 893 THE O2 MASKS AT 11DEF, 23ABC AND D LAV DO NOT DROP DURING DROP CHECK. FOUND IMPROPER PACKING. REPACKED MASKS AND PER FORMED DROP AGAIN. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007091800230 20070918 00230 SO 2007 9 18 C2XA07IA195 1 20070902 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 19554 3851 208 145587 MCI - DURING MAINTENANCE INSPECTION THE NUMBER 5 & 6 AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE A IRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007091800231 20070918 00231 NM 2007 9 18 HNAA0700163 1 20070820 A 3350 1013079 SOCKET DHAV DHC8 DHC8102 2809003 NM CABIN DEFECTIVE A HNAA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 07 814EX 318 ROW 7DF FLOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT SOCKET. 2 H 7 2 4T RT A13NM 2007091800233 20070918 00233 NM 2007 9 18 KCSA071334 1 20070908 A 3350 LIGHT BOEING 747 7472B4B 138481B NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 719CK 21099 MAIN DECK EMERGENCY LIGHT AT STA -390 INOP. 2 L 7 4 4F RT A20WE 2007091800235 20070918 00235 NM 2007 9 18 KCSA071336 1 20070908 A 3350 LIGHT BOEING 747 747209B 138489B NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 715CK 22447 EMERGENCY LIGHT AT STA -2260 L-5 DOOR INOP. 2 L 7 4 4F RT A20WE 2007091800237 20070918 00237 EA 2007 9 18 COMA0760550 1 20070831 A 3250 STEERING SYS CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA K NONE J WARNING INDICATION DE DESCENT 1 SO 01 926CA 7027 FLIGHT 5687 - DURING TAKEOFF ROLL, AIRCRAFT PULLED TO THE RIGHT. STEERING INOP MESSAGE IN FLIGHT. AIRCRAFT LANDED SAFE LY. PERFORMED HIGH SPEED TAXI CHECK, WITH NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007091800239 20070918 00239 EA 2007 9 18 HNAA0700165 1 20070907 A 3150 820081007 PANEL DHAV DHC8 DHC8311 1386006 EA COCKPIT MALFUNCTIONED A HNAA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 331EN 279 PILOT REPORT ELECTRICAL SMELL IN COCKPIT. T/S TO CAUTION LIGHT PANEL. REMOVED AND REPLACED CAUTION PANEL. NO EMERGENC Y DECLARED. 2 H 7 2 4T RT A13NM 2007091800240 20070918 00240 NM 2007 9 18 HNAA0700161 1 20070730 A 5610 8SC0043002 WINDSHIELD DHAV DHC8 DHC8102 2809003 NM COCKPIT DAMAGED A HNAA D RETURN TO BLOCK F FLT CONT AFFECTED CR CRUISE 1 EA 07 906HA 9 THERE WAS A BIRD STRIKE NEAR THE F/O WINDSHIELD ON CLIMBOUT. THE FLIGHT WAS 20 MINUTES OUT OF CLT. THE FLIGHT CREW WAS HEARING A NOISE AND THEN IT WENT AWAY. FLIGHT DIVERTED TO ROA. AFTER LANDING IN ROA THE CAPTAIN REPORTED THERE WAS A LOSS OF PRESSURE. MAINTENANCE REMOVED BIRD DEBRIS RT WING INBOARD AFT SIDE. SEALED AROUND INSIDE AND OUTSIDE OF F/O WI NDSCREEN, PRESSURIZED AIRCRAFT TO 5.25 DIFF IAW OUTSIDE SEAL REPAIR ESR 8-56-04-009. INSIDE REPAIR IAW SPECIAL PROCEDUR E 56-1. NO DEFECTS NOTED, OK FOR SERVICE. 2 H 7 2 4T RT A13NM 2007091800244 20070918 00244 NM 2007 9 18 UPS07M50614 1 20070906 A 2611 SMOKE DETECTOR DOUG MD11 MD11F 3023600 NM CABIN FALSE ACTIVATION A IPXA J A DUMP FUEL UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SO 01 287UP 48539 INSPECTION TYPE:N/A DIVERSION - CABIN SMOKE LEVEL 3 ALERT ILLUMINATED IN FLIGHT. CREW DECLARED AN EMERGENCY AND DUMPED ROUGHLY 30,000 LBS OF FUEL. MX DEFERRED NR 11 MAIN DECK SMOKE DETECTOR PER MEL M358114 ASSIGNED. REMOVED AND REPLACED NR 11 SMOKE DETECTOR IN REF TO MM 26-15-08-4, OPS CHECK OK. THIS CLEARS M358114. PLACARD REMOVED. 2 L 7 3 4F RT A22WE 2007091800246 20070918 00246 NM 2007 9 18 UPS07M50623 1 20070816 A 5712 ARB2850506 RIB DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 INSPECTION TYPE:4C RIGHT WING NR 16 SLAT TRACK I/B FITTING (RIB) IS CRACKED. REMOVED AND REPLACED RIGHT WING NR 16 SLAT TRACK I/B FITTING (RIB) IAW MD-11 SRM 51-33-01 AND 51-35-01. 2 L 7 3 4F RT A22WE 2007091800247 20070918 00247 SO 2007 9 18 C2XA07RI074 1 20070904 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 11539 145536 FLIGHT 2334 - EWR - CREW REPORTED EMERGENCY LIGHT SIGN DOES NOT ILLUMINATE. EWR MX REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW EMB 145 AMM 33-50-11. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVIC E. 2 L 7 2 4T RT T00011AT 2007091800249 20070918 00249 EA 2007 9 18 COMA0760552 1 20070901 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 918CA 698 7018 FLIGHT 5348 - FORWARDS EMERGENCY LIGHTS WILL NOT COME ON. REMOVED AND REPLACED NR 1 BATTERY PACK. 2 L 7 2 4F RT A21EA 2007091800250 20070918 00250 EA 2007 9 18 COMA0760553 1 20070901 A 3397 59465 CABLE CNDAIR CL600 CL6002B19 1900309 EA CABIN FAILED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 809CA 7366 FLIGHT 5259 - AFT 1/3RD OF EMERGENCY FLOOR LIGHTING INOP. REMOVED AND REPLACED CABLE JUMPER FOR EMERGENCY FLOOR LIGHTIN G. 2 L 7 2 4F RT A21EA 2007091800252 20070918 00252 EA 2007 9 18 COMA0760555 1 20070903 A 3350 362624 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 427CA 7460 FLIGHT 5088 - FORWARD FLOOR EMERGENCY FLOOR STRIP NOT ILLUMINATING. REMOVED AND REPLACED FLEX LAMP ASSEMBLY. 2 L 7 2 4F RT A21EA 2007091800253 20070918 00253 EA 2007 9 18 COMA0760556 1 20070904 A 2621 365000183 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY LOW A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 963CA 20401 7127 FLIGHT 5570 - CARGO BOTTLE LOW MESSAGE ILLUMINATED IN FLIGHT TO GSO. AIRCRAFT DIVERTED TO IAD AND LANDED SAFELY. REMOV ED AND REPLACED CARGO FIRE BOTTLE. 2 L 7 2 4F RT A21EA 2007091800254 20070918 00254 EA 2007 9 18 COMA0760557 1 20070904 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF POSITION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 716CA 7250 FLIGHT 5354 - PAC DOOR HANDLE CAUTION MESSAGE AT 8000 FT DURING CLIMB. QRH PROCEDURE COMPLETED. AIRCRAFT RETURNED BACK TO CHS AND LANDED SAFELY. UPON ARRIVAL FOUND THE PAX DOOR OUTER HANDLE OUT. PERFORMED OPS CHECK OF PAX DOOR OUTER HAN DLE, WITH NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007091800256 20070918 00256 NM 2007 9 18 SWAA074473 1 20070907 A 3350 6556633 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 LEFT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007091800257 20070918 00257 NM 2007 9 18 SWAA074460 1 20070907 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 320, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091800260 20070918 00260 NM 2007 9 18 SWAA074465 1 20070907 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND STRINGER 8R CRACKED AT BS 344. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007091800262 20070918 00262 2007 9 18 SWAA074474 4 20070907 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007091800263 20070918 00263 2007 9 18 SWAA074484 4 20070908 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 618WN 28034 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007091800264 20070918 00264 2007 9 18 SWAA074489 4 20070909 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007091800265 20070918 00265 NM 2007 9 18 SWAA074469 1 20070907 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 793SA 27888 DURING SCHEDULED HC1 CHECK, FWD CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007091800269 20070918 00269 NM 2007 9 18 USAA920070819 1 20070907 A 5514 65C251563 FITTING BOEING 737 7373B7 1384580 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 23704 CLT - MAJOR REPAIR - C-5 CHECK, LEFT HAND HORIZONTAL STABILIZER CENTER SECTION THRUST BEAM CORNER FITTING CRACKED, STABI LIZER STATION 83.05. REPLACED LEFT HAND HORIZONTAL STABILIZER CENTER SECTION THRUST BEAM CORNER FITTING, STABILIZER STA TION 83.05 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007091800272 20070918 00272 SO 2007 9 18 C2XA07SH068 1 20070908 A 5751 14574000405 PLATE EMB 145 EMB145LR 3260212 SO RT AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13997 145298 SHV - DURING C-CHECK MAINTENANCE FOUND RIGHT UPPER SHROUD WITH CORRODED BONDING PLATE. MAINTENANCE REPAIRED RIGHT UPPER AILERON SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007091800275 20070918 00275 SO 2007 9 18 C2XA07IA199 1 20070907 A 3350 LIGHT EMB 145 EMB145EP 3260221 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15926 145005 IAH - FLIGHT 2806, DURING POST FLIGHT INSPECTION, THE MIDDLE EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENA NCE VERIFIED NORMAL OPERATION OF THE EMERGENCY LIGHT SYSTEM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007091800277 20070918 00277 SO 2007 9 18 C2XA07SH060 1 20070906 A 5210 14533333401 NUT PLATE EMB 145 EMB145EP 3260221 SO PAX DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14942 145037 SHV - DURING C-CHECK MAINTENANCE FOUND 4 NUT PLATES LOCATED AT BOTTOM OF MAIN DOOR CORRODED. MAINTENANCE REPAIRED NUT P LATES AT THE BOTTOM OF THE MAIN DOOR IAW EC 5210-01152 ORIG. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007091800278 20070918 00278 SO 2007 9 18 C2XA07SH061 1 20070906 A 5311 14526246003 FRAME EMB 145 EMB145EP 3260221 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14942 145037 SHV - DURING C-CHECK MAINTENANCE FOUND FRAME 65 WITH CORROSION UNDER CARGO DOOR HOLD OPEN ROD SUPPORT BRACKET. MAINTENA NCE REPAIRED CARGO DOOR HOLD OPEN ROD SUPPORT BRACKET IAW EC 5330-01719. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007091800280 20070918 00280 SO 2007 9 18 C2XA07SH063 1 20070906 A 5751 14573900403 PANEL EMB 145 EMB145EP 3260221 SO AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14942 145037 SHV - DURING C-CHECK MAINTENANCE FOUND LOWER AILERON SHROUDS BONDING STRIPS WITH CORROSION. MAINTENANCE REPAIRED LOWER AILERON SHROUD IAW EC5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007091800282 20070918 00282 EU 2007 9 18 07FDEA03631 1 20070913 A 5730 A57350104 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 CHAFING MARKS FOUND AROUND MANHOLE 9 APERTURE ON THE UPPER SURFACE OF THE BOTTOM WING SKIN PANEL NR 2 BETWEEN RIB 14-15, BOTH WINGS. REPAIR PERFORMED BY SMOOTH BLEND OUT, NDT INSPECTION FOR CRACK FREE AND FILLING BLEND LEVEL RESIN IAW EA 6 -5720-92205 AND RAS/BAE/1001697/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091800284 20070918 00284 SO 2007 9 18 C2XA07ON021 1 20070903 A 3397 M8372375R1624N CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN UNSECURE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19554 145587 FLT 524 - MCI TO RDU - DURING PREFLIGHT CK, FLIGHT CREW DISCOVERED THE EMERGENCY LIGHTS WILL NOT SHUT OFF. MX PERSONNEL INSPECTED AND FOUND CONNECTOR ON NR 3 EMERGENCY BATTERY NOT PROPERLY SECURED. MX PERSONNEL RESECURED AND OPERATIONALLY CHECK EMERGENCY LIGHTING SYS AGAIN AND ALL CHECKED GOOD. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE IN AIRWORTHY COND ITIONS. 2 L 7 2 4T RT T00011AT 2007091800287 20070918 00287 NM 2007 9 18 KCSA071339 1 20070910 A 5320 TIE CLIP BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-360 FRAME STR-7R HAS CRACKED TIE CLIP 1 INCH. 2 L 7 4 4F RT A20WE 2007091800288 20070918 00288 NM 2007 9 18 KCSA071340 1 20070910 A 5311 FRAME BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-360 FRAME CRACKED AT STR-3L CUTOUT. 2 L 7 4 4F RT A20WE 2007091800290 20070918 00290 NM 2007 9 18 KCSA071342 1 20070910 A 5311 FRAME BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-400 FRAME CRACKED AT STR-10L CUTOUT .5 INCH. 2 L 7 4 4F RT A20WE 2007091800292 20070918 00292 NM 2007 9 18 KCSA071344 1 20070910 A 5320 TIE CLIP BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-460 STR-9R TIE CLIP HAS A CRACK .75 INCH. 2 L 7 4 4F RT A20WE 2007091800293 20070918 00293 NM 2007 9 18 KCSA071345 1 20070910 A 5311 FRAME BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-480 FRAME CRACKED AT STR-12L CUTOUT .5 INCH. 2 L 7 4 4F RT A20WE 2007091800295 20070918 00295 NM 2007 9 18 KCSA071347 1 20070910 A 5311 FRAME BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-500 FRAME OUTER FLANGE CRACKED .25 INCH AT RIVET HOLE ABOVE STR-10L. 2 L 7 4 4F RT A20WE 2007091800296 20070918 00296 NM 2007 9 18 KCSA071348 1 20070910 A 5311 FRAME BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-520 FRAME OUTER FLANGE CRACKED AT RIVET HOLE BELOW STR-11R .25 INCH. 2 L 7 4 4F RT A20WE 2007091800300 20070918 00300 NM 2007 9 18 KCSA071352 1 20070910 A 5311 FRAME BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-520 FRAME CRACKED ON OUTER FLANGE BETWEEN STR-8L AND 9L. 2 L 7 4 4F RT A20WE 2007091800301 20070918 00301 NM 2007 9 18 KCSA071353 1 20070910 A 5311 FRAME BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-520 FRAME CRACKED AT STRINGER CUTOUT AT STR-10A/L. 2 L 7 4 4F RT A20WE 2007091900001 20070919 00001 EU 2007 9 19 07FDEA03774 1 20070914 A 5730 A57247714203 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 CHAFING DAMAGE AT ONE POSITION AND CRACK WITH DEFORMATION AT ANOTHER LOCATION ON FIXED LEADING EDGE D-NOSE SKIN RT, BETW EEN TRACK 3 AND TRACK 4. REPAIR PERFORMED BY BLENDING OUT DAMAGES AT BOTH POSITIONS, REMOVING FASTENER OF HOLE IN AREA OF CRACK WITH ROTOTEST TO INSURE THE CRACK DOES NOT PROPAGATE FROM THE OTHER SIDE AWAY FROM THE SKIN EDGE, AREAS NDT INS PECTED, ALL IAW EA 6- 5740-92207 AND RAS/BAE/1001695/2005 ISSUE B. 2 L 7 2 4F RT A35EU 2007091900004 20070919 00004 EU 2007 9 19 07FDEA03771 1 20070914 A 5320 A53973413200 COUPLING AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION AT COUPLING, C 70, P 37RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900005 20070919 00005 EU 2007 9 19 07FDEA03770 1 20070914 A 5320 A53974232201 COUPLING AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION AT COUPLING, C 65, P 56 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900007 20070919 00007 EU 2007 9 19 07FDEA03768 1 20070914 A 5511 A55176100 RIB AIRBUS 310 A310324 3930206 EU ZONE 300 MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 THS TIPS ON LT AND RT SIDE WERE DAMAGED AND SENT TO AN OUTSIDE VENDOR FOR REPAIR, SO TIPS FROM N812FD WERE CANNIBALIZED FOR USE ON N815FD, BUT THE THS RIB FASTENER HOLES MISMATCH TO TIP HOLES. REPAIR PERFORMED BY REPLACEMENT OF RIB ON LT A ND RT THS IAW EA 6-5514-92191A AND RAS/CASA/4427/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091900008 20070919 00008 EU 2007 9 19 07FDEA03767 1 20070914 A 5320 A53974228201 COUPLING AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION AT COUPLING P 55RH, C 65. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900010 20070919 00010 EU 2007 9 19 07FDEA03765 1 20070914 A 5340 A53974275203 FITTING AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION AF FITTING C 54.2, P 45-46 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900011 20070919 00011 EU 2007 9 19 07FDEA03764 1 20070914 A 5320 A53970709203 FITTING AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION AF FITTING C 54.2, P 45-46 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900012 20070919 00012 EU 2007 9 19 07FDEA03763 1 20070914 A 5415 A54611219 FITTING AIRBUS 310 A310324 3930206 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 CORROSION ON THE WHOLE LOWER SURFACE OF THE LT PYLON PYRAMID, FWD PYLON TO ENGINE ATTACH FITTING. REPAIR PERFORMED AS P ER SRM 54-51-81 BY BLENDING OUT CORROSION, REPROTECTION BY CADMIUM PLATING AND HIGH TEMPERATURE PAINT IAW EA 6-5451-9217 4 AND RAS 039464/014/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091900013 20070919 00013 EU 2007 9 19 07FDEA03761 1 20070914 A 5320 A53978048 ANGLE AIRBUS 310 A310324 3930206 EU ZONE 200 MISMANUFACTURED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 815FD 638 LESS EDGE MARGIN (5-6 MM) AT ANGLE, STR 26 RT BETWEEN FRAME 65-66 AND FRAME 67-68 AND ON LT BETWEEN FRAME 70-71, STRG 26 . IT'S IMPOSSIBLE TO INSTALL DAN5-6X FASTENERS DURING PTOF. REPAIR PERFORMED BY INSTALLING REPAIR ANGLE FABRICATED IN EFW-DRS (RE0074-201 AND RE0074-200) IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900020 20070919 00020 EU 2007 9 19 07FDEA03751 1 20070914 A 5320 A53973925200 COUPLING AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION FOUND AT COUPLING AT C 65, P 57 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900021 20070919 00021 EU 2007 9 19 07FDEA03750 1 20070914 A 5320 A53974228200 COUPLING AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION FOUND AT COUPLING AT C 65, P 55 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900024 20070919 00024 EU 2007 9 19 07FDEA03747 1 20070914 A 5320 A53770978222 COUPLING AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION FOUND AT COUPLING AT C 26/32, P 45 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900027 20070919 00027 EU 2007 9 19 07FDEA03738 1 20070914 A 5330 A53611658 PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 FOUND EXFOLIATION CORROSION ON FAIL/SAFE RING AT LOWER AFT CORNER OF FWD PAX DOOR RT, FRAME 15-16A. REPAIR PERFORMED BY REWORK, NDT INSPECTION AND FILLING THE REWORKED AREA WITH SEALANT IAW EA 6-5312-92165 AND RAS/AS/0181/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091900028 20070919 00028 EU 2007 9 19 07FDEA03732 1 20070914 A 5320 A53771460200 STRAP AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 DAMAGED SEALING STRAP AT FWD CARGO DOOR CUT OUT, FRAME 25A RT, OUT OF LIMIT IAW SRM 51-10-10. REPLACEMENT OF STRAP IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900031 20070919 00031 EU 2007 9 19 07FDEA03728 1 20070914 A 5753 A57970371 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 FOUND DELAMINATION ON CORE FILLER AT TRAILING EDGE SKIN OF INBOARD FLAP RT. DELAMINATED CORE FILLER REPAIRED IAW SRM 57 -53-12/FIG 209/SH 2/VERSION 3. 2 L 7 2 4F RT A35EU 2007091900033 20070919 00033 EU 2007 9 19 07FDEA03726 1 20070914 A 5320 A53974341200 FLOOR SUPPORT AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 FOUND CORROSION ON LONGITUDINAL PROFILE BETWEEN FRAME 63-64, Y-805 RT, AFT CARGO COMPARTMENT FLOOR STRUCTURE. REPLACE MENT OF LONGITUDINAL PROFILE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900035 20070919 00035 EU 2007 9 19 07FDEA03724 1 20070914 A 5310 A53997308 BEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 FOUND CORROSION ON AFT CARGO DOOR SILL BEAM BETWEEN FRAME 59-59A. SILL BEAM REPAIR PERFORMED BY CUT OUT AND INSTALLING A FILLER IAW SRM 53-17-18/FIG 202, APPROVED BY EA 6-5317-92153 AND RAS/DATLS/0002685/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091900038 20070919 00038 NM 2007 9 19 07FDEA03668 1 20070913 A 5230 SEAL BOEING 727 727277 138408S NM CARGO DOOR FAILED A FDEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 244FE 21647 AT FL250, CABIN ALT HORN WENT OFF. RAN QRH REGAINED PRESS WITH CARGO OUTFLOW CLOSED. MECHANIC STATED LOWER CARGO DOOR SEAL FAILURE. FOUND THE LWR FWD CARGO DOOR SEAL ON THE LOWER EDGE PUSHED UNDER. LEFT SEAL AS IT WAS FOUND FOR FURTHER EVALUATION. SECURED DOOR SEAL AS NEEDED IAW SMP. PRESSURIZED A/C WITH RIGHT HAND PACK ONLY TO 3.0 PSI, NO DEFECTS NOT ED, NO LEAKS FOUND ON DOORS. ACCOMPLISHED EXCESSIVE CABIN PRESSURE LEAKAGE TEST IAW B727 JRH. FOUND TO BE WELL WITHIN LIMITS PER TEST AND PG 8-29, FIGURE 6. OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2007091900039 20070919 00039 NM 2007 9 19 07FDEA03664 1 20070913 A 5720 6521655 BRACKET BOEING 727 727233 138408A NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 UPPER TRAILING EDGE PANEL BRACKET IS CRACKED ABOVE ACTUATOR REMOVED AND REINSTALLED UPPER WING ROOT PANEL AT TRAILING E DGE. REMOVED AND REINSTALLED NR 8 SPOILER MOUNT. REMOVED AND REPLACED TRAILING EDGE PANEL BRACKET REPLACED STIFFENER S ON PANEL BRACKET, AND INSTALLED PANEL. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007091900041 20070919 00041 EU 2007 9 19 07FDEA03723 1 20070830 A 5230 A5237803920000 DOOR FRAME AIRBUS 310 A310222 3930315 EU ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 BULK CARGO COMPARTMENT DOOR FWD LOWER CORNER WITH CRACK ON EDGE MEMBER. DOOR FWD LOWER CORNER EDGE MEMBER WAS REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091800010 20070918 00010 NM 2007 9 18 UPS07M50600 1 20070722 A 5744 HINGE DOUG MD11 MD11F 3023600 NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C LEFT WING O/B FLAP I/B HINGE (WING MOUNTED), O/B LOWER ATTACHMENT SPOT FACES 02 EA FOUND CORROSION AS MARKED. AFFECTED AREA O/B HOLE SPOTFACE CORR REMOVD & FOUND EXCEED LIMIT CMM57- 44-08 PG 602-607 R58. ORG THK 0.482" R EMN THK 0.462" MIN ALLOW THK 0.72 0" MATL REMVD 0.020". FPI C/O DAC NDTSPM R13 PART 8. NO CORR & CRACK EVIDENT. O/B H OLE SPOTFACE THK 0.462" EVAL & FOUND ACCEPTED. REWORKED AREA ETCH INSPECT, FOUND SATISFACTORY BSOPM20-11-02R58. FLAP P EENING CARRIED OUT. 2 L 7 3 4F RT A22WE 2007091800011 20070918 00011 EU 2007 9 18 07FDEA03641 1 20070913 A 5320 A25574555000 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 CRACKED ATTACHMENT HOLES IN CORNER PROFILE AT FRAME 25A BETWEEN STRG 28-34 RT. REPLACEMENT OF CORNER PROFILE IAW SRM 51 -72-10 AND PTOF DRW, R255B0061. 2 L 7 2 4F RT A35EU 2007091800013 20070918 00013 EU 2007 9 18 07FDEA03642 1 20070913 A 5320 A25574555000 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 CRACKED ATTACHMENT HOLES IN CORNER PROFILE AT FRAME 25A BETWEEN STRG. 28-34 RT. REPLACEMENT OF CORNER PROFILE IAW SRM 5 1-72-10 AND PTOF DRW, R255B0061. 2 L 7 2 4F RT A35EU 2007091800014 20070918 00014 EU 2007 9 18 07FDEA03644 1 20070913 A 5320 A53978048 ANGLE AIRBUS 310 A310324 3930206 EU ZONE 100 MISMANUFACTURED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 812FD 467 LESS EDGE MARGIN (5-6 MM) AT ANGLES STRG 26 RT AT FRAME 69 AND STRG 26 LT FRAME 63 AND 65. IT'S IMPOSSIBLE TO INSTALL D AN5-6X OR DAN5-8 FASTENER DURING PTOF. REPAIR PERFORMED BY INSTALLING REPAIR ANGLES FABRICATED IN EFW-DRS (RE0074-201/R E0074-200) IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091800015 20070918 00015 EU 2007 9 18 07FDEA03646 1 20070913 A 5310 A53980070 BEAM AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CRACK ON LONGITUDINBAL BEAM C 74-76, P 11 LT/RT, (LT: 8MM, RT 15MM). REPAIR PERFORMED BY INSTALLING REPAIR ANGLES IAW SRM 53-181-18 FIG 204. 2 L 7 2 4F RT A35EU 2007091800031 20070918 00031 SO 2007 9 18 C2XA07RI073 1 20070831 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 48901 145501 RIC - MX - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY LIGHT ON SEAT 12A INOP. MX REMOVED THE EMERGENCY LIGHT ASSEMB LY AND FOUND CONNECTOR LOOSE. MX RESECURED CONNECTOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED T O RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007091800048 20070918 00048 EA 2007 9 18 TRAX200701312 1 20070905 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 834AS 7254 AAR - EXTERIOR PLACARD ON ESCAPE HATCH -EMERGENCY EXIT PUSH- IS WORN. 2 L 7 2 4F RT A21EA 2007091800083 20070918 00083 NE 2007 9 18 CNMA20070001 2 20070103 A 7230 COMPRESSOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2B 30018 NE ENGINE DAMAGED A CNMA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 07 720AX 48252 517533 NR 2 ENGINE FAILED ON TAKEOFF ROLL AT 70KTS TAKEOFF ABORTED. N1 WAS 103.0 EGT PEGGED. RAN ENGINE FIRE SEVERE DAMAGE CHEC K LIST NO FIRE. R & R NR 2 ENGINE IAW 10UN-201. ENGINE S/N 517-533 INSPECTION REVEALED NO SIGNS OF FOD TO THE COMPRESS OR SECTION BUT HEAVY IMPACT DAMAGE EXTENDING TO STG 4 LPT. 5 EA STAGE 1 NOZZLE SEGMENTS HAD LOST RETENTION AND HAD GONE IN CONTACT WITH THE STAGE 1 ROTOR BLADES. 2 L 7 3 4F 4 F A22WE E23EA 2007091800084 20070918 00084 NE 2007 9 18 CNMA20070014 2 20070715 A 7261 FFG022AC GOVERNOR BOEING 757 757200 1384950 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE LEAKING A CNMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 639AX 24528 LT ENGINE OIL CONSUMPTION HIGH BETWEEN 1.6 AND 3 QUARTS PER HOUR PRESS NORMAL. REMOVED AND REPLACED O-RING FOR ENG SPLIN E AND GEAR BOX SPLINE. RAN ENG AND FOUND TO BE LEAKING OUT OF ENG SPLINE CAVITY DRAIN AT ABOUT 10 DROPS PER SEC MSLP. REMOVED AND REPLACED GEARBOX ON NR1 ENG IAW MM 72-60-61. REMOVED AND REPLACED NR 1 ENG FFG IAW MM 73-21-01. FFG SHOP R EPORT CONFIRMED REASON FOR REMOVAL FOUND SMALL FLANGED BEARING TO BE (LOOSE). 2 L 7 2 4F 4 F RT A2NM E12EU 2007091800085 20070918 00085 WP 2007 9 18 CNMA20070004 1 20070125 A 5210 23111384 BOTTLE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2B 30018 NE NR 3 DOOR EMPTY A CNMA K NONE L NO TEST IN INSP/MAINT 1 SW 07 240NW 48319 NR 3 LT DOOR FAILED TO OPEN PNEUMATICALLY IN EMERGENCY OPERATION CHECK. NR3 LT DOOR EMERGENCY PNEUMATIC STORAGE BOTTLE REPLACED IAW MM 52-17-06. 2 L 7 3 4F 4 F A22WE E23EA 2007091800086 20070918 00086 NM 2007 9 18 2007UALA03519 1 20070903 A 5610 WINDOW BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT CRACKED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 516UA 24860 L1 WINDOW SHATTERED IN FLIGHT WITH ARCING AT BOTTOM OF WINDOW. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091800087 20070918 00087 EU 2007 9 18 BAQA200700029 1 20070813 A 5512 SKIN AEROSP AS355 AS355F 8680806 EU HORIZONTAL STAB CRACKED E BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 652PM 9729 5179 DURING 500 HOUR AIRFRAME INSPECTION FOUND A CRACK IN THE SKIN OF THE HORIZONTAL STABILIZER. REMOVED AND REPLACED THE HO RIZONTAL STABILIZER. 1 G 7 2 3U H11EU 2007091800089 20070918 00089 CE 2007 9 18 DJFA2007098 1 20070823 A 2611 FIRE WARNING RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP CARGO BAY FALSE INDICATION E DJFA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 23 725TA 258297 DURING CLIMB OUT CREW REPORTED BAGGAGE FIRE LIGHT ILLUMINATED INTERMITTENTLY. AIRCRAFT RETURNED TO FIELD WITHOUT INCIDE NT. MAINTENANCE PERFORMED A FUNCTIONAL CHECK OF THE SYSTEM AND WAS UNABLE TO DUPLICATE THE DISCREPANCY. 2 L 7 2 4F 4 F RT A3EU E6WE 2007091800090 20070918 00090 SW 2007 9 18 AC2A117289 1 20070831 A 7740 23054163 PICKUP BELL 430 430 1182150 SW ALLSN 250C 250C40B 03032 NE NR 1 ECU INOPERATIVE E AC2A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 07 430CF 49188 NR 1 ECU FAILED FIXED FLOW. AIRCRAFT WAS REPOSITIONING FOR TAKEOFF, AT A HOVER, THEN SET LIGHT ON SKIDS, PLACED INTO MA NUAL MODE, THROTTLE REDUCED, SET FULL ON GROUND AND SHUTDOWN WITH NO FUTHER ISSUES. 1 G 7 2 3U 3 U RT H9SW E1GL 2007091800097 20070918 00097 NM 2007 9 18 2007UALA03523 1 20070831 A 5320 FLOOR SUPPORT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 FLOOR SUPPORT HAS CORROSION AT SEVERAL PLACES ON UPPER SURFACE BS 767-827 STR 25R, RBL 14. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800107 20070918 00107 NM 2007 9 18 2007UALA03528 1 20070831 A 5743 BUSHING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LT MLG CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 LEFT MLG BEAM OUTBOARD BUSHING BORE HAS CORROSION ON THE INSIDE DIAMETER FWD END. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800117 20070918 00117 NM 2007 9 18 2007UALA03535 1 20070831 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 545UA 25323 CEILING EMERGENCY EXIT LIGHT AT SEAT 12ABC INOP WHEN EMERGENCY LIGHTS SELECTED ON. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091800129 20070918 00129 NE 2007 9 18 2007UALA03539 2 20070904 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 OIL CONSUMPTION A UALA O OTHER O OTHER CR CRUISE 1 WP 29 491UA 1741 V10483 NR 1 ENGINE HIGH OIL CONSUMPTION EXCEEDS LIMIT. FOUND NR 5 BEARING SEAL LEAK. REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007091800156 20070918 00156 EU 2007 9 18 07FDEA03680 1 20070913 A 5330 A53778629 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 815FD 638 FOUND OLD EXTERNAL DOUBLER REPAIR ON FUSELAGE SKIN BETWEEN FRAME 34-35, STRG 42-44 RT, NOT CONFORM TO REPAIR DRW R537-06 202 ISSUE B AND RAS/DABRE/1540.1/96 ISSUE A. REPAIR REMOVED, SKIN CUT AND NEW DOUBLER INSTALLED IAW EA 6-5314-92180A AN D RAS/DABRE/7005554/2005 ISSUE B. 2 L 7 2 4F RT A35EU 2007091800157 20070918 00157 EU 2007 9 18 07FDEA03679 1 20070913 A 5521 SPAR AIRBUS 310 A310203 3930313 EU RT ELEVATOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION FOUND ON RT ELEVATOR FRONT SPAR WEB NEAR RIB 2A AROUND ONE BONDING POINT REPAIR PERFORMED BY BLENDOUT UNTIL CO RROSION REMOVAL IAW EA 6-5520-79603 AND RAS/CASA/3692/2004 ISS A. 2 L 7 2 4F RT A35EU 2007091800158 20070918 00158 NM 2007 9 18 07FDEA03677 1 20070913 A 5330 SKIN BOEING 727 727233 138408A NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 AFT LOWER FUSELAGE STA 1183 BETWEEN STR 27L AND 29L SKIN DAMAGED. AFTER REMOVAL OF SKIN, FOUND TAIL SKID DRAG LINK HING E FITTING HAS A DRILL START, (HIDDEN DAMAGE) ON LT SIDE OF JACK CUTOUT. REMOVED DAMAGED HINGE FITTING, DRILLED UP AND I NSTALLED NEW FITTING, REF SRM 51-30-2 ,OPS CK'D TAIL SKID, REF MM 32-71-001. 2 L 7 3 4F RT A3WE 2007091800159 20070918 00159 EU 2007 9 18 07FDEA03676 1 20070913 A 5330 A53985240204 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 CORROSION PITS ON TOP SKIN PANEL BETWEEN FRAME 80-95, STRG 6 RT TO 6 LT. REPAIR PERFORMED BY REWORK AND FLAP PEENING IAW EA 6-5319-92157 AND RAS/DAHAM/4019752/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091800160 20070918 00160 EU 2007 9 18 07FDEA03675 1 20070913 A 5414 A54611752 SKIN AIRBUS 310 A310203 3930313 EU ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND ON PYLON NR 1 AT RIB 8 INBOARD AND OUTBOARD SIDE THE HOLE FOR SUPPORT WORN DOUBLER REPAIR PERFORMED IAW SRM 54-51- 31 FIG 201. 2 L 7 2 4F RT A35EU 2007091800161 20070918 00161 EU 2007 9 18 07FDEA03674 1 20070913 A 5540 R55370209018 HINGE FITTING AIRBUS 310 A310324 3930206 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 CORROSION ON AFT LUG OF HINGE FITTING NR 5 AND CHAFING MARKS INSIDE ATTACH, OUT OF LIMIT. REPAIR PERFORMED BY REPLACEME NT OF HINGE FITTING NR 5 IAW AMM 55-36-46 AND BLEND OUT SCRATCHES WITH FLAP PEENING INSIDE HINGE FITTING ATTACH IAW SRM 51-29-00. 2 L 7 2 4F RT A35EU 2007091800163 20070918 00163 EU 2007 9 18 07FDEA03673 1 20070913 A 5720 A57150784001 FITTING AIRBUS 310 A310203 3930313 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 AT RT SPIGOT FITTING FWD OUTBOARD SIDE FOUND WEAR MARKS REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5720-79 605 AND RAS/BAE/0818/2004 ISS A. 2 L 7 2 4F RT A35EU 2007091800164 20070918 00164 EU 2007 9 18 07FDEA03671 1 20070913 A 5415 A54611031 ATTACH FITTING AIRBUS 310 A310203 3930313 EU ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CHAFING MARKS, ENLARGED HOLES AND NOT CORRECT INSTALLED BUSHINGS AT PYLON NR 2 PYLON TO WING ATTACH FITTING LUGS A T RIB 12. REPAIR PERFORMED BY OVERSIZING THE BORES AND INSTALLING NEW REPAIR BUSHS IAW DRAWING R571-40283, APPROVED BY EA 6-5450-81064 AND RAS /BAE/0929/2004 ISS A. 2 L 7 2 4F RT A35EU 2007091800166 20070918 00166 EU 2007 9 18 07FDEA03667 1 20070913 A 5340 A53610607206 FITTING AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION AT RUN OUT FITTING AT P 44, C16A-17A LT. REPAIR PERFORMED BY REPLACEMENT OF RUNOUT FITTING IAW DRAWING R536-10440. 2 L 7 2 4F RT A35EU 2007091800167 20070918 00167 EU 2007 9 18 07FDEA03666 1 20070913 A 5330 A53989210201 SKIN PANEL AIRBUS 310 A310203 3930313 EU ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND DENT ON SKIN C 94-95, P3-4 RT OUT OF LIMIT. DOUBLER REPAIR PERFORMED IAW SRM 53-19-12 FIG 201. 2 L 7 2 4F RT A35EU 2007091800168 20070918 00168 NM 2007 9 18 07FDEA03665 1 20070913 A 5330 65259953 SKIN BOEING 727 727233 138408A NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 AFT LOWER FUSELAGE, STA 1183 BETWEEN STR 27L AND 29L, SKIN PANEL AT FWD EDGE OF TAIL STAND COMPARTMENT IS DEFORMED AND H AS NUMEROUS LOOSE/WORKING FASTENERS REMOVED TAIL STAND DOOR AND SURROUNDING STRUCTURE, DRAG LINK, FABRICATED SKIN PANEL FILLER AND SKIN ATTACH ANGLE, DRILLED UP PARTS, TREATED AND PRIMED. INSTALLED SKIN ATTACH ANGLE FILLER, AND REPLACEMENT SKIN REF EA NR 7-5330-7-113086, REV A. 2 L 7 3 4F RT A3WE 2007091800169 20070918 00169 EU 2007 9 18 07FDEA03663 1 20070913 A 5320 A53973599210 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 FOUND MISDRILLED HOLE IN CORNER FITTING ADJACENT AND LESS MARGIN TO ROLLER TRACK HOLE, FRAME 60, CARGO FLOOR STRUCTURE, Y1460 LT. REPAIR PERFORMED BY CREATING AN OBLONG HOLE AND INSTALLING FASTENER WITH STRENGTHENING PLATE IAW 6-5317-95859 AND RAS/DAHAM/4020259/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091800170 20070918 00170 EU 2007 9 18 07FDEA03662 1 20070913 A 5210 A53610655 DOOR FRAME AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 TOOLING IMPACTS FOUND ON DOOR FRAME 14 UNDER DOOR STOP 8 LH, PAX DOOR 1. REPAIR PERFORMED BY SMOOTH BLEND OUT, DVI INSPE CTING OF FASTENER HOLES AND HFEC INSPECTION OF BLENDED AREAS FOR CRACK FREE CONDITION IAW EA 6-5312-95486 AND RAS 041687 /013/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091800171 20070918 00171 EU 2007 9 18 07FDEA03661 1 20070913 A 5313 A53974267203 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION ON STRINGER P 56 RT, C 64-65 OUT OF LIMIT STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007091800177 20070918 00177 NM 2007 9 18 2007UALA03551 1 20070901 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 UPPER FUSELAGE DORSAL FIN SKIN HAS AREAS OF CHAFING FROM BS 860 AND BEYOND. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800190 20070918 00190 NM 2007 9 18 2007UALA03561 1 20070903 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 649UA 25286 EEL LIGHT INOP LOCATED AT FIRST CLASS ZONE RIGHT AISLE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007091800208 20070918 00208 NM 2007 9 18 2007UALA03576 1 20070904 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 570UA 26678 EEL LIGHT AT MID LAV INOP AND CARPETED OVER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091800242 20070918 00242 NM 2007 9 18 UPS07550625 1 20070803 A 5311 146N102848 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 415UP 23855 INSPECTION TYPE:C DENTS IN AFT CARGO FUSELAGE FRAME STA 1220, APPROX BETWEEN S25L AND S26L (3EA). REPAIR AT STA 1220, S 25L AND S26L (3EA) ACCOMPLISHED PER EA 757-5362- 27-A1724 AND UPS EO B757-5310-27480-A WITH NO DEVIATIONS. 2 L 7 2 4F RT A2NM 2007091800243 20070918 00243 NM 2007 9 18 UPS07550626 1 20070803 A 5311 146N102847 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 415UP 23855 INSPECTION TYPE:C DENTS IN AFT CARGO FUSELAGE FRAME STA 1280, APPROX BETWEEN STRINGER 25L AND S26L (3EA). REPAIR AT STA 1280 S25L AND S26L HAS BEEN ACCOMPLISHED PER PRELIMINARY NR 2 AND THE FINAL EA 757-5362-22-A1722 AND UPS EO B757-5310-2 7570-A. 2 L 7 2 4F RT A2NM 2007091800248 20070918 00248 SO 2007 9 18 C2XA07RI075 1 20070904 A 3350 78241 INVERTER EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 12934 145019 FLIGHT 2248 - EWR - CREW REPORTED EMERGENCY LIGHTS INOPERATIVE. EWR MX REMOVED AND REPLACED EMERGENCY LIGHT INVERTER NR 6 IAW EMB 145 AMM 33-50-11 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007091800251 20070918 00251 EA 2007 9 18 COMA0760554 1 20070902 A 2697 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA FIRE BOTTLE LOOSE A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 963CA 7127 FLIGHT 5005 - CARGO BOTTLE LOW MESSAGE. QRH FOLLOWED AND A/C DIVERTED TO BWI AND LANDED SAFELY. FOUND CONNECTOR LOOSE ON CARGO BOTTLE, RESECURED CONNECTOR, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007091800258 20070918 00258 NM 2007 9 18 SWAA074471 1 20070907 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007091800271 20070918 00271 SO 2007 9 18 C2XA07SH066 1 20070908 A 5751 14573900403 PLATE EMB 145 EMB145LR 3260212 SO LT AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13997 145298 SHV - DURING C-CHECK LEFT LOWER AILERON SHROUD HAS CORRODED BONDING PLATE. MAINTENANCE REPAIRED LEFT LOWER AILERON SHRO UD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007091800274 20070918 00274 SO 2007 9 18 C2XA07SH065 1 20070908 A 5320 14530642401 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13997 145298 SHV - DURING C-CHECK MAINTENANCE FOUND LEFT OMEGA BEAM WITH CORROSION BETWEEN FRAMES 19 & 23. MAINTENANCE REPAIRED LEFT OMEGA BEAM AT FRAME 20 IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007091800279 20070918 00279 SO 2007 9 18 C2XA07SH062 1 20070906 A 5730 14571502407 PANEL EMB 145 EMB145EP 3260221 SO WING CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14942 145037 SHV - DURING C-CHECK MAINTENANCE FOUND PNL 193 BONDING STRIPS WITH CORROSION. MAINTENANCE REPAIRED PNL 193 BONDING STRI PS IAW EC 5750-01315 REV D. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007091800283 20070918 00283 2007 9 18 C2XA07IA198 4 20070905 A 2300 313202 SWITCH EMB 145 EMB145LR 3260212 SO COCKPIT SHORTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 18982 145223 IAH - DURING MAINTENANCE INSPECTION THE CAPTAINS GLARESHIELD PUSH TO TALK SWITCH SHOCKED AND SMOKED WHEN DEPRESSED. MAI NTENANCE REMOVED AND REPLACED THE AFFECTED SWITCH, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007091800289 20070918 00289 NM 2007 9 18 KCSA071341 1 20070910 A 5311 FRAME BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-360 FRAME OUTER FLANGE CRACKED AT RIVET HOLE .5 INCH BETWEEN STR-1R AND STR-2R. 2 L 7 4 4F RT A20WE 2007091800291 20070918 00291 NM 2007 9 18 KCSA071343 1 20070910 A 5311 FRAME BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-420 FRAME CRACKED AT STR-10L TO STR-11L. 2 L 7 4 4F RT A20WE 2007091800294 20070918 00294 NM 2007 9 18 KCSA071346 1 20070910 A 5311 FRAME BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-500 FRAME CRACKED AT STR-11L CUTOUT .75 INCH. 2 L 7 4 4F RT A20WE 2007091800299 20070918 00299 NM 2007 9 18 KCSA071351 1 20070910 A 5311 FRAME BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-520 FRAME CRACKED ON OUTER FLANGE AT RIVET HOLE ABOVE STR-9R .25 INCH. 2 L 7 4 4F RT A20WE 2007091800303 20070918 00303 NM 2007 9 18 SCNA07011 1 20070909 A 3350 BALLAST BOEING 737 7378Q8 13844BX NM CABIN FAULTY A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 804SY 30689 MAINTENANCE FOUND LEFT FWD EMERGENCY EXIT SIDEWALL LIGHT INOP. MAINTENANCE REPLACED THE BALLAST FOR THE LIGHT. 2 L 7 2 4F RT A16WE 2007091900003 20070919 00003 EU 2007 9 19 07FDEA03772 1 20070914 A 5315 A53974219 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 HEAVY CORROSION ON CROSSBEAM FRAME 63 LT, Y1110 AND Y1160 IN AFT CARGO COMPARTMENT FLOOR STRUCTURE. CROSSBEAM SPLICE REPAIR PERFORMED IAW SRM 53-10-15/FIG 207. 2 L 7 2 4F RT A35EU 2007091900014 20070919 00014 EU 2007 9 19 07FDEA03757 1 20070914 A 5320 A53778338242 PLATE AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 CRACKED SHEAR PLATE BETWEEN FRAME 32-33, STRG 44 RT. REPLACEMENT OF SHEARPLATE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900015 20070919 00015 EU 2007 9 19 07FDEA03756 1 20070914 A 5320 A53973330202 COUPLING AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION ON COUPLING P 50 RH, C 69. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900016 20070919 00016 EU 2007 9 19 07FDEA03755 1 20070914 A 5415 A54640927500 FITTING AIRBUS 310 A310324 3930206 EU ZONE 400 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 GOUGE AT AFT PYLON TO ENGINE FITTING, RT PYLON. REPAIR PERFORMED BY SMOOTH BLEND OUT TO ELIMINATE SHARP EDGES AND REPRO TECTION AS PER SRM WITH CADMIUM PLATING AND HIGH TEMPERATURE PAINT IAW EA 6-5451-92173 AND RAS 039403/010/2005. 2 L 7 2 4F RT A35EU 2007091900019 20070919 00019 EU 2007 9 19 07FDEA03752 1 20070914 A 5320 A53981113 PLATE AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 HEAVY CORRODED AND CRACKED SHEAR PLATES BETWEEN FRAME 79-80, STRG 26 LT AND RT. REPLACEMENT OF SHEAR PLATES LT AND RT I AW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900022 20070919 00022 EU 2007 9 19 07FDEA03749 1 20070914 A 5320 STRAP AIRBUS 310 A310222 3930315 EU R1 DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 446FE 224 AREA IS RT FWD PAX/CREW DOOR CUTOUT. 1 1/8 INCH CRACK WITH POSSIBLE EXFOLIATION CORROSION EXISTS ALONG TOP EDGE OF FWD CORNER STRAP, BEGINNING APPROX 1 1/8 INCH FROM AFT EDGE OF CORNER STRAP, LOWER, FWD CORNER OF DOOR CUTOUT BEHIND FAILS AFE RING. AREA MARKED IN RED. FOUND USING HFEC INSPECTION. 09-20-07 REMOVED FWD TAPERED SHIM (CORNER STRAP) IAW FE DEX A310-200 SRM 51-40-21 PARA 7. INSTALLED TAPERED SHIM IAW FEDEX A310-200 SRM 51-40-21 PARA 7. MAJOR REPAIR 2 L 7 2 4F RT A35EU 2007091900029 20070919 00029 EU 2007 9 19 07FDEA03730 1 20070914 A 5320 A53989395221 ANGLE AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 FOUND CORRODED ANGLE AT FRAME 101 REAR SIDE OF FIREWALL, STRG 5 RT. REPLACEMENT OF ANGLE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900036 20070919 00036 WP 2007 9 19 07FDEA03706 1 20070913 A 5522 2024CT3 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 399FE 48262 LEFT OUTBOARD ELEVATOR UPPER SKIN BULGE/CRACKED AND CORRODED 1.5" FROM INBOARD END AND 2 FEET FROM TRAILING EDGE. REMO VED ENTIRE DAMAGED UPPER SKIN SECTION, APPROXIMATELY 18" TIMES 24", REQUIRED FOR DISCREPANCY CLEAN-UP AND REPAIRED IAW MD/DC10-10 SRM 55-10-00 FIG,8 VOL, 1. CALCULATED NEW WEIGHT AND BALANCE FOR LEFT OUTBOARD ELEVATOR AT 892.77 TAIL HEAVY INCH POUNDS, FOUND TO BE WITHIN LIMITS IAW MD/DC10 SRM 55-20-00 PAGE 1, PARAGRAPH 1A, VOL 11. 2 L 7 3 4F RT A22WE 2007091900044 20070919 00044 EU 2007 9 19 07FDEA03720 1 20070828 A 5330 A53981600201 SKIN AIRBUS 310 A310222 3930315 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 PREVIOUS REPAIR FOUND LOCATED ON RT FUSELAGE FR78 STA 4241 STRG 24-27 RT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR AN D IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO SONFORM TO AN SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 53-10-12 FIG 225 SHEET 1. 2 L 7 2 4F RT A35EU 2007091900045 20070919 00045 EU 2007 9 19 07FDEA03719 1 20070827 A 5753 A57970362200 SKIN AIRBUS 310 A310222 3930315 EU ZONE 600 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 PREVIOUS REPAIR FOUND LOCATED ON RT FLAP INBD LOWER SKIN, NEAR TRACK NR 2. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR D ETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SR M REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 57-52-12 FIG 205. 2 L 7 2 4F RT A35EU 2007091900046 20070919 00046 EU 2007 9 19 07FDEA03718 1 20070825 A 5330 A53978157200 SKIN AIRBUS 310 A310222 3930315 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 PREVIOUS REPAIR FOUND LOCATED ON RT FUSELAGE AFT BULK DOOR STA 3726/3779, FR 69-70, STRG 41-43 RT. REPAIR REQUIRES EVAL UATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND F OUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 53-10-12 FIG 224 SHEET1. 2 L 7 2 4F RT A35EU 2007091900050 20070919 00050 EU 2007 9 19 07FDEA03714 1 20070824 A 5347 A5381114400100 DUMMY RAIL AIRBUS 310 A310222 3930315 EU ZONE 100 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 DUMMY TRACK NR 6 RT BETWEEN FR 54 AND 54.2 WITH WEAR OF 1.1MM AT AFT ATTACHMENT HOLES. DUMMY TRACK REPAIRED IAW SRM 53- 15-16, FIG 203. 2 L 7 2 4F RT A35EU 2007091900051 20070919 00051 EU 2007 9 19 07FDEA03713 1 20070821 A 5330 A53610320201 SKIN AIRBUS 310 A310222 3930315 EU ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 FUSELAGE DENT BETWEEN FR 10A AND FR 11 AT 300MM TO THE RIGHT OF CENTERLINE, AT Z 2120. IT WAS REPAIRED IN ACCORDANCE WI TH SRM 53-12-12 FIG 201 SHEET 1. 2 L 7 2 4F RT A35EU 2007091900052 20070919 00052 EU 2007 9 19 07FDEA03712 1 20070821 A 5330 A53610320201 SKIN AIRBUS 310 A310222 3930315 EU ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 FUSELAGE DENT BETWEEN FR10A AND FR11 AT 300MM TO THE RIGHT OF CENTERLINE, AT Z 2120. IT WAS REPAIRED IN ACCORDANCE WITH SRM 53-12-12 FIG 201 SHEET 1. 2 L 7 2 4F RT A35EU 2007091900053 20070919 00053 NM 2007 9 19 07FDEA03711 1 20070913 A 5311 651592833 FRAME BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FLOORBEAM T-CAP CORRODED STA 560, LBL 2-25 BLENDED AREA, MAPPED OUT DAMAGE, REF SRM 51-10-6. REMOVED OLD FLOORBEAM REPA IR REF SRM 51-30-02. REMOVED AND REINSTALLED WEB AT STA 560-580, BL 0, REF SRM 51-30-02. REMOVED AND REINSTALLED WEB A ND ATTACH BRACKETS AT STA 560-580, LBL 25. REMOVED AND REINSTALLED SEAT TRACK AND SEAT TRACK STRAPS STA 480-600, BL 0. FABRICATED T-CAP AND REPAIR ANGLES REF DWG SR2753-034 REV F. REPAIR ANGLE HEAT TREATED AND CAD PLATED, TREATED AND PRI MED T-CAP, PRIMED REPAIR ANGLES. INSTALLED T-CAP AND REPAIR ANGLES REF DWG SR27-53-034 REV F. 2 L 7 3 4F RT A3WE 2007091900054 20070919 00054 EU 2007 9 19 07FDEA03710 1 20070818 A 5330 A53610945200 SKIN AIRBUS 310 A310222 3930315 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 N00180 STATIC DISCHARGE PEAK SITUATED BETWEEN FR2 AND FR3 NEXT TO Z-1051. IT WAS REPAIRED IN ACCORDANCE WITH 53-10-12 F IG 221, SHEET 1. 2 L 7 2 4F RT A35EU 2007091900056 20070919 00056 NM 2007 9 19 07FDEA03708 1 20070913 A 5320 BAC1509100146 FLOOR SUPPORT BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FWD PIT, CARGO FLOOR SUPPORT, HAS CORROSION AROUND NUTPLATED AT BS 640-646, RBL 3" REMOVED CORROSION REF SRM 51-10-2. O RIGINAL MATERIAL THICKNESS .071", AFTER BLEND .010 MATERIAL REMOVED FOR A REMAINING THICKNESS OF .061 AND IS OUT OF LIMI TS REF SRM 53-10-1. FABRICATED REPAIR PARTS SRM 53-10-5 AND INSTALLED REPAIR REF SRM 53-10-5 AND SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007091900057 20070919 00057 EU 2007 9 19 07FDEA03707 1 20070913 A 5320 A53778807202 FLANGE AIRBUS 310 A310203 3930313 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUR MISDRILLED HOLES AT UPPER FLANGE (BEAM) AT C 33 LT. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 2007091900058 20070919 00058 EU 2007 9 19 07FDEA03705 1 20070913 A 5320 A53778807202 FLANGE AIRBUS 310 A310203 3930313 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 TWO MISDRILLED HOLES AT UPPER FLANGE (BEAM) AT C 33 LT. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 2007091900062 20070919 00062 EU 2007 9 19 07FDEA03701 1 20070913 A 5320 A53611674200 SPLICE AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION AT SPLICE C20, P50 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900063 20070919 00063 EU 2007 9 19 07FDEA03700 1 20070913 A 5320 A53611673200 SPLICE AIRBUS 310 A310203 3930313 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION AT SPLICE C20, P46 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900066 20070919 00066 EU 2007 9 19 07FDEA03697 1 20070913 A 5712 A57242444 RIB AIRBUS 310 A310203 3930313 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND ON LT MLG FWD LUG INNER BORE RIB 5 THE BUSHING TO BE OUT OF ROUND, AFTER REMOVAL OF BUSHING FOUND CORROSION ON THE LUG REPAIR PERFORMED BY CORROSION REMOVAL AND REAM UP THE HOLE IAW DRAWING R572-49121, APPROVED BY EA 6-5751-8106 AND RAS/BAE/0979/2004 ISS A. 2 L 7 2 4F RT A35EU 2007091900069 20070919 00069 EU 2007 9 19 07FDEA03694 1 20070913 A 5313 A53612213210 LONGERON AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 HEAVY CORROSION ON LONGERON Y1959 LT, BETWEEN FRAME 12A-19, OUT OF LIMIT IAW SRM 53-10-00/TB 102. REPLACEMENT OF LONGER ON (SUPPORT) IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900071 20070919 00071 NM 2007 9 19 07FDEA03692 1 20070913 A 5711 6516275 SPAR BOEING 727 727233 138408A NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 RIGHT WING NR 6 LEADING EDGE ACTUATOR MOUNT ON FRONT SPAR IS CRACKED IN THE UPPER INBD CORNER (FLAP). REMOVED AND REPLA CED NR 6 LEADING EDGE ACTUATOR MOUNT UPPER I/B CORNER (KRUGER FLAP) REF MM 27-81-022, SRM 51-30-2 LEAK CHECK AND OPS C HECKED GOOD. 2 L 7 3 4F RT A3WE 2007091900072 20070919 00072 EU 2007 9 19 07FDEA03691 1 20070913 A 5310 A53974225236 CROSSBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 CORRODED AND OLD REPAIRED CROSSBEAM AT FRAME 58 IN BULK CARGO COMPARTMENT. REPLACEMENT OF CROSSBEAM IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900073 20070919 00073 EU 2007 9 19 07FDEA03690 1 20070913 A 5730 A57350100 SKIN PANEL AIRBUS 310 A310203 3930313 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 ELONGATED HOLES FOUND ON RT WING TO PYLON HYDRAULIC FITTING RIB 8 REPAIR PERFORMED BY REAM UP AND BUSH INSTALLATION IAW DRAWING R572-49184, APPROVED BY EA 6-5720-79595 AND RAS/BAE/0931/2004 ISS A. 2 L 7 2 4F RT A35EU 2007091900075 20070919 00075 EU 2007 9 19 07FDEA03688 1 20070913 A 5730 A57350100 SKIN PANEL AIRBUS 310 A310203 3930313 EU ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND ELONGATED HOLES ON LT WING TO PYLON HYDRAULIC FITTING HOLES RIB 8 REPAIR PERFORMED BY REAM UP AND INSTALL BUSHINGS IAW DRAWING R572-49184 , APPROVED BY EA 6-5720-79594 AND RAS/BAE/0931/2004 ISS A. 2 L 7 2 4F RT A35EU 2007091900076 20070919 00076 EU 2007 9 19 07FDEA03686 1 20070913 A 5753 A57970650000 VANE AIRBUS 310 A310203 3930313 EU ZONE 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND DENT ON LT INBOARD FLAP VANE NOSE SKIN, RIB 7-8 REPAIR PERFORMED BY CUTTING THE DAMAGED AREA AND INSTALLING A NEW SKIN WITH INNER STRAPS IAW EA 6-5752-81059 AND RAS/DABRE/7004146/2004 ISS A. 2 L 7 2 4F RT A35EU 2007091900079 20070919 00079 EU 2007 9 19 07FDEA03630 1 20070912 A 2822 PUMP AIRBUS 300 A300B4622R 3930312 EU FUEL CELL FAULTED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 728FD 581 AT 30000 FT, FUEL TRANSFERED TO TRIM TANK. AUTO FEED FAULT WITH CENTER TANK PUMPS FAULT. TURNED OFF CENTER PUMPS AS P ER ECAM. FOLLOWED QRH FOR PUMPS FAULTS AND MANUAL FEED. CENTER TANK PUMPS WILL NOT COME ON, PUMPS KEEP FAULTING. TRA PPED FUEL OF 7000 REMOVED AND REPLACED RELAYS 107QA, 108QA AND RELAY 92QA PER SMP. PERFORMED OPS TEST OF THE PUMPS AN D PUMP LOW PRESSURE WARNING SYSTEMS NORMAL. ACCOMPLISHED FUCTIONAL TEST OF THE AUTO-FUEL FEED SYSTEM. . ALSO PERFORMED OPERATIONAL TEST OF THE CENTER AND INNER TANK PUMPS AUTOMATIC CONTROL. . ALL TEST IN REF TO EA.6 -2821-107502 2 L 7 2 4F RT A35EU 2007091900080 20070919 00080 EU 2007 9 19 07FDEA03628 1 20070912 A 5313 A53974203 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 CORROSION ON STRINGER 53, 54 AND 55 LHS BETWEEN FRAME 70-71. STRINGER SPLICE REPAIRS PERFORMED IAW SRM 53-10-14/FIG 201 . 2 L 7 2 4F RT A35EU 2007091900081 20070919 00081 EU 2007 9 19 07FDEA03627 1 20070912 A 5320 A53986743200 WEB AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 FOUND DAMAGED WEB PLATE BETWEEN FRAME 86-87, STRG 36 LT. REPLACEMENT OF WEB PLATE IAW SRM 51-72-10 AND SRM 53-19-18/PG 76/ ITEM 40. 2 L 7 2 4F RT A35EU 2007091900083 20070919 00083 EU 2007 9 19 07FDEA03625 1 20070912 A 5320 A53572608 WEB AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 FOUND DAMAGED WEB PLATES BETWEEN FRAME 86-87, STRG 33 LT AND RT. REPLACEMENT OF WEB PLATES IAW SRM 51-72-10 AND SRM 53- 19-18/PG 53. 2 L 7 2 4F RT A35EU 2007091900087 20070919 00087 EU 2007 9 19 07FDEA03621 1 20070912 A 5230 A52372054202 PLATE AIRBUS 310 A310324 3930206 EU ZONE 800 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 SCRATCHED AND DENTED CORNER PLATE AT BEAM 5 FWD CARGO DOOR AT FRAME 25A. REPLACEMENT OF CORNER PLATE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900088 20070919 00088 EU 2007 9 19 07FDEA03620 1 20070912 A 5230 A52370073202 BEAM AIRBUS 310 A310324 3930206 EU ZONE 800 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 SCRATCHED AND DENTED BEAM 5 FWD CARGO DOOR BETWEEN FRAME 20B-21. REPLACEMENT OF BEAM IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900092 20070919 00092 EU 2007 9 19 07FDEA03614 1 20070912 A 5313 A53974202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 HEAVY CORROSION ON STRINGER 53 LT BETWEEN FRAME 55/58-59, OUT OF LIMIT. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10- 14 / FIG 201. 2 L 7 2 4F RT A35EU 2007091900094 20070919 00094 EU 2007 9 19 07FDEA03611 1 20070912 A 5313 A53980071205 LONGERON AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 HEAVY CORROSION AT LONGITUDINAL BEAM BETWEEN FRAME 73A-75, STRG 26 RHS. REPLACEMENT OF LONGITUDINAL BEAM IAW SRM 51-72- 10. 2 L 7 2 4F RT A35EU 2007091900095 20070919 00095 EU 2007 9 19 07FDEA03610 1 20070912 A 5320 A26270471 BRACKET AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 CRACKED BRACKETS (TWO) BETWEEN CROSSBEAM 32/33 AND 33/34 RHS, STRG 26-27, Y-2462. REPLACEMENT OF BOTH BRACKETS IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900100 20070919 00100 EU 2007 9 19 07FDEA03605 1 20070912 A 5340 A53974216202 STRINGER CLIP AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 HEAVY CORROSION ON STRINGER CLIP BETWEEN STRINGER 52-53, FRAME 59 LT. REPLACEMENT OF STRINGER CLIP IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900102 20070919 00102 EU 2007 9 19 07FDEA03603 1 20070912 A 5313 A53974203 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 CORRODED STRINGER BETWEEN FRAME 67-69, STRG 57 AD, OUT OF LIMIT. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14 / FI G. 201. 2 L 7 2 4F RT A35EU 2007091900103 20070919 00103 EU 2007 9 19 07FDEA03602 1 20070912 A 5340 A53974325201 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 FOUND CRACKED FITTING AT FRAME 66, STRG 50 LHS. REPLACEMENT OF FITTING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900104 20070919 00104 EU 2007 9 19 07FDEA03601 1 20070912 A 5320 A53974259200 FLOOR SUPPORT AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 HEAVY CORROSION ON LONGITUDINAL PROFIL IN BULK CARGO COMPARTMENT BETWEEN FRAME 65-66, AD. REPLACEMENT OF LONGITUDINAL I AW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900105 20070919 00105 EU 2007 9 19 07FDEA03600 1 20070912 A 5320 A25572173202 FLOOR SUPPORT AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 HEAVY CORROSION AT LONGITUDINAL PROFILE IN BULK CARGO COMP BETWEEN FRAME 67-69 RHS OUTBOARD, STRG 44. REPLACEMENT OF LO NGITUDINAL IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900108 20070919 00108 EU 2007 9 19 07FDEA03597 1 20070912 A 5230 A52374160 PLATE AIRBUS 310 A310324 3930206 EU ZONE 800 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 812FD 467 FOUND OLD DOUBLER REPAIR ON LOWER INNER SKIN OF AFT CARGO DOOR, FRAME 62-62A. REPAIR IS NOT PERFORMED IAW. SRM, NOT AL LOWED THAT DOUBLER ENDS AT FRAME. INNER DOUBLER REPAIR RENEWED IAW. TD/KO/S1/01693/2004 ISSUE A AND RAS/DATLS/0001693/ 2004 ISSUE A. 2 L 7 2 4F RT A35EU 2007091900110 20070919 00110 EU 2007 9 19 07FDEA03592 1 20070912 A 5330 A53978152200 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 812FD 467 FOUND OLD DOUBLER REPAIR ON FUSELAGE SKIN BETWEEN FRAME 71-72, STRG 26-27 RT CLOSE TO CIRCUMFERENTIAL JOINT FRAME 72. T HERE MUST BE A MINIMUM DISTANCE OF THREE FASTENER SPACING BETWEEN THE OUTER ROW OF THE DOUBLER TO THE FIRST FASTENER ROW OF A LONGITUDINAL CIRCUMFERENTIAL JOINT (REF. SRM 53-10-12 / FIG. 201A). REPAIR PERFORMED BY INSTALLING NEW EXTERNAL D OUBLER IAW SRM 53-10-12/FIG 233. APPROVED BY EA 6-5318-92198 AND RAS/DAHAM/4019984/2005 ISSUE B. 2 L 7 2 4F RT A35EU 2007091900111 20070919 00111 EU 2007 9 19 07FDEA03591 1 20070912 A 5320 A53989395234 SUPPORT AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 DAMAGED SECTION-SUPPORT AT AFT FIRE WALL, FRAME 101 LOWER AREA. REPAIR PERFORMED BY REPLACEMENT OF SECTION-SUPPORT IAW S RM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900112 20070919 00112 EU 2007 9 19 07FDEA03588 1 20070912 A 5753 SKIN AIRBUS 310 A310324 3930206 EU TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 FOUND DELAMINATION AT OLD REPAIRS OF LT INBOARD FLAP BETWEEN RIB 4-RIB 5 AND RIB 9-RIB 10. REPAIR DAMAGED AREAS OF IN BOARD FLAP BETWEEN RIB 4 AND RIB 5 IAW SRM 57-53-12 FIGURE 208. REPAIR DAMAGED AREAS OF INBOARD FLAP BETWEEN RIB 9 AND RIB 10 IAW SRM 57-53-12 PARAGRAPH 13, FIGURE 209 VERSION 3 EA 6-5752-92202, RAS/DABRE/7005881/2005 ISSUE C. 2 L 7 2 4F RT A35EU 2007091900113 20070919 00113 EU 2007 9 19 07FDEA03585 1 20070911 A 5753 SKIN AIRBUS 310 A310203 3930313 EU TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 FOUND DELAMINATION AT UPPER SKIN TRAILING EDGE BETWEEN RIB 16-17 OF LT INBOARD FLAP. METAL-SKINNED CORE REPAIR AT T/E P ERFORMED AS PER SRM 57-53-12/PARA 13 / FIG 208, APPROVED BY EA 6-5752-92199 AND RAS/DABRE/7005884/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091900115 20070919 00115 EU 2007 9 19 07FDEA03580 1 20070911 A 5753 SKIN AIRBUS 310 A310324 3930206 EU TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 FOUND DELAMINATION ON OLD REPAIR AT TRAILING EDGE OF RT INBOARD FLAP, UPPER AND LOWER SIDE BETWEEN RIB 11-13 AND RIB 8-9 . REPAIR PERFORMED AS PER SRM 57-53-12 / PARA 13 / FIG 209 AND 208, APPROVED BY EA 6-5752-92201A AND RAS/DABRE/7005882/ 2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091900118 20070919 00118 EU 2007 9 19 07FDEA03573 1 20070911 A 5730 A57243205203 SKIN AIRBUS 310 A310203 3930313 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 FOUND SEVERAL CHAFING MARKS ON LEADING EDGE D-NOSE SKIN RT BETWEEN TRACK 5 AND 6. REPLACEMENT OF D-NOSE SKIN IAW SRM 51 -72-10. 2 L 7 2 4F RT A35EU 2007091900121 20070919 00121 EU 2007 9 19 07FDEA03568 1 20070911 A 5730 A57350104 SKIN PANEL AIRBUS 310 A310203 3930313 EU ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 ELONGATED HYDRAULIC FITTING HOLES AT PYLON SUPPORT BRACKET AND BOTTOM OF LT WING, RIB 8. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLING BUSHES IAW R572-49184 ISSUE C, APPROVED BY EA 6-5720-92194 AND RAS/BAE/1001639/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091900122 20070919 00122 EU 2007 9 19 07FDEA03567 1 20070911 A 5730 A57350104 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 ELONGATED HYDRAULIC FITTING HOLES AT PYLON SUPPORT BRACKET AND BOTTOM OF RT WING, RIB 8. REPAIR PERFORMED BY OVERSIZING AND INSTALLING BUSHES IAW R572-49184 ISSUE C, APPROVED BY EA 6-5720-92194 AND RAS/BAE/1001639/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091900123 20070919 00123 EU 2007 9 19 07FDEA03566 1 20070911 A 5330 A53778628200 SKIN PANEL AIRBUS 310 A310203 3930313 EU ZONE 100 NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 OLD SKIN DOUBLER REPAIR AT C 34, BETWEEN P 54 LT-P54 RT NOT COMPATIBLE TO P TO F CONVERSION DOUBLER REPAIR RENEWED IAW E A 6-5314-79564 AND RAS/DABRE/7003949/2004 ISS A AND RAS/DABRE/7004007/2004 ISS A. 2 L 7 2 4F RT A35EU 2007091900125 20070919 00125 EU 2007 9 19 07FDEA03564 1 20070911 A 5311 A53771410 FRAME AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION AT Y-Z LATCH SUPPORT FITTING OF FRAME C 25A RT REPAIR PERFORMED IAW SRM 53-13-13 FIG 203. 2 L 7 2 4F RT A35EU 2007091900127 20070919 00127 EU 2007 9 19 07FDEA03551 1 20070911 A 5313 A53974527216 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION FOUND ON STRINGER P 52 LT, C 60-61 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007091900128 20070919 00128 EU 2007 9 19 07FDEA03547 1 20070911 A 5101 A53974235200 STRUCTURE AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION FOUND ON CONNECTING SECTION, C 55/58-59, P 50 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900131 20070919 00131 EU 2007 9 19 07FDEA03544 1 20070911 A 5313 A53974203 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION FOUND AT C64, P 52 LT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007091900132 20070919 00132 EU 2007 9 19 MALA070102 1 20070812 A 3350 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS NO TEST A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 418XJ 340B418 DURING TASK CARD 335003, EMERGENCY LIGHT POWER SUPPLY 23LN FAILED TEST. REMOVED AND REPLACED POWER SUPPLY 23LN WITH SER VICEABLE UNIT IAW SAAB AMM 33-50-10. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2007091900136 20070919 00136 EU 2007 9 19 MALA070111 1 20070824 A 5210 SKIN SAAB SF340 340B 7860101 EU PAX DOOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 411XJ 340B411 DURING N4K CHECK IN CWA FOUND, MAIN ENTRANCE DOOR OUTER SKIN DENT. REPAIRED IAW EO NR S52082 AND SRM 52-10-10. 2 L 7 2 4T RT A52EU 2007091900137 20070919 00137 EU 2007 9 19 MALA070108 1 20070811 A 5753 RIB SAAB SF340 340B 7860101 EU TE FLAP CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 414XJ 340B414 DURING N4K CHECK IN CWA FOUND, LT FLAP AFT BULKHEAD COVE FAIRING RIB IS CRACKED. REPLACED RIB IAW SRM 51-40-00 AND EO N R S57051. 2 L 7 2 4T RT A52EU 2007091900139 20070919 00139 EU 2007 9 19 MALA070107 1 20070811 A 5350 PANEL SAAB SF340 340B 7860101 EU FUSELAGE DEBONDED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 414XJ 340B414 DURING N4K CHECK IN CWA, FOUND 6 DENTS ON CENTER BELLY WING FUSELAGE PANEL DISBONDED. REPAIRED IAW EO NR S51031 AND SRM 51-70-50. 2 L 7 2 4T RT A52EU 2007091900142 20070919 00142 EU 2007 9 19 MALA070113 1 20070824 A 5533 UNKNOWN SAAB SF340 340B 7860101 EU VENTRAL FIN UNKNOWN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 411XJ 340B411 DURING N4K CHECK IN CWA FOUND, RT VENTRAL FIN LOWER EDGE. REPAIRED IAW EO NR S53466 AND SAAB REPAIR STATEMENT 340SDS012 863 REPAIRED IAW EO NR S53466 AND SAAB REPAIR STATEMENT 340SDS012863. 2 L 7 2 4T RT A52EU 2007091900143 20070919 00143 NM 2007 9 19 NWAA073046309 1 20070911 A 2530 CONTROLLER BOEING 747 747451 1384940 NM GALLEY ODOR A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 01 669US 24224 DURING FLIGHT, FLIGHT ATTENDANT REPORTED OVEN 2-7 HAS AN ODOR OF BURNED WIRE. MAINTENANCE REPLACED OVEN CONTROLLER. OP ERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007091900145 20070919 00145 NM 2007 9 19 AALA20071600 1 20070822 A 2530 OVEN BOEING 777 777223 1385213 NM GALLEY SMOKE A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 779AN 29955 LHR INFLIGHT T086/22AUG - NUMBER TWO OVEN IN FIRST CLASS GALLEY SMOKING. FLIGHT ATTENDANT TURNED OVEN OFF. CIRCUIT BRE AKERS PULLED AND BANDED. CLEANED BURNT RESIDUE FROM NUMBER TWO OVEN IN FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT T00001SE 2007091900147 20070919 00147 NM 2007 9 19 AALA20071613 1 20070824 A 2697 CONNECTOR BOEING 777 777223 1385213 NM SMOKE DETECTOR LOOSE A AALA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 21 759AN 32638 LHR INFLIGHT T156/24AUG - LEFT AND RIGHT NUMBER TWO LAVATORY SMOKE ALARMS WENT OFF AT TAKEOFF FOR ABOUT ONE SECOND. NO EVIDENCE OF SMOKE. RESEATED ELECTRICAL CONNECTORS FOR SMOKE ALARMS IN LEFT AND RIGHT NUMBER TWO LAVATORIES. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091900149 20070919 00149 WP 2007 9 19 AALA20071593 1 20070820 A 3397 TERMINAL DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DIRTY A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AA 49459 SFO - EMERGENCY LIGHTS AT LEFT AND RIGHT FORWARD OVERWING EXIT INOPERATIVE. CLEANED BATTERY TERMINALS FOR EMERGENCY LIG HTS AT LEFT AND RIGHT FORWARD OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007091900150 20070919 00150 2007 9 19 AALA20071592 4 20070820 A 2565 GIRT BAR BOEING 737 737823 13844BZ NM R1 DOOR MALFUNCTIONED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 915AN 29516 IAD - RIGHT NUMBER ONE DOOR SLIDE DISLODGED FROM PACK. DID NOT DEPLOY. REINSTALLED AND INSPECTED SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007091900152 20070919 00152 EU 2007 9 19 AALA20071608 1 20070822 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70074 517 JFK - SEAT MOUNTED EMERGENCY LIGHT AT LEFT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGH T AT LEFT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007091900153 20070919 00153 NM 2007 9 19 AALA20071605 1 20070822 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 752AN 30260 JFK EMERGENCY LIGHT AT SEAT 21C BROKEN BULB. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091900154 20070919 00154 NM 2007 9 19 AALA20071604 1 20070822 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 752AN 30260 JFK - EMERGENCY LIGHT AT SEAT 21C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091900155 20070919 00155 NM 2007 9 19 AALA20071607 1 20070822 A 2761 ACTUATOR BOEING 757 757223 1384957 NM SPOILERS LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 675AN 29425 MIA INFLIGHT T688/22AUG DFW TO SJU, LOST CENTER HYDRAULIC FLUID DURING FLIGHT. DIVERTED TO MIA AND LANDED WITHOUT INCID ENT. FOUND NUMBER ONE SPOILER ACTUATOR LEAKING. REPLACED NUMBER ONE SPOILER ACTUATOR. SYSTEM GROUND CHECKED NORMAL OP ERATION. 2 L 7 2 4F RT A2NM 2007091900156 20070919 00156 2007 9 19 AALA20071606 4 20070822 A 2565 100505201 SLIDE DOUG DC9 DC983 3022083 WP L2 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 433AA 49451 AUS LEFT NUMBER TWO DOOR SLIDE GIRT BAR FLAP DOES NOT HOLD. REPLACED LEFT NUMBER TWO DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007091900157 20070919 00157 WP 2007 9 19 AALA20071599 1 20070821 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7522A 49899 LGA - EMERGENCY LIGHT AT SEAT ROW 29DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 29DEF. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007091900158 20070919 00158 NM 2007 9 19 AALA20071598 1 20070821 A 3350 CM3071BPEGPL LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 JFK - EMERGENCY LIGHT AT SEAT 3D BROKEN. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 3D. SYSTEM GROUND CHECKED NORMAL OP ERATION. 2 L 7 2 4F RT T00001SE 2007091900159 20070919 00159 NM 2007 9 19 AALA20071602 1 20070822 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 753AN 30261 MIA - EMERGENCY LIGHT AT SEAT 25C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091900160 20070919 00160 NM 2007 9 19 AALA20071601 1 20070822 A 2910 HOSE BOEING 757 757223 1384957 NM HYD SYSTEM LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 21 607AM 27058 MIA INFLIGHT T1818/22AUG - ON SHORT FINAL, LOST LEFT HYDRAULIC QUANTITY DOWN TO .22. LANDED MIA WITHOUT INCIDENT. REPL ACED MAIN LANDING GEAR DOWN LOCK ACTUATOR HOSE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007091900162 20070919 00162 EU 2007 9 19 AALA20071553 1 20070815 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 JFK - EMERGENCY LIGHT AT SEAT MOUNTED RIGHT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT MO UNTED RIGHT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007091900163 20070919 00163 WP 2007 9 19 AALA20071610 1 20070823 A 3230 VALVE DOUG DC9 DC982 3022082 WP MLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 583AA 53160 SAT INFLIGHT T304/23AUG - LANDING GEAR WOULD NOT RETRACT. RETURNED TO SAT AND LANDED WITHOUT INCIDENT. FOUND GEAR DOOR BYPASS LEVER OPEN. REPAIRED VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007091900164 20070919 00164 NM 2007 9 19 AALA20071609 1 20070820 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 936AN 29532 TUL - EMERGENCY LIGHTS AT MID COACH CLASS INOPERATIVE. REPLACED BATTERY PACK AT SEAT 19A FOR EMERGENCY LIGHTS AT MID CO ACH CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007091900165 20070919 00165 NE 2007 9 19 AALA20071597 2 20070821 A 7261 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LEFT MAKING METAL A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 403A 49314 725852 BNA INFLIGHT T1531/21AUG - NUMBER ONE ENGINE OIL CLOG LIGHT ILLUMINATED DURING CLIMB. REDUCED NUMBER ONE ENGINE TO IDL E AND RETURNED TO BNA AND LANDED WITHOUT INCIDENT. FOUND METAL IN OIL FILTERS. REPLACED NUMBER ONE ENGINE ON 22 AUG AT BNA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007091900167 20070919 00167 NM 2007 9 19 AALA20071594 1 20070820 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 699AN 27051 DFW - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 9 TO 16 INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 9 FOR EMERGENCY LIGHTS AT SEAT ROWS 9 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007091900168 20070919 00168 WP 2007 9 19 NWAA073039867 1 20070911 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 776NC 47786 TAIL COMPARTMENT CATWALK EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. OPERATION CHECKS GOOD. 2 L 7 2 4F RT A6WE 2007091900169 20070919 00169 2007 9 19 SWIA200718672 2 20070908 A 7261 CARBON SEAL CNDAIR CL600 CL6002B19 1900309 EA NR 2 ENGINE LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 07 915SW 7615 FLT 6541 - ON APPROACH, RECEIVED AN "ENGINE OIL" WARNING. REPLACED NR 2 ENGINE SHAFT AND CARBON SEALS ON AGB IAW AMM 24 -11-01, 29-11-01 AND GE MM 72-00-00 SPECIAL PROCEDURE 63. 2 L 7 2 4F RT A21EA 2007091900170 20070919 00170 EA 2007 9 19 SWIA200718671 1 20070908 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 957SW 7829 LEFT SIDE COCKPIT WINDOW CRACKED. REPLACED LEFT SIDE WINDOW IAW MM 56-12-01, P/N OFF NP139322-1, S/N 03102H1757. 2 L 7 2 4F RT A21EA 2007091900171 20070919 00171 NM 2007 9 19 AALA20071575 1 20070817 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 196AA 32390 DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR SLIDE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007091800126 20070918 00126 EU 2007 9 18 AALA20071621 1 20070825 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 77080 626 MIA EMERGENCY LIGHT AT SEAT 18G INOPERATIVE. RECONNECTED WIRING FOR EMERGENCY LIGHT AT SEAT 18G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007091800127 20070918 00127 EU 2007 9 18 AALA20071629 1 20070826 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 41063 506 MIA EMERGENCY LIGHT AT SEAT 12G MISSING. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 12G. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007091800128 20070918 00128 WP 2007 9 18 AALA20071628 1 20070826 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 578AA 53155 LGA - EMERGENCY LIGHTS AT TAIL CONE INOPERATIVE. REPLACED BATTERY PACK AT AFT LAVATORY OVERHEAD FOR EMERGENCY LIGHTS AT TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007091800130 20070918 00130 EU 2007 9 18 AALA20071627 1 20070826 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 41063 506 MIA - EMERGENCY LIGHT AT SEAT 8C INOPERATIVE. SECURED PINS FOR EMERGENCY LIGHT AT SEAT 8C. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A35EU 2007091800131 20070918 00131 EU 2007 9 18 AALA20071620 1 20070825 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 77080 626 MIA - EMERGENCY LIGHT AT SEAT 2D MISSING. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 2D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007091800132 20070918 00132 WP 2007 9 18 AALA20071619 1 20070826 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 578AA 53155 LGA - EMERGENCY LIGHTS AT FORWARD GALLEY OVERHEAD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD GA LLEY OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007091800173 20070918 00173 NM 2007 9 18 2007UALA03547 1 20070903 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MID GALLEY SMOKE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 542UA 25276 ACRID SMELL WITH LITE SMOKE IN MID GALLEY. RAN GALLEY FIRE SMOKE QRC SMOKE DISSIPATED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091800202 20070918 00202 NM 2007 9 18 2007UALA03574 1 20070904 A 3350 767 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 570UA 26678 SLIDE LIGHT INOP AT DOOR 2R. AFT OVERWING SLIDE LIGHT INOP ON RIGHT SIDE OF AIRCRAFT. RELAMPED SLIDE LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091800218 20070918 00218 EU 2007 9 18 07FDEA03639 1 20070913 A 5313 A53880206202 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION ON STRINGER CONNECTION AT C80, P 38 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091800220 20070918 00220 EU 2007 9 18 07FDEA03638 1 20070913 A 5313 A53980670226 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION FOUND AT STRINGER P38, C79-80. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201 2 L 7 2 4F RT A35EU 2007091800221 20070918 00221 EU 2007 9 18 07FDEA03637 1 20070913 A 5320 A53981113 PLATE AIRBUS 310 A310324 3930206 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 CRACKED SHEAR PLATES BETWEEN FRAME 79-80/82, STRG 26 LT AND RT. REPLACEMENT OF BOTH SHEAR PLATES IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091800222 20070918 00222 EU 2007 9 18 07FDEA03636 1 20070913 A 5330 A53778628200 SKIN PANEL AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION FOUND ON INTERNAL SKIN C-37-38, P55LT-55RT DOUBLER REPAIR PERFORMED IAW SRM 53-10-12 FIG 221 AND 203. 2 L 7 2 4F RT A35EU 2007091800224 20070918 00224 EU 2007 9 18 07FDEA03635 1 20070913 A 5330 A53778398202 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION AT STRINGER P 37 RT, C37 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007091800234 20070918 00234 NM 2007 9 18 KCSA071335 1 20070908 A 3350 SIGN BOEING 747 7472B4B 138481B NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 719CK 21099 UPPER DECK RIGHT DOOR EMERGENCY EXIT SIGN INOP. 2 L 7 4 4F RT A20WE 2007091800236 20070918 00236 SO 2007 9 18 C2XA07SH069 1 20070910 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 21197 14500947 SHV - DURING C-CHECK, CENTER OMEGA BEAM CORRODED FR 20. MX REMOVED AND REPLACED CENTER OMEGA BEAM AT FR 20 DUE TO OUT O F LIMIT CORROSION. COMPLIED WITH EC 5320-0437 AND 5320-01140. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2007091800245 20070918 00245 NM 2007 9 18 UPS07M50622 1 20070816 A 5712 ARB2850505 RIB DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 INSPECTION TYPE:4C LEFT WING NR 16 SLAT TRACK I/B FITTING (RIB) IS CRACKED. REMOVED AND REPLACED LEFT WING NR 16 SLAT T RACK I/B FITTING (RIB) IAW MD-11 SRM 51-33-01 AND 51-35-01. 2 L 7 3 4F RT A22WE 2007091800259 20070918 00259 NM 2007 9 18 SWAA074481 1 20070907 A 3397 8100022607 CONNECTOR BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 474WN 33861 EEPLS INOP BETWEEN ROW 1 ABC AND ROW 5 ABC. FOUND LOOSE CONNECTOR. SECURED LOOSE CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2007091800261 20070918 00261 2007 9 18 SWAA074461 4 20070907 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007091800266 20070918 00266 NM 2007 9 18 SWAA074480 1 20070907 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 466WN 30677 DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM . 2 L 7 2 4F RT A16WE 2007091800276 20070918 00276 SO 2007 9 18 C2XA07SH067 1 20070908 A 5751 14573900403 PLATE EMB 145 EMB145LR 3260212 SO RT AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13997 145298 SHV - DURING C-CHECK MAINTENANCE FOUND RIGHT LOWER AILERON SHROUD WITH CORRODED BONDING PLATE. MAINTENANCE REPAIRED RIG HT LOWER AILERON SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007091800305 20070918 00305 EA 2007 9 18 TRAX200701323 1 20070904 A 5346 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 875AS 7559 AAR - UPPER WEB OF ENGINE BEAM, APPROXIMATELY CENTERED IN AFT EDGE AT MARKED RIVET, SUSPECT A CRACK. REPAIRED IAW EO 6 00-53-0169. 2 L 7 2 4F RT A21EA 2007091900002 20070919 00002 EU 2007 9 19 07FDEA03773 1 20070914 A 5320 A53974232200 COUPLING AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION AT COUPLING, C 65, P 56 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900006 20070919 00006 EU 2007 9 19 07FDEA03769 1 20070914 A 5320 A53773657202 PLATE AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION AT GROUND VALVE PLATE C 24-25 , P52-55 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900023 20070919 00023 EU 2007 9 19 07FDEA03748 1 20070914 A 5320 A53778330208 PLATE AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 DAMAGED SHEARPLATE (DENTED AND CRACKED) BETWEEN FRAME 38.1-38.2. REPLACEMENT OF SHEAR PLATE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900026 20070919 00026 EU 2007 9 19 07FDEA03745 1 20070914 A 5311 A53973021223 FRAME AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 815FD 638 NICK ON FRAME 61, STRG 15 LT AND THREE OPEN FASTENER HOLES. REPAIR PERFORMED BY BLEND OUT NICK AND CLOSING BLIND OPEN FA STENER HOLES IAW EA 6-5317-92170 AND RAS/DATLS/0002688/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091900030 20070919 00030 EU 2007 9 19 07FDEA03729 1 20070914 A 5315 A53978476200 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 HEAVY CORROSION ON CROSSBEAM FRAME 61 AFT CARGO COMP FLOOR STRUCTURE, RT. REPLACEMENT OF CROSSBEAM IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900034 20070919 00034 EU 2007 9 19 07FDEA03725 1 20070914 A 5320 A53970709202 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 HEAVY CORROSION ON CORNER FITTING FRAME 54.2 BETWEEN P41-45 LT. REPLACEMENT OF FITTING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900037 20070919 00037 EU 2007 9 19 07FDEA03684 1 20070913 A 5753 A57970372201 SKIN AIRBUS 310 A310203 3930313 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 DURING FUNCTION PHASE, THE RT INBOARD FLAP TRAILING EDGE WAS DAMAGED REPAIR PERFORMED IAW SRM 57-53-12 PARA 13 (FIG 209 ). 2 L 7 2 4F RT A35EU 2007091900042 20070919 00042 EU 2007 9 19 07FDEA03722 1 20070907 A 5230 A5237801020400 DOOR FRAME AIRBUS 310 A310222 3930315 EU ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 BULK CARGO COMPARTMENT DOOR FWD FRAME WITH CRACK. DOOR FWD FRAME WAS REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900065 20070919 00065 EU 2007 9 19 07FDEA03698 1 20070913 A 5512 A55177801200 SKIN AIRBUS 310 A310324 3930206 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 CORROSION PITS ON TOP FWD SKIN OF THS LT REMAINING THICKNESS IS WITHIN LIMITS GIVEN IN SRM BUT MAXIMUM AFFECTED SURFACE AREAS ARE >400 MMXMM AND THEREFORE ARE OUT OF LIMIT AS PER SRM 55-10-00/CONFIG 2/TB 101(PIT AREAS BETWEEN 200 AND 1500 M MXMM) REWORK AREAS DOCUMENTED AND APPROVED PER EA 6-5510-92156 AND RAS/CASA/4264/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091900077 20070919 00077 NM 2007 9 19 07FDEA03685 1 20070913 A 5315 652082758 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FLOORBEAM AT STA 500, RBL 28 - 42, HOLES ARE CORRODED UNDERNEATH FROM PREVIOUS REPAIR WITH NO TREAT AND PRIME REMOVED C ORROSION FROM DAMAGED AREA, REF SRM 53-10-1. REMOVED DAMAGED AREA REF DWG SR27-53-034 REV F, ORIGINAL THICKNESS .125, R EMAINING THICKNESS .095", MATERIAL LOSS .030. OUT OF LIMITS REF SRM 53-10-1. FABRICATED T ANGLE AND REPAIR ANGLES REF SR 27-53-034 REV F, REPAIR ANGLES SENT OUT FOR HEAT TREAT AND CAD PLATE TREATED AND PRIMED REF 51-10-2. REMOVED AND RE INSTALLED FASTENERS FROM SEAT TRACKS AND SEAT TRACK STRAPS, STA 462-520 RBL 24.5 - 48". INSTALLED T- ANGLE AND REPAIRS ANGLES REF DRAWING SR27-53-034. 2 L 7 3 4F RT A3WE 2007091900089 20070919 00089 EU 2007 9 19 07FDEA03619 1 20070912 A 5315 A53970197 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 FOUND MISDRILLED HOLES AT CROSSBEAM FRAME 54.1 AND 54.2, Y-805. CROSSBEAM SPLICE REPAIR ON BOTH CROSSBEAMS PERFORMED IA W SRM 53-10-15/FIG 207. 2 L 7 2 4F RT A35EU 2007091900090 20070919 00090 EU 2007 9 19 07FDEA03618 1 20070912 A 5330 A53974207 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 CORROSION SPOT BELOW STRG 57 ON LONGITUDINAL LAP JOINT AT INNER SKIN SURFACE IS OUT OF LIMIT, FRAME 65-66, STRG 57 AD. BLEND OUT REPAIR APPROVED EA 6-5317-92204 AND RAS/DAHAM/4020031/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091900096 20070919 00096 EU 2007 9 19 07FDEA03609 1 20070912 A 5320 A53989352 PLATE AIRBUS 310 A310324 3930206 EU ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 DEEP CHAFING MARKS ON LT AND RT ANTI CHAFING PLATE, FRAME 92-93, STRG 9-14. REPLACMENT OF ANTI-CHAFING PLATES LT AND RT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900109 20070919 00109 EU 2007 9 19 07FDEA03595 1 20070912 A 5330 A53981540 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 812FD 467 FOUND OLD REPAIR DOUBLER BETWEEN FRAME 75A-76, STRG 29-30 RT. DOUBLER ENDS ON THE LONGITUDINAL JOINT, NOT ALLOWED IAW S RM 53-10-12/FIG 203. REPAIR PERFORMED BY INSTALLING NEW EXTERNAL DOUBLER IAW EA 6-5318-92197 AND RAS/DAHAM/4019986/20 05 ISSUE B. 2 L 7 2 4F RT A35EU 2007091900124 20070919 00124 EU 2007 9 19 07FDEA03565 1 20070911 A 5313 A53778393200 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION AT STRINGER P 48, C38.2-39 OUT OF LIMIT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007091900126 20070919 00126 EU 2007 9 19 07FDEA03561 1 20070911 A 5313 A53970721200 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION FOUND ON STRINGER P44 RT AT C54.2 OUT OF LIMIT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007091900130 20070919 00130 EU 2007 9 19 07FDEA03545 1 20070911 A 5313 A53974202206 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION FOUND AT C64-65, P 44 LT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007091900133 20070919 00133 EU 2007 9 19 MALA070110 1 20070811 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 582 DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 414XJ 340B414 DURING N4K CHECK IN CWA FOUND, CENTER SEAT TRACK AT STA 582, TOP FLANGE IS BENT UPWARD AND HAS CRACKS. REMOVE DAMAGED S ECTION, SPLICED IN NEW SECTION OF TRACK IAW EO NR S53060 AND SRM 53-70-60. 2 L 7 2 4T RT A52EU 2007091900134 20070919 00134 EU 2007 9 19 MALA070109 1 20070811 A 5753 RIB SAAB SF340 340B 7860101 EU TE FLAP CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 414XJ 340B414 DURING N4K CHECK IN CWA FOUND, RT FLAP AFT BULKHEAD COVE FAIRING RIB IS CRACKED. REPLACED RIB IAW SRM 51-40-00 AND EO N R S57051. 2 L 7 2 4T RT A52EU 2007091900135 20070919 00135 EU 2007 9 19 MALA070112 1 20070824 A 5320 REINFORCEMENT SAAB SF340 340B 7860101 EU BS 288-294 UNKNOWN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 411XJ 340B411 DURING N4K CHECK IN CWA FOUND, FUSELAGE BOTTOM FRAME REINFORCEMENT BETWEEN STA 288-294 REPAIRED. REPAIRED IAW SRM 53-70 -30. SPECIAL REPAIR NR 7 AND EO NR S53362. 2 L 7 2 4T RT A52EU 2007091900138 20070919 00138 EU 2007 9 19 MALA070106 1 20070811 A 5311 FRAME SAAB SF340 340B 7860101 EU BS 258 MISREPAIRED A MALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 15 414XJ 340B414 DURING N4K CHECK IN CWA FOUND, PREVIOUS REPAIR OF BOTTOM FRAME UPPER FLANGE STA 258, LBL 10-RBL 12 DOES NOT C/W SRM 53-7 0-30 SPECIAL REPAIR NR 5. REPLACED PREVIOUS REPAIR IAW EO NR 53102. 2 L 7 2 4T RT A52EU 2007091900140 20070919 00140 EA 2007 9 19 MALA070115 1 20070905 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002D24 1390016 EA LAVATORY MALFUNCTIONED A MALA O OTHER N FALSE WARNING DE DESCENT 1 GL 15 904XJ 15135 DURING DECENT AFT LAV SMOKE MSG CAME ON. FOLLOWED QRH AND PULLED CB'S. MSG DID EXTINGUISH. FA'S STATED NO SMOKE APPEA RED. INSPECTED AFT LAV AREA FOR SIGNS OF FIRE OR HEAT DAMAGE. NONE NOTED. COMPLETED OPERATIONAL CHECK OF AFT LAV FIRE DETECTOR. OPS CHECK GOOD IAW CRJ AMM 26-16-00 PGS 501-502. RESET NOTED CIRCUIT BREAKERS. 2 L 7 2 4F RT A21EA 2007091900161 20070919 00161 NM 2007 9 19 AALA20071603 1 20070822 A 3350 0201720001 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 797AN 30012 JFK - EMERGENCY LIGHT AT SEAT 21G INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091900173 20070919 00173 NM 2007 9 19 AALA20071569 1 20070813 A 5320 145T87562 STIFFENER BOEING 767 767323 1385205 NM BS 1045-1060 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 366AA 25193 AFW - PRESSURE DECK LONGITUDINAL STIFFENER HAS TWO HOLES IN THE UPPER FLANGE AT RIGHT BUTTLINE 5.75 STATION 1045 AND 106 0. REPAIRED HOLES FOR THE PRESSURE DECK LONGITUDINAL STIFFENER IN THE UPPER FLANGE AT RIGHT BUTTLINE 5.75 STATION 1045 AND 1060. 2 L 7 2 4F RT A1NM 2007091900175 20070919 00175 NM 2007 9 19 AALA20071588 1 20070819 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 188AN 32382 ORD - EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007091900176 20070919 00176 NM 2007 9 19 AALA20071587 1 20070819 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 759AN 32638 MIA - EMERGENCY LIGHT AT SEAT ROW 26C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 26C. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091900177 20070919 00177 NM 2007 9 19 AALA20071565 1 20070813 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 AFW - EMERGENCY LIGHTS AT RIGHT NUMBER THREE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT NUMB ER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091900178 20070919 00178 NM 2007 9 19 AALA20071562 1 20070813 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 AFW - EMERGENCY LIGHTS AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091900180 20070919 00180 NM 2007 9 19 AALA20071563 1 20070813 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 AFW - EMERGENCY LIGHTS AT LEFT NUMBER FOUR DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091900182 20070919 00182 NM 2007 9 19 AALA20071586 1 20070819 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 759AN 32638 MIA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 24C MISSING LENS. REPLACED LENS FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 24C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091900184 20070919 00184 WP 2007 9 19 AALA20071584 1 20070819 A 3397 TERMINAL DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 492AA 49730 SFO - EMERGENCY LIGHT AT LEFT OVERWING EXIT INOPERATIVE. CLEANED BATTERY PACK TERMINAL AT SEAT 21D FOR EMERGENCY LIGHT AT LEFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007091900185 20070919 00185 NM 2007 9 19 AALA20071582 1 20070818 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 762AN 31479 DFW - EMERGENCY LIGHT AT SEAT ROW 32G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 32G. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091900186 20070919 00186 NM 2007 9 19 AALA20071561 1 20070814 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 AFW - EMERGENCY LIGHTS AT AFT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091900188 20070919 00188 NM 2007 9 19 AALA20071560 1 20070816 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 661AA 25295 MIA - EMERGENCY LIGHTS AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT NUMBER T WO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007091900190 20070919 00190 NM 2007 9 19 AALA20071559 1 20070816 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 661AA 25295 MIA - EMERGENCY LIGHTS AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT NUMBER O NE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007091900195 20070919 00195 NM 2007 9 19 AALA20071578 1 20070818 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 916AN 29517 DFW - EMERGENCY LIGHT AT AFT SEAT ROW 14D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT AFT SEAT ROW 14D . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007091900196 20070919 00196 NM 2007 9 19 AALA20071555 1 20070815 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 603AA 27054 SFO - EMERGENCY LIGHTS AT LEFT AND RIGHT LOWER EXIT DOOR INOPERATIVE. REPLACED BATTERY PACK M10952 AT STATION 690 FOR E MERGENCY LIGHTS AT LEFT AND RIGHT LOWER EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092000002 20070920 00002 EU 2007 9 20 F3LA200700232 1 20070915 A 3397 LIGHT AIRBUS A319 A319112 3930323 EU CABIN MISWIRED A F3LA D RETURN TO BLOCK W INADEQUATE Q C TX TAXI/GRND HDL 1 NM 03 909FR 1761 BLOCK TURN BACK, FLIGHT CREW REPORTED L2 DOOR EMERGENCY EXIT LIGHT 'ON' DURING TAXI, EMERGENCY EXIT SIGN 'OFF' DURING TA XI. MAINTENANCE FOUND 45WL, EXIT MARKING SIGN, AND 33WL, EMERGENCY CABIN LIGHT, WIRED INCORRECTLY. REWIRED 45WL AND 33 WL IAW AMM 33-51-00, SHEET 02, P101, FIG. 3. PERFORMED OPS CHECK IAW AMM 33-51-00, PAGE BLOCK 501, WITH NO DISCREPANCIE S NOTED. 2 L 7 2 4F RT A28NM 2007092000003 20070920 00003 2007 9 20 HNAA0700164 4 20070726 A 2565 DISK DHAV DHAV DHC8 DHC8311 1386006 EA DITCHING DAM BURST A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 333EN F2676 221 LEFT DITCHING DAM PRESSURE READS ZERO PSI. FOUND DISK BURST BUT DITCHING DAM DID NOT DEPLOY. REMOVED AND REPLACED DITC HING DAM DISK, BOTTLE AND BAG PER W/C 25-60-10R AND W/C 25-60-07R PARTS REPLACED - BURST DISK ADAPTER P/N A 68641, NITRO CLYLINDER P/N 410870-3, S/N 450, DITCHING DAM P/N 4MAN25-10, S/N F2548. 2 H 7 2 4T RT A13NM 2007092000005 20070920 00005 EA 2007 9 20 REXA200700056 1 20070621 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS LOOSE A REXA O OTHER O OTHER NR NOT REPORTED 1 SO 25 8423C 7423 EMERGENCY FLOOR LIGHTS FROM ROW 6 THROUGH 8 INOP. RESECURED CONNECTOR. 2 L 7 2 4F RT A21EA 2007092000007 20070920 00007 EA 2007 9 20 REXA200700058 1 20070724 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCONNECTED A REXA O OTHER O OTHER NR NOT REPORTED 1 SO 25 8733G 7733 EMERGENCY FLOOR LIGHT SEATS 2-5 INOP. LIGHT STRIP CONNECTOR WAS RECONNECTED. 2 L 7 2 4F RT A21EA 2007092000009 20070920 00009 NM 2007 9 20 DLM88071202 1 20070908 A 5320 ANGLE DOUG MD88 MD88 3023688 NM MLG WW CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 951DL 49882 CRACK ON ANGLE WITHIN RT W/W AT FWD JAMB RBL=40. REPLACED ANGLE IAW DOUGLAS DWG 5930584. 2 L 7 2 4F RT A6WE 2007092000010 20070920 00010 NM 2007 9 20 DLM88071203 1 20070908 A 5320 FLOOR SUPPORT DOUG MD88 MD88 3023688 NM BS 1250 DEFORMED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 951DL 49882 DEFORMED FLOOR SUPPORT STA 1250 BETWEEN LONGERON 30 AND 28 LT. REPAIRED PER DAC DWG 5952803. 2 L 7 2 4F RT A6WE 2007092000012 20070920 00012 NM 2007 9 20 DLM88071205 1 20070908 A 5320 FLOOR SUPPORT DOUG MD88 MD88 3023688 NM STA1307 L22R/L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 951DL 49882 CORROSION ON AFT PAX FLOOR STRUCTURE STA Y=1307 FROM LBL 22 TO RBL 22. FABRICATED AND REPLACED IAW DAC DWG 5930961. 2 L 7 2 4F RT A6WE 2007092000013 20070920 00013 2007 9 20 DL777071206 4 20070911 A 2350 63999001 MICROPHONE BOEING 777 777232 1385232 NM COCKPIT UNSERVICEABLE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 860DA 29951 FROM OBSERVERS POSITION HOT MIC ON PUSHBACK. REMOVED AND REPLACED MIC. OPS CK GOOD. 2 L 7 2 4F RT T00001SE 2007092000015 20070920 00015 NM 2007 9 20 DL75A071210 1 20070913 A 5330 141N32311 SKIN BOEING 757 757212 1384951 NM BS 430 S28L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 752AT 23128 FUSELAGE SKIN CORROSION AT THE AFT RT CORNER OF THE FWD LAVATORY SERVICE PANEL LOCATED AT STA 430, S-28L. CUTOUT THE DA MAGED SKIN AT INSTALLED A REPAIR DOUBLER. 2 L 7 2 4F RT A2NM 2007092000016 20070920 00016 NM 2007 9 20 DL76L071211 1 20070914 A 2910 000AE968D0165 LINE BOEING 767 767332 1382001 NM RT PYLON CRACKED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 177DN 25122 RT HYD QTY ZERO AFTER TAKEOFF AT 5000 FT. FOUND HYD PRESS LINE AT RT A/C PUMP CRACKED AT B NUT. REPLACED HYD LINE. RE SERVICED SYS AND OPERATED SYS. NO LEAKS RAN ENG AND OPS CHECK ENG PUMP OK. 2 L 7 2 4F RT A1NM 2007092000017 20070920 00017 NM 2007 9 20 DL757071212 1 20070915 A 5415 SUPPORT FITTING BOEING 757 757232 1384965 NM NR1 PYLON MIGRATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 658DL 24420 BUSHINGS MIGRATED IN NR 1 PYLON WING AND STRUT SUPPORT FITTINGS FOR UPPER LINK. BUSHINGS REPLACED PER EA 06-075079-03 A ND ERA 464036-14. 2 L 7 2 4F RT A2NM 2007092000018 20070920 00018 NE 2007 9 20 DL76G071214 2 20070915 A 7261 SCAVENGE PUMP BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 1 ENGINE UNSERVICEABLE A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 173DZ 29692 704738 AIRCRAFT 173 FLIGHT 161/15 DIVERTED TO SANTIAGO SPAIN, AFTER DEPARTING FROM ROME DUE TO LEFT ENGINE LOSS OF OIL QTY AND PRESSURE. ENGINE WAS SHUTDOWN PRIOR TO REACHING RED LINE. PERFORMED WINDMILL INSP, NO DEFECTS FOUND. REPLACED LUBE AN D SCAVENGE OIL PUMP PER MM. WINDMILLED ENG, NO LEAKING NOTED. RAN ENG FOR 5 MIN. INSPECTED MAIL OIL FILTER CLEANED BO WL RT ENG AGAIN 5 MIN TEMP PRESS NO LEAKS ALL OK. FILTER AND BOW CLEAN CHIP DETECTORS CLEAN. RESERVICED OIL TANK. 2 L 7 2 4F 4 F RT A1NM E13NE 2007092000020 20070920 00020 NM 2007 9 20 DL738071216 1 20070915 A 3350 B21506 FUSE BOEING 737 737832 13844CF NM EMERGENCY LIGHTS BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 381DN 30350 EMERGENCY LIGHTS IN SEATS 23DEF THROUGH 32DEF INOP DURING TEST. REPLACED ONE FUSE ON BATTERY POWER SUPPLY UNIT NUMBER M 01672. TEST GOOD. 2 L 7 2 4F RT A16WE 2007092000022 20070920 00022 NM 2007 9 20 QXEA200701427 1 20070914 A 2913 6618202 PUMP BOMBDR DHC8 DHC8402 1390042 NM HYD SYSTEM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 429QX 676 676 4161 RNO FLIGHT NR 2257: AFTER LANDING, NR 3 HYD PUMP CAUTION LIGHT ILLUMINATED. FOLLOWED E/A CHECKLIST. LIGHT REMAINED ON. MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC PUMP IAW 12-01-000-801, 12-01-400-801. BLED SYSTEM PER 29-10-00-870-80 3. OPS CHECK PER 29-12-01-710-801. RESERVICED NR 3 HYD SYSTEM IAW 12-10-29-611-807. OPS CHECK AND LEAK CHECK GOOD. R EPLACED RL4 RELAY AS REQUIRED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007092000024 20070920 00024 NM 2007 9 20 DL738071219 1 20070916 A 5240 DOOR BOEING 737 737832 13844CF NM POWER ACCESS OPEN A DALA A UNSCHED LANDING W E INADEQUATE Q C VIBRATION/BUFFET CR CRUISE 1 SO 27 380DA 30266 PASSING THRU 31000 SIGNIFICANT VIBRATION DEVELOPS IN THE NOSE PORTION OF AIRCRAFT FELT IT IN THE FLOOR. INTENSITY VARIE D A SMALL AMOUNT WITH CHANGE IN AIRSPEED. CONTACTED MX COOR AND DECISION WAS MADE TO DIVERT TO MCO TO CK IT OUT. FOUND EXT POWER ACCESS DOOR OPEN INSP DOOR FOR DAMAGE NONE NOTED ALL CKS NML. 2 L 7 2 4F RT A16WE 2007092000026 20070920 00026 NM 2007 9 20 DLM88071221 1 20070908 A 5320 FITTING DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 951DL 49882 FOUND CRACKED FITTING ON RT AFT ENTRANCE JAMB. REPLACED PER DWG3917624. 2 L 7 2 4F RT A6WE 2007092000027 20070920 00027 NM 2007 9 20 DLM88071222 1 20070908 A 5313 LONGERON DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 951DL 49882 FOUND CRACKED LONGERON. REPLACED PER DWG 5911406. 2 L 7 2 4F RT A6WE 2007092000029 20070920 00029 NM 2007 9 20 DLM88071224 1 20070908 A 5320 DOUBLER DOUG MD88 MD88 3023688 NM BULKHEAD CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 951DL 49882 FOUND CORROSION ON AFT PRESS DOME FWD VERTICLE DOUBLER. 2 L 7 2 4F RT A6WE 2007092000030 20070920 00030 NM 2007 9 20 DLM88071225 1 20070908 A 5730 SKIN DOUG MD88 MD88 3023688 NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 951DL 49882 FOUND CRACK ON WING FIXED L/E AT STA XRS 214, REPAIRED. 2 L 7 2 4F RT A6WE 2007092000031 20070920 00031 NM 2007 9 20 NWAA073096719 1 20070829 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 880 S9L CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING "M" CHECK, FOUND CRACKS IN FRAME WEB DOUBLER AT BS 880 S9L. REPAIRED PER EA 67-209743. 2 L 7 4 4F A20WE 2007092000032 20070920 00032 EA 2007 9 20 VNAA0708011 1 20070820 A 3244 H29X9015 TIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT MLG SEPARATED A VNAA O OTHER J WARNING INDICATION LD LANDING 1 GL 05 262PS 106 7962 CREW REPORTED DURING LANDING ROLLOUT RECEIVING A WOW INPUT CAUTION AND A PROX SYSTEM FAULT STATUS MESSAGES. MAINTENANCE INSPECTED AND FOUND THE LEFT HAND INBOARD MAIN TIRE TREAD HAD SEPARATED FROM THE WHEEL ASSEMBLY. MAINTENANCE REMOVED A ND REPLACED THE MAIN TIRE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE INSPECTED AND FOUND THE AIRCR AFT SAFE FOR FERRY FLIGHT TO DAYTON. MAINTENANCE REMOVED AND REPLACED DAMAGED FLAP ASSEMBLY. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007092000033 20070920 00033 EA 2007 9 20 VNAA0708012 1 20070821 A 5242 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE GROUND POWER OPEN A VNAA A UNSCHED LANDING O OTHER TO TAKEOFF 1 GL 05 710PS 10167 CREW RETURNED TO CLT DUE TO AN OPENED EXTERIOR AIRCRAFT PANEL. MAINTENANCE INSPECTED AND FOUND THE GROUND POWER DOOR LE FT OPEN. MAINTENANCE RESECURED DOOR CLOSED AND NO DAMAGE OR DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007092000034 20070920 00034 NM 2007 9 20 NWAA073166719 1 20070828 A 5320 TENSION TIE BOEING 747 747251F 1384898 NM CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING "M" CHECK, FOUND CRACKS IN UPPER LOBE TENSION TIE CHANNEL FASTENER HOLES AT BS 920 LBL 40 AND LBL 43. REPAIRED P ER EA 67-209741. 2 L 7 4 4F A20WE 2007092000035 20070920 00035 NM 2007 9 20 NWAA073176719 1 20070901 A 5330 SKIN BOEING 747 747251F 1384898 NM BS 1920 S31-34R DENTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING "M" CHECK, FOUND DENTS IN FUSELAGE SKIN AT BS 1920 S31R TO S34R. REPAIRED PER EA 67-209752. 2 L 7 4 4F A20WE 2007092000037 20070920 00037 NM 2007 9 20 NWAA073146719 1 20070828 A 5320 TENSION TIE BOEING 747 747251F 1384898 NM BS 820 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING "M" CHECK, FOUND CRACKS IN UPPER LOBE TENSION TIE CHANNEL FASTENER HOLES AT BS 820 RT. REPAIRED PER EA 67-209736 . 2 L 7 4 4F A20WE 2007092000038 20070920 00038 NM 2007 9 20 NWAA073156719 1 20070902 A 5320 FLOOR SUPPORT BOEING 747 747251F 1384898 NM BS 1140-1180 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING "M" CHECK, FOUND CORROSION ON UPPER CHORD OF MAIN DECK FLOOR BEAM BS 1140 TO BS 1180 RBL 55. REPAIRED PER EA 67- 209750. 2 L 7 4 4F A20WE 2007092000039 20070920 00039 2007 9 20 VNAA0708014 4 20070821 A 2360 STATIC WICK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HORIZ STAB DAMAGED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 249PS 7926 CREW REPORTED A LIGHTNING STRIKE ON LEFT SIDE OF NOSE. MAINTENANCE PERFORMED A VISUAL EN ROUTE INSPECTION FOR LIGHTNING STRIKE DAMAGE. MAINTENANCE PERFORMED A DETAILED LIGHTNING STRIKE INSPECTION AND FOUND DAMAGE TO THE LEFT HAND HORIZONT AL STAB TIP AND STATIC WICK AS WELL AS A DAMAGED RIVET ON TOP OF THE LEFT HAND ELEVATOR. MAINTENANCE REPLACED DAMAGED R IVET, STATIC WICK AND TEMP REPAIRED THE HORIZONTAL STAB TIP AS PER THE REO 10855 FROM BOMBARDIER. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007092000042 20070920 00042 NM 2007 9 20 NWAA073076719 1 20070902 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 1860 S11R DEFORMED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING "M" CHECK, FOUND DEFORMATION DAMAGE TO FRAME INNER CHORD AT BS 1860 S11R. REPAIRED PER EA 67-209754. 2 L 7 4 4F A20WE 2007092000044 20070920 00044 NM 2007 9 20 NWAA073086719 1 20070831 A 5320 REVEAL BOEING 747 747251F 1384898 NM BS 2231 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING "M" CHECK, FOUND CRACK IN MAIN DECK L5 DOOR FORWARD CUTOUT REVEAL DOUBLER AT BS 2231 BETWEEN S16L TO S18L. REPAI RED PER EA 67-209747. 2 L 7 4 4F A20WE 2007092000045 20070920 00045 NM 2007 9 20 NWAA073116719 1 20070902 A 5320 TENSION TIE BOEING 747 747251F 1384898 NM BS 800 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING "M" CHECK, FOUND CRACKS IN UPPER LOBE TENSION TIE CHANNEL FASTENER HOLES AT BS 800 LT. REPAIRED PER EA 67-209739 . 2 L 7 4 4F A20WE 2007092000046 20070920 00046 NM 2007 9 20 NWAA073126719 1 20070828 A 5320 TENSION TIE BOEING 747 747251F 1384898 NM BS 860 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING "M" CHECK, FOUND CRACKS IN UPPER LOBE TENSION TIE CHANNEL FASTENER HOLES AT BS 860 LT. REPAIRED PER EA 67-209738 . 2 L 7 4 4F A20WE 2007092000047 20070920 00047 NM 2007 9 20 NWAA073106719 1 20070831 A 5320 TENSION TIE BOEING 747 747251F 1384898 NM BS 900 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING "M" CHECK, FOUND CRACKS IN UPPER LOBE TENSION TIE FRAME WEB DOUBLER AT BS 900 LT. REPAIRED PER EA 67-209740. 2 L 7 4 4F A20WE 2007092000048 20070920 00048 WP 2007 9 20 DHLA200700044 1 20070918 A 2730 TRANSDUCER DOUG DC8 DC873F 302199F WP ELEVATOR MALFUNCTIONED A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 805DH 46125 REJECTED TAKEOFF DUE TO NO MOVEMENT ON EPI GAUGE. NO NOTICEABLE MOVEMENT OF ELEVATOR CONTROL DURING TAKEOFF ROLL. ELEV POS TXDCR CHANGED AND CHECKS SERV PER DC-8 M/M 27-30-0. A/C REPORTED TO HAVE OVER 300K LOAD W/FWD C/G LOADING ELEV SYS CHECKS SERV PER DC-8 M/M 27-30-0. 2 L 7 4 4F RT 4A25 2007092000049 20070920 00049 EA 2007 9 20 VNAA0708020 1 20070827 A 3244 18X44 TIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NLG FAILED A VNAA O OTHER O OTHER TO TAKEOFF 1 GL 05 213PS 69 7879 CREW REPORTED THE LEFT NOSE TIRE CAME APART ON TAKEOFF. CREW ELECTED TO CONTINUE ON TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CONFIRMED THE LEFT NOSE TIRE FAILURE AND DAMAGE TO THE NOSE LANDING GEAR FOLLOW UP DOOR. MA INTENANCE REMOVED AND REPLACED BOTH NOSE TIRES. MAINTENANCE ALSO REMOVED AND REPLACED NOSE LANDING GEAR DOOR IN ACCORDA NCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007092000050 20070920 00050 EU 2007 9 20 TRAX200701324 1 20070904 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 LEFT SEAT TRACK BETWEEN FR 36-39 FOUND CORRODED ON W/C 100-46. NEED TO FABRICATE NEW SEAT TRACK. FABRICATED AS PER SRM 53-63-00 FIG 201 LT SEAT TRACK INSTALLATION IS COVERED BY W/C 100-46. 2 H 7 2 4T RT 2007092000052 20070920 00052 EA 2007 9 20 TRAX200701327 1 20070905 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 834AS 7254 PAX DOOR STAIR 832CT IS CRACKED. REPAIRED IAW CRJ 200 SRM 51-40-11, 51-42-06, 51-42-21, 2 L 7 2 4F RT A21EA 2007092000053 20070920 00053 NE 2007 9 20 RU3A0708 2 20070830 A 7230 COMPRESSOR LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE RT ENGINE DAMAGED E RU3A A UNSCHED LANDING C F.O.D. AP APPROACH 1 SW 15 57 4197 039 PCE305198 WHILE CONDUCTING A LOW APPROACH (ILS-3 MANEUVER) AT THE LOGAN-CACHE, LOGAN, UTAH AIRPORT, AIRCRAFT INGESTED A BIRD WITHI N THE RIGHT ENGINE AS THE AIRCRAFT PASSED THE THRESHOLD AT AN ALTITUDE OF 50 FEET. THE WEATHER AT THE TIME OF THE INCID ENT WAS CLEAR SKY'S, GOOD VISIBILITY, AND CALM WINDS. THE AIRCRAFT EXPERIENCED NO ABNORMAL ENGINE INDICATIONS. THE FIR STINDICATION OF THE ENGINE BIRD INGESTION WAS A "FOUL" ODOR THROUGHOUT THE AIRCRAFT CABIN. THE RIGHT ENGINE BLEED AIR V ALVE WAS SELECTED OFF AND THE FLIGHT WAS SUBSEQUENTLY TERMINATED. A PRECAUTIONARY, UNEVENTFUL LANDING WAS MADE AT THE S ALT LAKE CITY INTL, SALT LAKE CITY, UTAH AIRPORT. THE AIRCRAFT WAS RELEASED TO MAINTENANCE FOR FURTHER EVALUATION. RT 2 L 7 2 4F 4 F RT A10CE E35NE 2007092000054 20070920 00054 EU 2007 9 20 TRBA2007076 1 20070911 A 3397 WIRE AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT BROKEN A TRBA O OTHER O OTHER NR NOT REPORTED 1 SO 29 288AM 288 EMERGENCY EXIT LIGHT ROW 6 INOPERATIVE. REPAIRED BROKEN WIRE ON EMERGENCY LIGHT ROW 6. PERFORMED OPERATIONAL CHECK AND FOUND WORKING PROPERLY PER MM 33-50-00. 2 H 7 2 4T RT A53EU 2007092000055 20070920 00055 SO 2007 9 20 SIMA200726002 1 20070917 A 3350 20131A BATTERY PACK EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHTS INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 722AE 145287 EMERGENCY LIGHTS ON BOTH OVERWING AND BACK SECTION OF CENTER AISLE EMERGENCY LIGHTS COME ON AND THEN GO DIM UNTIL COMPL ETELY OFF. REMOVED AND REPLACED NR 4 EMERGENCY LIGHTING ASSEMBLY IAW EMB AMM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RET URNED TO SERVICE 2 L 7 2 4F RT T00011AT 2007092000056 20070920 00056 SO 2007 9 20 SIAM200726003 1 20070916 A 2420 PC251123F INVERTER EMB 135 EMB135LR 3260305 SO BUSS MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 720AE 145279 AS CREW SET THRUST 115V BUSS OFF LINE WITH ASSOCIATED MESSAGES. DID LOW SPEED ABORT AND RETURNED TO GATE. REMOVED AND R EPLACED STATIC INVERTER IAW EMB135 AMM 24-20-01. OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007092000058 20070920 00058 SO 2007 9 20 RAIA00709004 1 20070906 A 5210 14539935405 CABLE EMB 145 EMB145EP 3260221 SO PAX DOOR WORN A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 826HK 145016 DURING SCHEDULED MAINTENANCE - RIC - MAINTENANCE FOUND THAT THE PASSENGER DOOR WOULD NOT OPEN AND CLOSE PROPERLY. MAINT ENANCE FOUND THE INTERNAL CABLE FOR THE HANDLE WORN. THE CABLE WAS REMOVED AND REPLACED AND THE PASSENGER DOOR FOLDING FLAP WAS ADJUSTED. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2007092000059 20070920 00059 NM 2007 9 20 DL76G071187 1 20070907 A 4900 APU BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE FAULTED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 169DZ 25374 29689 P1711 APU FAULT APU SHUT DOWN ON ENGINE START. STARTED ENGINE AT GATE NDF OK. PERFORMED BITE OF ECU LAST SHUTDOWN HIGH OIL T EMP CHECK APU OIL AND FILTER POP OUT. ALL CHECKS NORMAL, OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E13NE 2007092000064 20070920 00064 2007 9 20 HALA0700371 4 20070906 A 2565 5A32953 SLIDE & SLEEVE BOEING 767 76733A 1385209 NM L1 DOOR SLIDE UNWANTED DEPLOY A HALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 13 581HA 2134 28141 SLIDE RAFT AT L1 DOOR DEPLOYED. INSTALLED L1 DOOR SLIDE PER AMM 25-66-01. CLEARED MIC SHEET, REMOVED PLACARD. 2 L 7 2 4F RT A1NM 2007092000066 20070920 00066 NM 2007 9 20 F3LA200700234 1 20070914 A 5320 BLANKING PLATE AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 921FR 5402 2010 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON AFT BLANKING PLATE AT L2 DOOR. REPLACED L2 DOOR AFT GIRT BAR FITTING BLANKING PLATE IAW AMM 52-13-31-400-003. 2 L 7 2 4F RT A28NM 2007092000069 20070920 00069 NM 2007 9 20 SWAA074491 1 20070909 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 737JW 27869 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986, LBL 3 TO LBL 5. REPAIRED FLOORBEAM CHORD PER SRM. 2 L 7 2 4F RT A16WE 2007092000071 20070920 00071 NM 2007 9 20 SWAA074505 1 20070910 A 3350 417A5704 CAP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 466WN 30677 EEPLS END CAP LOOSE AT ROW 1 ABC. SECURED END CAP PER MM. 2 L 7 2 4F RT A16WE 2007092000072 20070920 00072 NM 2007 9 20 SWAA074507 1 20070910 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 513B, STR 15R. REMOVED AND REPLACED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007092000073 20070920 00073 NM 2007 9 20 SWAA074495 1 20070908 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 482B, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007092000076 20070920 00076 NM 2007 9 20 SWAA074494 1 20070908 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 790, STR 20L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007092000078 20070920 00078 NM 2007 9 20 SWAA074493 1 20070908 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007092000079 20070920 00079 NM 2007 9 20 SWAA074502 1 20070910 A 5315 6545810 FLOORBEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 12. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2007092000082 20070920 00082 NM 2007 9 20 SWAA074512 1 20070910 A 5330 6545890 BEAR STRAP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT BS 303.9, STR 10L TO STR 13L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007092000083 20070920 00083 NM 2007 9 20 SWAA074497 1 20070910 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092000085 20070920 00085 NM 2007 9 20 SWAA074506 1 20070910 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 L2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007092000086 20070920 00086 EA 2007 9 20 QXEA200701399 1 20070906 A 2430 TRU3502 TRU CNDAIR CL600 CL6002C10 1390015 EA INOPERATIVE A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 611QX 14425 10041 DEN - FLIGHT 4337, RECEIVED A TRU FAN FAIL MESSAGE. RETURNED TO THE GATE. MAINTENANCE PLACED THE TRU ON MEL. MAINTENA NCE REPLACED THE TRU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007092000087 20070920 00087 EA 2007 9 20 QXEA200701407 1 20070909 A 2751 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA TE FLAPS FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING AP APPROACH 1 NM 09 605QX 10022 ONT- FLIGHT 2567, RECEIVED A FLAPS FAIL CAUTION MESSAGE WHEN ATTEMPTING TO SELECT FLAPS TO 20 DEGREES. THE SYNOPTIC PAG E SHOWED THE FLAPS AND SLATS TO BE AT THE 1 DEGREE POSITION. ACCOMPLISHED THE CHECKLIST AND THE CAUTION CLEARED. ACCOM PLISHED A NORMAL LANDING. MAINTENANCE PERFORMED TASK 27-50-00-710-801-A01 OPERATIONAL CHECKS OF THE FLAPS AND SLATS WIT H NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007092000088 20070920 00088 NM 2007 9 20 SWAA074501 1 20070910 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092000089 20070920 00089 NM 2007 9 20 SWAA074498 1 20070910 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092000090 20070920 00090 EA 2007 9 20 QXEA200701405 1 20070910 A 2750 5913163 DETECTOR CNDAIR CL600 CL6002C10 1390015 EA TE FLAPS FAILED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 613QX 15284 10045 DEN - FLIGHT 2507, ON TAKEOFF ROLL, RECEIVED A FLAPS HALFSPEED STATUS MESSAGE. MAINTENANCE REPLACED THE LEFT INBOARD SK EW DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007092000091 20070920 00091 NM 2007 9 20 SWAA074500 1 20070910 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092000092 20070920 00092 NM 2007 9 20 SWAA074509 1 20070910 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007092000093 20070920 00093 EA 2007 9 20 QXEA200701406 1 20070909 A 2750 CONTROL HANDLE CNDAIR CL600 CL6002C10 1390015 EA TE FLAPS LACK OF LUBE A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 605QX 10022 ONT- FLIGHT 2568, ON TAXI TO THE RUNWAY, RECEIVED A FLAP HALFSPEED MESSAGE AND A SLATS HALFSPEED MESSAGE. RETURNED TO T HE GATE. MAINTENANCE CYCLED SHIPS POWER AND THE FLAP CONTROL HANDLE, AND LUBED THE FLAP CONTROL HANDLE. ALL CHECKS GOO D. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007092000094 20070920 00094 NM 2007 9 20 SWAA074513 1 20070910 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007092000095 20070920 00095 NE 2007 9 20 QXEA200701369 2 20070831 A 7320 4120T02P02 ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE NR 1 ENGINE LEAKING A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 610QX 13244 10033 PDX - FLIGHT 2523, LEFT ENGINE WEEPS FUEL WHEN THE BOOST PUMPS ARE SELECTED TO ON. MAINTENANCE FOUND THE MASTER COMPRES SOR VARIABLE GEOMETRY ACTUATOR WAS LEAKING ON NR 1 ENGINE. REPLACED ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 2007092000096 20070920 00096 NM 2007 9 20 SWAA074510 1 20070910 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 2007092000097 20070920 00097 NM 2007 9 20 SWAA074508 1 20070910 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 2007092000100 20070920 00100 NM 2007 9 20 SWAA074492 1 20070909 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 737JW 27869 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 12 TO LBL 17. REPAIRED FLOORBEAM CHORD PER SWA EA. 2 L 7 2 4F RT A16WE 2007092000101 20070920 00101 2007 9 20 SWAA074496 4 20070910 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007092000104 20070920 00104 CE 2007 9 20 20070907211RN 1 20070907 A 2435 66084582 STARTER GEN LEAR 35 31A 5170531 CE LEFT FAILED E S2KA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 EA 03 211RN 669 072 STARTER GENERATOR FAILED DURING FLIGHT, CREW NOTICED VIBRATION FOLLOWED BY ILLUMINATION OF THE LEFT GENERATOR LIGHT. AI RCRAFT LANDED WITHOUT INCIDENCE AND STARTER GENERATOR WAS REPLACED. 2 L 7 2 4F RT A10CE 2007092000105 20070920 00105 WP 2007 9 20 NWAA073019917 1 20070723 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 998 S28-29R CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 617NW 47235 DURING "H" CHECK, FOUND CRACKS IN FRAME AT BS 998 BETWEEN L29R AND L28R. REPAIRED PER EA 99-210168. 2 L 7 2 4F A6WE 2007092000106 20070920 00106 SO 2007 9 20 RAIA00709006 1 20070907 A 3230 23092900001 UPLOCK EMB 145 EMB145 3260210 SO NLG MALFUNCTIONED A RAIA A UNSCHED LANDING O OTHER TO TAKEOFF 1 CE 03 805HK 19889 10433 145096 FLT 3508 - BDL - ON TAKEOFF, LANDING GEAR INDICATED 3 UP AND LOCKED BUT THE NOSE GEAR DOORS APPEARED TO CLOSE SLOWLY CAU SING NOSE DRAG. MAINTENANCE REMOVED AND REPLACED THE NLG UPLOCK. ALL OPERATIONAL CHECK WERE GOOD. 2 L 7 2 4F RT T00011AT 2007092000109 20070920 00109 NM 2007 9 20 F3LA200700235 1 20070914 A 5210 BLANKING PLATE AIRBUS A319 A319111 3930336 NM R2 DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 921FR 5402 2010 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON FWD BLANKING PLATE AT R2 DOOR. REPLACED R2 DOOR FWD GIRT BAR FITTING BLANKING PLATE IAW AMM 52-13-31-400-003. 2 L 7 2 4F RT A28NM 2007092000110 20070920 00110 NM 2007 9 20 DHL2007746529 1 20070826 A 5743 BEAM BOEING 727 727224 1384076 NM MLG CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 LEFT WING, NR 4 FLAP TRACK TO MAIN LANDING GEAR BEAM ATTACH POINT HAS PITTING CORROSION (MARKED). REMOVED CORROSION FRO M MAIN LANDING GEAR BEAM AT THE NR 4 FLAP TRACK ATTACH AREA IAW B727 SRM 51-10-6 AND BOEING TELEX NR 1-520765353 TO A 5 TO 1 BLEND RATION WITH A 1" RADIUS. MAXIMUM MATERIAL LOSS AT ANY ONE AREA .125. HFEC REWORKED AREA NO DEFECTS NOTED IA W MM PT6 51-00-00. SHOT PEENED AREA IAW BOEING SOPM 20-10-03. TREATED AND PRIMED AREA IAW B727 SRM 51-10-2. FOUND REP AIRED AREA TO BE STRUCTURALLY ACCEPTABLE IAW BOEING TELEX NO 1-520795353. 2 L 7 3 4F A3WE 2007092000111 20070920 00111 NM 2007 9 20 DHL2007746533 1 20070903 A 5230 655714052 FRAME BOEING 727 727224 1384076 NM BS 600 GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 C1 DOOR LOWER FRAME GOUGED BODY STATION 600. REMOVED LOWER FRAME C1 DOOR IAW B727 SRM 51-30-2. DRILLED HOLES AT NEW FR AME SRM 51-30-5. NEW DEPRESSOR PN 65-57140-52 PO NR 7268213. INSTALLED NEW LOWER FRAME (DEPRESSOR) IAW B727 SRM 51-30- 2. LEAK CHECK GOOD IAW B727 MM 21-31-00. 2 L 7 3 4F A3WE 2007092000114 20070920 00114 EA 2007 9 20 SWIA200718639 1 20070702 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SW 7034 ANGLE AT FS 280 LBL 9-RBL 9 IS CORRODED. FOUND AT C-CHECK, REPLACED SUPPORT ANGLE PER SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007092000116 20070920 00116 NM 2007 9 20 2007UALA03591 1 20070905 A 2621 FIRE BOTTLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LT ENGINE LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 369UA 24538 LEFT ENGINE (FORWARD) FIRE BOTTLE LOW PSI, READS 700 PSI. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800188 20070918 00188 NM 2007 9 18 2007UALA03559 1 20070903 A 3397 CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN PULLED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 658UA 27113 EEL LIGHT CABLE PULLED OUT OF TRACK FWD OF SEAT 1E. 2 L 7 2 4F 4 F RT A1NM E24NE 2007091800194 20070918 00194 NM 2007 9 18 2007UALA03566 1 20070905 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EMERGENCY CEILING LIGHT INOP 5A. 2 L 7 4 4F 4 F RT A20WE E24NE 2007091800195 20070918 00195 NM 2007 9 18 2007UALA03567 1 20070905 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EEL3J FWD & 33H ARE INOP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007091800197 20070918 00197 NM 2007 9 18 2007UALA03569 1 20070903 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 THE -A- ZONE, EEL'S INOP RIGHT ROW OF SEATS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007091800199 20070918 00199 NM 2007 9 18 2007UALA03571 1 20070903 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 UPPER DECK FWD RT SEATS, EEL'S INOP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007091800201 20070918 00201 NM 2007 9 18 2007UALA03573 1 20070904 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE AFT CARGO BAY ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 522UA 24931 ELECTRICAL ODOR IN DOORWAY AREA OF AFT CARGO PIT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091800215 20070918 00215 EU 2007 9 18 2007UALA03578 1 20070904 A 3350 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS CRUSHED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 402UA 439 SEATS 1, 2, 3, 6, 19 FLOOR PROXIMITY LIGHTS INOP. FOUND CRUSHED WIRING AND WEAK BATTERY/EPSU. REPLACED BATTERY AND E PSU AND REPAIRED AND RELAMPED UNITS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007091800232 20070918 00232 NM 2007 9 18 KCSA071333 1 20070908 A 5311 DOUBLER BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA -520 FRAME DOUBLER CRACKED BETWEEN STRINGER -30L AND 31L 1.5 INCH. 2 L 7 4 4F RT A20WE 2007091800238 20070918 00238 EA 2007 9 18 COMA0760551 1 20070831 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA LANDING GEAR MALFUNCTIONED A COMA K NONE N FALSE WARNING AP APPROACH 1 SO 01 587SW 7062 FLIGHT 9423 - GEAR DISAGREE ON APPROACH AFTER 45 MINUTES AT 30,000 FT, APPROX 10 SECONDS AFTER SELECTING GEAR DOWN, CLEA RED ON ITS OWN. CYCLED 5 MORE TIMES, COULD NOT DUPLICATE. A/C LANDED SAFELY. RE-RIGGED RIGHT NLG DOOR UP PROX SENSOR. 2 L 7 2 4F RT A21EA 2007091800241 20070918 00241 NM 2007 9 18 UPS07550624 1 20070803 A 5311 146N10045 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 415UP 23855 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1260, S26L. ACCOMPLISHED PER FINAL EA 757-5362-27-A1730 AND UPS EO B757-5310- 27526-A AND SRM 53-00-07, DETAIL 1, FIG 201 (SHT 4 OF 15). THIS IS A CATEGORY -B- REPAIR AND REQUIRES INS PECTION PER TABLE 11, ZONE 1, FIG 201 (SHT 10 OF 15). 2 L 7 2 4F RT A2NM 2007091800255 20070918 00255 NM 2007 9 18 SWAA074488 1 20070909 A 5755 654645268A FITTING BOEING 737 7373H4 1384600 NM NR 4 SPOILER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED MV2 CHECK, FOUND LEFT WING NR 4 SPOILER OUTBOARD ACTUATOR FITTING BROKEN. REMOVED AND REPLACED NR 4 SP OILER PER MM. 2 L 7 2 4F RT A16WE 2007091800267 20070918 00267 SO 2007 9 18 C2XA07ON020 1 20070907 A 3350 1317 LIGHT EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12195 145943 FLT MX - ONT - WHILE PERFORMING 3A CHECK AND OPERATIONAL INSPECTION OF THE EMERGENCY LIGHTING SYSTEM. QC INSPECTOR FOUN D SERVICE DOOR EMERGENCY LIGHT DID NOT ILLUMINATE (DOOR PATH LIGHTING). MX PERSONNEL REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT BULB IAW EMB 145XR AMM 33-50-09. OPERATIONALLY CHECKED GOOD AND AIRCRAFT WAS RELEASE TO RETURN FOR SERV ICE IN AIRWORTHY CONDITIONS. 2 L 7 2 4F RT 2007091800268 20070918 00268 NM 2007 9 18 USAA920070818 1 20070907 A 5320 6946882 TIE CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR, CRACKED TIE CLIP, BS 360, S10L. REPLACED TIE CLIP, BS 360, S10L IAW 737-400 SRM 53-10-01 AND EO 530 5V203. 2 L 7 2 4F RT A16WE 2007091800270 20070918 00270 SW 2007 9 18 WGEA200700004 1 20070908 A 5310 531116812005 BEAM ECLIPS EA500 ECLIPSEEA500 3350000 SW COCKPIT DAMAGED E WGEA K NONE O OTHER IN INSP/MAINT 1 EA 27 119DJ 72 000022 REPAIR OF FORWARD UPPER RIGHT WINDSHIELD BEAM PART NUMBER 53-111681-2005. REPAIRED IAW ECLIPSE AVIATION SERVICE ENGINEE RING MEMO, MEMO SEM 500-0076 REV A. 1 L 7 2 4J RT A00002AC 2007091800273 20070918 00273 SO 2007 9 18 C2XAO7SH064 1 20070908 A 5320 14532638001 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13997 145298 SHV - DURING C-CHECK MAINTENANCE FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 29. MAINTENANCE REPAIRED THE LEFT OMEG A BEAM AT FRAME 29 IAW EMB 145 SRM 53-00-10 FIG 202. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007091800281 20070918 00281 SO 2007 9 18 C2XA07IA196 1 20070907 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18101 145590 IAH - FLIGHT 2050, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE CABIN EMERGENCY LIGHTS WERE INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS A PPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007091800285 20070918 00285 NM 2007 9 18 KCSA071337 1 20070910 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-1330 LBL-11 SEAT TRACK LOWER RADIUS HAS A 6 INCH CRACK AT CENTER GUIDE ALIGNMENT HOLE. 2 L 7 4 4F RT A20WE 2007091800286 20070918 00286 NM 2007 9 18 KCSA071338 1 20070910 A 5315 FLOORBEAM BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FLOORBEAM UPPER CHORD IS CORRODED AT STA-1700 LBL 21 WL-200. 2 L 7 4 4F RT A20WE 2007091800297 20070918 00297 NM 2007 9 18 KCSA071349 1 20070910 A 5311 FRAME BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-520 FRAME CRACKED AT STR-11R CUTOUT. 2 L 7 4 4F RT A20WE 2007091800298 20070918 00298 NM 2007 9 18 KCSA071350 1 20070910 A 5311 FRAME BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-520 FRAME CRACKED AT OUTER FLANGE AT RIVET HOLE BETWEEN STR-10R AND STR-10A/R .5 INCH. 2 L 7 4 4F RT A20WE 2007091800302 20070918 00302 NM 2007 9 18 KCSA071354 1 20070910 A 5711 SPAR CAP BOEING 747 7472B4B 138481B NM RT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 RIGHT WING FRONT SPAR BOTTOM CAP AT HOLES 1480 HAS CORROSION IN L/E CAVITY. 2 L 7 4 4F RT A20WE 2007091800304 20070918 00304 EA 2007 9 18 TRAX200701322 1 20070904 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 875AS 7559 AAR - WEB DOOR CUT OUT HAS A CRACKED CLIP ON LEFT CENTER SIDE AT FS 700. REPAIRED IAW CRJ 200 SRM 53-61-23. 2 L 7 2 4F RT A21EA 2007091900009 20070919 00009 EU 2007 9 19 07FDEA03766 1 20070914 A 5320 A53974408200 COUPLING AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION AT COUPLING P 53LT, C 55/58 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900017 20070919 00017 EU 2007 9 19 07FDEA03754 1 20070914 A 5313 A53974203225 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION ON STRINGER P 54 RT, C 68-69 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007091900018 20070919 00018 EU 2007 9 19 07FDEA03753 1 20070914 A 5320 STRAP AIRBUS 310 A310222 3930315 EU L1 DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 446FE 224 LT FWD PAX/CREW DOOR CUTOUT, HFEC INSPECTION INDICATES CRACK/CORROSION IN 5 LOCATIONS ALONG EDGE OF LOWER CORNER STRAPS AS FOLLOWS; (1) FWD LOWER CORNER- ONE 1/2" LONG AND ONE 1.0" LONG AND, (2) AFT LOWER CORNER - ONE 2 1/4" LONG, ONE 3/8 " LONG AND ONE 2" LONG. UNABLE TO VERIFY DEPTH USING ULTRASOUND PER NTM 53-30-02, 401, POSSIBLY DUE TO MINIMAL DEPTH OF DEFECTS. UNABLE TO SEE VISUALLY DUE TO PREVIOUS BUFFING OF AREA. 09-24-07 REMOVED FWD AND AFT TAPERED SHIMS, FABRIC ATED NEW FWD AND AFT TAPERED SHIMS, AND INSTALLED NEW FWD AND AFT TAPERED SHIMS IAW A310-200 SRM 51-20-41 AND AB DWG A53611516. ALODINED AND PRIMED IAW A310-200 MM 51-23-10-0. MAJOR REPAIR. 2 L 7 2 4F RT A35EU 2007091900025 20070919 00025 EU 2007 9 19 07FDEA03746 1 20070914 A 5320 A53778449200 ANGLE AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION FOUND ON REINFORCING ANGLE AT C38-39, P 48 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900032 20070919 00032 EU 2007 9 19 07FDEA03727 1 20070914 A 5320 STRAP AIRBUS 310 A310322 3930334 EU R1 DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 446FE 224 AREA IS RT FWD PAX/CREW DOOR CUTOUT, 3 5/8 INCH CRACK WITH POSSIBLE EXFOLIATION CORROSION EXISTS ALONG TOP EDGE OF AFT CORNER STRAP, BEGINNING 1" FROM FWD EDGE OF CORNER STRAP. (LOWER, AFT CORNER OF DOOR CUTOUT BEHIND FAIL/SAFE RING) AREA MARKED IN RED. SEE ATTACHMENTS FOR DETAILS. FOUND USING HFEC INSPECTION NOTE: EVIDENCE OF PREVIOUS BLENDOUT PRESENT I N SAME EXACT AREA. 09-20-07 REMOVED AFT TAPERED SHIM IAW A310-200 SRM 51-40-21 PARA 7. INSTALLED TAPERED SHIM IAW FEDEX A310-200 SRM 51-40-21 PARA 7. MAJOR REPAIR. 2 L 7 2 4F RT A35EU 2007091900040 20070919 00040 EU 2007 9 19 MALA070116 1 20070912 A 2150 7769106 ACM SAAB SF340 340B 7860101 EU RIGHT SEIZED A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 456XJ 340B456 AIR RETURN DUE TO ODOR COMING FROM RIGHT BLEED. FOUND ACM TO HAVE SEIZED. REPLACED RIGHT ACM - PN 776910-6. 2 L 7 2 4T RT A52EU 2007091900048 20070919 00048 EU 2007 9 19 07FDEA03716 1 20070824 A 5347 A53278423200 SEAT TRACK AIRBUS 310 A310322 3930334 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 AFT SEAT TRACK AT Y 1390 WITH CORROSION OUT OF SRM ALLOWABLE VALUES NEXT TO FR68. SEAT TRACK REPAIRED IAW SRM 53-16-10, FIG 202. 2 L 7 2 4F RT A35EU 2007091900055 20070919 00055 NM 2007 9 19 07FDEA03709 1 20070913 A 5315 6520821225 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 FLOORBEAM T- CAP CORRODED, STA 620, LBL 1-25 REMOVED CORROSION REF SRM 51-10-6, DUE TO SSI LOCATION NO BLENDING IS ALLOW ED. TRIMMED T- CAP AND MFG REPAIR PARTS REF SR27-53-034 AND INSTALLED REPAIR PARTS. REF SR27-53-034 AND SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007091900059 20070919 00059 EU 2007 9 19 07FDEA03704 1 20070913 A 5311 A53973020211 FRAME AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION AT MILLING FRAME C60, P 22RT REPAIR PERFORMED BY BLEND OUT CORROSION IAW RAS/DATLS/0001942/2004. 2 L 7 2 4F RT A35EU 2007091900061 20070919 00061 EU 2007 9 19 07FDEA03702 1 20070913 A 5313 A53612519202 LONGERON AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 HEAVY CORROSION ON EXTRUSION (LONGERON) Y-953 RT, BETWEEN FRAME 12A-14, OUT OF LIMIT IAW SRM 53-10-00/TB 102. EXTRUSION REPAIR PERFORMED BY INSTALLING REINFORCING PROFILES IAW SRM 53-12-15/FIG 207. 2 L 7 2 4F RT A35EU 2007091900068 20070919 00068 EU 2007 9 19 07FDEA03695 1 20070913 A 5313 A53612214200 LONGERON AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 HEAVY CORROSION ON LONGERON Y730, BETWEEN FRAME 11-14, OUT OF LIMIT IAW SRM 53-10-00/TB 102. REPLACEMENT OF LONGERON (S UPPORT) IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900070 20070919 00070 EU 2007 9 19 07FDEA03693 1 20070913 A 5320 A53974225 WEB AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 BOTH CROSS SHEETS AT FRAME 69 IN BULK CARGO COMPARTMENT DENTED AND CRACKED. REPLACEMENT OF BOTH CROSS SHEETS LT AND RT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900074 20070919 00074 EU 2007 9 19 07FDEA03689 1 20070913 A 5313 A53612213210 LONGERON AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 HEAVY CORROSION ON LONGERON Y-1959 RT, BETWEEN FRAME 12A -19, OUT OF LIMIT IAW SRM 53-10-00/TB 102. REPLACEMENT OF LONG ERON IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900082 20070919 00082 EU 2007 9 19 07FDEA03626 1 20070912 A 5320 A53986733207 WEB AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 FOUND DAMAGED WEB PLATE BETWEEN FRAME 86-87, STRG 39 RT. REPLACEMENT OF WEB PLATE IAW SRM 51-72-10 AND SRM 53-19-18 / P G 76 / ITEM 10. 2 L 7 2 4F RT A35EU 2007091900093 20070919 00093 EU 2007 9 19 07FDEA03612 1 20070912 A 5315 A53974219 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 812FD 467 OLD REPAIR AT CROSSBEAM FRAME 63 BETWEEN Y500 AND Y1160 IN AFT CARGO COMPARTMENT FLOOR STRUCTURE, NOT CONFORM TO SRM 5 3-10-15 / 207. SPLICE REPAIR RENEWED IAW SRM 53-10-15/FIG 207. 2 L 7 2 4F RT A35EU 2007091900097 20070919 00097 EU 2007 9 19 07FDEA03608 1 20070912 A 5313 A53974203 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 CORROSION ON STRINGER 57 BETWEEN FRAME 65-67 AD, OUT OF LIMIT. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 20 1. 2 L 7 2 4F RT A35EU 2007091900099 20070919 00099 EU 2007 9 19 07FDEA03606 1 20070912 A 5522 SKIN AIRBUS 310 A310324 3930206 EU ELEVATOR DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 FOUND DELAMINATION ON UPPER SKIN ON TRAILING EDGE OF RT ELEVATOR BETWEEN RIB 6-8. REPAIR OF CORE AND INSTALLING EXTERNA L REPAIR STRAP, PERFORMED BY EA 6-5521-92209 AND RAS/CASA/4419/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091900101 20070919 00101 EU 2007 9 19 07FDEA03604 1 20070912 A 5313 A53974202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 HEAVY CORROSION ON STRINGER 52 BETWEEN FRAME 55/58-60 LHS. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14 / FIG 201. 2 L 7 2 4F RT A35EU 2007091900106 20070919 00106 EU 2007 9 19 07FDEA03599 1 20070912 A 5347 A53612357200 SEAT TRACK AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 HEAVY CORROSION AT SEAT TRACK BETWEEN FRAME 14-19, STRG 26 RHS, OUT OF LIMIT. REPLACEMENT OF SEAT TRACK IAW SRM 51-72- 10. 2 L 7 2 4F RT A35EU 2007091900107 20070919 00107 EU 2007 9 19 07FDEA03598 1 20070912 A 5347 A53611640200 SEAT TRACK AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 HEAVY CORROSION AT SEAT TRACK BETWEEN FRAME 15A-19, STRG 26 RHS, OUT OF LIMIT. REPLACEMENT OF SEAT TRACK IAW SRM 51-72- 10. 2 L 7 2 4F RT A35EU 2007091900116 20070919 00116 EU 2007 9 19 07FDEA03576 1 20070911 A 5730 A57243206203 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 FOUND THREE CHAFING MARKS ON LEADING EDGE D-NOSE SKIN BETWEEN SLAT TRACK 6 AND JACK 4 RT WING. NOSE SKIN REPAIR PERFORM ED IAW SRM 57-41-12/ FIG 204 WITH ALTERNATIVE MATERIAL, APPROVED BY EA 6-5741-92200 AND RAS/BAE/1001636/2005 ISSUE B. 2 L 7 2 4F RT A35EU 2007091900166 20070919 00166 NM 2007 9 19 AALA20071596 1 20070821 A 3350 OL3071BPEGPL BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 775AN 29584 JFK - EMERGENCY LIGHT AT SEAT 37C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 37C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091900179 20070919 00179 NM 2007 9 19 AALA20071564 1 20070813 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 AFW - EMERGENCY LIGHTS AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT NUMBER T WO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091900193 20070919 00193 NM 2007 9 19 AALA20071557 1 20070815 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 603AA 27054 SFO - SEAT MOUNTED EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK M10959 AT STATION 1095 FOR SEAT MOUNTED EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007091900194 20070919 00194 NM 2007 9 19 AALA20071556 1 20070815 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 603AA 27054 SFO - EMERGENCY LIGHTS AT LEFT AND RIGHT LOWER EXIT DOOR INOPERATIVE. REPLACED BATTERY PACK M10801 AT STATION 1635 FOR EMERGENCY LIGHTS AT LEFT AND RIGHT LOWER EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007091900198 20070919 00198 NM 2007 9 19 AALA20071590 1 20070819 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 929AN 30078 LAX - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR SLIDE INOPERATIVE. FOUND MISCONNECTION FOR DOOR EXIT IDENTIFIER. RECONN ECTED WIRING FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092000011 20070920 00011 NM 2007 9 20 DLM88071204 1 20070908 A 5310 BEAM DOUG MD88 MD88 3023688 NM BS 370-427 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 951DL 49882 CORROSION ON LWR BEAM AT FWD COMPARTMENT JAMB STA 370-427, REPLACED BEAM PER SRM 53-05D FIG 804D. 2 L 7 2 4F RT A6WE 2007092000019 20070920 00019 SO 2007 9 20 C2XA07IA197 1 20070909 A 2120 UNKNOWN EMB 135 EMB135LR 3260305 SO COCKPIT ODOR A C2XA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION IN INSP/MAINT 1 SW 27 14514 145303 IAH - FLIGHT 2890, DURING PRE-FLIGHT INSPECTION, THE NUMBER ONE ELECTRIC HYDRAULIC PUMP FAILED AND A SMOKE SMELL WAS REP ORTED IN THE COCKPIT. MAINTENANCE OPERATIONALLY TESTED THE ELECTRIC HYDRAULIC PUMP WITH NO DEFECTS NOTED, AND COULD NOT DUPLICATE THE SMOKE SMELL. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007092000040 20070920 00040 NM 2007 9 20 NWAA073056719 1 20070831 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 280 S24L/R CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING "M" CHECK, FOUND CRACKS IN FRAME AT BS 280 S24R TO S24L. REPAIRED PER EA 67-209749. 2 L 7 4 4F A20WE 2007092000041 20070920 00041 NM 2007 9 20 NWAA073066719 1 20070901 A 5312 BULKHEAD BOEING 747 747251F 1384898 NM BS 2360 S26L WORN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING "M" CHECK, FOUND WEAR ON BULKHEAD AT BS 2360 S26L. REPAIRED PER EA 67-209753. 2 L 7 4 4F A20WE 2007092000060 20070920 00060 EU 2007 9 20 CPCP20070108 1 20070822 A 5752 CHANNEL AEROSP ATR72 ATR72212 8680945 EU AILERON TAB CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 414WF 414 LT AILERON, TRIM TAB, CLOSING CHANNEL CORRODED. NEW TRIM TAB CLOSING CHANNEL REPLACED ON LT AILERON IAW SRM 51-25-03. 2 H 7 2 4T RT A53EU 2007092000061 20070920 00061 SO 2007 9 20 RAIA00709005 1 20070906 A 2910 14533603439 TUBE EMB 145 EMB145LR 3260212 SO HYDRAULIC SYSTEM LEAKING A RAIA B A EMER. DESCENT UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 03 831HK 145232 FLT 7897 - LIT - HYDRAULIC SYSTEM LOW QUANTITY MESSAGE IN FLIGHT AND READING -0- QUANTITY ON THE GROUND. MAINTENANCE RE MOVED AND REPLACED A-HYDRAULIC TUBE AT THE WING STUB. LEAK CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007092000068 20070920 00068 NM 2007 9 20 SWAA074514 1 20070910 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 750SA 29802 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 36 TO LBL 43. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007092000070 20070920 00070 NM 2007 9 20 SWAA074504 1 20070910 A 3350 20121 CHARGER BOEING 737 7373H4 1384600 NM CABIN FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 MID CABIN EMERGENCY EXIT LIGHTS ILLUMINATED AND WOULD NOT TURN OFF. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007092000074 20070920 00074 NM 2007 9 20 SWAA074503 1 20070910 A 5330 6545768 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING DUCT EXHAUST BS 378, BL 0. REPAIRED SKIN P ER EA. 2 L 7 2 4F RT A16WE 2007092000075 20070920 00075 NM 2007 9 20 SWAA074515 1 20070910 A 5330 6545768 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 387 AND BS 395, STR 17R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007092000081 20070920 00081 NM 2007 9 20 AWXA200701111 1 20070814 A 5320 69434961 CHANNEL BOEING 737 7373G7 1384595 NM ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 MCN - MAJOR REPAIR - C-18 CHECK - NR 5987854, CORROSION ON AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL CHANNEL, BS 847 - BS 867, S26R. REPLACED AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL CHANNEL, BS 847 - BS 867, S26R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007092000098 20070920 00098 EA 2007 9 20 QXEA200701370 1 20070902 A 2612 47359719 DETECTOR CNDAIR CL600 CL6002C10 1390015 EA FIRE DETECTION FALSE INDICATION A QXEA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 615QX 13888 2798 10065 PDX - FLIGHT 2555, ON POWER UP RECEIVED A FIRE SYSTEM FAULT MESSAGE. MAINTENANCE REPLACED THE NR 2 FORWARD SMOKE DETECT OR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007092000099 20070920 00099 NM 2007 9 20 SWAA074499 1 20070910 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092000102 20070920 00102 NM 2007 9 20 USAA920070822 1 20070905 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 591US 23936 CLT - MAJOR REPAIR - CRACKED FUSELAGE SKIN, BS 727D, S23R. REPAIRED FUSELAGE SKIN, BS 727D, S23R IAW USAIRWAYS TYPICAL REPAIR 53-50-03A AND B737-300 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2007092000103 20070920 00103 NM 2007 9 20 NWAA073205654 1 20070917 A 2120 UNKNOWN BOEING 757 757251 1384970 NM CABIN ODOR A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 01 554NW 26501 FLIGHT ATTENDANT REPORTED ELECTRICAL ODOR COMING FROM AFT GALLEY BEHIND LAV D, NO SMOKE WAS SIGHTED BUT HEAVY ELECTRICAL ODOR. ALL AFT GALLEY POWER WAS REMOVED WITH NO HOT SPOTS FELT, ELECTRICAL ODOR DID DISSIPATE THEREAFTER. MAINTENANCE INSPECTED AFT GALLEY CIRCUIT BREAKERS, NO ELECTRICAL ODOR NOTED, NO CIRCUIT BREAKERS POPPED, AND INSPECTED AFT GALLEY. AIRCRAFT OK FOR RETURN TO SERVICE. 2 L 7 2 4F RT A2NM 2007092000108 20070920 00108 NM 2007 9 20 2007UALA02864 1 20070725 A 3510 MR35114 OXYGEN MASK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 836UA 1460 CREW O2 AT 750 PSI. *S/D* 2ND OBSERVERS MASK LEAKING. REPLACED 2ND OBSERVERS MASK AND SERVICED CREW O2 SYSTEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092000112 20070920 00112 NM 2007 9 20 P5CA0701533 1 20070916 A 7830 STRUCTURE BOEING 747 74747UF 1384812 NM THRUST REVERSER LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 416MC 32838 DURING DAILY CHECK, FOUND NR 1 THRUST REVERSER INNER WIRE MESH BONDING LOOSE AND MISSING BETWEEN 6 AND 10 O'CLOCK POSITI ONS. INTERIM REPAIR ACCOMPLISHED AS PER XEO 78-091604/FAA 8110-3. 2 L 7 4 4F RT A20WE 2007092000113 20070920 00113 SO 2007 9 20 LR7A07090 1 20070910 A 5320 FITTING LKHEED 382 382G 526414U SO FS 858,WL 256 BROKEN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 455 5025 DURING SCHEDULED A- CHECK PER JOB CARD HA1200, FOUND RT UPPER STANCHION FITTING BROKEN AT FS 858, WL256, RBL62. REPLACE D FITTING IAW SMP583 CHAPTER 51-70-04 AND DWG 343194. LOG PAGE 20343 ITEM M2. 2 H 7 4 4T A1SO 2007092000115 20070920 00115 NE 2007 9 20 NWAA073189967 2 20070914 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D15A 52051 NE NR 2 SEIZED A NWAA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION AP APPROACH 1 GL 01 9331 47263 688633 DURING APPROACH AT 1000 FEET FLIGHT CREW HEARD A LOUD BANG AND FELT AIRCRAFT YAW. FLIGHT CREW LOG ENTRY STATES ENGINE " SEIZED" AND N1, N2 INDICATING 0. FLIGHT CREW PERFORMED A UNEVENTFUL LANDING. MAINTENANCE REPLACED ENGINE NR 2. 2 L 7 2 4F 4 F A6WE E2EA 2007092000118 20070920 00118 EA 2007 9 20 QXEA200701414 1 20070910 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002C10 1390015 EA ELEVATOR SPLIT FALSE ACTIVATION A QXEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 09 602QX 10010 MFR - FLIGHT 2525 (PDX-SJC). IN LEVEL FLIGHT AT CRUISE ALTITUDE (39,000) FOR 3 MINUTES, THEN RECEIVED A ELEVATOR SPLIT C AUTION MESSAGE. DISCONNECTED THE AUTOPILOT PER THE CHECKLIST, CONTROLS FEEL NORMAL NO ADVERSE OR ABNORMAL CONTROL FEEL OR RESPONSE. SYNOPTIC PAGE SHOWED ELEVATORS MATCHED. DIVERTED TO MFR AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENAN CE PERFORMED FIM TASK 27-31-00-810-803-A01, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007092000119 20070920 00119 EA 2007 9 20 QXEA200701408 1 20070906 A 5210 601R317631 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 614QX 10049 DEN - MAIN CABIN DOOR OUTER HANDLE HAS A 1/2 INCH CRACK IN THE CIRCULAR BOSS (KEYHOLE REINFORCEMENT AREA). MAINTENANCE REPLACED THE MAIN CABIN DOOR OUTER HANDLE IAW AMM 52-11-03-400-801-A01. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007092000120 20070920 00120 EA 2007 9 20 QXEA200701409 1 20070908 A 5210 SKIN CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 614QX 10049 PDX - MAIN CABIN DOOR INNER SKIN CRACKED AT FUSELAGE STATION 335 NEXT TO INTERCOSTAL DD6. MAINTENANCE REPAIRED IN ACCOR DANCE WITH REO 670-52-11-277. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007092000121 20070920 00121 NM 2007 9 20 2007UALA03593 1 20070905 A 5520 ELEVATOR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU LEFT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 929UA 26652 LEFT HAND ELEVATOR FAILED FREE PLAY CHECK AND WAS FOUND WITH NO HINGE PUTTY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092000123 20070920 00123 EU 2007 9 20 07FDEA03549 1 20070911 A 5315 A53974219220 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 728FD 581 OLD CROSSBEAM REPAIR IN AFT CARGO FLOOR COMPARTMENT, FRAME 63 LT IS NOT CONFORM TO SRM 53-10-15/FIG 207 (REPAIR PROFIL THICKNESS). REPAIR RENEWED IAW SRM 53-10-15/FIG 207. 2 L 7 2 4F RT A35EU 2007092000124 20070920 00124 EU 2007 9 20 07FDEA03550 1 20070911 A 5315 A53974219220 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 OLD CROSSBEAM REPAIR IN AFT CARGO FLOOR COMPARTMENT, FRAME 63 LT IS NOT CONFORM TO SRM 53-10-15/FIG 207 (REPAIR PROFIL THICKNESS). REPAIR RENEWED IAW SRM 53-10-15/FIG 207. 2 L 7 2 4F RT A35EU 2007092000127 20070920 00127 NM 2007 9 20 2007UALA03595 1 20070905 A 2560 GIRT BAR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR OUT OF POSITION A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 937UA 26668 GIRT BAR AT 1L HANGING OUT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092000128 20070920 00128 NM 2007 9 20 2007UALA03596 1 20070906 A 3510 OXYGEN MASK BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE COCKPIT LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 673UA 29241 CAPTS O2 MASK BOTTOM HARNESS TUBE IS LEAKING. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092000130 20070920 00130 NM 2007 9 20 QXEA200701425 1 20070916 A 3233 ROD END BOMBDR DHC8 DHC8402 1390042 NM MLG ACTUATOR OUT OF ADJUST A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 401QX 4031 BLI FLIGHT NR 2488: AFTER GEAR UP SELECTION, LT MLG YELLOW AND RED GEAR INDICATION CAUTION AND WARNING LIGHTS AND YELLOW GEAR HANDLE REMAINED ILLUMINATED. AFTER 3 MINUTES IN MODERATE TURBULENCE, ALL GEAR LIGHTS EXTINGUISHED. GEAR EXTENDED NORMALLY ON LANDING WITH GEAR EXTENSION WITH GOOD GEAR DOWN AND LOCKED INDICATION. MAINTENANCE REMOVED NR 4 MLG RETRAC T ACTUATOR IAW Q400 AMM 32-31-11-000-801. ADJUSTED RETRACT ACTUATOR ROD END IAW GOODRICH LANDING GEAR CMM REF 32-31-06, PG 403, PARA C. ADJUSTED ROD END DIMENSION USING QX TOOL, P/N QXT 632439-101 S/N QXT1893. REINSTALLED THE SAME RETRAC T ACTUATOR IAW AMM TASK 32-31-06-400-801. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007092000132 20070920 00132 NM 2007 9 20 07FDEA03552 1 20070911 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 588FE 48490 LEFT NOSE LANDING GEAR TRUNNION FITTING SUSPECT WITH CRACK. 09-28-07 REPAIR CARRIED OUT AT LT HAND NOSE LANDING GEAR TRUNNION FITTING AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007092000135 20070920 00135 EU 2007 9 20 07FDEA03555 1 20070911 A 5313 A53973080202 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 FOUND HEAVY CORRODED STRINGER 46 RT BETWEEN FRAME 63-63A, TORSION BOX. STRINGER REPAIR PERFORMED IAW SRM 53-10-14/FIG 20 1 AND TORSION BOX-SPLICE REPAIR IAW SRM 53-17-18/FIG 206/SH 2. 2 L 7 2 4F RT A35EU 2007092000136 20070920 00136 EU 2007 9 20 07FDEA03556 1 20070911 A 5330 A53778018 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 OLD DOUBLER REPAIR AT FRAME 36, STRG 32-33 LT. DISAGREEMENT IN SRM REFERENCE IN OUTER RIVET ROW. REPAIR PERFORMED IAW SRM 53-10-12/FIG 207. REPAIR SOLUTION WITH SRM 53-10-12/FIG 225. 2 L 7 2 4F RT A35EU 2007092000140 20070920 00140 EU 2007 9 20 07FDEA03560 1 20070911 A 5311 A53776029 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 CHAFING MARKS AT FRAME 34 BETWEEN STRG 14-15 LHS, OUT OF LIMIT. REPAIR PERFORMED IAW SRM 53-10-13/FIG 202. FRAME COUPL ING INSTALLED. 2 L 7 2 4F RT A35EU 2007092000141 20070920 00141 EU 2007 9 20 07FDEA03562 1 20070911 A 5712 A57141283 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 600 - RH CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 FOUND CORROSION IN MLG RIB 5 FWD LUG ON BOTH WINGS. REPAIR PERFORMED BY SPOT FACING AND OVERSIZING WITH NEW BUSHES IAW REPAIR DRW R572-40221 ISSUE E, APPROVED BY EA 6-5751-95903 AND RAS/BAE/1002238/2006 ISSUE A. 2 L 7 2 4F RT A35EU 2007092000142 20070920 00142 EU 2007 9 20 07FDEA03563 1 20070911 A 5313 A53870153201 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 200 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 FOUND TWO OLD PILOTHOLES WITHOUT RIVETS AT FRAME 44, STRG 1 RT. PILOTHOLES CLOSED WITH RIVETS 2 4MM DIA IAW EA 6-5315-9 5894 AND RAS/DATLS/0002966/2006 ISSUE C. 2 L 7 2 4F RT A35EU 2007092000144 20070920 00144 NM 2007 9 20 DL757071165 1 20070902 A 2120 CONTROL PANEL BOEING 757 757232 1384965 NM COCKPIT ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 631DL 23612 RECEIVED EICAS MSG RT RECIRC FAN WITH ELEC ODOR. ODOR DISSIPATED WITH FAN OFF FWD RT RECIRC FAN TO MCO AND PLAC PER MEL 21-25-01A. FOUND CABIN ALTITUDE CONTROL PANEL LOADING DOWN BACKGROUND LIGHTING FOR ABOVE MENTIONED SYSTEMS REPLACED CA BIN ALTITUDE CONTROL PER AMM 21-31-01-404-007. REMOVED MCO AND PLACARD C/ ON NR CARD 71. 2 L 7 2 4F RT A2NM 2007092000145 20070920 00145 NE 2007 9 20 DLM90071167 2 20070903 A 7200 V2528D5 ENGINE DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 1 INTERMITTENT A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 906DA 10267 6425 53386 020027 LT ENG STRAINER CLOG ILLUMINATED DURING INITIAL CLIMB COMPLETED WITH CK LIST AND RETURNED TO LAND. ENG WAS NOT SHUT DOW N AND LANDING WAS NOT OVERWEIGHT. INSP/CLEANED SCAVENGE OIL FILTER PER MEL REF. NO DEPOSITS NOTED. FWD TO MCO AND PL AC PER MEL 79-36-01. ITEM TO CKD ONCE EACH FLT DAY. RAN ENG NO LEAKS. FOUND DEFECTIVE WIRING OB OF PYLON CONNECTOR. REPAIRED WIRING RAN ENGINE. ENG INDICATIONS NORMAL. MCO AND PLAC RMVD. REMOVED C FILTER LK CK OK. 2 L 7 2 4F 4 F RT A6WE E40NE 2007092000147 20070920 00147 NM 2007 9 20 DL76S071177 1 20070905 A 2121 211002542 FAN BOEING 767 767332 1382001 NM CABIN WORN A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 139DL 25984 ELECTRICAL BURNING ODOR IN COCKPIT. ON DESCENT INTO LBB, GOT FWD EQ EXH FAN STATUS MSG. INSPECTED FAN AND E AND E AREA . FOUND NO EVIDENCE OF FUMES OR BURNING SMELL. FWD EQ EXH FAN TO MCO PER MEL 21-58-04B. REPLACED FWD EQUIP SUPPLY FAN 1 PER AMM. OPS NML. NO MSGS. EI OPS NML. FAN REMOVED SMELLED BURNED AND INTERNAL BEARINGS LOOSE/WORN OUT. OK FOR S VC. 2 L 7 2 4F RT A1NM 2007092000150 20070920 00150 NM 2007 9 20 2007UALA03598 1 20070905 A 2611 SMOKE DETECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE L1 DOOR DIRTY A UALA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 29 826UA 989 ECAM MESSAGE SMOKE DETECTOR MESSAGE DOOR 1L FWD. SMOKE DETECTOR DIRTY. REMOVED, CLEANED AND REINSTALLED SMOKE DETE CTOR IN FWD LAV A. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092000151 20070920 00151 NM 2007 9 20 2007UALA03599 1 20070906 A 4920 SEAL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE APU LEAKING A UALA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 826UA 989 APU SMOKING UPON ARRIVAL INTO SFO AT GATE WITH OIL COMING OUT OF TAILPIPE. REPLACED APU. MANUFACTURER CHANGED EPOXY IN '06. UAL'S 1ST INCIDENT OCCURRED 12/23/06 AND HAS HAD 6 ADDITIONAL INCIDENTS SINCE. 4026 WAS THE 1ST SDR AND THE LAST OC CURRANCE. MANUFACTURER HAS SINCE ADDRESSED THE PROBLEM FOR ANY ESV'S AS OF 20070607. THE MTBF IS 2005 HRS, MCBF 2306. EP HAS REQUESTED A RESEARCH AS TO WHICH ENGINES HAVE THE OLD REPAIR METHOD APPLIED, CURRENTLY UNKNOWN. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092000152 20070920 00152 EU 2007 9 20 2007UALA03600 1 20070906 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 480UA 1555 AFT PIT STR 42L HAS CORROSION BETWEEN FRAMES 63 & 64. MAJOR REPAIR STRINGER DAMAGE REMOVED AND STRINGER WAS REPAIRED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092000154 20070920 00154 NM 2007 9 20 2007UALA03602 1 20070906 A 2711 AILERON BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU WING BINDING A UALA O OTHER F FLT CONT AFFECTED CL CLIMB 1 WP 29 308UA 23669 AILERONS SLIGHT BINDING WHEN COMING OUT OF A RIGHT TURN. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092000156 20070920 00156 NM 2007 9 20 2007UALA03604 1 20070907 A 7100 EEC BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE MALFUNCTIONED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 553UA 25277 726697 A-T DISCONNECTED FL380 IN CRUISE. CURRENT FAULT SHOWS AUTO DISC EEC L- PRIMARY. REPLACED LEFT EEC. NO FURTHER MAINT ENANCE ACTION NEEDED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092000160 20070920 00160 NE 2007 9 20 2007UALA03608 2 20070906 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 2 SURGES A UALA O OTHER O OTHER CR CRUISE 1 WP 29 670UA 29240 727337 ENG 2 SILENT SURGE DETECTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092000161 20070920 00161 NM 2007 9 20 2007UALA03609 1 20070906 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 513UA 24810 EMERGENCY ESCAPE PATH LIGHTS AT ROWS 23-30 INOP. REPLACED ONE LAMP AND SECURED SAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092000163 20070920 00163 NE 2007 9 20 DL75E071181 2 20070907 A 7200 ENGINE BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE NR 2 MAKING METAL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 702TW 22454 28162 727205 PLEASE REPLACE THE NR 2 ENG BECAUSE OF PREVIOUS METAL FINDING FROM THE NUMBER 5 BEARING AREA. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092000164 20070920 00164 NM 2007 9 20 2007UALA03611 1 20070906 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 502UA 24623 EMERGENCY LIGHTS INOP AT SEAT 5B. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092000166 20070920 00166 2007 9 20 DL757071182 4 20070908 A 3452 6224540001 TRANSCEIVER BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE DME SYSTEM ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 644DL 23998 727205 DURING DESCENT ACRID ODOR DETECTED IN COCKPIT AND REPORTED BY FLT ATTENDANTS AS WELL IN CABIN. PRIOR TO ODOR THE CABIN AIRFLOW CHANGED TO A SIGNIFICANTLY LESS INTENSITY. RT RECIRC FAN WAS TURNED OFF. LT DME C/B ALSO WAS NOTED POPPED. TH E ODOR DISSIPATED RAPIDLY. FOUND LT DME WITH STRONG BURNT ODOR. REPLACED LT DME TRANSCEIVER BORROWED FROM AMERICAN AIR LINES S/N 113 MFG P/N 622-4540-001. OPS CK NORMAL RESET RT RECIRC FAN AND OPERATED BOTH PACKS ALL CK NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092000167 20070920 00167 NM 2007 9 20 2007UALA03613 1 20070906 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 779UA 26941 EMERGENCY LIGHTS INOP AT SEATS 21C & 9F FWD LT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007092000168 20070920 00168 NM 2007 9 20 2007UALA03614 1 20070831 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 641UA 25091 LEFT SIDE EXTERIOR EMERGENCY LIGHTS (L388): (L389): (L313 ): (L395): AND (L642) INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092000169 20070920 00169 NM 2007 9 20 2007UALA03615 1 20070907 A 5230 STRUCTURE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FWD CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 175UA 24382 FWD CARGO PIT DOOR AFT LOWER CORNER APPEARS TO BE DAMAGED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092000170 20070920 00170 NM 2007 9 20 DL76G071183 1 20070908 A 2761 O-RING BOEING 767 767332 1382001 NM PWA 2037 PW2037 NE ACTUATOR LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 1603 29695 727205 ATB TO JFK FOR CTR HYD QTY FLUID LOSS NUMBER 4 SPOILER ACTUATOR FILTER HOUSING LEAKING. FOUND O-RING ON FILTER HOUSING DAMAGED. REPLACED SAME. OPS LEAK CHK OK. A/C OK FOR SERV. 2 L 7 2 4F 4 F RT A1NM E17NE 2007092000171 20070920 00171 NM 2007 9 20 2007UALA03617 1 20070907 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT LOW A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 850UA 1653 GATE CAPT FOUND 02 LOW. SERVICED THE O2 SYSTEM TO PROPER LEVELS. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092000172 20070920 00172 NM 2007 9 20 DL764071184 1 20070908 A 3320 BULB BOEING 767 767432ER 1385134 NM CABIN LIGHTS BURNED OUT A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 827MH 29698 LIGHT/BRIEF ODOR OF SMOKE NOTICED AROUND SEATS 23A/B. THIS OCCURED AT 3.5 AND 7 HRS INTO FLIGHT AT CRUISE. NO VISIBLE S MOKE SEEN OR DETECTED. F/A'S REPORT SLIGHT ODOR OF BURNING MATCH, CAR BACKFIRE, RUBBER. FOUND SEAT 21A READING LIGHT B URNED OUT. REPLACED BULB. INSPECTED AVU, EMPOWER, SEU FROM SEATS 21-25. NO COMPONENT OVERHEAT/MALF. NO BURNING/ARCHI NG OF WIRES OR CONNECTIONS. PACK AND GASPERS HAVE NO ODOR. 2 L 7 2 4F RT A1NM 2007092000175 20070920 00175 NM 2007 9 20 2007UALA03619 1 20070907 A 3510 OXYGEN MASK BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT LEAKING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 211UA 30217 OXYGEN MASK PROBLEM CREW COMMENTS: CAP OXYGEN MASK LEAKS. 10-11-07 REPLACED CAPTAIN'S OXYGEN MASK. LEAK CHECKS GOO D. OK FOR SERVICE. SUSPECT PRESSURIZATION CYCLES & CARELESS STOWAGE CAUSED THE LEAKAGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007092000179 20070920 00179 NM 2007 9 20 2007UALA03623 1 20070907 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 326UA 23958 EXTERNAL FUSELAGE SKIN CRACKED AT AFT END OF AVIONIC EXHAUST OUTLET. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLE D LARGE EXTERNAL SKIN DOUBLER AROUND E&E EXHAUST OUTLET & PREVENTIVE MODIFICATION DOUBLERS TO AFT RADIO ALTIMETER CUTOUT S. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092000183 20070920 00183 NM 2007 9 20 2007UALA03627 1 20070908 A 3350 3071BPEGPL LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 812UA 850 EEL LIGHT 1 EA BULB OUT AT SEAT 13C, 12C, 10C FWD COAT CLOSET. REPLACED LAMPS, OPS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007102300256 20071023 00256 EU 2007 10 23 2007UALA03628 1 20070908 A 2700 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 FAULTED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 466UA 1343 ELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. F-CTL CREW COMMENTS: ATTEMPTED 2 RESETS, NO JOY. 10-11-07 FOUND ELAC NR 1 FAULTED. REPLACED ELAC NR 1. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092000184 20070920 00184 EU 2007 9 20 2007UALA03629 1 20070907 A 3510 OXYGEN BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 485UA 1617 COCKPIT OXYGEN BOTTLE LOW. 10-11-07 SERVICED OXYGEN SYSTEM, NO LEAKS NOTED, NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092000185 20070920 00185 NM 2007 9 20 2007UALA03630 1 20070909 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 203UA 24718 EEL LIGHTS ARE INOP FROM SEAT ROW 13 TO 20. REPLACED LIGHT ASSY FROM ROW 13 TO 20. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092000186 20070920 00186 NM 2007 9 20 2007UALA03631 1 20070910 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 116UA 26908 EEL STRIPS ON SEATS 6A & 2J ARE FALLING OFF. 10-11-07 REINSTALLED EEL STRIPS IN BOTH SEAT POSITIONS AND CHKD OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092000187 20070920 00187 NM 2007 9 20 2007UALA03632 1 20070908 A 3350 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY LIGHT INOP, RIGHT OVERWING, BOTTOM 2. 10-11-07 REPLACED MODULE FUSE. AIRCRAFT OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092000188 20070920 00188 NM 2007 9 20 2007UALA03633 1 20070908 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY LIGHT AT SEAT 4A AFT INOP. 10-11-07 REPLACED EEL LIGHT ASSY. SYSTEM CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092000190 20070920 00190 NM 2007 9 20 2007UALA03635 1 20070907 A 5210 ARM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR MISINSTALLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 520UA 24890 DOOR 4R EMERGENCY POWER ASSIST BOTTLE HAS TRIGGER ARM IMPROPERLY INSTALLED. 10-11-07 THIS ASSIST BOTTLE PREVIOUSLY D ISCHARGED. INSTALLED NEW EMERGENCY POWER RESERVOIR FOR DOOR 4L FOUND CABLE INSTALLED PROPERLY; THE BOTTLE HAVING BEEN DISCHARGED HAD THE APPEARANCE OF INCORRECT INSTALLATION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092000192 20070920 00192 NM 2007 9 20 QXEA200701385 1 20070905 A 2711 TAB DHAV DHC8 DHC8202 2809007 NM OUT OF ADJUST A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 358PH 506 SEA - DURING CLIMB AND CONTINUING DURING CRUISE, THE AMOUNT OF FORCE NEEDED TO TURN THE AIRCRAFT TO THE LEFT WAS MORE TH AN USUAL. THE AMOUNT OF FORCE REQUIRED INCREASED WITH INCREASING AIRSPEED TO THE POINT OF BEING INCREDIBLY DIFFICULT AT HIGH SPEEDS. ON THE GROUND, BEFORE TAKEOFF, THE CONTROL CHECK WAS NORMAL. ALL PFCS INDICATORS APPEARED NORMAL AND THE AIRCRAFT WAS CONTROLLABLE AT ALL TIMES. REMOVED PANEL 121AL AND 121BL TO FOM. INSPECTED AILERON CABLE RUNS UNDER COCKP IT FLOOR FOR ANY OBVIOUS DEFECTS. NONE FOUND. REINSTALLED PANES AS REQUIRED. REMOVED PANELS 262DT AND 262LT TO FOM. INSPECTED AILERON SPLITTER QUADRANT AND CABLE RUND FOR ANY OBVIOUS DEFECTS. NONE FOUND. REINSTALLED PANELS AS REQUIRED 2 H 7 2 4T RT A13NM 2007092000193 20070920 00193 NM 2007 9 20 QXEA200701403 1 20070908 A 3040 NP15790111 WINDSHIELD DHAV DHC8 DHC8202 2809007 NM COCKPIT ODOR A QXEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 352PH 7419 494 PDX - DURING CRUISE FLIGHT CREW NOTICED ACRID/PLASTIC BURNING ODOR AND SMOKE IN COCKPIT. NO SMOKE OR ODOR IN CABIN. DE CLARED EMERGENCY AND RETURNED TO FIELD. SMOKE/HAZE NOTICED IN VICINITY OF HUD COMBINER. ELECTED NOT TO TURN-OFF ANY GE NERATOR SWITCHES DUE TO PROXIMITY OF AIRPORT. REPLACED PILOTS WINDSHIELD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED T O SERVICE. 2 H 7 2 4T RT A13NM 2007092000195 20070920 00195 NM 2007 9 20 QXEA200701411 1 20070907 A 2910 7G773 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007 NM HYD SYSTEM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 358PH 4178 506 SEA - SHORTLY AFTER TAKEOFF 3 MASTER CAUTIONS APPEARED, RUD PRESS, RUD FULL PRESS, NR 2 RUD HYD CREW RUN APPROPRIATE CHE CKLISTS. BLED RUDDER HYDRAULIC SYSTEM AND REPLACED RUD HYD PRESSURE SWITCHES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 H 7 2 4T RT A13NM 2007092000200 20070920 00200 NM 2007 9 20 QXEA200701404 1 20070910 A 2711 TRIM TAB DHAV DHC8 DHC8202 2809007 NM AILERON OUT OF ADJUST A QXEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 09 358PH 506 SEA - DURING INITIAL CLIMB FROM 34R WITH A LEFT QUARTERING HEADWIND AILERON CONTROL WAS STIFF WHEN APPLYING LEFT ROLL. W ITH 2 SHORT TAPS OF LWS AILERON TRIM DIFFICULTIES SEEMED TO DISAPPEAR AT 2K FT A RIGHT TURN WAS INITIATED AND THIS TIME THERE WAS DIFFICULTY WITH RIGHT ROLL. AGAIN TWO SHORT TAPS OF RWD AILERON TRIM RETURNED CONTROL FEEL TO NORMAL UNTIL LE FT AILERON WAS REQUIRED FOR ALL REQUIRED FOR ROLLOUT THIS CONTINUED TO ALL REQUIRED TURNS. MAINTENANCE RIGGED AILERON S PRING/TRIM TAB IAW TASK 27-13-11-830-801. NO PARTS REPLACED. OPERATIONAL CHECK FLIGHT GOOD. AIRCRAFT RETURNED TO SERV ICE. 2 H 7 2 4T RT A13NM 2007092000201 20070920 00201 NM 2007 9 20 2007UALA03639 1 20070909 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 563UA 26665 EXTERIOR EMERGENCY LIGHTS INOP AT DOORS 2R & 4L. 10-11-07 FOUND FUSED LAMPS. REPLACED LAMPS 2 L 7 2 4F 4 F RT A2NM E17NE 2007092000202 20070920 00202 NM 2007 9 20 F3LA200700236 1 20070912 A 5321 D5367180500400 FLOORBOARD AIRBUS A319 A319111 3930336 NM CABIN CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 921FR 5402 2010 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON SEVERAL AREAS OF FLOORBOARD PANEL 161FF. REPLACED FLOORBOARD PANEL 1 61FF IAW AMM 53-42-12, PB401. 2 L 7 2 4F RT A28NM 2007092000203 20070920 00203 NM 2007 9 20 DHL2007746526 1 20070825 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 1010 S27L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 SURFACE CORROSION ON EXISTING STRINGER SPLICE BODY STA 1010 FORWARD AND AFT OF STR 27L (MARKED). REMOVED SPLICE AT BODY STATION 1010 FORWARD AND AFT STR 27L IAW B727 SRM 51-30-2. FABRICATED SPLICE MATERIAL USED BAC1498-131 7075-T6 PO NR 9 003866 DIMENSION 12 1/4" IAW B727 SRM 53-10-2 FIG 9, 51-10-3 AND 51-30-5. TREATED AND PRIMED IAW B737 51-10-2. INSTALL ED SPLICE AT BODY STATION 1010 FORWARD AND AFT STR 27L IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007092000204 20070920 00204 NM 2007 9 20 2007UALA03640 1 20070909 A 2150 A/C PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT & CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 590UA 28708 FAINT BURNT OIL ODOR BEGAN ABOUT 1.5 HRS INTO FLIGHT. NOTICED ON FLIGHT DECK & IN CABIN. 10-11-07 CREW ELECTED TO T URN OFF LEFT PACK AND AIR QUALITY THEN IMPROVED SUBSTANTIALLY. COMPLETED A PACK BURN. THEN RAN ENG NR 1 FOR 2 HOURS, WH ICH REMOVED ODOR, REPLACED TRIM AIR MODULATING VALVE AND CABIN FILTERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092000206 20070920 00206 2007 9 20 2007UALA03641 4 20070909 A 2565 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR SLIDE CONTAMINATED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 584UA 26706 LIGHT FOR SLIDE AT DOOR 1R INOPERATIVE. 10-11-07 FOUND DEBRIS IN GIRT SLIDER AREA ON FLOOR CLEANED DEBRIS, LUBED SLI DE TRACKS AND CYCLED DOOR SEVERAL TIMES AND FOUND NORMAL OPERATIONS OF SLIDE LIGHT AND NORMAL ENGAGEMENT OF GIRT BAR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092000207 20070920 00207 NM 2007 9 20 DHL2007746531 1 20070825 A 5753 SUPPORT BOEING 727 727224 1384076 NM TE FLAP TRACK CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 NR 6 FLAP TRACK AFT ATTACH SUPPORT BLOCK IS CORRODED, WBL 203.8. REMOVED NR 6 FLAP TRACK AFT ATTACH SUPPORT BLOCK IAW B 727 SRM 51-30-2. FABRICATED NR 6 FLAP TRACK AFT ATTACH FILLER IAW B727 DRAWING NR 66-14734 MATERIAL USED 7075-T6 0.700 BY 7.5 BY 1.75" PO#9001938 (DIMENSION) OK TO TREAT AND PRIME. TREATED AND PRIMED IAW B727 SRM 51-10-2. OK TO INSTALL, INSTALLED SUPPORT BLOCK AT NR 6 FLAP TRACK WBL 203.0 IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007092000208 20070920 00208 NM 2007 9 20 2007UALA03642 1 20070908 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 778UA 26940 EEL LIGHT INOPERATIVE 42D. 10-11-07 RELAMPED AS PER MM33-51-05. OP CHECKED PER SAME, SYS OPS NORM. RETURNED AC BAC K TO NORMAL, OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007092000209 20070920 00209 NM 2007 9 20 2007UALA03643 1 20070909 A 3530 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY EXIT EEL LIGHT INOPERATIVE AT SEATS 5A AFT & 44 ABC. 10-11-07 REPLACED LIGHT ASSY IN BOTH SEAT POSITIONS. OPS. CHECKS. NORMAL. OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092000210 20070920 00210 NM 2007 9 20 07FDEA03586 1 20070911 A 3243 83216 VALVE BOEING 727 727233 138408A NM BRAKES LEAKING A FDEA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SO 25 270FE 22035 CALLED BACK BY RAMP. MX NOTICED HYD LEAK/PUDDLE ON GND AFTER WE TOOK OFF. REPLACED NR 3 BRAKE SHUTTLE VALVE PER B727 A MM 32-41-051-4. LK CKS GOOD. 2 L 7 3 4F RT A3WE 2007092000211 20070920 00211 NM 2007 9 20 2007UALA03644 1 20070909 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY EEL LIGHT INOP. JUST AFT OF DOOR 1R LOWER WALL. 10-11-07 REPLACED POWER FEEDER. EEL LIGHT OP CHECKS NORMA LLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092000212 20070920 00212 WP 2007 9 20 07FDEA03587 1 20070911 A 5330 ACA71601 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 FUSELAGE SKIN AND FRAME AT STA 642 HAVE OVERSIZED FASTENER HOLE. REPAIRED IAW EA 8-53-109196-FUSELAGE-EXISTING BUSHINGS FOUND AT STA 641.5 MCD, LOWER SILL-REPAIR. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2007092000213 20070920 00213 NM 2007 9 20 F3LA200700237 1 20070912 A 5321 D5367180500500 FLOORBOARD AIRBUS A319 A319111 3930336 NM CABIN CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 921FR 5402 2010 DURING C-3 CHECK, INSPECTION REPORTED SEVERAL AREAS OF CORROSION ON FLOORBOARD PANEL 163FF. REPLACED FLOORBOARD PANEL I AW AMM 53-42-12, PB401. 2 L 7 2 4F RT A28NM 2007092000214 20070920 00214 NM 2007 9 20 2007UALA03645 1 20070909 A 3350 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY EXIT CEILING LIGHTS INOP, FROM DOOR 3R THRU 4R. 10-11-07 REPLACED ELECTRICAL POWER SUPPLY UNIT, AND BATTER Y, CHECKED OK 2 L 7 4 4F 4 F RT A20WE E24NE 2007092000216 20070920 00216 NM 2007 9 20 2007UALA03646 1 20070909 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY EXIT LIGHT INOP, AT DOOR 4R AFT SILL LIGHT. 10-11-07 REPLACED LAMP. OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092000218 20070920 00218 NM 2007 9 20 DHL2007746525 1 20070830 A 5343 TRUNNION BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 LEFT NOSE LANDING GEAR TRUNNION BORE HAS CORROSION. REMOVED CORROSION AND REPAIRED NOSE LANDING GEAR TRUNNION SUPPORT F ITTING IAW B727 SRM 51-10-6 AND 53-40-01. NOSE LANDING GEAR, OPS/CHECK GOOD IAW B727 MM 32-33-00. 2 L 7 3 4F A3WE 2007092000219 20070920 00219 NM 2007 9 20 DL76P071178 1 20070905 A 5410 311T3065127 DOOR BOEING 767 767332 1382001 NM NR 2 PYLON MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 140LL 25988 FOUND BY MTC ON PDC WALK AROUND FOUND NUMBER 2 ENGINE PYLON INBOARD NACELLE STRUT ACCESS DOOR MISSING FWD TO CDL PER 54- 53-03 NEEDS DOOR MFG 311T3065-127. REPLACED ACCESS DOOR, MCO/PLACARD REMOVED. 2 L 7 2 4F RT A1NM 2007092000221 20070920 00221 2007 9 20 DLM88071192 4 20070911 A 3414 4057800901 INDICATOR DOUG MD88 MD88 3023688 NM COCKPIT UNSERVICEABLE A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 948DL 49879 ABORTED T/O AGAIN REPEAT CAPT AIRSPEED INDICATOR FLAG IN VIEW. F/O INDICATOR READ 40 KTS. REPLACED CAPT MACH/AIRSPEED INDICATOR PER M/M. SYS CKS GOOD WITH AIR DATA TEST SET. POWER FOR NR 1 ADC C/B CKS GOOD. INFO ON FIRST RTO, FOUND NR 1 ADC FAILING SELF TEST. REPLACED SAME PER M/M. REPLACED MACH/ASPD IND PER M/M SYS CK GOOD WITH AIR DATA TESTER FOR NR 1 CADC. C/B CKS GOOD. 2 L 7 2 4F RT A6WE 2007091900043 20070919 00043 NM 2007 9 19 07FDEA03721 1 20070913 A 5710 656233516 BEAM BOEING 727 727233 138408A NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 RT MLG BEAM LOWER SURFACE AND FASTENER HOLES EXPOSED BY REMOVAL OF LOWER T/E PANELS NEED TO BE CLEANED AND INSPECTED. F OUND CORROSION INSIDE HOLES REPAIRED DAMAGE HOLE. REF FED EX EA NR 7-5720-113948 CLEANED HOLES/ REWORKED HOLES REF EA. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007091900047 20070919 00047 EU 2007 9 19 07FDEA03717 1 20070825 A 5330 A53778160200 SKIN AIRBUS 310 A310222 3930315 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 PREVIOUS REPAIR FOUND LOCATED ON RT FUSELAGE STA 1764/1817, STRG 34-36 RT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR D ETERMINATION OR IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAIR WAS ACCOMPLISHED PER SRM 53-10-12 FIG 225 SHEET 1. 2 L 7 2 4F RT A35EU 2007091900060 20070919 00060 EU 2007 9 19 07FDEA03703 1 20070913 A 5320 A53773645200 FLANGE AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION FOUND ON UPPER FLANGE C25. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10 2 L 7 2 4F RT A35EU 2007091900064 20070919 00064 EU 2007 9 19 07FDEA03699 1 20070913 A 5512 A55177803200 SKIN AIRBUS 310 A310324 3930206 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 CORROSION PITS ON TOP REAR SKIN OF THS LT. REMAINING THICKNESS IS WITHIN LIMITS GIVEN IN SRM BUT MAXIMUM AFFECTED SURFA CE AREAS ARE >400 MMXMM AND THEREFORE ARE OUT OF LIMIT AS PER SRM 55-10-00/CONFIG 2/TB 101, PIT AREAS BETWEEN 200 AND 15 00 MMXMM) REWORK AREAS DOCUMENTED AND APPROVED PER EA 6-5510-92156 AND RAS/CASA/4264/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091900078 20070919 00078 EU 2007 9 19 07FDEA03683 1 20070913 A 5754 A57243204 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 CHAFING MARKS ON RT WING LEADING EDGE D-NOSE SKIN BETWEEN TRACK 5 AND 6 AND AREA AROUND JACK 3, OUT OF SRM LIMITS. PART IAL SKIN REPLACMENT BETWEEN TRACK 5 AND 6 AND AROUND JACK 3 IAW SRM 57-41-12/FIG 203, 204 SRM REQUIRES MATERIAL DTD5070 TO ACCOMPLISH REPAIR, EA 6-57-41-92182 AND RAS/BAE/1001398/2005 ISSUE A AUTHORIZES ALTERNATE MATERIAL AL-P2014A. 2 L 7 2 4F RT A35EU 2007091900084 20070919 00084 EU 2007 9 19 07FDEA03624 1 20070912 A 5320 A53974321000 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 CORROSION ON FITTING AT FRAME 63, STR 41-45 LT, OUT OF LIMIT. REPLACEMENT OF FITTING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900086 20070919 00086 EU 2007 9 19 07FDEA03622 1 20070912 A 5313 A53610797222 LONGERON AIRBUS 310 A310324 3930206 EU ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 812FD 467 FOUND TWO SPLICE REPAIRS ON EXTRUSION BETWEEN FRAME 15A-17, Y1959 LT, MATERIAL NOT CONFORM TO SRM 53-12-15/FIG 207. SPL ICE REPAIRS ON EXTRUSION RENEWED IAW SRM 53-12-15/FIG 207. 2 L 7 2 4F RT A35EU 2007091900098 20070919 00098 EU 2007 9 19 07FDEA03607 1 20070912 A 5522 A55276700207 SKIN AIRBUS 310 A310324 3930206 EU ZONE 300 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 DENT IN RT ELEVATOR BOTTOM SKIN TRAILING EDGE. REPAIR PERFORMED BY FILLING AND LAMINATING IAW SRM 55-21-11/FIG 204. 2 L 7 2 4F RT A35EU 2007091900114 20070919 00114 EU 2007 9 19 07FDEA03583 1 20070911 A 5753 SKIN AIRBUS 310 A310203 3930313 EU ZONE 600 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 812FD 467 OLD DOUBLER REPAIR ON T/E OF RT INBOARD FLAP, RIB 8-10, NOT CONFORM TO SRM 57-12-52, ONE RIVET ROW IS MISSING. REPAIR P ERFORMED AS PER SRM 57-53-12/FIG 208, APPROVED BY EA 6-5752-92201 AND RAS/DABRE/7005882/2005 ISSUE C. 2 L 7 2 4F RT A35EU 2007091900117 20070919 00117 EU 2007 9 19 07FDEA03574 1 20070911 A 5730 A57246242203 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 FOUND SEVERAL CHAFING MARKS ON LEADING EDGE D-NOSE SKIN RT BETWEEN SLAT TRACK 2 AND JACK 2. REPLACEMENT OF D-NOSE SKIN IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007091900119 20070919 00119 EU 2007 9 19 07FDEA03572 1 20070911 A 5330 A53610567 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CORROSION AT INTERNAL SKIN C17-18, P49 RH- P51 LT. REPAIR PERFORMED BY BLEND OUT THE CORROSION IAW SRM 53-12-12 F IG 104 AND RAS 031331/01/2004 ISS A, APPROVED BY EA 6-5330-79577. 2 L 7 2 4F RT A35EU 2007091900120 20070919 00120 EU 2007 9 19 07FDEA03569 1 20070911 A 5330 A53974207200 SKIN PANEL AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION FOUND ON INNER SKIN C 64-71, P56 LT-56 RT DOUBLER REPAIR PERFORMED AT C 66, P56 LT-56RT IAW RAS/DAHAM/4018310/ 2004 ISS A AND AT C 69, P56LT-56RT IAW RAS/DAHAM/4018309/2004 ISS A AND SMOOTH BLEND OUT OF CORROSION BETWEEN C 64-71, P 56 LT-56RT IAW RAS/DAHAM/4018287/2004 ISS D. APPROVED BY EA 6-5330-79574. 2 L 7 2 4F RT A35EU 2007091900129 20070919 00129 EU 2007 9 19 07FDEA03546 1 20070911 A 5313 A53970701216 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION FOUND AT C55/58-59, STRINGER P 50 LT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007091900141 20070919 00141 EU 2007 9 19 MALA070114 1 20070824 A 5330 PANEL SAAB SF340 340B 7860101 EU FUSELAGE DEBONDED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 411XJ 340B411 DURING N4K CHECK IN CWA FOUND, 4 DISBONDED DENTS ON CENTER BELLY PANEL. REPAIRED IAW EO NR S51031 AND SRM 51-70-50. 2 L 7 2 4T RT A52EU 2007091900144 20070919 00144 NM 2007 9 19 AALA20071612 1 20070824 A 2930 5271T0054 INDICATOR BOEING 757 757223 1384957 NM LT HYD SYS BLOWN A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 669AA 25334 MIA INFLIGHT T596/24AUG - LEFT HYDRAULIC LOSS IN FLIGHT. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. FOUND LEFT HYDRA ULIC INDICATOR ON FILTER HOUSING BLOWN. REPLACED LEFT HYDRAULIC FILTER INDICATOR. SYSTEM GROUND CHECKED NORMAL OPERATI ON. 2 L 7 2 4F RT A2NM 2007091900146 20070919 00146 EU 2007 9 19 AALA20071614 1 20070824 A 2760 73020 SERVO VALVE AIRBUS 300 A300B4605R 3930308 EU SPOILER INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 80057 465 MIA INFLIGHT T1075/24AUG MCO - SJU EXPERIENCED VIBRATIONS AND FOUND THE NUMBER FIVE SPOILER WAS FLOATING. TURNED OFF Y ELLOW SERVO CONTROLLER AND VIBRATIONS STOPPED BUT NUMBER THREE SPOILLER POPPED. DECLARED AN EMERGENCY AND DIVERTED IN M IA. LANDED WITHOUT INCIDENT. REPLACED LEFT NUMBER FIVE SPOILER SERVO VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007091900148 20070919 00148 NM 2007 9 19 AALA20071595 1 20070821 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 775AN 29584 JFK - EMERGENCY LIGHT AT SEAT 37C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 37C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091900151 20070919 00151 NM 2007 9 19 AALA20071611 1 20070823 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 JFK - EMERGENCY LIGHT AT SEAT 20C INOPERATIVE. REPAIRED LIGHT FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091900181 20070919 00181 NM 2007 9 19 AALA20071583 1 20070818 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 762AN 31479 DFW - EMERGENCY LIGHT AT SEAT ROW 40G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 40G. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007091900183 20070919 00183 WP 2007 9 19 AALA20071585 1 20070819 A 3397 TERMINAL DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 492AA 49730 SFO - EMERGENCY LIGHT AT RIGHT OVERWING EXIT INOPERATIVE. CLEANED BATTERY PACK TERMINAL AT 21D FOR EMERGENCY LIGHT RIGH T OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007091900187 20070919 00187 NM 2007 9 19 AALA20071581 1 20070818 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 916AN 29517 DFW - EMERGENCY LIGHT AT SEAT ROW 13F MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 13F. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007091900189 20070919 00189 NM 2007 9 19 AALA20071558 1 20070816 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 661AA 25295 MIA - EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007091900199 20070919 00199 WP 2007 9 19 AALA20071574 1 20070817 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 476AA 49651 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROW 13 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROW 13. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007091900200 20070919 00200 WP 2007 9 19 AALA20071573 1 20070817 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 476AA 49651 LGA - EMERGENCY LIGHT PASSENGER ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT PASSENGER ENTRY DO OR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007092000008 20070920 00008 EA 2007 9 20 REXA200700059 1 20070725 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A REXA O OTHER O OTHER NR NOT REPORTED 1 SO 25 7946A 7946A MAIN PASSENGER DOOR FLOOD LIGHT INOP. REPLACED LIGHT. 2 L 7 2 4F RT A21EA 2007092000014 20070920 00014 NM 2007 9 20 DL75A071209 1 20070913 A 5330 148N32145 SKIN BOEING 757 757212 1384951 NM 1720 S27-29R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 752AT 23128 FUSELAGE SKIN CORROSION AT STA 1720 BETWEEN S-27R AND S-29R. CUTOUT DAMAGED SKIN AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F RT A2NM 2007092000021 20070920 00021 NM 2007 9 20 QXEA200701423 1 20070914 A 5270 401020101 PROXIMITY SENSOR BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR MALFUNCTIONED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 400QX 4030 BOI FLIGHT 2391: JUST AFTER ROTATION, MASTER WARNING WITH FUSELAGE DOOR LIGHT ILLUMINATED ON THEN OFF. AIRCRAFT RETURNE D TO FIELD. MAINTENANCE PERFORMED FUNCTIONAL TEST OF AFT PAX DOOR IAW TASK 52-12-00-720-801. NO DEFECTS NOTED. INTERR OGATED PSEU HISTORY, NUMEROUS APDLK OPEN SHOWN. REMOVED AND REPLACED AFT PAX DOOR LOCK PROX SENSOR IAW AMM TASK 52-71-0 1-000-802 AND 52-41-01-400-802. OPS TEST GOOD. CLEARED PSEU FAULT HISTORY. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007092000028 20070920 00028 NM 2007 9 20 DLM88071223 1 20070908 A 5320 ANGLE DOUG MD88 MD88 3023688 NM BULKHEAD CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 951DL 49882 FOUND CORROSION ON AFT PRESS DOME ANGLE. REPLACED PER DWG 9915561. 2 L 7 2 4F RT A6WE 2007092000036 20070920 00036 NM 2007 9 20 NWAA073136719 1 20070824 A 5320 TENSION TIE BOEING 747 747251F 1384898 NM BS 840 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING "M" CHECK, FOUND CRACKS IN UPPER LOBE TENSION TIE CHANNEL AND WEB FASTENER HOLES AT BS 840 LT. REPAIRED PER EA 6 7-209737. 2 L 7 4 4F A20WE 2007092000043 20070920 00043 2007 9 20 VNAA0708019 4 20070825 A 2312 ANTENNA CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE NR 1 & 2 VHF DAMAGED A VNAA O OTHER O OTHER CR CRUISE 1 GL 05 716PS 10171 CREW REPORTED A POSSIBLE LIGHTNING STRIKE DURING FLIGHT. MAINTENANCE COMPLIED WITH A VISUAL EN ROUTE LIGHTNING STRIKE I NSPECTION. MAINTENANCE FOUND NR 2 ATS ANTENNA, NR 1 AND 2 VHF ANTENNAS DAMAGED. MAINTENANCE REMOVED AND REPLACED ALL D AMAGED ANTENNAS AND REPAIRED ALL DAMAGE. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007092000051 20070920 00051 2007 9 20 753003 4 20070914 A 2200 19642122 YAW DAMPER BOEING 747 747228F 1384895 NM RUDDER FAULTY A Q2SA J A DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 EA 63 753SA 21787 HAD SEVERAL HARD RUDDER KICKS. FOUND THAT SHUTTING DOWN LOWER YAW DAMPER PROBLEM WENT AWAY. DEFERRED ITEM IN ACCORDANC E WITH DDPG PROCEDURES 22-3. REMOVED AND REPLACED LOWER YAW DAMPER COMPUTER IN ACCORDANCE WITH AMM 22-16-02. OPERATIONA L CHECK GOOD. DEFERRAL CLOSED. 2 L 7 4 4F RT A20WE 2007092000057 20070920 00057 2007 9 20 SIMA200726001 4 20070914 A 3442 7021450601 RADAR EMB 135 EMB135KL 3260302 SO WX SYSTEM INOPERATIVE A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 817AE 145554 RADAR INOP IN FLIGHT DUE TO WEATHER EN ROUTE DISPATCH AND CREW ELECTED TO RETURN TO DFW. REMOVED AND REPLACED WEATHER R T UNIT, OPS CHK GOOD IAW EMB AMM 34-42-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007092000063 20070920 00063 NE 2007 9 20 DL76L071189 2 20070908 A 7261 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 LEAKING A DALA C ABORTED TAKEOFF K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 198DN 41362 28455 727650 2L LAV SMOKE DETECTOR GOES OFF ON TAKEOFF, BURNING ODOR DETERMINED RIGHT ENG IS PUTTING OUT OIL ODOR INTO PNEUMATIC SYST EM. DUE TO HISTORY WILL REQUIRE RIGHT ENG TO BE CHANGED. C/W TRANS 1T149 NR 2 ENG CHG. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092000067 20070920 00067 SO 2007 9 20 RAIA00709007 1 20070907 A 2932 156221 PRESSURE SWITCH EMB 145 EMB145 3260210 SO HYDRAULIC SYSTEM LEAKING A RAIA A B UNSCHED LANDING EMER. DESCENT K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 03 820HK 145064 FLT 5490 - STL - DURING CRUISE, HYDRAULIC SYSTEM NR 2 QUANTITY WENT TO ZERO FOLLOWED BY A HYDRAULIC SYSTEM NR 2 FAILURE. MAINTENANCE INSPECTED AND FOUND A LEAKING PRESSURE SWITCH LEAKING. THE SWITCH WAS REMOVED AND REPLACED WITH NO OTHER DEFECTS NOTED DURING TESTS/CHECKS. 2 L 7 2 4F RT T00011AT 2007092000077 20070920 00077 NM 2007 9 20 SWAA074516 1 20070910 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 770 AND BS 794, STR 18L AND STR 19L. REPAIRED SKIN PE R SRM. 2 L 7 2 4F RT A16WE 2007092000084 20070920 00084 NM 2007 9 20 AWXA200701113 1 20070822 A 5320 143N514029 INTERCOSTAL BOEING 757 7572S7 1384962 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 MCN - MAJOR REPAIR - C-11 CHECK - NR 5988574, CRACKED INTERCOSTAL ANGLE, BS 660- BS 680, BL 0, WL 208. REPLACED INTERCO STAL ANGLE, BS 660- BS 680, BL 0, WL 208 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007092000129 20070920 00129 NM 2007 9 20 QXEA200701424 1 20070916 A 3231 ROD END BOMBDR DHC8 DHC8402 1390042 NM MLG DOOR OUT OF ADJUST A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 402QX 4032 PDX FLIGHT: ON TAKEOFF, BROUGHT THE GEAR HANDLE UP AND RECEIVED THE NR 1 GEAR DOOR AND RED GEAR UNSAFE LIGHTS. CYCLED T HE GEAR DOWN AS PER THE EMERGENCY CHECKLIST. ALL INDICATIONS WERE NORMAL WITH THE GEAR DOWN. THEN BROUGHT THE GEAR BAC K UP AS PER THE CHECKLIST AND AGAIN RECEIVED THE NR 1 GEAR UNSAFE LIGHTS. AFTER 20-30 SECONDS, THE LIGHTS WENT OUT. TH E FA VERIFIED ALL DOORS WERE CLOSED. NO OTHER PROBLEMS EN ROUTE OR ON LANDING. MAINTENANCE REMOVED NR 1 MLG RETRACT AC TUATOR IAW Q400 AMM TASK 32-31-11-000-801J. ADJUSTED ROD END WITH SETTING TOOL QXT632439 AND APPLIED CORROSION INHIBITI NG COMPOUND AS REQUIRED. REINSTALLED THE NR 1 MLG RETRACT ACTUATOR IAW Q400 AMM TASK 32-31-11-400-801. NO DEFECTS NOTE 2 H 7 2 4T RT A13NM 2007092000131 20070920 00131 NM 2007 9 20 F3LA200700233 1 20070914 A 5210 BLANKING PLATE AIRBUS A319 A319111 3930336 NM R2 DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 921FR 5402 2010 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON AFT BLANKING PLATE AT R2 DOOR. REPLACED R2 DOOR AFT GIRT BAR FITTING BLANKING PLATE IAW AMM 52-13-31-400-003. 2 L 7 2 4F RT A28NM 2007092000134 20070920 00134 NM 2007 9 20 07FDEA03554 1 20070911 A 5311 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 588FE 48490 MAIN DECK - STA 1601, LONGERON 10R-11R FRAME FOUND DENTED. 09-26-07 REPAIR CARRIED OUT AS PER SRM 53-30- 00 FIG. 1 VOL.I. DAMAGE TOLERANCE INSPECTION REQUIREMENT REQUIRES INITIAL INSPECTION AT 14500 CYCLES FROM THE CURRENT 9821 CY CLES AND REPETITIVE INSPECTION AT 9500 CYCLES THEREAFTER. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007092000138 20070920 00138 EU 2007 9 20 07FDEA03558 1 20070911 A 5320 A53980187208 BRACKET AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 CRACKED BRACKET AT STRG 26 LT BETWEEN FRAME 75-75A. REPLACEMENT OF AFFECTED PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092000149 20070920 00149 NE 2007 9 20 DL76G071180 2 20070905 A 7200 CF680C2B6F ENGINE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 MALFUNCTIONED A DALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 27 1602 31647 29694 706101 AT CRZ RIGHT ENG HAD LOUD BANG A/C YAW AND THEN ENG FAILURE. DIVERTING TO TO MAO FOR REPAIRS. CHANGED ENG ON R/C DECK T RANS 76X1T161 CARD 1 THRU 34. 2 L 7 2 4F 4 F RT A1NM E13NE 2007092000155 20070920 00155 NM 2007 9 20 2007UALA03603 1 20070906 A 5230 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 326UA 23958 AFT CARGO DOOR OUTER SKIN HAS DEEP CREASES FWD LOWER AREA. DENT IS 6 INCHES LONG AND 6 INCHES WIDE, .125 DEEP. LOCATED 3 INCHES FROM LOWER EDGE AND 5 INCHES AFT OF LEADING EDGE, IT HAS 2 CREASES ABOUT 4 INCHES LONG, 3 INCHES APART. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092000158 20070920 00158 NM 2007 9 20 2007UALA03606 1 20070906 A 2560 GIRT BAR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L2 DOOR OUT OF POSITION A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 383UA 24658 DOOR 2L SLIDE GIRT FLAP APPEARS TO HAVE COME OFF OF BACKING PAN SHELF AND IS HANGING DOWN MAKING ARMING AND DISARMING DO OR DIFFICULT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092000159 20070920 00159 NM 2007 9 20 2007UALA03607 1 20070906 A 3260 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT ILLUMINATED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 657UA 27112 GEAR DISAGREE LIGHT ILLUM WHEN GEAR WAS EXTENDED FOLLOWED BY TAIL SKID LIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092000173 20070920 00173 2007 9 20 DL76G071185 4 20070908 A 3442 066500080406 TRANSCEIVER BOEING 767 767332 1382001 NM FWD E&E INOPERATIVE A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 1613B 32776 DURING FLIGHT KNOWN WEATHER DID NOT DISPLAY ON WX RADAR SCREEN. REPLACED RADAR R/T UNIT. AN TEST, ALL GOOD. 2 L 7 2 4F RT A1NM 2007092000174 20070920 00174 NM 2007 9 20 2007UALA03618 1 20070907 A 2120 COALESCER BAG BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN DIRTY A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 372UA 24637 OIL EXHAUST SMELL THROUGHOUT CABIN, CREW USED OXYGEN. HAPPENED AFTER BOTH ENGINES WERE STARTED. FOUND COALESCER FI LTERS CLOGGED/DIRTY. REPLACED COALESCER BAGS. NO REPEATS SINCE, 2 L 7 2 4F 4 F RT A16WE E21EU 2007092000177 20070920 00177 NM 2007 9 20 2007UALA03621 1 20070908 A 5730 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LT WING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 842UA 1569 LEFT WING CUTOUT FOR FUEL TANK PNL 540KB HAS 2 EA FASTENER HOLES FOR ATTACHMENT OF THE NUT PLATE CHANNEL TO THE WING SKI N ELONGATED BEYOND LIMITS. COLD WORKED FASTENER HOLES AND INSTALLED NEW REPAIR BUSHINGS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092000199 20070920 00199 NM 2007 9 20 2007UALA03638 1 20070908 A 3397 POWER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 EEL LAMP AT ROW 31 IS PARTIALLY COVERED BY POWER CABLE. 10-11-07 INSTALLED LAMP OVER POWER CABLE. LAMP NOW FULLY VI SIBLE. NO NEED FOR ANY REPLACEMENT OF COMPONENTS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092000220 20070920 00220 NM 2007 9 20 DL764071188 1 20070910 A 2913 291001935 PUMP BOEING 767 767432ER 1385134 NM HYD SYSTEM OVERHEATED A DALA D RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 836MH 29709 C2 HYD OVHEAT LIGHT CAME ON ON GROUND. REMOVED AND REPLACED C2 HYD PUMP PER M/M. OPS CKS GOOD MCO AND PLACARD REMOVE. 2 L 7 2 4F RT A1NM 2007092000222 20070920 00222 NM 2007 9 20 DLM88071193 1 20070908 A 5311 FRAME DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 951DL 49882 CORROSION ON FRAME AT STA Y=731 BETWEEN LONGERONS 30 AT C2 REPAIRED PER SRM 51-70-05D. 2 L 7 2 4F RT A6WE 2007092000226 20070920 00226 NM 2007 9 20 2007UALA03648 1 20070910 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY LIGHT AT ROWS 38 ABC, 43 ABC & 58 ABC ARE INOPERATIVE. 10-11-07 RELAMPED EMERGENCY LIGHT AT ALL SEAT POSIT IONS. ALL OP CHECKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092000228 20070920 00228 WP 2007 9 20 AALA20071549 1 20070814 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 481AA 49656 SFO - EMERGENCY LIGHT AT FORWARD OVERHEAD TAIL COMPARTMENT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT FORWARD OV ERHEAD TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007092000230 20070920 00230 2007 9 20 AALA20071551 4 20070815 A 2565 SLIDE BOEING 757 757223 1384957 NM L4 DOOR DISLODGED A AALA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 657AM 24615 MIA FLIGHT 2190/15AUG - LEFT NUMBER FOUR DOOR SLIDE FELL OFF DOOR WHEN CATERING OPENING UNARMED DOOR. SLIDE WAS DISLODG ED AND DID NOT DEPLOY. REPLACED SLIDE FOR LEFT NUMBER FOUR DOOR AND ASSIST BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F RT A2NM 2007092000231 20070920 00231 NM 2007 9 20 2007UALA03649 1 20070910 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY EXIT SIGN AFT GALLEY UPPER WALL INOP. 10-11-07 RESECURED EMERGENCY LIGHT CONNECTOR. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092000232 20070920 00232 EU 2007 9 20 AALA20071552 1 20070815 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 JFK - EMERGENCY LIGHT AT SEAT MOUNTED RIGHT SIDE FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT MOUNTED RIGHT SIDE FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007092000234 20070920 00234 WP 2007 9 20 07FDEA03589 1 20070912 A 5730 ARB1075503 SKIN DOUG DC10 DC1010 3022110 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 LT WING FOUND CRACK ON LOWER EXT SKIN L/E. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 SHT 1 VOL I. 2 L 7 3 4F A22WE 2007092000235 20070920 00235 WP 2007 9 20 07FDEA03590 1 20070912 A 5414 AUB703511 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 PYLON NR 1 EXT SKIN FOUND CRACK ON SKIN UPPER SIDE RT. 10-25-07 REPAIRED PYLON SKIN IAW SRM 51-00-01 VOL I FIG 100 & SRM 54-00-01 VOL I FIG 2B. 2 L 7 3 4F A22WE 2007092000236 20070920 00236 NM 2007 9 20 F3LA200700238 1 20070911 A 3350 32143031 BATTERY AIRBUS A319 A319111 3930336 NM EMERGENCY LIGHT INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 921FR 5402 2010 DURING C-3 CHECK, INSPECTION REPORTED RT OVERWING BATTERY FAILED CAPACITY CHECK. REPLACED 4 EMERGENCY POWER SUPPLY BATT ERIES 10WL, 11WL, 12WL AND 13WL IAW AMM 33-51-38-000-002 AND 33-51-38-400-002. PERFORMED OPS CHECK OF EPSU'S 10WL, 11WL , 12WL AND 13WL IAW AMM 33-51-38-400-002, PARA 4 B. OPS CHECK NORMAL. S/N'S FOR REMOVED BATTERIES: 32470, 23972, 3343 1, 1951. 2 L 7 2 4F RT A28NM 2007092000243 20070920 00243 2007 9 20 SIMA200725701 4 20070912 A 3414 INDICATOR CNDAIR CL600 CL6002C10 1390015 EA AIRSPEED CONTAMINATED A SIMA C ABORTED TAKEOFF C J F.O.D. WARNING INDICATION TO TAKEOFF 1 SW 21 509AE 10078 ABORTED TAKEOFF FOR STANDBY INDICATED AIR SPEED. INDICATED FALSE READING COMPARED TO LEFT AND RIGHT INDICATED AIR SPEED INDICATION. MTX FOUND AND CLEANED P2 LINES OF MOISTURE CONTAMINATION IAW AMM 34-11-12. OPS CHECK GOOD LEAK TESTED. N O LEAKS IAW AMM 34-11-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007092000244 20070920 00244 2007 9 20 SIMA200725702 2 20070911 A 7532 32158861 BLEED VALVE EMB 135 EMB135KL 3260302 SO NR 1 ENGINE MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 840AE 145656 ABORTED TAKEOFF DUE TO ENGINE 1 BLEED VALVE FAIL MESSAGE. REMOVED AND REPLACED SERVICEABLE NR 1 ENGINE BLEED VALVE IAW EMB 140 AMM 36-11-05. OPS CHECK GOOD. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007092000246 20070920 00246 SO 2007 9 20 SIMA200725703 1 20070913 A 2710 CONTROL CABLE EMB 135 EMB135LR 3260305 SO AILERONS OUT OF ADJUST A SIMA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SW 21 724AE 145301 CREW NOTIFIED IN FLIGHT THAT FLIGHT CONTROLS STIFF AND AIRCRAFT FLY’S TAIL HEAVY DURING FLIGHT CONTROL CHECKS FOR BEFORE TAKEOFF FOUND PITCH AND ROLL TO BE STIFFENER THAN NORMAL. WITH PITCH TRIM PROPERLY SET FOR TAKEOFF (17 PAX AND 348 CAR GO) AIRCRAFT WANTED TO ROTATE PRIOR TO REACHING VI/VR. UPON ROTATION FORWARD YOKE BIAS AND PITCH DOWN TRIM REQUIRED. I N LEVEL FLIGHT, PITCH WAS ZERO GENERALLY 1 OR 2 IN A 135 A/C ADDITIONALLY IN-FLT FLIGHT CONTROLS FELT SLUGGISH AND HEAVY . ADJUSTED AILERON CABLE TENSION. AIRCRAFT PASSED FUNCTIONAL CHECK FLIGHT. AIRCRAFT RETURNED TO SERVICED. 2 L 7 2 4F RT T00011AT 2007092000247 20070920 00247 EA 2007 9 20 SWIA200718673 1 20070716 A 5242 RETAINER CNDAIR CL600 CL6002B19 1900309 EA E/E DOOR SEA CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 929SW 7703 AVIONICS DOOR SEAL RETAINER HAS HEAVY CORROSION, FOUND AT C-CHECK. INSTALLED NEW SEAL RETAINERS ON AVIONICS DOOR PER SR M 51-42-06/51-42-13. 2 L 7 2 4F RT A21EA 2007092000248 20070920 00248 EA 2007 9 20 SWIA200718674 1 20070716 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 929SW 7703 FS 280 LOWER FLOORBEAM IS CRACKED AT RBL9, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 REO 601R 53-11-171 REV D DATED 02-13-07. 2 L 7 2 4F RT A21EA 2007092000250 20070920 00250 EA 2007 9 20 SWIA200718676 1 20070716 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 929SW 7703 PAX DOOR LOWER AFT CORNER IS CRACKED, FOUND AT C-CHECK. REPAIRED PAX DOOR LOWER AFT CORNER UNDER TOP STEP PER CRJ200 RE O 601R 52-11-279. 2 L 7 2 4F RT A21EA 2007092000251 20070920 00251 EA 2007 9 20 SWIA200718677 1 20070716 A 5210 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 929SW 7703 PAX DOOR INTERCOSTAL IS CRACKED, FOUND AT C-CHECK. INSTALLED NEW INTERCOSTAL PER CRJ200 SRM 51-42-06 PG 4/18. 2 L 7 2 4F RT A21EA 2007092000252 20070920 00252 EA 2007 9 20 SWIA200718678 1 20070718 A 5210 LEVER CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 718SK 10184 PAX DOOR OPEN AND CLOSE INTERNAL LEVER IS CRACKED AT LOWER BOTTOM AREA, FOUND AT C-CHECK. INSTALLED LEVER HANDLE PER CR J7/9 AMM 52-11-02-400-803-A02. 2 L 7 2 4F RT A21EA 2007092000253 20070920 00253 EA 2007 9 20 SWIA200718679 1 20070718 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 718SK 10184 FS 280 FLOORBEAM IS CRACKED AT RBL AND LBL 11, FOUND AT C-CHECK. INSTALLED FS 280 BEAM PER CRJ7/9 SRM 51-42-23/REO 670- 53-11-047. 2 L 7 2 4F RT A21EA 2007092000254 20070920 00254 NM 2007 9 20 2007UALA03652 1 20070909 A 2910 HYDRAULIC SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 583UA 26705 LANDED UNDER AMBER ALERT DUE TO LOSS OF CENTER SYSTEM HYDRAULIC PRESSURE. 10-11-07 CREW SECURED CENTER SYSTEM AC PUM PS AT 0.70. CENTER HYDRAULIC SYSTEM SERVICED TO FULL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092000255 20070920 00255 EA 2007 9 20 SWIA200718680 1 20070718 A 5753 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA TE FLAP DEFORMED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 718SK 10184 FOUND DENT ON RT INBD FLAP BETWEEN FLAP STATION 64.00 AND 67.00, FOUND AT C-CHECK. INSTALLED INNER DOUBLER, FLUSH PLATE AND SUPPORT BRACKET IAW CRJ700 SRM 51-42-06-001-001-A01, CRJ700/900 SRM 57-52-01 PG 201-212 AND 51-42-13 PG 2 AND REO 670-51-52-009 SHEET 1-8. 2 L 7 2 4F RT A21EA 2007092000256 20070920 00256 EA 2007 9 20 SWIA200718681 1 20070801 A 5210 SKIN CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 726SK 10190 PAX DOOR HAS A CRACK ON EXTERNAL SKIN ON AFT END, FOUND AT C-CHECK. INSTALLED REPAIR DOUBLER ON EXTERNAL SKIN OF PAX DO OR ON THE AFT SIDE IAW REO:601R-52-11-104. 2 L 7 2 4F RT A21EA 2007092000257 20070920 00257 EA 2007 9 20 SWIA200718682 1 20070801 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 726SK 10190 FS 280 FLOORBEAM IS CRACKED AT RBL AND LBL9.0, FOUND AT C-CHECK. REPLACED FS 280 BEAM AND INTERCOSTAL PER CRJ7/9 SRM 51 -42-06, REO 670-53-11-247 AND SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007092000260 20070920 00260 NM 2007 9 20 2007UALA03653 1 20070909 A 5754 SLAT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RT WING DAMAGED A UALA O OTHER O OTHER CL CLIMB 1 WP 29 667UA 29239 DAMAGE TO RIGHT LEADING EDGE SLAT BEYOND SRM LIMITS. 10-11-07 CREW REPORTED BIRD STRIKE ON RIGHT LEADING EDGE OF AIR CRAFT. CHK'D ENGINE FOR EVIDENCE OF INGESTION. NO DISCREPANCIES NOTED. NR 8 SLAT REMOVED FOR REPLACEMENT. AFTER CH ECK, AIRCRAFT OK FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092000269 20070920 00269 NM 2007 9 20 KCSA071357 1 20070911 A 5330 SKIN BOEING 747 7472B4B 138481B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-525 BETWEEN STR-46R AND STR 47R SKIN DAMAGED. 2 L 7 4 4F RT A20WE 2007092000271 20070920 00271 NM 2007 9 20 KCSA071359 1 20070911 A 5330 SKIN BOEING 747 7472B4B 138481B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-750 ABOVE STR-44L LAP SEAM, SKIN DAMAGED. 2 L 7 4 4F RT A20WE 2007092000273 20070920 00273 EA 2007 9 20 VNAA0708029 1 20070831 A 2810 FUEL CAP CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE FUEL SYSTEM MISSING A VNAA O OTHER O OTHER CL CLIMB 1 GL 05 708PS 10160 CREW REPORTED THE FUEL CAP MISSING ON CLIMBOUT. CREW ELECTED TO RETURN TO TLH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND MEL'D THE FUEL CAP. MAINTENANCE IN CLT REPLACED THE MISSING FUEL CAP, MEL WAS CLEARED. AIRCRAFT WAS REL EASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007092000274 20070920 00274 EA 2007 9 20 VNAA0709002 1 20070902 A 3244 H29X9015 TIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT MLG SEPARATED A VNAA O OTHER S AFFECT SYSTEMS LD LANDING 1 GL 05 248PS 137 7925 CREW REPORTED THE LEFT HAND INBOARD MAIN TIRE TREAD SEPARATED. MAINTENANCE INSPECTED AND FOUND THE TIRE FAILURE ALONG W ITH A DENT IN THE NOSE COWL AND TWO DAMAGED FAN BLADES. MAINTENANCE REMOVED AND REPLACED THE DAMAGED FAN BLADES IN ACCO RDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE REPAIRED THE LEFT HAND ENGINE INLET LIPSKIN PER TEMP REPAIR 10 862 AND REO 601R-71-61-3690. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007092000276 20070920 00276 EA 2007 9 20 VNAA0708021 1 20070828 A 5310 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE FUSELAGE DAMAGED A VNAA O OTHER O OTHER AP APPROACH 1 GL 05 706PS 10150 CREW REPORTED A BIRD STRIKE TO THE RIGHT SIDE OF THE NOSE AREA. MAINTENANCE INSPECTED AND CONFIRMED THE BIRD STRIKE HAD DONE EXTENSIVE DAMAGE TO THE NOSE AREA. THE AIRCRAFT WAS TEMP. REPAIRED AND FERRIED FOR FURTHER EVALUATION AND REPAIR . MAINTENANCE REPAIRED BIRD STRIKE DAMAGE TO THE RT FORWARD FUSELAGE FROM FS 169 TO FS 202.75. MAINTENANCE ALSO COMPLI ED WITH BIRD STRIKE INSPECTION IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. NO DEFECTS NOTED AT THIS TIME. AIRCRA FT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007092000278 20070920 00278 NM 2007 9 20 07FDEA03613 1 20070912 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 CENTER CARGO, STATION 1710 (TRANSVERSE SKIN SPLICE AREA), LONGERON 49L FOUND CRACKED. 09-24-07 CARRIED OUT REPAIR AS PER FEDEX E.A. 1-5310-113188. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007092000279 20070920 00279 EA 2007 9 20 VNAA0708023 1 20070829 A 2700 TRIM SWITCH CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF343B1 NE COCKPIT STICKING A VNAA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 05 251PS 7931 CREW REPORTED THE CAPTAINS TRIM SWITCH STICKING AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDEN T. MAINTENANCE INSPECTED AND CLEANED THE TRIM SWITCH. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE . 2 L 7 2 4F 4 F RT A21EA E15NE 2007092000280 20070920 00280 EA 2007 9 20 VNAA0708025 1 20070830 A 3244 H29X9015 TIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT MLG SEPARATED A VNAA O OTHER O OTHER LD LANDING 1 GL 05 260JS 193 7957 CREW REPORTED THE LEFT HAND INBOARD MAIN TIRE TREAD HAD PARTIALLY SEPARATED AND SHREDDED UPON LANDING. MAINTENANCE INSP ECTED AND FOUND DAMAGE TO THE LEFT HAND FLAP. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND INBOARD MAIN TIRE. MAINTE NANCE ISSUED TEMP REPAIR 10861 PER REO 601R-57-52-658 FOR THE FLAP DAMAGE. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007092000282 20070920 00282 EA 2007 9 20 VNAA0709006 1 20070904 A 2133 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN PRESSURE OPEN A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 237PS 7906 CLT - FLT 2207 - CREW REPORTED A CABIN ALT CAS MESSAGE FOLLOWED BY CABIN ALT RWP MESSAGE ON CLIMB-OUT. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE OVERBOARD SHUTOFF VALVE OPEN. MAINTENAN CE SECURED THE VALVE IN THE CLOSED POSITION IAW THE MEL 21-24-06 OPTION 2. PRESSURIZATION OPS CHECKS WERE GOOD AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007092000284 20070920 00284 EU 2007 9 20 TRAX200701289 1 20070827 A 5711 SPAR AEROSP ATR72 ATR72 EU WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 CRACK DET - REAR SPAR LWR SURFACE FLANGE AT WING TO FUSE JUNCTION AT RIB 2. COMPLIED WITH UNDER EXELTECH W/O YUL000780 NONROUTINE 286. REFER TO THIS NONROUTINE FOR MTC ACTION. SUPPLEMENTAL - SDR CLOSED 09/12/07. 2 H 7 2 4T RT 2007092000285 20070920 00285 EU 2007 9 20 TRAX200701290 1 20070827 A 5711 SPAR AEROSP ATR72 ATR72 EU WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 CRACK DET - FRONT SPAR LOWER SURFACE FLANGE AT RIB 2. COMPLIED WITH UNDER EXELTECH W/O YUL000780 NONROUTINE 285. REFER TO THIS NONROUTINE FOR MTC ACTION. SUPPLEMENTAL - SDR CLOSED 09/12/07. 2 H 7 2 4T RT 2007092000287 20070920 00287 EU 2007 9 20 TRAX200701292 1 20070827 A 5711 SPAR AEROSP ATR72 ATR72 EU WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 CRACK DETECT - FRONT SPAR LOWER SURFACE FLANGE AT RIB 4. COMPLIED WITH UNDER EXELTECH W/O YUL000780 NONROUTINE 278. RE FER TO THIS NONROUTINE FOR MTC ACTION. SUPPLEMENTAL - SDR CLOSED 09/12/07. 2 H 7 2 4T RT 2007092000288 20070920 00288 EA 2007 9 20 TRAX200701302 1 20070904 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 834AS 7254 AAR - "OPEN" AND "EXIT" PLACARDS ON PAX DOOR ARE DAMAGED. REMOVED UNSERVICEABLE "OPEN" AND "EXIT" PLACARDS FROM PAX DOO R AND INSTALLED SERVICEABLE P/N'S S1574-18 (EXIT) AND P/N S1574-14 (OPEN), IAW CRJ 200 AMM 11-30-00. SUPPLEMENTAL - SDR CLOSED 09/12/07. 2 L 7 2 4F RT A21EA 2007092000289 20070920 00289 EA 2007 9 20 TRAX200701304 1 20070904 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 875AS 7559 AAR - LEFT I/B CLIP AT FS 280 AND LBL 9.0 IS CRACKED. REMOVED LEFT I/B CLIP AT FS 280 AT LBL 9.0 AND INSTALLED NEW SERV ICEABLE CLIP P/N 601R31113-57 IAW CRJ 200 SRM 51-42-21. SUPPLEMENTAL - SDR CLOSED 9/12/07. 2 L 7 2 4F RT A21EA 2007092000290 20070920 00290 EA 2007 9 20 TRAX200701305 1 20070904 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 875AS 7559 AAR - RIGHT I/B CLIP AT FS 280 AND RBL 9.0 IS CRACKED. REMOVED RIGHT I/B CLIP AT FS 280 AND RBL 9.0. INSTALLED NEW SER VICEABLE CLIP P/N 601R31113-58 IAW CRJ 200 SRM 51-42-21. SUPPLEMENTAL - SDR CLOSED 09/12/07. 2 L 7 2 4F RT A21EA 2007092000292 20070920 00292 EA 2007 9 20 TRAX200701314 1 20070905 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 834AS 7254 AAR - LEFT O/B INTERCOSTAL AT FS 484 I/B AND O/B CLIPS CRACKED. CUT OUT DAMAGED ATTACHMENT FLANGE ON LEFT O/B INTERCOST AL FS 484 PER REO 601R-53-41-059 NOTE 1. REMOVED CRACKED INTERCOSTAL CLIP PER REO 601R-53-41-059. COMPLIED WITH LPI OF LEFT FS 486 O/B INTERCOSTAL CUTLINE AND FABRICATED REPLACEMENT ANGLES 2 EACH FOR I/B AND O/B LOCATIONS IAW REO 601R-53- 41-059. NO DEFECTS NOTED. COMPLIED WITH REO 601R-53-41-059. SUPPLEMENTAL - SDR CLOSED 09/12/07. 2 L 7 2 4F RT A21EA 2007092000293 20070920 00293 EA 2007 9 20 TRAX200701315 1 20070905 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 834AS 7254 AAR - LEFT I/B INTERCOSTAL AT FS 484 I/B CLIP CRACKED. REMOVED CRACKED LEFT I/B INTERCOSTAL CLIP AT FS 484 PER CRJ 200 SRM 51-42-06. LPI OF LEFT FS 484 I/B FABRICATED REPLACEMENT ANGLE IAW NDTM 51-20-08. NO DEFECTS NOTED. INSTALLED REPL ACEMENT ANGLE IAW CRJ 200 SRM 51-42-06. REFERENCE ATTACHED DOCUMENT FOR DETAILS. SUPPLEMENTAL - SDR CLOSED 09/12/07. 2 L 7 2 4F RT A21EA 2007092000295 20070920 00295 EA 2007 9 20 TRAX200701317 1 20070905 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 834AS 7254 AAR - RIGHT O/B INTERCOSTAL FS 484 I/B CLIP CRACKED. REMOVED DAMAGED ANGLE CLIP FROM RIGHT O/B INTERCOSTAL FS 484 I/B S IDE IAW CRJ 200 SRM 51-42-06. FABRICATED AND DRILLED ANGLE CLIP FROM 2024 T-3 .063" PO 950261 IAW CRJ 200 SRM 51-40-11. PERFORMED LPI ON FABRICATED ANGLE FOR INTERCOSTAL REPAIR IAW REO 601R-53-41-059. NO DEFECTS NOTED. REQUIRES OK FOR A LODINE PRIME AND PAINT. ALODINED AND PRIMED IAW CRJ 200 SRM 51-25-06. OK TO INSTALL. INSTALLED SERVICEABLE I/B CLIP O N RIGHT O/B INTERCOSTAL FS 484 IAW REO 601R-53-41-059. OK TO TOPCOAT. TOPCOATED IAW CRJ 200 SRM 51-25-16. SUPPLEMENTA L - SDR CLOSED 09/12/07. 2 L 7 2 4F RT A21EA 2007092000297 20070920 00297 NM 2007 9 20 CALA0700512 1 20070912 A 5230 6546921528 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A 0.35 INCH CRACK AT LIGHTENING HOLE IN C-1 CARGO DOOR INTERIOR SKIN. A REPAIR WAS INSTALLED IAW ECRA 5232-01090. 2 L 7 2 4F RT A16WE 2007092000299 20070920 00299 WP 2007 9 20 ABXA070279 1 20070822 A 5311 99115055 FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 WHILE COMPLYING WITH EA 53300036, FOUND CRACKED FRAME. REPAIRED FRAME IAW DC9 SRM 53-03, FIGURE 34. 2 L 7 2 4F A6WE 2007092000300 20070920 00300 WP 2007 9 20 ABXA070280 1 20070822 A 5311 99115057 FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 WHILE COMPLYING WITH EA 53300036, FOUND FRAME CRACKED. REPAIRED FRAME IAW DC9 SRM 53-03, FIGURE 34. 2 L 7 2 4F A6WE 2007092000301 20070920 00301 WP 2007 9 20 ABXA070281 1 20070908 A 5342 5939711501 ANGLE DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 DURING ROUTINE SERVICE BULLETIN INSPECTION OF LEFT DORSAL FIN ATTACH ANGLE, FOUND ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2007092000305 20070920 00305 NM 2007 9 20 ABXA070277 1 20070904 A 3350 20131A BATTERY BOEING 767 767231 1385131 NM CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 702AX 22566 EMERGENCY EXIT LIGHTS FADED OUT DURING TEST. SWITCHED BATTERY WITH SPARE IAW B767 MM 33-51-07. THE SPARE EMERGENCY LIG HT BATTERY WAS DEFERRED 56859 FOR MAINTENANCE TRACKING IAW ABX GMM 01.07.04. CLEARED DI 56859, REMOVED AND REPLACED SPA RE EMERGENCY LIGHT BATTERY IAW B767 MM. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2007092000307 20070920 00307 EU 2007 9 20 YENA2007080 1 20070907 A 2781 1702286A SENSOR EMB ERJ190 ERJ190100IGW 3260408 EU L/E SLAT MALFUNCTIONED A YENA O OTHER N FALSE WARNING CR CRUISE 1 EA 15 238JB 3317 19000039 FLT 1086, CLT-JFK, SLAT FAIL. PERFORMED TSM 27-81-00-810-805, FOUND LT WING OUTBOARD SLAT SKEW SENSOR 2/3 DEFECTIVE. R EMOVED AND REPLACED LT OUTBOARD SLAT SKEW SENSOR 2/3. OPS CHECK GOOD REF AMM 27-83-01 AND REMOVED AND REPLACED LT WING OUTBOARD SLAT SKEW SENSOR 2/3 WIRE HARNESS. OPS CHECK GOOD REF AMM 27-83-07. 2 L 7 2 4F RT A57NM 2007092000311 20070920 00311 NM 2007 9 20 KCSA071362 1 20070912 A 5320 WEB BOEING 747 7472B4B 138481B NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 SEVERAL DENTS IN LOWER BILGE TORQUE BOX TOP SKIN AT BS 1660 TO 1680, RBL-27 TO RBL-43. 2 L 7 4 4F RT A20WE 2007092000313 20070920 00313 EA 2007 9 20 SWIA200718684 1 20070726 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSLEAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 727SK 10191 FOUND COCKPIT FLOORBEAM ANGLE IS CRACKED AT RBL9, FOUND AT C-CHECK. INSTALLED COCKPIT FLOOR SUPPORT ANGLE PER CRJ700/90 0 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007092000316 20070920 00316 WP 2007 9 20 ABXA070285 1 20070807 A 5753 99575761 SKIN PANEL DOUG DC9 DC931 3022065 WP T/E FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 907AX 47203 LEFT FLAP UPPER OUTBOARD SURFACE HAD SKIN BULGING AND CUPPED RIVETS. REMOVED FLAP SEGMENT FOR REPAIR AND REINSTALLED IA W DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 2007092000317 20070920 00317 WP 2007 9 20 ABXA070284 1 20070830 A 5420 99581938 ANGLE DOUG DC9 DC941 302207N WP NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 960AX 47762 NR 2 PYLON WEB ANGLE ABOVE FORWARD EDGE OF PANEL 8206A INSIDE PYLON CRACKED. REPAIRED ANGLE IAW DC9 SSRM K05159. PO 42 1513435. INSTALLED WITH HI-LOKS IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2007092000318 20070920 00318 NM 2007 9 20 QXEA200701426 1 20070916 A 3260 PROXIMITY SENSOR BOMBDR DHC8 DHC8402 1390042 NM MLG OUT OF ADJUST A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 414QX 4061 SEA FLIGHT NR 2260: RIGHT MLG DOOR LIGHT ILLUMINATES RANDOMLY FOR ONE SECOND INTERVALS IN FLIGHT. OCCASIONAL GEAR BUMP FELT. MAINTENANCE INTERROGATED PSEU FOR PRESENT FAULTS AND FOUND 'LGDRCL RIGGING NEAR GAP TOO LARGE' AND 'RGDRCL RIGGIN G FAR GAP TOO SMALL' ADJUSTED BOTH LGDRCL AND RGDRCL PROX SENSORS IAW Q400 AMM TASK 32-61-06-830-801 FOR A NOMINAL GAP O F .050" AND AN INDUCTANCE NOMINAL VALVE OF 8.102 MH TO 8.522 MH. PRESENT FAULTS CLEARED. CYCLED GEAR DOORS 5 TIMES. O PS CHECK GOOD. FAULT HISTORY WAS ALSO CLEARED IAW Q400 AMM TASK 32-61-00-743-801. NO PARTS REPLACED. AIRCRAFT RETURNE D TO SERVICE. 2 H 7 2 4T RT A13NM 2007092000321 20070920 00321 EA 2007 9 20 SWIA200718685 1 20070726 A 5751 LINK CNDAIR CL600 CL6002C10 1390015 EA LT WING AILERON CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 727SK 10191 LEFT WING AILERON PCU LINK HAS SURFACE CORROSION, FOUND AT C-CHECK. REMOVED SURFACE CORROSION ON PCU LINK PER SRM 51-21 -06-001-001-A01 PART 6. 2 L 7 2 4F RT A21EA 2007092000322 20070920 00322 EA 2007 9 20 SWIA200718686 1 20070726 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 727SK 10191 FS 280 FLOOR SUPPORT BEAM IS CRACKED AT LBL9, FOUND AT C-CHECK. INSTALLED FS 280 FLOOR SUPPORT BEAM AND INTERCOSTALS PE R CRJ7/9 SRM 51-42-21, 51-42-06, SRM 51-23-00 AND REO:670-53-11-242 REV B. 2 L 7 2 4F RT A21EA 2007092000323 20070920 00323 EA 2007 9 20 SWIA200718687 1 20070913 A 5210 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 368CA 10075 CRACK IN PAX DOOR AFT DRAG ANGLE. REPAIRED CRACK IN PAX DOOR AFT DRAG ANGLE IAW REO 670-52-11-0054. 2 L 7 2 4F RT A21EA 2007092000326 20070920 00326 NE 2007 9 20 HALA0700378 2 20070914 A 7200 ENGINE BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE NR 1 SURGES A HALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, ACARS EXCEEDANCE REPORT NR 1 ENGINE SURGE AT 35,000FT. ACCOMPLISHED HAL M105 FILE NR 582038 I TEMS NR 1 AND NR 2 WITH FOLLOW UP ACTION AS NOTED ON LOG PG 196039 ITEM 64. OK FOR SERVICE, NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092000327 20070920 00327 NE 2007 9 20 HALA0700379 2 20070914 A 7200 ENGINE BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE NR 2 SURGES A HALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, ACARS EXCEEDANCE REPORT NR 2 ENGINE SURGE AT 35,000 FT. ACCOMPLISHED HAL M105 FILE NR 582038 ITEM NR 3. NO DEFECTS NOTED. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092000329 20070920 00329 NM 2007 9 20 HALA0700381 1 20070916 A 4940 211734220 ECU BOEING 767 767332 1382001 NM APU MALFUNCTIONED A HALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 13 598HA 3513 3513 23278 ETOPS SIGNIFICANT SYSTEM, APU WOULD NOT START ON GROUND TRIED STARING TWICE 1ST APU HUNG AT 30 PERCENT 2ND TIME HUNG AT 18 PERCENT. REMOVED AND REPLACED APU ECU BITE CHECK GOOD. OPS CHECK GOOD WORK DONE IAW AMM 49-61-05. 2 L 7 2 4F RT A1NM 2007092000330 20070920 00330 NM 2007 9 20 HALA0700383 1 20070916 A 4940 38880585 EXCITER BOEING 767 76733A 1385209 NM APU INOPERATIVE A HALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM, APU WOULD NOT START AFTER LANDING. REPLACED IGNITION EXCITER, IGNITION LEAD AND IGNITION PLUG PER AMM 49-41-03,49-41-02,49-41-01. OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2007092000331 20070920 00331 NE 2007 9 20 HALA0700382 2 20070916 A 7311 COOLER BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE FUEL/OIL LEAKING A HALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM, ON WALKAROUND FOUND EXCESS OIL ON BOTTOM OF ENGINE NR 1 COWLS. MOTORED ENGINE. FOUND OIL SEE PING FROM FUEL OIL COOLER, OIL LINE. TIGHTEN FOUR BOLTS. RAN ENGINE AT IDLE FOR FIVE MINUTES. NO LEAKS NOTED. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092000334 20070920 00334 WP 2007 9 20 AALA20071547 1 20070814 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 481AA 49656 SFO - EMERGENCY LIGHTS AT LEFT AND RIGHT OVERWING FORWARD EMERGENCY EXIT INOPERATIVE. REPLACED BATTERY PACK B5103 FOR E MERGENCY LIGHT AT LEFT AND RIGHT FORWARD OVERWING EMERGENCY EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007092000335 20070920 00335 WP 2007 9 20 AALA20071548 1 20070814 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 481AA 49656 SFO - EMERGENCY LIGHTS AT AFT STAIRS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT STAIRS. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007092000336 20070920 00336 NM 2007 9 20 AALA20071571 1 20070816 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 188AN 32382 SFO - EMERGENCY LIGHT AT SEAT 36D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 36D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092000339 20070920 00339 NM 2007 9 20 AWXA200701102 1 20070817 A 5754 114N407614 SKIN BOEING 757 7572S7 1384962 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 MCN - MAJOR REPAIR - C-11 CHECK - NR 5988285, LEFT WING NR 2 SLAT COVE SKIN CRACKED, OSS 665.50 - OSS 677.50. REPLACED LEFT WING NR 2 SLAT COVE SKIN, OSS 665.50 - OSS 677.50 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007092000340 20070920 00340 NM 2007 9 20 AWXA200701103 1 20070817 A 5754 114N407611 SKIN BOEING 757 7572S7 1384962 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 MCN - MAJOR REPAIR - C-11 CHECK - NR 5988286, LEFT WING NR 2 SLAT COVE SKIN CRACKED, OSS 691. REPLACED LEFT WING NR 2 S LAT COVE SKIN, OSS 691 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007092000341 20070920 00341 NM 2007 9 20 AWXA200701104 1 20070817 A 5754 114N407728 SKIN BOEING 757 7572S7 1384962 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 MCN - MAJOR REPAIR - C-11 CHECK - NR 5988289, LEFT WING NR 3 SLAT COVE SKIN CRACKED, OSS 542.70 - OSS 573.30. REPLACED LEFT WING NR 3 SLAT COVE SKIN, OSS 542.70 - OSS 573.30 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007092000343 20070920 00343 EU 2007 9 20 AWXA200701106 1 20070907 A 5320 D53475765200 SILL AIRBUS 320 A320232 3930326 EU ZONE 100 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 655AW 1075 SAL - MAJOR REPAIR - BC-6 CHECK - NR 5991441, 5991442, 5991443, 5991444 AND 5991445, CORROSION ON BULK CARGO DOOR CUT O UT LOWER SILL, BS 2830/FR 60 AND -Y680, BS 2830/FR 60 AND -Y670, BS 2883/FR 61 AND -Y650, BS 2883/FR 61 AND -Y640 AND BS 2883/FR 61 AND -Y630. REPAIRED BULK CARGO DOOR CUT OUT LOWER SILL, BS 2830/FR 60 AND -Y680, BS 2830/FR 60 AND -Y670, B S 2883/FR 61 AND -Y650, BS 2883/FR 61 AND -Y640 AND BS 2883 /FR 61 AND -Y630 IAW A320 SRM 53-41-49. 2 L 7 2 4F RT A28NM 2007092000345 20070920 00345 EU 2007 9 20 AWXA200701108 1 20070915 A 5751 SKIN AIRBUS 320 A320232 3930326 EU ZONE 600 CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 669AW 1792 PHX - MAJOR REPAIR - P-08 CHECK - NR 5881547, RIGHT WING AILERON INBOARD LOWER LEADING EDGE RUBBING ON FORWARD ACCESS PA NEL, WS 1200. REPAIRED RIGHT WING AILERON INBOARD LOWER LEADING EDGE, WS 1200 IAW A320 SRM 57-61-21. 2 L 7 2 4F RT A28NM 2007092000346 20070920 00346 NM 2007 9 20 AWXA200701110 1 20070817 A 5210 143N611032 STOP FITTING BOEING 757 7572S7 1384962 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 MCN - MAJOR REPAIR - C-11 CHECK - NR 5988104, CRACKED STOP FITTING, R2 DOOR, BS 726.50, RBL 78, WL 227. REPLACED STOP F ITTING, R2 DOOR , BS 726.50, RBL 78, WL 227 IAW USAIRWAYS EA 120230. 2 L 7 2 4F RT A2NM 2007092000347 20070920 00347 EU 2007 9 20 CPCP20070094 1 20070827 A 5312 BULKHEAD AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 414WF 414 CORROSION FOUND ON FWD PRESSURE BULKHEAD RT BL 187.5 AND BL 350. FWD PRESSURE BULKHEAD RT BL 187.5 AND BL 350 REPAIRED AS PER SRM 53-11-10 FIG 408. 2 H 7 2 4T RT A53EU 2007092000348 20070920 00348 EU 2007 9 20 CPCP20070093 1 20070827 A 5320 THRESHOLD AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CRACKED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 414WF 414 RT THRESHOLD GUTTER BETWEEN FRAME 36 TO 39 IS CRACKED AND CORRODED. RT THRESHOLD GUTTER FRAME 36-39. REPLACED IAW SRM 51-25-07. 2 H 7 2 4T RT A53EU 2007092000351 20070920 00351 EU 2007 9 20 CPCP20070097 1 20070824 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 414WF 414 LT SEAT TRACK BETWEEN FRAME 36 TO 39 IS CORRODED. LT SEAT TRACK BETWEEN FRAME 36-TO 39 IS REPLACED BY NEW ONE IAW SRM 5 1-25-04. 2 H 7 2 4T RT A53EU 2007092000352 20070920 00352 EU 2007 9 20 CPCP20070099 1 20070824 A 5320 BRACKET AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 414WF 414 LT FOLDING STEP BRACKETS ON THRESHOLD BETWEEN FRAME 36 TO 39 ARE CORRODED. LT FOLDING STEP BRACKET REPLACED IAW SRM 51- 25-04. 2 H 7 2 4T RT A53EU 2007092000354 20070920 00354 NM 2007 9 20 KCSA071363 1 20070912 A 5320 SHEAR WEB BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 CRACKED SHEAR WEB 1.5 INCH AT STA-820 TO 840 AT STR-11R. 2 L 7 4 4F RT A20WE 2007092000355 20070920 00355 NM 2007 9 20 KCSA071364 1 20070912 A 5320 SHEAR WEB BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 CRACKED SHEAR WEB 1.75 INCH AT STA-820 TO 840 STR-11L. 2 L 7 4 4F RT A20WE 2007092000357 20070920 00357 NM 2007 9 20 KCSA071366 1 20070912 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 CAPTAINS FWD O/B SEAT TRACK HAS 1.5 INCH CRACK IN FWD END. 2 L 7 4 4F RT A20WE 2007092000358 20070920 00358 NM 2007 9 20 KCSA071367 1 20070912 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 CAPTAINS AFT O/B SEAT TRACK HAS A 1.5 INCH CRACK FWD END. 2 L 7 4 4F RT A20WE 2007092000360 20070920 00360 NM 2007 9 20 KCSA071369 1 20070912 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 CAPTAINS I/B AFT SEAT TRACK HAS A 1.5 INCH CRACK IN WEB. 2 L 7 4 4F RT A20WE 2007092000361 20070920 00361 NM 2007 9 20 KCSA071370 1 20070912 A 5320 TORQUE BOX BOEING 747 7472B4B 138481B NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-1670 RBL-1 DENT IN TORQUE BOX TOP SKIN. 2 L 7 4 4F RT A20WE 2007092000363 20070920 00363 SO 2007 9 20 C2XA07TY048 1 20070912 A 5320 14521713005 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16525 145403 TYS - DURING THE CURRENT C-CHECK INSPECTION THE RIGHT OMEGA BEAM WAS FOUND TO HAVE CORROSION AROUND A NUT PLATE THAT WAS OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT OMEGA BEAM IAW EMB 135/145 SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2007092000364 20070920 00364 SO 2007 9 20 C2XA07TY049 1 20070912 A 5320 14521721009 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16525 145403 TYS - DURING A CURRENT C-CHECK INSPECTION THE FWD DIGITAL WAS FOUND WITH CORROSION. MAINTENANCE REMOVED THE CORRODED SE CTION, INSTALL A NEW SECTION WITH A DOUBLER. ALL WORK WAS IAW EMB EC 5320-01059. A/C WILL BE RELEASED AT THE END OF TH E CHECK. 2 L 7 2 4F RT T00011AT 2007092000367 20070920 00367 NM 2007 9 20 CALA0700514 1 20070912 A 5320 6517684638 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17328 23458 INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL AT STA 294, 12L. THE INTERCOSTAL WAS REPLACED IAW ECRA 5311-01356. 2 L 7 2 4F RT A16WE 2007092000368 20070920 00368 NM 2007 9 20 CALA0700515 1 20070912 A 5313 65617777 STRINGER SPLICE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17328 23458 INSPECTION FOUND A .75 INCH CRACK IN STRINGER SPLICE AT STA 360, S15L. THE STRINGER SPLICE WAS REPAIRED IAW ECRA 5311-0 1356. 2 L 7 2 4F RT A16WE 2007092000370 20070920 00370 EA 2007 9 20 TRAX200701306 1 20070904 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 875AS 7559 AAR - RIGHT O/B CLIP AT FS 280 AND RBL 9.0 IS CRACKED. REMOVED RIGHT O/B CLIP AT FS 280 AT RBL 9.0. FABRICATED NEW CLI P FROM S6144-4 AND INSTALLED SERVICEABLE CLIP IAW REO 601R-53-11-171. SUPPLEMENTAL - SDR CLOSED 09/14/07. 2 L 7 2 4F RT A21EA 2007092000374 20070920 00374 EA 2007 9 20 TRAX200701328 1 20070906 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 834AS 7254 AAR - O/B CLIP CRACKED AT FS 280 LBL 9. REFERENCE ROUTINE 50186/2000/0022 FOR CORRECTIVE ACTION 14211 9-11-07. SUPPLEM ENTAL - SDR CLOSED 09/14/07. 2 L 7 2 4F RT A21EA 2007092000375 20070920 00375 EA 2007 9 20 TRAX200701329 1 20070906 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 834AS 7254 AAR - INBOARD CLIP CRACKED AT FS 280 LBL 9. REFERENCE ROUTINE 50186/2000/0022 FOR CORRECTIVE ACTION 14211 9-11-07. SUP PLEMENTAL - SDR CLOSED 09/14/07. 2 L 7 2 4F RT A21EA 2007092000376 20070920 00376 WP 2007 9 20 ABXA070287 1 20070813 A 5755 3923258503 BRACKET DOUG DC9 DC931 3022065 WP SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 947AX 47004 LEFT WING TRAILING EDGE OUTBOARD SPOILERS INBOARD TORSION BAR BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW DC9 SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 2007092000377 20070920 00377 WP 2007 9 20 ABXA070288 1 20070828 A 5347 4925848M36000 SEAT TRACK DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 LITE CORROSION ON UPPER CARGO CENTER SEAT TRACK STA 256 - 294. REPLACED SECTION OF TRACK IAW DC9 51-30-1. 2 L 7 2 4F A6WE 2007091900172 20070919 00172 NM 2007 9 19 AALA20071570 1 20070816 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 188AN 32382 SFO - EMERGENCY LIGHT AT SEAT 34D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 34D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2007091900174 20070919 00174 NM 2007 9 19 AALA20071591 1 20070820 A 2697 WIRE HARNESS BOEING 767 767323 1385205 NM DAMAGED A AALA O OTHER N B FALSE WARNING SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 360AA 24041 FRA INFLIGHT T84/20AUG - DURING FLIGHT RECEIVED AFT CARGO HEAT OVERHEAD STATUS MESSAGE AND SEVER CIRCUIT BREAKERS RELATE D TO AFT AND BULK CARGO HEAT SYSTEM TRIPPED. AFTER NORMAL LANDING SMOKE REPORTED IN CABIN AND EMERGENCY DECLARED. PASS ENGERS DEPLANED AND NO INJURIES SUSTAINED. FERRIED AIRCRAFT TO AFW. REPAIRED WIRE BUNDLE W580. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007091900191 20070919 00191 NM 2007 9 19 AALA20071580 1 20070818 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 916AN 29517 DFW - EMERGENCY LIGHT AT SEAT ROW 13F INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 13F. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007091900192 20070919 00192 NM 2007 9 19 AALA20071579 1 20070818 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 916AN 29517 DFW - EMERGENCY LIGHT AT SEAT ROW 19D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 19D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007091900197 20070919 00197 NM 2007 9 19 AALA20071554 1 20070815 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 603AA 27054 SFO - EMERGENCY LIGHTS AT LEFT AND RIGHT LOWER EXIT DOOR INOPERATIVE. REPLACED BATTERY PACK M10798 AT STATION 400 FOR E MERGENCY LIGHTS AT LEFT AND RIGHT LOWER EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092000001 20070920 00001 NM 2007 9 20 DLM88071201 1 20070907 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 1032 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 951DL 49882 CRACK ON LT CUSP WEB AT STA1032 X=44. REPAIRED PER ERA 398191-14MA REV A. 2 L 7 2 4F RT A6WE 2007092000004 20070920 00004 EA 2007 9 20 REXA200700055 1 20070625 A 3350 59257 INVERTER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A REXA O OTHER O OTHER NR NOT REPORTED 1 SO 25 8944B 7944 EMERGENCY LIGHT FLOOR STRIP INOP AT THE EMERGENCY ROW LIGHT WAS NOT OPERATING BUT INVERTER WAS FOUND TO BE THE CAUSE. I NVERTER WAS REPLACED. 2 L 7 2 4F RT A21EA 2007092000006 20070920 00006 EA 2007 9 20 REXA200700057 1 20070716 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DAMAGED A REXA O OTHER O OTHER NR NOT REPORTED 1 SO 25 8674A 7674 FOUND FORWARD FLOOR EMERGENCY LIGHTS INOP. REPLACED CONNECTOR OF EMERGENCY LIGHT STRIP. 2 L 7 2 4F RT A21EA 2007092000023 20070920 00023 NM 2007 9 20 DL764071217 1 20070916 A 2597 WIRE HARNESS BOEING 767 767432ER 1385134 NM AFT GALLEY CHAFED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 839MH 29712 AFTER PUSHBACK, IN AFT GALLEY 2 FLT ATTENDANTS FELT A SHOCK WHEN TOUCHING A DOOR IN THE GALLEY. FOUND 1 WIRE CHAFED IN WIRE BUNDLE NEXT TO GALLEY DISCONNECT REPAIRED AND REWRAPPED AND REROUTED WIRE BUNDLE. WRAPPED WIRE BUNDLE. CKS GO OD. 2 L 7 2 4F RT A1NM 2007092000025 20070920 00025 NM 2007 9 20 DLM88071220 1 20070908 A 5311 FRAME DOUG MD88 MD88 3023688 NM BS 1510 BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 951DL 49882 FOUND BROKEN FRAME AT STA 1510. REPLACED FRAME. 2 L 7 2 4F RT A6WE 2007092000062 20070920 00062 NM 2007 9 20 F3LA200700231 1 20070912 A 5320 D5347217220400 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 921FR 5402 2010 DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM INBD OF GIRT BAR FLOOR MOUNTS IN L2 DOOR ENTRY WAY CORRODED ON NUT PLATE HOLES (BOTTOM AND TOP). REPLACED FLOORBEAM AT Y1292 BETWEEN FR66 AND FR 68 IAW SRM 51-42-11 AND EA A0-53T-11472. 2 L 7 2 4F RT A28NM 2007092000065 20070920 00065 NM 2007 9 20 HALA0700370 1 20070906 A 3610 9750172006 THERMAL SWITCH BOEING 767 76733A 1385209 NM FAULTED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 580HA 28140 AT 1500' ON T/O "RT ENG BLEED AND OVHT" EICAS MESSAGES AND LIGHTS ILLUMINATED, (BLEED AND OVERHEAT LIGHT). QRH DRILLS C ARRIED OUT, NIL FIX. EGR C/OUT AT T/O POWER 1.5 EPR AFTER 2-1/2 MINS DEFECT REOCCURRED RT OVERHEAT SWITCH REPLACED EXTE NSIVE EGRC/OUT AT T/O AND CLIMB POWER BLEEDS CYCLED NIL FAULTS. AT HAWAIIAN REQUEST HPSOV+HPSOV CONTROLLER REPLACED IAW AMM 36-11-07+36-11-08 WORK C/OUT ON AIR NZ S/O 70439029. PRV, HPSOV AND CONTROLLERS, PRSOV, FAN AIR VALVE AND TEMP SEN SOR SENSE LINES CHECK TIGHTENED SATISFACTORY. AIR SUPPLY BITE FAULTS RT HPSOV; HPSOV BUTTERFLY SHAFT AT MICRO-SWITCH FO UND WORN, FIM 36-10-00 C/OUT FIG 113, BLOCKS 2, 3, 4, AND 5 SATISFACTORY SUSPECT FAN AIR TEMP SENSOR/HPSOV PER BLOCKS 40 2 L 7 2 4F RT A1NM 2007092000080 20070920 00080 NM 2007 9 20 SWAA074511 1 20070910 A 5310 6545833 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 188 AND BS 196.5, STR 17L. REMOVED AND REPLACED W EB PER SRM. 2 L 7 2 4F RT A16WE 2007092000125 20070920 00125 EU 2007 9 20 AWXA200701109 1 20070911 A 2910 PRIORITY VALVE AIRBUS 320 A320231 3930325 EU HYD SYSTEM LEAKING A AWXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 621AW 053 CMH - EL - LOG 7781043 - DURING CRUISE, CREW RECEIVED A YELLOW SYSTEM LOW LEVEL MESSAGE. CREW DECLARED AN EMERGENCY. T HE LANDING WAS UNEVENTFUL AND THE A/C TAXIED TO THE GATE. MX DISCOVERED THE YELLOW SYSTEM PRIORITY VALVE LEAKING. MX R EPLACED THE YELLOW SYSTEM PRIORITY VALVE (3064GM) PER AMM 29-13-33-000-001. OPERATIONAL/LEAK CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007092000126 20070920 00126 NM 2007 9 20 2007UALA03594 1 20070905 A 5330 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 929UA 26652 RIGHT AFT SERVICE DOOR CUTOUT HAS CRACK AT LOWER FWD CORNER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092000143 20070920 00143 NE 2007 9 20 TSAA0772049 2 20070909 A 7200 JT8D9A ENGINE BOEING 737 737236 1384476 NM PWA JT8 JT8D9A 52048 NE NR 1 FAILED A TSAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 13 828AL 43832 23168 P707311B NON-ETOPS FLIGHT 90 HNL-KOA - ON TAKEOFF, THE NR 1 ENGINE DID NOT DEVELOP FULL POWER. THE CREW ELECTED TO TAKEOFF AND T HEN RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE ASSEMBLY IN ACCORDANCE W ITH MAINTENANCE FORMS M-211, M-212, M-213 AND M-215. ALL LEAK AND OPERATIONAL CHECKS SATISFACTORY. 2 L 7 2 4F 4 F RT A16WE E2EA 2007092000148 20070920 00148 NM 2007 9 20 DL76P071179 1 20070905 A 5414 311T3065127 DOOR BOEING 767 767332 1382001 NM NR 2 NACELLE MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1402A 25989 FOUND BY MTC ON DAILY RELIABILITY/WEEKLY CHECK NUMBER 2 ENGINE PYLON INBOARD STRUT DOOR MISSING. AOG PART 311T3065-127 INSTALLED NEW ACCESS PANEL PER MM. 2 L 7 2 4F RT A1NM 2007092000178 20070920 00178 NM 2007 9 20 2007UALA03622 1 20070907 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 326UA 23958 STRINGER CLIP BS 400 STRINGER 27L CRACKED IN CORNER. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED NEW STRINGER CLIP BS 400 STR (HMV) 2 L 7 2 4F 4 F RT A16WE E21EU 2007092000181 20070920 00181 NM 2007 9 20 2007UALA03625 1 20070907 A 2432 CHARGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE APU BATTERY FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 APU BATTERY DOES NOT SHOW ANY CHARGING AFTER STANDBY POWER CHECK. 10-11-07 REPLACED BATTERY CHARGER. SYSTEM SHOWS C HARGING ABILITY. AIRCRAFT OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092000189 20070920 00189 NM 2007 9 20 2007UALA03634 1 20070909 A 2497 WIRE HARNESS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE IDG DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 RIGHT IDG TRIPPED AFTER ENG START, GEN SW RESET, NO HELP. 10-11-07 FOUND BURNED PINS AT FIREWALL CONNECTOR D1292.N P INS B AND C. REPLACED ENGINE POWER FEEDER HARNESS AND PYLON HARNESS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092000191 20070920 00191 NM 2007 9 20 2007UALA03636 1 20070908 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 526UA 24994 EEL LAMP IN FRONT OF MID LAV IS COVERED BY CARPETING AND INOP. 10-11-07 REMOVED CARPET FROM OVER LIGHT ASSEMBLY. MA DE PERMANENT REPAIR TO LIGHT ASSEMBLY POWER LEAD, 2 L 7 2 4F 4 F RT A2NM E17NE 2007092000197 20070920 00197 NM 2007 9 20 QXEA200701384 1 20070904 A 2420 51608003 GCU DHAV DHC8 DHC8202 2809007 NM NR 2 MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 367PH 10263 511 ORH FLIGHT NR 2078, NR 2 AC CAUTION LIGHT WOULD NOT RESET VIA CHECKLIST. REPLACED NR 2 AC GCU, IAW Q200 AMM TASK 24-21- 00-720-801. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007092000205 20070920 00205 NM 2007 9 20 DHL2007746528 1 20070830 A 5343 TRUNNION BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 RIGHT NOSE LANDING GEAR TRUNNION BORE HAS CORROSION. REMOVED CORROSION AND REPAIRED NOSE LANDING GEAR TRUNNION SUPPORT FITTING IAW B727 SRM 51-10-6 AND 53-40-01. NOSE LANDING GEAR OPS/CHECK GOOD IAW B727 MM 32-33-00. 2 L 7 3 4F A3WE 2007092000215 20070920 00215 NM 2007 9 20 DHL2007746523 1 20070825 A 5322 SHEAR TIE BOEING 727 727224 1384076 NM BS 700 S28L/R CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 FORWARD CARGO COMPARTMENT STA 700 FRAME CLIP FROM STR 28LT TO 28RT HAS CORROSION ON AFT SIDE. REMOVED BODY PANEL NR 333 7 LEFT AND 3420 RIGHT, 3437 RIGHT FOR ACCESS IAW B727 SRM 51-30-2. REMOVED SHEAR TIE AT BODY STA 700 STR 28R TO 28L IAW B727 SRM 51-30-2. FABRICATED SHEAR TIE MATERIAL USED 7075T6 0.040" PO NR 9005551 DIMENSION 9 7/8" BY 2" IAW B727 SRM 5 3-10-2 FIG 3, SRM 51-10-3, 51-30-5. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED BODY PANEL NR 3337 LEFT, 3420 R IGHT AND 3437 RIGHT IAW B727 SRM 51-30-2. SHEAR TIE INSTALLED IAW B727 SRM 51-30-02. 2 L 7 3 4F A3WE 2007092000223 20070920 00223 EA 2007 9 20 REXA200700060 1 20070914 A 5524 HST22DU522 FITTING CNDAIR CL600 CL6002B19 1900309 EA ELEVATOR DAMAGED A REXA K NONE O OTHER IN INSP/MAINT 1 SO 25 8938A 7938 LEFT ELEVATOR NR 3 PCU FITTING -LINK ATTACHMENT, LOWER LOCK FASTENER IS SHEARED. REPLACED THE HI-LITE TO LINK ASSY. 2 L 7 2 4F RT A21EA 2007092000225 20070920 00225 NM 2007 9 20 2007UALA03647 1 20070909 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY EXIT CEILING LIGHTS INOP, FROM DOOR 3L THRU 4L. 10-11-07 REPLACED EPSU AND BATT, OP CHECKS OK FOR SERVICE . 2 L 7 4 4F 4 F RT A20WE E24NE 2007092000229 20070920 00229 NM 2007 9 20 AALA20071550 1 20070815 A 2797 CIRCUIT CARD BOEING 767 767223 1385123 NM PROX SENSOR INOPERATIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 323AA 22324 LAX INFLIGHT T003/15AUG - ON APPROACH WHEN SELECTING FLAPS 20 DEGREES THE MASTER CAUTION LIGHT AND LEADING EDGE SLAT ASY MMETRY EICAS MESSAGE ILLUMINATED. LANDED LAX WITHOUT INCIDENT. BITE CHECK OF PROXIMITY SENSOR ELECTRONIC UNIT FOUND FA ULT OF CARDS 001 AND 007. REPLACED CARDS 001 AND 007. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007092000238 20070920 00238 NM 2007 9 20 2007UALA03650 1 20070907 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 648UA 25285 FLIGHT DECK EMERGENCY LIGHT FAILS TO COME ON DURING TEST. 10-11-07 REPLACED EMERGENCY LIGHT ASSY. OP CHECKED OK . 2 L 7 2 4F 4 F RT A1NM E24NE 2007092000239 20070920 00239 EU 2007 9 20 07FDEA03594 1 20070912 A 5420 A54611051200 FITTING AIRBUS 300 A300B4605R 3930308 EU ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 DEEP CHAFING MARK FOUND ON PYLON NR 1SPIGOT FITTING FWD PYLON TO ENGINE MOUNT REPAIR PERFORMED BY BLEND OUT TO ELIMINATE SHARP EDGES IAW EA 6-5451-112496 AND RAS 053455/005/2007 ISS A. 2 L 7 2 4F RT A35EU 2007092000241 20070920 00241 NM 2007 9 20 DHL2007746530 1 20070903 A 5743 BEAM BOEING 727 727224 1384076 NM LT MLG CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 LEFT MAIN LANDING GEAR BEAM AFT MOUNT AREA FOR NR 4 FLAP TRACK, OUTBOARD MOUNT HOLE ELONGATED IN BEAM WITH POSSIBLE CORR OSON INSIDE BORE. ACCOMPLISHED BLEND OUT/REPAIR OF CORROSION AT LWBL 124.2 MAIN LANDING GEAR MATING SURFACE IAW BOEING TELEX 1D NR 1-520795353. 2 L 7 3 4F A3WE 2007092000249 20070920 00249 EA 2007 9 20 SWIA200718675 1 20070716 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 929SW 7703 FS 280 LOWER FLOORBEAM CRACKED AT LBL9, FOUND AT C-CHECK. INSTALLED REPAIR PER REO 601R-53-11-171 AND SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007092000258 20070920 00258 EA 2007 9 20 SWIA200718683 1 20070726 A 5210 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 727SK 10191 PAX DOOR AFT DRAG ANGLE IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO 670-52-11-072. 2 L 7 2 4F RT A21EA 2007092000259 20070920 00259 NM 2007 9 20 P5CA0701532 1 20070903 A 3150 285T0035202 CIRCUIT CARD BOEING 747 74746NF 13848BT NM POWER SUPPLY MALFUNCTIONED A P5CA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 15 452PA 30810 MASTER WARNING AND FIRE BELL CONTINUOUSLY DISPLAYED ACTIVATED WITH NO ASSOCIATED EICAS OR STATUS MESSAGES. RESEATED MAW EA CARDS AND SYSTEM BITE TESTED OK PER AMM 31-51-00-715-014 AS PRECAUTIONARY REPLACE MAWEA PWR SUPPLY CARDS PER MM 31-51 -01 AND C/W MM 31-52-00; OPS SYSTEM FUNCTION TESTED NO FAULTS NOTED. SYSTEM RETURN TO SVC. 2 L 7 4 4F RT A20WE 2007092000263 20070920 00263 NM 2007 9 20 2007UALA03654 1 20070908 A 2420 IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RIGHT LOW A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 590UA 28708 EICAS "R GEN DRIVE" & OVHD "DRIVE" LIGHT CAME ON DURING MOD TURBULENCE. LIGHT WENT OUT AFTER A FEW SEC'S. 10-11-07 SERVICED IDG APPROX 50 PUMPS OF OIL PER UA MANUAL. THIS ACFT IS TO FLY NON ETOPS DUE TO REPEAT ELECTRICAL IDG TRIPPING PROBLEMS ON THE RT ENGINE. ACFT TO REMAIN NON-ETOPS FOR FIVE FLIGHTS TO CONFIRM FIX AND NORMAL OPERATION OF BOTH ENGI NE IDG'S OF OIL UNTIL OVERFLOW. IDG PDI BUTTON NOT POPPED. PRIOR TO CF'G, SERVICED IDG (5 PUMPS) TOOK AIRCRAFT TO RUNU P FOR LONG PACK BURN. REPLACED FUEL OIL COOLER. LEAK CHECKED AND SERVICE IDG TO NORMAL CAPACITY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092000266 20070920 00266 SW 2007 9 20 WGEA200700005 1 20070910 A 5270 PROXIMITY SWITCH ECLIPS EA500 ECLIPSEEA500 3350000 SW DOOR OUT OF ADJUST E WGEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 119DJ 000022 DOOR WARNING LIGHT ILLUMINATED AT TOP OF CLIMB (FL260, CABIN ALT. 3800', ROC -0) 30 MINUTES LATER ON DESCENT UPON REACHI NG 10,000 FT, LIGHT WENT OUT (2500 CABIN ALT AP: 5.4, ROC 0). ADJUSTED AFT DOOR LOCK PROX SWITCH AND COMPLIED WITH DOOR TEST IAW EA500 AMM 52-00-00-071-011. 1 L 7 2 4J RT A00002AC 2007092000267 20070920 00267 NM 2007 9 20 KCSA071355 1 20070911 A 5315 STANCHION BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-1920 LEFT FLOORBEAM STANCHION CRACKED .25 INCH WL-118. 2 L 7 4 4F RT A20WE 2007092000272 20070920 00272 NM 2007 9 20 KCSA071360 1 20070911 A 5322 SHEAR TIE BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-360 SHEAR TIE BETWEEN STR-5L AND STR-6L IS CRACKED .25 INCH. 2 L 7 4 4F RT A20WE 2007092000291 20070920 00291 EA 2007 9 20 TRAX200701313 1 20070905 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 875AS 7559 AAR - LEFT O/B CLIP AT FS 280 AND LBL 9.0 IS CRACKED. REMOVED LEFT O/B CLIP AT FS 280 AND LBL 9.0 AND INSTALLED NEW CLI P P/N 601R31113-57 IAW CRJ 200 SRM 51-42-21. SUPPLEMENTAL - SDR CLOSED 09/12/07. 2 L 7 2 4F RT A21EA 2007092000298 20070920 00298 WP 2007 9 20 ABXA070278 1 20070822 A 5311 99115056 FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 WHILE COMPLYING WITH EA 53300036, FOUND CRACKED FRAME. REPAIRED FRAME IAW DC9 SRM 53-03, FIGURE 34. 2 L 7 2 4F A6WE 2007092000302 20070920 00302 WP 2007 9 20 ABXA070282 1 20070911 A 5230 59101419 PAN DOUG DC9 DC941 302207N WP FWD CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 DURING INSPECTION OF DOOR NEA 52300001-001, FOUND INNER DOOR PAN CRACKED. REPAIRED PAN IAW DC9 SRM 52-05, FIGURE 26A. 2 L 7 2 4F A6WE 2007092000315 20070920 00315 NM 2007 9 20 QXEA200701422 1 20070916 A 6120 697073002 PCU BOMBDR DHC8 DHC8402 1390042 NM NR 2 MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 427QX 15285 839 4156 SEA FLIGHT NR 2348: AFTER CONDITION LEVERS WERE ADVANCED TO MAX DURING ENGINE START, NR 2 PEC CAUTION LIGHT ILLUMINATED AND NR 2 PROP DID NOT GO ABOVE 190. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE REMOVED AND REPLACED NR 2 PCU. PCU RUNS P ASSED POWER ASSURANCE. PASSED LEAK CHECK, GOOD FOR NR 2 ENGINE. NR 2 PEC CAUTION LIGHT DID NOT ILLUMINATE. NO OTHER D EFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007092000324 20070920 00324 SO 2007 9 20 SWIA200718688 1 20070911 A 5753 SKIN EMB 120 EMB120ER 3260203 SO NACELLE FLAP CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 586SW 120354 RIGHT NACELLE FLAP SKIN IS CRACKED. REPLACED RIGHT NACELLE FLAP IAW MM 27-50-03, P/N 120-40327-002. 2 L 7 2 4T RT A31SO 2007092000325 20070920 00325 EA 2007 9 20 SWIA200718689 1 20070910 A 2131 CONTROL PANEL CNDAIR CL600 CL6002D24 1390016 EA CABIN PRESSURE FAULTY A SWIA G O2 MASK DEPLOYED J WARNING INDICATION NR NOT REPORTED 1 NM 07 812SK 15098 "ALT LIMITER" CAUTION MESSAGE, FOLLOWED BY DEPLOYING OF OXYGEN MASKS IN CABIN. REMOVED AND REPLACED CABIN PRESSURE CONT ROL PANEL REF CRJ 900 MM 21-31-04. RESTOWED ALL CABIN OXYGEN MASKS. OPS CHECK OF CPCP GOOD. NO FURTHER DEFECTS NOTED, PN: GG670-98001-11, SN ON: 00488 SN OFF: 80606. 2 L 7 2 4F RT A21EA 2007092000328 20070920 00328 NM 2007 9 20 HALA0700380 1 20070915 A 7720 ELECTRICAL BOX BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE MALFUNCTIONED A HALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, AFTER ENGINE START RIGHT ENGINE EGT DECREASED FROM 435DEG TO 20DEG AND REMAINED AT 20 DEG WHEN THROTTLE ADVANCED. STANDBY INDICATIONS INDICATE SAME CONDX. REPLACED JUNCTION BOX PER AMM 77-21-02-004. REMOVED, INST ALLED AMM-77-21-004. SECURITY CONDITION GOOD. OPS CHECK GOOD. GROUND OPS CHECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092000332 20070920 00332 NM 2007 9 20 07FDEA03629 1 20070912 A 5710 6521656 SUPPORT BEAM BOEING 727 727233 138408A NM ZONE 600 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 RT WING SPOILER SUPPORT BEAM LOWER CHORD ANGLE I/B OF NR 5 FLAP TRACK HAS INCORRECT REPAIR INSTALLED REF DWG SR 27-57- 038. REMOVED T/E PANELS, REPAIRED LOWER CHORD ANGLES IB OF NR 5 FLAP TRACK. REINSTALLED T/E PANELS REF SRM 51-30-2 PG 4, 3 AND 2, AND FED EX DWG SR 27-57-038. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007092000353 20070920 00353 EU 2007 9 20 Y2LA200700003 1 20070911 A 2120 UNKNOWN AIRBUS A319 A319112 3930323 EU CABIN ODOR A Y2LA D RETURN TO BLOCK J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 553SX 3171 WHILE STARTING ENG 1 AFTER ENG 2 START ECAM GAVE VENT AVNCS SYST FAULT. STARTED TO TROUBLESHOOT AND WERE PULLING FCOM U P, FLIGHT ATTENDANTS IN AFT REPORTED SMELLING SMOKE. FIRE DEPARTMENT RESPONDED AND PASSENGERS WERE DE-PLANED VIA L1 AND L2 BY AIRSTAIRS. 2 L 7 2 4F RT A28NM 2007092000362 20070920 00362 NM 2007 9 20 KCSA071371 1 20070912 A 5330 SKIN BOEING 747 7472B4B 138481B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA-760 STR-26L HAS SKIN DAMAGED. 2 L 7 4 4F RT A20WE 2007092000365 20070920 00365 SO 2007 9 20 C2XA07TY050 1 20070912 A 5320 14522460013 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16525 145403 TYS - DURING A CURRENT C-CHECK THE CENTER OMEGA BEAM WAS FOUND CORRODED FROM FR 18 TO FR 22. MAINTENANCE REMOVED AND RE PLACED THE CENTER OMEGA BEAM IAW EMB SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHE CK. 2 L 7 2 4F RT T00011AT 2007092000366 20070920 00366 NM 2007 9 20 CALA0700513 1 20070912 A 5320 6546881128 STRAP BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A .5 INCH CRACK IN STRAP ON RT SIDE OF FUSELAGE AT STA 1156, S13R BELOW HORIZONTAL STABILIZER. THE STR AP WAS REPAIRED IAW ECRA 5331-01344. 2 L 7 2 4F RT A16WE 2007092000369 20070920 00369 EA 2007 9 20 TRAX200701303 1 20070904 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 875AS 7559 AAR - FS 280 AFT FLOOR ANGLE 600-34017-595 IS CRACKED AT LBL 9.0 AND RBL 9.0. COMPLIED WITH REO 601R-53-11-136. 14031 9 -8-07. REPAIRED J-ANGLE ON THE PILOT'S BULKHEAD AT FS 280.0 FROM LBL 9.0 TO RBL 9.0 IAW ASA EO 600-53-0091. SUPPLEMENT AL - SDR CLOSED 09/14/07. 2 L 7 2 4F RT A21EA 2007092000371 20070920 00371 EA 2007 9 20 TRAX200701307 1 20070904 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 875AS 7559 AAR - FS 280 BULKHEAD HAS CRACK AT RBL 12.0 JUST ABOVE LOWER ANGLE RADIUS. COMPLIED WITH REO 601R-53-11-171. REPAIRED PILOTS BULKHEAD AT FS 280 FROM LBL 9.0 TO RBL 9.0 IAW ASA EO 600-53-0090. 13341. SUPPLEMENTAL - SDR CLOSED 09/14/07. 2 L 7 2 4F RT A21EA 2007092000372 20070920 00372 EA 2007 9 20 TRAX200701325 1 20070905 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 834AS 7254 AAR - FLOOR SUPPORT ANGLE AFT OF FS 280 O/B OF RBL 9 IS CRACKED. REFERENCE ROUTINE 50186/2000/0022 FOR CORRECTIVE ACTIO N. 14211 9-11-07. SUPPLEMENTAL - SDR CLOSED 09/14/07. 2 L 7 2 4F RT A21EA 2007092000378 20070920 00378 WP 2007 9 20 ABXA070293 1 20070815 A 5230 5912494501 PAN DOUG DC9 DC941 302207N WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 CRACKS EMANATING FROM REPAIR DOUBLERS TO EDGE OF PART ON FORWARD LOWER CARGO DOOR PAN AT ENDS OF NR 3 AND NR 4 BEAMS. R EPAIRED FORWARD END OF BEAMS NR 3 AND NR 4 IAW DC9 SRM 52-05, FIGURE 50. AFT END OF NR 2 AND NR 3 BEAMS WERE PREVIOUSLY COMPLIED WITH IAW DC9 SRM 52-05, FIGURE 50. 2 L 7 2 4F A6WE 2007092000382 20070920 00382 WP 2007 9 20 ABXA070292 1 20070814 A 5311 59135956 FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 FRAME CRACKED AT FASTENER AT FS 1152 AT LONGERON 19 RIGHT. REMOVED AND REPLACED LOWER FRAME SECTION IAW DC9 SRM 51-30-5 . 2 L 7 2 4F A6WE 2007092000384 20070920 00384 EA 2007 9 20 TRAX200701336 1 20070910 A 5330 STRAP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 834AS 7254 AAR - RIGHT FS 640 STR 8-13 SKIN BUTT JOINT STRAP IS CRACKED. COMPLIED WITH EC/TC REO 601R-53-61-506, 2 L 7 2 4F RT A21EA 2007092000385 20070920 00385 EA 2007 9 20 TRAX200701337 1 20070910 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 834AS 7254 PAX DOOR FORWARD COUNTER BALANCE ANCHOR FITTING IS CRACKED. 10-18-07 REMOVED FORWARD COUNTER BALANCE ANCHOR FITTIN G IAW CRJ 200 AMM 52-11-17. OK TO INSTALL NEW SERVICEABLE FORWARD COUNTER BALANCE ON COTTER FITTING INSTALLED NEW SERVIC EABLE FORWARD COUNTER BALANCE ANCHOR FITTING IAW CRJ 200 AMM 52-11-17. SN 1047, ANCHOR FITTING UPPER ADJUSTMENT BOLT REQ UIRES INSTALLATION ORDERED AGAINST WC 8000-0003. INSTALLED ANCHOR FITTING BOLTS IAW CRJ 200 AMM 52-11-17, REQUIRES AD JUSTMENT. CHECKED ADJUSTMENT AND RIG IAW CRJ 200 AMM 52-11-17. RIG AND ADJUSTMENT CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2007092000393 20070920 00393 NM 2007 9 20 SWAA074549 1 20070911 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092000395 20070920 00395 NM 2007 9 20 SWAA074542 1 20070911 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED A1 CHECK, FOUND RIGHT WING NR 4 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SWA EA. 2 L 7 2 4F RT A16WE 2007092000397 20070920 00397 NM 2007 9 20 SWAA074529 1 20070911 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092000398 20070920 00398 NM 2007 9 20 SWAA074526 1 20070911 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092000400 20070920 00400 NM 2007 9 20 SWAA074528 1 20070911 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092000403 20070920 00403 NM 2007 9 20 SWAA074533 1 20070911 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092000404 20070920 00404 NM 2007 9 20 SWAA074535 1 20070911 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092100001 20070921 00001 EU 2007 9 21 07FDEA03877 1 20070918 A 5315 A53978476200 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 HEAVY CORROSION ON CROSSBEAM AT FRAME 61 RT, CARGO COMPARTMENT FLOOR STRUCTURE, CARGO DOOR AREA. REPLACEMENT OF CROSS BEAM IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100002 20070921 00002 EU 2007 9 21 AALA20071673 1 20070901 A 2782 ACTUATOR AIRBUS 300 A300B4605R 3930308 EU SLATS INOPERATIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 70074 517 JFK INFLIGHT T2110/01SEP, SLATS SYSTEM ONE AND TWO FAULTED DURING APPROACH. LANDED WITH NO SLATS WITHOUT INCIDENT. REP LACED NUMBER THREE LEFT ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007092100005 20070921 00005 NM 2007 9 21 AALA20071696 1 20070906 A 2910 HOSE BOEING 757 757223 1384957 NM HYD SYSTEM DAMAGED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 645AA 24603 JFK TEST FLIGHT T9640/06SEP - AFTER TAKEOFF CREW REPORTED MAIN LANDING GEAR UNSAFE LIGHT. FOLLOWED BY LEFT SYSTEM HYDR AULIC LOSS. LANDED JFK WITHOUT INCIDENT. AFTER LANDING RIGHT GEAR DOOR WAS EXTENDED AND WHEEL WELL WAS SATURATED WITH HYDRAULIC FLUID. FOUND FLEX LINE TO RIGHT MAIN LANDING GEAR DOOR ACTUATOR WITH HOLE IN LINE. REPLACED HOSE. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092100006 20070921 00006 NM 2007 9 21 AALA20071694 1 20070906 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 192AN 32386 BOS - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT N UMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092100008 20070921 00008 NM 2007 9 21 AALA20071685 1 20070903 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 690AA 25696 DFW - EMERGENCY LIGHT AT FORWARD LEFT OVERWING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT FORWARD LEFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092100015 20070921 00015 EU 2007 9 21 AALA20071680 1 20070903 A 7930 21SN04334 PRESSURE SWITCH AIRBUS 300 A300B4605R 3930308 EU ENGINE INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 59081 639 JFK INFLIGHT T1781/03SEP DURING CLIMB CREW RECEIVED NUMBER ONE ENGINE OIL CLOG INDICATION FOLLOWED BY NUMBER TWO ENGINE OIL CLOG INDICATION. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE AND NUMBER TWO ENGINE OIL SCAVE NGE FILTER DIFFERENTIAL PRESSURE SWITCHES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007092100017 20070921 00017 EU 2007 9 21 07FDEA03879 1 20070918 A 5320 A25573781008 PROFILE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 HEAVY CORROSION ON WEDGE PROFILE AT FRAME 63 BETWEEN STRG 37-41 LT, REPLACEMENT OF WEDGE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100022 20070921 00022 EU 2007 9 21 07FDEA03885 1 20070918 A 5712 RIB AIRBUS 310 A310324 3930206 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND DAMAGE (NICK) ON RT WING TRAILING EDGE AILERON HINGE RIB, WITH MINIMUM REMAINING THICKNESS OF 2,2MM. REPAIR PERFO RMED BY BLEND OUT DAMAGE, HFEC INSPECTION AND FLAP PEENING IAW EA 6-5751-81123 AND RAS/BAE/1272/2004 ISSUE A. 2 L 7 2 4F RT A35EU 2007092100023 20070921 00023 NM 2007 9 21 07FDEA03886 1 20070918 A 5753 STOP FITTING DOUG MD11 MD11F 3023600 NM LT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 LEFT WING OUTBOARD FLAP SECONDARY UPSTOP FITTING FOUND CRACKED. 10-04-07 REMOVED AND REPLACED AS PER SRM 51-33-01 V OLUME II. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007092100024 20070921 00024 EU 2007 9 21 07FDEA03887 1 20070918 A 5712 RIB AIRBUS 310 A310324 3930206 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND DAMAGE (NICK) ON RT WING TRAILING EDGE AILERON HINGE RIB (INBOARD), WITH A MINIMUM REMAINING THICKNESS OF 1,7MM (N OMINAL 2,3MM). REPAIR PERFORMED BY BLEND OUT DAMAGE, HFEC INSPECTION AND FLAP PEENING IAW EA 6- 5751-81123 AND RAS/BAE /1272/2004 ISSUE A. 2 L 7 2 4F RT A35EU 2007092100026 20070921 00026 EU 2007 9 21 07FDEA03889 1 20070918 A 5410 A54611750 SPAR AIRBUS 310 A310324 3930206 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 CORROSION FOUND ON THE UPPER SURFACE OF THE LT PYLON LOWER SPAR BETWEEN RIBS 4-8, FURTHER TO HYDRAULIC FLUID CONTAMINATI ON. REPAIR PERFORMED BY BLENDING OUT CORROSION, CUTTING OUT THE MOST DAMAGED AREAS AND INSTALLING A DOUBLER TO REINFO RCE THE AREA IAW EA 6-5451-81096 AND RAS 034151/024/2004 ISSUE A. 2 L 7 2 4F RT A35EU 2007092100029 20070921 00029 EU 2007 9 21 07FDEA03797 1 20070825 A 5330 SKIN AIRBUS 310 A310222 3930315 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 PREVIOUS REPAIR FOUND LOCATED ON RT FUSELAGE BELOW AFT CARGO DOOR AT STA 3302/3355, BETWEEN STRG 45-48 RT. REPAIR REQUI RES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. THE REPAIR WAS EVALUATED AND FOUND NOT TO CONFORM TO EXISTING FEDEX EA 6-5330-87763. NEW REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH F EDEX EA 6-5330-87763. 2 L 7 2 4F RT A35EU 2007092100030 20070921 00030 NM 2007 9 21 07FDEA03799 1 20070915 A 2697 50086003 CIRCUIT BREAKER BOEING 727 7272S2F 1384O81 NM FAILED A FDEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 217FE 22938 IN CRUISE SMELL OF SMOKE AND THE SIGHT OF SMOKE COMING FROM BACK OF S/O PANEL. SMOKE MOVED TOWARD F/O SEAT. THE SMELL WAS LIKE CAR EXHAUST. RAN ALL FUMES AND ODORS CHECK LIST. ALSO SHUT OFF GASPER FAN. THE SMOKE ONLY LASTED FOR AROUND 15 SEC. NO OTHER INDICATIONS. REPLACED APU C/B REF MM 24-20-041-4. REINSTALLED ALL REMOVED ITEMS FROM F/E PANEL REF ESP MM 20-46-50 AFTER VACUUMING DEBRIS AND DUST. RAN ALL THREE ENG'S, OPS CK'D ALL REMOVED ITEMS. OPERATED PACKS AND GASPER, CK'D ALL PANEL LTS AND TRANSFORMERS. NO ABNORMALITIES NOTED. CLEANED WIRES AND TERMINALS TO C/B. REMOVED IDE NT MASKING TAPE. INSPECTED AREA FOR OTHER ARCING OR WATER DAMAGE. ALL OK. 2 L 7 3 4F A3WE 2007092100033 20070921 00033 NM 2007 9 21 07FDEA03802 1 20070916 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 588FE 48490 CENTER LANDING GEAR RIGHT MOUNTING. TRUNNION FITTING FORWARD AND AFT HOLE FOUND WITH CORROSION. 10-01-07 COMPLIED WITH FEDEX E.A. 1-5310-115190. CLASSIFIED AS A MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007092100034 20070921 00034 EU 2007 9 21 07FDEA03803 1 20070917 A 5347 A53612518200 SEAT TRACK AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 HEAVY CORROSION ON SEAT TRACK BETWEEN FRAME 14-19, Y-450 RT. REPLACEMENT OF SEAT TRACK IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100039 20070921 00039 EU 2007 9 21 07FDEA03808 1 20070917 A 5320 A53986774206 WEB AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 DAMAGED WEB PLATES BETWEEN FRAME 86-87, STRG 23 LT. REPLACMENT OF WEB PLATE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100040 20070921 00040 EU 2007 9 21 07FDEA03809 1 20070917 A 5520 A55276671 WEDGE AIRBUS 310 A310324 3930206 EU RT ELEVATOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND CORROSION ON RT ELEVATOR TRAILING EDGE WEDGE, BETWEEN RIB ER12-ER28. REPAIR OF ELEVATOR TRAILING EDGE WEDGE IAW S RM 55-21-11/CONFIG 2/PG 1-3. 2 L 7 2 4F RT A35EU 2007092100041 20070921 00041 EU 2007 9 21 07FDEA03810 1 20070917 A 5320 A53778329209 PLATE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 CORRODED SHEARPLATES AT FWD CARGO COMPARTMENT BETWEEN FRAME 36-37 AND FRAME 38.1-38.2 RT, STRG 43-44. REPLACEMENT OF SH EAR PLATES IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100042 20070921 00042 EU 2007 9 21 07FDEA03811 1 20070917 A 5320 A53778423207 PLATE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 CORRODED SHEAR PLATES AT FWD CARGO COMPARTMENT BETWEEN FRAME 38.2-39, STRG 43-44 LT AND RT. REPLACEMENT OF SHEAR PLATES IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100046 20070921 00046 WP 2007 9 21 07FDEA03816 1 20070917 A 5712 ARB1298505 RIB DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 RT WING L/E INT STRUCTURE FOUND CRACK ON RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I. 2 L 7 3 4F A22WE 2007092100047 20070921 00047 EU 2007 9 21 07FDEA03817 1 20070917 A 5320 A53978259202 ANGLE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 CORRODED COUPLING ANGLE AT FRAME 69, STRINGER 49-51 RHS. REPLACEMENT OF COUPLING ANGLE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100048 20070921 00048 WP 2007 9 21 07FDEA03818 1 20070917 A 5310 NCA604465 STRUCTURE DOUG DC10 DC1010F 3022111 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 FWD CARGO COMPT BILGE AREA HAS CRACK ON CAP TEE OF BULKHEAD. REPAIRED AREA IAW EA 8-5310-99388. 2 L 7 3 4F A22WE 2007092100049 20070921 00049 EU 2007 9 21 07FDEA03819 1 20070917 A 5313 A25572173202 LONGERON AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 CORROSION ON LONGITUDINAL PROFILE AT BULC CARGO COMPARTMENT FLOOR STRUCTURE BETWEEN FRAME 67-69, STRG 45-47 RT. REPLA CEMENT OF LONGITUDINAL PROFILE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100050 20070921 00050 WP 2007 9 21 07FDEA03820 1 20070917 A 5311 AFA00313 FRAME DOUG DC10 DC1010 3022110 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 MAIN CABIN STRUCTURE HAS CRACK ON FRAME. REPAIRED FRAME IAW SRM 53-30-00 FIG 5 VOL I. 2 L 7 3 4F A22WE 2007092100051 20070921 00051 WP 2007 9 21 07FDEA03821 1 20070917 A 5320 ABA720323 MEMBRANE DOUG DC10 DC1010 3022110 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 COCKPIT INT AFTER REMOVAL FLOOR PANEL WITH OAN J/C MD10-0600C210-1JR FOUND SEVERE CORROSION ON 2 HORIZ MEMBRANE: FROM STA 303 TO STA 330 FROM X= 7.50 TO X=17 LT SIDE; FROM STA 303 TO STA 330 FROM X= 27 TO X= 60 LT SIDE. THE FIRST CASE RE PLACED MEMBRANE IAW SRM 51-35-01 PAR 1-5 VOL II. THE SECOND CASE REPAIRED MEMBRANE IAW SRM 53-00-01 FIG 10 VOL I. 2 L 7 3 4F A22WE 2007092100053 20070921 00053 EU 2007 9 21 07FDEA03823 1 20070917 A 5320 PROFILE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 HEAVY CORROSION ON LONGITUDINAL PROFILE AT BULK CARGO COMP FLOOR STRUCTURE BETWEEN FRAME 64-67, Y-805, RT. REPLACEMENT OF LONGITUDINAL PROFILE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100065 20070921 00065 NM 2007 9 21 AALA20071652 1 20070830 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 387AM 27184 DFW - EMERGENCY LIGHT AT SEAT 5B INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 5B. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007092100066 20070921 00066 WP 2007 9 21 AALA20071662 1 20070831 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 461AA 49566 LGA - EMERGENCY LIGHTS AT TAIL CONE INOPERATIVE. CLEANED CORROSION ON BATTERY PACK FOR EMERGENCY LIGHTS AT TAIL CONE. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007092100067 20070921 00067 WP 2007 9 21 AALA20071663 1 20070901 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 461AA 49566 LGA - EMERGENCY LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD BIN SEAT 25DEF FOR EMERGENCY LIGHTS AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007092100068 20070921 00068 NM 2007 9 21 AALA20071664 1 20070901 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 619AA 24577 MIA - EMERGENCY LIGHT AT SEAT 35D INOPERATIVE. SECURED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 35D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092100071 20070921 00071 EU 2007 9 21 07FDEA03778 1 20070914 A 5313 A53811523 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 HEAVY CORROSION ON THE FLANGE OF STRINGER 51 RT, BETWEEN FRAME 45-46, REMAINING THICKNESS AFTER BLENDING IS OUT OF LIMIT . REPAIR PERFORMED BY CUTTING OUT DAMAGED PART AND INSTALLING A REPAIR ANGLE (4 MM THICK) IAW EA 6-5318-81086 AND RAS 0 34265/005/2004 ISSUE A. 2 L 7 2 4F RT A35EU 2007092100072 20070921 00072 EU 2007 9 21 07FDEA03779 1 20070914 A 5313 A53778392206 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 CORROSION ON STRINGER 51, BETWEEN FRAME 36-37 LT, AFTER BLENDING IS THE REMAINING THICKNESS OUT OF LIMIT IAW SRM 53-10 -00. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007092100073 20070921 00073 EU 2007 9 21 07FDEA03780 1 20070914 A 5310 A53973085 BEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 SEVERAL CORRODED AREAS ON SILLBEAM OF AFT CARGO COMPARTMENT CUT OUT. REPAIR PERFORMED BY REPLACEMENT BY INSTALLING AIRF RAME AND HARDWARE KIT: SR5317-99A00500 AND SR5317-99H01200 IAW SRM 53-17-18/FIG 207 / TB. 203. DEVIATIONS FROM SRM 53-1 7-18/FIG 207. INSTALLING SOME FASTENERS AT FRAME 61 AND 63) COVERED BY EA 6-5317-81082 AND RAS/DATLS/0002249/2004 ISSUE A (NON ROUTINE DR334). 2 L 7 2 4F RT A35EU 2007092100074 20070921 00074 EU 2007 9 21 07FDEA03781 1 20070914 A 5315 A53973509208 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 HEAVY CORROSION ON CROSSBEAM FRAME 60 LT, CARGO COMPARTMENT FLOOR STRUCTURE. SPLICE REPAIR AT CROSSBEAM PERFORMED IAW SRM 53-10-15/FIG 207. 2 L 7 2 4F RT A35EU 2007092100075 20070921 00075 EU 2007 9 21 07FDEA03782 1 20070914 A 5315 A53974219220 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 CORROSION ON CROSSBEAM AT FRAME 63 LT, CARGO COMPARTMENT FLOOR STRUCTURE. CROSSBEAM SPLICE REPAIR PERFORMED IAW SRM 53- 10-15/FIG 207. 2 L 7 2 4F RT A35EU 2007092100077 20070921 00077 EU 2007 9 21 07FDEA03784 1 20070914 A 5320 A53974242200 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 CORRODED FITTING AT FRAME 63, STRG 44 LT OF CARGO COMPARTMENT FLOOR STRUCTURE. REPAIR PERFORMED BY REPLACEMENT OF FITTI NG IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100081 20070921 00081 EU 2007 9 21 07FDEA03788 1 20070914 A 5311 A538737200 FRAME AIRBUS 310 A310222 3930315 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 446FE 224 FRAME CRACKED IN FASTENER HOLE AT FRAME 43A LOWER HOLE COMMON TO CRUCIFORM FITTING LT SIDE SEE JOB CARD 41X5271ALI FROM CABIN SIDE 1ST LAYER RUNNING IN THE 5 O`CLOCK DIRECTION .075 DEEP AND RUNNING TO THE 2ND LAYER 100 PERCENT ON SCREEN AMP LITUDE REMOVED AND REPLACED FRAME FITTING P/N A538-70037-200 IAW A310 SRM 51-40-02. 2 L 7 2 4F RT A35EU 2007092100084 20070921 00084 NM 2007 9 21 07FDEA03791 1 20070914 A 5740 6521655 BRACKET BOEING 727 727233 138408A NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 LT WING T/E PANEL BRACKET IS CRACKED, 2 EA. PLACES ABOVE AND JUST INBOARD OF THE NR 7 SPOILER ACTUATOR REPLACED PANEL BR ACKET AS PER SRM 51-30-02, AT WBL 71 TO 153, LT. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007092100086 20070921 00086 NM 2007 9 21 07FDEA03793 1 20070914 A 5740 112N7011 FITTING BOEING 757 7572B7 1384964 NM ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 LEFT WING DIAGONAL BRACE ATTACH FITTING (WING SIDE) HAS MIGRATING BUSHINGS. REMOVED, FABRICATED AND REPLACED MIGRATED B USHINGS IN ACCORDANCE WITH FEDEX EA NR F-5720-110765, DATED 7/30/2007 AND MAE TRAVELER NR T7/695654. CLASSIFIED AS A "M AJOR REPAIR" WITH NO FOLLOW UP ACTIONS REQUIRED. 2 L 7 2 4F RT A2NM 2007092100089 20070921 00089 EU 2007 9 21 07FDEA03858 1 20070917 A 5320 A53973173234 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 HEAVY CORROSION ON CLIP AT FRAME 60, BETWEEN STRG 55-56 LT. REPLACEMENT OF CLIP IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100090 20070921 00090 EU 2007 9 21 07FDEA03859 1 20070917 A 5320 A53973172234 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 HEAVY CORROSION ON CLIP AT FRAME 71, BETWEEN STRG 55-56 LT. REPLACEMENT OF CLIP IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100092 20070921 00092 EU 2007 9 21 07FDEA03861 1 20070917 A 5320 A53973183234 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 HEAVY CORROSION ON CLIP AT FRAME 70, BETWEEN STRG 55-56 LT. REPLACEMENT OF CLIP IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100095 20070921 00095 EU 2007 9 21 07FDEA03864 1 20070917 A 5313 A53974202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 HEAVY CORROSION ON FOLLOWING STRINGER RT, STRINGER 48 BETWEEN FRAME 55/58-63, STRINGER 49 BETWEEN FRAME 55/58-63, STRING ER 50 BETWEEN FRAME 55/58-61, STRINGER 51 BETWEEN FRAME 55/58-65, STRINGER 52 BETWEEN FRAME 55/58-65, STRINGER 53 BETWEE N FRAME 55/58-63, STRINGER 54 BETWEEN FRAME 55/58-67 AND STRINGER 55 BETWEEN FRAME 55/58-61. STRINGER SPLICE REPAIRS PE RFORMED IAW SRM 53-10-14/ FIG 201. 2 L 7 2 4F RT A35EU 2007092100096 20070921 00096 EU 2007 9 21 07FDEA03865 1 20070917 A 5313 A53974202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 HEAVY CORROSION ON FOLLOWING STRINGER LT, STRINGER 46 BETWEEN FRAME 55/58-65, STRINGER 50 BETWEEN FRAME 55/58-65, STRIN GER 51 BETWEEN FRAME 55/58-65, STRINGER 52 BETWEEN FRAME 55/58-65 AND STRINGER 53 BETWEEN FRAME 55/58-61. STRINGER SPL ICE REPAIRS PERFORMED IAW SRM 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007092100100 20070921 00100 EU 2007 9 21 07FDEA03871 1 20070827 A 5730 A57245109 PANEL AIRBUS 310 A310222 3930315 EU ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 PREVIOUS REPAIR FOUND LOCATED ON RT WING LOWER SURFACE T/E, STA 1787/1835, RIB 29-30. REPAIR REQUIRES EVALUATION FOR MA JOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUS REPAIR EVALUATED AND FOUND DEBONDED. RT WING T/E LOWER SURFACE WAS REPAIRED IAW FEDEX EA 6-5710-113165. 2 L 7 2 4F RT A35EU 2007092100101 20070921 00101 NM 2007 9 21 07FDEA03872 1 20070917 A 5315 BAC1518338 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 "PREVIOUS REPAIR'" FLOORBEAM AT STA 620, RBL 29-42 HAS CORROSION ON UNDERSIDE FROM AREA NOT TREATED AND PRIMED. REMOVED DAMAGED PORTION OF UPPER FLOORBEAM AT STA 620, RBL 29-42. FABRICATED AND INSTALLED UPPER CAP REPAIR. REF FED EX EA NR 7-5310-113099, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007092100102 20070921 00102 NM 2007 9 21 07FDEA03873 1 20070917 A 5720 6516216171 SUPPORT BEAM BOEING 727 727233 138408A NM ZONE 500 INOPERATIVE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 LT WING SPOILER SUPPORT BEAM LOWER CHORD ANGLE I/B OF NR 4 FLAP TRACK HAS INCORRECT REPAIR INSTALLED REF SR-27-57-038. REMOVED AND REINSTALLED LOWER WING T/E PANELS, REMOVED EXISTING DOUBLER. REMOVED AND REINSTALLED NR 4 SPOILER ACTUAT OR MOUNT, FLAP TORQUE TUBE, SPOILER LINKAGE AND CASTING. FABRICATED WEB DOUBLER AND CHORD REPAIR ANGLES. CUT OUT CHORD DRILLED UP REPLACEMENT CHORD REPAIR ANGLES AND WEB REPAIR DOUBLER. TREATED AND PRIMED ALL REPAIR PARTS REF SRM 51-10-2 . INSTALLED REPAIR ANGLES AND CHORD, DOUBLER ON WEB, REF SR27-57-038. 2 L 7 3 4F RT A3WE 2007092100104 20070921 00104 EU 2007 9 21 07FDEA03672 1 20070913 A 5415 A54611752 PANEL AIRBUS 310 A310203 3930313 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND CRACK ON PYLON NR 2 AT RIB 8 INBOARD AND OUTBOARD SIDE AT PANEL (ABOUT 8MM) DOUBLER REPAIR ON SIDEWALL PANELS PERF ORMED IAW SRM 5451-31 FIG 201. 2 L 7 2 4F RT A35EU 2007092100107 20070921 00107 NM 2007 9 21 AALA20071666 1 20070901 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 681AA 25338 MIA - EMERGENCY LIGHT AT SEAT ROW 2E INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 2E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092100109 20070921 00109 WP 2007 9 21 AALA20071668 1 20070901 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 409AA 49320 LGA - EMERGENCY LIGHT AT SEAT ROW 25 INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 25. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007092100111 20070921 00111 NM 2007 9 21 AALA20071670 1 20070901 A 3397 WIRE BOEING 767 767323 1385205 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 377AN 25446 LAX - EMERGENCY LIGHT AT AFT LEFT OVERWING EXIT SIGN INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHT AT AFT LEFT OVERW ING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007092100112 20070921 00112 EU 2007 9 21 07FDEA03875 1 20070918 A 5320 A53980210207 WEB AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 CRACKED SHEAR WEB BETWEEN FRAME 74-75, STRG 26 RT. REPLACEMENT OF SHEAR WEB IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100113 20070921 00113 CE 2007 9 21 DXTA200702435 1 20070829 A 7603 C805975 THROTTLE CABLE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE ENGINE BINDING E DXTA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 344QS 10919 5600344 PCEJC0232 DURING SPEEDBRAKE TEST, LT ENGINE POWER LEVER WAS ADVANCED AND BROUGHT TO IDLE STOP. LT ENGINE FLAMEOUT. LT ENGINE WOULD NOT RESTART. LARGE PUDDLE OF FUEL FORMED UNDERNEATH LT ENGINE. REMOVED AND REPLACED ALL FOUR THROTTLE CABLES. 2 L 7 2 4F 4 F RT A22CE E25EA 2007092100114 20070921 00114 NM 2007 9 21 AALA20071675 1 20070902 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 368AA 25195 ORD - EMERGENCY LIGHT AT SEAT 23B HAS BROKEN LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007092100115 20070921 00115 WP 2007 9 21 AALA20071683 1 20070903 A 3350 P4010021000 BATTERY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9618A 53565 SFO - EMERGENCY FLASH LIGHT AT AFT CABIN INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASH LIGHT AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007092100116 20070921 00116 NM 2007 9 21 AALA20071691 1 20070905 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 784AN 29588 JFK - EMERGENCY LIGHT AT SEAT 25C HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007092100117 20070921 00117 NM 2007 9 21 AALA20071677 1 20070902 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 383AN 26995 DFW - EMERGENCY LIGHT AT SEAT 34H HAS MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 34H. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007092100118 20070921 00118 NM 2007 9 21 AALA20071684 1 20070903 A 2560 P4010021000 BATTERY BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39365 24046 SFO - EMERGENCY FLASH LIGHT AT LEFT AFT FLIGHT ATTENDANT BULKHEAD JUMPSEAT INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASH LIGHT AT LEFT AFT FLIGHT ATTENDANT BULKHEAD JUMPSEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007092100119 20070921 00119 NM 2007 9 21 AALA20071690 1 20070905 A 3350 OL3071BPEGPL BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 JFK - EMERGENCY LIGHT AT SEAT 25C HAS BROKEN LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007092100120 20070921 00120 NE 2007 9 21 AALA20071681 2 20070903 A 7320 GENERATOR BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 655AA 24613 31593 MIA INFLIGHT T687/03SEP - RIGHT ENGINE SPEED CARD STATUS MESSAGE ILLUMINATED. RIGHT CENTER FUEL LOW PRESSURE AND RIGHT N3 FLUCTUATING 60 TO 80 WITH RIGHT ENGINE BLEED OFF LIGHT. REPLACED N2 SPEED CARD AND N3 TACH GENERATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2007092100121 20070921 00121 NM 2007 9 21 AALA20071679 1 20070902 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 607AM 27058 MIA - EMERGENCY LIGHT AT SEAT 10D INOPERATIVE. REPAIRED PIN ON CONNECTOR FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092100122 20070921 00122 NM 2007 9 21 AALA20071676 1 20070902 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 368AA 25195 ORD - EMERGENCY LIGHT AT SEAT 23B HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23B. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007092100131 20070921 00131 NM 2007 9 21 AALA20071713 1 20070909 A 3397 CONNECTOR BOEING 767 767223 1385123 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 335AA 22333 LAX - EMERGENCY LIGHT AT SEAT 28H INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 28H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007092100132 20070921 00132 NM 2007 9 21 AALA20071705 1 20070908 A 2823 SHUTOFF VALVE BOEING 737 737823 13844BZ NM FUEL SYSTEM INOPERATIVE A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 937AN 30082 DTW INFLIGHT T873/08SEP - TOWER REPORTED FLUID LEAK FROM LEFT WING AT TAKEOFF. RETURNED TO DTW AND LANDED WITHOUT INCID ENT. FOUND FUEL LEAK FROM LEFT WING TIP DUE TO FUEL SCAVENGE SYSTEM INOPERATIVE WITH VALVE OPEN. REPLACED FLOAT OPERAT ED SHUTOFF VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092100133 20070921 00133 NM 2007 9 21 AALA20071698 1 20070906 A 5610 WINDOW BOEING 757 757223 1384957 NM COCKPIT CRACKED A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 640A 24598 ORD INFLIGHT T2242/06SEP - RIGHT FORWARD WINDOW HEAT FAILED. TURNED OFF POWER TO WINDOW HEAT AND SECONDS LATER FIRST OF FICERS WINDOW DEVELOPED LARGE CRACK. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED FIRST OFFICERS NUMBER ONE W INDOW. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092100134 20070921 00134 NM 2007 9 21 AALA20071699 1 20070906 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 383AN 26995 MIA - EMERGENCY LIGHT AT SEAT 3B MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 3B. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A1NM 2007092100135 20070921 00135 WP 2007 9 21 AALA20071697 1 20070906 A 2612 FIRE DETECTOR DOUG DC9 DC983 3022083 WP CARGO BAY SHORTED A AALA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 21 9401W 53137 RDU INFLIGHT T1702/06SEP - AFT CARGO FIRE INDICATION ILLUMINATED AT 35000 FEET. CREW FIRED BOTTLES BUT INDICATION WOULD NOT EXTINGUISH. LANDED RDU WITHOUT INCIDENT. FOUND AFT CARGO COMPARTMENT FIRE DETECTION ELECTRONICS UNIT SHORTED AND INOPERATIVE DUE TO LEAKAGE FROM AFT GALLEY LEAKING COFFEE MAKER AND CLOGGED DRAIN. REPLACED COFFEE MAKER, CLEARED DRAIN , REPLACED AFT CARGO COMPARTMENT FIRE DETECTION ELECTRONICS UNIT AND BOTH AFT CARGO FIRE EXTINGUISHERS. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007092100136 20070921 00136 NM 2007 9 21 AALA20071700 1 20070906 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 383AN 26995 MIA - EMERGENCY LIGHT AT SEAT 26B BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 26B. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007092100137 20070921 00137 EU 2007 9 21 07FDEA03876 1 20070918 A 5315 A53978254204 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 HEAVY CORROSION ON CROSSBEAM AT FRAME 65 RT, CARGO COMPARTMENT FLOOR STRUCTURE, CARGO DOOR AREA. REPLACEMENT OF CROSS BEAM IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092100138 20070921 00138 NM 2007 9 21 AALA20071647 1 20070829 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 188AN 32382 SFO - EMERGENCY LIGHT AT OVERHEAD LEFT OVERWING EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK M10614 FOR EMERGENCY LIGHT AT OVERHEAD LEFT OVERWING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092100139 20070921 00139 WP 2007 9 21 AALA20071648 1 20070830 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 555AN 53085 LGA - EMERGENCY LIGHT AT OVERHEAD FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007092100140 20070921 00140 EU 2007 9 21 AALA20071646 1 20070829 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 JFK - EMERGENCY LIGHT AT RIGHT SIDE FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIGHT SIDE FI RST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007092400015 20070924 00015 EU 2007 9 24 07FDEA03890 1 20070918 A 5310 A53986426205 BEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 729FD 657 CORROSION FOUND AT EDGE BEAM, C89-90, RT REPAIR PERFORMED BY CORROSION REWORK IAW EA 6-5319-114902 AND RAS /DAHAM/402277 5/2007 ISS A. 2 L 7 2 4F RT A35EU 2007092400016 20070924 00016 EU 2007 9 24 07FDEA03892 1 20070918 A 5415 A57140236 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 729FD 657 FOUND IMPACT DAMAGE ON PYLON THRUST AND SIDE LOAD FITTING, RT WING REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5720-114892 AND RAS/BAE/1005535/2007 ISS A. 2 L 7 2 4F RT A35EU 2007092400017 20070924 00017 EU 2007 9 24 07FDEA03893 1 20070918 A 5415 A57140236 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 729FD 657 FOUND IMPACT DAMAGE ON PYLON THRUST AND SIDE LOAD FITTING, LT WING REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5720-114892 AND RAS/BAE/1005535/2007 ISS A. 2 L 7 2 4F RT A35EU 2007092400018 20070924 00018 EU 2007 9 24 07FDEA03894 1 20070918 A 5730 A57340085 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 600 - RH CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND SEVERAL OLD REPAIRS OF THE WING TOP SKIN PANEL BETWEEN RIB 9-23 RT WITH NEW CORROSIONS SPOTS. REPAIR PERFORMED BY BLEND OUT CORROSION, FLAP PEENING REWORKED AREAS IAW EA 6-5720-81120, RAS/BAE/0203/2000 ISSUE A AND RAS/BAE/1409/2004 I SSUE A. 2 L 7 2 4F RT A35EU 2007092400019 20070924 00019 EU 2007 9 24 07FDEA03895 1 20070918 A 5313 A53970713 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 HEAVY CORROSION ON STRINGER 53 LT AND RT BETWEEN FRAME 54-54.2. AFFECTED STRINGERS REPLACED IAW EA 6-5316-81072, APPROV ED BY RAS/DATLS/0002275/2004 ISSUE A. 2 L 7 2 4F RT A35EU 2007092400020 20070924 00020 EU 2007 9 24 07FDEA03896 1 20070918 A 5311 B53770380200 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 729FD 657 FOUND CHAFING MARKS ON MILLED FRAME FLANGE, C 28, P 8-21, LT REPAIR PERFORMED BY BLEND OUT THE AFFECTED AREA IAW EA 6-53 14-114895 AND RAS/DABRE/7008329/2007 ISS A. 2 L 7 2 4F RT A35EU 2007092400021 20070924 00021 EU 2007 9 24 07FDEA03897 1 20070918 A 5311 B53770012200 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CHAFED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 729FD 657 FOUND CHAFING MARKS ON MILLED FRAME FLANGE, C 28, P 8-21, LT. REPAIR PERFORMED BY BLEND OUT THE AFFECTED AREA IAW EA 6- 5314-114895 AND RAS/DABRE/7008329/2007 ISS A 2 L 7 2 4F RT A35EU 2007092400022 20070924 00022 EU 2007 9 24 07FDEA03898 1 20070918 A 5753 FLAP AIRBUS 310 A310324 3930206 EU ZONE 500 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND OLD REPAIR ON INNER FLAP LT AT RIB 21, POCKET REPAIRS AS PER SB A310-57-2054. REPLACEMENT OF END RIB AS PER SB A3 10-57-2055, ISSUED AND APPROVED PER EA 6-5752-81084. 2 L 7 2 4F RT A35EU 2007092400023 20070924 00023 EU 2007 9 24 07FDEA03899 1 20070918 A 5753 FLAP AIRBUS 310 A310324 3930206 EU ZONE 600 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND OLD REPAIR ON INNER FLAP RT AT RIB 21, POCKET REPAIRS AS PER SB A310-57-2054. REPLACEMENT OF END RIB AS PER SB A3 10-57-2055, ISSUED AND APPROVED PER EA 6-5752-81084. 2 L 7 2 4F RT A35EU 2007092400024 20070924 00024 EU 2007 9 24 07FDEA03900 1 20070918 A 5280 A52810625 SKIN AIRBUS 310 A310203 3930313 EU NLG DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 DURING UNCONTROLLED MOVEMENT OF HYDRAULIC CYLINDER THE RT NLG FWD DOOR SKIN WAS DAMAGED. REPAIR PERFORMED BY CUT OUT TH E SKIN AND INSTALLING A DOUBLER WITH SHIM IAW EA 6-5282-81079 AND RAS/AS/307/2004 ISS A 2 L 7 2 4F RT A35EU 2007092400025 20070924 00025 EU 2007 9 24 07FDEA03901 1 20070918 A 5730 A57340083 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND OLD BLEND OUT REPAIRS WITH NEW CORROSION SIGNS ON LT WING UPPER SKIN BETWEEN RIB 3 TO 5 NEAR THE REAR SPAR AND BET WEEN RIB 7 TO 8 AND RIB 10 TO 11 AT THE FRONT SPAR. THE CORRODED AREAS HAVE BEEN REPAIRED IAW WITH SRM 57-00-00/PG 201/ PARA 4C PART B AND TD/B/2004/0443 ISSUE B, APPROVED BY EA 6-5720-81121 AND RAS/BAE/1409/2004 ISSUE A. 2 L 7 2 4F RT A35EU 2007092400026 20070924 00026 EU 2007 9 24 07FDEA03902 1 20070918 A 5310 A53988424 STRUT AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION ON CROSS STRUT C 84 RT AND LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092400027 20070924 00027 EU 2007 9 24 07FDEA03903 1 20070918 A 5310 A53988724 STRUT AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION ON CROSS STRUT C 87 RT AND LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092400028 20070924 00028 EU 2007 9 24 07FDEA03904 1 20070918 A 5753 A57960657200 SKIN AIRBUS 310 A310324 3930206 EU TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 DENT ON LT WING OUTBOARD FLAP OUTER SKIN LOWER SIDE BETWEEN RIB 1-2. REPAIR PERFORMED BY CUT OUT OF DAMAGED SKIN AND CO RE AND INSTALLING FABRICATED REPAIR DOUBLER IAW SRM 51-77-12/FIG 217. 2 L 7 2 4F RT A35EU 2007092400029 20070924 00029 EU 2007 9 24 07FDEA03905 1 20070918 A 5730 A57340087 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 ELONGATED WING TO PYLON HYDRAULIC FITTING HOLES IN LOWER WING SKIN PANEL NR 2. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLING BUSHES IAW R572-49184 ISSUE C, APPROVED BY EA 6-5720-81095 AND RAS/BAE/1000166/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007092400030 20070924 00030 EU 2007 9 24 07FDEA03906 1 20070918 A 5730 A57340087 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 ELONGATED WING TO PYLON HYDRAULIC FITTING HOLES IN LOWER WING SKIN PANEL NR 2 RT WING. REPAIR PERFORMED BY OVERSIZING H OLES AND INSTALLING BUSHES IAW R572-49184 ISSUE C, APPROVED BY EA 6-5720-81095 AND RAS/BAE/1000166/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007092400031 20070924 00031 EU 2007 9 24 07FDEA03910 1 20070918 A 5311 A53978336200 COUPLING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND CORRODED COUPLING AT FRAME 55/58, STRG 44 LT. REPLACEMENT OF COUPLING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092400032 20070924 00032 EU 2007 9 24 07FDEA03911 1 20070918 A 5311 A53974409 COUPLING AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND CORRODED COUPLING AT FRAME 55/58, STRG 55 LT AND RT SIDE. REPLACEMENT OF COUPLING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092400033 20070924 00033 EU 2007 9 24 07FDEA03912 1 20070918 A 5311 A53974258 COUPLING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND CORRODED STRINGER COUPLING AT FRAME 55/58, STRG 56 LT AND RT SIDE. REPLACEMENT OF BOTH COUPLINGS IAW SRM 51-72-10 . 2 L 7 2 4F RT A35EU 2007092400034 20070924 00034 EU 2007 9 24 07FDEA03913 1 20070918 A 5311 A53974407201 COUPLING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND CORRODED STRINGER COUPLING AT FRAME 55/58, STRG 52 RT. REPLACEMENT OF COUPLING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092400035 20070924 00035 EU 2007 9 24 07FDEA03914 1 20070918 A 5313 A53974235202 STRINGER SPLICE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND CORRODED STRINGER COUPLING AT FRAME 55/58, STRG 51 RT. REPLACEMENT OF COUPLING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092400036 20070924 00036 EU 2007 9 24 07FDEA03915 1 20070918 A 5313 A53974408201 STRINGER SPLICE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND CORRODED STRINGER COUPLINGS AT FRAME 55/58, STRG 53 AND 54 RT. REPLACEMENT OF BOTH COUPLINGS IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092400037 20070924 00037 EU 2007 9 24 07FDEA03916 1 20070918 A 5313 A53973314200 STRINGER SPLICE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND FIVE CORRODED STRINGER COUPLINGS AT FRAME 55/58 BETWEEN STRG 45 AND 49 LT. REPLACEMENT OF THE FIVE COUPLINGS IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092400038 20070924 00038 EU 2007 9 24 07FDEA03917 1 20070918 A 5313 A53974235200 STRINGER SPLICE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND CORRODED STRINGER COUPLING AT FRAME 55/58, STRG 50 LT. REPLACEMENT OF COUPLING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092400039 20070924 00039 EU 2007 9 24 07FDEA03918 1 20070918 A 5313 A53974283200 STRINGER SPLICE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND CORRODED STRINGER COUPLING AT FRAME 55/58, STRG 51 LT. REPLACEMENT OF COUPLING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092400040 20070924 00040 EU 2007 9 24 07FDEA03919 1 20070918 A 5313 A53974407200 STRINGER SPLICE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND CORRODED STRINGER COUPLING AT FRAME 55/58, STRG 52 LT. REPLACEMENT OF COUPLING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092400041 20070924 00041 EU 2007 9 24 07FDEA03920 1 20070918 A 5313 A53974408200 STRINGER SPLICE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND TWO CORRODED STRINGER COUPLINGS AT FRAME 55/58, STRG 53 AND 54 LT. REPLACEMENT OF BOTH COUPLINGS IAW SRM 51-72-10 . 2 L 7 2 4F RT A35EU 2007092400042 20070924 00042 EU 2007 9 24 07FDEA03921 1 20070918 A 5313 A53973314201 STRINGER SPLICE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND TWO CORRODED STRINGER COUPLINGS AT FRAME 55/58, STRG 48 AND 49 RT. REPLACEMENT OF BOTH COUPLINGS IAW SRM 51-72-10 . 2 L 7 2 4F RT A35EU 2007092400043 20070924 00043 EU 2007 9 24 07FDEA03922 1 20070918 A 5313 A53974227200 STRINGER SPLICE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND CORRODED STRINGER COUPLING AT FRAME 55/58, STRG 50 RT. REPLACEMENT OF COUPLING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092400044 20070924 00044 EU 2007 9 24 07FDEA03923 1 20070918 A 5313 A53970721 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND PITTING CORROSION ON STRINGER 44 RT, BETWEEN FRAME 54-55/58. REPAIR PERFORMED BY REPLACEMENT OF STRINGER PORTION AS LONG AS POSSIBLE BY USING ADDITIONAL COUPLINGS AS PER SRM 53-10-14/FIG 201 AND IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092400045 20070924 00045 EU 2007 9 24 07FDEA03924 1 20070918 A 5313 A53970701 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND PITTING CORROSION ON FOLLOWING STRINGER: 48 AND 50 RT AND STRG 46, 47, 48, 50 AND 51 LT, BETWEEN FRAME 54-55/58. REPAIR PERFORMED BY REPLACEMENT OF STRINGER PORTION AS LONG AS POSSIBLE BY USING ADDITIONAL COUPLINGS AS PER SRM 53-10-1 4/FIG 201 AND IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092400046 20070924 00046 EU 2007 9 24 07FDEA03925 1 20070918 A 5310 A53973085210 BEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 CORROSION FOUND ON AFT CARGO DOOR SILL BEAM OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092400047 20070924 00047 EU 2007 9 24 07FDEA03926 1 20070918 A 5313 A53970713 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 804FD 549 FOUND PITTING CORROSION ON FOLLOWING MILLED STRINGER: 52, 53 AND 54 RT AND STRG 52, 53, 54 AND 56 LT, BETWEEN FRAME 54. 1-55/58. REPAIR PERFORMED BY REPLACEMENT OF STRINGER PORTIONS AS LONG AS POSSIBLE BY USING ADDITIONAL COUPLINGS AS PER SRM 53-10-14/FIG 201A AND IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092500003 20070925 00003 EU 2007 9 25 07FDEA03990 1 20070919 A 5320 A53610995205 STIFFENER AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 FOUND CRACK ON STIFFENER AT FRAME 12A LT, STRG 27. REPLACEMENT OF STIFFENER AS PER DWG A536-10318/SH 05. 2 L 7 2 4F RT A35EU 2007092500010 20070925 00010 NM 2007 9 25 QXEA200701435 1 20070913 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 599 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - FLOORBOARD FLANGE TO SEAT TRACK GUSSET AT STATION 599.0 INBOARD OF LEFT INBOARD SEAT TRACK HAS CORROSION ON LOW ER SURFACE AND ALONG EDGE ON FLANGE. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-40-11. 2 H 7 2 4T RT A13NM 2007092500020 20070925 00020 NM 2007 9 25 QXEA200701429 1 20070914 A 5313 STRINGER DHAV DHC8 DHC8202 2809007 NM BS 357 S21R CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - RIGHT STRINGER 21 HAS CORROSION ON INBOARD LEADING EDGE FLANGE AT STATION 357.70. REPAIRED IAW SRM 51-20-11, 5 1-20-16, 51-20-36, AND 51-20-26. 2 H 7 2 4T RT A13NM 2007092500021 20070925 00021 WP 2007 9 25 UPS07850635 1 20070908 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT FAULTY A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:N/A DURING PREFLIGHT EMERGENCY LIGHTS BATTERY CHARGING C/B POPPED AND WOULD NOT RESET. REMOVED AND REPL ACED EMERGENCY LIGHTING BATTERY PACK PER MM 33-50-01-2. SYSTEM OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2007092500026 20070925 00026 NM 2007 9 25 UPS07M50629 1 20070629 A 5730 SKIN DOUG MD11 MD11F 3023600 NM RT WING GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C RIGHT WING IN THE AREA OF THE LAST SLAT, HAS DEEP GOUGES, HARD CONTACT WITH OUTER/LAST SLAT. AFFECTED AREA DEEP GOUGES REMOVED & SMOOTHED. ORG THK 0.060" MATL REMAINN 0.024" MATL REMOVED 0.036" FOUND EXCEED LIMIT SRM 57- 00-01 FIG 3 VI R38. SKIN TRIM OUT EN1463-07. SKIN REMOVED EN1463-07. HFEC C/O & FOUND NO CRACK. NEW SKIN FAB EN1463- 07 USE MATL 6061-0-0.063. WELDING C/O ON RT WING SKIN FAB AREA EN1463-07. L/E SKIN O/B CONTACT OUTER SLAT INSTALLED. 2 L 7 3 4F RT A22WE 2007092500032 20070925 00032 NM 2007 9 25 KSCA07062 1 20070808 A 2120 UNKNOWN BOEING 747 747SR46 1384816 NM COCKPIT SMOKE A KCSA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 719CK 20923 AT FL 360 AT 0230Z, SMOKE APPEARED IN THE COCKPIT. THREE SECONDS LATER THE NR 4 EGT WENT TO RED LINE, THE RED EGT LIGHT ILLUMINATED, THE OIL QUANTITY WENT TO ZERO, THE OIL PRESSURE WENT TO ZERO, THE OIL TEMPERATURE WENT TO THE RED LINE, AN D N2 WENT TO ZERO. SEVER ENGINE CHECK LIST WAS COMPLETED. N1 GAUGE INDICATED 33 PERCENT, BUT VISUAL OBSERVATION SHOWED NO ROTATION OF THE N1 FAN BLADES. THE COCKPIT SMOKE CEASED AFTER THE IMMEDIATE ACTION ITEMS WERE ACCOMPLISHED. 2 L 7 4 4F RT A20WE 2007092500033 20070925 00033 2007 9 25 AALA20071757 4 20070917 A 2565 62772216 SLIDE BOEING 777 777223 1385213 NM R2 DOOR DISLODGED A AALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 778AN 29587 NRT - RIGHT NUMBER TWO DOOR SLIDE/RAFT INADVERTENTLY DROPPED FROM HOUSING. DID NOT DEPLOY. NRT UNABLE TO REPLACE. PLA CARDED AND BLOCKED SEATS ON OUTBOUND. SLIDE REPLACED AT LAX. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007092500042 20070925 00042 NM 2007 9 25 SWAA074519 1 20070911 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B22 13802 NE HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 408WN 27895 DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 151.1. REPAIRED SKIN IAW SRM. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007092500057 20070925 00057 NM 2007 9 25 SWAA074545 1 20070911 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092500058 20070925 00058 NM 2007 9 25 SWAA074546 1 20070911 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007092500060 20070925 00060 NM 2007 9 25 SWAA074532 1 20070911 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092500065 20070925 00065 NE 2007 9 25 HEEA116984 2 20070817 A 7297 CONNECTOR SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B 60037 NE ECU MALFUNCTIONED E HEEA O OTHER J WARNING INDICATION LD LANDING 1 SW 03 972AE 3234 AMBER GOV LIGHT ILLUMINATED PRIOR TO LANDING, UPON SHUTDOWN, ENGINE WOULD NOT REDUCE RPM FROM FLIGHT POSITION WHEN START SELECT SWITCH SET TO IDLE. ENGINE WOULD NOT RESTART. CLEANED CONNECTIONS AND REPLACED GOVERNOR FUSE, REPLACED FUSE HO LDER AND REPLACED ECU. 1 G 7 1 3U 3 U H9EU E00054EN 2007092500068 20070925 00068 CE 2007 9 25 DXTA200702445 1 20070903 A 2150 A/C PACK CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 948QS 7500149 COCKPIT PAC TEMPERATURE IS UNCONTROLLABLE AND PRODUCES A BURNING / SULFUR TYPE ODOR. TROUBLESHOT SYSTEM. FOUND ACM A ND TEMPERATURE CONTROL VALVES INOP. TEMP. CONTROL VALVE REMOVED PN 27241287-10, SN 10AT77. INSTALLED O/H PN 27241287, SN 4AR32. ACM REMOVED AND INSTALLED IAW CE750 MM CHAPTER 21-51-00 OPERATIONS CHECK GOOD. TEMP CONTROL VALVE REMOVAL AND INSTALLATION IAW CE750 MM CHAPTER 21-61-00. OPS CHECK GOOD. NO FURTHER DEFECTS AT THIS TIME. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007092500072 20070925 00072 CE 2007 9 25 DXTA200702457 1 20070909 A 3244 TIRE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG FAILED E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 904QS 7500210 NOSE GEAR SHIMMY DURING TAKEOFF AND TAKEOFF WAS ABORTED. BOTH NOSE WHEEL TIRES OUT OF ROUND. REMOVED TIRES AND INSTALLE D OVERHAULED WHEELS AT BOTH POSITIONS. SERVICED TIRES TO 140 PSI. WORK DONE I/A/W CE750 M/M 32-41-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007092500077 20070925 00077 CE 2007 9 25 DXTA200702453 1 20070907 A 2120 MOTOR CESSNA 500 560CESSNA 2076750 CE ALLSN AE3007 AE3007C GL A/C DRIVE SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 340QS 5600514 HEAVY SMOKE AND BURNING ODOR DISCOVERED IN THE BATTERY COMPARTMENT 7 MINUTES AFTER HOOKING UP GPU AND RUNNING AIR CONDIT IONER. REMOVED AND REPLACED AC COMPRESSOR DRIVE MOTOR, RECEIVER/DRYER P/N 1334140-3, COMPRESSOR DRIVE BELT PULLEY P/N FWA1250146-7, DRIVE BELT P/N FWA232L100 AND HIGH PRESS SERVICING PORT P/N 1134964. SERVICED SYS WITH R-134A REFRIGERANT. SYS OPS & LEAK CK GOOD IAW ENVIRO SYS CMM CHP 21-52-01. 2 L 7 2 4F 4 F RT A22CE TE6CH 2007092500080 20070925 00080 2007 9 25 DXTA200702459 4 20070909 A 2200 AUTOPILOT SYS CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MALFUNCTIONED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 926QS 7500026 CLIMBING OUT OF 5,000 FT, AUTOPILOT WAS ENGAGED THEN DISENGAGED WITH AN ABRUPT PITCH UP MOMENT. SHORTLY AFTER RETRIMMIN G, A/P DISENGAGED AGAIN, BUT WITH NO PITCH CHANGE. IT WAS DECIDED NOT TO RE-ENGAGE THE A/P. A SHORT TIME LATER WE RELI ZED THAT WE HAD A JAMMED STAB AT -1.3. WE FOLLOWED THE APPROPRIATE CHECKLIST. BURNED FUEL TO LAND, LESS THAN 27,000 LB S AND LANDING WITHOUT INCIDENT. REMOVED AND REPLACED HORIZONTAL STAB. ACTUATOR ECM WITH MODIFIED ECM IAW CESSNA 750MM. 27-40-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007092500084 20070925 00084 NM 2007 9 25 USAA920070820 1 20070908 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 23704 CLT - MAJOR REPAIR - C-5 CHECK, LEVEL 2 CORROSION ON STRINGER, BS 1006 - BS 1016, RBL 8. REPAIRED STRINGER, BS 1006 - B S 1016, RBL 8 IAW B737-300 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007092500088 20070925 00088 NM 2007 9 25 USAA920070821 1 20070907 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 23704 CLT - MAJOR REPAIR - C-5 CHECK, LEVEL 2 CORROSION ON FLOORBEAM, BS 986, LBL 10. REPAIRED FLOORBEAM, BS 986, LBL 10 IAW USAIRWAYS TYPICAL REPAIR 53-10-05B. 2 L 7 2 4F RT A16WE 2007092500092 20070925 00092 CE 2007 9 25 DXTA200702447 1 20070904 A 3150 CHIP DETECTOR CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE RT ENGINE CONTAMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 346QS 6800013 RT ENGINE CHIP DETECTOR CAS MESSAGE. 09-27-07 ACCOMPLISHED DEBRIS IN OIL CHECK IAW P&W P/I/M 72-00-00-1-135 C/W FIL TER CHANGE AND SOAP. SAMPLE REPLACED S/G & ALT MAGNETIC SEALS PER P&W REP. ALL WORK ACCOMPLISHED IAW P&W M/M 72-60-01. 2 L 7 2 4F 4 F RC T00012WI E35NE 2007092500093 20070925 00093 CE 2007 9 25 DXTA200702443 1 20070903 A 3150 WARNING MESSAGE CESSNA 750 750 2076810 CE PWC PW306 PW306C 52169 NE ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 923QS 7500023 FLAPS FAILED. CAS MESSAGE ILLUMINATED IN CRUISE FLIGHT AND REMAINED ILLUMINATED UNTIL WE PARKED. SLATS DID WORK. C/W FLAP SYSTEM OPS CHECK WITH BRAKE OUT BOXES INSTALLED SYSTEM OPS CHECK GOOD IAW CE750 M/M 27-50-00. UNABLE TO DUPLICATE D ISCREPANCY. NO DEFECTS NOTED. 2 L 7 2 4J 4 F RT T00007WI E35NE 2007092500097 20070925 00097 NE 2007 9 25 HEEA117201 1 20070901 A 6540 9235806801102 SENSOR SKRSKY S92 S92A NE GE CT7TS CT78A 30136 NE GEARBOX MALFUNCTIONED B HEEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 03 992PH 41 920055 DURING CRUISE INTERMEDIATE GEARBOX HOT LIGHT ILLUMINATED. PERFORMED EMERGENCY PROCEDURE. RETURNED TO HBP. LIGHT CAME ON AND OFF DURING RETURN FLIGHT. REPLACED CHIP DETECTOR-TEMP SENSOR AND HOUSING. 2 G 7 2 4U 4 U R00024BO E8NE 2007092500123 20070925 00123 CE 2007 9 25 DXTA200702481 1 20070916 A 3260 DOWNLOCK SWITCH BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA O OTHER P NO WARNING INDICATION LD LANDING 1 GL 07 151QS RK422 DID NOT GET A RT LANDING GEAR GREEN DOWN AND LOCKED INDICATION UPON GEAR EXTENTION. 09-28-07 REMOVED FAULTY RT MAIN GEAR DOWN AND LOCKED SWITCH AND INSTALLED NEW SWITCH IAW HAWKER 400XP MM CHAP. 32-10-00. AND TEMP REV 32-1. OPS CHECK GO OD. FOR DETAILS REF FAS WO 07-2259. 2 H 7 2 4F 4 F RT A16SW E25EA 2007092500131 20070925 00131 SO 2007 9 25 C2XA07TY053 1 20070911 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 29906 145472 BNA - FLIGHT ATTENDANT REPORTED A SMOKE SMELL FROM THE FOWARD CABIN. MAINTENANCE RAN BOTH PACKS FROM THE APU AND NR 1 A ND 2 ENGINE BLEEDSOURSES. INSPECTED BOTH PACK ASSEMBLIES, ALSO THE DUCTING IAW EMB 145 AMM 71-00-01 AND 36-00-00. NO S MOKE OR SMELL COULD BE DUPLICATED. A/C RELEASED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007092500132 20070925 00132 CE 2007 9 25 DXTA200702448 1 20070905 A 2720 ADAPTER BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE RUDDER BOOST FAILED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 132QS RK427 RDR BST FAIL LIGHT FLASHED INTERMITTENTLY DURING TAKEOFF, THEN CAME ON STEADY 1 MIN AFTER TAKEOFF. 09-27-07 INTERRO GATED AVIONICS STATUS ON THE MFD & FOUND NO CODES FOR RUDDER BOOST FAIL MESSAGE. PER THE RUDDER BOOST T/S CHART INTERRO GATED THE LRU FAULT HISTORY & FOUND THE FOLLOWING LRU FAILURES. REMOVED & REPLACED THE SIGNAL INTERFACE ADAPTER W/ OVERH AULED UNIT. FUNCTION CHECK OF THE SIGNAL INTERFACE ADAPTER GOOD IAW COLLINS SYSTEM MM 52-0775811 TABLE 5-74 STA TEST PR OCEDURES. 2 H 7 2 4F 4 F RT A16SW E25EA 2007092500137 20070925 00137 SO 2007 9 25 C2XA07RI077 1 20070910 A 3350 7287580505 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13964 145123 FLT 2355 EWR - EMERGENCY FLOOR PROXIMITY RIGHT STRIP INOPERATIVE. EWR MX REMOVED AND REPLACED EMERGENCY STRIP IAW EMB 1 45 AMM 33-50-12. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO FLIGHT. 2 L 7 2 4T RT T00011AT 2007092500144 20070925 00144 NM 2007 9 25 AMTA200700407 1 20070827 A 5340 MOUNT BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE BS 1320 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 LAV C AFT IB MOUNT AT FS 1320, LBL 23 CORRODED. MOUNT FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A FIG 101 SHEET 3 DET AIL VI SECTION B-B REPLACED MOUNT AT LAV C IAW 51-40-01.(K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007092500153 20070925 00153 SO 2007 9 25 C2XA07RI079 1 20070912 A 3350 LIGHT EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 14925 145004 FLT 2297 - EWR - CREW REPORTED EMERGENCY FLOOR LIGHTING WIRE IS VISIBLE OUTSIDE PLASTIC MOLDING AND STRIP IS INOPERATIVE BY SEAT 12A. EWR MX REMOVED AND REPLACED EMERGENCY FLOOR STRIP IAW EMB 145 AMM 33-50-12. MX PERFORMED OPERATIONAL CHE CK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007092500162 20070925 00162 SO 2007 9 25 C2XA07TY052 1 20070913 A 5320 14521725615 SILL EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSLEAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16525 145403 SERVICE DOOR AFT LOWER CORNER BRACKET HAS CORROSION. REMOVED AND REPLACED AFT SILL IAW SRM 51-40-02. AIRCRAFT STILL IN C CHECK. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007092500167 20070925 00167 EU 2007 9 25 HEER117214 1 20070903 A 6320 4649010008X TRANSMISSION UROCOP EC135 EC135P2 5620027 EU MAIN ROTOR CORRODED B HEER O OTHER O OTHER NR NOT REPORTED 1 SW 03 343PH 779 0456 DURING MAST REPLACEMENT FOUND INTERIOR SURFACES OF MAIN TRANSMISSION CORRODED AND RUSTED. REPLACED MAIN TRANSMISSION AN D WILL BE SENT TO MFG FOR CORE EXCHANGE. 1 G 7 2 3U H88EU 2007092500173 20070925 00173 NM 2007 9 25 GAIA07013OP 1 20070814 A 3350 1000679 LIGHT BOEING 727 727224 1384076 NM PWA JT8 JT8D9A 52048 NE L1 DOOR INOPERATIVE A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69735 20664 NO FLIGHT: DURING A CHECK, FOUND L-1 EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPS CHECK NORMAL. AC WAS RETURNED TO SERVICE. (K) 2 L 7 3 4F 4 F A3WE E2EA 2007092500175 20070925 00175 NM 2007 9 25 UPS07550650 1 20070823 A 5311 70750071C FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 432UP 25463 INSPECTION TYPE:C DENT IN AFT CARGO COMPARTMENT FUSELAGE FRAME STA 1520, BETWEEN S25R AND S26R. REPAIRED DENT IAW SRM 5 3-00-07, THIS IS A CATEGORY B, ZONE 1, M PER DETAIL V, TABLE II PG'S 212 AND 210 FIG 201 10 OF 15. REPAIR ACCOMPLISHED PER DETAIL I FIG 201, (SHT 4 OF 15). 2 L 7 2 4F RT A2NM 2007092500176 20070925 00176 CE 2007 9 25 MT92007F00000 1 20070716 A 3245 C2620230107 TUBE CESSNA 208 208B 2073701 CE PWA PT6 PT6A45 52043 EA RT MAIN TIRE SPLIT E MT9A O OTHER O OTHER NR NOT REPORTED 1 SW 05 162SA 15 208B0548 AIRCRAFT LANDED ON ITS SCHEDULED ROUTE, WHEN IT EXPERIENCED A FLAT TIRE ON ROLL OUT. THIS CAUSED THE CLOSURE OF THE ACT IVE RUNWAY. MAINTENANCE PERSONNEL REPLACED THE TIRE AND TOWED THE PLANE BACK TO THE RAMP. THE TIRE WAS DISASSEMBLED AN D IT WAS FOUND THAT THE TUBE HAD A PERPENDICULAR 2 INCH SPLIT ON THE OUTER RADIUS WITH NO MATCHING DAMAGE TO THE TIRE. (K) 1 H 7 1 3T 4 T A37CE E4EA 2007092500190 20070925 00190 EU 2007 9 25 M7K2007F00003 1 20070806 A 6220 704A33640088 FREQ ADAPTER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE M/R HEAD CRACKED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 808MH 1299 M2627 3914 DURING ROUTINE POSTFLIGHT INSPECTION THE CRACK WAS FOUND VISUALLY ON THE YELLOW BLADES FREQUENCY ADAPTER ELASTOMER SURFA CE TRAILING EDGE SIDE JUST BEGINNING TO EXCEED THE M LIMITATION OF 10 MM OF LENGTH. THIS IS A VERY COMMON FAILURE THAT OCCURS USUALLY BEFORE THE HALF LIFE OF THE COMPONENT IS REACHED. THE OLDER PN OF THIS DESIGN USED A DIFFERENT ELASTOMER FORMULA AND RARELY CRACKED BEFORE 3000 HOURS OF SERVICE. SUGGEST MFG RETURN TO OLDER ELASTOMER FORMULA OR VENDOR FOR T HE OLDER PN PARTS. (K) 1 G 7 2 3U 3 U H9EU E00054EN 2007092500194 20070925 00194 CE 2007 9 25 GUUA09130701 1 20070913 A 3297 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG CHAFED A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 29 190YV UE190 DURING FLIGHT LANDING GEAR LIGHTS FLICKER WITH LIGHT INOPERATIVE IN FLIGHT. REPAIRED CHAFED WIRE UNDER AIRSTAIR DOOR. OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007092500197 20070925 00197 NM 2007 9 25 KCSA071374 1 20070913 A 5322 SHEAR TIE BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 SHEAR TIE CRACKED ON STA 480 FRAME BETWEEN STR 26L AND STR 27L. 2 L 7 4 4F RT A20WE 2007092500200 20070925 00200 CE 2007 9 25 GLBA20060998 1 20070911 A 5310 ANGLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FUSELAGE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 251GL UE251 LT HEAVY ANGLE CRACKED APPROXIMATELY 1.6 INCHES AT F.S. 288.0 TO 289.6. MAINTENANCE REPAIRED LT HEAVY ANGLE IAW SRM 53-9 0. REPAIR LENGTH 13.5 INCHES. PN 114-430002-7179. AT FS 288 TO FS 301.5. RII INSPECTION COMPLIED WITH IAW TASKCARD 8. 2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007092500201 20070925 00201 CE 2007 9 25 DXTA200702434 1 20070828 A 2611 47359714 SMOKE DETECTOR RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP CARGO BAY INOPERATIVE E DXTA O OTHER N FALSE WARNING LD LANDING 1 GL 07 821QS 1864 258709 BAG FIRE LIGHTS REMAINS ILLUMINATED. THIS IS A REPEAT WRITE-UP FROM 08/27/07. REMOVED FWD SMOKE DETECTOR P/N 473597-14 S /N 0754 AND INSTALLED NEW UNIT S/N 1271. REMOVED AFT SMOKE DETECTOR P/N 473597-14 S/N 0758 AND INSTALLED SERVICEABLE UNI T S/N 0837. REMOVED LAV SMOKE DETECTOR P/N 473597-14 S/N 0729 AND INSTALLED SERVICEABLE UNIT 0829. SERVICEABLE UNIT WERE REMOVED FROM AIRCRAFT N884QS S/N 258734. OPS CHECK GO SYSTEM SHOWS ALL NORMAL OPERATION. ALL WORK PERFORMED IAW MM CHP 26-15-51. 2 L 7 2 4F 4 F RT A3EU E6WE 2007092500202 20070925 00202 SO 2007 9 25 GUUA09160701 1 20070916 A 3350 BULB EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE EMERGENCY LIGHT LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 283AS 120236 DURING PREFLIGHT DISCOVERED RT FWD OVERWING EMERGENCY LIGHT INOPERATIVE. SECURED BULB AT RT FWD OVERWING EMERGENCY LIGH T SOCKET. 2 L 7 2 4T 4 T RT A31SO E20NE 2007092500219 20070925 00219 CE 2007 9 25 DXTA200702489 1 20070920 A 5340 MOUNT CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MASTER CYLINDER MISINSTALLED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 691QS 5605290 LT BRAKE PEDAL IN CAPT'S (LT) SEAT WILL GO VERY FAR FWD AND PROHIBIT LT BRAKE FROM FULLY ENGAGING. THIS APPEARS MOST EV IDENT IN THE "FWD" PEDAL POSITION. 09-28-07 FOUND MOUNT FOR BRAKE MASTER CYLINDER, LOCK FASTENER WITH NO LOCKING COLL ARS INSTALLED. INSTALLED NEW (4) LOCK FASTENER PINS & COLLARS TO THE BRAKE & REINSTALLED PILOT MASTER CYLINDER LO, ADN B LED BRAKE SYSTEM IAW MODEL 560XL MM 32-42-00. OPERATIONAL CK GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007092500234 20070925 00234 SW 2007 9 25 AC2A117357 1 20070915 A 2435 23081018 STARTER GEN BELL 427 427 1182207 SW PWC PW207 PW207D NE FAILED E AC2A O OTHER O OTHER NR NOT REPORTED 1 SW 31 427CK 56043 STARTER GENERATOR WOULD NOT ENGAGE. WENT OFFSHORE TO REPLACE STARTER. ONCE OFFSHORE, ENGAGED STARTER SWITCH 3 TIMES AND THE STARTER WORKED AS ADVERTISED. ELECTED TO REPLACE THE STARTER TO PREVENT ANY FURTHER DELAYS AND THE STARTER RAN ONL Y 62.5 HOURS, REMAINING UNTIL TIME CHANGE. 1 G 7 1 3U 3 U R00001RC E42NE 2007092500260 20070925 00260 EU 2007 9 25 07FDEA03998 1 20070919 A 5313 A53974203228 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION ON STRINGER P 56 LT, C69-70 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007092500268 20070925 00268 EU 2007 9 25 07FDEA04003 1 20070919 A 5320 A53978482225 SUPPORT AIRBUS 310 A310324 3930206 EU ZONE 200 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 FOUND SUPPORT STRUT WITH LESS EDGE MARGIN BETWEEN FRAME 71-72, STRG 26 RT. REPLACEMENT OF STRUT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092500276 20070925 00276 NM 2007 9 25 07FDEA04010 1 20070919 A 5320 6557568950 ANGLE BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 AFT CARGO COMPARTMENT "Z" ANGLE HAS CORROSION IN 2 LOCATIONS FROM STA 950B TO 950E, RBL 24, WL 156 BLENDED CORROSION ON "Z" ANGLE STA 950B OUT OF LIMITS PER SRM 51-40-3. BLEND CORROSION AT STA 950D. REMOVED .005' FROM ORIGINAL THICKN ESS OF .056, WITHIN LIMITS REF SRM 53-10-1. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2007092500277 20070925 00277 NM 2007 9 25 SWAA074552 1 20070910 A 3350 147A5704 CAP BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 496WN 32478 EEPLS END CAP CRACKED AT ROW 1 ABC. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 2007092500282 20070925 00282 EU 2007 9 25 07FDEA04013 1 20070919 A 5313 A53970444207 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 OLD DAMAGE ON STRINGER 30 RT, BETWEEN FRAME 54.2-54.3. STRINGER SPLICE REPAIR IAW SRM 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007092500283 20070925 00283 NM 2007 9 25 SWAA074597 1 20070913 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 762SW 27876 RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007092500285 20070925 00285 NM 2007 9 25 SWAA074553 1 20070910 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 499WN 32481 DURING SCHEDULED RON CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007092500286 20070925 00286 NM 2007 9 25 SWAA074600 1 20070913 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 466WN 30677 EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007092500288 20070925 00288 NM 2007 9 25 SWAA074590 1 20070913 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 411WN 29821 EEPLS COVER MISSING AT ROW 14 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007092500289 20070925 00289 EU 2007 9 25 07FDEA04016 1 20070919 A 5313 A53970524200 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT STRINGER P 26 LT, C54-54.1 REPAIR PERFORMED BY PARTIAL REPLACEMENT OF CORRODED STRINGER IAW A300-600 FREIGHTER SRM 53-10-14 , APPROVED BY EA 6-5310-81053 AND RAS/DATLS/0002051/2004 ISS A. 2 L 7 2 4F RT A35EU 2007092500290 20070925 00290 NM 2007 9 25 SWAA074598 1 20070913 A 3350 417A5704 CAP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 202WN 33999 DURING SCHEDULED 1/2DHC2 CHECK, FOUND EEPLS END CAP LOOSE AT ROW 1 ABC. SECURED END CAP PER MM. 2 L 7 2 4F RT A16WE 2007092500291 20070925 00291 2007 9 25 SWAA074605 4 20070913 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 783SW 29809 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007092500292 20070925 00292 2007 9 25 SWAA074604 4 20070913 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 706SW 27840 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007092500294 20070925 00294 NM 2007 9 25 SWAA074569 1 20070910 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506D, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007092500295 20070925 00295 EA 2007 9 25 QXEA200701415 1 20070915 A 3297 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA ANTI SKID SYS SHORTED A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 606QX 10023 PDX - FLIGHT 2352- AFTER PUSH BACK RECEIVED A ANTI-SKID CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENANCE FOUND GROUN DING SHORT INSIDE CONNECTOR FOR NR 1 WHEEL SPEED TRANSDUCER. REPINNED PLUG AND GROUND SHIELD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007092500298 20070925 00298 NM 2007 9 25 SWAA074556 1 20070913 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 731, STR 23R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007092500299 20070925 00299 EU 2007 9 25 07FDEA03955 1 20070919 A 5320 A25572046200 STRUT AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 FOUND DAMAGED AT CROSS STRUT BETWEEN FRAME 68, STRG 38-45 LT. REPLACEMENT OF THE CROSS STRUT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092500300 20070925 00300 EU 2007 9 25 07FDEA03956 1 20070919 A 5330 A53611658204 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 EXFOLIATION CORROSION FOUND ON LT FWD PAX DOOR FRAMING AFT PANEL AT FRAME 16A, STRG 25 (IN A HOLE ATTACHING THE SCUFF PL ATE). REPAIR PERFORMED BY PARTIALLY REPLACEMENT THE AFFECTED SKIN PANEL: CUT OUT OF THE AFT DOOR SKIN PANEL AT STRG 23 AND INSTALLING NEW ONE AS PER DRW R536-11030 ISSUE B IAW EA 6-5312-81098 AND RAS/AS/0006/2005 ISSUE B. 2 L 7 2 4F RT A35EU 2007092500301 20070925 00301 NM 2007 9 25 SWAA074588 1 20070913 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007092500302 20070925 00302 EU 2007 9 25 07FDEA03957 1 20070919 A 5313 A53974202208 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT STRINGER P 45LH BETWEEN C 63-65 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007092500304 20070925 00304 EU 2007 9 25 07FDEA03958 1 20070919 A 5313 A53974203 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION ON STRINGER P 45 LT, C67-69 AND P 48 LT, C 65-66 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007092500306 20070925 00306 EU 2007 9 25 07FDEA03959 1 20070919 A 5754 A57844203 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 FOUND CHAFING MARKS ON LT SLAT NR 2 ON LEADING EDGE BETWEEN SLAT TRACK 5 AND TRACK 6. REPAIR PERFORMED BY FLUSH DOUBLER SKIN INSERT IAW SRM 57-41-12/FIG 204. 2 L 7 2 4F RT A35EU 2007092500308 20070925 00308 EU 2007 9 25 07FDEA03960 1 20070919 A 5313 A53778392200 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT STRINGER P 51 LT, C 37-38 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007092500311 20070925 00311 NM 2007 9 25 SWAA074573 1 20070913 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092500313 20070925 00313 NM 2007 9 25 SWAA074560 1 20070913 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007092500315 20070925 00315 NM 2007 9 25 SWAA074554 1 20070913 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 344, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007092500320 20070925 00320 NM 2007 9 25 SWAA074574 1 20070913 A 5311 6546549 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092500324 20070925 00324 NM 2007 9 25 SWAA074607 1 20070913 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092500325 20070925 00325 NM 2007 9 25 SWAA074585 1 20070913 A 5315 6546811 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986, LBL 45 TO RBL 45. REPAIRED FLOORBEAM CHORD PER ER. 2 L 7 2 4F RT A16WE 2007092500328 20070925 00328 NM 2007 9 25 SWAA074595 1 20070913 A 5330 6550570 SKIN BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007092500332 20070925 00332 NM 2007 9 25 SWAA074608 1 20070913 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092500333 20070925 00333 NM 2007 9 25 SWAA074609 1 20070913 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R ABD STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092500334 20070925 00334 NM 2007 9 25 SWAA074572 1 20070913 A 5311 65C25230 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092500335 20070925 00335 NM 2007 9 25 SWAA074571 1 20070910 A 5754 65C26601 SLAT BOEING 737 7373A4 1384585 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 5 L/E SLAT CRACKED AT INBOARD LOWER END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007092500338 20070925 00338 NM 2007 9 25 SWAA074566 1 20070913 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092500342 20070925 00342 NM 2007 9 25 SWAA074578 1 20070913 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092500343 20070925 00343 NM 2007 9 25 SWAA074579 1 20070913 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092500344 20070925 00344 NM 2007 9 25 SWAA074580 1 20070913 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092500345 20070925 00345 NM 2007 9 25 SWAA074581 1 20070913 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092500346 20070925 00346 NM 2007 9 25 SWAA074575 1 20070913 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092500349 20070925 00349 NM 2007 9 25 SWAA074601 1 20070913 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED 18Y CHECK, FOUND STRINGER 18R CRACKED AT BS 947. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007092500350 20070925 00350 NM 2007 9 25 SWAA074587 1 20070913 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER 23R CRACKED AT BS 500A. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007092500351 20070925 00351 NM 2007 9 25 SWAA074586 1 20070913 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER 22R CRACKED AT BS 494. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007092500352 20070925 00352 2007 9 25 SWAA074602 4 20070913 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007092500354 20070925 00354 2007 9 25 SWAA074551 4 20070910 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED RON CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007092500356 20070925 00356 EA 2007 9 25 DATA200700008 2 20070912 A 7261 AS3209017114 SEAL PWA STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA RT ENGINE BLEW OUT E DATA E ENGINE SHUTDOWN A FLAME/FIRE UK UNKNOWN 1 GL 13 336MV SH3018 PCE84172 RIGHT ENGINE CAUGHT FIRE DURING ENGINE START. AIRCRAFT WAS ON THE GROUND BEFORE FLIGHT. EVIDENCE OF ENGINE OIL ON PROP BLADES AND FUSELAGE. REPLACED SEALS TO PRESSURE OIL TRANSFER TUBE TO POWER SECTION MODULE. NO FIRE DAMAGE WAS NOTED O N ENGINE OR AIRCRAFT. TWO SEALS FAILED, AS3209-017, AS3209-114. 2 H 7 2 4T 4 T A41EU E4EA 2007092500358 20070925 00358 EU 2007 9 25 2007UALA02443 1 20070706 A 3510 SHUTOFF VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE O2 SYSTEM LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 420UA 489 THE O2 DECREASED TO 50 PSI AT CRUISE FL 380. LEAK AT SHUTOFF VALVE IN CAPTAIN`S SYSTEM. LEAK WAS STOPPED AND SYSTEM WA S SERVICED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092500360 20070925 00360 NM 2007 9 25 2007UALA03194 1 20070816 A 3350 150129 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 516UA 24860 AISLE EMERGENCY LIGHT AT SEAT 27D IS INOP. ON TROUBLESHOOTING FOUND THAT LIGHT LAMP WAS BAD. REMOVED AND INSTALLED NEW LAMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092500362 20070925 00362 2007 9 25 2007UALA03257 4 20070817 A 2565 416N250110 WEBBING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE FRAYED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 DOORS 1L, 1R, 2L & 4L SLIDE HARNESS WEBBINGS ARE FRAYED. REMOVED AND REPLACED DOOR 4L SLIDE HARNESS WEBBING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092500363 20070925 00363 NE 2007 9 25 2007UALA03292 2 20070820 A 7250 TURBINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE DAMAGED A UALA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 592UA 28143 727118 CREW REPORTED HIGH LEFT SIDE VIBRATION AT HIGHER POWER SETTINGS. FOUND LAST 2 STAGES LPT DAMAGED AND METAL IN TAILPIPE. REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092500364 20070925 00364 NM 2007 9 25 2007UALA03317 1 20070821 A 7910 1A8211 MANIFOLD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OIL SYSTEM CRACKED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 559UA 26657 FLIGHT DIVERTED DUE TO NR 2 ENG LOSS OF OIL QTY AND LOW OIL PRESSURE. REPORT OF BREATHER MANIFOLD CRACKED AND CLAMP BRO KEN. NO DEBRIS FOUND. REPLACED MANIFOLD AND SECURED COWLING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092500365 20070925 00365 NM 2007 9 25 2007UALA03366 1 20070823 A 5710 STRUCTURE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT WING LEAKING A UALA O OTHER W K INADEQUATE Q C FLUID LOSS CL CLIMB 1 WP 29 659UA 27114 LEFT MAIN FUEL QTY DECREASED WITH LT CENTER FUEL PUMP ON AND 30,000 LBS IN CENTER TANK. AFTER TROUBLESHOOTING, FOUND LT FUEL TANK DRY BAY HAS RUNNING FUEL LEAK. RESEALED LEAK AT BOTTOM STRINGER BETWEEN LEFT TANK AND OUTBOARD OF DRYBAY AT 1700. ACCOMPLISHED LEAK CHECK; NO LEAKS. FUEL BALANCED. ACCOMPLISHED ADDÕL TROUBLESHOOTING ON LAYOVER; NO FAULTS NOTE D. CHANGED LEFT CENTER TANK OVERRIDE PUMP PRECAUTIONARY. NO FURTHER REPORT OF FUEL IMBALANCE PROBLEM. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092500366 20070925 00366 EU 2007 9 25 2007UALA03373 1 20070823 A 2730 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED CL CLIMB 1 WP 29 478UA 1533 AFTER TAKEOFF, EXPERIENCED AC PITCH UP ATTITUDE, HAD TO HOLD CONSTANT PRESSURE OF NOSE DOWN TO CORRECT. SYS OK WITH AUT O PILOT ON. TURNED OFF ELAC 2 AND NOW PITCH PROBLEM RESOLVED. NO FAULT OR ECAM WARNINGS PRESENT. NR 2 ELAC OVERHEAT A ND TRANSDUCER FAILURE IN CAPT SIDESTICK. REPLACED NR 2 ELAC AND NR 2 ELAC COMPUTER. ALSO REPLACED CAPT SIDESTICK TRANS DUCER 4CE1 DUE TO RELATED FAULTS FOUND. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092500369 20070925 00369 NM 2007 9 25 2007UALA03658 1 20070910 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 518UA 24871 L1 DOOR HANDLE BOX CRACKED. 10-11-07 REMOVED AND REPLACED HANDLE BOX ASSEMBLY FOR DOOR 1L. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092500370 20070925 00370 NM 2007 9 25 2007UALA03659 1 20070910 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN MISINSTALLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY LIGHT STRIP ON UD STAIRS NOT PROPERLY ATTACHED. 10-11-07 REINSTALLED EMERGENCY LIGHT STRIP ALONG STAIRWAY. REPLACED EEL POWER SUPPLY CABLE TO SAME. CHECKED EMERGENCY LIGHTS IN STAIRWELL. CK OK 2 L 7 4 4F 4 F RT A20WE E24NE 2007092500371 20070925 00371 NM 2007 9 25 2007UALA03660 1 20070911 A 3350 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 LEFT OVERWING EMERGENCY EXIT LIGHTS INOP, 4 EACH. 10-11-07 REPLACED FUSES, OP CHECKED OK 2 L 7 4 4F 4 F RT A20WE E24NE 2007092500372 20070925 00372 NM 2007 9 25 2007UALA03662 1 20070910 A 2560 GIRT BAR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EVAC SLIDE OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 928UA 26651 FWD GALLEY DOOR EVAC SLIDE GIRT BAR HANGING OUT TOO FAR. NEEDS REPACK. REMOVED SLIDE COVER AND TUCKED IN GIRT BAR MATE RIAL. VERIFIED SAFETY PIN IN POCKET. REINSTALLED SLIDE COVER ON THE FWD GALLEY DOOR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092400109 20070924 00109 NM 2007 9 24 AALA20071718 1 20070910 A 5610 141W74001 WINDOW BOEING 777 777223 1385213 NM COCKPIT CRACKED A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 750AN 30259 LHR INFLIGHT T292/10SEP ORD TO DEL - CAPTAINS FORWARD WINDSHIELD CRACKED IN FLIGHT AT 37000 FEET WITH ARCING ACROSS HEAT ER ELEMENT. DIVERTED TO LHR FOR REPLACEMENT AND LANDED WITHOUT INCIDENT. REPLACED WINDSHIELD. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007092400110 20070924 00110 NM 2007 9 24 AALA20071717 1 20070910 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 361AA 24042 CDG - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR EXIT SIGN MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007092500004 20070925 00004 SO 2007 9 25 SIMA200726301 1 20070919 A 2150 8152403 ACM EMB 135 EMB135LR 3260305 SO NR 2 SEIZED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 731BE 145356 ON SHUT DOWN, SMOKE AND BURNING ODOR ENTERED COCKPIT, SLIGHTLY VISIBLE SMOKE. CEASED WHEN PACK WAS SELECTED OFF. FOUND NR 2 AIRCYCLE MACHINE SEIZED UP. REMOVED AND REPLACED NR 2 AIRCYCLE MACHINE IAW AMM 21-51-03-00. OPS CHECK GOOD. AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007092500018 20070925 00018 NM 2007 9 25 QXEA200701434 1 20070913 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 599 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - FLOORBOARD NUT PLATE AND FLANGE ARE CORRODED AT STATION 599.0 INBOARD OF LEFT INBAORD SEAT TRACK. REPAIRED IAW SRM 51-40-11, 51-20-11, 51-20-36. 2 H 7 2 4T RT A13NM 2007092500019 20070925 00019 WP 2007 9 25 UPS07850634 1 20070910 A 2560 NUT PLATE DOUG DC8 DC871F 302199D WP GIRT BAR FITTING DEFECTIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:N/A FWD GIRT BAR FITTING IS LOOSE, (NUT PLATE IS BAD). REMOVED AND REPLACED NUT PLATE AND SECURED GIRT BAR FITTING. REF SRM 51-01-21-0. 2 L 7 4 4F RT 4A25 2007092500028 20070925 00028 NM 2007 9 25 QXEA200701444 1 20070920 A 3210 LANDING GEAR BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 409QX 4051 SEA FLIGHT NR 2368: LEFT MAIN GEAR AMBER GEAR UNSAFE RED AND AMBER GEAR HANDLE ADVISORY LIGHTS REMAINED ILLUMINATED AFTE R TAKEOFF. C/W 'GEAR FAILS TO RETRACT' EA CHECKLIST AND ALL 3 GEAR EXTENDED AND RETRACTED NORMALLY. GEAR EXTENDED NORM ALLY UPON APPROACH AND LANDING IN SEA. MAINTENANCE PERFORMED RETRACT AND EXTENSION TEST OF THE LANDING GEAR IAW AMM TAS K 32-31-00-867-801. WAS UNABLE TO DUPLICATED DISCREPANCY. REMOVED BOTH RT AND LT MLG RETRACTION ACTUATORS IAW AMM TASK 32-31-11-000-801. PERFORMED VERIFICATION AND ADJUSTMENT OF THE ACTUATORS ROD ENDS IAW RD 8/4-32-059 AND SCR 086-07 REV C. REINSTALLED BOTH MLG RETRACTION ACTUATORS IAW AMM TASK 32-11-400-801. PERFORMED BLEEDS OF THE PRIMARY EXTENSION AN 2 H 7 2 4T RT A13NM 2007092500029 20070925 00029 WP 2007 9 25 MWEA070213 1 20070910 A 5752 5910051502 TRIM TAB DOUG DC9 DC981 3022081 WP RT AILERON CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 RIGHT WING AILERON TRIM TAB HAS CORROSION UNDER SKIN, OUTBOARD TRAILING EDGE. REMOVED CORROSION AND FABRICATED AND INST ALLED AILERON TRIM TAB. 2 L 7 2 4F A6WE 2007092500030 20070925 00030 NM 2007 9 25 MWEA070211 1 20070910 A 3350 08163065708 LIGHT DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 823ME 49766 EMERGENCY FLOOR TRACK RED LIGHTS AT ROW 20 ARE INOPERATIVE. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A6WE 2007092500044 20070925 00044 NM 2007 9 25 SWAA074520 1 20070911 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B22 13802 NE HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 408WN 27895 DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 184.7. REPAIRED SKIN IAW SRM. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007092500046 20070925 00046 NM 2007 9 25 AALA20071758 1 20070917 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 767AJ 33539 NRT - EMERGENCY LIGHT AT GALLEY NUMBER FIVE LEFT AISLE CENTER INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT GALLEY NUMBER 5 LEFT AISLE CENTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007092500056 20070925 00056 NM 2007 9 25 SWAA074539 1 20070911 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092500081 20070925 00081 EU 2007 9 25 EMB07003 1 20070911 A 3222 SEAL EMB ERJ190 ERJ190100IGW 3260408 EU NLG STRUT UNKNOWN A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 945UW 19000062 FLIGHT 1812, PHL - BOS, CREW STATES, ALTER GEAR RETRACTION EICAS MESSAGE -LG WOW SYS FAIL-. MESSAGE DISAPPEARED AFTER G EAR EXTENSION. RETURNED TO PHL. MAINTENANCE REPACKED THE NOSE STRUT. 2 L 7 2 4F RT A57NM 2007092500085 20070925 00085 SO 2007 9 25 UG8A2007GM07S 1 20070829 A 5730 1159WM54575 SKIN GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE RT WING CHAFED E UG8A K NONE O OTHER IN INSP/MAINT 1 GL 23 5101 5623 550 DURING COMPLIANCE WITH POST FLIGHT INSPECTION IT WAS NOTED THAT THE LT AND RT WING A FLAP TRACK ISLAND HAT PANELS WERE C HAFING THROUGH THE WING TRAILING EDGE FIXED COVE PANEL. MFG ENGINEERING DISPOSITION NR CS117877 RELEASED OUTLINING REPA IR FOR CONDITION. REPAIRED IAW ENGINEERING DISPOSITION AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A12EA E00057EN 2007092500096 20070925 00096 NM 2007 9 25 SB07076 1 20070912 A 7933 56B94 BULB BOEING 737 737301 1384611 NM NR 2 ENGINE FAULTY A USAA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 EA 19 591US 23936 PIT - FLT 1158 EN ROUTE FROM LGA TO PIT, APPROXIMATELY 75 MILES SOUTHEAST OF PIT, CREW NOTICED THE NR 2 ENGINE OIL TEM PERATURE WAS OUT OF LIMITS. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND SHUT DOWN THE NR 2 ENGINE. FLIGHT LA NDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 25 MINUTES. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE OIL TEMPERATURE BULB. OPERATIONAL CHECK GOOD. ACCOMPLISHED ENGINE POWER RUN. OIL TEMPERATUR E INDICATION CHECKED NORMAL PER MM 71-00-44. 2 L 7 2 4F RT A16WE 2007092500100 20070925 00100 CE 2007 9 25 DXTA200702464 1 20070910 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG LOCKED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 304QS 5600408 CO-PILOTS BRAKES GRAB UNEVENLY DURING HIGH SPEED APPLICATION. 09-27-07 BLEED OUT BRAKES ON COPILOTS SIDE AND FOUND AI R, SUSPECTED AIR CAME FROM COPILOTS LT AND RT MASTER CYLINDERS PERFORMED IAW CE560 MM 32-42-01 AND 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007092500119 20070925 00119 EA 2007 9 25 TRAX200701334 1 20070909 A 5210 STEP CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 659CA 10153 ASD LOWER STEP BROKEN. 2 L 7 2 4F RT A21EA 2007092500139 20070925 00139 CE 2007 9 25 DXTA200702468 1 20070911 A 3260 DOWNLOCK SWITCH BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE RT MLG FAILED E DXTA O OTHER P NO WARNING INDICATION LD LANDING 1 GL 07 151QS RK422 DID NOT GET A RT LANDING GEAR GREEN DOWN NR LOCKED INDICATION UPON GEAR EXTENTION. 09-27-07 RESEATED LANDING GEAR D OWN LIGHT CLUSTER SOCKET, NO DEFECTS NOTED, INSPECTED RT MLG DOWNLOCK SWITCH FOR SAFETY AND SECURITY, JACKED ACFT IAW 40 0A MM 32-00-00, OPS CHECKED NORMAL AT THIS TIME, NO FURTHER DEFECTS NOTED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007092500147 20070925 00147 SO 2007 9 25 C2XA07RI078 1 20070910 A 3350 LIGHT EMB 135 EMB135BJ 3260306 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 16501 145145 FLT 2154 - EWR - CREW REPORTED EMERGENCY EXIT ROW 9A LIGHTS INOPERATIVE. EWR MX RESET ACFT ELECTRIC POWER, AND PERFORME D OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007092500151 20070925 00151 CE 2007 9 25 S2YA07006 1 20070908 A 5310 1144300027179 ANGLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FUSELAGE CRACKED A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 91SK 14599 UE91 DURING STRUCTURAL INSPECTION OF THE AIRCRAFT, A CRACK WAS FOUND IN THE LT FUSELAGE TO WING ANGLE. THE ANGLE IS LOCATED NEAR FS 288 IN THE AREA OF STRINGER 10L AND 10R. THE ANGLE WAS CRACKED IN THE RADIUS AT THE FORWARD END: THE CRACK WAS N O GREATER THEN 1.80 INCHES LONG. THIS AREA HAD BEEN PREVIOUSLY REPAIRED, RECORDED AND SUBMITTED ON A 337 DATED 08/15/00. THE DAMAGE WAS REPAIRED IAW REPORT 6873-1 REVISION IR. THE REPAIR CONSISTED OF REPLACING THE OLD DOUBLER WITH A NEW DOU BLER MADE FROM A REPLACEMENT ANGLE P/N 114-430002-7179. THE TIME BETWEEN THE (2) MAJOR REPAIRS WAS 14599.6. 2 L 7 2 4T 4 T RT A24CE E26NE 2007092500172 20070925 00172 EU 2007 9 25 UPS07150645 1 20070912 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 130UP 0814 INSPECTION TYPE:N/A WITH EMERGENCY LIGHTS SWITCH IN DISARM, DISARM LIGHT INOP. PERFORMED ANNUNCIATION LIGHT TEST ON OVE RHEAD LIGHTS, EMERGENCY LIGHTS DISARM WORKS GOOD. NO PROBLEMS FOUND. 2 L 7 2 4F RT A35EU 2007092500174 20070925 00174 EU 2007 9 25 UPS07150653 1 20070914 A 3350 SWITCH AIRBUS A300 A300F4622R 3930360 EU COCKPIT MALFUNCTIONED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 133UP 0816 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT SWITCH IN THE DISARM POSITION DOES NOT DISARM THE LIGHTS. CYCLED SWITCH MANY T IMES TO GET DISARM LIGHT TO ILLUMINATE. T/S PER TSM 33-61-00 COULD NOT DUPLICATE AT THIS TIME. 2 L 7 2 4F RT A35EU 2007092500189 20070925 00189 CE 2007 9 25 GUUA09130702 1 20070913 A 3234 1013841377 HANDLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG FAILED A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 29 69549 9870 UE194 DURING APPROACH LANDING GEAR DID NOT EXTEND ON THE FIRST AND SECOND SELECTION OF THE GEAR SELECTOR KNOB TO THE DOWN POSI TION. RETURNED TO FLL LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR HANDLE. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007092500192 20070925 00192 NM 2007 9 25 NOCA15107 1 20070912 A 2930 7586631 INDICATOR BOEING 767 767324 1385203 NM GE CF6 CF680C2B7 NE HYD SYSTEM LEAKING A NOCA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 767NA 27569 LT HYDRAULIC EICAS MESSAGE ACTION FOUND NR1 ENGINE LT EDP CASE DRAIN PRESSURE INDICATOR LEAKING REPLACED EDP CASE PRESSU RE INDICATOR AND PACKINGS IAW MM 29-11-17OPS AND LEAK CHECK OK. 2 L 7 2 4F 4 F RT A1NM E13NE 2007092500209 20070925 00209 EU 2007 9 25 HEEA117053 1 20070824 A 2697 TERMINAL SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B 60037 NE FIRE WARNING CORRODED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 151AE 3814 ENGINE FIRE WARNING LIGHT ILLUMINATED DURING START UP. CLEANED CORROSION FROM LT REAR FIRE DETECTOR WIRE TERMINALS IAW MM 26-10-10, ASB072760 AND EMM TASK 26-11-00-050-001. PERFORMED OPERATIONAL CHECK WITH PILOT. CHECKS GOOD. 1 G 7 1 3U 3 U H9EU E00054EN 2007092500212 20070925 00212 WP 2007 9 25 MWEA070217 1 20070913 A 5320 5936034501 ANGLE DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 FUSELAGE ANGLE CRACKED ON LOWER FLANGE APPROXIMATELY AT FRAME STATION 994 LONGERON 20 LEFT, JUST ABOVE FLAP BUS CABLE. FABRICATED AN INSTALLED ANGLE. 2 L 7 2 4F A6WE 2007092500217 20070925 00217 EA 2007 9 25 TRAX200701342 1 20070912 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 878AS 7590 STRONG ODOR OF OIL COMING FROM THE PAC'S ON DESCENT, OCCURED BEFORE SWITCHING BLEEDS. 2 L 7 2 4F RT A21EA 2007092500218 20070925 00218 CE 2007 9 25 DXTA200702488 1 20070920 A 2741 SWITCH CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE STAB MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 640QS 5605240 STAB MISCOMPARE CAME ON AFTER LANDING, DIVERTED. 09-28-07 REMOVED & REPLACED FAULTY SWITCH IAW C560XL MM 27-40-00. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007092500221 20070925 00221 NM 2007 9 25 CO1Y200700006 1 20070914 A 7120 AUB7500502 TRUSS FITTING DOUG MD11 MD11 3023602 NM NR 3 ENGINE CORRODED B CO1Y K NONE O OTHER IN INSP/MAINT 1 EA 33 702BC 48504 ON ENGINE NR 3 FORWARD TRUSS FITTING, FOUND 4EA HOLES WITH CORROSION. 2 L 7 3 4F RT A22WE 2007092500254 20070925 00254 EU 2007 9 25 07FDEA03993 1 20070919 A 5730 A57350143 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 CRACK IN TRAILING EDGE OF BOTTOM SKIN PANEL NR 2, ON LT ZONE 575CB TWO HOLES WITH CRACKS IN SKIN. FOR LOCATION SEE EA 6 -5710-81091/PG 3 CRACK LENGTH IN HOLES ABOUT 2 AND 4MM. DOUBLER PLATE INSTALLED, REPAIR PERFORMED IAW. DRW. R573-49237 AND EA 6-5710- 81091. 2 L 7 2 4F RT A35EU 2007092500259 20070925 00259 EU 2007 9 25 07FDEA03997 1 20070919 A 5313 A53776019202 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 SEVERAL OLD MISDRILLED HOLES ON STRINGER 15 LT, BETWEEN FRAME 35-36. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/ FIG 201. 2 L 7 2 4F RT A35EU 2007092500262 20070925 00262 EU 2007 9 25 07FDEA03999 1 20070919 A 5313 A53978278200 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION ON STRINGER SEGMENT P46RH, C 64-65 STRINGER SEGMENT REPAIR PERFORMED BY BLEND OUT UNTIL CORROSION REMOVA L IAW EA 6-5317-81052 AND RAS/DATLS/0002039/2004 ISS A. 2 L 7 2 4F RT A35EU 2007092500266 20070925 00266 EU 2007 9 25 07FDEA04002 1 20070919 A 5320 A53811642200 SPLICE AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT C39,P 55, BOTTOM SPLICE. REPAIR PERFORMED BY REWORK OF CORROSION IAW RAS 032422/009/2004 ISS A. 2 L 7 2 4F RT A35EU 2007092500279 20070925 00279 NM 2007 9 25 SWAA074589 1 20070913 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED MV2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007092500296 20070925 00296 NM 2007 9 25 SWAA074555 1 20070913 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 482B, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007092500303 20070925 00303 NM 2007 9 25 SWAA074568 1 20070910 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 929, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007092500305 20070925 00305 NM 2007 9 25 SWAA074596 1 20070913 A 5330 6545776 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 938, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007092500307 20070925 00307 NM 2007 9 25 SWAA074614 1 20070913 A 5311 6545805 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092500310 20070925 00310 NM 2007 9 25 SWAA074565 1 20070913 A 5753 6546431279 SKIN BOEING 737 7373A4 1384585 NM FORE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND LEFT WING OUTBOARD FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007092500312 20070925 00312 NM 2007 9 25 SWAA074559 1 20070913 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007092500318 20070925 00318 NM 2007 9 25 SWAA074610 1 20070913 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092500330 20070925 00330 NM 2007 9 25 SWAA074564 1 20070913 A 5753 6573731 SKIN BOEING 737 7373A4 1384585 NM MID FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD MID FLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007092500331 20070925 00331 NM 2007 9 25 SWAA074591 1 20070913 A 5753 6573732 FLAP BOEING 737 7375H4 138449D NM MID FLAP SEPARATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED 18Y CHECK, FOUND RT WING OUTBOARD MID FLAP T/E SKIN SEPARATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007092500339 20070925 00339 NM 2007 9 25 SWAA074583 1 20070913 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092500341 20070925 00341 NM 2007 9 25 SWAA074577 1 20070913 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092500359 20070925 00359 NM 2007 9 25 2007UALA02759 1 20070720 A 3260 106122629 SWITCH BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU GROUND SENSING INTERMITTENT A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 346UA 24250 RTFL WITH NAVIGATION ISSUES. FOUND INTERMITTENT S105 SWITCH IN GROUND SENSING AREA. REPLACED SWITCH S105. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092500367 20070925 00367 NE 2007 9 25 2007UALA03656 2 20070907 A 7261 SEAL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 432UA 587 V10897 HIGH OIL CONSUMPTION EXCEEDS LIMITS. NR 1 ENG USED 6 QTS OF OIL DURING 2 HOUR FLIGHT. 10-11-07 FOUND NR 5 BEARING S EAL LEAKING OIL. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092500373 20070925 00373 NM 2007 9 25 2007UALA03663 1 20070911 A 5310 DOOR FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 928UA 26651 FWD CARGO DOOR CUTOUT, AFT FRAME CRACKED AT INBOARD RADIUS ABOVE LOWER STOP FITTING AND IN WEB INBOARD OF FITTING AT UPP ER BOLT. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED & INSTALLED EXTERNAL NESTED ANGLE & FILLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092500374 20070925 00374 NM 2007 9 25 2007UALA03665 1 20070911 A 3350 EPSU AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 812UA 850 RIGHT EPSU FAULT ON EMERGENCY LIGHT TEST. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092500376 20070925 00376 NM 2007 9 25 2007UALA03668 1 20070911 A 5310 DOOR FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 928UA 26651 FWD CARGO DOOR CUTOUT, AFT FRAME CRACKED AT INBOARD RADIUS ABOVE LOWER STOP FITTING AND IN WEB INBOARD OF FITTING AT UPP ER BOLT. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED EXTERNAL NESTED ANGLE & FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092500377 20070925 00377 2007 9 25 2007UALA03669 4 20070911 A 2312 VHF COMM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 416UA 479 FLT CREW EXPERIENCED DIFFICULTIES TRANSMITTING VIA VHF RADIO SHORTLY AFTER TAKEOFF. DECISION MADE TO DIVERT FLIGHT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092500379 20070925 00379 NM 2007 9 25 2007UALA03671 1 20070911 A 3350 INVERTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 508UA 24744 EMERGENCY EXIT LIGHTS INOP AT ROWS 9-11, 16 & 19. 10-05-07 REPLACED INVERTER AT ROW 9 AND OPERATIONS NORMAL FOR ROWS 9-11. REPLACED SEAT LIGHTS AT ROWS 16 AND 19 AND OPERATIONS CK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092500380 20070925 00380 NM 2007 9 25 2007UALA03672 1 20070911 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 518UA 24871 R-2 DOOR HANDLE BOX CORRODED. 10-05-07 REPLACED DOOR 2R HANDLE BOX. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092500381 20070925 00381 NM 2007 9 25 2007UALA03673 1 20070911 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 518UA 24871 R-1 DOOR HANDLE BOX CRACKED. 10-05-07 REPLACED DOOR 1R HANDLE BOX. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092500382 20070925 00382 NM 2007 9 25 2007UALA03674 1 20070911 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 518UA 24871 LWR GATE CORRODED ALL THE WAY THROUGH FROM INSIDE TO OUTSIDE SURFACE. 10-05-07 REPLACED LOWER GATE 2 L 7 2 4F 4 F RT A2NM E17NE 2007092500383 20070925 00383 NM 2007 9 25 2007UALA03675 1 20070911 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1640 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 518UA 24871 FLOORBEAM UPPER SURFACE AT STA 1640 AND RBL 77 IS CORRODED. 10-05-07 MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED TEE CAP SECTION, FABRICATED T-CAP REPAIR PARTS AND INSTALLED BETWEEN LBL 25 TO RBL 77. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092500385 20070925 00385 EU 2007 9 25 07FDEA03961 1 20070919 A 5313 A53778391202 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT STRINGER 50L, C 37 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007092500386 20070925 00386 EU 2007 9 25 07FDEA03962 1 20070919 A 5730 A57350143 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 ELONGATED HYDRAULIC FITTING HOLES ( 2 AND 4 ) AT PYLON SUPPORT BRACKET, BOTTOM WING SKIN LT, RIB 8. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLATION OF BUSHINGS IAW EA 6-5720-81089 AND RAS/BAE/100174/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007092500388 20070925 00388 EU 2007 9 25 07FDEA03964 1 20070919 A 5313 A53778392200 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT STRINGER P 52LT, C 38.1-38.2. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007092500395 20070925 00395 EU 2007 9 25 07FDEA03970 1 20070919 A 5313 A53773461206 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 807FD 492 FOUND OLD CUTTED STRINGER FLANGE AT STRINGER 54 RT, BETWEEN FRAME 21-22, NOT CONFORM TO SRM REPAIR CRITERIAS. REPLACEME NT OF STRINGER IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092500396 20070925 00396 NM 2007 9 25 07FDEA03971 1 20070919 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 755 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 MAIN DECK CARGO COMPARTMENT SEAT TRACK STA 755, X= 8.5 FOUND EDGE CHIPPED. 10-04-07 REPAIRED BY SECTIONAL SEAT TRACK R EPLACEMENT. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007092500397 20070925 00397 EU 2007 9 25 07FDEA03972 1 20070919 A 5754 SKIN AIRBUS 310 A310324 3930206 EU NR 3 SLAT DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 DENT ON OUTER SKIN LOWER GIRDER AREA AT OUTBOARD BAY OF RT SLAT NR 3. THE DEPTH OF DENT IS 2, 4MM, SPAN WISE WIDE OF 30 MM AND CHORD WISE WIDE OF 38MM. REPAIR PERFORMED BY FILLING DENT WITH FILLERALU (MAT 05-051) OR HYSOL EA9394 AS PER SRM 51-73-10 / PARA.3.C, NIL CRACK FINDINGS DURING HFEC INSPECTION. ALL IAW EA 6-5744-81083 AND RAS/SA/155/2004 ISSUE A. 2 L 7 2 4F RT A35EU 2007092500398 20070925 00398 EU 2007 9 25 07FDEA03973 1 20070919 A 5313 A53974203228 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION ON STRINGER P56 LT, C65-69 STRINGER REPAIR PERFORMED IAW. SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007092500400 20070925 00400 EU 2007 9 25 07FDEA03975 1 20070919 A 5320 A25572173202 FLOOR SUPPORT AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA L ABORTED APPROACH O OTHER IN INSP/MAINT 1 SO 25 807FD 492 CORROSION ON LONGITUDINAL PROFILE (LONGERON) BETWEEN FRAME 67-69, STRG 44 RTS. REPLACEMENT OF LONGERON IAW SRM 51-72-10 . 2 L 7 2 4F RT A35EU 2007092500401 20070925 00401 EU 2007 9 25 CPCP20070100 1 20070824 A 5320 FLOOR SUPPORT AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 414WF 414 RT FLOOR SUPPORT BETWEEN FRAME 36 TO 38 IS CORRODED. RT FLOOR SUPPORT BETWEEN 36-38 REPLACED IAW SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007092500402 20070925 00402 EU 2007 9 25 CPCP20070101 1 20070824 A 5320 THRESHOLD AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 414WF 414 RT THRESHOLD PLATE AT FRAME 36 IS CORRODED. RT THRESHOLD PLATE REPLACED IAW SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007092500403 20070925 00403 NM 2007 9 25 AWXA200701099 1 20070823 A 5320 146N52468 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 MCN - MAJOR REPAIR - C-11 CHECK - NR 5988769, CORROSION ON CABIN FLOOR SUPPORT, BS 1640 - BS 1660, RBL54 - RBL 55, WL 20 8. REPLACED CABIN FLOOR SUPPORT, BS 1640 - BS 1660, RBL54 - RBL 55, WL 208 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007092500405 20070925 00405 NM 2007 9 25 AWXA200701101 1 20070824 A 5320 146N52466 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 MCN - MAJOR REPAIR - C-11 CHECK - NR 5988773, CORROSION ON CABIN FLOOR SUPPORT, BS 1660 - BS 1681.8, RBL 54, WL 208. RE PLACED CABIN FLOOR SUPPORT, BS 1660 - BS 1681.8, RBL 54, WL 208 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007092500406 20070925 00406 EU 2007 9 25 CPCP20070098 1 20070824 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 414WF 414 RT SEAT TRACK BETWEEN FRAME 36-39 IS CORRODED. RT SEAT TRACK BETWEEN FRAME 36-39 IS REPLACED BY NEW ONE IAW SRM 51-25-0 4. 2 H 7 2 4T RT A53EU 2007092500407 20070925 00407 EU 2007 9 25 CPCP20070107 1 20070822 A 5751 STRUCTURE AEROSP ATR72 ATR72212 8680945 EU LT AILERON CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 414WF 414 LT AILERON, LIGHTING STRIP CORRODED AND DISBONDED ON TOP SURFACE. LT AILERON LIGHTING STRIP REPLACED ON NWRC 180721. 2 H 7 2 4T RT A53EU 2007092500410 20070925 00410 EU 2007 9 25 CPCP20070106 1 20070822 A 5751 CHANNEL AEROSP ATR72 ATR72212 8680945 EU LT AILERON CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 414WF 414 LT AILERON, CLOSING CHANNEL CORRODED. LT AILERON, CLOSING CHANNEL (NEW) REPLACED IAW SRM 51-25-03. 2 H 7 2 4T RT A53EU 2007092500413 20070925 00413 EU 2007 9 25 07FDEA03978 1 20070919 A 5313 A53974202206 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION ON STRINGER P44, C60-62 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007092500415 20070925 00415 EU 2007 9 25 07FDEA03980 1 20070919 A 5313 A53970701 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 CORROSION ON STRINGER 51 AT FRAME 54.3 LT. REPAIR PERFORMED BY REPLACING STRINGER PARTIAL, SPLICE WITH ORIGINAL REINFOR CEMENT BETWEEN FRAME 54.2-54.3 AND STRINGER SPLICE REPAIR IAW SRM 53-10-14/FIG 201 BETWEEN FRAME 54.3-55/58. 2 L 7 2 4F RT A35EU 2007092500417 20070925 00417 EU 2007 9 25 07FDEA03982 1 20070919 A 5315 A53974224200 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION OUT OF LIMIT AT CROSSBEAM C 65 SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 2007092500419 20070925 00419 EU 2007 9 25 07FDEA03984 1 20070919 A 5315 A53974360200 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 HEAVY CORROSION ON CROSSBEAM AT FRAME 67. CROSSBEAM REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092500420 20070925 00420 EU 2007 9 25 07FDEA03985 1 20070919 A 5313 A53974203220 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION ON STRINGER P52 LT, C59 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007092500421 20070925 00421 EU 2007 9 25 07FDEA03986 1 20070919 A 5315 A53974222 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 HEAVY CORROSION ON CROSSBEAM AT FRAME 66. CROSSBEAM SPLICE REPAIR PERFORMED IAW SRM 53-10-15/FIG 207. 2 L 7 2 4F RT A35EU 2007092500422 20070925 00422 EU 2007 9 25 07FDEA03987 1 20070919 A 5313 A53974262202 LONGERON AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 HEAVY CORROSION ON LONGITUDINAL PROFILE (LONGERON) BETWEEN FRAME 66-69 LHS, Y140 OF BULK CARGO COMPARTMENT FLOOR STRUCTU RE. REPLACEMENT OF LONGERON IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092500423 20070925 00423 EU 2007 9 25 07FDEA03988 1 20070919 A 5320 A53974261202 FLOOR SUPPORT AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 HEAVY CORROSION ON LONGITUDINAL PROFILE (LONGERON) BETWEEN FRAME 66-69 LHS, Y805 OF BULK CARGO COMPARTMENT FLOOR STRUCTU RE. REPLACEMENT OF LONGERON IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092500424 20070925 00424 NM 2007 9 25 DHL2007746532 1 20070829 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 720F-740 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 FORWARD CARGO COMPARTMENT, STRINGER 27L IS CORRODED WITH EXFOLIATION FROM BODY STA 720F +10 INCHES TO BODY STA 740. CUT OUT DAMAGED SECTION OF STRINGER 27L STA 720F +10 TO 740 IAW B727 SRM 53-10-3 FIG 1, 10" LONG. REMOVED CORROSION ON SKI N IAW B727 SRM 51-10-6. FOUND CORROSION OUT OF LIMITS. FABRICATED AND INSTALLED REPAIRS FOR STRINGER AND SKIN IAW B727 SRM 53-10-3 FIG 1 AND COTNEY EO NR AE03-53-101 REV IR. ALL PARTS AND AREA TREATED AND PRIMED IAW B727 SRM 51-10-2. RE PAIR PARTS: STRINGER FROM BAC1498-147, 11.159 INCH LONG, PO NR 7178178, SPLICE FROM BAC1498-131, 9.25" LONG, PO NR 40038 66, DOUBLER FROM 2024-T3 .160" BY 21" BY 15.5" PO NR 900844, FILLER REPAIR FROM 2024-T3, .080" BY 22" BY 11.75", PO NR71 2 L 7 3 4F A3WE 2007092500425 20070925 00425 NM 2007 9 25 2007UALA03677 1 20070911 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 795UA 26927 SEAT 36C EEL LIGHT IS INOP. 10-05-07 REPLACED LIGHT. CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007092500426 20070925 00426 NM 2007 9 25 2007UALA03678 1 20070910 A 2997 CONNECTOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE HYD PUMP DAMAGED A UALA O OTHER M OVER TEMP NR NOT REPORTED 1 WP 29 799UA 26926 HYD PUMP DEM C2 LOW CENTER HYDRAULIC DEMAND PUMP NR 2 PRESSURE WHEN COMMANDED ON, OR CENTER DEMAND PUMP NR 2 OVERHEATED. 10-05-07 AFTER TROUBLESHOOTING & HISTORY REVIEW, DETERMINED THAT NR 2 CONTROL HYD PUMP OPERATED OK FOR SEVERAL LEG S AFTER PIN D7716B (OF WDM29-11-40) WAS REPOSITIONED. REMOVED CONNECTOR PINS AND RE-PINNED UNIT. TESTED OK FOR SERVICE . 2 L 7 2 4F 4 F RT T0001SE E46NE 2007092500429 20070925 00429 NM 2007 9 25 2007UALA03681 1 20070912 A 3350 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY CEILING LIGHTS INOP AT ROW 13 & ROW 32L. 10-5-07 RELAMPED EMERGENCY CEILING LIGHTS IN BOTH SEAT POSITIONS. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092500431 20070925 00431 NM 2007 9 25 2007UALA03684 1 20070911 A 2750 FLAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU WING MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 305UA 23666 CREW COMMENTS: FLAPS STOPPED AT 27 DEGREES AND WOULD NOT MOVE MORE OR LESS. REPLACED FLAP INDICATOR UNIT. FLAP LOCKOU T OCCURRED BECAUSE THERE WAS A F LAP NEEDLE SPLIT, MOST LIKELY ENOUGH TO LOCK OUT FLAPS ASYMETRY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092500434 20070925 00434 EU 2007 9 25 2007UALA03687 1 20070913 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 445UA 826 EXTERNAL FUSELAGE SKIN 7 INCH AFT OF FRAME 70 BETWEEN STR 41R AND 42R IS DAMAGED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092500435 20070925 00435 NM 2007 9 25 2007UALA03688 1 20070912 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 518UA 24871 FUSELAGE SKIN GOUGED AROUND DRILLED OFF SCREW SHANK, STA 1304, STR 19L, AT LEFT HAND FUSELAGE BODY FAIRING. 10-5-07 M AJOR REPAIR ACCOMPLISHED. CUTOUT DAMAGE AND INSURE CUT. FABRICATED DOUBLER AND INSTALLED REPAIR AS PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092500436 20070925 00436 NM 2007 9 25 2007UALA03689 1 20070912 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMEGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 643UA 25093 EMERGENCY CEILING LIGHT AT ROW 17AB INOP. 10-5-07 FOUND LAMP ASSY BROKEN. REPLACED LAMP ASSY. OP CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092500438 20070925 00438 NM 2007 9 25 2007UALA03691 1 20070912 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 643UA 25093 EMERGENCY EEL LIGHTS FROM ROW 28AB-35AB INOP. 10-5-07 FOUND SMALL SECTION AT AFT GALLEY LIGHT STRIP (15" CROSS AISLE ) SHORTING OUT THE WHOLE SECTION. REPLACED 15 INCH CROSS AISLE EEL STRIP IN AFT GALLEY -- EEL LIGHTS CK OK 28AB THRU 35A B. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092500441 20070925 00441 EU 2007 9 25 2007UALA03694 1 20070912 A 3510 MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT LEAKING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 473UA 1469 F/O'S OXYGEN HARNESS FAILS TO INFLATE, IS LEAKING. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092500442 20070925 00442 NM 2007 9 25 DHL2007746527 1 20070831 A 5344 MS20001167200 HINGE BOEING 727 727224 1384076 NM BS 640 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 EXTERNAL FUSELAGE BODY STATION 640 WL 299 MCD FUSELAGE SIDE AFT MOST HINGE SEGMENT AFT LOBE IS CRACKED. REMOVED AFT SEC TION OF MCD HINGE IAW B727 SRM 51-30-2. FABRICATED NEW HINGE FROM MS20001-16-7200 PO NR 9002527 DIMENSION 17 7/8" BY 4 1/4" IAW AEI BOEING 727-200 FREIGHTER M/M CHAPTER 52 FIG 52 01B PAGE 18. ALODINE AND PRIMED IAW B727 SRM 51-10-2. INST ALLED NEW HINGE AT MCD BODY STATION 640 WL 299 IAW AEI BOEING 727-200 FREIGHTER M/M CHAPTER 52 FIG 52 01B. OPS/CHECK GO OD IAW B727-200 FREIGHTER MM CHAPTER 52. 2 L 7 3 4F A3WE 2007092500443 20070925 00443 2007 9 25 HNAA0700166 4 20070807 A 3442 MI5853512RECON DISPLAY DHAV DHC8 DHC8311 1386006 EA WEATHER RADAR FADED A HNAA D RETURN TO BLOCK O OTHER CR CRUISE 1 EA 07 331EN 31861 194 279 RADAR SCREEN FADED AND HARD TO READ. AFTER AIRCRAFT DEPARTED PHL, DISPATCH HAD ACFT RETURN TO FIELD, TO REPAIR RADAR. REMOVED AND REPLACED WEATHER RADAR SYSTEM. OPS CHECKS GOOD. 2 H 7 2 4T RT A13NM 2007092500444 20070925 00444 NM 2007 9 25 07FDEA03953 1 20070918 A 5740 ARC7490501 TEE FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 AFTER BUSHING REMOVAL, LEFT HAND WING INBOARD FLAP VANE INBOARD TEE FITTING BORE FOUND CORRODED. LEFT HAND WING INBO ARD FLAP VANE INBOARD TEE FITTING REMOVED AND REPLACED AS PER AMM 27- 50-22-4. FLAP OPERATION TEST CARRIED OUT AS PER AMM 27-50-00-860-801. 2 L 7 3 4F RT A22WE 2007092500445 20070925 00445 EA 2007 9 25 S9BA1407 1 20070717 A 5753 ARM DHAV DHC6 DHC6300 2802606 EA FLAP HINGE CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 888PV 620 LEFT HAND I/B FORE FLAP O/B HINGE ARM CORRODED. REMOVED AND REPLACED FORE FLAP 1 H 7 2 3T RT A9EA 2007092600001 20070926 00001 NM 2007 9 26 HALA0700408 1 20070923 A 3150 WARNING LIGHT BOEING 717 717200 1383700 NM STAB FALSE ACTIVATION A HALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 13 479HA 55124 T/O ABORT DUE TO STABILIZER AURAL WARNING, EAD TURNING RED. PERFORMED RTS ON NR 1 AND NR 2 VIA AND NR 1 AND NR 2 FCC ST AB TRIM. ALL TEST PASS PER MM 31-61-00 AND 22-10-00 OK FOR SERVICE. 2 L 7 2 4F TR A6WE 2007092600002 20070926 00002 NM 2007 9 26 HALA0700409 1 20070923 A 3230 INDICATION SYS BOEING 717 717200 1383700 NM MLG MALFUNCTIONED A HALA O OTHER N FALSE WARNING LD LANDING 1 WP 13 476HA 55118 GEAR EXTENTION FOR LANDING PROCEDURE UNSAFE INDICATIONS ON BOTH THE GEAR DOWN LIGHTS AND CONFIG PAGE GEAR RECYCLED AND A PPEARED NORMAL. NO FAULTS NOTED. PERFORM FIM 32-60 TASK 803 CHECK OK. OK FOR SERVICE PER FIM. 2 L 7 2 4F TR A6WE 2007092600003 20070926 00003 NM 2007 9 26 HALA0700410 1 20070923 A 3350 3305087 BATTERY BOEING 767 767332 1382001 NM EMERGENCY LIGHTS INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 597HA 23277 AISLE EMERGENCY LIGHTS BETWEEN SEATS 16AB THRU 24AB AND 16HJ THRU 24HJ EXTINGUISHED WITH TEST SWITCH ON. REMOVED AND RE PLACED BATTERY POWER SUPPLY AT SEAT 17AB AMM 33-51-07. EMERGENCY LTS TEST NORMAL. 2 L 7 2 4F RT A1NM 2007092600004 20070926 00004 EU 2007 9 26 07FDEA04018 1 20070907 A 5311 R539H01433204 FRAME AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 CORROSION FOUND AT AFT CARGO COMPARTMENT DOOR FRAME - FR59A, BETWEEN STRG 26 RT AND 29 RT. AFT CARGO COMPARTMENT DOOR FRAME WAS REPAIRED BETWEEN STR 26-29 RT IAW FEDEX EA 6-5310-113171. 2 L 7 2 4F RT A35EU 2007092600005 20070926 00005 EU 2007 9 26 07FDEA04019 1 20070919 A 5311 A53610669 FRAME AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 OLD REPAIR ON FRAME 13, STRG 14 LT, FUSELAGE NOSE SECTION. THE REINFORCEMENT REPAIR ANGLE AT FRAME SEGMENT WAS CHAFED A ND AFTER REWORK OUT OF LIMIT. REPAIR PERFORMED BY INSTALLING NEW REPAIR ANGLE AT OLD REPAIR AS PER PRINCIPLE IN SRM 53- 10-13. 2 L 7 2 4F RT A35EU 2007092600006 20070926 00006 EU 2007 9 26 07FDEA04020 1 20070919 A 5311 A53980047244 FRAME AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT FRAME C75A, P11. REPAIR PERFORMED IAW SRM 53-18-13 FIG 202. 2 L 7 2 4F RT A35EU 2007092600007 20070926 00007 EU 2007 9 26 07FDEA04021 1 20070919 A 5315 A53974225 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 HEAVY CORROSION ON CROSSBEAM AT FRAME 69 LT, BULK CARGO COMP FLOOR STRUCTURE. CROSSBEAM REPAIR PERFORMED IAW SRM 53-1 0-15. 2 L 7 2 4F RT A35EU 2007092600008 20070926 00008 EU 2007 9 26 07FDEA04022 1 20070919 A 5320 A53974263202 FLOOR SUPPORT AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 HEAVY CORROSION ON LONGITUDINAL PROFILE (LONGERON) BETWEEN FRAME 66-69 AD, BULK CARGO COMP FLOOR STRUCTURE. REPLACEMENT OF LONGERON IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092600009 20070926 00009 EU 2007 9 26 07FDEA04023 1 20070827 A 5753 SKIN AIRBUS 310 A310222 3930315 EU TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 PREVIOUS REPAIR FOUND LOCATED ON LT INBD LOWER SKIN, T/E RIB 2-4. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINAT ION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND EXISTING REPAIR WAS FOUND DEBONDED AND WAS REMOVED. NEW REPAIR WAS INSTALLED PER EA 6-5710-113162. 2 L 7 2 4F RT A35EU 2007092600010 20070926 00010 EU 2007 9 26 07FDEA04024 1 20070919 A 5315 A53974219 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 HEAVY CORROSION ON CROSSBEAM AT FRAME 63 RT, CARGO COMP FLOOR STRUCTURE. CROSSBEAM REPAIR PERFORMED IAW SRM 53-10-15. 2 L 7 2 4F RT A35EU 2007092600011 20070926 00011 EU 2007 9 26 07FDEA04025 1 20070919 A 5310 A53980070210 BOX BEAM AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 CORROSION AND CRACKS FOUND ON RT AFT PAX DOOR UPPER TORSION BOX BEAM, C 73-75A, P 9-11. REPAIR PERFORMED BY CUT OUT TH E DAMAGED PARTS, INSTALLING REPAIR PART AND FILLER IAW EA 6-5318-81066 AND RAS/DAHAM/4018653/2004 ISS A. 2 L 7 2 4F RT A35EU 2007092600014 20070926 00014 EU 2007 9 26 07FDEA04028 1 20070827 A 5753 SKIN AIRBUS 310 A310222 3930315 EU TE FLAP FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 PREVIOUS REPAIR FOUND LOCATED ON LT OUTBOARD FLAP, UPPER SKIN, MAIN SPAR RIB 2. REPAIR REQUIRES EVALUATION FOR MAJOR/MI NOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS EVALUATED AND FOUND NOT CONFO RM TO SRM. A NEW REPAIR WAS ACCOMPLISHED IAW FEDEX EA-6-5710-113163. 2 L 7 2 4F RT A35EU 2007092600015 20070926 00015 EU 2007 9 26 07FDEA04029 1 20070919 A 5313 A53970701 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 DURING NON ROUTINE DR0115, FOUND CORROSION ON STRINGER 51 LT, BETWEEN FRAME 54.1-54.2. PARTIAL STRINGER REPLACEMENT WIT H SPLICE REPAIR PERFORMED, BETWEEN FRAME 54.1-54.2 IAW SRM 53-10-14/FIG 201 AND 54.2-54.3 (DR0115). 2 L 7 2 4F RT A35EU 2007092600018 20070926 00018 EU 2007 9 26 07FDEA04032 1 20070919 A 5753 A57970330002 RIB AIRBUS 310 A310324 3930206 EU TE FLAP NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 OLD REPAIR ON LT INBOARD FLAP AT END RIB 21. CUSTOMER DECISION TO FINAL REPAIR PER SB A310-57-2055, REPLACEMENT OF END RIB 21. 2 L 7 2 4F RT A35EU 2007092600019 20070926 00019 EU 2007 9 26 07FDEA04033 1 20070919 A 5100 A57970330003 RIB AIRBUS 310 A310324 3930206 EU ZONE 600 NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 OLD REPAIR ON RT INBOARD FLAP AT END RIB 21. CUSTOMER DECISION TO FINAL REPAIR PER SB A310-57-2055, REPLACEMENT OF END RIB 21. 2 L 7 2 4F RT A35EU 2007092600020 20070926 00020 EU 2007 9 26 07FDEA04034 1 20070919 A 5330 A53610318 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 807FD 492 FOUND OLD DOUBLER REPAIR BETWEEN FRAME 11-11A, STRG 27-28 LT, NOT CONFORM TO REPAIR REFERENCE AS PER SRM 53-12-12/FIG 20 1. DOUBLER REPAIR RENEWED IAW SRM 53-12-12/FIG 201. 2 L 7 2 4F RT A35EU 2007092600021 20070926 00021 EU 2007 9 26 07FDEA04035 1 20070919 A 5415 A54611915 PANEL AIRBUS 310 A310203 3930313 EU ZONE 400 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 DURING ACCOMPLISHMENT OF EO 6-5450-7-3304 (SB 54-2026 EMBODIMENT) FOUND AT PYLON NR 2 AN OLD CRACK REPAIR AND LOWER SKIN WAVINESS. REPAIR PERFORMED BY STRAIGHTEN OUT THE DENTED AREA AND INSTALLING REPAIR PARTS AND DOUBLER IAW DRAWING R546- 10305, APPROVED BY EA6-5450-81073 AND RAS 032684/009/2004 ISS A. 2 L 7 2 4F RT A35EU 2007092600024 20070926 00024 EU 2007 9 26 07FDEA04038 1 20070919 A 5532 A55373311 PANEL AIRBUS 310 A310203 3930313 EU ZONE 300 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 VERTICAL STABILIZER LEADING EDGE PANEL 322CL WAS DELAMINATED. THE DIMENSION FOR REPAIR IAW SRM TO GREAT. REPAIR PERFOR MED IAW SRM 55-32-00 FIG 203 AND FIG 216, APPROVED BY EA 6-5532-81077 AND RAS/DAHAM/4018735/2004. 2 L 7 2 4F RT A35EU 2007092600025 20070926 00025 EU 2007 9 26 07FDEA04039 1 20070919 A 5753 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 807FD 492 OLD EXTERNAL DOUBLER REPAIR ON INBOARD FLAP RT ON LOWER SIDE BETWEEN RIB 10-11, NOT CONFORM TO OLD RECORDS AS PER SRM 57 -52-12/FIG 204: EXTERNAL DOUBLER IS ON LOWER SURFACE INSTEAD OF UPPER SURFACE, NO FILLER ON UPPER SURFACE INSTALLED AND NO RIVETS ON TRAILING EDGE. REPAIR OF INBOARD FLAP TRAILING EDGE IAW SRM 57-53-12/FIG 208, APPROVED BY EA 6-5752-81107 AND RAS/DABRE/7009414/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007092600027 20070926 00027 EU 2007 9 26 07FDEA04041 1 20070919 A 5753 SKIN AIRBUS 310 A310203 3930313 EU TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 DENT FOUND AT LT INBOARD FLAP, RIB 18-19, P 4-5 REPAIR PERFORMED IAW SRM 57-52-12 FIG 205, APPROVED BY RAS/DABRE/7004356 /2004 ISS A. 2 L 7 2 4F RT A35EU 2007092600028 20070926 00028 EU 2007 9 26 07FDEA04042 1 20070919 A 5730 A57350103201 SKIN AIRBUS 310 A310203 3930313 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND ELONGATED HOLES AT PYLON TO WING HYDRAULIC FITTING HOLES, RT WING BOTTOM SKIN REPAIR PERFORMED IAW DRAWING R572- 59184 (BUSHING REPAIR), APPROVED BY EA 6-5720-81069 AND RAS/BAE/1026/2004 ISS A. 2 L 7 2 4F RT A35EU 2007092600029 20070926 00029 EU 2007 9 26 07FDEA04043 1 20070919 A 5730 A57350103200 SKIN AIRBUS 310 A310203 3930313 EU ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND ELONGATED HOLES AT PYLON TO WING HYDRAULIC FITTING HOLES, LT WING BOTTOM SKIN. REPAIR PERFORMED IAW DRAWING R572- 59184 (BUSHING REPAIR), APPROVED BY EA 6-5720-81069 AND RAS/BAE/1026/2004 ISS A. 2 L 7 2 4F RT A35EU 2007092600032 20070926 00032 EU 2007 9 26 07FDEA04046 1 20070919 A 5730 A57350101202 SKIN PANEL AIRBUS 310 A310203 3930313 EU ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FRETTING DAMAGE ON LT BOTTOM SKIN PANEL NR 2, RIB 8-9 REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5720-8106 8 AND RAS/BAE/1126/2004 ISS A. 2 L 7 2 4F RT A35EU 2007092600035 20070926 00035 EU 2007 9 26 07FDEA04049 1 20070919 A 5313 A53811073200 STRINGER SPLICE AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION ON SPLICE C39, P 47 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092600036 20070926 00036 EU 2007 9 26 07FDEA04050 1 20070919 A 5210 A52175004 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 800 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FOUND GROOVES ON OUTER SKIN PANEL, AFT LOWER CORNER AT AFT PAX DOOR LT, ZONE 833 AND ON SKIN PANEL, LOWER EDGE AREA AT A FT PAX DOOR RT, ZONE 843. REPAIR PERFORMED BY INSTALLING EXTERNAL DOUBLER AS PER SRM 52-11-00/PB 235/PAR 5F/FIG 206 ON LT PAX DOOR AND IAW SRM 52-11-00/PB 217/PAR 5C/FIG 203 ON RT PAX DOOR. 2 L 7 2 4F RT A35EU 2007092600037 20070926 00037 NM 2007 9 26 HALA0700394 1 20070917 A 5300 SEAT TRACK BOEING 767 76733A 1385209 NM BS 927-1053 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 LEVEL 1 CORROSION SECTION 45 SEAT TRACK RBL 54-75. CORROSION AT STATION 927,939, AND 1053. AREAS REWORKED AND FOUND WI THIN LIMITS PER SRM 53-00-52. REWORKED AREAS ALODINED AND PAINTED. 2 L 7 2 4F RT A1NM 2007092600038 20070926 00038 NM 2007 9 26 HALA0700396 1 20070917 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 543-780 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 LEVEL 1 CORROSION ON SEAT TRACK LBL 11, AT STATION 543, 566, 580, 600, 642, 715, AND 780. REWORKED CORROSION. CORROSIO N AREAS FOUND WITHIN LIMITS PER SRM 53-00-52. REWORKED AREAS ALODINED AND PAINTED. 2 L 7 2 4F RT A1NM 2007092600040 20070926 00040 NM 2007 9 26 HALA0700388 1 20070915 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 795-1062 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 LEVEL 1 CORROSION ON SEAT TRACK RBL 11 STA 795, 842, 889, 903, 934, 953, 966, 980, 1016, 1044 AND 1062. REWORKED AREAS WITHIN LIMITS PER SRM 53-00-52. REWORKED AREAS PRIMED AND PAINTED. 2 L 7 2 4F RT A1NM 2007092600041 20070926 00041 NM 2007 9 26 HALA0700385 1 20070918 A 2720 SWITCH BOEING 717 717200 1383700 NM RUDDER CONTROL MALFUNCTIONED A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 486HA 55131 AFTER ENGINE START RUDDER PWR OFF ALERT ILLUMINATED WITH BOTH ENGINES RUNNING, AUX AND HYD TRANS PUMPS ON. CHECKED RUDD ER OPERATION WHICH APPEARED NORMAL. PERFORMED FIM 27-20-00-810, NO DEFAULT NOTED OK FOR SERVICE, 2ND BTB: SWAP TO ACFT 476, ACFT 486. REMOVED AND REPLACED RUDDER CONTROL MANUAL SWT. OPS CHECK OK ACFT RELEASE FOR SERVICE. 2 L 7 2 4F TR A6WE 2007092600042 20070926 00042 EU 2007 9 26 07FDEA04051 1 20070919 A 5310 A52271017200 BEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT EMERGENCY EXIT DOOR, BEAM NR 5 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092600045 20070926 00045 EU 2007 9 26 07FDEA04055 1 20070823 A 5753 A57971301006 SKIN AIRBUS 310 A310222 3930315 EU ZONE 600 DEBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 RT WING, OUTBD FLAP RIB 10 T/E DEBONDING THE REPAIR WAS ACCOMPLISHED IAW FEDEX EA 6-5710-113163. 2 L 7 2 4F RT A35EU 2007092600046 20070926 00046 NM 2007 9 26 HALA0700392 1 20070917 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 1090-1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 LEVEL 1 CORROSION ON SEAT TRACK AT SECTION 46, SEAT TRACK RBL 11. CORROSION AT STATION 1090, 1106, 1197+46, 1197+63, 119 7+96 AND 1197+128. AREAS REWORKED AND FOUND WITHIN LIMITS PER SRM 53-00-52. REWORKED AREAS ALODINED AND PAINTED. 2 L 7 2 4F RT A1NM 2007092600049 20070926 00049 2007 9 26 HALA0700387 4 20070917 A 3422 INDICATOR BOEING 767 767332 1382001 NM COCKPIT INOPERATIVE A HALA O OTHER O OTHER CR CRUISE 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM, F/O RDMI INOP SHOWS HDG FLAG AND APPEARS TO BE UNPOWERED, BOTH DME WINDOWS BLANK. REPLACED F/ O RDMI OPS CHK NML IAW AMM 34-22-05. 2 L 7 2 4F RT A1NM 2007092600050 20070926 00050 NM 2007 9 26 DL764071230 1 20070915 A 3350 BATTERY PACK BOEING 767 767432ER 1385134 NM EMERGENCY LIGHTS NO TEST A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 831MH 29702 EMERGENCY BATTERY PACK M737 FAILS DEEP CYCLE. REMOVED AND REPLACED (M737) EMERGENCY BATTERY PACK. OPS CK GOOD IAW MM 3 3-51-07. 2 L 7 2 4F RT A1NM 2007092600051 20070926 00051 NM 2007 9 26 DL764071231 1 20070914 A 3350 BATTERY PACK BOEING 767 767432ER 1385134 NM EMERGENCY LIGHTS NO TEST A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 831MH 29702 EMERGENCY BATTERY PACK M738 FAILS DEEP CYCLE. REMOVED AND REPLACED M738 EMERGENCY BATTERY PACK OPS CK GOOD IAW B767 MM3 3-51-07 . 2 L 7 2 4F RT A1NM 2007092600053 20070926 00053 NM 2007 9 26 DL764071233 1 20070912 A 3350 BATTERY PACK BOEING 767 767432ER 1385134 NM EMERGENCY LIGHTS NO TEST A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 831MH 29702 EMERGENCY BATTERY PACK M730 FAILS DEEP CYCLE. REMOVED AND REPLACED M730 EMERGENCY BATTERY PACK. OPS CK GOOD IAW B767 M M 33-51-07 . 2 L 7 2 4F RT A1NM 2007092600054 20070926 00054 NM 2007 9 26 DL764071234 1 20070917 A 3520 RELAY BOEING 767 767432ER 1385134 NM PAX OXYGEN FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831MH 29702 PASSENGER OXYGEN SYSTEM FAILS MANUAL DEPLOYMENT CHECK. REMOVED AND REPLACED K466 RELAY IAW BOEING SWP 20-81-11 PASSENGE R OXYGEN SYSTEM MANUAL DEPLOYMENT TEST. OPS CHECKS GOOD IAW B767 MM 35-21-00-705-054. 2 L 7 2 4F RT A1NM 2007092600055 20070926 00055 NM 2007 9 26 DL764071235 1 20070919 A 3350 LIGHT BOEING 767 767432ER 1385134 NM CABIN BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831MH 29702 EMERGENCY LIGHT ASSY AT SEATS 26R, 32L, 43R DAMAGED. REMOVED AND REPLACED BROKEN EMERGENCY LIGHT ASSY AT SEATS 26R,32L, 43R. OPS CK GOOD IAW B767 MM 33-51-01. 2 L 7 2 4F RT A1NM 2007092500130 20070925 00130 NE 2007 9 25 DXTA200702482 2 20070916 A 7200 ENGINE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE RIGHT POWER LOSS E DXTA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 07 147QS RK436 PCEJA0660 ON TAKEOFF FROM SAN T/O POWER COMPUTED AS 99 PERCENT N1. WITH THRUST LEVERS FIREWALLED, LT ENGINE N1 AT 99 PERCENT, RT E NGINE N1 AT 97.8 PERCENT. CONDITIONS AT SAN: SEA LEVEL, 22DEG C WIND 250 AT 7KNTS. 29.95. 2 H 7 2 4F 4 F RT A16SW E25EA 2007092500140 20070925 00140 CE 2007 9 25 DXTA200702470 1 20070911 A 2120 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL COCKPIT SMOKE E DXTA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 07 921QS 7500241 STATIC TAKEOFF: ALL ENGINES AND AIRCRAFT INDICATIONS GOOD. AT 60 KIAS RT SEAT PILOT CALLED FOR ABORT DUE TO SMOKE IN COC KPIT. SMOKE WAS BLUE IN COLOR, OIL ODOR. 09-27-07 CLEANED LEFT AND RIGHT OZONE CONVERTERS IAW CE-750 M/M CHAPTER 21- 71-00. CLEANED COALESCERS (LT & RT) IAW CE-750 MM TASK 12-10-01-160. OPERATIONAL AND LEAK CHECKS GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007092500146 20070925 00146 CE 2007 9 25 DXTA200702484 1 20070918 A 3310 HOLDER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL YOKE DAMAGED E DXTA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 07 921QS 7500241 SMOKE OBSERVED COMING FROM THE PILOTS YOKE CLIP LIGHT WITH THE RHEOSTAT IN THE OFF POSITION. 09-28-07 REPLACED PILOT 'S CHART HOLDER, P/N 10-62-01, AND INSTALLED NEW CHART HOLDER, PN 10-62-01, LIGHTS OPS CHECK GOOD. IAW CE-750 INTERIOR MAINT MANUAL CHAP 25. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007100300030 20071003 00030 CE 2007 10 3 DXTA200702493 1 20070922 A 4940 51989262 STARTER CESSNA 750 750 2076810 CE APU ARCED E DXTA A UNSCHED LANDING B H SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC DE DESCENT 1 GL 07 953QS 702 7500153 DURING DESCENT & STARTING APU, BUS CTRL 2 FAIL CAS MESSAGE CAME ON. BUSS CONTROL SWITCH ON PANEL SWITCHED TO EMERGENCY AUTOMATICALLY WHILE OTHER ASSOCIATAED CAS MSGS. APU ABORTED START SEQUENCE AUTOMATICALLY. RT AVIONICS LOST POWER & EIC AS ONLY DISPLAY LT INFO. COMPLIED WITH BUSS CONTROL FAIL CHECK LIST & LANDED UNEVENTFULLY. STARTED BOTH ENGINES & SHU TDOWN APU. RESTARTED APU & NO FAILURES NOTED BUT APU SLOW TO START WITH A HIGH AMP DRAW. SHUTDOWN APU & RESTARTED ACFT I N AIR MODE & BOTH ENGINES RUNNING. NO ELECTRICAL FAILURES OCCURED BUT APU ONCE AGAIN STARTED SLOW & A HIGH AMP DRAW ON R T BUSS. SHUTDOWN ENGINES & INSPECTED APU STARTER. FOUND APU STARTER POSITIVE TERMINAL LOOSE, BURNED, & MELTED SOLDER ARO 2 L 7 2 4J RT T00007WI 2007092500168 20070925 00168 EU 2007 9 25 HEER117215 1 20070902 A 6230 L623M1006103 ROTOR SHAFT UROCOP EC135 EC135P2 5620027 EU MAIN ROTOR UNBONDED B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 343PH 779 0456 FOUND STRAIN GAUGE UNBONDED WHILE TROUBLESHOOTING MAST MOMENT PROBLEM. REPLACED ROTOR HUB SHAFT ASSY. TO BE SENT TO MF G FOR CORE EXCHANGE. 1 G 7 2 3U H88EU 2007092500169 20070925 00169 2007 9 25 UPS07150638 4 20070911 A 2213 CONTROLLER AIRBUS A300 A300F4622R 3930360 EU AUTOPILOT SYS FAILED A IPXA K A NONE UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 141UP 0824 INSPECTION TYPE:N/A DIV - CREW EXPERIENCED MULTIPLE AUTOPILOT AND FLIGHT DIRECTOR FAILURES WHILE EN ROUTE TO DFW. FLIGH T DIVERTED TO DEN. REMOVED AND REPLACED FLIGHT CONTROL UNIT PER A300 MM 22-15-12-04 BY CAT QUALIFIED TECH. ALL SYSTEMS CHECKS OK. 2 L 7 2 4F RT A35EU 2007092500182 20070925 00182 EU 2007 9 25 M7K2007F00001 1 20070806 A 5310 350A23422320 SUPPORT FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAILBOOM DAMAGED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 808MH 493 3914 23058 DURING ROUTINE POSTFLIGHT INSPECTION THE CRACK WAS FOUND VISUALLY ON THE RT LOWER SUPPORT FITTING POSITION ON THE PARTS TRAILING EDGE FACE AND FOUND TO EXTEND ALMOST 2 INCHES OR ALMOST HALF WAY ACROSS THE PART. THIS IS A COMMON FAILURE FOR THIS PART. BELIEVE THIS PART HAS A DESIGN OR MATERIALS ISSUE THAT IS OVERALL STRENGTH RELATED. PART REQUIRES SHIMMING SOME TIMES TO PREVENT IT BEING PRELOADED IN SERVICE THAT IF NOT DONE CAREFULLY COULD AGGRAVATE THIS PROBLEM. MOST PROB LEMS HAVE OCCURRED WITH THE SHIMMING OF THE PART NOT BEING A FACTOR AS THE FIT WAS CORRECT FOR THE NEW PART. (K) 1 G 7 2 3U 3 U H9EU E00054EN 2007092500207 20070925 00207 EU 2007 9 25 HEEA117043 1 20070822 A 2821 402A124 FUEL FILTER AEROSP AS355 AS355* EU TMECA ARRIEL ARRIEL1 60030 NE CLOGGED E HEEA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 03 945AE 3004 FUEL FILTER LIGHT ILLUMINATED DURING TAKEOFF. MAINTENANCE REPLACED FUEL FILTER. 1 G 7 2 3U 3 U H11EU E19EU 2007092500213 20070925 00213 CE 2007 9 25 DXTA200702433 1 20070827 A 2612 FIRE DETECTOR RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP CARGO BAY MALFUNCTIONED E DXTA O OTHER N FALSE WARNING LD LANDING 1 GL 07 821QS 258709 BAG FIRE LIGHT ILLUMINATED ON TOUCHDOWN. CHECKED ELECTRICAL CONNECTIONS AT FWD, AFT AND LAV SMOKE DETECTORS, SMOKE DETEC TOR AMPLIFIER AND ALL THREE TEST SWITCHES AND FOUND NO DEFECTS. TAXIED AIRCRAFT, ALL OPS CHECKED NORMAL IAW AMM 26-10-00 . 2 L 7 2 4F 4 F RT A3EU E6WE 2007092500215 20070925 00215 EA 2007 9 25 TRAX200701341 1 20070911 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 861AS 7445 LEFT BONDED SKIN DOUBLER IS CRACKED. IN REFERENCE TO EO 600-53-81 REP. 10-18-07 PREFORMED LT BONED SKIN DOUBLER R EPAIR ALL WORK DONE IAW WITH REO 601R-53-61-506. REFERENCE JOB SIGN OFF INCLUDED IN TASK CARD REO 601R-53-61-506. 2 L 7 2 4F RT A21EA 2007092500222 20070925 00222 NM 2007 9 25 CO1Y200700007 1 20070914 A 7120 AUB7500501 TRUSS FITTING DOUG MD11 MD11 3023602 NM NR 1 E ENGINE CORRODED B CO1Y K NONE O OTHER IN INSP/MAINT 1 EA 33 702BC 48504 ON ENGINE NR 1 FORWARD TRUSS FITTING, FOUND 4EA HOLES WITH CORROSION. 2 L 7 3 4F RT A22WE 2007092500224 20070925 00224 EA 2007 9 25 TRAX200701343 1 20070913 A 3350 STRIP CNDAIR CL600 CL6002B19 1900309 EA CABIN CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 827AS 7212 EMERGENCY LIGHT STRIP CRACKED AT ROW 12. 2 L 7 2 4F RT A21EA 2007092500229 20070925 00229 WP 2007 9 25 ASMF200709004 1 20070912 A 2130 SWITCH DOUG DC9 DC987 3022087 WP CABIN PRESSURE OUT OF POSITION W ASMF B EMER. DESCENT W N INADEQUATE Q C FALSE WARNING AP APPROACH 1 SW 23 214AM 49585 AIRCRAFT PERFORMED AN EMERGENCY DESCENT 20 MINUTES PRIOR TO LANDING, DUE TO UNCONTROLLABLE DEPRESSURATION. MAINTENANCE P ERSONNEL VERIFIED THE PNEUMATIC SYSTEM FOR LEAKS AS WELL AS THE AIR CONDITIONED SYSTEM AND THE DUCTS OF ANTI-ICE SYSTEM IAW MPCM 36-10-00, 21-10-00 AND 30-10-00, ALL CORRECT. PRESSURIZATION TESTS WAS PERFORMED WITH BOTH ENGINES IAW MM 21-3 0-00, ALL CORRECT. DURING CABIN CHECK, THE SW (RADIO RACK) WAS CHANGED FROM VENTURY TO FAN POSITION, TESTED CORRECT. 2 L 7 2 4F RT A6WE 2007092500230 20070925 00230 NM 2007 9 25 ASMF200709005 1 20070917 A 3250 49640741 SPRING DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE NLG STEERING BROKEN W ASMF C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SW 23 168PL 53174 AIRCRAFT REJECTED TAKEOFF AT 60 KNOTS, DURING TAKEOFF RUN THE STEERING CONTROL WAS INOPERATIVE. AT PLATFORM MAINTENANCE PERSONNEL PERFORMED OPERATIONAL TEST OF THE STEERING CONTROL AND RUDDER MOVEMENT RESULTED CORRECT, SO AIRPLANE WAS SENT TO THE HANGAR AND DURING THE OVERNIGHT CHECK THE CENTERING SPRING OF PEDAL STEERING OVERRIDE MECHANISM WAS FOUND BROKEN, SO IT WAS REPLACED IAW MM 32-51-00 AND TESTED IAW MM 32-52-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2007092500233 20070925 00233 NE 2007 9 25 KPVA200714 2 20070831 A 7250 TURBINE BLADES PWA PW121 DHAV DHC8 DHC8103 1386005 NM PWA PW121 PW121 52124 NE NR 2 ENGINE SEPARATED A KPVA E ENGINE SHUTDOWN Z J SIGNIFICANT FAILURE REPORT WARNING INDICATION CL CLIMB 1 WP 13 809WP PCE120968 146 PCE120968 NR 2 ENGINE TURBINE FAILURE, 2ND STAGE LP TURBINE BLADE SEPARATION WITH DAMAGE TO THE 1ST STAGE LP TUBINE BLADES AND 2ND STAGE GUIDE VANES. LP SECTION FROZEN BUT PROP SHAFT TURNS. 2 H 7 2 4T 4 T RT A13NM E20NE 2007092500247 20070925 00247 CE 2007 9 25 GUUA07260704 1 20070726 A 5711 SPAR CAP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT WING CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 47542 UE198 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT WING REAR SPAR LOWER CAP CRACKED FROM RIVET HOLE TO REAR EDGE AT LWS 117.50. REMOVED DAMAGED SECTION OF LT LOWER AFT SPAR FROM LWS 73 TO LWS 129.86 SPLICED IN NEW SECTION OF SPAR IAW FIELD REPAIR FR-CO-01583 REV 2. 2 L 7 2 4T 4 T RT A24CE E26NE 2007092500269 20070925 00269 NM 2007 9 25 USAA920070831 1 20070911 A 5320 TIE CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 23700 CLT - MAJOR REPAIR - NR 6007482, CRACKED FRAME TIE CLIP, BS 360, S14L - S15L. REPLACED FRAME TIE CLIP, BS 360, S14L - S 15L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007092500275 20070925 00275 NM 2007 9 25 SWAA074615 1 20070911 A 2810 112A0001678 TANK BOEING 737 7373T5 1384608 NM RT WING FOD A SWAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SW 29 692SW 23062 AIR TURNBACK/INFLIGHT SHUTDOWN. CLIMBING THROUGH 22,000 FT NOTICED FUEL INBALANCE. ATTEMPTED TO BALANCE FUEL, RT FUEL TANK FELL 2,000 POUNDS BELOW LT FUEL TANK. INSPECTED FUEL SYSTEM, NO DEFECTS FOUND PER MM. AIRBORNE FROM BNA TO HOU WI TH CROSSFEED VALVE OPEN, ALL BOOST PUMPS ON FUEL ONLY USED FROM RT FUEL TANK. INSPECTED FUEL TANKS, FOUND FOD IN TANKS. REMOVED FOD PER MM. 2 L 7 2 4F RT A16WE 2007092500278 20070925 00278 EU 2007 9 25 07FDEA04011 1 20070919 A 5310 A53973085 BEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 CORROSION ON TOP SURFACE OF AFT CARGO COMP SILL BEAM FLANGE BETWEEN FRAME 59-59A AROUND A RIVET NUT. REMAINING THICKNES S AFTER REWORK IS 0,8MM, NOMINAL: 2,0MM. REPAIR PERFORMED BY CUT OUT AFFECTED AREA AND INSTALLING FILLER AND REPAIR ANG LE IAW ENG-STATEMENT: REA 0492-007 AND EA 6-5317-81087. 2 L 7 2 4F RT A35EU 2007092500280 20070925 00280 EU 2007 9 25 07FDEA04012 1 20070828 A 5310 R536H01433204 DOOR FRAME AIRBUS 310 A310322 3930334 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 AFT CARGO COMPARTMENT DOOR FRAME FOUND CORRODED, FR59A, BETWEEN STRG27 RT AND 36 RT. THE AFFECTED FRAME WAS REPAIRED BE TWEEN STRG 27-36RT. 2 L 7 2 4F RT A35EU 2007092500309 20070925 00309 NM 2007 9 25 SWAA074599 1 20070913 A 5753 6546430130 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C2 CHECK, FOUND RIGHT INBOARD FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FLAP PER MM . 2 L 7 2 4F RT A16WE 2007092500314 20070925 00314 NM 2007 9 25 SWAA074562 1 20070913 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007092500319 20070925 00319 NM 2007 9 25 SWAA074567 1 20070913 A 5311 6546541 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 3R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007092500326 20070925 00326 NM 2007 9 25 SWAA074594 1 20070913 A 5310 6547980 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 1006 AND BS 1016, STR 17L. REMOVED AND REPLACED W EB PER SRM. 2 L 7 2 4F RT A16WE 2007092500347 20070925 00347 NM 2007 9 25 SWAA074606 1 20070913 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 1121, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007092500353 20070925 00353 2007 9 25 SWAA074603 4 20070913 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007092500361 20070925 00361 NM 2007 9 25 2007UALA03202 1 20070814 A 2620 346000137 SQUIB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE BLOWN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 540UA 25252 RIGHT ENGINE SQUIB TEST LIGHT WILL NOT LIGHT UP DURING TEST POSITION 2. AS PART OF TROUBLESHOOTING VERIFIED SQUIB CIRCU IT, AND DURING TEST FOUND RIGHT ENGINE SQUIB BOTTLE BLOWN. REPLACED SQUIB. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092500387 20070925 00387 EU 2007 9 25 07FDEA03963 1 20070919 A 5313 A53970380207 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT STRINGER P 31RH, C 54.2. STRINGER REPAIR PERFORMED IAW. SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007092500390 20070925 00390 EU 2007 9 25 CPCP20070103 1 20070824 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 414WF 414 FLOORBEAM AT FRAME 40 IS CORRODED. FLOORBEAM AT FRAME 40 REPAIRED AS PER 53-00-00 FIG 435. 2 H 7 2 4T RT A53EU 2007092500394 20070925 00394 EU 2007 9 25 07FDEA03969 1 20070919 A 5320 A53773213224 SHEAR PLATE AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 CRACKED SHEAR PLATE BETWEEN FRAME 21-22, STRG 44 LT, FWD CARGO COMP. REPLACMENT OF SHEAR PLATE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092500418 20070925 00418 EU 2007 9 25 07FDEA03983 1 20070919 A 5315 A53974268 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 HEAVY CORROSION ON CROSSBEAM AT FRAME 55/58. CROSSBEAM SPLICE REPAIR PERFORMED IAW SRM 53-10-15/FIG 207. 2 L 7 2 4F RT A35EU 2007092500433 20070925 00433 2007 9 25 2007UALA03686 4 20070912 A 2565 6572097 HOSE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EVAC SLIDE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 677UA PK0072 30029 HOSE WAS FOUND DAMAGED DURING HOSE TEST. 10-5-07 HOSE WAS LEAKING THRU OUTSIDE SURFACE WITHOUT VISIBLE EVIDENCE OF DA MAGE. REPLACED HOSE. SLIDE AND AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092500437 20070925 00437 NM 2007 9 25 2007UALA03690 1 20070912 A 3397 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 643UA 25093 EMERGENCY EEL LIGHTS FROM ROW 5AB-14AB & AT LEFT MID LAV ARE INOPERATIVE. 10-5-07 REPLACED POWER SUPPLY FEEDER CABLE. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092500447 20070925 00447 WP 2007 9 25 07FDEA04008 1 20070919 A 5320 ABA72034 WEB DOUG DC10 DC1010F 3022111 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 PERFORMED INSPECTION AFTER REMOVAL FLOOR PANEL IN COCKPIT WITH OAN J/C SP10530208-2JR, FOUND MODERATE CORROSION AND CR ACK 2" LONG ON MEMBRANE. REPLACED WEB SECTION IAW SRM 53-00-01 VOL I FIG 10. 2 L 7 3 4F A22WE 2007092500448 20070925 00448 NM 2007 9 25 07FDEA04017 1 20070919 A 5313 BAC1498131 STRINGER SPLICE BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 AFT PIT STA 1010, LBL 23, WL 150 STRINGER SPLICE HAS CORROSION. REMOVED OLD SPLICE, REMOVED CORROSION FROM STRINGER, OR IGINAL MATERIAL .070". REMOVED .005, REMAINING .065", FOUND TO BE WITH IN LIMITS. FABRICATED NEW STRINGER SPLICE, TR EATED AND PRIMED, INSTALLED, REF SRM 51-10-2 PG 2, SRM 51-30-2 PG 2, SRM 53-10-1 FIG 5. THIS IS CLASSIFIED AS A MINOR R EPAIR. LEVEL 1 CORROSION. 2 L 7 3 4F A3WE 2007092600013 20070926 00013 EU 2007 9 26 07FDEA04027 1 20070919 A 5730 A57112300 SKIN AIRBUS 310 A310203 3930313 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION ON CENTER TANK TOP SKIN C 45-46 LT, C 41-46 RT REPAIR PERFORMED IAW SRM 57-10-12 FIG 201 AND IN ADDITION THE HOLES OVERSIZED IAW EA 6-5710-81049 AND RAS//AS/0256/2004 ISS A. 2 L 7 2 4F RT A35EU 2007092600022 20070926 00022 EU 2007 9 26 07FDEA04036 1 20070919 A 5310 A53611698204 DOOR FRAME AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 DURING LT FWD PAX DOOR FRAMING AFT PANEL REPLACEMENT, A DOUBLE HOLE WAS PERFORMED AT FRAME 18, STRG 26 IN LOWER BEAM W EB AT ITS REAR END AND IN STRG 26 COUPLING. REPLACEMENT OF STRINGER 26 COUPLING BY NEW ONE IAW EA 6-5312-81117 AND RAS/ AS/0017/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007092600026 20070926 00026 EU 2007 9 26 07FDEA04040 1 20070919 A 5720 A57350110201 REINFORCEMENT AIRBUS 310 A310203 3930313 EU ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CHAFING DAMAGE TO REINFORCING PLATE ADJACENT TO THRUST AND SIDE LOAD FITTING RIB 9 REPAIR PERFORMED BY BLEND OUT T O SMOOTH CONTOUR AND NDT FOR CRACK FREE IAW EA 6-5720-81076 AND RAS/BAE/1125/2004 ISS A. 2 L 7 2 4F RT A35EU 2007092600030 20070926 00030 EU 2007 9 26 07FDEA04044 1 20070919 A 5344 A52111346000 HINGE FITTING AIRBUS 310 A310324 3930206 EU ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 NEW CORROSION ON OLD REPAIR, FOUND ON FWD PAX DOOR RT ON DOOR HINGE FITTING (LOWER ARM WEB - BOTTOM SIDE). CORROSION RE MOVED (TOTAL OF 53 PERCENT REMOVED), FILLER AND OLD REPAIR DOUBLER INSTALLED IAW EA 6-5211-82884 AND RAS/AS/115/2005 ISS UE A. 2 L 7 2 4F RT A35EU 2007092600047 20070926 00047 NM 2007 9 26 HALA0700384 1 20070918 A 7500 CONTROLLER BOEING 767 7673CB 1385187 NM PWA 4060 PW4060 52119 NE RT BLEED SYS MALFUNCTIONED A HALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 590HA 33423 ATB: RT ENG BLEED OVHT UNABLE TO RESET PER QRH 2 RT ENG BLEED OVHT. BITE CK AIR SYS CTL MOD FOUND HPC FAULT. REPLACED PNEU TEMP SWITCH FOR RT BLEED. REPLACED HP CONTROLLER PER AMM 36-11-08 OP CK GOOD ON HIGH POWER RUN UP NO DEFECTS NOTE D. REPLACED PCA CARD BLEED AIR CONTROL CONDITION SAME. REPLACED TEMP SENSOR OPS CKD GOOD PER FIM 36-10-00 RAN ENGINE H IGH POWER RUN OPS CK GOOD PER AMM 36-22-00. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092600048 20070926 00048 2007 9 26 HALA0700386 4 20070919 A 2210 AUTOPILOT SYS BOEING 767 7673G5 1385126 NM MALFUNCTIONED A HALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 584HA 24258 ETOPS SIGNIFICANT SYSTEM, A/P FAILED TO MAINTAIN G.S. PROPERLY AT 1000' ABOVE A/P FLEW AIRCRAFT 1/2 LOW DOT ON GLIDESLOP E. PERFORMED TEST OF BOTH MMR PER FIM 34-31-00 FIG 103. NO DISCREPANCIES. MCDP TEST 1-40-ALL PASSED. NO FLIGHT FAULT S. A/C REMAINS LAND 3. 2 L 7 2 4F RT A1NM 2007092600056 20070926 00056 NM 2007 9 26 DLM88071237 1 20070919 A 5330 5936667501 SKIN DOUG MD88 MD88 3023688 NM BS 1231 L27R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 918DE 49959 FUSELAGE SKIN/DOUBLER WERE DENTED AT TWO LOCATIONS AT APPROXIMATELY STA 1231, L-27R AFT OF THE CARGO DOOR CUTOUT. THE D AMAGE IN THE SKIN AND DOUBLER WAS CUT OUT AND REPAIR DOUBLERS WERE INSTALLED. 2 L 7 2 4F RT A6WE 2007092600057 20070926 00057 NM 2007 9 26 DL757071238 1 20070919 A 5330 146N37805 SKIN BOEING 757 757232 1384965 NM BS 1696 S21L PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 661DN 24972 FUSELAGE PUNCTURED AT STA 1696 ABOVE STR 29L. SKIN CUTOUT AND AN EXTERNAL REPAIR DOUBLER WAS INSTALLED. 2 L 7 2 4F RT A2NM 2007092600058 20070926 00058 NM 2007 9 26 HALA0700399 1 20070920 A 2120 20224324 ACTUATOR BOEING 767 7673CB 1385187 NM RAM AIR DOOR MALFUNCTIONED A HALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 588HA 18282 18282 33466 ATB - UNABLE TO KEEP CABIN TEMP REASONABLE W/R PACK IN STBY W. REMOVED AND REPLACED RT PACK RAM AIR INLET DOOR ACTUATOR . OPERATION OF RT PACK GOOD. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007092600060 20070926 00060 EU 2007 9 26 07FDEA04064 1 20070920 A 5313 A53973984214 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION ON STRINGER SEGMENT P 43, C55/58 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092600061 20070926 00061 EU 2007 9 26 07FDEA04065 1 20070920 A 5730 A57350143 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 ELONGATED HYDRAULIC FITTING HOLES ON PYLON NR 2 SUPPORT BRACKET, BOTTOM WING SKIN PANEL 2. REPAIR PERFORMED BY OVERSIZI NG HOLES AND INSTALLING BUSHINGS IAW EA 6-5720-82887 AND RAS/BAE/1000947/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007092600063 20070926 00063 EU 2007 9 26 07FDEA04067 1 20070920 A 5730 A57350143 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 ELONGATED HYDRAULIC FITTING HOLES ON PYLON NR 1 SUPPORT BRACKET, BOTTOM WING SKIN PANEL 2. REPAIR PERFORMED BY OVERSIZI NG HOLES AND INSTALLING BUSHINGS IAW EA 6-5720-82887 AND RAS/BAE/1000947/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007092600064 20070926 00064 EU 2007 9 26 07FDEA04068 1 20070920 A 5320 AA53988424202 STRUT AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT CROSS STRUT C 84 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092600066 20070926 00066 EU 2007 9 26 07FDEA04069 1 20070920 A 5320 A53988624205 STRUT AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 CORROSION FOUND AT CROSS STRUT C 86 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092600069 20070926 00069 EU 2007 9 26 07FDEA04072 1 20070920 A 5320 A53988724200 STRUT AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT CROSS STRUT C 87 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092600071 20070926 00071 EU 2007 9 26 07FDEA04074 1 20070920 A 5755 A57710027 SKIN AIRBUS 310 A310324 3930206 EU NR 2 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FOUND DELAMINATION ON SPOILER NR 2 RT, LOWER SKIN (100 BY 30 MM). REPAIR PERFORMED IAW SRM 57-70-00/201/PARA 12. 2 L 7 2 4F RT A35EU 2007092600072 20070926 00072 EU 2007 9 26 07FDEA04075 1 20070920 A 5311 A53973261226 FRAME AIRBUS 310 A310203 3930313 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND MISDRILLED HOLES AT FRAME SEGMENT C 59, P47 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092600077 20070926 00077 WP 2007 9 26 070156 1 20070912 A 3040 DEICE SYSTEM DOUG DC9 DC983 3022083 WP WINDSHIELD FAILED A WX0A K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 19 860GA 49786 DURING PILOTS PREFLIGHT INSPECTION, SMOKE STARTED TO FILL THE COCKPIT. NOTICED THE SMOKE COMING FROM THE CAPTAINS LEFT CORNER OF THE WINDSHIELD. SHUT OFF ALL AC ELECTRICAL POWER AND SMOKE WAS EXTINGUISHED. WINDSHIELD DE ICE SYSTEM WAS D EFERRED IAW ALLEGIANT AIR MEL PROCEDURES AND THE AIRCRAFT WAS FLOWN TO LAS VEGAS. MAINTENANCE DEPARTMENT PERSONNEL REMO VED AND REPLACED THE CAPTAINS WINDSHIELD IAW THE AMM 56-10-02. OPERATIONAL AND LEAK CHECKS PERFORMED NORMAL AND THE AIR CRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007092600078 20070926 00078 WP 2007 9 26 070155 1 20070906 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 864GA 49912 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007092600079 20070926 00079 2007 9 26 TRBA2007079 4 20070920 A 3425 INDICATOR AEROSP ATR72 ATR72212 8680945 EU COCKPIT FAILED A TRBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 29 448AM 448 DURING T/O ROLL, F/O'S EHSI WENT BLANK. ABORTED TAKEOFF AND RETURNED TO BLOCK. REMOVED AND REPLACED F/O EHSI AND PERFO RMED OPT CK IAW JIC NR 34-75-81 AND FOUND SYSTEM WORKING PROPERLY. 2 H 7 2 4T RT A53EU 2007092600080 20070926 00080 EU 2007 9 26 07FDEA04082 1 20070920 A 5414 A54611752 PANEL AIRBUS 310 A310324 3930206 EU NR 2 NACELLE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FOUND DAMAGED HOLES ON BUTTERFLY REPAIR DOUBLER AT INBOARD SIDEWALL PANEL, PYLON NR 2 RT. REPAIR PERFORMED BY INSTALLIN G NEW DOUBLER ON SIDEWALL PANEL IAW SRM 54-51-31/FIG 201. 2 L 7 2 4F RT A35EU 2007092600081 20070926 00081 EU 2007 9 26 07FDEA04084 1 20070920 A 5414 A54611752 PANEL AIRBUS 310 A310324 3930206 EU ZONE 400 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FOUND DAMAGED HOLES ON BUTTERFLY REPAIR DOUBLERS AT INBOARD AND OUTBOARD SIDEWALL PANEL, PYLON NR 1 LT. REPAIR PERFORME D BY INSTALLING NEW DOUBLERS ON SIDEWALL PANELS IAW SRM 54-51-31/FIG 201. 2 L 7 2 4F RT A35EU 2007092600082 20070926 00082 EU 2007 9 26 07FDEA04088 1 20070920 A 5310 A53980070 BOX BEAM AIRBUS 310 A310324 3930206 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 TWO CRACKS IN HOLE (EACH 10MM) FOUND IN THE UPPER TORSION BOX IN BEAM AT FRAME 75, STRG 11 LT. REPAIR PERFORMED BY CUT OUT OF DAMAGED AREA, INSTALLATION OF FILLER AND REPAIR ANGLE IAW EA 6-5318-82894 AND RAS/DAHAM/4019625/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007092600083 20070926 00083 EU 2007 9 26 07FDEA04089 1 20070920 A 5313 A53973306200 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT STRINGER SEGMENT C 72, P45 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092600085 20070926 00085 EU 2007 9 26 07FDEA04091 1 20070920 A 5330 A53610633 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORROSION ON FAIL/SAFE RING, LT FWD PAX DOOR, SOME AREAS OUT OF LIMIT. REPAIR PERFORMED BY SMOOTH REWORK AND HFEC/ROTOT EST INSPECTION IAW EA 6-5312-82878 AND RAS 037837/015/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007092600086 20070926 00086 EU 2007 9 26 07FDEA04092 1 20070920 A 5320 A53974242200 FITTING AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT CORNER FITTING C 63, P 44 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092600087 20070926 00087 EU 2007 9 26 07FDEA04093 1 20070920 A 5330 A53611658 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORROSION ON FAIL/SAFE RING, LT FWD PAX DOOR, SOME AREAS OUT OF LIMIT. REPAIR PERFORMED BY SMOOTH REWORK AND HFEC/ROTOT EST INSPECTION IAW EA 6-5312-82878 AND RAS 037837/015/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007092600089 20070926 00089 EU 2007 9 26 07FDEA04095 1 20070920 A 5313 A53974232200 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT STRINGER SEGMENT C65, P56 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092600092 20070926 00092 EU 2007 9 26 07FDEA04098 1 20070920 A 5315 A53978267208 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT CROSS BEAM C67 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092600093 20070926 00093 EU 2007 9 26 07FDEA04099 1 20070920 A 5730 A57243205202 SKIN AIRBUS 310 A310324 3930206 EU ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FOUND CHAFING MARKS ON LEADING EDGE SKIN BETWEEN SLAT TRACK NR 5 AND 6 LT WING. REPLACEMENT OF DAMAGED NOSE SKIN IAW SR M 51-72-10. 2 L 7 2 4F RT A35EU 2007092600096 20070926 00096 NM 2007 9 26 HALA0700407 1 20070913 A 5314 KEELBEAM BOEING 767 76733A 1385209 NM BS 967 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 LEVEL 1 CORROSION ON KEEL BEAM HORIZONTAL WEB-SURFACE, CORROSION AT 1 RIVET HEAD AT BS 967, BL 0. ALL REWORK WITHIN LIM ITS IAW SRM 53-50-12 REV 74. 2 L 7 2 4F RT A1NM 2007092600097 20070926 00097 NM 2007 9 26 HALA0700402 1 20070920 A 3610 2780539103 ISOLATION VALVE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE RIGHT MALFUNCTIONED A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 596HA 23276 ETOPS SIGNIFICANT SYSTEM, RT ISOLATION VALVE ILLUMINATED. REPLACED ISOLATING VALVE RIGHT SIDE INSTALLED PER AMM 36-11-0 4. REMOVED PER AMM 36-11-04. SECURITY CONDITION GOOD. OPS CK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092600099 20070926 00099 NM 2007 9 26 HALA0700400 1 20070920 A 2410 IDG BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE RT ENGINE LEAKING A HALA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, FOUND RT ENG IDG LEAKING OIL FROM FILL PORT FITTING. REPLACED IDG FILL PORT FITTING AND O-RIN G. RAN ENG. CKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092600100 20070926 00100 NM 2007 9 26 HALA0700405 1 20070917 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 460-785 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 LEVEL 1 CORROSION ON SEAT TRACK RBL 88.5 AT STA 460, 532, 561, 591, 605, 622, 654 AND 785.9. REWORKED AREAS, REWORKED A REAS WITHIN LIMITS IAW SRM 53-00-52, REWORKED AREAS ALODINED AND PAINTED. 2 L 7 2 4F RT A1NM 2007092600103 20070926 00103 2007 9 26 DL764071239 4 20070920 A 3460 COMPUTER BOEING 767 767432ER 1385134 NM LT FMC MALFUNCTIONED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 840MH 29717 LOST CAPT FMC CDU UNABLE TO RECOVER DIVERTING TO SNN FOR REPAIRS. REMOVED AND REPLACED CENTER CDU CKS GOOD MCO AND PLAC ARD REMOVED. 2 L 7 2 4F RT A1NM 2007092600105 20070926 00105 EU 2007 9 26 TRBA2007078 1 20070919 A 2121 011260500 FAN AEROSP ATR72 ATR72212 8680945 EU ODOR A TRBA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 29 348AE 349 BURN ODOR IN CABIN, EARLY IN GROUND EXTRACT FAN WAS REPORTED MAKING LOUD NOISE. ITEM DEFERRED ON MEL 21-06 AUTH 090137D -C. REMOVED AND REPLACED AIR EXTRACTION FAN IAW JIC 21-23-21. THIS ACTION CLEARS MEL 21-06. PERFORMED FLIGHT COMPARTM ENT AND CABIN AIR DISTRIBUTION OPERATIONAL CHECK. NO BURN ODOR NOTICED IAW 21-22-00. 2 H 7 2 4T RT A53EU 2007092600107 20070926 00107 NM 2007 9 26 DHL2007746534 1 20070830 A 5712 65172769 RIB BOEING 727 727224 1384076 NM WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 NR 5 SLAT AT ACTUATOR ATTACH HAS O/B FRAME CRACKED ON FWD LOWER CORNER. REMOVED AND REPLACED RIB AT NR 5 SLAT O/B IAW B -727 SRM 51-30-5 AND 51-30-2, RIB P/N 65-17276-9, PO: 7268244. 2 L 7 3 4F A3WE 2007092600109 20070926 00109 NM 2007 9 26 CALA0700524 1 20070918 A 5315 6545810 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND TOP SURFACE OF FLOORBEAM CORRODED NEAR FOWRD ENTRY DOOR AT STA 312, BL 0 TO LBL 10. THE UPPER CHORD WA S REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007092600112 20070926 00112 NM 2007 9 26 F3LA200700240 1 20070914 A 5755 LUG AIRBUS A319 A319111 3930336 NM NR 4 SPOILER GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 921FR 5402 2010 DURING C-3 CHECK INSPECTION REPORTED THE RIGHT WING NR 4 SPOILER ANTI-ROTATION LUG GOUGED. FABRICATED AND INSTALLED REI NFORCING PLATE FOR RIGHT NR 4 SPOILER CENTER HINGE FITTING PER EA A9-57R-12142, REV A. 2 L 7 2 4F RT A28NM 2007092600120 20070926 00120 SO 2007 9 26 C2XA07IA207 1 20070915 A 3110 645071 PANEL EMB 145 EMB145XR 3260214 SO COCKPIT INOPERATIVE A C2XA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SW 27 18114 145664 IAH - FLIGHT 2163, THE CREW REPORTED LANDING GEAR LEVER, BACKLIGHTING PANEL, UP POSITION WILL NOT ILUMINATE. THE AIRCRA FT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED & REPLACED BACKLIGHTING PANEL ON LANDING GEAR LEVER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007092600122 20070926 00122 WP 2007 9 26 MWEA070226 1 20070924 A 5230 PAN DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 809ME 48071 MID CARGO COMPARTMENT DOOR AFT EDGE CRACKED JUST BELOW UPLOCK CAM. FABICATED AND INSTALLED PAN. 2 L 7 2 4F A6WE 2007092600124 20070926 00124 2007 9 26 HNAA0700177 4 20070810 A 3442 M15853512RECON RADAR DHAV DHC8 DHC8102 2809003 NM WX SYSTEM INOPERATIVE A HNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 07 911HA 034 PDT FLT 4189 PHL/CRW HAD THE WEATHER RADAR FAIL IN FLIGHT. CAPTAIN TRIED SEVERAL METHODS OF GETTING RADAR TO WORK, FLIG HT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED WEATHER RADAR, OPS CHECK OK. 2 H 7 2 4T RT A13NM 2007092600128 20070926 00128 EU 2007 9 26 2007UALA03169 1 20070815 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 429UA 539 EXTERNAL FUSELAGE SKIN LT SIDE, APPROX 9 FT AFT OF NOSE GEAR, 4 FEET ABOVE FUSELAGE CENTER LINE. *S/D* ACCOMPLISHED MA JOR REPAIR ON AREA. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092600131 20070926 00131 EA 2007 9 26 TRAX200701347 1 20070914 A 2560 BATTERY CNDAIR CL600 CL6002B19 1900309 EA FLASHLIGHT DISCHARGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 CAPTAIN`S FLASHLIGHT INOP. WILL NOT TURN OFF. BATTERY DEAD. 2 L 7 2 4F RT A21EA 2007092600134 20070926 00134 EU 2007 9 26 TRAX200701350 1 20070914 A 1100 PLACARD AEROSP ATR72 ATR72 EU CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 EMERGENCY EXIT PLACARD IS MISSING BY SEAT 1A, CLOSE TO THE FLOOR. 2 H 7 2 4T RT 2007092600142 20070926 00142 NM 2007 9 26 ASAA0772052 1 20070916 A 5320 146A81236 WEB BOEING 737 737790 13844CN NM BS 794-847 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 627AS 30794 AFT PIT THRESHOLD WEB CORRODED. REPAIRED IAW SRM 51-40-08 AND 51-40-02. 2 L 7 2 4F RT A16WE 2007092600144 20070926 00144 NM 2007 9 26 ASAA0772049 1 20070916 A 5330 143A611021 SKIN BOEING 737 737790 13844CN NM BS 458-468 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 627AS 30794 DENT IN FWD CARGO DOOR AT STA 460. REPAIRED IAW SRM 52-00-01 REPAIR 3. 2 L 7 2 4F RT A16WE 2007092600150 20070926 00150 NM 2007 9 26 HNAA0700167 1 20070812 A 6123 300500024 TSCU DHAV DHC8 DHC8102 2809003 NM DHAV DH5220 DH5220P WP AUTOFEATHER SYS INOPERATIVE A HNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 07 931HA 48819 214 132 891126 AUTOFEATHER ARM LIGHT REMAIN ILLUMINATED AFTER AUTOFEATHER SWITCH SELECTED OFF. DIVERTED TO MDT. REMOVED AND REPLACED TSCU AND REMOTE C/B 2431-CB4. OPS CHECKS GOOD. 2 H 7 2 4T RT A13NM 5 N A8EU 2007092600154 20070926 00154 NM 2007 9 26 2007UALA03700 1 20070913 A 5280 DOOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RT NLG DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 RIGHT NOSE LANDING GEAR DOOR DAMAGED LOWER EDGE FRONT 14 INCHES. REPLACED RIGHT NOSE LANDING GEAR DOOR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092600155 20070926 00155 NM 2007 9 26 2007UALA03701 1 20070913 A 3150 WARNING MESSAGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BATTERY CHARGER ILLUMINATED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 543UA 25698 BATTERY CHARGER STATUS MESSAGE. 10-9-07 INSTALLED NEW MAIN EQUIPMENT LOWER BATTERY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092600156 20070926 00156 NM 2007 9 26 2007UALA03702 1 20070914 A 3350 3071BPEGL LAMP AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE SEAT 16 ABC BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 834UA 1420 EEL LIGHT AT SEAT 16 ABC HAS ONE BULB OUT. RELAMPED EEL, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092600157 20070926 00157 NM 2007 9 26 2007UALA03703 1 20070913 A 2131 CONTROLLER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN PRESSURE FAILED A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 327UA 24147 CABIN PRESSURE NOT CONTROLLED ON DESCENT IN STANDBY MODE. AT 5.0 PRESSURE BUMP & CABIN CLIMBED TO MATCH ACFT ALT. NO T IME TO SELECT MANUAL. FOUND CABIN PRESSURE CONTROLLER FAILED. REPLACED CABIN PRESSURE CONTROLLER. ALL TESTS PERFORMED NORMALLY- NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092600158 20070926 00158 NM 2007 9 26 2007UALA03704 1 20070914 A 2612 CONTROL PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FIRE DETECTION FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 329UA 24149 FIRE, FWD PIT ARMED, & 2ND BTL ARMED, LIGHTS DO NOT ILLUMINATE DURING CARGO FIRE DETECTION AND SUPPRESSION SYSTEM TEST. FOUND FIRE DETECTION / SUPPRESSION PANEL FAULTY. REPLACED CARGO FIRE DETECTION AND SUPPRESSION CONTROL PANEL. NO REPE ATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092600159 20070926 00159 NM 2007 9 26 2007UALA03705 1 20070913 A 3350 INVERTER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 348UA 24252 EEL LIGHTS INOP FROM ROWS 3 TO 8. REPLACED INVERTER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092600160 20070926 00160 NM 2007 9 26 2007UALA03706 1 20070913 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ROW 30 ABC UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 EMERGENCY LIGHTING POPPED OUT OF FLOOR AT 30 ABC. 10-9-07 SECURED FLOOR LIGHTING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092600162 20070926 00162 NM 2007 9 26 2007UALA03708 1 20070913 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 644UA 25094 EEL LIGHTS INOP RIGHT SIDE ROWS 15 THRU 27. 10-9-07 REPLACED SHORTED EEL LAMP. ALL EEL OP CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092600163 20070926 00163 NM 2007 9 26 KCSA071375 1 20070917 A 5311 FRAME BOEING 747 7472B4B 138481B NM BS 1900 S13R CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FUSELAGE FRAME CRACKED AT STR 13R. 2 L 7 4 4F RT A20WE 2007092600168 20070926 00168 NE 2007 9 26 CR33955 3 20070830 A 6111 BEARING BEECH 1900 1900D 1154162 CE PWC PT6 PT6A67AG 52211 NE HARTZL HCE4A HCE4A3I NE PROPELLER BLADE BROKEN B RC2R K NONE O OTHER IN INSP/MAINT 1 EA 63 HJ378A PROPELLER BLADE MAIN BEARING BROKEN IN HUB SOCKET. BEARING RETURNED TO BIG SKY AIRLINES FOR REVIEW. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2007092600170 20070926 00170 WP 2007 9 26 UPS07850665 1 20070821 A 5740 57732521 FITTING DOUG DC8 DC873F 302199F WP FLAP ACTUATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 LEFT INBOARD FLAP ACTUATOR FITTING IS CRACKED, STA 97. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUAT OR FITTING AT STA 97 IAW DWG 7981564, AND DC8 AMM 20-16-00. 2 L 7 4 4F RT 4A25 2007092600171 20070926 00171 WP 2007 9 26 UPS07850671 1 20070915 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 EMERGENCY EXIT LIGHTS WON'T CHECK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD PER AMM 33-50-00- 4. 2 L 7 4 4F RT 4A25 2007092600172 20070926 00172 WP 2007 9 26 UPS07850672 1 20070914 A 3350 5708458503 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:N/A EMERGENCY LIGHT BATTERY PACK DRAINED. EMERGENCY LIGHT BATTERY PACK REPLACED AND TESTED IAW DC8 AMM 33-50-01-2-4. FUNCTION TESTED SERVICEABLE. 2 L 7 4 4F RT 4A25 2007092600173 20070926 00173 WP 2007 9 26 UPS07850673 1 20070915 A 3350 LAMP DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS WILL NOT DISARM. REPLACED LAMP FOR "DISARM" LIGHT. OPERATION CHECK GOOD PER DC8 AMM 33-50-00. 2 L 7 4 4F RT 4A25 2007092600174 20070926 00174 NM 2007 9 26 UPS07M50666 1 20070817 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1273-1381 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C CTR CABIN - SEAT TRACK FROM STA 1273 - STA 1381, -X27.5 SEVERAL SCRATCH MARKS FOUND ON CROWN & CHANNEL SURFACE AS MARKED. CTR CABIN SEAT TRACK FR STA 1273-1381 X=-27.5 RT SCRATCH MARKS ON CROWN & CHANNEL REMOVED FOUND EXC EED LIMIT. SCRATCH MARK SEAT TRACK TRI TRIMMED OFF AT STA 1284 & 1391. HFEC INSP CUTOUT ON TRIMMED OFF AREAS FOUND NO CRACK. NEW SEAT TRACK, SPLICE HAT & SPLICE PLATE FAB, HOLES PICKED UP, PROTECTED, PAINT TOUCHED UP & INSTALLED. 2 L 7 3 4F RT A22WE 2007092600175 20070926 00175 NM 2007 9 26 2007UALA03709 1 20070913 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 35G INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 214UA 30220 EMERGENCY LIGHT AT SEAT 35G INOP. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007092600177 20070926 00177 NM 2007 9 26 2007UALA03711 1 20070914 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EEL 4E, 5E, 5J INOPERATIVE. 10-9-07 SECURED EEL FEEDER CONNECTOR. OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092600179 20070926 00179 NM 2007 9 26 2007UALA03713 1 20070913 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 17B LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 177UA 24384 THE 17B EMERGENCY STRIP FALLING OFF. 10-9-07 REINSTALLED STRIP AND EEL CHECKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092600183 20070926 00183 NM 2007 9 26 2007UALA03717 1 20070915 A 3350 BATTERY BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 930UA 26655 EEL STRIP LIGHT FROM SEAT ROW 4ABC TO 8ABC IS INOP. REPLACED AND OPS CHECKED THE POWER SUPPLY BATTERY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092600184 20070926 00184 NM 2007 9 26 2007UALA03718 1 20070916 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU SEAT 18 ABC FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 314UA 23675 FLOOR EEL LIGHTS VERY DIM FROM SEAT 18 ABC TO AFT GALLEY. REPLACED 3 EEL STRIP LIGHT ASSY'S. EEL LIGHTS OPCK NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092600185 20070926 00185 NM 2007 9 26 2007UALA03719 1 20070916 A 2612 NONE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C 13802 EU FIRE DETECTION NONE A UALA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 364UA 24533 RTFL DUE TO A MASTER CAUTION APU FIRE INDICATION. CLEANED AND TESTED. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092600186 20070926 00186 NM 2007 9 26 2007UALA03720 1 20070915 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 LEFT OVERWING EMERGENCY LIGHT SECOND FROM BOTTOM ONE BULB INOP & SECOND FROM TOP ONE LIGHT INOP. 10-9-07 RELAMPED BO TH POSITIONS. EEL LIGHTS OP CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092600187 20070926 00187 NM 2007 9 26 2007UALA03721 1 20070915 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 CEILING UPPER DECK EMERGENCY LIGHTS INOP FROM ROW 12 UP TO ROW 16. 10-9-07 RELAMPED ALL POSITIONS. RESTORED EEL LIG HTS. OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092600188 20070926 00188 NM 2007 9 26 2007UALA03722 1 20070917 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 4A AFT UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 182UA 25279 SEAT 4A AFT EEL STRIP LIGHT FOUND BROKEN AWAY FROM SEAT TRIM. 10-9-07 REPLACED EEL STRIP LIGHT. LIGHTING OP CHECKS N ORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092600190 20070926 00190 NM 2007 9 26 2007UALA03725 1 20070914 A 3397 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 520UA 24890 DOOR 4L EMERGENCY LIGHT SWITCH OVER DOOR IS INOP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092600191 20070926 00191 NM 2007 9 26 2007UALA03726 1 20070915 A 5414 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 NACELLE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 520UA 24890 NR 2 PYLON FWD I/B SIDE SKIN AT NAC STA 125 HAS EXISTING FASTENER HOLE ELONGATED. HFEC INSPECTED, NO DEFECTS NOTED. IN STALLED 2EA FREEZE PLUGS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092600192 20070926 00192 NM 2007 9 26 2007UALA03727 1 20070915 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1794 S22-23R DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 520UA 24890 FUSELAGE EXTERNAL SURFACE DENTED AT BS 1794 BETWEEN STR 22R-23R. 10-9-07 MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE AND INSTALLED REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092600194 20070926 00194 NM 2007 9 26 2007UALA03729 1 20070916 A 3350 20131A BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 579UA 26697 EEL LIGHT INOP ROW 14ABC. REPLACED BATTERY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092600195 20070926 00195 NM 2007 9 26 2007UALA03730 1 20070915 A 5310 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOORWAY DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 518UA 24871 L2 UPPER HINGE ARM BEARING BLOCK AREA DOOR FRAME HAS A VERY DEEP PUNCTURE GOUGE IN RADIUS. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FORMED & INSTALLED NEW INTERCOSTAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092600196 20070926 00196 NM 2007 9 26 2007UALA03731 1 20070915 A 3350 582233 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 641UA 25091 LEFT SIDE EEL IS INOP FROM SEAT 27 TO AFT GALLEY. REPLACED BATTERY & EEL CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092600200 20070926 00200 WP 2007 9 26 ASAA0782016 1 20070913 A 5313 592480215 LONGERON DOUG DC9 DC983 3022083 WP BS 246 L17L DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 LONGERON DENTED. REPLACED DAMAGED SECTION WITH SPLICES PER SRM 53-02. 2 L 7 2 4F RT A6WE 2007092600202 20070926 00202 WP 2007 9 26 ASAA0782018 1 20070913 A 5322 993607319 SHEAR TIE DOUG DC9 DC983 3022083 WP BS 1211 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 53-03. 2 L 7 2 4F RT A6WE 2007092600203 20070926 00203 WP 2007 9 26 ASAA0782019 1 20070913 A 5311 9957739137 FRAME DOUG DC9 DC983 3022083 WP BS 1287 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 FRAME CORRODED. REPLACED FRAME PER SRM 53-03. 2 L 7 2 4F RT A6WE 2007092600204 20070926 00204 WP 2007 9 26 ASAA0782020 1 20070913 A 5320 99365845 INTERCOSTAL DOUG DC9 DC983 3022083 WP BS 1287-1309 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 INTERCOSTAL CRACKED. REPLACED INTERCOSTAL PER SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F RT A6WE 2007092700003 20070927 00003 EU 2007 9 27 MALA070120 1 20070920 A 3350 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS MALFUNCTIONED A MALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 15 433XJ 340B433 AFTER ENGINE SHUTDOWN, THE EMERGENCY LIGHTS WOULD NOT SHUT OFF. AFTER PLUGGING IN THE GPU, THEY WOULD NOT ARM. REMOVED AND REPLACED BATTERY PACKS IAW AMM 33-50-10-04-1. PN: 3301-51 PERFORMED OPS TEST IAW AMM 33-50-00-05-1. OPS TEST GOOD. REF CONT CARDS FOR DETAILS. 2 L 7 2 4T RT A52EU 2007092700004 20070927 00004 CE 2007 9 27 S2KA200709071 1 20070907 A 2435 66084582 STARTER GEN LEAR 35 31A 5170531 CE LT ENGINE FAILED E S2KA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 EA 03 211RN 669 072 STARTER GENERATOR FAILED DURING FLIGHT, CREW NOTICED VIBRATION FOLLOWED BY ILLUMINATION OF THE LEFT GENERATOR LIGHT. AI RCRAFT LANDED WITHOUT INCIDENCE AND STARTER GENERATOR WAS REPLACED. 2 L 7 2 4F RT A10CE 2007092700011 20070927 00011 WP 2007 9 27 MWEA070218 1 20070905 A 5330 59360151 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 LEFT LOWER FUSELAGE HAS A 6 INCH GOUGE APPROXIMATELY AT FRAME STATION 1190 LONGERON 23 LEFT. FABRICATED AND INSTALLED D OUBLER. 2 L 7 2 4F A6WE 2007092700013 20070927 00013 SO 2007 9 27 RAIA00709010 1 20070911 A 7830 THRUST REVERSER EMB 145 EMB145LR 3260212 SO NR 2 MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 CE 03 815HK 145048 FLT NR 5491 - STL - THRUST REVERSER NR 2 DISAGREE. MAINTENANCE DEFERRED PER MEL. 2 L 7 2 4T RT T00011AT 2007092700017 20070927 00017 NM 2007 9 27 AALA20071785 1 20070924 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 772AN 29580 JFK - EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT RIGHT NUMBER THREE DOOR POSITION FOR EMERGENC Y LIGHTS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007092700018 20070927 00018 SO 2007 9 27 RAIA00707013 1 20070912 A 5210 ROLLER EMB 145 EMB145 3260210 SO PAX DOOR OUT OF ADJUST A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 804HK 145082 PRE FLT NR 3574 - STL - MAIN DOOR WILL NOT OPEN. MAINTENANCE ADJUSTED DOOR ROLLER STOP. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007092700019 20070927 00019 NE 2007 9 27 AALA20071784 2 20070923 A 7323 FFG022AD GOVERNOR BOEING 757 757223 1384957 NM RROYCE RB211 RB211535* NE RT ENGINE INOPERATIVE A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SW 21 698AN 26980 31369 BDA INFLIGHT T1857/23SEP EWR TO SJU - RIGHT ENGINE UNABLE TO MAINTAIN CRUISE POWER. DIVERTED TO BDA AND LANDED WITHOUT INCIDENT. REPLACED FUEL FLOW GOVERNOR FOR RIGHT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2007092700021 20070927 00021 2007 9 27 AALA20071789 4 20070228 A 2565 SLIDE DOUG DC9 DC983 3022083 WP R1 DOOR DISLODGED A AALA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 980TW 53630 OKC RIGHT NUMBER ONE DOOR SLIDE DISLODGED FROM DOOR AND FELL TO RAMP. SLIDE WAS NOT ARMED. SLIDE BOTTLE PRESSURE SHOWS ZERO. REPLACED RIGHT NUMBER ONE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007092700023 20070927 00023 NM 2007 9 27 AALA20071793 1 20070727 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 902AN 29504 TUL - EMERGENCY LIGHTS AT AFT RIGHT COACH CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT RIGHT CO ACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092700024 20070927 00024 SO 2007 9 27 RAIA00709011 1 20070911 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO LT MLG MALFUNCTIONED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 817HK 145058 FLT NR 5523 - STL - UPON GEAR RETRACTION, LANDING GEAR LEVER DISAGREE ON EICAS. MAINTENANCE REMOVED AND REPLACED BOTH L EFT/HAND MAIN GEAR UPLOCK PROX SWITCHES AND THE CONNECTOR TO THE UPPER UPLOCK PROX SWITCH. SWING GEAR, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007092700025 20070927 00025 NM 2007 9 27 KCSA071379 1 20070917 A 3350 S1686B LIGHT BOEING 747 747212B 1384886 NM CABIN FAILED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 UPPER DECK AFT CEILING EMERGENCY LIGHT EXTINGUISHES AFTER 5 SECONDS. 2 L 7 4 4F A20WE 2007092700026 20070927 00026 NM 2007 9 27 ANCF200700020 1 20070920 A 3150 WARNING LIGHT DOUG MD80 MD83 3023681 NM COCKPIT MULTIPLE IND W ANCF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 23 583AN 53183 DURING TAKEOFF RUN AT 80 KNOTS "AUTO SPOILER FAIL" ANNUNCIATION CAME ON. AT 95 KNOTS SLAT "DISAG" LIGHT ILLUMINATED SLA T "TO" LIGHT WENT OFF AND "TO" WARNING SOUND: "SLATS" TO WAS DISCONTINUED IAW AMM 27-81-00 PAGE 109 WAS PERFORMED T/S; T O AUTO SPOILER SYSTEM AND AUTO SLAT SYSTEM T/O CONFIGURATION WARNING CHECK WAS OK; RESET AND BITE TO PSEU AND STALL WARN ING COMPUTERS OK. 2 L 7 2 4F RT 2007092700027 20070927 00027 EU 2007 9 27 AWXA200701119 1 20070911 A 5347 D53112782200 SEAT TRACK AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 SAL - MAJOR REPAIR - C-4 CHECK - NR 5975579, CORROSION ON CABIN SEAT TRACK, BS 808/FR 20, BS 843/FR 21 AND BS 897/FR 23, -Y765. REPLACED CABIN SEAT TRACK, BS 808/FR 20 - BS 897/FR 23, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007092700028 20070927 00028 EU 2007 9 27 AWXA200701120 1 20070912 A 5320 D5311283620200 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 SAL - MAJOR REPAIR - C-4 CHECK - NR 5975016, CORROSION ON CABIN FLOORBEAM, BS 808/FR 20, -Y189. REPLACED CABIN FLOORB EAM, BS 808/FR 20 - BS 897/FR 23, -Y189 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007092700029 20070927 00029 EU 2007 9 27 AWXA200701121 1 20070913 A 5315 D53472189202 FLOORBEAM AIRBUS 320 A320231 3930325 EU ZONE 200 - FUSEL CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 SAL - MAJOR REPAIR - C-4 CHECK - NR 5975709, CORROSION ON CABIN FLOORBEAM, BS 3207/FR 67, -Y1180. REPLACED CABIN FLOO RBEAM, BS 3207/FR 67, -Y1180 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007092500281 20070925 00281 NM 2007 9 25 SWAA074584 1 20070913 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007092500284 20070925 00284 EU 2007 9 25 07FDEA04014 1 20070919 A 5313 A53980668218 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 CORROSION ON STRINGER 42 RT, BETWEEN FRAME 72-73. STRINGER SPLICE REPAIR IAW SRM 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007092500287 20070925 00287 EU 2007 9 25 07FDEA04015 1 20070919 A 5320 A53981113200 SHEAR PLATE AIRBUS 310 A310324 3930206 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 CRACKED SHEAR PLATE AT STR 26 LT, BETWEEN FRAME 79-80. REPLACEMENT OF SHEAR PLATE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092500293 20070925 00293 EA 2007 9 25 QXEA200701416 1 20070915 A 3240 TRANSDUCER CNDAIR CL600 CL6002C10 1390015 EA WHEEL SPEED MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 606QX 10023 PDX - FLIGHT 2290 - ON TAXI, RECEIVED A ANTI-SKID OUTBOARD CAUTION MESSAGE AND A SPOILER STAB FAULT. RETURNED TO THE GA TE. MAINTENANCE FOUND THE BACKSHELL OF THE NR 1 WHEEL SPEED TRANSDUCER NOT ENGAGED. RESECURED AND RESET SSCU'S. OPERA TIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007092500297 20070925 00297 EU 2007 9 25 07FDEA03954 1 20070919 A 5320 A53986743210 WEB AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 THE WEB PLATE BETWEEN FRAME 86-87 RT, STRINGER 36 IS CRACKED. REPLACEMENT OF WEB PLATE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092500316 20070925 00316 NM 2007 9 25 SWAA074561 1 20070913 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007092500317 20070925 00317 NM 2007 9 25 SWAA074611 1 20070913 A 5311 6546531 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 22L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092500321 20070925 00321 NM 2007 9 25 SWAA074592 1 20070913 A 5311 6546560 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 947, STR 18L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007092500322 20070925 00322 NM 2007 9 25 SWAA074613 1 20070913 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, BL 0. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007092500323 20070925 00323 NM 2007 9 25 SWAA074612 1 20070913 A 5312 6546568 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD LOWER STIFFENER CRACKED AT BS 1016, 5 O'CLOCK POSITION. REPAIR ED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2007092500327 20070925 00327 NM 2007 9 25 SWAA074557 1 20070909 A 5330 6550570 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007092500329 20070925 00329 NM 2007 9 25 SWAA074563 1 20070913 A 5753 6573731 SKIN BOEING 737 7373A4 1384585 NM MID FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND LEFT WING INBOARD MID FLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007092500336 20070925 00336 NM 2007 9 25 SWAA074570 1 20070910 A 5754 65C26602 SLAT BOEING 737 7373A4 1384585 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT INBOARD LOWER END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007092500337 20070925 00337 NM 2007 9 25 SWAA074558 1 20070909 A 3350 65C27093 LENS BOEING 737 7373Y0 1384671 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007092500340 20070925 00340 NM 2007 9 25 SWAA074576 1 20070913 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092500348 20070925 00348 NM 2007 9 25 SWAA074582 1 20070913 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092500355 20070925 00355 2007 9 25 SWAA074593 4 20070913 A 2565 D31354433 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007092500375 20070925 00375 NM 2007 9 25 2007UALA03666 1 20070911 A 3260 WARNING SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 833UA 1401 LANDING GEAR NOT LOCKED MSG ON UPPER ECAM WITH HORN & ALERT LIGHTS ILLUMINATED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092500378 20070925 00378 NE 2007 9 25 2007UALA03670 2 20070912 A 7250 BLADE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT ENGINE FAILED A UALA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 WP 29 773UA 26929 777035 RTFL DUE TO RIGHT ENGINE FAILURE. ENGINE REPLACED. SHOP TEARDOWN REVEALED AN HPT STAGE-1 BLADE FAILED AT THE ROOT. THE REMAINDER OF THE TURBINE SUFFERED HEAVY RESULTANT DAMAGE. STRESS CORROSION CRACKING, A KNOWN FAILURE MODE, IS SUSPECTED , BUT COULD NOT BE CONFIRMED. CONSEQUENTLY, THE BLADE HAS BEEN RETURNED TO MANUFACTURER FOR FURTHER ANALYSIS. A NEW BLA DE WITH IMPROVED UNDER PLATFORM COATING IS BEING INCORPORATED AT SHOP VISIT. UA'S FLEET IS 50% MODIFIED. THE FLD BLADE WAS NOT CONTAINED IN ONE OF THE MODIFIED ENGINES. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007092500391 20070925 00391 EU 2007 9 25 07FDEA03966 1 20070919 A 5311 A53981259200 FRAME AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 CORROSION FOUND AT LT AFT PAX DOOR FRAME INNER FLANGE C73A, P 26-27 LT. REPAIR PERFORMED BY BLEND OUT UNTIL CORROSION R EMOVAL IAW EA 6-5318-81048 AND RAS/DATLS/0002044/2004 ISS. A 2 L 7 2 4F RT A35EU 2007092500392 20070925 00392 EU 2007 9 25 07FDEA03967 1 20070919 A 5330 A53778628 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 FOUND OLD EXTERNAL SKIN DOUBLER REPAIR AT FRAME 33 BETWEEN STRG 49-51 LT, NOT CONFORM TO PTOF CONVERSION: FRAME AND STRA P INSTALLATION FRAME 33 TO DRW, R537B1150-006. REPAIR PERFORMED BY NEW ENLARGED DOUBLER FOLLOW THE PRINCIPLE OF SRM 53- 10-12/FIG 225/SH 2, APPROVED BY RAS/DABRE/7004561/2004 ISSUE A. 2 L 7 2 4F RT A35EU 2007092500399 20070925 00399 NM 2007 9 25 07FDEA03974 1 20070919 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 755 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 MAIN DECK CARGO COMPARTMENT SEAT TRACK STA 755, X = 47.5 FOUND EDGE CHIPPED. 10-04-07 REPAIRED BY SECTIONAL SEAT TRAC K REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007092500404 20070925 00404 NM 2007 9 25 AWXA200701100 1 20070824 A 5754 114N20721 SLAT TRACK BOEING 757 7572S7 1384962 NM ZONE 500 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 MCN - MAJOR REPAIR - C-11 CHECK - NR 5988782, CORROSION ON LEFT WING NR 2 SLAT OUTBOARD TRACK, SS 665.75. REPLACED LEFT WING NR 2 SLAT OUTBOARD TRACK, SS 665.75 IAW B757-200 AMM 27-81-13-4. 2 L 7 2 4F RT A2NM 2007092500408 20070925 00408 EU 2007 9 25 CPCP20070104 1 20070824 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 414WF 414 FLOORBEAM AT FRAME 38 IS CORRODED. NEW FLOORBEAM INSTALLED IAW SRM 51-25-01 AND 51-25-04. 2 H 7 2 4T RT A53EU 2007092500409 20070925 00409 EU 2007 9 25 CPCP20070105 1 20070824 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 414WF 414 UPPER FLOORBEAM AT FRAME 41 IS CORRODED. UPPER FLOOR AT FRAME 41 IS REPAIRED IAW SRM 53-00-00 FIG 450. 2 H 7 2 4T RT A53EU 2007092500411 20070925 00411 WP 2007 9 25 IXXA070047O 1 20070911 A 5280 STRUCTURE DOUG DC8 DC871F 302199D WP MLG DOOR DAMAGED A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 821BX 88182 2287 45811 DURING CLIMB-OUT FROM KIAH, THE CREW NOTICED WHEN THE GEARS ARE UP RED LANDING GEAR UNSAFE LIGHT REMAINED ON, THE CREW R ECYCLED THE GEAR AND NO CHANGE, DURING UPLATCH CHECK GEAR UNSAFE LIGHT REMAINED ON, BUT DOOR LIGHT DID NOT ILLUMINATE. THE CREW FELT MOVEMENT AND VIBRATION DURING UPLATCH CHECK, PRESSURE AND QUANTITY OK. THE CREW RETURNED TO KIAH, AND LAN DED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE MAIN LANDING GEAR DOORS AND FOUND LEFT DOOR OUTER SECTION DAMAGED. MAI NTENANCE REMOVED THE DAMAGED SECTION OF THE DOOR, AND FOUND TO BE IN SAFE CONDITION TO FERRY FLIGHT TO KTOL. IN KTOL, M AINTENANCE REPLACED MAIN LANDING GEAR DOOR, AND MAIN LANDING GEAR DOOR CONTROL VALVE. MAINTENANCE ACCOMPLISHED OPERATIO 2 L 7 4 4F RT 4A25 2007092600016 20070926 00016 EU 2007 9 26 07FDEA04030 1 20070919 A 5414 A54611752504 PANEL AIRBUS 310 A310203 3930313 EU NR 2 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 CRACK (ABOUT 8MM) FOUND AT INBOARD SIDE WALL PANEL, RIB 8, PYLON NR 2 REPAIR PERFORMED IAW SRM 54-51-31 FIG 201. 2 L 7 2 4F RT A35EU 2007092600017 20070926 00017 EU 2007 9 26 07FDEA04031 1 20070827 A 5753 SKIN AIRBUS 310 A310222 3930315 EU TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 PREVIOUS REPAIR FOUND LOCATED ON RT OUTBD FLAP, UPPER SKIN, MAIN SPAR RIB 3. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT CONFORM WITH SRM REPAIR. NEW REPAIR WAS ACCOMPLISHED IAW FEDEX EA 6-5710-113163. 2 L 7 2 4F RT A35EU 2007092600033 20070926 00033 EU 2007 9 26 07FDEA04047 1 20070919 A 5347 A53611640212 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT SEAT TRACK C 15A-C19, Y-1959. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092600043 20070926 00043 EU 2007 9 26 07FDEA04052 1 20070919 A 5310 A52271028200 DOOR FRAME AIRBUS 310 A310203 3930313 EU ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT EMERGENCY EXIT DOOR, FRAME SEGMENT 3.1. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092600044 20070926 00044 EU 2007 9 26 07FDEA04053 1 20070919 A 5310 A52271017203 BEAM AIRBUS 310 A310203 3930313 EU ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT RT EMERGENCY EXIT DOOR, BEAM NR 5. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092600052 20070926 00052 NM 2007 9 26 DL764071232 1 20070913 A 3350 BATTERY PACK BOEING 767 767432ER 1385134 NM EMERGENCY LIGHTS NO TEST A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 831MH 29702 EMERGENCY BATTERY PACK M1210 FAILS DEEP CYCLE. REMOVED AND REPLACED M1210 EMERGENCY BATTERY PACK. OPS CK GOOD IAW B767 MM 33-51-07 . 2 L 7 2 4F RT A1NM 2007092600070 20070926 00070 EU 2007 9 26 07FDEA04073 1 20070920 A 5755 A57710027 SKIN AIRBUS 310 A310324 3930206 EU NR 2 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FOUND DELAMINATION ON SPOILER NR 2 LT, LOWER SKIN (100 BY 30 MM). REPAIR PERFORMED IAW SRM 57-70-00/201/PARA 12. 2 L 7 2 4F RT A35EU 2007092600075 20070926 00075 WP 2007 9 26 070158 1 20070914 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP ZONE 100 DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 881GA 49708 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007092600088 20070926 00088 EU 2007 9 26 07FDEA04094 1 20070920 A 5313 A53974228200 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT STRINGER SEGMENT C65, P54 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092600098 20070926 00098 NM 2007 9 26 HALA0700401 1 20070920 A 7830 PROXIMITY SENSOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE THRUST REVERSER MALFUNCTIONED A HALA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM DURING A CK, FOUND RT REVERSER GREEN LIGHT NOT ON WITH NR 2 ENG IN REVERSE. FOUND OUTBOARD PRO X SENSOR TARGET OUT OF RIG. ADJ TARGET. CKS OK, PER AMM 78-36-00. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092600108 20070926 00108 WP 2007 9 26 MWEA070219 1 20070917 A 2560 P4010021 BATTERY DOUG DC9 DC981 3022081 WP FLASHLIGHT INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 FORWARD GALLEY EMERGENCY FLASHLIGHT INSTALLED BACKWARDS. REMOVED AND REPLACED BATTERY AND INSTALLED FLASHLIGHT BACK IN HOLDER CORRECTLY. 2 L 7 2 4F A6WE 2007092600123 20070926 00123 WP 2007 9 26 MWEA070227 1 20070924 A 5230 PAN DOUG DC9 DC982 3022082 WP AFT CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 809ME 48071 AFT CARGO DOOR CORNER PAN CRACKED AT AFT LOWER SIDE OF DOOR. FABRICATED AND INSTALLED PAN. 2 L 7 2 4F A6WE 2007092600126 20070926 00126 EU 2007 9 26 2007UALA03162 1 20070813 A 3510 6490376 OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 479UA 1538 FIRST OBSERVERS SEAT QUICK O2 MASK INOP BOX ASSY NEEDS CHANGED. *S/D* REPLACED FIRST OBS O2 STOW BOX ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092600136 20070926 00136 2007 9 26 2007UALA03203 4 20070815 A 2210 6449038 ACTUATOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE YAW DAMP LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 853UA 1688 LOST GREEN HYD RESERVOIR FLUID. *S/D* LEAKING YAW DAMPER ACTUATOR. REPLACED YAW DAMP ACT, SERVICED GREEN SYS HYDRO - NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092600143 20070926 00143 NM 2007 9 26 ASAA0772048 1 20070916 A 5330 146A3215 SKIN BOEING 737 737790 13844CN NM BS 798-810 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 627AS 30794 FUSELAGE SKIN DENTED AND CREASED AT STA 807. REPAIRED IAW SRM 53-00-01. 2 L 7 2 4F RT A16WE 2007092600151 20070926 00151 NM 2007 9 26 2007UALA03697 1 20070913 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE E/E BAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 E/E COMPARTMENT, FLOORBEAM AT STA 246, APPROX RBL 19 HAS A CRACK IN VERTICAL STIFFENER. MAJOR REPAIR ACCOMPLISHED: REM OVED & REPLACED CRACKED STIFFENER. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092600178 20070926 00178 NM 2007 9 26 2007UALA03712 1 20070914 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EEL AT DOOR 1R GALLEY SIDEWALL INOP. 10-9-07 SECURED FEEDER CONNECTOR. EEL LIGHTS TESTED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092600197 20070926 00197 2007 9 26 2007UALA03732 4 20070915 A 2565 CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE OVERWING SLIDE KINKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 RIGHT OVERWING SLIDE AFT DOOR OPENING ACTUATOR CABLE, UNTWISTED, PREVIOUSLY BIRD CAGED, KINKED. 10-9-07 REMOVED AND REPLACED RH OW ESC SLIDE AFT ACT CABLE PER MM 25-65-10. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092700002 20070927 00002 WP 2007 9 27 ASAA0782024 1 20070914 A 5313 591143271 LONGERON DOUG DC9 DC983 3022083 WP BS 1415-1430 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 LONGERON IS CRACKED. REPLACED DAMAGED SECTION WITH SPLICE PER SRM 53-02. 2 L 7 2 4F RT A6WE 2007092700005 20070927 00005 EU 2007 9 27 AWXA200701115 1 20070912 A 5347 D53112833200 DUMMY RAIL AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 SAL - MAJOR REPAIR - C-4 CHECK - CORROSION ON CABIN DUMMY RAIL, BS 709/FR 16, -Y1379.5. REPLACED CABIN DUMMY RAIL, BS 7 09/FR 16, -Y1379.5 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007092700006 20070927 00006 EU 2007 9 27 AWXA200701116 1 20070912 A 5347 D53112818202 DUMMY RAIL AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 SAL - MAJOR REPAIR - C-4 CHECK - NR 5975014, CORROSION ON CABIN DUMMY RAIL, BS 709/FR 16, BS 732/FR 17, BS 808/FR 20, +Y 254. REPLACED CABIN DUMMY RAIL, BS 605/FR 12 - BS 950/FR 20, +Y254 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007092700012 20070927 00012 SO 2007 9 27 RAIA00709009 1 20070910 A 2751 WARNING SYSTEM EMB 145 EMB145 3260210 SO FLAP SYSTEM MALFUNCTIONED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 803HK 145077 FLT NR 3551 - SDF - FLAP FAIL MESSAGE STALL PROTECTION SYSTEM ADV MESSAGE. MAINTENANCE PERFORMED OPS CHECK OF FLAP SYST EM. NO DEFECTS NOTED. 2 L 7 2 4F RT T00011AT 2007092700016 20070927 00016 2007 9 27 AALA20071788 4 20070115 A 2565 SLIDE BOEING 737 737823 13844BZ NM L1 DOOR DISLODGED A AALA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 977AN 29550 BZE - LEFT NUMBER ONE DOOR SLIDE FELL OFF OF DOOR AND DID NOT DEPLOY. PLASTIC HOUSING COVER CAME LOOSE. SLIDE WAS DISA RMED. REINSTALLED SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092700030 20070927 00030 EU 2007 9 27 AWXA200701122 1 20070912 A 5320 D53480020342 SHEAR PLATE AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 SAL - MAJOR REPAIR - C-4 CHECK - NR 5975702, CORROSION ON CABIN SHEAR PLATE, BS 3257/FR 68 - BS 3310/FR 69, S23L. REPLA CED CABIN SHEAR PLATE, BS 3257/FR 68 - BS 3310/FR 69, S23L IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007092700031 20070927 00031 EU 2007 9 27 AWXA200701123 1 20070913 A 5320 D53112198200 FITTING AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 SAL - MAJOR REPAIR - C-4 CHECK - NR 5975764, CORROSION ON L1 DOOR THRESHOLD CENTER FITTING, BS 709/FR 16 - BS 783/FR 19, S23L. REPLACED L1 DOOR THRESHOLD CENTER FITTING, BS 709/FR 16 - BS 783/FR 19, S23L IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007092700032 20070927 00032 NM 2007 9 27 CALA0700517 1 20070914 A 3230 580250501 CABLE BOEING 737 737500 138449E NM RT MLG BINDING A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 15659 28920 THE GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM EWR. ABNORMAL PROCEDURES WERE FOLLOWED AND THE GEAR RETRACTED USING THE O VERRIDE TRIGGER, BUT STILL HAD PARTIAL ABNORMALITIES. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT . MAINTENANCE FOUND THAT THE RIGHT MLG GROUND SPOILER INTERLOCK VALVE CABLE (GROUND SENSE CABLE) WAS BINDING AND THE UP LOCK SENSOR TARGET WAS MISALIGNED (BENT) . THE RIGHT MLG GROUND SPOILER VALVE CABLE WAS REMOVED AND REPLACED AND THE GE AR WAS CYCLED SEVERAL TIMES WITH NO DEFECTS NOTED IAW MM 27-62-51 AND 32-32-00. IN ADDITION, THE RIGHT MLG UPLOCK SENSO R GAP WAS ADJUSTED IAW MM 32-61-21. 2 L 7 2 4F RT A16WE 2007092700033 20070927 00033 EU 2007 9 27 AWXA200701124 1 20070913 A 5320 D53112198201 FITTING AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 SAL - MAJOR REPAIR - C-4 CHECK - NR 5975761, CORROSION ON R1 DOOR THRESHOLD CENTER FITTING, BS 709/FR 16 - BS 783/FR 19, S23R. REPLACED R1 DOOR THRESHOLD CENTER FITTING, BS 709/FR 16 - BS 783/FR 19, S23R IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007092700036 20070927 00036 NM 2007 9 27 DU4R2007166 1 20070909 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM BS 1640 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 6711M 30483 FOUND FLOORBEAM CORRODED AT BS 1640 BL-0 RBL-4, W/L 208.1. REPAIRED BY CUTTING OUT CORRODED AREA. FABRICATED AND INSTA LLED FLOORBEAM 29-3/4” FROM BAC1505-100617/7075-T73 AND 2 REPAIR ANGLES 35 BY 1/4 BY 2-1/4 FROM 7075-T6 .063 AND 2 ANGLE S 41” BY 1-1/4 BY 2-1/4 FROM 7075-T6 .063 IAW B757 SRM 53-00-51 FIG 201, 51-20-01. 2 L 7 2 4F RT A2NM 2007092700037 20070927 00037 WP 2007 9 27 UPS07850655 1 20070816 A 5753 5614372503 FITTING DOUG DC8 DC873F 302199F WP LT FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 LEFT I/B FLAP CANOE FITTING I/B SIDE GOUGED. REPAIRED LEFT I/B FLAP CANOE FITTING IAW UPS EA 008-275 0-01-A1062 AND UPS RAA DC8-57-20229. 2 L 7 4 4F RT 4A25 2007092700038 20070927 00038 GL 2007 9 27 ARWA20070902 2 20070925 A 7200 ENGINE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 1 FLAMED OUT A ARWA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 19 68041 46900 451387 NR 1 ENGINE FLAMED OUT; ENGINE FAILED/SHUTDOWN IN FLIGHT CHECKLIST COMPLETED (ENGINE VIBRATION STOPPED) SHUTDOWN O505Z; WINDMILLING O.P. 10 PSI. TROUBLESHOOT FUEL SYSTEM AND FOUND METAL DEBRIE IN FUEL FILTER. REMOVED AND REPLACED FUEL PAC KAGE IN ACCORDANCE WITH M/M 73-12-01; FOUND SHROUDED FUEL TUBE AT 6 O'CLOCK DAMAGE. REMOVED AND REPLACED FUEL SHROUDED T UBE IN ACCORDANCE WITH M/M 73-13-02. OPERATIONAL CHECK NORMAL, NO LEAKS FOUND. 2 L 7 3 4F 4 F A22WE E23EA 2007092700040 20070927 00040 WP 2007 9 27 UPS07850657 1 20070815 A 5522 PANEL DOUG DC8 DC873F 302199F WP RT ELEVATOR GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 RIGHT ELEVATOR PANEL 75 CHAFED AND GOUGED. REPAIRED RIGHT ELEVATOR PANEL 75 IAW EO DC8-5720-7767 APP X A. 2 L 7 4 4F RT 4A25 2007092700042 20070927 00042 WP 2007 9 27 UPS07850659 1 20070826 A 5315 38956271 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 FLOORBEAM END FITTING HAS LARGE GOUGE AND CUT IN THE SIDE AT FS 8 AND RBL 30. REMOVED, FABRICATED AN D INSTALLED FLOORBEAM END FITTING IAW SRM 51-01-20D, DWG 3895627, SRM 51-1-8, SRM 51-3-0 AND SRM 51-3-2. 2 L 7 4 4F RT 4A25 2007092700043 20070927 00043 NM 2007 9 27 CHQA20070043 1 20070831 A 2740 3094334 TRIM SWITCH BOMBDR CL600 CL6002D15 NM GE CF34 CF343B1 NE CAPTAIN'S YOKE MALFUNCTIONED A CHQA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 11 638BR 7311 GEE872506 IAH TO SDF - WHILE CLIMBING THROUGH 12,000FT EXPERIENCED A NOSE DOWN PITCH TRIM RUNAWAY. ACCOMPLISHED PITCH TRIM RUNAWA Y MEMORY ITEMS AND DECLARED AN EMERGENCY. LANDED IN IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN 'S PITCH TRIM SWITCH, AND IT WAS OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2007092700044 20070927 00044 WP 2007 9 27 UPS07850660 1 20070814 A 5531 SPAR CAP DOUG DC8 DC873F 302199F WP VERTICAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 CORROSION ON INBOARD FACE OF VERTICAL STAB REAR SPAR CAP RIGHT SIDE AT 6 BOLTS ABOVE 2ND HINGE ARM. REPAIRED DAMAGED AREA OF THE VERTICAL STAB REAR SPAR CAP IAW SAA EA 008-5520-01-A1073, UPS RAA DC8-55-20109, AND FAA FOR M 8100-9. 2 L 7 4 4F RT 4A25 2007092700045 20070927 00045 WP 2007 9 27 UPS07850661 1 20070814 A 5531 SPAR CAP DOUG DC8 DC873F 302199F WP VERTICAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 HEAVY CORROSION ON INBOARD FACE OF VERTICAL STAB REAR SPAR LEFT CAP ABOVE NR 2 RUDDER HINGE ARM. REP AIRED DAMAGED VERTICAL STAB SPAR CAP ABOVE NR 2 RUDDER HINGE ARM IAW SAA EA 008-5520-01-A1073, UPS RAA DC8-55-20109, AN D FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007092700046 20070927 00046 NM 2007 9 27 CHQA200700044 1 20070909 A 2740 70609 TRIM SYSTEM BOMBDR CL600 CL6002D15 NM GE CF34 CF343B1 NE STAB MALFUNCTIONED A CHQA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 11 484CA 1321 7702 GEE873537 CHS TO IAH - AT 11,000FT DESCENDING TO 10,000FT, EXPERIENCED A STAB TRIM RUNAWAY. NOTICED STAB TRIM INDICATIONS FLUCTUA TING EXCESSIVELY, FOLLOWED BY AN IMMEDIATE DISCONNECT OF THE AUTOPILOT AND TRIM RUNAWAY CLACKER. COMPLETED MEMORY ITEMS AND QRH DECLARED EMERGENCY. CONTROL PRESSURE AT 10,000 FT WERE DIFFICULT, BUT IMPROVED DRAMATICALLY AS AIRCRAFT WAS CO NFIGURED FOR LANDING AND SLOWED. STAB TRIM RUNAWAY STOPPED AT 6.0 WHICH IS IN THE RANGE FOR NORMAL LANDING. LANDED WIT H FLAPS AT 20 PER QRH, COMPLETED ALL CHECKLISTS PRIOR TO APPROACH AND DID NOT NEED EXTRA TIME OR VECTORS. MAINTENANCE W AS ABLE TO DUPLICATE FAULT AND REMOVED AND REPLACED THE HSTCU, AND THE TEST FLIGHT WAS SUCCESSFUL. 2 L 7 2 4F 4 F RT A21EA E15NE 2007092700047 20070927 00047 WP 2007 9 27 UPS07850662 1 20070822 A 5531 SPAR CAP DOUG DC8 DC873F 302199F WP VERTICAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 EXFOLIATING CORROSION ON VERTICAL STAB RIGHT AFT SPAR AT STA ZV299. REPAIRED DAMAGED VERTICAL STAB S PAR CAP AT STA ZV299 IAW SAA EA 008- 5520-01-A1074, UPS RAA DC8-55-20110, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007092700048 20070927 00048 WP 2007 9 27 UPS07850663 1 20070822 A 5531 SPAR CAP DOUG DC8 DC873F 302199F WP VERTICAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 CORROSION ON VERTICAL STAB REAR SPAR CAP, RIGHT SIDE NEAR STA ZR=100. REPAIRED DAMAGED SPAR CAP ON V ERTICAL STAB REAR SPAR CAP AT STA ZR=100 IAW SAA EA 008-5520-01-A1067, UPS RAA DC8-55-20108, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007092700050 20070927 00050 SO 2007 9 27 CHQA200700045 1 20070513 A 2913 MPEV30086 PUMP EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL HYD SYSTEM LEAKING A CHQA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 11 836RP 17250 5942 14500713 CAE311994 CVG TO PWM - EN ROUTE HYDRAULIC 1 LOW QUANTITY INDICATION, FOLLOWED QRH AND APPROXIMATELY 3 MINUTES LATER, INDICATION WE NT TO NEAR ZERO. DECLARED EMERGENCY AND DIVERTED TO CLE. UPON LANDING RECEIVED ENG 1 HYD PUMP FAIL INDICATION AND FAIL URE OF HYDRAULIC SYSTEM 1. REQUIRED TUG TO GATE. MAINTENANCE INSPECTED AND FOUND HYDRAULIC FLUID COMING FROM DRAIN OF NR 1 SYSTEM EMDP. MAINTENANCE REMOVED AND REPLACED NR 1 SYSTEM EMDP, SERVICED AND OPERATIONALLY AND LEAK CHECKED PUMP. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007092700051 20070927 00051 SO 2007 9 27 02783 2 20070918 A 7421 RHB32S SPARK PLUG CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO HARTZL HCJ3Y PHCJ3YF1 GL NR 1 CYLINDER BROKEN E J4PA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 13 633SR 2014 689791 FP5906B DURING CRUISE FLIGHT FROM KPDK TO KGEV, THE ENGINE DEVELOPED A VIBRATION AND AIRCRAFT WAS LANDED AT KMRN. TWO PASSENGER S ONBOARD AND LANDED WITHOUT INCIDENT. IT WAS FOUND TO BE A NR 1 CYLINDER SPARK PLUG WITH A BROKEN INSULATOR CAUSING TH E ROUGH RUNNING AND VIBRATION. 1 L 7 1 3O 3 O NT A00009CH E3SO 5 C P36EA 2007092700052 20070927 00052 SO 2007 9 27 SIMA200726308 1 20070920 A 5320 14521725015 SILL EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 826AE 145592 DURING MBV INSPECTION, FOUND SERVICE DOOR AFT SILL CORRODED. REMOVED AND REPLACE AFT SILL IAW EMB SRM 51-40-02. AIRCRA FT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007092700053 20070927 00053 NE 2007 9 27 SA07059 2 20070916 A 7200 ENGINE AIRBUS A321 A321211 3930370 EU CFMINT CFM56 CFM565B3P 13006 NE NR 2 OVERTEMP A USAA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 19 165US 1431 779828 PHX - FLT 1540 EN ROUTE PHX TO CLT. AFTER ROTATION, CREW RECEIVED A NUMBER 2 ENGINE OVERTEMP WARNING. THE EGT WAS 972 DEGREES FOR 22 SECONDS. THE CREW SHUT DOWN THE NUMBER 2 ENGINE. THE FLIGHT RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. SINGLE ENGINE TIME WAS 20 MINUTES. MAINTENANCE BORESCOPED THE NUMBER 2 ENGINE, AND PERFORMED A FADEC NON-MO TOR CHECK AND A VBV VISUAL INSPECTION. NO DEFECTS WERE FOUND. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A28NM E37NE 2007092700054 20070927 00054 SO 2007 9 27 SIMA200726306 1 20070920 A 5320 14530643401 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 826AE 145592 DURING MBV INSPECTION, FOUND LT OMEGA BEAM CORRODED. REPAIRED OMEGA BEAM IAW SRM 53-00-10. AIRCRAFT WAS RETURNED TO SE RVICE. 2 L 7 2 4F RT T00011AT 2007092700055 20070927 00055 NM 2007 9 27 CALA0700518 1 20070914 A 5330 6546547 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17328 23458 INSPECTION FOUND A 0.2 INCH CRACK IN FUSELAGE SKIN TO FRAME SHEAR TIE AT STA 727, S14L. REPAIRED IAW ECRA 5310-04656. 2 L 7 2 4F RT A16WE 2007092700057 20070927 00057 SO 2007 9 27 SIMA200726309 1 20070920 A 5320 14000492403 PROFILE EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 826AE 145592 DURING MBV INSPECTION, FOUND VERTICAL PROFILE AT FRAME 23 AND STRINGER 15R CORRODED. REMOVED AND REPLACED PROFILE IAW E MB 140 SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007092700058 20070927 00058 SO 2007 9 27 SIMA200726304 1 20070919 A 5320 14522457003 PROFILE EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 826AE 145592 DURING MBV INSPECTION, FOUND CENTER HAT BEAM UPPER PROFILE TO RAMP PROFILE CORRODED AT FRAME 20 CROSSMEMBER. REMOVED AN D REPLACED PROFILE IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007092700063 20070927 00063 NM 2007 9 27 C1HA200781003 1 20070920 A 5315 1505100617 FLOORBEAM BOEING 727 7272S7 138407Z NM BS 380 CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 681CA 22020 CORROSION ON FLOORBEAM BS 380 BL O TO RBL 45. FABRICATED REPAIR FOR FLOOR BEAM BS 380 BL-O TO RBL - 45- AND INSTALLED I AW B727 53-10-8 FIG 3. 2 L 7 3 4F A3WE 2007092700064 20070927 00064 NM 2007 9 27 CIHA200781004 1 20070920 A 5347 15207927178 SEAT TRACK BOEING 727 7272S7 138407Z NM BS 344-480 CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 681CA 22020 CORROSION SEAT TRACK BS 344 - 480 LBL 45. REMOVED AND REPLACED SEAT TRACK BS 344 - 480 LBL 45 IAW B727 SRM 53-10-2 FIG. 7 AND 53-10-5 2 L 7 3 4F A3WE 2007092700067 20070927 00067 NM 2007 9 27 C1HA200781001 1 20070920 A 5714 SKIN BOEING 727 7272S7 138407Z NM CENTER WING CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 681CA 22020 WING CENTER SECTION LWR SKIN CORROSION, LT PRIMARY HEAT EXCHANGER PLENUM AREA. REMOVED CORROSION AND FOUND OUT OF LIMIT S IAW B727 SRM 57-30-1 FIG 4. REPAIRED IAW CHAMPION AIR, EO-727-5710-05. 2 L 7 3 4F A3WE 2007092700068 20070927 00068 NM 2007 9 27 CALA0700521 1 20070915 A 5314 6562125U26 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17326 23456 INSPECTION FOUND KEEL BEAM CORRODED AT STA 500D, S29R. THE KEEL BEAM WAS REPAIRED IAW SRM 53-60-12, REPAIR NR 3. 2 L 7 2 4F RT A16WE 2007092700071 20070927 00071 NM 2007 9 27 UIEA200700342 1 20070905 A 5753 PANEL BOEING 747 7472D7B 1384803 NM RT WING TE FLAP CONTAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 RT WING I/B T/E PANEL FOUND WATER. REPLACE RHW I/B T/E PANEL AS PER SRM 51-10-01 AND SRM 51-30-02. 2 L 7 4 4F RT A20WE 2007092700074 20070927 00074 NM 2007 9 27 UIEA200700344 1 20070905 A 5240 DOOR FRAME BOEING 747 7472D7B 1384803 NM BS 1275 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 R3 DOOR FWD UPPER CORNER FRAME FOUND CRACKED. C/OUT AS PER SRM 52-10-02, FIG 10. 2 L 7 4 4F RT A20WE 2007092700076 20070927 00076 NM 2007 9 27 NWAA073273119 1 20070922 A 5210 FE240004 CYLINDER DAMPER AIRBUS A319 A319114 3930350 NM PAX DOOR DISCHARGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 319NB 19450 19450 1346 DURING LINE CHECK, FOUND RT AFT CABIN DOOR EMERGENCY OPERATION CYLINDER PRESSURE AT ZERO. MSP LINE MAINTENANCE REPLACED DOOR CYLINDER PER AMM 52-13-14. 2 L 7 2 4F RT A28NM 2007092700077 20070927 00077 NM 2007 9 27 SWAA074639 1 20070916 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 430WN 33659 EEPLS INOP AT ROW 8 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007092700079 20070927 00079 NM 2007 9 27 SWAA074634 1 20070915 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 712SW 27846 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 10 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007092700080 20070927 00080 NM 2007 9 27 SWAA074628 1 20070914 A 3350 3071BPLEGPL LIGHT BOEING 737 737317 138447P NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 23 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007092700081 20070927 00081 2007 9 27 ARWA20070901 2 20070923 A 7200 ENGINE DOUG DC8 DC863F 302198F WP NR 1 POWER LOSS A ARWA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 19 441J 45988 ABORT TAKEOFF DUE TO NR 1 ENGINE UNABLE TO MAKE MAXIMUM TAKEOFF POWER EPR I-68 AT FIREWALL. ABORTED PRIOR REACHING 80 K NOTS. OPERATIONAL CHECKED NR 1 ENGINE AT ENGINE RUN-UP IN ACCORDANCE TO M/M 71-00; NOTED NR 1 EPR READING 0.1 LOW. ALL OTHER INDICATION NORMAL. ENTER NR 1 EPR IN DMI NR 21038 IN ACCORDANCE WITH MEL 77-1-2 CAT "A". CHECKED PT-2 & PT-7 L INES AND FOUND NORMAL IN ACCORDANCE WITH DC-8 M/M 77-11-0. CLEANED PT-7 LINE FOR DEBIRS IN ACCORDANCE WITH M/M 71-11-0; PERFORMED ENGINE RUN-UP, FOUND NORMAL IAW M/M 71-00; CLEARED DMI 21038. 2 L 7 4 4F 4A25 2007092700082 20070927 00082 NM 2007 9 27 SWAA074638 1 20070916 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 23 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007092700083 20070927 00083 NM 2007 9 27 SWAA074641 1 20070916 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 466WN 30677 EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007092700084 20070927 00084 NM 2007 9 27 SWAA074640 1 20070916 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 460WN 32464 EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007092700085 20070927 00085 NM 2007 9 27 SWAA074637 1 20070916 A 3350 417A5701 COVER BOEING 737 737705 13844SC NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 270WN 29089 EEPLS COVER LOOSE AT ROW 6 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007092700087 20070927 00087 NM 2007 9 27 SWAA074616 1 20070914 A 3350 471A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 257WN 32515 EEPLS COVER MISSING AT ROW 5 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007092700088 20070927 00088 NM 2007 9 27 SWAA074633 1 20070915 A 5755 65448114 FITTING BOEING 737 737317 138447P NM NR 4 SPOILER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED C4 CHECK, FOUND LEFT WING NR 4 GROUND SPOILER OUTBOARD ACTUATOR FITTING BROKEN. REMOVED AND REPLACED A CTUATOR PER MM. 2 L 7 2 4F RT A16WE 2007092700093 20070927 00093 NM 2007 9 27 SWAA074617 1 20070916 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092700094 20070927 00094 NM 2007 9 27 SWAA074618 1 20070916 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092700095 20070927 00095 NM 2007 9 27 SWAA074620 1 20070916 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092700097 20070927 00097 NM 2007 9 27 SWAA074627 1 20070914 A 5311 65C22910 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007092700098 20070927 00098 2007 9 27 SIMA200726703 4 20070921 A 3416 C14130AA ALTIMETER EMB 135 EMB135LR 3260305 SO STANDBY READS LOW A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 725AE 145312 NOTIFIED BY DISPATCH CREW ELECTED TO DIVERT TO LGA DISC-DURING CLIMB AT APPROX 15,000 STANDBY AIRSPEED STARTED TOWARD 0' BY 20,000 STANDBY AI SHOWED 0 AND STANDBY ALTIMETER WAS APROX 6,000 FT LOW. REMOVED AND REPLACED STANDBY AIRSPEED INDI CATOR AND STANDBY ALTIMETER. STANDBY AIRSPEED IND P/N OFF 64050-663-1 S/N OFF 5173. LEAK AND OPS CHECKS GOOD. AIRCRAF T RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007092700101 20070927 00101 NM 2007 9 27 SWAA074625 1 20070916 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092700102 20070927 00102 NM 2007 9 27 SWAA074644 1 20070916 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 908, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092700104 20070927 00104 NM 2007 9 27 SWAA074643 1 20070916 A 2913 849589 PUMP BOEING 737 7377H4 1384404 NM NR 2 ENGINE FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 29 765SW 29805 DIVERSION, HYDRAULIC B-SYSTEM FAILURE. REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYDRAULIC PUMP PER MM. 2 L 7 2 4F RT A16WE 2007092700105 20070927 00105 NM 2007 9 27 SWAA074624 1 20070916 A 5313 BAC1498 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 28R CORRODED AT BS 326. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007092700106 20070927 00106 NM 2007 9 27 SWAA07623 1 20070914 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED SPV CHECK, FOUND STRINGER 15L CRACKED AT BS 380. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007092700107 20070927 00107 NM 2007 9 27 SWAA074631 1 20070915 A 2560 PH22300L GLOWSTRIP BOEING 737 737317 138447P NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN BETWEEN ROW 14 DEF AND ROW 17 DEF. REMOVED AND REPLA CED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 2007092700108 20070927 00108 NM 2007 9 27 SWAA074629 1 20070914 A 2560 PH22300L GLOWSTRIP BOEING 737 737317 138447P NM CABIN DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND MID CABIN EEPLS PHOTOLUMINESCENT STRIPS DELAMINATED. REMOVED AND REPLACED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 2007092700109 20070927 00109 NM 2007 9 27 HNAA0700172 1 20070903 A 3610 16032311 PIPE DHAV DHC8 DHC8301 1386003 NM BLEED AIR SYS CRACKED A HNAA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 EA 07 343EN 340 F/A REPORTS, ELECTRICAL SMELL IN MID CABIN. FOUND BLEED PIPE CRACKED. FERRY TO ROA FOR REPAIR. 2 H 7 2 4T RT A13NM 2007092700112 20070927 00112 NM 2007 9 27 UIEA200700354 1 20070906 A 3210 LINK BOEING 747 7472D7B 1384803 NM RT MLG BROKEN A UIEA O OTHER O OTHER LD LANDING 1 EA 15 524MC 21784 ON LANDING INTO DOV, HEAVY SPARKS REPORTED DOWN RUNWAY. MX FOUND RIGHT BODY GEAR, FWD BRAKE TORSION LINK AT NR 10 BRAKE GAVE WAY, CAUSING DAMAGE (GROOVE) TO RUNWAY. BOTH THE NR 10 AND NR 12 BRAKES WERE REMOVED PER DDPG 32-5, AND THE AIRCR AFT WAS MADE READY FOR A MAINTENANCE FERRY FLIGHT WITH GEAR DOWN TO JFK. 2 L 7 4 4F RT A20WE 2007092700115 20070927 00115 NM 2007 9 27 UIEA200700356 1 20070822 A 5754 SKIN BOEING 747 7472D7B 1384803 NM LT WING LE FLAP DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 527MC 22471 LEFT WING NR 7 VARIABLE CAMBER FLAP OUTER SKIN HAS LOWER EDGE RIVETS LOOSE AND UPPER EDGE FASTENER HEADS BROKEN. REMOVE D LT WING NR 7 L/E FLAP TO FACILITATE ACCESS FOR SHEET METAL REPAIR. REPLACED RIVETS AND FASTENERS AS NECESSARY AS PER SRM 51-30-02. REINSTALLED FLAP IAW MM 27-81-02. 2 L 7 4 4F RT A20WE 2007092700120 20070927 00120 WP 2007 9 27 ASAA0782025 1 20070914 A 5313 593666715 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 LONGERON CORRODED. REPLACED DAMAGED SECTION WITH SPLICE PER SRM 53-02. 2 L 7 2 4F RT A6WE 2007092700122 20070927 00122 GL 2007 9 27 UIEA200700361 2 20070911 A 7250 1538M90P12 TURBINE BLADES GE BOEING 747 74747UF 1384812 NM GE CF6 CF680C2* GL HPT ROTOR CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 409MC 17179 17179 53X06214 30558 704892 ESN 704892 - HPT STAGE 1 BLADES AND STAGE 2 BLADES FOUND WITH UNDER PLATEFORM CORROSION AND CRACKS. STAGE 1 P/N 1538M90 P12 (80EA) STAGE 2 P/N 1881M52G05 (74EA). 2 L 7 4 4F 4 F RT A20WE E23EA 2007092700124 20070927 00124 NE 2007 9 27 DHLA200700045 2 20070922 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D17A 52049 NE NR 1 POWER LOSS A DHLA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 05 781DH 21996 NUMBER ONE ENGINE DID NOT MAKE TAKEOFF THRUST, TAKEOFF REJECTED. ABNORMAL PROCEDURE COMPLETED N1 INDICATION 86 PERCENT ALL OTHER ENGINE PARAMETERS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2007092700125 20070927 00125 NM 2007 9 27 UIEA200700384 1 20070921 A 5730 PANEL BOEING 747 7472D7B 1384803 NM LT WING DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 LT WING, UPPER LEADING EDGE FIXED PANEL AT WING STATION 766 HAS AN AREA OF 12.0 INCH BY 12.0 INCH OF DELAMINATION. PERM ANENT REPAIR WAS ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18, SHEETS 1, 3 AND 5, AND SRM 51-40-12. ALSO, REFERENCE ATLAS AIR XEO NR 57-092107. 2 L 7 4 4F RT A20WE 2007092700126 20070927 00126 NM 2007 9 27 UIEA200700385 1 20070921 A 5751 SKIN BOEING 747 7472D7B 1384803 NM RT AILERON DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 RT OUTBOARD AILERON HAS A 5.250 INCH SCRATCH/GROOVE AT UPPER LEADING EDGE. PERMANENT REPAIR WAS ACCOMPLISHED AS PER B74 7-200 SRM 51-40-02 FIG 1, SHEETS 1, 2 AND 3. TOTAL WEIGHT OF MATERIAL USED FOR THIS REPAIR IS 0.15 LBS AND DOES NOT REQ UIRE BALANCE ADJUSTMENT AS PER B747-200 SRM 51-80-02. ALSO, REFERENCE ATLAS AIR XEO NR 57-092107-1. 2 L 7 4 4F RT A20WE 2007092700127 20070927 00127 WP 2007 9 27 ASAA0782027 1 20070914 A 5320 59360717 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 INTERCOSTAL CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-4 AND 51-30-5. 2 L 7 2 4F RT A6WE 2007092700128 20070927 00128 NM 2007 9 27 NWAA073225506 1 20070818 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM BS 365 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 506US 23195 DURING "H" CHECK, FOUND CORROSION ON FLOOR SUPPORT ANGLE AT BS 365 BL 0. REPAIRED PER EA 55-209997. 2 L 7 2 4F RT A2NM 2007092700130 20070927 00130 EU 2007 9 27 AWXA200701127 1 20070920 A 5320 D53480048203 SILL AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 SAL - MAJOR REPAIR - C-4 CHECK - NR 5975813, CORROSION ON THE R2 DOOR CUT OUT SHAPE SILL, BS 3158/FR 66 - BS 3257/FR 68, 23R. REPLACED THE R2 DOOR CUT OUT SHAPE SILL, BS 3158/FR 66 - BS 3257/FR 68, 23R IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007092700131 20070927 00131 WP 2007 9 27 ASAA0782028 1 20070914 A 5313 3914677501 LONGERON SPLICE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 LONGERON SPLICE CORRODED. REPLACED SPLICE PER SRM 51-10-4 AND 51-30-5. 2 L 7 2 4F RT A6WE 2007092700133 20070927 00133 EU 2007 9 27 AWXA200701129 1 20070913 A 5320 D53480048202 SILL AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 SAL - MAJOR REPAIR - C-4 CHECK - NR 5975817, CORROSION ON THE L2 DOOR CUT OUT SHAPE SILL, BS 3158/FR 66 - BS 3257/FR 68, 23L. REPLACED THE L2 DOOR CUT OUT SHAPE SILL, BS 3158/FR 66 - BS 3257/FR 68, 23L IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007092700134 20070927 00134 EU 2007 9 27 AWXA200701130 1 20070912 A 5210 FE174004 DAMPER AIRBUS 320 A320231 3930325 EU ZONE 800 MALFUNCTIONED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 55102 18863 317 SAL - EES - C-04 CHECK - NR 5975045, THE L1 DOOR ASSIST DAMPER CYLINDER DOES NOT FUNCTION PROPERLY. REPLACED AND OPERAT IONAL CHECKED THE L1 DOOR ASSIST DAMPER CYLINDER IAW A320 AMM 52-11-14. 2 L 7 2 4F RT A28NM 2007092700137 20070927 00137 WP 2007 9 27 NWAA073219869 1 20070827 A 5330 SKIN DOUG DC9 DC951 3022051 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 778NC 48100 DURING "L" CHECK FOUND CRACKS IN FUSELAGE SKIN AT FORWARD UPPER CORNER OF FORWARD PASSENGER DOOR JAMB. REPAIRED PER EA 98-210174 SECT I. SECTION II INSPECTION TO BE PERFORMED EVERY 3000 CYCLES. PERMANENT REPAIR PER SECTION III TO BE ACCO MPLISHED ON OR BEFORE 2 YEARS/24 MONTHS AFTER SECTION I ACCOMPLISHMENT. 2 L 7 2 4F RT A6WE 2007092700145 20070927 00145 WP 2007 9 27 ASAA0782033 1 20070914 A 5320 9911500188 SUPPORT ANGLE DOUG DC9 DC983 3022083 WP NLG WW CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 NLG WHEEL WELL FORWARD BULKHEAD SUPPORT ANGLE CRACKED. REPLACED ANGLE PER SRM 51-30-02 AND 51-10-02. 2 L 7 2 4F RT A6WE 2007092700147 20070927 00147 WP 2007 9 27 ASAA0782035 1 20070914 A 5320 5936064503 FITTING DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 CARGO BAY STUB FRAME CLIP CORRODED. REPLACED CLIP PER SRM 51-10-3 AND DAC DWG 5936064. 2 L 7 2 4F RT A6WE 2007092700149 20070927 00149 WP 2007 9 27 ASAA0782037 1 20070914 A 5311 991224671 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 AFT ACCESSORY COMPARTMENT FRAME PUNCTURED. REPLACED DAMAGED SECTION OF FRAME WITH REPAIR DOUBLER PER SRM 51-70-4 AND 53 -14. 2 L 7 2 4F RT A6WE 2007092700151 20070927 00151 WP 2007 9 27 ASAA0782047 1 20070914 A 5320 995301630 ATTACH ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 AFT ACCESSORY COMPARTMENT FRAME TO SKIN ATTACH ANGLE CRACKED. REPLACED DAMAGED ANGLE PER SRM 51-10-4, 51-30-2 AND 51-30 -5. 2 L 7 2 4F RT A6WE 2007092700152 20070927 00152 WP 2007 9 27 ASAA0782039 1 20070914 A 5330 5936667 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 FUSELAGE DENTED. RECONTOURED SKIN AND INSTALLED REPAIR DOUBLER PER SRM 53-04. 2 L 7 2 4F RT A6WE 2007092700153 20070927 00153 WP 2007 9 27 ASAA0782040 1 20070914 A 5330 5924802133 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 FUSELAGE DENTED. COLD WORKED DENT AND INSTALLED INTERNAL DOUBLER PER SRM 53-04. 2 L 7 2 4F RT A6WE 2007092700154 20070927 00154 WP 2007 9 27 ASAA0782041 1 20070914 A 5330 593600731 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 FUSELAGE SKIN DENTED. COLD FORMED SKIN AND INSTALLED INTERNAL DOUBLER PER SRM 53-04. 2 L 7 2 4F RT A6WE 2007092700156 20070927 00156 WP 2007 9 27 ASAA0782043 1 20070914 A 5753 5910042511 VANE DOUG DC9 DC983 3022083 WP T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 LEFTHAND OUTBOARD CENTER FLAP VANE DENTED. COMPOSITE REPAIRED PER SRM 51-70-2. 2 L 7 2 4F RT A6WE 2007092700157 20070927 00157 WP 2007 9 27 ASAA0782044 1 20070914 A 5753 5930494501 VANE DOUG DC9 DC983 3022083 WP T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 LEFTHAND INBOARD FLAP VANE HAS MULTIPLE DENTS. REMOVED DAMAGED SECTION. INSTALLED FILLER AND REPAIR DOUBLER PER SRM 51 -70-2. 2 L 7 2 4F RT A6WE 2007092700158 20070927 00158 SO 2007 9 27 C2XA07CL078 1 20070915 A 3350 110049 POWER SUPPLY EMB 145 EMB145EP 3260221 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12934 145019 DURING ROUTINE MAINTENANCE THE AFT OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE N R 4 EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2007092700161 20070927 00161 EA 2007 9 27 SWIA200718695 1 20070909 A 3350 LENS CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS MISSING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 776SK 10241 GALLEY SERVICE DOOR OVERHEAD EMERGENCY EXIT SIGN LENS IS MISSING. INSTALLED GALLEY SERVICE DOOR OVERHEAD EMERGENCY EXIT SIGN LENS. 2 L 7 2 4F RT A21EA 2007092700163 20070927 00163 EA 2007 9 27 SWIA200718697 1 20070726 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 479CA 7675 ENGINE SUPPORT BEAM LOWER RIGHT WEB HAS INDICATION OF CRACK, FOUND AT C-CHECK. COMPLIED WITH REPAIR OF ENGINE SUPPORT B EAM LOWER RIGHT WEB IAW REO:601R-53-61-358 REV A. 2 L 7 2 4F RT A21EA 2007092700164 20070927 00164 EA 2007 9 27 SWIA200718698 1 20070726 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 479CA 7675 FS 621 RBL42 FLOOR SUPPORT ANGLE IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED NEW REPAIR ANGLE AND SPLICE AT FS 621 RBL 42 FLOOR SUPPORT ANGLE PER REO NO 601R-53-61-117 REV A. 2 L 7 2 4F RT A21EA 2007092700167 20070927 00167 EA 2007 9 27 SWIA200718700 1 20070918 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DIRTY A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 959SW 7840 FLT 6406 - FIRST FIVE ROWS OF EMERGENCY EXIT FLOOR LIGHTING INOP. CLEANED FLOOR EMERGENCY STRIP CONNECTOR. OPS CHECK G OOD. 2 L 7 2 4F RT A21EA 2007092700168 20070927 00168 EU 2007 9 27 NWAA073233352 1 20070919 A 2913 PUMP AIRBUS A330 A330223 3940031 EU HYD SYSTEM MALFUNCTIONED A NWAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 852NW 0614 AT CRUISE RECEIVED "HYD B ENG 1 PUMP LO PR","HYD B SYS LO PR" AND "HYD B RSVR LO LVL", LANDING WAS UNEVENTFUL. REPLACED PRESSURE LINE AND EDP AND CHECKED OK. 2 L 7 2 4F RT A46NM 2007092700172 20070927 00172 2007 9 27 AALA20071768 4 20070919 A 2565 100505201 GIRT BAR DOUG MD80 MD83 3023681 NM EMERGENCY SLIDE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9414W 53189 MSP - EMERGENCY SLIDE GIRT BAR HANDLE HOLDER WORN OUT AT AFT GALLEY DOOR. REPLACED SLIDE FOR EMERGENCY SLIDE GIRT BAR H ANDLE HOLDER AT AFT GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2007092700174 20070927 00174 NM 2007 9 27 AALA20071782 1 20070922 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 374AA 25201 DFW - EMERGENCY LIGHT EXIT MARKER AT RIGHT NUMBER ONE DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT EXIT MARKER AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007092700176 20070927 00176 NM 2007 9 27 AALA20071774 1 20070919 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 963AN 29543 DFW - EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092500384 20070925 00384 NM 2007 9 25 2007UALA03676 1 20070911 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 795UA 26927 SEATS 1E & 1F EACH HAVE ONE EEL LIGHT MISSING. 10-05-07 REPLACED LIGHT IN EACH SEAT POSITION. CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007092500389 20070925 00389 EU 2007 9 25 07FDEA03965 1 20070919 A 5315 A53974268200 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION IN AFT CARGO COMPARTMENT AT CROSSBEAM C 55/58 SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 201. 2 L 7 2 4F RT A35EU 2007092500393 20070925 00393 EU 2007 9 25 07FDEA03968 1 20070919 A 5320 A53778338248 SHEAR PLATE AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 CRACKED SHEAR PLATE BETWEEN FRAME 38.1-38.2, STRG 44 LT, FWD CARGO COMP. REPLACMENT OF SHEAR PLATE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092500412 20070925 00412 NM 2007 9 25 07FDEA03977 1 20070919 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 MAIN DECK CARGO COMPARTMENT SEAT TRACK STA 770, X = 75.25 FOUND EDGE CHIPPED. 10-04-07 REPAIRED BY SECTIONAL SEAT TR ACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007092500414 20070925 00414 EU 2007 9 25 07FDEA03979 1 20070919 A 5340 A53974275203 FITTING AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT FITTING OF CROSSBEAM C 55/58 , P45 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092500416 20070925 00416 NM 2007 9 25 07FDEA03981 1 20070919 A 5340 ATTACH FITTING DOUG MD11 MD11F 3023600 NM LT MLG WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 LEFT MAIN LANDING GEAR WHEEL WELL, FOUND STRUT ATTACHMENT FLIPPER DOOR CRACKED. 10-04-07 CARRIED OUT REPAIR AS PER S RM 52-10-00 FIGURE 18 VOLUME I. OPS CHECK CARRIED OUT AS PER AMM 32-31-00-700-803 FOUND 'SAT'. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007092500430 20070925 00430 NM 2007 9 25 2007UALA03683 1 20070911 A 2432 WARNING MESSAGE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 772UA 26930 BATTERY CHARGER APU; STATUS MESSAGE RECEIVED. 10-5-07 REPLACED APU BATTERY CHARGER, BATTERY, AND CARD M24406A4 IN PA NEL P310, OP CHECKS OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007092500432 20070925 00432 NM 2007 9 25 2007UALA03685 1 20070911 A 3250 STEERING SYS BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C 13802 EU NLG MALFUNCTIONED A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 308UA 23669 NWS PROBLEMS: WHEN CENTERED IT DRIFTS TO THE LEFT OCCASIONALLY. ALSO SEEMS TO BIND. FOUND STEERING METERING VALVE FA ULTY. REPLACED THE STEERING METERING VALVE AND PERFORMED A VISUAL INSPECTION OF STEERING CABLES. PERFORMED SEVERAL TA XI TESTS WITH NO BINDING OR PROBLEMS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092500439 20070925 00439 NM 2007 9 25 2007UALA03692 1 20070912 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 643UA 25093 EEL LIGHT AT LEFT AFT LAV INOP. 10-5-07 REPLACED 15" CROSS AISLE EEL SEGMENT IN THE AFT GALLEY. EEL CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092500446 20070925 00446 EU 2007 9 25 U1V2007F00000 1 20070801 A 3220 LN9037M5X22 BOLT DIAMON DA42 DA42 2990004 EU NLG TORQUE LINK BENT H U1VM O OTHER O OTHER NR NOT REPORTED 1 NM 07 104TS 616 42053 ON JUNE 28, 2007, THE NOSE LANDING GEAR TORQUE LINKS WERE REMOVED TO FACILITATE OTHER MAINTENANCE. THE 4 BOLTS USED TO SECURE THE TORQUE LINKS WERE FOUND TO BE BENT AND JOGGLED DUE TO , PRESUMABLY, SHEAR LOADS. (K) 1 L 7 2 3I RT A57CE 2007092600031 20070926 00031 EU 2007 9 26 07FDEA04045 1 20070919 A 5730 A57350101203 SKIN AIRBUS 310 A310203 3930313 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND ON RT WING UPPER SKIN PANEL RIB 15 T/E WAS CUT OUT AND A SEALING STRIP HAD COME A DRIFT. REPAIR PERFORMED BY REMO VING THE SEALING STRIP, ENSURE CUT OUT TO SMOOTH PROFILE AND INSTALL A NEW REPAIR STRIP ON UPPER SURFACE IAW EA 6-5720-8 1075 AND RAS/BAE/1105/2004 ISS A. 2 L 7 2 4F RT A35EU 2007092600034 20070926 00034 EU 2007 9 26 07FDEA04048 1 20070919 A 5313 A53773456202 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION ON STRINGER P 50 RT, C 23-25 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092600039 20070926 00039 NM 2007 9 26 HALA0700397 1 20070917 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 714-778 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 LEVEL 1 CORROSION ON SEAT TRACK RBL 11, AT STATION 714, 748, 763, 765, AND 778. REWORKED CORROSION, REWORKED AREAS FOUN D WITHIN LIMITS, PER SRM 53-00-52. REWORKED AREAS ALODINED AND PAINTED. 2 L 7 2 4F RT A1NM 2007092600062 20070926 00062 EU 2007 9 26 07FDEA04066 1 20070920 A 5320 A53988424205 STRUT AIRBUS 310 A310203 3930313 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT CROSS STRUT C 84 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092600067 20070926 00067 NM 2007 9 26 07FDEA04070 1 20070920 A 5320 WEB DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 588FE 48490 LEFT AIRCONDITIONING COMPARTMENT CENTER LOWER INBOARD WEB FOUND WITH CORROSION. 10-01-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-115193. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007092600068 20070926 00068 EU 2007 9 26 07FDEA04071 1 20070920 A 5320 A53988724205 STRUT AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT CROSS STRUT AT C87 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092600076 20070926 00076 WP 2007 9 26 070157 1 20070913 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 880GA 49625 DURING A PREFLIGHT INSPECTION FLIGHT CREW REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WAS INOP THE FI RST THREE METERS. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007092600084 20070926 00084 EU 2007 9 26 07FDEA04090 1 20070920 A 5313 A53973306200 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT STRINGER SEGMENT C 72, P45 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092600094 20070926 00094 EU 2007 9 26 07FDEA04100 1 20070920 A 5320 A53978264200 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CRACKED FITTING BETWEEN STRG 45-47 RT AT FRAME 67, CARGO COMP FLOOR STRUCTURE. REPLACEMENT OF FITTING IAW SRM 51-72-1 0. 2 L 7 2 4F RT A35EU 2007092600095 20070926 00095 NM 2007 9 26 HALA0700406 1 20070917 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 460-755 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 LEVEL 1 CORROSION ON SEAT TRACK LBL 88.5 AT STATION 460, 560, 591, 664, 654 +27, 693 AND 755. REWORKED AREAS, REWORKED AREAS FOUND WITHIN LIMITS PER SRM 53-00-52. REWORKED AREAS ALODINED AND PAINTED. 2 L 7 2 4F RT A1NM 2007092600101 20070926 00101 NM 2007 9 26 HALA0700404 1 20070911 A 5230 SKIN BOEING 767 76733A 1385209 NM CARGO DOOR DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28414 BULK CARGO DOOR EXTERNAL SKIN DENT DAMAGE 10" DOWN FROM TOP, 5" BACK FROM FRONT. DAMAGE HAD BEEN REWORKED AND PAINTED P REVIOUSLY. DAMAGE BEYOND LIMITS IAW SRM 52-30-01, DUE TO SHARP CREASE AT THE BOTTOM OF THE DOOR. ULTRASONIC THICKNESS PLOT CARRIED OUT. NEGLIGIBLE MATERIAL HAD BEEN REMOVED IN PREVIOUS REWORK. UNABLE TO OBTAIN CORRECT BLEND RATIO SO DAM AGE FILLED OUT IAW SRM 53-00-01 REPAIR 8, HOLE HFEC CARRIED OUT, RIVETED PATCH, IAW SRM 53-00-01 REPAIR 8. 2 L 7 2 4F RT A1NM 2007092600102 20070926 00102 NM 2007 9 26 HALA0700403 1 20070920 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 175-362 DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 FUSE SKIN LIGHTING STRIKES ON FASTENERS BS175 S27L, BS 196 S27L, BS 212, S25L, BS 220 S26-27L, BS 236 S27L, BS 244 S27L, BS 287 S24L - 25L, BS 305 S22L, BS 341 S 23L-24L, BS 362 S-23L. REWORKED PER SRM 53-00-01 FIG 201 REPAIR 8. 2 L 7 2 4F RT A1NM 2007092600106 20070926 00106 EU 2007 9 26 TRBA2007077 1 20070916 A 3350 SOCKET AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHT DIRTY A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 533AT 533 PASSENGER DOOR EMERGENCY EXIT LIGHT OUT. CLEANED LINE SOCKET AND OPS CHECK GOOD IAW JIC 33-50-00. 2 H 7 2 4T RT A53EU 2007092600113 20070926 00113 SO 2007 9 26 C2XA07CL080 1 20070917 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11113 145662 DURING ROUTINE MAINTENANCE THE RIGHT EMERGENCY EXIT SIGN DID NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE NR 5 INVE RTER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2007092600114 20070926 00114 NM 2007 9 26 F3LA200700241 1 20070914 A 5755 LUG AIRBUS A319 A319111 3930336 NM NR 3 SPOILER GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 921FR 5402 2010 DURING C-3 CHECK, INSPECTION REPORTED RIGHT WING NR 3 SPOILER ANTI-ROTATION LUG GOUGED. FABRICATED AND INSTALLED REINFO RCING PLATE FOR RIGHT NR 3 SPOILER CENTER HINGE FITTING IAW EA A9-57R-12143, REV A. 2 L 7 2 4F RT A28NM 2007092600115 20070926 00115 NM 2007 9 26 F3LA200700242 1 20070914 A 5755 LUG AIRBUS A319 A319111 3930336 NM NR 4 SPOILER GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 921FR 5402 2010 DURING C-3 CHECK, INSPECTION REPORTED LEFT WING NR 4 SPOILER ANTI-ROTATION LUG GOUGED. FABRICATED AND INSTALLED REINFOR CING PLATE FOR LEFT NR 4 SPOILER CENTER HINGE FITTING IAW EA A9-57R-12144. 2 L 7 2 4F RT A28NM 2007092600118 20070926 00118 NM 2007 9 26 CALA0700535 1 20070924 A 5340 BAC1493248 STRINGER CLIP BOEING 737 7373T0 1384582 NM BS 540 S26L CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70330 23460 INSPECTION FOUND STRINGER TIE IN FORWARD BAGGAGE BIN CORRODED AT STA 540, S26L. THE STRINGER TIE WAS REPAIRED IAW SRM 5 1-40-02 AND GMM 10-900-01. 2 L 7 2 4F RT A16WE 2007092600119 20070926 00119 NM 2007 9 26 CALA0700536 1 20070924 A 5340 6545783U502 BRACKET BOEING 737 7373T0 1384582 NM BS 500A CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70330 23460 INSPECTION FOUND A 1 INCH CRACK IN FORWARD BAGGAGE BIN STA 500A VHF ANTENNA MOUNTING BRACKET. A NEW ANTENNA MOUNTING BR ACKET WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007092600127 20070926 00127 EU 2007 9 26 2007UALA03168 1 20070814 A 2612 73040102 INDICATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FIRE DETECTION FAULTY A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 429UA 539 ENGINE 1 FIRE LOOP A FAULT INTERMITTENT. *S/D* FIRE DETECTION INDICATION UNIT FAULT. REPLACED 2WD1 FDIU. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092600129 20070926 00129 EU 2007 9 26 2007UALA03178 1 20070813 A 3510 SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE OXYGEN MASK LOOSE A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 420UA 489 REGUL LO PR DISPLAYED ON DOOR-OXY SYSTEM ECAM PAGE - DOOR-OXY. *S/D* LEAKING F/O MASK (PRESS TO TEST SWITCH LOOSE). R ESEATED PRESS TO TEST BUTTON AND SERVICED O2 SYSTEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092600132 20070926 00132 EA 2007 9 26 TRAX200701348 1 20070914 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 EMERGENCY LIGHTS REMAIN ON IN ARMED POSITION. 2 L 7 2 4F RT A21EA 2007092600135 20070926 00135 NM 2007 9 26 2007UALA03696 1 20070913 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD CABIN SHEAR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 FWD CABIN SHEAR TIE CRACKED AT BS 360 BETWEEN STR 14L & 15L. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKED SHEAR TIE. IN STALLED REPLACEMENT PART. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092600139 20070926 00139 NM 2007 9 26 SB07079 1 20070915 A 3350 20131ASM1 BATTERY PACK BOEING 737 7374B7 1384702 NM EMERGENCY LIGHTS DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 435US 24557 PVD - MAINTENANCE REPORTED THE AFT LEFT ENTRY DOOR OVERHEAD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLAC ED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007092600146 20070926 00146 NM 2007 9 26 HNAA0700168 1 20070911 A 3350 40005130003 SWITCH DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS MALFUNCTIONED A HNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 07 810EX 308 EMERGENCY LIGHTS FLICKER ON & OFF IN FLIGHT. PROBLEM FOUND TO BE IN F/A SWITCH. REMOVED AND REPLACED EMERGENCY LIGHT S WITCH. 2 H 7 2 4T RT A13NM 2007092600149 20070926 00149 NM 2007 9 26 CALA0700534 1 20070924 A 5313 BAC1498159 STRINGER BOEING 737 7373T0 1384582 NM BS 540 S26L CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70330 23460 INSPECTION FOUND STRINGER 26L CORRODED AT STA 540. A REPAIR WAS INSTALLED IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 2007092600152 20070926 00152 NM 2007 9 26 2007UALA03698 1 20070913 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE BS 246 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 677UA 30029 FLOORBEAM STA 246 VERTICAL STIFFENER LBL 40 CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED DAMAGED STIFFENER. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092600161 20070926 00161 NM 2007 9 26 2007UALA03707 1 20070913 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 644UA 25094 ENTIRE FIRST CLASS EEL LIGHTS INOP LEFT SIDE AND X AISLE. 10-9-07 RECONNECTED AND SECURED FEEDER CONNECTOR.OPS CHECKE D EEL LIGHTS, OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092600164 20070926 00164 NM 2007 9 26 KCSA071376 1 20070917 A 5311 FRAME BOEING 747 7472B4B 138481B NM BS 1880 S13R DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FUSELAGE FRAME DENTED AT BS 1880, STR 13R. 2 L 7 4 4F RT A20WE 2007092600165 20070926 00165 NM 2007 9 26 KCSA071377 1 20070917 A 5311 FRAME BOEING 747 7472B4B 138481B NM BS 400 S16L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FUSELAGE FRAME AND DOUBLER CRACKED AT BS 400, STR 16L. 2 L 7 4 4F RT A20WE 2007092600167 20070926 00167 EA 2007 9 26 HNAA0700169 1 20070912 A 3350 82410162005 CONTROL BOX DHAV DHC8 DHC8311 1386006 EA EMERGENCY LIGHTS INOPERATIVE A HNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 07 331EN 279 EMERGENCY LIGHT SYS FAILED OPS CHECK. REMOVED AND REPLACED EMERGENCY LIGHT CONTROL BOX. OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2007092600169 20070926 00169 NM 2007 9 26 BB07073 1 20070917 A 3397 WIRE BOEING 767 7672B7 1385107 NM EMERGENCY LIGHTS BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 256AY 26847 MAINTENANCE FOUND 1 EMERGENCY LIGHT INOPERATIVE IN AFT CABIN/GALLEY AREA. REPAIRED DAMAGED WIRING. NO FURTHER FAULTS. 2 L 7 2 4F RT A1NM 2007092600189 20070926 00189 NM 2007 9 26 2007UALA03724 1 20070914 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 520UA 24890 R-1 DOOR EXTERNAL EMERGENCY LIGHT IS INOP. 10-9-07 TROUBLESHOOTING THE SYSTEM, FOUND BROKEN GROUND JIFFY SPLICE WIRE , REPAIRED SPLICE ON DOOR 4L EMERGENCY LIGHT TEST SWITCH, ALSO REPLACED BATTERY PACK DOOR 4L FWD CEILING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092600199 20070926 00199 WP 2007 9 26 ASAA0782046 1 20070914 A 5230 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 AFT CARGO DOOR DENTED AT PREVIOUS REPAIR. REMOVED DAMAGED SECTION AND INSTALLED FILLERS FINGER DOUBLERS AND INTERNAL DO UBLER PER ASA EA5230 01382. 2 L 7 2 4F RT A6WE 2007092600205 20070926 00205 WP 2007 9 26 ASAA0782021 1 20070914 A 5311 995823967 FRAME DOUG DC9 DC983 3022083 WP BS 1361 CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 FRAME CHAFED. REMOVED DAMAGED AREA. INSTALLED REPAIR ANGLE FILLER AND REPAIR PLATE PER SRM 53-03. 2 L 7 2 4F RT A6WE 2007092700010 20070927 00010 NM 2007 9 27 SB07078 1 20070914 A 3260 BACC18Z3R CIRCUIT BREAKER BOEING 737 7374B7 1384702 NM COCKPIT FAULTY A USAA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 EA 19 445US 24863 CLT - FLT 1579 AFTER TAKEOFF FROM CLT, EN ROUTE TO JAX, THE CREW DID NOT RECEIVE ANY GEAR INDICATION LIGHTS TO VERIFY G EAR WAS UP AFTER RETRACTION. CREW RECYCLED GEAR PER QRH WITH NO HELP. PHONE PATCH WITH MAINTENANCE ADVISED ON RESETTIN G -LANDING GEAR AIR/GROUND RELAY & LIGHTS- CIRCUIT BREAKER THAT WAS FOUND TRIPPED. AFTER RESETTING CIRCUIT BREAKER, CRE W RECEIVED THREE GREEN LIGHTS CONFIRMING GEAR WAS UP. CAPTAIN DECIDED TO RETURN TO FIELD AT CLT TO HAVE AIRCRAFT CHECKE D. MAINTENANCE PERFORMED MULTIPLE LANDING GEAR RETRACTION AND EXTENSION WITH THROTTLES ADVANCED. NO FAULTS NOTED. AS PRECAUTIONARY, REMOVED AND REPLACED -LANDING GEAR AIR/GROUND RELAY AND LIGHTS- CIRCUIT BREAKER C404. AIRCRAFT OK FOR SE 2 L 7 2 4F RT A16WE 2007092700022 20070927 00022 NM 2007 9 27 AALA20071792 1 20070727 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 902AN 29504 TUL - EMERGENCY LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS CABI N. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092700035 20070927 00035 NM 2007 9 27 CALA0700516 1 20070913 A 3230 65917001222 UNKNOWN BOEING 737 737500 138449E NM RT MLG MALFUNCTIONED A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 15659 28920 AFTER T/O WHEN GEAR RETRACTED, A LOUD THUMP WAS HEARD AND SHUTTER WAS FELT. AFTER RETRACTION RT MAIN UNSAFE LIGHT ILLUM INATED. RECYCLED LANDING GEAR UP/DOWN AND STILL HAD A RED UNSAFE LIGHT W/GEAR UP POSITION. LOWERED LANDING GEAR, NO UN SAFE LIGHT. RETURNED TO FIELD FOR NORMAL LANDING. REF CITEX FOR RIGHT MAIN LANDING GEAR CHANGE AND GEAR SWING W/ NO DE FECT NOTED AT THIS TIME. 2 L 7 2 4F RT A16WE 2007092700049 20070927 00049 WP 2007 9 27 UPS07850664 1 20070809 A 5311 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 MAIN CABIN FRAME FITTING CRACKED AT STA 980 L19L. REPAIRED MAIN CABIN FRAME FITTING AT STA 980 L19L IAW SAA EA 008- 5310-01-A1020, UPS RAA DC8-53-20655, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007092700060 20070927 00060 NM 2007 9 27 C1HA200781006 1 20070920 A 5311 65C3440615 FRAME BOEING 727 7272S7 138407Z NM BS 1183 CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 681CA 22020 BS 1183 VERT FRAME RBL 35 WL 233 CRACK IN AFT RADIUS. STOP DRILLED CRACK AND INSTALLED REPAIR PARTS PER S/B 727-53-0192 REV 1 DATED 5/30/91. 2 L 7 3 4F A3WE 2007092700062 20070927 00062 NM 2007 9 27 CALA0700519 1 20070914 A 5230 6547952537 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17328 23458 INSPECTION FOUND A .5 INCH CRACK IN C-2 DOOR INNER SKIN AROUND LIGHTENING HOLE LIP 13.5 INCHES FROM THE LOWER EDGE OF DO OR AND 4.5 INCHES FROM THE FORWARD EDGE OF DOOR. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5232-01091. 2 L 7 2 4F RT A16WE 2007092700066 20070927 00066 NM 2007 9 27 CALA0700520 1 20070914 A 5230 6547952537 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17328 23458 INSPECTION FOUND A 0.3 INCH CRACK IN AFT CARGO DOOR SKIN AT LIGHTENING HOLE 7.5 INCHES FROM THE FORWARD EDGE OF THE DOOR AND 21.5 INCHES FROM UPPER EDGE OF THE DOOR. A REPAIR WAS INSTALLED IAW ECRA 5232-01091. 2 L 7 2 4F RT A16WE 2007092700070 20070927 00070 NM 2007 9 27 CALA0700522 1 20070916 A 5330 654576987 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17326 23456 INSPECTION FOUND SKIN CORRODED AT STA 492 BETWEEN S27R AND S28R. THE SKIN WAS REPAIRED IAW ECRA 5330-03720. 2 L 7 2 4F RT A16WE 2007092700089 20070927 00089 NM 2007 9 27 SWAA074622 1 20070914 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515A, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007092700090 20070927 00090 NM 2007 9 27 SWAA074621 1 20070914 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 366, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007092700091 20070927 00091 NM 2007 9 27 SWAA074630 1 20070914 A 5330 6545766 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 516 AND BS 500D, STR 16L AND STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007092700099 20070927 00099 EA 2007 9 27 SIMA200726701 1 20070922 A 2150 GG670950095 ACM CNDAIR CL600 CL6002C10 1390015 EA LEFT FAILED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 521AE 10142 CREW REPORTED TO MTX WHILE SITTING AT THE GATE LEFT PACK AUTO FAIL FOLLOWED BY LEFT PACK OVERHEAT CAUTION COCKPIT STARTE D FILLING UP WITH SMOKE. ISSUED PACK MEL REMOVED AND REPLACED AIR CYCLE MACHINE IAW 21-51-00. AIRCRAFT RETURNED TO SER VICE. 2 L 7 2 4F RT A21EA 2007092700100 20070927 00100 NM 2007 9 27 SWAA074626 1 20070916 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092700103 20070927 00103 2007 9 27 SWAA074642 4 20070916 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM EVAC SLIDE MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 632SW 27707 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2007092700110 20070927 00110 GL 2007 9 27 SIMA200726702 2 20070912 A 7261 CARBON SEAL EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL LT ENGINE LEAKING A SIMA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 805AE 145489 STRONG OIL ODOR IN BLEED/PACK SYSTEM AFTER TAKEOFF. MEL ISSUED 21-29 WHEN PACK NR 1 WAS FOUND CAUSING ODOR. REMOVED AN D REPLACED LT ZERO CARBON SEAL IAW EMB MM 72-25-25. PERFORMED OPS CHECK ON LT BLEED AIR SYS IAW EMB MM 21-20-00. NO OI L ODOR NOTED, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007092700114 20070927 00114 NM 2007 9 27 HNAA0700171 1 20070901 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM CARGO BAY MALFUNCTIONED A HNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 07 938HA 152 AFTER PUSHBACK AND ENGINE START, FLIGHT GO A BAG COMPARTMENT SMOKE DETECTOR WARNING LIGHT. CAPTAIN NOTIFIED F/A TO HAST ILY DEPLANE THE PASSENGERS AND HAD THE F/O CALL FOR A FIRE TRUCK TO CHECK IT OUT. THERE WAS NO FIRE OR SMOKE EVIDENT. 2 H 7 2 4T RT A13NM 2007092700132 20070927 00132 EU 2007 9 27 AWXA200701128 1 20070920 A 5315 D5311262200 FLOORBEAM AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 SAL - MAJOR REPAIR - C-4 CHECK - NR 5975013, CORROSION ON CABIN FLOOR SUPPORT ANGLE (JOINT COVER), BS 657/FR 14, -Y35. REPLACED CABIN FLOOR SUPPORT ANGLE (JOINT COVER), BS 657/FR 14, -Y35 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007092700139 20070927 00139 SO 2007 9 27 SWIA200718690 1 20070815 A 5310 RIB EMB 120 EMB120ER 3260203 SO WINDOW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 581SW 120349 LEFT DV WINDOW CENTER SUPPORT RIB AT AFT END OF CUT OUT IS CRACKED, DISCOVERED AT C-CHECK. REPLACED LEFT WINDOW CENTER SUPPORT RIB PER EMB SRM 51-40-02. 2 L 7 2 4T RT A31SO 2007092700146 20070927 00146 WP 2007 9 27 ASAA0782034 1 20070914 A 5320 993061225 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 RIGHTHAND CUSP WEB CORRODED. REPLACED DAMAGED SECTION WITH DOUBLER PER SRM 53-05. 2 L 7 2 4F RT A6WE 2007092700155 20070927 00155 WP 2007 9 27 ASAA0782042 1 20070914 A 5330 593602161 DOUBLER DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 TEMPORARY FUSELAGE SKIN REPAIR GOUGED IN AFT LAVATORY SERVICE DOOR AREA. REPLACED EXISTING REPAIR DOUBLER PER ASA ER 53 30 02233. 2 L 7 2 4F RT A6WE 2007092700162 20070927 00162 EA 2007 9 27 SWIA200718696 1 20070915 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 969SW 7876 FLT 5921 - EMERGENCY CEILING FLOOD LIGHT IS INOP. REPLACED CEILING FLOOD LIGHT BULB IAW CRJ AMM 33-51-00. 2 L 7 2 4F RT A21EA 2007092700170 20070927 00170 EU 2007 9 27 SIMA200726406 1 20070919 A 5347 7253742409 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 211NE 22399 5000 340B211 DURING A MBV INSPECTION, THE SEAT TRACK AT BL 36R WAS FOUND TO BE CORRODED. REPLACED SEAT TRACK WITH NEW ONE IAW CHAPTE R 53-70-60. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007092700171 20070927 00171 WP 2007 9 27 AALA20071765 1 20070919 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 412AA 49323 LGA - EMERGENCY LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD ELECTRIC BAY FOR EMERGENCY L IGHTS IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007092700177 20070927 00177 NM 2007 9 27 AALA20071772 1 20070919 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 963AN 29543 DFW - EMERGENCY LIGHT AT SEAT 14D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092700178 20070927 00178 GL 2007 9 27 UIEA200700363 2 20070911 A 7250 1538M90P12 TURBINE BLADES GE BOEING 747 74747UF 1384812 NM GE CF6 CF680C2* GL HPT ROTOR CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 409MC 20830 20830 53X06103 30558 706103 ESN 706103 - HPT STAGE 1 BLADES FOUND WITH UNDER PLATEFORM CORROSION AND CRACKS.STAGE 1 P/N 1538M90P12 (80EA). 2 L 7 4 4F 4 F RT A20WE E23EA 2007092700179 20070927 00179 NM 2007 9 27 UIEA200700366 1 20070918 A 5753 STRUCTURE BOEING BOEING 747 74747UF 1384812 NM TE FLAP DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 497MC 29258 AIRCRAFT ARRIVED IN DUBAI WITH DAMAGE TO THE LEADING EDGE CAP OF THE LEFT OUTBOARD AFT FLAP. INTERIM REPAIRED LEFT OUTB OARD AFT TRAILING EDGE FLAP AS PER SRM 57-53-01 REPAIR 1, FIGURE 201 AND XEO 57-091807. 2 L 7 4 4F RT A20WE 2007092700180 20070927 00180 NM 2007 9 27 9182007 1 20070918 A 7830 BACH8A08NN0246 HOSE BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE THRUST REVERSER DAMAGED A PCSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 17 994AJ 20942 696554 NR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON IN CLIMBOUT 6000 FT. LIGHT WENT OUT ON REDUCING POWER TO 1.4 EPR. THE AIRCRAF T RETURNED TO MIA. THE THRUST REVERSER FLEXIBLE HOSE WAS FOUND DAMAGED. THE HOSE WAS REPLACED AND THE AIRCRAFT RETURNE D TO SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2007092700182 20070927 00182 NM 2007 9 27 UIEA200700368 1 20070912 A 5730 SKIN BOEING 747 747230B 1384889 NM ZONE 600 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 SURF CORROSION EVIDENT AROUND FASTENER HEAD FROM WS 528 TO WS 724.5 BETWEEN FRONT SPAR AND MID SPAR. SURF CORROSION REM OVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 2007092700184 20070927 00184 NM 2007 9 27 UIEA200700369 1 20070912 A 5730 SKIN BOEING 747 747230B 1384889 NM ZONE 600 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 SURF CORROSION EVIDENT AROUND FASTENER HEAD FROM WS 528 TO SIDE OF FUS BODY BETWEEN FRONT SPAR AND MID SPAR. SURF CORRO SION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 2007092700186 20070927 00186 NM 2007 9 27 UIEA200700372 1 20070912 A 5730 SKIN BOEING 747 747230B 1384889 NM ZONE 600 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 RHW UPP SKIN PNL: WS1141-WS1337, FRONT SPAR TO REAR SPAR SEVERAL AREAS OF CORROSION EVIDENCED. SURF CORROSION REMOVED A ND REPROTECTED IAW SRM 51-10-01 AND SOPM 20-43-03. 2 L 7 4 4F A20WE 2007092700188 20070927 00188 SO 2007 9 27 C2XA07IA204 1 20070916 A 3260 8005701 SQUAT SWITCH EMB 145 EMB145EP 3260221 SO RT MLG INOPERATIVE A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 16927 145006 IAH - FLIGHT 2845, THE CREW REPORTED A GEAR LEVER AIR/GRND FAIL. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT I NCIDENT, AND MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE WEIGHT ON WHEELS PROXIMITY DETECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007092700189 20070927 00189 SO 2007 9 27 C2XA07IA203 1 20070915 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO CARGO BAY DEFECTIVE A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 34110 11810 41 145658 IAH - FLIGHT 2172, THE CREW REPORTED A BAGGAGE SMOKE INDICATION AFTER T/O. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE NUMBER TWO BAGGAGE SMOKE DETECTOR, OPER ATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007092700190 20070927 00190 NM 2007 9 27 UIEA200700374 1 20070912 A 5755 SKIN BOEING 747 747230B 1384889 NM ZONE 500 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 LHW SPOILER: NR 4 SPOILER O/B CORNER DELAMINATION EVIDENCE. REPAIR CARRIED OUT IAW SRM 51-40-24. 2 L 7 4 4F A20WE 2007092700191 20070927 00191 NM 2007 9 27 TSAA0732050 1 20070919 A 3260 189915 SENSOR BOEING 737 7372X6C 1384552 NM LT MLG OUT OF ADJUST A TSAA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 WP 13 840AL 23124 NON-ETOPS FLIGHT 913 HNL-LIH, ON APPROACH TO LIH, THE CREW PLACED THE LANDING GEAR HANDLE TO THE DOWN POSITION AND NOTED THAT THE LEFT MAIN LANDING GEAR INDICATION FAILED TO SHOW DOWN AND LOCKED. THE CREW DECLARED AN EMERGENCY AND ELECTED TO RETURN TO HNL. ON APPROACH TO HNL, WHEN THE LANDING GEAR WAS LOWERED AGAIN, ALL THREE LANDING GEAR INDICATED DOWN AN D LOCKED. THE CREW LANDED IN HNL WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE LEFT DOWN LOCK SENSOR PER AMM 32-6 1-31 AND COMPLETED A LANDING GEAR SWING TEST WITH ALL CHECKS SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007092700192 20070927 00192 NM 2007 9 27 UIEA200700348 1 20070905 A 5754 FRAME BOEING 747 7472D7B 1384803 NM ZONE 600 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 AFT REMOVAL OF L/E NOSE CAP FOUND THAT "D" SECTION CRACKED. CARRY OUT REPAIR AS PER SRM 57-20-03. 2 L 7 4 4F RT A20WE 2007092700196 20070927 00196 NE 2007 9 27 NWAA073245653 2 20070919 A 7200 ENGINE BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 1 FLAMED OUT A NWAA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION AP APPROACH 1 GL 01 553NW 26500 716494 DURING APPROACH DESCENDING THROUGH 20,000 FT, ENGINE NR 1 FLAMED OUT. FLIGHT CREW PERFORMED AN UNEVENTFUL LANDING. MAI NTENANCE REPLACED ENGINE NR 1. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092700200 20070927 00200 SO 2007 9 27 C2XA07IA205 1 20070915 A 3397 2LA00727830 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 13990 145277 EWR - FLIGHT 2762 THE CREW REPORTED AN ELECTRICAL SMOKE SMELL IN THE VICINITY SEAT 1A. FOUND LUMINESCENT LIGHT BULB ARC HING AT CONTACT PINS, LIGHT BULB REMOVED; SYSTEM CHECKED NO ARCHING NO SMELL. A/C RELEASED IAW MEL 33-20-00/1 CAT C CON TROL 129030, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT SUBSEQUENTLY RON'D IN IAH WHERE MAINTENA NCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007092700201 20070927 00201 SO 2007 9 27 SIMA200726401 1 20070920 A 2750 3631001005 FCU EMB 135 EMB135LR 3260305 SO TE FLAPS MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 707EB 145195 DURING TAKEOFF ROLL AIRCRAFT HAD A TRIPLE CHIME FOLLOWED BY FLAPS AURAL WARNING MESSAGE. AIRCRAFT ABORTED TAKEOFF AT 11 0KTS WITH NO OTHER DISCREPANCIES. FLAP CHANNEL 1 CURRENTLY UNDER MEL 27-9. CMC DOWNLOAD SHOWED FAULTS FLAP SHORT CIRCU IT AND FLAP RT MOTOR BRAKE FAIL CHECKED RESISTANCE OF LT/RT MOTORS AND FLAP POWER TRANSITION UNIT ALL GOOD RAR FLAP ELEC TRONIC CONTROL UNIT IAW EMB MM 27-53-02. OPS CHECK GOOD IAW EMB MM 27-53-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007092700202 20070927 00202 SO 2007 9 27 C2XA07IA206 1 20070914 A 3234 8271013 CONTROL HANDLE EMB 135 EMB135LR 3260305 SO COCKPIT DEFECTIVE A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 15527 323 323 145413 IAH - FLIGHT 2206, THE CREW REPORTED LANDING GEAR DOES NOT RETRACT PROPERLY, LANDING GEAR HANDLE SELECTED UP GEAR INDICA TION 3 DOWN FOR 5 - 10 SEC THEN IN TRANSIT AND THEN GEAR UP. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR HANDLE, OPS CHECK GOOD REF EMB 145 MM 32-32-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. 2 L 7 2 4F RT T00011AT 2007092700204 20070927 00204 EU 2007 9 27 MALA070119 1 20070919 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 452XJ 340B452 ARMED LIGHT FOR EMERGENCY LIGHTS ON FLIGHT ATTENDANTS PA PANEL IS INOP. REMOVED AND REPLACED SWITCH 5LN EMERGENCY LIGHT S ALL CHECKS GOOD IAW SF340 MM CH 33-50 SEE 409 CARD 291184 AND CONT CARD 020231 FOR DETAILS. MX NOTIFIED 4632. 2 L 7 2 4T RT A52EU 2007092700205 20070927 00205 EU 2007 9 27 AWXA200701125 1 20070912 A 5347 D53112830200 DUMMY RAIL AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 SAL - MAJOR REPAIR - C-04 CHECK - NR 5975012, CORROSION ON CABIN DUMMY RAIL, BS 683/FR 15, -Y81. REPLACED CABIN DUMMY R AIL, BS 683/FR 15, -Y81 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007092700208 20070927 00208 WP 2007 9 27 NWAA073269989 1 20070913 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 1004 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8945E 47181 DURING "H" CHECK, FOUND CRACKS AND WEAR IN FRAME ANGLE AT BS 1004 BS 0. REPAIRED PER EA 99-210176. 2 L 7 2 4F A6WE 2007092700209 20070927 00209 NM 2007 9 27 UIEA200700350 1 20070905 A 7810 NOZZLE BOEING 747 7472D7B 1384803 NM ZONE 400 DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 NR 3 ENGINE EXHAUST NOZZLE EXTERIOR SKIN DENTED AT 0900. NDT CHECKED NIL CRACK DENT AREA WITHIN LIMIT AMM 78-11-01 PAGE 601. 2 L 7 4 4F RT A20WE 2007092700212 20070927 00212 SO 2007 9 27 C2XA07SH072 1 20070919 A 5320 14530375001 CAP EMB 145 EMB145EP 3260221 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14947 145054 SHV - DURING C-CHECK CENTER OMEGA BEAM END CAP AT FR 23 HAS CORROSION. MX REMOVED AND REPLACED CENTER OMEGA BEAM END CA P AT FR23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 2007092700213 20070927 00213 NM 2007 9 27 UIEA200700346 1 20070905 A 5311 FRAME BOEING 747 7472D7B 1384803 NM ZONE 200 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 R1 MED LOWER AFT CORNER FRAME CRACKED AT STA 490 RT S-25R TO S-26R AREA. C/OUT AS PER SRM 52-10-02 FIG 10. 2 L 7 4 4F RT A20WE 2007092700214 20070927 00214 NM 2007 9 27 KCSA071382 1 20070919 A 3350 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 703CK 21939 UPPER DECK RT SLIDE LIGHT INOPERATIVE. 2 L 7 4 4F A20WE 2007092700215 20070927 00215 NM 2007 9 27 UIEA200700347 1 20070905 A 5753 WEB BOEING 747 7472D7B 1384803 NM TE FLAP CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 UPON L/E CAP REMOVAL OLES 1522, NR 26VC FLAP UPPER STOP FTG FWD WEB DOUBLER FOUND CRACKED. DOUBLER REPLACED IAW SRM 51- 10-01. 2 L 7 4 4F RT A20WE 2007092700216 20070927 00216 EU 2007 9 27 SA07060 1 20070917 A 3397 D9299200900000 WIRE HARNESS AIRBUS A319 A319112 3930323 EU CABIN SHORTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 711UW 1033 PHL - SEAT 8D LOW LEVEL EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED SEAT HARNESS FROM THE SEAT TO THE S IDEWALL. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007092700217 20070927 00217 NM 2007 9 27 UIEA200700349 1 20070905 A 7810 NOZZLE BOEING 747 7472D7B 1384803 NM NR 1 ENGINE DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 NR 1 ENGINE EXHAUST NOZZLE DENTED AT 0300. NDT CHECKED NIL CRACK DENT AREA WITHIN LIMITS AMM 78-11-01 PAGE 601. 2 L 7 4 4F RT A20WE 2007092700218 20070927 00218 EU 2007 9 27 SA07061 1 20070917 A 3350 32145410 EPSU AIRBUS A321 A321211 3930370 EU CABIN FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 187US 19913 1704 PIT - THE LEFT, MID-CABIN EMERGENCY POWER SUPPLY UNIT FAILED THE OPERATIONAL CHECK. MAINTENANCE REPLACED THE LEFT, MID- CABIN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007092700219 20070927 00219 NM 2007 9 27 AALA20071778 1 20070922 A 3350 CM3071BPEGPL BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 757AN 32636 JFK - EMERGENCY LIGHT AT SEAT 26C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007092700221 20070927 00221 WP 2007 9 27 ABXA070295 1 20070904 A 3350 60030451 POWER SUPPLY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 973AX 362 47511 EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW DC9 MM 33-53-02-4. 2 L 7 2 4F A6WE 2007092700222 20070927 00222 NM 2007 9 27 DL76L071242 1 20070920 A 4920 491003096 APU BOEING 767 767332 1382001 NM APU BAY MAKING METAL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 190DN 39131 28447 METAL FOUND IN ON APU CHIP DETECTOR. REPLACED APU. 2 L 7 2 4F RT A1NM 2007092700223 20070927 00223 WP 2007 9 27 ABXA070297 1 20070915 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 984AX 47258 EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM. 2 L 7 2 4F A6WE 2007092700224 20070927 00224 NM 2007 9 27 DL757071243 1 20070922 A 5510 SPAR BOEING 757 757232 1384965 NM HORIZONTAL STAB DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 612DL 22819 INSERVICE DAMAGE TO THE RT HORIZTONTAL STABILIZER LEADING EDGE, AUX SPAR WEB, AND AUX SPAR LOWER CHORD. REWORKED THE LE ADING EDGE, SPLICED IN A NEW SECTION OF AUX SPAR WEB, AND INSTALLED A REPAIR FOR THE AUX SPAR LOWER CHORD. 2 L 7 2 4F RT A2NM 2007092700229 20070927 00229 EA 2007 9 27 TRAX200701353 1 20070915 A 3350 BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 712EV 10074 NR 2 EMERGENCY LIGHTS BATTERY PACK IS FULLY DISCHARGED. NEEDS TO BE RECHARGED OR REPLACED. 2 L 7 2 4F RT A21EA 2007092700232 20070927 00232 EA 2007 9 27 TRAX200701355 1 20070915 A 3350 BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 712EV 10074 NR 4 EMERGENCY LIGHTS BATTERY PACK IS FULLY DISCHARGED. NEEDS TO BE RECHARGED OR REPLACED. 2 L 7 2 4F RT A21EA 2007092700233 20070927 00233 NM 2007 9 27 DL757071247 1 20070924 A 5414 311N345017 SKIN BOEING 757 757232 1384965 NM NR 2 NACELLE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 667DN 25035 NAC STA 128 CUTOUT FOR THE CENTER THRUST REVERSER FORWARD EQUALIZATION ROD ON THE NR 2 PYLON HAD A CRACK IN THE AFT HOLE AND EDGE DAMAGE ON THE FORWARD HOLE. DAMAGE WAS TRIMMED OUT AND A DOUBLER AND TRIPLER WERE INSTALLED. 2 L 7 2 4F RT A2NM 2007092700234 20070927 00234 EA 2007 9 27 TRAX200701356 1 20070915 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 EMERGENCY LIGHTS REMAIN ON WHEN IN ARMED POSITION. 2 L 7 2 4F RT A21EA 2007092700235 20070927 00235 NM 2007 9 27 AALA20071779 1 20070922 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 757AN 32636 JFK - EMERGENCY LIGHT AT SEAT 26C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007092700236 20070927 00236 EA 2007 9 27 TRAX200701357 1 20070915 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 EMERGENCY LIGHTS REMAIN ON WHEN IN THE ARMED POSITION. 2 L 7 2 4F RT A21EA 2007092700237 20070927 00237 EA 2007 9 27 COMA0760558 1 20070907 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION CR CRUISE 1 SO 01 659BR 7509 FLIGHT 5383 - FLIGHT LEVEL 32,000 FT, OAT -39C, FLAPS FAIL CAUTION MESSAGE. FLAPS FAILED AT 0 DEGREES. COMPLIED WITH A D 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RE SET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007092700238 20070927 00238 EU 2007 9 27 AALA20071780 1 20070922 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7083A 645 MIA - EMERGENCY LIGHT AT SEAT 32G INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 32G. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007092700239 20070927 00239 NM 2007 9 27 AALA20071781 1 20070922 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 634AA 24592 SJU - EMERGENCY LIGHTS AT SEAT ROWS 9 TO 16 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 9 TO 1 6. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092700245 20070927 00245 NM 2007 9 27 AALA20071769 1 20070919 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 963AN 29543 DFW - EMERGENCY LIGHT EXIT MARKER AT RIGHT AFT DOOR HAS BROKEN BASE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT EXIT M ARKER AT RIGHT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092700246 20070927 00246 EA 2007 9 27 COMA0760560 1 20070908 A 2620 M835366025M RELAY CNDAIR CL600 CL6002B19 1900309 EA FIRE PROTECTION FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 963CA 7127 FLIGHT 5180 - RECEIVED CARGO BOTTLE LOW MESSAGE. PERFORMED QRH, SQUIBS DID NOT TEST. DIVERTED TO CRW, LANDED WITHOUT INCIDENT. REPLACED RELAY K6HL. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007092700247 20070927 00247 WP 2007 9 27 AALA20071775 1 20070920 A 7933 SENSOR DOUG DC9 DC982 3022082 WP RT ENGINE INOPERATIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 426AA 49338 STL INFLIGHT T755/20SEP ORD TO SAT - RIGHT ENGINE OIL TEMPERATURE FLUCTUATED DURING CLIMB FROM 110 DEGREES TO 130 DEGREE S. AT CRUISE THE TEMPERATURE ROSE TO ABOVE 140 DEGREES. DIVERTED TO STL AND LANDED WITHOUT INCIDENT. REPLACED RIGHT E NGINE OIL TEMPERATURE SENSOR AND RIGHT ENGINE OIL FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007092700248 20070927 00248 NM 2007 9 27 AWXA200701112 1 20070917 A 2560 P2070001214 FLASHLIGHT BOEING 737 7373G7 1384595 NM MAIN CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 303AW 24010 PHX - EEL - 8813229 - MX REPORTED FWD F/A VERTICALLY MOUNTED EMERGENCY FLASHLIGHT NOT CHARGING. MX REPLACED THE FORWARD F/A FLASHLIGHT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2007092700249 20070927 00249 NM 2007 9 27 AWXA200701114 1 20070918 A 2611 PPA110100 SMOKE DETECTOR AIRBUS A319 A319132 3930340 NM LAVATORY FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 823AW 23204 8846 1463 PHX - OTH - LOG 7798768 - CREW REPORTED SMOKE LAV AND CARGO DET FAULT MESSAGE. MX REPLACED BOTH SMOKE DETECTORS. OPERA TIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007092700250 20070927 00250 EA 2007 9 27 COMA0760561 1 20070908 A 2620 M835366025M RELAY CNDAIR CL600 CL6002B19 1900309 EA FIRE PROTECTION FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 963CA 7127 FLIGHT 5180 - RECEIVED CARGO BOTTLE LOW MESSAGE. PERFORMED QRH, SQUIBS DID NOT TEST. DIVERTED TO CRW, LANDED WITHOUT I NCIDENT. REPLACED RELAY K7HL. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007092700251 20070927 00251 EU 2007 9 27 TRBA2007080 1 20070924 A 3350 7012210 LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT BURNED OUT A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 407AT 407 EMERGENCY EXIT LIGHT AT BASE OF MAIN CABIN DOOR IS BURNED OUT, EXTERNAL FLOOD LIGHT. REPLACED BULB ON MAIN CABIN DOOR E MERGENCY LIGHT ASSY. PERFORMED OPERATIONAL CHECK AND FOUND WORKING PROPERLY PER M/M 33-50-00. 2 H 7 2 4T RT A53EU 2007092700253 20070927 00253 NM 2007 9 27 AALA20071766 1 20070919 A 2910 HOSE BOEING 757 757223 1384957 NM HYD SYSTEM LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 698AN 26980 DFW INFLIGHT T1866/19SEP - DURING CLIMB CREW RECEIVED LEFT HYDRAULIC QUANTITY INDICATION FOLLOWED BY LOSS OF LEFT HYDRAU LIC SYSTEM PRESSURE. USED ALTERNATE FLAP EXTENSION AND GEAR PROCEDURES. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND LEFT HYDRAULIC LINE DAMAGE. REPLACED FLEX LINE IN RIGHT WHEEL WELL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007092700254 20070927 00254 EU 2007 9 27 AALA20071767 1 20070919 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4605R 3930308 EU LAVATORY INOPERATIVE A AALA O OTHER N FALSE WARNING DE DESCENT 1 SW 21 40064 507 MIA INFLIGHT T970/19SEP FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. LAVATORY Y SMOKE ALARM CHIME ALERTED FLIGHT ATTENDANT WITH INDICATION ON PURSER PANEL. LANDED MIA WITHOUT INCIDENT. DETERMINED IT WAS A FALSE ALARM. REPLACED SMOKE DETECT OR ASSEMBLY AT LAVATORY Y. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007092700255 20070927 00255 EA 2007 9 27 COMA0760563 1 20070909 A 2760 4916405 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA E&E BAY IMPROPER PART A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 920CA 25420 7022 FLIGHT 5781 - RECEIVED CONFIG SPOILER WARNING ON TAKEOFF. FOUND -5 AND -6 SECU'S INTERMIXED. REPLACED NR 2 SECU WITH - 6 NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007092700256 20070927 00256 NM 2007 9 27 AALA20071763 1 20070918 A 3397 WIRE BOEING 777 777223 1385213 NM EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 765AN 32879 ORD - EMERGENCY LIGHTS AT SEAT 20C INOPERATIVE. RELAMPED NO HELP. PLACARDED SEAT 20C. 20 SEP LHR REPLACED LIGHT ASSEMBL Y AND CHECKED HARNESS WITH NO FAULTS FOUND. SUSPECT JUNCTION BOX PROBLEM. FOUND WIRING DISCONNECTED. SECURED WIRING F OR EMERGENCY LIGHTS AT SEAT 20C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007092700257 20070927 00257 NM 2007 9 27 AALA20071764 1 20070918 A 3397 WIRE BOEING 777 777223 1385213 NM EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 765AN 32879 ORD - EMERGENCY LIGHTS AT SEAT 20G INOPERATIVE. RELAMPED NO HELP. PLACARDED SEAT 20C. REPLACED LIGHT ASSEMBLY AND CHE CKED HARNESS WITH NO FAULTS FOUND. SUSPECT JUNCTION BOX PROBLEM. FOUND WIRING DISCONNECTED. SECURED WIRING FOR EMERGE NCY LIGHTS AT SEAT 20G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007092700259 20070927 00259 EA 2007 9 27 COMA0760564 1 20070909 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 973CA 7146 FLIGHT 5578 - EMERGENCY LIGHTS ON SIDEWALL ROW 8AB NOT ILLUMINATED. RELAMPED EMRGENCY LIGHTS. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007092700261 20070927 00261 EA 2007 9 27 COMA0760566 1 20070910 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A COMA K NONE L NO TEST UK UNKNOWN 1 SO 01 973CA 2211 7146 EMERGENCY LIGHTS AT LEFT OVERWING EXIT NOT ILLUMINATED. REPLACED EMERGENCY LIGHT BATTERY PACK AND CHARGER ASSEMBLY. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007092700262 20070927 00262 EA 2007 9 27 COMA0760567 1 20070911 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 933CA 7040 FLIGHT 5459 - FLAP FAIL CAUTION MESSAGE RECEIVED. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. COMPLIED WITH AD 200 6-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET W ITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007092700263 20070927 00263 NM 2007 9 27 UPS07550679 1 20070826 A 5412 311N3271 BULKHEAD BOEING 757 75724APF 1384969 NM NR 2 PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 432UP 25463 INSPECTION TYPE:C NR 2 PYLON, AFT BULKHEAD (RT) OUTBOARD LOWER SURFACE CHAFED. BULKHEAD MILL WAS DONE ON TRAV T7/698748 PER PRELIMINARY 1 EA 757-5453-27-A1738. HFEC WAS DONE ON TRAV T7/698748 PER PRELIMINARY 1 EA 757-5453-27-A1738. 3. 1.2 5W X 2.1L X .040 REMOVED PER PRELIMINARY 1 EA 757-5453-27-A1738. 2 L 7 2 4F RT A2NM 2007092700265 20070927 00265 NM 2007 9 27 UPS07550687 1 20070919 A 5330 SKIN BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 429UP 25460 INSPECTION TYPE:N/A DENT IN FUSELAGE LEFT SIDE APPROX 5 FT AFT OF CREW ENTRY DOOR. ACCOMPLISHED HFEC INSP OF AREA PER N DTM PART 6, 51-00-19, NO CRACKS WERE DETECTED PP QC 0558905. ACCOMPLISHED INTERIM ACTIONS PER PARAGRAPH 6A OF EO B757-5 330-27682-A. OK FOR CONTINUED SERVICE. ACCOMPLISHED PERMANENT REPAIR WITHIN 30 DAYS. 2 L 7 2 4F RT A2NM 2007092700267 20070927 00267 WP 2007 9 27 UPS07850683 1 20070906 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C1 CORROSION ON FUSELAGE EXTERIOR L35L, STA 1075. REPAIRED DAMAGED EXTERIOR FUSELAGE SKIN AT STA L35L, STA 1075 IAW SAA EA 008-5330-01-A1087, UPS RAA DC8-53-20656, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007092700268 20070927 00268 WP 2007 9 27 UPS07850684 1 20070905 A 5320 ANGLE DOUG DC8 DC873F 302199F WP COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:N/A REFER TO LOG PAGE 657107. UPON REMOVAL OF CAPT SIDE WINDOW FOUND CORROSION ON LOWER ZEE ANGLE. BLE NDED ZEE ANGLE IAW MM IAW SRM 53-20. 2 L 7 4 4F RT 4A25 2007092700269 20070927 00269 2007 9 27 UPS07850685 4 20070918 A 2565 SLIDE DOUG DC8 DC873F 302199F WP PAX DOOR OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:N/A SLIDE CAME OUT OF COVER WHEN RT GIRT BAR WAS TAKEN OUT OF LOCK DETENT. RESECURED FWD ENTRY DOOR SLI DE/CONTAINER - SLIDE CHECKS OK IAW DC8 AMM 25-60-01-2. A/C OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2007092700270 20070927 00270 WP 2007 9 27 UPS07850686 1 20070917 A 3350 BATTERY DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PER 33-50-01-2, DC8 AMM . LIGHTS OP'S OK. 2 L 7 4 4F RT 4A25 2007092700271 20070927 00271 WP 2007 9 27 UPS07850689 1 20070918 A 3350 BATTERY DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT FAILED PREFLIGHT TEST. REPLACED BATTERY AND RELAY UNIT W/REF M 33-50-01-2, OPS TEST GOOD. 2 L 7 4 4F RT 4A25 2007092700273 20070927 00273 NM 2007 9 27 UPS07M50675 1 20070718 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C CENTER CARGO AT STATION 1658 TO STATION 1786 (BILGE AREA) LONGERON 52 STRINGER FOUND CORRODED AS MARKE D. ATTACH STA 1658-1879 LONG 52 SKIN FASTENERS & INNER AREA PARTS REMOVED PER SRM 51-31-01 VII R38. CORRODED LONG REMO VED PER SRM 53-10-00 VI R38. HFEC INSP C/O PER DAC NDTSPM R13 06-10-01.001, NO CRACK FOUND. REPAIR LONG & SPLICE FAB S RM 53-10-00 VI R38. FPI C/O DPS 4.707 REV AW ON FAB PARTS, NO CRACK FOUND. LONG PARTS & SPLICE INSTALLED SRM 53-10-00 VI R38. 2 L 7 3 4F RT A22WE 2007092700274 20070927 00274 NM 2007 9 27 UPS07M50676 1 20070807 A 5320 STRUCTURE DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C CENTER CARGO COMPT AT STATION 1841 IN BETWEEN LONGERON 51 LT TO 51 RT FOUND CORROSION AS MARKED. CTR CARGO COMPT STA 1841 BETWEEN L51 LT - L51 RT CORROSION REMOVED FOUND EXCEEDED LIMITS. REPAIR CHANNEL FAB FROM MAT'L 707 5-0 0.080". CHANNEL HEAT TREATED & HARNESS VALUES HRB 82.2 AS PER DPS 1.05-3. REPAIR CHANNEL REPROTECTED. REPAIR CHAN NEL PAINTED. REPAIR CHANNEL INSTALLED. PAINT TOUCHED UP ON REWORK AREA. 2 L 7 3 4F RT A22WE 2007092700275 20070927 00275 NM 2007 9 27 UPS07M50677 1 20070817 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE SCRATCHED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C CTR CABIN - SEAT TRACK FROM STA 1273 - STA 1381, +X27.5 SEVERAL SCRATCH MARKS FOUND ON CROWN & CHANNEL SURFACE AS MARKED. CABIN SEAT TRACK STA 1273 - 1381 X=27.5 SCRATCH MARK AT CROWN & CHANNEL SURFACE REMOVED FOUND EXCEE DS LIMIT. SEAT TRACK WITH SCRATCH MARKS TRIMMED OFF AT STA 1247 & 1391. HFEC INSP CUTOUT ON TRIMMED OFF FOUND NO CRACK . NEW SEAT TRACK, SPLICE HAT & PLATE FAB, HOLES PICK UP, REPROTECTED, PAINTED & INSTALLED. 2 L 7 3 4F RT A22WE 2007092700276 20070927 00276 NM 2007 9 27 UPS07M50678 1 20070817 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE SCRATCHED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C CTR CABIN - SEAT TRACK FROM STA 1273 - STA 1381 -X27.5 SEVERAL SCRATCH MARKS FOUND ON CROWN & CHANNEL SURFACE AS MARKED. CTR CABIN SEAT TRACK FROM STA 1273-1381 X=-27.5 RT SCRATCH MARKS ON CROWN & CHANNEL REMOVED FOUND EX CEEDS LIMIT. SCRATCH MARK SEAT TRACK TRIMMED OFF AT STA 1284 & 1391 REMOVE. HFEC INSP CUTOUT ON TRIMMED AREAS FOUND NO CRACK. NEW SEAT TRACK, SPLICE HAT & PLATE FAB, HOLES PICK UP, REPROTECTED, PAINTED & INSTALLED. 2 L 7 3 4F RT A22WE 2007092700277 20070927 00277 EA 2007 9 27 COMA0760568 1 20070913 A 2910 601R7514719 HYDRAULIC LINE CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYS LEAKING A COMA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 597SW 7293 FLIGHT 9456 - RECEIVED -HYD 2 LOW PRESS- CAUTION. HYD 2 QTY IS 0%. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLA CED LEAKING HYDRAULIC LINE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007092600059 20070926 00059 EU 2007 9 26 07FDEA04063 1 20070920 A 5753 SKIN AIRBUS 310 A310324 3930206 EU TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FOUND DELAMINATION AROUND OLD REPAIR ON TRAILING EDGE OF INNER FLAP RT, UPPER AND LOWER SKIN. REPLACEMENT OF RT INBOARD FLAP TRAILING EDGE PER DRW A579-70868, SOLID FASTENERS ARE REPLACED BY BLIND FASTENERS. REPAIR APPROVED BY EA 6-5752-9 2147 AND RAS/DABRE/7005360/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007092600065 20070926 00065 2007 9 26 C8GA20070009 2 20070914 A 7510 39270811 CONTROL VALVE BOEING 727 727223 1384074 NM ANTI ICE SYSTEM MALFUNCTIONED A C8GA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 29 899AA 22015 FLT 720 FROM TOL TO ATL, DURING CRUISE OPERATION THE AIRCRAFT EXPERIENCED ICING CONDITIONS WITH BOTH ENGINE AND WING ANT I-ICE ON, THE LOWER AFT CARGO SMOKE DETECTOR BELL RANG AND INDICATED A FIRE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. PERFORMED POST FLIGHT INSPECTION, CHECKED DUCTING AND VALVES VISUALLY, PERFORMED GROUND TEST ON BOTH WINGS, RAN ALL THREE ENGINES AND COULD NOT GET DUCT TEMP TO EXCEED 70 DEGREES C. INSPECTED CARGO FOR SIGNS OF S MOKE OR FIRE NONE NOTED. SMOKE DETECTION SYSTEM CHECKED GOOD. PRECAUTIONARY REMOVED AND REPLACED NR 2 ENGINE NOSE COWL ANTI-ICE THERMOSTATIC CONTROL VALVE, OPS CHECK GOOD. REMOVED AND REPLACED LOWER CARGO SMOKE DETECTOR CENTRAL CONTROL U 2 L 7 3 4F A3WE 2007092600073 20070926 00073 EU 2007 9 26 07FDEA04076 1 20070920 A 5753 SKIN AIRBUS 310 A310324 3930206 EU ZONE 500 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FOUND SEVERAL DELAMINATIONS TO TRAILING EDGE ON UPPER AND LOWER SKIN OF INBOARD FLAP LT. REPLACEMENT OF LT INBOARD FL AP TRAILING EDGE PER DRW A579-70868, SOLID FASTENERS ARE REPLACED BY BLIND FASTENERS. REPAIR APPROVED BY EA 6-5752-9214 7 AND RAS/DABRE/7005328/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007092600074 20070926 00074 EU 2007 9 26 07FDEA04078 1 20070920 A 5330 A53611658 SKIN AIRBUS 310 A310324 3930206 EU ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 803FD 378 FOUND OLD EXTERNAL DOUBLER REPAIR ON FUSELAGE SKIN AT BUTT-JOINT FRAME 18 BETWEEN STRG 22-26 LT, NOT CONFORM TO SRM (RIV ET SIZE). FOUND CORROSION AFTER REMOVAL. NEW DOUBLER REPAIR PERFORMED IAW DRW R536-11046 ISSUE B, HFEC AND ROTOTEST IN SPECTION PERFORMED. REPAIR APPROVED BY EA 6-5312-82883 AND RAS 037833/025/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007092600090 20070926 00090 EU 2007 9 26 07FDEA04096 1 20070920 A 5320 A53610607 FITTING AIRBUS 310 A310324 3930206 EU ZONE 100 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 OLD REPAIR, FRAME 17, STR 44 LT WITH NO OLD RECORDS FOR RUN OUT FITTING REPLACEMENT OR PERMANENT REPAIR. STRUCTURE RE PAIR PERFORMED IAW INSTRUCTION R536-10440 ISSUE C. 2 L 7 2 4F RT A35EU 2007092600091 20070926 00091 EU 2007 9 26 07FDEA04097 1 20070920 A 5230 A52374160206 SKIN AIRBUS 310 A310203 3930313 EU ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT AFT CARGO DOOR INNER SKIN, BETWEEN LONGERON 4-5. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51- 72-10. 2 L 7 2 4F RT A35EU 2007092600104 20070926 00104 NM 2007 9 26 DL757071240 1 20070920 A 5330 146N37505 SKIN BOEING 757 757232 1384965 NM FS 1653 S20L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 661DN 24972 DENT IN FUSELAGE SKIN AT STA 1653 STR 20L. SKIN CUTOUT AND A REPAIR DOUBLER WAS INSTALLED. 2 L 7 2 4F RT A2NM 2007092600110 20070926 00110 WP 2007 9 26 ASAA0782045 1 20070914 A 5753 5930495507 VANE DOUG DC9 DC983 3022083 WP TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 LEFTHAND INBOARD FLAP VANE DENTED. BONDED REPAIR DOUBLER IN DAMAGED AREA PER SRM 51-70-2. 2 L 7 2 4F RT A6WE 2007092600111 20070926 00111 SO 2007 9 26 LR7A07091 1 20070918 A 2697 WIRE LKHEED 382 382G 526414U SO OVERHEAT SWITCH BROKEN A LR7A A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 AL 03 403LC 1359 4590 DURING CRUISE, FLIGHT CREW REPORTED NR 4 ENGINE TURBINE OVERHEAT LIGHT CAME ON, RETARDED THROTTLES AND LIGHT WENT OUT AT 900 DEGREES AT 1856Z. MAINTENANCE REPAIRED WIRE AT TURBINE OVERHEAT SWITCH AND REPORTED OPERATIONAL CHECK SATISFACTORY . LOG PAGE 25371 ITEM 1. 2 H 7 4 4T A1SO 2007092600116 20070926 00116 NM 2007 9 26 CALA0700532 1 20070923 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND TOP SURFACE OF FLOORBEAM CORRODED AT FORWARD ENTRY STA 344, BL 0. REPAIRED FLOORBEAM IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2007092600117 20070926 00117 NM 2007 9 26 CALA0700533 1 20070923 A 5310 6520723U66 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70330 23460 INSPECTION FOUND A .5 INCH CRACK AT LOWER STOP PAD HOLES OF FORWARD BAG BIN DOOR CUTOUT AFT FRAME. THE FRAME WAS REMOVE D AND REPLACED IAW SRM 51-40-02 AND BOEING DRAWING 65-20723. 2 L 7 2 4F RT A16WE 2007092600121 20070926 00121 NM 2007 9 26 CALA0700523 1 20070916 A 2597 CIRCUIT BOARD BOEING 757 757200 1384950 NM PSU BURNED A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 13138 30351 SMOKE WAS NOTED FROM OVERHEAD PSU PANEL AT ROW 4 WHILE EN ROUTE FROM CGN TO EWR. HALON AND WATER FIRE EXTINGUISHERS WER E USED ON THE OVERHEAD AND THE AIRCRAFT WAS DIVERTED TO SNN WHERE IT LANDED WITHOUT INCIDENT. TROUBLESHOOTING FOUND PSU AT ROW 4 WITH A BURNT CIRCUIT BOARD. MEL WAS APPLIED TO PSU 3EF AND 4EF. 2 L 7 2 4F RT A2NM 2007092600125 20070926 00125 EU 2007 9 26 2007UALA02180 1 20070622 A 2700 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE VIBRATION A UALA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 446UA 834 ENCOUNTERED HIGH SPEED BUFFET AT FL260 AT 320 KNOTS. FLT ATTENDANT REPORTED UP & DOWN MOTION WORST IN AFT CABIN. *S/D* COMPLETED ELEVATOR PLAY CHECKS- ALL GOOD - RIGGED ELEV 5 DEG NOSE DOWN. NO REPEATS SINCE 21 JUNE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092600130 20070926 00130 EA 2007 9 26 TRAX200701346 1 20070914 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 870AS 7530 FLAPS FAIL AT 20' ON FINAL APPROACH INTO ATL- LANDING UNEVENTFUL. SELECTING FLAPS 30' WHEN THE FAILURE OCCURED. EMERGE NCY DECLARED. EMERGENCY EQUIP ON STANDBY. 2 L 7 2 4F RT A21EA 2007092600137 20070926 00137 NM 2007 9 26 KCSA071381 1 20070918 A 5311 FRAME BOEING 747 7472B4B 138481B NM BS 520 S12L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 BS 520 FRAME CRACKED AT STR 12L CUTOUT. 2 L 7 4 4F RT A20WE 2007092600138 20070926 00138 EU 2007 9 26 2007UALA03204 1 20070814 A 2611 RAI2800M0706 SMOKE DETECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO BAY FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 497UA 1847 CARGO SMOKE WILL NOT TEST ON OVERHEAD. FAULTY SDCU. REPLACED SDCU, ALL OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092600140 20070926 00140 NM 2007 9 26 ASAA0772050 1 20070916 A 5320 146A75034 FLOOR SUPPORT BOEING 737 737790 13844CN NM BS 800-813 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 627AS 30794 AFT PIT FLOOR SUPPORT AT STA 807 HAS MISDRILLED HOLES. REPAIRED IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2007092600141 20070926 00141 NM 2007 9 26 ASAA0772051 1 20070916 A 5321 453A261017 FLOOR PANEL BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 627AS 30794 AFT PIT FLOOR PANEL NR 3 CORRODED AT EDGES. REPAIRED IAW DRAWING 453A2610. 2 L 7 2 4F RT A16WE 2007092600145 20070926 00145 NM 2007 9 26 ASAA0772053 1 20070916 A 5542 SKIN BOEING 737 737790 13844CN NM RUDDER DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 COMPOSITE DAMAGE ON LOWER RT SIDE OF RUDDER. REPAIRED IAW SRM 51-70-05 REPAIR 10. 2 L 7 2 4F RT A16WE 2007092600147 20070926 00147 NM 2007 9 26 ASAA072055 1 20070912 A 5230 HOUSING BOEING 737 737890 1384527 NM DOOR HANDLE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 35176 FWD CARGO DOOR HANDLE HOUSING HAS INTERIOR SCRATCHES. REPAIRED IAW EA 5230 011213. 2 L 7 2 4F RT A16WE 2007092600148 20070926 00148 NM 2007 9 26 ASAA072057 1 20070918 A 5330 143A3232 SKIN BOEING 737 737890 1384527 NM BS 448-488 SCRATCHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 35175 RAMP CREW STRUCK FWD PIT SCUFF PLATE WITH BELT LOADER. TWO SMALL SCRATCHES ON EDGE OF SKIN AND BEAR STRAP. BLENDED EDG E OF BEAR STRAP AND SKIN. PERFORMED HFEC INSPECTION, CRACK FREE. REPLACED DAMAGED FWD AND CTR SCUFF PLATES IAW EA 5330 02237. 2 L 7 2 4F RT A16WE 2007092600153 20070926 00153 NM 2007 9 26 2007UALA03699 1 20070913 A 2701 YOKE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT LOOSE A UALA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 933UA 26659 YOKE HAS 1.5 UNITS OF PLAY IN-FLIGHT (LOOSE FEEL) BOTH LEFT AND RIGHT. PERFORMED CHECK OF CONTROL WHEEL PLAY AND BACKL ASH. CHECKED AILERON TRIM ACTUATOR MOVEMENT. CHECKED AILERON CONTROL CABLES AA, AB,ACBA AND ACBB.NO DEFECTS FOUND.CONT ROL WHEEL AILERON CONTROL PLAY WITHIN LIMITS. COULD NOT DUPLICATE REPORTED CONDITION ON GROUND, NO FURTHER REPORTS OF THIS CONDITION ON SUBSEQUENT FLIGHTS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092600166 20070926 00166 NM 2007 9 26 KCSA071378 1 20070917 A 5322 TENSION TIE BOEING 747 7472B4B 138481B NM BS 800 GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 MAIN DECK TENSION TIE AFT CHANNEL UPPER SURFACE GOUGED AT BS 800, LBL 22. 2 L 7 4 4F RT A20WE 2007092600180 20070926 00180 NM 2007 9 26 2007UALA03714 1 20070913 A 2820 LINE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUEL TRANSFER LEAKING A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 199UA 28717 UNWANTED FUEL TRANSFER PROBLEM. 10-9-07 AFTER TROUBLESHOOTING, ISOLATED PROBLEM TO CRACKED & LEAKING LT SCAVENGE SYS TEM. INSTALLED NEW SCAVENGE LINE PN 343U1023-35 REF 28-00-00-0201. SCAVENGE SYS OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092600181 20070926 00181 NM 2007 9 26 2007UALA03715 1 20070915 A 5210 ACCUMULATOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R2 DOOR READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 816UA 871 DOOR 2R EMERGENCY CYLINDER ACCUMULATOR PRESSURE LOW. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092600182 20070926 00182 NM 2007 9 26 2007UALA03716 1 20070915 A 3350 LIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU ROW 2AB FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 930UA 26655 BULLNOSE EMERGENCY EXIT LIGHT DIM ABOVE SEAT ROW 2AB. REPLACED AND OPS CHECKED THE BULLNOSE AISLE EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092600193 20070926 00193 2007 9 26 2007UALA03728 4 20070914 A 2565 STRAP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GIRT BAR BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 564UA 26666 NR 1 LEFT MED SLIDE GIRT BAR STRAP BROKEN RIVETS. 10-9-07 REPLACED LT MAIN ENTRY DOOR SLIDE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092600198 20070926 00198 EU 2007 9 26 YENA2007081 1 20070915 A 3234 9037B000104 HANDLE EMB ERJ190 ERJ190100IGW 3260408 EU MLG INOPERATIVE A YENA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 15 274JB 710 19000082 FLT 1703, BOS-BDA, RETURNED TO BOS, LANDING GEAR HANDLE WOULD NOT COME UP. REPLACED LANDING GEAR CONTROL LEVER IAW AMM 32-33-01-000-801-A. A/C JACKED IAW AMM 7-10-01, OPERATIONAL TEST OF THE LANDING GEAR EXTENSION AND RETRACTION SYSTEM AC COMPLISHED SUCCESSFUL IN IAW AMM TASK 32-33-00-710-801-A/500. NOSE GEAR AND MAIN GEAR SHOCK PRE-CHARGE CHECK SATISFACTO RY IAW AMM 12-12-09-600-802-A. JACKS REMOVED. A/C OK FOR SERVICE. 2 L 7 2 4F RT A57NM 2007092600201 20070926 00201 WP 2007 9 26 ASAA0782017 1 20070913 A 5320 593607133 INTERCOSTAL DOUG DC9 DC983 3022083 WP BS 1215 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 INTERCOSTAL CORRODED. REPLACED INTERCOSTAL PER SRM 51-30-5 AND 51-30-2. 2 L 7 2 4F RT A6WE 2007092700001 20070927 00001 WP 2007 9 27 ASAA0782022 1 20070914 A 5313 591143271 LONGERON DOUG DC9 DC983 3022083 WP CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 LONGERON CRACKED. REPLACED DAMAGED SECTION WITH SPLICE PER SRM 53-02. 2 L 7 2 4F RT A6WE 2007092700007 20070927 00007 EU 2007 9 27 AWXA200701117 1 20070913 A 5315 D53472190202 FLOORBEAM AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 SAL - MAJOR REPAIR - C-4 CHECK - NR 5975707, CORROSION ON CABIN FLOORBEAM, BS 3043/FR 64, +Y765. REPLACED CABIN FLOORBE AM, BS 3043/FR 64 - BS 3158/FR 66, +Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007092700008 20070927 00008 EU 2007 9 27 AWXA200701118 1 20070911 A 5347 D53112782202 SEAT TRACK AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 SAL - MAJOR REPAIR - C-4 CHECK - NR 5975580, CORROSION ON CABIN SEAT TRACK, BS 808/FR 20, BS 843/FR 21 AND BS 897/FR 23, -Y1292. REPLACED CABIN SEAT TRACK, BS 605/FR 12 - BS 950/FR 24, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007092700009 20070927 00009 SW 2007 9 27 304ME 1 20070802 A 2150 DRIVE BELT BOLKMS 117 BK117C2 5626002 SW TMECA ARRIEL ARRIEL1E 60034 NE AIR CONDITIONIN DETERIORATED E E3MA O OTHER O OTHER AA AIR AMBULANCE 1 EA 03 304ME 359 359 9097 THE AIR CONDITIONING DRIVE BELT HAD CRACKS IN IT AT A BELT TOTAL TIME OF 359.3. THE LIFE LIMIT OF THIS BELT IS 1000 HOUR S. 1 G 7 2 3U 3 U H13EU E19EU 2007092700014 20070927 00014 SW 2007 9 27 984ME 1 20070827 A 2110 COMPRESSOR BOLKMS 117 BK117C2 5626002 SW TMECA ARRIEL ARRIEL1E 60034 NE AIR-CONDITIONER SEIZED E E3MA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 03 984ME 759 759 9080 THE AIR-CONDITIONING COMPRESSOR SEIZED, THE DRIVE BELT CONTINUED TURNING, SMOKING UNTIL IT BROKE. 1 G 7 2 3U 3 U H13EU E19EU 2007092700020 20070927 00020 SO 2007 9 27 RAIA00709012 1 20070911 A 3231 22250100003 SOLENOID VALVE EMB 145 EMB145 3260210 SO NLG DOOR FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 805HK 19865 19865 145096 FLT NR 3535 - RIC - NOSE GEAR DOORS DID NOT CLOSE ON GEAR RETRACTION. MAINTENANCE REMOVED AND REPLACED NOSE GEAR DOOR V ALVE SOLENOID. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007092700039 20070927 00039 WP 2007 9 27 UPS07850656 1 20070815 A 5753 DOUBLER DOUG DC8 DC873F 302199F WP RT FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 RIGHT I/B FLAP STA 98 UPPER SURFACE EXISTING REPAIR DOUBLER GOUGED. REPAIRED RIGHT I/B FLAP STA 98 U PPER SURFACE IAW EO DC8-5720-7720-A. 2 L 7 4 4F RT 4A25 2007092700056 20070927 00056 SO 2007 9 27 SIMA200726307 1 20070920 A 5320 14000491013 SUPPORT EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 826AE 145592 DURING MBV INSPECTION, FOUND SERVICE DOOR AFT SILL SUPPORT CLIP CORRODED. REMOVED AND REPLACED CLIP IAW EMB SRM 51-40-0 2. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007092700059 20070927 00059 SO 2007 9 27 SIMA200726305 1 20070920 A 5320 14521725401 SILL EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 826AE 145592 DURING MBV INSPECTION, FOUND SERVICE DOOR FORWARD SILL CORRODED. REMOVED AND REPLACED FORWARD SILL IAW EMB SRM 51-40-02 . AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007092700061 20070927 00061 NM 2007 9 27 C1HA200781002 1 20070920 A 5347 15207927178 SEAT TRACK BOEING 727 7272S7 138407Z NM BS 400-420 CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 681CA 22020 CORROSION ON SEAT TRACK RBL 25-BS 400 - 420. REMOVED AND REPLACED SEAT TRACK RBL 25 BS 400 - 420 IAW B727 SRM 53-10-2 A ND 53-10-5 FIG 7. 2 L 7 3 4F A3WE 2007092700065 20070927 00065 NM 2007 9 27 C1HA200781005 1 20070920 A 5347 15207927178 SEAT TRACK BOEING 727 7272S7 138407Z NM BS 344-380 CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 681CA 22020 CORROSION ON SEAT TRACK BS 344 -480 LBL 25. REMOVED AND REPLACED SEAT TRACK BS 344 - 480 LBL 25 IAW B727 SRM 53-10-2 AN D 53-10-5 2 L 7 3 4F A3WE 2007092700072 20070927 00072 NM 2007 9 27 UIEA200700343 1 20070905 A 5320 WEB BOEING 747 7472D7B 1384803 NM BS 1980-2030 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 BULK CARGO BS 1980-2030 DOOR LOWER SILL FLOOR WEB, CORRODED. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-10-01 AND SRM 51-10-02 WITHIN ALLOWABLE LIMIT AS PER SRM 53-10-01. 2 L 7 4 4F RT A20WE 2007092700078 20070927 00078 NM 2007 9 27 DHL2007749006 1 20070924 A 5310 TORQUE BOX BOEING 727 727223 1384074 NM BS 1228 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 DURING "A" CHECK, REF N/R 099779 , DISCREPANCY, RT AIRSTAIR TORQUE BOX CRACKED AT LIGHTING HOLE BS 1228. STOP DRILLED AT THE END OF CRACK WITH .250" IAW B727 SRM 51-10-01. C/W HFEC IAW B727 NDTM, PT 6 51-00-00, FIG 23, CRACK TERMINATE IN STOP DRILL HOLE. FAB DOUBLER REPAIR FROM 7075-T6 .032" PO NR 9004042 DIM 5 3/8" BY 2 1/2" IAW SRM 53-10-2 FIG 6. TREA TED AND PRIMED DOUBLER IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM 53-10-2 FIG 6. 2 L 7 3 4F A3WE 2007092700086 20070927 00086 NM 2007 9 27 SWAA074636 1 20070916 A 3350 417A5701 LENS BOEING 737 737705 13844SC NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 270WN 29089 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007092700096 20070927 00096 NM 2007 9 27 SWAA074619 1 20070916 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092700113 20070927 00113 NM 2007 9 27 UIEA200700355 1 20070822 A 5753 SKIN BOEING 747 7472D7B 1384803 NM ZONE 500 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 527MC 22471 LEFT WING INBOARD FOREFLAP HAS 2" CRACK ON LEADING EDGE 12" FROM OUTBOARD EDGE. REPAIRED PER SRM 51-40-12 AND 51-40-08. 2 L 7 4 4F RT A20WE 2007092700117 20070927 00117 2007 9 27 HNAA0700170 4 20070820 A 3442 MI5853512RECON RADAR DHAV DHC8 DHC8102 2809003 NM WEATHER RADAR INOPERATIVE A HNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 07 809EX 302 FLIGHT 4353 MDT/PHL RETURNED TO MDT DUE TO THE WX RADAR WENT INOP. DUE TO WEATHER EN ROUTE THE FLIGHT COULD NOT CONTINU E. THE FLIGHT RETURNED TO MDT WITHOUT INCIDENT. 2 H 7 2 4T RT A13NM 2007092700135 20070927 00135 WP 2007 9 27 ASAA0782029 1 20070914 A 5320 99367183 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 INTERCOSTAL CORRODED. REPLACED INTERCOSTAL PER SRM 53 01 51 10 04 AND 51 30 05. 2 L 7 2 4F RT A6WE 2007092700138 20070927 00138 WP 2007 9 27 ASAA0782030 1 20070914 A 5347 593665505 CARGO TRACK DOUG DC9 DC983 3022083 WP CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 RIGHTHAND CARGO TRACK CORRODED. REPLACED TRACK PER SRM 51-10-4 AND 51-30-01. 2 L 7 2 4F RT A6WE 2007092700142 20070927 00142 EA 2007 9 27 SWIA200718692 1 20070914 A 2913 887055 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 NM 07 965SW 9976 1765 7871 FLT 5892 - HYDRAULIC 2 LO PRESS CAUTION MESSAGE APPEARED. REPLACED NR 2 EDP IAW CRJ AMM 29-11-01 AND INSPECTED NR 2 HYD RAULIC SYSTEM IAW AMM 05-51-33. 2 L 7 2 4F RT A21EA 2007092700143 20070927 00143 WP 2007 9 27 ASAA0782032 1 20070914 A 5320 9911500188 SUPPORT ANGLE DOUG DC9 DC983 3022083 WP NLG WW CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 NLG WHEEL WELL FORWARD BULKHEAD SUPPORT ANGLE CRACKED. REPLACED ANGLE PER SRM 51-30-02 AND 51-10-02. 2 L 7 2 4F RT A6WE 2007092700148 20070927 00148 WP 2007 9 27 ASAA0782036 1 20070914 A 5320 995301629 ATTACH ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 ACCESSORY COMPARTMENT FRAME TO SKIN ANGLE CRACKED. REPLACED ANGLE PER SRM 51-10-11, 51-30-02 AND 51-30-05. 2 L 7 2 4F RT A6WE 2007092700150 20070927 00150 WP 2007 9 27 ASAA0782038 1 20070914 A 5311 591359577 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 AFT ACCESSORY COMPARTMENT FRAME CRACKED. STOP DRILLED CRACKED AND REPAIRED PER SRM 53-03. 2 L 7 2 4F RT A6WE 2007092700169 20070927 00169 SO 2007 9 27 SIMA200726405 1 20070915 A 5320 14521413605 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO OMEGA BEAM CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 658AE 5000 145760 DURING A MBV INSPECTION, THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED. REPAIRED BEAM IAW SRM CHAPT ER 53-00-10 FIG 203. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007092700181 20070927 00181 NM 2007 9 27 UIEA200700367 1 20070912 A 5730 SKIN BOEING 747 747230B 1384889 NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 SURF CORROSION EVIDENT AROUND FASTENER HEAD FROM SIDE OF BODY TO WS 528 BETWEEN MID SPAR AND REAR SPAR. SURF CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 2007092700185 20070927 00185 NM 2007 9 27 UIEA200700370 1 20070912 A 5730 SKIN BOEING 747 747230B 1384889 NM ZONE 600 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 SURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM WS 724.50 TO WS 917.00 BETWEEN FRONT SPAR AND MID SPAR. SURF CORROS ION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 2007092700195 20070927 00195 NM 2007 9 27 AWXA200701131 1 20070921 A 5610 5893543110 WINDSHIELD BOEING 737 7373G7 1384595 NM COCKPIT CRACKED A AWXA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 28 302AW 31960 28129 24009 PHX - EL - LOG 7816283 - DURING CLIMB-OUT, THE FO'S WINDSHIELD OUTER PANE CRACKED. THE CREW RETURNED TO PHX. THE LANDI NG WAS UNEVENTFUL. MX REPLACED THE FO'S WINDSHIELD. OPERATIONAL/LEAK CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2007092700199 20070927 00199 SO 2007 9 27 SIMA200726404 1 20070919 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 658AE 9840 5000 145760 DURING A MBV INSPECTION, THE LT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED. REPAIRED BEAM IAW REPAIR STATEM ENT IC2007-145/06287 PARA 1 DATED SEPT 11, 2007. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007092700206 20070927 00206 NM 2007 9 27 DHL2007749005 1 20070924 A 5320 TORQUE BOX BOEING 727 727223 1384074 NM BS 1233 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 WHILE AT FLIGHTSTAR AIRCRAFT SERVICES FOR A CHECK, REF N/R 099780, DISCREPANCY, RT AIRSTAIR TORQUE BOX CRACKED AT LIGHTN ING HOLE ATBS 1233. STOPPED DRILLED HOLE AT THE END OF CRACK WITH .250 IAW SRM 51-10-01, C/W HFEC IAW NDTM PT 6, 51-00- 00 FIG 23, CRACK TERMINATED AT STOP DRILL, FAB DOUBLER REPAIR FROM 7075T6 .032 PO 9004042 DIM 5 BY 2.5 IAW SRM 53-10-2 F IG 6. INSTALLED DOUBLER REPAIR IAW SRM 53-10-2 FIG 6. 2 L 7 3 4F A3WE 2007092700210 20070927 00210 SO 2007 9 27 C2XA07SH071 1 20070919 A 5700 14571556007 PLATE EMB 145 EMB145EP 3260221 SO WING CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14947 145054 SHV - DURING C-CHECK PANEL 191 BONDING PLATES HAVE CORROSION. MX REMOVED AND REPLACED CORRODED BONDING PLATES ON PANEL 191 IAW EC 5750-01315 REV D. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 2007092700211 20070927 00211 EU 2007 9 27 NWAA073253201 1 20070919 A 2910 HYDRAULIC SYSTEM AIRBUS 320 A320211 3930320 EU LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 301US 031 LOST ALL GREEN HYDRAULIC PRESSURE AND FLUID AS GEAR RETRACTED AFTER TAKEOFF. CREW FOLLOWED COM PROCEDURES. AIRCRAFT TU RNED BACK TO MSP. ALTERNATE EXTENSION OF GEAR AND LANDING ACCOMPLISHED UNEVENTFULLY. AIRCRAFT TOWED OFF OF RUNWAY TO G ATE. REPLACED GREEN LEAK MEASUREMENT MANIFOLD, SWUNG GEAR, LEAK CHECKS OK. 2 L 7 2 4F RT A28NM 2007092700226 20070927 00226 EA 2007 9 27 TRAX200701351 1 20070915 A 5260 STEP CNDAIR CL600 CL6002C10 1390015 EA STAIRS BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 709EV 10068 BOTTOM CABIN STEP BROKEN. FLT 4476 DEL 92 MINS. 2 L 7 2 4F RT A21EA 2007092700231 20070927 00231 EA 2007 9 27 TRAX200701354 1 20070915 A 3350 BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 712EV 10074 NR 3 EMERGENCY LIGHTS BATTERY PACK IS FULLY DISCHARGED. NEEDS TO BE RECHARGED OR REPLACED. 2 L 7 2 4F RT A21EA 2007092700240 20070927 00240 EA 2007 9 27 COMA0760559 1 20070908 A 2760 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA SPOILER SYS MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 920CA 7022 FLIGHT 5619 - ON TAKEOFF ROLL RECEIVED CONFIG SPOILER WARNING, WITH SPOILERS IN CORRECT POSITION AND TAKEOFF OKAY MESSAG E. PERFORMED OPS CHECK WITH POWER RUN (80%). NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007092700241 20070927 00241 WP 2007 9 27 AALA20071776 1 20070922 A 3350 BULB DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 976TW 53626 SEA - EMERGENCY LIGHT AT SEAT 4E MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 4E. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A6WE 2007092700242 20070927 00242 WP 2007 9 27 AALA20071777 1 20070922 A 3350 LENS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 976TW 53626 SEA EMERGENCY LIGHT AT SEAT 4E MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 4E. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT A6WE 2007092700243 20070927 00243 NM 2007 9 27 AALA20071770 1 20070919 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 963AN 29543 DFW - EMERGENCY LIGHT EXIT MARKER AT LEFT AFT DOOR HAS BROKEN BASE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT EXIT MA RKER AT LEFT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092700244 20070927 00244 NM 2007 9 27 AALA20071771 1 20070919 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 963AN 29543 DFW - EMERGENCY LIGHT EXIT MARKER AT LEFT OVERWING HAS BROKEN BASE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT EXIT MA RKER AT LEFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092700260 20070927 00260 EA 2007 9 27 COMA0760565 1 20070910 A 3350 59257 INVERTER CNDAIR CL600 CL6002B19 1900309 EA CABIN FAULTY A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 954CA 7100 FLIGHT 5243 - EMERGENCY LIGHT FLOOR STRIP AND SIDEWALL EMERGENCY EXIT LIGHTS INOP ROWS 9CD THROUGH 6CD. FOUND NR 3 BATT ERY PACK INVERTER FAULTY. REPLACED INVERTER. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007092700272 20070927 00272 NM 2007 9 27 UPS07M50674 1 20070825 A 5330 AJC7060 SKIN DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 INSPECTION TYPE:4C RIGHT AFT EXTERIOR FUSELAGE SKIN STA 1879 TO 2153, LOWER AREA HAS CORROSION DAMAGE. REMOVED CORROSIO N FROM RIGHT AFT EXTERIOR FUSELAGE SKIN STA 1879-2153. ALL AREAS FOUND WITHIN LIMITS EXCEPT AT STA 2153 WAS OUT OF LIMI TS. CUT OUT DAMAGE, FABRICATED REPAIR FILLER & DOUBLER, AND INSTALLED REPAIR PARTS IAW MD-11 SRM 53-20-00 FIGURE 13. 2 L 7 3 4F RT A22WE 2007092700278 20070927 00278 EA 2007 9 27 COMA0760569 1 20070913 A 2751 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA RIGHT FAULTY A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 659BR 14456 7509 FLIGHT 5673 - RECEIVED FLAP FAIL MESSAGE. LANDED WITHOUT INCIDENT. REPLACED RIGHT BPSU AND PERFORMED EO 27-046AD. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007092700281 20070927 00281 NM 2007 9 27 QXEA200701448 1 20070921 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS FALSE ACTIVATION A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 402QX 4032 PDX FLIGHT NR 2466: FLAP POWER LIGHT ILLUMINATED. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE C/W FIM 27-50-00-810-802. N O DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007092700282 20070927 00282 EA 2007 9 27 COMA0760572 1 20070915 A 2760 FE210302 THROTTLE SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 920CA 33431 7022 FLIGHT 5423 - ON TAKEOFF RECEIVED CONFIG SPOILERS WARNING MESSAGE. PERFORMED REJECTED TAKEOFF. REMOVED AND REPLACED AC SU. 2 L 7 2 4F RT A21EA 2007092700283 20070927 00283 EA 2007 9 27 COMA0760573 1 20070916 A 2760 4916406 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAULTY A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 920CA 11510 7022 FLIGHT 5548 - ADVANCING THRUST LEVER FOR TAKEOFF RECEIVED CONFIG SPOILERS WARNING. ABORTED TAKEOFF. REMOVED AND REPLAC ED NR 1 SECU. 2 L 7 2 4F RT A21EA 2007092700285 20070927 00285 EA 2007 9 27 COMA0760574 1 20070916 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 917CA 7017 FLIGHT 5040 - DURING APPROACH TO LANDING FLAPS FAIL CAUTION MESSAGE. ACCOMPLISHED QRH THEN LANDED SAFELY. COMPLIED WIT H AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WA S RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007092700286 20070927 00286 EA 2007 9 27 COMA0760575 1 20070916 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA A/C BAY MALFUNCTIONED A COMA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 01 934CA 7042 FLIGHT 5546 - DURING CLIMB COCKPIT SHUT OFF WITH ONLY A LEFT PACK STATUS MESSAGE, LEFT PACK WAS RESET AND CONTINUED TO F UNCTION NORMAL. LATER AT FLIGHT LEVEL 250 FT LEFT PACK SHUT OFF TO LEFT PACK HIGH TEMP. DESCENDED TO 10,000 LEFT PACK WAS RESET AND CONTINUED TO FUNCTION NORMALLY. PERFORMED OPS CHECK OF LEFT PACK, SYS CONTROLLABLE IN AUTO AND MANUAL MOD E. 2 L 7 2 4F RT A21EA 2007092700290 20070927 00290 NM 2007 9 27 AALA20071794 1 20070827 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 933AN 30080 TUL - EMERGENCY LIGHTS AT FORWARD ENTRY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD ENTRY CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092700291 20070927 00291 NM 2007 9 27 SWAA074657 1 20070918 A 3350 210013 SWITCH BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED MV2 CHECK, FOUND AFT LIGHT ATTENDANT STATION EMERGENCY LIGHT SWITCH INOP. REMOVED AND REPLACED SWITCH PER MM. 2 L 7 2 4F RT A16WE 2007092700292 20070927 00292 NM 2007 9 27 SWAA074652 1 20070918 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 760SW 27874 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 10 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007092700293 20070927 00293 NM 2007 9 27 SWAA074656 1 20070918 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED HC1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 2 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007092700294 20070927 00294 NM 2007 9 27 SWAA074653 1 20070918 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 202WN 33999 EEPLS COVER MISSING AT 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007092700297 20070927 00297 NM 2007 9 27 QXEA200701449 1 20070923 A 3620 8209076 SHUTOFF VALVE BOMBDR DHC8 DHC8402 1390042 NM BLEED AIR SYS FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 400QX 299 299 4030 SEA FLIGHT NR 2320: NR 2 BLEED HOT CAUTION LIGHT ILLUMINATED AT 12,000 FT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE REM OVED AND REPLACED NR 2 HP SHUTOFF VALVE IAW Q400 AMM 36-11-09, PG 401-406. GROUND RAN NR 2 ENGINE WITH NR 2 BLEED ON AN D NR 2 BLEED HOT CAUTION DID NOT REOCCUR. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007092700299 20070927 00299 NM 2007 9 27 QXEA200701450 1 20070921 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM MAIN PAX DIRTY A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 424QX 4006 SEA FLIGHT: FA REPORTS AFT PASSENGER DOOR HARD TO OPEN AND CLOSE. MAINTENANCE CLEANED AND LUBRICATED AFT PAX DOOR. OPS CHECK GOOD. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007092700300 20070927 00300 2007 9 27 SWAA074682 4 20070918 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 495WN 33869 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007092700301 20070927 00301 NM 2007 9 27 SWAA074646 1 20070918 A 3350 61047895 BATTERY PACK BOEING 737 7373H4 1384600 NM L1 DOOR DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007092700302 20070927 00302 NM 2007 9 27 SWAA074674 1 20070918 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518D, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007092700305 20070927 00305 NM 2007 9 27 SWAA074675 1 20070918 A 5330 6545778 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 930 AND BS 952, STR 23R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007092700306 20070927 00306 NM 2007 9 27 QXEA200701451 1 20070919 A 3220 CONTROL LATCH BOMBDR DHC8 DHC8402 1390042 NM NLG GROUND LOCK INOPERATIVE A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 424QX 4006 SEA FLIGHT: RAMP TOW TEAM ADVISES THAT NLG GROUND LOCK MECHANISM WILL NOT LOCK. MAINTENANCE REMOVED AND REPLACED NLG GR OUND LOCK CONTROL LATCH ASSEMBLY. NO ADJUSTMENTS TO GROUND LOCK MECHANISM MADE. PERFORMED OPERATIONAL TEST OF NLG GROU ND LOCK POSITION INDICATION SYSTEM IAW Q400 AMM TASK 32-25-06-710-801. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007092700307 20070927 00307 NM 2007 9 27 SWAA074679 1 20070916 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED C2 CHECK, FOUND L2 FUSELAGE SKIN CRACKED AT LOWER HINGE CUTOUT LOWER END. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007092700308 20070927 00308 NM 2007 9 27 SWAA074678 1 20070916 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED C2 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED OUTBOARD END. REMOVED AND REPLACED FLAP PE R MM. 2 L 7 2 4F RT A16WE 2007092700310 20070927 00310 NM 2007 9 27 SWAA074661 1 20070918 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092700311 20070927 00311 NM 2007 9 27 SWAA074673 1 20070918 A 5311 6546538 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092700314 20070927 00314 NM 2007 9 27 QXEA200701456 1 20070918 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - NUMBER 4 SEAT TRACK FLANGE CORRODED AT MAIN CABIN DOOR ENTRY. REPAIRED IAW RD8-53-4473 AND RD8-53-1102. 2 H 7 2 4T RT A13NM 2007092700317 20070927 00317 NM 2007 9 27 SWAA074670 1 20070918 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092700321 20070927 00321 NM 2007 9 27 SWAA074664 1 20070918 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092700323 20070927 00323 NM 2007 9 27 SWAA074669 1 20070918 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007092700324 20070927 00324 NM 2007 9 27 QXEA200701463 1 20070917 A 5551 MOUNT DHAV DHC8 DHC8202 2809007 NM HORIZONTAL STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - HORIZONTAL STAB FORWARD RIGHT MOUNTING STRUCTURE HAS NICKS AND GOUGES ON OUTBOARD SIDE. REPAIRED IAW RD8-55-84 7, SRM 51-20-51, 51-20-16. 2 H 7 2 4T RT A13NM 2007092700325 20070927 00325 NM 2007 9 27 SWAA074668 1 20070918 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092700328 20070927 00328 NM 2007 9 27 SWAA074666 1 20070918 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092700329 20070927 00329 NM 2007 9 27 SWAA074648 1 20070918 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 FUSELAGE SKIN CRACKED AT BS 518, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007092700330 20070927 00330 NM 2007 9 27 SWAA074681 1 20070918 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 490WN 32476 DURING SCHEDULED MV2 CHECK, FOUND RT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB P ER MM. 2 L 7 2 4F RT A16WE 2007092700331 20070927 00331 NM 2007 9 27 SWAA074672 1 20070918 A 5330 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 745D AND BS 730E, STR 24L AND STR 23L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007092700332 20070927 00332 2007 9 27 SWAA074659 4 20070918 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007092700333 20070927 00333 NM 2007 9 27 SWAA074660 1 20070918 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 793SA 27888 DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007092700334 20070927 00334 NM 2007 9 27 SWAA074651 1 20070918 A 3350 MS155721 LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007092700335 20070927 00335 NM 2007 9 27 SWAA074680 1 20070915 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2007092700336 20070927 00336 NM 2007 9 27 SWAA074658 1 20070918 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 7 DEF. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007092700337 20070927 00337 NM 2007 9 27 SWAA074650 1 20070918 A 3397 W4142011220 WIRE BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 460WN 32464 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LIGHT INOP AT ROW 3 ABC. REPAIRED BROKEN WIRE PER MM. 2 L 7 2 4F RT A16WE 2007092700338 20070927 00338 NM 2007 9 27 KCSA071385 1 20070919 A 5330 SKIN BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 SKIN HAS CORROSION AT STA 1000 BETWEEN STR 44R AND STR 45R. 2 L 7 4 4F RT A20WE 2007092700343 20070927 00343 NM 2007 9 27 QXEA200701464 1 20070920 A 5280 ARM DHAV DHC8 DHC8202 2809007 NM MLG DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - RIGHT NACELLE CUTOUT FOR FORWARD MAIN LANDING GEAR DOOR AFT HINGE ARM HAS DENT AND GOUGE IN SUPPORT RIB, AFT SI DE OF OPENING. REPAIRED IAW SRM 51-20-11, 51-40-11. 2 H 7 2 4T RT A13NM 2007092700346 20070927 00346 NM 2007 9 27 QXEA200701470 1 20070920 A 5313 STRINGER DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - AT STRINGER 23L X492 THERE IS CORROSION AT A RIVET HEAD. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-20-26. 2 H 7 2 4T RT A13NM 2007092700347 20070927 00347 NM 2007 9 27 QXEA200701471 1 20070921 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - X487 STRINGER 23L THERE IS CORROSION FORWARD OF FRAME AT ATTACH CLIP. REPAIRED IAW SRM 51-20-11, 51-20-16, 51- 20-26. 2 H 7 2 4T RT A13NM 2007092700352 20070927 00352 NM 2007 9 27 QXEA200701469 1 20070920 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - AT STRINGER 23L X511 THERE IS CORROSION SHOWING AROUND A RIVET HEAD. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-2 0-26. 2 H 7 2 4T RT A13NM 2007092700353 20070927 00353 NM 2007 9 27 QXEA200701474 1 20070922 A 5320 WEB DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - MTX REQUEST - CORROSION ON WEB MATING SURFACE TO STRINGER 24L FROM STATION X487 TO X501. REPAIRED IAW SRM 51-2 0-11, 51-40-11. 2 H 7 2 4T RT A13NM 2007092700355 20070927 00355 NM 2007 9 27 QXEA200701481 1 20070916 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - SUSPECT CRACK IN FORWARD RIGHT CLOSING ANGLE RADIUS AT STATION X387, STRINGER 5 RIGHT UNDER PANEL 261JT. REPAI RED IAW RD8-53-5192. 2 H 7 2 4T RT A13NM 2007092700358 20070927 00358 NM 2007 9 27 QXEA200701477 1 20070923 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 445-435 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - RIGHT INBOARD SEAT TRACK HAS WEAR DAMAGE, BOTTOM OF TRACK FRAME STATION X445 - X435/Y9.2. REPAIRED IAW RD8-53- 1339. 2 H 7 2 4T RT A13NM 2007092700359 20070927 00359 NM 2007 9 27 QXEA200701478 1 20070923 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 445-435 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - LEFT INBOARD SEAT TRACK HAS WEAR DAMAGE, BOTTOM OF TRACK FRAME STATION X445 - X435/ Y9.2. REPAIRED IAW RD8-53- 1339. 2 H 7 2 4T RT A13NM 2007092700360 20070927 00360 NM 2007 9 27 QXEA200701479 1 20070916 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 473-484 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - LEFT INBOARD SEAT TRACK HAS WEAR DAMAGE, BOTTOM OF TRACK FRAME STATION X473 - X484/ Y9.2. REPAIRED IAW RD8-53- 1339. 2 H 7 2 4T RT A13NM 2007092700361 20070927 00361 EA 2007 9 27 QXEA200701447 1 20070923 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002C10 1390015 EA RT A/C PACK FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 603QX 10011 BOI- FLIGHT 2564. ON TAXI RECEIVED A RIGHT PACK CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENANCE CYCLED THE RAM AIR SWITCH. GROUND RAN THE NR 2 SYSTEM AND PERFORMED OPERATIONAL CHECK. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PA RTS REPLACED. 2 L 7 2 4F RT A21EA 2007092700362 20070927 00362 EA 2007 9 27 QXEA200701446 1 20070923 A 2780 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA SLATS MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 618QX 10205 PDX - FLIGHT 2585 - ON TAXI RECEIVED A SSCU NR 1 FAULT. RETURNED TO THE GATE. MAINTENANCE REVIEWED THE MDC AND FOUND A SSCU1 CHANNEL A COMMUNICATIONS FAULT. REINITALIZED SSCU AND PERFORMED SELF TEST. CHECKS GOOD. AIRCRAFT RETURNED TO SE RVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007092700363 20070927 00363 NM 2007 9 27 QXEA200701453 1 20070918 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 247-195 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - NUMBER 7 SEAT TRACK, TOP SURFACE CORRODED FROM STATION 242 THRU 195, GALLEY AND LAV ATTACH AREA. REPAIRED IAW SRM 51-40-11, RD8-53-1102 AND RD8-53-4473. 2 H 7 2 4T RT A13NM 2007092700366 20070927 00366 NM 2007 9 27 AALA20071796 1 20070905 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 973AN 29548 TUL - EMERGENCY LIGHTS IN MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092700367 20070927 00367 NM 2007 9 27 AALA20071797 1 20070905 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 973AN 29548 TUL - EMERGENCY LIGHTS IN MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092700368 20070927 00368 NM 2007 9 27 QXEA200701482 1 20070923 A 3210 DRAG STRUT DHAV DHC8 DHC8202 2809007 NM MLG CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - RIGHT DRAG STRUT INBOARD ATTACH POINT IS CHAFED. REPAIRED IAW SRM 51-20-26. 2 H 7 2 4T RT A13NM 2007092700369 20070927 00369 NM 2007 9 27 QXEA200701483 1 20070915 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - SUSPECT CRACK RIGHT AFT CLOSING ANGLE AT STINGER 6 RIGHT UNDER FLAP PCU. REPAIRED IAW RD8-53-5192. 2 H 7 2 4T RT A13NM 2007092700370 20070927 00370 EU 2007 9 27 07FDEA04101 1 20070920 A 5330 A53810543 DOUBLER AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT DOUBLER C54, P14, P15, P16, P25 (LT) AND P14, P15, P17, P25 (RT). REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092700373 20070927 00373 EU 2007 9 27 07FDEA04104 1 20070920 A 5313 A53973984222 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT STRINGER SEGMENT C 65, P43LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092700375 20070927 00375 EU 2007 9 27 07FDEA04106 1 20070920 A 5310 A53978255200 CROSSBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT CROSSBEAM C 63 OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092700379 20070927 00379 EU 2007 9 27 07FDEA04110 1 20070920 A 5330 A53985240204 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FOUND EXISTING REPAIR DOUBLER ON FUSELAGE SKIN AFT OF FRAME 78 BETWEEN STRG 1LH - 1RH, NOT CONFORM TO SRM. OLD REPAIR R EMOVED AND RENEWED IAW SRM 53-10-12/FIG 226. 2 L 7 2 4F RT A35EU 2007092700380 20070927 00380 EU 2007 9 27 07FDEA04111 1 20070920 A 5330 A53980666 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FOUND OLD SMALL FLUSH DOUBLER REPAIR BETWEEN FRAME 72-73, STRG 41-42 LHS, NOT CONFORM TO SRM. REPAIR PERFORMED BY INSTA LLING NEW EXTERNAL DOUBLER IAW SRM 53-10-12/FIG 227. 2 L 7 2 4F RT A35EU 2007092700381 20070927 00381 EU 2007 9 27 07FDEA04112 1 20070920 A 5311 A53811500200 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 OLD REPAIRS WITH NEW CORROSION AT FRAME 40 BETWEEN 51-52 LT, 54-55 LT, 54-55 RT AND 50-51 RT. REPAIR PERFORMED BY REMOV E EXISTING REPAIR ANGLES AND INSTALLING NEW FABRICATED ANGLES IAW EA 6-5315-82860 AND RAS 037936/008/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007092700382 20070927 00382 EU 2007 9 27 07FDEA04113 1 20070920 A 5315 A53873176212 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 HEAVY CORROSION ON CROSSBEAM FRAME 63 LT, CARGO COMP FLOOR STRUCTURE. CROSSBEAM SPLICE REPAIR PERFORMED IAW SRM 53-10-1 5/FIG 207. 2 L 7 2 4F RT A35EU 2007092700383 20070927 00383 EU 2007 9 27 07FDEA04114 1 20070920 A 5220 A52271025200 DOOR FRAME AIRBUS 310 A310203 3930313 EU ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION AT EMERGENCY EXIT DOOR FRAME SEGMENT 2.1. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092700384 20070927 00384 EU 2007 9 27 07FDEA04115 1 20070920 A 5541 A55471560202 RIB AIRBUS 310 A310324 3930206 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FOUND CORRODED RIB 54 ON RUDDER. REPLACEMENT OF RIB 54 IAW SRM 55-41-19. 2 L 7 2 4F RT A35EU 2007092700387 20070927 00387 NM 2007 9 27 BB07074 1 20070917 A 2120 DIFFUSER BOEING 757 7572B7 1384964 NM COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 201UU 27810 FLIGHT 731, LGW-PHL: DURING FLIGHT, THE CAPTAIN REPORTED DIFFICULTY HEARING RADIO TRANSMISSIONS DUE TO EXCESSIVE AIR NO ISE IN THE COCKPIT. DIVERTED TO SNN. MAINTENANCE PLACED THE LEFT PACK ON MEL. SUBSEQUENT TROUBLESHOOTING DETERMINED T HAT THE F/O'S WINDSHIELD AIR DIFFUSER WAS CRACKED AND A LOUD HUM WOULD DEVELOPE WITH THE PACK ON. REPAIRED DIFFUSER. N O FURTHER FAULTS. 2 L 7 2 4F RT A2NM 2007092700388 20070927 00388 EA 2007 9 27 COMA0770050 1 20070919 A 5320 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 378CA 10097 FS 280 CROSSBEAM CORRODED BEYOND LIMITS. REPLACED THE FS 280 CROSSBEAM IAW REO 670-53-11-046. 2 L 7 2 4F RT A21EA 2007092700389 20070927 00389 EU 2007 9 27 07FDEA04137 1 20070920 A 5720 A57111092 PANEL AIRBUS 300 A300B4622 3930401 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 CRACK FINDING DURING INSPECTION IAW SB 57-6086 HOLE NR F -1MM IN BOTTOM PANEL AND HOLE NR G-8MM IN FWD FITTING. REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL CRACK REMOVAL IAW EA 6-5710-73898 AND RAS/AS/310/2003 ISS A. 2 L 7 2 4F RT A35EU 2007092700034 20070927 00034 NM 2007 9 27 DU4R2007165 1 20070924 A 5320 146N852264 SUPPORT BOEING 757 757232 1384965 NM BS 1400-1420 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 6711M 30483 FOUND CORROSION ON THRESHOLD SUPPORT STRUCTURE OF AFT CARGO DOOR AT BS 1400 - 1420, RBL 27. REPAIRED BY REMOVING AND RE PLACING LOWER CHORD P/N 146N8522-64 IAW B757 SRM 51-40-02, 51-40-05, 51-20-01 AND BOEING DWG 146N3305. 2 L 7 2 4F RT A2NM 2007092700041 20070927 00041 WP 2007 9 27 UPS07850658 1 20070813 A 5753 5614374505 FITTING DOUG DC8 DC873F 302199F WP T/E FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 LEFT FLAP STA 219 I/B CANOE FITTING GOUGED. REPAIRED LEFT FLAP CANOE FITTING STA 219 I/B CANOE FITTI NG IAW EA 008- 2750-01-A1064. 2 L 7 4 4F RT 4A25 2007092700073 20070927 00073 NM 2007 9 27 SWAA074635 1 20070915 A 5315 149A5510 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 735SA 27867 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 47. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007092700075 20070927 00075 NM 2007 9 27 UIEA200700345 1 20070905 A 5310 DOOR FRAME BOEING 747 7472D7B 1384803 NM BS 1670 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 M/D R4 MED FWD UPPER CORNER FRAME CRACKED AT STA 1670 S-16R TO S-17R AREA. CARRY OUT REPAIR AS PER SRM 52-10-02, FIG 10 . 2 L 7 4 4F RT A20WE 2007092700092 20070927 00092 NM 2007 9 27 SWAA074632 1 20070915 A 5330 6545776 SKIN BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 967, STR 27L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007092700111 20070927 00111 NM 2007 9 27 DHL2007746536 1 20070821 A 5320 INTERCOSTAL BOEING 727 727224 1384076 NM BS 950F-970 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 AFT CARGO COMPT BS 950F-970 INTERCOSTAL AT STRINGER 28 LT IS CORRODED. REMOVED INTERCOSTAL IAW B-727, SRM 51-30-2. FAB RICATED NEW INTERCOSTAL, MAT USED 7075 T6, 0.040, PO NR 9005634, DIMENSION 20" BY 7 1/2 IAW B-727, SRM, 53-10-2, FIG-5 A ND 51-10-3, AND 51-30-5. TREATED AND PRIMED AREA IAW B-727 SRM 51-10-2. INSTALLED NEW INTERCOSTAL AT BS 950 F TO 970 I AW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007092700116 20070927 00116 NM 2007 9 27 UIEA200700357 1 20070823 A 5753 FLAP TRACK BOEING 747 7472D7B 1384803 NM TE FLAPS CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 527MC 22471 NR 1 MOVABLE FLAP TRACK FAIRING HAS SMALL CRACK LOWER SURFACE. REPAIRED PER SRM 51-40-09 AND 51-40-12. 2 L 7 4 4F RT A20WE 2007092700118 20070927 00118 NM 2007 9 27 USAA920070832 1 20070912 A 5320 6517684 WEB BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 23700 CLT - MAJOR REPAIR - NR 6007491, CRACKED WEB, BS 294.5, S7L. REPLACED WEB, BS 294.5, S7L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007092700119 20070927 00119 NM 2007 9 27 UIEA200700358 1 20070825 A 3830 DRAIN VALVE BOEING 747 7472D7B 1384803 NM TOILET CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 527MC 22471 DURING SCHEDULED TIME REMOVAL OF THE TOILET SERVICE DRAIN VALVE FOUND HEAVY CORROSION ON THE BRACKET ABOVE THE PAN AND S ERVICE DOOR INSTALLATION. REMOVED ALL BRACKET THAT HAD CORROSION DAMAGE. REPAIRED INTERNAL STRAPS PER SRM 53-30-03. R EPAIRED INTERNAL SECTION USING FLAT PATTERN METHOD WITH SRM 51-20-01. 2 L 7 4 4F RT A20WE 2007092700121 20070927 00121 WP 2007 9 27 ASAA0782026 1 20070914 A 5313 LONGERON SPLICE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 LONGERON REPAIR SPLICE CORRODED. REMOVED EXISTING REPAIR SPLICE AND INSTALLED REPLACEMENT SPLICE PER SRM 53-02. 2 L 7 2 4F RT A6WE 2007092700123 20070927 00123 GL 2007 9 27 UIEA200700362 2 20070911 A 7250 1538M90P12 TURBINE BLADES GE BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL HPT ROTOR CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 450PA 28578 28578 53X06199 30808 706199 ESN 706199 - HPT STAGE 1 BLADES FOUND WITH UNDER PLATEFORM CORROSION AND CRACKS, STAGE 1 P/N 1538M90P12 (80EA). 2 L 7 4 4F 4 F RT A20WE E23EA 2007092700129 20070927 00129 EU 2007 9 27 AWXA200701126 1 20070921 A 5320 D53480043202 SILL AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 SAL - MAJOR REPAIR - C-04 CHECK - NR 5976234, CORROSION FOUND ON L2 DOOR SILL, BS 3158/FR 66 TO BS 3257/FR 68, S23L. R EPAIRED L2 DOOR SILL, BS 3158/FR 66 TO BS 3257/FR 68, S23L IAW A320 SRM 53-41-14. 2 L 7 2 4F RT A28NM 2007092700136 20070927 00136 NM 2007 9 27 DHL2007746535 1 20070821 A 5322 SHEAR TIE BOEING 727 727224 1384076 NM BS 950A CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 AFT CARGO COMPT BS, 950 A O/B AT STR 29 RT, LOWER FRAME HAS EXFOLIATING CORROSION. REMOVED SHEAR TIE AT AFT CARGO COMPT IAW B-727 SRM 51-30-2. FABRICATED SHEAR TIE, MAT USED BAC 1505-29222, 7075-T6, PO NR 9004670, DIMENSION 7", IAW.B-727. SRM 53-10-2, FIG-5 AND 51-30-5. TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED NEW SHEAR TIE AT BS 950A, STR 29R , IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007092700140 20070927 00140 WP 2007 9 27 ASAA0782031 1 20070914 A 5347 5936665501 CARGO TRACK DOUG DC9 DC983 3022083 WP CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 972AS 53448 CARGO TRACK CORRODED. REPLACED TRACK PER SRM 51-30-02 AND 51-30-01. 2 L 7 2 4F RT A6WE 2007092700141 20070927 00141 SO 2007 9 27 SWIA200718691 1 20070815 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 581SW 120349 RIGHT WING LOWER STRINGER NR 10 IS CRACKED BETWEEN RIBS 7R AND 9R, DISCOVERED AT C-CHECK. REPAIRED RIGHT WING LOWER STR INGER PER SRM 57-20-03. 2 L 7 2 4T RT A31SO 2007092700144 20070927 00144 EA 2007 9 27 SWIA200718693 1 20070917 A 5240 BEARING CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 973SW 7949 FLT 6691 - SERVICE DOOR IS DIFFICULT TO OPEN FROM THE OUTSIDE. REPLACED CAM BEARING PER AMM 52-41-03. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007092700159 20070927 00159 SO 2007 9 27 C2XA07CL079 1 20070917 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO CABIN FAULTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11113 145662 DURING ROUTINE MAINTENANCE THE AFT OVERHEAD EXIT SIGN WAS ONLY PARTIALLY ON. MAINTENANCE INSPECTED AND REPLACED THE NR 6 INVERTER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2007092700160 20070927 00160 EA 2007 9 27 SWIA200718694 1 20070917 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 963SW 7865 FLT 6526 - CENTER PLY OF FIRST OFFICERS WINDSHIELD SHATTERED. REPLACED THE WINDSHIELD IAW AMM 36-11-01, P/N OFF 601R330 33-18, S/N OFF 03164H6305. 2 L 7 2 4F RT A21EA 2007092700165 20070927 00165 EA 2007 9 27 SWIA200718699 1 20070726 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA PAX DOORWAY CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 479CA 7675 PAX DOOR LOWER SILL IS CORRODED, DISCOVERED AT C-CHECK. INSTALLED NEW PAX DOOR LOWER SILL PER CRJ200 SRM 51-42-06 PG 11 , 51-42-21 PG 17, 51-41-02 PG 5. 2 L 7 2 4F RT A21EA 2007092700166 20070927 00166 NM 2007 9 27 ASAA0742054 1 20070916 A 3350 2073771008 LENS BOEING 737 7374Q8 138447Q NM CABIN CRACKED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 784AS 28199 EXIT INDICATOR AT EMERGENCY EXIT DOOR ROW 13 LEFT LENS FELL OFF. FOUND LENS CRACKED DUE OVER TORQUED. REPLACED LENS. 2 L 7 2 4F RT A16WE 2007092700173 20070927 00173 NM 2007 9 27 AALA20071773 1 20070919 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 963AN 29543 DFW - EMERGENCY LIGHT AT SEAT 7D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092700175 20070927 00175 NM 2007 9 27 AALA20071783 1 20070923 A 3350 SHROUD BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 920AN 29521 DFW - EMERGENCY LIGHT AT SEAT 7D AFT SHROUD BROKEN. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 7D AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007092700183 20070927 00183 NM 2007 9 27 KCSA071380 1 20070918 A 5313 STRINGER BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 STR 38L CRACKED BETWEEN BS 480 AND 500. 2 L 7 4 4F RT A20WE 2007092700193 20070927 00193 NM 2007 9 27 UIEA200700352 1 20070905 A 5753 WEB BOEING 747 7472D7B 1384803 NM CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 OLEO 1450 FWD CRACKED JUST FWD OF NR 25 V/C FLAP UPPER FITTING. CARRY OUT REPAIR AS PER SRM 51-40-03. 2 L 7 4 4F RT A20WE 2007092700197 20070927 00197 SO 2007 9 27 SIMA200726402 1 20070919 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO SERVICE DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 658AE 9840 5000 145760 DURING MBV INSPECTION, THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. REPLACED SILL WITH NEW SILL IAW EMB 145 SRM 51-2 0-01, 51-20-03, 51-40-02, 51-40-06 AND CPM 51-21-04, 51-21-05, AND 51-21-06. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007092700198 20070927 00198 SO 2007 9 27 SIMA200726403 1 20070919 A 5310 14525480603 BEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 658AE 9840 5000 145760 DURING A MBV INSPECTION, THE BAGGAGE DOOR CUT OUT LOWER CENTER BEAM WAS FOUND CORRODED. REPLACED BEAM WITH NEW BEAM PN 145-25480-006 IAW EMB SRM CHAPTERS 51-40--02, 51-20-03, AND 51-40-06. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007092700220 20070927 00220 WP 2007 9 27 ABXA070296 1 20070915 A 2170 1808491 COALESCER BAG DOUG DC9 DC941 302207N WP A/C BAY DEFECTIVE A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 23 969AX 47464 AT V1, STRONG ODOR NOTICED THROUGH A/C DUCTS, STARTED TO DISSIPATE OUT OF 2500 FEET. REPLACED LT & RT PACK WATER SEPARA TOR COALESCER BAGS IAW DC9 MM. 2 L 7 2 4F A6WE 2007092700225 20070927 00225 NM 2007 9 27 DL76G071244 1 20070922 A 3610 2780539104 ISOLATION VALVE BOEING 767 767332 1382001 NM BLEED AIR SYS OPEN A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 1607B 30388 AIRCRAFT 1607 ON FLT 130/22 RTB DUE TO THE RT ISOLATION VALVE STUCK OPEN. REPLACED VALVE CKS OK. 2 L 7 2 4F RT A1NM 2007092700227 20070927 00227 NM 2007 9 27 DLM88071245 1 20070923 A 2910 B-NUT DOUG MD88 MD88 3023688 NM HYD SYSTEM LEAKING A DALA D RETURN TO BLOCK K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 989DL 53341 AFTER LANDING AND STARTING APU, PASSENGER AND FLIGHT ATTENDANT IN COACH COMPLAINED OF ACRID, ELEC TYPE ODOR IN MAIN CABI N, SHUTDOWN APU AND WITH EXT AIR AND POWER ODOR WENT AWAY. MTC IN PROGRESS. FOUND HYD LEAK IN TAIL COMPARTMENT, LEFT S YSTEM AND APU INLET CONTAMINATION. 2 L 7 2 4F RT A6WE 2007092700252 20070927 00252 EA 2007 9 27 COMA0760562 1 20070908 A 2620 M835366025M RELAY CNDAIR CL600 CL6002B19 1900309 EA FIRE PROTECTION FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 963CA 7127 FLIGHT 5180 - RECEIVED CARGO BOTTLE LOW MESSAGE. PERFORMED QRH, SQUIBS DID NOT TEST. DIVERTED TO CRW, LANDED WITHOUT I NCIDENT. REPLACED RELAY K8HL. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007092700264 20070927 00264 NM 2007 9 27 UPS07550681 1 20070917 A 2560 ESCAPE ROPE BOEING 757 75724APF 1384969 NM COCKPIT OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 430UP 25461 INSPECTION TYPE:N/A ESCAPE ROPE NEEDS TO BE PACKED. REPACKED ESCAPE ROPES PER B757 AMM 25-61-00-4. 2 L 7 2 4F RT A2NM 2007092700279 20070927 00279 EA 2007 9 27 COMA0760570 1 20070913 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 659BR 7509 FLIGHT 5120 - RECEIVED FLAP CAUTION MESSAGE. LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C) FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2007092700280 20070927 00280 EA 2007 9 27 COMA0760571 1 20070915 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILER FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 920CA 11418 7022 FLIGHT 4982 - CONFIG SPOILERS WARNING ON TAKEOFF. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT WING INBOARD SPOILER PCU. 2 L 7 2 4F RT A21EA 2007092700284 20070927 00284 2007 9 27 AALA20071787 4 20070112 A 2565 100504205 SLIDE DOUG DC9 DC983 3022083 WP R1 DOOR PARTIAL INFLATE A AALA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 564AA 49346 SFO - RIGHT NUMBER ONE DOOR EMERGENCY SLIDE INADVERTENTLY UNSUCCESSFULLY DEPLOYED WHEN OPEN FROM OUTSIDE BY CATERING PER SONNEL. REPLACED RIGHT NUMBER ONE DOOR EMERGENCY SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007092700295 20070927 00295 NM 2007 9 27 SWAA074649 1 20070918 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 415WN 29836 EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007092700315 20070927 00315 NM 2007 9 27 SWAA074665 1 20070918 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092700341 20070927 00341 NM 2007 9 27 QXEA200701458 1 20070923 A 5397 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 597 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - CORROSION ON NR 9 SEAT TRACK AT STATION X597.5. REPAIRED IAW RD8-53-784. 2 H 7 2 4T RT A13NM 2007092700348 20070927 00348 NM 2007 9 27 QXEA200701472 1 20070921 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - X487 AND STRINGER 23L FORWARD OF FRAME AND UNDERSIDE THERE IS CORROSION IN 3 SPOTS. REPAIRED IAW SRM 51-20-11, 51-20-36. 2 H 7 2 4T RT A13NM 2007092700349 20070927 00349 NM 2007 9 27 QXEA200701473 1 20070920 A 5411 FRAME DHAV DHC8 DHC8202 2809007 NM NR 2 NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - NR 2 NACELLE, FRAME FITTING FOR FORWARD MAIN LANDING GEAR DOOR, AFT HINGE ARM SUPPORT RIB HAS ONE FASTENER HOLE BLOWN OUT. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2007092700354 20070927 00354 NM 2007 9 27 QXEA200701480 1 20070916 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - PITTING ON RIGHT INBOARD FLAP, LOWER SIDE OF UPPER NR 2 TRACK AT ZERO DEGREE ROLLER INDICATION. REPAIRED IAW R D8-57-986. 2 H 7 2 4T RT A13NM 2007092700356 20070927 00356 NM 2007 9 27 QXEA200701475 1 20070926 A 5414 SKIN DHAV DHC8 DHC8202 2809007 NM NR 1 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - ON NR 1 NACELLE SKIN AT THE FORWARD INBOARD CUTOUT RADIUS FOR THE FORWARD GEAR DOOR. THE NACELLE SKIN IS CRACK ED 1/4" LONG. REPAIRED IAW RD8-54-873. 2 H 7 2 4T RT A13NM 2007092700357 20070927 00357 NM 2007 9 27 QXEA200701476 1 20070923 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 507-516 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - RIGHT INBOARD SEAT TRACK HAS WEAR DAMAGE, BOTTOM OF TRACK FRAME STATION X507 - X516 Y9.2. REPAIRED IAW RD8-53- 1339. 2 H 7 2 4T RT A13NM 2007092700371 20070927 00371 EU 2007 9 27 07FDEA04102 1 20070920 A 5753 SKIN AIRBUS 310 A310324 3930206 EU ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CHAFING MARK ON INBOARD FLAP VANE LT, CAUSED BY NOT INSTALLED PROTECTIVE PLATE AT VANE-NOSE-SKIN FOR JAM RETRACTED MICRO SWITCH STRIKER, RIB 2-22. REPAIR PERFORMED BY SMOOTH BLEND OUT CHAFING MARK IAW EA 6-5752-82885 AND RAS/DABRE/7005373/2 005 ISSUE B AND INSTALLATION OF PROTECTION PLATE IAW SRM 57-52-12/201/PARA 4 C. 2 L 7 2 4F RT A35EU 2007092700374 20070927 00374 EU 2007 9 27 07FDEA04105 1 20070920 A 5330 A53610633233 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORROSION ON FWD DOOR FRAME PANEL, RT FWD PAX DOOR, BETWEEN FRAME 13-14C, STRG 9-14, SOME AREAS OUT OF LIMIT. REPAIR PE RFORMED BY SMOOTH REWORK AND HFEC/ROTOTEST INSPECTION IAW EA 6-5312-82923 AND RAS 037817/008/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007092700394 20070927 00394 EU 2007 9 27 07FDEA04143 1 20070921 A 5320 A53981165 WEB AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 HEAVY CORROSION ON TWO SHEAR WEBS AT STRINGER 26 LT AND RT, BETWEEN FRAME 75A-76. REPLACEMENT OF BOTH SHEAR WEBS LT AND RT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007092700395 20070927 00395 SO 2007 9 27 C2XA07RI080 1 20070913 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 27 29906 145472 FLIGHT 2882 - BNA - CREW REPORTED SMOKE SMELL IN CABIN, BUT NO SIGN OF SMOKE DURING LANDING. BNA MX INSPECTED ACFT AND RAN THE ENGINES, NO SMELL OR SMOKE NOTED. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007092700396 20070927 00396 EU 2007 9 27 07FDEA04144 1 20070921 A 5311 A53981260205 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORROSION ON WEB AND INNER FLANGE OF FRAME 75A RT, AFT PAX DOOR BETWEEN STRG 26-27 RT. REPAIR PERFORMED BY SMOOTH BLEND OUT, HFEC INSPECTION AND FLAP PEENING IAW EA 6- 5318-82893 AND RAS/DAHAM/4019630/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007092700397 20070927 00397 NM 2007 9 27 07FDEA04145 1 20070921 A 5311 AFA00283 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 MAIN DECK CARGO COMPARTMENT, MAINFRAME STA 1681 AT LONGERON 12L FOUND WITH DENT. 10-04-07 REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG I VOL I, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OU T AS PER SRM 53-30-00 FIG I VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007092800001 20070928 00001 NM 2007 9 28 07FDEA04138 1 20070920 A 5297 WIRE BOEING 727 727225 1384077 NM UPLOCK SWITCH DAMAGED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 465FE 21289 AFT AIRSTAIR LIGHT ILLUMINATED AT ROTATION. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 30SEP07 " MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT, INOP. PLEASE WORK IN CONJUNCTION WITH TSI: 52-62 9704. REPAIRED WI RE AT SW S273 (UPLOCK SWITCH) AND REPLACED SW S395 (AIRSTAIR HANDLE DETENT SW). INSP CABLES, LATCHES AND CAMS. ALL CK GOOD PER MM 2-70-001-5. 2 L 7 3 4F A3WE 2007092800002 20070928 00002 NM 2007 9 28 SWAA074749 1 20070923 A 5753 69466493 TORQUE TUBE BOEING 737 7373H4 1384600 NM LT WING TE FLAP WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED A1 CHECK, FOUND LEFT WING NR 4 T/E FLAP DRIVE TORQUE TUBE WORN. REMOVED AND REPLACED TORQUE TUBE PER M M. 2 L 7 2 4F RT A16WE 2007092800004 20070928 00004 2007 9 28 SWAA074752 4 20070921 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007092800005 20070928 00005 2007 9 28 SWAA074756 4 20070923 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007092800008 20070928 00008 NM 2007 9 28 SWAA074800 1 20070925 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 472WN 33831 DURING SCHEDULED HC1 CHECK, FOUND EEPLS LENS CRACKED AT ROW 2 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007092800010 20070928 00010 NM 2007 9 28 SWAA074801 1 20070925 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 472WN 33831 DURING SCHEDULED HC1 CHECK, FOUND EEPLS LENS CRACKED AT ROW 3 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007092800011 20070928 00011 2007 9 28 SWAA074796 4 20070925 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007092800013 20070928 00013 NM 2007 9 28 SWAA074809 1 20070925 A 5310 6547980 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 867-887 S17L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 867 AND BS 887, STR 17L. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007092800014 20070928 00014 NM 2007 9 28 SWAA074808 1 20070925 A 5551 6551524 FITTING BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND RT AND LT HORIZONTAL STABILIZER FITTING CLEVIS LUG FACES CORRODED. REPAIRED FITTING P ER BOEING SB. 2 L 7 2 4F RT A16WE 2007092800019 20070928 00019 SO 2007 9 28 C2XA07RI082 1 20070914 A 3320 7287500507 LIGHT EMB 145 EMB145LR 3260212 SO CABIN DEFECTIVE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13990 145277 FLT 2754 - YOW - CREW REPORTED ELECTRICAL ODOR FROM SEAT 1A AREA. MX FOUND FLUORESCENT LIGHT ARCING AT CONTACT. MX REM OVED AND REPLACED LIGHT ASSEMBLY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007092800020 20070928 00020 NM 2007 9 28 SWAA074750 1 20070923 A 5753 69466493 TORQUE TUBE BOEING 737 7373H4 1384600 NM RT WING TE FLAP WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED A1 CHECK, FOUND RIGHT WING NR 5 T/E FLAP DRIVE TORQUE TUBE WORN. REMOVED AND REPLACED TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007092800021 20070928 00021 NM 2007 9 28 SWAA074778 1 20070924 A 3350 10107415 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 715SW 27849 DURING SCHEDULED HC2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007092800022 20070928 00022 NM 2007 9 28 SWAA074781 1 20070924 A 3350 10107451 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 771SA 27879 FWD CABIN EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007092800023 20070928 00023 NM 2007 9 28 SWAA074771 1 20070924 A 3350 101114 COVER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 FWD CABIN EMERGENCY EXIT SIGN COVER LOOSE. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007092800025 20070928 00025 NM 2007 9 28 SWAA074790 1 20070924 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 217JC 34232 EEPLS LENS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007092800027 20070928 00027 2007 9 28 SWAA074780 4 20070924 A 2565 63551101 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 757LV 29850 L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007092800028 20070928 00028 NM 2007 9 28 SWAA074775 1 20070924 A 5312 6516300 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, LBL 4.75. REPAIRED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2007092800029 20070928 00029 NM 2007 9 28 SWAA074776 1 20070924 A 5310 6516382 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 2 DOOR STOP. REMOVED AND REPLACED FRAME PER ACO. 2 L 7 2 4F RT A16WE 2007092800030 20070928 00030 NM 2007 9 28 SWAA074787 1 20070924 A 5330 6545776 BEAR STRAP BOEING 737 737317 138447P NM BS 957 S25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT BS 957, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007092800032 20070928 00032 NM 2007 9 28 SWAA074772 1 20070924 A 5753 6546435278 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV1 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED AF T FLAP PER MM. 2 L 7 2 4F RT A16WE 2007092800033 20070928 00033 NM 2007 9 28 SWAA074791 1 20070924 A 5311 6546531 FRAME BOEING 737 7375H4 138449D NM BS 482 S20L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 20L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092800035 20070928 00035 NM 2007 9 28 2007UALA03733 1 20070914 A 3350 LAMP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 228UA 30556 DOOR 3R EXTERIOR EMERGENCY LIGHT FAILED TO ILLUMINATE DURING TEST. 10-9-07 REPLACED LAMP. EMERGENCY LIGHT OP CHECKE D OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007092800036 20070928 00036 NM 2007 9 28 2007UALA03744 1 20070916 A 3510 OXYGEN MASK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CAPTAIN'S NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 CAPT O2 MASK TEST NOT CORRECT. EMERGENCY P-TO TEST BUTTON STICKS OPEN. 10-19-07 REPLACED CAPTAIN'S MASK ASSY, OP ERATIONAL TEST OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092800037 20070928 00037 NM 2007 9 28 2007UALA03745 1 20070915 A 5610 WINDOW BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT FAILED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 925UA 26646 CAPT SLIDING WINDOW 2L OUTER PANE SHATTERED AT FL320 NO ARCING NOTICED. REPLACED WINDOW. ROOT CAUSE IS UNKNOWN. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092800041 20070928 00041 NM 2007 9 28 2007UALA03736 1 20070916 A 5200 DOOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OVERWING SLIDE OPEN A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 503UA 24624 BOTH LEFT & RIGHT OVERWING SLIDE SERVICE ACCESS DOORS PROTRUDING INTO AIRSTREAM. RIGHT SIDE HINGE IS CRACKED, LEFT SIDE HAS BROKEN SPRINGS. 10-9-07 INTERIM REPAIR MADE, RECHECKED DAILY AT FIRST MAINTENANCE. REPLACED BOTH OF THE ACCESS DOOR HINGE ASSEMBLIES. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092800044 20070928 00044 EU 2007 9 28 2007UALA03739 1 20070917 A 3040 ANTI-ICE SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT WINDOW ARCED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 435UA 613 WINDOW 1L HAS REPORTED ARCING AND DAMAGE. WINDOW HEAT INOP. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092800045 20070928 00045 EU 2007 9 28 2007UALA03740 1 20070917 A 3510 CYLINDER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW OXYGEN READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 423UA 504 CREW O2 CYLINDER NEEDS SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092800046 20070928 00046 EU 2007 9 28 2007UALA03741 1 20070914 A 3510 OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE 2ND OBSERVER'S LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 433UA 589 THE 2ND OB'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). 2 L 7 2 4F 4 F RT A28NM E40NE 2007092800050 20070928 00050 NM 2007 9 28 F3LA200700239 1 20070913 A 5755 LUG AIRBUS A319 A319111 3930336 NM NR 3 SPOILER GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 921FR 5402 2010 DURING C-3 CHECK, INSPECTION REPORTED THE ANTI-ROTATION LUG ON THE LEFT NR 3 SPOILER ACTUATOR ATTACH POINT GOUGED. FABR ICATED AND INSTALLED REINFORCING PLATE FOR LEFT NR 3 SPOILER CENTER HINGE FITTING IAW EA A9-57R-12137, REV A. 2 L 7 2 4F RT A28NM 2007092800052 20070928 00052 NM 2007 9 28 2007UALA03750 1 20070917 A 5754 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 6 SLAT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 RIGHT WING NR 6 SLAT LOWER LEADING EDGE SKIN CRACKED AT 2EA FASTENERS LOCATED AT INBOARD AUXILLARY TRACK. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED LOWER SKIN EXTERNAL DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092800056 20070928 00056 NM 2007 9 28 2007UALA03754 1 20070918 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY CEILING LIGHT ABOVE ROW 13 INOP. 10-19-07 RELAMPED. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092800058 20070928 00058 NM 2007 9 28 2007UALA03756 1 20070918 A 2560 CONTROL PANEL BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EVAC HORN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 198UA 28716 UPPER DECK RT EXIT, EVACUATION SIGNAL SOUND IS CONTINUOUS. 10-19-07 REPLACED EVAC SIGNAL PANEL. OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092800059 20070928 00059 NM 2007 9 28 2007UALA03757 1 20070918 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 DOOR 5L EMERGENCY EVACUATION LIGHT INOP. 10-19-07 RELAMPED EEL, OP CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092800062 20070928 00062 SO 2007 9 28 C2XA07CL081 1 20070920 A 3260 355022002 CONTROL UNIT EMB 145 EMB145XR 3260214 SO COCKPIT FAULTY A C2XA O OTHER N FALSE WARNING CL CLIMB 1 SW 27 25134 25113 12728 145714 CLE FLIGHT 2178 - THE CREW REPORTED A CLICKING NOISE FROM THE NOSE WHEN THE GEAR WAS RETRACTED AND THE MAIN GEAR CYCLED BETWEEN INTRANSIT AND LOCKED FOR ABOUT 15 SECONDS THEN LOCKED. GEAR EXTENSION NORMAL. MAINTENANCE INSPECTED AND REPLAC ED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2007092800063 20070928 00063 NM 2007 9 28 SWAA074770 1 20070923 A 3350 101074 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 409WN 27896 R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007092800064 20070928 00064 NM 2007 9 28 SWAA074744 1 20070923 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 FWD CABIN EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2007092800065 20070928 00065 NM 2007 9 28 SWAA074747 1 20070921 A 3350 311500 LENS BOEING 737 7373K2 13844BA NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 10 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007092800066 20070928 00066 NM 2007 9 28 SWAA074753 1 20070921 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 459WN 32497 EEPLS LENS LOOSE AT ROW 10 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007092800067 20070928 00067 NM 2007 9 28 SWAA074741 1 20070921 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 226WN 32494 DURING SCHEDULED MV3 CHECK, FOUND EEPLS LENS MISSING AT ROW 5 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007092800068 20070928 00068 NM 2007 9 28 SWAA074742 1 20070921 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 256WN 32514 DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS LOOSE AT ROW 13 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007092800069 20070928 00069 NM 2007 9 28 SWAA074758 1 20070921 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 729SW 27861 EEPLS LENS MISSING AT ROW 8 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007092800072 20070928 00072 NM 2007 9 28 SWAA074745 1 20070921 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 474 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 474, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007092800073 20070928 00073 NM 2007 9 28 SWAA074755 1 20070923 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM BS 934 S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007092800074 20070928 00074 NM 2007 9 28 SWAA074757 1 20070923 A 5330 6545776 SKIN BOEING 737 737317 138447P NM BS 986 S27LR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 986, STR 27L AND STR 27R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007092800077 20070928 00077 NM 2007 9 28 UPS07M50693 1 20070717 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORZ STAB CONSTANT SECTION BARREL NUT BORE RIGHT NR 15 FOUND WITH CORROSION. CORROSION REMOVED PER SR M 51-21-01 VII R38. BORE BOTTOM SURFACE REMN BLEND OUT 0.065" DEEP. BORE REAMED TO 1.067 INCH DIA, REMN BLEND OUT 0.05 0 INCH DEEP, FOUND EXCEED LIMITS PER EO-MD11-5510-19409-L. 10X MAGNIFICATION INSP C/O, FOUND NO CORROSION. REPAIR SLEEV E BUSHING FAB & PROTECTED. SEALANT APPLIED & SLEEVE BUSHING INSTALLED. REPAIR C/O AT BARREL NUT BORE 15 IS ACCEPTABLE. 2 L 7 3 4F RT A22WE 2007092800078 20070928 00078 NM 2007 9 28 UPS07M50694 1 20070726 A 5230 SKIN DOUG MD11 MD11F 3023600 NM AFT CARGO DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C AFT CARGO DOOR CUTOUT LWR AFT EDGE FOUND PREVIOUS BLEND OUT AS MARKED. AFT CARGO DOOR CUTOUT LWR AFT EXT SKIN PREVIOUS BLEND OUT AREA FASTENERS REMOVED. PREVIOUS BLEND OUT EXT SKIN & INNER DOUBLER TRIMMED OUT HFEC INSP C /OUT ON REWORKED AREA FOUND NO CRACK. REPAIR DOUBLERS 2 EA & FILLERS 2EA FAB, REPROTECTED, PAINTED & INSTALLED. REPAIR DOUBLER RS 2EA & FILLERS 2EA INSTALLED AT AFT CARGO DOOR CUTOUT LWR AFT. 2 L 7 3 4F RT A22WE 2007092800079 20070928 00079 NM 2007 9 28 UPS07M50695 1 20070808 A 5730 DOUBLER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C RIGHT WING L/E COMPARTMENT AT STA XORS 538 APPROX FOUND UPPER DOUBLER CRACKED AS MARKED. FRAMES REMOV ED FOR ACCESS. CRACKED AREA TRIMMED OFF. HFEC INSP C/O ON TRIMMED OFF FOUND NO CRACK. REPAIR ANGLES FABRICATED, HEAT TREATED & HARDNESS VALUES HRB84.2 PER DPS 1.05-3. REPAIR FILLER & DOUBLER FABRICTAED, REPROTECTED, PRIMER TOUCH UP & INS TALLED. 2 L 7 3 4F RT A22WE 2007092800080 20070928 00080 NM 2007 9 28 UPS07M50696 1 20070808 A 5730 DOUBLER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C RIGHT WING L/E COMPARTMENT AT STA XORS 710 APPROX FOUND UPPER DOUBLER CRACKED AS MARKED. RIBS REMOVED FOR ACCESS. CRACKED AREA TRIMMED OFF. HFEC INSP C/OUT ON TRIMMED OFF AREA FOUND NO CRACK. REPAIR ANGLES FABRICATED, HEAT TREATED & HARDNESS VALUES HRB 84.3 PER DPS 1.05-3. REPAIR FILLER & DOUBLER FABRICATED, REPROTECTED, PRIMER TOUCHED UP & INSTALLED. 2 L 7 3 4F RT A22WE 2007092800082 20070928 00082 NM 2007 9 28 SB07080 1 20070921 A 3350 20121 POWER SUPPLY BOEING 737 7374B7 1384702 NM EMERGENCY LIGHTS INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 453UW 24980 CLT - MAINTENANCE REPORTED THE AFT LEFT GALLEY EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGE R ASSEMBLY AND BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007092800083 20070928 00083 NM 2007 9 28 ASAA072058 1 20070919 A 3220 NC243 BEARING BOEING 737 737890 1384527 NM NLG RETRACT ACT MIGRATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 35091 DURING DAILY CHECK, FOUND NLG RETRACT ACTUATOR ATTACH LUG BEARING MIGRATION LEFT OF CENTER OUT OF LIMITS REF EA 3230 010 55 STEP 1. BEARING MIGRATION MEASURES .155 LEFT OF CENTER. PREVIOUSLY ON DEFERRAL REF L P 6264563. BEARING MIGRATION CONDITION WAS REPAIRED REF L P 6351796. BEARING WAS REMOVED AND REPLACED RE-SWAGED. 2 L 7 2 4F RT A16WE 2007092800086 20070928 00086 NM 2007 9 28 UPS07550700 1 20070911 A 5311 70750080C FRAME BOEING 757 75724APF 1384969 NM BS 1340 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 434UP 25465 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1340, BETWEEN S25R AND S26R. REPAIR FRAME AT STA 1340, BETWEEN S 25R AND S26R ACCOMPLISHED PER SRM 53-00-07, DETAIL III PG 208. THIS IS A CATEGORY B-REPAIR AND REQUIRES REINSPECTION IA W TABLE II, PG 210 AND DETAIL V PG 212, FIG 201 (SHT 12OF15) ZONE NR 1. 2 L 7 2 4F RT A2NM 2007092800087 20070928 00087 EU 2007 9 28 MAC090701 1 20070901 A 5751 TEE FITTING AEROSP AEROSP ATR42 ATR42300 8680920 EU AILERON CORRODED A MTNA K NONE O OTHER IN INSP/MAINT 1 SO 33 923FX 135 DURING INSPECTION, LEVEL 3 CORROSION WAS FOUND ON 4 T-FITTINGS INSIDE THE LEFT WING AILERON. THE PROBABLE CAUSE IS DISS IMILAR MATERIALS (STEEL BOLTS IN ALUMINUM FITTINGS ATTACHED TO A COMPOSITE SPAR). THE FITTINGS WERE REPLACED AT RIBS 4, 11/12, AND 19. REFERENCE ATR SRM 57-61-10 PAGES 115 AND 116. THE TYPE OF CORROSION WAS EXFOLIATION. THE FITTING P/N ARE: S57610025200, S57610025204, AND S57610025202. 2 H 7 2 4T RT A53EU 2007092800088 20070928 00088 NM 2007 9 28 2007UALA03760 1 20070917 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 644UA 25094 LEFT FWD GALLEY AISLE EEL LIGHT INOPERATIVE. 10-9-07 REPLACED LAMP, OP CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092800089 20070928 00089 NM 2007 9 28 2007UALA03761 1 20070917 A 3350 SWITCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 644UA 25094 AFT ATTENDANT EMERGENCY LIGHT SWITCH LIGHT INOP. 10-9-07 EMERGENCY LIGHT SWITCH CONNECTED BACKWARDS. REWIRED SWITCH PER WDM 33-51-11, OP CHECK OK 2 L 7 2 4F 4 F RT A1NM E24NE 2007092800090 20070928 00090 NM 2007 9 28 2007UALA03762 1 20070917 A 3350 SWITCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 644UA 25094 EMERGENCY EXIT LIGHTS ON W- SWITCH IN ARMED POSITION. 10-19-07 REPLACED FLT DECK AND AFT FLT ATTEND. SWITCHES REF WD 33-51-11 PG.1D OPS CKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092800091 20070928 00091 NM 2007 9 28 2007UALA03763 1 20070917 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SEATS 5J & 24J INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 671UA 30026 SEAT 5J AND 24J EEL LIGHT INOPERATIVE. 10-19-07 REPLACED EEL LIGHTS . OP CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092800092 20070928 00092 NM 2007 9 28 2007UALA03764 1 20070917 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 308UA 23669 EXIT PATH LIGHTING EEL STRIPS INOP AT SEAT 1B & DOOR 2L INOP. REPLACED INVERTER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092800096 20070928 00096 NM 2007 9 28 2007UALA03768 1 20070918 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 989-994 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 CABIN FLOOR Z-ANGLE (CREASE BEAM) CORRODED AT BS 989-994, RBL 46, WL 208. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPLACE MENT FLOOR Z-ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092800097 20070928 00097 NM 2007 9 28 2007UALA03769 1 20070918 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE GALLEY G5 LT BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 GALLEY G5 LEFT WALL FWD END, EEL CABLE & PIN BROKEN. 10-16-07 RELAMPED & REPLACED EEL CABLES, OP CHECKED OK . SUS PECT IMPACT BY SERVING CART OR CUSTOMER CARRY-ON ITEM. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092800098 20070928 00098 NM 2007 9 28 2007UALA03770 1 20070918 A 5710 STRUCTURE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LT WING DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 198UA 28716 DENT FOUND MEASURING 5 INCHES ROUND INBOARD OF LEFT WING LANDING LIGHT. MAJOR REPAIR ACCOMPLISHED: INSTALLED FLUSH REP AIR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092800101 20070928 00101 NM 2007 9 28 ABXA070298 1 20070913 A 3397 A062011 WIRE BOEING 767 767281 1385109 NM EMERGENCY LIGHTS MISSING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 784AX 23017 COVER ON EMERGENCY EXIT LIGHT SWITCH MISSING WIRE. REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHT/CREW 02 SWITCH PANEL I AW B767 AMM 35-51-08-4. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2007092800103 20070928 00103 NM 2007 9 28 SWAA074712 1 20070919 A 5311 141A8353 FRAME BOEING 737 7377H4 1384404 NM BS 295 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 735SA 27867 DURING SCHEDULED 8Y CHECK, FOUND R1 DOOR CUTOUT FWD FRAME CRACKED AT BS 295, STR 15L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007092800104 20070928 00104 NM 2007 9 28 SWAA074700 1 20070919 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 986 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 735SA 27867 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 986, LBL 35. REPAIRED FLOORBEAM WEB PER MM. 2 L 7 2 4F RT A16WE 2007092800106 20070928 00106 NM 2007 9 28 SWAA074710 1 20070919 A 3350 1619 LAMP BOEING 737 7373Q8 1384670 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007092800109 20070928 00109 2007 9 28 KCSA071386 4 20070923 A 2565 TRACK BOEING 747 7472B4B 138481B NM ESCAPE SLIDE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 UPPER DECK ESCAPE SLIDE I/B TRACK CORRODED BETWEEN BS 400 AND 460, RBL-45. 2 L 7 4 4F RT A20WE 2007092800111 20070928 00111 NM 2007 9 28 KCSA071388 1 20070923 A 5340 FITTING BOEING 747 7472B4B 138481B NM BS 1910 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 AFT PIT, AFT PALLET STOP BATHTUB FITTING CRACKED AR BS 1910, RBL 25. 2 L 7 4 4F RT A20WE 2007092800112 20070928 00112 NM 2007 9 28 KCSA071389 1 20070923 A 5340 FITTING BOEING 747 7472B4B 138481B NM BS 1910 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 AFT PIT, AFT PALLET STOP BATHTUB FITTING CRACKED AT BS 1910, LBL 45. 2 L 7 4 4F RT A20WE 2007092800115 20070928 00115 NM 2007 9 28 SWAA074697 1 20070919 A 3350 3017BPEGPL LAMP BOEING 737 737317 138447P NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007092800117 20070928 00117 NM 2007 9 28 SWAA074803 1 20070925 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 344 S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007092800118 20070928 00118 NM 2007 9 28 SWAA074807 1 20070925 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 440 S23R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED 10Y CHECK, FOUND STRINGER 23R CRACKED AT BS 440. REPAIRED STRINGER PER EA. 2 L 7 2 4F RT A16WE 2007092800119 20070928 00119 WP 2007 9 28 UPS07850723 1 20070831 A 5350 FRAME DOUG DC8 DC873F 302199F WP BS 1973 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 TAIL CONE LWR NAV LIGHT LENS FWD FRAME HEAVILY CORRODED AT STA 1973. REPAIRED TAIL CONE LOWER NAV LI GHT LENS FORWARD FRAME IAW SRM 51-01- 04, DWG 5704663-3, SRM 53-05-03, SRM 51-1-8 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007092800120 20070928 00120 WP 2007 9 28 UPS07850724 1 20070914 A 5347 3657504501 SEAT TRACK DOUG DC8 DC873F 302199F WP 2ND OBSERVERS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 2ND OBSERVERS AFT SEAT TRACK WORN, CORRODED. REMOVED AND REPLACED 2ND OBSERVERS AFT SEAT TRACK IAW S RM 51-03-00 AND SRM 51-01-24. 2 L 7 4 4F RT 4A25 2007092800126 20070928 00126 NM 2007 9 28 KCSA071394 1 20070924 A 5411 FLANGE BOEING 747 7472B4B 138481B NM NR 2 PYLON WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 NR 2 PYLON LOWER AFT FLANGE WORN FROM PNUEMATIC DUCT ANTI-ROTATION CLIPS NAC STA 240. 2 L 7 4 4F RT A20WE 2007092800127 20070928 00127 NM 2007 9 28 KCSA071395 1 20070924 A 5420 WEB BOEING 747 7472B4B 138481B NM NR 2 NACELLE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 NR 2 PYLON NAC STA 202 LOWER WEB IS CRACKED .5 INCH. 2 L 7 4 4F RT A20WE 2007092800130 20070928 00130 NM 2007 9 28 SWAA074696 1 20070919 A 3350 3017BPEGPL LAMP BOEING 737 737317 138447P NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007092800137 20070928 00137 NM 2007 9 28 SWAA074685 1 20070916 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM BS 803 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 803, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007092800138 20070928 00138 NM 2007 9 28 SWAA074706 1 20070919 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 750 S18L CRACKED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007092800140 20070928 00140 NM 2007 9 28 SWAA074714 1 20070919 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM BS 706 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007092800143 20070928 00143 NM 2007 9 28 SWAA074688 1 20070919 A 5755 SKIN BOEING 737 7373Q8 1384670 NM RT WING SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING NR 9 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007092800144 20070928 00144 NM 2007 9 28 SWAA074686 1 20070919 A 3350 65C27093 LIGHT BOEING 737 7373Q8 1384670 NM L1 DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007092800148 20070928 00148 NM 2007 9 28 SWAA074694 1 20070919 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 685 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092800150 20070928 00150 2007 9 28 SWAA074711 4 20070919 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007092800151 20070928 00151 NM 2007 9 28 SWAA074713 1 20070919 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 793SA 27888 DURING SCHEDULED MV2 CHECK, FOUND FLIGHT DECK EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007092800153 20070928 00153 NM 2007 9 28 SWAA074707 1 20070919 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 3 ABC. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007092800154 20070928 00154 NM 2007 9 28 2007UALA03773 1 20070919 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 UPPER DECK EMERGENCY EXIT CEILING LIGHTS INOP JUST AFT OF ROW 15 & AT ROW 17. 10-16-07 REPLACED EMERGENCY EXIT LIG HT LAMPS IN TWO POSITIONS. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092700187 20070927 00187 NM 2007 9 27 UIEA200700373 1 20070912 A 5755 SKIN BOEING 747 747230B 1384889 NM ZONE 600 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 LHW SPOILER: NR 1 SPOILER I/B EDGE DELAMINATION EVIDENCE. NR 1 SPOILER PNL REPLACED IAW AMM 27-61-02. 2 L 7 4 4F A20WE 2007092700194 20070927 00194 NM 2007 9 27 UIEA200700353 1 20070904 A 5280 65B0794826 SEAL BOEING 747 7472D3B 1384805 NM NLG DOOR DAMAGED A UIEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 506MC 21252 AIR TURN BACK DUE TO NOSE GEAR DOOR OPEN INDICATION AFTER GEAR RETRACTION. FLIGHT CREW ADVISED, ACTUAL DOOR OPEN FAULT AND NOT INDICATION. AFTER ARRIVAL, MX INSPECTED AND FOUND FWD DOOR SEAL PARTIALLY OUT OF RETAINER. UPON MORE DETAILED INSPECTION AND MULTIPLE OPS CHKS. MX WAS ABLE TO REPRODUCE FAULT ON GROUND. FOUND PROX SWITCH TARGET BRACKET BENT AND SHIMS FROM RIGHT NOSE DOOR CATCHING THE SEAL. REPAIRED DAMAGE AS PER XEO 53-090507. 2 L 7 4 4F RT A20WE 2007092700203 20070927 00203 EU 2007 9 27 MALA070118 1 20070911 A 3350 330151 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 456XJ 340B456 DURING TASK CARD 335003 EMERGENCY POWER SUPPLIES 23LN AND 24LN FAILED BATTERY CAPACITY CHECK. REPLACED 23LN AND 24LN PO WER SUPPLIES WITH SERVICEABLE UNITS, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2007092700207 20070927 00207 SO 2007 9 27 C2XA07IA208 1 20070915 A 2611 DETECTION SYS EMB 145 EMB145XR 3260214 SO LAVATORY MALFUNCTIONED A C2XA O OTHER N FALSE WARNING IN INSP/MAINT 1 SW 27 11119 145677 IAH - FLIGHT 2163, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED A LAV SMOKE WARNING. MAINTENANCE INSPECTED THE AIRCRA FT, OPERATIONALLY CHECKED THE LAV SMOKE DETECTOR WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. 2 L 7 2 4F RT 2007092700228 20070927 00228 EA 2007 9 27 TRAX200701352 1 20070915 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR TORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 978EV 7723 PAX DOOR PLACARDS -EXIT- & -TO OPEN- TORN. 2 L 7 2 4F RT A21EA 2007092700230 20070927 00230 NM 2007 9 27 DL76G071246 1 20070924 A 5315 BAC1505101303 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 325 RBL26-54 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 156DL 25354 FLOORBEAM UPPER CHORD FOUND CORROSION AT BS 325 RBL 26-54. REMOVED AND REPLACED FLOORBEAM PER SRM 53-00-51D. 2 L 7 2 4F RT A1NM 2007092700266 20070927 00266 WP 2007 9 27 UPS07850682 1 20070919 A 3350 5708458503 BATTERY DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT FAILED PREFLIGHT TEST. REPLACED BATTERY AND RELAY UNIT W/REF M/M 33-50-01-2, OPS TEST GOOD. 2 L 7 4 4F RT 4A25 2007092700288 20070927 00288 EA 2007 9 27 COMA0770049 1 20070916 A 2780 766389M CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA E&E BAY FAULTY A COMA K NONE J WARNING INDICATION LD LANDING 1 SO 01 641CA 10614 10122 FLIGHT 9754 - SLATS FAILED AT 0 DEGREES. LANDED WITH 45 DEGREES OF FLAPS SAFELY. REMOVED AND REPLACED NR 2 SFECU. 2 L 7 2 4F RT A21EA 2007092700289 20070927 00289 NM 2007 9 27 SWAA074647 1 20070918 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 MID CABIN EMERGENCY EXIT LIGHTS ILLUMINATED WITH SWITCH IN ARMED POSITION. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007092700298 20070927 00298 NM 2007 9 27 SWAA074645 1 20070916 A 3320 480962 LENS BOEING 737 7377H4 1384404 NM CABIN CONTAMINATED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 443WN 29838 DECLARED EMERGENCY, FLIGHT ATTENDANT SAW SMOKE FROM READING LIGHT AT ROW 22F. FOUND READING LIGHT BULB AND LENS SOILED WITH CANDY. REMOVED AND REPLACED LIGHT BULB AND LENS PER MM. 2 L 7 2 4F RT A16WE 2007092700303 20070927 00303 NM 2007 9 27 SWAA074655 1 20070918 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007092700304 20070927 00304 NM 2007 9 27 SWAA074683 1 20070918 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 23L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007092700316 20070927 00316 NM 2007 9 27 QXEA200701460 1 20070918 A 5310 DOOR FRAME DHAV DHC8 DHC8202 2809007 NM PAX DOORWAY CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - CHAF ON FRAME AT STATION 222 - 2100, LEFT SIDE, MAIN CABIN DOOR FORWARD SIDE. REPAIRED IAW RD8-53-9791. 2 H 7 2 4T RT A13NM 2007092700320 20070927 00320 NM 2007 9 27 SWAA074671 1 20070918 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092700322 20070927 00322 NM 2007 9 27 QXEA200701462 1 20070919 A 5410 SUPPORT BRACKET DHAV DHC8 DHC8202 2809007 NM RT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - RIGHT NACELLE INBOARD FRAME SUPPORT BRACKET CHAFED. REPAIRED IAW SRM 51-20-51, RD8-54-2397. 2 H 7 2 4T RT A13NM 2007092700326 20070927 00326 NM 2007 9 27 QXEA200701457 1 20070921 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 342 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - CORROSION ON NR 1 SEAT TRACK AT STATION X342. REPAIRED IAW RD8-53-1342, SRM 51-40-00. 2 H 7 2 4T RT A13NM 2007092700339 20070927 00339 NM 2007 9 27 KCSA071383 1 20070919 A 5320 FITTING BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 AFT PIT, AFT AFT STOP BATHTUB FITTING IS CRACKED AT LBL 25 AT STA 1910. 2 L 7 4 4F RT A20WE 2007092700340 20070927 00340 NM 2007 9 27 KCSA071384 1 20070919 A 5210 DOOR BOEING 747 7472B4B 138481B NM R2 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 R-2 DOOR FWD LOWER VERTICAL CHORD HAS A 3 INCH CRACK NEAR RADIUS AREA. 2 L 7 4 4F RT A20WE 2007092700342 20070927 00342 NM 2007 9 27 QXEA200701459 1 20070919 A 5412 FIREWALL DHAV DHC8 DHC8202 2809007 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - THERE IS A CRACK IN THE RIGHT FIREWALL ABOUT 2" LONG JUST ABOVE AND INBOARD OF THE RIGHT ENGINE FIRE EXTINGUSHI NG LINE. REPAIRED IAW RD8-54-2396. 2 H 7 2 4T RT A13NM 2007092700344 20070927 00344 NM 2007 9 27 QXEA200701465 1 20070920 A 5313 STRINGER DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - STRINGER 24L CLEAT IS CORRODED AFT SIDE OF FRAME 424.124 AT STATION X426-X429. REPAIRED IAW SRM 51-20-11, 51-4 0-11. 2 H 7 2 4T RT A13NM 2007092700364 20070927 00364 NM 2007 9 27 QXEA200701454 1 20070923 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 473-484 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 C5 PDX - RIGHT INBOARD SEAT TRACK HAS WEAR DAMAGE, BOTTOM OF TRACK FRAME STATION X473 - 484. REPAIRED IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 2007092700376 20070927 00376 EU 2007 9 27 07FDEA04107 1 20070920 A 5330 A53610633 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORROSION ON UPPER SIDE (FRAME 14, STRG 11) ) OF THE FWD RT PAX DOOR FAIL/SAFE RING. REPAIR PERFORMED BY SMOOTH REWORK, HFEC/ROTOTEST INSPECTION AND OVERSIZING HOLES IN CORRODED AREA IAW EA 6-5312-82879 AND RAS/AS/151/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007092700377 20070927 00377 EU 2007 9 27 07FDEA04108 1 20070920 A 5313 A53778399206 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 434FE 355 FOUND CORROSION ON STRINGER P44 RT, C 34-35 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007092700378 20070927 00378 EU 2007 9 27 07FDEA04109 1 20070920 A 5330 A53985240204 SKIN PANEL AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORROSION ON THE INTEGRAL SKIN PANEL BETWEEN FRAME 76-80, STRG 6 LT - 6 RT AND BETWEEN FRAME 80-91, STRG 8 LT - 8 RT. R EPAIR PERFORMED BY CUT OUT SOME AREAS (OUT OF SRM LIMIT) AND INSTALLATION OF FIVE EXTERNAL DOUBLERS IAW EA 6-5319-82905 AND RAS/DAHAM/4800124/2005 ISSUE B. 2 L 7 2 4F RT A35EU 2007092700392 20070927 00392 EU 2007 9 27 07FDEA04141 1 20070921 A 5313 A53778398 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORRODED STRINGER 54 RT BETWEEN FRAME 37-38. PARTIAL STRINGER INSTALLATION WITH TWO STRINGER SPLICE REPAIRS BETWEEN FRA ME 36-37 AND 37-38 PERFORMED IAW SRM 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007092800007 20070928 00007 NM 2007 9 28 SWAA074797 1 20070925 A 3350 311500 LENS BOEING 737 7373K2 13844BA NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED SPV CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 10 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007092800012 20070928 00012 NM 2007 9 28 SWAA074802 1 20070925 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM BS 421 S17R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 421, STR 17R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007092800015 20070928 00015 2007 9 28 SWAA074799 4 20070925 A 2565 6557463 FITTING BOEING 737 7377H4 1384404 NM R1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 441WN 29837 R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER MM. 2 L 7 2 4F RT A16WE 2007092800017 20070928 00017 NM 2007 9 28 SWAA074804 1 20070925 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 294 S13R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007092800026 20070928 00026 2007 9 28 SWAA074779 4 20070924 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 717SA 27851 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007092800031 20070928 00031 NM 2007 9 28 SWAA074793 1 20070924 A 5755 ATTACH FITTING BOEING 737 7375H4 138449D NM RT WING SPOILER LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED HC2 CHECK, FOUND RIGHT WING INBOARD GROUND SPOILER OUTBOARD ATTACH POINT LOOSE. REMOVED AND REPLACED S POILER PER MM. 2 L 7 2 4F RT A16WE 2007092800038 20070928 00038 2007 9 28 2007UALA03747 4 20070917 A 8300 BEARING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE AGB FAILED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 588UA 26717 726502 RTFL DUE TO HIGH OIL TEMPERATURE & ENGINE OIL BYPASS MESSAGE. 10-19-07 ON DESCENT OIL TEMP SPIKED TO 171. 161 TO 1 71 DURING ENTIRE DESCENT. SUPPLEMENTAL DATA UPDATE ANGLE GEARBOX AB1 BEARING FAILED AND OUTER RACE OF BEARING FRACTURED . ALUMINUM BASE MATERIAL OF AGB HOUSING RELEASED DURING THE FAILURE EVENT CLOGGED THE OIL FILTER TO TRIP THE DELTA P SW ITCH. ENGINE WAS SHUT DOWN IN A TIMELY MANNER TO MITIGATE ENGINE DAMAGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092800039 20070928 00039 NM 2007 9 28 2007UALA03734 1 20070915 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LAVATORY SMOKE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 510UA 24780 SMOKE WAS DETECTED IN THE 2L LAV. 10-9-07 FLT ATTENDANT NOTED OVERHEATED ELECTRICAL ODOR IN LAV AT 2L UPON ARRIVAL; CAPTAIN CONFIRMED ODOR. TRIED TROUBLESHOOTING BY OPERATING ALL EQUIPMENT AND INSPECTING ALL COMPONENTS IN 2L LAV. FOUN D ALL EQUIPMENT WORKING. NO ODOR DETECTED. POWERED AIRCRAFT AND COULD NOT DUPLICATE SMOKE ODOR AFTER ACFT WAS MOVED TO HANGER. INSPECTED INTERIOR LAV PANELS AND ABOVE CEILING PANELS AROUND LAVATORY. TURNED ON VIDEO SYSTEM, STILL NO DISCRE PANCIES NOTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092800051 20070928 00051 2007 9 28 2007UALA03749 4 20070917 A 2565 SLIDE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU L2 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 903UA 25003 DOOR 2L SKIRT IS TOO LONG. F/A'S REPORTED, SKIRT MAKES IT HARD TO ARM-DISARM DOOR. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092800054 20070928 00054 2007 9 28 2007UALA03752 4 20070918 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 2R READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 DOOR 2R SLIDE PRESSURE READS AT GREEN & RED BAND, BELOW NR 3 SVC LIMITS. 10-19-07 REPLACED DOOR 2R SLIDE ASSEMBLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092800061 20070928 00061 NM 2007 9 28 2007UALA03759 1 20070918 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 CABIN, B-ZONE LEFT EEL'S INOP. 10-19-07 REPLACED EEL BATTERY PACK. OP CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092800071 20070928 00071 NM 2007 9 28 SWAA074746 1 20070921 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 760 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007092800102 20070928 00102 NM 2007 9 28 ABXA070299 1 20070916 A 5412 BULKHEAD BOEING 767 767231 1385131 NM NR 2 NACELLE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 709AX 22572 NR 2 PYLON AFT TORQUE BOX BULKHEAD SIDE BRACE ATTACH LUG HAD LOCK FASTENER HEAD SHEARED OFF LEFT SIDE. REPLACED BROKEN AND MISSING HI-LOKS IAW B767 MM 54-51-03, DC9 SRM 51-40-02, AND DWG 311T3180 AS PER RFTS 42887. 2 L 7 2 4F RT A1NM 2007092800116 20070928 00116 NM 2007 9 28 SWAA074811 1 20070925 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 907 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007092800121 20070928 00121 WP 2007 9 28 UPS07850725 1 20070916 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1746, L17R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 FUSELAGE EXTERIOR SKIN CRACKED AT STA 1746 AND L17R. REPAIRED FUSELAGE EXTERIOR SKIN AT STA 1746 AND L17R IAW SRM 53-02- 01 FIG 7. 2 L 7 4 4F RT 4A25 2007092800123 20070928 00123 NM 2007 9 28 KCSA071391 1 20070924 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 517 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA 517 LBL 46 SEAT TRACK HAS CORROSION. 2 L 7 4 4F RT A20WE 2007092800125 20070928 00125 NM 2007 9 28 KCSA071393 1 20070924 A 5210 ATTACH ANGLE BOEING 747 7472B4B 138481B NM R5 DOOR CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 R-5 DOOR HAS CORROSION ON ATTACH ANGLE BELOW LOWER HINGE CLOSE OUT WEB STA 2250. 2 L 7 4 4F RT A20WE 2007092800155 20070928 00155 NM 2007 9 28 2007UALA03774 1 20070919 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EXIT LIGHT INOP AT TOP OF UPPER DECK STAIRS JUST AFT OF ROW 18 CEILING LIGHT. 10-16-07 REPLACED LAMP. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092800156 20070928 00156 NM 2007 9 28 2007UALA03775 1 20070919 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 RIGHT EXTERIOR OVERWING EMERGENCY EXIT LIGHT ASSY INOP, SECOND FROM AFT LIGHT ASSY ONE BULB INOP. 10-16-07 REPLACED LAMP. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092800159 20070928 00159 NM 2007 9 28 2007UALA03778 1 20070919 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 RIGHT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOP, MOST AFT LIGHT ASSY, ONE BULB INOP. 10-16-07 REPLACED LIGHT ASS Y. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092800161 20070928 00161 NM 2007 9 28 2007UALA03780 1 20070918 A 4940 STARTER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE APU MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 785UA 26954 APU START SYSTEM APUC DETECTED FAILURE IN THE ELECTRIC STARTER, FUEL SCHEDULING, IGNITION, OR LUBE DEPRIME SYSTEMS OR NO SIGNAL FROM ELMS TO THE APUC. 10-16-07 REPLACED APU IGNITOR PLUG NR 1 PER MM49-41-02, AND IGNITION LEAD NR 1 PER MM49-41-04. APU BITE TEST ACCOMPLISHED. CHECKD OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007092800163 20070928 00163 NM 2007 9 28 2007UALA03782 1 20070918 A 3520 OXYGEN MASK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE SEAT 11 DEF UNWANTED DEPLOY A UALA O OTHER O OTHER LD LANDING 1 WP 29 851UA 1664 THE 11 DEF OXYGEN MASKS DEPLOYED ON LANDING. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092800164 20070928 00164 2007 9 28 2007UALA03783 4 20070918 A 2565 INDICATOR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU DOOR SLIDE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 929UA 26652 AFT GALLEY DOOR EVAC SLIDE PRESSURE GAUGE IS DISCOLORED AND NOT EASILY VISIBLE. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092800165 20070928 00165 NM 2007 9 28 CALA0700525 1 20070920 A 3230 65448106 ACTUATOR BOEING 737 737300 1384610 NM LT MLG UPLOCK INOPERATIVE A CALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 69348 60665 23586 THE LEFT MLG DID NOT INDICATE DOWN & LOCKED WHEN GEAR WAS EXTENDED ON APPROACH TO IAH. MANUAL EXTENSION WAS PERFORMED A ND YAW WAS FELT WHEN LEFT MAIN EXTENDED. THE GEAR INDICATED 3 GREEN AND LANDING WAS NORMAL. THE GEAR WAS SWUNG SEVERA L TIMES WITH NO FAULTS NOTED. THE LEFT MAIN GEAR UPLOCK ACTUATOR WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE IA W M/M 32-32-41. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2007092800166 20070928 00166 NM 2007 9 28 CALA0700526 1 20070920 A 3350 11260653 BATTERY PACK BOEING 737 737800* NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 77258 30802 THE L-1 DOOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. THE BATTERY PACK WAS REPLACED AND OPERATIONAL CHECKS WERE G OOD. 2 L 7 2 4F RT A16WE 2007092800168 20070928 00168 SO 2007 9 28 LR7A07093 1 20070917 A 5320 3393943 FITTING LKHEED 382 382G 526414U SO FS 477 RBL 71 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 646 4590 DURING SCHEDULED B-2 CHECK, PER JOBCARD HB5301, FOUND CENTER FUSELAGE EXTERIOR STRUT UPPER FITTING CRACKED AT FS 477 WL 150 RBL 71. FITTING REPLACED IAW SMP583 FIG 51-60 & 51-70. P/N:339394-3. 2 H 7 4 4T A1SO 2007092800169 20070928 00169 SO 2007 9 28 LR7A07094 1 20070917 A 5312 LS4312 BULKHEAD LKHEED 382 382G 526414U SO FS 880 RBL 62 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 646 4590 DURING SCHEDULED B-2 CHECK, PER JOBCARD HB5302 FOUND AFT FUSELAGE INTERIOR UPPER BHD WEB CRACKED AT FS 880, WL 260, RBL 62. REPAIR CARRIED OUT IAW SMP583 FIG 53-50-05. P/N:7075T6 .063". 2 H 7 4 4T A1SO 2007092800171 20070928 00171 SO 2007 9 28 LR7A07096 1 20070917 A 5320 LS27263 SUPPORT LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 646 4590 DURING SCHEDULED B-2 CHECK, PER JOBCARD HB5301, FOUND RAMP DOOR FLOORBEAM SUPPORT BROKEN AT RS6 BL 0. SUPPORT FABRICATE D & REPLACED IAW SMP583 CHAPTER 51-60 & 51-70. 2 H 7 4 4T A1SO 2007092800174 20070928 00174 NM 2007 9 28 2007UALA03784 1 20070915 A 2697 SOCKET BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FIRE LOOP BROKEN A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 182UA 25279 THE 'ENG 1 FIRE LP A' EICAS STATUS MSG DISPLAYED. ENG 1 FIRE LOOP A FIRE OR FAULT OUTPUT. 0-16-07 AFTER TROUBLESH OOTING & REPLACING FIRE OVERHEAT DETECTION LOGIC CARD, DETERMINED THAT PROBLEM WAS A BROKEN SOCKET IN THE FIRE LOOP CIRC UIT. W4515-104-20R WAS BROKEN AT CONN D43696P. INSTALLED NEW SOCKET AND SECURED. OPS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092800175 20070928 00175 NM 2007 9 28 2007UALA03785 1 20070917 A 2913 PUMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE HYD SYSTEM FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 775UA 26947 777022 NR 2 ENG EDP FAILED DURING ENG RUN. 10-16-07 REPLACED ENGINE DRIVEN HYDRAULIC PUMP PER MM 29-11-0 5. FOUND SLUDGE IN LINES & FLUSHED SYSTEM LINES. ALL VALVES CHECKED OK. HYDRAULIC SYSTEM CHECKS OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007092800177 20070928 00177 NM 2007 9 28 2007UALA03787 1 20070919 A 8011 STARTER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ENGINE FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 661UA 27158 717604 UNABLE TO START RIGHT ENGINE. 10-19-07 REPLACED RIGHT ENGINE STARTER AND START VALVE. NOW RIGHT ENGINE STARTS NORM ALLY. ALSO ALL INDICATIONS NORMAL . 2 L 7 2 4F 4 F RT A1NM E24NE 2007092800178 20070928 00178 NM 2007 9 28 2007UALA03788 1 20070918 A 2780 FSEU BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 2 FAILED A UALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 29 772UA 26930 PRIMARY SLATS FAIL ON FINAL. 10-16-07 REPLACED FSEU 2 PER MM 27-51-01. ACCOMPLISHED MAT TEST AND TEST PASSED. SLA T PROBLEM STILL CHRONIC. REPLACED SLAT PRIMARY CONTROL VALVE PER 27-81-05. LEAK CHECK OK. PERFORMED SLAT PRIMARY CONTRO L VALVE TEST. FOLLOWING REPLACEMENT OF THE CONTROL VALVE, THE MESSAGES ARE CLEARED. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007092800179 20070928 00179 NM 2007 9 28 2007UALA03789 1 20070919 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 848UA 1647 RIGHT I/B FLOORBEAM FROM FRAME 42 THROUGH 47-51 IS GOUGED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED: REPLACED SEAT TRAC K. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092800180 20070928 00180 NM 2007 9 28 2007UALA03790 1 20070919 A 5347 SEAT TRACK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 848UA 1647 LEFT O/B SEAT TRACK FROM FRM 42 THRU 47-51 IS GOUGED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED: REPLACED SEAT TRACK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092800182 20070928 00182 NM 2007 9 28 2007UALA03792 1 20070919 A 5310 DOOR FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 929UA 26652 FWD CARGO DOOR CUTOUT AFT FRAME IS CRACKED IN RADIUS ON AFT SIDE OF FRAME AT UPPER INBOARD CORNER OF LOWER STOP FITTING. MAJOR REPAIR ACCOMPLISHED: INSTALLED FRAME ANGLE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092800187 20070928 00187 WP 2007 9 28 ABXA070320 1 20070907 A 5320 4924659501 FITTING DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 CRACKED FITTING RIGHT BUTT LINE 6 AT P-DOME DOOR JAMB - LOWER. REMOVED AND REPLACED FITTING IAW DC9 SRM. 2 L 7 2 4F A6WE 2007092800189 20070928 00189 WP 2007 9 28 ABXA070313 1 20070905 A 5311 9923409501 FRAME DOUG DC9 DC933F 302207A WP BS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 LEFT AFT MAIN FRAME STA 737 WAS CRACKED ON UPPER INBOARD FORWARD FLANGE BETWEEN Z-CLIP FASTENERS. REPAIRED MAIN FRAME S TA 737 LEFT IAW EA 53400310. 2 L 7 2 4F A6WE 2007092800191 20070928 00191 WP 2007 9 28 ABXA070315 1 20070905 A 5322 99577397 SHEAR TIE DOUG DC9 DC933F 302207A WP BS 945 L14-15L CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 SHEAR TIE CRACKED 2 PLACES FS 945, LONGERON 14 - 15 LEFT. REPAIRED SHEAR TIE IAW DC9 SRM. 2 L 7 2 4F A6WE 2007092800193 20070928 00193 WP 2007 9 28 ABXA070317 1 20070905 A 5322 SHEAR TIE DOUG DC9 DC933F 302207A WP BS 965 L14R CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 SHEAR TIE FS 965 LONGERON 14 RIGHT CRACKED. REPAIRED CRACKED SHEAR TIE IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 2007092800194 20070928 00194 WP 2007 9 28 ABXA070318 1 20070905 A 5322 99577397N SHEAR TIE DOUG DC9 DC933F 302207A WP BS 945 S15R CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 SHEAR TIE FS 945 LONGERON 15 RIGHT WAS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2007092800195 20070928 00195 WP 2007 9 28 ABXA070319 1 20070907 A 5310 39132949501 BEAM DOUG DC9 DC933F 302207A WP CARGO DOORWAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 FORWARD LOWER CARGO DOOR BEAM END CRACKED NR 4 BEAM FORWARD END STEEL CAP. REPLACED FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2007092800197 20070928 00197 EU 2007 9 28 TRAX200701359 1 20070904 A 5720 FRAME AEROSP ATR72 ATR72 EU WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 AT JCT FR 25 & WING RIB 4, WING BOX FRAME FOUND CRACKED AROUND RIVET. 2 H 7 2 4T RT 2007092800201 20070928 00201 EA 2007 9 28 TRAX200701363 1 20070916 A 3350 CHARGER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 NR 4 EMERGENCY LIGHTS BATTERY CHARGER NEEDS REPLACED. 2 L 7 2 4F RT A21EA 2007092800205 20070928 00205 NM 2007 9 28 2007UALA03797 1 20070920 A 2910 UNKNOWN BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE HYD SYSTEM MALFUNCTIONED A UALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 WP 29 673UA 29241 MADE A GO-AROUND AND LANDED UNDER AMBER ALERT DUE TO FLAP INDICATION PROBLEMS ON APPROACH. 10-16-07 ACCOMPLISHED V ISUAL CHK OF FLAPS AND SLATS. ACCOMPLISHED BITE OF BOTH FSEU, AND FSPM CARDS BOTH CHECKED OK. NO FAULTS, OK LIGHTS AND M ESSAGES CLEARED. CYCLED FLAPS-SLATS THRU ENTIRE RANGE TWICE WITH HYDRAULICS. OP CHECKS OK. MESSAGES AND LIGHTS CLEARED W HEN RUN ELECTRICALLY AND HYDRAULICALLY. UNABLE TO DUPLICATE PROBLEM. OPS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092800206 20070928 00206 NM 2007 9 28 2007UALA03798 1 20070920 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY CEILING LIGHTS ABOVE ROW 5 RT, 8 LT AND 15 ARE INOPERATIVE. 10-16-07 RELAMPED EMERGENCY LIGHTS IN ALL T HREE POSITIONS. ALL OP CHECKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092800207 20070928 00207 2007 9 28 2007UALA03799 4 20070920 A 2565 GIRT BAR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE R2 DOOR SLIDE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 786UA 26938 CREW VERBAL: FLIGHT ATTENDANT REPORTS DOOR 2R DISARM LEVER IS STIFF. 10-16-07 REINSTALLED GIRT BAR ACP INSPECTION OF DOOR AND ARMING MECHANISM .DOOR OPS NORMAL. REPLACED GIRT BAR PICK-UP FITTING. FOUND AFT HOOK ASSY. BENT. GIRT BAR IS BINDING ON AFT FLOOR FITTING. ADJUSTED AFT GIRT BAR FLOOR FITTING POSITION PER MM 52-11-00. DOOR OPEN AND CLOSE OPS FINE. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007092800208 20070928 00208 NM 2007 9 28 2007UALA03800 1 20070919 A 7810 EXHAUST DUCT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 1 ENGINE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 819UA 893 V10019 NR 1 ENG TAILCONE HAS MANY CRACKS AT THE ATTACH WELD MOUNTS. OVER 12 INCHES TOTAL LENGTH OF CRACKS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092800209 20070928 00209 WP 2007 9 28 ABXA070310 1 20070902 A 5553 591214129 ATTACH ANGLE DOUG DC9 DC933F 302207A WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 VERTICAL STABILIZER RIGHT ATTACH ANGLE COMMON TO FUSELAGE CRACKED - AFT. REPAIRED RIGHT VERTICAL STABILIZER ATTACH ANGL E IAW DC9 SRM 53-05. 2 L 7 2 4F A6WE 2007092800210 20070928 00210 WP 2007 9 28 ABXA070312 1 20070904 A 5415 591326245N ATTACH ANGLE DOUG DC9 DC933F 302207A WP LT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 LEFT PYLON LOWER ATTACH ANGLE WAS CRACKED FS 990. REPAIRED LOWER PYLON ATTACH ANGLE IAW DC9 SRM. 2 L 7 2 4F A6WE 2007092800211 20070928 00211 WP 2007 9 28 ABXA070309 1 20070902 A 5534 5912103501 BRACKET DOUG DC9 DC933F 302207A WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 VERTICAL STABILIZER UPPER RUDDER ATTACH HINGED BRACKET - RIGHT - CRACKED. REMOVED AND REPLACED RUDDER BRACKET IAW DC9 S RM. 2 L 7 2 4F A6WE 2007092800213 20070928 00213 NM 2007 9 28 UPS07M50726 1 20070923 A 3350 1829 LAMP DOUG MD11 MD11F 3023600 NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP 48575 INSPECTION TYPE:N/A FOUND ONE EMERGENCY LIGHT U/S AT ABOVE LT FWD ENTRY DOOR. REPLACED LAMP AS PER AMM 33-52-0-4. EMER GENCY LIGHT TEST COND NORMAL AS PER AMM 33-52-01. 2 L 7 3 4F RT A22WE 2007092800215 20070928 00215 NM 2007 9 28 UPS07M50729 1 20070629 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 839-939 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C CORROSION ON SEAT TRACK CROWN, CHANNEL & FLANGE FROM STA 839-939 X=-75. CABIN SEAT TRACK X=-75, STA 8 39-939, CROWN CHANNEL & FLANGE AREA CORR RMVD & AREA REPROTECTED SRM 51-21-01 VII R38. FLANGE ORG THK 0.080" MAT'L REM ND 0.042". MATL RMVD 0.038" FOUND EXCEED LIMIT SRM 53-70-00 FIG 3 VI R38. CORR SEAT TRACK TRIM OFF AT STA 832-969. CO RR SEAT TRACK RMVD. FEC INSP C/O, NO CRACK. NEW SEAT TRACK, SPLICE & PLATE FAB & INSTALLED SRM 51-31-01 VII R38. 2 L 7 3 4F RT A22WE 2007092800222 20070928 00222 SO 2007 9 28 C2XA07CL082 1 20070923 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NLG FAULTY A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 14905 145476 EWR FLIGHT 2764 THE CREW REPORTED NOISE FROM FORWARD COMPARTMENT AND DIVERTED INTO CLE. MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR DOORS NOT RETRACTING. THE LANDING GEAR UPLOCK PROXIMITY SWITCH WAS REPLACED. OPERATIONAL CHECKS WERE GO OD. 2 L 7 2 4T RT T00011AT 2007092800223 20070928 00223 NM 2007 9 28 USAA920070833 1 20070917 A 5330 6545775 SKIN BOEING 737 737301 1384611 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 DCA - MAJOR REPAIR - WEEKLY CHECK - NR 75715036, CRACKED FUSELAGE SKIN, BS 727E - BS 747, S21R. REPAIRED FUSELAGE SKIN, BS 727E - BS 747, S21R IAW 737-300 SRM 53-00-01. 2 L 7 2 4F RT A16WE 2007100100001 20071001 00001 NM 2007 10 1 07FDEA04273 1 20070925 A 5720 6521795282 BRACKET BOEING 727 727227 1384078 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 RT WING, OTBD FLAP, INBD FLAP TRACK FAIRING IS CRACKED, AT CHANNEL SUPPORT ANGLE 16 INCHES AFT OF FWD EDGE, RT SIDE REMO VED DAMAGED TEE AND INSTALLED NEW ONE IAW SRM 51-30-2 AND 51-30-5 PG 5. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2007100100002 20071001 00002 EU 2007 10 1 07FDEA04274 1 20070925 A 5720 A57246666 DEFLECTOR AIRBUS 300 A300B4605R 3930308 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 FOUND DAMAGED EDGE BAND OF DEFLECTOR DOOR 572CB AT LT WING. BONDING REPAIR PERFORMED IAW SRM 51-77-12, APPROVED BY EA 6 -5755-112454 AND RAS/BAE/1005223/2007 ISSUE A. 2 L 7 2 4F RT A35EU 2007100100003 20071001 00003 NM 2007 10 1 07FDEA04275 1 20070925 A 5330 6517527 SKIN BOEING 727 727227 1384078 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 AFT FUSELAGE AT FS 1320 IN SECTION 48 ZONE, SKIN HAS 2 PREVIOUS PUNCTURES FILLED WITH SEALANT ON LT SIDE OF A/C BETWEEN STRINGERS 3L AND 6L JUST BELOW VERTICAL STAB. REMOVED DAMAGE SRM 53-30-3 FIG 13A. FABRICATED REPAIR DOUBLER SRM 53-30- 3 FIG 13 A. NDT AT STR 3L AND 6L IAW 727 MAN PART 4 51-00-00 FIG 2, PART 6 51-00-00 FIG 23 ORG "T" .055, REMAINING "T" .052, LOSS .003 AT 6L, NO DEFECTS AT 3L AND 6L. ALODINED AND PRIMED DOUBLER AT 3L AND AREA AT 6L SRM 51-10-2 PG 7 AND 8 . INSTALLED DOUBLER AT 3L SRM 53-30-3 PG 74C. PAINTED AREAS AT 3L AND 6L SRM 53-30-3 PG 74C. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007100100004 20071001 00004 EU 2007 10 1 07FDEA04276 1 20070925 A 5311 A53810788200 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 CRACKED HOLE "H1" ON FRAME 46 LT, STR 27. REPAIR PERFORMED BY OVERSIZING HOLE IAW SB A300-53-6122 AND REV 02 OF SB 53-6 125 (OVERSIZING, FRAME FOOT CUT OUT AT HOLE H1 AND COLD EXPANSION), IAW EA 6-5315-82931. 2 L 7 2 4F RT A35EU 2007100100005 20071001 00005 NM 2007 10 1 KCSA071427 1 20070927 A 5330 SKIN BOEING 747 7472B4B 138481B NM BS 665 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA 665 ABOVE STR 44R SKIN DAMAGED. 2 L 7 4 4F RT A20WE 2007100100006 20071001 00006 NM 2007 10 1 KCSA071428 1 20070927 A 5315 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 760 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FLOORBEAM AT STA 760 IS DAMAGED ON AFT SIDE AT LBL 30 TO LBL 33. 2 L 7 4 4F RT A20WE 2007100100007 20071001 00007 WP 2007 10 1 WRLA2007099 1 20070925 A 5313 LONGERON SPLICE DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE BS 1986 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 303WL 46917 DURING C-CHECK FOUND LONGERON LT 44 JOINT SECTION AT STA 1986 CRACKED. N/R 67297. LONGERON JOINT REPLACED REF.BOEING D WG NGA6313 AND DC10 SRM VOL.1 53-30-00 FIG.5 REV. MAY 15/96. 2 L 7 3 4F 4 F RT A22WE E23EA 2007100100008 20071001 00008 WP 2007 10 1 WRLA2007100 1 20070918 A 2620 SEAL DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE BS 1441 MISSING A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 303WL 46917 DURING C-CHECK FOUND THE LOWER CENTER CARGO COMP FIRE EXTINGUISHING LINE JOINT IS OPEN AND SEAL RING IS MISSING AT STA14 41. N/R 66723. REINSTALL THE LINE JOINT WITH SEAL RING AND TEST THE DEPLOYMENT LINES REF DC10 AMM 26-22-03.201 REV 81. 2 L 7 3 4F 4 F RT A22WE E23EA 2007100100009 20071001 00009 NM 2007 10 1 SB07082 1 20070926 A 3350 20131ASMI BATTERY PACK BOEING 737 737401 1384701 NM EMERGENCY LIGHTS DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 PIT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 23 THRU 25 AND THE AFT OVERHEAD EXIT SIGN WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT BATTERY PACK. OPERATIONAL CHECK GOOD PER MM 33-51-51. 2 L 7 2 4F RT A16WE 2007100100010 20071001 00010 NM 2007 10 1 MASA200700484 1 20070805 A 3510 OXYGEN MASK DHAV DHC8 DHC8202 2809007 NM COCKPIT DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 455YV 455 ASH 7104 DEN-HDN. F/O CLICK ON OXYGEN MASK MISSING HEAD PAD. MX CHANGED THE OXYGEN MASK. 2 H 7 2 4T RT A13NM 2007100100012 20071001 00012 SO 2007 10 1 C2XA07IA209 1 20070914 A 3150 WARNING LIGHT EMB 145 EMB145XR 3260214 SO CARGO FIRE FALSE ACTIVATION A C2XA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 27 34110 145658 IAH - FLIGHT 2021, THE CREW REPORTED THAT THE BAGGAGE EXT LIGHT CAME ON DURING CRUISE AND REMAINED ON FOR THE REMAINDER OF THE FLIGHT WITH NO ASSOCIATED EICAS MESSAGE OR FIRE OR SMOKE OBSERVED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT W HERE MAINTENANCE RESET THE BAGGAGE EXTINGUISHING SYSTEM, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT W AS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007100100013 20071001 00013 SO 2007 10 1 C2XA07IA210 1 20070915 A 3350 2013BR BATTERY PACK EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17513 754 754 145292 IAH - DURING MAINTENANCE INSPECTION, THE LEFT HAND FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFETCS, AND THE AIRCRA FT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007100100017 20071001 00017 NM 2007 10 1 MASA200700529 1 20070828 A 2697 CONNECTOR DHAV DHC8 DHC8202 2809007 NM SMOKE DETECTION LOOSE A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 991HA 431 ASH 2896 PHX. INTERMITTENT SMOKE WARNING LIGHT. MX RESECURED CONNECTOR ON FWD SMOKE DETECTOR. 2 H 7 2 4T RT A13NM 2007100100018 20071001 00018 NM 2007 10 1 KCSA071404 1 20070925 A 5310 PANEL BOEING 747 747122 1384872 NM TORQUE BOX PUNCTURED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 FWD PIT BILGE TORQUE BOX UPPER PANEL PUNCTURED AT BS 670, RBL 50. 2 L 7 4 4F A20WE 2007100100019 20071001 00019 NM 2007 10 1 KCSA071405 1 20070925 A 5310 PANEL BOEING 747 747122 1384872 NM TORQUE BOX PUNCTURED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 AFT PIT BILGE TORQUE BOX UPPER PANEL PUNTURED AT BS 1650, LBL 50. 2 L 7 4 4F A20WE 2007100100023 20071001 00023 NM 2007 10 1 USAA920070854 1 20070923 A 5311 652072328 FRAME BOEING 737 7374B7 1384702 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - MAJOR REPAIR - FPBH INSPECTION - NR 6006801, FORWARD CARGO COMPARTMENT DOOR CUTOUT FORWARD FRAME CRACKED, BS 492, S25R. REPAIRED FORWARD CARGO COMPARTMENT DOOR CUTOUT FORWARD FRAME, BS 492, S25R IAW USAIRWAYS EA 98884. 2 L 7 2 4F RT A16WE 2007100100024 20071001 00024 NM 2007 10 1 USAA920070855 1 20070924 A 5330 6545775 SKIN BOEING 737 7373B7 1384580 NM BS 727D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 533AU 24515 PIT - MAJOR REPAIR - NR 7639350, CRACKED FUSELAGE SKIN, BS 727D, S22R. REPAIRED FUSELAGE SKIN, BS 727D - 727E, S22R - S 23R IAW USAIRWAYS TYPICAL REPAIR 53-60-03A. 2 L 7 2 4F RT A16WE 2007100100036 20071001 00036 NM 2007 10 1 KCSA071417 1 20070926 A 5313 STRINGER BOEING 747 7472B4B 138481B NM BS 2360 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STR 38R END FITTING CORRODED FWD OF BS 2360. 2 L 7 4 4F RT A20WE 2007100100037 20071001 00037 NM 2007 10 1 KCSA071418 1 20070926 A 5313 FITTING BOEING 747 7472B4B 138481B NM BS 2360 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STR 46R END FITTING CORRODED FWD OF BS 2360. 2 L 7 4 4F RT A20WE 2007100100038 20071001 00038 EU 2007 10 1 USAA920070858 1 20070921 A 5347 D53371110010 SEAT TRACK AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 636AW 098 SAL - MAJOR REPAIR - C-05 CHECK - NR 5989144, CORROSION ON CABIN SEAT TRACK, -Y765, BS 1650 / FR 41 - BS 1976 / FR 47. REPLACED CABIN SEAT TRACK, -Y765, BS 1650 / FR 41 - BS 1976 / FR 47 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007100100040 20071001 00040 EA 2007 10 1 TRAX200701382 1 20070922 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 914EV 7752 INSIDE ASD ACCESS PANEL 832BR FOUND CRACK IN THE UPPER RADIUS OF THE AFT INTERCOSTAL. (AS VIEWED FACING ACFT WITH DOOR O PEN). ALSO MARKED ON THE OUTSIDE SKIN AS REFERENCE. 2 L 7 2 4F RT A21EA 2007100100041 20071001 00041 EA 2007 10 1 TRAX200701383 1 20070922 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 848AS 7339 PAX DOOR HANDLE BROKEN. COULD NOT OPEN DOOR FROM INSIDE. 2 L 7 2 4F RT A21EA 2007100100046 20071001 00046 NM 2007 10 1 USAA920070838 1 20070914 A 5320 46N8722 WEB BOEING 757 757225 1384959 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916UW 22192 PIT - MAJOR REPAIR - C-4 CHECK, CORROSION ON WEB, BS 1681 - BS 1701, S17L. REPLACED WEB, BS 1681 - BS 1701, S17L IAW B7 57-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007100100047 20071001 00047 NM 2007 10 1 USAA920070839 1 20070912 A 5320 146N5242 CHANNEL BOEING 757 757225 1384959 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916UW 22192 PIT - MAJOR REPAIR - C-4 CHECK, CORROSION ON CHANNEL, BS 1640 - BS 1660, BL 0. REPLACED CHANNEL, BS 1640 - BS 1660, BL 0 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007100100050 20071001 00050 NM 2007 10 1 USAA920070842 1 20070914 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916UW 22192 PIT - MAJOR REPAIR - C-4 CHECK, CRACKED INTERCOSTAL, BS 660 - BS 680, BL 0. REPLACED INTERCOSTAL, BS 660 - BS 680, BL 0 IAW B757-200 SRM 50-30-51. 2 L 7 2 4F RT A2NM 2007100100051 20071001 00051 NM 2007 10 1 USAA920070843 1 20070915 A 5320 ANGLE BOEING 757 757225 1384959 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916UW 22192 PIT - MAJOR REPAIR - C-4 CHECK, CORROSION ON ANGLE, BS 480 - BS 500, RBL 10. REPLACED ANGLE, BS 480 - BS 500, RBL 10 IA W B757-200 SRM 53-00-051. 2 L 7 2 4F RT A2NM 2007100100055 20071001 00055 NM 2007 10 1 2007UALA03801 1 20070919 A 2840 2008100000201 COMPENSATOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 FUEL TANK MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 171UA 24322 AIRCRAFT EXPERIENCING FUEL QUANTITY/FUEL TRANSFER PROBLEMS. 10-16-07 AFTER TROUBLESHOOTING ISOLATED PROBLEM TO FUE L COMPENSATOR IN NR 4 TANK. REPLACED NR 4 FUEL MAIN TANK COMPENSATOR WITH NEW UNIT PER MM 28-41-02-4 01. SYSTEM CHEC KED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007100100056 20071001 00056 SO 2007 10 1 C2XA07RI081 1 20070913 A 2750 3631001007MOD3 CONTROL UNIT EMB 145 EMB145LR 3260212 SO TE FLAPS DEFECTIVE A C2XA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 SW 27 12540 13508 13365 145537 FLT 2692 - EWR - CREW REPORTED FLAP FAIL & SPS ADVANCE MESSAGE IN FLIGHT. CREW DECLARED EMERGENCY. ACFT LANDED UNEVENT FULLY. EWR MX REMOVED AND REPLACED FECU AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO S ERVICE. 2 L 7 2 4T RT T00011AT 2007100100061 20071001 00061 EA 2007 10 1 TRAX200701367 1 20070917 A 2530 COFFEEMAKER CNDAIR CL600 CL6002B19 1900309 EA GALLEY ODOR A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 857AS 7411 CLIMBING THRU F260 TO F300 HAD A STRONG SMOKE LIKE ODOR. SMELLED LIKE BURNING RUBBER OR PLASTIC. F/A REPORTED, BEFORE DEPARTURE COFFEE WAS SPILLED IN THE COFFEEMAKER. 2 L 7 2 4F RT A21EA 2007100100065 20071001 00065 NM 2007 10 1 DHLA200700046 1 20070926 A 3350 LIGHT BOEING 727 727264 138408M NM CABIN DISLODGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 765AT 23014 FOUND UPPER EMERG EXIT LIGHT DISLODGED. RE INSTALLED UPPER EMERGENCY EXIT LIGHT PER MM 33-50-00. 2 L 7 3 4F A3WE 2007100100075 20071001 00075 EU 2007 10 1 07FDEA04277 1 20070925 A 5320 A53973054200 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 DAMAGED FITTING BETWEEN FRAME 63-63A, STGR 43 RT, CARGO DOOR AREA. REPLACEMENT OF FITTING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100080 20071001 00080 NM 2007 10 1 07FDEA04282 1 20070925 A 5542 SKIN BOEING 727 727227 1384078 NM RUDDER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 VERTICAL STAB, UPPER RUDDER TAB HAS SPOT OF SKIN DISBOND, 2" BY 3" AREA AT 25" UP FROM LWR END 1" AFT OF FWD EDGE. REPA IRED UPPER RUDDER TAB REF SRM 51-40-20 PAR 7, 8, 14, 15, 19-22 AND APPLIED EXTERIOR PROTECTIVE FINISH REF MM 51-20-151-7 . 2 L 7 3 4F A3WE 2007100100081 20071001 00081 NM 2007 10 1 07FDEA04283 1 20070925 A 5542 657278830 SKIN BOEING 727 727227 1384078 NM RUDDER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 VERTICAL STAB UPPER RUDDER TAB UPPER END POTTING BROKEN OPEN AND SKIN DISBONDED ON BOTH SIDES, LEFT SIDE 6-12" FWD OF T/ E, RIGHT 5-13" AND DOWN 4" ALSO T/E TIP CORNER OPEN. REPAIRED UPPER RUDDER TAB ON LEFT AND RIGHT SIDES REF SRM 51-40-20 PAR 7, 8, 14, 15, AND 20-22, TAP CHECKS GOOD COOK TICKET ATTACHED, "THIS IS CLASSIFIED AS A MAJOR REPAIR". 2 L 7 3 4F A3WE 2007100100085 20071001 00085 NM 2007 10 1 07FDEA04287 1 20070925 A 5311 651593731 FRAME BOEING 727 727227 1384078 NM ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 PREVIOUS DAMAGE: LT FUSE (SAT 680) STR 14L, FRAME ABOVE 14L HAS DEEP GOUGES BLENDED DAMAGED AREA ORIGINAL MATERIAL .045" MATERIAL LOSS .015" MATERIAL REMAINING .030" AND IS OUT OF LIMITS REF SRM 53-10-1. REMOVED DAMAGED SECTION, FABRICATED REPAIR SPLICE. INSTALLED NEW FRAME SECTION AND FRAME REPAIR SPLICE REF EA NR 7-5310-113101-FUSELAGE-MAIN FRAME. 2 L 7 3 4F A3WE 2007100100088 20071001 00088 NM 2007 10 1 07FDEA04189 1 20070921 A 5313 AEA75452 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 RT WING TO FUSELAGE BODY FAIRING ENCLOSED AREA FOUND LONGERON 28 AT STA 1289 WITH CORROSION. 10-04-07 CORROSION REMO VED AS PER SRM 51-31-012 VOLUME II. HOLES PICKED UP ON NEW LONGERON AND INSTALLED AS PER SRM 51-31-01 VOLUME II. REP IAR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007100100089 20071001 00089 EU 2007 10 1 07FDEA04190 1 20070923 A 2780 SHAFT AIRBUS 300 A300B4622R 3930312 EU RT WING SLAT FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 730FD 659 ON DEPT 18L(KMEM) RECEIVED ECAM FOR SLATS SYS 1/2 FAULT W/CORRESPONDING SLAT LIGHT ON FWD PANEL. RECYCLE UNSUCCESSFUL. FOLLOWED QRH. NORMAL LANDING LNG GW 281.0. VERIFIED LEFT AND RIGHT WING SLATS WERE FULL UP AT "0" DEGREES POSITION IN REF TO AMM 27-80-00-3. INSTALLED RT WING SLAT TRANSMISSION SHAFTS. PERFORMED OPERATIONAL BITE TEST OF FLAP/SLATS. NO FAULTS. NOTED ON EITHER SFCC. OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2007100100090 20071001 00090 EU 2007 10 1 07FDEA04191 1 20070924 A 5313 A53773455 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 HEAVY CORROSION ON STRINGER 44 LHS, BETWEEN FRAME 20-23. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007100100091 20071001 00091 EU 2007 10 1 07FDEA04192 1 20070924 A 5311 A53778969200 FRAME AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 HEAVY CORROSION ON FRAME 37 BETWEEN STRG 54 LT AND 53 RT. FRAME SPLICE REPAIR PERFORMED IAW SRM 53-10-13/FIG 203. 2 L 7 2 4F RT A35EU 2007100100094 20071001 00094 EU 2007 10 1 07FDEA04195 1 20070924 A 5320 A53810967200 DIAPHRAGM AIRBUS 300 A300B4605R 3930308 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 733FD 715 FOUND DENTS AND NICKS IN DIAPHRAGM C 48-49, TR2-3 LT. REPAIR PERFORMED BY CUT OUT DAMAGED AREA AND INSTALLING A DOUBLER IAW EA 6-5315-112500 AND RAS 053448/012/2007 ISS A . 2 L 7 2 4F RT A35EU 2007100100098 20071001 00098 EU 2007 10 1 07FDEA04199 1 20070924 A 5754 A57863251160 SKIN AIRBUS 300 A300B4622 3930401 EU ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND ABRASION AT SLAT NR 1 LT ON TRAILING EDGE LOWER SKIN RIB 21. REPAIR PERFORMED BY INSTALLING A EXTERNAL DOUBLER AN D BONDING THE INTERNAL STRUCTURE IAW EA 6-5742-70335 AND RAS/FOK172/2003 ISS A. 2 L 7 2 4F RT A35EU 2007100100099 20071001 00099 NM 2007 10 1 F3LA200700249 1 20070925 A 4940 270450604 STARTER AIRBUS A319 A319111 3930336 NM APU SEIZED A F3LA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 03 939FR 2448 MAINTENANCE REPORTED ELECTRICAL SMOKE ODOR IN APU COMPARTMENT AFTER APU AUTO SHUTDOWN. INSPECTED APU COMPARTMENT IAW TS M 24-00-00-810-823 AND IDENTIFIED ODOR WAS FROM STARTER. FOUND APU SENSE WIRE HEAT DAMAGED AND HEAT SHRINK ON POSITIVE WIRE DAMAGED. STARTER WAS SEIZED. REMOVED AND REPLACED APU STARTER IAW AMM 49-42-51-000-004 AND AMM 49-42-51-400-004. WIRE DAMAGED FROM HEAT NEEDS TO BE REPAIRED/REPLACED PER ESPM. APU SYSTEM WAS DEACTIVATED IAW MEL 49-10-01A, CONTROL N UMBER 1029980, AND TRANSFERRED TO SUPPLEMENTAL SHEET. 2 L 7 2 4F RT A28NM 2007100100100 20071001 00100 EU 2007 10 1 07FDEA04200 1 20070924 A 5542 A554715000 SKIN AIRBUS 310 A310324 3930206 EU RUDDER DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FOUND DAMAGED AREA ON RUDDER, TRAILING EDGE, LOWER SIDE. REPAIR PERFORMED BY LAMINATING THE EDGE IAW SRM 55-41-12/FIG 2 08A WITH GLASFABRIC. 2 L 7 2 4F RT A35EU 2007100100102 20071001 00102 EU 2007 10 1 07FDEA04202 1 20070924 A 5754 A53510322209 BEAM AIRBUS 300 A300B4622 3930401 EU DRUEGER FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND CORROSION AT BEAM C 38-39 KRUEGER FLAP FWD FAIRING RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 57-45-11. 2 L 7 2 4F RT A35EU 2007100100103 20071001 00103 EU 2007 10 1 07FDEA04203 1 20070924 A 5754 SKIN AIRBUS 300 A300B4622 3930401 EU NR 1 SLAT DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND ABRASION AT SLAT NR 1 RT TRAILING EDGE LOWER SKIN RIB 21 REPAIR PERFORMED BY INSTALLING AN EXTERNAL DOUBLER AND BO NDING THE INTERNAL STRUCTURE IAW EA 6-5742-7034 AND RAS/FOK/173/2003 ISS A. 2 L 7 2 4F RT A35EU 2007100100106 20071001 00106 EU 2007 10 1 07FDEA04206 1 20070924 A 5411 A54611222500 SPAR AIRBUS 300 A300B4622 3930401 EU LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND AT LT PYLON SPAR RIB 18 AT PYLON TO WING FITTING CORROSION. REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW E A 6-5440-70338 AND RAS 027276/007/2003. 2 L 7 2 4F RT A35EU 2007100100108 20071001 00108 EU 2007 10 1 07FDEA04207 1 20070924 A 5542 SKIN AIRBUS 300 A300B4622 3930401 EU ZONE 300 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND DELAMINATION AT RUDDER SIDE PANEL IN THE AREA OF HINGE ATTACHMENT FITTINGS, LT: BR1, BR4, BR5, BR6, BR7 RT: BR1- BR6 REPAIR PERFORMED IAW SRM 55-41-12 FIG 216. 2 L 7 2 4F RT A35EU 2007100100110 20071001 00110 EU 2007 10 1 07FDEA04209 1 20070924 A 5315 A53778807202 FLOORBEAM AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND CORROSION AT TOP CAP BEAM UPPER FLANGE 27. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10 2 L 7 2 4F RT A35EU 2007100100112 20071001 00112 EU 2007 10 1 07FDEA04211 1 20070924 A 5311 A52271028203 FRAME AIRBUS 310 A310324 3930206 EU ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CRACKED VERTICAL FRAME SEGMENT 3.1 ON RT EMERGENCY EXIT DOOR BETWEEN FRAME 42A-43A, BETWEEN BEAM 5 AND 6. REPLACEMENT O N FRAME SEGMENT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007100100113 20071001 00113 EU 2007 10 1 07FDEA04212 1 20070924 A 5312 BULKHEAD AIRBUS 300 A300B4622 3930401 EU ZONE 400 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND DENTS AT PRESSURE BULKHEAD FLOOR STRUCTURE C 49-50 (WITH CRACK 2MM) AND C 50-51 AT TR 4-5 LT ; C 52-53 AT TR 2-3 L T, C 48-49 AT TR 4-5 RT. REPAIR PERFORMED BY INSTALLING A DOUBLER AT TR 4-5 LT, C49-50 AND LET THAT DENTS AT THE OTHER AREAS AS IT IAW EA 6-5315-70336 AND RAS/AS/0282/2003 ISS A. 2 L 7 2 4F RT A35EU 2007100100115 20071001 00115 EU 2007 10 1 07FDEA04214 1 20070924 A 5315 A53778807202 FLOORBEAM AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND CORROSION AT FLANGE OF TOP CAP BEAM C 32. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 2007100100117 20071001 00117 EU 2007 10 1 07FDEA04216 1 20070924 A 5755 SKIN AIRBUS 310 A310324 3930206 EU ZONE 500 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FOUND EXISTING REPAIRS ON THE STOP-SURFACES ON SPOILER NR 4 LT, MONEL RIVETS NSA5414-32 AND WASHERS WERE USED INSTEAD OF NSA1919-M FASTENERS ON TOP SKIN RIB 01 AND 19, DELAMINATION ON TOP SKIN AT STOP-FITTING AREAS. REPAIR PERFORMED BY FAB RICATE BOND AN ANGLE CARBON PRE-CURED DOUBLER AND INSTALLING BLIND RIVETS MONEL NSA1919-M04S-W ON DELAMINATED AREAS AT TOP SKIN IAW EA 6-5773-82925 AND RAS 038772/012/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100100118 20071001 00118 EU 2007 10 1 07FDEA04217 1 20070924 A 5755 SKIN AIRBUS 310 A310324 3930206 EU ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FOUND EXISTING REPAIRS ON THE STOP-SURFACES ON SPOILER NR 4 RT, MONEL RIVETS NSA5414-32 AND WASHERS WERE USED INSTEAD OF NSA1919-M FASTENERS ON TOP SKIN RIB 01 AND 19, DELAMINATION ON TOP SKIN AT STOP-FITTING AREAS. REPAIR PERFORMED BY FAB RICATE BOND AN ANGLE CARBON PRE-CURED DOUBLER AND INSTALLING BLIND RIVETS MONEL NSA1919-M04S-W ON DELAMINATED AREAS AT TOP SKIN IAW. EA 6-5773-82925 AND RAS 038772/012/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007100100119 20071001 00119 EU 2007 10 1 07FDEA04218 1 20070924 A 5313 A53773634202 STRINGER AIRBUS 300 A300B4622 3930401 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND OLD STRINGER REPAIRS C20-21, P 53 LT NOT COMPATIBLE WITH P TO F CONVERSION. STRINGER REPAIR RENEWED IAW SRM 53-10 -14 FIG 201. 2 L 7 2 4F RT A35EU 2007100100120 20071001 00120 2007 10 1 F3LA200700248 4 20070922 A 2565 GIRT BAR AIRBUS A319 A319111 3930336 NM L1 DOOR SLIDE OUT OF POSITION A F3LA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 03 921FR 2010 FLIGHT CREW REPORTED L1 DOOR SLIDE WOULD NOT ARM. REMOVED L1 DOOR GIRT BAR AND REPOSITIONED MOORING LINE. REINSTALLED L1 DOOR GIRT BAR. PERFORMED OPS CHECK IAW 25-62-44-000-002. CHECKED GOOD. 2 L 7 2 4F RT A28NM 2007100100122 20071001 00122 EU 2007 10 1 07FDEA04220 1 20070924 A 5313 A53778456 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORROSION ON STRINGER 43 LT AT FRAME 38. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007100100123 20071001 00123 NM 2007 10 1 07FDEA04221 1 20070924 A 5753 ARC24443 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 LT WING INBOARD FLAP LOWER SEGMENT FOUND WITH SEVERAL DENTS. 10-05-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 2 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007101000091 20071010 00091 EA 2007 10 10 S9BA200700016 1 20070917 A 5554 C6TFM102931 ATTACH BRACKET DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA RUDDER CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 19820 125 573 RUDDER MID HINGE ATTACHMENT BRACKET CORRODED. REMOVED AND REPLACED RUDDER MID HINGE ATTACHMENT BRACKET. 1 H 7 2 3T 4 T RT A9EA E4EA 2007101000098 20071010 00098 NE 2007 10 10 HEER117365 2 20070917 A 7200 3066T90G02 ENGINE SKRSKY S92 S92A NE GE CT7TS CT78A 30136 NE NR 2 INOPERATIVE B HEER O OTHER O OTHER TX TAXI/GRND HDL 1 SW 03 392PH 2111 920015 GEE947245 ON THE FOURTH START OF THE DAY, THE NR 2 ENGINE WOULD NOT TURN OVER WHEN THE STARTER WAS ENGAGED. REMOVED THE STARTER, APPLIED TORQUE TO THE A AXIS DRIVE, COULD NOT ROTATE THE GEARBOX SECTION OF THE ENGINE. REMOVED AND REPLACED THE NR 2 E NGINE. 2 G 7 2 4U 4 U R00024BO E8NE 2007101000102 20071010 00102 NM 2007 10 10 PIDR07006 1 20070919 A 5330 SKIN BOEING 737 737300 1384610 NM BS 986 CORRODED B PIDR K NONE O OTHER IN INSP/MAINT 1 SO 05 XAUGL 22958 DURING MAINTENANCE CHECK, NOTED CORROSION ON STRINGER AND FUSELAGE SKIN AT BS 986.5 AND LBL 4. REMOVED CORROSION FR OM SKIN, WITHIN LIMITS OF SRM 53-00-01. REPLACED STRINGER SECTION IAW SRM 53-00-03 REPAIR 1. 2 L 7 2 4F RT A16WE 2007101000103 20071010 00103 NM 2007 10 10 PIDR07007 1 20070919 A 5330 SKIN BOEING 737 737300 1384610 NM BS 757 CRACKED B PIDR K NONE O OTHER IN INSP/MAINT 1 SO 05 XAUGL 22958 DURING MAINTENANCE CHECK, NOTED CRACK AT BS 757 AT STR 21RT. DUE TO PROXIMITY TO ADJACENT REPAIRS, REPLACED SKIN PANEL FROM BS 727C +10 TO BS 767 AND STR 20RT TO STR 25RT IAW EA 53-252. 2 L 7 2 4F RT A16WE 2007101000104 20071010 00104 EU 2007 10 10 RMXA2007 1 20070920 A 5302 11203025211 SKIN PANEL BOLKMS BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1E 60034 NE TAILBOOM CRACKED E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 317MC 10996 7505 DURING A SCHEDULED INSPECTION, SEVERAL CRACKS WERE FOUND ON THE TAILBOOM TOP SKIN PT NR1120-32052.11 AROUND THE ATTACHIN G RIVET HOLES ON THE AFT LT EDGE. 1 G 7 2 3U 3 U NC H13EU E19EU 2007101000109 20071010 00109 NM 2007 10 10 PIDR07008 1 20070921 A 5522 SKIN BOEING 737 737300 1384610 NM LT ELEVATOR PUNCTURED D PIDR K NONE O OTHER IN INSP/MAINT 1 SO 05 XAUGL 22958 DURING MAINTENANCE CHECK, NOTED PUNCTURE DAMAGE TO LOWER SURFACE OF LT ELEVATOR APPROXIMATELY EIGHTEEN INCHES OB OF THE TAB. REPAIRED DAMAGED AREA IAW SRM 51-70-17. 2 L 7 2 4F RT A16WE 2007101000116 20071010 00116 NM 2007 10 10 BJ6A200712901 1 20070914 A 3350 D71702001 CHARGER BOEING 737 7377BC 1384509 NM CFMINT CFM56 CFM567B26US NE EMERGENCY LIGHTS FAILED E BJ6A K NONE L NO TEST IN INSP/MAINT 1 EA 63 129QS 1957 30329 DURING GROUND OPERATIONAL TEST OF THE EMERGENCY LIGHTING SYSTEM, SEVERAL EMERGENCY LIGHTS AT THE AFT LAVATORY AREA AND L 2 DOOR FAILED TO ILLUMINATE. REPLACED EMERGENCY BATTERY CHARGER TO RESTORE NORMAL OPERATION. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007101000118 20071010 00118 CE 2007 10 10 DXTA200702497 1 20070925 A 2797 S23494 CONNECTOR CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE SPEED BRAKES CORRODED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 647QS 2616 5605547 NO TAKEOFF ANNUNCIATOR AND AURAL WARNING TRIGGERED UPON APPLICATION OF TAKEOFF POWER. ABORTED TAKEOFF. REPLACED SPEED BRAKE CONNECTOR IAW MM 20-10-04. SPEED BRAKES OP'S OK IAW MM 27-61-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007101000122 20071010 00122 CE 2007 10 10 DXTA200702501 1 20070926 A 3240 BRAKE ASSY CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 639QS 5605139 ON LANDING, LT BRAKE PEDAL WENT TO THE FLOOR WHEN PRESSURE APPLIED WITH NO LT SIDE BRAKING. AC STOPPED WITH NO INCIDENT AND AFTER PUMPING BRAKES REGAINED MINIMAL PRESSURE ON LT SIDE. DID NOT USE EMERGENCY BRAKING. NOT REQUIRED TO STOP AIRCR AFT. CONFIRMED DISCREPANCY. PERFORMED BRAKE BLEED PROCEDURES ON MAIN BRAKES. PERFORMED TAXI CHECK WITH NO DISCREPANCI ES NOTED. WORK PERFORMED IAW MM 32-40-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007101000124 20071010 00124 SO 2007 10 10 C2XA07RI084 1 20070924 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14974 145161 EWR - DURING ROUTINE MAINTENANCE, MX FOUND FIRST EMERGENCY LIGHT STRIP INOPERATIVE. MX REMOVED AND REPLACED EMERGENCY L IGHT INVERTER IAW EMB145 AMM 33-50-11 AND PERFORMED OPERATIONAL SUCCESFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007101000125 20071010 00125 CE 2007 10 10 092607N324CS1 1 20070926 A 3260 MS25237327 BULB CESSNA 500 550 2076604 CE PWA 530 PW530A NE MLG INDICATOR INOPERATIVE E Z5FA O OTHER P NO WARNING INDICATION AP APPROACH 1 EA 63 324CS 5501059 UPON APPROACH, CREW NOTICED NO RT GEAR DOWN INDICATION AFTER GEAR EXTENSION. CREW FOLLOWED AFM ABNORMAL PROCEDURES. NO RT GEAR DOWN IN TEST. CREW ELECTED TO DECLARE EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL FOUND BULB OUT FOR RT GEAR DOWN. REPLACED BULB, RESET EMERGENCY CONTROL, SERVICED GEAR BLOWDOWN BOTTLE AND CYCLED GEAR. OPS CH ECK SATISFACTORY. 1 L 7 2 4F 4 F A22CE E00053EN 2007101000126 20071010 00126 SO 2007 10 10 C2XA07RI085 1 20070919 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14974 145161 EWR - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY LIGHT FLOOR STRIPS 6, 7 AND 8 INOPERATIVE. MX REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW EMB145 AMM 33-50-11 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RE TURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007101000130 20071010 00130 NM 2007 10 10 UPS07M50741 1 20070808 A 5720 STIFFENER DOUG MD11 MD11F 3023600 NM RWS 568 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C RIGHT WING L/E COMPARTMENT AT STA XORS 568 APPROX FOUND UPPER STIFFENER CRACKED AS MARKED. CRACKED ST IFFENER & ATTACH PARTS REMOVED. NEW STIFFENER FABBED USING MAT'L 7075-0-0.071" PER DOUGLAS DWG ARB3954. STIFFENER HEAT TREATED PER DPS 7.00-1 & HARDNESS VALUES HRB 84.0 PER DPS 1.02-3. NEW STIFFENER HOLES P/UP, REPROTECTED & PAINTED. NE W STIFFENER INSTALLED AS PER SRM 51-33-01 VOL II REV 38 & SRM 51-35-01 VOL II REV 38. 2 L 7 3 4F RT A22WE 2007101000132 20071010 00132 NM 2007 10 10 UPS07M50743 1 20070730 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT BORE LEFT NR 17 FOUND WITH CORROSION. CORROSION AT BARREL NUT BORE REMOVED PER SRM 51-21-01 VII R38. BORE BOTTOM RMN BLEND OUT 0.030" DEEP. REAMED TO 1.067" DIA & RMN BLEND OU T 0.070" DEEP, EXCEED LIMITS. BARREL NUT BORE, BLEND OUT VOID & BOTTOM PERIPHERY RADIUS, SMOOTHEN & PROTECTED. SLEEVE BUSHING FAB, PROTECTED & INSTALLED. REPAIR C/O AT BARREL NUT BORE NR 17 LT ACCEPTABLE PER EN1477-07. 2 L 7 3 4F RT A22WE 2007101000152 20071010 00152 EU 2007 10 10 2007UALA03580 1 20070904 A 5270 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO DOOR WARNING LIGHT A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 414UA 472 RTFL DUE TO AFT CARGO DOOR INDICATION. DUE TO HISTORY OF THIS DOOR, REPLACED DOOR HANDLE SPRING, INSPECTED AFT CARGO DO OR LATCHING MECHANISM AND PROX SENSORS, NO DEFECTS NOTED. CHECKED PROX SENSOR 34WV FOR CONDITION AND CLEANED SENSOR. O PERATED DOOR AND LATCHING MECH POSITION CORRESPONDS WITH ECAM INDICATION. DISCREPANCY HAS NOT REPEATED SINCE SEPT 4. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101000207 20071010 00207 SO 2007 10 10 SWIA200718722 1 20070923 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DISCHARGED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 232SW 8503 8503 120306 FLT 3708 - SEVERAL EMERGENCY LIGHTS IN THE CABIN ARE INOP. REPLACED AFT ELBP IAW 33-50-02. LIGHTING OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2007101000208 20071010 00208 EA 2007 10 10 SWIA200718723 1 20070925 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 915EV 7754 FOUND FORWARD CEILING EMERGENCY POD LIGHT INOP. RELAMPED FORWARD CEILING EMERGENCY LIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007101000209 20071010 00209 SO 2007 10 10 SWIA200718724 1 20070802 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 213SW 120277 FOUND AT C-CHECK, CORROSION AT PAX DOOR AREA ON FLOORBEAM. REMOVED AND REPLACED OMEGA BEAM AND BUTTSTRAP IAW SRM 51-10- 02. 2 L 7 2 4T RT A31SO 2007101000210 20071010 00210 SO 2007 10 10 SWIA200718725 1 20070802 A 5313 STRINGER EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 213SW 120277 FOUND AT C-CHECK, STRINGER CORRODED NEAR PAX DOOR AFT ACTUATOR ATTACH POINT. REPAIRED STRINGER SECTION AT PAX DOOR AREA IAW SRM 120 53-10-03 PG 201. 2 L 7 2 4T RT A31SO 2007101000211 20071010 00211 EA 2007 10 10 SWIA200718726 1 20070923 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 954SW 7815 FLT 5859 - FOUND EMERGENCY EXIT LIGHT IN GALLEY IS INOP. RELAMPED GALLEY EMERGENCY EXIT LIGHT IAW 33-41-01. 2 L 7 2 4F RT A21EA 2007101000212 20071010 00212 SO 2007 10 10 SWIA200718727 1 20070802 A 5310 WINDOW POST EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 213SW 120277 FOUND AT C-CHECK, LEFT WINDSHIELD SIDE ATTACHMENT POST APPEARS TO BE CRACKED. REPLACED LOWER WINDSHIELD STRUCTURE IAW S RM 120 51-10-02 PG 3 SEC 3A. 2 L 7 2 4T RT A31SO 2007101000213 20071010 00213 NM 2007 10 10 DU4R2007171 1 20070905 A 5414 SKIN BOEING 757 757232 1384965 NM ZONE 400 DAMAGED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 642DL 23996 NR 1 PYLON I/B SKIN HAS TEMPORARY REPAIR. ACCOMPLISHED PERMANENT REPAIR TO NR 1 PYLON O/B SKIN IAW DELTA EA 06-074338-0 3 REV B DATED 01/30/2003 IAW DELTA ERA 454288-14 REV ORIG AND B757 SRM 51-00-00D PG 1 APPROVED PER 14 CFR 121.379(B). 2 L 7 2 4F RT A2NM 2007101000214 20071010 00214 NM 2007 10 10 HALA0700422 1 20071001 A 3150 WARNING LIGHT BOEING 767 76733A 1385209 NM APU BATTERY FALSE ACTIVATION A HALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, STATUS MSG APU BAT CHARGER DISPLAYED AND APU BAT DISCH LT EXTINGUISHED. REF M/M 24-31-01,24-3 1-02 OPS OF BATTERY/CHARGER OK MESSAGE CLEARED, NO DEFECTS NOTED. 2 L 7 2 4F RT A1NM 2007101000215 20071010 00215 NM 2007 10 10 HALA0700423 1 20071001 A 2613 DETECTION SYS BOEING 767 7673G5 1385126 NM PWA 4060 PW4060 52119 NE RT ENGINE MALFUNCTIONED A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 584HA 24258 ETOPS SIGNIFICANT SYSTEM, ON ETOPS CHECK FOUND EICAS MSG "R ENG OH LP 1". TROUBLESHOOT PER FIM 26-11-00 SWAPPED OVERHEA T CARD M689 AND M687 CONDITION SAME RE-INSTALLED OVERHEAT CARD TO ORIGINAL POSITION REPLACED RT ENGINE OVERHEAT DETECTOR S PER AMM 26-11-02, OPS CK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101000221 20071010 00221 EU 2007 10 10 07FDEA04462 1 20071002 A 5210 A52175271203 CHANNEL AIRBUS 310 A310324 3930206 EU CREW DOOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 LT AFT CREW DOOR LOWER CHANNEL HAS A NOTCH OUT OF LIMIT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007101000234 20071010 00234 EU 2007 10 10 07FDEA04476 1 20071002 A 5313 STRINGER AIRBUS 310 A310222 3930315 EU AFT CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 FOUND AFT CARGO PIT AT FRAME 58 S-57 IS CORRODED. 10-16-07 REMOVED STRINGER IAW A310 SRM 51-72-10 PARA 5, RECIEVED NEW STRINGER, TRANSFERRED REPAIR PART HOLES IAW A310 SRM 53-10-14 PARA 2, INSTALLED REPAIR PARTS IAW A310 SRM 53-10-14 PARA 4, APPLIED TOP COAT TO THE FASTNERS IAW A310 AMM 51- 25-10, REMOVED AND REISTALLED TEMP SENOR COVER IAW A310 SRM 5 1-40-21 PARA 2. 2 L 7 2 4F RT A35EU 2007101000235 20071010 00235 EU 2007 10 10 07FDEA04477 1 20071002 A 5322 SHEAR TIE AIRBUS 310 A310222 3930315 EU AFT CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 AFT CARGO PIT AT FRAME 54.1 BETWEEN SHEARTIE IS CORRODED AND CRACKED S-51L TO S-52L. 10-29-07 REMOVED AND REPLACED SHEAR TIE AT FRAME 54.1 BETWEEN SRINGER 51L AND 52L IAW FEDEX A310 SRM 51-40-21 PG 30. 2 L 7 2 4F RT A35EU 2007101000236 20071010 00236 SO 2007 10 10 SIMA200727602 1 20071002 A 2131 22250N030301 CONTROLLER EMB 145 EMB145LR 3260212 SO CABIN PRESSURE FAILED A SIMA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 21 615AE 145087 AT 36000 CABIN ALTITUDE BEGAN TO CLIMB AFTER CONTROLLER WAS WORKING FOR ONE + HOURS. RATE OF CLIMB SUCH THAT HABITUAL L EVELS COULD NOT BE MAINTAINED W/O DESCENT TO LOWER ALT, AUTO SYSTEM WORKED GOOD AND SCHEDULED DIFFERENTIALS AND ALTS MAI NTAINED AS DESIGNED. REMOVED AND REPLACED DIGITAL CONTROLLER AS PER EMB AMM 21-31-01. OPS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007101000237 20071010 00237 SO 2007 10 10 SIMA200727601 1 20071002 A 2730 TRIM SYSTEM EMB 145 EMB145LR 3260212 SO MAIN PITCH INOPERATIVE A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 685AE 14500836 AIRCRAFT RETURNED TO FIELD FOR MAIN PITCH TRIM INOP. RESET SYSTEM AND OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007101000238 20071010 00238 2007 10 10 SIMA200727603 4 20071002 A 3442 70214550601 TRANSCEIVER EMB 145 EMB145LR 3260212 SO WX RADAR INOPERATIVE A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 624AE 145111 EN ROUTE WEATHER RADAR TESTED GOOD BUT WEATHER RADAR WOULD NOT PAINT. REMOVED AND REPLACED WEATHER RADAR RT UNIT IAW AM M TASK 34-42-01-000- AND TASK 34-42-01-1100-801-A. PERFORMED OPS CK OF WEATHER RADAR IAW AMM 34-42-00-700-801. AIRCRA FT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007101000239 20071010 00239 NM 2007 10 10 QXEA200701507 1 20071002 A 2430 400SG163Q GENERATOR BOMBDR DHC8 DHC8402 1390042 NM NR 1 INOPERATIVE A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 415QX 49 49 4081 SEA - ONFLIGHT 2344, ON CLIMB, GOT A NR 1 DC GENERATOR CAUTION LIGHT. AFTER RUNNING THE CHECKLIST IT STAYED ON. MAINTE NANCE REMOVED AND REPLACED NR 1 DC GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007101000240 20071010 00240 NM 2007 10 10 DLM90071273 1 20070901 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FS 598-655 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 PAX CABIN LT CUSP WEB IS CORRODED AT FS 598-655. REMOVED AND REPLACED WITH NEW WEB IAW MD-90 SRM 51-10-05 AND 51-30-02 ON N/R 63156 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007101100001 20071011 00001 NM 2007 10 11 AMTA200700442 1 20070919 A 3350 BATTERY PACK BOEING 737 73783N 13844HI NM EMERGENCY LIGHTS INOPERATIVE A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 318TZ 28247 EMERGENCY LIGHTS (INTERIOR) BY 1L DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. IAW AMM 33-51-06-960-805. OPS CHECK GOOD. (K) 2 L 7 2 4F RT A16WE 2007101100009 20071011 00009 2007 10 11 AMTA200700441 4 20070916 A 3460 4052506955 COMPUTER BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE FLT MANAGE UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 560TZ 33525 RT FMC FAILED. REPLACED RT FMC IAW AMM 34-61-01-4. CROSS LOADED SOFTWARE AND NAV DATA TO CURRENT CYCLE. OPS CHECK, OK . (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007101100015 20071011 00015 NM 2007 10 11 DLM90071290 1 20071001 A 5230 SKIN DOUG MD90 MD9030 3023690 NM CARGO DOOR SCRATCHED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 MULTIPLE SCRATCHES ON FWD CARGO DOOR OUTER SKIN. REPAIRED FWD CARGO DOOR IAW MD-90 SRM 52-01-01 FIG 3 VOL 1 ON N/R 8000 -0054 ON HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007101100023 20071011 00023 WP 2007 10 11 AALA20071843 1 20071003 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 433AA 49451 SDF - AIRCRAFT BATTERIES AND EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. CHARGED AIRCRAFT BATTERY AND REPLACED BATTE RY PACK FOR EMERGENCY LIGHTS AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007101100027 20071011 00027 NM 2007 10 11 AALA20071835 1 20070930 A 3350 1722331 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 372AA 25199 JFK - EMERGENCY LIGHT AT SEAT ROW 2HJ INOPERATIVE. REPLACED CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 2HJ. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007101100036 20071011 00036 WP 2007 10 11 070162 1 20070926 A 3350 408822101 BATTERY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 878GA 53487 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007101100041 20071011 00041 SO 2007 10 11 SIMA200727703 1 20070929 A 3610 E3548207 BUSHING EMB 145 EMB145 3260210 SO RAM AIR VALVE UNKNOWN A SIMA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SW 21 612AE 145079 UNUSUAL AIRFRAME VIBRATION IN FLIGHT ALONG THE LONGITUDINAL AXIS. REMOVED AND REPLACED RIGHT RAM AIR VALVE SHAFT BUSHIN GS IAW EMB CMM 21-25-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007101100042 20071011 00042 NM 2007 10 11 QXEA200701508 1 20071004 A 2611 SMOKE DETECTOR BOMBDR DHC8 DHC8402 1390042 NM CARGO BAY FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 404QX 4046 SEA FLIGHT NR 2324: NR 2 AFT BAGGAGE SMOKE DETECTOR FAILS TO TEST. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE C/W OPS TES T OF THE AFT BAGGAGE SMOKE DETECTORS IAW AMM 26-12-06-710-801. OPS CHECK GOOD. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007101100095 20071011 00095 EU 2007 10 11 07FDEA04501 1 20071005 A 5730 A57340084203 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION ON AFT RUN OUT OF TOP SKIN PANEL NR 2, RT WING WITH ADDITIONAL CRACK FINDING AFTER CORROSION REMOVAL REP AIR PERFORMED BY CUT OUT THE DAMAGE AND INSTALLING A REPAIR DOUBLER IAW EA 6-5720-106529 AND RAS/BAE/1005083/2007 ISS A. 2 L 7 2 4F RT A35EU 2007101100101 20071011 00101 WP 2007 10 11 AALA20071848 1 20071004 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMEGENCY LGIHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7535A 49989 LGA - EMERGENCY LIGHTS AT TAIL CONE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT TAIL CONE. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007101100103 20071011 00103 NM 2007 10 11 AALA20071850 1 20071004 A 3350 LENS BOEING 737 737823 13844BZ NM EMEGENCY LGIHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 972AN 30097 LGA - EMERGENCY LIGHT AT SEAT ROW 15DEF MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 15DEF. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007101100105 20071011 00105 NM 2007 10 11 AALA20071852 1 20071004 A 3350 OL3071BPEGPL BULB BOEING 737 737823 13844BZ NM EMEGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 972AN 30097 LGA - EMERGENCY LIGHT AT SEAT ROW 15DEF MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 15DEF. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007101100106 20071011 00106 NM 2007 10 11 AALA20071853 1 20071004 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AA 25201 MIA - EMERGENCY LIGHT AT OVERHEAD COCKPIT ENTRY EXIT SIGN INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT O VERHEAD COCKPIT ENTRY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007101100111 20071011 00111 NM 2007 10 11 HALA0700427 1 20071003 A 2841 H61057AA07 PROCESSOR BOEING 767 767332 1382001 NM FUEL QTY MALFUNCTIONED A HALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 594HA 23275 DURING CLIMB-OUT REC'D EICAS " LOW FUEL" MESSAGE. RT FUEL QTY IND BLANK ALONG WITH TOTALIZER QTY, WAITED ALMOST 10 MINS FOR POSSIBLE RESET, BUT THE DISPLAY REMAINED BLANK UNTIL JUST BEFORE DESCENT ON TURNBACK. ACCOMP FUEL QTY BITE TEST. THE FOLLOWING FAULTS WERE NOTED: CHANNEL 1-C1, C7, C6, 31-39, 81-94, 74 AND CHANNEL 2 C5, C7, C6, 31-39, 81-94, 79 AFTER RESETTING PER FIM 28-41-00 TASK 101 HARD FAULT 31 WAS THE ONLY FAULT TO REMAIN. ACCOMP FIM 28-41-00 TABLE 126 GO TO ST EP 1 AND VERIFIED NO WATER IN THE TANK. PRIOR TO RESPOTTING ACFT TO HARDSTAND ALL INDICATIONS NORMAL. DURING TOW TO HA RDSTAND RT QTY WENT BLANK AGAIN. AFTER A/C PARKED AT HARDSTAND ALL INDICATION NORMAL AGAIN. BITE CHECK CARRIED OUT AGA 2 L 7 2 4F RT A1NM 2007101100115 20071011 00115 EU 2007 10 11 1218 1 20071006 A 5347 S5337500121602 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 LEFT INBOARD SEAT TRACK BETWEEN FRAMES 13 AND 23 CORRODED. CORROSION WAS REMOVED AND TRACK WAS FOUND TO BE OUT OF LIMIT S PER MANUFACTURES STRUCTURAL REPAIR MANUAL. SEAT TRACK WAS REPLACED. 2 H 7 2 4T RT A53EU 2007101100116 20071011 00116 EU 2007 10 11 1219 1 20071006 A 5347 S5337500120002 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 RIGHT OUTBOARD SEAT TRACK BETWEEN FRAMES 13 AND 23 CORRODED. CORROSION WAS REMOVED AND TRACK WAS FOUND TO BE OUT OF LIM ITS PER MANUFACTURES STRUCTUAL REPAIR MANUAL. SEAT TRACK WAS REPLACED. 2 H 7 2 4T RT A53EU 2007101100121 20071011 00121 NM 2007 10 11 F3LA200700260 1 20070927 A 5755 PLATE AIRBUS A319 A319111 3930336 NM LT WING GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED GOUGES ON LT WING NR 3 SPOILER ANTI-ROTATION LUG SURFACES. MACHINED ANTI-ROTATION FLAT, PERFORMED HFEC, AND BONDED REINFORCING PLATE IAW EA NR A9-57R-12172. 2 L 7 2 4F RT A28NM 2007101100123 20071011 00123 NM 2007 10 11 F3LA200700262 1 20070927 A 5755 LUG AIRBUS A319 A319111 3930336 NM NR 4 SPOILER GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 922FR 5713 2012 DURING C-3 CHECK, INSPECTION REPORTED GOUGES ON RT WING NR 4 SPOILER ANTI-ROTATION LUG SURFACE. MACHINED ANTI-ROTATION FLAT, PERFORMED HFEC, AND BONDED REINFORCING PLATE IAW EA A9-57R-12170. 2 L 7 2 4F RT A28NM 2007101100126 20071011 00126 EU 2007 10 11 SIMA200728104 1 20071006 A 3150 WARNING LIGHT SAAB SF340 340B 7860101 EU FALSE ACTIVATION A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 324AE 340B324 CREW REPORTED A LOW SPEED ABORT DUE TO NO RIGHT APR (AUTO POWER RESERVE) LIGHT ON. ISSUED CREW PLACARD ON APR SYS MEL 7 602. COULD NOT DUPLICATE, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007101100131 20071011 00131 SO 2007 10 11 SIMA200728102 1 20071005 A 5240 PLATE EMB 145 EMB145LR 3260212 SO SERVICE DOOR LOOSE A SIMA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 21 679AE 14500814 CREW NOTED 2 MINUTES INTO FLIGHT, HEARD A FLAPPING NOISE COMING FROM THE SERVICE DOOR AREA. THE CAPT DECLARED AN EMERGE NCY AND WENT TO ORD FOR MTX. LANDED WITHOUT INCIDENT. NO OVERWEIGHT LANDING. REMOVED AND RE-INSTALLED SVC DOOR PROTEC TIVE PLATE IAW EMB 145 AMM 53-21-13. THIS PLATE WAS LOOSE AND CAUSED FLAPPING SOUND. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007101100132 20071011 00132 SO 2007 10 11 SIMA200628103 1 20070930 A 5310 14515201001 SUPPORT BEAM EMB 135 EMB135KL 3260302 SO FWD FUSELAGE CRACKED A SIMA O OTHER E VIBRATION/BUFFET AP APPROACH 1 SW 21 854AE * 145743 ON APPROACH, PASSING THROUGH 210 KTS A HEAVY VIBRATION STARTED THROUGH CONTROL COLUMN. WITH AUTO PILOT ENGAGED, AFTER S LOWING IT WAS NOT AS INTENSIVE. BUT STILL PREVALENT, MEL 2201 APPLIED. REPAIRED CRACKED SUPPORT BEAM FOR AHRS MOUNTS I AW EO EM-53MR-840. AUTOPILOT OPS CHECKS GOOD. FUNCTIONAL CHECK FLIGHT REVEALED NO DISCREPANCIES. MEL ITEM RESTORED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007101100143 20071011 00143 EA 2007 10 11 QXEA200701516 1 20071006 A 3150 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA ILLUMINATED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 617QX 10130 DEN - ON FLIGHT 4277, RECEIVED A PROX SYSTEM 2 FAULT STATUS MESSAGE. RETURNED TO GATE. MAINTENANCE PLACED ON MEL NR 52 -70-4A. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007101100148 20071011 00148 NM 2007 10 11 AALA20071859 1 20071005 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 JFK - EMERGENCY LIGHTS AT OVERHEAD FROM SEAT ROW 30AB TO 37AB INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS A T OVERHEAD FROM SEAT ROW 30AB TO 37AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007101100155 20071011 00155 NM 2007 10 11 AALA20071864 1 20070921 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 AFW - EMERGENCY LIGHT BATTERY PACK AT RT NR 2 DOOR M33097 INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK AT RT NR 2 DOOR M33097. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007101100161 20071011 00161 WP 2007 10 11 AALA20071874 1 20071005 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 578AA 53155 DFW - EMERGENCY LIGHT AT SEAT 18D HAD BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 18D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007101100163 20071011 00163 NM 2007 10 11 AALA20071866 1 20070928 A 5330 SKIN BOEING 767 767323 1385205 NM BS 448 S34L CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 362AA 24043 AFW - FUSELAGE SKIN AT STATION 448 AND STRINGER 34 LEFT HAD MINOR CORROSION ON INNER SURFACE. MATERIAL REMAINING IS BEY OND SRM LIMITS. BLEND IS 0.6 INCH BY 0.3 INCH AND 0.011 INCH DEEP. CONFIRMED SURROUNDING STRUCTURE WITHIN A 22 INCH RA DIUS FROM CENTER OF BLEND OUT IS CORROSION AND DAMAGE FREE. PERFORMED A 10X VISUAL INSPECTION OF THE BLENDOUT TO ENSURE COMPLETE CORROSION REMOVAL. PERFORMED SURFACE HIGH FREQUENCY EDDY CURRENT INSPECTION OF THE BLEND OUT TO ENSURE CRACK OR DAMAGE FREE. APPLIED ALODINE TO ALL BARE SURFACES THEN APPLIED TWO COATS OF BMS 10-11 TYPE 1 PRIMER AND ALLOWED DRY TIMES BETWEEN COATS. 2 L 7 2 4F RT A1NM 2007101100175 20071011 00175 NM 2007 10 11 HALA0700430 1 20070917 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 1142 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 LEVEL 1 CORROSION ON SEAT TRACK RBL 56, AT STATION 1142. AREA REWORKED AND FOUND WITHIN LIMITS PER SRM 53-00-52. REWOR KED AREA ALODINED AND PAINTED. 2 L 7 2 4F RT A1NM 2007101100176 20071011 00176 NM 2007 10 11 HALA0700432 1 20070917 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 1255 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 LEVEL 1 CORROSION ON SEAT TRACK RBL 75 AT STATION 1255. AREA REWORKED AND FOUND TO BE WITHIN LIMITS PER SRM 53-00-52. REWORKED AREA WAS ALODINED AND PAINTED. 2 L 7 2 4F RT A1NM 2007101100178 20071011 00178 EA 2007 10 11 A6WA200740524 1 20070921 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 FOUNF FS 280 RBL 9 INBOARD CLIP CRACKED. 10-24-07 MAINTENANCE REMOVED AND REPLACED CLIP P/N 601R31113-58 IAW CRJ SRM 51-42-06, 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007101100179 20071011 00179 EA 2007 10 11 A6WA200740525 1 20070921 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 FOUND FS 280 LBL 9 INBOARD CLIP CRACKED. 10-24-07 MAINTENANCE REMOVED AND REPLACED CLIP P/N 601R31113-57 IAW CRJ SRM 51-42-06, 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007101100181 20071011 00181 EA 2007 10 11 A6WA200740527 1 20070921 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 FOUND FS 280 LBL 9 OUTBOARD ATTACH CLIP CRACKED. 10-24-07 MAINTENANCE REMOVED AND REPLACED CLIP P/N 601R31113-57, IA W CRJ SRM 51-42-06, 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007101100183 20071011 00183 NM 2007 10 11 AMTA200700460 1 20070922 A 3397 CONNECTOR BOEING 737 73783N 13844HI NM EMERGENCY LIGHT DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 318TZ 28247 RT FWD EMERGENCY EXIT LIGHTING INOPERATIVE. FOUND CONNECTING PLUG FOR BATTERY DISCONECTED REINSTALLED. OPS CK NORMAL I AW 33-51-06-2. (K) 2 L 7 2 4F RT A16WE 2007101100184 20071011 00184 NM 2007 10 11 AMTA200700461 1 20070921 A 2460 CIRCUIT BREAKER BOEING 737 73783N 13844HI NM UNKNOWN A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 323TZ 30033 ATTITUDE DISPLAY ON STANDBY ISFD DISAGREES WITH PIMARY DISPLAY. NO FLAG SHOWS. RESET CB STBY DEDICATED BATTERY CHARGER IAW FIM 34-24-00-810-814. (K) 2 L 7 2 4F RT A16WE 2007101100188 20071011 00188 WP 2007 10 11 AMTA200700464 1 20070927 A 3350 5165744 CHARGER LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE EMERGENCY LIGHTS UNSERVICEABLE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 164AT 1238 EMERGENCY LIGHTS AT THE R4 DOOR ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK @ SEAT ROW 32 IAW MM 33-51-03, OPS C HECKS GOOD. (K) 2 L 7 3 4F 4 F A23WE E12EU 2007101100190 20071011 00190 NM 2007 10 11 AMTA200700472 1 20070928 A 5220 144A66111 HINGE BOEING 737 73783N 13844HI NM EMERGENCY EXIT BROKEN A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 310TZ 28243 RT AFT OVERWING EMERGENCY DOOR HINGE ASSY BROKEN. INSTALLED NEW SERVICEABLE DOOR HINGE IAW CMM 52-26-07. (K) 2 L 7 2 4F RT A16WE 2007101100192 20071011 00192 EA 2007 10 11 A6WA200740517 1 20070920 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 468AW 7916 FOUND RIGHT 621 ANGLE IS CRACKED APPROX 1.5 INCH LONG. 10-25-07 MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-5 3-61-117. (M) 2 L 7 2 4F RT A21EA 2007101100193 20071011 00193 2007 10 11 AMTA200700474 4 20071002 A 2310 9640453011 COUPLER BOEING 757 75723N 1384973 NM HF RADIO UNSERVICEABLE A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 522AT 29330 RT HF RADIO WILL NOT TUNE (CONTINUOUS TONE). REMOVED AND REPLACED RT HF COUPLER IAW MM 23-11-01-4, OPS CHECK OK. 2 L 7 2 4F RT A2NM 2007101100194 20071011 00194 EA 2007 10 11 A6WA200740518 1 20070920 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 468AW 7916 FOUND LEFT 621 ANGLE IS CRACKED APPROX 1.5 INCH LONG. 10-25-07 MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R 5361117. (M) 2 L 7 2 4F RT A21EA 2007101100196 20071011 00196 NM 2007 10 11 AMTA200700476 1 20071003 A 3397 WIRE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHTS DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 514AT 27971 ROWS 10 THRU 12 EMERGENCY FLOOR TRACK LIGHTING INOPERATING. RECONNECT WIRES TO LIGHT ASSY AT ROW 12. OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007101100197 20071011 00197 EA 2007 10 11 A6WA200740519 1 20070920 A 5320 S6144A14 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 468AW 7916 FOUND RIGHT 484 ANGLE IS CRACKED AT RBL 27 APPROX .25 INCH LONG. 10-25-07 MAINTENANCE REMOVED CRACKED ANGLE AT FS 484 RBL 27. FABRICATED REPAIR ANGLE FROM PERFORMED ANGLE LOCATED, DRILLED AND INSTALLED IAW BSC STANDARD REPAIR 601R-53 -0029B. (M) 2 L 7 2 4F RT A21EA 2007101100199 20071011 00199 EA 2007 10 11 A6WA200740520 1 20070920 A 5320 S6144A14 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 468AW 7916 FOUND RIGHT 484 ANGLE IS CRACKED AT RBL 36 APPROX .25 INCH LONG. 10-25-07 MAINTENANCE REPAIRED IAW REO 601R-53-41-0 59. (M) 2 L 7 2 4F RT A21EA 2007101100201 20071011 00201 NM 2007 10 11 QXEA200701517 1 20071007 A 5230 SEAL BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR LOOSE A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 413QX 4060 CLIMBING THROUGH 19,000 FT, GOT MASTER WARNING 'FUSELAGE DOORS' WARNING LIGHT. DOORS PAGE SHOWED AFT BAGGAGE DOOR IN RE D. NO LOSS OF PRESSURIZATION. AIRCRAFT RETURNED TO FIELD. MAINTENANCE PERFORMED GVI OF AFT CARGO DOOR AND DOOR FRAME. FOUND LOWER PORTION OF PRESSURIZATION SEAL NOT IN RETAINER. INSPECTED SEAL, CLEANED AND REINSTALLED. PERFORMED OPS C HECK OF AFT BAGGAGE DOOR IAW 52-31-00-710-801. DOOR OPERATES NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007101100202 20071011 00202 NM 2007 10 11 QXEA200701518 1 20071008 A 5100 NONE BOMBDR DHC8 DHC8402 1390042 NM NONE NONE A QXEA D RETURN TO BLOCK W INADEQUATE Q C TX TAXI/GRND HDL 1 NM 09 421QX 4149 SEA FLIGHT NR 2229, ON TAXI OUT, ADC1 MESSAGE ON BOTH PFD'S. ALSO FO'S IVSI SHOWS 10 FPM CLIMB INTERMITTENTLY. AIRCRAF T RETURNED TO BLOCK. MAINTENANCE FOUND ADC SOURCE SWITCH TO BE IN ADC1 POSITION. PLACED SWITCH TO NORMAL POSITION AND PFD DISPLAYED CORRECTLY, ADC1 STATUS MESSAGE WENT AWAY. REMOVED AND REPLACED ADU2 IAW MTC 6341101. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007101100203 20071011 00203 NM 2007 10 11 QXEA200701519 1 20071005 A 3620 8209076 SWITCH BOMBDR DHC8 DHC8402 1390042 NM NR 2 BLEED FAILED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 413QX 273 273 4060 SEA FLIGHT NR 2459: ON PUSH BACK, GOT THE NR 2 BLEED HOT CAUTION LIGHT. THE LIGHT STAYED ON ALL THE WAY BACK TO THE GAT E AND AFTER SHUT DOWN. MAINTENANCE INTERROGATED CDS AND FOUND FAULT CODE 1701 'R BLD TMP SW'. C/W Q400 FIM TASK 36-10-0 0-810-802. REPLACED NR 2 BLEED OVER TEMP SWITCH IAW Q400 MM 36-11-16, PG 401-406. GROUND RAN AIRCRAFT WITH BLEED ON FO R SEVERAL MINUTES. OPS CHECK GOOD. NO CAUTION LIGHTS OR FAULT CODES NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007101100205 20071011 00205 NM 2007 10 11 NOMB071001001 1 20071001 A 2923 5718610 PUMP BOEING 727 727200RE 1384071 NM PWA JT8 JT8D217C 52053 NE NR 1 POSITION INOPERATIVE G NOMB K NONE L NO TEST IN INSP/MAINT 1 GL 23 727M 1473 22541 NR 1 ELECTRICAL HYDRAULIC PUMP: NO PRESSURE/POPS CIRCUIT BREAKER ON STARTUP FOR DEPARTURE. 2 L 7 3 3F 4 F RT A3WE E9NE 2007101100206 20071011 00206 EU 2007 10 11 74509272007 1 20070927 A 3320 57F3444 RELAY BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL CABIN LIGHTS FAILED E QMLA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 03 485EC S754 ODOR OF BURNING INSULATION DETECTED IN CABIN. NO SMOKE PRESENT. CHECKED FOR TRIPPED CIRCUIT BREAKERS. NONE FOUND. RE CYCLED/RESET BOTH GENERATORS TO CHECK LOAD ON EACH. NO PROBLEMS DETECTED AND RESTORED BOTH GENERATORS. CONTINUED TO FI NAL LANDING AT BASE AND TURNED AIRCRAFT OVER TO MECHANIC FOR TROUBLESHOOTING. AIRCRAFT OPERATED ON GROUND WITH BOTH ENG INES RUNNING AND BOTH GENERATORS OPERATING IN A ELECTRICALLY LOADED CONDITION. NO ODOR NOTED, SYSTEMS OPERATED NORMALLY. OPERATED ELECTRICAL/ AVIONICS USING GROUND POWER FOR GREATER THAN ONE HOUR, NO ODOR NOTED. CABIN CEILING LIGHTS FOUND I NOPERATIVE. FOUND CABIN LIGHT RELAY IN A FAILED CONDITION. DEACTIVATED CABIN LIGHTS IAW MEL. NEW RELAY ON ORDER. 1 G 7 2 3U 3 U H3EU E4CE 2007101100207 20071011 00207 EU 2007 10 11 BAQA200700031 1 20070925 A 5302 112030406 SPAR BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101* NE VERTICAL STAB CRACKED E BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 136AE 7519 157 7234 TAILBOOM VERTICAL FIN MAIN SPAR CRACKED AT UPPER LIGHTNING HOLE NEAR TAIL ROTOR GEARBOX MOUNT. 1 G 7 2 3U 3 U NC H13EU E5NE 2007101100212 20071011 00212 NE 2007 10 11 2007F00055 2 20070928 A 7200 ENGINE SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL2S1 60057 NE POWER LOSS E A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 11 760AF 760523 2059720568 DURING CLIMB OUT FROM CONFINED AREA, ENGINE AND ROTOR RPM FLUCTUATED. ROTOR RPM DROOPED, COLLECTIVE APPLIED, ACTIVATED N R 2 ENGINE OEI LIGHT. 1 G 7 2 3U 4 U NC H1NE E00054EN 2007101100214 20071011 00214 EU 2007 10 11 COEA0706821 1 20070817 A 5310 S53673000205 CREASE BEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE DAMAGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FE 253 FOUND TOOLING DAMAGE (3) PLACES ON CREASE BEAM WEB. FABRICATED REPLACEMENT CREASE BEAM WEB. WO NR 72242, NR 200066. ( K) 2 H 7 2 4T RT A53EU 2007101100215 20071011 00215 EU 2007 10 11 COEA0709821 1 20070905 A 5210 S52176243214 DOOR AEROSP ATR72 ATR72202 8680940 EU MAIN PAX CRACKED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. FOUND CRACK ON BACKUP FITTING, AFT PASSENGER DOOR. FABRICATED AND INSTALLED REPLACEMENT BACK UP FITTING. (K) 2 H 7 2 4T RT A53EU 2007101100216 20071011 00216 EU 2007 10 11 COEA0708821 1 20070817 A 5230 SKIN AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE CARGO DOOR CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. FOUND LEVEL 2 CORROSION ON PREVIOUS REPAIR LT AFT CARGO DOOR. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER. WO NR 72242, NR 200009. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007101100221 20071011 00221 EA 2007 10 11 ERH2007F00000 1 20070908 A 5521 SPAR DHAV DHC3 DHC3 2800202 EA PWA PT6 PT6A34 52043 EA HARTZL HCB3T HCB3TN3 GL LT ELEVATOR CRACKED E ERHA O OTHER O OTHER NR NOT REPORTED 1 AL 03 727KT 13082 419 RBO177 BUA19518 PILOT REPORTED A CRACK FOUND ON THE LT ELEVATOR WHILE PERFORMING A PREFLIGHT INSPECTION. THE ELEVATOR WAS REMOVED FROM THE AIRCRAFT FOR CLOSER INSPECTION. THE CRACK WAS IN THE FORWARD SPAR AND HAD ORIGINATED FROM UNDER THE OB ATTACH FITTI NG. FATIGUE. RECOMMENDATIONS TO PREVENT RECURRENCE: NDT AT SPECIFIC TIME IN SERVICE INTERVALS. (K) 1 H 7 1 3R 4 T A815 E4EA 6 C P15EA 2007101100222 20071011 00222 EA 2007 10 11 BJF2007F00000 2 20070910 A 8530 4SL36006WA20P CYLINDER CESSNA 172 172S 2072439 CE LYC IO360 IO360L2A EA MCAULY 1A170 1A170* GL NR 3 CRACKED B BJFR K NONE O OTHER IN INSP/MAINT 1 EA 23 269LP 1346 172S8206 L2826751A TC032 AIRCRAFT EXPERIENCED PARTIAL POWER LOSS. LANDED WITHOUT INCIDENT. INSPECTED ENGINE NOTED HOLE, NR 3 SPARK PLUG WITH A LARGE CRACK EXTENDING DOWN TO EXHAUST PORT FLANGE. FURTHER INSPECTION ALSO FOUND NR 1 CYLINDER CRACKED AT SAME LOCATION BUT HAD NOT YET HAD COMPLETE FAILURE. POSSIBLE CAUSE MAY BE IMPROPER LEANING PROCEDURES. NOT: AIRCRAFT USED EXTENSIVE LY FOR FLIGHT TRAINING. (K) 1 H 7 1 3O 3 O NT 3A12 1E10 5 N P857 2007101100224 20071011 00224 EU 2007 10 11 IJA2007F00000 1 20070829 A 7720 614764031 TACHOMETER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE FAILED A IJAA O OTHER O OTHER NR NOT REPORTED 1 CE 07 406EM 3661 9042 9759 DURING A PATIENT TRANSPORT, THE PILOT RECEIVED A LOS NR TACH INDICATION OF 320 RPM. THE NR WARNING HORN NEVER ACTIVATED . THE HELICOPTER MADE A PRECAUTIONARY LANDING. THE PATIENT WAS GROUND TRANSPORTED TO HOSPITAL. MAINTENANCE WAS DISPAT CH. THE HELICOPTER WAS TROUBLESHOT AND THE DUAL TACHOMETER INDICATOR PN 61476-403-1 WAS REPLACED WITH A NEW INDICATOR. (K) 1 G 7 1 3U 3 U H9EU E19EU 2007101200002 20071012 00002 WP 2007 10 12 UPS07850763 1 20070919 A 3260 UPLOCK SWITCH DOUG DC8 DC873F 302199F WP MLG DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 RIGHT MLG DOOR UPLOCK SWITCH HOLES ARE ELONGATED. FABRICATED AND INSTALLED REPAIR DOUBLER AT RIGHT M LG UPLOCK SWITCH IAW EO DC8-3260-16914-A. 2 L 7 4 4F RT 4A25 2007101200003 20071012 00003 WP 2007 10 12 UPS07850764 1 20070919 A 3260 UPLOCK SWITCH DOUG DC8 DC873F 302199F WP LT MLG DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 LEFT MLG UPLOCK SWITCH HOLES ARE ELONGATED. FABRICATED AND INSTALLED REPAIR DOUBLER AT LEFT MLG UPLO CK SWITCH IAW UPS EO DC8-3260-16914-A. 2 L 7 4 4F RT 4A25 2007101200004 20071012 00004 WP 2007 10 12 UPS07850765 1 20070913 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT TE FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 RIGHT INBOARD FLAP INBOARD UPPER SURFACE SKIN HAS DEEP GOUGE AT STA 3. FABRICATED AND INSTALLED REPA IR DOUBLER AT RIGHT INBOARD FLAP A STA 3 IAW DWG 5652681, AND SRM 51-01-15-0. 2 L 7 4 4F RT 4A25 2007101200005 20071012 00005 WP 2007 10 12 UPS07850766 1 20070920 A 5310 FITTING DOUG DC8 DC873F 302199F WP FS 902 L18R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 FITTING CRACKED AT STA 902 L18R. REMOVED, FABRICATED AND INSTALLED REPAIR FITTING AT STA 902 L18R IA W DWG 479496, AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 2007101200006 20071012 00006 WP 2007 10 12 UPS07850767 1 20070920 A 5310 FITTING DOUG DC8 DC873F 302199F WP FS 1260 L20R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 FITTING CRACKED AT STA 1260 L20R FWD SIDE. REMOVED, FABRICATED, AND INSTALLED REPAIR FITTING AT STA 1260 L20R IAW DWG 4750419, AND SRM 51-01-20D-0. 2 L 7 4 4F RT 4A25 2007101200007 20071012 00007 WP 2007 10 12 UPS07850768 1 20070918 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CANNING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 FUSELAGE NOSE EXTERIOR SKIN IS OIL CANNING AND DENTED AT STA -3 TO -12 L21L TO L22L. CUT OUT DAMAGED AREA IAW SRM 53-2-0 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER, AND FINGER DOUBLER AT STA -32 TO -12 L21L TO L22L IAW SRM 53-2-01 FIG 7. 2 L 7 4 4F RT 4A25 2007101200008 20071012 00008 WP 2007 10 12 UPS07850769 1 20070920 A 5310 FITTING DOUG DC8 DC873F 302199F WP FS 905 L19R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 FITTING CRACKED AT STA 905 L19R. REMOVED, FABRICATED AND INSTALLED REPAIR FITTING AT STA 905 L19R IA W DWG 3779498, AND SRM 51-03-02. 2 L 7 4 4F RT 4A25 2007101200009 20071012 00009 WP 2007 10 12 UPS07850770 1 20070920 A 5310 FITTING DOUG DC8 DC873F 302199F WP FS 1220 L19R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 FITTING CRACKED AT STA 1220 L19R AFT SIDE. REMOVED, FABRICATED, AND INSTALLED REPAIR FITTING AT STA 1220 L19R IAW DWG 4750419, AND SRM 51-01-20D-0. 2 L 7 4 4F RT 4A25 2007101200011 20071012 00011 WP 2007 10 12 UPS07850772 1 20070921 A 5310 FITTING DOUG DC8 DC873F 302199F WP FS 1380 L19R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 MAIN CABIN INTERCOSTAL TO FRAME ATTACH FITTING HEAVY CORROSION AT STA 1380 L19R. REMOVED, FABRICATED , AND INSTALLED REPAIR ATTACH FITTING AT STA 1380 L19R IAW DWG 2702605, AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 2007101200012 20071012 00012 WP 2007 10 12 UPS07850773 1 20070919 A 5310 FITTING DOUG DC8 DC873F 302199F WP FS 900 L19R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 FITTING CRACKED AT STA 900 L19R. REMOVED, FABRICATED, AND INSTALLED REPAIR FITTING AT STA 900 L19R I AW DWG 3779498, AND SRM 51-01-24. 2 L 7 4 4F RT 4A25 2007101200013 20071012 00013 WP 2007 10 12 UPS07850775 1 20070919 A 5310 FITTING DOUG DC8 DC873F 302199F WP FS 700 L13R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 FITTING CRACKED AT STA 700 L13R. REMOVED, FABRICATED, AND INSTALLED REPAIR FITTING AT STA 700 L13R I AW DWG 3779978, AND SRM 51-01-20D-0. 2 L 7 4 4F RT 4A25 2007101200015 20071012 00015 WP 2007 10 12 UPS07850780 1 20070927 A 5542 SKIN DOUG DC8 DC873F 302199F WP LWR RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 RUDDER LEFT SIDE VERY LWR FASTENER HOLE CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPA IR DOUBLER ON RUDDER SKIN LWR LEFT SIDE IAW SRM 55-02-00-0, AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007101200016 20071012 00016 EA 2007 10 12 COMA0760585 1 20070929 A 3297 601R572181PE WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA NLG DOOR FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 587SW 7062 FLIGHT 5527 - GEAR DISAGREE AND NOSE DOOR WARNING CAME ON WHEN GEAR WAS SELECTED DOWN ON APPROACH. PERFORMED GO-AROUND AND LANDED SAFELY. REMOVED AND REPLACED NLG CONTROL HARNESS NR 2. (DI 15). 2 L 7 2 4F RT A21EA 2007101200017 20071012 00017 EA 2007 10 12 COMA0760586 1 20070929 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 957CA 7109 FLIGHT 5646 - FLAPS FAILED AFTER PUSHBACK. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007101200020 20071012 00020 NM 2007 10 12 CALA0700545 1 20071001 A 5230 6547952U133 PAN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A 1 INCH CRACK IN C-2 DOOR FORWARD UPPER PAN AT PULLEY BRACKET ATTACH POINT. THE FRAME PAN WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007101200021 20071012 00021 NM 2007 10 12 CALA0700546 1 20070927 A 5330 65C33756 SKIN BOEING 737 7373T0 1384582 NM BS 328-344 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A 0.8 INCH CRACK IN R-1 DOOR CUTOUT AFT LOWER CORNER OUTER SKIN, STA 328-344, S16R TO S17R. A REPAIR W AS INSTALLED IAW SRM 53-10-01, REPAIR 2, FIGURE 201. 2 L 7 2 4F RT A16WE 2007101200024 20071012 00024 EU 2007 10 12 TRAX200701427 1 20070928 A 5311 FRAME AEROSP ATR72 ATR72 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 RIGHT BELLY AFT SURFACE ON FR 27 NEAR STRINGER 14R FOUND CRACKED. 10-16-07 CRACK ON RT BELLY FR 27 REMOVED IAW DO/T S 4R1/07-9315 E/C PERFORMED ON CUTOUT BY HEATHAIR AMO 46-90 W/O 37536 IAW NTM NO CRACKS FOUND RT BELLY FR 27 REPAIRED IA W DO/TS 4191/07-9315 FABRICATION OF DOUBLER COVER ON W/C 2000-165 REPAIRED FAIRING FR 27 PER TC EO 72-53-0255. 2 H 7 2 4T RT 2007101200025 20071012 00025 EA 2007 10 12 TRAX200701435 1 20070928 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 MAIN AIRSTAIR DOOR HARD TO OPEN. WITH AP SHOWING 0.0 (AIRCRAFT DEPESSURIZED) THERE IS A PRESSURIZATION SPIKE & IT TAKES ABOUT 20 SECONDS FOR F/A TO OPEN THE DOOR. THE F/A STATED THAT THE HANDLE WON'T PULL FULLY UP. 2 L 7 2 4F RT A21EA 2007101200026 20071012 00026 EA 2007 10 12 VNAA0709010 1 20070916 A 7160 INTAKE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT ENGINE DAMAGED A VNAA O OTHER O OTHER AP APPROACH 1 GL 05 254PS 7935 CREW REPORTED A BIRD STRIKE ON APPROACH TO THE RIGHT HAND ENGINE INTAKE COWLING LEADING EDGE. MAINTENANCE INSPECTED AND FOUND THE DAMAGE TO BE 2 INCH LENGTH BY 1 INCH WIDTH BY .15 DEEP. DAMAGE WITHIN LIMITS IN ACCORDANCE WITH THE SHORTS CMA CMM 71-61-01. TEMPORARY AIRCRAFT DAMAGE AUTHORIZATION 20044 ISSUED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007101200027 20071012 00027 EA 2007 10 12 VNAA0709011 1 20070917 A 5240 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE GROUND POWER OPEN A VNAA D RETURN TO BLOCK W INADEQUATE Q C TO TAKEOFF 1 GL 05 720PS 10178 CREW REPORTED AN EXTERNAL GPU DOOR LEFT OPEN AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE GPU DOOR OPEN. MAINTENANCE SECURED DOOR CLOSED AND NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007101200028 20071012 00028 EU 2007 10 12 USA2007F00012 1 20070818 A 5330 SKIN AIRBUS A321 A321211 3930370 EU CFMINT CFM56 CFM565B32P 13008 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 185UW 19917 1666 CORRODED RIVET TAILS WERE FOUND IN THE FUSELAGE FORWARD CARGO COMPARTMENT BETWEEN FRAME28 TO 35.5 STRINGER 38R TO 38L. APPROX 450 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD THE PAINT FLAKING OFF THE RIVET TAILS THAT WERE CLEANED AND HAD PRIMER AND PAINT REAPPLIED. AIRCRAFT WAS MFG JANUARY 2002. (K) 2 L 7 2 4F 4 F RT A28NM 2007101200032 20071012 00032 NM 2007 10 12 SWAA074891 1 20071001 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 425LV 29829 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007101200033 20071012 00033 NM 2007 10 12 SWAA074888 1 20071001 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 287WN 32537 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007101200034 20071012 00034 NM 2007 10 12 SWAA074853 1 20070930 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 287WN 32537 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007101200035 20071012 00035 NM 2007 10 12 SWAA074870 1 20070930 A 3350 417A5701 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LENS MISSING AT ROW 12 DEF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007101200037 20071012 00037 NM 2007 10 12 SWAA074898 1 20071001 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 276WN 32530 EEPLS END CAP MISSING AT ROW 1 ABC. INSTALLED END CAP PER MM. 2 L 7 2 4F RT A16WE 2007101200038 20071012 00038 NM 2007 10 12 SWAA074895 1 20071001 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 360 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED A3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 360, STR 4R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007101200040 20071012 00040 NM 2007 10 12 SWAA074854 1 20070930 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 504 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007101200041 20071012 00041 NM 2007 10 12 SWAA074894 1 20071001 A 5553 6546572 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED BRDG CHECK, FOUND VERTICAL STABILIZER FITTING CLEVIS LUG FACES CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2007101200044 20071012 00044 2007 10 12 SWAA074863 4 20070930 A 2565 6557463 BRACKET BOEING 737 7373H4 1384600 NM L1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR BRACKET LOOSE. SECURED BRACKET PER MM. 2 L 7 2 4F RT A16WE 2007101200045 20071012 00045 2007 10 12 SWAA074867 4 20070930 A 2565 6557463 BRACKET BOEING 737 7377H4 1384404 NM R1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 783SW 29809 R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR BRACKET LOOSE. SECURED BRACKET PER MM. 2 L 7 2 4F RT A16WE 2007101200049 20071012 00049 NM 2007 10 12 SWAA074871 1 20071001 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 380 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007101200050 20071012 00050 NM 2007 10 12 SWAA074876 1 20071001 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 685 S3L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007101200051 20071012 00051 NM 2007 10 12 SWAA074873 1 20071001 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007101200053 20071012 00053 NM 2007 10 12 SWAA074874 1 20071001 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 927 S26R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007101200054 20071012 00054 NM 2007 10 12 SWAA074892 1 20071001 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 400 S14L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007101200055 20071012 00055 NM 2007 10 12 SWAA074893 1 20071001 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 440 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007101200056 20071012 00056 NM 2007 10 12 SWAA074858 1 20070930 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 947 S26R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007101200057 20071012 00057 NM 2007 10 12 SWAA074859 1 20070930 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 277 S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007101200058 20071012 00058 NM 2007 10 12 SWAA074860 1 20070930 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 277 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007101200061 20071012 00061 NM 2007 10 12 SWAA074877 1 20071001 A 5311 65C33512 FRAME BOEING 737 7375H4 138449D NM BS 482 S8L/R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007101200065 20071012 00065 NM 2007 10 12 SWAA074875 1 20071001 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM BS 380 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 16L CRACKED AT BS 380. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007101200066 20071012 00066 2007 10 12 SWAA074862 4 20070930 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007101200068 20071012 00068 SO 2007 10 12 C2XA07IA213 1 20070923 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 48901 145501 LCH - FLIGHT 3015, THE CREW REPORTED THE LEFT HAND WALL EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE NR 4 EMERGENCY EXIT LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007101200070 20071012 00070 SO 2007 10 12 C2XA07IA215 1 20070928 A 3350 20131A BATTERY PACK EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12166 16449 1868 14500831 MCI - DURING MAINTENANCE INSPECTION, THE MAIN DOOR, AND GALLEY EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENAN CE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRC RAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007101100195 20071011 00195 NM 2007 10 11 AMTA200700475 1 20071001 A 4970 WARNING LIGHT BOEING 737 73783N 13844HI NM APU FALSE ACTIVATION A AMTA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 317TZ 28246 APU MASTER CAUTION LIGHT ILLUMINATED WHEN ELECT POWER TRS TO ENG DRIVEN GENERATORS REMAINS ILLUMINATED WHEN APU SHUTDOWN . INTERROGATED CDU PERFORMED BITE TEST ON APU NO RECENT FAULT OR ANY HISTORY FAULTS NOTED ON ANY LEGS, SHOT DOWD AC POW ER CYCLE AC POWER APU MASTER CAUTION LIGHT IS OFF PERFORMED SECOND APU BITE TEST OK. (K) 2 L 7 2 4F RT A16WE 2007101100204 20071011 00204 EA 2007 10 11 A6WA200740521 1 20070920 A 5320 S6144A14 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 468AW 7916 FOUND LEFT 484 ANGLE IS CRACKED AT LBL 36 APPROX .25 INCH LONG. 10-25-07 MAINTENANCE REPAIRED IAW REO 601R-53-41-059 . (M) 2 L 7 2 4F RT A21EA 2007101100218 20071011 00218 EU 2007 10 11 COEA0710821 1 20070920 A 5720 S57112244201 SKATE ANGLE AEROSP ATR72 ATR72202 8680940 EU FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. FOUND LEVEL 2 CORROSION ON PREVIOUS REPAIR TO THE RT NACELLE, IB SKATE ANGLE. BLENDED OUT CO RROSION IAW SRAS DO/TS-3872/07-9231 REPAIR INSTRUCTIONS. SHEET REFERENCE: DO/TS-3872/07-4247. (K) 2 H 7 2 4T RT A53EU 2007101200001 20071012 00001 NM 2007 10 12 USAABB07078 1 20070928 A 2432 893003 CHARGER BOEING 757 757225 1384959 NM MASTER BATTERY FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 915AW 50 50 22209 FLT 569 PHX - MCO CREW RECEIVED MAIN BATTERY CHARGER STATUS MESSAGE ALONG WITH A BURNING ODOR IN COCKPIT. RETURNED TO P HX. MAINTENANCE REPLACED MAIN BATTERY CHARGER. 2 L 7 2 4F RT A2NM 2007101200010 20071012 00010 WP 2007 10 12 UPS07850771 1 20070920 A 5310 FITTING DOUG DC8 DC873F 302199F WP FS 1220 L18R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 FITTING CRACKED AT STA 1220 L18R FWD SIDE. REMOVED, FABRICATED, AND INSTALLED REPAIR FITTING AT STA 1220 L18R IAW DWG 4750418, AND SRM 51-01-24. 2 L 7 4 4F RT 4A25 2007101200018 20071012 00018 2007 10 12 ZZDA2007275 4 20070928 A 2565 5A33075 SLIDE BOEING 737 73776N 13844CH NM L1 DOOR UNSECURE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 299AT 32678 F/A REPORTS L1 DOOR SLIDE NEEDS TO BE RESECURED. REMOVED AND REPLACED FWD ENTRY DOOR SLIDE ASSY REF ATMM 25-66. 2 L 7 2 4F RT A16WE 2007101200019 20071012 00019 NM 2007 10 12 CALA0700544 1 20071001 A 5230 65C2518022 DOOR FRAME BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A 1 INCH CRACK IN C-2 DOOR AT FORWARD LOWER PAN PULLEY BRACKET. THE LOWER FRAME PAN WAS REMOVED AND RE PLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007101200042 20071012 00042 2007 10 12 SWAA074883 4 20071001 A 2565 6557463 FITTING BOEING 737 7373H4 1384600 NM L1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER MM. 2 L 7 2 4F RT A16WE 2007101200052 20071012 00052 NM 2007 10 12 SWAA074857 1 20070930 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 539 S28L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 539, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007101200060 20071012 00060 NM 2007 10 12 SWAA074881 1 20071001 A 5311 65C33509 FRAME BOEING 737 7375H4 138449D NM BS 787 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 787, STR 16L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007101200064 20071012 00064 NM 2007 10 12 SWAA074884 1 20071001 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM BS 1006 S21R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER 21R CRACKED AT BS 1006. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007101200071 20071012 00071 2007 10 12 2007UALA03877 4 20070924 A 2397 WIRE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE OXY MASK MIC CRUSHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 804UA 759 F/O'S OXYGEN MASK MICROPHONE IS INOPERATIVE. *S/D* MIC WIRE DISCONNECTED/CRUSHED. REPLACED MASK ASSY, OPS CHECK OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101200073 20071012 00073 EU 2007 10 12 2007UALA03896 1 20070925 A 3397 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 466UA 1343 OVERHEAD EMERGENCY LIGHT ABOVE ROWS 18-19 INOP. *S/D* LOOSE PIN IN CONNECTOR. SECURED LOOSE PIN -J- IN TERM BLOCK 722 2VT. SYSTEM OPS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101200078 20071012 00078 EU 2007 10 12 2007UALA03932 1 20070927 A 2700 B372BAM0509 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 SEC FAULTY A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 483UA 1586 ELAC 2 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN, F-CTL. *S/D* SEC NR 2 AND RELAY 36CE3 FAULT. REPLACED SEC NR 2 AND RELAY 36CE3, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101200081 20071012 00081 NM 2007 10 12 2007UALA03940 1 20070927 A 5512 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZONTAL STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 RIGHT HORIZONTAL STAB LOWER SKIN CRACKED 59.5" - 61" OUTBOARD FROM INBOARD END OF STAB, 1.5" FWD OF AFT SPAR. MAJOR REP AIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF STAB SKIN & ACCOMPLISHED NDT FOR CRACK CONTAINMENT. FABRICATED 2EA ACCESS HOLES TO FACILITATE REPAIR. FABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR BETWEEN STAB STA 111-166. INSTALLED ACCESS PANELS IN ACCESS HOLES. 2 L 7 2 4F 4 F RT A16WE E21EU 2007101200082 20071012 00082 NM 2007 10 12 2007UALA03941 1 20070928 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU SERVICE DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 305UA 23666 CABIN FWD GALLEY SERVICE ENTRY DOOR CUTOUT AFT LWR JAMB AREA CRACKED. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REP AIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007101200084 20071012 00084 2007 10 12 2007UALA03943 4 20070927 A 2565 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 CREW REPORTS ESCAPE SLIDE AT DOOR 1LT SLIDE IS PARTIALLY OUT OF THE DOOR PACK. REINSTALLED SLIDE PACK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007101200085 20071012 00085 NE 2007 10 12 2007UALA03944 2 20070927 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MALFUNCTIONED A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 511UA 24799 726523 PER CREW, ENG WOULDN'T SHUTDOWN, HAD TO CYCLE FUEL CUTOFF SWITCH SEVERAL TIMES TO GET ENG TO SHUT DOWN. ALSO HAD A LOT OF FUEL VAPOR COMING OUT OF TAILPIPE. ENGINE WAS PUT THROUGH SEVERAL START/STOP SEQUENCES AND NO PROBLEM WAS FOUND. TH IS AIRCRAFT ENGINE HAS NOT FAULTED SINCE THIS ORIGINAL REPORT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101200086 20071012 00086 NM 2007 10 12 2007UALA03945 1 20070927 A 2721 TRIM SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RUDDER FAILED A UALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 WP 29 552UA 26641 RUDDER TRIM FAILED ON APPROACH. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101200088 20071012 00088 NM 2007 10 12 2007UALA03947 1 20070928 A 3350 321431 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 830UA 1243 EMERGENCY POWER SUPPLY UNIT BATTERY L FAILED CHECK. REPLACED LT EPSU BATTERY AT OVERWING EXIT. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101200089 20071012 00089 NM 2007 10 12 NOCA07107 1 20070323 A 2620 3460001222 FIRE BOTTLE BOEING 767 767304 NM APU BAY DISCHARGED A NOCA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 769NA 28039 PRIOR TO DEPARTURE THE APU SHUTDOWN AND THE APU FIRE BOTTLE DISCHARGE LIGHT CAME ON. INSPECTED THE APU COMPARTMENT AND FOUND NO EVIDENCE OF APU FIRE, THERE WAS EVIDENCE THAT THE APU FIRE BOTTLE HAD DISCHARGED. REPLACED APU FIRE BOTTLE, PE RFORMED BITE ON THE ECU PER FIM 49-11-00 FIG 103, NO FAULTS. INSPECTED APU COMPARTMENT AND APU EXHAUST, NO DAMAGE OF EV IDENCE OF A FIRE FOUND. 2 L 7 2 4F RT A1NM 2007101200091 20071012 00091 NM 2007 10 12 CALA0700550 1 20071002 A 5320 69489852 SUPPORT BOEING 737 7373T0 1384582 NM BS 360 S8L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A 5 INCH CRACK IN L-1 DOOR CUTOUT AFT SIDE STA 360 SUPPORT CLIP AT STRINGER 8L. THE CLIP WAS REMOVED A ND REPLACED IAW ECRA 5311-01363. 2 L 7 2 4F RT A16WE 2007101200095 20071012 00095 NM 2007 10 12 CALA0700554 1 20071002 A 5315 140W25213 FLOORBEAM BOEING 777 777224 1385225 NM BS 676 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 77012 29860 INSPECTION FOUND A 3 INCH CRACK IN FORWARD CARGO COMPARTMENT FLOORBEAM AT STA 676 24 INCHES I/B FROM RIGHT O/B ROLLER TR ACK, RBL 33 - RBL 39. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-53, FIGURE 203, REPAIR 4. 2 L 7 2 4F RT T00001SE 2007101200098 20071012 00098 EA 2007 10 12 HNAA0700181 1 20071001 A 4940 AJA4N176 CONTACTOR DHAV DHC8 DHC8311 1386006 EA APU STARTER SEIZED A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 330EN 32511 32511 274 MAIN BATTERY TEMP AT 55 DEG AND VOLTAGE AT 15 VOLTS WITH MAIN AND AUX BATTERY CAUTION LIGHTS ILLUMINATED, AIRCRAFT RETUR NED TO GATE AND SHUTDOWN POWER. WHEN EXTERNAL POWER APPLIED, FIRE DETECTION WARNING LIGHTS ILLUMINATED AND APU FIRE PAN EL WAS BLANK, CREW NOTED SMOKE COMING FROM APU COMPARTMENT. THE CREW WAS ADVISED TO SHUT OFF POWER AND CONTACT THE FIRE DEPARTMENT. THE FIRE DEPARTMENT RESPONDED, NO FIRE WAS NOTED, BUT A LOT OF SMOKE WAS COMING FROM THE APU COMPARTMENT. APU START CONTACTOR APPEARS TO BE WELDED AND CIRCUIT BREAKER N-8 (APU AUX) WAS POPPED CAUSING THE STARTER TO OVERHEAT A ND GENERATE THE SMOKE. REMOVED AND REPLACED APU START CONTACTOR AND STARTER/GENERATOR, OPS CHECK GOOD. PERFORMED HIDDE 2 H 7 2 4T RT A13NM 2007101200099 20071012 00099 EA 2007 10 12 TRAX200701444 1 20070929 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR LACK OF LUBE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 659CA 10153 F/A REPORTS, DOOR MAIN CABIN NOT ALIGNED AND DIFFICULT TO CLOSE. LUBE UP PAX STOW HANDLE. OPS CHECK GOOD. NO DEFECTS NOTED IAW CRJ 200 700 52-12-00. ALL TOOLS AND EQUIP REMOVED. 2 L 7 2 4F RT A21EA 2007101200100 20071012 00100 EA 2007 10 12 TRAX200701439 1 20070928 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 CABIN DOOR HANDLE WILL NOT GO UP IN ORDER TO OPEN. FLT 4509 DEL 22 MINS. 2 L 7 2 4F RT A21EA 2007101200101 20071012 00101 EA 2007 10 12 TRAX200701440 1 20070928 A 2910 HYDRAULIC SYSTEM CNDAIR CL600 CL6002B19 1900309 EA NR 1 LEAKING A ASOA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 829AS 7232 HYDRAULIC SYSTEM NR 1 LOST HYDRAULIC FLUID WHILE IN FLIGHT. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007101200102 20071012 00102 EA 2007 10 12 TRAX200701441 1 20070928 A 3350 SIGN CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 EXIT SIGN AT SERVICE DOOR IS MISSING. FLT 4235 DEL 23 MINS. 2 L 7 2 4F RT A21EA 2007101200103 20071012 00103 EA 2007 10 12 TRAX200701442 1 20070929 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 880AS 7606 ASD AFT DRAG ANGLE IS CRACKED (MTC). 2 L 7 2 4F RT A21EA 2007101200104 20071012 00104 EA 2007 10 12 TRAX200701443 1 20070929 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 922EV 7822 EMERGENCY LIGHTS ARE ON IN THE ARMED POSITION. FLT 4766 DEL 17 MINS. 2 L 7 2 4F RT A21EA 2007101200106 20071012 00106 NM 2007 10 12 HNAA0700184 1 20070927 A 3097 8351091 TERMINAL DHAV DHC8 DHC8102 2809003 NM WINDSHIELD HEAT BURNED A HNAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 980HA 376 CAPTAIN`S WINDSHIELD SELECTED TO WARM UP, SMOKED FROM ELEMENT LEADS. MEL'ED THE WINDSHIELD HEATER SYSTEMS. INSPECTION FOUND L1 TERMINAL BURNT, NO OTHER DAMAGE NOTED. REMOVED AND REPLACED CAPTAIN`S WINDSHIELD HEAT SCREWS AND L1 TERMINAL A S PER FCD8-56-07-0023. GROUND RAN A/C, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007101200107 20071012 00107 EU 2007 10 12 YENA2007086 1 20071001 A 3350 340022 BATTERY PACK EMB ERJ190 ERJ190100IGW 3260408 EU EMERGENCY LIGHTS FAILED A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 197JB 4295 19000020 COCKPIT EMERGENCY LIGHT DOES NOT ILLUMINATE WITH SWITCH IN THE ON POSITION. REMOVED AND REPLACED NR 1 BATTERY PACK IAW AMM 33-50-00, OPS CHECK OK. 2 L 7 2 4F RT A57NM 2007101200108 20071012 00108 NM 2007 10 12 HNAA0700185 1 20071003 A 2933 974641 SWITCH DHAV DHC8 DHC8102 2809003 NM ISOLATION VALVE INOPERATIVE A HNAA O OTHER N FALSE WARNING CR CRUISE 1 EA 07 808EX 299 NR 2 HYD ISO VALVE CAUTION LIGHT ILLUMINATED IN FLIGHT QTY'S AND PRESSURE NORM. FERRY FROM AVP TO MDT. REPLACED ISO LO W LEVEL SWITCH AND BLEED NR 2 HYD SYSTEM OPS CHECK GOOD IAW 29-43-00. 2 H 7 2 4T RT A13NM 2007101200111 20071012 00111 NM 2007 10 12 HNAA0700189 1 20070904 A 5330 85711802005 PANEL DHAV DHC8 DHC8102 2809003 NM CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 839EX 226 CORROSION FOUND ON RIGHT STRESS PANEL 622AT. GREEN PRIMER APPLIED ON COUNTER SINKS OF PANEL 622AT AS PER AMM 20-34-11 C ORROSION FOUND OUT OF LIMITS, NEW ACCESS PANEL INSTALLED PER 05-00-21. 2 H 7 2 4T RT A13NM 2007101200112 20071012 00112 NM 2007 10 12 HNAA0700191 1 20070906 A 5320 85320686101 THRESHOLD DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 839EX 226 PAX DOOR CORRODED AROUND TEFLON STRIP. PAX DOOR THRESHOLD REPLACED WITH NEW PART 85320686-101 AND 85321229-101 NYLON RU BSTRIP INSTALLED WITH SOLID RIVETS IAW SRM 51-40-00. 2 H 7 2 4T RT A13NM 2007101200113 20071012 00113 NM 2007 10 12 HNAA0700192 1 20070904 A 5240 85321086S059 PANEL DHAV DHC8 DHC8102 2809003 NM SERVICE DOOR CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 947HA 167 LAV SERVICE DOOR PNL SURROUND LOWER STRUCTURE IS CORRODED. DAMAGE CUT OUT AND REPAIR PACKER & ANGLE INSTALLED ON LAV S ERVICE PANEL AS PER EO08-53-07-3346. HFEC CUTOUT, NO CRACKS FOUND. 2 H 7 2 4T RT A13NM 2007101200121 20071012 00121 SO 2007 10 12 LR7A07099 1 20070927 A 5311 FRAME LKHEED 382 382G 526414U SO FS 902 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 519 5025 DURING SCHEDULED B-3 CHECK PER JOB CARD HB5302 FOUND AFT FUSELAGE INTERIOR LT BHD INBOARD CAP CRACKED AT FS 902, WL 190, LBL 63. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-50-17. 2 H 7 4 4T A1SO 2007101200122 20071012 00122 SO 2007 10 12 LR7A07100 1 20070927 A 5311 FRAME LKHEED 382 382G 526414U SO FS 577 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 519 5025 DURING SCHEDULED B-3 CHECK PER JOB CARD HB3200 FOUND RT UPPER WHEEL WELL FRAME INBOARD CAP BROKEN AT FS 577, WL 253, RBL 63. REPAIR ACCOMPLISHED IAW LYNDEN AIR CARGO MEA 382-53-07-058. MENTIONED AREAS ATTACHING BOLTS REPLACED WITH P/N:MS2 1250-05020. 2 H 7 4 4T A1SO 2007101200124 20071012 00124 NM 2007 10 12 USAA920070885 1 20070929 A 5753 113N23632 SUPPORT BEAM BOEING 757 7572S7 1384962 NM ZONE 600 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 903AW 23323 MCN - MAJOR REPAIR - NR 5979695 - RIGHT WING INBOARD FLAP, INBOARD FLAP BELLCRANK SUPPORT BEAM CRACKED, WS 152. REMOVED AND REPLACED RIGHT WING INBOARD FLAP, INBOARD FLAP BELLCRANK SUPPORT BEAM FITTING, WS 152 - RIG AND OPS CHECK GOOD IAW BOEING SOPM 20-50-01 PG 1-5 AND B757-200 AMM 27-51-13-4. 2 L 7 2 4F RT A2NM 2007101200126 20071012 00126 NM 2007 10 12 USAA920070887 1 20070904 A 5240 SKIN BOEING 737 7373B7 1384580 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 23704 CLT - MAJOR REPAIR - C-5 CHECK, FORWARD SERVICE DOOR EXTERIOR SKIN CRACKED AT UPPER HINGE CUTOUT. REPAIRED FORWARD SER VICE DOOR EXTERIOR SKIN AT UPPER HINGE CUTOUT IAW USAIRWAYS TYPICAL REPAIR 52-10-13. 2 L 7 2 4F RT A16WE 2007101200128 20071012 00128 NM 2007 10 12 USAA920070889 1 20070920 A 5510 69730953 HINGE PIN BOEING 737 7374B7 1384702 NM HORIZONTAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 456UW 25020 CLT - MAJOR REPAIR - C-5 CHECK, CORROSION ON THE RIGHT HORIZONTAL STABILIZER CENTER SECTION TO BODY OUTER HINGE PIN. RE PLACED RIGHT HORIZONTAL STABILIZER CENTER SECTION TO BODY OUTER HINGE PIN IAW B737-400 AMM 27-41-31. 2 L 7 2 4F RT A16WE 2007101200130 20071012 00130 NM 2007 10 12 USAA920070891 1 20070920 A 5510 69730963 HINGE PIN BOEING 737 7374B7 1384702 NM HORIZONTAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 456UW 25020 CLT - MAJOR REPAIR - C-5 CHECK, CORROSION ON THE RIGHT HORIZONTAL STABILIZER CENTER SECTION TO BODY INNER HINGE PIN. RE PLACED RIGHT HORIZONTAL STABILIZER CENTER SECTION TO BODY INNER HINGE PIN IAW B737-400 AMM 27-41-31. 2 L 7 2 4F RT A16WE 2007101200132 20071012 00132 NM 2007 10 12 USAA920070893 1 20070928 A 5340 69389396 STRINGER CLIP BOEING 737 7373G7 1384595 NM BS 344 S11R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6505095, CRACKED STRINGER CLIP, BS 344, S11R. REPLACED STRINGER CLIP, BS 344, S11R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007101200134 20071012 00134 NM 2007 10 12 USAA920070895 1 20070928 A 5340 654797621 ATTACH ANGLE BOEING 737 7373G7 1384595 NM BS 807-827 S17L CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6504936, CORROSION ON CUSP WEB TO CREASE BEAM ATTACH ANGLE, BS 807 - BS 827, S17L. REPLACED CUSP WEB TO CREASE BEAM ATTACH ANGLE, BS 807 - BS 827, S17L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007101200139 20071012 00139 NM 2007 10 12 SWAA074947 1 20071003 A 5315 147A55067 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 753SW 29848 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 40. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007101200140 20071012 00140 NM 2007 10 12 SWAA074948 1 20071003 A 2560 33500003 GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 753SW 29848 DURING SCHEDULED 8Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIPS WORN AT MID CABIN. REMOVED AND REPLACED STRIPS PER MM. 2 L 7 2 4F RT A16WE 2007101200141 20071012 00141 NM 2007 10 12 SWAA074921 1 20071003 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 405WN 27893 EEPLS LENS MISSING AT ROW 15 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007101200143 20071012 00143 NM 2007 10 12 SWAA074937 1 20071003 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM BS 727E-750E CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727E AND BS 750E, STR 19R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007101200145 20071012 00145 NM 2007 10 12 SWAA074919 1 20071003 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 947 S25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007101200146 20071012 00146 NM 2007 10 12 SWAA074920 1 20071003 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 947 S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007101200149 20071012 00149 NM 2007 10 12 SWAA074935 1 20071003 A 5330 6545866 SKIN BOEING 737 7373A4 1384585 NM BS 701 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED C3 CHECK, FOUND RIGHT KEEL BEAM PANEL CRACKED AT BS 701. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007101200150 20071012 00150 NM 2007 10 12 SWAA074954 1 20071003 A 5311 6546301 FRAME BOEING 737 7373H4 1384600 NM BS 188 S17R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 188, STR 17R. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007101200154 20071012 00154 NM 2007 10 12 SWAA074946 1 20071003 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM BS 500C S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500C, STR 21L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007101200156 20071012 00156 NM 2007 10 12 SWAA074934 1 20071003 A 5320 6546568 STIFFENER BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD LEFT LOWER CENTER RADIAL STIFFENER CRACKED. REPAIRED STIFFENER PER ACO. 2 L 7 2 4F RT A16WE 2007101200157 20071012 00157 NM 2007 10 12 SWAA074941 1 20071003 A 5311 6558280 FRAME BOEING 737 7375H4 138449D NM BS 360 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007101200158 20071012 00158 NM 2007 10 12 SWAA074939 1 20071003 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM BS 500B S22L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 22L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007101200159 20071012 00159 NM 2007 10 12 SWAA074951 1 20071003 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 344 S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007101200160 20071012 00160 NM 2007 10 12 SWAA074924 1 20071003 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 867 S6R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007101200161 20071012 00161 NM 2007 10 12 SWAA074952 1 20071003 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 294 S11L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007101200162 20071012 00162 NM 2007 10 12 SWAA074925 1 20071003 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 520 S14R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 14R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007101200166 20071012 00166 NM 2007 10 12 SWAA074930 1 20071003 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007101200169 20071012 00169 CE 2007 10 12 DXTA200702508 1 20070928 A 7500 31J285704 ACTUATOR CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE RT ENGINE BLEED INOPERATIVE E DXTA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 07 617QS 2887 5605509 PCEDD0016 RT EEC INOP ON TAKEOFF ROLL AND COULD NOT REACH TAKEOFF POWER SETTING IN MANUAL POSITION. REMOVED & REPLACED R/H BLEED TORQUE MOTOR. RAN A/C FOR LEAK & OPS CHECKS. SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME. ENG MAKES POD IN BOTH MANUAL & AUTO. ALL WORK DONE I.A.W. PWC 545B M/M 71-00-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007101200170 20071012 00170 CE 2007 10 12 DXTA200702507 1 20070928 A 3246 315381 WHEEL CESSNA 750 750 2076810 CE PWA JT15 JT15D5 52112 NE NLG OUT OF BALANCE E DXTA C ABORTED TAKEOFF E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 GL 07 961QS 786 786 7500061 DURING TAKEOFF, SEVERE NOSE WHEEL SHIMMY BEGAN AT 35 KTS. AS FORWARD NOSE PRESSURE RELEASED, SHIMMY GOT WORSE AND ABORT INITIATED AT 50 KTS. AHRS 1 AND 2 FAILED AND FORWARD EMER LIGHT ILLUMINATED. FOUND BOTH LT & RT NOSE WHEEL/TIRE UNBAL ANCED & TIRE WORN. REMOVED & REPLACED BOTH L&R NOSE WHEEL/TIRE ASSY IAW 750 M.M. CHAPTER 32-41-01. 2 L 7 2 4J 4 F RT T00007WI E25EA 2007101200171 20071012 00171 CE 2007 10 12 DXTA200702509 1 20070929 A 2720 EM407011 ACTUATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RUDDER INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 966QS 6063 7500166 ON CLIMB OUT, GOT A "RUDDER LIMIT FAIL A" MSG. FLIGHT CONTROL PAGE CONFIRMED 20 PERCENT LIMIT. REMOVED UPPER RUDDER L IMITER ACTUATOR AND INSTALLED NEW ACTUATOR I.A.W. THE 750 MM. CHAPTER 27-23-00. OPERATIONAL CHECK NORMAL. SCSC. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007101200173 20071012 00173 2007 10 12 DXTA200702511 4 20070930 A 3420 701700081161 COMPUTER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE FWD AVIONICS BAY INOPERATIVE E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 399QS 7415 5600510 COPILOT'S PFD SHOWED RED X'S ON ASI, ALT, AND VSI DURING TAKEOFF ROLL. REMOVED AND REPLACED THE COPILOTS IC-600 WITH E XCHANGE. PERFORMED OPERATIONAL TEST. OPERATION TESTS GOOD. WORK DONE IAW CESSNA 560 MM CH 34-23-02. 2 L 7 2 4F 4 F RT A22CE E25EA 2007101200174 20071012 00174 2007 10 12 DXTA200702512 4 20070930 A 2210 7002800901 ACTUATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL YAW DAMPER INOPERATIVE E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 930QS 3076 7500130 THE LOWER YAW DAMPER FAILED, A CAS MSG AT 60 KTS. REMOVED, REPLACED AND OPS CHECK GOOD OF LOWER YAW DAMP ACTUATOR "A" D UE TO INTERMITTENT FAILURE IAW 750 MM 27-24-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007101200175 20071012 00175 CE 2007 10 12 DXTA200702513 1 20070930 A 2130 6711351 SOLENOID CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL VENT DOOR INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 916QS 7256 7500116 CABIN VENT DOOR OPENED AND "CABIN DOOR OPEN" CAS MESSAGE CAME ON AFTER TAKEOFF. AIRCRAFT WOULD NOT PRESSURIZE. TROUBLE SHOT TO FAULTY VENT DOOR SOLENOID. REMOVED SOLENOID AND REPLACED WITH NEW. OPERATIONAL CHECKS GOOD. MAINT IAW CC 750 MM CHPTR 52-10-07. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007101200176 20071012 00176 SO 2007 10 12 SIMA200727408 1 20070929 A 3230 355022002 ELECTRONIC UNIT EMB 135 EMB135KL 3260302 SO MLG MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 811AE 145529 AFTER TAKEOFF, CREW TRIED TO RETRACT THE GEAR AND NOTHING HAPPENED. NO SINK RATE WAS BELOW 200 FT/MIN. INSPECTED LANDI NG GEAR AND FOUND NLG DOWN LOCK PROX SWITCHES OUT OF ADJUSTMENT. ADJUSTED NLG DOWN LOCK SWITCHES IAW EMB MM 32-63-05-70 0-804-A. ALSO REMOVED AND REPLACED LANDING GEAR ELECTRONIC CONTROL UNIT IAW EMB MM 32-32-01-000-801-A. PERFORMED GEAR RE TRACT IAW EMB MM 32-30-00-710-001 LANDING GEAR SYSTEM OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT T00011AT 2007101200177 20071012 00177 NM 2007 10 12 UPS07650847 1 20070920 A 5311 143T105145 FRAME BOEING 767 76734AF 1385212 NM BS 654 S7L PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 328UP 27754 INSPECTION TYPE:C1 FRAME BENT AND PUNCTURED STA 654+66 STR 7L. CUT OUT DAMAGED, FABRICATED & INSTALLED REPAIR PARTS PER ER 07-3560. 2 L 7 2 4F RT A1NM 2007101200178 20071012 00178 NM 2007 10 12 UPS07650848 1 20070923 A 5347 143T52405 SEAT TRACK BOEING 767 76734AF 1385212 NM BS 527 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 329UP 27755 INSPECTION TYPE:C1 FUSELAGE UPPER LOBE, CORROSION ON I/B FLANGE OF SEAT TRACK AT NUT PLATE HOLE, BS 527, LBL 55, WL 200. BLENDED CORROSION, FABRICATED & INSTALLED REPAIR PARTS PER ER 07-3583. 2 L 7 2 4F RT A1NM 2007101200179 20071012 00179 NM 2007 10 12 UPS07650849 1 20070923 A 5347 143T52405 SEAT TRACK BOEING 767 76734AF 1385212 NM BS 527 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 328UP 27754 INSPECTION TYPE:C1 FUSELAGE UPPER LOBE, CORROSION ON I/B FLANGE OF SEAT TRACK AT NUT PLATE HOLE, BS 527, LBL 55, WL 200. BLENDED CORROSION, FABRICATED & INSTALLED REPAIR PARTS PER ER 07-3583. 2 L 7 2 4F RT A1NM 2007101200180 20071012 00180 WP 2007 10 12 UPS07850852 1 20070918 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FS 1781 L17L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 L17L CRACKED BEHIND END FITTING IN 60 COMPT. REMOVED, FABRICATED, AND INSTALLED REPAIR LONGERON SEGM ENT AT L17L IN 60 COMPT IAW DWG S1616757, AND SRM 53-5-1 FIG 1. 2 L 7 4 4F RT 4A25 2007101200181 20071012 00181 WP 2007 10 12 UPS07850854 1 20070922 A 5313 LONGERON SPLICE DOUG DC8 DC873F 302199F WP FS 1050 L31L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 LONGERON SPLICE FITTING CRACKED AT STA 1050 L31L. REMOVED, AND REPLACED LONGERON SPLICE FITTING AT S TA 1050 L31L IAW SRM 51-01-20D. 2 L 7 4 4F RT 4A25 2007101200182 20071012 00182 WP 2007 10 12 UPS07850855 1 20070926 A 5753 ATTACH ANGLE DOUG DC8 DC873F 302199F WP TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 RIGHT WING AT STA 3 FITTING ATTACH L-ANGLE IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPAIR L-A NGLE AT RIGHT WING FLAP STA 3 IAW DWG 5643117, AND SRM 51-03-00. 2 L 7 4 4F RT 4A25 2007101200183 20071012 00183 WP 2007 10 12 UPS07850856 1 20070921 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FS 65 L21L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 STA 65 L21L, L-1 DOOR THRESHOLD AFT CORNER CRACKED AT RADIUS. STOP DRILLED CRACK IAW SRM 53-2-00 FIG 001B. FABRICATED AND INSTALLED REPAIR ANGLE AT STA 65 L21L L-1 DOOR AFT LWR CORNER IAW SRM 53-02-00 FIG 001B. 2 L 7 4 4F RT 4A25 2007101200184 20071012 00184 WP 2007 10 12 UPS07850857 1 20070918 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FS 902 L10R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 902 L10R. REMOVED, FABRICATED AND INSTALLED REPAIR END FITTING A T STA 902 L10R IAW DWG 3779658, AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 2007101200185 20071012 00185 WP 2007 10 12 UPS07850858 1 20070922 A 5313 LONGERON SPLICE DOUG DC8 DC873F 302199F WP FS 1265 L34R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 LONGERON SPLICE FITTING CRACKED AT STA 1265 L34R. REMOVED AND REPLACED LONGERON SPLICE FITTING AT ST A 1265 L34R IAW SRM 51-1-24, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007101200186 20071012 00186 NM 2007 10 12 SWAA074929 1 20071003 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 520 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007101200187 20071012 00187 NM 2007 10 12 HNAA0700204 1 20070609 A 5410 85410741107 HEAT SHIELD DHAV DHC8 DHC8102 2809003 NM NACELLE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 907HA 011 HEAT SHIELD PANEL AND STRAP AFT NACELLE STRUCTURE CORRODED. LEFT NACELLE FABRICATED PER DRAWING 85410741, 85411027 INST ALLED PER SRM 51-40-00. 2 H 7 2 4T RT A13NM 2007101200188 20071012 00188 NM 2007 10 12 HNAA0700207 1 20070609 A 2760 82700500001 CONTROL CABLE DHAV DHC8 DHC8102 2809003 NM LT SPOILER WORN A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 907HA 011 LEFT SPOILER OUTBOARD (UPPER AND LOWER) CABLES AND SPOILERS INBOARD UPPER CABLE WORN TO LIMIT. REMOVED AND REPLACED OUT BOARD (UPPER AND LOWER) CABLES AND SPOILER INBOARD UPPER CABLE AS PER AMM 27-14-00 SPOILER WING & FUSELAGE CABLES RIGGED PER AMM 27-14-00, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007101200189 20071012 00189 WP 2007 10 12 UPS07850871 1 20070922 A 5230 SUPPORT ANGLE DOUG DC8 DC873F 302199F WP CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 LATCH SPOOL FITTING SUPPORT ANGLE CORRODED AT FWD SIDE OF NR 4 LATCH SPOOL. REMOVED AND REPLACED FIT TING IAW SRM 51-3-0. 2 L 7 4 4F RT 4A25 2007101200190 20071012 00190 NM 2007 10 12 HNAA0700201 1 20070609 A 5347 85320430135 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 182-264 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 907HA 011 RIGHT SEAT TRACK RAILS FOUND CORRODED BETWEEN STA X 182 TO X 264. RIGHT SEAT RAIL REMOVED AND REPLACED WITH SOLID RIVET S IAW SRM 51-40-00 AND BOLTS IAW AMM 20-14-00. 2 H 7 2 4T RT A13NM 2007101200191 20071012 00191 NM 2007 10 12 HNAA0700202 1 20070609 A 5313 85320873103 STRINGER SPLICE DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 907HA 011 CORROSION ON ORIGINAL STRINGER SPLICE BELOW LAV SERVICE BOX. STRINGER SPLICE BELOW LAV SERVICE BOX FABRICATED IAW 85320 873. CORROSION AROUND RIB ANGLE UNDER LAV FLOOR BELOW LAV SERVICE BOX REMOVED AND REPROTECTED AND FOUND WITHIN LIMITS I AW SRM 53-00-16. ANGLE REPLACED AND INSTALLED IAW 51-40-00. 2 H 7 2 4T RT A13NM 2007101200192 20071012 00192 NM 2007 10 12 WRLA2007103 1 20071005 A 3320 BALLAST DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE ROW 10/11 FAILED A WRLA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 804DE 48475 EDDP/OKBK ROW 10 & 11 SEATS A, B & C OVERHEAD CEILING LIGHT ABOVE & BEHIND LUGGAGE BIN WAS HOT WITH BURNING PLASTIC ODOR LIGHT WAS DISCONNECTED. 10-18-07 R & R BALLAST. 2 L 7 3 4F 4 F RT A22WE E24NE 2007101200193 20071012 00193 NM 2007 10 12 HNAA0700203 1 20070609 A 5330 PAGY2J9341 BLANKING PLATE DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 907HA 011 DOUBLER AND BLANKING PLATE OF RADIO ALT AFT ANTENNA FOUND CORRODED. DOUBLER AND BLANKING PLATE OF RADIO ALT LOCALLY FAB RICATED AS PER SAMPLE. INSTALLED PER SRM 51-40-00. 2 H 7 2 4T RT A13NM 2007101200194 20071012 00194 NM 2007 10 12 SWAA075003 1 20071007 A 5312 6545819 PRESSURE PANEL BOEING 737 7373A4 1384585 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND LEFT NLG W/W CEILING PANEL CRACKED AT BS 250 RBL 7.5. REPAIRED CEILING PANEL PER SRM. 2 L 7 2 4F RT A16WE 2007101200195 20071012 00195 NM 2007 10 12 HNAA0700205 1 20070609 A 7600 87600513001 CONTROL CABLE DHAV DHC8 DHC8102 2809003 NM LT ENGINE WORN A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 907HA 011 LEFT ENGINE CONDITION CONTROL UPPER CABLE AND POWER CONTROL UPPER AND LOWER CABLES ARE WORN TO LIMIT. ENGINE 1 UPPER CO NDITION CABLE AND BOTH POWER CONTROL CABLES REPLACED AS PER 76-10-11 AND TASK 76-00-00. 2 H 7 2 4T RT A13NM 2007101200196 20071012 00196 NM 2007 10 12 SWAA074942 1 20071003 A 5311 65C33509 FRAME BOEING 737 7375H4 138449D NM BS 400 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 9L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007101200197 20071012 00197 NM 2007 10 12 SWAA074940 1 20071003 A 5311 65C34355 FRAME BOEING 737 7375H4 138449D NM BS 482 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007101200198 20071012 00198 NM 2007 10 12 SWAA074949 1 20071003 A 5315 BAC1509100046 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 772 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 605SW 27956 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 772, RBL 8. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007101200199 20071012 00199 2007 10 12 SWAA074933 4 20071003 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007101200200 20071012 00200 NM 2007 10 12 SWAA074922 1 20071003 A 2560 P4010021 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 413WN 29819 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2007101500011 20071015 00011 NM 2007 10 15 SWAA075012 1 20071008 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM BS 801 S19L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 801, STR 19L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007101500013 20071015 00013 NM 2007 10 15 SWAA075014 1 20071008 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 766SW 29806 DURING SCHEDULED CABIN VISIT, FOUND L2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007101500015 20071015 00015 NM 2007 10 15 SWAA075002 1 20071007 A 5312 6545819 PRESSURE PANEL BOEING 737 7373A4 1384585 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND RIGHT NLG W/W CEILING PANEL CRACKED AT BS 250 RBL 7.5. REPAIRED CEILING PANEL PER SRM . 2 L 7 2 4F RT A16WE 2007101500016 20071015 00016 NM 2007 10 15 HNAA0700199 1 20070608 A 5320 85320686101 THRESHOLD DHAV DHC8 DHC8102 2809003 NM PAX DOORWAY CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 907HA 011 PAX DOOR ENTRANCE THRESHOLD CORRODED. DOOR SEAL REMOVED, PAX DOOR THRESHOLD REMOVED AND REPLACED PER SRM 51-40-00, DOOR SEAL INSTALLED PER AMM 52-05-11. 2 H 7 2 4T RT A13NM 2007101500017 20071015 00017 SO 2007 10 15 C2XA07TY055 1 20071005 A 3350 2013BR BATTERY PACK EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16149 145753 TYS - DURING ROUTINE MAINTENANCE VARIOUS EMERGENCY LIGHTS WERE FOUND NOT WORKING. THE NR 1 BATTERY PACK WAS REMOVED AND REPLACED IAW EMB 145XR AMM 33-50-04. OPS CHECKS WERE GOOD AND THE A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT 2007101500018 20071015 00018 WP 2007 10 15 UPS07850864 1 20070920 A 5340 564348350LN FITTING DOUG DC8 DC873F 302199F WP FS 878 L22R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 FRAME FITTING CRACKED AND EXFOLIATION CORROSION AT STA 878 L22R. REMOVED AND REPLACED FRAME FITTING AT STA 878 L22R IAW SRM 51-3-2 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007101500019 20071015 00019 WP 2007 10 15 UPS07850867 1 20070920 A 5340 FITTING DOUG DC8 DC873F 302199F WP FS 1120 L20R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 FITTING CRACKED AT STA 1120 L20R AFT SIDE. REMOVED AND REPLACED FITTING AT STA 1120 L20R IAW SRM 51- 1-20D AND SRM 51-03-02. 2 L 7 4 4F RT 4A25 2007101500022 20071015 00022 NM 2007 10 15 UPS07M50860 1 20070829 A 5320 SUPPORT DOUG MD11 MD11F 3023600 NM BS 1359 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C CORROSION ON SUPPORT FLANGE OF LWR CTR FUEL TANK UPPER SURFACE AT STA1359 X=-100. CORROSION REMOVED 0 .073" X L=4.75" X W=1.5", MATL ORG THK 0.269", REMN 0.196" & FOUND OUT OF LIMITS PER SRM 53-00-01 FIG 1A VI R38. FPI C/ O PER DACNDTS PM REV13 PART08 ON BLEND OUT AREA, NO CORR & CRACK FOUND. FLAP PEENING C/O ON REWORKED AREA PER EN1561-07 . REWORK AREA REPROTECTED W/ VAPOR BARRIER COATING & SEALANT. LEAK CHECK C/O PER AMM28-11-00R50, SATISFACTORY. 2 L 7 3 4F RT A22WE 2007101500027 20071015 00027 NM 2007 10 15 UPS07550830 1 20070924 A 5311 70750080C FRAME BOEING 757 75724APF 1384969 NM BS 1480 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 434UP 25465 INSPECTION TYPE:C DENT IN AFT CARGO COMP FUSELAGE FRAME STA 1480 BETWEEN S26L AND S27L. REPAIRED FRAME PER SRM 53-00-09 T/R53-09. REPAIR CATEGORY-B REPAIR REQUIRES REINSPECTION PER SRM 53-00-07 ZONE 1 DETAIL V FIG 201 SHEET 12 OF 15. TAB LE II FIG 201 SHEET 10 OF 15. 37,500 FLIGHT CYCLES FROM REPAIRED INSTALLED. 2 L 7 2 4F RT A2NM 2007101500029 20071015 00029 NM 2007 10 15 UPS07550832 1 20070922 A 5311 70750080C FRAME BOEING 757 75724APF 1384969 NM BS 1520 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 434UP 25465 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1520, BETWEEN S26L TO S27L. REPAIRED PER SRM 53-00-07 R/R 53-09 REPAIR CATEGORY B REPAIR RE-INSPECTION REQUIRED PER SRM 53-00-07 ZONE 2 DETAIL V FIG 201 SHEET 12 OF 15 TABLE II FIG 201 SHEET 10 OF 15. 25,000 FLIGHT CYCLES AFTER REPAIR INSTALLED. 2 L 7 2 4F RT A2NM 2007101500031 20071015 00031 EA 2007 10 15 MASA200700370 1 20070627 A 3230 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 646BR 7392 ASH 1034 HNL. RETURNED TO THE FIELD AND DECLARED AN EMERGENCY DUE TO A GEAR DISAGREE AFTER TAKEOFF. MX REPLACED THE PR IORITY VALVE AND SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2007101500032 20071015 00032 SO 2007 10 15 C2XA07CL086 1 20071008 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NLG INTERMITTENT A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 15912 145439 CLE FLIGHT 3018 - THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. THE AIRCRAFT DIVERTED INTO CL E AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR WOW PROXIMITY SWITCH AND SERVICED THE N OSE LANDING GEAR STRUT. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007101500033 20071015 00033 EA 2007 10 15 MASA200700392 1 20070703 A 5210 LATCH CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF ADJUST A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7264V 7264 ASH 2834 TUS. MAIN CABIN DOOR HARD TO OPEN. MX ADJUSTED DOOR HANDLE LATCH AND DOOR COUNTER BALANCE. 2 L 7 2 4F RT A21EA 2007101500034 20071015 00034 EA 2007 10 15 MASA200700443 1 20070721 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STIFF A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37228 7228 ASH 2775 PHX. PAX DOOR DIFFICULT TO OPEN AND CLOSE. FERRIED A/C TO TUS FOR TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 2007101500036 20071015 00036 EA 2007 10 15 MASA200700449 1 20070723 A 4900 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA APU UNKNOWN A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 649BR 7414 ASH RON DTW. PILOT REPORTED THAT UPON STARTING THE APU, NOTICED A STRONG FUEL ODOR IN THE COCKPIT AND CABIN, AND ABORTE D THE START SEQUENCE. NO ODOR NOTED. 2 L 7 2 4F RT A21EA 2007101500038 20071015 00038 NM 2007 10 15 WRLA2007102 1 20071005 A 5730 ARB2886504 SKIN DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE RT WING CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 273WA 48519 DURING 4C + 12A CHECK FOUND RIGHT WING FIXED L/E SKIN CRACK AT CORNERS OF CUTOUT L=0.3 INCH, AT STA XOS 464 L=0.5 INCH S TA XOS 470. 10-25-07 REPAIRED THE RT WING FIXED LEADING EDGE SKIN CRACK AT CORNERS OF CUTOUT AT STA XOS=464,470 PE R MD11 SRM VOL.I 57-10-00 FIGURE 43 REV.40. 2 L 7 3 4F 4 F RT A22WE E24NE 2007101500040 20071015 00040 NM 2007 10 15 UPS07650846 1 20070920 A 5314 145T86292 SUPPORT ANGLE BOEING 767 76734AF 1385212 NM BS 827-877 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 328UP 27754 INSPECTION TYPE:C1 LOWER FUSELAGE, KEEL BEAM PANEL SUPPORT ANGLE HAS SURFACE CORROSION COMMON TO NUT PLATE LOCATIONS, BS 827, BS 877, BLENDED CORROSION. FABRICATED & INSTALLED REPAIR PARTS PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007101500042 20071015 00042 NM 2007 10 15 WRLA2007104 1 20071006 A 2120 UNKNOWN DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE COCKPIT ODOR A WRLA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 278WA 48746 FLT 1001 FNLU/KIAH. DURING CRUISE FLT 9+20HRS AFTER DEPART ELEC ODOR EMANATING NEAR INSTRUMENT PANEL. NO SMOKE WAS OBS ERVED. SOURCE OF ODOR UNKNOWN. ELEC ODOR DISSIPATED OVER TIME. SEL ANNUNCIATOR LIGHT TEST IND MASTER WARNING, MASTER CAUTION AND ABS DISARM WARNING LIGHTS WILL NOT TEST IN CRUISE. HOWEVER, ENG/APU FIRE TEST ILLUM WHEN COMMANDED BY OTHER LVL 2 CONDITIONS. 2 L 7 3 4F 4 F RT A22WE E24NE 2007101500043 20071015 00043 EA 2007 10 15 MASA200700539 1 20070831 A 5210 TRACK CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DIRTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 97325 7325 MAIN DOOR WILL NOT OPEN. CLEANED TRACKS AND PINS. 2 L 7 2 4F RT A21EA 2007101500044 20071015 00044 EA 2007 10 15 MASA200700547 1 20070903 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA SMOKE A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 7264V 5552 7264 CREW REPORTED SMOKE IN CABIN ON GROUND. CREW DE-PLANED PASSENGERS UNDER NORMAL CONDITIONS. MX REMOVED AND REPLACED AM AND RAM AIR CHECK VALVE, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007101500045 20071015 00045 EA 2007 10 15 MASA200700551 1 20070904 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77331 7331 PAX DOOR WILL NOT OPEN. MX LUBED AND CYCLED DOOR, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007101500046 20071015 00046 EA 2007 10 15 MASA200700553 1 20070904 A 2560 P487220187220021 BATTERY CNDAIR CL600 CL6002B19 1900309 EA FLASHLIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75994 7367 AFT F/A EMERGENCY FLASHLIGHT IS INOP. MX CHANGED BATTERY. 2 L 7 2 4F RT A21EA 2007101500047 20071015 00047 EA 2007 10 15 MASA200700574 1 20070913 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA RIGHT HOT A MASA O OTHER M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 SW 07 75984 19114 7489 ASH FLT 7212 ORD. RT PACK HOT, SMOKE IN TOILET WITH ASSOCIATED CAUTION MESSAGE. REMOVED AND REPLACED ACM. 2 L 7 2 4F RT A21EA 2007101500048 20071015 00048 WP 2007 10 15 UPS07850868 1 20070921 A 5230 37730521N FITTING DOUG DC8 DC873F 302199F WP BS 130 L21L CRACKED A IPXA K NONE O I OTHER FLT. ATTITUDE INST. IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 FITTING CRACKED INSIDE MCD JAMB TORQUE BOX AT STA 130 L21L. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-03-02, 51-03-0, 51-1-21, AND 51-01-20D. 2 L 7 4 4F RT 4A25 2007101500050 20071015 00050 NM 2007 10 15 SWAA074976 1 20071007 A 5312 6545819 PRESSURE PANEL BOEING 737 737301 1384611 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED C1 CHECK, FOUND LNG W/W CEILING PANEL WEB CUTOUT CRACKED AT OUTBOARD END. REPAIRED WEB PER ACO. 2 L 7 2 4F RT A16WE 2007101500051 20071015 00051 NM 2007 10 15 SWAA074986 1 20071005 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM BS 380 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007101500052 20071015 00052 NM 2007 10 15 SWAA074987 1 20071005 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8L/R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007101500054 20071015 00054 NM 2007 10 15 SWAA074991 1 20071005 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM BS 867 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007101500055 20071015 00055 NM 2007 10 15 SWAA074990 1 20071005 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007101500056 20071015 00056 NM 2007 10 15 SWAA075001 1 20071007 A 5330 6550570 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRAKCED AT R2 DOOR UPPER HINGE CUTOUT AFT END. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007101500057 20071015 00057 2007 10 15 SWAA074995 4 20071007 A 2565 6557463 FITTING BOEING 737 7377H4 1384404 NM R1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 440LV 29835 R1 DOOR EMERGENCY EVAC SLIDE FORWARD GIRT BAR FITTING LOOSE. SECURED FITTING PER MM. 2 L 7 2 4F RT A16WE 2007101500060 20071015 00060 NM 2007 10 15 SWAA074982 1 20071007 A 5755 FITTING BOEING 737 7373H4 1384600 NM NR 4 SPOILER WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 14Y CHECK, FOUND LEFT WING NR 4 SPOILER INBOARD ACTUATOR FITTING WORN. REPAIRED SPOILER PER SRM. 2 L 7 2 4F RT A16WE 2007101500061 20071015 00061 WP 2007 10 15 UPS07850809 1 20070914 A 5340 ATTACH ANGLE DOUG DC8 DC873F 302199F WP FS 1766 L6R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 AFT PRESS BULKHEAD ATTACH ANGLE CRACKED AT STA 1766 L6R. REMOVED, FABRICATED, AND INSTALLED REPAIR A TTACH ANGLE AT STA 1766 L6R AFT PRESS BULKHEAD IAW DWG 5773844, AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 2007101500062 20071015 00062 WP 2007 10 15 UPS07850824 1 20070927 A 5330 SKIN DOUG DC8 DC873F 302199F WP FS -80 L19L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 SKIN DENTED AND CRACKED AT STA -80.00 LT SIDE. REPAIRED FUSELAGE SKIN CRACK AT STA -80.00 LT SIDE IA W SRM 51-1-21 53-2-1, SRM 53-02-01 FIG 7. 2 L 7 4 4F RT 4A25 2007101500064 20071015 00064 WP 2007 10 15 UPS07850827 1 20070920 A 5340 4750419U501 FITTING DOUG DC8 DC873F 302199F WP BS 1228 L19R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 FITTING CRACKED AT STA 1228 L19R FWD SIDE. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51- 1-24. 2 L 7 4 4F RT 4A25 2007101500065 20071015 00065 WP 2007 10 15 UPS07850828 1 20070922 A 5340 3750257U503 FITTING DOUG DC8 DC873F 302199F WP BS 1050 L31L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C2 LONGERON SPLICE FITTING CRACKED AT STA 1050 L31L. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-03-00, 51-1-20D, AND 51-1-24. 2 L 7 4 4F RT 4A25 2007101500066 20071015 00066 WP 2007 10 15 UPS07850829 1 20070915 A 5540 MOUNT DOUG DC8 DC873F 302199F WP STATIC WICK DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 LIGHTNING STRIKE DAMAGE ON/AROUND STATIC WICK BASE ON RUDDER T/E AT TOP LEFT SIDE. REMOVED, FABRICAT ED AND INSTALLED REPLACEMENT END CAP ON TOP OF RUDDER IAW SRM 51-1-21, 55-2-0, 51-1-21A, 51-1-8, AND DWG 5654883. 2 L 7 4 4F RT 4A25 2007101500067 20071015 00067 NM 2007 10 15 UPS07M50810 1 20070803 A 5320 BRACKET DOUG MD11 MD11F 3023600 NM BS 1236 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C LEFT UNDERSIDE CANTED PANEL AREA AT STA 1236.0 FOUND CANTED PANEL BRACKET CRACKED AS MARKED. REMOVED LWR AUX BLADDER CELL DECKING PANEL LEFT AT STA 1236.0 FOR S/M ACCESS. FTG AT STA 1236 FRAME TO CANT PANEL REMOVED FOR A CCESS. EXISTING CRACKED BRACKET REMOVED. NEW BRACKET FASTENER HOLES PICKED UP & INSTALL. FTG AT STA 1236 FRAME TO CAN T PANEL REINSTALLED. LOWER AUX BLADDER CELL DECKING PANEL LINER AT LEFT STA 1236 REINSTALLED. 2 L 7 3 4F RT A22WE 2007101100198 20071011 00198 NM 2007 10 11 AMTA200700477 1 20071003 A 3244 TIRE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE NR 4 MLG DAMAGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 517AT 27973 UPON AC ARRIVAL FOUND NR 4 MAIN TIRE MISSING 80 PERCENT OF THE CAP. REMOVED AND REPLACED NR 4 MLG TIRE AND WHEEL IAW MM 32-45-01-4. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007101100200 20071011 00200 WP 2007 10 11 AMTA200700478 1 20071004 A 5100 UNKNOWN LKHEED 1011 10113853 5265020 WP RROYCE AVON AVON524B 54517 EU UNKNOWN A AMTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 11 162AT 1220 REJECTED T/O, SPEED 70 KTS, WEIGHT 380.0 LBS. PERFORMED CLAPPER LUB IAW MM 72-31-05. INSPECTED MASTER GB CHIP DETECTOR , NO DEBRIS DETECTED. NO EVIDENCE OF ENG FAILURE. NR 3 ENG. (K) 2 L 7 3 4F 4 J A23WE E307 2007101100209 20071011 00209 CE 2007 10 11 DJFA2007109 1 20070916 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 467LX 1385 RK447 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER IB RIB AND BRACKET ASSEMBLIES, BOTH THE RT AND LT IB ROLLER BRACKETS WERE FOUND CRACKED. DETAILED INSPECTION INSTR UCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. MAINTENANCE REPLACED BOTH RIBS WITH THE UPGRADED ASSEMBLIES. 2 H 7 2 4F RT A16SW 2007101100210 20071011 00210 EU 2007 10 11 BAQA200700032 1 20070924 A 5302 1053040212 FITTING BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1E 60034 NE T/R GEARBOX CRACKED E BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 911TG 6943 7506 TAILROTOR GEAR BOX MOUNT FITTING AT TOP OF VERTICAL FIN CRACKED AND TAIL ROTOR GEAR BOX MOUNTING STUD ROSSET FITTING LOO SE. 1 G 7 2 3U 3 U NC H13EU E19EU 2007101100217 20071011 00217 EU 2007 10 11 COEA0707821 1 20070828 A 5310 S53673000205 CREASE BEAM AEROSP ATR72 ATR72202 8680940 EU FUSELAGE DAMAGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. FOUND TOOLING DAMAGE FIVE PLACES ON CREASE BEAM WEB. FABRICATED AND INSTALLED REPLACEMENT CR EASE BEAM WEB. (K) 2 H 7 2 4T RT A53EU 2007101100223 20071011 00223 CE 2007 10 11 A9J2007F00000 1 20070826 A 3040 6600393004 SENSOR LEAR 35 31A 5170531 CE GARRTT TFE731 TFE731* 01518 WP WINDSHIELD FAILED E A9JA O OTHER O OTHER NR NOT REPORTED 1 EA 13 3VJ 400 035 ALL SENSORS ON A NEW WINDSHIELD FAILED. THERE ARE A TOTAL OF 400 HRS SINCE NEW. (K) 2 L 7 2 4F 4 F RT A10CE E6WE 2007101200014 20071012 00014 WP 2007 10 12 UPS07850777 1 20070913 A 5330 SKIN DOUG DC8 DC873F 302199F WP FS 1746 L17L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 FUSELAGE SKIN CRACKED AT STA 1746 L17L. REPAIRED FUSELAGE SKIN AT STA 1746 L17L IAW SRM 53-02-01-0 F IG 7. THIS REPAIR IS A CLASS 2 REPAIR. 2 L 7 4 4F RT 4A25 2007101200022 20071012 00022 NM 2007 10 12 CALA0700547 1 20070930 A 5322 6941602501 SHEAR TIE BOEING 737 7373T0 1384582 NM BS 947 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT STA 947 BETWEEN STRINGERS 23L AND 24L. THE SHEAR TIE WAS R EMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007101200023 20071012 00023 NM 2007 10 12 CALA0700548 1 20071001 A 5330 6545775594 SKIN BOEING 737 7373T0 1384582 NM BS 727D S23R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A 0.5 INCH CRACK IN FUSELAGE SKIN AT STA 727D +3 BELOW STRINGER 23R. A DOUBLER WAS INSTALLED IAW ECRA 5330-03730 AND SRM 53-00-01, FIGURE 201, REPAIR 31. 2 L 7 2 4F RT A16WE 2007101200029 20071012 00029 NM 2007 10 12 SWAA074896 1 20071001 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 752SW 29804 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 15 TO RBL 25. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2007101200030 20071012 00030 NM 2007 10 12 SWAA074899 1 20071001 A 5315 149A5510 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 753SW 29848 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 20. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007101200031 20071012 00031 NM 2007 10 12 SWAA074856 1 20070930 A 3350 3071BPEGPL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED MV3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007101200036 20071012 00036 NM 2007 10 12 SWAA074887 1 20071001 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 226WN 32494 EEPLS LENS LOOSE AT ROW 3 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007101200039 20071012 00039 NM 2007 10 12 SWAA074885 1 20071001 A 5330 6545765 SKIN BOEING 737 7373T0 1384582 NM BS 520 S28L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007101200043 20071012 00043 2007 10 12 SWAA074897 4 20071001 A 2565 6557463 FITTING BOEING 737 7377H4 1384404 NM R1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 783SW 29809 R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER MM. 2 L 7 2 4F RT A16WE 2007101200046 20071012 00046 NM 2007 10 12 SWAA074864 1 20070930 A 3350 65C27093 LIGHT BOEING 737 737317 138447P NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007101200047 20071012 00047 NM 2007 10 12 SWAA074855 1 20070930 A 3350 65C27093 LIGHT BOEING 737 7373K2 13844BA NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007101200048 20071012 00048 NM 2007 10 12 SWAA074872 1 20071001 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 277 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007101200059 20071012 00059 NM 2007 10 12 SWAA074868 1 20070930 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727C S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007101200062 20071012 00062 NM 2007 10 12 SWAA074878 1 20071001 A 5311 65C34355 FRAME BOEING 737 7375H4 138449D NM BS 482A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007101200063 20071012 00063 NM 2007 10 12 SWAA074886 1 20071001 A 5330 65C381921 SKIN BOEING 737 7373Q8 1384670 NM BS 375 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 375, STR 8L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007101200067 20071012 00067 2007 10 12 SWAA074882 4 20071001 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 607SW 27927 DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007101200069 20071012 00069 SO 2007 10 12 C2XA07IA214 1 20071001 A 3240 429513 CONTROL UNIT EMB 145 EMB145LR 3260212 SO BRAKES INOPERATIVE A C2XA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 14916 15527 15527 145415 IAH - FLIGHT 2802, DURING TAXI THE CREW REPORTED A BRAKE OUTBOARD MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO THE GATE W HERE MAINTENANCE REMOVED AND REPLACED THE BRAKE CONTROL UNIT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WA S APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007101200072 20071012 00072 NM 2007 10 12 2007UALA03895 1 20070925 A 7160 VALVE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 1 ENGINE MISRIGGED A UALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 WP 29 825UA 980 V10189 ENGINE NR 1 COMPRESSOR STALL IN CRUISE. MISRIGGED VSV SYSTEM. ACP CHECKS PER MM 71-00-00 FOUND VSV UNISON RING MISRIGG ED AT VGV AND STAGE 5. ADJ 1 TURN EA, OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101200074 20071012 00074 EU 2007 10 12 2007UALA03908 1 20070926 A 2597 ELECTRICAL SYS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ESCAPE SLIDE FAULTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 434UA 592 EMERGENCY LIGHTS FAIL TEST, EPSU EXT FAULT. *S/D* ELECTRONICS INSIDE SLIDE PACK FAULTY. REPLACED DOOR 1L SLIDE PACK - ALL LIGHTS OPS CHECK NORMAL. NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101200080 20071012 00080 NM 2007 10 12 2007UALA03939 1 20070927 A 5310 6520723U54 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOORWAY DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 FWD CARGO DOOR CUTOUT AFT FRAME IS DAMAGED. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED FWD CARGO DOOR CUTOUT AFT FR AME. (P/N 65-20723U54) 2 L 7 2 4F 4 F RT A16WE E21EU 2007101200090 20071012 00090 NM 2007 10 12 CALA0700549 1 20071002 A 5313 65617777 STRINGER BOEING 737 7373T0 1384582 NM BS 360 S15L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A 5 INCH CRACK IN L-1 DOOR CUTOUT AFT SIDE STRINGER 15L AT STA 360. REPAIRED IAW ECRA 5311-01363. 2 L 7 2 4F RT A16WE 2007101200093 20071012 00093 NM 2007 10 12 CALA0700552 1 20071002 A 5320 69489854 SUPPORT BOEING 737 7373T0 1384582 NM BS 360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR AFT SIDE SUPPORT CLIP AT STA 360, S10L. THE CLIP WAS REMOVED AND REPLACED IAW ECRA 5311-01363. 2 L 7 2 4F RT A16WE 2007101200109 20071012 00109 NM 2007 10 12 CALA0700563 1 20071004 A 5230 6547952162 SKIN BOEING 737 7373T0 1384582 NM C-2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A .5 INCH CRACK IN C-2 DOOR OUTER SKIN AT DOOR HANDLE CUTOUT. THE CRACKED AREA OF SKIN WAS CUTOUT AND A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 52-00-01 AND 51-20-01. 2 L 7 2 4F RT A16WE 2007101200110 20071012 00110 NM 2007 10 12 HNAA0700188 1 20070904 A 5347 8533499102 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 597 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 839EX 226 CORROSION FOUND ON RIGHT SEAT TRACK AT STATION X597.500. RIGHT INBOARD SEAT TRACK REPLACED FROM STATION X526.500 TO X61 8.00. INSTALLED WITH SOLID RIVETS PER SRM 51-41-00. 2 H 7 2 4T RT A13NM 2007101200114 20071012 00114 NM 2007 10 12 HNAA0700190 1 20070824 A 5313 85300129101 STRINGER SPLICE DHAV DHC8 DHC8102 2809003 NM BS 531 S32R CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 943HA 167 CORROSION FOUND ON SPLICE STRINGER 32 RIGHT SIDE AT STA 531. SPLICE STRINGER 32 RIGHT AT 531 REPLACED WITH NEW PART LOC ALLY MADE AS PER DWG 85300129 AND INSTALLED. 2 H 7 2 4T RT A13NM 2007101200120 20071012 00120 SO 2007 10 12 LR7A07098 1 20070927 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FS 610 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 519 5025 DURING SCHEDULED B-3 CHECK FOUND PER JOB CARD HB3200 LT MLG BHD CRACKED AT FS 610, WL183, LBL 62. REPAIR ACCOMPLISHED I AW SMP583 FIG 53-40-10. 2 H 7 4 4T A1SO 2007101200123 20071012 00123 SO 2007 10 12 LR7A07101 1 20070927 A 5312 PRESSURE PANEL LKHEED 382 382G 526414U SO FS 577 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 519 5025 DURING SCHEDULED B-3 CHECK, WHEN REPAIRING RT MLG BEAM INNER CAP, FOUND A CRACKED PRESSURE WEB AT FS 577, WL 250, RBL 61 . REPAIR ACCOMPLISHED IAW LYNDEN AIR CARGO MEA 382-53-07-059. 2 H 7 4 4T A1SO 2007101200125 20071012 00125 NM 2007 10 12 USAA920070886 1 20070925 A 5230 SKIN BOEING 737 7373B7 1384580 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 517AU 23703 CLT - MAJOR REPAIR - C-3 CHECK - NR 6006731, AFT CARGO DOOR EXTERIOR SKIN CRACKED AT UPPER CORNER OF HANDLE CUTOUT. REP LACED AFT CARGO DOOR IAW USAIRWAYS JOB CARD J3-57-52301. 2 L 7 2 4F RT A16WE 2007101200127 20071012 00127 NM 2007 10 12 USAA920070888 1 20070920 A 5510 69730953 HINGE PIN BOEING 737 7374B7 1384702 NM HORIZONTAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 456UW 25020 CLT - MAJOR REPAIR - C-5 CHECK, CORROSION ON THE LEFT HORIZONTAL STABILIZER CENTER SECTION TO BODY OUTER HINGE PIN. REP LACED LEFT HORIZONTAL STABILIZER CENTER SECTION TO BODY OUTER HINGE PIN IAW B737-400 AMM 27-41-31. 2 L 7 2 4F RT A16WE 2007101200131 20071012 00131 NM 2007 10 12 USAA920070892 1 20070929 A 5340 69353523 STRINGER CLIP BOEING 737 7373G7 1384595 NM BS 947 S26R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6505163, CRACKED STRINGER CLIP, BS 947, S26R. REPLACED STRINGER CLIP, BS 947, S26R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007101200133 20071012 00133 NM 2007 10 12 USAA920070894 1 20070921 A 5315 69770163 STRINGER CLIP BOEING 737 7373G7 1384595 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6505244, CORROSION ON FLOORBEAM VERTICAL CLIP, BS 1016, LBL 41.0, WL 208.1. REPLAC ED FLOORBEAM VERTICAL CLIP, BS 1016, LBL 41.0, WL 208.1 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007101200142 20071012 00142 NM 2007 10 12 SWAA074923 1 20071003 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 459WN 32497 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007101200144 20071012 00144 NM 2007 10 12 SWAA074938 1 20071003 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM BS 750 S18R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007101200147 20071012 00147 NM 2007 10 12 SWAA074953 1 20071003 A 5311 6545816 FRAME BOEING 737 7373H4 1384600 NM BS 322 S20L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 322, STR 20L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007101200148 20071012 00148 NM 2007 10 12 SWAA074936 1 20071003 A 5330 6545866 SKIN BOEING 737 7373A4 1384585 NM BS 671 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED C3 CHECK, FOUND LEFT KEEL BEAM PANEL CRACKED AT BS 671. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007101200151 20071012 00151 NM 2007 10 12 SWAA074931 1 20071003 A 5753 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED HC1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007101200152 20071012 00152 NM 2007 10 12 SWAA074945 1 20071003 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM BS 500C S26L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500C, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007101200153 20071012 00153 NM 2007 10 12 SWAA074944 1 20071003 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM BS 500C S23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500C, STR 23L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007101200172 20071012 00172 CE 2007 10 12 DXTA200702510 1 20070929 A 7330 COMPUTER RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP NR 2 MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 07 815QS 258705 DURING TAKEOFF ROLL AT APPROXIMATELY V1 OF 111KIAS, THE NR2 COMPUTER FAILED (STEADY LIGHT) IT WAS ACCOMPANIED BY A ROLL BACK OF THE NR2 ENGINE AND A SUBSEQUENT APR TRIGGER (EVENT) DURING INITIAL CLIMBOUT. THE NR2 ITT READ 996 DEG FOR APPROX IMATELY 1 MINUTE UNTIL WE COULD PULL THE ENGINE BACK TO MAINTAIN LIMITS. 2 L 7 2 4F 4 F RT A3EU E6WE 2007101200201 20071012 00201 NM 2007 10 12 HNAA0700196 1 20070627 A 5320 85330499101 ANGLE DHAV DHC8 DHC8102 2809003 NM BS 636 CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 907HA 011 ANGLE CRACKED IN THE CARGO BAY AT FUSELAGE STA X618.00 AND Z114.5 ANGLE AT FUSELAGE STA X 618 Z 114.5 RT HAS BEEN DONE I AW DRAWING 85330499 INSTALLED PER SRM 51-40-00. 2 H 7 2 4T RT A13NM 2007101500001 20071015 00001 NM 2007 10 15 HNAA0700220 1 20070704 A 5730 SKIN DHAV DHC8 DHC8102 2809003 NM WING CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 940HA 156 CORROSION FOUND ON PANEL 623AT, 622AT, 521AT, 522AT, CORROSION LOCATED ON COUNTER SINKS. RD8-57-1420 COMPLETED ON PANEL 623AT, 523AT, 521AT. PANEL 522AT AND 622AT REPLACE INSTALLATION OF ALL PANELS W/C 05-00-21I MORE TO FOLLOW. 2 H 7 2 4T RT A13NM 2007101500002 20071015 00002 NM 2007 10 15 HNAA070028 1 20070609 A 2710 82700518001 CONTROL CABLE DHAV DHC8 DHC8102 2809003 NM AILERON WORN A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 907HA 011 LEFT AILERON INBOARD AND OUTBOARD WING REAR SPAR CABLES (UPPER AND LOWER) WORN TO LIMITS. LEFT WING INBOARD AND OUTBOAR D AILERON CABLES UPPER AND LOWER REMOVED AND REPLACED PER SRM 27-12-00. 2 H 7 2 4T RT A13NM 2007101500003 20071015 00003 NM 2007 10 15 HNAA0700210 1 20070609 A 2710 82700515001 CONTROL CABLE DHAV DHC8 DHC8102 2809003 NM AILERON WORN A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 907HA 011 RIGHT AILERON INBOARD AND OUTBOARD WING REAR SPAR WORN TO LIMITS. RIGHT INBOARD AND OUTBOARD AILERON CABLES REMOVED AND REPLACED IAW 27-12-00. 2 H 7 2 4T RT A13NM 2007101500004 20071015 00004 EA 2007 10 15 MASA200700469 1 20070731 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 931LR 15031 ASH 2604 CLT-ORF. EMERGENCY CEILING FLOOD LIGHT ROW 17 INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2007101500005 20071015 00005 EA 2007 10 15 MASA200700471 1 20070802 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17275 7275 ASH RON DSM. MX REPORTED THAT THE NR 4 EMERGENCY LIGHT BATTERY PACK WAS INOP. MX CLEANED AND RESECURED THE CONNECTION TO THE BATTERY PACK, OPS CHECK WAS NORMAL. 2 L 7 2 4F RT A21EA 2007101500006 20071015 00006 EA 2007 10 15 MASA200700472 1 20070802 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 593ML 7465 ASH 7155 ORD. 8A EMERGENCY LIGHTS & ROW 2-5 FLOOR PATH LIGHTS INOP. MX RESECURED WIRING. 2 L 7 2 4F RT A21EA 2007101500007 20071015 00007 EA 2007 10 15 MASA200700473 1 20070802 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 912FJ 15012 ASH 2726 LAS-SEA. OVERHEAD EMERGENCY EXIT LIGHT ROW 17 INOP. MX RELAMPED EMERGENCY LIGHT ASSY. 2 L 7 2 4F RT A21EA 2007101500008 20071015 00008 EA 2007 10 15 MASA200700474 1 20070803 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27173 7173 ASH 7185 CLE-IAD. PILOT REPORTED, THAT THE CEILING LEVEL EMERGENCY FLOOD LIGHT BETWEEN ROWS 4/5 WAS INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2007101500009 20071015 00009 NM 2007 10 15 SWAA075013 1 20071008 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007101500010 20071015 00010 NM 2007 10 15 SWAA075010 1 20071008 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 209WN 32484 EEPLS LENS MISSING AT RIGHT OVERWING EMERGENCY EXIT. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007101500012 20071015 00012 NM 2007 10 15 SWAA075011 1 20071008 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM BS 947 S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007101500014 20071015 00014 NM 2007 10 15 HNAA0700222 1 20070704 A 5246 85321086S059 ANGLE DHAV DHC8 DHC8102 2809003 NM LAV SERV DOOR CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 940HA 156 TOILET SERVICE PANEL DOOR ANGLE FOUND HEAVY CORRODED. REPLACED SERVICE DOOR AS PER SRM 51-40-00. 2 H 7 2 4T RT A13NM 2007101500021 20071015 00021 NM 2007 10 15 UPS07M50851 1 20070808 A 5730 SKIN DOUG MD11 MD11F 3023600 NM RWS 510 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C RIGHT WING LOWER SURFACE L/E ACCESS PANEL CUTOUT STRUCTURE AT STA XORS 51 0 APPROX FOUND CRACK AS MARK ED. HFEC INSP C/OUT & CRACK FOUND AS MARKED. CRACKED DOUBLER REMOVED. RIGHT WING LOWER SURFACE APPROX XORS 510 DOUBLE R FABBED USING MAT'L 7075T6-0.090" PER DOUGLAS DWG ARB2933. NEW DOUBLER FASTENER HOLES PICKED UP, REPROTECTED & PAINTED . NEW DOUBLER INSTALLED AS PER SRM 51-31-01 VOL II REV 38. 2 L 7 3 4F RT A22WE 2007101500023 20071015 00023 NM 2007 10 15 UPS07M50861 1 20070718 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM BS 5-113 L48 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C CENTER CARGO PIT ON L48 AT STA 5-113 FOUND CORROSION AS MARKED. CORR LONGERON L48 TRIM OFF FROM STA 5 -119 TO 5-103 PER SRM 53-10-00 VI R378. HFEC INSP C/O ON TRIM OFF AREA. NO CRACK FOUND. REPAIR LONGERON PARTS FAB, PE R EN1502-07, REPROTECTED AND PAINTED. STA 1541 LONG 48L CORR CUTOFF. HFEC INSP C/O ON CUTOFF AREA, NO CRACK FOUND. RE PAIR LONGERON & SPLICES FAB & INSTALLED PER EN1502-07 & SRM 51-31-01 VII R38. 2 L 7 3 4F RT A22WE 2007101500024 20071015 00024 NM 2007 10 15 HNAA0700208 1 20070609 A 2710 82700518001 CONTROL CABLE DHAV DHC8 DHC8102 2809003 NM AILERON WORN A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 907HA 011 LEFT AILERON INBOARD AND OUTBOARD WING REAR SPAR CABLES (UPPER AND LOWER) WORN TO LIMITS. LEFT WING INBOARD AND OUTBOAR D AILERON CABLES UPPER AND LOWER REMOVED AND REPLACED PER SRM 27-12-00. 2 H 7 2 4T RT A13NM 2007101500026 20071015 00026 NM 2007 10 15 UPS07550826 1 20071003 A 5610 HANDLE BOEING 757 75724APF 1384969 NM L2 WINDOW DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 INSPECTION TYPE:N/A DURING PREFLIGHT FOUND CAPTAIN'S L2 WINDOW CRANK HANDLE PIN/BOLT SHEARED. REINSTALLED WINDOW CRANK. SECURED WITH BOLT ASSY CLAMP PER MM 56-11-04-4, OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2007101500030 20071015 00030 NM 2007 10 15 UPS07550833 1 20070924 A 5330 SKIN BOEING 757 75724APF 1384969 NM BS 1480 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 448UP 27737 INSPECTION TYPE:C DENT IN AFT CARGO COMP FUSELAGE STA 1480 BETWEEN S24L AND S25L. REPAIRED FRAME PER SRM 53-00-07 T/R 5 3-09. THIS IS A CAT-B REPAIR REINSPECTION REQUIRED PER SRM 53-00-07 ONE 1 DETAIL V FIGURE 201 SHEET 12 OF 15 TABLE II F IG 201 SHEET 10 OF 15. 37,500 FLIGHT CYCLES AFTER INSTALLATION OF REPAIR. 2 L 7 2 4F RT A2NM 2007101500035 20071015 00035 EA 2007 10 15 MASA200700447 1 20070723 A 4900 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA APU UNKNOWN A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 649BR 7414 ASH 7178 IAD. AFTER APU START STRONG ODOR OF FUEL. MX OPS CHECKED NORMAL, NO ODOR NOTED. 2 L 7 2 4F RT A21EA 2007101500037 20071015 00037 EA 2007 10 15 MASA200700457 1 20070727 A 3250 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING UNKNOWN A MASA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 591ML 7388 ASH 7284 ORD-SBN. DECLARED AN EMERGENCY DUE TO A NOSE WHEEL STEERING FAULT IN FLIGHT. MX INSPECTED THE NOSE WHEEL STEE RING SYSTEM AND WERE UNABLE TO DUPLICATE THE FAULT. 2 L 7 2 4F RT A21EA 2007101500049 20071015 00049 WP 2007 10 15 UPS07850869 1 20070921 A 5340 37558201 FITTING DOUG DC8 DC873F 302199F WP BS 1380 L11L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 FITTING HAS DEEP PITTING, DEEP GOUGE AND POSSIBLE CRACK STA 1380 L11L. REMOVED AND REPLACED FITTING IAW SRM 51-3-0, 51-1-20D, AND 51-1-8. 2 L 7 4 4F RT 4A25 2007101500058 20071015 00058 2007 10 15 SWAA075000 4 20071007 A 2565 6557463 FITTING BOEING 737 7373H4 1384600 NM R2 DOOR GIRT BAR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CRACKED. REMOVED AND REPLACED FITTI NG PER MM. 2 L 7 2 4F RT A16WE 2007101500059 20071015 00059 NM 2007 10 15 SWAA074988 1 20071005 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM BS 360 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007101500063 20071015 00063 WP 2007 10 15 UPS07850825 1 20070813 A 5330 SKIN DOUG DC8 DC873F 302199F WP FS 1580-1620 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 SEVERAL DENTS ON EXT FUSELAGE SKIN AT STA 1600 L22R AND L23R. REPAIRED FUSELAGE SKIN AT STA 1600 L22 R AND L23R IAW SAA EA 008-5330- 01-A1086, UPS EO DC8-5330-27794-A, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007101500068 20071015 00068 NM 2007 10 15 UPS07M50811 1 20070803 A 5330 DOUBLER DOUG MD11 MD11F 3023600 NM BS 5-125 L43R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C CTR CARGO COMPT AT STATION 5-125 LONGERON 43 RIGHT FOUND SUSPECTED CRACKED ON DOUBLER. HFEC INSP C/OU T FOUND CRACK APPROX 1 INCH AS MARKED. CRACKED LONGERON DOUBLER REMOVED AT STA 5-125 LONGERON 43 RIGHT. SPLICE MACHINE FROM 1D1104- 7150-T61511 PER DOUGLAS DWG A5A7114. FPI C/OUT ON FAB SPLICE FOUND NO CRACK. FAB SPLICE HOLES PICKED UP, REPROTECTED & PAINTED. LONGERON SPLICE INSTALLED AT CTR CARGO COMPT STA 5-125 LONGERON 43 RIGHT. 2 L 7 3 4F RT A22WE 2007101500069 20071015 00069 NM 2007 10 15 UPS07M50812 1 20070808 A 5720 STIFFENER DOUG MD11 MD11F 3023600 NM RWS 714 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C RIGHT WING L/E COMPARTMENT AT STA XORS 714 APPROX FOUND UPPER STIFFENER CRACKED AS MARKED. CRACKED ST IFFENER REMOVED. NEW STIFFENER FABRICATED USING MAT'L 707 5-0-0.071" AS PER DOUGLAS DWG ARB3954. STIFFENER HEAT TREATE D PER DPS 7.00-1 & HARDNESS VALUES HRB 88.7. RIGHT WING L/E COMPT AT STA XORS 714 STIFFENER HOLES PICKED UP & REPROTECT ED. NEW STIFFENER PAINT TOUCH UP & INSTALLED. 2 L 7 3 4F RT A22WE 2007101500070 20071015 00070 NM 2007 10 15 UPS07M50813 1 20070810 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM BS 1954 L51L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C AFT CARGO COMPT AT STA 1954 BILGE AREA LONGERON 51 LEFT FOUND SURFACE CORROSION. AFT CARGO COMPT STA 1954 BILGE AREA LONGERON 51 LEFT FASTENERS REMOVED FRAME SHEAR CLIP AREA CORROSION RMVD FOUND EXCEEDS LIMIT. CORRODED S HEAR CLIP REMOVED AT STA 1954 LONG 49RT-50LT AFT CARGO AREA. SHEAR CLIP FAB FORM MAT'L 7075-0-0.071" PER DWG AGA7133. FAB SHEAR CLIP HOLES PICKED UP, REPROTECTED, PAINTED & INSTALLED AT AFT CARGO COMPT. 2 L 7 3 4F RT A22WE 2007101500072 20071015 00072 NM 2007 10 15 UPS07M50816 1 20070719 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT BORE RT 21 FOUND WITH CORROSION. CORR AT BARREL NUT BORE REMOVED PER SRM 51-21-01 VII R38. BORE BOTTOM REMN 0.0 70" DEEP, BORE REAM TO 1.067" DIA, REMN BLEND OUT 0.100" DEEP, E XCEED LIMITS. BARREL NUT BORE FURTHER REAM TO 1.121" DIA & BOTTOM BORE DOWN 0.070" DEEP. SLEEVE BUSHING FAB, PROTECTED & INSTALLED. REPAIR C/O AT BARREL NUT BORE 21 RT, IS ACCEPTABLE PER EN1468-07. 2 L 7 3 4F RT A22WE 2007101500074 20071015 00074 NM 2007 10 15 UPS07M50817 1 20070813 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT RIGHT 19 FOUND WITH CORROSION. CORR AT BARREL NUT BORE RE MOVED PER SRM 51-21-01 VII R38. BOTTOM BORED THRU & BORE REAM TO 1.067" DIA, REMN BLEND OUT 0.045" DEEP, EXCEED LIMITS. BORE REAM TO 1.105" DIA. BARREL NUT BORE, BLEND OUT VOIDS, PERIPHERY RADIUS SMOOTHEN/PROTECTED. BUCKET BUSHING FAB, PROTECTED & INSTALLED REPAIR C/O AT BARREL NUT BORE 19 RT IS ACCEPTABLE PER EN1521-07. 2 L 7 3 4F RT A22WE 2007101500080 20071015 00080 NM 2007 10 15 UPS07M50835 1 20070718 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM BS 1541 L48 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C CENTER CARGO PIT ON L48 FOUND CORROSION STA 1541.0 AS MARKED. CORR LONGERON SPLICE & ANGLE SPLICE REM OVED PER SRM 51-33-01 VII R38. NEW LONGERON SPLICE & ANGLE SPLICE FABRICATED PER DOC DWG: A5A7125 & A5A71 24. NEW LONG ERON SPLICE & ANGLE SPLICE REPROTECTED & PRIMER TOUCHED UP PER SRM 51-21-01 VII R38. NEW LONGERON SPLICE & ANGLE SPLICE INSTALLED PER SRM 51-33-01 VII R38. 2 L 7 3 4F RT A22WE 2007101500082 20071015 00082 NM 2007 10 15 SWAA074999 1 20071007 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 482 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007101500083 20071015 00083 NM 2007 10 15 SWAA074970 1 20071007 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 312 S18R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 312, STR 18R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007101500090 20071015 00090 NM 2007 10 15 HNAA0700206 1 20070609 A 7600 87600501001 CONTROL CABLE DHAV DHC8 DHC8102 2809003 NM RT ENGINE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 907HA 011 RIGHT ENGINE CONDITION CONTROL AND POWER CONTROL CABLES ARE CORRODED IN THE NACELLE AREA. INSTALLED NEW CONDITION AND P OWER CABLES ON RIGHT ENGINE AS PER 76-10-00 RIGGED IAW 76-10-14. 2 H 7 2 4T RT A13NM 2007101500091 20071015 00091 WP 2007 10 15 UPS07850872 1 20070922 A 5230 4773295U1 SUPPORT ANGLE DOUG DC8 DC873F 302199F WP CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 SUPPORT ANGLE CORRODED AT FWD SIDE OF NR 2 LATCH SPOOL FITTING MCD JAMB. REMOVED AND REPLACED FITTIN G IAW SRM 51-3-0. 2 L 7 4 4F RT 4A25 2007101500092 20071015 00092 NM 2007 10 15 HNAA0700217 1 20070705 A 5347 85320490135 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 222-242 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 940HA 156 RIGHT SEAT TRACK AT STA 222.7000 AND 242.200 SURFACE CORROSION. RIGHT SEAT TRACK REPLACED BY NEW PART AND INSTALLED WIT H SOLID RIVETS AS PER SRM 51-40-00 AND DEFLECTOR REPLACED BY NEW PART AND INSTALLED WITH SOLID RIVETS IAW SRM 51-40-00. 2 H 7 2 4T RT A13NM 2007101500093 20071015 00093 NM 2007 10 15 SWAA074968 1 20071007 A 3350 3071BPLEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 261WN 32517 EEPLS INOP ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007101500094 20071015 00094 NM 2007 10 15 SWAA074960 1 20071004 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 430 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, LBL 3. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007101500099 20071015 00099 NE 2007 10 15 SWAA074978 2 20071005 A 7200 CFM567B24G22 ENGINE BOEING 737 7377H4 1384404 NM GE CFM56 CFM567B24 NE LEFT FAILED A SWAA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SW 29 796SW 27889 876297 INFLIGHT SHUTDOWN/DECLARED EMERGENCY. CLIMBING THROUGH FL 1000 AGL, NR 1 ENGINE FAILED. LOUD BANG, RPM ROLLED BACK, EG T ROSE. REMOVED AND REPLACED NR 1 ENGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007101500100 20071015 00100 NM 2007 10 15 HNAA0700198 1 20070609 A 5544 85540112101 WEB DHAV DHC8 DHC8102 2809003 NM RUDDER CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 907HA 011 WEB FOUND CORRODED ON FORE RUDDER MID HINGE. WEB ON FORE RUDDER MID HINGE LOCALLY FABRICATED AS PER DRAWING NUMBER 8554 0112, INSTALLATION CARRIED OUT ON WORK CARD SEQ 3041. 2 H 7 2 4T RT A13NM 2007101500101 20071015 00101 NM 2007 10 15 SWAA074957 1 20071004 A 5311 6545805 FRAME BOEING 737 7373H4 1384600 NM BS 277 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007101500105 20071015 00105 NM 2007 10 15 SWAA074965 1 20071004 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 360 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007101500106 20071015 00106 NM 2007 10 15 SWAA074963 1 20071004 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 277 S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277 STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007101500108 20071015 00108 NM 2007 10 15 HNAA0700215 1 20070705 A 5730 85710219 DOUBLER DHAV DHC8 DHC8102 2809003 NM WING CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 940HA 156 CORROSION FOUND ON LT FUEL PUMP CUTOUT DOUBLER IN THE FUEL TANK. HFECC NO DEFECTS NOTED. CORROSION REMOVED IAW RD8-57- 3701 AND RD8-57-1907. 2 H 7 2 4T RT A13NM 2007101500111 20071015 00111 WP 2007 10 15 UPS07850875 1 20070913 A 2770 GUST LOCK DOUG DC8 DC873F 302199F WP BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 FITTING BROKEN AROUND GUST LOCK LEVER BASE. FABRICATED AND INSTALLED REPAIR DOUBLER ON GUST LOCK LEV ER BASE IAW SAA EA 008-2510-01-A1124, AND UPS RAA DC8-25-20130. 2 L 7 4 4F RT 4A25 2007101500112 20071015 00112 WP 2007 10 15 UPS07850876 1 20070918 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 NUMEROUS DEFECTS ON WEB BETWEEN UPPER AND LOWER L-1 DOOR HINGES. REMOVED WEB ON L-1 DOOR UPPER AND L OWER HINGES IAW SRM 51-3-0, FABRICATED AND INSTALLED REPAIR WEB ON L-1 DOOR UPPER AND LWR HINGES IAW DWG 5597646-107, AN D SRM 51-3-0. 2 L 7 4 4F RT 4A25 2007101500113 20071015 00113 WP 2007 10 15 UPS07850880 1 20070926 A 5313 LONGERON SPLICE DOUG DC8 DC873F 302199F WP FS 1050 L1 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 LONGERON SPLICE FITTING BROKEN AT STA 1050 L1. REMOVED AND REPLACED LONGERON SPLICE FITTING AT STA 1 050 L1 IAW SRM 51-01-24. 2 L 7 4 4F RT 4A25 2007101500114 20071015 00114 WP 2007 10 15 UPS07850881 1 20071008 A 3350 BATTERY DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY AND RELAY UNIT AND TESTED OK PER MM 33-50 -01. 2 L 7 4 4F RT 4A25 2007101500119 20071015 00119 SO 2007 10 15 C2XA07SH082 1 20071009 A 3260 8005701 PROXIMITY SENSOR EMB 135 EMB135LR 3260305 SO MLG DOOR DEFECTIVE A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 27 17513 145292 FLIGHT 2536 SHV - PILOTS REPORTED NOSE LANDING GEAR DOORS REMAIN OPEN WHEN NOSE GEAR IS UP. MAINTENANCE REMOVED & REPLA CED NOSE LANDING GEAR SEQUENCE PROX SWITCH IAW EMB 135 AMM 32-63-03, OPS CHECK GOOD. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007101500120 20071015 00120 NM 2007 10 15 UPS07M50882 1 20071008 A 3350 BATTERY PACK DOUG MD11 MD11F 3023600 NM EMERGENCY LIGHTS DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 280UP 48634 INSPECTION TYPE:N/A EMERGENCY BATTERY LOW. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PER 33-51-01-4. OPS CHECK G OOD. 2 L 7 3 4F RT A22WE 2007101500122 20071015 00122 NM 2007 10 15 SWAA074966 1 20071007 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 209WN 32484 EEPLS LENS MISSING AT RIGHT OVERWING EMERGENCY EXIT. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007101500124 20071015 00124 NM 2007 10 15 SWAA074967 1 20071007 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 222WN 34290 EEPLS COVER LOOSE AT ROW 5 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007101500125 20071015 00125 NM 2007 10 15 SWAA074975 1 20071007 A 3397 487191 CONNECTOR BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 458WN 33857 EEPLS INOP BETWEEN ROW 1 ABC AND ROW 3 ABC. FOUND LOOSE CONNECTOR. SECURED CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2007101500126 20071015 00126 NM 2007 10 15 SWAA074993 1 20071007 A 3397 487191 CONNECTOR BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 417WN 29822 DURING SCHEDULED MV3 CHECK, FOUND EEPLS INOP AT MID CABIN. FOUND BROKEN CONNECTOR. REMOVED AND REPLACED CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2007101500129 20071015 00129 WP 2007 10 15 MWEA070237 1 20071005 A 5320 5910142U11 WEB DOUG DC9 DC981 3022081 WP BS 370-389 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 814ME 48010 FORWARD CARGO DOOR LOWER CUTOUT BETWEEN FUSELAGE STATION 370 & 389 FLOOR WEB HAS SURFACE CORROSION. REMOVED CORROSION A ND REMOVED AND INSTALLED WEB. 2 L 7 2 4F A6WE 2007101500130 20071015 00130 EU 2007 10 15 USAA070724 1 20071005 A 5347 SEAT TRACK AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 186US 1701 FWD WET AREA FR 12-14 BL 10L HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SR 51-72-11; CORR TASK JA-2 20-53500; LEVEL 1. DEFECT SIZE: 3 X 24 INCHES. 2 L 7 2 4F RT A28NM 2007101500134 20071015 00134 NM 2007 10 15 SWAA075009 1 20071007 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 736SA 27868 DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PA CK PER MM. 2 L 7 2 4F RT A16WE 2007101500135 20071015 00135 NM 2007 10 15 SWAA074994 1 20071007 A 2560 P4010021 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 423WN 29827 AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2007101500136 20071015 00136 NM 2007 10 15 SWAA074973 1 20071007 A 5520 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED BRDG CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BEARING AND BOL T PER MM. 2 L 7 2 4F RT A16WE 2007101500137 20071015 00137 EA 2007 10 15 VNAA0710001 1 20071002 A 2916 73021 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 HYD SYS FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 248PS 8205 7925 CREW REPORTED A NR 2 HYDRAULIC HIGH TEMPERATURE AMBER CAS MESSAGE AFTER TAKEOFF. CREW FOLLOWED THE QRH AND LANDED IN CL T WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 HYDRAULIC RESERVOIR IN ACCORDANCE WITH THE AIRCRAFT MAINT ENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007101500141 20071015 00141 EU 2007 10 15 USAA070721 1 20071005 A 5320 FLOOR SUPPORT AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 186US 1701 FLOORBEAM Y1292 BETWEEN FRAMES C69-C65 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM PER SR 53-00-14, DEFECT SIZE: 1 X 2 INCHES AT 2 AREAS. 2 L 7 2 4F RT A28NM 2007101500142 20071015 00142 EU 2007 10 15 USAA070720 1 20071005 A 5320 FLOOR SUPPORT AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 186US 1701 FLOOR SUPORT Y1292 BETWEEN FRAMES C69-C65 HAS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 53-00-14; CORR TASK JA-160-53500; LEVEL 1, DEFECT SIZE: 1 X 2 INCHES AT 3 AREAS. 2 L 7 2 4F RT A28NM 2007101500144 20071015 00144 EU 2007 10 15 USAA070718 1 20071005 A 5320 FLOOR SUPPORT AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 186US 1701 FLOOR SUPPORT -Y1292 BETWEEN FR 64-69 HAS CORROSION. REMOVED AND REPLACED PAX FLOOR SUPPORT PER SRM 51-72-11; CORR TASK JA-260-53500; CORR LEVEL 1, DEFECT SIZE: 1 SQ INCH. 2 L 7 2 4F RT A28NM 2007101500145 20071015 00145 EU 2007 10 15 USAA070717 1 20071005 A 5320 FLOOR SUPPORT AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 186US 1701 FLOOR SUPPORT - Y1292 BETWEEN FR 64-69 HAS CORROSION. REMOVED AND REPLACED PAX FLOOR SUPPORT PER SRM 51-72-11; CORR TAS K JA-260-53500; CORR LEVEL 1, DEFECT SIZE: 2.5 SQ INCH. 2 L 7 2 4F RT A28NM 2007101500146 20071015 00146 EU 2007 10 15 USAA070716 1 20071005 A 5320 FLOOR SUPPORT AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 186US 1701 PAX FLOOR SUPPORT AT FR 20 40 INCHES RIGHT OF BL 0. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-72-11; CORR TASK JA-2 20-53500, CORR LEVEL 1, DEFECT SIZE: 2 SQ INCHES. 2 L 7 2 4F RT A28NM 2007101500147 20071015 00147 NM 2007 10 15 HNAA0700200 1 20070609 A 5311 85320689105 FRAME DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 907HA 011 PAX DOOR ENTRANCE FRAME CORRODED. PAX DOOR ENTRANCE FRAME REMOVED AND REPLACED IAW SRM 51-40-00. 2 H 7 2 4T RT A13NM 2007101500148 20071015 00148 NM 2007 10 15 CALA0700564 1 20071004 A 3350 3114981 REFLECTOR BOEING 737 7373TO 138447G NM EMERGENCY LIGHT CONTAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 THE L-1 DOOR EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE EMERGENCY LIGHT REFLECTOR ASSEMBLY WAS REMOVED AN D REPLACED IAW MM 33-51-02 AND 33-51-11. 2 L 7 2 4F RT A16WE 2007101500150 20071015 00150 EA 2007 10 15 HNAA0700211 1 20071006 A 2120 UNKNOWN DHAV DHC8 DHC8311 1386006 EA CABIN ODOR A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 331EN 279 ELECTRICAL ODOR COMING FROM BEHIND THE COAT CLOSET. INSPECTED AREA BEHIND THE COAT CLOSET AND AVIONICS BAY RESULTING IN NO DEFECTS NOTED. GROUND RAN THE AIRCRAFT AND OPS CHECKED ALL SYSTEMS DURING 20 MIN RUN TIME. COULD NOT DUPLICATE. 2 H 7 2 4T RT A13NM 2007101500152 20071015 00152 NM 2007 10 15 KCSA071442 1 20071005 A 5330 SKIN BOEING 747 7472B4B 138481B NM BS 980 S39L CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 EXTERNAL SKIN HAS CHAFE DAMAGE FROM DUCT CLAMP AT STA 980 STR 39L. 2 L 7 4 4F RT A20WE 2007101500154 20071015 00154 WP 2007 10 15 UPS07850802 1 20071002 A 5340 FITTING DOUG DC8 DC873F 302199F WP FS 1690 L28L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:SP L28L STA 1690 AFT END FITTING CORRODED OUT OF LIMITS. REMOVED AND REPLACED LONGERON END FITTING AT S TA 1690 L28L IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007101500155 20071015 00155 WP 2007 10 15 UPS07850807 1 20070913 A 5753 SKIN DOUG DC8 DC873F 302199F WP TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 RIGHT WING FLAP VERY INBOARD LWR SUPPORT STRUCTURE CRACKED. CUT OUT DAMAGED AREA FROM RIGHT I/B FLAP IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR DOUBLER ON RIGHT I/B FLAP SUPPORT STRUCTURE IAW SRM 57-07-00, AND SRM 57-02-05. 2 L 7 4 4F RT 4A25 2007101500158 20071015 00158 WP 2007 10 15 MWEA070239 1 20071005 A 5532 591024287 ACCESS PANEL DOUG DC9 DC981 3022081 WP BS 1437 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 814ME 48010 VERTICAL STABILIZER DORSAL FIN ACCESS PANEL LEADING EGDE OPENING HAS FRETTING CORROSION AT STATION 1437, STRINGER 1. RE MOVED CORROSION. REMOVED AND REPLACED AFT FLANGE AT VERTICAL STABILIZER. 2 L 7 2 4F A6WE 2007101500159 20071015 00159 WP 2007 10 15 MWEA070240 1 20071005 A 5350 591140311 SKIN DOUG DC9 DC981 3022081 WP RADOME PEELING A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 814ME 48010 FUSELAGE AT STATION 37 RADOME HINGE AREA SKIN PEELED UP AT RADOME HINGE POINT. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2007101500161 20071015 00161 NM 2007 10 15 HNAA0700194 1 20070907 A 5413 85410734101 STRINGER DHAV DHC8 DHC8102 2809003 NM LT NACELLE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 839EX 226 BOTH STRINGERS CRACKED IN LEFT NACELLE UNDER HEAT SHIELD FOR EXHAUST. BOTH STRINGERS CUT AND REPAIRED IAW RD8-54-310, I NSTALLED WITH SOLID RIVETS AND HI-LOKS IAW SRM 51-40-00. 2 H 7 2 4T RT A13NM 2007101500162 20071015 00162 NM 2007 10 15 HNAA0700195 1 20070609 A 5320 ANGLE DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 907HA 011 ANGLE CRACKED AT FUSELAGE ST 636.00-Z118.5 RT ANGLE AT FUSELAGE ST 636-118.5 HAS BEEN REMOVED AND NEW PART INSTALLED IAW 50-40-00. FABRICATED IAW DRAWING NUMBER 85330499. 2 H 7 2 4T RT A13NM 2007101500163 20071015 00163 NM 2007 10 15 UPS07550841 1 20070922 A 5311 7075C080C FRAME BOEING 757 75724APF 1384969 NM BS 1520 DENTED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 448UP 27737 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1520, BETWEEN S26L TO S27L. ***THIS SDR REPLACES UPS07550832. V ENDOR ENTERED THIS INFO UNDER TAIL N434UP.*** REPAIRED PER SRM 53-00-07 R/R 53-09. REPAIR CATEGORY-B REPAIR RE-INSPECT ION REQUIRED PER SRM 53-00-07 ZONE 2 DETAIL V FIG 201 SHEET 1 OF 15 TABLE II FIG 201 SHEET 10 OF 15. 25,000 FLIGHT CYCL ES AFTER REPAIR INSTALLED. 2 L 7 2 4F RT A2NM 2007101500164 20071015 00164 NM 2007 10 15 UPS07550842 1 20070922 A 5311 70750071C FRAME BOEING 757 75724APF 1384969 NM BS 780 DENTED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 448UP 27737 INSPECTION TYPE:C DENT IN FWD CARGO COMPARTMENT FUSELAGE FRAME STA 780, APPROX BETWEEN S24R AND S25R. ***THIS SDR REPLA CES UPS07550831. VENDOR ENTERED THIS DATA UNDER N434UP.*** REPAIRED FRAME PER SRM 53-00-07 T/R 53-09, CATEGORY B-REPAI R. RE-INSPECTION REQUIRED PER SRM 53-00-07 DETAIL V ZONE 1 FIG 201 SHEET 11 OF 15 TABLE II FIG 201 SHEET 10 OF 15. 37, 500 FLIGHT CYCLES AFTER REPAIR INSTALLED. 2 L 7 2 4F RT A2NM 2007101500165 20071015 00165 NM 2007 10 15 UPS07550844 1 20070922 A 5311 143N1024138 FRAME BOEING 757 75724APF 1384969 NM BS 660 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 448UP 27737 INSPECTION TYPE:C DENTS IN FWD CARGO COMPARTMENT FUSELAGE FRAME STA 660, APPROX BETWEEN S23R TO S24R (2EA). ACCOMPLISHE D REPAIR PER FINAL EA 757-5330-27-A1752 AND UPS EO B757-5310-27807-A. 2 L 7 2 4F RT A2NM 2007101500168 20071015 00168 NM 2007 10 15 WRLA2007105 1 20071004 A 5420 AUB7562299 RETAINER DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE NR 3 PYLON DAMAGED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 273WA 48519 DURING C-CHECK, FOUND NR 3 PYLON AFT LOWER FAIRING RETAINER DAMAGE. 10-29-07 ACCOMPLISHED ERA NUMBER 07-54-107. RE PLACED NR 3 PYLON AFT LOWER FAIRING RETAINER. 2 L 7 3 4F 4 F RT A22WE E24NE 2007101500172 20071015 00172 2007 10 15 ZZDA2007279 4 20071007 A 2565 D29982225 SLIDE BOEING 717 717200 1383700 NM R1 DOOR UNWANTED DEPLOY A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 945AT 55008 R1 DOOR SLIDE DEPLOYED. INSTALLED R-1 DOOR SLIDE IAW AMM 25-61. 2 L 7 2 4F TR A6WE 2007101500173 20071015 00173 NM 2007 10 15 USAA920070899 1 20071002 A 5340 69165096 STRINGER CLIP BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT - MAJOR REPAIR - FPBH INSPECTION, CRACKED TIE CLIP ANGLE, BS 360, S16L. REPLACED TIE CLIP ANGLE, BS 360 S16L IAW BO EING DRAWING 65-17685. 2 L 7 2 4F RT A16WE 2007101500174 20071015 00174 NM 2007 10 15 USAA920070900 1 20071002 A 5340 69265552 STRINGER CLIP BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT - MAJOR REPAIR - FPBH INSPECTION, CRACKED CLIP ANGLE, BS 360, S16L. REPLACED CLIP ANGLE, BS 360 S16L IAW BOEING DRA WING 65-17685. 2 L 7 2 4F RT A16WE 2007101500175 20071015 00175 NM 2007 10 15 USAA920070901 1 20071006 A 5320 6978163 WEB BOEING 737 7373B7 1384580 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 23381 CLT - MAJOR REPAIR -C-4 CHECK, CRACKED WEB, BS 727, S18A RIGHT. REPLACED WEB, BS 727, S18A RIGHT IAW B737-300 SRM 51-10 -02 AND 51-40-00. 2 L 7 2 4F RT A16WE 2007101500176 20071015 00176 NM 2007 10 15 USAA920070902 1 20071006 A 5330 6545775 SKIN BOEING 737 7373B7 1384580 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 23381 CLT - MAJOR REPAIR - C-4 CHECK, CRACKED FUSELAGE SKIN, BS 767, S21R. REPAIRED FUSELAGE SKIN, BS 767, S21R IAW B737-300 SRM 53-00-01. 2 L 7 2 4F RT A16WE 2007101500178 20071015 00178 NM 2007 10 15 USAA920070904 1 20071005 A 5311 9078223 STRAP BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 23381 CLT - MAJOR REPAIR - C-4 CHECK, CRACKED FRAME STRAP, BS 312, S13L. REPLACED FRAME STRAP, BS 312, S13L IAW BOEING DRAWIN G 65-17684. 2 L 7 2 4F RT A16WE 2007101500179 20071015 00179 NM 2007 10 15 HNAA0700213 1 20071007 A 3320 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN ODOR A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 807EX 292 ELECTRICAL BURNING ODOR NOTICED IN AFT CABIN AREA, REQUESTED MDT MAINTNANCE FOR HELP. SWAPPED 804EX WITH 807EX REMOVED AND REPLACED OVERHEAD LIGHT ASSY ABOVE SEAT POSITION 2AC, OPS CHECK GOOD. OK FOR SERVICE IAW 33-25-00. MORE TO FOLLOW. 2 H 7 2 4T RT A13NM 2007101500180 20071015 00180 NM 2007 10 15 SWAA075004 1 20071007 A 5330 6545765 SKIN BOEING 737 7373TO 138447G NM BS 520 S28L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007101500183 20071015 00183 NM 2007 10 15 SWAA075006 1 20071007 A 5330 6545774 SKIN BOEING 737 7373TO 138447G NM BS 740D S18R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740D, STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007101500185 20071015 00185 SO 2007 10 15 C2XA07CL085 1 20070930 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12957 145080 DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT SIGN OVER THE SERVICE DOOR, EXIT SIGN AT SEAT 3BC, AND THE EXIT SIGN AT TH E LEFT ESCAPE HATCH WERE ALL INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 3 EMERGENCY LIGHT INVERTER. OPERAT IONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007101200075 20071012 00075 EU 2007 10 12 2007UALA03910 1 20070926 A 2920 D2927008000066 SOLENOID AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RAT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 462UA 1272 RAT WILL NOT STOW. *S/D* RAT SOLENOID FAULTY. REPLACED RAT SOLENOID AND PRESSURE SWITCH. RETRACTION NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101200076 20071012 00076 NM 2007 10 12 2007UALA03912 1 20070926 A 3520 PSU AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 813UA 858 DURING OPERATIONAL CHECK OF PASSENGER EMERGENCY OXYGEN SYSTEM, ROWS 12,18 LEFT AND 21, 22 AND 24 RIGHT FAILED TO DROP. *S/D* REPLACED O2 CONTAINERS AT LOCATIONS THAT FAILED TO OPEN. CHECKED AND ADJUSTED RIGGING. TESTED AGAIN AND ALL ARE NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101200077 20071012 00077 NM 2007 10 12 2007UALA03913 1 20070927 A 3350 321454 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 831UA 1291 BATTERIES AT EMERGENCY EXIT LEFT AND RIGHT FAILED TEST. *S/D* FAULTY BATTERIES. REPLACED BOTH LEFT AND RIGHT EMERGENC Y EXIT LIGHT BATTERIES, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101200083 20071012 00083 NM 2007 10 12 2007UALA03942 1 20070927 A 5347 SEAT TRACK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 850UA 1653 FOUR EA SEAT TRACKS HAVE LUGS WORN BEYOND LIMITS. WEAR IS WHERE FWD SEAT LEG ANTI-RATTLE NUTS ARE LOCATED. THE 4 TRACK S ALL RUN FROM FR41 THRU FR 47-51 AND ARE THE LEFT I/B, LEFT O/B, RIGHT I/B AND RIGHT O/B TRACKS. MAJOR REPAIR ACCOMPLI SHED: REPLACED SEAT TRACKS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101200087 20071012 00087 NM 2007 10 12 2007UALA03946 1 20070927 A 3350 321454 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 814UA 862 ACFT FAILED CABIN EMERGENCY LIGHT CHECK ITEM 2 ON 3 SVC. POWER SUPPLY FAULT/FAILURE. REPLACED POWER SUPPLY 11WL AND RE LAMPED 63WL, 61WL. OPS CHECK NORMAL AFTER MTX. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101200094 20071012 00094 NM 2007 10 12 CALA0700553 1 20070929 A 5542 65C25961 SKIN BOEING 737 7373T0 1384582 NM RUDDER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND LT SIDE OF RUDDER T/E SKIN DELAMINATED AT STA 175.0. THE DELAMINATION MEASURED 0.4"L X 0.2"W. A PERMA NENT REPAIR WAS INSTALLED IAW ECRA 5540-01243. 2 L 7 2 4F RT A16WE 2007101200096 20071012 00096 SO 2007 10 12 LR7A07097 1 20070926 A 2612 892541100 CONTROL UNIT LKHEED 382 382G 526414U SO FIRE DETECTION MALFUNCTIONED A LR7A E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 AL 03 403LC 8964 4590 DURING CRUISE, FLIGHT CREW REPORTED NR 2 ENGINE FIRE WARNING INDICATION, AND PERFORMED PRECAUTIONARY ENGINE SHUT DOWN AN D FIRE BOTTLE DISCHARGE. MAINTENANCE FOUND MALFUNCTIONING FIRE DETECTION CONTROL UNIT AND REPLACED WITH SERVICEABLE UNI T, NR 1. 2 H 7 4 4T A1SO 2007101200097 20071012 00097 EA 2007 10 12 HNAA0700182 1 20071001 A 2620 YD4N RELAY DHAV DHC8 DHC8311 1386006 EA APU BAY UNKNOWN A HNAA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 07 330EN 32511 32511 274 CREW ATTEMPTED TO DISCHARGE APU FIRE BOTTLE. FIRE BOTTLE DID NOT DISCHARGE. (VERIFIED IN ROA ON 2 OCT 07). VERIFIED 2 8 VOLTS AT SQUIB CONNECTOR. REPLACED SQUIB AS PRECAUTION. OPS CHECKED OLD SQUIB, CHECKED GOOD. SUSPECT FAULT CAUSED B Y APU AIR/GROUND RELAY 7615-K4 WHICH IS ENERGIZED BY RT MAIN BUS, DE-ENERGIZED WHEN APU GENERATOR CONTACTOR FAILED CAUSI NG LARGE BUSS VOLTAGE DROP TAKING POWER FROM SQUIB CARTRIDGE. REMOVED AND REPLACED RELAY 7615-K4 AS PRECAUTION. 2 H 7 2 4T RT A13NM 2007101200105 20071012 00105 WP 2007 10 12 MWEA070232 1 20071002 A 5311 FRAME DOUG DC9 DC981 3022081 WP BS 1382 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 814ME 48010 LEFT PNEUMATIC DUCT VALVE CHAFING AGAINST WEB AT FRAME STATION 1382 BELOW STRINGER 4 LEFT. REMOVED DAMAGED WEB DOUBLER, FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2007101200115 20071012 00115 EU 2007 10 12 TRAX200701445 1 20070927 A 5720 ANGLE AEROSP ATR72 ATR72 EU RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 RIGHT WING PRESSURE DECK ANGLE FR 27 CRACK FOUND IN Y AXIS. 10-16-07 HFEC PERFORMED W/O 37536. CRACK CONFIRM, D OES NOT EXTEND BEYOND FASTENER. PRC 870 APPLIED IAW SRI DO/TS-4165/07-9309 INSPECTED PRESSURE DECK ANGLE AND EXISTING CR ACK PER TC EO 72-53-0254. 2 H 7 2 4T RT 2007101200116 20071012 00116 EA 2007 10 12 TRAX200701446 1 20070927 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 855AS 7395 PAX DOOR IN AREA OF ACCESS PANEL 832AL WEB FOUND CRACK. 10-16-07 REPAIRED CRACK FOUND IN PAX DOOR IN AREA OF ACCES S PANEL 832AL WEB AS PER 51-12-11 FIG 6. 2 L 7 2 4F RT A21EA 2007101200117 20071012 00117 EA 2007 10 12 TRAX200701447 1 20070930 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 F/A REPORTS, CABIN DOOR HANDLE WOULD NOT GO ALL THE WAY UP. TOOK 4X TO GET DOOR OPEN. 2 L 7 2 4F RT A21EA 2007101200118 20071012 00118 NM 2007 10 12 HNAA0700193 1 20070812 A 5210 85210299102 BRACKET DHAV DHC8 DHC8102 2809003 NM PAX DOOR CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 943HA 167 SEVERE CORROSION FOUND ON LOWER AFT PAX DOOR BRACKET (INBOARD). LOWER AFT PAX DOOR BRACKET I/B REPLACED WITH NEW PART I NSTALLED WITH BOLT IAW AMM 20-14-01. 2 H 7 2 4T RT A13NM 2007101200119 20071012 00119 NM 2007 10 12 HNAA00194 1 20070907 A 5413 85410734101 STRINGER DHAV DHC8 DHC8102 2809003 NM NACELLE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 839EX 226 BOTH STRINGERS CRACKED IN LEFT NACELLE UNDER HEAT SHIELD FOR EXHAUST. BOTH STRINGERS CUT AND REPAIRED IAW RD8-54-310, I NSTALLED WITH SOLID RIVETS AND HI-LOKS IAW SRM 51-40-00. 2 H 7 2 4T RT A13NM 2007101200129 20071012 00129 NM 2007 10 12 USAA920070890 1 20070920 A 5510 69730963 HINGE PIN BOEING 737 7374B7 1384702 NM HORIZONTAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 456UW 25020 CLT - MAJOR REPAIR - C-5 CHECK, CORROSION ON THE LEFT HORIZONTAL STABILIZER CENTER SECTION TO BODY INNER HINGE PIN. REP LACED LEFT HORIZONTAL STABILIZER CENTER SECTION TO BODY INNER HINGE PIN IAW B737-400 AMM 27-41-31. 2 L 7 2 4F RT A16WE 2007101200135 20071012 00135 EU 2007 10 12 USAA920070896 1 20070924 A 5540 D5537131800000 HINGE FITTING AIRBUS 320 A320231 3930325 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 644AW 317 SAL - MAJOR REPAIR - C-04 CHECK - NR 5975508, RUDDER HINGE FITTING NR 2 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STA 1926 / RIB 4. REPLACED RUDDER HINGE FITTING NR 2, VERTICAL STABILIZER STA 1926 / RIB 4 IAW A320 AMM 55-36-41. 2 L 7 2 4F RT A28NM 2007101200136 20071012 00136 SO 2007 10 12 C2XA07SH081 1 20071004 A 5315 14521713003 FLOORBEAM EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11109 145657 SHV - DURING C-CHECK CORROSION AROUND NUT PLATE ON RIGHT OMEGA BEAM AT FR23. MAINTENANCE REPAIRED RT OMEGA BEAM AT FR 2 3 AROUND NUT PLATE IAW EC5320-01228 REV D. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2007101200137 20071012 00137 NM 2007 10 12 SWAA074932 1 20071003 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 636WN 27709 L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007101200138 20071012 00138 NM 2007 10 12 SWAA074927 1 20071003 A 3040 101618333 CONTROLLER BOEING 737 7375H4 138449D NM WINDOW HEAT FAULTY A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 515SW 25154 FLIGHT DECK L1 WINDOW ARCING. REMOVED AND REPLACED WINDOW HEAT CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 2007101200155 20071012 00155 NM 2007 10 12 SWAA074943 1 20071003 A 5311 6546548 FRAME BOEING 737 7375H4 138449D NM BS 747 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007101200163 20071012 00163 NM 2007 10 12 SWAA074950 1 20071003 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500A S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 2007101200164 20071012 00164 NM 2007 10 12 SWAA074926 1 20071003 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 578 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007101200165 20071012 00165 NM 2007 10 12 SWAA074928 1 20071003 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 482B S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007101500020 20071015 00020 NM 2007 10 15 UPS07M50850 1 20070808 A 5320 BRACKET DOUG MD11 MD11F 3023600 NM BS 495 S27R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C FWD CABIN - RIGHT SIDEWALL AREA 01EA L-ANGLE BRACKET AT STA 495, S-27R FOUND CRACK NEAR FASTENER AS MA RKED. FWD CABIN - RIGHT AT STA 495 S-27R CRACK AREA TRIMMED OFF. TRIMMED OFF AREA PROTECTED. HFEC INSP C/OUT ON TRIMM ED OFF, FOUND NO CRACK EVIDENT 01EA FILLER FAB FROM MAT'L 7075T6-0.080" & REPAIR ANGLE FAB FROM ET MAT'L S2929486 PER EA RN EN1536-07.5. NEW FAB PARTS FASTENER HOLES PICKED UP, PROTECTED, PAINTED & INSTALLED. 2 L 7 3 4F RT A22WE 2007101500025 20071015 00025 NM 2007 10 15 HNAA0700209 1 20070609 A 2760 82700500001 CONTROL CABLE DHAV DHC8 DHC8102 2809003 NM SPOILERS WORN A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 907HA 011 RIGHT SPOILER INBOARD AND OUTBOARD CABLES WORN TO LIMITS. RIGHT WING SPOILER CABLES REPLACED IAW 27-14-00. 2 H 7 2 4T RT A13NM 2007101500028 20071015 00028 NM 2007 10 15 UPS07550831 1 20070922 A 5311 70750071C FRAME BOEING 757 75724APF 1384969 NM BS 780 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 434UP 25465 INSPECTION TYPE:C DENT IN FWD CARGO COMPARTMENT FUSELAGE FRAME STA 780, APPROX BETWEEN S24R AND S25R. REPAIRED FRAME PE R SRM 53-00-07 T/R 53-09 CATEGORY B REPAIR. RE-INSPECTION REQUIRED PER SRM 53-00-07 DETAIL V ZONE 1 FIG 201 SHEET 11 OF 15. TABLE II FIG 201 SHEET 10 OF 15. 37,500 FLIGHT CYCLES AFTER REPAIR INSTALLED. 2 L 7 2 4F RT A2NM 2007101500039 20071015 00039 NM 2007 10 15 UPS07M50862 1 20070730 A 5411 RIB DOUG MD11 MD11F 3023600 NM NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C NR 1 ENG PYLON, (LT SIDE) AFT OF BULKHEAD 286, FWD LT & RT UPPER SUPPORT RIB FOUND CRACKED UPPER AREA APPROX .75 INCH AS MARKED. SUPPORT RIB CRACKED AREAS TRIM OUT PER EN1497-07. HFEC INSP C/O ON TRIM OUT AREA, FOUND NO CRACK. 04 EA REPAIR FILLERS, 02 EA DOUBLERS & 01 EA SPLICE DOUBLER FAB PER EN1492-07. REPAIR PARTS & REWORKED AREA PAI NTED. FILLERS, DOUBLERS & SPLICE DOUBLER AT NR 1 PYLON BULKHEAD YN 286 AREA INSTALLED PER EN1492-07 & SRM 51-33-01 VII R38. 2 L 7 3 4F RT A22WE 2007101500041 20071015 00041 NM 2007 10 15 UPS07M50863 1 20070705 A 5730 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C RIGHT WING L/E LOWER ACCESS AT SLAT TRACK NR 10 TO 21 INCHES I/B, FOUND L/E UPPER CORRUGATED SKIN CRAC KED AT 3EA PLACES AS MARKED. HFEC INSP C/O ON CRACK AREA & CRACK END MARKED OUT APPROX. 0.25". FASTENERS AT CRACK AREA REMOVED & CRACK AREA TRIM OUT. HFEC C/O ON TRIM OUT AREA, FOUND NO CRACK. 03EA REPAIR FILLERS, 03EA DOUBLERS & ANGLES FAB, REPROTECTED & PAINTED. NEW FILLERS, DOUBLERS & ANGLES INSTALLED PER SRM 51-35-01 VII R38 & SRM 51-33-01 VII R38. 2 L 7 3 4F RT A22WE 2007101500075 20071015 00075 NM 2007 10 15 UPS07M50818 1 20070801 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT BORE RIGHT 20 FOUND WITH CORROSION. CORR AT BARREL NUT BO RE REMVD PER SRM 51-21-01 VII R38. BTM SURFACE CLEANED BORE REAMED TO 1.067" DIA, REMN BLEND OUT 0.040" DEEP, EXCEED LIM IT. BARREL NUT BORE, BLEND OUT VOID, BTM PERIPHERY RADIUS SMOOTHEN/PROTECT SLEEVE BUSHING FAB, PROTECTED & INSTALLED. REPAIR C/O AT BARREL NUT BORE 20 RIGHT IS ACCEPTABLE PER EN1482-07. 2 L 7 3 4F RT A22WE 2007101500078 20071015 00078 2007 10 15 UPS07M50822 4 20071003 A 2565 SWITCH DOUG MD11 MD11F 3023600 NM L1 DOOR SLIDE INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 251UP 48744 INSPECTION TYPE:N/A L1 DOOR ESCAPE SLIDE PRESSURE REMOTE PUSH TO TEST SWITCH INOP. DEFERRED PER MEL 25-61-2 CONTROL M35 9900 ASSIGNED C/W DMP 25-61-2. REMOVED AND REPLACED L1 DOOR REMOTE PRESSURE INDICATOR ASSY IN REFERENCE TO MM 25-61-04. OPS CHECKS GOOD. THIS CLEARS M359900 PLACARD REMOVED. 2 L 7 3 4F RT A22WE 2007101500084 20071015 00084 NM 2007 10 15 SWAA074998 1 20071007 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM BS 440 S13R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 13R CRACKED AT BS 440. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007101500085 20071015 00085 NM 2007 10 15 SWAA074972 1 20071007 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 809 S17L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED SERVICE CHECK, FOUND STRINGER 17L CRACKED AT BS 809. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007101500086 20071015 00086 NM 2007 10 15 SWAA074997 1 20071007 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM BS 1006 S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 7L CRACKED AT BS 1006. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007101500087 20071015 00087 NM 2007 10 15 UPS07M50837 1 20070801 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT BORE RT 17 FOUND WITH CORROSION. CORR AT BARREL NUT BORE REMOVED PER SRM 51-21-01 VII R38. BOTTOM BORED THRU BORE REAMED TO 1.067" DIA, REMN BLEND OUT DEPTH 0.175", EXCEED LIMI TS. BORE FURTHER REAMED TO 1.130" & THEN TO 1.189" DIA BARREL NUT BORE, BLEND OUT VOIDS & PERIPHERY RADIUS SMOOTHEN & P ROTECTED. BUCKET BUSHING FAB, PROTECTED & INSTALLED. REPAIR C/O IS ACCEPTABLE PER EN 1497-07. 2 L 7 3 4F RT A22WE 2007101500096 20071015 00096 NM 2007 10 15 SWAA074956 1 20071004 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 964 S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 964, STR 5R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007101500098 20071015 00098 WP 2007 10 15 UPS07850870 1 20070922 A 5230 4773295U1 FITTING DOUG DC8 DC873F 302199F WP CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 SUPPORT ANGLE CORRODED AT FWD SIDE OF NR 3 LATCH SPOOL FITTING AT MCD JAMB. REMOVED AND REPLACED SUP PORT FITTING IAW SRM 51-3-0. 2 L 7 4 4F RT 4A25 2007101500103 20071015 00103 NM 2007 10 15 SWAA074964 1 20071004 A 5313 6551698 STRINGER SPLICE BOEING 737 7373A4 1384585 NM BS 360 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007101500104 20071015 00104 NM 2007 10 15 SWAA074961 1 20071004 A 5754 SKIN BOEING 737 7373H4 1384600 NM NR 5 SLAT DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 14Y CHECK, FOUND RIGHT WING NR 5 L/E SLAT OUTBOARD T/E WEDGE DISBONDED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007101500110 20071015 00110 WP 2007 10 15 UPS07850874 1 20070915 A 5330 PANEL DOUG DC8 DC873F 302199F WP FS 1990 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 AT FULL RIGHT THROW, RUDDER STRIKES TAIL CONE SKIN AT LEFT SIDE. REMOVED LEFT SIDE FLANGE OF RUDDER BOTTOM PANEL IAW SRM 51-1-20D, FABRICATED AND INSTALLED REPAIR PANEL AT LEFT RUDDER SKIN FLANGE IAW DWG 565507A AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007101500115 20071015 00115 WP 2007 10 15 UPS07850884 1 20070913 A 5310 DOUBLER DOUG DC8 DC873F 302199F WP FS -156 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 FUSELAGE NOSE EXTERIOR, NOSE PNEUMATIC HOOK UP DOOR DOUBLER IS CRACKED. REMOVED, FABRICATED, AND INS TALLED REPAIR DOUBLER AT NOSE PNEUMATIC HOOKUP DOOR IAW SRM 53-03-03-00 FIG 023 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007101500116 20071015 00116 WP 2007 10 15 UPS07850885 1 20070929 A 5210 WEB DOUG DC8 DC873F 302199F WP L1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C2 L-1 DOOR LWR WEB IS CRACKED AT EDGE. STOP DRILLED CRACK IN WEB AT L-1 DOOR. FABRICATED, AND INSTALL ED REPAIR DOUBLER AT L-1 DOOR LWR WEB IAW SRM 52-02-00, AND SRM 52-03-00. 2 L 7 4 4F RT 4A25 2007101500117 20071015 00117 WP 2007 10 15 UPS07850892 1 20071009 A 3350 BATTERY DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:N/A EMERGENCY LIGHTS WILL NOT TEST. ON PREVIOUS FLIGHT, NEW BATTERY INSTALLED. REMOVED AND REPLACED EM ERGENCY LIGHTING BATTERY AND RELAY UNIT AND WARNING LIGHT DIMMING BOX. OPS CHECK GOOD IAW MM 33-50-01 AND WDM 33-50-01. 2 L 7 4 4F RT 4A25 2007101500118 20071015 00118 NM 2007 10 15 HNAA0700223 1 20071009 A 2910 826069149 LINE DHAV DHC8 DHC8102 2809003 NM HYD SYSTEM CHAFED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 810EX 308 WHILE PERFORMING AN INSPECTION FOR SB8-24-83 AND AD2007-04-22 THE RUDDER PRESSURE AND RETURN HYDRAULIC LINES WERE FOUND CHAFED PASSING THROUGH ASSEMBLY PART NUMBER 820335-001. REMOVED AND REPLACED THE RUDDER HYDRAULIC LINES. THIS IS THE T HIRD OCCURRENCE FOUND DURING THIS INSPECTION. 2 H 7 2 4T RT A13NM 2007101500128 20071015 00128 WP 2007 10 15 MWEA070236 1 20071005 A 5330 59360381 SKIN DOUG DC9 DC981 3022081 WP BS 636-693 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 814ME 48010 MID CARGO DOOR LOWER CUTOUT, BETWEEN FUSELAGE STATION 636 & 693 HAS SEVERAL SMALL SPOTS OF CORROSION. REMOVED DAMAGE, F ABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2007101500131 20071015 00131 EU 2007 10 15 USAA070723 1 20071005 A 5320 D5311281820401 FLOOR SUPPORT AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 186US 1701 Y254 FLOOR SUPPORT BETWEEN FRAMES 16-20 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11, DE FECT SIZE: 1 INCH DIA AT 3 SPOTS. 2 L 7 2 4F RT A28NM 2007101500149 20071015 00149 2007 10 15 SWAA074979 4 20071004 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 224WN 32493 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007101500156 20071015 00156 WP 2007 10 15 UPS07850808 1 20070914 A 5340 ATTACH ANGLE DOUG DC8 DC873F 302199F WP FS 1766 L6L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C2 AFT PRESS BULKHEAD ATTACH ANGLE CRACKED AT STA 1766 L6L. REMOVED, FABRICATED, AND INSTALLED REPAIR A NGLE ON AFT PRESS BULKHEAD AT STA 1766 L6L IAW DWG 5773844, AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 2007101500157 20071015 00157 WP 2007 10 15 MWEA070238 1 20071005 A 5350 591140311 RADOME DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 814ME 48010 CRACK FOUND AT LEFT RADOME HINGE FASTENER. CUT OUT DAMAGE. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2007101500182 20071015 00182 NM 2007 10 15 SWAA075005 1 20071007 A 5330 6545774 SKIN BOEING 737 7373TO 138447G NM BS 730C S19R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730C, STR 19R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007101500186 20071015 00186 SO 2007 10 15 C2XA07IA218 1 20071006 A 3234 7455503 SELECTOR EMB 145 EMB145XR 3260214 SO COCKPIT INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 11113 12409 12409 145662 BJX - FLIGHT 2193, THE CREW REPORTED A LANDING GEAR LEVER DISAGREE, AND THE GEAR WAS STUCK DOWN AFTER T/O. THE AIRCRAFT RETURNED TO BJX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND IT WAS FERRIED TO IAH WHERE I T LANDED WITHOUT INCIDENT. IAH MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR SELECTOR LEVER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007101500191 20071015 00191 NM 2007 10 15 SWAA074969 1 20071007 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007101500192 20071015 00192 NM 2007 10 15 P5CA0701535 1 20070930 A 4900 398321051 ISOLATION VALVE BOEING 747 74747UF 1384812 NM APU MALFUNCTIONED A P5CA O OTHER O OTHER CR CRUISE 1 EA 15 416MC 32838 APU EICAS MESSAGE AFTER T/O. ALSO HEARD LOUD SOUND FROM ABOVE MAIN DECK SIDE CARGO DOOR. AIR TURNBACK. REPLACED APU I SOLATION VALVE, INSEPCTED DUCTS NO DEFECTS NOTED. ACCOMPLISHED PRESSURIZATION CHECK OF CARGO DOOR AND INSPECTED SEALS. NO DEFECTS NOTED, PER MM 36-11-09. 2 L 7 4 4F RT A20WE 2007101500195 20071015 00195 WP 2007 10 15 07FDEA04506 1 20071005 A 5712 ARB0760 RIB DOUG DC10 DC1010 3022110 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 FOUND UPPER RIB CAP CRACKED ON LT WING PNL 534AT. REPLACED RIB IAW SRM 57-20-00 FIG 38 SHT 1-2-3 VOL I. 2 L 7 3 4F A22WE 2007101500196 20071015 00196 WP 2007 10 15 07FDEA04507 1 20071005 A 5712 ARB0760 RIB DOUG DC10 DC1010F 3022111 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 FOUND UPPER RIB CAP CRACKED ON RT WING PNL 634AT. REPLACED RIB IAW SRM 57-20-00 FIG 38 SHT 1-2-3 VOL I. 2 L 7 3 4F A22WE 2007101500197 20071015 00197 WP 2007 10 15 07FDEA04509 1 20071005 A 5510 ALC72271 PANEL DOUG DC10 DC1030F 3023504 WP HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 DURING U/S INSP OF HORIZONTAL STAB, FOUND CRACK ON PANEL P/N 7227-1, POSITION 14, CRACK IS IN FLYABLE LIMITS, ATTACHED I NSPECTION FINDING FORM FOR A11 DETAIL. REPAIRED AREA IAW EA 8-5510-111537. 2 L 7 3 4F RT A22WE 2007101500198 20071015 00198 EU 2007 10 15 07FDEA04510 1 20071005 A 5730 A57340088 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION AT RT WING LOWER SKIN RIB 11-12, P15-16. REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTECTION IAW E A 6-5720-112459 AND RAS/BAE/1005301/2007 ISS A. 2 L 7 2 4F RT A35EU 2007101500199 20071015 00199 WP 2007 10 15 07FDEA04511 1 20071005 A 5512 ALC72812 SKIN DOUG DC10 DC1030F 3023504 WP HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 DURING VISUAL INSP OF HORIZONTAL STAB SKIN PANEL INSPECTION, FOUND CRACK ON PANEL P/N 7439-2 SERIES -10, REPAIRED AREA I AW EA# 8-5510-111620. 2 L 7 3 4F RT A22WE 2007101500200 20071015 00200 EU 2007 10 15 07FDEA04512 1 20071005 A 5712 A57340088 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION AT RT WING LOWER SKIN RIB 10-12, REAR SPAR AND AFT REPAIR PERFORMED BY BLEND OUT CORROSION AND REP ROTECTION IAW EA 6-5720-112459 AND RAS/BAE/1005247/2007 ISS A. 2 L 7 2 4F RT A35EU 2007101500201 20071015 00201 EU 2007 10 15 07FDEA04513 1 20071005 A 5730 A57340088 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION AT RT WING LOWER SKIN RIB 10-12, FWD OF FRONT SPAR. REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTE CTION IAW EA 6-5720-112459 AND RAS/BAE/1005247/2007 ISS A. 2 L 7 2 4F RT A35EU 2007101500202 20071015 00202 EU 2007 10 15 07FDEA04514 1 20071005 A 5730 A57340088 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION AT RT WING LOWER SKIN RIB 13-14. REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTECTION IAW EA 6-5720 -112459 AND RAS/BAE/1005302/2007 ISS A. 2 L 7 2 4F RT A35EU 2007101500204 20071015 00204 EU 2007 10 15 07FDEA04516 1 20071005 A 5730 A57340088 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU RT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND OLD REPAIR ON RT OUTER WING AT FASTENER HOLE 939, RIB 9-10 IN BAD CONDITION. REPAIR PERFORMED BY OVERSIZING THE H OLE AND INSTALLING NEW TAPER OK IAW EA 6-5720-106520 AND RAS/BAE/0564/2003 ISS B. 2 L 7 2 4F RT A35EU 2007101500206 20071015 00206 EU 2007 10 15 07FDEA04518 1 20071005 A 5320 A53989155208 STIFFENER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSIONN ON T-STIFFENER C91. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007101500213 20071015 00213 2007 10 15 2007UALA04003 4 20071001 A 2565 131W18221201 BRACKET BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE DOOR 2R GIRT BAR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 DOOR 2R GIRT BAR PICK UP LINKAGE BRACKET DAMAGED. REMOVED FROM RT SIDE. REPLACED BRACKET AND REINSTALLED SLIDE. OK FO R SERVICE 2 L 7 2 4F 4 F RT T0001SE E46NE 2007101500219 20071015 00219 NM 2007 10 15 2007UALA04009 1 20070930 A 3397 CONNECTOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LGIHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 222UA 30553 EEL AT FIRST CLASS SEAT 3E INOP. SECURED EEL CONNECTOR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007101500220 20071015 00220 NM 2007 10 15 2007UALA04010 1 20070930 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 EMERGENCY LIGHTS INOP AT 4E AFT, 4J AFT, 5J AFT, 43 ABC AND 58 ABC. REPLACED LIGHT ASSEMBLIES. 2 L 7 4 4F 4 F RT A20WE E24NE 2007101500223 20071015 00223 NM 2007 10 15 2007UALA04013 1 20070929 A 3350 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 FOUND RIGHT OVERWING AFT TWO EMERGENCY LIGHTS ARE INOP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007101500226 20071015 00226 WP 2007 10 15 DXT2007F00001 2 20070929 A 7200 30751604 ENGINE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP RT ENGINE POWER LOSS E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 815QS 4227 258705 P107686 DURING TAKEOFF ROLL AT APPROXIMATELY V1 OF 111KIAS, THE NR 2 COMPUTER FAILED (STEADY LIGHT) IT WAS ACCOMPANIED BY A ROLL BACK OF THE NR 2 ENGINE AND A SUBSEQUENT APR TRIGGER (EVENT) DURING INITIAL CLIMBOUT. THE NR 2 ITT READ 996 DEG FOR APP ROXIMATELY 1 MINUTE UNTIL WE COULD PULL THE ENGINE BACK TO MAINTAIN LIMITS. REPLACED NR 2 ENGINE, OPS/LEAK CHECKS GOOD. ALL WORK DONE IAW HAWKER 800XP AMM 71-01-00 & 72-00-00 REF (LIT) WO: 19-1307-1.1 2 L 7 2 4F 4 F RT A3EU E6WE 2007101500228 20071015 00228 EU 2007 10 15 BAQA200700033 1 20071002 A 6410 117317411 BLADE BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR CRACKED E BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 117NC 2216 182 7517 WHILE PERFORMING A PREFLIGHT A CRACK WAS FOUND IN THE TAIL ROTOR BLADE NEAR THE DATA TAG. 1 G 7 2 3U 3 U NC H13EU E19EU 2007101500232 20071015 00232 CE 2007 10 15 N3B2007F00002 1 20070910 A 3230 50410015 BELLCRANK CESSNA 402 402B 207590P CE CONT O520 TSIO520EB 17040 SO LT MLG TRUNNION BROKEN E N3BA O OTHER O OTHER LD LANDING 1 SW 01 402BF 10616 402B1076 271015R LT MAIN LANDING COLLAPSED ON LANDING. IT APPEARS THAT BELLCRANK ASSEMBLY, PN 50410015 FAILED DURING EXTENSION CYCLE. ( K) 1 L 7 2 3O 3 O A7CE E8CE 2007101600006 20071016 00006 CE 2007 10 16 GUUA09280701 1 20070928 A 3210 130909B38 BOLT BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT MLG UNKNOWN A GUUA O OTHER J WARNING INDICATION CL CLIMB 1 SO 29 87552 UE216 AFTER TAKEOFF AT TNT LT MAIN LANDING GEAR GREEN ANNUNCIATOR BLANK OUT AND RED HANDLE ILLUMINATED. RECYCLED LANDING GEAR TWO TIMES WITH SAME RESULTS.CONTINUED TO FLL. MANUALLY EXTENDED LANDING GEAR LANDED WITHOUT INCIDENT. INSPECTED LANDIN G GEAR SYSTEM INSTALLED BOLT ON LT LANDING GEAR DRAG BRACE RIG-PLATE.OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101600007 20071016 00007 SO 2007 10 16 GUUA09280702 1 20070928 A 3260 PQD120411261 PROXIMITY SWITCH EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE MLG MALFUNCTIONED A GUUA O OTHER N FALSE WARNING CL CLIMB 1 SO 29 266AS 120188 AFTER TAKEOFF UPON LANDING GEAR RETRACTION RIGHT MAIN GEAR "A" RED LIGHT ILLUMINATED WITH SOUND OF DOOR OPEN IN SLIPSTRE AM. REPLACED RT MAIN LANDING GEAR UPLOCK "A" PROXIMITY SWITCH. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 2007101600017 20071016 00017 GL 2007 10 16 DJFA2007111 2 20070928 A 7261 CARBON SEAL EMB 135 EMB135BJ 3260306 SO ALLSN AE300 AE3007A GL ENGINE LEAKING E DJFA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 23 907LX 1490 14500966 CAE312924 THE CREW REPORTED A NORMAL TAXI AND WERE CLEARED FOR TAKEOFF. AT 80 KNOTS THE CREW DETECTED SMOKE. THEY ACHIEVED V1 AT THAT TIME AND THE CREW WAS CERTAIN IT WAS SMOKE THE CREW COMPLETED THEIR TAKEOFF AND NOTIFIED ATC AND REQUESTED AN ATB TO CLE ALL THE EMERGENCY CKECKLIST WAS COMPLETED. MX TROUBLESHOT SMOKE IN CABIN / COCKPIT AND FOUND NR1 ENG "0" CARBON SEAL LEAKING. ZERO CARBON SEAL WAS REPLACED, MX RAN AIRCRAFT WITH NO SMOKE/ SMELL NOTED. 2 L 7 2 4F 4 F RT TE6CH 2007101600022 20071016 00022 EU 2007 10 16 RMXA2007002 1 20071004 A 5311 FRAME2L FRAME BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101750B1 41560 NE TAILCONE CRACKED E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 117MK 8535 629 7196 DURING SCHEDULED INSPECTION A 18MM LONG CRACK WAS DISCOVERED ON THE LT 'A' FUSELAGE FRAME 2L. THE CRACK IS ON THE LOWER SKIN ONLY OF A DOUBLE SKIN ASSEMBLY. THE CRACK ORIGINATES FROM A BOLT HOLE, EXTENDS 9MM IN EACH DIRECTION FROM THE BOL T HOLE. THE BOLT IS USED FOR THE LOWER FORWARD ATTACHING SUPPORT FOR THE ECU (ENVIRONMENTAL CONTROL UNIT) 1 G 7 2 3U 3 U NC H13EU E5NE10 2007101600023 20071016 00023 SW 2007 10 16 2007F00057 1 20071004 A 5330 3P5340A01131 PANEL AGUSTA AB139 AB139 0260110 SW FUSELAGE DELAMINATED B U0GA K NONE O OTHER IN INSP/MAINT 1 EA 17 139EH 1491 31027 AFT UPPER DECK BETWEEN STATIONS 7920MM AND 7720MM IS DEBONDED. THE AREA IS APPROXIMATELY 800MM WIDE AND 200MM LONG. WATE R WAS FOUND INSIDE THE HONEYCOMB CORE. 2 G 7 2 4U R00002RD 2007101600025 20071016 00025 CE 2007 10 16 DJFA2007113 1 20071001 A 2120 UNKNOWN BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE LAVATORY ODOR E DJFA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 473LX RK518 CREW NOTED AN "ACRID ODOR" FROM THE LAV AREA. AIRCRAFT DIVERTED AND LANDED SAFELY. MAINTENANCE PERFORMED A VISUAL INSP ECTION OF THE LAV AREA AND FOUND NO DISCREPANCIES. MAINTENANCE PERFORMED AN ENGINE RUN WITH NO DEFECTS NOTED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007101600027 20071016 00027 CE 2007 10 16 AMWA0828013A 1 20071002 A 5730 1181100152 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT WING DAMAGED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 176YV 26646 UE176 RT UPPER WING SKIN BETWEEN WS117.5 AND WS133 HAD NUMEROUS ELONGATED HOLES FROM OVERSIZED RIVETS. REPAIRED IAW REPORT NR 6878-1 REV IR. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101600032 20071016 00032 CE 2007 10 16 AMWA0828013H 1 20071002 A 5311 12943003623 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FS 363.25 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 176YV 26646 UE176 REPAIRED FUSELAGE FRAME DAMAGED BY FRICTION CHAFING AT RT FS 363.25. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101600035 20071016 00035 CE 2007 10 16 AMWA0828013D 1 20071002 A 5311 1294300321 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FS 243.25 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 176YV 26646 UE176 REPAIRED FUSELAGE FRAME DAMAGED BY FRICTION CHAFING AT FS 243.25, RT. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101600039 20071016 00039 CE 2007 10 16 AMWA0828013 1 20071002 A 5711 1181000131 SPAR CAP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT WING CORRODED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 176YV 26646 UE176 BIO CORROSION LT MAIN SPAR, LWR CAP FROM APPROX WS119.5 TO WS122. REPAIRED IAW REPORT NR 6872 REV IR. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101600040 20071016 00040 EU 2007 10 16 BAQA200700034 1 20071001 A 6320 1171200501 GEARBOX BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101* NE MAIN ROTOR MISALIGNED E BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 296GL 7883 2736 7222 WHILE PERFORMING THE FIRST SPACER TUBE INSPECTION SINCE OVERHAUL ON THE MAIN GEARBOX THE LOWER MOUNT P/N 117-12415-01 S/ N KA-0267 WAS REMOVED AND HAD MECHANICAL DAMAGE DUE TO THE ANTI-ROTATION PINS ON THE SPACER ASSY. P/N 117-12418-01 BEING MISALIGNED ON THE MOUNT CAUSING DAMAGE TO THE SPACER ALSO. 1 G 7 2 3U 3 U NC H13EU E5NE 2007101600042 20071016 00042 SW 2007 10 16 200709152121 1 20070915 A 2697 472110 FEEDER CABLE BELL 222 222UT 1182148 SW LYC LTS101 LTS101750C1 41560 NE FIRE WARNING SYS SHORTED E RMXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 05 911MK 47515 CABLE SHORTED, CAUSING FALSE FIRE WARNING INDICATION. 1 G 7 2 3U 3 U H9SW E5NE 2007101600044 20071016 00044 CE 2007 10 16 DJFA2007114 1 20071003 A 5511 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 413LX RK209 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THI S AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. MAINTENANCE REPLACED THE RIB. 2 H 7 2 4F 4 F RT A16SW E25EA 2007101600047 20071016 00047 CE 2007 10 16 100407N342CS 1 20071004 A 3260 V332 DOWNLOCK SWITCH CESSNA 500 550 2076604 CE CONT C85 C85* 17008 SO NLG FAILED E Z5FA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 63 342 2346 5501101 ON APPROACH, AFTER LANDING GEAR SELECTION NOSE LANDING GEAR DOWNLOCK GREEN LIGHT DID NOT ILLUMINATED. AIRCRAFT LANDED UN EVENTFULLY. NOSE LANDING GEAR ACTUATOR REPLACED AND AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 4F 3 O A22CE E233 2007101600048 20071016 00048 SW 2007 10 16 904510062007 1 20071006 A 2197 609001 WIRE BOLKMS 117 BK117C2 5626002 SW CABIN FAN ARCED E QMLA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NM 03 103VU 9054 DURING SEVERAL FLIGHTS ON OCTOBER 5, 2007 THE FLIGHT CREW NOTICED A BURNING ODOR IN THE AIRCRAFT BUT COULD NOT DETERMINE A SOURCE FOR THE ODOR. THE ODOR WAS THAT OF BURNING RUBBER AND ONLY OCCURRED DURING LANDING AS AIRCRAFT PASSED THROUGH ETL (EFFECTIVE TRANSLATIONAL LIFT), HOWEVER THE ODOR THE NOT OCCUR ON EACH LANDING. AFTER EACH LANDING THE AIRCRAFT WAS CHECKED WITH NO SOURCE OF THE ODOR BEING FOUND BUT IT WAS MORE PRONOUNCED IN THE BACK CABIN AREA. THE MECHANIC TODAY TOO K THE AIRCRAFT OUT OF SERVICE TO PERFORM MAINTENANCE AND INSPECTED THE AIRCRAFT TO TRY AND DETERMINE THE SOURCE OF THE B URNING ODOR. AFTER DROPPING THE PANELS FOR THE AFT AIR CONDITIONING IT WAS DISCOVERED THAT THE POWER WIRE FOR THE AFT CA 1 G 7 2 3U H13EU 2007101600049 20071016 00049 EA 2007 10 16 NW6A0071001 1 20071006 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE EMERGENCY LIGHT INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 162GJ 10254 RT FORWARD EMERGENCY LIGHT INOP, REPLACED BULB. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007101600053 20071016 00053 NM 2007 10 16 200700301 1 20071008 A 3350 L47 LIGHT BOEING 757 7572Q8 1384972 NM PWA 2037 PW2040 NE ESCAPE SLIDE INOPERATIVE B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 405JS 29380 EMERGENCY SLIDE LIGHT L47 AT DOOR L3 IS DEACTIVATED DUE TO EXCESSIVE CURRENT DRAW ON EMERGENCY LIGHT PACK ASSEMBLY M735 WHICH CAUSES ALL EMERGENCY LIGHTS ASSOCIATED WITH THAT PACK TO BE RENDERED INOPERATIVE. REMOVED LAMP FROM LIGHT ASSY L47 . TRANSFERRED TO EOS AIRCRAFT MAINTENANCE LOG BOOK PAGE 03755 ITEM 2M. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101600056 20071016 00056 CE 2007 10 16 GUUA09260701 1 20070926 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 213 S13-14L DAMAGED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87555 UE234 AT SCHEDULED INSPECTION DISCOVERED LT FUSELAGE SKIN EXFOLIATED AT FS 213.250 BETWEEN STRINGERS 13L TO 14L. REMOVED DAMAG ED SKIN AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW SRM 51-70-06. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101600057 20071016 00057 CE 2007 10 16 GUUA09160702 1 20070916 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 290-326 CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81536 UE152 AT SCHEDULED INSPECTION DISCOVERED SEVERAL SPOTS OF SURFACE CORROSION ON AIRCRAFT BELLY SKIN BETWEEN LBL 29.06 AND RBL 2 9.06 FS 290.50 AND 326.00.REMOVED DAMAGED SKIN FABRICATED AND INSTALLED NEW SKIN PANEL FROM IAW FAA APPROVED DATA CONT AINED IN FIELD REPAIR FR-CO-01592, REV 1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101600058 20071016 00058 CE 2007 10 16 GUUA09240702 1 20070924 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 288 CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 49543 UE181 AT SCHEDULED INSPECTION DISCOVERED AIRCRAFT BELLY RT SIDE HAS A FUSELAGE CRACK AT FS 288.0. STOP DRILLED CRACK AND INST ALLED EXTERNAL REINFORCEMENT DOUBLER IAW STRUCTURAL REPAIR MANUAL 53-90-18. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101600059 20071016 00059 CE 2007 10 16 DXTA200702525 1 20071005 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 351QS 5600451 THE BRAKE PEDALS NEED TO BE PUSHED HALF WAY DOWN TO GET BRAKES TO ACTIVATE AND DURING TAXI BRAKES PULSATE/GRAB. 10-29-0 7 COMPLIED WITH ON-GROUND MODE TEST & ANTI-SKID SELF TEST IAW AMM 32-42-00 & FOUND NO DEFECTS. BOTH BRAKE PRESSURES WER E AT 800 PSI WITH EITHER WHEEL SPEED TRANSDUCERS SPINNING. NO FAULT FLAGS INDICATED ON ANTI-SKID FAULT DISPLAY BEFORE, D URING, OR AFTER FUNCTIONAL TEST OF ANTI-SKID SYS. COMPLIED WITH BLEED ANTI-SKID BRAKE SYS & FOUND AIR TRAPPED IN BRAKE S YS. BLED AIR FROM BRAKE SYS IAW AMM 32-42-00. COMPLIED WITH VISUAL INSPECTION OF WHEEL SPEED TRANSDUCER, NO DEFECTS NOTE D IAW WITH MM CH. 32-42-00. PERFORMED BRAKE OPS TAXI CHECK. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A22CE E25EA 2007101600060 20071016 00060 CE 2007 10 16 DXTA200702526 1 20071005 A 2460 CIRCUIT BREAKER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL FAILED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 936QS 7500036 CLIMBING THROUGH 17,000 FT, X'S APPEARED IN CAPTAINS PFD ON AIRSPEED & ALTIMETER TAPES, ADC1 FAIL MESSAGE APPEARED ON F MS SCRATCH PAD, FADEC FAIL L-R, MESSAGE APPEARED ON EICAS. FADECS WOULD NOT RESET. 10-29-07 TESTED, DID NOT CONFIRM. CHECKED FAULT HISTORY IN IMT. SAW SEVERAL ADC INVALID ERRORS LOGGED ON 10/5/07. CHECKED ADC BREAKER WHEN PULLED BREAKE R DID NOT MAKE NORMAL "CLICK" SOUND WHEN PULLED. HEAD EXTENDED BEYOND NORMAL, & HEAD SPUN. BREAKER INTERNALLY BAD. REPLA CED BREAKER. OPS CHECK GOOD IAW 34-11-07 OF MM. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007101600061 20071016 00061 CE 2007 10 16 DXTA200702527 1 20071005 A 3240 BRAKE ASSY CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG FAILED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 697QS 5605197 AFTER RELEASING THE PARKING BRAKE TO BEGIN TAXIING, THE AIRCRAFT BEGAN TO PULL HARD RT. 10-29-07 REMOVED FAULTY BR AKE ASSY. INSTALLED OVERHAULED BRAKE ASSY OF SAME P/N, BLED BRAKES. OPS CHECK GOOD. IAW MM 32-41-02. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007101600062 20071016 00062 NM 2007 10 16 DXTA200702530 1 20071006 A 3240 ISOLATION VALVE AMD FALC50 FALCON2000 2730170 NM PWC PW308 PW308C 52182 NE BRAKE MALFUNCTIONED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 223QS 86 WHEN BRAKES ARE APPLIED DURING LOW SPEED TAXI, BRAKES WILL RELEASE INTERMITTENTLY. 10-29-07 REPLACED DEFECTIVE BRA KE ISOLATION VALVE WITH UNIT INSPECTED BY EATON FH3R501L. REPLACED DEFECTIVE BRAKE SERVO VAVE WITH UNIT REPAIRED BY APR O XPER689K IN ACCORDANCE WITH F2000 EXEASY M/M 29-004 AND 32-412. OPERATIONAL AND LEAK CHECKS GOOD 2 L 7 2 4F 4 F RT A50NM E00065EN 2007101600063 20071016 00063 CE 2007 10 16 DXTA200702528 1 20071006 A 3260 SQUAT SWITCH CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 348QS 5600348 THE CABIN WOULD NOT PRESSURIZE AFTER TAKEOFF. 10-29-07 TROUBLESHOT TO INTERMITTENTLY FAILED LEFT SQUAT SWITCH. RE MOVED AND REPLACED LT SQUAT SWITCH. OPERATIONAL CHECKS GOOD AT THIS TIME. WORK DONE IAW. CESSNA MODEL 560 M.M. CHAPTER 21-31-04. 2 L 7 2 4F 4 F RT A22CE E25EA 2007101600064 20071016 00064 CE 2007 10 16 DXTA200702529 1 20071006 A 5210 HANDLE CESSNA 560 560XL 2076702 CE PAX DOOR OUT OF ADJUST E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 648QS 5605574 THE CABIN DOOR ANNUNCIATOR ILLUMINATED WHILE PASSING FL190. 10-29-07 ADJUSTED DOOR HANDLE SWITCH AND LUBED DOOR PINS . IAW CE-560XL M.M. 52-10-01. OP'S CHECK NUMEROUS TIMES. OP'S CK GOOD. 2 L 7 2 4F RT A22CE 2007101600065 20071016 00065 SO 2007 10 16 RAIA00710004 1 20071007 A 2720 GROMMET EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL RUDDER CABLES OBSTRUCTED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 829HK 145281 FLT NR 5513-STL-RUDDER FELT JAMMED; DRAGS WHEN PUSHED LT. MAINTENANCE INSPECTED RUDDER CABLES FOUND DUST DEBRIS IN GROMM ENTS UNDER CABIN FLOOR AND REMOVED. FUNCTION TEST ALL FLIGHT CONTROLS MOVEMENT OF RUDDER NORMAL. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007101600067 20071016 00067 CE 2007 10 16 DJFA2007115 1 20071005 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 785TA 6873 738 RK239 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER IB RIB AND BRACKET ASSEMBLIES, BOTH THE RT AND LT IB ROLLER BRACKETS WERE FOUND CRACKED. DETAILED INSPECTION INSTR UCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. MAINTENANCE REPLACED BOTH RIB ASSEMBLIES WITH THE IMPROVED ASSE MBLIES. 2 H 7 2 4F 4 F RT A16SW E25EA 2007101600068 20071016 00068 CE 2007 10 16 DXTA200702531 1 20071008 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 374QS 5600475 F/O'S BRAKES GO TO THE FLOOR WHEN PRESSED. 11-01-07 FOUND BRAKES TO BE SPONGY. BLEED BRAKES THREE TIMES IAW CE-560MM CH 32-42-00. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2007101600069 20071016 00069 CE 2007 10 16 GLBA20061009 1 20071008 A 5230 1294400491 HINGE FITTING BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CARGO DOOR DAMAGED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 261GL UE261 CARGO DOOR HINGE HALF FORWARD AND AFT LUGS MISSING AND SEVERAL LOOSE RIVETS. MAINTENANCE REPLACED HINGE HALF ON CARGO DO OR IAW SRM 52-90. RII INSPECTION COMPLIED WITH IAW TASKCARD 8.2.1. IWO NR 94171, L/P NR 207464. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101600070 20071016 00070 CE 2007 10 16 GUUA09270703 1 20070927 A 5510 1016200121 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT STABILIZER CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87555 UE234 AT SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT IB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED RT IB ELE VATOR HINGE BRACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101600071 20071016 00071 CE 2007 10 16 GUUA09270702 1 20070927 A 5510 1016200111 HINGE BRACKET BEECH 1900 1900C 1154161 CE PWA PT6 PT6A67D NE HORIZONTAL STAB CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87555 UE234 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED RT OB ELEVATOR HINGE BRACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101600078 20071016 00078 NM 2007 10 16 2007UALA04016 1 20071001 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROWS 32-34 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 FOUND EEL AT ROW 32-34 HJK AND 52HJK ARE INOP. REPAIRED SHORT CIRCUIT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007101600079 20071016 00079 NM 2007 10 16 2007UALA04017 1 20071001 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 FOUND EMERGENCY EXIT SIGN INOP DR 3R AFT. REPAIRED WIRING. 2 L 7 4 4F 4 F RT A20WE E24NE 2007101600080 20071016 00080 NM 2007 10 16 2007UALA04018 1 20071001 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 FOUND DR 1L EMERGENCY SLIDE ILLUM LIGHT INOP. RELAMPED 2 L 7 4 4F 4 F RT A20WE E24NE 2007101600084 20071016 00084 2007 10 16 2007UALA04022 4 20071001 A 2565 SLIDE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE AFT GALLEY DOOR, OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 932UA 26658 AFT GALLEY DOOR EVAC SLIDE GIRT, LOWER AFT PORTION HANGING OUT TOO FAR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600086 20071016 00086 NM 2007 10 16 2007UALA04024 1 20071002 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 FOUND UPPER DECK SEAT AREA 15AB CEILING EMERGENC Y LIGHT IS INOP. RELAMPED 2 L 7 4 4F 4 F RT A20WE E24NE 2007101600090 20071016 00090 NM 2007 10 16 2007UALA04029 1 20071002 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1425-1435 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 RT CREASE BEAM HAS CORROSION ON WEB UPPER SURFACE APPROX AT STA 1425-1435 FOUND OUT OF LIMITS. 10-26-07 MAJOR REPA IR ACCOMPLISHED. REMOVED DAMAGED AREA AND FABRICATED AND INSTALLED REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101600092 20071016 00092 NM 2007 10 16 2007UALA04032 1 20071001 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 FOUND LEFT AFT FLOOR EEL DIM ONLY. REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101600093 20071016 00093 EU 2007 10 16 2007UALA04033 1 20071002 A 2133 OUTFLOW VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN PRESSURE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 434UA 592 FLIGHT DIVERTED WITH PRESSURIZATION PROBLEM. 10-19-07 FOUND OUTFLOW VALVE 22HQ FAILED. REPLACED OUTFLOW VALVE 22HQ . 2 L 7 2 4F 4 F RT A28NM E40NE 2007101600096 20071016 00096 NM 2007 10 16 2007UALA04037 1 20071002 A 3350 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 850UA 1653 FOUND OVERWING EMERGENCY LIGHTS, LT AND RT SIDES INOP. 10-19-07 FOUND EPSU FAILED. REPLACED EPSU AND OPS CHECKED G OOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101600098 20071016 00098 NM 2007 10 16 2007UALA04039 1 20071003 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 3A BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 FOUND SEAT 3A SEAT MOUNTED EMERGENCY LIGHT BROKEN OFF. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007101600099 20071016 00099 NM 2007 10 16 2007UALA04040 1 20071002 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE 20HJ-25HJ INTERMITTENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 677UA 30029 20HJ TO 25HJ EMERGENCY STRIP LIGHTING ON AISLE SIDE OF SEATS FLICKERS ON INTERMITTENTLY. CYCLED SWITCHES COULD NOT DUPL ICATE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101600101 20071016 00101 NE 2007 10 16 2007UALA04042 2 20071004 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 SURGES A UALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 408UA 457 V10008 NR 2 ENGINE SURGED ON RUNWAY AT 140 KNOTS. 10-19-07 ACP HPC, HPT AND CLAPPER BORO INSPECTION. NO DAMAGE NOTED. AC P 7TH AND 10TH STAGE BLEED VALVE AND SOLONID CHECKED GOOD. ALSO LUBED VSV AND LPC. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101600104 20071016 00104 NM 2007 10 16 2007UALA04045 1 20071003 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 865 GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 FOUND UPPER FUSELAGE SKIN UNDER DORSAL FIN STA 865 BL 0 HAS DEEP GOUGE. MAJOR REPAIR: FABRICATED AND INSTALLED EXTERNA L DOUBLER, TRIPLER STRAPS AND FILLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600105 20071016 00105 NM 2007 10 16 2007UALA04046 1 20071003 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 787 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 FOUND AFT PIT SHEAR TIE CORRODED STA 787 STR 28L TO 28R LBL 5 RBL 5. MAJOR REPAIR: FABRICATED AND INSTALLED SHEAR TIE FRAME ATTACH REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600109 20071016 00109 NM 2007 10 16 2007UALA04050 1 20071003 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 S9L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 LT UPPER INTERIOR FUSELAGE STA 294.5 FRAME OB FLANGE AT STR 9L+2" HAS TOOLING DAMAGE THROUGH FLANGE. CUTOUT TOOLING DAM AGE. FABRICATED AND INSTALLED ANGLE DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600111 20071016 00111 2007 10 16 2007UALA04052 4 20071003 A 2565 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R3 DOOR SLIDE INOPERATIVE A UALA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 WP 29 509UA 24763 FOUND SLIDE ARM LIGHT NOT ON AT 3R. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101600112 20071016 00112 NM 2007 10 16 2007UALA04053 1 20071003 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ROWS 23 AFT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 552UA 26641 FOUND EEL LIGHTS VERY DIM ROWS 23 AFT. REPLACED POWER STRIP AND ALL LAMPS FROM ROW 22 AFT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101600113 20071016 00113 2007 10 16 2007UALA04054 4 20071003 A 2565 62773317 SLIDE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE L3 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 NR 3 LT MED SLIDE IS FAULTY. REPLACED SLIDE ASSY. OK FOR RETURN FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007101500071 20071015 00071 NM 2007 10 15 UPS07M50815 1 20070710 A 5753 HINGE DOUG MD11 MD11F 3023600 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C LEFT O/B FLAP I/B HINGE (FLAP MOUNTED) PIVOT LUG I/B BORE & SPOT FACES FOUND CORROSION AS MARKED. COR ROSION REMVD FROM AFFECTED AREAS & FOUND EXCEED LIMITS PER CMM57-52-0 4 PG 621-622 R58. ORG DIA 1.139" THK 0.497" FINAL DIA 1.189" THK 0.490" MATERIAL REVMD 0.007" MAX ALLOWED DIA 1.150" MIN ALLOWED THK 0.450". FPI C/O ON REWORK AREA, FOU ND NO CORR & CRACK. FLAP PEENING C/O BUSHING FAB, HEAT TREATED & INSTALLED PER EN1506-07. 2 L 7 3 4F RT A22WE 2007101500073 20071015 00073 NM 2007 10 15 SWAA074984 1 20071007 A 5755 FITTING BOEING 737 7373H4 1384600 NM NR 5 SPOILER WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 14Y CHECK, FOUND LEFT WING NR 5 SPOILER INBOARD ACTUATOR FITTING WORN. REPAIRED SPOILER PER SRM. 2 L 7 2 4F RT A16WE 2007101500076 20071015 00076 NM 2007 10 15 UPS07M50819 1 20070813 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT RIGHT 16 FOUND WITH CORROSION. CORR AT BARREL NUT BORE RE MVD PER SRM 51-21-01 VII R38. BTM BORE THRU & BORE REAM TO 1.067" DIA, REMN BLEND OUT 0.050" DEEP, EXCEED LIMITS. BARR EL NUT BORE, BLEND OUT VOID RADIUS SMOOTHEN & PROTECTED. BUCKET BUSHING FABRICATED, PROTECTED & INSTALLED. REPAIR C/O AT BARREL NUT BORE 16 RT IS ACCEPTABLE PER EN1520-07. 2 L 7 3 4F RT A22WE 2007101500077 20071015 00077 NM 2007 10 15 UPS07M50821 1 20070803 A 5320 BRACKET DOUG MD11 MD11F 3023600 NM BS 1216 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C LEFT UNDERSIDE CANTED PANEL AREA AT STA 1216.0 FOUND CANTED PANEL BRACKET CRACKED AS MARKED. REMOVED LWR AUX BLADDER CELL DECKING PNL LEFT AT STA 1216.0 FOR S/M ACCESS. FITTING AT STA 1216 FRAME TO CANT PANEL REMOVED. C RACKED BRACKET REMOVED. NEW BRACKET FASTENER HOLES PICKED UP. NEW BRACKET INSTALLED. FITTING AT STA 1216 FRAME TO CAN T PANEL REINSTALLED. LOWER AUX BLADDER CELL DECKING PANEL LINER AT LEFT STA 1216.0 INSTALL. 2 L 7 3 4F RT A22WE 2007101500079 20071015 00079 NM 2007 10 15 UPS07M50834 1 20070920 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 835-869 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C MAIN DECK FROM BS 835 TO BS 869, ALONG -X=9 (RBL 9 SEAT TRACK CROWN & FLANGE AREA FOUND CORRODED. REM OVED FOR ACCESS C/OUT ON CORROSION AFFECTED AREA AS MARKED MENTIONED ABOVE PER SRM 51-21-01 V2 REV 35, FOUND LIMIT EXCEE DED PER SRM 53-70-00 FIG 3 V1 REV 35. CORRODED SEAT TRACK REMOVED FROM STA 816 TO 869 RBL 9. NEW SEAT TRACK REWORKED P ER SRM 53-70-00D FIG 1 V1 R35 & HOLES P/UP COMPLETED. NEW SEAT TRACK RE-INSTALLED FROM STA 816 TO 869 PER SRM 51-31-01 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2007101500081 20071015 00081 NM 2007 10 15 UPS07M50836 1 20070716 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZONTAL STAB LEFT 01 BARREL NUT BORE FOUND CORRODED. CORR AT BARREL NUT BORE REMOVED PER SRM 51-21 -01 VII R38. BORE BOTTOM REMN BLEND OUT 0.030" DEEP & BORE REAMED TO 1.549" DIA, REMN BLEND OUT 0.050" DEEP, EXCEED LIM IT. BARREL NUT BORE, BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED PER SRM 51-21-01 VII R38. SLEEVE B USHING FAB, PROTECTED & INSTALLED. REPAIR C/O IS ACCEPTABLE PER EN1435-07. 2 L 7 3 4F RT A22WE 2007101500088 20071015 00088 NM 2007 10 15 HNAA0700218 1 20070705 A 5340 85310777110 CLAMP DHAV DHC8 DHC8102 2809003 NM WINDSHIELD CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 940HA 156 CORROSION FOUND ON LOWER CLAMP PLATE OF RIGHT WINDSHIELD. LOWER CLAMP PLATE OF RIGHT WINDSHIELD REPLACED IAW 56-10-11. 2 H 7 2 4T RT A13NM 2007101500089 20071015 00089 NM 2007 10 15 UPS07M50838 1 20070801 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT BORE RT 23 FOUND WITH CORROSION. CORR AT BARREL NUT BORE REMOVED PER SRM 51-21-01 VII R38. BOTTOM SURFACE CLEANED & BORE REAMED TO 1.067" DIA, REMN BLEND OUT 0.030" DEEP, EXCEE DS LIMIT. BARREL NUT BORE REAM FURTHER TO 1.105" DIA BARREL NUT BORE, BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHE N & PROTECTED. SLEEVE BUSHING FAB, PROTECTED & INSTALLED. REPAIR C/O IS ACCEPTABLE PER EN1488-07. 2 L 7 3 4F RT A22WE 2007101500095 20071015 00095 NM 2007 10 15 SWAA074959 1 20071004 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 410 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, RBL 3. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007101500097 20071015 00097 NM 2007 10 15 SWAA074958 1 20071004 A 5311 6545805 FRAME BOEING 737 7373H4 1384600 NM BS 277 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 15L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007101500102 20071015 00102 NM 2007 10 15 SWAA074962 1 20071004 A 5315 6546814 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 360 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 360, RBL 25. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007101500107 20071015 00107 NM 2007 10 15 SWAA074955 1 20071004 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 294 S11L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007101500109 20071015 00109 WP 2007 10 15 UPS07850873 1 20070918 A 5540 BRACKET DOUG DC8 DC873F 302199F WP JACKSCREW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 RUDDER TRIM JACKSCREW SUPPORT BRACKET CRACKED AT LWR AFT OUTBOARD CORNER. REMOVED JACKSCREW SUPPORT BRACKET IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR DOUBLER ON RUDDER JACKSCREW SUPPORT BRACKET IAW DWG 3700623 AN D SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007101500121 20071015 00121 NM 2007 10 15 SWAA074981 1 20071004 A 3350 311500 LENS BOEING 737 7373Q8 1384670 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 20 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007101500123 20071015 00123 NM 2007 10 15 SWAA074974 1 20071007 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 409WN 27896 EEPLS LENS CRACKED AT ROW 5 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007101500127 20071015 00127 WP 2007 10 15 MWEA070235 1 20071005 A 5311 FRAME DOUG DC9 DC981 3022081 WP BS 1497 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 814ME 48010 AFT FUSELAGE CANTED FRAME STATION 1497 IS CHAFED AT LOWER RIGHT SIDE. CUT OUT DAMAGE AND FABRICATED AND INSTALLED DOUBL ER. 2 L 7 2 4F A6WE 2007101500132 20071015 00132 NM 2007 10 15 HNAA0700212 1 20071006 A 2701 YOKE DHAV DHC8 DHC8102 2809003 NM COCKPIT STUCK A HNAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 07 827EX 390 FLIGHT CONTROL YOKE HUNG UP MOMENTARY DURING APPROACH. PILOT STATED THAT THE YOKE HANG UP HAPPENED IMMEDIATELY AFTER AU TO PILOT WAS DISENGAGED AND DURING ROLL. INSPECTED ENTIRE AILERON AND SPOILER CABLE CIRCUIT NO DEFECTS NOTED. PERFORME D GN OPS OF AUTO PILOT SUSPECT AILERON SERVO HUNG UP. REMOVED AND REPLACED AILERON SERVO IAW 22-12-00. SENT FOR AN EVA LUATION FLIGHT, EVALUATION SATISFACTORY. MORE TO FOLLOW. 2 H 7 2 4T RT A13NM 2007101500133 20071015 00133 2007 10 15 SWAA074985 4 20071003 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007101500139 20071015 00139 NM 2007 10 15 HNAA0700197 1 20070612 A 5311 SPAR DHAV DHC8 DHC8102 2809003 NM LT WING CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 907HA 011 ANGLE FOUND CRACKED AT JUNCTION OF LEFT NACELLE AND FRONT SPAR, STA YW39.00. LT FRONT SPAR BLEED AIR TUBE REMOVED TO AC CESS PER AMM 20-14-01. ANGLE REMOVED AND REPLACED IAW SRM 51-40-00. REINSTALLED BLEED TUBE. 2 H 7 2 4T RT A13NM 2007101500140 20071015 00140 EU 2007 10 15 USAA070722 1 20071005 A 5322 D5347112420100 SHEAR TIE AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 186US 1701 SHEAR PLATE AT SIDE BETWEEN FRAME 69-70 S-23R HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72- 11, DEFECT SIZE: 2 SQ INCHES. 2 L 7 2 4F RT A28NM 2007101500143 20071015 00143 EU 2007 10 15 USAA070719 1 20071005 A 5320 FLOOR SUPPORT AIRBUS A321 A321211 3930370 EU FLOOR BEAM -Y129 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 186US 1701 FLOOR SUPPORT -Y1292 BETWEEN FR 64-69 HAS CORROSION. REMOVED AND REPLACED PAX FLOOR SUPORT PER SRM 51-72-11, DEFECT SIZ E: 2 INCHES. 2 L 7 2 4F RT A28NM 2007101500151 20071015 00151 EA 2007 10 15 VNAA0710002 1 20071005 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE CABIN ODOR A VNAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 05 725PS 10186 CREW REPORTED A STRONG ODOR OF FUEL IN THE CABIN SHORTLY AFTER TAKEOFF AT APPROXIMATELY 4,000 FEET. CREW ELECTED TO RET URN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE RAN THE PACKS OFF THE ENGINE AND APU AND COULD NOT DUPLICATE THE PR OBLEM ON THE GROUND. AIR CONDITIONING SYSTEM OPS CHECKS GOOD IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. SUSPE CT ODOR CAME FROM PREVIOUS AIRCRAFT THAT TOOK OFF PRIOR TO THIS ONE. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007101500153 20071015 00153 NM 2007 10 15 KCSA071443 1 20071005 A 5311 FRAME BOEING 747 7472B4B 138481B NM BS 1920 S41-42L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA 1920 FRAME IS CRACKED 1 INCH BETWEEN STR 41L AND STR 42L. 2 L 7 4 4F RT A20WE 2007101500160 20071015 00160 EU 2007 10 15 YENA2007089 1 20071005 A 2910 D2901010201200 LINE AIRBUS 320 A320232 3930326 EU NR 2 PYLON RUPTURED A YENA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 15 544JB 21660 1835 ABOUT 1 HR FROM LANDING HYD Y RSVR LO LVL. THEN NO FLUID, HYD Y LOW AIR PRESSURE. FOUND CRACKED LINE IN NR 2 PYLON PER MM 29-11-49-04. REMOVED AND REPLACED NR 2 ENG HYD EDP PRECAUTIONARY DUE TO OPS WITHOUT FLUID POSSIBLE PER AMM 29-13-51 -000-010. OPS CHECK & LEAK CHECK OK. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2007101500166 20071015 00166 NM 2007 10 15 UPS07550866 1 20071005 A 3350 LAMP BOEING 757 75724APF 1384969 NM EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 452UP 25473 EMERGENCY LIGHT ASSY HAS SIX LAMPS INOP. RELAMPED THE SIX LAMPS IN THE EMERGENCY LIGHT ASSY PER MM 33-51-01-2, OPS CHEC KS GOOD. 2 L 7 2 4F RT A2NM 2007101500167 20071015 00167 NM 2007 10 15 UPS07650845 1 20070920 A 5320 143T592546 PLATE BOEING 767 76734AF 1385212 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 328UP 27754 INSPECTION TYPE:C1 CORROSION ON NUT PLATE HOLE. BLENDED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-00-51. 2 L 7 2 4F RT A1NM 2007101500169 20071015 00169 NM 2007 10 15 HNAA0700221 1 20070704 A 5754 NAS75703L BUSHING DHAV DHC8 DHC8102 2809003 NM FLAP TRACK CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 940HA 156 RIGHT FLAP TRACK NR 4 FOUND ALL FOUR BUSHING AT FLAP TRACK ATTACHMENT CORRODED. RIGHT FLAP TRACK CARRIAGE NR 4, FOUR BU SHING INSTALLED AS PER 20-19-02. 2 H 7 2 4T RT A13NM 2007101500170 20071015 00170 NM 2007 10 15 ZZDA2007277 1 20071004 A 5320 PAN BOEING 717 717200 1383700 NM CARGO DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 955AT 55017 FWD CARGO COMPARTMENT LOWER DOOR CUTOUT PAN. CUT OUT BETWEEN FUSELAGE STA 370 TO 427 HAS SURFACE CORROSION. REPLACED L OWER DOOR PAN AT FWD CARGO COMPARTMENT IAW B717 SRM 53-20-15 REPAIR 6. 2 L 7 2 4F TR A6WE 2007101500171 20071015 00171 NM 2007 10 15 ZZDA2007278 1 20071005 A 5311 FRAME BOEING 717 717200 1383700 NM BS 1178 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 955AT 55017 TWO EACH CRACKS, BOTH 1 INCH LONG IN RADIUS OF CANTE FRAME LEFT SIDE STA 1178 LONG 16 LEFT. INSTALLED FORMED ANGLE REPA IR PER SRM 51-70-11 F-201. 2 L 7 2 4F TR A6WE 2007101500177 20071015 00177 NM 2007 10 15 USAA920070903 1 20071005 A 5313 65C3079911 STRINGER BOEING 737 7373B7 1384580 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 23381 CLT - MAJOR REPAIR - C-4 CHECK, CRACKED STRINGER WEB, BS 727, S18A LEFT. REPAIRED STRINGER WEB, BS 727, S18A LEFT IAW U SAIRWAYS EA 98912. 2 L 7 2 4F RT A16WE 2007101500181 20071015 00181 NM 2007 10 15 SWAA074977 1 20071007 A 5330 6545774 SKIN BOEING 737 7373G7 1384595 NM BS 739E S18R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739E, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007101500184 20071015 00184 NM 2007 10 15 SWAA074983 1 20071007 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 947-967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CORRODED BETWEEN BS 947 AND BS 967, STR 26L AND STR 27L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007101500187 20071015 00187 SO 2007 10 15 C2XA07IA217 1 20071007 A 3240 429515 CONTROL UNIT EMB 145 EMB145EP 3260221 SO MLG BRAKES INOPERATIVE A C2XA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 13935 7354 7354 145022 IAH - FLIGHT 2185, THE CREW REPORTED THAT BOTH RIGHT MAIN LANDING GEAR BRAKES WERE INOP. MAINTENANCE REMOVED AND REPLAC ED THE BRAKE CONTROL UNIT (BCU), OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. 2 L 7 2 4F RT T00011AT 2007101500188 20071015 00188 SO 2007 10 15 C2XA07IA219 1 20071006 A 3230 355022002 ELECTRONIC UNIT EMB 145 EMB145XR 3260214 SO MLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 11113 13598 13598 145662 BJX - FLIGHT 2193, THE CREW REPORTED A LANDING GEAR LEVER DISAGREE, AND THE GEAR WAS STUCK DOWN AFTER T/O. THE AIRCRAFT RETURNED TO BJX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND IT WAS FERRIED TO IAH WHERE I T LANDED WITHOUT INCIDENT. IAH MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT, (LGEU), OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007101500189 20071015 00189 SO 2007 10 15 C2XA07IA216 1 20071003 A 2530 COFFEEMAKER EMB 145 EMB145LR 3260212 SO GALLEY ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 14998 145302 IAH - FLIGHT 2145, THE CREW REPORTED AN ELECTRICAL BURNING ODOR COMING FROM ABOVE THE COFFEE POTS. MAINTENANCE OPERATIO NALLY CHECKED BOTH COFFEEMAKERS WITH NO DEFECTS, AND FOUND THE ODOR TO BE COMING FROM OLD COFFEE IN THE POTS. THE AIRCR AFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007101500193 20071015 00193 NM 2007 10 15 PCCA0701536 1 20071002 A 2780 1267629 DRIVE SYSTEM BOEING 747 74747UF 1384812 NM TE FLAPS FAILED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 416MC 32838 STATUS MESSAGE LE MULTI DRIVE AND EICAS FLAPS PRIMARY. GOT MSG AFTER EXTENDING FLAPS T/O. RETURNED TO GATE. REMOVED A ND REPLACED 3-R L/E DRIVE 2 L 7 4 4F RT A20WE 2007101500194 20071015 00194 EU 2007 10 15 07FDEA04505 1 20071005 A 5711 A57110430 SPAR AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CRACKS IN SEVERAL HOLES ON CENTER SPAR WEB C 44 REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL CRACK REMOVAL, BUSH AND NEW FASTENER INSTALLTION IAW EA 6-5710-106488 AND RAS 052365/022/2007 ISS A. 2 L 7 2 4F RT A35EU 2007101500203 20071015 00203 EU 2007 10 15 07FDEA04515 1 20071005 A 5730 A57340088 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION AT RT WING LOWER SKIN RIB 20-21. REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTECTION IAW EA 6-5720 -112459 AND RAS/BAE/1005302/2007 ISS A. 2 L 7 2 4F RT A35EU 2007101500205 20071015 00205 EU 2007 10 15 07FDEA04517 1 20071005 A 5730 A57340088 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND ON LT OUTER WING ON MANHOLE FLANGE RIB 23-24 CORROSION. REPAIR PERFORMED BLEND OUT CORROSION IAW SRM 57-20-12 PAR A 4 A, NDT FOR CRACK FREE IAW EA 6-5720-106525 AND RAS//BAE/1005053/2007 ISS A. 2 L 7 2 4F RT A35EU 2007101500207 20071015 00207 NM 2007 10 15 TSAA0721054 1 20071001 A 5297 AN32101 WIRE BOEING 737 7372X6C 1384552 NM E/E BAY DOOR BROKEN A TSAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 840AL 23124 NON-ETOPS CARGO FLIGHT 909 HNL-LIH - DURING CLIMB, THE CREW NOTED THAT THE PRESSURE CONTROL PANEL SHOWED AUTO FAIL AND T HE AIRCRAFT WAS NOT PRESSURIZING. THE CREW ATTEMPTED TO SWITCH TO STANDBY CONTROL AND WERE STILL UNABLE TO PRESSURIZE T HE CABIN. THE CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE ELECTRONIC EQUIPMENT BAY DOOR UNLAT CHED AND OPEN. MAINTENANCE ALSO FOUND A DAMAGED WIRE ON THE DOOR OPEN SWITCH INDICATOR CIRCUIT. THIS PREVENTED DOOR OP EN ANNUNCIATION ON THE FLIGHT DECK. THE AIRCRAFT WAS PRESSURE CHECKED WITH THE DOOR CLOSED AND RETURNED TO SERVICE UNDE R MEL 52-3 FOR THE INOPERATIVE DOOR INDICATION. MAINTENANCE LATER REPAIRED THE BROKEN SWITCH WIRE AND FUNCTION CHECKED 2 L 7 2 4F RT A16WE 2007101500208 20071015 00208 EU 2007 10 15 2007UALA03998 1 20071001 A 2700 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ELAC SYS FAULTED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 403UA 442 ELAC 2 FAULT DISPLAYED ON LOWER ECAM. 10-19-07 FOUND ELAC NR 2 FAULT. REPLACED AND RESET ELAC 2 AND ACP AFS TEST - NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101500209 20071015 00209 NM 2007 10 15 2007UALA03999 1 20071001 A 3150 WARNING LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE ILLUMINATED A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 907UA 25007 FEEL DIFF PRESS ILLUM AGAIN DURING DESCENT. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101500210 20071015 00210 EU 2007 10 15 2007UALA04000 1 20071002 A 2910 HYDRAULIC SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN SYS CONTAMINATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 477UA 1514 GREEN RSVR LOW LVL DISPLAYED ON ECAM. A/C TOWED TO THE GATE. 10-19-07 FOUND HYDRAULIC SYSTEM CONTAMINATED. REPLAC ED NR 1 EDP AND HYDRAULIC LINE, FILTERS DOWNLINE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101500211 20071015 00211 EU 2007 10 15 2007UALA04001 1 20071001 A 2820 ACTUATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE TRANFER SYS FAULTED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 412UA 465 FLIGHT DIVERTED DUE TO A FUEL TRANSFER PROBLEM. 10-19-07 FOUND FAULTY NR 2 RIGHT WING TRANSFER VALVE ACTUATOR. R EPLACED NR 2 RIGHT WING TRANSFER VALVE ACTUATOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101500214 20071015 00214 2007 10 15 2007UALA04004 4 20071001 A 2565 SLIDE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE R2 DOOR MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 768UA 26919 DOOR 2R ESCAPE SLIDE PACK IS FAULTY. 2R ESCAPE SLIDE PACK REPLACED. SLIDE APPEARED TO BE IMPROPERLY INSTALLED. AIRCRA FT OK SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007101500216 20071015 00216 NM 2007 10 15 2007UALA04006 1 20070929 A 3350 POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 675UA 29243 EMERGENCY PATH LIGHTING TRIM AT SEAT 28A BROKEN. REPLACED POWER SUPPLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101500221 20071015 00221 NM 2007 10 15 2007UALA04011 1 20070929 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26877 FOUND SEATS 5A FWD, 8A AFT AND 56 HJK ARE INOPERATIVE. RELAMPED 2 L 7 4 4F 4 F RT A20WE E24NE 2007101500222 20071015 00222 NM 2007 10 15 2007UALA04012 1 20070929 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE R2 DOOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 FOUND DOOR 2R AFT SILL EMERGENCY LIGHT IS INOPERATIVE. RELAMPED 2 L 7 4 4F 4 F RT A20WE E24NE 2007101500224 20071015 00224 NM 2007 10 15 2007UALA04014 1 20070929 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 UPPER DECK FWD TWO CEILING EMERGENCY LIGHTS ARE INOP. RELAMPED 2 L 7 4 4F 4 F RT A20WE E24NE 2007101500225 20071015 00225 NM 2007 10 15 2007UALA04015 1 20071001 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CEILING ROWS 35 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 FOUND EMERGENCY CEILING LIGHTS INOP ROWS 35 HJK - 46 HJK. RELAMPED 2 L 7 4 4F 4 F RT A20WE E24NE 2007101600005 20071016 00005 CE 2007 10 16 GUUA09240701 1 20070924 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CABIN ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 29 53545 UE185 FLIGHT: 2043 TNT/FLL, DURING FLIGHT AIRCRAFT COCKPIT SMELLS LIKE FUEL THE ODOR WAS OVERWELMING. INSPECTED AIRCRAFT FOUN D NO EVIDENCE OF FUEL LEAK. PERFORMED ENGINE RUNS AT VARIOUS POWER SETTINGS NO FUEL ODOR NOTED. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101600008 20071016 00008 EU 2007 10 16 BAQA200700035 1 20071003 A 6720 742A070001 CLEVIS BOLKMS 117 BK117B2 5626013 EU TAIL ROTOR WORN E BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 296G 104 7222 WEAR DETECTED ON THE YAW ACTUATOR OF THE TAIL ROTOR IN THE CARDAN JOINT (CLEVIS) BUSHING BORE WHERE THE BOLT ATTACHES TO THE LOWER MOUNT SUPPORT. BORE WAS WORN TO AN EGG SHAPE. THE SUBJECT OF THIS PROBLEM IS ADDRESSED IN MFG ALERT SERVICE BULLETIN ASB-MBB-BK117-40-112 ISSUED MARCH 19,2007. PART ON ORDER. 1 G 7 2 3U NC H13EU 2007101600019 20071016 00019 CE 2007 10 16 DXTA200702522 1 20071003 A 3230 LANDING GEAR CESSNA 680 680CE 2076811 CE INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 378QS 6800103 AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT MOVE TO RETRACT LANDING GEAR. 10-29-07 ADJUSTED NOSE LANDING GEAR SQU AT SWITCH. OPS CHECKED GOOD. WORK DONE IAW 680 M.M. CHAPTER 32-60-00. 2 L 7 2 4F RC T00012WI 2007101600026 20071016 00026 CE 2007 10 16 DXTA200702524 1 20071004 A 2730 WARNING LIGHT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL STAB TRIM ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 964QS 7500164 PRIMARY STAB TRIM FAILED CLIMBING THROUGH FL280, NO CAS MESSAGE PRESENT. (10-29-07) R & R HORIZ STAB ECM IAW MM 27-40- 00. CHECK OK. PERFORMED VOLTAGE CHECKS ON ECM CONNECTORS PV003 & PV004, VOLTAGES & GROUNDS OK. RECEIVED POWER TO BOTH S EC. & PRIM. ACTUATORS. PERFORMED RESISTANCE CHECKS TO BOTH SEC. & PRIM. CLUTCH & BRAKE ASSY, CHECKS OK. TROUBLESHOOTING FOUND CONNECTORS PV003 & PV004 SWAPPED. CONNECTORS CORRECTED & PROBLEMS MOVED TO SECONDARY STAB & MOVING INTERMITTENTLY. CLEANED & TIGHTENED CONNECTORS, NO HELP. ECM BAD. TROUBLESHOT IAW MM 27-40-00 & CESSNA 750 EXPERT SYS. REMOVED ECM & IN STALLED MODIFIED ECM. PERFORMED PRIMARY CHANNEL A/B TRAVEL CHECKS PER MM TASK 27-40-00-721, NO FAULTS NOTED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007101600028 20071016 00028 CE 2007 10 16 AMWA0828013E 1 20071002 A 5311 12943003136 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 258.25 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 176YV 26646 UE176 REPAIRED LT AND RT FUSELAGE FRAMES DAMAGED BY FRICTION CHAFFING AT FS 258.25. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101600029 20071016 00029 CE 2007 10 16 AMWA0828013F 1 20071002 A 5311 12943003621 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 303.25 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 176YV 26646 UE176 REPAIRED FUSELAGE FRAME DAMAGED BY FRICTION CHAFING AT RT FS 303.25. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101600030 20071016 00030 CE 2007 10 16 AMWA0828013I 1 20071002 A 5311 12943003132 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FS 378.25 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 176YV 26646 UE176 REPAIRED FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT LT AND RT FS 378.25. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101600031 20071016 00031 CE 2007 10 16 AMWA0828013K 1 20071002 A 5311 1294400671 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FS 438.25 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 176YV 26646 UE176 REPAIRED FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT LT AND RT FS 438.25. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101600036 20071016 00036 CE 2007 10 16 AMWA0828013J 1 20071002 A 5311 12943003132 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FS 408.25 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 176YV 26646 UE176 REPAIRED FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT LT AND RT FS 408.25. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101600050 20071016 00050 CE 2007 10 16 GLBA20061008 1 20071001 A 5311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 177 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 261GL UE261 FRAME CRACKED AT STRINGER CUTOUT FS 177 AT STRINGER 9AR. REPAIRED FRAME AT STRINGER RELIEF HOLE FS 177 AND STRINGER 9AR IAW 1900D SRM 51-70. REPAIR DIMENSIONS 4.5 BY 2.5 . 2024 T-3 .080. RII COMPLIED WITH IAW TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101600052 20071016 00052 NM 2007 10 16 200700300 1 20071008 A 3350 S10294 SWITCH BOEING 757 7572Q8 1384972 NM PWA 2037 PW2040 NE EMERGENCY LIGHTS BROKEN B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 405JS 29380 MID AFT EMERGENCY LIGHT TEST SWITCH S10294 AT DOOR L3 IS BROKEN AND INOPERATIVE. TRANSFERRED TO EOS AIRCRAFT MAINTENANC E LOG BOOK PAGE 03755 ITEM 1M. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101600055 20071016 00055 SO 2007 10 16 GUUA10040701 1 20071004 A 3231 DOOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE MLG OUT OF ADJUST A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 29 268AS 120202 DURING APPROACH LANDING GEAR WOULD NOT EXTEND NORMALLY PERFORMED LANDING GEAR ELECTRICAL OVERIDE EXTENSION. LANDED WITH OUT INCIDENT. ADJUSTED IB AFT LANDING GEAR DOOR ON RT MAIN LANDING GEAR. LANDING GEAR SYSTEM OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2007101600072 20071016 00072 SO 2007 10 16 GUUA10060701 1 20071006 A 3260 922AA2YA6P2722 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE MLG FAILED A GUUA O OTHER N FALSE WARNING AP APPROACH 1 SO 29 268AS 120202 DURING APPROACH LANDING GEAR WOULD NOT EXTEND NORMALLY PERFORMED GEAR ELECTRICAL OVERRIDE EXTENSION. LANDED WITHOUT INC IDENT. REPLACED DOWN "A" PROXIMITY SENSOR. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 2007101600076 20071016 00076 CE 2007 10 16 DXTA200702519 1 20071003 A 3260 WARNING LIGHT CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG FALSE ACTIVATION E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 608QS 5605308 AFTER TAKEOFF, RETRACTED GEAR. THE RED GEAR UNLOCK LIGHT REMAINED ILLUMINATED. PERFORMED SLOW CYCLE TEST OF LANDING GEA R IAW MM CHAPTER 32-01-00. OPS CHECK GOOD. INSPECTED GEAR UPLOCKS IAW MM CHAPTER 32-30-05. NO DEFECTS NOTED. PERFORM ED (2) POSITION STAB OPS CHECK IAW MM CHAPTER 27-40-00. OPS CHECK GOOD. OPERATED GEAR IN CONJUNCTION WITH (2) POSITION STAB, NO DEFECTS NOTED. SYSTEMS OPS CHECK GOOD IAW MM CHAPTER 27-40-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007101600077 20071016 00077 CE 2007 10 16 DXTA200702520 1 20071003 A 2752 ACTUATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS OUT OF ADJUST E DXTA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 07 979QS 7500079 FLAPS FAIL AMBER CAS MESSAGE AFTER T/O. UNABLE TO RESET, FLAPS REMAINED STUCK AT 15 DEGREES. TROUBLESHOT DISCREPANCY T O A BINDING LT IB FLAP PANEL. ADJUSTED NR 5 ACTUATOR AND PROVIDED CLEARANCE. O/S CHECK GOOD. WORK PERFORMED IAW CHAPT ER 27-50-00 OF THE MM. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007101600085 20071016 00085 NM 2007 10 16 2007UALA04023 1 20071001 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 STRINGER 13L INTERCOSTAL ATTACHED ANGLE CRACKED AT STR 13L ON FWD SIDE OF FWD ENTRY DOOR CUTOUT ON REMOVAL FOR ACCESS FO R DOOR HINGE CUTOUT REPAIR. MAJOR REPAIR: REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600087 20071016 00087 NM 2007 10 16 2007UALA04025 1 20071002 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 FOUND SEATS 33 ABC, 37 ABC, 52 ABC AND 53 ABC EMERGENCY LIGHTS ARE INOPERATIVE. RELAMPED 2 L 7 4 4F 4 F RT A20WE E24NE 2007110700006 20071107 00006 EU 2007 11 7 2007UALA04451 1 20071027 A 2700 3945128102 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ELAC FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 419UA 487 AILERON SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. FOUND NR 1 ELAC FAULT CAUSING AIL SERVO FAULT DISPLAY. REPLACED N R 1 ELAC. OPS CHECK OK, NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101600088 20071016 00088 NM 2007 10 16 2007UALA04027 1 20071002 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1340 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 AFT PIT FRAME DENTED AT STA 1340 LT AND RT SLOPE AREAS. 10-26-07 MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE AREA A ND FABRICATED AND INSTALLED AN APPROVED REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101600089 20071016 00089 NM 2007 10 16 2007UALA04028 1 20071002 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1405-1420 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 RT CREASE BEAM HAS CORROSION ON WEB UPPER SURFACE AND SEVERAL RIVET HEADS AT STA 1405-1420 FOUND OUT OF LIMITS. 10-26 -07 MAJOR REPAIR ACCOMPLISHED. RIVET HEADS AT STA 1405-1420 FOUND OUT OF LIMITS. REMOVED DAMAGE AREA AND FABRICATE D REPAIR AND INSTALLED PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101600094 20071016 00094 NM 2007 10 16 2007UALA04035 1 20071002 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE 14AB LEFT LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 FOUND EXIT PATH LIGHTING LOOSE AT 14AB LEFT SIDE. REPAIRED DAMAGED EEL LIGHT CIRCUIT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101600095 20071016 00095 NM 2007 10 16 2007UALA04036 1 20071002 A 3350 BATTERY PACK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 823UA 952 EMERGENCY LIGHT TEST FOUND BATTERY FAULT AFT GALLEY AREA. 10-19-07 FOUND EPSU FAULTED. REPLACED EPSU. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101600097 20071016 00097 2007 10 16 2007UALA04038 4 20071002 A 2565 SLIDE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD GALLEY DOOR UNRELIABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FWD GALLEY DOOR EVAC SLIDE PRESSURE GAUGE NOT VISIBLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600100 20071016 00100 NE 2007 10 16 2007UALA04041 2 20071003 A 7230 BLADE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE COMPRESSOR FAILED A UALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 670UA 29240 727337 COMPRESSOR STALL ON TAKEOFF ROLL. CREW HEARD THREE LOUD POPS. ENGINE REPLACED. SHOP TEARDOWN REVEALED 1 BROKEN STAGE- 6 VARIABLE STATOR VANE ARM. THE FRACTURE SURFACE WAS DIRTY, INDICATING THAT THE VANE ARM BROKE IN SERVICE, AND NOT AT D ISASSEMBLY. THE BROKEN ARM RESULTED IN AN HPC BLADE TIP FRACTURE, AND SUBSEQUENT DOWNSTREAM HPC DAMAGE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101600107 20071016 00107 NM 2007 10 16 2007UALA04048 1 20071003 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 787 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 AFT PIT FUSELAGE INTERIOR SKIN CORRODED AT BS 787 RBL 5 TO LBL 5. FABRICATED AND INSTALLED EXTERNAL DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600108 20071016 00108 NM 2007 10 16 2007UALA04049 1 20071003 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 787 S25R CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 FOUND AFT PIT DOOR SURROUND WEB UPPER FLANGE, LOWER SIDE HAS CORROSION, BS 787+13" STR 25R. REMOVED CORROSION. FABRICAT ED AND INSTALLED FORMED SECTION REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600110 20071016 00110 NM 2007 10 16 2007UALA04051 1 20071003 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 794 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 FOUND AFT PIT FRAME CORRODED STA 794 RBL TO 15-28 STR 25-27R. FABRICATED AND INSTALLED REPAIR ANGLE, STRINGER CLIP AND REPAIR ANGLE CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600116 20071016 00116 NM 2007 10 16 2007UALA04057 1 20071003 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 309UA 23670 FOUND EEL FLOOR LIGHT INOP AT FWD FIRST CLASS CLOSET. REPLACED LIGHT STRIP. OP CHK GOOD 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600117 20071016 00117 NM 2007 10 16 2007UALA04058 1 20071003 A 3397 FEEDER CABLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 309UA 23670 FOUND EEL FLOOR LIGHTS INOP FROM SEAT 17 TO SEAT 21. REATTACHED FEEDER CABLE AND SECURED. OP CHK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600121 20071016 00121 NM 2007 10 16 2007UALA04062 1 20071004 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 FWD ENTRY DOOR CUTOUT UPPER HINGE HAS 2 EA FASTENER HOLES CRACKED. AFT ROW 1 EA ABOVE AND 1 EA BELOW HINGE CUTOUT. INS TALLED EXTERNAL SKIN DOUBLER AT HINGE CUTOUT. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600129 20071016 00129 NM 2007 10 16 2007UALA04070 1 20071003 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 853 S21-23R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 AFT CARGO DOOR CUTOUT, AFT SIDE BS 853 BETWEEN STRINGERS 21R-23R IS DAMAGED. MAJOR REPAIR: SKIN REPLACED. EXTERNAL DOU BLER TRIPLER REPAIR REINSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600131 20071016 00131 NM 2007 10 16 2007UALA04072 1 20071002 A 2800 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUEL SYSTEM UNKNOWN A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 641UA 25091 CREW COMMENTS: FUEL OVERBURN BY 6000 PLUS POUNDS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101600132 20071016 00132 NM 2007 10 16 2007UALA04073 1 20071001 A 2611 FIRE LOOP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 NACELLE FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 656UA 25394 EICAS MSG "ENG 1 FIRE LP2" DISPLAYED AT SHUTDOWN. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101600133 20071016 00133 NM 2007 10 16 2007UALA04074 1 20071002 A 2160 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN TEMP UNKNOWN A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 657UA 27112 CREW COMMENTS: TEMPS VERY DIFFICULT IN COCKPIT, FIRST, BUS CLASSES. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101600134 20071016 00134 2007 10 16 2007UALA04075 4 20071003 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 FOUND DOOR 4R SLIDE DIFFICULT TO ARM. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101600136 20071016 00136 NM 2007 10 16 07FDEA04481 1 20071003 A 5320 CHANNEL BOEING 727 7272S2F 1384O81 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 205FE 22927 THE RT WING TIP FWD FAIRING NUT PLATE CHANNEL IS CRACKED. THIS DISCREPANCY WAS DISCOVERED WHILE COMPLYING WITH NON-ROUT INE NR N00015. REPLACED CHANNEL IAW NR 7-5730-115028. REMOVED AND REPLACED NUTPLATE CHANNEL. 2 L 7 3 4F A3WE 2007101600137 20071016 00137 EU 2007 10 16 07FDEA04491 1 20071005 A 5712 A5796011320100 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 726FD 575 LT WING INBOARD FLAP RIB 25 FOUND CRACKED. REPLACED FLAP RIB 25 AND RUB AND ROLLER TRACK. 2 L 7 2 4F RT A35EU 2007101600140 20071016 00140 NM 2007 10 16 07FDEA04524 1 20071006 A 5753 65413321 CARRIAGE BOEING 727 727225 1384077 NM TE FLAPS DAMAGED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 462FE 22550 SPLIT FLAPS OUTBOARD ON DEPARTURE. COMPLIED WITH QRH FLAPS WOULD NOT RETRACT VIA ALTERNATE METHOD. CREW DEBRIEFED OUT BD FLAPS STAYED AT 5 DEG WHILE INBD FLAPS CAME TO 2 DEG AS COMMAMDED. L/E VALVE C/B ON P6 PANEL PULLED BY CREW AS PART OF QRH. REF WRI 27-50/9927. FOUND LT O/B FLAP, I/B SEQUENCING CARRIAGE, (ON TOP OF FLAP CARRIAGE) HAS ROLLERS MISSING. NO DAMAGE NOTED ON FLAP TRACK, OR TO THE SEQUENCING CARRIAGE CASTING. COMPLETED INSTALLATION OF LT WING, O/B FLAP, I/ B TRACK TOGGLE LINK CARRIAGE PER 727-200 M/M 27-51-014-2. 2 L 7 3 4F A3WE 2007101600141 20071016 00141 NM 2007 10 16 07FDEA04525 1 20071007 A 3220 FITTING DOUG MD11 MD11F 3023600 NM ZONE 700 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 NOSE LANDING GEAR RIGHT SIDE LOAD FITTING, FOUND AREA HOLE ELONGATED. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX E A 1-5310-115220, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007101600142 20071016 00142 NM 2007 10 16 07FDEA04526 1 20071008 A 5730 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 LEFT WING, NR 5 LEADING EDGE SLAT OUTBOARD TRACK CUTOUT LOWER EDGE FOUND CRACK. 10-24-07 REPAIR CARRIED OUT AS PER S RM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007101600143 20071016 00143 NM 2007 10 16 07FDEA04527 1 20071008 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 FASTENER HOLE FOUND CRACK AT 3 O'CLOCK POSITION AT NOSE LANDING GEAR LEFT TRUNNION FITTING LOWER LONGERON. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-115207, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007101600144 20071016 00144 NM 2007 10 16 07FDEA04528 1 20071008 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 FASTENER HOLE FOUND CRACK AT 3 O'CLOCK POSITION AT NOSE LANDING GEAR RIGHT TRUNNION FITTING LOWER LONGERON. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-115206. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007101600145 20071016 00145 NM 2007 10 16 07FDEA04529 1 20071008 A 5730 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 CRACK INDICATIONS REVEALED FASTENER HOLES AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT EDGE. 10-24-07 REPAIR CARRIE D OUT AS PER FEDEX EA 1-5710-115213. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007101600147 20071016 00147 NM 2007 10 16 07FDEA04531 1 20071008 A 5730 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 RIGHT WING LEADING EDGE SLAT NR 6 INBOARD SLAT TRACK CUTOUT (SLAT TRACK NR 12), FOUND CRACK AT CORNER EDGE. 10-24-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 . 2 L 7 3 4F RT A22WE 2007101600149 20071016 00149 EU 2007 10 16 07FDEA04533 1 20071008 A 5340 A5387006820000 FITTING AIRBUS 310 A310222 3930315 EU UPPER CARGO CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 CABIN FRAME 44 TIE CLIP TO LT EMERGENCY DOOR CUT OUT FRAME AT FLOOR LEVEL IS CORRODED. REMOVED CORRODED TIE CLIP IAW FE DEX A310-200 SRM 51-40-21 PARA 7, RECEIVED, LOCATED, AND DRILLED NEW FITTING PO NR 589661.1 IAW FEDEX A31-200 SRM 51-40- 30. INSTALLED NEW FITTING IAW FEDEX A310-200 SRM 51-40-21 PARA 7. 2 L 7 2 4F RT A35EU 2007101600150 20071016 00150 EU 2007 10 16 MALA070124 1 20071007 A 3610 CLAMP SAAB SF340 340B 7860101 EU LT BLEED SYS LOOSE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 453XJ 340B453 SHORTLY AFTER TAKEOFF RECEIVED AN AIR COND CAUTION AND LEFT BLEED AIR LEAK. COMPLETED ARH AND LEFT BLEED AIR LEAK WENT OUT. RETURNED TO MSP INSPECTED LT RUBBER DUCT CONNECTIONS, FOUND UPPER CLAMP OFF. REPOSITIONED CLAMP, RAN ENGINE OPS A ND LEAK CHECKS GOOD IAW AMM 36-11-35-04. 2 L 7 2 4T RT A52EU 2007101600152 20071016 00152 NM 2007 10 16 HALA0700437 1 20070917 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 LEVEL 1 CORROSION ON SEAT TRACK 46 LBL 11-00 AT STATION 1197. AREA REWORKED AND FOUND WITHIN LIMITS PER SRM 53-00-52. REWORKED AREA WAS ALODINED AND PAINTED. 2 L 7 2 4F RT A1NM 2007101600154 20071016 00154 NM 2007 10 16 HALA0700439 1 20070917 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 1319 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 LEVEL 1 CORROSION ON SEAT TRACK 46 LBL 11-00 AT STATION 1319. AREA REWORKED AND FOUND TO BE WITHIN LIMITS PER SRM 53-00 -52. AREA ALODINED AND PAINTED. 2 L 7 2 4F RT A1NM 2007101600158 20071016 00158 NM 2007 10 16 HALA0700433 1 20070917 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 LEVEL 1 CORROSION ON SEAT TRACK SECTION 46 LBL 11-00 AT STATION 1197. AREAS REWORKED AND FOUND WITHIN LIMITS, PER SRM 5 3-00-52. REWORKED AREA ALODINED AND PAINTED. 2 L 7 2 4F RT A1NM 2007101600159 20071016 00159 NM 2007 10 16 HALA0700435 1 20070917 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 1140 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 LEVEL 1 CORROSION ON SEAT TRACK 46 LBL 11-00 AT STATION 1140. AREA REWORKED AND FOUND WITHIN LIMITS PER SRM 53-00-52. REWORKED AREA ALODINED AND PAINTED. 2 L 7 2 4F RT A1NM 2007101600160 20071016 00160 NM 2007 10 16 UIEA200700433 1 20071008 A 5753 65B3901169 WEDGE BOEING 747 74747UF 1384812 NM TE FLAP DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 492 29253 LT INBD TRAILING EDGE FOREFLAP DAMAGED. THE DAMAGE IS 10 FOOT LONG PIECE MISSING FROM THE T/E WEDGE. THE PIECE MISSING VARIES FROM 0.5" WIDE AT O/B END, AND IS 1.0" WIDE AT I/B END (LAST 4") AND IS 9 FEET I/B FROM I/B EDGE. IT IS BELIEVE D THIS DAMAGE HAS BEEN CAUSED BY MID FLAP ATTACH SPINDLE ACCESS PANEL, ON MID FLAP UPPER SURFACE, SCREW COMING ADRIFT AN D CONTACTING WITH THE FOREFLAP T/E WEDGE. 2 L 7 4 4F RT A20WE 2007101600162 20071016 00162 EA 2007 10 16 A6WA200740522 1 20070920 A 5320 S6144A14 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 468AW 7916 FOUND LEFT 484 ANGLE IS CRACKED AT LBL 27 APPROX .25 INCH LONG. 10-15-07 MAINTENANCE REMOVED CRACKED ANGLE AT FS 484 LBL 27. FABRICATED REPAIR ANGLE FROM PREFORMED ANGLE LOCATED DRILLED AND INSTALLED IAW BSC STANDARD REPAIR 601R-53-002 9B. (M) 2 L 7 2 4F RT A21EA 2007101600163 20071016 00163 EA 2007 10 16 ATWA200740511 1 20070915 A 5330 PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 425AW 7663 FOUND RIGHT KIDNEY PANEL CUTOUT AT FORWARD FUSELAGE HAS ONE ELONGATED HOLE. (M) 2 L 7 2 4F RT A21EA 2007101600164 20071016 00164 EA 2007 10 16 A6WA200740512 1 20070917 A 5320 6013501251 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 468AW 7916 FOUND RIGHT FS 621 TO FS 625.30 INTERCOSTAL AT STRINGER 14R IS CRACKED NEAR RADIUS APPROX 1 INCH LONG. 10-25-07 MA INTENANCE REPLACED RT INTERCOSTAL AT FS 621 TO 625.30 AT STRINGER 14R IAW CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007101600165 20071016 00165 EA 2007 10 16 A6WA200740513 1 20070917 A 5320 6013501251 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 468AW 7916 FOUND LEFT FS 621 TO 625.30 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. 10-25-07 MAINTE NANCE REMOVED AND REPLACED LT SIDE INTERCOSTAL LOCATED AT FS 621 TO 625.30 STRINGER 14 P/N 601-35012-51 IAW CRJ200 SRM 5 1-42-06. (M) 2 L 7 2 4F RT A21EA 2007101600166 20071016 00166 NM 2007 10 16 QXEA200701522 1 20071007 A 3230 LANDING GEAR BOMBDR DHC8 DHC8402 1390042 NM LEFT MALFUNCTIONED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 412QX 4059 ON FLIGHT 2429, AFTER TAKEOFF LEFT MAIN GEAR DOOR AMBER LIGHT STAYED ILLUMINATED. FLIGHT ATTENDANT CONFIRMED GEAR DOORS OPEN. PERFORMED EMERGENCY CHECKLIST, LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED GVI OF LEFT MAIN LANDING GEAR DOO RS. NO DEFECTS NOTED. INTERROGATED PSU FAULT HISTORY ONLY FOUND "LGDRCL FAULT UNREASONABLE FAR". COMPLIED WITH OPERAT IONAL TEST OF LANDING GEAR PRIMARY EXTENSION AND RETRACTION SYSTEM NUMEROUS TIMES, NO DEFECTS NOTED. GEAR DOOR INDICATI ONS NORMAL. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007101600168 20071016 00168 NM 2007 10 16 QXEA200701523 1 20071005 A 3260 46503107 UPLOCK TARGET BOMBDR DHC8 DHC8402 1390042 NM RT MLG MISSING A QXEA O OTHER P NO WARNING INDICATION CL CLIMB 1 NM 09 417QX 4086 SEA - ON FLIGHT 2250, RIGHT MAIN GEAR DOOR FAILED AFTER TAKEOFF, LIMITED SPEED 185 KIAS ALT GEAR EXTENSION USED. MAINTE NANCE CHECKED PSEU AND FOUND FAULTS RGUPLK FAULT UNREASONABLE FAR AND RG-DRCL FAULT UNREASONABLE FAR. INSPECTED RIGHT GE AR UPLOCK ASSY AND FOUND TARGET FOR PROX SENSOR MISSING. INSTALLED NEW TARGET, CLEARED FAULTS FROM PSEU. LANDING GEAR EXTENSION RETRACTION SYSTEM OPERATIONAL TEST GOOD. ALL INDICATIONS NORMAL. NO PSEU FAULTS RETURNED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007101600171 20071016 00171 2007 10 16 QXEA200701521 4 20071007 A 2310 C12432AA05 PROCESSOR BOMBDR DHC8 DHC8402 1390042 NM INOPERATIVE A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 411QX 11472 11472 4055 ON FLIGHT 2414, JUST AFTER TAKEOFF, NR 1 ARCDU HAD A FAIL MESSAGE IN THE "INT" BOX. SYSTEM STAYED FAILED FOR ABOUT AN H OUR AND THE SYSTEM STARTED WORKING AGAIN. TURNING ARCDU OFF AND ON PER CHECKLIST HAD NO EFFECT AT TIME OF FAILURE. MAI NTENANCE INTERROGATED CDS AND FOUND IOP 1 FAULT. REMOVED AND REPLACED IOP 1. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNE D TO SERVICE. 2 H 7 2 4T RT A13NM 2007101600176 20071016 00176 WP 2007 10 16 07FDEA01449 1 20070411 A 5730 DOUBLER DOUG MD10 MD1010F 3022112 WP CENTER WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 397FE 46631 FOUND DOUBLER ON CENTER WING STA 1216 TO STA 1257 RT SIDE B/T XCW 47 TO XCW 81. DOUBLER INSTALLED PER P TO F MOD, EF DW G S110570002 AND VSP0022 SEE FAA FORM 337, DATED 26 JUNE 1998, SEE ENGINEERING RECOMMENDED ACTION. 2 L 7 3 4F RT A22WE 2007101600177 20071016 00177 EU 2007 10 16 07FDEA04519 1 20071006 A 5313 STRINGER AIRBUS 300 A300F4605R 3930327 EU BS 4377 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 670FE 777 STRINGER 49R IS DAMAGED STA 4377 REMOVED DAMAGED STRINGER SECTION, FABRICATED REPAIR COUPLING IAW SRM 53-10-14 FIG 201. TREATED, PRIMED AND TRIMMED STRINGER IAW SRM 51-21-10. SEALED AND INSTALLED REPAIR COUPLING IAW 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007101600178 20071016 00178 EU 2007 10 16 07FDEA04520 1 20071006 A 5347 A5327400584T7 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 670FE 777 MAIN CARGO DECK SEAT TRACK FROM FR 76 TO FR 74 LBL42 HAS 2 AREAS WITH CORROSION REMOVED DAMAGED SEAT TRACK. FABRICATED REPLACEMENT FROM PART NR A5324005/84 T7 AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-21 AND 51-10-16. 2 L 7 2 4F RT A35EU 2007101600179 20071016 00179 EU 2007 10 16 07FDEA04521 1 20071006 A 5347 R53070088206 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 670FE 777 MAIN CARGO DECK SEAT TRACK FROM FR 78 TO FR 73 RBL25 HAS 7 AREAS WITH CORROSION REMOVED AND REPLACED DAMAGED SEAT TRACK IAW 51-40-21. 2 L 7 2 4F RT A35EU 2007101600180 20071016 00180 EU 2007 10 16 07FDEA04534 1 20071009 A 5720 A57246670 PLATE AIRBUS 300 A300B4622R 3930312 EU LT WING DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 DELAMINATION ON LT WING OUTER SHROUD BOX FLAP DEFLECTOR PLATE, AROUND THE ROLLER SUPPORT. REPAIR PERFORMED BY REMOVING DAMAGED PLIES AND INSTALLING REPAIR PLIES USING PRINCIPLES OF SRM 51-77-12/PARA.2A(3), ALL IAW EA 6-5755-106530 AND RAS/ BAE/1005093/2007 ISSUE A. 2 L 7 2 4F RT A35EU 2007101600184 20071016 00184 EU 2007 10 16 2007UALA04078 1 20071004 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 490UA 1728 CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. CREW COMMENTS: SHOWS 650 PSI. 10-19-07 SERVICED CREW O2. CHECKED ALL FLT DECK MASKS FOR OPERATION AND LEAKS, OPERATION CKD NORMAL AND NO LEAKS NOTED. NO REPEATS SINCE ORI GINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101600185 20071016 00185 NM 2007 10 16 2007UALA04079 1 20071004 A 3350 BATTERY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 677UA 30029 EEL LIGHTS AT SEAT 17HJ-23HJ AND EMERGENCY EXIT DOOR LIGHTS AT 17HJ AND 18HJ INOP. REPLACED EEL BATTERY, GROUND CHECK N ORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101600186 20071016 00186 NM 2007 10 16 2007UALA04080 1 20071004 A 3231 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NLG DOOR UNKNOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 505UA 24626 NOSE GEAR DOOR IS OPEN AND UNABLE TO CLOSE WITH HYDRAULICS PRESSURIZED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101600187 20071016 00187 NM 2007 10 16 2007UALA04082 1 20071005 A 2612 6937307149 MODULE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FIRE DETECTION FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 FAULT LIGHT ON FIRE TEST NORMAL TEST WITH NR 2 ENG OVHT DET SWITCH PLACED IN "A" POSITION. SUSPECT FIRE DETECTION MOD ULE FAULTY. REPLACED FIRE DETECTION MODULE OPS CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600192 20071016 00192 NM 2007 10 16 2007UALA04087 1 20071005 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 44ABC UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 FOUND EMERGENCY LIGHT AT ROW 44ABC. RESECURED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007101600193 20071016 00193 EU 2007 10 16 2007UALA04088 1 20071005 A 2933 INDICATION SYS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYD QTY MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 425UA 508 YELLOW SYSTEM OVERHEAT AND YELLOW RESERVOIR LOW LEVEL ECAM DISPLAYED. 10-19-07 ACCOMPLISHED TEMP TEST WITH EXTERNAL THERMOMETER, NO OVERHEAT DETECTED. DRAINED EXCESS FLUID. DETERMINED PROBLEM TO BE INDICATION ONLY. REPLACED LOW LEVEL S WITCH. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101600195 20071016 00195 NM 2007 10 16 2007UALA04090 1 20071006 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN SMOKE A UALA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 508UA 24744 717939 SMOKE IN CABIN ON TAKEOFF ROLL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101600198 20071016 00198 2007 10 16 2007UALA04093 4 20071006 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 FOUND DOOR 4R SLIDE PRESSURE IS LOW. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101600200 20071016 00200 NM 2007 10 16 2007UALA04095 1 20071007 A 2420 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE APU GENERATOR ILLUMINATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 651UA 25389 APU GENERATOR "OFF" LIGHT ILLUMINATES AFTER RIGHT ENGINE STARTS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101600201 20071016 00201 NM 2007 10 16 2007UALA04096 1 20071006 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE ROW 18 AISLE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 811UA 847 FOUND ROW 18 AISLE EMERGENCY LIGHT INOPERATIVE. 10-19-07 FOUND LAMP ASSY FAULTED. REPLACED LAMP ASSY - OPS CHECK OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101600202 20071016 00202 EU 2007 10 16 2007UALA04097 1 20071008 A 3350 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 408UA 457 FOUND CABIN EMERGENCY LIGHTS DID NOT TEST. 10-19-07 FOUND EPSU FAULTED. REPLACED EPSU ASSY - OPS CHECK OK --NO RE PEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101600203 20071016 00203 EU 2007 10 16 2007UALA04098 1 20071007 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 426UA 510 FOUND EEL LIGHT OUT AT SEAT 6C. 10-19-07 FOUND WIRING DAMAGED AT SEAT 6C. REPAIRED EEL LIGHT WIRING AT SEAT 6C. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101700001 20071017 00001 EU 2007 10 17 2007UALA04099 1 20071006 A 3350 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 445UA 826 EMERGENCY LIGHTS WILL NOT CHECK. FOUND BATTERY FAULTY. 10-19-07 FOUND EPSU FAULTED. REPLACED EPSU-NO REPEATS SINC E ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101700004 20071017 00004 NM 2007 10 17 2007UALA04102 1 20071007 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE BS 452 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 933UA 26659 CABIN CREASE BEAM CUT TO FACILITATE FRAME REPLACEMENT AT BS 452. MAJOR REPAIR: FABRICATED AND INSTALLED REPAIR SPLICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101700005 20071017 00005 NM 2007 10 17 2007UALA04103 1 20071007 A 3350 LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE SEAT 20C FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 904UA 25004 FOUND EMERGENCY ESCAPE LIGHTING STRIP SEAT 20C STICKING OUT FROM CLEAR PLASTIC HOUSING. REPLACED LIGHT IN HOUSING. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101500190 20071015 00190 NM 2007 10 15 SWAA074980 1 20071003 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 274WN 32529 R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007101500215 20071015 00215 NM 2007 10 15 2007UALA04005 1 20070929 A 3397 WIRE HARNESS BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 669UA 30025 FOUND EMERGENCY LIGHT INOP AT SEAT 37H. REPLACED HARNESS FOR EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 37HJ. OPS CHECK NORM AL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101500217 20071015 00217 NM 2007 10 15 2007UALA04007 1 20070928 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SEAT 21H MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 677UA 30029 TECH REPORTS SEAT 21H MISSING EMERGENCY EXIT LIGHT. REPLACED MISSING LIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101500218 20071015 00218 NM 2007 10 15 2007UALA04008 1 20070930 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 222UA 30553 EEL AT FIRST CLASS SEAT 2E INOPERATIVE. RECONNECTED 2 L 7 2 4F 4 F RT T0001SE E46NE 2007101600020 20071016 00020 CE 2007 10 16 DXTA200702523 1 20071003 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE MALFUNCTIONED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 367QS 5600367 CO-PILOT'S BRAKES WENT TO THE FLOOR TWICE AT THE END OF LANDING ROLLOUT. 10-29-07 ACCESSED BRAKE RESERVOIR, ATTACH ED BRAKE BLEEDING KIT. BLED THE ANTI-ICE BRAKE SYSTEM SEVERAL TIMES, AND REMOVED ALL VISIBLE AIR FROM SYSTEM. OPERATED BRAKE PEDALS FROM PILOT & CO-PILOTS SIDE, BRAKES FEEL FIRM. REMOVED BLEED KIT AND CLOSED ACCESS SERVICED RESERVIOR AND LEAK CHECKED BRAKE FITTING, LEAK CHECK GOOD OPS CHECK GOOD. ALL WORK DONE IAW CH 32-42-00 OF THE 560 MM. 2 L 7 2 4F RT A22CE 2007101600024 20071016 00024 CE 2007 10 16 DJFA2007112 1 20071001 A 3897 CONNECTOR RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP LAV TANK BURNED E DJFA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 EA 23 733TA 9137 258337 CREW REPORTED SMELL OF SMOKE FROM THE LAV AND BAGGAGE FIRE ILLUMINTATED. AIRCRAFT LANDED SAFELY. MAINTENANCE DISCOVERE D A BURNED PIN IN THE LAV WATER TANK CONNECTOR BURNED. THE BURNED PIN WAS REPLACED. NO OTHER FAULTS WERE DETECTED. 2 L 7 2 4F 4 F RT A3EU E6WE 2007101600033 20071016 00033 CE 2007 10 16 AMWA0828013G 1 20071002 A 5311 12943003637 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FS 318.25 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 176YV 26646 UE176 REPAIRED FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT LT AND RT FS 318.25. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101600043 20071016 00043 NE 2007 10 16 BAQA200700036 2 20071004 A 7261 704A34410054 LINE AEROSP AS365 AS365N2 8680815 EU TMECA ARRIEL ARRIEL2C 60054 NE OIL VENT BURNED E BAQA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 EA 03 520CF 1641 6537 UPON SHUTDOWN, PILOT SMELLED SMOKE, SAW SMOKE COMING FROM NR1 ENGINE, OPENED COWLING SAW SMALL FIRE ON STARTER GENERATOR , RAN BACK TO COCKPIT ACQUIRED THE HANDHELD FIRE EXTINGUISHER, AND PUT FIRE OUT. DISCOVERED A BRAIDED OIL VENT LINE CAME IN CONTACT WITH THE TERMINAL ON THE STARTER GENERATOR, AND CAUGHT THE RUBBER PROTECTIVE BOOT OF THE STARTER GENERATOR O N FIRE. NO FURTHER DAMAGE. 1 G 7 2 3U 4 U RT H10EU E00054EN 2007101600045 20071016 00045 CE 2007 10 16 DELA200720009 1 20071005 A 2840 INDICATION SYS LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP LOW FUEL INTERMITTENT E DELA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 773DL 174 LOW FUEL LIGHT ILLUMINATED WITH 4000 LBS TOTAL FUEL ON AIRPLANE AND 1200 LBS FUEL IN THE WINGS. FUEL READER GAUGE INDICA TED 400 LBS OF FUEL ON RT WING. LATER ON WENT BACK TO INDICATE 1200 LBS ON THE WINGS. TAKEOFF (SIC) WITH 4000 LBS TOTAL LANDING WEIGHT WAS 13,800. MX ACTIONS: CLEANED FQ C/B CONTACTS, SUMPED FUEL TANKS (NO CONTAMINATION FOUND), PERFORMED GR OUND ENGINE RUN WHILE OBSERVING CKPT INDICATIONS. OPS NML. (MAX LANDING WEIGHT 14300). 2 L 7 2 4F 4 F A10CE E6WE 2007101600046 20071016 00046 NM 2007 10 16 ASMF200710001 1 20071004 A 5610 141A48104 WINDSHIELD BOEING 737 737705 13844SC NM CFMINT CFM567 CFM567B22 13802 NE COCKPIT CRACKED W ASMF O OTHER O OTHER CR CRUISE 1 SW 23 842AM 3398 509 32842 CAPTAIN REPORTED THAT DURING CRUISE, THE LIGHT OF THE OVERHEAT RT SIDE WINDOW NR 2 TURNED ON AND THE WINDOW CRACKED. MAI NTENANCE PERSONNEL REPLACED SUCH WINDOW AND ITS TEMPERATURE CONTROLLER IAW MM 56-12-11 AND MM 30-41-11, TESTED CORRECT I AW MM 30-41-00. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007101600054 20071016 00054 2007 10 16 WGEA200700012 4 20071005 A 2210 271032101003 CABLE ECLIPS EA500 ECLIPSEEA500 3350000 SW YAW DAMPER OUT OF RIG E WGEA C ABORTED TAKEOFF G F J MULTIPLE FAILURE FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 EA 27 134DJ 89 000035 ON T/O ROLL, APR ARMED, THE A/P INOP AND YAW DAMPER FAIL CAS CAME ON. ABORTED TAKEOFF. CREW PERFORMED PROCEDURES IN QRH AND A/P TEST, ALL APPEARED NORMAL. SECOND T/O SAME. CHECKED CABLE TENSIONS ON YAW, PITCH AND ROLL SERVO'S. FOUND ROLL SERVO TO BE OUT OF LIMITS. YAW AND PITCH CHECKED WITHIN LIMITS. RIGGED ROLL SERVO CABLE IAW EA500 MM 27-00-01. PERFORME D AUTO FLIGHT SYSTEM ADJUSTMENT TEST IAW EA500 MM 22-00-00. SYSTEM OP'S CHECK GOOD. 1 L 7 2 4J RT A00002AC 2007101600074 20071016 00074 SW 2007 10 16 WGEA200700010 1 20071004 A 3150 70000078102 DISPLAY ECLIPS EA500 ECLIPSEEA500 3350000 SW MALFUNCTIONED E WGEA O OTHER N FALSE WARNING AP APPROACH 1 EA 27 119DJ 119 000022 LT PFD BECAME PIXELATED ON FINAL APPROACH, COMPLETLEY UNUSEABLE, RT PFD DISPLAY WERE FINE. PROBLEM CLEARED UP FEW MINUTE S LATER. REMOVED AND REPLACED LT PFD IAW EA500 AMM 31-10-16. PERFORMED DISPLAY AND CONTROL PANEL ADJUSTMENT/TEST IAW A MM 31-10-00 AND TRANSPONDER SYSTEM ADJUSTMENT/TEST IAW AMM 34-50-60. ALL CHECKS GOOD. VERIFIED NR 1 AND NR 2 COMPLY WIT H FAR 91.413, AND FAR 43 APPENDIX F. PERFORMED ALTITUDE REPORTING CORRELATION TEST IAW PARA.(C) OF FAR PART 43 APPENDIX E, NO DATA CORRESPONDENCE ERRORS FOUND FOR TRANSPONDER NR 1 AND NR 2. 1 L 7 2 4J RT A00002AC 2007101600081 20071016 00081 NM 2007 10 16 2007UALA04019 1 20071001 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 FOUND EEL AT DR 3R AND L XAISLE INOP. SECURED CONNECTOR AT LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007101600082 20071016 00082 NM 2007 10 16 2007UALA04020 1 20071001 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 FOUND EEL 4J FWD INOPERATIVE. RELAMPED 2 L 7 4 4F 4 F RT A20WE E24NE 2007101600083 20071016 00083 EU 2007 10 16 2007UALA04021 1 20071002 A 3350 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 411UA 464 FOUND CABIN EMERGENCY LIGHTS CHECK FAILED BATTERY PACK FWD LT. 10-19-07 REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110700023 20071107 00023 WP 2007 11 7 IXXA070054O 1 20071026 A 3260 WARNING SYSTEM DOUG DC8 DC873F 302199F WP ZONE 700 MALFUNCTIONED A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 603AL 98499 356 46003 DURING CLIMB-OUT FROM KDFW TO KIAH, AFTER GEAR RETRACTION THE CREW NOTICED DOOR NOT LATCH LIGHT STAYED ON UNTIL THE CREW RECYCLED THE GEARS AND LIGHT WENT OUT. CREW LANDED AT KIAH WITHOUT INCIDENT. MAINTENANCE INSPECTED MAIN LANDING GEAR DOOR TARGET AND STRIKERS, CLEANED OPERATIONAL CHECK GOOD IAW DC8 MAINTENANCE MANUAL 32-60-0. AIRCRAFT WAS RETURNED TO S ERVICE. 2 L 7 4 4F RT 4A25 2007101600091 20071016 00091 NM 2007 10 16 2007UALA04031 1 20071001 A 3350 SWITCH BOEING 757 757222 1384956 NM EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 518UA 24871 FOUND EMERGENCY EXIT LIGHTS FAILS TEST. 10-26-07 REPLACED EMERGENCY LIGHTS CONTROL SWITCH. 2 L 7 2 4F RT A2NM 2007101600102 20071016 00102 NM 2007 10 16 2007UALA04043 1 20071003 A 5522 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT ELEVATOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 LEFT ELEVATOR TRAILING EDGE OUTBD CORNER HAS BURN DAMAGE. DAMAGE IS ON OUTBD TRAILING EDGE CORNER OF ELEVATOR SKIN, NOT ON ELEVATOR TIP ASSY. ROUTED ELEVATOR TO SHOP. REMOVAL, REPAIR AND RE-INSTALL ESTIMATE 5 SHIFTS. REPAIRS COMPLETED. IN STALLED LT ELEVATOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600103 20071016 00103 NM 2007 10 16 2007UALA04044 1 20071003 A 3397 WIRE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 314UA 23675 FOUND CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED BROKEN WIRES NEAR LAST ROW AND REMOVED WATER RESIDUE. OPS NORM AL. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600114 20071016 00114 NM 2007 10 16 2007UALA04055 1 20071003 A 5210 410045091 RESERVOIR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE R4 DOOR ASSIST FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 779UA 26941 FOUND DOOR 4R POWER ASSIST RESERVOIR SQUIB FAILS TEST. REPLACED DOOR ASSIST RESERVOIR. BITE TEST OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007101600118 20071016 00118 NM 2007 10 16 2007UALA04059 1 20071003 A 2820 PUMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUEL SYS FAULTED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 654UA 25392 FOUND FLICKERING FAULT AND L FUEL JET PUMP EICAS MSG. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101600119 20071016 00119 EU 2007 10 16 2007UALA04060 1 20071003 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 412UA 465 FOUND EMERGENCY LIGHTING FAILS 3CK TESTS. 10-19-07 RESET EPSU AND SYSTEM CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101600120 20071016 00120 NM 2007 10 16 2007UALA04061 1 20071003 A 5610 WINDOW BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT DELAMINATED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 536UA 25156 WINDOW EICAS MSG DISPLAYED POSITION 2. CAPT'S SLIDING WINDOW (L2) DELAMINATING BOTTOM CENTER OF WINDOW. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101600124 20071016 00124 NM 2007 10 16 2007UALA04065 1 20071004 A 5320 507946 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 295 S8L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 51211 24638 FWD CABIN STRINGER S-8L AT BS 295 INTERCOSTAL CRACKED AT FWD I-B CORNER. FABRICATED AND INSTALLED REPLACEMENT INTERCOST AL AND BRACKET REPAIR. ACP REPEAT INSPECTIONS PER SB- 737-53-1204. EC 955313099SD & AMM 53-13-99 CREATED TO INSPECT REPA IR EVERY 6000 CYCLES. IT IS MONITORED BY EQ 1855. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600125 20071016 00125 NM 2007 10 16 2007UALA04066 1 20071004 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 295 S7L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 FWD CABIN STRINGER S-7L AT BS 295 INTERCOSTAL CRACKED AT FWD I-B CORNER. FABRICATED NEW INTERCOSTAL AND ASSOCIATED STR AP-FILLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600126 20071016 00126 NM 2007 10 16 2007UALA04067 1 20071004 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 295 S11 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 FWD CABIN STRINGER S11 BS 295 INTERCOSTAL CRACKED AT FWD I-B CORNER. MAJOR REPAIR: FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL AND ASSOCIATED ANGLES AND BRACKETS. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600127 20071016 00127 NM 2007 10 16 2007UALA04068 1 20071004 A 5320 CHANNEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 359 S16L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 STR 16L SPLICE CHANNEL IS CRACKED BS 359 UPPER FLANGE. MAJOR REPAIR: FABRICATED AND INSTALLED REPLACEMENT SPLICE CHANNE L. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600130 20071016 00130 NM 2007 10 16 2007UALA04071 1 20071004 A 3510 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FIRST OFFICER'S FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 FIRST OFFICER'S O2 MASK RUNS CONTINUOUSLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101600135 20071016 00135 NM 2007 10 16 2007UALA04076 1 20071004 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1360 S26R DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 FOUND AFT PIT STA 1360 STR 26R MAIN FRAME HAS DENT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101600139 20071016 00139 NM 2007 10 16 07FDEA04523 1 20070930 A 5311 53FX1350 FRAME BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 283FE 22350 FWD LOWER CARGO STUB FRAME AT STA 580 BETWEEN STR 21L AND 22L HAS A CRACK. REMOVED 53FX1350 STUB FRAME, FABRICATED AND INSTALLED NEW STUB FRAME IAW 727 SRM 51-10-01 AND DWG 53FX1370. 2 L 7 3 4F RT A3WE 2007101600172 20071016 00172 NM 2007 10 16 QXEA200701527 1 20071007 A 3297 697071272 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM PROX SENSOR DAMAGED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 407QX 4049 LAX - ON FLIGHT 2424 RETURNED TO GATE. ON PUSHBACK, NOSE DOORS OPENED AND CLOSED 2 OR 3 TIMES THEN OPENED WITH NO GREEN LIGHT, NO DOOR CAUTION AND NO RED NOSE LIGHT AND HANDLE LIGHTS ON. MAINTENANCE REMOVED AND REPLACED NLG K1 PROX SENSOR HARNESS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007101600174 20071016 00174 EA 2007 10 16 QXEA200701529 1 20071009 A 3020 VENT CNDAIR CL600 CL6002C10 1390015 EA LT NACELLE CONTAMINATED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 613QX 10045 SFO - ON FLIGHT 2525, RECEIVED L COWL A/I DUCT WARNING MESSAGE. CREW COMPLIED WITH CHECKLIST AND SHUT OFF LT COWL. WAR NING MSG EXTINGUISHED. AIRCRAFT WAS RETURNED TO FIELD. MAINTENANCE INTERROGATED MDC AND FOUND NO CURRENT FAULTS. COMP LIED WITH FIM TASK 10-21-00-810-A01. NO LEAKS NOTED. CLEANED CONTAMINATION FROM VENT HOLES. COMPLIED WITH FAULT CONFI RMATION FOR FIM TASK 30-21-00-810-802-A01. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007101600189 20071016 00189 NM 2007 10 16 2007UALA04084 1 20071004 A 3350 POWER SUPPLY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 777UA 26916 FOUND AFT CABIN ALL SEAT EEL INOP. REPLACED POWER SUPPLY 2 L 7 2 4F 4 F RT T0001SE E46NE 2007101600190 20071016 00190 NM 2007 10 16 2007UALA04085 1 20071005 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 FOUND EMERGENCY LIGHT ROW 35 ABC INOP. RELAMPED 2 L 7 4 4F 4 F RT A20WE E24NE 2007101600197 20071016 00197 EU 2007 10 16 2007UALA04092 1 20071007 A 2700 SERVO AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FAULTED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 415UA 475 ELEV SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. F-CTL CREW COMMENTS: ELEV SERVO FAULTED. 10-19-07 REPLACED ELAC 1. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101700008 20071017 00008 NM 2007 10 17 2007UALA04106 1 20071006 A 3350 20131A BATTERY PACK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 307UA 23668 FOUND EEL LIGHTS INOP FWD OVHD PANEL. REPLACED BATTERY ASSY. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101700009 20071017 00009 2007 10 17 2007UALA04107 4 20071005 A 2565 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE 4R DOOR OUT OF POSITION A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 521UA 24891 FOUND DOOR 4R GIRT BAR ENGAGEMENT ARM LIGHT IS INOP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101700010 20071017 00010 NM 2007 10 17 2007UALA04108 1 20071007 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 521UA 24891 NR 1 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT OPS CHK GOOD, 2 L 7 2 4F 4 F RT A2NM E17NE 2007101700012 20071017 00012 NM 2007 10 17 2007UALA04110 1 20071006 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 218-228 S16L CANNING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 FOUND EXTERNAL FUSELAGE AT STA 218 TO 228 STRINGER 16L IS OIL CANNING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101700013 20071017 00013 NM 2007 10 17 2007UALA04111 1 20071006 A 3397 WIRE HARNESS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 531UA 25042 FOUND FLOOR EEL LIGHTS OUT FROM 31A TO AFT LAV. FOUND WIRE HARNESS BROKEN. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101700014 20071017 00014 NM 2007 10 17 2007UALA04112 1 20071005 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE STRIP AT ROW 13 UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 596UA 28749 STRIP OF EMERGENCY LIGHTS BUNCHED UP AT ROW 13. 10-30-07 RE-SECURED LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101700016 20071017 00016 NM 2007 10 17 2007UALA04114 1 20071006 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INTERMITTENT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 653UA 25391 EMERGENCY LIGHTS ON RIGHT AISLE ROWS 15-18 COMING ON AND OFF. LEAVING EMERGENCY LIGHT SWITCH OFF FOR A TIME NO HELP. C HECKED ALL CONNECTIONS AND TESTED SYSTEM. ALL OPERATIONAL. NO DEFECTS FOUND. COULD NOT REPRODUCE PROBLEM. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101700017 20071017 00017 NM 2007 10 17 2007UALA04115 1 20071007 A 4900 SWITCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE APU FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 APU AUTOSHUTDOWN 5 TIMES WITHIN 10 SECONDS AFTER STABILIZING AT 95PC RPM. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101700020 20071017 00020 NM 2007 10 17 2007UALA04118 1 20071008 A 5754 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 14 SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 794UA 26953 NR 14 LEADING EDGE SLAT DELAMINATED OTBD END. REMOVED THE SLAT, BONDING REPAIRED, AND INSTALLED THE SLAT, PERFORMED A DJUSTMENT. PERFORMED SLAT SYS PRIMARY CONTROL TEST.TEST OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007101700021 20071017 00021 NM 2007 10 17 2007UALA04119 1 20071006 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 673UA 29241 FOUND DOOR 1R EMERGENCY LIGHT INOP. RELAMPED 2 L 7 2 4F 4 F RT A1NM E24NE 2007101700022 20071017 00022 NM 2007 10 17 2007UALA04120 1 20071006 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SEATS 14HJ, 22HJ INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 673UA 29241 FOUND IN SEAT EEL LIGHTS ARE INOP AT SEATS 22HJ, 14HJ, AND 28AB. REPLACED EEL LIGHT BARS ON SEATS 22HJ, AND 28AB. OPS C HECKS NORMAL 2 L 7 2 4F 4 F RT A1NM E24NE 2007101700027 20071017 00027 NM 2007 10 17 2007UALA04125 1 20071008 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 FOUND EMERGENCY LIGHT INOP 3A AFT AND 5E AFT. REPLACED LIGHT ASSEMBLY 2 L 7 4 4F 4 F RT A20WE E24NE 2007101700032 20071017 00032 NM 2007 10 17 AALA20071877 1 20071006 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 909AN 29511 MIA - EMERGENCY LIGHT AT LEFT OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT OVERWING EXI T. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007101700033 20071017 00033 NM 2007 10 17 AALA20071880 1 20071006 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 966AN 30094 DFW - EMERGENCY LIGHT AT SEAT ROW 22DEF INOPERATIVE. SECURED PIN UNDER J BOX FOR EMERGENCY LIGHT AT LEFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007101700034 20071017 00034 WP 2007 10 17 AALA20071881 1 20071007 A 2613 SWITCH DOUG DC9 DC983 3022083 WP TURBINE TEMP INOPERATIVE A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 9620D 53591 STL INFLIGHT T4XG/07OCT - TAIL COMPARTMENT TEMPERATURE LIGHT ILLUMINATED. SHUT OFF LEFT AIR CONDITIONING PACK AND LIGHT WENT OUT AFTER TWO MINUTES. RETURNED TO STL AND LANDED WITHOUT INCIDENT. REPLACED TURBINE INLET TEMPERATURE SWITCH AN D COMPRESSOR DISCHARGE SWITCH AND LEFT AIR CYCLE MACHINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007101700038 20071017 00038 WP 2007 10 17 AALA20071885 1 20071007 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN DETACHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 962TW 53612 DFW - FOUND SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 11DEF DETACHED. SECURED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 11DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007101700039 20071017 00039 NM 2007 10 17 AALA20071886 1 20071007 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 640A 24598 DFW - EMERGENCY LIGHT AT LEFT AFT OVERWING EXIT INOPERATIVE. REPLACED LAMP AND REMOVED LIGHT CORROSION FOR EMERGENCY LI GHT AT LEFT AFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007101700041 20071017 00041 WP 2007 10 17 AALA20071879 1 20071006 A 2560 STRAP DOUG DC9 DC982 3022082 WP F/A SEAT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 458AA 49563 LGA - EMERGENCY FLASHLIGHT AT AFT FLIGHT ATTENDANT SEAT MISSING RETAINING STRAP. REPLACED RETAINING STRAP FOR EMERGENCY FLASHLIGHT AT AFT FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007101700043 20071017 00043 EA 2007 10 17 SWIA200718744 1 20070804 A 7120 BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 472CA 7667 FOUND AT C-CHECK, CRACK IN RADIUS OF ENGINE BEAM AT FS 640. COMPLIED WITH SB 601R-53-065. 2 L 7 2 4F RT A21EA 2007101700044 20071017 00044 EA 2007 10 17 SWIA200718745 1 20070804 A 5310 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA BS 640 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 472CA 7667 FOUND AT C-CHECK, DOUBLER CRACKED AT FS 640 ON LEFT SIDE OF SUPPORT BEAM. COMPLIED WITH SB 601R-53-065. 2 L 7 2 4F RT A21EA 2007101700045 20071017 00045 EA 2007 10 17 SWIA200718747 1 20070804 A 7120 SPHERICAL BEARIN CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 472CA 7667 FOUND AT C-CHECK, RIGHT ENGINE FORWARD MOUNT LINK HAS CORROSION ON SPHERICAL BEARING. UPPER FLOATING BUSHING IS CORRODE D. REPLACED ENGINE FORWARD MOUNT LINK AND UPPER FLOATING BUSHING IAW CRJ MM 71-21-01-400-801. 2 L 7 2 4F RT A21EA 2007101700046 20071017 00046 EA 2007 10 17 SWIA200718748 1 20070807 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 732SK 10194 FOUND AT C-CHECK, FLOOR SUPPORT ON FORWARD SIDE OF FS 280 BEAM IS CRACKED. REPLACED FLOOR SUPPORT AT FS 280 PER CRJ700/ 900 SRM 51-42-06 PAGE 7. 2 L 7 2 4F RT A21EA 2007101700047 20071017 00047 EA 2007 10 17 SWIA200718749 1 20070807 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 785-792 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 732SK 10194 FOUND AT C-CHECK, SEVERAL AREAS OF CORROSION ON LEFT SIDE SEAT RAIL AT FS 785. REPLACED SEAT RAIL AT FS785.15-792.00 AS PER CRJ700/900 SRM 51-42-13-001-001-A01. 2 L 7 2 4F RT A21EA 2007101700050 20071017 00050 EA 2007 10 17 SWIA200718752 1 20071007 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DENTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 466SW 7856 FLT 3782 - DENT ON FUSELAGE BETWEEN RIGHT TRU DOOR AND WINDSHIELD WIPER ARM. REPLACED DAMAGED INTERCOSTAL IAW CRJ SRM 5 1-42-06 AND REPAIRED DENT IN FUSELAGE IAW CRJ SRM 51-24-00. 2 L 7 2 4F RT A21EA 2007101700051 20071017 00051 SO 2007 10 17 SWIA200718753 1 20071004 A 3310 LIGHT EMB 120 EMB120ER 3260203 SO COCKPIT SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 216SW 120285 FIRST OFFICERS STORM LIGHT IS SMOKING. REPLACED STORM LIGHT ASSEMBLY WITH A SERVICEABLE UNIT. 2 L 7 2 4T RT A31SO 2007101700052 20071017 00052 EA 2007 10 17 SWIA200718754 1 20070925 A 5210 CABLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR ASSIST BINDING A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 412SW 7101 FLT 6729 - MAIN CABIN DOOR WOULD NOT OPEN ON ARRIVAL. FOUND DOOR ASSIST CABLE BINDING ON PULLEYS. REPLACED PULLEYS AND DOOR MOTOR ASSEMBLY IAW AMM 52-11-08. 2 L 7 2 4F RT A21EA 2007101700053 20071017 00053 EA 2007 10 17 SWIA200718755 1 20071006 A 2150 DUCT CNDAIR CL600 CL6002B19 1900309 EA LT A/C PACK LOOSE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 983SW 7961 FLT 6159 - RIGHT PACK OVERPRESSURIZES AFTER TRANSFER TO ENGINE BLEED. RETURNED TO LAX. SECURED DUCT ON LEFT PACK. OPE RATED BOTH PACKS WITH NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007101700054 20071017 00054 EA 2007 10 17 SWIA200718756 1 20071002 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DENTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 429SW 7518 BIRDSTRIKE INDUCED DENT JUST AFT OF LEFT TRU DOOR. REPLACED SKIN PANEL AND TWO DAMAGED INTERCOSTALS IAW CRJ SRM 51-23-0 0, 51-40-11, 51-42-06, 51-42-13, AND 51-42-21. 2 L 7 2 4F RT A21EA 2007101700057 20071017 00057 SO 2007 10 17 SWIA200718759 1 20071004 A 5210 SWITCH EMB 120 EMB120ER 3260203 SO PAX DOOR DIRTY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 582SW 120350 FLT 3681 - CABIN DOOR WOULD NOT OPEN FOR DEPLANEMENT. CLEANED THE DOOR "CLOSE" SWITCH. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007101700058 20071017 00058 SO 2007 10 17 SWIA200718760 1 20071006 A 3350 BULB EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 292SW 120319 FLT 5592 - THE ODOR OF SMOKE FILLED THE COCKPIT AND C/B A30 POPPED. REPLACED COURTESY LIGHT BULB. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007101700064 20071017 00064 NM 2007 10 17 UIEA200700375 1 20070912 A 5755 SKIN BOEING 747 747230B 1384889 NM NR 2 SPOILER DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 NR 2 SPOILER I/B EDGE DELAMINATION EVIDENCE. REPAIR CARRIED OUT IAW SRM 51-40-24. 2 L 7 4 4F A20WE 2007101700065 20071017 00065 NM 2007 10 17 UIEA200700376 1 20070912 A 5711 SPAR BOEING 747 747230B 1384889 NM ZONE 500 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 WS 317 - WS 1141, FRONT SPAR TO REAR SPAR CORROSION EVIDENCED. SURFACE CORROSION REMOVED AND REPROTECTED IAW SRM 51-10- 01 AND 51-10-02. 2 L 7 4 4F A20WE 2007101700068 20071017 00068 NM 2007 10 17 UIEA200700380 1 20070925 A 5730 SKIN BOEING 747 747230B 1384889 NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 LHW UPPER SURFACE WS 807 STR S16 CORROSION EVIDENT. SURF CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-0 2. 2 L 7 4 4F A20WE 2007101700069 20071017 00069 NM 2007 10 17 UIEA200700379 1 20070925 A 5347 SEAT TRACK BOEING 747 747230B 1384889 NM BS 1980 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 BS 1980 RBL 90 SEAT TRACK FOUND CORROSION. BLEND OUT CORROSION IAW SRM 51-10-01 AND REPROTECTED IAW 51-10-02. 2 L 7 4 4F A20WE 2007101700070 20071017 00070 NM 2007 10 17 UIEA200700378 1 20070925 A 5347 SEAT TRACK BOEING 747 747230B 1384889 NM ZONE 200 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 BS 1960 LBL 99 SEAT TRACK FOUND CORROSION. BLEND OUT CORROSION IAW SRM 51-10-01 AND REPROTECTED IAW 51-10-02. 2 L 7 4 4F A20WE 2007101700072 20071017 00072 NM 2007 10 17 UIEA200700386 1 20070924 A 5347 SEAT TRACK BOEING 747 74747UF 1384812 NM BS 1879-1880 BROKEN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 492MC 29253 LOWER AFT CARGO COMPARTMENT HAS SEAT TRACK BROKEN AT STA 1879 LBL 25. REPLACED SEAT TRACK IAW SRM 53-60-03 AND 53-00-52 REPAIRS 7 AND 10. 2 L 7 4 4F RT A20WE 2007101700073 20071017 00073 NM 2007 10 17 UIEA200700387 1 20070925 A 5753 SKIN BOEING 747 74747UF 1384812 NM RT WING TE FLAP DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 496MC 29257 RIGHT WING OUTBOARD FORE FLAP HAS DELAMINATION FROM WBL 804-WBL 817. REPAIRED RIGHT OUTBOARD FOREFLAP LEADING EDGE AT W BL 804 TO WBL 817 IAW SRM 51-70-07 AND ATLAS XEO 57-091507. 2 L 7 4 4F RT A20WE 2007101700075 20071017 00075 NM 2007 10 17 UIEA200700392 1 20070925 A 7830 COWL FASTENER BOEING 747 74747UF 1384812 NM THRUST REVERSER MIGRATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 496MC 29257 NR 1 ENGINE REVERSER RIGHT SIDE TRANSLATING COWL OUTER SKIN FORWARD SECTION SEVERAL RIVETS MIGRATED. REMOVED AND REPLAC ED LOOSE AND MIGRATED RIVETS IAW SRM 51-40-02. 2 L 7 4 4F RT A20WE 2007101700078 20071017 00078 NM 2007 10 17 UIEA200700371 1 20070925 A 5730 SKIN BOEING 747 747230B 1384889 NM RT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 SURFACE CORROSION EVIDENT AROUND HEAD FROM WS 724.50 TO WS 917.00 BETWEEN REAR SPAR AND MID SPAR. SURF, CORROSION REMOV ED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 2007101700081 20071017 00081 NM 2007 10 17 UIEA200700377 1 20070925 A 5347 SEAT TRACK BOEING 747 747230B 1384889 NM BS 520 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 U/D BS 520 RBL 46 SEAT TRACK CORROSION. REPAIR SEAT TRACK IAW SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2007101700083 20071017 00083 NM 2007 10 17 UIEA200700395 1 20070926 A 5730 SKIN BOEING 747 747230B 1384889 NM ZONE 600 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 RIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM WS 528 TO WS 724.5 BETWEEN MID SPAR AND FRONT SPAR. CORR OSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 2007101700084 20071017 00084 NM 2007 10 17 UIEA200700396 1 20070926 A 5730 SKIN BOEING 747 747230B 1384889 NM ZONE 600 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 RIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM SIDE OF BODY TO WS 528 BETWEEN MID SPAR AND FRONT SPAR. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 2007101700085 20071017 00085 NM 2007 10 17 UIEA200700397 1 20070926 A 5730 SKIN BOEING 747 747230B 1384889 NM ZONE 600 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 RIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM SIDE OF BODY TO WS 528 BETWEEN MID SPAR AND FRONT SPAR. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 2007101700086 20071017 00086 NM 2007 10 17 UIEA200700398 1 20070926 A 5730 SKIN BOEING 747 747230B 1384889 NM ZONE 600 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 RIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM WS 528 TO WS 724.5 BETWEEN MID SPAR AND REAR SPAR. CORRO SION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 2007101700087 20071017 00087 NM 2007 10 17 UIEA200700399 1 20070926 A 5730 SKIN BOEING 747 747230B 1384889 NM ZONE 600 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 RIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM WS 724.5 TO WS 917 BETWEEN MID SPAR AND REAR SPAR. CORRO SION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 2007101700088 20071017 00088 NM 2007 10 17 UIEA200700400 1 20070926 A 5730 SKIN BOEING 747 747230B 1384889 NM ZONE 600 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 RIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM WS 724.5 TO WS 917 BETWEEN MID SPAR AND FRONT SPAR. CORR OSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 2007101700089 20071017 00089 NM 2007 10 17 UIEA200700405 1 20070926 A 3230 BEARING BOEING 747 747230B 1384889 NM RETRACT CYLINDER CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 RIGHT BODY GEAR RETRACT ACTUATOR LOWER END BEARING CORRODED. REMOVED CORROSION AS PER TEC - XMN-07-01832 PROPOSAL REF O HM 32-33-11. 2 L 7 4 4F A20WE 2007101700090 20071017 00090 NM 2007 10 17 UIEA200700401 1 20070926 A 5711 SPAR BOEING 747 747230B 1384889 NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 LEFT WING UPPER SURFACE MID SPAR WS 1112, WS 1280, WS 1330 AND WS 1392 HAS MINOR SURFACE CORROSION EVIDENT. CORROSION R EMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 2007101700091 20071017 00091 NM 2007 10 17 UIEA200700402 1 20070926 A 5730 SKIN BOEING 747 747230B 1384889 NM ZONE 500 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 LEFT WING UPPER SURFACE WS 353 TO WS 586 REAR SPAR HAS MINOR SURFACE CORROSION EVIDENT. CORROSION REMOVED AND REPROTECT ED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 2007101700092 20071017 00092 NM 2007 10 17 UIEA200700403 1 20070926 A 5730 SKIN BOEING 747 747230B 1384889 NM ZONE 500 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 LEFT WING UPPER SURFACE WS 807 TO STR 516 SURFACE CORROSION EVIDENT. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 2007101700093 20071017 00093 NM 2007 10 17 UIEA200700404 1 20070926 A 5315 FLOORBEAM BOEING 747 747230B 1384889 NM BS 1720 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 MAIN DECK BS 1720 LBL 76- LBL 98 FLOORBEAM UPPER CHORD HAS LEVEL 2 CORROSION. REPAIRED PER SRM 53-10-07 FIG 2. RAM FOR M AND CPCP SUBMITTED TO ENGINEERING. 2 L 7 4 4F A20WE 2007101700094 20071017 00094 NM 2007 10 17 UIEA200700406 1 20070928 A 7830 FAIRING BOEING 747 747230B 1384889 NM THRUST REVERSER DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 NR 3 ENGINE LT T/R AFT UPPER FAIRING FOUND TORN AND MATERIAL MISSING. REPAIRED PER EO4778A109. 2 L 7 4 4F A20WE 2007101700096 20071017 00096 NM 2007 10 17 UIEA200700407 1 20070928 A 5330 SKIN BOEING 747 747230B 1384889 NM BS 1241 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 BS 1241 LBL 11- RBL 11 CTR SECTION UPPER SKIN CORROSION, LEVEL 1. BLENDED OUT IAW SRM 51-10-01 AND BOEING MESSAGE NUMBE R 1-598402422-7. 2 L 7 4 4F A20WE 2007101700098 20071017 00098 NM 2007 10 17 UIEA200700409 1 20070928 A 5330 SKIN BOEING 747 747230B 1384889 NM BS 1241 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 BS 1241 LBL 55- LBL 76 CTR SECTION UPPER SKIN CORROSION, LEVEL 1. BLENDED OUT IAW SRM 51-10-01 AND BOEING MESSAGE NUMBE R 1-598402422-7. 2 L 7 4 4F A20WE 2007101700099 20071017 00099 NM 2007 10 17 UIEA200700411 1 20070928 A 5711 SPAR BOEING 747 747230B 1384889 NM RT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 RIGHT WING AT WS 917- WS 1141 FRONT SPAR TO REAR SPAR HAS CORROSION EVIDENT. CORROSION REMOVED PER SRM 51-10-01. 2 L 7 4 4F A20WE 2007101700100 20071017 00100 NM 2007 10 17 UIEA200700412 1 20070928 A 5755 SKIN BOEING 747 747230B 1384889 NM NR 2 SPOILER DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 NR 2 SPOILER OUTBOARD EDGE DELAMINATED. REPAIR CARRIED OUT PER SRM 51-40-24. 2 L 7 4 4F A20WE 2007101700101 20071017 00101 NM 2007 10 17 UIEA200700413 1 20070928 A 5755 SKIN BOEING 747 747230B 1384889 NM NR 4 SPOILER DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 NR 4 SPOILER OUTBOARD CORNER DELAMINATED. REPAIR CARRIED OUT PER SRM 51-40-24. 2 L 7 4 4F A20WE 2007101700106 20071017 00106 NM 2007 10 17 UIEA200700419 1 20070929 A 5753 FAIRING BOEING 747 7472D7B 1384803 NM RT WING TE FLAP DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 RT WING NR 5 FLAP TRACK FORWARD FIXED FAIRING AT WBL 235.20, OUTBOARD SIDE HAS AN AREA 12.0 INCH LONG BY 2.0 INCH WIDE O F DELAMINATION AND CRACK. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 6, SHEETS 1 THRU 4 AND SRM 51- 40-12. ALSO, REFERENCE ATLAS AIR EO NR 4757A395. 2 L 7 4 4F RT A20WE 2007101700107 20071017 00107 NM 2007 10 17 UIEA200700418 1 20070929 A 5730 PANEL BOEING 747 7472D7B 1384803 NM ZONE 600 DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 LT WING UPPER L/E FIXED PANEL AT WS 490.00 HAS AN AREA OF 2.0 INCH LONG BY 2.0 INCH WIDE OF DELAMINATION. PERMANENT REP AIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18, SHEETS 1 THRU 5 AND SRM 51-40-12. ALSO, REFERENCE ATLAS AIR EO NR 4757A393. 2 L 7 4 4F RT A20WE 2007101700108 20071017 00108 NM 2007 10 17 UIEA200700420 1 20070929 A 5280 DOOR BOEING 747 7472D7B 1384803 NM ZONE 600 DEBONDED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 RT WING GEAR INBOARD STRUT DOOR AFT EDGE, CENTER AREA HAS A 10.0 INCH LONG BY 4.0 INCH WIDE OF MATERIAL SEPARATING AT BS 1343.3. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 12, SHEETS 1 THRU 4 AND SRM 51-40-12. ALSO, RE FERENCE ATLAS AIR EO NR 4752A125. 2 L 7 4 4F RT A20WE 2007101700109 20071017 00109 NM 2007 10 17 UIEA200700421 1 20070929 A 5411 FRAME BOEING 747 7472D7B 1384803 NM NR 3 NACLLE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 NR 3 ENGINE RT CORE COWL FORWARD FRAME HAS A HOLE AND CRACK. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-20-01 FIG 4 AND SRM 51-40-03 FIG 1. ALSO, REFERENCE ATLAS AIR XEO NR 71-092807. 2 L 7 4 4F RT A20WE 2007101700110 20071017 00110 NM 2007 10 17 UIEA200700423 1 20071001 A 5311 FRAME BOEING 747 7472D3B 1384805 NM BS 2638 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 AFT LOWER FUSELAGE AT FS 2638 FRAME LOWER SURFACE SCRAPED DUE TO TAIL DRAG. PERMANENT REPAIR ACCOMPLISHED AS PER B747-2 00 SRM 51-20-01 FIG 3, AND SRM 51-30-02. ALSO REFERENCE ATLAS AIR XEO NR 53-093007-1. 2 L 7 4 4F RT A20WE 2007101700111 20071017 00111 NM 2007 10 17 UIEA200700424 1 20071001 A 5311 FRAME BOEING 747 7472D3B 1384805 NM BS 2658 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 AFT LOWER FUSELAGE AT FS 2658 FRAME LOWER SURFACE SCRAPED DUE TO TAIL DRAG. PERMANENT REPAIR ACCOMPLISHED AS PER B747-2 00 SRM 53-10-04 FIG 75 SHEETS 1 THRU 15. REFERENCE ATLAS AIR XEO 53-093007. 2 L 7 4 4F RT A20WE 2007101700112 20071017 00112 NM 2007 10 17 UIEA200700426 1 20071001 A 5330 SKIN BOEING 747 7472D3B 1384805 NM BS 2594-2604 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 LOWER AFT FUSELAGE EXTERIOR SKIN DOUBLER/TRIPLER AT FS 2594 TO 2604.0 PREVIOUS REPAIR DAMAGED WITH HEAVY ABRASION/SCRAPI NG DUE TO TAIL DRAG. REMOVED AND REPLACED DOUBLER/TRIPLER REPAIR AS PER 747-200 SRM 51-30-02 AND 51-30-03 FIG 1 SHEETS 1 THRU 6. REFERENCE ATLAS XEO 53-092807. 2 L 7 4 4F RT A20WE 2007101700113 20071017 00113 NM 2007 10 17 UIEA200700422 1 20071001 A 5330 SKIN BOEING 747 7472D3B 1384805 NM BS 2742-2792 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 FUSELAGE TAIL CONE LOWER AREA FROM FS 2742 TO 2792 SKIN AND FRAMES SCRAPED AND DENTED DUE TO TAIL DRAG. REMOVE AND REPL ACED LOWER SECTION OF CONE FROM STA 2742 TO 2792, ASSY P/N 65B02785-1 AND PERMANENT REPAIRS ACCOMPLISHED AS PER B747-200 SRM 51-20-01 FIG 3, SRM 51-30-02 AND 51-10-02. ALSO REF: ATLAS AIR XEO NR 53-092907. 2 L 7 4 4F RT A20WE 2007101700115 20071017 00115 NM 2007 10 17 UIEA200700427 1 20071001 A 5522 SKIN BOEING 747 7472D3B 1384805 NM ZONE 100 TORN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 LT INBOARD ELEVATOR, TRAILING EDGE COMPOSITE SKIN TIP AREA HAD GROUND DAMAGE. PERMANENT REPAIR ACCOMPLISHED AS PER B747 SRM 51-40-09, FIG 1A, SHEET 1 AND FIG 8, SHEETS 1 AND 2. REFERENCE ATLAS AIR EO NR 4755A049. 2 L 7 4 4F RT A20WE 2007101700116 20071017 00116 NM 2007 10 17 UIEA200700428 1 20071002 A 5753 SKIN BOEING 747 74747UF 1384812 NM RT WING TE FLAP NICKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 499MC 29260 RIGHT INBOARD T/E FLAP AFT FLAP LOWER SURFACE HAS VARIOUS NICKS. INTERIM REPAIR CARRIED OUT IAW SRM 57-53-01, AND XEO 5 7-092607. 2 L 7 4 4F RT A20WE 2007101700117 20071017 00117 NM 2007 10 17 UIEA200700429 1 20071002 A 5753 SKIN BOEING 747 74747UF 1384812 NM LT WING TE FLAP NICKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 499MC 29260 LEFT WING T/E FLAP INBOARD AFT FLAP LOWER SURFACE HAS VARIOUS NICKS AND SCRATCHES. INTERIM REPAIR CARRIED OUT IAW SRM 5 7-53-01, AND XEO 57-092607. 2 L 7 4 4F RT A20WE 2007101700119 20071017 00119 NM 2007 10 17 UIEA200700430 1 20071002 A 7800 COWLING BOEING 747 74747UF 1384812 NM THRUST REVERSER CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 499MC 29260 NR 3 ENGINE RIGHT T/R TRANSLATING COWL LOWER FAIRING HAS A CRACK APPROX 3.0 INCHES AT THE FORWARD SECTION AND RIVETS PUL LING THROUGH AT THE AFT SECTION. RIVETS REPLACED IAW SRM 51-40-02. AN INTERIM REPAIR WAS DONE TO THE CRACKED FAIRING B Y STOP DRILLING AND INSTALLING AN EXTERNAL DOUBLER IAW XEO 78-092607. 2 L 7 4 4F RT A20WE 2007101700120 20071017 00120 NM 2007 10 17 UIEA200700435 1 20071009 A 7160 9366M14G29 INLET GUIDE VANE BOEING 747 74747UF 1384812 NM GE CF6 CF680C2* GL NR 2 ENGINE BENT A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 492 29253 704719 NR 2 ENG 3 IGV BENT<4DEG AT 1230 O/C POSITION. NR 2 ENG 3 LEVER ARMS REPLACED AT 1230 O/C POSITION IAW 72-36-00-408-005 -REV 60. 2 L 7 4 4F 4 F RT A20WE E23EA 2007101700123 20071017 00123 NM 2007 10 17 UIEA200700438 1 20071009 A 7160 9609M123P02 BEARING BOEING 747 74747UF 1384812 NM GE CF6 CF680C2* GL RT VSV WORN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 492 29253 704719 NR 2 ENG RT VSV ACTUATOR ROD END BEARING CONNECTION TO VSV LEVER ARM WORN AND ALSO SLIDE (GUIDE) BLOCK WORN. NR 2 ENG R T VSV ACTUATOR. REMOVED AND REPLACED IAW AMM SLIDER BLOCK. REPLACED IAW GE MM 72-32-10. 2 L 7 4 4F 4 F RT A20WE E23EA 2007101700124 20071017 00124 NM 2007 10 17 NWAA073376301 1 20070925 A 5311 FRAME BOEING 747 747451 1384940 NM BS 340 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 661US 23719 DURING "M" CHECK, FOUND CRACK COMMON TO THE BL 0 CROWN INTERCOSTAL AT BS 340. REPAIRED PER EA 63-210143 SECTION I, SECT ION II OF EA 63-210143 TO BE ACCOMPLISHED 12 MONTHS FROM SEPT 24, 2007. 2 L 7 4 4F RT A20WE 2007101700125 20071017 00125 NM 2007 10 17 NWAA073386301 1 20070926 A 5330 COLLAR BOEING 747 747451 1384940 NM FUSELAGE MISINSTALLED A NWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 01 661US 23719 DURING "M" CHECK WHILE ACCOMPLISHING FUSELAGE SKIN MODIFICATION AT BS 460 S13R AND S14R FOUND 5 LOCK FASTENER COLLARS TH AT WERE NOT SITTING FLUSH DUE TO FASTENER HOLES TOO CLOSE TO THE FRAME FLANGE. REPAIRED PER EA 63-210152. 2 L 7 4 4F RT A20WE 2007101700127 20071017 00127 NM 2007 10 17 DL757071281 1 20071001 A 2420 241080105 IDG BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 27 6711M 30483 716481 FLIGHT 418 DIVERTED TO LGA, APU ALREADY ON MEL PER 49-11-01, LOST LEFT GENERATOR. A/C LANDED AT LGA. MAINTENANCE IN PR OGRESS. REPLACED LEFT ENG IDG PER M/M. RAN ENG PER M/M. NO LEAKS NOTED. OPS NML. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101700129 20071017 00129 NM 2007 10 17 DL76G071295 1 20071003 A 5315 BAC1509100682 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 654 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 156DL 25354 FLOORBEAM STA654+110 LBL40"AREA CORRODED. REPLACED FLOORBEAM PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007101700130 20071017 00130 NM 2007 10 17 DL76G071296 1 20071004 A 5315 BAC150931233 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 1197 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 156DL 25354 FOUND STA 1197+44 LBL 5 AND LBL 18 CARGO FLOORBEAM TOP SURFACE CORRODED. BEAM REPLACED PER SRM 53-00-07. 2 L 7 2 4F RT A1NM 2007101700131 20071017 00131 NM 2007 10 17 DLM90071297 1 20071003 A 5320 PAN DOUG MD90 MD9030 3023690 NM CARGO DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 FWD CARGO DOOR FRAME PAN LWR VERT AND HORIZ LEGS CORRODED FS 370 TO 427. REPAIRED FWD CARGO DOOR FRAME PAN IAW MD88 SRM 53-05D FIG 44. 2 L 7 2 4F RT A6WE 2007101700132 20071017 00132 NM 2007 10 17 DLM90071298 1 20071001 A 5310 DOOR FRAME DOUG MD90 MD9030 3023690 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 MID PIT LOWER DOOR JAMB IS CORRODED. REPAIRED MID PIT LWR DOOR JAMB IAW MD80 SRM 53-05D FIG 63. 2 L 7 2 4F RT A6WE 2007101700133 20071017 00133 NM 2007 10 17 DLM90071299 1 20071002 A 5330 SKIN DOUG MD90 MD9030 3023690 NM FS 225 L30L DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 FWD CARGO COMPT FS 225 L30 DRAIN ATTACHMENT HOLES LARGER THAN ALLOWABLE LIMITS. REPAIRED DAMAGED AREA IN SKIN FS 225 L3 0 IAW MD80 SRM 53 04D FIG 12B. 2 L 7 2 4F RT A6WE 2007101700134 20071017 00134 NM 2007 10 17 DLM90071300 1 20071001 A 5315 FLOORBEAM DOUG MD90 MD9030 3023690 NM BS 1364 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 FLOORBEAM AT FS 1364 BETWEEN ENG PYLON SUPPORT BLKHDS HAS CORROSION. REPAIRED FLOORBEAM AT FS 1364 BETWEEN ENG PYLON SU PPORT BLKHDS IAW MD90 SRM 53 20 01 FIG 2 AND 51 70 01 FIG 2. 2 L 7 2 4F RT A6WE 2007101700137 20071017 00137 NM 2007 10 17 DL738071303 1 20071005 A 5330 143A32128 SKIN BOEING 737 737832 13844CF NM FS 390 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 394DA 30562 DURING PSV 8, MTC FOUND TWO DENTS LOCATED BETWEEN FS 380-400 AND L18 AND L19. THE FORWARD DAMAGE CUTOUT MEASURED 3" BY 3.2", AND THE AFT DAMAGE CUTOUT MEASURES 3.5" BY 3.2". THERE IS 4.5" BETWEEN EACH OF THE CUTOUTS. THE ER/A 464323-14 W ILL INSTALL A REPAIR DOUBLER IN ACCORDANCE WITH SRM 53-00-01 REPAIR 3. 2 L 7 2 4F RT A16WE 2007101700138 20071017 00138 NE 2007 10 17 DL76G071304 2 20071005 A 7200 CF680C2B6 ENGINE BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6 30025 NE NR 2 MAKING METAL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 154DL 59276 5912 25241 695376 WHILE PERFORMING OPN 4050 ON NR 2 ENGINE, FOUND FERROUS MATERIAL ON MAG CHIP DETECTOR MATERIAL SENT TO SHOP FOR EVALUATI ON. DUE TO LAB FINDINGS, RECOMMEND ENGINE CHANGE. REPLACED NR 2 ENGINE PER TRANS 1T161. 2 L 7 2 4F 4 F RT A1NM E13NE 2007101700142 20071017 00142 NM 2007 10 17 DL764071308 1 20071004 A 3244 TIRE BOEING 767 767432ER 1385134 NM MLG DAMAGED A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 827MH 29698 DURING CHECK, FOUND WHEEL NR 7 TIRE FOD DAMAGE TIRE TREAD CAME APART AND DAMAGE THE RT ENG FAN, RT TE FLP, NR 7 SPOILER , MLG ELECT CONDUIT. ALL ITEMS ON OTHER LOG ENTRIES. REPLACED NR 7 WHEEL ASSY. 2 L 7 2 4F RT A1NM 2007101700143 20071017 00143 NE 2007 10 17 DL777071313 2 20071005 A 7200 ENGINE BOEING 777 777232 1385232 NM RROYCE RB211 RB211TRENT89 NE NR 1 MALFUNCTIONED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 860DA 31095 29951 51194 NR 1 ENG CHANGE DUE TO STAGGER. REPLACED ENGINE ON TRANS 11T003. 2 L 7 2 4F 4 F RT T00001SE E00050EN 2007101700144 20071017 00144 NM 2007 10 17 DLM90071314 1 20071008 A 5330 5911432517 SKIN PANEL DOUG MD90 MD9030 3023690 NM BS 1476 S2R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 DURING HMV AT AAR/OKC, THE FUSELAGE SKIN PANEL WAS FOUND CRACKED AT STA 1476, S-2R. THE DAMAGE WAS REPAIRED PER ER/A 02 -464026-14AD. 2 L 7 2 4F RT A6WE 2007101700145 20071017 00145 NM 2007 10 17 DL76L071316 1 20071004 A 8011 7748860A4 STARTER BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE FAILED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 191DN 28448 724151 RIGHT ENGINE STARTER MOTOR FAILED DURING START CYCLE. STARTER MOTOR REPLACED. OIL SERVICE ACTIONED. DRY CYCLE OK. CH ECK START ACTIONED ON PUSHBACK. MF PART NR 774860A4. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101700146 20071017 00146 NM 2007 10 17 DL76L071317 1 20071007 A 3610 361002290 VALVE BOEING 767 767332 1382001 NM RT ENGINE MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 172DN 24775 RT PNEUMATIC ISOLATION VALVE LIGHT STAYS ON REGARDLESS OF SWITCH POSITION, NO IND OF RT DUCT PRESS CANNOT OPEN START VAL VE CANNOT GET N2 ROTATION. REMOVED AND REPLACED RT ISOLATION VALVE, CYCLED SWITCH SEVERAL TIMES, OPS CHECK NORMAL, DUCT PRESS NORMAL PRESS FOLLOWS VALVE CMD. 2 L 7 2 4F RT A1NM 2007101700148 20071017 00148 NM 2007 10 17 DL76L071320 1 20071008 A 3246 WHEEL BOEING 767 767332 1382001 NM MLG DAMAGED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 175DN 24803 RTB - ON TAXI SHORT OF RUNWAY, TOWER INFORMED OF POSSIBLE FLAT TIRE TAXIED CLEAR OF RUNWAY. INFORMED OF SMOKE FROM WHEE L WELL STOPPED A/C BRAKES INDICATIONS NORMAL INFORMED A/C HAVE TWO FLAT TIRES/C PERFORMED INSPECTION PER MM 05-51-16-201 . FLAT TIRE LOSS MAINT PRACTICES CK OK. REPLACED NR 7 AND 8 WHEEL ASSY AND BRAKES. 2 L 7 2 4F RT A1NM 2007101700149 20071017 00149 NM 2007 10 17 DLM90071321 1 20071008 A 5313 LONGERON DOUG MD90 MD9030 3023690 NM BS 1385 L29L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 AFT PIT LONGERON 29L CORRODED AROUND FASTENER AT STA 1385. REPAIRED IAW MD90 SRM 53-10-01 FIG 7. 2 L 7 2 4F RT A6WE 2007101700150 20071017 00150 NM 2007 10 17 DLM90071322 1 20071008 A 5347 593054767 SEAT TRACK DOUG MD90 MD9030 3023690 NM FS 648 TO FS 740 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 FOUND CABIN SEAT TRACK RBL 24 IS OUT OF LIMITS AT FS 700. REPAIRED SEAT TRACK RBL 24 FROM FS 648 TO FS 740 IAW MD90 SRM 53-40-01 FIG 6. 2 L 7 2 4F RT A6WE 2007101700152 20071017 00152 NM 2007 10 17 DLM90071324 1 20071007 A 5320 99305389 CUSP WEB DOUG MD90 MD9030 3023690 NM FS 655-769 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 FOUND LEFT CUSP WEB CORRODED FS 655 TO FS 769. REMOVED AND REPLACED CUSP WEB, LT IAW MD90 SRM 51-30-2, 51-30-5 AND 51-3 0-1. 2 L 7 2 4F RT A6WE 2007101700153 20071017 00153 NM 2007 10 17 DLM90071325 1 20071007 A 5347 593054767 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 1130 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 CABIN SEAT TRACK RBL 24 IS OUT OF LIMITS AT FS 1130. REPAIRED CABIN SEAT TRACK RBL 24 FS 973 TO 1184 IAW MD90 SRM 53-40 -01 FIG 6. 2 L 7 2 4F RT A6WE 2007101700154 20071017 00154 NM 2007 10 17 DLM90071326 1 20070901 A 5311 FRAME DOUG MD90 MD9030 3023690 NM BS 1344 S28-29L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 AFT PIT FWD SIDE OF FRAME CORRODED STA1344 28L-29R. REPAIRED FRAME AT STA 1344 IAW MD90 SRM 53-10-02A VOL I. 2 L 7 2 4F RT A6WE 2007101700155 20071017 00155 NM 2007 10 17 DLM90071327 1 20071005 A 5230 PAN DOUG MD90 MD9030 3023690 NM CARGO DOOR GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 C-1 DOOR PAN GOUGED AT LWR AFT LATCH CAM. REPAIRED DAMAGED AREA ON C-1 DR IAW MD80 SRM 52-05D FIG 26B SH2. 2 L 7 2 4F RT A6WE 2007101700156 20071017 00156 NM 2007 10 17 DLM90071328 1 20071005 A 5330 5936667 SKIN DOUG MD90 MD9030 3023690 NM BS 1379 S28-29L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 FOUND MINOR DENT AT STA 1379 BETWEEN S28L AND 29L WITHIN LIMITS PER SRM 53-30-02 TABLE 3 CONDITION 2 WILL REQUIRE REPAIR WITHIN 3500 FLT HOURS. REPAIRED DAMAGED AREA AT STA 1379 BETWEEN S 28L AND 29L IAW MD90 SRM 53-30-01 FIG 1. INSTALLED ID TAG IAW DAL PS 900-5-1 NR 4. 2 L 7 2 4F RT A6WE 2007101700158 20071017 00158 EU 2007 10 17 SIMA200728301 1 20070926 A 5347 7253725191 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 304AE 340B304 DURING MBV INSPECTION, THE SEAT TRACK A BL 0.0 WAS FOUND CORRODED. REPLACED SEAT TRACK USING PN 7253725-191 IAW SAAB SR M CHAPTER 53-70-60 PARA 10. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007101700160 20071017 00160 SO 2007 10 17 SIMA200728303 1 20071008 A 3320 7287500505 FIXTURE EMB 145 EMB145LR 3260212 SO CABIN LIGHTS ODOR A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 622AE 145108 ON TAXI IN, PAX AND FLIGHT ATTENDANT NOTICED A BURNING ODOR AROUND ROW 3. REMOVED AND REPLACED LIGHTNING FIXTURE IAW AM M 33-21-06. MEL RESTORED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007101700161 20071017 00161 SO 2007 10 17 SIMA200728304 1 20071008 A 3200 7455501 LANDING GEAR EMB 135 EMB135LR 3260305 SO UNKNOWN A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 728AE 145328 AFTER TAKEOFF CREW REPORTED AIR/GROUND FAIL WARNING. REPLACED GEAR HANDLE PN 7455501 SN 0589. REPLACED LGEU PN 3550220 02 SN 5270. ALSO, CLEANED AND SERVICED ALL LG STRUTS PERFORMED FUNCTIONAL TEST OF EXTENSION AND RETRACTION IAW AMM 32-3 0-00. CHECKED ALL 5 WOW PROX SWITCHES AND GAP CHECK IAW 32-63-05. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007101700162 20071017 00162 NM 2007 10 17 C1HA200786006 1 20071008 A 2131 RELIEF VALVE BOEING 727 7272S7 138407Z NM CABIN PRESSURE FAILED A C1HA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 GL 15 686CA 22021 UNABLE TO CONTROL CABIN PRESSURE WITH ANY MODE OF CONTROLLER. REMOVED AND REPLACED OUT FLOW VALVE IAW MM 21-31-11, PERF ORMED ADJ TEST IAW MM 21-31-00, OPS CHECK NORMAL. IN ALL MODES OF PRESSURIZATION, CABIN PRESSURE/ALTITUDE CLIMBS WHEN D IFF PRESS HITS 7.7 PSI. FOUND LT PRESS RELIEF VALVE NOT SEATED. REMOVED AND REPLACED SAME PER M/M 21-32-11. FOUND RT SAFTEY VALVE OPENING EARLY. REMOVED AND REPLACED RT CABIN PRESS RELIEF VALVE PER MM 21-32-11. PRESSURIZED A/C ABOVE 8. 2, A/C HELD PRESSURE OK FOR SERVICE. 2 L 7 3 4F A3WE 2007101600115 20071016 00115 2007 10 16 2007UALA04056 4 20071003 A 2565 410045091 BOTTLE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE DOOR SLIDE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 NR 3 MED EMERG SLIDE DOOR ASST BOTTLE NEEDS SERVICING. REPLACED BOTTLE AND SQUIB ASSEMBLY. OK FOR SERVICE 2 L 7 2 4F 4 F RT T0001SE E46NE 2007101600122 20071016 00122 NM 2007 10 16 2007UALA04063 1 20071004 A 5210 HINGE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE PAX DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 FWD ENTRY DOOR CUTOUT LWR HINGE HAS 2 FASTENER HOLES CRACKED. AFT ROW 1 ABOVE AND 1 BELOW HINGE CUTOUT. FABRICATED AN D INSTALLED EXTERNAL SKIN DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600123 20071016 00123 NM 2007 10 16 2007UALA04064 1 20071004 A 5340 BRACKET BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE PAX DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 FWD ENTRY DOORWAY, FWD 2" OF STA 303.9 AT END OF STR 10L HAS WEB ATTACH BRACKET CRACKED. FABRICATED AND INSTALLED INTER COSTAL AND ASSOCIATED ANGLE, CLIPS AND STRAPS. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600138 20071016 00138 NM 2007 10 16 07FDEA04522 1 20070930 A 5311 53FX1350 FRAME BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 283FE 22350 FWD CARGO, LOWER STUB FRAME EXTENSION AT STA 600 BETWEEN STR 21L AND 22L HAS A CRACK. REMOVED 53FX1350 STUB FRAME, FAB' D AND INSTALLED A NEW STUB FRAME IAW SRM 51-10-01 AND DWG 53FX1370. 2 L 7 3 4F RT A3WE 2007101600146 20071016 00146 NM 2007 10 16 07FDEA04530 1 20071008 A 5730 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 CRACK INDICATIONS REVEALED FASTENER HOLES AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT EDGE. 10-24-07 REPAIR CARR IED OUT AS PER FEDEX EA 1-5710-115214, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007101600148 20071016 00148 NM 2007 10 16 07FDEA04532 1 20071008 A 5730 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 RIGHT WING LEADING EDGE SLAT NR 6 OUTBOARD SLAT TRACK CUTOUT, SLAT TRACK NR 14, FOUND CRACK AT CORNER EDGE. 10-24-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007101600151 20071016 00151 NM 2007 10 16 HALA0700438 1 20070917 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 1221 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 LEVEL 1 CORROSION ON SEAT TRACK 46 LBL 11-00 AT STATION 1221. AREA REWORKED AND FOUND TO BE WITHIN LIMITES PER SRM 53-0 0-52. REWORKED AREA ALODINED AND PAINTED. 2 L 7 2 4F RT A1NM 2007101600153 20071016 00153 NM 2007 10 16 HALA0700441 1 20070917 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 1034 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 LEVEL 1 CORROSION ON SEAT TRACK SECTION 45 LBL 75 AT STATION 1034. AREA REWORKED AND FOUND WITHIN LIMITS PER SRM 53-00- 52. REWORKED AREA ALODINED AND PAINTED. 2 L 7 2 4F RT A1NM 2007101600155 20071016 00155 NM 2007 10 16 HALA00428 1 20071004 A 5343 ATTACH FITTING BOEING 767 767332 1382001 NM MLG BROKEN A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 598HA 23278 RIGHT LANDING GEAR DRAG BRACE DOOR AFT ATTACH FITTING BROKEN. REPAIRED PER HAL M105 FILE NR 598057. 2 L 7 2 4F RT A1NM 2007101600156 20071016 00156 NM 2007 10 16 HALA0700429 1 20070917 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 1109 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 LEVEL 1 CORROSION ON SEAT TRACK RBL - 55, AT STATION 1109. AREA REWORKED AND FOUND WITHIN LIMITS PER SRM 53-00-52. REW ORKED AREA ALODINED AND PAINTED. 2 L 7 2 4F RT A1NM 2007101600157 20071016 00157 NM 2007 10 16 HALA0700431 1 20070917 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 LEVEL 1 CORROSION ON SEAT TRACK RBL 69 AT STATION 1197 + 82. AREAS REWORKED AND FOUND WITHIN LIMITS, PER SRM 53-00-52. REWORKED AREA ALODONED AND PAINTED. 2 L 7 2 4F RT A1NM 2007101600161 20071016 00161 NM 2007 10 16 UIEA200700434 1 20071008 A 5730 PANEL BOEING 747 74747UF 1384812 NM RT WING DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 492 29253 DAMAGE TO THE RT FIXED UPPER WING TRAILING EDGE PANEL WBL 235 ALONG THE TRAILING EDGE 7" FROM THE OUTBD END 1"IN LENGTH BY 1/4" WIDE . 2 L 7 4 4F RT A20WE 2007101600167 20071016 00167 NM 2007 10 16 QXEA200701526 1 20071005 A 5270 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR FALSE ACTIVATION A QXEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 09 401QX 4031 STS - ON FLIGHT 2467, RETURNED TO FIELD. DOOR WARNING LIGHT IN-FLIGHT. MAIN CARGO DOOR AFTER TAKEOFF. THE DOOR T-HAND LE WAS OUT. MAINTENANCE INSPECTED AFT CARGO DOOR. NO DEFECTS NOTED. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO S ERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007101600169 20071016 00169 NM 2007 10 16 QXEA200701524 1 20071005 A 2751 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 409QX 4051 GEG - FLAP POWER CAUTION LIGHT ON. CHECKLIST COMPLIED WITH, DID NOT CORRECT. MAINTENANCE COMPLIED WITH FIM. CAUTION L IGHT CLEARED, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007101600170 20071016 00170 NM 2007 10 16 QXEA200701520 1 20071005 A 2721 8DK4075001 CONTROL UNIT BOMBDR DHC8 DHC8402 1390042 NM RUDDER TRIM MALFUNCTIONED A QXEA O OTHER O OTHER AP APPROACH 1 NM 09 411QX 4055 PDX - ON FIIGHT 2359, ON APPROACH THE RUDDER TRIM QUIT WORKING. ON THE SECOND ATTEMPT RIGHT RUDDER TRIM MOVED THE TRIM RAPIDLY TO THE RIGHT. LEFT RUDDER TRIM MOVED THE TRIM FURTHER AND RAPIDLY TO THE RIGHT AS WELL. CIRCUIT BREAKER PULLED PER RUNAWAY CHECKLIST. MAINTENANCE REMOVED AND REPLACED RUDDER TRIM/AILERON TRIM CONTROL PANEL. RESET CIRCUIT BREAKER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007101600173 20071016 00173 NM 2007 10 16 QXEA200701525 1 20071007 A 3080 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM ICE DETECTOR FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 402QX 4032 BOI - ON FLIGHT 2384, DURING AFTER START CHECKLIST, ICE DETECT WAS DISPLAYED ON ED IT WAS +14 C. CYCLED REF SPEED SWITC H INCREASE AND BACK OFF. MESSAGE WENT AWAY. NO FROST OR ICE ON AIRCRAFT. MAINTENANCE PERFORMED TEST OF ICE DETECTS AN D PERFORMED GVI OF PROBES. NO MESSAGES ON ED FOUND. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007101600175 20071016 00175 NM 2007 10 16 QXEA200701528 1 20071008 A 7600 SWITCH DHAV DHC8 DHC8202 2809007 NM ENGINE MALFUNCTIONED A QXEA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 NM 09 357PH 504 EUG - FLIGHT NR 2193, JUST AFTER ROTATION AS THE GEAR WAS COMING UP THE NR 2 ENGINE BEGAN SURGING BETWEEN TOP AND BETWEE N 125 PERCENT AND 140 PERCENT. AT 100 FT, THE ENGINE FAILURE CHECKLIST WAS COMPLETED PRIOR TO BEGINNING THE CHECKLIST B OTH NR 2 TORQUE AND NR 2 NP WERE FLUCTUATING, AS THE POWER WAS REDUCED T FLIGHT IDLE THE TORQUE CONTINUED SURGING APPROX IMATELY 20 PERCENT. ONCE THE CONDITION LEVER WAS MOVED TO START FEATHER THE SURGING DISSIPATED AND THE NR 2 NH SEEMED S TABLE AT 76 PERCENT. MAINTENANCE C/W MTC NR 9721004 OVERTORQUE INSPECTION PROCEDURES. FDR DOWNLOAD CONFIRMED TORQUE TO BE 121.6 PERCENT. NO MAINTENANCE ACTION ON TURBO AND RGB REQUIRED. OK FOR CONTINUED SERVICE. PROPELLER ASSEMBLY OK F 2 H 7 2 4T RT A13NM 2007101600181 20071016 00181 NM 2007 10 16 07FDEA04536 1 20071009 A 5753 6521630250 SKIN BOEING 727 727233 138408A NM FORE FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 RIGHT WING INBOARD FORE FLAP UPPER SURFACE GOUGE, 93" FROM INBOARD EDGE. REPAIR SURFACE DELAMINATION REF SRM 51-40-20 P ARA, S 7, 14, 15, 19, 20, 22 TAP TEST GOOD. PRIMED AND PAINTED AREA REF MM 51-20-151-7. THIS IS CLASSIFIED A MINOR REP AIR. 2 L 7 3 4F RT A3WE 2007101600182 20071016 00182 NM 2007 10 16 07FDEA04537 1 20071009 A 5753 SKIN BOEING 727 727233 138408A NM ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 RIGHT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED 96" FROM INBD EDGE. REPAIR SURFACE DELAMINATION REF SRM 51-40-20 P ARA'S 7, 14, 15, 19, 20, 22. TAP TEST GOOD PRIMED AND PAINTED REPAIR AREA, REF MM 51-20-151-7. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007101600183 20071016 00183 NM 2007 10 16 2007UALA04077 1 20071005 A 2421 6819006 IDG BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 1 FAILED A UALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 WP 29 128UA 30023 RTFL DUE TO NR 1 GEN AND NR 1 ELEC A/C BUSS INOP. OTHER A/C BUSSES WOULD NOT PICK UP LOAD. REPLACED NR 1 IDG. SHOP FO UND FAILED ROTOR. REPLACED LOG, ROTOR, SHAFT SEAL, & FILTER. 2 L 7 4 4F 4 F RT A20WE E24NE 2007101600188 20071016 00188 NM 2007 10 16 2007UALA04083 1 20071004 A 3411 STATIC INVERTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SMOKE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 592UA 28143 FOUND COCKPIT AND CABIN FILLED WITH SMOKE. OBSERVED SMOKE COMING FROM STATIC INVERTER. CB'S DID NOT POP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101600191 20071016 00191 NM 2007 10 16 2007UALA04086 1 20071005 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 43 ABC UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 FOUND EMERGENCY LIGHT ROW 43 ABC INOP. RESECURED EMERGENCY LIGHT. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007101600194 20071016 00194 NM 2007 10 16 2007UALA04089 1 20071002 A 2612 CGAB140001 FIRE LOOP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE AFT CARGO FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 922UA 26642 FOUND CARGO FIRE DETECTION AFT B LOOP FAIL LIGHT ILLUMINATED. SUSPECT FAULTY FIRE LOOPS. REPLACED FIRE LOOPS IN POSIT ION 1 AND POSITION 2 OPS CHECK NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600196 20071016 00196 NM 2007 10 16 2007UALA04091 1 20071008 A 2700 UNKNOWN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE UNKNOWN A UALA O OTHER F FLT CONT AFFECTED CL CLIMB 1 WP 29 936UA 26667 AC ROLLS RIGHT WHEN FLAPS EXT BEYOND POS 1 ON AND OFF AUTOPILOT. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101600199 20071016 00199 NM 2007 10 16 2007UALA04094 1 20071007 A 2730 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE ELEVATOR ILLUMINATED A UALA O OTHER J WARNING INDICATION LD LANDING 1 WP 29 674UA 29242 ELEVATOR CONTROL ABNORMAL LIGHT AT TOUCHDOWN. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101700003 20071017 00003 NM 2007 10 17 2007UALA04101 1 20071007 A 5310 DOOR FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CARGO DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 933UA 26659 FWD CARGO DOOR CUT-OUT AFT FRAME IS CRACKED ON AFT SIDE OF FRAME IN UPPER-INNER RADIUS AT INBD CORNER OF LOWER STOP FITT ING. MAJOR REPAIR: REMOVED CRACKED FRAME SECTION AND INSTALLED NEW FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101700018 20071017 00018 NM 2007 10 17 2007UALA04116 1 20071007 A 5210 S283W2031 BATTERY PACK BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE R2 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 227UA 30555 FOUND DOOR 2R EPAS BITE LIGHT IS NOT BLINKING GREEN. REPLACED EPAS BATTERY PACK. OP CHECK OK FOR SERVICE 2 L 7 2 4F 4 F RT T0001SE E46NE 2007101700019 20071017 00019 NM 2007 10 17 2007UALA04117 1 20071006 A 5530 1755518302 HINGE FITTING BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE VERTICAL STAB DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 794UA 44520 26953 FOUND LIGHTNING STRIKE DAMAGE IS AT VERTICAL STAB REAR SPAR UPPER RUDDER HINGE FITTING AT RUB STA 522. REMOVED AND REPL ACED HINGE FITTING. A/C OK FOR SERVICE 2 L 7 2 4F 4 F RT T0001SE E46NE 2007101700023 20071017 00023 NM 2007 10 17 2007UALA04121 1 20071006 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 674UA 29242 L MID SLIDE GROUND ILLUM LT INOPERATIVE. RELAMPED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101700024 20071017 00024 NM 2007 10 17 2007UALA04122 1 20071006 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE 24ABC, 28ABC INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 674UA 29242 FOUND 24ABC, 28ABC AND 31ABC EEL STRIPS ARE INOPERATIVE. REPLACED EEL STRIPS 2 L 7 2 4F 4 F RT A1NM E24NE 2007101700025 20071017 00025 NM 2007 10 17 2007UALA04123 1 20071006 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 674UA 29242 FOUND OVERHEAD EMERGENCY LIGHT RT SIDE ROW 36 INOPERATIVE. RELAMPED 2 L 7 2 4F 4 F RT A1NM E24NE 2007101700026 20071017 00026 NM 2007 10 17 2007UALA04124 1 20071008 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 FOUND CEILING EMERGENCY LIGHTS AT 26 RT, 41 RT AND LAV 100 ARE INOPERATIVE. RELAMPED 2 L 7 4 4F 4 F RT A20WE E24NE 2007101700028 20071017 00028 NM 2007 10 17 2007UALA04126 1 20071008 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 DOOR 1R BOTH SILL EMERGENCY LIGHTS, EMERGENCY EXIT SIGN ABOVE DOOR 1R, CEILING EMERGENCY EXIT LIGHT AT DOOR 1R AND AISLE EMERGENCY EXIT SIGN AT DOOR 1R ARE INOPERATIVE. 11-01-07 RECONNECTED BATTERY PACK CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007101700030 20071017 00030 NM 2007 10 17 2007UALA04128 1 20071006 A 2160 32148621 VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN TEMP FAULTY A UALA O OTHER O OTHER CR CRUISE 1 WP 29 651UA 25389 FWD CABIN TEMP CONTROL FAILED TO CONTROL DESIRED TEMP. CREW COMMENTS: FWD AND MID CABINS EXTREMELY COLD. AFTER EXTENSI VE TROUBLE SHOOTING FOUND FAULTY FWD TRIM AIR VALVE AND LOW LIMIT CONTROL VALVE. REPLACED BOTH VALVES OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101700036 20071017 00036 NM 2007 10 17 AALA20071882 1 20071007 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 JFK - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED BATTERY PACK AT M33409 FOR EMERGENCY LIGHT AT RIG HT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007101700037 20071017 00037 WP 2007 10 17 AALA20071884 1 20071007 A 3350 LENS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 962TW 53612 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 22 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROW 22. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007101700040 20071017 00040 WP 2007 10 17 AALA20071878 1 20071006 A 2432 CHARGER DOUG DC9 DC983 3022083 WP MASTER BATTERY INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 976TW 53626 LBB INFLIGHT T1873/06OCT DFW TO ABQ - DURING CRUISE BATTERY CHARGER LIGHT ILLUMINATED. LANDED LBB WITHOUT INCIDENT. RE PLACED BATTERY CHARGER, SHIP BATTERIES AND BATTERY CHARGER TRANSFER RELAY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007101700048 20071017 00048 EA 2007 10 17 SWIA200718750 1 20070807 A 2780 PINION GEAR CNDAIR CL600 CL6002C10 1390015 EA LT WING SLAT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 732SK 10194 FOUND AT CHECK, LEFT WING PINION GEAR FOR SLAT TRACK 1-3 HAS PITTING. INSTALLED NEW SLAT PINION AND TRACK GEAR PER CRJ7 00/900 AMM 27-81-09-400-802-A01. 2 L 7 2 4F RT A21EA 2007101700049 20071017 00049 EA 2007 10 17 SWIA200718751 1 20070807 A 2780 PINION GEAR CNDAIR CL600 CL6002C10 1390015 EA LT WING SLAT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 732SK 10194 FOUND AT C-CHECK, LEFT WING PINION GEAR FOR SLAT TRACK 1-1 HAS PITTING. REPLACED SLAT PINION GEAR PER CRJ700/900 AMM 27 -81-11-400-801-A01. 2 L 7 2 4F RT A21EA 2007101700059 20071017 00059 EA 2007 10 17 SWIA200718761 1 20071006 A 2621 346000371 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY LOW A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 941SW 7750 FLT 5818 - CARGO BTL LOW CAUTION MESSAGE INFLIGHT. DIVERTED TO MLI. REMOVED AND REPLACED BOTH CARGO FIRE BOTTLES IAW A MM 26-25-01. 2 L 7 2 4F RT A21EA 2007101700060 20071017 00060 SO 2007 10 17 SWIA200718762 1 20070929 A 3520 OXYGEN MASK EMB 120 EMB120ER 3260203 SO CABIN UNWANTED DEPLOY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 284YV 120284 FLT 5620 - OXYGEN MASKS AT ROW 5 DROPPED. RESTOWED MASKS AND SECURED PANEL AT ROW 5. NO DISCREPANCIES NOTED. 2 L 7 2 4T RT A31SO 2007101700061 20071017 00061 EA 2007 10 17 SWIA200718763 1 20071004 A 5210 SWITCH CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR ASSIST DIRTY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 929SW 7703 FLT 6515 - COULD NOT OPEN PAX DOOR AT THE GATE. CLEANED DOOR POWER ASSIST BUTTON. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007101700062 20071017 00062 EA 2007 10 17 SWIA200718764 1 20071006 A 2701 YOKE CNDAIR CL600 CL6002B19 1900309 EA FIRST OFFICER'S LACK OF LUBE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 494CA 7765 FLT 2912 - FIRST OFFICERS YOKE MAKES A CLICKING NOISE. CLEANED AND LUBRICATED YOKE ASSEMBLY, BEARINGS AND PULLEYS. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007101700067 20071017 00067 NM 2007 10 17 UIEA200700390 1 20070925 A 7830 SKIN PANEL BOEING 747 74747UF 1384812 NM THRUST REVERSER DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 496MC 29257 NR 1 ENGINE REVERSER RIGHT SIDE THRUST REVERSER FIXED AFT SECTION BEAVER TAIL OUTER SKIN PANEL DENTED. REWORKED DENTED AREA IAW SRM 51-70-01. 2 L 7 4 4F RT A20WE 2007101700071 20071017 00071 NM 2007 10 17 UIEA200700391 1 20070925 A 7830 ACCESS PANEL BOEING 747 74747UF 1384812 NM THRUST REVERSER DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 496MC 29257 NR 1 ENGINE REVERSER RIGHT SIDE LOWER AFT SECTION TENSION LATCH ACCESS PANEL SEVERAL RIVETS MIGRATED. REMOVED AND REPLA CED MIGRATED RIVETS IAW SRM 51-40-02. 2 L 7 4 4F RT A20WE 2007101700074 20071017 00074 NM 2007 10 17 UIEA200700388 1 20070925 A 7830 BLOWOUT PANEL BOEING 747 74747UF 1384812 NM THRUST REVERSER BROKEN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 496MC 29257 NR 1 ENGINE REVERSER LEFT SIDE LOWER FORWARD SECTION FORWARD END OF BLOW OUT PANEL SIDE SUPPORT BRACKET SECTION DAMAGED. REMOVED BROKEN RIVETS AND REPLACED WITH NEW RIVETS IAW SRM 51-40-02. 2 L 7 4 4F RT A20WE 2007101700076 20071017 00076 NM 2007 10 17 UIEA200700383 1 20070925 A 5730 SKIN BOEING 747 747230B 1384889 NM WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 SURF CORROSION EVIDENT AROUND HEAD FROM WS 528 TO WS 724.5 BETWEEN REAR SPAR AND MID SPAR. SURF CORROSION REMOVED AND R EPROTECTED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 2007101700077 20071017 00077 NM 2007 10 17 UIEA200700382 1 20070925 A 5730 SKIN BOEING 747 747230B 1384889 NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 LHW UPPER SURFACE MID SPAR WS 1112 WS 1280 WS 1330 WS 1392 CORROSION EVIDENT. SURF CORROSION REMOVED AND REPROTECTED IA W SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 2007101700079 20071017 00079 NM 2007 10 17 UIEA200700381 1 20070925 A 5711 SPAR BOEING 747 747230B 1384889 NM ZONE 500 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 LHW UPPER SURFACE WS 353 TO WS 586 SPAR SURF CORROSION EVIDENT. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 2007101700080 20071017 00080 NM 2007 10 17 UIEA200700393 1 20070925 A 5730 SKIN BOEING 747 747230B 1384889 NM RT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 RIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10 -02. 2 L 7 4 4F A20WE 2007101700095 20071017 00095 NM 2007 10 17 UIEA200700410 1 20070928 A 5347 SEAT TRACK BOEING 747 747230B 1384889 NM ZONE 200 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 MAIN DECK BS 459 LBL 64 SEAT TRACK CORROSION, LEVEL 2. REPAIRED SEAT TRACK IAW SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2007101700097 20071017 00097 NM 2007 10 17 UIEA200700408 1 20070928 A 5330 SKIN BOEING 747 747230B 1384889 NM BS 1241 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 BS 1241 LBL 11- LBL 33 CTR SECTION UPPER SKIN CORROSION, LEVEL 1. BLENDED OUT IAW SRM 51-10-01 AND BOEING MESSAGE NUMBE R 1-598402422-7. 2 L 7 4 4F A20WE 2007101700102 20071017 00102 NM 2007 10 17 UIEA200700414 1 20070928 A 5755 SKIN BOEING 747 747230B 1384889 NM NR 1 SPOILER DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 NR 1 SPOILER INBOARD EDGE DELAMINATED. REPAIR CARRIED OUT PER SRM 51-40-24. 2 L 7 4 4F A20WE 2007101700103 20071017 00103 NM 2007 10 17 UIEA200700415 1 20070928 A 5711 SPAR BOEING 747 747230B 1384889 NM RT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 RIGHT WING STATION 1337 FRONT SPAR TO REAR SPAR HAS CORROSION EVIDENT. REMOVED CORROSION IAW SRM 51-10-01. 2 L 7 4 4F A20WE 2007101700104 20071017 00104 NM 2007 10 17 UIEA200700416 1 20070928 A 5311 FRAME BOEING 747 747230B 1384889 NM BS 1760 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 FOUND MAIN DECK STA 1760 FRAME CRACKED AT STR 13R - 14R. REPAIRED PER BOEING MESSAGE 1-542767421-2. 2 L 7 4 4F A20WE 2007101700114 20071017 00114 NM 2007 10 17 UIEA200700425 1 20071001 A 5330 SKIN BOEING 747 7472D3B 1384805 NM BS 2613 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 LOWER AFT FUSELAGE EXTERIOR SKIN DOUBLER/TRIPLER AT FS 2613 PREVIOUS REPAIR DAMAGED WITH HEAVY ABRASION/SCRAPING DUE TO TAIL DRAG. REMOVED AND REPLACED DOUBLER/TRIPLER REPAIR AS PER 747-200 SRM 51-30-02 AND 51-30-03 FIG 1 SHEETS 1 THRU 6. REFERENCE ATLAS XEO 53-092807. 2 L 7 4 4F RT A20WE 2007101700118 20071017 00118 NM 2007 10 17 UIEA200700431 1 20071002 A 5280 SKIN BOEING 747 74747UF 1384812 NM RT WONG DOOR DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 499MC 29260 RIGHT WING GEAR GULL WING DOOR FORWARD EDGE DELAMINATED. DELAMINATION REPAIRED IAW SRM 52-80-02 AND XEO 57-092907-1. 2 L 7 4 4F RT A20WE 2007101700121 20071017 00121 NM 2007 10 17 UIEA200700436 1 20071009 A 7160 9609M08P03 BEARING BOEING 747 74747UF 1384812 NM GE CF6 CF680C2* GL NR 2 VSV WORN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 492 29253 704719 NR 2 ENG RT VSV ACTUATOR ROD END BEARING CONNECTION TO VSV LEVER ARM WORN AND ALSO SLIDE (GUIDE) BLOCK WORN. NR 2 ENG R T VSV ACTUATOR REMOVED AND REPLACED IAW AMM SLIDER BLOCK. REPLACED IAW GE MM 72-32-10. 2 L 7 4 4F 4 F RT A20WE E23EA 2007101700122 20071017 00122 NM 2007 10 17 UIEA200700437 1 20071009 A 7160 9609M13P02 SLIDE BLOCK BOEING 747 74747UF 1384812 NM GE CF6 CF680C2* GL NR 2 VSV WORN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 492 29253 704719 NR 2ENG LT VSV ACTUATOR SLIDE BLOCK WORN. SLIDE BLOCK REMOVED AND REPLACED IAW BOEING 747 REV 60 SUBTASK 72-36-00-408-0 15-500. 2 L 7 4 4F 4 F RT A20WE E23EA 2007101700126 20071017 00126 EU 2007 10 17 F3LA200700277 1 20071008 A 2432 2758 BATTERY AIRBUS A319 A319112 3930323 EU MASTER DISCHARGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1876 FLIGHT CREW REPORTED EMERGENCY LIGHTS "ON" CAUSING LOW VOLTAGE ON AIRCRAFT BATTERY. REMOVED AND REPLACED NR 1 MAIN BATT ERY IAW AMM 24-38-37 PB401. OPS CHECKED GOOD. 2 L 7 2 4F RT A28NM 2007101700128 20071017 00128 NM 2007 10 17 DLM90071294 1 20071003 A 3320 BALLAST DOUG MD90 MD9030 3023690 NM CABIN LIGHTS SHORTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 905DA 53385 FLT ATTENDANT REPORT STRONG ODOR OF SMOKE LIKE MATCH BEING LIT BETWEEN 19-25. NOR VISUAL IND OF SMOKE. IT DISSIPATED A FTER 5 MIN. NO ABNORMAL INDICATIONS NO SMOKE DETECTOR ALARMS. OP VIDEO SYS, CKS NML O2 GENERATORS AND VDUS INSP. INSP ECTED BATTERY PACKS FOR EMERG LIGHTS ALL OK. FOUND FAILED FLUORESCENT OVERHEAD LIGHT BALLAST. REMOVED BULB ROW 18-19, FWD TO MCO AND PLAC PER MEL 33-20-01A. NEEDS BALLAST AND BULBS, REPLACED BALLAST AND LIGHT AT 18 AND 19. OPS NORMAL MC O AND PLAC REMOVED. 2 L 7 2 4F RT A6WE 2007101700135 20071017 00135 2007 10 17 DL76L071301 4 20071004 A 3442 20414440401 ANTENNA BOEING 767 767332 1382001 NM WX RADAR SYS FAILED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 188DN 27583 AFTER T/O, WX RADAR FROZE HARDOVER RT SIDE DISPLAYING A PENCIL BEAM. WX RADAR WILL NOT PAINT AND DISPLAY LOCKS UP. WX XCVER FAILED BITE. REMOVED/REPLACED WX RADAR XCVER. REMOVED/REPLACED WX RADAR ANTENNA. BITE CHECK PER FIM 34-43-00 CH KS OK. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007101700136 20071017 00136 NM 2007 10 17 DL757071302 1 20071005 A 5330 143N34714 SKIN BOEING 757 757232 1384965 NM FS 534 S27L GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 GOUGE BEYOND LIMITS, REPAIRED PER SRM 53-00-01. REPAIR 3 REF ERA 464376-14 REV ORIG FUSELAGE/SKIN/FS 534, S-27L/GOUGE. 2 L 7 2 4F RT A2NM 2007101700140 20071017 00140 NE 2007 10 17 DL757071306 2 20071007 A 7200 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 SHUTDOWN A DALA D RETURN TO BLOCK Y J ENGINE STOPPAGE WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 635DL 47839 23762 716596 RIGHT ENGINE ROLLED BACK AND SHUTDOWN DURING TAXI. MAINTENANCE IN PROGRESS DNTC. RAN ENG AT IDLE AND TAKEOFF AND MONIT ORED ALL ENGINE, PARAMETERS. NO PROBLEMS NOTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101700151 20071017 00151 NM 2007 10 17 DLM90071323 1 20071006 A 5311 FRAME DOUG MD90 MD9030 3023690 NM BS 1542 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 AFT ACC BAY STA 1542 CANT FRAME IS CRACKED RT JUST O/B OF AIRSTAIR CUTOUT. REPAIRED FRAME IAW MD90 SRM 51-70-01 FIG 1. 2 L 7 2 4F RT A6WE 2007101700163 20071017 00163 GL 2007 10 17 ARWA20071001 2 20071009 A 7261 OIL SYSTEM DOUG DC10 DC1030F 3023504 WP GE CF6 CF6* 30020 GL NR 1 ENGINE LEAKING A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 478CT 47819 455411 NR 1 ENGINE OIL QUANTITY STEADY CAME DOWN TO 1 1/2 QUARTS OF OIL REMAINING AND PRESSURE BEGAN TO FLUCTUATE, SHUT DOWN FO R PRECAUTION AT 1321-Z. 10-19-07 FOUND NR 1 ENGINE WAS REMOVED AND REPLACED AS PER ARROW W/C 141R7101M AND DC10 MM 71-00-00. OPERATIONAL CHECK NORMAL ON RUN-UP IN ACCORDANCE WITH MM 71-00-00. 2 L 7 3 4F 4 F RT A22WE E23EA 2007101700166 20071017 00166 SO 2007 10 17 CHQA20070053 1 20070917 A 3240 39807 CONTROL VALVE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL MLG BRAKES FAULTED A CHQA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 11 376SK 15404 145578 CAE312007 STL TO MSP - UPON LOWERING LANDING GEAR ON FINAL APPROACH, CREW RECEIVED "INBOARD BRAKE INOP" EICAS MESSAGE. THE CREW D ID A GO-AROUND TO CONSULT THE QRH AND EVALUATE THE SITUATION. AS A PRECAUTION, AN EMERGENCY WAS DECLARED AND THE AIRCRA FT LANDED ON THE LONGEST RUNWAY. THE AIRCRAFT LANDED AND TAXIED TO THE GATE WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE FAULT WITH THE CMC TO THE INBOARD BRAKE CONTROL VALVE, WHICH WAS REPLACED AND THE AIRCRAFT BRAKING SYSTEM OPS CHECKE D GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007101700167 20071017 00167 SO 2007 10 17 CHQA20070054 1 20071007 A 3150 WARNING LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL ILLUMINATED A CHQA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 11 292SK 145488 CAE311794 ORF TO IAD - THE AIRCRAFT WAS HEAVY ON FUEL FOR LANDING IN IAD, THE CREW EXTENDED FLAPS AND LANDING GEAR IN ORDER TO BUR N FUEL TO ENSURE AIRCRAFT WAS UNDER MAXIMUM LANDING WEIGHT ON A 25 MILE FINAL. UPON EXTENDING, THE LANDING GEAR, CREW R ECEIVED "LG AIR/GND FAIL" MESSAGE ON EICAS, THOUGH THE GEAR INDICATIONS WERE GREEN AND THERE WAS OBVIOUS DRAG CREATED BY THE EXTENDED GEAR. CREW ELECTED TO DO A LOW-ALTITUDE FLYOVER IN ORDER TO HAVE THE TOWER ENSURE THAT THE GEAR APPEARED DOWN AND LOCKED IN ADDITION TO GOING THROUGH THE REQUIRED QRH CHECKLISTS. THE TOWER DID NOT OBSERVE ANY ABNORMALITIES I N THE GEAR FROM THEIR VISUAL INSPECTION AND THE AIRCRAFT LANDED SAFELY ON THE SECOND APPROACH. UPON LANDING THE SPOILER 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007101700168 20071017 00168 NM 2007 10 17 CHQA200700055 1 20071008 A 3244 184F234 TIRE BOMBDR CL600 CL6002D15 NM GE CF34 CF343B1 NE NLG FAILED A CHQA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 11 647BR 9 7399 GEE872717 IAH-DFW AT ROTATION ON TAKEOFF, A LARGE BANG AND SHUDDER WAS FELT FROM THE NOSE GEAR. THE TAKEOFF WAS CONTINUED BUT T HE LANDING GEAR WAS NOT RETRACTED BECAUSE IT WAS SUSPECTED THAT THERE HAD BEEN A NOSE TIRE FAILURE. IAH TOWER WAS ADVIS ED AND THEY DISCOVERED TIRE DEBRIS AT THE ROTATION POINT ON THE RUNWAY. THE AIRCRAFT REMAINED INT THE LOCAL IAH AREA WH ILE THE APPROPRIATE CHECKLISTS WERE RUN, MAINTENANCE CONTROL WAS CONTACTED, AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT WAS FLOWN ON A LOW FLY-BY TO HAVE THE NOSE GEAR INSPECTED WHERE IT WAS CONFIRMED THAT THE RIGHT NOSE WHEEL WAS DAMAGED. THE FIRST OFFICER EXECUTED A SOFT TOUCH DOWN AND SLOW ROLLOUT TO THE END OF THE RUNWAY. THE AIRCRAFT WAS THEN TAXIED 2 L 7 2 4F 4 F RT A21EA E15NE 2007101700170 20071017 00170 NM 2007 10 17 07FDEA04539 1 20071009 A 5754 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM LT WING LE SLAT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 LEFT WING, NR 3 LEADING EDGE SLAT MIDDLE SUPPORT FITTING FOUND CORROSION. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5740-115218, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007101700171 20071017 00171 NM 2007 10 17 07FDEA04540 1 20071009 A 5754 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM LT WING LE SLAT CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 LEFT WING, NR 3 LEADING EDGE SLAT O/B SUPPORT FITTING FOUND CHAFE MARK. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX E A 1-5740-115218, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007101700173 20071017 00173 NM 2007 10 17 07FDEA04542 1 20071009 A 5754 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM LT WING LE SLAT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 LEFT WING, NR 3 LEADING EDGE SLAT O/B SUPPORT FITTING MOUNTING HOLE ELONGATED. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5740-115218. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007101700174 20071017 00174 NM 2007 10 17 07FDEA04543 1 20071009 A 5754 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM LT WING LE SLAT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 LEFT WING, NR 3 LEADING EDGE SLAT I/B SUPPORT FITTING FOUND CORROSION. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5740-115218. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007101700175 20071017 00175 EU 2007 10 17 07FDEA04544 1 20071010 A 5320 A5397425920200 FLOOR SUPPORT AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 ALC FLOOR SUPPORT STRUCTURE BETWEEN FRAME 64-65 LBL5 IS CORRODED REMOVED DAMAGED ALC FLOOR SUPPORT AT LBL 5 BETWEEN FRAM E 64-65 IAW A310-200 SRM 51-40-21. RECEIVED NEW PROFILE, LOCATED AND DRILLED NEW PROFILE IAW A310-200 SRM 51-40-44. IN STALLED NEW PROFILE IAW A310-200 SRM 51-40-21 MAJOR REPAIR. 2 L 7 2 4F RT A35EU 2007101700177 20071017 00177 WP 2007 10 17 07FDEA04550 1 20071010 A 5347 NBA6022 SEAT TRACK DOUG DC10 DC1010F 3022111 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 ENTRY WAY, DURING REMOVAL FLOOR PANELS WITH OAN J/C MD10-0600C220-1JR FOUND SEVERE EXFOLIATION CORROSION INTERNAL SEAT T RACK. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F A22WE 2007101700178 20071017 00178 EU 2007 10 17 07FDEA04551 1 20071010 A 7830 THRUST REVERSER AIRBUS 300 A300F4605R 3930327 EU NR 1 ENGINE MALFUNCTIONED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 660FE 759 ENG NR 1 REV PRESSURIZED WHEN APPLYING TAKEOFF POWER. 10-19-07 R & R PRSOV LEAK & OPS NORMAL REACTIVATED T/R, OPS NORMAL PERFORMED ENG RUN AT POWER NO "REV PRESSURIZED WARNING " ALL MAINT PER A300 MM 78-31-05-4-05, 78-31-00-5-05, 78- 31-00-9-F. 2 L 7 2 4F RT A35EU 2007101700182 20071017 00182 EU 2007 10 17 07FDEA04557 1 20071010 A 5753 A5796011320100 RIB AIRBUS 300 A300F4605R 3930327 EU ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 DURING COMPLIANCE WITH EO NR 6-5750-7-5000 P2, RT INBD FLAP RIB 25 WAS FOUND TO BE CRACKED IN UPPER RADIUS REPLACEMENT O F DAMAGED PART. 2 L 7 2 4F RT A35EU 2007101700183 20071017 00183 EU 2007 10 17 07FDEA04558 1 20071010 A 5753 A5796011320100 RIB AIRBUS 300 A300F4605R 3930327 EU ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 DURING COMPLIANCE WITH EO NR 6-5750-7-5000 P2, RT INBD FLAP RIB 25 WAS FOUND TO BE CRACKED IN UPPER RADIUS REPLACEMENT O F DAMAGED PART. 2 L 7 2 4F RT A35EU 2007101700186 20071017 00186 NM 2007 10 17 07FDEA04561 1 20071010 A 5347 FX511002N567 SEAT TRACK BOEING 757 7572B7 1384964 NM ZONE 200 MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 FS 377-440, LBL 45.5, SEAT TRACK ASSY REPLACE PER CUSTOMER REQUEST. REMOVED SEAT TRACK ASSY FROM FS 377-440, LBL 45.5, PER SRM 51-40-02. FABRICATED SEAT TRACK ASSY ON MAE FAB SHOP TRAVELER NR T7/704367, PART NUMBER FX-51-10-02-N567. LO CATED AND DRILLED SEAT TRACK ASSY IAW SRM 51-40-02. TREATED AND PRIMED SEAT TRACK ASSY IAW SRM 51-20-02. INSTALLED SEA T TRACK ASSY IAW SRM 51-40-02, CENTER ROW ONLY. FASTENERS THAT GET INSTALLED THROUGH THE SEAT TRACK FLANGES WILL BE ACC OMPLISHED ON RCB MODIFICATION WORK CARD NR 118350472RCB AS THAT MOD PROGRESSES. 2 L 7 2 4F RT A2NM 2007101700187 20071017 00187 EA 2007 10 17 MASA200700458 1 20070728 A 3350 110049 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 715SF 10657 7115 ASH 7410 IAD. EMERGENCY PATH LIGHTING AT ROWS 2/4 AND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. MX R2 BATTERY PACK FOR OVERWING AND THE PACK AND LIGHT STRIP FOR THE PATH LIGHTING, BOTH OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007101700189 20071017 00189 EA 2007 10 17 MASA200700460 1 20070728 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 917FJ 15017 ASH 2646 CLT. AFT CABIN EMERGENCY FLOOD LIGHT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2007101700190 20071017 00190 EA 2007 10 17 MASA200700462 1 20070729 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37218 7218 ASH 2721 PHX. REPORTED THE EMERGENCY EXIT LIGHTS WILL NOT TURN OFF. MX RESET THE ESSENTIAL BUSS AND COULD NOT DUPLICAT E THE PROBLEM. 2 L 7 2 4F RT A21EA 2007101700193 20071017 00193 CE 2007 10 17 BSAASDR0725 1 20071005 A 5753 SKIN BEECH 1900 1900D 1154162 CE RT TE FLAP TORN A BSAA O OTHER O OTHER NR NOT REPORTED 1 NM 05 182YV UE182 RIGHT FLAP HUMP MISSING LARGE SECTION OF SHEET METAL. FLAP WAS REMOVED AND REPLACED. 2 L 7 2 4T RT A24CE 2007101700194 20071017 00194 NM 2007 10 17 SWAA074996 1 20071004 A 2121 215201 FAN BOEING 737 7377H4 1384404 NM CABIN AIR FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 472WN 33831 F/A REPORTED, ELECTRICAL ODOR IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2007101700195 20071017 00195 NM 2007 10 17 SWAA075008 1 20071007 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 736SA 27868 DURING SCHEDULED HC2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS INOP AT ROW 11 ABC. REMOVED AND REPLACED LIGHT BULB PE R MM. 2 L 7 2 4F RT A16WE 2007101700196 20071017 00196 NM 2007 10 17 SWAA075007 1 20071007 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 736SA 27868 DURING SCHEDULED HC2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS INOP AT ROW 9 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007101700199 20071017 00199 WP 2007 10 17 ASAA0782064 1 20071003 A 3220 VARIOUS LANDING GEAR DOUG DC9 DC983 3022083 WP NLG MALFUNCTIONED A ASAA O OTHER O OTHER AP APPROACH 1 NM 02 949AS 53022 ON APPROACH TO FAI LANDING GEAR WOULD NOT EXTEND (GEAR HANDLE WOULD NOT MOVE). EXTENDED GEAR MANUALLY AND LANDED SAFELY . FERRIED AIRCRAFT TO ANC FOR REPAIR WITH GEAR PINNED IN EXTENDED POSTION. EXERCISED GEAR REPEATEDLY ON GROUND. COULD NOT DUPLICATE PROBLEM. LUBED LANDING GEAR CONTROL LEVER AND BELLCRANKS. REPAIRED MINOR TO LT AND RT MLG DOOR SKIDS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007101700200 20071017 00200 NM 2007 10 17 ASAA0742088 1 20070928 A 5230 65C362311 SKIN BOEING 737 737490 1384715 NM CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 709AS 28896 AFT CARGO DOOR EXTERNAL SKIN IS DENTED 6 INCHES AFT OF FWD EDGE. SKIN REPAIRED IAW BOEING SRM 52-30-01 PG 201 REPAIR 2. 2 L 7 2 4F RT A16WE 2007101700201 20071017 00201 WP 2007 10 17 ASAA0782077 1 20071005 A 5322 9911840165 SHEAR TIE DOUG DC9 DC983 3022083 WP BS 1437 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 SHEAR TIE IS CRACKED. REPLACED SHEAR TIE PER SRM 51-10-4, 51-30-2 AND 51-30-5. 2 L 7 2 4F RT A6WE 2007101700204 20071017 00204 WP 2007 10 17 ASAA0782080 1 20071005 A 5313 591143289 LONGERON DOUG DC9 DC983 3022083 WP BS 1418-1419 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 LONGERON CRACKED. REMOVED DAMAGED SECTION OF LONGERON. INSTALLED REPLACEMENT SECTION PER SRM 53-02 (SPLICE REPAIR). 2 L 7 2 4F RT A6WE 2007101700205 20071017 00205 WP 2007 10 17 ASAA0782065 1 20071005 A 5347 5933054768 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 196-241 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 CABIN SEAT TRACK EXISTING REPAIR SPLICE CORRODED. REMOVED DAMAGED SECTION OF TRACK. INSTALLED REPLACEMENT PER SRM 51-1 0-4 AND 53-05. 2 L 7 2 4F RT A6WE 2007101700206 20071017 00206 WP 2007 10 17 ASAA0782066 1 20071005 A 5321 99365443 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 160-196 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007101700208 20071017 00208 WP 2007 10 17 ASAA0782068 1 20071005 A 5321 99365543 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 196-256 BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 CABIN FLOOR PANEL HAS BROKEN INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007101700211 20071017 00211 WP 2007 10 17 ASAA0782071 1 20071005 A 5321 99365479 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 180-200 BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 CABIN FLOOR PANEL HAS DAMAGED INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007101700213 20071017 00213 WP 2007 10 17 ASAA0782073 1 20071005 A 5321 993654511 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 160-196 BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 CABIN FLOOR PANEL HAS DAMAGED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007101700214 20071017 00214 WP 2007 10 17 ASAA0782074 1 20071005 A 5321 9936552013 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 200-256 BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 CABIN FLOOR PANEL HAS DAMAGED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007101700215 20071017 00215 WP 2007 10 17 ASAA0782075 1 20071005 A 5320 9936534139 TRACK DOUG DC9 DC983 3022083 WP BS 160-200 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 CABIN FALSE TRACK IS CORRODED. REPLACED TRACK PER SRM 51-10-3, 51-10-4, 53-14-1, AND 51-30-5. 2 L 7 2 4F RT A6WE 2007101700216 20071017 00216 WP 2007 10 17 ASAA0782076 1 20071005 A 5320 993653473 TRACK DOUG DC9 DC983 3022083 WP BS 160-200 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 CABIN FLOOR FALSE TRACK IS CORRODED. REPLACED FALSE TRACK PER SRM 51-10-3, 51-10-4, 53-14-1 AND 51-30-5. 2 L 7 2 4F RT A6WE 2007101700218 20071017 00218 NM 2007 10 17 ASAA0742090 1 20070928 A 5347 034053001037 SEAT TRACK BOEING 737 737490 1384715 NM BS 420 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 709AS 28896 CABIN RT LATERAL SEAT TRACK AT BS 420 IS GOUGED. REPLACED WITH FABRICATED REPAIR PART IAW PEMCO IPC SUPPLEMENT 53-21-01 FIG 11 & PEMCO ENGINEERING DWG 0340 53 0010 REV D & BOEING SRM 51-40-05 & 51-40-02. 2 L 7 2 4F RT A16WE 2007101700219 20071017 00219 NM 2007 10 17 ASAA0742091 1 20070928 A 5311 654653969 FRAME BOEING 737 737490 1384715 NM BS 616 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 709AS 28896 RT OVERWING BODY FRAME AT BS 616 INNER CHORD IS CRACKED AT BTM FASTENER HOLE. REPAIRED IAW CASCADE ERO7243 & ALASKA EA5 320 01814. 2 L 7 2 4F RT A16WE 2007101700222 20071017 00222 WP 2007 10 17 ASAA0782083 1 20071005 A 5754 99375681 RIB DOUG DC9 DC983 3022083 WP SLAT DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 LEFTHAND WING NR 5 L/E SLAT OUTBOARD RIB HOLES OVERSIZED. REPLACED WORN RIB PER SRM 51-10-4 AND 51-30-2. 2 L 7 2 4F RT A6WE 2007101700230 20071017 00230 EA 2007 10 17 TRAX200701426 1 20070927 A 5312 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 621 BULKHEAD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 855AS 7395 ON REAR PRESSURE BULKHEAD AFT SIDE AT FS 621.00 LBL 46.00 WL 93.00 AND RBL 46.00 WL 93.00 ANGLES FOUND CRACKED. BOTH CR ACKED ANGLES OF F/S 621.00 AFT SIDE REMOVED AS PER SRM 51-42-20. NEW ANGLES FABRICATED AS PER SRM 51-24-16 AND TREATED AS PER SRM 51-21-11 AND 51-25-06 FABRICATED ANGLE INSTALLED AS PER SRM 51-42-20. 2 L 7 2 4F RT A21EA 2007101700233 20071017 00233 EU 2007 10 17 TRAX200701430 1 20070928 A 5315 FLOORBEAM AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 ETNRC - FLOORBEAM 39 CORRODED. CORROSION ON FLOORBEAM 39 REMOVED IAW SRM 51-21-42 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42 MAT ERIAL THICKNESS: 0.071 MATERIAL REMOVED: 0.002 WITHIN LIMITS AS PER SRM: 53-00-00 FIG 305. 2 H 7 2 4T RT 2007101800001 20071018 00001 EU 2007 10 18 TRAX200701431 1 20070928 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 ETNRC - LT SEAT TRACK BETWEEN FR 36-38 CORRODED. CORROSION ON LT SEAT TRACK BTW FR 36-38 REMOVED IAW SRM 51-21-42 R EPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED I N ACCORDANCE WITH SRM 51-21-42 MATERIAL THICKNESS: 0.043. MATERIAL REMOVED: 0.003 WITHIN LIMITS AS PER SRM: 53-00- 00 FIG 304. 2 H 7 2 4T RT 2007101800002 20071018 00002 EU 2007 10 18 TRAX200701432 1 20070928 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 ETNRC - RT SEAT TRACK BETWEEN FR 36-38 CORRODED. CORROSION ON RT SEAT TRACK BTW FR 36-38 REMOVED IAW SRM 51-21-42 R EPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42 MATERIAL THICKNESS: 0.043. MATERIAL REMOVED: 0.004 WITHIN LIMITS AS PER SRM: 53-00-00 F IG 304. 2 H 7 2 4T RT 2007101800003 20071018 00003 EU 2007 10 18 TRAX200701433 1 20070928 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 ETNRC - RIGHT SEAT TRACK CORRODED BETWEEN FR 387-40. CORROSION ON RT SEAT TRACK BTW FR 38-40 REMOVED IAW SRM 51-21-4 25 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHE D IN ACCORDANCE WITH SRM 51-21-42 MATERIAL THICKNESS: 0.043. MATERIAL REMOVED: 0.003 WITHIN LIMITS AS PER SRM: 53-0 0-00 FIG 304. 2 H 7 2 4T RT 2007101800004 20071018 00004 EU 2007 10 18 TRAX200701434 1 20070928 A 5320 FLOOR SUPPORT AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 ETNRC - RT FLOOR SUPPORT CORRODED BETWEEN FR 39-41. CORROSION ON RT FLOOR SUPPORT REMOVED IAW SRM 51-21-42 REPAIR D ETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCO RDANCE WITH SRM 51-21-42 MATERIAL THICKNESS: 0.050. MATERIAL REMOVED: 0.002 WITHIN LIMITS AS PER SRM: 53-61-00 FIG 301 2 H 7 2 4T RT 2007101800005 20071018 00005 EU 2007 10 18 TRAX200701437 1 20070927 A 5310 DOOR FRAME AEROSP ATR72 ATR72 EU BS 6250 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 CARGO DOOR ACTUATOR AFT FITTING FRAME CRACKED AT FS STA 7065. HFER PERFORMED BY HEATHAIR W/O 37536 CRACK CINFIRMED ON STA, CARGO DOOR FRAME STA 6250, REPAIRED IAW SRM 52-31-00 FIG 402. 2 H 7 2 4T RT 2007101800006 20071018 00006 EU 2007 10 18 07FDEA04446 1 20071002 A 5740 A57150234201 LUG AIRBUS 310 A310324 3930206 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND CORROSION ONE BEARING BORE OF RT WING PYLON OUTBOARD MOUNTING LUG REPAIR PERFORMED BY BLEND OUT CORROSION, NDT FOR DAMAGE FREE IAW EA 6-5720- 81124 AND RAS/BAE/1000347/2005 ISS A. 2 L 7 2 4F RT A35EU 2007101800007 20071018 00007 EU 2007 10 18 07FDEA04451 1 20071002 A 5754 SKIN AIRBUS 310 A310324 3930206 EU NR 2 SLAT DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FOUND DENT AT SLAT NR 2 LT OUT OF LIMIT. NOSE SKIN REPAIR PERFORMED IAW SRM 57-43-11 FIG 202. 2 L 7 2 4F RT A35EU 2007101800008 20071018 00008 CE 2007 10 18 DXTA200702518 1 20071002 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LEFT WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 394QS 5600394 CAPTAIN SIDE LT BRAKE GOES SOFT INTERMITTENTLY. WHEN PEDAL PRESSURE RELEASED AND BRAKE REAPPLIED OPERATION IS NORMAL. P ERFORMED ANTI-SKID BRAKE BLEED PROCEDURE IAW 560 MM 32-42-00. SYSTEM CHECK NORMAL AT THIS TIME. 2 L 7 2 4F 4 F RT A22CE E25EA 2007101800014 20071018 00014 EU 2007 10 18 07FDEA04499 1 20071005 A 5753 A5796011320000 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 726FD 575 RT INBOARD FLAP RIB 25 FOUND CRACKED REMOVED SKIN AND STRINGERS. REMOVED DAMAGED RIB 25. INSTALLED NEW RIB 25 AND RE-I NSTALLED SKIN AND STRINGERS. SEALED AND PAINTED. 2 L 7 2 4F RT A35EU 2007101800015 20071018 00015 SW 2007 10 18 WGEA200700013 1 20071008 A 2741 271125681004 ACTUATOR ECLIPS EA500 ECLIPSEEA500 3350000 SW ELEVATOR TRIM STUCK E WGEA O OTHER J WARNING INDICATION CL CLIMB 1 EA 27 131DJ 70 000033 AFTER TAKEOFF "ELEVATOR TRIM TAB SPLIT " ADVISORY CAS APPEARED. LT TAB MOVEMENT WAS NORMAL AND RT TAB WAS STUCK AT 10 PERCENT NOSE DOWN. REMOVED AND REPLACED R/H ELEVATOR TRIM ACTUATOR I/A/W EA500 M/M 27-33-15. CHECKED ELEVATOR AND ELEVA TOR TRIM RIG I/A/W EA500 M/M 27-00-01, RIG CHECK GOOD. 1 L 7 2 4J RT A00002AC 2007101800021 20071018 00021 CE 2007 10 18 GLBA20061011 1 20071009 A 5320 1144300027180 ANGLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 211GL UE211 LT HEAVY ANGLE CRACKED AT FS 288. MX REPAIRED THE LT HEAVY ANGLE AT FS 288 IAW BEECH 1900D SRM 53-90. REPAIR DIMENSION S 13.5. PN 114-430002-7180. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101800022 20071018 00022 WP 2007 10 18 UPS07850893 1 20071009 A 3350 INVERTER DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:N/A ON PREFLIGHT, EMERGENCY LIGHT INVERTOR INOP. FOUND FUSE P21AB BLOWN. R&R RUSE. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2007101800026 20071018 00026 EU 2007 10 18 07FDEA04562 1 20071010 A 5347 A5327400584 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 670FE 777 MAIN CARGO DECK SEAT TRACK FROM FR 76 TO FR 75 RBL 58 HAS 3 AREAS WITH CORROSION. REMOVED, FABRICATED AND REPLACED SEA T TRACK IAW SRM 53-10-16 AND SRM 51-40-44. 2 L 7 2 4F RT A35EU 2007101800027 20071018 00027 WP 2007 10 18 07FDEA04563 1 20071010 A 5311 ACA00501 FRAME DOUG DC10 DC1010F 3022111 WP BS 588 S42-43L CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 NR 1 AIR CONDITIONING COMPT BYPASS VALVE PUSH-PULL CABLE CHAFING AGAINST FRAME TOP CHORD STA 588. REPAIRED FRAME IAW EA 8-5310-10920B, FUSELAGE-AIR CONDITIONING BAY FRAME CHAFED. ON INNER FLANGE-REPAIR. 2 L 7 3 4F A22WE 2007101900001 20071019 00001 WP 2007 10 19 ASAA0782085 1 20071005 A 5753 5930496506 DOUBLER DOUG DC9 DC983 3022083 WP FLAP VANE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 RIGHTHAND WING OUTBOARD FLAP INBOARD FIXED VANE L/E DOUBLER IS CHAFED. REPLACED EXISTING DOUBLER PER SRM 51-70-2. 2 L 7 2 4F RT A6WE 2007101900004 20071019 00004 NM 2007 10 19 HNAA0700214 1 20071006 A 3350 85 LIGHT DHAV DHC8 DHC8102 2809003 NM SWITCH INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 981HA 378 YELLOW LIGHT ON EMERGENCY LIGHT SWITCH INOP. REMOVED AND REPLACED BULB AND CLEANED SOCKET. 2 H 7 2 4T RT A13NM 2007101900005 20071019 00005 NM 2007 10 19 KCSA071456 1 20071009 A 5420 STIFFENER BOEING 747 7472B4B 138481B NM NR 2 PYLON GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 NR 2 PYLON I/B STIFFENER CHORD OF CLOSURE WEB AT NAC STA 272, NAC WL 180 IS GOUGED. 2 L 7 4 4F RT A20WE 2007101900012 20071019 00012 EU 2007 10 19 MALA070126 1 20070924 A 5230 SKIN SAAB SF340 340B 7860101 EU CARGO DOOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446XJ 340B446 DENT IN CARGO DOOR EXTERIOR SKIN 5.75'' FROM AFT EDGE AND 26.25'' FROM BOTTOM. REPAIRED PER EO#S52028. 2 L 7 2 4T RT A52EU 2007101900015 20071019 00015 NM 2007 10 19 NOCA15607 1 20070918 A 3350 S417T51013 LIGHT BOEING 767 76736N 1385152 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 768NA 29898 MID GALLEY LEFT SIDE FLOOR EMERGENCY LIGHT INOP. LIGHT ASSY NOT SECURED. REMOVED AND REPLACED MID GALLEY EMERGENCY LIG HT ASSY PER 33-51-16 WDM. OPS CHECK OK PER MM 33-51-10. 2 L 7 2 4F RT A1NM 2007101900017 20071019 00017 2007 10 19 NOCA15507 4 20070918 A 2565 60176104 SLIDE BOEING 767 76736N 1385152 NM RIGHT UNKNOWN A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 768NA 29898 REMOVE AND REPLACE SLIDE POS EMERGENCY RIGHT P/N 60174-104, S/N 0359. REMOVED AND REPLACED SLIDE POS EMERGENCY RIGHT SI DE PER MM 25-66-10. OK FOR SERVICES. 2 L 7 2 4F RT A1NM 2007101900018 20071019 00018 EU 2007 10 19 TRAX200701474 1 20071005 A 5210 UNKNOWN AEROSP ATR72 ATR72 EU PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 F/A REPORTS MAIN CABIN DOOR HARD TO OPEN AND CLOSE. 2 H 7 2 4T RT 2007101900022 20071019 00022 EU 2007 10 19 MALA07132 1 20070924 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 301 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446XJ 340B446 FOUND SEAT TRACK CORRODED LBL18.3 STA 301. REPLACED SEAT TRACK PER EO NR S53342. 2 L 7 2 4T RT A52EU 2007101900023 20071019 00023 EU 2007 10 19 MALA07133 1 20070924 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446XJ 340B446 FOUND DENTS IN BELLY FAIRING PANEL 193AL. REPAIRED PER EO NR S51031. 2 L 7 2 4T RT A52EU 2007101900025 20071019 00025 NM 2007 10 19 AALA20071891 1 20071008 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 790AN 30251 JFK - EMERGENCY LIGHTS AT SEAT ROWS 9D TO 13D INOPERATIVE. REPLACED BATTERY PACK AT RIGHT NUMBER TWO DOOR FOR EMERGENCY LIGHTS AT SEAT ROWS 9D TO 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007101900028 20071019 00028 NM 2007 10 19 AALA20071889 1 20071008 A 3397 WIRE BOEING 767 767323 1385205 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 381AN 25450 ORD - EMERGENCY LIGHTS AT SEAT ROWS 31H TO 36H INOPERATIVE. SECURED WIRE CONNECTION AT SEAT ROW 32H FOR INOPERATIVE EME RGENCY LIGHTS AT SEAT ROWS 31H TO 36H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007101900029 20071019 00029 NM 2007 10 19 AALA20071890 1 20071008 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 NRT - EMERGENCY LIGHT AT FIRST CLASS CLOSET LOWER LEFT POSITION INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGH T AT FIRST CLASS CLOSET LOWER LEFT POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007101900031 20071019 00031 NM 2007 10 19 AALA20071895 1 20071008 A 3350 1317 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 JFK - EMERGENCY LIGHT AT FIRST CLASS GALLEY OVERHEAD RIGHT CENTER AISLE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT FIRST CLASS GALLEY OVERHEAD RIGHT CENTER AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007101900032 20071019 00032 NM 2007 10 19 AALA20071896 1 20071008 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 616AA 24524 MIA - EMERGENCY LIGHT AT SEAT ROW 17 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 17. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007101900034 20071019 00034 WP 2007 10 19 AALA20071898 1 20071008 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 555AN 53085 LAX - EMERGENCY LIGHT AT SEAT ROW 16D HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 16D. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007101900035 20071019 00035 WP 2007 10 19 AALA20071899 1 20071008 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 555AN 53085 LAX - EMERGENCY LIGHT AT SEAT ROW 29D BROKEN. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 29D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007101900036 20071019 00036 WP 2007 10 19 AALA20071900 1 20071008 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 555AN 53085 LAX - EMERGENCY LIGHT AT SEAT ROW 29D HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 29D. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007101700006 20071017 00006 NM 2007 10 17 2007UALA04104 1 20071006 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 537 S12R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 FUSELAGE SKIN HAS SUBSURFACE CRACK ALONG THE CHEM-MILL EDGE 1.25"IN LENGTH LWR SIDE OF RIVET ROW STA 537 STR 12R. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101700007 20071017 00007 2007 10 17 2007UALA04105 4 20071006 A 2565 D31591478U1 SLIDE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE L1 DOOR UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 FOUND ESCAPE SLIDE DOOR 1L CAME OUT OF CONTAINER WHEN DOOR OPENED. SUSPECT IMPROPERLY INSTALLED. REINSTALLED SLIDE AS PER MM 25-6 1-35. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101700011 20071017 00011 NM 2007 10 17 2007UALA04109 1 20071006 A 5322 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1700 S28-29R CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 AFT PIT STA 1700 BETWEEN STR 28R AND 29R SHEAR TIE HAS CORROSION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101700031 20071017 00031 NM 2007 10 17 AALA20071876 1 20071006 A 2611 PU90471WR4 SMOKE DETECTOR BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 LHR FLIGHT DECK CREW REST SMOKE DETECTOR FAILED CABIN SYSTEM CONTROL PANEL FUNCTIONAL TEST. REPLACED FLIGHT DECK CREW R EST SMOKE DETECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007101700035 20071017 00035 NM 2007 10 17 AALA20071887 1 20071007 A 2741 6355B000103 ACTUATOR BOEING 737 737823 13844BZ NM STAB TRIM INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 960AN 29542 LAX INFLIGHT T2206/07OCT SNA TO DFW DIVERTED TO LAX - STABILIZER TRIM FAULTED AFTER TAKEOFF. LANDED LAX WITHOUT INCIDE NT. AIRCRAFT TAKEN OUT OF SERVICE. REPLACED STABILIZER TRIM ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007101700042 20071017 00042 NM 2007 10 17 AALA20071883 1 20071007 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 633AA 24591 MIA - EMERGENCY LIGHT AT SEAT 18D AFT IS BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 18D AFT. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007101700055 20071017 00055 SO 2007 10 17 SWIA200718757 1 20071001 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 235SW 120310 FOUND EMERGENCY EXIT SIGN AT ROW 6A BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 2007101700056 20071017 00056 SO 2007 10 17 SWIA200718758 1 20071002 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DAMAGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 563SW 120338 FLT 5417 - WHITE FLOOR EMERGENCY LIGHTS ARE INOP BELOW GALLEY. REPAIRED FLOOR EMERGENCY LIGHT WIRING. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007101700063 20071017 00063 NM 2007 10 17 UIEA200700389 1 20070925 A 7830 COWL FASTENER BOEING 747 74747UF 1384812 NM THRUST REVERSER DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 496MC 29257 NR 1 ENGINE REVERSER LEFT SIDE TRANSLATING COWL FWD SECTION LOWER HALF HAS SEVERAL RIVETS MIGRATED. REMOVED AND REPLACE D LOOSE AND MIGRATED RIVETS IAW SRM 51-40-02. 2 L 7 4 4F RT A20WE 2007101700066 20071017 00066 2007 10 17 UIEA200700432 4 20071003 A 3418 2566A30A SENSOR BOEING 747 7472D3B 1384805 NM STALL WARNING FAILED A UIEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 505MC 21251 AIR TURN BACK, AT ROTATION STICK SHAKER CAME ON AND STAYED ON UNTIL LANDING. VR SPEED WAS 129 KNOTS. REMOVED AND REPLA CED LEFT AOA SENSOR AND STALL WARNING COMPUTER IAW 27-30-01, OPS CHECKED NORMAL IAW 27-30-00. 2 L 7 4 4F RT A20WE 2007101700082 20071017 00082 NM 2007 10 17 UIEA200700394 1 20070926 A 5730 SKIN BOEING 747 747230B 1384889 NM RT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 RIGHT WING SURFACE CORROSION EVIDENT AROUND FASTENER HEAD FROM SIDE OF BODY TO WS 528 BETWEEN MID SPAR AND REAR SPAR. C ORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 2007101700105 20071017 00105 NM 2007 10 17 UIEA200700417 1 20070929 A 5730 PANEL BOEING 747 7472D7B 1384803 NM RT WING DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 RT WING UPPER L/E FIXED PANEL AT WS 317.32 HAS AN AREA OF 2.0 INCH LONG BY 2.0 INCH WIDE OF DELAMINATION. PERMANENT REP AIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18, SHEETS 1 THRU 5 AND SRM 51-40-12. ALSO, REFERENCE ATLAS AIR EO NR 4757A393. 2 L 7 4 4F RT A20WE 2007101700141 20071017 00141 NM 2007 10 17 DL76S071307 1 20071007 A 3150 WARNING LIGHT BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 ENGINE ILLUMINATED A DALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 27 122DL 36337 3560 23436 580387 DURING T/O ROLL, RT ENG FUEL FILTER ADVISORY STATUS MSG INDICATED. OCCURRED APPROX 100-110 KNTS T/S PER FIM. REMOVED F UEL FILTER ELEMENT INSP FOR DEBRIS, NONE FOUND. INSTALLED NEW FILTER ELEMENT PER MM. RAN ENG, OPS CHECK AND LEAK CHECK OK. 2 L 7 2 4F 4 F RT A1NM E13NE 2007101700147 20071017 00147 NM 2007 10 17 DL76L071319 1 20071008 A 2530 828450407M0DA OVEN BOEING 767 767332 1382001 NM MID GALLEY DIRTY A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 199DN 28456 FLIGHT ATTENDANT REPORTS ELEC OR HOT METAL ODOR IN MID GALLEY. TURNED OFF OVEN AND CHILLER AND OPENED CIRCUIT BREAKERS IN MID GALLEY. OPERATED COFFEEMAKERS. OVENS AND CHILLERS FOR SEVERAL HRS ON GND FOUND ODOR COMING FROM OVEN TRAYS, NOT IFIED CATERING TO REMOVE SAME AND CLEANED OVENS. OK FOR SERVICE AFTER OVEN CLEANING. 2 L 7 2 4F RT A1NM 2007101700157 20071017 00157 NM 2007 10 17 DL76L071330 1 20071009 A 3240 26124121A BRAKE BOEING 767 767332 1382001 NM NR 5 OVERHEATED A DALA O OTHER M J OVER TEMP WARNING INDICATION LD LANDING 1 SO 27 191DN 28448 EXCESSIVELY HOT BRAKES FOLLOWING LANDING. LEFT AFT MAIN OUTBOARD WAS 9 DURING TAXI NR 5, NUMBER FWD OF IT HEATING AS RE SULT 6 BRAKE TEMP SUSPECT POSSIBLE DRAGGING BRAKE. NO OTHER INDICATIONS. REPLACED NR 5 MAIN BRAKE PER M/M. PERFORMED CONDITIONAL INSPECTION OF BRAKES AND TIRES ON LT LANDING GEAR PER M/M 05-51-14-212-094 DUE TO HIGH TEMP AND NR 5 MAIN TI RE FUSE PLUG MELTING. NO DAMAGE NOTED ON REMAING TIRES AND BRAKES. NO DAMAGE NOTED ON NR 5 BRAKE AXLE. OPERATED BRAKE S CKS GOOD. 2 L 7 2 4F RT A1NM 2007101700159 20071017 00159 EU 2007 10 17 SIMA200728302 1 20071004 A 5347 7253725191 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 304AE 21126 500 340B304 DURING A MBV INSPECTION, THE SEAT TRACK AT B.L. 18.3L WAS FOUND TO BE CORRODED. REPAIRED IAW SAAB SRM CHAPTER 53-70-60 PARA 10. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007101700169 20071017 00169 NM 2007 10 17 07FDEA04538 1 20071009 A 2120 DUCT BOEING 727 727233 138408A NM CABIN AIR BLOWN A FDEA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SO 25 278FE 22345 HEARD LOUD BANG WHILE CLIMBING PAST 32,000 FEET. BANG APPEARED TO BE BELOW AND FORWARD OF THE INSTRUMENT PANEL. DID NO T NOTICE ANY ENGINE OR PRESSURIZATION FLUCTUATIONS. FOUND GASPER AIR DUCT BLOWN. COMPLETED TEMP REPAIR WITH CARGO PIT TAPE PER EA 7-2120-115556 PT 1. DUCT JOINT LOCATED IN E/E COMPARTMENT RT SIDE JUST FWD OF THE EXTERNAL POWER C/B PANEL. 2 L 7 3 4F RT A3WE 2007101700176 20071017 00176 WP 2007 10 17 07FDEA04549 1 20071010 A 5315 AFA0043 FLOORBEAM DOUG DC10 DC1010F 3022111 WP ZONE 200 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 FOUND EXISTING REPAIR CTR CARGO COMPARTMENT FLOORBEAM. REPAIRED AREA IAW SRM 53-60-01 FIG 3 VOL I. 2 L 7 3 4F A22WE 2007101700191 20071017 00191 NE 2007 10 17 KPVA200716 2 20071004 A 7261 3037479 TUBE DHAV DHC8 DHC8103 1386005 NM PWA PW121 PW121 52124 NE NR 2 ENGINE FAILED A KPVA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 13 979HA 373 PCE121320 (PIREP) ON CLIMBOUT AT 3000FT, THE NR 2 ENGINE OIL PRESSURE LIGHT ILLUMINATED AND ZERO OIL PRESSURE ON THE GAUGE. SHUT THE ENGINE DOWN PER CHECKLIST AND LANDED WITHOUT INCIDENT. (MX) REMOVED AND REPLACED NR 2 ENGINE IAW RORM AIA M-105. O PS AND LEAK CHECK IAW DHC-8 MM 71-00-00 PG 529-532. 2 H 7 2 4T 4 T RT A13NM E20NE 2007101700197 20071017 00197 NM 2007 10 17 SWAA074992 1 20071007 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 417WN 29822 DURING SCHEDULED MV3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007101700198 20071017 00198 NM 2007 10 17 SWAA074971 1 20071007 A 5310 6545815 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR CUTOUT LOWER FWD STUB FRAME CRACKED AT AFT END. REPAIRED STUB FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007101700202 20071017 00202 WP 2007 10 17 ASAA0782078 1 20071005 A 5320 591359581 STIFFENER DOUG DC9 DC983 3022083 WP BS 1418 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 FRAME STIFFENER CRACKED. REPLACED STIFFENER PER SRM 51-30-5, 51-30-2 AND DAC DWG 5913595. 2 L 7 2 4F RT A6WE 2007101700209 20071017 00209 WP 2007 10 17 ASAA0782069 1 20071005 A 5321 99365535 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 196-256 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007101700212 20071017 00212 WP 2007 10 17 ASAA0782072 1 20071005 A 5321 993655133 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 196-256 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007101800012 20071018 00012 EU 2007 10 18 HYIA12110 1 20071006 A 5347 S5337500120302 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 23 AND 29 CORRODED. CORROSION WAS REMOVED AND TRACK WAS FOUND TO BE OUT OF LIMI TS PER MANUFACTURES STRUCTURAL REPAIR MANUAL. SEAT TRACK WAS REPLACED. 2 H 7 2 4T RT A53EU 2007101800013 20071018 00013 EU 2007 10 18 HYIA12111 1 20071006 A 2711 S271100970320 ROD AEROSP ATR42 ATR42320 8680930 EU LT AILERON CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 LEFT AILERON TRIM TAB CONTROL ROD WAS FOUND TO BE CORRODED. CORROSION WAS FOUND TO BE BEYOND MANUFACTURERS LIMITS. ROD WAS REMOVED AND REPLACED. 2 H 7 2 4T RT A53EU 2007101800020 20071018 00020 CE 2007 10 18 GLBA20061010 1 20071009 A 5311 1144300027180 ANGLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 288 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 219GL UE219 RT HEAVY ANGLE CRACKED AT FS 288. MAINTENANCE REPAIRED THE RIGHT HAND HEAVY ANGLE AT FS 288 IAW BEECH 1900D SRM 53-90. REPAIR DIMENSIONS 13.5.PN 114-430002-7180. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101900002 20071019 00002 NM 2007 10 19 ASAA0742086 1 20070920 A 5753 6546486155 SKIN BOEING 737 737490 1384715 NM MID FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 709AS 28896 LEFT WING INBOARD MID FLAP TRAILING EDGE WEDGE LWR SURFACE HAS SEVERAL DENTS. WEDGE DENTS REPAIRED IAW BOEING SRM & ALA SKA AIRLINES EA5750 02393 & CASCADE ERO7260. 2 L 7 2 4F RT A16WE 2007101900003 20071019 00003 NM 2007 10 19 ASAA0742087 1 20070921 A 5753 6546430189 SKIN BOEING 737 737490 1384715 NM FORE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 709AS 28896 LEFT WING INBOARD FORE FLAP UPPER SURFACE HAS DENT. REPAIRED IAW BOEING SRM CHAPTER 51 70 10 REPAIR 3. 2 L 7 2 4F RT A16WE 2007101900008 20071019 00008 EU 2007 10 19 SA07063 1 20071008 A 3350 32145510 EPSU AIRBUS A321 A321211 3930370 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 169UW 23662 1455 TPA - THE EMERGENCY LIGHTS FAILED TEST WITH -R MID (R2) FAULT-. MAINTENANCE REPLACED THE RIGHT SIDE, MID-CABIN EMERGENC Y POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007101900021 20071019 00021 EU 2007 10 19 MALA070131 1 20070924 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 301 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446XJ 340B446 FOUND SEAT TRACK CORRODED BLO STA 301. REPLACED SEAT TRACK PER EO NR S53342. 2 L 7 2 4T RT A52EU 2007101900030 20071019 00030 NM 2007 10 19 AALA20071894 1 20071008 A 3350 1317 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 JFK - EMERGENCY LIGHT AT OVERHEAD SEAT 6B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 6B. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007101900038 20071019 00038 2007 10 19 TSAA0734055 4 20071005 A 3417 HG480B42 DADC BOEING 737 737282C 13844AU NM NR 2 FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 826AL 23051 NON-ETOPS CARGO FLIGHT 946 HNL-KOA - DURING CLIMB, THE CREW NOTED WARNING FLAGS IN THE FIRST OFFICER’S AIRSPEED INDICATO R, ALTIMETER AND VERTICAL SPEED INDICATOR. THE CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE DIGITAL AIR DATA COMPUTER PER AMM 34-12-11 WITH ALL CHECKS SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERV ICE. 2 L 7 2 4F RT A16WE 2007101900040 20071019 00040 EU 2007 10 19 12112 1 20071010 A 5315 S53672407202 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 FOUND FLOORBEAM 38 IS CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS ALLOWABLE LIMITS. REMOVED AND R EPLACED FLOORBEAM 38 IN ACCORDANCE WITH SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007101900041 20071019 00041 EU 2007 10 19 12113 1 20071010 A 5315 S53672409218 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 FOUND FLOORBEAM 40 IS CORRODED. REMOVED CORROSION AND FOUND TO BE BEYOND MANUFACTURERS LIMITS. REMOVED AND REPLACED FL OORBEAM IN ACCORDANCE WITH SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007101900042 20071019 00042 EU 2007 10 19 12115 1 20071010 A 5347 S5367800120202 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 SEAT TRACK RIGHT INBOARD BETWEEN FRAMES 29 AND 36 CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS LIMI TS. REMOVED AND REPLACED SEAT TRACK IN ACCORDANCE WITH SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007101900043 20071019 00043 EU 2007 10 19 HYIA12116 1 20071010 A 5347 S5367800120102 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 SEAT TRACK RIGHT OUTBOARD BETWEEN FRAMES 29 AND 36 CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS LIM ITS. REMOVED AND REPLACED SEAT TRACK IN ACCORDANCE WITH SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007101900048 20071019 00048 EU 2007 10 19 07FDEA03758 1 20070914 A 5313 20240 STRINGER SPLICE AIRBUS 310 A310222 3930315 EU ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 446FE 224 STGR SPLICE REPAIR BETWEEN FRAME 72/73 ON STGR 56R REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS A CCOMPLISHED USING FAA APPROVED DATA VISUALLY INSPECTED STGR SPLICE REPAIR BETWEEN FRAME 72/73 AT STGR 56 RT AND FOUND MA TERIAL TYPE FOR STGR COUPLING DID NOT CONFORM TO SRM GUIDE LINES. REMOVED AND REPLACED STGR COUPLING IAW A310 SRM 53-10 -14 FIG 201. 2 L 7 2 4F RT A35EU 2007101900050 20071019 00050 NM 2007 10 19 USAA920070911 1 20070930 A 5320 651768469 ATTACH ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT - MAJOR REPAIR - FPBH INSPECTION, CRACKED STRINGER ATTACH ANGLE, BS 300, S13L. REPLACED STRINGER ATTACH ANGLE BS 30 0, S13L IAW B737-300 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007101900053 20071019 00053 WP 2007 10 19 07FDEA04566 1 20071010 A 5347 S492913012000 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 1360-1364 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 MAIN CABIN, STN 1360 - STN 1364, RBL 46, "SEAT TRACK GOUGED" SCALLOPS ELONGATED CHECKED LIMITS, BLENDOUT AREA IS .510 OU T OF .500 MAX OUT OF LIMITS IAW DC/MD-10 SRM 53-70-00 VOL I PG 21 FIG 5 SHT 1. REMOVED DAMAGED SECTION AND INSTALLED NE W SECTION IAW DC/MD-10 SRM 53-70-00 VOL I PG 3/4 AND DC/MD-10 SRM 51-31-01 VOL II PG 1. MAT ' ID AND FABBED SECTION AND SPLICE HAT AND PLATE IAW DC/MD-10 SRM 53-70-00 VOL I PG 3/4. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01 VOL II PG 1 AND 21. 2 L 7 3 4F A22WE 2007101900054 20071019 00054 NM 2007 10 19 07FDEA04567 1 20071011 A 5347 AEA732515 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1211-1239 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 FOUND UPPER CARGO COMPARTMENT, SEAT TRACK RBL 75 CORRODED AT STA 1211 TO BS 1239. 10-24-07 REPAIR CARRIED OUT AS P ER SRM 53-70-00 FOULME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007101900056 20071019 00056 NM 2007 10 19 SB07086 1 20071006 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 451UW 24934 BDL - MAINTENANCE FOUND MANY CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN T HE AFT GALLEY, UNDER THE CENTER LIGHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007101900058 20071019 00058 NM 2007 10 19 MWEA070241 1 20071007 A 3297 WIRE DOUG MD88 MD88 3023688 NM WARNING SYSTEM CHAFED A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 13 823ME 49766 NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF. FOUND CHAFED WIRE NEAR LOCKED POSITION SENSOR. 2 L 7 2 4F RT A6WE 2007101900059 20071019 00059 2007 10 19 SB07087 4 20071006 A 2565 D37022101 BOTTLE AIRCRUISERS BOEING 737 7374B7 1384702 NM EVAC SLIDE LOW PRESSURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 453UW 01079 24980 CLT - MAINTENANCE REPORTED THE FORWARD LEFT ENTRY DOOR EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE LOW. MAINTENANCE REMOVED AND REPLACED THE FORWARD LEFT ENTRY DOOR EMERGENCY ESCAPE SLIDE PER MM 25-61-32. 2 L 7 2 4F RT A16WE 2007101900062 20071019 00062 NM 2007 10 19 MWEA070242 1 20071009 A 7830 7150922505 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 907ME 55171 LEFT THRUST REVERSER LOWER DEFLECTOR DOOR Z-FRAME CRACK. INSTALLED REPAIR ANGLE. 2 L 7 2 4F TR A6WE 2007101900063 20071019 00063 2007 10 19 F3LA200700278 4 20071009 A 2565 GIRT BAR AIRBUS A319 A319111 3930336 NM ESCAPE SLIDE MALFUNCTIONED A F3LA O OTHER O OTHER CR CRUISE 1 NM 03 922FR 2012 FLIGHT CREW REPORTED SLIDE ARMING LEVER ON R2 DOOR POPPED OUT DURING FLIGHT (1") AND CANNOT PUSH IT IN. REPACKED GIRT B AR ASSEMBLY AND PERFORMED ADJUSTMENT TEST OF THE RELEASE MECHANISM OF THE EMERGENCY ESCAPE SLIDE. PERFORMED OPS CHECK A ND INDICATIONS NORMAL. REF A319-11 AMM 52-13-22-820-001. 2 L 7 2 4F RT A28NM 2007101900064 20071019 00064 NM 2007 10 19 MWEA070243 1 20071009 A 7830 7150922505 FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 907ME 55171 LEFT THRUST REVERSER UPPER DEFLECTOR DOOR Z-FRAME CRACKED. INSTALLED REPAIR ANGLE. 2 L 7 2 4F TR A6WE 2007101900065 20071019 00065 EA 2007 10 19 QXEA200701538 1 20071010 A 4920 4157T43P01 SHUTOFF VALVE CNDAIR CL600 CL6002C10 1390015 EA APU MALFUNCTIONED A QXEA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 NM 09 613QX 10045 PDX - ON FLIGHT 2557, ON TAKEOFF RECEIVED A MASTER WARNING FOR SMOKE COMING FROM THE AFT LAVATORY. FLIGHT ATTENDANT NOT ICED "HAZE" UPON OPENING LAV DOOR. AFTER A FEW MINUTES HAZE DISAPPEARED. RETURNED TO GATE. MAINTENANCE PERFORMED GVI OF ENGS NR 1, NR 2, AND APU FOR SIGNS OF OIL LEAKAGE. FOUND OIL IN NR 2 ENG 4TH STAGE AND AFT. REPLACED 4TH STAGE SOV ON NR 2 ENG. REMOVED AND REINSTALLED NR 2 SEAL PRESSURE REGULATOR VALVE. COMPLIED WITH COMPRESSOR WASH TO GET RID OF R ESIDUAL OIL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007101900067 20071019 00067 EA 2007 10 19 TRAX200701476 1 20071006 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 877AS 7579 CEILING EMERGENCY LIGHT INOP AT SEAT 8AB. 2 L 7 2 4F RT A21EA 2007101900068 20071019 00068 NM 2007 10 19 SB07088 1 20071010 A 3260 CONDUIT BOEING 737 737301 1384611 NM NLG OUT OF POSITION A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 591US 23936 CMH FLT 1456 AFTER TAKEOFF FROM CMH, EN ROUTE TO DCA, CREW RECEIVED A RED NLG UNSAFE LIGHT UPON GEAR RETRACTION. CREW FOLLOWED QRH PROCEDURES, EXTENDED GEAR AND RECEIVED NORMAL GEAR INDICATION OF THREE GREEN LIGHTS. FLIGHT RETURNED TO FI ELD AT CMH AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REPOSITIONED NOSE LANDING GEAR LOCK SENSOR CONDUIT TO GAIN CLEARANCE WHEN GEAR RETRACTED. SWUNG GEAR SEVERAL TIMES. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007101900070 20071019 00070 NM 2007 10 19 QXEA200701532 1 20071006 A 2160 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM CABIN HEAT ILLUMINATED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 429QX 4161 GEG - ON FLIGHT 2392, CABIN DUCT HOT CAUTION ILLUMINATED AT 3000' INTO CLIMB. AFTER RUNNING EMERGENCY CHECKLIST HAD CON TROL OF HEAT. MAINTENANCE COMPLIED WITH FIM. ECS SYSTEM WORKS NORMAL. NO ASSOCIATED CAUTION LIGHT. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007101900071 20071019 00071 NM 2007 10 19 UPS07M50889 1 20070929 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C CABIN - SEAT TRACK AT STA 842 - 909, X=8.5 AFTER CLEANING FOUND CORROSION AS MARKED. CORROSION ON SEA T TRACK AT STA 842 - 909 X=8.5 RMVED FOUND EXCEEDS LIMITS. CORRODED SEAT TRACK AT STA 850 - 909 REMOVED. REPAIR SEAT T RACK REWORKED AS PER SRM 53-70-00 VOL I FIG 1A REV 38. REPAIR SEAT TRACK FASTENER HOLES PICKED UP, PROTECTED & PAINTED. REPAIR SEAT TRACK INSTALLED AS PER SRM 51-31-01 VOL II REV 38. 2 L 7 3 4F RT A22WE 2007101900073 20071019 00073 WP 2007 10 19 ABXA070328 1 20070919 A 5320 99579113 INTERCOSTAL DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 INTERCOSTAL AT LONGERON 29 LEFT, CRACKED AND BENT FROM STA 351 TO STA 370. REMOVED AND REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 2007101900075 20071019 00075 WP 2007 10 19 ABXA070330 1 20070921 A 5220 995773521 ATTACH FITTING DOUG DC9 DC941 302207N WP EMERGENCY EXIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 RIGHT FORWARD EMERGENCY EXIT DOOR LOWER BEAM AFT END ATTACH CLIP WAS CRACKED. REMOVED AND REPLACED CLIP IAW DC9 SRM. 2 L 7 2 4F A6WE 2007101900076 20071019 00076 WP 2007 10 19 ABXA070331 1 20070928 A 5512 5922577507 SKIN DOUG DC9 DC941 302207N WP HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 RIGHT HORIZONTAL STABILIZER UPPER SURFACE WAS CORRODED APPROXIMATELY 30 INCHES OUTBOARD OF THE VERTICAL CAP. REPAIRED A REA IAW DC9 SRM 55-01 FIGURE 2, SHEET 2. 2 L 7 2 4F A6WE 2007101900077 20071019 00077 WP 2007 10 19 ABXA070332 1 20070928 A 5330 5911412115 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 LEFT STATIC PORT SKIN WAS CORRODED ON INSIDE OF FORWARD LOWER CARGO BETWEEN FS 332 AND 351, LONGERON 27 AND 26 LEFT. IN STALLED REPAIR IAW DC9 SRM 53-04, FIGURE 12C. 2 L 7 2 4F A6WE 2007101900078 20071019 00078 WP 2007 10 19 ABXA070333 1 20070917 A 5312 59101303 BULKHEAD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 AFT PRESSURE BULKHEAD CUTOUT LOWER LEFT UNMODIFIED CORNER HAD CRACK OF UNKNOWN LENGTH IN LOWER INBOARD SKIN TAB PORTION OF SKIN. REPAIRED AFT PRESSURE BULKHEAD ON LEFT AND RIGHT LOWER CORNERS IAW DC9 SRM. 2 L 7 2 4F A6WE 2007101900079 20071019 00079 NM 2007 10 19 QXEA200701533 1 20071007 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM STICK PUSHER FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 426QX 4154 PDX-ON FLIGHT 2355, PUSHER SYSTEM FAIL CAUTION LIGHT ON. TAXI OFF THE RUNWAY AFTER LANDING. RAN CHECKLIST, MOMENTARY W HEN TESTING NR 2 STALL WARNING. MAINTENANCE CYCLED POWER AND COMPLIED WITH STICK PUSHER ADJUSTMENT TEST. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007101900081 20071019 00081 WP 2007 10 19 ABXA070326 1 20070919 A 5347 S2914913M24000 SEAT TRACK DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 UPPER CARGO SEAT TRACK CRACKED STA 160 - 200 LEFT BUTT LINE 44. REMOVED AND REPLACED SEAT TRACK FS 160 - 228 LEFT BUTT LINE 44. 2 L 7 2 4F A6WE 2007101900082 20071019 00082 WP 2007 10 19 ABXA070327 1 20070919 A 5240 99115793 BEAM DOUG DC9 DC941 302207N WP SERVICE DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 SERVICE DOOR UPPER BEAM AFT END WAS CRACKED. REPAIRED AREA IAW DC9 SRM 52-05, FIGURE 25. 2 L 7 2 4F A6WE 2007101900084 20071019 00084 WP 2007 10 19 ABXA070334 1 20070918 A 5347 S2914913M24000 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 LEFT BUTT LINE 44 STA 218 TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK STA 160 - 230, LEFT BUTT LINE 44 IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 2007101900086 20071019 00086 WP 2007 10 19 ABXA070336 1 20070918 A 5347 S2914913M24000 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 LEFT BUTT LINE 44 STA 220 TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK LEFT BUTT LINE 44, STA 160 - 230 IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 2007101900087 20071019 00087 NM 2007 10 19 QXEA200701535 1 20071009 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM CABIN PRESSURE FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 429QX 4161 PDX - ON FLIGHT 2464, CABIN PRESSURE FAULT LIGHT ILLUMINATED. COMPLIED WITH EMERGENCY CHECKLIST. PRESSURE IN MANUAL MO DE OK. MAINTENANCE INSPECTED AFT OUTFLOW VALVE. NO DEFECTS NOTED. NO CSC FAULT LIGHT ON PRESSURIZATION CONTROL PANEL. PERFORMED FUNCTIONAL TEST. FUNCTIONAL TEST CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007101900089 20071019 00089 NM 2007 10 19 QXEA200701536 1 20071009 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM STICK PUSHER FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING LD LANDING 1 NM 09 421QX 4149 PDX - ON FLIGHT 2239, AFTER LANDING AND CLEARING RUNWAY, PUSHER SYSTEM FAIL CAUTION LIGHT ILLUMINATED. RAN EMERGENCY CH ECKLIST DIRECTED STALL WARNING TEST WITH NO CHANGE. MAINTENANCE COMPLIED WITH OPERATOR ACTION CYCLED SPM NR 1 AND SPM N R 2 CIRCUIT BREAKERS. LIGHT CLEARED. NO MAINTENANCE ACTION REQUIRED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED . 2 H 7 2 4T RT A13NM 2007101900090 20071019 00090 NM 2007 10 19 2007UALA01804 1 20070604 A 5280 BUSHING AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE MLG DOOR DAMAGED A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 814UA 862 LIGHT AIRFRAME VIBRATION PASSING 320 KIAS AT FL240 ON CLIMB-OUT. VIBS STOPPED AS CREW SLOWED BACK THROUGH 320 KIAS. FO UND WORN ROD ENDS ALLOWING PLAY IN CONTROL SURFACES AND GEAR DOORS. REPLACED WORN ROD ENDS IN LT GREEN ELEVATOR, RT YEL LOW ELEVATOR. ALSO REPLACED LT INBD AND RT OTBD ELEVATOR PCA'S AFTER FAILING FREE PLAY CHECK. REPLACED LT AND RT AFT G EAR DOOR HINGE BUSHINGS AND LOWER ATTACH ARM BUSHINGS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101900092 20071019 00092 NM 2007 10 19 2007UALA03177 1 20070814 A 2150 RELAY BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE A/C ACCESS UNIT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 399UA 24674 RTFL DUE TO PACK PROBLEM. FOUND FAULTY AIR CONDITIONING ACCESSORY UNIT. REPLACED ACCESSORY UNIT. SHOP FINDINGS: FOUND BAD K1 RELAY. REPLACED RELAY. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101900097 20071019 00097 NM 2007 10 19 CHQA200700057 1 20071008 A 3244 299K631 TIRE BOMBDR CL600 CL6002D15 NM GE CF34 CF343B1 NE MLG FAILED A CHQA O OTHER E VIBRATION/BUFFET LD LANDING 1 GL 11 458CA 153 7613 GEE873283 CHS TO IAH - THE AIRCRAFT TOUCHED DOWN SMOOTHLY AND THE INITIAL ROLLOUT WAS NORMAL. AFTER THRUST REVERSER DEPLOYMENT TH E AIRCRAFT COULD BE FELT PULLING TO THE RIGHT. THE FLIGHT CREW CHECKED THE REVERSE INDICATIONS AND BOTH ENGINES WERE OP ERATING NORMALLY AND PROVIDING THE SAME AMOUNT OF THRUST. AT THAT TIME A BUFFET STARTED ON THE RIGHT SIDE OF THE AIRCRA FT. THE AIRCRAFT WAS BROUGHT TO A STOP ON THE HIGHSPEED TAXIWAY. ATC WAS THEN NOTIFIED THAT THERE HAD BEEN A TIRE BLOW OUT ON THE RIGHT MAIN LANDING GEAR. MAINTENANCE CONTROL AND OPERATIONS WERE NOTIFIED AND THE CREW AND PASSENGERS WERE DEPLANED ONTO BUSES. MAINTENANCE REPLACED BOTH RIGHT MAIN TIRES AND THEN INSPECTED THE AIRCRAFT FOR DAMAGE. THE FLAP W 2 L 7 2 4F 4 F RT A21EA E15NE 2007101900100 20071019 00100 NM 2007 10 19 ZZDA2007280 1 20071008 A 5320 VENT BOEING 717 717200 1383700 NM FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 925AT 55079 AFT FUSELAGE RIGHT HAND VENT BOX CRACKED. INSTALLED DOUBLER REPAIR ON RIGHT HAND VENT BOX PER EO 17-5320-2023. 2 L 7 2 4F TR A6WE 2007101900101 20071019 00101 NM 2007 10 19 SWAA075016 1 20071009 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 230WN 34592 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007101900102 20071019 00102 NM 2007 10 19 SWAA075017 1 20071009 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 254WN 32512 EEPLS LENS MISSING AT ROW 5 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007101900107 20071019 00107 NM 2007 10 19 SWAA075029 1 20071009 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 20R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007101900108 20071019 00108 NM 2007 10 19 CHQA200700060 1 20070923 A 3222 16050109 STRUT BOMBDR CL600 CL6002D15 NM GE CF34 CF343B1 NE NLG UNDERSERVICED A CHQA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 GL 11 642BR 16346 7356 GEE872617 IAH TO AEX - UPON GEAR RETRACTION, THE NOSE LANDING GEAR DID NOT RETRACT. THE CREW FOLLOWED THE APPROPRIATE QRH PROCEDU RES AND RETURNED TO LAND AT IAH. AN EMERGENCY WAS DECLARED IN THE EVEN THAT THE NOSE WHEEL STEERING DID NOT WORK AND TH E AIRCRAFT WOULD BECOME DISABLED ON THE RUNWAY. THE AIRCRAFT LANDED WITHOUT INCIDENT AND THE STEERING WORKED PROPERLY. THE AIRCRAFT WAS TAXIED BACK TO THE GATE AND TURNED OVER TO MAINTENANCE. MAINTENANCE PUT THE AIRCRAFT ON JACKS AND THE NOSE STRUT DID NOT FULLY EXTEND WHEN THE WHEELS WERE OFF OF THE GROUND. AFTER THUMPING ON THE NOSE WHEELS THE NOSE STR UT EXTENDED FULLY. WHEN THE AIRCRAFT WAS LOWERED DOWN OFF JACKS THE NOSE STRUT REMAINED FULLY EXTENDED. MAINTENANCE TH 2 L 7 2 4F 4 F RT A21EA E15NE 2007101900109 20071019 00109 EU 2007 10 19 TRBA2007083 1 20071010 A 3350 7012210 LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS INOPERATIVE A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 420AT 420 EMERGENCY LIGHT ON MAIN PAX DOOR INOPERATIVE. REMOVED AND REPLACED LIGHT BULB AND PERFORMED OPERATIONAL CHECK IAW JIC N R 33-50-00. 2 H 7 2 4T RT A53EU 2007101900111 20071019 00111 NM 2007 10 19 AALA20071901 1 20071008 A 2751 18195820 TRANSMITTER BOEING 767 767323 1385205 NM TE FLAP INOPERATIVE A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 21 359AA 24040 DFW INFLIGHT T48/08OCT - ON FINAL APPROACH FLAP DISAGREE LIGHT ILLUMINATED. LANDED DFW WITHOUT INCIDENT. REPLACED AND ADJUSTED NUMBER THREE TRAILING EDGE FLAP TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007101900112 20071019 00112 NM 2007 10 19 AALA20071903 1 20071009 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 649AA 24607 SFO - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 22, 23, 25 AND LEFT EXIT IDENTIFIERS INOPERATIVE. REPLACED BATTERY PACK M7 35 FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 22, 23, 25, AND LEFT EXIT IDENTIFIERS. SYSTEM GROUND CHECKED NORMAL OPERA TION. 2 L 7 2 4F RT A2NM 2007101900113 20071019 00113 WP 2007 10 19 AALA20071902 1 20071008 A 2916 RESERVOIR DOUG DC9 DC982 3022082 WP RT HYD SYSTEM LOW PRESSURE A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 470AA 49600 PHX INFLIGHT T2435/08OCT - LOST RIGHT HYDRAULIC SYSTEM. RIGHT HYDRAULIC PRESSURE LOW AND RUDDER MANUAL LIGHTS ILLUMINAT ED. LANDED PHX WITHOUT INCIDENT. LANDED WITH GEAR DOOR EXTENDED. INSPECTED GEAR DOORS WITH NO DAMAGE NOTED. BLED AIR FROM RIGHT HYDRAULIC RESERVOIR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007101900114 20071019 00114 NM 2007 10 19 SWAA075024 1 20071009 A 5752 6546455 TAB BOEING 737 7373H4 1384600 NM LT AILERON DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED BRDG CHECK, FOUND LEFT WING AILERON TAB DISBONDED AT AFT OUTBOARD CORNER. REPAIRED TAB PER SRM. 2 L 7 2 4F RT A16WE 2007101900115 20071019 00115 NM 2007 10 19 SWAA075023 1 20071009 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 25R. REPAIRED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007101900116 20071019 00116 NM 2007 10 19 SWAA075025 1 20071009 A 5755 6573730 SKIN BOEING 737 7373H4 1384600 NM NR 8 SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING NR 8 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007101900117 20071019 00117 NM 2007 10 19 SWAA075028 1 20071009 A 5754 65C26602 SLAT BOEING 737 737301 1384611 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 2 L/E SLAT CRACKED OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007101900118 20071019 00118 NM 2007 10 19 SWAA075027 1 20071009 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007101900119 20071019 00119 NM 2007 10 19 SWAA075026 1 20071009 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007101900120 20071019 00120 NM 2007 10 19 SWAA075021 1 20071009 A 5523 69223189 ROD BOEING 737 7375H4 138449D NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, LEFT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED INPUT ROD PER MM. 2 L 7 2 4F RT A16WE 2007101900121 20071019 00121 NM 2007 10 19 SWAA075019 1 20071009 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 25R CORRODED AT BS 350. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007101900123 20071019 00123 2007 10 19 MASA200700464 4 20070730 A 2561 P01074201 LIFE VEST CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 654BR 2229 7454 ASH RON HNL. THREE ADULT LIFE VEST AND 1 INFANT LIFE VEST WERE MISSING. MX INSTALLED NEW LIFE VESTS. 2 L 7 2 4F RT A21EA 2007101900124 20071019 00124 SO 2007 10 19 SWIA200718765 1 20071007 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DISCHARGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 232SW 8848 8848 120306 FLT 5473 - AFT EMERGENCY LIGHTS NOT WORKING. REPLACED AFT ELBP. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2007101900130 20071019 00130 EA 2007 10 19 MASA200700466 1 20070730 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 650ML 7137 ASH 7222 PHX. AFT EXTERIOR EMERGENCY LIGHT ON LEFT SIDE INOP. MX RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2007101900131 20071019 00131 EA 2007 10 19 SWIA200718770 1 20070802 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 907SW 7511 PAX DOOR FORWARD AND AFT WEB IS CRACKED, FOUND AT C-CHECK. INSTALLED WEB REPAIR PARTS PER CRJ200 REO 601R-52-11-702 (RE V A). 2 L 7 2 4F RT A21EA 2007101900132 20071019 00132 EA 2007 10 19 SWIA200718771 1 20070802 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 907SW 7511 RIGHT ENGINE THRUST FITTING IS CORRODED, FOUND AT C-CHECK. REPLACED ENGINE THRUST FITTING PER CRJ200 AMM 71-22-01-400-8 01. 2 L 7 2 4F RT A21EA 2007101900135 20071019 00135 EA 2007 10 19 SWIA200718774 1 20070802 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 907SW 7511 FRAME BELOW RIGHT MAIN GEAR UPLOCK ACTUATOR IS DAMAGED FROM DOOR ROD, FOUND AT C-CHECK. PERFORMED REPAIR PER REO 601R-5 3-41-568. 2 L 7 2 4F RT A21EA 2007101900137 20071019 00137 NM 2007 10 19 NWAA073446306 1 20071011 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 666US 23821 DURING LINE CHECK, FOUND UPPER DECK LT EMERGENCY DOOR BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK PER AMM 52-23-14. 2 L 7 4 4F RT A20WE 2007101900138 20071019 00138 NM 2007 10 19 DHLA200700052 1 20071010 A 2120 UNKNOWN BOEING 727 727224 1384076 NM CABIN ODOR A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 05 745DH 20665 INTERMITTENT BURNING ELECTRICAL ODOR DETECTED BOTH INFLIGHT AND AFTER LANDING. VISUALLY INSPECTED COCKPIT, E/E BAY AND FWD RADAR BAY AREA AND NO DEFECTS OR ODORS NOTED. ALL LIGHTS AND INSTRUMENTS WORKING NORMAL. CHECKS MADE WITH PACKS ON AND OFF. UNABLE TO DUPLICATE. 2 L 7 3 4F A3WE 2007101900139 20071019 00139 WP 2007 10 19 07FDEA04570 1 20071011 A 5347 ABA7684507 SEAT TRACK DOUG DC10 DC1010F 3022111 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 CORROSION ON SEAT TRACK BETWEEN STA 420 TO STA 448 RBL 27 REMOVED AND REPLACED SEAT TRACK ABA7684-507, STA 421.5 TO STA 484.7, RBL 27.5, IN REF TO DC10/MD10 SRM 51-33-01 VOL II PG 1. 2 L 7 3 4F A22WE 2007101900141 20071019 00141 NM 2007 10 19 07FDEA04572 1 20071011 A 5753 SKIN DOUG MD11 MD11F 3023600 NM LT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 620FE 48791 LT WING INBOARD FLAP LOWER SURFACE FOUND DENTED. 10-29-07 REPAIR CARRIED OUT AT LT WING INBOARD FLAP LOWER SURFACE AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007101900142 20071019 00142 WP 2007 10 19 07FDEA04573 1 20071012 A 5311 AFA00303 FRAME DOUG DC10 DC1010 3022110 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 DURING MD10 ACF MODIFICATION, FOUND CRACK 4,5" LONG ON THE FRAME AT STA 1781 TO STRINGER 13 LT PERFORMED REPAIR FOR SRM VOL I 53-30-00 FIG 5. 2 L 7 3 4F A22WE 2007101900143 20071019 00143 WP 2007 10 19 07FDEA04574 1 20071012 A 5311 AFA003121 FRAME DOUG DC10 DC1010 3022110 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 DURING MD10 ACF MODIFICATION, FOUND CRACK 4.5" LONG ON THE FRAME AT STA 1801 TO NEXT STR 13 RT SIDE AND 2 RIVET MISSING ON THE SPLICE FO. PERFORMED REPAIR FOR SRM 53-30-00 FIG 5 VOL I. INSTALLED RIVETS FOR SRM 51-35-01. 2 L 7 3 4F A22WE 2007101900144 20071019 00144 WP 2007 10 19 07FDEA04575 1 20071012 A 5720 ARC04624 INTERCOSTAL DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 MD10 TO ACF MODIFICATION FOUND RT WING TRAILING EDGE LOWER SIDE STA XORS 241 ABOUT INTERCOSTAL WITH CRACK. REPLACED INT ERCOSTAL FOR SRM 51-35-01. 2 L 7 3 4F A22WE 2007101900147 20071019 00147 NM 2007 10 19 HALA0700445 1 20071010 A 2697 WIRE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE OVERHEAT DETECT SHORTED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 598HA 23278 ETOPS SIGNIFICANT SYSTEM, STATUS MSG LEFT ENG OH LP2 DISPLAYED. T/S AND FOUND WIRES SHORTED TO THE UPPER FWD OVHT DETEC TOR W314-458R-16 AND W314-457R-16. PERFORMED TYPLICAL TEMP REPAIR IAW BOEING STANDARD WIRING PRACTICE MANUAL 20-10-13. OPS CK IAW M/M 26-11-00. OK FOR CONTINUED SERVICE OTHER REF SWPM 20-30-12. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101900148 20071019 00148 EA 2007 10 19 MASA200700467 1 20070730 A 3350 STRIP CNDAIR CL600 CL6002D24 1390016 EA FUSELAGE MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 906FJ 15006 ASH 2730 COS-PHX. LEFT FWD EMERGENCY EXIT FLOOR LIGHT STRIP MISSING. FERRIED TO PHX WHERE MX INSTALLED STRIP. 2 L 7 2 4F RT A21EA 2007101900151 20071019 00151 EA 2007 10 19 MASA200700476 1 20070803 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 37218 7218 ASH 2750 PHX. REPORTED CENTER AISLE EMERGENCY EXIT LIGHTS AND ONE EXIT SIGN INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2007101900156 20071019 00156 EU 2007 10 19 MALA070135 1 20071010 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297-304 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 447XJ 340B447 CORROSION DAMAGE TO LOWER FLANGE AND WEB OF SEAT TRACK FROM STA 297 TO 304, LBL 18.3. REPAIRED PER EO NR S53342 2 L 7 2 4T RT A52EU 2007101900157 20071019 00157 EU 2007 10 19 MALA070136 1 20071010 A 5220 SKIN SAAB SF340 340B 7860101 EU EMERGENCY EXIT DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 447XJ 340B447 DENT IN LT OVERWING EMERGENCY EXIT DOOR SKIN, 18 INCHES FROM FWD EDGE, 19 INCHES FROM LWR EDGE. REPAIRED PER EO NR S520 28. 2 L 7 2 4T RT A52EU 2007101900159 20071019 00159 EU 2007 10 19 MALA070138 1 20071010 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 294-302 UNKNOWN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 447XJ 340B447 REPAIRED RT IB SEAT TRACK RAIL AT STA 294 TO 302 RBL 18.3. REPAIRED PER EO NR S53132. 2 L 7 2 4T RT A52EU 2007101900160 20071019 00160 EU 2007 10 19 MALA070139 1 20071010 A 5320 WEB SAAB SF340 340B 7860101 EU GALLEY CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 447XJ 340B447 LT AFT CORNER OF AFT GALLEY WEB CHAFED FROM AIRSTAIRS. REPAIRED CHAFING ON WEB IAW SAAB EO NR S53362. 2 L 7 2 4T RT A52EU 2007101900161 20071019 00161 EU 2007 10 19 MALA070142 1 20071010 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 350-363 CANNING A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 447XJ 340B447 REPAIR OF FUSELAGE SKIN STA 350-363, SL 1515-1517 DUE TO OIL CANNING DENT. REPAIRED PER EO NR S53009. 2 L 7 2 4T RT A52EU 2007101900164 20071019 00164 EU 2007 10 19 MALA070145 1 20071010 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 134 CANNING A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 447XJ 340B447 DENT IN RT NOSE SKIN AT STA134 ON WL79 IS ALSO OIL CANNING. INSTALLED DOUBLER IAW EO NR S53484. 2 L 7 2 4T RT A52EU 2007101900166 20071019 00166 WP 2007 10 19 NWAA073459961 1 20071011 A 2131 CONTROLLER DOUG DC9 DC931 3022065 WP CABIN PRESSURE MALFUNCTIONED A NWAA B EMER. DESCENT O OTHER CR CRUISE 1 GL 01 924RW 4629 4629 47185 FLIGHT CREW REQUIRED TO PERFORM AN EMERGENCY DESCENT DUE TO LOSS OF CABIN PRESSURIZATION. AIRCRAFT WAS DESCENDED FROM F L350 TO FL310 WHEN THE RED "CABIN PRESS" WARNING LIGHT CAME ON AND CABIN CLIMBING AT 500 FPM. THE CREW WAS ABLE TO MANU ALLY CLOSE THE OUTFLOW VALVE AND EVENTUALLY REGAINED CONTROL OF THE PRESSURE SYSTEM. CABIN PRESSURE WAS STABLE FOR THE REST OF THE FLIGHT AT FL310, INCLUDING AN UNEVENTFUL LANDING AT MSP. MAINTENANCE DID PERFORM BITE AND REPLACED A FAULTE D NR 2 PRESSURE CONTROLLER. SYSTEM CHECK INCLUDED BITE OF PRESSURE CONTROLLERS AND A VISUAL INSPECTION FOR VESSEL LEAKS AND DUCT LEAKS. NO TROUBLE WAS FOUND AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007101900167 20071019 00167 SW 2007 10 19 WGEA200700014 1 20071011 A 3233 EM411511 ACTUATOR ECLIPS EA500 ECLIPSEEA500 3350000 SW ZONE 700 FAILED E WGEA A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 EA 27 135DJ 54 000036 LANDED WITH LANDING GEAR FAIL CAS. RIGHT MAIN GEAR NOT DOWN AND LOCKED. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR A CTUATOR, OPS CHECK GOOD IAW EA500 AMM 32-30-20. 1 L 7 2 4J RT A00002AC 2007101900168 20071019 00168 EA 2007 10 19 MASA200700479 1 20070803 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 77278 7278 ASH 2946 PHX-MEM. PILOT REPORTED THE CEILING LEVEL EMERGENCY FLOODLIGHT ROW 5 WAS INOP. MX RELAMPED AND OPS WERE NORMA L. 2 L 7 2 4F RT A21EA 2007101900169 20071019 00169 NM 2007 10 19 USAA920070914 1 20071004 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916UW 22192 PIT - MAJOR REPAIR - C-4 CHECK, CORROSION ON INTERCOSTAL, BS 640. REPLACED INTERCOSTAL, BS 640 IAW B757 SRM 53-00-51 AN D 51-70-12. 2 L 7 2 4F RT A2NM 2007101900170 20071019 00170 EU 2007 10 19 DHLA200700053 1 20071012 A 2910 HYDRAULIC SYSTEM AIRBUS 300 A300B4203 3930306 EU BRAKES CONTAMINATED A DHLA O OTHER O OTHER LD LANDING 1 GL 05 362DH 084 WITH ANTI-SKID IN ON /ALT THE LEFT BRAKES GRAB AND PULL AIRCRAFT TO THE LEFT. BLED BRAKING SYS GREEN AND YELLOW AND OPS CK NORMAL PER MM 32-42-00. 2 L 7 2 4F RT A35EU 2007101900172 20071019 00172 EU 2007 10 19 TRBA200784 1 20071013 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHTS FAILED A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 541AT 541 F/A COULD NOT OPERATE ALL CABIN EMERGENCY LIGHTS USING AFT EMERGENCY LIGHTS PUSH BUTTON. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK FIN NR 62WL IAW JIC NR 33-51-20. 2 H 7 2 4T RT A53EU 2007101900179 20071019 00179 SO 2007 10 19 SIMA200728805 1 20071012 A 2750 FLAP SYSTEM EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A SIMA O OTHER O OTHER AP APPROACH 1 SW 21 671AE 145793 FLAP EXTENDED ABOVE AIRSPEED LIMITATION ON APPROACH AND IMMEDIATELY SELECTED FLAPS 22. COMPLIED WITH AE MTX WORK CARD 05-200-06 FLAP EXCEEDANCE CONDITION INSPECTION. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007101900180 20071019 00180 2007 10 19 SIAM200728806 4 20071011 A 3140 7013348948 DAU EMB 145 EMB145LR 3260212 SO NR 2 MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 697AB 14500875 ABORTED TAKEOFF DUE TO DAU 2 FAIL SELF CLEARED AFTER MOVING THRUST LEVERS TO IDLE. REMOVED AND REPLACED NR 2 DAU IAW EM B 145 AMM 31-41-01. OPS CHECK GOOD. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007101900183 20071019 00183 NM 2007 10 19 KCSA071463 1 20071010 A 5330 SKIN BOEING 747 7472B4B 138481B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA 2040 TO 2060 AT STR 44R TO 46R SKIN DAMAGED. 2 L 7 4 4F RT A20WE 2007101900184 20071019 00184 EU 2007 10 19 YENA2007091 1 20071005 A 2131 2079102AB CONTROLLER AIRBUS 320 A320232 3930326 EU CABIN PRESSURE MALFUNCTIONED A YENA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 15 652JB 23672 62 3029 CABIN PRESSURE EXCEEDS CAB ALT ECAM AT FLT LEVEL 340. TROUBLESHOT ITEM PER FIM, FOUND NR 1 CPC AT FAULT. REMOVED AND R EPLACED CPC IAW AMM 21-31-34-04, ALL TESTS OK NR 1 & 2 SYSTEMS, CHECK GOOD. 2 L 7 2 4F RT A28NM 2007101900185 20071019 00185 NM 2007 10 19 HNAA0700233 1 20070704 A 5320 85320686101 THRESHOLD DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 940HA 156 PASSENGER DOOR THRESHOLD WAS FOUND CORRODED. PASSENGER DOOR THRESHOLD WAS REPLACED WITH NEW PART IAW 51-40-00. 2 H 7 2 4T RT A13NM 2007101900186 20071019 00186 NM 2007 10 19 0700565 1 20071010 A 3350 D71702030 BATTERY PACK BOEING 737 737924 13848A1 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 30401 30118 EMERGENCY LIGHTS INOP IN FIRST CLASS AND L1 + R1 EXITS. INSTALLED 2 NEW BATTERY PACKS PER MM 33-51-00, 33-51-06. 2 L 7 2 4F RT A16WE 2007101900187 20071019 00187 2007 10 19 0700566 4 20071009 A 2330 RDAV980301 VIDEO MONITOR BOEING 757 757224 1384958 NM CABIN MALFUNCTIONED A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 12114 27556 SMOKE COMING FROM VIDEO SCREEN 7ABC & 8ABC SYSTEM. SHUT OFF, C/B PULLED AND SMOKE STOPPED. REPLACED VIDEO SCREEN 7ABC. VIDEO SCREEN 8ABC OPS CHECK NORMAL. 2 L 7 2 4F RT A2NM 2007101900189 20071019 00189 NM 2007 10 19 0700568 1 20071008 A 5311 652072275 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14325 23455 UPPER FRAME SECTION STA 440 STR 17R-14R HAS CRACK AT FASTENER HOLE. REPLACED UPPER FRAME AT STA 440 IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007101900190 20071019 00190 NM 2007 10 19 0700569 1 20071009 A 5310 65479592 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14325 23455 C-2 DOOR CUTOUT FWD FRAME HAS CRACK. REPLACED FWD FRAME PER SRM 51-40-02 BOEING DRAWING 65-47959. 2 L 7 2 4F RT A16WE 2007101900195 20071019 00195 SO 2007 10 19 SIMA200728804 1 20071010 A 5270 WARNING MESSAGE EMB 145 EMB145LR 3260212 SO CARGO DOOR ILLUMINATED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 659AE 145762 SHORTLY AFTER TAKE OFF CREW GOT A BAGGAGE DOOR WARNING. CREW CHOOSE TO RETURN TO CLT. ISSUED MEL 52-05 IN CLT. 2 L 7 2 4T RT T00011AT 2007101900196 20071019 00196 NM 2007 10 19 0700573 1 20071010 A 5310 652072270 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14325 23455 C-1 DOOR CUTOUT FED FRAME CRACKED AT LWR STOP PAD MOUNT. REMOVED AND REPLACED PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007101900197 20071019 00197 NM 2007 10 19 0700574 1 20071011 A 5310 6520723U54 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14334 23572 FWD CARGO DOOR CUTOUT AFT FRAME CRACKED. REPLACED FRAME PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007101900202 20071019 00202 EU 2007 10 19 TRAX200701479 1 20070927 A 5312 BULKHEAD AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 FWD PRESSURE BULKHEAD AT LBL 10 LWR AREA, FITTING CORROSION FOUND (0.125 INCH) ON WEB. 2 H 7 2 4T RT 2007101900203 20071019 00203 EU 2007 10 19 TRAX200701480 1 20071002 A 5753 BRACKET AEROSP ATR72 ATR72 EU T/E FLAP BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 ON RIGHT WING O/B FLAP ARM AT RIB 13, 1 OMEGA BRACKET BROKEN OFF TO BE FABRICATED. 2 H 7 2 4T RT 2007101900204 20071019 00204 EA 2007 10 19 TRAX200701481 1 20071005 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 876AS 7576 AAR - 8051 - *REWORK* CREW ESCAPE HATCH REQUIRES PLACARD REPLACEMENT AND REPAINTING DO TO PLACARD DAMAGE. 2 L 7 2 4F RT A21EA 2007101900205 20071019 00205 EA 2007 10 19 TRAX200701482 1 20071007 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 713EV 10081 CAPTAIN FLASHLIGHT NOT WORKING. 2 L 7 2 4F RT A21EA 2007101900206 20071019 00206 NM 2007 10 19 WRLA2007106 1 20071008 A 5730 APB74411 SKIN DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE WING CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 273WA 48519 DURING 4C+12A CHECK, SEVERAL CORROSION AREAS WERE FOUND ON CENTER WING TANK UPPER SKIN AT XCW=-110 TO XCW=-106 BETWEEN S -15 TO S-22 AND STA XCW=107 BETWEEN S-18 TO S-15. 10-29-07 REPAIRED PER EGAT ENGINEERING INSTRUCTION W2007A57B-638 R EV.00. 2 L 7 3 4F 4 F RT A22WE E24NE 2007101900208 20071019 00208 NM 2007 10 19 WRLA2007108 1 20071008 A 5313 1D0545D LONGERON DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 273WA 48519 DURING 4C+12A CHECK, LONGERON CORROSION FOUND AT STA 1953 L44R. 10-26-07 REPAIRED THE DAMAGED AREA PER MD11 SRM 53 -10-00 VOL.I REV.40 2 L 7 3 4F 4 F RT A22WE E24NE 2007101900210 20071019 00210 EA 2007 10 19 MASA200700316 1 20070609 A 5210 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7264V 7264 ASH 2878 PHX. PAX DOOR WILL NOT OPEN. MX CYCLED DOOR MULTIPLE TIMES WITH NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007101900211 20071019 00211 EA 2007 10 19 MASA200700397 1 20070708 A 5210 BRACKET CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LOOSE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 17337 7337 PHX 2728 PHX. MAIN CABIN DOOR SUPPORT WHEEL LOOSE. MX CHANGED WHEEL BRACKET. 2 L 7 2 4F RT A21EA 2007101900213 20071019 00213 EA 2007 10 19 MASA200700430 1 20070716 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF ADJUST A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 37228 7228 ASH 2781 PHX. MAIN CABIN DOOR HARD TO OPEN. ADJUST DOOR. 2 L 7 2 4F RT A21EA 2007101900214 20071019 00214 EA 2007 10 19 MASA200700436 1 20070717 A 5210 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17337 7337 ASH 2932 LAS. CAPT REPORTS THE MAIN CABIN DOOR WILL NOT OPEN. CREW MOVED THE AIRCRAFT APPROX 10 FEET FORWARD PRIOR TO MAINT ARRIVING. MX OPENED THE MAIN CABIN DOOR FROM INSIDE AND OUTSIDE WITHOUT PROBLEM. 2 L 7 2 4F RT A21EA 2007101900215 20071019 00215 EA 2007 10 19 MASA200700435 1 20070717 A 5210 SPRING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DEFECTIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37228 7228 ASH 2985 PHX. MAIN CABIN DOOR HARD TO OPEN. REPLACED COUNTER BAL SPRINGS AND CAM FITTNGS AND RIGGED DOOR. 2 L 7 2 4F RT A21EA 2007101900216 20071019 00216 EA 2007 10 19 MASA200700437 1 20070718 A 5210 FASTENER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LOOSE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 17337 7337 ASH 2765 PHX. MAIN CABIN DOOR DIFFICULT TO OPEN. MX SECURED PASSENGER DOOR PRESSURE VALVE ACTUATING ROD HARDWARE. NO FURTHER DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007101900221 20071019 00221 EA 2007 10 19 MASA200700519 1 20070823 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 97325 7325 ASH 2944 PHX. CREW REPORTED THE PAX DOOR STUCK CLOSED. MAINTENANCE ARRIVED AND THE DOOR OPENED NORMALLY. MX LUBED THE DOOR. PAX DOOR OPERATES NORMALLY. 2 L 7 2 4F RT A21EA 2007101700164 20071017 00164 NM 2007 10 17 QXEA200701531 1 20071009 A 2120 UNKNOWN DHAV DHC8 DHC8202 2809007 NM CABIN ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 365PH 526 PDX - DURING STARTUP, AFTER BLEEDS ON SMOKE IN CABIN FLIGHT DECK. COMPLIED WITH ISOLATION IAW PW123 EMM 72-00-01, FIGUR E 119. PERFORMED DH8-SL-21-027 FOR ECS CONTAMINATION. SMOKE/OIL ODOR DID NOT REOCCUR. OPERATIONAL CHECK GOOD. NO PAR TS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007101700165 20071017 00165 EA 2007 10 17 CHQA20070052 1 20071004 A 3250 16735109 RVDT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NLG STEERING FAILED A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 642BR 1660 7356 GEE872617 SDF TO IAH. DURING CRUISE FLIGHT CREW RECEIVED A "STEERING INOP" CAS MESSAGE. CREW RAN APPROPRIATE CHECKLIST AND SPOKE TO DISPATCH AND MAINTENANCE CONTROL ABOUT THE SITUATION. IAH OPERATIONS WAS CONTACTED TO HAVE A TUG STANDING-BY NEAR T HE RUNWAY IF A TOW BACK TO GATE WAS REQUIRED. ATC WAS INFORMED OF THE SITUATION AND THE LONGEST AVAILABLE RUNWAY WAS RE QUESTED, BUT THAT THERE WAS NO NEED TO DECLARE AND EMERGENCY. ATC APPROVED RUNWAY 27 AND DECLARED AN EMERGENCY FOR THE CREW. PASSENGERS WERE BRIEFED OF THE SITUATION. THE AIRCRAFT LANDED WITHOUT INCIDENT AND WAS ABLE TO TAXI CLEAR OF THE RUNWAY. THE AIRCRAFT WAS TOWED BACK TO GATE TO PREVENT ANY POSSIBLE FURTHER DAMAGE OR PROBLEMS ASSOCIATED WITH TAXING 2 L 7 2 4F 4 F RT A21EA E15NE 2007101700179 20071017 00179 2007 10 17 07FDEA04552 4 20071010 A 3418 2566A21 VANE BOEING 727 727233 138408A NM FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 265FE 4147 4147 21671 CAPT'S STICK SHAKER WENT OFF. A/C WAS PROPERLY CONFIGURED FOR T/O. PULL C/B. REMOVED AND REPLACED AOA VANE. VANE OPS CKS GOOD, REF B727-200MM, RPT BY: 437820. PERFORMED OPS CK OF EGPWS AND FOUND AOA VANE FAULT FOR LAST FLIGHT LEG. PUL LED LEVER LATCH C/B WHILE AOA VANE WAS IN FAIRED POSITION AND STICK SHAKER GOES OFF IMMEDIATELY. REMOVED AND REPLACED A OA VANE. VANE OPS CKS GOOD REF B727-200MM SEC 34-18-051-4. ALSO, CHANGED STICK SHAKER MODULE AS A PRECAUTIONARY MEASUR E. STICK SHAKER SYSTEM, OPS CHECKS GOOD, REF B727-200MM SEC 34-18-001-5 AND 34-18-041-4. 2 L 7 3 4F RT A3WE 2007101700181 20071017 00181 EU 2007 10 17 07FDEA04556 1 20071010 A 5347 A5327400584 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 670FE 777 MAIN CARGO DECK SEAT TRACK FROM FR 73 TO FR 78, LBL 15 HAS CORROSION IN 8 AREAS REMOVED. FABRICATED AND REPLACED SEAT T RACK IAW 53-10-16. 2 L 7 2 4F RT A35EU 2007101700185 20071017 00185 NM 2007 10 17 07FDEA04560 1 20071010 A 5347 FX511002N566 SEAT TRACK BOEING 757 7572B7 1384964 NM ZONE 200 MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 FS 377-440, LBL 24.75, SEAT TRACK REPLACED PER CUSTOMER REQUEST. REMOVED SEAT TRACK ASSY AT FS 377-440, LBL 24.75 IAW S RM 51-40-02. FABRICATED NEW SEAT TRACK ASSY ON MAE FAB SHOP TRAVELER NR T7/704366 AND SRM 51-10-02. PART NUMBER OF FAB RICATED SEAT TRACK ASSY IS FX-51-10-02-N566. LOCATED AND DRILLED, FABRICATED SEAT TRACK ASSY IAW SRM 51-40-02. TREATED AND PRIMED SEAT TRACK ASSY IAW SRM 51-20-02. INSTALLED SEAT TRACK ASSY IAW SRM 51-40-02, CENTER ROW ONLY. RCB MODIFIC ATION WORK CARD NR 118350472RCB WILL INSTALL REMAINDER OF FASTENERS IN THE FLANGES OF THE SEAT TRACK AS THAT MOD PROGRES SES. 2 L 7 2 4F RT A2NM 2007101700188 20071017 00188 EA 2007 10 17 MASA200700459 1 20070728 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA ROW 12 INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH 2864 PHX. EMERGENCY PATH LIGHTING AT ROW 12 D/F INOP. MX REMOVED AND REPLACED PATH STRIP. 2 L 7 2 4F RT A21EA 2007101700192 20071017 00192 NM 2007 10 17 NOCA15307 1 20071005 A 3397 CONNECTOR BOEING 767 767304 NM EMERGENCY LIGHTS DISCONNECTED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 769NA 28039 E-PATH FLOOR LIGHTING STRIP INOP AT SEAT AREA 2AB. RE-INSTALLED CONNECTOR TO E-PATH FLOOR LIGHTING STRIP. E-PATH LIGHT S OPS CHECKS NORMAL AS PER AMM 33-51-10. 2 L 7 2 4F RT A1NM 2007101700207 20071017 00207 WP 2007 10 17 ASAA0782067 1 20071005 A 5321 99365465 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 160-200 BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 CABIN FLOOR PANEL CRACKED WITH DAMAGED INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007101700210 20071017 00210 WP 2007 10 17 ASAA0782070 1 20071005 A 5321 993653917 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 148-160 BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 CABIN FLOOR PANEL HAS BROKEN INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007101700220 20071017 00220 WP 2007 10 17 ASAA0782081 1 20071005 A 5320 993061267 CUSP WEB DOUG DC9 DC983 3022083 WP BS 1297-1301 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 CUSP WEB CRACKED. STOP DRILLED CRACK. INSTALLED REPAIR PARTS PER SRM 53-05. 2 L 7 2 4F RT A6WE 2007101700224 20071017 00224 SO 2007 10 17 SIMA200727407 1 20070928 A 3220 11700000008 LANDING GEAR EMB 135 EMB135KL 3260302 SO NOSE DAMAGED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 807AE 145506 AT ROTATION AND LIFT OFF GEAR WOULD NOT RETRACT AT THE SAME TIME GOT EICAS MESSAGE OF 'AIR GROUND FAILED'. RETURNED TO SFO AND MADE FLAPS 45 LANDING AT 0-50FPM SINC RATE AND 38270 POUND GROSS WEIGHT. SFP TO LAX. REMOVED AND REPLACED NOSE LANDING GEAR IAW EMB MM 32-20-01 OPS CHECK GOOD AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT T00011AT 2007101700225 20071017 00225 CE 2007 10 17 DXTA200702514 1 20071001 A 3040 85611 CONTROL UNIT CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE WINDSHIELD HEAT INOPERATIVE E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 667QS 2 5605365 RT WINDSHIELD FAULT LIGHT COMES ON AS SOON AS THE POWER LEVERS ARE FORWARD TO ABOUT 80 PERCENT. LIGHT GOES AWAY AT POWE R IDLE. ABORTED T/O. REPLACED R/H WINDSHIELD TEMP. CONTROL UNIT IAW CE 560XL MM CH - 24-20-01. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007101700226 20071017 00226 NM 2007 10 17 DXTA200702515 1 20071001 A 3240 BRAKE ASSY AMD FALC50 FALCON2000 2730170 NM MLG INTERMITTENT E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 223QS 86 AIRPLANE BRAKES WORKING INTERMITENTLY. POWERED UP AIRCRAFT AND INTERROGATED CMC. NO FAULTS FOUND FOR BRAKE SYSTEM OR C AS MESSAGE PRESENT. PERFORMED BRAKE PRESSURE CHECKS ON SYSTEM 1 AND 2. NO DEFECTS NOTED. BLED BOTH BRAKE SYSTEM. BRAKE S YSTEM OPS CHECK GOOD. WORK PERFORMED PER F2000 EX M/M 34-412, 32-414, 32-415, 32-419 & 32-446 2 L 7 2 4F RT A50NM 2007101700227 20071017 00227 CE 2007 10 17 DXTA200702516 1 20071001 A 3246 315381 WHEEL CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG OUT OF BALANCE E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 924QS 189 189 7500124 DURING TAKE OFF ROLL AT APPROXIMATELY 60 KIAS THE NOSE WHEEL SHOOK VIOLENTLY. DUST WAS COMING OUT OF THE HEAD LINER. AB ORTED T/O. REMOVED AND REPLACED BOTH NOSE WHEEL ASSY, IAW CESSNA 750 M/M 32-41-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007101700228 20071017 00228 CE 2007 10 17 DXTA200702517 1 20071001 A 2750 FLAP SYSTEM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS MALFUNCTIONED E DXTA O OTHER F FLT CONT AFFECTED LD LANDING 1 GL 07 932QS 7500032 FLAPS WOULD NOT EXTENDED IN FLIGHT, PRESSING FLAPS RESET BUTTON & PULLING FLAP CONTROL CB DID NOT FIX THE PROBLEM. PERF ORMED AN OPERATIONAL CHECK OF THE FLAP SLAT SYSTEMS SEVERAL TIMES FROM THE FULL DEPLOY TO THE FULL STOW POSITIONS. FOUN D THE FLAPS & SLATS FOLLOWED THE INDICATIONS IN THE COCKPIT AS REQUIRED. PULLED SLAT A & SLAT B CB'S INDEPENDANTLY & MOV ED HANDLE & SLAT FAIL CAS MESSAGE ANNUNCIATOR AS REQUIRED. RESET CB'S & SYSTEM FUNCTIONED AS REQUIRED W/NO DEFECTS NOTED . ALL WORK PERFORMED IAW CE750 MM 27-50-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007101700229 20071017 00229 EA 2007 10 17 TRAX200701425 1 20070927 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 855AS 7395 ON REAR PRESSURE BULKHEAD AR FS 621.00 RBL 36 MOUNT ISOLATOR BRACKET FOUND CRACKED. REPLACE ON REAR PRESSURE BULKHEAD A T FS 621.00 RBL 36, MOUNT ISOLATOR BRACKET REMOVED AND REPLACED IAW SRM 51-2-13. 2 L 7 2 4F RT A21EA 2007101800016 20071018 00016 NM 2007 10 18 HNAA0700216 1 20070703 A 5751 RIB DHAV DHC8 DHC8102 2809003 NM RT AILERON CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 940HA 156 RIB CRACKED INSIDE RIGHT AILERON APPROX YW 444. RIGHT AILERON RIB AT STA YW 4444 (APPROX) REPLACED AND INSTALLED WITH B LIND RIVETS AS PER THE SRM 51-40-00. REPAIRED SKIN PER SRM 57-60-21. 2 H 7 2 4T RT A13NM 2007101800019 20071018 00019 NM 2007 10 18 07FDEA04535 1 20071009 A 2612 4059027903 COMPUTER DOUG MD11 MD11F 3023600 NM FIRE WARNING MALFUNCTIONED A FDEA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SO 25 624FE 48443 ON 4 MILE FINAL TO RW23L IND, REC'D LVL III "CABIN SMOKE" ALERT. DONNED O2 MASKS, CHECKED AIR SYNOPTIC, SAW ONE DETECTO R MID CARGO CABIN AMBER COLOR. COMPLETED CONFIGURATION FOR LANDING, DECLARED EMERGENCY, LANDED, PERFORMED EMERGENCY SHU TDOWN, EMERG EVACUATION CHECKLISTS AND VACATED A/C VIA PORT SIDE SLIDE. PER CREW DEBRIEF AND FIRE DEPT NO SMOKE IN THE COCKPIT OR CABIN. NR 4 SMOKE DETECTOR (MAIN DECK) SHOWED FAILED ON THE SYNOPTIC PAGE. RANG WIRES SHOOK DOWN WIRES, R& R THE NR 2R SMOKE DETECTOR., MSC AND NR 1 DEU . CK OK DURING TAXIJ CK 2 L 7 3 4F RT A22WE 2007101800023 20071018 00023 EU 2007 10 18 07FDEA04553 1 20071010 A 5313 A5398621700000 STRINGER SPLICE AIRBUS 310 A310222 3930315 EU FUSELAGE MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 AFT PIT STRINGER SPLICE REPAIR AT STRINGER 52L FRAME 59/60 REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPA IR WAS ACCOMPLISHED USING APPROVED DATA. STRINGER COUPLING MATERIAL TYPE AND MATERIAL TEMPER DID NOT CONFORM TO A310 SR M REQUIREMENTS, REMOVED AND RPLACED STRINGER COUPLING REPAIR IAW A310- 200 SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007101800024 20071018 00024 EU 2007 10 18 07FDEA04554 1 20071010 A 5313 A5399621700000 STRINGER SPLICE AIRBUS 310 A310322 3930334 EU FUSLEAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 451FE 303 AFT PIT STRINGER SPLICE REPAIR AT STRINGER 52L FRAME 60/61 REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPA IR WAS ACCOMPLISHED USING FAA APPROVED DATA. FOUND THAT STGR COUPLING MATERIAL TYPE AND MATERIAL TEMPER DID NOT CONFORM TO A310 SRM REQUIREMENTS, REMOVED AND REPLACED STRINGER COUPLING REPAIR IAW A310 SRM 53- 10-14 FIG 201 2 L 7 2 4F RT A35EU 2007101800025 20071018 00025 EU 2007 10 18 TRAX200701478 1 20070926 A 5310 DOOR FRAME AEROSP ATR72 ATR72 EU CARGO DOORWAY CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 CARGO DOOR FRAME REPAIR CRACKED AT STA 6619.5. CRACK CONFIRMED, REPAIRED WITH DOUBLE. REPAIRED INTERCOSTAL ON CARGO DOOR PER EC EO 72-52-0107. 2 H 7 2 4T RT 2007101900011 20071019 00011 EU 2007 10 19 MALA070125 1 20070924 A 5754 SKIN SAAB SF340 340B 7860101 EU LT TE FLAP DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446XJ 340B446 TWO DENTS IN THE LT FLAP SKIN PANEL WS 192.71. REPAIRED PER EO NR S57060. 2 L 7 2 4T RT A52EU 2007101900013 20071019 00013 NE 2007 10 19 NOCA15207 2 20070915 A 7530 C8E3812 CONTROL UNIT BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E437 54555 NE RT ENGINE MALFUNCTIONED A NOCA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 EA 15 754NA 29381 EGT N2 N3 EXCEEDED LIMITS REJECTED T/O RIGHT ENGINE EGT 889 N2 105 N3 100. PERFORMED FIM 71-05-00 CHECK INLET AND EXHAU ST INSPECTED CHIPS REPLACED BVCU AS PER MM 75-32-01. 2 L 7 2 4F 4 F RT A2NM E12EU 2007101900014 20071019 00014 EU 2007 10 19 MALA070127 1 20070924 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446XJ 340B446 RT FUSELAGE SKIN DENTS BENEATH ICE GUARD PANELS 6, 7, AND 8. REPAIRED PER EO NR S53005. 2 L 7 2 4T RT A52EU 2007101900044 20071019 00044 NM 2007 10 19 NWAA073426301 1 20071002 A 5330 SKIN BOEING 747 747451 1384940 NM BS 2658 S12L DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 661US 23719 DURING "M" CHECK, FOUND FASTENERS SHEARED AND HOLES ELONGATED ON FUSELAGE SKIN AT S12L BS 2658. REPAIRED PER EA 63-2106 88. 2 L 7 4 4F RT A20WE 2007101900046 20071019 00046 NM 2007 10 19 NWAA073406301 1 20070929 A 5312 BULKHEAD BOEING 747 747451 1384940 NM BS 1238 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 661US 23719 DURING "M" CHECK, FOUND CRACKS IN PRESSURE DECK CANTED BULKHEAD AT BS 1238. REPAIRED PER EA 63-210685 SECTION I. SECTI ON II REQUIRES DVI INSPECTIONS TO BE ACCOMPLISHED EVERY 4000 CYCLES. 2 L 7 4 4F RT A20WE 2007101900061 20071019 00061 NM 2007 10 19 QXEA200701537 1 20071010 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 425QX 4039 SEA FLIGHT NR 2431 - FLAP POWER CAUTION LIGHT. TROUBLESHOT FLAP POWER CAUTION REF FIM 27-50-00. CLEARED FLAP NVM. PER FORMED OPERATIONAL TEST OF WING FLAPS IAW Q400 AMM TASK 27-50-00-710-801. NO REOCCURRENCE OF FAULT. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007101900072 20071019 00072 NM 2007 10 19 UPS07M50890 1 20070929 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C CABIN - SEAT TRACK AT STA 775 - 909, X=8.5 AFTER CLEANING FOUND CORROSION AS MARKED. SEAT TRACK CORRO SION AT STA 775 - 909 X=8.5 REMOVED FOUND EXCEEDED LIMITS. CORRODED SEAT TRACK AT STA 785 - 909 REMOVED. REPAIR SEAT T RACK REWORKED PER SRM 53-70-00 VOL I FIG 1A REV 38. REPAIR SEAT TRACK FASTENER HOLES PICKED UP, PROTECTED & PAINTED. R EPAIR SEAT TRACK INSTALLED AT REWORKED AREA AS PER SRM 51-31-01 VOL II REV 38. 2 L 7 3 4F RT A22WE 2007101900104 20071019 00104 NM 2007 10 19 SWAA075015 1 20071009 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 225WN 34333 EEPLS LENS CRACKED AT ROW 3 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007101900122 20071019 00122 NM 2007 10 19 SWAA075020 1 20071009 A 5523 REP4HE8 BEARING BOEING 737 7375H4 138449D NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED INPUT ROD BEARING PER MM. 2 L 7 2 4F RT A16WE 2007101900125 20071019 00125 SO 2007 10 19 SWIA200718766 1 20071002 A 3350 LENS EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS MISSING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 569SW 120344 FLT 3680 - EMERGENCY LIGHT LENS BELOW FA SEAT IS MISSING. INSTALLED NEW LENS. 2 L 7 2 4T RT A31SO 2007101900128 20071019 00128 EA 2007 10 19 SWIA200718768 1 20070802 A 5340 NUT CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 907SW 7511 FOUND AT C-CHECK, FLOORBEAM CLIP AT FS484 LBL36 IS CRACKED. INSTALLED REPAIR ANGLES PER CRJ200 REO 601R 53-41-059 STEPS 8, 11, 12 AND 14. 2 L 7 2 4F RT A21EA 2007101900129 20071019 00129 EA 2007 10 19 SWIA200718769 1 20070802 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 907SW 7511 PAX DOOR FORWARD WEB UPPER CORNER IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS ON PAX DOOR PER REO NO 601R-52-1 1-1299. 2 L 7 2 4F RT A21EA 2007101900140 20071019 00140 NM 2007 10 19 07FDEA04571 1 20071011 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM NLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 620FE 48791 NOSE LANDING GEAR RT TRUNNION FITTING CRACKED. CARRIED OUT REPAIR AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLAS SIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007101900146 20071019 00146 SO 2007 10 19 CHQA200700061 1 20071011 A 2840 INDICATOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUEL QTY MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 11 286SK 145443 CAE311567 CLE TO ATL - DURING CRUISE FROM CLE TO ATL, THE FUEL QUANTITY INDICATION ON THE LEFT TANK WENT FROM ROUGHLY 2200LBS TO A MBER DASHES, AND THE TOTAL QUANTITY DID THE SAME, WITH ASSOCIATED TRIPLE CHIME AND THE EICAS MESSAGE "FUEL 1 LO LEVEL". FOLLOWING THE QRH, A FUEL CROSS FEED WAS INITIATED. SHORTLY AFTER THIS WAS DONE, THE MESSAGE WENT AWAY AND THE INDICA TION FOR THE LEFT TANK CAME BACK TO 2000 LBS. AT THAT TIME THE CREW WAS ATTEMPTING TO CONTACT DISPATCH THROUGH ATL RADI O TO INFORM THEM OF THE SITUATION AND TALK TO MAINTENANCE CONTROL. WHILE ATTEMPTING TO CONTACT DISPATCH THE FUEL INDICA TION WENT TO "0" FOR THE NR 1 TANK WITH A RED BOX AND THE TOTAL FUEL QUANTITY WENT TO RED, SHOWING ONLY WHAT WAS IN THE 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007101900150 20071019 00150 EA 2007 10 19 MASA200700468 1 20070731 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 17156 7156 NR 3 EXTERNAL EMERGENCY LIGHT WAS INOP. MX RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2007101900165 20071019 00165 EA 2007 10 19 MASA200700477 1 20070803 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN UNSECURE A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 7291Z 7291 ASH 2766 LGB. EMERGENCY PATH LIGHTING INOP AT ROWS 9-12. MX RESECURED CONNECTION AND OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2007101900175 20071019 00175 SO 2007 10 19 C2XA07CL087 1 20071009 A 3350 CD296CYC28V20 CONTROL PANEL EMB 145 EMB145EP 3260221 SO CABIN FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14937 145026 CLE FLIGHT 2457. THE CREW REPORTED THE EMERGENCY LIGHTS WOULD TURN OFF VIA THE DIM SWITCH ON THE F/A CONTROL PANEL. MA INTENANCE INSPECTED AND REPLACED THE F/A'S CONTROL PANEL. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2007101900176 20071019 00176 NM 2007 10 19 KCSA071459 1 20071010 A 5711 STIFFENER BOEING 747 747SR46 1384816 NM LT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 LEFT WING FRONT SPAR VERTICAL STIFFENER HAS CORROSION AT FS 1280. 2 L 7 4 4F RT A20WE 2007101900182 20071019 00182 NM 2007 10 19 KCSA071462 1 20071010 A 5313 STRINGER BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STR 27A CRACKED THREE PLACES AT FASTENER HOLES STA 380 TO 400 LEFT SIDE. 2 L 7 4 4F RT A20WE 2007101900191 20071019 00191 NM 2007 10 19 0700570 1 20071008 A 5330 654577572 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 RIGHT FUSELAGE SKIN CRACKED 2.125 - 3 INCHES AFT OF PREV REPAIR AT EMERGENCY LIGHT. REPAIRED PER ECRA 5330-03461 (REV A ). 2 L 7 2 4F RT A16WE 2007101900192 20071019 00192 NM 2007 10 19 0700571 1 20071010 A 5311 6573743 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14325 23455 FWD CARGO LWR FRAME HAS CORROSION ON FED SIDE AT STA 500D LBL 16 TO LBL 21. REPLACED FWD CARGO LWR FRAME PER SRM 53-00- 07. 2 L 7 2 4F RT A16WE 2007101900193 20071019 00193 EU 2007 10 19 SIMA200728801 1 20071010 A 3230 D49412001 CONTROL PANEL SAAB SF340 340B 7860101 EU MLG MALFUNCTIONED A SIMA L ABORTED APPROACH G MULTIPLE FAILURE AP APPROACH 1 SW 21 238AE 340B238 ABORTED APPROACH DUE TO GEAR FAIL TO EXTEND ON FINAL APPROACH, LANDING GEAR WAS SELECTED DOWN AND THE GEAR DID NOT EXTEN D, FOLLOWED AOM 1 PROCEDURE FOUND CB F7(LDG CONTROL) POPPED RESET CB, LANDING GEAR EXTENDED NORMALLY AND LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED LANDING GEAR CONTROL PANEL IAW SAAB 340 AMM 32-30-00 GEAR RETRACTION PERFORMED S ATISFACTORY. AIRCRAFT RETURN TO SERVICE 2 L 7 2 4T RT A52EU 2007101900201 20071019 00201 SO 2007 10 19 SIMA200728810 1 20071001 A 5320 14525480603 SILL EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 817AE 12828 5000 145554 DURING A MBV INSPECTION, THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND LIMITS. REPAIRED SILL IAW EMB SRM C HAPTER 51-40-02. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007101900222 20071019 00222 EA 2007 10 19 MASA200700520 1 20070824 A 5210 MECHANISM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 97325 7325 ASH 2525 PHX. MAIN CABIN DOOR HARD TO OPEN. MX CLEANED & LUBED INNER MECHANISMS. 2 L 7 2 4F RT A21EA 2007101900223 20071019 00223 EA 2007 10 19 MASA200700577 1 20070913 A 3234 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 27314 12401 7314 ASH FLT 7134 IAD-GSP. GEAR DISAGREE MESSAGE WITH NOSE DOOR OPEN MESSAGE ON EXTENSION. CYCLED AGAIN SEVERAL TIMES WITH NO NLG EXTENSION. MANUALLY EXTENDED THE NLG GEAR AND GOT 3 GREEN INDICATIONS, DECLARED AND EMERGENCY AND LANDED SAFELY. MX R2 THE NOSE GEAR SELECTOR VALVE, OPS NORMAL. 2 L 7 2 4F RT A21EA 2007101900224 20071019 00224 EA 2007 10 19 MASA200700607 1 20070918 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 591ML 7388 ASH FLT 7275 CAE-OVERNIGHT. FLIGHT DECK DOOR STICKING DURING OPENING AND CLOSING. MX LUBED AND ADJUSTED THE DOOR, OP C HECK GOOD. 2 L 7 2 4F RT A21EA 2007101900225 20071019 00225 EA 2007 10 19 MASA200700616 1 20070920 A 5270 BRACKET CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT OUT OF ADJUST A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 47202 7202 ASH FLT 7192 IAD. LEFT EMERGENCY DOOR CAUTION MESSAGE IN FLIGHT. ADJUSTED DOOR SENSOR BRACKET. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007101900227 20071019 00227 EA 2007 10 19 MESA200700328 1 20070613 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA A/C BAY OVERHEATED A MASA O OTHER M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 17358 7358 ASH 2767 BOI. RETURNED TO GATE DUE TO LEFT HAND PACK OVERHEAT WITH SMOKE IN CABIN. CONTRACT MX PLACED LEFT HAND PACK O N MEL, ACFT CONTINUED OPERATIONS. 2 L 7 2 4F RT A21EA 2007101900230 20071019 00230 EA 2007 10 19 MASA200700340 1 20070619 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17156 7156 ASH 7487 CAE. F/A REPORTS THE MAIN CABIN DOOR IS HARD TO OPEN. MAINTENANCE IS TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 2007101900231 20071019 00231 EA 2007 10 19 MASA200700342 1 20070619 A 5210 SPRING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR FAULTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37208 7208 ASH RON ORD. PAX DOOR WILL NOT CLOSE. MAINTENANCE CHANGED OUT PAX DOOR SPRINGS. 2 L 7 2 4F RT A21EA 2007101900233 20071019 00233 EA 2007 10 19 MASA200700347 1 20070621 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY DOOR NOT SEATED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 75999 7471 ASH 7409 HSV-IAD. PILOT REPORTED A RIGHT EMERGENCY DOOR CAUTION MESSAGE IN FLIGHT. RESEATED DOOR, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007101900234 20071019 00234 EA 2007 10 19 MASA200700351 1 20070622 A 5210 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR FAULTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 593ML 7465 ASH 7304 IAD. PAX DOOR NOT SUPPORTED BY DOOR WHEEL. REMOVED AND REPLACED SUPPORTABLE. 2 L 7 2 4F RT A21EA 2007101900235 20071019 00235 SO 2007 10 19 SIMA200728803 1 20071010 A 2750 FLAP SYSTEM EMB 145 EMB145LR 3260212 SO TE FLAPS MALFUNCTIONED A SIMA B EMER. DESCENT F FLT CONT AFFECTED AP APPROACH 1 SW 21 628AE 145124 UPON APPROACH WITH FLAPS AT 0 AND THEN SELECTED TO 9 DEGREES, FLAP FAIL APPEARED ON EICAS AND FLAPS STUCK AT 0. AN EMER GENCY WAS DECLARED WITH NO ABNORMAL LANDING AND NO OTHER ISSUES. 2 L 7 2 4T RT T00011AT 2007101900236 20071019 00236 EA 2007 10 19 MASA200700356 1 20070624 A 4930 SOLENOID VALVE CNDAIR CL600 CL6002B19 1900309 EA APU LEAKING A MASA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 592ML 7410 ASH 7275 IDA. PILOT REPORTED A STRONG EXHAUST ODOR IN THE FLIGHT DECK WITH THE LEFT PACK ON. MX FOUND THE APU FUEL SOL ENOID VLV LEAKING. CHANGED VLV, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007101900238 20071019 00238 EA 2007 10 19 MASA200700362 1 20070626 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37228 7228 ASH 2781 PHX. CAPT REPORTS THE MAIN CABIN DOOR IS DIFFICULT TO OPEN. MAINTENANCE INSPECTED AND FOUND NO FAULTS, DOOR O PERATED NORMALLY. 2 L 7 2 4F RT A21EA 2007101900239 20071019 00239 EA 2007 10 19 MASA200700365 1 20070627 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77331 7331 ASH 7491 IAD. REPORTED HAVING TROUBLE OPENING THE PAX DOOR FROM THE CABIN AND THE GROUND. MAX LUBBEL HANDLE. 2 L 7 2 4F RT A21EA 2007101900247 20071019 00247 EA 2007 10 19 MASA200700379 1 20070627 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 97325 7325 ENGINE SUPPORT BEAM AT LBL RBL 36.2. REPAIRED. 2 L 7 2 4F RT A21EA 2007101900248 20071019 00248 EA 2007 10 19 MASA200700380 1 20070625 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 97325 7325 THE 640 FRAMED DOUBLER & FRAME CRACKED. REPLACED LEFT 640 FRAME. 2 L 7 2 4F RT A21EA 2007101900250 20071019 00250 EA 2007 10 19 MASA200700384 1 20070630 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 651ML 7139 ASH 7188 ORD. PILOT REPORTED THE MAIN CABIN DOOR FLOOR LEVEL EMERGENCY FLOODLIGHT WAS INOP. OPS CHECK NORMAL. 2 L 7 2 4F RT A21EA 2007101900253 20071019 00253 NM 2007 10 19 SWAA075042 1 20071010 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730E, STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007101900256 20071019 00256 NM 2007 10 19 SWAA075033 1 20071010 A 5753 654643099 SKIN BOEING 737 7373Q8 1384670 NM FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED C1 CHECK, FOUND LEFT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM . 2 L 7 2 4F RT A16WE 2007101900257 20071019 00257 NM 2007 10 19 SWAA075040 1 20071010 A 5315 6546812 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 14. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007101900258 20071019 00258 NM 2007 10 19 SWAA075036 1 20071010 A 5210 6551530 SKIN BOEING 737 7373H4 1384600 NM L2 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR SKIN CRACKED AT LOWER AFT CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007101900259 20071019 00259 NM 2007 10 19 SWAA075041 1 20071010 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007101900260 20071019 00260 NM 2007 10 19 SWAA075038 1 20071010 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007101900261 20071019 00261 2007 10 19 SWAA075039 4 20071010 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007101900262 20071019 00262 2007 10 19 SWAA075035 4 20071010 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007101900264 20071019 00264 NM 2007 10 19 USAA920070917 1 20071001 A 5320 6554862505 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 5976405, CRACKED AFT PRESSURE BULKHEAD INTERCOSTAL WEB, BS 1016, LBL 26.38 - LBL 45 , WL 208.1. REPLACED AFT PRESSURE BULKHEAD INTERCOSTAL WEB, BS 1016, LBL 26.38 - LBL 45, WL 208.1 IAW B737-300 SRM 51-4 0-02. 2 L 7 2 4F RT A16WE 2007101900265 20071019 00265 NM 2007 10 19 USAA920070918 1 20071010 A 5315 141N517048 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 903AW 23323 MCN - MAJOR REPAIR - C-12 CHECK - NR 6501492, CORROSION ON CABIN FLOOR SUPPORT, BS 365.25 - BS 377.70, LBL 60, WL 208. REPLACED CABIN FLOOR SUPPORT, BS 365.25 - BS 377.70, LBL 60, WL 208 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007101900267 20071019 00267 NM 2007 10 19 USAA920070920 1 20071011 A 5320 TIE CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C-20 CHECK, CRACKED TIE CLIP, BS 663, S10L. REPLACED TIE CLIP, BS 663, S10L IAW B737-300 SRM 51-10 -02. 2 L 7 2 4F RT A16WE 2007101900268 20071019 00268 NM 2007 10 19 USAA920070921 1 20071010 A 5320 SUPPORT BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C-20 CHECK, CRACKED SUPPORT WEB, BS 345, LBL 10. REPLACED SUPPORT WEB, BS 345, LBL 10 IAW B737-300 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007101900269 20071019 00269 NM 2007 10 19 USAA920070922 1 20071006 A 5311 6546921126 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6504625, FORWARD CARGO COMPARTMENT DOOR CUTOUT FORWARD FRAME CRACKED, BS 442, S25R. REPLACED FORWARD CARGO COMPARTMENT DOOR CUTOUT FORWARD FRAME , BS 442, S25R IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007101900270 20071019 00270 NM 2007 10 19 USAA920070923 1 20071011 A 5744 654652023 ATTACH FITTING BOEING 737 7373G7 1384595 NM RT AILERON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 5976581, RIGHT AILERON INBOARD ATTACH FITTING CRACKED, WS 517.75. REPLACED RIGHT A ILERON INBOARD ATTACH FITTING, WS 517.75 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007101900271 20071019 00271 NM 2007 10 19 USAA920070924 1 20071011 A 5312 6546568515 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6505193, AFT PRESSURE BULKHEAD WEB CRACKED, BS 1016, LBL 58, WL 270. REPAIRED AFT PRESSURE BULKHEAD WEB, BS 1016, LBL 58, WL 270 IAW B737-300 SRM 53-80-08-2R7, FIGURE 201. 2 L 7 2 4F RT A16WE 2007101900272 20071019 00272 NM 2007 10 19 USAA920070925 1 20071011 A 5320 65528775 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 5966928, L2 DOOR CUTOUT WEB BROKEN, BS 1010, S7L. REPLACED L2 DOOR CUTOUT WEB, BS 1010, S7L IAW B737-300 SRM 551-40-02. 2 L 7 2 4F RT A16WE 2007101900273 20071019 00273 EU 2007 10 19 WRNA200700050 1 20070916 A 5320 STRUCTURE AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 504TA 216 DURING MAINTENANCE CHECK, CORROSION WAS FOUND AT BOTTOM OF AIRCRAFT AT STA 2559 RT, FRAME 39. REMOVED CORROSION, 2 LOCA TIONS EXCEEDED LIMITS PER SRM 51-40-11. FABRICATED REPAIR DOUBLER'S FROM .160 2024 T-3 AND FILLERS FROM .124 2024 T-3 A ND INSTALLED PER SRM 51-70-10; 51-70-2- AND 53-10-20. 2 L 7 2 4F RT A35EU 2007101900274 20071019 00274 SO 2007 10 19 C2XA07TY056 1 20071011 A 5751 14569009409 BRACKET EMB 145 EMB145XR 3260214 SO LT AILERON DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14105 145649 TYS - DURING A CURRENT C-CHECK INSPECTION THE LT AILERON PCA BRACKET HAD A BUSHION THAT WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REPLACED THE PCA BRACKET AND REINSTALL THE AILERON IAW EMB 145XR AMM 27-10-00 AND EC 5750-01177. ALL WORK W AS ACCOMPLISHED AND OPS CHECK GOOD. A/C WILL BE RELEASED AT THE END OF THE C-CHECK. 2 L 7 2 4F RT 2007101900275 20071019 00275 SO 2007 10 19 C2XA07TY057 1 20071011 A 5751 14569009410 BRACKET EMB 145 EMB145XR 3260214 SO RT AILERON DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14105 145649 TYS DURING A CURRENT C-CHECK INSPECTION THE RIGHT AILERON PCA BRACKET WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REPLA CED THE PCA BRACKET IAW EMB 145XR AMM 27-10-00 AND EC 5750-01177. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. OPS CHECKS WERE GOOD. 2 L 7 2 4F RT 2007101900276 20071019 00276 NM 2007 10 19 KCSA071464 1 20071011 A 5412 BULKHEAD BOEING 747 747SR46 1384816 NM NR 4 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 NR 4 PYLON FWD ENGINE MOUNT BULKHEAD CHORD HAS CHAFING ON FWD OF NAC STA 128. 2 L 7 4 4F RT A20WE 2007101900277 20071019 00277 NM 2007 10 19 KCSA071465 1 20071011 A 5320 SUPPORT BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA 580 AT STR 39L SIDE GUIDE SUPPORT HAS 1.5 INCH CRACK. 2 L 7 4 4F RT A20WE 2007101900280 20071019 00280 CE 2007 10 19 199WA0830007 1 20070830 A 5740 501200744 ATTACH FITTING BEECH 99 B99 1154004 CE LT WING CRACKED E AXSA K NONE O OTHER IN INSP/MAINT 1 EA 65 199WA 34399 U154 LEFT HAND UPPER FWD WING ATTACH FITTING (INBOARD) WAS FOUND WITH CRACK DURING DYE PENETRANT INSPECTION IN ACCORDANCE WIT H SRM AND AD 92-15-13. CRACK WAS ON THE TOP OF THE FITTING WRAPPING AROUND INTO THE COUNTER BORE RADIUS WITH THREE MICR O CRACKS NEXT TO IT. FITTING WAS REPLACED WITH FACTORY NEW PART. LEFT HAND LOWER FWD WING ATTACH FITTING (INBOARD) BOL T HOLE WAS FOUND TO BE ELONGATED DURING INSPECTION IN ACCORDANCE WITH AD 92-15-13. FITTING WAS REMOVED AND MODIFIED / R EPAIRED IN ACCORDANCE WITH HAWKER BEECHCRAFT CORP. FIELD REPAIR DRAWING FR-CO-01604, REINSTALLED AND RETURNED TO SERVIC E. 1 L 7 2 3T A14CE 2007101900282 20071019 00282 NM 2007 10 19 WRLA2007112 1 20071011 A 5320 TEE FITTING DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 273WA 48519 DURING 4C+12A CHECK, FOUND STA Y=2007 X=57 BULKHEAD TEE CORRODED. REPLACED DAMAGED TEE PER MD11 SRM VOL.II 51-35-01 REV .40. REF EGAT NRC U05041. 2 L 7 3 4F 4 F RT A22WE E24NE 2007101900283 20071019 00283 SO 2007 10 19 C2XA07TY058 1 20071007 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13979 145181 PILOT REPORTED BURN SMELL IN COCKPIT. MAINTENANCE OPS CHECKED TAT & PITOT HEAT RELAYS, CHECKED COOLING FANS IN FWD AVIO NICS ALL OPS CHECKED GOOD. COULD NOT DUPLICATE PROBLEM. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007101900284 20071019 00284 NM 2007 10 19 SB07089 1 20071012 A 3350 20121 CHARGER BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 516AU 23702 BDL - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT THE LEFT AFT OVER DOOR SIGN AND THE RIGHT AFT ESCAPE SLIDE INOPERATIV E. MAINTENANCE REMOVED AND REPLACED THE M1137 CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007101900286 20071019 00286 EA 2007 10 19 TRAX200701484 1 20071008 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 886AS 7531 EMERGENCY LIGHT ON IN ARMED POSITION. 2 L 7 2 4F RT A21EA 2007101900290 20071019 00290 EA 2007 10 19 TRAX200701488 1 20071009 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 859AS 7421 MAIN DOOR HANDLE WOULD NOT TURN FROM OUTSIDE. 2 L 7 2 4F RT A21EA 2007101900292 20071019 00292 EA 2007 10 19 TRAX200701492 1 20071011 A 3260 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA COCKPIT MALFUNCTIONED A ASOA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 706EV 10054 NOSE GEAR DISAGREE AFTER GEAR RETRACTION, FOLLOWED QRH AND GOT GOOD GEAR INDICATION. RETURNED TO ROC. {A/C RETURNED TO ROC AFTER T/O}. EMERGENCY EQUIPMENT ON STANDBY. FLT 4931 CX. 2 L 7 2 4F RT A21EA 2007101900293 20071019 00293 WP 2007 10 19 ABXA070341 1 20071008 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 966AX 47510 EMERGENCY LIGHTS WOULD NOT ILLUMINATE DURING PREFLIGHT. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-5 3-00-8. 2 L 7 2 4F A6WE 2007101900297 20071019 00297 SO 2007 10 19 C2XA07IA222 1 20071010 A 5610 12000737001 LOCK EMB 145 EMB145LR 3260212 SO COCKPIT DEFECTIVE A C2XA O OTHER O OTHER LD LANDING 1 SW 27 15973 145159 IAH - FLIGHT 2711, THE CREW REPORTED THAT THE CAPTAINS DV WINDOW POPPED OPEN DURING LANDING. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT. REMOVED AND REPLACED THE CAPTAINS DV WINDOW LOCK BAR AND AD JUSTED IAW EMB-145 MM56-11-00, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. 2 L 7 2 4T RT T00011AT 2007101900300 20071019 00300 EU 2007 10 19 MALA070150 1 20070912 A 5542 SKIN SAAB SF340 340B 7860101 EU RUDDER DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 415XJ 340B415 LT RUDDER SURFACE HAS DENT. REPAIRED IAW EOS55125 2 L 7 2 4T RT A52EU 2007101900301 20071019 00301 SO 2007 10 19 C2XA07IA220 1 20071009 A 2611 SMOKE WARNING EMB 145 EMB145XR 3260214 SO CARGO BAY MALFUNCTIONED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 17185 14500922 IAH - FLIGHT 537, THE CREW REPORTED A BAGGAGE SMOKE INDICATION ON CLIMB. THE CARGO FIRE BOTTLES WERE DISCHARGED, AND TH E AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE BAGGAGE SMOKE DETECTORS WITH NO DEFECTS NOTED, REPLACED THE DISCHARGED FIRE BOTTLES, AND THE AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE. 2 L 7 2 4F RT 2007101900302 20071019 00302 EU 2007 10 19 MALA070151 1 20070912 A 5542 SKIN SAAB SF340 340B 7860101 EU RUDDER DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 415XJ 340B415 LT RUDDER SURFACE HAS DENT. REPAIRED IAW EOS51031. 2 L 7 2 4T RT A52EU 2007101900305 20071019 00305 NM 2007 10 19 SWAA075047 1 20071011 A 3350 20131A BATTERY PACK BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED BRDG CHECK, FOUND FWD FUSELAGE EMERGENCY EXIT EXTERIOR LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007101900311 20071019 00311 EU 2007 10 19 MALA070156 1 20070912 A 5311 FRAME SAAB SF340 340B 7860101 EU BS 677 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 415XJ 340B415 FUSELAGE FRAME AT STA 677 AT FLOOR LEVEL DENTED. REPAIRED IAW EOS53152. 2 L 7 2 4T RT A52EU 2007101900312 20071019 00312 NM 2007 10 19 SWAA075056 1 20071011 A 5310 6519603 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 360 AND BS 380, RBL 70. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007101900313 20071019 00313 NM 2007 10 19 SWAA075051 1 20071011 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 FUSELAGE SKIN CRACKED AT BS 817, STR 15L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007101900314 20071019 00314 NM 2007 10 19 SWAA075048 1 20071011 A 5330 6545800 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT FWD END. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007101900315 20071019 00315 NM 2007 10 19 SWAA075050 1 20071011 A 5753 6573732 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 DURING SCHEDULED BRDG CHECK, FOUND LEFT WING OUTBOARD MID FLAP INBOARD L/E DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007101900317 20071019 00317 NM 2007 10 19 SWAA075043 1 20071011 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007101900320 20071019 00320 NM 2007 10 19 SWAA075044 1 20071011 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 10L CRACKED AT BS 294. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007101900321 20071019 00321 NM 2007 10 19 SWAA075053 1 20071011 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 777QC 30592 DURING SCHEDULED HC2 CHECK, LEFT OVERWING CABIN EMERGENCY EXIT BATTERY PACK FAILS LONG TEST. REMOVED AND REPLACED BATTE RY PACK PER MM. 2 L 7 2 4F RT A16WE 2007101900322 20071019 00322 NM 2007 10 19 SWAA075052 1 20071011 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 777QC 30592 DURING SCHEDULED HC2 CHECK, LEFT FWD CABIN EMERGENCY EXIT BATTERY PACK FAILS LONG TEST. REMOVED AND REPLACED BATTERY PA CK PER MM. 2 L 7 2 4F RT A16WE 2007101900325 20071019 00325 EU 2007 10 19 MALA070159 1 20070912 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 415XJ 340B415 DENTS IN THE RT FUSELAGE SKIN BENEATH THE NR 7 AND NR 8 ICE GUARDS. REPAIRED PER EOS53472. 2 L 7 2 4T RT A52EU 2007101900326 20071019 00326 EU 2007 10 19 UPS07150907 1 20071011 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU LAVATORY INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 165UP 0005 INSPECTION TYPE:N/A EMERGENCY AUX WALL MOUNTED MIRROR LIGHT IN LAVATORY INOP. RELAMPED WITH A SERVICEABLE LAMP IAW A-30 0-600 AMM 33-51-21-4. 2 L 7 2 4F RT A35EU 2007101900328 20071019 00328 EU 2007 10 19 MALA070162 1 20070912 A 5540 STRUCTURE SAAB SF340 340B 7860101 EU RUDDER PUNCTURED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 415XJ 340B415 RUDDER LEADING EDGE PUNCTURE. REPAIRED PER EOS55127. 2 L 7 2 4T RT A52EU 2007101900329 20071019 00329 EU 2007 10 19 TRBA2007085 1 20071012 A 3350 LP1670 LAMP AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHTS INOPERATIVE A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 550LL 550 EMERGENCY FLOOR LIGHTS AT GALLEY AREA INOPERATIVE. REMOVED AND REPLACED LAMPS IAW JIC NR 33-50-00 AND FOUND WORKING PRO PERLY. 2 H 7 2 4T RT A53EU 2007101900332 20071019 00332 EU 2007 10 19 CPCP00112 1 20070919 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 425MJ 425 LT O/B SEAT TRACK BETWEEN FRAME 29-36 CORRODED. SEAT TRACK FRAME 29-36 LT OUTB REPLACED IAW SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007101900333 20071019 00333 EU 2007 10 19 CPCP200700109 1 20070919 A 5320 THRESHOLD AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 425MJ 425 GUTTER ON RT THRESHOLD BETWEEN FRAME 36-39 IS CORRODED. GUTTER IS REMOVED AND REPLACED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007101900334 20071019 00334 EU 2007 10 19 CPCP200700112 1 20070919 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 425MJ 425 LT O/B SEAT TRACK BETWEEN FRAME 29-36 CORRODED. SEAT TRACK FRAME 29-36 LT OUTB REPLACED IAW SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007101900335 20071019 00335 NM 2007 10 19 QXEA200701543 1 20071012 A 7603 SWITCH DHAV DHC8 DHC8202 2809007 NM POWER LEVER FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 358PH 506 PDX FLIGHT NR 2078 SHORTLY AFTER ROTATION NR 1 ENGINE MANUAL CAUTION LIGHT ILLUMINATED ACCOMPANIED BY 10 PERCENT TORQUE INCREASE NR 1 ECU REMAINED ON WITH SELECTOR SET AT TOP. ALL ENGINE INSTRUMENTS OPERATED ACCURATELY. POWER LEVER SPLIT CONSISTENT WITH MANUAL MODE. INSPECTED AND FOUND BETA LOCKOUT SYSTEM ACTIVATED FOR NR 1 ENGINE DUE TO FAULTY POWER LEVE R MICROSWITCH 6121-S11 SUPPLYING 28V TO PIN C1 OF RELAY 6141-K3. REPLACED AND ADJUSTED NR 1 POWER LEVER MICROSWITCH 612 1-S11 IAW DHC-8-200 ENGINE RIG MANUAL PART 7, PARAGRAPH 4-4B, PAGES 7-21 TO 7-22. BETA LOCKOUT SYSTEM OPERATIONAL TEST GOOD. BETA BACKUP SYSTEM FUNCTION TEST GOOD. NR 1 ALTERNATE FEATHER/UNFEATHER TEST GOOD. AIRCRAFT RETURNED TO SERVICE 2 H 7 2 4T RT A13NM 2007101900336 20071019 00336 NM 2007 10 19 GTIA200700024 1 20071001 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM BS 765 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 516NK 2704 FLOORBEAM AT Y STATION 765 BETWEEN FR 66 AND FR 70 CORRODED. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2007101900337 20071019 00337 NM 2007 10 19 GTIA200700025 1 20071001 A 5347 SEAT TRACK AIRBUS A319 A319132 3930340 NM BS 765 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 516NK 2704 FOUND SEAT TRACK AT Y STATION -765 AT FR 66 CORRODED. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2007101900338 20071019 00338 NM 2007 10 19 GTIA200700026 1 20071001 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM BS 1292 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 516NK 2704 FLOORBEAM AT Y STATION -1292 AT FR 68 CORRODED. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2007101900339 20071019 00339 NM 2007 10 19 GTIA200700027 1 20071001 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM BS 765 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 516NK 2704 FLOORBEAM AT Y STATION -765 AND FR 68 CORRODED. REPAIRED FLOORBEAM. 2 L 7 2 4F RT A28NM 2007101900341 20071019 00341 NM 2007 10 19 GTIA200700029 1 20071001 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 516NK 2704 AFT FLOORBEAM UNDER AFT GALLEY CORRODED. REPAIRED FLOORBEAM UNDER AFT GALLEY. 2 L 7 2 4F RT A28NM 2007101900343 20071019 00343 NM 2007 10 19 AALA20071926 1 20071011 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 671AA 25336 DFW - EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK M10801 FOR EMERGENCY LIGHTS AT AFT CABIN. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007101900345 20071019 00345 NE 2007 10 19 AALA20071904 2 20071009 A 7261 TUBE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LEFT ENGINE LEAKING A AALA E A ENGINE SHUTDOWN UNSCHED LANDING K M J FLUID LOSS OVER TEMP WARNING INDICATION CR CRUISE 1 SW 21 553AA 53083 725737 DFW INFLIGHT T2485/09OCT ORD TO AUS - NUMBER ONE ENGINE HIGH OIL TEMPERATURE INDICATION. ALL OTHER ENGINE INDICATIONS NORMAL. CREW SHUT DOWN NUMBER ONE ENGINE. DIVERTED TO DFW AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME 25 MINUTES. FOUND OIL LEAK FROM COMBUSTION CHAMBER DRAIN TUBE. REPLACED NUMBER ONE ENGINE ON 10 OCT 2007 AT DFW. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007101900346 20071019 00346 EU 2007 10 19 AALA20071929 1 20071012 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 JFK - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007101900347 20071019 00347 WP 2007 10 19 AALA20071930 1 20071012 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 443AA 49469 LGA - OVERHEAD EMERGENCY LIGHTS AT SEAT ROWS 23 TO 25 INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 25 FOR OVERHEAD EM ERGENCY LIGHTS AT SEAT ROWS 23 TO 25. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007101900348 20071019 00348 WP 2007 10 19 AALA20071906 1 20071009 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 573AA 53092 SFO - EMERGENCY LIGHTS AT LEFT AND RIGHT FORWARD EXIT SIGNS AT SEAT ROW 20DEF INOPERATIVE. REPLACED BATTERY PACK FOR EM ERGENCY LIGHTS AT LEFT AND RIGHT FORWARD EXIT SIGNS AT SEAT ROW 20DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007101900349 20071019 00349 WP 2007 10 19 AALA20071907 1 20071009 A 3397 WIRE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 591AA 53254 SFO - EMERGENCY LIGHTS AT SEATS 26D AND 29D INOPERATIVE. REPAIRED WIRING AT SEAT 26D FOR EMERGENCY LIGHTS AT SEATS 26D AND 29D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007101900350 20071019 00350 WP 2007 10 19 AALA20071908 1 20071009 A 3350 LENS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 591AA 53254 SFO - EMERGENCY LIGHT AT SEAT 26D NEEDS NEW LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007101900351 20071019 00351 WP 2007 10 19 AALA20071910 1 20071009 A 3350 BULB DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 591AA 53254 SFO - EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A6WE 2007101900354 20071019 00354 WP 2007 10 19 AALA20071912 1 20071009 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7541A 49995 DFW - EMERGENCY LIGHT AT SEAT 15D NEEDS NEW SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007101900361 20071019 00361 NM 2007 10 19 AALA20071927 1 20071011 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 650AA 24608 DFW - EMERGENCY LIGHTS AT SEAT ROWS 16DEF TO 25DEF INOPERATIVE. REPLACED BATTERY PACK AT CEILING AT BIN 20DEF FOR EMERG ENCY LIGHTS AT SEAT ROWS 16DEF TO 25DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007101900363 20071019 00363 NM 2007 10 19 AALA20071914 1 20071009 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 795AN 30257 DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NR 1 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007101900364 20071019 00364 NM 2007 10 19 AALA20071915 1 20071009 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 795AN 30257 DFW - EMERGENCY LIGHTS AT FIRST CLASS CEILING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS CE ILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007101900365 20071019 00365 WP 2007 10 19 AALA20071916 1 20071010 A 2910 HOSE DOUG DC9 DC982 3022082 WP HYD SYSTEM CRACKED A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 471AA 49601 STL INFLIGHT T1646/10OCT - ON APPROACH, LOST RIGHT HYDRAULIC PRESSURE AND EXTENDED ALTERNATE GEAR HANDLE. LANDED STL WI THOUT INCIDENT. FOUND GROUND SPOILER DOWN PRESSURE LINE CRACKED AT FLARE AT CONTROL VALVE. REPLACED HOSE. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007101900366 20071019 00366 WP 2007 10 19 AALA20071921 1 20071011 A 3350 0202226001 SHROUD DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 965TW 53615 SFO - EMERGENCY LIGHT AT 10EG HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 10EG. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007101900367 20071019 00367 WP 2007 10 19 AALA20071922 1 20071011 A 3350 LENS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 965TW 53615 SFO - EMERGENCY LIGHT AT 10EG HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 10EG. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007101900368 20071019 00368 WP 2007 10 19 AALA20071923 1 20071011 A 3350 OL1098BPEGPL BULB DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 965TW 53615 SFO - EMERGENCY LIGHT AT 10EG HAS BROKEN LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 10EG. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007101900370 20071019 00370 NM 2007 10 19 EIA2007187 1 20070930 A 3350 900835A BATTERY PACK BOEING 747 747230B 1384889 NM EMERGENCY LIGHTS NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487EV 23286 EXIT SIGN UPPER DECK RIGHT CREW EXIT DOOR WILL NOT ILLUMINATE ON TEST. REPLACED UPPER DECK EXIT SIGN RIGHT BATTERY CART RIDGE PER 33-51-00. OPS CHECKED GOOD. 2 L 7 4 4F A20WE 2007101900371 20071019 00371 NM 2007 10 19 EIA2007151 1 20070825 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM EMERGENCY EXIT NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 485EV 20712 EMERGENCY EXIT LIGHT AT ATATION 400 UPPER DECK BY CREW DOOR INOP. REPLACED SODERBERG EMERGENCY EXIT LIGHT AT STATION 40 0 PER B747MM 33-51-00. OPS CHECKED GOOD. 2 L 7 4 4F A20WE 2007101900372 20071019 00372 NM 2007 10 19 EIA2007152 1 20070827 A 3350 S1356B37 LIGHT BOEING 747 747273C 1384896 NM CABIN NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 471EV 20651 EMERGENCY LIGHT UPPER DECK CABIN RIGHT SIDE INOP. UPPER DECK RIGHT SIDE EMERGENCY EXIT LIGHT REPLACED PER B747MM 33-51- 00. OPS CHECKED GOOD. 2 L 7 4 4F A20WE 2007101900375 20071019 00375 NM 2007 10 19 EIA2007179 1 20070919 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM BS 380 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 478EV 19898 MAIN DECK BS 380 FLOORBEAM LOWER CHORD CRACKED. MAIN DECK BS 380 FLOORBEAM LOWER CHORD REPAIRED PER EA-53-1183. 2 L 7 4 4F A20WE 2007101700172 20071017 00172 NM 2007 10 17 07FDEA04541 1 20071009 A 5754 LINK DOUG MD11 MD11F 3023600 NM LT WING LE SLAT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 LEFT WING, NR 3 LEADING EDGE SLAT O/B TRACK LINK FOUND CORROSION. 10-24-07 REPAIR CARRIED AS PER FEDEX EA 1-5740-1 15219. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007101700180 20071017 00180 EU 2007 10 17 07FDEA04555 1 20071010 A 5712 A5796011320000 RIB AIRBUS 300 A300F4605R 3930327 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 DURING COMPLIANCE WITH EO NR 6-5750-7-5000 P1, LT INBOARD FLAP RIB NR 25 WAS FOUND TO BE CRACKED. REPLACEMENT OF DAMAGE D RIB NR 25. 2 L 7 2 4F RT A35EU 2007101700203 20071017 00203 WP 2007 10 17 ASAA0782079 1 20071005 A 5311 591359577 FRAME DOUG DC9 DC983 3022083 WP BS 1418 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 FRAME CRACKED. REPLACED FRAME PER SRM 53-03. 2 L 7 2 4F RT A6WE 2007101700217 20071017 00217 NM 2007 10 17 ASAA0742089 1 20070928 A 5347 034053001037 SEAT TRACK BOEING 737 737490 1384715 NM BS 480 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 709AS 28896 CABIN RT LATERAL SEAT TRACK AT BS 480 GOUGED. REPLACED WITH FABRICATED REPAIR PART IAW PEMCO IPC SUPPLEMENT 53-21-01 FI G 11 & PEMCO ENGINEERING DWG 0340 53 0010 REV D & BOEING SRM 51-40-05 & 51-40-02. 2 L 7 2 4F RT A16WE 2007101700221 20071017 00221 WP 2007 10 17 ASAA0782082 1 20071005 A 5553 59670952 ATTACH ANGLE DOUG DC9 DC983 3022083 WP VERTICAL STAB CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 RIGHTHAND SIDE OF VERTICAL STABILIZER EXTERNAL VERTICAL TO FUSELAGE JOIN STRAP (ATTACH ANGLE) IS CRACKED. REPLACED DAMA GED SECTION OF JOIN STRAP PER SRM 53-05. 2 L 7 2 4F RT A6WE 2007101700223 20071017 00223 WP 2007 10 17 ASAA0782084 1 20071005 A 5753 5930496507 VANE DOUG DC9 DC983 3022083 WP TE FLAP GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 LEFTHAND WING OUTBOARD FLAP INBOARD VANE L/E DOUBLER REPAIR IS GOUGED. REPLACED EXISTING REPAIR DOUBLER PER SRM 51-70-2 . 2 L 7 2 4F RT A6WE 2007101700231 20071017 00231 EU 2007 10 17 TRAX200701428 1 20070928 A 5340 STRINGER CLIP AEROSP ATR72 ATR72 EU CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 ETNRC - LEFT STRINGER CLIP AT FR 38 AND STRINGER 21L FOUND CORRODED. CORROSION REMOVED ON LT STR CLIP AT FR 38 AND STR 21L IAW SRM 51-21-42. FABRICATION LT STR CLIP AT FR 38 AND STR 21L COVER W/C 2000-63. LT STR CLIP REPLACED IAW SRM 5 1-25-01 AND 51-25-03. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A . REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42 MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.013 WITHIN LIMITS AS PER SRM: OUT LIMITS AS PER SRM 53-61-00 FIG 301. 2 H 7 2 4T RT 2007101700232 20071017 00232 EU 2007 10 17 TRAX200701429 1 20070928 A 5315 FLOORBEAM AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 ETNRC - FLOORBEAM 38 CORRODED. CORROSION ON FLOORBEAM 38 REMOVED IAW SRM 51-21-42. REPAIR DETERMINED NOT TO BE A MAJ OR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42 MATERIAL THICKNESS: 0.071 MATERIAL REMOVED: 0.003 WITHIN LIMITS AS PER SRM: 53-00-00 FIG 305 . 2 H 7 2 4T RT 2007101800010 20071018 00010 EU 2007 10 18 07FDEA04319 1 20070926 A 5753 A5796011320000 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 728FD 581 LT RIB 25 AND RT RIB 25 FOUND CRACKED IN "B" CHECK. REPLACED RIB 25 LEFT AND RIGHT INBOARD FLAPS. 2 L 7 2 4F RT A35EU 2007101800011 20071018 00011 CE 2007 10 18 GLBA20061007 1 20071001 A 5313 STRINGER SPLICE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 246-250 CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 261GL UE261 BELLY CORROSION FOUND AT APPROXIMATELY FS 246 TO FS 250 ON STRINGER 15R. MAINTENANCE REPLACED DAMAGED STRINGER SECTION P ER ENGINEERING ORDER 07-UE261-01. APPROXIMATE STRINGER REPLACEMENT 15" WITH 11" NEW STRINGER SPLICE. PART NUMBER 131686 . RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101800017 20071018 00017 EU 2007 10 18 TRAX200701472 1 20071002 A 5240 STRUCTURE AEROSP ATR72 ATR72 EU SERVICE DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 SERVICE DOOR SURROUND 256DW CRACKED. REPAIRED AS PER CMM 25-00-01 SERVICE DOOR SURROUND 256DW PAINTED AS PER SRM 51-2 1-28. 2 H 7 2 4T RT 2007101800018 20071018 00018 EU 2007 10 18 TRAX200701473 1 20071002 A 5240 STRUCTURE AEROSP ATR72 ATR72 EU SERVICE DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 SERVICE DOOR SURROUND 256EW CRACKED. REPAIRED AS PER CMM 25-00-01 SERVICE DOOR SURROUND 256EW PAINTED AS PER SRM 51- 21-28 2 H 7 2 4T RT 2007101900006 20071019 00006 NM 2007 10 19 KCSA071457 1 20071009 A 5412 BULKHEAD BOEING 747 747236B 1384804 NM NR 1 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 NR 1 PYLON BULKHEAD CHORD CHAFED AT NAC STA 129. 2 L 7 4 4F A20WE 2007101900007 20071019 00007 NM 2007 10 19 KCSA071458 1 20071009 A 5412 BULKHEAD BOEING 747 747236B 1384804 NM NR 2 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 NR 2 PLYON BULKHEAD CHORD CHAFED AT NAC STA 129. 2 L 7 4 4F A20WE 2007101900009 20071019 00009 2007 10 19 EMB07004 4 20071008 A 2565 1040031 SLIDE EMB ERJ190 ERJ190100IGW 3260408 EU L1 DOOR OUT OF POSITION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 947UW 860 19000078 PHL - MAINTENANCE PERSONNEL FOUND THE L1 DOOR SLIDE ASSEMBLY HAD FALLEN AWAY FROM THE MOUNTING OF THE L1 DOOR. THE NUT PLATE AND CLIP WERE DISCOVERED AT THE BOTTOM OF THE DOOR FRAME. MAINTENANCE REPLACED THE ESCAPE SLIDE AND THE NUT PLATE . 2 L 7 2 4F RT A57NM 2007101900010 20071019 00010 EU 2007 10 19 MALA070123 1 20071004 A 3234 CONTROL HANDLE SAAB SF340 340B 7860101 EU MLG MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 444XJ 340B444 CREW CALLED AFTER DEPARTING MEM, THE GEAR WOULD NOT RETRACT. PINS ARE STOWED, 3 GREEN DOWN AND LOCKED INDICATION, RAN Q RH CHECK LIST, DID NOT RELEASE OR USE RELEASE BUTTON IN ORDER TO MAINTAIN STRUCTURAL INTEGRITY, NORMAL LANDING. THEY HA D ALL THE DOWN AND LOCK INDICATIONS SO DISCUSSED WITH MXC AND DECIDED TO RETURN TO MEM. REMOVED AND REPLACED LANDING GE AR CONTROL HANDLE REF AMM 32-31-05-02 PN OFF AND ON D494-12-001, SN OFF 079/07-85 ON 675/05-98. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2007101900016 20071019 00016 NM 2007 10 19 NOCA15407 1 20070904 A 3350 S417T51013 LIGHT BOEING 767 76736N 1385152 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 768NA 29898 FWD GALLEY RIGHT EMERGENCY LIGHT STRIP INOP. REMOVED AND REPLACED FWD GALLEY RIGHT EMERGENCY LIGHT STRIP, WDM 33-51-16. OPS CHECK OK. 2 L 7 2 4F RT A1NM 2007101900019 20071019 00019 NM 2007 10 19 USAA920070909 1 20070930 A 5320 TIE CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT - MAJOR REPAIR - FPBH INSPECTION, CRACKED TIE CLIP, BS 294.5, S11L. REPLACED TIE CLIP, BS 294.5, S11L IAW B737-300 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007101900020 20071019 00020 NM 2007 10 19 USAA920070910 1 20071002 A 5320 6916970501 FITTING BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT - MAJOR REPAIR - FPBH INSPECTION, CRACKED CLIP BS 360, S15L. REPLACED CLIP, BS 360, S15L IAW BOEING DRAWING 65-1768 5. 2 L 7 2 4F RT A16WE 2007101900024 20071019 00024 EU 2007 10 19 MALA070134 1 20070924 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446XJ 340B446 BELLY FAIRING PANEL 193AL CHAFE AT GROUND AIR CONNECT PANEL OPENING. REPAIRED PER EO NR S51031. 2 L 7 2 4T RT A52EU 2007101900026 20071019 00026 NM 2007 10 19 AALA20071893 1 20071008 A 3350 B21506 FUSE BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 768AA 33540 JFK - EMERGENCY LIGHTS AT SEAT ROWS 20CG TO 26CG INOPERATIVE. REPLACED FUSE IN BATTERY PACK AT RIGHT NUMBER THREE DOOR FOR EMERGENCY LIGHT AT SEAT ROWS 20CG TO 26CG. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007101900027 20071019 00027 WP 2007 10 19 AALA20071888 1 20071007 A 3231 39567851 LINK DOUG DC9 DC983 3022083 WP NOSE GEAR DOOR STIFF A AALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 21 435AA 49453 SFO INFLIGHT T562/07OCT - AFTER GEAR RETRACTION CREW REPORTED LOUD NOISE AND VIBRATION FROM NOSE GEAR AREA. CYCLED GEAR THREE TIMES WITH NO IMPROVEMENT. NOISE AND VIBRATION INCREASED WITH AIR SPEED. RETURNED TO SFO AND LANDED WITHOUT INC IDENT. FOUND RIGHT NOSE LANDING GEAR DOOR OPEN ON ARRIVAL WITH RIGHT DOOR LINK STIFF. REPLACED RIGHT NOSE LANDING GEAR DOOR LINK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007101900033 20071019 00033 WP 2007 10 19 AALA20071897 1 20071008 A 3350 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 555AN 53085 LAX - EMERGENCY LIGHT AT SEAT ROW 16D BROKEN. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 16D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F A6WE 2007101900037 20071019 00037 WP 2007 10 19 AALA20071892 1 20071008 A 2613 SENSOR DOUG DC9 DC982 3022082 WP A/C PACK TEMP LEAKING A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 227AA 49177 DFW INFLIGHT T2236/08OCT - TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED DURING CLIMB. RETURNED TO DFW AND LANDE D WITHOUT INCIDENT. REPLACED WASHER FOR AIR CONDITION HIGH TEMPERATURE SENSOR IN TAIL COMPARTMENT. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007101900045 20071019 00045 NM 2007 10 19 NWAA073396307 1 20070907 A 5510 HINGE FITTING BOEING 747 747451 1384940 NM HORIZONTAL STAB CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 661US 23719 DURING "M" CHECK WHILE ACCOMPLISHING SB 747-55A2050, FOUND CRACKED FASTENER HOLE 29 ON LT HORIZONTAL STABILIZER CENTER L T HINGE FITTING. REPAIRED PER EA 63-210684 SECTION I. SECTION II OF EA REQUIRES DVI INSPECTION OF REPAIRED AREA AT "L" CHECK INTERVALS. SECTION III REQUIRES A HFEC INSPECTION ON ALL HORIZONTAL STABILIZER FITTING HOLES TO ENSURE A CRACK F REE CONDITION. 2 L 7 4 4F RT A20WE 2007101900047 20071019 00047 NM 2007 10 19 NWAA073416301 1 20070925 A 5753 SPAR BOEING 747 747451 1384940 NM TE FLAP GOUGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 661US 23719 DURING "M" CHECK, FOUND GOUGE ON AFT WEB OF THE INBOARD FORE FLAP FRONT SPAR JUST OUTBOARD OF WBL 134.8. REPAIRED PER E A 63-210697 SECTION I. SECTION II REQUIRES INSPECTION OF REPAIR AT "L" CHECK INTERVALS. SECTION III CALLS OUT PERMANEN T REPAIR NEXT "H" CHECK. 2 L 7 4 4F RT A20WE 2007101900057 20071019 00057 WP 2007 10 19 NWAA073439863 1 20071008 A 4930 15621011 FUEL HEATER HONEYWELL DOUG DC9 DC951 3022051 WP APU UNSERVICEABLE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 772NC 66193 66193 P27474DCA 47774 SHORTLY AFTER TAKEOFF STRONG FUEL FUMES ENTERED THE CABIN. FLIGHT CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT PERFORMIN G AN UNEVENTFUL LANDING. MAINTENANCE FOUND FUEL LEAK AT APU FUEL/AIR HEATER. FUEL HEATER AND APU WERE REPLACED. 2 L 7 2 4F RT A6WE 2007101900094 20071019 00094 WP 2007 10 19 ABXA070340 1 20070927 A 5330 59111037 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 FUSELAGE SKIN CORRODED AT AFT LOWER CARGO DOOR STOP ADJUSTMENT SCREW MAT. REPAIRED AREA IAW DC9 SRM. 2 L 7 2 4F A6WE 2007101900098 20071019 00098 SO 2007 10 19 CHQA200700058 1 20071001 A 3510 MC1002117 OXYGEN MASK EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL COCKPIT LEAKING A CHQA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 11 267SK 13019 11979 145268 CAE311659 DFW TO CLE - DURING CRUISE, THE FLIGHT CREW NOTICED THAT THE CREW OXYGEN PRESSURE WAS DROPPING. THE CREW WAS UNABLE TO LOCATE THE SOURCE OF THE SLOW LEAK. ONCE THE PRESSURE DROPPED BELOW 1100 PSI THE CREW DESCENDED THE AIRCRAFT TO 10,000F T. THE AIRCRAFT WAS DIVERTED TO SDF SINCE THERE WAS INSUFFICIENT FUEL ONBOARD TO CONTINUE THE FLIGHT TO CLE. ONCE IN S DF THE AIRCRAFT WAS TURNED OVER TO MAINTENANCE.MAINTENANCE INSPECTED THE CREW OXYGEN SYSTEM AND FOUND THAT THE CAPTAIN' S OXYGEN MASK WAS LEAKING FROM THE INFLATABLE STRAPS. THE OXYGEN MASK WAS REPLACED AND THE CREW OXYGEN SYSTEM WAS LEAK CHECKED AND SERVICED, WITH NO FURTHER LEAKS DETECTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007101900099 20071019 00099 WP 2007 10 19 ABXA070337 1 20070918 A 5320 33234845 STRUCTURE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 STA 200 LEFT BUTT LINE 50 CORRODED ON SUBFLOOR. REMOVED CORROSION AND REPAIRED IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 2007101900103 20071019 00103 NM 2007 10 19 SWAA075018 1 20071009 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 285WN 32536 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007101900105 20071019 00105 NM 2007 10 19 SWAA075030 1 20071009 A 5310 6516352 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT UPPER CORNER. REPAIRED FRAME PER ACO. 2 L 7 2 4F RT A16WE 2007101900126 20071019 00126 EA 2007 10 19 SWIA200718767 1 20070802 A 7830 TRACK CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 907SW 7511 RIGHT THRUST REVERSER NR 4 MAIN TRACK IS CRACKED, FOUND AT C-CHECK. REPLACED NR 4 THRUST REVERSER TRACK PER CRJ200 AMM 70-34-11-400-801. 2 L 7 2 4F RT A21EA 2007101900127 20071019 00127 EA 2007 10 19 MASA200700465 1 20070730 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77278 7278 ASH 2728 PHX. PILOT REPORTED THE EMERGENCY LIGHTS FROM ROWS 2-5 WERE INOP. MX OP CHECKED LIGHTS AND ALL LIGHTS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2007101900136 20071019 00136 EU 2007 10 19 12127 1 20071011 A 5347 S5367800121202 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 RIGHT SEAT TRACK BETWEEN FRAMES 39 AND 40 IS CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS LIMITS. REMOVED AND REPLACED SEAT TRACK IN ACCORDANCE WITH SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007101900145 20071019 00145 EU 2007 10 19 07FDEA04576 1 20071012 A 5347 A5327400584 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 670FE 777 MCD SEAT TRACK FROM FR 78 TO FR 73, RBL15 HAS 7 AREAS WITH CORROSION. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK IAW SRM 53-10-16- AND 51-50-21. 2 L 7 2 4F RT A35EU 2007101900149 20071019 00149 NE 2007 10 19 HALA0700443 2 20071010 A 7261 HOUSING BOEING 767 7673CB 1385187 NM PWA 4060 PW4060 52119 NE NR 4 BEARING LEAKING A HALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 590HA 33467 ETOPS SIGNIFICANT SYSTEM, NR 2 ENGINE HIGH OIL CONSUMPTION 8 PINTS ADDED. ACCOMPLISHED AMM TASK 79-00-00-206 STEP G. L EAKAGE DETECTION INSPECTION ON NR 2 ENGINE, FOUND LEAK AT NR 4 BEARING OIL STRAINER HOUSING. TORQUED AND SAFETY B-NUT, NO LEAKS NOTED ON ENGINE RUN UP. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101900153 20071019 00153 NM 2007 10 19 HALA0700446 1 20071003 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 1012 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 582HA 28139 LEVEL 1 CORROSION ON RBL BS 1012 AT SECTION 45. REPAIRED SEAT TRACK AT BS 1012 SECTION 45, IAW SRM 53-00-52. REPAIRED AREA WAS ALODINED AND PAINTED. 2 L 7 2 4F RT A1NM 2007101900154 20071019 00154 NM 2007 10 19 HALA0700442 1 20071009 A 2150 CONTROL VALVE BOEING 767 7673CB 1385187 NM FLOW MALFUNCTIONED A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 590HA 33467 ETOPS SIGNIFICANT SYSTEM, L PACK OFF LIGHT ILLUMINATED. CYCLED FLOW CONTROL VALVE, LT OPS NORMAL. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007101900158 20071019 00158 EU 2007 10 19 MALA070137 1 20071010 A 5311 FRAME SAAB SF340 340B 7860101 EU BS 294 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 447XJ 340B447 DURING WORK ON RT WRAP AROUND FOUND FRAME AT STA 294 CRACKED AT RBL 18.3. INSTALLED REPAIR DOUBLER ON FRAME AT STA 294 RBL18314W EO NR S53132. 2 L 7 2 4T RT A52EU 2007101900173 20071019 00173 NM 2007 10 19 USAA920070915 1 20071004 A 5347 143N5090 SEAT TRACK BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916UW 22192 PIT - MAJOR REPAIR - C-4 CHECK, CORROSION ON CABIN SEAT TRACK, BS 640, RBL 45.50. REPAIRED SEAT TRACK, BS 640, RBL 45.5 0 IAW B757 SRM 53-00-52 AND 51-70-12. 2 L 7 2 4F RT A2NM 2007101900177 20071019 00177 NM 2007 10 19 KCSA071460 1 20071010 A 5310 DOOR FRAME BOEING 747 7472B4B 138481B NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 AFT PIT CARGO DOOR FWD FRAME DENTED 12 INCHES ABOVE THE FWD PULL IN LATCH AT STA 1820 STR 37R. 2 L 7 4 4F RT A20WE 2007101900181 20071019 00181 NM 2007 10 19 KCSA071461 1 20071010 A 5210 STRUCTURE BOEING 747 7472B4B 138481B NM R4 DOOR CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 R-4 DOOR LOWER FWD CORNER HORIZONTAL CHORD HAS CORROSION STA 1680 WL 206. 2 L 7 4 4F RT A20WE 2007101900198 20071019 00198 SO 2007 10 19 SIMA200728808 1 20071010 A 2150 DUCT EMB 135 EMB135KL 3260302 SO A/C PACK DISCONNECTED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 822AE 145581 IN CLIMB FLIGHT ATTENDANT REPORTED THAT THE CABIN WOULD NOT COOL, CREW TRIED TO RESET PACKS AND NR 1 PACK DROPPED OFF LI NE. PRESS IN CABIN WOULD NOT HOLD SO CREW DROPPED TO 10,000 FT AND TRIED TO RESET PACKS AND BLEED NR 1 PACK STILL DROP PED OFF AND CABIN STILL NOT COOLING RETURNED TO CLT. RECONNECTED PACK NR 2 BLEED DUCT LINE IAW EMB AMM 36-11-09-400-801 -A. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007101900199 20071019 00199 EA 2007 10 19 TRAX200701477 1 20070925 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 855AS 7395 QTY (4) FLOOR SUPPORT ANGLE UNDER CROSS BEAM AT FS 280.00 RBL 9 AND LBL 9. 2 L 7 2 4F RT A21EA 2007101900209 20071019 00209 EA 2007 10 19 MASA200700310 1 20070608 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 593ML 7465 ASH 7263 ORD. STRONG FUEL ODOR WHEN PACK TEMP AT 30 DEGREES. MX INSPECTED APU/PACK PERFORMED 2 MX ENGINE RUNS. NO DEF ECTS NOTED. 2 L 7 2 4F RT A21EA 2007101900212 20071019 00212 EA 2007 10 19 MASA200700398 1 20070708 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF RIG A MASA K NONE O OTHER LD LANDING 1 SW 07 7264V 7264 ASH 2922 PHX. PAX DOOR WOULD NOT OPEN AFTER FLIGHT. MX RE-RIGGED PAX DOOR. 2 L 7 2 4F RT A21EA 2007101900217 20071019 00217 EA 2007 10 19 MASA200700475 1 20070803 A 5210 ROLLER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 27318 7318 ASH 2719 PHX. REPORTED HAVING TROUBLE OPENING THE PAX DOOR FROM THE GROUND. MX LUBED THE PINS AND ROLLERS. 2 L 7 2 4F RT A21EA 2007101900220 20071019 00220 EA 2007 10 19 MASA200700492 1 20070807 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 27318 7318 ASH 2834 PHX-TUS. CREW DECLARED AND EMERGENCY ON APPROACH. CREW REPORTED THE F/O'S WINDSHIELD DELAMINATED WITH ARCING. MX REPORTED THE WINDSHIELD WAS CRACKED AS WELL. MX REMOVED AND REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 2007101900237 20071019 00237 EA 2007 10 19 MASA200700360 1 20070625 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 592ML 7410 ASH 7180 CAE. REPORTED HAVING AN EXHAUST ODOR ON LANDING. MX ISOLATED BOTH PACKS, ENGINES, AND APU BUT COULD NOT DUPLI CATE THE SOURCE OF THE LEAK. OPS NORMAL. 2 L 7 2 4F RT A21EA 2007101900242 20071019 00242 EA 2007 10 19 MASA200700371 1 20070627 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR JAMMED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 154SF 7154 ASH 7222 ORD. PAX DOOR WILL NOT OPEN. UNJAMMED DOOR. 2 L 7 2 4F RT A21EA 2007101900245 20071019 00245 EA 2007 10 19 MASA200700376 1 20070617 A 5330 60021031 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DENTED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 47202 7202 TWO DENTS LOCATED ON THE FUSELAGE SKIN AT FS 58.50% AND FS 64.50% BETWEEN STRINGERS 26L AND 26R DENTED. REPAIRED BY REM OVING DAMAGE, FABRICATING AND INSTALLING NON-FLUSH DOUBLER IAW. 2 L 7 2 4F RT A21EA 2007101900246 20071019 00246 EA 2007 10 19 MASA200700377 1 20070619 A 5330 FS310STR16 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 47202 7202 FS 310 HAS DAMAGE ON PREVIOUS SKIN REPAIR. PERFORMED A PERMANENT REPAIR TO FUSELAGE SKIN FS 310 STR 16-17. 2 L 7 2 4F RT A21EA 2007101900266 20071019 00266 NM 2007 10 19 USAA920070919 1 20071008 A 5754 114N40614 SLAT TRACK BOEING 757 7572S7 1384962 NM L/E SLAT CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 903AW 23323 MCN - MAJOR REPAIR - C-12 CHECK - NR 5976782, CORROSION ON RIGHT WING 7 SLAT OUTBOARD MAIN TRACK, SS 404.80. REPLACED RIGHT WING 7 SLAT OUTBOARD MAIN TRACK, SS 404.80 IAW B757-200 AMM 27-81-12-4. 2 L 7 2 4F RT A2NM 2007101900278 20071019 00278 NM 2007 10 19 KCSA071466 1 20071011 A 5322 SHEAR TIE BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA 400 FRAME FROM STR 15L TO STR 19L HAS 17 SMALL CRACKS AT SHEAR TIE FASTENER HOLES RANGING FROM .25 TO 1 INCH. 2 L 7 4 4F RT A20WE 2007101900279 20071019 00279 2007 10 19 195WA101007 4 20071010 A 3442 40009465201 INDICATOR BEECH 99 99 1154002 CE WEATHER RADAR MALFUNCTIONED E AXSA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 65 195WA 327 U38 FLIGHT 1058 (MHT-MPV) EN ROUTE PILOT NOTICED SMOKE AND SMELL OF BURNING WIRES IN COCKPIT BETWEEN LEB VOR AND MPV VOR. T HE PILOT ELECTED TO CONTINUE TO MPV AND LANDED WITHOUT INCIDENT. MAINTENANCE EVALUATION REVEALED SMOKE COMING FOR WEATH ER RADAR INDICATOR. THE RADAR INDICATOR WAS REMOVED FROM THE AIRCRAFT AND THE SYSTEM WAS DEFERRED PER MEL 34-4 AND THE AIRCRAFT WAS RETURNED TO SERVICE WITH NO OTHER DEFECTS NOTED. 1 L 7 2 3T A14CE 2007101900287 20071019 00287 EA 2007 10 19 TRAX200701485 1 20071008 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 931EV 8015 SERVICE DOOR HANDLE STUCK AND DOOR WILL NOT CLOSE OR OPEN ALL THE WAY. FLT 4479 DEL 65 MINS. 2 L 7 2 4F RT A21EA 2007101900291 20071019 00291 EA 2007 10 19 TRAX200701491 1 20071011 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 883AS 7504 LEFT AFT OVERWING EMERGENCY LIGHT LAMP INOP. 2 L 7 2 4F RT A21EA 2007101900294 20071019 00294 2007 10 19 SIMA200728807 2 20071012 A 7532 32158862 BLEED VALVE EMB 135 EMB135KL 3260302 SO NR 2 ENGINE FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 818AE 145561 CREW GOT A BLEED 2 VALVE FAIL AND RETURNED TO LAX FOR MTX. THE RETURN TO LAX WAS DUE TO ICING CONDITIONS ONLY. MTX REM OVED AND REPLACED H2 BLEED TWO VALVE IAW EMB 140 AMM 36-11-05, OPS CHECKS GOOD AT THIS TIME AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007101900298 20071019 00298 EU 2007 10 19 MALA070148 1 20070912 A 5753 RIB SAAB SF340 340B 7860101 EU RT TE FLAP CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 415XJ 340B415 RT FLAP, AFT COVE RIB IS CRACKED AND HAS SHEARED RIVET. REPLACED AFT COVE RIB ON RT FLAP P/N 7257840-082. 2 L 7 2 4T RT A52EU 2007101900299 20071019 00299 EU 2007 10 19 MALA070149 1 20070912 A 5522 SKIN SAAB SF340 340B 7860101 EU LT ELEVATOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 415XJ 340B415 LT ELEVATOR HAS 1 DENT IN UPPER SKIN SURFACE. REPAIRED DENT IAW EO NR S51031. 2 L 7 2 4T RT A52EU 2007101900303 20071019 00303 NM 2007 10 19 SWAA075054 1 20071011 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 777QC 30592 DURING SCHEDULED HC2 CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.50. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007101900304 20071019 00304 EU 2007 10 19 MALA070152 1 20070912 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 415XJ 340B415 BOTTOM FRAME UPPER FLANGE REINFORCEMENT CHAFED. REPAIRED IAW EOS53362 2 L 7 2 4T RT A52EU 2007101900306 20071019 00306 EU 2007 10 19 MALA070153 1 20070912 A 5311 FRAME SAAB SF340 340B 7860101 EU BS 258 MISREPAIRED A MALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 15 415XJ 340B415 PREVIOUS REPAIR ON BOTTOM FRAME STA 258, UPPER FLANGE DOES NOT COMPLY WITH EOS53102. REMOVED OLD REPAIR AND INSTALLED N EW REPAIR IAW EOS53108. 2 L 7 2 4T RT A52EU 2007101900309 20071019 00309 2007 10 19 SWAA075045 4 20071011 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 462WN 32466 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007101900310 20071019 00310 2007 10 19 SWAA075055 4 20071011 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 796SW 27889 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007101900316 20071019 00316 NM 2007 10 19 SWAA075057 1 20071011 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND LEFT WING NR 2 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007101900318 20071019 00318 NM 2007 10 19 SWAA075046 1 20071011 A 5753 65C30462 SKIN BOEING 737 7375H4 138449D NM FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED 18Y CHECK, FOUND RIGHT WING INBOARD FOREFLAP DELAMINATED AT UPPER SURFACE. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007101900327 20071019 00327 EU 2007 10 19 MALA070160 1 20070912 A 5542 SKIN SAAB SF340 340B 7860101 EU LT ELEVATOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 415XJ 340B415 LT ELEVATOR 2ND UPPER SKIN DENT 11.5" FROM THE INBD END 9.0" FWD OF THE T/E REPAIRED PER EOS51031. 2 L 7 2 4T RT A52EU 2007101900342 20071019 00342 WP 2007 10 19 AALA20071925 1 20071011 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 478AA 49653 DFW - EMERGENCY LIGHT AT FIRST CLASS FLOOR OPPOSITE LAVATORY MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT FIRST C LASS FLOOR OPPOSITE LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007101900355 20071019 00355 WP 2007 10 19 AALA20071918 1 20071010 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 560AA 53090 LGA - EMERGENCY FLASHLIGHT AT AFT FORWARD POSITION HAS BROKEN STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT FOR WARD POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007101900356 20071019 00356 NM 2007 10 19 AALA20071919 1 20071011 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 362AA 24043 MIA - EMERGENCY LIGHTS AT SEAT ROWS 32H TO 41H AND CEILING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT S EAT ROWS 32H TO 41H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007101900358 20071019 00358 WP 2007 10 19 AALA20071909 1 20071009 A 3350 SHROUD DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 591AA 53254 SFO - EMERGENCY LIGHT AT SEAT 26D NEEDS NEW SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 26D. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007101900362 20071019 00362 NM 2007 10 19 AALA20071924 1 20071011 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 760AN 31477 DFW - EMERGENCY LIGHT BATTERY PACK M33096 FAILED TEST. REPLACED BATTERY PACK M33096 FOR EMERGENCY LIGHTS. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007101900376 20071019 00376 NM 2007 10 19 EIA2007180 1 20070916 A 5311 FRAME BOEING 747 747132 1384882 NM BS 1960 S37L CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 AFT CARGO BS 1960 STR 37L FRAME FOUND CORRODED. AFT CARGO BS 1960 STR 37L FRAME REPAIRED PER EA-53-1186. 2 L 7 4 4F A20WE 2007101900378 20071019 00378 NM 2007 10 19 EIA2007156 1 20070904 A 5310 TENSION TIE BOEING 747 747212B 1384886 NM BS 800 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 STA 800 RT TENSION TIE HAS ONE DEFECTIVE FASTENER HOLE AFTER MAX ALLOWABLE REAM TO .309" PER SB 747-53-2502 VERIFIED WIT H OPEN HOLE HFEC INSPECTION. REMOVED TENTION TIE (DAMAGED). FABRICATED TENSION TIE BEAM AND SPLICE PER B747 SRM 53-10- 11 FIG 2 AND INSTALLED PER B747 SRM 53-10-11, 51-30-02 PAGE 8 AND 9 AND ECRA 486-53-065-2. 2 L 7 4 4F A20WE 2007102200002 20071022 00002 NM 2007 10 22 USAA920070932 1 20071012 A 5311 654655211 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6505052, CRACKED FRAME, BS 827, S9L. REPAIRED FRAME, BS 827, S9L IAW USAIRWAYS EA 120272. 2 L 7 2 4F RT A16WE 2007102200016 20071022 00016 EU 2007 10 22 UPS07150909 1 20071011 A 5610 WINDSHIELD AIRBUS A300 A300F4622R 3930360 EU COCKPIT FAILED A IPXA O OTHER O OTHER CR CRUISE 1 SO 01 126UP 0810 CAPTAIN'S WINDSHIELD SHATTERED IN FLIGHT. REMOVED AND REPLACED LEFT CAPTAIN'S WINDSHIELD WITH REF TO MM 56-11-11-04. W INDOW HEAT OPS CHECKS GOOD. 2 L 7 2 4F RT A35EU 2007102200018 20071022 00018 NM 2007 10 22 2007UALA04198 1 20071011 A 5753 SKIN BOEING 747 747422 1384935 NM LT TE FLAP DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 181UA 25278 ON ARRIVAL FOUND DAMAGE AT LEFT INBOARD T/E FLAP LOWER SKIN BY 2.5 INCH X 1 INCH DENT AND 2.5 U-SHAPE CRACK AND 1.25 INC H IN SIDE DENT. DENT IS 5 INCHES FROM T/E SIDE FASTENER AND 11 INCHES FROM L/E FASTENER. ALSO, 17.5 INCH FROM FLAP L/E AND 20 INCHES FROM T/E. REPAIRED FLAP PER SRM 51-70-10 REPAIR 4 PG 201. AC OK FOR SERVICE. 2 L 7 4 4F RT A20WE 2007102200022 20071022 00022 2007 10 22 2007UALA04209 4 20071014 A 2565 POWER SUPPLY AIRBUS 320 A320232 3930326 EU L1 DOOR SLIDE FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 434UA 592 AFTER REPLACING SLIDE AT DOOR 1L EMERGENCY TEST FAULTED EPSU BATTERY L. REPLACED BATTERY AT 1L AND GOT EPSU UNIT L. 10-26-07 FOUND FAULTY EPSU. REPLACED EPSU- NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F RT A28NM 2007102200023 20071022 00023 NM 2007 10 22 USAA920070926 1 20071006 A 5310 141N832259 CREASE BEAM BOEING 757 7572S7 1384962 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 903AW 23323 MCN - MAJOR REPAIR - C-12 CHECK - NR 6501595, CORROSION ON CREASE BEAM WEB, BS 877 - BS 395, LBL 65, WL 208.1. REPLACED CREASE BEAM WEB, BS 877 - BS 395, LBL 65, WL 208.1 IAW B757-200 SRM 53-10-13-01, FIGURE 1 & BOEING DRAWING 141N8322. 2 L 7 2 4F RT A2NM 2007102200024 20071022 00024 EU 2007 10 22 2007UALA04210 1 20071013 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 413UA 470 EMERGENCY LIGHT TEST MESSAGE, INT LOADS EMER L ATA 33-51-38. 10-26-07 FOUND FAULTY POWER SUPPLY. REPLACED LEFT O W POWER SUPPLY. 2 L 7 2 4F RT A28NM 2007102200025 20071022 00025 NM 2007 10 22 USAA920070944 1 20071006 A 5320 65C334192 SHEAR WEB BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 5976438, CRACKED CABIN FLOOR SHEAR WEB, BS 1025, RBL 2, WL 208.1. REPLACED CABIN F LOOR SHEAR WEB, BS 1016 - BS 1025, BL 0 - RBL 45, WL 208.1 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007102200026 20071022 00026 NM 2007 10 22 USAA920070945 1 20071014 A 5315 143N51292 FLOORBEAM BOEING 757 7572S7 1384962 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 903AW 23323 MCN - MAJOR REPAIR - C-12 CHECK - NR 5976877, CRACKED FLOORBEAM VERTICAL SUPPORT ANGLE, BS 700, RBL 24.75, WL 208. REPL ACED FLOORBEAM VERTICAL SUPPORT ANGLE, BS 700, RBL 24.75, WL 208 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007102200028 20071022 00028 NM 2007 10 22 USAA920070947 1 20071006 A 5315 65C334191 FLOORBEAM BOEING 737 7373G7 1384595 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6505100, CORROSION ON FLOORBEAM SHEAR WEB, BS 1016, LBL 55, WL 208. REPLACED FLOOR BEAM SHEAR WEB, BS 1016, LBL 55, WL 208 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007102200033 20071022 00033 EA 2007 10 22 TRAX200701497 1 20071013 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 760EV 10212 THE 4TH CABIN CEILING EMERGENCY LIGHT FROM ENTRY FOUND INOP. 2 L 7 2 4F RT A21EA 2007102200036 20071022 00036 NM 2007 10 22 KCSA071470 1 20071015 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 320 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 MAIN DECK SEAT TRACK CRACKED AT BS 320, LBL 12. 2 L 7 4 4F RT A20WE 2007102200037 20071022 00037 NM 2007 10 22 2007UALA04236 1 20071013 A 3350 SOCKET BOEING 747 747422 1384935 NM EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY LIGHT NEAR CLOSET FWD OF LAV 104 INOP. 11-01-07 FOUND SOCKET LOOSE UNDER CARPET, RECONNECTED AND OPS CH ECKED NORMAL. 2 L 7 4 4F RT A20WE 2007102200039 20071022 00039 NM 2007 10 22 KCSA071472 1 20071015 A 5313 FITTING BOEING 747 7472B4B 138481B NM BS 1241 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 S25R AFT FITTING DAMAGED AT BS 1241. 2 L 7 4 4F RT A20WE 2007102200040 20071022 00040 NM 2007 10 22 2007UALA04237 1 20071013 A 3350 LIGHT BOEING 747 747422 1384935 NM AFT GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY LIGHT AFT GALLEY RT BOTTOM WALL INOP. REPLACED SIDEWALL EMERGENCY LIGHT. OP CHECKED NORMAL 2 L 7 4 4F RT A20WE 2007102200042 20071022 00042 2007 10 22 BA07014 4 20071012 A 2565 7A1539115 SLIDE AIRBUS 330 A330323 3930335 EU L2 DOOR FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 277AY 18442 1584 0380 DURING OPERATIONAL CHECK OF L2 DOOR SLIDE, THE SLIDE FAILED TO MAINTAIN PRESSURE DUE TO A HOLE IN THE LOWER RIGHT SIDE O F THE SLIDE. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. 2 L 7 2 4F RT A46NM 2007102200044 20071022 00044 2007 10 22 UPS07150912 4 20071012 A 2210 K157ABM6 CONTROL UNIT AIRBUS A300 A300F4622R 3930360 EU FLT CONTROLS INOPERATIVE A IPXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 171UP 0005 AT FL 390 LOST BOTH AUTOPILOTS, BOTH FLIGHT DIRECTORS AND MODE CONTROL PANEL - A/C WAS DOWN TO BASIC INSTRUMENTS. REMOV ED AND REPLACED FCU PER MM 22-15-12-04. OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2007102200048 20071022 00048 NM 2007 10 22 BB07082 1 20071012 A 3350 2012 CHARGER BOEING 757 7572B7 1384964 NM EMERGENCY LIGHTS FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 929UW 27144 MAINTENANCE FOUND THAT EMERGENCY LIGHTS IN R4 DOOR AREA WOULD NOT TURN OFF AFTER TEST. REPLACED AFT RIGHT EMERGENCY BAT TERY CHARGER. NO FURTHER FAULTS. 2 L 7 2 4F RT A2NM 2007102200049 20071022 00049 NM 2007 10 22 USAA920070939 1 20071013 A 5315 6545410163 FLOORBEAM BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6505201, CRACKED FLOORBEAM TEE CAP, BS 663.75, BL 0, WL 208. REPAIRED FLOORBEAM TE E CAP, BS 663.75, BL 0, WL 208 IAW USAIRWAYS EA 120277. 2 L 7 2 4F RT A16WE 2007102200051 20071022 00051 NM 2007 10 22 SWAA075076 1 20071014 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM BS 1016 S23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 23L. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007102200052 20071022 00052 EU 2007 10 22 TRAX200701493 1 20070928 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 INSPECT & REPAIR OR REPLACE EMERGENCY LIGHTS TRACK IAW CMM AS REQ'D. 2 H 7 2 4T RT 2007102200053 20071022 00053 EA 2007 10 22 TRAX200701494 1 20071012 A 7830 TRACK CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 878AS 7590 RIGHT THRUST REVERSER LOWER INBOARD MAIN TRACK CRACKED. 10-30-07 REMOVED RT THRUST REVERSER TRACK IAW CRJ AMM 78-3 4-11. PICKED UP NUTPLATES ON SERVICABLE MAIN TRACK IAW CRJ SRM 51-45-00. INSTALLED SERVICABLE MAIN TRACK IAW CRJ AMM 78- 34-11, 10-15-07. OPS CHECK GOOD IAW CRJ MM 71-00-05. 2 L 7 2 4F RT A21EA 2007102200057 20071022 00057 NM 2007 10 22 2007UALA04191 1 20071011 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 661UA 27158 C-ZONE LEFT SIDE EMERGENCY LIGHTS AND EXIT SIGNS INOP. 11-01-07 REPLACED BATTERY PACKS. 2 L 7 2 4F RT A1NM 2007102200060 20071022 00060 NM 2007 10 22 CALA0700576 1 20071014 A 3350 AD20131A20121 BATTERY PACK BOEING 737 7373T0 1384582 NM EMERGENCY LIGHTS INOPERATIVE A CALA O OTHER O OTHER CR CRUISE 1 SW 27 14347 23585 EMERGENCY EXIT SIGN IN ADT GALLEY CENTER ASSOCIATED WITH CUSTOMER CALL LIGHT ILLUMINATES INTERMITTENTLY INFLIGHT. FOUND PROBLEM PIN NR 2 ON PWR SUPP CONNECTOR. REPINNED AND REPLACED BATTERY PACK AND POWER SUPPLY. 2 L 7 2 4F RT A16WE 2007102200062 20071022 00062 NM 2007 10 22 CALA0700578 1 20071012 A 5320 65165096 ANGLE BOEING 737 7373T0 1384582 NM BS 348-350 S16L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14325 23455 ANGLE CRACKED STA 348-350 STR 16L. REMOVED & REPLACED ANGLE PER ECRA 5311-01364. 2 L 7 2 4F RT A16WE 2007102200063 20071022 00063 NM 2007 10 22 CALA0700579 1 20071012 A 5320 69265552 BRACKET BOEING 737 7373T0 1384582 NM BS 351 S16L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14325 23455 ANGLE BRACKET CRACKED STA 351 STR 16L. REMOVED AND REPLACED BRACKET PER ECRA 5311-01364. 2 L 7 2 4F RT A16WE 2007102200064 20071022 00064 NM 2007 10 22 CALA0700580 1 20071012 A 5320 69265553 BRACKET BOEING 737 7373T0 1384582 NM BS 348-351 S16L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14325 23455 ANGLE BRACKET CRACKED STA 348-351 STR 16L. REMOVED & REPLACED BRACKET PER ECRA 5311-01364. 2 L 7 2 4F RT A16WE 2007102200066 20071022 00066 NM 2007 10 22 CALA0700582 1 20071013 A 5314 65C385021 KEELBEAM BOEING 737 7373T0 1384582 NM BS 500D-520 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14334 23572 KEELBEAM CORRODED ON I/B AND O/B FLANGES AROUND FASTENERS STA 500D-520 & O/B FLANGE STA 520. REMOVED & REPLACED FWD SEC OF LEFT KEELBEAM FROM STA 500C TO STA 540 PER SRM 51-40-02 & 53-60-12 FIG 201. 2 L 7 2 4F RT A16WE 2007102200071 20071022 00071 NM 2007 10 22 2007UALA04247 1 20071015 A 3600 BLEED AIR SYS BOEING 777 777222 1385219 NM LT ENGINE UNKNOWN A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 229UA 30557 222253 LEFT ENGINE BLEED PROBLEM. REPLACED UPPER FLOW CONTROL ISOLATION VALVE. OP CHECKS GOOD & AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T0001SE 2007102200072 20071022 00072 SO 2007 10 22 C2XA07TY059 1 20071015 A 3350 20131A BATTERY EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT DEFECTIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18120 145681 TYS - ON A OVERNIGHT A/C SEAT 12A EMERGENCY LIGHT WAS INOP. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT B ATTERY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. A/C RELEASED TO SERVICE. 2 L 7 2 4F RT 2007102200074 20071022 00074 NM 2007 10 22 ASAA0752105 1 20071015 A 2840 3012803 PROCESSOR BOEING 737 737890 1384527 NM FUEL QTY INTERMITTENT A ASAA O OTHER N FALSE WARNING CR CRUISE 1 NM 02 557AS 35176 IN CRUISE AT FL390 CTR TANK QUANTITY & TOTAL FUEL QUANTITY DISPLAYS BLANKED. FMC AMBER P RST LIGHT ILLUMINATED. FMC SC RATCH PAD NOTE "VERIFY GW & FUEL QTY" ILLUMINATED. DISPLAY RETURNED TO NORMAL AFTER ABOUT 60 MINUTES. FQIS FFR SHOWS 2 FLTS WITH CENTER QTY BLANK. ONE OR MORE TANK UNITS OPEN FAULT. CENTER TANK INDICATOR CURRENTLY GOOD. CURRENT STATUS AND GROUND TEST GOOD. 2 L 7 2 4F RT A16WE 2007102200075 20071022 00075 SO 2007 10 22 C2XA07IA223 1 20071014 A 3320 7287501545 LIGHT EMB 145 EMB145 3260210 SO CABIN BURNED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 27962 145110 IAH - FLIGHT 2481, ON POST FLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL ODOR IN THE CABIN. MAINTENANCE INSPECTED T HE AIRCRAFT AND REMOVED AND REPLACED THE LIGHT ASSEMBLY ABOVE SEAT 6A, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AI RCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008010300013 20080103 00013 NM 2008 1 3 07FDEA05060 1 20071215 A 2752 269002913 ACTUATOR BOEING 727 7272S2F 1384O81 NM FLAPS FAILED A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 207FE 30151 30151 22929 AFTER T/O, NON FLYING PILOT SELECTED FLAPS FROM 5 DEG TO 2 DEG CREW NOTICED AN ILLUMINATED LE FLAPS AMBER LIGHT WITH ASS OCIATED LOSS OF SYS A HYDRAULIC FLUID. SO FLAP CONFIGURATION PANEL INDICATED AN AMBER NR 4 SLAT. CREW FOLLOWED ALL APP LICABLE QRH PROCEDURES THEN RETURNED TO LANDING. DID NOT SHUT OFF SYS A FLUID SWITCHES. VERIFIED NR 4 SLAT ACTUATOR FA ILED. REMOVED AND REPLACED NR 4 LEADING EDGE SLAT ACTUATOR OPS AND LEAK CHECK GOOD PER M/M 27-81-032-4. R/I FROM FACT , PREMATURE REMOVED AND REPLACED OFF MFG 2-690029-13, 2 L 7 3 4F A3WE 2007102200078 20071022 00078 NM 2007 10 22 SWAA075083 1 20071015 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 444WN 29839 EEPLS LENS LOOSE AT ROW 5 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007102200079 20071022 00079 NM 2007 10 22 SWAA075091 1 20071015 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 222WN 34290 EEPLS LENS LOOSE AT ROW 3 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007102200084 20071022 00084 NM 2007 10 22 SWAA075069 1 20071014 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM BS 360 S28L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 360, STR 28L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007102200085 20071022 00085 NM 2007 10 22 ZZDA2007286 1 20071010 A 5320 PAN BOEING 717 717200 1383700 NM CARGO DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 956AT 55018 FWD BAG BIN DOOR FRAME PAN HAS CORROSION BEYOND LIMITS. INSTALLED PAN SPLICE REPAIR PER SRM 53-20-15 REPAIR 6. 2 L 7 2 4F TR A6WE 2007102200088 20071022 00088 NM 2007 10 22 ASAA0792094 1 20071009 A 5315 993061221 FLOORBEAM BOEING 737 737990 NM BS 7271 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 305AS 30013 AFT CARGO PIT FLOORBEAM TEE CORRODED AT BS 727I+6. REPAIRED FLOORBEAM TEE IAW 51-40-05. 2 L 7 4 4F RT A16WE 2007102200090 20071022 00090 NM 2007 10 22 ASAA0792092 1 20071009 A 5512 10001022 SKIN BOEING 737 737990 NM HORIZONTAL STAB DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 305AS 30013 DENT ON LEFT HORIZ STAB L/E 5FT FROM ROOT. REPAIRED DENT ON L/E IAW SRM 55-10-01. 2 L 7 4 4F RT A16WE 2007102200092 20071022 00092 NM 2007 10 22 USAA920070942 1 20071012 A 5340 ATTACH ANGLE BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C-20 CHECK, CRACKED STRINGER SPLICE ATTACH ANGLE, BS 348, S14L - S15L. REPLACED STRINGER SPLICE ATTACH ANGLE, BS 348, S14L - S15L IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007102200093 20071022 00093 NM 2007 10 22 USAA920070943 1 20071012 A 5313 STRINGER BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C-20 CHECK, CRACKED STRINGER CHANNEL, BS 360, S15L. REPLACED STRINGER CHANNEL, BS 360, S15L IAW B7 37 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007102200100 20071022 00100 NM 2007 10 22 2007UALA04201 1 20071011 A 3097 WIRE BOEING 737 737522 138449F NM WINDSHIELD HEAT OPEN A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 933UA 26659 RIGHT FWD WINDOW HEAT WILL NOT STAY ON. PWR TO WINDOW STAYS ON FOR 1 MIN AFTER SWITCH RECYCLED - 3RD HIT. SUSPECT WINDO W HEAT WIRE OPEN. REPLACED FWD RH WINDOW ASSEMBLY. AC OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2007102200104 20071022 00104 NM 2007 10 22 2007UALA04239 1 20071015 A 3350 LAMP BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHT SEAT 5E FWD INOP. 11-01-07 RELAMPED. 2 L 7 4 4F RT A20WE 2007102200106 20071022 00106 NM 2007 10 22 USAA920070927 1 20071011 A 5320 WEB BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C-20 CHECK, CRACKED SUPPORT WEB, BS 345, LBL 10. REPLACED SUPPORT WEB, BS 345, LBL 10 IAW B737-300 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007102200109 20071022 00109 WP 2007 10 22 MWEA070251 1 20071014 A 7830 3938072501 FASTENER DOUG DC9 DC981 3022081 WP THRUST REVERSER MISSING A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 812ME 48006 LEFT ENGINE THRUST REVERSER, BOTH LEFT AND RIGHT STANGS ARE MISSING RIVETS AT THE TIP. INSTALLED FASTENERS. 2 L 7 2 4F A6WE 2007102200110 20071022 00110 WP 2007 10 22 MWEA070252 1 20071016 A 5320 527779224 STIFFENER DOUG DC9 DC981 3022081 WP BS 1431 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 812ME 48006 STIFFENER CORRODED ON CANTED BULKHEAD FRAME STATION 1431 LEFT ADJACENT TO STRINGER 11 LEFT. REMOVED STIFFENER AT CANTED BULKHEAD, FABRICATED AND INSTALLED STIFFENER. 2 L 7 2 4F A6WE 2007102200113 20071022 00113 WP 2007 10 22 MWEA070255 1 20071017 A 3350 60030451 BATTERY PACK DOUG DC9 DC981 3022081 WP ROWS 9-13, 19-26 INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 CEILING EMERGENCY LIGHTS ARE INOPERATIVE AT ROWS 9 - 13 F, E, C AND ROWS 19 - 26 F, E, C. REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 2007102200115 20071022 00115 NM 2007 10 22 2007UALA04213 1 20071014 A 5330 SKIN BOEING 737 737322 1384676 NM BS 380 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24148 LOWER FUSELAGE EXTERNAL SKIN IS DAMAGED AT EQUIPMENT COOLING EXHAUST CUTOUT AT BS 380 & BL 0. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED EXTERNAL AND INTERNAL REPAIR DOUBLER. 2 L 7 2 4F RT A16WE 2007102200116 20071022 00116 NM 2007 10 22 2007UALA04214 1 20071014 A 5330 DOUBLER BOEING 737 737317 138447P NM BS 368 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24148 INTERNAL DOUBLER AT EQUIPMENT COOLING EXHAUST DUCT CUTOUT IS CRACKED AT FWD END BS 368 AT RBL 1. REMOVED DAMAGE. FABR ICATED AND INSTALLED NEW DOUBLER. 2 L 7 2 4F RT A16WE 2007102200123 20071022 00123 2007 10 22 2007UALA04223 4 20071012 A 2565 SLIDE BOEING 757 757222 1384956 NM L2 DOOR UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 588UA 26717 DOOR 2L DIFFICULT TO ARM. RESECURED SLIDE LACING AND THE ARMING OF DOOR RETURNED TO NORMAL. 2 L 7 2 4F RT A2NM 2007102200126 20071022 00126 NM 2007 10 22 2007UALA04232 1 20071013 A 3350 LIGHT BOEING 747 747422 1384935 NM CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY CEILING LIGHT FAULTY. 11-01-07 REPLACED LIGHT HOUSING AND RELAMPED. 2 L 7 4 4F RT A20WE 2007102200127 20071022 00127 NM 2007 10 22 KCSA071468 1 20071014 A 5420 STIFFENER BOEING 747 747246F 1384850 NM NR 3 NACELLE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 707CK 21681 NR 3 PYLON STIFFENER HORIZONTAL FLANGE CRACKED AT NAC STA 132, NAC WL 164. 2 L 7 4 4F RT A20WE 2007102200128 20071022 00128 EU 2007 10 22 TRAX200701496 1 20071012 A 3350 LIGHT AEROSP ATR72 ATR72 EU PAX DOOR INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 PASSENGER DOOR EMERGENCY LIGHT INOP. 2 H 7 2 4T RT 2007102200129 20071022 00129 SO 2007 10 22 C2XA07CL088 1 20071012 A 3350 SG963 LIGHT EMB 145 EMB145XR 3260214 SO GALLEY MISSING A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17138 145727 CLE FLIGHT 2219. THE CREW REPORTED THE EMERGENCY LIGHT STRIP WAS MISSING NEAR THE GALLEY. MAINTENANCE INSPECTED AND IN STALLED MISSING LIGHT STRIP NEAR THE GALLEY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2007102200130 20071022 00130 NM 2007 10 22 CAL0700592 1 20071017 A 5320 6517684638 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 294 S12L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14334 23572 INTERCOSTAL CRACKED AT STA 294.5 STR 12L. FABRICATED AND INSTALLED PER ECRA 5311-01368. 2 L 7 2 4F RT A16WE 2007102200131 20071022 00131 NM 2007 10 22 CAL0700594 1 20071017 A 5314 6562125 KEELBEAM BOEING 737 7373T0 1384582 NM BS 500D S28R CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14334 23572 FBB KEEL BEAM S-28R HAS CORROSION ON I/B FLANGE AROUND FASTENER HOLES AFT OF 500D. REPAIRED RT KEEL BEAM AFT OF STA 500 D PER ECRA 5311-01367 AND SRM 53-30-12 FIG 201 REPAIR 2. 2 L 7 2 4F RT A16WE 2007102200132 20071022 00132 NM 2007 10 22 CAL0700595 1 20071018 A 5340 651768465 BRACKET BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14334 23572 S-10L, UPPER HINGE, LOWER INTERCOSTAL, O/B ATTACHMENT CLIP CRACKED .75 INCH IN AT AFT BEND. REPAIRED PER ECRA 5311-0136 9. 2 L 7 2 4F RT A16WE 2007102200133 20071022 00133 NM 2007 10 22 CALA0700590 1 20071017 A 5313 BAC1498163 STRINGER BOEING 737 7373T0 1384582 NM BS 500 S28R CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14334 23572 FBB STRINGER S-28R HAS SEVERE CORROSION AFT STA 500 FRAME CUTOUT DAMAGE. REPAIR PER SRM 53-00-03 FIG 201. 2 L 7 2 4F RT A16WE 2007102200140 20071022 00140 2007 10 22 SWAA075063 4 20071014 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 408WN 27895 L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007101900039 20071019 00039 EU 2007 10 19 12114 1 20071010 A 5315 S53672410284 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 FOUND UPPER FLOORBEAM 41 IS CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS LIMITS. REMOVED AND INSTA LLED FLOORBEAM IN ACCORDANCE WITH SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007101900051 20071019 00051 WP 2007 10 19 07FDEA04565 1 20071010 A 5347 4929151 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 374-420 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 CABIN/CORROSION ON SEAT TRACK (EQUIPMENT TIE DOWN TRACK) AT BL 78 LT AND BETWEEN FS 374 AND 420 REMOVED CORROSION IAW MD /DC-10 SRM 53-70-00 FIG 5 SHEET 2 VOL I MIN THAT CAN BE REMAINING IS .060 IAW MD/DC-10 SRM 53-70-00 FIG 5 SHEET 2 VOL I OUT OF LIMITS IAW MD/DC-10 SRM 53-70-00 FIG 5 SHEET 2 VOL I UT GAUGE USED T82530. REMOVED AND REPLACED SEAT TRACK IAW M D/DC-10 SRM 51-31-01 VOL II PG 1-2. REPAIR CLASSIFIED AS MINOR. 2 L 7 3 4F A22WE 2007101900052 20071019 00052 NM 2007 10 19 USAA920070912 1 20070930 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT - MAJOR REPAIR - FPBH INSPECTION, CRACKED BULKHEAD WEB, BS 178, LBL 5, WL 184. REPAIRED BULKHEAD WEB, BS 178, LBL 5 , WL 184 IAW USAIRWAYS EA 98903. 2 L 7 2 4F RT A16WE 2007101900055 20071019 00055 EU 2007 10 19 USAA920070913 1 20071003 A 2910 O-RING AIRBUS 320 A320231 3930325 EU NR 1 ENGINE HCU LEAKING A USAA O OTHER J WARNING INDICATION CR CRUISE 1 EA 19 625AW 064 PHX - IAH - FLT 274 - THE CREW REPORTED THE A/C LOST GREEN HYDRAULIC SYSTEM WHICH RENDERS NOSE WHEEL STEERING INOP. THE CREW DECLARED AN EMERGENCY. THE LANDING WAS UNEVENTFUL AND THE A/C WAS TOWED TO THE GATE. MX REPLACED THE NR 1 ENGINE HCU DIFFERENTIAL PRESSURE HOUSING O-RING. OPERATIONAL / LEAK CHECK WAS GOOD. THE A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2007101900060 20071019 00060 WP 2007 10 19 IXXA070052O 1 20071011 A 3250 UNKNOWN DOUG DC8 DC871F 302199D WP ZONE 700 UNKNOWN A IXXA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 11 820BX 89797 718 46065 DURING TAKEOFF FROM KLRD, THE NOSE WHEEL STEERING WAS VERY SLOW TO RESPOND TO TILLER. THE CREW REJECTED TAKEOFF DUE TO UNABLE TO HOLD AIRCRAFT TO CENTER LINE OF RUNWAY ON INITIAL TAKEOFF ROLL. THE CREW RETURNED TO BLOCKS AT KLRD WITHOUT I NCIDENT. MAINTENANCE INSPECTED NOSE WHEEL STEERING SYSTEM ACCUMULATOR SERVICED AS REQUIRED. INSPECTED AND LUBED ALL CA BLES FOR STEERING, CHECKED TIRE PRESSURE, ACCOMPLISHED OPERATIONAL CHECK GOOD IAW DC8 MAINTENANCE MANUAL 32-52-6, N/R J/ C NUMBER 13.01-5, AND ATI ERH 09.01-1. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2007101900066 20071019 00066 EU 2007 10 19 TRAX200701475 1 20071006 A 3350 LIGHT AEROSP ATR72 ATR72 EU AIRSTAIRS INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 634AS 370 ASD EMERGENCY LIGHT INOP. 2 H 7 2 4T RT 2007101900069 20071019 00069 NM 2007 10 19 UPS07M50888 1 20070830 A 5720 STRUCTURE DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C LEFT WING LOWER SURFACE L/E ACCESS PANEL CUTOUT STRUCTURE AT STA XORS 51 0 APPROX FOUND CRACK AS MARKE D. LEFT WING LOWER SURFACE L/E APPROX XORS 510 DOUBLER REMOVED. NEW DOUBLER FABRICATED USING MAT'L 7075-T6-0.090" PER DOUGLAS DWG ARB2933. NEW DOUBLER FASTENER HOLES PICKED UP, REPROTECTED & PAINTED. NEW DOUBLER INSTALLED AS PER SRM 51- 31-01 VOL II REV 38. 2 L 7 3 4F RT A22WE 2007101900074 20071019 00074 WP 2007 10 19 ABXA070329 1 20070920 A 5313 59114087 LONGERON DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 LONGERON 4 LEFT CRACKED AT STA 160 AT OUTBOARD FASTENER. REPLACED SECTION OF LONGERON 4 IAW DC9 SRM 53-02 FIGURE 18. 2 L 7 2 4F A6WE 2007101900080 20071019 00080 WP 2007 10 19 ABXA070325 1 20070922 A 5420 99581937 ANGLE DOUG DC9 DC941 302207N WP LT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 NR 1 PYLON STRUCTURE CRACKED FORWARD OF CONNECTOR. REPAIRED NR 1 PYLON STRUCTURE FORWARD OF CONNECTOR IAW DC9 SSRM DWG K05159. 2 L 7 2 4F A6WE 2007101900083 20071019 00083 NM 2007 10 19 QXEA200701534 1 20071008 A 2530 180140 HOT WATER POT BOMBDR DHC8 DHC8402 1390042 NM GALLEY ODOR A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 09 409QX 4051 BZN - ON FLIGHT NUMBER 2311, FLIGHT ATTENDANT REPORTS MAPCOS HAVE ELECTRIC SMELL. MAINTENANCE REMOVED AND REPLACED HOT WATER JUGS. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007101900085 20071019 00085 WP 2007 10 19 ABXA070335 1 20070918 A 5347 S2914913M24000 SEAT TRACK DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 LEFT BUTT LINE 44 STA 170 TRACK CRACKED. REMOVED AND REPLACED SEAT TRACK LEFT BUTT LINE 44, STA 160 - 230 IAW DC9 SRM 5 1-30-1. 2 L 7 2 4F A6WE 2007101900088 20071019 00088 WP 2007 10 19 ABXA070338 1 20070918 A 5210 3917853503 BRACKET DOUG DC9 DC932 3022066 WP AFT ENTRY DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 AFT ENTRY DOOR LOWER LEFT LOCK MECHANISM BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW DC9 SRM. 2 L 7 2 4F A6WE 2007101900091 20071019 00091 WP 2007 10 19 ABXA070339 1 20070924 A 5230 59101575 PAN DOUG DC9 DC932 3022066 WP AFT CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 AFT LOWER CARGO DOOR OUTER PAN CRACKED AT BARREL NUT HOLE AT FORWARD END OF BEAM NR 3. REPAIRED AREA IAW DC9 SRM 52-03, FIGURE 9. 2 L 7 2 4F A6WE 2007101900093 20071019 00093 NM 2007 10 19 2007UALA03661 1 20070909 A 2720 810A000003 ROD END AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE RUDDER SERVO WORN A UALA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 814UA 862 FLIGHT ATTENDANTS STATED FELT SUBSTANTIAL VIBRATION IN AFT CABIN AND FORWARD CABIN FOR ABOUT 1 MIN. FOUND EXCESSIVE RUD DER FREE PLAY IN THE SERVO ROD ENDS. REPLACED ALL THREE RUDDER SERVO ROD ENDS. AT HMV, RUDDER HINGE BEARINGS REPLACED, ELEV HINGE BEARINGS REPLACED AND LEFT ELEV GREEN SYS SERVO FAILED FREE PLAY CHECK AT HMV. REPLACED LEFT ELEV GREEN SER VO. 2 L 7 2 4F 4 F RT A28NM E40NE 2007101900095 20071019 00095 NM 2007 10 19 2007UALA03664 1 20070910 A 2720 33215209 PCU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RUDDER FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 541UA 25253 DURING THE TEST OF THE RUDDER PCU'S THE TEST FAILED USING THE LT HYDRAULIC SYSTEM. THE SYSTEM TESTED OK USING THE RT AN D CENTER HYDRAULIC SYSTEMS. USING THE LT SYSTEM ALONE THE RUDDER HAD NO MOVEMENT TO THE LEFT AND SLIGHT MOVEMENT TO THE RIGHT AND WOULD NOT RETURN TO CENTER. SUPPLEMENTAL DATA UPDATE, NO DISCREPANCIES FOUND WITH LEFT POWER CONTROL UNIT FO R THE RUDDER. FAULT WAS WITH THE CENTER PCU. REPLACED PCU. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101900096 20071019 00096 NM 2007 10 19 CHQA200700056 1 20070921 A 3244 299K631 TIRE BOMBDR CL600 CL6002D15 NM GE CF34 CF343B1 NE MLG FAILED A CHQA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 11 469SM 241 7650 GEE873397 LBB TO IAH. IMMEDIATELY AFTER ROTATION ON TAKEOFF, CREW RECEIVED "WOW INPUT" EICAS MESSAGE. FOLLOWED QRH AND CONTACTE D MAINTENANCE CONTROL VIA ATL RADIO. HALF AN HOUR INTO FLIGHT, CENTER CALLED AND TOLD CREW THAT RUBBER DEBRIS HAD BEEN FOUND ON THE RUNWAY IN LBB. APPROACH WAS NOTIFIED AND REQUESTED EMERGENCY EQUIPMENT BE STANDING BY FOR LANDING. UPON L ANDING, ONLY THRUST REVERSERS WERE USED TO SLOW THE AIRCRAFT UNTIL IT COULD BE TAXIED OFF THE RUNWAY. THE AIRCRAFT WAS TAXIED CLEAR OF THE RUNWAY AND EMERGENCY PERSONNEL INSPECTED THE AIRCRAFT AND FOUND THE RIGHT OUTBOARD MAIN TIRE HAD BLO WN AND THE INBOARD WAS LOW. THE PASSENGERS WERE DEPLANED BY BUS, AND THE AIRCRAFT WAS TURNED OVER TO MAINTENANCE. MAIN 2 L 7 2 4F 4 F RT A21EA E15NE 2007101900106 20071019 00106 SO 2007 10 19 CHQA20070059 1 20070923 A 2120 UNKNOWN EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL CABIN SMOKE A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 841RP 145737 CAE11599 CMH TO MCO - DURING INITIAL CLIMB-OUT, JUST AFTER ACCELERATION ALTITUDE, A LAV SMOKE WARNING MESSAGE APPEARED ON EICAS. THE FLIGHT ATTENDANT CALLED THE CABIN AND REPORTED THAT THE LAVATORY SMOKE DETECTOR WAS GOING OFF AND THERE APPEARED TO BE SOME SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED AND AN IMMEDIATE RETURN TO FIELD WAS REQUESTED. AS THE AIRCRAFT TURNED DOWNWIND AND THE FLIGHT CREW WAS STARTING ON THE QRH FOR LAVATORY SMOKE, THE EICAS WARNING WENT AWAY. THE FLIGH T ATTENDANT WAS ASKED TO CONFIRM THAT IT HAD GONE AWAY, AND THE FLIGHT ATTENDANTS INDICATIONS HAD GONE AWAY AND THERE WA S NO SMOKE IN THE CABIN. THE AIRCRAFT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE AND WAS TURNED OVER TO MAINTENANCE 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007101900110 20071019 00110 NM 2007 10 19 SWAA075022 1 20071009 A 5753 6546435237 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED HC1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007101900133 20071019 00133 EA 2007 10 19 SWIA200718772 1 20070802 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 907SW 7511 FOUND AT C-CHECK, LEFT ENGINE THRUST FITTING IS CORRODED. INSTALLED NEW ENGINE THRUST FITTING PER CRJ200 AMM 71-22-01-4 00-801. 2 L 7 2 4F RT A21EA 2007101900134 20071019 00134 EA 2007 10 19 SWIA200718773 1 20070802 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DEFORMED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 907SW 7511 FRAME BELOW LEFT MAIN GEAR UPLOCK ACTUATOR HAS DAMAGE FROM DOOR ROD, FOUND AT C-CHECK. INSTALLED ALL REPAIR PARTS ON LE FT MAIN GEAR SUPPORT STRUCTURE PER REO 601R-53-41-568 REV- A. 2 L 7 2 4F RT A21EA 2007101900152 20071019 00152 NM 2007 10 19 HALA0700444 1 20071009 A 2497 CONNECTOR BOEING 767 76733A 1385209 NM LT GENERATOR DIRTY A HALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, ATO - L GEN OFF EICAS ILLUMINATED ON T/O ROLL. PER FIM 24-20-00 PERFORMED BITE BPCU, ONE FOUL OVER VOLT TRIP GEN/WIRING. OPENED LEFT ENGINE REMOVED AND CLEAN CONNECTORS FROM IDG RUN ENG FOR 5 MIN. RESET L/GEN OP S CHECK NORMAL. 2 L 7 2 4F RT A1NM 2007101900155 20071019 00155 EU 2007 10 19 MALA070146 1 20071008 A 3350 RELAY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425XJ 340B425 AFTER SHUTDOWN, EMERGENCY LIGHTS FAILED TO TURN OFF. FOUND CIRCUIT BREAKER L-8 POPPED. VERIFIED THERE IS A SHORT IN TH E SYSTEM CONTROL FUNCTION. PULLED AND SECURED CONTROL CB L-8. INSPECTED AIRCRAFT AND FOUND SAFE FOR ONE-TIME FERRY FRO M TUP TO MEM FOR REPAIR. REPLACED RELAY PN: M93536/10/024M, RDI 16LN. 2 L 7 2 4T RT A52EU 2007101900162 20071019 00162 EU 2007 10 19 MALA070143 1 20071010 A 5751 SKIN SAAB SF340 340B 7860101 EU LT AILERON PUNCTURED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 447XJ 340B447 COMPOSITE REPAIR TO PUNCTURED/DISBOND SKIN OF LT UPPER AILERON SURFACE, 1 1/4 INCH DIA, 47 INCH' FROM IB, 4 INCH FROM T/ E. REPAIRED PER EO NR S51031. 2 L 7 2 4T RT A52EU 2007101900163 20071019 00163 EU 2007 10 19 MALA070144 1 20071010 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 447XJ 340B447 DENT LOCATED 9'' ABOVE NLG DOOR OPENING LT SIDE, 1 3/4'' AFT OF RADOME. INSTALLED DOUBLER IAW EO NR S53484. 2 L 7 2 4T RT A52EU 2007101900171 20071019 00171 EU 2007 10 19 TRBA200084 1 20071013 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHTS FAILED A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 541AT 541 F/A COULD NOT OPERATE ALL CABIN EMERGENCY LIGHTS USING AFT EMERGENCY LIGHTS PUSH BUTTON. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK FIN NR 62WL IAW JIC NR 33-51-20. 2 H 7 2 4T RT A53EU 2007101900174 20071019 00174 NM 2007 10 19 USAA920070916 1 20070915 A 5330 6545774105 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6504500, CRACKED FUSELAGE SKIN, BS 727D, S27L. REPAIRED FUSELAGE SKIN, BS 727D, S 27L IAW B737 SRM 53-00-01-2R31, FIGURE 201. 2 L 7 2 4F RT A16WE 2007101900178 20071019 00178 EU 2007 10 19 SIMA200728802 1 20071010 A 2750 6225027002 SERVO SAAB SF340 340B 7860101 EU MALFUNCTIONED A SIMA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SW 21 317AE 340B317 ON CLIMB 160 KIAS AUTO PILOT ENGAGED NOTED FORE AND AFT MOVEMENT OF YOKE ACCOMPANIED BY PITCH MOVEMENT AND VIBRATION IN CONTROLS AND IN AIRCRAFT. REMOVED AND REPLACED ELEVATOR SERVO IAW SAAB AMM 22-10-26, PERFORMED SAAB VIBRATION WORK CAR D, REMOVED AND REPLACED ELEVATOR SERVO IAW SAAB 22-10-26. REMOVED AND REPLACED SERVO MOUNT ELEVATOR REMOVED AND REPLAC ED LEFT AND RIGHT AILERON CONTROLLER MECHANISM BEARING AND CAM ASSY AMM 27-11-45, RIGGED AILERON CABLE SYS AMM 27-11-00. FCF PASSED AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4T RT A52EU 2007101900188 20071019 00188 NM 2007 10 19 0700567 1 20071006 A 3300 ADDD71701100 BATTERY PACK BOEING 737 737924 13848A1 NM CABIN MALFUNCTIONED A CALA O OTHER O OTHER NR NOT REPORTED 1 SW 27 35407 30124 EMERGENCY BATTERY PACK BAD ROW 26L AND 21R. REPLACED BATTERY PACK PER CARD 29-3350-1-9100. 2 L 7 2 4F RT A16WE 2007101900194 20071019 00194 NM 2007 10 19 0700572 1 20071010 A 5313 6545800 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14325 23455 FWD CARGO STRINGER 27L HAS CORROSION ON IT AT STA 500C+18 LBL. REPAIRED STRINGER PER SRM 53-00-03. 2 L 7 2 4F RT A16WE 2007101900200 20071019 00200 SO 2007 10 19 2007SIMA28809 1 20071001 A 5322 14525175001 SHEAR TIE EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 817AE 145554 DURING A MBV INSPECTION, THE CARGO DOOR FWD LOWER SHEAR CLIP AT FRAME 65 WAS FOUND CORRODED. REPAIRED SHEAR CLIP IAW EM B IC2007-145/06674 DATED 1 OCT 07. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007101900207 20071019 00207 NM 2007 10 19 WRLA2007107 1 20071008 A 5347 AFA7789550 SEAT TRACK DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 273WA 48519 DURING 4C+12A CHECK, SEAT TRACK CORROSION FOUND AT STA X=-67 Y=517. 10-25-07 REPLACED DAMAGED SEAT TRACK PER MD-11 SRM VOL.I 53-70-00 FIG.8 REV.40. 2 L 7 3 4F 4 F RT A22WE E24NE 2007101900218 20071019 00218 2007 10 19 MASA200700482 4 20070805 A 2561 P01074201 LIFE VEST CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 654BR 1104 7454 ASH 1020 HNL-LIH. SEAT 11A LIFE VEST WAS MISSING. MX INSTALLED A NEW LIFE VEST. 2 L 7 2 4F RT A21EA 2007101900219 20071019 00219 EA 2007 10 19 MASA200700485 1 20070806 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA LAVATORY ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 97325 7325 ASH 2712 LAS-FAT RETURNED TO THE FIELD DUE TO A SMOKE SMELL IN THE LAV. MX RAN PACKS OFF ENG, OPS CHECKED NORMAL. CHEC KED WIRING AND BALLASTS AND OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2007101900228 20071019 00228 EA 2007 10 19 MASA200700330 1 20070615 A 2612 FIRE LOOP CNDAIR CL600 CL6002B19 1900309 EA APU OUT OF POSITION A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 37208 7208 ASH 7447 IAD. APU FIRE WARNING MESSAGE IN FLIGHT. MAINTENANCE REPOSITIONED LOOPS. 2 L 7 2 4F RT A21EA 2007101900229 20071019 00229 EA 2007 10 19 MASA200700331 1 20070616 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA DOOR OUT OF POSITION A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37218 7218 ASH 2764 PHX. OUTER HANDLE WILL NOT STOW WHEN F/A CLOSES DOOR. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007101900243 20071019 00243 EA 2007 10 19 MASA200700374 1 20070606 A 5311 FS640 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 77331 7331 MODIFICATION OF THE FRAME AT FS 640 CRACKED. REPAIRED FRAME. 2 L 7 2 4F RT A21EA 2007101900244 20071019 00244 EA 2007 10 19 MASA200700375 1 20070615 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 97325 7325 CRACKED INTERCOSTAL AT FS 625.3 STR 14. REPAIRED CRACKED INTERCOSTAL. 2 L 7 2 4F RT A21EA 2007101900249 20071019 00249 EA 2007 10 19 MASA200700383 1 20070630 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR FAULTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27318 7318 ASH 2721 PHX. MAIN PAX DOOR HANDLE WILL NOT STOW. MX INSPECTING DOOR. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007101900254 20071019 00254 NM 2007 10 19 SWAA075037 1 20071010 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 945, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007101900285 20071019 00285 EA 2007 10 19 TRAX200701483 1 20071008 A 2560 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 908EV 7654 EXIT SIGN ROW 8 BROKEN. 2 L 7 2 4F RT A21EA 2007101900295 20071019 00295 EU 2007 10 19 MALA070147 1 20070912 A 5753 RIB SAAB SF340 340B 7860101 EU LT TE FLAP CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 415XJ 340B415 LT FLAP, AFT COVE RIB IS CRACKED AND HAS SHEARED RIVET. REPLACED AFT COVE RIB ON LT FLAP P/N 7257840-081. 2 L 7 2 4T RT A52EU 2007101900296 20071019 00296 SO 2007 10 19 C2XA07IA221 1 20071010 A 3397 W101851220 WIRE EMB 145 EMB145LR 3260212 SO CABIN BROKEN A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 27 13994 145291 MCI - FLIGHT 2955, THE CREW REPORTED THAT THE EMERGENCY LIGHTS ILLUMINATE INTERMITTANTLY DURING FLIGHT. THE AIRCRAFT LA NDED AT MCI WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH N O DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE DISCREPANCY REPEATED ON FLIGHT 2547 INTO IAH, WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPAIRED THE WIRING AT J8524, OPERA TIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007101900324 20071019 00324 EU 2007 10 19 MALA070158 1 20070912 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 339-363 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 415XJ 340B415 RT FUSELAGE SKIN DENTS STA 339-363, SL 1615-1616. REPAIRED PER EOS53009. 2 L 7 2 4T RT A52EU 2007101900330 20071019 00330 EU 2007 10 19 CPCP200700110 1 20070919 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 425MJ 425 FLOORBEAM FR 38, TOP SURFACE IS CORRODED BETWEEN STR 17-20 AND UNDER CLIPNUT. FLOORBEAM AT FRAME 38 REPAIRED AS PER SRM 53-00-00 FIG 450. 2 H 7 2 4T RT A53EU 2007101900340 20071019 00340 NM 2007 10 19 GTIA200700028 1 20071001 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM BS 765 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 516NK 2704 FLOORBEAM BETWEEN Y STATIONS -765 AND -254 AT FR 68 CORRODED. REPLACED DAMAGED AREA. 2 L 7 2 4F RT A28NM 2007101900353 20071019 00353 NM 2007 10 19 AALA20071911 1 20071009 A 3040 CONTROL UNIT BOEING 757 757223 1384957 NM WINDOW HEAT SMOKE A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 662AA 25296 JFK INFLIGHT T160/09OCT - SMOKE REPORTED FROM ELECTRICAL CONNECTOR AT LOWER LEFT CORNER OF CAPTAINS FORWARD WINDOW. WI NDOW HEAT SWITCHED TURNED OFF AND SMOKE DISSIPATED. LANDED JFK WITHOUT INCIDENT. REPLACED FORWARD WINDOW AND WINDOW HE AT CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007101900359 20071019 00359 NM 2007 10 19 AALA20071913 1 20071010 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 946AN 30600 MIA - EMERGENCY LIGHT IN COCKPIT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IN COCKPIT. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT A16WE 2007101900360 20071019 00360 EU 2007 10 19 AALA20071917 1 20071010 A 2780 SLAT SYSTEM AIRBUS 300 A300B4605R 3930308 EU JAMMED A AALA O OTHER J WARNING INDICATION LD LANDING 1 SW 21 14056 463 BOG INFLIGHT T915/10OCT - ZERO SLAT LOCKOUT ON LANDING. LANDED BOG WITHOUT INCIDENT. ACCOMPLISHED BITE TO SLAT FLAT CO NTROL COMPUTERS ONE AND TWO. FAULTS SLAT JAM AND FLAP SUPPLY RESET AND CLEARED. UNABLE TO DUPLICATE. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007101900374 20071019 00374 NM 2007 10 19 EIA2007174 1 20070916 A 5311 FRAME BOEING 747 747132 1384882 NM BS 488 S25L CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 MAIN DECK BS 488 LT FRAME WEB FOUND CRACK AT STR 25 AREA. MAIN DECK BS 488 LT FRAME WEB REPAIRED PER SRM 53-10-04 FIG 9 2. 2 L 7 4 4F A20WE 2007102200019 20071022 00019 EU 2007 10 22 2007UALA04207 1 20071013 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU CREW READS LOW A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 472UA 1435 CREW O2 LOW. 10-26-07 PRE SVC LEVELS WERE RECORDED AT 1500 PSI. NO INFO AVAILABLE AS TO SERVICE PERFORMED OR JUST AN INCORRECT PILOT ASSESSMENT. 2 L 7 2 4F RT A28NM 2007102200141 20071022 00141 NM 2007 10 22 SWAA075058 1 20071014 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 410 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, BL 0. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007102200145 20071022 00145 NM 2007 10 22 UPS07M50926 1 20070807 A 5730 SKIN DOUG MD11 MD11F 3023600 NM LT WING CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C LT WING LEADING EDGE SKIN CHAFED AT SLAT TRACK NR 2 AREA STICKER 5712. LT WING L/E SKIN CHAFED AT SLA T TRACK NR 2 AREA CHAFED MARK REMOVED FOUND W/N LIMIT & REPROTECTED. HFEC INSP C/OUT FOUND CRACK APPROX .75 INCH LONG W ING L/E ACCESS PANEL 515BT & NR 2 SLAT TRACK DOOR REMOVED. REPAIR DOUBLER & FILLER FAB PER EN1621-07. REPAIR DOUBLER & FILLER HOLES, PICKED UP PAINTED & INSTALLED. NR 2 SLAT TRACK DOOR PNL 515BT INSTALLED. 2 L 7 3 4F RT A22WE 2007102200146 20071022 00146 NM 2007 10 22 USAA920070929 1 20071012 A 5313 STRINGER SPLICE BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C-20 CHECK, CRACKED STRINGER SPLICE, BS 360, S14L. REPLACED STRINGER SPLICE, BS 360, S14L IAW B737 -300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007102200147 20071022 00147 WP 2007 10 22 ASAA0782103 1 20071014 A 5320 9936534139 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP BS 160-200 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 REMOVED DAMAGED CABIN FLOOR TRACK, LOCATED, DRILLED AND INSTALLED A REPLACEMENT TRACK IAW MD80 SRM 51-10-4 PG 1. 2 L 7 2 4F RT A6WE 2007102200148 20071022 00148 NM 2007 10 22 ASAA0792093 1 20071009 A 5320 INTERCOSTAL BOEING 737 737990 NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 305AS 30013 AFT CARGO PIT LT INTERCOSTAL RACK CORRODED AT BS 727. REPAIRED INTERCOSTAL RACK IAW SRM 53-00-53. 2 L 7 4 4F RT A16WE 2007102200149 20071022 00149 NM 2007 10 22 ASAA0742096 1 20071005 A 5320 654580731 INTERCOSTAL BOEING 737 7374Q8 138447Q NM BS 294 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 MAIN CABIN AT FWD SERVICE DOOR CUTOUT BS 294 BETWEEN STR 11R AND 12R HAS CRACK IN AFT END OF INTERCOSTAL ANGLE. REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE IAW B737 SRM 51-40-2 AND BAC DWG 65 45007. 2 L 7 2 4F RT A16WE 2007102200150 20071022 00150 NM 2007 10 22 ASAA0742097 1 20071005 A 5340 654580730 ATTACH ANGLE BOEING 737 7374Q8 138447Q NM BS 294 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 MAIN CABIN AT FWD SERVICE DOOR CUTOUT BS 294 BETWEEN STR 12R AND 13R CRACK IN AFT END OF INTERCOSTAL ANGLE. REMOVED AND REPLACED ANGLE IAW B737 400 SRM 51-40-2 AND BAC DWG 65 45807. 2 L 7 2 4F RT A16WE 2007102200152 20071022 00152 SO 2007 10 22 RAIA00710012 1 20071014 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 816HK 145055 PRE FLT NR 5497 - STL - EMERGENCY LIGHT FLOOR STRIP FLOOR PROXIMITY LIGHTS INOP. MAINTENANCE RESECURED WIRING TO FLOOR STRIP EMERGENCY LIGHT AND RESET POWER, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007102200155 20071022 00155 NM 2007 10 22 SWAA075059 1 20071014 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 430 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, BL 1. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007102200157 20071022 00157 NM 2007 10 22 ASAA0752104 1 20071014 A 2840 3012803 PROCESSOR BOEING 737 737890 1384527 NM FUEL QTY INTERMITTENT A ASAA O OTHER O OTHER DE DESCENT 1 NM 02 557AS 35176 CENTER FUEL QUANTITY AND TOTAL FUEL QUANTITY DISPLAYS ARE BLANK. DISPLAYS RETURNED DURING APPROACH. COMPLETED FQIS CUR RENT STATUS & GROUND TESTS. BOTH PASS, NO FAULTS. NO HISTORY 90 DAYS. 2 L 7 2 4F RT A16WE 2007102200158 20071022 00158 NM 2007 10 22 UPS07M50927 1 20070807 A 5712 RIB DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C LEFT WING LEADING EDGE HAS NOSE RIB CRACKED BETWEEN SLAT TRACKS 12 AND 13 STICKER 7058. CRACKED RIB R EMOVED. NEW RIB FABBED USING MAT'L 7075-0-0.040" PER DWG ARB2922. RIB HEAT TREATED AS PER DPS 7.00-1 & HARDNESS VALUES HRB 83.1 AS PER DPS 1.05-3. NEW RIB HOLES PICKED UP AND PROTECTED. NEW RIB PAINTED & INSTALLED. 2 L 7 3 4F RT A22WE 2007102200161 20071022 00161 NM 2007 10 22 ZZDA2007282 1 20071010 A 5311 FRAME BOEING 717 717200 1383700 NM BS 1178 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 956AT 55018 AFT ACCESSORY COMP CANTE FRAME CRACKED, FS 1178 BELOW LONG 17 LT. INSTALLED FORMED ANGLE REPAIR PER SRM 51-70-11. 2 L 7 2 4F TR A6WE 2007102200165 20071022 00165 SO 2007 10 22 C2XA07TY060 1 20071015 A 5542 DOUBLER EMB 145 EMB145LR 3260212 SO RUDDER MISSING A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14953 145071 TYS - A/C WAS FOUND WITH A NUT PLATE MISSING AND THE HOLE ELONGATED ON THE RUDDER 2. MAINTENANCE FABRICATED A FILLER AN D A INTERNAL DOUBLER. ALODINED AND EPOXY PRIMED THE PARTS. INSTALL FABRICATED PARTS ON THE RUDDER IAW EC 5540--01077. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007102200166 20071022 00166 NM 2007 10 22 SWAA075082 1 20071015 A 5553 6545166 ROD END BOEING 737 7373H4 1384600 NM VERTICAL STAB BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 14Y CHECK, FOUND VERTICAL STABILIZER STANDBY ACTUATOR, INPUT ROD END BROKEN. REMOVED AND REPLACED ROD END PER MM. 2 L 7 2 4F RT A16WE 2007102200167 20071022 00167 NM 2007 10 22 2007UALA04195 1 20071012 A 3350 LAMP BOEING 747 747422 1384935 NM EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY EXIT LIGHT INOP AT DOOR 5 LEFT BUSTLE. 11-01-07 REPLACED LAMP ASSY. 2 L 7 4 4F RT A20WE 2007102200169 20071022 00169 NM 2007 10 22 2007UALA04216 1 20071014 A 5330 SKIN BOEING 757 757222 1384956 NM BS 430 S22-23R BURNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 BURN IN SKIN STA 430 BETWEEN STR 22R AND 23R & ADJACENT FASTENER AT STA 385 AND STR 24R. MAJOR REPAIR ACCOMPLISHED. R EMOVED BURN AND INSTALLED BLIND FASTENERS AND SKIN REPAIR. 2 L 7 2 4F RT A2NM 2007102200170 20071022 00170 NM 2007 10 22 2007UALA04225 1 20071014 A 2612 SMOKE DETECTOR BOEING 767 767322 1385200 NM LT LAVATOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 648UA 25285 MID LEFT LAVATORY HAS INOP SMOKE DETECTOR. REPLACED SMOKE DETECTOR. OP CHECKS OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007102200171 20071022 00171 NM 2007 10 22 2007UALA04233 1 20071013 A 3350 SIGN BOEING 747 747422 1384935 NM EMERGENCY EXIT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY EXIT SIGN DOOR 3L BELOW MONITOR INOP. REPLACED BULB OP CHECKED NORMAL. 2 L 7 4 4F RT A20WE 2007102200172 20071022 00172 2007 10 22 2007UALA04241 4 20071013 A 2565 GIRT BAR BOEING 747 747422 1384935 NM L4 DOOR OUT OF ADJUST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 DOOR 4L WILL NOT ARM. DOOR 4L GIRT BAR READJUSTED. OP CHECKS GOOD. 2 L 7 4 4F RT A20WE 2007102200173 20071022 00173 NM 2007 10 22 2007UALA04242 1 20071014 A 3350 LIGHT BOEING 747 747422 1384935 NM ROW 49 HJK INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY EXIT EEL LIGHT INOPERATIVE AT ROW 49 HJK. 11-01-07 REPLACED LIGHT ASSY. OPS CHECKED NORMAL. 2 L 7 4 4F RT A20WE 2007102200174 20071022 00174 NM 2007 10 22 2007UALA04243 1 20071014 A 3350 LAMP BOEING 747 747422 1384935 NM EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY EXIT LIGHT INOP AT CEILING ROW 6L. 11-01-07 RELAMPED. 2 L 7 4 4F RT A20WE 2007102200181 20071022 00181 NM 2007 10 22 KCSA071475 1 20071016 A 5210 WEB BOEING 747 7472B4B 138481B NM L1 DOOR CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 L-1 DOOR INNER WEB CORRODED INSIDE DOOR AT STA 445 WL 251. 2 L 7 4 4F RT A20WE 2007102200189 20071022 00189 NE 2007 10 22 SA07065 2 20071011 A 7200 ENGINE AIRBUS A321 A321211 3930370 EU CFMINT CFM56 CFM565B42P 13013 NE RIGHT STALLED A USAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 EA 19 172US 1472 MCI FLT 1167 EN ROUTE CLT TO MCI. AT FL 320, THE RIGHT ENGINE HAD A COMPRESSOR STALL AND WENT TO IDLE. THE FLIGHT DES CENDED TO FL 180 AND PERFORMED AN IN-FLIGHT START OF THE ENGINE. THE ENGINE REMAINED AT MINIMUM POWER. THE FLIGHT DIVE RTED TO MCI. UPON TOUCHDOWN, THE NUMBER TWO ENGINE SHUTDOWN AGAIN. SINGLE ENGINE TIME WAS 42 MINUTES. MAINTENANCE ACT ION PENDING. 2 L 7 2 4F 4 F RT A28NM 2007102200206 20071022 00206 NM 2007 10 22 2007UALA04204 1 20071012 A 5210 CYLINDER AIRBUS A319 A319131 3930317 NM DOOR ASSIST READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 846UA 1600 DOOR 2R EMERGENCY CYLINDER ACCUMULATOR PRESSURE IS LOW. 10-26-07 SERVICED CYLINDER- NO REPEATS. 2 L 7 2 4F RT A28NM 2007102200208 20071022 00208 NM 2007 10 22 KCSA071469 1 20071015 A 3350 LIGHT BOEING 747 747209F 1384800 NM EMERGENCY EXIT INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 704CK 22299 UPPER DECK RIGHT AFT EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE BS 570. 2 L 7 4 4F RT A20WE 2007110800072 20071108 00072 NM 2007 11 8 ASAA0772164 1 20071018 A 5320 146A75021 CHANNEL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 AFT CARGO PIT LT ZEE CHANNEL FROM BS 727+4 BS 847 LBL 21 CORRODED. ZEE CHANNEL REPLACED 727+4 TO BS 847 LBL 21. 2 L 7 2 4F RT A16WE 2007102200216 20071022 00216 NM 2007 10 22 SWAA075061 1 20071014 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 779-792 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 779 AND BS 792, STR 18L AND STR 19L. REPAIRED SKIN P ER SRM. 2 L 7 2 4F RT A16WE 2007102200218 20071022 00218 NM 2007 10 22 SWAA075065 1 20071014 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM BS 930 S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007102200220 20071022 00220 NM 2007 10 22 SWAA075068 1 20071014 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007102200221 20071022 00221 NM 2007 10 22 SWAA075072 1 20071014 A 5753 65C30462 SKIN BOEING 737 7375H4 138449D NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED 18Y CHECK, FOUND RIGHT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007102200222 20071022 00222 2007 10 22 SWAA075062 4 20071014 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED A2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF AJDJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007102200223 20071022 00223 NM 2007 10 22 SWAA075087 1 20071015 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM BS 806 S19L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 806, STR 19L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007102200224 20071022 00224 NM 2007 10 22 SWAA075078 1 20071015 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 779-792 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 779 AND BS 792, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007102200228 20071022 00228 SO 2007 10 22 RAIA007100007 1 20071010 A 3350 BULB EMB 145 EMB145 3260210 SO EMERGENCY LIGHT BURNED OUT A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 807HK 145119 POST FLT NR 3568 - PIT - AFT CEILING EMERGENCY SIGN AISLE FLOOD LIGHT INOP. MAINTENANCE RELAMPED EMERGENCY LIGHT, OPS C HECK GOOD AT THIS TIME. 2 L 7 2 4F RT T00011AT 2007102200229 20071022 00229 SO 2007 10 22 RAIA007100008 1 20071011 A 3350 316 BULB EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS BURNED OUT A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 805HK 145096 POST FLT NR 3551 - PIT - PAX DOOR HAND-RAIL EMERGENCY LIGHT OUT. MAINTENANCE REMOVED AND REPLACED BULB ON HANDRAIL, OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT T00011AT 2007102200233 20071022 00233 NM 2007 10 22 UPS07450908 1 20071010 A 5313 STRINGER BOEING 747 747200 1384847 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 STR 45L DAMAGED. REMOVED STR 45L DAMAGE AS PER SRM 53-10-03. FABRICATED SPLICES FOR REPAIR AS PER SRM 53-10-03. INSTA LLED NEW STRINGER AND SPLICES AS PER SRM 53-10-03. 2 L 7 4 4F RT A20WE 2007102200243 20071022 00243 EU 2007 10 22 TRAX200701126 1 20070806 A 5320 SUPPORT ANGLE AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 CORROSION FOUND ON STIFFENER SUPPORT ANGLE LT SIDE AT FR 26 BL 0. CORROSION REMOVED ON STIFFENER SUPPORT ANGLE LT SIDE AT FR 26 BL 0 AS PER SRM 51-21-42, MATERIAL THICKNESS 0.040, MATERIAL REMOVED 0.003 WITHIN LIMITS AS PER SRM 53-51-00 FI G 301. SUPPLEMENTAL - SDR CLOSED 10/18/07. 2 H 7 2 4T RT 2007102200247 20071022 00247 WP 2007 10 22 ABXR070345 1 20070927 A 5320 99578608 ANGLE DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 231US 48114 RIGHT ANGLE CRACKED STA 69.550 TO 83.550 X = 10.00. REPLACED ANGLE IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 2007102300002 20071023 00002 EU 2007 10 23 200710161 1 20071012 A 2910 158508601HP FITTING EMB ERJ170 ERJ170100SE 3260406 EU HYDRAULIC SYSTEM CHAFED A UHLA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 GL 11 868RW 17000131 FLIGHT 6496 DFW TO JFK IN CRUISE, CREW HAD A HYDRAULIC 2 LOW QUANTITY EICAS MESSAGE FOLLOWED BY LOSS OF HYDRAULIC 2 SYST EM PRESSURE. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND A UNION FITTING C HAFED AND LEAKING AT NR 2 ENGINE HYDRAULIC PUMP HIGH PRESSURE LINE. REMOVED AND REPLACED FITTING. NR 2 ENGINE HYDRAULI C PUMP WAS REPLACED AS A PRECAUTIONARY MEASURE DUE TO LOSS OF SYSTEM 2 PRESSURE. 2 L 7 2 4F RT A56NM 2007102300005 20071023 00005 CE 2007 10 23 DXTA200702544 1 20071015 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 316QS 5600516 WHEN TAXIING AND MAINTAINING LIGHT BRAKE PRESSURE ON BOTH BRAKE PEDALS, RT PEDAL PRESSURE DROPS AND PEDAL DEPRESSES ALL THE WAY TO STOP. BLED BOTH LT AND RT BRAKES IAW CE-560 MM, CHAPTER 32-42-00. OPERATIONAL CHECKS GOOD. FOR DETAILS OF W ORK ACCOMPLISHED, SEE EJM HPN WO 8216. 2 L 7 2 4F 4 F RT A22CE E25EA 2007102300018 20071023 00018 CE 2007 10 23 GUUA10100701 1 20071010 A 2497 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CHAFED A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 29 53545 UE185 FLIGHT:9152 EYW/TPA DURING APPROACH ADF BEGAN SMOKING AND CIRCUIT BREAKER POPPED TURNED OFF ADF AND SMOKE CEASED. CONTIN UED, LANDED WITHOUT INCIDENT. REPAIRED CHAFED WIRE SYSTEM OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2007102300024 20071023 00024 NM 2007 10 23 SWAA075093 1 20071016 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 262WN 32519 DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007102300028 20071023 00028 NM 2007 10 23 SWAA075103 1 20071016 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT AIR CONDITIONER HOOK UP CUTOUT, BS 510, STR 28L. REPAIRED SK IN PER SWA EA. 2 L 7 2 4F RT A16WE 2007102300029 20071023 00029 NM 2007 10 23 SWAA075105 1 20071016 A 5330 6545866 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 DURING SCHEDULED HC2 CHECK, FOUND RT KEEL BEAM PANEL CRACKED AT BS 685. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007102300031 20071023 00031 NM 2007 10 23 SWAA075109 1 20071016 A 5311 6546555 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007102300040 20071023 00040 NM 2007 10 23 USAA920070949 1 20071015 A 3250 C247360012 SERVO VALVE AIRBUS A319 A319132 3930340 NM NLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 834AW 11687 11687 2302 PHX - EL - FLT 565 - CREW REPORTED DURING CLIMB, CREW RAISED GEAR, AFTER GEAR WAS UP CREW RECEIVED AN ECAM NOSE WHEEL ST EERING FAULT MESSAGE. CREW RECYCLED THE ANTI SKID AND NOSE WHEEL STEERING SWITCH AND THE N/W/S FAULT MESSAGE CLEARED AN D THAN RETURNED. THE CREW DECLARED AN EMERGENCY, RETURNED TO PHX. THE LANDING WAS UNEVENTFUL. THE A/C WAS TOWED TO TH E GATE. MX REPLACED THE NOSE LANDING GEAR CONTROL SERVO. OPERATIONAL CHECK WAS GOOD. THE A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2007102300041 20071023 00041 NM 2007 10 23 WRLA2007113 1 20071015 A 5347 AFA7789548 SEAT TRACK DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 273WA 48519 DURING 4C+12A CHECK, FOUND RIGHT AFT FLOOR CURVED SEAT TRACK HAS CORROSION AT STA Y=2007 X=107.25. PER MD11 SRM VOL.I 5 3-70-00 FIG. 1 REV.40. 2 L 7 3 4F 4 F RT A22WE E24NE 2007102300042 20071023 00042 EU 2007 10 23 BA07015 1 20071016 A 2120 33215590001 ACTUATOR AIRBUS 330 A330323 3930335 EU RAM AIR INLET FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 277AY 0380 FLIGHT 718, PHL-FCO: CREW REPORTED THAT THE RIGHT PACK TEMPERATURE WOULD INCREASE ANYTIME THE THROTTLES WERE ADVANCED. FLIGHT RETURNED TO PHL. MAINTENANCE REPLACED THE RIGHT RAM AIR INLET ACTUATOR. 2 L 7 2 4F RT A46NM 2007102300044 20071023 00044 EA 2007 10 23 COMA0770054 1 20071007 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR ACTIVATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 642CA 10125 FLIGHT 5070 - PAX DOOR OUTER HANDLE MESSAGE ON T/O. T/O ABORTED SAFELY. TRANSFERRED TO DMI LIST PER MEL 52-70-01. 2 L 7 2 4F RT A21EA 2007102300045 20071023 00045 EA 2007 10 23 COMA0770055 1 20071010 A 2150 GG670950093 ACM CNDAIR CL600 CL6002C10 1390015 EA A/C BAY FAILED A COMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 369CA 10750 10079 FLIGHT 5128 - RIGHT PACK SMOKING. REMOVED AND REPLACED RIGHT ACM. 2 L 7 2 4F RT A21EA 2007102300049 20071023 00049 EA 2007 10 23 COMA0770057 1 20071016 A 5347 SH670RPA0045 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 690CA 7565 10182 FLIGHT 5347 - RIGHT SIDE SEAT TRACK RAILS HAVE CORROSION AND GOUGES BETWEEN FS 533 TO FS 830. BLENDED CORROSION/GOUGES AND REPLACED TRACK SECTION AT FS 784 - FS 830 IAW REO 670-53-00-074. 2 L 7 2 4F RT A21EA 2007102300056 20071023 00056 NM 2007 10 23 AMTA200700491 1 20071012 A 5414 SKIN BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE NACELLE CRACKED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 UPON REMOVAL OF HEAT SHIELD ON NR 1 STRUT OB SIDE FOUND SKIN, INTERNAL DOUBLER AND SHIM CRACKED AT PRECOOLER LANDING APP ROX PP STA 182.00. (K) REPAIRED PER SAA EA 757-5450-09-A1018. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2007102300059 20071023 00059 NM 2007 10 23 USAA920070951 1 20071011 A 5754 65C26602223 SLAT BOEING 737 7373G7 1384595 NM LT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 PHX - MAJOR REPAIR - LEFT WING NR 2 SLAT DELAMINATED. REMOVED, REPAIRED AND REINSTALLED THE LEFT WING NR 2 SLAT IAW B73 7 AMM 27-81-00 AND 57-41-01. 2 L 7 2 4F RT A16WE 2007102300060 20071023 00060 NM 2007 10 23 USAA920070952 1 20071017 A 5320 143N833825 INTERCOSTAL BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 903AW 23323 MCN - MAJOR REPAIR - C-12 CHECK - CRACKED INTERCOSTAL, BS 680, S12R. REPLACED INTERCOSTAL, BS 680 - BS 686, S12R IAW TA SK CARD M1C53606. 2 L 7 2 4F RT A2NM 2007102300061 20071023 00061 NM 2007 10 23 USAA920070953 1 20071017 A 5320 143N833427 INTERCOSTAL BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 903AW 23323 MCN - MAJOR REPAIR - C-12 CHECK - CRACKED INTERCOSTAL, BS 680, S12L. REPLACED INTERCOSTAL, BS 680, S12L IAW TASK CARD M 1C53608. 2 L 7 2 4F RT A2NM 2007102300062 20071023 00062 CE 2007 10 23 16KB10 1 20071015 A 3213 62412092 STRUT CESSNA 650 650 2076802 CE LT MLG LEAKING E DBCA K NONE O OTHER IN INSP/MAINT 1 GL 13 16KB 7332 145 6507008 POSTFLIGHT ON ARRIVAL AT STL CREW NOTED LEFT MLG STRUT WAS LOW. LEFT MLG STRUT WAS REPLACED WITH A RENTAL UNIT. ORIGIN AL STRUT WAS SENT TO VENDOR FOR OVERHAUL. 2 L 7 2 4F A9NM 2007102300063 20071023 00063 CE 2007 10 23 DXTA200702521 1 20071003 A 3260 DOWNLOCK SWITCH CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RT MLG OUT OF ADJUST E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 916QS 7500116 AFTER TAKEOFF GEAR WAS RETRACTED RIGHT MAIN STILL HAD GREEN DOWN LIGHT ON, RED IN TRANSIT LIGHT WAS OFF. VERIFIED DISC REPANCY. ADJUSTED RT MAIN GEAR DOWNLOCK SWITCH. CYCLED LANDING GEAR. OPS CHECK GOOD. WORK DONE IAW CESSNA 750 MAINTENANC E MANUAL CHP 32-30-04. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007102300064 20071023 00064 CE 2007 10 23 2007F00058 1 20071008 A 5610 WINDSCREEN BEECH 200 B200 1152922 CE PWA PT6 PT6* 52043 EA COCKPIT CRACKED E A UNSCHED LANDING O OTHER CR CRUISE 1 SW 13 277GE 6820 BB1389 COPILOTS WINDSHIELD INNER PANE CRACKED. 1 L 7 2 4T 3 T A24CE E2NE 2007102300079 20071023 00079 EA 2007 10 23 COMA0760591 1 20071002 A 3230 46193 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 819CA 15453 7415 FLIGHT 5604 - NOSE LANDING GEAR DID NOT EXTEND. FOLLOWED QRH, GEAR EXTENDED, LANDED WITHOUT INCIDENT. REPLACED MLG PRI ORITY VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007102300081 20071023 00081 EA 2007 10 23 COMA0760606 1 20071002 A 3230 400019000001 BYPASS VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 819CA 18635 7415 FLIGHT 5604 - NOSE LANDING GEAR DID NOT EXTEND. FOLLOWED QRH, GEAR EXTENDED, LANDED WITHOUT INCIDENT. REPLACED NLG RUN AROUND BYPASS VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007102300082 20071023 00082 EA 2007 10 23 NAH2007F00000 2 20070907 A 8530 71133 NUT PIPER PA23 PA23250 7102308 SO LYC O540 IO540C4B5 41532 EA NR 3 CYLINDER FAILED E NAHA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 EA 17 62BA 274859 L186848 NR 3 CYLINDER DEPARTED THE ENGINE AFTER FAILURE OF THE CYLINDER HOLD DOWN NUTS TO MAINTAIN PROPER TORQUE. (3) ADDITIONA L CYLINDERS FROM THE SAME ENGINE WERE INSPECTED REVEALING (5) MORE UNDER TORQUED CYLINDER HOLD DOWN NUTS. 1 L 7 2 3O 3 O 1A10 1E4 2007102300084 20071023 00084 EA 2007 10 23 COMA0760592 1 20071001 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYSTEM FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 819CA 12614 7415 FLIGHT 5054 - NOSE GEAR DISAGREE MESSAGE ON APPROACH. QRH COMPLIED WITH, AIRCRAFT LANDED SAFELY. FOUND HYD SYSTEM NR 3 3A ACMP TO HAVE LOW PRESSURE. REMOVED AND REPLACED HYD SYSTEM NR 3, 3A ACMP. 2 L 7 2 4F RT A21EA 2007102300085 20071023 00085 EA 2007 10 23 COMA0760593 1 20071003 A 2751 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 931CA 955 7037 FLIGHT 5616 - RECEIVED FLAP FAIL INDICATION. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LT BPSU. NO FURTHE R DEFECTS. 2 L 7 2 4F RT A21EA 2007102300090 20071023 00090 EA 2007 10 23 COMA0760594 1 20071005 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 781CA 7312 FLIGHT 5670 - FLAPS FAIL MESSAGE WHEN SELECTING 8 TO 20 DEGREE FLAPS. AIRCRAFT LANDED SAFELY. COMPLIED WITH AD 2006-12 -21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007102300096 20071023 00096 CE 2007 10 23 DXTA200702532 1 20071010 A 3230 LANDING GEAR BEECH MU300 400A 1155402 CE MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 138QS RK492 AFTER TAKEOFF, GEAR RETRACTED BUT IN TRANSIT RED LIGHT IN HANDLE DIDN'T GO OUT. TOWER REPORTED AT LEAST BOTH MAIN GEAR D OORS WERE OPEN. 11-01-07 JACKED AIRCRAFT, PERFORMED 5 GEAR SWINGS. NO DEFECTS NOTED. INSPECTED ALL GEAR UPLOCK HOO KS, SWITCHES AND RIGGING. NO DEFECTS NOTED. INSPECTED NOSE GEAR DOOR RIGGING. NO DEFECTS NOTED. PERFORMED 5 MORE GEAR SW INGS NOTING NO DEFECTS. NOTED NO PRIOR RELATED DISCREPANCIES. OPERATIONAL CHECK GOOD AT THIS TIME. ALL WORK IAW CH 32-0 2-03 OF THE H-400 M.M. 2 H 7 2 4F RT A16SW 2007102300099 20071023 00099 2007 10 23 AMWA87824 4 20071004 A 3422 HSI BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA COCKPIT ODOR A AMWA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 07 176YV 13655 2555 UE176 ELECTRICAL ODOR REPORTED IN COCKPIT ON CLIMBOUT. RETURNED TO FIELD AND MAINTENANCE VERIFIED THAT PROBLEM ORIGINATING IN CAPTAIN'S EHSI. REMOVED AND REPLACED UNIT, OPERATIONAL CHECK WAS SATISFACTORY. 2 L 7 2 4T 3 T RT A24CE E2NE 2007102300104 20071023 00104 EA 2007 10 23 TRAX200701507 1 20071015 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 878AS 7590 FS 484 CLIP CRACKED AT I/B SIDE OF LBL 36.0. 10-25-07 REMOVED UNSERVICEABLE CLIP AT FS 484 LBL 36.0. DUPLICATED I/ B CLIP AT F.S. 484 LBL 36.0 FROM .050" 7075 T-6 IAW CRJ 200 SRM 53-41-43 AND CRJ 200 SRM 51-24-16. OK TO ALODINE AND PRI ME. ALODINED, PRIMED, AND TOPCOATED IAW CRJ 200 SRM 51-25-00. OK TO INSTALL. INSTALLED SERVICEABLE CLIP TO I/B SIDE OF L BL 36.0 AT FS 484 IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21. REQUIRES BOLTS REINSTALLED TO RUDDER CONTROL CABLE FAIRLEADS. REINSTALLED BOLTS ON RUDDER CABLE FAIRLEADS IAW CRJ SRM 51-41-02. 2 L 7 2 4F RT A21EA 2007102300105 20071023 00105 EA 2007 10 23 TRAX200701508 1 20071015 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 878AS 7590 FS 484 CLIP CRACKED AT O/B SIDE OF LBL 27.0. 10-25-07 REMOVED UNSERVICEABLE CLIP AT FS 484 LBL 27.0. REMOVED HARDW ARE FROM RUDDER CONTROL CABLE PULLEYS. 13362. DUPLICATED O/B CLIP AT FS 484 LBL 27.0 FROM .063" 2024 T-3 IAW REO 601R-53 -41-059 AND CRJ 200 SRM 51-24-16. OK TO ALODINE AND PRIME. ALODINED PRIMED AND TOPCOATED IAW CRJ 200 SRM 51-25-00. OK TO INSTALL. INSTALLED SERVICEABLE CLIP TO O/B SIDE OF LBL 27.0 AT FS 484 IAW CRJ 200 SRM 51-42-21. RUDDER CABLE PULLEYS RE QUIRE REINSTALLATION. REINSTALLED RUDDER CABLE PULLEYS IAW CRJ SRM 51-41-02. 2 L 7 2 4F RT A21EA 2007102300107 20071023 00107 EA 2007 10 23 TRAX200701510 1 20071015 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA EXIT SIGN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 753EV 10169 L/R EMERGENCY EXIT LIGHTED EXIT SIGNS HAVE LIGHT BULBS OUT. 2 L 7 2 4F RT A21EA 2007102300108 20071023 00108 EA 2007 10 23 TRAX200701511 1 20071016 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 PLACARDS ON EMERGENCY ESCAPE HATCH REQUIRES REPLACEMENT. 10-25-07 REMOVED EMERGENCY ESCAPE HATCH PLACARDS IAW CRJ 200 AMM 11-10-03. INSTALLED SERVICEABLE PLACARDS OPEN P/N S1875, CLOSED P/N S1874, CURVED ARROW P/N S1887, EMERG. EXIT P USH AND P/N S1859 IAW CRJ 200 AMM 11-20-00. 2 L 7 2 4F RT A21EA 2007102300111 20071023 00111 EA 2007 10 23 TRAX200701512 1 20071016 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 PAX DOOR FWD ANCHOR FITTING IS CRACKED. 11-01-07 REMOVED UNSERVICEABLE PAX DOOR FWD ANCHOR FITTING IAW CRJ 200 AMM 52-11-17-400-803. OK TO INSTALL. INSTALLED FWD ANCHOR FITTING P/N 601R38074-6 PO 95-1202 IN SERVICEABLE CONDITION IAW C RJ 200 AMM STILL REQUIRES PIN FOR CABLE. INSTALLED SERVICEABLE UPPER PIN ON PAX DOOR FWD CABLE (PIN P/N MS20392-3C23) AS PER CRJ 200 52-11-17. REQUIRES OPS CHECK. PERFORMED OPS CHECK OF PAX DOOR COUNTERBALANCE AS PER CRJ 200 AMM 52-11-17. T ESTED GOOD. PERFORMED THE ADJUSTMENT OF PAX DOOR COUNTER BALANCE SYSTEM AS PER CRJ 200 AMM 52-11-17. 2 L 7 2 4F RT A21EA 2007102300113 20071023 00113 SO 2007 10 23 RAIA00710006 1 20071008 A 4900 APU EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL SMOKE A RAIA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 CE 03 850HK 145003 FLT NR 7986-IAD-ODOR IN COCKPIT, NO SMOKE. MAINTENANCE RAN ENGINES AND PACKS, OPERATING MANUAL FOUND ODOR TO BE FROM APU WITH PACKS RUNNING. APU TEMP TO HIGH WITH PACKS RUNNING. DEFERRED APU IAW MEL. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007102300117 20071023 00117 EA 2007 10 23 TRAX200701516 1 20071017 A 5320 BEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 722EV 10127 SURFACE CORROSION ON 280 TRANSVERSE BEAM ON UPPER SURFACE. 10-24-07 REMOVED SURFACE CORROSION ON 280 TRANSVERSE BEAM O N UPPER SURFACE IAW SRM 51-21-06. RT OUT OF LIMITS. REMOVE RT 280 FRAME & RBL 19 AND 27 INTERCOSTAL IAW CRJ 700 SRM 51-4 2-06 AND 51-42-21. REMOVED RT PITOT STATIC LINE IAW CRJ 700 AMM 34-11-00. CUT NEW 280 FRAME & DRILLED FASTNER HOLES LAB ELS DONE IAW IS67053110026. INSTALLED RT 280 FRAME IAW IS67053110026 & 280 FRAME SPLICE IAW REO 670-53-11-047. INSTALLE D FASTENERS IN ITANIUM DOUBLERS PER MODSUM IS67053110026 CONTINUE INSTALLATION OF FASTENERS THROUGH UPPER PORTION OF TIT ANIUM. FINISHED INSTALLATION OF RT SIDE OF 280 TRANSVERSE BEAM PER IS67053110026 AND REO 670-53-11-045. 2 L 7 2 4F RT A21EA 2007102300118 20071023 00118 EA 2007 10 23 TRAX200701517 1 20071017 A 5320 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA COCKPIT FLOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 722EV 10127 AFT COCKPIT FLOOR LAND AT FS 280 IS CORRODED. 10-24-07 REMOVED AFT COCKPIT FLOOR LAND AT FS 280 IAW CRJ 700 51-42- 06 AND 1-42-21. DRILLED UP NEW AFT COCKPIT FLOOR LAND WORK DONE IAW CRJ 700 SRM 51-42-06. INSTALLED AFT COCKPIT FLOORBOA RD ANGLE AND CAMLOCK RECEPTACLES (2) PER CRJ 700 SRM 51-42-06. COMPLIED WITH RII INSPECTION OF AFT COCKPIT FLOOR LAND INSTALLATION AT FS 280 PER ASA SP 607 AND CRJ 700 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007102300119 20071023 00119 EA 2007 10 23 TRAX200701520 1 20071017 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 722EV 10127 RBL 9 SEAT TRACK CORRODED AT FS 349.00. 2 L 7 2 4F RT A21EA 2007101900232 20071019 00232 EA 2007 10 19 MASA200700345 1 20070620 A 3250 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING MALFUNCTIONED A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 17156 7156 ASH 7414 IAD-MDT. PAX DOOR HANDLE WAS STICKING AND STEERING INOP CAUTION WITH GEAR EXTENDED ON LANDING. MX FOUND THE P AX DOOR HANDLE OPERATED NORMALLY AS WELL AS THE NWS STEERING. 2 L 7 2 4F RT A21EA 2007101900240 20071019 00240 NE 2007 10 19 MASA200700366 2 20070627 A 7261 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT ENGINE OVERSERVICED A MASA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 SW 07 75993 7372 ASH 7007 RDU. RIGHT ENGINE LOW OIL PRESSURE WARNING IN FLIGHT. CREW REPORTED GETTING THE RIGHT ENGINE LOW OIL PRESSURE WARNING IN FLIGHT WITH 25 PSI INDICATED. CREW DECLARED AN EMERGENCY AND DIVERTED TO PIT. CREW DID NOT SHUT DOWN THE E NGINE. FOUND OIL OVER SERVICED & DRAINED. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2007101900241 20071019 00241 EA 2007 10 19 MASA200700368 1 20070627 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37228 7228 ASH 2864 PHX. PAX DOOR WAS DIFFICULT TO OPEN FROM INSIDE. MX PERFORMED OPERATIONAL CHECKS OF THE DOOR AND FOUND NO FAU LTS. 2 L 7 2 4F RT A21EA 2007101900251 20071019 00251 EA 2007 10 19 MASA200700382 1 20070701 A 5240 LOCK CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37342 7342 ASH 7222 ORD. PILOT REPORTED THAT THE SERVICE DOOR RELEASE HANDLE WAS BROKEN. MX REPLACED THE LOCKING MECHANISM. 2 L 7 2 4F RT A21EA 2007101900252 20071019 00252 NM 2007 10 19 SWAA075031 1 20071010 A 3350 417A5704 CAP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 226WN 32494 EEPLS END CAP LOOSE AT ROW 1 ABC. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 2007101900255 20071019 00255 NM 2007 10 19 SWAA075032 1 20071010 A 5753 6546430130 SKIN BOEING 737 7373Q8 1384670 NM FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED C1 CHECK, FOUND RIGHT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER M M. 2 L 7 2 4F RT A16WE 2007101900263 20071019 00263 2007 10 19 SWAA075034 4 20071010 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007101900288 20071019 00288 EA 2007 10 19 TRAX200701486 1 20071009 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 879AS 7600 CEILING FORWARD MOST EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007101900289 20071019 00289 EU 2007 10 19 TRAX200701487 1 20071009 A 5210 DOOR AEROSP ATR72 ATR72 EU PAX DOOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 F/A REPORTS MAIN CABIN DOOR HARD TO OPEN. 2 H 7 2 4T RT 2007101900307 20071019 00307 EU 2007 10 19 MALA070154 1 20070912 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE MISREPAIRED A MALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 15 415XJ 340B415 PREVIOUS REPAIR ON BOTTOM FRAME, UPPER FLANGE REINFORCEMENT DOES NOT COMPLY WITH SRM 51-70-30. REMOVED OLD REPAIR AND IN STALLED NEW REPAIR IAW EOS53362. 2 L 7 2 4T RT A52EU 2007101900308 20071019 00308 EU 2007 10 19 MALA070155 1 20070912 A 5321 FLOOR PANEL SAAB SF340 340B 7860101 EU BS 176-186 MISREPAIRED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 415XJ 340B415 LT FLIGHT DECK FLOOR PREVIOUS REPAIR OUTBD OF CONTROL COLUMN STA 176 TO 186 IS NOT APPROVED FOR THIS PARTICULAR REPAIR. CORRECT REPAIR PERFORMED OF THE LT FLIGHT DECK FLOOR. 2 L 7 2 4T RT A52EU 2007101900319 20071019 00319 NM 2007 10 19 SWAA075049 1 20071011 A 5753 65C3570329 FLAP BOEING 737 7375H4 138449D NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED HC2 CHECK, FOUND LEFT WING OUTBOARD FOREFLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007101900323 20071019 00323 EU 2007 10 19 MALA070157 1 20070912 A 5730 SKIN PANEL SAAB SF340 340B 7860101 EU LT WING PUNCTURED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 415XJ 340B415 LT WING TRAILING EDGE UPPER SKIN PANEL PUNCTURE 3.0" FWD OF T/E ST WS 52. REPAIRED PER EOS51031. 2 L 7 2 4T RT A52EU 2007101900331 20071019 00331 EU 2007 10 19 CPCP200700111 1 20070919 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 425MJ 22428 FLOORBEAM AT FRAME 39, TOP SURFACE IS CORRODED AT STR 17, AND UNDER CLIPNUTS. FLOORBEAM AT FRAME 39 REPAIRED IAW SRM 53 -00-00 FIG 429. 2 H 7 2 4T RT A53EU 2007101900344 20071019 00344 NM 2007 10 19 AALA20071928 1 20071011 A 3040 141T480149 WINDSHIELD BOEING 767 767323 1385205 NM COCKPIT ARCED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 372AA 25199 CDG T062/11OCT - CAPTAINS NUMBER ONE WINDOW HAD ARCING. ARCING STOPPED WHEN LEFT FORWARD SWITCH TURNED OFF. REPLACED C APTAINS NUMBER ONE WINDSHIELD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007101900352 20071019 00352 NM 2007 10 19 AALA20071905 1 20071009 A 3350 BULB BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 951AA 29538 MIA - EMERGENCY LIGHT AT FORWARD OVERWING DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT FORWARD OVERWING DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007101900357 20071019 00357 NM 2007 10 19 AALA20071920 1 20071011 A 3397 WIRE BOEING 767 767223 1385123 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 335AA 22333 JFK - EMERGENCY LIGHT AT MID GALLEY LEFT INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHT AT MID GALLEY LEFT. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007101900369 20071019 00369 NM 2007 10 19 EIA2007153 1 20070827 A 3350 S1356B37 LIGHT BOEING 747 747273C 1384896 NM EMERGENCY EXIT NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 471EV 20651 EMERGENCY LIGHT UPPER DECK OVERHEAD CREW EXIT DOOR, NEAR FIRE WARNING PANEL, INOP. EMERGENGY LIGHT REPLACED PER B747 MM 33-51-00. OPS CHECKED GOOD. 2 L 7 4 4F A20WE 2007101900373 20071019 00373 NM 2007 10 19 EIA2007169 1 20070924 A 5310 WINDOW FRAME BOEING 747 747132 1384882 NM BS 340 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 BS 340 RT R3 WINDOW LOWER CORNER CRACKED. TRIMMED OUT CRACKED AREA, FABRICATED REPAIR AND INSTALLED PER B747 SRM 53-30- 03 FIG 49. 2 L 7 4 4F A20WE 2007102200004 20071022 00004 NM 2007 10 22 USAA920070934 1 20071012 A 5311 65465292 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6504944, CRACKED FRAME, BS 440, S9R. REPAIRED FRAME, BS 440, S9R IAW USAIRWAYS EA 120272. 2 L 7 2 4F RT A16WE 2007102200008 20071022 00008 NM 2007 10 22 ZZDA2007283 1 20071011 A 2420 762904E PCDU BOEING 717 717200 1383700 NM LEFT UNSERVICEABLE A ZZDA O OTHER H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 37 926AT 55078 ON TAKEOFF, RECEIVED LT GEN OFF, LOST LT SIDE OF AIRCRAFT NR 3 DU, RESET GEN, WILL NOT RESET. LOST LT DC BUSS. WENT T O EMERGENCY PWR. REMOVED AND REPLACED LEFT PCDU. 2 L 7 2 4F TR A6WE 2007102200011 20071022 00011 NM 2007 10 22 ZZDA2007285 1 20071010 A 5320 PAN BOEING 717 717200 1383700 NM CARGO DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 956AT 55018 AFT CARGO COMPT LOWER PAN CORRODED. INSTALLED LOWER JAMB PAN AND SPLICES AS PER B717 SRM 53-20-15 REPAIR 6. 2 L 7 2 4F TR A6WE 2007102200012 20071022 00012 NM 2007 10 22 SWAA075084 1 20071015 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 474WN 33861 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007102200013 20071022 00013 NM 2007 10 22 HNAA0700235 1 20071012 A 3397 06967 ELEC CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LIGHTS ODOR A HNAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 810EX 308 ELECTRICAL SMELL WAS NOTICED IN THE CABIN AROUND ROW 6. DEACTIVATED THE PASSENGER OVERHEAD LIGHTING SYSTEM. REPOSITION ED THE PLANE TO SBY, THEN SPLICED IN A NEW CONNECTOR, OPS CHECK WAS GOOD. ALSO PERFORMED A HIDDEN DAMAGE INSPECTION IAW MP&P WOL 2 33.1. 2 H 7 2 4T RT A13NM 2007102200029 20071022 00029 NM 2007 10 22 USAA920070948 1 20071016 A 5330 6545775 SKIN BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 168AW 23629 PHX - MAJOR REPAIR - DAILY - NR 4312054, FUSELAGE SKIN CRACK, BS 727E, S22R. MX REPAIRED FUSELAGE SKIN CRACK AT BS 727E , S22R IAW SRM 53-00-01-2R 31 DETAIL XII. 2 L 7 2 4F RT A16WE 2007102200034 20071022 00034 EA 2007 10 22 TRAX200701498 1 20071013 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 F/O'S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007102200035 20071022 00035 NM 2007 10 22 2007UALA04229 1 20071012 A 3350 SIGN BOEING 767 767322 1385200 NM COCKPIT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 664UA 29236 FLIGHT DECK EMERGENCY EXIT SIGN INOPERATIVE. REPLACED EMERGENCY EXIT SIGN ASSY IN FLIGHT DECK..OP'S CHECKED GOOD. 2 L 7 2 4F RT A1NM 2007102200038 20071022 00038 NM 2007 10 22 KCSA071471 1 20071015 A 5330 SKIN BOEING 747 7472B4B 138481B NM BS 460 S13L DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FUSELAGE SKIN DAMAGED ABOVE L-1 DOOR AT BS 460, STR 13L. 2 L 7 4 4F RT A20WE 2007102200043 20071022 00043 NE 2007 10 22 2007UALA04177 2 20071011 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2040 NE NR 1 SHUTDOWN A UALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 WP 29 571UA 26681 726667 FLIGHT DIVERTED DUE TO NR 1 ENGINE FOR INFLIGHT SHUTDOWN. 2 L 7 2 4F 4 F RT A2NM E17NE 2007102200045 20071022 00045 NM 2007 10 22 UPS07650911 1 20071014 A 4900 SWITCH BOEING 767 76734AF 1385212 NM APU BAY FAILED A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 322UP 27748 INSPECTION TYPE:ETOP DIVERSION - ETOPS - APU FAILED EN ROUTE WITH LT IDG ON DEFERRAL. DIVERTED TO BANGKOK. 10-24-07 R & R DOOR SWITCH, NO HELP. FOUND TARGET BRACKET ON DOOR BROKEN. REMOVED APU INLET DOOR PER MM 49-15-05. INSTALLED APU INLET DOOR PER MM 49-15-05. OPS CHECKS NORMAL. 2 L 7 2 4F RT A1NM 2007102200069 20071022 00069 NM 2007 10 22 CALA0700585 1 20071014 A 5313 65C35767 STRINGER BOEING 737 7373T0 1384582 NM BS 500C S26L CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14325 23455 FWD CARGO STA 500C S26L CORROSION. INSTALLED REPAIR AT S26L STA 500C IN FWD CARGO IAW SRM 53-00-03 REPAIR 1. 2 L 7 2 4F RT A16WE 2007102200070 20071022 00070 NM 2007 10 22 CALA0700586 1 20071015 A 5330 6545769 SKIN BOEING 737 7373T0 1384582 NM BS 500C CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14325 23455 FWD CARGO FUSELAGE SKIN HAS CORROSION AT STA 500C+18 LBL-17. SKIN REPAIR PER SRM 53-00-01 REPAIR 31 FIG 201. 2 L 7 2 4F RT A16WE 2007102200082 20071022 00082 NM 2007 10 22 SWAA075086 1 20071015 A 3350 PH22300L STRIP BOEING 737 7373Y0 1384671 NM EMERGENCY LIGHTS WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT FWD CABIN. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007102200091 20071022 00091 SO 2007 10 22 C2XA07RI090 1 20071015 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13956 145078 FLT 2216 - EWR - CREW REPORTED EMERGENCY EXIT LIGHT BY MAIN CABIN DOOR INOPERATIVE. EWR MX PERFORMED OPERATIONAL TEST S UCCESSFULLY AND NO FAULT FOUND. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007102200107 20071022 00107 NM 2007 10 22 USAA920070928 1 20071010 A 5340 6935352 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C-20 CHECK, CRACKED STRINGER TIE CLIP, BS 663, S10R. REPLACED STRINGER TIE CLIP, BS 663, S10R IAW B737-300 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007102200108 20071022 00108 NM 2007 10 22 HNAA0700236 1 20071012 A 3260 88722411872202 PROXIMITY SENSOR DHAV DHC8 DHC8102 2809003 NM RT MLG MALFUNCTIONED A HNAA O OTHER G MULTIPLE FAILURE CR CRUISE 1 EA 07 940HA 156 WEIGHT ON WHEELS CAUTION LIGHT ILLUMINATED ON GEAR RETRACTION & EXTINGUISHED ON GEAR EXTENSION. COMPLIED WITH PSEU TEST AND FOUND LEFT HAND OUTBOARD SENSOR FAULT AND NOSE LANDING GEAR RIGHT HAND TARGET FAULT. REMOVED AND REPLACED OUTBOARD PROX SENSOR & ADJUSTED LEFT AND RIGHT HAND NOSE LANDING GEAR WOW SENSORS IAW 32-61-00. 2 H 7 2 4T RT A13NM 2007102200114 20071022 00114 NM 2007 10 22 2007UALA04212 1 20071013 A 5246 SKIN BOEING 737 737322 1384676 NM FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 50721 24639 RIGHT SIDE FUSELAGE NEAR FWD LAV SERVICE PANEL HAS A SMALL DENT. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED EX TERNAL SKIN DOUBLER.AC OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2007102200117 20071022 00117 NM 2007 10 22 2007UALA04215 1 20071014 A 5720 SUPPORT FITTING BOEING 737 737322 1384676 NM LT WING DAMAGED A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 341UA 24245 FUEL LEAKING AT AFT SPAR JUST OUTBOARD OF LEFT MAIN GEAR, FROM UPPER REAR SPAR CHORD REINFORCEMENT DOUBLER LOCK FASTENER . BEAM LEFT SUPPORT FITTING HAS 6 ELONGATED HOLES IN UPPER SKIN. 2 L 7 2 4F RT A16WE 2007102200119 20071022 00119 NM 2007 10 22 2007UALA04194 1 20071012 A 3397 CONNECTOR BOEING 747 747422 1384935 NM EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY EXIT EEL INOP AT ROW 53 LEFT. 11-01-07 SECURED CONNECTOR. 2 L 7 4 4F RT A20WE 2007102200120 20071022 00120 2007 10 22 2007UALA04202 4 20071012 A 2565 60461103 ASPIRATOR BOEING 757 757222 1384956 NM ESCAPE SLIDE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 0237 25222 ASPIRATOR CRACKED. REPLACED ASPIRATOR. 2 L 7 2 4F RT A2NM 2007102200135 20071022 00135 NM 2007 10 22 CALA0700593 1 20071017 A 5340 66142101 BRACKET BOEING 737 7373T0 1384582 NM BS 294 S11L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14334 23572 INTERCOSTAL ATTACH BRACKET CRACKED AT STA 294.5 STR 11L. REMOVED AND REPLACED BRACKET PER ECRA 5311-01368. 2 L 7 2 4F RT A16WE 2007102200143 20071022 00143 NE 2007 10 22 2007UALA04180 2 20071012 A 7200 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE UNKNOWN A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 403UA 422 V10305 PYLON ISSUES MANDATE NR 2 ENG REPLACEMENT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007102200144 20071022 00144 WP 2007 10 22 UPS07850925 1 20071010 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FS 55 RBL 48 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 CORROSION AND DEEP TOOLING MARKS/GOUGES ON GUSSET AT BOTTOM OF STA 55 FLOORBEAM RBL 48. REMOVED, FAB RICATED, AND INSTALLED REPAIR GUSSET AT STA 55 RBL 48 FLOORBEAM IAW DWG 5641543, AND SRM 51-3-2, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007102200160 20071022 00160 NM 2007 10 22 MWEA070247 1 20071015 A 7830 7150922REVC ANGLE BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 906ME 55170 RIGHT UPPER THRUST REVERSER DOOR FRAME AT STATION 26.666 IS CRACKED AT THE INBOARD END. CUT OUT DAMAGE AND INSTALLED A NGLE. 2 L 7 2 4F TR A6WE 2007102200176 20071022 00176 NM 2007 10 22 HNAA0700234 1 20071012 A 2844 7G980 PRESSURE SWITCH DHAV DHC8 DHC8102 2809003 NM NR 1 ENGINE INOPERATIVE A HNAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 07 980HA 376 FLIGHT WAS HEADED FROM PHL TO IPT AND DIVERTED TO MDT DUE TO NR 1 ENGINE FUEL LOW PRESSURE LIGHT ILLUMINATING IN FLIGHT. REMOVED AND REPLACE THE NR 1 PRESSURE SWITCH IAW 73-31-00. LEAK AND OPS CHECKS WERE GOOD. 2 H 7 2 4T RT A13NM 2007102200177 20071022 00177 NM 2007 10 22 SB07090 1 20071012 A 3234 655421940 CONTROL LEVER BOEING 737 7374B7 1384702 NM MLG LOOSE A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 453UW 24980 DCA FLT 1575. DURING GEAR EXTENSION, CREW REPORTED THE LANDING GEAR LEVER WON'T STAY COMPLETELY IN AND WILL GIVE 3 GEAR UNSAFE LIGHT INDICATIONS. CREW ACCOMPLISHED FLY-BY TO VERIFY GEAR WAS DOWN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER ASSEMBLY PER MM 32-31-11. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A16WE 2007102200179 20071022 00179 NM 2007 10 22 2007UALA04245 1 20071014 A 3350 LAMP BOEING 747 747422 1384935 NM EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY EXIT EEL LIGHT INOP AT DOOR 5L LOWER AFT WALL. 11-01-07 RELAMPED. 2 L 7 4 4F RT A20WE 2007102200180 20071022 00180 NM 2007 10 22 2007UALA04246 1 20071015 A 3350 LIGHT BOEING 747 747422 1384935 NM ROW 55 FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 198UA 28716 THE 'EMER LIGHTS' EICAS ADVISORY MESSAGE DISPLAYED. RIGHT ELECTRONIC INTERFACE UNIT INPUT DISAGREES WITH EIU-L&C INTERM ITTENT RESET CB R EIU. REPLACED EIU. EMERGENCY LT ADJ TEST OK PER MM33-51-00. 2 L 7 4 4F RT A20WE 2007102200198 20071022 00198 WP 2007 10 22 UPS07850915 1 20070922 A 5340 FITTING DOUG DC8 DC873F 302199F WP FS 240 L21L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 LATCH SPOOL SUPPORT FITTING CORRODED AT AFT SIDE OF NR 6 FITTING. REMOVED AND REPLACED NR 6 LATCH SP OOL FITTING IAW SRM 51-01-24-0 AND DWG 4773295. 2 L 7 4 4F RT 4A25 2007102200199 20071022 00199 WP 2007 10 22 UPS07850916 1 20070922 A 5340 FITTING DOUG DC8 DC873F 302199F WP FS 200 L21L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 LATCH SPOOL SUPPORT FITTING CORRODED AT FWD SIDE OF NR 5 FITTING. REMOVED, FABRICATED, AND INSTALLED NR 5 LATCH SPOOL SUPPORT FITTING IAW DWG 4773295, AND SRM 51-01-24-0. 2 L 7 4 4F RT 4A25 2007102200201 20071022 00201 WP 2007 10 22 UPS07850917 1 20070922 A 5340 ATTACH ANGLE DOUG DC8 DC873F 302199F WP FS 683 RBL 29 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 BELLY PANEL ATTACH ANGLE CRACKED AT STA 683 RBL 29. REMOVED, FABRICATED, AND INSTALLED REPAIR ANGLE AT STA 683 RBL 29 IAW DWG 564788, AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 2007102200207 20071022 00207 SO 2007 10 22 C2XA07RI091 1 20071007 A 2910 15H0048PH PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO HYD SYSTEM MALFUNCTIONED A C2XA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 14952 145067 FLT 2416 - EWR - CREW REPORTED HYDRAULIC SYSTEM 1 LOW QTY MESSAGE ON TAXI AND HYDRAULIC SYSTEM 1 FAIL MESSAGE ON DURING GATE RETURN. DURING TAXI BACK TO GATE, LOSS OF TILLER COMMAND. EWR MX FOUND HYDRAULIC SYSTEM 1 PRESSURE SWITCH LOOSE. MX RESECURED PRESSURE SWITCH AND PERFORMED OPERATIONAL CHECKS FOR HYDRAULIC SYSTEM AND TILLER SUCCESSFULLY. ACFT WAS A PPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007102200213 20071022 00213 NM 2007 10 22 2007UALA04182 1 20071011 A 5330 SKIN AIRBUS A319 A319131 3930317 NM FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 845UA 1585 FUSELAGE SKIN DENT AT FRAME 3 BETWEEN 41 AND 42 LT SIDE. 10-26-07 ACCOMPLISHED MAJOR REPAIR ON AREA AT FRAME 3. (4 1, 42 LT) 2 L 7 2 4F RT A28NM 2007102200219 20071022 00219 NM 2007 10 22 SWAA075060 1 20071014 A 5330 6545777 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007102200225 20071022 00225 NM 2007 10 22 SWAA075079 1 20071015 A 3350 65C27028 LIGHT BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED BRDG CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS INOP AT 5 DEF. FOUND LIGHT ASSY DISCONNECTED. RECONN ECTED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007102200227 20071022 00227 SO 2007 10 22 RAIA00710014 1 20071015 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 833HK 145240 POST FLT NR 7883 - IAD - EMERGENCY LIGHT GALLEY WALL EXIT LOCATOR INOP. MAINTENANCE RESET EMERGENCY LIGHT SWITCH AND SE CURED LIGHT CONNECTOR, OPS NORMAL. 2 L 7 2 4T RT T00011AT 2007102200232 20071022 00232 SO 2007 10 22 RAIA00710011 1 20071013 A 3350 1317 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BURNED OUT A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 847HK 14500857 PRE FLT NR 7931 - ORD - LEFT SIDE OVERWING EMERGENCY INSPECTION LIGHT INOP. MAINTENANCE REPLACED LEFTHAND AFT EMERGENCY LAMP, CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2007102200235 20071022 00235 NM 2007 10 22 2007UALA04185 1 20071011 A 3350 LAMP BOEING 757 757222 1384956 NM EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 522UA 26641 EMERGENCY FLOOR LIGHTING STRIP BY DOOR 2L IS LOOSE. 11-01-07 INSTALLED EEL LAMP AND COVER. 2 L 7 2 4F RT A2NM 2007102200238 20071022 00238 NM 2007 10 22 CALA0700587 1 20071015 A 5230 6547952 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14334 23572 C2 DOOR CRACKED AT EXTERIOR DOOR HANDLE CUTOUT. TRIMMED OUT CRACKED AREA AND INSTALLED FILLER AND REPAIR DOUBLER PER SR M 52-00-01 FIG 201. 2 L 7 2 4F RT A16WE 2007102300016 20071023 00016 NM 2007 10 23 KPVA200717 1 20071013 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8103 1386005 NM FALSE ACTIVATION A KPVA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 13 808WP 026 (PIREP) SMOKE MASTER WARNING CAME ON DURING TAXI. F/A VERIFIED THERE WAS NO SMOKE. (MX) PERFORMED MASTER WARNING CAUTI ON LIGHT TEST IAW DHC-8 MM 26-12-05. ADDITIONAL NOTES: TWO DIFFERENT P/N SMOKE DETECTORS ON BOARD THIS AIRCRAFT. NR 1 - P/N 30-231-3, S/N 35007 TIME SINCE REPAIR 174.8 HR. NR 2 - P/N 473054, S/N 0054W, TIME SINCE REPAIR 1326.8 HR. EXPE RIENCED IN THE PAST THAT CELL PHONE USAGE TRIGGERS THE SMOKE WARNING AND BELIEVE THIS TO BE A DESIGN ISSUE. THEREFORE, DON'T KNOW WHICH DETECTOR (OR BOTH) MAY HAVE GIVEN THE FALSE WARNING, SO ONLY A FUNCTIONAL TEST ON THE DETECTORS WAS PER FORMED. 2 H 7 2 4T RT A13NM 2007102300019 20071023 00019 NM 2007 10 23 SWAA075096 1 20071016 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 L1 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007102300020 20071023 00020 NM 2007 10 23 SWAA075111 1 20071016 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 755SA 27871 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM UPPER TEE CAP CORRODED AT BS 986, LBL 34 TO LBL 44. REMOVED AND REPLACED TEE CAP PER SWA EA. 2 L 7 2 4F RT A16WE 2007102300021 20071023 00021 NM 2007 10 23 SWAA075098 1 20071016 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 410WN 27897 DURING SCHEDULED HC1 CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 128.50. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007102300023 20071023 00023 NM 2007 10 23 SWAA075106 1 20071016 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 709SW 27843 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 3 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007102300030 20071023 00030 NM 2007 10 23 SWAA075104 1 20071016 A 5330 6545866 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 DURING SCHEDULED HC2 CHECK, FOUND LT KEEL BEAM PANEL CRACKED AT BS 700. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007102300033 20071023 00033 NM 2007 10 23 SWAA075097 1 20071016 A 3350 65C27028 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 407WN 29817 BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 11 DEF. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007102300038 20071023 00038 NM 2007 10 23 SWAA075099 1 20071016 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 410WN 27897 DURING SCHEDULED HC1 CHECK, LT FWD EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007102300047 20071023 00047 NM 2007 10 23 1018200701 1 20071018 A 2611 100012703 CONTROL UNIT BOEING 727 7272K5 138004P NM PWA JT8 JT8D17 52049 NE SMOKE DETECTOR MALFUNCTIONED A PCSA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 17 909PG 21852 AMERIJET FLIGHT 843 DURING TAXI LOWER CARGO FIRE RED LIGHT ILLUMINATED AND REMAINS ILLUMINATED. THE AIRCRAFT RETURNED T O BLOCKS, THE CHANNEL A LOWER CARGO SMOKE DETECTOR CONTROL UNIT WAS REPLACED, AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2007102300050 20071023 00050 EA 2007 10 23 COMA0760587 1 20070927 A 2130 VALVE CNDAIR CL600 CL6002B19 1900309 EA CABIN PRESSURE OUT OF POSITION A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 659BR 7509 FLIGHT 5148 - AIRCRAFT WOULD NOT PRESSURIZE. FOLLOWED QRH, RETURNED TO CVG, LANDED WITHOUT INCIDENT. FOUND OVERBOARD A ND INBOARD VALVES IN WRONG POSITION. REPOSITIONED VALVES. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007102300057 20071023 00057 CE 2007 10 23 AMWA88061 1 20071016 A 5330 12943006413 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA BS 213-228 CORRODED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 127ZV 25146 UE127 SURFACE TYPE CORROSION FOUND ON INTERIOR SURFACE OF FUSELAGE SKIN IN AIRCRAFT BELLY. FS213.25 STR 13R-15R, STR 14L-16, 2 28.25 STR 13R-16. INSPECTED, CLEANED, AND REPAIRED IAW B1900D SRM. 2 L 7 2 4T 3 T RT A24CE E2NE 2007102300093 20071023 00093 EA 2007 10 23 COMA0760595 1 20071005 A 3250 TRANSDUCER CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 785CA 7326 FLIGHT 5350 - RECEIVED STEERING INOP CAUTION. RAN QRH, DIVERTED TO PHL, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. A /C WAS TUGGED FROM RUNWAY. REPLACED RIGHT NOSE STEERING RVDT. 2 L 7 2 4F RT A21EA 2007102300100 20071023 00100 EA 2007 10 23 TRAX200701503 1 20071015 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 878AS 7590 AAR - FS 280 CLIP CRACKED AT RBL 9.0 O/B. 2 L 7 2 4F RT A21EA 2007102300116 20071023 00116 EA 2007 10 23 TRAX200701515 1 20071017 A 5346 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 LT UPPER ENGINE BEAM O/B ATTACH ANGLE OF AFT RADIUS, CRACKED. 10-30-07 REMOVED CRACKED LT UPPER ENGINE BEAM O/B ATT ACH ANGLE. LOCATED NEW SERVICEABLE ANGLE. OK TO INSTALL. INSTALLED ANGLE IAW CRJ SRM 51-42-21. OK TO TOPCOAT FASTENERS. APPLIED TOPCOAT TO FASTENERS IAW CRJ SRM 51-21-16. 2 L 7 2 4F RT A21EA 2007102300120 20071023 00120 EA 2007 10 23 TRAX200701521 1 20071017 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 978EV 7723 LEFT CENTER EMERGENCY LIGHT OVER WING IS INOP. 2 L 7 2 4F RT A21EA 2007102300121 20071023 00121 EA 2007 10 23 TRAX200701522 1 20071018 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 722EV 10127 LEFT FLOOR SEAT TRACK FS 374.00 TO 485.00 CORRODED AND BENT (MARKED). 2 L 7 2 4F RT A21EA 2007102300122 20071023 00122 EA 2007 10 23 TRAX200701523 1 20071018 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 722EV 10127 LEFT FLOOR SEAT TRACK FS 485.00 TO FS 581.00 HAS SURFACE CORROSION. 2 L 7 2 4F RT A21EA 2007102300125 20071023 00125 EA 2007 10 23 TRAX200701526 1 20071018 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 722EV 10127 RIGHT FLOOR SEAT TRACK FS 581.00 TO FS 677.00 HAS SURFACE CORROSION. 2 L 7 2 4F RT A21EA 2007102300133 20071023 00133 CE 2007 10 23 DJFA2007116 1 20071009 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 425CW 3998 353 RK345 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER IB RIB AND BRACKET ASSEMBLIES, THE RT IB ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THI S AREA ARE OUTLINED IN COMMUNIQUE' NR 70. MAITNENANCE REPLACED THE RIB. 2 H 7 2 4F 4 F RT A16SW E25EA 2007102300136 20071023 00136 2007 10 23 C2XA07IA224 4 20071016 A 2213 7021170951 CONTROLLER EMB 145 EMB145XR 3260214 SO AUTOPILOT SYS MALFUNCTIONED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 13118 11128 4464 145675 IAH - FLIGHT 2170, THE CREW REPORTED THAT THE COCKPIT HAD A TOXIC ODOR. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND TH E FLIGHT GUIDANCE CONTROLLER TO BE BURNT. MAINTENANCE REMOVED AND REPLACED THE FLIGHT GUIDANCE CONTROLLER, OPERATIONALL Y CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007102300139 20071023 00139 SO 2007 10 23 C2XA07IA226 1 20071012 A 3350 78241 INVERTER EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13936 145025 IAH - FLIGHT 2828, THE CREW REPORTED THAT THE FORWARD EMERGENCY LIGHT WAS OUT. MAINTENANCE REMOVED AND REPLACED THE NUM BER FOUR EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007102300146 20071023 00146 2007 10 23 DXTA200702543 4 20071014 A 2210 COMPUTER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL FLT GUIDANCE FAULTED E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 978QS 7500187 ON FINAL APPROACH, FGC B FAIL CASS MESSAGE APPEARED AND SYSTEM SWITCHED TO FGC A. CHECKED SYSTEM IN PROPER OPERATION - COULD NOT DUPLICATE- REPOSITIONED NR 1&2 IC-800'S- OPS CHECKED GOOD IAW 750 M/M CH 34-25-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007102300150 20071023 00150 CE 2007 10 23 DXTA200702542 1 20071014 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 351QS 5600451 BRAKES ARE SPONGY ON APPLICATION OF PEDAL PRESSURE WHICH DELAYED BRAKING ACTION RESULTS. BLED LT AND RT BRAKES NO AIR WAS NOTED IN SYSTEM OPS CHECK GOOD. NO DEFECTS NOTED. WORK PERFORMED IAW CE-560 MM CHAP 32-42-00. FOR DETAILS REF FAS W/O 07-2508 2 L 7 2 4F 4 F RT A22CE E25EA 2007102300154 20071023 00154 NM 2007 10 23 UPS07650935 1 20071017 A 3610 PRESSURE VALVE BOEING 767 76734AF 1385212 NM RT ENGINE DEFECTIVE A IPXA K NONE J WARNING INDICATION CL CLIMB 1 SO 01 329UP 27755 INSPECTION TYPE:ETOP DIVERSION - ON CLIMB AT FL 250, HAD A R ENGINE BLEED OVHT EICAS MSG & OVHT ON PANEL, LTV LIST COMPL ETE, HAD 10 PSI OF PRESSURE ON R SIDE, R BLEED AIR SWITCH OFF. CYCLED BLEED AIR SWITCH WITH PWR REDUCTION & LIGHT STAYE D ON 20 MINS STRAIGHT. BITE MODULE SHOWED PRV FAILED. FOUND PRV DEFECTIVE AND HPSOV BOTH WITH WORN SHAFTS. CHANGED HP SOV AND PRV PER MM 36-11-07-4, 36-11-1-8-4. 2 L 7 2 4F RT A1NM 2007102300155 20071023 00155 CE 2007 10 23 GUUA10080701 1 20071008 A 3297 CONNECTOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG LOOSE A GUUA O OTHER N FALSE WARNING AP APPROACH 1 SO 29 47542 UE198 DURING APPROACH LANDING GEAR FAILED TO EXTEND WHEN GEAR HANDLE PLACED IN THE DOWN POSITION. RETURNED TO DEPARTURE. MANUA LLY EXTENDED LANDING GEAR. LANDED WITHOUT INCIDENT. SECURED LOOSE CONNECTOR P200 AT LANDING GEAR CONTROL. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007102300156 20071023 00156 CE 2007 10 23 GUUA10120701 1 20071012 A 3297 1143610441 WIRE HARNESS BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG DAMAGED A GUUA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 46AR UE27 AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT, J HOOK, MANUALLY OVERRIDE GEAR STILL WOULD NOT RETRACT. RETURNED TO PBI. LANDED WITHOUT INCIDENT.REPLACED RT MLG DOWNLOCK SWITCH AND SQUAT SWITCH HARNESS. RIGGED LANDING GEAR. EXTENSION AND RETRACTION OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007102300157 20071023 00157 EU 2007 10 23 720110122007 1 20071013 A 2435 STARTER GEN BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE OUT OF ADJUST E QMLA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 NM 03 211SL 7201 EXTREMELY FAINT ELECTRICAL BURNING ODOR DETECTED. ASKED TRANSPORT TEAM IF THEY DETECTED ODOR AND THEY INDICATED THAT THE Y DID NOT. PILOT NOTICED NR 2 GENERATOR AMP GAUGE INDICATING APPROXIMATELY 50 AMPS WHILE NR 1 GENERATOR AMP GAUGE INDICA TED APPROXIMATELY 10 AMPS. NO OTHER INDICATIONS NOTED SWITCHED OFF NR 2 GENERATOR AND LOAD INCREASED ON NR 1 GENERATOR T O APPROXIMATELY 40 AMPS. SWITCHED NR 2 GENERATOR BACK ON AND ORIGINAL LOAD IMBALANCE RETURNED. AS THE ODOR WAS NO LONGER DETECTABLE, & THERE WERE NO INDICATIONS OF A MALFUNCTION, OTHER THAN AMPERAGE LOAD IMBALANCE, FLT CONTINUED TO ORIGINAL DESTINATION. UPON RETURN TO BASE, INCIDENT REPORTED TO MX & AN ENTRY MADE BY PILOT IN ACFT MX LOG. MECHANIC DIAGNOSED P 1 G 7 2 3U 3 U H13EU E5NE10 2007102300158 20071023 00158 EA 2007 10 23 NW6A0071002 1 20071013 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE EMERGENCY LIGHT INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 163GJ 10255 MX-STL-EXTERIOR LT AFT EMERGENCY LIGHT INOP. REPLACED BULB. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007102300159 20071023 00159 GL 2007 10 23 AC2A117834 2 20071013 A 7200 23004545 ENGINE BELL 206 206L3 1182108 SW ALLSN 250C 250C30 03013 GL NOISY B AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 6533U 52439 CAE895100 NOTICED ENGINE WHINE WHICH INCREASED IN LOUDNESS AND PITCH WITH INCREASE OR DECREASE IN POWER. REPORTED TO MAINTENANCE. DEMONSTRATED PROBLEM TO MX & CONFIRMED PROBLEM. MECHANIC NOTICED STARTER GENERATOR MAKING NOISE, CHANGED STARTER GEN. D ID NOT CORRECT PROBLEM. REMOVED AND REPLACED ENGINE. 1 G 7 1 3U 3 U H2SW E1GL 2007102300163 20071023 00163 CE 2007 10 23 DXTA200702545 1 20071015 A 2435 STARTER GEN CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE NR 2 FAILED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 357QS 6800155 ABORTED NR 2 ENGINE START WHEN LINE MAN SIGNALED CUT AFTER SMOKE WAS SEEN EMANATING FROM THE BOTTOM OF THE ENGINE NACELL E, ITT STAYED WITHIN LIMITS. REMOVED AND REPLACED RT ENG STARTER GEN. OPS CHECK GOOD IAW CESSNA 680 M/M 24-30-00. 2 L 7 2 4F 4 F RC T00012WI E35NE 2007102300171 20071023 00171 NM 2007 10 23 AMTA200700495 1 20071013 A 5321 FLOOR PANEL BOEING 737 73783N 13844HI NM BS 500D-540 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 308TZ 28244 FWD CARGO FLOOR PANEL 120DF HAS CORROSION AROUND EDGES. UPPER SURFACE STA 500D-540, LBL 25- RBL 25. FABRICATED AFT CAR GO FLOOR PANEL 120DF, ALODINED AND PRIMED, IAW 53-30-53-0I, SRM 51-20-01. (K) 2 L 7 2 4F RT A16WE 2007102300172 20071023 00172 NM 2007 10 23 AMTA200700496 1 20071013 A 5321 FLOOR PANEL BOEING 737 73783N 13844HI NM BS 887-947 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 308TZ 28244 AFT CARGO FLOOR PANEL 140DF, (AFT) HAS CORROSION AROUND EDGES OF UPPER SURFACE STA 887- 947, LBL 14- RBL 25. FABRICATED NEW FLOOR PANEL IAW SRM 53-70-54-01 (2024 T-3 .071) ALODINED AND PRIMED IAW SRM 51-20-01. (K) 2 L 7 2 4F RT A16WE 2007102300173 20071023 00173 WP 2007 10 23 UPS07850934 1 20070918 A 5320 CUSP WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 CUSP CRACKED AT STA 1260 L21L. REPAIRED CUSP AT STA 1260 L21L IAW SRM 53-02-05 FIG 015. 2 L 7 4 4F RT 4A25 2007102300178 20071023 00178 NM 2007 10 23 UPS07M50931 1 20070805 A 5311 FRAME DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C CENTER CARGO COMPT AT STATION 1841 X-48 AFT FRAME FOUND CRACKED. CENTER CARGO COMPT STA 1841 X=0 -48R T CRACK FRAME WEB REMOVED. FRAME WEB FAB FROM MAT'L 7075T6-0.050" AS PER DWG AGA7170. FRAME WEB HOLES PICKED UP & REPR OTECTED. FRAME WEB PAINTED. FRAME WEB INSTALLED AT CTR CARGO COMPT STA 1841 X=0 -48RT AS PER SRM 51-31-01 VOL II REV 3 8. 2 L 7 3 4F RT A22WE 2007102300180 20071023 00180 NM 2007 10 23 UPS07M50932 1 20070805 A 5311 FRAME DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C CENTER CARGO COMPT AT STATION 1841 X+50 AFT FRAME FOUND CRACKED. CNTR CARGO COMPT STA 1841 X=0 -50LT CRACK FRAME WEB REMOVED. FRAME WEB FAB FROM MAT'L 7075T6-0.050" AS PER DWG AGA7170. FRAME WEB HOLES PICKED UP & REPROT ECTED. FRAME WEB PAINTED. FRAME WEB INSTALLED AT CNTR CARGO COMPT STA 1841 X=0 -50LH AS PER SRM 51-31-01 VOL II REV 38 . 2 L 7 3 4F RT A22WE 2007102300181 20071023 00181 NM 2007 10 23 AMTA200700500 1 20071013 A 5321 FLOOR PANEL BOEING 737 73783N 13844HI NM BS 727D CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 308TZ 28244 AFT CARGO PNL 140BF STRAP HAS CORROSION ON LWR SURFACE STA 727D, LBL 25 - RBL 25. FABRICATED TEE STRAP IAW SRM 53-42-11 -26. REPLACED TEE STRAP IAW 51-40-02. (K) 2 L 7 2 4F RT A16WE 2007102300182 20071023 00182 NM 2007 10 23 SWAA075143 1 20071018 A 3310 1111133 LENS BOEING 737 7373Q8 1384670 NM COCKPIT ACTIVATED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 687SW 23388 DIVERSION, ELECTRICAL-RUBBER BURNING ODOR IN COCKPIT. INSPECTED AND FOUND F/O GRIMES LIGHT INTERNAL LENS MELTED. REMOV ED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007102300183 20071023 00183 NM 2007 10 23 SWAA075124 1 20071018 A 3350 20121 CHARGER BOEING 737 7373K2 13844BA NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007102300184 20071023 00184 NM 2007 10 23 AMTA200700501 1 20071014 A 5551 ATTACH FITTING BOEING 737 73783N 13844HI NM HORIZONTAL STAB DAMAGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 308TZ 28244 UPON INNSPECTION OF FORWARD SPAR ATTACHMENT BOLTS FOUND THE RT LOWER AND RT UPPER BOLTS DEFECTIVE, GALLING AND FRETTING WEAR. COMPLIED WITH EO 737-55AD-2935, REPLACED (2) BOLTS WITH PN 180A1611-3. (K) 2 L 7 2 4F RT A16WE 2007102300186 20071023 00186 NM 2007 10 23 SWAA075135 1 20071018 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 612SW 27930 L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007102300187 20071023 00187 NM 2007 10 23 AMTA200700503 1 20071014 A 5753 SKIN BOEING 737 73783N 13844HI NM LT WING TE FLAP DAMAGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 308TZ 28244 LT WING AFT FLAP LOWER SURFACE HAS MULTIPLE DENTS AND DINGS. REPAIRED IAW SAA EA 737-5753-09-A1150, INTERM REPAIR REINS PECT EVERY 3500 FLIGHT HOURS OR 24 MONTHS WHICHEVER COMES FIRST IAW ATA ERA 737-57R-6171. (K) 2 L 7 2 4F RT A16WE 2007102300192 20071023 00192 NM 2007 10 23 SWAA075112 1 20071015 A 2824 405742 ACTUATOR BOEING 737 7373H4 1384600 NM FUEL SYSTEM FAULTY A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 29 320SW 23341 DIVERSION / DECLARED EMERGENCY. AFTER CROSS FEEDING FUEL, TURNED OFF CROSS FEED VALVE, NOTICED LIGHT STAYED ILLUMINATED . NOTICED START OF FUEL IMBALANCE. REMOVED AND REPLACED CROSS FEED VALVE ACTUATOR AND CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2007102300194 20071023 00194 NM 2007 10 23 SWAA075128 1 20071018 A 3350 417A5703 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 485WN 32473 EEPLS LIGHT ASSY LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007102300195 20071023 00195 NM 2007 10 23 SWAA075146 1 20071018 A 5210 507945264 DOOR FRAME BOEING 737 7373H4 1384600 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR FWD FRAME CRACKED AT SNUBBER CUTOUT. REMOVED AND REPLACED DOOR PER MM. 2 L 7 2 4F RT A16WE 2007102300196 20071023 00196 NM 2007 10 23 SWAA075141 1 20071018 A 5220 507978 DOOR FRAME BOEING 737 7373H4 1384600 NM EMERGENCY EXIT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 14Y CHECK, FOUND RT OVERWING EMERGENCY EXIT HATCH LOWER FRAME CRACKED AT LOWER CENTER FITTING. REMOVED AND REPLACED LOWER FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007102300197 20071023 00197 NM 2007 10 23 SWAA075116 1 20071018 A 5610 5893543130 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT CRACKED A SWAA K NONE O OTHER CR CRUISE 1 SW 29 315SW 23337 AT FL 330 FLIGHT DECK R1 WINDOW ARCED THEN OUTER WINDOW PANE CRACKED. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2007102300198 20071023 00198 NM 2007 10 23 SWAA075127 1 20071018 A 5610 58935577 WINDOW BOEING 737 7377H4 1384404 NM COCKPIT ARCED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 445WN 29841 FLIGHT DECK L2 WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2007102300199 20071023 00199 2007 10 23 SWAA075120 4 20071018 A 2565 61620 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007102300202 20071023 00202 NM 2007 10 23 SWAA075123 1 20071018 A 5523 6545166 ROD END BOEING 737 7373H4 1384600 NM ELEVATOR TAB SEIZED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED C3 CHECK, FOUND RIGHT OUTBOARD ELEVATOR TAB PUSHROD AFT ROD END SEIZED. REMOVED AND REPLACED PUSHROD A SSY PER MM. 2 L 7 2 4F RT A16WE 2007102300203 20071023 00203 NM 2007 10 23 SWAA075117 1 20071018 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 372, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007102300204 20071023 00204 NM 2007 10 23 SWAA075145 1 20071018 A 5753 6546430189 FLAP BOEING 737 737301 1384611 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED BRDG CHECK, FOUND LEFT WING INBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007102300205 20071023 00205 NM 2007 10 23 SWAA075136 1 20071018 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 613SW 27931 DURING SCHEDULED BRDG CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007102300207 20071023 00207 NM 2007 10 23 SWAA075115 1 20071018 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 460, STR 17R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007102300208 20071023 00208 NM 2007 10 23 SWAA075137 1 20071018 A 5311 6546534 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007102300212 20071023 00212 NM 2007 10 23 SWAA075114 1 20071018 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 22L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007102300213 20071023 00213 NM 2007 10 23 SWAA075149 1 20071018 A 5754 65C26601 SLAT BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND RIGHT NR 5 L/E SLAT DELAMINATED AT OUTBOARD T/E. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007102300217 20071023 00217 NM 2007 10 23 SWAA075140 1 20071018 A 3350 B21506 FUSE BOEING 737 7377H4 1384404 NM CABIN BLOWN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 725SW 27857 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 6 ABC. REMOVED AND REPLACED FUSE PER MM. 2 L 7 2 4F RT A16WE 2007102300218 20071023 00218 NM 2007 10 23 SWAA075126 1 20071018 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 17L CRACKED AT BS 188. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007102300219 20071023 00219 NM 2007 10 23 SWAA075147 1 20071018 A 5315 BAC1503100146 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 732 LBL 3. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007102300221 20071023 00221 2007 10 23 SWAA075132 4 20071018 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007101900377 20071019 00377 NM 2007 10 19 EIA2007182 1 20070922 A 5311 FRAME BOEING 747 747132 1384882 NM BS 860 S37-38L CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 FORWARD CARGO BS 860 LT BETWEEN STR 37L AND 38L FRAME FOUND CRACKED. FORWARD CARGO BS 860 LT BETWEEN STR 37L AND 38L FR AME REPAIRED PER EA-53-1180. 2 L 7 4 4F A20WE 2007102300224 20071023 00224 NM 2007 10 23 07FDEA04548 1 20071010 A 7932 TRANSMITTER BOEING 727 7272S2F 1384O81 NM PWA JT8 JT8D7 52053 NE NR 2 OIL PRESS LOOSE A FDEA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 SO 25 204FE 22926 689890 NR 2 LOW OIL PRESSURE FILTER BYPASS LIGHT ILLUMINATED IN DESCENT FOLLOWED BY OIL PRESSURE DROP TO ZERO. QRH PERFORMED, ENGINE SHUT DOWN WITH OIL PRESSURE AT 5 TO 10 PSI OIL QUANTITY NORMAL. TEMP RISING GRADUALLY ENGINE SHUTDOWN 13 MINUTES AFTER FIRST INDICATION. ENGINE WIND MILLED APPROXMATELY 15 MINUTES BEFORE LANDING. DURING NR 2 ENG PURGE PROCESS, FOU ND THAT THE OIL LINE TO THE OIL PRESSURE TRANSMITTER WAS LOOSE AT THE TRANSMITTER CONNECTION FITTING. PRATT-WHITNEY HA S BEEN SATISFIED THAT THE NR 2 ENG IS OK FOR SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2007102300227 20071023 00227 NM 2007 10 23 SWAA075125 1 20071018 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 351SW 24572 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2007102300239 20071023 00239 NM 2007 10 23 USAA920070956 1 20071014 A 5320 141N51502 CHANNEL BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 903AW 23323 MCN - MAJOR REPAIR - C-12 CHECK - CRACKED CHANNEL, BS 365.25, LBL 45.5, WL 201. REPAIRED CHANNEL, BS 365.25, LBL 45.5, WL 201 IAW B757-200 SRM 53-10-51-2R1, FIGURE 201. 2 L 7 2 4F RT A2NM 2007102300240 20071023 00240 NM 2007 10 23 EIA2007166 1 20070917 A 5312 PRESSURE PANEL BOEING 747 747212B 1384886 NM NLG WW CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 NOSE LANDING GEAR WHEEL WELL, RT UPPER AT APPROX STA 280 HAS CORROSION BELOW AND UNDER STANDOFF. REMOVED CORROSION UNDE R LINES SUPPORT (WEB) STA 280 RT WL 190 FOUND TO BE OUT OF LIMITS PER B747 SRM 53-30-01 AND 51-10-01. CUT OUT CORRODED SECTION AND INSTALLED REPAIR DOUBLER AND FILLER PER B747 SRM 53-10-04 PG 707-711AND SRM 51-30-02 PG 2-9. 2 L 7 4 4F A20WE 2007102300245 20071023 00245 EA 2007 10 23 HNAA0700240 1 20071018 A 2612 CIRCUIT BREAKER DHAV DHC8 DHC8311 1386006 EA COCKPIT POPPED A HNAA O OTHER N FALSE WARNING CR CRUISE 1 EA 07 331EN 279 IN FLIGHT CHECKFIRE DETECT WARNING AND MASTER WARNING LIGHT ILLUMINATED ALONG WITH FAULT B ON NUMBER 2 ENGINE FIRE PROTE CTION PANEL. INSP AND FOUND CIRCUIT BREAKER LABELED ENGINE NR 2 FIRE PROTECTION POPPED. RESET CIRCUIT BREAKER AND GROU ND RAN AIRCRAFT WITH ALL ELECTRICAL BUSSES POWERED. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007102300248 20071023 00248 NM 2007 10 23 UPS07450936 1 20071018 A 7920 TUBE BOEING 747 747123F NM OIL SYSTEM CHAFED A IPXA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 SO 01 677UP 20391 INSPECTION TYPE:N/A IFSD - CREW INFORMED FLIGHT CONTROL THAT THE OIL PRESSURE ON NR 1 ENG WAS RUNNING IN THE YELLOW BAND AND OCCASSIONALLY WAS HITTING THE RED LINE. IT WAS ALSO INDICATED THE OIL PRESSURE LIGHT WAS FLICKERING. CREW DELARED EMERGENCY, SHUT DOWN NR 1 ENGINE AND CONTINUED TO CTS. FOUND CHAFED OIL PRESS TUBE WITH PIN HOLE. C/W EO JT9D-7930-27 881A. C/OUT ENG WINDMILLING INSP PER MM 72-00-01 FIG 3, SATIS. REMOVED AND REPLACED ENG MAIN OIL STRAINER AND RAN ENG PER MM 71-00-00. FOUND SATIS. NO LEAK NOTED. OIL ADDED 18 QTS. A/C OK FOR SERVICE. 2 L 7 4 4F A20WE 2007102300249 20071023 00249 NM 2007 10 23 UPS07450948 1 20071016 A 5320 WEB BOEING 747 747121 1384871 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C NWW RT SIDE PANEL STA 294 WL 170 SIDE PANEL WEB 1EA SUSPECT CRACK INDICATION FOUND ADJACENT LWR SIDE O F EXTERNAL STRAP APPROX. 0.5" LENGTH CRACK LENGTH 0.5" APPROX. NOSE WHEEL WELL SIDE PANEL REPAIRED AT BS 293 - BS 295 W L 170 AREA AS PER SRM 53-10-04 FIG 116 SUBSEQUENT INSPECTIONS ARE NECESSARY AS PER SRM 53-10-04 FIG 116 TABLE II. 2 L 7 4 4F A20WE 2007102300251 20071023 00251 WP 2007 10 23 UPS07850960 1 20070928 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 BULGING SKIN AT STA 100 L35R. CUT OUT DAMAGED AREA AT STA 100 L35R IAW SRM 53-02-01 FIG 7. FABRICAT ED AND INSTALLED REPAIR DOUBLER, FINGER DOUBLER AND FILLER AT STA 100 L35R IAW SRM 53-02-01 FIG 7. 2 L 7 4 4F RT 4A25 2007102300252 20071023 00252 NM 2007 10 23 UPS07M50942 1 20070920 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C MAIN DECK: FROM BS 825 TO 835, ALONG X=76 (LBL76), SEAT TRACK FLANGE AREAS FOUND CORRODED. CORROSION REMOVAL AS A/MENTIONED AREA, FOUND EXCEEDS LIMIT PER SRM 53-7 0-00D F3.V1.R35. REMOVAL C/OUT TO GAIN ACCESS OF AFFECTE D SEAT/TRK CORRODED, SEAT/T TRIMMED OFF PER SRM 53-70-00D F1 V1 R35. SEAT/T & SPLICE AT AFFECTED AREA REWORK PER SRM 53 -70-00D, F1 V1.R35. PICKED UP HOLES & INSTL OF SEAT/T SRM 51-33-01 & 51-3101 V.2 R35., FOUND SATIS. 2 L 7 3 4F RT A22WE 2007102300253 20071023 00253 NM 2007 10 23 UPS07M50943 1 20070920 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C MAIN DECK: FROM BS 819 TO 939, ALONG X=28 (LBL28), SEAT TRACK CROWN & FLANGE AREAS FOUND CORRODED. C ORROSION REMOVAL C/OUT PER A/M AREA FOUND EXCEEDED LIMIT PER SRM 53-70 -00D F3.V1.R35. REMOVAL C/OUT TO GAIN ACCESS TO TRIMMED OFF CORROSION AFFECTED AREA ON SEAT/T PER SRM 51-31-01 V2 R35 & 53-70-00DV1 R35. NEW SEAT/T & SPLICE REWORK PER SRM 53-70-00D F1.V1R35. RWK PARTS P/ HOLES & INSTL C/OUT PER SRM 51-31-01 V2, 51-31-01 & 51-33-01 R35, SATIS. 2 L 7 3 4F RT A22WE 2007102300257 20071023 00257 NE 2007 10 23 2007UALA04081 2 20071006 A 7200 ENGINE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 1 STALLED A UALA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 29 825UA 980 V10189 NR 1 ENG STALL AT FL380 IN SMOOTH AIR. ENGINE RECOVERED QUICKLY. ENGINE REPLACED DUE TO MANY CHRONIC REPORTS OF ENGINE STALLS AND SEVERAL PARTS REPLACED. NO REPEATS SINCE ENGINE CHANGE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007102300258 20071023 00258 EU 2007 10 23 2007UALA04129 1 20071006 A 3250 C2473600102 CONTROL MODULE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG STEERING FAULTY A UALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 416UA 479 NW STEERING FAULT DISPLAYED ON UPPER ECAM SCREEN. *S/D* NOSE GEAR STEERING MODULE FAULTY. REPLACED NOSE GEAR STEERING SERVO CONTROL MODULE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007102300264 20071023 00264 NM 2007 10 23 2007UALA04135 1 20071008 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE MISREPAIRED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 570UA 26678 RT RVSM AREA: PORTION OF PREVIOUS DOUBLER REPAIR (APPROX 6IN SQUARE) EXTENDS INTO RVSM AREA APPROX 1.5 INCHES. MAJOR R EPAIR ACCOMPLISHED: DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007102300280 20071023 00280 NM 2007 10 23 2007UALA04148 1 20071005 A 2613 OVERHEAT SYS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 538UA 25222 RIGHT ENGINE OVERHEAT DOES NOT TEST. 2 L 7 2 4F 4 F RT A2NM E17NE 2007102300281 20071023 00281 NM 2007 10 23 2007UALA04149 1 20071009 A 2697 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FIRE LIGHT BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 504UA 24625 UNABLE TO GET GOOD ENGINE FIRE TEST, RIGHT ENGINE OVERHEAT AND ENGINE 1 DISCH BTL LIGHT BURNED OUT. 11-01-07 FOUND OV ERHEAT AND ENGINE 1 DISCHARGE BOTTLE LIGHT BURNED OUT. ALSO FOUND BROKEN WIRE ON ENGINE OVERHEAT SWITCH. REPLACED FIRE CONTROL PANEL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007102300283 20071023 00283 NM 2007 10 23 2007UALA03861 1 20070923 A 3510 MC1019101 OXYGEN MASK BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE COCKPIT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 670UA 29240 CREW OXYGEN MASK PROBLEM, POSITION 1.(1=CAPT,2=FO, 3=1ST OBS,4=2ND OBS). CREW COMMENTS: RED SQUEEZE TAB BROKE OFF. RE PLACED O2 MASK ASSY. OP & LEAK CHECKS OK FOR SERVICE. SUSPECT MASK DAMAGED DURING REPEATED STOWAGES. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102300290 20071023 00290 NM 2007 10 23 2007UALA03866 1 20070921 A 3350 582233 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 677UA 30029 EMERGENCY LIGHTS ROW 19 TO 23 LEFT ARE INOP. REMOVED AND REPLACED BATTERY PACK M1559. EEL SYSTEM OP CHECKED OK FOR SER VICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102300292 20071023 00292 NM 2007 10 23 2007UALA03868 1 20070923 A 2560 P4010021 BATTERY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FLASHLIGHT DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 677UA 30029 EMERGENCY FLASH LIGHT BY 1L RED LIGHT NOT BLINKING. REPLACED BATTERY, OP CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102300295 20071023 00295 NM 2007 10 23 2007UALA03871 1 20070922 A 3397 78941 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 215UA 30221 CREW REPORT - EEL STRIP LIGHT AT SEAT 3F LOOSE. LIGHTING IN PLACE BUT NOT WORKING. RECONNECTED CONNECTOR AND EEL STRIP , OPS CHECKS OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007102300298 20071023 00298 NM 2007 10 23 2007UALA03885 1 20070924 A 5313 146T3003 STRINGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 64030 25392 AFT PIT BS 1223 STR 36L IS CORRODED. REMOVED DAMAGE & FABRICATED REPAIR PART. INSTALLED STRINGER DOUBLER. INSPECTED & APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102300300 20071023 00300 NM 2007 10 23 2007UALA03887 1 20070924 A 3350 363674 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 672UA 30027 SEAT 3HJ ESCAPE PATH LIGHT INOP MISSING. REPLACED EEL PATH LIGHT. TEST OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102300302 20071023 00302 NM 2007 10 23 2007UALA03889 1 20070924 A 3350 362624 STRIP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 661UA 27158 EMERGENCY LIGHT STRIP BY 1E TRIM CAME OFF AND IS A TRIPPING HAZARD. SECURED LOOSE EEL LIGHT STRIP. OP CHECKED OK FOR S ERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102300306 20071023 00306 NM 2007 10 23 2007UALA03893 1 20070925 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY LIGHT DOOR 4 RT SILL FWD INOP. REPLACED LAMP, OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102300307 20071023 00307 NM 2007 10 23 2007UALA04152 1 20071008 A 8011 STARTER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 NR 2 ENGINE STARTER BLEW DURING START. DAMAGED REVERSER & FAN COWL. 11-01-07 REPLACING STARTER & STARTER VALVE. O P CHECK OF STARTER INDICATES BOTH ARE GOOD FOR SERVICE. SUSPECT BEARING DETERIORATION & RELEASE OF ROTOR CAUSING RESUL TANT IMBALANCE AND DISINTEGRATION. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102300308 20071023 00308 EU 2007 10 23 2007UALA04155 2 20071008 A 7200 7147M10G04 PMC BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 ENGINE MALFUNCTIONED A UALA O OTHER O OTHER CL CLIMB 1 WP 29 399UA 24674 725210 NR 1 THROTTLE 2 KNOBS FWD OF NR 2 ON T/O. NR 1 ENG SURGES AT HIGH THRUST SETTINGS 91-97 PERCENT N1. ACCOMPLISHED NR 1 ENGINE POWER MANAGEMENT CONTROL PLA VOLTAGE CHECK MM73-21-00 P.500E. PMC COMPONENT CHECK MM 73-21-00 P.500C. CIT SENSOR CHECK MM 73-21-02 P.601 & T2 SENSOR CHECK MM 73 -21-09 P.601. NO FAULTS FOUND. REPLACED NR 1 ENGINE PMC PER MM 73-21-0 4 P.401 ACCOMPLISHED POWER ASSURANCE 2 L 7 2 4F 4 F RT A16WE E21EU 2007102300311 20071023 00311 NM 2007 10 23 2007UALA04161 1 20071009 A 5414 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 PYLON DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 NR 1 PYLON NAC STA 140 OUTBOARD SIDE SKIN FASTENER HOLE ELONGATED THRU SKIN AND DOUBLER. 11-01-07 MAJOR REPAIR ACCO MPLISHED. REAMED HOLES 1, 2, AND 3 TO BE TRUE ROUND AND CONCENTRIC. ACCOMPLISHED HFEC. INSTALLED FASTNERS IN HOLES 2 AN D 3. MACHINED FREEZE PLUGS WITH 75T6 AND 15-5PH AND INSTALLED FREEZE PLUGS AND FASTNERS IN HOLE 1. 2 L 7 2 4F 4 F RT A2NM E17NE 2007102300313 20071023 00313 NM 2007 10 23 2007UALA04163 1 20071009 A 2611 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SMOKE DETECTOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 649UA 25286 DURING EQUIP COOLING TEST, SMOKE LIGHT DOES NOT COME ON AND NO FWD EQUIPMENT SMOKE ADVISORY MESSAGE. RELAMPED SMOKE DET ECTOR. OPS CK OK PER JC EQUIP COOLING TEST. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102300317 20071023 00317 NM 2007 10 23 2007UALA04167 1 20071010 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 RIGHT OVERWING 2 FWD ASSY. EMERGENCY LIGHT INOP. 11-01-07 REPLACED POWER SUPPLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102300318 20071023 00318 NM 2007 10 23 2007UALA04168 1 20071010 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY CEILING LIGHT INOP AT ROW 32 ABC. 11-01-07 RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102400003 20071024 00003 NM 2007 10 24 EIA2007177 1 20070905 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 1580-1600 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 MAIN DECK BS 1580-1600 RBL 11 TO RBL 11 SEAT TRACK FOUND CRACKED. MAIN DECK BS 1580-1600 RBL 11 TO RBL 11 SEAT TRACK RE PAIRED AS PER 51-30-02. 2 L 7 4 4F A20WE 2007102400004 20071024 00004 NM 2007 10 24 EIA2007181 1 20070916 A 5755 SUPPORT BEAM BOEING 747 747132 1384882 NM NR 6 SPOILER CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 CRACK FOUND ON LOWER TRAILING EDGE SUPPORT BEAM LWR CHORD AT NR 6 SPOILER SUPPORT FITTING. LOWER T/E SUPPORT BEAM LOWER CHORD AT NR 6 SPOILER SUPPORT FITTING REPAIRED PER EA-57-0590. 2 L 7 4 4F A20WE 2007102400006 20071024 00006 NM 2007 10 24 EIA2007171 1 20070917 A 5311 FRAME BOEING 747 747132 1384882 NM BS 1560 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 AFT CARGO BS 1560 STR 37L FRAME FOUND CRACKED. AFT CARGO BS 1560 STR 37L FRAME REPAIRED PER EA-53-1185. 2 L 7 4 4F A20WE 2007102400010 20071024 00010 NM 2007 10 24 EIA2007183 1 20070926 A 5730 65B016261 SKIN BOEING 747 747132 1384882 NM LT WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 LEFT WING LOWER SKIN AT FSSI 1050-1070 SKIN UPPER FOWARD SIDE OF FRONT SPAR FOUND CORROSION. BLENDED OUT SKIN CORROSION PER B747 SRM 51-10-01. PERFORMED DVI OF BLEND AREA AND HFEC OF HOLES AND SURFACE. FLAP PEEN AREA PER SOPM 20-10-03. FABRICATED REPAIR PER EA-57-0593. 2 L 7 4 4F A20WE 2007102400011 20071024 00011 NM 2007 10 24 EIA2007186 1 20070925 A 5512 SKIN BOEING 747 747132 1384882 NM HORIZONTAL STAB CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 LT HORIZONIAL STAB TOP SKIN CRACKED AT STAB STA 560. TRIMMED OUT DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 55-10 -03 FIG 7 AND EA-55-0053. 2 L 7 4 4F A20WE 2007102400012 20071024 00012 NM 2007 10 24 EIA2007184 1 20070919 A 5311 FRAME BOEING 747 747132 1384882 NM BS 1500 S34-35L CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 FOUND AFT CARGO PIT STA 1500 STR 35L-34L FRAME CRACKED. REMOVED AND REPLACED FRAME PER BOEING DRAWING 65B04839-55/-59 A ND EA-53-1185. 2 L 7 4 4F A20WE 2007102400014 20071024 00014 NM 2007 10 24 07FDEA04578 1 20071012 A 5753 ARC1984502 SUPPORT BRACKET DOUG MD11 MD11F 3023600 NM FLAP FAIRING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 RIGHT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING SUPPORT OUTBOARD LOWER MOUNTING BORE FOUND CORROSION. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-116494. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007102400015 20071024 00015 NM 2007 10 24 07FDEA04579 1 20071012 A 3010 VALVE DOUG MD11 MD11F 3023600 NM ANTI ICE SYSTEM MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 523FE 48479 ON INITIAL CLIMB-OUT PASSING 2,500' LVL "AIR SYS 3 OFF" FOLLOWED BY LVL 2 "WING A-ICE R DISAG" AFTER TURNING WING ANTI- ICE ON. RECEIVED ICE DETECTED ALERT. RAN CHECKLIST DEPARTED ICING CONDITIONS, RETURNED ANC. REPLACED RT WING A/T VAL VE PER MM 30-11-01-4. REMOVED AND REPLACED RT WING A/I DP SWITCH PER MM 30-11-02-4, LEAK AND OPS CHECKS NORMAL ON GROUN D. 2 L 7 3 4F RT A22WE 2007102400018 20071024 00018 NM 2007 10 24 07FDEA04583 1 20071013 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 635 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 620FE 48791 MAIN DECK CARGO COMPARTMENT LEFT FLOOR SEAT TRACK AT STATION 635, X = 27.5 FOUND CRACKED APPROXIMATELY 3 INCHES. 10- 30-07 REPAIRED BY REPLACEMENT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007102400020 20071024 00020 NM 2007 10 24 07FDEA04585 1 20071014 A 5753 SKIN BOEING 727 727233 138408A NM RT WING TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 RIGHT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED 72" FROM INBOARD EDGE. REPAIRED SURFACE DELAMINATION REF SRM 51-4 0-20 PARA'S 7, 14, 15, 19, 20, 22 TAP TEST GOOD. THIS IS CLASSIFIED AS A MAJOR REPAIR. PRIMED AND PAINTED REPAIR AREA REF M/M 51-20-151-7. 2 L 7 3 4F RT A3WE 2007102400021 20071024 00021 NM 2007 10 24 07FDEA04586 1 20071014 A 5340 66118096 STRINGER CLIP BOEING 727 727233 138408A NM BS 1070 S28L CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 STRINGER CLIP CRACKED ON STR 28L, FS 1070. REMOVED STRINGER CLIP REF SRM 51-30-2. FABRICATE NEW STRINGER CLIP 7075-T6 .040 REF BOEING DRW 66-11809-6 PG 1/2. TREATED STRINGER CLIP REF SRM 51-10-2. PRIMED STRINGER CLIP REF SRM 51-10-2. I NSTALLED STRINGER CLIP REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007102400025 20071024 00025 EU 2007 10 24 07FDEA04591 1 20071015 A 5510 A55177965000 HINGE FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION ON LT THS HINGE FITTING NR 2. REPAIR PERFORMED BY CORROSION BLEND OUT, NDT FOR CRACK FREE AND REPROTECT ING THE AREA IAW EA 6-5516-106523 AND RAS/CASA/5537/2007 ISS A. 2 L 7 2 4F RT A35EU 2007102400028 20071024 00028 EU 2007 10 24 07FDEA04594 1 20071015 A 5730 A57340088 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION ON LT WING BOTTOM SKIN LOWER SURFACE RIB 11 REPAIR PERFORMED BY BLEND OUT CORROSION, APPROVED BY EA 6-5720-112530 AND RAS/BAE/1005161/2007 ISS A. 2 L 7 2 4F RT A35EU 2007102400030 20071024 00030 EU 2007 10 24 07FDEA04596 1 20071015 A 5730 A57340087 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION ON LT WING BOTTOM SKIN LOWER SURFACE RIB 5, AROUND SEVERAL HOLES. REPAIR PERFORMED BY BLEND OUT CORROSI ON, APPROVED BY EA 6-5720-112530 AND RAS/BAE/1005161/2007 ISS A. 2 L 7 2 4F RT A35EU 2007102400031 20071024 00031 EU 2007 10 24 07FDEA04598 1 20071015 A 5730 A5734088 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION ON RT WING LEADING EDGE BOTTOM SKIN UPPER SURFACE AND RIB NEAR TRACK NR 5-7 REPAIR PERFORMED BY BLEND OU T THE CORROSION AND OVERSIZING THE HOLES IAW EA 6-5741-106528 AND RAS BAE/1005113/2007 ISS A. 2 L 7 2 4F RT A35EU 2007102400032 20071024 00032 EU 2007 10 24 07FDEA04599 1 20071015 A 5730 A57340088 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION ON RT WING LEADING EDGE BOTTOM SKIN UPPER SURFACE AND RIB NEAR TRACK NR 7. REPAIR PERFORMED BY BLEND OU T THE CORROSION AND OVERSIZING THE HOLES IAW EA 6-5741-106528 AND RAS BAE/1005113/2007 ISS A. 2 L 7 2 4F RT A35EU 2007102400039 20071024 00039 NM 2007 10 24 DL764071333 1 20071010 A 2120 EXHAUST VALVE BOEING 767 767432ER 1385134 NM E/E BAY FAILED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 838MH 29711 FWD EQUIP EXHAUST VALVE EICAS MSG AFTER 2ND ENG START, RTB. 2 L 7 2 4F RT A1NM 2007102400041 20071024 00041 NM 2007 10 24 DL764071336 1 20071010 A 5330 SKIN BOEING 767 767432ER 1385134 NM BS 907 S10R DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 833MH 29706 DURING MAINTENANCE CHECK AT TIMCO GSO; AN ELONGATED HOLE WAS FOUND IN SKIN AT A PREVIOUS LIGHTNING STRIKE LOCATED AT STA 901 AND S-10R. THE SKIN WAS REPAIRED PER 767-400 SRM 53-00-01 REPAIR 1 (DOCUMENTED ALSO IN ER/A INSTRUCTIONS), AND STR INGER WAS REPAIRED WITH BUSHING INSTALLATION PER 51-20-07 AND REPAIR PARTS PER 53-00-03 REPAIR 3. ALL INSTRUCTIONS FOR REPAIRS ARE DOCUMENTED IN ER/A 464163-14 2 L 7 2 4F RT A1NM 2007102400044 20071024 00044 NM 2007 10 24 DLM88071339 1 20071012 A 2910 HYDRAULIC SYSTEM DOUG MD88 MD88 3023688 NM LEFT UNKNOWN A DALA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 923DL 49705 L HYD PRESS DROP TO ZERO QTY 19 FROM 12 BLED AIR FROM LT HYD RES TO CORRECT LEVEL RAN ALL HYD, OPERATED SYSTEMS. NO LEA KS OR PRESS DROPS QTY STAYED NORMAL CKS OK. 2 L 7 2 4F RT A6WE 2007102400045 20071024 00045 NM 2007 10 24 DLM90071340 1 20071011 A 5340 991199117 ATTACH ANGLE DOUG MD90 MD9030 3023690 NM BS 1458-1475 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 AFT ACCESSORY BETWEEN STA 1458 AND 1475 AIRSTAIR CUTOUT RIGHT OUTBOARD SIDE ATTACH ANGLE IS CORRODED. REMOVED AND REPLA CED ANGLE IAW MD90 SRM 51-30-02 AND 51-30-05. 2 L 7 2 4F RT A6WE 2007102400046 20071024 00046 NM 2007 10 24 DLM90071341 1 20071012 A 5330 591143283 SKIN DOUG MD90 MD9030 3023690 NM FS 1476 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 FS 1476 UPPER FUSELAGE RIGHT SKIN IS CRACKED BELOW LOWER FORWARD VERTICAL STABILIZER FAIRING. REPAIRED SKIN AT FS 1476 BELOW VERTICAL STABILIZER FAIRING IAW DELTA EA 464026-14AD. REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE ONLY. ADD ITIONAL ENGINEERING AUTHORIZATION (ERA REVISION) IS REQUIRED FOR CONTINUED SERVICE OF THIS REPAIR LONGER THAN 24 MONTHS FROM REPAIR ACCOMPLISHMENT. 2 L 7 2 4F RT A6WE 2007102400050 20071024 00050 NM 2007 10 24 DL764071345 1 20071013 A 3350 LIGHT BOEING 767 767432ER 1385134 NM SEAT 47GF INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 833MH 29706 FOUND EMERGENCY LIGHT ABOVE 47GF INOP. RELAMPED AND OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2007102400051 20071024 00051 NM 2007 10 24 DL764071346 1 20071013 A 3350 LIGHT BOEING 767 767432ER 1385134 NM SEAT 37AB INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 833MH 29706 EMERGENCY LIGHT ON LT SEAT ROW INOP FROM 37AB AFT. T/SHO FOUND LOOSE DEEDS CONNECTION, SEVERAL AND RECONNECTED FEEDER. 2 L 7 2 4F RT A1NM 2007102400055 20071024 00055 NM 2007 10 24 DL777071353 1 20071011 A 8011 BEARING BOEING 777 777232 1385232 NM RROYCE RB211 RB211TRENT89 NE STARTER FAILED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 866DA 19059 29738 051193 DURING ENG START GND CREW REPORTED SPARKS IN NR 2 ENG THEN SIGNALED A TAIL PIPE FIRE ENG AUTO SHUTDOWN CK LIST ACCOMPLIS HED. INSPECTED TAIL PIPE NO DEFECTS NOTED. FOUND NR 2 ENG STARTER BEARINGS FAILED. REMOVED AND REPLACED NR 2 ENG STAR TER PER M/M. LEAK CK AND OPS CKS GOOD, MFG P/N 3505788-7, S/N OFF 489C, S/N ON 593C. 2 L 7 2 4F 4 F RT T00001SE E00050EN 2007102400057 20071024 00057 NM 2007 10 24 DL76G071357 1 20071015 A 2530 FAN BOEING 767 767332 1382001 NM MID GALLEY OVEN SEIZED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 174DZ 29693 POSSIBLE AIR CONDITIONING TRANSIENT SMELL AT FL380. DESCENDED TO FL240 TURNED OFF RECIRC FANS, NO FURTHER SMELL. AFTER LANDING FLT ATT REPORT ELECTRICAL SMELL FORM MID GALLEY. UPON INSPECTION FOUND MID GALLEY AFT LOWER OVEN FAN SEIZED. ALSO ELECT SMELL PRESENT IN OVEN FWD OVEN TO MCO AND PLAC PER MEL. 2 L 7 2 4F RT A1NM 2007102400059 20071024 00059 EA 2007 10 24 SWIA200718776 1 20071009 A 3350 COVER CNDAIR CL600 CL6002C10 1390015 EA SIGN MISSING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 742SK 10197 FLT 6758 - OVERHEAD EMERGENCY EXIT SIGN IN CABIN IS MISSING COVER. REPLACED EXIT SIGN COVER. 2 L 7 2 4F RT A21EA 2007102400062 20071024 00062 2007 10 24 SWIA200718779 4 20071010 A 3425 COMPUTER CNDAIR CL600 CL6002D24 1390016 EA AHRS INTERMITTENT A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 817SK 15107 AHARS COMPUTER NR 1 AND NR 2 DROPPED OFF LINE TWO SEPARATE TIMES IN FLIGHT. REPLACED BOTH AHRS COMPUTERS IAW AMM 34-21- 01, P/N 622-9336-400, S/N OFF 275LP, 275LC. 2 L 7 2 4F RT A21EA 2007102400063 20071024 00063 EA 2007 10 24 SWIA200718780 1 20071011 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 970SW 7881 FLT 6028 - AFT CEILING LEVEL EMERGENCY FLOODLIGHT IS INOP. RELAMPED AFT CEILING EMERGENCY LIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007102400064 20071024 00064 EA 2007 10 24 SWIA200718781 1 20071011 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR LACK OF LUBE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 925SW 7682 FLT 6729 - SERVICE DOOR WILL NOT OPEN FROM THE OUTSIDE. LUBED SERVICE DOOR OUTER HANDLE. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007102400070 20071024 00070 NM 2007 10 24 07FDEA04606 1 20071016 A 5753 ARC40091 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM LT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 620FE 48791 CRACK FOUND DURING HFEC OPEN HOLE INSPECTION ON THE MOST OUTBOARD, LOWER FASTENER HOLE COMMON TO THE ARC4008 AND ARC4009 LEFT OUTBOARD FLAP SUPPORT FITTING. 10-30-07 REMOVED AND REPLACED AS PER MD11 CMM 57-52-04. FLAP ADJUSTMENT TES T CARRIED OUT AS PER AMM 27-50-00-830-805. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007102400071 20071024 00071 EU 2007 10 24 07FDEA04607 1 20071016 A 5753 A5734008 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION ON RT TOP SKIN ON WHOLE AREA AROUND FASTENER HOLES. REPAIR PERORMED BY BLENDOUT CORROSION, OVERSIZING T HE HOLES AND FLAP PEENING IAW EA 6-5720-112522 AND RAS/BAE/1005287/2007 ISS A. 2 L 7 2 4F RT A35EU 2007102400072 20071024 00072 EU 2007 10 24 07FDEA04608 1 20071016 A 5315 A53779699200 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 670FE 777 MAIN CARGO COMPARTMENT FLOORBEAM CRACKED FRAME 27 BETWEEN YD AND YE(RBC 37 AND RBL18). FABRICATED AND INSTALLED CROSSBE AM COUPLING IAW SRM 53-10-15. 2 L 7 2 4F RT A35EU 2007102400073 20071024 00073 NM 2007 10 24 07FDEA04609 1 20071016 A 5330 6561611 SKIN BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 19TH RT WINDOW PLUG EXTERIOR SURFACE HAS CORROSION (APPROX 720C 6"). REMOVED AND REPLACED WINDOW PLUG REF MM 56-20-000- 4, PRIMED AND PAINTED REF SRM 51-10-2 APPLIED LPS REF 51-10-2. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007102400076 20071024 00076 NE 2007 10 24 AALA20071932 2 20071013 A 7323 GOVERNOR BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4B3 NE RT ENGINE INOPERATIVE A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 638AA 24596 31151 CLE INFLIGHT T222/13OCT LAX TO BOS - RIGHT ENGINE WOULD NOT REACH CLIMB POWER. MAXIMUM ENGINE PRESSURE RATIO (EPR) ATTA INABLE WAS ABOUT 1.4 EPR. LANDED CLE WITHOUT INCIDENT. REPLACED RIGHT FUEL FLOW GOVERNOR. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2007102400077 20071024 00077 WP 2007 10 24 AALA20071936 1 20071015 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 237AA 49253 LGA - EMERGENCY LIGHT AT SEAT ROW 8 INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD BIN FOR EMERGENCY LIGHT AT SEAT ROW 8. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007102400078 20071024 00078 EU 2007 10 24 AALA20071937 1 20071015 A 3350 BR964814 FIXTURE AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70072 515 JFK - EMERGENCY LIGHT AT SEAT ROW 10G INOPERATIVE. REPLACED LIGHT ASSEBMLY FOR EMERGENCY LIGHT AT SEAT ROW 10G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007102400079 20071024 00079 NM 2007 10 24 AALA20071938 1 20071015 A 3350 P4010049 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 329AA 22329 JFK - EMERGENCY LIGHTS AT RIGHT AFT SECTION OF COACH INOPERATIVE. REPLACED BATTERY PACK AT FOR EMERGENCY LIGHTS AT RIGH T AFT SECTION OF COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007102400080 20071024 00080 NM 2007 10 24 AALA20071939 1 20071015 A 3350 P4010049 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 329AA 22329 JFK - EMERGENCY LIGHT AT RIGHT AFT SECTION OF BUSINESS CLASS AND FORWARD SECTION OF COACH INOPERATIVE. REPLACED BATTERY PACK AT M9029 FOR EMERGENCY LIGHT AT RIGHT AFT SECTION OF BUSINESS CLASS AND FORWARD SECTION OF COACH. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007102400082 20071024 00082 NM 2007 10 24 AALA20071933 1 20071013 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 768AA 33540 JFK - EMERGENCY LIGHTS AT SEAT ROWS 20 TO 26 INOPERATIVE. REPLACED BATTERY PACK AT RIGHT NUMBER THREE DOOR FOR EMERGENC Y LIGHTS AT SEAT ROWS 20 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007102400084 20071024 00084 NM 2007 10 24 AALA20071935 1 20071015 A 3350 1104441 MOUNT BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 385AM 27059 ORD - EMERGENCY EXIT LIGHT OVERHEAD COCKPIT DOOR INOPERATIVE. REPLACED EXIT SIGN BASE PLATE FOR EMERGENCY EXIT LIGHT OV ERHEAD COCKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007102400086 20071024 00086 NM 2007 10 24 NWAA073476306 1 20071014 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY EXIT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 666US 23821 DURING LINE CHECK, FOUND UPPER DECK LT EMERGENCY DOOR PACK INOPERATIVE. REPLACED BATTERY PACK PER AMM 52-23-14. 2 L 7 4 4F RT A20WE 2007102400087 20071024 00087 NM 2007 10 24 F3LA200700280 1 20071012 A 5330 SKIN AIRBUS A319 A319111 3930336 NM FUSELAGE DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 947FR 2806 BIRD STRIKE TO FWD LT SIDE OF FUSELAGE. LT SKIN PANEL DENTED AT FR 4, 11.5" ABOVE STBY STATIC PORT, 2.5" ABOVE SIDE STR 3" BY 4" BY .067. LT SKIN PANEL DENTED AT FR 5 15.5" FROM STBY STATIC PORT, 2.5" ABOVE LT SIDE STR 3.8" BY 2.8"BY .037 . INSPECTED AREA PER EA A9-53R-12191. NO ADDITIONAL DAMAGE FOUND. INITIATED TDI 0000682 FOR PERMANENT REPAIR, TO BE D ETERMINED BY ENGINEERING WITHIN 50 FLIGHT CYCLES. PERFORMED HFEC AND DVI INSPECTIONS OF AREAS TO BE REPAIRED IAW NTM 51 -10-08 AND 51-90-00 NORTEC 2000S AND S/N F9TAB2309C, CAL DUE DATE 08/2008. REWORKED DAMAGED SKIN AREA FR 4 AND FR 5 TO WITHIN LIMITS IAW SRM 51-73-00 FIG 5 AND EA A9-53R-12191. REMOVED SAID FASTENERS IN FR 4 AND FR 5 PER EA A9-53R-12191 A 2 L 7 2 4F RT A28NM 2007102400088 20071024 00088 NM 2007 10 24 F3LA200700281 1 20071014 A 3397 WIRE HARNESS AIRBUS A319 A319111 3930336 NM EMERGENCY LIGHTS DAMAGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 906FR 1684 INSPECTION REPORTED SEAT ROW 9ABC SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED WIRE HARNESS AT SEAT R OW 9ABC IAW ESPM 20-33-00. PERFORMED OPERATIONAL TEST ON EMERGENCY LIGHTS IAW AMM 33-51-00-710-007. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 2007102400090 20071024 00090 2007 10 24 F3LA200700283 4 20071012 A 2565 LANYARD AIRBUS A319 A319111 3930336 NM ESCAPE SLIDE MISSING A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 945FR 2751 DURING C-1 CHECK, INSPECTION REPORTED RT OVERWING EMERGENCY ESCAPE SLIDE RELEASE CABLE FAILED TO RETRACT DURING MANUAL R ELEASE TEST. REMOVED AND REPLACED PULL CABLE AND OPS CHECKED RT OVERWING EXIT SLIDE RELEASE CABLE IAW AMM 52-21-00, PB5 01, AND TASK CARD C522101-3. 2 L 7 2 4F RT A28NM 2007102400091 20071024 00091 NM 2007 10 24 QXEA200701568 1 20071013 A 5270 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM GALLEY DOOR FALSE ACTIVATION A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 431QX 4164 LAX FLIGHT NR 2446: CLIMBING THROUGH 7000 FT, RECEIVED THE FUSELAGE DOORS MASTER WARNING. THE GALLEY SERVICE DOOR SHOWE D OPEN ON DOOR PAGE. FA ADVISED DOOR HANDLE WAS OUT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE, DURING TAXI TO GATE, NO TICED AFT SERVICE DOOR EXTERNAL HANDLE EXTENDING OUT APPROX 1/4". PERFORMED OPS TEST OF AFT SERVICE DOOR. OPS CHECK GO OD. PRESSURIZED A/C IAW Q400 AMM TASK 21-00-00-863-801. AFT SERVICE DOOR REMAINED LOCKED. DEPRESSURIZED A/C IAW TASK 21-00-00-863-802. PERFORMED GVI OF AFT SERVICE DOOR. OPS TEST OF AFT SERVICE DOOR IAW TASK 52-41-00-710-801. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102400092 20071024 00092 EU 2007 10 24 07FDEA04613 1 20071017 A 5730 A5734008 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION ON LT WING TOP SKIN OVER THE WHOLE WING AREA IN AREA OF FASTENER HOLES REPAIR PERFORMED BLEND OUT THE CORROSION, FLAP PEENING AND NDT FOR CRACK FREE IAW EA 6-5720-112521 AND RAS/BAE/1005138/2007 ISS A. 2 L 7 2 4F RT A35EU 2007102400097 20071024 00097 NM 2007 10 24 07FDEA04618 1 20071017 A 5280 ARC28272 DOOR DOUG MD11 MD11F 3023600 NM RT MLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 620FE 48791 RIGHT MAIN LANDING GEAR FLIPPER DOOR FOUND CRACKED PASS THROUGH STOP DRILL. 10-30-07 REMOVED AND REPLACED AS PER AMM 32-14-10-4. OPERATION CHECK CARRIED OUT AS PER AMM 32-31 -00-700-803. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 . 2 L 7 3 4F RT A22WE 2007102400100 20071024 00100 WP 2007 10 24 07FDEA04621 1 20071017 A 5340 AFA32461 FITTING DOUG DC10 DC1010F 3022111 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 CTR CARGO COMPT RT TUNNEL SEVERE CORROSION WITH EXFOLIATION ON FITTING. ACCOMPLISHED EA NR 8-5310-111460. 2 L 7 3 4F A22WE 2007102400104 20071024 00104 NM 2007 10 24 07FDEA04629 1 20071017 A 5340 69133532 ATTACH FITTING BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 5" CRACK ON RT ATTACH FITTING FOR BULKHEAD 1183 BEAM AT BS 1182, BL 0, WL 166 TO 161. REPLACED CHANNEL, REF DWG 69-133 53, REF SRM 51-30-2 PG 1. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007102400105 20071024 00105 NM 2007 10 24 07FDEA04630 1 20071017 A 5311 65163517 FRAME BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 CORROSION ON FWD FRAME AROUND MESC ACCESS DOOR FWD LOCK PIN PLATE, FS 423, BL 0 WL 151. REMOVED CORROSION ON FWD FRAME FOR MESC DOOR, ORIGINAL .040, REMOVED .012", REMAINING .028". LOT OF LIMITS REF SRM 51-10-1 PG 2, NOTE J, AND 53-10-1 PG 2A FIG 1. SHEET 3 DETAIL 4, TOOL NR IN17-0623, CAL DUE 9-18-08. REMOVED AND INSTALLED NEW FRAME.REF 51-20-1 PG 14 FIG 3. HEAT TREATED NEW FABBED FRAME REF NR N00461. REMOVED AND REINSTALLED PANELS FOR ACCESS AT RBL 14, STA 420-450, LBL 14 STA 420-450. REF SRM 51-30-2. TREATED AND PRIMED REF 51-10-2 APPLIED RESIN, POTTING COMPOUND REF SRM 51-40-1 A MM 52-00-00 ADJUSTED DOOR REF MM 52-40-011-1, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007102400111 20071024 00111 NM 2007 10 24 QXEA200701569 1 20071017 A 3260 LAMP BOMBDR DHC8 DHC8402 1390042 NM MLG INDICATOR NO TEST A QXEA L ABORTED APPROACH L NO TEST AP APPROACH 1 NM 09 405QX 4047 HLN FLIGHT NR 2324: ON APPROACH, GEAR SELECTED DOWN W/3 GREEN INDICATED. ON SHORT FINAL, R MAIN INDICATOR DID NOT SHOW GREEN. EXECUTED MISSED APPROACH ON GO-AROUND. NR 1 POWER LEVER ADVANCED PAST RATING DETENT. NOTED 109 PERCENT TORQUE. ON GO-AROUND, NOTED 3 GREEN ON ALTERNATE EXTENSION INDICATION. C/W LAMP TEST. RT LAMP LIGHT DOES NOT TEST. MAINTENA NCE INSPECTED AND FOUND RT MLG DOWNLOCK LAMPS INOP. RELAMPED IAW CMM SUBTASK 32-31-15-960-003. RT MLG DOWN LOCK LIGHT NOW OPS CHECKS GOOD. NO OTHER DEFECTS NOTED WITH LANDING GEAR INDICATION. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102400115 20071024 00115 EA 2007 10 24 QXEA200701540 1 20071013 A 2133 OUTFLOW VALVE CNDAIR CL600 CL6002C10 1390015 EA CABIN PRESSURE OBSTRUCTED A QXEA B A EMER. DESCENT UNSCHED LANDING C J F.O.D. WARNING INDICATION CR CRUISE 1 NM 09 604QX 10019 RNO - FLIGHT 2516, AT CRUISE FLIGHT AT 38,000 FEET RECEIVED A MASTER CAUTION MESSAGE FOR THE CABIN ALTITUDE. CABIN ALTI TUDE CONTINUED TO CLIMB TO 11,400. THE PASSENGER OXYGEN MASKS DEPLOYED AND STARTED A DESCENT TO A SAFE ALTITUDE. DIVER TED TO RENO AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE FOUND THE NR 1 SAFETY OUTFLOW VALVE HAD LOOSE INSULATION AROUND IT KEEPING THE VALVE IN THE OPEN POSITION. CLEARED INSULATION FROM AREA. PERFORMED A OPERATIONAL CHECK OF THE PRESSURIZATION SYSTEM. CHECKS GOOD WITH NO DEFECTS. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007102400118 20071024 00118 EA 2007 10 24 QXEA200701545 1 20071016 A 2611 SMOKE WARNING CNDAIR CL600 CL6002C10 1390015 EA LAVATORY ACTIVATED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 613QX 10045 PDX - FLIGHT 2557 (PDX-BUR) ON TAKEOFF ROLL AT 130 KNOTS, RECEIVED A LAVATORY SMOKE DETECTOR WARNING. ABORTED TAKEOFF A ND RETURNED TO THE GATE. AIRCRAFT CURRENTLY DOWN FOR REPAIRS. 2 L 7 2 4F RT A21EA 2007102400119 20071024 00119 EA 2007 10 24 QXEA200701546 1 20071015 A 2131 GG6709800111 CONTROLLER CNDAIR CL600 CL6002C10 1390015 EA CABIN PRESSURE FAILED A QXEA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 610QX 12615 9311 10033 MFR - FLIGHT 2526 (SMF-PDX), EN ROUTE AT CRUISE FLIGHT (38,000 FT) RECEIVED A CABIN PRESSURE WARNING. DEPLOYED THE PASS ENGER OXYGEN MASKS AND DESCENT TO 11,000 FEET. DIVERTED TO MFR AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE FOUN D A CABIN PRESSURE CONTROLLER FAILURE (CODE 009). REPLACED THE CONTROLLER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007102400121 20071024 00121 2007 10 24 TSAA0731057 4 20071015 A 3460 9650649005 FDAU BOEING 737 7372X6C 1384552 NM FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 841AL 23123 NON-ETOPS FLIGHT 278 HNL-KOA, AT 5000 FT, THE CREW NOTED THE FLIGHT RECORDER OFF LIGHT ILLUMINATED. THE CREW RETURNED T O HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLIGHT DATA ACQUISITION UNIT PER AMM 31-24-11 WITH ALL CHECKS SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007102400125 20071024 00125 NM 2007 10 24 QXEA200701573 1 20071017 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM NOSE TRIM ILLUMINATED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 415QX 4081 PDX FLIGHT NR 3150: TAKEOFF CONFIG RELATED TO NOSE TRIM. COULD NOT GET FULL NOSE UP TRIM. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE REINITIALIZED FLIGHT CONTROL SYSTEM BY CYCLING FCS ECU 1 AND 2 CB'S. ALL INDICATIONS CHECK NORMAL. NO DEF ECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102400127 20071024 00127 EA 2007 10 24 SWIA200718783 1 20071014 A 2530 COFFEEMAKER CNDAIR CL600 CL6002B19 1900309 EA GALLEY ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 958SW 7833 CREW REPORTS BURNING ODOR COMING FROM COFFEEMAKERS. REPLACED NR 1 AND NR 2 COFFEEMAKERS AS REQUIRED. 2 L 7 2 4F RT A21EA 2007102400128 20071024 00128 EA 2007 10 24 SWIA200718784 1 20071014 A 7830 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER ILLUMINATED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 932SW 7714 FLT 6709 - RIGHT REVERSE UNLOCK MESSAGE APPEARED INFLIGHT. DEFERRED THRUST REVERSER PER MEL 71-30-1 APPENDIX M-2 SECTIO N D. NO MESSAGES SHOWN AT THIS TIME. 2 L 7 2 4F RT A21EA 2007102400130 20071024 00130 SO 2007 10 24 SWIA200718786 1 20071012 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 291SW 120318 FLT 5550 - EXIT SIGN AT SEAT 9C IS BROKEN. REPLACED EMERGENCY EXIT SIGN ASSEMBLY. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007102400131 20071024 00131 SO 2007 10 24 SWIA200718787 1 20071015 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 290SW 120317 FLT 5581 - EXIT SIGN AT 6A BROKEN. REPLACED EMERGENCY EXIT SIGN ASSEMBLY AT 6A. OPS TEST GOOD. 2 L 7 2 4T RT A31SO 2007102400132 20071024 00132 NM 2007 10 24 NWAA072486304 1 20071016 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 664US 23819 DURING OVERNIGHT LINE CHECK, FOUND LEFT SIDE OF AFT FUSELAGE EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED PO WER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007102400133 20071024 00133 NM 2007 10 24 NWAA073486304 1 20071016 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 664US 23819 DURING OVERNIGHT LINE CHECK, FOUND LEFT SIDE OF AFT FUSELAGE EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED PO WER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007102400134 20071024 00134 WP 2007 10 24 07FDEA04622 1 20071017 A 5347 607158 SEAT TRACK DOUG DC10 DC1030F 3023504 WP BS 735-755 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 320FE 47835 MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREAS AT F/S 735-755 LBL 8. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 VOL 1 FIG 1 SHEET 4. 2 L 7 3 4F RT A22WE 2007102400144 20071024 00144 EU 2007 10 24 07FDEA04642 1 20071018 A 5320 R538D104820200 ADAPTER AIRBUS 310 A310203 3930313 EU MAIN CABIN CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 MAIN CABIN FR44, RT SIDE, ADAPTER CRACKED OVERWING BOX REPLACED FR 44 RT SIDE ADAPTER IAW SRM 51-40-21 P7 AND A310-200 A MM 20-21-12. 2 L 7 2 4F RT A35EU 2007102400145 20071024 00145 EU 2007 10 24 07FDEA04644 1 20071018 A 5320 R538D104820200 ADAPTER AIRBUS 310 A310203 3930313 EU MAIN CABIN CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 MAIN CABIN FR 43 RT SIDE, ADAPTER CRACKED OVERWING BOX REPLACED FR 43 RT SIDE ADAPTER IAW A310-200 SRM 51-40-21 P7 AND M A310-200 AMM 20-21-12 BY TIMCO EMP NR 5252/QC204. 2 L 7 2 4F RT A35EU 2007102400151 20071024 00151 NE 2007 10 24 DHLA200700057 2 20071018 A 7314 PUMP BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE FUEL SYSTEM FAILED A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 754DH 22008 AT START OF TAKEOFF, 1.4 EPR NR 2 ENGINE FAILED COMPLETED ABNORMAL PROCEDURE. REPLACED NR 2 ENG FUEL PUMP IAW PRATT AND WHITNEY JT8D M/M GROUND RAN AND LEAK CK GOOD AT THIS TIME IAW 73-11-01. PERFORMED MPA RUN PER JRH 7.7. 2 L 7 3 4F 4 F A3WE E2EA 2007102400154 20071024 00154 NM 2007 10 24 DU4R2007176 1 20071012 A 5311 146N1017 FRAME BOEING 757 757232 1384965 NM BS 1520 DENTED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 6713Y 30777 FOUND DENTED FRAME AT BS 1520 S-26L (IN AFT PIT). REPAIRED BY REMOVING DOUBLER, FABRICATED AND INSTALLED DOUBLER REPAIR CHANNEL 21-1/2 BY 2-1/2 BY 1 FROM 7075-T6 .080 IAW B757 SRM 51-40-05, 51-20-01 AND 51-40-02. 2 L 7 2 4F RT A2NM 2007102400155 20071024 00155 NM 2007 10 24 DU4R2007177 1 20071012 A 5311 146N104217 FRAME BOEING 757 757232 1384965 NM BS 1500 DENTED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 6713Y 30777 FOUND DENTED FRAME AT BS 1500 S-26L (IN AFT PIT). REPAIRED BY REMOVING DOUBLER AND STRINGER TIES, FABRICATED AND INSTAL LED DOUBLER REPAIR CHANNEL 21-1/2 BY 2-1/2 BY 1 FROM 7075-T6 .080 IAW B757 SRM 51-40-02, 51-40-05 AND 51-00-00D. 2 L 7 2 4F RT A2NM 2007102400160 20071024 00160 NM 2007 10 24 07FDEA04653 1 20071019 A 5311 53FX13501 FRAME BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 LOWER STUB FRAME EXTENTION AT BS 560, WEB IS CRACKED ABOVE AND INBD OF STR 21 L, AT RIVET HOLE MARKED END OF DOT WITH BL ACK DOT REPLACED LOWER STUB FRAME EXTENSION REF SRM 51-30-2, AND DWG 53FX1350. TREATED AND PRIMED REF SRM 51-10-2. 2 L 7 3 4F RT A3WE 2007102400167 20071024 00167 NM 2007 10 24 AALA20071944 1 20071016 A 3350 BULB BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 681AA 25338 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE EXIT DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT AND RIGHT NUM BER ONE EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007102400171 20071024 00171 NM 2007 10 24 AALA20071941 1 20071015 A 3241 TRANSDUCER BOEING 757 757223 1384957 NM ANTI SKID SYS MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 SW 21 616AA 24524 JFK INFLIGHT T592/15OCT MIA TO LGA - AIRCRAFT DIVERTED TO JFK DUE TO ANTI-SKID EICAS MESSAGE. LANDED JFK WITHOUT INCIDE NT. REPLACED ANTI-SKID TRANSDUCER ON NUMBER FIVE BRAKE. NO FURTHER INCIDENTS SINCE TRANSDUCER REPLACED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007102400172 20071024 00172 EA 2007 10 24 QXEA200701577 1 20071018 A 3250 9752753 VALVE CNDAIR CL600 CL6002C10 1390015 EA NLG STEERING FAILED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 610QX 11907 10033 PDX - FLIGHT 2432, ON TAXI OUT RECEIVED A STEERING INOP CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENENCE REPLACED TH E NR 3 HYDRAULIC BALANCE RELIEF VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007102400176 20071024 00176 NM 2007 10 24 DHLA200700054 1 20071010 A 5330 SKIN BOEING 727 727214 138407R NM FUSELAGE DAMAGED A DHLA K NONE O OTHER TX TAXI/GRND HDL 1 GL 05 788AT 21958 DURING PUSHBACK TOWBAR BROKE AND A/C HIT TUG. REPAIRED DAMAGED SKIN AREA IAW BOEING 727 SRM 53-30-03. REPLACED 2 INTER COSTALS IAW BOEING 727SRM 51-30-02. FABRICATED INTERCOSTALS PER BOEING DWG 69-16996. 2 L 7 3 4F A3WE 2007102400178 20071024 00178 GL 2007 10 24 11470 1 20071019 A 2460 C4B CIRCUIT BREAKER CIRRUS 120 CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO HARTZL HCJ3Y PHCJ3YF1 GL MCU TRIPPED E J4PA O OTHER J WARNING INDICATION CR CRUISE 1 SO 13 851CD 00376 1493 917741 FP4176B DURING A FLIGHT FROM KAAF TO KLUL, THE NR 1 GARMIN BECAME INOPERATIVE. RETURN TO ORIGIN NO INCIDENT. FERRIED TO KSGJ F OR REPAIR. FOUND CB FOR PARTIAL POWER OF MAIN BUSS OPEN. RESET CB. GROUND CHECKED GOOD. LEFT KSGJ FOR KMLB AND THE C B TRIPPED AGAIN. FERRIED THE AIRCRAFT BACK TO KSGJ FOR REPAIRS AGAIN. REPLACED THE ENTIRE MCU, OPS CHECKED SATISFACTOR Y. 1 L 7 1 3O 3 O NT A00009CH E3SO 5 C P36EA 2007102400180 20071024 00180 NM 2007 10 24 NWAA073516301 1 20070929 A 5310 SHEAR WEB BOEING 747 747451 1384940 NM BS 1120 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 661US 23719 DURING "M" CHECK, FOUND CRACKS IN RT AND LT SHEAR WEBS AT TENSION TIE AREA BS 1120. REPAIRED PER EA 63-210136. 2 L 7 4 4F RT A20WE 2007102400181 20071024 00181 NM 2007 10 24 QXEA200701580 1 20071020 A 3230 LANDING GEAR BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 425QX 4039 SEA FLIGHT NR 2319: AFTER TAKEOFF IN YEG, SELECTED GEAR UP. ALL 3 GEAR DOOR LIGHTS ILLUMINATED AND ALL 3 GEAR UP SAFE L IGHT ILLUMINATED. THE 3 GREEN GEAR DOWN LOCKED LIGHTS EXTINGUISHED. GEAR STAYED IN THIS CONFIGURATION FOR APPROX 10 SE CONDS. THEN LANDING GEAR INOP AND MASTER CAUTION ILLUMINATED FOR 10 SECONDS THEN EXTINGUISHED. GEAR THEN SEEMED TO GO UP NORMALLY. MAINTENANCE FOUND THE PSEU SHOWS FAULT RGDRCL UNREASONABLE FAR. RIGGED RIGHT MAIN GEAR AFT DOORS IAW DHC- 8-400 MM TASK 32-12-01-830-801. CLEARED FAULTS FROM PSEU. LANDING GEAR PRIMARY EXTENSION AND RETRACTION SYSTEM OPS CHE CK GOOD 12 TIMES IAW DHC-8-400 MM TASK 32-31-00-710-801. ALL GEAR INDICATIONS NORMAL DURING OPS TESTS. NO PARTS REPLAC 2 H 7 2 4T RT A13NM 2007102400187 20071024 00187 SO 2007 10 24 SIMA200729301 1 20071015 A 2130 CABIN PRESSURE EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A SIMA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 21 627AE 145121 IN CRUISE FLT AT FL250 HAD A SLOW CABIN DEPRESSURIZATION. CABIN ALT GOT TO 10,100 FEET. DID EMERGENCY DESCENT TO 10,00 0 FEET. RAN PRESS AUTO FAIL AND CABIN ALTITUDE IN AMBER RANGE CHECK LISTS. LEVEL AT 10,000 FEET. CABIN ALT STABILIZED AT 8,000 IN MANUAL MODE. 2 L 7 2 4T RT T00011AT 2007102400188 20071024 00188 SO 2007 10 24 SIMA200829302 1 20071014 A 2520 7277226501 PCU EMB 145 EMB145LR 3260212 SO CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 694AE 14500869 MELD PSU LIGHTS FLICKERED DURING TAXI FOLLOWED BY ELECTRICAL ODOR IN CABIN AND COCKPIT. REMOVED AND REPLACED PCB ASSY P ER AMM 25-22-05. OPS CHECK OK RESTORED MEL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007102400189 20071024 00189 SO 2007 10 24 SIMA200729303 1 20071014 A 2120 UNKNOWN EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL FUMES A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 805AE 145489 TURBINE OIL FUMES ARE BEING INTRODUCED INTO THE CABIN AND COCKPIT THROUGH ENG BLEED 1. IF BOTH PACKS ARE DRIVEN FROM BL EED 2. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007102400190 20071024 00190 2007 10 24 SIMA200729304 2 20071014 A 7240 LINER EMB 135 EMB135KL 3260302 SO COMBUST CHAMBER DAMAGED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 848AE 145710 CREW NOTED IN CLIMB-OUT AT 14000 NR 1 ENGINE ITT FLUCTUATED FROM 788-747 +/- 4*. PERFORMED BOROSCOPE OF LT ENGINE COMBU STER LINER FOUND LINER TO HAVE OUT OF LIMITS DAMAGE. ENGINE REQUIRED REPLACEMENT. REMOVED AND REPLACED LT ENGINE IAW W C 71-000-00. FCF PASSED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007102400191 20071024 00191 SO 2007 10 24 SIMA200729502 1 20071018 A 2150 ACTUATOR EMB 135 EMB135KL 3260302 SO FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 825AE 145589 RAM AIR FAIL MSG ON EICAS AFTER TAKEOFF COMPLIED WITH AOM VOL 1 RETURNED TO ABI. ADJ RT RAM AIR LINER ACTUATOR IAW EMB- 140 AMM 21-25-03. SYS CKS GOOD AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007102400193 20071024 00193 SO 2007 10 24 SIMA200729604 1 20071019 A 2120 UNKNOWN EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL CABIN ODOR A SIMA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 805AE 145489 CAE311416 STRONG OIL ODOR IN BLEED SYSTEM AFTER TAKEOFF AND ON FINAL APPROACH. REMOVED AND REPLACED NR 1 ENGINE IAW EMB WORK CARD NR 71-000-00. GROUND RAN AND LEAK CHECKED IAW EMB WORK CARD 72-700-00. NO DEFECTS AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007102400194 20071024 00194 2007 10 24 SIMA200729501 2 20071016 A 7261 23073561 CARBON SEAL EMB 145 EMB145LR 3260212 SO ENGINE LEAKING A SIMA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 932AE 14500915 EN ROUTE TO PIA CREW GOT 'LAV SMOKE' ON EICAS. SOME SMOKE NOTED IN GALLEY. NO OTHER SMOKE NOTED. REMOVED AND REPLACED ENGINE 2 ZERO-CARBON SEAL IAW RRMM 72-25-25-000-801 AND 72-25-25-400-801-A. NO FURTHER OIL LEAK NOTED. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007102400195 20071024 00195 EA 2007 10 24 QXEA200701585 1 20071021 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA CABIN ODOR A QXEA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 604QX 10019 DEN - RECEIVED A APU FAULT MESSAGE ON START-UP. CAUTION THEN WENT AWAY AND THERE WAS A OIL ODOR FROM THE PACKS. MAINTE NANCE PERFORMED 3 STARTS OF THE APU WITH NO FAULTS NOTED. THE MDC DATA SHOWED A HUNG START. FOUND NO ODOR IN THE PACKS . APU OPERATES NORMALLY WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007102400197 20071024 00197 NM 2007 10 24 QXEA200701583 1 20071019 A 3260 CONTROL PANEL BOMBDR DHC8 DHC8402 1390042 NM MLG FALSE INDICATION A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 425QX 381 381 4039 PDX FLIGHT NR 2229: AFTER TAKEOFF FROM SEA, RIGHT MAIN GEAR DOOR CAUTION LIGHT ILLUMINATED. STAYED ON ALL THE WAY TO PD X. DID NOT EXCEED 185 KTS. PERFORMED ALTERNATE GEAR EXTENSION. MAINTENANCE C/W OPERATIONAL TEST OF PRIMARY EXTENSION AND RETRACTION SYSTEM IAW Q400 AMM TASK 32-31-00-710-801. ALL GEAR DOORS OPERATED NORMALLY AND ALL LANDING GEAR INDICAT IONS WERE NORMAL. INTERROGATED PSEU AND FOUND FAULT 'DIN01A UNREASONABLE FALSE'. REMOVED AND REPLACED LANDING GEAR SEL ECTOR PANEL. FUNCTIONAL CHECK OF PANEL WAS GOOD. NO DEFECTS NOTED AFTER NUMEROUS CYCLES OF LANDING GEAR EXTENSION RETR ACTION. OPS CHECK FLIGHT PERFORMED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102400198 20071024 00198 NM 2007 10 24 QXEA200701584 1 20071018 A 3010 4100S01806 TMU BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 422QX 1705 1705 4150 RNO FLIGHT NR 2255: IN CRUISE, RECEIVED DEICE PRESSURE MASTER CAUTION. PERFORMED THE CHECK LIST AND FOUND THE SECOND SE GMENT INBOARD FROM THE RIGHT WING WAS NOT INFLATING AND THE LIGHT DID NOT ILLUMINATE ON THE OVER HEAD PANEL. FLIGHT WAS DIVERTED. MAINTENANCE FOUND THE NR 2 DDV RECEIVING INTERMITTENT OPEN VOLTAGE OF 14.6V. RANG WIRES FROM NR 2 DDV TO TM U WIRES. CHECK GOOD. REPLACED TMU. GROUND RAN BOOTS FOR 1 HOUR WITH NEW TMU. CDS LOGGED NO FAULTS. AIRCRAFT RETURNE D TO SERVICE. 2 H 7 2 4T RT A13NM 2007102400199 20071024 00199 NM 2007 10 24 NWAA073525649 1 20071019 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 549US 26496 DURING OVERNIGHT CHECK, FOUND EXIT SIGN AT DOOR 2R INOP. MAINTENANCE REMOVED AND REPLACED POWER PACK. OPERATIONAL CHEC KED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007102400203 20071024 00203 EU 2007 10 24 07FDEA04658 1 20071021 A 5340 A53070037201 FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 LEFT SIDE CRACK INDICATION IN FR 43A LOWER HOLE APPROX 12 O'CLOCK IN FRAME FITTING ONLY REMOVED LOWER FRAME FITTING AT F R 43A THAT IS CRACKED. INSTALLED NEW FITTING IAW A310 51-40-40, 51-40-21 PG 24. 2 L 7 2 4F RT A35EU 2007102400204 20071024 00204 NM 2007 10 24 07FDEA04659 1 20071021 A 5220 50797890 SKIN BOEING 727 727233 138408A NM ZONE 800 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 RT OVERWING DOOR EXT SKIN IS CORRODED/GOUGED ALONG LWR EDGE. REMOVED CORROSION AND GOUGE REF SRM 51-10-02 AND SRM 52-00 -2, CHECKED LIMITS, ORIGINAL "T" IS .045, MATERIAL "T" REMOVED .015" REMAINING "T" IS .030". OUT OF LIMITS VERIFIED B Y SRM 52-00-2 PAGE 3 FIG 2. MANUFACTURED REPAIR PARTS REF SRM 53-00-3 FIG 4 PG 8. REPAIR DOUBLER REF SRM 52-00-3 FIG NR 4. INSTALLED FILLER AND DOUBLER REF SRM 51-30-2 PG 2. RE-FINISHED REF SRM 51-10-2. THIS IS CLASSIFIED AS A MAJOR R EPAIR. 2 L 7 3 4F RT A3WE 2007102400209 20071024 00209 SO 2007 10 24 CHQA20070062 1 20071018 A 2730 UNKNOWN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL ELEVATORS MALFUNCTIONED A CHQA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 11 257JQ 145812 CAE311677 IND TO LGA - DURING TAKEOFF, FLIGHT CONTROLS BECAME INEFFECTIVE (ELEVATOR) REQUIRING AN EMERGENCY LANDING/RETURN TO FIEL D. DURING THE DOWNWIND SEGMENT OF FLIGHT, THE ELEVATOR REGAINED SOME EFFECTIVENESS, BUT VERY LITTLE. RETURNED TO FIELD AFTER RUNNING APPROPRIATE CHECKLISTS AND TURNED THE AIRCRAFT OVER TO MAINTENANCE. MAINTENANCE INSPECTED ALL CONTROL CA BLES AND FLIGHT CONTROLS AND FOUND NO DEFECTS. THE AIRCRAFT WAS TEST FLOWN AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007102400210 20071024 00210 EA 2007 10 24 CHQ200700063 1 20071019 A 2750 FCU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A CHQA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 11 639BR 7313 GEE872507 TUL TO IAH - A STANDARD CHAUTAUQUA TAKEOFF WAS MADE OUT OF TUL. AT V2+20 FLAPS WERE SELECTED UP. IMMEDIATELY AFTER MOV ING THE FLAP LEVER TO ZERO DEGREES THE FLIGHT CREW RECEIVED A MASTER CAUTION FLAPS FAIL MESSAGE. FIRST OFFICER CONTINUE D TO FLY THE AIRCRAFT WHILE THE CAPTAIN RAN THE APPROPRIATE QRH CHECKLISTS. THE CREW STAYED AT 3500AGL AND INFORMED ATC THAT THEY WOULD BE RETURNING TO TUL. CREW RECEIVED VECTORS FOR THE LONGEST RUNWAY, THE PASSENGERS AND FLIGHT ATTENDANT WERE BRIEFED ON THE SITUATION. ATC WAS ALSO NOTIFIED TO HAVE EMERGENCY VEHICLES STANDING BY. THE AIRCRAFT MADE AN UNE VENTFUL LANDING AND WAS TURNED OVER TO MAINTENANCE. MAINTENANCE RESET FLAP SYSTEM WITH NO FIX, THEN RERACKED FECU AND TH 2 L 7 2 4F 4 F RT A21EA E15NE 2007102400214 20071024 00214 NM 2007 10 24 070170 1 20071005 A 3350 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 873GA 49658 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT 2007102400215 20071024 00215 WP 2007 10 24 070171 1 20071007 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 878GA 53487 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENC Y EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BA TTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007102400216 20071024 00216 WP 2007 10 24 070166 1 20070926 A 5322 SHEAR TIE DOUG DC9 DC982 3022082 WP BS 1150 L29-30R DAMAGED A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 894GA 49660 AFT CARGO COMPARTMENT SHEAR TIE HAS CORROSION AT STATION 1150 BETWEEN L29R AND L30R. FABRICATED FORMER FROM 7075-T6 .06 3 AND REPAIR SPLICE FROM 7075-T6 .063 PER SRM 53-03 FIGURE 3. 2 L 7 2 4F A6WE 2007102400218 20071024 00218 NM 2007 10 24 GTIA200700030 1 20071011 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 517NK 2711 FLOORBEAM CORROSION AT Y-1732 15" AFT OF FRAME 67. REPLACED SECTION OF FLOORBEAM. 2 L 7 2 4F RT A28NM 2007102400219 20071024 00219 NM 2007 10 24 GTIA200700031 1 20071011 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 517NK 2711 FLOORBEAM CORROSION, 6" AFT OF FRAME 67 AT Y765. REPAIRED DAMAGED AREA. 2 L 7 2 4F RT A28NM 2007102400220 20071024 00220 NM 2007 10 24 DL764071332 1 20071010 A 2121 211002542 FAN BOEING 767 767432ER 1385134 NM CABIN FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 826MH 29697 IN FLIGHT-NOTED ACRID ELECTRICAL ODOR IN COCKPIT AND FWD CABIN AREA. FOUND FWD EQ SUPPLY FAN CIRCUIT BREAKER CLOSED WHE N ON MEL CALLS FOR PULLING BREAKER-PULLED BREAKER AND CONT ON MEL. REPLACED FWD EQUIPT COOLING SUPPLY FAN. OPS CKS NML . MCO AN PLAC REMOVED. 2 L 7 2 4F RT A1NM 2007102400221 20071024 00221 NM 2007 10 24 DL76L071358 1 20071015 A 3244 TIRE BOEING 767 767332 1382001 NM MLG FAILED A DALA O OTHER O OTHER TO TAKEOFF 1 SO 27 195DN 28452 NR 2 MAIN TIRE RECAP DEPARTED ON T/O FROM ATL. REPLACED NR 1 AND NR 2 WHEEL ASSY PER M/M. PERFORMED BURST/FLAT SPOTTED TIRE INSP OK PERFORMED TIRE TREAD LOSS CON IN GOOD MCC CONTACTED P/N 2608811-5. 2 L 7 2 4F RT A1NM 2007102400222 20071024 00222 NM 2007 10 24 DL757071360 1 20071016 A 3350 BR9279108 LIGHT BOEING 757 757232 1384965 NM LT FWD OVERWING SMOKE A DALA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 619DL 22909 DURING PUSHBACK PAX REPORTED SMOKE FROM LEFT FORWARD OVERWING EXIT VERTICAL EMERGENCY EXIT SIGN. F/A USED HALON FIRE EX TINGUISHER. REPLACED LIGHT ASSY CABIN HALON BOTTLE AND PBE. EMERGENCY LIGHTS CK GOOD. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2007102400224 20071024 00224 NM 2007 10 24 DL76G071362 1 20071017 A 5610 UKN WINDOW BOEING 767 767332 1382001 NM L1 FAILED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 171DZ 29690 CAPTS FWD WINDSHILED OUTER PNL, SHATTERED AT FL320. RAN QRH CHK LIST. DETERMINED DEFORMATION AND DIVERTED. REPLACED F WD WINDSHILED PER MM 56-11-01. 2 L 7 2 4F RT A1NM 2007102400226 20071024 00226 NM 2007 10 24 DL757071369 1 20071020 A 5330 141N38502 SKIN BOEING 757 757232 1384965 NM BS 290 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 656DL 24396 FUSELAGE SKIN HAS A DENT/CREASE AT STA 290 BETWEEN WL 216 AND 240 ON THE RT SIDE. THE DAMAGE IS FORWARD OF THE R1 DOOR. CUTOUT THE DAMAGED SKIN AND INSTALLED A REPAIR DOUBLER AND TRIPLER. 2 L 7 2 4F RT A2NM 2007102400227 20071024 00227 NM 2007 10 24 DL738071371 1 20071020 A 3350 D71701100 BATTERY PACK BOEING 737 737832 13844CF NM AFT GALLEY DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 391DA 30560 ON LAYOVER, FOUND AFT GALLEY AND L2 DOOR EMERGENCY LIGHTS INOP. 2 L 7 2 4F RT A16WE 2007102400230 20071024 00230 NM 2007 10 24 DL76G071374 1 20071021 A 3610 21SN4182A SWITCH BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 ENGINE UNKNOWN A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 173DZ 29692 704739 ANNUNCIATED AS ADVANCED POWER FOR T/O, DISC TO AT 74 KTS. NO LIGHT ON RECALL. T/S PER FIM. PRV CHECKED NORMAL. REPLA CED OVERPRESSURE SWITCH PER AMM. 2 L 7 2 4F 4 F RT A1NM E13NE 2007102400231 20071024 00231 NM 2007 10 24 DL76G071375 1 20071021 A 3620 PRESSURE SWITCH BOEING 767 767332 1382001 NM NR 2 ENGINE UNKNOWN A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 173DZ 29692 RTO DUE TO PRV VALVE STATUS MSG. REPLACED OVER PRESS SWITCH. 2 L 7 2 4F RT A1NM 2007102400232 20071024 00232 NM 2007 10 24 DL76G071378 1 20071021 A 7330 21SN04333 SWITCH BOEING 767 7673P6 1385105 NM NR 2 ENGINE FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 156DL 25354 AIR TURN BACK, DUE TO RT ENG FUEL FILTER MESSAGE. FOUND FUEL DP SWITCH BAD, REF IPC 73-34-01-06 NR 55J. 2 L 7 2 4F RT A1NM 2007102500001 20071025 00001 NE 2007 10 25 G41A2007003 2 20071009 A 7200 GECJ6106 ENGINE LEAR 25 25B 5170511 CE GE CJ610 CJ6106 30006 NE LEFT FLAMED OUT E G41A O OTHER X J ENGINE FLAMEOUT WARNING INDICATION AA AIR AMBULANCE 1 SW 01 26AT 13466 6 130 240C204A LEARJET N26AT WAS ON THE WAY FROM ELP TO LAX AT FL 410, THE CREW WAS EXPERIENCING SEVERE WEATHER AND REQUESTED TO GO TO FL 450. DURING THE CLIMB THEY HIT TURBULENCE AND THE LT ENGINE FLAMED OUT. THEN REQUESTED TO GO DOWN TO FL 250, RELIT THE LT ENGINE, THEN CLIMBED BACK TO FL 410 AND CONTINUED THE FLIGHT WITH NO FURTHER INTERRUPTIONS. 2 L 7 2 4J 4 J A10CE 1E16 2007102200001 20071022 00001 NM 2007 10 22 USAA920070931 1 20071012 A 5311 654655734 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6505054 AND 6505050, CRACKED FRAME, BS 887, S9L AND S9R. REPAIRED FRAME, BS 887, S 9L AND S9R IAW USAIRWAYS EA 120272. 2 L 7 2 4F RT A16WE 2007102200003 20071022 00003 NM 2007 10 22 USAA920070933 1 20071012 A 5311 65465548 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6505053, CRACKED FRAME, BS 847, S9L. REPAIRED FRAME, BS 847, S9L IAW USAIRWAYS EA 120272. 2 L 7 2 4F RT A16WE 2007102200005 20071022 00005 NM 2007 10 22 USAA920070935 1 20071012 A 5311 65465302 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6504945, CRACKED FRAME, BS 480, S9R. REPAIRED FRAME, BS 480, S9R IAW USAIRWAYS EA 120272. 2 L 7 2 4F RT A16WE 2007102200006 20071022 00006 NM 2007 10 22 USAA920070936 1 20071012 A 5311 90526911 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6504946, CRACKED FRAME, BS 767, S9R. REPAIRED FRAME BS 767, S9R IAW USAIRWAYS EA 1 20272. 2 L 7 2 4F RT A16WE 2007102200007 20071022 00007 WP 2007 10 22 UPS07850896 1 20071002 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FS 1660-1666 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 CABIN LEFT STA 1660-1666 2 EA INTERCOSTALS ARE DAMAGED. FABRICATED AND INSTALLED REPAIR INTERCOSTALS AT STA 1660-1666 IAW SRM 51-1-20D AND DWG 9751059. 2 L 7 4 4F RT 4A25 2007102200009 20071022 00009 NM 2007 10 22 USAA920070940 1 20071013 A 5330 6545775 SKIN BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6504599, CRACKED FUSELAGE SKIN, BS 727D, S23R. REPAIRED FUSELAGE SKIN, BS 727D, S2 3R IAW USAIRWAYS EA 120316. 2 L 7 2 4F RT A16WE 2007102200010 20071022 00010 NM 2007 10 22 SWAA075073 1 20071014 A 5310 6547973 CREASE BEAM BOEING 737 7375H4 138449D NM BS 639 S17R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 639, STR 17R. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007102200014 20071022 00014 NM 2007 10 22 2007UALA04187 1 20071011 A 5320 SUPPORT BOEING 757 757222 1384956 NM R2 DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 CABIN R2 DOOR FWD CUTOUT AREA AT 680 STR 12R DOOR SUPPORT STRUCTURE CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED CRACK ED WEB. 2 L 7 2 4F RT A2NM 2007102200015 20071022 00015 2007 10 22 UPS07150902 4 20071011 A 2565 SWITCH AIRBUS A300 A300F4622R 3930360 EU ESCAPE SLIDE MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 165UP 0005 INSPECTION TYPE:N/A EMERGENCY ESCAPE SLIDE DIFFERENTIAL PRESSURE WARNING HORN SOUNDS IN FLIGHT W/SLIDE ARMED, RED WARNIN G LIGHT ILLUMINATED. DEFERRED DOOR SLIDE PER MEL 52-11-01-3 DMP ACCOMPLISHED. PER CONVERSATION WITH CREW DETERMINED BU ZZER AND WARNING LIGHT WERE FOR THE SLIDE ARMING NOT DIFFERENTIAL PRESSURE. REMOVED AND REPLACED SWITCH 9WN IAW MM 52-7 3-13-04 AND PERFORMED ADJ & TEST IAW 52-73-13-05. CHECKS OK. THIS CLEARS M 360383. PLACARD REMOVED. 2 L 7 2 4F RT A35EU 2007102200017 20071022 00017 NM 2007 10 22 UPS07450898 1 20071010 A 3110 INTAKE BOEING 747 747123F NM INSTRUMENT PANEL CLOGGED A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 677UP 20391 LOUD HUMMING SOUND HEARD 5 TIMES FROM FORWARD INSTRUMENT PANEL, FIRST TWO TIMES WITH STRONG ODOR OF HOT ELECTRONICS. CL EARED CLOGGED AIR INTAKES ON NR 1 AND NR 2 INS CDU'S. INSPECTED FORWARD INSTRUMENTAL PANEL AREA. PERFORMED EQUIPMENT C OOLING TEST. ALL CHECKS GOOD. 2 L 7 4 4F A20WE 2007102200020 20071022 00020 NM 2007 10 22 ZZDA2007284 1 20071011 A 2530 64769001005 COFFEEMAKER BOEING 717 717200 1383700 NM GALLEY ODOR A ZZDA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 37 895AT 55047 DURING DESCENT F/A ADVISED OF SMOKE IN THE CABIN. IN FLIGHT EMERGENCY WAS DECLARED. ALL CIRCUIT BREAKERS SET & GALLEY POWER SWITCH THEN BEING TURNED OFF. OPERATED ALL NORMAL OPERATIONS WITHIN THE GALLEY FOUND NR 3 COFFEEMAKER TO BE EMITT ING A FOUL ODOR. REMOVED AND REPLACED NR 3 COFFEEMAKER BREWED NUMEROUS TIMES, NO DEFECTS NOTED REF AMM 25-00. 2 L 7 2 4F TR A6WE 2007102200021 20071022 00021 EU 2007 10 22 2007UALA04208 1 20071013 A 3397 WIRE AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS OUT OF POSITION A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 426UA 510 DURING EMERGENCY LIGHT TEST, RT POWER SUPPLY FAILED TEST. 10-26-07 FOUND MISWIRING OF EITHER 42WL, 22WL4 OR 22WL6. R EWIRED SYSTEM OPS CHECK OK. 2 L 7 2 4F RT A28NM 2007102200027 20071022 00027 NM 2007 10 22 USAA920070946 1 20071014 A 5315 143N50632 FLOORBEAM BOEING 757 7572S7 1384962 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 903AW 23323 MCN - MAJOR REPAIR - C-12 CHECK - NR 5976770, CRACKED FLOORBEAM, BS 700, RBL 24.75, WL 208. REPAIRED FLOORBEAM, BS 700, RBL 24.75, WL 208 IAW B737-300 SRM 53-00-51-2R1, FIGURE 201. 2 L 7 2 4F RT A2NM 2007102200030 20071022 00030 NM 2007 10 22 2007UALA04220 1 20071015 A 3510 OXYGEN SYSTEM BOEING 747 747422 1384935 NM CREW UNKNOWN A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 128UA 30023 FLIGHT DIVERTED DUE TO CREW OXYGEN INDICATION. SERVICED CREW O2 BOTTLE TO 1750 PSI PER MM12-15-08. PERFORMED CYLINDER CHECK PER MM35-41-03 CREW O2 SYSTEM LEAK CHECK PER MM 35-11-00, NO LEAKING FOUND. RECHECKED PRESSURE ON BOTTLE AND EICAS 12 HOURS AFTER SERVICING. BOTH READS 1750 PSI. 2 L 7 4 4F RT A20WE 2007102200031 20071022 00031 NM 2007 10 22 2007UALA04221 1 20071014 A 5330 SKIN BOEING 757 757222 1384956 NM BS 420-440 S2-3R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 578UA 26694 TWO BURNS IN SKIN BETWEEN STA 420 AND 440, AND BETWEEN STR 2R AND 3R. MAJOR REPAIR ACCOMPLISHED. ACFT OPENED UP AND DI SCOVERED 70 HITS, MANY SEVERE. WORKING FASTENER REPLACED & ACCOMPLISHED BURNISHING REPAIRS. 2 L 7 2 4F RT A2NM 2007102200032 20071022 00032 WP 2007 10 22 MWEA070250 1 20071014 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP ROWS 17-21 INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 809ME 48071 CEILING EMERGENCY LIGHTS AT ROWS 17-21 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 2007102200041 20071022 00041 NM 2007 10 22 2007UALA04238 1 20071015 A 3397 CONNECTOR BOEING 747 747451 1384940 NM ROWS 3A INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHT ROWS 3A AFT, 3J FWD & 61CB ARE INOP. RESECURED CONNECTOR. 2 L 7 4 4F RT A20WE 2007102200046 20071022 00046 NM 2007 10 22 UPS07M50910 1 20070925 A 5320 INTERCOSTAL DOUG MD11 MD11F 3023600 NM BS 1761-1781 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C CTR CARGO INTERCOSTAL AT LT 42, LT 43 STA 1761 - 1781 FOUND CRACKED. CTR CARGO STA 1761-1781 LONGERON 42-43 LT CRACKED INTERCOSTAL REMOVED. INTERCOSTAL FABRICATED FROM MAT'L 7075-0 CONDITION AS PER DWG AC A7049. INTERCO STAL HEAT TREATED PER DPS 7.00-1 & HARDNESS VALUES HRB 86.9 AS PER DPS 1.05-3. INTERCOSTAL HOLES PICKED UP, REPROTECTED & PAINTED. INTERCOSTAL INSTALLED AT CTR CARGO STA 1761 - 1781 LT 42-43. 2 L 7 3 4F RT A22WE 2007102200050 20071022 00050 NM 2007 10 22 SWAA075074 1 20071014 A 5753 6546434 SKIN BOEING 737 7377H4 1384404 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 755SA 27871 DURING SCHEDULED 8Y CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD T/E. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007102200054 20071022 00054 EU 2007 10 22 TRAX200701495 1 20071012 A 3220 DRAG BRACE AEROSP ATR72 ATR72 EU NLG DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 NLG DRAG BRACE TO BE REPLACED. 2 H 7 2 4T RT 2007102200055 20071022 00055 NM 2007 10 22 2007UALA04188 1 20071011 A 3350 LIGHT BOEING 757 757222 1384956 NM L2 DOOR SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 524UA 24977 L2 DOOR SLIDE LIGHT IS INOPERATIVE. 11-01-07 REMOVED AND REPLACED SLIDE LIGHT ASSY. 2 L 7 2 4F RT A2NM 2007110800073 20071108 00073 NM 2007 11 8 ASAA0772165 1 20071018 A 5320 146A75021 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 AFT CARGO PIT FLOOR SUPPORT ZEE AT LBL 21 BETWEEN BS 727 & BS 847 CORRODED. ZEE CHANNEL REPLACED. 2 L 7 2 4F RT A16WE 2007102200056 20071022 00056 WP 2007 10 22 UPS07850899 1 20071011 A 2560 ESCAPE ROPE DOUG DC8 DC873F 302199F WP COCKPIT DISLODGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:N/A ESCAPE ROPE ABOVE CAPTAIN'S WINDOW FELL OUT. REPLACED CAPTAIN'S ESCAPE ROPE PER MM 25-60-02-2. 2 L 7 4 4F RT 4A25 2007102200059 20071022 00059 NM 2007 10 22 CALA0700575 1 20071015 A 3350 S283T0143 BATTERY PACK BOEING 757 757224 1384958 NM EMERGENCY LIGHTS INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18112 27302 EMERGENCY LIGHT INOP AT ROWS 15-25ABC. REPLACED EMERGENCY BATTERY PACK PER MM 33-51-01. 10-23-07 FOUND EMERGENCY LI GHT BATTERY PACK M10699 BAD. REMOVED AND REPLACED M10699 EMERGENCY BATTERY PACK AS PER M/M 33-51 -01.PERFORMED OPS/TEST ALL TEST SATISFACTORY. 2 L 7 2 4F RT A2NM 2007102200061 20071022 00061 NM 2007 10 22 CALA0700577 1 20071012 A 5414 311A1450 SKIN BOEING 737 7373T0 1384582 NM LT NACELLE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14325 23455 NR 1 ENG PYLON CRACKED AT ACCESS PANEL 5727. INSTALLED DOUBLER PER ECRA 5430-01230. 2 L 7 2 4F RT A16WE 2007102200065 20071022 00065 NM 2007 10 22 CALA0700581 1 20071012 A 5311 6545801512 FRAME BOEING 737 7373T0 1384582 NM BS 227 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14325 23455 STA 227 LBL 5 TO RBL 5 FRAME CORRODED. REPAIR ACCOMP PER ECRA 5311-01366. 2 L 7 2 4F RT A16WE 2007102200067 20071022 00067 NM 2007 10 22 CALA0700583 1 20071001 A 5320 146N5391165 PANEL BOEING 757 757324 1384930 NM BS 1440-1480 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 75851 32810 AFT CARGO PIT RIGHT SIDE PLATE FROM STA 1440-1480 HAS CORROSION. REPAIRED SIDE PLATE AT INDICATED AREA IAW ECRA 5321-01 501. 2 L 7 2 4F RT A2NM 2007102200068 20071022 00068 NM 2007 10 22 CALA0700584 1 20071015 A 5313 6545776 STRINGER BOEING 737 7373T0 1384582 NM BS 867 S26R CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14325 23455 AFT BAG BIN STA 867 STRINGER 26 RT HAS CORROSION. INSTALLED REPAIR PER SRM 53-00-03 FIG 201. 2 L 7 2 4F RT A16WE 2007102200073 20071022 00073 NM 2007 10 22 KCSA071477 1 20071017 A 5330 SKIN BOEING 747 7472B4B 138481B NM BS 1270-1283 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 R-3 DOOR FWD UPPER CUTOUT INTERNAL SKIN HAS SURFACE CORROSION AT WL 279 TO WL 279 AT STA 1270 TO STA 1283. 2 L 7 4 4F RT A20WE 2007102200076 20071022 00076 NM 2007 10 22 2007UALA04200 1 20071010 A 2611 SQUIB BOEING 747 747422 1384935 NM EXTINGUISHER INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 CREW REPORT, NR 4 ENGINE FIRE EXTINGUISHER SQUIB 1 WOULD NOT TEST. SQUIB 2 TESTS FINE. FOUND TEST LIGHT INOPERATIVE. REPLACED LAMP TEST GOOD. AC OK FOR SERVICE. 2 L 7 4 4F RT A20WE 2007102200077 20071022 00077 NM 2007 10 22 SWAA075089 1 20071015 A 3350 101073 LENS BOEING 737 737705 13844SC NM EMERGENCY LIGHTS CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 270WN 29089 L2 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007102200080 20071022 00080 NM 2007 10 22 SWAA075090 1 20071015 A 5311 6516352 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT LOWER DOOR STOP. REMOVED AND REPLACED FRAM E PER ACO. 2 L 7 2 4F RT A16WE 2007102200081 20071022 00081 NM 2007 10 22 SWAA075088 1 20071015 A 3350 D71702030 CHARGER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 749SW 29801 DURING SCHEDULED MV3 CHECK, FOUND LEFT AFT CABIN EMERGENCY EXIT BATTERY PACK CHARGER FAULTY. REMOVED AND REPLACED BATTE RY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007102200083 20071022 00083 NM 2007 10 22 ASAA0742099 1 20071012 A 5311 65465262 FRAME BOEING 737 7374Q8 138447Q NM BS 400 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 MAIN CABIN STA 400 BETWEEN STR 8R AND 9R FRAME CRACKED AT HAT BIN ATTACH BRACKET POINT. REMOVED DAMAGED AREA IAW B737 4 00 SRM 57 00 7 NDT VERIFIED NO CRACK. IAW B737 NOT MANUAL PART 6 CH 51-00-00 FIG 23. FABRICATED AND ATTACHED REPAIR PAR TS IAW B737 400 SRM. 2 L 7 2 4F RT A16WE 2007102200086 20071022 00086 NM 2007 10 22 ASAA0742100 1 20071012 A 5311 65465252 FRAME BOEING 737 7374Q8 138447Q NM BS 380 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 MAIN CABIN STA 380 RT AT STR 8 & 9 FRAME HAS CRACK AT OVERHEAD BIN BRACKET HOLE. REMOVED DAMAGE AREA NOT VERIFIED CRACK CONTAINED IAW 737 NOT MANUAL PART 6 CH 51-00-00 FIG 23. REPAIRED AREA IAW SRM 53-00-7 FIG 201 B737 400. 2 L 7 2 4F RT A16WE 2007102200087 20071022 00087 WP 2007 10 22 ASAA0782102 1 20071014 A 5320 993061221 CUSP WEB DOUG DC9 DC983 3022083 WP BS 1212-1231 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 RIGHT CUSP WEB CORRODED STA 1212 TO STR 1231. REMOVED, CUT OUT DAMAGED AREA OF CUSP WEB, FABRICATED DOUBLER, LOCATED DR ILLED AND INSTALLED DOUBLER REPAIR IAW MD80 SRM 53-05 PG 563 FIG 96. 2 L 7 2 4F RT A6WE 2007102200089 20071022 00089 NM 2007 10 22 ASAA0792095 1 20071009 A 5320 146A7502 INTERCOSTAL BOEING 737 737990 NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 305AS 30013 AFT CARGO PIT LEFT INTERCOSTAL TRACK CORRODED AT BS 727. REPAIRED INTERCOSTAL TRACK IAW SRM 53-00-53 FIG 202. 2 L 7 4 4F RT A16WE 2007102200094 20071022 00094 WP 2007 10 22 MWEA070245 1 20071012 A 5230 SR095200133 ANGLE DOUG DC9 DC981 3022081 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 812ME 48006 FORWARD CARGO DOOR HAS A CRACK ON THE OUTER PAN RADIUS AT UPPER FORWARD AREA 1.25 INCHES LONG. FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F A6WE 2007102200095 20071022 00095 WP 2007 10 22 UPS07850921 1 20070921 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 CORROSION L-1 ENTRY DOOR FLOOR AREA AFT OF MCD CONTROL PANEL. REMOVED DAMAGE, FABRICATED DOUBLER, IN STALLED DOUBLER IAW SRM 51-1-21, 53-02-00, 21-02-00, AND DWG 5615180-5. 2 L 7 4 4F RT 4A25 2007102200096 20071022 00096 NM 2007 10 22 HNAA0700237 1 20071017 A 3240 BRAKE ASSY DHAV DHC8 DHC8102 2809003 NM LT MLG SMOKE A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 845EX 344 THE LEFT HAND INBOARD BRAKE ASSEMBLY WAS SMOKING AFTER GATE ARRIVAL. MAINTENANCE INSPECTED THE NR 2 BRAKE & TAXIED THE AIRCRAFT. NO DISCREPANCIES NOTED. 2 H 7 2 4T RT A13NM 2007102200097 20071022 00097 NM 2007 10 22 SWAA075070 1 20071014 A 5314 6562125 KEELBEAM BOEING 737 7373H4 1384600 NM BS 500D CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED BRDG CHECK, FOUND KEELBEAM CORRODED AT BS 500D, RBL 6.5. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2007102200098 20071022 00098 NM 2007 10 22 SB07091 1 20071015 A 3350 20131ASMI BATTERY PACK BOEING 737 737301 1384611 NM EMERGENCY LIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 589US 23934 CLT - MAINTENANCE REPORTED A FORWARD CABIN EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD OU TBOARD BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007102200099 20071022 00099 NM 2007 10 22 2007UALA04193 1 20071012 A 3350 LIGHT BOEING 747 747422 1384935 NM CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY EXIT EEL INOPERATIVE AT ROWS 35 LEFT & 51 RIGHT. 11-01-07 REPLACED LIGHT ASSY. OPS CHECKED NORMAL. 2 L 7 4 4F RT A20WE 2007102200101 20071022 00101 EU 2007 10 22 2007UALA04211 1 20071014 A 3350 CONTROL PANEL AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 448UA 842 DOOR 2L EMERGENCY EXIT LIGHT COVER MISSING. 10-26-07 REPLACED CABIN LIGHT CONTROL PANEL. 2 L 7 2 4F RT A28NM 2007102200102 20071022 00102 NM 2007 10 22 2007UALA04222 1 20071014 A 5330 SKIN BOEING 757 757222 1384956 NM BS 440-600 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 578UA 26694 SIX BURNS IN SKIN BETWEEN STA 440 AND 600, AND BETWEEN STR 2R AND 3R. MAJOR REPAIR ACCOMPLISHED. ACFT OPENED UP AND DI SCOVERED 70 HITS, MANY SEVERE. WORKING FASTENER REPLACED & ACCOMPLISHED BURNISHING REPAIRS. REPAIRED 6EA BURNED AREAS A T STA 454,480,490,517,536,592 BETWEEN STR 2R AND 3R. 2 L 7 2 4F RT A2NM 2007102200103 20071022 00103 NM 2007 10 22 2007UALA04230 1 20071015 A 3350 LIGHT BOEING 747 747422 1384935 NM CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 D-ZONE LEFT COLUMN EEL NOT ON. 11-01-07 REPLACED BATTERY PACK. 2 L 7 4 4F RT A20WE 2007102200105 20071022 00105 NM 2007 10 22 UPS07M50906 1 20070808 A 5730 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C RIGHT WING LOWER SURFACE FIXED L/E SKIN AT I/B FWD CORNER OF REFUELING PANEL FOUND CRACK AS MARKED. F ASTENERS AT RIGHT WING REFUELING PANEL CRACKED AREA REMOVED. DAMAGED AREA TRIMMED OFF. HFEC INSP C/OUT ON TRIMMED OFF AREA FOUND NO CRACK. REPAIR DOUBLER & FILLER FABRICATED, HOLES PICKED UP, PROTECTED & PAINTED. REPAIR DOUBLER & FILLER INSTALLED AS PER SRM 51-31-01 VOL II & SRM 57-10-00 FIG 21 VOL I REV 38. 2 L 7 3 4F RT A22WE 2007102200111 20071022 00111 WP 2007 10 22 MWEA070253 1 20071017 A 5340 ATTACH ANGLE DOUG DC9 DC981 3022081 WP BS 1439.5 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 812ME 48006 LEFT DORSAL FIN ATTACH ANGLE HAS FASTENER HEAD PULLED THROUGH ANGLE, FRAME STATION 1439.9. REMOVED FASTENER, FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F A6WE 2007102200112 20071022 00112 WP 2007 10 22 MWEA070254 1 20071017 A 2612 531905 HANDLE DOUG DC9 DC981 3022081 WP FIRE HANDLE FAILED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 812ME 48006 LEFT FIRE HANDLE DOES NOT ILLUMINATE DURING TEST. REMOVED AND REPLACED FIRE HANDLE ASSEMBLY. 2 L 7 2 4F A6WE 2007102200118 20071022 00118 NM 2007 10 22 MWEA070256 1 20071018 A 7830 7150923REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 926ME 55192 LEFT ENGINE THRUST REVERSER LOWER BUCKET ZEE FRAME IS CRACKED AT THRUST REVERSER STATION 35 OUTBOARD. REMOVED DAMAGE, F ABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F TR A6WE 2007102200121 20071022 00121 GL 2007 10 22 C2XA07RI088 2 20070927 A 7200 ENGINE EMB 145 EMB145EP 3260221 SO ALLSN AE300 AE3007A GL NR 1 FLAMED OUT A C2XA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 27 13992 1450284 CAE311496 CREW REPORTED ENGINE NR 1 FLAME-OUT. ACFT LANDED WITHOUT INCIDENT. EWR MX REMOVED AND REPLACED ENGINE NR 1 AND PERFORM ED OPERATIONAL TEST SUCCESSFULLY. ACFT APPROVED TO RETURN TO SERVICE. MANUFACTURE PERFORMED ENGINE BREAK DOWN AND REPO RTED THAT THE PRIMARY FAILED ITEM (PFI) WAS THE RADIAL DRIVE BEVEL PINION GEAR SHAFT, P/N 23061402 S/N GQ36716, ALSO KNO WN AS THE UPPER BEVEL GEAR. THE ENGINE SHUTDOWN DUE TO THE FRACTURE OF THE UPPER BEVEL GEAR. THE ROOT CAUSE OF THIS FRAC TURE IS A VIBRATORY MODE (3DOC) IN THE GEAR WHICH CAUSES A CRACK AND SUBSEQUENT BREAKAGE. THE CORRECTIVE ACTION IS TO DA MPEN/ELIMINATE THE RESPONSE OF THE GEAR TO A KNOWN RESONANCE MODE NEAR THE OPERATING RANGE PER SB 72-339. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007102200122 20071022 00122 2007 10 22 SWAA075081 4 20071015 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007110800075 20071108 00075 NM 2007 11 8 ASAA0772161 1 20071029 A 5330 147431101 SKIN BOEING 737 737790 13844CN NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 SKIN DENTED AFT OF L2 DOOR 12FT AFT OF EMERGENCY LIGHT. REPAIRED SKIN IAW B737 700 SRM 53-00-01 FIG 201. 2 L 7 2 4F RT A16WE 2007102200124 20071022 00124 NM 2007 10 22 1014200701 1 20071014 A 2613 356644400 OVERHEAT LOOP BOEING 727 727233 138408A NM PWA JT8 JT8D17A 52049 NE NR 3 STRUT OUT OF POSITION A PCSA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 17 495AJ 20937 709461 AT CRUISE FL 310 AMERIJET FLIGHT 875 NUMBER 3 STRUT OVERHEAT LIGHT ILLUMINATED. LIGHT WENT OUT AFTER 2 MINUTES AND REMA INED OUT WITH ENGINE AT IDLE ONLY. THE FLIGHT DIVERTED TO KIN. MAINTENANCE DISCOVERED THE STRUT OVERHEAT DETECTOR TOUC HING THE PNEUMATIC DUCT. THE ELEMENT WAS REPOSITIONED, A POWER RUN WAS PERFORMED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2007102200125 20071022 00125 NM 2007 10 22 2007UALA04231 1 20071013 A 2780 FLAP SYSTEM BOEING 777 777222 1385219 NM SLATS MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 221UA 30552 FLAP SLAT STATUS MESSAGE DISPLAYED. REPLACED FLAP/SLAT ELECTRONICS UNIT 1 PER MM 27- 51-01. MSG CLEARED, SYSTEM OK FO R SERVICE. 2 L 7 2 4F RT T0001SE 2007102200134 20071022 00134 NM 2007 10 22 CALA0700591 1 20071017 A 5320 6517684634 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 294 S16L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14334 23572 INTERCOSTAL CRACKED AT STA 294.5. S-16L. REMOVED AND REPLACED PER ECRA 5311-01368. 2 L 7 2 4F RT A16WE 2007102200136 20071022 00136 NM 2007 10 22 SWAA075064 1 20071014 A 3350 101114 LENS BOEING 737 7375H4 138449D NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 FWD CABIN EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007102200137 20071022 00137 NM 2007 10 22 2007UALA04240 1 20071015 A 3350 LIGHT BOEING 747 747451 1384940 NM ROW 35ABC UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHT ROW 35ABC INOP. RESECURED LIGHT. 2 L 7 4 4F RT A20WE 2007102200138 20071022 00138 NM 2007 10 22 SWAA075066 1 20071014 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 249WN 34951 EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007102200139 20071022 00139 NM 2007 10 22 SWAA075067 1 20071014 A 3350 417A5704 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 286WN 32471 EEPLS END CAP BROKEN AT ROW 1 ABC. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 2007102200142 20071022 00142 EU 2007 10 22 SA07066 1 20071012 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU ZONE 200 FAULTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 708UW 24775 6112 0972 RIC - THE RIGHT HAND, MID-CABIN EMERGENCY POWER SUPPLY UNIT FAILED OPERATIONAL TEST. MAINTENANCE REPLACED THE RIGHT HAN D, MID-CABIN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007102200151 20071022 00151 NM 2007 10 22 ASAA0742098 1 20071011 A 5340 654580733 ATTACH ANGLE BOEING 737 7374Q8 138447Q NM BS 278-293 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 MAIN FRAME AT FWD SERVICE DOOR CUTOUT BS 294 BETWEEN STR 10R AND 11R ANGLE CRACKED AT AFT END LWR SIDE OF INTERCOSTAL. R EMOVED AND REPLACED ANGLE P/N 65 45807. 2 L 7 2 4F RT A16WE 2007102200153 20071022 00153 NM 2007 10 22 USAA920070937 1 20071012 A 5311 90526911 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6504947, CRACKED FRAME, BS 807, S9R. REPAIRED FRAME, BS 807, S9R IAW USAIRWAYS EA 120272. 2 L 7 2 4F RT A16WE 2007102200154 20071022 00154 SO 2007 10 22 C2XA07RI089 1 20071017 A 3397 WIRE EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT DAMAGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 34111 1450659 RIC - MX - DURING ROUTINE MAINTENANCE, MX FOUND NR 2 CEILING PANEL EMERGENCY LIGHT INOPERATIVE. MX FOUND SPLICE (SP9032 ) DEFECTIVE. MX REPAIRED SPLICE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007102200156 20071022 00156 NM 2007 10 22 SWAA075075 1 20071014 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM BS 277 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007102200159 20071022 00159 NM 2007 10 22 MWEA070246 1 20071015 A 7830 7150922REVC ANGLE BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 906ME 55170 RIGHT UPPER THRUST REVERSER DOOR Z-FRAME AT STATION 26.666 IS CRACKED AT THE OUTBOARD END. CUT OUT DAMAGE AND INSTALLED ANGLE. 2 L 7 2 4F TR A6WE 2007102200162 20071022 00162 NM 2007 10 22 MWEA070248 1 20071015 A 7830 7150923REVC ANGLE BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 906ME 55170 RIGHT UPPER THRUST REVERSER Z-FRAME AT STATION 35.669 IS CRACKED AT THE INBOARD END. CUT OUT DAMAGE AND INSTALLED ANGLE . 2 L 7 2 4F TR A6WE 2007102200163 20071022 00163 NM 2007 10 22 MWEA070249 1 20071015 A 7830 7150922REVC ANGLE BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 906ME 55170 RIGHT LOWER THRUST REVERSER DOOR Z-FRAME AT STATION 26.666 IS CRACKED AT THE OUTBOARD END. CUT OUT FRAME AND INSTALLED ANGLE. 2 L 7 2 4F TR A6WE 2007102200164 20071022 00164 NM 2007 10 22 2007UALA04181 1 20071011 A 5347 SEAT TRACK AIRBUS A319 A319131 3930317 NM FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 845UA 1585 LEFT I/B & O/B AND RIGHT I/B & O/B SEAT TRACKS BETWEEN FR 42 & 47-51 REQUIRE REPLACEMENT DUE TO WEAR OF TRACK LUGS AT FW D SEAT LEG LOCATIONS. MAJOR REPAIR ACCOMPLISHED: REPLACED 4EA SEAT TRACKS. 2 L 7 2 4F RT A28NM 2007102200168 20071022 00168 2007 10 22 2007UALA04203 4 20071011 A 2565 B14056904 O-RING BOEING 757 757222 1384956 NM SLIDE UNSERVICEABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 0707 24763 LOW BOTTLE PRESSURE. REPLACED O-RING 2 L 7 2 4F RT A2NM 2007102200175 20071022 00175 NM 2007 10 22 2007UALA04244 1 20071014 A 3397 CONNECTOR BOEING 747 747422 1384935 NM EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY EXIT EEL LIGHT INOP, UPPER DECK LOWER WALL ACROSS LAVS. 11-01-07 SECURED LOOSE CONNECTOR. 2 L 7 4 4F RT A20WE 2007102200178 20071022 00178 EU 2007 10 22 U5QA06007 1 20071010 A 5350 J3081X SEAL HAWKER BAE125 BAE125700B 7450007 EU WING TO BODY LOOSE E U5QA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 05 903SC NA0218 CREW REPORTED STRANGE NOISE FROM RIGHT SIDE OF FUSELAGE DURING CLIMB. SOUNDED LIKE SOMETHING VIBRATING AGAINST THE OUTS IDE OF FUSELAGE JUST ABOVE THE WING. AFTER LANDING THE CREW REPORTED THAT THE WING TO FUSELAGE RUBBER SEAL HAD COME LOO SE AT THE TRAILING EDGE. 2 L 7 2 4F RT A3EU 2007102200182 20071022 00182 NM 2007 10 22 2007UALA04235 1 20071013 A 3350 LAMP BOEING 747 747422 1384935 NM EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY CEILING LIGHT ABOVE ROW 6 LEFT INOP. 11-01-07 RELAMPED. 2 L 7 4 4F RT A20WE 2007102200183 20071022 00183 NM 2007 10 22 USAA920070941 1 20071012 A 3350 321431 BATTERY AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 824AW 1490 PHX - EEL - FLT 210. MX REPORTED LT EPSU AT OVERWING HAS DEAD BATTERY. MX REPLACED THE LT EPSU BATTERY. OPERATIONAL C HECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007102200184 20071022 00184 NM 2007 10 22 2007UALA04226 1 20071012 A 3350 LIGHT BOEING 767 767322 1385200 NM CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 THE EEL EMERGENCY FLOOR LIGHTS BY THE EXIT DOORS FLICKER ON AND OFF. ON TAKEOFF THE EMERGENCY LT SYS CAME ON THE LEFT S IDE OF CABIN IN FIRST CLASS. ALSO CAME ON IN BUSINESS CLASS. EVENTUALLY WENT OFF. 11-01-07 REPLACED BATTERY PACK , OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2007102200185 20071022 00185 NM 2007 10 22 2007UALA04205 1 20071012 A 3350 LAMP AIRBUS A319 A319131 3930317 NM EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 846UA 1600 AISLE SEAT 7C EMERGENCY LIGHT INOPERATIVE. 10-26-07 RELAMPED FIXTURE. 2 L 7 2 4F RT A28NM 2007102200186 20071022 00186 EU 2007 10 22 2007UALA04206 1 20071015 A 3350 BATTERY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 406UA 454 RIGHT SIDE MID CABIN EMERGENCY LIGHT BATTERY DISPLAYED FAULT. 10-26-07 FOUND FAULTY EMERGENCY LIGHT BATTERY. REPLA CED EMERGENCY LIGHT BATTERY 2 L 7 2 4F RT A28NM 2007102200187 20071022 00187 NM 2007 10 22 2007UALA04234 1 20071013 A 3397 CABLE BOEING 747 747422 1384935 NM EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY LIGHT ROW 35 HJK INOPERATIVE. 11-01-07 FOUND CABLE DISCONNECTED. 2 L 7 4 4F RT A20WE 2007102200188 20071022 00188 EA 2007 10 22 TRAX200701499 1 20071014 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 855AS 7395 EMERGENCY LIGHT TRACK ROW 2 TO 5 AND FLOOR PROXIMITY EXIT SIGN INOP. 2 L 7 2 4F RT A21EA 2007102200190 20071022 00190 WP 2007 10 22 MWEA070244 1 20071012 A 5311 991185959 BLOCK DOUG DC9 DC981 3022081 WP BS 1446 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 812ME 48006 CORROSION ON FRAME TO STRINGER TIE RADIUS BLOCKS AT CANTED FRAME STATION 1446 AT STRINGER 12 LEFT & 14 LEFT. REMOVED DA MAGE, FABRICATED AND INSTALLED RADIUS BLOCK. 2 L 7 2 4F A6WE 2007102200191 20071022 00191 NM 2007 10 22 2007UALA04227 1 20071012 A 3350 LAMP BOEING 767 767322 1385200 NM SLIDE LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 664UA 29236 AFT LEFT FUSELAGE SLIDE LIGHT INOPERATIVE. RELAMPED SLIDE LIGHT. OP CHECKED GOOD. 2 L 7 2 4F RT A1NM 2007102200192 20071022 00192 NM 2007 10 22 2007UALA04228 1 20071012 A 3350 LIGHT BOEING 767 767322 1385200 NM SEAT 27ABC MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 664UA 29236 SEAT 27ABC EEL STRIP MISSING. 11-01-07 REPLACED LIGHT. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2007102200193 20071022 00193 NM 2007 10 22 2007UALA04196 1 20071012 A 3350 BULB BOEING 747 747422 1384935 NM EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY EXIT LIGHT INOP RIGHT EXTERIOR OVERWING 3RD FROM FWD LIGHT ASSY (ONE BULB INOP) AND LEFT EXTERIOR OVERWING 2ND FROM FWD LIGHT ASSY (BOTH BULBS INOP). 11-01-07 RELAMPED. 2 L 7 4 4F RT A20WE 2007102200194 20071022 00194 WP 2007 10 22 ASAA0782106 1 20071016 A 5330 591140659 SKIN DOUG DC9 DC983 3022083 WP L1 DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 LEFT EXT FUSELAGE SKIN AFT OF L1 DOOR DENT OUT OF LIMITS STA 213 ABOVE LONG 166 DIA = .800 DEPTH = .034 RATIO OF 23.52 R ECON TOURED DENT YAW MD80 SUM 53 04 FIG 38. HEFT INSPECTED, NO CRACKS NOTED YAW MD80 SUM 53 04 FIG 38 AND NUDISM PT 6.0 6 10 00 001. FABRICATED, LOCATED, DRILLED AND INSTALLED DOUBLERS REPAIR YAW MD80 SUM 53 04 VIEW E. 2 L 7 2 4F RT A6WE 2007102200195 20071022 00195 NM 2007 10 22 ZZDA2007281 1 20071010 A 5311 FRAME BOEING 717 717200 1383700 NM BS 1178 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 956AT 55018 AFT ACCESSORY COMP CANTE FRAME CRACKED FS 1178 BELOW LONG 17 RT. INSTALLED FORMED ANGLE REPAIR PER SRM 51-70-11. 2 L 7 2 4F TR A6WE 2007102200196 20071022 00196 NM 2007 10 22 2007UALA04186 1 20071011 A 5330 SKIN BOEING 757 757222 1384956 NM FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 L2 DOOR UPPER HINGE CUTOUT IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. DOOR 2L UPPER HINGE CUTOUT TRIMMED ALL THE WAY UP TO BEND LINE OF FRAME. DRILLED, TRIMMED, FITTED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F RT A2NM 2007102200197 20071022 00197 NM 2007 10 22 2007UALA04219 1 20071014 A 3350 SIGN BOEING 757 757222 1384956 NM EMERGENCY LIGHTS UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 556UA 26650 AFT EMERGENCY EXIT SIGN FELL OFF. SECURED SIGN. 2 L 7 2 4F RT A2NM 2007102200200 20071022 00200 SO 2007 10 22 C2XA07SH083 1 20071013 A 5315 14521700007 FLOORBEAM EMB 145 EMB145EP 3260221 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14943 145040 SHV - DURING C-CHECK LEFT OMEGA BEAM HAS CORROSION ON FR 20. MX REPAIRED LEFT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 53-00 -13. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 2007102200202 20071022 00202 WP 2007 10 22 UPS07850918 1 20070922 A 5320 SUPPORT ANGLE DOUG DC8 DC873F 302199F WP FS 140 L21L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 SUPPORT ANGLE CORRODED AT AFT SIDE OF NR 1 MCD LATCH SPOOL FITTING. REMOVED, FABRICATED, AND INSTALL ED REPAIR SUPPORT ANGLE AT AFT SIDE OF MCD NR 1 LATCH SPOOL FITTING IAW DWG 4773295, AND SRM 51-01-24-0. 2 L 7 4 4F RT 4A25 2007102200203 20071022 00203 WP 2007 10 22 UPS07850920 1 20070922 A 5320 SUPPORT ANGLE DOUG DC8 DC873F 302199F WP FS 280 L21L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 SUPPORT ANGLES CORRODED ON BOTH SIDES OF NR 7 MCD LATCH SPOOL FITTING. REMOVED, FABRICATED, AND INST ALLED REPAIR SUPPORT ANGLES ON NR 7 MCD LATCH SPOOL FITTING IAW DWG 4773295, AND SRM 51-3-2. 2 L 7 4 4F RT 4A25 2007102200204 20071022 00204 NM 2007 10 22 KCSA071473 1 20071015 A 5315 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 780 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FLOORBEAM AT STA 780 IS DAMAGED ON AFT SIDE AT LBL 50 TO LBL 53 ON THE UPPER SIDE OF CHORD. 2 L 7 4 4F RT A20WE 2007102200205 20071022 00205 NM 2007 10 22 KCSA071474 1 20071015 A 5320 FLOOR SUPPORT BOEING 747 7472B4B 138481B NM BS 1241-1350 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA 1241 TO STA 1350 LBL 98 FLOOR SUPPORT T-ANGLE CORRODED. 2 L 7 4 4F RT A20WE 2007102200209 20071022 00209 EU 2007 10 22 USAA920070930 1 20071008 A 3610 6774E010000 PRESSURE VALVE AIRBUS 320 A320232 3930326 EU NR 1 ENGINE FAILED A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 649AW 26912 6532 803 LAS - YVR - EL - FLT 437 - LOG 7628896. CREW REPORTED DURING CLIMB BOTH ENGINES WERE SURGING. CREW DECLARED AN EMERGEN CY AND RETURNED TO LAS. MX REPLACED NR 1 ENGINE PRESSURE REGULATOR VALVE IAW AMM 36-11. MX ALSO REPLACED THE ZONE CONT ROL VALVE. OPERATIONAL CHECK WAS GOOD. A/C PASSED CHECK FLIGHT. A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2007102200210 20071022 00210 NM 2007 10 22 KCSA071467 1 20071012 A 5313 STRINGER BOEING 747 7472B4B 138481B NM BS 442 S28AL CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STR 28A LEFT SIDE IS CRACKED AT STA 442. 2 L 7 4 4F RT A20WE 2007110800090 20071108 00090 NM 2007 11 8 QXEA200701631 1 20071030 A 6123 3014403 TSCU DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS FAILED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 349PH 161 486 PDX - ON FLIGHT 2048, NR 2 PROPELLER FAILED AUTOFEATHER TEST. FEATHER LIGHT DID NOT ILLUMINATE. MAINTENANCE REMOVED AN D REPLACED AUTOFEATHER CONTROL RELAYS 6121-K6, 6121-K8. COMPLIED WITH AUTOFEATHER TEST BUT FEATHER STILL FAILED TO ILLU MINATE. REPLACED NR 2 TSCU IAW PWC EMM 72-01-10 PG 420 PARA 7A-B. C/W TC 9720019. OPERATIONS CHECKS GOOD. AIRCRAFT R ETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102200211 20071022 00211 NM 2007 10 22 UPS07M50928 1 20070817 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C RT WING UNDERSIDE IN NR 3 FUEL TANK ACCESS CUTOUT 638AB FOUND UPPER STRINGER NR 9 XORS 819.0 SUSPECT C RACK. HFEC INSP C/OUT FOUND CRACK APPROX 6.5 INCHES. STRINGER NR 9 XORS 819 FASTENER & SPLICE REMOVED. REPAIR DOUBLER S FAB & HEAT TREATED. SLOT OPENED ON STR 9 XORS 819 & REPROTECTED. HFEC INSP C/OUT ON SLOTTED OUT AREA, FOUND NO CRACK . FUEL LINES IN NR 3 FUEL TANK ACCESS CUTOUT 638AB, NR 3 FUEL TANK FILL S/O VLV CONTROLLER & SHUTOFF VALVE BODY REMOVED . 2 L 7 3 4F RT A22WE 2007102200212 20071022 00212 NM 2007 10 22 SWAA075071 1 20071014 A 3397 W4142001220 WIRE BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 439WN 29834 EEPLS INOP BETWEEN ROW 3 ABC AND ROW 6 ABC. FOUND LOOSE WIRE. SECURED WIRE PER MM. 2 L 7 2 4F RT A16WE 2007102200215 20071022 00215 NM 2007 10 22 2007UALA04197 1 20071011 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 D-ZONE LEFT EMERGENCY PATH LIGHT OUT. 11-01-07 REPLACED BATTERY PACK. OPS CHECKED NORMAL. 2 L 7 4 4F RT A20WE 2007102200217 20071022 00217 NM 2007 10 22 SWAA075077 1 20071014 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 727D-727E CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727D AND BS 727E, STR 19R. REPAIRED SKIN PER SWA E A. 2 L 7 2 4F RT A16WE 2007102200226 20071022 00226 SO 2007 10 22 RAIA00710013 1 20071015 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 813HK 145044 PRE FLT NR 5511 - STL - FLOOR EXIT LIGHTING INOP ROW 2 THRU 14. MAINTENANCE RESECURED LOOSE CONNECTOR, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007102200230 20071022 00230 SO 2007 10 22 RAIA00710010 1 20071013 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DIRTY A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 833HK 145240 POST FLT NR 7901 - ORD - EMERGENCY LIGHT AT LEFT OVERWING INOP. MAINTENANCE CLEANED CONNECTOR, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007102200231 20071022 00231 NM 2007 10 22 USAA920070938 1 20071012 A 5311 65465588 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 MCN - MAJOR REPAIR - C-18 CHECK - NR 6505051, CRACKED FRAME, BS 907, S9R. REPAIRED FRAME, BS 907, S9R IAW USAIRWAYS EA 120272. 2 L 7 2 4F RT A16WE 2007102200234 20071022 00234 2007 10 22 2007UALA04184 2 20071011 A 7261 CARBON SEAL BOEING 737 737322 1384676 NM NR 1 ENGINE LEAKING A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 336UA 24240 NR 1 THRUST REVERSER WOULD NOT DEPLOY ON ROLLOUT. NR 2 ENG OIL WENT FROM 95 TO 6 PERCENT: REPLACED NR 2 ENGINE STARTER DRIVE CARBON SEAL PER MM 72-63-03 PG 201. ACCOMPLISHED HIGH POWER RUN REF JRH. NO ANNOMILIES NOTED NO FURTHER LEAKS NOT ED, ALL QUANTITIES, AND PRESSURES NORMAL. 2 L 7 2 4F RT A16WE 2007102200236 20071022 00236 NM 2007 10 22 HNAA0700238 1 20071015 A 3350 6013211X BATTERY PACK DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS INOPERATIVE A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 845EX 35890 5707 344 THE RIGHT HAND FRONT EMERGENCY EXIT LIGHTING INOP. REMOVED AND REPLACED EMERGENCY BATTERY NR 2. 2 H 7 2 4T RT A13NM 2007102200237 20071022 00237 NM 2007 10 22 KCSA071476 1 20071017 A 5412 BULKHEAD BOEING 747 747209F 1384800 NM NR 1 NACELLE CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 NR 1 PYLON NAC STA 129 BULKHEAD CHORD ANGLE CHAFED. 2 L 7 4 4F RT A20WE 2007102200239 20071022 00239 NM 2007 10 22 CALA0700588 1 20071016 A 5230 2024T3036 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14334 23572 C1 DOOR CRACKED AT EXT HANDLE CUTOUT. INSTALLED AND REPAIR DOUBLER IAW SRM 52-00-01 REPAIR 3. 2 L 7 2 4F RT A16WE 2007102200240 20071022 00240 NM 2007 10 22 CALA0700589 1 20071016 A 5230 6549621528 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 FWD CARGO DOOR INNER SKIN LIGHTNING HOLE CRACKED, AFT SIDE CENTER ROW. REPAIRED SKIN IAW ECRA 5232-01094. 2 L 7 2 4F RT A16WE 2007102200241 20071022 00241 NM 2007 10 22 SWAA075085 1 20071015 A 3350 65C27093 LIGHT BOEING 737 7373Y0 1384671 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007102200242 20071022 00242 NM 2007 10 22 SWAA075080 1 20071015 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007102200244 20071022 00244 WP 2007 10 22 ABXA070342 1 20071012 A 2697 WIRE DOUG DC9 DC941 302207N WP FIRE DETECTION DISCONNECTED A ABXA F ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 GL 23 972AX 47631 DURING DESCENT INTO ILN, APU FIRE INDICATION. APU WAS NOT OPERATING AT THE TIME. COMPLETED APU FIRE EMERGENCY CHECKLIS T INCLUDING DISCHARGE OF FIRE BOTTLES. LIGHT WENT OUT AFTER APPROX 3 MINUTES. LIGHT RE-ILLUMINATED APPROX 5 MINUTES LA TER FOR APPROX 30 SECONDS. FOUND WIRE PULLED OUT OF PLUG P1-278. REPLACED PLUG P1-278, TESTED FIRE LOOP SYSTEM PER DC9 MM 26-10-02-2 WITH APU RUNNING AND WITH APU SHUT OFF. NO DEFECTS NOTED. 2 L 7 2 4F A6WE 2007102200245 20071022 00245 WP 2007 10 22 ABXA070343 1 20071012 A 3350 60030451 POWER SUPPLY DOUG DC9 DC941 302207N WP EMERGENCY LIGHTS DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 24 47596 EMERGENCY LIGHTING IN COCKPIT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW DC9 MM 33-53-00-5. 2 L 7 2 4F A6WE 2007102200246 20071022 00246 WP 2007 10 22 ABXR070344 1 20070924 A 5311 99115057 FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 231US 48114 CENTER FRAME LEFT END CRACKED MORE THAN 1.12 INCH, BUT LESS THAN 2.50 INCH, STA 83.55 AND X = 10.00. REPAIRED FRAME IAW DC9 SRM 53-03, FIGURE 34. 2 L 7 2 4F A6WE 2007102200248 20071022 00248 WP 2007 10 22 ABXR070346 1 20070927 A 5320 99578605 BRACKET DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 231US 48114 LEFT VERTICAL BRACKET CRACKED, STA 69.55 AND X = 10.00. REPLACED BRACKET IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2007102200249 20071022 00249 WP 2007 10 22 ABXR070347 1 20070927 A 5320 99578606 BRACKET DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 231US 48114 RIGHT VERTICAL BRACKET CRACKED, STA 69.55 AND X = 10.00. REPLACED BRACKET IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2007102200250 20071022 00250 NM 2007 10 22 EIA2007175 1 20070919 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 1740-1760 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 AFT CARGO PIT BS 1740-1760 STRINGER 36L FOUND CRACKED. AFT CARGO PIT BS 1740-1760, REPAIRED STR 36L PER 53-10-03. 2 L 7 4 4F A20WE 2007102300006 20071023 00006 CE 2007 10 23 DXTA200702546 1 20071015 A 3241 ANTI-SKID SYS CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG STICKING E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 336QS 5600336 BRAKE RELEASE, GRAB WITH THE ANTISKID ON. BLED BRAKES IAW CE560 MM 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007102300009 20071023 00009 CE 2007 10 23 DXTA200702548 1 20071016 A 3150 65430087 UPLOCK SWITCH CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 650QS 5605150 AFTER GEAR RETRACTION,GEAR UNLOCK LIGHT AND HYD PRESS ANNUNCIATOR REMAINED ILLUMINATED. REMOVED AND REPLACED NJG UPLOCK SWITCH. IAW CE 560XL M/M CHPT. 32-30-05. GEAR FUNCTIONAL. CHECK SATISFACTORY. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007102300013 20071023 00013 NM 2007 10 23 AMTA200700488 1 20071012 A 5753 WEDGE BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE TE FLAPS PUNCTURED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 310TZ 28243 INSPECTION FOUND NUMEROUS DENTS, CRACKS AND PUNCTURES ON THE LT IB AFT FLAP TRAILING EDGE WEDGE LOWER SKIN PN 113A2700-1 7. ACCOMPLISHED REPAIR IAW SAA EA 737-5753-09-A1098. (M) 2 L 7 2 4F 4 F RT A16WE E2GL 2007102300014 20071023 00014 NM 2007 10 23 AMTA200700489 1 20071012 A 5753 WEDGE BOEING 737 73783N 13844HI NM TE FLAP DAMAGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 310TZ 28243 SAA, INSPECTION FOUND NUMEROUS DENTS, CRACKS AND PUNCTURES ON THE RT IB AFT FLAP WEDGE LOWER SKIN PN 133A2700-18. REPAI RED IAW EA`S 737-5753-09A1099 AND 737-5753-09A1098. REPAIR IS INTERIM AND REQUIRES RE-INSPECTION EVERY 3500 FLIGHT CYCL ES OR 24 MONTHS WHICHEVER COMES FIRST. (M) 2 L 7 2 4F RT A16WE 2007102300025 20071023 00025 NM 2007 10 23 SWAA075092 1 20071016 A 3397 487190 CONNECTOR BOEING 737 7377H4 1384404 NM CABIN FAULTY A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 217JC 34232 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED CONNECTOR AND LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007102300026 20071023 00026 NM 2007 10 23 SWAA075094 1 20071016 A 5610 589354 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT ARCED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 310SW 22949 FLIGHT DECK L1 WINDOW ARCING. REMOVED AND REPLACED WINDOW AND WINDOW HEAT CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 2007102300027 20071023 00027 NM 2007 10 23 SWAA075095 1 20071016 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007102300032 20071023 00032 NM 2007 10 23 SWAA075108 1 20071016 A 5753 6546586 WEDGE BOEING 737 7375H4 138449D NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED 18Y CHECK, FOUND RIGHT WING INBOARD MID FLAP T/E WEDGE LOWER SURFACE DELAMINATED. REMOVED AND REPLACED WEDGE PER MM. 2 L 7 2 4F RT A16WE 2007102300034 20071023 00034 NM 2007 10 23 SWAA075107 1 20071016 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER 25R CRACKED AT BS 505C. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007102300035 20071023 00035 NM 2007 10 23 SWAA075110 1 20071016 A 5313 BAC1498 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 21R CORRODED AT BS 360. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007102300036 20071023 00036 2007 10 23 SWAA075102 4 20071016 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007102300037 20071023 00037 2007 10 23 SWAA075101 4 20071016 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007102300039 20071023 00039 NM 2007 10 23 SWAA075100 1 20071016 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 410WN 27897 DURING SCHEDULED HC1 CHECK, LT OVERWING EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007102300043 20071023 00043 EA 2007 10 23 COMA0770053 1 20071005 A 5320 CC67034175701 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 398CA 10112 FS 280.0 CROSSBEAM IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06. 2 L 7 2 4F RT A21EA 2007102300046 20071023 00046 NM 2007 10 23 HNAA0700239 1 20071008 A 5522 85520001001 SKIN DHAV DHC8 DHC8102 2809003 NM LT ELEVATOR DETERIORATED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 839EX 41111 41111 226 WHILE PAINTING THE AIRCRAFT, RIVET HEADS WERE FOUND TO HAVE BEEN SANDED DOWN ON THE LT ELEVATOR LOWER SKIN. REMOVED AND REPLACED THE RIVETS IAW SRM 51-40-00 AND EO 8- 57-07-3382. 2 H 7 2 4T RT A13NM 2007102300048 20071023 00048 EA 2007 10 23 COMA0770056 1 20071016 A 5320 CC670341757 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 690CA 7565 10182 FS 280 CROSSBEAM AND RIGHT WEB ARE CORRODED BEYOND LIMITS. REPLACED FS 280 CROSSBEAM IAW REO 670-53-11-045 AND INSTALLE D FABRICATED WEB IAW COMAIR EA 70-5311-01892. 2 L 7 2 4F RT A21EA 2007102300053 20071023 00053 EU 2007 10 23 USAA070725 1 20071018 A 5347 R53070089200 SEAT TRACK AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 186US 1701 INBOARD SEAT TRACK Y765 FRAME 47.1 & 47.2 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK PER SR 53-00-15, DEFECT SIZE: 1" X 4" X .090". 2 L 7 2 4F RT A28NM 2007102300054 20071023 00054 NM 2007 10 23 USAA920070950 1 20071016 A 5754 114N4076 SKIN BOEING 757 7572S7 1384962 NM L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 903AW 23323 MCN - MAJOR REPAIR - C-12 CHECK - RIGHT WING NR 9 SLAT COVE SKIN CRACKED, WS 652.50. REPLACED RIGHT WING NR 9 SLAT COVE SKIN, WS 652.50 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007102300055 20071023 00055 NM 2007 10 23 AMTA200700487 1 20071012 A 5710 UNKNOWN BOEING 737 73783N 13844HI NM SPAR UNKNOWN A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 310TZ 28243 INSPECTION OF THE SECONDARY FUEL VAPOR-BARRIER APPLICATION, WING CENTER SECTION TOP PANEL AND FRONT SPAR, 7 EA AREAS FAI LED INSPECTION. C/W EO737-57-AD3096. (K) 2 L 7 2 4F RT A16WE 2007102300073 20071023 00073 CE 2007 10 23 A3W2007F00000 1 20070824 A 5320 071349562 SUPPORT CESSNA 185 A185F 2072821 CE CONT O520 IO520D 17032 SO MCAULY D3A34 D3A34C401 GL RT MLG WW CRACKED E A3WC O OTHER O OTHER NR NOT REPORTED 1 AL 03 21709 3595 18503064 282882 042282 WHILE TAXING, ONCE SNOW COVERED GLACIER, THE RT GEAR OUTER SUPPORT CRACKED AND FAILED, DAMAGING THE SUPPORT BULKHEAD. R OUGH SURFACE AND HIGH PART TT IS SUSPECTED AS CAUSE. NO OTHER AIRCRAFT STRUCTURES WERE DAMAGED. (K) 1 H 7 1 3O 3 O 3A24 E5CE 5 C P47GL 2007102300076 20071023 00076 EA 2007 10 23 COMA0760589 1 20071001 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 518CA 7816 FLIGHT 5384 - FLAPS FAIL CAUTION MESSAGE AT 40 DEGREES. A/C LANDED SAFELY. COMPLIED WITH AD 2006-12-21 FLAP CAUTION ME SSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAU TION MESSAGES. 2 L 7 2 4F RT A21EA 2007102300089 20071023 00089 2007 10 23 WGEA200700011 4 20071008 A 3414 WARNING MESSAGE ECLIPS EA500 ECLIPSEEA500 3350000 SW AIRSPEED ILLUMINATED E WGEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 135DJ 000036 "AIRSPEED DISAGREE" CAS MESSAGE DURING TAKEOFF. RWY 09 KLAL, WINDS 060 AT 10 G15, MOD RAIN, XWIND 5-8 FROM LT, SPEEDS AT ABORT 68 LT PFD, 68 STBY, 74 RT PFD. SUPPLEMENTARY INFORMATION, PERFORMED FLIGHT ENVIRONMENT DATA ADJUSTMENT TEST IAW E A500 MM 34-10-00. SYSTEM GOOD TO SPECIFICATIONS. 1 L 7 2 4J RT A00002AC 2007102300097 20071023 00097 CE 2007 10 23 AMWA87942BC 1 20071010 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MASTER DISCHARGED A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 127ZV 5660 20 UE127 BATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT. BATTERY WAS REPLACED AND DISCREPANCY WAS CLEARED. THIS BATTERY CHARGE ANNUNCIATOR WRITEUP IS CONSIDERED A NUISANCE INDICATION AND IS DISTRACTING TO THE FLIGHTCREW. 2 L 7 2 4T 3 T RT A24CE E2NE 2007102300098 20071023 00098 EA 2007 10 23 TRAX200701502 1 20071015 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 878AS 7590 AAR - MINOR SURFACE CORROSION ON LOWER AFT FUSELAGE AT FS 409.94 APPROX 12FT FROM CENTER LINE (MARKED). 2 L 7 2 4F RT A21EA 2007102300101 20071023 00101 EA 2007 10 23 TRAX200701504 1 20071015 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 722EV 10127 ASD EXTERNAL HANDLE CRACKED. 10-26-07 REMOVED AND REPLACED ASD EXTERNAL HANDLE IAW CRJ SRM 51-40-11, 51-25-06,51-2 5-16 AND CRJ 700 MM 25-11-03. 2 L 7 2 4F RT A21EA 2007102300102 20071023 00102 EA 2007 10 23 TRAX200701505 1 20071015 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 878AS 7590 AAR - FS 484 CLIP CRACKED AT I/B SIDE OF RBL 36.0. 2 L 7 2 4F RT A21EA 2007102300103 20071023 00103 EA 2007 10 23 TRAX200701506 1 20071015 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 878AS 7590 FS 484 CLIP CRACKED AT O/B SIDE OF RBL 27.0. 10-25-07 REMOVED UNSERVICEABLE CLIP AT FS 484 O/B SIDE OF RBL 27.0. R EMOVED HARDWARE FROM RUDDER CONTROL CABLE PULLEYS. DUPLICATED O/B CLIP AT FS 484 RBL 27.0 FROM .063" 2024 T-3 IAW REO 60 1R-53-41-059 AND CRJ 200 SRM 51-24-16. OK TO ALODINE AND PRIME. ALODINED, PRIMED, AND TOPCOATED IAW CRJ 200 SRM 51-25-00 . OK TO INSTALL. INSTALLED SERVICEABLE CLIP TO O/B SIDE OF RBL 27.0 AT FS 484 IAW CRJ 200 SRM 51-42-21. RUDDER CABLE PUL LEYS REQUIRE REINSTALLATION. REINSTALLED RUDDRE CABLE PULLEYS IAW CRJ SRM 51-41-02. 2 L 7 2 4F RT A21EA 2007102300106 20071023 00106 EA 2007 10 23 TRAX200701509 1 20071015 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 CABIN DOOR WON'T OPEN FROM OUTSIDE. 2 L 7 2 4F RT A21EA 2007102300110 20071023 00110 SO 2007 10 23 RAIA00710005 1 20071008 A 3350 66368 LIGHT EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 803HK 145077 PRE FLT NR 3542-STL-EMERGENCY FLOOR PROXIMITY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT STRIP, SYSTEM CHECKS GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007102300112 20071023 00112 EA 2007 10 23 TRAX200701513 1 20071016 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 AAR - PAX DWR AFT DRAG ANGLE CRACKED. 10-30-07 CUT AWAY DAMAGED SECTION OF AFT DRAG ANGLE AND REMOVED BURRS AND SH ARP EDGES IAW BOMBARDIER REO 601R-52-11-513, PERFORMED LPI PER NDTM 51-20-08 ON REORKED AREAS AND CUTOUT EDGES OF PAX DO OR AFT DRAG ANGLE IAW REO 601R-52-11-513, NO DEFECTS NOTED. TOUCHED UP CUT EDGES IAW REO 601R-52-11-513. FABRICATED REPA IR ANGLE AND SPLICE ANGLES IAW REO 601R-52-11-513. OK TO INSTALL. INSTALLED REPAIR ANGLE AND SPLICE ANGLES, SANDED FARI NG SURFACES, FILLET SELECTED EDGES, APPLIED TOPCOAT IAW BOMBARDIER REO 601R-52-11-513. 2 L 7 2 4F RT A21EA 2007102300114 20071023 00114 CE 2007 10 23 100607N409CS 1 20071006 A 7110 635272516 COWLING CESSNA 525 525 2076601 CE WILINT FJ44 FJ44 66000 GL RT ENGINE DEPARTED E Z5FA O OTHER D E INFLIGHT SEPARATION VIBRATION/BUFFET CR CRUISE 1 EA 63 409CS 1724 525B0050 DURING FLIGHT, THE RT ENGINE LOWER COWL SEPARATED FROM THE ENGINE. DAMAGE TO THE RT HORIZONTAL STABILIZER OCCURRED CAUSE D BY IMPACT DAMAGE. CREW REPORTED FEELING A SLIGHT "BUMP" DURING THE FLIGHT, HOWEVER THERE WAS NO INDICATION OR ABNORMAL FLIGHT CHARACTERISTICS. DURING POST FLIGHT THE CREW DISCOVERED THE COWL MISSING AND THE DAMAGE TO THE RT HORIZONTAL STA BILIZER. 1 L 7 2 4F 4 F RT A1WI E3GL 2007102300115 20071023 00115 EA 2007 10 23 TRAX200701514 1 20071016 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ODOR A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 978EV 7723 CREW O2 LOW DUE FUEL SMELL IN COCKPIT CREW USED O2 MASK IN FLT. 2 L 7 2 4F RT A21EA 2007110600024 20071106 00024 EA 2007 11 6 TRAX200701518 1 20071017 A 5720 HINGE FITTING CNDAIR CL600 CL6002C10 1390015 EA LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 722EV 10127 LT MFS HINGE FITTING OUTBOARD AT WS 216.95 CRACKED. 10-29-07 R & R LT MFS FITTING IAW CRJ 700 SB 670-BA-57-010. REM OVED BUTTE DOORS FROM LT WING. BEGAN REMOVING HINGE FITTING IAW BOMBARDIER SB 70BA-57-010. INSTALLED LT WING MFS PCU PE R CRJ 700 AMM 27-62-01-400-801-A01. INSTALLED LT WING FLAP TORQUE TUBE IAW CRJ 700 AMM 27-52-01. INSTALLED LT WING AIL ERON CIRCUIT CABLES IAW CRJ 700 AMM 27-11-13. LT WING AILERON CABLES TENSIONED IN MLG BAY IAW CRJ AMM CHAPTER 27-11-00. REATTACHED LT WING WIRE HARNESS FROM WS 178.00 TO 231.00 FOLLOWING S/M REPAIR IAW SB 670-BA-57-010. TRANSFERED HOLES & DEBUFED NEW PART & INSTALLED LOCK FASTENERS THRU TANK IAW SB 670-BA-57-010. COMPLETED INSTALLATION OF CENTER HINGE F 2 L 7 2 4F RT A21EA 2007102300123 20071023 00123 EA 2007 10 23 TRAX200701524 1 20071018 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 722EV 10127 RIGHT FLOOR SEAT TRACK FS 485.00 TO FS 581.00 HAS SURFACE CORROSION. 2 L 7 2 4F RT A21EA 2007102300124 20071023 00124 EA 2007 10 23 TRAX200701525 1 20071018 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 722EV 10127 LEFT FLOOR SEAT TRACK FS 581.00 TO FS 677.00 HAS SURFACE CORROSION. 2 L 7 2 4F RT A21EA 2007102300126 20071023 00126 EA 2007 10 23 TRAX200701527 1 20071018 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 847AS 7335 EMERGENCY LIGHT STRIP DOES NOT ILLUMINATE. 2 L 7 2 4F RT A21EA 2007102300128 20071023 00128 CE 2007 10 23 DXTA200702533 1 20071011 A 2750 WARNING LIGHT CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE TE FLAPS ILLUMINATED E DXTA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 07 646QS 5605246 DURING FLAP/STAB RETRACTION CYCLE RECEIVED STAB MISCOMPARE AT 203 KIAS. FOUND NOSE GEAR UPLOCK SWITCH BARELY MAKING CON TACT. ADJUSTED NOSE GEAR UP-LOCK ACTUATOR IAW CE560XL MM 32-30-05. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007102300131 20071023 00131 NM 2007 10 23 DXTA200702536 1 20071011 A 2780 SLAT SYSTEM GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE MALFUNCTIONED E DXTA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 GL 07 712QS 073 AFTER DEPARTURE AT APPROPRIATE SPEED, WE SELECTED SLATS UP, KRUEGERS RETRACTED SLATS WENT TO AN INTERMEDIATE POSITION. FLAP/SLAT OPS CHECK I/A/W G200 MM 27-51-45 NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A53NM E35NE 2007102300142 20071023 00142 EU 2007 10 23 UPS07150938 1 20071018 A 2560 ESCAPE ROPE AIRBUS A300 A300F4622R 3930360 EU COCKPIT OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 137UP 0820 INSPECTION TYPE:N/A CAPT ESCAPE ROPE IS FALLING OUT OF STORAGE SPOT. RESECURED AS REQUIRED. 2 L 7 2 4F RT A35EU 2007102300149 20071023 00149 CE 2007 10 23 DXTA200702541 1 20071014 A 2120 UNKNOWN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE AFT SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 382QS 5600382 ON POST FLIGHT INSPECTION, FOUND "HELL HOLE" AREA FULL OF WHITE/GREY SMOKE AND STRONG BURNED RUBBER ODOR. REMOVED & REP LACED A/C MOTOR ASSY. OPS CHECK GOOD IAW 1134400-9 ASSY CMM. 2 L 7 2 4F 4 F RT A22CE E25EA 2007102300164 20071023 00164 CE 2007 10 23 DXTA200702547 1 20071015 A 3260 INDICATOR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG UNKNOWN E DXTA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 333QS 5600333 DURING APPROACH TO LANDING THERE WAS AN UNSAFE RT MLG INDICATION (GREEN LIGHT OUT) WITH NO OTHER UNSAFE INDICATIONS EMER GENCY EXTENSION WAS PERFORMED WITH BOTTLE. T/S SYS AND FOUND RT GEAR INDICATOR BULB INOP. REPLACED WITH NEW FROM A/C FLYAWAY KIT. SERVICED BLOW DOWN SYS AND BLED. OPS CHECK GOOD. IAW MM 32-01-00 AND 32-61-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007102300169 20071023 00169 NM 2007 10 23 AMTA200700494 1 20071013 A 5321 FLOOR PANEL BOEING 737 73783N 13844HI NM BS 440-500 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 308TZ 28244 FWD CARGO FLOOR PANEL 120BF HAS CORROSION ON EDGE OF UPPER SURFACE AS MARKED STA 440-500, LBL25-RBL 20. FABRICATED FLOO R PANEL 120BF, MAT`L 2024-T3, .071, IAW SRM 53-30-53-01, SRM 51-20-01-0E. (K) 2 L 7 2 4F RT A16WE 2007102300170 20071023 00170 WP 2007 10 23 UPS07850929 1 20071009 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 SEAT TRACK AT STA 1380-1400 BL 0 IS CORRODED OUT OF LIMITS. CUT OUT CORRODED SEAT TRACK FROM STA 138 0-1400 BL 0 IAW SRM 53-02-03 -0 FIG 006D. INSTALLED 4 HOLE SEAT TRACK PLUG AT STA 1380-1400 BL 0 IAW SRM 51-3-0. 2 L 7 4 4F RT 4A25 2007102300175 20071023 00175 2007 10 23 UPS07850941 4 20071018 A 2565 SLIDE DOUG DC8 DC871F 302199D WP OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:N/A ESCAPE SLIDE NOT PROPERLY STOWED. REPACK ESCAPE SLIDE, OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2007102300185 20071023 00185 NM 2007 10 23 AMTA200700502 1 20071014 A 5753 SKIN BOEING 737 73783N 13844HI NM RT WING TE FLAP DAMAGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 308TZ 28244 RT WING IB AFT FLAP LOWER SURFACE HAS MULTIPLE NICKS AND GOUGES IN MLG TIRE PATHWAYS. REPAIRED IAW SAA EA 737-5753-09-A 1150 INTERM REPAIR REINSPECT EVERY 3500, FLIGHT CYCLES OR 24 MONTHS WHICHEVER COMES FIRST IAW ATA ERA 737-57R-6170 1405- 523. (K) 2 L 7 2 4F RT A16WE 2007102300189 20071023 00189 NM 2007 10 23 SWAA075144 1 20071018 A 2121 215201 FAN BOEING 737 7373H4 1384600 NM E&E BAY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 649SW 27719 F/A REPORTED SMOKE SMELL IN FIRST 5 ROWS OF CABIN, SMELL GOES AWAY WITH RECIRC AND GASPER FANS OFF. REMOVED AND REPLACE D RECIRC AND GASPER FANS PER MM. 2 L 7 2 4F RT A16WE 2007102300193 20071023 00193 NM 2007 10 23 SWAA075113 1 20071018 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 230WN 34592 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007102300200 20071023 00200 2007 10 23 SWAA075122 4 20071018 A 2565 61620 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007102300206 20071023 00206 NM 2007 10 23 SWAA075129 1 20071018 A 5753 6546435303 FLAP BOEING 737 7375H4 138449D NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED MV2 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007102300209 20071023 00209 NM 2007 10 23 SWAA075148 1 20071018 A 5310 6546956 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 400 AND BS 420, LBL 70. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007102300210 20071023 00210 NM 2007 10 23 SWAA075121 1 20071018 A 5330 6550570 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE LOWER AFT CUTOUT. REPAIRED SKIN PER SWA E A. 2 L 7 2 4F RT A16WE 2007102300211 20071023 00211 2007 10 23 SWAA075134 4 20071018 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM. 2 L 7 2 4F RT A16WE 2007102300214 20071023 00214 NM 2007 10 23 SWAA075138 1 20071018 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007102300220 20071023 00220 2007 10 23 SWAA075131 4 20071018 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007102300223 20071023 00223 NM 2007 10 23 SWAA075133 1 20071018 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 608SW 27928 DURING SCHEDULED BRDG CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007102300225 20071023 00225 NM 2007 10 23 EIA2007157 1 20070905 A 5420 STAND OFF BOEING 747 747212B 1384886 NM NR 4 NACELLE BROKEN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 NR 4 ENGINE NACELLE I/B INSIDE 3RD ACCESS DOOR UPPER ROW, HYD STAND OFF BRACKET IS BROKEN AT BOTTOM WITH FASTENERS PULLE D THROUGH WEB FRAME. REMOVED AND REPLACED HYD STAND-OFF BRACKET AND REPLACED WEB WHERE FASTENERS PULLED THROUGH WEB FRA ME ON NR 4 ENGINE NACELLE I/B SIDE 3RD ACCESS DOOR UPPER ROW PER B747 SRM 54-10-03 FIG 12. 2 L 7 4 4F A20WE 2007102300226 20071023 00226 NM 2007 10 23 EIA2007158 1 20070828 A 5414 SKIN BOEING 747 747212B 1384886 NM NR 1 NACELLE CHAFED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 NUMBER ONE ENGINE PYLON RIGHT SIDE NACELLE STA 180 TO NACELLE STA 236YLON SKIRT CHAFED AND FASTENERS SHEARED. REMOVED E XISTING DAMAGE NR 1 PYLON, RT SKIRT REPAIR DOUBLER AND SHEARED FASTENERS, FABRICATED AND INSTALLED NEW REPAIR DOUBLER AN D NEW FASTENERS ON NR 1 PYLON, RT LOWER SKIRT BETWEEN NAC 180 TO STA 236 PER B747 SRM 54-30-03 FIG 36 SHEETS 1-4. 2 L 7 4 4F A20WE 2007102300229 20071023 00229 NM 2007 10 23 EIA2007159 1 20070921 A 5330 65B02699126 SKIN BOEING 747 747212B 1384886 NM BS 2412-2436 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 EXTERNAL FUSELAGE EMPENNAGE CUTOUT DOOR SKIN RETAINER, FRAME ARE CORRODED AND PAINT DETERIORATED. WORK ACCOMPLISHED PER ECRA NR 486-53-062-2. 2 L 7 4 4F A20WE 2007102300233 20071023 00233 NM 2007 10 23 EIA2007162 1 20070918 A 5320 PLATE BOEING 747 747212B 1384886 NM BS 840 MISINSTALLED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 TENSION TIE STEEL PLATE STA 840 LT HAS ONE PREVIOUSELY DAMAGED FASTENER HOLE WITH SHORT ESGE MARGIN. FABRICATED REPAIR PARTS (STRAPS) PER ECRA 486-53-065-2 AND INSTALLED PER B747 SRM 51-30-02 PAGES 8-19 AND EO 53-747-1818-03 REV "A". 2 L 7 4 4F A20WE 2007102300234 20071023 00234 NM 2007 10 23 USAA920070954 1 20071019 A 3350 21008 SWITCH BOEING 757 7572S7 1384962 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 903AW 23323 MCN - EEL - C-12 CHECK - EMERGENCY LIGHT TEST SWITCH ABOVE L3 DOOR DOES NOT ACTIVATE EMERGENCY LIGHTS. REPLACED AND OPE RATIONAL CHECKED EMERGENCY LIGHT TEST SWITCH ABOVE L3 DOOR IAW B757-200 WDM 33-51-14 TR 33-020 AND TASK CARD A1C33606. 2 L 7 2 4F RT A2NM 2007102300235 20071023 00235 NM 2007 10 23 EIA2007163 1 20070811 A 5311 FRAME BOEING 747 747212B 1384886 NM BS 560 DENTED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 IN FWD PIT BILGE AREA DENT IN BS 560 FRAME WEB LBL19. IN FWD PIT BS 560 LBL 19 MEASURED DENT IN FRAME WERE FOUND TO BE OUT OF LIMITS PER SRM 53-10-01 FIG 1. REMOVED DAMAGE PER B747 SRM 51-40-02 FIG 1, FABRICATED DOUBLER PER B747 SRM 51-20 -01 PAGES 11, 14-20 LOCATED AND DRILLED PER B747 SRM 51-30-05 PAGE 5. ALODINED DOUBLER PER B747 SRM 51-10-02. PRIMED P ER BSOPM 20-41-02 AND INSTALLED PER B747 SRM 51-40-02 DETAIL I. 2 L 7 4 4F A20WE 2007102300236 20071023 00236 NM 2007 10 23 EIA2007164 1 20070918 A 5311 FRAME BOEING 747 747212B 1384886 NM BS 880 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 WHALE BONE (WING TO BODY FAIRING FRAME) CORRODED AT STA 880 STRINGER 46R TO 48R UPPER SURFACE OF LOWER BEAM. REPLACED W HALE BONE AT STA 880 BETWEEN STR 46R TO 48R PER ECRA NR 486-53-059-2. 2 L 7 4 4F A20WE 2007102300244 20071023 00244 EA 2007 10 23 HNAA0700241 1 20071018 A 2612 6504 FIRE DETECTOR DHAV DHC8 DHC8311 1386006 EA NR 2 ENGINE DEFECTIVE A HNAA O OTHER N FALSE WARNING CR CRUISE 1 EA 07 331EN 34390 34390 279 IN FLIGHT CHECK FIRE DETECT WARNING AND MASTER WARNING LIGHTS ILLUMINATED ALONG WITH NR 2 FAULT B ON FIRE PROTECTION PAN EL. ALL ENGINE PARAMETERS WERE NORMAL. CIRCUIT BREAKER K8 ON LEFT ESSENTIAL BUSS FOUND POPPED. RESET CIRCUIT BREAKER AND FOUND, WHEN NR 2 SELECTED TO LOOP B ONLY LOOP TEST INTERMITTENTLY. REMOVED AND REPLACED FIRE DETECTION UNIT AND REP AIRED CHAFED WIRES AT C/P'S 26113P3 AND P5. OPS CHECK GOOD IAW 26-11-00. 2 H 7 2 4T RT A13NM 2007102300255 20071023 00255 NM 2007 10 23 UPS07M50945 1 20070920 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C MAIN DECK: FROM BS 819 TO 849, ALONG -X=28 (RBL 28), SEAT TRACK CROWN & FLANGE AREAS FOUND CORRODED. CORROSION REMOVAL C/OUT & FOUND LIMIT EXCEEDED PER SRM 53-70-00D F3, V1, R35. REMOVAL C/OUT TO GAIN ACCESS AT AFFECTED AREA & CORRODED SEAT/T REMOVED FOR REWORKED. SEAT/T TRIMMED OFF & RWK PER 53-70-00D, F1, V2, R35. HOLES P/UP ON NEW S EAT/T PER SRM 51-31-01 & 51-21-01 V2, R35. NEW SEAT/T AT STA 816 TO 849 INSTL PER SRM 51-33-01 & 51-31-01 V2, R35. FOU ND SATIS. 2 L 7 3 4F RT A22WE 2007102300262 20071023 00262 NM 2007 10 23 2007UALA04133 1 20071005 A 5753 BEARING AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FLAP CARRIAGE MIGRATED A UALA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 806UA 788 A-C HAD A ROUGH BUFFET WITH FLAPS FULL. ALL OTHER CONFIGURATIONS NORMAL. PROBLEM RECURRED ON FLT 0532-15OCT. INSPECTE D NR 1 FLAP CARRIAGE SPHERICAL BEARING FOUND SLIGHTLY MIGRATED BUT AIRWORTHY. OPENED A REPETITIVE INSPECTION PROGRAM TO TRACK THE MIGRATION UNTIL REPLACEMENT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007102300263 20071023 00263 EU 2007 10 23 2007UALA04134 1 20071008 A 2710 3945128102 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ELAC FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 408UA 457 RECEIVED AN "ELAC1 AILERON ORDER DISAGREE" MESSAGE. NR 1 ELAC COMPUTER FAULTY. REPLACED NR 1 ELAC COMPUTER, NO REPEATS . 2 L 7 2 4F 4 F RT A28NM E40NE 2007102300266 20071023 00266 NM 2007 10 23 2007UALA04136 1 20071009 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 178UA 24385 STATION 400-420 S41-42R, EXTERNAL FUSELAGE SKIN IS DENTED. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SKIN. FABRICAT ED & INSTALLED DOUBLER REPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102300267 20071023 00267 2007 10 23 2007UALA04137 4 20071009 A 2565 CYLINDER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EVAC SLIDE LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 178UA 24385 NR 5R MED ESCAPE SLIDE CYLINDER PRESSURE LOW. SUSPECT FAULTY RELEASE VALVE SEAL. REPLACED SLIDE RAFT ASSEMBLY. AC OK F OR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102300268 20071023 00268 CE 2007 10 23 GLBA20061013 1 20071011 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 258 CHAFED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 219GL UE219 LT IB FORWARD WING TO BODY FAIRING FUSELAGE SKIN CHAFFED AT F.S. 258.25 AT B.L. 29.06. REPAIRED LEFT HAND INBOARD FORW ARD WING TO FUSELAGE SKIN FROM F.S. 258.25 TO 267.25 I.A.W. BEECH 1900D SRM 51-70. REPAIR DIMENSIONS APPROXIMATELY 11.5" BY 2".2024 T3. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007102300269 20071023 00269 2007 10 23 2007UALA04138 4 20071009 A 2565 SEAL BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EVAC SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 178UA 24385 ESCAPE SLIDE PRESSURE LOW, UPPER DECK RT AFT. SUSPECT FAULTY RELEASE VALVE SEAL. REPLACED WITH SERVICEABLE RESERVOIR A T UPPER DECK RT AFT PER AMM 25-68-02. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102300270 20071023 00270 NM 2007 10 23 2007UALA04139 1 20071009 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 122UA 29168 SEAT 3J, EEL LIGHT BROKEN. 11-01-07 REPLACED EEL LIGHT ASSY. OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102300271 20071023 00271 NM 2007 10 23 WRLA2007110 1 20071011 A 5320 S292288312000 BRACKET DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 273WA 48519 DURING 4C+12A CHECK, FOUND CABIN FLOOR PANEL SUPPORT BRACKET HAS CORROSION AT STA Y=1887 & X=-68. REPLACED WITH NEW PAR TS PER MD-11 SRM 51-35-01 VOL.2 REV.40 2 L 7 3 4F 4 F RT A22WE E24NE 2007102300272 20071023 00272 NM 2007 10 23 2007UALA04140 1 20071009 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 WALL EEL INOP: CLOSET FWD OF LAV 104, CROSS AISLE & LT SIDE OF LAV 110 & LT SIDE FWD GALLEY ACROSS FROM LAV 100. 11-01 -07 SECURED LOOSE CONNECTIONS IN EACH POSITION, EEL SYSTEM OP CHECKED GOOD FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102300274 20071023 00274 NM 2007 10 23 2007UALA04142 1 20071009 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 WALL EEL INOP: LEFT SIDE MID LAV. 11-01-07 REPLACED WALL LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102300275 20071023 00275 NM 2007 10 23 2007UALA04143 1 20070915 A 5311 FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 929UA 42335 26652 AFT PIT FRAME AT BS 787 & RBL 22 HAS A 0.40 DEEP GOUGE ON UPPER FLANGE. SUSPECT DAMAGED DUE TO NORMAL LOADING AND OFF L OADING OF AC. REMOVED DAMAGE & ACP NDT FOR CRACK CONTAINMENT. FABRICATED & INSTALLED REPAIR DOUBLER. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007102300276 20071023 00276 NM 2007 10 23 2007UALA04144 1 20071009 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 ALL LEFT SEAT EEL INOP B-ZONE. 11-01-07 FOUND LOOSE CONNECTOR. SECURED CONNECTOR & EEL SYSTEM OP CHECKED OK FOR SE RVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102300278 20071023 00278 NM 2007 10 23 2007UALA04146 1 20070919 A 3397 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 529UA 25019 EEL LIGHTS INOP ROWS 7-13. 11-01-07 REPLACED EEL LEAD IN CABLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007102300279 20071023 00279 NM 2007 10 23 2007UALA04147 1 20071009 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EXIT EEL SIGN INOP: DOOR 2L AFT SIDE. 11-01-07 SECURED LOOSE CONNECTION. EXIT LIGHT OP CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102300282 20071023 00282 NM 2007 10 23 2007UALA04151 1 20071008 A 5753 FLAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LT WING GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 LT INBOARD FORE FLAP INBOARD EDGE HAS GOUGES CREATED BY TOO LONG OF SCREWS INSTALLED IN UPPER FIXED PANEL. FOUND IMPROP ER SCREW LENGTH INSTALLED IN PANEL ABOVE DAMAGED FLAP. REMOVED LT INB FORE FLAP AND SENT TO SHOP FOR REPAIR. A/C RECEIV ED A ROBBED FLAP FROM ANOTHER A/C. 2 L 7 2 4F 4 F RT A16WE E21EU 2007102300284 20071023 00284 NM 2007 10 23 2007UALA03862 1 20070921 A 3350 363674 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 670UA 29240 EEL STRIP LIGHT ON SIDE OF SEAT 6B MISSING. REPLACED MISSING EEL LIGHT STRIP. TESTS OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102300286 20071023 00286 NM 2007 10 23 2007UALA03864 1 20070921 A 5315 255T12412 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 677UA 21024 30029 CRACKED ANGLE ON FLOORBEAM BS 246, RBL 16, PULLEY SUPPORT ANGLE. REMOVED DAMAGED, FABRICATED AND INSTALLED REPLACEMENT ANGLE DOUBLER. REPAIRED IAW SRM 51-40-020. INSPECTED & OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102300287 20071023 00287 2007 10 23 F3LA200700279 4 20071009 A 2565 GIRT BAR AIRBUS A319 A319111 3930336 NM R2 DOOR SLIDE UNKNOWN A F3LA O OTHER J WARNING INDICATION CR CRUISE 1 NM 03 922FR 2012 ON FLIGHT FROM KDEN TO KSTL, FLIGHT CREW REPORTED SLIDE ARMING LEVER ON R2 DOOR POPPED OUT DURING FLIGHT. THE FWD F/A P ANEL REGISTERED IT AS DISENGAGED, WHICH WAS CONFIRMED ON THE ECAM PAGE. AIRCRAFT WAS FERRIED ON THE RETURN TRIP TO KDEN . MAINTENANCE ADJUSTED THE R2 DOOR ESCAPE SLIDE AND GIRT BAR FITTINGS IAW AMM 52-13-00-820-057. PRESSURIZED AIRCRAFT I AW AMM 05-53-00-780-002-01. DOOR OPERATION AND INDICATION NORMAL. PERFORMED OPERATIONAL CHECK FLIGHT AND DISCREPANCY D ID NOT DUPLICATE. 2 L 7 2 4F RT A28NM 2007102300288 20071023 00288 EU 2007 10 23 SA07064 1 20070809 A 2530 CHILLER AIRBUS A319 A319112 3930323 EU ZONE 200 SMOKE A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 741UW 1269 LGA - CABIN CREW REPORTED AN ELECTRICAL ODOR IN THE AFT GALLEY. WHEN THE CREW SECURED THE CHILLERS AND COFFEE POTS, THE ODOR SUBSIDED. MAINTENANCE REPLACED THE AFT CHILLER. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007102300289 20071023 00289 NM 2007 10 23 2007UALA03865 1 20070921 A 5512 182T42002 SKIN PANEL BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE HORIZ STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 677UA 21024 30029 RT HORIZ STABILIZER LOWER SURFACE HAS DENT AT APPROX STA 290. REMOVED DAMAGE FROM RT HORIZ LOWER SURFACE & FABRICATED R EPAIR DOUBLERS AND FILLERS. INSTALLED IAW SRM 55-10-01. INSPECTED AND APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102300291 20071023 00291 NM 2007 10 23 2007UALA03867 1 20070921 A 3350 1317 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 677UA 30029 AFT LEFT EMERGENCY EXTERIOR LIGHT IS INOP. RELAMPED, EEL LIGHT OP CHECKED OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102300293 20071023 00293 NM 2007 10 23 2007UALA03869 1 20070923 A 2560 141T612162 HANDLE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE R1 DOOR DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 677UA 30029 DOOR 1R WILL NOT ARM, AND DOOR 2R ARM BUTTON WILL NOT EXTEND. FOUND OUTER DOOR HANDLE NOT STOWED ON DOOR 1-LEFT. CLEAN ED POP OUT BUTTON ON DOOR 1-RIGHT. DOOR ARMS PROPERLY. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102300296 20071023 00296 NM 2007 10 23 2007UALA03876 1 20070921 A 2620 L26504GD TERMINAL BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EXTINGUISH SYS CORRODED A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 787UA 26939 APU DISCHARGE LIGHT ON INTERMITTENTLY. CLEANED CORRODED TERMINALS AT L26504 GD TERMINAL 2, AT P5 BTL DISCH AND AT P40 B TL DISCH LIGHT. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007102300304 20071023 00304 NM 2007 10 23 2007UALA03891 1 20070925 A 3350 20131A POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 RIGHT OVERWING TOP EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY. EEL OPERATES GOOD FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102300305 20071023 00305 NM 2007 10 23 2007UALA03892 1 20070925 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY LIGHT SEAT 4A FWD INOP. REPLACED LIGHT, OP CHECKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102300309 20071023 00309 EU 2007 10 23 2007UALA04159 1 20071009 A 5270 DHE1141 PROXIMITY SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY EXIT FAULTY A UALA K NONE N FALSE WARNING NR NOT REPORTED 1 WP 29 439UA 683 R AFT EMER EXIT DISPLAYED ON UPPER ECAM SCREEN. DOOR CREW COMMENTS: CABIN PRESSURE IS NORMAL. PROX SWITCH FAULTY. RE PLACED PROX SWITCH HANDLE FLAP RIGHT AFT EMERGENCY EXIT DOOR 21WV2. 2 L 7 2 4F 4 F RT A28NM E40NE 2007102300312 20071023 00312 2007 10 23 2007UALA04162 4 20071009 A 2565 SLIDE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 648UA 25285 RIGHT EMERGENCY ESCAPE SLIDE TESTS INOP DURING SQUIB TEST. REPLACED OFF WING ESCAPE SYS. EMERGENCY BATTERY FOR RIGHT SI DE. (M962) ESCAPE SLIDE SQUIBS TEST NORMAL 2 L 7 2 4F 4 F RT A1NM E24NE 2007102300315 20071023 00315 NE 2007 10 23 2007UALA04165 2 20071009 A 7310 8088001 FMU BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUEL SYSTEM LEAKING A UALA O OTHER W K INADEQUATE Q C FLUID LOSS IN INSP/MAINT 1 WP 29 783UA 26950 FUEL LEAKING BETWEEN FUEL PUMP AND FMU. REPLACED NR 2 ENG FMU UNIT. LEAK CHECKED OK. CAUSE WAS CONNECTION SECURITY OR FAULTY SEAL. VERIFICATION FLIGHT CONFIRMS NORMAL OPERATION. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007102300316 20071023 00316 NM 2007 10 23 2007UALA04166 1 20071010 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY LIGHT INOP AT SEAT 43HJK & AT SEAT ABC. 11-01-07 RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102300320 20071023 00320 2007 10 23 2007UALA04170 4 20071004 A 2565 68014916 O-RING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SLIDE BOTTLE LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 198UA 28716 MAIN ENTRY DOOR SLIDE PRESSURE GAUGE IS NOT WITHIN THE GREEN BAND. PRESSURE TESTED FOR LEAK. O-RING AT GAUGE ELBOW ASSE MBLY LEAKING. REMOVED AND REPLACED O-RING. RETESTED AND TESTED OK 2 L 7 4 4F 4 F RT A20WE E24NE 2007102300323 20071023 00323 NM 2007 10 23 EIA2007165 1 20070917 A 5330 SKIN BOEING 747 747212B 1384886 NM BS 380-400 S44R CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 EXTERNAL FUSELAGE STA 390 STR 44R SKIN IS CRACKED AT FASTENER HOLE. REPAIRED EXTERNAL FUSELAGE AT STA 390 STR 44R PER E CRA NR 486-53-061-2 PART 1. 2 L 7 4 4F A20WE 2007102300324 20071023 00324 WP 2007 10 23 07FDEA04611 1 20071016 A 5347 S49291471 SEAT TRACK DOUG DC10 DC1010F 3022111 WP BS 880 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 MAIN CABIN STA 880, RBL 76 SEAT TRACK CORRODED. REMOVED, FAB'D AND INSTALLED SEAT TRACK IAW DC/MD 10 SRM 51-31-01 VOL I I PAGE 1 AND DAC DRAWING AFA 7433 REV AD. ALODINED AND PRIMED IAW DC/MD 10 SRM 51-21-01 VOL II PAGE 1 AND 21. 2 L 7 3 4F A22WE 2007102300325 20071023 00325 EU 2007 10 23 07FDEA04580 1 20071013 A 5315 A53779699206 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 670FE 777 MAIN CARGO COMPARTMENT FLOORBEAM CRACKED FRAME 30 BETWEEN YD TO YE. FABRICATED AND INSTALLED CROSSBEAM COUPLING IAW SR M 53-10-15 . 2 L 7 2 4F RT A35EU 2007102300326 20071023 00326 EU 2007 10 23 07FDEA04588 1 20071015 A 5712 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND OLD REPAIR ON RT WING BOTTOM SKIN RIB 9 UNDER JOINT STRAP WITH NEW CORROSION AND FINDINGS REPAIR PERFORMED BY CO RROSION BLEND OUT, NDT FOR CRACK FREE AND REPROTECTING THE AREA IAW EA 6-5720-106519. 2 L 7 2 4F RT A35EU 2007102300327 20071023 00327 EU 2007 10 23 07FDEA04597 1 20071015 A 5730 A57340087 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION ON LT WING BOTTOM SKIN LOWER SURFACE RIB 4-5, AROUND SEVERAL HOLES. REPAIR PERFORMED BY BLEND OUT CORRO SION, APPROVED BY EA 6-5720-112530 AND RAS/BAE/1005161/2007 ISS A. 2 L 7 2 4F RT A35EU 2007102300328 20071023 00328 NM 2007 10 23 EIA2007170 1 20070920 A 5330 SKIN BOEING 747 747132 1384882 NM BS 1315 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 R3 DOOR UPPER AQFT CORNER SKIN CRACKED STA 1315 STR R17. TRIMMED OUT CRACK, FABBED AND INSTALLED REPAIR PER B747 SRM 53 -30-03 FIG 44. 2 L 7 4 4F A20WE 2007102400007 20071024 00007 NM 2007 10 24 EIA2007173 1 20070925 A 5311 FRAME BOEING 747 747132 1384882 NM BS 800 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 LT BS 800 L2 DOOR FRAME STRIP FASTENER HOLE CRACKED. LT BS 800 FRAME STRIP FASTENER HOLE CRACK REPAIRED PER EA-53-1187. 2 L 7 4 4F A20WE 2007102400013 20071024 00013 EU 2007 10 24 07FDEA04577 1 20071012 A 7830 SEAL GE AIRBUS 310 A310203 3930313 EU THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 430FE 34482 10085 R535122 394 DURING SCHEDULED B CHECK INSPECTION NR 1 LT THRUST REVERSER LIP SEAL WAS FOUND TO BE CRACKED. REPLACEMENT OF DAMAGED RE VERSER. 2 L 7 2 4F RT A35EU 2007102400016 20071024 00016 NM 2007 10 24 07FDEA04581 1 20071013 A 5712 RIB DOUG MD11 MD11F 3023600 NM RWS 789 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 620FE 48791 RIGHT WING LEADING EDGE CAVITY RIB DOUBLER AT STATION XOS 789 (XORS 683) FOUND CRACKED. 10-29-07 REMOVED CRACKED RIB DOUBLER AS PER SRM 51-31-01 VOLUME II AND FABRICATED RIB DOUBLER AS PER DOUGLAS DRAWING ARB3954 AND INSTALLED AT RI GHT HAND WING LEADING EDGE CAVITY AT XOS 789 AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007102400017 20071024 00017 NM 2007 10 24 07FDEA04582 1 20071013 A 5712 RIB DOUG MD11 MD11F 3023600 NM LWS 584 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 620FE 48791 LEFT WING LEADING EDGE CAVITY AREA RIB ANGLE AT STATION XOS 584 FOUND CRACKED. 10-29-07 REMOVED CRACKED RIB ANGL E (FORMER) AS PER SRM 51-31-01 VOLUME II AND FABRICATED FORMER AS PER DOUGLAS DRAWING ARB2931 AND INSTALLED FORMER AT LE FT HAND WING LEADING EDGE CAVITY AREA AT XOS 584 AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-1 00. 2 L 7 3 4F RT A22WE 2007102400019 20071024 00019 NM 2007 10 24 07FDEA04584 1 20071013 A 5347 ACA7399501 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 635 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 620FE 48791 MAIN DECK CARGO COMPARTMENT LEFT FLOOR SEAT TRACK AT STATION 635, X = 47.5 FOUND CRACKED APPROXIMATELY 3 INCHES. 10 -30-07 REPAIRED BY REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007102400023 20071024 00023 EU 2007 10 24 07FDEA04589 1 20071015 A 5510 A55177510000 HINGE FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION ON LT THS HINGE FITTING NR 1 REPAIR PERFORMED BY CORROSION BLEND OUT, NDT FOR CRACK FREE AND REPROTECTIN G THE AREA IAW EA 6-5516-106523 AND RAS/CASA/5537/2007 ISS A. 2 L 7 2 4F RT A35EU 2007102400024 20071024 00024 EU 2007 10 24 07FDEA04590 1 20071015 A 5510 A55177545000 HINGE FITTING AIRBUS 300 A300B4622R 3930312 EU HORIZONTAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION ON LT THS HINGE FITTING NR 7. REPAIR PERFORMED BY CORROSION BLEND OUT, NDT FOR CRACK FREE AND REPROTECT ING THE AREA IAW EA 6-5516-106523 AND RAS/CASA/5537/2007 ISS A. 2 L 7 2 4F RT A35EU 2007102400027 20071024 00027 EU 2007 10 24 07FDEA04593 1 20071015 A 5730 A57340087 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION ON LT WING BOTTOM SKIN LOWER SURFACE RIB 8. REPAIR PERFORMED BY BLEND OUT CORROSION, APPROVED BY EA 6-5 720-112530 AND RAS/BAE/1005161/2007 ISS A. 2 L 7 2 4F RT A35EU 2007102400029 20071024 00029 EU 2007 10 24 07FDEA04595 1 20071015 A 5730 A57340093 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION ON LT WING BOTTOM SKIN LOWER SURFACE RIB 5, AROUND SEVERAL HOLES. REPAIR PERFORMED BY BLEND OUT CORROSI ON, APPROVED BY EA 6-5720-112530 AND RAS/BAE/1005161/2007 ISS A. 2 L 7 2 4F RT A35EU 2007102400033 20071024 00033 NM 2007 10 24 07FDEA04600 1 20071015 A 5313 65602081 STRINGER BOEING 727 727233 138408A NM BS 1178 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 AFT PIT BILGE STRINGER END FITTING IS CORRODED BS 1178, STR 29L, WL155 (MKD). REMOVED AND REPLACED STR 29L END FITTING PN NR 65-60208-1 IAW 51-30-2. REMOVED CORRODED SECTION OF STR 29L AND REPAIRED STR 29L IAW SRM 53-10-3 FIG I DETAIL I S TA 1178-1164. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007102400035 20071024 00035 NM 2007 10 24 QXEA200701548 1 20071013 A 2910 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN UNKNOWN A QXEA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 NM 09 423QX 4153 SMF FLIGHT NR 2302: LOUD HUM WITH PTU AND STANDBY PUMP ACTIVATED. ALL PRESSURE GOOD. AIRCRAFT RETURNED TO BLOCK. MAIN TENANCE C/W Q400 AMM TASK 29-11-36-710-801 AND TASK 29-11-61-710-801. ALL TESTS NORMAL WITH NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102400036 20071024 00036 NM 2007 10 24 QXEA200701549 1 20071015 A 3010 DEICE SYSTEM BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 416QX 4083 SEA FLIGHT NR 2316: AFTER AIRCRAFT WAS STARTED, BOTH ENGINES RUNNING, DEICE PRESSURE CAUTION ILLUMINATED. BOTH SIDES IN DICATED 6 PSI. SELECTING MANUAL ON AIRFRAME MODE SELECTOR RETURNED DEICE PRESSURE TO 18 PSI. SELECTING OFF AGAIN, PRES SURE AGAIN DROPPED TO 18 PSI. CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE STARTED BOTH ENGINES . DEICE PRESSURE WAS 18 PSI. TURNED BLEEDS ON WITH NO FLUCTUATION IN DEICE PRESSURE NOTED. C/W AIRFRAME DEICE SYSTEM OPS CHECK PER AMM 30-11-00-720-801. OPS CHECK GOOD. NO OTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102400037 20071024 00037 WP 2007 10 24 NWAA073469866 1 20071014 A 3240 FUSE DOUG DC9 DC951 3022051 WP BRAKE ASSY FAILED A NWAA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 01 775NC 47785 AS THE AIRCRAFT WAS TAXING OUT FOR DEPARTURE THE LEFT HYDRAULIC SYSTEM LOST ALL FLUID AND PRESSURE. THE AIRCRAFT RETURN ED TO THE GATE WITHOUT ANY FURTHER PROBLEMS. MAINTENANCE FOUND THE LEFT MAIN LANDING GEAR BOTTOM BRAKE FUSE "CAME APART " AND THE LEFT HYDRAULIC SYSTEM RESERVOIR WAS EMPTY. THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP AND FILTERS WERE REPLACED. LEAK CHECK AND OPERATIONAL CHECK WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007102400040 20071024 00040 NE 2007 10 24 DL76G071335 2 20071010 A 7321 EEC BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 ENGINE FAILED A DALA D RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 1602 29694 704809 CREW REPORTED ON RT ENG START HAD R EEC CONTROL STATUS MSG AND EEC CHAN "A" CB POPPED. CB WOULD NOT RESET. NO DISPATCH FAULT. REPLACED RT EEC. ALL MESSAGES CLEARED. 2 L 7 2 4F 4 F RT A1NM E13NE 2007102400042 20071024 00042 NM 2007 10 24 DL764071337 1 20071010 A 4920 38006081 ENGINE BOEING 767 767432ER 1385134 NM APU INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 826MH 15526 29697 AIRCRAFT RESTRICED FROM ETOPS DUE TO HISTORY OF APU NOT STARTING. REPLACED APU AND STARTER PER MM. OPS CK. APU AND ST ARTER OPS NORMAL. SERVICED FLUID LEVELS TO FULL. 2 L 7 2 4F RT A1NM 2007102400047 20071024 00047 NM 2007 10 24 DL764071342 1 20071013 A 3350 LIGHT BOEING 767 767432ER 1385134 NM SEAT 11GF INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 833MH 29706 EMERGENCY LIGHT IN CEILING INOP AT SEAT 11FG. RELAMPED AND OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2007102400048 20071024 00048 NM 2007 10 24 DL764071343 1 20071013 A 3350 LIGHT BOEING 767 767432ER 1385134 NM PAX 17GF INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 833MH 29706 EMERGENCY LIGHT IN CEILING ABOVEE SEAT 17GF INOP. RELAMED AND OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2007102400049 20071024 00049 NM 2007 10 24 DL764071344 1 20071013 A 3350 LIGHT BOEING 767 767432ER 1385134 NM PAZ 25E INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 833MH 29706 EMERGENCY LIGHT IN CEILING ABOVE 25E INOP. RELAMPED AND OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2007102400053 20071024 00053 NM 2007 10 24 DL764071348 1 20071013 A 3350 LIGHT BOEING 767 767432ER 1385134 NM SEAT 14E INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 833MH 29706 EMERGENCY LIGHT IN CEILING INOP AT SEAT 14E. RELAMPED AND OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2007102400054 20071024 00054 NM 2007 10 24 DL764071349 1 20071013 A 3350 LIGHT BOEING 767 767432ER 1385134 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 833MH 29706 FOUND EMERGENCY LIGHT INOP ON RT SEAT ROW A ZONE. 2 L 7 2 4F RT A1NM 2007102400060 20071024 00060 EA 2007 10 24 SWIA200718777 1 20071013 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 466SW 7856 FLT 3854 - HYDRAULIC PUMP 3A MAKES NOISE AND HAS A NOTABLE BURNING SMELL. REPLACED PUMP 3A IAW 29-12-03. OPS CHECK GOO D. 2 L 7 2 4F RT A21EA 2007102400068 20071024 00068 NM 2007 10 24 07FDEA04604 1 20071016 A 5347 ADA83901 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 755 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 620FE 48791 MAIN DECK CARGO COMPARTMENT RIGHT FLOOR SEAT TRACK AT STATION 755, X = -8.5, FOUND CRACKED APPROXIMATELY 3 INCHES. 10 -30-07 REPAIRED BY REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007102400074 20071024 00074 NM 2007 10 24 07FDEA04610 1 20071016 A 5330 6561611 SKIN BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 13TH LT WINDOW PLUG AFT OF AFT OVERWING EXIT HAS CORROSION ON EXT SURFACE INSTALLED NEW WINDOW PLUG REF MM 56-20-000-4 A PPLIED CIC TO INTERIOR REF SRM 51-10-2, PAINTED TO MATCH SRM 51-10-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007102400075 20071024 00075 WP 2007 10 24 07FDEA04612 1 20071016 A 5347 ABA7680503 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 SEAT TRACK (EQUIPMENT TIE DOWN TRACK) AT APPROX BL 91 LT AND BETWEEN FS 392 AND 25 HAS CORROSION. REMOVED, FAB'D AND IN STALLED SEAT TRACK IAW SRM 53-70-00 FIG 5 SHT 2 VOL I AND DAC DWG ABA 7680. 2 L 7 3 4F A22WE 2007102400094 20071024 00094 WP 2007 10 24 07FDEA04615 1 20071017 A 5522 ALC7386 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 RT STAB, INBD ELEVATOR, MODERATE CORROSION BTWN UPPER SKIN AND RIB. REPAIRED AREA IAW SRM 55-10-00 FIG 7 VOL I. 2 L 7 3 4F A22WE 2007102400096 20071024 00096 WP 2007 10 24 07FDEA04617 1 20071017 A 5730 NRC6053 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 RT WING OUTBOARD FLAP CRACK ON EXT SKIN UPPER SIDE. REPAIRED AREA IAW SRM 57-10-00 FIG 7 VOL I. 2 L 7 3 4F A22WE 2007102400099 20071024 00099 WP 2007 10 24 07FDEA04620 1 20071017 A 5320 AEA01613 WEB DOUG DC10 DC1010F 3022111 WP ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 LT MLG W/W FOUND CRACK ON VERTICAL WEB. REPAIRED WEB IAW SRM 53-00-01 FIG 10 VOL I. 2 L 7 3 4F A22WE 2007102400107 20071024 00107 NM 2007 10 24 07FDEA04632 1 20071017 A 5320 655756729 CHANNEL BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 AFT PIT FLOOR SUPPORT "C" CHANNEL IS CORRODED BS 1165, RBL 7, WL 160. REMOVED DAMAGE IAW SRM 51-10-1 PG 1. FABRICATED REPAIR CHANNEL, AND 2 ANGLES IAW SRM 53-10-5 PG 9/10. INSTALLED REPAIR PARTS IAW 53-10-5, AND 51-30-02 THIS IS CLASSI FIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007102400108 20071024 00108 NM 2007 10 24 07FDEA04633 1 20071017 A 5740 651928917 ATTACH FITTING BOEING 727 727233 138408A NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 RT AILERON (OTBD) CAVITY HAS CRACKED ATTACH CLIP LOCATED BET WING TRAILING EDGE RIB AT STA 658.63 AND CAVITY AFT SPAR FA BRICATED CLIP BETWEEN WING TRAILING EDGE, STA 658.63 CAVITY AFT SPAR. REF SRM 51-30-02, DWG 65-19289 PG 1. THIS IS CLA SSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007102400113 20071024 00113 NM 2007 10 24 QXEA200701571 1 20071017 A 3010 DEICE SYSTEM BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 422QX 4150 SEA FLIGHT NR 2439: DEICE PRESSURE CAUTION ILLUMINATED AFTER BOOTS SELECTED TO SLOW. AS PER CHECKLIST, CAUTION CLEARED. SELECTOR TO SLOW, DEICE CAUTION LIGHT ILLUMINATED AGAIN. NR 2 BOOT SET ON RIGHT WING WILL NOT INFLATE. CORRESPONDING LIGHT DOES NOT ILLUMINATE. PRESSURE NORMAL DURING ALL BOOT CYCLES. MAINTENANCE STARTED NR 1 ENGINE. INSPECTED RT WIN G BOOTS, NDN, CYCLED BOOTS 4 CYCLES, NDN, CYCLED BOOTS IN SLOW, NDN, CYCLED BOOTS IN FAST, NDN, (3 CYC MADE IN FAST AND SLOW) STARTED NR 2 ENGINE. CHECKED BOOTS ON LT WING, NDN, CYCLED BOOT IN MANUAL FOR 3 CYCLES, NDN, CYCLED BOOTS IN SLOW FOR 3 CYCLES, NDN, CYCLED BOOTS IN FAST FOR 3 CYCLES NDN, STARTED NR 1 ENGINE. CYCLED BOOTS FOR 3 CYCLES EACH IN MANUA 2 H 7 2 4T RT A13NM 2007102400117 20071024 00117 EA 2007 10 24 QXEA200701544 1 20071015 A 2611 4462534 SMOKE DETECTOR CNDAIR CL600 CL6002C10 1390015 EA LAVATORY FAILED A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 09 613QX 15534 10045 PDX - FLIGHT 9850 (PART 91 OPERATIONAL CHECK FLIGHT), ON TAKEOFF ROLL AT 100 KNOTS RECEIVED A LAV SMOKE DETECTOR MESSAGE . ABORTED TAKEOFF. MAINTENANCE REPLACED THE LAVATORY SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO S ERVICE. 2 L 7 2 4F RT A21EA 2007102400122 20071024 00122 EU 2007 10 24 F3LA200700284 1 20071018 A 3350 LIGHT AIRBUS A318 A318111 3940019 EU ROW 15ABC INOPERATIVE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 804FR 2051 DURING HEAVY SERVICE CHECK, INSPECTION REPORTED 1 LAMP INOPERATIVE IN SEAT ROW 15ABC EMERGENCY SEAT MOUNTED LIGHT. REMO VED AND REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSY AT ROW 15ABC IAW AMM 33-51-19-PB401. OPS CHECK GOOD. 2 L 7 2 4F RT 2007102400123 20071024 00123 EU 2007 10 24 F3LA200700285 1 20071018 A 3350 LAMP AIRBUS A318 A318111 3940019 EU EMERGENCY LIGHT INOPERATIVE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 804FR 2051 DURING HEAVY SERVICE CHECK, INSPECTION REPORTED 1 LAMP TOP INOPERATIVE IN L1 DOOR LOWER EMERGENCY EXIT SIGN. RELAMPED W ALL MOUNTED EXIT SIGN BY L1 DOOR IAW AMM 33-51-13-PB401. OPS CHECKED GOOD. 2 L 7 2 4F RT 2007102400126 20071024 00126 EA 2007 10 24 SWIA200718782 1 20071016 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER AP APPROACH 1 NM 07 472CA 7667 FLT 2511 - RIGHT WINDOW CRACKED ON APPROACH. REPLACED RIGHT SIDE WINDOW IAW CRJ 200 MM 56-12-01. 2 L 7 2 4F RT A21EA 2007102400129 20071024 00129 EA 2007 10 24 SWIA200718785 1 20071013 A 7120 BUSHING CNDAIR CL600 CL6002C10 1390015 EA ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 368CA 10075 RIGHT ENGINE FORWARD MOUNT LINK BUSHING IS CORODED. INSTALLED NEW LINK WITH NEW BUSHING IAW MM 71-00-00. 2 L 7 2 4F RT A21EA 2007102400136 20071024 00136 WP 2007 10 24 07FDEA04624 1 20071017 A 5347 607158 SEAT TRACK DOUG DC10 DC1030F 3023504 WP BS 615-635 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 320FE 47835 MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREAS AT F/S 615-635 RBL 48. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 VO L 1 FIG 1. 2 L 7 3 4F RT A22WE 2007102400138 20071024 00138 NM 2007 10 24 07FDEA04636 1 20071017 A 5280 65C271282 SKIN BOEING 727 727233 138408A NM ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 RT MLG GEAR DOOR INSIDE SKIN IS CRACKED REMOVE DAMAGED AREA, INSTALL REPAIR SKIN, DBLR, ACCESS PLATE, REF EO7-5280-7-430 1 AND SRM 51-30-2, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007102400139 20071024 00139 NM 2007 10 24 07FDEA04637 1 20071017 A 5753 652163585 SKIN BOEING 727 727233 138408A NM TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 LT OUTBOARD AFT FLAP, T/E INBOARD CORNER IS DELAMINATED REPAIRED LT OUTBOARD AFT FLAP T/E CORNER REF SRM 51-40-20 PARA 6, 7, 19, -21. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007102400140 20071024 00140 NM 2007 10 24 07FDEA04638 1 20071017 A 5330 6561611 SKIN BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 LT 10TH WINDOW PLUG AFT OF AFT OVERWING EXIT HAS CORROSION INSTALLED NEW WINDOW PLUG, PAINTED TO MATCH, REF MM 51-20-013 -PG 1-3 AND MM 51-20- 151-7 PAGES 1-3. 2 L 7 3 4F RT A3WE 2007102400141 20071024 00141 NM 2007 10 24 07FDEA04639 1 20071017 A 5720 6521658149 RETAINER BOEING 727 727233 138408A NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 RIGHT WING LOWER TRAILING EDGE PANEL JUST BELOW NR 11 FLIGHT SPOILER ACTUATOR BULB SEAL RETAINER CRACKED. REPLACED SEAL RETAINER REF 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007102400142 20071024 00142 EU 2007 10 24 07FDEA04640 1 20071017 A 5320 A5361068856702 ATTACH ANGLE AIRBUS 310 A310222 3930315 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 L1 DOOR SCUFF PLATE ATTACH ANGLE HAS ALL HOLES OUT OF ROUND OVERSIZED. REMOVED AND REPLACED FITTING IAW A310-200-SRM 51 -40-21 PAR 7. 2 L 7 2 4F RT A35EU 2007102400147 20071024 00147 EU 2007 10 24 07FDEA04646 1 20071018 A 5340 A5361068856802 ATTACH ANGLE AIRBUS 310 A310222 3930315 EU R-1 DOOR AREA DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 R-1 DOOR SCUFF PLATE ATTACH ANGLE HAS HOLES OUT OF ROUND AND OVERSIZED. REMOVED AND REPLACED R-1 DOOR SCUFF PLATE FITTI NG IAW A31-200 SRM 51-40-21 PARA 7. 2 L 7 2 4F RT A35EU 2007102300051 20071023 00051 EA 2007 10 23 COMA0760588 1 20071001 A 4920 38004883 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY MALFUNCTIONED A COMA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 SO 01 926CA 15953 7027 FLIGHT 5618 - FLAME REPORTED IN APU EXHAUST. REPLACED APU ASSEMBLY. 2 L 7 2 4F RT A21EA 2007102300065 20071023 00065 WP 2007 10 23 EWCR200700003 2 20071018 A 7261 OIL SYSTEM CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP LT ENGINE LEAKING E EWCA A B UNSCHED LANDING EMER. DESCENT K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 39 750CK 6507015 102133 THE AIRCRAFT WAS A CRUISE ALTITUDE 37,000 WHEN THE PILOTS NOTICED FIRST BLUE, AND THEN WHITE SMOKE FILLING THE FLIGHT D ECK AND CABIN. REDUCED POWER, DECLARED AN EMERGENCY, AND LANDED AT LAGRANGE, GA. THERE WAS STILL SOME SMOKE IN THE AIR CRAFT UPON LANDING. AFTER EXITING THE AIRCRAFT, THE PILOTS REPORTED THAT THERE WAS OIL ON THE OUTSIDE OF THE LEFT ENGIN E COWLING AND INSIDE TAILPIPE. NEITHER ENGINE WAS SHUT DOWN DURING THE INCIDENT. AT PRESENT, SUSPECT OIL LEAKAGE INTO BLEED AIR SYSTEM FROM DEFECTIVE CARBON SEAL INSIDE COMPRESSOR SECTION. 2 L 7 2 4F 4 F A9NM E6WE 2007102300066 20071023 00066 CE 2007 10 23 CB52007F00000 1 20071001 A 3233 FITTING CESSNA 303 T303 2073820 CE CONT O520 LTSIO520AE 17040 SO MCAULY 3AF32C 3AF32C505 GL ACTUATOR SHEARED I CB5Y L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 35 57MT T30300211 THE PILOT REPORTED THE GEAR UNSAFE WARNING IN FLIGHT. THE GEAR WAS SELECTED DOWN AND NOSE AND RT MAIN GREEN LIGHT ONLY ILLUMINATED. THE PILOT DID FLYBY OF THE TOWER, WHO CONFIRMED THE LT GEAR APPEARED DOWN. THE AIRCRAFT CONTINUED IN FLIG HT AND LANDED AT DESTINATION. FOLLOWING WAS NOTED ON INSP OF LT LANDING GEAR: THE HYDRAULIC ACTUATOR RAM HAD SHEARED A T THE END FITTING THREADS. THE FREE ACTUATOR RAM HAD JAMMED FORWARD OF THE DOWNLOCK BRACKET. THE DOWNLOCK BRACKET WAS BENT PREVENTING THE DOWNLOCK ENGAGING WITH DRAG LINK STRUT. THE CAUSE OF THE ACTUATOR FAILURE IS UNKNOWN. (K) 1 L 7 2 3O 3 O A34CE E8CE 5 C P22EA 2007102300077 20071023 00077 EA 2007 10 23 COMA0760590 1 20071002 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 819CA 15453 7415 FLIGHT 5604 - NOSE LANDING GEAR DID NOT EXTEND. FOLLOWED QRH, GEAR EXTENDED, LANDED WITHOUT INCIDENT. REPLACED NLG PRI ORITY VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007102300094 20071023 00094 EU 2007 10 23 TRAX200701500 1 20071015 A 3350 LIGHT AEROSP ATR72 ATR72 EU ASD INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 637AS 383 ASD EMERGENCY LIGHT INOP. 2 H 7 2 4T RT 2007102300095 20071023 00095 EA 2007 10 23 TRAX200701501 1 20071015 A 5342 DRAG BRACE CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 722EV 10127 DRAG BRACE FOR FUSELAGE TO VERTICAL STAB, T/E CRACKED. 10-29-07 REPAIRED DRAG BRACE ANGLE IAW REO 670-55-31-018. 2 L 7 2 4F RT A21EA 2007103000002 20071030 00002 SO 2007 10 30 SIMA200729707 1 20071020 A 3150 WARNING MESSAGE EMB 145 EMB145LR 3260212 SO RUDDER FALSE ACTIVATION A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 906AE 14500894 NOTIFIED BY CREW VIA GRD LINE. ABORTED T/O AT LOW SPEED DUE TO RUD SYS 1 FAIL EICAS MSG. THE MESSAGE WENT AWAY AFTER F OLLOWING CHECK LIST. PERFORMED FIM OF RUDDER SYS INOP ON EICAS PER EMB 145 FIM 27-22-00-810. PERFORMED TEST OF RUDDER P ER EMB 145 MM 27-23-00 NO DEFECTS FOUND AT THIS TIME. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4T RT T00011AT 2007102300129 20071023 00129 CE 2007 10 23 DXTA200702534 1 20071011 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE WEAK E DXTA A UNSCHED LANDING O OTHER TX TAXI/GRND HDL 1 GL 07 374QS 5600475 CAPT AND FO BRAKES ARE SPONGY. COMPLIED WITH TAXI AND BRAKE CHECK OF AIRCRAFT NO DEFECTS NOTED. WORK DONE IAW CE560 MM 32-42-00 2 L 7 2 4F 4 F RT A22CE E25EA 2007102300130 20071023 00130 CE 2007 10 23 DXTA200702535 1 20071011 A 3230 LANDING GEAR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LEFT MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 328QS 5600428 LT MAIN GEAR DID NOT INITALLY RETRACT AFTER TAKEOFF OTHER GEAR RETRACTED NORMALLY. REMOVED LEFT MAIN GEAR UPLOCK SWITCH DUE TO HIGH RESISTANCE. INSTALLED NEW SWITCH IAW CE560 M/M CH 32-30-00, OPS CHECKED GOOD DURING GEAR SWING. 2 L 7 2 4F 4 F RT A22CE E25EA 2007102300141 20071023 00141 SO 2007 10 23 C2XA07IA225 1 20071018 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15983 145239 IAH - FLIGHT 2455, THE CREW REPORTED THAT THE FORWARD CEILING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007102300143 20071023 00143 NM 2007 10 23 UPS07550937 1 20071018 A 3620 SENSOR BOEING 757 75724APF 1384969 NM RT ENGINE MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 453UP 25474 INSPECTION TYPE:N/A DIVERSION - RIGHT ENGINE BLEED INOP. A/C DIVERTED TO ONT DUE TO WEATHER RESTRICTIONS. REMOVED AND REPLACED PNEU EQUIPMENT STRUT TEMP SENSOR SYSTEM. OPS CHECK NORMAL. 2 L 7 2 4F RT A2NM 2007102300145 20071023 00145 NM 2007 10 23 UPS07550939 1 20071018 A 2560 SEAL BOEING 757 75724APF 1384969 NM ESCAPE REEL MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 469UP 25485 INSPECTION TYPE:N/A EMERGENCY ESCAPE REEL SECOND FROM FWD NO SEALS. REMOVED AND REPLACED SECOND FROM FWD EMERGENCY ESCA PE REEL AS PER MM 25-61-02-2. 2 L 7 2 4F RT A2NM 2007102300147 20071023 00147 CE 2007 10 23 DXTA200702538 1 20071012 A 2120 UNKNOWN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE COCKPIT ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 319QS 5600519 THERE IS A BURNING ELECTRICAL ODOR IN COCKPIT WHEN DEFOG FAN IS SELECTED ON. REMOVED & REPLACED DEFOG BLOWER WITH OVERH AULED UNIT IAW CE-560 MM CH 21-21-01. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2007102300148 20071023 00148 CE 2007 10 23 DXTA200702540 1 20071014 A 3230 LANDING GEAR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LEFT MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 651QS 5605251 LT LANDING GEAR INDICATOR LIGHT REMAINED ON WHEN GEAR RETRACTED. CYCLED GEAR WITH THE SAME RESULT AND UNABLE TO VERIFY G EAR UP OR DOWN. PERFORMED EMERGENCY GEAR BLOW DOWN PROCEDURE AS PRECAUTION. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007102300152 20071023 00152 SO 2007 10 23 N93A10102007 1 20071010 A 3250 1206P0153 PRESSURE SWITCH GULSTM GIV GIVG400 3980204 SO RROYCE TAY TAY6118 EU NLG STEERING UNKNOWN E N93A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 13 413QS 1521 AFTER TAKEOFF, STEER BY WIRE FAIL LIGHT, ILLUMINATED THEN WENT OUT AFTER 5 MINUTES 2 L 7 2 4F 4 F RT A12EA E25NE 2007102300176 20071023 00176 NM 2007 10 23 AMTA200700497 1 20071013 A 5321 FLOOR PANEL BOEING 737 73783N 13844HI NM BS 777-887 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 308TZ 28244 AFT CARGO FLOOR PANEL 140CF HAS CORROSION AROUND EDGES OF UPPER SURFACE. FABRICATED AFT CARGO FLOOR PANEL 140CF ALODINE D AND PRIMED IAW SRM 53-60-53, SRM 51-20-01-06. (K) 2 L 7 2 4F RT A16WE 2007102300179 20071023 00179 NM 2007 10 23 AMTA200700498 1 20071013 A 5321 FLOOR PANEL BOEING 737 73783N 13844HI NM BS 727-727D CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 308TZ 28244 AFT CARGO PNL 140AF HAS CORROSION AROUND EDGES UPPER SURFACE STA 727+4 - 727D, LBL 25- 25 RBL. FABRICATED AFT CARGO FLO OR PNL 140AF ALODINED AND PRIMED, IAW SRM 53-60-53-0I, SRM 51-20-01-0G. (K) 2 L 7 2 4F RT A16WE 2007102300188 20071023 00188 NM 2007 10 23 AMTA200700504 1 20071013 A 4900 UNKNOWN BOEING 737 73783N 13844HI NM APU UNKNOWN A AMTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 11 305TZ 30706 APU WOULD NOT POWER LEFT A/C BUSS. (K) 10-26-07 REMOVED AND REPLACED MODULE IAW AMM 24-21-51-4, OPS CHECK NORMAL PER AMM 24-21-00-5. (M) 2 L 7 2 4F RT A16WE 2007102300190 20071023 00190 2007 10 23 AMTA200700505 4 20071014 A 3460 COMPUTER BOEING 737 73783N 13844HI NM FLT MANAGE FAULTED A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 323TZ 30033 SINGLE FMC OPERATION FMC MESSAGE. F/O MAP DISPLAY HAS MAP AND VTK YELLOW BOX. SWAPPED FMC`S FOR T/S, NO FAULTS FOUND A FTER SWAP. OPS CHECK GOOD IAW AMM 34-61-00-5. PN 176200-01-01. (K) 2 L 7 2 4F RT A16WE 2007102300201 20071023 00201 2007 10 23 SWAA075119 4 20071018 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR UNWANTED DEPLOY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED RON CHECK, L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM . 2 L 7 2 4F RT A16WE 2007102300215 20071023 00215 NM 2007 10 23 SWAA075139 1 20071018 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 27L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007102300216 20071023 00216 NM 2007 10 23 SWAA075118 1 20071018 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 906, STR 4L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007102300228 20071023 00228 NM 2007 10 23 SWAA075130 1 20071018 A 2560 PH22300L GLOWSTRIP BOEING 737 7375H4 138449D NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 4 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007102300230 20071023 00230 NM 2007 10 23 EIA2007160 1 20070914 A 5311 65B018532 FRAME BOEING 747 747212B 1384886 NM BS 670 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 FWD PIT DOOR CUT OUT, AFT LOWER SIDE, FRAME WEB HAS DRILL STARTS, NEXT TO ATTACH LOCATIONS, FOUND UPON REMOVAL OF SEAL D EPRESSOR FOR REPAIR. REPAIRED DAMAGED AREA ON WEB AT FWD PIT DOOR CUT OUT AFT LOWER SIDE PER ECRA 3 486-53-063-2. 2 L 7 4 4F A20WE 2007102300232 20071023 00232 CE 2007 10 23 16SU10 1 20071015 A 7797 9914303 CONNECTOR CESSNA 650 650 2076802 CE ITT CORRODED E DBCA K NONE O OTHER AP APPROACH 1 GL 13 16SU 6500025 ON APPROACH TO BED THE RIGHT ITT INDICATOR TAPE STARTED FLUCTUATING. ALL OTHER ENGINE INDICATIONS WERE NORMAL. AIRCRAF T LANDED AT BED. LANDING WAS UNEVENTFUL. TROUBLESHOT AND FOUND ITT CONNECTOR IN ENGINE PYLON HAD LITE CORROSION. CLEA NED AND RESECURED CONNECTOR. OPERATIONS CHECKED GOOD. 2 L 7 2 4F A9NM 2007102300237 20071023 00237 NM 2007 10 23 USAA920070955 1 20071013 A 5320 141N516078 CHANNEL BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 903AW 23323 MCN - MAJOR REPAIR - C-12 CHECK - CORROSION ON THE R1 DOOR CUTOUT CHANNEL, BS 350, RBL 60, WL 208. REPLACED THE R1 DOOR CUTOUT CHANNEL, BS 345 - BS 365.25 , RBL 60, WL 208 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007102300238 20071023 00238 NM 2007 10 23 EIA2007167 1 20070914 A 5311 65B018552 FRAME BOEING 747 747212B 1384886 NM BS 1810 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 AFT PIT BOOR CUT OUT FWD LOWER SIDE FRAME WEB AND SKIN CUT. FOUND UPON REMOVAL OF SEAL DEPRESSOR FOR REPAIR. REPAIRED PER ECRA NR 486-53-064-2. 2 L 7 4 4F A20WE 2007102300242 20071023 00242 NM 2007 10 23 USAA920070957 1 20071014 A 5320 143N536654 PANEL BOEING 757 7572S7 1384962 NM CARGO BAY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 903AW 23323 MCN - MAJOR REPAIR - C-12 CHECK - CORROSION ON FORWARD CARGO COMPARTMENT DOOR CUTOUT LOWER SILL PANEL, BS 560 - BS 620, S26R. REPLACED FORWARD CARGO COMPARTMENT DOOR CUTOUT LOWER SILL PANEL, BS 560 - BS 620, S26R IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007102300243 20071023 00243 EU 2007 10 23 USAA920070958 1 20071008 A 5751 D57640003200 SPAR AIRBUS 320 A320231 3930325 EU LOT AILERON DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 636AW 098 SAL - MAJOR REPAIR - C-5 CHECK - LEFT AILERON LEADING EDGE SPAR IS DELAMINATED, WS 13464 - WS 14057. REPAIRED LEFT AIL ERON LEADING EDGE SPAR, WS 13464 - WS 14057 IAW USAIRWAYS EA 120326A. 2 L 7 2 4F RT A28NM 2007102300247 20071023 00247 NM 2007 10 23 HNAA0700243 1 20071018 A 5730 85711802005 PANEL DHAV DHC8 DHC8102 2809003 NM LT WING CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 828EX 392 THE LEFT HAND WING PANEL 522AT WAS FOUND TO HAVE PITTING DAMAGE FROM CORROSION. REPLACED THE PANEL WITH A NEW PART FRO M STORES. 2 H 7 2 4T RT A13NM 2007102300250 20071023 00250 NM 2007 10 23 UPS07550963 1 20071020 A 2560 HOLDER BOEING 757 75724APF 1384969 NM COCKPIT DETACHED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 402UP 23724 INSPECTION TYPE:N/A EMERGENCY DESCENT ESCAPE DEVICE CABLE HOLDERS DETACHED FROM CEILING ABOVE SUPERNUMERARY SEATS. SECU RED MOLDING TO CEILING WITH STRUCTURE 1 ADHESIVE PER B757 SRM CHAPTER 51-00 OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2007102300259 20071023 00259 2007 10 23 2007UALA04130 4 20071005 A 2210 SENSOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU ELEVATOR OUT OF ADJUST A UALA O OTHER F FLT CONT AFFECTED CL CLIMB 1 WP 29 340UA 24244 IN CLIMBING FLT ACFT PITCHES DOWN AGGRESSIVELY WHEN A OR B A-P SELECTED IN ANY MODE, CLIMB, CRUISE. FOUND ELEVATOR NEUT RAL SHIFT SENSOR MIS-ADJUSTED. ADJUSTED NEUTRAL SHIFT SENSOR. ACCOMPLISHED DFCS BITE. NO FAULTS FOUND. ACFT OK FOR CAT I II. 2 L 7 2 4F 4 F RT A16WE E21EU 2007102300260 20071023 00260 NM 2007 10 23 2007UALA04131 1 20071007 A 2750 01812996 INDICATOR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 935UA 26663 FLAP SPLIT INDICATED BY .5 NEEDLE WIDTH. NO ROLL TENDENCY. EACH TIME LOOKS LIKE RIGHT NEEDLE LAGGED BY .5 NEEDLE WIDTH AND THEN CATCHES UP WITH LEFT NEEDLE. CYCLED FLAP POSITION INDICATOR C-B AND DID GET NEEDLES TO PAIR UP. SUSPECT POSI TION INDICATOR FAULTY. REPLACED FLAP POSITION INDICATOR ACCOMPLISHED OPERATIONAL CHECK OF FLAP POSITION INDICATOR. IND ICATOR OPERATES NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007102300261 20071023 00261 NM 2007 10 23 2007UALA04132 1 20071007 A 2130 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN PRESSURE MALFUNCTIONED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 314UA 23675 AUTO FAIL LIGHT AND LOST CABIN PRESSURE AT 4000 FEET. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110700009 20071107 00009 EU 2007 11 7 07FDEA04687 1 20071025 A 5320 A5361164422000 FLOOR SUPPORT AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 INTERGRANULAR CORROSION ON TOP OF MAIN CABIN FLOORBEAM AND AROUND FLOOR PANEL HOLES, LONGITUDINAL FLOORBEAM UNDER LT FWD LAV MARKED. REMOVED CORROSION IAW A310 SRM 51-74-10. ORIGINAL THICKNESS .079, REMOVED .040, .039 REMAINING. MATERIAL LOSS BEYOND ALLOWABLE LIMITS IAW A310 SRM 53-10-00. UT GAUGE NR T82530. REMOVED CORRODED BEAM IAW A310 SRM 51-40-21. LOCATED AND DRILLED HOLES IN NEW BEAM IAW A310 SRM 51-40-44, PART NR 5361164422000 PO 593006.1. INSTALLED NEW BEAM I AW A310 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007102300294 20071023 00294 NM 2007 10 23 2007UALA03870 1 20070923 A 2612 586557331 INDICATOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FIRE WARNING FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 215UA 30221 BOTTLE DISCHARGE LIGHT AND FIRE BOTTLE ARMED LIGHT ON NOSE GEAR APU GROUND CONTROL PANEL WILL NOT PRESS TO TEST. RELAMP ED BOTTLE DISCHARGE LIGHT, NO HELP. REPLACED FIRE BOTTLE ARMED LIGHT INDICATOR. OP CHECKS OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007102300297 20071023 00297 NM 2007 10 23 2007UALA03884 1 20070924 A 2497 W20400210 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 IDG CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 NR 2 ENG IDG POWER FEED WIRES OUTER INSULATION IS CRACKED IN A FEW AREAS. REPAIRED NR 2 ENG IDG POWER FEEDER CABLES AT CRACKED AREAS IAW GNMM 2-0-15-1. INSP BY QC INSPECTOR AND RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102300310 20071023 00310 NM 2007 10 23 2007UALA04160 1 20071010 A 2621 EXTINGUISHER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RT WING LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 127UA 28813 RT WING "B" EXTINGUISHER BOTTLE LOW PRESS LIGHT ON, VERIFIED BOTTLE LOW. REPLACED "B" EXTINGUISHER BOTTLE (RT WING) AND RELATED SQUIBS. REF. MM 26-21-03 AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102300314 20071023 00314 NM 2007 10 23 2007UALA04164 1 20071009 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 776UA 26937 DOOR 4R EMERGENCY LIGHT IS INOP. 11-01-07 RELAMPED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007102300322 20071023 00322 NM 2007 10 23 2007UALA04172 1 20071010 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN SMOKE A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 29 508UA 24744 SMOKE IN CABIN ON TAKEOFF ROLL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007102400001 20071024 00001 NM 2007 10 24 EIA2007172 1 20070925 A 5755 SUPPORT FITTING BOEING 747 747132 1384882 NM NR 6 SPOILER CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 476EV 19898 LT WING NR 6 SPOILER HINGE SUPPORT FITTING I/B AND O/B LOWER FLANGE CRACKED. NR 6 SPOILER HINGE SUPPORT FITTING I/B ANS O/B LOWER FLANGE REPAIRED PER EN-EA-57-0590. 2 L 7 4 4F A20WE 2007102400002 20071024 00002 NM 2007 10 24 EIA2007176 1 20070912 A 5311 FRAME BOEING 747 747132 1384882 NM BS 840 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 UPPER DECK BS 840 RT FRAME FOUND CRACKED AT TENSION TIE JOINT AREA. UPPER DECK BS 840 RT FRAME REPAIRED PER SRM 53-10-0 4 FIG 133. 2 L 7 4 4F A20WE 2007102400005 20071024 00005 NM 2007 10 24 EIA2007155 1 20070909 A 3350 S135610A BATTERY PACK BOEING 747 747212B 1384886 NM EMERGENCY LIGHTS INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 485EV 20712 AFT CABIN CEILING EMERGENCY LIGHT OUT. REMOVED AND REPLACED BATTERY PACK PER B747MM 33-51-04, TEST GOOD PER MM 33-51-04 . 2 L 7 4 4F A20WE 2007102400009 20071024 00009 NM 2007 10 24 EIA2007185 1 20070924 A 5311 FRAME BOEING 747 747132 1384882 NM BS 880 S37-38L CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 FORWARD CARGO PIT LT SIDE BS 880 STR 37-38 FRAME WEB CRACKED. TRIMMED OUT DAMAGE, FABBED AND INSTALLED REPAIR PER ES-53 -1150, B747 SRM 51-30-05 AND 51-30-08. 2 L 7 4 4F A20WE 2007102400022 20071024 00022 EU 2007 10 24 07FDEA04587 1 20071015 A 5730 A57246666 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 729FD 657 FOUND OLD REPAIR ON RT INNER DEFLECTOR DOOR 672CB NOT CONFORM TO SRM REPAIR RENEWED IAW SRM 51-77-12 PARA 3C WITH DEVIAT IONS, APPROVED BY EA 6-5755-114909 AND RAS/BAE/1005629/2007. 2 L 7 2 4F RT A35EU 2007102400043 20071024 00043 NM 2007 10 24 DL764071338 1 20071012 A 3520 RELAY BOEING 767 767432ER 1385134 NM OXYGENY SYSTEM FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 833MH 29706 OXYGEN SYSTEM FAILS AUTO DEPLOYMENT, REMOVED AND REPLACED K455 OXYGEN CONT TIME DELAY RELAY IAW WDM 25-21-11 AMM B767. OPS CHECKS GOOD IAW AMM B767 35-21-00. 2 L 7 2 4F RT A1NM 2007102400052 20071024 00052 NM 2007 10 24 DL764071347 1 20071013 A 3350 Q LIGHT BOEING 767 767432ER 1385134 NM R/H MID GALLEY INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 833MH 29706 FOUND EMERGENCY LIGHTS IN RT MID GALLEY INOP. RELAMCPED AND OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2007102400056 20071024 00056 NM 2007 10 24 DL76G071356 1 20071013 A 4910 SWITCH BOEING 767 767332 1382001 NM APU DOORS UNKNOWN A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 171DZ 29690 APU DOOR STATUS MSG COMES ON. AFTER APU SHUTDOWN. FWD TO MCO AND PLACARD APU DOOR STATUS MSG APU DOOR OPS NORM INDICAT ION IS INOP PER MEL 49-15-01B. 2 L 7 2 4F RT A1NM 2007102400058 20071024 00058 SO 2007 10 24 SWIA200718775 1 20071013 A 5210 STOP EMB 120 EMB120ER 3260203 SO PAX DOOR OUT OF ADJUST A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 236SW 120312 FLT 5774 - MAIN CABIN DOOR IS DIFFICULT TO OPEN. ADJUSTED MAIN CABIN DOOR BACKSTOPS IAW MM 52-11-00. 2 L 7 2 4T RT A31SO 2007102400081 20071024 00081 EU 2007 10 24 AALA20071931 1 20071003 A 5610 WINDSHIELD AIRBUS 300 A300B4605R 3930308 EU COCKPIT CRACKED A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 80084 675 MIA INFLIGHT T917/03OCT - FIRST OFFICERS WINDSHIELD CRACKED CLIMBING OUT OF MIA. RETURNED TO MIA AND LANDED WITHOUT INC IDENT. REPLACED FIRST OFFICERS WINDSHIELD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007102400085 20071024 00085 EU 2007 10 24 MALA070163 1 20070902 A 5753 SKIN SAAB SF340 340B 7860101 EU TE FLAP DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 340B424 REMOVED RT FLAP FOR FOM FOR REPAIRS TO LOWER SIDE FOR EO NR S57154. REPAIRED FLAP SKIN DAMAGE PER EO NR S57154. INSTAL LED SERVICEABLE FLAP ASSEMBLY PN ON/OFF: 7257800-574; SN OFF: 1315, SN ON: 1307, IAW AMM 27-53-10. 2 L 7 2 4T RT A52EU 2007102400089 20071024 00089 2007 10 24 F3LA200700282 4 20071012 A 2565 LANYARD AIRBUS A319 A319111 3930336 NM ESCAPE SLIDE MISSING A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 945FR 2751 DURING C-1 CHECK, INSPECTION REPORTED LT OVERWING EMERGENCY ESCAPE SLIDE LOWER ACTUATING CABLE WAS MISSING THE LOWER END PIECE TO ATTACH TO THE SLIDE RELEASE BOTTLE/TEST FIXTURE. REMOVED, REPLACED AND OPS CHECKED LT OVERWING EMERGENCY ESCA PE SLIDE LOWER ACTUATING CABLE IAW AMM 25-62-43-000-001, 25-62-43-400-001, 52-21-00, PB 501, AND TASK CARD 528001-11. 2 L 7 2 4F RT A28NM 2007102400095 20071024 00095 WP 2007 10 24 07FDEA04616 1 20071017 A 5522 ALC7390 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 RT INBD ELEVATOR LWR SURFACE FOUND SEVERE CORROSION ON SKIN AND SUSPECT CORROSION UNDER SKIN. REPAIRED AREA IAW SRM 55- 10-00 FIG 7 VOL I. 2 L 7 3 4F A22WE 2007102400101 20071024 00101 WP 2007 10 24 07FDEA04625 1 20071017 A 5320 NDA6034 SILL DOUG DC10 DC1010F 3022111 WP BS 879-886 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 FWD CARGO COMPT FOUND CORROSION WITH EXFOLIATION ON FITTING SILL DOOR INSIDE JAMB FWD. 2 L 7 3 4F A22WE 2007102400102 20071024 00102 WP 2007 10 24 07FDEA04627 1 20071017 A 5313 AFA3280501 LONGERON DOUG DC10 DC1010F 3022111 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 CTR CARGO COMPT CRACK ON LONGERON. REPAIRED LONGERON IAW SRM 53-10-00 FIG 1-2 VOL I. 2 L 7 3 4F A22WE 2007102400106 20071024 00106 NM 2007 10 24 07FDEA04631 1 20071017 A 5320 651759369 FLOOR SUPPORT BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 MAIN CABIN, FS 312 TO 328, LBL 30 FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT REF DWG 65-17593 AND SRM SRM 51-30-02 PG 1. 2 L 7 3 4F RT A3WE 2007102400112 20071024 00112 2007 10 24 QXEA200701570 4 20071016 A 3160 DISPLAY BOMBDR DHC8 DHC8402 1390042 NM COCKPIT MALFUNCTIONED A QXEA O OTHER O OTHER CR CRUISE 1 NM 09 406QX 4048 ED SCREEN WORKS BUT NUMERICAL INFORMATION DISAPPEARED. CYCLED ED SCREEN OFF THEN AS PER CHECKLIST, APPEARED TO WORK. M AINTENANCE INSPECTED ED CONNECTORS FOR SECURITY. PERFORMED ED OPS TEST IAW Q400 AMM TASK 31-61-00-710-801 AND OP TESTS IAW TC 6314101. ALL TEST GOOD. AIRCRAFT AND PLACARD REFLECT CAT I DUE TO HGS FAILURE. NO PARTS REPLACED. AIRCRAFT RE TURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102400120 20071024 00120 NM 2007 10 24 TSAA0777056 1 20071015 A 7797 CONNECTOR BOEING 737 7372P6 1C84609 NM EPR INDICATOR MISINSTALLED A TSAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 13 835AL 21613 NON-ETOPS FLIGHT 278 HNL-KOA, ON TAKEOFF AFTER THROTTLE ADVANCE, THE CREW NOTED THE NR 1 EPR AT 2.22 AND THE NR 2 EPR AT 1.74. THE CREW ABORTED THE TAKEOFF AT 100 KTS INDICATED AIRSPEED. THE CREW RETURNED TO THE GATE WITHOUT FURTHER INCID ENT. MAINTENANCE FOUND BOTH EPR CONNECTOR IMPROPERLY CONFIGURED. MAINTENANCE REINSTALLED BOTH EPR CONNECTORS. AN OPER TIONAL CHECK OF ENGINE INDICATING WAS COMPLETED DURING A FLIGHT TEST 27OCT07. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007102400135 20071024 00135 WP 2007 10 24 07FDEA04623 1 20071017 A 5347 607158 SEAT TRACK DOUG DC10 DC1030F 3023504 WP BS 615-635 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 320FE 47835 MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREAS AT F/S 615-635 RBL 8. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 VOL 1 FIG 5. 2 L 7 3 4F RT A22WE 2007102400149 20071024 00149 NM 2007 10 24 07FDEA04648 1 20071018 A 5310 65C80678107 RETAINER BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 RT FWD OVERWING DOOR FRAME, PRESSURE SEAL ATTACH ANGLE IS CRACKED/CORRODED ON ALL FOUR SIDES AS MARKED REMOVED UPPER AND LOWER SEAL ATTACH ANGLES. INSTALLED 2 NEW ANGLE TO DOOR FRAME REF 51-30-02. REPAIR IS CLASSIFIED AS A MINOR. 2 L 7 3 4F RT A3WE 2007102400152 20071024 00152 NE 2007 10 24 ARWA20071002 2 20071018 A 7200 CF650C2 ENGINE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 VIBRATION A ARWA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SO 19 524MD 75275 1662 46999 455130 DURING CLIMB-OUT, NR 3 ENGINE HEAVY VIBRATION. TROUBLESHOT NR 3 ENGINE PER TAFI 72-00-00; FOUND VIBRATION AT FUEL LEVER AND THROTTLE, OUT OF ADJUSTMENT. ADJUSTED FUEL LEVER PER DC-10 M/M 76-12-00 AND THROTTLE PER DC-10 M/M 76-11-00. OPER ATIONAL CHECK NORMAL ON ENGINE RUN-UP PER DC-10 M/M 71-00-00. A/C OK FOR SERVICE. 2 L 7 3 4F 4 F A22WE E23EA 2007102400153 20071024 00153 WP 2007 10 24 Y2PA200700025 1 20070924 A 5311 9911505567 FRAME DOUG DC9 DC931 3022065 WP BS 73 CRACKED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 231US 48114 DURING INSPECTION TO COMPLY WITH AD 2002-21-09 AND S/B 53-290 NOSE SKIN, STA 73, LBL 10, P/N 5911403-3 FOUND CRACKS ON T HE AFFECTED FRAMES, P/N 9911505-5/-6/-7. THE -7 FRAME WAS CRACKED 0.0625 INCHES BEYOND THE 1.125 INCH LIMIT. THE MOD R EQUIRED BY S/B 53-290 AND SR09530268-7013 COCKPIT REPAIR, FRONT WINDOW LOWER SILL SURROUND WAS ACCOMPLISHED. AIRCRAFT W AS RETURNED TO SERVICE AT THE COMPILATION OF MOD. 2 L 7 2 4F A6WE 2007102400156 20071024 00156 WP 2007 10 24 07FDEA04649 1 20071019 A 5311 ABA73483 FRAME DOUG DC10 DC1030F 3023504 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 FWD AVIONICS COMPT ON FRAME FOUND CRACK. 2 L 7 3 4F RT A22WE 2007102400157 20071024 00157 NM 2007 10 24 07FDEA04650 1 20071019 A 5315 651627910 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 SEVERAL LOCATIONS OF CORROSION ON FLOORBEAM FROM FS 760 TO 840, RBL 45.5. REMOVED FLOORBEAM STA 760 - 840, RBL 45.5. F ABRICATED AND INSTALLED REPLACEMENT FLOORBEAM IAW DWG 65-16279 AND SRM 51-30-02 P1. THIS IS CLASSIFIED AS A MAJOR REPA IR. 2 L 7 3 4F RT A3WE 2007102400158 20071024 00158 NM 2007 10 24 07FDEA04651 1 20071019 A 5330 655457211 SKIN BOEING 727 727233 138408A NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 LOWER FORWARD PIT DOOR CUTOUT FORWARD SIDE FUSELAGE SKIN DENTED MEASURE DENT A=2" Y= .073" A/Y= 13.69 DENT WAS OUT OF LI MITS. TRIMMED OUT DENT. REMOVED .310" MATERIAL. REPAIR IS WITHIN LIMITS REF EA 7-5330-113955. USED TOOL IN17-0023 CA L DUE 12-13-08 TO MEASURE DENT. REF SRM 51-30-1 PG 2A. THIS IS A TIME LIMITED REPAIR LIMITED TO 24 MONTHS OR 3000 FLIG HT CYCLES WHICH EVER OCCURS FIRST. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007102400159 20071024 00159 WP 2007 10 24 07FDEA04652 1 20071019 A 5311 ACA00533 FRAME DOUG DC10 DC1030F 3023504 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 AIR CONDITIONING COMPT RT SIDE ON FRAME JAMB DOOR FOUND CRACK. 2 L 7 3 4F RT A22WE 2007102400161 20071024 00161 NM 2007 10 24 07FDEA04654 1 20071019 A 5320 657517215 FLOOR SUPPORT BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 LOWER FOWARD PIT, STATION 680, FRAME AFT SIDE, RBL 13, BETWEEN STRINGERS 27R AND 28R, FRAME TO FLOOR SUPPORT STRUCTURE A NGLE GOUGE/CRACKED IN RADIUS. REMOVED CRACKED FLOOR SUPPORT CLIP. FABBED NEW CLIP AND DRILLED REF BOEING DWG 65-75172. 2 L 7 3 4F RT A3WE 2007102400164 20071024 00164 NM 2007 10 24 AALA20071942 1 20071015 A 2761 332148016 ACTUATOR BOEING 757 757223 1384957 NM SPOILERS INOPERATIVE A AALA O OTHER J WARNING INDICATION DE DESCENT 1 SW 21 692AA 26972 HNL INFLIGHT T297 - SPOILER LIGHT ILLUMINATED ON EICAS AND OVERHEAD WARNING PANEL. LANDED HNL WITHOUT INCIDENT. REPLAC ED POWER CONTROL ACTUATOR NUMBER 6. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007102400165 20071024 00165 NE 2007 10 24 AALA20071940 2 20071015 A 7230 BLADES DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT ENGINE DAMAGED A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 965TW 53615 709873 DFW INFLIGHT T1157/15OCT - RIGHT ENGINE PRESSURE RATIO FLUCTUATION AND VIBRATION ON TAKEOFF ROLL ENGINE COMPRESSORS STAL LED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE ON 16 OCT 2007 AT DFW DUE TO FAN FOD DAMA GE DURING TAKEOFF. FAN BLADE BENT FORWARD AND SOME REPORTS STATE BIRD FOD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A6WE E9NE 2007102400166 20071024 00166 NM 2007 10 24 AALA20071943 1 20071016 A 3350 PBS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 391AA 27451 ORD - EMERGENCY LIGHTS AT LEFT AND RIGHT NUMBER ONE EXIT DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT AND RIGHT NUMBER ONE EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007102400169 20071024 00169 2007 10 24 AALA20071947 2 20071016 A 7321 ECU BOEING 757 757223 1384957 NM LT ENGINE INOPERATIVE A AALA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SW 21 634AA 24592 MIA INFLIGHT T1047/16OCT - NUMBER ONE ENGINE GENERATOR FAILED AND CREW WAS UNABLE TO ESTABLISH POWER WITH AUXILLIARY POW ER UNIT (APU). LANDED MIA WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE ELECTRONIC CONTROL UNIT AND SERVICED INTEGRATED DRIVE GENERATOR. PLACARDED APU. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007102400170 20071024 00170 NM 2007 10 24 AALA20071946 1 20071016 A 3350 SIGN BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 681AA 25338 DFW - EMERGENCY LIGHT PLACARD AT AFT RIGHT OVERWING EXIT DOOR DAMAGED. REPLACED PLACARD FOR EMERGENCY LIGHT AT AFT RIGH T OVERWING EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007102400173 20071024 00173 EA 2007 10 24 QXEA200701576 1 20071018 A 3240 BRAKE ASSY CNDAIR CL600 CL6002C10 1390015 EA MLG LEAKING A QXEA O OTHER K G J FLUID LOSS MULTIPLE FAILURE WARNING INDICATION LD LANDING 1 NM 09 617QX 10130 FAT- FLIGHT 2531 - DURING LANDING ROLL OUT, THE RIGHT BRAKES DID NOT WORK. DURING TAXI IN, THE BRAKE TEMPERATURE INDICA TED ZERO FOR THE RIGHT BRAKES. AFTER PARKING POST FLIGHT INSPECTION SHOWED FLUID LEAK FROM THE RIGHT BRAKE ASSEMBLY. M AINTENANCE FOUND NR 3 AND NR 4 BRAKE LINES NOT SECURED. RESECURED QUICK DISCONNECT FITTINGS AND PERFORMED A OPERATIONAL TEST OF THE BRAKE SYSTEM IAW AMM 32-43-00-710-801-A01. FLIGHT CREW TAXIED AIRCRAFT TO VERIFY BRAKE FUNCTION. ALL CHEC KS GOOD WITH NO DEFECTS NOTED. ALSO CHECKED NR 1 AND NR 2 BRAKE DISCONNECTS, AND THERE WERE NO DEFECTS NOTED. NO LEAKS NOTED AND HYDRAULIC LEVELS WITHIN LIMITS. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007102400174 20071024 00174 NM 2007 10 24 P5CA0701537 1 20071016 A 5340 ATTACH ANGLE BOEING 747 74746NF 13848BT NM CARGO DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 453PA 30811 DAMAGE WAS FOUND ON THE MAIN DECK SIDE CARGO DOOR BS 1920 SEAL DEPRESSOR AND ATTACH ANGLE. CRACKS WERE FOUND ON SAID ITE MS AT APPROXIMATELY 24" FROM LOWER AFT CORNER. INTERIM REPAIR ACCOMPLISHED AS PER PART 1 OF MA A4 5300-09-00:00 FAA 811 0-3. 2 L 7 4 4F RT A20WE 2007102400175 20071024 00175 NM 2007 10 24 UIEA200700458 1 20071018 A 5753 STRUCTURE BOEING 747 74747UF 1384812 NM TE FLAP DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 412 30559 DAMAGE WAS FOUND TO THE I/B END OF THE LT O/B MID FLAP. THE DAMAGE IS DUE TO CONTACT OF THE MID FLAP WITH THE FIXED STR UCTURE ADJACENT TO THE I/B AILERON. REPAIRED IAW XEO 57-101507-1. 2 L 7 4 4F RT A20WE 2007102400177 20071024 00177 NM 2007 10 24 L43A102207001 1 20071018 A 2750 285T004953 FSEU BOEING 767 767205 1385121 NM PWA JT9 JT9D7R4D 52054 NE TE FLAPS FAULTED A L43A A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 27 260MY 23057 AFTER TAKEOFF WHEN MLG SELECTED UP & MLG DOOR LIGHTS EXTINGUISHED A "GEAR NOT DOWN" EICAS MESSAGE DISPLAYED. AS FLAPS S ELECTED FROM 5 TO 1 DEGREE A "T/E FLAP DISAGREE" MESSAGE DISPLAYED. ALTERNATE T/E SWITCH CYCLED & AS FLAPS WENT TO 1 D EGREE "T/E FLAP DISAGREE" MESSAGE EXTINGUISHED. FLAPS SELECTED TO 0 DEGREES & "L/E SLAT ASYM" EICAS MESSAGE DISPLAYED. FLAP INDICATOR NEVER MOVED FROM 1 DEGREE POSITION. CREW THEN CONTACTED DISPATCH ADVISING OF THE PROBLEM AND MADE THE D ECISION TO RETURN TO JFK. THE FLAP HANDLE WAS THEN RETURNED TO THE 1 DEGREE POSITION AND THE "L/E SLAT ASYM" EICAS MESS AGE EXTINGUISHED AND THEN POSITIONED BACK TO THE 0 DEGREE PROSTITUTION AT WHICH POINT THE MESSAGE RETURNED. THE LANDING 2 L 7 2 4F 4 F RT A1NM E3NE 2007102400179 20071024 00179 NM 2007 10 24 NWAA073506303 1 20071014 A 5753 WEB BOEING 747 747451 1384940 NM TE FLAPS CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 663US 23818 DURING "L" CHECK, FOUND CRACK IN LT WING INBOARD TRAILING EDGE FORE FLAP OUTBOARD WEB ASSEMBLY AT WBL 442.0. REPAIRED P ER EA 63-210880. 2 L 7 4 4F RT A20WE 2007102400182 20071024 00182 NM 2007 10 24 QXEA200701581 1 20071020 A 3097 697071272 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM PROP DEICE DAMAGED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 403QX 4037 SEA FLIGHT NR 2486: THE CAPTAIN'S SIDE PROP DEICE WAS CAUSING THE PROP DEICE CAUTION LIGHT TO ILLUMINATE. AIRCRAFT RETU RNED TO FIELD. MAINTENANCE REMOVED AND REPLACED NR 6 PROP DEICE WIRE HARNESS IAW Q400 AMM 61-10-06-400-805. PERFORMED FUNCTIONAL TEST OF PROP DEICE SYSTEM IAW Q400 AMM 30-61-00-720-801. OPS CHECK GOOD WITH NO FURTHER DEFECTS NOTED. AIRC RAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102400183 20071024 00183 SO 2007 10 24 SIMA200728901 1 20071014 A 3320 7277226501 PSU EMB 135 EMB135KL 3260302 SO CABIN LIGHTS ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 853AE 145742 PASSENGER SERVICE UNIT LIGHTS FLICKERED DURING TAXI FOLLOWED BY ELECTRICAL ODOR IN CABIN AND COCKPIT. REMOVED AND REPLA CED PASSENGER SERVICE UNIT ASSY PER AMM 25-22-05. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007102400186 20071024 00186 2007 10 24 SIMA200729307 4 20071018 A 3442 7021450601 COMPUTER EMB 135 EMB135KL 3260302 SO WX RADAR SYS FAILED A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 801AE 145469 NOTIFIED BY THE FLT CREW, RADAR FAILED CODE: 11 POC O MAGNETRON. CAPTAIN ELECTED TO DIVERT TO CMH DUE TO WEATHER CONDIT IONS. REMOVED AND REPLACED RTU IAW EMB AMM 34-42-01 AND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007102400200 20071024 00200 NM 2007 10 24 07FDEA04655 1 20071021 A 5620 6561611 WINDOW BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 RT WINDOW PLUG AT BS 950 PLUS 10" AND 1020 HAVE CORROSION ON EXT SURFACE. REMOVED AND REPLACED WINDOW PLUGS AT BS 950 P LUS 10" AND 1020 RT SIDE INSTALLED BONDING STRAP (GROUND), PAINTED NEW PLUGS REF MM 56-20-004, SOPM 20-41-02, SWPM 20-20 -00 PG4-8. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007102400201 20071024 00201 EU 2007 10 24 07FDEA04656 1 20071021 A 5340 A53070037201 FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 RIGHT SIDE CRACK INDICATION IN FR43A LOWER HOLE AT APPROX 12 O'CLOCK AND 6 O'CLOCK IN FRAME FITTING ONLY REMOVED LOWER FRAME FITTING AT FR 43A, THAT IS CRACKED. INSTALLED NEW FITTING IAW A31 SRM 51-40-21 PG 24 AND 51-40-40 PG 17. 2 L 7 2 4F RT A35EU 2007102400205 20071024 00205 WP 2007 10 24 07FDEA04660 1 20071022 A 5312 NCA624627 BULKHEAD DOUG DC10 DC1030F 3023504 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 AIR CONDITIONING COMPT LT SIDE ON VERTICAL BHD FOUND CRACK. 2 L 7 3 4F RT A22WE 2007102400206 20071024 00206 EU 2007 10 24 07FDEA04661 1 20071022 A 5310 A53970875 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU ZONE 200 SCRATCHED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 729FD 657 FOUND SCRUB MARKS ON CROSS SHEET C55-57.1, LT AND RT REPAIR PERFORMED BY REWORK OF DAMAGED AREA, NDT FOR CRACK FREE IAW EA 6-5316-114890 AND RAS /DATLS/0003844/2007 ISS A. 2 L 7 2 4F RT A35EU 2007102400207 20071024 00207 EU 2007 10 24 MALA070164 1 20071021 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E BAY MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 437XJ 340B437 AVIONICS SMOKE LIGHT ILLUMINATED IN FLIGHT AND CAPTAIN DIVERTED TO MTC. SMOKE DETECTOR WAS SUBSEQUENTLY DEFERRED, MORE INFORMATION WILL BE ADDED TO THIS REPORT UPON COMPLETION OF MX. 2 L 7 2 4T RT A52EU 2007102400208 20071024 00208 EU 2007 10 24 NWAA073533301 1 20071017 A 5712 RIB AIRBUS 330 A330323 3930335 EU WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 801NW 0524 DURING INSPECTION PER AD 2006-22-14, FOUND CRACK IN AFT TOP FASTENER HOLE OF WING RIB 6. REPAIRED PER EA 33-210974. 2 L 7 2 4F RT A46NM 2007102400211 20071024 00211 NM 2007 10 24 070167 1 20071014 A 5330 SKIN DOUG MD80 MD83 3023681 NM BS 229-275 PUNCTURED A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 892GA 49826 ON THE GROUND IN CHA, AIRCRAFT OUTER SKIN WAS PUNCTURED BY BELT LOADER. ACCOMPLISHED TEMPORARY REPAIR TO DAMAGED FUSELA GE BETWEEN STA 229 AND STA 275 IN ACCORDANCE WITH ERO 5330-002. AIRCRAFT FERRIED TO TUL FOR PERMENANT REPAIR. OPEN ITE M 2 L 7 2 4F RT 2007102400212 20071024 00212 2007 10 24 070168 2 20071018 A 7261 7838314501 HOSE DOUG DC9 DC983 3022083 WP ENGINE OIL RUPTURED A WX0A E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 19 863GA 49911 RIGHT ENGINE INDICATED A LOSS OF OIL PRESSURE AND FLIGHT CREW PERFORMED QRH PROCEDURE TO SHUT DOWN THE RIGHT IN ENGINE. AIRCRAFT LANDED SAFELY IN LBB. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED AND FOUND THE OIL DIFFERENTIAL PRESSURE SWIT CH LINE RUPTURED. OIL LINE WAS REPLACED, ENGINE WAS SERVICED AND GROUND RUN PERFORMED NORMAL. AIRCRAFT RETURNED TO SER VICE. 2 L 7 2 4F RT A6WE 2007102400217 20071024 00217 WP 2007 10 24 070172 1 20071012 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 886GA 49931 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007102400223 20071024 00223 NM 2007 10 24 DL757071361 1 20071016 A 3350 LIGHT BOEING 757 757232 1384965 NM ROW 19 INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 644DL 23998 DURING TRANSIT CHECK INSPECTION FOUND SEAT MOUNTED EMERGENCY LIGHTS INOP FROM ROW 19 TO 26 RIGHT SIDE OF AIRCRAFT. 2 L 7 2 4F RT A2NM 2007102400225 20071024 00225 NM 2007 10 24 DLM88071364 1 20071018 A 3222 STRUT DOUG MD88 MD88 3023688 NM NLG DAMAGED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 985DL 53312 AFTER TAKEOFF GEAR HANDLE UP GOT RED NOSE GEAR INDICATION SOUNDED LIKE NOSE GEAR DID NOT RETRACT, RETURNED TO ATL. MTC IN PROGRESS ON NOSE STRUT. REPACKED NOSE LANDING GEAR C/W OPN 4702 ACJIC CARD 5 RETRACT AND EXTENSION CHECKS NORMAL. 2 L 7 2 4F RT A6WE 2007102500003 20071025 00003 EU 2007 10 25 07FDEA04662 1 20071023 A 5310 A53612180000 WINDOW FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 729FD 657 FOUND WEAR MARKS ON SLIDING WINDOW FRAME, LHS REPAIR PERFORMED BY SMOOTH BLEND OUT, NDT FOR CRACK FREE IAW EA 6-5612-114 907 AND RAS 054606/005/2007 ISS A. 2 L 7 2 4F RT A35EU 2007102500004 20071025 00004 NM 2007 10 25 QXEA200701591 1 20071020 A 3010 DEICE SYSTEM BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 422QX 4150 GEG FLIGHT NR 2376: DURING DESCENT, DEICE CAUTION ILLUMINATED. AFTER RUNNING CHECKLIST, DEICE PRESSURE ON BOTH SIDES OF SYSTEM REMAINED AT 18 PSI. SECOND GREEN LIGHT FROM RIGHT WING TIP DOES NOT ILLUMINATE AND BOOT SET DOES NO APPEAR TO I NFLATE. MAINTENANCE PERFORMED FUNCTIONAL CHECK IAW AMM TASK 30-11-720-801. CYCLED THROUGH FAST, SLOW AND MANUAL SEVERA L TIMES. NO DEFECTS NOTED. INFLATED BOOT. LEAK CHECK WITH NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102500006 20071025 00006 NM 2007 10 25 AALA20071948 1 20071016 A 2613 SENSOR BOEING 737 737823 13844BZ NM RT OVERHEAT INOPERATIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 929AN 30078 CUN INFLIGHT T2199/16OCT - DURING CLIMB-OUT RIGHT WING TO BODY OVERHEAT INDICATION ILLUMINATED. LANDED CUN WITHOUT INCI DENT. REPLACED SENSOR M1763. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007102500007 20071025 00007 NM 2007 10 25 AALA20071954 1 20070926 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 935AN 30081 TUL - EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK M1674 FOR EMERGENCY LIGHTS AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007102500008 20071025 00008 NM 2007 10 25 AALA20071955 1 20070926 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 935AN 30081 TUL - EMERGENCY LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK M1670 FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007102500010 20071025 00010 EU 2007 10 25 07FDEA04643 1 20071018 A 5340 R538D104820200 ATTACH FITTING AIRBUS 310 A310 EU BS 2506 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 MAIN CABIN FR45 RT SIDE ADAPTER CRACKED OVER WING BOX REPLACED FR45 ADAPTER IAW SRM 51-40-21 P7 AND AMM 20-21-12. 2 L 7 2 4F RT A35EU 2007102500011 20071025 00011 EU 2007 10 25 HYIA12137 1 20071011 A 5312 S5317400214 STIFFENER AEROSP ATR42 ATR42320 8680930 EU BULKHEAD CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 FORWARD PRESSURE BULKHEAD LEFTHAND OUT BOARD STIFFNER CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS L IMITS. REMOVED AND INSTALLED STIFNER IN ACCORDANCE WITH SRM 5125-01 AND 51-25-04. 2 H 7 2 4T RT A53EU 2007102500014 20071025 00014 NM 2007 10 25 2007UALA04156 1 20071009 A 3350 POWER SUPPLY AIRBUS A319 A319131 3930317 NM EMERGENCY LIGHT FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 827UA 1022 EMERGENCY LIGHT SYSTEM TEST FAILED ON PTP PANEL, DISPLAYS EPSU FWD L. FOUND EPSU (FWD) IS FAULTY. REPLACED EPSU. NO R EPEATS SINCE ORIGINAL. 2 L 7 2 4F RT A28NM 2007102500015 20071025 00015 EU 2007 10 25 2007UALA04157 1 20071009 A 3510 6490375 OXYGEN MASK AIRBUS 320 A320232 3930326 EU 1ST OBSERVER'S LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 416UA 479 THE 1ST OB'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). CREW COMMENTS: O2 FLOWS CONTINUOUSLY. SUPPLEMENTAL DATA UP DATE CAUSE: REGULATOR LEAKING ON O2 MASK. REPLACED MASK ASSY AND PROPERLY RESTOWED. SERVICED O2 SYSTEM TO PROPER LIMI T. 2 L 7 2 4F RT A28NM 2007102500016 20071025 00016 2007 10 25 2007UALA04158 4 20071009 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 433UA 589 CIDS TEST FAULT "EXT LOADS AFT L". REPLACED SLIDE ASSY. NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007102500017 20071025 00017 EU 2007 10 25 UPS07150940 1 20071019 A 2597 WIRE AIRBUS A300 A300F4622R 3930360 EU EMERGENCY EXIT BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 162UP 0005 SLIDE ARM TEST BUTTON HORN INOP, FLASHING RED LIGHT DOES NOT WORK. REPAIRED BROKEN WIRES BETWEEN TB 6035VT & P/B TEST SWITCH 39WN REF WDM 52-73-01. THIS CLEARS M360929 360929 2 L 7 2 4F RT A35EU 2007102500018 20071025 00018 NM 2007 10 25 MWEA070257 1 20071018 A 5230 59101575 PAN BOEING 717 717200 1383700 NM CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 902ME 55166 AFT CARGO DOOR PAN IS CRACKED ON FORWARD SIDE WHERE GUIDE ANGLE ATTACHES TO PAN. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2007102500019 20071025 00019 NM 2007 10 25 MWEA070258 1 20071018 A 5230 59101577 PAN BOEING 717 717200 1383700 NM CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 902ME 55166 AFT CARGO PAN IS CRACKED AT FORWARD SIDE WHERE GUIDE ANGLE ATTACHES. FABRICATED AND INSTALLED DOUBLER 2 L 7 2 4F TR A6WE 2007102500020 20071025 00020 NM 2007 10 25 AALA20071959 1 20071001 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 975AN 29549 TUL - EMERGENCY LIGHTS AT LEFT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT AFT CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007102500021 20071025 00021 NM 2007 10 25 AALA20071960 1 20071001 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 975AN 29549 TUL - EMERGENCY LIGHTS AT LEFT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT MID CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007102500022 20071025 00022 NM 2007 10 25 AALA20071961 1 20071001 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 975AN 29549 TUL - EMERGENCY LIGHTS AT RIGHT AFT CABIN OVERHEAD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT AFT CABIN OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007102500023 20071025 00023 NM 2007 10 25 AALA20071962 1 20071001 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 975AN 29549 TUL - EMERGENCY LIGHTS AT RIGHT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007102500024 20071025 00024 NM 2007 10 25 AALA20071958 1 20071001 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 975AN 29549 TUL - EMERGENCY LIGHTS AT LEFT AFT CABIN OVERHEAD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT AFT C ABIN OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007102500025 20071025 00025 NM 2007 10 25 AALA20071966 1 20071017 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 941AN 29534 TUL - EMERGENCY LIGHT AT LEFT OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT OVERWING EXI T. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007102500026 20071025 00026 NM 2007 10 25 AALA20071965 1 20071007 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 941AN 29534 TUL - EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007102500027 20071025 00027 NM 2007 10 25 AALA20071967 1 20071010 A 5740 113W13403 SUPPORT BOEING 777 777223 1385213 NM TE FLAP ACTUATOR DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 787AL 30010 AFW - FLAP SUPPORT ACTUATOR HAS HOLES FOR BEARING 165 THAT ARE BEYOND PUBLISHED SIZE OF ESO 20174. REPAIRED PER AA MRB 777 218. 2 L 7 2 4F RT T00001SE 2007102500028 20071025 00028 NM 2007 10 25 AALA20071963 1 20071001 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 975AN 29549 TUL - EMERGENCY LIGHTS AT FORWARD RIGHT DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD RIGHT D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007102500029 20071025 00029 NM 2007 10 25 AALA20071949 1 20071016 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 DFW - EMERGENCY LIGHT AT SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007102500030 20071025 00030 NM 2007 10 25 AALA20071950 1 20071016 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 40G INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 40G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007102500031 20071025 00031 NM 2007 10 25 AALA20071951 1 20071016 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 DFW - EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007102500032 20071025 00032 NM 2007 10 25 AALA20071952 1 20071016 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 DFW - EMERGENCY LIGHTS AT OVERHEAD LEFT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD LEFT FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007102500033 20071025 00033 NM 2007 10 25 AALA20071953 1 20070926 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 935AN 30081 TUL - EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK M1676 FOR EMERGENCY LIGHTS AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007102500034 20071025 00034 NM 2007 10 25 AALA20071968 1 20071017 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 785AN 30005 DFW - EMERGENCY LIGHT AT SEAT 39C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 39C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007102500035 20071025 00035 NM 2007 10 25 AALA20071969 1 20071017 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 DFW - EMERGENCY LIGHT AT OVERHEAD FIRST CLASS LEFT INOPERATIVE. REPLACED BATTERY PACK M33424 FOR EMERGENCY LIGHT AT OVE RHEAD FIRST CLASS LEFT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007102500036 20071025 00036 NM 2007 10 25 AALA20071970 1 20071017 A 3350 BULB BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 376AN 25445 ORD - EMERGENCY LIGHT AT OVERHEAD SEAT 24G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 24G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007102500037 20071025 00037 NM 2007 10 25 AALA20071971 1 20071017 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 JFK - EMERGENCY EXIT SIGN LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. REPLACED BATTERY PACK M33407 FOR EMERGENCY EXIT S IGN LIGHT AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007102500038 20071025 00038 WP 2007 10 25 AALA20071972 1 20071017 A 2560 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN UNSECURE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 LGA - EMERGENCY FLASHLIGHT AT AFT DOOR HAS DAMAGED STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007102500039 20071025 00039 WP 2007 10 25 AALA20071973 1 20071017 A 3231 SENSOR DOUG DC9 DC982 3022082 WP NLG LOCK INOPERATIVE A AALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 21 427AA 49339 DFW INFLIGHT T852/17OCT - NOSE GEAR WARNING DURING LANDING. PERFORMED GO AROUND AND ALL INDICATIONS NORMAL. LANDED DFW WITHOUT INCIDENT. REPLACED NOSE GEAR LOCK SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007102500040 20071025 00040 NM 2007 10 25 AALA20071956 1 20071001 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 975AN 29549 TUL - EMERGENCY LIGHTS AT LEFT FORWARD GALLEY OVERHEAD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT AND FORWARD GALLEY OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007102500041 20071025 00041 NM 2007 10 25 AALA20071957 1 20071001 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 975AN 29549 TUL - EMERGENCY LIGHTS AT RIGHT FORWARD GALLEY OVERHEAD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGH T FORWARD GALLEY OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007102500042 20071025 00042 NM 2007 10 25 QXEA200701592 1 20071021 A 3350 800A1C1D223L2N1A SWITCH BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY LIGHTS MALFUNCTIONED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 415QX 4081 PDX FLIGHT: EMERGENCY LIGHTS ILLUMINATE WHEN SWITCH IS ARMED. MAINTENANCE REMOVED AND REPLACED FWD FLIGHT ATTENDENT EME RGENCY LIGHT SWITCH. PERFORMED OPS CHECK OF THE EMERGENCY LIGHT SYSTEM IAW Q400 AMM TASK 35-51-00-710-801. OPS CHECK G OOD. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102500043 20071025 00043 EA 2007 10 25 QXEA200701550 1 20071009 A 5310 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA BS 394 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - C4 CHECK, REFERENCE REO 670-53-11-188 SHEET 1 MAP A, BURNED MATERIAL FOUND AROUND FASTENER HOLE AT STATION FS 394 2.9" DOWN AT STRINGER 8L. REQUIRED REPAIR. HFEC AROUND FASTENER HOLES, NO CRACKS NOTED. REPAIRED IAW STEPS 5-8 OF REO 670-53-11-188 PAGE 3 MAP A. 2 L 7 2 4F RT A21EA 2007102500044 20071025 00044 EA 2007 10 25 QXEA200701551 1 20071009 A 5310 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA BS 421 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - C4 CHECK. REFERENCE REO 670-53-11-199 SHEET 1 MAP B, BURNED MATERIAL AROUND FASTENER HOLE .80" FORWARD OF FS 241 S TRINGER 8L. REQUIRED REPAIR. HFEC FASTENER HOLE WITH NO CRACKS NOTED. COMPLIED WITH STEPS 5-8 OF REO 670-53-11-188 PA GE 3 MAP B. 2 L 7 2 4F RT A21EA 2007102500045 20071025 00045 EA 2007 10 25 QXEA200701552 1 20071009 A 5310 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA BS 501 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - C4 CHECK. REFERENCE REO 670-53-11-188 SHEET 1 MAP C, BURNED MATERIAL AROUND FASTENER HOLE AT FS 501. 2.4" DOWN STR INGER 6L, REQUIRES REPAIR. HFEC PERFORMED AROUND FASTENER HOLES WITH NO DEFECTS NOTED. COMPLIED WITH REO 670-53-11-188 PAGE 3 MAP C. 2 L 7 2 4F RT A21EA 2007102500046 20071025 00046 EA 2007 10 25 QXEA200701553 1 20071009 A 5310 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA BS 533 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - C4 CHECK, REFERENCE REO 670-53-11-188 SHEET 1 MAP E, BURNED MATERIAL AROUND FASTENER HOLE AT FS 533. .52" UP STRIN GER 6L. HFEC COMPLIED WITH, NO CRACKS NOTED. COMPLIED WITH REO 670-53-11-188 PAGE 3 MAP E. 2 L 7 2 4F RT A21EA 2007102300222 20071023 00222 2007 10 23 SWAA075142 4 20071018 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 456WN 32463 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007102300231 20071023 00231 NM 2007 10 23 EIA2007161 1 20070917 A 5730 65B1448622 SKIN BOEING 747 747212B 1384886 NM RT WING DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 RIGHT WING LANDING LIGHT SKIN PANEL OUTBOARD HAS NUMEROUS RIVETS PULLED/WORN THRU SKIN AND FASTENERS DISTRESSED. REPAIR ED RT LEADING EDGE LANDING LIGHT SKIN PANEL PER ECRA NR 486-57-057-2. 2 L 7 4 4F A20WE 2007102300241 20071023 00241 NM 2007 10 23 EIA2007168 1 20070920 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM BS 440 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 U/D LT UPPER DECK FLOORBEAM BS 440 CRACK FOUND ON FLOORBEAM UPPER CHORD INSP HOLE. FABRICATED AND INSTALLED REPAIR NEW STRAP PER BOEING PROPOSAL 1-568670402 (EA-53-1182). 2 L 7 4 4F A20WE 2007102300246 20071023 00246 NM 2007 10 23 HNAA0700242 1 20071018 A 5720 85711069 PLATE DHAV DHC8 DHC8102 2809003 NM WING CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 828EX 392 CRACK AT FORWARD INBOARD CORNER OF LADDER PLATE ON PANEL 522AT WAS FOUND DURING INSPECTION. REPAIRED IAW EO 8-57-07-024 2. 2 H 7 2 4T RT A13NM 2007102300254 20071023 00254 NM 2007 10 23 UPS07M50944 1 20070920 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C MAIN DECK: FROM BS 869 TO BS 6-05, ALONG -X=9 (RBL 9), SEAT TRACK CROWN & FL FLANGE AREAS FOUND CORRO DED. CORROSION REMOVAL C/OUT A/M AREA PER SRM 53-70-00D.F1 V2 R35. FOUND EXCEED ED LIMIT. REMOVAL C/OUT TO GAIN OF CO RRODED SEAT/T, CORRODED SEAT/T REMOVED PER SRM 51-31-01 V2 R35. NEW SEAT/T & SPLICE RWK PER SRM 53-70-00D V1 R3 5. RWK PARTS HOLES UP & INSTL C/OUT PER SRM 51-31-01, 51-21-01 V2, R35 & INSTALLED PER SRM 51-33-01 & 51-31-01 V2, R35. FOUND SATIS. 2 L 7 3 4F RT A22WE 2007102300265 20071023 00265 NM 2007 10 23 WRLA2007109 1 20071008 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 273WA 48519 DURING 4C+12A CHECK, SEAT TRACK CORROSION FOUND AT STA X=-75.25 Y=1870. REPAIRED PER MD-11 SRM 53-70-00 VOL.1 FIG.1 REV .40. 2 L 7 3 4F 4 F RT A22WE E24NE 2007102300273 20071023 00273 NM 2007 10 23 2007UALA04141 1 20071009 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EMERGENCY LIGHT INOPERATIVE: CEILING ROWS 4R, 12 & 17. 11-01-07 REPLACED LAMP IN EACH POSITION. ALL OP CHECKED GO OD FOR RETURN TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102300301 20071023 00301 NM 2007 10 23 2007UALA03888 1 20070924 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 673UA 29241 BOTH SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS ON SEAT 1B ARE INOP. REPLACED BOTH EEL LIGHT ASSYS, TEST OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102300321 20071023 00321 NM 2007 10 23 2007UALA04171 1 20071010 A 5210 6552873180 DOOR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU L2 OUT OF RIG A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 919UA 25386 DOOR 2L HANDLE LIFTS IN FLIGHT CAUSING AFT SERVICE DOOR WARNING LIGHT TO ILLUMINATE. SUSPECT DOOR OUT OF RIG. ACCOMPLIS HED SERVICE TIP 52-00-96-101. ADJUSTED DOOR STOPS. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007102400008 20071024 00008 NM 2007 10 24 EIA2007178 1 20070906 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 640 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 MAIN DECK BS 640 LBL 99 SEAT TRACK FOUND CRACKED. MAIN DECK BS 640 LBL 99 SEAT TRACK REPAIRED PER SRM 51-30-02. 2 L 7 4 4F A20WE 2007102400026 20071024 00026 EU 2007 10 24 07FDEA04592 1 20071015 A 5730 SKIN AIRBUS 300 A300B4622R 3930312 EU LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION ON LT WING BOTTOM SKIN LOWER SURFACE RIB 1-2, P4-6 REPAIR PERFORMED BY BLEND OUT CORROSION, REPAIR IAW S B 57-6047, APPROVED BY EA 6-5720-112530 AND RAS/BAE/1005161/2007 ISS A. 2 L 7 2 4F RT A35EU 2007102400034 20071024 00034 NM 2007 10 24 QXEA200701547 1 20071014 A 3150 INDICATOR BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 09 429QX 4161 SEA FLIGHT NR 2295: 'TAKE OFF WARNING' ILLUMINATED ON HGS DURING LOW VISIBILITY TAKEOFF. ABORTED TAKEOFF AND RETURNED T O BLOCK. MAINTENANCE PERFORMED OPS CHECK OF HGS SYSTEM IAW QX MTC 6343501. OPS CHECK GOOD. AIRCRAFT REMAINS CAT 3. P LACARD REFLECTS SUCH. MTX CONTROL NOTIFIED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102400038 20071024 00038 NM 2007 10 24 DL76G071331 1 20071010 A 3610 77328915 CONTROLLER BOEING 767 767332 1382001 NM LT BLEED SYS FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 178DZ 30596 NO BLEED AIR FROM LT ENG. REPLACED THE LT HPC AND OPS CK OK. 2 L 7 2 4F RT A1NM 2007102400061 20071024 00061 EA 2007 10 24 SWIA200718778 1 20071011 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DAMAGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 952SW 7805 FLT 6718 - EMERGENCY LIGHT ON GALLEY SERVICE DOOR DOES NOT ILLUMINATE. REPAIRED WIRE AT LIGHT ASSEMBLY. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007102400065 20071024 00065 NM 2007 10 24 07FDEA04601 1 20071016 A 5313 ACA37962 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 620FE 48791 ONE FASTENER HOLE FOUND CRACK AT 3 AND 9 O'CLOCK POSITION AT RIGHT SIDE TRUNNION FITTING LOWER LONGERON. 10-30-07 REMOVED AS PER SRM 51-31-01 VOLUME II. LONGERON FABRICATED AS PER FEDEX EA 1-5310-116497, REPAIR CLASSIFIED AS MAJOR PE R GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007102400066 20071024 00066 NM 2007 10 24 07FDEA04602 1 20071016 A 5340 ATTACH FITTING DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 620FE 48791 AFT FUSELAGE INTERIOR FOUND DOG HOUSE LOCATION WITH FRAME CLIP QUANTITY 01 EACH CRACKED AT STATION Y2069. 10-30-07 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007102400067 20071024 00067 NM 2007 10 24 07FDEA04603 1 20071016 A 5347 ACA7399501 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 635 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 620FE 48791 MAIN DECK CARGO COMPARTMENT RIGHT FLOOR SEAT TRACK AT STATION 635, X = -47.5, FOUND CRACKED APPROXIMATELY 3 INCHES. 1 0-30-07 REPAIRED BY REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007102400069 20071024 00069 NM 2007 10 24 07FDEA04605 1 20071016 A 5753 ARC40092 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 620FE 48791 CRACK FOUND DURING HFEC OPEN HOLE INSPECTION ON THE MOST OUTBOARD, LOWER FASTENER HOLE COMMON TO THE ARC4008 AND ARC4009 RIGHT WING OUTBOARD FLAP SUPPORT FITTING. 10-30-07 REMOVED AND REPLACED AS PER MD11 CMM 57-52-04. FLAP ADJUSTME NT TEST CARRIED OUT AS PER AMM 27-50-00-830-805. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007102400083 20071024 00083 NM 2007 10 24 AALA20071934 1 20071015 A 3350 233T32101033 CONTROL PANEL BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 385AM 27059 ORD - EMERGENCY EXIT LIGHT OVERHEAD COCKPIT DOOR INOPERATIVE. REPLACED LIGHT SWITCH PANEL FOR EMERGENCY EXIT LIGHT OVER HEAD COCKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007102400093 20071024 00093 EU 2007 10 24 07FDEA04614 1 20071017 A 5730 A57340085 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION ON TOP SKIN LT WING RIB 25-29 AROUND FASTENER HOLES REPAIR PERFORMED BY BLEND OUT CORROSION, OVERSIZING THE HOLES, FLAP PEENING AND NDT FOR CRACK FREE IAW EA 6-5720-112521 AND RAS/BAE/1005138/2007 ISS A. 2 L 7 2 4F RT A35EU 2007102400098 20071024 00098 WP 2007 10 24 07FDEA04619 1 20071017 A 5512 ALC72041 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 DURING U/S INSP FOUND PANEL P/N 7206-1 AND 7204-1 OF STAB LOWER SURFACE WITH CRACK IN FLYABLE LIMITS, SEE ATTACHED "INSP FINDING FORM" FOR DETAIL. ACCOMPLISHED EA NR 8-5510-111454. 2 L 7 3 4F RT A22WE 2007102400103 20071024 00103 WP 2007 10 24 07FDEA04628 1 20071017 A 5313 AFA32801 LONGERON DOUG DC10 DC1010F 3022111 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 CTR CARGO COMPT CRACK ON LONGERON. REPAIRED LONGERON IAW SRM 53-10-00 FIG 1-2 VOL I. 2 L 7 3 4F A22WE 2007102400109 20071024 00109 NM 2007 10 24 07FDEA04634 1 20071017 A 5310 507978113 DOOR FRAME BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 RT AFT OVERWING DOOR FRAME EXTERIOR SURFACE IS CORRODED ALONG PRESSURE SEAL ATTACH ANGLE AT 5:00 TO 8:00, POS AS VIEWED FROM OUTSIDE. REMOVED CORROSION FROM FRAME SURFACE REF SRM 51-10-1 PG 14-16. MEASURED THICKNESS REF. 727 NDT MAN. P T. 4, 51-00-00. FIG 2, ORIGINAL "T" .040", REMANING "T" .036" IN DEEPEST LOCATION. REMOVED .004" MATERIAL LOSS WITHIN LIMITS REF SRM 52-00-2 PG 3, NOTE A TOOL NR 22-029 CAL DUE 9-28-08. TREATED AND PRIMED, REF SRM 51-10-2. LEVEL 1 CORRO SION. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007102400110 20071024 00110 2007 10 24 IXXA070053O 4 20071017 A 3421 EADI DOUG DC8 DC873F 302199F WP COCKPIT FAILED A IXXA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 SW 11 605AL 98218 1656 46106 DURING TAKEOFF ROLL PRIOR TO 80 KIAS, FIRST OFFICER'S EADI WENT BLANK WITH FLAGS IN VIEW, BAR WITH ATT IN VIEW, GA .AND INST 2 FLAG. THE CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS AT KIAH WITH OUT INCIDENT. MAINTENANCE INSPECTED AND FOU ND NUMBER 2 INSTRUMENT RACK LOOSE. MAINTENANCE RESECURED INSTRUMENT RACK OPERATIONAL CHECK GOOD IAW ATI DC8 MAINTENANCE MANUAL 34-01-07. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2007102400114 20071024 00114 EA 2007 10 24 QXEA200701539 1 20071013 A 2751 FLAP SYSTEM CNDAIR CL600 CL6002C10 1390015 EA TE FLAPS FALSE INDICATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 612QX 10042 BOI - FLIGHT 2590, RECEIVED A FLAP HALF-SPEED STATUS MESSAGE. RETURNED TO THE GATE. MAINTENANCE CHECKED THE MDC AND RA N THE SFECU 1/2 TEST. TEST PASSED AND CLEARED INHIBITS. FLAPS OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007102400116 20071024 00116 EA 2007 10 24 QXEA200701541 1 20071014 A 4970 RELAY CNDAIR CL600 CL6002C10 1390015 EA APU MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 610QX 10033 PDX - FLIGHT 2575, RECEIVED A APU SOV FAIL MESSAGE WHEN SHUTTING DOWN APU. RETURNED TO THE GATE. MAINTENANCE REPLACED THE K-103 RELAY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007102400124 20071024 00124 NM 2007 10 24 QXEA200701572 1 20071016 A 3010 4100S00503 VALVE BOMBDR DHC8 DHC8402 1390042 NM DEICE SYSTEM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 422QX 1438 128 4150 SEA FLIGHT NR 2276: DEICE PRESSURE CAUTION ILLUMINATED ON FLIGHT. RAN EA CHECKLIST AND LIGHT EXTINGUISHED WHEN SELECTED TO MANUAL. LIGHT CAME ON AFTER FEW CYCLES. DEICE PRESSURE WAS NORMAL ON BOTH SIDES. ALL BOOT ADVISORY LIGHTS WORK NOR MALLY. MAINTENANCE REMOVED 613AR IAW Q400 AMM TASK 57-23-01-00-801. REMOVED AND REPLACED NR 2 DDV IAW Q400 AMM TASK 30 -11-16-000-801 AND 3-11-16-400-801. OPS CHECK GOOD. REINSTALLED 613AR IAW Q400 AMM 57-23-01-400-801. OPS CHECK OF A/ F DEICE SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102400137 20071024 00137 NM 2007 10 24 07FDEA04635 1 20071017 A 5310 50797890 DOOR FRAME BOEING 727 727233 138408A NM BS 760-783 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 RT FWD OVERWING DOOR FRAME EXTERIOR SURFACE IS CORRODED AT 7:00 POS AS VIEWED FROM OUTSIDE REMOVED CORROSION ON DOOR FRA ME REF SRM 51-10-6, MEASURED THICKNESS REF 727 NDT MAN PT 4, 51-00-00, FIG 2 ORIGINAL "T" .063". REMAINING "T" IS .060 " IN DEEPEST LOCATION .003 MATERIAL LOSS WITHIN LIMITS REF SRM 52-00-2 PG 3 NOTE A TOOL II IN22-0029. CAL DUE 9-28-08 T REATED AND PRIMED REF SRM 51-10-2. LEVEL 1 CORROSION. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007102400143 20071024 00143 EU 2007 10 24 07FDEA04641 1 20071018 A 5340 R538D104820200 ADAPTER AIRBUS 310 A310203 3930313 EU MAIN CABIN CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 MAIN CABIN FR 42 LT SIDE, ADAPTER CRACKED OVERWING BOX REMOVED CRACKED ADAPTER IAW SRM 51-40-21 PAR 7. INSTALLED NEW AD APTER IAW SRM 51-40-21 AND AMM 20-21-12-0. 2 L 7 2 4F RT A35EU 2007102400146 20071024 00146 EU 2007 10 24 07FDEA04645 1 20071018 A 5340 R538D104820200 ATTACH FITTING AIRBUS 310 A310203 3930313 EU MAIN CABIN CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 MAIN CABIN FS 42 RT SIDE ADAPTER CRACKED OVERWING BOX REPLACED FR 42 RT SIDE ADAPTER IAW A310-200 SRM 51-40-21 P7 AND A3 10-200 AMM 20-21-12. 2 L 7 2 4F RT A35EU 2007102400148 20071024 00148 NM 2007 10 24 07FDEA04647 1 20071018 A 5270 WARNING LIGHT BOEING 727 727227 1384078 NM AIRSTAIR DOOR FALSE ACTIVATION A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 492FE 21530 AFT AIRSTAIR LIGHT ILLUMINATED IN FLIGHT AT FL330. LIGHT WENT OUT AT 10000 FT ENGINE ANTI-ICE WAS OPEN WHEN AFT AIRSTAI R LIGHT WAS ON. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C . 10-30-07 2 L 7 3 4F A3WE 2007102400150 20071024 00150 NM 2007 10 24 NWAA073495652 1 20071010 A 5330 SKIN BOEING 757 757251 1384970 NM BS 620 S15-16L DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 552NW 26499 DURING GROUND OPERATIONS JETWAY CONTACTED FUSELAGE DAMAGING SKIN AND FRAME AT BS 620 S15L-S16L. REPAIRED PER EA 56-2107 31. 2 L 7 2 4F RT A2NM 2007102400162 20071024 00162 NM 2007 10 24 QXEA200701578 1 20071018 A 2751 WARNING MESSAGE BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 423QX 4153 EUG FLIGHT NR 2280: FLAP POWER CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE. MAINTENANCE RESET FLAP NUM AND PU LLED C/B L7. RAN FLAPS DOWN AND UP. NO DEFECTS NOTED PER SL DH8-400-SL-27-00-2A. NO PARTS REPLACED. AIRCRAFT RETURNE D TO SERVICE. 2 H 7 2 4T RT A13NM 2007102400163 20071024 00163 NM 2007 10 24 QXEA200701579 1 20071017 A 3240 60070511 VALVE BOMBDR DHC8 DHC8402 1390042 NM BRAKES MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 419QX 2069 2069 4145 GEG FLIGHT NR 2394: ON APPROACH, NR 1 ISO VALVE AND INBD SPOILER CAUTION LIGHTS ILLUMINATED INTERMITTENTLY (FLICKERING). IT THEN WENT STEADY FOR AWHILE, THEN THE CAUTION LIGHTS DISAPPEARED, THEN REAPPEARED. RAN THE NR 1 ISO VALVE CHECKLIS T. UPON LANDING, THE FO WAS ABLE TO APPLY BRAKES INITIALLY BY THE TIMES TRANSFER OF CONTROL WAS MADE, CAPTAIN'S SIDE HA D NO BRAKES. ABLE TO SHOW AIRCRAFT TO TAXI OFF RUNWAY AND STOP WITH PARKING BRAKE. MAINTENANCE REPLACED LT OUTBD, RT I NBD AND RT OUTBD FUSE/SHUTTLE VALVE IAW AMM 32-42-11, PAGES 401-407. LEAK CHECK GOOD. PERFORMED NR 1 HYD ISO VALVE FIM TASK 29-10-00-810-801. NO TRANSFER OF FLUID OR OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102400168 20071024 00168 NM 2007 10 24 AALA20071945 1 20071016 A 3350 SIGN BOEING 757 757223 1384957 NM LT OVERWING DOOR DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 681AA 25338 DFW - EMERGENCY LIGHT PLACARD AT AFT LEFT OVERWING EXIT DOOR DAMAGED. REPLACED PLACARD FOR EMERGENCY LIGHT AT AFT LEFT OVERWING EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007102400184 20071024 00184 SO 2007 10 24 SIMA200729305 1 20071019 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS UNSECURE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 610AE 145073 EMERGENCY EXIT SIGN OVERHEAD MID CABIN WILL NOT ILLUMINATE. RESECURED CONNECTOR PIN FOR FORWARD OVERHEAD "EXIT" SIGN AT EMERGENCY EXIT ROW. OPS CHECK GOOD IAW EMB AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007102400185 20071024 00185 SO 2007 10 24 SIMA200729306 1 20071019 A 5610 67M534 SEAL EMB 145 EMB145LR 3260212 SO WINDOW FAILED A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 682AE 14500826 IN FLIGHT LT DV WINDOW STARTED TO MAKE A VERY LOUD NOISE. PRESS CONTROL WOULD NOT HOLD DESCENDED TO 10,000 FEET. DIVER TED TO SHV DUE TO LACK OF FUEL AT 10,000 FT FOR FLIGHT TO DFW NO OTHER PROBLEMS NOTED LANDED AT SHV. FOUND SEAL TO BE DEFECTIVE ISSUED MEL 21-18 IAW ETN GN-52-001. REMOVED AND REPLACED RIGHT DV WINDOW SEAL IAW EMB 145 AMM 56-11-02 MEL 21 -28. RESTORED MEL. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007102400192 20071024 00192 SO 2007 10 24 SIMA200729503 1 20071017 A 3320 BR900022 BALLAST EMB 135 EMB135KL 3260302 SO CABIN LIGHTS FAILED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 21 815AE 145545 SLIGHT ODOR COMING FROM CABIN CEILING LIGHTS. FLIGHT ATTENDANT SAID WHEN DIMMED THE LIGHTS ROW 2 AND ONE LIGHT WENT FUL L BRIGHT. THAT IS WHEN SMELL STARTED. NO SMOKE. REMOVED BULB AT ROW 2 AND ISSUED MEL 33-02. REMOVE AND REPLACE CARGO LIGHT BALLAST AT SEAT 4 IAW 33-31-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007102400196 20071024 00196 NM 2007 10 24 QXEA200701582 1 20071016 A 3297 401020101 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM MLG DAMAGED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 425QX 4039 RDD FLIGHT: AFTER SELECTING GEAR UP AFTER TAKEOFF, ALL GEAR LIGHTS EXTINGUISHED EXCEPT FOR THE 'R-DOOR' AMBER LIGHT. FO LLOWED EMERGENCY CHECK LIST STAYING UNDER 185 KTIAS. PERFORMED ALTERNATE GEAR EXTENSION FOR EMERGENCY CHECK LIST FOR SU BSEQUENT LANDING. MAINTENANCE, AFTER TROUBLESHOOTING, REMOVED AND REPLACED RGUPLK, RGDLK, AND RGDLK2 PROXIMITY SENSORS PER Q400 AMM TASKS 32-61-06-000-802 AND 32-61-06-400-802. FUNCTIONAL TEST WAS GOOD. NO PARTS REPLACED. AIRCRAFT RETUR NED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102400202 20071024 00202 NM 2007 10 24 07FDEA04657 1 20071021 A 5320 651627910 FLOOR SUPPORT BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 218FE 21101 SEVERAL LOCATIONS OF CORROSION ON UPPER CHORD FROM FS 760 TO 840, LBL 45.5 REMOVED CORROSION BY REMOVING DAMAGED UPPER C HORD AT STA 760-850, LBL 45.5 REF SRM 51-30-2. REMOVED FLOOR SUPPORT T-CHORD AND ATTACHED FLOOR SUPPORT ASSY'S AT LBL 4 5.5-62.0 -25.0-45.5 STA 760-850 REF SRM 51-30-2 AND BOEING DWG 65-16279. INSTALLED SEAT TRACK TO NEW UPPER T-CHORD AT S TA 760 - 850, LBL 45.5 REF SOPM20-50- 01. INSTALLED NEW BUSHING AT STA 738 REF AMM 20-10-007. INSTALLED FWD SEAT TRAC K AND FITTING AT STA 850-870 PLUS FITTING AT STA 774, LBL 44, REF SRM 51-30-2 AND 51-30-4. INSTALLED T-CHORD STRAPS REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007102400213 20071024 00213 WP 2007 10 24 070169 1 20071006 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 871GA 53296 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007102400228 20071024 00228 NM 2007 10 24 DL76G071372 1 20071020 A 4920 380029817 ENGINE BOEING 767 767332 1382001 NM APU INOPERATIVE A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 175DZ 21938 29696 APU FAILED TO START SEVERAL TIMES. ECU FAULTS SHOW P2 TROUBLE SHOT BY TROUBLESHOOTING TEAM NEEDS UPPER HARNESS. REPLAC ED APU PER AMM. 2 L 7 2 4F RT A1NM 2007102400229 20071024 00229 NM 2007 10 24 DL76G071373 1 20071021 A 4920 380029817 ENGINE BOEING 767 767332 1382001 NM AFT MAKING METAL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1605 30198 FOUND APU MAIN CHIP DETECTOR FULL OF METEL. REMOVED/REPLACED REF AMM. OPS LEAK CHECK GOOD. 2 L 7 2 4F RT A1NM 2007102400233 20071024 00233 EA 2007 10 24 A6WA200740503 1 20070910 A 2121 AE0804AA2 FAN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 427ZW 7685 REQUEST INSPECTION FOR SMOKE ODOR IN COCKPIT. HEARD GRINDING NOISE FROM DISPLAY OR ARNIC FAN. INSPECTED AIRCRAFT AND T ESTED AVIONIC COOLING SYSTEM PER CRJ AMM 21-24-00-710-801. REPLACED DISPLAY FILTER. COULD NOT DUPLICATE PROBLEM. NO S MOKE ODOR. NO NOISE. REMOVED AND REPLACED DISPLAY COOL FAN. (M) 2 L 7 2 4F RT A21EA 2007102500002 20071025 00002 NM 2007 10 25 NWAA073545811 1 20071022 A 3240 BRAKE ASSY BOEING 757 757351 1384991 NM NR 1 FIRE A NWAA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 GL 01 591NW 32991 DURING ROLL UP TO GATE, NR 1 BRAKE CAUGHT FIRE AND THEN SPREAD TO NR 2 BRAKE. GROUND PERSONNEL USED FIRE EXTINGUISHERS TO EXTINGUISH THE FIRE. THERE WERE NO INJURIES. MAINTENANCE REMOVED AND REPLACED BOTH BRAKES AND TIRES, ALSO CLEANED A ND INSPECTED THE MAIN AXLES. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007102500013 20071025 00013 NM 2007 10 25 2007UALA04153 1 20071010 A 3250 CONTROL UNIT AIRBUS A319 A319131 3930317 NM NLG STEERING MALFUNCTIONED A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 818UA 0882 NOSE WHEEL STEERING PULLS TO THE RIGHT WHEN TILLER AT ZERO. FOUND BSCU FAULTY. REPLACED BSCU, NO REPEATS. 2 L 7 2 4F RT A28NM 2007102600001 20071026 00001 EA 2007 10 26 A6WA200740543 1 20070922 A 2910 AE7090061 LINE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LOOSE A A6WA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 GL 31 418AW 7618 HYDRAULIC NR 1 LOW PRESSURE CAUTION MESSAGE ILLUMINATED INFLIGHT, COMPLIED WITH QRH, FLUID QUANTITY INDICATED ZERO. FOU ND PRESSURE LINE ON LT EDP LOOSE AND TIGHTENED IAW 51-40, OPERATION TEST AND FUNCTION TEST OF EDP PERFORMED IAW AMM 29-1 1-01, CHECKED GOOD. SERVICED HYD NR 1 SYSTEM. (M) 2 L 7 2 4F RT A21EA 2007102600004 20071026 00004 EA 2007 10 26 A6WA200740572 1 20070926 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 MINOR PITTING DAMAGE RT LOWER WING PLANK WAS 12.245 ACCESS PANEL 610AB, .001 INCH-.002 INCH DEEP IN CRITICAL AND NON-CRI TICAL AREAS. MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV F. (M) 2 L 7 2 4F RT A21EA 2007102600005 20071026 00005 EA 2007 10 26 A6WA200740570 1 20070926 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 MINOR PITTING DAMAGE LT LOWER WING PLANK WS 188.040 FUEL ACCESS PANEL 550BB IN NON-CRITICAL AREA .001 INCH -.002 INCH DE EP. MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030. (M) 2 L 7 2 4F RT A21EA 2007102600006 20071026 00006 EU 2007 10 26 12117 1 20071011 A 5311 S53871603200 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 FOUND FRAME 44 BETWEEN STRINGERS LEFT AND RIGHT 21 CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS LIM ITS. FRAME 44 REPAIRED IN ACCORDANCE WITH SRM 53-81-40 FIGURE 403. 2 H 7 2 4T RT A53EU 2007102600009 20071026 00009 EU 2007 10 26 HYIA12120 1 20071011 A 5347 S5337500121802 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 LEFT OUTBOARD SEAT TRACK BETWEEN FRAMES 13 AND 23 IS CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS L IMITS. REMOVED AND REPLACED SEAT TRACK IN ACCORDANCE WITH SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007102600010 20071026 00010 EU 2007 10 26 HYIA12121 1 20071011 A 5347 S5337500121702 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 13 AND 23 IS CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS L IMITS. REMOVED AND REPLACED SEAT TRACK IN ACCORDANCE WITH SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007102600012 20071026 00012 EU 2007 10 26 HYIA12123 1 20071011 A 5347 S5357020120202 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 LEFT OUTBOARD SEAT TRACK BETWEEN FRAMES 23 AND 29 IS CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS L IMITS. REMOVED AND REPLACED SEAT TRACK IN ACCORDANCE WITH SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007102600013 20071026 00013 EU 2007 10 26 HYIA12124 1 20071011 A 5347 S5357020120202 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 RIGHT OUTBOARD SEAT TRACK BETWEEN FRAMES 23 AND 29 IS CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS LIMITS. REMOVED AND REPLACED SEAT TRACK IN ACCORDANCE WITH SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007102600014 20071026 00014 EU 2007 10 26 HYIA12125 1 20071011 A 5347 S5307030820002 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 RIGHT SEAT TRACK BETWEEN FRAMES 41 AND 44 IS CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS LIMITS. REMOVED AND REPLACED SEAT TRACK IN ACCORDANCE WITH SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007102600016 20071026 00016 EU 2007 10 26 HYIA12128 1 20071011 A 5347 S5367800121402 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 LEFT SEAT TRACK BETWEEN FRAMES 39 AND 41 IS CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS LIMITS. R EMOVED AND REPLACED SEAT TRACK IN ACCORDANCE WITH SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007102600017 20071026 00017 EU 2007 10 26 HYIA12129 1 20071011 A 5320 S53573000210 RETAINER SEAL AEROSP ATR42 ATR42320 8680930 EU CRACKED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 UPPER WING DECK PRESSURE SEAL RETAINER CRACKED. SEAL RETAINER REPAIRED IN ACCORDANCE WITH AIRCRAFT MANUFACTURES STRUCTU RAL REPAIR INSTRUCTIONS DO/TS3909/01-9238. 2 H 7 2 4T RT A53EU 2007102600018 20071026 00018 EU 2007 10 26 HYIA12130 1 20071011 A 5313 S53070204244245 STRINGER AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 RIGHT STRINGER 20 BETWEEN FRAMES 13 AND 25 CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS LIMITS. RE MOVED AND REPLACED AS PER SRM 53-00-00 FIGURE 428. 2 H 7 2 4T RT A53EU 2007102600020 20071026 00020 EU 2007 10 26 HYIA12132 1 20071011 A 5320 S53671318280 THRESHOLD AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 RIGHT THRESHOLD BETWEEN FRAMES 36 AND 39 CORRODED. CORROSION WAS REMOVED AND FOUND TO BE BEYOND MANUFACTURERS LIMITS. REMOVED AND REPLACED THRESHOLD IN ACCORDANCE WITH SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007102600022 20071026 00022 EU 2007 10 26 HYIA12134 1 20071011 A 5315 S53372411210 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 FOUND FLOORBEAM AT FRAME 13 IS CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS LIMITS. REPAIRED FLOOR BEAM WITH SPLICE IN ACCORDANCE WITH SRM 53-00-00 FIGURE 435. 2 H 7 2 4T RT A53EU 2007102600024 20071026 00024 EU 2007 10 26 HYIA12136 1 20071011 A 5315 S53672215202 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 FOUND FLOORBEAM AT FRAME 39 IS CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS LIMITS. REMOVED AND RE PLACED FLOORBEAM IN ACCORDANCE WITH 51-25-01. 2 H 7 2 4T RT A53EU 2007102600025 20071026 00025 EU 2007 10 26 HYIA12138 1 20071011 A 5312 S53871409214 STIFFENER AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 AFT PRESSURE BULKHEAD STIFFENER, BETWEEN STRINGERS LEFT 21 AND RIGHT 21, CORRODED. CORROSION REMOVED AND FOUND TO BE BE YOND MANUFACTURERS LIMITS. REMOVED AND INSTALLED STIFFENER IN ACCORDANCE WITH SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007102600027 20071026 00027 EU 2007 10 26 HYIA12140 1 20071019 A 5720 S2728175600402 SUPPORT BRACKET AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 RUDDER SPRING TAB LEVER SUPPORT ASSEMBLY CORRODED. CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED IN AC CORDANCE WITH SRM. 2 H 7 2 4T RT A53EU 2007102600028 20071026 00028 EU 2007 10 26 HYIA12141 1 20071019 A 5330 S5397091624900 FACEPLATE AEROSP ATR42 ATR42320 8680930 EU RT WING CRACKED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 RIGHT WIING BOX FACE PLATE CRACKED AT FRAME 29. REMOVED AND REPLACED THE FACE PLATE IN ACCORDANCE WITH SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007102600031 20071026 00031 EA 2007 10 26 A6WA200740557 1 20070928 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 PAX DOOR FORWARD WEB SKIN IS CRACKED IN RADIUS BETWEEN STEP 832CT AND FIXED STEP. MAINTENANCE CUT AWAY DAMAGED SKIN AND INSTALLED REPAIR DOUBLER AND ANGLES IAW BOMBARDIER REO 601R-52-11-702 REV A AND BSC EO 601R-52-13284. (M) 2 L 7 2 4F RT A21EA 2007102600035 20071026 00035 EA 2007 10 26 CHQA200700064 1 20071022 A 3250 601R8610091 RVDT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NLG STEERING MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 642BR 145 7356 GEE872617 IAH-LBB - ON CLIMB-OUT FROM IAH WHILE PASSING THROUGH 5000 FT MSL, CREW RECEIVED EICAS CAUTION MESSAGE "STEERING INOP". AFTER CONSULTING QRH, THE NOSE WHEEL STEERING SWITCH WAS RESET BUT THE MESSAGE WOULD NOT CLEAR. AFTER LANDING THE AIRC RAFT WAS TAXIED OFF THE RUNWAY AND STOPPED ON THE ADJACENT TAXI WAY WITHOUT NOSE WHEEL STEERING. THE AIRCRAFT WAS THEN TOWED BACK TO THE GATE AND TURNED OVER TO MAINTENANCE. MAINTENANCE TROUBLESHOT THE NOSE WHEEL STEERING SYSTEM AND FOUND FAULT CODES FOR THE LEFT FEEDBACK RVDT. THE SYSTEM WAS TROUBLESHOT FURTHER AND THE FEEDBACK RVDT WAS FOUND TO OPERATE NORMALLY. THE RIG OF THE STEERING SYSTEM WAS THEN CHECKED AND FOUND TO BE WITHIN LIMITS. THE AIRCRAFT WAS TAXI CHECKED 2 L 7 2 4F 4 F RT A21EA E15NE 2007102600036 20071026 00036 EA 2007 10 26 A6WA200740567 1 20070923 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 PAX DOOR AFT STAIRS SKIN IS CRACKED BETWEEN PANEL 832CT AND 832DT STEPS, CRACK IS .250 LONG. MAINTENANCE CUT AWAY DAMAG ED SKIN AND INSTALLED REPAIR DOUBLER AND ANGLES IAW BOMBARDIER REO 601R-52-11-702 REV A. (M) 2 L 7 2 4F RT A21EA 2007102600039 20071026 00039 EA 2007 10 26 A6WA200740551 1 20071001 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 411ZW 7569 FOUND FS 280 FLOORBEAM CLIP AT RBL 9.0, OUTBOARD, IS CRACKED IN RADIUS APPROX .50 INCH LONG. (M) MAINTENANCE REMOVED C RACKED CLIP AND INSTALLED NEW CLIP P/N 601R31113-58 IAW BSC SR 601R-53-0057A AND CRJ SRM 51-42-13, 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007102600043 20071026 00043 NM 2007 10 26 QXEA200701595 1 20071015 A 3350 XD4N RELAY BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY LIGHTS MALFUNCTIONED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 415QX 4081 PDX FLIGHT: EMERGENCY LIGHTS COME ON WHEN SWITCH IS SELECTED TO THE 'ARM' POSITION IN THE FLIGHT DECK AND FA SWITCH IN T HE 'NORM' POSITION. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT RELAY 3351-K1 AND 3351-K2. C/W EMERGENCY LIGHT OP S CHECK IAW Q400 AMM TASK 33-51-00-710-801. ALL OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102600044 20071026 00044 NM 2007 10 26 QXEA200701596 1 20071006 A 3350 LIGHT BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 415QX 4081 GEG FLIGHT NR 2463: EMERGENCY LIGHT 'ON' IN ARMED POSITION. MAINTENANCE CYCLED SHIPS POWER. EMERGENCY LIGHT SYSTEM WOR KS NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102600045 20071026 00045 NM 2007 10 26 QXEA200701597 1 20070923 A 3350 LIGHT BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 415QX 4081 BOI FLIGHT 2403: EMERGENCY LIGHTS 'ON' WHEN 'ARMED'. MAINTENANCE CYCLED EMERGENCY LIGHTS CIRCUIT BREAKERS. OPS CHECK N ORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102600046 20071026 00046 NM 2007 10 26 QXEA200701598 1 20071021 A 2130 VALVE BOMBDR DHC8 DHC8402 1390042 NM CABIN PRESSURE MALFUNCTIONED A QXEA O OTHER E VIBRATION/BUFFET CL CLIMB 1 NM 09 414QX 4061 BOI FLIGHT NR 2403: AIRCRAFT CLIMBED-OUT UNPRESSURIZED TO 10,000 FT. AFTER 5 MINUTES THERE WAS A THUD FROM THE FWD CABI N AND THE AIRCRAFT PRESSURIZED RAPIDLY. REST OF FLIGHT WAS NORMAL. MAINTENANCE PERFORMED OPS CHECK OF PRESSURE CONTROL IN MANUAL MODE IAW MM TASK 21-31-00-710-803. OPS CHECK GOOD. PERFORMED FUNCTIONAL CHECK OF PRESSURE CONTROL IAW MM TA SK 21-31-00-720-801. OPS CHECK GOOD. VERIFIED CLEANLINESS OF FWD SAFETY VALVE, NO DEFECTS NOTED. DUE TO TEMP AND WEAT HER, SUSPECT ICE. VERIFIED MCD AND AFT CARGO DOOR SEALS FOR LEAKS, NO DEFECTS NOTED. INTERROGATED CDS PRESSURIZATION WITH NO FAULTS FOUND. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102600048 20071026 00048 EA 2007 10 26 A6WA200740553 1 20070929 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 411ZW 7569 RIGHT SIDE UNDER FLOORBEAM HAS A CRACKED ATTACH ANGLE AT THE OUTBOARD SIDE OF RBL 27, FS 484, WL 70.73. (M) MAINTENANC E PERFORMED REPAIR TO RT SIDE FLOOR SUPPORT INTERCOSTAL ATTACH ANGLE OUTBOARD SIDE OF RBL 27 FS 484 IAW BSC SR 601R-53-0 029B AND CRJ 200 SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007102600049 20071026 00049 EA 2007 10 26 A6WA200740554 1 20070929 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 411ZW 7569 FOUND LEFT SIDE UNDER FLOORBEAM HAS A CRACKED ATTACH ANGLE AT THE OUTBOARD SIDE OF LBL 27, FS 484, WL 70.73. (M) MAINT ENANCE REMOVED CRACKED ANGLE, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW BSC SR 601R-53-0029B. (M) 2 L 7 2 4F RT A21EA 2007102600056 20071026 00056 WP 2007 10 26 07FDEA04665 1 20071024 A 5347 WSP0846503 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 FOUND 1 CRACK 4" ON SEAT TRACK AT STA 635 X= 67 CUT APPROX AT STA 666 AND 624 AND REPAIR IAW SRM 53-70-00 VOL 1 FIG 1 AN D FIG 11. 2 L 7 3 4F A22WE 2007102600057 20071026 00057 WP 2007 10 26 07FDEA04666 1 20071024 A 5320 AFA31661 ANGLE DOUG DC10 DC1010 3022110 WP ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 371FE 46609 EXFOLIATION CORROSION ON CAP ANGLE AT STA 1561 L NR 52 REPAIR IAW SRM 53-30-00 VOL 1 FIG 8 SHEET 1. 2 L 7 3 4F A22WE 2007102600059 20071026 00059 WP 2007 10 26 07FDEA04668 1 20071024 A 5510 NLC6043504 HINGE DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 HINGE ASSY ITEM 360 BROKEN (REF IPC 55-22-02-01). REPLACED LATCH IAW FEDEX STD REWORK DWG SR10-55-501. 2 L 7 3 4F A22WE 2007102600060 20071026 00060 WP 2007 10 26 07FDEA04669 1 20071024 A 5730 ARB1231503 SKIN DOUG DC10 DC1010 3022110 WP ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 LT WING L/E SKIN LOWER SLAT TRACK CUT OUT NR 8 AT STA XOS 549 EXISTING REPAIR. REPLACED REPAIR PER SRM 57-10-00 VOL.1 F IG 68. 2 L 7 3 4F A22WE 2007102600062 20071026 00062 WP 2007 10 26 07FDEA04671 1 20071024 A 5320 NCA6048105 STIFFENER DOUG DC10 DC1010 3022110 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 VANE AIR CONDITION COMPARTIMENT LT PACK N°2 INTERNAL SIDE STA 475 TEE P/N NCA6048-105 WITH CRACK 4 INCH. REPAIRED STIFF ENER FOR SRM 53-40-00 FIG 10 VOL I. 2 L 7 3 4F A22WE 2007102600063 20071026 00063 NM 2007 10 26 07FDEA04672 1 20071024 A 5311 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 526FE 48600 MAIN DECK CARGO COMPARTMENT, RIGHT STA 1721 FRAME AT ABOUT STRINGER 12R AREA FOUND DENT. 11-05-07 CARRIED OUT REPA IR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CATEGORY B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTIONS AT EVERY 9,500 CYCLES. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007102600065 20071026 00065 NM 2007 10 26 07FDEA04674 1 20071024 A 5311 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 526FE 48600 MAIN DECK CARGO COMPARTMENT, RIGHT STA 1681 FRAME AT ABOUT STRINGER 12R AREA FOUND DENT. 11-05-07 CARRIED OUT RE PAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CATEGORY B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WIT H REPETITIVE INSPECTION AT EVERY 9,500 CYCLES. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007102600067 20071026 00067 EU 2007 10 26 07FDEA04676 1 20071024 A 5320 A5397425920200 FLOOR SUPPORT AIRBUS 310 A310222 3930315 EU CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 AFT PIT FLOOR BOARD SUPPORT ANGLE AT LBL50 FRAME 64-65 IS CORRODED FOUND SUPPORT AND FITTING CORRODED AND CRACKED OUT OF LIMITS IAW A310 SRM 53-10- 00 TABLE 102; REMOVED AND REPLACED SUPPORT AND FITTING IAW A310 SRM 51-40-21, 53-17-15 PGA1 3,FIG 9, 51-40-44. 2 L 7 2 4F RT A35EU 2007102600069 20071026 00069 EA 2007 10 26 A6WA200740561 1 20071003 A 5210 PANEL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 411ZW 7569 PAX DOOR STAIR AFT SIDE PANEL IS CRACKED IN ZONES 2 AND 3 APPROX .250 INCH LONG IN RADIUS. MAINTENANCE REPAIRED ZONES 2 AND 3 ON PAX DOOR AFT SIDE PANEL IAW BOMBARDIER REO 601R-52-11-702 AND BSC EO 601R-52-13410. (M) 2 L 7 2 4F RT A21EA 2007102600070 20071026 00070 EA 2007 10 26 A6WA200740562 1 20071003 A 5210 PANEL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 411ZW 7569 PAX DOOR STAIR FORWARD SIDE PANEL IS CRACKED IN ZONE 2 AND 3 APPROX .250 INCH LONG IN RADIUS. MAINTENANCE REPAIRED ZONE S 2 AND 3 ON PAX DOOR FORWARD SIDE PANEL IAW BOMBARDIER REO 601R-52-11-702 AND BSC EO 601R-52-13411A. (M) 2 L 7 2 4F RT A21EA 2007102600071 20071026 00071 EA 2007 10 26 A6WA200740563 1 20071008 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 499 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 411ZW 7569 FOUND RIGHT PRESSURE FLOOR SILL PLATE ANGLE AT FS 499, RBL 43 CORRODED, APPROX .750 INCH DIAMETER. MAINTENANCE FOUND CO RROSION TO BE LIGHT REMOVED APPROX .002 INCH MATERIAL IAW CRJ SRM 51-21-06 3B 1-5. (M) 2 L 7 2 4F RT A21EA 2007102600072 20071026 00072 EA 2007 10 26 A6WA200740564 1 20071008 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 461 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 411ZW 7569 RIGHT PRESSURE FLOOR SILL PLATE ANGLE AT FS 461, RBL 43 CORRODED APPROX .750 INCH DIAMETER. MAINTENANCE FOUND CORROSION TO BE LIGHT. REMOVED APPROX .002 INCH MATERIAL IAW CRJ 200 SRM 51-21-06 3B 1-5. (M) 2 L 7 2 4F RT A21EA 2007102600073 20071026 00073 EA 2007 10 26 A6WA200740565 1 20071008 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 499 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 411ZW 7569 LT PRESSURE FLOOR SILL PLATE ANGLE AT FS 499.0, LBL 43 CORRODED APPROX .750 INCH DIAMETER. MAINTENANCE FOUND CORROSION TO BE LIGHT. REMOVED APPROX .022 INCH MATERIAL IAW CRJ SRM 51-21-06 3B 1-5. (M) 2 L 7 2 4F RT A21EA 2007102600074 20071026 00074 EA 2007 10 26 A6WA200740566 1 20071008 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 544 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 411ZW 7569 LEFT PRESSURE FLOOR SILL PLATE ANGLE AT FS 544, LBL 43 CORRODED APPROX .750 INCH DIAMETER. MAINTENANCE FOUND CORROSION TO BE LIGHT. REMOVED APPROX .002 INCH MATERIAL IAW CRJ SRM 51-21-06 3B 1-5. (M) 2 L 7 2 4F RT A21EA 2007102600075 20071026 00075 EA 2007 10 26 A6WA200740577 1 20070925 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 468AW 7916 RIGHT LOWER WING PLANK FUEL PANEL CUT OUT FOR PANEL 640BB HOLE NR 1 HAS MINOR CORROSION IN NON-CRITICAL AREA APPROX .003 INCH DEEP. MX REPAIRED RIGHT LOWER WING PLANK FUEL PANEL CUT OUT FOR PANEL 640BB HOLE NR 1 IAW AIR WISCONSIN E06/021/4 57 AND BOMBARDIER REO 601R-57-21-030 REV F. (M) 2 L 7 2 4F RT A21EA 2007102600076 20071026 00076 EA 2007 10 26 A6WA200740575 1 20070925 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 468AW 7916 LT LOWER WING PLANK FUEL PANEL CUTOUT FOR PANEL 510AB HOLE NR 2 HAS MINOR CORROSION IN NON-CRITICAL AREA APPROX .003 INC H DEEP. MAINTENANCE REPAIRED LT LOWER WING PLANK FUEL PANEL CUT OUT FOR PANEL 510AB HOLE NR 2 IAW AIR WISCONSIN E06/021 /457 AND BOMBARDIER REO 601R-57-21-030 REV F. (M) 2 L 7 2 4F RT A21EA 2007102600080 20071026 00080 NM 2007 10 26 AMTA200700483 1 20070106 A 2150 58489991 DOOR BOEING 737 73783N 13844HI NM A/C PACK BYPASS MALFUNCTIONED A AMTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 315TZ 28245 LT PACK TRIP LIGHT ON TAKE OFF ROLL. RESET OK AFTER CLEAN UP. INSTALLED NEW LT PACK FAN BYPASS CHECK VALVE DOOR. OPS CHECK NORMAL. OK FOR SERVICE. (K) 2 L 7 2 4F RT A16WE 2007102600081 20071026 00081 NM 2007 10 26 PIDR07010 1 20071012 A 5320 SUPPORT BRACKET BOEING 737 737301 1384611 NM BS 440 S9R CRACKED B PIDR K NONE O OTHER IN INSP/MAINT 1 SO 05 XAVIV 23560 DURING C CHECK, FOUND CRACK AT THE IB FASTENER FOR THE CABIN AIR CONDITIONING OUTLET SUPPORT BRACKET AT BS440 JUST ABOVE STR 9RT. REPAIRED PER SB 737-53-1216. 2 L 7 2 4F RT A16WE 2007102600083 20071026 00083 NM 2007 10 26 PIDR07013 1 20071012 A 5310 CREASE BEAM BOEING 737 737301 1384611 NM BS 180 CRACKED B PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 XAVIV 23560 DURING C CHECK, FOUND CRACK AT THE END OF THE LT SIDE CREASE BEAM AT BS 180. REPAIRED IAW SRM 51-70-12 AND SRM 51-40-01 . 2 L 7 2 4F RT A16WE 2007102600084 20071026 00084 NM 2007 10 26 PIDR07009 1 20071010 A 5330 SKIN BOEING 737 737301 1384611 NM BS 727E-747 S21R CRACKED B PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 XAVIV 23560 DURING C CHECK, FOUND CRACK IN THE CHEM-MILL POCKET OF FUSELAGE SKIN AT STR 21RT. BETWEEN BS727E AND BS747. REPAIRED IA W SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2007102600085 20071026 00085 NM 2007 10 26 PIDR07011 1 20071012 A 5320 SUPPORT BRACKET BOEING 737 737301 1384611 NM BS 440 S9L CRACKED B PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 XAVIV 23560 DURING C CHECK, FOUND CRACK AT THE IB FASTENER FOR THE CABIN AIR CONDITIONING OUTLET SUPPORT BRACKET AT BS 440 JUST ABOV E STR 9LT. REPAIRED IAW SB 737-53-1216. 2 L 7 2 4F RT A16WE 2007102600087 20071026 00087 CE 2007 10 26 DXTA200702551 1 20071018 A 3240 195183 SHUTTLE VALVE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG DEFECTIVE E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 374QS 5600475 CAPT AND FO'S BRAKES ARE SPONGY. PEDALS REQUIRES MORE THAN USUAL PRESSURE TO ACHIEVE BRAKING ACTION. REMOVED DEFECTIVE RT BRAKE SHUTTLE VALVE , INSTALLED SHUTTLE VALVE IAW CMM 32-46-43. OPERATIONAL AND LEAK CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2007102600089 20071026 00089 SW 2007 10 26 EVAC010192007 1 20071019 A 5100 UNKNOWN BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL SMOKE E EVCA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 03 133AE 45280 CAE896520 EXCESSIVE SMOKE FROM EXHAUST ON SHUTDOWN. 1 G 7 1 3U 3 U H2SW E1GL 2007102600092 20071026 00092 NM 2007 10 26 ASMF200710003 1 20071018 A 2750 4034241974 COMPUTER DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE RIGHT INOPERATIVE W ASMF O OTHER J WARNING INDICATION CR CRUISE 1 SW 23 160PL 16344 49763 CAPTAIN REPORTED THE RT ENGINE BELOW LIMITS DURING DESCENT ON IDLE; LT FUEL TEMPERATURE WAS MORE THAN 10 DEGREES LOWER A GAINST THE RT ONE, THE LAPS OVERSPEED WARNING ACTIVATED DURING SLATS EXTENSION AT 275 KNOTS AND DURING FINAL APPROACH TH E ATS DISENGAGED LIGHT CAME ON OCCASIONAL IN ALL FLAP, LANDING WITH 28. MAINTENANCE PERSONNEL PERFORMED TRIM TO RT ENGI NE IAW MM 71-00-00; FUEL TEMPERATURE DIFFERENCE WAS DEFERRED IAW MEL 73-2 CAT C; OVERSPEED SLATS AND FLAPS CHECK WAS PER FORMED IAW MM 05-51-06 NO STRUCTURAL DAMAGE WAS FOUND; DFGC NR 2 WAS REPLACED IAW MM 22-01-01 AND RETURN TO SERVICE TES T WAS PERFORMED IAW MM 22-01-05, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2007102600099 20071026 00099 CE 2007 10 26 GLBA20061015 1 20071015 A 5311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA BS 451 S10R CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 247GL UE247 FRAME AT FS 451.0 CRACKED AT STRINGER 10R RELIEF CUTOUT CRACK IS .6250 IN LONG. MAINTENANCE REPAIRED FRAME FLANGE AT FS 451.0 IAW 1900D SRM 51-70. REPAIR APPROXIMATELY 6 INCH BY 2 INCH 2024 T3 .063. RII COMPLIED WITH IAW TASKCARD 8.2.1. 2 L 7 2 4T 3 T RT A24CE E2NE 2007102600101 20071026 00101 NE 2007 10 26 ASMF200710005 2 20071019 A 7200 GE9094B ENGINE BOEING 777 777* UTILUSE NM GE GE90 GE9085B 30044 NE LEFT OVERTEMP W ASMF C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SW 23 746AM 7217 32719 900481 CAPTAIN REPORTED THAT DURING TAKEOFF RUN THE LT ENGINE EGTS INDICATION EXCEEDED RED DIAL; CAPTAIN REDUCED THE THRUST REC OVERING NORMAL INDICATIONS. AT CDG, MAINTENANCE DETERMINED THAT EXCEED WAS WITHIN LIMITS IAW MM 71-00-00-613, REQUIRING BOROSCOPIC INSPECTION WITHIN 10 CYCLES. LATER, FIM PROCEDURE 73-22 TASK 819 WAS PERFORMED TO THE LT ENGINE AND OVER TEMP ERATURE BOROSCOPIC INSPECTION WAS PERFORMED IAW MM 71-00-00-200-814-G00 AND 72-00-00-290-812G00, NO DAMAGES WERE FOUND. LT ENGINE WAS WASHED IAW MM 72-00-00-100-807-G00, AND THE POWER CHECK NR 7 WAS PERFORMED IAW MM 71-00-00-700-807-G00, AL L CORRECT. 2 L 7 2 4F 4 F RT T00001SE E00049EN 2007102600102 20071026 00102 EU 2007 10 26 TRBA2007087 1 20071019 A 3350 7012210 LAMP AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE EMERGENCY LIGHT INOPERATIVE A TRBA O OTHER O OTHER NR NOT REPORTED 1 SO 29 414WF 414 EMERGENCY LIGHT IN MAIN CABIN DOOR INOPERATIVE. RELAMPED MAIN CABIN DOOR EMERGENCY LIGHT. 2 H 7 2 4T 4 T RT A53EU E20NE 2007102600103 20071026 00103 2007 10 26 ANCF200700025 4 20071019 A 2210 6224717004 CONTROL PANEL BOEING 757 757236 1384971 NM RROYCE RB211 RB211535E4 54555 NE AFCS MALFUNCTIONED W ANCF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 521NA 25592 A/T FAILED TO ENGAGE WHEN EPR MODE SELECTED ON T/O THE EPR SW DID NOT ENGAGE. THE T/O WAS DISCONNECTED, IAW MCC THE PR OCEDURE FOR T/O WILL PERFORM MANUALLY A SECOND ATTEMPT WAS MADE AND THE TIME TO ENGAGE THE AUTOPILOT INFLIGHT DID NOT E NGAGE L,C OR R. IAW AMM 22-11-02/201 THE AFCS CONTROL PANEL WAS REPLACED AND PERFORMED TEST MCDP GROUND 04 MCP IAW AMM 22-00-02/201 AND 22-11-02/207 IS SATISFACTORY. 2 L 7 2 4F 4 F RT A2NM E12EU 2007102600104 20071026 00104 NM 2007 10 26 ANCF200700023 1 20071016 A 2910 PACKING DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE HYD SYSTEM BROKEN W ANCF O OTHER K FLUID LOSS LD LANDING 1 SO 23 632CT 49632 DURING APP AT BOG, R HYD QTY DROPPED TO 1 QT WITH THE SYSTEMS PRESSURIZED. THERE WAS NOT R HYD QTY ANNU ON THE EOAP. (T HIS CAUSES EMERGENCY LANDING) SEVERE HYD LEAK FOUND AT FWD OUTLET LINE FITTING OF MOTOR OPERATED DUAL SHUTOFF VALVE. DU RING INSPECTION FITTING PACKING WAS FOUND BROKEN AND THE FITTING LOOSE. FOLLOWING AMM 29-10-08 P201 NEW TTING AND PACKIN G INSTALLED. REMAINING LINES VERIFIED FOR PROPER ADJUSTMENT. 2 L 7 2 4F 4 F RT E9NE 2007102600147 20071026 00147 NM 2007 10 26 2007UALA03894 1 20070924 A 3397 7956185 CIRCUIT BREAKER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 ROWS 22 AND 26 LEFT SIDE EEL ARE INTERMITTENT. RESET EMERGENCY LIGHT LOGIC CIRCUIT BREAKERS AND OP CHECKED EMERGENCY LI GHT SYS. CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102600148 20071026 00148 NM 2007 10 26 2007UALA03899 1 20070926 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY EXIT LIGHTS INOP AT ROW 5R CEILING & UPPER DECK CEILING AT ROW 12. *S/D* RELAMPED BOTH CEILING LOCATIONS. E EL OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102600149 20071026 00149 NM 2007 10 26 2007UALA03900 1 20070926 A 3350 9F19948501 SIGN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE R3 DOOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY EXIT EEL LIGHT INOP AT ACROSS DOOR 3 RIGHT LOWER WALL AISLE. *S/D* REPLACED EEL SIGN ACROSS DOOR 3, RIGHT LO WER WALL. OP CHECKS GOOD FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102600150 20071026 00150 NM 2007 10 26 2007UALA03901 1 20070926 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 55 ABC INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY EXIT EEL LIGHT INOPERATIVE AT SEAT 55 ABC. *S/D* REPLACED EEL LIGHT, OP CHECKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102600152 20071026 00152 NM 2007 10 26 2007UALA03904 1 20070925 A 3350 20131A POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EXIT LIGHTS FLASHING BETWEEN SEATS 22 TO 26. *S/D* REPLACED POWER SUPPLY AT DOOR 2L FOR ROWS 22-26AB. GROUN D CHECKS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102600153 20071026 00153 NM 2007 10 26 2007UALA03925 1 20070926 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SEAT 1H FWD EEL OUT OF POSITION A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 664UA 29236 THE 1H EMERGENCY LIGHT STRIP FELL OFF. *S/D* REPLACED LIGHT ASSY AT SEAT 1H, FWD. EEL OP CHECKED GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102500005 20071025 00005 NM 2007 10 25 AALA20071964 1 20071001 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 975AN 29549 TUL - EMERGENCY LIGHTS AT AFT FIRST CLASS AND RIGHT COACH INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AF T FIRST CLASS AND RIGHT COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007102600002 20071026 00002 2007 10 26 A6WA200740544 4 20070922 A 3417 ADC CNDAIR CL600 CL6002B19 1900309 EA NR 2 MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 428AW 7695 AIR RETURN, AFTER TAKEOFF RECEIVED AIRSPEED, ALTITUDE, HEADING MESSAGES ON PFD2, COMPLIED WITH QRH FOR EACH AS WELL AS A DC FAILURE. REPLACED NR 2 ADC USING AMM 34-13-01. PERFORMED OPS CHECK OF ADC NR 2 USING AMM 34-13-01-710-801 CHECK GOO D. PERFORMED FUNCTIONAL CHECK OF PITOT/STATIC SYSTEM USING AMM 34-11-00-720-801, CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2007102600003 20071026 00003 EA 2007 10 26 A6WA200740569 1 20070926 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 LT LOWER WING PLANK HAS MINOR PITTING DAMAGE IN A NON-CRITICAL AREA .001-.002 DEEP AT WING ACCESS PANEL 540BB. MAINTENA NCE REPAIRED LT LOWER WING PLANK IAW BOMBARDIER REO 601R-57-21-030 REV F. (M) 2 L 7 2 4F RT A21EA 2007102600011 20071026 00011 EU 2007 10 26 HYIA12122 1 20071011 A 5347 S5357020120002 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 LEFT INBOARD SEAT TRACK BETWEEN FRAMES 23 AND 29 IS CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS LI MITS. REMOVED AND REPLACED SEAT TRACK IN ACCORDANCE WITH SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007102600021 20071026 00021 EU 2007 10 26 HYIA12133 1 20071011 A 5320 S53672350202 THRESHOLD AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 LEFT THRESHOLD BETWEEN FRAMES 36 AND 39 CORRODED. CORROSION WAS REMOVED AND FOUND TO BE BEYOND MANUFACTURERS LIMITS. R EMOVED AND REPLACED THRESHOLD IN ACCORDANCE WITH SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007102600023 20071026 00023 EU 2007 10 26 HYIA12135 1 20071011 A 5315 S53672406208 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 FOUND FLOORBEAM AT FRAME 36 IS CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS LIMITS. REMOVED AND RE PLACED FLOORBEAM IN ACCORDANCE WITH 51-25-01. 2 H 7 2 4T RT A53EU 2007102600038 20071026 00038 EA 2007 10 26 A6WA200740550 1 20071001 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 411ZW 7569 FOUND FS 280 FLOORBEAM CLIP AT RBL 9.0, INBOARD, IS CRACKED IN RADIUS APPROX .50 INCH LONG. (M) MAINTENANCE REMOVED CR ACKED SLIP AND INSTALLED NEW CLIP P/N 601R31113-58 IAW BSC SR 601R-53-0057A AND CRJ SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007102600041 20071026 00041 EA 2007 10 26 A6WA200740552 1 20071001 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 280 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 411ZW 7569 PILOTS BULKHEAD FS 280 HAS CORROSION APPROX .010 INCH DEEP BETWEEN LBL 9.0 AND RBL 9.0 AT WL 73.10. (M) MAINTENANCE IN STALLED NEW ANGLE IAW CRJ SRM 51-42-06 AND 51-42-13. (M) 2 L 7 2 4F RT A21EA 2007102600042 20071026 00042 NM 2007 10 26 QXEA200701594 1 20071012 A 3350 LIGHT BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 415QX 4081 PDX FLIGHT NR 2311: EMERGENCY LIGHTS ACTIVE IN THE ARM POSITION. MAINTENANCE CYCLED SHIPS POWER. EMERGENCY LIGHT CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102600050 20071026 00050 EA 2007 10 26 A6WA200740555 1 20070929 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 411ZW 7569 FOUND LEFT AND RIGHT FS 621 TO 625 OBLIQUE ANGLES ARE CRACKED. MAINTENANCE REMOVED CRACKED ANGLES AND INSTALLED NEW ANG LES P/N 601R-35012-51, 601-35012-52 IAW CRJ SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007102600052 20071026 00052 EA 2007 10 26 A6WA200740560 1 20071006 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 319 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 411ZW 7569 FOUND SERVICE DOOR LOWER SILL JOINT BRACKET P/N 601R38335-1 CORRODED AT FS 319.70 WL 73. MAINTENANCE REPLACED LOWER SIL L JOINT ANGLE ON SERVICE DOOR IAW CRJ 200 SRM 51-42-06, 51-42-21 AND BSC EO 601R-53-13486. (M) 2 L 7 2 4F RT A21EA 2007102600053 20071026 00053 NM 2007 10 26 C1HA200796013 1 20071021 A 2750 FLAP SYSTEM BOEING 727 7272J4 1384006 NM NR 6 MALFUNCTIONED A C1HA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 GL 15 696CA 22574 UPON FLAP RETRACTION LE FLAP NR 6 DID NOT RETRACT. DISPATCH AND MC NOTIFIED. RETURN TO STL, REMOVED AND REPLACED NR 6 FLAP ACT IAW 27-81-22. OPS AND LEAK CK NORMAL. 2 L 7 3 4F RT A3WE 2007102600055 20071026 00055 WP 2007 10 26 07FDEA04664 1 20071024 A 5713 STRINGER DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 RT WING L/E INTERNAL STRUCTURE FOUND 1 CRACK 0,75" LONG ON FIXED TEE AT XOS 906 REPAIR WING LOWER L/E STRINGER DOUBLER I AW SRM 57-10-00 FIG 49 VOL 1. 2 L 7 3 4F A22WE 2007102600058 20071026 00058 WP 2007 10 26 07FDEA04667 1 20071024 A 5320 AFA31651 ANGLE DOUG DC10 DC1010 3022110 WP ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 371FE 46609 CTR CARGO COMPT EXFOLIATION CORROSION ON CAP ANGLE AT STA 1541 L NR 52 REPAIR CAP IAW SRM 53-30-00 VOL 1 FIG 8 SHEET 1. 2 L 7 3 4F A22WE 2007102600064 20071026 00064 NM 2007 10 26 07FDEA04673 1 20071024 A 5311 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 526FE 48600 MAIN DECK CARGO COMPARTMENT, RIGHT STA 1701 FRAME AT ABOUT STRINGER 12R AREA FOUND DENT. 11-05-07 CARRIED OUT RE PAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CATEGORY B REPAIR, INITIAL INSPECTION IS REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTIONS AT EVERY 9,500 CYCLES. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007102600066 20071026 00066 NM 2007 10 26 07FDEA04675 1 20071024 A 5311 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 526FE 48600 MAIN DECK CARGO COMPARTMENT, LEFT STA 1761 FRAME AT ABOUT STRINGER 12R AREA FOUND CRACKED. 11-07-07 MAIN DECK CA RGO COMPARTMENT - LEFT HAND STA 1761 FRAME AT STRINGER 12L CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 3 VOLUME I. DUE TO CATEGORY B REPAIR, INITIAL INSPECTION REQUIRED AT 12,000 CYCLES WITH REPETITIVE INSPECTIONS AT EVERY 8,000 CYCLES. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007102600077 20071026 00077 EA 2007 10 26 A6WA200740576 1 20070925 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 468AW 7916 RIGHT LOWER WING PLANK FOR FUEL PANEL 650AB CUT OUT HOLE NR 9 HAS MINOR CORROSION IN NON-CRITICAL AREA APPROX .003 INCH DEEP. MAINTENANCE REPAIRED RT LOWER WING PLANK FOR FUEL PANEL 650AB CUT OUT HOLE NR 9 IAW AIR WISCONSIN E06/021/457 AND BOMBARDIER REO 601R-57-21-030 REV F. (M) 2 L 7 2 4F RT A21EA 2007102600091 20071026 00091 NM 2007 10 26 G6OA200700008 1 20071013 A 3241 ANTI-SKID SYS DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE BRAKES INOPERATIVE A G6OA O OTHER O OTHER LD LANDING 1 EA 27 701GC 48434 ON TOUCHDOWN RT BRAKE SYSTEM INOP. NR 10 TIRE THERMAL DISCHARGE, NR 10 BRAKE OVERTEMP. 2 L 7 3 4F 4 F RT A22WE E31N3 2007102600151 20071026 00151 NM 2007 10 26 2007UALA03902 1 20070925 A 3350 78671 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY LIGHT SEAT 38 ABC INOPERATIVE. REPLACED LAMP, EEL OP CHECKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102600158 20071026 00158 NM 2007 10 26 2007UALA04260 1 20071015 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 524UA 24977 MID CABIN EEL LIGHT BAR AT MID LAV INOPERATIVE. 11-01-07 REPLACED LIGHT BAR, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007102600159 20071026 00159 NM 2007 10 26 2007UALA04261 1 20071015 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE BS 1360 S27R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 665UA 29237 RT FUSELAGE APPROX 20 INCHES AFT OF AFT CARGO DOOR STA 1360 STR 27 HAS DAMAGE. ACCOMPLISHED REPAIR PER EVA-70734A AND SRM 53-00-01 FIG201. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102600160 20071026 00160 NM 2007 10 26 2007UALA04263 1 20071015 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 670UA 29240 ROW 15 AFT RIGHT SIDE OVERHEAD EMERGENCY FLOOD LIGHTS INOP. 11-01-07 RELAMPED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102600161 20071026 00161 NM 2007 10 26 2007UALA04264 1 20071015 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SEAT ROW 17AB IMPROPER PART A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 670UA 29240 UPON ARRIVAL FOUND SEAT EEL ROW 17AB FULL ORANGE, SHOULD BE HALF GREEN. 11-01-07 R & R LIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102600162 20071026 00162 NM 2007 10 26 2007UALA04265 1 20071016 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EEL INOP ROWS 35-44 LEFT & EMERGENCY EXIT SIGN INOP DOOR 3L FWD. 11-01-07 REPLACED CABLE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102600163 20071026 00163 NM 2007 10 26 2007UALA04266 1 20071016 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EEL INOP DOOR 4L LOWER GALLEY WALL. 11-01-07 SECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102600164 20071026 00164 NM 2007 10 26 2007UALA04267 1 20071016 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 52R INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EEL INOP ROW 52R. 11-01-07 RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102600165 20071026 00165 NE 2007 10 26 2007UALA04269 2 20071016 A 7314 PUMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUEL FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 642UA 25092 FLIGHT DIVERTED DUE TO LOSS OF RIGHT MAIN FUEL PUMPS. PUMP CONNECTORS WHERE CROSSED. ALSO FOUND FOUND RIGHT AFT BOOST P UMP CKT BK R OUT C371 .REPLACED BREAKER,FOUND WIRE ARCHING ACCOUNT OF SCREW CROSS THREADED. PERFORMED OPS CHECK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102600166 20071026 00166 NM 2007 10 26 2007UALA04270 1 20071016 A 2130 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN PRESSURE UNKNOWN A UALA O OTHER O OTHER DE DESCENT 1 WP 29 377UA 24642 CABIN ALT CLIMBS WHEN AIRCRAFT DESCENDING ON APPROACH. 2 L 7 2 4F 4 F RT A16WE E21EU 2007102600168 20071026 00168 NM 2007 10 26 2007UALA04272 1 20071016 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 947-998 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 RIGHT AFT GALLEY CREASE BEAM UPPER SURFACE CORRODED BS 947-998. REMOVED AND INSTALLED REPLACEMENT CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E21EU 2007102600170 20071026 00170 NM 2007 10 26 2007UALA04274 1 20071016 A 3510 MC1019151 OXYGEN MASK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 F/O O2 MASK DEFECTIVE. REPLACED 2ND OBSERVERS O2 MASK ASSEMBLY. LEAK CHECKED GOOD PER AMM 35-11-18-401 ITEM 4. AC OK FO R SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102600171 20071026 00171 NM 2007 10 26 2007UALA04275 1 20071016 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 540 S26-27L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 FORWARD PIT FRAME AT STA 540 BETWEEN STR 26L AND 27L HAS DENT. MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING PRODUCTION SPLICE BETWEEN STR 23L-26L AND FABRICATED A NEW PRODUCTION SPLICE AND STRINGER CLIPS AND REPLACED SHEAR TIE -664 ABOVE STR-24L, 2 L 7 2 4F 4 F RT A2NM E17NE 2007112100002 20071121 00002 EA 2007 11 21 COMA0760636 1 20071109 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 821CA 7420 FLIGHT 5286 - AFTER LANDING WHEN THE FLAPS WERE RAISED TO 20 DEGREES, FLAPS FAIL CAUTION MESSAGE AND FLAPS STOPPED AT 35 DEGREES. DETERMINED THAT THE SKEW DETECTION SYSTEM CAUSED THE FLAP FAIL. DEFERRED SKEW DETECTION SYSTEM PER MEL 27-51 -03. FLAPS OPERATE NORMAL. 2 L 7 2 4F RT A21EA 2007102900002 20071029 00002 NM 2007 10 29 2007UALA04286 1 20071018 A 3040 HEATER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE WINDSHIELD MALFUNCTIONED A UALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 WP 29 853UA 1688 FLIGHT DIVERTED DUE TO CRACKLING/HOT WINDSHIELD & LACK OF FUEL TO REACH PLANNED DESTINATION. 11-01-07 WINDSHIELD CR ACKED DUE TO VARIANT HEATING ACROSS THE SURFACE (ELECTRICAL FAILURE) AND SEAL WAS LOOSE AND SLAPPING ACROSS NR 2 WINDOW . REPLACED SLIDING WINDSHIELD AND SEAL. CLEANED NR 2 WINDOW- NO DAMAGE WAS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007102900004 20071029 00004 NM 2007 10 29 2007UALA04288 1 20071017 A 3510 89151114 BOTTLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW OXYGEN LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 175UA 24382 CREW O2 PRESSURE SHOWS 1580. SERVICED CREW OXYGEN BOTTLE TO 1730 PSI. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102900007 20071029 00007 NM 2007 10 29 2007UALA04294 1 20071018 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 35 HJK INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 EEL INOP: SEAT 35 HJK. 11-01-07 REPLACED LIGHT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102900008 20071029 00008 NM 2007 10 29 2007UALA04295 1 20071018 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 COCKPIT CEILING EMERGENCY LIGHT INOP. RELAMPED 2 L 7 4 4F 4 F RT A20WE E24NE 2007102900010 20071029 00010 NM 2007 10 29 2007UALA04297 1 20071018 A 3250 METERING VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NLG STEERING MALFUNCTIONED A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 556UA 26650 A/C PULLS RT DURING TAXI. FOUND NLG DOES NOT CENTER. NEW NLG STEERING METERING VALVE INSTALLED AND RIGGING ACCOMPLI SHED BEFORE TEST RUN. 2 L 7 2 4F 4 F RT A2NM E17NE 2007102900011 20071029 00011 2007 10 29 2007UALA04298 4 20071017 A 2211 105E7206G3 COMPUTER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE AUTOPILOT UNKNOWN A UALA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 677UA 30029 AIRPLANE HAS PITCH OSCILLATION (PORPOISES) WITH ANY A-P CHANNEL IN CMD AND (V-S, ALT HOLD, FLCH, VNAV) MODE SELECTED. S USPECT THRUST MANAGEMENT COMPUTER. REPLACED THRUST MANAGEMENT COMPUTER, GROUND TEST OK. AUTOPILOT CAT III CKS GOOD. A CFT OK FOR SERVICE 2 L 7 2 4F 4 F RT A1NM E24NE 2007102900014 20071029 00014 NM 2007 10 29 2007UALA04173 1 20071010 A 2750 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FLAP HANDLE VIBRATES A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 570UA 26678 AT FLAPS 1 HANDLE IN DETENT ON CLIMBOUT LOUD VIBRATION FELT AND HEARD IN FLAP HANDLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007102900015 20071029 00015 2007 10 29 2007UALA04174 4 20071010 A 2565 GIRT BAR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT OVERWING BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 661UA 27158 RIGHT OVERWING SLIDE PACK RETENTION BAR CLAMP IS BROKEN AND COMPARTMENT DOOR LATCHES (4 EA) CORRODED AT WBL 97.9. SLIDE REPLACED ON JC 61960 4016. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102900016 20071029 00016 2007 10 29 2007UALA04175 4 20071010 A 2565 GIRT BAR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT OVERWING BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 661UA 27158 LEFT OVERWING SLIDE PACK RETENTION BAR CLAMPS BROKEN. SLIDE REPLACED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102900017 20071029 00017 EU 2007 10 29 2007UALA04176 1 20071011 A 2910 HOSE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN HYD SYS DAMAGED A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 401UA 435 FLIGHT LOST GREEN HYDRAULIC SYSTEM SOMETIME AFTER DEPARTING LCQ. DECLARED EMERGENCY WITH ATC. FOD DAMAGE IN WHEEL WELL . REPLACED THE RIGHT GEAR DOWNLOCK ACTUATOR HOSE. SERVICED GREEN HYDRO SYSTEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007102900019 20071029 00019 EU 2007 10 29 WRNA200700052 1 20070706 A 5343 TRUNNION AIRBUS 300 A300B4203 3930306 EU MLG CORRODED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 510TA 100 DURING M-96 CHECK, CORROSION WAS FOUND IN LT MAIN LANDING GEAR AFT TRUNNION FORWARD LUG FITTING BORE AND FACE. REMOVED CORROSION BY OVERSIZING BORE AND SPOT FACING THE LUG FACE AND INSTALLED NEW BUSHING IAW REPAIR DESIGN APPROVAL SHEET R AS/BAE/1005347/2007. 2 L 7 2 4F RT A35EU 2007102900024 20071029 00024 NM 2007 10 29 KCSA071480 1 20071021 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 570 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FWD PIT SEAT TRACK DAMAGED AT BS 570, RBL 46. 2 L 7 4 4F RT A20WE 2007102900026 20071029 00026 NM 2007 10 29 KCSA071482 1 20071021 A 5330 SKIN BOEING 747 7472B4B 138481B NM BS 555 S38R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FUSELAGE SKIN DAMAGED AT BS 555, STR 38R. 2 L 7 4 4F RT A20WE 2007102900027 20071029 00027 NM 2007 10 29 KCSA071483 1 20071021 A 5330 SKIN BOEING 747 7472B4B 138481B NM BS 1980 S33-37R CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FUSELAGE SKIN CORRODED AT BS 1980 BETWEEN STR 33R AND STR 37R. 2 L 7 4 4F RT A20WE 2007102900028 20071029 00028 NM 2007 10 29 KCSA071484 1 20071021 A 5312 STIFFENER BOEING 747 7472B4B 138481B NM BS 1265 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 CORROSION ON STIFFENER ON BOTTOM OF PRESSURE DECK AT BS 1265, LBL 78 TO LBL 114, WL 190. 2 L 7 4 4F RT A20WE 2007102900029 20071029 00029 NM 2007 10 29 KCSA071485 1 20071021 A 5311 FRAME BOEING 747 7472B4B 138481B NM BS 380 S17L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 BS 380 FUSELAGE FRAME CRACKED AT STR 17L CUTOUT. 2 L 7 4 4F RT A20WE 2007102900031 20071029 00031 EU 2007 10 29 WRNA200700055 1 20070629 A 5753 A5796005000400 RIB AIRBUS 300 A300B4203 3930306 EU TE FLAP UNSERVICEABLE A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 510TA 100 DURING M96 COMPLY WITH S/B A300-57-0245, REPLACEMENT OF LT INBOARD FLAP RIB NR 7. REMOVED LEFT WING INBOARD FLAP, RIB N R 7, PERFORMED HFEC INSPECTION IAW A300-57-0245, NO DEFECTS NOTED. INSTALLED NEW NR 7 RIB P/N A5796005000400 IAW S/B A3 00-57-0245. 2 L 7 2 4F RT A35EU 2007102900036 20071029 00036 NM 2007 10 29 UPS07M50946 1 20070924 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1321-1531 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C MAIN DECK: FROM BS 1321 TO BS 1531, ALONG-X=78 (RBL 78), SEAT TRACK CROWN AREAS, FLANGE AREAS & CROWN BASE AREAS FOUND CORRODED. CORROSION REMOVAL C/OUT ON SEAT/T AT STA 1321 TO 1371, FOUND EXCEEDED LIMIT PER SRM 53-70-0 0D, F3, V1, R35. REMOVAL C/OUT TO GAIN ACCESS & CORRODED SEAT/T REMOVED & NEW SEAT/T REWORKED PER SRM 53-70-00D, F3, V1 , R35. NEW SEAT/T HOLES P/UP C/OUT & INSTALLATION C/OUT PER SRM 51-31-01 & 51-33-0 1, V2, R35 AT STA 1301 TO 1371, FOUN D SATIS. 2 L 7 3 4F RT A22WE 2007102900038 20071029 00038 NM 2007 10 29 UPS07M50949 1 20070921 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C MAIN DECK: FROM STA 6-5 TO STA 6-10, ALONG X=9 (LBL 9), SEAT TRACK CROWN BASE AREAS FOUND CORRODED. CORROSION REMOVAL ON A/M AREAS C/OUT FOUND EXCEEDED LIMIT PER SRM 53-70 -00D, F3, V1, R35. TO GAIN ACCESS TO REMOVE COR RODED SEAT/T AND SPLICE SOS AS TO RWK, NEW SEAT/TRACK AND SPLICE PER SRM 53-70-00D, F1, V1, R35. HOLES PICKED UP SRM 51 -31-01 & 5121-01, V2, R35. NEW SEAT/T FROM STA 6-02 TO 1129 LBL 9, INSTALLED PER SRM 51-33-01 & 51-31-01, V2, R35. FOU ND SATIS. 2 L 7 3 4F RT A22WE 2007102900039 20071029 00039 NM 2007 10 29 UPS07M50950 1 20070923 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C MAIN DECK: FROM STA 6-5 TO 6-10, ALONG -X=9 (RBL 9), SEAT TRACK CROWN BASE & FLANGE AREAS FOUND CORRO DED. CORROSION REMOVAL C/OUT ON A/M AREAS FOUND EXCEEDED LIMIT, PER SRM 53-70-00D, F3, V1, R35. TO GAIN ACCESS TO REMO VE CORRODED SEAT/T & SPLICE AS WELL AS TO RWK NEW SEAT/T & SPLICE PER SRM 53-70-00D, F1, V1, R35. HOLES PICKED PER SRM 51-31-01 & 51-21-01, F1, V2, R35. NEW SEAT/T FROM STA 6-05 TO STA 1129, RBL 9 INSTALLED PER SRM 51-33-01 & 51-31-01, V2 , R35. FOUND SATIS. 2 L 7 3 4F RT A22WE 2007102900050 20071029 00050 NM 2007 10 29 CALA0700600 1 20071021 A 5320 6552878U124 ANGLE BOEING 737 7373T0 1384582 NM BS 907-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 907-1016, LBL 45. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40- 02. 2 L 7 2 4F RT A16WE 2007102900053 20071029 00053 NM 2007 10 29 ZZDA2007290 1 20070707 A 5330 SKIN BOEING 737 7377BD 1384511 NM BS 840 DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 313AT 33927 BELT LOADER STRUCK AFT CARGO BIN FUSELAGE DAMAGED. PERFORMED BOEING 737 SRM REPAIR BY REMOVING DAMAGE FROM AREA AND ATT ACHING DOUBLER AS OUTLINED IN SRM 53-00-01 REPAIR 1. 2 L 7 2 4F RT A16WE 2007102900056 20071029 00056 EU 2007 10 29 USAA920070960 1 20071015 A 5347 D53472190202 SEAT TRACK AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - CORROSION ON CABIN SEAT RAIL BEAM, BS 3158 / FR 66, +Y765. REPLACED CABIN SEAT RAIL BE AM, BS 3043 / FR 64 - BS 3158 / FR 66, +Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007102900057 20071029 00057 EU 2007 10 29 USAA920070961 1 20071016 A 5347 D53112782202 SEAT TRACK AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C-07 CHECK - CORROSION ON CABIN SEAT TRACK, BS 808 / FR 20, -Y765. REPLACED CABIN SEAT TRACK, BS 6 05 / FR 12 - BS 950 / FR 24, -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007102900058 20071029 00058 EU 2007 10 29 USAA920070962 1 20071019 A 5347 D53112815 SEAT TRACK AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C-07 CHECK - CORROSION ON CABIN SEAT TRACK, BS 709 / FR 16, +Y765. REPLACED CABIN SEAT TRACK, BS 6 05 / FR 12 - BS 950 / FR 24, +Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007102900059 20071029 00059 EU 2007 10 29 USAA920070963 1 20071019 A 5347 D5311278220000 SEAT TRACK AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C-07 CHECK - CORROSION ON CABIN SEAT TRACK, BS 709 / FR 16 - BS 808 / FR 20, -Y1292. REPLACED CABI N SEAT TRACK, BS 605 / FR 12 - BS 950 / FR 24, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007102900060 20071029 00060 EU 2007 10 29 USAA920070964 1 20071019 A 5347 D53112815200 SEAT TRACK AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C-07 CHECK - CORROSION ON CABIN SEAT TRACK, BS 709 / FR 16, +Y1292. REPLACED CABIN SEAT TRACK, BS 605 / FR 12 - BS 950 / FR 24, +Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007102900062 20071029 00062 EU 2007 10 29 USAA920070966 1 20071019 A 5320 D53112827201 DUMMY RAIL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C-07 CHECK - CORROSION ON CABIN DUMMY RAIL, BS 605 / FR 12 - BS 709 / FR 16, +Y503.2. REPLACED CAB IN DUMMY RAIL, BS 605 / FR 12 - BS 709 / FR 16, +Y503.2 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007102900063 20071029 00063 EU 2007 10 29 USAA920070967 1 20071013 A 5320 D53480043203 SILL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C-07 CHECK - CORROSION ON THE R2 DOOR CUTOUT LOWER SILL PREVIOUSLY REPAIRED AREA, BS 3101 / FR 65, -Y1732. REPAIRED THE R2 DOOR CUTOUT LOWER SILL, BS 3101 / FR 65, -Y1732 IAW A320 SRM 53-41-14. 2 L 7 2 4F RT A28NM 2007102900064 20071029 00064 EU 2007 10 29 USAA920070968 1 20071019 A 5320 D5347112420100 SHEAR PLATE AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C-07 CHECK - CORROSION ON CABIN SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70, -Y1732. REPLACED C ABIN SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70, -Y1732 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007102900069 20071029 00069 NM 2007 10 29 SWAA075201 1 20071021 A 5320 147A5507 FLOOR SUPPORT BOEING 737 7377H4 1384404 NM BS 995-1007 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 755SA 27871 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM WEB CORRODED BETWEEN BS 995 AND BS 1007, RBL 39. REMOVED AND REPLACED WEB PE R SRM. 2 L 7 2 4F RT A16WE 2007102900070 20071029 00070 NM 2007 10 29 SWAA075178 1 20071021 A 5512 182A4002 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 705SW 27839 DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 157.10. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007102900071 20071029 00071 NM 2007 10 29 SWAA075155 1 20071020 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007102900072 20071029 00072 NM 2007 10 29 SWAA075198 1 20071021 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007102900073 20071029 00073 NM 2007 10 29 SWAA075152 1 20071020 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 239WN 34714 EEPLS LENS MISSING AT ROW 11 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007102900075 20071029 00075 2007 10 29 SWAA075196 4 20071021 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 430WN 33659 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007102900077 20071029 00077 NM 2007 10 29 SWAA075180 1 20071021 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 504A-500D CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 504A AND BS 500D, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007102900081 20071029 00081 NM 2007 10 29 SWAA075177 1 20071021 A 5753 6546432 SKIN BOEING 737 7377H4 1384404 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 705SW 27839 DURING SCHEDULED HC2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SWA EA. 2 L 7 2 4F RT A16WE 2007102900082 20071029 00082 NM 2007 10 29 SWAA075186 1 20071021 A 5755 654645262A SKIN BOEING 737 7373H4 1384600 NM NR 5 SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED A2 CHECK, FOUND RT WING NR 5 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007102900084 20071029 00084 NM 2007 10 29 SWAA075193 1 20071021 A 5755 65465168A SPOILER BOEING 737 7373H4 1384600 NM LH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED A2 CHECK, FOUND LT WING NR 2 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007102900085 20071029 00085 NM 2007 10 29 SWAA075192 1 20071021 A 5755 65465168A SKIN BOEING 737 7373H4 1384600 NM NR 1 SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED A2 CHECK, FOUND LT WING NR 1 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007102900089 20071029 00089 NM 2007 10 29 SWAA075187 1 20071021 A 5755 65465168A SKIN BOEING 737 7373H4 1384600 NM NR 6 SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED A2 CHECK, FOUND RIGHT WING NR 6 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM . 2 L 7 2 4F RT A16WE 2007102900090 20071029 00090 NM 2007 10 29 SWAA075190 1 20071021 A 5755 65465170A SKIN BOEING 737 7373H4 1384600 NM NR 9 SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED A2 CHECK, FOUND RIGHT WING NR 9 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM . 2 L 7 2 4F RT A16WE 2007102900092 20071029 00092 NM 2007 10 29 SWAA075175 1 20071021 A 5311 6546526 FRAME BOEING 737 737317 138447P NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007102900094 20071029 00094 NM 2007 10 29 SWAA075161 1 20071021 A 5311 6546536 FRAME BOEING 737 7375H4 138449D NM BS 559 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007102900100 20071029 00100 NM 2007 10 29 SWAA075172 1 20071021 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 727B S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007102900105 20071029 00105 NM 2007 10 29 SWAA075171 1 20071021 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 727B S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007102900106 20071029 00106 NM 2007 10 29 SWAA075174 1 20071021 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 335 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 335, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007102900108 20071029 00108 NM 2007 10 29 SWAA075170 1 20071021 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 727B S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007102900109 20071029 00109 NM 2007 10 29 SWAA075179 1 20071021 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 847 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 18L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007102900110 20071029 00110 NM 2007 10 29 SWAA075195 1 20071021 A 5753 65C30462 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED 14Y CHECK, FOUND RT WING OUTBOARD FORE FLAP INBOARD END DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007102900112 20071029 00112 NM 2007 10 29 SWAA075160 1 20071021 A 5311 65C34355 FRAME BOEING 737 7375H4 138449D NM BS 482 S8L/R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007102900113 20071029 00113 2007 10 29 SWAA075184 4 20071021 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM R2 DOOR SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM. 2 L 7 2 4F RT A16WE 2007102900122 20071029 00122 NM 2007 10 29 ASAA0752126 1 20071017 A 2160 6240181 SENSOR BOEING 737 737890 1384527 NM TEMP CONTROL DIRTY A ASAA O OTHER J WARNING INDICATION CR CRUISE 1 NM 02 558AS 35177 AFT CABIN TEMP CONTROLLER WILL NOT MAINTAIN TEMPERATURE. WITH KNOB AT 2 O`CLOCK TEMP INDICATES 7 DEGREES. C DUCT SUPPL Y STABILIZES IN MANUAL MODE. VERIFIED TEMP CONTROL WITH TRIM AIR SWITCH SELECTED OFF. NO FAULTS LOGGED ON CONTROLLERS. 2 L 7 2 4F RT A16WE 2007102900125 20071029 00125 NM 2007 10 29 ASAA0792112 1 20071004 A 5315 FLOORBEAM BOEING 737 737990 NM BS 787 S26L/R CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 305AS 30013 AFT CARGO BAY TEE FITTING IS CORRODED AT BS 787 RBL 17 LBL 17. AFT CARGO PIT -TEE- AT BS 787 LBL 17 TO RBL 17 WAS REP LACED WITH MADE REPAIR PART IAW B737 900 SRM 51-40-02. 2 L 7 4 4F RT A16WE 2007102900126 20071029 00126 NM 2007 10 29 ASAA0792113 1 20071007 A 5320 INTERCOSTAL BOEING 737 737990 NM BS 727-767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 305AS 30013 AFT CARGO PIT RT INTERCOSTAL TRACK ZEE ANGLE FOUND CORRODED FROM BS 727 TO BS 767. AFT CARGO PIT RT INTERCOSTAL TRACK ( ZEE ANGLE) BS 727 TO BS 767 REPLACED WITH A MADE REPAIR PART IAW B737 900 SRM 53-00-53 FIG 202. 2 L 7 4 4F RT A16WE 2007102900131 20071029 00131 NM 2007 10 29 ASAA0742123 1 20071019 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7374Q8 138447Q NM BS 312 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 MAIN CABIN STA 312 LBL 12 RBL 20 FLOORBEAM HAS CORROSION ON TEE CAP. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW B7 3753 10 51 FIG 101 (SHEET 11 OF 16). REMOVED AND REPLACED UPPER CHORD IAW B737 SRM 53-10-51 FIG 2D (SHEET 1 4). 2 L 7 2 4F RT A16WE 2007102900132 20071029 00132 NM 2007 10 29 ASAA0792124 1 20071019 A 5320 146A75026 CHANNEL BOEING 737 737990 NM BS 727D-847 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 303AS 30016 AFT CARGO PIT RT ZEE CHANNEL BS 787 TO BS 727D+6 CORRODED. AFT CARGO PIT RT ZEE CHANNEL BS 787 TO BS 727D+6 REPLACED IA W B737 900 SRM 51-40-05 AND 51-40-02. 2 L 7 4 4F RT A16WE 2007102900133 20071029 00133 NM 2007 10 29 ASAA0792125 1 20071018 A 5320 146A75021 CHANNEL BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 303AS 30016 AFT CARGO PIT LT ZEE CHANNEL BS 847 TO BS 727 D+6 CORRODED. AFT CARGO PIT LT ZEE CHANNEL AT BS 847 TO BS 727D+6 REPLACE D WITH MADE REPAIR PARTS IAW B737 900 SRM 51-40-05 AND 51-40-02. 2 L 7 4 4F RT A16WE 2007102900135 20071029 00135 NM 2007 10 29 ASAA0792119 1 20071007 A 5320 143A7510 INTERCOSTAL BOEING 737 737990 NM BS 500I CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 305AS 30013 FWD CARGO PIT RT BAFFEL AT BS 500I RBL 21 BELOW RT ZEE CHANNEL IS CRACKED. BAFFEL AT RT FWD CARGO PIT AT BS 500G RBL 21 REPLACED WITH MADE REPAIR PART IAW B737 900 SRM 53-30-53 FIG 2 AND 51-40-02. 2 L 7 4 4F RT A16WE 2007102900136 20071029 00136 NM 2007 10 29 ASAA0792121 1 20071007 A 5320 146A7502 SILL BOEING 737 737990 NM BS 500A-500L CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 305AS 30013 FWD CARGO PIT RT SIDE STA 500A TO STA 500L DUST SILL HAS CORROSION ON TOP SURFACE FWD CARGO PIT RT SIDE STA 500F + 6 TO 500L. DUST SILL REPLACED IAW B737 900 SRM 53-00-53 FIG 202 REPAIR 5. 2 L 7 4 4F RT A16WE 2007102900137 20071029 00137 NM 2007 10 29 ASAA0792111 1 20071008 A 5512 186A385210001022 SKIN BOEING 737 737990 NM HORIZONTAL STAB DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 305AS 30013 RAMP REPORTS DENTS ON LT HORIZ STAB 2E 5FT FROM ROOT. REPAIRED IAW B737 900 SRM 55-10-01 REPAIR 1. 2 L 7 4 4F RT A16WE 2007102900138 20071029 00138 NM 2007 10 29 ASAA0792116 1 20071008 A 5712 115A29899 BULKHEAD BOEING 737 737990 NM LWS 201 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 305AS 30013 LEFT WING TRAILING EDGE BULKHEAD AT WBL 201 90 WEB ASSY CRACKED. WEB ASSY REPLACED WITH NEW PART IAW B737 900 SRM 51-40 -02. 2 L 7 4 4F RT A16WE 2007102900139 20071029 00139 NM 2007 10 29 ASAA0792117 1 20071007 A 5712 115A298210 BULKHEAD BOEING 737 737990 NM RWS 201 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 305AS 30013 RIGHT WING TRAILING EDGE BULKHEAD AT WBL 201.90 WEB ASSY CRACKED. WEB ASSY REPLACED WITH NEW PART IAW B737 900 SRM 51-4 0-02. 2 L 7 4 4F RT A16WE 2007102900147 20071029 00147 EA 2007 10 29 COMA0760599 1 20071011 A 2910 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NOSE HYD BAY FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 967CA 28329 7134 FLIGHT 5041 - RECEIVED NOSE GEAR DISAGREE WARNING ON APPROACH, AND "FAULTED" NOSE DOORS. DECLARED EMERGENCY, LANDED WIT HOUT INCIDENT. REPLACED NOSE GEAR SELECTOR VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007102900148 20071029 00148 EA 2007 10 29 COMA0760600 1 20071011 A 2750 860D10018ABCD CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 523CA 10031 7821 FLIGHT 5350 - RECEIVED FLAP FAIL CAUTION MESSAGE. DECLARED EMERGENCY, DIVERTED TO JFK, LANDED WITHOUT INCIDENT. REPLAC ED FECU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007103000038 20071030 00038 EA 2007 10 30 VNAA0710011 1 20071015 A 2133 OUTFLOW VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN PRESSURE MALFUNCTIONED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 229PS 7898 CREW REPORTED THE AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. CREW ELECTED TO RETURN TO DAY AND LANDED WITHOUT INCIDEN T. MAINTENANCE INSPECTED AND FOUND THE OVERBOARD EXHAUST VALVE IN THE OPEN POSITION. MAINTENANCE CLOSED THE OVERBOARD EXHAUST SHUT-OFF VALVE IN THE CLOSED POSITION AS PER THE MEL 21-24-06-2. AIRCRAFT PRESSURE CHECK WAS GOOD. AIRCRAFT WA S RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007103000039 20071030 00039 NE 2007 10 30 VNAA0710003 2 20071008 A 7200 BLADE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENGINE DAMAGED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 223JS 7892 CREW REPORTED A BIRD STRIKE TO THE LEFT ENGINE. MAINTENANCE INSPECTED AND FOUND ONE BLADE DAMAGED. MAINTENANCE REPAIRE D THE DAMAGED BLADE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007103000040 20071030 00040 EU 2007 10 30 TRAX200701553 1 20071022 A 5320 INTERCOSTAL AEROSP ATR72 ATR72 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 TOP ANGLE CRACKED ON INTERCOSTAL (LT NLG AREA) AT FR 25. 2 H 7 2 4T RT 2007103000041 20071030 00041 EU 2007 10 30 TRAX200701554 1 20071022 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 CORROSION FOUND ON LT INBOARD SEAT TRACK BETWEEN FR 13 TO FR 17. SEAT TRACK SPLICES IAW SRM 53-00-00 FIG 434 MATERI AL THICKNESS: 0.394 MATERIAL REMOVED: 0.040 WITHIN LIMITS AS PER SRM: 53-00-00 FIG 304. 2 H 7 2 4T RT 2007103000042 20071030 00042 EU 2007 10 30 TRAX200701555 1 20071022 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 CORROSION FOUND ON RT SEAT TRACK BETWEEN FR 36 - 39. 2 H 7 2 4T RT 2007103000043 20071030 00043 EU 2007 10 30 TRAX200701556 1 20071022 A 5711 FRAME AEROSP ATR72 ATR72 EU LT WING BOX CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 LEFT WING BOX FRAME 28 CRACKED. REPLACED IAW SRM 51-25-01. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WIT H S.P. 663 AND FAR 43, APPENDIX A. 2 H 7 2 4T RT 2007103000044 20071030 00044 EU 2007 10 30 TRAX200701557 1 20071022 A 5711 FRAME AEROSP ATR72 ATR72 EU LT WING BOX CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 LEFT WING BOX FRAME 28A FACE PLATE FOUND CRACKED. REPLACED IAW SRM 51-25-01REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01. 2 H 7 2 4T RT 2007103000045 20071030 00045 NM 2007 10 30 SWAA075291 1 20071024 A 5311 6546555 FRAME BOEING 737 737317 138447P NM BS 867 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007103000046 20071030 00046 NM 2007 10 30 SWAA075292 1 20071024 A 5311 6546557 FRAME BOEING 737 737317 138447P NM BS 887 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007103000047 20071030 00047 NM 2007 10 30 SWAA075280 1 20071024 A 5311 6546558 FRAME BOEING 737 7375H4 138449D NM BS 907 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007103000048 20071030 00048 NM 2007 10 30 SWAA075279 1 20071024 A 5553 6547450 FITTING BOEING 737 7375H4 138449D NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED 18Y CHECK, FOUND VERTICAL STABILIZER FITTING FWD AND AFT LUG FACES CORRODED. REPAIRED FITTING PER EA. 2 L 7 2 4F RT A16WE 2007103000049 20071030 00049 NM 2007 10 30 SWAA075302 1 20071024 A 5312 6549892 BULKHEAD BOEING 737 7373H4 1384600 NM BS 1016 S6L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 14Y CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AT BS 1016, STR 6L. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 2007103000050 20071030 00050 NM 2007 10 30 SWAA075286 1 20071024 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 727C S6R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000051 20071030 00051 NM 2007 10 30 SWAA075309 1 20071024 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 277 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000052 20071030 00052 NM 2007 10 30 SWAA075308 1 20071024 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 685 S3L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000053 20071030 00053 NM 2007 10 30 SWAA075307 1 20071024 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 616 S3L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000054 20071030 00054 SO 2007 10 30 C2XA07TY062 1 20071026 A 3350 BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13964 145123 EMERGENCY PROX LIGHT INOP. RERACKED EMERGENCY LIGHT BATTERY NR 2 & 3 IAW EMB 145 SWPM 20-21-00, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007103000055 20071030 00055 NM 2007 10 30 SWAA075224 1 20071022 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 482A S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482A, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000056 20071030 00056 NM 2007 10 30 SWAA075225 1 20071022 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 482B S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000057 20071030 00057 NM 2007 10 30 SWAA075226 1 20071022 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 559 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000058 20071030 00058 NM 2007 10 30 SWAA075227 1 20071022 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 616 S3R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000059 20071030 00059 NM 2007 10 30 SWAA075228 1 20071022 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 685 S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000060 20071030 00060 NM 2007 10 30 SWAA075229 1 20071022 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 706 S3R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000098 20071030 00098 EA 2007 10 30 TRAX200701574 1 20071023 A 5755 SEAL CNDAIR CL600 CL6002B19 1900309 EA RT WING SPOILER CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 914EV 7752 RIGHT WING SPOILER I/B AND CENTER METAL SEALS ON TRAILING EDGE OF WING ARE CRACKED. 10-30-07 REMOVED IAW SRM 51-42 -06 AND SRM 51-42-21. REPLACED IAW SRM 51-42-06 AND SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007103000099 20071030 00099 EA 2007 10 30 TRAX200701575 1 20071023 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 FS 280 HAS CRACKED CLIP AT 10.25 RBL POSITION. 10-30-07 REMOVED DAMAGED CLIP AT FS 280 LBL 9 I/B POSITION AND DUPL ICATED PER CRJ SRM 53-21-43 FIG. 1 ITEM 6, IAW CRJ SRM 51-24-21, 51-40-11, 51-21-16 AND INSTALLED IAW CRJ SRM 51-23-00 A ND 51-42-21 AT FS 280 LBL 9 I/B POSITION. 2 L 7 2 4F RT A21EA 2007103000100 20071030 00100 EA 2007 10 30 TRAX200701576 1 20071023 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 FS 280 HAS CRACKED CLIP AT 19.5 LBL POSITION. 10-30-07 REMOVED DAMAGED CLIP AT FS 280 LBL 9 O/B POSITION AND DUPLI CATED PER CRJ SRM 53-21-43 FIG 1 ITEM 6, IAW CRJ SRM 51-24-21, 51-40-11, 51-26-16 AND INSTALLED IAW CRJ SRM 51-23-00 AN D 51-42-21 AT FS 280 LBL 9 O/B POSITION. 2 L 7 2 4F RT A21EA 2007103000101 20071030 00101 EA 2007 10 30 COMA0760607 1 20071018 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA BS 654-682 DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 809CA 7366 AIRCRAFT SKIN AT STA 654.50 TO 682.00 BETWEEN STR A8 AND A9 LEFT IS DENTED. MANUFACTURED AND INSTALLED REPAIR DOUBLER F OR DENT BETWEEN STA 654.50 AND 672.20 IAW EA 10-5361-01894 DATED 10-18-07. 2 L 7 2 4F RT A21EA 2007103000102 20071030 00102 NM 2007 10 30 KCSA071493 1 20071023 A 5315 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 820 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FORWARD BILGE, FLOORBEAM UPPER CHORD IS DAMAGED AT STA 820, LBL 28 TO LBL 29. 2 L 7 4 4F RT A20WE 2007103000103 20071030 00103 NM 2007 10 30 MWEA070260 1 20071020 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 926ME 55192 RIGHT THRUST REVERSER UPPER BUCKET -Z- FRAME IS CRACKED AT THRUST REVERSER STATION 26 OUTBOARD. FABRICATED AND INSTALLE D DOUBLER. 2 L 7 2 4F TR A6WE 2007103000104 20071030 00104 NM 2007 10 30 MWEA070261 1 20071020 A 7830 7150923REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 926ME 55192 RIGHT THRUST REVERSER UPPER BUCKET -Z- FRAME IS CRACKED AT THRUST REVERSER STATION 35 OUTBOARD. FABRICATED AND INSTALLE D DOUBLER. 2 L 7 2 4F TR A6WE 2007103000105 20071030 00105 NM 2007 10 30 SWAA075296 1 20071024 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 727C S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007102500009 20071025 00009 NM 2007 10 25 2007UALA04179 1 20071012 A 3250 TILLER AIRBUS A319 A319131 3930317 NM NLG STEERING MALFUNCTIONED A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 855UA 1737 CAPTAIN'S NOSEWHEEL STEERING TILLER IS OVERLY SENSITIVE TO INPUTS. TOO MUCH TENSION. 10-26-07 ACP FUNCTIONAL CHECK OF NOSE WHEEL STEERING PER AMM -FOUND NO IRREGS. CHECK BSCU FOUND NO FAULTS. TAXI CHECK GOOD. COULD NOT DUPLICATE CONDI TION DESCRIBED BY PILOTS.--NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F RT A28NM 2007102500012 20071025 00012 CE 2007 10 25 101107N423CS 1 20071011 A 3244 0266180 TIRE CESSNA 525 525 2076601 CE MLG RUPTURED E Z5FA O OTHER E C VIBRATION/BUFFET F.O.D. LD LANDING 1 EA 63 423CS 127 0824 525B0121 DURING LANDING ROLL OUT, BEFORE BRAKES WERE APPLIED A SEVERE VIBRATION WAS FELT AND THE AIRCRAFT SUDDENLY PULLED TO THE RIGHT. AIRCRAFT WAS STOPPED ON A TAXIWAY AND CREW DISCOVERED RIGHT MAIN TIRE MISSING AND WHEEL DAMAGED. 1 L 7 2 4F RT A1WI 2007102600007 20071026 00007 EU 2007 10 26 12118 1 20071011 A 5347 S5367800121002 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 FOUND SEAT TRACK LEFT SIDE BETWEEN FRAMES 36 AND 39 CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS LI MITS. SEAT TRACK WAS REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007102600019 20071026 00019 EU 2007 10 26 HYIA12131 1 20071011 A 5313 S53070204224225 STRINGER AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 RIGHT STRINGER 21 BETWEEN FRAMES 13 AND 25 CORRODED. REMOVED CORROSION AND FOUND TO BE BEYOND MANUFACTURER LIMITS. REM OVED AND REPLACED IN ACCORDANCE WITH SRM 53-31-00 FIGURE 301. 2 H 7 2 4T RT A53EU 2007102600026 20071026 00026 EU 2007 10 26 HYIA12139 1 20071011 A 5320 SS5367800820005 FLOOR SUPPORT AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 LEFT ZEE FLOOR BETWEEN FRAMES 39 AND 40 CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS LIMIT. REMOVE D AND REPLACED AS PER SRM 51-25-03. 2 H 7 2 4T RT A53EU 2007102600033 20071026 00033 EA 2007 10 26 A6WA200740568 1 20070926 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 LT LOWER WING PLANK AT ACCESS PANEL 540 CB HAS MINOR PITTING DAMAGE IN NON-CRITICAL AREA, .001-.002 INCH DEEP. MAINTENA NCE REPAIRED LT LOWER WING PLANK PER BOMBARDIER REO 601R-57-21-030 REV F. (M) 2 L 7 2 4F RT A21EA 2007102600047 20071026 00047 NM 2007 10 26 QXEA200701614 1 20071019 A 2130 81150C020201 VALVE BOMBDR DHC8 DHC8402 1390042 NM CABIN PRESSURE MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 432QX 662 662 4166 SEA FLIGHT NR 2433: IN AUTO MODE, PRESSURE WOULD VARY 1 FULL SCALE IN RATE. RAN PRESSURE FAIL CHECK LIST. MANUAL PRESS URE DIDN'T WORK CORRECTLY. IN AUTO WITH BLEEDS SELECTED IN MAX, PRESSURE WAS MORE STABLE. MAINTENANCE REPLACED FWD SAF ETY VALVE IAW Q400 MM TASK 21-31-00-000-801 AND 21-31-00-400-801. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102600078 20071026 00078 SW 2007 10 26 HEER117546 1 20070923 A 6230 222010400131FM SWASHPLATE BELL 230 230 1182149 SW ALLSN 250C 250C30G2 03013 GL MAIN ROTOR BROKEN B HEER O OTHER O OTHER NR NOT REPORTED 1 SW 03 14UH 6651 23028 THE MECHANIC NOTICED THE CYCLIC LINK HAD COME IN CONTACT WITH THE INNER RING AND DURING HIS INVESTIGATION TO DETERMINE T HE CAUSE OF THIS UNUSUAL CONDITION, HE FOUND SEVERAL PARTS TO BE EXCESSIVELY DAMAGED CAUSED BY A BROKEN BOLT 20-057-6-1 6D, TOTAL TIME 1688.10 OR WORN SLIDERS 222-310-469-103, TOTAL TIME 1688.10. THE SWASHPLATE WAS REMOVED FROM AIRCRAFT AN D SENT TO OVERHAUL SHOP TO DETERMINE CAUSE OF FAILURE. COMPLIED WITH ALL CONDITIONAL INSPECTIONS AND OVERHAUL REQUIREM ENTS. CONTACTED MFG CUSTOMER REP FOR ADDITIONAL INSTRUCTIONS THAT MFG MAY WANT TO PERFORM. LIST OF DAMAGED PARTS AS FO LLOWS -TOTAL TIME ON ALL 1688.10 - 1 EA. BOLT 20-057-6-16D CRACKED; 1 EA. BOLT 20-057-6-16D EX. 1 G 7 2 3U 3 U NC H9SW E1GL 2007102600079 20071026 00079 GL 2007 10 26 HEER117772 2 20071004 A 7260 23064128 ALTERNATOR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL GEARBOX FAILED B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 425PH CAG47357 53684 CAE847357 ENGINE WAS REMOVED DUE TO METAL IN OIL. UPON DISASSEMBLY FOUND METAL UNDER PERMANENT MAGNET ALTERNATOR. APPEARS TO BE BEARING FAILURE IN PERMANENT MAGNET ALTERNATOR. PART WILL BE SENT TO VENDOR FOR POSSIBLE REPAIR. 1 G 7 1 3U 3 U O H2SW E1GL 2007102600088 20071026 00088 CE 2007 10 26 DXTA200702552 1 20071018 A 3260 SQUAT SWITCH CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG OUT OF ADJUST E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 919QS 7500224 GEAR WOULD NOT RETRACT AFTER TAKEOFF. GEAR LEVER WAS STUCK DOWN AND WOULD NOT MOVE. SERVICED NOSE STRUT & ADJUSTED NOS E GEAR SQUAT SWITCH. OP'S CHECK GOOD IAW MM 32-60-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007102600090 20071026 00090 EU 2007 10 26 12142 1 20071015 A 2910 LINE AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE HYDRAULIC SYS LEAKING A HYIA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NE 01 42836 200 WHEN COMMING IN FOR LANDING ON FLIGHT NR 9596 LANDING GEAR DID NOT EXTEND WHEN SELECTED DOWN. GEAR EXTENSION WAS ACCOMP LISHED WITH THE EMERGENCY GEAR EXTENSION HANDLE WITH NORMAL RESULTS. AIRCRAFT LANDED SAFELY WITH NO FURHTER INCIDENTS. AIRCRAFT WAS FERRY FLOWN TO MAINTENANCE BASE IAW SFP NR 2007-003. CORRECTIVE ACTION WAS REPAIR OF EXTENSION HYDRAULIC PR ESSURE LINE AND AS A PRECAUTIONARY MEASURE, REMOVAL AND INSTALLING OF THE NOSE LANDING GEAR ACTUATOR. THERE WAS NO SHUT DOWN OF ENGINES OR FEATHERING OF PROPELLERS. NO DELAYS WITH 10 CANCELATIONS. 2 H 7 2 4T 4 T RT A53EU E20NE 2007102600093 20071026 00093 NE 2007 10 26 ASMF200710004 2 20071018 A 7200 GE9094B ENGINE BOEING 777 777* UTILUSE NM GE GE90 GE9090B NE LT SIDE OVERTEMP W ASMF C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SW 23 745AM 7736 32718 900475 AIRCRAFT REJECTED TAKEOFF AT 101 KNOTS DUE TO HIGH TEMPERATURE INDICATION ON THE LT ENGINE, REACHING 1035 CELSIUS DEGREE S MOMENTARY AND 1015 DURING 11 SECONDS. MAINTENANCE PERSONNEL PERFORMED FIM PROCEDURE 73-22 TASK 819 FOUND ALL CORRECT, ADDITIONALLY HIGH ENERGY STOP INSPECTION WAS PERFORMED IAW 05-51-14, DETECTING DAMAGES IN THE MAIN LANDING GEAR WHEELS, SO ALL OF THEM WERE REPLACED IAW MM 32-45-01. 2 L 7 2 4F 4 F RT T00001SE E00049EN 2007102600094 20071026 00094 CE 2007 10 26 135375 1 20071015 A 2460 CM358950 MASTER SWITCH CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO COCKPIT INOPERATIVE A HYIA O OTHER O OTHER CR CRUISE 1 NE 01 375R 312 402C0468 AVIONICS MASTER SWITCH FAILED IN FLIGHT. AIRCRAFT LANDED WITH NO FURTHER DIFFICULTIES. MAINTENANCE REMOVED AND REPLACE D THE AVIONICS MASTER SWITCH IAW AIRCRAFT MM. 1 L 7 2 3O 3 O A7CE E8CE 2007102600100 20071026 00100 CE 2007 10 26 GLBA20061016 1 20071015 A 5313 STRINGER BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA BS 451 S10R CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 247GL UE247 STRINGER 10R CRACKED AT FS 451 IAW CRACK IS ABOUT .5 IN LONG AT STRINGER RELIEF CUTOUT. CRACKED AT STRINGER FLANGE. REPA IRED STRINGER FLANGE AT FS 451 IAW. 1900D SRM 51-70. REPAIR DIMENSIONS APPROXIMATELY 9.375 IN BY 1 IN. 2024 T-3 .050. RII COMPLIED WITH IAW TASKCARD 8.2.1. 2 L 7 2 4T 3 T RT A24CE E2NE 2007102600167 20071026 00167 NM 2007 10 26 2007UALA04271 1 20071015 A 3150 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ILLUMINATED A UALA D RETURN TO BLOCK J WARNING INDICATION NR NOT REPORTED 1 WP 29 661UA 27158 CREW REPORT: FLAP-SLAT ELEC LWR EICAS MESSAGE APPEARS AT FLAP POS 5 THEN DISAPPEARS WHEN FLAPS > 20. REPLACED FLAP- SLAT ELECTRONICS UNIT. OPERATION OF FLAP SLAT SYSTEM NORMAL. NO FAULTS OR EICAS MESSAGES DISPLAYED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102600169 20071026 00169 NM 2007 10 26 2007UALA04273 1 20071016 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 360 S14-15L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 FUSELAGE FRAME SHEAR TIE CRACKED BS 360 BETWEEN STR'S 14L-15L. REPLACED SHEAR TIE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112100003 20071121 00003 EA 2007 11 21 COMA0760637 1 20071110 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 523CA 9240 7821 FLIGHT 4950 - EN ROUTE ATL-YYZ FLAPS FAIL CAUTION MESSAGE. A/C DIVERTED TO CVG AND LANDED SAFELY. REMOVED AND REPLACED LEFT BPSU. 2 L 7 2 4F RT A21EA 2007102600175 20071026 00175 NM 2007 10 26 2007UALA04280 1 20071016 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 305-320 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 578UA 26694 TWO EACH MISSING FASTENERS NEAR STR 0 AT ABOUT STA 305 AND 320 NEED BLIND RIVETS INSTALLED TO FILL HOLES. MAJOR REPAIR ACCOMPLISHED. INSTALLED BLIND RIVETS AND INSPECTED 2 EACH RIVETS FOR VERIFICATIONS. NO DEFECTS FOUND AND A/C WAS RELEA SED FOR SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007102600177 20071026 00177 NM 2007 10 26 2007UALA04282 1 20071016 A 8011 STARTER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RIGHT ENGINE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 SPARKS SEEN COMING FROM R ENG DURING START. REPLACED STARTER AND START VALVE. PERFORMED ENG CHK START AS PER JRH AND AL L OPS NOW NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102600178 20071026 00178 NM 2007 10 26 2007UALA04283 1 20071016 A 4900 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE APU FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 APU WILL NOT START. BATTERY VOLTAGE 16 VOLTS. BATTERY VOLTAGE 16V, REPLACED BATTERY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007103000106 20071030 00106 EA 2007 10 30 TRAX200701533 1 20071019 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 FLOOR SUPPORT ANGLE CRACKED AT FS 280, O/B OF LBL 9.00. 10-30-07 COMPLIED WITH ASA CARD NR REO 601R-53-11-138. 2 L 7 2 4F RT A21EA 2007103000107 20071030 00107 EA 2007 10 30 TRAX200701534 1 20071019 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 FS 280 CLIP CRACKED, RBL 9.0 I/B. 10-30-07 REMOVED DAMAGED CLIP AT FS 280 RBL 9 I/B POSITION AND DUPLICATED PER CR J SRM 53-21-43 FIG. 1 ITEM 6. IAW CRJ SRM 51-24-21, 51-40-11, 51-21-16 AND INSTALLED IAW CRJ SRM 51-23-00 AND 5142-21 A T FS 280 RBL 9 I/B POSITION. 2 L 7 2 4F RT A21EA 2007103000108 20071030 00108 EA 2007 10 30 TRAX200701535 1 20071019 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 FS 280 CLIP CRACKED RBL 9.0 O/B. 10-30-07 REMOVED UNSERVICEABLE CLIP FS 280 O/B OF FS 9. INSTALLED NEW CLIP. 2 L 7 2 4F RT A21EA 2007103000109 20071030 00109 EA 2007 10 30 TRAX200701536 1 20071019 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 PAX DOOR OUTER HANDLE IS CRACKED. 11-01-07 REMOVED UNSREVICEABLE PAX DOOR OUTER HANDLE ASSY IAW CRJ 200 AMM 52-11- 03-020-007. INSTALLED NEW SERVICEABLE SLEX HANDLE ON NEW SERVICEABLE HANDLE IAW CRJ 200 SRM 51-42-06. INSTALLED THE REMA INDER OF HARDWARE ON NEW SERVICEABLE HANDLE IAW CRJ 200 AMM 52-11-03. OK TO ISTALL ON PAX DOOR. INSTALLED NEW SERVICEABL E PAX DOOR OUTER HANDLE. COLLARS, WASHERS IAW CRJ 200 AMM 52-11-03-420-003. INSTALLED PLACARD, TO OUTER HANDLE IAW CRJ 2 00 AMM 11-20-00. 2 L 7 2 4F RT A21EA 2007103000110 20071030 00110 NM 2007 10 30 SWAA075284 1 20071024 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 727A S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000111 20071030 00111 EA 2007 10 30 TRAX200701537 1 20071019 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 PAX DOOR STAIRS AFT SKIN IS CRACKED IN RADIUS UNDER STEP 832DT. 10-30-07 REMOVED DAMAGE SECTION OF AFT PAX DOOR ST AIRS SKIN UNDER STEP 832DT IAW REO 601R-52-11-702. CUTOUT REQUIRES LPI OF THE EDGES. PERFORMED LPI ON THE PAX DOOR STAIR S AFT SKIN UNDER STEP 832DT REPAIR CUTOUT IAW CRJ 200 NDTM 51-20-08. NO DEFECTS NOTED, REPAIR COMPLETED IAW REO 601R-52 -11-702. 2 L 7 2 4F RT A21EA 2007103000112 20071030 00112 EA 2007 10 30 TRAX200701538 1 20071019 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 PAX DOOR STAIRS FWD SKIN IS CRACKED IN RADIUS UNDER STEP 832DT. 10-30-07 REMOVED DAMAGE SECTION OF PAX DOOR STAIRS SKIN UNDER FWD STEP 832 DT IAW REO 601R-52-11-702. CUTOUT REQUIRES LPI OF THE EDGES. PERFORMED LPI OF THE PAX DOOR STAI RS FWD SKIN UNDER STEP 832 DT REPAIR CUTOUT IAW CRJ 200 NDTM 51-20-08, NO DEFECTS NOTED. REPAIR COMPLETED IAW REO 601R-5 2-11-702. 2 L 7 2 4F RT A21EA 2007103000113 20071030 00113 NM 2007 10 30 2007UALA04351 1 20071023 A 2611 FIRE WARNING BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU NR 2 NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 924UA 26645 NR 2 FIRE HANDLE DOES NOT ILLUMINATE DURING FIRE TEST. 2 L 7 2 4F 4 F RT A16WE E21EU 2007103000114 20071030 00114 EA 2007 10 30 TRAX200701539 1 20071019 A 5320 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 AFT FS 280 SUPPORT BEAM CRACKED AT 12 O'CLOCK RBL POSITION ON LOWER RADIUS. 10-30-07 COMPLIED WITH REO 601R-53-11- 171 IAW ASA EO 600-53-0090. 2 L 7 2 4F RT A21EA 2007103000115 20071030 00115 EA 2007 10 30 TRAX200701540 1 20071019 A 5320 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 914EV 7752 FOUR FLOOR SUPPORT BRACKETS CRACKED AT FS 280. 10-30-07 REMOVED AND REPLACED IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007103000116 20071030 00116 NM 2007 10 30 WRLA2007116 1 20071028 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM PWA 4460 PW4460 NE BS 635 DAMAGED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 48407 MAIN DECK CARGO SEAT TRACK DAMAGED STA Y=635 X=27.50. REPLACED SEAT TRACK REF SRM 53-70-00 FIG1 REV 40. 2 L 7 3 4F 4 F RT A22WE E24NE 2007103000117 20071030 00117 EA 2007 10 30 TRAX200701577 1 20071023 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 SEAT TRACK NR 2 FROM FWD ON RIGHT SIDE FLOOR HAS CORROSION (MARKED). 10-30-07 REMOVED CORROSION FROM SEAT TRACK NR 2 FROM FWD ON RT SIDE FLOOR IAW CRJ 200 SRM 51-21-06. APPLIED CHEMICAL CORROSION COATING TO REPAIRD AREA IAW CRJ 200 SRM 51-21-11. THE CORROSION REMOVED WAS WITHIN THE ALLOWABLE LIMITS OF CRJ 200 SRM 53-31-49. REMOVED .003 THICKNESS FROM SE AT TRACK THICKNESS. 2 L 7 2 4F RT A21EA 2007103000118 20071030 00118 WP 2007 10 30 VGCA200700003 1 20071023 A 5740 KF580530500021 ATTACH FITTING CVAC 340 340CVAC 242270A WP ZONE 500 CRACKED A VGCA K NONE O OTHER IN INSP/MAINT 1 GL 23 391FL 9190 9190 278 DURING VISUAL INSPECTION OF WING ATTACH FITTING FOUND CRACKS BETWEEN RIVET HOLES UPPER FWD PORTION OF FITTING (LT AFT WI NG TO FUSELAGE ATTACH FITTING). 2 L 7 2 4R 6A6 2007103000132 20071030 00132 EU 2007 10 30 2007UALA04355 1 20071021 A 5100 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE VIBRATION A UALA O OTHER E F VIBRATION/BUFFET FLT CONT AFFECTED CL CLIMB 1 WP 29 446UA 834 VERY ROUGH VIBRATION. PRONOUNCED FLUTTERING FELT LIKE COMING FROM TAIL DURING CLIMB FROM 18000. MAINT TEXT: CREW STAT ES VIBRATION FELT ALL FLT LEVELS AT HIGH SPEED SLOWING 30KNTS VIBRATION LESS NOTICEABLE. REPLACED RT ELEVATOR SERVO CO NTROL 34CE2. FOLLOWING FLIGHTS REPORTED NO VIBRATION-SMOOTH CONTROL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007103000133 20071030 00133 NM 2007 10 30 2007UALA04356 1 20071021 A 3150 WARNING MESSAGE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE ILLUMINATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 827UA 1022 ELAC 1 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. FOUND ELAC1 COMPUTER FAULT. REPLACED ELAC1 COMPUTER- OPS CHECK O K-NO PEPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007103000134 20071030 00134 NM 2007 10 30 2007UALA04357 1 20071022 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 3A AFT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 199UA 28717 AFT EEL LIGHT ON SEAT 3A BROKEN OFF. REPLACED EEL LIGHT 2 L 7 4 4F 4 F RT A20WE E24NE 2007103000136 20071030 00136 NM 2007 10 30 SWAA075212 1 20071022 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 709SW 27843 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138.50. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007103000137 20071030 00137 NM 2007 10 30 SWAA075204 1 20071022 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 273WN 32528 EEPLS LENS MISSING AT ROW 8 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007103000138 20071030 00138 2007 10 30 SWAA075213 4 20071022 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 709SW 27843 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007103000139 20071030 00139 NM 2007 10 30 SWAA075210 1 20071022 A 3233 654482516 ACTUATOR BOEING 737 7373H4 1384600 NM RT MLG FAULTY A SWAA O OTHER J WARNING INDICATION CL CLIMB 1 SW 29 611SW 27697 ON CLIMBOUT RIGHT MLG DID NOT INDICATED UP AND LOCKED. CYCLED GEAR NO CHANGE. REMOVED AND REPLACED RIGHT MLG UPLOCK AC TUATOR PER MM. 2 L 7 2 4F RT A16WE 2007103000140 20071030 00140 NM 2007 10 30 SWAA075231 1 20071022 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 444 S28R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 444, STR 28R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007103000141 20071030 00141 NM 2007 10 30 SWAA075230 1 20071022 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 451 S28L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 451, STR 28L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007103000142 20071030 00142 NM 2007 10 30 2007UALA04359 1 20071023 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 598UA 28751 FWD LEFT OVERWING EMERGENCY HATCH & AFT LEFT OVERWING EMERGENCY HATCH LIGHTS ARE INOPERATIVE. RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007103000143 20071030 00143 EA 2007 10 30 TRAX200701541 1 20071019 A 5320 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT MLG WW CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 914EV 7752 RIGHT MLG BAY HYD SUPPORT BRACKET CRACK. RT MLG BAY HYD. SUPPORT BRAQUET REPLACE IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007103000144 20071030 00144 NM 2007 10 30 KCSA071488 1 20071023 A 5311 FRAME BOEING 747 7472B4B 138481B NM BS 920 S5-6L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 MAIN CABIN LEFT SIDE FRAME IS CRACKED AT TENSION TIE TO FRAME INTERFACE AT STA 920, BETWEEN STR 5L TO 6L. 2 L 7 4 4F RT A20WE 2007103000145 20071030 00145 NM 2007 10 30 KCSA071490 1 20071023 A 5315 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 800 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FORWARD BILGE, FLOORBEAM UPPER CHORD IS DAMAGED AT STA 800 LBL 48 TO LBL 52. 2 L 7 4 4F RT A20WE 2007103100003 20071031 00003 NM 2007 10 31 SWAA075398 1 20071028 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 500B S1 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103100004 20071031 00004 NM 2007 10 31 SWAA075363 1 20071027 A 3397 W4142001220 WIRE BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 468WN 33858 EEPLS INOP AT ROW 5 ABC. FOUND LOOSE WIRE. SECURED WIRE PER WDM. 2 L 7 2 4F RT A16WE 2007103100006 20071031 00006 NM 2007 10 31 SWAA075327 1 20071025 A 5311 6546595 FRAME BOEING 737 7375H4 138449D NM BS 727A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007103100007 20071031 00007 NM 2007 10 31 SWAA075345 1 20071025 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 578 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103100008 20071031 00008 NM 2007 10 31 SWAA075330 1 20071025 A 5552 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 DURING SCHEDULED BRDG CHECK, LEFT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED INPUT ROD BEARINGS PER MM. 2 L 7 2 4F RT A16WE 2007103100011 20071031 00011 NM 2007 10 31 SWAA075346 1 20071025 A 5313 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 597 S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103100012 20071031 00012 NM 2007 10 31 SWAA075331 1 20071025 A 5552 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 DURING SCHEDULED BRDG CHECK, RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED INPUT ROD BEARINGS PER MM. 2 L 7 2 4F RT A16WE 2007103100014 20071031 00014 NM 2007 10 31 SWAA075404 1 20071027 A 2913 623337 PUMP BOEING 737 7375H4 138449D NM NR 1 ENGINE FAULTY A SWAA O OTHER J WARNING INDICATION CL CLIMB 1 SW 29 514SW 25153 RAISING GEAR HANDLE DURING CLIMBOUT, ENGINE AND ELECTRICAL -A- SYSTEM HYRAULIC LOW PRESSURE LIGHTS ILLUMINATED. PRESSUR E WENT TO ZERO AND QUANTITY FLUCTUATED, THEN BOTH LIGHTS WENT OUT. AFTER LANDING WITH REVERSERS DEPLOYED -A- SYSTEM HYD RAULIC LOW PRESSURE LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP PER MM. 2 L 7 2 4F RT A16WE 2007103100015 20071031 00015 NM 2007 10 31 SWAA075402 1 20071029 A 5754 65C26601 STRUCTURE BOEING 737 7373A4 1384585 NM NR 2 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND LEFT WING NR 2 L/E SLAT CRACKED AT LOWER OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007103100020 20071031 00020 NM 2007 10 31 UPS07650965 1 20071022 A 3230 A320141 DOWNLOCK BOEING 767 76734AF 1385212 NM MLG INOPERATIVE A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 331UP 27757 REROUTED TO DFW WITH GEAR DOWN AT 265 KT SW IND LEFT MAIN GEAR WOULD NOT RETRACT. WITH GEAR HANDLE IN UP POSITION - ALL LIGHTS OUT, WITH HANDLE IN OFF POSITION GREEN LIGHT ILLUM. RECYCLED GEAR, SAME IND AT 205 KNOTS IND. REMOVED GEAR PIN FROM LEFT MAIN GEAR FWD OVERCENTER LINK OK TO CONTINUE AIRSPEED UNDER 270 REF AMM 05-51-07-2 AND A/C AOM. 2 L 7 2 4F RT A1NM 2007103100021 20071031 00021 WP 2007 10 31 UPS07850961 1 20070918 A 5320 WEB DOUG DC8 DC873F 302199F WP FS 80 L17L DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 LARGE DENT IN WEB AT L-1 DOOR JAMB NEXT TO BAYONET RECEIVER FITTING. REPAIRED DENT IN WEB AT THE L-1 DOOR JAMB IAW SAA EA 008-5320-01- A1133, UPS RAA DC8-53-20662, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007103100024 20071031 00024 WP 2007 10 31 UPS07850988 1 20071016 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FS 1290 LBL 59 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 CRACK AND HEAVY CORROSION ON SEAT TRACK AT STA 1360 LBL 59. CUT OUT DAMAGED SEAT TRACK AT STA 1290-1 370 IAW SRM 51-3-0. INSTALLED REPAIR SEAT TRACK SECTION AT STA 1290-1370 LBL 59 IAW SRM 53-07-03 FIG 3D. 2 L 7 4 4F RT 4A25 2007103100027 20071031 00027 NM 2007 10 31 UPS07M51022 1 20070906 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C EMPENNAGE LT HORIZONTAL STABILIZER BARREL NUT NR 16 FOUND BORE WITH CORROSION. CORROSION AT BARREL NU T BORE REMOVED, FOUND EXCEEDS LIMIT. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLE ND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEV E BUSHING FAB & PROTECTED PER EO MD11-5510-19409-L FIG 5. PR 1422 B1/2 SEALANT APP. 2 L 7 3 4F RT A22WE 2007103100028 20071031 00028 NM 2007 10 31 UPS07M51023 1 20070828 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C RIGHT HORIZONTAL STABILIZER BARREL NUT HOLE 36R HAS CORROSION IN BORE. TORQUE BOX WEB CUT FOR ACCESS. BARREL NUT BORE CORROSION REMOVED & BORE REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE REAM FURTHER & BORE BOTTOM MACHINE DOWN DEEPER. BARREL NUT BORE BLEND OUT & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. CUT OUT FR PRIMER. 2 L 7 3 4F RT A22WE 2007103100031 20071031 00031 NM 2007 10 31 UPS07M51026 1 20070830 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C EMP - LEFT HORZ STAB NR 18 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BOR E REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT & NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT BUSHING. 2 L 7 3 4F RT A22WE 2007103100032 20071031 00032 NM 2007 10 31 UPS07M51027 1 20070830 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C EMP - RIGHT HORZ STAB NR 23 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BO RE REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. B ARREL NUT BORE BLEND OUT VOID & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BO RE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP. 2 L 7 3 4F RT A22WE 2007103100033 20071031 00033 WP 2007 10 31 ASAA0782133 1 20071022 A 5347 593056671 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 1130-1211 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 CABIN SEAT TRACK CORRODED STA 1211 TO 1130 LBL 44. REMOVED DAMAGED SEAT TRACK, LOCATED, DRILLED AND INSTALLED A REPLACE MENT SEAT TRACK AND SPLICES IAW MD 80 SRM 53-05 FIG 4B 1 AND FIG 4 F. 2 L 7 2 4F RT A6WE 2007103100034 20071031 00034 WP 2007 10 31 ASAA0782135 1 20071022 A 5321 993655133 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 196-256 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 CABIN FLOOR PANEL CORRODED AND BROKEN INSERTS STA 196 TO STA 256 LBL 16 TO LBL 22. FABRICATED AND INSTALLED A REPLACEME NT CABIN FLOOR PANEL IAW MD 80 SRM 53-05 PAR 59 AND DAC DRAWING S4932106. 2 L 7 2 4F RT A6WE 2007103100036 20071031 00036 WP 2007 10 31 ASAA0782137 1 20071022 A 5321 SMO953001535 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 1174-1250 PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 CABIN FLOOR PANEL STA 1174 TO STA 1250 LBL 22 TO RBL 22. PUNCTURED, FABRICATED AND INSTALLED A REPLACEMENT CABIN FLOOR PANEL IAW MD80 SRM 53-05 PAR 59 AND DAC DRAWING S4932106. 2 L 7 2 4F RT A6WE 2007103100037 20071031 00037 WP 2007 10 31 ASAA0782138 1 20071022 A 5321 SMO953001537 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 1117-1174 PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 CABIN FLOOR PANEL STA 1117 TO STA 1174 BL 0 TO RBL 22. PUNCTURED, FABRICATED AND INSTALLED A REPLACEMENT FLOOR PANEL IA W MD 80 SRM 53-05 PAR 59 AND DAC DRAWING S4932106. 2 L 7 2 4F RT A6WE 2007103100038 20071031 00038 WP 2007 10 31 ASAA0782139 1 20071022 A 5321 SMO953001533 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 1117-1174 PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 CABIN FLOOR PANEL STA 1117 TO STA 1174 BL 0 TO LBL 22 PUNCTURED. FABRICATED AND INSTALLED A REPLACEMENT CABIN FLOOR PAN EL IAW MD80 SRM 53-05 PAR 59 AND DAC DWG S4932106. 2 L 7 2 4F RT A6WE 2007103100039 20071031 00039 WP 2007 10 31 ASAA0782140 1 20071022 A 5321 993654755 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 180 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 CABIN FLOORBOARD STA 160 TO STA 180 RBL 8 TO RBL 44 CORRODED. INSERTS FABRICATED AND INSTALLED A REPLACEMENT CABIN FLOO R PANEL IAW MD80 SRM 53-05 PAR 59 AND DAC DRAWING S4932106. 2 L 7 2 4F RT A6WE 2007103100040 20071031 00040 WP 2007 10 31 ASAA0782142 1 20071022 A 5321 993654511 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 160-195 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 CABIN FLOOR PANEL STA 160 TO STA 195 LBL 8 TO LBL 44 BROKEN AND CORRODED INSERTS. FABRICATED AND INSTALLED A REPLACEMEN T CABIN FLOOR PANEL IAW MD80 SRM 53-05 PAR 59 AND DAC DRAWING S 4932106. 2 L 7 2 4F RT A6WE 2007103100041 20071031 00041 WP 2007 10 31 ASAA0782146 1 20071023 A 5321 993655211 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 256 BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 CABIN FLOOR PANEL STA 200 TO STA 256 LBL16 TO RBL 22 PULLED OUT AND DAMAGED BROKEN INSERTS. FABRICATED AND INSTALLED A REPLACEMENT CABIN FLOOR PANEL IAW MD80 53 05 PGS 251, 257 AND DAC DRAWING S4932106. 2 L 7 2 4F RT A6WE 2007103100046 20071031 00046 NM 2007 10 31 UPS07M51028 1 20070831 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C EMP - LEFT HORZ STAB NR 24 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BOR E REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BA RREL NUT BORE BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BO RE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP. 2 L 7 3 4F RT A22WE 2007103100048 20071031 00048 NM 2007 10 31 SWAA075304 1 20071024 A 5311 65C34356 FRAME BOEING 737 7375H4 138449D NM BS 482A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007103100049 20071031 00049 NM 2007 10 31 SWAA075301 1 20071024 A 5322 69353656 SHEAR TIE BOEING 737 7375H4 138449D NM BS 360 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007103100050 20071031 00050 NM 2007 10 31 SWAA075281 1 20071024 A 5322 69353656 SHEAR TIE BOEING 737 7375H4 138449D NM BS 360 S14L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007103100051 20071031 00051 NM 2007 10 31 SWAA075312 1 20071024 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 740A S26L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER 26L CORRODED AT BS 740A. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007103100054 20071031 00054 NM 2007 10 31 KCSA071496 1 20071024 A 5320 STIFFENER BOEING 747 7472B4B 138481B NM BS 371 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 NOSE WHEEL WELL TUNNEL STIFFENER IS CRACKED (.5 INCH) IN LOWER TRIM RADIUS AT STA 371, LBL 10, WL 132. 2 L 7 4 4F RT A20WE 2007103100056 20071031 00056 NM 2007 10 31 UPS07M50968 1 20070902 A 5730 ACCESS PANEL DOUG MD11 MD11F 3023600 NM LWS 536AB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C LEFT WING ACCESS PANEL 536AB CUTOUT AREA FOUND CRACK INDICATION DURING NDT INSPECTION. HOLES REAMED F OR LEFT WING ACCESS PANEL 536AB CUTOUT AREA AS PER EN1639-07. HFEC OPEN HOLE INSPEC C/OUT ON REWORKED HOLE FOUND NO CRA CK. BUSHINGS 17EA FA AS PER EN1639-07. NEW FAB BUSHINGS 17EA & REWORKED AREA REPROTECTED AS PER SRM 51-21-01 VOL II RE V 38 IAW EN1639-07. BUSHINGS 17EA INSTALLED AS PER EN1639-07. 2 L 7 3 4F RT A22WE 2007103100059 20071031 00059 NM 2007 10 31 UPS07M50971 1 20070918 A 5313 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM BS 6-100 S6R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C X-RAY C/OUT FOUND CRACK INDICATION AT STA 6-100, STR 6 (1EA) RT AT LONGERON SPLICE AS MARKED. STA 6-1 00 STR 6 RT CRACKED LONGERON ATTACHED SPLICE REMOVED. CRACKED LONGERON TRIMMED OFF AT STA 1149 & REMOVED. TRIMMED OFF AREA PROTECTED. HFEC INSP C/OUT ON TRIMMED OFF AREA FOUND NO CRACK. LONGERON & REPAIR SPLICE FAB PER SRM 53-10-00 FIG 1 VOL I REV 38. FAB LONGERON & REPAIR SPLICE FASTENERS PICKED UP. FAB LONGERON & REPAIR SPLICE PROTECTED. 2 L 7 3 4F RT A22WE 2007103100060 20071031 00060 NM 2007 10 31 UPS07M50972 1 20070808 A 5714 STRUCTURE DOUG MD11 MD11F 3023600 NM BS 1239- 189 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C LEFT SIDE CENTER WING BOX TOPSIDE AT STA 1239.0 - 1189.0 X=108.0 FOUND CORROSION AROUND FASTENERS AS M ARKED. LEFT SIDE CENTER WING BOX TOPSIDE AT STA 1239.0-1189.0 X=108.0 FASTENER AS MARK & CORRODED AREAS REMOVED. CORRO SION ON UPP SKIN REMOVED. REWORKED AREAS PROTECTED. FPI & HFEC OPEN HOLE INSP C/OUT ON REWORKED AREA FOUND NO CRACK & NO CORROSION. REWORKED AREAS SKIN P/N APB7441-1 MAT'L REMOVED & REMAINED, ALL FOUND EXCEED LIMITS. FLAP PEENING C/OUT. 2 L 7 3 4F RT A22WE 2007103100063 20071031 00063 EA 2007 10 31 TRAX200701550 1 20071021 A 5720 NUT CNDAIR CL600 CL6002B19 1900309 EA LT WING BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 904EV 7628 LEFT WING AND RIGHT WING 3 ANCHOR NUT FOR BUTTE DOOR (594SB, 594PB, 694LB) BROKEN. 2 L 7 2 4F RT A21EA 2007103100064 20071031 00064 EA 2007 10 31 TRAX200701551 1 20071021 A 2751 DETECTION SYS CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTED A ASOA O OTHER J WARNING INDICATION DE DESCENT 1 SO 27 907EV 7648 FLAP FAIL CAUTION MSG AN DESCENT WITH FLAPS SET TO ZERO. FOUND SKEW DETECTION UNIT AT FAULT. EMERGENCY EQUIPMENT ROLLE D AS A PRECAUTION. FLT 9970 DEL 370 MINS. NC FLTS 4583, 4652 CX. SKEW DETECTION SYSTEM. 2 L 7 2 4F RT A21EA 2007103100066 20071031 00066 NM 2007 10 31 SWAA075278 1 20071024 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 445WN 29841 DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007103100067 20071031 00067 EU 2007 10 31 2007UALA04360 1 20071019 A 3510 OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 424UA 506 CAPTAIN'S O2 MASK DOES NOT TEST. WHEN OBS MASK TEST CAPTAIN'S MASK DOES PARTIAL TEST. FOUND CONTROL BOX LEAKING. R EPLACED CAPT CONTROL BOX. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007103100070 20071031 00070 NM 2007 10 31 2007UALA04364 1 20071023 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1420 S25-26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 AFT PIT STA 1420 MAIN FRAME BETWEEN STR 25L AND 26L HAS 1 DENT. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE & INSTALLED ANGLE REPAIR. INSTALLED NEW STRINGER CLIP AT STA 1420, STR 25L. REPAIR INSTALLED BETWEEN STR 24L & 26L. 2 L 7 2 4F 4 F RT A2NM E17NE 2007103100073 20071031 00073 NM 2007 10 31 KCSA071497 1 20071024 A 5320 STIFFENER BOEING 747 7472B4B 138481B NM BS 364 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 NOSE WHEEL WELL TUNNEL STIFFENER IS CRACKED (.25 INCH) IN LOWER TRIM RADIUS AT STA 364, RBL 10, WL 132. 2 L 7 4 4F RT A20WE 2007103100075 20071031 00075 NM 2007 10 31 SWAA075272 1 20071024 A 3350 OL3071BPEGPL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED C1 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007103100077 20071031 00077 NM 2007 10 31 HNAA0700246 1 20071020 A 2913 8290001 PUMP DHAV DHC8 DHC8102 2809003 NM HYD SYSTEM MALFUNCTIONED A HNAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 07 827EX 30400 9776 390 UPON GEAR EXTENSION, NR 2 ENGINE HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED. NR 2 MAIN HYDRAULIC INDICATION WENT TO ZERO PSI. AFTER GEAR DOWN, PRESSURE RETURNED TO 3000 PSI. CAUTION LIGHT REMAINED ILLUMINATED. NR 2 SYSTEM QUANTITY REMAINE D AT 4 QTS. REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYDRAULIC PUMP AND CASE DRAIN FILTER IAW MAINTENENCE MANUAL PROCEDU RES. GROUND RUN AND LEAK CHECK WERE GOOD. 2 H 7 2 4T RT A13NM 2007103100079 20071031 00079 NM 2007 10 31 KCSA071499 1 20071024 A 5330 SKIN BOEING 747 7472B4B 138481B NM BS 260 S13-14R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 EXTERNAL FUSELAGE SKIN IS DAMAGED AT STA 260, BETWEEN STR 13R & 14R. 2 L 7 4 4F RT A20WE 2007103100081 20071031 00081 EA 2007 10 31 TRAX200701589 1 20071025 A 5270 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR ILLUMINATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 829AS 7232 IN FLIGHT SHORTLY AFTER TAKEOFF, RECEIVED AT PAX OUTER DOOR CAUTION MSG FOLLOWED BY A PAX DOOR WARNING RED MSG. COMPLIE D WITH QRH THIRD WRITE UP ON DOOR. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. FLT 4814 DEL 50 MINS. 2 L 7 2 4F RT A21EA 2007103100083 20071031 00083 EA 2007 10 31 COMA0760602 1 20071013 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 931CA 12292 7037 FLIGHT 9608 - FLAPS FAILED AT 20 DEGREES. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED PDU. 2 L 7 2 4F RT A21EA 2007103100085 20071031 00085 NM 2007 10 31 2007UALA04365 1 20071023 A 5230 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CARGO DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 FWD CARGO PIT DOOR HAS SMALL DENT ON LOWER LEFT CORNER. CUTOUT DAMAGE. INSTALLED FILLER & DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007103100087 20071031 00087 EA 2007 10 31 TRAX200701587 1 20071024 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA BS 640-625 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 914EV 7752 UPPER WEB OF ENGINE SUPPORT BEAM BETWEEN FS 640.0 AND FS 625.00 IS CRACK AT RBL 8.0. 2 L 7 2 4F RT A21EA 2007103100088 20071031 00088 NM 2007 10 31 CALA0700601 1 20071022 A 5320 6552878102 ANGLE BOEING 737 737524 1384721 NM BS 907-1006 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11612 27325 INSPECTION FOUND AN L-2 DOOR Z-ANGLE CORRODED AT STA 907-1006, LBL 43 TO LBL 60. THE Z-ANGLE WAS REMOVED AND REPLACED I AW SRM 51-40-02 AND BOEING DRAWING 65-52878. 2 L 7 2 4F RT A16WE 2007103100089 20071031 00089 NM 2007 10 31 CALA0700603 1 20071003 A 5230 6547952524B SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND CRACKS IN THE INNER SKIN OF THE AFT CARGO DOOR AT LIGHTENING HOLES ABOVE THE DOOR HANDLE CUTOUT. THE S KIN WAS REPAIRED IAW ECRA 5232-01092. 2 L 7 2 4F RT A16WE 2007103100090 20071031 00090 NM 2007 10 31 NOCA15707 1 20071009 A 3350 3071 LAMP BOEING 757 75728A 1384976 NM EMERGENCY LIGHTS INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 756NA 32448 EMERGENCY EXIT PATH LIGHTING INOP AT SEAT 28ABC. RELAMPED AS REQUIRED. 2 L 7 2 4F RT A2NM 2007103100091 20071031 00091 NM 2007 10 31 2007UALA04366 1 20071023 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1460 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 AFT PIT STA 1460 MAIN FRAME BETWEEN STR 23L AND 24L HAS 1 DENT. MAJOR REPAIR ACCOMPLISHED: REMOVED FRAME SPLICE, CUT O UT DAMAGE. FABRICATED & INSTALLED REPAIR ANGLE. INSTALLED NEWLY FABRICATED STRINGER CLIP (P/N 140N2005-25) AT STR 23L. 2 L 7 2 4F 4 F RT A2NM E17NE 2007103100094 20071031 00094 NM 2007 10 31 SWAA075258 1 20071023 A 5313 6551698 STRINGER SPLICE BOEING 737 7375H4 138449D NM BS 908 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER S RM. 2 L 7 2 4F RT A16WE 2007103100095 20071031 00095 2007 10 31 SWAA075256 4 20071023 A 2565 6557463 FITTING BOEING 737 7377H4 1384404 NM L1 DOOR GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 758SW 27873 DURING SCHEDULED 8Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007103100096 20071031 00096 NM 2007 10 31 SWAA075250 1 20071023 A 5311 65C22909 FRAME BOEING 737 737317 138447P NM BS 500C S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007103100097 20071031 00097 NM 2007 10 31 SWAA075245 1 20071023 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007103100098 20071031 00098 NM 2007 10 31 SWAA075269 1 20071023 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 706 S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103100099 20071031 00099 NM 2007 10 31 SWAA075268 1 20071023 A 5313 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 663 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103100100 20071031 00100 NM 2007 10 31 SWAA075266 1 20071023 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 420 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103100101 20071031 00101 NM 2007 10 31 SWAA075246 1 20071023 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 500D S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103100103 20071031 00103 NM 2007 10 31 SWAA075248 1 20071023 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 616 S2R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103100104 20071031 00104 NM 2007 10 31 SWAA075263 1 20071023 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 747 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103100106 20071031 00106 NM 2007 10 31 SWAA075264 1 20071023 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 867 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103100107 20071031 00107 NM 2007 10 31 SWAA075255 1 20071023 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 794 S26R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 794, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103100108 20071031 00108 NM 2007 10 31 SWAA075259 1 20071023 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 787 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103100109 20071031 00109 EU 2007 10 31 TRAX200701580 1 20071023 A 5320 INTERCOSTAL AEROSP ATR72 ATR72 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 RIGHT MLG INTERCOSTAL AT FR 25 CRACKED. REPLACED AND INSTALL IAW SRM 51-25-01. 2 H 7 2 4T RT 2007103100110 20071031 00110 NM 2007 10 31 2007UALA04367 1 20071023 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 EEL STRIP BY RIGHT SIDE FWD GALLEY AND RIGHT SIDE FC AREA INOP. REPAIRED BROKEN SECTION. OPS CHECK, OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007103100111 20071031 00111 NM 2007 10 31 2007UALA04368 1 20071024 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EEL INOP: DOOR 5L CROSS AISLE. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007103100112 20071031 00112 NM 2007 10 31 2007UALA04369 1 20071024 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHT INOP: DOOR 5R SLIDE ILLUM. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007103100122 20071031 00122 NM 2007 10 31 SWAA075243 1 20071023 A 5753 65C30462 SKIN BOEING 737 7375H4 138449D NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED 18Y CHECK, FOUND RT WING INBOARD FOREFLAP DELAMINATED AT UPPER SURFACE. REMOVED AND REPLACED FOREFLAP PER MM. 2 L 7 2 4F RT A16WE 2007103100123 20071031 00123 NM 2007 10 31 SWAA075234 1 20071023 A 3350 767 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 285WN 32536 DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER M M. 2 L 7 2 4F RT A16WE 2007103100125 20071031 00125 2007 10 31 NOCA15907 4 20071023 A 2565 7A14893 SLIDE BOEING 767 76739H 1385311 NM L2 DOOR UNWANTED DEPLOY A NOCA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 EA 15 760NA 26257 DOOR SLIDE 2L BLOWN ADVERTENTLY BY FLT ATTENDANT. THE 2L SLIDE PREVIOUSLY REMOVED REF PG 39524 ITEM 1M PAD 76. INSTALL ED 2L SLIDE PER JOB CARD 25-029-01 AND AMM 25-66-01. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007103100127 20071031 00127 NM 2007 10 31 CALA0700567 1 20071006 A 3350 ADD71701100 BATTERY PACK BOEING 737 737924 13848A1 NM EMERGENCY LIGHTS DISCHARGED A CALA O OTHER O OTHER NR NOT REPORTED 1 SW 27 35407 30124 EMERGENCY BATTERY PACK BAD ROW 26L 21R AFT LEFT DOOR. REPLACED EMERGENCY BATTERY PACK ON ROW 26L, 21R AND AFT LEFT GALL EY DOOR PER CHECK CARD 29-3350-1-9100, OPS GOOD. 2 L 7 2 4F RT A16WE 2007103100128 20071031 00128 NM 2007 10 31 2007UALA04374 1 20071024 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EEL INOP: MID GALLEY LT SIDEWALL. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007103100129 20071031 00129 NM 2007 10 31 2007UALA03746 1 20070917 A 5754 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT LE SLAT CORRODED A UALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 WP 29 568UA 26674 FLT DIVERTED DUE TO RIGHT L/E SLAT MATERIAL LIBERATION. THE RIGHT SLAT BETWEEN THE ENGINE AND THE FUSELAGE WAS DISINTEG RATING. AT THE TIME OF THE RADIO PATCH THE AIRCRAFT HAD A 12 X 8 X 2 INCH PIECE MISSING FROM THE SLAT. MAJOR REPAIR AC COMPLISHED. THE PRIMARY FAILURE MODE IS MOISTURE INGRESSION. THIS LED TO CORROSION OF HONEYCOMB AND A WEAKENED BONDING RESULTING IN HONEYCOMB PULLING OUT OF ADHESIVE FILLETS. THE LAST SHOP REPAIR DID NOT REPLACE ALL OF THE HONEYCOMB SECT IONS. APPLIED FIBERGLASS REPAIR TO TWO INBOARD AREAS OF DELAMINATION AND CONTOURED HONEYCOMB ON 4 OUTBOARD REPAIRS AND SANDED PAINT FROM REPAIR AREAS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007103100130 20071031 00130 NM 2007 10 31 2007UALA03903 1 20070925 A 2810 O-RING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2 FUEL TANK LEAKING A UALA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 29 196UA 28715 UNWANTED FUEL TRANSFER. NR 2 MAIN TO CENTER 100LBS EVERY 4+ MINUTES. *S/D* FOUND COUPLINGS ON THE SCAVENGE SYSTEM LEA KING IN THIRD BAY, LEFT SIDE, AT THE BOTTOM. REPLACED O-RINGS. OPS CHECK AND LEAK CHECK GOOD. SUSPECT VIBRATION & MUL TIPLE USE CYCLES LED TO O-RING DETERIORATION. 2 L 7 4 4F 4 F RT A20WE E24NE 2007103100132 20071031 00132 NM 2007 10 31 HNAA0700247 1 20071022 A 2721 H914A ACTUATOR DHAV DHC8 DHC8102 2809003 NM RUDDER MISRIGGED A HNAA O OTHER F FLT CONT AFFECTED CR CRUISE 1 EA 07 935HA 47574 1529 142 IN FLIGHT WITH CHARTED TORQUE AND CHARTED PITCH, RUDDER REQUIRES ¼ LEFT HAND TRIM FOR, 0 BALL FLIGHT. ADJUSTED RUDDER T RIM ACTUATOR AS PER MM 27-20-37, OPERATION CHECK GOOD. 2 H 7 2 4T RT A13NM 2007103100133 20071031 00133 NM 2007 10 31 SWAA075277 1 20071024 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 445WN 29841 DURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007103100134 20071031 00134 NM 2007 10 31 SWAA075276 1 20071024 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 425LV 29829 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 3 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007103100139 20071031 00139 2007 10 31 SWAA075238 4 20071023 A 2565 D31354 SLIDE BOEING 737 7373K2 13844BA NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007103100143 20071031 00143 NM 2007 10 31 HNAA070245 1 20071017 A 6120 V319 SWITCH DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 984HA 30998 30998 377 AFTER TAKEOFF AND GEAR RETRACTED NR 1 ENGINE BETA LOCKOUT SYSTEM ACTIVATED. TORQUE REACHED 98 PERCENT ON INDICATOR, RED UCED TORQUE BY RETARDING POWER AND CONDITION LEVER TO 900 RPM. FOUND SWITCH 6141-S3 BAD. REPLACED SWITCH. RESET BETA SWITCHES, RAN AIRCRAFT PER WORK CARD 61-20-010, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007102500047 20071025 00047 EA 2007 10 25 QXEA200701554 1 20071009 A 5310 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA BS 597 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - C4 CHECK, REFERENCE REO 670-53-11-188 SHEET 1 MAP H, BURNT MATERIAL AROUND FASTENER HOLE 4.7" FORWARD FOR FS 597 S TRINGER 0. HFEC COMPLIED WITH NO CRACKS NOTED. COMPLIED WITH REO 670-53-11-188 SHEET 1 MAP H. 2 L 7 2 4F RT A21EA 2007102500048 20071025 00048 EA 2007 10 25 QXEA200701555 1 20071009 A 5310 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA BS 597 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - C4 CHECK, REFERENCE REO 670-53-11-188 SHEET 1 MAP I, BURNT MATERIAL AROUND FASTENER HOLE AT FS 597, 3.2 INCH DOWN FROM STRINGER 5L. HFEC COMPLIED WITH WITH NO CRACKS NOTED. COMPLIED WITH REO 670-53-11-188 SHEET 1 MAP I. INSTALLED R EPAIR DOUBLER AND FILLER ASPER IAW REO 670-53-11-188 STEP 28 PAGE 3. 2 L 7 2 4F RT A21EA 2007102500049 20071025 00049 EA 2007 10 25 QXEA200701556 1 20071009 A 5310 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA BS 613 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - C4 CHECK, REFERENCE REO 670-53-11-188 SHEET 1 MAP J, BURNED MATERIAL AROUND FASTENER HOLE AT FS 613, 1.7" DOWN FRO M STRINGER 5L. HFEC COMPLIED WITH AROUND FASTENER HOLES WITH NO CRACKS NOTED. FABRICATED REPAIR DOUBLER AND FILLER AS PER REO 670-53-11-188 STEP 28 PAGE 3. PAINTED DOUBLER IAW SRM 51-25-01. 2 L 7 2 4F RT A21EA 2007102500050 20071025 00050 EA 2007 10 25 QXEA200701557 1 20071009 A 5310 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA BS 816 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX- C4 CHECK, REFERENCE REO 670-53-11-188 SHEET 3 MAP L. BURNED MATERIAL AROUND FASTENER HOLE AT FS 816.7, BELOW STRING ER 5L. HFEC AROUND FASTENER HOLES WITH NO CRACKS NOTED. COMPLIED WITH REO 670-53-11-188 PAGE 3 MAP L. 2 L 7 2 4F RT A21EA 2007102500051 20071025 00051 NM 2007 10 25 QXEA200701590 1 20071022 A 3040 SYLZ50970 CONTROLLER DHAV DHC8 DHC8202 2809007 NM WINDSHIELD HEAT MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 352PH 23135 494 SEA - ON DESCENT FOR APPROACH GOT RIGHT WINDSHIELD HOT CAUTION LIGHT. COMPLETED CHECKLIST AND LIGHT WENT OUT. MAINTENA NCE PERFORMED ELECTRICAL CONTINUITY CHECK ON CO-PILOTS WINDSHIELD, NO DEFECT NOTED. REPLACED CO-PILOTS WINDSHIELD HEAT CONTROL BOX AND RELAY 3041-K10. PERFORMED OPERATIONAL CHECK, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102500052 20071025 00052 NM 2007 10 25 QXEA200701593 1 20071020 A 3260 LAMP DHAV DHC8 DHC8202 2809007 NM BRAKE INDICATOR INOPERATIVE A QXEA D RETURN TO BLOCK P NO WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 357PH 504 PSC - PARK BRAKE LIGHT INOP. MAINTENANCE RELAMPED PARK BRAKE CAUTION LIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNE D TO SERVICE. 2 H 7 2 4T RT A13NM 2007102500053 20071025 00053 NM 2007 10 25 QXEA200701587 1 20071019 A 3040 SYLZ50970 CONTROLLER DHAV DHC8 DHC8202 2809007 NM WINSHIELD HEAT MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 357PH 8235 504 PSC FLIGHT NR 2025, LEFT WINDSHIELD HOT CAUTION ILLUMINATED AFTER SELECTING WINDSHIELD HEAT FROM WARMUP TO NORMAL. THE LEFT WINDSHIELD HOT EXTINGUISHED UPON SELECTING BACK TO WARMUP. REPLACED WINDSHIELD HEAT CONTROLLER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102500054 20071025 00054 NM 2007 10 25 QXEA200701588 1 20071020 A 3150 WARNING LIGHT DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE NR 2 ENGINE FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 356PH 502 RDM FLIGHT NR 2126, ON START UP NR 2 ENGINE MANUAL CAUTION LIGHT ILLUMINATED. COMPLIED WITH SUPPLEMENTAL PROCEDURE ON D ASH 8 FSM PAGE 7.3.11. NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007102500055 20071025 00055 NM 2007 10 25 QXEA200701586 1 20071020 A 2133 10306814 OUTFLOW VALVE DHAV DHC8 DHC8202 2809007 NM CABIN PRESSURE MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 354PH 18091 1735 498 SEA FLIGHT NR 2190 AT LEVEL FLIGHT CABIN DIFFERENTIAL PRESSURE GRADUALLY DECREASED FROM 5.4 PSID TO 0 PSID. UNABLE TO C ONTROL CABIN PRESSURE IN MANUAL MODE. MAINTENANCE REPLACED THE FORWARD OUTFLOW VALVE. PRESSURIZED AIRCRAFT IN MANUAL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102500056 20071025 00056 NM 2007 10 25 QXEA200701589 1 20071020 A 2910 LINE DHAV DHC8 DHC8202 2809007 NM HYD SYSTEM BROKEN A QXEA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 358PH 506 SEA FLIGHT NR 2138, AFTER STARTING OUR TAXI OUT TO RUNWAY, NOTICED THE NR 2 HYDRAULIC QUANTITY WAS SLOWLY DEPLETING. ST ARTING AT 3.5 QUARTS ALL THE WAY DOWN TO ZERO. TROUBLESHOT TO BROKEN LINE AT INLET OF PART BRAKE ACCUMULATOR CHECK VALV E. REPLACED HYDRAULIC LINE. SERVICED NR 2 HYDRAULIC SYSTEM. BLED NR 2 HYDRAULIC SYSTEM. LEAK CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007102500057 20071025 00057 SO 2007 10 25 SWIA200718789 1 20071017 A 5413 STRINGER SPLICE EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 292UX 120292 RIGHT NACELLE INBOARD SIDE WHEEL WELL CLOSE OUT STRINGER SPLICE IS CRACKED AT FRAME NR 10, FOUND AT C-CHECK. REPLACED N ACELLE INBOARD SIDE WHEEL WELL CLOSE OUT STRINGER SPLICE AND STRINGER PER EMB 120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2007102500058 20071025 00058 EA 2007 10 25 SWIA200718790 1 20071018 A 7120 MOUNT CNDAIR CL600 CL6002C10 1390015 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 340CA 10062 RIGHT ENGINE, FORWARD ENGINE MOUNT LINK ASSEMBLY LOWER BUSHING AND THROUGH BUSHING IS CORRODED. REPLACED FORWARD MOUNT LINK AND BUSHING IAW 71-23-01. 2 L 7 2 4F RT A21EA 2007102500059 20071025 00059 EA 2007 10 25 SWIA200718791 1 20071019 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 927SW 7693 FIRST OVERHEAD EMERGENCY LIGHT IS BURNED OUT, FLIGHT NR 5901. REPLACED LAMP. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007102500060 20071025 00060 EA 2007 10 25 SWIA200718792 1 20071016 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 506CA 7793 RIGHT FORWARD WING EMERGENCY EXIT LIGHT IS INOP. REPLACED BULB AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007102500061 20071025 00061 SO 2007 10 25 SWIA200718793 1 20071017 A 2197 WIRE EMB 120 EMB120ER 3260203 SO GROUND FAN DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 583SW 120351 FOUND RCCB FOR LEFT GROUND FAN WITH DAMAGED WIRES. REPAIRED WIRES AND REPLACED RCCB IAW 24-34-01. GROUND FAN OPS CHECK S GOOD. 2 L 7 2 4T RT A31SO 2007102500062 20071025 00062 EA 2007 10 25 SWIA200718794 1 20071017 A 3244 TIRE CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 406SW 7030 FLT 6472 - ABORTED TAKEOFF WHEN THE NOSE WHEELS STARTED A MODERATE VIBRATION. FOUND BOTH NOSE TIRES BLOWN OUT. INSPECT ED AND REPLACED THE LEFT AND RIGHT NOSE WHEEL ASSEMBLIES IAW CRJ AMM 32-42-01, PN 5010598, SN/OFF NOV03-5276, PN 5010598 , SN/OFF, JAN04-1336. 2 L 7 2 4F RT A21EA 2007102500063 20071025 00063 EA 2007 10 25 A6WA200740502 1 20070910 A 2497 DIODE CNDAIR CL600 CL6002B19 1900309 EA DC SYSTEM FAILED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 430AW 7719 AFTER DEPARTURE DC EMERGENCY BUS CAUTION MESSAGE CAME ON AND OFF REPEATEDLY. COMPLIED WITH QRH. NO ASSOCIATED FAULT ME SSAGES FOR SYSTEMS ASSOCIATED WITH DC EMERGENCY BUS APU BATTERY DIRECT FEED FLOWLINE REMAINED GREEN. REMOVED AND REPLAC ED DC EMERGENCY DIODE AND RELATED HARDWARE, OPS CHECK OF DC ELECTRICAL POWER NORMAL REF WDM 24-60-00. (M) 2 L 7 2 4F RT A21EA 2007102500064 20071025 00064 EA 2007 10 25 A6WA200740541 1 20070918 A 2700 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A A6WA A UNSCHED LANDING F E FLT CONT AFFECTED VIBRATION/BUFFET CL CLIMB 1 GL 31 411ZW 7569 LONGITUDINAL OSCILLATIONS BEGAN CLIMBING THRU APPROX 26,000 FT FOR APPROX 30 SECONDS OSCILLATIONS RETURNED IN LEVEL CRUI SE FLIGHT AT 33,000 WITH AUTOPILTO ON OR OFF. OSCILLATION STOPPED WHEN BEGAN DESCENT. 2 L 7 2 4F RT A21EA 2007102500065 20071025 00065 EA 2007 10 25 A6WA200740542 1 20070917 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY MALFUNCTIONED A A6WA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 31 405AW 7362 RECEIVED SMOKE CARGO WARNING DURING TAXI OUT, MESSAGE LIT FOR 5 SECONDS AND EXTINGUISHED RAMP INSPECTED CARGO BAY AND FO UND NO EVIDENCE OF SMOKE AND FIRE. DEACTIVATED BOTH CARGO SMOKE DETECTORS IAW AMM 26-15-00-040-801. (M) 2 L 7 2 4F RT A21EA 2007102500066 20071025 00066 EA 2007 10 25 A6WA200740545 1 20070924 A 2697 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA NR 1 FIRE DETECT DAMAGED A A6WA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 31 425AW 7663 ON TAKEOFF ROLL, THRUST LEVER ADVANCEMENT GOT LEFT JET OVERHEAT FAIL CAS MESSAGE. ABORTED TAKEOFF AT 10 KNOTS, MAX BTMS READING IS 4, TAKEOFF WEIGHT 44,300 LBS. REMOVED AND REPLACED ENGINE NR 1 FIRE DETECTION HARNESS PER AMM 26-11-07. OP S CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007102500067 20071025 00067 EA 2007 10 25 A6WA200740546 1 20070925 A 4990 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA APU LOW A A6WA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 GL 31 431AW 7256 APU OIL CAUTION MESSAGE IN FLIGHT. SERVICED APU OIL IAW AMM 12-13-49. ADDED 1 PINT. PERFORMED, OPS TEST OF APU IAW 49 -10-01, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007102600008 20071026 00008 EU 2007 10 26 12119 1 20071011 A 5347 S5367800121002 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 SEAT TRACK RIGHT SIDE BETWEEN FRAMES 36 AND 39 CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS LIMITS. SEAT TRACK WAS REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007102600015 20071026 00015 EU 2007 10 26 HYIA12126 1 20071011 A 5347 S5307030820202 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 LEFT SEAT TRACK BETWEEN FRAMES 41 AND 44 IS CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS LIMITS. R EMOVED AND REPLACED SEAT TRACK IN ACCORDANCE WITH SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007102600029 20071026 00029 CE 2007 10 26 HYIA1352471 1 20071022 A 5312 52113622 BULKHEAD CESSNA 402 402C 207590R CE BS 154.5 CORRODED E HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 247GS 402C0637 BULKHEAD LOCATED ON THE RIGHT FUSELAGE WALL JUST AFT OF FIRST OFFICERS SIDE WINDOW AT FUSELAGE STATION 154.5 FOUND TO BE CORRODED BEYOND MANUFACTURERS LIMITS. REMOVED CORRODED AREA AND SPLICED IN NEW BULK HEAD. 1 L 7 2 3O A7CE 2007102600030 20071026 00030 EA 2007 10 26 A6WA200740571 1 20070926 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 MINOR PITTING ON RIGHT LOWER WING PLANK WS 54.897 ACCESS PANEL 640BB IN NON-CRITICAL AREA. MAINTENANCE REPAIRED IAW BOM BARDIER REO 601R-57-21-030. (M) 2 L 7 2 4F RT A21EA 2007102600032 20071026 00032 EA 2007 10 26 A6WA200740574 1 20070919 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 PAX DOOR AFT STAIR SIDE SKIN CRACKED APPROX .70 INCH BETWEEN MID UPPER STEP AND MID STEP. MAINTENANCE CUT AWAY DAMAGED SKIN AND INSTALLED REPAIR DOUBLER AND ANGLES IAW BOMBARDIER REO 601R-52-11-702 REV A. (M) 2 L 7 2 4F RT A21EA 2007102600034 20071026 00034 EA 2007 10 26 A6WA200740573 1 20070919 A 5210 601R317725 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 PAX DOOR AFT DRAG ANGLE CRACKED APPROX 1 INCH AT DOOR ASSIST CABLE PULLEY IN RADIUS OF ANGLE. MAINTENANCE REPAIRED ANGL E IAW BOMBARDIER AERO SPACE REO 601R-52-11-513. (M) 2 L 7 2 4F RT A21EA 2007102600037 20071026 00037 EA 2007 10 26 A6WA200740548 1 20071001 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 411ZW 7569 FOUND FS 280 FLOORBEAM CLIP AT LBL 9.0, OUTBOARD, IS CRACKED IN RADIUS APPROX .50 INCH LONG. MAINTENANCE REMOVED CRACKE D CLIP AND INSTALLED NEW CLIP P/N 601R31113-57, IAW BSC SR 601R-53-0057A, CRJ SRM 51-42-13, AND 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007102600040 20071026 00040 WP 2007 10 26 NWAA073559989 1 20071013 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 185-210 DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8945E 47181 DURING GROUND OPERATIONS, FUSELAGE SKIN WAS DAMAGED BY VEHICLE IMPACT AT BS 185 TO BS 210 S26R-S30R AND BS 194 TO BS 229 S24R-S26R. REPAIRED PER EA 99-210976. 2 L 7 2 4F A6WE 2007102600051 20071026 00051 EA 2007 10 26 A6WA200740556 1 20071005 A 5753 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT TE FLAP DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 411ZW 7569 LEFT INBOARD FLAP UPPER SKIN DENTED 15 INCHES FROM INBOARD EDGE, 7 INCHES FROM TRAILING EDGE APPROX 1.25 INCH LONG BY 1 INCH WIDE BY .022 INCH DEEP. MAINTENANCE REPAIRED LT INBOARD FLAP UPPER SKIN USING NON-FLUSH REPAIR IAW CRJ 200 SRM 57- 52-00 REPAIR NR 03. (M) 2 L 7 2 4F RT A21EA 2007102600054 20071026 00054 EU 2007 10 26 07FDEA04663 1 20071023 A 5315 A5361079723100 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 MAIN CABIN FLOORBEAM STRUCTURE BENEATH LT FWD LAV BETWEEN FR 14 AND 14B HAS INTERGRANULAR CORROSION. REMOVED CORROSION IAW A310 SRM 51-74-10. ORIGINAL THICKNESS .079. REMOVED .045. REMAINING MATERIAL NOT WITHIN ALLOWABLE LIMITS IAW A310 SRM 53-10-00. UT GAUGE NR 8225I. REMOVED CORRODED FLOORBEAM IAW A310 SRM 51-40-21. LOCATED AND DRILLED HOLES IN NEW F LOORBEAM PART NR A5361079723100, PO NR 593163.1 IAW A310 SRM 51-40-40. INSTALLED NEW FLOORBEAM IAW A310 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007102600061 20071026 00061 WP 2007 10 26 07FDEA04670 1 20071024 A 5311 ACA0061501 FRAME DOUG DC10 DC1010 3022110 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 VANE AIR CONDITION LT SIDE STRUCTURE FRAME STA 535 DEFORMED AND CORROSION . SUSPECT SUPPORT FITTING CRACKED. PERFORMED NDI CHECK ON SUPPORT NO FOUND CRACK. REPAIRED SECTION FRAME FOR SRM 53-30-00 FIG 5 VOL I AND PROTECT FOR SRM 51-21-01 VOL II. 2 L 7 3 4F A22WE 2007102600068 20071026 00068 EU 2007 10 26 07FDEA04677 1 20071024 A 5311 LN9497A420 FRAME AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 FORWARD LOWER CARGO FRAME 38.2 LBL 8 TOP CAP IS CORRODED. REMOVED CORROSION IAW A310 SRM 51-74-10, ORIGINAL THICKNESS W AS .125 REMAINING THICKNESS IS .079, OUT OF LIMITS IAW A310 SRM 53-10-00. REMOVED AND FABRICATED NEW T-CAP AND SPLICE COUPLING IAW A310 SRM 53-10-15. TREATED AND INSTALLED IAW A310 SRM 51-21-10 AND 51-23-10 AND 51-40-30. 2 L 7 2 4F RT A35EU 2007102600082 20071026 00082 NM 2007 10 26 PIDR07012 1 20071012 A 5320 SUPPORT BRACKET BOEING 737 737301 1384611 NM BS 500C S9R CRACKED B PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 XAVIV 23560 DURING C CHECK, FOUND CRACK AT THE IB FASTENER FOR THE CABIN AIR CONDITIONING OUTLET SUPPORT BRACKET AT BS 500C JUST ABO VE S9R. REPAIRED IAW SB 737-53-1216. 2 L 7 2 4F RT A16WE 2007110800058 20071108 00058 NE 2007 11 8 DXTA200702550 2 20071018 A 7321 FLOW DIVIDER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LT ENGINE OUT OF RIG E DXTA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 333QS 5600333 LT ENGINE SHUTS DOWN ON SPEED BRAKE TEST. T/S LT ENGINE. FOUND ENG RIGGING LOOSE AND WITH EXCESS PLAY AT FLOW DIVIDER. RIGGED LT ENGINE. OPS CHECK GOOD. CHECKED RT ENG FOUND IN SAME CONDITION. RERIGGED. RT ENG OPS CHECK GOOD. ALSO CHECKED SPEED BRAKE TEST WITH NO DEFECTS. IAW MM 73-20-01. 2 L 7 2 4F 4 F RT A22CE E25EA 2007102600098 20071026 00098 CE 2007 10 26 GLBA20061014 1 20071015 A 5320 ANGLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA BS 288 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 247GL UE247 LT HEAVY ANGLE CRACKED AT FS 288. CRACK LENGTH APPROXIMATELY 1.75 INCH. MAINTENANCE REPAIRED LT HEAVY ANGLE AT FS 288 IA W 1900D SRM 53-90. REPAIR DIMENSIONS APPROXIMATELY 13.5 INCHES. RII COMPLIED WITH IAW TASKCARD 8.2.1. 2 L 7 2 4T 3 T RT A24CE E2NE 2007102600108 20071026 00108 EU 2007 10 26 COEA0718821 1 20070914 A 5751 S2711201300000 ARM AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE LT AILERON CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. FOUND LEVEL 2 CORROSION ON AILERON PENDULUM ARM. REPLACED ARM. WO NR 72241/NR 601039. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007102600155 20071026 00155 NM 2007 10 26 2007UALA04256 1 20071015 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 967-993 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 AFT GALLEY LT CREASE UPPER FLANGE CORRODED AT SERVICE DOOR CUTOUT AT FLOOR LEVEL BS 967-993 AT LBL 47-53. REMOVED AND REPLACED CREASE BEAM WITH NEW PART. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112000035 20071120 00035 NM 2007 11 20 07FDEA04774 1 20071113 A 3230 656021132MOD1 ACCESSORY UNIT BOEING 727 727225 1384077 NM MLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 465FE 21289 AFTER TAKEOFF, WITH GEAR RETRACTED, WHEN WE WENT FROM FLAPS 5 TO FLAPS 2 GOT THE TAKEOFF WARNING HORN, WOULD ONLY EXTING UISH BY REDUCING POWER. ALSO GOT THE HORN WHEN WE WENT FROM FLAPS 25 TO FLAPS 30 AT LANDING. R & R MLG ACCESSORY UNIT IAW MM 32-09-121-4 AND TESTED NORMALLY IAW MM 32-09-121-5. PERFORMED MLG MODULE ADJ/TEST MIN CHECKED OK IAW MM 32-09-12 2-5. ACCOMPLISHED NORMAL T/O WARNING SYS TESTS IAW MM 31-26-000-5. SUBSEQUENT TESTS NORM. VERIFIED WIRING OK TO SENSORS. RESISTANCES THRU THE SENSORS MATCH. 2 L 7 3 4F A3WE 2007112000036 20071120 00036 EU 2007 11 20 07FDEA04776 1 20071113 A 5340 R538D104820200 ADAPTER AIRBUS 310 A310203 3930313 EU SEAT TRACK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 MAIN CABIN FR 46 RT SIDE, ADAPTER CRACKED (OVER WING BOX) BS 2553 RBL 60. REMOVED AND REPLACED SEAT TRACK ADAPTER IAW SRM 51-40-21 PG7. 2 L 7 2 4F RT A35EU 2007102600172 20071026 00172 NM 2007 10 26 2007UALA04276 1 20071016 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 R2 DOOR UPPER HINGE CUTOUT TRIMMED ALL THE WAY UP TO BEND LINE OF FRAME REQUIRES REPAIR. FOUND NO CRACKS ON FRAME AFTE R NDT INSPECTION, INSTALLED REPAIR DOUBLER AS A PRECAUTIONARY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007102600173 20071026 00173 NM 2007 10 26 2007UALA04277 1 20071016 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 558UA 26654 EMERGENCY LIGHTS DOORS 1R & 4R EXTERIOR ARE INOP. 11-01-07 RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007102600174 20071026 00174 NM 2007 10 26 2007UALA04278 1 20071016 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 558UA 26654 CABIN EEL INOP ABOVE SEAT ROW 11 ABC. 2 L 7 2 4F 4 F RT A2NM E17NE 2007103100145 20071031 00145 2007 10 31 NOCA16107 4 20071024 A 2215 A718827 SERVO VALVE BOEING 767 76739H 1385311 NM AUTOPILOT MALFUNCTIONED A NOCA O OTHER J WARNING INDICATION CR CRUISE 1 EA 15 760NA 26257 CENTER AUTOPILOT WILL NOT ENGAGE. REPLACED CENTER AUTOPILOT SERVO VALVE PER MM 22-13-03. 2 L 7 2 4F RT A1NM 2007103100155 20071031 00155 NM 2007 10 31 2007UALA03930 1 20070926 A 3150 WARNING MESSAGE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE ILLUMINATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 792UA 26934 WINDSHEAR PREDICTIVE STATUS MSG. R SYS OK L SYS INOP. WINDSHEAR ALERTING FUNCTIONS ARE FAILED SUCH THAT WINDSHEAR ALERT ING CAPABILITY IS REDUCED OR NOT AVAILABLE. A REACTIVE WINDSHEAR FAILURE WILL ONLY SET THE MESSAGE WITH THE REACTIVE WI NDSHEAR OPTION ACTIVE. CYCLED POWER TO SYSTEM, MSG CLEARED. NO REPEAT MSG. AIRCRAFT OK FOR SERVICE. NO REPEAT MSG OV ER 14 DAYS. NO HARDWARE OR SOFTWARE CHANGE REQ'D. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007112100015 20071121 00015 NM 2007 11 21 CALA0700680 1 20071112 A 5313 6551628Y25 STRINGER BOEING 737 7373T0 1384582 NM BS 907-1016 S26L CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND STRINGER 26L CORRODED AT STA 907-1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-40-02, PAGE 1. 2 L 7 2 4F RT A16WE 2007103100161 20071031 00161 NM 2007 10 31 2007UALA04377 1 20071024 A 5343 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 FOUND CORROSION IN THE BORE OF THE NR 4 AFT TORQUE LINK FWD ATTACH POINT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007103100166 20071031 00166 EU 2007 10 31 2007UALA04384 1 20071024 A 3397 CONTACTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 461UA 1266 EMERGENCY LIGHT TEST FAILS MID CABIN EPSU RIGHT. FOUND DIRTY CONTACTS. CLEANED RIGHT OVER WING EXIT SIGN CONTACTS. EMERGENCY LIGHT SYSTEM TESTS OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007103100170 20071031 00170 NM 2007 10 31 2007UALA04302 1 20071018 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 584UA 26706 FOUND CORROSION IN AFT PIT AFT OF DOOR. FOUND CRACKED FLOOR SUPPORT WHICH WAS REPAIRED. AFT CARGO PIT WAS FOUND DAMAGE D AT ALL THREE AFT PIT FLOORBOARDS. SEVERAL PULLED SCREWS AT MULTI SPOTS TO CAUSE EDGE DELAMINATION DAMAGE. SOME DAM AGE IS LARGER THAN 1 INCH AND AT LEAST ONE HAD PUNCTURED THROUGH IN PANEL. THIS IS A MAJOR CORROSION REPAIR. REPLACED AFT CARGO FLOORBOARDS THAT ARE NOT REPAIRABLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007103100173 20071031 00173 SO 2007 10 31 RAIA00710027 1 20071023 A 3350 LIGHT EMB 145 EMB145 3260210 SO EXTERIOR INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 805HK 145096 POST FLT NR 3526 - PIT - MAIN DOOR EXTERIOR FLOOD LIGHT INOP. MAINTENANCE DEFERRED AS PER MEL. 2 L 7 2 4F RT T00011AT 2007103100174 20071031 00174 SO 2007 10 31 RAIA00710028 1 20071023 A 3234 8271013 CONTROL HANDLE EMB 145 EMB145LR 3260212 SO MLG MALFUNCTIONED A RAIA O OTHER J WARNING INDICATION TO TAKEOFF 1 CE 03 813HK 145044 FLT NR 5560 - OKC - GEAR WILL NOT RETRACT (GEAR HANDLE WILL RETRACT). MAINTENANCE REMOVED AND REPLACED LANDING GEAR CON TROL LEVER, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007103100175 20071031 00175 NM 2007 10 31 2007UALA04387 1 20071024 A 5230 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 FORWARD CARGO DOOR ASSY LOWER AFT FRAME INSIDE RADIUS CRACKED. FOUND STRESS FRACTURE. REPLACED LOWER AFT FRAME. 2 L 7 2 4F 4 F RT A16WE E21EU 2007103100176 20071031 00176 NM 2007 10 31 WRLA2007114 1 20071021 A 5753 ARC4125501 RIB DOUG MD11 MD11 3023602 NM PWA PW4062 PW4062 NE LT WING FLAP CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 273WA 48519 DURING 4C+12A CHECK, FOUND LT OUTBOARD FLAP NR 2 STOP FITTING CRACKED REF EGAT NRC U05061. PERFORMED BOEING SERVICE BUL LETIN MD11-57-075, REPLACED DAMAGED RIB REV 00. 2 L 7 3 4F 4 F RT A22WE E24NE 2007103100178 20071031 00178 SO 2007 10 31 C2XA07CL090 1 20071024 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NOSE GEAR DAMAGED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 15980 145202 MDW FLIGHT 2432 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT. THE AIRCRAFT RETURNED TO MDW AND LA NDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR WOW PROXIMITY SWITCH. OPERATIONAL CHEC KS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007103100179 20071031 00179 EA 2007 10 31 TRAX200701591 1 20071016 A 3350 COVER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 722EV 10127 LT AND RT EMERGENCY LIGHT LUMINESCENT STRIP PROTECTORS DAMAGED MID WAY THROUGH CABIN. 2 L 7 2 4F RT A21EA 2007103100182 20071031 00182 NM 2007 10 31 2007UALA04350 1 20071023 A 2497 W0820201B22 WIRE HARNESS BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SHORTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 677UA 30029 LAVATORY CALL SMOKE DETECTOR SYS CIRCUIT BREAKER P34 TRIPPED. FOUND WIRE BUNDLE W820 ABOVE FWD LAV (F1) WIRES WERE BEIN G SMASHED BY L1 DOOR WHEN DOOR HANDLE WAS PLACED IN CLOSE POSITION. SPLICED FOLLLOWING WIRES. W 0820-201B-22, 007-22, 01 4-22, 013-16, 015-22, 024-20, 001-20, 00 8-22, 018-18, 019-20, 016-22, 032-20. WD33-25-11PG3. SYS CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007103100184 20071031 00184 NE 2007 10 31 2007UALA04305 2 20071019 A 7250 BLADE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ENGINE FAILED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 483UA 1586 V11075 CREW COMMENTS: HEARD A BANG, GOT ECAM ENG 2 STALL. NO ABNORMAL ENG INDICATIONS, ENG RUNNING NORMAL SINCE. 11-01-07 FOUND NR 2 ENGINE STALL DUE TO DAMAGED HPC STAGE 6 BLADE- FOUND TORN AND BEYOND DAMAGE TOLERANCES. REPLACED NR 2 ENGI NE DUE TO DAMGE OF HPC STG 6 BLADE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007103100192 20071031 00192 NM 2007 10 31 2007UALA04313 1 20071019 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE R4 DOOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 BUSSEL EMERGENCY LIGHT INOP AT 4RT. 11-01-07 REPLACED LIGHT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110100007 20071101 00007 NM 2007 11 1 CALA0700610 1 20071025 A 5330 6545774 SKIN BOEING 737 7373T0 1384582 NM BS 727E+3 S23R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12327 23457 INSPECTION FOUND A .75 INCH CRACK IN FUSELAGE SKIN THREE INCHES AFT OF OF STA 727E AND JUST BELOW STRINGER 23R. REPAIRE D IAW ECRA 5331-01359. 2 L 7 2 4F RT A16WE 2007110100013 20071101 00013 NM 2007 11 1 SWAA075378 1 20071028 A 5311 6546554 FRAME BOEING 737 737317 138447P NM BS 500C S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110100014 20071101 00014 NM 2007 11 1 SWAA075381 1 20071028 A 5313 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 787 S13R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 13R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007110100015 20071101 00015 NM 2007 11 1 SWAA075396 1 20071028 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 727B S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007110100016 20071101 00016 NM 2007 11 1 SWAA075366 1 20071027 A 5753 65C30462 SKIN BOEING 737 7373H4 1384600 NM LT WING FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 DURING SCHEDULED BRDG CHECK, FOUND LT WING OUTBOARD FOREFLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007110100021 20071101 00021 NM 2007 11 1 SWAA075351 1 20071025 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED HC2 CHECK, LT FWD CABIN EMERGENCY EXIT LIGHTS WOULD NOT SHUT OFF WITH PILOT SWITCH. REMOVED AND REPLAC ED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007110100029 20071101 00029 NM 2007 11 1 SWAA075388 1 20071028 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM BS 947 S26L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND STRINGER 26L CORRODED AT BS 947. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007110100031 20071101 00031 NM 2007 11 1 SWAA075326 1 20071025 A 5311 6558280 FRAME BOEING 737 7375H4 138449D NM BS 360 S4-8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L AND 4L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110100033 20071101 00033 NM 2007 11 1 SWAA075341 1 20071025 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 727B S3L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007110100035 20071101 00035 2007 11 1 SWAA075364 4 20071028 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPL ACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007110100036 20071101 00036 NM 2007 11 1 SWAA075313 1 20071025 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 250WN 34972 DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007110100037 20071101 00037 NM 2007 11 1 SWAA075353 1 20071025 A 7160 314A1013 RIB BOEING 737 7373H4 1384600 NM NR 2 INLET CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED 14Y CHECK, FOUND NR 2 ENGINE INLET FWD BULKHEAD RIB CRACKED AT 10 O'CLOCK POSITION. REMOVED AND REPLAC ED BULKHEAD RIB PER SRM. 2 L 7 2 4F RT A16WE 2007110100040 20071101 00040 NM 2007 11 1 SWAA075380 1 20071028 A 5330 6545800 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT LOWER CORNER. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 2007110100041 20071101 00041 NM 2007 11 1 SWAA075367 1 20071028 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110100042 20071101 00042 NM 2007 11 1 SWAA075375 1 20071028 A 5311 6546529 FRAME BOEING 737 737317 138447P NM BS 440 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110100043 20071101 00043 NM 2007 11 1 UPS07M50985 1 20070813 A 2810 TANK DOUG MD11 MD11F 3023600 NM BS 1258 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C LT SIDE CENTER WING BOX TOPSIDE STA 1258.0 X=108.0 FOUND CORROSION ON TANK SKIN AS MARKED. LEFT SIDE CENTER WING BOX TOPSIDE STA 1258.0 X=108.0 FUEL TANK FASTENER AS MARK REMOVED. CORROSION ON UPP SKIN REMOVED & REWORKED AREAS PROTECTED. FPI & HFEC OPEN HOLE INSP C/OUT ON REWORKED AREA FOUND NO CRACK & NO CORROSION. REWORKED AREA UPP SK IN MAT'L REMOVED & REMAINED FOUND EXCEED LIMITS. FLAP PEENING C/OUT ON REWORKED AREA PER EN1638-07. 2 L 7 3 4F RT A22WE 2007110100046 20071101 00046 NM 2007 11 1 SWAA075321 1 20071025 A 5315 6584176 FLOORBEAM BOEING 737 7375H4 138449D NM BS 706 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CRACKED AT BS 706, LBL 49. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007110100047 20071101 00047 NM 2007 11 1 SWAA075370 1 20071028 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110100048 20071101 00048 WP 2007 11 1 UPS07851007 1 20071025 A 2910 HYDRAULIC SYSTEM DOUG DC8 DC871F 302199D WP FAILED A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 755UP 46055 INSPECTION TYPE:N/A ATB - HYDRAULIC SYSTEM FAILURE, LEAK IN RT MLG WHEEL WELL. INSTALL SERVICE HOSE/FTG PER MM 32-32-03 -2 & AMM 20-13-00-2. REMOVED AND REPLACED LT & RT ENG HYD PUMP CASE DRAIN FILTER ELEMENTS PER AMM 29-10-15-2-2. INSPEC T PER MM 29-10-16-2. NO FOREIGN MATERIAL OR LEAKS NOTED. OPS CHECK ON EA EDP PER AMM 29-10-12-4, OPS NORMAL SERVICED H YD RESERVOIR PER AMM 12-30- 01-3. OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2007110100049 20071101 00049 2007 11 1 UPS07851013 4 20071026 A 2565 HOUSING DOUG DC8 DC873F 302199F WP ESCAPE SLIDE OPEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 ESCAPE SLIDE HOUSING IS PARTIALLY OPEN. SECURED ESCAPE SLIDE HOUSING PER MM 25-60-01-2. 2 L 7 4 4F RT 4A25 2007110100051 20071101 00051 NM 2007 11 1 SWAA075352 1 20071025 A 7160 314A1013 RIB BOEING 737 7373H4 1384600 NM NR 2 INLET CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED 14Y CHECK, FOUND NR 2 ENGINE INLET FWD BULKHEAD RIB CRACKED AT 2 O'CLOCK POSITION. REMOVED AND REPLACE D BULKHEAD RIB PER SRM. 2 L 7 2 4F RT A16WE 2007110100053 20071101 00053 NM 2007 11 1 SWAA075384 1 20071028 A 5311 6546593 FRAME BOEING 737 7373A4 1384585 NM BS 500A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110100054 20071101 00054 2007 11 1 SWAA075360 4 20071026 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007110100055 20071101 00055 NM 2007 11 1 CALA0700611 1 20071025 A 5330 6545774 SKIN BOEING 737 7373T0 1384582 NM BS 727E S26L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12327 23457 INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT STA 727E + 3, S23L. REPAIRED IAW SRM 53-00-01, REPAIR 31, FIGURE 20 1, PROCEDURE 5. 2 L 7 2 4F RT A16WE 2007110100059 20071101 00059 NM 2007 11 1 SWAA075337 1 20071025 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 727D S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007110100061 20071101 00061 NE 2007 11 1 SWAA075320 2 20071023 A 7200 CFM567B24G22 ENGINE BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B22 13802 NE NR 1 SEIZED A SWAA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SW 29 433LV 33716 889231 INFLIGHT SHUT DOWN/DECLARED, EMERGENCY/AIR TURNBACK. NR 1 ENGINE SEIZED AT 22,000 FT. REMOVED AND REPLACED NR 1 ENGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007110100063 20071101 00063 2007 11 1 SWAA075379 4 20071028 A 2565 MS51923599 PIN BOEING 737 7373T5 1384608 NM L2 DOOR GIRT BAR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR GUIDE PIN MISSING. INSTALLED PIN PER MM. 2 L 7 2 4F RT A16WE 2007110100065 20071101 00065 NM 2007 11 1 SWAA075385 1 20071028 A 5311 6546538 FRAME BOEING 737 7373A4 1384585 NM BS 597 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110100068 20071101 00068 NM 2007 11 1 SWAA075399 1 20071028 A 5313 6551698 STRINGER SPLICE BOEING 737 737317 138447P NM BS 908 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER S RM. 2 L 7 2 4F RT A16WE 2007110100073 20071101 00073 NM 2007 11 1 SWAA075343 1 20071025 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 727B S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007110100075 20071101 00075 2007 11 1 SWAA075314 4 20071025 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 267WN 32525 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007110100080 20071101 00080 NM 2007 11 1 SWAA075393 1 20071028 A 3350 D717021000 CHARGER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 770SA 30589 DURING SCHEDULED MV2 CHECK, FOUND LT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007110100081 20071101 00081 NM 2007 11 1 2007UALA04316 1 20071019 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHT INOP 48 HJK. 11-01-07 RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110100082 20071101 00082 NM 2007 11 1 2007UALA04317 1 20071019 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHTS AT 2J AFT, 23 ABC & 44 HJK ARE INOPERATIVE. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110100083 20071101 00083 EU 2007 11 1 2007UALA04318 1 20071019 A 3150 WARNING LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 490UA 1728 RTFL DUE TO ECAM YELLOW ENGINE 2 PUMP FAULT. FOUND PUMP NR 2 FAILED AND LEAKING. REPLACED PUMP. LEAK CHECKED ALL NORMA L. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110100084 20071101 00084 EU 2007 11 1 2007UALA04319 1 20071020 A 3310 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT/CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 409UA 462 DURING INITIAL CLIMBOUT STRONG ELECTRICAL ODOR IN CABIN AND COCKPIT, ODOR DISSIPATED SHORTLY. 11-01-07 FOUND F/O MAP LIGHT SHORTING. REPLACED THE F/O MAP LIGHT ON THE F/O WINDOW. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110100087 20071101 00087 NM 2007 11 1 SWAA075242 1 20071023 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 448WN 33721 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007110100088 20071101 00088 NM 2007 11 1 SWAA075239 1 20071023 A 3350 417A5703 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED HC1 CHECK, FOUND EEPLS INOP AT ROW 8 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007110100094 20071101 00094 NM 2007 11 1 SWAA075254 1 20071023 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 947, RBL 6. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007110100098 20071101 00098 NM 2007 11 1 SWAA075251 1 20071023 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM BS 480 S27R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 480, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007110100100 20071101 00100 NM 2007 11 1 SWAA075397 1 20071028 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 400 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007110100101 20071101 00101 NE 2007 11 1 2007UALA04338 2 20071022 A 7230 BLADE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE HPC BENT A UALA O OTHER C F.O.D. NR NOT REPORTED 1 WP 29 644UA 25094 6TH STAGE HPC BLADE HAS BENT AND DISTORTED IMPACT DAMAGE 0.5 INCH FROM BLADE TIP. LENGTH OF DAMAGE 0.5 AND BEND IS .125 INCH. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110100103 20071101 00103 NM 2007 11 1 2007UALA04389 1 20071025 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY CEILING LIGHT AT ROW 25ABC INOPERATIVE. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110100106 20071101 00106 NM 2007 11 1 2007UALA04392 1 20071024 A 5210 LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR ASSIST DISCONNECTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 582UA 26702 EMERGENCY POWER RESERVOIR LINE WAS NOT CONNECTED TO DOOR ASSIST PRESSURE BOTTLE DOOR 2R. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110100107 20071101 00107 NM 2007 11 1 2007UALA04393 1 20071024 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 582UA 26702 DOOR 2R AND RIGHT OVERWING FWD EXTERIOR EMERGENCY LIGHTS INOP, WHEN SELECTED BY EMERGENCY LIGHT TEST ON NLG. RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110100112 20071101 00112 NM 2007 11 1 2007UALA04396 1 20071024 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 648UA 25285 EMERGENCY LIGHT PATH IN FRONT OF MIDDLE LT LAVATORY INOP. RECONNECTED PATH CONNECTOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110100115 20071101 00115 EU 2007 11 1 TRAX200701582 1 20071023 A 5320 ANGLE AEROSP ATR72 ATR72 EU LT MLG WW CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 RIGHT MLG LWR ANGLE ON FWD SURFACE AT FR 27 BL 0 CORRODED. CORROSION REMOVED IAW SRM 51-21-42 FOUND WITHIN LIMIT OF S RM 51-10-10MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.002 WITHIN LIMITS AS PER SRM: 51-10-10. 2 H 7 2 4T RT 2007110100116 20071101 00116 NM 2007 11 1 SWAA075325 1 20071025 A 3350 10107451 SIGN BOEING 737 7375H4 138449D NM EMERGENCY EXIT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 FWD CABIN EMERGENCY EXIT SIGN MISSING. INSTALLED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007110100118 20071101 00118 2007 11 1 2007UALA04323 4 20071021 A 2565 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE DOOR 2R SLIDE READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 437UA 655 DOOR 2R SLIDE BOTTLE PRESSURE LOW. SERVICED DOOR ACCUMULATOR AS NEEDED. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110100120 20071101 00120 EU 2007 11 1 2007UALA04324 1 20071020 A 3397 FEEDER CABLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 437UA 655 FWD EEL STRIP IN FIRST CLASS INOPERATIVE. FOUND BROKEN WIRE. REPLACED CABLE. CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110100124 20071101 00124 NM 2007 11 1 2007UALA04328 1 20071020 A 5300 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 310-350 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 FWD CABIN CREASE BEAM AT DOOR 1L CORRODED, BS 310-350. REPLACED FORWARD ENTRY DOOR WAY CABIN FLOOR CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110100126 20071101 00126 NM 2007 11 1 2007UALA04330 1 20071021 A 2612 S332T10135 FIRE DETECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU APU BAY NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 312UA 23673 APU FIRE LIGHT WON'T TEST. AFTER EXTENSIVE TROUBLE SHOOTING FOUND FIRE LOOP WEAR. REPLACED LOOP OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110100127 20071101 00127 NM 2007 11 1 SWAA075317 1 20071025 A 2761 654485114 ACTUATOR BOEING 737 7373H4 1384600 NM SPOILER WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD GROUND SPOILER OUTBOARD ACTUATOR WORN. REMOVED AND REPLACED ACTUATOR P ER MM. 2 L 7 2 4F RT A16WE 2007110100128 20071101 00128 NM 2007 11 1 SWAA075355 1 20071025 A 5311 6545632 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110100130 20071101 00130 NM 2007 11 1 ASAA0752158 1 20071024 A 2742 251A45105 ACTUATOR BOEING 737 737890 1384527 NM STAB TRIM INOPERATIVE A ASAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 02 579AS 35187 STABILIZER OUT OF TRIM LIGHT ILLUMINATED DURING ACCELERATION. APPEARS AUTO PILOT NOSE DOWN TRIM IS INOP. REPLACED STAB ILIZER TRIM MOTOR. 2 L 7 2 4F RT A16WE 2007110100132 20071101 00132 2007 11 1 ASAA0752157 2 20071024 A 7532 1074926 BLEED VALVE BOEING 737 737890 1384527 NM NR 2 ENGINE FAULTY A ASAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 02 577AS 35186 RT BLEED TRIP OFF LIGHT ON CLIMBOUT. WOULD NOT EXTINGUISH. DUCT PRESSURE SPLIT BEFORE TRIP RT=15PSI LT= 45 PSI. REPLA CED NR 2 ENGINE BLEED AIR REGULATOR. 2 L 7 2 4F RT A16WE 2007110100134 20071101 00134 NM 2007 11 1 ASAA0742155 1 20071024 A 5340 69374023 ATTACH ANGLE BOEING 737 7374Q8 138447Q NM BS 277-291 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 CLIP WEB ATTACH ANGLE STA 277 291 RBL 56 HAS 6 EACH ELONGATED HOLES. FABRICATED AND INSTALLED NEW ANGLE IAW BAC DWG 69 37402 AND 65 45875. 2 L 7 2 4F RT A16WE 2007110100138 20071101 00138 EU 2007 11 1 TRAX200701560 1 20071022 A 5720 PLATE AEROSP ATR72 ATR72 EU WING BOX CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 RIGHT WING BOX FR 28A FACE PLATE CRACKED. REPLACED IAW SRM 51-25-01. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACC ORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01. 2 H 7 2 4T RT 2007110100139 20071101 00139 EU 2007 11 1 TRAX200701561 1 20071022 A 5711 FRAME AEROSP ATR72 ATR72 EU WING BOX CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 RIGHT WING BOX FR 28 CRACKED. REPLACED IAW SRM 51-25-01 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01. 2 H 7 2 4T RT 2007110100140 20071101 00140 NM 2007 11 1 SWAA075374 1 20071028 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 460 S1 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007110100144 20071101 00144 EU 2007 11 1 TRAX200701571 1 20071022 A 5210 SKIN AEROSP ATR72 ATR72 EU PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 PAX DOOR INNER SKIN CRACKED TWO LOCATIONS AROUND NUT PLATE HOLES FWD TOP AREA. 2 H 7 2 4T RT 2007110100145 20071101 00145 NM 2007 11 1 SWAA075356 1 20071025 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 328 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007110100146 20071101 00146 2007 11 1 SWAA075347 4 20071025 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007110100147 20071101 00147 2007 11 1 SWAA075350 4 20071025 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007110100149 20071101 00149 NM 2007 11 1 SWAA075348 1 20071025 A 3350 D71702030 CHARGER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 770SA 30589 DURING SCHEDULED MV2 CHECK, FOUND LT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007110100156 20071101 00156 NE 2007 11 1 2007UALA04337 2 20071020 A 7250 BLADE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ENGINE FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 641UA 25091 727886 ECM HAS DETECTED PARAMETERS SHIFT AT BOTH TAKEOFF AND CRUISE. ENGINE REPLACED. SHOP TEARDOWN REVEALED HEAVY HPC BLADE DAMAGE. THE DAMAGE WAS A RESULT OF FAILURE IN A 5TH STAGE DISK KNIFE EDGE. A 5-INCH SECTION OF THE FRONT KNIFE EDGE FRA CTURED, CAUSING A 2-INCH SECTION OF THE STAGE-5 BLADE LEADING EDGE TO LIBERATE, AND SUBSEQUENT DOWNSTREAM BLADE DAMAGE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110100158 20071101 00158 NM 2007 11 1 SWAA075274 1 20071024 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 787 S19L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 19L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007110100160 20071101 00160 NM 2007 11 1 SWAA075299 1 20071024 A 5753 SKIN BOEING 737 7377H4 1384404 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 758SW 27873 DURING SCHEDULED 8Y CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED INBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007110100161 20071101 00161 NM 2007 11 1 SWAA075305 1 20071024 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM BS 520 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 9R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007110100163 20071101 00163 EA 2007 11 1 A6WA200740558 1 20070918 A 5220 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ESCAPE HATCH FAILED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 WO 114147, MWC 144, CREW ESCAPE HATCH OUTER HANDLE WILL NOT OPEN. REMOVED AND REPLACED CREW ESCAPE HATCH OUTSIDE HANDLE IAW CMM 52-22-03, FUNCTIONAL TEST OF OUTSIDE HANDLE GOOD IAW CMM 52-22-03. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007110100167 20071101 00167 EU 2007 11 1 COEA0712821 1 20070827 A 5310 S53673000211 CREASE BEAM AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE DAMAGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. FOUND TOOLING DAMAGE 3 PLACES ON CREASE BEAM WEB. FABRICATED REPLACEMENT CREASE BEAM WEB. ( K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007102600156 20071026 00156 NM 2007 10 26 2007UALA04257 1 20071015 A 3260 1171188 SWITCH BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE MLG LOCK FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 104UA 26902 THE "RIGHT BODY GEAR RIGHT ACTUATOR LOCK SWITCHES DISAGREE" HAS OCCURRED AT LEAST 3 OUT OF LAST 5 FLT. FOUND RT GEAR ST EARING ACTUATOR, ALTERNATE INBOARD SWITCH SHOWING UNLOCKED. REPLACED RT BODY LANDING GEAR RT ACTUATOR ALTERNATE SWITCH IAW MM 32-53-16. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102600157 20071026 00157 NM 2007 10 26 2007UALA04258 1 20071015 A 3510 MC1019151 OXYGEN MASK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CAPTAIN'S LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26877 OXYGEN MASK STOWAGE COMPARTMENT DEFECTIVE - CAPT. REW COMMENTS: CAPT O2 MASK LEAKS WHEN DEPLOYED AND LEFT PANEL IN CLO SED FOR COMMS PLUNGER IS OUT OF ADJUSTMENT. REPLACED CAPTAIN 02 MASK, OPS CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102900003 20071029 00003 NM 2007 10 29 2007UALA04287 1 20071017 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 580 S22-24L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 FWD PIT STA 580 MAIN FRAME BETWEEN STR 22L AND 24L HAS 2 DENTS. 10-30-07 MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGE . INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007102900009 20071029 00009 NM 2007 10 29 2007UALA04296 1 20071018 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 EEL INOP: SEATS 3A FWD SECTION & 4J AFT SECTION. 11-01-07 RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102900012 20071029 00012 NM 2007 10 29 2007UALA04299 1 20071017 A 2750 CONTROL CABLE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE TE FLAPS OUT OF RIG A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 673UA 29241 EICAS MSG T/E FLAP DISAGREE DISPLAYED, TRAILING EDGE LIGHT ILLUMINATED, WHEN ANY T/E FLAP POSITION SELECTED. FLAPS FAIL TO MOVE TO SELECTED POSITION. FLAPS 25 TO 20. FOUND FLAP CONTROL LEVER CABLE RUN WFA AND CABLE RUN WFB TENSION LOW AT APPROX. 35 LBS ON EACH CABLE RIGGED CABLES PER MM27-51- 25. REPLACED M548 TRANSFORMER REF MM27-81- 11. ADJ. REF TABLE 4 02 FSEU TEST OK. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102900013 20071029 00013 NM 2007 10 29 2007UALA04300 1 20071017 A 3260 WARNING LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MLG ILLUMINATED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 533UA 25073 AFTER DEPARTURE "GEAR DISAGREE" INDICATION WAS DISPLAYED ON EICAS. MESSAGE WAS DISPLAYED FOR APPROX 15 MIN UNTIL AIRCRA FT ENCOUNTERED SLIGHT TURBULENCE AND CAUSED MESSAGE TO CLEAR AND AMBER "GEAR" LIGHT TO EXTINGUISH. 2 L 7 2 4F 4 F RT A2NM E17NE 2007102900020 20071029 00020 EU 2007 10 29 WRNA200700053 1 20070723 A 5410 6361507 SUPPORT AIRBUS 300 A300B4203 3930306 EU NR 2 NACELLE CRACKED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 510TA 100 DURING M-96 CHECK, A 3 INCH CRACK WAS FOUND IN THE NR 2 ENGINE OUTBOARD CORE COWL SUPPORT. ACCOMPLISHED WELD REPAIR IAW ENGINEERING ORDER 2-54907-800 FROM EMTEQ. 2 L 7 2 4F RT A35EU 2007102900021 20071029 00021 EU 2007 10 29 WRNA200700054 1 20070624 A 5315 FLOORBEAM AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 510TA 100 DURING M-96 CHECK, FLOOR SUPPORT BEAM IN AFT CARGO A7 FRAME 63 WAS FOUND CORRODED AND HAD A 5 INCH CRACK BETWEEN STR 41L AND 43L. CUT OUT DAMAGED SECTION OF FLOORBEAM CAP ANGLE AND INSTALLED 12 INCH LENGTH OF FLOORBEAM AND REPAIR DOUBLER I AW SRM 51-41-40. 2 L 7 2 4F RT A35EU 2007102900022 20071029 00022 NM 2007 10 29 KCSA071478 1 20071021 A 5315 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 760 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FWD PIT FLOORBEAM UPPER CHORD DAMAGED AT BS 760, LBL 10. 2 L 7 4 4F RT A20WE 2007102900023 20071029 00023 NM 2007 10 29 KCSA071479 1 20071021 A 5330 SKIN BOEING 747 7472B4B 138481B NM BS 1319 S16R CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 MAIN DECK R-3 DOOR OPENING AFT UPPER INTERNAL SKIN CORRODED AT BS 1319, STR 16R. 2 L 7 4 4F RT A20WE 2007102900025 20071029 00025 NM 2007 10 29 KCSA071481 1 20071021 A 5330 SKIN BOEING 747 7472B4B 138481B NM BS 672 S38R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FUSELAGE SKIN DAMAGED AT BS 675, STR 38R. 2 L 7 4 4F RT A20WE 2007102900032 20071029 00032 EU 2007 10 29 WRNA200700056 1 20070625 A 5315 FLOORBEAM AIRBUS 300 A300B4203 3930306 EU FUSELAGE CRACKED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 510TA 100 DURING M-96 CHECK, FOUND LOWER CROSS BEAM OF FLOORBEAM AT FRAME 57 BL 0 CRACKED. STOP DRILLED CRACK AND INSTALLED REPAI R DOUBLER IAW SRM 51-40-30. 2 L 7 2 4F RT A35EU 2007102900034 20071029 00034 EU 2007 10 29 RNA200700054 1 20070624 A 5315 FLOORBEAM AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 510TA 100 DURING M-96 CHECK, FLOOR SUPPORT BEAM IN AFT CARGO AT FRAME 63 WAS FOUND CORRODED AND HAD A 5 INCH CRACK BETWEEN STR 41L AND 43L. CUT OUT DAMAGED SECTION OF FLOORBEAM CAP ANGLE AND INSTALLED 12 INCH LENGTH OF FLOORBEAM AND REPAIR DOUBLER I AW SRM 51-41-40. 2 L 7 2 4F RT A35EU 2007102900044 20071029 00044 NM 2007 10 29 UPS07M50955 1 20071010 A 5754 ARB2850506 RIB DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 279UP 48573 INSPECTION TYPE:2C RIGHT NR 16 SLAT TRACK INBOARD L/E RIB FITTING IS CRACKED. REMOVED AND REPLACED RIGHT NR 16 SLAT TRA CK INBOARD L/E RIB FITTING IAW MD-11 SRM 51-31-01 AND 51-33-01. 2 L 7 3 4F RT A22WE 2007102900048 20071029 00048 NM 2007 10 29 CALA0700598 1 20071022 A 5315 BAC1518940 FLOORBEAM BOEING 737 737524 1384721 NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11612 27325 INSPECTION FOUND SURFACE CORROSION ON FLOORBEAM AT STA 986, RBL 40. A REPAIR STRAP WAS INSTALLED IAW SRM 53-60-51. 2 L 7 2 4F RT A16WE 2007102900049 20071029 00049 NM 2007 10 29 CALA0700599 1 20071022 A 5315 BAC1518940 FLOORBEAM BOEING 737 737524 1384721 NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11612 27325 INSPECTION FOUND SURFACE CORROSION ON FLOORBEAM AT STA 986, RBL 4. A REPAIR STRAP WAS INSTALLED IAW SRM 53-60-51. 2 L 7 2 4F RT A16WE 2007102900055 20071029 00055 EU 2007 10 29 USAA920070959 1 20070921 A 5210 A5211002520000 STOP AIRBUS 320 A320231 3930325 EU ZONE 800 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 636AW 098 SAL - MAJOR REPAIR - C-05 CHECK - CORROSION ON THE L2 DOOR STOP ASSEMBLY, BEAM 3. REPLACED THE L2 DOOR STOP ASSEMBLY, B EAM 3 IAW A320 AMM 52-11-00. 2 L 7 2 4F RT A28NM 2007102900088 20071029 00088 NM 2007 10 29 SWAA075188 1 20071021 A 5755 65465168A SKIN BOEING 737 7373H4 1384600 NM NR 7 SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED A2 CHECK, FOUND RIGHT WING NR 7 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM . 2 L 7 2 4F RT A16WE 2007102900096 20071029 00096 NM 2007 10 29 SWAA075197 1 20071021 A 5311 6546596 FRAME BOEING 737 7375H4 138449D NM BS 727B S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007102900102 20071029 00102 NM 2007 10 29 SWAA075167 1 20071021 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 360 S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007102900103 20071029 00103 NM 2007 10 29 SWAA075168 1 20071021 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 706 S2R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007102900107 20071029 00107 NM 2007 10 29 SWAA075165 1 20071021 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 747 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007102900123 20071029 00123 NM 2007 10 29 ASAA0752130 1 20071018 A 2430 284A04214 CONTROL UNIT BOEING 737 737890 1384527 NM E&E BAY INOPERATIVE A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 583AS 35681 ELECT WARNING LIGHT ON OVERHEAD PANEL ILLUMINATED. BITE TEST SHOWS SPCU INOP. REPLACED SPCU, OP CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2007102900127 20071029 00127 NM 2007 10 29 ASAA0792114 1 20071008 A 5315 FLOORBEAM BOEING 737 737990 NM BS 727I S26L/R CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 305AS 30013 AFT CARGO PIT FLOOR SUPPORT TEE BS 727I+6 RBL 17 TO LBL 17 FOUND CORRODED. AFT CARGO PIT SUPPORT TEE AT BS 727I+6 RBL 1 7 TO LBL 17 WAS REPLACED WITH MADE REPAIR PART IAW B737 900 SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007102900140 20071029 00140 WP 2007 10 29 ASAA0782129 1 20071022 A 5753 5950494504 VANE DOUG DC9 DC983 3022083 WP TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 RIGHT WING I/B FLAP I/B VANE LWR SURFACE HAS GRAVEL DAMAGE (DENTED). PREPARED DAMAGED AREA, FABRICATED FILLER AND REPAI R DOUBLER BONDED AND INSTALLED FASTENERS IAW MD80 SRM 51-70-2 PGS 23, 43, 46, 59, 63 AND 64. 2 L 7 2 4F RT A6WE 2007102900162 20071029 00162 EA 2007 10 29 A6WA071024001 1 20071001 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 411ZW 7569 FOUND FS 280 FLOOR SUPPORT BEAM CLIP AT LBL 9.0, INBOARD, IS CRACKED IN RADIUS APPROX .50 INCH LONG. (M) 2 L 7 2 4F RT A21EA 2007103000061 20071030 00061 EA 2007 10 30 TRAX200701529 1 20071016 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 PAX DOOR EXIT PLACARD IS DAMAGED. 2 L 7 2 4F RT A21EA 2007103000062 20071030 00062 EA 2007 10 30 TRAX200701530 1 20071018 A 5340 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 RIGHT I/B BATH TUB FITTING CRACKED. 10-30-07 REMOVED 2 ACCESS PANELS JUST O/B OF BATHTUB FITTING IAW CRJ 200 SRM 5 1-41-02. LOCATED HOLES IN SERVICEABLE FITTING P/N 600-31068-19 IAW CRJ 200 SRM 51-40-11. OK TO INSTALL. INSTALLED ALL L OCK FASTENERS THROUGH SERVICEABLE FITTING P/N 600-31068019 IAW CRJ 200 SRM 51-42-21. REQUIRES INSTALLATION OF SOLID RIVE TS. ISNTALLED SOLID RIVETS IAW CRJ SRM 51-42-06. OK TO REINSTALL TWO EA INSP PNLS O/B OF FILLING. REINSTALLED 2EA PNLS I AW CRJ SRM 51-41-02. REINSTALLED PREVIOUS REMOVED 4EA WIRE BUNDLE TIE DOWN BRACKETS. IAW CRJ SRM 51-41-02. 2 L 7 2 4F RT A21EA 2007103000063 20071030 00063 EA 2007 10 30 TRAX200701531 1 20071019 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 CLIP CRACKED AT FS 484 I/B OF RBL 36. 10-30-07 CUT AWAY DAMAGED ATTACHMENT FLANGE OF 601R31171-15 REF AS SHOWN IN SH EET 3 OF REO 601R-53-41-059 REV A. PERFORMED LPI OF CUTLINE PER DNTM 51-20-08 IAW ASA REO 601R-53-41-059 REV A SHEET 3 STEP 2. NO DEFECTS NOTED. OK TO TOUCH UP CUT EDGE TOUCH UP FINISH A023 PER CRJ SRM 51-21-16 FABRICATED ANGLE, INSTALL ED ANGLE IAW ASA REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2007103000064 20071030 00064 EA 2007 10 30 TRAX200701532 1 20071019 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 CLIP CRACKED AT FS 484 O/B OF RBL 27. 10-30-07 REMOVED CRACKED CLIP AT FS 484. LOCATED AND DRILLED NEW ANGLE IAW REO 601R-53-41-057. OK TO TREAT AND PRIME. TREATED PRIMED AND TOPCOATED IAW CRJ SRM 51-21-11 51-25-06 51-25-16. OK TO INSTALL NEW ANGLE. INSTALLED CLIP IAW CRJ SRM 51-42-21 AND REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2007103000065 20071030 00065 NM 2007 10 30 KCSA071502 1 20071026 A 5311 FRAME BOEING 747 7472B4B 138481B NM BS 500 S14L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA 500 FRAME SPLICE ANGLE CRACKED AT STR 14L CUT OUT CRACK IS .5 INCH. 2 L 7 4 4F RT A20WE 2007103000066 20071030 00066 NM 2007 10 30 SWAA075306 1 20071024 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 482A S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482A, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000067 20071030 00067 EU 2007 10 30 SA07067 1 20071019 A 3350 32145510 EPSU AIRBUS A321 A321211 3930370 EU EMERGENCY LIGHTS FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 162UW 23927 1412 TPA - SEVERAL EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE RIGHT HAND, CENTER EMERGENCY POWER SUPP LY UNIT. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007103000068 20071030 00068 EU 2007 10 30 SA07068 1 20071019 A 3350 Z040H0005110 DEU AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHTS FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 700UW 26991 0885 PIT - THE EMERGENCY EXIT LIGHTS ON EMERGENCY EXIT DOORS 2L & 2R WERE FOUND INOPERATIVE. MAINTENANCE REPLACED DEU B (FIN 300RH5). OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007103000069 20071030 00069 EU 2007 10 30 SA07069 1 20071020 A 2150 A/C PACK AIRBUS A321 A321211 3930370 EU CABIN AIR INOPERATIVE A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 181UW 1531 PHX FLT 700 EN ROUTE PHX TO PHL. AT APPROXIMATELY 100 MILES EAST OF ABQ, AT FL310, THE CABIN ALTITUDE HAD CLIMBED TO 13 ,000 FT. THE CREW REPORTED A PACK ONE FAULT WITH THE NUMBER TWO PACK ON MEL AT THE TIME. THE FLIGHT DESCENDED TO 10,00 0 FEET AND RETURNED TO FIELD PHX WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NO PACK OR BLEED FAULTS ON THE POST FLIGHT REPORT. PERFORMED A BITE CHECK OF THE CABIN PRESSURE CONTROLLER AND TEMPERATURE CONTROLLER. NO FAULTS FOUND. RAN BOT H ENGINES WITH BLEED AND PACK INDICATION NORMAL. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2007103000070 20071030 00070 SO 2007 10 30 C2XA07SH089 1 20071029 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11551 411 SHV - DURING C-CHECK CENTER OMEGA BEAM CORROED BEYOND ALLOWABLE LIMITS ON FR 20. MAINTENANCE REMOVED AND REPLACED CENTE R OMEGA BEAM FROM 18 TO 23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007103000071 20071030 00071 SO 2007 10 30 C2XA07SH088 1 20071026 A 3350 110049 CHARGER EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12934 145019 SERVICE ROUTINE EMERGENCY LIGHT AT PANELS 194 AND 195 INOP. MAINTENANCE REMOVED AND REPLACED NR 4 BATTERY CHASSIS ASSEM BLY IAW EMB 145 AMM 33-50-04, OPS CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007103000072 20071030 00072 SO 2007 10 30 RAIA00710029 1 20071023 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 816HK 145055 PRE FLT NR 5579 - STL - EMERGENCY LIGHT FLOOR PROXIMITY LIGHT INOP. MAINTENANCE RESECURED LOOSE CONNECTION & OPS CHECKE D GOOD. 2 L 7 2 4T RT T00011AT 2007103000073 20071030 00073 SO 2007 10 30 C2XA07IA227 1 20071022 A 3350 7287580501 LIGHT EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14514 145303 DURING SCHEDULED MAINTENANCE THE EMERGENCY STRIP LIGHT AT ROW 3A TO 7A WAS FOUND TO BE INOPERATIVE. THE FLOOR STRIP WIR ING WAS FOUND TO BE CHAFED. THE AFFECTED WIRE WAS REPAIRED, THE LIGHTS OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED . 2 L 7 2 4F RT T00011AT 2007103000074 20071030 00074 SO 2007 10 30 C2XA07SH085 1 20071024 A 5330 14538924402 PANEL EMB 145 EMB145XR 3260214 SO DEBONDED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11113 662 SHV - DURING C-CHECK MAINTENANCE FOUND PANEL 197 DR WITH DEBONDED BONDING PLATE. MAINTENANCE REPAIRED PANEL 197 DR BOND ING PLATE IAW EC5750-01315 REV E. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007103000075 20071030 00075 SO 2007 10 30 C2XA07SH084 1 20071022 A 2131 912R0201 CONTROLLER EMB 135 EMB135LR 3260305 SO CABIN PRESSURE DEFECTIVE A C2XA G O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 SW 27 12530 553 FLIGHT 2449 - SHV - PILOT REPORTED LVL AT FL260 SLOW LOSS OF CABIN PRESSURE AT CABIN ALT 9500FT TRIED QRH AND MANUAL CON TROL BUT CABIN THEN WENT QUICKLY UP TO 10,500, 12,500 AND PEAKED AT 14,000FT CABIN ALT. PAX O2 MASKS AUTO DEPLOYED AND WERE USED. FAILURE OF CPAM OR ELECTRO PNEUMATIC VALVE. MAINTENANCE REMOVED AND REPLACED MANUAL CONTROLLER IAW EMB 135 AMM 21-31-02. PERFORMED ALL OPS CHECK, ALL OPS CHECK GOOD NO DEFECTS NOTED. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE . 2 L 7 2 4F RT T00011AT 2007103000076 20071030 00076 SO 2007 10 30 C2XA07SH086 1 20071024 A 5330 14538924404 PANEL EMB 145 EMB145XR 3260214 SO DEBONDED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11113 662 SHV - DURING C-CHECK MAINTENANCE FOUND PANEL 197CL WITH DEBONDED BONDING PLATE. MAINTENANCE REPAIRED PANEL 197CL IAW EC 5750-01315 REV E. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007103000077 20071030 00077 NM 2007 10 30 SWAA075282 1 20071024 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 685 S2R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000078 20071030 00078 NM 2007 10 30 SWAA075283 1 20071024 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 685 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000079 20071030 00079 NM 2007 10 30 SWAA075293 1 20071024 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 727D S5L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000080 20071030 00080 NM 2007 10 30 SWAA075285 1 20071024 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 727A S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000081 20071030 00081 NM 2007 10 30 SWAA075294 1 20071024 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 727D S6L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000082 20071030 00082 NM 2007 10 30 SWAA075288 1 20071024 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 727D S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000083 20071030 00083 NM 2007 10 30 SWAA075289 1 20071024 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 727D S6R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000084 20071030 00084 NM 2007 10 30 SWAA075297 1 20071024 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 727C S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000085 20071030 00085 NM 2007 10 30 SWAA075217 1 20071022 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 727A S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000086 20071030 00086 NM 2007 10 30 SWAA075216 1 20071022 A 5311 65C33511 FRAME BOEING 737 7375H4 138449D NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007103000087 20071030 00087 NM 2007 10 30 SWAA075206 1 20071022 A 5311 65C34356 FRAME BOEING 737 7375H4 138449D NM BS 482A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007103000088 20071030 00088 NM 2007 10 30 SWAA075214 1 20071022 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 360 S22L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER 22L CORRODED AT BS 360. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007103000089 20071030 00089 NM 2007 10 30 SWAA075205 1 20071022 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 402 S19L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER 19L CRACKED AT BS 402. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007103000090 20071030 00090 SO 2007 10 30 RAIA00710019 1 20071019 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BURNED OUT A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 837HK 145255 POST FLT NR 7901 - STL - COCKPIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT. OPS CHECKS GOOD . 2 L 7 2 4T RT T00011AT 2007103000091 20071030 00091 SO 2007 10 30 RAIA00710017 1 20071017 A 3350 WIRE EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 821HK 145068 PRE FLT NR 5564 - OKC - FLOOR EMERGENCY LIGHT FLOOR PROXIMITY LIGHTS INOP. MAINTENANCE REPAIRED WIRE AND OPS CHECK GOOD . 2 L 7 2 4F RT T00011AT 2007103000092 20071030 00092 SO 2007 10 30 RAIA00710022 1 20071020 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX LACK OF LUBE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 831HK 145232 PRE FLT NR 7908 - ORD - PAX DOOR WILL NOT OPEN ALL THE WAY. MAINTENANCE LUBED PAX DOOR AND OPS CHECKED SEVERAL TIMES. OPS CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2007103000093 20071030 00093 SO 2007 10 30 RAIA00710023 1 20071020 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS NO TEST A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 838HK 145321 PRE FLT NR 7988 - STL - EMERGENCY LIGHTS SERVICE DOOR EXIT MARKER AND GALLEY WALL EXIT LOCATOR INOP. MAINTENANCE REMOVE D AND REPLACED NR 1 & 2 EMERGENCY BATTERY POWER SUPPLY, CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2007103000094 20071030 00094 SO 2007 10 30 RAIA00710024 1 20071021 A 3350 1317 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 840HK 145341 POST FLT NR 8016 - ORD - LEFTHAND EMERGENCY DOOR FLOOD LIGHT INOP. MAINTENANCE REPLACED LAMP. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007103000095 20071030 00095 SO 2007 10 30 RAIA00710020 1 20071019 A 5210 STOP EMB 145 EMB145EP 3260221 SO PAX DOOR OUT OF POSITION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 826HK 145016 POST FLT NR 5461 - STL - PAX DOOR DIFFICULT TO OPEN. MAINTENANCE ADJUSTED PHENOLIC STOP ON UPPER FWD SIDE OF FUSELAGE E NTRY AREA. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007103000096 20071030 00096 EA 2007 10 30 COMA0760603 1 20071014 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 917CA 7017 FLIGHT 5298 - FLAPS FAIL AT 23 DEGREES UPON EXTENTION ON FINAL APPROACH. AIRCRAFT LANDED SAFELY. COMPLIED WITH AD 2006 -12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WI TH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007103000097 20071030 00097 NM 2007 10 30 SWAA075287 1 20071024 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 727C S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000146 20071030 00146 EA 2007 10 30 TRAX200701542 1 20071019 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 880AS 7606 FLOOR LEVEL EMERGENCY LIGHT STRIP ROW 6 THRU 8 INOP. FLT 4418 DEL 33 MINS. 2 L 7 2 4F RT A21EA 2007103000147 20071030 00147 EA 2007 10 30 TRAX200701543 1 20071019 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 880AS 7606 LOWER EMERGENCY EXIT SIGN ROW 8D INOP. 2 L 7 2 4F RT A21EA 2007103000148 20071030 00148 EA 2007 10 30 TRAX200701544 1 20071019 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 867AS 7463 FLAPS FAIL AT 8 ON APPROACH COMPLIED WITH QRH. EMERGENCY DECLARED. EMERGENCY EQUIPMENT ON STANDBY. FLT 4576 CX AND ON 10/20 FLT 4572 CX. 2 L 7 2 4F RT A21EA 2007103000149 20071030 00149 EA 2007 10 30 TRAX200701545 1 20071019 A 3350 LENS CNDAIR CL600 CL6002B19 1900309 EA MISSING MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 979EV 7737 EMERGENCY EXIT SIGN AT ROW 8 IN CABIN LENS IS MISSING. FLT 4843 DEL 19 MINS. 2 L 7 2 4F RT A21EA 2007103000150 20071030 00150 EU 2007 10 30 TRAX200701546 1 20071019 A 2750 FLAP SYSTEM AEROSP ATR72 ATR72 EU TE FLAPS MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 633AS 344 FLAP ASYM AFTER TAKEOFF. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. 2 H 7 2 4T RT 2007103000151 20071030 00151 NM 2007 10 30 KCSA071491 1 20071023 A 5347 ATTACH FITTING BOEING 747 7472B4B 138481B NM BS 965 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FORWARD BILGE, ATTACH FITTING FOR CARGO END STOP IS CRACKED 6 INCHES AT STA 965, RBL 46. 2 L 7 4 4F RT A20WE 2007103000152 20071030 00152 EA 2007 10 30 COMA0760604 1 20071015 A 2131 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA CABIN PRESSURE MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 971CA 7145 FLIGHT 5196 - AIRCRAFT CABIN AT 500FT/MIN THEN STOPPED CLIMBING AND CABIN ALT STOPPED AT 6000 FT. LEVEL AT FLT 10 PERFO RMED QRH PROCEDURE AB2-5 AND RETURNED TO LGA AND LANDED SAFELY. PERFORMED OPS CHECK OF BOTH CABIN PRESSURE CONTROLLERS. AIRCRAFT PRESSURIZED NORMAL. 2 L 7 2 4F RT A21EA 2007103000153 20071030 00153 EA 2007 10 30 COMA0760605 1 20071001 A 3231 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG DOOR MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 938CA 7046 FLIGHT 5161 - NOSE GEAR DOORS FAILED TO CLOSE AFTER GEAR RETRACTION. REPLACED NLG DOOR SELECTOR VALVE. NO FURTHER DEFE CTS. 2 L 7 2 4F RT A21EA 2007110100169 20071101 00169 EU 2007 11 1 COEA0701919 1 20070826 A 5753 S5701007200640 STRUT AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE LT TE FLAP CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 919FX 266 FOUND DURING HEAVY CHECK. FOUND LEVEL 2 CORROSION. LT WING FLAP HORIZONTAL HINGE FITTING SUPPORT STRUT AT WING RIB 9. HAS EXFOLIATION ON IB END OF FITTING FORK. REMOVED AND INSTALLED NEW FLAP HINGE SUPPORT STRUT. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007110100194 20071101 00194 CE 2007 11 1 AMWA88091BC 1 20071018 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE MASTER DISCHARGED A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 176YV 14025 244 UE176 BATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT. BATTERY REPLACED BY MAINTENANCE, DISCREPANCY CLEARED. THIS TYPE ANNUN CIATOR DISCREPANCY IS CONSIDERED A NUISANCE ITEM AND DISTRACTION TO CREW. 2 L 7 2 4T RT A24CE 2007110100196 20071101 00196 NM 2007 11 1 AMTA200700553 1 20071020 A 2697 WIRE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE DAMAGED A AMTA O OTHER N FALSE WARNING CR CRUISE 1 GL 11 560TZ 33525 RT STRUT O/H DET 2 DISPLAYED ON EICAS. TROUBLESHOT SYSTEM IAW FIM 26-12-00 FOUND CONDUCTOR AT SWITCH S10204 CONTACTING SHIELDING, REPAIRED WIRE SYSTEM OPS CHECKED NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007110200073 20071102 00073 EA 2007 11 2 SWIA200718803 1 20071021 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DAMAGED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 426SW 7468 FLT 3987 - FOUND EXIT LIGHT ON LEFT SIDE OF SERVICE DOOR IS INOP. REPAIRED WIRE ON THE EXIT LIGHT IAW WM 20-00-00. OPS CHECK IS OK. 2 L 7 2 4F RT A21EA 2007110200074 20071102 00074 SW 2007 11 2 WGEA200700018 1 20071031 A 3243 1094 MASTER CYLINDER ECLIPS EA500 ECLIPSEEA500 3350000 SW ZONE 700 LEAKING E WGEA K NONE O OTHER LD LANDING 1 EA 27 145DJ 12 000057 LEFT BRAKE INOP. REMOVED AND REPLACED PILOTS LEFT MASTER CYLINDER (LEAKING) WITH A NEW MASTER CYLINDER IAW EA500 AMM 32 -41-11. BLED AND SERVICED BRAKE SYSTEM IAW EA500 AMM 32-40-00. TAXI CHECK GOOD. 1 L 7 2 4J RT A00002AC 2007110200075 20071102 00075 EU 2007 11 2 07FDEA04678 1 20071025 A 5311 A57112125 FRAME AIRBUS 310 A310222 3930315 EU BS 2612 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 RT FRAME 47 HOLE 11 SHOWS CRACK INDICATION FIG 7 SHEET 3 SAYS CONTACT AIRBUS IF CRACK IS DETECTED COMPLIED WITH FEDEX EA 6-5710-112976, WINGS -AD2006-09-05 WING R/S INTERNAL ANGLE FASTENER HOLE 11 AND 39 RT AND 10 AND 61 LT CRACK REPAIR. R EAMED HOLES TO REMOVE CRACK INDICATIONS. 2 L 7 2 4F RT A35EU 2007110200076 20071102 00076 EU 2007 11 2 07FDEA04679 1 20071025 A 5311 A57112125 FRAME AIRBUS 310 A310222 3930315 EU FUELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 RT FRAME 47 HOLE 39 SHOWS CRACK INDICATION. THE HOLE HAS BEEN REAMED TO MAX DIAMETER PER FED EX CARD E6-5710-7-3322 PT1 . COMPLIED WITH FEDEX EA 6-5710-112976 WINGS- AD2006-09-05 WING R/S INTERNAL ANGLE FASTENER HOLES 11 AND 39 RT AND 10 A ND 61 LT CRACK REPAIR. REAMED HOLE TO REMOVE CRACK INDICATION. 2 L 7 2 4F RT A35EU 2007110200077 20071102 00077 EU 2007 11 2 COEA0728821 1 20070822 A 5755 S5721210920103 HINGE FITTING AEROSP ATR72 ATR72202 8680940 EU RT WING SPOILER CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK, LEVEL 2 CORROSION, CORROSION ON RT WING SPOILER OUTBOARD HINGE FITTING. REMOVED AND REPLACED FITTING. (M) 2 H 7 2 4T RT A53EU 2007110200078 20071102 00078 2007 11 2 AMTA200700554 4 20071017 A 2565 SLIDE DOUG DC10 DC1030 3023501 WP PAX DOOR NO TEST A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 705TZ 46915 DURING PREFLIGHT, DOOR SLIDE TEST LIGHT WOULD NOT PRESS TO TEST. RELAMPED SLIDEPACK PRESSURE INDICATOR. OPS CHECK NORM AL IAW 25-61-01. (M) 2 L 7 3 4F A22WE 2007110200081 20071102 00081 NM 2007 11 2 AMTA200700542 1 20071019 A 5321 FLOOR PANEL BOEING 757 75733N 1384931 NM FS 550-654 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 550TZ 32584 FORWARD CARGO COMPARTMENT FLOOR PANEL 121 AFT LOWER SURFACE HAS CORROSION AROUND EDGES. FABRICATED NEW PANEL PER SRM 53 -60-53. TREATED SRM 51-20-01. (M) 2 L 7 2 4F RT A2NM 2007110200082 20071102 00082 NM 2007 11 2 AMTA200700544 1 20071020 A 5321 FLOOR PANEL BOEING 757 75733N 1384931 NM BS 1470-1510 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 550TZ 32584 AFT CARGO COMPARTMENT FLOOR PANEL NR 161 AF AND STRAP HAS CORROSION NUMEROUS PLACES UPPER AND LOWER SURFACES STATION 147 0 TO 1510 LBL 20 TO RBL 20. FAB NEW PANEL IAW 53-60-53 FIG 1. (M) 2 L 7 2 4F RT A2NM 2007110200085 20071102 00085 NM 2007 11 2 QXEA200701622 1 20071024 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM MAIN PAX STIFF A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 424QX 4006 LAX FLIGHT NR 2469: LEFT REAR PAX DOOR DIFFICULT TO OPEN AND CLOSE. MAINTENANCE PERFORMED VISUAL INSPECTION OF THE AFT PAX DOOR AND SURROUND INSIDE AND OUTSIDE. NO DEFECTS WERE NOTED. PERFORMED OPS CHECK OF AFT ENTRY DOOR IAW Q400 AMM TA SK 52-12-00-710-801. OPS CHECK GOOD WITH NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007110200089 20071102 00089 NM 2007 11 2 AMTA200700529 1 20071019 A 5321 FLOOR PANEL BOEING 757 75733N 1384931 NM BS 1470-1510 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 550TZ 32584 AFT CARGO COMPT FLOOR PANEL NR 161AF AND STRAP HAS CORROSION ON NUMEROUS PLACES UPPER AND LOWER SURFACE, OFF A/C PART, S TATION 1470 TO 1510 LBL 20 TO RBL 20. FABRICATED AFT CARGO COMPARTMENT FLOOR PANEL 161AF PER SRM 53-60-53 FIG 1 MATERIA L 2024 T-3 .071 ALODINE AND PRIME PER SRM 51-20-01. (M) 2 L 7 2 4F RT A2NM 2007110200090 20071102 00090 NM 2007 11 2 AMTA200700531 1 20071019 A 5330 PANEL BOEING 757 75733N 1384931 NM BS 1200-1330 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 550TZ 32584 AFT CARGO COMPARTMENT PANEL NR 153AF HAS CORROSION ON UPPER AND LOWER SURFACE NUMEROUS AREAS AT STATION 1200 TO 1330 LBL 20 TO RBL 20. FABRICATED NEW FLOOR PANEL 153AF PER SRM 53-60-53 FIG 1 MATERIAL 2024 T3 .071. TREATED SRM 51-20-01. ( M) 2 L 7 2 4F RT A2NM 2007110200091 20071102 00091 EU 2007 11 2 MALA070167 1 20071023 A 5330 PANEL SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 COMPOSITE DAMAGE TO BELLY PANEL 193 AL. GENERIC COLD BOND (WET LAY-UP) REPAIR IAW SRM 51-70-50, EO NR S51031. 2 L 7 2 4T RT A52EU 2007110200092 20071102 00092 NM 2007 11 2 AMTA200700218 1 20070524 A 5347 CARGO TRACK BOEING 737 73783N 13844HI NM BS 787 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 304TZ 30675 AFT PIT B/S 787 RBL 17 CORROSION EXISTS ADJACENT TO CARGO NET TIE DOWN FITTING ON LONGERON. REMOVED CORROSION SRM 51-10 -02. ORIG .080 MECHANICAL MEASURE CALIPER NR 07-01 CAL DUE 07-03-07. LOSS .001-.003, DEPTH GAUGE NR 07-802 CAL DUE 08- 12-07 IS WITHIN LIMITS SRM 53-00-53. TREAT AND PRIME SRM 51-20-01. (M) 2 L 7 2 4F RT A16WE 2007110200094 20071102 00094 2007 11 2 SIMA200729704 4 20071019 A 2210 MODULE SAAB SF340 340B 7860101 EU YAW DAMPER MALFUNCTIONED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 324AE 340B324 YAW DAMPER AND AUTOPILOT WILL NOT ENGAGE. DISCONNECT AURAL ALERT KEEPS COMING ON. GA MODE COMES ON UNCOMMANDED. REMOV ED AND REPLACED YAW TRIM MODULE OPERATIONAL CHECK OF THE AUTOPILOT SYSTEM OK AT THIS TIME IAW SAAB AMM 22-10-00. NO DEF ECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007110200096 20071102 00096 2007 11 2 SIMA200729903 4 20071024 A 3140 701700083430 COMPUTER EMB 135 EMB135KL 3260302 SO ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 21 813AE 145539 IC BUS FAIL, ILLUMINATED ON EICAS IC2 C/B POPPED. FLIGHT ATTENDANT SMELLED SMOKE FOR A BRIEF PERIOD OF TIME BUT IT DISS IPATED QUICKLY. REMOVED AND REPLACED IC-600 COMP IAW EMB140 AMM 31-42-01. PERFORMED OPS CHECK IAW EMB140 AMM 31-42-00. OPS CHECK GOOD. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007110200097 20071102 00097 SO 2007 11 2 SIMA200729901 1 20071022 A 3350 LIGHT EMB 135 EMB135KL 3260302 SO CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 833AE 145629 LEFT EXTERNAL OVERWING EMERGENCY LIGHT INOP. ISSUED MEL 33-29 AUTH 100824D-C. 2 L 7 2 4F RT T00011AT 2007110200102 20071102 00102 SO 2007 11 2 SIMA200729912 1 20071023 A 5310 14523122421 DOOR FRAME EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 145081 DURING MBV INSP, AFT LOWER SERVICE DOOR FRAME CORRODED. REPAIRED FRAME IAW EO EM-53MR-842. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007110200103 20071102 00103 SO 2007 11 2 SIMA200729913 1 20071022 A 5310 14523775601 DOOR FRAME EMB 145 EMB145 3260210 SO GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 20383 5000 145079 DURING A MBV INSPECTION, THE CARGO DOOR FORWARD FRAME WAS FOUND TO BE GOUGED. REMOVED GOUGED FRAME AND REPLACE WITH NEW FRAME PN 145-23775-601 IAW SRM CHAPTERS 51-10-03, 51-40-02, AND 51-40-04. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007110200105 20071102 00105 NM 2007 11 2 AMTA200700221 1 20070504 A 5313 LONGERON BOEING 737 73783N 13844HI NM BS 775-792 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 304TZ 30675 AFT PIT BS 775-792 RBL 22 CORROSION MARKED 6 SPOTS ON LONGERON. REMOVED CORROSION SRM 51-10-02. ORIG .050 SRM 53-30-53 LOSS .004-.003 IS WITHIN LIMITS SRM 53-00-53. DEPTH GAUGE NR 07-802 CALDUE 08-12-07. TREAT AND PRIME SRM 51-20-01. ( M) 2 L 7 2 4F RT A16WE 2007110200106 20071102 00106 EA 2007 11 2 SWIA200718795 1 20071018 A 7830 SWITCH CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER OUT OF ADJUST A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 932SW 7714 FLT 5936 - RIGHT REVERSER UNLOCKED MESSAGE. RE-RIGGED STOW SWITCH ON RIGHT THRUST REVERSER IAW 78-37-01. 2 L 7 2 4F RT A21EA 2007110200110 20071102 00110 EA 2007 11 2 SWIA200718799 1 20071018 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN SMOKE A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 452SW 7716 FLT 3938 - RETURNED TO FIELD FOR SMOKE IN THE CABIN AND A "SMOKE TOILET" MESSAGE. OPERATED BOTH PACKS FOR 15 MINUTES AN D CLEARED RESIDUAL SMOKE ODOR OUT OF PACK SYSTEMS. 2 L 7 2 4F RT A21EA 2007110200113 20071102 00113 EA 2007 11 2 SWIA200718802 1 20071023 A 5610 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA O OTHER O OTHER AP APPROACH 1 NM 07 340CA 10062 FLT 4011 - CAPTAINS SIDE WINDOW CRACKED. REPLACED CAPTAINS SIDE WINDOW IAW 56-12-01P/N: NP-139322-11, S/N OFF: 02098H3 465. 2 L 7 2 4F RT A21EA 2007110200119 20071102 00119 NE 2007 11 2 QXEA200701615 2 20071022 A 7200 3038400 ENGINE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 2 SMOKE A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 365PH 21356 78 526 AG0062 YKM FLIGHT NR 2003 - AFTER ENGINE START AND NR 2 BLEED TURNED ON, SMOKE FILLED COCKPIT AND STARTED TO APPEAR AS A HAZE I N CABIN. MAINTENANCE REPLACED THE ENGINE. OPERATIONALS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007102900001 20071029 00001 NM 2007 10 29 2007UALA04284 1 20071016 A 2920 PLUNGER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RAT MISSING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 670UA 29240 RAT WILL NOT DEPLOY WITH PITOT PRESSURE APPLIED, RAT WOULD NOT HAVE DEPLOYED IN AUTO. TROUBLESHOT AND FOUND RT AUX PIT OT PROBE MISSING CENTER PLUNGER IN QUICK DISCONNECT FITTING. REPLACED PLUNGER PER DWG 233T9122, ACCOMPLISHED PROBE HEATE R CIRCUIT CHECKS. CHECKS GOOD PER MM 30-31-00, PITOT LOW RANGE LEAK CHECK GOOD PER MM 34-11-01 AND RAT PITOT PRESSURE DE PLOY OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007102900006 20071029 00006 NM 2007 10 29 2007UALA04293 1 20071017 A 2721 TRIM SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RUDDER INOPERATIVE A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 529UA 25019 RUDDER TRIM INOP IN BOTH DIRECTIONS IN ACCENT, CRUISE AND DESCENT. RUDDER TRIM INTERMITTENT ON TESTING. REPLACED RUDDE R TRIM ACTUATOR 2 L 7 2 4F 4 F RT A2NM E17NE 2007102900018 20071029 00018 2007 10 29 ABXA070348 4 20071017 A 2565 GIRT BAR BOEING 767 767281 1385109 NM PAX DOOR SLIDE MALFUNCTIONED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 783AX 23016 MAIN ENTRY DOOR SLIDE WOULD NOT ARM. FOUND GIRT BAR LOCK PANEL NOT TURNING. INSTALLED BUSTLE. OPERATED EMERGENCY ESCA PE SLIDE IAW B767 AMM 25-66-01-4-10. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2007102900030 20071029 00030 NM 2007 10 29 KCSA071486 1 20071021 A 5330 SKIN BOEING 747 7472B4B 138481B NM BS 690 S14-42R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FUSELAGE SKIN DAMAGED AT BS 690 BETWEEN STR 41R AND STR 42R. 2 L 7 4 4F RT A20WE 2007102900033 20071029 00033 EU 2007 10 29 WRNA200700051 1 20071018 A 2497 NAS931304500 CIRCUIT BREAKER AIRBUS 300 A300B4203 3930306 EU WEAK A WRNA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 05 510TA 100 AFTER TAKEOFF, FUEL PUMP NR 1; 1A; 2 CIRCUIT BREAKERS POPPED, AND AFCS AND FLIGHT ENGINEER PANEL LIGHTS WENT OFF. RETUR NED TO FIELD AND MADE A SAFE LANDIBG. REPLACED FAULTY BREAKER IN 101VU PANEL. 2 L 7 2 4F RT A35EU 2007102900035 20071029 00035 WP 2007 10 29 ABXA070349 1 20071016 A 3350 41B004AD07G3 BATTERY PACK DOUG DC9 DC931 3022065 WP EMERGENCY LIGHTS DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 EMERGENCY EVACUATION LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00-8. 2 L 7 2 4F A6WE 2007102900037 20071029 00037 NM 2007 10 29 UPS07M50947 1 20070920 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 816-1079 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C MAIN DECK: FROM BS 816 TO BS 1079, ALONG X=9 (LBL 9), SEAT TRACK CROWN & FLANGE AREAS FOUND CORRODED. CORROSION REMOVAL C/OUT FOUND LIMIT EXCEEDED PER SRM 53-70-00D, F3, V1, R35. REMOVAL TO GAIN ACCESS TO REPAIR AFFECTE D SEAT/T C/OUT FROM STA 816 TO 1079. CORRODED SEAT/T TRIMMED OFF PER SRM 53-70-00D, F1, V1, R35. SEAT / T & SPLICE RWK SRM 53-70-00D, F1, V1, R35. HOLES PICK UP C/OUT & INSTALLATION OF NEW SEAT/T C/OUT PER SRM 51-33-01 & 51-3101,V2, R35. FOUND SATIS. 2 L 7 3 4F RT A22WE 2007102900040 20071029 00040 NM 2007 10 29 UPS07M50951 1 20070923 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C MAIN DECK: FROM BS 6-80 TO BS 1129, ALONG X=9 (LBL 9), SEAT TRACK CROWN AREAS AND CROWN BASE AREAS FO UND CORRODED. CORROSION REMOVAL C/OUT ON A/M AREAS FOUND EXCEEDED LIMIT PER SRM 53-70-00D, F3, V1, R35. CORRODED SEAT/ T FROM 6-05 TO STA 1129, LBL 9 REMOVED PER SRM 51-31-01, V2, R35. NEW SEAT/T FROM 6-05 TO STA 1129, LBL 9 RWK PER SRM 5 3-70-00D, F1, V1, R35. HOLES PICKED UP FOR NEW SEAT/T PER SRM 51-21-01,V2 R35. NEW SEAT/T FROM 6-05 TO 1129, LBL 9 INS TL PER SRM 51-33-01 & 31-01, V2, R35. 2 L 7 3 4F RT A22WE 2007102900041 20071029 00041 NM 2007 10 29 UPS07M50952 1 20070920 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C MAIN DECK: FROM BS 855 TO BS 959, ALONG -X=28 (RBL 28), SEAT TRACK CROWN & FLANGE AREAS FOUND CORRODE D. CORROSION REMOVAL C/OUT ON A/M AREAS FOUND EXCEEDED SRM 53-70-00 LIMIT TO GAIN ACCESS TO REMOVE & REWORK AFFECTED SE AT/T & SPLICE C/OUT PER SRM 53-70-00D, F1, V1, R35. NEW SEAT /T & SPLICE RWK PER SRM 53-70-00D, F1, V1, R35. NEW SEAT/ T PICK UP HOLES PER SRM 51-31-01 & 51-21-01 V2, R35. NEW SEAT/T FROM STA 849 TO 969 RBL 28 REPAIRED & INSTALLED SRM 51- 33-01, FOUND SATIS. 2 L 7 3 4F RT A22WE 2007102900042 20071029 00042 NM 2007 10 29 UPS07M50953 1 20070927 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C MAIN DECK: FROM BS 5-113 TO BS 1661, ALONG-X=28, SEAT TRACK CROWN AREAS & CROWN AREAS FOUND CORRODED. CORROSION REMOVAL C/OUT ON A/M AFFECTED AREAS FOUND EXCEEDED LIMIT SRM 53-70-00D, F1, V1, R35. CORRODED SEAT/T TRIMME D OFF PER SRM 53-70-00D, F1, V1, R35. NEW SEAT/T FROM STA 5-113 TO 1671 RBL 28 RWK PER SRM 53-70-00D F1, V1, R35. NEW SEAT/T FROM STA 5-113 TO 1671 RBL 28 REPAIRED & INSTALLED PER SRM 51-31-01 & 51-33-01, V2, R35. FOUND SATIS. 2 L 7 3 4F RT A22WE 2007102900043 20071029 00043 NM 2007 10 29 UPS07M50954 1 20070924 A 5340 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C MAIN DECK: FROM BS 1341 TO BS 1361, ALONG -X=107 (RBL 107), SEAT TRACK CROWN AREAS, FLANGE & CROWN BA SE AREAS FOUND CORRODED. CORROSION REMOVAL C/OUT ON A/M AREAS FOUND EXCEEDED SRM LIMITS PER SRM 53-70-00D, F3, V1, R35. CORRODED SEAT/T AT STA 1331 & 1411, RBL 107 TRIMMED OFF PER SRM 53-70-00D, F1, V1, R35. NEW SEAT/T & SPLICE RWK PER S RM 53-70-00 D, F1, V1, R35. NEW SEAT/T FROM STA 1321 TO 1421, RBL 107 REPAIRED & INSTALLED PER SRM 51-31-01 & 51-33-01 V2, R35. FOUND SATIS. 2 L 7 3 4F RT A22WE 2007102900045 20071029 00045 WP 2007 10 29 MWEA070259 1 20071017 A 2611 PU90471WR3 SMOKE DETECTOR DOUG DC9 DC982 3022082 WP AFT LAVATORY FAULTY A MWEA O OTHER N FALSE WARNING CL CLIMB 1 GL 13 810ME 48072 LEFT REAR LAV SMOKE ALARM SOUNDED. REMOVED AND REPLACED AFT LEFT LAVATORY SMOKE DETECTOR. 2 L 7 2 4F A6WE 2007102900046 20071029 00046 NM 2007 10 29 CALA0700596 1 20071019 A 5330 654577678 SERVICE PANEL BOEING 737 7373T0 1384582 NM BS 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14325 23455 INSPECTION FOUND CORROSION AND 3 POPPED RIVETS AT FORWARD EDGE OF LAV SERVICE PANEL, STA 986.5, RBL 25. A REPAIR WAS IN STALLED IAW ECRA 5331-01355. 2 L 7 2 4F RT A16WE 2007102900047 20071029 00047 NM 2007 10 29 CALA0700597 1 20071021 A 5315 BAC1518338 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED ON UPPER AND LOWER SURFACES AT STA 360, BL 0. REPAIRED IAW SRM 53-30-51. 2 L 7 2 4F RT A16WE 2007102900051 20071029 00051 NM 2007 10 29 ZZDA2007288 1 20071015 A 5330 SKIN BOEING 717 717200 1383700 NM BS 229.9 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 990AT 55134 TWO DENTS AT FUSELAGE STA 229.9 ABOVE LONGERON 18 LEFT. INSTALLED FLUSH SKIN REPAIR PER SRM 53-00-01 FIG 201. 2 L 7 2 4F TR A6WE 2007102900052 20071029 00052 NM 2007 10 29 ZZDA2007289 1 20070115 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 896AT 55048 RIGHT DOUBLER REPAIR CRACKED. INSTALLED DOUBLER REPAIR AT AFT FUSELAGE RIGHT SIDE VENT BOX IAW AIRTRAN T/C 17-5320-2023 FIG 1. 2 L 7 2 4F TR A6WE 2007102900054 20071029 00054 NM 2007 10 29 ZZDA2007287 1 20071012 A 5330 SKIN BOEING 717 717200 1383700 NM BS 365-415 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 943AT 55006 ACFT DAMAGE FWD ABOVE CARGO DOOR FOUR FOOT SCRATCH, DENT DUE TO BAGGAGE CART. CUT OUT DAMAGED AREA IAW EA 17-53-010764B . PERFORMED HFEC AT ALL OPEN HOLES AND CUT OUT OF DAMAGE AREA IAW NT SRM 06-10-01. NO CRACKS NOTED. FAB REPAIR DOUBLE RS, INSTALLED DOUBLERS AND 1 FELLE IAW EA 17-53-00764B. 2 L 7 2 4F TR A6WE 2007102900061 20071029 00061 EU 2007 10 29 USAA920070965 1 20071019 A 5320 D5311283020200 DUMMY RAIL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C-07 CHECK - CORROSION ON CABIN DUMMY RAIL, BS 605 / FR 12 - BS 709 / FR 16, -Y81. REPLACED CABIN DUMMY RAIL, BS 605 / FR 12 - BS 709 / FR 16, -Y81 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007102900065 20071029 00065 EU 2007 10 29 USAA920070969 1 20071014 A 5320 D53480020342 COVER AIRBUS 320 A320232 3930326 EU ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C-07 CHECK - CRACKED CABIN COVER SHEET, BS 3257 / FR 68 - BS 3310 / FR 69, +Y1732. REPLACED CABIN COVER SHEET, BS 3257 / FR 68 - BS 3310 / FR 69, +Y1732 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007102900066 20071029 00066 EU 2007 10 29 USAA920070970 1 20071019 A 5321 D5367180500300 FLOOR PANEL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C-07 CHECK - CORROSION ON CABIN FLOORBOARD 262 FF, BS 3158 / FR 66 - BS 3257 / FR 68. REPLACED CA BIN FLOORBOARD 262 FF, BS 3158 / FR 66 - BS 3257 / FR 68 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007102900067 20071029 00067 NM 2007 10 29 USAA920070971 1 20071008 A 5311 652072328 FRAME BOEING 737 7373B7 1384580 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 529AU 24411 CLT - MAJOR REPAIR - FPBH INSPECTION, FORWARD CARGO COMPARTMENT DOOR CUTOUT AFT FRAME CRACKED, BS 492, S24R. REPAIRED F ORWARD CARGO COMPARTMENT DOOR CUTOUT AFT FRAME, BS 492, S24R IAW USAIRWAYS EA 98913. 2 L 7 2 4F RT A16WE 2007102900068 20071029 00068 NM 2007 10 29 SWAA075173 1 20071021 A 5610 141A48103 WINDOW BOEING 737 73776Q 13845AA NM FLIGHT DECK ARCED A SWAA O OTHER O OTHER NR NOT REPORTED 1 SW 29 551WN 30280 FLIGHT DECK L2 WINDOW ARCING. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2007102900074 20071029 00074 NM 2007 10 29 SWAA075159 1 20071021 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 485WN 32473 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007102900076 20071029 00076 2007 10 29 SWAA075157 4 20071020 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 439WN 29834 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007102900078 20071029 00078 NM 2007 10 29 SWAA075203 1 20071021 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 444 S28R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 444, STR 28R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007102900079 20071029 00079 NM 2007 10 29 SWAA075181 1 20071021 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 922 S25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 922, STR 25R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007102900080 20071029 00080 NM 2007 10 29 SWAA075202 1 20071021 A 5315 6545812 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 328, LBL 28. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 2007102900083 20071029 00083 NM 2007 10 29 SWAA075194 1 20071021 A 5755 65465168A SKIN BOEING 737 7373H4 1384600 NM NR 3 SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED A2 CHECK, FOUND LT WING NR 3 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007102900086 20071029 00086 NM 2007 10 29 SWAA075191 1 20071021 A 5755 65465168A SKIN BOEING 737 7373H4 1384600 NM LT WING SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED A2 CHECK, FOUND LEFT WING 0 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007102900087 20071029 00087 NM 2007 10 29 SWAA075189 1 20071021 A 5755 65465168A SKIN BOEING 737 7373H4 1384600 NM NR 8 SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED A2 CHECK, FOUND RIGHT WING NR 8 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM . 2 L 7 2 4F RT A16WE 2007102900091 20071029 00091 NM 2007 10 29 SWAA075163 1 20071021 A 5311 6546525 FRAME BOEING 737 7375H4 138449D NM BS 380 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007102900093 20071029 00093 NM 2007 10 29 SWAA075153 1 20071020 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 480 S25L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 480, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007102900095 20071029 00095 NM 2007 10 29 SWAA075162 1 20071021 A 5311 6546552 FRAME BOEING 737 7375H4 138449D NM BS 827 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007102900097 20071029 00097 2007 10 29 SWAA075158 4 20071020 A 2565 6557463 BRACKET BOEING 737 7377H4 1384404 NM L1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 439WN 29834 DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR BRACKET LOOSE. ADJUSTED BRACKET PER MM. 2 L 7 2 4F RT A16WE 2007102900098 20071029 00098 NM 2007 10 29 SWAA075199 1 20071019 A 5754 65C26602258A SKIN BOEING 737 7373A4 1384585 NM NR 5 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 RIGHT WING NR 5 L/E SLAT INBOARD END DELAMINATED. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 2007102900099 20071029 00099 NM 2007 10 29 SWAA075151 1 20071020 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 227WN 34450 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007102900101 20071029 00101 NM 2007 10 29 SWAA075166 1 20071021 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 685 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007102900104 20071029 00104 NM 2007 10 29 SWAA075169 1 20071021 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 727A S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007102900111 20071029 00111 NM 2007 10 29 SWAA075164 1 20071021 A 5311 65C33511 FRAME BOEING 737 7375H4 138449D NM BS 440 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007102900114 20071029 00114 NM 2007 10 29 SWAA075156 1 20071019 A 2131 7638106 CONTROLLER BOEING 737 7373H4 1384600 NM CABIN PRESSURE OVERHEATED A SWAA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 29 334SW 23938 AIR TURNBACK / DECLARED EMERGENCY. PASSING 10,000 MSL CREW REPORTED STRONG BURNING SMELL IN CABIN. SMELL INTENSIFIED A ND REMAINED UNTIL AFTER LANDING AND SHUT DOWN. FOUND CABIN PRESSURE CONTROLLER OVERHEATING. REMOVED AND REPLACED PRESS URE CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 2007102900115 20071029 00115 NM 2007 10 29 SWAA075185 1 20071021 A 2450 941D3354 CIRCUIT BREAKER BOEING 737 7373H4 1384600 NM FLIGHT DECK FAULTY A SWAA O OTHER O OTHER NR NOT REPORTED 1 SW 29 326SW 23690 NR 1 GENERATOR TRIPPED OFF-LINE RESET, THEN TRIPPED AGAIN. BOTH PILOTS SMELLED ELECTRICAL BURNING ODOR IN COCKPIT. REM OVED AND REPLACED BUSS TIE BREAKER PER MM. 2 L 7 2 4F RT A16WE 2007102900116 20071029 00116 NM 2007 10 29 SWAA075154 1 20071020 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 450 S26L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER 26L CORRODED AT BS 450. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007102900117 20071029 00117 2007 10 29 SWAA075183 4 20071021 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007102900118 20071029 00118 2007 10 29 SWAA075182 4 20071021 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007102900119 20071029 00119 NM 2007 10 29 SWAA075176 1 20071021 A 3350 MS155721 LAMP BOEING 737 7373Y0 1384671 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007102900120 20071029 00120 NM 2007 10 29 SWAA075200 1 20071021 A 2560 P4010021 BATTERY BOEING 737 7373Q8 1384670 NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED MV1 CHECK, FOUND AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2007102900121 20071029 00121 NM 2007 10 29 SWAA075150 1 20071020 A 3397 W412015225 WIRE BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 207WN 34012 EEPLS INOP AT ROW 17 ABC. SECURED LOOSE WIRE PER MM. 2 L 7 2 4F RT A16WE 2007102900124 20071029 00124 NM 2007 10 29 ASAA0752128 1 20071018 A 2822 343A280123 PUMP BOEING 737 737890 1384527 NM CENTER TANK UNKNOWN A ASAA O OTHER O OTHER CR CRUISE 1 NM 02 579AS 35187 FUEL PUMP LEFT CENTER TANK -LOW PRESS- LIGHT DOES NOT EXTINGUISH WITH PUMP ON & CENTER FUEL JUST OVER 1000 LBS. UNABLE TO VERIFY DISCREPANCY. PASSES ALL TESTS PER FIM. 2 L 7 2 4F RT A16WE 2007102900128 20071029 00128 NM 2007 10 29 ASAA0792115 1 20071008 A 5320 INTERCOSTAL BOEING 737 737990 NM BS 727-767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 305AS 30013 AFT CARGO PIT LT INTERCOSTAL TRACK (ZEE ANGLE) FOUND CORRODED FROM BS 727 TO 767 + 10 AFT CARGO PIT. LT INTERCOSTAL TRA CK (ZEE ANGLE) REPLACED FROM BS 727 TO 767+10 IAW B737 900 SRM 51-40-02 AND 53-00-53 FIG 202. 2 L 7 4 4F RT A16WE 2007102900129 20071029 00129 NM 2007 10 29 ASAA0792120 1 20071007 A 5320 143A7510 INTERCOSTAL BOEING 737 737990 NM BS 500J-500K CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 305AS 30013 FWD PIT RT INTERCOSTAL BS 500J TO BS500K FOUND CRACKED. INTERCOSTAL RT AT FWD PIT REPLACED WITH MADE REPAIR PART IAW B7 37 900 SRM 51-40-20 AND 53-30-53. 2 L 7 4 4F RT A16WE 2007102900130 20071029 00130 NM 2007 10 29 ASAA0792122 1 20071007 A 5320 143A7510 INTERCOSTAL BOEING 737 737990 NM BS 460-480 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 305AS 30013 FWD PIT RT INTERCOSTAL BS 460 TO BS 480 FOUND CRACKED. CRACK ON INTERCOSTAL AT FWD PIT BS 460, 480 REPAIRED IAW B737 90 0 SRM 51-70-11 FIG 201. 2 L 7 4 4F RT A16WE 2007102900134 20071029 00134 NM 2007 10 29 ASAA0792118 1 20071007 A 5320 143A7510 INTERCOSTAL BOEING 737 737990 NM BS 500G CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 305AS 30013 FWD CARGO PIT RT BAFFEL AT BS 500G RBL 21 BELOW RT ZEE CHANNEL IS CRACKED. BAFFEL AT RT FWD CARGO PIT AT BS 500G RBL 21 REPLACED WITH MADE REPAIR PART IAW B737 400 SRM 53-30-53 FIG 2 AND 51-40-02. 2 L 7 4 4F RT A16WE 2007102900141 20071029 00141 WP 2007 10 29 ASAA0782131 1 20071022 A 5753 5930496507 VANE DOUG DC9 DC983 3022083 WP TE FLAP GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 LEFT WING O/B FLAP I/B VANE GOUGED ON L/E AREA MARKED. REMOVED PREVIOUS REPAIR DOUBLER, PREPARED AREA, FABRICATED REPAI R DOUBLER BONDED AND INSTALLED FASTENERS IAW MD 80 SRM 51-70-2 PG 11 23 PAR 10C PG 32 AND PAR 18B PG 91. 2 L 7 2 4F RT A6WE 2007102900142 20071029 00142 WP 2007 10 29 ASAA0782127 1 20071021 A 5753 5930495507 VANE DOUG DC9 DC983 3022083 WP FLAP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 LEFT INBOARD FLAP OUTBOARD FLAP VANE DELAMINATED ON UPPER SURFACE 53 INCHES FROM OUTBOARD END. PREPARED DAMAGED AREA, F ABRICATED FILLER AND DOUBLER REPAIR PARTS, LOADED AND INSTALLED FASTENERS IAW MD 80 SRM 51-70-2 PAT 18B PGS 91 95. 2 L 7 2 4F RT A6WE 2007102900143 20071029 00143 EA 2007 10 29 COMA0760596 1 20071008 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 957CA 7109 FLIGHT 4961- RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C) FLAP SYSTEM WAS RESET WITH NO FURTHE R MESSAGES. 2 L 7 2 4F RT A21EA 2007102900144 20071029 00144 EA 2007 10 29 COMA0760597 1 20071009 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 957CA 13750 7109 FLIGHT 4961 - RECEIVED FLAP FAIL INDICATION. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED RIGHT BPSU. NO FUR THER DEFECTS. 2 L 7 2 4F RT A21EA 2007102900145 20071029 00145 NM 2007 10 29 HNAA0700244 1 20071022 A 8000 AJA4N176 CONTACTOR DHAV DHC8 DHC8102 2809003 NM STARTER SMOKE A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 EA 07 931HA 49286 49286 132 THE CREW REPORTED NUMBER 2 ENGINE ROTATES AND SMOKE COMING FROM THE STARTER GENERATOR WHEN GROUND POWER IS APPLIED TO TH E AIRCRAFT. THE NUMBER 2 STARTER GENERATOR AND START CONTACTOR WERE REMOVED AND REPLACED. 2 H 7 2 4T RT A13NM 2007102900146 20071029 00146 EA 2007 10 29 COMA0760598 1 20071009 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 957CA 7109 FLIGHT 4961 - FLAPS FAIL MESSAGE AT 30 DEGREES ON DESCENT. AIRCRAFT LANDED SAFELY. COMPLIED WITH AD 2006-12-21 FLAP CA UTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007102900149 20071029 00149 EA 2007 10 29 COMA0760601 1 20071012 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 01 805CA 7354 FLIGHT 5085 - FLAPS FAILED AT 20 DEGREES. AIRCRAFT LANDED SAFELY. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FI RST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MES SAGES. 2 L 7 2 4F RT A21EA 2007102900150 20071029 00150 NM 2007 10 29 2007UALA04250 1 20071015 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 831UA 1291 LOW CREW OXYGEN PSI. SERVICED CREW O2 SYSTEM FROM 100 PSI TO CORRECT OP PSI. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007102900151 20071029 00151 NM 2007 10 29 2007UALA04251 1 20071015 A 5330 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 845UA 1585 EXTERNAL FUSELAGE SKIN DENTED STR 41 RT, 14 INCHES FWD OF FRAME 29. ACCOMPLISHED MAJOR REPAIR AT HMV. 2 L 7 2 4F 4 F RT A28NM E40NE 2007102900152 20071029 00152 NM 2007 10 29 2007UALA04252 1 20071015 A 5311 FRAME AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE STR 43L CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 845UA 1585 CORROSION AT AFT PIT STR 43L FRAME 52 AND 47-51. REPLACED ANGLE AT STR 43L, FR52 2 L 7 2 4F 4 F RT A28NM E40NE 2007102900153 20071029 00153 2007 10 29 2007UALA04253 4 20071015 A 2565 D31516113 SLIDE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE L1 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 853UA 1688 DOOR 1L SLIDE ASSY AFT ATTACH FITTING BROKEN. REPLACED DOOR 1L SLIDE ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007102900155 20071029 00155 EU 2007 10 29 2007UALA04255 1 20071015 A 5347 SEAT TRACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 484UA 1609 LEFT INBOARD, RIGHT INBOARD AND RIGHT OUTBOARD SEAT TRACKS BETWEEN FR 42 AND FR 47 HAVE WEAR AT LUGS WHERE FWD SEAT LEGS LOCK INTO TRACKS. REPLACED SEAT TRACK BETWEEN FR 42 AND FR 47. MAJOR REPAIR AT HMV. 2 L 7 2 4F 4 F RT A28NM E40NE 2007102900156 20071029 00156 EU 2007 10 29 2007UALA04268 1 20071016 A 2840 INDICATION SYS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUEL QTY MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 403UA 442 FLIGHT DIVERTED DUE TO LOSS OF FUEL QUANTITY INDICATIONS FOR THE RIGHT WING. REPLACED CADENSCION. 2 L 7 2 4F 4 F RT A28NM E40NE 2007102900157 20071029 00157 EU 2007 10 29 2007UALA04289 1 20071017 A 5320 MXP401600U STRUCTURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE OXYGEN MASK BOX FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 490UA 1728 F/O SIDE O2 PRESS TO TEST INOP DUE TO PLUNGER NOT ENGAGED TO DOOR MECHANISM MASK WORKS FINE. REPLACED FO O2 MASK BOX, S ERVICED SYSTEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007102900159 20071029 00159 NM 2007 10 29 2007UALA04291 1 20071017 A 2611 D2549000900089 SMOKE DETECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LAVATORY A FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 822UA 948 LAVATORY DETECTOR FAULT DISPLAYED ON UPPER ECAM SCREEN, SMOKE. REPLACED LAV A SMOKE DETECTOR- NO MSGS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007102900160 20071029 00160 EU 2007 10 29 2007UALA04301 1 20071018 A 5610 WINDOW AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT OUT OF ADJUST A UALA O OTHER O OTHER CR CRUISE 1 WP 29 409UA 462 LOUD SQUEAL F/O SLIDING WINDOW FL260 CABIN ALT 4250. STOPPED FL130 CABIN ALTITUDE 2650. PROBLEMS RECURRED ON FLT 166- 19 CAUSING DIVERSION TO DEN. FOUND AFT ROLLER OF FO WINDOW OUT OF ADJUSTMENT. ADJUSTED FO WINDOW AFT ROLLER PRESSU RIZED A/C WITH NO NOTED PROBLEMS. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007102900161 20071029 00161 EA 2007 10 29 TRAX200701528 1 20071017 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 722EV 10127 RIGHT AND LEFT 280 WEBS HAVE SIGNS OF SURFACE CORROSION JUST ABOVE 280 TRANSVERSE BEAM. REMOVED SURFACE CORROSION ON LT AND RT 280 WEBS PER CRJ700 SRM 53-11-10. 2 L 7 2 4F RT A21EA 2007103000001 20071030 00001 EA 2007 10 30 ASOA200701505 1 20071015 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 878AS 7590 FS 484 CLIP CRACKED AT I/B SIDE OF RBL 36.0. REMOVED BOLTS FROM RUDDER CONTROL CABLE FAIRLEAD AT FS 484 RBL 36.0. 14 212. DUPLICATED I/B CLIP AT FS 484 RBL 36.0 FROM .050" 7075 T-6 IAW CRJ 200 SRM 53-41-43 AND CRJ 200 SRM 51-24-16. 13362 . OK TO ALODINE AND PRIME. ALODINED PRIMED AND TOPCOATED IAW CRJ 200 SRM 51-25-00. 13362. OK TO INSTALL. INSTALLED SERVI CEABLE CLIP TO IB SIDE OF RBL 36.0 AT FS 484 IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21. REQUIRES BOLTS REINSTALL ED TO RUDDER CONTROL CABLE FAIRLEADS. REINSTALLED BOLTS ON RUDDER CABLE FAIRLEADS IAW CRJ SRM 51-41-02. 2 L 7 2 4F RT A21EA 2007103000003 20071030 00003 EU 2007 10 30 SIMA200729909 1 20071025 A 3150 WARNING LIGHT SAAB SF340 340B 7860101 EU LT APR FALSE ACTIVATION A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 394AE 340B394 LOW SPEED ABORT, NOTIFIED VIA TELESYS, LT APR LIGHT ON. ISSUED MEL 7602. PERFORMED OPERATIONAL CHECK OF APR SYSTEM IA W AE MTX WORK CARD 76-2813. OPS CHECK GOOD MEL RESTORED. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4T RT A52EU 2007103000004 20071030 00004 NM 2007 10 30 2007UALA04339 1 20071019 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS OUT OF ADJUST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 655UA 25393 EMERGENCY EEL LIGHT TURN ON AND OFF AT SEATS 1AB. ADJUSTED PLUG AT POWER SUPPLY NEXT TO THE SEAT 1AB. CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007103000005 20071030 00005 NM 2007 10 30 2007UALA04340 1 20071019 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SEAT 5B FWD SIDE MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 674UA 29242 THE 5B EMERGENCY EXIT LIGHT CAME OUT. REPLACED LIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007103000006 20071030 00006 NM 2007 10 30 2007UALA04341 1 20071019 A 3350 SIGN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 224UA 30225 MAIN AISLE EXIT SIGN AT 3L FOUND HANGING BY WIRE HARNESS. RESECURED SIGN. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007103000007 20071030 00007 NM 2007 10 30 2007UALA04342 1 20071020 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SEAT 2E AFT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 228UA 30556 EMERGENCY LIGHT INOP SEAT 2E AFT LIGHT. REPLACED LIGHT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007103000008 20071030 00008 NM 2007 10 30 SWAA075290 1 20071024 A 5311 6546554 FRAME BOEING 737 737317 138447P NM BS 847 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007103000009 20071030 00009 NM 2007 10 30 2007UALA04343 1 20071020 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ROW 17-22 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 507UA 24743 EEL LIGHTS AT 1ST CLASS CLOSET AND ROWS 17 - 22 ARE INOP. REPLACED LIGHT. CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007103000010 20071030 00010 EA 2007 10 30 TRAX200701573 1 20071023 A 5230 ANGLE CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 914EV 7752 FOUND ONE ANGLE CRACKED IN MEMBER BEAM OF CARGO DOOR AREA ON PRESSURE BLKD FS 621. 2 L 7 2 4F RT A21EA 2007103000011 20071030 00011 EA 2007 10 30 TRAX200701584 1 20071023 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 857AS 7411 UNABLE TO CLOSE SERVICE DOOR. 2 L 7 2 4F RT A21EA 2007103000012 20071030 00012 SO 2007 10 30 C2XA07CL089 1 20071023 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13958 145085 DURING ROUTINE MAINTENANCE THE RIGHT EMERGENCY EXIT SIDEWALL LIGHT WAS FOUND INOPERATIVE ALONG WITH THE AFT GALLEY EMERG ENCY LIGHT. MAINTENANCE INSPECTED AND REPLACED THE NR 3 & 5 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007103000013 20071030 00013 SO 2007 10 30 RAIA00710025 1 20071022 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 833HK 145240 PRE FLT NR 7928- ALB - LEFTHAND OVERWING EXIT MARKER EMERGENCY LIGHT INOP. MAINTENANCE RESET POWER, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007103000014 20071030 00014 NM 2007 10 30 KCSA071503 1 20071027 A 5320 WEB BOEING 747 7472B4B 138481B NM BS 920-940 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FORWARD BILGE WEB UNDER SEAT TRACK AT STA 920 TO 940, RBL 46 IS CRACKED (1.5 & 2 INCH) IN 2 AREAS. 2 L 7 4 4F RT A20WE 2007103000015 20071030 00015 NM 2007 10 30 2007UALA04344 1 20071020 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EMERGENCY EXIT EEL LIGHTS INOP AT SEAT 2A AFT LIGHT ASSY, SEAT 39 HJK & SEAT 47 HJK. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007103000016 20071030 00016 NM 2007 10 30 KCSA071492 1 20071023 A 5315 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 640 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FORWARD BILGE, FLOORBEAM UPPER CHORD IS DAMAGED AT STA 640, LBL 22. 2 L 7 4 4F RT A20WE 2007103000017 20071030 00017 NM 2007 10 30 2007UALA04345 1 20071020 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EMERGENCY EXIT LIGHT INOP AT DOOR 5 RIGHT BUSTLE LIGHT. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007103000018 20071030 00018 NM 2007 10 30 2007UALA04346 1 20071022 A 3350 SWITCH BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INTERMITTENT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EXIT LIGHTS FLICKER OVER 5R AND IN ECONOMY AISLE. EXECISED EMERGENCY LIGHT SWITCH AT DOOR 1L. 2 L 7 4 4F 4 F RT A20WE E24NE 2007103000019 20071030 00019 NM 2007 10 30 2007UALA04347 1 20071021 A 4920 211734220 ECU BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SHUTDOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 664UA 29236 APU AUTO SHUTDOWN AT DEPARTURE TWICE. REPLACED HIGH OIL TEMP SENSOR AND DRAINED OIL TANK. REPLACED ECU SYSTEM OP CHECKE D OK. REPLACED STARTER OP CHECK OK. FLT CREW ACCOMPLISHED VERIFICATION FLT AND SENT APPROPRIATE MESSAGE FOR NORMAL OPER ATION OF THE APU. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007103000020 20071030 00020 NM 2007 10 30 KCSA071500 1 20071025 A 5743 FITTING BOEING 747 7472B4B 138481B NM LT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 LEFT WING LANDING GEAR BEAM OUTBOARD END FITTING UT INSPECTION HAS CRACK/CORROSION INDICATION APPROX 7 O'CLOCK POSITION ON AFT HALF OF FITTING AT WS 586. 2 L 7 4 4F RT A20WE 2007103000021 20071030 00021 NM 2007 10 30 SWAA075233 1 20071022 A 5314 6545776 KEELBEAM BOEING 737 7373H4 1384600 NM BS 707-727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 707 AND BS 727. REMOVED AND REPLACED KEEL BEAM PER S RM. 2 L 7 2 4F RT A16WE 2007103000022 20071030 00022 SO 2007 10 30 C2XA07CL091 1 20071025 A 3097 TERMINAL BLOCK EMB 145 EMB145LR 3260212 SO WINDOW HEAT SHORTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 14959 5210 145091 CLE FLIGHT 2477 - THE CREW REPORTED A STRONG BURNING SMELL IN THE COCKPIT. MAINTENANCE INSPECTED AND FOUND THE TERMINAL BLOCK MELTED ON THE CAPTAINS WINDSHIELD. MAINTENANCE REPLACED THE CAPTAIN'S WINDSHIELD. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007103000023 20071030 00023 EU 2007 10 30 TRAX200701572 1 20071022 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 TWO MINUTE LIGHTING WILL NOT SHUT OFF. FLT 4726 DEL 32 MINS. 2 H 7 2 4T RT 2007103000024 20071030 00024 EA 2007 10 30 TRAX200701583 1 20071023 A 5270 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR ILLUMINATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 829AS 7232 PAX DOOR WARNING MESSAGE. A/C RETURNED TO YOW AFTER T/O. EMERGENCY EQUIPMENT ON STANDBY. FLT 4568 CX. 2 L 7 2 4F RT A21EA 2007103000025 20071030 00025 SO 2007 10 30 C2XA07RI092 1 20071022 A 3320 BR90002 BALLAST EMB 145 EMB145LR 3260212 SO CABIN LIGHTS DEFECTIVE A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 14959 145091 FLT 2322 - EWR - DURING TAXIING OUT OF THE GATE, CREW REPORTED A BURNING ODOR IN CABIN AND GALLEY AREA. CREW RETURNED T O GATE AND EWR MX FOUND BALLAST IN GALLEY AREA DEFECTIVE. MX REMOVED AND REPLACED BALLAST IN GALLEY AREA AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007103000026 20071030 00026 NM 2007 10 30 SWAA075232 1 20071022 A 5340 6545801 TEE FITTING BOEING 737 737301 1384611 NM BS 227 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED BRDG CHECK, FOUND BULKHEAD LOWER TEE CHORD CORRODED AT BS 227, BETWEEN LBL 10 AND RBL 10. REPAIRED TEE CHORD PER SWA EA. 2 L 7 2 4F RT A16WE 2007103000027 20071030 00027 NM 2007 10 30 SWAA075215 1 20071022 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 500C S23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500C, STR 23L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007103000028 20071030 00028 NM 2007 10 30 SWAA075207 1 20071022 A 5311 6546534 FRAME BOEING 737 7375H4 138449D NM BS 520 S8 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007103000029 20071030 00029 NM 2007 10 30 SWAA075211 1 20071022 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007103000030 20071030 00030 NM 2007 10 30 SWAA075219 1 20071022 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 482B S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000031 20071030 00031 NM 2007 10 30 SWAA075208 1 20071022 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 482A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482A, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000032 20071030 00032 NM 2007 10 30 SWAA075209 1 20071022 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 727A S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000033 20071030 00033 NM 2007 10 30 SWAA075218 1 20071022 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 706 S1 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000034 20071030 00034 NM 2007 10 30 SWAA075220 1 20071022 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 520 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000035 20071030 00035 NM 2007 10 30 SWAA075221 1 20071022 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 482B S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000036 20071030 00036 NM 2007 10 30 SWAA075222 1 20071022 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000037 20071030 00037 NM 2007 10 30 SWAA075223 1 20071022 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 460 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103000119 20071030 00119 SO 2007 10 30 C2XA07TY061 1 20071019 A 5330 SKIN EMB 145 EMB145XR 3260214 SO FUSELAGE DAMAGED A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 11150 145756 THE RIGHT FWD FUSELAGE II, CENTRAL FUSELAGE I SKIN AND SEVERAL UNDERLYING STRUCTURAL MEMBERS WERE DAMAGED AS A RESULT OF A TUG STRIKING THE AIRCRAFT. THE DAMAGE IS CONTAINED BETWEEN FRAMES 7 & 14, STR 16R & 20R. THE A/C IS BEING REPAIRED IAW EA5330-01106. 2 L 7 2 4F RT 2007103000120 20071030 00120 NM 2007 10 30 ASAA0752149 1 20071021 A 2131 CONTROLLER BOEING 737 737890 1384527 NM CABIN PRESSURE UNKNOWN A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 579AS 35187 THE "AUTO FAIL" & "ALTN" LIGHTS ILLUMINATED. COULD NOT DUPLICATE DISCREPANCY. REPLACED CABIN PRESS CONTROLLER AS A PRE CAUTION. ALL BITE TESTS PASS. 2 L 7 2 4F RT A16WE 2007103000121 20071030 00121 NM 2007 10 30 ASAA0752145 1 20071020 A 2160 6937319308 CONTROLLER BOEING 737 737890 1384527 NM CABIN TEMP UNKNOWN A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 584AS 35682 ZONE TEMP LIGHT FOR CONTROL CABIN CAME ON AFTER START OF ENGINES. COULD NOT EXTINGUISH. BITE ON NR 1 & 2 CABIN TEMP CO NTROLLERS SHOW FAULT FLIGHT DECK CABIN SENSOR. ACCOMPLISHED FIM 21 62 TASK 801. FAULT & ZONE TEMP LIGHT CLEARED. BITE CHECKS GOOD. 2 L 7 2 4F RT A16WE 2007103000122 20071030 00122 2007 10 30 ASAA0752147 4 20071021 A 2210 8221567102 CONTROL PANEL BOEING 737 737890 1384527 NM ALTITUDE UNKNOWN A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 557AS 35176 ALTITUDE SELECTOR FROZEN ON MCP PANEL (STUCK AT 50,000). CYCLED MODE CNTL PANEL POWER. DISPLAY CONTROL RETURNED. MCP CHECKS OK. 2 L 7 2 4F RT A16WE 2007103000123 20071030 00123 NM 2007 10 30 ASAA0752150 1 20071022 A 2822 343A2801 PUMP BOEING 737 737890 1384527 NM NR 1 FUEL TANK LOW PRESSURE A ASAA O OTHER J WARNING INDICATION CR CRUISE 1 NM 02 583AS 35681 NR 1 AFT MAIN FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED AT CRUISE WITH ALL 6 PUMPS ON. PUMP WAS TURNED OFF & LEFT OFF PE R QRH. VERIFIED PUMP, OPS NORMAL DURING FUEL TRANSFER (FIM 28 77 802). 2 L 7 2 4F RT A16WE 2007103000124 20071030 00124 NM 2007 10 30 ASAA0752143 1 20071019 A 2822 343A2801 PUMP BOEING 737 737890 1384527 NM NR 1 FUEL TANK LOW PRESSURE A ASAA O OTHER O OTHER DE DESCENT 1 NM 02 583AS 35681 NR 1 AFT FUEL LOW PRESSURE LIGHT ILLUMINATED ON DESCENT. LIGHT WAS ON DIM, WENT BRIGHT WHEN PUMP TURNED OFF. 3,900LBS OF FUEL IN TANK. PERFORMED FIM TASK 28 22 TASK 803. NO FAULTS FOUND. SUMPED NR 1 TANK, NO WATER FOUND. INSPECTED CON NECTOR ON PRESSURE SWITCH, NO DAMAGE FOUND. 2 L 7 2 4F RT A16WE 2007103000125 20071030 00125 NM 2007 10 30 ASAA0752141 1 20071019 A 2130 71231997302AB CONTROL MODULE BOEING 737 737890 1384527 NM CABIN PRESSURE UNKNOWN A ASAA O OTHER J WARNING INDICATION CR CRUISE 1 NM 02 579AS 35187 THE "AUTO FAIL" & "ALTN" LIGHTS ILLUMINATED. COULD NOT DUPLICATE. REPLACED CABIN PRESSURE CONTROL MODULE AS A PRECAUTI ON. ALL BITE TESTS PASS. 2 L 7 2 4F RT A16WE 2007103000126 20071030 00126 WP 2007 10 30 ASAA0782134 1 20071022 A 5320 993658019 INTERCOSTAL DOUG DC9 DC983 3022083 WP BS 228-237 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 INTERCOSTAL UPPER FLANGS EXFOILATED STA 228 AT LBL 34. REMOVED DAMAGED INTERCOSTAL, LOCATED DRILLED AND INSTALLED A REP LACEMENT INTERCOSTAL AND REPAIR PARTS FOR WIRE FEED THRU IAW MD80 SRM 51-30-5 PG 1, 53-01 FIG 2 PG 13. 2 L 7 2 4F RT A6WE 2007103000127 20071030 00127 SO 2007 10 30 C2XA07SH087 1 20071023 A 3350 AD20131A BATTERY EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12934 019 DURING SERVICE ROUTINE EMERGENCY LIGHT IN GALLEY AND FLOOR (1-3) INOP. MAINTENANCE REMOVED AND REPLACED NR 2 EMERGENCY BATTERY (SVC DOOR) IAW EMB 145 AMM 33-50-04, OPS CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007103000128 20071030 00128 2007 10 30 UHLA200710231 4 20071020 A 2565 4A40302 SLIDE EMB ERJ170 ERJ170100SE 3260406 EU L1 DOOR MISMANUFACTURED A UHLA K NONE L NO TEST IN INSP/MAINT 1 GL 11 635RW 17000056 DURING A SCHEDULED OPS CHECK OF L1 DOOR AND SLIDE THE SLIDE EXTENDED INVERTED (COMPLETELY UPSIDE DOWN) WHICH CAUSED MINO R DAMAGE BENEATH L1 DOOR OPENING. THE FUSELAGE DAMAGE WAS ADDRESSED WITH AN IC2007-170/07425. THE SLIDE VENDOR HAS BEE N CONTACTED AND AN INVESTIGATION IS UNDERWAY TO DISCOVER THE ROOT CAUSE. 2 L 7 2 4F RT A56NM 2007103000129 20071030 00129 NM 2007 10 30 2007UALA04352 1 20071021 A 2130 CLAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU A/C PACK BROKEN A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 341UA 24245 AIRCRAFT UNABLE TO MAINTAIN PRESSURE WITH SINGLE PACK OPERATION. FOUND APU BELLOWS CLAMP WAS FOUND LOOSE/BROKEN AND LE AKING PRESSURE. REPLACED CLAMP. PERFORMED SINGLE PACK PRESSURIZATION OF A/C. ALL CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007103000130 20071030 00130 NM 2007 10 30 2007UALA04353 1 20071023 A 7830 STRUCTURE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE THRUST REVERSER GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 104UA 26902 ON WALK AROUND FOUND GOUGE ON NR 2 OUTER REVERSER HALF AT THE 7 O'CLOCK POSITION. REPAIRED IAW UA EVA-70729 AND SRM 54 -30-01. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007103000131 20071030 00131 EU 2007 10 30 2007UALA04354 1 20071021 A 7160 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NOSE COWL PUNCTURED A UALA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 WP 29 476UA 1508 TAKEOFF RUNWAY DEBRIS CAUSED NR 2 ENG NOSE COWL OUTER SKIN PUNCTURE AND FAN COWL SKIN DAMAGE. A/C STRIKING FOD TO NR 2 ENG AREA OR FUESLAGE FROM BLOWING CONSTRUCTION DEBRIS ON TAKE OFF. A/C FERRIED TO ORD WHERE NOSE NR 2 NOSE COWLING WAS REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007103100005 20071031 00005 NM 2007 10 31 SWAA075357 1 20071025 A 5315 147A5006 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 756SA 27872 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 45 TO RBL 40. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007103100009 20071031 00009 NM 2007 10 31 SWAA075340 1 20071025 A 3350 10107451 SIGN BOEING 737 7373A4 1384585 NM EMERGENCY EXIT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND AFT CABIN EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007103100016 20071031 00016 2007 10 31 UPS07851058 4 20071026 A 2565 SLIDE DOUG DC8 DC873F 302199F WP PAX DOOR UNSECURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 ESCAPE SLIDE CAME LOOSE. RESECURED ESCAPE SLIDE TO FWD ENTRY DOOR B DC8 25-60. 2 L 7 4 4F RT 4A25 2007103100017 20071031 00017 WP 2007 10 31 UPS07850993 1 20071005 A 5340 5887709501 FITTING DOUG DC8 DC873F 302199F WP FS 580 L33R BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 B-PIT FS 580 L33R FWD L-FITTING BROKEN (P/N 5887709-501). REMOVED, FABRICATED AND INSTALLED REPLACEM ENT FITTING IAW SRM 51-1-20D, 51-01-24 AND 51-03-00. 2 L 7 4 4F RT 4A25 2007103100023 20071031 00023 GL 2007 10 31 UPS07850983 2 20071023 A 7200 ENGINE DOUG DC8 DC871F 302199D WP GE CFM CFM562 GL NR 4 FLAMED OUT A IPXA E ENGINE SHUTDOWN X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 01 705UP 45949 692442 NNNDURING CRUISE FLT W/ENG ANTI-ICE ON (TAT -1), NR 4 ENGINE FLAMED OUT. ENG INDICATIONS WERE NORMAL. RESTART ACCOMPLI SHED. ENG OPERATED NORMALLY FOR REMAINDER OF FLT. PERFORMED NR 4 ENG FLAME OUT T/S CHART PER AMM 71-00-00-1 FIG 139. INSPECTED CHIP DETECTORS, FUEL FILTER, CDP TUBE FOR LEAKS, FUEL CONTAMINATION, N1 & N2 ROTORS, NO ABNORMALITIES FOUND. ACCOMPLISHED ENG MAX PWR ASSURANCE RUN PER AMM 71-00-00-5 ADJ/TEST. NR 4 ENG OPS CHECKED NORMAL. A/C RETURN TO SERVICE . 2 L 7 4 4F 4 F RT 4A25 E2GL 2007103100025 20071031 00025 WP 2007 10 31 UPS07850989 1 20070924 A 5711 SPAR DOUG DC8 DC873F 302199F WP RWS 98 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 RIGHT WING FLAP STA 98 ACTUATOR FWD FITTING ON AFT SPAR HAS DEEP PITTING CORROSION ON BOTH LUGS. REM OVED AND REPLACED RIGHT WING FLAP STA 98 FWD FITTING ON AFT SPAR IAW SRM 51-12-2 AND AMM 20-14-00-2. 2 L 7 4 4F RT 4A25 2007103100026 20071031 00026 NM 2007 10 31 UPS07M50967 1 20070730 A 5712 RIB DOUG MD11 MD11F 3023600 NM RT WING SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C RIGHT WING NR 16 SLAT TRACK I/B RIB FITTING SUSPECTED CRACK AS MARKED. HFEC INSP C/OUT FOUND CRACK AS MARKED. RIGHT WING NR 8 EXT & RET CABLES DISCONNECTED. RIGHT WING NR 16 SLAT TRACK DOOR, ATTACHED HARDWARES & ROLLERS & SLAT TRACK REMOVED. RIGHT WING NR 16 SLAT WIRING, CLAMPS & RIB REMOVED. NEW HOLES TRANSFERED ONTO NEW RIB PER DOUGL AS DWG ARB2873. DAMAGE AREA AT WING SKIN & DOUBLER TRIM OFF. HFEC INSP C/OUT ON TRIMMED OFF AREA FOUND. 2 L 7 3 4F RT A22WE 2007103100030 20071031 00030 NM 2007 10 31 UPS07M51025 1 20070829 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C LEFT HORIZONTAL STABILIZER BARREL NUT HOLE 1L HAS CORROSION IN HOLE. CORROSION AT BARREL NUT BORE REM OVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROS ION. BARREL NUT BORE BLEND OUT & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APPLIED. 2 L 7 3 4F RT A22WE 2007103100042 20071031 00042 2007 10 31 ASAA0752152 4 20071023 A 2310 BUTTON BOEING 737 737890 1384527 NM AUDIO CONTROL STICKING A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 559AS 35178 F/O'S AUDIO PANEL: HF NR 1 TRANSMIT BUTTON STICKS TOUGH TO ACTIVATE. REPLACED F/O'S AUDIO CONTROL PANEL. OPS NORMAL. 2 L 7 2 4F RT A16WE 2007103100043 20071031 00043 2007 10 31 ASAA0742151 4 20071023 A 2565 65C168201 LATCH BOEING 737 7374Q8 138447Q NM L2 DOOR SLIDE MISINSTALLED A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 779AS 25111 FLIGHT ATTENDANT UNABLE TO ARM L2 DOOR. FOUND LATCH ASSY INSTALLED INCORRECTLY. PROPERLY INSTALLED LATCH ASSY. (REF M M25 61 35 PG 209 & MM SUPP 25 61 35) 2 L 7 2 4F RT A16WE 2007103100057 20071031 00057 NM 2007 10 31 UPS07M50969 1 20070904 A 2810 TANK DOUG MD11 MD11F 3023600 NM BS 1239-1255 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C LEFT SIDE CENTER AUX TANK STA 1239.0 - 1255.0, X=103.0 FOUND CORROSION A ROUND FASTENERS AS MARKED. L EFT SIDE CTR AUX TANK STA 1239.0-1255.0 X=103.0 FASTENER AS MARK REMOVED. CORROSION ON UPPER SKIN REMOVED & REWORKED AR EA PROTECTED. HFEC OPEN HOLE & FPI C/OUT ON REWORKED AREA FOUND NO CRACK & NO CORROSION. REWORKED AREA UPP SKIN MAT'L REMOVED & REMAINED ALL FOUND EXCEED LIMITS. FLAP PEENING C/OUT ON REWORKED AREA PER EN1638-07. REWORKED AREA. 2 L 7 3 4F RT A22WE 2007103100078 20071031 00078 WP 2007 10 31 ASAA0782144 1 20071023 A 5753 5930496510 VANE DOUG DC9 DC983 3022083 WP TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 RIGHT WING O/B FLAP I/B VANE REPAIR DOUBLER IS CHAFED AT I/B CORNER. REMOVED PREVIOUS REPAIR DOUBLER, PREPARED AND FABR ICATED REPAIR DOUBLER, LOADED AND INSTALLED FASTENERS IAW MD80 SRM 51-70-2 PG 11 PAR 6 23 59. 2 L 7 2 4F RT A6WE 2007103100086 20071031 00086 EA 2007 10 31 TRAX200701586 1 20071024 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR TORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 EXIT PLACARD ON PAX DOOR TORN AND NOT SECURE. 2 L 7 2 4F RT A21EA 2007103100092 20071031 00092 NM 2007 10 31 SWAA075270 1 20071023 A 5753 6549509 FLAP TRACK BOEING 737 737301 1384611 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 2 FLAP TRACK CRACKED. REMOVED AND REPLACED FLAP TRACK PER SRM. 2 L 7 2 4F RT A16WE 2007103100093 20071031 00093 NM 2007 10 31 SWAA075271 1 20071023 A 5753 6549509 FLAP TRACK BOEING 737 737301 1384611 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED BRDG CHECK, FOUND RT WING NR 7 FLAP TRACK CRACKED. REMOVED AND REPLACED FLAP TRACK PER SRM. 2 L 7 2 4F RT A16WE 2007103100116 20071031 00116 NM 2007 10 31 2007UALA04373 1 20071024 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EEL LT INOP: MID LAV CROSS AISLE. SECURED LOOSE CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007103000154 20071030 00154 WP 2007 10 30 ASAA0782132 1 20071022 A 5347 593056675 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 1042-1231 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 CABIN SEAT TRACK CORRODED TOP AND BOTTOM STA 1042 TO STA 1231 AT LBL 22. REMOVED DAMAGED SEAT TRACK, LOCATED, DRILLED A ND INSTALLED A REPLACEMENT SEAT TRACK AND SPLICE DOUBLERS IAW MD80 SRM 51-10-4 PGS 1 AND 2, 53-05 FIG 4F SHTS 1 & 2. 2 L 7 2 4F RT A6WE 2007103100118 20071031 00118 NM 2007 10 31 SWAA075260 1 20071023 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 847 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103100120 20071031 00120 NM 2007 10 31 SWAA075262 1 20071023 A 5313 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 907 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103100126 20071031 00126 NM 2007 10 31 NOCA15807 1 20071020 A 2612 UL27939 FIRE LOOP BOEING 757 75728A 1384976 NM NR 1 MALFUNCTIONED A NOCA K NONE N FALSE WARNING IN INSP/MAINT 1 EA 15 756NA 32448 RIGHT ENG 1 EICAS STATUS MSG. REMOVED AND REPLACED NR 4 DETECTOR ON THE NR 2 ENG PER AA E58 CARD 9325657 PER MM 26-11-0 1. OPS CHECK NORMAL, NO EICAS MSG. 2 L 7 2 4F RT A2NM 2007103100131 20071031 00131 NM 2007 10 31 2007UALA03907 1 20070926 A 2497 31T42501 GROUND STUD BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 1 GENERATOR ARCED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 675UA 29243 MULTIPLE ELECTRICAL FLUCTUATIONS EXPERIENCED IN FLIGHT. ARCING DAMAGE FOUND ON BOTH GROUND STUDS AND ATTACHING HARDWARE . REPLACED NR 1 ENGINE GENERATOR FEEDER CABLE GROUND STUDS AND SELF LOCKING NUTS REF GNMM 2-0-7-002. BONDING CHECKS GO OD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007103100138 20071031 00138 2007 10 31 SWAA075241 4 20071023 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007103100140 20071031 00140 NM 2007 10 31 CALA0700602 1 20071021 A 3350 D71702030 CHARGER BOEING 767 767424ER 1385270 NM EMERGENCY LIGHTS INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59053 29448 THE EMERGENCY PATH LIGHT AT SEATS 5, 6 AND 7 WOULD NOT ILLUMINATE. THE EMERGENCY POWER SUPPLY D21296 WAS REMOVED AND RE PLACED IAW AMM 33-51-07. 2 L 7 2 4F RT A1NM 2007103100141 20071031 00141 NM 2007 10 31 CALA0700565 1 20071010 A 3350 D71702100 BATTERY PACK BOEING 737 737924 13848A1 NM EMERGENCY LIGHTS DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 30401 30118 EMERGENCY LIGHTS INOP IN FIRST CLASS AND L1 + R1 EXITS. INSTALLED 2 NEW BATTERY PACKS, OPS CHECKS OK MM 33-51-00 33-51- 06. 2 L 7 2 4F RT A16WE 2007103100146 20071031 00146 NM 2007 10 31 KCSA071494 1 20071024 A 5330 SKIN BOEING 747 7472B4B 138481B NM BS 2320 S22L DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 EXTERNAL FUSELAGE SKIN IS DAMAGED AT STA 2320, STR 22L. 2 L 7 4 4F RT A20WE 2007103100147 20071031 00147 NE 2007 10 31 2007UALA03909 2 20070926 A 7200 PW4077 ENGINE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 FOD A UALA O OTHER C F.O.D. NR NOT REPORTED 1 WP 29 780UA 38199 26944 777037 LEFT ENGINE HAS SIGNS OF BIRD STRIKE. ACCOMPLISHED INSPECTION OF ENGINE PER MM 72-00-00. CONFIRMED FOD DAMAGE TO 7TH S TAGE COMPRESSOR. 7TH STAGE BLADE IS OUT OF LIMITS. WHEN LOOKING THROUGH AP5 PORT. ALSO FOUND LESS SIGNIFICANT DAMAGE TO 10TH AND 11TH STAGE. DAMAGE TO 7TH STAGE OUT OF ACCEPTABLE LIMITS. REPLACED ENGINE. PERFORMED HIGH POWER ENGINE RU N. OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007103100163 20071031 00163 NM 2007 10 31 2007UALA04381 1 20071024 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 309UA 23670 EMERGENCY LIGHT CAME LOOSE FROM FLOOR. REPLACED DAMAGED LIGHT AND SECURED COVER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007103100180 20071031 00180 2007 10 31 2007UALA04348 4 20071021 A 3442 20414440402 DRIVE UNIT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE WX RADAR SYS FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 786UA 26938 WEATHER RADAR SYSTEM FAILURE. REPLACED RADAR ANTENNA DRIVE UNIT, OPS CHEKS OK. SUSPECT BAD ANTENNA CONNECTION. AC OK F OR SERVICE 2 L 7 2 4F 4 F RT T0001SE E46NE 2007103100183 20071031 00183 NM 2007 10 31 2007UALA04304 1 20071018 A 3350 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 840UA 1522 EMERGENCY LIGHT SYSTEM TEST FAILED ON PTP PANEL (EPSU AFT L). 11-01-07 FOUND FAULTY EPSU. REPLACED EPSU. 2 L 7 2 4F 4 F RT A28NM E40NE 2007103100185 20071031 00185 2007 10 31 2007UALA04306 4 20071018 A 2565 69451433 WINDOW BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU DOOR SLIDE BOTTL MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 330UA 24191 AFT GALLEY DOOR SLIDE COVER IS MISSING BOTTLE PRESSURE VIEWING WINDOW. SUSPECT CREW OR PASSENGER DISLODGED WINDOW. RE MOVED SLIDE, INSTALLED NEW WINDOW & REINSTALLED SLIDE. AC OK FOR SERVICE 2 L 7 2 4F 4 F RT A16WE E21EU 2007103100188 20071031 00188 NM 2007 10 31 2007UALA04309 1 20071018 A 5740 SUPPORT BRACKET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT WING FLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 RIGHT WING OUTBOARD FLAP INBOARD JACK SCREW FWD JACKSCREW SUPPORT BRACKET INBOARD LWR RADIUS ABOVE BORE LUG CRACKED. R T WING OTBD FLAP INBD JACK SCREW FWD JACK SCREW SUPPORT BRACKET INBD LOWER RADIUS ABOVE BORE LUG CRACKED. REMOVED AND R EPLACED FLAP JACKSCREW SUPPORT BRACKET. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110100001 20071101 00001 NM 2007 11 1 CALA0700605 1 20071023 A 5340 BAC1506210 ANGLE BOEING 737 7373T0 1384582 NM BS 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND TEE ANGLE AT L-2 DOOR GIRT BAR HOLE CORRODED, STA 986.5, WL 208.1, BL 0 TO LBL 40. A REPAIR WAS INSTAL LED IAW ECRA 5311-01370. 2 L 7 2 4F RT A16WE 2007110100008 20071101 00008 NM 2007 11 1 SWAA075392 1 20071028 A 5315 141A5504 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 758SW 27873 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 26. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007110100023 20071101 00023 NM 2007 11 1 SWAA075322 1 20071025 A 3350 6556633 SIGN BOEING 737 7375H4 138449D NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 LEFT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2007110100026 20071101 00026 NM 2007 11 1 SWAA075324 1 20071025 A 3350 6556633 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007110100027 20071101 00027 NM 2007 11 1 SWAA075390 1 20071028 A 3350 3071BPEGPL LAMP BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007110100028 20071101 00028 NM 2007 11 1 SWAA075369 1 20071028 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM BS 867 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110100034 20071101 00034 NM 2007 11 1 SWAA075339 1 20071025 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 727B S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007110100039 20071101 00039 NM 2007 11 1 SWAA075389 1 20071028 A 5330 6545776 SKIN BOEING 737 7373T5 1384608 NM BS 948 S21R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 948, STR 21R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007110100050 20071101 00050 WP 2007 11 1 UPS07851015 1 20071025 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REPLACED EMERGENCY BATTERY PACK PER AMM 33-50-01-2-4. OPS GOOD. 2 L 7 4 4F RT 4A25 2007110100058 20071101 00058 NM 2007 11 1 SWAA075358 1 20071027 A 3350 10107451 SIGN BOEING 737 7377H4 1384404 NM EMERGENCY EXIT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 229WN 32498 R2 DOOR EMERGENCY EXIT SIGN MISSING. REMOVED AND REPLACED SIGN PER MM. 2 L 7 2 4F RT A16WE 2007110100064 20071101 00064 NM 2007 11 1 SWAA075371 1 20071028 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM BS 520 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110100070 20071101 00070 NM 2007 11 1 SWAA075395 1 20071028 A 5314 6562125 KEELBEAM BOEING 737 7375H4 138449D NM BS 487 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED 18Y CHECK, FOUND RT KEEL BEAM CORRODED AT BS 487. REPAIRED KEEL BEAM PER EA. 2 L 7 2 4F RT A16WE 2007110100074 20071101 00074 NM 2007 11 1 2007UALA04314 1 20071019 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 CEILING EMERGENCY LIGHTS AT AFT CREW REST AREA, 8R AND AT 33R ARE INOPERATIVE. 11-01-07 RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110100093 20071101 00093 NM 2007 11 1 SWAA075253 1 20071023 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM BS 1006 S27L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 1006, STR 27L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007110100096 20071101 00096 NM 2007 11 1 SWAA075244 1 20071023 A 5311 6546525 FRAME BOEING 737 7375H4 138449D NM BS 380 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16R. REPAIRED FRAME PER EA. 2 L 7 2 4F RT A16WE 2007110100097 20071101 00097 NM 2007 11 1 SWAA075257 1 20071023 A 5311 6546526 FRAME BOEING 737 7377H4 1384404 NM BS 400 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 790SW 30604 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 16R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110100104 20071101 00104 NM 2007 11 1 2007UALA04390 1 20071025 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY LIGHT AT SEAT 5J INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110100105 20071101 00105 NM 2007 11 1 2007UALA04391 1 20071024 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 7B UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EXIT LIGHT HANGING OFF SEAT 7B. SECURED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110100109 20071101 00109 NM 2007 11 1 SWAA075376 1 20071028 A 5311 6546552 FRAME BOEING 737 737317 138447P NM BS 827 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110100114 20071101 00114 EU 2007 11 1 TRAX200701558 1 20071022 A 5714 BRACKET AEROSP ATR72 ATR72 EU WING BOX CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 WING BOX FR 24 L-BRACKET CRACKED 291BL. 2 H 7 2 4T RT 2007110100122 20071101 00122 NM 2007 11 1 2007UALA04326 1 20071022 A 5280 DOOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE RT MLG DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 809UA 825 RIGHT GEAR DOOR DAMAGED, AT TIP SEAL AREA, PART OF TIP SEAL IS MISSING FROM DOOR AND HONEYCOMB IS EXPOSED. REPLACED RI GHT GEAR DOOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110100129 20071101 00129 NM 2007 11 1 NOCA16007 1 20071025 A 3350 SIGN BOEING 767 76739H 1385311 NM EMERGENCY LIGHTS BROKEN A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 760NA 26257 L1 DOOR EMERGENCY LIGHT EXIT SIGN BROKEN. REMOVED AND REPLACED L1 DOOR EXIT SIGN ASSY IAW 33-51-01, OPS CHECKS OK. 2 L 7 2 4F RT A1NM 2007110100141 20071101 00141 EU 2007 11 1 TRAX200701565 1 20071022 A 5753 BRACKET AEROSP ATR72 ATR72 EU LT TE FLAP CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 LEFT INBOARD FLAP 2 OMEGA BRACKET CRACKED ON FLAP BEAM RIB 5. 2 H 7 2 4T RT 2007110100159 20071101 00159 NM 2007 11 1 2007UALA04034 1 20071002 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 680 DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 518UA 24871 BS 680 LBL 26", BS 720 LBL 26" ON FRAME UPPER CAPS HAVE MIS-DRILLED HOLES. *S/D* MAJOR REPAIR ACCOMPLISHED. AFTER DTA THESE REPAIRS HAVE BEEN CONSIDERED CAT 'C' OR TIME LIMITED. ENGINEERING TO REVIEW CURRENT REPAIRS FOR CAT 'A' OR 'B' C ONSIDERATIONS. ALL REPAIRS TO BE COMPLETED AT NEXT HMV-3. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110100171 20071101 00171 EU 2007 11 1 COEA0703919 1 20070924 A 5310 S53671217210 CREASE BEAM AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 919FX 266 FOUND DURING HEAVY CHECK. LEVEL 2 CORROSION. CORROSION ON LT CREASE BEAM WEB UPPER SURFACE. REMOVED AND INSTALLED FAB RICATED CREASE BEAM WEB. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007110100174 20071101 00174 EU 2007 11 1 USA2007F00013 1 20070906 A 5330 SKIN AIRBUS A321 A321211 3930370 EU LYC ALF502 ALF502R5 41580 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 184US 20303 1651 CORRODED RIVET TAILS WERE FOUND IN THE FUSELAGE FORWARD CARGO COMPARTMENT BETWEEN FRAME 26 TO 35.7 STRINGER 38R TO 38L. APPROXIMATELY 217 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD T HE PAINT FLAKING OFF THE RIVET TAILS THAT WERE CLEANED AND HAD PRIMER AND PAINT REAPPLIED. AIRCRAFT WAS MFG 31 JANUARY 2002. (K) 2 L 7 2 4F 4 F RT A28NM E6NE 2007110100179 20071101 00179 EU 2007 11 1 IJO2007F00000 1 20070930 A 3260 WARNING LIGHT BRAERO DH125 BAE125800A 1500285 EU GARRTT TFE731 TFE731* 01518 WP MLG FALSE INDICATION E IJOA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 15 150SB 258197 AFTER TAKEOFF, LANDING GEAR SELECTED UP. AT ABOUT 1,000 FT AGL, NOSE & RT MLG RED TRANSITION LIGHTS WERE STILL ILLUMINA TED. SELECTED LANDING GEAR DOWN, AT WHICH TIME ALL 3 GREEN SAFE LIGHTS ILLUMINATED, ALONG WITH AN INCREASED WIND NOISE LEVEL FROM THE EXTENDED LANDING GEAR. NOTIFIED ATC THE FLT WAS RETURNING. LANDING WAS NORMAL. MX PLACED AIRCRAFT ON J ACKS, AND PERFORMED A VISUAL INSPECTION OF THE LANDING GEAR WITH NO ANOMALIES NOTED. THE AUXILIARY HYDRAULIC VALVE RECY CLED, AND THE NOSE STRUT PRESSURE WAS VERIFIED AS CORRECT. THE LANDING GEAR SYSTEM WAS CYCLED SEVERAL TIMES IAW MM WITH NO DISCREPANCIES NOTED. THE AC WAS RETURNED TO SERVICES. 2 L 7 2 4F 4 F RT A3EU E6WE 2007110100180 20071101 00180 CE 2007 11 1 DXTA200702549 1 20071017 A 3260 DOWNLOCK SWITCH BEECH MU300 400A 1155402 CE MLG MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 132QS RK427 ON FINAL APPROACH THE RT MAIN GEAR (GREEN) LIGHT FAILED TO ILLUMINATE. ACCESSED CONNECTOR P272 IN RT WW. OHMED OUT DOW N LOCK SWITCH FOUND 2 OHMS RESISTANCE THROUGH CLOSED CONTACTS OF SWITCH, REMOVED SWITCH AND INSTALLED NEW CUSTOMER SUPPL IED SWITCH. REINSTALLED CONNECTOR P272 OPS CHECKED NO DEFECTS NOTED PER 400XP MM 32-10-02 2 H 7 2 4F RT A16SW 2007110100184 20071101 00184 EA 2007 11 1 S9BA200700021 1 20071016 A 5753 SKIN DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA TE FLAP CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 12 573 RT TRAILING FLAP SKIN CORRODED AT ATTACHMENT HINGE FITTING. REMOVED AND REPLACED RT TRAILING FLAP. 1 H 7 2 3T 4 T RT A9EA E4EA 2007110200080 20071102 00080 NM 2007 11 2 AMTA200700539 1 20071019 A 5330 PANEL BOEING 757 75733N 1384931 NM BS 1310-1410 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 550TZ 32584 AFT CARGO PIT BILGE LT SIDE PANEL HAS CORROSION ON UPPER AND LOWER SURFACES FROM STATION 1310 TO 1410. REMOVED CORROSIO N SRM 51-10-00. FOUND OUT OF LIMITS PER SRM 53-60-53. REPAIRED PANEL SRM 51-70-11 FROM STATION 1410 TO 1360. REMOVED CORROSION FROM 1360 TO 1310 ORIG MATL .063 MAT REMOVED .005 WITHIN LIMITS PER SRM 53-60-53. TREATED PER SRM 51-00-00. (M) 2 L 7 2 4F RT A2NM 2007110200083 20071102 00083 2007 11 2 AMTA200700555 4 20071017 A 2565 LIGHT DOUG DC10 DC1030 3023501 WP L4 DOOR SLIDE INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 705TZ 46915 DURING PRE FLIGHT 4L DOOR SLIDETEST LIGHT WOULD NOT PRESS TO TEST. RELAMP SLIDEPACK PRESSURE INDICATOR. OPS CHECK NORM AL IAW 25-61-01. (M) 2 L 7 3 4F A22WE 2007110200086 20071102 00086 NM 2007 11 2 AMTA200700525 1 20071018 A 2700 UNKNOWN BOEING 757 75733N 1384931 NM AILERON CONTROL UNKNOWN A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 550TZ 32584 EO 757-27AD-3162 AILERON CONTROL, ADDITION OF LATERAL DAMPER TO THE FIRST OFFICERS AILERON CONTROL QUADRANT. COMPLIED W ITH EO 757-27AD-3162. (M) 2 L 7 2 4F RT A2NM 2007110200087 20071102 00087 2007 11 2 MALA070174 4 20071010 A 2200 RELAY SAAB SF340 340B 7860101 EU AUTOPILOT UNKNOWN A MALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 15 407XJ 340B407 L ROLL INDICATION TRAVELED FULL UP ON ITS OWN. ALL CAUTION LIGHT CAME UP. AUTOPILOT WAS ON. RETRIMMED THE L AILERON. REPLACED AUTOPILOT TRIM SERVO RELAYS, FLIGHT CONTROL COMPUTER, AILERON TRIM ACTUATOR, TRIM CONTROL PANEL. REF CONT CAR D FOR DETAILS. NR 1 CHANGE AUTO TRIM RELAYS FOR PRECAUTIONARY MEASURES. REMOVED AND REPLACED RELAYS 13FD, 14FD, 15 FD, 16 FD, 14 CC, 22 CC, 24CC IAW SF340 MM CH 22-10. NR 2 CHANGE AILERON TRIM ACTUATOR FOR PRECAUTIONARY MEASURES. REF SA AB AMM CH 27-12-10-12. NR 3 FOR PRECAUTION REPLACE THE FCC. REMOVED AND REPLACED FLT CONTROL COMPUTER PN 622-7491-210, SN ON 2382, SN OFF 2367. OPS CHECK GOOD IAW SF340 MM CH 34-22-05. NR 4 CHANGE TRIM CONTROL PANEL ASSY FOR PRECAUTIONA 2 L 7 2 4T RT A52EU 2007110200093 20071102 00093 NM 2007 11 2 AMTA200700522 1 20071017 A 5313 LONGERON BOEING 757 75733N 1384931 NM FS 1330 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 550TZ 32584 AFT CARGO PIT CORROSION ON LONGERON AT STATION 1330 LBL 10.45. REMOVED CORROSION MATERIAL LOSS .030 OUT OF LIMITS. REP AIRED IAW SRM 53-30-53-1A. (M) 2 L 7 2 4F RT A2NM 2007110200100 20071102 00100 SO 2007 11 2 SIMA200729904 1 20071025 A 5250 7312212505 DOOR EMB 145 EMB145LR 3260212 SO LAVATORY STUCK A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 681AE 14500824 LAV DOOR STUCK CLOSED. REMOVED AND REPLACED LAV DOOR IAW EMB 145 AMM 25-44-01, OPS CHECK GOOD. AIRCRAFT RETURN TO SERV ICE. 2 L 7 2 4T RT T00011AT 2007110200101 20071102 00101 2007 11 2 SIMA200729705 4 20071018 A 2210 YAW DAMPER CNDAIR CL600 CL6002C10 1390015 EA MALFUNCTIONED A SIMA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CR CRUISE 1 SW 21 502AE 10018 ITEM-1 SUBTLE YET NOTICEABLE UNCOMMANDED RIGHT YAW DURING FLIGHT W/AUTO PILOT ON. AILERONS TRIED TO CORRECT. NO ENGINE TROUBLE. FELT AS THOUGH RUDDER WAS BEING PRESSED. FLT CONTROL SYNOPTIC PAGE REVEALED NOTHING ABNORMAL. CAUTION DISAP PEARED WHEN AUTO PILOT WAS TURNED OFF. ITEM-2. YD2 INOP STATUS MSG CAME ON (WHILE TAXIING IN) ON GROUND. ISSUED MEL 2 2-11. 2 L 7 2 4F RT A21EA 2007110200109 20071102 00109 EA 2007 11 2 SWIA200718798 1 20071021 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 932SW 7714 FLT 350 - RIGHT SIDE WINDSHIELD SHATTERED AT FL350. REPLACED WINDOW IAW MM 56-12-01, P/N: NP-139322-12, S/N OFF: 021974 1245. 2 L 7 2 4F RT A21EA 2007110200111 20071102 00111 EA 2007 11 2 SWIA200718800 1 20071021 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR LACK OF LUBE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 468CA 7649 SERVICE DOOR OUTER HANDLE WILL NOT OPEN. CLEANED AND LUBED OUTER SERVICE DOOR HANDLE IAW AMM 12-20-52. 2 L 7 2 4F RT A21EA 2007110200112 20071102 00112 SO 2007 11 2 SWIA200718801 1 20071018 A 5210 HINGE EMB 120 EMB120ER 3260203 SO PAX DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 581SW 120349 FLT 5440 - MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE. REPLACED BOTH PAX DOOR HINGES IAW EMB 120 MM 52-10-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007110200114 20071102 00114 EU 2007 11 2 MALA070170 1 20071023 A 5210 SKIN SAAB SF340 340B 7860101 EU PAX DOOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 MAIN ENTRY DOOR OUTER SKIN DENT AT 27.5" ABOVE DOOR SKIN LOWER EDGE AND 5.50" AFT OF DOOR FWD EDGE. REPAIR PER IAW EO N R S52089 AND SAAB REPAIR STATEMENT 340SDS012743. 2 L 7 2 4T RT A52EU 2007110200116 20071102 00116 SW 2007 11 2 WGEA200700015 1 20071023 A 7931 35C155103 SENSOR ECLIPS EA500 ECLIPSEEA500 3350000 SW RT ENGINE MALFUNCTIONED E WGEA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 EA 27 131DJ 6 000033 SHUT DOWN RIGHT ENGINE, ACCT LOW OIL PRESSURE WARNING. RIGHT ENGINE OPERATED AT WINDMILL RPM FOR APPROXIMATE 20 MINUTES . RIGHT ENGINE PARAMETERS OTHER THAN OIL PRESSURE WERE NORMAL. REMOVED AND REPLACED RIGHT ENGINE MOP/MOT SENSOR IAW P& WC EMM 79-30-04, AND RIGHT ENGINE ACS WIRING HARNESS IAW P&WC EMM 73-20-02. 1 L 7 2 4J RT A00002AC 2007110200118 20071102 00118 EU 2007 11 2 COEA0729821 1 20070824 A 5420 S57112245200 ANGLE AEROSP ATR72 ATR72202 8680940 EU LT NACELLE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK, LT NACELLE OUTBOARD SKATE ANGLE CORROSION FORWARD AND AFT AREAS ON PREVIOUS BLENDS. REMOVED C ORROSION PER SRAS DO/TS-3852/070-09218, SHEET REF DO/TS 3852/07. (M) 2 H 7 2 4T RT A53EU 2007110200124 20071102 00124 NM 2007 11 2 AMTA200700521 1 20071017 A 5313 LONGERON BOEING 757 75733N 1384931 NM FS 1330 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 550TZ 32584 AFT CARGO PIT LONGERON CORRODED AT STATION 1330 LBL 2.9. REMOVED CORROSION MATERIAL LOSS .024, FOUND TO BE OUT OF LIMIT S. REPAIRED IAW SRM 53-00-53. (M) 2 L 7 2 4F RT A2NM 2007110200125 20071102 00125 SW 2007 11 2 WGEA200700016 1 20071024 A 2731 271125681004 ACTUATOR ECLIPS EA500 ECLIPSEEA500 3350000 SW ZONE 300 INOPERATIVE E WGEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 134DJ 101 000035 ON PREFLIGHT CAS MESSAGE UNCOMMANDED TRIM, ELEVATOR SPLIT TRIM DISPLAYED. REMOVED AND REPLACED RIGHT ELEVATOR PITCH TRI M ACTUATOR. OPS CHECK GOOD IAW EA500 AMM 23-33-15. 1 L 7 2 4J RT A00002AC 2007110200126 20071102 00126 EU 2007 11 2 MALA070165 1 20071023 A 3244 TIRE SAAB SF340 340B 7860101 EU RT MLG MISSING A MALA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 GL 15 426XJ 340B426 CREW NOTED RT OB TIRE WAS MISSING ON POST FLIGHT. REMOVED AND REPLACED RT LOWER MAIN LANDING GEAR SUB ASSEMBLY IAW TASK CARD 3211-301. MLG SUB ASSEMBLY PN OFF/ON: AIR6654/AIR136654, SN OFF/ON: 0512074/LK9601557SA; IB MAIN TIRE PN OFF/ON: 5010488-2, SN OFF/ON: FEB00-3178/MAR98-2526. OB MAIN TIRE PN OFF/ON 5010488-2, SN OFF/ON: JAN97-2059/OCT00-3319. BRAKE ASSEMBLY RT OB PN OFF/ON: 5012589-3, SN OFF/ON: OCT96-0305/JUN94-1170. RT OB ANTI-SKID TRANSDUCER. 2 L 7 2 4T RT A52EU 2007110200127 20071102 00127 EU 2007 11 2 07FDEA04680 1 20071025 A 5311 A57112125 FRAME AIRBUS 310 A310222 3930315 EU WING ROOT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 LT FRAME 47 HOLE 10 SHOWS CRACK INDICATION, FIG 7 SHEET 3 SAYS CONTRACT AIRBUS IF CRACK IS DETECTED. COMPLIED WITH FEDE X EA 6-5710-112976 WINGS AD2006-09-05 WING R/S INTERNAL ANGLE FASTENER HOLES 11 AND 39 RT AND 10 AND 61 LT CRACK REPAIR. REAMED HOLES TO REMOVE CRACK INDICATION. 2 L 7 2 4F RT A35EU 2007110200129 20071102 00129 EU 2007 11 2 COEA0705919 1 20070924 A 5711 SPAR CAP AEROSP ATR42 ATR42300 8680920 EU LT WING CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 919FX 266 FOUND DURING HEAVY CHECK, MAJOR REPAIR, LEVEL 2 CORROSION, CORROSION ON LT WING AFT SPAR UPPER CAP. REMOVED CORROSION A ND DAMAGE BLENDED PER SRAS, DO/TS-4213/07. (M) 2 H 7 2 4T RT A53EU 2007110200131 20071102 00131 2007 11 2 COEA0707911 4 20071009 A 3497 103FN2 WIRE AEROSP ATR42 ATR42300 8680920 EU CONTROL UNIT SHORTED A COEA O OTHER O OTHER CR CRUISE 1 NM 13 911FX 045 WHILE EN ROUTE FROM KTN-SIT, THE NR 2 HEADING BUG AND INDICATOR FAILED. CREW ELECTED TO OVERFLY SIT AND CONTINUE ON TO JUN FOR MAINTENANCE. SECURED LOOSE WIRING, CLEANED AND RE-CLAMPED CONNECTOR ON THE COURSE AND HEADING CONTROL UNIT. (M ) 2 H 7 2 4T RT A53EU 2007110200132 20071102 00132 EU 2007 11 2 07FDEA04681 1 20071025 A 5311 A57112125 FRAME AIRBUS 310 A310222 3930315 EU WING ROOT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 LT FRAME 47 HOLE 61 SHOWS CRACK DAMAGE INDICATION. E6-5710-7-3322 PT1 FIG7 SHEET 3 SAYS CONTACT AIRBUS IF CRACK IS DETEC TED COMPLIED WITH FEDEX EA 6-5710-112976 WINGS AD 2006-09-05 WING R/S INTERNAL ANGLE FASTENER HOLES 11 AND 39 RT 10 AND 61 LT. REAMED HOLES TO REMOVE CRACK INDICATION. 2 L 7 2 4F RT A35EU 2007110200135 20071102 00135 WP 2007 11 2 07FDEA04684 1 20071025 A 5347 AFA7433 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 MAIN CABIN ON SEAT TRACK FOUND DEEP WEAR. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F RT A22WE 2007110200137 20071102 00137 NM 2007 11 2 07FDEA04686 1 20071025 A 2780 40173 SWITCH BOEING 727 727233 138408A NM ZONE 600 FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 270FE 22035 ON FLAP RETRACTION TO 2 DEGREES, NR 2 LE FLAP REMAINS EXTENDED. NORMAL HYDRAULICS. RECYCLED TO 5 DEGREES AND BACK TO 2 DEGREES IAW QRH. NO LUCK. NO ASYMMETRIC CONTROL FORCES NOTED. OBTAINED NORMAL FLAPS 30 LANDING CONFIGURATION. REM OVED AND REPLACED NR 2 LEADING EDGE KRUGER FLAP INDICATING SWITCH PER AMM 27-82-001-4. OPS CHECK OF LEADING EDGE FLAPS REF MM 27-82-001-04. 2 L 7 3 4F RT A3WE 2007110200141 20071102 00141 2007 11 2 SIMA200729907 4 20071019 A 2210 6229968001 DAMPENER CNDAIR CL600 CL6002C10 1390015 EA MALFUNCTIONED A SIMA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CR CRUISE 1 SW 21 502AE 10018 SUBTLE YET NOTICEABLE UNCOMMENTED RIGHT YAW DURING FLIGHT WITH AUTO PILOT ON. AILERONS TRIED TO CORRECT. NO ENGINE TRO UBLE. FELT AS THOUGH RUDDER WAS BEING PRESSED. FLT CONTROL SYNOPTIC PAGE REVEALED NOTHING ABNORMAL. CAUTION DISAPPEAR ED WHEN AUTO PILOT WAS TURNED OFF. YD2 INOP STATUS MSG CAME ON (WHILE TAXIING IN). ISSUED MEL 22-11. REMOVED AND REPL ACED NR 2 YAW DAMPER IAW AMM 27-22-01. OPS CHECK GOOD MEL 22-11 IS RESTORED AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4F RT A21EA 2007110200144 20071102 00144 SO 2007 11 2 SIMA200729701 1 20071022 A 3350 66368 LIGHT EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A SIMA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 729AE 145343 FLOOR PROXIMITY STRIPS INOP, ONE STRIP BETWEEN ROW 9-11. REMOVED AND REPLACED EMERGENCY FLOOR LIGHTS IAW EMB 135 AMM 33 -50-12. OPS CHECK GOOD ACTION RESTORES MEL/CLEARED MIC SHEET. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007110200145 20071102 00145 SO 2007 11 2 SIMA200729908 1 20071023 A 2730 3621001013 CONTROL UNIT EMB 135 EMB135KL 3260302 SO STAB TRIM MALFUNCTIONED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 821AE 145577 AIRCRAFT WAS RETURNING TO FIELD WITH A TRIM PROBLEM CREW REPORTED ON THE GROUND THAT THE MAIN PITCH TRIM WAS INOP FOLLOW ED THE AOM RETURNED TO LAX. REMOVE AND REPLACE HSCU IAW EMB 140 AMM 27-40-01, OPS CHK GOOD. AIRCRAFT RETURN TO SERVIC E. 2 L 7 2 4F RT T00011AT 2007110200147 20071102 00147 EA 2007 11 2 SIMA200729708 1 20071016 A 2150 GG670950093 ACM CNDAIR CL600 CL6002C10 1390015 EA LEFT WARNING MESSAGE A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 523AE 10152 LEFT PACK AUTO CAUTION MESSAGE ON EICAS ALONG WITH SMOKE IN THE COCKPIT. ISSUED MEL 21-12 FOR LT PACK. REMOVED AND REP LACED LEFT AIR CYCLE MACHINE IAW AMM 21-51-08. MEL ITEM RESTORED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007110200151 20071102 00151 NM 2007 11 2 AMTA200700519 1 20071017 A 5313 LONGERON BOEING 757 75733N 1384931 NM BS 1330 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 550TZ 32584 AFT CARGO PIT LOWER BILGE LONGERON CORROSION STATION 1330 RBL 10.43. REMOVED 2 NUTPLATES BLENDED, CORROSION MATERIAL LO SS .020 FOUND TO BE OUT OF LIMITS. REPAIRED IAW 53-00-53, 53-60-53. (M) 2 L 7 2 4F RT A2NM 2007110500003 20071105 00003 NM 2007 11 5 ASMF200710008 1 20071023 A 2420 976J2528 GENERATOR DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE LEFT DAMAGED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 160PL 22904 4074 49763 CAPTAIN REPORTED THAT DURING TAXING, LT GENERATOR WAS OUT OF SERVICE. MAINTENANCE PERSONNEL DEFERRED REPORT IAW MEL 24- 1 CAT B. LATER DURING NEXT TRANSIT CHECK, LT GENERATOR WAS REPLACED IAW MM 24-20-01, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007110500005 20071105 00005 NM 2007 11 5 ASMF200710006 1 20071022 A 3411 PITOT HEAD BOEING 737 73776Q 13845AA NM RIGHT WARNING MESSAGE W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 997AM 30283 AIRCRAFT RETURNED TO PLATFORM, THE RT ELEVATOR PITOT LIGHT TURNED ON. MAINTENANCE PERSONNEL REPLACED THE PITOT PROBE RT ELEVATOR IAW MM 27-31-94 AND TESTED CORRECT IAW MM 27-31-17 AND FIM PROCEDURE 30-31 TASKS 808-809. 2 L 7 2 4F RT A16WE 2007110500006 20071105 00006 NM 2007 11 5 ASMF200710007 1 20071022 A 7500 ENGINE BOEING 737 737* NM CFMINT CFM567 CFM567B22 13802 NE RIGHT LOW PRESSURE W ASMF K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 23 906AM 29356 CAPTAIN REPORTED LT ENGINE WITH LOW PNEUMATIC PRESSURE INDICATION, RT ENGINE 40 PSI AND LT 20 PSI. MAINTENANCE PERSONNEL PERFORMED THE FIM PROCEDURE 36-10, TESTED CORRECT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007110500064 20071105 00064 NM 2007 11 5 ANCF200700027 1 20071030 A 2821 FILTER BOEING 767 767259 1385136 NM PWA 4056 PW4056 NE FUEL SYSTEM CLOGGED W ANCF A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 23 985AN 24618 724201 RT ENGINE FUEL FILTER DISPLAYED ON EICAS MESSAGE IAW AMM 73-11-02 /401 THE FUEL PUMP FILTER WAS REMOVED AND REPLACED AND TEST WITH RUNNING ENGINE SATISFACTORY (FILTER PN 218321). 2 L 7 2 4F 4 F RT A1NM E24NE 2007110500103 20071105 00103 NM 2007 11 5 AMF200710009 1 20071026 A 2410 761574B GENERATOR BOEING 737 737* NM CFMINT CFM567 CFM567B22 13802 NE LEFT DAMAGED W ASMF A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 23 852AM 5859 33787 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, DUE TO DRIVE LIGHT OF LT GENERATOR TURNED ON. CAPTAIN PERFORMED ABNORMAL PROC EDURE BUT APU DID NOT START AT FL 400, IT LANDED. MAINTENANCE PERSONNEL VERIFIED APU GENERAL CONDITION AND STARTED IT CO RRECTLY; REGARDING LT GENERATOR REPORT, IT WAS DEFERRED IAW MEL PROCEDURE 24-1-3. LATER DURING THE NEXT TRANSIT CHECK AT MEX, THE GENERATOR WAS REPLACED IAW MM 24-11-11, TESTED CORRECT. OVERWEIGHT LANDING INSPECTION WAS PERFORMED IAW MM 05 -51-35, NO DAMAGES WERE FOUND. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007110500128 20071105 00128 EU 2007 11 5 USAA920070972 1 20071016 A 5347 D5713014720004 SEAT TRACK AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C-07 CHECK - CORROSION ON CABIN SEAT TRACK, BS 1590 / FR 36 - BS 1810 / FR 41, -Y765. REPLACED CAB IN SEAT TRACK, BS 1590 / FR 36 - BS 1810 / FR 41, -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007110500129 20071105 00129 EU 2007 11 5 USAA920070973 1 20071016 A 5347 D53371112004 SEAT TRACK AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C-7 CHECK - CORROSION ON CABIN SEAT TRACK, BS 1810 / FR 41 - BS 2136 / FR 47, +Y1292. REPLACED CAB IN SEAT TRACK, BS 1810 / FR 41 - BS 2136 / FR 47, +Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007110500133 20071105 00133 EU 2007 11 5 USAA920070977 1 20071024 A 5530 D5537131800200 HINGE FITTING AIRBUS 320 A320232 3930326 EU ZONE 300 WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C-07 CHECK - RUDDER HINGE NR 4 FITTING WORN, VERTICAL STABILIZER STATION 2632 / RIB 6. REPLACED RU DDER HINGE NR 4 FITTING VERTICAL STABILIZER STATION 2632 / RIB 6 IAW A320 AMM 27-21-00 AND 55-36-41. 2 L 7 2 4F RT A28NM 2007103100001 20071031 00001 NM 2007 10 31 SWAA075365 1 20071028 A 3350 10107451 SIGN BOEING 737 7375H4 138449D NM EMERGENCY EXIT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 L1 DOOR EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN PER MM. 2 L 7 2 4F RT A16WE 2007103100002 20071031 00002 NM 2007 10 31 SWAA075377 1 20071028 A 5311 6546554 FRAME BOEING 737 737317 138447P NM BS 847 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007103100010 20071031 00010 NM 2007 10 31 SWAA075315 1 20071025 A 5755 CASTING BOEING 737 7373H4 1384600 NM RT WING SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD GROUND SPOILER OUTBOARD CASTING CRACKED. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007103100013 20071031 00013 NM 2007 10 31 SWAA075403 1 20071026 A 3260 189915 SENSOR BOEING 737 7373H4 1384600 NM NLG FAULTY A SWAA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 29 300SW 22940 EXTENDING LANDING GEAR NOSE GEAR RED LIGHT ILLUMINATED. REMOVED AND REPLACED NLG SENSOR PER MM. 2 L 7 2 4F RT A16WE 2007103100018 20071031 00018 EA 2007 10 31 TRAX200701585 1 20071023 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 741EV 10155 RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. 2 L 7 2 4F RT A21EA 2007103100019 20071031 00019 EU 2007 10 31 YENA2007092 1 20071023 A 3230 7620801 SAFETY VALVE AIRBUS 320 A320232 3930326 EU MLG FAILED A YENA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 603JB 12212 2352 FLT 59, JFK-MCO, ATB TO JFK, ON TAKEOFF LANDING GEAR NOT UPLOCKED INDICATION & ECAM GEAR. GEAR FAILED TO RECYCLE. GEAR INDICATIONS NORMAL IN DOWN LOCKED POSITION. FOUND SAFETY VALVE AT FAULT. REMOVED AND REPLACED SAFETY VALVE IAW 32-31- 00-810-856. ACCOMPLISHED NORMAL ALT GEAR OPERATION IAW 32-31-16-720-050, ALL FOUND NORMAL. A/C OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2007103100022 20071031 00022 WP 2007 10 31 UPS07850981 1 20070914 A 5315 3774605501 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 58 LBL36 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 FLOORBEAM HEAVILY CORRODED AND CRACKED IN A/C COMP'T CEILING, STA 58 LBL 36. REMOVED AND REPLACED FL OORBEAM UPPER FLANGE IAW SRM 51-01-08, 51-01- 20, 51-01-21, AND SAA EA 008-5310-01-A1170. 2 L 7 4 4F RT 4A25 2007103100029 20071031 00029 NM 2007 10 31 UPS07M51024 1 20070829 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C RIGHT HORIZONTAL STABILIZER BARREL NUT HOLE 8R HAS CORROSION IN BORE. CORROSION AT BARREL NUT BORE RE MOVED & BORE BOTTOM SURFACE CLEANED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDS LIMITS. 10X MAGNIFICATION DETAIL VIS UAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID & BOTTOM PERIPHERY RADIUS SMOOTHEN/PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. FAB REP SLEEVE BUSHING & PROTECT. 2 L 7 3 4F RT A22WE 2007103100045 20071031 00045 NM 2007 10 31 KCSA071498 1 20071024 A 5320 STIFFENER BOEING 747 7472B4B 138481B NM BS 371 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 NOSE WHEEL WELL TUNNEL STIFFENER IS CRACKED (.25 INCH) IN LOWER TRIM RADIUS AT STA 371, RBL 10, WL 132. 2 L 7 4 4F RT A20WE 2007103100055 20071031 00055 NM 2007 10 31 HNAA0700248 1 20071023 A 3260 5352011 CONTROLLER DHAV DHC8 DHC8102 2809003 NM MLG NO INDICATION A HNAA O OTHER P NO WARNING INDICATION AP APPROACH 1 EA 07 810EX 32433 17446 308 WHEN LANDING GEAR WAS SELECTED DOWN, NOSE GEAR GREEN DOWN LIGHT DID NOT ILLUMINATE. VERIFIED GEAR DOWN AND LOCKED. CRE W PRESSED ON GEAR ADVISORY LIGHT. LIGHT ILLUMINATED AND WORKED NORMALLY FOR TWO GEAR CYCLES. CREW DID NOT DECLARE AN E MERGENCY. REPOSITIONING FLIGHT ONLY WITH NO PASSENGERS ON BOARD. MAINTENANCE PERFORMED A PSEU SELF TEST AND NOSE GEAR DOWNLOCK CODE WAS INDICATED. REMOVED AND REPLACED LANDING GEAR CONTROLLER. OPS CHECK WAS GOOD ON THREE GEAR SWINGS IAW MAINTENANCE MANUAL PROCEDURES. 2 H 7 2 4T RT A13NM 2007103100058 20071031 00058 NM 2007 10 31 UPS07M50970 1 20070918 A 5313 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM BS 6-100 S1R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C X-RAY C/OUT FOUND CRACK INDICATING AT STA 6-100, STR 1 (1EA) AT RT LONGERON SPLICE AS MARKED. STA 6-1 00 STR 1 RT CRACKED LONGERON SPLICE REMOVED. CRACKED LONGERON TRIMMED OFF & REMOVED. TRIMMED OFF AREA REPROTECTED. HF EC INSP C/OUT ON TRIMMED OFF AREA FOUND NO CRACK. LONGERON & REPAIR SPLICE FAB PER SRM 53-10-00 FIG 1 VOL 1 REV 38. LO NGERON & REPAIR SPLICE FASTENERS PICKED UP. FAB LONGERON & REPAIR SPLICE PROTECTED. 2 L 7 3 4F RT A22WE 2007103100072 20071031 00072 NM 2007 10 31 HNAA0700250 1 20071024 A 3260 864202 SENSOR DHAV DHC8 DHC8102 2809003 NM NR 1 NACELLE MISRIGGED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 943HA 47297 47297 167 LEFT MAIN GEAR DOOR AMBER LIGHT DID NOT EXTINGUISH AFTER GEAR RETRACTION, CYCLED GEAR AND LIGHT ILLUMINATED AGAIN. RETU RNED TO FIELD. FOUND LEFT MAIN GEAR FORWARD DOOR (CODE 07) FAULTED. CLEANED AND ADJUSTED SENSOR PER DASH 8 MAINTENANCE MANUAL. CYCLED GEAR 10 TIMES, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007103100074 20071031 00074 NM 2007 10 31 SWAA075298 1 20071024 A 3260 ES54101538 RELAY BOEING 737 7373G7 1384595 NM MLG FAULTY A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 690SW 23783 AIR TUNBACK, ON CLIMBOUT OF LAS NOSE GEAR UNSAFE LIGHT REMAINDED ON AFTER GEAR RETRACTION. GEAR LIGHT STAYED ON WITH HA NDLE IN OFF POSITION. REMOVED AND REPLACED R374 RELAY PER MM. 2 L 7 2 4F RT A16WE 2007103100084 20071031 00084 EA 2007 10 31 HNAA0700249 1 20071024 A 5610 NP15790213 WINDSHIELD DHAV DHC8 DHC8311 1386006 EA COCKPIT DISTORTED A HNAA O OTHER O OTHER CR CRUISE 1 EA 07 343EN 22258 22258 340 CAPTAINS SIDE WINDOW HEATING ELEMENT BURNT, AND HAS SEVERAL AIR BUBBLES. WHEN HEAT IS SELECTED ON, VIEW THROUGH WINDOW IS DISTORTED. MAINTENENCE INSPECTED SIDE WINDOW AND OK'ED AIRCRAFT FOR FERRY FLIGHT TO SBY. SIDE WINDOW REMOVED AND RE PLACED. OP'S CHECK GOOD. 2 H 7 2 4T RT A13NM 2007103100117 20071031 00117 NM 2007 10 31 KCSA071501 1 20071025 A 3350 LIGHT BOEING 747 7472B4B 138481B NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 713CK 21099 UPPER DECK HAS THREE EMERGENCY LIGHTS INOP ONE ON FWD WALL OF LAV NEXT TO EXIT AND TWO ON AFT SIDE OF OVERHEAD CIRCULAR LIGHT. 2 L 7 4 4F RT A20WE 2007103100121 20071031 00121 NM 2007 10 31 SWAA075247 1 20071023 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 597 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103100124 20071031 00124 NM 2007 10 31 SWAA075235 1 20071023 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 947 S26L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND STRINGER 26L CORRODED AT BS 947. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007103100135 20071031 00135 NM 2007 10 31 SWAA075273 1 20071024 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 500D S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007103100144 20071031 00144 EA 2007 10 31 VNAA0710012 1 20071018 A 3260 895304 PSEU CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE MLG FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 05 719PS 6982 10177 CREW REPORTED A GLD UNSAFE MESSAGE SHORTLY AFTER TAKEOFF. APPROXIMATELY ONE MINUTE AFTER GLD UNSAFE MESSAGE, CREW RECEI VED AN UNSAFE GEAR INDICATION WITH THREE AMBER UP BOXES BLINKING WITH THE HORN. CREW ELECTED TO RETURN TO CLT AND LANDE D WITHOUT INCIDENT. MAINTENANCE INSPECTED AND TROUBLESHOT THE SSCU AND THE PSEU. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007103100152 20071031 00152 NM 2007 10 31 2007UALA03926 1 20070926 A 3350 78941 LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 774UA 26936 THE 12F AFT EEL LIGHT INOPERATIVE. *S/D* RELAMPED AS PER MM 33-51-05 OPS CKD PER SAME, SYS OPERATED NORMALLY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007103100164 20071031 00164 NM 2007 10 31 2007UALA04382 1 20071025 A 2797 CONNECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE TE FLAPS LOOSE A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 665UA 29237 FLAP - SLAT ELEC EICAS MSG DISPLAYED. REPLACED FLAP POSITION TRANSMITTER. SECURED CONNECTOR ON FLAP POSITION TRANSMITT ER 1L ON LEFT WING. OPERATED FLAPS, NO MESSAGES, BITE TEST OF FSEU SHOWED NO FAULTS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007103100167 20071031 00167 EU 2007 10 31 2007UALA04385 1 20071024 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 461UA 1266 EMERGENCY LIGHT WIRING UNDER SEAT 16A PULLED OUT OF CONNECTOR. STRAIGHTENED SOCKET LOCK AND REINSTALLED CONTACTS IN P LUG- OPS CHECK NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007103100169 20071031 00169 NM 2007 10 31 WRLA2007117 1 20071028 A 5347 CARGO TRACK DOUG MD11 MD11F 3023600 NM PWA 4460 PW4460 NE CARGO BAY DAMAGED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 48407 MAIN DECK CARGO SEAT TRACK DAMAGED STA Y=635 X=47.50. REPLACED SEAT TRACK REF SRM 53-70-00 FIG 1 REV 40. 2 L 7 3 4F 4 F RT A22WE E24NE 2007103100171 20071031 00171 NM 2007 10 31 2007UALA04303 1 20071019 A 3350 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 802UA 690 DURING EMERGENCY LIGHT SYSTEM TEST ON PTP PANEL, TEST FAILED FAULTING LEFT AFT ESPU BATTERY. 11-01-07 REPLACED EPSU. 2 L 7 2 4F 4 F RT A28NM E40NE 2007103100172 20071031 00172 SO 2007 10 31 RAIA00710026 1 20071022 A 3350 BULB EMB 145 EMB145 3260210 SO EMERGENCY LIGHT INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 807HK 145119 PRE FLT NR 3525 - IAD - EMERGENCY LIGHT IN DOOR RAIL BURNED OUT. MAINTENANCE RELAMPED LIGHT AND OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007103100187 20071031 00187 NM 2007 10 31 2007UALA04308 1 20071018 A 2612 CGAB140001 SMOKE DETECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CARGO BAY FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 350UA 24301 AFT CARGO COMPARTMENT LOOP 'A' SMOKE DETECTOR INOPERATIVE. SUSPECT DETECTOR FAULTY. REPLACED AFT PIT SMOKE DETECTOR AT POSITION A OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007103100191 20071031 00191 NM 2007 10 31 2007UALA04312 1 20071018 A 2420 CIRCUIT BREAKER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE APU BURNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 787UA 26939 APU GEN IS INOPERATIVE. REPLACED APB CONTACTOR . APU OPS CHECKED GOOD. SUSPECT AUX POWER BREAKER BURNED AND UNABLE TO HOLD SET POSITION. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007110100005 20071101 00005 NE 2007 11 1 SWAA075405 2 20071027 A 7200 CFM567B24G22 ENGINE BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B22 13802 NE NR 2 FAILED A SWAA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SW 29 743SW 29279 877667 AIR TURNBACK/DECLARED EMERGENCY/INFLIGHT SHUTDOWN NR 2 ENGINE FAILED ON CLIMBOUT. REMOVED AND REPLACED NR 2 ENGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007110100006 20071101 00006 NM 2007 11 1 CALA0700609 1 20071025 A 5330 6545774 SKIN BOEING 737 7373T0 1384582 NM BS 727D CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12327 23457 INSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT STA 727D, S23R BELOW EMERGENCY LIGHT. REPAIRED IAW ECRA 5331-01359. 2 L 7 2 4F RT A16WE 2007110100025 20071101 00025 NM 2007 11 1 SWAA075323 1 20071025 A 3350 6556633 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007110100030 20071101 00030 NM 2007 11 1 SWAA075318 1 20071025 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 403WN 29815 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 15 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007110100032 20071101 00032 NM 2007 11 1 SWAA075342 1 20071025 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 727B S5L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007110100052 20071101 00052 NM 2007 11 1 SWAA075386 1 20071028 A 5311 6546529 FRAME BOEING 737 7373A4 1384585 NM BS 440 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110100056 20071101 00056 2007 11 1 SWAA075329 4 20071025 A 2565 65C16820 HOOK BOEING 737 7375H4 138449D NM R1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM. 2 L 7 2 4F RT A16WE 2007110100057 20071101 00057 NM 2007 11 1 SWAA075338 1 20071025 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 727D S5L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007110100069 20071101 00069 NM 2007 11 1 SWAA075383 1 20071028 A 5311 6558280 FRAME BOEING 737 7373A4 1384585 NM BS 360 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110100077 20071101 00077 EA 2007 11 1 VNAA0710013 1 20071019 A 5200 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE COMMS OPEN A VNAA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 GL 05 702PS 10135 CREW REPORTED THE GROUND COMMUNICATION DOOR LEFT OPEN AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT I NCIDENT. MAINTENANCE INSPECTED AND FOUND NO DEFECTS. MAINTENANCE PERFORMED OPS CHECKS AND CLOSED DOOR. AIRCRAFT WAS R ELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007110100079 20071101 00079 EA 2007 11 1 VNAA0710015 1 20071014 A 5710 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT WING DAMAGED A VNAA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 GL 05 220PS 7887 WHILE BEING MARSHALED ON TO GATE E19 DURING TAXI, THE LEFT WING STRUCK A STATIONARY TUG. MAINTENANCE INSPECTED AND FOUN D DAMAGE TO THE LEADING EDGE OF THE LEFT WING. AIRCRAFT WAS FERRIED TO AIR CENTER FOR REPAIR. MAINTENANCE REMOVED AND REPLACED THE LT OUTBOARD LEADING EDGE. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007110100099 20071101 00099 NM 2007 11 1 SWAA075249 1 20071023 A 5311 6546532 FRAME BOEING 737 737317 138447P NM BS 480 S8L/R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110100102 20071101 00102 NM 2007 11 1 2007UALA04388 1 20071025 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 RIGHT OVERWING SLIDE EMERGENCY LIGHT LOWER TWO ASSY INOPERATIVE. RELAMPED. LIGHT OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110100108 20071101 00108 NM 2007 11 1 2007UALA04394 1 20071024 A 2740 STAB SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 WP 29 584UA 26706 PRIOR TO TOUCHDOWN STABILIZER RAN UNCOMMANDED TO FULL UP TO LIMIT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110100110 20071101 00110 EU 2007 11 1 TRAX200701581 1 20071023 A 5343 FLANGE AEROSP ATR72 ATR72 EU RT MLG CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 RIGHT MLG LWR FLANGE ON FWD SURFACE AT FR 27 CORRODED. CORROSION REMOVED IAW SRM 51-21-42 FOUND WITHIN LIMITS OF SRM 51-10-10 MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.002 WITHIN LIMITS AS PER SRM: 51-10-10. 2 H 7 2 4T RT 2007110100119 20071101 00119 NM 2007 11 1 SWAA075368 1 20071028 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110100123 20071101 00123 2007 11 1 2007UALA04327 4 20071019 A 2565 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU DOOR 1L DISLODGED A UALA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 WP 29 371UA 24540 DOOR 1L SLIDE FELL OUT OF CASING. SUSPECT SLIDE IMPROPERLY INSTALLED. REPLACED L1 DOOR SLIDE ASSEMBLY IAW MM-25-61-35. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110100135 20071101 00135 NM 2007 11 1 SWAA075354 1 20071025 A 5311 6545805 FRAME BOEING 737 7375H4 138449D NM BS 277 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER EA. 2 L 7 2 4F RT A16WE 2007110100137 20071101 00137 EU 2007 11 1 TRAX200701559 1 20071022 A 5720 ANGLE AEROSP ATR72 ATR72 EU WING BOX CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 RIGHT WING BOX FR 28A ANGLE CRACKED. 2 H 7 2 4T RT 2007110100143 20071101 00143 EU 2007 11 1 TRAX200701567 1 20071022 A 5740 SHEAR TIE AEROSP ATR72 ATR72 EU LT WING CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 LEFT WING SKIN FLANGE FOR PANEL 522CT CORRODED. BLENDED IAW SRM 57-14-12 FIG 401U/T E/C IAW NTM NO CRACKS FOUND. INSTA LLED SRM 51-25-01 FABRICATION COVER ON W/C 2000-206 MATERIAL THICKNESS: 0.753 MATERIAL REMOVED: 0.009 WITHIN LIMITS AS P ER SRM: 57-14-12 FIG 301. 2 H 7 2 4T RT 2007110100148 20071101 00148 NM 2007 11 1 SWAA075362 1 20071027 A 3350 100031 SIGN BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2007110100150 20071101 00150 NM 2007 11 1 2007UALA04331 1 20071019 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 330UA 24191 FWD CARGO DOOR CUTOUT, AFT FRAME CRACKED ON UPPER INNER RADIUS, ADJACENT TO THE LOWER DOOR STOP FITTING. FABRICATED AND INSTALLED DOUBLER REPAIR ANGLES REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110100152 20071101 00152 NM 2007 11 1 2007UALA04333 1 20071019 A 5230 TEE FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 330UA 24191 AFT CARGO DOOR LOWER INTERNAL TEE FITTING, AFT SIDE IS CRACKED. REPLACED LOWER INTERNAL DOOR TEE FITTING. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110100155 20071101 00155 NM 2007 11 1 2007UALA04336 1 20071021 A 2622 GH3JH EXTINGUISHER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 HALON FIRE EXTINGUSHER STARTED LEAKING IN COCKPIT. SUSPECT FAULTY RELEASE VALVE. REPLACED COCKPIT HALON FIRE EXTINGUISH ER. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110100157 20071101 00157 NM 2007 11 1 SWAA075300 1 20071024 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM BS 468 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 468, BL 0. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2007110100164 20071101 00164 EA 2007 11 1 A6WA200740559 1 20071005 A 2760 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SPOILER FAULTED A A6WA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 31 465AW 8481 7893 INFLIGHT RECEIVED SPOILERON FAULT YELLOW CAUTION MESSAGE AND IB AND OB GROUND SPOILER FAULT STATUS MESSAGES. COMPLIED W ITH QRH (FERRY TO PHL).INTERROGATED SECU NR 1 AND SECU NR 2 FAULT LOG FOUND CODE 13 (SECU 1 MODULE A) REMOVED AND REPL ACED SECU NR 1 IAW 27-61-05. OPS CHECK GOOD IAW 27-61-00. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007110100183 20071101 00183 EA 2007 11 1 S9BA200700022 1 20071016 A 5730 SKIN DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA RT WING CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 19915 12 573 RT WING BOTTOM SKIN CORRODED AT BOTTOM IB WING ROOT STATION 47.5. REMOVED AND REPLACED BOTTOM SKIN IB WING ROOT FROM RI B 2 TO RIB 1 IAW RD6-57-164. 1 H 7 2 3T 4 T RT A9EA E4EA 2007110100190 20071101 00190 CE 2007 11 1 DJFA2007117 1 20071015 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 461LX 748 748 RK368 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER INBOARD RIB AND BRACKET ASSEMBLIES, BOTH THE RIGHT AND LEFT INBOARD ROLLER BRACKETS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN BEECHJET COMMUNIQUE' NUMBER 70. MAINTENANCE REPLACED BOTH RIB ASSE MBLIES WITH THE IMPROVED ASSEMBLIES. 2 H 7 2 4F RT A16SW 2007110100195 20071101 00195 CE 2007 11 1 AMWA88093BC 1 20071018 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MASTER DISCHARGED A AMWA O OTHER J WARNING INDICATION CL CLIMB 1 CE 07 146ZV 13965 23 UE146 BATTERY CHARGE ANNUNCIATOR ILLUMINATED AFTER TAKEOFF. BATTERY WAS REPLACED AND DISCREPANCY WAS CLEARED. THIS TYPE ANNUNC IATOR DISCREPANCY IS CONSIDERED A NUISANCE ITEM AND DISTRACTION TO CREW. 2 L 7 2 4T 3 T RT A24CE E2NE 2007110200001 20071102 00001 SW 2007 11 2 N9V2007F00000 1 20071005 A 6510 SKCP2348101 DRIVE SHAFT BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL TAIL ROTOR BROKEN D N9VA A UNSCHED LANDING E VIBRATION/BUFFET NR NOT REPORTED 1 SO 03 2HV 1808 2560 PILOT MADE EASY RT TURN. FELT AN INCREASE IN VIBRATION. HE MADE A PRECAUTIONARY LANDING AT THE NEAREST AIRPORT. FOUND THAT A FLEX FRAME HAD BROKEN ON THE MOST FORWARD END OF THE DRIVESHAFT THROUGH THE BOLT HOLE. THE DRIVESHAFT HAD A JUM P ROPE EFFECT WHEN TURNED. ALL THE TORQUE SEALS WERE STILL IN TACK. INSTALLED NEW DRIVESHAFT AND VIBREX 200 PLUS. THE MAIN ROTOR WAS BALANCED AT .41 IPS VERTICAL AND .07 IPS LATERAL. INSPECTED ALL THE TRANSMISSION AND ENGINE MOUNTS AND SURROUNDING AREAS. NOTHING NOTED. LIFTED THE TRANSMISSION TO SEE IF THE ISOLATION MOUNT COULD BE FAULTY BUT WAS NOT. FOUND THE PYLON SUPPORT LINKS FOR THE TRANSMISSION WITH WEIGHT OFF THEM WERE LOOSE. INSPECTED AND RETORQUED ALL THE SUP 1 G 7 1 3U 3 U H2SW E4CE 2007110200084 20071102 00084 NM 2007 11 2 QXEA200701621 1 20071022 A 5100 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA ENGINE MULTIPLE FAIL A QXEA E ENGINE SHUTDOWN G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 NM 09 406QX 12639 900 4048 PECFA0060 PSC FLIGHT NR 2268: DURING FLIGHT HAD NR 1 ENGINE OIL FAILED (DASH LINE NOT 0) THEN NR 1 ENGINE FADEC FAIL. SHUT ENGINE DOWN. ALSO HAD A NR 1 PEC CAUTION LIGHT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW MTC'S 6710003 AND 67100 04. ALSO, REMOVED AND REPLACED NR 1 PROP (P/N 697070003, S/N DAP0042), NR 1 AC GEN (P/N 28B555-1, S/N 108C-0136) AND NR 1 OIL COOLER (P/N D2887-815A, S/N 03040252) FOR OIL CONTAMINATION. ALL OPS AND LEAKS CHECKS WERE GOOD. AIRCRAFT WAS R ETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2007110200088 20071102 00088 NM 2007 11 2 QXEA200701618 1 20071024 A 2910 LINE DHAV DHC8 DHC8202 2809007 NM HYD SYSTEM LEAKING A QXEA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 352PH 494 LMT FLIGHT NR 2035, ON TAXI IN BODY ODOR TYPE ODOR NOTED BY BOTH FLIGHT CREW. BOTH BLEEDS WERE SHUTOFF, SMELL CONTINUED AFTER PARKING, HAZE WAS VISIBLE IN COCKPIT. FIRST OFFICER OBSERVED SMOKE COMING FROM BELOW RIGHT FMS AREA. STRONG ODO R OF POSSIBLY BURNT PLASTIC OR ELECTRICAL. FLIGHT ATTENDANT SAYS CABIN HAD NO SMOKE OR ODOR. ALL POWER WAS SHUT OFF. SMOKE STOPPED ACCUMULATING. INVESTIGATION FOUND TO BE HYDRAULIC LEAK CAUSING MIST UNDER COCKPIT FLOOR. REPAIRED HYDRAU LIC TUBE, NLG DOWN PRESSURE LINE USING RIGHT-LOK PERMANENT FITTINGS AND SPLICE TUBE IAW AMM 20-50-55-3660-801. BLED LIN E AND PRESSURE CHECKED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007110200098 20071102 00098 SO 2007 11 2 SIMA200729905 1 20071024 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 622AE 145108 EN ROUTE TO CRP FLIGHT ATTENDANT NOTICED BURNING ODOR IN CABIN. FLIGHT DIVERTED TO AUS. LANDED UNEVENTFULLY. EMERGENC Y WAS DECLARED. DID NOT LAND OVERWEIGHT. PERFORMED OPS CHECK OF A/C COOLING SYSTEM IAW AMM 21-20-00 RAN BOTH PACKS ON APU BLEED FOR 1 HR OPS CHECK WERE GOOD NO SMOKE IN COCKPIT OR CABIN. RAN BOTH PACKS FOR 1HR ON ENG BLEEDS AGAIN COULD N OT DUPLICATE SMOKE PROBLEM. CHECKED BOTH ENG FOR LEAKS NO INTERNAL OR EXTERNAL LEAKS NOTED AT THIS TIME. REMOVED FLOOR BOARDS IN CABIN INCEPTED AC DUCTS NO DEFECTS FOUND. FUNCTIONAL CHECK FLIGHT PASSED SATISFACTORY AIRCRAFT RETURN TO SER VICE. 2 L 7 2 4T RT T00011AT 2007110200104 20071102 00104 SO 2007 11 2 SIMA200729914 1 20071018 A 5320 14525480603 SILL EMB 145 EMB145 3260210 SO CARGO DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 20383 5000 145079 DURING A MBV INSPECTION, THE CARGO DOOR CUT OUT LOWER SILL WAS FOUND TO BE CORRODED. REMOVED THE SILL AND REPLACED WITH A NEW SILL PN 145-25480-603 IAW EMBRAER SRM CHAPTERS 51-20-01, 51-20-03, 51-40-02,51-40-06, 51-40-09 AND EMBRAER CPM CH APTERS 51-21-04, 51-21-05 AND 51-21-06. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007110200115 20071102 00115 EU 2007 11 2 MALA070172 1 20071023 A 5320 DOUBLER SAAB SF340 340B 7860101 EU BS 252-275 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 DURING THE N4K CHECK, THE PASSENGER DOOR CUT-OUT REINFORCEMENT DOUBLER WAS FOUND SEVERELY CORRODED FROM FS 252-275, SL15 22 TO JUST BELOW SL1523. THE DISCREPANCY WAS TRANSFERRED TO MM01 PG. 1688720. AIRCRAFT FERRIED TO VENDOR FOR REPAIR IA W SAAB REPAIR STATEMENT 340SDS013342. 2 L 7 2 4T RT A52EU 2007110200117 20071102 00117 EU 2007 11 2 COEA0731821 1 20070822 A 5751 HINGE FITTING AEROSP ATR72 ATR72202 8680940 EU R AILERON CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY C-CHECK, LEVEL 2 CORROSION, CORROSION ON RT AILERON OUTBOARD HINGE FITTING ON LOWER SPAR FLANGE. REM OVED AND REPLACED FITTING. (M) 2 H 7 2 4T RT A53EU 2007110200149 20071102 00149 EA 2007 11 2 CHQA200700067 1 20071030 A 2750 865D1007 DRIVE UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS BINDING A CHQA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 11 639BR 34444 34444 7313 GEE872507 AMA TO IAH - ON DOWNWIND FOR LANDING IN IAH, THE AIRCRAFT WAS SLOWED TO 180 KNOTS AND 8 DEGREES OF FLAPS WERE ADDED. WH EN THE AIRCRAFT TURNED ONTO THE BASE LEG, THE FLAP LEVER WAS SET TO 20 DEGREES AND A FLAP FAIL MESSAGE APPEARED ON EICAS . THE QRH WAS FOLLOWED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS TAXIED TO THE GATE AND TURNED OVER T O MAINTENANCE. MAINTENANCE CHECKED THE FLAP ELECTRONIC CONTROL UNIT FOR FAULT CODES AND FOUND CODES POINTING TO THE FLA P POWER DRIVE UNIT. THE PDU WAS FOUND TO BE BINDING INTERNALLY AND WAS REPLACED. THE FLAPS WERE THEN RIGGED AND THE FL AP SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2007110500130 20071105 00130 EU 2007 11 5 USAA920070974 1 20071019 A 5315 D53472090000 FLOORBEAM AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3101 / FR 65 - BS 3207 / FR 67, +Y1292. REPLACED CABI N FLOORBEAM, BS 3101 / FR 65 - BS 3207 / FR 67, +Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007110500135 20071105 00135 EU 2007 11 5 USAA920070979 1 20071015 A 5315 D53472189204 FLOORBEAM AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3257 / FR 68 - BS 3366 / FR 70, -Y1162. REPLACED CAB IN FLOORBEAM, BS 3257 / FR 68 - BS 3366 / FR 70, -Y1162 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007110500136 20071105 00136 EU 2007 11 5 USAA920070980 1 20071019 A 5320 D53472090011 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 - FUSEL CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3043 / FR 64 - BS 3158 / FR 66, -Y1292. REPLACED CAB IN FLOORBEAM, BS 3043 / FR 64 - BS 3158 / FR 66, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007110500137 20071105 00137 EU 2007 11 5 USAA920070981 1 20071015 A 5320 D53472172204 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3158 / FR 66, +Y1292. REPLACED CABIN FLOORBEAM, BS 31 58 / FR 66 - BS 3257 / FR 68, +Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007110500138 20071105 00138 NM 2007 11 5 USAA920070982 1 20071024 A 5320 146N5180 STRAP BOEING 757 7572B7 1384964 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - CRACKED CABIN FLOOR STABILIZATION STRAP, BS 1661, LBL 24.75, WL 204. REPAIRED CABIN FLO OR STABILIZATION STRAP, BS 1661, LBL 24.75, WL 204 IAW USAIRWAYS TR 53-.35-01. 2 L 7 2 4F RT A2NM 2007110500139 20071105 00139 NM 2007 11 5 USAA920070983 1 20071024 A 5320 146N518023 STRAP BOEING 757 7572B7 1384964 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - CRACKED CABIN FLOOR STABILIZATION STRAP, BS 1681, RBL 24.75, WL 204. REPAIRED CABIN FLO OR STABILIZATION STRAP, BS 1681, RBL 24.75, WL 204 IAW USAIRWAYS TR 53-.35-01. 2 L 7 2 4F RT A2NM 2007110500142 20071105 00142 NM 2007 11 5 UPS07551006 1 20071025 A 2720 TRIM SYSTEM BOEING 757 75724APF 1384969 NM RUDDER LOCKED A IPXA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 SO 01 475UP 28845 INSPECTION TYPE:N/A ATB - RUDDER TRIM LOCKED UP. REPLACED TRIM CONTROL PANEL, OPS NORMAL. REF AMM 27-21-23-2 & AMM 27- 21-00-5. 2 L 7 2 4F RT A2NM 2007110500143 20071105 00143 2007 11 5 UPS07650990 2 20071024 A 7300 ECU BOEING 767 76734AF 1385212 NM LT ENGINE INOPERATIVE A IPXA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 SO 01 304UP 27242 INSPECTION TYPE:ETOP PILOT REPORTED IDLE DISAGREE & LT ENG W/NOT RESPOND TO THROTTLE INPUT DURING TURBULENCE. TAT=32,22 0 TAC=10,447 TEC=8138 TET=27155 TSR=14222. *SUPPLEMENTAL ETOPS* REPLACED LEFT ENGINE ECU IAW 73-21-15-4. SYSTEM O PS CHECK NORMAL. OK TO CONTINUE. 2 L 7 2 4F RT A1NM 2007110500145 20071105 00145 NM 2007 11 5 UPS07651010 1 20071024 A 5347 SEAT TRACK BOEING 767 76734AF 1385212 NM COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 307UP 27760 INSPECTION TYPE:SEG2 F/O'S SEAT TRACK HAVE CORROSION. REPLACED SEAT TRACK PER SRM. 2 L 7 2 4F RT A1NM 2007110500148 20071105 00148 WP 2007 11 5 UPS07850992 1 20070920 A 5340 FITTING DOUG DC8 DC873F 302199F WP FS 1120 L19R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 FITTING CRACKED AT STA 1120 L19R AFT SIDE. REMOVED, FABRICATED AND INSTALLED REPAIR FITTING AT STA 1 120 L19R IAW SRM 51-1-21, AND SRM 51-03-02. 2 L 7 4 4F RT 4A25 2007110500149 20071105 00149 NM 2007 11 5 UPS07M50997 1 20070921 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 2007 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C MAIN DECK: ALONG BS 2007, ALONG -X=107 (RBL 107), RT MOST O/B SEAT TRACK TOP SURFACE BODY AREAS FOUND CORRODED. AFTER CORROSION REMOVAL ON A/M AREAS C/OUT FOUND LIMIT EXCEEDED PER SRM 53-70-00D, F3, V1, R35. CORRODED SE AT TRACK AT STA 1831, RBL 107 TRIMMED OFF PER SRM 53-70-00D, F1, V1, R35. NEW CURVED SEAT TRACK & REPAIR & RWK C/OUT PE R SRM 53-70-00D, F1, V1, R35. NEW CURVED SEAT TRACK FROM STA 1831-2007 RBL 107 INSTALLED PER SRM 51-31-01 & 51-33-01, V 2, R35. FOUND SATIS. 2 L 7 3 4F RT A22WE 2007110500150 20071105 00150 NM 2007 11 5 USAA920070995 1 20071025 A 5330 6545774 SKIN BOEING 737 737401 1384701 NM BS 752-755 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 CLT - MAJOR REPAIR - CRACKED FUSELAGE SKIN, BS 752.5 - BS 755, S25L. REPAIRED FUSELAGE SKIN, BS 752.5 - BS 755, S25L IA W B737 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2007110500154 20071105 00154 NM 2007 11 5 USAA920070999 1 20071023 A 5313 654500124 STRINGER BOEING 737 7373G7 1384595 NM BS 324 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, CORROSION AND CRACK ON STRINGER, BS 324, BL 0. REPLACED STRINGER, BS 324, BL 0 IAW B737 -300 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007110500155 20071105 00155 NM 2007 11 5 USAA920071000 1 20071014 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 827 S8-9L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, CRACKED FRAME, BS 827, S8L - S9L. REPAIRED FRAME, BS 827, S8L - S9L IAW USAIRWAYS EA 98 915 AND TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2007110500156 20071105 00156 NM 2007 11 5 USAA920071001 1 20071018 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 360 S7-11L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, CRACKED FRAME, BS 360, S7L - S11L. REPAIRED FRAME, BS 360, S7L - S11L IAW USAIRWAYS EA 98915 AND TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2007110500157 20071105 00157 NM 2007 11 5 USAA920071002 1 20071026 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 787 S8-9R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, CRACKED FRAME, BS 787, S8R - S9R. REPAIRED FRAME, BS 787, S8R - S9R IAW USAIRWAYS EA 98 915 AND TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2007110500158 20071105 00158 NM 2007 11 5 USAA920071003 1 20071026 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 887 S8-9R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, CRACKED FRAME, BS 887, S8R - S9R. REPAIRED FRAME, BS 887, S8R - S9R IAW USAIRWAYS EA 98 915 AND TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2007110500159 20071105 00159 NM 2007 11 5 USAA920071004 1 20071026 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 807 S8-9R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, CRACKED FRAME, BS 807, S8R - S9R. REPAIRED FRAME, BS 807, S8R - S9R IAW USAIRWAYS EA 98 915 AND TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2007110500160 20071105 00160 NM 2007 11 5 USAA920071005 1 20071022 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 360 S13R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, CRACKED FRAME, BS 360, S13R. REPAIRED FRAME, BS 360, S13R IAW USAIRWAYS EA 98944, EA 98 948 AND TYPICAL REPAIR 53-10-01. 2 L 7 2 4F RT A16WE 2007110500164 20071105 00164 NM 2007 11 5 USAA920071009 1 20071022 A 5210 507945178 STOP FITTING BOEING 737 7373G7 1384595 NM ZONE 800 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, FORWARD ENTRY DOOR STOP FITTING CRACKED, BS 328, 4TH ONE FROM THE BOTTOM. REPAIRED FORW ARD ENTRY DOOR STOP FITTING, BS 328, 4TH ONE FROM THE BOTTOM IAW B737-300 SRM 51-70-11. 2 L 7 2 4F RT A16WE 2007110500167 20071105 00167 2007 11 5 WRNA200700058 4 20071023 A 3414 LINE AIRBUS 300 A300B4203 3930306 EU PITOT/STATIC OBSTRUCTED A WRNA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 SO 05 510TA 100 DURING TAKEOFF ROLL, FIRST OFFICERS AIR SPEED LAGGED BEHIND CAPTAINS BY 40-60 KNOTS, ABORTED TAKEOFF. FLUSHED DEBRIS FR OM PITOT PRESSURE LINES, ACCOMPLISHED PITOT/STATIC TEST IAW 34-11-10 PAGE 501. TEST NORMAL. AIRCRAFT RELEASED FOR SERV ICE. 2 L 7 2 4F RT A35EU 2007110500168 20071105 00168 NM 2007 11 5 HNAA0700251 1 20071025 A 3060 7826891 BRUSH BLOCK DHAV DHC8 DHC8102 2809003 NM PROP HEAT UNKNOWN A HNAA O OTHER O OTHER CR CRUISE 1 EA 07 810EX 10307 642 308 EMERGENCY LIGHTS ILLUMINATED IN FLIGHT. THERE IS A LOT OF HISTORY WITH THE EMERGENCY LIGHTS. THE EMERGENCY CONTROL PAN EL HAS BEEN CHANGED TWICE. THE EMERGENCY BATTERIES CHANGED ONCE ALONG WITH THE RIGHT HAND BRUSH BLOCK. THE CAPTAIN REP ORTED THAT THE PROP HEAT WAS ON. MAINTENANCE WILL REPLACE THE LT BRUSH BLOCK. REMOVED AND REPLACED THE RIGHT HAND BRUS H BLOCK FOR TROUBLESHOOTING IAW 61-10-11, PROP HEAT OPS CHECK WAS GOOD. CHECKED EMERGENCY LIGHTS IAW 33-51-00, OPS CHEC K GOOD. 2 H 7 2 4T RT A13NM 2007110500169 20071105 00169 EA 2007 11 5 HNAA0700253 1 20071027 A 3350 6013211 BATTERY PACK DHAV DHC8 DHC8311 1386006 EA EMERGENCY LIGHTS INOPERATIVE A HNAA O OTHER P NO WARNING INDICATION TX TAXI/GRND HDL 1 EA 07 337EN 32429 679 284 TWO ADJACENT FLOOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. THE BATTERY PACKS WERE SLAVED IN FOR PS1 AND PS2 IN T HE COAT CLOSET. THIS DID NOT FIX THE PROBLEM. SO THE ORIGINALS BATTERY PACKS WERE REINSTALLED. NEXT THE PS2 BASE WAS SLAVED IN AND THAT DID NOT FIX THE PROBLEM EITHER. THE ORIGINAL BASE WAS REINSTALLED. THE EMERGENCY BATTERY POWER SUPP LY 3352-PS2 AT ROW 3D WAS REMOVED AND REPLACED. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007110500171 20071105 00171 NM 2007 11 5 HNAA0700252 1 20071025 A 2120 UNKNOWN DHAV DHC8 DHC8102 2809003 NM COCKPIT ODOR A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 336EN 336 THE PILOT REPORTED A STRONG ELECTRICAL ODOR ON FLIGHT DECK. THE FLIGHT COMPARTMENT AND DC CONTACTOR BAY WERE INSPECTED FOR DAMAGE NONE FOUND. THERE WAS NO ELECTRICAL ODOR NOTED. STARTED THE ENGINES AND RAN ALL SYSTEMS. NO DEFECTS WERE F OUND AND NO CIRCUIT BREAKERS WERE POPPED. NO ODOR NOTED, OK FOR SERVICE. 2 H 7 2 4T RT A13NM 2007110500172 20071105 00172 NM 2007 11 5 HNAA0700255 1 20071026 A 3231 DOOR DHAV DHC8 DHC8102 2809003 NM MLG DOOR OUT OF RIG A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 805EX 228 AFTER TAKEOFF DURING THE GEAR RETRACTION THE LT AMBER GEAR DOOR LIGHT ILLUMINATED. ALSO THE LEFT AFT GEAR DOOR STAYED O PEN. THE CREW DID NOT DECLARE AN EMERGENCY. CYCLED GEAR AND THE LIGHT WENT OUT. FOUND FORWARD MAIN LANDING GEAR DOOR OUT OF ADJUSTMENT ON AFT END. RIGGED THE FORWARD MAIN LANDING GEAR DOOR IAW DASH 8 MAINTENANCE MANUAL 32-10-36, OPS CHE CK GOOD. 2 H 7 2 4T RT A13NM 2007110500176 20071105 00176 EU 2007 11 5 UPS07151059 1 20071026 A 2150 A/C PACK AIRBUS A300 A300F4622R 3930360 EU ODOR A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 168UP 0005 BAD ODOR IN COCKPIT/CABIN AREA WHEN FIRST TURNING ON PACKS. ODOR DOES NOT GO AWAY. OPERATED PACKS FOR 30 MINUTES, NO O DOR DETECTED. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2007110500178 20071105 00178 NM 2007 11 5 UPS07551052 1 20071018 A 5311 143N1024138 FRAME BOEING 757 75724APF 1384969 NM BS 660 S23-24R DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 450UP 25472 INSPECTION TYPE:C DENT IN FWD CARGO COMPARTMENT FUSELAGE FRAME FRAME STA 660, S23R AND S24R. ACCOMPLISHED REPAIR PER F INAL EA 757-5330-27A-1755 AND UPS EO B757-5310-27937-A. 2 L 7 2 4F RT A2NM 2007110500179 20071105 00179 NM 2007 11 5 UPS07551053 1 20071013 A 5311 143N1024138 FRAME BOEING 757 75724APF 1384969 NM BS 660 S24-25R DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 450UP 25472 INSPECTION TYPE:C DENT IN FWD CARGO COMPARTMENT FUSELAGE FRAME STA 660, S24R AND S25R. ACCOMPLISHED REPAIR ON FINAL EA 757-5330-27-A1755 AND UPS EO B757-5310-27937A. 2 L 7 2 4F RT A2NM 2007110500183 20071105 00183 NM 2007 11 5 UPS07M51031 1 20070903 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C EMP - RT HORIZ STAB NR 6 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL BORE REMOVED, BORE REAM & REMAINING BLEND OUT EXCEEDS LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE REPAIR SLEE VE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APPL. 2 L 7 3 4F RT A22WE 2007110500185 20071105 00185 NM 2007 11 5 UPS07M51033 1 20070905 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C EMP - LT HORZ STAB NR 31 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDS LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP. REPAIR SLEEVE BUSHI NG FAB & PROTECTED. PR 1422 B1/2 SEALANT APPLIED AT BLEND OUT. 2 L 7 3 4F RT A22WE 2007110500187 20071105 00187 NM 2007 11 5 UPS07M51035 1 20070907 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C EMP - LT HORZ STAB NR 20 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDS LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP. 2 L 7 3 4F RT A22WE 2007110500188 20071105 00188 NM 2007 11 5 UPS07M51036 1 20070907 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C EMP - RT HORZ STAB NR 18 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDS LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP. 2 L 7 3 4F RT A22WE 2007110500191 20071105 00191 NM 2007 11 5 UPS07M51039 1 20070916 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C EMPENNAGE RT HORIZONTAL STABILIZER BARREL NUT NR 19 FOUND BORE WITH CORROSION. CORROSION AT BARREL NU T BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDS LIMIT. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND N O CORROSION. BARREL NUT BORE BLEND OUT VOID & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP A T BARREL NUT BORE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP. 2 L 7 3 4F RT A22WE 2007110500193 20071105 00193 NM 2007 11 5 UPS07M51041 1 20070917 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C EMP - RT HORZ STAB NR 28 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT EXCEEDS LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT B ORE BLEND OUT VOID & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE REPAIR S LEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APPLIED. 2 L 7 3 4F RT A22WE 2007110500195 20071105 00195 NM 2007 11 5 UPS07M51043 1 20070725 A 5754 SKIN DOUG MD11 MD11F 3023600 NM NR 5 SLAT DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C RIGHT NR 5 SLAT L/E 6 DENTS IN A ROW. RIGHT WING NR 5 SLAT L/E DENTS MEASURED FOUND OUT OF LIMIT. DA MAGE AREA TRIM OFF AS PER EN1663-07. HFEC INSP C/OUT ON TRIM OFF AREA FOUND NO CRACK. REPAIR PARTS FAB PER SRM 57-10-0 0 FIG 5 VOL I REV 38 & EN1663-07. REPAIR PARTS HOLES PICKED UP, PROTECTED & PAINTED. RIGHT NR 5 SLAT REPAIR PARTS INST ALLED AS PER EN1663-07. 2 L 7 3 4F RT A22WE 2007110500196 20071105 00196 NM 2007 11 5 UPS07M51044 1 20070814 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1921 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C CABIN - LT STA 1921, Y=107.25 SEAT TRACK FOUND CORROSION AS MARKED. CABIN LT STA 1921 Y=107.25 CORROS ION ON SEAT TRACK REMOVED FOUND EXCEED LIMIT. CORRODED SEAT TRACK TRIMMED OFF AT STA 1831 & PROTECTED. HFEC INSP C/OUT ON TRIMMED OFF AREA FOUND NO CRACK. SEAT TRACK SPLICE & SPLICE PLATE FAB PER SRM 53-70-00 FIG 1A VOLI REV38. FAB PART S FASTENER HOLES PICK UP, PROTECTED & PAINTED. NEW SEAT TRACK FASTENER HOLES. 2 L 7 3 4F RT A22WE 2007110500197 20071105 00197 NM 2007 11 5 UPS07M51045 1 20070830 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C EMP - LT HORZ STAB NR 12 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED. BORE REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BAR REL NUT BORE BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BOR E. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP. 2 L 7 3 4F RT A22WE 2007110500198 20071105 00198 NM 2007 11 5 UPS07M51046 1 20070830 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C EMP - RIGHT HORZ STAB NR 17 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BO RE REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. B ARREL NUT BORE REAM FURTHER PER EN1574-07. BARREL NUT BORE B/OUT VOIDS, BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED C/ OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING. 2 L 7 3 4F RT A22WE 2007110500202 20071105 00202 NM 2007 11 5 UPS07M51055 1 20070808 A 5710 DOUBLER DOUG MD11 MD11F 3023600 NM RWS 548 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C RIGHT WING: L/E COMPARTMENT AT STA XORS 548 APPROX FOUND UPPER DOUBLER CRACKED AS MARKED. REPAIR ANG LE FAB PER EN 1538-07 & SRM 57-10-00 FIG 28 R.TR 57-5. CRACKED AREA AT RT WING L/E COMPARTMENT AT STA XORS 548 TRIMMED OUT PER EN 15 38-07. HFEC INSP C/O ON TRIMMED OUT FOUND NO CRACK EVIDENT. REPAIR FAB PER EN 1538-07 AND INSTALLED AS P ER SRM 51-31-01 VOL II AND EN 153-8-07. 2 L 7 3 4F RT A22WE 2007110500203 20071105 00203 WP 2007 11 5 MWEA070263 1 20071028 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 810ME 48072 FLOOR TRACK EMERGENCY LIGHT INOPERATIVE FROM ROW 27 AFT. FOUND SPLICE BROKEN REPLACED SPLICE. 2 L 7 2 4F A6WE 2007110500207 20071105 00207 NM 2007 11 5 CALA0700614 1 20071026 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM BS 747 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11612 27325 INSPECTION FOUND A .5 INCH CRACK AT FORWARD FASTENER HOLE OF FRAME AT STA 747 BETWEEN STRINGERS 8L AND 9L. THE FRAME WA S REPAIRED IAW ECRA 5310-04668. 2 L 7 2 4F RT A16WE 2007110500208 20071105 00208 NM 2007 11 5 CALA0700615 1 20071026 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM BS 787 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11612 27325 INSPECTION FOUND A .5 INCH CRACK AT FORWARD FASTENER HOLE OF FRAME AT STA 787 BETWEEN STRINGERS 8R AND 9R. THE FRAME WA S REPAIRED IAW ECRA 5310-04668. 2 L 7 2 4F RT A16WE 2007103100035 20071031 00035 WP 2007 10 31 ASAA0782136 1 20071022 A 5321 SMO953001531 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 1097-1117 PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 968AS 53016 CABIN FLOOR PANEL STA 1097 TO STA 1117 LBL 22 TO RBL 22 PUNCTURED. FABRICATED AND INSTALLED A REPLACEMENT CABIN FLOOR P ANEL IAW MD80 SRM 53-05 PAR 59 AND DAC DRAWING S4932106. 2 L 7 2 4F RT A6WE 2007103100044 20071031 00044 2007 10 31 ASAA0752153 2 20071023 A 7321 2042M67P02 EEC BOEING 737 737890 1384527 NM NR 2 ENGINE MALFUNCTIONED A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 577AS 35186 FOUND FAULT CODE 73 30312 ON NR 2 ENGINE START. SWITCH SIGNAL AND ARINC BUSS DATA DISAGREE. COMPLETED FIM 73 24 STEP E (1) THROUGH L. NO FAULTS SHOWING AT THIS TIME. REPLACED NR 2 ENGINE EEC. REF MM 73 21 60 & MM SUPP 73 21 60. COMPLE TED FIM 73 24 TASK 813. REPAIR CONFIRMED. 2 L 7 2 4F RT A16WE 2007103100047 20071031 00047 NM 2007 10 31 SWAA075295 1 20071024 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 727D S6R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103100052 20071031 00052 2007 10 31 SWAA075275 4 20071024 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007103100053 20071031 00053 WP 2007 10 31 VGCA200700001 1 20071023 A 5740 KF580530500021 ATTACH FITTING CVAC 340 340CVAC 242270A WP LT WING CRACKED A VGCA K NONE O OTHER IN INSP/MAINT 1 GL 23 391FL 9190 9190 278 DURING VISUAL INSPECTION OF WING ATTACH FITTING FOUND CRACKS BETWEEN RIVET HOLES UPPER FWD PORTION OF FITTING (LT AFT WI NG TO FUSELAGE ATTACH FITTING). 2 L 7 2 4R 6A6 2007103100061 20071031 00061 NM 2007 10 31 UPS07M50973 1 20070919 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM BS 6-100 S6R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C CRACK INDICATION FOUND APPROX 0.3 INCH IN LENGTH DURING HFEC INSPECTION AT STA 6-100 FWD SECTION LONGE RON EDGE OF STR 6R AS MARKED. STA 6-100 FWD SECTION LONGERON ATTACHED SPLICE REMOVED. CRACKED LONGERON TRIMMED OFF AT STA 6-80 & REMOVED. TRIMMED OFF AREA REPROTECTED. HFEC INSP C/OUT ON TRIMMED OFF AREA FOUND NO CRACK. LONGERON & REPA IR SPLICE FAB PER SRM 53-10-00 FIG 1 VOL I REV 38. NEW FAB LONGERON & REPAIR SPLICE FASTENER HOLES PICKED UP, PROTECTED , PAINTED & INSTALLED. 2 L 7 3 4F RT A22WE 2007103100062 20071031 00062 NM 2007 10 31 UPS07M50984 1 20070810 A 2810 TANK DOUG MD11 MD11F 3023600 NM BS 1210 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C CTR CABIN - UNDER FLOOR AREA FUEL TANK TOP SURFACE AT STA 1210, -X103 01EA CORROSION FOUND NEAR FASTEN ER. CTR CABIN UNDER FLOOR AREA FUEL TANK TOP SURFACE AT STA 1210 -X103 FUEL TANK SCREW AS MARK REMOVED FOR S/M ACCESS. CORROSION ON FUEL TANK TOP SURFACE REMOVED FOUND EXCEEDED LIMIT. FPI & HFEC OPEN HOLE INSP C/OUT ON REWORKED AREA FOU ND NO CRACK & NO CORROSION. FLAP PEENING C/ OUT ON REWORKED AREA PER EN1642-07. REWORKED AREA REPROTECTED, PAINT. 2 L 7 3 4F RT A22WE 2007103100065 20071031 00065 EA 2007 10 31 TRAX200701552 1 20071021 A 2701 YOKE CNDAIR CL600 CL6002B19 1900309 EA BINDING A ASOA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SO 27 936EV 8038 FELT A POP AND BINDING WHEN TURNING YOKE TO THE LEFT. EXCESSIVE FORCE OR STRENGTH NEEDED TO TURN YOKE LEFT ALSO. A/C R ETURNED TO DAY AFTER T/O. EMERGENCY DECLARED. FLT 4434 DEL 61 MINS. NC FLT 4434 CX. 2 L 7 2 4F RT A21EA 2007103100068 20071031 00068 EU 2007 10 31 2007UALA04361 2 20071019 A 7200 FAN BLADE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU ENGINE LACK OF LUBE A UALA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 328UA 24148 A NOISE AND VIBRATION ARE HEARD AND FELT THROUGHOUT THE CABIN 30 SECONDS ON 30 SECONDS OFF. LUBED NR 1 ENGINE FAN BLAD ES AND REPLACED 8 FASTENERS ON TRAP PANEL ON PYLON. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110700024 20071107 00024 EU 2007 11 7 07FDEA04689 1 20071026 A 2131 CONTROLLER AIRBUS 300 A300F4605R 3930327 EU CABIN PRESSURE MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 662FE 761 AT FL 330 CABIN V/S CONSTANTLY AT 150 CLIMB, FWD OUTFLOW VALVE SHOWED NEARLY OPEN, SYS 1 REG FAULTED. SYS 2 TOOK OVER AS NECESSARY BUT CABIN V/S INCREASED TO 200FPM, THEN SELECTED MANUAL BUT OUTFLOW VALVE WOULD NOT CLOSE. ELECTED TO MA KE PRECAUTIONARY LANDING IN PHX AS UNABLE TO MAINTAIN CABIN ALT BELOW 10,000FT. FOLLOWED ALL ECAM AND QRH PROCEDURES. MEL/CDL: 21-31-02-A CATEGORY: C EXPIRATION: 05NOV07 "MEL 21-31-02-A: CABIN PRESS CTL SYSTEM NR 1 INOP SYSTEM 1. REM OVED AND REPLACED CABIN PRESSURE CONTROLLER POSITION NR 1 TEST OK AND BITE CHECKS NORMAL WRI 21-30/9624 COMPLETED PER TS I. REMOVED AND REPLACED AFT CABIN PRESSURE OUTFLOW VALVE, OPS CHECK GOOD, REF A300-600 AMM 21-31-12-4. 2 L 7 2 4F RT A35EU 2007103100071 20071031 00071 NM 2007 10 31 KCSA071487 1 20071023 A 5310 STRUCTURE BOEING 747 7472B4B 138481B NM TORQUE BOX CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FORWARD BILGE UPPER TORQUE BOX WEB IS CRACKED .5 INCH AT STA 663, LBL 15. 2 L 7 4 4F RT A20WE 2007103100076 20071031 00076 NM 2007 10 31 MWEA070262 1 20071024 A 3260 833702 PROXIMITY SENSOR DOUG MD88 MD88 3023688 NM MLG ILLUMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 822ME 49759 UPON GEAR RETRACTION RED NOSE LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED NOSE GEAR UP & DOWN PROXIMITY SENSOR. 2 L 7 2 4F RT A6WE 2007103100080 20071031 00080 EA 2007 10 31 TRAX200701588 1 20071024 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 908EV 7654 FORWARD BULKHEAD ILLUMINATED EXIT SIGN NEAR AIRSTAIR DOOR IS BROKE OFF MISSING. FLT 4499 DEL 79 MINS. 2 L 7 2 4F RT A21EA 2007103100082 20071031 00082 EA 2007 10 31 TRAX200701590 1 20071025 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA ROW 2-3 INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 919EV 7780 EMERGENCY FLOOR LIGHTS AT ROW 2 AND 3 INOP. 2 L 7 2 4F RT A21EA 2007103100102 20071031 00102 EA 2007 10 31 VNAA0710008 1 20071011 A 5710 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT WING DENTED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 207PS 7873 CREW REPORTED A BIRD STRIKE TO THE MIDDLE OF THE LEFT WING LEADING EDGE. MAINTENANCE INSPECTED AND FOUND A DENT RESULTI NG FROM THE CONTACT. MAINTENANCE REMOVED AND REPLACED THE LT MID LEADING EDGE. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007103100105 20071031 00105 NM 2007 10 31 SWAA075265 1 20071023 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 887 S6R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103100113 20071031 00113 NM 2007 10 31 2007UALA04370 1 20071024 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHTS INOP: CEILING ROWS 17 & 61 LT. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007103100114 20071031 00114 NM 2007 10 31 2007UALA04371 1 20071024 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHT INOP: ROW 32L. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007103100119 20071031 00119 NM 2007 10 31 SWAA075261 1 20071023 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 887 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007103100136 20071031 00136 NM 2007 10 31 SWAA075311 1 20071024 A 5330 6545767 SKIN BOEING 737 737301 1384611 NM BS 450 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, BL 0. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007103100137 20071031 00137 NM 2007 10 31 SWAA075310 1 20071024 A 5330 6545767 SKIN BOEING 737 737301 1384611 NM BS 410 S28L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, STR 28L. REPAIRED SK IN PER SWA EA. 2 L 7 2 4F RT A16WE 2007103100142 20071031 00142 2007 10 31 CALA0700566 4 20071009 A 2330 RDAV980301 VIDEO MONITOR BOEING 757 757224 1384958 NM ROW 7ABC SMOKE A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 12114 27556 SMOKE COMING FROM VIDEO SCREEN AT SEATS 7ABC & 8ABC. SYSTEM SHUT OFF AND VIDEO C/B PULLED. SMOKE STOPPED. FOUND VIDEO MONITOR AT 7ABC SMELLED OF SMOKE. REMOVED AND REPLACED 7ABC & RAN MOVIES FOR 15 MINUTES. NO MORE SMOKE NOTED. VIDEO MONITOR ROW 8ABC CHECKED OK. ALL OPS NORMAL. ROTABLE PARTS CHANGE WAS INDICATED - TT 0104718, S/N OFF 00779 IPC REFERE NCE. 2 L 7 2 4F RT A2NM 2007103100151 20071031 00151 NM 2007 10 31 2007UALA03921 1 20070927 A 3397 7945243 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY LIGHT AFT GALLEY WALL LEFT INOP. *S/D* REPLACED EEL LIGHT FEEDER CABLE, AFT GALLEY WALL, LEFT SIDE. OP CHEC KS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007103100154 20071031 00154 NM 2007 10 31 2007UALA03928 1 20070926 A 2130 CABIN PRESSURE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FLUCTUATES A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 211UA 30217 FLIGHT EXPERIENCED PRESSURIZATION FLUCTUATIONS. PERFORMED GROUND TEST OF ( L) AND (R) AUTO PRESS CONTROLLERS AND CHECK ED NORMAL. NO HISTORY ON THIS AUTO PRESS CONTROL SYS. AS PRECAUTION ALSO CHECKED MANUAL OPERATION OF FWD AND AFT OUTFL OW VLVS. CONDUCTED VERIFICATION FLT. NO REPEAT OF PRESSURIZATION FLUCTUATION. UNABLE TO DUPLICATE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007103100156 20071031 00156 2007 10 31 2007UALA03934 4 20070924 A 3442 20414460401 DRIVE UNIT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE WEATHER RADAR FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 651UA 25389 RECEIVED "WXR FAIL ANT" ON EHSI. *S/D* REPLACED WEATHER RADAR ANTENNA DRIVE UNIT AS PER MM 34-43-05-401, TEST PASSED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007103100158 20071031 00158 NM 2007 10 31 KCSA071495 1 20071024 A 5320 SUPPORT ANGLE BOEING 747 7472B4B 138481B NM BS 670 S40R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FUSELAGE STRINGER SUPPORT ANGLE IS DAMAGED AT STA 670, STR 40R. 2 L 7 4 4F RT A20WE 2007103100189 20071031 00189 NM 2007 10 31 2007UALA04310 1 20071018 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 365 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 MAIN CABIN FLOORBEAM TEE CAP CORRODED RBL 24 TO RBL 56, BS 365. REPLACED TEE CAP LBL 8 TO RB L 56, STA 365. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110100002 20071101 00002 NM 2007 11 1 CALA0700606 1 20071024 A 5320 BAC1517706 STRUCTURE BOEING 737 737524 1384721 NM BS 616 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11612 27325 INSPECTION FOUND A 1 INCH CRACK AT LOWER FASTENER HOLE IN RT FUSELAGE INNER CHORD ABOVE WING CENTER SECTION STA 616, S17 R. A STIFFENING ANGLE AND FILLER WERE INSTALLED IAW ECRA 5311-01158. 2 L 7 2 4F RT A16WE 2007110100003 20071101 00003 NM 2007 11 1 CALA0700607 1 20071024 A 5320 FITTING BOEING 737 737524 1384721 NM BS 349 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11612 27325 INSPECTION FOUND A 1.5 INCH CRACK AT DOOR FITTING FASTENER IN L-1 DOOR OPENING AFT SIDE STRUCTURAL STRAP, STA 349, S16L. A REPAIR WAS INSTALLED IAW SRM 53-10-04. 2 L 7 2 4F RT A16WE 2007110100004 20071101 00004 NM 2007 11 1 CALA0700608 1 20071024 A 5313 BAC1498157 STRINGER BOEING 737 7373T0 1384582 NM BS 500C S16L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND A .5 INCH CRACK IN STRINGER 16L JUST AFT OF STA 500C FORWARD OF WING SCANNING LIGHT HOUSING. THE STRIN GER WAS REPAIRED IAW SRM 53-00-03, PAGE 201, FIGURE 201, REPAIR 1. 2 L 7 2 4F RT A16WE 2007110100009 20071101 00009 NM 2007 11 1 SWAA075400 1 20071028 A 5310 146A5900 CREASE BEAM BOEING 737 7377H4 1384404 NM BS 986-997 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 758SW 27873 DURING SCHEDULED 8Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 986 TO BS 997, RBL 48. REMOVED AND REPLACED WEB PER SRM . 2 L 7 2 4F RT A16WE 2007110100010 20071101 00010 NM 2007 11 1 SWAA075391 1 20071028 A 5315 147A5006 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 758SW 27873 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 5 TO RBL 40. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007110100011 20071101 00011 NM 2007 11 1 SWAA075373 1 20071028 A 3350 1619 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 613SW 27931 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007110100012 20071101 00012 NM 2007 11 1 SWAA075401 1 20071028 A 3350 20131A BATTERY BOEING 737 737301 1384611 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007110100017 20071101 00017 NM 2007 11 1 SWAA075335 1 20071025 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 727A S6L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007110100018 20071101 00018 NM 2007 11 1 SWAA075344 1 20071025 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 727A S6L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007110100019 20071101 00019 NM 2007 11 1 SWAA075332 1 20071025 A 3350 1619 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 613SW 27931 DURING SCHEDULED BRDG CHECK, FOUND RT FWD FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007110100020 20071101 00020 NM 2007 11 1 SWAA075349 1 20071025 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 794SW 30605 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS 129.5. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007110100022 20071101 00022 NM 2007 11 1 SWAA075334 1 20071025 A 5311 6546595 FRAME BOEING 737 737317 138447P NM BS 727A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110100038 20071101 00038 NM 2007 11 1 SWAA075359 1 20071026 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 294WN 32540 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007110100045 20071101 00045 NM 2007 11 1 UPS07M50987 1 20070816 A 5322 SHEAR TIE DOUG MD11 MD11F 3023600 NM BS 1974 S51L/R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C AFT WASTE AREA AT STATION 1974 IN BETWEEN LONGERON 51R TO 51L FOUND SHEAR CLIP WITH SURFACE CORROSION. AFT WASTE AREA STA 1974 IN BETWEEN LONGERON 51R - 51L SHEAR CLIP AREA FASTENERS AS PER SRM 51-33-01 VII R38. SHEAR CL IP CORROSION REMOVED FOUND EXCEEDED LIMIT. CORRODED SHEAR TEE REMOVED AT STA 1974 LONGERON 49 LT - 49 RT PER SRM 51-33- 01 VII R38. SHEAR TEE REWORK PER DWG AGA8002. SHEAR TEE INSTL AT AFT WASTE AREA STA 1974 L49LT - 49RT PER SRM 51-33-01 VII R38. 2 L 7 3 4F RT A22WE 2007110100067 20071101 00067 NM 2007 11 1 SWAA075361 1 20071026 A 5312 6549892 BULKHEAD BOEING 737 7373H4 1384600 NM BS 1016 S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED C1 CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AT BS 1016, STR 5R. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 2007110100071 20071101 00071 NM 2007 11 1 SWAA075319 1 20071025 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 408WN 27895 DURING SCHEDULED MV3 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007110100072 20071101 00072 NM 2007 11 1 SWAA075328 1 20071025 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 887 S2R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007110100076 20071101 00076 NM 2007 11 1 SWAA075316 1 20071025 A 5310 6516352 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007110100085 20071101 00085 NM 2007 11 1 2007UALA04320 1 20071021 A 5620 SEAL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE OVERWING EXIT OUT OF POSITION A UALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 29 841UA 1545 FLIGHT DIVERTED DUE TO VIBRATION ON AN OVERWING EXIT WINDOW. FLIGHT DIVERTED FOR A SECOND TIME TO ORD UNDER AMBER ALERT DUE TO SAME PROBLEM. 11-01-07 FOUND OVERWING EXIT DOOR SEAL OUT OF PLACE. REMOVED AND REPLACED OVERWING EXIT DOO R SEAL. ACCOMPLISHED TEST FLIGHT- NO NOISE OR VIBRATION NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110100086 20071101 00086 NM 2007 11 1 2007UALA04321 1 20071021 A 3810 TOILET BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LAVATORY LEAKING A UALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 WP 29 227UA 30555 RTFL DUE TO WATER LEAK FROM THE GALLEY, SOAKING THE CREW REST AREA / PASSENGER SECTION. SUSPECT TOILET ASSEMBLY. REMOVE D AND REPLACED THREE TOILET ASSEMBILES AT LAV 101, 131,141. REPLACED AFT DRAIN RESTRICTOR VALVE. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007110100111 20071101 00111 EA 2007 11 1 TRAX200701549 1 20071020 A 2910 LINE CNDAIR CL600 CL6002C10 1390015 EA HYD SYSTEM CHAFED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 390CA 10106 FOUND RIGHT ENG PYLON HYDRAULIC PRESSURE LINE CHECK VALVE AT FIREWALL CHAFED. REMOVED CHECK VALVE IAW CRJ 700 AMM 29-11 -00. EN ROUTE TO ATL A/C DIVERTED TO AEX DUE TO MTC. RELATED TO DEFECT 360869-1 &-2 AND 360870-1. EMERGENCY DECLARED. REF AFDL 360869, ITEM 1 FOR INDICATION & AFDL 360870 ITEM 1 FOR LEAK / OPS CHECK. 2 L 7 2 4F RT A21EA 2007110100117 20071101 00117 NM 2007 11 1 SWAA075387 1 20071028 A 5311 6546549 FRAME BOEING 737 7373A4 1384585 NM BS 767 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110100121 20071101 00121 NM 2007 11 1 2007UALA04325 1 20071020 A 2697 CONTACT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU APU FIRE DETECT DIRTY A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 937UA 26668 DURING APU START ON GROUND APU FIRE WARNING SOUNDED. PULLED HANDLE AND DISCHARGED BOTTLE. FOUND DIRTY CONTROL BOX CON TACTS. CLEANED CONTACTS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110100133 20071101 00133 NM 2007 11 1 ASAA0742156 1 20071025 A 5320 69730542 INTERCOSTAL BOEING 737 7374Q8 138447Q NM BS 400 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 STA 400 LBL 24.75 INTERCOSTAL BELOW SEAT TRACK CRACKED. FABRICATED AND INSTALLED NEW INTERCOSTAL WEB IAW BAC DWG 69 730 54 AND SRM 51-40-2. 2 L 7 2 4F RT A16WE 2007110100136 20071101 00136 NM 2007 11 1 SWAA075394 1 20071028 A 5314 6562125 KEELBEAM BOEING 737 7375H4 138449D NM BS 482 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED 18Y CHECK, FOUND LT KEEL BEAM CORRODED AT BS 482. REPAIRED KEEL BEAM PER EA. 2 L 7 2 4F RT A16WE 2007110100151 20071101 00151 NM 2007 11 1 2007UALA04332 1 20071019 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 285 S3L GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 330UA 24191 UPPER FUSELAGE SKIN GOUGED IN THREE PLACES AT STR 3L ABOVE DOOR 1L BS 285. FABRICATED AND INSTALLED EXTERNAL FUSELAGE S KIN DOUBLER TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110100181 20071101 00181 NE 2007 11 1 HCM2007F00001 2 20070928 A 7300 UNKNOWN UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE UNKNOWN E HCMA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 WP 13 11QG 3534 23043 AT APPROX 8000 FT ALTITUDE AT CRUISE FLT, NOTICED 2 MINOR KICKS & SLIGHT YAWS APPROX 30 SECONDS APART, REVIEWED INSTRUME NTS AND GAUGES, NOTHING ABNORMAL DETECTED. FLT CONTINUED, AT 1 HOUR INTO CRUISE FLT, APPROX 100 KNOTS AIRSPEED, AC EXPE RIENCED A SUBSTANTIAL YAW NOSE TO THE RT, THEN LOW ROTOR AUDIO WARNING (SOLID TONE) ACTIVATED, PILOT VERIFIED THAT ROTOR RPM HAD DETERIORATED AND WAS BELOW 360 NR AND DECREASING, PILOT ALSO OBSERVED THAT A YELLOW WARNING LIGHT HAD ILLUMINAT ED (POSSIBLY THE AMBER (GOV) LIGHT (NOT CONFIRMED) ON WARNING PANEL, PILOT ENTERED AN AUTOROTATION AND AFTER APPROX 8 SE CONDS RECOVERED ROTOR RPM INTO NORMAL RANGE. PILOT CONTINUED WITH AUTOROTATION AND WHEN APPROACHING HIS SELECTED LANDIN 1 G 7 2 3U 3 U H9EU E00054EN 2007110200099 20071102 00099 SO 2007 11 2 SIMA200729902 1 20071023 A 3260 PROXIMITY SWITCH EMB 135 EMB135KL 3260302 SO NLG OUT OF LIMITS A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 816AE 145552 LANDING GEAR AIR/GND FAIL ON TAKEOFF. COULD NOT RAISE GEAR. RETURNED TO FIELD AND MADE NORMAL LANDING. INSP MLG PROX SWITCH CLEARANCES. ALL WITHIN. INSP NLG PROX SWITCHES AND FOUND TO BE OUT OF LIMITS. ADJUSTED AS PER AMM 32-63-05-700 -803A. PERFORMED GEAR RETRACTION AND NO DEFECTS NOTED. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007110200122 20071102 00122 NM 2007 11 2 C8GA20070010 1 20071013 A 2910 LINE BOEING 727 727223 1384074 NM HYD SYSTEM LEAKING A C8GA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 29 715AA 22470 FLT 811 FROM SJU TO MCO - DURING CLIMB OPERATION, THE AIRCRAFT EXPERIENCED NR 2 ENGINE "A" SYSTEM HYDRAULIC FAILURE/FLUI D LOSS. THE AIRCRAFT RETURNED TO SJU WERE AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGH T INSPECTION REVEALED AN ELEVATOR POWER CONTROL UNIT FLEX LINE LEAKING. THE FLEX LINE WAS REMOVED AND REPLACE, HYDRAULI C SYSTEM SERVICED, OPS AND LEAK CHECKED GOOD. 2 L 7 3 4F A3WE 2007110200128 20071102 00128 SW 2007 11 2 WGEA20070017 1 20071024 A 3242 3266B BRAKE ECLIPS EA500 ECLIPSEEA500 3350000 SW LEFT RESTRICTED E WGEA O OTHER O OTHER LD LANDING 1 EA 27 145DJ 000057 VERY LITTLE LEFT BRAKE ON LANDING, PEDAL TO THE FLOOR, RIGHT BRAKE IS NORMAL. PERFORMED BRAKE BLEEDING ON BOTH BRAKES I AW 32-40-00. BRAKES OPERATE WITH NO DEFECTS NOTED IAW EA500 M/M 32-40-00. 1 L 7 2 4J RT A00002AC 2007110200130 20071102 00130 EU 2007 11 2 COEA0708902 1 20070915 A 7714 56787048011 INDICATOR AEROSP ATR42 ATR42320 8680930 EU NR 2 TORQUE FLUCTUATES A COEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 13 902FX 175 FLT 7813 - ON TAKEOFF ROLL, THE NR 2 TORQUE GAUGE WAS FLUCTUATING BY GREATER THAN 10 PERCENT. TAKEOFF ABORTED. COULD N OT DUPLICATE DURING MAINTENANCE RUNS. (M) 2 H 7 2 4T RT A53EU 2007110200134 20071102 00134 WP 2007 11 2 07FDEA04683 1 20071025 A 5347 AFA7433 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 MAIN CABIN ON SEAT TRACK FOUND DEEP WEAR. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F RT A22WE 2007110200143 20071102 00143 EU 2007 11 2 SIMA200729911 1 20071025 A 6120 WARNING LIGHT SAAB SF340 340B 7860101 EU AUTOCOARSEN ILLUMINATED A SIMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 21 324AE 340B324 ABORTED TAKEOFF DUE TO AUTOCOARSEN HIGH LIGHT FAILED TO ILLUMINATE DURING TAKEOFF ROLL. DISPATCH AND CREW AGREE TO RETU RN TO THE BLOCK DUE TO MEL WEIGHT LIMITATIONS. FOUND RPL MIN T/O CIRCUIT BREAKER POPPED RESET BREAKER PERFORMED. OPS C HECKS IAW AMM 61-22-02 OPS CHECK GOOD. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4T RT A52EU 2007110200148 20071102 00148 EA 2007 11 2 CHQA200700066 1 20071027 A 2913 887055 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 LEAKING A CHQA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 11 701BR 12899 418 7448 GEE872845 CMH TO IAH - DURING CRUISE FLIGHT, LOST HYDRAULIC SYSTEM 2 FLUID AND PRESSURE. CREW RAN APPROPRIATE CHECKLISTS AND LAND ED AT THE NEAREST SUITABLE AIRPORT (LITTLE ROCK). AFTER LANDING, THE AIRCRAFT WAS TURNED OVER TO MAINTENANCE. MAINTENA NCE SERVICED THE NR 2 HYDRAULIC SYSTEM AND INSPECTED FOR LEAKS. THE NR 2 ENGINE DRIVEN PUMP WAS FOUND TO BE LEAKING. T HE NR 2 ENGINE DRIVEN HYDRAULIC PUMP WAS REPLACED AND THE HYDRAULIC SYSTEM WAS LEAK TESTED. AFTER THE SUCCESSFUL LEAK C HECK, THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007110500132 20071105 00132 EU 2007 11 5 USAA920070976 1 20071024 A 5530 D5537131800200 HINGE FITTING AIRBUS 320 A320232 3930326 EU ZONE 300 WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C-07 CHECK - RUDDER HINGE NR 3 FITTING WORN, VERTICAL STABILIZER STATION 2279 / RIB 5. REPLACED RU DDER HINGE NR 3 FITTING VERTICAL STABILIZER STATION 2279 / RIB 5 IAW A320 AMM 27-21-00 AND 55-36-41. 2 L 7 2 4F RT A28NM 2007110500140 20071105 00140 NM 2007 11 5 USAABB07083 1 20071025 A 3350 2012 BATTERY BOEING 757 757225 1384959 NM EMERGENCY LIGHTS INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925UW 22205 MAINTENANCE FOUND EMERGENCY LIGHTS IN MID TO AFT CABIN AREA COMING ON INTERMITTENTLY. REPLACED THE M732 AND M733 POWER PACKS. NO FURTHER FAULTS. 2 L 7 2 4F RT A2NM 2007110500146 20071105 00146 NM 2007 11 5 UPS07651011 1 20071024 A 5347 SEAT TRACK BOEING 767 76734AF 1385212 NM COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 307UP 27760 INSPECTION TYPE:SEG2 F/O'S SEAT TRACKS HAVE CORROSION. REPLACED SEAT TRACK PER SRM. 2 L 7 2 4F RT A1NM 2007110500174 20071105 00174 EU 2007 11 5 UPS07151003 1 20071025 A 7997 WIRE HARNESS AIRBUS A300 A300F4622R 3930360 EU OIL PRESSURE UNKNOWN A IPXA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SO 01 138UP 0821 INSPECTION TYPE:N/A ATB - IFSD - NR 2 ENGINE SHUT DOWN TO LOW OIL PRESSURE. *S/D* REMOVED AND REPLACED OIL PRESSURE TR ANSMITTER HARNESS, WIRES 072057, 072056, 072055 FROM CONNECTOR DT583 & D4952P REF P&W CMM 71-51-01. REF LP 651061 REMOV ED AND REPLACED NR 2 OIL PRESSURE REGULATOR VALVE IAW MM 79-21-04-04. 2 L 7 2 4F RT A35EU 2007110500180 20071105 00180 NM 2007 11 5 UPS07551054 1 20071013 A 5311 146N102886 FRAME BOEING 757 75724APF 1384969 NM BS 1340 S25-26R DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 450UP 25472 INSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1340, BET WEEN S25R AND S26R (2EA). ACCOMPLISHED REPAIR PER FINA L EA 757-5330-A1756 AND UPS EO B757-5310-27941-A. 2 L 7 2 4F RT A2NM 2007110500182 20071105 00182 NM 2007 11 5 UPS07M51030 1 20070831 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C EMP - LT HORZ STAB NR 30 BARREL NUT BORE FOUND CORROSIONS. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARR EL NUT BORE BLEND OUT VOID, BOTTOM PERIPHERY RADIUS SMOOTHEN/PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE REP AIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP. 2 L 7 3 4F RT A22WE 2007110500184 20071105 00184 NM 2007 11 5 UPS07M51032 1 20070905 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C EMP - LT HORZ STAB NR 36 BARREL NUT BORE FOUND CORROSIONS. TORQUE BOX WEB CUT FOR ACCESS. CORROSION AT BARREL NUT BORE REMOVED. BORE REAM & REMAINING BLEND OUT FOUND EXCEEDS LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHENED & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING. 2 L 7 3 4F RT A22WE 2007110500200 20071105 00200 NM 2007 11 5 UPS07M51048 1 20071003 A 5753 STRUCTURE DOUG MD11 MD11F 3023600 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C RIGHT WING: DURING O/B FLAP I/B FWD HINGE PIVOT BEARING REPLACEMENT FOUND PIVOT BORE CORRODED AS MARK ED. RIGHT O/B FLAP I/B FWD HINGE REMOVED PER AMM 57-53-01 R.50. RIGHT FWD O/B FLAP I/B HINGE PIVOT BORE CORROSION REMO VED & FOUND EXCEED LIMIT PER CMM5 7-44-08. FPI C/O PER DAC NDT SPM R.13 PT 08, NO CORROSION FOUND ON BORE SURFACE. CAD IUM PLATING C/O ON REWORK AREA PER BSOPM20-10-01 R.58. BUSHING FAB AND INSTALLED AS PER EN 1667-07. 2 L 7 3 4F RT A22WE 2007110500204 20071105 00204 2007 11 5 WRNA200700059 4 20071026 A 3441 46300181300413 INU BOEING 747 747230B 1384889 NM NR 1 FAILED A WRNA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 05 531TA 22669 DURING CLIMB AT 300 FEET NR 1 INU FAILED, NR 3 INU WAS ON MEL 34-27-2A. DUMPED 50,000 POUNDS OF FUEL AND RETURNED TO FI ELD FOR A SAFE LANDING. REPLACED NR 1 INU IAW MM 34-41-03 PG 401 AND TESTED IAW MM 34-41-04 PG 501. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 4 4F A20WE 2007110500210 20071105 00210 NM 2007 11 5 CALA0700617 1 20071026 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM BS 867 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11612 27325 INSPECTION FOUND A 5 INCH CRACK AT FORWARD FASTENER HOLE OF FRAME AT STA 867 BETWEEN STRINGERS 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04668. 2 L 7 2 4F RT A16WE 2007110500211 20071105 00211 NM 2007 11 5 CALA0700618 1 20071026 A 5311 6546557 FRAME BOEING 737 737524 1384721 NM BS 787 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11612 27325 INSPECTION FOUND A .5 INCH CRACK AT FORWARD FASTENER HOLE OF FRAME AT STA 787 BETWEEN STRINGERS 8L AND 9L. THE FRAME WA S REPAIRED IAW ECRA 5310-04668. 2 L 7 2 4F RT A16WE 2007110500212 20071105 00212 NM 2007 11 5 CALA0700619 1 20071026 A 5311 6546525 FRAME BOEING 737 737524 1384721 NM BS 380 S8R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11612 27325 INSPECTION FOUND A .5 INCH CRACK IN AFT SIDE OF FUSELAGE FRAME AT STA 380 AROUND RIVET BELOW S8R. THE FRAME WAS REPAIRE D IAW ECRA 5310-04668. 2 L 7 2 4F RT A16WE 2007110500213 20071105 00213 NM 2007 11 5 CALA0700620 1 20071026 A 5311 65C33510 FRAME BOEING 737 737524 1384721 NM BS 440 S8R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11612 27325 INSPECTION FOUND A . 5 INCH CRACK IN AFT SIDE OF FUSELAGE FRAME AT STA 440 AROUND RIVET BELOW S8R. THE FRAME WAS REPAIR ED IAW ECRA 5310-04668. 2 L 7 2 4F RT A16WE 2007110500214 20071105 00214 NM 2007 11 5 CALA0700621 1 20071026 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AT STA 328, RBL 11. THE FLOORBEAM SECTION WAS REMOVED AND REPLACED IAW S RM 51-40-02. 2 L 7 2 4F RT A16WE 2007110500215 20071105 00215 NM 2007 11 5 CALA0700622 1 20071027 A 5311 6546532 FRAME BOEING 737 7373T0 1384582 NM BS 480 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 480 BETWEEN S8R AND S9R. THE FRAME WAS REPAIRED IAW ECRA 5310 -04669. 2 L 7 2 4F RT A16WE 2007110500216 20071105 00216 NM 2007 11 5 CALA0700623 1 20071027 A 5311 6546532 FRAME BOEING 737 7373T0 1384582 NM BS 480 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 480 BETWEEN S8L AND S9L. THE FRAME WAS REPAIRED IAW ECRA 5310 -04669. 2 L 7 2 4F RT A16WE 2007110500218 20071105 00218 NM 2007 11 5 CALA0700625 1 20071027 A 5311 6546549 FRAME BOEING 737 7373T0 1384582 NM BS 767 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 767, S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04669. 2 L 7 2 4F RT A16WE 2007110500220 20071105 00220 EU 2007 11 5 USAA920071012 1 20071016 A 5347 D53472090005 SEAT TRACK AIRBUS 320 A320232 3930326 EU BS 3043-3158 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN SEAT RAIL BEAM, BS 3101 / FR 65, -Y1292. REPLACED CABIN SEAT RAIL B EAM, BS 3043 / FR 64 - BS 3158 / FR 66, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007110500221 20071105 00221 NM 2007 11 5 USAA920071020 1 20071021 A 5340 69560371 STRINGER CLIP BOEING 737 7373B7 1384580 NM BS 616 S5L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED STRINGER TIE CLIP, BS 616, S5L. REPLACED STRINGER TIE CLIP, BS 616, S5L IAW B7 37-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007110500225 20071105 00225 EU 2007 11 5 USAA920071024 1 20071018 A 5321 D5367180500500 FLOORBOARD AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - CORROSION ON CABIN FLOORBOARD 262F, BS 3158 / FR 66 - BS 3257 / FR 68. REPLACED CABIN FLOORBOARD 262F, BS 3158 / FR 66 - BS 3257 / FR 68 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007110500226 20071105 00226 EU 2007 11 5 USAA920071025 1 20071013 A 5320 D53475765200 SILL AIRBUS 320 A320232 3930326 EU ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - CORROSION ON BULK CARGO COMPARTMENT DOOR CUT OUT LOWER SILL, BS 2830 / FR 60, -Y660. R EPAIRED BULK CARGO COMPARTMENT DOOR CUTOUT LOWER SILL, BS 2830 / FR 60, -Y660 IAW A320 SRM 53-41-49. 2 L 7 2 4F RT A28NM 2007110500227 20071105 00227 NM 2007 11 5 ASAA0752160 1 20071028 A 2822 21C1321 PRESSURE SWITCH BOEING 737 737890 1384527 NM FUEL BOOST INTERMITTENT A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 583AS 35681 LEFT MAIN FUEL TANK AFT FUEL PUMP LIGHT IS ON INTERMITTENTLY WITH THE SWITCH IN THE ON POSITION. REPLACED NR 1 AFT FUEL BOOST PUMP PRESSURE SWITCH. 2 L 7 2 4F RT A16WE 2007110500228 20071105 00228 NM 2007 11 5 ASAA0752159 1 20071028 A 4960 2118966222 CONTROL UNIT BOEING 737 737890 1384527 NM APU INTERMITTENT A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 579AS 35187 AT PUSHBACK APU MAINTENANCE LIGHT ILLUMINATED. ACCOMPLISHED FIM 49 40 TASK 806 & FIM 49 60 TASK 801. COULD NOT VERIFY DISCREPANCY. 2 L 7 2 4F RT A16WE 2007110500229 20071105 00229 NM 2007 11 5 CALA0700628 1 20071029 A 5610 6531914102 RELEASE MECH BOEING 737 7373TO 138447G NM COCKPIT WINDOW INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 THE FIRST OFFICER'S SLIDING WINDOW (R2) FAILED OPERATIONAL TEST FROM OUTSIDE THE CONTROL CABIN (WINDOW DID NOT UNLOCK AN D OPEN WHEN THE EXTERNAL RELEASE HANDLE WAS PULLED). THE EMERGENCY RELEASE MECHANISM WAS LUBRICATED AND THE AREA WAS CL EANED. A FUNCTIONAL CHECK WAS GOOD IAW AMM 56-12-11. 2 L 7 2 4F RT A16WE 2007110500230 20071105 00230 NM 2007 11 5 CALA0700626 1 20071029 A 5313 BAC1498157 STRINGER BOEING 737 7373T0 1384582 NM BS 340-360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND STRINGER 25R CORRODED AT STA 340-360. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-00-03, REPAIR 1, FIGU RE 201, DETAIL VII. 2 L 7 2 4F RT A16WE 2007110500233 20071105 00233 EU 2007 11 5 2007UALA04397 1 20071026 A 3350 CONTROL PANEL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 422UA 503 AFT ATTND PANEL, EMERGENCY LIGHT SWITCH IS INOP. SWITCH WILL NOT STAY ON. FOUND SWITCH IS FAULTY. REPLACED ATTEND PA NEL CONTROL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110500235 20071105 00235 EU 2007 11 5 2007UALA04399 1 20071025 A 5347 SEAT TRACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 482UA 1584 RIGHT INBOARD SEAT TRACK BETWEEN FRAME 36 & 41 IS WORN OUT OF LIMITS. REPLACED SEAT TRACK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110500237 20071105 00237 NM 2007 11 5 2007UALA04401 1 20071025 A 5210 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU PAX DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 FWD ENTRY DOOR AFT SIDE, 6TH STOP PIN CUTOUT FROM TOP, INNER SKIN HAS CRACK. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACK & ACCMP NDT FOR CRACK CONTAINMENT. FABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110500242 20071105 00242 NM 2007 11 5 2007UALA04406 1 20071025 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 218 S18L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 EXTERIOR FUSELAGE STA 218, STR 18L SKIN DENTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110600001 20071106 00001 WP 2007 11 6 NWAA073579929 1 20071023 A 2780 SLAT SYSTEM DOUG DC9 DC931 3022065 WP LE SLATS UNKNOWN A NWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 01 8923E 45838 ON APPROACH FOR LANDING AT ABOUT 200 KTS, THE YELLOW "SLAT DISAGREEMENT" LIGHT ILLUMINATED WHEN SLATS WERE SELECTED TO E XTEND. THE AIRCRAFT ALSO EXPERIENCED AN UNCOMMANDED ROLL TO THE RIGHT WHEN THE LEADING EDGE SLATS FAILED TO DEPLOY SYMM ETRICALLY. AS THE AIRCRAFT SLOWED THROUGH 190 KTS AN AUDIBLE BANG WAS HEARD, BLUE "SLAT EXTEND" LIGHT CAME ON, AND THE "SLAT DISAGREEMENT" LIGHT EXTINGUISHED. LANDING WAS COMPLETED WITHOUT ANY FURTHER PROBLEM. MAINTENANCE INSPECTED THE S LAT SYSTEM BUT WAS UNABLE TO DUPLICATE THE FAULT OR TO FIND ANY PROBLEM AT ALL. THE T-DUCT O-RINGS AND SEALS WERE REPLA CED PER MC DIRECTION. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007110600003 20071106 00003 EU 2007 11 6 07FDEA04697 1 20071029 A 5755 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 4 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 729FD TS0717 657 FOUND DELAMINATION ON UPPER SKIN OF SPOILER 4 LT , P/N A577-71000-004-00F, S/N TS0717. REPAIR PERFORMED BY REPLACEMENT OF SPOILER IAW AMM 276151 PB 400. 2 L 7 2 4F RT A35EU 2007110600004 20071106 00004 EU 2007 11 6 07FDEA04698 1 20071029 A 5755 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 5 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 729FD TS721 657 FOUND DELAMINATION ON UPPER SKIN OF SPOILER 5 LT , P/N A577-71000-004-00F, S/N TS0721. REPAIR PERFORMED BY REPLACEMEN T OF SPOILER IAW AMM 276151 PB 400. 2 L 7 2 4F RT A35EU 2007110600006 20071106 00006 EA 2007 11 6 SWIA200718810 1 20071022 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA STUCK A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 947SW 7786 FLT 3820 - SERVICE DOOR WILL NOT CLOSE OR OPEN. CYCLED SERVICE DOOR HANDLE AND CLOSED DOOR. 2 L 7 2 4F RT A21EA 2007110600007 20071106 00007 EU 2007 11 6 07FDEA04706 1 20071031 A 5315 A5397826720400 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 BULK PIT BELOW FLOOR, CORROSION ON FLOOR FRAME 67 UNDER NUTPLATE AT RBL 38. REMOVED CORROSION IAW A310 SRM 51-22-00 PG 11, CHECKED LIMITS, ORIG MAT 0.130, MAT. REMOVED .040, MAT REMAINING .090. FOUND OUT OF LIMITS IAW A310 SRM 53-10-15 P G 101 UTG NR 8225-B. REMOVED BEAM IAW A310 SRM 51-40-21 PG 7, RECEIVED NEW BEAM P/N A5397826720400 PO 594281.3. DRILLE D AND LOCATED IAW A310 SRM 51-40-40 AND INSTALLED IAW A310 SRM 51-40-21 PG 7. 2 L 7 2 4F RT A35EU 2007110600009 20071106 00009 NM 2007 11 6 07FDEA04708 1 20071101 A 5311 FRAME DOUG MD11 MD11F 3023600 NM BS 1721 L12L DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 527FE 48601 MAIN DECK LEFT SIDEWALL STRUCTURE, FRAME STA 1721 DENTED AT LONGERON 12. REPAIR CARRIED OUT AT MAIN DECK LEFT HAND SIDE WALL STRUCTURE, FRAME STA 1721, LONGERON 12 AS PER SRM 53-30-00 FIGURE 1 VOLUME I AND SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007110600011 20071106 00011 NM 2007 11 6 07FDEA04710 1 20071101 A 5740 112N700358 FITTING BOEING 757 7572B7 1384964 NM ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 RT WING I/B LOAD FITTING HAS 3 FASTENER HOLES DAMAGED COMMON TO THE SIDE LOAD FITTING. REF S/B 757-54-0035 FIG 7, PANEL 3, STEPS 2 AND 3 IAW EA NR F-5450-108908, REAMED EACH HOLE TO REMOVE DAMAGE. ACCOMPLISHED BHEC OF THE REWORKED HOLES P ER 757 NDT MANUAL D6-34N301, PART 6, SUB 51-00-16. FABRICATED 3 EACH REPAIR BUSHINGS AND INSTALLED THEM WET WITH BMS 5- 95 PER SOPM 20-50-03. REAMED ALL 3 REPAIR BUSHINGS ON CENTER TO 0.325" TO 0.328". PERFORMED A DVI AFTER FINAL REAMING OF BUSHINGS. APPLIED ALODINE AND BMS 10-11, TYPE 1 PRIMER TO THE REPAIR AREA AND THE BUSHING ID'S. 2 L 7 2 4F RT A2NM 2007110600012 20071106 00012 SO 2007 11 6 SWIA200718820 1 20071031 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY EXIT MISSING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 223SW 120291 FLT 5446 - EMERGENCY EXIT SIGN MISSING FROM 6A. INSTALLED NEW EMERGENCY LIGHT FIXTURE AT 6A. 2 L 7 2 4T RT A31SO 2007110600013 20071106 00013 EA 2007 11 6 SWIA200718821 1 20071028 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 927SW 7693 FLT 6024 - PAX DOOR FLOOR LEVEL EMERGENCY FLOOD LIGHT IS INOP. REPLACED FLOOR LEVEL EMERGENCY LIGHT ASSEMBLY IAW CRJ 20 0 MM 33-51-19. 2 L 7 2 4F RT A21EA 2007110600014 20071106 00014 EA 2007 11 6 SWIA200718822 1 20071030 A 3520 OXYGEN MASK CNDAIR CL600 CL6002B19 1900309 EA CABIN UNWANTED DEPLOY A SWIA G O2 MASK DEPLOYED O OTHER NR NOT REPORTED 1 NM 07 492SW 7168 FLT 3797 - O2 MASKS AT SEATS 8A AND B DROPPED. RESTOWED OXYGEN MASKS AT SEAT 8A AND B AS NEEDED. 2 L 7 2 4F RT A21EA 2007110600025 20071106 00025 NM 2007 11 6 WRLA2007118 1 20071028 A 3230 CABLE DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE MLG BROKEN A WRLA O OTHER J WARNING INDICATION CL CLIMB 1 SO 11 276WA 48632 RIGHT MAIN GEAR SHOWED UNLOCKED AFTER TAKEOFF. BOTH INDICATOR BY GEAR HANDLE AND CONFIG PAGE WERE RED. CYCLED GEAR, OK NEXT TIME. FOUND RIGHT GEAR FOLLOW UP CABLE BROKEN AND LOWER GEAR DOOR DAMAGED. PER MX FERRY PERMIT ALL 4 GEAR PINS I NSTALLED AND SAFETIED. RIGHT GEAR DOOR SAFETY LOCK INSTALLED AND SAFETIED, ADC MMO LEFT AND RIGHT SW TO GEAR DOWN FERRY . 2 L 7 3 4F 4 F RT A22WE E24NE 2007110700007 20071107 00007 EU 2007 11 7 2007UALA04452 1 20071027 A 2611 RAI2800M0706 CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SMOKE DETECTION FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 415UA 475 SMOKE LAV+CRG DET FAULT ECAM. FOUND SDCU FAILED. REPLACED SDCU AND DETECTOR WH4. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110700008 20071107 00008 NM 2007 11 7 07FDEA04702 1 20071030 A 5330 SKIN BOEING 727 727227 1384078 NM BS 312-328 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 479FE 21461 FWD LT LOWER HALF EXTERNAL FUSELAGE BET STA 312-328, STR 22L SKIN HAS DENT. REMOVED PREVIOUS SKIN DOUBLER, FABRICATED S KIN DOUBLER IAW SRM 53-30-3. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2. REPAIR IS CLASSIFIED AS MAJOR REPAIR. 2 L 7 3 4F A3WE 2007110700025 20071107 00025 EU 2007 11 7 07FDEA04693 1 20071027 A 5540 R5537020901800 ARM AIRBUS 310 A310203 3930313 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 NR 5 RUDDER HINGE ARM (3EA) BEARINGS WORN, CORROSION ON LUG FACE REMOVED CORROSION FROM LUG FACE IAW A310-200 MM 51-24-1 0-8 LUG THICKNESS OUT OF LIMITS IAW A310-200 SRM 55-30-00. ORDERED AND RECEIVED SERVICEABLE NR 5 HINGE ARM S/N776235. HINGE ARM WAS INSTALLED ON FEDX CARD 43S2082 STEP 5G.3. 2 L 7 2 4F RT A35EU 2007110700026 20071107 00026 EU 2007 11 7 07FDEA04695 1 20071027 A 5540 A550785000463 ARM AIRBUS 310 A310222 3930315 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 451FE 303 NR 3 RUDDER ATTACH ARM, BOTH FWD BEARINGS WORN, LUGS FOUND TO HAVE CORROSION REMOVED AND REPLACED BEARING ASSEMBLIES IAW EA6-5540-109209 STABILIZERS-RUDDER NR 2 AND NR 3 HINGE ARM OVERSIZE BUSHING INSTALLATION-REPAIR, NR 3 HINGE ARM TO BE R EINSTALLED ON FEDEX CARD 43S2082 RUDDER HINGE FITTINGS DETAILED INSPECTION. 2 L 7 2 4F RT A35EU 2007110700027 20071107 00027 NM 2007 11 7 C8GA20070011 1 20071024 A 2612 CONTROL UNIT BOEING 727 7272A1 138407F NM FIRE WARNING MALFUNCTIONED A C8GA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 29 286SC 21601 FLT 738 FROM TOL TO SLW - DURING CRUISE OPERATION THE LOWER CARGO FIRE WARNING CAME ON. AIRCRAFT DIVERTED TO EVV, EMERG ENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED, LOWER CARGO COMPARTME NT WAS EMPTY NO DEFECTS WERE NOTED. REMOVED AND REPLACED CENTRAL CONTROL UNIT OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2007110700028 20071107 00028 NM 2007 11 7 AALA20071994 1 20071020 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 MIA - EMERGENCY LIGHTS AT SEAT 32G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 32G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007103100148 20071031 00148 NM 2007 10 31 2007UALA03918 1 20070927 A 3350 9F19948501 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 THE 5A EXIT LIGHT INOP. *S/D* REPLACED EXIT EEL LIGHT AT DOOR 5A. OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007103100149 20071031 00149 NM 2007 10 31 2007UALA03919 1 20070927 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 DOOR SILL EEL LIGHT, DOOR 2R INOPERATIVE. *S/D* RELAMPED LIGHT. OP CHECKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007103100150 20071031 00150 NM 2007 10 31 2007UALA03920 1 20070927 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY CEILING LIGHT ABOVE ROW 35 INOP. *S/D* RELAMPED EEL CEILING LIGHT. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007103100153 20071031 00153 NM 2007 10 31 2007UALA03927 1 20070926 A 3350 78942 LENS BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 774UA 26936 THE 33C, 35G & 37G EEL LIGHT LENSES ARE MISSING. RE-LENSED AS PER MM 33-51-05. OP CHECKED PER SAME, SYS OPS NORMALLY. RETURNED AC BACK TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007103100157 20071031 00157 NM 2007 10 31 2007UALA03936 1 20070927 A 2797 BACC63BP14A7SN CONNECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE AILERON LCKOUT FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 674UA 29242 AILERON LOCKOUT MSG. *S/D* PERFORMED EXTENSIVE TROUBLESHOOTING. BOTH AIL-LOCKOUT ACTUATOR CONNECTORS WERE REPLACED. ALSO REPLACED INOPERATIVE RIGHT AIL-LOCKOUT ACTUATOR. AIL-LOCKOUT SYS OPERATED NORMALLY PER MM 27-11-44 (3H). 2 L 7 2 4F 4 F RT A1NM E24NE 2007103100159 20071031 00159 NM 2007 10 31 KCSA071489 1 20071023 A 5330 SKIN BOEING 747 7472B4B 138481B NM BS 865 S1-2R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 EXTERNAL FUSELAGE SKIN IS DAMAGED AT STA 865, BETWEEN STR 1R & 2R. 2 L 7 4 4F RT A20WE 2007103100160 20071031 00160 EU 2007 10 31 2007UALA04376 1 20071024 A 5100 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE UNKNOWN A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 444UA 824 FLIGHT DIVERTED DUE TO A VENT EXTRACT FAULT. FOUND EXTRACT FAN SEIZED. REPLACED EXTRACT FAN (VALVE 21HQ) 2 L 7 2 4F 4 F RT A28NM E40NE 2007103100162 20071031 00162 NM 2007 10 31 2007UALA04380 1 20071023 A 5754 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 6 SLAT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 341UA 24245 NR 6 SLAT (RT WING) CRACKED, LOCATED ON BOTTOM SURFACE. REMOVED DAMAGED AREA AND PERFORMED A REPAIR TO THE NR 6 SLAT (BOTTOM SURFACE). 2 L 7 2 4F 4 F RT A16WE E21EU 2007103100165 20071031 00165 EU 2007 10 31 2007UALA04383 1 20071024 A 3350 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 461UA 1266 EMERGENCY LIGHT SYSTEM TEST FAILS EPSU L FWD. FOUND EPSU FAILURE. REPLACED LEFT FWD EPSU- NO REPEATS SINCE ORIGINAL . 2 L 7 2 4F 4 F RT A28NM E40NE 2007103100177 20071031 00177 NM 2007 10 31 WRLA2007115 1 20071021 A 5753 ARC4125502 RIB DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE TE FLAP CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 273WA 48519 DURING 4C+12A CHECK, FOUND RT OUTBOARD FLAP NR 2 STOP FITTING CRACKED. REF EGAT NRC U05062. PERFORMED BOEING SERVICE B ULLETIN MD-11-57-075, REPLACED DAMAGE RIB REV 00. 2 L 7 3 4F 4 F RT A22WE E24NE 2007103100190 20071031 00190 NM 2007 10 31 2007UALA04311 1 20071018 A 2120 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY ODOR A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 649UA 25286 ELECTRICAL BURNING ODOR IN MID GALLEY AREA AND AIRCRAFT RETURNED TO BLOCKS. INSP GALLEY AREA AND OVERHEAD AREA FOR EVID ENCE OF BURNING NO OBVIOUS SIGHT OF SMOKE OR BURNING. FIRE BRIGADE PERFORMED HEAT DECTECTOR EQUIPMENT NO SIGN FOUND.NO H ISTORY () INSP CHILLERS ALL OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110100024 20071101 00024 NM 2007 11 1 SWAA075333 1 20071025 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 633SW 27936 DURING SCHEDULED MV4 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT ASSY LOOSE AT ROW 2 ABC. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007110100044 20071101 00044 NM 2007 11 1 UPS07M50986 1 20070904 A 2810 TANK DOUG MD11 MD11F 3023600 NM BS 1245 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C RT SIDE CENTER AUX TANK STA 1245.0, X=-103.0 FOUND CORROSION AROUND FASTENER. RT SIDE CENTER AUX TANK STA 1245.0 X=-103.0 FASTENER AS MARK REMOVED. RT SIDE CENTER AUX TANK STA 1245 X=-103 CORROSION REMOVED. REWORKED ARE AS PROTECTED. FPI & HFEC INSP C/OUT ON REWORKED AREA FOUND NO CRACK & NO CORROSION. REWORKED AREAS UPP SKIN MAT'L REMO VED & REMAINED FOUND EXCEED LIMITS. FLAP PEENING C/OUT ON REWORKED AREA PER EN1642-0. 2 L 7 3 4F RT A22WE 2007110100060 20071101 00060 NM 2007 11 1 SWAA075336 1 20071025 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 727C S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007110100062 20071101 00062 NM 2007 11 1 SWAA075372 1 20071028 A 5520 DAS414A1 BUSHING BOEING 737 7373H4 1384600 NM ELEVATOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED BRDG CHECK, FOUND RT HORIZONTAL TO ELEVATOR HINGE POINT BUSHINGS CORRODED. REMOVED AND REPLACED BUSHIN GS PER MM. 2 L 7 2 4F RT A16WE 2007110100066 20071101 00066 NM 2007 11 1 SWAA075382 1 20071028 A 5322 6546546 SHEAR TIE BOEING 737 7373A4 1384585 NM BS 827 S27L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007110100078 20071101 00078 NM 2007 11 1 2007UALA04315 1 20071019 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 CILL EMERGENCY LIGHT INOP 2R. 11-01-07 RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110100089 20071101 00089 NM 2007 11 1 SWAA075240 1 20071023 A 3350 417A5703 LIGHT BOEING 737 7373H4 1384600 NM ROW ABC INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED HC1 CHECK, FOUND EEPLS INOP AT ROW 13 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007110100090 20071101 00090 NM 2007 11 1 SWAA075252 1 20071023 A 5210 507945 SKIN BOEING 737 7373A4 1384585 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR CENTER SKIN CRACKED AT LOWER END. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007110100091 20071101 00091 NM 2007 11 1 SWAA075236 1 20071023 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM BS 360 S24R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 360, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007110100092 20071101 00092 NM 2007 11 1 SWAA075237 1 20071023 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM BS 506C S14R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506C, STR 14R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007110100095 20071101 00095 NM 2007 11 1 SWAA075267 1 20071023 A 5330 6545800 SKIN BOEING 737 7373A4 1384585 NM BS 294 S14R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 294, STR 14R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007110100113 20071101 00113 NM 2007 11 1 2007UALA04322 1 20071022 A 2560 BOTTLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY OXYGEN DISCHARGED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 854UA 1731 FLIGHT DIVERTED DUE TO SEVERAL PASSENGERS REQUESTING OXYGEN AND ONBOARD SUPPLIES EXHAUSTED. EARLIER IN FLIGHT AIRCRAFT EXPERIENCED A GRADUAL LOSS OF CABIN PRESSURE, DESCENDED TO FL240, PROBLEM RESOLVED. FLIGHT CONTINUED AT FL360. FOUND C PC MALFUNCTIONED. REPLACED CPC1 WITH SERVICABLE CPC FROM THE CPC2 POSITION. NEW ITEM CREATED TO DEFER CPC2 INOP. CPC1 RE PLACED PER MM. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110100131 20071101 00131 2007 11 1 ASAA0742154 4 20071024 A 2565 69746521 CONTAINER BOEING 737 7374Q8 138447Q NM R1 DOOR SLIDE LACK OF LUBE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 769AS 25103 R1 DOOR EMERGENCY SLIDE TWISTED 90 DEGS DURING DEPLOYMENT AND USE DURING TEST BY FLIGHT CREW. LUBRICATED THE SLIDE CONT AINER LOWER FLAP HINGE (SHELF ASSY) WHICH WAS FOUND TO BE STIFF. SLIDE THEN DEPLOYED PROPERLY. 2 L 7 2 4F RT A16WE 2007110100142 20071101 00142 EU 2007 11 1 TRAX200701566 1 20071022 A 5740 SHEAR TIE AEROSP ATR72 ATR72 EU LT WING SKIN CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 LEFT WING SKIN FLANGE FOR PANEL 521DT CORRODED. BLENDED IAW SRM 57-14-12 FIG 401U/T E/C IAW NTM NO CRACKS FOUND IAW SR M 51-25-01. 2 H 7 2 4T RT 2007110100154 20071101 00154 NM 2007 11 1 2007UALA04335 1 20071019 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 331UA 24192 AFT GALLEY EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110100162 20071101 00162 NM 2007 11 1 SWAA075303 1 20071024 A 5311 6546537 FRAME BOEING 737 7375H4 138449D NM BS 578 S14R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 578, STR 14R. REPAIRED FRAME PER EA. 2 L 7 2 4F RT A16WE 2007110100170 20071101 00170 EU 2007 11 1 COEA0702919 1 20070927 A 5315 42700047 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE FUSELAGE CRACKED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 919FX 266 FOUND DURING HEAVY CHECK. FOUND M7 STC NR ST01189WI FLOORBOARD SUPPORT BEAM CRACKED IN RADIUS. REMOVED AND INSTALLED N EW FABRICATED SUPPORT BEAM. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007110100191 20071101 00191 CE 2007 11 1 DJFA2007118 1 20071017 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 417LX RK230 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER IB RIB AND BRACKET ASSEMBLIES, THE RT IB ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THI S AREA ARE OUTLINED IN BEECHJET COMMUNIQUE' NR 70. MAINTENANCE REPLACED THE RIB. 2 H 7 2 4F 4 F RT A16SW E25EA 2007110200079 20071102 00079 2007 11 2 QXEA200701619 2 20071025 A 7421 IGNITER CNDAIR CL600 CL6002C10 1390015 EA ENGINE INOPERATIVE A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 290RB 10029 PDX - ON FLIGHT 2541, NR 2 ENGINE DID NOT START. AIRCRAFT WAS RETURNED TO GATE AND MAINTENANCE PLACED IT ON MEL NR 74-1 1-1A. MEL CLEARED ON 10/26/2007 BY REPLACING LEFT IGNITION LEAD AND IGNITER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007110200095 20071102 00095 EU 2007 11 2 SIMA200729910 1 20071025 A 3150 WARNING LIGHT SAAB SF340 340B 7860101 EU NO INDICATION A SIMA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 SW 21 393AE 340B393 APR LIGHTS DID NOT ILLUMINATE DURING TAKEOFF AND CTOT WILL NOT ENGAGE. CREW ELECTED TO RETURN TO THE GATE. 2 L 7 2 4T RT A52EU 2007110200107 20071102 00107 EA 2007 11 2 SWIA200718796 1 20071023 A 2421 820465 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA ADG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 967SW 7872 FLT 5921 - ADG DEPLOYED AT ROTATION. REPLACED ADG AUTO DEPLOY CONTROL PANEL. OPS CHECK GOOD IAW MM 24-23-15. 2 L 7 2 4F RT A21EA 2007110200108 20071102 00108 EA 2007 11 2 SWIA200718797 1 20071022 A 4930 DRAIN MAST CNDAIR CL600 CL6002B19 1900309 EA APU LEAKING A SWIA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 457SW 7773 FLT 3932 - AFTER STARTING APU, THERE WAS A STRONG ODOR OF FUEL. CREW REPORTS FUEL LEAKING FROM APU DRAIN MAST. REPLACE D THE APU FUEL SHUTOFF SOLENOID VALVE IAW CRJ 200 MM 49-31-05. 2 L 7 2 4F RT A21EA 2007110200121 20071102 00121 NM 2007 11 2 QXEA200701620 1 20071022 A 3234 LATCH BOMBDR DHC8 DHC8402 1390042 NM MLG RELEASE STUCK A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 424QX 4006 SEA FLIGHT NR 2380: LANDING GEAR ALTERNATE EXTENSION DOOR WILL NOT OPEN. MAINTENANCE REMOVED AND REPLACED LANDING GEAR ALTERNATE RELEASE DOOR LATCH AND PLACARD. DOOR OPERATION NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007110200123 20071102 00123 NM 2007 11 2 QXEA200701623 1 20071023 A 2750 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS WARNING LIGHT A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 424QX 4006 SMF FLIGHT NR 2300: AFTER PUSHBACK, ENGINE START, PROPS WERE BROUGHT OUT OF FEATHER AND FLAP POWER CAUTION LIGHT ILLUMIN ATED. FLAPS WERE AT 0, AND FLAP SELECTOR WAS IN 0 DETENT. NO FLAP SELECTION HAD BEEN MADE, FLAP POWER CAUTION CHECKLIS T WAS RAN. FLAP POWER CAUTION REMAINS ILLUMINATED. MAINTENANCE CLEARED NVM, PERFORMED OPS TEST OF WING FLAP SYSTEM IAW Q400 AMM TASK 27-50-00-710-801. OPS CHECK GOOD. FAULT LIGHT CLEARED. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007110200133 20071102 00133 WP 2007 11 2 07FDEA04682 1 20071025 A 5347 ADA7656 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 MAIN CABIN ON SEAT TRACK FOUND DEEP WEAR. REPAIRED SEAT TRACK IAW SRM 57-70-00 FIG 1 VOL I. 2 L 7 3 4F RT A22WE 2007110200136 20071102 00136 WP 2007 11 2 07FDEA04685 1 20071025 A 5347 ACA7105 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 MAIN CABIN ENTRY WAY SEVERE CORROSION ON SEAT TRACK. 2 L 7 3 4F RT A22WE 2007110200138 20071102 00138 EU 2007 11 2 COEA0704919 1 20070921 A 5751 S57610176202 FITTING AEROSP ATR42 ATR42300 8680920 EU LT AILERON GOUGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 919FX 266 FOUND DURING HEAVY CHECK, TOOLING DAMAGE TO THE LT AILERON UPPER SPAR FLANGE ANGLE FITTING. REMOVED AND INSTALLED FABRI CATED ANGLE FITTING. (M) 2 H 7 2 4T RT A53EU 2007110200139 20071102 00139 EU 2007 11 2 MALA070173 1 20071028 A 6120 COMPUTER SAAB SF340 340B 7860101 EU AUTOCOARSEN MALFUNCTIONED A MALA E ENGINE SHUTDOWN O OTHER AP APPROACH 1 GL 15 423XJ 340B423 DURING LANDING IN LBE, WHEN THE POWER LEVERS WERE RETARDED, THE RT PROP AUTO COARSENED OVER THE THRESHOLD. CREW CONTINU ED THE LANDING AND SHUT DOWN ENGINE ONCE ON GROUND. PULLED FDR AND DOWNLOADED. ENGINE DID NOT SHUT DOWN IN FLIGHT. DI D BOROSCOPE P-3 LINE CHECKS, CAPPED AND UNCAPPED RUNS. COMPLETED AUTO COARSEN CHECK AND NP O/S CHECK. SELECTED NORMAL. REMOVED AND REPLACED RT ENGINE ANTI-ICING START BLEED VALVE IAW GE MM75-00-00, 2 L 7 2 4T RT A52EU 2007110500007 20071105 00007 NM 2007 11 5 ANCF200700026 1 20071025 A 3250 UNKNOWN BOEING 757 757236 1384971 NM RROYCE RB211 RB211535E4 54555 NE NLG STEERING UNKNOWN W ANCF C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 23 521NA 25592 BOG 13L. DURING ROLLING TAKEOFF, THE NOSE WHEEL STEERING GOT STUCK AND THEN THE TAKEOFF WAS REJECTED, THE AIRPLANE WENT TO THE RT, OUT OFF THE RUNWAY WITHOUT CONTROL. IN PROCCESS; THE SYSTEMS AND SUB-SYSTEMS ARE BEING CHECKED AND INSPECTED BY TROUBLESHOOTING TO DETERMINE THE FAULT CAUSES. THE COCKPIT VOICE RECORDER AND THE FLIGHT DATA RECORDER WERE REMOVED FOR READING IN SHOP. 2 L 7 2 4F 4 F RT A2NM E12EU 2007110500131 20071105 00131 EU 2007 11 5 USAA920070975 1 20071024 A 5530 D5537131800000 HINGE FITTING AIRBUS 320 A320232 3930326 EU ZONE 300 WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C-07 CHECK - RUDDER HINGE NR 1 FITTING WORN, VERTICAL STABILIZER STATION 780 / RIB 2. REPLACED RUD DER HINGE NR 1 FITTING VERTICAL STABILIZER STATION 780 / RIB 2 IAW A320 AMM 27-21-00 AND 55-36-41. 2 L 7 2 4F RT A28NM 2007110500134 20071105 00134 EU 2007 11 5 USAA920070978 1 20071015 A 5320 D53112818204 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - CORROSION ON CABIN FLOOR SUPPORT, BS 657 / FR 14 - BS 897 / FR 23, +Y254. REPLACED CA BIN FLOOR SUPPORT, BS 605 / FR 12 - BS 950 / FR 24, +Y254 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007110500141 20071105 00141 NM 2007 11 5 USAASB07092 1 20071022 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM EMERGENCY LIGHTS DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 PVD - MAINTENANCE REPORTED THE BATTERY PACK FOR THE AFT RIGHT OVERHEAD DOOR EMERGENCY LIGHT WAS VERY WEAK. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007110500144 20071105 00144 NM 2007 11 5 UPS07651008 1 20071024 A 5347 SEAT TRACK BOEING 767 76734AF 1385212 NM COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 307UP 27760 INSPECTION TYPE:SEG2 F/O'S SEAT TRACKS HAVE CORROSION. REPLACED SEAT TRACK PER SRM. 2 L 7 2 4F RT A1NM 2007110500151 20071105 00151 NM 2007 11 5 USAA920070996 1 20071018 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 827 S8L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, CRACKED FRAME, BS 827, S8L - S9L. REPAIRED FRAME BS 827, S8L - S9L IAW USAIRWAYS TYPICA L REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2007110500152 20071105 00152 NM 2007 11 5 USAA920070997 1 20071018 A 5313 STRINGER BOEING 737 7373G7 1384595 NM BS 907 S4L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, CRACKED STRINGER SPLICE, BS 907, S4L. REPLACED STRINGER SPLICE, BS 907, S4L IAW B737-30 0 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007110500153 20071105 00153 NM 2007 11 5 USAA920070998 1 20071024 A 5313 65516982 STRINGER SPLICE BOEING 737 7373G7 1384595 NM BS 907 S4R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, CRACKED STRINGER SPLICE BS 907, S4R. REPLACED STRINGER SPLICE, BS 907, S4R IAW B737-300 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007110500161 20071105 00161 NM 2007 11 5 USAA920071006 1 20071023 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 887 S26R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, CRACKED FRAME, BS 887, S26R. REPAIRED FRAME, BS 887, S26R IAW B737-300 SRM 51-70-11. 2 L 7 2 4F RT A16WE 2007110500162 20071105 00162 NM 2007 11 5 USAA920071007 1 20071014 A 5313 STRINGER SPLICE BOEING 737 7373G7 1384595 NM BS 907 S4L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, CRACKED STRINGER SPLICE, BS 907, S4L. REPLACED STRINGER, BS 907, S4L IAW B737-300 SRM 5 1-10-02. 2 L 7 2 4F RT A16WE 2007110500163 20071105 00163 NM 2007 11 5 USAA920071008 1 20071010 A 5320 WEB BOEING 737 7373G7 1384595 NM BS 328 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, CRACKED SUPPORT WEB, BS 328, LBL 10. REPLACED SUPPORT WEB, BS 328, LBL 10 IAW B737-300 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007110500173 20071105 00173 NM 2007 11 5 BB07084 1 20070926 A 3230 SEQUENCE VALVE BOEING 757 757225 1384959 NM NLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 915AW 22209 FLIGHT 567, PHX-MCO: CREW RECEIVED A GEAR DOOR WARNING LIGHT AFTER TAKEOFF. FLIGHT RETURNED TO PHX. MAINTENANCE REPLA CED THE NOSE LANDING GEAR SEQUENCE VALVE SLIDER OUTPUT CRANK. 2 L 7 2 4F RT A2NM 2007110500177 20071105 00177 NM 2007 11 5 UPS07551051 1 20071013 A 5311 7075071C FRAME BOEING 757 75724APF 1384969 NM BS 760 S22-23L DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 450UP 25472 INSPECTION TYPE:C DENT IN FWD CARGO COMPARTMENT FUSELAGE FRAME STA 760, S22L TO S23L. REPAIRED FRAME DENT STA 760L IAW SRM 53-00-07 T/E 53-09. PER DETAIL II FIG 201 SHEET 5 OF 15. RE-INSPECTION PER SRM 53-00-07 T/E 53-09 DETAIL IV ZONE 1 FIG 201 SHEET 11 OF 15 TABLE II FIG 201 SHEET 10 OF 15 CLASS B REPAIR MPI P19496. 2 L 7 2 4F RT A2NM 2007110500189 20071105 00189 NM 2007 11 5 UPS07M51037 1 20070907 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C EMP - RT HORZ STAB NR 24 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARR EL NUT BORE BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE . REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP. 2 L 7 3 4F RT A22WE 2007110500192 20071105 00192 NM 2007 11 5 UPS07M51040 1 20070917 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C EMP - RT HORZ STAB NR 25 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDS LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP. 2 L 7 3 4F RT A22WE 2007110500194 20071105 00194 NM 2007 11 5 UPS07M51042 1 20070920 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C EMP - RT HORZ STAB NR 7 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED, BORE R EAM & REMAINING BLEND OUT FOUND EXCEEDS LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE. REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP. 2 L 7 3 4F RT A22WE 2007110500201 20071105 00201 NM 2007 11 5 UPS07M51049 1 20070807 A 5350 BRACKET DOUG MD11 MD11F 3023600 NM TAIL CONE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C EMP - FWD TAIL CONE, RIGHT UPPER ALIGNMENT PIN MOUNTING BRACKET CRACKED. EMP FWD TAIL CONE AFT FUSE F IXED FAIRING 317AR REMOVED PER AMM20-50-02 R.50. EMP FWD TAIL CONE RIGHT UPPER ALIGNMENT PIN MOUNTING CRACKED AREA CUT OFF PER EN 1600-07. HFEC INSP C/O PER DACNDTSPM R.13 PT 06-10-01-001 ON CUTOFF AREA FOUND NO CRACK EVIDENT. FAB NEW CL IP, REPAIR DOUBLER & FRAME DOUBLER PER EN 1600-07. INSTALL NEW CLIP & DOUBLERS PER EN1600-07. 2 L 7 3 4F RT A22WE 2007110700029 20071107 00029 WP 2007 11 7 AALA20071990 1 20071019 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 298AA 49310 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROW 6 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROW 6. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110700030 20071107 00030 WP 2007 11 7 AALA20071991 1 20071019 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 580AA 53157 LGA - EMERGENCY LIGHTS AT SEAT ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROW 20. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110700051 20071107 00051 WP 2007 11 7 AALA20071982 1 20071018 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9402W 53138 SFO - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 17D TO 27D INOPERATIVE. REPLACED RESEATED BATTERIES IN BATTERY PACK AT SEA T ROW 20D FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 17D TO 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007110700052 20071107 00052 WP 2007 11 7 AALA20071981 1 20071018 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 3515 49892 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 18 TO 20 INOPERATIVE. REPLACED RESET BATTERY PACK AT SEAT ROW 20 FOR EMERG ENCY LIGHTS AT OVERHEAD SEAT ROWS 18 TO 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110700053 20071107 00053 NM 2007 11 7 AALA20071988 1 20071019 A 3350 P4010051112 MODULE BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 185AN 32379 SFO - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 16DEF TO 26DEF INOPERATIVE. REPLACED MODULE FOR EMERGENCY LIGHTS AT SE AT ROWS 16DEF TO 26DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007110700054 20071107 00054 NM 2007 11 7 AALA20071998 1 20071020 A 2621 AAP3353 EXTINGUISHER BOEING 737 737823 13844BZ NM CARGO BAY DISCHARGED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 921AN 29522 RDU INFLIGHT T1256/20OCT MIA TO LGA - CARGO FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED IN FLIGHT. REPLACED CARGO COM PARTMENT FIRE EXTINGUISHER BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007110700055 20071107 00055 2007 11 7 QXEA200701626 4 20071026 A 3418 C16258AA TRANSDUCER CNDAIR CL600 CL6002C10 1390015 EA STALL WARNING FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 617QX 11023 10130 DEN - ON FLIGHT 4275, RECEIVED A "STALL FAIL" CAUTION MESSAGE. PUSHER WAS SELECTED OFF PER EA CHECKLIST. MAINTENANCE R EMOVED AND REPLACED R ANGLE-OF-ATTACK TRANSDUCER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007110700056 20071107 00056 2007 11 7 QXEA200701627 4 20071028 A 2350 601R591447 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA AUDIO SYSTEM FAILED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 607QX 13225 10024 PDX - ON FLIGHT 2512, CAPTAIN'S SIDE MIC WAS INOPERATIVE. AC WAS RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED AU DIO ELECTRONIC CONTROL UNIT (AECU ). OPERATIONAL CHECK TESTS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007110700057 20071107 00057 NM 2007 11 7 QXEA200701628 1 20071028 A 3220 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM NLG VIBRATES A QXEA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 NM 09 400QX 4030 SMF - ON FLIGHT 2240, LIGHT BUMPING WAS ASSOCIATED WITH TAXI SPEED. AIRCRAFT WAS RETURNED TO GATE. MAINTENANCE INSPECT ED MAIN AND NOSE GEAR TIRES AND AREA. NO ABNORMAL NOISES NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007110700058 20071107 00058 2007 11 7 QXEA200701629 4 20071028 A 3414 INDICATOR BOMBDR DHC8 DHC8402 1390042 NM AIRSPEED MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 405QX 4047 LAX - ON FLIGHT 2330, FLIGHT OFFICER'S AIRSPEED INDICATOR SHOWS ALL RED. AIRCRAFT WAS RETURNED TO GATE. MAINTENANCE CY CLED AIRCRAFT POWER. FO'S DISPLAY SHOWS NORMAL. OPERATIONS CHECKS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007110700059 20071107 00059 2007 11 7 HALA0700459 4 20071023 A 3460 LAMP BOEING 767 76733A 1385209 NM NLG INDICATOR INOPERATIVE A HALA L ABORTED APPROACH P NO WARNING INDICATION LD LANDING 1 WP 13 591HA 33423 NOSE GEAR (DOWN) LIGHT INOP. RELAMPED DOWN NOSE GEAR INDICATION LIGHT. OPS CHECK OK. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007110700060 20071107 00060 NM 2007 11 7 HALA0700449 1 20071013 A 2150 R25104 RELAY BOEING 717 717200 1383700 NM A/C PACK UNKNOWN A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 485HA 55130 ATB - LOST BOTH AC PACKS ON T/O. ACCOMPLISHED FIM 21-22- TASK 805 BITE CHECK FCC-1 AND FCC-2. NO FAULTS NOTED. REPLAC ED R2-5104 PER AWB 21-51-00 TEST OKAY. 2 L 7 2 4F TR A6WE 2007110700063 20071107 00063 NE 2007 11 7 HALA0700452 2 20071021 A 7532 BLEED VALVE BOEING 767 767300 1385204 NM PWA 4060 PW4060 52119 NE LT ENGINE MALFUNCTIONED A HALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 596HA 23276 ETOPS SIGNIFICANT SYSTEM - ATB - LEFT ENG BLEED VALVE CAME ON. DID QRH PROC, NO CHANGE DIVERTED TO SFO FOR MX. NO FURTH ER PROBLEMS. (HPSOV LOCKED CLOSED SHORTING PLUG INSTALLED). OK TO CONTINUE PER C 36-11-2. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110700064 20071107 00064 NM 2007 11 7 HALA0700453 1 20071020 A 2612 89973202 CIRCUIT CARD BOEING 767 76733A 1385209 NM RROYCE BR700 BR700715A130 NE FIRE DETECTION MALFUNCTIONED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 589HA 33422 NR 1 ENG B-LOOP EICAS MESSAGE. CHECKED NR 1 ENG LOOP B WIRING NOTED OK PER AMM 26-10-01-401. FIRE DETECTION CARD FILE REMOVED/INSTALLED GROUND ENG RUN OPERATIONAL CK OK. 2 L 7 2 4F 4 F RT A1NM E00061EN 2007110800001 20071108 00001 CE 2007 11 8 194WA10232007 1 20071023 A 2913 993880027 POWERPACK BEECH 99 99 1154002 CE HYDRAULIC SYSTEM SEIZED E AXSA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 65 194WA 4475 4475 U64 FLIGHT 1060 MHT-PWM DURING APPROACH FOR RWY 29 PILOT SELECTED GEAR DOWN (3 GREEN LIGHTS INDICATED) AND NOTED THE SMELL O F SMOKE. THE COCKPIT BEGAN TO FILL WITH SMOKE AND THE PILOT NOTED THE LANDING GEAR CIRCUIT BREAKER POPPED. THE PILOT M ADE A NORMAL APPROACH AND LANDING. THE AIRCRAFT WAS PARKED AND UNLOADED AND COMPANY WAS NOTIFIED. A FERRY PERMIT WAS O BTAINED FROM PWM FSDO AND THE AIRCRAFT WAS MOVED TO MHT. INSPECTION REVEALED THE LANDING GEAR HYDRAULIC POWER PACK SEIZ ED CAUSING THE ELECTRIC MOTOR TO FAIL RESULTING IN THE ACCUMULATION OF SMOKE IN THE COCKPIT. THE ELECTRIC MOTOR AND HYD RAULIC POWER PACK WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 2 3T A14CE 2007110800003 20071108 00003 2007 11 8 C2XA07CL092 4 20071030 A 2211 7021170951 COMPUTER EMB 145 EMB145LR 3260212 SO AUTOPILOT SYSTEM SHORTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 14953 145071 CLEVELAND MAINTENANCE REPORTED THE GUIDANCE CONTROL UNIT (GC-550) HAD SMOKE COMING FROM IT. MAINTENANCE INSPECTED AND R EPLACED THE GUIDANCE CONTROL COMPUTER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007110800004 20071108 00004 CE 2007 11 8 DXTA200702566 1 20071024 A 3246 315381 WHEEL CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG VIBRATES E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 929QS 289 289 7500129 AT THE BEGINNING OF TAKE-OFF ROLL THE NOSE WHEEL STARTED TO SHIMMY AS THE AIR SPEED INCREASED THE SHIMMY BECAME WORSE. T AKE OFF WAS ABORTED. REMOVED LH NLG WHEEL ASSY P/N 3-1538-1 S/N 0060 &INSTALLED OVERHAULED ASSY P/N 3-1538-1 S/N ON 037 0. REMOVED RH NLG WHEEL ASSY P/N 3-1538-1 S/N 0847 &INSTALLED OVERHAULED ASSY P/N 3-1538-1 S/N 0681 PER CE750 MM 32-41-0 1. ALL TESTS PASS AT THIS TIME. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007110800009 20071108 00009 NM 2007 11 8 2007UALA04407 1 20071025 A 2560 PLATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 CORROSION FOUND ON DOORS 2R, 1R & 1L ESCAPE SLIDE GIRT BAR LOCK PLATES. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110800011 20071108 00011 NM 2007 11 8 DXTA200702571 1 20071024 A 2150 CONDESOR AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE CABIN AIR ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 07 203QS 198 AFTER LANDING AND APU START, VERY STRONG ODOR OF RAW JET FUEL IS COCKPIT AND CABIN. RAN APU. NOTED MUSTY ODOR COMING F ROM VENTS. AFTER 2 MINUTES ODOR BEGAN TO DISIPATE. REMOVED AND INSPECTED THE WATER SEPERATOR AND THE WATER SEPERATOR F ILTER. NO DISCREPANCIES NOTED. REMOVED AND INSPECTED THE CONDENSOR. NOTED STRONG MUSTY ODOR COMING FROM THE CONDENSOR . CLEANED THE CONDENSOR, WATER SEPERATOR, AND FILTER. RAN APU. NO DISCREPANCIES NOTED. OPS CHECK GOOD. PERFORMED A LEAK CHECK OF THE WATER SEPERATOR, FILTER, AND CONDENSOR. LEAK CHECK GOOD. WORK DONE IAW CH. 21-505 AND 21-206 OF THE F-2000 MM. 2 L 7 2 4F 4 F RT A50NM E44NE 2007110800013 20071108 00013 NM 2007 11 8 2007UALA04411 1 20071024 A 2432 18550000 BATTERY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE MAIN DISCHARGED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 673UA 29241 MAIN BATTERY DEAD. REPLACED MAIN BATTERY PER MM 24-31-01, OPS OK. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110800015 20071108 00015 EU 2007 11 8 2007UALA04412 1 20071026 A 2910 FLUID AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYDRAULIC SYSTEM DISCHARGED A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 406UA 454 WHILE TAXIING LOST NOSE WHEEL STEERING, FOLLOWED BY HYD GREEN RSVR LOW LVL STATUS MESSAGE. ALL GREEN SYSTEM FLUID DUMPE D ONTO RAMP FROM AIRCRAFT WHEEL WELL AREA. FOUND DAMAGED GREEN SYS HYD LINE IN AFT PIT UNDER FLOOR, RING LOCK PULLED AP ART. REPAIRED GREEN SYS HYD LINE (RING LOCK REPAIR PLUS A NEW LINE) SERVICED GREEN HYD SYS- NO LEAKS NOTED, ALL SYSTE MS REPORTING NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110800020 20071108 00020 EU 2007 11 8 2007UALA04416 1 20071027 A 3500 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LOW A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 459UA 1192 OXYGEN LEVEL READS LOW. SERVICED 02 SYSTEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110800022 20071108 00022 NM 2007 11 8 2007UALA04419 1 20071027 A 3210 SUPPORT FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RT MLG CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 RT MLG OUTBOARD AFT SUPPORT FITTING IS CRACKED AT TRAILING EDGE NR 2 HOLE AT THE 6 O'CLOCK POSITION. MAJOR REPAIR ACCO MPLISHED, INSTALLED REPLACEMENT FITTING 2 L 7 2 4F 4 F RT A16WE E21EU 2007110800024 20071108 00024 NM 2007 11 8 2007UALA04420 1 20071026 A 2620 CONTROL PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FIRE BOTTLE FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 379UA 24654 CARGO FIRE DET SYSTEM 1ST BOTTLE ARMED GREEN LIGHT IS ILLUM. ARM SWITCH IS AUTO. SYSTEM TEST OK. REPLACED CARGO FIRE CONTROL PANEL- ALL INDICATIONS ARE NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110800026 20071108 00026 NM 2007 11 8 2007UALA04421 1 20071027 A 2621 METERING VALVE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FIRE BOTTLE LEAKING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 379UA 24654 CARGO FIRE BOTTLE 2 ARMED LIGHT INOP WITH BOTH BITE AND LIGHTS TEST. FOUND LEAKING SQUIB. REPLACED FIRE BOTTLE AND M ETERING VALVE. NO LEAKS, NO REPEATS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110800030 20071108 00030 NM 2007 11 8 2007UALA04424 1 20071027 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY LIGHTS AT ROWS 2J FWD & 5F FWD ARE INOPERATIVE. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110800034 20071108 00034 NM 2007 11 8 2007UALA04427 1 20071027 A 5320 141N516079 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 MAIN CABIN FLOOR SUPPORT CORRODED STA 324 TO 377, RBL 6 0. MAJOR REPAIR ACCOMPLISHED: REPLACED FLOOR SUPPORT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110800035 20071108 00035 NM 2007 11 8 2007UALA04428 1 20071027 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCONNECTED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 EMERGENCY LIGHT ON OVERHEAD AISLE DISCONNECTED AND HANGING LOOSE. SECURED LIGHT ASSEMBLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110800038 20071108 00038 NM 2007 11 8 2007UALA04430 1 20071028 A 2560 SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 588UA 26717 CREW REPORT: DOOR 1R ARMING LIGHT WILL NOT STAY ILLUMINATED IT IS OFF WITH DOOR ARMED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110800039 20071108 00039 NM 2007 11 8 2007UALA04431 1 20071028 A 2750 BRACKET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE T/E FLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 LEFT WING, NR 2 FLAP TRACK JACKSCREW FITTING ON INBOARD SIDE, FITTING ASSY-TRACK GEAR BOX SUPPORT, P/N 113N1304-7 IS CRA CKED ON INBOARD LOWER RADIUS FOR NEAR FAIRING ATTACH. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110800040 20071108 00040 NM 2007 11 8 2007UALA04432 1 20071028 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 DOOR R1 HANDLE BOX CRACKED AT CAM BASKET HOLES. INSTALLED SERVICEABLE HANDLE BOX. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110800041 20071108 00041 NM 2007 11 8 2007UALA04433 1 20071028 A 5753 FITTING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE T/E FLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 RIGHT WING NR 7 FLAP TRACK, FITTING ASSY TRACK GEARBOX IS CRACKED, INBOARD SIDE NEAR FLAP FAIRING ATTACH POINT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110800042 20071108 00042 NM 2007 11 8 2007UALA04435 1 20071026 A 2560 FASTENER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 CORRODED FASTENERS IN DOOR R4 ESCAPE SLIDE GIRT BAR LOCK PLATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110800044 20071108 00044 NM 2007 11 8 2007UALA04437 1 20071027 A 2697 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 PYLON BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 NR 2 PYLON L/E FIRE LOOP -A- HAS BROKEN CONNECTOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110800050 20071108 00050 NM 2007 11 8 2007UALA04449 1 20071026 A 8010 STARTER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 MAKING METAL A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 NR 2 ENG STARTER MAG CHIP DETECTOR SHOWS LARGE FLAKES OF METAL. ALSO THE NR 1 ENG STARTER DRAINED AN INSUFFICIENT AMOUN T OF OIL. ALSO BLACK AND BURNED AND HAS AN ODOR. NR 1 STARTER FOUND WITH LOW OIL AND OIL LOOKS BLACK AND BURNED REPLAC ED STARTER. AFTER SERVICING NR 2 STARTER FOUND WITH LARGE METAL CHIPS. REPLACED NR 2 STARTER. AC OK FOR SERVICE 2 L 7 2 4F 4 F RT A1NM E24NE 2007110800056 20071108 00056 WP 2007 11 8 ABXA070351 1 20071006 A 5320 39135771 INTERCOSTAL DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 CRACKED INTERCOSTAL AT STA 775, LEFT BUTT LINE 52-5, AS VIEWED FROM OUTBOARD LIGHTENING HOLES. BLENDED OUT DAMAGE IAW D C9 SRM. 2 L 7 2 4F A6WE 2007110800059 20071108 00059 WP 2007 11 8 ABXA070353 1 20071005 A 5320 99105035 CUSP WEB DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 962AX 47768 CUSP WEB CRACKED AT STA 1022 - 1036. REPLACED CUSP WEB AS REQUIRED IAW DC9 SRM. 2 L 7 2 4F A6WE 2007110800060 20071108 00060 WP 2007 11 8 ABXA070354 1 20071005 A 5320 99105035 CUSP WEB DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 962AX 47768 CUSP WEB CRACKED ON LEFT SIDE AT STA 980. REPAIRED CRACKED WEB IAW REA E-43520. 2 L 7 2 4F A6WE 2007110800061 20071108 00061 WP 2007 11 8 ABXA070355 1 20071006 A 5230 3913249503N FITTING DOUG DC9 DC941 302207N WP AFT CARGO BAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 962AX 47768 AFT LOWER CARGO DOOR BEAM END FITTING WAS CRACKED AFT END OF NR 2 BEAM. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30- 5. 2 L 7 2 4F A6WE 2007110800062 20071108 00062 WP 2007 11 8 ABXA070357 1 20071008 A 5210 99557529 ANGLE DOUG DC9 DC941 302207N WP PAX DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 962AX 47768 MAIN ENTRY DOOR UPPER AFT CORNER, ANGLE CRACKED INSIDE LIGHTENING HOLE. REPAIRED MAIN ENTRY DOOR UPPER AFT ANGLE IAW DC 9 SRM. 2 L 7 2 4F A6WE 2007110800066 20071108 00066 EA 2007 11 8 TRAX200701652 1 20071031 A 5340 S61444 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 LBL 27 O/B CLIP CRACKED. REMOVED CRACKED CLIP FS 484 LBL 27 O/B. FABRICATED NEW ANGLE IAW CRJ 200 SRM 53-41-43. OK T O ALODINE AND PRIME. ALODINED AND PRIMED, IAW CRJ 200 SRM 51-21-11. OK TO TOPCOAT, APPLIED TOPCOAT, IAW SRM 51-21-16. O K TO INSTALL NEW CLIP. INSTALLED NEW CLIP, IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007110800070 20071108 00070 WP 2007 11 8 ABXA070358 1 20071008 A 5310 59124921 DOOR FRAME DOUG DC9 DC941 302207N WP FUSELAGE GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 962AX 47768 DOOR JAMB STA 200, LONGERON 15 RIGHT GOUGED. REPAIRED DOOR JAMB IAW DC9 SRM. 2 L 7 2 4F A6WE 2007110800071 20071108 00071 NM 2007 11 8 ASAA0772163 1 20071019 A 5320 1464940121 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 AFT CARGO PIT FLOOR SUPPORT TEE CORRODED BS 887 RBL 20. REPLACED WITH NEW PART. 2 L 7 2 4F RT A16WE 2007110800088 20071108 00088 EA 2007 11 8 TRAX200701601 1 20071026 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 974EV 7594 F/A AND PASSENGERS REPORTED MOMENTARY ELECTRICAL BURNING SMELL AT 7A/B IN FLIGHT. APU NOT RUNNING, WING AND COWL ANTI-I CE ON. NO SMELL IN LAV OR COCKPIT. FLT 4673 DEL 60 MINS. 2 L 7 2 4F RT A21EA 2007110800089 20071108 00089 EA 2007 11 8 TRAX200701602 1 20071026 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 846AS 7328 RECEIVED A SMOKE TOILET MESSAGE IN FLIGHT. EN ROUTE TO GRK A/C DIVERTED TO MGM DUE TO MTC. EMERGENCY DECLARED. EMERGE NCY EQUIPMENT ON STANDBY. FLT 4549 DEL 63 MINS. 2 L 7 2 4F RT A21EA 2007110800091 20071108 00091 EU 2007 11 8 07FDEA04691 1 20071026 A 2131 82010C051100 CONTROLLER AIRBUS 300 A300B4605R 3930308 EU CABIN PRESSURE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 662FE 12052 643 761 AT FL 330 CABIN V/S CONSTANTLY AT 150 CLIMB, FWD OUTFLOW VALVE SHOWED NEARLY OPEN SYS 1 REG FAULTED. SYS 2 TOOK OVER A S NECESSARY BUT CABIN V/S INCREASED TO 200FPM, THEN SELECTED MANUAL BUT OUTFLOW VALVE WOULD NOT CLOSE. ELECTED TO MAKE PRECAUTIONARY LANDING IN PHX AS UNABLE TO MAINTAIN CABIN ALT BELOW 10,000FT. FOLLOWED ALL ECAM AND QRH PROCEDURE ACN RELEASED FOR SERVICE PER MEL/CDL: 21-31-02-A CATEGORY: C EXPIRATION: 05NOV07 , FLT CONTINUED TO MEM AND IS INWORK: REM OVED AND REPLACED NR 1 CABIN CONTROLLER AND AFT OUTFLOW VALVE (21-30/9624). TEST SYSTEM 21-31-00-5. 2 L 7 2 4F RT A35EU 2007110800092 20071108 00092 EA 2007 11 8 TRAX200701603 1 20071026 A 2560 MEGAPHONE CNDAIR CL600 CL6002C10 1390015 EA CABIN INTERMITTENT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 F/A REPORT MEGAPHONE WORKS INTERMITTENTLY. FLT 4469 DEL 86 MINS. 2 L 7 2 4F RT A21EA 2007110200120 20071102 00120 NM 2007 11 2 AMTA200700532 1 20071019 A 5321 FLOOR PANEL BOEING 757 75733N 1384931 NM BS 1330-1470 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 550TZ 32584 AFT CARGO COMPARTMENT FLOOR PANEL 161BF HAS CORROSION ON UPPER AND LOWER SURFACE NUMEROUS AREAS, STATION 1330 TO 1470 LB L 20 TO RBL 20. FABRICATED NEW PANEL 161BF IAW SRM 53-60-53 FIG 1 MATERIAL 2024 T-3 .071, TREATED 51-20-01 SRM. (M) 2 L 7 2 4F RT A2NM 2007110200140 20071102 00140 SO 2007 11 2 SIMA200729915 1 20071018 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AE 20383 5000 145079 DURING A MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 29 WAS FOUND TO BE CORRODED. REMOVED CORRODED AREA AND REPLACED A REA IAW SRM 53-00-10. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007110200142 20071102 00142 EA 2007 11 2 SIAM200729706 1 20071022 A 3020 54011485 ANTI-ICE SYSTEM CNDAIR CL600 CL6002C10 1390015 EA MALFUNCTIONED A SIMA A UNSCHED LANDING L NO TEST CL CLIMB 1 SW 21 505AE 10053 CREW REPORTED DURING CLIMB-OUT OF DFW GOT A RIGHT COWL ANTI ICE CAUTION FOLLOWED AOM AND RETURNING TO DFW. REMOVED AND REPLACE A/I VALVE IAW CRJ 700 MM 30-20-00. OPERATIONAL CHECK OK IAW CRJ 700 AMM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007110200146 20071102 00146 SO 2007 11 2 SIMA200729702 1 20071023 A 3260 PROXIMITY SWITCH EMB 135 EMB135KL 3260302 SO NLG OUT OF ADJUST A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 816AE 145552 LANDING GEAR LEVER FAIL ON TAKEOFF RETURNED TO MIA. JACKED ACFT INSPECTED MLG PROX SWITCH CLEARANCES WITHIN LIMITS. IN SP NLG PROX SWITCHES AND ADJUSTED PROX SWITCH. PERFORMED GEAR RETRACTION OF LANDING GEAR OPERATIONAL CHECK GOOD. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007110200150 20071102 00150 NM 2007 11 2 AMTA200700518 1 20071017 A 5313 LONGERON BOEING 757 75733N 1384931 NM BS 1330 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 550TZ 32584 AFT CARGO PIT LONGERON HAS CORROSION STATION 1330 RBL 16.10. REMOVED CORROSION MATERIAL LOSS .026 OUT OF LIMITS REPAIRE D IAW SRM 53-60-53, 53-00-53. (M) 2 L 7 2 4F RT A2NM 2007110200152 20071102 00152 NM 2007 11 2 AMTA200700543 1 20071019 A 5321 FLOOR PANEL BOEING 757 75733N 1384931 NM FS 1330-1470 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 550TZ 32584 AFT CARGO COMPARTMENT FLOOR PANEL 153BF HAS CORROSION UPPER AND LOWER SURFACE. FABRICATED NEW PANEL IAW 53-60-53. (M) 2 L 7 2 4F RT A2NM 2007110200153 20071102 00153 EU 2007 11 2 MALA070166 1 20071022 A 3020 DEICE SYSTEM SAAB SF340 340B 7860101 EU LT INTAKE SHORTED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 441XJ 340B441 BURNING SME LEFT ENGINE INTAKE DE-ICE MAT HAS SHORT AND BURNED THROUGH. REMOVED AND REPLACED LT LOWER DUCT ASSY P/N OFF AND ON NH24668-165 SN OFF L198082 SN ON L169214 REF SAAB JC NR 7160-301. 2 L 7 2 4T RT A52EU 2007110200154 20071102 00154 2007 11 2 SIMA200729703 2 20071023 A 7532 321935 BLEED VALVE SAAB SF340 340B 7860101 EU RT ENGINE MALFUNCTIONED A SIMA C ABORTED TAKEOFF L NO TEST TO TAKEOFF 1 SW 21 298AE 340B298 ON TAKEOFF WHEN CREW SELECTED RT BLEED CLOSED. CREW DID NOT GET RT BLEED CLOSE LIGHT. CREW ABORTED TAKEOFF AND RETURNE D TO THE GATE FOR MAINTENANCE. REMOVED AND REPLACED RT ENG HIGH PRESS BLEED AIR VALVE IAW SAAB 340 AMM 36-11-10-02. OP S CK GOOD. NO DEFECTS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007110200155 20071102 00155 CE 2007 11 2 UIEA200700462 1 20071024 A 5414 SKIN CESSNA 337 T337G 2075726 CE GE CF6 CF650E2 30018 NE NR 4 NACELLE CRACKED C UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 424 P3370259 NR 4 PYLON LT SKIN WAS FOUND CRACK AT 483AL ACCESS PANEL CUTOUT LOWER AFT CORNER. 1 H 7 2 3O 4 F A6CE E23EA 2007110500104 20071105 00104 NM 2007 11 5 ASMF200710010 1 20071028 A 3241 26123021 BRAKE ASSY BOEING 737 737* NM CFMINT CFM567 CFM567B22 13802 NE RIGHT LEAKING W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 904AM 6562 28262 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, DUE TO AIRPORT BEING CLOSE. MAINTENANCE PERSONNEL DETECTED A HYDRAULIC LEAK IN THE MAIN LANDING GEAR BRAKE NR 2. MAINTENANCE PERSONNEL REPLACED THE BRAKE NR 2 IAW MM 32-41-41, TESTED CORRECT. LATE R DURING OVERNIGHT CHECK, BRAKES SYSTEM TEST WAS PERFORMED IAW MM 32-41-41, ALL CORRECT. OVERWEIGHT LANDING INSPECTION W AS NOT NECESSARY DUE TO THE AIRCRAFT LANDED WITH 50048 KG AND THE MAXIMUM LANDING WEIGHT IS 58059 KG. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007110500147 20071105 00147 NM 2007 11 5 UPS07651012 1 20071024 A 5347 SEAT TRACK BOEING 767 76734AF 1385212 NM COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 307UP 27760 INSPECTION TYPE:SEG2 C.O.'S I/B AFT SEAT TRACK IS CORRODED BEYOND LIMITS. REPLACED PER SRM. 2 L 7 2 4F RT A1NM 2007110500165 20071105 00165 NM 2007 11 5 USAA920071010 1 20071015 A 5330 143N36504 SKIN BOEING 757 7572B7 1384964 NM BS 750-780 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON FUSELAGE SKIN, BS 750 - BS 780, S18L - S21L. REPAIRED FUSELAGE SKIN, BS 75 0 - BS 780, S18L - S21L IAW B757 SRM 53-00-01 FIGURE 201. 2 L 7 2 4F RT A2NM 2007110500166 20071105 00166 2007 11 5 WRNA200700057 4 20071023 A 3414 0851HV PITOT TUBE AIRBUS 300 A300B4203 3930306 EU LEAKING A WRNA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 05 510TA 100 DURING TAKEOFF THE FIRST OFFICERS AIRSPEED INDICATOR LAGGED 40-60 KNOTS BEHIND CAPTAINS AIRSPEED INDICATOR. FOUND RT PI TOT PROBE LEAKING, REPLACED RT PITOT PROBE IAW A300 MM 34-11-15 PAGE 401. ACCOMPLISHED LEAK CHECK IAW A300 MM 34-11-10 PAGE 501. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A35EU 2007110500175 20071105 00175 EU 2007 11 5 UPS07151005 1 20071024 A 7500 DUCT AIRBUS A300 A300F4622R 3930360 EU BLEED AIR CONTAMINATED A IPXA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 01 143UP 0826 INSPECTION TYPE:N/A DIVERSION - AFT & BULK SMOKE DETECTED IN FLIGHT. BOTH BOTTLES DISCHARGED. *S/D* PERFORMED CARGO C OMP SMOKE DET ADJ/TEST PROCEDURE IAW MM 26-16-00-05 ALL SYS CHECKED GOOD. REMOVED 4 EA DUCTS FWD OF MIXING CHAMBER FOUN D HYDRAULIC FLUID RESIDUE. CLEANED PER 20 -41-11-00. REINSTALLED 4EA DUCTS & LEAK CHECKED GOOD. RAN ENGS & APU WITH A LL ZONES TO DUCT TEMP. 2 L 7 2 4F RT A35EU 2007110500181 20071105 00181 NM 2007 11 5 UPS07M51029 1 20070831 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C EMP - LT HORZ STAB NR 27 BARREL NUT BORE FOUND CORROSIONS. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BAR REL NUT BORE BLEND OUT VOIDS, BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE . REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT AP. 2 L 7 3 4F RT A22WE 2007110500186 20071105 00186 NM 2007 11 5 UPS07M51034 1 20070907 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C EMP - LT HORZ STAB NR 11 BARREL NUT BORE FOUND CORROSIONS. CORROSION AT BARREL NUT BORE REMOVED, BORE REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BAR REL NUT BORE BLEND OUT VOID & BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE . REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP. 2 L 7 3 4F RT A22WE 2007110500190 20071105 00190 NM 2007 11 5 UPS07M51038 1 20070907 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C EMP - RT HORZ STAB NR 27 BARREL NUT BORE FOUND CORROSION. CORROSION AT BARREL NUT BORE REMOVED. BORE REAM & REMAINING BLEND OUT FOUND EXCEEDING LIMITS. 10X MAGNIFICATION DETAIL VISUAL INSP C/OUT FOUND NO CORROSION. BAR REL NUT BORE BLEND OUT VOIDS, BOTTOM PERIPHERY RADIUS SMOOTHEN & PROTECTED. C/OUT FR PRIMER TOUCH UP AT BARREL NUT BORE . REPAIR SLEEVE BUSHING FAB & PROTECTED. PR 1422 B1/2 SEALANT APP. 2 L 7 3 4F RT A22WE 2007110500199 20071105 00199 NM 2007 11 5 UPS07M51047 1 20070816 A 5320 FLOOR SUPPORT DOUG MD11 MD11F 3023600 NM BS 1841 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C CENTER CARGO COMPT AT STATION 1841,X-56 TO X+56 FOUND FLOOR SUPPORT W WITH SURFACE CORROSION. CENTER CARGO COMPT STA 1841 X=56 LT-56 RT FLOOR SUPPORT CORROSION REMOVED FOUND EXCEED LIMIT PER SRM 53-00-01 FIG 1A VI R38. F PI C/O PER DACNDTS PM R.13 PT 08 ON REWORK AREA FOUND NO CORROSION EVIDENT. REPAIR ANGLE QTY 03EA FAB PER EN 1659-07. FLOOR SUPPORT RWK AREA & REPAIR ANGLE 3EA REPROTECT PER SRM 51-21-01 VII. REPAIR ANGLES 3EA INSTL PER EN 1659-07. 2 L 7 3 4F RT A22WE 2007110500205 20071105 00205 NM 2007 11 5 CALA0700612 1 20071026 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM BS 400 S8R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11612 27325 INSPECTION FOUND A .5 INCH CRACK IN AFT SIDE OF FUSELAGE FRAME AT STA 400 AROUND RIVET BELOW S8R. THE FRAME WAS REPAIRE D IAW ECRA 5310-04668. 2 L 7 2 4F RT A16WE 2007110500206 20071105 00206 NM 2007 11 5 CALA0700613 1 20071026 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM BS 400 S8L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11612 27325 INSPECTION FOUND A .5 INCH CRACK IN AFT SIDE OF FUSELAGE FRAME AT STA 400 AROUND RIVET BELOW S8L. THE FRAME WAS REPAIRE D IAW ECRA 5310-04668. 2 L 7 2 4F RT A16WE 2007110500217 20071105 00217 NM 2007 11 5 CALA0700624 1 20071027 A 5311 6546555 FRAME BOEING 737 7373T0 1384582 NM BS 867 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 867, S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04669. 2 L 7 2 4F RT A16WE 2007110500222 20071105 00222 NM 2007 11 5 USAA920071021 1 20071021 A 5340 693535214 STRINGER CLIP BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED STRINGER TIE CLIP, BS 639, S4L. REPLACED STRINGER TIE CLIP, BS 639, S4L IAW B7 37-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007110500223 20071105 00223 NM 2007 11 5 USAA920071022 1 20071022 A 5340 693535214 STRINGER CLIP BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED STRINGER TIE CLIP, BS 616, S4R. REPLACED STRINGER TIE CLIP, BS 616, S4R IAW B7 37-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007110500224 20071105 00224 EU 2007 11 5 USAA920071023 1 20071014 A 5321 D5367180500400 FLOORBOARD AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - CORROSION ON CABIN FLOORBOARD 261FF, BS 3158 / FR 66 - BS 3257 / FR 68. REPLACED CABIN FLOORBOARD 261FF, BS 3158 / FR 66 - BS 3257 / FR 68 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007110500234 20071105 00234 2007 11 5 2007UALA04398 4 20071025 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE DOOR 2L FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 405UA 452 DOOR 2L SLIDE WILL NOT ARM. ATTACH POINTS WERE FOUND DISLODGED. REPLACED BOTH ATTACH (UPPER) ASSYS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110500238 20071105 00238 NM 2007 11 5 2007UALA04402 1 20071026 A 5754 STRUCTURE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 1 SLAT DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 852UA 1671 CREW REPORTS EVIDENCE OF BIRDSTRIKE ON LT WING INBOARD OF ENG WITH SIGNIFICANT DENT. NR 1 L/E SLAT LT WING DENT MEASURE S .46875 DEEP, 3.5 WIDE AND 5.25 LONG, OUT OF LIMITS. REPLACED NR 1 LE SLAT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110500239 20071105 00239 NM 2007 11 5 2007UALA04403 1 20071025 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 303 S4L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 PASSENGER CABIN BS 303 AT STR 4L HAS CRACKED INTERCOSTAL. MAJOR REPAIR ACCOMPLISHED, REPLACING BS 303, S4L INTERCOSTAL . 2 L 7 2 4F 4 F RT A16WE E21EU 2007110500240 20071105 00240 NM 2007 11 5 2007UALA04404 1 20071025 A 2621 FIRE BOTTLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NACELLE LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 341UA 24245 FWD ENGINE FIRE BOTTLE PRESSURE AT LIMIT. REPLACED BOTTLE OF FWD ENG SYS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110600005 20071106 00005 EU 2007 11 6 07FDEA04699 1 20071029 A 5755 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 5 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 729FD TS0418 657 FOUND DELAMINATION ON UPPER SKIN OF SPOILER 5 RT. REPAIR PERFORMED BY REPLACEMENT OF SPOILER IAW AMM 276151 PB 400. 2 L 7 2 4F RT A35EU 2007110600008 20071106 00008 NM 2007 11 6 07FDEA04707 1 20071101 A 5311 FRAME DOUG MD11 MD11F 3023600 NM BS 1701 L12L CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 527FE 48601 MAIN DECK LEFT SIDEWALL STRUCTURE, FRAME STA 1701 CRACKED AT LONGERON 12. REPAIR CARRIED OUT AT MAIN DECK LEFT HAND SI DEWALL STRUCTURE, FRAME STA 1701, LONGERON 12 AS PER SRM 53-30-00 FIGURE 1 VOLUME I AND SRM 51-33-01 VOLUME II. REPAI R CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007110600016 20071106 00016 NM 2007 11 6 2007UALA04379 1 20071024 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 660 S24L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 FWD PIT STA 660 MAIN FRAME BETWEEN STR 24L AND 25L HAS 1 DENT. MAJOR REPAIR ACCOMPLISHED: REMOVED PRODUCTION SPLICE & S TRINGER CLIP AT STR 24L. CUTOUT RIB DAMAGE. INSTALLED REPAIR PER SRM 53-00-07 & SRM 51-40-02 FROM 3" BELOW STR 37L TO 1" ABOVE STR 24L. NEW STR CLIP INSTALLED AT STR 24L. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110600017 20071106 00017 EU 2007 11 6 TRAX200701562 1 20071022 A 5310 CREASE BEAM AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 CREASE BEAM CORRODED AT STR 14 BETWEEN FR 13+17. REPAIRED. 2 H 7 2 4T RT 2007110600018 20071106 00018 EU 2007 11 6 TRAX200701563 1 20071022 A 5310 CREASE BEAM AEROSP ATR72 ATR72 EU FUSELAGE NONE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 RIGHT CREASE BEAM ZEE FLOOR CORRODED AT FLOORBEAM 40. FOUND WITHIN LIMITS. 2 H 7 2 4T RT 2007110600019 20071106 00019 EU 2007 11 6 TRAX200701564 1 20071022 A 5315 FLOORBEAM AEROSP ATR72 ATR72 EU FUSELAGE NONE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 FLOORBEAM 36 TOP SURFACE CORRODED. CORROSION REMOVED, FOUND WITHIN LIMITS. 2 H 7 2 4T RT 2007110600020 20071106 00020 EA 2007 11 6 TRAX200701578 1 20071023 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 FLOOR SUPPORT ANGLE AT PAX DOOR ENTRANCE HAS CORROSION. REMOVED CORROSION FROM FLOOR SUPPORT ANGLE AT PAX DOOR ENTRANCE IAW CRJ 200 SRM 51-21-06. OK TO ALODINE, PRIME AND TOPCOAT. ALODINE REPAIR AREA IAW CRJ 200 SRM 51-21-11. APPLIED PRIME TO REPAIR AREA IAW CRJ 200 SRM 51-25-06 AND APPLIED TOPCOAT TO REPAIR AREA IAW CRJ 200 SRM 51-25-16. THE CORROSION REMO VED WAS WITHIN THE ALLOWABLE LIMITS OF THE CRJ 200 SRM 53-00-00. REMOVED .003 THICKNESS FROM ANGLE. 2 L 7 2 4F RT A21EA 2007110600021 20071106 00021 EU 2007 11 6 TRAX200701579 1 20071023 A 5320 INTERCOSTAL AEROSP ATR72 ATR72 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 RIGHT MLG ANGLE ON AFT SURFACE AT INTERCOSTAL FR 27 CRACKED. RT MLG ANGLE ON AFT SURFACE AT INTERCOSTAL FR 27 INSTALLED IAW SRM 51-25-01 FABRICATION COVER ON W/C 2000-167 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 6 63 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01. 2 H 7 2 4T RT 2007110600022 20071106 00022 2007 11 6 NOCA16207 4 20071024 A 2210 8221261101 COMPUTER BOEING 767 76739H 1385311 NM AUTOPILOT INTERMITTENT A NOCA O OTHER O OTHER CR CRUISE 1 EA 15 760NA 26257 FOUND LEFT A/P ENGAGES INTERMITTENTLY REPLACED LEFT AFCS PER MM 22-11-01. 2 L 7 2 4F RT A1NM 2007110600023 20071106 00023 GL 2007 11 6 SIMA200730202 2 20071028 A 7200 AE3007A1 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL SHUTDOWN A SIMA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SW 21 676AE 14500807 CAE311719 NR 1 ENGINE UNCOMMANDED SHUT DOWN IN FLIGHT. CREW LANDED AT JFK WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE. AI RCRAFT RETURNED TO SERVICE 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007110700012 20071107 00012 2007 11 7 QXEA200701624 4 20071022 A 2210 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM YAW DAMPER UNKNOWN A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 414QX 4061 SEA FLIGHT NR 2367: Y/D DISENGAGED IN CLIMB WITH FLASHING MESSAGES ON PFD'S. A/P WAS NOT ENGAGED AT THE TIME. CLEARED M ESSAGES PER E/A CHECKLIST. ENGAGED A/P, Y/D WORK NORMAL. MAINTENANCE CLEANED SCREEN ON IOP BOX AND RE-RACKED NR 1 FGM. C/W CAT 3 CHECK IAW MTC 6221101 WITH NO DEFECTS. ALSO C/W Y/D CHECK IAW AMM 22-11-36-710-801 WITH NO DEFECTS. A/C RE MAINS CAT 3. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007110700013 20071107 00013 NM 2007 11 7 QXEA200701625 1 20071024 A 2120 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM COCKPIT ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 09 406QX 4048 GEG FLIGHT NR 9852: DURING DESCENT FROM CRUISE ALTITUDE, THERE WAS A STRONG ODOR (STINKY SOCKS) IN THE COCKPIT. MAINTEN ANCE REMOVED ODOR FROM AIR CONDITIONING DUCTS IAW AMM TASK 21-00-00-160-801, SUBTASK 21-00-00-160-002. NO FILTER REMOVA L NECESSARY. NO PARTS REMOVED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007110700014 20071107 00014 EU 2007 11 7 CPCP20070113 1 20070919 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 425MJ 425 LT I/B SEAT TRACK BETWEEN FRAME 29-36 CORRODED. SEAT TRACK FRAME 29-36 LT I/B REPLACED IAW SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007110700015 20071107 00015 EU 2007 11 7 CPCP200700114 1 20071012 A 5320 THRESHOLD AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 322AC 320 RT THRESHOLD BTW FRAME 36-39 GUTTER CORRODED. RT THRESHOLD BTW FRAME 36-39 GUTTER REPLACED IAW SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007110700016 20071107 00016 EU 2007 11 7 CPCP200700115 1 20071012 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 322AC 320 FLOORBEAM 39 CORRODED ON UPPER AND LOWER SURFACE. CORROSION OF FLOORBEAM 39 REPAIRED IAW SRM 53-00-00 FIGURE 450 AT 2 L OCATIONS. 2 H 7 2 4T RT A53EU 2007110700017 20071107 00017 EU 2007 11 7 CPCP200700116 1 20071012 A 5320 SUPPORT BRACKET AEROSP ATR72 ATR72212 8680945 EU FOLDING STEP CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 322AC 320 FWD "T" BRACKET OF FOLDING STEP CORRODED. FWD "T" BRACKET OF FOLD ONG STEP REPLACED IAW SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007110700018 20071107 00018 EU 2007 11 7 TRBA2007088 1 20071026 A 3213 GA63893 SPACER AEROSP ATR72 ATR72212 8680945 EU RT MLG CRACKED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 410AT 410 RT MLG SWINGING LEVER SPACER CRACKED. REMOVED AND REPLACED RT MLG SWINGING LEVER SPACER AS PER EO NR E2-3200-029R2 (SB #631-32-165). LANDING GEAR PART NUMBER CHANGED TO SUFFIX -20. PERFORMED RETRACTION, FUNCTIONAL AND EMERGENCY EXTENSION TEST AND FOUND SATISFACTORY. 2 H 7 2 4T RT A53EU 2007110700019 20071107 00019 SO 2007 11 7 SMIA200730201 1 20071028 A 3320 BR900027 BALLAST EMB 145 EMB145LR 3260212 SO CABIN LIGHTS FAILED A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 648AE 145225 STRONG ELECTRICAL BURNING ODOR DURING TAXI. CREW RETURNED TO GATE. REMOVED AND REPLACED BALLAST AT SEAT 1A IAW EMB 145 AMM 33-12-03. OPERATIONAL CHECK GOOD IAW EMB145 AMM 33-21-50. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007110700020 20071107 00020 EU 2007 11 7 SIMA200730203 1 20071027 A 3250 7085742 ACTUATOR SAAB SF340 340B 7860101 EU NLG STEERING MALFUNCTIONED A SIMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 21 393AE 340B393 WHEN BRINGING POWER UP FOR THE REQUIRED METHOD A TAKEOFF THE AIRCRAFT PULLED SEVERELY TO THE LEFT WITH THE BRAKES APPLIE D AFTER ABOVE EVENT AIRCRAFT REQUIRED EXCESSIVE LIGHT INPUT ON THE TILLER TO STEER STRAIGHT. REMOVED AND REPLACED NLG S TEERING ACTUATOR IAW SAAB 340 AMM 32-50-25. OPERATION CHECK GOOD. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007110700021 20071107 00021 EU 2007 11 7 SIMA200730204 1 20071019 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 305AE 21126 5000 340B305 DURING A MBV INSPECTION, CORROSION WAS FOUND ON THE RIGHT SIDE OF FRAME 72. REPAIRED FRAME 72 IAW SAAB SRM CHAPTER 53-7 0-30. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007110700022 20071107 00022 NM 2007 11 7 754001 1 20071028 A 2612 FIRE LOOP BOEING 747 747228F 1384895 NM APU BAY INOPERATIVE A Q2SA F ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 EA 63 754SA 21576 DURING CLIMB-OUT, APU FIRE BELL AND LIGHTS ACTIVATED. APU FIRE CHECKLIST PERFORMED BUT DID NOT STOP BELL RINGING OR LIG HTS FLASHING. SELECTED FIRE WARNING SYSTEM "A" AND CONDITION CLEARED. INSPECTED APU COMPARTMENT AND FOUND NO EVIDENCE OF FIRE. FOUND APU FIRE WARNING LOOP "A" AND "B" INOPERATIVE. DEACTIVATED APU AND DEFERRED IAW DDPG PROCEDURES. 2 L 7 4 4F A20WE 2007110700061 20071107 00061 NE 2007 11 7 HALA0700450 2 20071012 A 7321 114E7842G120 EEC BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE LT ENGINE FAULTED A HALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 487HA 55132 ENG L SYSTEM FAIL LIGHT ILLUMINATED INFLIGHT. FOUND EEC 1 FAULT 732142 EEC BOX FAULT REMOVED AND REPLACED NR 1 ECC IAW AMM 73-21-01. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007110700067 20071107 00067 NM 2007 11 7 HALA0700456 1 20071025 A 5230 SKIN BOEING 717 717200 1383700 NM CARGO DOOR DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 476HA 55118 AFT CARGO DOOR APPROX 10" UP FROM AFT LOWER CORNER DOOR SKIN BENT ALONG EDGE. CLEANED AND EDDY CURRENT AREA, NO DEFECTS NOTED (COLD WORK AREA PER SRM 52-00-00-2R-3 BEFORE EDDY CURRENT WAS PERFORMED). 2 L 7 2 4F TR A6WE 2007110700075 20071107 00075 NM 2007 11 7 DL75E071334 1 20071010 A 2530 OVEN BOEING 757 7572Q8 1384972 NM GALLEY SMOKE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 707TW 27625 FWD GALLEY NR 1 OVEN REPORTED SMOKE AFTER OVEN FOOD SPILL. CLEANED OVEN THEN CYCLED OVEN FOR 2 HRS OK FOR SVC MCO/PL R MVD. 2 L 7 2 4F RT A2NM 2007110700076 20071107 00076 NM 2007 11 7 DLM88071381 1 20071023 A 4997 TERMINAL BLOCK DOUG MD88 MD88 3023688 NM APU FEEDER CABLE BURNED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 935DL 49722 AIRCRAFT HAS ELECTRICAL SMELL IN CABIN. FOUND APU FEEDER CABLE TERMINAL BLOCK BURNED BELOW CIRCUIT BREAKER PANEL BEHIND CAPTS SEAT. REMOVED TERMINAL BLOCK. FEE CABLE NEEDS RETERMINATED. REPLACED TERMINAL BLOCK S3-23 AND REPAIRED FEEDER CABLE 3X1B00AAL PER BSWPM CH 20. APU OPN AN APU ELECTRICS CK NML ACFT. OK FOR SVC. 2 L 7 2 4F RT A6WE 2007110700077 20071107 00077 NM 2007 11 7 DLM88071384 1 20071024 A 5330 593600419 SKIN DOUG MD88 MD88 3023688 NM BS 712-731 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 CORROSION DAMAGED THE SKIN AND DOUBLER FROM FS 712 TO 731 BETWEEN L-29L AND L-28R. A PREVIOUS REPAIR, ER/A 363898-14,WA S ALSO IN THIS AREA. A MX SPLICED THE SKIN AND DOUBLER FROM FS 655 TO FS 759 AT THE C-2 DOOR. 2 L 7 2 4F RT A6WE 2007110700078 20071107 00078 NM 2007 11 7 DL76L071385 1 20071023 A 3610 77328810 SHUTOFF VALVE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 174DN 24802 724682 UNUSUAL AIR SURGE SOUND DURING TAXI IN LEFT ENG IS 23 PSI AND RT ENG IS 34. REMOVED AND REPLACED LEFT ENG PRSOV, ENG RU N VALVE OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110700079 20071107 00079 NM 2007 11 7 DL76S071386 1 20071024 A 5343 TRUNNION BOEING 767 767332 1382001 NM NLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 124DE 23438 LT AND RT NOSE LANDING GEAR TRUNNION FITTINGS CORRODED IN THE INNER DIAMETER. CORROSION CLEANED UP AND OVERSIZED BUSHIN GS WERE INSTALLED. 2 L 7 2 4F RT A1NM 2007110700080 20071107 00080 NM 2007 11 7 DL757071387 1 20071024 A 2121 6457053 FAN BOEING 757 757232 1384965 NM CABIN SMOKE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 666DN 25034 LT RECIRC FAN INOP. LT RECIRC FAN NOISY CAUSING SMOKE IN CABIN. NEED DL P/N 216001033 FWD TO MCO/PLAC PER MEL 21- 25-01B. REMOVED LT FAN 964727. INSTALLED LT RECIRC FAN, OPS NML MCO A PLAC REMOVED. 2 L 7 2 4F RT A2NM 2007110700081 20071107 00081 NM 2007 11 7 DLM90071389 1 20071025 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 870 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 LT CUSP AT FS 870 CORRODED OUT OF LIMITS. REPAIRED LT CUSP WEB IAW MD-80 ERA 53-05D FIG 827D ON N/R 2400-0241 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007110800012 20071108 00012 NM 2007 11 8 2007UALA04409 1 20071025 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 LEFT EXTERNAL FUSELAGE BETWEEN STA 740 AND 760 BETWEEN STR 15L AND 16L FUSELAGE SKIN HAS 3 DENTS IN ONE BAY. MAJOR REP AIR ACCOMPLISHED. REPAIRED DAMAGE AREA. REPAIR IS INTERM PENDING. COMPLETION OF FATIGUE AND DTA BY OEM BOEING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110800031 20071108 00031 NM 2007 11 8 2007UALA04425 1 20071027 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 RIGHT OVERWING EMERGENCY LIGHT 3RD FROM TOP I BULB INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110800032 20071108 00032 CE 2007 11 8 DXTA200702577 1 20071028 A 3220 1283500421 BEARING BEECH MU300 400A 1155402 CE NLG WORN E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 153QS 535 RK490 AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT. REMOVED NOSE GEAR. DISASSEMBLED AND INSPECTED. REPLACED NLG LOWER BEARING W ITH NEW BEARING P/N 128-350042-1, SCRAPER RING WITH EW RING P/N 2145-24-0160 AND ALL INTERNAL AND EXTERNAL SEALS. SERVIC ED AND REINSTALLED STRUT. PERFORMED RETRACTION TEST. ALL TEST SATISFACTORY ALL WORK PERFORMED IAW MM 12-10, 32-20 CMM 3 2-23. 2 H 7 2 4F RT A16SW 2007110800033 20071108 00033 NM 2007 11 8 2007UALA04426 1 20071027 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 RIGHT OVERWING EMERGENCY LIGHT 3RD FROM TOP I BULB INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110800036 20071108 00036 EU 2007 11 8 TRAX200701593 1 20071023 A 3210 LANDING GEAR AEROSP ATR72 ATR72 EU RIGHT CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 RIGHT MLG LWR FLANGE ON AFT SURFACE AT FR 27 CORRODED. RT MLG LWR FLANGE ON AFT SURFACE AT FR 27, CORROSION REMOVED IA W SRM 51-21-42 FOUND WITHIN LIMITS OF SRM 51-10-10 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 66 3 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42 MATERIAL THICKNESS: 0.063 MATERIAL REMOVED : 0.002 WITHIN LIMITS AS PER SRM: 51-10-10. 2 H 7 2 4T RT 2007110800037 20071108 00037 NM 2007 11 8 2007UALA04429 1 20071026 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 556UA 26650 THE 4L EMERGENCY EGRESS LIGHT INOPERATIVE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110800045 20071108 00045 NM 2007 11 8 2007UALA04438 1 20071027 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN BROKEN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 646UA 25283 EMERGENCY LIGHTING STRIP BROKEN AT 2B. REPAIRED BROKEN SECTION. OPS CHECK, OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110800053 20071108 00053 NM 2007 11 8 KCSA071505 1 20071030 A 5310 DOOR FRAME BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 L5 MAIN ENTRY DOOR LOWER O/B HORIZONTAL FRAME CRACKED BS 2240. 2 L 7 4 4F RT A20WE 2007110800055 20071108 00055 EU 2007 11 8 TRAX200701599 1 20071026 A 5720 PLATE AEROSP ATR72 ATR72 EU LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 LEFT WING BOX FR 28, FACE PLATE CRACKED. LT WING BOX FR 28 FACE PLATE REPLACED IAW SRM 51-25-01. 2 H 7 2 4T RT 2007110800057 20071108 00057 WP 2007 11 8 ABXA070352 1 20071009 A 5210 4915171 FITTING DOUG DC9 DC941 302207N WP PAX DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 MAIN ENTRY DOOR UPPER SEAL DEPRESSOR HINGE DRIVE FITTING WAS CRACKED. REMOVED AND REPLACED UPPER SEAL DEPRESSOR HINGE D RIVE FITTING IAW DC9 SRM 51-30-04. 2 L 7 2 4F A6WE 2007110800077 20071108 00077 NM 2007 11 8 DL777071390 1 20071027 A 3040 7858973 CONTROLLER BOEING 777 777232 1385232 NM WINDOW HEAT UNKNOWN A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 862DA 29734 ATB DUE TO L1 WINDOW HEAT STATUS MESSAGE. REPLACED CONTROLLER. 2 L 7 2 4F RT T00001SE 2007110800078 20071108 00078 2007 11 8 DL76S071392 4 20071027 A 3414 INDICATOR BOEING 767 767332 1382001 NM AIRSPEED MALFUNCTIONED A DALA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 27 124DE 23438 AFTER TO, F/O AIRSPEED INDICATOR BECAME UNREADABLE AND ROSE STEADILY TO 400 KTS. NO FLAGS OR OTHER INDICATIONS, OTHER T HAN OVERSPEED WARNING. ACTUAL AIRSPEED ON CAPTS IND NORMAL. FOUND QUICK DISCONNECT DAMAGED ON PITOT PRESS ON RT ADC. R EPLACED SAME. LEAK CHECKED PITOT/STATIC SYSTEM CHECKED GOOD. PERFORMED MCDP TEST 30 TEST PASSED. ADC LEFT AND RIGHT B ITE CHECKED GOOD. 2 L 7 2 4F RT A1NM 2007110800080 20071108 00080 2007 11 8 DL757071393 4 20071028 A 2565 D31393110 SLIDE BOEING 757 757232 1384965 NM RT OVERWING PARTIAL INFLATE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 675DL 25980 UPON PERFORMING SLIDE DEPLOYMENT TRANSMITTAL 6T129 FOR RIGHT OVERWING ESCAPE SLIDE, SLIDE DID NOT FULLY DEPLOY 2 L 7 2 4F RT A2NM 2007110800081 20071108 00081 NM 2007 11 8 DU4R2007178 1 20071016 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM BS 1640 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 6714Q 30485 FOUND CORRODED FLOORBEAM AT BS 1640 BETWEEN LBL 24 - RBL 28 IN MAIN CABIN AFT SECTION. REPAIRED BY CUTTING OUT 18 CORRO DED SECTION OF T CAP. FABRICATED DRILLED AND INSTALLED T CAP REPAIR 32-5/8 FROM BAC1505-100617, 2 SPLICES 9 BY 2 BY 1 A ND 6 BY 2 BY 1 FROM 7075-T6 .071 AND 7075-T6 .063 IAW DELTA B757 SRM 53-00-51, 51-20-01 AND DELTA PS 900-2 NR 5. 2 L 7 2 4F RT A2NM 2007110800083 20071108 00083 NM 2007 11 8 DU4R2007179 1 20071027 A 5320 SILL BOEING 757 757232 1384965 NM BS 1380-1440 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 6714Q 30485 FOUND CORROSION IN AFT CARGO DOOR WAY FROM BS 1380 TO BS 1440 LOWER SILL ZONE 154. REPAIRED BY REMOVING AND REPLACING C HORD P/N 146N8522-64 IAW B757 SRM 51-40-02 AND DELTA SRM 51-00-00D. 2 L 7 2 4F RT A2NM 2007110800084 20071108 00084 EU 2007 11 8 TRAX200701597 1 20071025 A 5210 DOOR AEROSP ATR72 ATR72 EU PAX DOOR OUT OF ADJUST A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 PAX DOOR HARD TO OPEN / CLOSE. PAX DOOR ADJUSTED AND FOUND SERVICEABLE IAW JIC 52-11-00. 2 H 7 2 4T RT 2007110800085 20071108 00085 NM 2007 11 8 DU4R2007180 1 20071026 A 5320 146N852257 FLOOR SUPPORT BOEING 757 757232 1384965 NM BS 1375-1440 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 6714Q 30485 FOUND CORRODED AFT CARGO THRESHOLD/FLOOR SUPPORT STRUCTURE AT DOOR STA 1375 - 1440 RBL 20. REPAIRED BY REMOVING AND REP LACING LOWER CHORD P/N 146N8522-57 IAW B757 SRM 51-40-02, 51-20-01, DELTA B757 SRM 51-00-00D. 2 L 7 2 4F RT A2NM 2007110800087 20071108 00087 NM 2007 11 8 DU4R2007181 1 20071019 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM BS 600 GOUGED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 6714Q 30485 FOUND FWD CABIN FLOORBEAM GOUGED AT BS 600 LBL 27, 44. REPAIRED BY CUTTING OUT GOUGED AREA BS 600 LBL 7 TO LBL 71. FAB RICATED AND INSTALLED T CHORD REPAIR 69 BY 2-1/8 BY 0.125 FROM BAC1505-100617 AND REPAIR ANGLE 11 BY 2 BY 0.063" FROM BA C1490-2734 AND ANGLE REPAIR 7-1/2 BY 2 BY 0.063 IAW B757 SRM 53-00-51 REPAIR 3 FIG 201, 51-40-02 AND 51-20-01. 2 L 7 2 4F RT A2NM 2007110800093 20071108 00093 NM 2007 11 8 07FDEA04700 1 20071029 A 5711 SPAR CAP DOUG MD11 MD11F 3023600 NM LT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 527FE 48601 LEFT WING, REAR SPAR UPPER CAP 1EA FASTENER HOLE ELONGATED AT XORS 669. REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-11651 0, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007110800094 20071108 00094 EA 2007 11 8 TRAX200701604 1 20071026 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR FAULTY A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 717EV 10088 F/A UNABLE TO CLOSE AND LOCK MAIN ENTRY DOOR. 2 L 7 2 4F RT A21EA 2007110800095 20071108 00095 EA 2007 11 8 TRAX200701605 1 20071026 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 971EV 7528 EMERGENCY EXIT LIGHT RIGHT SIDE AFT OF EMERGENCY EXIT HATCH INOP. 2 L 7 2 4F RT A21EA 2007110800097 20071108 00097 NM 2007 11 8 07FDEA04701 1 20071029 A 5720 DUCT DOUG MD11 MD11F 3023600 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 527FE 48601 LT WING, LEADING EDGE UPPER SURFACE TELESCOPING DUCT CUTOUT I/B AND O/B CORNERS FOUND CRACK. REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-116509, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007110800098 20071108 00098 EU 2007 11 8 USAA920071035 1 20071027 A 5554 D5537131800000 HINGE FITTING AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - RUDDER HINGE FITTING NR 1 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STA 780 / RIB 2. REP LACED RUDDER HINGE FITTING NR 1, VERTICAL STABILIZER STA 780 / RIB 2 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007110800102 20071108 00102 EU 2007 11 8 USAA920071039 1 20071028 A 5554 D5537131800000 HINGE FITTING AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - RUDDER HINGE FITTING NR 5 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STA 2985 / RIB 7. RE PLACED RUDDER HINGE FITTING NR 5, VERTICAL STABILIZER STA 2985 / RIB 7 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007110800103 20071108 00103 NM 2007 11 8 USAA920071043 1 20071022 A 5313 6546877144 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, STRINGER 18A RIGHT WEB CRACKED, BS 663 - BS 747. REPLACED STRINGER 18A RIGHT WEB, BS 66 3 - BS 747 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007110800108 20071108 00108 NM 2007 11 8 USAA920071046 1 20071026 A 5340 693535241 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, CRACKED STRINGER TIE CLIP, BS 867, S21R. REPLACED STRINGER TIE CLIP, BS 867, S21R IAW B 737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007110800113 20071108 00113 NM 2007 11 8 USAA920071047 1 20071017 A 5310 6520723 DOOR FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, AFT CARGO COMPARTMENT DOOR CUTOUT AFT FRAME CRACKED, BS 846.5, S24R. REPAIRED AFT CARGO COMPARTMENT DOOR CUTOUT AFT FRAME, BS 846.5, S24R IAW B737 SRM 53-00-53. 2 L 7 2 4F RT A16WE 2007110800125 20071108 00125 NM 2007 11 8 USAA920071049 1 20071017 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, CRACKED FRAME, BS 480, S1R. REPAIRED FRAME, BS 480, S1R IAW USAIRWAYS EA 98915. 2 L 7 2 4F RT A16WE 2007110800128 20071108 00128 NM 2007 11 8 USAA920071050 1 20071019 A 5320 ATTACH ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, CRACKED FRAME ATTACH ANGLE, BS 348, S14L - S15L. REPLACED FRAME ATTACH ANGLE, BS 348, S 14L - S15L IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007110800144 20071108 00144 NM 2007 11 8 USAA920071052 1 20071026 A 5311 6545807 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, CRACKED FRAME, BS 312, S7R - S8R. REPLACED FRAME, BS 312, S7R - S8L IAW B737 SRM 51-40- 03. 2 L 7 2 4F RT A16WE 2007110800152 20071108 00152 NM 2007 11 8 TSAA0753059 1 20071028 A 5330 65458001000 SKIN BOEING 737 7372X6C 1384552 NM BS 747 S21-22L CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 IN THE PROCESS OF SSIP, NDT INSPECTION DISCOVERED LT SKIN CRACKED INSIDE LT WING TO BODY FAIRING. CRACK LOCATED AT BS 7 47 +19 BETWEEN STRINGER 21L AND 22L. CRACK APPROXIMATELY 1.5 INCHES LONG. CRACK WAS REPAIRED IN ACCORDANCE WITH ECO 36 84. 2 L 7 2 4F RT A16WE 2007110800154 20071108 00154 SO 2007 11 8 SWIA200718804 1 20071025 A 5412 FIREWALL EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 569SW 120344 LEFT ENGINE FORWARD FIREWALL IS CRACKED AT 12:00 POSITION. REPAIRED IAW EMB120 SRM 51-70-00. 2 L 7 2 4T RT A31SO 2007110800155 20071108 00155 SO 2007 11 8 SWIA200718805 1 20071020 A 5220 DOOR EMB 120 EMB120ER 3260203 SO EMERGENCY EXIT LOOSE A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 560SW 120334 FLT 3704 - AIRCRAFT WOULD NOT PRESSURIZE ON DEPARTURE. INSPECTED AND RE-INSTALLED LEFT OVERWING EXIT DOOR. NO ABNORMAL DISCREPANCIES NOTED. 2 L 7 2 4T RT A31SO 2007110800156 20071108 00156 SO 2007 11 8 SWIA200718806 1 20070924 A 5347 GALLEY TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 270YV 120270 FOUND AT C-CHECK, TOP OF GALLEY FLOOR TRACK IS CORRODED. REPLACED GALLEY FLOOR TRACK. 2 L 7 2 4T RT A31SO 2007110800157 20071108 00157 SO 2007 11 8 SWIA200718807 1 20070924 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 270YV 120270 FOUND AT C-CHECK, ENTRY WAY FLOOR TRACK IS CORRODED. REPLACED FLOOR TRACK IAW AMM 53-00-00. 2 L 7 2 4T RT A31SO 2007110800159 20071108 00159 EA 2007 11 8 SWIA200718808 1 20071021 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCONNECTED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 417SW 7400 FLT 2912 - FLOOR LEVEL EMERGENCY EXIT LIGHT NEAR PAX DOOR IS INOP. SECURED PIN IN CONNECTOR OF EMERGENCY LIGHT IAW MM 3 3-51-00. 2 L 7 2 4F RT A21EA 2007110800160 20071108 00160 SO 2007 11 8 SWIA200718809 1 20071027 A 2750 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO TE FLAPS LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 NM 07 229SW 16838 16838 120305 FLT 5608 - LOST BLUE SYSTEM HYDRAULIC FLUID AFTER SELECTING FLAPS 15 ON APPROACH. REPLACED RIGHT NACELLE FLAP ACTUATOR IAW 27-50-03. 2 L 7 2 4T RT A31SO 2007110800161 20071108 00161 SO 2007 11 8 SWIA200718811 1 20071026 A 5753 STIFFENER EMB 120 EMB120ER 3260203 SO LT NACELLE FLAP CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 224SW 120294 THE LEFT NACELLE FLAP INTERNAL STIFFENER IS CRACKED. REPLACED THE LEFT NACELLE FLAP ASSEMBLY. 2 L 7 2 4T RT A31SO 2007110800162 20071108 00162 SO 2007 11 8 SWIA200718812 1 20071022 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO RT WING DAMAGED A SWIA O OTHER K FLUID LOSS NR NOT REPORTED 1 NM 07 582SW 120350 RIGHT DEFUEL PANEL HAS ONE RIVET LEAKING FUEL. ACCOMPLISHED REPAIR TO NR 8 STRINGER IAW SRM 57-20-03. 2 L 7 2 4T RT A31SO 2007110800163 20071108 00163 EA 2007 11 8 SWIA200718813 1 20071028 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA LEFT ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 955SW 7817 FLT 6445 - LEFT PACK IS EMITTING FUEL TYPE ODOR. CLEARED OVERBOARD DRAIN IAW 21-51-00. 2 L 7 2 4F RT A21EA 2007110800164 20071108 00164 2007 11 8 SWIA200718814 2 20071028 A 7230 ENGINE CNDAIR CL600 CL6002C10 1390015 EA COMPRESSOR LEAKING A SWIA C ABORTED TAKEOFF B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 NM 07 367CA 10069 FLT 4082 - ON TAKEOFF ROLL, RECEIVED MASTER WARNING "SMOKE FWD LAV" AND "SMOKE AFT LAV." FOUND OIL MIGRATING INTO COMPR ESSOR AND BLEED SYSTEM. REPLACED RIGHT ENGINE ASSEMBLY IAW 71-00-00, P/N CF34-BC5B1, S/N OFF 965366. 2 L 7 2 4F RT A21EA 2007110800165 20071108 00165 SO 2007 11 8 SWIA200718815 1 20071022 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO CABIN SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 07 232SW 120306 FLT 5749 - ON DESCENT, THE CABIN FILLED WITH SMOKE AND THE LAV SMOKE DETECTOR WENT OFF. RAN AIRCRAFT TO FLIGHT CONFIGUR ATION WITH ENGINES AND PACKS TO FULL POWER. COULD NOT DUPLICATE. 2 L 7 2 4T RT A31SO 2007110800166 20071108 00166 SO 2007 11 8 SWIA200718816 1 20071019 A 2611 SMOKE DETECTOR EMB 120 EMB120ER 3260203 SO FALSE INDICATION A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 227SW 120304 FLT 5460 - SMOKE ALARM ANNUNCIATING IN BACK WITH NO FIRE NOTED. RAN APU BLEED FOR 20 MIN. NO SMOKE ALARM SOUNDED. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007110800167 20071108 00167 EA 2007 11 8 SWIA200718817 1 20071027 A 7830 DRIVE UNIT CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER FAULTY A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 930SW 7713 FLT 6133 - RIGHT REVERSER UNLOCK MESSAGE INFLIGHT. REPLACED PNEUMATIC DRIVE UNIT PER CRJ 200 MM 78-32-03. OPS CHECK GO OD, P/N: 126758-7, S/N OFF: 2178. 2 L 7 2 4F RT A21EA 2007110800168 20071108 00168 EA 2007 11 8 SWIA200718818 1 20071024 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 429SW 7518 FLT NR 3916 - OVERHEAD CEILING EMERGENCY FLOODLIGHT IS INOP. RELAMPED EMERGENCY LIGHT AS REQUIRED. 2 L 7 2 4F RT A21EA 2007110800169 20071108 00169 EU 2007 11 8 TRBA2007089 1 20071030 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS FAILED A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 377AT 377 FWD CABIN EMERGENCY LIGHTS (UPPER AND LOWER) INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK 43WL IAW JI C NR 33-51-21. 2 H 7 2 4T RT A53EU 2007110800170 20071108 00170 NE 2007 11 8 MASA200700749 2 20071027 A 7250 5121T31G01 BOLT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENGINE BROKEN A MASA O OTHER O OTHER IN INSP/MAINT 1 SW 07 75984 7489 872941 LEFT ENGINE HAS 3 BROKEN BOLTS ON LPT TO HPT OUTER CASING. REMOVED AND REPLACED BOLTS AND LPTM TO FACILITATE REMOVAL OF BROKEN BOLTS IN LPT TRANSITION FLANGE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007110800173 20071108 00173 EU 2007 11 8 WRNA200700060 1 20071031 A 3610 80310423 DUCT AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE BROKEN A WRNA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 506TA 207 DURING TAKE OFF, NR 2 ENGINE EGT EXCEEDED 960 C, POWER WAS REDUCED BELOW TAKEOFF SETTING, EGT DROPPED BELOW 945 C. DURI NG CLIMB, NR 2 ENGINE MANIFOLD PRESS 10 PSI, BLEED VALVE REGULATOR LIGHT ON, THEN NR 2 -B- LOOP LIGHT ILLUMINATED, SWITC HED TO -A- LOOP, -A- LOOP LIGHT ILLUMINATED. ENGINE WAS SHUT DOWN, VISUAL INSPECTION DURING FLIGHT INDICATED NO FIRE. RETURNED TO FIELD FOR A SAFE LANDING. REPLACED BROKEN PNEUMATIC DUCT IAW MM 75-26-01 PG 401. CHECKED ENGINE EGT LIMITA TION IAW MM 72-00-00 PAGE 604, FOUND WITHIN LIMITS. RAN ENGINE, FOUND OK IAW 72-00-00. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A35EU 2007110800175 20071108 00175 NE 2007 11 8 NWAA073589993 2 20071028 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D15A 52051 NE NR 1 MALFUNCTIONED A NWAA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 GL 01 8986E 47402 696478 DURING FLIGHT, ENGINE NR 1 PARAMETERS WERE ERRATIC AND THROTTLE LEVER SPLIT OF 1.5 KNOBS. ENGINE NR 1 FLAMED OUT AT APP ROX 14,000 FT. FLIGHT CREW DIVERTED AC TO GRR AND PERFORMED AN UNEVENTFUL LANDING. GROUND PERSONNEL REPORTED FUEL LEAK AT ENGINE. MAINTENANCE REMOVED AND REPLACED ENGINE NR 1. 2 L 7 2 4F 4 F A6WE E2EA 2007110800176 20071108 00176 WP 2007 11 8 MWEA070264 1 20071029 A 5330 591140047 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 809ME 48071 WAVE IN FUSELAGE SKIN AFT OF LEFT NOSE GEAR DOOR HAS A CRACK IN SKIN EMINATING FROM THE RIVET HOLE AT 12 O'CLOCK. FABRI CATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2007110800177 20071108 00177 NM 2007 11 8 MWEA070265 1 20071029 A 5347 593054768 SEAT TRACK DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 601ME 49762 CABIN FLOOR SEAT TRACK NR 4 FROM LEFT STATION 237-260 UNDER FLOOR PANEL SEAT TRACK HAS CORROSION. REMOVED DAMAGE SEAT T RACK AND INSTALLED NEW SEAT TRACK. 2 L 7 2 4F RT A6WE 2007110800178 20071108 00178 NM 2007 11 8 MWEA070266 1 20071029 A 5230 SR095200633 PAN DOUG MD88 MD88 3023688 NM CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 601ME 49762 FORWARD CARGO DOOR OUTER PAN, FORWARD UPPER CORNER UNDER DOOR STOP PAD IS CRACKED. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 2007110800181 20071108 00181 NE 2007 11 8 TRAX200701606 2 20071027 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 1 VIBRATION A ASOA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 27 974EV 7594 AT 27000 FT W/ ANTI ICE ON HEAVY VIBRATION IN ENG NR 1 (OVER 3.5) DESCENED TO 24000 NR 2 STARTED VIBRATION FOR 15 SEC. EN ROUTE TO ATL A/C DIVERTED TO CAE DUE TO MTC. EMERGENCY DECLARED. 2 L 7 2 4F 4 F RT A21EA E15NE 2007110800183 20071108 00183 EU 2007 11 8 UPS07151073 1 20071030 A 2560 FITTING AIRBUS A300 A300F4622R 3930360 EU GIRT BAR OBSTRUCTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 127UP 0811 INSPECTION TYPE:N/A SLIDE ARMING LEVEL ON DOOR IS VERY STIFF & HARD TO DISARM. REMOVED DEBRIS FROM GIRT BAR FLOOR FITTI NGS. OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2007110800186 20071108 00186 EU 2007 11 8 UPS07151074 1 20071029 A 2560 LIGHT AIRBUS A300 A300F4622R 3930360 EU EVAC SLIDE INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 138UP 0821 INSPECTION TYPE:N/A EVACUATION SLIDE WARNING SYSTEM LIGHTS DO NOT ILLUMINATE WHEN TESTED M361512. FOUND ASPSU IN MAINTE NANCE CYCLE. RESET ASPSU CB 3WN AND TESTED ASPSU IAW MM 52-73-00-05. RESIDUAL PRESSURE WARNING SYSTEM ALL TESTED NORMA L. THIS CLEARS M361512. PLACARD REMOVED. 2 L 7 2 4F RT A35EU 2007110800193 20071108 00193 WP 2007 11 8 UPS07851071 1 20071010 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 FLOOR SUPPORT AT STA 1734 LBL 20 IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FLOOR SU PPORT AT STA 1734 LBL 20 IAW SRM 53-07-01-0 FIG 011A. 2 L 7 4 4F RT 4A25 2007110800196 20071108 00196 EU 2007 11 8 F3LA200700286 1 20071017 A 5320 SUPPORT AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED SHEAR WEB AND SUPPORT PLATE AT FR70R BLOWN OUT FROM CORROSION. REMOVED AND REPL ACED SHEAR PLATE SUPPORT IAW SRM 51-42-11, PARAGRAPHS 6, 7, AND 77, AND DWG D53474180. 2 L 7 2 4F RT A28NM 2007110500219 20071105 00219 EU 2007 11 5 USAA920071011 1 20071019 A 5347 D5347209001000 SEAT TRACK AIRBUS 320 A320232 3930326 EU BS 3043-3458 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN SEAT RAIL BEAM, BS 3158 / FR 66, +Y1292. REPLACED CABIN SEAT RAIL BE AM, BS 3043 / FR 64 - BS 3158 / FR 66, +Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007110500231 20071105 00231 NM 2007 11 5 CALA0700627 1 20071029 A 5330 6545783U502 MOUNT BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND A 1 INCH CRACK IN NR 2 VHF ANTENNA MOUNTING BRACKET AT FORWARD CARGO BIN BETWEEN S28L AND S28R. THE MO UNTING BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007110500232 20071105 00232 NE 2007 11 5 SA07070 2 20071029 A 7200 ENGINE AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4P NE NR 1 SMOKE A USAA E ENGINE SHUTDOWN B E SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET DE DESCENT 1 EA 19 113UW 1141 575141 SAN FLT 883 EN-ROUTE LAS TO SAN - CREW SHUT DOWN THE NUMBER TWO ENGINE AFTER A REPORT FROM ANOTHER FLIGHT ABOUT A TRAIL OF SMOKE COMING FROM THE ENGINE. THE ENGINE HAD ALSO JUST BEGUN TO HAVE HIGH LEVELS OF VIBRATION. MAINTENANCE ACTION PENDING (OPEN). 2 L 7 2 4F 4 F RT A28NM E38NE 2007110500236 20071105 00236 NM 2007 11 5 2007UALA04400 1 20071025 A 5512 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZONTAL STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 GROUND PERSONNEL REPORT DENT IN RIGHT HORIZONTAL STAB MID SPAN. MAINT EVALUATED DENT ON RIGHT STAB LEADING EDGE AT APPR OX STA 220 MEASURES 2.625" X 1.5" X .125" DEEP. ACCOMPLISHED MAJOR REPAIR TO RT STAB LE BY APPLYING FLUSH PATCH TO DAMA GED AREA. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110500241 20071105 00241 NM 2007 11 5 2007UALA04405 1 20071026 A 3097 WIRE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU WINDOW HEAT FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 365UA 24534 RTFL DUE TO SHATTERING OF LEFT SLIDING COCKPIT WINDOW. HIGH INTERNAL RESISTANCE ON T271, CAUSING THE WHC TO FAIL OVE RHEAT CONDITION. OVERHEAT OCCURRED AND WINDOW WAS SHATTERED AS A RESULT. REPLACED WINDOW AND RESPLICED SENSOR WIRING (CAUSING THE HIGH RESISTANCE). TESTED WINDOW -OK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110600002 20071106 00002 EU 2007 11 6 07FDEA04696 1 20071029 A 5310 A53978224200 DOOR FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 729FD 657 FOUND CRACKED SEALING SECTION AT AFT CARGO DOOR C63A , P 26A-P30. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-7 2-10. 2 L 7 2 4F RT A35EU 2007110600010 20071106 00010 NM 2007 11 6 07FDEA04709 1 20071101 A 5711 SPAR CAP DOUG MD11 MD11F 3023600 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 527FE 48601 RIGHT WING REAR SPAR UPPER CAP FOUND WITH CORROSION AT XORS 1044 AND XORS 1046. REPAIR CARRIED OUT AS PER FEDEX EA 1 -5710-116512, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007110600015 20071106 00015 EA 2007 11 6 SWIA200718823 1 20071030 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 461SW 7811 FLT 3879 - RIGHT COCKPIT SIDE WINDOW CRACKED. REPLACED RIGHT COCKPIT SIDE WINDOW IAW MM 56-11-01, P/N: NP-139322-12, S/ N OFF: 03065H7918. 2 L 7 2 4F RT A21EA 2007110700001 20071107 00001 EU 2007 11 7 2007UALA04445 1 20071029 A 5210 D5211084000660 DIAPHRAGM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR ASSIST LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 437UA 655 DOOR ASSIST CYLINDER ON R2 DOOR HAS ZERO PRESSURE. FOUND LEAKING DOOR ASSIST CYLINDER. REPLACED DOOR ASSIST CYLINDER ON R2 DOOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110700002 20071107 00002 EU 2007 11 7 2007UALA04446 1 20071029 A 5310 STRUCTURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FWD GALLEY CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 438UA 678 FWD GALLEY HAS CORROSION DAMAGE. FOUND WATER PENETRATION BELOW GALLEY SUBFLOOR. REPAIRED FLOOR STRUCTURE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110700003 20071107 00003 NM 2007 11 7 2007UALA04447 1 20071029 A 3250 UNKNOWN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NLG STEERING UNKNOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 802UA 690 DURING TAXI AIRCRAFT TENDS UNSAFELY TO THE RIGHT. ALSO BRAKE TEMP WENT UP TO 185 DEG VS 35 DEG ON OPPOSITE SIDE TO KEEP NOSE CENTERED ONLINE. REPLACED SEVERAL PARTS AND COMPONENTS, LASTLY A NOSE WHEEL STEERING SERVO CONTROL UNIT WHICH BR OUGHT THE A/C BACK INTO MM LIMITS UNDER STEERING CONTROL INPUTS. NOTE; DUE TO TEMP DIFFERENCES ON THE MAIN BRAKES, BOT H MLG BRAKES WERE REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110700004 20071107 00004 EU 2007 11 7 2007UALA04448 1 20071029 A 5754 STRUCTURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 SLAT DAMAGED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 407UA 456 LEFT WING L/E SLAT OUTBOARD OF NR 1 ENGINE DAMAGED. REPLACED NR 2 LE SLAT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110700005 20071107 00005 EU 2007 11 7 2007UALA04450 1 20071027 A 3510 OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE OXYGEN MASK INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 427UA 512 F/O OXYGEN REGULATOR INOPERATIVE. REPPLACED FO'S O2 MASK OPS CHECK'D GOOD- NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110700010 20071107 00010 EU 2007 11 7 07FDEA04688 1 20071026 A 5270 SWITCH AIRBUS 300 A300B4622R 3930312 EU ACCESS DOOR DIRTY A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 727FD 579 AFTER TAKEOFF RECEIVED ECAM FOR LOWER ACCESS DOOR NOT CLOSED. FORWARD AND AFT LOWER ACCESS DOORS SWITCHES CLEANED. CH ECKED INDICATION ON ECAM, NORMAL. 2 L 7 2 4F RT A35EU 2007110700011 20071107 00011 WP 2007 11 7 07FDEA04690 1 20071026 A 5347 AGA385521 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 AFT CARGO COMPT SEVERE EXFOLIATION CORROSION ON SEAT TRACK. REPAIRED SEAT TRACK SECTION IAW SRM 53-70-00 VOL I FIG 1. 2 L 7 3 4F RT A22WE 2007110700031 20071107 00031 WP 2007 11 7 AALA20072002 1 20071020 A 3241 TRANSDUCER DOUG DC9 DC983 3022083 WP ANTI SKID SYS INOPERATIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 599AA 53289 COS INFLIGHT T1009/20OCT - EXTENDED LANDING GEAR ON FINAL. ATTEMPTED TO ARM AUTO BRAKES NUMBER TWO. ANTI-SKID LIGHT IL LUMINATED ON LEFT OUTBOARD AND RIGHT INBOARD. ALSO, LANDING WHEEL NOT TURNING INDICATION. LANDED COS WITHOUT INCIDENT. BOTH LEFT OUTBOARD AND RIGHT INBOARD TRANSDUCERS BAD. REPLACED ANTI-SKID CONTROL BOX. SYSTEM GROUND CHECKED NORMAL O PERATION. 2 L 7 2 4F RT A6WE 2007110700032 20071107 00032 NM 2007 11 7 AALA20071989 1 20071019 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 185AN 32379 SFO - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 16DEF TO 26DEF INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EME RGENCY LIGHTS AT SEAT ROWS 16DEF TO 26DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007110700033 20071107 00033 WP 2007 11 7 AALA20071975 1 20071018 A 2497 CABLE DOUG DC9 DC983 3022083 WP SEAT 5EF DISCONNECTED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 964TW 53614 MEM INFLIGHT T482/18OCT DFW TO IND, SMOKE REPORTED COMING FROM AREA BELOW SEATS 5EF AN 6EF. LANDED MEM WITHOUT INCIDENT . SMOKE DISSIPATED PRIOR TO ARRIVAL AT GATE. FOUND TWO WIRES TO SEAT 5EF POWERPORT DISCONNECTED BUT NO ARCING WAS EVID ENT. INSPECTED CARGO AREA WITH NO DAMAGED NOTED. REATTACHED POWERPORT CABLE AT SEAT 5EF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007110700034 20071107 00034 NM 2007 11 7 AALA20071992 1 20071020 A 3350 P4010049 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 329AA 22329 JFK - EMERGENCY LIGHTS AT SEAT ROWS 9B TO 11B, 17B AND 19B INOPERATIVE. REPLACED BATTERY PACK M9030 AISLE FOR EMERGENCY LIGHTS AT SEAT ROWS 9B TO 11B, 17B AND 19B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007110700035 20071107 00035 NM 2007 11 7 AALA20071999 1 20071020 A 2613 OVERHEAT LOOP BOEING 737 737823 13844BZ NM RT ENGINE INOPERATIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 973AN 29548 DFW INFLIGHT T1847/20OCT - MASTER CAUTION AND RIGHT WING BODY OVERHEAT LIGHT ILLUMINATED. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. REPLACED LOOP M1763 AT RIGHT ENGINE PYLON. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007110700036 20071107 00036 NM 2007 11 7 AALA20072000 1 20071020 A 2613 ELEMENT BOEING 737 737823 13844BZ NM RIGHT WING FAULTED A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 958AN 30091 DFW INFLIGHT T2196/20OCT - RIGHT WING BODY OVERHEAT LIGHT ILLUMINATED DURING CLIMB-OUT. THE LIGHT EXTINGUISHED AFTER PROCEDURES COMPLETED. RIGHT PACK PRESSURE WAS BELOW 20 POUNDS PER SQUARE INCH DURING CLIMB-OUT. LANDED DFW WITHOUT INC IDENT. REPLACED M1763 ELEMENT AT RIGHT ENGINE PYLON. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007110700037 20071107 00037 NM 2007 11 7 AALA20071997 1 20071020 A 3350 LAMP BOEING 767 767223 1385123 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 328AA 22328 JFK - EMERGENCY LIGHT AT SEAT 30H MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 30H. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007110700038 20071107 00038 NM 2007 11 7 AALA20071984 1 20071018 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 DFW - EMERGENCY LIGHT AT SEAT 25C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110700039 20071107 00039 NM 2007 11 7 AALA20071985 1 20071018 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 770AN 29578 DFW - EMERGENCY LIGHT AT SEAT 26C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110700040 20071107 00040 NM 2007 11 7 AALA20071986 1 20071018 A 3350 BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 DFW - EMERGENCY LIGHT AT SEAT 34G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 34G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110700041 20071107 00041 NM 2007 11 7 AALA20071996 1 20071020 A 3350 LENS BOEING 767 767223 1385123 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 328AA 22328 JFK - EMERGENCY LIGHT AT SEAT 30H MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 30H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007110700042 20071107 00042 NM 2007 11 7 AALA20071987 1 20071018 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 DFW - EMERGENCY LIGHT AT SEAT 31G INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 31G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110700043 20071107 00043 NM 2007 11 7 AALA20071983 1 20071018 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 DFW - EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110700044 20071107 00044 NM 2007 11 7 AALA20071976 1 20071018 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 755AN 30263 MIA - EMERGENCY LIGHT AT SEAT 24C DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110700045 20071107 00045 NM 2007 11 7 AALA20071977 1 20071018 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 755AN 30263 MIA - EMERGENCY LIGHT AT SEAT 25C DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110700046 20071107 00046 NM 2007 11 7 AALA20071978 1 20071018 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 755AN 30263 MIA - EMERGENCY LIGHT AT SEAT 32C DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 32C. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110700047 20071107 00047 NM 2007 11 7 AALA20071995 1 20071020 A 3350 OL3071BPEGPL BULB BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 MIA - EMERGENCY LIGHTS AT SEAT 42G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 42G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110700048 20071107 00048 NM 2007 11 7 AALA20071979 1 20071018 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 755AN 30263 MIA - EMERGENCY LIGHT AT SEAT 34C DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 34C. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110700049 20071107 00049 WP 2007 11 7 AALA20071980 1 20071018 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 3515 49892 LGA - EMERGENCY LIGHTS AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110700050 20071107 00050 NM 2007 11 7 AALA20071993 1 20071020 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AA 25201 JFK - EMERGENCY LIGHT AFT OF MID GALLEY RIGHT SIDE INOPERATIVE. RECONNECTED LOOSE PLUG FOR EMERGENCY LIGHT AFT OF MID G ALLEY RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007110700062 20071107 00062 NM 2007 11 7 HALA0700451 1 20071018 A 3697 WIRE BOEING 767 7673G5 1385126 NM SHUTOFF VALVE DAMAGED A HALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM - ATB - L-HPSOV EICAS AND "BLEED" LT ON PANEL INTERMITTENT AT FL 32000. PERFORMED BITE CHECK O N PNEUMATIC SUPPLY MODULE, LT PSOV WIRING FAULT DISPLAYED. REPAIRED WIRE TERMINAL ON HPSOV CONNECTOR NR 1. NO MESSAGES OR FAULT LIGHTS DURING HIGH POWER ENGINE RUN-UP. OPERATIONAL TEST NORMAL IAW AMM 36-11-00. 2 L 7 2 4F RT A1NM 2007110700065 20071107 00065 NM 2007 11 7 HALA0700454 1 20071023 A 3150 3103440 CONTROL MODULE BOEING 767 7673CB 1385187 NM DISPLAY MALFUNCTIONED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 588HA 33466 ETOPS SIGNIFICANT SYSTEM, CENTER ENGINE UPPER AND LOWER CRT'S FLASHED BLACK, THEN BACK ON AND NORMAL, 7+ TIMES DURING FL IGHT. ALL OTHER INDICATIONS NORMAL, BOTH FLASHED TOGETHER. T/S PER FIM 31-41-00 FIG 104, 105. REMOVED UPPER AND LOWER DU'S CHECK COOLING. NO FAULTS FOUND. AFTER T/S AND A/C POWER UP UPPER DU FAILED TO DISPLAY. FOUND BAD PIN ON UPPER D ISPLAY SW MODULE M10417. REMOVED AND REPLACED DU'S PER AMM 31-41-01-004-001/404-002. REMOVED AND REPLACED CONTROL MODU LE PER AMM 31-41-04-004-001/404-001. PRFD EICAS BITE OPS PIN CK OK. 2 L 7 2 4F RT A1NM 2007110700066 20071107 00066 NM 2007 11 7 HALA0700455 1 20071024 A 7830 BLOCKER DOOR BOEING 767 7673G5 1385126 NM PWA 4060 PW4060 52119 NE THRUST REVERSER BROKEN A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 NR 1 ENG THRUST REVERSER BLOCKER DOOR BROKE OFF 6 O'CLK POS. OK TO CONTINUE PER L CDL78-31-3. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110700068 20071107 00068 NE 2007 11 7 HALA0700457 2 20071024 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE MALFUNCTIONED A HALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, AT TOP OF DESCENT W/BOTH THROTTLES BACK THE FOLLOWING ENG READINGS NR 1 N1 50.2 EGT 316 N2 78. 5 F/F 1000 NR 2 ENG READING WERE N1 36.2 EGT 306 N2 69.0 F/F 500. AT 19,000 FT TO 18,000 BOTH ENGS READ THE SAME. ENGI NES APPROACH IDLE W/SN LIMITS PER AMM 71-01-02-201. OK FOR SVC ACCOMP BITE CHK OF EEG'S. NO DEFECTS NOTED REQUEST BARO , OAT DATA. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110800005 20071108 00005 CE 2007 11 8 DXTA200702567 1 20071024 A 3220 6740215 ELASTOMER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG WORN E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 941QS 7079 7500141 EXTREME NOSE WHEEL SHIMMY DURING T/O ROLL. ABORTED TAKEOFF. REPLACED LNLG WHEEL/TIRE ASSY P/N 3-1538-1, S/N 1384, TIRE S P/N M15601, S/N 6275A063 W/ WHEEL/ TIRE S/N 0350, TIRE S/N 6270A197. REPLACED RNLG WHEEL/TIRE ASSY AN3-1538-1, S/N 13 81, TIRE P/N M15601, S/N 6276A111 W/ WHEEL/TIRE S/N 0665, TIRE S/N 6271A103. REPLACED ELASTEMERS P/N 674021-5, SPACERS 6242217-5, SUPPORT CUPS 6742217 - 6, PIN 674 2217-9 & WASHERS 6242217-3. IAW 12-10-30, 32-47-01, AFM 75FM-10-2-7, & 32 -30-03. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007110800006 20071108 00006 CE 2007 11 8 DXTA200702568 1 20071024 A 5320 MS35061 RECEPTACLE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE GROUND POWER DAMAGED E DXTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 142QS 1295 RK432 AIRCRAFT TAXIED WITH GPU STILL ATTACHED. REMOVED AND REPLACED GPU POWER RECEPTACLE IAW 24-40-00. OPS CHECK WAS GOOD. 2 H 7 2 4F 4 F RT A16SW E25EA 2007110800007 20071108 00007 CE 2007 11 8 DXTA200702569 1 20071024 A 3243 9536717 MASTER CYLINDER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE BRAKES INTERMITTENT E DXTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 394QS 698 5600394 CAPTAIN -SIDE BRAKES ARE EXTREMELY MUSHY AND INTERMITTENT. LT PEDAL WENT TO THE FLOOR AND BRAKING WAS LOST ON THAT SIDE . REPLACED PILOTS LT WHEEL MASTER CYLINDER WITH AN OVERHAULED UNIT IAW MM 32-42-00 SYSTEM OP CK'S GOOD. REPLACED PIL OTS RT WHEEL MASTER CYLINDER WITH AN OVERHAULED UNIT FROM SAF INDUSTRIES CRS GK0R519Y IAW MM 32-42-00 PERFORMED TAXI T EST CAPTAINS SIDE BRAKES OP CK GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2007110800017 20071108 00017 EU 2007 11 8 2007UALA04414 1 20071028 A 3350 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 430UA 568 DURING 3SVC CHECK FOUND EMERGENCY LIGHT TEST FAIL DOOR 1L. FOUND BATTERY FAILED. REPLACED EPSU (FWD LEFT) OPS CHECK G OOD -NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110800029 20071108 00029 NM 2007 11 8 2007UALA04423 1 20071027 A 2611 2156756 SMOKE DETECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 180UA 25224 MSG SMOKE DR 5 REST CAME ON. SUSPECT FAULTY SMOKE DETECTOR. REPLACED SMOKE DETECTOR ZONE 1A. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110800048 20071108 00048 NM 2007 11 8 2007UALA04441 1 20071027 A 5315 ANGLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 MAIN CABIN AT STA 287 APPROX RBL 80, FLOORBEAM ANGLE P/N 141T5111-45 IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REPLACED ANGLE P/N 141T5111-45. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110800069 20071108 00069 WP 2007 11 8 ABXA070356 1 20071008 A 5210 59100817 REPAIR DOUG DC9 DC941 302207N WP PAX DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 962AX 47768 MAIN ENTRY DOOR FORWARD LOWER CORNER REPAIR CRACKED. REMOVED AND REPLACED REPAIR IAW DC9 SRM 52-01 FIG 4. 2 L 7 2 4F A6WE 2007110800082 20071108 00082 EU 2007 11 8 TRAX200701595 1 20071025 A 5330 SKIN AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 EXT FUSELAGE SKIN CORRODED FR 30, LEFT STR 21. CORROSION ON SKIN REMOVED IAW SRM 51-21-42 WITHIN TOLERENCE IAW 53-61- 00 FIG 301 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMP LISHED IN ACCORDANCE WITH SRM 51-21-42. MATERIAL THICKNESS: MATERIAL REMOVED: 0.001WITHIN LIMITS AS PER SRM: 53-61-00 FI G 301. 2 H 7 2 4T RT 2007110800086 20071108 00086 EA 2007 11 8 TRAX200701600 1 20071026 A 3350 COVER CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 826AS 7210 EMERGENCY TRACK LIGHTING COVER LOOSE AT ROW 1 AND END CAP MISSING. FLT 4630 DEL 28 MINS. 2 L 7 2 4F RT A21EA 2007110800100 20071108 00100 EU 2007 11 8 USAA920071037 1 20071027 A 5554 D5537131800200 HINGE FITTING AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - RUDDER HINGE FITTING NR 3 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STA 2279 / RIB 5. RE PLACED RUDDER HINGE FITTING NR 3, VERTICAL STABILIZER STA 2279 / RIB 5 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007110800101 20071108 00101 EU 2007 11 8 USAA920071038 1 20071028 A 5554 D5537131800200 HINGE FITTING AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - RUDDER HINGE FITTING NR 4 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STA 2632 / RIB 6. RE PLACED RUDDER HINGE FITTING NR 4, VERTICAL STABILIZER STA 2632 / RIB 6 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007110800120 20071108 00120 NM 2007 11 8 USAA920071048 1 20071019 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, CRACKED FRAME, BS 480, S8L - S9L. REPAIRED FRAME, BS 480, S8L - S9L IAW USAIRWAYS TYPIC AL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2007110800146 20071108 00146 NM 2007 11 8 USAA920071053 1 20071030 A 5330 65C30803 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 PHX - MAJOR REPAIR - CRACKED FUSELAGE SKIN, BS 757, S23R. REPAIRED FUSELAGE SKIN CRACK, BS 757, S23R IAW B737 SRM 53-00 -01. 2 L 7 2 4F RT A16WE 2007110800174 20071108 00174 NM 2007 11 8 SB07093 1 20071027 A 3350 20121 CHARGER BOEING 737 737401 1384701 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 417US 23984 BOS - MAINTENANCE FOUND THE AISLE EMERGENCY LIGHTS AT SEAT ROWS 6 THRU 9, LEFT-HAND SIDE, INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007110800190 20071108 00190 WP 2007 11 8 UPS07851063 1 20071010 A 5320 ATTACH FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 ATTACH FITTING CRACKED AT STA 820 L22L. REMOVED AND REPLACED ATTACH FITTING AT STA 820 L22L IAW SRM 551-03- 02, AND SRM 51-01-20B. 2 L 7 4 4F RT 4A25 2007110800191 20071108 00191 WP 2007 11 8 UPS07851067 1 20071011 A 5313 LONGERON SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 L33R SPLICE FITTING AT STA 1040-1060 IS CRACKED. REMOVED AND REPLACED LONGERON SPLICE FITTING AT STA 1040-1060 L33R IAW SRM 51-1-20D, AND SRM 51-03-02. 2 L 7 4 4F RT 4A25 2007110800192 20071108 00192 WP 2007 11 8 UPS07851069 1 20071007 A 5730 DOUBLER DOUG DC8 DC873F 302199F WP WING PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 REPAIR DOUBLER PUNCTURED ON WING SKIN PANEL BOTTOM SURFACE, IN LT WHEEL WELL NEAR UPLATCH. REMOVED A ND REPLACED REPAIR DOUBLER ON WING SKIN PANEL IN LT WHEEL WELL IAW SRM 51-3-00, AND SRM 57-03-00-0. 2 L 7 4 4F RT 4A25 2007110800226 20071108 00226 EU 2007 11 8 USAA920071013 1 20071018 A 5347 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274AY 342 BFM - MAJOR REPAIR - C2 CHECK, CORROSION ON CABIN SEAT TRACK, BS 4842 / FR 58 - BS 5054 /FR 62. REPAIRED CABIN SEAT TRA CK BS 4842 / FR 58 - BS 5054 /FR 62 IAW A330 SRM 53-00-15, 51-44-11 AND 51-42-11. *SUPP* AIRCRAFT MANUFACTURER AND MOD EL WAS CHANGED FROM BOEING 767201ER TO AIRBUS A330323. 2 L 7 2 4F RT A46NM 2007110800227 20071108 00227 EU 2007 11 8 USAA920071014 1 20071018 A 5347 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274AY 342 BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 3940 / FR 53.1, -Y450. REPAIRED CABIN SEAT TRACK, BS 3940 / FR 53.1, -Y450 IAW A330 SRM 53-31-15 AND 51-42-00. AIRCRAFT MANUFACTURER AND MODEL WAS CHANGED FROM BOEING 7672 01ER TO AIRBUS A330323. 2 L 7 2 4F RT A46NM 2007110800232 20071108 00232 EU 2007 11 8 USAA920071019 1 20071019 A 5350 BRACKET AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274AY 342 BFM - MAJOR REPAIR - C2 CHECK, CORROSION ON BODY FAIRING SUPPORT STRUCTURE BRACKET, BS 2948 / FR 39.2. REPLACED BODY FA IRING SUPPORT STRUCTURE BRACKET, BS 2948 / FR 39.2 IAW A330 SRM 53-35-14 AND 51-42-00. AIRCRAFT MANUFACTURER AND MODEL WAS CHANGED FROM BOEING 767201ER TO AIRBUS A330323. 2 L 7 2 4F RT A46NM 2007110800233 20071108 00233 NM 2007 11 8 USAA920071056 1 20071030 A 5340 69403672 STRINGER CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED STRINGER CLIP, BS 1121, S2R. REPLACED STRINGER CLIP, BS 1121, S2R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007110800236 20071108 00236 NM 2007 11 8 ASAA0772169 1 20071017 A 5320 141A541012 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 CABIN FLOORBEAM AT BS 217 RBL 30 INTERCOSTAL CRACKED. REPLACED WITH NEW PART. 2 L 7 2 4F RT A16WE 2007110800242 20071108 00242 NM 2007 11 8 ASAA0772175 1 20071018 A 5321 453A261016 FLOOR PANEL BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 CORROSION AROUND EDGES OF FLOOR PANEL NR 1 BETWEEN BS 727+4 AND BS 727D AFT CARGO PIT. REPLACED WITH MADE REPAIR PART I AW B737 700 SRM 53-60-53 FIG 2 & 51-40-05. 2 L 7 2 4F RT A16WE 2007110800246 20071108 00246 NM 2007 11 8 ASAA0772179 1 20071019 A 5315 147A55067 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 AFT CABIN BS 986.5 FLOORBEAM UPPER CAP CORRODED AT RBL 10. REPLACE UPPER CAP IAW ERD 7360. 2 L 7 2 4F RT A16WE 2007110800248 20071108 00248 NM 2007 11 8 ASAA0772181 1 20071019 A 5315 147A55067 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 AFT CABIN BS 986.5 FLOORBEAM UPPER CAP CORRODED AT RBL 32. REPLACED UPPER CAP IAW ERD 7360. 2 L 7 2 4F RT A16WE 2007110800252 20071108 00252 NM 2007 11 8 ASAA0772185 1 20071019 A 5320 STRIP BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 CORROSION ON CAP STRIP BETWEEN BS 847 AND BS 947 RT SIDE AFT CARGO. REPLACED CAP STRIP IAW ERD 7347 & B DRWG 453A2611. 2 L 7 2 4F RT A16WE 2007110800254 20071108 00254 NM 2007 11 8 KPVA200718 1 20071028 A 3244 222K682 TIRE DHAV DHC8 DHC8103 1386005 NM NLG FLAT A KPVA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 WP 13 805WP 353 (PIREP) UPON DEPARTURE IN JHM, VIOLENT SHAKING FROM NOSE. TAXI CLEAR, REALIZED 2 NOSEWHEEL TIRES FLAT. (MX) REMOVED AN D REPLACED NLG WHEEL ASSY NR 1 & 2 IAW DHC-8 MM 32-41-16 PG 201-205. (1) P/N 3-1448 S/N 1323 (2) P/N 3-1448 S/N 2401. INSPECTION OF TIRES AND WHEEL ASSY SHOWS NO VISIBLE DEFECTS. 2 H 7 2 4T RT A13NM 2007110800255 20071108 00255 NM 2007 11 8 KPVA200719 1 20071030 A 2120 UNKNOWN DHAV DHC8 DHC8103 1386005 NM COCKPIT SMOKE A KPVA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 13 829EX 146 CLIMBING OUT OF JHM AT 500FT AGL, SMOKE IN COCKPIT. (MX) INSPECTED WARDROBE, FLIGHT DECK, CABIN, AVIONICS RACKS. RAN A IRCRAFT ON GROUND. RUN UP, OPS CHECKS GOOD. NO SMOKE OR ODOR NOTED. AIRCRAFT RELEASED FOR A POST MAINTENANCE CHECK FL IGHT. CHECK FLIGHT SATISFACTORY. 2 H 7 2 4T RT A13NM 2007110800257 20071108 00257 SO 2007 11 8 LR7A07103 1 20071001 A 5320 CHANNEL LKHEED 382 382G 526414U SO NLG WW CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2661 4763 DURING SCHEDULED C-7 CHECK PER JOB CARD HC3215 FOUND NOSE WW BULKHEAD U-CHANNEL CRACKED AT FS 196 WL 145 BL 0. REPAIR A CCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70. 2 H 7 4 4T A1SO 2007110800258 20071108 00258 SO 2007 11 8 LR7A07104 1 20071001 A 5320 ATTACH ANGLE LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2661 4763 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5324 FOUND UPPER MWW ATTACH ANGLE WITH MULTIPLE CRACKS AT FS 477 TO 517 WL 280 RBL 62.5. REPAIR ACCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70 USING 7075T6 .050". 2 H 7 4 4T A1SO 2007110800261 20071108 00261 SO 2007 11 8 LR7A07107 1 20071001 A 5320 BEAM LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2661 4763 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5324 FOUND RT UPPER MWW BOW BEAM CRACKED AT FS 537 WL 202 RBL 64. REPAIR ACCO MPLISHED IAW SMP583 FIG 53-40-14 USING 7075T6 .100". 2 H 7 4 4T A1SO 2007110800262 20071108 00262 SO 2007 11 8 LR7A07108 1 20071001 A 5320 339482 MANIFOLD LKHEED 382 382G 526414U SO RT MLG WW CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2661 4763 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5324 FOUND RIGHT MWW MANIFOLD CRACKED AT FS 607 WL 146 RBL 62. REPAIR ACCOMPL ISHED BY REPLACING MANIFOLD IAW SMP583 CHAPTER 51-60 & 51-70. 2 H 7 4 4T A1SO 2007110800263 20071108 00263 SO 2007 11 8 LR7A07109 1 20071001 A 5230 SKIN LKHEED 382 382G 526414U SO CARGO DOOR CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2661 4763 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5212 FOUND AFT CARGO DOOR AFT BULKHEAD SKIN CRACKS AT FASTENER HOLES FS 1040 W L 268 LBL 44 RBL 44. REPAIR ACCOMPLISHED BY REPLACING SKIN IAW SMP583 CHAPTER 51-60 & 51-70 USING 7075T6 .025". 2 H 7 4 4T A1SO 2007110800264 20071108 00264 SO 2007 11 8 LR7A07110 1 20071001 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE DEFORMED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2661 4763 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5321 FOUND BELLY EXTERIOR SKIN DENTS / SCRATCHES WITH EXISTING PATCHES AT FS 3 77 TO 417 BL 61L TO 61R. REPAIR ACCOMPLISHED BY REPLACING BELLY SKIN IAW SMP583 CHAPTER 51-60 & 51-70 USING 2024T3 .071 ". 2 H 7 4 4T A1SO 2007110800265 20071108 00265 SO 2007 11 8 LR7A07111 1 20071001 A 5531 LONGERON LKHEED 382 382G 526414U SO VERTICAL STAB CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2661 4763 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5511 FOUND LT & RT DORSAL FIN LOWER LONGERON REPAIR DOUBLER FOUND CRACKED AT F S 850. REPAIR ACCOMPLISHED IAW LYNDEN AIR CARGO MEA382-53-00-087 AND MEA382-53-00-088. 2 H 7 4 4T A1SO 2007110800266 20071108 00266 SO 2007 11 8 LR7A07112 1 20071001 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2661 4763 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5313 FOUND AFT FUSELAGE INTERIOR BULKHEAD WEB CRACK AT HI-LOK PIN HOLE FS 880 WL 210 RBL 73. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-17 USING 7075T6 .040". 2 H 7 4 4T A1SO 2007110800270 20071108 00270 SO 2007 11 8 LR7A07116 1 20071001 A 2120 33138901 BRACKET LKHEED 382 382G 526414U SO CARGO BAY CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2661 4763 DURING SCHEDULED C-7 CHECK PER JOB CARD HC2111 FOUND CARGO AIR COND AUX VENT DUCT ASSY UPPER & LOWER MOUNTING BRACKET CR ACKED. REPAIR ACCOMPLISHED IAW LYNDEN AIR CARGO MEA 382-21-07-066. 2 H 7 4 4T A1SO 2007110800271 20071108 00271 SO 2007 11 8 LR7A07117 1 20071001 A 4980 331127857 BRACKET LKHEED 382 382G 526414U SO APU EXHAUST CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2661 4763 DURING SCHEDULED C-7 CHECK PER JOB CARD HC4912 FOUND APU EXHAUST DUCT ASSY BRACKET CRACKS. REPAIR ACCOMPLISHED IAW LYND EN AIR CARGO MEA 382-49-07-065. 2 H 7 4 4T A1SO 2007110800273 20071108 00273 SO 2007 11 8 LR7A07119 1 20071001 A 5311 FRAME LKHEED 382 382G 526414U SO FUSELAGE BROKEN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2661 4763 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5324 FOUND RT MLG FRAME OUTBOARD CAP BROKEN AT FS 528 WL 209 & 232 RBL 66. RE PAIR ACCOMPLISHED IAW LYNDEN AIR CARGO MEA 382-53-07-063. 2 H 7 4 4T A1SO 2007110800276 20071108 00276 NM 2007 11 8 CALA0700629 1 20071031 A 5313 6559664501 STRINGER SPLICE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND STRINGER SPLICE 27L CORRODED AT STA 360. THE CHANNEL SPLICE WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND AMM 51-31-00. 2 L 7 2 4F RT A16WE 2007110800280 20071108 00280 EU 2007 11 8 TRAX200701596 1 20071025 A 5714 ANGLE AEROSP ATR72 ATR72 EU WING BOX BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 WING BOX INTERCOSTAL ANGLE BROKEN AT FR 23D, RIGHT STR 2. TRANSFER ON W/C 2000-8. SUPPLEMENTAL - SDR CLOSED 11/01/07. 2 H 7 2 4T RT 2007110800281 20071108 00281 EU 2007 11 8 TRAX200701598 1 20071025 A 5242 DOUBLER AEROSP ATR72 ATR72 EU E&E BAY DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 AFT AVIONIC DOOR AFT HINGE DOUBLER CORRODED. AFT AVIONIC DOOR AFT HINGE DOUBLER CORROSION REMOVED IAW SRM 51-21-42 AND WITHIN LIMITS AS PER SRM 53-81-00 FIG 301. SUPPLEMENTAL - SDR CLOSED 11/01/07. 2 H 7 2 4T RT 2007110800284 20071108 00284 EA 2007 11 8 TRAX200701607 1 20071028 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 849AS 7347 F/O'S WINDSHIELD CRACKED AT FL280. EN ROUTE TO SAT A/C DIVERTED TO JAN DUE TO MTC. EMERGENCY DECLARED. EMERGENCY EQUI PMENT ON STANDBY. 2 L 7 2 4F RT A21EA 2007110800285 20071108 00285 EA 2007 11 8 TRAX200701608 1 20071028 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE J WARNING INDICATION CR CRUISE 1 SO 27 907EV 7648 FLAPS FAIL CAUTION MESSAGE DURING CRUISE. THE FLAPS WERE AT 0 DEGREES. THERE WERE NO CHANGES ON THE ON THE FLAP SELECT OR. A NO FLAP APPROACH AND LANDING WERE DONE. REPEAT WRITE-UP. TOWER DECLARED EMERGENCY. EMERGENCY EQUIPMENT ON STAN DBY. 2 L 7 2 4F RT A21EA 2007110800286 20071108 00286 EA 2007 11 8 TRAX200701609 1 20071028 A 3260 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 828AS 7213 SELECTING GEAR DOWN GEAR DISAGREE WARNING NOSE GEAR INDICATED DOWN LT AND RT MAIN WERE NOT DOWN. FOLLOWED QRH USED MLG MANUAL RELEASE TO EXTEND GEAR. EMERGENCY EQUIPMENT ON STANDBY. FLTS 4269, 4263, 4646, 4665 CX. LANDING GEAR RETRACTIO N SYSTEM. 2 L 7 2 4F RT A21EA 2007110800287 20071108 00287 NM 2007 11 8 USAA920071058 1 20071023 A 5320 6545834525 INTERCOSTAL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED CABIN INTERCOSTAL, BS 344 - BS 360, BL0, WL 208.1. REPLACED CABIN INTERCOSTAL, BS 344 - BS 360, BL 0, WL 208.1 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007110800290 20071108 00290 NM 2007 11 8 SWAA075449 1 20071030 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED OTS CHECK, FOUND STRINGER 28R CORRODED AT BS 322. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007110800292 20071108 00292 NM 2007 11 8 SWAA075407 1 20071028 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 792, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007110800293 20071108 00293 NM 2007 11 8 SWAA075408 1 20071028 A 5210 6545874132 DOOR FRAME BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR LOWER FRAME CRACKED AT AFT END. REMOVED AND REPLACED DOOR PER MM. 2 L 7 2 4F RT A16WE 2007110800294 20071108 00294 NM 2007 11 8 SWAA075409 1 20071028 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515D, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007110800296 20071108 00296 NM 2007 11 8 SWAA075451 1 20071030 A 5320 6545819 WEB BOEING 737 7373H4 1384600 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED HC2 CHECK, FOUND NOSE W/W UPPER CEILING PANEL WEB CRACKED AT BS 229, RBL 16. REPAIRED CEILING PANEL PE R SWA EA. 2 L 7 2 4F RT A16WE 2007110800300 20071108 00300 NM 2007 11 8 SWAA075413 1 20071031 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110800302 20071108 00302 NM 2007 11 8 SWAA075415 1 20071030 A 3350 417A5701 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 428WN 29844 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007110800303 20071108 00303 NM 2007 11 8 SWAA075416 1 20071030 A 2560 10107451 SIGN BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 434WN 32454 RIGHT FWD CABIN EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007110800306 20071108 00306 NM 2007 11 8 SWAA075419 1 20071030 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 475WN 32474 DURING SCHEDULED HC1 CHECK, FWD LT EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007110800307 20071108 00307 NM 2007 11 8 SWAA075420 1 20071030 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 475WN 32474 DURING SCHEDULED HC1 CHECK, AFT LEFT EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007110800308 20071108 00308 NM 2007 11 8 SWAA075421 1 20071030 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 475WN 32474 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK FAILED LONG TEST AT ROW 16 ABC. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2007110800309 20071108 00309 NM 2007 11 8 SWAA075422 1 20071031 A 3350 101331 LENS BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 RIGHT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007110800313 20071108 00313 NM 2007 11 8 SWAA075425 1 20071031 A 3350 65C27093 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 513SW 24190 R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007110800316 20071108 00316 NM 2007 11 8 SWAA075431 1 20071031 A 5311 6546525 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007110800317 20071108 00317 NM 2007 11 8 SWAA075432 1 20071031 A 5311 6546593 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007110800318 20071108 00318 NM 2007 11 8 SWAA075433 1 20071031 A 5311 6546557 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900001 20071109 00001 NM 2007 11 9 AALA20072056 1 20071027 A 3350 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 338AA 22335 JFK - EMERGENCY LIGHTS AT LEFT NUMBER THREE AND LEFT NUMBER FOUR DOOR EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER M1210 FOR EMERGENCY LIGHTS AT LEFT NUMBER THREE AND LEFT NUMBER FOUR DOOR EXIT SIGNS. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A1NM 2007110900002 20071109 00002 EU 2007 11 9 F3LA200700290 1 20071018 A 5320 NUT PLATE AIRBUS A319 A319112 3930323 EU R2 DOOR SILL CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION IN THE AFT OTBD NUTPLATE HOLE OF THE R2 DOOR SILL FWD GIRT BAR FITTING MOUNT PLATE. PERFORMED HFEC ON DAMAGED AREA IAW NTM 51-10-08, PAGES 601-608, AND FOUND NO DEFECTS. FABRICATED AND INS TALLED REPAIR DOUBLER IAW SRM 51-42-11, 53-41-14, 51-74-00, 51-11-13, 51-21-11 AND EA A9-53R-12220. 2 L 7 2 4F RT A28NM 2007110900003 20071109 00003 NM 2007 11 9 DHL2007743A 1 20071101 A 5754 65C8067818 ANGLE BOEING 727 727225 1384077 NM NR 5 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 FOUND RIGHT WING SPAR ANGLE FITTING AT THE INBOARD SIDE OF NR 5 L/E SLAT ACTUATOR TRUNNION CRACKED AT FORWARD END. 2 L 7 3 4F A3WE 2007110900004 20071109 00004 EU 2007 11 9 F3LA200700291 1 20071018 A 5320 NUT PLATE AIRBUS A319 A319112 3930323 EU L2 DOOR SILL CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION IN THE AFT OTBD NUTPLATE HOLE OF THE L2 DOOR SILL FWD GIRT BAR FITTING MOUNT PLATE. PERFORMED ROTO PROBE INSPECTION ON HOLE IAW NTM 51-10-01, PAGES 601-622 AND AND FOUND A CRACK BETWEEN RIV ET HOLE AND FASTENER HOLE. REMOVED DAMAGE AND PERFORMED HFEC, NO DEFECTS FOUND. FABRICATED AND INSTALLED REPAIR DOUBLE R AND FILLER AND INSTALLED NEW NUTPLATE ON REPAIR DOUBLER. WORK ACCOMPLISHED IAW SRM 53-41-14, 51-74-00, 51-10-01, 51-1 0-08, 51-11-13, 51-75-12, 51-42-11 AND EA A9-53R-12218. 2 L 7 2 4F RT A28NM 2007110900006 20071109 00006 EU 2007 11 9 F3LA200700293 1 20071017 A 5330 THRESHOLD AIRBUS A319 A319112 3930323 EU R1 DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED R1 DOOR THRESHOLD STRIP CORRODED ON LOWER SURFACE. REMOVED AND REPLACED R1 DOOR THRESHOLD STRIP IAW MM 53-12-12-400-001. 2 L 7 2 4F RT A28NM 2007110900008 20071109 00008 EU 2007 11 9 TRAX200701594 1 20071025 A 5350 SKIN AEROSP ATR72 ATR72 EU FAIRING CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 ON MLG SKIN CORRODED AT FR 27 BL 0. CORROSION REMOVED ON MLG SKIN AT FR 27 BL 0 IAW SRM 51-21-42 U/T PERFORMED IAW NTM NOM=0.063" MIN=0.060". REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. R EPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42 MATERIAL THICKNESS: 0.063. MATERIAL REMOVED: 0.003 WITHIN LIMITS AS PER SRM: 53-51-00 FIG 301. SUPPLEMENTAL - SDR CLOSED 11/01/07. 2 H 7 2 4T RT 2007110900009 20071109 00009 NM 2007 11 9 QXEA200701636 1 20071030 A 3150 WARNING MESSAGE BOMBDR DHC8 DHC8402 1390042 NM FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 425QX 4039 SEA - ON FLIGHT 2295, RECEIVED POWERPLANT WARNING MESSAGE. CREW RETURNED AIRCRAFT TO GATE. MAINTENANCE INTERROGATED CD S AND FOUND FAULT CODE 130. CLEARED FAULT CODES. OPERATION CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERV ICE. 2 H 7 2 4T RT A13NM 2007110900010 20071109 00010 NM 2007 11 9 USAA920071057 1 20071021 A 5320 654797322 SHEAR WEB BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED CABIN SHEAR WEB, BS 616 - BS 639, S17R, WL 208.1. REPLACED CABIN SHEAR WEB, BS 616 - BS 639, S17R, WL 208.1 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007110900013 20071109 00013 NM 2007 11 9 USAA920071061 1 20071021 A 5340 693535214 STRINGER CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED STRINGER CLIP, BS 578, S8R. REPLACED CRACKED STRINGER CLIP, BS 578, S8R IAW B7 37 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007110900015 20071109 00015 NM 2007 11 9 USAA920071063 1 20071024 A 5340 69414372 STRINGER CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED STRINGER CLIP, BS 663, S10R. REPLACED CRACKED STRINGER CLIP, BS 663, S10R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007110900016 20071109 00016 NM 2007 11 9 USAA920071064 1 20071024 A 5340 66235743 STRINGER CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED STRINGER CLIP, BS 706, S11L. REPLACED CRACKED STRINGER CLIP, BS 706, S11L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007110900018 20071109 00018 NM 2007 11 9 2007UALA03163 1 20070813 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN CONTAMINATED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 330UA 24191 EEL LIGHTING STRIP INOP FROM SEAT 15 ABC TO THE REAR GALLEY. FOUND EEL STRIP NEAR THE GALLEY IN WATER, SHORTING EEL STR IP. REPLACED EEL POWER STRIP AND TWO EEL LIGHTING STRIPS. EEL LIGHTING, OP CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110900019 20071109 00019 NM 2007 11 9 2007UALA03193 1 20070815 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 303UA 23644 EMERGENCY FLOOR LIGHTS INOP. FOUND LAST ROW OF EEL LIGHT SHORTED OUT. REPLACED ALL LIGHTS, CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110900024 20071109 00024 NM 2007 11 9 2007UALA04443 1 20071027 A 3350 CAP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN MISSING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 654UA 25392 EEL STRIP END CAPS MISSING IN FC AND BC ZONES, 5 EA. REPLACED MISSING EEL STRIP END CAPS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110900029 20071109 00029 NM 2007 11 9 2007UALA04463 1 20071029 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 246 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 MAIN CABIN FRAME CAP CORRODED STA 246 BL80R TO BL84R. SUSPECT MOISTURE CONTAMINATION. REMOVED CAP SECTION AND FABRICATE D NEW SECTION. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110900034 20071109 00034 NM 2007 11 9 2007UALA04469 1 20071029 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY EXIT LIGHT INOP AT DOOR 4R CEILING AISLE. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110900036 20071109 00036 NM 2007 11 9 2007UALA04472 1 20071030 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY LIGHT ROW 6GH FWD INOP. RELAMPED LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110900037 20071109 00037 NM 2007 11 9 2007UALA04473 1 20071030 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 CEILING EMERGENCY LIGHT ABOVE ROW 53 RIGHT INOP. RELAMPED LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110900038 20071109 00038 NM 2007 11 9 2007UALA04474 1 20071030 A 5311 FRAME BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BS 1265 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 181UA 25278 BS 1265 LEFT FRAME WEB CRACKED AT NR 1 FASTENER HOLE. REPAIRED FRAME WEB ACCOMPLISHED COA 897887102. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110900040 20071109 00040 NM 2007 11 9 2007UALA04476 1 20071030 A 3350 9F19948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 DOOR 1L EMERGENCY LIGHT INOPERATIVE. REPLACED DOOR 1L DOOR SLIDE EMERGENCY LIGHT ASSY. OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110900041 20071109 00041 2007 11 9 2007UALA04478 4 20071027 A 3460 FMC BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE COCKPIT MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 787UA 26939 CAPTAIN'S FMC POINTING 15 DEGREES RIGHT, F/O' S POINTS STRAIGHT AHEAD. LEFT CALCULATED BEARING HEADING 15 DEGREES DIFFE RENCE FROM RIGHT. EXTENSIVE TROUBLE SHOOTING PERFORMED ON AIMS. UNABLE TO DUPLICATE FAULT. FMC TESTS NORMALLY AFTER RE SET. A/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007110900043 20071109 00043 NM 2007 11 9 2007UALA04484 1 20071030 A 5310 DOOR FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 934UA 26662 FORWARD CARGO COMPARTMENT DOOR CUTOUT FWD FRAME IS CRACKED ON AFT SIDE OF LOWER OUTBOARD CORNER OF BOTTOM DOOR STOP FITT ING. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112800152 20071128 00152 NM 2007 11 28 SWAA075785 1 20071119 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 727E S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 13, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007110900044 20071109 00044 NM 2007 11 9 2007UALA04486 1 20071030 A 2560 SLEEVE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU GIRT BAR FRAYED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 FWD ENTRY DOOR SLIDE GIRT BAR NYLON SLEEVE IS FRAYED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110900046 20071109 00046 NM 2007 11 9 2007UALA04489 1 20071030 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 AFT CARGO PIT STRINGER CLIP CRACKED AT STATION 747 STRINGER 24L. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110900049 20071109 00049 NM 2007 11 9 2007UALA04492 1 20071031 A 5210 DOOR FRAME BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE R1 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 181UA 25278 NR 1 RIGHT MED UPPER FRAME CRACKED AT CENTER UPPER GATE HINGE ATTACH HOLE. REPAIRED CRACK PER IAW FRR UAL-744-0317. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110900050 20071109 00050 NM 2007 11 9 2007UALA04493 1 20071030 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 L2 DOOR AT UPPER HINGE CUTOUT IS DAMAGED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110900052 20071109 00052 NM 2007 11 9 2007UALA04496 1 20071030 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 EXTERIOR SKIN AT STA 416 BETWEEN STR 1L AND 2L IS DENTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110900053 20071109 00053 NM 2007 11 9 2007UALA04497 1 20071030 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 SMALL DENT AT NOSE AREA LEFT SIDE AFT OF PLANE NOSE NUMBER. CUT OUT DAMAGE AND INSTALLED REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110900054 20071109 00054 NM 2007 11 9 2007UALA04498 1 20071031 A 2560 BULB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FLASHLIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 646UA 25283 EMERGENCY FLASHLIGHT AT MID GALLEY CLOSET INOP. SUSPECT FAULTY BULB OR BATTERIES. REPLACED FLASHLIGHT, NOW OPS OK. ACF T OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110900055 20071109 00055 2007 11 9 2007UALA04499 4 20071031 A 2565 HOSE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE COLLAPSED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 HOSE ASSY FOR RAMP SLIDE INFLATION HAS COLLAPSED. SUSPECT HOSE DAMAGED DURING MAINTENANCE. REPLACED HOSE ASSEMBLY. ACF T OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110900056 20071109 00056 NM 2007 11 9 2007UALA04482 1 20071030 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE AFT CARGO PIT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 AFT CARGO PIT HAS 8 STRINGER CLIPS CRACKED, FOUND DURING COA SKIN REPMT BS 727E STR 22L, BS767 STR'S 21L AND 25L, BS787 STR'S 21L AND 24L, BS 827 STR'S 22L AND 25L, ADD BS847 STR25L. 2 L 7 2 4F 4 F RT A16WE E2GL 2007110900057 20071109 00057 NM 2007 11 9 2007UALA04501 1 20071030 A 2721 TRIM SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RUDDER MALFUNCTIONED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 545UA 25323 CREW REPORT: UNABLE TO MOVE RUDDER TRIM WITH RUDDER TRIM KNOB. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110700069 20071107 00069 NE 2007 11 7 HALA0700458 2 20071020 A 7250 PW40603 TURBINE BLADES BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE ENGINE DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 589HA 11176 11176 33422 ETOPS SIGNIFICANT SYSTEM, DURING BOROSCOPE INSP LOOKING THROUGH AP-11 ACCESS. PORT FOUND 2 STAGE HIGH STAGE PRESSURE TU RBINE BLADE DAMAGE ON NR 2 ENG. ACCOMPLISHED ENGINE INSTALLATION IAW HAL M275-767 NR 2 ENGINE. OPS AND LEAK CHECK GOOD . OK FOR SERVICE. VERIFICATION FLIGHT CHECKED GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110700070 20071107 00070 NM 2007 11 7 HALA0700448 1 20071011 A 8011 774860A4 STARTER BOEING 767 767300 1385204 NM PWA 4060 PW4060 52119 NE RT ENGINE FAILED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM, UPON STARTING THE RIGHT ENGINE, EVERYTHING APPEARED NORMAL AT 26 PERCENT N2. INTRODUCE FUEL, FUEL FLOW NORMAL GOOD LIGHT OFF, N1 READING. AT ABOUT 1 MIN AND 45 SEC N2 STARTING TO DECREASE TO 22% N2. DISCONTINUE START MOTORED FOR 30 SEC (EGT AT 390 NORMAL). REMOVED AND REPLACED RT ENGINE STARTER WITH NEW STARTER AS PER AMM 80-11- 01. SERVICED STARTER OIL AS PER AMM 12-13-02/301. RT ENGINE GROUND RUN UP SATISFACTORY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110700071 20071107 00071 NM 2007 11 7 TSAA0753060 1 20071028 A 5330 65458001000 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 817AL 23292 IN THE PROCESS OF ECO 3512, NDT INSPECTION DISCOVERED THE AFT CARGO DOOR CUTOUT AFT FRAME CRACKED. REPLACED THE FRAME IN ACCORDANCE WITH ECO 3512. 2 L 7 2 4F RT A16WE 2007110700072 20071107 00072 NM 2007 11 7 TSAA0753058 1 20071028 A 5330 65458001000 SKIN BOEING 737 7372X6C 1384552 NM BS 927-940 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 IN THE PROCESS OF SSIP, NDT INSPECTION DISCOVERED RT SKIN CRACKED IS BETWEEN LAP JOINT AND LARGE EXISTING REPAIR. CRAC K LOCATED AT BS 927 +13 BETWEEN STRINGER 20R AND 21R. CRACK APPROXIMATELY 3.5 INCHES LONG. 11/11/07 - CRACK WAS REPAIR ED IN ACCORDANCE WITH ECO 3685. 2 L 7 2 4F RT A16WE 2007110700073 20071107 00073 NM 2007 11 7 NWAA073566310 1 20071025 A 3350 FUSE BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670US 24225 DURING OVERNIGHT CHECK, FOUND RIGHT BODY FAIRING EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED FUSE O N POWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007110700074 20071107 00074 SO 2007 11 7 888331 2 20071029 A 7314 64624019A1 PUMP CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO RT ENGINE SEIZED E HYIA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 NE 01 88833 343 343 402C0265 832090R AIRCRAFT WAS IN CRUISE AND THE RIGHT ENGINE SHUT DOWN WITHOUT WARNING. PILOT PERFORMED EMERGENCY CHECK LIST, DECLARED A ND EMERGENCY AND DIVERTED TO MVY AIRPORT. AIRCRAFT LANDED WITH NO FURTHER INCIDENT, TAXIED TO GATE ON 1 ENGINE, AND DEP LANED 7 PASSENGERS. MAINTENANCE INSPECTED AND FOUND THE RIGHT ENGINE DRIVEN PUMP TO BE SEIZED. MAINTENANCE REMOVED AND REPLACED PUMP, AND OPERATIONALLY CHECKED THE PUMP SATISFACTORY. 1 L 7 2 3O 3 O A7CE E8CE 2007110800014 20071108 00014 CE 2007 11 8 DXTA200702572 1 20071023 A 2730 66600031 CONTROL CABLE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE ELEVATOR FRAYED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 663QS 3257 5605263 ELEVATOR TRIM CABLE FRAYED IN TAIL OF AIRCRAFT AT THE DEICE BOOT PRESSURE SWITCHES. REMOVED PANELS FOR ACCESS CABLE R & R AFT LT TRIM CABLE IAW MM 27-32-02. DURING TRAVEL CHECKS FOUND RT AFT CABLE FRAYED. NEW CABLE ASSY P/N 6660003-1 ON O RDER. BEGAN REMOVING CABLE ASSEMBLIES. OK TO INSTALL NEW AFT ELEVATOR TRIM CABLE ASSY REMOVED AFT ELEVATOR TRIM CABLE ASSY. BEGAN INSTALLING NEW CABLE ASSY. INSTALLED NEW CABLE ASSY IAW MM 27-32-02. IAW MM 27-31-03 AND 27-31-00. COMPLIED WITH TENSION CHECK & TRAVEL CHECK. TENSION & TRAVEL CHECK GOOD. INSTALLED ELEVATOR TRIM ACTUATOR ACCESS PANELS & STAB PA NELS AS REQUIRED. INSTALLED AFT BELLY PANEL AS REQUIRED. INSTALLED AFT BAGGAGE ACCESS PANELS AS REQUIRED. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007110800016 20071108 00016 EU 2007 11 8 2007UALA04413 1 20071027 A 3350 LAMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 421UA 500 EMERGENCY LIGHT TEST FAILED ON 3SVC. FOUND LAMPS AT OVER WING LOCATION WERE OUT AND BATTERY FAILED AT FWD LOCATION. RE PLACED BATTERY AT FWD MED AND RELAMPED EMER LIGHTS ON OVER WING EXIT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110800019 20071108 00019 CE 2007 11 8 DXTA200702573 1 20071025 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LT & RT WEAK E DXTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 316QS 5600516 PILOTS RT BRAKE PEDAL GOES SOFT AFTER INITIAL APPLICATION. THE RT PEDAL TRAVELS SIGNIFICANTLY FURTHER THAN THE LT BRAKE PEDAL. BLED LT AND RT BRAKES IAW MM 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007112800024 20071128 00024 NM 2007 11 28 SWAA075733 1 20071116 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 751 S14R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 751, STR 14R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007110800021 20071108 00021 NM 2007 11 8 2007UALA04418 1 20071026 A 5754 SLAT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 4 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 NR 4 SLAT AFT ROW FASTENER HOLES CRACKED AT LOWER SIDE OF I/B AUX TRACK. MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGE, FA BRICATED FILLER AND SPLICE PLATE, TREATED, PRIMED, INSTALLED REPAIR AND PAINTED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110800023 20071108 00023 CE 2007 11 8 DXTA200702574 1 20071025 A 3240 321053 METERING UNIT CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE BRAKE ASSY INTERMITTENT E DXTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 619QS 235 5605562 AT TAXI SPEEDS OF 15 MPH AND LESS, BOTH BRAKES GRAB INTERMITTENTLY AND INDEPENDENTLY OF EACH OTHER. THE BRAKES CAUSED TH E AIRCRAFT TO LURCH AND SHUDDER. REMOVED & REPLACED FAULTY BRAKE METERING VALVE IAW C560XL M.M. 32-44-20. OPS & LEAK CH ECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007110800025 20071108 00025 CE 2007 11 8 DXTA200702575 1 20071026 A 3220 STRUCTURE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG DAMAGED E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 947QS 7500047 ON TAKEOFF, NOSE WHEEL SHIMMY WAS ENOUGH TO CAUSE GYROS TO GO OFF LINE SO TAKEOFF WAS ABORTED. FOUND UPPER SCISSOR LT S IDE HARDWARE TO BE WORN. R & R HARDWARE WITH NEW IAW MM 32-20-00- NO OTHER DEFECTS NOTED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007110800028 20071108 00028 CE 2007 11 8 DXTA200702576 1 20071027 A 3230 55275043 UPLOCK CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE NLG INOPERATIVE E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 650QS 6580 5605150 AFTER NORMAL T/O AND GEAR RETRACTION, THE HYD PRESSURE AND GEAR UNLOCK ANNUNCIATOR REMAINED ILLUMINATED. REMOVED THE NO SE GEAR UPLOCK ACTUATOR AND REPLACED WITH A NEW NOSE GEAR UPLOCK ACTUATOR SUPPLIED BY CESSNA AIRCRAFT COMPANY. PERFORMED THE NOSE GEAR UPLOCK ADJUSTMENT/TEST ALL WORK PERFORMED IAW MM 32-30-05. LUBRICATED ALL GEAR LINKAGES PERFORMED SEVERAL LANDING GEAR EXTENSION AND RETRACTION CHECKS IAW MM 32-30. ALL CHECKS SATISFACTORY AT THIS TIME. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007110800043 20071108 00043 NM 2007 11 8 2007UALA04436 1 20071026 A 5210 RESERVOIR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR UNRELIABLE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 517UA 24861 DOOR 4L EMERGENCY POWER RESERVOIR MISSING LIFT LIMIT AND MANUFACTURE DATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110800046 20071108 00046 NM 2007 11 8 2007UALA04439 1 20071026 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 MAIN CABIN FRAME T-CAP CORRODED STA 303 BL51R TO BL55R. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SECTION OF T-CAP. FABRICATED T-CAP SPLICE. INSTALLED TEE CHORD, ANGLE & SPLICE REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110800049 20071108 00049 NE 2007 11 8 2007UALA04444 2 20071027 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 VIBRATION A UALA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 658UA 27113 724698 ENG 2 VIBRATIONS SHIFTED UP FROM 0.2 TO 0.8 UNITS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110800052 20071108 00052 NM 2007 11 8 KCSA071504 1 20071030 A 5315 FLOORBEAM BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FORWARD PIT FLOORBEAM UPPER CHORD CORRODED AT BS 960, RBL 44. 2 L 7 4 4F RT A20WE 2007110800054 20071108 00054 WP 2007 11 8 ABXA070350 1 20071025 A 5330 59114031 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 LEFT FUSELAGE SKIN CRACKED AT STATIOIN 180 AT LONGERON 22. REPAIRED SKIN IAW EA 53300001-003-4, CONFIG -7009. 2 L 7 2 4F A6WE 2007110800063 20071108 00063 EU 2007 11 8 07FDEA04714 1 20071102 A 2133 VST1650 OUTFLOW VALVE AIRBUS 300 A300B4622R 3930312 EU CABIN AIR FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 25 726FD 575 OVBD FLOW EXTRACT FAN FAULT WENT OVERBOARD THEN LOST PRESSURIZATION. DECLARED EMERGENCY DIVERTED TO MEMPHIS, WARNING H ORN BREAKER H60 PULLED FOR MAINT PURPOSES. FOUND VENT-EXTRACT FAN AND VALVES CNTL C/B TRIPPED. RESETT. C/B TRIPPED W HEN VENT EXTRACT SELECTED OFF AND OVERBOARD EXTRACT VALVE TRIED TO DRIVE CLOSED. REMOVED AND REPLACED OVERBOARD EXTRACT VALVE 75HR. IN REF TO A300-600 AMM. 21-23-13-4. OPS TEST NORMAL. 2 L 7 2 4F RT A35EU 2007110800065 20071108 00065 EA 2007 11 8 TRAX200701648 1 20071031 A 5320 6013501251 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 LEFT OBLIQUE ANGLE AT FS 625 IS CRACKED. REMOVED LT CRACKED OBLIQUE ANGLE AT FS 625. OK TO INSTALL NEW SERVICABLE OBLIQ UE ANGLE. INSTALLED NEW SERVICABLE OBLIQUE ANGLE AT FS 625 IAW CRJ 200 SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007110800067 20071108 00067 EA 2007 11 8 TRAX200701653 1 20071031 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 LBL 36 I/B CLIP CRACKED. CUT-OUT ATTACHMENT FLANGE FS 484 LBL 36 I/B. IAW REO 601-53-41-059. PERFORMED LPI PER NDTM 5 1-20-08 ON CUT-OUT AREA OF FS 484 INTERCOSTAL AT LBL 36, IAW REO 601R-53-41-059, REV A (NO DEFECTS NOTED). INSTALLED RE PAIR, IAW REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2007110800068 20071108 00068 CE 2007 11 8 DXTA200702564 1 20071023 A 2740 615101 BYPASS VALVE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 650QS 4076 4076 5605150 AFTER NORMAL T/O FOLLOWING SOP'S GOT A FLASHING MASTER CAUTION HDG, STAB MISCOMPARE. REMOVED AND REPLACED BYPASS AND LAN DING VALVE IAW MM 29-11-04 GROUND AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007110800074 20071108 00074 NM 2007 11 8 ASAA0772166 1 20071017 A 5320 146481273 WEB BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 AFT CARGO PIT FLOOR SUPPORT WEB BETWEEN B767 & 787 RBL 20 CORRODED. REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 53- 60-15, 51-30-01 & 51-40-02. 2 L 7 2 4F RT A16WE 2007110800076 20071108 00076 NM 2007 11 8 ASAA0772162 1 20071020 A 5347 146A750125 CARGO TRACK BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 AFT CARGO PIT RIGHT TIE DOWN TRACK CORROSION FOUND FROM STA 767 TO 857. CORRODED SECTION FROM SEA 747+12 887 REPLACED W ITH NEW PART IAW B737 700 SRM 53-00-53 FIG 201. 2 L 7 2 4F RT A16WE 2007110800079 20071108 00079 EU 2007 11 8 TRAX200701592 1 20071022 A 1100 PLACARD AEROSP ATR72 ATR72 EU MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 EXTERIOR AND INTERIOR PLACARD ON A/C IS MISSING OR DAMAGED. INSTALLED AS PER AMM 11-00-00. 2 H 7 2 4T RT 2007110800104 20071108 00104 NM 2007 11 8 USAA920071044 1 20071027 A 5320 ATTACH ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, CRACKED INTERCOSTAL ATTACH ANGLE, AFT SIDE OF FLOORBEAM, BS 380, RBL 24.5. REPLACED INT ERCOSTAL ATTACH ANGLE, AFT SIDE OF FLOORBEAM, BS 380, RBL 24.5 IAW B737 SRM 51-70-11. 2 L 7 2 4F RT A16WE 2007110800105 20071108 00105 EU 2007 11 8 07FDEA04703 1 20071026 A 5310 STRUCTURE AIRBUS 310 A310324 3930206 EU CONTAMINATED A FDEA O OTHER F N FLT CONT AFFECTED FALSE WARNING CL CLIMB 1 SO 25 815FD 638 CTR TANK FUEL QUANTITY FLUCTUATES IN FLIGHT FROM 60 LBS TO 1080 LBS. SHOWED 1.0 IN CTR FOR TAKEOFF. STAB TRIM WAS ADJU STED ACCORDINGLY. NOSE WAS VERY LIGHT ON TAKEOFF ROLL AND TOOK EXCESSIVE NOSE DOWN TRIMMING TO GET AIRCRAFT IN TRIM. ONCE IN FLIGHT RECHECKED T/O SETTING AND THEY ARE CORRECT. VERIFIED FUEL QTY IN CENTER TANK. NO FLUCTUATION AND FUEL Q UANTITY READS NORMAL. FOUND WATER TRAPPED IN THS COMPARTMENT MEASURED 14 INCHES DEEP, AFT PRESSURE BULKHEAD. APPROX 60 GALLONS. BLEW OPEN DRAIN AT MAST AND DRAINED ALL WATER FROM COMPARTMENT. ENSURED DRAIN IS OPEN AND COMPARTMENT IS EMP TY OF WATER AMM 51-80-41-6. 2 L 7 2 4F RT A35EU 2007110800107 20071108 00107 WP 2007 11 8 AALA20072003 1 20071021 A 2697 CONNECTOR DOUG DC9 DC982 3022082 WP LT NACELLE INOPERATIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 446AA 49472 DFW INFLIGHT T1306/21OCT - LEFT ENGINE FIRE LOOP ILLUMINATED FOLLOWED BY FIRE INDICATION. SHUT ENGINE DOWN. RETURNED T O DFW AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME 5 MINUTES. FOUND 2 CONNECTORS BAD ON LOWER SUPPORT DETECTOR. R EPLACED NEW CONNECTORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110800109 20071108 00109 NM 2007 11 8 AALA20072008 1 20071021 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 765AN 32879 DFW - EMERGENCY LIGHT AT OVERHEAD RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD RIGH T NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110800110 20071108 00110 NM 2007 11 8 AALA20072021 1 20071023 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 612AA 24488 DFW - EMERGENCY LIGHT AT SEAT ROW 2E INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 2E. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007110800111 20071108 00111 NM 2007 11 8 AALA20072026 1 20071024 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 791AN 30254 ORD - EMERGENCY LIGHT AT SEAT ROW 22C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 22C. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110800112 20071108 00112 EU 2007 11 8 AALA20072031 1 20071025 A 3397 WIRE HARNESS AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70054 461 JFK - EMERGENCY LIGHT AT SEAT ROW 17G INOPERATIVE. REPLACED HARNESS FOR EMERGENCY LIGHT AT SEAT ROW 17G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007110800114 20071108 00114 NM 2007 11 8 AALA20072020 1 20071023 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AA 24488 DFW - EMERGENCY LIGHT AT SEAT ROW 2E MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 2E. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007110800115 20071108 00115 WP 2007 11 8 AALA20072027 1 20071024 A 2560 BATTERY DOUG DC9 DC982 3022082 WP FLASHLIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 561AA 53091 LGA - FORWARD LOWER EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY FOR FORWARD LOWER EMERGENCY FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110800116 20071108 00116 WP 2007 11 8 AALA20072029 1 20071024 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 561AA 53091 LGA - EMERGENCY LIGHT AT SEAT ROW 28D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 28D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110800117 20071108 00117 NM 2007 11 8 AALA20072023 1 20071023 A 3350 PLATE BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AA 24488 DFW - EMERGENCY LIGHT AT SEAT ROW 2E MISSING BACK PLATE. REPLACED BACK PLATE FOR EMERGENCY LIGHT AT SEAT ROW 2E. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007110800118 20071108 00118 2007 11 8 AALA20072024 4 20071024 A 2565 SLIDE DOUG DC9 DC982 3022082 WP GALLEY DOOR FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 MSY - AFT GALLEY SERVICE DOOR SLIDE DISLODGED BY AIRCRAFT CLEANERS. DID NOT DEPLOY. REPLACED AFT GALLEY SERVICE DOOR S LIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110800119 20071108 00119 NM 2007 11 8 AALA20072025 1 20071024 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 ORD - EMERGENCY LIGHT AT SEAT ROW 22C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 22C. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110800121 20071108 00121 NM 2007 11 8 AALA20072037 1 20071025 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 798AN 30797 DFW - SEAT MOUNTED EMERGENCY LIGHTS AT LEFT AND RIGHT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED E MERGENCY LIGHTS AT LEFT AND RIGHT AND FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110800122 20071108 00122 NM 2007 11 8 AALA20072038 1 20071025 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 798AN 30797 DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIGHT NUMBER O NE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110800123 20071108 00123 NM 2007 11 8 AALA20072009 1 20071022 A 3350 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 329AA 22329 JFK - EMERGENCY LIGHTS AT LEFT AND RIGHT OVERWING EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK M01209 FOR EMERGENCY LI GHTS AT LEFT AND RIGHT OVERWING EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007110800124 20071108 00124 WP 2007 11 8 AALA20072028 1 20071024 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 561AA 53091 LGA - EMERGENCY LIGHT AT SEAT ROW 28D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 28D. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110800126 20071108 00126 WP 2007 11 8 AALA20072030 1 20071024 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 561AA 53091 LGA - EMERGENCY LIGHT AT SEAT ROW 28D MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 28D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110800127 20071108 00127 NM 2007 11 8 AALA20072013 1 20071023 A 3350 0201984006 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 958AN 30091 LGA - EMERGENCY LIGHT AT AFT OVERWING EXIT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT AFT OVERWING EXI T. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007110800129 20071108 00129 NM 2007 11 8 AALA20072022 1 20071023 A 3397 WIRE HARNESS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 612AA 24488 DFW - EMERGENCY LIGHT AT SEAT ROW 19D INOPERATIVE. REPLACED HARNESS FOR EMERGENCY LIGHT AT SEAT ROW 19D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007110800130 20071108 00130 WP 2007 11 8 AALA20072032 1 20071025 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 498AA 49736 DFW - EXTERNAL EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR EXTERNAL EMERGENCY LIGHTS. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110800131 20071108 00131 NM 2007 11 8 AALA20072039 1 20071025 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 798AN 30797 DFW - EMERGENCY LIGHT AT SEAT ROW 39G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 39G. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110800132 20071108 00132 NM 2007 11 8 AALA20072004 1 20071021 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 345AN 33084 DFW - EMERGENCY LIGHTS AT RIGHT SEAT ROWS 5H TO 13H INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT SE AT ROWS 5H TO 13H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007110800133 20071108 00133 WP 2007 11 8 AALA20072005 1 20071021 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 402A 49313 LGA - EMERGENCY LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT CABIN. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110800134 20071108 00134 WP 2007 11 8 AALA20072006 1 20071021 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 402A 49313 LGA - EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS CABI N. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110800135 20071108 00135 WP 2007 11 8 AALA20072007 1 20071021 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 402A 49313 LGA - EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS CABI N. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110800136 20071108 00136 WP 2007 11 8 AALA20072015 1 20071023 A 2931 VALVE DOUG DC9 DC982 3022082 WP RT HYD SYSTEM LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 21 420AA 49332 DFW INFLIGHT T417/23OCT - ON SLAT EXTENSION RIGHT HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. LOST RIGHT HYDRAULIC QUANT ITY. MANUALLY EXTENDED GEAR. LANDED DFW WITHOUT INCIDENT. FOUND RESIDUE FROM RIGHT SPOILER SHUTOFF VALVE. REPLACED R IGHT SPOILER SHUTOFF VALVE AND SERVICED HYDRAULIC SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110800137 20071108 00137 NM 2007 11 8 AALA20072012 1 20071022 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 632AA 24590 JFK - EMERGENCY LIGHT AT LEFT MID CABIN FLIGHT ATTENDANT JUMP SEAT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LE FT MID CABIN FLIGHT ATTENDANT JUMP SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007110800139 20071108 00139 NM 2007 11 8 AALA20072018 1 20071023 A 3350 BPS73 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 319AA 22320 JFK - EMERGENCY LIGHTS AT LEFT AND RIGHT NUMBER ONE DOORS INOPERATIVE. REPLACED BATTERY PACK AT LEFT NUMBER ONE DOOR FO R EMERGENCY LIGHTS AT LEFT AND RIGHT NUMBER ONE DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007110800140 20071108 00140 NM 2007 11 8 AALA20072010 1 20071022 A 3350 LAMP BOEING 767 767223 1385123 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 329AA 22329 JFK - FORWARD EXTERIOR EMERGENCY LIGHT AT AFT CARGO DOOR INOPERATIVE. REPLACED LAMP FOR FORWARD EXTERIOR EMERGENCY LIGH T AT AFT CARGO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007110800141 20071108 00141 EU 2007 11 8 AALA20072011 1 20071022 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80052 460 JFK - SEAT MOUNTED EMERGENCY LIGHTS AT LEFT COACH INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT LEFT COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007110800142 20071108 00142 NM 2007 11 8 AALA20072019 1 20071023 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AA 24488 DFW - EMERGENCY LIGHT AT FIRST CLASS GALLEY FLOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT FIRST CLASS GALLEY FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007110800143 20071108 00143 WP 2007 11 8 AALA20072033 1 20071025 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 498AA 49736 DFW - EXTERNAL EMERGENCY LIGHT AT RIGHT OVERWING INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT RIGHT OVERW ING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110800145 20071108 00145 WP 2007 11 8 AALA20072034 1 20071025 A 3350 SCREW DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 DFW - EXTERNAL EMERGENCY EXIT LIGHT AT RIGHT HAS TWO SCREWS MISSING. REPLACED SCREWS FOR EXTERNAL EMERGENCY EXIT LIGHT AT RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110800147 20071108 00147 WP 2007 11 8 AALA20072036 1 20071025 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT MOUNT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 586AA 53249 LGA - FORWARD LOWER EMERGENCY FLASHLIGHT HAS BROKEN STRAP. REPLACED STRAP FOR FORWARD LOWER EMERGENCY FLASHLIGHT. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110800148 20071108 00148 NM 2007 11 8 AALA20072014 1 20071023 A 3350 CM767 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 349AN 33088 JFK - EMERGENCY LIGHT AT SEAT 24B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24B. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A1NM 2007110800149 20071108 00149 NM 2007 11 8 AALA20072016 1 20071023 A 3397 1721651 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 621AM 24579 SFO - EMERGENCY LIGHTS AT SEAT ROW 34DEF INOPERATIVE. REPLACED CONNECTOR AND SOCKET 1703663 FOR EMERGENCY LIGHTS AT SEA T ROW 34DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007110800150 20071108 00150 NM 2007 11 8 AALA20072017 1 20071023 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 766AN 32880 DFW - EMERGENCY LIGHT AT SEAT ROW 12F MISSING LENS INOPERATIVE. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 12F. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110800151 20071108 00151 WP 2007 11 8 AALA20072035 1 20071025 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 234AA 49181 LGA - EMERGENCY LIGHT AT OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERWING. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110800179 20071108 00179 NM 2007 11 8 MWEA070268 1 20071030 A 5313 5919707147 LONGERON BOEING 717 717200 1383700 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 912ME 55175 LONGERON 30, BETWEEN STATION 920 AND 927 HAS THREE AREAS OF EXFOLIATION CORROSION. REMOVED AREAS OF CORROSION AND INSTA LLED NESTED U-CHANNEL. 2 L 7 2 4F TR A6WE 2007110800188 20071108 00188 NM 2007 11 8 UPS07651060 1 20071027 A 5751 FRAME BOEING 767 76734AF 1385212 NM AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 323UP 27749 INSPECTION TYPE:N/A LEFT WING I/B AILERON I/B HINGE SUPPORT FRAME CRACKED BETWEEN UPPER TWO FASTENER HOLES AND OUT TO TH E LOWER FASTENER EDGE. REPAIRED LEFT WING INBOARD AILERON INBOARD HINGE SUPPORT FRAME PER EO B767-5740-27949-A. 2 L 7 2 4F RT A1NM 2007110800194 20071108 00194 NM 2007 11 8 07FDEA04705 1 20071031 A 5311 FRAME BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 UPPER LOBE STATION 700 FRAME, BELOW STRINGER 1L IS CORRODED. REMOVED CORR ON BS 700 FRAME IAW SRM 53-00-07. ORIGINAL MATERIAL THICKNESS WAS .063". MATERIAL REMOVED WAS .018". MATERIAL REMAINING WAS .046", OUT OF LIMITS PER SRM 53-00-07 . FABRICATED REPAIR SPLICE PER MAE TRAV NR T7/686708. TREATED AND PRIMED IAW SRM 51-20-01. INSTALLED FRAME SPLICE REP AIR IAW SRM 53-00-07, FIGURE 201 AND FIGURE 203, REPAIR NR 3. MAE ENG APPROVED THE USE OF THE ABOVE NOTED SRM PER MAE E AR NR 67597370080. REQUIRED INITIAL REPEAT INSP PRIOR TO 10,000 FC AFTER REPAIR IS INSTALLED. AFTER INITIAL INSP, REPE AT INSP ARE REQ. EVERY 12,000 FC INTERVALS PER SRM 53-00-07, FIG.203, PAGE 207, ITEM D. 2 L 7 2 4F RT A2NM 2007110800195 20071108 00195 EU 2007 11 8 F3LA200700288 1 20071019 A 5310 DUMMY RAIL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM Y503.2 CORRODED ON UPPER SURFACE BETWEEN FRAMES 14 AND 16. DETERMINED CORROSION ON DUMMY RAIL Y503.2 TO BE OUT OF LIMITS IAW A319 SRM 53-11-14, FIG 106. REMOVED AND INSTALLED DUMMY RAIL Y5 03.2 IAW 51-42-11, AND 51-44-11. 2 L 7 2 4F RT A28NM 2007110800224 20071108 00224 2007 11 8 UPS07M51066 4 20071030 A 2565 SLIDE DOUG MD11 MD11F 3023600 NM EMERGENCY EXIT DEPLOYED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE:N/A ESCAPE SLIDE DEPLOYED ON LEFT CREW ENTRY. REMOVED AND REPLACED ESCAPE SLIDE PER AMM 26-61-15-4. 2 L 7 3 4F RT A22WE 2007110800225 20071108 00225 NM 2007 11 8 SB07094 1 20071030 A 5610 5893543129 WINDSHIELD BOEING 737 7373B7 1384580 NM COCKPIT CRACKED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 517AU 11485 11485 23703 BNA FLT 1552 - DURING CRUISE, CREW REPORTED THE CAPTAIN'S L1 WINDSHIELD BEGAN TO ARC AND THEN SHATTERED. CREW ACCOMPLIS HED QRH PROCEDURES. PRESSURIZATION REMAINED NORMAL. OUTER PANE WAS CONFIRMED SHATTERED, WHEREAS, INNER PANE WAS NOT AF FECTED. FLIGHT LANDED AT BDL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S L1 WINDSHIELD PE R MM 56-11-11. ALSO, REPLACED L1 WINDOW HEAT CONTROLLER. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007110800229 20071108 00229 EU 2007 11 8 USAA920071016 1 20071017 A 5347 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274AY 342 BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 4842 / FR 58 - BS 5478 / FR 70, +Y450. REPAIRED CABIN SEAT TRACK, BS 4842 / FR 58 - BS 5478 / FR 70, +Y450 IAW A330 SRM 53-31-15, 53-00-15 AND 51-42-00. AIRCRAFT MANUFACTUR ER AND MODEL WAS CHANGED FROM BOEING 767201ER TO AIRBUS A330323. 2 L 7 2 4F RT A46NM 2007110800237 20071108 00237 NM 2007 11 8 ASAA0772170 1 20071018 A 5320 146A7502 CHANNEL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 AFT CARGO PIT RT SIDEWALL ZEE CHANNEL BADLY CORRODED FROM STD 727+4 TO 767. AFT CARGO PIT RT SIDE PLATE ZEE CHANNEL AT BS 727+4 TO BS 767 WAS REPAIRED IAW B737 700 SRM 53 00 53. 2 L 7 2 4F RT A16WE 2007110800239 20071108 00239 NM 2007 11 8 ASAA0772172 1 20071019 A 5320 146A94018 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 AFT CARGO CORROSION ON FLOOR SUPPORT TEE. REPLACED WITH NEW PART IAW B737 700 SRM 53-00-53. 2 L 7 2 4F RT A16WE 2007110800240 20071108 00240 NM 2007 11 8 ASAA0772173 1 20071018 A 5321 453A261012 FLOOR PANEL BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 AFT CARGO PIT CORROSION AROUND EDGES ON FLOOR PANEL NR 4 BETWEEN BS 887 AND BS 947.5. REPLACED WITH MADE REPAIR PART IA W B737 700 SRM 53-70-53 FIG 2 & 51-40-05. 2 L 7 2 4F RT A16WE 2007110800243 20071108 00243 NM 2007 11 8 ASAA0772176 1 20071018 A 5321 A53A261018 FLOOR PANEL BOEING 737 737790 13844CN NM CARGO BAY DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 AFT CARGO PIT FLOOR PANEL NR 3 WITH TEMPORARY REPAIRS AND MISSING EDGE. REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 53-60-53 FIG 2 & 51-40-05. 2 L 7 2 4F RT A16WE 2007110800244 20071108 00244 NM 2007 11 8 ASAA0772177 1 20071019 A 5315 147A55067 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 AFT CABIN BS 986.5 FLOORBEAM UPPER CAP CORRODED AT LBL 24. REPLACED UPPER CAP IAW ERD 7360 & EA5310 02739. 2 L 7 2 4F RT A16WE 2007110800256 20071108 00256 SO 2007 11 8 LR7A07102 1 20071001 A 5311 RIB LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2661 4763 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5311 FOUND COCKPIT RIB CRACKED AT FS 132 WL 207 TO 215 LBL 61. REPAIR ACCOMPL ISHED IAW SMP583 CHAPTER 51-60 & 51-70 USING 2024T3 .050". 2 H 7 4 4T A1SO 2007110800267 20071108 00267 SO 2007 11 8 LR7A07113 1 20071001 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2661 4763 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5321 FOUND BELLY EXTERIOR SKIN CRACKED AT FS 477 WL 128 BL 3R. REPAIR ACCOMPL ISHED IAW SMP583 FIG 51-140-12 CHAPTER 51-70 USING 2024T3 .080". 2 H 7 4 4T A1SO 2007110800268 20071108 00268 SO 2007 11 8 LR7A07114 1 20071001 A 5320 339482 MANIFOLD LKHEED 382 382G 526414U SO LT MLG WW CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2661 4763 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5323 FOUND LT MWW MANIFOLD CRACKED AT FS 507, 542 & 567 WL 146 BL 62. REPAIR ACCOMPLISHED BY REPLACING IAW SMP583 CHAPTER 51-60 & 51-70. 2 H 7 4 4T A1SO 2007110800269 20071108 00269 SO 2007 11 8 LR7A07115 1 20071001 A 5320 ATTACH ANGLE LKHEED 382 382G 526414U SO FS477WL284RBL32 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2661 4763 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5316 FOUND RT AERODYNAMIC FAIRING ATTACH ANGLE CRACKED, DURING SP-126 INSPECTI ON AT FS 417 WL 284 RBL 32-60. REPAIR ACCOMPLISHED BY REPLACING ATTACH ANGLE IAW AD92-10-14, SB 382-53-27 R1, SMP583 CH APTER 51-60 & 51-70. 2 H 7 4 4T A1SO 2007110800288 20071108 00288 NM 2007 11 8 SWAA075447 1 20071030 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 214WN 32486 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007110800295 20071108 00295 NM 2007 11 8 SWAA075450 1 20071030 A 5320 6545819 WEB BOEING 737 7373H4 1384600 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED HC2 CHECK, FOUND NOSE W/W UPPER RIGHT CEILING PANEL WEB CRACKED. REPAIRED CEILING PANEL PER ACO. 2 L 7 2 4F RT A16WE 2007110800305 20071108 00305 NM 2007 11 8 SWAA075418 1 20071030 A 5522 65C25745 SKIN BOEING 737 7377H4 1384404 NM LT ELEVATOR DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 475WN 32474 DURING SCHEDULED HC1 CHECK, FOUND LT ELEVATOR DELAMINATED AT UPPER SURFACE STATION 265.45. REPAIRED ELEVATOR PER SRM. 2 L 7 2 4F RT A16WE 2007110800310 20071108 00310 NM 2007 11 8 SWAA075423 1 20071031 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 17R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007110800315 20071108 00315 NM 2007 11 8 SWAA075430 1 20071031 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007110900014 20071109 00014 NM 2007 11 9 USAA920071062 1 20071023 A 5340 693535214 STRINGER CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED STRINGER CLIP, BS 400, S10L. REPLACED CRACKED STRINGER CLIP, BS 400, S10L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007110900048 20071109 00048 NM 2007 11 9 2007UALA04491 1 20071031 A 5210 DOOR FRAME BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L1 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 181UA 25278 NR 1 LEFT MED UPPER FRAME CRACKED AT CENTER UPPER GATE HINGE ATTACH HOLE. REPAIRED CRACK PER IAW FRR UAL-744-0317. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110900059 20071109 00059 NM 2007 11 9 2007UALA04506 1 20071031 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 520 S24-25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 FWD PIT STA 520 MAIN FRAME BETWEEN STR 24L AND 25L FRAME HAS 2 DENTS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110900063 20071109 00063 NM 2007 11 9 2007UALA04508 1 20071031 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE 3R DOOR SLIDE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 585UA 26709 SLIDE LIGHT AT 3R NOT LIT UP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110900064 20071109 00064 NM 2007 11 9 2007UALA04510 1 20071031 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS LOOSE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 654UA 25392 END CAPS MISSING FROM FRONT OF ESCAPE PATH LIGHTING STRIPS IN FIRST CLASS. ALSO CONNECTIONS LOOSE IN SAME AREA. RECON NECTED, OPS CHECK AND INSTALLED END CAPS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110900066 20071109 00066 NM 2007 11 9 2007UALA04512 1 20071101 A 5330 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 795UA 26927 DENT ON STA 277 ABOVE STR 28 LT. NDT, NO CRACKS OUT OF LIMITS. ACCOMPLISHED CAT B. REPAIR . REQ FUTURE REINSPECTION. N EW CF WILL BE CREATED. PERMANENT REPAIR WITHIN 16,000 FC OR NEXT HMV. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007110900068 20071109 00068 NM 2007 11 9 2007UALA04509 1 20071031 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1480 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 AFT PIT STA 1480 MAIN FRAME AT STR 26L FRAME HAS 2 DENTS. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGE AND INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110900069 20071109 00069 NE 2007 11 9 2007UALA04514 2 20071101 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OIL CONSUMPTION A UALA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 29 551UA 25399 726522 OIL CONSUMPTION TRENDING UP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110900070 20071109 00070 NM 2007 11 9 2007UALA04516 1 20071101 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EEL 5A AFT INOPERATIVE. RELAMPED LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110900072 20071109 00072 NM 2007 11 9 2007UALA04517 1 20071101 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EEL 61 HJ INOPERATIVE. SECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110900075 20071109 00075 EU 2007 11 9 F3LA200700294 1 20071019 A 5320 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM Y254 CORRODED ON UPPER SURFACE BETWEEN FRAMES 16 AND 18. FABRICATED A ND INSTALLED FLOOR SUPPORT REPAIR PARTS IAW SRM 53-11-14, 51-47-00, 51-23-00, 51-75-12, 51-44-11, EAR 910-4551, AND EA A 9-53R-12224. 2 L 7 2 4F RT A28NM 2007110900077 20071109 00077 SO 2007 11 9 SWIA200718819 1 20071029 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 223SW 120291 FLT 5491 - WHITE FLOOR EMERGENCY LIGHT IS INOP. REPLACED LIGHT ASSEMBLY ON FLOOR TRACK. 2 L 7 2 4T RT A31SO 2007110900079 20071109 00079 EA 2007 11 9 SWIA200718825 1 20071029 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 452SW 7716 FLT 3968 - LEFT WINDOW CAUTION MESSAGE ILLUMINATED. REPLACED LEFT COCKPIT WINDOW IAW CRJ AMM 56-11-01, P/N NP139322-11 S/N OFF 06347H9678. 2 L 7 2 4F RT A21EA 2007110900080 20071109 00080 EU 2007 11 9 F3LA200700289 1 20071017 A 5315 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT FR67R CORRODED IN NUTPLATE HOLES. REMOVED AND REPLACED FLOORBEAM I AW SRM 51-42-11, PARA 5, AND 71-72-11. 2 L 7 2 4F RT A28NM 2007110900081 20071109 00081 EU 2007 11 9 F3LA200700295 1 20071017 A 5320 WEB AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION AT FLOOR WEB NUTPLATE IN FWD CARGO COMPARTMENT AT FR 28, 6" INBD OF C1 DOOR CUTOUT. REMOVED AND REPLACED TRANSITION STRIP IAW SRM 51-42-11, 51-72-11 AND 51-21-11. 2 L 7 2 4F RT A28NM 2007110900083 20071109 00083 2007 11 9 F3LA200700296 4 20071017 A 2565 WEB AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION AT FWD CARGO COMPARTMENT FLOOR WEB NUTPLATES, RT SIDE WHERE TRANSITION PANEL AND FLOOR MEET, BETWEEN FR 28 AND FR 29. REMOVED AND REPLACED CORRODED TRANSITION STRIP IAW SRM 51-42-11 AND 51- 44-11. 2 L 7 2 4F RT A28NM 2007110900084 20071109 00084 EU 2007 11 9 F3LA200700297 1 20071018 A 5210 BLANKING PLATE AIRBUS A319 A319112 3930323 EU R1 GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON R1 DOOR GIRT BAR FITTING AFT BLANKING PLATE. REPLACED R1 DOOR AFT GIRT BAR FITTING BLANKING PLATE IAW AMM 53-11-31-PB401. 2 L 7 2 4F RT A28NM 2007110900085 20071109 00085 NM 2007 11 9 SWAA075434 1 20071031 A 5322 6546529 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, RBL 7. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007110900087 20071109 00087 2007 11 9 F3LA200700298 4 20071018 A 2565 BLANKING PLATE AIRBUS A319 A319112 3930323 EU L2 GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON L2 DOOR GIRT BAR FITTING BLANKING PLATE. REMOVED AND REPLACED L2 D OOR BLANKING PLATE IAW AMM 53-11-31-PB401. 2 L 7 2 4F RT A28NM 2007110900089 20071109 00089 2007 11 9 F3LA200700299 4 20071018 A 2565 BLANKING PLATE AIRBUS A319 A319112 3930323 EU L1 GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON L1 DOOR GIRT BAR FITTING AFT BLANKING PLATE. REMOVED AND REPLACED L1 DOOR AFT GIRT BAR BLANKING PLATE IAW AMM 53-11-31-PB401. 2 L 7 2 4F RT A28NM 2007110900090 20071109 00090 NM 2007 11 9 SWAA075435 1 20071030 A 5330 6545774 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007110900091 20071109 00091 EU 2007 11 9 TRBA2007090 1 20071101 A 3350 3011210 LIGHT AEROSP ATR72 ATR72212 8680945 EU PAX DOOR FAILED A TRBA O OTHER L NO TEST NR NOT REPORTED 1 SO 29 260AE 263 PAX DOOR STAIR EMERGENCY FLOOD LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLOOD LIGHT ASSEMBLY IAW JIC NR 33-51- 24. PERFORMED OP CK. 2 H 7 2 4T RT A53EU 2007110900092 20071109 00092 NM 2007 11 9 SWAA075436 1 20071030 A 5330 6545774 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739E, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007110900093 20071109 00093 NM 2007 11 9 SWAA075437 1 20071031 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT UPPER CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007110900094 20071109 00094 NM 2007 11 9 SWAA075438 1 20071031 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 19R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900095 20071109 00095 GL 2007 11 9 ARWA20071003 2 20071026 A 7200 CF650C2 ENGINE DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C 30018 GL NR 1 MAKING METAL A ARWA E ENGINE SHUTDOWN K E FLUID LOSS VIBRATION/BUFFET CL CLIMB 1 SO 19 478CT 86067 3137 47819 455871 AFTER DEPARTURE FROM SVVA, FELT VIBRATION IN COCKPIT, THEN SMOKE IN COCKPIT, NR 1 ENGINE OIL QUANTITY TO ZERO AND OIL PR ESSURE BEGAN FLUCTUATING; SHUTDOWN ENGINE NR 1 AT 1758Z. TROUBLESHOOT NR 1 ENGINE PER TAFI 79-00-00; FOUND METAL CONTAM INATION ON SCAVAGE PUMP CHIP DETECTOR. NR 1 ENGINE WAS REMOVED AND REPLACED AS PER WORKCARD NR 141R7101M. OPERATIONAL CHECK AND RUN UP NORMAL AS PER DC-10 A/M/M 72-06-00. 2 L 7 3 4F 4 F RT A22WE A23EA 2007110900097 20071109 00097 NM 2007 11 9 07FDEA04692 1 20071026 A 5311 53FX1350 FRAME SPLICE BOEING 727 727233 138408A NM BS 580 S21-22L CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 265FE 21671 FWD LOWER CARGO SPLICE FRAME AT STA 580 BETWEEN STR 21L AND 22L HAS A CRACK. REMOVED 53FX1350 SPLICE FRAME, FABRICATED AND INSTALLED NEW SPLICE FRAME IAW 727 SRM 51-10-01 AND FEDEX DRG 53FX1370. 2 L 7 3 4F RT A3WE 2007110900098 20071109 00098 NM 2007 11 9 SWAA075440 1 20071030 A 5311 6546548 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 27R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007110900101 20071109 00101 EU 2007 11 9 07FDEA04712 1 20071102 A 5310 A53810876 BEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 729FD 657 FOUND CRACK (ABOUT 12MM) AT GANTRY 5 LT, C50B REPAIR PERFORMED IAW DRAWING R538-10737-204, APPROVED BY EA 6-5315-114912 AND RAS/054790/009/2007 ISS A . 2 L 7 2 4F RT A35EU 2007110900102 20071109 00102 EU 2007 11 9 07FDEA04713 1 20071102 A 5320 R53810537204 STRAP AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 729FD 657 DURING REPAIR IAW DRAWING R538-10537 (DR280) FOUR WRONG SPOTFACING WERE PERFORMED ON REPAIR STRAP. REPAIR PERFORMED B Y INSTALLING TAPERED WASHER AND SPACER R538-10621 IAW EA 6-5315-114912 AND RAS/054790/009/2007 ISS A. 2 L 7 2 4F RT A35EU 2007112800026 20071128 00026 NM 2007 11 28 SWAA075734 1 20071117 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM L1 DOOR INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED L1 DOOR EMERGENCY EXIT LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007110900105 20071109 00105 2007 11 9 SWAA075444 4 20071031 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 725SW 27857 L2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007110900106 20071109 00106 WP 2007 11 9 07FDEA04716 1 20071102 A 5310 ABA72006 DOOR FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 MAIN CABIN R1 DOOR FWD JAMB DURING PERFORM OAN J/C SP10240272-7001-2J FOUND CRACK ON FRAME. REPAIRED FRAME IAW SRM 53-0 0-01 VOL I FIG 8. 2 L 7 3 4F RT A22WE 2007110900107 20071109 00107 NM 2007 11 9 SWAA075445 1 20071030 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 747SA 29799 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007110900108 20071109 00108 2007 11 9 SWAA075446 4 20071031 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 780SW 27885 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007110900109 20071109 00109 WP 2007 11 9 ARWA20071101 1 20071101 A 3234 HANDLE DOUG DC10 DC1030F 3023504 WP MLG STUCK A ARWA J A DUMP FUEL UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 478CT 47819 AFTER TAKEOFF GEAR HANDLE WILL NOT GO UP. ACCOMPLISHED EXPANDED CHECKLIST, NOT HELP. RETURN TO KMIA. ACCOMPLISHED FUE L DUMP PROCEDURE TO BRING A/C TO MAX LANDING WEIGHT. REMOVED AND REPLACED RUPTURED BOGIE TRIM LINE ON LT MAIN LANDING GEAR. BLEAD SYSTEM AND OPERATIONAL CHECK IN ACCORDANCE WITH M/M 33-37-01. OPERATIONS NORMAL. 2 L 7 3 4F RT A22WE 2007110900113 20071109 00113 NM 2007 11 9 UPS07451082 1 20071023 A 3397 CONNECTOR BOEING 747 747123 1384873 NM EMERGENCY LIGHTS DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 EMERGENCY LIGHTS ABOVE R1 DOOR DO NOT WORK. FOUND TERMINAL END ON EXIT SIGN BROKEN. REPLACED PER BOEING SSWD 20-30-11. FUSE BLOWN ON POWER PACK MODULE. REPLACED MODULE X328 MM 33-51-04/2. ALSO, FOUND WIRES AT PLUG DC228 BROKEN. REPLAC ED PLUG PER BOEING SSWD 20-61-11. EMERGENCY LIGHTS OPS NORMAL IAW MM 31-51-04. 2 L 7 4 4F A20WE 2007110900115 20071109 00115 WP 2007 11 9 UPS07851079 1 20071013 A 5310 WINDOW FRAME DOUG DC8 DC873F 302199F WP FS 117 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 C2 COCKPIT LT CENTER WINDSHIELD "Z" FRAME HAS HEAVY CORROSION. REMOVED, DRILLED UP, AND INSTALLED REPLACEMENT "Z" FRAME ON COCKPIT LT CENTER WINDSHIELD IAW SRM 51-21-1, AND SRM 51-03-02 FIG 005. 2 L 7 4 4F RT 4A25 2007110900116 20071109 00116 2007 11 9 SB07096 4 20071031 A 2565 D37022101 BOTTLE AIRCRUISERS BOEING 737 7373B7 1384580 NM EVAC SLIDE LOW PRESSURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 532AU 000742 24479 BWI - MAINTENANCE REPORTED THE FORWARD LEFT ENTRY DOOR EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE LOW. MAINTENANCE REMOVED AND REPLACED THE FORWARD LEFT ENTRY DOOR EMERGENCY ESCAPE SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007110900117 20071109 00117 NM 2007 11 9 UPS07M51083 1 20071101 A 8097 DC6028M15SX CONNECTOR DOUG MD11 MD11F 3023600 NM NR 2 START VALVE SHORTED A IPXA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SO 01 281UP 48538 NR 2 ENGINE START VALVE LIGHT ILLUMINATED IN FLIGHT. DURING T/S, FOUND PIN "D" ON SOCKET R5-8235 SHORTED. REQUESTED P/ N;DC60-28M15SX AND DC63-28K15PX. REPAIRED AT CONNECTOR P1-8235, REF STANDARD WIRING PRACTICES MANUAL CHAPTER 20. NR 2 ENG START VALVE AND LIGHT OPS CHECKED NORMAL ON IDLE ENG ENG RUN IAW 71-02-01. 2 L 7 3 4F RT A22WE 2007110900119 20071109 00119 2007 11 9 UPS07M51084 4 20071101 A 2565 SLIDE DOUG MD11 MD11F 3023600 NM R1 DOOR INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 282UP 48452 R1 DOOR SLIDE INOP M361751 ISSUED. REMOVED AND REPLACED RT DOOR SLIDE ASSY IAW MD11 MM 25-61-01-4. OPS CHECK OK. THIS CLEARS M361751. 2 L 7 3 4F RT A22WE 2007110900120 20071109 00120 WP 2007 11 9 UPS07851077 1 20071028 A 5523 TAB DOUG DC8 DC873F 302199F WP ELEVATOR PUNCTURED A IPXA K NONE O OTHER NR NOT REPORTED 1 SO 01 812UP 46112 INSPECTION TYPE:N/A LEFT ELEVATOR INBOARD CONTROL TAB HAS A .3125 INCH PUNCTURE ON BOTTOM OF TAB. TRANS TO NRC 107944. CHECKED LEFT I/B ELEVATOR AREA ON AIRCRAFT SIDE FOR HARDWARE/ATTACH FITTING. NO DISCREPANCY FOUND. OK TO INSTALL ELEV ATOR CONTROL TAB. INSTALLED SERVICEABLE LEFT ELEVATOR CONTROL TAB. REF AMM 27-30-02-2. LP 868935. 2 L 7 4 4F RT 4A25 2007110900121 20071109 00121 NM 2007 11 9 NWAA073626309 1 20071101 A 3397 WIRE BOEING 747 747451 1384940 NM EMERGENCY LIGHTS DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 DURING OVERNIGHT CHECK EMERGENCY FLOOR LIGHTING AT ROWS 21 THRU 31 LEFT WERE INOP. MAINTENANCE REMOVED AND REPLACED L-2 DOOR POWER SUPPLY, FUSE AND REPAIRED WIRE. OPERATIONALLY CHECKED GOOD. AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007110900122 20071109 00122 EU 2007 11 9 TRBA2007091 1 20071102 A 3350 7012210 LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS INOPERATIVE A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 417AT 417 PAX DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPAIRED LAMP IAW JIC NR 33-50-00. OP CK OK. 2 H 7 2 4T RT A53EU 2007110900123 20071109 00123 NM 2007 11 9 AALA20072076 1 20071030 A 3397 CONNECTOR BOEING 767 767223 1385123 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 325AA 22326 ORD - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 38H INOPERATIVE. RECONNECTED CONNECTOR FOR SEAT MOUNTED EMERGENCY LIGHT AT S EAT 38H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007110900126 20071109 00126 EU 2007 11 9 AALA20072100 1 20071031 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14068 511 JFK - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007110900127 20071109 00127 EU 2007 11 9 AALA20072104 1 20071031 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14068 511 JFK - SEAT MOUNTED EMERGENCY LIGHTS AT LEFT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT A FT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007110900128 20071109 00128 EU 2007 11 9 AALA20072102 1 20071031 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14068 511 JFK - EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007110800096 20071108 00096 EU 2007 11 8 USAA920071034 1 20071018 A 5321 D5361087600100 FLOORBOARD AIRBUS 320 A320232 3930326 EU CABIN CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - CORROSION ON CABIN FLOORBOARD 222FF, BS 709 / FR 16 - BS 80/ / FR 20. REPLACED CABIN F LOORBOARD 222FF, BS 709 / FR 16 - BS 80/ FR 20 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007110800099 20071108 00099 EU 2007 11 8 USAA920071036 1 20071027 A 5554 D5537131800000 HINGE FITTING AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - RUDDER HINGE FITTING NR 2 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STA 1926 / RIB 4. RE PLACED RUDDER HINGE FITTING NR 2, VERTICAL STABILIZER STA 1926 / RIB 4 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007110800106 20071108 00106 NM 2007 11 8 USAA920071045 1 20071016 A 5315 STRAP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, CRACKED FLOORBEAM STABILIZER STRAP, BS 328, BL 0. REPAIRED FLOORBEAM STABILIZER STRAP, BS 328, BL 0 IAW B737 SRM 53-10-51. 2 L 7 2 4F RT A16WE 2007110800138 20071108 00138 NM 2007 11 8 USAA920071051 1 20071015 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, CRACKED FLOORBEAM INNER CHORD, BS 639. REPAIRED FLOORBEAM INNER CHORD, BS 639 IAW EA 98 917. 2 L 7 2 4F RT A16WE 2007110800153 20071108 00153 NM 2007 11 8 ASAA0752167 1 20071029 A 2161 233A3101 CONTROLLER BOEING 737 737890 1384527 NM COCKPIT INTERMITTENT A ASAA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 02 557AS 35176 ZONE TEMP CONTROL CABIN LIGHT ILLUMINATED ON RECALL CHECK. PREVIOUS FLIGHT SHOWS NR 2 CONTROLLER WITH FLT DECK TRIM VAL VE FAULT. VERIFY TEST NR 2 CONTROLLER GOOD. RESET, FAULT DID NOT REOCCUR. 2 L 7 2 4F RT A16WE 2007110800158 20071108 00158 SO 2007 11 8 C2XA07TY063 1 20071030 A 3397 M3902932248 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN DEFECTIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12564 145618 TYS - MAIN DOOR EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED FEMALE SPLICE CONNECTOR SP7376 IAW EMB 145 WM 20-50-02. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007110800171 20071108 00171 NM 2007 11 8 HNAA0700256 1 20071030 A 3320 BA080061 BALLAST DHAV DHC8 DHC8102 2809003 NM CABIN DEFECTIVE A HNAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 826EX 30382 30382 389 THE FLIGHT ATTENDANT REPORTS ELECTRICAL BURNING SMELL IN CABIN. AIRCRAFT RETURNED TO GATE AND THE LIGHTS WERE DEACTIVAT ED. A HIDDEN DAMAGE INSPECTION WAS PERFORMED AND REMOVED BULB FROM THE SIDE WALL LIGHT AT ROW 7AC. THE BALLAST AND BUL B HOLDER WERE REPLACED. 2 H 7 2 4T RT A13NM 2007110800172 20071108 00172 NM 2007 11 8 HNAA0700219 1 20070704 A 5347 85330217007 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 940 156 CARGO FLOOR SEAT TRACK RAIL TO BE CLEANED AND PRIMED. LEFT I/B AFT SEAT RAIL REPLACED AND INSTALLED WITH SOILD RIVETS I AW DRAWING AND SRM 51-40-00. 2 H 7 2 4T RT A13NM 2007110800180 20071108 00180 WP 2007 11 8 NWAA073599873 1 20071029 A 2150 DUCT DOUG DC9 DC951 3022051 WP ACM LOOSE A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 782NC 48107 AS THE AIRCRAFT CLIMBED OUT WITH BOTH PACKS CONTROLS SET TO "COLD", THE FO NOTICED THAT THE RIGHT PACK WAS INDICATING 94 DEGREES AND THE RIGHT VALVE SHOWED FULL HOT. THE CREW SELECTED MANUAL PACK CONTROL AND WENT TO FULL COLD. THE LEAD FL IGHT ATTENDANT NOTIFIED THE COCKPIT THAT THERE WAS VISIBLE SMOKE IN THE CABIN AND THE AFT LAVATORIES SMOKE DETECTORS WER E SOUNDING. FLIGHT CREW PERFORMED EMERGENCY COM PROCEDURES AND RETURNED TO A NORMAL SAFE LANDING BACK AT MEM. MAINTENA NCE REPLACED BOTH WATER SEPARATORS, INSPECTED ALL APPLICABLE DUCTS AND VALVES, AND EACH ENGINE AND APU INTAKES FOR EVIDE NCE OF OIL LEAKS OR FOD INGESTION. NO SOURCE OF SMOKE FOUND AND ACM DUCT WAS ONLY ONE FOUND TO BE LOOSE. OPERATIONAL C 2 L 7 2 4F RT A6WE 2007110800182 20071108 00182 EU 2007 11 8 NWAA073603353 1 20071030 A 2120 UNKNOWN AIRBUS A330 A330223 3940031 EU CABIN ODOR A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 853NW 0618 STRONG ODOR OF BURNING PLASTIC FILLED THE CABIN, AND DISSIPATED SLIGHTLY ON CLIMB-OUT. ODOR DISSIPATED WHEN HOT AIR 1 W AS TURNED OFF. FLIGHT CONTINUED AND LANDING WAS UNEVENTFUL. INSPECTED AND FOUND NO DEFECTS, OPERATED PACKS WITH BOTH T HE APU AND ENGINE NR 1 BLEED AND NO SMELL FOUND. 2 L 7 2 4F RT A46NM 2007110800184 20071108 00184 NM 2007 11 8 NWAA073616717 1 20071029 A 3097 TERMINAL BLOCK BOEING 747 747251F 1384898 NM WINDOW HEAT SMOKE A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 617US 21121 DURING FLIGHT, SMOKE WAS NOTED PILOTS L-1 WINDOW LOWER LEFT TERMINAL BLOCK WAS SMOKING AND APPEARS MELTED. POWER TO L-1 WINDOW WAS TURNED OFF AND SMOKE AND SMELL DISSIPATED. FLIGHT CONTINUED ON AND LANDING WAS UNEVENTFUL. MAINTENANCE REM OVED AND REPLACED NR 1 WINDSHIELD. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F A20WE 2007110800185 20071108 00185 NM 2007 11 8 QXEA200701632 1 20071031 A 3246 83220001057 WHEEL DHAV DHC8 DHC8202 2809007 NM NLG VIBRATES A QXEA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 09 358PH 9790 125 506 PDX - ON FLIGHT 2126, VIBRATION WAS FELT FROM NOSEWHEEL AFTER TAKEOFF AND ALSO DURING LANDING (OF LESSER MAGNITUDE). PI LOT RETURNED AIRCRAFT TO FIELD. MAINTENANCE REMOVED AND REPLACED NLG TIRES NR 1 AND NR 2. OPERATION CHECKS GOOD. AIRC RAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007110800187 20071108 00187 NM 2007 11 8 07FDEA04694 1 20071027 A 5320 69181946 SUPPORT BOEING 727 727247 138408F NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 TWO .250 CRACKS FOUND IN NOSE LANDING GEAR DOWN LOCK ACTUATOR SUPPORT ASSY. DURING SCHEDULED K CHECK INSPECTION. DAMAG E PART REPLACED. 2 L 7 3 4F A3WE 2007110800189 20071108 00189 WP 2007 11 8 UPS07851061 1 20071011 A 5522 SKIN DOUG DC8 DC873F 302199F WP RT ELEVATOR CANNING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 RT ELEVATOR MIDDLE LWR SKIN HAS OIL CANNING. FABRICATED AND INSTALLED REPAIR DOUBLER ON RT ELEVATOR STA XE 103.2 IAW SRM 55-02-01 FIG 1. 2 L 7 4 4F RT 4A25 2007110800223 20071108 00223 WP 2007 11 8 UPS07851076 1 20071011 A 5522 SKIN DOUG DC8 DC873F 302199F WP RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 RT ELEVATOR HAS CRACK IN EXTERIOR SKIN JUST OUTBOARD OF GEARED TAB. CUT OUT DAMAGED AREA ON RT ELEVA TOR EXTERIOR SKIN IAW SRM 55-2-1 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER ON RT ELEVATOR EXTERIOR SKIN JUST OUTBO ARD OF GEARED TAB IAW SRM 55-2-1 FIG 7. 2 L 7 4 4F RT 4A25 2007110800228 20071108 00228 EU 2007 11 8 USAA920071015 1 20071017 A 5347 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274AY 342 BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 4789 / FR 57.4 - BS 4842 / FR 58, -Y450. REPAIRED CAB IN SEAT TRACK, BS 4789 / FR 57.4 - BS 4842 / FR 58, -Y450 IAW A330 SRM 53-31-15 AND 51-23-00. AIRCRAFT MANUFACTURER AND MODEL WAS CHANGED FROM BOEING 767201ER TO AIRBUS A330323. 2 L 7 2 4F RT A46NM 2007110800234 20071108 00234 NM 2007 11 8 ASAA0792186 1 20071029 A 5240 571411 LATCH BOEING 737 737990 NM SERVICE DOOR BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 315AS 30019 RELEASE LATCH ON RIGHT FWD SVC DOOR BROKEN. REPLACED R2 DOOR HOLD RELEASE BUTTON. 2 L 7 4 4F RT A16WE 2007110800235 20071108 00235 NM 2007 11 8 ASAA0772168 1 20071017 A 5320 143A751012 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 FWD CARGO RBL 22 INTERCOSTAL BS 5004 500B UPPER FLANGE CRACKED. REPAIR IAW B737 700 SRM 51-70-11 FOR 201. 2 L 7 2 4F RT A16WE 2007110800238 20071108 00238 NM 2007 11 8 ASAA0772171 1 20071019 A 5320 146A94014 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 AFT CARGO PIT CORROSION ON FLOOR SUPPORT TEE. REPLACED WITH NEW PART IAW B737 700 SRM 53-00-53. 2 L 7 2 4F RT A16WE 2007110800245 20071108 00245 NM 2007 11 8 ASAA0772178 1 20071019 A 5315 147A55067 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 AFT CABIN BS 986.5 FLOORBEAM UPPER CAP CORRODED AT LBL 18. REPLACED UPPER CAP IAW CASCADE ERD 7360. 2 L 7 2 4F RT A16WE 2007110800247 20071108 00247 NM 2007 11 8 ASAA0772180 1 20071019 A 5315 147A55067 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 AFT CABIN BS 986.5 FLOORBEAM UPPER CAP CORRODED AT RBL 4. REPLACED UPPER CAP IAW ERD 7360. 2 L 7 2 4F RT A16WE 2007110800250 20071108 00250 NM 2007 11 8 ASAA0772183 1 20071019 A 5315 147A55067 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 AFT CABIN BS 986.5 FLOORBEAM UPPER CAP CORRODED AT RBL 22. REPLACED UPPER CAP IAW ERD 7360. 2 L 7 2 4F RT A16WE 2007110800251 20071108 00251 NM 2007 11 8 ASAA0772184 1 20071019 A 5315 147A55067 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 AFT CABIN BS 986.5 FLOORBEAM UPPER CAP CORRODED AT RBL 17. REPLACED UPPER CAP IAW ERD 7360. 2 L 7 2 4F RT A16WE 2007110800253 20071108 00253 NM 2007 11 8 ASAA0742187 1 20071030 A 5313 6549886133 STRINGER BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 FWD CARGO COMPARTMENT STA 500A STG 19L CRACKED IN UPPER FLANGE. INSTALLED SPLICE REPAIR TO STG 19L STA 500A IAW B737 40 0 SRM 53-30-03 FIG 1 AND FIG 101 AND 53-00-03 FIG 201. 2 L 7 2 4F RT A16WE 2007110800259 20071108 00259 SO 2007 11 8 LR7A07105 1 20071001 A 5311 SPLICE LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2661 4763 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5317 FOUND CABIN OVERHEAD RING SEGMENT SPLICER CRACKED AT FS 477 WL 285 RBL 20 . REPAIR ACCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70. 2 H 7 4 4T A1SO 2007110800260 20071108 00260 SO 2007 11 8 LR7A07106 1 20071001 A 5320 BEAM LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2661 4763 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5324 FOUND RIGHT UPPER MWW BOW BEAM CRACKED AT FS 557 WL 202 RBL 64. REPAIR A CCOMPLISHED IAW SMP583 FIG 53-40-14 USING 7075T6, .100". 2 H 7 4 4T A1SO 2007110800274 20071108 00274 NM 2007 11 8 NOCA16407 1 20071030 A 3350 LIGHT BOEING 757 75728A 1384976 NM EXTERIOR INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 755NA 30043 EXTERIOR EMERGENCY LIGHT AT R2 AND R4 INOP. REPLACED LIGHT AS PER MM 33-51-01. 2 L 7 2 4F RT A2NM 2007110800279 20071108 00279 NM 2007 11 8 ASAA0752189 1 20071031 A 2131 71231997302 CONTROL MODULE BOEING 737 737890 1384527 NM CABIN PRESSURE BROKEN A ASAA K NONE O OTHER NR NOT REPORTED 1 NM 02 585AS 35683 AUTO PRESSURE CONTROL FLT ALTITUDE DOES NOT MOVE IN 500FT INCREMENTS. REPLACED CABIN PRESSURE CONTROL MODULE. 2 L 7 2 4F RT A16WE 2007110800283 20071108 00283 NM 2007 11 8 ZZDA2007292 1 20071031 A 5610 58935734 WINDOW BOEING 737 73776N 13844CH NM COCKPIT CRACKED A ZZDA O OTHER O OTHER CR CRUISE 1 SO 37 174AT 32667 RIGHT SIDE EYE BROW WINDOWS MIDDLE PANE CRACKED R4. REMOVED AND REPLACED RIGHT SIDE EYE BROW WINDOWS R4 REF MM 56-11, L EAK CHECK OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2007110800289 20071108 00289 NM 2007 11 8 SWAA075406 1 20071029 A 3350 311500 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 226WN 32494 DURING SCHEDULED HC1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 16 ABC. REMOVED AND REPLACED LENS P ER MM. 2 L 7 2 4F RT A16WE 2007110800297 20071108 00297 NM 2007 11 8 SWAA075410 1 20071029 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007110800298 20071108 00298 NM 2007 11 8 SWAA075411 1 20071029 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007110800299 20071108 00299 NM 2007 11 8 SWAA075412 1 20071031 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110800311 20071108 00311 NM 2007 11 8 SWAA075424 1 20071031 A 5312 6516300 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED SPV CHECK, FOUND VERTICAL WEB CRACKED FWD BULKHEAD BS 178, LBL 17, WL 227. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007110800312 20071108 00312 NM 2007 11 8 SWAA075426 1 20071031 A 3350 311500 LENS BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 11 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007110800314 20071108 00314 NM 2007 11 8 SWAA075427 1 20071030 A 5330 6545772 SKIN BOEING 737 7375H4 138449D NM FUSELAGE WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN AT UPPER BS 1008, RBL 12.75, WORN. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007110900007 20071109 00007 NM 2007 11 9 QXEA200701635 1 20071030 A 3231 DOOR BOMBDR DHC8 DHC8402 1390042 NM MLG MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 425QX 4039 SEA - ON FLIGHT 2488, RIGHT MAIN LANDING GEAR DOOR REMAINED OPEN AFTER GEAR RETRACTION. CREW RAN THROUGH LANDING GEAR D OOR MALFUNCTION CHECKLIST THEN RETURNED TO FIELD. MAINTENANCE INTERROGATED PSEU AND FOUND PRESENT FAULTS. PRESSURIZED NR 2 HYDRAULIC SYSTEM. ALL GEAR DOORS CLOSED AND ALL PRESENT FAULTS WENT AWAY. OPERATION CHECKS GOOD. NO PARTS REPLAC ED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007110900011 20071109 00011 NM 2007 11 9 USAA920071059 1 20071023 A 5320 654580733 STIFFENER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED CABIN ANGLE STIFFENER, BS 291.5, S10R - S11R. REPLACED CABIN ANGLE STIFFENER, BS 291.5, S10R - S11R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007110900012 20071109 00012 NM 2007 11 9 USAA920071060 1 20071023 A 5320 654580731 STIFFENER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED CABIN ANGLE STIFFENER, BS 291.5, S11R - S12R. REPLACED CABIN ANGLE STIFFENER, BS 291.5, S11R - S12R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007110900017 20071109 00017 NM 2007 11 9 USAA920071065 1 20071024 A 5340 66235744 STRINGER CLIP BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED STRINGER CLIP, BS 706, S11R. REPLACED CRACKED STRINGER CLIP, BS 706, S11R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007110900026 20071109 00026 NM 2007 11 9 2007UALA04455 1 20071030 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 CRACK FOUND RT SIDE FUSELAGE AFT OF FLAP FWD OF CARGO DOOR CUTOUT PIT. MAJOR REPAIR OF SKIN AREA PERFORMED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110900031 20071109 00031 NM 2007 11 9 2007UALA04465 1 20071029 A 5313 146T3001 STRINGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1263 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 65644 25391 MAIN CABIN, RT FUSELAGE INTERNAL, STR 13R HAS SURFACE CORROSION JUST AFT OF STA 1263. SUSPECT MOISTURE CONTAMINATION. R EMOVED DAMAGED AND FABRICATED REPAIR AND INSTALLED PER SRM 53-00-03. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110900035 20071109 00035 NM 2007 11 9 2007UALA04471 1 20071030 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY LIGHTS AT ROW 5E, ALL ALONG UPPER DECK STAIRS & ALONG WALL ACROSS DOOR 3L ARE INOPERATIVE. SECURED CONNECTOR . 2 L 7 4 4F 4 F RT A20WE E24NE 2007110900047 20071109 00047 NM 2007 11 9 2007UALA04490 1 20071031 A 5210 DOOR FRAME BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L5 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 181UA 25278 NR 5 LT MED UPPER FRAME CRACKED AT CENTER UPPER GATE HINGE ATTACH HOLE. REPAIRED CRACK PER IAW SRM 80-52-10-08-JD PG 15 & SRM 51-70-11. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110900060 20071109 00060 NM 2007 11 9 2007UALA04507 1 20071031 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 1R UPPER CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 R-1 DOOR UPPER GATE CRACKED. REPLACED GATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110900071 20071109 00071 EA 2007 11 9 QXEA200701638 1 20071031 A 2820 PUMP CNDAIR CL600 CL6002C10 1390015 EA CROSSFLOW WARNING LIGHT A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 615QX 10065 GEG - ON FLIGHT 2517, RECEIVED XFLOW PUMP CAUTION MESSAGE. AIRCRAFT RETURNED TO FIELD. ACCOMPLISHED UNEVENTFUL LANDING . PLACED ON MEL IAW REF 28-13-10. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007110900078 20071109 00078 SO 2007 11 9 SWIA200718824 1 20071029 A 7910 CAP EMB 120 EMB120ER 3260203 SO ENGINE OIL LEAKING A SWIA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 250YV 120250 FLT 5781 - ON TAXI OUT, RECEIVED A TRIPLE CHIME WITH AURAL "OIL PRESSURE" MESSAGE. FOUND OIL LEAKING PAST THE FILLER CA P. ADJUSTED CAP TENSION WITH NO FURTHER LEAKS NOTED. 2 L 7 2 4T RT A31SO 2007110900096 20071109 00096 NM 2007 11 9 SWAA075439 1 20071031 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 516 AND BS 487, STR 26L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900099 20071109 00099 EU 2007 11 9 07FDEA04711 1 20071102 A 5712 A57141272200 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 729FD 657 FOUND CRACK IN RIB 13 LT WING FWD AREA. REPAIR PERFORMED IAW SRM 57-20-19 PB.200, PARA 4 D . 2 L 7 2 4F RT A35EU 2007110900110 20071109 00110 2007 11 9 F3LA200700300 4 20071017 A 2565 BLANKING PLATE AIRBUS A319 A319112 3930323 EU R2 GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON R2 DOOR FWD AND AFT GIRT BAR PADS. REMOVED AND REPLACED FWD AND AF T R2 DOOR GIRT BAR BLANKING PLATES IAW AMM 52-13-31-PB401 AND 52-13-31-400-007. 2 L 7 2 4F RT A28NM 2007110900112 20071109 00112 SO 2007 11 9 C2XA07SH090 1 20071101 A 3350 INVERTER EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13929 009 SHV - DURING MAINTENANCE ROUTINE CHECK MAINTENANCE FOUND SERVICE DOOR OVERHEAD EMERGENCY EXIT SIGN INOP. MAINTENANCE RE MOVED AND REPLACED SERVICE DOOR INVERTER (I/B) IAW EMB 145 SWPM 20-50-00. OPS CHECK GOOD. AIRCRAFT WAS APPROVED TO RET URN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007110900118 20071109 00118 NM 2007 11 9 HNAA0700257 1 20071029 A 3232 82970018011 DOOR ACTUATOR DHAV DHC8 DHC8102 2809003 NM LANDING GEAR MALFUNCTIONED A HNAA O OTHER J WARNING INDICATION TO TAKEOFF 1 EA 07 805EX 22853 22853 228 AFTER TAKEOFF THE LEFT HAND FORWARD GEAR DOOR REMAINED OPEN AFTER THE GEAR WAS SELECTED TO THE UP POSTION. REMOVED AND REPLACED LT FORWARD DOOR ACTUATOR REF -8 MM 32-10-36. SWUNG GEAR SEVERAL TIMES, NO DEFECTS NOTED. SERVICED AND BLEED T HE HYDRAULICS SYSTEM. 2 H 7 2 4T RT A13NM 2007110900132 20071109 00132 EU 2007 11 9 AALA20072099 1 20071031 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14068 511 JFK - EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER THREE DOO R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007110900133 20071109 00133 WP 2007 11 9 AALA20072094 1 20071031 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 566AA 49348 SFO - EMERGENCY LIGHT AT SEAT 29D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 29D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007110900134 20071109 00134 NM 2007 11 9 AALA20072093 1 20071031 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 969AN 29546 MSP - EMERGENCY LIGHT AT SEAT 8ABC INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 8ABC. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007110900135 20071109 00135 WP 2007 11 9 AALA20072082 1 20071030 A 3397 TERMINAL DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 931TW 49527 SFO - EMERGENCY LIGHTS AT LEFT AND RIGHT OVERWING DOOR SEAT ROW 20 INOPERATIVE. CLEANED TERMINALS ON BATTERY FOR EMERGE NCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007110900136 20071109 00136 NM 2007 11 9 AALA20072088 1 20071031 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 757AN 32636 DFW - EMERGENCY LIGHT AT SEAT 25C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110900137 20071109 00137 NM 2007 11 9 AALA20072089 1 20071031 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 757AN 32636 DFW - EMERGENCY LIGHT AT SEAT 31C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110900138 20071109 00138 NM 2007 11 9 AALA20072090 1 20071031 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 757AN 32636 DFW - EMERGENCY LIGHT AT SEAT 44C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 44C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110900139 20071109 00139 NM 2007 11 9 AALA20072091 1 20071031 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 MIA - EMERGENCY LIGHT AT SEAT 26C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110900145 20071109 00145 NM 2007 11 9 AALA20072087 1 20071030 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 753AN 30261 DFW - EMERGENCY LIGHT AT SEAT 30C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 30C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110900146 20071109 00146 EU 2007 11 9 AALA20072098 1 20071031 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14068 511 JFK - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOO R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007110900148 20071109 00148 WP 2007 11 9 AALA20072080 1 20071030 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 33502 49739 LGA - EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD FIRS T CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110900149 20071109 00149 NM 2007 11 9 AALA20072070 1 20071030 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 761AJ 31478 JFK - EMERGENCY LIGHT AT SEAT 20C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110900150 20071109 00150 NM 2007 11 9 AALA20072071 1 20071030 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 761AJ 31478 JFK - EMERGENCY LIGHT AT SEAT 21C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110900151 20071109 00151 NM 2007 11 9 AALA20072084 1 20071030 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 753AN 30261 DFW - EMERGENCY LIGHT AT OVERHEAD RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD RIGH T NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110900154 20071109 00154 NM 2007 11 9 AALA20072073 1 20071030 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 761AJ 31478 JFK - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110900156 20071109 00156 NM 2007 11 9 AALA20072075 1 20071030 A 3397 P4010051112 CONTROL MODULE BOEING 767 767223 1385123 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 329AA 22329 SFO - EMERGENCY LIGHTS AT LEFT SEAT ROWS 9 TO 19 INOPERATIVE. REPLACED MODULE FOR EMERGENCY LIGHTS AT LEFT SEAT ROWS 9 TO 19. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007110900159 20071109 00159 NM 2007 11 9 AALA20072069 1 20071029 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 357AA 24038 SFO - EMERGENCY LIGHT AT OVERHEAD A6 LAVATORY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD A6 LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007110900160 20071109 00160 NE 2007 11 9 AALA20072059 2 20071028 A 7261 FC3520100 OIL CAP BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4B3 NE LT ENGINE LOOSE A AALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 191AN 32385 31072 PTY INFLIGHT T966/28OCT UIO TO MIA - LEFT ENGINE OIL QUANTITY WENT TO ZERO IN CRUISE FOLLOWED BY PRESSURE AND PRESSURE I NDICATION LIGHT ILLUMINATED. CREW SHUT DOWN ENGINE. LANDED PTY WITHOUT INCIDENT. SINGLE ENGINE TIME 60 MINUTES. FOUN D OIL TANK CAP LOOSE. SERVICED ENGINE WITH OIL. REPLACED OIL CAP AT PTY. MIA REPLACED CAP ASSEMBLY HOUSING AND CHECK VALVE FOR ENGINEERING EVALUATION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2007110900164 20071109 00164 NM 2007 11 9 AALA20072001 1 20071020 A 2913 PUMP BOEING 767 767323 1385205 NM HYD SYSTEM LEAKING A AALA J A DUMP FUEL UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 380AN 25449 DFW INFLIGHT T963/20OCT - RIGHT HYDRAULIC QUANTITY LIGHT ILLUMINATED WITH LOSS OF PRESSURE. FLIGHT DUMPED 33000 POUNDS OF FUEL AT FLIGHT LEVEL 330. FOUND DAMAGED O-RING IN RIGHT PYLON. LANDED DFW WITHOUT INCIDENT. REPLACED RIGHT ENGINE DRIVEN PUMP AND BOTH FILTERS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007110900165 20071109 00165 NM 2007 11 9 AALA20071974 1 20071018 A 2897 CONNECTOR BOEING 777 777223 1385213 NM FUEL PUMP LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 797AN 30012 MIA INFLIGHT T995/18OCT - RIGHT CENTER FUEL PUMP WOULD NOT TURN OFF. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. FOUN D LOOSE CONNECTOR FOR RIGHT CENTER FUEL PUMP POUNDS PER SQUARE INCH SWITCH. REPLACED SWITCH. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110900166 20071109 00166 EU 2007 11 9 TRBA2007092 1 20071102 A 3350 7012210 LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS INOPERATIVE A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 308AE 309 PAX DOOR EMERGENCY STAIR LIGHT INOPERATIVE. REPOSITIONED LAMP AND PERFORMED OP CK IAW JIC NR 33-50-00. 2 H 7 2 4T RT A53EU 2007110900167 20071109 00167 NM 2007 11 9 EIA2007188 1 20071011 A 5330 SKIN BOEING 747 747273C 1384896 NM BS 2762 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 BS 2762 BWL 292.5 SKIN PREVIOUS REPAIR FILLER DAMAGED. REMOVED OLD REPAIR, FABRICATED NEW REPAIR PER B747 SRM 53-30-03 FIG 1A. 2 L 7 4 4F A20WE 2007110900173 20071109 00173 NE 2007 11 9 HNAA0700258 2 20071101 A 7314 5009984C PUMP DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE NR 1 ENGINE CLOGGED A HNAA E B ENGINE SHUTDOWN EMER. DESCENT J WARNING INDICATION TO TAKEOFF 1 EA 07 937HA 44657 9012 148 120447 THE NUMBER ONE ENGINE MANUAL CAUTION LIGHT ILLUMINATED AT ROTATION, SHORTLY THERE AFTER (1500FT) TORQUE DROPPED OFF. TH EN THE PROP WENT INTO FEATHER. THE MAX TORQUE REACH AT 107 PERCENT. THE CREW MANUALLY SHUT DOWN THE ENGINE. DECLARED AN EMERGENCY AND DID AN AIR TURN AROUND. CHECKED THE ENGINE CONTROL PANEL FOR FLAGS, FOUND THAT THE NUMBER ONE ENGINE C ONTROL UNIT WAS FLAGGED. REMOVED AND REPLACED THE NR 1 EEC, HMU/FUEL PUMP IAW W/C’S 73-20-01R AND 76-00-01Q, OPS AND LE AK CHECKS GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2007110900174 20071109 00174 SO 2007 11 9 SIMA200730604 1 20071104 A 2540 462081 TOILET EMB 135 EMB135KL 3260302 SO LAVATORY ODOR A SIMA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 827AE 145602 ON CLIMB-OUT, FLIGHT ATTENDANT REPORTED FAINT ODOR OF BURNING RUBBER IN CABIN. ODOR WENT AWAY AFTER 5 MINUTES. FOUND O DOR COMING FROM LAV. FOUND LAV LEAKING. REMOVED AND REPLACED LAV TOILET UNIT IAW EMB140 AMM 38-32-01. NO LEAKS OR ODO R NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007110900175 20071109 00175 NM 2007 11 9 CALA0700632 1 20071101 A 5320 141A54103 INTERCOSTAL BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33209 30581 INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL AT STA 294.5, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51- 40-02. 2 L 7 2 4F RT A16WE 2007110900176 20071109 00176 SO 2007 11 9 SIMA200730902 1 20071102 A 2720 15H0048PH PRESSURE SWITCH EMB 135 EMB135KL 3260302 SO RUDDER MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 829AE 145609 CREW ELECTED TO RETURN INTO CLT DUE TO RUDDER SYS 1/2 INOPERATIVE MESSAGE ON EICAS FOLLOWED BY AUTO PILOT AND YAW DAMPER FAIL ON EICAS AIRCRAFT RETURNED TO CLT WITH NO FURTHER INCIDENT DISC-YAW DAMPER AND AUTO PILOT FAIL IN FLIGHT, RUDDER SYSTEM 1 INOP INTERMITTENT, RUD SYS 2 INOP INTERMITTENT. REMOVED AND REPLACED RUDDER PRESSURE SWITCH FOR SYS 1 AND 2. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007110900179 20071109 00179 NM 2007 11 9 CALA0700634 1 20071101 A 5320 141A541059 INTERCOSTAL BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33209 30581 INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL AT STA 328-344, LBL 47. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007110900180 20071109 00180 NM 2007 11 9 CALA0700635 1 20071101 A 5320 141A541012 INTERCOSTAL BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33209 30581 INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL AT STA 328, RBL 32. THE INTERCOSTAL WAS REPAIRED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007110900183 20071109 00183 NM 2007 11 9 NWAA073636314 1 20071102 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 674US 30269 DURING LINE CHECK, FOUND UPPER DECK RT EMERGENCY DOOR BATTERY PACK INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTER Y PACK PER AMM 52-23-14. FUNCTIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2007110900184 20071109 00184 NM 2007 11 9 CALA0700637 1 20071101 A 5315 BAC14902811 FLOORBEAM BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33209 30581 INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, LBL 11. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, REPAIR 1. 2 L 7 2 4F RT A16WE 2007110900185 20071109 00185 NM 2007 11 9 CALA0700638 1 20071101 A 5320 141A541012 INTERCOSTAL BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33209 30581 INSPECTION FOUND A 1.6 INCH CRACK IN INTERCOSTAL AT STA 312-328, LBL 45. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW S RM 51-40-02. 2 L 7 2 4F RT A16WE 2007110900189 20071109 00189 EU 2007 11 9 F3LA200700302 1 20071016 A 2597 WIRE HARNESS AIRBUS A319 A319112 3930323 EU R1 DOOR SLIDE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED R1 DOOR SLIDE ELECTRICAL HARNESS CAME FROM THE FACTORY PINCHED IN THE SLIDE ASSY , AND CANNOT BE ROUTED AS SHOWN IN AMM FIG 25-62-44-911-003, SHEET 404.2/3. REMOVED AND REPLACED DAMAGED R1 DOOR SLIDE IAW AMM 25-62-44-400-007. 2 L 7 2 4F RT A28NM 2007110900190 20071109 00190 EU 2007 11 9 F3LA200700303 1 20071017 A 5320 D5361019720000 THRESHOLD AIRBUS A319 A319112 3930323 EU L1 DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED L1 DOOR THRESHOLD STRIP CORRODED ON LOWER SURFACE. REMOVED AND REPLACED L1 DOOR THRESHOLD STRIP IAW AMM 53-12-12-400-001. 2 L 7 2 4F RT A28NM 2007110900191 20071109 00191 EU 2007 11 9 F3LA200700304 1 20071018 A 5320 SUPPORT AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED SUPPORT FRAME AT FR70 CORRODED ON UNDERSIDE AT NUTPLATE CUTOUT, WHICH WAS FOUND AFTER REMOVAL OF THE SHEAR WEB. REMOVED SUPPORT FRAME AT LT SIDE OF FR70 IAW A319 SRM 51-42-11. DETERMINED TO BE OUT O F LIMITS IAW SRM 53-41-14, FIG 2. INSTALLED SHEAR PLATE TO NEW SUPPORT FRAME IAW SRM 51-72-11 AND 51-42-11. 2 L 7 2 4F RT A28NM 2007110900192 20071109 00192 EU 2007 11 9 F3LA200700305 1 20071017 A 5320 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM BETWEEN FR 68 AND FR 69 AT Y1292, INBD AND AFT OF L1 DOOR FRAME, CORRO DED. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11, PARA 7. 2 L 7 2 4F RT A28NM 2007110900194 20071109 00194 EU 2007 11 9 F3LA200700307 1 20071017 A 5315 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED CABIN FLOORBEAM AT FR 69 RT CORRODED IN NUTPLATE HOLE. REMOVED AND REPLACED FLO ORBEAM IAW SRM 53-00-14, FIG. 102, 51-42-11 AND 51-72-11. 2 L 7 2 4F RT A28NM 2007110900196 20071109 00196 WP 2007 11 9 UPS07851089 1 20071102 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 851UP 46051 EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK. CKS OK IAW MM 33-50-01-2. 2 L 7 4 4F RT 4A25 2007110900198 20071109 00198 EA 2007 11 9 A6WA200740549 1 20071001 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 411ZW 7569 FS 280 FLOOR SUPPORT BEAM CLIP AT LBL 9, INBOARD, IS CRACKED IN RADIUS APPROX .50 INCH LONG. MAINTENANCE CRACKED CLIP A ND INSTALLED NEW CLIP P/N 601R31113-57 IAW BSC SR 601R-53-0057A AND CRJ SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007110900199 20071109 00199 EU 2007 11 9 F3LA200700308 1 20071017 A 5321 D5361087600000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 221FF CORRODED ON LOWER SURFACE, FWD EDGE. REMOVED AND REPLACED FLO OR PANEL 221FF IAW AIRBUS AMM 53-12-12-400-001, 53-12-12-PB401, AND WORK CARD CP753-12. 2 L 7 2 4F RT A28NM 2007110900200 20071109 00200 NM 2007 11 9 CALA0700639 1 20071101 A 5315 BAC14902887 FLOORBEAM BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33209 30581 INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, RBL 41. THE UPPER CHORD OF FLOORBEAM WAS REPLACED IAW ECRA 5321-01508. 2 L 7 2 4F RT A16WE 2007110900202 20071109 00202 NM 2007 11 9 CALA0700641 1 20071101 A 5315 BAC14902811 FLOORBEAM BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33209 30581 INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, BL 0 TO LBL 13. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01504. 2 L 7 2 4F RT A16WE 2007110900203 20071109 00203 NM 2007 11 9 MWEA070267 1 20071101 A 5315 593056035 FLOORBEAM DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 601ME 49762 AT STATION 1311 FLOOR LEVEL CENTER AREA BETWEEN AFT LAVATORY HAS CORROSION AT FLOOR BEAM. REMOVED AND REPLACED FLOORBEA M. 2 L 7 2 4F RT A6WE 2007110900204 20071109 00204 EA 2007 11 9 TRAX200701611 1 20071029 A 5512 TIP CAP CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 AAR - LEFT HORIZONTAL STABILIZER TIP HAS CRACK ON LEADING EDGE TIP. 2 L 7 2 4F RT A21EA 2007110900205 20071109 00205 EU 2007 11 9 TRAX200701612 1 20071029 A 5320 FITTING AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 CLIP FWD OF FR 23 BETWEEN STR 21 RT & LT CORRODED. GASKET AND DOUBLER REMOVED / REPLACED IAW JIC 34-43-21. AND FOUND S ERVICEABLE. 2 H 7 2 4T RT 2007110900207 20071109 00207 EU 2007 11 9 TRAX200701613 1 20071029 A 5320 ANGLE AEROSP ATR72 ATR72 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 ANGLE CRACKED AT LEFT FR 26 STRINGER 4 (INTERNAL STRUCTURE). ANGLE REPLACED AT L/H FR 26 STRG 4 IAW SRM 51-25-01 AND 51 -25-04. 2 H 7 2 4T RT 2007110900209 20071109 00209 EU 2007 11 9 TRAX200701615 1 20071029 A 5714 INTERCOSTAL AEROSP ATR72 ATR72 EU WING BOX CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 INTERCOSTAL CRACKED ON RIGHT WING BOX BETWEEN FAIRING FR 25 + 26. REPAIRED IAW NTO ANA/YUL07/260/338-005 REPAIR DETERM INED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH NTO NA/YUL/07/260/338-005. 2 H 7 2 4T RT 2007110900210 20071109 00210 WP 2007 11 9 ABXA070359 1 20071022 A 5320 99155541 INTERCOSTAL DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 SUPPORT INTERCOSTAL BETWEEN FRAMES 427 - 446 AT LONGERON 29 LEFT WAS CRACKED. REPAIRED INTERCOSTAL IAW DC9 SRM. 2 L 7 2 4F A6WE 2007110900211 20071109 00211 WP 2007 11 9 ABXA070360 1 20071023 A 5320 S2914913M24000 FLOOR SUPPORT DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 EXFOLIATED FLOOR SUPPORT FROM FS 993 TO 1072 LEFT. REMOVED AND REPLACED TRACK SUPPORT FLOOR IAW DC9 SRM 53-05, FIG 4G, SHEET 1. 2 L 7 2 4F A6WE 2007110900213 20071109 00213 WP 2007 11 9 ABXA070362 1 20071025 A 5320 991555047 INTERCOSTAL DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 INTERCOSTAL BETWEEN STA 1056 - 1072 AT LONGERON 27 - 28 LEFT CORRODED. REMOVED AND REPLACED INTERCOSTAL IAW DC9 SRM 51- 30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2007110900214 20071109 00214 WP 2007 11 9 ABXA070363 1 20071024 A 5347 S2914913M24000 SEAT TRACK DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 RIGHT BUTT LINE 44.5 SEAT TRACK UPPER FLANGE CRACKED AT STA 240. REPLACED SEAT TRACK SECTION IAW DC9 SRM 51-30-01. 2 L 7 2 4F A6WE 2007110900215 20071109 00215 SO 2007 11 9 RAIA00710035 1 20071026 A 3610 V8545A7257226 O-RING EMB 145 EMB145LR 3260212 SO BLEED AIR SYS WORN A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 817HK 145058 FLT 5592 - STL - NR 1 ENGINE BLEED LEAK. MAINTENANCE REMOVED AND REPLACED BLEED O-RING. 2 L 7 2 4T RT T00011AT 2007110900216 20071109 00216 SO 2007 11 9 RAIA00710031 1 20071024 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 813HK 145044 POST FLT 5461 - STL - EMERGENCY LIGHT FLOOR PROXIMITY LIGHT INOP. MAINTENANCE RESET POWER TO EMERGENCY LIGHT SYSTEM, OP S CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007110900217 20071109 00217 SO 2007 11 9 RAIA00710033 1 20071026 A 3610 O-RING EMB 145 EMB145LR 3260212 SO BLEED AIR SYS WORN A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 816HK 145055 FLT 5492 - IAD - BLEED 1 LEAK ON CLIMBOUT. MAINTENANCE REMOVED AND REPLACED NR 1 BLEED SYSTEM O-RING SEAL IN CENTER OF CARGO BAY, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007110900223 20071109 00223 EU 2007 11 9 TRAX200701631 1 20071029 A 5753 BRACKET AEROSP ATR72 ATR72 EU T/E FLAP BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 LEFT O/B FLAP ARM AT FLAP RIB 1A, 2 OMEGA BRACKETS BROKEN. REPLACED IAW SRM 51-25-04. 2 H 7 2 4T RT 2007110900226 20071109 00226 EU 2007 11 9 TRAX200701635 1 20071029 A 5260 STEP AEROSP ATR72 ATR72 EU AIRSTAIRS CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 ON STAIR CASE OF PAX DOOR CORROSION FOUND ON STEP NR 4. 2 H 7 2 4T RT 2007110900230 20071109 00230 EA 2007 11 9 TRAX200701656 1 20071031 A 5530 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 759EV 10211 VERTICAL STAB-TO-FUSELAGE LT DRAG ANGLE CRACKED AT AFT END. 2 L 7 2 4F RT A21EA 2007110900233 20071109 00233 EA 2007 11 9 TRAX200701645 1 20071030 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 828AS 7213 GEAR DISAGREE MSG UPON EXTENSION OF HANDLE. RAN QRH, GEAR DEPLOYED USING FREE FALL METHOD. EMERGENCY DECLARED. EMERGE NCY EQUIPMENT ON STANDBY. LANDING GEAR RETRACTION SYSTEM. 2 L 7 2 4F RT A21EA 2007110900237 20071109 00237 EA 2007 11 9 TRAX200701647 1 20071031 A 3350 SIGN CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 713EV 10081 LEFT INTERIOR OVERWING LOWER EMERGENCY EXIT SIGN IS INOP. 2 L 7 2 4F RT A21EA 2007110900239 20071109 00239 EA 2007 11 9 TRAX200701649 1 20071031 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 RIGHT OBLIQUE AND AT FS 625 IS CRACKED. REMOVED DAMAGED OBLIQUE ANGLE AND REPLACED WITH NEW SERVICEABLE PART PN 601-35 012-52 IAW CRJ SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007110900240 20071109 00240 EA 2007 11 9 TRAX200701650 1 20071031 A 5220 HINGE CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 ESCAPE HATCH, LT HINGE ARM CRACKED. REMOVED CRACKED HINGE IAW CRJ 200 AMM 52-22-00. INSTALLED SERVICEABLE ESCAPE HATCH H INGE ARM & SHROUD IAW CRJ AMM 52-22-00. PERFORMED FUNCTIONAL TEST IAW ASA TASK CARD ASA-2-838008. WHILE PERFORMING FUNCI TONAL TEST OF CREW ESCAPE HATCH FOUND STEP CLEARANCE TO BE OUT OF LIMITS. ADJUSTED CREW ESCAPE HATCH IAW CRJ AMM 52-22-0 0. REQUIRES OPS CHECK OF BLEED AIR CONTROL PANEL, FUEL CONTROL PANEL & PRESSURIZED GAP CHECKS. PERFORMED OPS CHECK OF B LEED AIR CONTROL PANEL IAW CRJ AMM 36-21-00. PERFORMED OPS CHECK OF FUEL CONTROL PANEL IAW CRJ AMM 28-00-00. OPS CHECK G OOD. REQUIRES PRESSURIZATION GAP CHECKS. PERFORMED PRESSURIZATION GAP CHECK IAW CRJ AMM 21-31-00. LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2007110900242 20071109 00242 EA 2007 11 9 TRAX200701654 1 20071031 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 934EV 8028 SEVERAL EMERGENCY LIGHTS INOP. 2 L 7 2 4F RT A21EA 2007110900248 20071109 00248 NE 2007 11 9 A6WA200740594 2 20071021 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT ODOR A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 422AW 7341 AFTER ENGINE SHUTDOWN, NR 1, NOTICED FUEL ODOR AND MORE THAN AVERAGE SMOKE FROM TAIL PIPE. FOUND ENGINE NR 1 THROTTLE A ND PULL CONTROL RIG OFF, RERIGGED LT ENGINE REF AMM 76-10-00. INSPECTED LT ENGINE, CLEANED EXCESS OIL OUT OF COWLING DR Y MOTOR ENGINE, NO SIGN OF SMOKE, PERFORMED OPERATIONAL RUN UP OF ENGINE. OPS CHECK GOOD. NO SIGNS OF SMOKE. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007110900250 20071109 00250 NM 2007 11 9 SWAA075488 1 20071101 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900251 20071109 00251 NM 2007 11 9 SWAA075487 1 20071101 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 14L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900252 20071109 00252 NM 2007 11 9 SWAA075468 1 20071031 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900257 20071109 00257 NM 2007 11 9 SWAA075475 1 20071101 A 3397 W414201220 WIRE BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 480WN 33998 EEPLS INOP AT ROW 13 DEF. FOUND LOOSE WIRE. SECURED WIRE PER WDM. 2 L 7 2 4F RT A16WE 2007110900258 20071109 00258 NM 2007 11 9 SWAA075456 1 20071031 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900259 20071109 00259 NM 2007 11 9 SWAA075452 1 20071031 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900260 20071109 00260 NM 2007 11 9 SWAA075453 1 20071031 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900262 20071109 00262 NM 2007 11 9 SWAA075455 1 20071031 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900264 20071109 00264 NM 2007 11 9 QXEA200701653 1 20071102 A 2930 6617303 VALVE BOMBDR DHC8 DHC8402 1390042 NM HYD SYSTEM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 423QX 353 239 4153 SEA FLIGHT NR 2244: ON APPROACH, NR 1 ENGINE HYD PUMP CAUTION ILLUMINATED WITH A DROP OF NR 1 HYD PRESSURE TO 0. PRESSU RE RETURNED TO 3000 PSI WITH SELECTION OF STANDBY HYD PUMP. CAUTION EXTINGUISHED MOMENTARILY, BUT ILLUMINATED WHEN FLAP S WERE SELECTED. MAINTENANCE REMOVED AND REPLACED NR 1 HYD SYSTEM EDP AND NR 1 ENGINE HYD NACELLE SHUTOFF VALVE. FLUSH ED NR 1 HYD SYSTEM IAW Q400 AMM 29-10-00 PAGES 319-321. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007110900265 20071109 00265 2007 11 9 SWAA075457 4 20071031 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007110900268 20071109 00268 NM 2007 11 9 SWAA075484 1 20071101 A 5330 65465767 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, STR 28L. REPAIRED SK IN PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900270 20071109 00270 NM 2007 11 9 SWAA075482 1 20071101 A 5523 69633915 BOLT BOEING 737 737301 1384611 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED BRDG CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED BUSHING AND BOLT PER MM. 2 L 7 2 4F RT A16WE 2007110900271 20071109 00271 NM 2007 11 9 SWAA075481 1 20071101 A 2730 654518710 TORQUE TUBE BOEING 737 737301 1384611 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED BRDG CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007110900272 20071109 00272 NM 2007 11 9 SWAA075477 1 20071101 A 5755 6545321 FITTING BOEING 737 737301 1384611 NM SPOILER WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED BRDG CHECK, FOUND LT WING INBOARD GROUND SPOILER OUTBOARD ACTUATOR FITTING WORN. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900273 20071109 00273 NM 2007 11 9 SWAA075486 1 20071101 A 3350 65C27093 LIGHT BOEING 737 737301 1384611 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007110900274 20071109 00274 EA 2007 11 9 A6WA200740593 1 20071022 A 2400 SWITCH CNDAIR CL600 CL6002B19 1900309 EA LAVATORY SIGN ARCED A A6WA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 409AW 7447 ORDINANCE SIGN CIRCUIT BREAKER POPPED. LAV OCCUPIED MICROSWITCH HAD SIGNS OF ELECTRICAL ARCING. REMOVED AND REPLACED L AV OCCUPIED SWITCH PER AMM 33-25-11. OPS CHECK GOOD. REMOVED PLACARD, REMOVED FROM MEL. (M) 2 L 7 2 4F RT A21EA 2007110900275 20071109 00275 EA 2007 11 9 A6WA200740592 1 20071017 A 3411 DRAIN CNDAIR CL600 CL6002B19 1900309 EA AIRSPEED CONTAMINATED A A6WA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 31 407AW 7424 ABORTED TAKEOFF BELOW 80 KNOTS DUE TO FAILED STANDBY AIRSPEED INDICATOR 0 KNOTS. ALL BRAKE TEMPERATURES INDICATE NORMAL . FOUND WATER IN P3 DRAIN. PERFORMED P3 CONTAMINATION REMOVAL PER AMM 34-11-00. PERFORMED LEAK TEST OF P3 PER AMM 34- 11-00-790-803 TEST OK. (M) 2 L 7 2 4F RT A21EA 2007110900276 20071109 00276 EA 2007 11 9 A6WA200740578 1 20071014 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 469AW 7917 FOUND FLOOR SUPPORT STRUCTURE CLIP AT FS 280, RBL 9, OUTBOARD IS CRACKED IN RADIUS APPROX .6 INCH LONG. MAINTENANCE REM OVED CRACKED CLIP AT FS 280 RBL 9.0 OUTBOARD LOCATED, DRILLED, INSTALLED NEW SERVICEABLE CLIP, P/N 601R31113-58 IAW CRJ SRM 51-42-13, 51-42-21 AND BSC SR 601R-53-0057A. (M) 2 L 7 2 4F RT A21EA 2007110900277 20071109 00277 EA 2007 11 9 A6WA200740579 1 20071014 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 469AW 7917 FOUND FLOOR SUPPORT STRUCTURE CLIP AT FS 280, RBL 9, INBOARD IS CRACKED IN RADIUS APPROX .5 INCH LONG. MAINTENANCE REMO VED INBOARD FS 280 CLIP AT RBL 9 AND INSTALLED SERVICEABLE CLIP P/N 601R31113-58, IAW CRJ 200 SRM 51-42-21 AND BSC STAND ARD REPAIR 601R-53-0057A. (M) 2 L 7 2 4F RT A21EA 2007110900278 20071109 00278 EA 2007 11 9 A6WA200740580 1 20071014 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 469AW 7917 FOUND FLOOR SUPPORT STRUCTURE CLIP AT FS 280, LBL 9, INBOARD IS CRACKED IN RADIUS APPROX .3 INCHES LONG. MAINTENANCE RE MOVED INBOARD 280 CLIP AT LBL 9 AND REINSTALLED NEW SERVICEABLE CLIP P/N 601R31113-57, IAW CRJ SRM 51-42-21 AND BSC STAN DARD REPAIR 601R-53-0057A. (M) 2 L 7 2 4F RT A21EA 2007110900279 20071109 00279 EA 2007 11 9 A6WA200740581 1 20071014 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 469AW 7917 FOUND FLOOR SUPPORT STRUCTURE CLIP AT FS 280, LBL 9, OUTBOARD IS CRACKED IN RADIUS APPROX .5 INCH LONG. MAINTENANCE REM OVED CRACKED CLIP AT FS 280 LBL 9.0 OUTBOARD. LOCATED, DRILLED, INSTALLED NEW SERVICEABLE CLIP, P/N 601R31113-57, IAW C RJ SRM 51-42-13, 51-42-21 AND BSC SR 601R-53-0057A. (M) 2 L 7 2 4F RT A21EA 2007110800197 20071108 00197 EU 2007 11 8 F3LA200700287 1 20071017 A 5320 SHEAR WEB AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED SHEAR WEB AT FR 70L CORRODED. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11 AND 51-72-11. 2 L 7 2 4F RT A28NM 2007110800198 20071108 00198 WP 2007 11 8 AALA20072040 1 20071026 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 484AA 49677 BOS - EMERGENCY LIGHTS AT AFT OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 21DEF FOR EMERGENCY LIGHT AT AFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110800199 20071108 00199 WP 2007 11 8 AALA20072048 1 20071027 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9405T 53141 LGA - EMERGENCY LIGHT AT SEAT ROW 29DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 29DEF. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007110800200 20071108 00200 WP 2007 11 8 AALA20072063 1 20071028 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7521A 49898 DFW - EMERGENCY LIGHT AT SEAT ROW 10D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 10D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110800201 20071108 00201 NM 2007 11 8 AALA20072066 1 20071029 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 342AN 33081 SFO - EXTERIOR EMERGENCY LIGHT AT AFT LEFT EXIT DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT AFT LEF T EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007110800202 20071108 00202 NM 2007 11 8 AALA20072062 1 20071028 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7375A 25202 SFO - EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK M738 FOR EMERGENCY LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007110800203 20071108 00203 2007 11 8 AALA20072065 2 20071029 A 7310 PRESSURE SWITCH BOEING 737 737823 13844BZ NM LEFT ENGINE INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 976AN 30099 LAX INFLIGHT - LEFT ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED. RETURNED TO LAX AND LANDED OVERWEIGHT WITHOUT INCIDENT . ACCOMPLISHED OVERWEIGHT INSPECTION. REPLACED FUEL FILTER AND FUEL PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F RT A16WE 2007110800204 20071108 00204 NM 2007 11 8 AALA20072064 1 20071028 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 942AN 30084 DFW - EMERGENCY LIGHT AT LEFT LOWER EXTERIOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT LOWER EXTERIOR. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007110800205 20071108 00205 NM 2007 11 8 AALA20072049 1 20071027 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 636AM 24594 DFW - EMERGENCY LIGHT AT SEAT ROW 11 INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 11. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007110800206 20071108 00206 NM 2007 11 8 AALA20072050 1 20071027 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 636AM 24594 DFW - SEAT MOUNTED EMERGENCY LIGHT AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHT AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007110800207 20071108 00207 WP 2007 11 8 AALA20072057 1 20071028 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 589AA 53252 LGA - EMERGENCY LIGHTS AT SEAT ROWS 29 TO 30 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 29 TO 30. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007110800208 20071108 00208 NM 2007 11 8 AALA20072055 1 20071027 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 684AA 25341 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 36 RIGHT SIDE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEA T ROW 36 RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007110800209 20071108 00209 WP 2007 11 8 AALA20072058 1 20071028 A 4900 INLET DOUG DC9 DC982 3022082 WP APU CONTAMINATED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 278AA 49294 PHX INFLIGHT T1770/28OCT - FLIGHT ATTENDANTS REPORTED BLUE SMOKE OR HAZE IN CABIN AND ODOR NOTED IN COCKPIT. RETURNED TO PHX AND LANDED WITHOUT INCIDENT. FOUND OIL IN APU INLET. ACCOMPLISHED PACK BURN OUT AND REPLACED BOTH COALESCER BA GS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110800210 20071108 00210 NM 2007 11 8 AALA20072061 1 20071028 A 3350 1000679 LIGHT BOEING 767 767323 1385205 NM COCKPIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7375A 25202 SFO - EMERGENCY EXIT LIGHT IN COCKPIT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT LIGHT IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007110800211 20071108 00211 NM 2007 11 8 AALA20072044 1 20071026 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 604AA 27055 DFW - EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007110800212 20071108 00212 NM 2007 11 8 AALA20072045 1 20071026 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 671AA 25336 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 11D MISSING LENS. REPLACED LENS FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007110800213 20071108 00213 NM 2007 11 8 AALA20072046 1 20071026 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 671AA 25336 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 11D MISSING LAMP. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007110800214 20071108 00214 NM 2007 11 8 AALA20072060 1 20071028 A 3350 630262 SWITCH BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 978AN 30100 DFW - EMERGENCY LIGHT AT OVERWING RIGHT EXIT DOOR INOPERATIVE. REPLACED SWITCH FOR EMERGENCY LIGHT AT OVERWING RIGHT EX IT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007110800215 20071108 00215 WP 2007 11 8 AALA20072041 1 20071026 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 446AA 49472 LGA - EMERGENCY FLASHLIGHT AT RIGHT AFT LAVATORY HAS MISSING STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT RIGHT AF T LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110800216 20071108 00216 NM 2007 11 8 AALA20072052 1 20071027 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 658AA 24616 DFW - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR EXIT SIGN INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHT AT RIG HT NUMBER FOUR DOOR EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007110800217 20071108 00217 NM 2007 11 8 AALA20072053 1 20071027 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 684AA 25341 DFW - EMERGENCY LIGHT AT RIGHT OVERHEAD AISLE AT SEAT ROW 29 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT OV ERHEAD AISLE AT SEAT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007110800218 20071108 00218 NM 2007 11 8 AALA20072054 1 20071027 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 684AA 25341 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 33 RIGHT SIDE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEA T ROW 33 RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007110800219 20071108 00219 WP 2007 11 8 AALA20072047 1 20071027 A 3260 TARGET DOUG DC9 DC983 3022083 WP MLG DOOR BROKEN A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 438AA 49456 SLC INFLIGHT T416/27OCT - GEAR DOOR OPEN LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTION. RETURNED TO SLC AND LANDED WITHOUT INCIDENT. FOUND LEFT MAIN LANDING GEAR PROXIMITY TARGET ASSEMBLY BROKEN OFF. REPLACED LEFT MAIN LANDING GEAR P ROXIMITY TARGET ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007110800220 20071108 00220 NM 2007 11 8 AALA20072043 1 20071026 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 604AA 27055 DFW - EMERGENCY LIGHT AT SEAT ROW 23 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 23. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007110800221 20071108 00221 NM 2007 11 8 AALA20072042 1 20071026 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 604AA 27055 DFW - EMERGENCY LIGHTS FROM SEAT ROW 15 TO AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT ROW 15 TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007110800222 20071108 00222 WP 2007 11 8 UPS07851072 1 20071010 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 INTERCOSTAL BETWEEN STA 1734-1746 LBL 36 IS BROKEN. REMOVED, FABRICATED, AND INSTALLED REPAIR INTERC OSTAL AT STA 1734- 1746 LBL 36 IAW DWG 5755032, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007110800230 20071108 00230 EU 2007 11 8 USAA920071017 1 20071017 A 5350 WEB AIRBUS 330 A330323 3930335 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274AY 342 BFM - MAJOR REPAIR - C2 CHECK - CRACK ON AFT BELLY FAIRING SUPPORT STRUCTURE WEB, BS 3990 / FR 53.2, +Y2820, WL -Z1650. REPAIRED AFT BELLY FAIRING SUPPORT STRUCTURE WEB, BS 3990 / FR 53.2, +Y2820, WL -Z1650 IAW A330 SRM 53-35-14. AIRCRAFT MANUFACTURER AND MODEL WAS CHANGED FROM BOEING 767201ER TO AIRBUS A330323. 2 L 7 2 4F RT A46NM 2007110800231 20071108 00231 EU 2007 11 8 USAA920071018 1 20071017 A 5350 WEB AIRBUS 330 A330323 3930335 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274AY 342 BFM - MAJOR REPAIR - C2 CHECK - CRACK ON AFT BELLY FAIRING SUPPORT STRUCTURE WEB, BS 3990 / FR 53.2, -Y2820, WL -Z1650. REPAIRED AFT BELLY FAIRING SUPPORT STRUCTURE WEB 3990 / FR 53.2, -Y2820, WL -Z1650 I/A/W A330 SRM 53-35-14 AND 51-44-11 . AIRCRAFT MANUFACTURER AND MODEL WAS CHANGED FROM BOEING 767201ER TO AIRBUS A330323. 2 L 7 2 4F RT A46NM 2007110800241 20071108 00241 NM 2007 11 8 ASAA0772174 1 20071018 A 5321 453A261014 FLOOR PANEL BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 AFT CARGO PIT CORROSION AROUND EDGES ON FLOOR PANEL NR 2 BETWEEN BS 727D AND BS 787. REPLACED WITH MADE REPAIR PARTS IA W B737 700 SRM 53-60-53 FIG 2 & 51-40-05. 2 L 7 2 4F RT A16WE 2007110800249 20071108 00249 NM 2007 11 8 ASAA0772182 1 20071019 A 5315 147A55067 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 AFT CABIN BS 986.5 FLOORBEAM UPPER CAP CORRODED AT RBL 28. REPLACED UPPER CAP IAW ERD 7360. 2 L 7 2 4F RT A16WE 2007110800272 20071108 00272 SO 2007 11 8 LR7A07118 1 20071001 A 5311 FRAME LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 2661 4763 DURING SCHEDULED C-7 CHECK PER JOB CARD HC5324 FOUND RIGHT MLG FRAME INNER CAP CRACKED AT FS 528 WL 232-240 RBL 66. REP AIR ACCOMPLISHED IAW LYNDEN AIR CARGO MEA 382-53-07-063. 2 H 7 4 4T A1SO 2007110800275 20071108 00275 NM 2007 11 8 NOCA16307 1 20071028 A 3620 WARNING SYSTEM BOEING 767 76736N 1385152 NM GE CF6 CF680 30025 NE COCKPIT ACTIVATED A NOCA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 15 768NA 29898 RIGHT ENG HPSOV EICAS MESSAGE. CREW FOLLOWED QRH AND TURNED OFF BLEED SWITCH. CREW STATED THAT THE RIGHT PACK WAS INOP AFTER TURNING BLEED SWITCH OFF. WITH BLEED ISSUE AND INOP PACK THE A/C CANNOT CONTINUE ETOPS A/C DIVERTING TO GANDER. SDR REMAINS OPEN. 2 L 7 2 4F 4 F RT A1NM E13NE 2007110800277 20071108 00277 NM 2007 11 8 CALA0700630 1 20071031 A 5311 6546595 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11612 27325 INSPECTION FOUND A .5 INCH CRACK AT FORWARD FASTENER HOLE OF FRAME BETWEEN STRINGER 8R AND 9R, STA 727-827. A DOUBLER A ND STRAP WERE INSTALLED IAW ECRA 5310-04668, REV B. 2 L 7 2 4F RT A16WE 2007110800278 20071108 00278 NM 2007 11 8 CALA0700631 1 20071101 A 5311 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND A .5 INCH CRACK IN MAIN FRAME AT STA 616 JUST BELOW CABIN FLOOR, S17L. THE FRAME WAS REPAIRED IAW ECRA 5311-01158. 2 L 7 2 4F RT A16WE 2007110800291 20071108 00291 NM 2007 11 8 SWAA075448 1 20071030 A 5330 6545804 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 277 AND BS 299, STR 22R AND STR 23R. REPAIRED SKIN P ER SWA EA. 2 L 7 2 4F RT A16WE 2007110800301 20071108 00301 NM 2007 11 8 SWAA075414 1 20071031 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110800304 20071108 00304 NM 2007 11 8 SWAA075417 1 20071031 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 469WN 33859 EEPLS LIGHT LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007110900005 20071109 00005 EU 2007 11 9 F3LA200700292 1 20071019 A 5321 FLOOR PANEL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 262FF CORRODED ON BOTTOM SIDE. REMOVED AND REPLACED FLOOR PANEL 262 FF IAW WORK CARD CP753-36 AND AMM 53-42-12-PB401. 2 L 7 2 4F RT A28NM 2007110900020 20071109 00020 NM 2007 11 9 QXEA200701637 1 20071030 A 2121 011749500 COOLING FAN BOMBDR DHC8 DHC8402 1390042 NM NR 1 FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 400QX 16650 4030 GEG - ON FLIGHT 2439, RECEIVED AVI FAN CAUTION MESSAGE. RETURNED AIRCRAFT TO FIELD. MAINTENANCE REMOVED AND REPLACED C OOLING FAN NR 1. OPERATION CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007110900022 20071109 00022 NM 2007 11 9 2007UALA04410 1 20071025 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 GALLEY EEL STRIP ADJACENT TO DOOR 1R INOPERATIVE. *S/D* RECONNECTED POWER CONNECTOR, OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110900023 20071109 00023 NM 2007 11 9 2007UALA04442 1 20071027 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN UNSECURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 654UA 25392 EMERGENCY FLOOR LIGHTING ON LEFT SIDE OF CABIN AFT OF ROW 15 COMES ON INTERMITTENTLY. SECURED, RESET CONNECTIONS ON EEL STRIP LEFT SIDE OF CABIN. OPS CHECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110900025 20071109 00025 NM 2007 11 9 2007UALA04454 1 20071030 A 5630 WINDOW BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU R4 DOOR CRACKED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 348UA 24252 CREW REPORTS R4 WINDOW MIDDLE PANE IS CRACKED. REPLACED R4 WINDOW. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110900027 20071109 00027 NM 2007 11 9 2007UALA04461 1 20071029 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 CORROSION FOUND AT STA 1380 TO STA 1400 AT STR 17R,CREASE BEAM IN MAIN CABIN. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110900028 20071109 00028 NM 2007 11 9 2007UALA04462 1 20071029 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 CORROSION FOUND AT STA 1420 TO STA 1440 AT CREASE BEAM IN MAIN CABIN. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110900030 20071109 00030 NM 2007 11 9 2007UALA04464 1 20071029 A 5315 141T510616 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 287 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 MAIN CABIN FLOORBEAM CORRODED AT OUTBOARD END BS 287 AT FWD LOWER CORNER OF R-1 DOOR CUTOUT. SUSPECT MOISTURE CONTAMINA TION. REMOVED DAMAGED SECTION OF CAP AND FABRICATED CAP SECTION, ANGLES AND STRAPS AND INSTALLED PER SRM 53-00-51. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110900032 20071109 00032 NM 2007 11 9 2007UALA04466 1 20071030 A 3350 1317 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 204UA 28713 EMERGENCY LIGHTS AT LT & RT SIDE BUSS CLASS AND COACH DIVIDER ARE OUT. RELAMPED EMERGENCY LIGHTS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007110900033 20071109 00033 NM 2007 11 9 2007UALA04468 1 20071030 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 204UA 28713 SEAT 1E FWD EEL INOP. REPLACED LIGHT ASSY AT 1E, OP CHECKS OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007110900039 20071109 00039 NM 2007 11 9 2007UALA04475 1 20071030 A 5210 DOOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE R1 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 181UA 25278 NR 1 LT & 1 RT PAX DOORS HAVE DAMAGE. REPAIRED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110900042 20071109 00042 NM 2007 11 9 2007UALA04480 1 20071030 A 2421 IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE MALFUNCTIONED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 595UA 28748 AT CRUISE, LEFT IDG DRIVE LT AND DRIVE MESSAGE, CREW ACCOMPLISHED LEFT IDG DISCONNECT PER AFM. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110900045 20071109 00045 NM 2007 11 9 2007UALA04487 1 20071030 A 3210 FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LT MLG CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 LEFT MLG OUTBOARD AFT SUPPORT FITTING CRACKED AT THE NR 2 HOLE, CRACK IS ADJACENT TO THE OUTBOARD SIDE OF NR 2 HOLE, CRA CK DOES NOT PASS THRU HOLE, AND THUS EXCEEDS LIMITS. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110900051 20071109 00051 NM 2007 11 9 2007UALA04495 1 20071030 A 3397 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 517UA 24861 L-1 DOOR EMERGENCY EXIT SIGN ABOVE DOOR INOP. RESEATED PINS IN CONNECTOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110900061 20071109 00061 NM 2007 11 9 2007UALA04502 1 20071031 A 5210 624EN338R SWITCH BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE L3 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 779UA 26941 DOOR 3L EPAS POWER SUPPLY FAILS TEST. FOUND DOOR OPEN SWITCH BAD (S52125). WILL ALSO NEED SLIDE ASSY REPLACED. REPLAC ED DOOR OPEN SWITCH AT 3L. OP CHECKED GOOD, NO FAULTS. SLIDE ASSY REPLACED. A/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007110900062 20071109 00062 NM 2007 11 9 2007UALA04505 1 20071031 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 517UA 24861 ROW 8AB AFT SEAT EEL INOPERATIVE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110900067 20071109 00067 NM 2007 11 9 2007UALA04513 1 20071101 A 5330 141W2313 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUSELAGE NICKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 795UA 43909 26927 NICK WAS FOUND ON OUTER SKIN OF LWR FUSELAGE CENTER LINE, STA 529, STR 46R. INSTALLED DOUBLER REPAIR OF SKIN DAMAGE. OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007110900073 20071109 00073 NM 2007 11 9 2007UALA04518 1 20071101 A 3350 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY LIGHT AT DOOR 2L BUSTLE INOP. REPLACED POWER SUPPLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110900088 20071109 00088 NM 2007 11 9 SWAA075428 1 20071031 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007110900100 20071109 00100 NM 2007 11 9 SWAA075441 1 20071030 A 5322 6546569 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 927, STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007110900104 20071109 00104 NM 2007 11 9 SWAA075443 1 20071030 A 2560 65C16820 HOOK BOEING 737 7377H4 1384404 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 713SW 27847 L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2007110900111 20071109 00111 EU 2007 11 9 UPS07151081 1 20071031 A 2120 UNKNOWN AIRBUS A300 A300F4622R 3930360 EU COCKPIT ODOR A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 146UP 0829 STRONG CLEANING SOLVENT TYPE ODOR DETECTABLE ONLY FROM COPILOT'S SIDE OF C/P IN AIR AND ON GROUND. NO ODOR DETECTED IN AVIONICS BAY. POTENTIAL HEALTH SIDE AFFECTS DUE TO EXPOSURE OF SAID UNKNOWN ODOR. UNLOADED AIRCRAFT. RAN PACKS AND EN GINES. INSPECTED ALL CARGO COMPARTMENTS AND AVIONICS BAY NO ODOR DETECTED AT THIS TIME. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2007110900114 20071109 00114 NM 2007 11 9 SB07095 1 20071031 A 2120 UNKNOWN BOEING 737 737401 1384701 NM CABIN ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 409US 23879 RIC FLT 1924 - EN ROUTE FROM CLT TO BWI, DURING CRUISE, THE AIRCRAFT DEVELOPED A SMELL IN THE CABIN. CABIN CREW MEMBERS AND A FEW PASSENGERS EXPERIENCED NAUSEA AND BECAME LIGHTHEADED. PARAMEDICS WERE CALLED OUT TO TREAT PASSENGERS AND CAB IN CREW. CREW DECLARED AN EMERGENCY AND DIVERTED TO RIC WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED CABIN AND CARGO BINS. NO SMELL NOTED. BOTH PACKS CHECK NORMAL. NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2007110900141 20071109 00141 EU 2007 11 9 AALA20072096 1 20071031 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14068 511 JFK - EMERGENCY LIGHTS AT LEFT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT MID CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007110900142 20071109 00142 WP 2007 11 9 AALA20072079 1 20071030 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 33502 49739 LGA - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 20DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 20D EF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110900143 20071109 00143 NM 2007 11 9 AALA20072083 1 20071030 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 194AA 32388 SFO - EMERGENCY LIGHTS AT SEAT ROWS 27 TO 36 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 27 TO 36. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007110900152 20071109 00152 NM 2007 11 9 AALA20072085 1 20071030 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 753AN 30261 DFW - EMERGENCY LIGHT AT OVERHEAD RIGHT NUMBER TWO DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD RIG HT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110900157 20071109 00157 NM 2007 11 9 AALA20072077 1 20071030 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 794AN 30256 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR AT PARTITION INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR AT PARTITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110900162 20071109 00162 NM 2007 11 9 AALA20072067 1 20071029 A 3350 WIRE HARNESS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 342AN 33081 SFO - EMERGENCY LIGHT AT FORWARD GALLEY INOPERATIVE. RECONNECTED WIRES AT LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007110900163 20071109 00163 NM 2007 11 9 AALA20072068 1 20071029 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 342AN 33081 SFO - EMERGENCY EXIT SIGN LIGHT AT RIGHT AFT DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN LIGHT AT R IGHT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007110900177 20071109 00177 NM 2007 11 9 CALA0700633 1 20071101 A 5315 7075T6100 FLOORBEAM BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33209 30581 INSPECTION FOUND FLOORBEAM CORRODED AT STA 360, LBL 9. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01505. 2 L 7 2 4F RT A16WE 2007110900181 20071109 00181 SO 2007 11 9 SIMA200730901 1 20071029 A 2150 81152915 SWITCH EMB 145 EMB145LR 3260212 SO NR 2 A/C PACK MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 626AE 145117 PACK 2 OVERLOAD OVERTEMP, CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. REMOVED AND REPLACED OVER TEMP SWITCH. AIRCRA FT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007110900186 20071109 00186 EU 2007 11 9 TRBA2007093 1 20071103 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS FAILED A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 322AC 320 CABIN EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY 62WL AND PERFORMED OP CK IAW JIC NR 33-50-00. 2 H 7 2 4T RT A53EU 2007110900187 20071109 00187 EU 2007 11 9 TRBA2007094 1 20071104 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS FAILED A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 414WF 414 CABIN DOOR EMERGENCY "EXIT" LIGHT SIGN INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AND PERFORMED OP CK IAW JIC NR 33-50-00. 2 H 7 2 4T RT A53EU 2007110900197 20071109 00197 EU 2007 11 9 1483401 1 20071101 A 3350 3011180A POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU EMERGENCY LIGHTS WEAK A HYIA K NONE L NO TEST IN INSP/MAINT 1 NE 01 14834 193 EMERGENCY AISLE PATH AND LOWER EXIT SIGNS FOR PASSENGER AND SERVICE DOORS ILLUMINATE DIMLY WHEN EMERGENCY EXIT LIGHTS AR E ARMED AISLE PATH LIGHTS ARE ON ONLY AFT OF ROW 10. MAINTENANCE REMOVED AND INSTALLED EMERGENCY LIGHTING POWER SUPPLY. OPERATIONALLY TESTED GOOD. 2 H 7 2 4T RT A53EU 2007110900206 20071109 00206 EA 2007 11 9 TRAX200701610 1 20071029 A 5512 TIP CAP CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 AAR - RIGHT HORIZONTAL STABILIZER TIP HAS CRACK ON LEADING EDGE TIP. 2 L 7 2 4F RT A21EA 2007110900208 20071109 00208 EU 2007 11 9 TRAX200701614 1 20071029 A 5714 STRUCTURE AEROSP ATR72 ATR72 EU WING BOX CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 WING BOX RIGHT FR 22 CRACKED. FABRICATION COVER ON W/C 2000-119 WING BOX R/H FR 28 ANGLE REPLACED IAW SRM 51-25-01REP AIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCOR DANCE WITH SRM 51-25-01. 2 H 7 2 4T RT 2007110900219 20071109 00219 SO 2007 11 9 RAIA00710030 1 20071024 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 813HK 145044 PRE FLT 5461 - CID - EMERGENCY LIGHT FLOOR PROXIMITY LIGHT INOP. MAINTENANCE DEFERRED PER MEL. 2 L 7 2 4T RT T00011AT 2007110900220 20071109 00220 EU 2007 11 9 TRAX200701619 1 20071029 A 5315 FLOORBEAM AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 FLOORBEAM 36 CORRODED. CORROSION REMOVED AS PER SRM 51-21-42 AND IT IS OUT OF LIMITS AS PER SRM 53-61-00. NEW BEAM SP LICED INSTALLED IAW SRM 51-25-01 AND 51-25-04 FABRICATION COVERED ON W/C 2000-199. MATERIAL THICKNESS: 0.063 MATERIAL RE MOVED: 0.047 OUT OF LIMITS AS PER SRM: 53-61-00 FIG 301. 2 H 7 2 4T RT 2007110900221 20071109 00221 EU 2007 11 9 TRAX200701625 1 20071029 A 5315 FLOORBEAM AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 LOWER FLOORBEAM AT FR 41, STR 17 RIGHT CORRODED. 2 H 7 2 4T RT 2007110900225 20071109 00225 EU 2007 11 9 TRAX200701633 1 20071029 A 5220 BRACKET AEROSP ATR72 ATR72 EU EMERGENCY EXIT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 ON RIGHT EMERGENCY EXIT INSIDE THE DOOR LWR AFT BRACKET FOUND CRACKED. INSTALLED NEW IAW SRM 51-25-01 AND SRM 51-25-04 FABREICATION COVER ON W/C 2000-88 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, AP PENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-24-01. 2 H 7 2 4T RT 2007110900227 20071109 00227 EU 2007 11 9 TRAX200701643 1 20071030 A 5210 SKIN AEROSP ATR72 ATR72 EU PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 ON INNER SKIN OF PAX DOOR LWR FWD CRACK FOUND. REPAIRED AS PER SRM 52-11-00 FIG 414. 2 H 7 2 4T RT 2007110900228 20071109 00228 EU 2007 11 9 TRAX200701644 1 20071030 A 5320 BRACKET AEROSP ATR72 ATR72 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 BRACKET CRACKED AT FR 39 STRINGER 13L. REPLACED IAW SRM 51-25-04. 2 H 7 2 4T RT 2007110900231 20071109 00231 EU 2007 11 9 F3LA200700310 1 20071015 A 5330 SKIN AIRBUS A319 A319112 3930323 EU FUSELAGE DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 1781 DURING C4/S1 CHECK, INSPECTION REPORTED A SMALL DENT IN THE LT FUSELAGE AT FR 15, STR30, AFT AND ABOVE 02 SERVICE DOOR. REMOVED PAINT FROM AREA IAW SRM 51-75-11 AND BLENDED AREA IAW SRM 51-73-00. DEPTH OF DENT IS .007, SIZE OF DENT IS .4" WIDE BY .5" LONG, 10" FROM CORNER OF DOOR CUTOUT AREA. PERFORMED HFEC ON BLENDED AREA IAW NTM 51-10-08, PART 6, NO CRA CKS NOTED. REMOVED TWO FASTENERS, AND PERFORMED ROTOPROBE TEST OF BOTH HOLES IAW NTM 51-10-01, PAGES 601-622, NO FAULTS FOUND. ACCOMPLISHED IAW EA A9-53R-12213. 2 L 7 2 4F RT A28NM 2007110900232 20071109 00232 NM 2007 11 9 QXEA200701651 1 20071103 A 5270 COMPUTER BOMBDR DHC8 DHC8402 1390042 NM DOOR SENSOR FAULTED A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 404QX 4046 SEA FLIGHT NR 2490: MASTER WARNING: MAIN AFT BAGGAGE DOOR INDICATES OPEN. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE FOUN D AFT BAGGAGE DOOR HANDLE SEATED, SECURED AND LOCKED ON RETURN TO GATE. FOUND 'ABDRLK' OPEN FAULT IN THE PROX SENSOR CO MPUTER. OPENED AND CLOSED DOOR NUMEROUS TIMES. DOOR ALWAYS INDICATES CLOSED AND LOCKED. PRESSURIZED AIRCRAFT. ALL DO ORS ALWAYS INDICATE CLOSED AND LOCKED. UNABLE TO INDUCE FAULT. ALWAYS CHECKED GOOD DURING TESTING. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007110900236 20071109 00236 EU 2007 11 9 TRBA2007095 1 20071102 A 5540 S55470003208 WEB AEROSP ATR72 ATR72212A 8680902 EU RUDDER BROKEN A TRBA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SO 29 541AT 541 VIBRATION FELT IN FLIGHT DURING CRUISE. DURING INSPECTION FOUND BROKEN WEB ON RUDDER ASSEMBLY. ALSO, THE RIB THAT IS C OVERED BY THIS WEB ITS DAMAGED AND DELAMINATED, REFERENCE IPC NR 55-91-40 FIG 15 ITEMS 40, 50 AND 60. WORK IN PROGRESS. 2 H 7 2 4T RT A53EU 2007110900241 20071109 00241 EU 2007 11 9 TRAX200701651 1 20071031 A 5714 ANGLE AEROSP ATR72 ATR72 EU RT WING BOX CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 RIGHT WING BOX FRAME 28A REPAIR ANGLE CRACKED. 2 H 7 2 4T RT 2007110900249 20071109 00249 NM 2007 11 9 SWAA075467 1 20071031 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900255 20071109 00255 NM 2007 11 9 SWAA075473 1 20071101 A 3350 8100022602 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 469WN 33859 EEPLS LIGHT ASSY LOOSE AT ROW 5 ABC. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007110900256 20071109 00256 NM 2007 11 9 SWAA075474 1 20071101 A 2560 65C16820 HOOK BOEING 737 7377H4 1384404 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 476WN 32475 L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2007110900266 20071109 00266 NM 2007 11 9 SWAA075478 1 20071101 A 5312 6545801 TEE FITTING BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED BRDG CHECK, FOUND BULKHEAD LOWER TEE CHORD CORRODED AT BS 227, LBL 10 TO RBL 10. REPAIRED CHORD PER SW A EA. 2 L 7 2 4F RT A16WE 2007110900283 20071109 00283 NM 2007 11 9 SWAA075465 1 20071031 A 5311 6546538 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900287 20071109 00287 EA 2007 11 9 A6WA200740586 1 20071014 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 469AW 7917 FOUND LT FS 621 FLOOR SUPPORT ANGLE CRACKED APPROX .75 INCH LONG. MAINTENANCE CUT AWAY DAMAGED SECTION OF ANGLE AND INS TALLED REPAIR ANGLE AND DOUBLER IAW BOMBARDIER REO 601R-53-61-117 REV C. (M) 2 L 7 2 4F RT A21EA 2007110900290 20071109 00290 NM 2007 11 9 SWAA075466 1 20071031 A 5311 6546593 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900291 20071109 00291 NM 2007 11 9 SWAA075463 1 20071031 A 5311 6546554 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900294 20071109 00294 NM 2007 11 9 SWAA075460 1 20071031 A 5311 6546529 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900295 20071109 00295 NM 2007 11 9 SWAA075459 1 20071031 A 5322 6545646 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007110900297 20071109 00297 NE 2007 11 9 SA07071 2 20071030 A 7200 ENGINE AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B4P NE NR 1 MALFUNCTIONED A USAA A UNSCHED LANDING E A VIBRATION/BUFFET FLAME/FIRE CL CLIMB 1 EA 19 738US 1254 575165 RIC FLT 1673 - EN ROUTE RIC TO CLT. AT APPROXIMATELY FL190, THE FLIGHT EXPERIENCED EXTREME VIBRATION COMING FROM THE NU MBER ONE ENGINE. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. UPON REACHING THE GATE, IT WAS REPO RTED THAT PASSENGERS AND CABIN CREW NOTICED FLAMES COMING FROM THE REAR OF THE ENGINE. MAINTENANCE ACTION PENDING (OPEN ). 2 L 7 2 4F 4 F RT A28NM E38NE 2007110900298 20071109 00298 EU 2007 11 9 USAA920071066 1 20071016 A 5347 D53371110010 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON MAIN CABIN SEAT TRACK, BS 1810 / FR 41 - BS 2136 / FR 47, -Y765. REPLACED MAIN CABIN SEAT TRACK, BS 1810 / FR 41 - BS 2136 / FR 47, -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007110900300 20071109 00300 NM 2007 11 9 USAA920071068 1 20071018 A 5330 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, CRACKED FUSELAGE SKIN, BS 294.5, S13L AT LOWER DOOR HINGE CUTOUT. REPAIRED CRACKED FUSE LAGE SKIN, BS 294.5, S13L AT LOWER DOOR HINGE CUTOUT IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007110900301 20071109 00301 EU 2007 11 9 NWAA073653220 1 20071103 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320211 3930320 EU EMERGENCY LIGHT MALFUNCTIONED A NWAA O OTHER O OTHER CL CLIMB 1 GL 01 320US 213 AFTER TAKEOFF, FORWARD 2 EXIT LIGHTS AND AISLE EMERGENCY LIGHTS IN FIRST CLASS AND FIRST 3 ROWS OF CABIN WERE FLASHING, THEN ON STEADY. CYCLED COCKPIT EMERGENCY LIGHT SWITCH OFF, THEN TO ARM BUT NO HELP. LIGHTS EXTINGUISHED 20 MINUTES LAT ER. REPLACED FORWARD (10WL) EPSU, TESTS OK. 2 L 7 2 4F RT A28NM 2007110900304 20071109 00304 NM 2007 11 9 QXEA200701640 1 20071101 A 2820 AV24B1319D3 VALVE DHAV DHC8 DHC8202 2809007 NM FUEL/DEFUEL LEAKING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 580 484 SEA - FUEL LEAKING FROM THE NR 2 AFT NACELLE AREA. MAINTENANCE REPLACED THE FUEL TUBE AND THE MASTER REFUEL/DEFUEL VALV E. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007110900305 20071109 00305 NM 2007 11 9 ASAA0742190 1 20071002 A 5320 654587545 ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 MAIN CABIN CUSP WEB ANGLE AT BOTTOM OF RI DOOR CUTOUT STA 277 318 HAS CORROSION. REMOVED AND REPLACED CUSP WEB ANGLE IA W 737 400 SRM 51-40-2, 51-40-5 AND 53-10-15 FIG 101 SHT 13. 2 L 7 2 4F RT A16WE 2007110900306 20071109 00306 EA 2007 11 9 QXEA200701641 1 20071102 A 2730 ELEVATOR CNDAIR CL600 CL6002C10 1390015 EA NONE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 607QX 10024 SEA - ELEVATOR CONTROL HAS A FLAT FEEL. THE CONTROLS MOVE BACK AND FORTH A COUPLE OF INCHES WITH NO ELEVATOR MOVEMENT. AIRCRAFT FERRIED TO PORTLAND FOR REPAIRS. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE ELEVATOR CONTROL SYSTEM IAW AMM TASK 27-31-00-710-801-A01. OPERATIONAL CHECKS GOOD WITH NO DEFECTS NOTED. PERFORMED MOVEMENT CHECK WITH AC AND ELE CTRIC HYDRAULIC PUMPS ACTIVE WITH NO DEFECTS NOTED. PERFORMED GENERAL VISUAL INSPECTION OF THE CONTROL QUADRANTS WITH N O DEFECTS NOTED. COULD NOT DUPLICATE ORIGINAL DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007110900307 20071109 00307 EA 2007 11 9 QXEA200701642 1 20071103 A 3241 6007302 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA ANTI SKID SYS MALFUNCTIONED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 615QX 14559 10065 PDX - ON TAXI THE ANTI-SKID RELEASES AND GRABS WHEN SLOWING THROUGH ABOUT 10 KNOTS. THE TRANSITION IS NOT SMOOTH. MAIN TENANCE FOUND A MDC FAULT FOR THE ANTI-SKID CONTROL UNIT. REPLACED THE ANTI SKID CONTROL UNIT. OPERATIONAL CHECKS GOOD . AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007110900308 20071109 00308 NM 2007 11 9 ASAA0742191 1 20071005 A 5320 65458078 INTERCOSTAL BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 MAIN CABIN AT FWD SERVICE DOOR CUTOUT BS 277 BETWEEN STG 14R HAS CRACK AT FWD END OF INTERCOSTAL. REMOVED AND REPLACED INTERCOSTAL IAW BAC 737 400 SRM 51-40-2. 2 L 7 2 4F RT A16WE 2007110900309 20071109 00309 NM 2007 11 9 ASAA0742192 1 20071102 A 5320 WEB BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 MAIN CABIN CUSP WEB STA 355 RBL 58 HAS ELONGATED 1 4 INCH HOLE. REMOVED WEB IAW 737 SRM 51-40-2 OBTAINED NEW WEB P/N 65 45875 62 P/O 0740866 DRILLED AND INSTALLED PER BAC DRAWING 65 45875 2 L 7 2 4F RT A16WE 2007110900310 20071109 00310 2007 11 9 QXEA200701644 4 20071104 A 3444 6222855011 ALTIMETER CNDAIR CL600 CL6002C10 1390015 EA MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 605QX 10352 10022 SEA - FLIGHT 2503. ON TAXI RECEIVED A GLD UNSAFE MESSAGE. RETURNED TO THE GATE. MAINTENANCE PLACED THE RADIO ALTIMETER SYSTEM ON MEL 34-41-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE REPLACED THE CAPTAIN'S RADIO ALTIMETER R/T. OPERATI ONAL CHECKS GOOD. MEL CLEARED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007110900312 20071109 00312 EU 2007 11 9 07FDEA04718 1 20071105 A 5720 A57111092202 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 729FD 657 FOUND ON LOWER JUNCTION FITTING LT CENTER TANK, INTERNAL, SEVERAL HOLES WITH CRACK FINDINGS. REPAIR PERFORMED BY REAM UP UNTIL DAMAGE REMOVAL IAW EA 6-5710-114908 AND RAS/054537/070/2007 ISS A. 2 L 7 2 4F RT A35EU 2007110900313 20071109 00313 EU 2007 11 9 07FDEA04719 1 20071105 A 5730 A57340087 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 729FD 657 FOUND ON RT WING BOTTOM SKIN AND PYLON SUPPORT BRACKET ELONGATED HOLES AT HYDRAULIC FITTINGS REPAIR PERFORMED BY OVERSIZ ING THE HOLES, INSTALLING FREEZE PLUGS IAW DRAWING R 571-50532, APPROVED BY EA 6-2900-114891 AND RAS/BAE/1005593/2007 IS S A. 2 L 7 2 4F RT A35EU 2007110900315 20071109 00315 NM 2007 11 9 QXEA200701650 1 20071105 A 6120 PUSHROD DHAV DHC8 DHC8202 2809007 NM PCU OUT OF ADJUST A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 369PH 513 PDX FLIGHT NR 2169, DURING TAXI WITH THE POWER LEVERS AT FLIGHT IDLE NR 2 PROPELLER GROUND RANGE LIGHT REMAINED ILLUMINA TED. PERFORMED INITIAL POSITION CHECK OF THE POWER LEVER CONTROL SYSTEM AND FOUND PCU POWER LEVER PIN SLOT (K) DID NOT LINE UP. ADJUSTED PCU PUSHROD END AND REINSPECTED ENGINE POWER AND CONDITION CONTROL RIGGING. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007110900317 20071109 00317 NE 2007 11 9 QXEA200701649 2 20071104 A 7230 VALVE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE P2.5 SMOKE A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 09 348PH 484 SEA FLIGHT NR 2106, DURING DESCENT WITH POWER LEVERS NEAR FLIGHT IDLE, FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. SH ORTLY AFTER SMOKE CAME INTO COCKPIT AND LAV SMOKE DETECTOR ALARM CAME ON. PER CHECKLIST TURNED OFF BLEED 1. SHORTLY TH ERE AFTER SMOKE CEASED, REPLACED P2.5/P3 VALVE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007110900318 20071109 00318 NM 2007 11 9 QXEA200701646 1 20071102 A 3600 WARNING SYSTEM DHAV DHC8 DHC8202 2809007 NM NR 1 BLEED FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 345PH 476 PDX FLIGHT NR 2058 - DURING CLIMB-OUT, NR 1 BLEED HOT CAUTION MESSAGE. PER CHECKLIST TURNED BLEED SELECTOR TO MIN LIGHT STOPPED CYCLING. PERFORMED BLEED AIR FUNCTIONAL TEST COULD NOT DU0PLICATE PROBLEM REPLACED NR 1 BLEED AIR OVERTEMP SWI TCH AS A PRECAUTIONARY MEASURE. GROUND RAN AIRCRAFT AND PERFORMED BLEED AIR FUNCTION TEST. AIRCRAFT OK FOR CONTINUED S ERVICE. 2 H 7 2 4T RT A13NM 2007110900319 20071109 00319 NM 2007 11 9 QXEA200701647 1 20071103 A 7500 7788683 SHUTOFF VALVE DHAV DHC8 DHC8202 2809007 NM NR 1 ENGINE MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 345PH 7230 476 SEA FLIGHT NR 2152 DURING CLIMB THROUGH 17,000, NR 1 BLEED HOT CAUTION LIGHT ILLUMINATED. CYCLING ON AND OFF. CAUTION LIGHT EXTINGUISHED AFTER SELECTING FLOW SELECTOR KNOB. PERFORMED BLEED AIR FUNCTION TEST. FOUND NR 1 ENGINE SLOW TO SW ITCH FROM LP AIR TO HP AIR. REPLACED HIGH PRESSURE NR 1 SWITCH. REPLACED NR 2 HIGH PRESSURE SWITCH. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007110900320 20071109 00320 NM 2007 11 9 QXEA200701648 1 20071103 A 7500 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007 NM NR 1 BLEED MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 367PH 511 SEA FLIGHT NR 2104, AFTER ENGINE START NOTICED LOW FLOW OUT OF NR 1 BLEED, ISOLATED BOOT SYSTEM AND NOTED NR 1 DEICE PRE SSURE AT 10 PSI WHILE NR 2 WAS 18 PSI WITH ENGINES OUT OF FEATHER AND POWER LEVERS JUST ABOVE DISC. MAINTENANCE REPLACE D NR 1 AND NR 2 55 AND 65 HIGH PRESSURE SWITCHES. REPLACED 2121-K6 RELAY, DURING TROUBLESHOOTING WIRING. OPERATIONAL C HECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007110900321 20071109 00321 NM 2007 11 9 HALA0700461 1 20071031 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 955-958 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 LEVEL 2 CORROSION SEAT TRACK AT LBL88.5 STATION 955-958 CORROSION BLEND OUT BEYOND SRM LIMITS. REMOVED DAMAGED SEAT TRA CK IAW SRM 53-00-52 FIG 201 REPAIR 3 FROM STATION 922-989. 2 L 7 2 4F RT A1NM 2007110900323 20071109 00323 2007 11 9 HALA0700460 4 20071102 A 3460 4052506955 FMC BOEING 767 7673G5 1385126 NM MALFUNCTIONED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM: DUAL FMS FAILURE AUTO PILOT AND AUTOTHROTTLE FAIL EICAS MESSAGE AFTER 10 MINUTES FMS'S RESPOND ED TO PROGRAMMING. CHECK EQUIPMENT COOLING IN COCKPIT AND E/E, TESTED BOTH FMC'S ALL CHECK GOOD PER AMM 34-61-00. ALL FMC DATA WAS CORRECT. ALSO, REMOVED AND REPLACED LEFT AND RIGHT FLT MANAGEMENT COMPUTERS PER AMM 34-61-01-424-005 AND C ROSS LOADED PER AMM 34-61-00-422-053-001 FMC CHECKS GOOD. 2 L 7 2 4F RT A1NM 2007110900326 20071109 00326 EU 2007 11 9 NWAA073663302 1 20071026 A 5712 RIB AIRBUS 330 A330323 3930335 EU LT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 802NW 0533 DURING LINE CHECK WHILE PERFORMING INSPECTION PER AD 2006-22-14, FOUND CRACK IN LT WING RIB 6. REPAIRED PER EA 33-21114 4. 2 L 7 2 4F RT A46NM 2007110900328 20071109 00328 EA 2007 11 9 QXEA200701643 1 20071104 A 2150 GG670950095 ACM CNDAIR CL600 CL6002C10 1390015 EA RIGHT SMOKE A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 606QX 5870 1425 10023 SMF - FLIGHT 2576, AT THE GATE DURING ENGINE START, RECEIVED SMOKE IN THE CABIN AND A RIGHT AC PACK FAIL MESSAGE. REMOV ED THE PASSENGERS FROM THE PLANE WITHOUT INCIDENT. MAINTENANCE PLACED THE RIGHT PACK ON MEL 21-51-1B. AIRCRAFT RETURNE D TO SERVICE. MAINTENANCE REPLACED THE RIGHT AIR CYCLE MACHINE AND THE RIGHT PACK DISCHARGE SENSOR. OPERATIONAL AND LE AK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007110900329 20071109 00329 NM 2007 11 9 EIA2007191 1 20071029 A 5330 SKIN BOEING 747 747212B 1384886 NM BS 1320 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 EXTERNAL SKIN AT BS 1320 HAS ELONGATED FASTENER HOLES JUST 4" AFT OF R3 DOOR CUT-OUT. REPAIRED EXTERNAL SKIN AT BS 1324 FASTENER HOLE AFT OF R3 DOOR CUT-OUT PER ECRA 482-53-220-2. 2 L 7 4 4F A20WE 2007110900334 20071109 00334 EU 2007 11 9 TRAX200701659 1 20071101 A 5313 STRINGER AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 FOUND STRINGER 12R BTW FR 36-38 CORRODED. REPAIRED AS PER SRM 53-00-00 FIG 426. 2 H 7 2 4T RT A53EU 2007110900338 20071109 00338 EA 2007 11 9 TRAX200701663 1 20071101 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 PAX DOOR AFT DRAG ANGLE HAS A SUSPECTED CRACK (AS MARKED). PERFORMED LPI PER NDTM 51-20-08 OF SUSPECTED CRACKED AREA ON PAX DOOR AFT DRAG ANGLE (DEFECTS NOTED), FOUND REPAIRABLE PER REO 601R-52-11-513, REMOVED CRACKED SECTION IAW REO 601R- 52-11-513. PERFORMED LPI PER NDTM 51-20-08 & CUTOUT EDGES TO ENSURE CRACK FREE IAW REO 601R-52-11-513 (NO DEFECTS NOTED) . FABRICATED SECTION & DOUBLERS USING ATTACH ANGLE IAW REO 601R-52-11-513. OK TO INSTALL ATTACH ANGLE & DOUBLERS. INST ALLED ATTACH ANGLE & DOUBLERS. IAW REO 601R-52-11-513. OK TO FILLET SEAL & TOPCOAT REPAIRED AREA & FASTENERS. FILLET SE ALED & TOPCOATED REPAIRED AREA IAW BOMBARDIER REO 601R-52-11-513. 2 L 7 2 4F RT A21EA 2007110900339 20071109 00339 EA 2007 11 9 TRAX200701664 1 20071101 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 PAX DOOR OUTER HANDLE CRACKED. REMOVED HARDWARE FROM OUTER HANDLE IAW CRJ 200 AMM 52-11-03. 14212. OK TO INSTALL NEW HANDLE. COMPLIED WITH PAX DOOR OUTER HANDLE INSTALLATION IAW CRJ AMM 52-11-03. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007112100012 20071121 00012 NM 2007 11 21 CALA0700677 1 20071112 A 5311 65C27494 SKIN BOEING 737 737524 1384721 NM HORIZONTAL STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 52616 27329 INSPECTION FOUND A .5 INCH CRACK IN RT HORIZONTAL STABILIZER SKIN FROM STAB STA 97-126. A PERMANENT REPAIR WAS PERFORME D BY INSTALLING A DOUBLER IAW ECRA 5510-01724, REV A. 2 L 7 2 4F RT A16WE 2007110900340 20071109 00340 EA 2007 11 9 TRAX200701666 1 20071101 A 5220 HANDLE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT OBSTRUCTED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 LT OVERWING EMERGENCY EXIT PULL HANDLE HARD TO PULL, HAS INSULATION WEDGED BELOW OUTER PUSH PLATE. 2 L 7 2 4F RT A21EA 2007110900344 20071109 00344 EU 2007 11 9 TRAX200701670 1 20071102 A 5330 LAP JOINT AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 CORROSION FOUND ON FUSELAGE SKIN LAP JOINT BTW FR 23A-23C STR 11L. REMOVED AS PER SRM 51-21-42, SKIN REPAIRED IAW SRM 53-00-00 FIG 424 MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.012 OUT OF LIMITS AS PER SRM: 53-31-00 FIG 301. 2 H 7 2 4T RT A53EU 2007110900346 20071109 00346 EA 2007 11 9 TRAX200701673 1 20071102 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS WARNING LIGHT A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 900EV 7608 OBSERVED FLAPS FAIL MSG ON APPROACH WHEN FLAP HANDLE AT 8*, EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007110900347 20071109 00347 EU 2007 11 9 TRAX200701674 1 20071102 A 3350 LIGHT AEROSP ATR72 ATR72212 8680945 EU CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 FLT 4508 - EMERGENCY LIGHT ON CABIN DOOR NOT WORKING. DEL 225 MINS. 2 H 7 2 4T RT A53EU 2007110900349 20071109 00349 EA 2007 11 9 TRAX200701676 1 20071102 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 937EV 8042 LT OVERWING FWD EMERGENCY LIGHT BULB BURNED OUT. 2 L 7 2 4F RT A21EA 2007110900350 20071109 00350 NM 2007 11 9 HNAA0700259 1 20071101 A 3350 6013211X POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN FAULTY A HNAA K NONE J WARNING INDICATION CR CRUISE 1 EA 07 810EX 38740 4686 308 FLOOR LEVEL EMERGENCY LIGHTS FLICKERED IN FLIGHT. CHECKED THE BRUSH BLOCK WIRES FROM THE BRUSH BLOCK TO RELAY PANEL, NO DEFECTS NOTED. INSPECTED BOTH AC CONTACTOR BOXES, NO DEFECTS NOTED. REMOVED AND REPLACED THE EMERGENCY BATTERY POWER SUPPLY. 2 H 7 2 4T RT A13NM 2007110900352 20071109 00352 SO 2007 11 9 C2XA07SH091 1 20071104 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 125 SHV - DURING C-CHECK CENTER OMEGA BEAM FR 17-23 HAS CORROSION BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED CENTER OM EGA BEAM AT FR 18-23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007110900354 20071109 00354 NM 2007 11 9 BB07085 1 20071102 A 3232 273N10011 ACTUATOR BOEING 757 7572B7 1384964 NM NLG DOOR FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 206UW 27808 FERRY FLIGHT 9243, MCN-PHL: AFTER TAKEOFF, CREW RECEIVED EICAS MESSAGE GEAR DISAGREE AND GEAR DOORS. RETURNED TO MCN. MAINTENANCE REPLACED THE NLG DOOR ACTUATOR. NO FURTHER FAULTS. 2 L 7 2 4F RT A2NM 2007110900355 20071109 00355 SO 2007 11 9 C2XA07CL093 1 20071103 A 3230 23092900401 UPLOCK EMB 145 EMB145LR 3260212 SO RT MLG FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 17984 145246 CLE FLIGHT 2251 THE CREW REPORTED A LANDING GEAR LEVER DISAGREE WARNING IN FLIGHT. THE AIRCRAFT DIVERTED TO CLEVELAND A ND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT LANDING GEAR UPLOCK BOX. OPERATIONAL CHECKS W ERE GOOD. 2 L 7 2 4T RT T00011AT 2007110900359 20071109 00359 EU 2007 11 9 YENA2007093 1 20071104 A 3350 Z020H0001112 CONTROL PANEL AIRBUS 320 A320232 3930326 EU CABIN MALFUNCTIONED A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 661JB 247 3228 OPS TEST OF EMERGENCY LIGHTS BY TEST BUTTON ON PROGRAM & TEST PANEL INOP. REMOVED & REPLACED PROGRAMMING & TEST PANEL I AW AMM 23-73-18-04, OPS TEST NORMAL, OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2007110900362 20071109 00362 WP 2007 11 9 ASAA0782193 1 20071104 A 5330 59360213 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 977AS 53453 RIGHT EXTERNAL FUSELAGE SKIN DENTED 27 INCHES BELOW PYLON STA 1308 DENT MEASURES .700 DIA DEPTH .032 RATIO OF 21.8 COLD WORKED DENT IAW MD80 SRM 53-04 FIG 38. EDDY CURRENT INSPECTED COLD WORKED AREA NO CRACKS NOTED IAW MD80 NTSPM 06 10 00. 001 PROCEDURE 1. FABRICATED INTERNAL DOUBLER COATED DRILLED AND INSTALLED IAW MD80 SRM FIG 38. 53-04. 2 L 7 2 4F RT A6WE 2007110900363 20071109 00363 EU 2007 11 9 200711051 1 20071102 A 2752 C1548122 ACTUATOR EMB ERJ170 ERJ170100SE 3260406 EU T/E FLAP DEFECTIVE A UHLA O OTHER J WARNING INDICATION DE DESCENT 1 GL 11 638RW 17000053 FLIGHT 7582 ORD TO YUL ON APPROACH WHEN SELECTING FLAPS 2 CREW RECEIVED FLAP FAIL AMBER EICAS MESSAGE. LANDED WITHOUT I NCIDENT. MAINTENANCE REMOVED AND REPLACED LEFT NR 3 FLAP ACTUATOR. 2 L 7 2 4F RT A56NM 2007110900366 20071109 00366 NM 2007 11 9 USAA920070984 1 20071022 A 5320 146N51905 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN INTERCOSTAL WEB, BS 1661 - BS 1681, RBL 9.2, WL 208. REPLACE D CABIN INTERCOSTAL WEB, BS 1661 - BS 1681, RBL 9.2, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007110900367 20071109 00367 NM 2007 11 9 USAA920070985 1 20071024 A 5320 141N5160207 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN INTERCOSTAL FILLER, BS 295 - BS 310.5, RBL 2, WL 208. REPLAC ED CABIN INTERCOSTAL FILLER, BS 295 - BS 310.5, RBL 2, WL 208 IAW BOEING DRAWING 141N5160. 2 L 7 2 4F RT A2NM 2007110900065 20071109 00065 NM 2007 11 9 2007UALA04511 1 20071031 A 5730 113T161330 PANEL BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE LT WING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 673UA 29241 FOUND ON ARRIVAL 5 BY 7 INCH SECTION OF PANEL 551VB MISSING LOWER LEFT WING JUST INBOARD OF LEFT MLG. SUSPECT FATIGUE F ROM NORMAL AC OPERATION. FABRICATED ALUMINUM DOUBLER .040 THICK AND INSTALLED. NEED NEW 551VB PANEL MF1544 CREATED TO MONITOR UNTIL PANEL IS REPLACED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110900086 20071109 00086 NM 2007 11 9 SWAA075429 1 20071031 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007110900103 20071109 00103 NM 2007 11 9 SWAA075442 1 20071031 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 710SW 27844 DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS INOP AT ROW 10 DEF. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007110900124 20071109 00124 WP 2007 11 9 AALA20072081 1 20071030 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 931TW 49527 SFO - EMERGENCY LIGHT AT SEAT 16D INOPERATIVE. RESET CONNECTOR FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007110900125 20071109 00125 NM 2007 11 9 AALA20072095 1 20071031 A 7720 PROBE BOEING 737 737823 13844BZ NM RT ENGINE INOPERATIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 917AN 29518 MIA INFLIGHT T651/31OCT - NUMBER TWO ENGINE INDICATED HIGH ENGINE GAS TEMPERATURE ON TAKEOFF. RETURNED TO MIA AND LANDE D WITHOUT INCIDENT. REPLACED TOP LEFT T49.5 PROBE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007110900131 20071109 00131 EU 2007 11 9 AALA20072097 1 20071031 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14068 511 JFK - EMERGENCY LIGHTS AT RIGHT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007110900140 20071109 00140 NM 2007 11 9 AALA20072092 1 20071031 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 26C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110900144 20071109 00144 NM 2007 11 9 AALA20072086 1 20071030 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 753AN 30261 DFW - EMERGENCY LIGHT AT SEAT 30C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 30C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110900147 20071109 00147 EA 2007 11 9 AALA20072101 1 20071031 A 3350 LAMP WACO YK YKC 9600816 EA EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14058 3974 JFK - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 1 Q 7 1 3R A533 2007110900153 20071109 00153 NM 2007 11 9 AALA20072072 1 20071030 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 761AJ 31478 JFK - EMERGENCY LIGHT AT SEAT 31G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 31G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110900155 20071109 00155 NM 2007 11 9 AALA20072074 1 20071030 A 3350 OL3071BPEGPL LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 761AJ 31478 JFK - FOUND EMERGENCY LIGHT AT FORWARD SEAT 4D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT FORWARD SEAT 4D. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007110900168 20071109 00168 NM 2007 11 9 EIA2007190 1 20071029 A 3350 S1356B32 LIGHT BOEING 747 747200F 1384866 NM PWA JT9 JT9D7J 52054 NE CABIN BURNED OUT A EIAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 09 485EV "MAIN DECK FWD RT CEILING EMERGENCY LIGHT INOP. REPLACED EE LIGHT ASSY ZONE A AND B". 2 L 7 4 4F 4 F RT A20WE E20EA 2007110900169 20071109 00169 NM 2007 11 9 EIA2007189 1 20071021 A 3040 CONTROLLER BOEING 747 7474J6 NM R1 WINDOW MALFUNCTIONED A EIAA J A DUMP FUEL UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 NM 09 747BC 25879 ON CLIMB AT 240 WIINDOW R1 ARCING WITH APPROX 3 FOOT CRACK ON OUTER PANE. REMOVED AND REPLACED R1 FWD WINDSHIELD HEAT C ONTROL UNIT PER MM 30-41-01 AND R1 WINDSHIELD PER MM 56-11-01 WINDOW HEAT SYSTEM. OPS CHECKED GOOD PER MM 30-41-01. (GO OD MODEL) 2 L 7 4 4F RT A20WE 2007110900170 20071109 00170 SO 2007 11 9 SIMA200730402 1 20071030 A 7500 O-RING EMB 145 EMB145LR 3260212 SO NR 1 BLEED LEAKING A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 614AE 145086 DURING CLIMB-OUT, NR 1 BLEED LEAK INDICATION EXTINGUISHED ONCE BLEED VALVE WAS CLOSED RETURNED TO DFW. REMOVED AND REPL ACED BLEED LINE O-RING AT JOINTS 7, 9, 11, 17 AND JOINT ABOVE 17 FOR NR 1 BLEED IAW EMB-145-AMM 36-11-10, LEAK CHECK GOO D AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007110900171 20071109 00171 SO 2007 11 9 SIMA200730401 1 20071029 A 2150 A/C PACK EMB 145 EMB145LR 3260212 SO NR 2 OVERHEATED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 626AE 145117 ABORTED TAKEOFF FOR PACK 2 OVER LOAD OVER TEMP, ISSUED MEL 21-27. 2 L 7 2 4T RT T00011AT 2007110900178 20071109 00178 2007 11 9 SIMA200730903 4 20071031 A 3418 0861DT5 PROBE EMB 135 EMB135KL 3260302 SO AOA MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 829AE 145609 CREW REPORTED ON TAKE OFF ROLL AT APPROX 10 KIAS, "SPS ADVANCE" MESSAGE ILLUMINATED ON EICAS. CREW ELECTED TO ABORT TAK EOFF AND RETURN TO THE GATE. AIRCRAFT RETURNED TO THE GATE SAFELY FOR MAINTENANCE. REMOVED AND REPLACED NUMBER 2 AOA I AW EMB140 MM 27-36-01. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007110900193 20071109 00193 EU 2007 11 9 F3LA200700306 1 20071017 A 5320 SILL AIRBUS A319 A319112 3930323 EU R2 DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION IN R2 DOOR SILL NUTPLATE HOLE AT FR 66. BLENDED MATERIAL AT FWD END O F R2 DOOR SILL AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14, FIG. 101. FABRICATED REPAIR FILLER IAW SRM 53-41-14, FIG . 201, REPAIR PRINCIPLE NR 6 (SHEET 4). FABRICATED REPAIR ANGLES IAW SRM 53-41-14, PAGES 215/216, AND SRM 53-41-14, PAG E 217, FIG 201. REPAIR COMPLETED IAW SRM 53-41-14, FIG. 201, REPAIR PRINCIPAL NR 6 (SHEETS 1 AND 4). 2 L 7 2 4F RT A28NM 2007110900201 20071109 00201 NM 2007 11 9 CALA0700640 1 20071101 A 5315 BAC1505100703 FLOORBEAM BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33209 30581 INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, RBL 16. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01507. 2 L 7 2 4F RT A16WE 2007110900218 20071109 00218 SO 2007 11 9 RAIA00710032 1 20071026 A 3610 CLAMP EMB 145 EMB145LR 3260212 SO BLEED AIR SYS LOOSE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 816HK 145055 FLT 5492 - IAD - E1 BLEED LEAK MESSAGE. MAINTENANCE SECURED LOOSE CLAMP ON BLEED DUCT LINE IN AFT ELECTRONICS BAY AND O PS CHECK GOOD ON GROUND. 2 L 7 2 4T RT T00011AT 2007110900234 20071109 00234 EA 2007 11 9 TRAX200701646 1 20071030 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN DISCHARGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 751EV 10163 FWD F/A FLASHLIGHT WEAK. 2 L 7 2 4F RT A21EA 2007110900238 20071109 00238 SO 2007 11 9 CHQA200700068 1 20071102 A 2752 3635001003 BRAKE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL FLAP XMSN FAULTED A CHQA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 11 297SK 1065 145522 CAE311245 STL TO DSM - DURING CLIMB-OUT OF STL, FLIGHT CREW RECEIVED FLAP FAIL EICAS MESSAGE. CAPTAIN RAN QRH AND IT WAS DECIDED TO RETURN TO STL. THE AIRCRAFT LANDED WITHOUT INCIDENT IN STL AND WAS TURNED OVER TO MAINTENANCE. MAINTENANCE CHECKED THE CMC MESSAGES AND FOUND A CMC MESSAGE FOR FLAP JAMMING. THE FAULT WAS TRACED TO THE RT FLAP TRANSMISSION BRAKE AND T HE TRANSMISSION BRAKE WAS REPLACED. THE FLAPS WERE RIGGED AFTER REPLACEMENT OF THE TRANSMISSION BRAKE AND THE FLAP SYST EM CHECKED GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007110900243 20071109 00243 EA 2007 11 9 TRAX200701655 1 20071101 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR JAMMED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 PASSENGER DOOR HANDLE WILL NOT STOW FROM INSIDE. ALSO PASSENGER DOOR WILL NOT OPEN FROM INSIDE. DOOR IS JAMMED CLOSED. FLT 4705 DEL 38 MINS. 2 L 7 2 4F RT A21EA 2007110900246 20071109 00246 NM 2007 11 9 SWAA075470 1 20071101 A 5512 65C25727 SKIN BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED C3 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 132. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007110900247 20071109 00247 WP 2007 11 9 N921RM81664 1 20071026 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 1400 CRACKED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 921R 69652 46145 "D" PIT DOOR DAMAGED FORWARD UPPER SKIN AT CORNER. APPROX .375 INCH CRACK RADIATED FROM EDGE OF FUSELAGE SKIN IN DOOR R ADIUS AND TERMINATED AT FIRST FASTENER. 2 L 7 4 4F 4A25 2007110900253 20071109 00253 NM 2007 11 9 SWAA075471 1 20071101 A 5755 654645258 SPOILER BOEING 737 7373H4 1384600 NM NR 4 SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED CABIN VISIT CHECK, FOUND LT WING NR 4 GROUND SPOILER OUTBOARD HINGE CRACKED. REMOVED AND REPLACED SPOI LER PER MM. 2 L 7 2 4F RT A16WE 2007110900263 20071109 00263 NM 2007 11 9 SWAA075476 1 20071101 A 5752 6546455 TAB BOEING 737 7373H4 1384600 NM LT AILERON DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED BRDG CHECK, FOUND LT WING AILERON TAB DELAMINATED. REPAIRED TAB PER SRM. 2 L 7 2 4F RT A16WE 2007110900280 20071109 00280 EA 2007 11 9 A6WA200740582 1 20071013 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 469AW 7917 FOUND RIGHT SIDE FS 621 TO FS 625.30 INTERCOSTAL AT STRINGER 14R IS CRACKED NEAR RADIUS APPROX 1 INCH LONG. MAINTENANCE REMOVED RT INTERCOSTAL FS 621 TO 625.30 IAW CRJ 200 SRM 51-42-06. INSTALLED NEW INTERCOSTAL P/N 601-35012-52 IAW CRJ 20 0 SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007110900281 20071109 00281 NM 2007 11 9 SWAA075479 1 20071101 A 5330 6545777 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT UPPER AFT CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007110900289 20071109 00289 NM 2007 11 9 SWAA075464 1 20071031 A 5311 6546555 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900292 20071109 00292 NM 2007 11 9 SWAA075462 1 20071031 A 5311 6546551 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900303 20071109 00303 EA 2007 11 9 QXEA200701639 1 20071030 A 2730 510007 PCU CNDAIR CL600 CL6002C10 1390015 EA ELEVATOR MALFUNCTIONED A QXEA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 09 602QX 14813 10010 DEN - FLIGHT CREW NOTICED A LAG IN THE PITCH CONTROL FROM NEUTRAL TO AFT 1-1.5". WORSE AT LOW SPEEDS, WITH FLAPS AND GE AR DOWN ALMOST 3" OF PLAY, PULLS THROUGH NEUTRAL WITH BUMPS AND A LAG. MAINTENANCE REPLACED ALL THREE LEFT ELEVATOR PCU 'S AND ADJUSTED THE ELEVATOR POSITION INDICATOR. COMPLIED WITH PCU RIGGING. OPERATIONAL CHECK FLIGHT GOOD. AIRCRAFT R ETURNED TO SERVICE, S/N'S OF PCU'S MAL0137, MAL0051, MAL0047. 2 L 7 2 4F RT A21EA 2007110900314 20071109 00314 EU 2007 11 9 07FDEA04720 1 20071105 A 5730 A57340087 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 729FD 657 FOUND ON LT WING BOTTOM SKIN AND PYLON SUPPORT BRACKET ELONGATED HOLES AT HYDRAULIC FITTINGS. REPAIR PERFORMED BY OVERS IZING THE HOLES, INSTALLING FREEZE PLUGS IAW DRAWING R 571-50532, APPROVED BY EA 6-2900-114891 AND RAS/BAE/1005593/2007 ISS A. 2 L 7 2 4F RT A35EU 2007110900322 20071109 00322 NM 2007 11 9 HALA0700462 1 20071102 A 5343 113T1632 SUPPORT BOEING 767 76733A 1385209 NM RT MLG CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 2531 SEAL SUPPORT CRACKED ON THE RIGHT MLG SUPPORT BEAM JUST I/B OF RT MLG. REPLACED SEAL SUPPORT PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007110900324 20071109 00324 NM 2007 11 9 HALA0700463 1 20071101 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 650-654 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 LEVEL 2 CORROSION ON SEAT TRACK RBL 88.5 STATION 650 TO 654+44. REPLACED SEAT TRACK PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007110900325 20071109 00325 NM 2007 11 9 HALA0700464 1 20071101 A 5420 313T3380381 BRACKET BOEING 767 76733A 1385209 NM LT NACELLE CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 CRACK ON "L" SECTION BRACKET LEFT ENGINE NACELLE STRUT HYDRAULIC COMPARTMENT FORWARD LOWER CORNER. REPLACED ANGLE BRACK ET PER SRM 51-40-06. 2 L 7 2 4F RT A1NM 2007110900330 20071109 00330 NM 2007 11 9 EIA2007192 1 20071026 A 3350 900835A BATTERY PACK BOEING 747 747212B 1384886 NM EMERGENCY LIGHTS INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482EV 20713 CREW SERVICE DOOR GROUND/SLIDE LIGHTS INOP MOUNTED ON DOOR JAMB. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER B747 M M 33-51-04. OPS CHECKED NORMAL PER B747 MM 33-51-04 PAGE 204. 2 L 7 4 4F A20WE 2007110900335 20071109 00335 EU 2007 11 9 TRAX200701660 1 20071101 A 5320 TORQUE BOX AEROSP ATR72 ATR72212 8680945 EU RIGHT CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 TORQUE BOX BTW FR 36-38 CORRODED (ON RT SIDE). CORROSION REMOVED AS PER SRM 51-21-42 TOURQUE BOX REPLACED IAW SRM 51-2 5-01 MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.030 OUT OF LIMITS AS PER SRM: 53-61-00 FIG 301. 2 H 7 2 4T RT A53EU 2007110900336 20071109 00336 EU 2007 11 9 TRAX200701661 1 20071101 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 LT OUTBD SEAT TRACK BTW FR 13-17 CORRODED FOUND. 2 H 7 2 4T RT 2007110900348 20071109 00348 EA 2007 11 9 TRAX200701675 1 20071102 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A ASOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 861AS 7445 FA REPORTS STRONG ELECTRICAL ODOR BETWEEN ROW 9 AND 11 OUT BOUND FROM ATL. EN ROUTE TO BTR A/C DIVERTED TO JAN DUE TO M TC. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007110900368 20071109 00368 NM 2007 11 9 SWAA075489 1 20071103 A 3350 W4142001220 WIRE BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 222WN 34290 EEPLS INOP AT ROW 6 ABC. FOUND LOOSE WIRE. SECURED WIRE PER MM. 2 L 7 2 4F RT A16WE 2007110900369 20071109 00369 NM 2007 11 9 SWAA075522 1 20071101 A 5610 141A4810 WINDOW BOEING 737 7377H4 1384404 NM COCKPIT ARCED A SWAA K NONE O OTHER NR NOT REPORTED 1 SW 29 227WN 34450 FLIGHT DECK R2 WINDOW ARCING. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2007110900370 20071109 00370 NM 2007 11 9 SWAA075490 1 20071103 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 250WN 34972 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007110900371 20071109 00371 NM 2007 11 9 SWAA075491 1 20071102 A 3350 20121A CHARGER BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007110900372 20071109 00372 NM 2007 11 9 SWAA075517 1 20071104 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CORRODED BETWEEN BS 951 AND BS 960, STR 27L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007110900373 20071109 00373 NM 2007 11 9 SWAA075492 1 20071102 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 416, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007110900374 20071109 00374 NM 2007 11 9 SWAA075493 1 20071102 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 408, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007110900378 20071109 00378 NM 2007 11 9 SWAA075525 1 20071104 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900379 20071109 00379 NM 2007 11 9 SWAA075526 1 20071104 A 5311 6546595 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900380 20071109 00380 NM 2007 11 9 USAA920070986 1 20071022 A 5320 146N52466 SUPPORT ANGLE BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN SUPPORT ANGLE, BS 1676, LBL 58.22. REPLACED CABIN SUPPORT AN GLE, BS 1676, LBL 58.22 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007110900381 20071109 00381 NM 2007 11 9 USAA920070987 1 20071025 A 5320 146N872241 ANGLE BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR STRUCTURE ANGLE, BS 1640, LBL 58.22, WL 208. REPLACED CABIN FLOOR STRUCTURE ANGLE, BS 1640, LBL 58.22, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007110900382 20071109 00382 EU 2007 11 9 F3LA200700312 1 20071017 A 5315 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM BETWEEN FRAME 68R AND 69R CORRODED. BLENDED CORRODED AREA AND FOUND F LOORBEAM TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG 102. REMOVED AND INSTALLED FLOORBEAM IAW SRM'S 51-42-11, 51-44-00, A ND 51-72-11. 2 L 7 2 4F RT A28NM 2007110900384 20071109 00384 2007 11 9 2007UALA04524 4 20071101 A 2565 GIRT BAR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE ESCAPE SLIDE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 AFT ENTRY DOOR ESCAPE SLIDE GIRT HANGING DOWN TOO FAR. REPLACED AFT ENTRY SLIDE ASSY. 2 L 7 2 4F 4 F RT A16WE E2GL 2007110900385 20071109 00385 NM 2007 11 9 2007UALA04525 1 20071101 A 3350 1317 LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 774UA 26936 EXIT EMERGENCY LIGHT AT DR 3R IS BURNT OUT. RELAMPED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007110900386 20071109 00386 NM 2007 11 9 2007UALA04526 1 20071101 A 5712 RIB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 LT WING NR 1 FUEL TANK INTERIOR RIB AT STA 135.5 LOWER CHORD AT FORWARD UPPER EDGE OF L-2 STRINGER CUT-OUT CRACKED. REP AIRED PER EA NR I070802. REMOVED AND REPLACED RIB AT STA 135.5 STRINGER L2. REF SB 737-57-1186 ON N-R 12553-5000-0015. 2 L 7 2 4F 4 F RT A16WE E2GL 2007110900391 20071109 00391 NM 2007 11 9 2007UALA04531 1 20071101 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 860-887 WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 EXTERNAL FUSE SKIN HAS SEVERAL AREAS OF WEAR UNDER DORSAL FIN LANDING FROM BS 860-887, BLENDED WORN AREAS AND ACP NDT FO R CRACKS AND MATERIAL LOSS. FABRICATED AND INSTALLED EXTERNAL DOUBLER AND INTERNAL TEAR STRAP DOUBLERS AND BONDED. 2 L 7 2 4F 4 F RT A16WE E2GL 2007110900392 20071109 00392 NM 2007 11 9 2007UALA04532 1 20071101 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 540 S24-25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 FWD PIT STA 540 MAIN FRAME BETWEEN STR 24L AND 25L HAS 1 DENT. CUTOUT DAMAGE AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110900393 20071109 00393 NM 2007 11 9 2007UALA04533 1 20071101 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1400 S25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 AFT PIT STA 1400 MAIN FRAME STR 25L HAS 1 DENT, CUTOUT DAMAGE AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007110900395 20071109 00395 NM 2007 11 9 USAA920070988 1 20071025 A 5320 141N517031 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 310 - BS 324, LBL 19.75, WL 208. REPLACED CABIN FLOOR SUPPORT, BS 310 - BS 324, LBL 19.75, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007111300001 20071113 00001 NM 2007 11 13 MWEA070269 1 20071101 A 5280 59107845 ANGLE BOEING 717 717200 1383700 NM MLG DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 912ME 55175 FORWARD CHANNEL AT LEFT MAIN GEAR DOOR OPENING HAS A CRACK JUST AFT OF HYDRAULIC SERVICE DOOR. FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F TR A6WE 2007111300002 20071113 00002 NM 2007 11 13 MWEA070270 1 20071103 A 5320 SG09530053 CUSP WEB DOUG MD88 MD88 3023688 NM BS 1174-1193 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 601ME 49762 CABIN CORROSION ON CUSP WEB AT STATION 1174-1193 LEFT SIDE AFT OF SERVICE DOOR. REMOVED CORROSION, FABRICATED AND INSTA LLED DOUBLER. 2 L 7 2 4F RT A6WE 2007111300005 20071113 00005 NM 2007 11 13 MWEA070273 1 20071105 A 7830 7150922505 STACK BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 907ME 55171 Z FRAME CRACKED AT RADIUS AT STATION 26.666 LEFT SIDE, BOTTOM BUCKET. FABRICATED AND INSTALLED STACK. 2 L 7 2 4F TR A6WE 2007111300007 20071113 00007 NM 2007 11 13 MWEA070275 1 20071105 A 7830 7150922505 ANGLE BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 907ME 55171 Z FRAME CRACKED AT RADIUS AT STATION 26.666 RIGHT UPPER BUCKET. FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F TR A6WE 2007111300008 20071113 00008 NM 2007 11 13 MWEA070276 1 20071105 A 7830 7150922505 DOOR FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 907ME 55171 LOWER DEFLECTOR DOOR Z FRAME CRACKED AT RADIUS AT STATION 26.6 RIGHT SIDE. FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F TR A6WE 2007111300009 20071113 00009 NM 2007 11 13 MWEA070277 1 20071105 A 5280 9911511 BRACKET DOUG MD88 MD88 3023688 NM MLG DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 601ME 49762 R1 DOOR UPPER FORWARD INTERIOR AREA HAS CRACKED BRACKET 8-9. REMOVED DAMAGE BRACKET AND INSTALLED BRACKET. 2 L 7 2 4F RT A6WE 2007111300010 20071113 00010 NM 2007 11 13 MWEA070278 1 20071102 A 5310 59107845 DOOR FRAME BOEING 717 717200 1383700 NM LT MLG DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 921ME 55183 LEFT MAIN LANDING FORWARD DOOR FRAME CRACKED AT STATION X56.25, Y764.50, Z30.25. = 80 INCHES LONG. FABRICATED AND INSTA LLED DOUBLER. 2 L 7 2 4F TR A6WE 2007111300015 20071113 00015 CE 2007 11 13 DXTA200702582 1 20071029 A 3246 315381 WHEEL CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG OUT OF ROUND E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 904QS 140 140 7500210 ABORTED TAKEOFF DUE TO SEVERE NOSE SHIMMY. LT & RT TIRES OUT OF ROUND. REMOVED AND REPLACED TIRE ASSEMBLIES IAW 750 MM 32-41-01. VERIFIED NO FAULTS OF YAW DAMP SYSTEM (27-24-00) OF ADC SYSTEM (34-11-07) ALL OPS CHECK GOOD IAW SAME. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007111300016 20071113 00016 CE 2007 11 13 DXTA200702583 1 20071030 A 3243 FITTING CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MASTER CYLINDER LOOSE E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 336QS 5600336 1ST OFFICERS BRAKES ARE MUSHY AND REQUIRE A COUPLE OF PUMPS AFTER INTITAL PRESSURE TO FIRM UP. INSPECTED BRAKE SYSTEM, FOUND PILOTS LT MASTER CYLINDER FITTINGS LOOSE. TIGHTENED FITTINGS. BLEED BRAKE SYS MULTIPLE TIMES. OPS LEAK CHECK GOOD IAW CESSNA 560 MM 32-42-00 2 L 7 2 4F 4 F RT A22CE E25EA 2007111300017 20071113 00017 CE 2007 11 13 DXTA200702584 1 20071030 A 3250 714878 CONTROL UNIT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG STEERING INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 975QS 2795 2795 7500175 NOSE GEAR WILL NOT RETRACT. RED GEAR UNLOCK AND GREEN NOSE GEAR DOWN LIGHTS STAY ON. REMOVED AND REPLACED NOSE WHEEL S TEERING UNIT. TRAVELCHECK,LEAK CHECK AND OPS CHECK GOOD. IAW CE750 MM 32-50-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007111300018 20071113 00018 CE 2007 11 13 DXTA200702585 1 20071030 A 3243 MASTER CYLINDER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE RT BRAKE BYPASSING E DXTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 316QS 5600516 PILOTS RT BRAKE PEDAL GOES SOFT AFTER 15-20 SEC OF INITIAL BRAKE APPLICATION. (LOSSED APPX 2-3 INCHES OF PEDAL TRAVEL). INSTALLED 1EA NEW PILOTS RH BRAKE MASTER CYLINDER AND BLED SYSTEM. OPERATED ENGINES AND TAXI CHECKED NORM, WORK DONE I AW C560 M/M 32-42-02, 32-42-00 AND P.O.H. 2 L 7 2 4F 4 F RT A22CE E25EA 2007111300019 20071113 00019 EU 2007 11 13 2007UALA04456 1 20071029 A 3350 D9239003500060 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 472UA 1435 CABIN EMERGENCY LIGHTS TEST FAILS. FOUND EPSU FAILED. REPLACED THE EPSU, AND CYCLED FSB NO SMOKING SIGNS AND MASTER EM ERGENCY LIGHT SWITCH. RAN EMERGENCY LIGHT TEST AT PANEL, SYSTEM CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007111300020 20071113 00020 EU 2007 11 13 2007UALA04457 1 20071029 A 2611 RAI2800M0706 CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE DETECTOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 418UA 485 LAVATORY AND CARGO DETECTOR FAULT DISPLAYED ON UPPER ECAM SCREEN - SMOKE. FOUND SDCU FAILED. REPLACED SDCU. 2 L 7 2 4F 4 F RT A28NM E40NE 2007111300021 20071113 00021 EU 2007 11 13 2007UALA04458 1 20071029 A 3350 LAMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 426UA 510 RIGHT UNIT FAIL EMERGENCY LIGHT TEST. FOUND LAMPS WERE FAULTY. RELAMPED CABIN CEILING EXIT LIGHT AND LT OVERWING EXIT- -OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007111300022 20071113 00022 EU 2007 11 13 2007UALA04477 1 20071030 A 5310 STRUCTURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 409UA 462 AFT OF L1 DOOR BETWEEN FRAMES 23 & 24, S22-23L. A LARGE DENT MEASURING 3.5 INCHES BY 2 INCHES AND .250 INCHES DEEP. PAT CH ON FWD EDGE IS ALSO DENTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007111300023 20071113 00023 NM 2007 11 13 2007UALA04483 1 20071031 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 850UA 1653 CREW OXYGEN SYSTEM LOW RECORD PRESSURE PRIOR TO SERVICING. SERVICED CREW O2 SYSTEM TO 1800 PSI- NO REPEATS SINCE ORIGI NAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007111300024 20071113 00024 EU 2007 11 13 2007UALA04500 1 20071030 A 3510 RCF6705 TRANSMITTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 418UA 485 COCKPIT OXYGEN DOWN TO 1040. FOUND PRESSURE REGULATOR LEAKING AT FILL PORT. REPLACED PRESSURE REGULATOR TRANSMITTER. LE AKING AT FILL PORT. SERVICED O2 SYSTEM TO PROPER LEVELS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007111300025 20071113 00025 EU 2007 11 13 2007UALA04503 1 20071031 A 5753 FLAP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LEFT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 438UA 678 LEFT OUTBOARD FLAP IS DAMAGED. REPLACED FLAP AND PERFORMED TEST FLIGHT- OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007111300026 20071113 00026 NM 2007 11 13 2007UALA04504 1 20071031 A 5753 FLAP AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE RT WING TE FLAP DAMAGED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 808UA 804 BIRD STRIKE RT WING OUTBOARD FLAP. ACCOMPLISHED REPAIR ON RIGHT WING OUTBOARD FLAP. 2 L 7 2 4F 4 F RT A28NM E40NE 2007111300027 20071113 00027 EU 2007 11 13 2007UALA04515 1 20071101 A 2700 3945128102 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ELAC FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 490UA 1728 ELAC 2 PITCH FAULT ECAM MESSAGE DISPLAYED AFTER PUSHBACK. TRIED CYCLING ELAC C/B AS WELL AS CONTROL SWITCH, ALL NO HELP . FOUND ELAC2 FAILURE. REPLACED ELAC2 AND MESSAGE CLEARED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007111300028 20071113 00028 NM 2007 11 13 2007UALA04536 1 20071101 A 5210 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LOWER ROLLER GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 342UA 24246 FWD ENTRY DOOR FWD LOWER ROLLER FITTING GOUGED. LIGHTLY BLENDED FITTING. INSTALLED HORSESHOE SHIM. 2 L 7 2 4F 4 F RT A16WE E2GL 2007111300029 20071113 00029 NM 2007 11 13 2007UALA04537 1 20071030 A 7160 NOSE COWL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 726522 BIRDSTRIKE ON NR 2 ENG INLET DEPTH OF DENT BEYOND SRM LIMITS BY FACTOR OF TWO. NR 2 ENG NOSE COWL LE LIP HAS A DENT APP ROX 3 INCHES IN DIA AND 1-4TH INCH DEEP AT 9 O'CLOCK POS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007111300030 20071113 00030 NM 2007 11 13 2007UALA04541 1 20071105 A 2750 FLAP SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TE FLAPS MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 530UA 25043 CREW REPORTS HAD TE FLAG DISAGREE MSG , FLAP HANDLE SELECT 25 DEG, FLAP IND STOPPED AT 21 DEG. CREW REPORTED LANDING SM OOTH 138K WT 174TH. 2 L 7 2 4F 4 F RT A2NM E17NE 2007111300031 20071113 00031 NM 2007 11 13 2007UALA04542 1 20071102 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 S10L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 FOUND BS 360 STRINGER 10L STR ATTACH CLIP IS CRACKED. 2 L 7 2 4F 4 F RT A16WE E2GL 2007111300032 20071113 00032 NM 2007 11 13 2007UALA04543 1 20071102 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 S8L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 FOUND BS 360 STRINGER 8L, STRINGER ATTACH CLIP IS CRACKED. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007111300033 20071113 00033 NM 2007 11 13 2007UALA04544 1 20071102 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294-303 S16L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 PASSENGER CABIN INTERCOSTAL BETWEEN BS 294 - 303 AT STRINGER 16L HAS CRACK AT FWD END. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007111300034 20071113 00034 NM 2007 11 13 2007UALA04545 1 20071102 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 FWD ENTRY DOOR WAY LOWER HINGE CUTOUT HAS 2 FASTENER HOLES WITH CRACK INDICATIONS. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007111300035 20071113 00035 NM 2007 11 13 2007UALA04546 1 20071102 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 351 S15L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 FOUND BS 351 (FWD SIDE) AT STR 15L ATTACH CLIP CRACKED. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007111300036 20071113 00036 NM 2007 11 13 2007UALA04547 1 20071102 A 5313 STRINGER SPLICE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 S14L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 FOUND BS 360 STRINGER 14L, STR SPLICE CHANNEL IS CRACKED. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007111300037 20071113 00037 NM 2007 11 13 2007UALA04548 1 20071102 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 FWD ENTRY DOOR WAY UPPER HINGE CUTOUT HAS 2 FASTENERS WITH CRACK INDICATIONS. CRACKS ARE IN FASTENERS HOLES. ACCOMPLIS HED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007111300038 20071113 00038 NM 2007 11 13 2007UALA04549 1 20071102 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 S11L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 FOUND BS 360 AT STRINGER 11L STR ATTACH CLIP IS CRACKED. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007111300039 20071113 00039 NM 2007 11 13 2007UALA04550 1 20071102 A 5313 STRINGER SPLICE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 S15L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 FOUND BS 360 STRINGER 15L, STR SPLICE CHANNEL IS CRACKED. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007111300041 20071113 00041 NM 2007 11 13 2007UALA04552 1 20071102 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 303 S10L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 PASSENGER CABIN BS 303 AT STR 10L HAS A CRACKED INTERCOSTAL SUPPORT ANGLE. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007120600005 20071206 00005 SO 2007 12 6 SIMA200733207 1 20071126 A 3020 678083 VALVE EMB 135 EMB135KL 3260302 SO ANTI-ICE SYS MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 827AE 145602 NR 2 ENGINE ANTI ICE SYSTEM FAILED IN ROUTE TO LEX. A/C DIVERTED TO ICT DUE TO IN ROUTE WEATHER. CONTRACT MX ISSUED MEL 30-11 TO THE AIRCRAFT. REMOVED AND REPLACED NR 2 ENG ANTI-ICE VALVE IAW EMB AMM 30-21-01 OPS CHECK GOOD IAW EMB AMM P/T 30-00-00-700-802-A MEL ITEM RESTORED AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT T00011AT 2007111300042 20071113 00042 2007 11 13 2007UALA04554 4 20071103 A 2565 7A146722 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE R1 DOOR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 193UA 26890 PRIOR TO DEPARTURE FLIGHT ATTENDANT REQUEST CHECK 1R DOOR. FOUND ESCAPE SLIDE RAFT CAME DOWN FROM THE DOOR. SUSPECT IMP ROPER INSTALLATION OF SLIDE. REPOSITIONED ESCAPE SLIDE RAFT PER MM 25-69-01. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007111300098 20071113 00098 EA 2007 11 13 QXEA200701558 1 20071009 A 5310 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA BS 893 S5L DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - C4 CHECK, REFERENCE REO 670-53-11-188 SHEET 3 MAP M, BURNT MATERIAL AROUND FASTENER HOLE AT FS 893 2" BELOW STRING ER 5L. REPAIRED IAW REO 670-53-11-188 PAGE 3 MAP M STEPS 9 10 AND 11. 2 L 7 2 4F RT A21EA 2007111300099 20071113 00099 NM 2007 11 13 HALA0700467 1 20071105 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 1098-1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 SEAT TRACK CORROSION BEYOND SRM LIMITS RIGHT BODY LINE 88.5 STATION 1098 TO 1197+11. REPLACED TRACK PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007111300100 20071113 00100 NM 2007 11 13 HALA0700466 1 20071031 A 5511 SPAR BOEING 767 76733A 1385209 NM HORIZONTAL STAB CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 LEVEL 1 CORROSION ON FASTENERS ON LEFT HORIZONTAL STABLIZER REAR SPAR OUTBOARD END. REMOVED CORROSION PER SRM 51-10-02 AND TREATED PER SRM 51-20-01. 2 L 7 2 4F RT A1NM 2007111300101 20071113 00101 NM 2007 11 13 HALA0700465 1 20071105 A 4940 38880585 EXCITER BOEING 767 76733A 1385209 NM APU INOPERATIVE A HALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM: AFTER LANDING APU WOULD NOT START. REMOVED AND REPLACED IGNITION UNIT PER AMM 49-41-03. 2 L 7 2 4F RT A1NM 2007111300102 20071113 00102 WP 2007 11 13 DHL2007801503 1 20071018 A 5754 STRUCTURE DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 RT INNER WING OUTBD EXTENDED L/E SLOT PLATING CRACKED 1.500" STA XFS 207.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG . 38 PG 2, TR NR 57-85 DATED 11-22-00. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED REPAI R DOUBLER (AL7075T6 0.071") AND FILLER (AL7075T6 0.063") IAW SRM 57-2-1 FIG 38 PG 2, TR NR 57-85, SRM 57-3-3 FIG 3 SHEET 3 PG 11 ITEM H. CLEANED, TREATED AND PRIMED AREA, FILLER AND INNER FACE OF REPAIR DOUBLER IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 57-2-1 FIG 38 PG 2, TR NR 57-85, SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007111300103 20071113 00103 EU 2007 11 13 DHL2007366501 1 20070926 A 5347 TMS6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 366DH 249 MAIN CARGO FLOOR SEAT TRACK HAS SCRATCHES AT FR 29 LBL 37. REMOVED AND REPLACED SEAT TRACK SECTION BETWEEN FR 27 TO FR 33 LBL 37". SEAT TRACK INSTALLED OF 7075-T6 511 P/N TMS 6022457, PO NR 94091935 AS PER A-300 SRM 53-10-10. 2 L 7 2 4F RT A35EU 2007111300104 20071113 00104 NM 2007 11 13 DHLA200700055 1 20071106 A 5310 TORQUE BOX BOEING 727 727214 138407R NM BS 1223-1233 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 DURING AN"A" CHECK, TORQUE BOX AREA, LIGHTING HOLES AT STA 1223 LT AND RT HAVE SMALL CRACKS 2 AFT AIR STAIR AREA (PREVIO USLY REJECTED ON NR 138359). CUT OUT DAMAGED AREA AT TORQUE BOX AREA LIGHTING HOLES/H DIMENSION CUTOUT 3/4" BY 1/4" IAW B727 SRM 53-10-1 FIG1. CUTOUT DAMAGED AREA AT LIGHTING HOLES LT DIMENSION CUTOUT 1/2" BY 1/4" IAW B727 SRM 51-10-1 FIG 1FAB. DOUBLER REPAIR RT AND LT MATERIAL USED 7075T6 .040 POX> 9005892 RT DIMENSION 4" BY 2 1/2". LT DIMENSION 4" BY 2 1/2" IAW B727 SRM 53-10-2 FIG 6 AND SRM 51-10-2. INSTALLED DOUBLER REPAIR AT TORQUE BOX AREA LIGHTING HOLES LT STA 122 3 AND RT STA 1233 IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007111300105 20071113 00105 WP 2007 11 13 DHL2007801500 1 20071016 A 5754 FRAME DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 RT WING CENTRAL L/E FORMER SHOWS 1" CRACK AT STA XFS 341.500. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE A ND FABRICATED (2EA) ANGLE DOUBLER FROM AL7075T6 0.032 INCH IAW SRM 57-2-0 PG 9 AND 10. CLEANED, TREATED AND PRIMED ANGL E DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-20D, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007111300106 20071113 00106 WP 2007 11 13 DHL2007801502 1 20071015 A 5730 SKIN DOUG DC8 DC873F 302199F WP RWS 429 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 RT WING CTR L/E UPPER SKIN CORRODED, STA XFS 429.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38 PG 2, TR NR 57-85. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16 . CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER (AL7075T6 0.071") AND FILLER (AL7075T6 0.063") IAW SRM 57-2-1 F IG 38 PG 2, TR NR 57-85 DATED 11-22-00, SRM 57-3-3 FIG 5 SHEET 1 PG 14 ITEM "A". CLEANED, TREATED AND PRIMED AREA, FILL ER AND INNER FACE OF REPAIR DOUBLER IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 57-2-1 FIG 38 PG 2, TR NR 57-85, SR M 51-1-11, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007111300107 20071113 00107 EU 2007 11 13 DHL2007366504 1 20071006 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 366DH 249 MAIN CABIN FLOOR SEAT TRACK CORRODED AT FR 61 RBL 77. ACCOMPLISHED MAJOR PERMANENT REPAIR BY REPLACING A 50" PREVIOUSLY SPLICED SECTION OF SEAT TRACK AT MAIN CABIN RBL 77" BETWEEN FRAMES 58.5 AND 61 IAW A300 SRM 53-10-10, P/N 6022457 P/O 0 35166. 2 L 7 2 4F RT A35EU 2007111300108 20071113 00108 WP 2007 11 13 DHL2007801506 1 20071022 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 801DH 85401 46033 LT WING NR 1 STUB WING EXTERNAL PART SHOWS REPAIR NOT IAW SRM 57-2-1A AT STA XFS 533-375. PERFORMED MAJOR REPAIR IAW SR M 57-2-1A FIG 1. REMOVED NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED EXTERNAL REPAIR DOUBLER (AL7075 T6 0.080") AND INTERNAL DOUBLER (AL7075"0" 0.063") IAW SRM 57-2-1A ITEM J,K. HEAT TREATED INTERNAL DOUBLER FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 1,13,17. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 57-2-1A FIG 1, SRM 51-1-11, SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007111300109 20071113 00109 EU 2007 11 13 DHL2007366500 1 20070926 A 5347 TMS6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 366DH 249 ASTAR N/R 115888: MAIN CARGO FLOOR SEAT TRACK HAS SCRATCHES AT FR 29 LBL 37. REMOVED AND REPLACED SEAT TRACK SECTION BE TWEEN FR 27 TO FR 33 LBL 37". SEAT TRACK INSTALLED OF 7075-T6 511 P/N TMS 6022457, PO NR 94091935 AS PER A-300 SRM 53-1 0-10. 2 L 7 2 4F RT A35EU 2007111300110 20071113 00110 EU 2007 11 13 DHL2007366505 1 20071009 A 4910 SKIN AIRBUS 300 A300B4203 3930306 EU APU DOORS DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 366DH 249 APU LEFT DOOR HAS HOLE ABOVE 3RD LATCH FORWARD SIDE. CUTOUT DAMAGED AREA OF APU LEFT DOOR EXTERNAL SKIN AND FABRICATED AND INSTALLED REPAIR DOUBLER IAW A300 SRM 52-40-00 (PB701). MATERIAL USED 2024-T3 (0.032") ALUMINUM SHEET PO NR 046981 SIZE 6" BY 4". PREPARE SURFACE AND PAINTED IAW A-300 SRM 51-40-12. THIS IS A MAJOR REPAIR CLASS "A" (PERMANENT). 2 L 7 2 4F RT A35EU 2007111300111 20071113 00111 EU 2007 11 13 DHL2007366502 1 20070926 A 5347 TMS6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 366DH 249 ASTAR N/R 115888: MAIN CARGO FLOOR SEAT TRACK HAS SCRATCHES AT FR 29 LBL 37. REMOVED AND REPLACED SEAT TRACK SECTION BE TWEEN FR 27 TO FR 33 LBL 37". SEAT TRACK INSTALLED OF 7075-T6 511 P/N TMS 6022457, PO NR 94091935 AS PER A-300 SRM 53-1 0-10. 2 L 7 2 4F RT A35EU 2007111300112 20071113 00112 EU 2007 11 13 DHL2007366506 1 20071006 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 366DH 249 MAIN CABIN FLOOR SEAT TRACK AT FR 57 TO FR 60 RBL 58 2 SPOTS OF CORROSION. ACCOMPLISHED A PERMANENT MAJOR REPAIR AT MAI N CARGO COMPARTMENT SEAT TRACK AT FR 57 - 60 BY SPLICING A SEAT TRACK SECTION P/N 60-22457 AND SPLICES P/N R532-70490-20 0 IAW A300 SRM 53-10-10 FIG 725. TREATED, PRIMED AND PAINTED IAW A300 SRM 51-40-12 AND INSTALLED PER A300 SRM 51-30-30. 2 L 7 2 4F RT A35EU 2007111300113 20071113 00113 EU 2007 11 13 DHL2007366503 1 20071009 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 366DH 249 MAIN CARGO SEAT TRACK BETWEEN FR 23 - 27 LBL 58" WITH CORROSION AROUND CLIPNUTS HOLES. REMOVED AND REPLACED SEAT TRACK AT MAIN CABIN FROM FR 19 TO FR 27 LBL 58 AS PER A300 SRM 53-10-10. THIS IS A MAJOR PERMANENT REPAIR, P/N 60-22457 PO NR 035166. 2 L 7 2 4F RT A35EU 2007111300114 20071113 00114 WP 2007 11 13 DHL2007801501 1 20071015 A 5753 STRUCTURE DOUG DC8 DC873F 302199F WP LT WING TE FLAP BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 LT INBD FLAP UPPER PLATING BROKEN 1" STA XW 106.000. PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1 PG 2. REMOVED DAMAGED PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040") IAW SRM 57-7-1 FIG 1 PG 2 ITEM D. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF NEW PLATING IAW SRM 51-1-8B. INSTALLED NEW PLATING IAW SRM 51-1-11, SRM 51-1-21, SRM 51-3-0, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007111300115 20071113 00115 NM 2007 11 13 DHL2007749001 1 20070924 A 5320 WEB BOEING 727 727223 1384074 NM BS 1233 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 WHILE AT FLIGHTSTAR AIRCRAFT SERVICES FOR A CHECK, REF N/R 099780, DISCREPANCY, RT AIRSTAIR TORQUE BOX CRACKED AT LIGHTN ING HOLE AT BS 1233. STOPPED DRILLED HOLE AT THE END OF CRACK WITH .250 IAW SRM 51-10-01, C/W HFEC IAW NDTM PT 6, 51-00 -00 FIG 23, CRACK TERMINATED AT STOP DRILL. FAB DOUBLER REPAIR FROM 7075T6 .032 PO 9004042 DIM 5 BY 2.5 IAW SRM 53-10-2 FIG 6. INSTALLED DOUBLER REPAIR IAW SRM 53-10-2 FIG 6. 2 L 7 3 4F A3WE 2007111300116 20071113 00116 NM 2007 11 13 DHL2007743 1 20071030 A 5754 MOUNT BOEING 727 727225 1384077 NM NR 7 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 RIGHT WING AT NR 7 SLAT ACTUATOR INBD TRUNNION MOUNT HAS DOUBLER THAT APPEARS TO BE CRACKED. 2 L 7 3 4F A3WE 2007111300117 20071113 00117 WP 2007 11 13 DHL2007801505 1 20071017 A 5754 STRUCTURE DOUG DC8 DC873F 302199F WP RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 RT INNER WING OUTBD EXTENDED L/E SLOT PLATING CORRODED, STA XILD 42. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38 PG 2, TR NR 57-85 DATED 11-22-00. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER (AL7075T6 0.071") AND FILLER (AL7 075T6 0.063") IAW SRM 57-2-1 FIG 38 PG 2, TR NR 57-85, SRM 57-3-3 FIG 3 SHEET 3 PG 11 ITEM H. CLEANED, TREATED AND PRIM ED AREA, FILLER AND INNER FACE OF REPAIR DOUBLER IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 57-2-1 FIG 38 PG 2, SR M 51-1-21, SRM 51-1-20D, SRM 51-1-11, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007111300118 20071113 00118 WP 2007 11 13 DHL2007801504 1 20071026 A 5730 DOUBLER DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 LT WING L/E LWR INTERNAL DOUBLER CRACKED 1" STA XFS 335.250. REMOVED CRACKED INTERNAL DOUBLER IAW SRM 51-1-21. FABRICA TED NEW DOUBLER (AL7075T6 0.090") IAW SRM 57-3-3 FIG 5. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 PG 2A. 2 L 7 4 4F RT 4A25 2007111300119 20071113 00119 NM 2007 11 13 DHL2007749002 1 20070924 A 5320 WEB BOEING 727 727223 1384074 NM BS 1233 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 WHILE AT FLIGHTSTAR AIRCRAFT SERVICES FOR A CHECK, REF N/R 099780, DISCREPANCY, RT AIRSTAIR TORQUE BOX CRACKED AT LIGHTN ING HOLE ATBS 1233. STOPPED DRILLED HOLE AT THE END OF CRACK WITH .250 IAW SRM 51-10-01, C/W HFEC IAW NDTM PT 6, 51-00- 00 FIG 23, CRACK TERMINATED AT STOP DRILL. FAB DOUBLER REPAIR FROM 7075T6 .032 PO 9004042 DIM 5 BY 2.5 IAW SRM 53-10-2 FIG 6. INSTALLED DOUBLER REPAIR IAW SRM 53-10-2 FIG 6. 2 L 7 3 4F A3WE 2007111300120 20071113 00120 WP 2007 11 13 NWAA073679855 1 20071101 A 5415 ATTACH ANGLE DOUG DC9 DC951 3022051 WP NACELLE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 764NC 47717 DURING "H" CHECK, FOUND CRACK IN LOWER PYLON ATTACH ANGLE AT BS 1167. REPAIRED PER EA 98-210188. 2 L 7 2 4F RT A6WE 2007111300122 20071113 00122 SO 2007 11 13 SWIA200718826 1 20071029 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN MISSING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 580SW 120348 FLT 5473 - "EXIT" SIGN MISSING ON EMERGENCY EXIT DOOR AT ROW 6 BC. REPLACED EXIT LIGHT ASSEMBLY AT 6BC. OPS CHECK GOOD . 2 L 7 2 4T RT A31SO 2007111300123 20071113 00123 EA 2007 11 13 SWIA200718827 1 20071025 A 5753 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA TE FLAP DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 969SW 7876 FLT 5947 - RIGHT INBOARD FLAP AND STANG FAIRING IS DAMAGED FROM TIRE BLOW OUT. REPLACED RIGHT INBOARD FLAP AND STANG FA IRING WITH SERVICEABLE UNITS IAW MM 27-54-01 AND 52-52-08, PN 601R14002-2, SN/OFF SB/RJ/903. 2 L 7 2 4F RT A21EA 2007111300124 20071113 00124 EA 2007 11 13 SWIA200718828 1 20071025 A 5710 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA RT WING DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 455SW 7760 RIGHT WINGLET UPPER LEADING EDGE IS DAMAGED FROM BIRD STRIKE. INSTALLED NEW UPPER WINGLET LEADING EDGE IAW SRM 51-42-06 . 2 L 7 2 4F RT A21EA 2007111300125 20071113 00125 EA 2007 11 13 SWIA200718829 1 20071028 A 3230 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 409SW 7056 FLT 3805 - RECEIVED A GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGE AFTER SELECTING GEAR DOWN. ALTERNATE GEAR EXTENS ION COMPLIED WITH. REPLACED MAIN LANDING GEAR DOOR SELECTOR VALVE IAW 32-22-00. OP AND LEAK CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007111300126 20071113 00126 SO 2007 11 13 SWIA200718830 1 20071021 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 308SW 120326 FLT 5589 - MULTIPLE FLOOR LEVEL EMERGENCY LIGHTS ARE INOPERATIVE. REPAIRED WIRING ON FLOOR EMERGENCY LIGHTS. 2 L 7 2 4T RT A31SO 2007111300127 20071113 00127 EA 2007 11 13 SWIA200718831 1 20071030 A 3350 INVERTER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 920SW 7660 EMERGENCY FLOOR LIGHTING AFT OF OVERWING EXIT IS INOP. REPLACED NR 4 EMERGENCY LIGHT POWER INVERTER. OPS CHECK GOOD IA W CRJ 200 MM 33-51-00. 2 L 7 2 4F RT A21EA 2007111300128 20071113 00128 EA 2007 11 13 SWIA200718832 1 20071102 A 5297 WIRE CNDAIR CL600 CL6002C10 1390015 EA CARGO DOOR BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 744SK 10200 FLT 6438 - RECEIVED A PROX SYSTEM FAULT 2 STATUS MESSAGE AT THE GATE. REPAIRED BROKEN WIRE ON FORWARD CARGO DOOR HARNES S. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007111300129 20071113 00129 EA 2007 11 13 SWIA200718833 1 20071104 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 416SW 7089 FLT 3945 - OUTER HANDLE ON PAX DOOR WILL NOT STOW. REPLACED DAMAGED BOLT IN HANDLE MECHANISM IAW CMM 52-43-03. OPS CHE CK GOOD. 2 L 7 2 4F RT A21EA 2007111300130 20071113 00130 EA 2007 11 13 SWIA200718834 1 20071103 A 2150 ACM CNDAIR CL600 CL6002C10 1390015 EA RIGHT SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 753SK 10214 FLT 6438 - RIGHT PACK AUTO FAILED WITH ASSOCIATED SMOKE IN THE CABIN. REPLACED RIGHT ACM AS REQUIRED IAW CRJ 700 AMM 21 -51-08. ALL OPS CHECK GOOD, PN GG670-95009-1, SN/OFF 00990. 2 L 7 2 4F RT A21EA 2007111300131 20071113 00131 EA 2007 11 13 SWIA200718835 1 20071023 A 3244 TIRE CNDAIR CL600 CL6002B19 1900309 EA RT MLG FAILED A SWIA O OTHER O OTHER LD LANDING 1 NM 07 969SW 7876 FLT 5947 - THE RIGHT INBOARD MAIN TIRE BLEW OUT. REPLACED NR 3 AND NR 4 MAIN WHEEL ASSEMBLIES IAW CRJ MM 32-41-01, PN 5 010571-1, SN/OFF APR02-4838, PN 5010571-1, SN/OFF JAN00-2803. 2 L 7 2 4F RT A21EA 2007111300132 20071113 00132 2007 11 13 SIMA200742301 2 20071105 A 7532 7858023 BLEED VALVE SAAB SF340 340B 7860101 EU MALFUNCTIONED A SIMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 21 301AE 340B301 BEFORE TAKEOFF CHECKLIST NOTED RIGHT BLEED VALVE NOT CLOSED FOUND CB H16 POPPED. CONTACTED MOC. ADVISED TO RESET CB. CB H16 POPPED A SECOND TIME. CREW ELECTED TO RETURN TO THE GATE. REMOVED AND REPLACED PRSO VALVE IAW SAAB340 AMM 36-11- 05-02. OPS CK NORMAL, PER SAAB 340 AMM 36-11-00-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007111300133 20071113 00133 SO 2007 11 13 SIMA200732502 1 20071105 A 3230 7455503 MODULE EMB 135 EMB135LR 3260305 SO MLG MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 715AE 145262 AIRCRAFT DIVERTED TO JFK, ON TAKEOFF FROM DCA HEADING TO BOS RECEIVED LANDING GEAR AIR/GROUND FAIL MSG AND GEAR HANDLE W OULD NOT GO TO THE UP POSITION. FLEW WITH GEAR DOWN INTO JFK FOR REPAIR. DID DECLARE EMERGENCY. LANDED WITHOUT INCIDE NT. REMOVED AND REPLACED NOSE LANDING GEAR DOWN LOCK PROX SWITCH, BOTH LT MLG PROX SWITCH, AND LANDING GEAR MODULE. AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007111300134 20071113 00134 NE 2007 11 13 Y2PA200700026 2 20071102 A 7200 696233B CSD DOUG DC9 DC932F 3022067 WP PWA JT8 JT8D9A 52048 NE NR 2 ENGINE FAILED A Y2PA B A EMER. DESCENT UNSCHED LANDING E X J VIBRATION/BUFFET ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 GL 23 208US 47220 665458 CREW REPORTED ENGINE VIBRATION THEN FAILURE ON NR 2 ENGINE. IRREGULARITY FILLED OUT BY CREW REPORTED AS FOLLOWS. AFTER DEPARTURE IN CLIMB, VIBRATION FOLLOWED BY NR 2 ENGINE FLAME OUT AT FL190 FOLLOWED BY AIRCRAFT CROSSTIE LOCKOUT. CREW D ECLARED AN EMERGENCY AND RETURNED TO POINT OF DEPARTURE AT MMCU. AIRCRAFT MADE AN UNEVENTFUL LANDING AT MMCU. AFTER AI RCRAFT LANDED MAINTENANCE WAS SENT TO MMCU TO INSPECT ENGINE AND AIRCRAFT. USA JET MECHANIC PERFORMED A VISUAL INSPECTI ON ON THE ENGINE AND FOUND NO DEFECTS IN THE INLET OR EXHAUST. THE MECHANIC FOUND DURING TROUBLING SHOOTING THE NR 2 CS D/GENERATOR HAD FAILED. THE ON-SITE MECHANIC PULLED , INSPECTED AND REPLACED WITH NEW THE NR 2 ENGINE OIL FILTER WITH N 2 L 7 2 4F 4 F A6WE E2EA 2007111300156 20071113 00156 2007 11 13 DHLA200700037 4 20070807 A 3420 INDICATOR AIRBUS 300 A300B4203 3930306 EU COCKPIT INOPERATIVE A DHLA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 05 366DH 249 REJECTED T/O NO CAPT A/S EITHER DIGITAL OR ANALOG. REJECTED AT 80 KTS, 273000 GTOW TEMP 25 DEGS C, NORMAL BREAK ENERGY. FLUSHED NR 1 PITOT SYS AS PER MM 34-11-10. DEBRIS CLEARED FROM LINES. 2 L 7 2 4F RT A35EU 2007111300157 20071113 00157 EU 2007 11 13 TRAX200701569 1 20071022 A 5344 HINGE AEROSP ATR72 ATR72212 8680945 EU EMERGENCY EXIT BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 FITTING HINGE (AFT) BROKEN ON RT EMERGENCY EXIT (RESOLVED ON W/O: 71093 TASKCARD: N/R-00253 ), FITTING HINGE ON RT EMERG ENCY EXIT REPLACED AND INSTALLED IAW SRM 51-25-04. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-04, SUPPLEMENTAL. 2 H 7 2 4T RT A53EU 2007111300158 20071113 00158 EA 2007 11 13 TRAX200701678 1 20071031 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 759EV 10211 FOUND FS 280 CROSSBEAM HAS CORROSION DAMAGE. 2 L 7 2 4F RT A21EA 2007111300159 20071113 00159 EA 2007 11 13 TRAX200701679 1 20071031 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 759EV 10211 FOUND FS 280 FWD ATTACH ANGLE HAS CORROSION DAMAGE. 2 L 7 2 4F RT A21EA 2007110900129 20071109 00129 EU 2007 11 9 AALA20072103 1 20071031 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14068 511 JFK - EMERGENCY LIGHT AT RIGHT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER THREE D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007110900130 20071109 00130 EU 2007 11 9 AALA20072105 1 20071031 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14068 511 JFK - SEAT MOUNTED EMERGENCY LIGHTS AT RIGHT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007110900158 20071109 00158 WP 2007 11 9 AALA20072078 1 20071030 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 33502 49739 LGA - EMERGENCY LIGHTS AT OVERHEAD TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK AT STATION 1338 FOR EMERGENCY LI GHTS AT OVERHEAD TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007110900161 20071109 00161 2007 11 9 AALA20072051 2 20071026 A 7597 WIRE BOEING 767 767323 1385205 NM LEFT ENGINE CHAFED A AALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 383AN 26995 MIA INFLIGHT T963/26OCT DFW TO GRU - LEFT ENGINE PRESSURE RELIEF VALVE EICAS STATUS MESSAGE ILLUMINATED AT FLIGHT LEVEL 300. LANDED MIA WITHOUT INCIDENT. FOUND GROUND WIRE CHAFING WITH STUDS AT NUMBER ONE ENGINE PRESSURE RELIEF VALVE. RE PLACED GROUNDING WIRE AND PRESSURE RELIEF VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007110900172 20071109 00172 EU 2007 11 9 SIMA200730403 1 20071019 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 304AE 21126 5000 340B304 DURING A MBV INSPECTION CORROSION WAS FOUND ON THE RT SIDE OF FRAME 72. REPAIRED FRAME 72 IAW SAAB SRM CHAPTER 53-70-30 . AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007110900182 20071109 00182 NM 2007 11 9 CALA0700636 1 20071101 A 5320 141A5211U1 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33209 30581 INSPECTION FOUND SUPPORT CHANNEL CORRODED AT STA 270, BL 0. THE SUPPORT CHANNEL WAS REPAIRED IAW ECRA 5321-01506. 2 L 7 2 4F RT A16WE 2007110900188 20071109 00188 2007 11 9 F3LA200700301 4 20071029 A 2565 D5211009820000 UPLOCK HOOK AIRBUS A319 A319112 3930323 EU L2 DOOR SLIDE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED THAT UPON INSTALLATION OF THE L2 DOOR SLIDE, THE L2 DOOR HANDLE COULD BE MOVED I NTO THE CLOSED POSITION BEFORE THE DOOR WAS IN THE HOLE. REMOVED AND REPLACED L2 DOOR UP-LOCK HOOK IAW 52-11-21-400-001 , SUBTASK AMM 52-11-21-420-052. 2 L 7 2 4F RT A28NM 2007110900195 20071109 00195 2007 11 9 UPS07851088 4 20071104 A 2565 INDICATOR DOUG DC8 DC873F 302199F WP ESCAPE SLIDE OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 ESCAPE SLIDE PRESSURE IND SLIDE DOWN BELOW VIEWING WINDOW. REPOSITIONED ESCAPE SLIDE. 2 L 7 4 4F RT 4A25 2007110900212 20071109 00212 WP 2007 11 9 ABXA070361 1 20071023 A 5315 49157191 STRAP DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 FS 775, LEFT BUTT LINE 12, FLOORBEAM ATTACH STRAP CRACKED. REMOVED AND REPLACED ATTACH STRAP FS 775, LEFT BUTT LINE 12 IAW DC9 SRM. 2 L 7 2 4F A6WE 2007110900222 20071109 00222 EU 2007 11 9 TRAX200701627 1 20071029 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 SEAT TRACK RIGHT I/B BETWEEN FR 29 & 39 CORRODED. REMOVED CORROSION AS PER SRM 51-21-42 AND IS OUT OF LIMITS AS PER SR M 53-00-00 PART FABRICATED ON W/C 2000-210 SEAT TRACK REPAIRED IAW SRM 53-00-00 FIG 434 MATERIAL THICKNESS: 0.083 MATER IAL REMOVED: 0.062 OUT OF LIMITS AS PER SRM: 53-00-00. 2 H 7 2 4T RT 2007110900224 20071109 00224 EU 2007 11 9 TRAX200701632 1 20071029 A 5753 BRACKET AEROSP ATR72 ATR72 EU T/E FLAP BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 RIGHT O/B FLAP ARM OMEGA BRACKET AT RIB 10 BROKEN. REPLACED AND INSTALLED IAW AMM 20-21-12. 2 H 7 2 4T RT 2007110900235 20071109 00235 NM 2007 11 9 QXEA200701652 1 20071103 A 3231 DOOR BOMBDR DHC8 DHC8402 1390042 NM MLG STUCK A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 415QX 4081 EUG FLIGHT NR 2280: ALT GEAR EXTENSION DOOR STUCK OPEN. MAINTENANCE CLEANED AND LUBED ALT GEAR EXTENSION MANIFOLD ROD. OPS TEST GOOD. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007110900244 20071109 00244 NM 2007 11 9 SWAA075469 1 20071101 A 3350 147A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 245WN 32506 DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007110900254 20071109 00254 NM 2007 11 9 SWAA075472 1 20071101 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 409WN 27896 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007110900261 20071109 00261 NM 2007 11 9 SWAA075454 1 20071031 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900267 20071109 00267 NM 2007 11 9 SWAA075485 1 20071101 A 5330 65465767 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, STR BL 0. REPAIRED S KIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900269 20071109 00269 NM 2007 11 9 SWAA075483 1 20071101 A 5313 BAC1498 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 21R CORRODED AT BS 360. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007110900282 20071109 00282 EA 2007 11 9 A6WA200740583 1 20071013 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 469AW 7917 FOUND LT SIDE FS 621 TO FS 625.30 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. MAINTENANCE REMOVED LT INTERCOSTAL FS 621 TO FS 625.30 IAW CRJ 200 SRM 51-42-06. INSTALLED NEW INTERCOSTAL P/N 601-35012-51 IAW CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007110900285 20071109 00285 EA 2007 11 9 A6WA200740584 1 20071014 A 5520 LINK CNDAIR CL600 CL6002B19 1900309 EA ELEVATOR PCU DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 469AW 7917 RIGHT ELEVATOR NR 2 PCU ATTACH FITTING LINK, BOTTOM LOCK FASTENER HAS SHEARED. MAINTENANCE REMOVED SHEARED LOCK FASTENE R AND INSTALLED NEW SERVICEABLE LOCK FASTENER AND COLLAR IAW CRJ200 SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007110900286 20071109 00286 EA 2007 11 9 A6WA200740585 1 20071014 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 469AW 7917 FOUND RIGHT FS 621 FLOOR SUPPORT ANGLE CRACKED APPROX .75 INCH LONG. MAINTENANCE CUT AWAY DAMAGED SECTION OF ANGLE AND INSTALLED REPAIR ANGLE AND DOUBLE IAW BOMBARDIER REO 601R-53-61-117 REV C. (M) 2 L 7 2 4F RT A21EA 2007110900293 20071109 00293 NM 2007 11 9 SWAA075461 1 20071031 A 5311 6546536 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900296 20071109 00296 NM 2007 11 9 SWAA075480 1 20071101 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 700GS 27835 DURING SCHEDULED HC1 CHECK, FOUND HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 129.50. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900327 20071109 00327 NE 2007 11 9 NACA20070020 2 20071103 A 8530 356993 CYLINDER DOUG DC6 DC6A 3021706 WP PWA R2800 CB3 52026 NE NR 2 ENGINE CRACKED A NACA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 AL 03 6174C 1030 1030 44075 P33192 NR 2 ENGINE SHUT DOWN DUE TO RUNNING ROUGH. REPLACED NR 18 CYLINDER DUE TO CRACKED HEAD. REF: NAC DC-6 MM SECT V PG 16 AND 16A. 2 L 7 4 4R 4 R 6A3 E264 2007110900331 20071109 00331 NM 2007 11 9 EIA2007193 1 20071101 A 3350 S1356B37 LIGHT BOEING 747 747273C 1384896 NM R5 DOOR INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 470EV 20653 SOLDERBURG LIGHT ASSY AT R-5 DOOR INOP. REMOVED AND REPLACED WITH SERVICEABLE UNIT PER BOEING 747 MM 33-51-07. TESTED GOOD PER BOEING 747 MM 33-51-07 PAGE 202. 2 L 7 4 4F A20WE 2007110900337 20071109 00337 EU 2007 11 9 TRAX200701662 1 20071101 A 5753 RIB AEROSP ATR72 ATR72212 8680945 EU RT WING TE FLAP CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 RT O/B FLAP CAM GUIDE AT FLAP RIB 13 CORRODED. 2 H 7 2 4T RT A53EU 2007110900341 20071109 00341 EA 2007 11 9 TRAX200701667 1 20071101 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 PAX DOOR "EXIT" PLACARD ON STEP (832BT) IS DAMAGED. 2 L 7 2 4F RT A21EA 2007110900342 20071109 00342 EA 2007 11 9 TRAX200701669 1 20071101 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 PAX DOOR SKIN STRUCTURE UNDER STEP (832DT) IS CRACKED IN THE AFT RADIUS. REPAIRED PAX DOOR SKIN STUCTURE UNDER STEP (83 2 DT) BY PERFORMING REO-601R-52-11-702. 2 L 7 2 4F RT A21EA 2007110900343 20071109 00343 EA 2007 11 9 TRAX200701668 1 20071101 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 PAX DOOR SKIN STRUCTURE UNDER STEP (832DT) IS CRACKED IN THE FWD RADIUS. REPAIRED PAX DOOR SKIN STUCTURE UNDER STEP (83 2 DT) FWD RADIUS IAW REO 601R-52-11-702. 2 L 7 2 4F RT A21EA 2007110900351 20071109 00351 NM 2007 11 9 HNAA0700260 1 20071101 A 3350 6038443LB POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 826EX 389 DURING RON MAINTENANCE IT WAS FOUND THAT THE EMERGENCY LIGHTS ON THE RIGHT FWD EXIT WAS NOT WORKING. THE POWER SUPPLY W AS REMOVED AND REPLACED, OPS CHECK WAS GOOD. 2 H 7 2 4T RT A13NM 2007110900356 20071109 00356 NM 2007 11 9 KCSA071506 1 20071105 A 3350 LIGHT BOEING 747 747246F 1384850 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 705CK 21034 UPPER DECK AFT LEFT EMERGENCY LIGHT INOP. 2 L 7 4 4F RT A20WE 2007110900357 20071109 00357 NM 2007 11 9 KCSA071507 1 20071105 A 5330 SKIN BOEING 747 747246F 1384850 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 FUSELAGE SKIN DAMAGED AT BS 740 ABOVE STR 34L. 2 L 7 4 4F RT A20WE 2007110900358 20071109 00358 NM 2007 11 9 KCSA071508 1 20071105 A 5330 SKIN BOEING 747 747246F 1384850 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 FUSELAGE SKIN DAMAGED AT BS 460 BETWEEN STR 36R AND 37R. 2 L 7 4 4F RT A20WE 2007110900361 20071109 00361 NM 2007 11 9 HNAA0700261 1 20071103 A 2910 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM NLG LEAKING A HNAA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 826EX 389 DURING FLIGHT THE CAPTAIN REPORTED, THERE WAS SMOKE/FUMES IN THE COCKPIT. THE SMELL WAS BURNING THEIR EYES. IT WAS FOU ND THAT THE NOSE LANDING GEAR DOWN HYDRAULIC LINE HAD A PIN HOLE IN IT. HOLE WAS REPAIRED IAW DASH 8 MAINTENANCE MANUAL 20-50-55, THE FLUID THAT HAD BUILT UP WAS LEAKED AS WELL. LEAK AND OPS CHECK WERE GOOD. 2 H 7 2 4T RT A13NM 2007110900375 20071109 00375 NM 2007 11 9 SWAA075518 1 20071101 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 407 AND BS 414, STR 26L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900376 20071109 00376 NM 2007 11 9 SWAA075495 1 20071103 A 3350 417N5101001 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 L1 DOOR EMERGENCY EXIT SLIDE LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007110900387 20071109 00387 NM 2007 11 9 2007UALA04527 1 20071101 A 5712 RIB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 RT WING NR 2 FUEL TANK INTERIOR RIB AT STA 135.5 LOWER CHORD AT FORWARD UPPER EDGE OF STRINGER L2 CUT-OUT CRACKED. REPA IRED PER EA I7070802. REMOVED AND REPLACED RIB CHORD AT STA 135.5 STRINGER L2. 2 L 7 2 4F 4 F RT A16WE E2GL 2007110900394 20071109 00394 NM 2007 11 9 2007UALA04534 1 20071101 A 3397 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 517UA 24861 FOUND ROW 8 LEFT BULLNOSE EMERGENCY LIGHT INOP. RECONNECTED THE CONNECTOR AND SECURED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007111300006 20071113 00006 NM 2007 11 13 MWEA070274 1 20071105 A 7830 7150922505 ANGLE BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 907ME 55171 Z FRAME CRACKED AT RADIUS AT STATION 35.669 LEFT SIDE, BOTTOM BUCKET. FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F TR A6WE 2007111300011 20071113 00011 CE 2007 11 13 DXTA200702578 1 20071028 A 3243 991205018 MASTER CYLINDER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE RT BRAKE LEAKING E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 398QS 82 5600522 DURING TAXI OUT, CO-PILOTS RT BRAKE IS SPONGY CAUSING A/C TO VEER LT. FOUND CO-PILOTS RT MASTER CYLINDER LEAKING. REMO VED AND REPLACED MASTER CYLINDER WITH NEW UNIT. OPS AND LEAK CHECK GOOD AT THIS TIME. IAW CE 560 M/M 32-42-01 2 L 7 2 4F 4 F RT A22CE E25EA 2007111300012 20071113 00012 CE 2007 11 13 DXTA200702579 1 20071028 A 5610 NP13972110 WINDSHIELD CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE COCKPIT FAILED E DXTA O OTHER O OTHER DE DESCENT 1 GL 07 622QS 4997 5605286 WHILE DESCENDING THROUGH 12000 FT AT 250 KTS, THE RT SIDE FORWARD COCKPIT WINDSHIELD SHATTERED AND THE RT W/S FAULT LIGH T ILLUMINATED. 30-60 SECONDS LATER, THE RT WINDSHIELD SHATTERED, FOLLOWED BY THE LT W/S FAULT LIGHT ILLUMINATION. REMOV ED & INSTALLED NEW UNIT AND PERFORMED LEAK AND OPERATIONAL CHECK GOOD. WORK DONE IAW MM 56-11-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007111300013 20071113 00013 NE 2007 11 13 DXTA200702580 2 20071028 A 7320 263952 FLOW DIVIDER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE NR 1 ENGINE MALFUNCTIONED E DXTA O OTHER Y ENGINE STOPPAGE TX TAXI/GRND HDL 1 GL 07 327QS 3922 5600327 PCE500154 DURING SPEED BRAKE CHECK THE LT ENGINE SHUTDOWN. REMOVED AND REPLACED FLOW DIVIDER PERFORMED OPS CK AND LEAK CHECK NO D EFECTS FOUND OPS CHECK SPEED BRAKE SYSTEM OPS CHECK GOOD IAW MM CH 73-10. 2 L 7 2 4F 4 F RT A22CE E25EA 2007111300014 20071113 00014 CE 2007 11 13 DXTA200702581 1 20071029 A 3260 41EN496 SQUAT SWITCH CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LT MLG READS HIGH E DXTA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 302QS 9333 5600402 LOST CABIN PRESSURIZATION AT FL290. CABIN PRESSURE ROSE TO 13500 PA AND STABILIZED. ON DESCENT, CABIIN PRESSURE DESCEND ED WITH THE AIRCRAFT ALTITUDE. FOUND LT SQUAT SWITCH TO HAVE HIGH RESISTANCE AND CHANGING WITH PRESSURE ON ARM. REPLACE D SWITCH WITH NEW IAW 560 MM 32-61-00. OPS CKED GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2007111300144 20071113 00144 WP 2007 11 13 UPS07851093 1 20071011 A 5310 FINGER DOUBLER DOUG DC8 DC873F 302199F WP FS 123 L31R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 FINGER DOUBLER AT STA 123 L31R IS CORRODED AND CRACKED. REMOVED, FABRICATED, AND INSTALLED REPAIR FI NGER DOUBLER AT STA 123 L31R IAW SRM 51-1-20D, AND DWG 5773316. 2 L 7 4 4F RT 4A25 2007111300166 20071113 00166 WP 2007 11 13 NWAA073709873 1 20071104 A 2150 DUCT DOUG DC9 DC951 3022051 WP LT ACM CRACKED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 782NC 48107 AS THE AIRCRAFT CLIMBED THROUGH 4000 FEET, THE FLIGHT ATTENDANTS INFORMED THE COCKPIT CREW THAT THE AFT RIGHT LAVATORY S MOKE DETECTOR WAS SOUNDING AND THAT THE CABIN HAD A HOT SMELL. FLIGHT CREW MADE NOTE OF POWER SETTINGS AND RETURNED TO A NORMAL SAFE LANDING BACK AT MSP. NO MENTION OF COMPLIANCE OR CABIN HEAT SELECTOR POSITION. MAINTENANCE PERFORMED "SM OKE IN CABIN" TROUBLESHOOTING PROCEDURES AND FOUND A CRACKED DUCT BETWEEN THE LEFT ACM AND COALESCER BUT NO SOURCE OF SM OKE. AFTER THE DUCT WAS REPLACED AND THE COALESCER BAGS CHANGED, PACK BURN OUT PROCEDURES WERE COMPLIED WITH. THE AIRC RAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007111300167 20071113 00167 NM 2007 11 13 AALA20072134 1 20071104 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 379AA 25448 MIA - EXTERNAL EMERGENCY LIGHT AT LEFT AFT OF WING INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT LEFT AFT OF WING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007111300168 20071113 00168 NM 2007 11 13 AALA20072121 1 20071101 A 2100 EXHAUST VALVE BOEING 767 767323 1385205 NM EQUIP COOLING BROKEN A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SW 21 378AN 25447 CVG INFLIGHT T1697/01NOV - FORWARD EQUIPMENT OVERHEAT CAUTION LIGHT ILLUMINATED. LANDED CVG WITHOUT INCIDENT. FOUND EQ UIPMENT COOLING EXHAUST VALVE BROKEN. REPLACED EQUIPMENT COOLING EXHAUST VALVE AND DUCT WORK. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007111300169 20071113 00169 NM 2007 11 13 AALA20072122 1 20071102 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 347AN 33086 MIA - EMERGENCY LIGHT AT OVERHEAD BETWEEN SEATS 3G AND 3H INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD BE TWEEN SEATS 3G AND 3H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007111300170 20071113 00170 NM 2007 11 13 AALA20072123 1 20071102 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 787AL 30010 ORD - EMERGENCY LIGHT AT OVERHEAD RIGHT SIDE AT SEAT ROW 31 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD RIGHT SIDE AT SEAT ROW 31. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007111300171 20071113 00171 WP 2007 11 13 AALA20072131 1 20071103 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 973TW 53623 SJC - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 5E TO 18D INOPERATIVE. CLEANED CONNECTOR FOR BATTERY PACK B523 FOR EMERGEN CY LIGHTS AT OVERHEAD SEAT ROWS 5E TO 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007111300172 20071113 00172 NM 2007 11 13 AALA20072138 1 20071104 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971AN 29547 MIA - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. RESET CONNECTOR FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOO R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007111300173 20071113 00173 WP 2007 11 13 AALA20072145 1 20071104 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 485AA 49678 DFW - SEAT MOUNTED EMERGENCY LIGHT AT AFT SEAT 7D BROKEN. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHT AT A FT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007111300174 20071113 00174 WP 2007 11 13 AALA20072146 1 20071104 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 485AA 49678 DFW - SEAT MOUNTED EMERGENCY LIGHT AT AFT SEAT 18D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGH T AT AFT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007111300175 20071113 00175 WP 2007 11 13 AALA20072133 1 20071103 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 973TW 53623 SJC - EMERGENCY LIGHTS AT OVERHEAD RIGHT AFT LAVATORY INOPERATIVE. CLEANED CONNECTOR FOR BATTERY PACK B527 FOR EMERGENC Y LIGHTS AT OVERHEAD RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007111300176 20071113 00176 EU 2007 11 13 AALA20072135 1 20071104 A 2913 PUMP AIRBUS 300 A300B4605R 3930308 EU HYD SYSTEM INOPERATIVE A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 25071 514 MIA INLFIGHT T902/04NOV - CREW REPORTED YELLOW HYDRAULIC SYSTEM OVERHEAT. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE DRIVEN PUMP YELLOW SYSTEM, NUMBER TWO ENGINE CASE DRAIN FILTER AND RESERVOIR FILTER FOR YELL OW HYDRAULIC SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007111300177 20071113 00177 EU 2007 11 13 AALA20072124 1 20071102 A 2750 JACKSCREW AIRBUS 300 A300B4605R 3930308 EU TE FLAPS INOPERATIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 80058 466 SJU INFLIGHT T861/02NOV - DUAL FLAP FAULT ON APPROACH. LANDED SJU WITHOUT INCIDENT. LUBRICATED RIGHT WING JACK SCREW N UMBER TWO. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007111300178 20071113 00178 NM 2007 11 13 AALA20072126 1 20071102 A 2750 TRANSMISSION BOEING 757 757223 1384957 NM TE FLAP TRIPPED A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 671AA 25336 AUA INFLIGHT T1013/02NOV - TRAILING EDGE FLAP DISAGREE LIGHT ILLUMINATED ON APPROACH. LANDED AUA WITHOUT INCIDENT. FOU ND LEFT INBOARD TRAILING EDGE FLAP TRANSMISSION TRIPPED. RESET AND LUBED FLAP ROLLERS AND JACK SCREW. SYSTEM CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007111300179 20071113 00179 NM 2007 11 13 AALA20072127 1 20071102 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 611AM 24487 MIA - EMERGENCY LIGHT AT OVERHEAD SEAT 12ABC INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 12ABC. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007111300180 20071113 00180 NM 2007 11 13 AALA20072128 1 20071102 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 198AA 32392 DFW - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 9 TO 15 INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 9 FOR SEAT MOUN TED EMERGENCY LIGHTS AT SEAT ROWS 9 TO 15. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007111300181 20071113 00181 NM 2007 11 13 AALA20072130 1 20071103 A 2560 FLASHLIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 976AN 30099 MIA - EMERGENCY FLASHLIGHT AT AFT FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT AT AFT FLIGHT ATTEND ANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007111300182 20071113 00182 WP 2007 11 13 AALA20072132 1 20071103 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 973TW 53623 SJC - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 21D TO 28D INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD SEAT 25F FOR EME RGENCY LIGHTS AT OVERHEAD SEAT ROWS 21D TO 28D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007111300183 20071113 00183 NM 2007 11 13 AALA20072137 1 20071104 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971AN 29547 MIA - EMERGENCY LIGHT AT RIGHT OVERWING EXIT DOOR INOPERATIVE. RESET CONNECTOR FOR EMERGENCY LIGHT AT RIGHT OVERWING EX IT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007111300184 20071113 00184 WP 2007 11 13 AALA20072144 1 20071104 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 485AA 49678 DFW - EMERGENCY EXIT SIGN LIGHT FORWARD OF FORWARD SERVICE DOOR BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT SIGN LIGHT FORWARD OF FORWARD SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007111300185 20071113 00185 WP 2007 11 13 AALA20072149 1 20071104 A 2560 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 485AA 49678 DFW - EMERGENCY FLASHLIGHT AT FORWARD CABIN INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT AT FORWARD CABIN. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007111300186 20071113 00186 NM 2007 11 13 AALA20072125 1 20071102 A 7930 21SN04224 PRESSURE SWITCH BOEING 767 767323 1385205 NM LT ENGINE INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 352AA 24033 YYR INFLIGHT T88/02NOV ORD TO BRU - LEFT ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. CREW SHUT DOWN LEFT ENGINE. LANDE D YYR WITHOUT INCIDENT. SINGLE ENGINE TIME SIX MINUTES. REPLACED OIL SCAVENGE FILTER. NO DEBRIS FOUND ON OIL SCAVENGE FILTER. REPLACED OIL FILTER DIFFERENTIAL PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007111300187 20071113 00187 NM 2007 11 13 AALA20072129 1 20071102 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 198AA 32392 DFW - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 26 TO 36 INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 26 TO 36. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007111300188 20071113 00188 NM 2007 11 13 AALA20072136 1 20071104 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971AN 29547 MIA - EMERGENCY LIGHT AT SEAT 17D INOPERATIVE. RESET CONNECTOR FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007111300189 20071113 00189 WP 2007 11 13 AALA20072142 1 20071104 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 485AA 49678 DFW - EMERGENCY LIGHT AT RIGHT FORWARD OVERWING EXIT SIGN HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RIGHT FORWARD OVERWING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007111300190 20071113 00190 WP 2007 11 13 AALA20072150 1 20071104 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 485AA 49678 DFW - EMERGENCY EXIT SIGN LIGHT AT AFT STAIR DOOR BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT SIGN LIGHT AT AFT STAIR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007111300191 20071113 00191 NM 2007 11 13 AALA20072139 1 20071104 A 3397 CONNECTOR BOEING 737 737823 13844CB NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971AN 29547 MIA - EMERGENCY LIGHT AT RIGHT LOWER GALLEY INOPERATIVE. RESET CONNECTOR FOR EMERGENCY LIGHT AT RIGHT LOWER GALLEY. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007111300192 20071113 00192 NM 2007 11 13 AALA20072140 1 20071104 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971AN 29547 MIA - EMERGENCY LIGHT AT OVERHEAD SEAT 7D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 7D. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007111300193 20071113 00193 NM 2007 11 13 AALA20072141 1 20071104 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971AN 29547 MIA - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007111300194 20071113 00194 WP 2007 11 13 AALA20072147 1 20071104 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 485AA 49678 DFW - SEAT MOUNTED EMERGENCY LIGHT AT FORWARD SEAT 21D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHT AT FORWARD SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007111300195 20071113 00195 WP 2007 11 13 AALA20072148 1 20071104 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 485AA 49678 DFW - EMERGENCY EXIT ARROW SIGN LIGHT AT AFT LEFT SERVICE DOOR INOPERATIVE. REPLACED BATTERY PACK AB54 FOR EMERGENCY EX IT ARROW SIGN LIGHT AT AFT LEFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007111300196 20071113 00196 WP 2007 11 13 AALA20072143 1 20071104 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 485AA 49678 DFW - EMERGENCY EXIT SIGN LIGHT AT FORWARD GALLEY AISLE WALL AT FLOOR IS BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT SIGN LIGHT AT FORWARD GALLEY AISLE WALL AT FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007111300197 20071113 00197 NM 2007 11 13 07FDEA04727 1 20071107 A 5754 SKIN DOUG MD11 MD11F 3023600 NM LT WING LE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 591FE 48527 LEFT WING, FIXED LEADING EDGE SKIN AT STATION XOS 467 TO XOS 479 FOUND CHAFED. CHAFED MARK SMOOTHENED OFF AS PER SRM 51-21-01 VOLUME II. MATERIAL REMOVED = 0.026", ORIGINAL THICKNESS = 0.090", REMAINING THICKNESS = 0.064" AT STA XOS 467 TO XOS 473 AND FOUND EXCEEDED LIMIT AS PER SRM 57-10-00 FIGURE 13 VOLUME I. CARRIED OUT REPAIR AT STA XOS 467 TO XOS 473 AS PER SRM 57-10-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007111300198 20071113 00198 NM 2007 11 13 07FDEA04728 1 20071107 A 5753 SKIN DOUG MD11 MD11F 3023600 NM TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 591FE 48527 LEFT WING, INBOARD FLAP INBOARD SEGMENT LOWER SURFACE FOUND WITH DENT. CARRIED OUT REPAIR AS PER SRM 57-10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007111300199 20071113 00199 NM 2007 11 13 07FDEA04730 1 20071107 A 5753 SKIN DOUG MD11 MD11F 3023600 NM RT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 591FE 48527 RIGHT WING INBOARD FLAP OUTBOARD AFT SEGMENT LOWER SKIN FOUND DENTED. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 2 V OLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007111400001 20071114 00001 NM 2007 11 14 5700 1 20071027 A 5720 STIFFENER BOEING 727 727212 138407G NM LT WING CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 41343 21945 LEFT WING REAR SPAR VERTICAL STIFFENER CORRODED AT LOWER END W.S. 200 2 L 7 3 4F A3WE 2007111400002 20071114 00002 NM 2007 11 14 MWEA070279 1 20071104 A 2530 2530127 OVEN BOEING 717 717200 1383700 NM GALLEY INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 908ME 55172 FLIGHT ATTENDANT REPORTED NR 3 OVEN MADE A STRANGE SOUND WHEN TURNED ON, FOLLOWED BY A ELECTRICAL SMELL. REMOVED AND RE PLACED NR 3 OVEN. 2 L 7 2 4F TR A6WE 2007111400005 20071114 00005 NM 2007 11 14 MWEA070282 1 20071102 A 5320 SG095500053 CUSP WEB DOUG MD88 MD88 3023688 NM BS 260-579 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 601ME 49762 CORROSION ON RIGHT FLOOR SUPPORT STRUCTURE PASSENGER CUSP MEMBRANE CABIN BETWEEN STATION 1138-1165. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 2007111400007 20071114 00007 NM 2007 11 14 MWEA070285 1 20071102 A 5320 SG095300053 CUSP WEB DOUG MD88 MD88 3023688 NM BS 845-826 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 601ME 49762 CORROSION ON FLOOR SUPPORT STRUCTURE PASSENGER CABIN CUSP MEMBRANE LEFT STATION 845-826. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 2007111400008 20071114 00008 NM 2007 11 14 MWEA070286 1 20071102 A 5320 SG095300053 CUSP WEB DOUG MD88 MD88 3023688 NM BS 1212-1231 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 601ME 49762 CORROSION ON RIGHT FLOOR SUPPORT STRUCTURE PASSENGER CUSP MEMBRANE CABIN BETWEEN STATION 1212-1231. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 2007111400012 20071114 00012 EU 2007 11 14 07FDEA04732 1 20071010 A 5540 A5537010600600 ARM AIRBUS 310 A310324 3930206 EU RUDDER HINGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 802FD 542 NR 2 RUDDER HINGE ARM WITH CORROSION IN LUG BORE. REPAIRED IN ACCORDANCE WITH FEDEX EA 6-5510-115292. 2 L 7 2 4F RT A35EU 2007111400015 20071114 00015 EU 2007 11 14 07FDEA04735 1 20071010 A 5540 A5537009700400 ARM AIRBUS 310 A310324 3930206 EU RUDDER HINGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 802FD 542 NR 4 RUDDER HINGE ARM WITH CORROSION AT LUG BORES. REPAIR ACCOMPLISHED IN ACCORDANCE WITH 6-5510-115292. 2 L 7 2 4F RT A35EU 2007111400016 20071114 00016 NM 2007 11 14 07FDEA04736 1 20071107 A 5311 90522692 FRAME BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 UPPER FUSELAGE STATION 720D FRAME, AFT EDGE IS CORRODED AT STRINGER 4 RIGHT REMOVED CORROSION AT UPPER FUSELAGE STA 720D FRAME AFT EDGE AT STR 4 RIGHT AREA REF SRM 51-10-6 ORIGINAL MATERIAL .064", MATERIAL REMAINING .048", MATERIAL LOSS .01 6'. FOUND TO BE OUT OF LIMITS REF, SRM 53-10-1 FIG 1. FABRICATED REPAIR DOUBLER, REF SRM 51-40-3 FIG 1, MATERIAL USED 7075-0 .063, HEAT TREATED TO T-6. TRACKING NR 2007-11-015. TREATED AND PRIMED DOUBLER AND INSTALLED REF 51-10-2, 51-30 -2 THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007111400018 20071114 00018 NM 2007 11 14 07FDEA04739 1 20071107 A 5347 BAC1520792 SEAT TRACK BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 AFT CABIN CENTER SEAT TRACK RIGHT FLANGE UPPER SURFACE CORRODED BETWEEN BS 1100-1110 REMOVED CORROSION VERIFIED REMOVAL TO BE OUT OF LIMITS ORIG THICKNESS .0947 REMAINING .0536 REMOVED .0411. FABRICATED SEAT TRACK AND REPAIR STRAP AND ANGL ES. INSTALLED REPAIR AND SEAT TRACK. REF SRM 53-10-5 FIG 1, SRM 53-10-1 FIG 3 THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007111400020 20071114 00020 WP 2007 11 14 07FDEA04741 1 20071107 A 5730 ARB1232504 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 RT WING L/E DURING INSPECTION REPAIR ASSESMENT FOUND NR 3 DENTS ON EXT SKIN, 1.5" BY 1.5" DEEP .09", 1" BY 1.5" DEEP .04 ",BY 1" BY 1" DEEP .07". REPAIRED AREA IAW SRM 57-10-00 VOL I FIG 40. 2 L 7 3 4F RT A22WE 2007111400021 20071114 00021 NM 2007 11 14 07FDEA04742 1 20071107 A 5314 6518636 KEELBEAM BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 LOWER FUSELAGE STATION 742, RBL 1 TO RBL 4, KEEL BEAM LOWER WEB CORRODED, REMOVED CORROSION IN REF TO SRM 51-10-1 PG 1, ORIG MAT'L .080, MAT'L REMAINING .045', OUT OF LIMITS. REMOVED DAMAGE AREA OF KEEL BEAM WEB 51-10-2 PG 10. FABRICATED DOUBLER AND FILLER IN REF TO SRM 51-40-2 FIG 1. TREAT AND PRIMED DOUBLER AND FILLER AND INSTALLED REF MM 51-20-021-07, MM 51-20-031-07. 2 L 7 3 4F A3WE 2007111400024 20071114 00024 NM 2007 11 14 DLM90071395 1 20071029 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 705 LBL 24 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 CABIN SEAT TRACK CORRODED OUT OF LIMITS FS 705 LBL 24. REMOVED AND REPLACED SEAT TRACK FS 705 LBL 24 PER SRM 53-40-01 V OL II ON N/R 2700-0210 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007111400027 20071114 00027 NM 2007 11 14 DLM88071400 1 20071031 A 2120 5924037513 DUCT DOUG MD88 MD88 3023688 NM BLOWN A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 27 995DL 53362 TAIL COMPARTMENT HIGH MSG FL 180 AND CLIMBING. FOLLOWED QRH LIGHT EXTINGUISHED AND THEN CAME BACK ON. DURING DESCENT T O ATL LIGHT STAYED EXTINGUISHED. MTC IS PROGRESS DNTC. FOUND DUCT ASSY BLOWN REF: 21-20-00-04 ITEM 385 MFG NR 5924037 -513 DUCT ASSY (HEADER). 2 L 7 2 4F RT A6WE 2007111400028 20071114 00028 NM 2007 11 14 DL76S071402 1 20071101 A 2822 5006003D PUMP BOEING 767 767332 1382001 NM FUEL SYSTEM FAILED A DALA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 131DN 24852 LEFT AFT FUEL PUMP FAILED, LIGHT AND EICAS, THEN 20 MINUTES LATER THE LT FWD FUEL PUMP FAILED. GOT BOTH PUMP LOW PRESS LIGHT AND L FUEL SYSTEM PRESS EICAS. REPLACED BOTH FUEL BOOST PUMPS (BORROWED FROM AA IN LAX). 2 L 7 2 4F RT A1NM 2007111400029 20071114 00029 NM 2007 11 14 DL76L071403 1 20071102 A 5330 141T32133 SKIN BOEING 767 767332 1382001 NM BS 179, LBL 28 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 175DN 24803 FUSELAGE SKIN HAS A DENT AT STA 179, LBL 28. CUTOUT THE DAMAGED SKIN AN INSTALLED A REPAIR DOUBLER/TRIPLER. 2 L 7 2 4F RT A1NM 2007111400031 20071114 00031 NM 2007 11 14 DL76L071405 1 20071102 A 3110 LAMP BOEING 767 767332 1382001 NM IDG INDICATOR INOPERATIVE A DALA D RETURN TO BLOCK P NO WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 192DN 28449 RTB DUE TO RT IDG GEN LIGHT INOP. MTC RELAMPED. NO HELP. CLEANED CONNECTOR, OPS CK GOOD. 2 L 7 2 4F RT A1NM 2007111400036 20071114 00036 NM 2007 11 14 DL738071410 1 20071105 A 5210 DOOR BOEING 737 737832 13844CF NM L1 OUT OF RIG A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 3732J 30380 1L DOOR NOT SEATED. UNABLE TO MAINTAIN CABIN PRESSURE. DEADHEADING CAPT INSPECTED DOOR, OBSERVED DOOR ROLLER OUT OF EN GAGEMENT WITH 1/2" TO 3/4" GAP AT TOP TO BOTTOM OF DOOR. RETURNED TO JFK. FOUND DOOR OUT OF RIG. ADJUSTED DOOR RIGGIN G, OPS NOW OK. 2 L 7 2 4F RT A16WE 2007111400037 20071114 00037 NM 2007 11 14 DLM88071411 1 20071105 A 5330 59360033 SKIN DOUG MD88 MD88 3023688 NM BS 598 S22R DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 LIGHTNING STRIKES AT L-22R FS 598 RESULTED IN TWO 1.25" DIAMETER HOLE CUTOUTS. AN INTERNAL TITANIUM FINGER DOUBLER WAS INSTALLED AS THE REPAIR. 2 L 7 2 4F RT A6WE 2007111400039 20071114 00039 NE 2007 11 14 DLM88071413 2 20071106 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE LEFT SHUTDOWN A DALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 27 903DE 40528 53380 725790 AT FL320, THE LEFT ENGINE SHUT DOWN. THE N2/HYD PRESSURE/OIL PRESSURE WENT TO -0-. THE ENGINE WINDMILLED FOR 25 MINS W ITH -0- OIL PRESSURE. REMOVED AND REPLACED NR 1 ENGINE PER TRAS 9T102. 2 L 7 2 4F 4 F RT A6WE E9NE 2007111400040 20071114 00040 2007 11 14 DL738071414 4 20071106 A 2397 CONNECTOR BOEING 737 737832 13844CF NM ENTERTAIN SYS BURNED A DALA J A DUMP FUEL UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 3751B 29669 PASSENGER REPORTED SMALL AMOUNT OF SMOKE CAME FRM UNDER SEAT2AD. AUDIO ENT SYS WENT INOP AFTER SEEING SMOKE. CREW TURN ED OFF MASTER ENT SWITCHES AND PULLED C/BS TO ISOLATE ENT SYS SMOKE AND SMELL DISSIPATED. MTC FOUND SEAT ELEC UNIT UNDE R SEAT 2A BURNED. DISCONNECTED CONNECTORS FRM SEU. TURNED OFF AUDIO/VIDEO MASTER SWITCHES AND PULLED ENT C/BS TO ISOLA TE PASS ENT SYS. FWD TO MCO AND PLAC. REPLACED 2A SEB AND CABLE ASSEMBLY FROM 1A TO 2A. POWER TO RIGHT SIDE ENTERTAIN MENT SYSTEM CHECKS GOOD. MCO/PLAC REMOVED. 2 L 7 2 4F RT A16WE 2007111400042 20071114 00042 NM 2007 11 14 DLM90071417 1 20071001 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 924-962 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 RT CUSP WEB CORRORED OUT OF LIMITS FS 924-962 RBL 54. REPAIRED RT CUSP WEB IAW ERA 398191-14MA REV ORG 9-18-02 ON N/R 2 400-0234 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007111400043 20071114 00043 NM 2007 11 14 DLM90071418 1 20071001 A 5320 MEMBRANE DOUG MD90 MD9030 3023690 NM FS 195-200 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 FWD CABIN SUBFLOOR MEMBRANE CORRODED AT FS 195-200 RBL 54. REPAIRED WEB IAW MD-90 SRM 51-11-01 ON N/R 2400--0283 AT HMV -2 IN OKC. 2 L 7 2 4F RT A6WE 2007111400045 20071114 00045 NM 2007 11 14 DLM90071420 1 20071104 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM FS 1140-1160 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 CABIN SEAT TRACK CORRODED OUT OF LIMITS FS 1140-1160 RBL 54. REMOVED AND REPLACED SEAT TRACK IAW MD-90 SRM 53-40-01 VOL I FIG 6 ON N/R 2700-0202 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007111400046 20071114 00046 NM 2007 11 14 DLM90071421 1 20071001 A 5530 ANGLE DOUG MD90 MD9030 3023690 NM VERTICAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 VERTICAL STABILIZER ANGLE IS CRACKED ON RT SIDE BELOW INLET SCOOP. REMOVE AND REPLACE ANGLE IAW MD-90 SRM 51-30-05 ON N /R 3000-0048 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007111400048 20071114 00048 NM 2007 11 14 DLM90071423 1 20071001 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM FS 485-579 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 CABIN SEAT TRACK CORRODED OUT OF LIMITS FS 485-579 RBL 24. REPAIRED SEAT TRACK IAW MD-90 SRM 53-40-01 FIG 6 VOL I ON N/ R 2700-0208 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007111400049 20071114 00049 NM 2007 11 14 DLM90071424 1 20071010 A 5310 DOUBLER DOUG MD90 MD9030 3023690 NM CARGO BAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 MID CARGO LOWER JAMB DOUBLER PLATE HAS CORROSION FROM FWD END TO AFT END REF TASK 53-12-02-02. REPAIRED LOWER DOOR JAMB DOUBLER IAW MD-90 53-05D FIG 63 ON N/R 1000-0043 ON HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007111400050 20071114 00050 NM 2007 11 14 DLM90071425 1 20071031 A 5754 SKIN DOUG MD90 MD9030 3023690 NM NR 3 SLAT GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 RT WING SKIN GOUGED 20 INCHES I/B OF NUMBER 3 SLAT TRK. REPAIRED RT WING L/E IAW MD-90 SRM 57-20-01 FIG 11 VOL 1 ON N/R 6200-0040 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007111400051 20071114 00051 NM 2007 11 14 DLM90071426 1 20071031 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM FS 455-530 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 CABIN SEAT TRACK CORRODED OUT OF LIMITS FS 455-530 LBL 24. REPAIR SEAT TRACK IAW MD-90 SRM 53-40-01 FIG 6 VOL II ON N/R 2700-0209 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007111400053 20071114 00053 NM 2007 11 14 DLM90071428 1 20071031 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM FS 237 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 CABIN SEAT TRACK CORRODED OUT OF LIMITS FS 237 RBL 24. REPAIRED CABIN SEAT TRACK IAW MD-90 SRM 53-40-01 FIG B VOL I ON N/R 2700-0207 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007111400054 20071114 00054 NM 2007 11 14 DLM90071429 1 20071106 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM FS 826 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 CABIN SEAT TRACK CORRODED OUT OF LIMITS FS 826 RBL 24. REPAIRED SEAT TRACK IAW MD-90 SRM 53-40-01 VOL I FIG 6 ON N/R 27 00-0205 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007111400055 20071114 00055 NM 2007 11 14 DLM90071430 1 20071106 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM FS 598-700 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 CABIN SEAT TRACK CORRODED OUT OF LIMITS FS 598-700 RBL 24. REPAIRED SEAT TRACK IAW MD-90 SRM 53-40-01 FIG 6 VOL I ON N/ R 2700-0204 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007111400057 20071114 00057 NM 2007 11 14 QXEA200701704 1 20071104 A 3233 468305 ACTUATOR BOMBDR DHC8 DHC8402 1390042 NM MLG DOOR MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 425QX 3181 3181 4039 MSO FLIGHT NR 2397: UPON TAKEOFF AND LANDING, GEAR RETRACTION RIGHT MAIN GEAR DOOR REMAINED OPENED WITH RIGHT GEAR DOOR UNSAFE INDICATION. FLIGHT CONTINUED TO SEA. MAINTENANCE REMOVED AND REPLACED THE RT MLG DOOR ACTUATOR AND RT MLG SOLEN OID SEQUENCE VALVE (P/N 48302-3, S/N FAH0151). INSPECTED WIRING BETWEEN PSEU AND SOLENOID VALVE AND FLUSHING, RESERVICE D AND BLED RT MLG HYDRAULIC SYSTEM. ACCOMPLISHED 25 LANDING GEAR EXTENSION, RETRACTION CYCLES IAW DHC-8-400 AMM TASK 32 -31-00-710-801 AND 5 ALTERNATE CYCLES IAW TASK 32-34-00-710-801. ALL CHECKS ARE GOOD. NO DEFECTS NOTED. OPS CHECK FLI GHT WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007111400059 20071114 00059 EA 2007 11 14 SIMA200731202 1 20071106 A 5610 234523127 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT FAILED A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 511AE 10107 CREW REPORT THAT AT FL 360 THE CAPT FWD WINDOW SHATTERED. CREW DIVERTED TO STL. REMOVED AND REPLACED CAPT FORWARD WIND SHIELD IAW CRJ 700 AMM 56-11-01. ISSUED TDMI FOR BLANKET. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007111400061 20071114 00061 NM 2007 11 14 MWEA070289 1 20071107 A 5315 9936656U30 FLOORBEAM DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 601ME 49762 LEFT AFT LAVATORY FLOORBEAM HAS CORROSION LBL 18. REMOVED CORROSION, REMOVED AND REPLACED FLOORBEAM. 2 L 7 2 4F RT A6WE 2007111400062 20071114 00062 WP 2007 11 14 MWEA070290 1 20071107 A 3350 1001191 BATTERY PACK DOUG DC9 DC981 3022081 WP EMERGENCY LIGHTS INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 814ME 48010 EMERGENCY LIGHTS ON REAR OVERHEAD PANEL WOULD NOT ILLUMINATE WITH SWITCH ON. REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 2007111400064 20071114 00064 EA 2007 11 14 TRAX200701682 1 20071104 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 920EV 7810 FOUND RT FORWARD EXTERIOR EMERGENCY LIGHT IS INOP. 2 L 7 2 4F RT A21EA 2007111400065 20071114 00065 EU 2007 11 14 TRAX200701641 1 20071030 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 FOUND FLOORBEAM 39 CORRODED, RESOLVED ON W/O: 74559 TASKCARD: N/R-00277. FLOORBEAM 39 CORROSION REMOVED IAW SRM 51-21-4 2 BUT IT IS OUT OF LIMIT AS PER SRM 53-61-00 FIG 301. FLOORBEAM 39 REPAIRED IAW SRM 53-00-00 FIG 450. FABRICATION OF P ARTS COVER ON W/C 2000-111 MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.027, OUT OF LIMITS AS PER SRM: 53-61-00 FIG 301 . 2 H 7 2 4T RT A53EU 2007111400067 20071114 00067 NM 2007 11 14 07FDEA04747 1 20071107 A 5730 SKIN DOUG MD11 MD11F 3023600 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 591FE 48527 LEFT WING FIXED LEADING EDGE NR 12 SLAT TRACK CUTOUT AT STATION XOS 774 FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 57 -10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007111400068 20071114 00068 NM 2007 11 14 07FDEA04748 1 20071107 A 5311 FRAME DOUG MD11 MD11F 3023600 NM BS 1701 L12L DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 591FE 48527 CABIN, LEFT STA 1701 L-12 FRAME FOUND DENTED. CARRIED OUT REPAIR AS PER SRM 53- 30-00 FIGURE 1 VOLUME I. REPAIR CLAS SIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007111400069 20071114 00069 NM 2007 11 14 07FDEA04749 1 20071107 A 5311 FRAME DOUG MD11 MD11F 3023600 NM BS 1721 L12L DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 591FE 48527 CABIN, LEFT STA 1721 L-12 FRAME FOUND DENTED. CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASS IFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007111400071 20071114 00071 NM 2007 11 14 07FDEA04751 1 20071107 A 5313 STRINGER BOEING 757 7572B7 1384964 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 BULK CARGO AREA STA 1510 - S29R - AREA ON STRINGER EXFOLIATED. BLENDED AREA IAW SRM 53-60-03 FIG NR 101 DETAIL 1 STA 15 10 S29R. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-03, L 3.0" BY W 2.0" BY D .039". REMOVED DAMAGED STR STA 1510 IAW SRM 53-00-03. REMOVED STRINGER CLIP PER SRM 51-40-02 STA 1520 S29R. FABRICATED REPAIR STR FROM 1498 -204 BATCH NR 1303 562 AND FABRICATED FILLER FROM 7075-T6 .090 BATCH NR 001217927 IAW SRM 53-00-03 FIG NR 202. INSTALLED SPLICE REPAIR STA 1520 S29R IAW SRM 53-00-03 REPAIR NR 2 PAGE 201 DETAIL 1. FABRICATED STRINGER CLIP FROM MAT BAC 1518 NR 1360-3376 7075 -T6 IAW SRM 51-10-02. REPAIR ACCEPTED PER EAR 67597370077. 2 L 7 2 4F RT A2NM 2007111400074 20071114 00074 2007 11 14 HALA0700473 4 20071106 A 2310 TRANSMITTER BOEING 767 7673G5 1385126 NM LT HF SYSTEM INOPERATIVE A HALA O OTHER O OTHER CR CRUISE 1 WP 13 585HA 24259 ETOPS SIGNIFICANT SYSTEM LEFT HF WILL NOT TUNE OR TRANSMIT. RECEPTION OK RAN SYSTEM TEST PER AMM TASK 23-11-00-735-042 ALL TEST NORMAL. 2 L 7 2 4F RT A1NM 2007111400075 20071114 00075 NM 2007 11 14 HALA0700468 1 20071029 A 5320 146T5705 BRACKET BOEING 767 76733A 1385209 NM BS 1480 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 ANGLE BRACKET HAS CORROSION AT STATION 1480 LBL 71 BELOW AFT LEFT LAV DOOR THRESHOLD. REPLACED BRACKET PER DRAWING 146T 5705 AND SRM 51-40-06. 2 L 7 2 4F RT A1NM 2007111400076 20071114 00076 NM 2007 11 14 HALA0700469 1 20071022 A 5347 654T05131146 SEAT TRACK BOEING 767 76733A 1385209 NM BS 1208-1428 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 SEAT TRACK CORRODED BEYOND SRM LIMITS AT STN 1208 TO 1428 RBL 88.5. REPLACED SEAT TRACK IAW 767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007111400078 20071114 00078 NM 2007 11 14 HALA0700470 1 20071106 A 5420 313T3355233 DOUBLER BOEING 767 76733A 1385209 NM NR 1 NACELLE CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 NR 1 ENGINE NACELLE LOWER PAN DOUBLER AT NAC STA 352 CRACKED. REPLACED DOUBLER PER SRM 51-40-02 AND DRAWING 313T3355. 2 L 7 2 4F RT A1NM 2007111400079 20071114 00079 2007 11 14 HALA0700472 4 20071106 A 2397 9640453011 COUPLER BOEING 767 76733A 1385209 NM NR 1 HF SYSTEM DAMAGED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM NR 1 HF WOULD NOT INITIALIZE. REPLACED NR 1 HF COUPLER UNIT PER AMM 23-11-61. 2 L 7 2 4F RT A1NM 2007111400080 20071114 00080 NM 2007 11 14 HALA0700474 1 20071024 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 654 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 LEVEL 2 CORROSION SECTION 43 SEAT TRACK CORROSION BEYOND SRM LIMITS AT STA 654+56 THRU 654+66 RBL 20. REPLACED SEAT TRA CK PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007111400082 20071114 00082 2007 11 14 QXEA200701707 4 20071108 A 3425 7003360941 AHRS DHAV DHC8 DHC8202 2809007 NM NR 2 INOPERATIVE A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 379PH 12192 12192 530 RDM - ON FLIGHT 2034, RETURNED TO GATE, AHRS DATA INVALID AND HSI HEADING MISMATCH ADVISORY MESSAGE. MAINTENANCE REMOVE D AND REPLACED NR 2 AHRS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007111400083 20071114 00083 NM 2007 11 14 MWEA070291 1 20071109 A 3350 8039251 BATTERY PACK BOEING 717 717200 1383700 NM EMERGENCY LIGHTS INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 921ME 55183 AFT BULKHEAD DOOR EXIT MARKER SIGN IS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F TR A6WE 2007111400084 20071114 00084 NM 2007 11 14 MWEA070292 1 20071108 A 5230 PAN BOEING 717 717200 1383700 NM CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 910ME 55174 AFT CARGO DOOR OUTER PAN HAS A CRACK LOCATED AT THE FORWARD SIDE BY CRANK GUIDE. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2007111400085 20071114 00085 NM 2007 11 14 MWEA070293 1 20071108 A 5230 PAN BOEING 717 717200 1383700 NM CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 910ME 55174 AFT CARGO DOOR INNER PAN CRACKED AT FORWARD CRANK GUIDE. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2007111400086 20071114 00086 NM 2007 11 14 07FDEA04756 1 20071108 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1541-1551 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 591FE 48527 CABIN STA 1541 TO 1551 LBL 8 SEAT TRACK FOUND DAMAGED. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REP AIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007111400097 20071114 00097 SO 2007 11 14 CHQA200700074 1 20071109 A 2752 3633001019 ACTUATOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL TE FLAPS CONTAMINATED A CHQA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 GL 11 262SK 21154 145168 CAE312351 CLE TO BDL.- ON DESCENT, FLAPS WERE SELECTED FROM 0 TO 9 AND A FLAP FAIL MESSAGE APPEARED ON EICAS. THE QRH WAS FOLLOWE D AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE CMC FOR FAULT CODES AND FOUND CODES FOR FLAP J AMMING. THE FLAP SYSTEM WAS RESET AND WAS WORKING NORMALLY ON THE GROUND. THE AIRCRAFT WAS FERRIED TO CMH FOR FURTHER TROUBLESHOOTING. ONCE IN CMH MAINTENANCE INSPECTED THE FLAP ACTUATORS FOR FAULTS AND DISCOVERED THE OUTBOARD ACTUATOR F OR THE RIGHT INBOARD FLAP HAD WATER CONTAMINATION INSIDE. THE ACTUATOR WAS REPLACED ALONG WITH THREE OTHERS AS A PRECAU TION. AFTER THE ACTUATOR WAS REPLACED, THE AIRCRAFT WAS TEST FLOWN AT ALTITUDE AND NO FATHER DEFECTS WERE NOTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007111400098 20071114 00098 EA 2007 11 14 CHQA200700075 1 20071109 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A CHQA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 GL 11 701BR 7448 GEE872845 IAH TO MAF - ON APPROACH TO MAF, CREW RECEIVED A FLAP FAIL MESSAGE WHEN FLAPS WERE SELECTED TO 30 DEGREES. THE FLAPS FA ILED AT 30 DEGREES AND THE QRH WAS FOLLOWED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE FLAP S YSTEM, AND RESET IT AFTER FINDING NO MESSAGES. THE FLAP SYSTEM OPERATED NORMALLY AFTER RESET. 2 L 7 2 4F 4 F RT A21EA E15NE 2007111400099 20071114 00099 NM 2007 11 14 07FDEA04761 1 20071110 A 5313 655458347 STRINGER BOEING 727 727200 138407E NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 AFT PIT STR 28L HAS CORROSION BET STA 1053 TO STA 1054 CORROSION FOUND DURING REPAIR ON N00489 AFTER SKIN WAS REMOVED CU T OUT DAMAGED STRINGER. FABRICATED REPAIR PARTS TREATED AND FR PRIMED. INSTALLED STRINGER REPAIR REF SRM 53-10-3 FIG 1 . THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007111400100 20071114 00100 NM 2007 11 14 07FDEA04762 1 20071110 A 5330 6554583164 SKIN BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 AFT PIT BILGE SKIN CORRODED OB SIDE OF STR 28L, STA 1045-1048, LBL 16-17. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA OF SKIN. FABRICATED REPAIR DOUBLER AND FILLER. TREATED AND FR PRIMED. INSTALLED EXTERNAL REPAIR REF SRM 53-30-3 FIG 3. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007111400101 20071114 00101 NM 2007 11 14 07FDEA04763 1 20071110 A 5311 90522692 FRAME BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 UPPER FUSELAGE STATION 720D FRAME, AFT EDGE IS CORRODED AT STRINGER 4 RIGHT AREA REMOVED CORROSION AT UPPER FUSELAGE ST A 720D FRAME AFT EDGE AT STR 4 RIGHT AREA REF SRM 51-10-6 ORIGINAL MATERIAL .064", MATERIAL REMAINING .048" MATERIAL LOS S .016". FOUND TO BE OUT OF LIMITS REF SRM 53-10-1 FIG 1. FABRICATED REPAIR DOUBLER REF SRM 51-40-3 FIG 1, MATERIAL U SED 7075-0, .063" HEAT TREATED TO T-6, TRACKING NR 2007- 11-015 W/O N00740. TREATED AND PRIMED DOUBLER AND INSTALLED RE F SRM 51-10-2, 51-30- 2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007111400102 20071114 00102 NM 2007 11 14 07FDEA04764 1 20071110 A 5330 6554575 SKIN BOEING 727 727225 1384077 NM ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 FUSELAGE SKIN JUST FWD OF LANDING LIGHT IS GOUGED REMOVED INBD LT LEADING EDGE REF SRM 51-30-2 MANUFACTURED REPAIR DOUBL ER AND FILLER REF SRM 53-30-3. TREATED AND PRIMED REPAIR DOUBLER AND FILLER, REF SRM 51-10-2. INSTALLED REPAIR DOUBLER AND FILLER REF SRM 53-30-3. INSTALLED LEADING EDGE REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007111400103 20071114 00103 NM 2007 11 14 07FDEA04765 1 20071110 A 5310 BAC1495170 FRAME BOEING 727 727225 1384077 NM BODY FAIRING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 BODY FAIRING FRAME HAS CORROSION LOCATED FORWARD END OF PANEL 3455R. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, ORIG INAL .050'. REMOVED .025", REMAINING .025", IAW SRM 53-10-1. TOOL AAR23841 CAL DATE . 2 L 7 3 4F A3WE 2007111400104 20071114 00104 NM 2007 11 14 07FDEA04766 1 20071110 A 5312 651630047 BULKHEAD BOEING 727 727225 1384077 NM ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 FUSELAGE STA 178 FORWARD SIDE OF PRESSURE BULHEAD, SKIN HAS A GOUGE 2.5" IN FROM OUTER EDGE AT LEFT SIDE, 4TH RADOME A TTACH NUTPLATE FITTING DOWN BLENDED GOUGE, ORIGINAL MATERIAL IS .030" BONDED TO .056", MATERIAL REMOVED IS .008" MATERI AL REMAINING IS .022. HFEC DAMAGE. ALODINED AND PRIMED, REF FED EX EA 7-5330- 13117, THIS IS CLASSIFIED AS A MINOR RE PAIR. 2 L 7 3 4F A3WE 2007111400105 20071114 00105 NM 2007 11 14 07FDEA04767 1 20071110 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 635 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 591FE 48527 CABIN, UPON THRUST REVERSER MODIFICATION E 1-7830-7-5009 ACCESS OPEN UP AT STATION 635 LBL 47 SEAT TRACK FOUND CRACKED . CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007110900284 20071109 00284 NM 2007 11 9 SWAA075458 1 20071031 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 804, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007110900288 20071109 00288 NM 2007 11 9 NWAA073645534 1 20071102 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 534US 24265 DURING OVERNIGHT LINE CHECK, FOUND ESCAPE PATH LIGHTS ON FLOOR INOP BETWEEN ROWS 23 THRU 32. MAINTENANCE REMOVED AND RE PLACED 2 BATTERY PACKS AND A TEST SWITCH AT THE FORWARD FLIGHT ATTENDANT PANEL. OPERATIONAL CHECKED GOOD AND AIRCRAFT W AS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007110900299 20071109 00299 NM 2007 11 9 USAA920071067 1 20071101 A 5347 SEAT TRACK BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, CRACKED VERTICAL LEG OF SEAT TRACK, BS 673, LBL 24. REPAIRED CRACKED VERTICAL LEG OF SE AT TRACK, BS 673, LBL 24 IAW USAIRWAYS EA 98938. 2 L 7 2 4F RT A16WE 2007110900302 20071109 00302 EU 2007 11 9 F3LA200700311 1 20071015 A 5315 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON UPPER SURFACE OF FLOORBEAM Y254, BETWEEN FRAMES 16 AND 18. BLENDED 3 AREAS ON FLOOR SUPPORT Y254, ALL FOUND TO BE OUT OF LIMITS PER SRM 53-11-14-FIG 104. CUT OUT CORRODED UPPER CAP SECT ION OF FLOOR SUPPORT IAW SRM 53-11-14, PARA 5 AND FIG 201. FABRICATED REPAIR PARTS AND INSTALLED FLOOR SUPPORT REPAIR I AW SRM 53-11-14, 51-47-00, 51-23-00, AND EAR 910-4551. 2 L 7 2 4F RT A28NM 2007110900311 20071109 00311 EU 2007 11 9 07FDEA04717 1 20071105 A 5720 A57111092203 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 729FD 657 FOUND ON LOWER JUNCTION FITTING CENTER TANK INTERNAL SEVERAL HOLES WITH CRACK FINDINGS REPAIR PERFORMED BY REAM UP UN TIL DAMAGE REMOVAL IAW EA 6-5710-114908 AND RAS/054537/070/2007 ISS A. 2 L 7 2 4F RT A35EU 2007110900316 20071109 00316 NM 2007 11 9 QXEA200701645 1 20071102 A 2120 UNKNOWN DHAV DHC8 DHC8202 2809007 NM COCKPIT ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 358PH 506 SEA FLIGHT NR 2131 - STRONG ODOR OF JET FUEL IN FLIGHTDECK AND CABIN FOLLOWING NR 2 BLEED ACTIVATION. MAINTENANCE PERFO RMED GENERAL VISUAL INSPECTION OF NR 2 ENGINE FOR ANY OBVIOUS LEAKS. NO NOTED. GROUND RUN AIRCRAFT WEIGHT NR 2 BLEED O N, NO STRONG ODOR OF JET FUEL NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007110900332 20071109 00332 EU 2007 11 9 TRAX200701657 1 20071029 A 5753 BRACKET AEROSP ATR72 ATR72212 8680945 EU LT TE FLAP BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 LT INBD FLAP AT RIB 9, 3 OMEGA BRACKETS FOUND BROKEN. INSTALLED IAW AMM 20-21-11 FABRICATION COVERED ON W/C 2000-101. 2 H 7 2 4T RT A53EU 2007110900333 20071109 00333 EU 2007 11 9 TRAX200701658 1 20071029 A 5753 BRACKET AEROSP ATR72 ATR72212 8680945 EU LT TE FLAP BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 LT INBD FLAP AT RIB 5 1 OMEGA BRACKET FOUND BROKEN FOR FABRICATION SEE WC NR 2000-102. NSTALLED IAW SRM 51-25-01FABRICA TION COVERED ON W/C 2000-102REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDI X A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007110900345 20071109 00345 EA 2007 11 9 TRAX200701672 1 20071102 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 872AS 7542 FO'S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007110900353 20071109 00353 SO 2007 11 9 C2XA07SH092 1 20071104 A 5320 14525480003 THRESHOLD EMB 145 EMB145XR 3260214 SO CARGO BAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 41104 646 SAH - DURING C-CHECK CARGO DOOR CUTOUT LOWER THRESHOLD HAS MULTIPLES AREAS OF CORROSION AT FR 64-67. MAINTENANCE REMOVE D AND REPLACED CARGO DOOR CUTOUT LOWER THRESHOLD AT FR 64-67 IAW EMB 145 SRM 51-40-02 AND REMOVED AND REPLACED NUT PLATE S IAW EMB 145 EC 5320-01137. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2007110900360 20071109 00360 EA 2007 11 9 TRAX200701677 1 20071102 A 3260 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 828AS 7213 UPON SELECTION OF GEAR HANDLE TO DOWN BOTH RT AND LT GEAR INDICATORS SHOWED UNSAFE, FOLLOWED BY GEAR DISAGREE WARNING. C OMPLIED WITH QRH PROCEDURES AND USED LANDING GEAR MANUAL RELEASE HANDLE TO GET MAIN GEAR DOWN, EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007110900364 20071109 00364 NM 2007 11 9 ZZDA2007293 1 20071102 A 3350 LIGHT BOEING 717 717200 1383700 NM CABIN MISSING A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 977AT 55036 LENS AND BULBS FOR ESCAPE PATH LIGHT ON SIDE OF 1D IS MISSING. REPLACED LENS (RED) AND BULBS, OPS CHECK GOOD REF AMM 33 -51. 2 L 7 2 4F TR A6WE 2007110900365 20071109 00365 NM 2007 11 9 ZZDA2007294 1 20071104 A 3260 WARNING SYSTEM BOEING 737 7377BD 1384511 NM LANDING GEAR MALFUNCTIONED A ZZDA O OTHER N FALSE WARNING DE DESCENT 1 SO 37 328AT 33934 AFTER SELECTING GEAR DOWN RECEIVED THREE GREEN AND THREE RED INDICATIONS. PERFORMED FAULT ISOLATION MANUAL PROXIMITY SW ITCH ELECTRONICS BITE PROCEDURE 32-09 TASK 801. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. OK FOR CONTINUED SERVI CE. 2 L 7 2 4F RT A16WE 2007110900377 20071109 00377 NM 2007 11 9 SWAA075524 1 20071104 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 16R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007110900388 20071109 00388 NM 2007 11 9 2007UALA04528 1 20071101 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 440 S24R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 FWD CARGO DOOR CUTOUT, FWD FRAME BS 440 AT STR 24R, HAS CRACK EMINATING FROM LOWER BOTTOM STOP FITTING, APPROX 1". MAJO R REPAIR ACP'D, INST'D NESTED DOUBLER TRIPLER REPAIR ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007110900390 20071109 00390 NM 2007 11 9 2007UALA04530 1 20071101 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 537 S12R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 FOUND FUSELAGE SKIN SUBSURFACE CRACK ALONG THE CHEM-MILL EDGE 1.25" IN LENGTH LOWER LT SIDE OF RIVET ROW, STA 537 STR 12 R. REPAIRED PER EA NR I070773IR AND INSTALLED AIR DISTRIBUTION DUCT REF MM 21-23-25 ON N-R 12553 -2000-0007 BY AAR MECH ANIC 10885 AND RII INSPECTED BY NR 80. REPAIR CONSISTS OF EXTERNAL DOUBLER AND A FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2007111300004 20071113 00004 NM 2007 11 13 MWEA070272 1 20071105 A 7830 7150922505 DOOR FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 907ME 55171 UPPER DEFLECTOR DOOR FRAME CRACKED IN RADIUS AT STATION 25 LEFT SIDE. FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F TR A6WE 2007111300061 20071113 00061 NM 2007 11 13 2007UALA04577 1 20071102 A 3297 W7435101118 WIRE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NLG DAMAGED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 784UA 26951 NLG RED SAFETY LIGHT WILL NOT ILLUMINATE WHEN PTT SWITCH IS CLOSED. ALSO, WHEN CLOSING MLG AND NLG DOORS FROM GROUND C IRCUIT BREAKER IN COCKPIT FOR SAFETY VALVE TRIPS. SUSPECT BROKEN WIRE. REPAIRED WIRE IN LT MAIN WHEEL WELL. CLEANED LI GHT SOCKET IN NOSE WHEEL WELL. ACCOMPLISHED LAMP TEST AND OPERATED DOORS, OPS CKS NORMAL. AC OK FOR SERVICE 2 L 7 2 4F 4 F RT T0001SE E46NE 2007111300062 20071113 00062 EA 2007 11 13 MALA070175 1 20071008 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002D24 1390016 EA NLG STEERING ILLUMINATED A MALA O OTHER J WARNING INDICATION LD LANDING 1 GL 15 902XJ 15131 STEERING INOP CAUTION LIGHT ILLUMINATED ON LANDING. AIRCRAFT WAS TUGGED TO THE GATE. COMPLETED FAULT ISOLATION PROCEDU RES 32-50-00-810-802-A01. EICAS MESSAGE NO LONGER APPEARS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007111300063 20071113 00063 EU 2007 11 13 MALA070176 1 20071102 A 5230 SKIN SAAB SF340 340B 7860101 EU CARGO DOOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 406XJ 340B406 SMALL DENT IN CARGO DOOR SKIN. PERFORMED PERMANENT REPAIR IAW MAL EO NR S52028. 2 L 7 2 4T RT A52EU 2007111300064 20071113 00064 EU 2007 11 13 MALA070177 1 20071102 A 5230 SKIN SAAB SF340 340B 7860101 EU CARGO DOOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 406XJ 340B406 SMALL DENT IN CARGO DOOR SKIN. PERFORMED PERMANENT REPAIR IAW MAL EO NR S52028. 2 L 7 2 4T RT A52EU 2007111300065 20071113 00065 EU 2007 11 13 MALA070178 1 20071102 A 5230 SKIN SAAB SF340 340B 7860101 EU CARGO DOOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 406XJ 340B406 SMALL DENT IN CARGO DOOR SKIN. PERFORMED PERMANENT REPAIR IAW MAL EO NR S52028. 2 L 7 2 4T RT A52EU 2007111300066 20071113 00066 EU 2007 11 13 MALA070179 1 20071102 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 319 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 406XJ 340B406 LT AISLE SEAT TRACK HAS CORROSION FROM ENTRY WAY TO STATION 319. REPAIRED BY REMOVING AND REPLACING THE FWD 32" OF PRE. INSTALLED REPLACEMENT SECTION OF SEAT RAIL IAW MAL EONR S53060, STA 294 TO 319 LBL 18.3. 2 L 7 2 4T RT A52EU 2007111300067 20071113 00067 EU 2007 11 13 MALA070180 1 20071106 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN BROKEN A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 427XJ 340B427 EMERGENCY FLOOR TRACK LIGHTING BROKEN 41LN. REMOVED AND REPAIRED 41LN, EMERGENCY LIGHT ASSEMBLY FLOOR PROX, IAW MM 33-5 0-20-04. ALL CHECKS GOOD, PN ON/OFF: 7433-1. 2 L 7 2 4T RT A52EU 2007111300068 20071113 00068 EU 2007 11 13 AALA20072115 1 20071101 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 59081 639 JFK - EMERGENCY EXIT LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007111300069 20071113 00069 EU 2007 11 13 AALA20072116 1 20071101 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 59081 639 JFK - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007111300070 20071113 00070 EU 2007 11 13 AALA20072117 1 20071101 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 59081 639 JFK - EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007111300071 20071113 00071 EU 2007 11 13 AALA20072118 1 20071101 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 59081 639 JFK - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007111300072 20071113 00072 EU 2007 11 13 AALA20072119 1 20071101 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 59081 639 JFK - EMERGENCY LIGHTS AT RIGHT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT FORWARD C ABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007111300073 20071113 00073 WP 2007 11 13 AALA20072108 1 20071101 A 4990 5940405503 APU DOUG DC9 DC982 3022082 WP LEAKING A AALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 447AA 6312 49473 ORD INFLIGHT T1502/01NOV - WHITE SMOKE REPORTED IN CABIN WITH OIL ODOR. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. R EPLACED AUXILLIARY POWER UNIT (APU) DUE TO INGESTION OF OIL FROM LEAK. ACCOMPLISHED PNEUMATIC DUCT BURNOUT. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007111300074 20071113 00074 EU 2007 11 13 AALA20072109 1 20071030 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 MIA - EMERGENCY LIGHTS AT SEAT ROWS 27G TO 37G INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 27G TO 37G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007111300075 20071113 00075 NM 2007 11 13 AALA20072110 1 20071101 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 368AA 25195 ORD - OVERWING EMERGENCY LIGHT AT SEAT 20A HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20A. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007111300076 20071113 00076 WP 2007 11 13 AALA20072114 1 20071025 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS PINCHED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 255AA 49287 TUL - EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED PINCHED WIRE AT FORWARD ESCAPE PATH LIGHTING PANEL FOR EM ERGENCY LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007111300077 20071113 00077 NM 2007 11 13 AALA20072111 1 20071101 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 182AN 29592 SFO- EMERGENCY LIGHT AT AFT SEAT 18A HAS LENS BROKEN OFF WALL MOUNT. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT AFT SEAT 18A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007111300078 20071113 00078 WP 2007 11 13 AALA20072120 1 20071101 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 954U 49426 LGA - EMERGENCY OVERWING EXIT LIGHT AT SEAT ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY OVERWING EXIT LIGHT AT SEAT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007111300079 20071113 00079 NM 2007 11 13 AALA20072106 1 20071101 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 772AN 29580 JFK - EMERGENCY LIGHT AT SEAT 21C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007111300080 20071113 00080 NM 2007 11 13 AALA20072107 1 20071101 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 772AN 29580 JFK - EMERGENCY LIGHT AT SEAT 2D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 2D. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT T00001SE 2007111300081 20071113 00081 EU 2007 11 13 AALA20072112 1 20071030 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 MIA - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 19 TO 37 INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 19 TO 37. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007111300082 20071113 00082 NM 2007 11 13 AALA20072113 1 20071022 A 3397 WIRE HARNESS BOEING 737 737800* NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 919AN 29520 TUL - EMERGENCY LIGHT AT SEAT 15D INOPERATIVE. REPLACED HARNESS FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007111300083 20071113 00083 NM 2007 11 13 07FDEA04721 1 20071106 A 5730 SKIN DOUG MD11 MD11F 3023600 NM LWS 889 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 591FE 48527 LEFT WING, FIXED LEADING EDGE NR 14 SLAT TRACK CUTOUT STA XOS 889 FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 57-10-0 0 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007111300084 20071113 00084 EU 2007 11 13 07FDEA04722 1 20071011 A 5753 A5797086900000 SKIN AIRBUS 310 A310324 3930206 EU LT WING TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 802FD 542 LT WING, FLAP INBD W/ DBONDS AT THE T/E BETWEEN RIB 2 AND RIB 8 REPLACE TRAILING EDGE IAW FEDEX EA 6-5710-115293. 2 L 7 2 4F RT A35EU 2007111300085 20071113 00085 EU 2007 11 13 07FDEA04723 1 20071009 A 5753 A5797086900100 SKIN AIRBUS 310 A310324 3930206 EU RT WING TE FLAP DEBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 802FD 542 RT WING INBD FLAP T/E W/ VARIOUS DEBONDS TRAILING EDGE WAS REPLACED IAW SRM 51-72-10 AND EA 6-5710-115293. 2 L 7 2 4F RT A35EU 2007111300086 20071113 00086 WP 2007 11 13 07FDEA04724 1 20071106 A 5347 607158 SEAT TRACK DOUG DC10 DC1030F 3023504 WP BS 515 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 317FE 46835 MCD - SEAT TRACK AT STA 515 LBL 27.5 IS EXFOLIATED. REMOVE, FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-70-00 AN D 51-31-01. 2 L 7 3 4F RT A22WE 2007111300087 20071113 00087 WP 2007 11 13 07FDEA04725 1 20071106 A 5347 607158 SEAT TRACK DOUG DC10 DC1030F 3023504 WP BS 1079-1099 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 317FE 46835 MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREA AT F/S 1079-1099 LBL 48 REMOVED AND REPLACED SEAT TRACK SECTION IAW SRM 53-7 0-00 FIG1 SHEET 1. 2 L 7 3 4F RT A22WE 2007111300088 20071113 00088 WP 2007 11 13 07FDEA04726 1 20071106 A 5347 607158 SEAT TRACK DOUG DC10 DC1030F 3023504 WP BS 899-919 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 317FE 46835 MAIN DECK COMPT SEAT TRACK HAS GOUGED AREAS AT F/S 899-919 LBL 48 REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW S RM 53-70-00 AND 51-31-01. 2 L 7 3 4F RT A22WE 2007111300089 20071113 00089 EA 2007 11 13 QXEA200701560 1 20071009 A 5310 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA BS 661 S4L DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - C4 CHECK. REFERENCE REO 670-53-11-188 SHEET 3 MAP Q, BURNED MATERIAL AROUND FASTENER HOLE 1" AFT OF FS 661 AT STRI NGER 4L, REQUIRES REPAIR. REPAIRED IAW REO 670-53-11-188 SHEET 3 MAP Q. INSTALLED REPAIR DOUBLER AND FILLER AND PAINTE D. 2 L 7 2 4F RT A21EA 2007111300090 20071113 00090 EA 2007 11 13 QXEA200701559 1 20071009 A 5310 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA BS 953 S5L DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX C4 CHECK, REFERENCE REO 670-53-11-188 SHEET 3 MAP O, BURNT MATERIAL AROUND FASTENER HOLE AT FS 953, 2.9" BELOW STRIN GER 5L, REQUIRES REPAIR. REPAIRED IAW REO 670-53-11-188 SHEET 3 MAP O. INSTALLED REPAIR DOUBLER AND FILLER AND PAINTED . 2 L 7 2 4F RT A21EA 2007111300091 20071113 00091 EA 2007 11 13 QXEA200701567 1 20071009 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - C4 CHECK. LOWER TCAS ANTENNA FUSELAGE SKIN HAS LIGHT SURFACE CORROSION. POLISHED OUT CORROSION PER SRM 51-21-06. MATERIAL REMOVED .003" WITHIN LIMITS. NDT AREA FOR CRACKS, NONE NOTED. ETCHED AND ALODINED. 2 L 7 2 4F RT A21EA 2007111300092 20071113 00092 EA 2007 11 13 QXEA200701561 1 20071009 A 5310 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA BS 724 S3L DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX- C4 CHECK. REFERENCE REO 670-53-11-188 SHEET 3 MAP R. BURNT MATERIAL AROUND FASTENER HOLE AT FS 724.08, 2.1" BELOW S TRINGER 3L REQUIRES REPAIR. HFEC AREA AND FOUND NO CRACKS, INSTALLED REPAIR DOUBLER IAW REO 670-53-11-188 SHEET 3 MAP R . INSTALLED FILLER AND PAINTED. 2 L 7 2 4F RT A21EA 2007111300093 20071113 00093 EA 2007 11 13 QXEA200701564 1 20071009 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 310 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - C4 CHECK - FORWARD PASSENGER DOOR SURROUND STRUCTURE FORWARD FUSELAGE SKIN HAS DAMAGE. NICKS, SCRAPES AND DENTS A T FS 310 WL 90. BLENDED NICKS AND SCRAPES ON EXTERNAL SKIN. DIMENSION CHECKED HIGH = .130" LOW= .124". PERFORMED NDT ON BLENDED AREA WITH NO CRACKS NOTED. APPROX MATERIAL REMOVED .006". WITHIN SRM LIMITS. ETCHED AND ALODINED AND PRIMED AND PAINTED AREA. 2 L 7 2 4F RT A21EA 2007111300094 20071113 00094 EA 2007 11 13 QXEA200701563 1 20071009 A 5310 DOOR FRAME CNDAIR CL600 CL6002C10 1390015 EA BS 1047 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - C4 CHECK. CORROSION AT 2 NUTPLATES AT FRAME AFT OF CARGO DOOR ABOVE FLOOR LEVEL AT FS 1047 WL 98-106. REMOVED NUTP LATES AND REMOVED CORROSION BY BLENDING WITH SCOTCHBRITE. HFEC AREA WITH NO CRACKS NOTED. BLEND FOUND TO BE WITHIN LIMIT S MAX MATERIAL REMOVED IS .002". ALODINED AREA AND PRIMED AND PAINTED. INSTALLED NEW NUTPLATES. 2 L 7 2 4F RT A21EA 2007111300095 20071113 00095 EA 2007 11 13 QXEA200701565 1 20071009 A 5210 ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - C4 CHECK,FORWARD PASSENGER DOOR INNER DOOR SKIN TO STEP ASSEMBLY ANGLE IS CRACKED, AFT MID DOOR. REPAIRED THE CRA CKED ANGLE BY INSTALLING SPLICE ANGLE IAW REO 670-52-11-072. 2 L 7 2 4F RT A21EA 2007111300096 20071113 00096 EA 2007 11 13 QXEA200701566 1 20071009 A 5754 SKIN CNDAIR CL600 CL6002C10 1390015 EA SLAT GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - C4 CHECK, LEFT WING LEADING EDGE IS GOUGED AT SS 195. BLENDED GOUGE AREA REMOVED .007" AND WITHIN LIMITS. PERFOR MED NDT FOR CRACKS, NONE FOUND. ALODINED PRIMED AND PAINTED AREA IAW REO 670-57-41-035 AND SRM 57-41-01. 2 L 7 2 4F RT A21EA 2007111300097 20071113 00097 EA 2007 11 13 QXEA200701562 1 20071009 A 5310 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA BS 453 S1L DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - C4 CHECK. REFERENCE REO 670-53-11-188 SHEET 3 MAP S, BURNT MATERIAL AROUND FASTENER HOLE 2.8" FORWARD OF FS 453 AT STRINGER 1L REQUIRES REPAIR. HFEC AREA WITH NO CRACKS NOTED. COMPLIED WITH STEPS 5-8 OF REO 670-53-11-188 PAGE 3 MAP S. 2 L 7 2 4F RT A21EA 2007111300135 20071113 00135 NM 2007 11 13 070175 1 20071102 A 2120 UNKNOWN DOUG MD80 MD83 3023681 NM CABIN ODOR A WX0A A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 WP 19 872GA 53295 AFTER TAKEOFF HAD A BURNING OIL ODOR, THEN BOTH AFT LAVATORY SMOKE DETECTORS ALARMS WENT OFF. RETURNED TO LAS PER CONVE RSATION WITH MAINTENANCE CONTROL PERSONNEL. LAS MAINTENANCE DEPARTMENT PERSONNEL PERFORMED HIGH POWER ENGINE GROUND RUN S, REFERENCE AMM 71-00-00. WITH ENGINES AT HIGH POWER, RAN AIRCRAFT AIR CONDITIONING PACKS LEFT AND RIGHT FOR 20 MINUTE S, REFERENCE AMM 21-00-00. NO CABIN OR LAVATORY SMOKE NOTED, AIRCRAFT IS OK FOR SERVICE. 2 L 7 2 4F RT 2007111300136 20071113 00136 WP 2007 11 13 070174 1 20071024 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1155 S27-28R CORRODED A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 894GA 49660 FRAME AT STA 1155 CORRODED. REMOVED AND REPLACED FRAME P/N 5AA9936073-9 AT STATION 1155 L27R AND 28R IAW SRM 51-30-05 A ND 51-30-02. 2 L 7 2 4F A6WE 2007111300137 20071113 00137 WP 2007 11 13 070173 1 20071024 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1155 S26R CORRODED A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 894GA 49660 FOUND LONGERON AT STA 1155 CORRODED. REMOVED AND REPLACED LONGERON P/N 5936037-501 AT STATION 1155 L-29R IAW SRM 51-30- 05 AND 51-30-02. 2 L 7 2 4F A6WE 2007111300138 20071113 00138 WP 2007 11 13 NWAA073699992 1 20071103 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8960E 45869 TAIL COMPARTMENT CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BULBS AND POWER PACK. OPERATION CHECKS GOOD. 2 L 7 2 4F A6WE 2007111300139 20071113 00139 NM 2007 11 13 UPS07451107 1 20071106 A 2410 CSD BOEING 747 747123 1384873 NM NR 2 ENGINE OVERHEATED A IPXA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 SO 01 676UP 20101 IFSD, NR 2 ENG CSD HAD HIGH OIL TEMP. FLIGHT CREW TRIED TO DISCONNECT BUT COULDN'T. FOLLOWED CHECK LIST AND SHUT DOWN ENGINE. MX INSPECTED NR 2 ENG CSD AND FOUND THAT OIL HAD LEAKED OUT AND CSD OVERHEATED. CSD REMOVED AND REPLACED AND GEAR BOX INSPECTION IN WORK. 2 L 7 4 4F RT A20WE 2007111300140 20071113 00140 NM 2007 11 13 UPS07651106 1 20071030 A 5712 RIB BOEING 767 76734AF 1385212 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 307UP 27760 SEG2 RT WING FIXED L/E AIR LOAD RIB LOWER CHORD AFT END IS CRACKED AT FSS 688. REPAIRED PER SRM 51-40-05-0G AND 51-40-0 2-0G. 2 L 7 2 4F RT A1NM 2007111300141 20071113 00141 WP 2007 11 13 UPS07851086 1 20071102 A 2121 5007025381 FAN DOUG DC8 DC873F 302199F WP LAV/CABIN FROZEN A IPXA F A ACTIVATE FIRE EXT. UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 880UP 46080 DIVERSION, CREW SMELLED SMOKE IN CABIN. DISCHARGE HAND EXTINGUISHER IN LAV, CREW REPORTED LAV PUMP WAS TURNING. PARKED FOR FAA EVALUATION. FOUND RECIRCULATING FAN FROZE UP. REMOVED AND REPLACED IAW AMM 21-1-01-2. OPS CHECK GOOD. INSPE CTED SURROUNDING AREA AND FOUND NO OTHER DEFECTS OR DAMAGE. A/C OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2007111300142 20071113 00142 WP 2007 11 13 UPS07851090 1 20071027 A 5310 DOUBLER DOUG DC8 DC873F 302199F WP WINDOW RETAINER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 AFTER REMOVAL OF EXTERIOR RT CV WINDOW RETAINER FOUND INTERNAL DOUBLER CRACKED AT UPPER FWD CORNER ST A -72. REPAIRED RT CV WINDOW INTERNAL DOUBLER AT STA -72 IAW SAA EA NR 008- 5600-01-A1197, UPS RAA NR DC8-53-20669, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2007111300143 20071113 00143 WP 2007 11 13 UPS07851092 1 20071011 A 5340 FITTING DOUG DC8 DC873F 302199F WP FS 1150 L33R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 C2 BANANA FITTING CRACKED AT STA 1150 L33R. REMOVED, AND INSTALLED REPLACEMENT BANANA FITTING AT STA 1150 L33R IAW SRM 51-1-20D, AND SRM 51-01-24. 2 L 7 4 4F RT 4A25 2007111300145 20071113 00145 WP 2007 11 13 UPS07851094 1 20071015 A 5310 FITTING DOUG DC8 DC873F 302199F WP FS 1766 L19R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 INSIDE 60 HOLE LONGERON END FITTING CRACKED AT STA 1766 L19R. REMOVED AND REPLACED LONGERON END FITT ING AT STA 1766 L19R IAW SRM 51-1-21, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2007111300146 20071113 00146 WP 2007 11 13 UPS07851095 1 20071015 A 5310 WINDOW FRAME DOUG DC8 DC873F 302199F WP FS -67 L11L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 WINDOW FRAME AT STA -67 L11L CAPT SIDE HAS EXFOLOIATED CORROSION. REPAIRED CAPT LT AFT WINDOW FRAME AT STA -67 L11L IAW SAA EA NR 008- 5310-01-A1194, UPS RAA NR DC8-53-20665, AND BAC SERV ID 1-659403655. 2 L 7 4 4F RT 4A25 2007111300147 20071113 00147 WP 2007 11 13 UPS07851096 1 20071011 A 5522 SKIN DOUG DC8 DC873F 302199F WP LT ELEVATOR CANNING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 L/ELEV UPPER INBD EXTERIOR SKIN OIL CANS. REPAIRED L/ELEV UPPER INBD SKIN IAW SRM 55-2-1, 51-1-21, A ND DWG 5655942. 2 L 7 4 4F RT 4A25 2007111300148 20071113 00148 WP 2007 11 13 UPS07851098 1 20071009 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FS 1220 BL-0 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 SEAT TRACK BL-0 STA 1220-1240 CORRODED. REMOVED AND REPLACED SEAT TRACK PLUG AT STA 1220 BL-O IAW SR M 53-02-03-0 FIG 12, AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 2007111300149 20071113 00149 WP 2007 11 13 UPS07851099 1 20071030 A 5340 3755847U2 FITTING DOUG DC8 DC873F 302199F WP FS 1230 L33R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 FITTING AT STA 1230 L33R IS CRACKED. REMOVED AND REPLACED END FITTING AT STA 1230 L33R IAW SRM 51-01 -20D AND SRM 51-01-24. 2 L 7 4 4F RT 4A25 2007111300150 20071113 00150 WP 2007 11 13 UPS07851100 1 20071106 A 3350 BATTERY DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS WEAK A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 EMERGENCY EXIT LIGHTS ARE VERY DIM AND FLIGHT DECK LIGHT GOES OUT IN APPROX 2 MINUTES. REPLACED EMERGENCY LIGHTING BATT ERY AND RELAY UNIT IAW DC8 AMM 33-50-01-2. OPS TEST NORMAL. 2 L 7 4 4F RT 4A25 2007111300151 20071113 00151 WP 2007 11 13 UPS07851101 1 20071024 A 5512 SKIN DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 RT HORIZ STAB AFT SPAR WEB ACCESS HOLES HAVE CRACKS AT FASTNER HOLE SKIN ON NR 2, 3, 6, 7, 8, 9, 11, AND 12. STOP DRILLED ALL CRACKS AT ACCESS HOLES IN RT HORIZ STAB STA XH 28.843-149.00. FABRICATED AND INSTALLED 12 EA DOUBLERS ON RT HORIZ STAB ACCESS HOLES AT STA XH 28.843-149.00 IAW SRM 55-03-01 FIG 3, AND SRM 55-02-00 FIG 2. 2 L 7 4 4F RT 4A25 2007111300152 20071113 00152 WP 2007 11 13 UPS07851102 1 20071008 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 STA 60 BL0 HAS CORROSION BETWEEN FLOOR BOARD AND 9G NET LATCH TRAY. REPAIRED FLOORBEAM STA 60 BL0 IA W SRM 51-03-00-0, SRM 51-1-8 AND SRM 53-03-03. 2 L 7 4 4F RT 4A25 2007111300153 20071113 00153 WP 2007 11 13 UPS07851104 1 20071012 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 CORROSION INTERIOR SKIN ABOVE CAPT LT AND RT AFT SIDE WINDOW. REPAIRED SKIN AT STA -52 ABOVE CAPT LT AND RT SIDE WINDOW IAW SRM 51-09-00-0, AND DWG 5643170. 2 L 7 4 4F RT 4A25 2007111300155 20071113 00155 WP 2007 11 13 UPS07851114 1 20071107 A 3310 LIGHT DOUG DC8 DC871F 302199D WP COCKPIT SMOKE A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 708UP 46048 HAD LIGHT ODOR OF SMOKE IN COCKPIT. F/E PANEL LIGHTS WENT OUT. APPEARS TO BE A 5 AMP FUSE HAS BLOWN ON F/E PANEL DID N OT REPLACE IN FLIGHT. REMOVED AND REPLACED F/E PANEL LIGHT. FUSE 5 IAW MM 33-13-00-5. OPS CHKS GOOD. 2 L 7 4 4F RT 4A25 2007111400003 20071114 00003 NM 2007 11 14 MWEA070280 1 20071102 A 5347 593056671 SEAT TRACK DOUG MD88 MD88 3023688 NM BS 1271 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 601ME 49762 CABIN FLOOR SEAT TRACK LEFT SIDE, TRACK NR 2 FROM STATION 1271 TO END OF TRACK HAS SURFACE CORROSION. REMOVED CORROSION , INSTALLED NEW SEAT TRACK. 2 L 7 2 4F RT A6WE 2007111400006 20071114 00006 NM 2007 11 14 MWEA070284 1 20071102 A 5320 SG095300053 CUSP WEB DOUG MD88 MD88 3023688 NM BS 541-560 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 601ME 49762 CORROSION ON LEFT SUPPORT STRUCTURE PASSENGER CUSP MEMBRANE CABIN BETWEEN STATION 541-560. REMOVED CORROSION, FABRICATE D AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 2007111400010 20071114 00010 NM 2007 11 14 MWEA070283 1 20071102 A 5320 SG095300053 CUSP WEB DOUG MD88 MD88 3023688 NM BS 560-579 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 601ME 49762 CORROSION ON LEFT FLOOR SUPPORT STRUCTURE PASSENGER CUSP MEMBRANE CABIN. REMOVED CORROSION, FABRICATED AND INSTALLED DO UBLER. 2 L 7 2 4F RT A6WE 2007111400013 20071114 00013 EU 2007 11 14 07FDEA04733 1 20071010 A 5540 A5537160200000 ARM AIRBUS 310 A310324 3930206 EU RUDDER HINGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 802FD 542 NR 3 RUDDER HINGE ARM WITH CORROSION AT LUG BORES. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FEDEX EA 6-5510-115292. 2 L 7 2 4F RT A35EU 2007111400019 20071114 00019 NM 2007 11 14 07FDEA04740 1 20071107 A 5315 652082757 FLOORBEAM BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 MAIN CARGO COMP STA 480 RBL 10" FLOORBEAM LOWER SURFACE CORRODED REMOVED CORROSION IAW SRM 53-10-1 PG1, ORIGINAL .135", REMOVED .035' REMAINING .096". FOUND TO BE OUT OF LIMITS AAR TOOL NR 280087 CAL DATE 4-27-08. REPAIRED IAW SRM 53-10 -8 FIG 8. TREATED AND PRIMED IAW SRM 51-10-2. REMOVED AND REINSTALLED CABLE GUIDE IAW 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007111400023 20071114 00023 NM 2007 11 14 07FDEA04744 1 20071107 A 5315 BAC1505100246 FLOORBEAM BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 MAIN DECK FLOORBEAM UPPER FLG IS FRETTED/CORRODED AT FASTENER HOLE BS 312, LBL 4, WL 208. REMOVED CORROSION, FOUND OUT OF LIMITS, IAW SRM 51-10-6, 53-10-1 53-10-2 FIG 7 SHT 1, ITEM 18, ORIGINAL MAT. .080" REMOVED .026" REMAINING .064" TOOL AAR IN17-0213 CAL DATE 10-15-08. REPAIRED FLOORBEAM IAW SRM 53-10-8 FIG 7. REMOVED AND REINSTALLED PULLEY BRACKET IAW SRM 51-30-2, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007111400025 20071114 00025 NM 2007 11 14 DLM90071396 1 20071029 A 5730 SKIN DOUG MD90 MD9030 3023690 NM LT WING GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 LT WING FIXED L/E JUST O/B OF SLAT-TRACK NR 4 SKIN IS GOUGED. REPAIRED L/E WING IAW SRM 57-20-01 FIG II VOL II ON N/R 5 200-0045 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007111400026 20071114 00026 NM 2007 11 14 DL777071397 1 20071030 A 3350 LIGHT BOEING 777 777232 1385232 NM CABIN MALFUNCTIONED A DALA O OTHER O OTHER CR CRUISE 1 SO 27 865DA 29737 EMERGENCY LIGHTS IN CABIN ILLUMINATED INTERMITTENTLY DURING CRUISE. PERFORM EMERGENCY LIGHTS DAILY OPERATIONAL TEST AND EMERGENCY LIGHTS OPERATIONAL TEST WITH CONTROL SWITCHES PER AMM 33-51-00-710-801 AND AMM 33-51-00-710-803. EMERGENCY L IGHTS CHK OK. 2 L 7 2 4F RT T00001SE 2007111400030 20071114 00030 NM 2007 11 14 DL76G071404 1 20071102 A 3350 BULB BOEING 767 767332 1382001 NM ROWS 3AB & 5AB INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1613B 32776 FOUND AISLE EMERGENCY LIGHTS AT ROWS 3AB AND 5AB INOP. RELAMPED SAME PER AMM. OPS CKS GOOD. 2 L 7 2 4F RT A1NM 2007111400032 20071114 00032 NM 2007 11 14 DL76G071406 1 20071103 A 3620 80217010 VALVE BOEING 767 767332 1382001 NM NR 1 ENGINE MALFUNCTIONED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 173DZ 29692 RTO FOR LEFT ENG PRV MESSAGE. REMOVED L ENG PRV. REMOVED AND REPLACED LT ENG PRV CONTROLLER PER AMM. INSTAL LT ENG PR V VLV AND REPLACED MUSCLE AIR FLEX LINE. PERFORMED ENG RUN-UP SYSTEM OPS CK OK PER MM. 2 L 7 2 4F RT A1NM 2007111400087 20071114 00087 NM 2007 11 14 07FDEA04757 1 20071108 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1761 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 591FE 48527 CABIN, STA 1761 LBL 8 SEAT TRACK FOUND DAMAGED. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASS IFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007111400088 20071114 00088 NM 2007 11 14 07FDEA04758 1 20071109 A 5313 65561852 STRINGER BOEING 727 727225 1384077 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 AFT PIT STR 27R, END FITTING IS CRACKED AT BS 1056, REMOVED END FITTING, P/N 65-56185-1. INSTALLED PN 65-56185-2, IAW S RM 51-30-1 AND DWG 65-56185. 2 L 7 3 4F A3WE 2007111400089 20071114 00089 SO 2007 11 14 CHQA200700072 1 20071108 A 2752 3632001003 DRIVE UNIT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL TE FLAPS FAULTY A CHQA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 GL 11 262SK 19094 145168 CAE312351 RDU TO CLE - ON APPROACH TO CLE FLAPS WERE SELECTED FROM 0 TO 9 DEGREES AND SHORTLY AFTERWARDS, A FLAP LOW SPEED MESSAGE APPEARED FOLLOWED BY FLAP FAIL. THE FLAP POSITION INDICATOR SHOWED FLAPS AT ZERO DEGREES. THE QRH WAS FOLLOWED AND TH E AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE CMC FOR FAULT CODES AND FOUND A MESSAGE FOR FLAP JAMMI NG. DURING TROUBLE SHOOTING THE RIGHT FLAP VELOCITY SENSOR, RIGHT FLAP MOTOR BRAKE, AND THE RIGHT FLAP MOTOR WERE ALL R EPLACED WITH NO FIX. THE SYSTEM WAS FINALLY TROUBLESHOT DOWN TO A FAULTY FLAP POWER DRIVE UNIT. THE FLAP POWER DRIVE U NIT WAS REPLACED AND THE FLAPS WERE RIGGED TO THE ZERO POSITION. FLAP OPERATIONAL CHECKS ON THE GROUND AND DURING THE T 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007111400090 20071114 00090 NM 2007 11 14 QXEA200701633 1 20071030 A 5320 FLOOR SUPPORT BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - THE AFT FLOOR SUPPORT FLANGE FOR FLOOR PANEL 131DZ HAS CORROSION AT THE SCREW HOLES STATION 32.4. REPAIRED IAW SRM 51-21-00, 5114-00. 2 H 7 2 4T RT A13NM 2007111400091 20071114 00091 NM 2007 11 14 QXEA200701634 1 20071030 A 5730 ACCESS PANEL BOMBDR DHC8 DHC8402 1390042 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - LEFT WING FUEL PANEL 524BT HAS MINOR CHAFE DAMAGE INBOARD AND OUTBOARD ENDS. REPAIRED IAW SRM 51-14-00, 51-25- 10, 51-21-01. 2 H 7 2 4T RT A13NM 2007111400092 20071114 00092 2007 11 14 HALA0700475 4 20071109 A 2397 9640453011 COUPLER BOEING 767 76733A 1385209 NM NR 2 HF SYSTEM DAMAGED A HALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 13 589HA 33422 AIR TURN BACK ETOPS SIGNIFICANT SYSTEM UNABLE TO TRANSMIT ON BOTH HF RADIOS. REPLACED NR 2 HF COUPLER PER AMM 23-11-01- 024-001 AND 23-11-01-424-008. 2 L 7 2 4F RT A1NM 2007111400093 20071114 00093 NM 2007 11 14 DU4R2007182 1 20071029 A 5711 SPAR BOEING 757 7572Q8 1384972 NM RWS 790 CUT B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 710TW 28169 RT WING REAR SPAR UPPER CHORD CUT APPROX 4 FROM SPAR END FITTING AT WSTA 790. REPAIRED BY CUTTING OUT SECTION OF CHORD, FABRICATED AND INSTALLED CHORD AND SPLICE ANGLES IAW BOEING DWG 112N1006 AND DELTA/TIMCO MRR NR CPZ-LCQ-07-291-67-60001 -IR. 2 L 7 2 4F RT A2NM 2007111400094 20071114 00094 NM 2007 11 14 DU4R2007183 1 20071109 A 5315 FLOORBEAM BOEING 757 7572Q8 1384972 NM BS 1640 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 710TW 28169 FOUND CORROSION IN MAIN CABIN FLOORBEAM UPPER CAP AT BS 1640 BETWEEN LBL 6 TO RBL 6. REPAIRED BY FABRICATING AND INSTAL LED REPAIR ANGLES AND STRAPS FROM 7075-T6 .063 AND 7075-T6 .071, S ANGLE FROM BAC1490-2865 IAW B757 SRM 53-00-51 AND 51- 40-02. 2 L 7 2 4F RT A2NM 2007111400123 20071114 00123 NM 2007 11 14 DL76G071444 1 20071111 A 5315 BAC1505100393 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 645 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 152DL 24984 CABIN BS645+66 AT RBL 32 FLOORBEAM UPPER CHORD CORRODED. REPAIRED PER 53-00-51 FIGURE 201 ON NR CARD APP521473 BY REPLA CEMENT OF UPPER CHORD. 2 L 7 2 4F RT A1NM 2007111400124 20071114 00124 NM 2007 11 14 DL76S071445 1 20071110 A 3350 FUSE BOEING 767 767332 1382001 NM EMERGENCY LIGHTS BLOWN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 134DL 25123 EMERGENCY LIGHTS FROM 13AB TO 20AB INOP. FOUND FUSE BLOWN ON PWR SUPPLY M9008. REPLACED SAME EMERGENCY LIGHTS FROM 13A B TO 20AB, OP CK NML. 2 L 7 2 4F RT A1NM 2007111400125 20071114 00125 NM 2007 11 14 DL76G071446 1 20071112 A 2913 PUMP BOEING 767 767332 1382001 NM HYD SYSTEM UNKNOWN A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 1607B 30388 C HYD PUMP NR 1, RETURNED TO GATE, C1 ELECT HYD PUMP OPS OK AT GATE WITH ENGINES RUNNING SUSPECT ELECT LOAD SHED PROBLEM ALL OPS OK NOW. 2 L 7 2 4F RT A1NM 2007111400126 20071114 00126 NM 2007 11 14 DL738071448 1 20071112 A 3220 B73738N WHEEL BOEING 737 737832 13844CF NM NLG VIBRATION A DALA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SO 27 3739 30541 EXCESSIVE NOSE WHEEL VIBRATION/SHIMMY DURING TAKEOFF ROLL. DID NOT EXCEED 40 - 50 KNOTS. REPLACED BOTH NOSE WHEEL ASSY S. 2 L 7 2 4F RT A16WE 2007111400127 20071114 00127 NM 2007 11 14 DLM88071449 1 20071002 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM 1117-1148 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 FOUND AT HMV-3 CORROSION ON RT CUSP WEB BTWN STA 1117 AND 1148. REPAIRED PER 51-70-4. 2 L 7 2 4F RT A6WE 2007111400128 20071114 00128 NM 2007 11 14 DLM88071450 1 20070927 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 1136-1174 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 EXFOLIATION CORROSION ON LT CUSP WEB AT STA Y=1136 TO 1174. REPLACED WEB PER BOEING DWG 9930612. 2 L 7 2 4F RT A6WE 2007111400146 20071114 00146 2007 11 14 DLM88071469 4 20070927 A 2565 BRACKET DOUG MD88 MD88 3023688 NM L2 DOOR GIRT BAR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 EXFOLIATION CORROSION ON L2 DOOR GIRT BAR SUPPORT BRACKETS. REPLACED BRACKETS PER SRM 51-30-2 / 51-20-0. 2 L 7 2 4F RT A6WE 2007111400147 20071114 00147 NM 2007 11 14 DLM88071470 1 20070928 A 5320 ANGLE DOUG MD88 MD88 3023688 NM BS 160 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 EXFOLIATION CORROSION ON WEB AT FWD CABIN STRUCTURE STA Y=160 LBL 14 TO 54. REPLACED ANGLE PER DWG 9955780. 2 L 7 2 4F RT A6WE 2007111400148 20071114 00148 NM 2007 11 14 DLM88071471 1 20071006 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 1155-1174 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 CORROSION IN RT CUSP WEB BTWN STA 1155/1174. REPAIRED PER SRM 51-70-4. 2 L 7 2 4F RT A6WE 2007111400149 20071114 00149 NM 2007 11 14 DLM88071472 1 20071006 A 5347 SEAT TRACK DOUG MD88 MD88 3023688 NM BS 465 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 CORROSION ON SEAT TRACK AT STA Y=465 RBL54. REPLACED SEAT TRACK. 2 L 7 2 4F RT A6WE 2007111400150 20071114 00150 NM 2007 11 14 DLM88071473 1 20071006 A 5347 SEAT TRACK DOUG MD88 MD88 3023688 NM BS 498 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 CORROSION ON SEAT TRACK AT STA Y=498 RBL 54. REPLACED SEAT TRACK. 2 L 7 2 4F RT A6WE 2007111400151 20071114 00151 NM 2007 11 14 DLM88071474 1 20071007 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 1309 S6-7R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 CRACK ON FUS SKIN STA 1309 BTW LONG 6R ANR 7R. REPAIRED PER SRM 53-04D. 2 L 7 2 4F RT A6WE 2007111400152 20071114 00152 NM 2007 11 14 DLM88071475 1 20071012 A 5311 FRAME DOUG MD88 MD88 3023688 NM BS 1463 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 FOUND CRACKED ANGLES ON FRAME AT STA Y=1463 AFT SIDE. REPLACED ANGLES PER SRM 53-14-4. 2 L 7 2 4F RT A6WE 2007111400153 20071114 00153 NM 2007 11 14 DLM88071476 1 20071003 A 5347 SEAT TRACK DOUG MD88 MD88 3023688 NM BS 469-533 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 CORROSION ON SEAT TRACK AT LBL 22 STA Y=469 TO 471, 485/487501/502, 515/518, 530/533. REPLACED SEAT TRACKS. 2 L 7 2 4F RT A6WE 2007111400154 20071114 00154 NM 2007 11 14 DLM90071477 1 20071112 A 3260 833703 PROXIMITY SENSOR DOUG MD90 MD9030 3023690 NM RT MAIN GEAR INTERMITTENT A DALA O OTHER J WARNING INDICATION LD LANDING 1 SO 27 907DA 53387 RT MAIN GEAR INDICATION INOP. GREEN INDICATION LIGHT CAME ON DURING TAXI ROLL OUT AFTER LANDING . SUSPECT DOWN LOCK PR OX SENSOR. WILL UPDATE WHEN A/C BACK IN SERVICE. REPLACED RT GEAR DOWN/LOCK SENSOR. SWUNG GEAR SEVERAL TIMES. ALL CK S OK. 2 L 7 2 4F RT A6WE 2007111400159 20071114 00159 NM 2007 11 14 CALA0700646 1 20071102 A 5311 65C22910 FRAME BOEING 737 7373T0 1384582 NM BS 500D S26L CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND FRAME CORRODED AT STA 500D, ABOVE S26L. THE FRAME WAS REPAIRED IAW SRM 53-00-07. 2 L 7 2 4F RT A16WE 2007111400186 20071114 00186 EU 2007 11 14 USAA920071072 1 20071016 A 5320 D53112827200 DUMMY RAIL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - CORROSION ON CABIN DUMMY RAIL, BS 683 / FR 15 - BS 709 / FR 16, +Y503.2. REPLACED CABI N DUMMY RAIL, BS 683 / FR 15 - BS 709 / FR 16, +Y503.2 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007111500001 20071115 00001 EU 2007 11 15 USAA920071073 1 20071023 A 5320 D53480043203 SILL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - CORROSION ON R2 DOOR CUTOUT LOWER SILL, BS 3158 / FR 66, -Y1392. REPAIRED R2 DOOR CUTO UT LOWER SILL, BS 3158 / FR 66, -Y1392 IAW A320 SRM 53-41-14. 2 L 7 2 4F RT A28NM 2007111500003 20071115 00003 EU 2007 11 15 USAA920071075 1 20071028 A 5320 D53475765206 SILL AIRBUS 320 A320232 3930326 EU ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - CORROSION ON BULK CARGO DOOR CUTOUT LOWER SILL, BS 2883 / FR 61, -Y650. REPAIRED BULK CARGO DOOR CUTOUT LOWER SILL, BS 2883 / FR 61, -Y650 IAW A320 SRM 53-41-49. 2 L 7 2 4F RT A28NM 2007111500004 20071115 00004 EU 2007 11 15 USAA920071076 1 20071028 A 5320 D53475765206 SILL AIRBUS 320 A320232 3930326 EU ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - CORROSION ON BULK CARGO DOOR CUTOUT LOWER SILL, BS 2883 / FR 61, -Y640. REPAIRED BULK CARGO DOOR CUTOUT LOWER SILL, BS 2883 / FR 61, -Y640 IAW A320 SRM 53-41-49. 2 L 7 2 4F RT A28NM 2007111500005 20071115 00005 NM 2007 11 15 USAA920071077 1 20071026 A 5320 654580730 ANGLE BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED CABIN WEB ANGLE, BS 291.5, S12R - S13R. REPLACED CABIN WEB ANGLE, BS 291.5, S1 2R - S13R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007111500007 20071115 00007 NM 2007 11 15 USAA920071079 1 20071028 A 5340 69387902 STRINGER CLIP BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C-20 CHECK - CRACKED STRINGER CLIP, BS 597, S10L. REPLACED STRINGER CLIP, BS 597, S10L IAW B737 SR M 51-40-02. 2 L 7 2 4F RT A16WE 2007111500009 20071115 00009 NM 2007 11 15 USAA920071081 1 20071030 A 5753 SKIN BOEING 737 7373B7 1384580 NM LT WING TE FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 0332 23384 MCN - MAJOR REPAIR - C-20 CHECK - LEFT WING TRAILING EDGE INBOARD MIDFLAP LOWER SURFACE DELAMINATED, WBL 153 - WBL 155. REPAIRED LEFT WING TRAILING EDGE INBOARD MIDFLAP LOWER SURFACE, WBL 153 - WBL 155 IAW B737 SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007111500012 20071115 00012 NM 2007 11 15 USAA920071084 1 20071101 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED INTERCOSTAL STRAP, BS 330.5, LBL 12. REPLACED INTERCOSTAL STRAP, BS 330.5, LBL 12 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007111500013 20071115 00013 NM 2007 11 15 USAA920071085 1 20071101 A 5320 651768469 INTERCOSTAL BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED L1 DOOR CUTOUT INTERCOSTAL ANGLE, BS 303.9, S13L. REPLACED L1 DOOR CUTOUT INTE RCOSTAL, BS 254 - BS 303, S13L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007111500014 20071115 00014 NM 2007 11 15 USAA920071086 1 20071005 A 5754 114N407519 PANEL BOEING 757 7572B7 1384964 NM NR 1 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEFT WING NR 1 SLAT COVE PANEL CRACKED, WS 736. REPLACED LEFT WING NR 1 SLAT COVE PANEL , WS 736 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007111500016 20071115 00016 NM 2007 11 15 USAA920071088 1 20071009 A 5320 SUPPORT ANGLE BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON THE R4 DOOR CUT LOWER SILL THRESHOLD FORWARD SUPPORT ANGLE CHANNEL CLIP, BS 1640, RBL 58.22. REPLACED THE R4 DOOR CUT LOWER SILL THRESHOLD FORWARD SUPPORT ANGLE CHANNEL CLIP, BS 1640, RBL 58.22 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007111500017 20071115 00017 NM 2007 11 15 USAA920071089 1 20071009 A 5320 146N876948 SUPPORT ANGLE BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON THE R4 DOOR CUT LOWER SILL THRESHOLD MID SUPPORT ANGLE, BS 1671, RBL 58.22. REPLACED THE R4 DOOR CUT LOWER SILL THRESHOLD MID SUPPORT ANGLE, BS 1671, RBL 58.22 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007111500019 20071115 00019 NM 2007 11 15 USAA920071091 1 20071012 A 5754 114T3166 ATTACH ANGLE BOEING 767 767201 1385125 NM ZONE 600 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 248AY 23900 MIA - MAJOR REPAIR - C-2 CHECK - RIGHT WING SLAT NR 7 INNER LOWER SKIN ATTACH ANGLE CRACKED, WS 274.7. REPLACED RIGHT W ING SLAT NR 7 INNER LOWER SKIN ATTACH ANGLE, WS 274.7 IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007111500020 20071115 00020 NM 2007 11 15 USAA920071092 1 20071012 A 5754 114T316672 ATTACH ANGLE BOEING 767 767201 1385125 NM NR 7 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 248AY 23900 MIA - MAJOR REPAIR - C-2 CHECK - RIGHT WING SLAT NR 7 INNER LOWER SKIN ATTACH ANGLE CRACKED, WS 284.7. REPLACED RIGHT WING SLAT NR 7 INNER LOWER SKIN ATTACH ANGLE, WS 284.7 IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007111500021 20071115 00021 NM 2007 11 15 USAA920071093 1 20071011 A 5753 113T317521 SUPPORT ANGLE BOEING 767 767201 1385125 NM LT WING TE FLAP CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 248AY 23900 MIA - MAJOR REPAIR - C-2 CHECK - LEFT WING TRAILING EDGE OUTBOARD FLAP INBOARD EDGE AFT SUPPORT ANGLE CRACKED, WS 355. REPLACED LEFT WING TRAILING EDGE OUTBOARD FLAP INBOARD EDGE AFT SUPPORT ANGLE CRACKED, WS 355 IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007111500022 20071115 00022 NM 2007 11 15 USAA920071094 1 20071103 A 5210 507945178 DOOR FRAME BOEING 737 7373G7 1384595 NM BS 344 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, CRACKED FORWARD ENTRY DOOR AFT FRAME, BS 344, WL 232. REPAIRED FORWARD ENTRY DOOR AFT F RAME, BS 344, WL 232 IAW USAIRWAYS EA 98952. 2 L 7 2 4F RT A16WE 2007111500024 20071115 00024 NM 2007 11 15 SWAA075528 1 20071104 A 5312 6545819 PRESSURE PANEL BOEING 737 7373H4 1384600 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND NLG W/W UPPER CEILING PANEL CRACKED AT RBL 7.75. REPAIRED PANEL PER ACO. 2 L 7 2 4F RT A16WE 2007111500025 20071115 00025 NM 2007 11 15 SWAA075529 1 20071104 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 440 S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007111500026 20071115 00026 NM 2007 11 15 SWAA075530 1 20071104 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500D S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007111500029 20071115 00029 NM 2007 11 15 SWAA075523 1 20071104 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500032 20071115 00032 NM 2007 11 15 SWAA075514 1 20071101 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 733A S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733A, STR 4R. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007111500033 20071115 00033 NM 2007 11 15 SWAA075497 1 20071103 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED MV2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007111500034 20071115 00034 NM 2007 11 15 SWAA075498 1 20071104 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 960-967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED 14Y CHECK, FOUND STRINGER 27L CORRODED BETWEEN BS 960 AND BS 967. REPAIRED STRINGER PER ER. 2 L 7 2 4F RT A16WE 2007111500035 20071115 00035 NM 2007 11 15 SWAA075515 1 20071104 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500037 20071115 00037 NM 2007 11 15 SWAA075500 1 20071103 A 5755 6552132 ATTACH FITTING BOEING 737 7373H4 1384600 NM NR 4 SPOILER WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED 14Y CHECK, FOUND LT WING NR 4 SPOILER INBOARD ATTACH FITTING LOOSE. REPAIRED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007111500038 20071115 00038 NM 2007 11 15 SWAA075501 1 20071103 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM BS 867 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500039 20071115 00039 NM 2007 11 15 SWAA075502 1 20071101 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 424WN 29828 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 146. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500047 20071115 00047 NM 2007 11 15 SWAA075516 1 20071104 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 400 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED ANAD REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007110900383 20071109 00383 EU 2007 11 9 F3LA200700313 1 20071017 A 5320 SUPPORT AIRBUS A319 A319112 3930323 EU FUSLEAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION AT FLOOR WEB NUTPLATE IN FWD CARGO COMPARTMENT, AFT RT CORNER, WHERE T RANSITION PANEL, AFT CARGO WALL AND FLOOR MEET. REMOVED CORRODED TRANSITION STRIP AT AFT BULKHEAD IAW SRM 51-42-11, PAR A. 6. INSTALLED NEW TRANSITION STRIP AT AFT BULKHEAD IN FWD CARGO COMPARTMENT IAW SRM 51-42-11, PARA 6 AND 17. 2 L 7 2 4F RT A28NM 2007110900389 20071109 00389 NM 2007 11 9 2007UALA04529 1 20071101 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 887 S20L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 LT FUSELAGE SKIN 2 EACH DENTS AT BS 887 APPROX 6 INCHES ABOVE STRINGER L20 JUST FWD AND AFT OF OF 887 L FRAME. REMOVED DAMAGE AND INSTALLED REPAIR REF SRM 53-00-01 REPAIR 31 FIG 201. 2 L 7 2 4F 4 F RT A16WE E2GL 2007111300003 20071113 00003 NM 2007 11 13 MWEA070271 1 20071105 A 7830 715923505 DOOR FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 907ME 55171 UPPER DEFLECTOR DOOR Z FRAME CRACKED IN RADIUS AT STATION 26.6 LEFT SIDE AT OUTER SKIN JOINT LOCATION. FABRICATED AND I NSTALLED ANGLE. 2 L 7 2 4F TR A6WE 2007111300043 20071113 00043 NM 2007 11 13 2007UALA04556 1 20071102 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 580 S22-23L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 FWD CARGO PIT FUSELAGE FRAME, DENTED AT UPPER FLANGE, BS 580 AND STR 22L-23L. 2 L 7 2 4F 4 F RT A2NM E17NE 2007111300044 20071113 00044 NM 2007 11 13 2007UALA04557 1 20071104 A 3397 59191 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 EMERGENCY ESCAPE PATH LIGHTING AFT OF DOOR 2L BETWEEN SEATS 9-13 INOPERATIVE. REPLACED EEL LAMP CABLE. OPS CHECKED OKA Y. 2 L 7 2 4F 4 F RT A2NM E17NE 2007111300045 20071113 00045 NM 2007 11 13 2007UALA04558 1 20071104 A 3350 1317 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 540UA 25252 EMERGENCY LIGHT BETWEEN SEAT 3-4 LH UNDER STOW BIN INOP. RELAMPED. OPS CHECKED OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007111300046 20071113 00046 2007 11 13 2007UALA04559 4 20071102 A 2565 COVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 CABIN SERVICE REPORTED AFT LT DOOR SLIDE COVER FELL OFF. 2 L 7 2 4F 4 F RT A2NM E17NE 2007111300047 20071113 00047 NM 2007 11 13 2007UALA04560 1 20071104 A 3520 OXYGEN BOTTLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 BOTH OXYGEN BOTTLES IN AFT CABIN RIGHT SIDE SHOW BELOW THE GREEN ARC. SUSPECT LEAK AT FILLER VALVE. REPLACED BOTTLES. A CFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007111300048 20071113 00048 NM 2007 11 13 2007UALA04561 1 20071104 A 2913 731966 PUMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE HYD SYSTEM UNKNOWN A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 649UA 25286 RTFL DUE TO CENTER HYDRAULIC PUMP PROBLEM. REPLACED HYDRAULIC AIR DRIVEN PUMP. ALSO REPLACED HYD LINES & PUMP MOUNTS . PERFORMED SYSTEM CHKS. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007111300049 20071113 00049 NM 2007 11 13 2007UALA04562 1 20071102 A 3350 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 FOUND ROWS 15-18 LEFT SIDE OF ACFT EMERGENCY EXIT LIGHTS KEEP COMING ON. REPLACED BATTERY AND FOUND CONNECTOR LOOSE, SY STEM CHECKED NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007111300050 20071113 00050 NM 2007 11 13 2007UALA04563 1 20071103 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 BUSINESS CLASS FLOOR LIGHTING INOP ON LEFT SIDE. SECURED CONNECTOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2007111300051 20071113 00051 NM 2007 11 13 2007UALA04564 1 20071103 A 4900 893003 CHARGER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE APU BATTERY FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 664UA 29236 APU BATTERY DOES NOT CHARGE. SUSPECT FAULTY BATTERY CHARGER. REPLACED APU BATTERY AND CHARGER OPS CHECKED GOOD. ACFT O K FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007111300053 20071113 00053 NM 2007 11 13 2007UALA04566 1 20071102 A 2910 LINE BOEING 727 727222 1384073 NM PWA PW4077 PW4077 NE HYD SYSTEM LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 WP 29 780UA 26944 HYD QTY LOW C CENTER HYDRAULIC SYSTEM LOW RESERVOIR QUANTITY. FOUND LT MLG SIDE BRACE DOWNLOCK ACTUATOR HOSE LEAKING RE F IPC 32-32-04 ITEM 30. REPLACED HYDRAULIC LINE, CLEANED AREA, PRESSURIZED HYD SYSTEM &LEAK CHECKED OK. 2 L 7 3 4F 4 F A3WE E46NE 2007111300054 20071113 00054 NM 2007 11 13 2007UALA04567 1 20071102 A 3520 OXYGEN SYSTEM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE PAX READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 196UA 28715 PAX O2 LOW. 2 L 7 4 4F 4 F RT A20WE E24NE 2007111300055 20071113 00055 NM 2007 11 13 2007UALA04568 1 20071102 A 5100 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE UNKNOWN UNKNOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 595UA 28748 FA REPORTS HOT SPOT AT SEAT 15A SIDEWALL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007111300056 20071113 00056 2007 11 13 2007UALA04571 4 20071104 A 2397 COUPLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HF SYSTEM INOPERATIVE A UALA O OTHER O OTHER CR CRUISE 1 WP 29 547UA 25368 RIGHT HF INOPERATIVE IN TRANSMIT. TRIED NEW TRANCEIVER NO HELP. SWAPPED RADIO CONTROL PANELS, NO HELP. REPLACED RIGHT HF COUPLER, CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007111300057 20071113 00057 NE 2007 11 13 2007UALA04572 2 20071103 A 7261 ENGINE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 1 LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 666UA 29238 727850 (NR 1 ENG HOC): OIL LEAKING FROM FUEL PUMP DRAIN 4 DPM WITH ENG STATIC. 2 L 7 2 4F 4 F RT A1NM E24NE 2007111300058 20071113 00058 NM 2007 11 13 2007UALA04573 1 20071104 A 2421 FILTER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LT IDG CLOGGED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 226UA 30226 LEFT IDG "FILTER BLOCKED" ON ELECTRICAL PAGE. DELTA P IS POPPED. NO DEPOSITS FOUND IN FILTER. INSTALLED NEW FILTER PER MM24-11-02. OPERATED ENGINE AT IDLE AND FILTER MSG ON ELECT PAGE NOW NORMAL. A/C OK FOR SERVICE 2 L 7 2 4F 4 F RT T0001SE E46NE 2007111300059 20071113 00059 NM 2007 11 13 2007UALA04575 1 20071104 A 3510 OXYGEN SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 303UA 23644 CREW O2 LOW READS 700LBS. SERVICED CREW OXYGEN AND CHECKED SYSTEM FOR LEAKS- NONE FOUND. NO REPEATS. 2 L 7 2 4F 4 F RT A16WE E2GL 2007111400004 20071114 00004 NM 2007 11 14 MWEA070281 1 20071102 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 617-598 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 601ME 49762 CORROSION ON LEFT FLOOR SUPPORT STRUCTURE PASSENGER CUSP MEMBRANE CABIN BETWEEN STATION 617 TO 598. REMOVED CORROSION F ABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 2007111400009 20071114 00009 NM 2007 11 14 MWEA070287 1 20071102 A 5315 FLOORBEAM DOUG MD88 MD88 3023688 NM BS 1331 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 601ME 49762 AT STATION 1311 FLOOR LEVEL CENTER AREA BETWEEN AFT LAVATORY HAS CORROSION AT FLOORBEAM. REMOVED CORROSION, FABRICATED AND INSTALLED FLANGE. 2 L 7 2 4F RT A6WE 2007111400014 20071114 00014 NM 2007 11 14 07FDEA04734 1 20071107 A 5320 651759369 ANGLE BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 MAIN DECK FLOOR SUPPORT IS CORRODED, BS 328-344, LBL 29, WL 208. REMOVED CORROSION IAW SRM 51-10-6, FOUND TO BE OUT OF LIMITS ORIGINAL .080'. REMOVED .025" (DEEPEST POINT ) REMAINING .055', IAW SRM 53-10-01, TOOL AAR IND -0213, CAL DUE 10 -15-08. REMOVED FLOOR SUPPORT, FABRICATED, TREATED AND PRIMED, AND INSTALLED FLOOR SUPPORT, AND FILLER IAW SRM 51-30- 2, 51-10-2, 51-20-1, AND BOEING DWG, 65-17593. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2007111400017 20071114 00017 NM 2007 11 14 07FDEA04738 1 20071107 A 5315 BAC14902773 FLOORBEAM BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 MAIN DECK FLOORBEAM UPPER FLANGE IS CRACKED AT FLOOR PANEL FASTENER HOLE, BS 328 FWD, LBL 19, WL 208. CUT OUT DAMAGE AT BS 328, LBL 18.25 TO LBL 21. FABRICATED AND DRILLED REPAIR PARTS. TREATED AND PRIMED AND TOP COATED REPAIR PARTS. I NSTALLED REPAIR TOP COATED UPPER SURFACE OF FLOORBEAM AT REPAIR AREA. APPLIED 1 COAT OF LPS TO REPAIR AREA. REF SRM 5 3-10-8 FIG 9, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007111400022 20071114 00022 NM 2007 11 14 07FDEA04743 1 20071107 A 5720 651928917 ANGLE BOEING 727 727225 1384077 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 LT OTBD AILERON BAY BAFFLE SEAL IS CRACKED AT INBD ANGLE (MKD) TO FASTENER HOLE REMOVED AND REPLACED AILERON BAY BAFFLE ANGLE REF DWG 65-19289 AND SRM 51-30-2. APPLIED PN FX 65-19289-17 REF FED EX GMM 7-0-1001. 2 L 7 3 4F A3WE 2007111400034 20071114 00034 NM 2007 11 14 DL777071408 1 20071102 A 2530 72077500 OVEN BOEING 777 777232 1385232 NM GALLEY ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 861DA 29952 F/C GALLEY OVENS (BOTH) OVERHEATS AND HAS ELECT ODOR. ODOR DISSIPATED WITH BOTH OVEN C/B`S PULLED. FWD TO MCO AND PLAC ARD PER MEL 25-20-01G. OTHER ITEMS IN FWD GALLEY CHECKED, NO PROBLEMS FOUND. RAN BOTH OVENS FOR 1 HR NOTED NO ELECTRIC AL ODOR. OVENS OK SERVICE. MCO/PLAC REMOVED. 2 L 7 2 4F RT T00001SE 2007111400035 20071114 00035 NM 2007 11 14 DL757071409 1 20071104 A 2121 6457053 FAN BOEING 757 757232 1384965 NM RECIRCULATION FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 6712B 30484 DIVERSION DUE TO SULFUR ODOR IN COCKPIT AND CABIN. FOUND LEFT RECIRCULATION FAN AS SOURCE OF ODOR. LEFT RECIRCULATION FAN REPLACED. 2 L 7 2 4F RT A2NM 2007111400044 20071114 00044 NM 2007 11 14 DLM90071419 1 20071001 A 5320 INTERCOSTAL DOUG MD90 MD9030 3023690 NM FS 1326 L30 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 AFT CARGO FS 1326 L-30 INTERCOSTAL TIE CLIP CORRODED ON LOWER SURFACE. FABRICATED NEW PART IAW MD-90 SRM 51-10-05 VOL I I ON N/R 1600-0248 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007111400047 20071114 00047 NM 2007 11 14 DLM90071422 1 20071001 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM FS 1212-1364 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 CABIN SEAT TRACK CORRODED OUT OF LIMITS FS 1212-1364 RBL 24. REMOVED AND REPLACED SEAT TRACK IAW MD-90 SRM 53-40-01 AND 51-30-02 ON N/R 2700-0206 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007111400052 20071114 00052 NM 2007 11 14 DLM90071427 1 20071031 A 5330 SKIN DOUG MD90 MD9030 3023690 NM BS 229 L17L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 LEFT FUSELAGE SKIN AT STATION 229 AND LONG 17 LT IS A DENT. CUT OUT DAMAGE AND REPAIRED IAW MD-80 SRM 53-04D FIG 12 B S H 35 ON N/R 2000-0068 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007111400060 20071114 00060 SO 2007 11 14 SIMA200731201 1 20071104 A 2120 UNKNOWN EMB 135 EMB135KL 3260302 SO CABIN SMOKE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 827AE 145602 SMOKE IN CABIN AFTER TAKEOFF, SMOKE DISSIPATED. 2 L 7 2 4F RT T00011AT 2007111400063 20071114 00063 EU 2007 11 14 TRAX200701671 1 20071102 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 RT SEAT TRACK BTW FR 39-40 FOUND CORRODED OUT OF LIMIT ON W/C 200-115 NEEDS TO BE FABRICATED, RESOLVED ON W/O: 74559 TAS KCARD: N/R-00552. NEW RT SEAT TRACK BTW FR 39-40 HAS BEEN FABRICATED IAW SRM 53-33-00 FIG 101. INSTALLATION COVERED ON W/C 200-115. 2 H 7 2 4T RT A53EU 2007111400070 20071114 00070 NM 2007 11 14 07FDEA04750 1 20071107 A 5313 STRINGER BOEING 757 7572B7 1384964 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 S26L HAS MINOR DAMAGE ON FREE FLANGE BETWEEN STA 510 AND 560 REMOVED DAMAGED SECTION OF STRINGER IAW SRM 53-00-03 REPAIR NR 2. FABRICATED 2 STRINGER SPLICES FROM BAC 1498-294 BATCH 3332A6. FABRICATED 3 SHIMS FROM 7075 T6 .025 BATCH 125602 2 IAW SRM 53-00-03. REPAIR NR 2 FABRICATED STRINGER CLIP PER TRAVELER T7/691821. TREATED AND PRIMED STRINGER SPLICES, SHIMS (3 EACH) AND STRINGER CLIP IAW SRM 51-20-01. INSTALLED SPLICES, SHIMS AND STRINGER CLIP IAW SRM 51-40-02. REPAI R ACCEPTED PER EAR 67597370071. 2 L 7 2 4F RT A2NM 2007111400073 20071114 00073 NM 2007 11 14 07FDEA04755 1 20071108 A 5320 ANGLE BOEING 757 7572B7 1384964 NM BS 1640 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 AFT CARGO PIT, STA 1640 - FRAME AT LBL 7, L ANGLE SUPPORT HAS A DRILL START AND BARE METAL. BLENDED AREA IAW SRM 53-00- 03. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03, FIG 101. REMOVED AND FABRICATED NEW L ANGLE/CHORD IAW SRM 51-10-02 AND MAE TRAVELER NR T7/690614. TREATED, PRIMED AND PAINTED FABRICATED L ANGLE/CHORD IAW SRM 51-20-01. INSTALLED NEWLY FAB RICATED L ANGLE/CHORD IAW SRM 51-40-02. THIS REPAIR IS ACCEPTED BY MAE ENGINEERING PER EAR NR 67597370061. REPAIR IS A MAJOR DUE TO EFFECTING THE FRAME, BY MEANS OF ATTACHMENT. 2 L 7 2 4F RT A2NM 2007111400077 20071114 00077 NM 2007 11 14 HALA070071 1 20071029 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 654 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 LEVEL 1 CORROSION ON SEAT TRACK AT RBL 11 STAT 654+13 TO 654+18. REMOVED CORROSION IAW 767 SRM 51-10-02 WITHIN LIMITS O F SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2007111400081 20071114 00081 2007 11 14 QXEA200701706 4 20071108 A 3420 IRS DHAV DHC8 DHC8202 2809007 NM MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 369PH 513 PDX - ON FLIGHT 2154, RETURNED TO GATE, UNABLE TO GET IRS TO ALIGN. MAINTENANCE REINITIALIZED IRS. OPERATIONAL CHECK G OOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007111400095 20071114 00095 NM 2007 11 14 DU4R2007184 1 20071111 A 5315 FLOORBEAM BOEING 757 7572Q8 1384972 NM BS 345 CORRODED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 710TW 28169 FOUND CORROSION IN MAIN CABIN FLOORBEAM UPPER CAP AT BS 345 RBL 2. REPAIRED BY CUTTING OUT CORRODED AREA OF FLOORBEAM, FABRICATED AND INSTALLED REPAIR 7075-T6 .071" IAW B757 SRM 53-00-51 AND 51-40-02. 2 L 7 2 4F RT A2NM 2007111400096 20071114 00096 SO 2007 11 14 CHQA200700073 1 20071108 A 2760 852701 PROXIMITY SWITCH EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL SPOILERS FAILED A CHQA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 11 374SK 145544 CAE311206 STL TO BDL. - WHILE CLIMBING PAST 26,000 FT EN ROUTE TO BDL, FLIGHT CREW RECEIVED "SPOILER FAIL" EICAS MESSAGE, ACCOMPAN IED BY AN OPEN SPOILER INDICATION. THERE WERE NO CHANGES TO THE FLIGHT CHARACTERISTICS OF THE AIRCRAFT, AND IT WAS LEVE LED OFF TO TROUBLESHOOT AND RUN THROUGH THE QRH. THE AIRCRAFT LANDED WITHOUT INCIDENT AND WAS TURNED OVER TO MAINTENANC E. MAINTENANCE TROUBLESHOT THE SPOILER SYSTEM AND REPLACED THE RIGHT OUTBOARD SPOILER PROXIMITY SWITCH. AFTER REPLACEM ENT OF THE PROXIMITY SWITCH, THE SPOILER SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007111400120 20071114 00120 NM 2007 11 14 DLM90071439 1 20071108 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FS 543 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 RT CUSP WEB CORRODED OUT OF LIMITS FS 543. REPAIRED RT CUSP WEB FS 503-597 IAW MD-88 SRM 53-05D ON N/R 2400-0233 AT HMV -2 IN OKC. 2 L 7 2 4F RT A6WE 2007111400121 20071114 00121 GL 2007 11 14 DL764071440 2 20071109 A 7200 CF680C2B8F ENGINE BOEING 767 767424ER 1385270 NM GE CF6 CF680C2* GL NR 2 FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 828MH 24552 29699 706163 ENG FAILED OPERATION 5040. REMOVED AND REPLACED NR 2 ENG PER TRANS 14T104. 2 L 7 2 4F 4 F RT A1NM E23EA 2007111400122 20071114 00122 NM 2007 11 14 DLM90071442 1 20071109 A 3260 862102 UPLOCK SENSOR DOUG MD90 MD9030 3023690 NM RIGHT OUT OF ADJUST A DALA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 27 908DA 53388 RT MLG SLOW TO RETRACT. FOUND SENSOR D1-25 OUT OF ADJUSTMENT ADJUSTED SAME CKS OK. 2 L 7 2 4F RT A6WE 2007111500006 20071115 00006 NM 2007 11 15 USAA920071078 1 20071025 A 5320 69374024 ANGLE BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C-20 CHECK - CRACKED SPLICE ANGLE, BS 294, S17R, WL 208. REPLACED SPLICE ANGLE, BS 294, S17R, WL 2 08 IAW BOEING DRAWING 69-37402-4. 2 L 7 2 4F RT A16WE 2007111500015 20071115 00015 NM 2007 11 15 USAA920071087 1 20071009 A 5320 146N52465 SUPPORT ANGLE BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON THE L4 DOOR CUT LOWER SILL SUPPORT ANGLE, BS 1640 - BS 1676, LBL 58.22. RE PLACED THE L4 DOOR CUT LOWER SILL SUPPORT ANGLE, BS 1640 - BS 1676, LBL 58.22 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007111500031 20071115 00031 2007 11 15 SWAA075496 4 20071102 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007111500036 20071115 00036 2007 11 15 SWAA075499 4 20071103 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED 14Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM. 2 L 7 2 4F RT A16WE 2007111500041 20071115 00041 NM 2007 11 15 SWAA075503 1 20071101 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 433LV 33716 DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500042 20071115 00042 NM 2007 11 15 SWAA075519 1 20071101 A 3350 307BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 458WN 33857 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007111500043 20071115 00043 NM 2007 11 15 SWAA075505 1 20071104 A 3350 767 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 467WN 33830 DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007111500044 20071115 00044 NM 2007 11 15 SWAA075521 1 20071101 A 3350 8100022602 LIGHT BOEING 737 7377H4 1384404 NM ROW 1 ABC LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 469WN 33859 EEPLS STRIP LOOSE AT ROW 1 ABC. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007111500045 20071115 00045 2007 11 15 SWAA075520 4 20071101 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 476WN 32475 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007111500046 20071115 00046 NM 2007 11 15 SWAA075506 1 20071104 A 3350 20131A BATTERY PACK BOEING 737 7375H4 138449D NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SERVICE CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 2 DEF. REMOVED AND REPLACED BATTERY PAC K PER MM. 2 L 7 2 4F RT A16WE 2007111500048 20071115 00048 NM 2007 11 15 SWAA075507 1 20071104 A 3350 1619 LAMP BOEING 737 73776Q 13845AA NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 551WN 30280 DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER M M. 2 L 7 2 4F RT A16WE 2007111500051 20071115 00051 NM 2007 11 15 SWAA075494 1 20071031 A 2121 215201 FAN BOEING 737 7373H4 1384600 NM GASPER INOPERATIVE A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 626SW 27702 GASPER FAN CONTROL C/B TRIPPED INFLIGHT. RESET ATTEMPTED DUE TO FUMES IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM . 2 L 7 2 4F RT A16WE 2007111500052 20071115 00052 NM 2007 11 15 SWAA075533 1 20071104 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 500 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 633SW 27936 DURING SCHEDULED SPV CHECK, FOUND STRINGER 16R CRACKED AT BS 500. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007111500053 20071115 00053 NM 2007 11 15 SWAA075510 1 20071103 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM EMERGENCY EXIT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 LEFT FWD CABIN EMERGENCY EXIT SIGN LOOSE. SECURED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007111500054 20071115 00054 NM 2007 11 15 SWAA075511 1 20071102 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM BS 980 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 980, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007111500055 20071115 00055 NM 2007 11 15 SWAA075512 1 20071103 A 3350 3071BPEGPL LAMP BOEING 737 7373Q8 1384670 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 5 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007111500057 20071115 00057 EA 2007 11 15 COMA0770058 1 20071024 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS DISCHARGED A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 642CA 23955 10125 FLIGHT 5273 - SEVERAL CABIN EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY PACK. 2 L 7 2 4F RT A21EA 2007111500058 20071115 00058 EA 2007 11 15 COMA0770059 1 20071024 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS DISCHARGED A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 642CA 28206 10125 FLIGHT 5273 - SEVERAL CABIN EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED NR 1 EMERGENCY BATTERY PACK. 2 L 7 2 4F RT A21EA 2007111500059 20071115 00059 EA 2007 11 15 COMA0770060 1 20071024 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS DISCHARGED A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 642CA 22970 10125 FLIGHT 5273 - SEVERAL CABIN EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY PACK. 2 L 7 2 4F RT A21EA 2007111500061 20071115 00061 EA 2007 11 15 COMA0770061 1 20071024 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS DISCHARGED A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 642CA 3860 10125 FLIGHT 5273 - SEVERAL CABIN EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED NR 3 EMERGENCY BATTERY PACK. 2 L 7 2 4F RT A21EA 2007111500062 20071115 00062 EA 2007 11 15 COMA0760608 1 20071022 A 2120 FILTER CNDAIR CL600 CL6002B19 1900309 EA CABIN AIR UNKNOWN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 932CA 7038 FLIGHT 5127 - RECEIVED DISPLAY COOL CAUTION MESSAGE. DECLARED EMERGENCY, RETURNED TO MDT AND LANDED WITHOUT INCIDENT. CLEANED DEBRIS FROM DISPLAY SUPPLY FILTER. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007111500064 20071115 00064 2007 11 15 ASAA0752196 4 20071102 A 2310 8220990004 TRANSCEIVER BOEING 737 737890 1384527 NM HF DATA LINK INOPERATIVE A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 584AS 35682 HF DATA LINK INOP. CW MM 23-11-00 NORMAL AND MM 23-27-00 NORMAL. UNABLE TO DUPLICATE. AIRCRAFT RELEASED FOR A NON ETO PS VERIFICATION FLIGHT TO CHECK NR 2 HF DATA LINK. NON ETOPS VERIFICATION FLIGHT SATISFACTORY. 2 L 7 2 4F RT A16WE 2007111500065 20071115 00065 NM 2007 11 15 ASAA0752195 1 20071101 A 4940 38007021 STARTER GEN BOEING 737 737890 1384527 NM APU FAULTY A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 579AS 35187 APU "MAINT" LIGHT ILLUMINATED. PERFORMED BITE TEST OF APU REF FIM 49 60 TASK 801. MAINT MSG SHOWS NR 49 41244 START CO NV SHOWS FAILED GENERATOR DIODE. REPLACED APU STARTER CONVERTER AND STARTER GENERATOR. 2 L 7 2 4F RT A16WE 2007111500066 20071115 00066 NM 2007 11 15 ASAA0752197 1 20071102 A 4960 2118966222 ECU BOEING 737 737890 1384527 NM APU FAULTED A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 587AS 35684 APU AUTO SHUTDOWN AT GATE. REPLACED APU ECU IAW MM 49-61-12. 2 L 7 2 4F RT A16WE 2007111500068 20071115 00068 EA 2007 11 15 COMA0760610 1 20071024 A 5210 SWITCH CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 988CA 7204 FLIGHT 4956 - OVERBOARD COOL CAUTION ON CLIMBOUT. AIRCRAFT RETURNED TO CVG AND LANDED SAFELY. CLEANED AND LUBRICATED P AX DOOR OUTER HANDLE MICRO SWITCH DI 13. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007111500069 20071115 00069 EA 2007 11 15 COMA0760611 1 20071025 A 3010 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYS UNKNOWN A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 914CA 7012 FLIGHT 5588 - RECEIVED ANTI-ICE WARNING MESSAGE FOR LEFT FUSELAGE. DIVERTED TO ATL, LANDED WITHOUT INCIDENT. INSPECTED DUCTS AND LOOPS IN AFT EQUIPMENT BAY AND LEFT WHEEL WELL. PERFORMED RUN. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007111500070 20071115 00070 EA 2007 11 15 COMA0760612 1 20071025 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 933CA 7040 FLIGHT 4989 - EMERGENCY LIGHT INOP AT PAX DOOR. RELAMPED INOP EMERGENCY LIGHT. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007111500073 20071115 00073 NM 2007 11 15 2007UALA04523 1 20071101 A 3350 362624 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 RIGHT FWD OVERWING EXTERIOR EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007111500074 20071115 00074 EA 2007 11 15 COMA0760613 1 20071025 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS FAULTY A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 588SW 22100 7069 FLIGHT 5103 - EMERGENCY LIGHTS AT MAIN CABIN DOOR AND SERVICE DOOR INOP. REPLACED EMERGENCY LIGHT BATTERY PACK. NO FUR THER DEFECTS. 2 L 7 2 4F RT A21EA 2007111500076 20071115 00076 EA 2007 11 15 COMA0760615 1 20071025 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS FAULTY A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 588SW 21964 7069 FLIGHT 5103 - EMERGENCY LIGHTS AT MAIN CABIN DOOR AND SERVICE DOOR INOP. REPLACED EMERGENCY LIGHT BATTERY PACK. NO FUR THER DEFECTS. 2 L 7 2 4F RT A21EA 2007111500078 20071115 00078 EA 2007 11 15 COMA0760617 1 20071025 A 2760 SECU CNDAIR CL600 CL6002B19 1900309 EA SPOILERS MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 958CA 7111 ON FINAL RECEIVED GLD NOT ARMED MESSAGE AS WELL AS CAS MISCOMPARE STATUS MESSAGE. PERFORMED GO-AROUND AND QRH. GLD DID NOT DEPLOY. LANDED WITHOUT INCIDENT. NO FAULTS IN SECU. PERFORMED SECU BITE AND SPOILER SYSTEM TEST. RESET SYSTEM. PERFORMED SEVERAL OPS CHECKS. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007111500081 20071115 00081 EA 2007 11 15 COMA0760620 1 20071030 A 7830 1267587 PDU CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE FAULTY A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 403CA 512 7428 FLIGHT 5003 - LEFT T/R UNLOCK CAUTION MESSAGE EN ROUTE FROM BGR TO CVG. AIRCRAFT DIVERTED TO CMM AND LANDED SAFELY. RE MOVED AND REPLACED LEFT T/R PDU. 2 L 7 2 4F RT A21EA 2007111500082 20071115 00082 EU 2007 11 15 USAA920071096 1 20071103 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 647AW 28629 9594 762 FLT 9248 SFO - PHX - EEL - EMERGENCY LIGHTS AT ROWS 13L,17L, 22L, 26L AND AFT GALLEY INOP. REMOVED AND REPLACED BATTERY LT AFT EPSU, OPS AND BITE CHECK GOOD. 2 L 7 2 4F RT A28NM 2007111500083 20071115 00083 NM 2007 11 15 KCSA071509 1 20071106 A 5330 SKIN BOEING 747 747209B 138489B NM BS 680 S31-32R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 FUSELAGE SKIN DAMAGED AT SIDE OF FWD CARGO DOOR OPENING AT STA-680 BETWEEN STR-31R AND STR-32R. 2 L 7 4 4F RT A20WE 2007111500085 20071115 00085 NM 2007 11 15 SWAA075534 1 20071105 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 250WN 34972 DURING SCHEDULED MV3 CHECK, FOUND EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007111500086 20071115 00086 NM 2007 11 15 SWAA075535 1 20071105 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 254WN 32512 EEPLS LENS MISSING AT ROW 5 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007111500087 20071115 00087 NM 2007 11 15 SWAA075536 1 20071105 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2007111500088 20071115 00088 NM 2007 11 15 SWAA075538 1 20071105 A 5330 6445767 SKIN BOEING 737 7373H4 1384600 NM BS 675 S26R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 475, STR 26R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007111500089 20071115 00089 NM 2007 11 15 SWAA075537 1 20071105 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM BS 270 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 270, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500091 20071115 00091 NM 2007 11 15 SWAA075566 1 20071105 A 5311 6546595 FRAME BOEING 737 7373H4 1384600 NM BS 727A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500093 20071115 00093 NM 2007 11 15 SWAA075562 1 20071105 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727A S6R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007111500095 20071115 00095 NM 2007 11 15 SWAA075567 1 20071105 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM BS 727D S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500097 20071115 00097 NM 2007 11 15 SWAA075560 1 20071105 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727A S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007111500099 20071115 00099 NM 2007 11 15 SWAA075540 1 20071105 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 753 S25L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 753, STR 25L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500100 20071115 00100 NM 2007 11 15 SWAA075539 1 20071105 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 761 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 761, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500101 20071115 00101 NM 2007 11 15 SWAA075541 1 20071105 A 5330 6545777 SKIN BOEING 737 7373H4 1384600 NM BS 957 S27L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 957, STR 27L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007111500102 20071115 00102 NM 2007 11 15 SWAA075545 1 20071105 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM BS 380 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500103 20071115 00103 NM 2007 11 15 SWAA075546 1 20071105 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8L/R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500104 20071115 00104 NM 2007 11 15 SWAA075544 1 20071105 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8L/R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500106 20071115 00106 NM 2007 11 15 SWAA075556 1 20071105 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM BS 360 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500107 20071115 00107 NM 2007 11 15 SWAA075547 1 20071105 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500109 20071115 00109 NM 2007 11 15 SWAA075548 1 20071105 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM BS 747 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500113 20071115 00113 NM 2007 11 15 SWAA075552 1 20071105 A 5311 65C25230 FRAME BOEING 737 7373A4 1384585 NM BS 727E S8L/R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500114 20071115 00114 2007 11 15 SWAA075557 4 20071105 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007111500115 20071115 00115 NM 2007 11 15 SWAA075554 1 20071105 A 5754 SKIN BOEING 737 7377H4 1384404 NM NR 6 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 700GS 27835 DURING SCHEDULED 10Y CHECK, FOUND RIGHT WING NR 6 L/E SLAT T/E DELAMINATED AT INBOARD END. REMOVED AND REPLACED SLAT PE R MM. 2 L 7 2 4F RT A16WE 2007111500117 20071115 00117 NM 2007 11 15 SWAA075553 1 20071105 A 5754 SKIN BOEING 737 7377H4 1384404 NM NR 7 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 700GS 27835 DURING SCHEDULED 10Y CHECK, FOUND RT WING NR 7 L/E SLAT T/E DELAMINATED AT INBOARD END. REMOVED AND REPLACED SLAT PER M M. 2 L 7 2 4F RT A16WE 2007111500118 20071115 00118 NM 2007 11 15 SWAA075558 1 20071105 A 5320 6541852 ANGLE BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 756SA 27872 DURING SCHEDULED 8Y CHECK, FOUND ZEE ANGLE CORRODED AT R2 DOOR CUTOUT. REMOVED AND REPLACED ZEE ANGLE PER SRM. 2 L 7 2 4F RT A16WE 2007111500119 20071115 00119 SO 2007 11 15 C2XA07TY064 1 20071106 A 5751 14569009410 BUSHING EMB 145 EMB145XR 3260214 SO RT AILERON LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16112 145660 RIGHT AILERON BRACKET, O/B AND I/B BUSHING IS LOOSE. REMOVED AND REPLACED PCA BRACKET IAW EC 5750-01177, EMB 135/145 CP M 51-21-04 AND EMB 145XR SRM 51-40-02. 2 L 7 2 4F RT 2007111500121 20071115 00121 NM 2007 11 15 CALA0700649 1 20071105 A 5320 6545807U31 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 290 S10R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL ANGLE AT STA 290 BELOW S10R FORWARD OF R-1 DOOR. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007111500122 20071115 00122 NM 2007 11 15 CALA0700650 1 20071105 A 5313 BAC1498156 STRINGER BOEING 737 7373T0 1384582 NM BS 360 S25L CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND STRINGER 25L CORRODED AT STA 360. A REPAIR STRINGER SPLICE WAS INSTALLED IAW SRM 53-00-03, FIGURE 201. 2 L 7 2 4F RT A16WE 2007111500123 20071115 00123 NM 2007 11 15 CALA0700651 1 20071101 A 5320 65458078 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 280 S14R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL AT STA 280, S14R FORWARD OF R-1 DOOR. THE INTERCOSTAL WAS REMOVED AND RE PLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007111500124 20071115 00124 NM 2007 11 15 CALA0700652 1 20071106 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM BS 380 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 52616 27329 INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 380 BETWEEN STRINGERS 8R AND 9R. THE CRACKED AREA WAS CUT OUT AND REPAI R DOUBLERS WERE INSTALLED IAW ECRA 5310-04672. 2 L 7 2 4F RT A16WE 2007111500125 20071115 00125 NM 2007 11 15 CALA0700653 1 20071106 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM BS 400 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 52616 27329 INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 400 BETWEEN STRINGERS 8L AND 9L. REPAIR ANGLES WERE INSTALLED IAW ECR A 5310-04672. 2 L 7 2 4F RT A16WE 2007111500126 20071115 00126 NM 2007 11 15 CALA0700654 1 20071106 A 5311 FRAME BOEING 737 737524 1384721 NM BS 520 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 52616 27329 INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 520 BETWEEN STRINGERS 8R AND 9R. THE CRACKED AREA WAS CUT OUT AND REPAI R DOUBLERS WERE INSTALLED IAW ECRA 5310-04672. 2 L 7 2 4F RT A16WE 2007111500127 20071115 00127 NM 2007 11 15 CALA0700655 1 20071106 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM BS 440 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 52616 27329 INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 440 BETWEEN STRINGERS 8L AND 9L. THE CRACKED AREA WAS CUT OUT AND REP AIR DOUBLERS WERE INSTALLED IAW ECRA 5310-04672. 2 L 7 2 4F RT A16WE 2007111500129 20071115 00129 NM 2007 11 15 CALA0700657 1 20071107 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM BS 400 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 52616 27329 INSPECTION FOUND A 0.2 INCH CRACK IN FRAME AT STA 400 BETWEEN STRINGERS 8R AND 9R. THE CRACKED AREA WAS CUT OUT AND A R EPAIR DOUBLER WAS INSTALLED IAW ECRA 5310-04672. 2 L 7 2 4F RT A16WE 2007111500130 20071115 00130 NM 2007 11 15 CALA0700658 1 20071018 A 5330 141T3840100 SKIN BOEING 767 767224 1385170 NM BS 142-157 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76153 30432 THE AIRCRAFT SUSTAINED LIGHTNING STRIKE FUSELAGE SKIN DAMAGE AT STA 157, WL 235 AND AT STA 142, WL 226. THE DAMAGE AT S TA 142 WAS REPAIRED IAW ECRA 5330-03743. THE DAMAGE AT STA 157 WAS REPAIRED IAW ECRA 5330-03739. 2 L 7 2 4F RT A1NM 2007111500131 20071115 00131 NM 2007 11 15 CALA0700659 1 20071017 A 5330 UNK SKIN BOEING 767 767224 1385170 NM BS 256.25 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76153 30432 INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO THE RIGHT FUSELAGE SKIN AT STA 256.25, STRINGER 13R. THE DAMAGE WAS REPAIRE D IAW ECRA 5330-03742. 2 L 7 2 4F RT A1NM 2007111500132 20071115 00132 NM 2007 11 15 CALA0700660 1 20071024 A 5330 654577572 SKIN BOEING 737 7373T0 1384582 NM BS 727D S23R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 A WALKAROUND INSPECTION FOUND A CRACK IN THE FUSELAGE SKIN AT STA 727D, S23R. THE SKIN WAS REPAIRED IAW ECRA 5330-03745 . 2 L 7 2 4F RT A16WE 2007111500133 20071115 00133 EU 2007 11 15 YENA2007094 1 20071104 A 7997 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE OIL PRESS IND CHAFED A YENA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 15 584JB 2149 11609 FLT 759, BOS-SJU, AT CRUISE GOT ECAM ENG NR 2 OIL LOW PRESSURE. ENG PAGE PSI SHOWED XX, THEN FLASHED NORMAL THEN FLASHE D "0" PSI. PERFORMED QRH PROCEDURE SHUT NR 2 ENG DOWN AND DIVERTED TO CLOSEST SUITABLE AIRPORT. ENG RUN CARRIED OUT OI L PX CHECKS NORMAL, DUE TO PREVIOUS HISTORY R & R NR 1 & NR 2 SDAC PER MM 31-55-34-04. R & R NR 2 EIU PRECAUTIONARY. F OUND NR 2 ENG OIL PRESS WIRE CHAFED AT TM824 (WIRE 8P082W20) PIN A. REPAIRED WIRE 8P082W20 PER ESPM 20-53-21. A/C OK F OR SERVICE. PROVIDED SECONDARY INSULATION AS REQUIRED, OIL PRESS SYS OPS CHECK GOOD. CONFIDENCE/ASSURANCE FLT ACCOMPLI SHED BY FLIGHT CREW, NO FAULTS NOTED WITH NR 2 ENGINE OIL PRESSURE INDICATION. 2 L 7 2 4F 4 F RT A28NM E40NE 2007111500135 20071115 00135 NM 2007 11 15 ASAA0792200 1 20071102 A 5347 143A7501116 CARGO TRACK BOEING 737 737990 NM BS 494 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 307AS 30015 FWD CARGO PIT LEFT TIE DOWN TRACK BS 494 LBL 17.4 DAMAGED. TRACK REPLACED. 2 L 7 4 4F RT A16WE 2007111500136 20071115 00136 NM 2007 11 15 ASAA0792201 1 20071101 A 5320 146A81271 WEB BOEING 737 737990 NM BS 767-787 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 307AS 30015 AFT CARGO PIT RBL 21 FLOOR WEB CORROSION FOUND AT TOP AND BOTTOM SURFACES AROUND NUT PLATE HOLES FROM BS 767 TO 787. RE PLACED WITH MADE REPAIR PART IAW B737 900 SRM. 2 L 7 4 4F RT A16WE 2007111500138 20071115 00138 NM 2007 11 15 ASAA0792204 1 20071030 A 5320 ANGLE BOEING 737 737990 NM BS 500G-500L CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 307AS 30015 LEFT ZEE ANGLE BETWEEN STA 500G+16 AND 500L HAS CORROSION FWD CARGO PIT. LEFT ZEE ANGLE BETWEEN STA 500G+16 AND 500L WA S REPAIRED AND REPLACED IAW B737 900 SRM 53-00-53, 51-40-05 AND 51-40-02. 2 L 7 4 4F RT A16WE 2007111500139 20071115 00139 NM 2007 11 15 ASAA0792206 1 20071102 A 5315 143A948535 FLOORBEAM BOEING 737 737990 NM BS 500L CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 307AS 30015 FWD CARGO PIT FLOOR SUPPORT ASSY AT BS 500L RBL 25 TO LBL 25 FOUND CORRODED. FWD CARGO PIT FLOOR SUPPORT ASSY AT BS 500 L RBL 25 TO LBL 25 REPLACED WITH NEW PART. 2 L 7 4 4F RT A16WE 2007111500140 20071115 00140 NM 2007 11 15 ASAA0792203 1 20071029 A 5753 113A370012 SKIN BOEING 737 737990 NM RT WING TE FLAPS CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 307AS 30015 RIGHT WING O/B AFT FLAP LOWER SURFACE T/E WEDGE HAS CHAFING AT 23.5 INCHES FROM I/BOARD EDGE AND 11.0 INCHES FROM THE T/ E. RIGHT WING O/B AFT FLAP LOWER SURFACE T/E WEDGE CHAFING AT 23.5 INCHES FROM I/B EDGE AND 11.0 INCHES FROM THE T/E RE PAIRED IAW B737 900 SRM CH 51-70-10 REPAIR 4. 2 L 7 4 4F RT A16WE 2007111500141 20071115 00141 NM 2007 11 15 ASAA0792205 1 20071029 A 5753 STRUCTURE BOEING 737 737990 NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 307AS 30015 LEFT INBOARD AFT FLAP HAS SMALL DENT. DAMAGE FOUND TO BE PUNCTURE LOCATED 12 INCHES FROM INBOARD EDGE. LEFT INBOARD AF T FLAP DAMAGE REPAIRED IAW B737 900 SRM CH 51-70-10 REPAIR 2, LOCATED 12 INCHES FROM INBOARD EDGE. 2 L 7 4 4F RT A16WE 2007111500142 20071115 00142 NM 2007 11 15 ASAA0792207 1 20071103 A 5420 RUB STRIP BOEING 737 737990 NM NR 2 NACELLE WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 307AS 30015 NR 2 ENG INBOARD FAN COWL UPPER RUB STRIP WORN. NR 2 ENG INBOARD FAN COWL UPPER RUB STRIP REPLACED AND AREA REPAIRED IA W B737 900 SRM 54-20-01 FIG 202 REPAIR 7. 2 L 7 4 4F RT A16WE 2007111500143 20071115 00143 NM 2007 11 15 ASAA0752208 1 20071104 A 2844 PRESSURE SWITCH BOEING 737 737890 1384527 NM CENTER FUEL TANK FAULTY A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 558AS 35177 RIGHT CENTER TANK FUEL PUMP LOW PRESSURE LIGHT DID NOT ILLUMINATE MOMENTARILY WHEN PUMP SWITCHED ON. REPLACED LOW PRESS URE RIGHT CENTER FUEL SWITCH. SIGNIFICANT SYSTEM VERIFICATION SUCCESSFUL. 2 L 7 2 4F RT A16WE 2007111500144 20071115 00144 NE 2007 11 15 ASAA0752209 2 20071106 A 7200 ENGINE BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE NR 2 OIL CONSUMPTION A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 577AS 35186 NR 2 ENGINE OIL CONSUMPTION 0.71QPH, OUT OF ETOPS LIMITS. INSPECTED INLET & EXHAUST RAN NR 2 ENGINE. NO LEAKS NOTED AT THIS TIME. AIRCRAFT RESTRICTED FROM ETOPS UNTIL NEW CONSUMPTION RATE IS CALCULATED. SERVICED ENGINE TO FULL WITH 0.5Q TS. CALCULATED TO .15QPH. ETOPS STATUS RESTORED. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007111500146 20071115 00146 EA 2007 11 15 VNAA0710019 1 20071029 A 5297 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR DAMAGED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 05 262PS 7962 CREW REPORTED A PASSENGER DOOR TRIPLE CHIME RED WARNING AT 10,000 FEET AND CAS REPEATED MULTIPLE TIMES. CREW ALSO REPOR TED HEARING A THUMP AT THE MAIN CABIN DOOR. CREW ELECTED TO DIVERT TO JAX AND LANDED WITHOUT INCIDENT. MAINTENANCE REM OVED AND REPLACED THE PASSENGER DOOR WIRING HARNESS. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007111500147 20071115 00147 EU 2007 11 15 YENA2007095 1 20071106 A 2700 3945128102 CONTROLLER AIRBUS 320 A320232 3930326 EU ELAC MALFUNCTIONED A YENA O OTHER F FLT CONT AFFECTED DE DESCENT 1 EA 15 562JB 19782 1948 FLT 433, BOS-MCO, ON A/P OFF DESCENT FROM 7000FT TO 2000FT FLAPS 1 SPEED 190 KT5.TO HOLD LEVEL FLIGHT LEFT AILERON WAS D ISPLACED 1/3 DN. RT 1/3 UP. NR 1, 2, 3 & 4 FOR FLIGHT CONTROL CKS PERFORMED WITH NO FAULTS NOTED. PER MCC REQUEST REMO VED AND REPLACED ELAC # IAW AMM 27-93-34-000-001, OPS TEST NORMAL. 2 L 7 2 4F RT A28NM 2007111500148 20071115 00148 NM 2007 11 15 SWAA075579 1 20071106 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM BS 380 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500155 20071115 00155 NM 2007 11 15 SWAA075575 1 20071106 A 5313 6519603 STRINGER BOEING 737 7375H4 138449D NM BS 908 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED 16Y CHECK, FOUND STRINGER 4L CRACKED AT BS 908. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007111500158 20071115 00158 NM 2007 11 15 SWAA075569 1 20071106 A 5743 115A5211 TRUNNION BOEING 737 7377H4 1384404 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 717SA 27851 DURING SCHEDULED MV3 CHECK, FOUND RT MLG FWD TRUNNION FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500159 20071115 00159 NM 2007 11 15 SWAA075570 1 20071106 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 729SW 27861 L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007111500160 20071115 00160 EU 2007 11 15 SA07072 1 20071104 A 2150 A/C PACK AIRBUS A319 A319112 3930323 EU CONTAMINATED A USAA G O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 768US 1389 PLS FLT 833 EN-ROUTE CLT TO PLS. DURING APPROACH INTO PLS, CABIN CREW NOTICED FUMES COMING FROM THE AFT CABIN. COCKP IT CREW NOTICED FUMES SHORTLY AFTERWARDS. CREW FOLLOWED PROCEDURES AND DONNED O2 MASKS. FLIGHT LANDED IN PLS WITHOUT F URTHER INCIDENT. MAINTENANCE CARRIED OUT DETAILED INSPECTIONS OF THE ENGINES, LANDING GEAR, HYDRAULIC SYSTEMS, APU AND AIR CONDITIONING PACKS. ALL CHECKS OK. 2 L 7 2 4F RT A28NM 2007111500161 20071115 00161 EU 2007 11 15 SA07073 1 20071105 A 2120 UNKNOWN AIRBUS A319 A319112 3930323 EU CABIN ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 744P 1287 DCA FLT 2022 EN-ROUTE DCA TO BOS. AFTER TAKEOFF, CREW NOTICED A STRONG, SULFUR LIKE ODOR IN THE COCKPIT AND CABIN. TH E FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING (OPEN). 2 L 7 2 4F RT A28NM 2007111500163 20071115 00163 SO 2007 11 15 C2XA07CL095 1 20071107 A 3231 22250100003 SOLENOID VALVE EMB 145 EMB145LR 3260212 SO NLG DOORS FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14959 13062 145091 CLE FLIGHT 3023 - THE CREW REPORTED A LOUD NOISE AND VIBRATION FROM THE NOSE WHEEL COMPARTMENT. AIRCRAFT RETURNED TO CL E AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR DOORS WOULD NOT RETRACT. THE NOSE LANDING GEAR SOLENOID VALVE WAS REPLACED. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007111500164 20071115 00164 EU 2007 11 15 YENA2007096 1 20071107 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU CABIN ODOR A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 535JB 1739 FLT 718, SJU-JFK, BETWEEN 20:00 TO 23:00 Z, CUSTOMER COMPLAINED INFLIGHT, CONFIRMED ODOR BURNING, FROM ROW 10 FORWARD, L IVE TV WAS DEACTIVATED AND ODOR DISSIPATED. PERFORMED TSM 23-39-00-810-801, TASK 4.C, REPORT OF ELECTRICAL ODOR THROUGH OUT CABIN ALSO INSPECTED ALL LIVE TV COMPONENTS AND CABLES FROM ROW 12 TO ROW 1 ABC AND DEF, NO DEFECTS NOTED INSPECTION LIMITED TO CABIN ONLY NOT BEHIND SIDEWALLS. PERFORMED TSM TASK 24-00-00-810-823. NO ABNORMALITIES FOUND IN CABIN OR G ALLEYS. NO ODOR EVIDENT THROUGHOUT CABIN. OK TO CONTINUE. 2 L 7 2 4F RT A28NM 2007111500165 20071115 00165 WP 2007 11 15 ABXA070364 1 20071105 A 2120 UNKNOWN DOUG DC9 DC941 302207N WP COCKPIT SMOKE A ABXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 955AX 47619 AIRCRAFT HAD FUMES/SMOKE IN COCKPIT. GROUND RAN APU A/C PACKS, NR 1 & 2 ENGINES, POWERED UP COCKPIT ELECTRICAL SYSTEMS, NO FUMES OR SMOKE NOTICED. INSPECTED TAIL COMPARTMENT, BAG BINS, E & E COMPARTMENT AND NOSE COMPARTMENT. NO EVIDENCE OF OVERHEATING NOTED. 2 L 7 2 4F A6WE 2007111500167 20071115 00167 NM 2007 11 15 ABXA070366 1 20071107 A 3350 HOLDER BOEING 767 767232 1385132 NM EMERGENCY LIGHTS INOPERATIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 739AX 22216 MAIN ENTRY DOOR SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED MAIN ENTRY DOOR SLIDE EMERGENCY LAMP HOLDER IAW B767 MM 33- 51-06. 2 L 7 2 4F RT A1NM 2007111500170 20071115 00170 EA 2007 11 15 COMA0760622 1 20071103 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 821CA 18480 7420 FLIGHT 5315 - RECEIVED FLAPS DEGRADED MESSAGE AND FLAP FAIL MESSAGE. DECLARED EMERGENCY, RAN QRH, LANDED WITHOUT INCIDE NT. REPLACED PDU, RIGGED BPSU'S, PERFORMED EO 27-046AD. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007111500171 20071115 00171 EA 2007 11 15 COMA0760623 1 20071104 A 5610 NP1393219 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA O OTHER O OTHER CR CRUISE 1 SO 01 591SW 29202 7079 FLIGHT 4991 - CAPTAIN'S WINDSHIELD CRACKED IN FLIGHT. CONTINUED FLIGHT. LANDED LGA WITHOUT INCIDENT. REPLACED CAPTAIN 'S WINDSHIELD. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007111500172 20071115 00172 NM 2007 11 15 ASAA0752210 1 20071107 A 4990 38809381 FILTER ELEMENT BOEING 737 737890 1384527 NM APU CLOGGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 570AS 35185 WHILE COMPLETING TASK CARD 78349013 APU OIL FILTER DELTA P INDICATOR INSPECTION FOUND FILTER INDICATOR EXTENDED. REPLAC ED APU FILTER ELEMENT IAW 49-91-13 & 78349013. 2 L 7 2 4F RT A16WE 2007111300160 20071113 00160 EU 2007 11 13 MALA070171 1 20071023 A 5220 SKIN SAAB SF340 340B 7860101 EU EMERGENCY EXIT DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 EMERGENCY EXIT AT RT EMERGENCY EXIT 7" FROM AFT EDGE OF DOOR AND 9 1/2" FROM TOP OF DOOR, 0600-814-01E, RT MAIN EXIT DOO R OUTER SKIN DENTED 7" FROM FWD EDGE IS 1' W BY 2" L BY .008" DEEP. EVALUATED DENT AND FOUND TO BE DISBONDED. REPAIRED DAMAGE IAW SF3 EO NR S52028 AND SAAB SRM 52-10-10 PAR 1. 2 L 7 2 4T RT A52EU 2007111300161 20071113 00161 EA 2007 11 13 TRAX200701680 1 20071103 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 880AS 7606 FOUND CABIN EMERGENCY FLOOR LIGHTS INOP AT ROWS 6CD THRU 8CD. 2 L 7 2 4F RT A21EA 2007111300162 20071113 00162 EA 2007 11 13 TRAX200701681 1 20071103 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 828AS 7213 FLT 4666 - GEAR DISAGREE WARNING MSG "BOTH MAIN GEARS UP" FOLLOWED QRH, MANUALLY DEPLOYED MAIN GEARS, EMERGENCY DECLARED . LANDING GEAR RETRACTION SYSTEM. 2 L 7 2 4F RT A21EA 2007111300163 20071113 00163 EU 2007 11 13 MALA070168 1 20071023 A 5230 SKIN SAAB SF340 340B 7860101 EU CARGO DOOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 DENT IN CARGO DOOR SKIN AT STA 681.1 ABOVE UPPER EDGE OF SEAL AT BOTTOM OF DOOR. GENERIC REPAIR PER IAW EO NR S52028 AT STA 681.1. 2 L 7 2 4T RT A52EU 2007111300164 20071113 00164 EU 2007 11 13 MALA070169 1 20071023 A 5230 SKIN SAAB SF340 340B 7860101 EU CARGO DOOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 DENT IN CARGO DOOR SKIN AT STA 675.1, 3 1/2" ABOVE THE DOOR SEAL AT BOTTOM EDGE OF DOOR. GENERIC REPAIR PER IAW EO NR S 52028 AT STA 675.1. 2 L 7 2 4T RT A52EU 2007111300165 20071113 00165 NM 2007 11 13 NWAA073716309 1 20071106 A 3397 WIRE BOEING 747 747451 1384940 NM EMERGENCY LIGHTS BROKEN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 DURING OVERNIGHT CHECK, FOUND E ZONE RIGHT SIDE EMERGENCY FLOOR PATH LIGHTS INOP. MAINTENANCE REPAIRED BROKEN WIRE. OP ERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007111400011 20071114 00011 NM 2007 11 14 07FDEA04731 1 20071107 A 5754 SLAT TRACK DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 591FE 48527 RIGHT WING SLAT TRACK NR 14 CUTOUT LOWER CORNER FOUND CRACKED. CUT-OUT LOWER CORNER CRACKED AREA CRACKED TRIMMED OUT AN D REPAIR AS PER SRM 57-10-00 VOLUME I, FIGURE 21. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007111400033 20071114 00033 NM 2007 11 14 DL76L071407 1 20071104 A 5420 311T31571 ANGLE BOEING 767 767332 1382001 NM NACELLE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 175DN 24803 CRACKED CLOSEOUT ANGLE FOUND DURING AD 2005-19-23 INSPECTIONS. INSPECTED AND REPLACED ANGLE PER B/P. 2 L 7 2 4F RT A1NM 2007111400038 20071114 00038 NM 2007 11 14 DLM88071412 1 20071106 A 5330 59670632 SKIN DOUG MD88 MD88 3023688 NM BS 1437 S2-5R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 DURING HMV AT GDL, SKIN CRACKS WERE FOUND AT STA 1437 BETWEEN S-2R AND S-5R. THE CRACKS WERE REMOVED AND REPAIRED PER E R/A 464563-14. 2 L 7 2 4F RT A6WE 2007111400041 20071114 00041 NE 2007 11 14 DL76L071416 2 20071106 A 7261 LINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE ENGINE OIL SYS LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 176DN 63068 25061 724638 NR 1 ENG LOOSING OIL QTY STEADY DROP DIVERTING TO LGW FOR REPAIRS. OPENED LT ENG FOUND OIL RETURN LINE LEAKING AT TUBE ASSY SCAVENGE PUMP TO OIL FILTER P/N 59T347 IPC 79-21-05-05 ITEM 36 543778. REPLACED TUBE ASSY RETURNED A/C TO NML, PER F ENG RUN/LEAK CHECK ALL OPS/IND NML. A/C OK FOR SVC. 2 L 7 2 4F 4 F RT A1NM E24NE 2007111400056 20071114 00056 NM 2007 11 14 QXEA200701705 1 20071107 A 2930 ACCUMULATOR BOMBDR DHC8 DHC8402 1390042 NM HYD SYSTEM UNDERSERVICED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 419QX 4145 RNO FLIGHT NR 2256: AFTER START, DURING ELEVATOR CHECK, THE ELEVATOR PRESS LIGHT IS EXTINGUISHED INTERMITTENTLY, NR 3 HY D PUMP IS ILLUMINATING MOMENTARILY AND HYD PRESSURE 3 VALUE IS FLUCTUATING FROM 3200 PSI TO 700-800 PSI UNDER LOAD. AIR CRAFT RETURNED TO BLOCK. MAINTENANCE SERVICED THE NR 3 MAIN AND BOOTSTRAP ACCUMULATOR WS IAW D8-400 MM TASKS 12-10-29-6 14-801 AND 12-10-29-614-802. SERVICED THE NR 3 HYD FLUID LEVEL AND BLED THE NR 3 HYD SYSTEM. OPERATED THE SYSTEM NUMER OUS TIMES WITH NO FAULTS NOTED. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007111400058 20071114 00058 SO 2007 11 14 SIMA200731203 1 20071107 A 2710 SWITCH EMB 135 EMB135LR 3260305 SO ROLL TRIM FAILED A SIMA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SW 21 727AE 145326 ROLL TRIM SWITCH FAILED IN FLIGHT. CLEANED TRIM SWITCHES IAW EMB AMM 27-14-0. OPS CHECK GOOD AIRCRAFT RETURNED TO SERV ICE. 2 L 7 2 4F RT T00011AT 2007111400066 20071114 00066 NM 2007 11 14 07FDEA04746 1 20071107 A 5411 SPAR CAP DOUG MD11 MD11F 3023600 NM NR 2 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 591FE 48527 NR 2 PYLON LEFT UPPER SPAR CAP OF THE TAIL PYLON CRACKED. REPAIRED AS PER E.A. 1-5410-117046, REPAIR CLASSIFIED AS M AJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007111400072 20071114 00072 WP 2007 11 14 07FDEA04753 1 20071108 A 5713 ARB0945502 STRINGER DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 FOUND 2" CRACK ON RT WING STRINGER NR 40 AT XORS 346. REPAIR PER SRM 57-20-00 VOL 1 FIG 36 CONF. 2 L 7 3 4F A22WE 2007111400116 20071114 00116 NM 2007 11 14 HALA0700482 1 20071029 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 656 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 CORROSION AROUND SEAT TRACK LBL 11, STATION 656+21 TO STATION 656+32. REPLACE SEAT TRACK AT LBL 11, STATION 656+21 TO S TATION 656+32. 2 L 7 2 4F RT A1NM 2007111400117 20071114 00117 NM 2007 11 14 HALA0700483 1 20071025 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 654 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 CORROSION FOUND AT 3S 654+120 LBL 22. SEAT TRACK SECTION REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007111400118 20071114 00118 NM 2007 11 14 DLM90071432 1 20071107 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FS 342 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 RT CUSP WEB AT FS 342 CRACKED AT LIGHTNING HOLE. REPAIRED RT CUSP FS 342 AT LIGHTNING HOLE IAW MD80 SRMD FIG 827D ON N/ R 2700-0282 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007111400119 20071114 00119 NM 2007 11 14 DL757071433 1 20071108 A 5330 141N333112 SKIN BOEING 757 757232 1384965 NM BS 426-440 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 694DA 29726 FUSELAGE SKIN HAD TWO DENTS/GOUGES BETWEEN STA 426 AND STA 440 AND S-15L TO S-16L. CUTOUT THE DAMAGED SKIN AND INSTALLE D A REPAIR DOUBLER. 2 L 7 2 4F RT A2NM 2007111400139 20071114 00139 NM 2007 11 14 DLM88071461 1 20071001 A 5210 ANGLE DOUG MD88 MD88 3023688 NM R1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 CRACK ON RT FWD SERVICE DOOR R1 AT AFT UPPER CORNER OF BEAM NR 1 ANGLE. REPLACED ANGLE PER DWG 9919579. 2 L 7 2 4F RT A6WE 2007111400140 20071114 00140 NM 2007 11 14 DLM88071463 1 20071015 A 5320 CHANNEL DOUG MD88 MD88 3023688 NM VENTRAL STAIR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 DEFORMED AND CRACKED C CHANNELS ON LT VENTRAL STAIRWAY PANEL. REPLACED CHANNELS PER DWG 5910395. 2 L 7 2 4F RT A6WE 2007111400141 20071114 00141 NM 2007 11 14 DLM88071464 1 20071008 A 5350 STRUCTURE DOUG MD88 MD88 3023688 NM TAIL CONE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 CRACKED LOWER TAIL CONE STRUCTURE. REPAIRED PER SRM 51-90-0D. 2 L 7 2 4F RT A6WE 2007111400142 20071114 00142 NM 2007 11 14 DLM88071465 1 20070828 A 5321 FLOOR PANEL DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 EXFOLIATION CORROSION ON FWD FLOOR PANEL UNDER 61 POTABLE WATER PIPING CONNECTION PANEL. REPAIRED PER SRM 51-70-4. 2 L 7 2 4F RT A6WE 2007111400143 20071114 00143 NM 2007 11 14 DLM88071466 1 20070924 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 522-598 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 EXFOLIATION CORROSION ON LT CUSP WEB FROM STA Y=522 TO 598. REPLACED WEB PER SRM 51-10-3D. 2 L 7 2 4F RT A6WE 2007111400144 20071114 00144 NM 2007 11 14 DLM88071467 1 20071012 A 5320 SUPPORT BRACKET DOUG MD88 MD88 3023688 NM BS 1503 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 CRACKED SUPPORT BRACKET AT FUSELAGE STRUCTURE STA Y=1503 CANT PROJECTION OF LONG 17R. REPLACED BRACKET PER DWG 5930556 . 2 L 7 2 4F RT A6WE 2007111400145 20071114 00145 NM 2007 11 14 DLM88071468 1 20071013 A 5320 BRACKET DOUG MD88 MD88 3023688 NM BS 1463 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 CRACKED BRACKET ON FRAME AT STA Y=1463 CANT AT 10:30 POS. REPLACED BRACKET PER DWG 5920838. 2 L 7 2 4F RT A6WE 2007111400160 20071114 00160 NM 2007 11 14 CALA0700647 1 20071102 A 5311 65C22910 FRAME BOEING 737 7373T0 1384582 NM BS 500D S26-27L CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND FRAME CORRODED AT STA 500D BETWEEN STRINGERS 26L AND 27L. THE FRAME WAS REPAIRED IAW SRM 53-00-07. 2 L 7 2 4F RT A16WE 2007111400161 20071114 00161 NM 2007 11 14 CALA0700648 1 20071102 A 5313 BAC1498158 STRINGER BOEING 737 7373T0 1384582 NM BS 986 S27L CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND HEAVY CORROSION ON STRINGER 27L AT STA 986.5. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 2007111400162 20071114 00162 SO 2007 11 14 C2XA07IA228 1 20071030 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13968 1765 1765 145138 IAH - FLIGHT 2618, DURING PREFLIGHT INSPECTION THE CREW REPORTED THE CENTER AISLE PATH EMERGENCY LIGHTS TO BE INOPERATIV E. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, A ND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007111400163 20071114 00163 SO 2007 11 14 C2XA07IA229 1 20071101 A 7740 2305885401 RESISTOR EMB 145 EMB145LR 3260212 SO LT ENGINE TRIM LOOSE A C2XA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 27 22971 145149 IAH - FLT 2185 - DURING CLIMB THE CREW REPORTED THAT ENGINE 1 WAS SURGING ON TAKEOFF AND LOST 5% ON N1. THE AIRCRAFT RE TURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RE-SECURED THE TRIM RESISTOR IN THE ENGINE 1 -A- HARNESS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007111400164 20071114 00164 NM 2007 11 14 USAA920070989 1 20071025 A 5320 141N517048 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 - FUSEL CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 365.25 - BS 377.7, LBL 61, WL 208. REPLACE D CABIN FLOOR SUPPORT, BS 365.25 - BS 377.7, LBL 61, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007111400165 20071114 00165 NM 2007 11 14 USAA920070990 1 20071024 A 5320 141N51605 CHANNEL BOEING 757 7572B7 1384964 NM ZONE 200 - FUSEL CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR INTERCOSTAL CHANNEL, BS 310.5 - BS 324, BL 0, WL 208. REPLACED CABIN FLOOR INTERCOSTAL CHANNEL, BS 310.5 - BS 324, BL 0, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007111400166 20071114 00166 NM 2007 11 14 USAA920070991 1 20071025 A 5315 141N5160203 FLOORBEAM BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 297, RBL 5 - RBL 16, WL 208. REPLACED CABI N FLOOR SUPPORT, BS 297, RBL 5 - RBL 16, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007111400167 20071114 00167 NM 2007 11 14 USAA920070992 1 20071025 A 5315 141N29321 FLOORBEAM BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOORBEAM UPPER CHORD, BS 324, LBL 10 - RBL 42, WL 208. REPA IRED CABIN FLOORBEAM UPPER CHORD, BS 324, LBL 10 - RBL 42, WL 208 IAW B757 SRM 51-70-12. 2 L 7 2 4F RT A2NM 2007111400168 20071114 00168 NM 2007 11 14 USAA920070993 1 20071025 A 5320 141N842241 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR ANGLE, BS 310.5 - BS 365.20, RBL 65, WL 208. REPLACED CABIN FLOOR ANGLE, BS 310.5 - BS 365.20, RBL 65, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007111400169 20071114 00169 NM 2007 11 14 USAA920070994 1 20071025 A 5320 146N519139 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR ANGLE, BS 1661 - BS 1681, RBL 9.2, WL 208. REPLACED CA BIN FLOOR FLOOR ANGLE, BS 1661 - BS 1681, RBL 9.2, WL 208, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007111400170 20071114 00170 NM 2007 11 14 USAA920071026 1 20071009 A 5320 141N516079 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 324 - BS 345, RBL 58.22, WL 208. REPLACED CABIN FLOOR SUPPORT, BS 324 - BS 345, RBL 58.22, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007111400171 20071114 00171 NM 2007 11 14 USAA920071027 1 20071009 A 5315 141N51703 FLOORBEAM BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 338, LBL 33 - LBL 38, WL 208. REPLACED CAB IN FLOOR SUPPORT, BS 338, LBL 33 - LBL 38, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007111400172 20071114 00172 NM 2007 11 14 USAA920071028 1 20071009 A 5320 141N51911 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 345 - BS 377.7, BL 0, WL 208. REPLACED CAB IN FLOOR SUPPORT, BS 345 - BS 377.7, BL 0, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007111400173 20071114 00173 NM 2007 11 14 USAA920071029 1 20071009 A 5320 141N5170 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 324 - BS 345, LBL 33, WL 208. REPLACED CAB IN FLOOR SUPPORT, BS 324 - BS 345, LBL 33, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007111400174 20071114 00174 NM 2007 11 14 USAA920071030 1 20071009 A 5320 141N516078 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 345 - BS 360.25, RBL 58.22, WL 208. REPLAC ED CABIN FLOOR SUPPORT, BS 345 - BS 360.25, RBL 58.22, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007111400175 20071114 00175 NM 2007 11 14 USAA920071031 1 20071009 A 5320 141N517030 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 324 - BS 345.5, LBL 19.75, WL 208. REPLACE D CABIN FLOOR SUPPORT, BS 324 - BS 345.5, LBL 19.75, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007111400176 20071114 00176 NM 2007 11 14 USAA920071032 1 20071009 A 5320 141N516139 SUPPORT FITTING BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON GALLEY SUPPORT FITTING, BS 324 - BS 345, RBL 1.0, WL 208. REPLACED GALLEY SUPPORT FITTING, BS 324 - BS 345, RBL 1.0, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007111400177 20071114 00177 NM 2007 11 14 USAA920071033 1 20071009 A 5315 141N5810 FLOORBEAM BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON FLOORBEAM, BS 310.5, LBL 19 - RBL 42, WL 208. REPAIRED FLOORBEAM, BS 310.5, LBL 19 - RBL 42, WL 208 IAW B757 SRM 51-70-12. 2 L 7 2 4F RT A2NM 2007111400178 20071114 00178 NM 2007 11 14 USAA920071040 1 20071009 A 5320 141N516152 FITTING BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON FITTING, BS 365.25 - BS 377.7, RBL 15.0, WL 208. REPLACED FITTING, BS 365.25 - BS 377.7, RBL 15.0, WL 208 IAW B757 SRM 51-10-02, 51-40-05 AND 51-40-02. 2 L 7 2 4F RT A2NM 2007111400179 20071114 00179 NM 2007 11 14 USAA920071041 1 20071009 A 5315 141N5113 FLOORBEAM BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOORBEAM, BS 377.7, LBL 48.0, WL 208. REPAIRED CABIN FLOORB EAM, BS 377.7, LBL 48.0, WL 208 IAW USAIRWAYS TYPICAL REPAIR 53-15-01 AND EA 98947. 2 L 7 2 4F RT A2NM 2007111400180 20071114 00180 NM 2007 11 14 USAA920071042 1 20071009 A 5315 141N5112 FLOORBEAM BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOORBEAM, BS 365.25, RBL 10 - RBL 65, WL 208. REPAIRED CABI N FLOORBEAM, BS 365.25, RBL 10 - RBL 65, WL 208 IAW USAIRWAYS TYPICAL REPAIR 53-15-01 AND EA 98947. 2 L 7 2 4F RT A2NM 2007111400181 20071114 00181 NM 2007 11 14 USAA920071054 1 20071009 A 5320 141N516627 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 377.7 - BS 395, RBL 58.22, WL 208. REPLACE D CABIN FLOOR SUPPORT, BS 377.7 - BS 395, RBL 58.22, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007111400182 20071114 00182 NM 2007 11 14 USAA920071055 1 20071009 A 5320 141N516046 CHANNEL BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR STRUCTURE CHANNEL, BS 310 - BS 324, RBL 42, WL 208. RE PLACED CABIN FLOOR STRUCTURE CHANNEL, BS 310 - BS 324, RBL 42, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007111400183 20071114 00183 NM 2007 11 14 USAA920071069 1 20071009 A 5320 141N516512 INTERCOSTAL BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 206UW 27808 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL UPPER TEE FITTING, BS 297, RBL 20, WL 208. REPLACED IN TERCOSTAL UPPER TEE FITTING, BS 297, RBL 20, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007111400184 20071114 00184 NM 2007 11 14 USAA920071070 1 20071104 A 5330 6545774 SKIN BOEING 737 7374B7 1384702 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 457UW 25021 CLT - MAJOR REPAIR - LOG PAGE 4243052, FUSELAGE SKIN CRACKED, BS 727E, S20L. REPAIRED FUSELAGE SKIN, BS 727E, S20L IAW USAIRWAYS EA 98996. 2 L 7 2 4F RT A16WE 2007111400185 20071114 00185 EU 2007 11 14 USAA920071071 1 20071014 A 5321 D53610600500000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - CORROSION ON L1 DOOR ENTRYWAY FLOOR PANEL 221FF, BS 709 / FR 16 - BS 808 / FR 20. REPL ACED L1 DOOR ENTRYWAY FLOOR PANEL 221FF, BS 709 / FR 16 - BS 808 / FR 20 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007111500002 20071115 00002 EU 2007 11 15 USAA920071074 1 20071028 A 5320 D53475765206 SILL AIRBUS 320 A320232 3930326 EU ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - CORROSION ON BULK CARGO DOOR CUTOUT LOWER SILL, BS 2830 / FR 60, -Y680. REPAIRED BULK CARGO DOOR CUTOUT LOWER SILL, BS 2830 / FR 60, -Y680 IAW A320 SRM 53-41-49. 2 L 7 2 4F RT A28NM 2007111500008 20071115 00008 NM 2007 11 15 USAA920071080 1 20071028 A 5340 69489852 ATTACH ANGLE BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C-20 CHECK - CRACKED INTERCOSTAL ATTACH CLIP, BS 360, S18L. REPLACED INTERCOSTAL ATTACH CLIP, BS 3 60, S18L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007111500011 20071115 00011 NM 2007 11 15 USAA920071083 1 20071031 A 5320 66142081 INTERCOSTAL BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED INTERCOSTAL WEB, BS 292.5, S11L. REPLACED INTERCOSTAL WEB, BS 292.5, S11L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007111500023 20071115 00023 NM 2007 11 15 SWAA075527 1 20071104 A 5312 6545819 PRESSURE PANEL BOEING 737 7373H4 1384600 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND NLG W/W UPPER CEILING PANEL CRACKED AT LBL 7.75. REPAIRED PANEL PER ACO. 2 L 7 2 4F RT A16WE 2007111500027 20071115 00027 NM 2007 11 15 SWAA075531 1 20071104 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007111500028 20071115 00028 NM 2007 11 15 SWAA075532 1 20071104 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 440 S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 7L CRACKED AT BS 440. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007111500040 20071115 00040 2007 11 15 SWAA075504 4 20071101 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 433LV 33716 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007111500049 20071115 00049 NM 2007 11 15 SWAA075508 1 20071102 A 5753 SKIN BOEING 737 7373H4 1384600 NM FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED BRDG CHECK, FOUND LT WING INBOARD FOREFLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007111500056 20071115 00056 SO 2007 11 15 C2XA07ON025 1 20071102 A 2530 500064001 COFFEEMAKER EMB 145 EMB145XR 3260214 SO GALLEY SMOKE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 11194 9190 14500940 FLT 216 - SAT TO SMF - CREW REPORTED RIGHT COFFEE POT WAS SMOKING A/C WAS RELEASED ON MEL 25-60-02/03 CAT D CONTROL 1322 21. A/C ARRIVED TO ONT FOR SVC/RTN CHECKS AND OVERNIGHT INSPECTION. MX BREWED COFFEE SEVERAL TIMES AND NO SMOKE WAS NO TED AT ANY TIME, OPERATIONALLY CHECKED SATISFACTORY AND A/C WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2007111500063 20071115 00063 EA 2007 11 15 COMA0760609 1 20071022 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA MACH/STAB TRIM FAULTY A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 818CA 583 7408 FLIGHT 5384 - RECEIVED AUTOPILOT PITCH MESSAGE. STAB AND MACH TRIM DISCONNECT WHEN TRIMMING NOSE DOWN. DECLARED EMERGE NCY, LANDED WITHOUT INCIDENT. REPLACED STAB ACTUATOR. 2 L 7 2 4F RT A21EA 2007111500072 20071115 00072 EU 2007 11 15 2007UALA04522 1 20071101 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 440UA 702 EEL LIGHTS INOP AT ROWS 21, 22 & 23. FOUND BROKEN WIRE UNDER ROW 22, SPLICED WIRE AND OPS CHECK GOOD ALL ROWS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007111500075 20071115 00075 EA 2007 11 15 COMA0760614 1 20071025 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS FAULTY A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 588SW 17021 7069 FLIGHT 5103 - EMERGENCY LIGHTS AT MAIN CABIN DOOR AND SERVICE DOOR INOP. REPLACED EMERGENCY LIGHT BATTERY PACK. NO FUR THER DEFECTS. 2 L 7 2 4F RT A21EA 2007111500077 20071115 00077 EA 2007 11 15 COMA0760616 1 20071025 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS FAULTY A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 588SW 31104 7069 FLIGHT 5103 - EMERGENCY LIGHTS AT MAIN CABIN DOOR AND SERVICE DOOR INOP. REPLACED EMERGENCY LIGHT BATTERY PACK. NO FUR THER DEFECTS. 2 L 7 2 4F RT A21EA 2007111500079 20071115 00079 EA 2007 11 15 COMA0760618 1 20071028 A 2910 601R7528639 LINE CNDAIR CL600 CL6002B19 1900309 EA LEFT NACELLE LEAKING A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 735CA 7267 FLIGHT 5349 - HYD SYSTEM NR 1 FAILED. DECLARED EMERGENCY, RETURNED TO ACY AND LANDED WITHOUT INCIDENT. REPLACED CHAFED AND LEAKING NR 1 EDP RETURN LINE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007111500080 20071115 00080 EA 2007 11 15 COMA0760619 1 20071029 A 5610 NP1393219 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 447CA 15131 7552 FLIGHT 5129 - PILOT SIDE WINDOW ARCED AND THEN CRACKED. DECLARED EMERGENCY, DIVERTED TO SYR, LANDED WITHOUT INCIDENT. REPLACED PILOT SIDE WINDOW. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007111500096 20071115 00096 NM 2007 11 15 SWAA075559 1 20071105 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 380 S6L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007111500116 20071115 00116 NM 2007 11 15 SWAA075555 1 20071105 A 5754 SKIN BOEING 737 7377H4 1384404 NM NR 5 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 700GS 27835 DURING SCHEDULED 10Y CHECK, FOUND RIGHT WING NR 5 L/E SLAT T/E DELAMINATED AT INBOARD END. REMOVED AND REPLACED SLAT PE R MM. 2 L 7 2 4F RT A16WE 2007111500149 20071115 00149 NM 2007 11 15 SWAA075578 1 20071106 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM BS 380 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500150 20071115 00150 NM 2007 11 15 SWAA075577 1 20071106 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 616 S5L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007111500152 20071115 00152 NM 2007 11 15 SWAA075571 1 20071106 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM BS 520 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500153 20071115 00153 NM 2007 11 15 SWAA075572 1 20071106 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 411WN 29821 DURING SCHEDULED 6Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 180. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007111500156 20071115 00156 NM 2007 11 15 SWAA075574 1 20071106 A 5310 6519603 CREASE BEAM BOEING 737 7375H4 138449D NM BS 320-338 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 320 AND BS 338, LBL 70. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2007111500166 20071115 00166 WP 2007 11 15 ABXA070365 1 20071105 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC933F 302207A WP EMERGENCY LIGHTS DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 EMERGENCY LIGHTS WILL ARM BUT WOULD NOT ILLUMINATE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY IAW DC9 MM 33-53-00-8 . 2 L 7 2 4F A6WE 2007111500173 20071115 00173 EA 2007 11 15 COMA0760624 1 20071105 A 2110 350023000 CHECK VALVE CNDAIR CL600 CL6002B19 1900309 EA RAM AIR BROKEN A COMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 920CA 19905 7022 FLIGHT 5479 - CABIN SMOKE OCCURRED AFTER TRANSFERRING BLEED TO APU ON GROUND. TAXIED TO GATE WITHOUT INCIDENT. REPLACE D RIGHT RAM AIR CHECK VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007111500174 20071115 00174 EA 2007 11 15 COMA0760625 1 20071105 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA RIGHT SMOKE A COMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 920CA 16450 7022 FLIGHT 5479 - CABIN SMOKE OCCURRED AFTER TRANSFERRING BLEED TO APU ON GROUND. TAXIED TO GATE WITHOUT INCIDENT. REPLACE D RIGHT ACM. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007111500175 20071115 00175 EA 2007 11 15 COMA0760626 1 20071105 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA CABIN AIR ODOR A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 796CA 7338 FLIGHT 5188 - AFTER BLEED TRANSFER, NOTED STRONG ODOR FOLLOWED BY SMOKE IN TOILET CAUTION MESSAGE. RETURNED TO LEX, LAN DED WITHOUT INCIDENT. FOUND OIL IN WATER SEPARATOR. REMOVED OIL AND CLEANED COALESCER BAGS. INSPECTED PACK FOR LEAKS. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007111500176 20071115 00176 SO 2007 11 15 C2XA07RI093 1 20071103 A 3397 CONNECTOR EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS DISCONNECTED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11109 1450657 RIC - DURING ROUTINE MAINTENANCE, MX FOUND FORWARD AISLE OVERHEAD EMERGENCY LIGHT INOPERATIVE. MX RECONNECTED CONNECTOR P8525 ABOVE FORWARD CABIN CEILING PANEL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO S ERVICE. 2 L 7 2 4F RT 2007111500177 20071115 00177 SO 2007 11 15 C2XA07RI094 1 20071106 A 3230 LANDING GEAR EMB 145 EMB145EP 3260221 SO MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 14947 145054 FLT 2581 - EWR - CREW REPORTED THAT AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT FOR ABOUT 2 MINUTES AFTER THE GEAR HANDLE WAS SELECTED UP. EWR MX PERFORMED OPERATIONAL CHECKS OF THE LANDING GEAR SYSTEM (EXTENSION & RETRACTION) IAW EM B AMM 32-30-00 AND COULD NOT DUPLICATE THE PROBLEM. NO FAULT FOUND DURING TEST. ACFT WAS APPROVED TO RETURN TO SERVICE . 2 L 7 2 4F RT T00011AT 2007111500179 20071115 00179 2007 11 15 COMA0760628 4 20071106 A 3418 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING MALFUNCTIONED A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 588SW 7069 FLIGHT 5531 - STALL FAIL CAUTION MESSAGE EN ROUTE TO LGA. AIRCRAFT LANDED SAFELY. PERFORMED STALL PROTECTION SYSTEM RE SET. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007111500181 20071115 00181 EA 2007 11 15 COMA0760630 1 20071106 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER FALSE ACTIVATION A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 403CA 7428 FLIGHT 5689 - LEFT REV UNLOCK CAUTION MESSAGE EN ROUTE TO CVG AT FS 240. AIRCRAFT DIVERTED TO SYR AND LANDED SAFELY. T RANSFERRED TO DEFERRED LIST PER MEL 78-30-01. 2 L 7 2 4F RT A21EA 2007111500184 20071115 00184 NM 2007 11 15 USAA920071098 1 20071024 A 5340 69265553 STRINGER CLIP BOEING 737 7373B7 1384580 NM BS 348 S16L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED STRINGER CLIP, BS 348.2, S16L. REPLACED STRINGER CLIP, BS 348.2, S16L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007111500185 20071115 00185 EU 2007 11 15 200711081 1 20071105 A 2782 1700593C ACTUATOR EMB ERJ170 ERJ170100SE 3260406 EU SLATS DEFECTIVE A UHLA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 11 637RW 17000051 FLIGHT 1556 ORD TO YHZ DURING INITIAL APPROACH WHEN FLAPS 1 WAS SELECTED THE CREW RECEIVED A SLAT FAILURE CAUTION MESSAG E ON THE EICAS. THE CREW WAS ABLE TO EXTEND FLAPS TO 2, DECLARED AN EMERGENCY AND LANDED THE AIRCRAFT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT NR 5 SLAT ACTUATOR. 2 L 7 2 4F RT A56NM 2007111500187 20071115 00187 NM 2007 11 15 2007UALA04579 1 20071105 A 2752 ACTUATOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU TE FLAPS FAILED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 382UA 24657 FOUND NR 2 L/E FLAP WILL NOT FULLY RETRACT. FOUND ACTUATOR FAILED INTERNALLY. REPLACED NR 2 LE FLAP ACTUATOR AND OPS C HECKED SYSTEM. 2 L 7 2 4F 4 F RT A16WE E21EU 2007111500191 20071115 00191 NM 2007 11 15 2007UALA04584 1 20071106 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 4A FWD INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 4A FWD LIGHT ASSY. REPLACED LIGHT ASSEMBLY 2 L 7 4 4F 4 F RT A20WE E24NE 2007111500192 20071115 00192 NM 2007 11 15 2007UALA04585 1 20071106 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1500 S26-27L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 AFT PIT DENT IN FRAME AT STA 1500 BETWEEN STR 26L AND STR 27L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. ACP'D HFEC, NO CRACK FOUND. FABRICATED & INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007111500199 20071115 00199 NM 2007 11 15 2007UALA04592 1 20071105 A 2797 WIRE HARNESS BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SKEW SENSOR DAMAGED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 210UA 30216 FLAP SLAT SKEW MSG IN VIEW. FOUND WIRE HARNESS DAMAGED ON RT OUTBOARD FLAP-SLAT SKEW. REPLACED SKEW SENSOR NR 7 WIRING HARNESS. OP CHECKED PASSED. AC OK FOR SERVICE 2 L 7 2 4F 4 F RT T0001SE E46NE 2007111500204 20071115 00204 NM 2007 11 15 2007UALA04599 1 20071106 A 5514 ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZONTAL STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 306UA 23667 HORIZONTAL STAB CENTER SECTION LT SECONDARY BEAM AT LT PRIMARY BEAM INTERSECTION, AFT SIDE OF SECONDARY BEAM LOWER ANGLE CRACKED. REPLACED ANGLE ON HORIZONTAL STABILIZER CENTER SECTION AT LT PRIMARY BEAM INTERSECTION AFT SIDE LOWER END. 2 L 7 2 4F 4 F RT A16WE E21EU 2007111500205 20071115 00205 NM 2007 11 15 2007UALA04600 1 20071107 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEATS 5 & 4 UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY EXIT LIGHTS ON THE SIDES OF SEATS 5E & 4B ARE LOOSE, 1 IS OFF + IN THE COCKPIT. RESECURED LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007111500208 20071115 00208 NM 2007 11 15 2007UALA04604 1 20071108 A 2700 TRIM SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FAILED A UALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 29 377UA 24642 ON CLIMBOUT AT 17K LOST MAIN ELEC NOSE DOWN TRIM PER CAPTAIN. 2 L 7 2 4F 4 F RT A16WE E21EU 2007111500209 20071115 00209 NM 2007 11 15 2007UALA04605 1 20071107 A 5512 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZONTAL STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 306UA 23667 LEFT HORIZONTAL STAB LOWER SKIN 63 INCHES FROM I/B EDGE 1 INCH FWD OF AFT SPAR CRACKED. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007111500210 20071115 00210 2007 11 15 2007UALA04606 4 20071107 A 2565 FLAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L2 DOOR SLIDE OBSTRUCTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 F/A STATES DOOR 2L STILL DIFFICULT TO DISARM. BOTTOM FLAP STILL GETS IN WAY WHEN DISARMING. FOUND LATCH CABLE INTERFER ENCE. REPOSITIONED LATCH CABLE, SLIDE ARMS AND DISARMS MORMALLY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007111500212 20071115 00212 NM 2007 11 15 2007UALA04608 1 20071107 A 2611 CONTROL PANEL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE ENG-APU FIRE NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 813UA 858 ENG 2 AGENT1 SQUIB LT DOES NOT ILLUMINATE DURING TEST. FOUND ENG/APU FIRE CONTROL PANEL FAULT. REPLACED ENG/APU FIRE CONTROL PANEL. ALL SYSTEMS TESTED AND OPS CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007111600001 20071116 00001 EA 2007 11 16 2007F00066 1 20071017 A 2797 MILDTL2750018TG3 WIRE HARNESS CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF343A1 30015 NE TRIM SYSTEM SHORTED G H DEACTIVATE SYST/CIRCUITS O OTHER UK UNKNOWN 1 SO 17 28KA 5286 5174 ON THE IB FLIGHT, THE NR 1 PITCH TRIM CIRCUIT BREAKER POPPED. THE AIRCRAFT WAS TAKEN TO MFG AND THE TECHNICIANS WERE UNA BLE TO DUPLICATE THE PROBLEM. AT MAINTENANCE REQUEST,THE TAIL WIRE HARNESS (FROM THE PRESSURE BULKHEAD TO THE STABILIZER TRIM ACTUATOR) WAS REMOVED AND FOUND TO HAVE A DAMAGED SPOT IN THE INSULATION. THE HARNESS WAS REPLACED WITH NEW WIRE A ND A NEW CONNECTORS.A FUNCTIONAL TEST FLIGHT WAS ACCOMPLISHED UNSUCCESSFULLY,A TEST HARNESS WAS FABRICATED AND TEMPORARI LY INSTALLED INSIDE THE PRESSURE VESSEL.IT WAS DETERMINED THAT THE HSTCU P/N 601-56156-5 HAD FAILED DUE TO THE SHORTED W IRES PREVIOUSLY REPLACED. THE AIRCRAFT ACCOMPLISHED ANOTHER FUNCTIONAL TEST FLIGHT THAT WAS SUCCESSFUL. 2 L 7 2 4F 4 F RT A21EA E15NE 2007111900001 20071119 00001 NM 2007 11 19 2007UALA04611 1 20071107 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ROW 23 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 538UA 25222 EEL LIGHT INOP AT ROW 23. INSTALLED NEW EMERGENCY LIGHT SECTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007111900002 20071119 00002 NM 2007 11 19 2007UALA04612 1 20071108 A 3150 WARNING MESSAGE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NLG ILLUMINATED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 127UA 28813 TAKEOFF ABORTED AT 100KTS ON ACCT NOSE GEAR PRESSURE SWITCH INDICATION. 2 L 7 4 4F 4 F RT A20WE E24NE 2007111900003 20071119 00003 NM 2007 11 19 SWAA075622 1 20071107 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 767 S14R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 14R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007111900004 20071119 00004 NM 2007 11 19 SWAA075621 1 20071107 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 277 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 10R CRACKED AT BS 277. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007111900006 20071119 00006 NM 2007 11 19 SWAA075619 1 20071107 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 360 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 15L CRACKED AT BS 360. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007111900008 20071119 00008 NM 2007 11 19 SWAA075582 1 20071107 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111900009 20071119 00009 NM 2007 11 19 SWAA075583 1 20071107 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111900010 20071119 00010 NM 2007 11 19 SWAA075580 1 20071107 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM BS 727D S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111900011 20071119 00011 NM 2007 11 19 SWAA075584 1 20071107 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 733A S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733A, STR 4R. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007111900012 20071119 00012 NM 2007 11 19 SWAA075585 1 20071107 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 380 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007111900014 20071119 00014 NM 2007 11 19 SWAA075587 1 20071107 A 5512 65C25727 SKIN BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 DURING SCHEDULED C3 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 132. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007111900015 20071119 00015 NM 2007 11 19 SWAA075588 1 20071107 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 448WN 33721 DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007111900016 20071119 00016 NM 2007 11 19 SWAA075589 1 20071107 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 448WN 33721 DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007111900017 20071119 00017 NM 2007 11 19 SWAA075590 1 20071107 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM ROW 1 ABC INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 458WN 33857 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007111900018 20071119 00018 NM 2007 11 19 SWAA075591 1 20071106 A 3233 654482817 ACTUATOR BOEING 737 7375H4 138449D NM RT MLG FAULTY A SWAA O OTHER O OTHER NR NOT REPORTED 1 SW 29 504SW 24181 RIGHT MLG WOULD NOT REMAIN UP ON INITIAL RETRACTION. SECOND ATTEMPT GEAR STAYED UP. REMOVED AND REPLACED RIGHT MLG UPL OCK ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2007111900019 20071119 00019 NM 2007 11 19 SWAA075592 1 20071107 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 887 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007111900021 20071119 00021 NM 2007 11 19 SWAA075594 1 20071107 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 827 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007111900022 20071119 00022 NM 2007 11 19 SWAA075595 1 20071107 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 847 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007111900023 20071119 00023 NM 2007 11 19 SWAA075596 1 20071107 A 5311 65C38578 FRAME BOEING 737 7375H4 138449D NM BS 482B S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482B, STR 10L. REPAIRED FRAME PER SRM AND BOEING DRAWING . 2 L 7 2 4F RT A16WE 2007111900028 20071119 00028 NM 2007 11 19 SWAA075600 1 20071107 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM ROW 11 ABC WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 11 ABC. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007111900029 20071119 00029 NM 2007 11 19 SWAA075599 1 20071107 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM ROW 1 DEF WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 1 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007111900030 20071119 00030 NM 2007 11 19 SWAA075602 1 20071107 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED MV1 CHECK, FOUND AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2007111900031 20071119 00031 NM 2007 11 19 SWAA075604 1 20071107 A 5330 6545774 SKIN BOEING 737 737317 138447P NM BS 752 S23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 752, STR 23L. REPAIRED SKIN PER ACO. 2 L 7 2 4F RT A16WE 2007111900032 20071119 00032 NM 2007 11 19 SWAA075605 1 20071107 A 5330 6545774 SKIN BOEING 737 737317 138447P NM BS 752 S23R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 752, STR 23R. REPAIRED SKIN PER ACO. 2 L 7 2 4F RT A16WE 2007111900034 20071119 00034 NM 2007 11 19 SWAA075607 1 20071107 A 5322 6546569 SHEAR TIE BOEING 737 737317 138447P NM BS 947 S24L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 947, STR 24L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007111900035 20071119 00035 NM 2007 11 19 SWAA075618 1 20071107 A 5311 6546547 FRAME BOEING 737 737317 138447P NM BS 727 S12L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727, STR 12L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007111900038 20071119 00038 NM 2007 11 19 SWAA075611 1 20071107 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM BS 783 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 783, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007111900039 20071119 00039 NM 2007 11 19 SWAA075613 1 20071107 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 706 S5L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007111900040 20071119 00040 NM 2007 11 19 SWAA075612 1 20071107 A 5311 65C25230 FRAME BOEING 737 7373A4 1384585 NM BS 727E S8L/R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111900044 20071119 00044 NM 2007 11 19 SWAA075614 1 20071107 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 706SW 27840 DURING SCHEDULED HC2 CHECK, AFT LT EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007111900045 20071119 00045 NM 2007 11 19 SWAA075615 1 20071107 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 706SW 27840 DURING SCHEDULED HC2 CHECK, FWD RT EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007111900046 20071119 00046 2007 11 19 SWAA075616 4 20071107 A 2565 63551101 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 709SW 27843 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPL ACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007111900047 20071119 00047 NM 2007 11 19 SWAA075617 1 20071107 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 756SA 27872 DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FLOORBEAM UPPER TEE CAP CORRODED AT BS 986.5, LBL 6. REPAIRED TEE CAP PER SWA EA. 2 L 7 2 4F RT A16WE 2007111900048 20071119 00048 SO 2007 11 19 C2XA07ON026 1 20071107 A 2611 FAU751A4 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO FAULTY A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 14204 2905 2905 14500968 FLT 147 - TUS TO ONT - FLIGHT CREW ENCOUNTER SMOKE DETECTION INDICATION DURING CLIMB OUT AT 2000FT. EMERGENCY WAS DECLA RED AND AIRCRAFT RETURNED TO BLOCK SATISFACTORY. MX REMOVED AND REPLACED THE SMOKE DETECTOR SENSOR, INSPECTED PANELS AN D FOUND THEM IN GOOD CONDITION, RAN ENGINES AND OPERATIONALLY CHECKED THE BLEED SYSTEM WITH NO RELEVANT DEFECTS NOTED. ALL SYSTEMS CHECKED GOOD. A/C WAS RETURNED FOR SERVICE IN AIRWORTHY CONDITIONS. 2 L 7 2 4F RT 2007111900049 20071119 00049 SO 2007 11 19 C2XA07ON027 1 20071107 A 2810 14569685901 O-RING EMB 145 EMB145LR 3260212 SO FUEL PANEL DAMAGED A C2XA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 27 11551 145411 FLT 115 - BOI TO ONT - FLIGHT CREW REPORTED RIGHT WING FUEL LEAK DURING PRE-FLIGHT WALK AROUND. MX SENT A MECHANIC TO B OI WITH PART TO BE CHANGED AND REPOSITION AIRCRAFT TO ONT. MX REMOVED AND REPLACED O-RING AND GASKET FROM WING FUEL PAN EL, OPERATIONALLY CHECKED GOOD AND LEAK CHECKED GOOD A/C WAS RETURNED FOR SERVICE IN AIRWORTHY CONDITIONS. 2 L 7 2 4T RT T00011AT 2007111900051 20071119 00051 NM 2007 11 19 BB07087 1 20071109 A 3350 893003 CHARGER BOEING 767 7672B7 1385107 NM EMERGENCY LIGHTS FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 251AY 24764 MAINTENANCE FOUND EMERGENCY LIGHTS AT ROW 24-27RT INOPERATIVE. REPLACED BATTERY CHARGER AND LIGHT ASSEMBLY. NO FURTHER FAULTS. 2 L 7 2 4F RT A1NM 2007111900052 20071119 00052 NM 2007 11 19 HNAA0700262 1 20071106 A 3350 51001072 SWITCH DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS MALFUNCTIONED A HNAA O OTHER O OTHER CR CRUISE 1 EA 07 810EX 308 THE FLOOR LEVEL EMERGENCY LIGHTS FLICKERED IN FLIGHT. TRIED TO RESET FROM FLIGHT DECK. REMOVED AND REPLACED BOTH FLIGH T ATTENDANTS AND COCKPITS EMERGENCY LIGHT SWITCHES. GROUND RAN AIRCRAFT, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007111900053 20071119 00053 NM 2007 11 19 HNAA0700263 1 20071107 A 3350 3351K2 RELAY DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS MALFUNCTIONED A HNAA O OTHER O OTHER CR CRUISE 1 EA 07 810EX 308 ALL THE CABIN EMERGENCY LIGHTS FLICKERED IN FLIGHT. LIGHTS ILLUMINATED MOMENTARILY RIGHT AFTER TAKEOFF AND IN CRUISE. THIS HAPPENED FIVE OR SIX TIMES DURING FLIGHT. THE PROP HEAT WAS OFF, ON CLIMBOUT. MEGGED WIRES FROM CIRCUIT BREAKER T O EMERGENCY LIGHTING CONTROL BOX, NO DEFECTS NOTED. REMOVED AND REPLACED RELAY 3351-K2 NOT ABLE TO REPRODUCE FAILURE ON GROUND, REQUIRES TEST FLIGHT. TEST FLIGHT WAS GOOD. 2 H 7 2 4T RT A13NM 2007111900058 20071119 00058 NM 2007 11 19 CALA0700664 1 20071020 A 2520 SHADE BOEING 757 757224 1384958 NM CABIN BURNED A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 58101 27291 THE FLIGHT CREW INDICATED THEY SAW AND SMELLED SMOKE IN THE CABIN AREA WITH LIGHTS ON DIM WHILE AT CRUISE. LIGHTS WERE T URNED OFF AND THE SMOKE AND ODOR DISSIPATED. THE FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEM. TROUBLESHOOTING BY MAIN TENANCE FOUND THE LT OVERWING EXIT WINDOW SHADE STUCK IN THE UPWARD POSITION. WHEN IT WAS PULLED DOWN IT WAS FOUND TO B E BURNED, DISCOLORED, AND MELTED. THE SIDEWALL WAS REMOVED AND NO OTHER EVIDENCE OF BURNING WAS FOUND. IT WAS ALSO NOT ED THAT THE WINDOW SHADE HAD BEEN INSTALLED UPSIDE DOWN. EXTENSIVE TROUBLESHOOTING WAS UNABLE TO FIND A CAUSE OF THE PR OBLEM. ENGINEERING IS CONTINUING THE INVESTIGATION INTO THE CAUSE. THE WINDOW SHADE WAS REMOVED AND REPLACED. OPEN 2 L 7 2 4F RT A2NM 2007111900061 20071119 00061 SO 2007 11 19 RAIA00711003 1 20071104 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 805HK 145096 PRE FLT NR 3508 - PIT - EMERGENCY LIGHT FLOOR PROXIMITY LIGHT STRIP INOP. MAINTENANCE DEFFERED PER MEL. 2 L 7 2 4F RT T00011AT 2007111400106 20071114 00106 NM 2007 11 14 07FDEA04768 1 20071110 A 5720 SUPPORT DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 591FE 48527 HFEC OPEN HOLE INSPECTION CARRIED OUT FOUND 1 HOLE CRACK AT RIGHT WING OUTBOARD FLAP HINGE SUPPORT LOWER OUTBOARD HOLE C OMMON TO THE ARC4008 SUPPORT AND ARC4009. REMOVED AND REPLACED AS PER AMM 27-50-30-4. OUTBOARD FLAP VANE ADJUSTMENT CARRIED OUT AS PER AMM 27-50-32-5. OUTBOARD FLAP ADJUSTMENT CARRIED OUT AS PER AMM 27-50-00-830-805. OUTBOARD FLAP STR UCTURAL ADJUSTMENT CARRIED OUT AS PER AMM 27-50-30-5. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007111400107 20071114 00107 NM 2007 11 14 07FDEA04769 1 20071110 A 5720 SUPPORT DOUG MD11 MD11F 3023600 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 591FE 48527 HFEC OPEN HOLE INSPECTION CARRIED OUT FOUND 1 EACH HOLE CRACK AT LEFT WING OUTBOARD FLAP HINGE LOWER OUTBOARD HOLE SUPPO RT COMMON TO THE ARC4008 SUPPORT. REMOVED AND REPLACED AS PER AMM 27-50-30-4. OUTBOARD FLAP VANE ADJUSTMENT CARRIED OUT AS PER AMM 27-50-32-5. OUTBOARD FLAP ADJUSTMENT CARRIED OUT AS PER AMM 27-50-00-830-805. OUTBOARD FLAP STRUCTURAL ADJUSTMENT CARRIED OUT AS PER AMM 27-50-30-5. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007111400108 20071114 00108 EU 2007 11 14 07FDEA04771 1 20071112 A 2150 A/C PACK AIRBUS 310 A310203 3930313 EU NR 1 ODOR A FDEA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 25 429FE 364 PDIS - POWER WAS COMING UP ON TAKEOFF ROLL STARTED SMELLING STRONG ODOR WHICH WAS GETTING STRONGER. ABORTED TAKEOFF AT APPROX 80-90 KIAS- ODOR BEGAN TO DISSIPATE AS SOON AS POWER CAME BACK. THERE WERE NO ABNORMAL INDICATIONS OR ECAM WAR NING. WHILE TAXIING BACK IN AS POWER WAS ADDED FOR TAXI THE ODOR STARTS AGAIN, TRIED TURNING OFF NR 1 PACK ODOR GOES AW AY. REMOVED AND REPLACED COALESCER BAGS ON PACKS 1 AND 2 RAN PACKS WITH APU SUPPLY NO ODOR NOTICED REF A310AMM 21-51-16 -3. A/C OK FOR SERVICE, TSI 2150-8766. C/W THE PACK DUCT CLEANING STEP PER THE AMM 21-51-00-3, NO DEFECTS FOUND. 2 L 7 2 4F RT A35EU 2007111400109 20071114 00109 WP 2007 11 14 07FDEA04772 1 20071112 A 5320 NCA604641 STIFFENER DOUG DC10 DC1030F 3023504 WP ZONE 100 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 AIR CONDITIONING COMPT LT SIDE ON VERTICAL BULKHEAD ON NR 2 VERT STIFFENER FOUND DEEP WEAR. 2 L 7 3 4F RT A22WE 2007111400110 20071114 00110 WP 2007 11 14 07FDEA04773 1 20071112 A 5512 ALC72251 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 308FE 48297 DURING INSP OF CONSTANT SECTION UPPER AND LOWER INTERIOR SKIN PANEL FOUND CRACK IN FLYABLE LIMITS. 2 L 7 3 4F RT A22WE 2007111400111 20071114 00111 NM 2007 11 14 HALA0700479 1 20071023 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 530-650 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 SEAT TRACK CORROSION BEYOND SRM LIMITS, SECTION 43, AT FS 534 THRU FS 650 RBL 88.5. REPAIR BY REPLACEMENT OF SEAT TRACK , FS 530 THRU FS 650 AT RBL 88.5 IAW SRM 53-00-52 REPAIR 3. 2 L 7 2 4F RT A1NM 2007111400113 20071114 00113 NM 2007 11 14 HALA0700478 1 20071024 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 654 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 SEAT TRACK CORROSION BEYOND SRM LIMITS, SECTION 43, AT FS 654+56 THRU 654+66, LBL 20. REPAIR BY SEAT TRACK REPLACEMENT STA 632 THRU 654+66, LBL 20, IAW SRM 1.40.02. 2 L 7 2 4F RT A1NM 2007111400114 20071114 00114 NM 2007 11 14 HALA0700477 1 20071110 A 2750 849704 PSEU BOEING 767 76733A 1385209 NM TE FLAPS MALFUNCTIONED A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 580HA 10085 10085 28140 "BTB" ON TAXI OUT, GOT LEADING EDGE FLAP ASSEMBLY LIGHT. TRIED TO RETRACT BACK UP BUT GOT STUCK IN EXTENDED POSITION. BITE CHECKED FSEU-MESS NR 27-81-02 BITE PSEU CARD FAULT. REMOVED AND REPLACED PSEU PER M/M 32-09-04 OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2007111400115 20071114 00115 NM 2007 11 14 HALA0700481 1 20071025 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 188-654 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 CORROSION AROUND SEAT TRACK ATTACH FLANGE AT STA 654 + 88 TO 118. REPLACED SEAT TRACK. 2 L 7 2 4F RT A1NM 2007111400129 20071114 00129 NM 2007 11 14 DLM88071451 1 20070928 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 1212-1250 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 EXFOLIATON CORROSION ON LT CUSP WEB AT STA Y=1212 TO 1230, 1233 TO 1250. REPAIRED PER SRM 51-70-4. 2 L 7 2 4F RT A6WE 2007111400130 20071114 00130 NM 2007 11 14 DLM88071452 1 20070928 A 5320 INTERCOSTAL DOUG MD88 MD88 3023688 NM BS 1321 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 GALVANIC CORROSION ON AFT FLOOR STRUCTURE INTERCOSTAL BETWEEN STA Y=1321 AND X=0. REPLACED INTERCOASTAL PER DOUGLAS DWG 9936705. 2 L 7 2 4F RT A6WE 2007111400131 20071114 00131 NM 2007 11 14 DLM88071453 1 20070929 A 5320 ANGLE DOUG MD88 MD88 3023688 NM BS 1338 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 CRACKED STIFFENER ANDLE ON P-DOME AT STA Y=1338. REPLACED ANGLE PER DOUGLAS DWG 9915558. 2 L 7 2 4F RT A6WE 2007111400132 20071114 00132 NM 2007 11 14 DLM88071454 1 20071001 A 5320 ANGLE DOUG MD88 MD88 3023688 NM BS 1231-1250 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 CRACK ON AFT UPPER WINDOW RING PAN BTW STA Y=1231 AND 1250 LT. REPAIR ANGLE PER SRM DRD 56-01. 2 L 7 2 4F RT A6WE 2007111400133 20071114 00133 NM 2007 11 14 DLM88071455 1 20071001 A 5320 ANGLE DOUG MD88 MD88 3023688 NM BS 984-1003 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 CRACK ON RT WINDOW RING PANE BTW STA 984 AND 1003 RT FWD LOWER CORNER. REPAIRED PER SRM 56-01D 2 L 7 2 4F RT A6WE 2007111400134 20071114 00134 NM 2007 11 14 DLM88071456 1 20071001 A 5320 ANGLE DOUG MD88 MD88 3023688 NM BS 1021 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 CRACKED LT WINDOW RING PAN AT STA Y=1021. REPAIRED PER SRM DRD 56-01. 2 L 7 2 4F RT A6WE 2007111400135 20071114 00135 NM 2007 11 14 DLM88071457 1 20071001 A 5320 ANGLE DOUG MD88 MD88 3023688 NM BS 1022-1041 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 CRACKED LT WINDOW RING PAN BTWN STA Y=1022/1041. REPAIRED PER SRM DRD 56-01D. 2 L 7 2 4F RT A6WE 2007111400136 20071114 00136 NM 2007 11 14 DLM88071458 1 20071001 A 5320 ANGLE DOUG MD88 MD88 3023688 NM BS 1193-1212 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 CRACKED LT WINDOW RING PAN BTWN STA Y=1193 TO 1212. REPAIRED PER SRM DRD 56-01D. 2 L 7 2 4F RT A6WE 2007111400137 20071114 00137 NM 2007 11 14 DLM88071459 1 20071008 A 5712 RIB DOUG MD88 MD88 3023688 NM RWS 448 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 CRACK ON RT WING FIXED LEADING EDGE RIB ANGLE AT STA XOS=448. REPLACED ANGLE PER DWG 9919329. 2 L 7 2 4F RT A6WE 2007111400138 20071114 00138 NM 2007 11 14 DLM88071460 1 20071008 A 5712 RIB DOUG MD88 MD88 3023688 NM RWS 455 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 49884 CRACK ON RT WING FIXED LEADING EDGE RIB ANGLE AT STA XOS=455. REPLACED ANGLE PER DWG 9919329. 2 L 7 2 4F RT A6WE 2007111400155 20071114 00155 NM 2007 11 14 CALA0700642 1 20071101 A 5330 6545769 SKIN BOEING 737 7373T0 1384582 NM BS 500D CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND FUSELAGE SKIN CORRODED JUST FORWARD OF STA 500D ABOVE S27R. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201. 2 L 7 2 4F RT A16WE 2007111400156 20071114 00156 NM 2007 11 14 CALA0700643 1 20071102 A 5311 65C352436 FRAME BOEING 737 7373T0 1384582 NM BS 847 S23-24R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR CUTOUT AFT FRAME AT LOWER DOOR STOP FITTING, STA 847 BETWEEN STRINGER 23R AND 24R. THE CRACKED FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW SRM 51-40-02, PARAGRAPH 4 AND 7 AND BAC D RAWING 65C35243. 2 L 7 2 4F RT A16WE 2007111400157 20071114 00157 NM 2007 11 14 CALA0700644 1 20071102 A 5320 141A541023 INTERCOSTAL BOEING 737 737824 13844BZ NM BS 344-360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33209 30581 INSPECTION FOUND A 1 INCH CRACK AT FORWARD HOLE OF INTERCOSTAL UPPER FLANGE, STA 344-360, BL 0. THE INTERCOSTAL WAS REP AIRED IAW 5321-01453. 2 L 7 2 4F RT A16WE 2007111400158 20071114 00158 NM 2007 11 14 CALA0700645 1 20071102 A 5340 69353501 ATTACH FITTING BOEING 737 7373T0 1384582 NM BS 747 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND AFT CARGO COMPARTMENT STRINGER 26R ATTACH CLIP CORRODED AT STA 747. A NEW CLIP WAS INSTALLED IAW SRM 5 1-40-02. 2 L 7 2 4F RT A16WE 2007111500010 20071115 00010 NM 2007 11 15 USAA920071082 1 20071030 A 5320 6916970501 ANGLE BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED CABIN FRAME SUPPORT CLIP ANGLE, BS 348.2, S15L. REPLACED CABIN FRAME SUPPORT C LIP ANGLE, BS 348.2, S15L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007111500018 20071115 00018 NM 2007 11 15 USAA920071090 1 20071011 A 5711 114T022212 SPAR BOEING 767 767201 1385125 NM ZONE 600 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 248AY 23900 MIA - MAJOR REPAIR - C-2 CHECK - CORROSION ON RIGHT WING LOWER SURFACE FRONT SPAR LOWER CHORD, WS 226.3. REPAIRED RIGHT WING LOWER SURFACE FRONT SPAR LOWER CHORD, WS 226.3 IAW USAIRWAYS EA 136479. 2 L 7 2 4F RT A1NM 2007111500030 20071115 00030 NM 2007 11 15 SWAA075513 1 20071101 A 5755 SKIN BOEING 737 7373H4 1384600 NM NR 3 SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW MA10787 24133 LEFT WING INBOARD NR 3 FLIGHT SPOILER DELAMINATED AT INBOARD CORNER. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007111500084 20071115 00084 NM 2007 11 15 NOCA16507 1 20071016 A 3350 BULB BOEING 757 75728A 1384976 NM EMERGENCY LIGHTS INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 754NA 29381 EMERGENCY EXIT LIGHT OUTSIDE R4 INOP. RELAMPED BULB PER MM 33-51-00. 2 L 7 2 4F RT A2NM 2007111500090 20071115 00090 NM 2007 11 15 SWAA075564 1 20071105 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 520 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007111500098 20071115 00098 NM 2007 11 15 SWAA075561 1 20071105 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727D S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007111500108 20071115 00108 NM 2007 11 15 SWAA075542 1 20071105 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 S8L/R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500110 20071115 00110 NM 2007 11 15 SWAA075549 1 20071105 A 3350 767 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 467WN 33830 DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007111500120 20071115 00120 SO 2007 11 15 C2XA07CL094 1 20071106 A 3350 66367 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13956 145078 CLE FLIGHT 2038 THE CREW REPORTED THE EMERGENCY EXIT PATH LIGHTING STRIP WAS INOPERATIVE. MAINTENANCE INSPECTED AND REP LACED EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007111500145 20071115 00145 EA 2007 11 15 VNAA0710020 1 20071031 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT DELAMINATED A VNAA O OTHER O OTHER AP APPROACH 1 GL 05 202PS 7858 CREW REPORTED A BIRD STRIKE TO THE CAPTAIN SIDE WINDSHIELD ON SHORT FINAL. MAINTENANCE INSPECTED AND FOUND POSSIBLE DEL AMINATION TO THE WINDOW. MAINTENANCE COMPLIED WITH INSPECTION OF LEFT HAND WINDSHIELD AND FOUND TO BE SURFACE DISCOLORA TION ONLY IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 56-11-01-210-801. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007111500162 20071115 00162 NM 2007 11 15 KCSA071510 1 20071108 A 5320 WEB BOEING 747 747246F 1384850 NM BS 2245 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 L5 MAIN ENTRY DOOR LOWER HINGE CUTOUT WEB CORRODED AT BS 2245.31, WL 230.8. 2 L 7 4 4F RT A20WE 2007111500169 20071115 00169 EA 2007 11 15 COMA0770062 1 20071103 A 3150 NONE CNDAIR CL600 CL6002C10 1390015 EA WARNING MESSAGE NONE A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 391CA 10108 FLIGHT 5506 - RECEIVED ANTI-ICE DUCT WARNING AND RIGHT FUSELAGE DUCT RED ON SYNOPTIC PAGE. DECLARED EMERGENCY, PERFORME D QRH AND LANDED WITHOUT INCIDENT. RAN BOTH ENGINES AND PERFORMED OPS CHECK OF ANTI-ICE SYSTEM. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007111500188 20071115 00188 NM 2007 11 15 2007UALA04581 1 20071105 A 2740 TRIM SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU MALFUNCTIONED A UALA O OTHER O OTHER CL CLIMB 1 WP 29 350UA 24301 ELECTRIC TRIM DOES NOT ENGAGE AFTER T/O FROM EITHER YOKE, TAKES SEVERAL TRIES WITH THE SWITCH. ACCOMPLISHED OPS TEST W ITH FLAPS UP AND AT 1 UNIT. BOTH SW'S OPS NORMAL. MANUAL OPS WAS SMOOTH. INSPECTED EXTERIOR OF STAB AND STAB JACKSCREW A REA, ALL OK. NO HISTORY AND NO FURTHER OCCURANCES SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007111500190 20071115 00190 NM 2007 11 15 2007UALA04583 1 20071106 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY EXIT LIGHT INOP. UPPER DECK ROW 12 CEILING. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007111500193 20071115 00193 NM 2007 11 15 2007UALA04586 1 20071106 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1400 S21L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 AFT PIT STA 1400 STR 21L FRAME DENTED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE, FABRICATED & INSTALLED FRAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2007111500195 20071115 00195 NM 2007 11 15 2007UALA04588 1 20071105 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 571UA 26681 FLOOR EEL LIGHTS INOP ROW 9-22. REPLACED BATTERY ON POWER SUPPLY 2 L 7 2 4F 4 F RT A2NM E17NE 2007111500203 20071115 00203 NM 2007 11 15 2007UALA04597 1 20071107 A 2751 TARGET BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FLAP SYSTEM CONTAMINATED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 676UA 30028 AT FL360, THE FLAP INDICATOR IS FLICKERING BETWEEN UP AND 1 DEG' WITH ASSOCIATED `LE SLAT ASYM' MSG. CREW ALSO NOTED A CLICKING OR CHATTERING TYPE NOISE IN THE OVERHEAD PANEL AREA BY THE 'RAT' SW AREA THAT FELT QUITE WARM. FOUND SLAT IND ICATION TARGETS FULL OF GREASE DUE TO NORMAL AC MAINTENANCE. CLEANED ALL TARGETS ACCOMPLISHED FSEU & PSEU BITE WITH NO F AULTS. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007111500206 20071115 00206 NM 2007 11 15 2007UALA04601 1 20071106 A 3397 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 OVERHEAD EEL LIGHT OUT AT DOOR 2L. 2 L 7 2 4F 4 F RT A2NM E17NE 2007111900024 20071119 00024 NM 2007 11 19 SWAA075623 1 20071107 A 5311 6546558 FRAME BOEING 737 7375H4 138449D NM BS 907 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111900026 20071119 00026 2007 11 19 SWAA075598 4 20071107 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007111900033 20071119 00033 NM 2007 11 19 SWAA075606 1 20071107 A 5322 6546529 SHEAR TIE BOEING 737 737317 138447P NM BS 480 S17R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 480, STR 17R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007111900037 20071119 00037 NM 2007 11 19 SWAA075608 1 20071107 A 5330 6545776 SKIN BOEING 737 7373Y0 1384671 NM BS 980 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 980, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007111900041 20071119 00041 NM 2007 11 19 SWAA075610 1 20071107 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM BS 426-446 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BETWEEN BS 426 AND BS 446, LBL 3 AND BL 0. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007111900043 20071119 00043 NM 2007 11 19 SWAA075624 1 20071107 A 5311 6546549 FRAME BOEING 737 7373A4 1384585 NM BS 767 S27R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, STR 27R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007111900054 20071119 00054 SO 2007 11 19 C2XA07CL096 1 20071108 A 5210 CABLE EMB 145 EMB145LR 3260212 SO PAX DOOR OUT OF ADJUST A C2XA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 27 13989 145271 CLE FLIGHT 2266 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. MAINTENANCE INSPECTED AND ADJUSTED THE FORWARD LOCK BOX CABLE. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007111900056 20071119 00056 NM 2007 11 19 CALA0700661 1 20071107 A 5320 BAC15064521 STRUCTURE BOEING 737 737824 13844BZ NM STA 303-351 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 73251 30582 INSPECTION FOUND LOWER INNER CHORD CORRODED AT L-1 DOOR, STA 303.4-351.2, LBL 45 TO LBL 65. THE CHORD WAS REMOVED AND R EPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007111900062 20071119 00062 SO 2007 11 19 RAIA00711002 1 20071103 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS NO TEST A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 811HK 145256 POST FLT NR 5530 - STL - AFT SIDE AFT CEILING EXIT LOCATOR LIGHT INOP. MAINTENANCE REMOVED AND REPLACED NR 4 INVERTER, CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007111900065 20071119 00065 SO 2007 11 19 RAIA007110001 1 20071101 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BURNED OUT A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 815HK 145048 POST FLT NR 5465 - STL - MAIN DOOR FLOOD LIGHT INOP. MAINTENANCE RELAMPED EMERGENCY LIGHT, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007111900066 20071119 00066 SO 2007 11 19 RAIA00710038 1 20071030 A 3230 2309290000 UPLOCK EMB 145 EMB145LR 3260212 SO LT MLG FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 814HK 22442 145046 FLT NR 5489 - IAD - LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED LEFT MAIN UPLOCK BO X, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007111900067 20071119 00067 SO 2007 11 19 RAIA00710037 1 20071030 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 821HK 145068 POST FLT NR 5558 - STL - EMERGENCY EXIT LIGHT AT SERVICE DOOR INOP. MAINTENANCE RECONNECTED LOOSE CONNECTOR ABOVE SERVI CE DOOR FOR EXIT MARKER, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007111900068 20071119 00068 SO 2007 11 19 RAIA00710036 1 20071030 A 7830 WARNING LIGHT EMB 145 EMB145 3260210 SO THRUST REVERSER ILLUMINATED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 802HK 145066 FLT NR 3525 - PIT - E2 THRUST REVERSER DISAGREE. MAINTENANCE DEFERRED THRUST REVERSER PER MEL. 2 L 7 2 4F RT T00011AT 2007111900069 20071119 00069 NM 2007 11 19 HNAA0700264 1 20071105 A 2910 82910009123 LINE DHAV DHC8 DHC8102 2809003 NM HYDRAULIC SYS LEAKING A HNAA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 07 980HA 376 ACID/CITRUS ODOR IN COCKPIT WHEN BLEEDS OFF ON APPROACH OK IN CRUISE. THERE WAS NO REPORT OF THIS ODOR IN THE CABIN. F OUND HOLES IN HYDRAULIC LINE BELOW FLIGHT DECK. SPLICED IN REPAIR SECTION. USING A QUICK FIT COUPLINGS, IAW 20-50-54 L EAK CHECK GOOD. SERVICED NR 2 HYDRAULICS. 2 H 7 2 4T RT A13NM 2007111900071 20071119 00071 SO 2007 11 19 C2XA07TY067 1 20071107 A 5330 SKIN EMB 145 EMB145XR 3260214 SO FUSELAGE DENTED A C2XA O OTHER O OTHER DE DESCENT 1 SW 27 11155 145782 THE FWD FUSELAGE I UPPER NOSE SKIN AND SEVERAL UNDERLYING STRUCTURAL MEMBERS WERE DAMAGED AS A RESULT OF A BIRD STRIKE. THE DAMAGE IS CONTAINED BETWEEN FRMS 1 & 2, STR 3R & 4L. MAINTENANCE IS REPAIRING DAMAGE IAW EA5330-01107. 2 L 7 2 4F RT 2007111900072 20071119 00072 EA 2007 11 19 TRAX200701683 1 20071105 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 916EV 7757 EMERGENCY FLOOR TRACK LIGHTING BETWEEN ROWS 1 AND 5 INOP. 2 L 7 2 4F RT A21EA 2007111900073 20071119 00073 EA 2007 11 19 TRAX200701684 1 20071105 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA LT OVERWING INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 916EV 7757 LOWER EMERGENCY LIGHT AT LT OVERWING EMERGENCY EXIT INOP. 2 L 7 2 4F RT A21EA 2007111900074 20071119 00074 EA 2007 11 19 TRAX200701685 1 20071105 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 883AS 7504 PANEL 832 BT ON PAX DOOR HAS 1 EACH DAMAGED EXIT PLACARD. 2 L 7 2 4F RT A21EA 2007111900076 20071119 00076 EA 2007 11 19 TRAX200701687 1 20071105 A 5220 ESCAPE HATCH CNDAIR CL600 CL6002B19 1900309 EA STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 883AS 7504 CREW ESCAPE HATCH FAILS FUNCTIONAL TEST, REQUIRES MORE THAN 120 INCH POUNDS TO OPEN. REMOVED CREW ESCAPE HATCH HANDLE ASSEMBLY. 13254. OK TO INSTALL NEW CREW ESCAPE HATCH HANDLE. 2 L 7 2 4F RT A21EA 2007111900082 20071119 00082 EA 2007 11 19 TRAX200701697 1 20071106 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 838AS 7276 FLAP FAIL DURING APPROACH AT ZERO. TOWER DECLARED EMERGENCY. EMERGENCY EQUIPMENT ON STANDBY. FLT 4877 CX. 2 L 7 2 4F RT A21EA 2007111900083 20071119 00083 EA 2007 11 19 TRAX200701700 1 20071107 A 5100 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A ASOA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 850AS 7355 THUMPING IN CONTROL WHEEL AND UNDER F/AS FLOOR AFTER GEAR RETRACTION. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARE D. FLT 4215 DEL 173 MINS. 2 L 7 2 4F RT A21EA 2007111900084 20071119 00084 EA 2007 11 19 TRAX200701701 1 20071107 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA RT OVERWING INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 971EV 7528 OVERWING EMERGENCY LIGHT ON RIGHT SIDE INOP. 2 L 7 2 4F RT A21EA 2007111900085 20071119 00085 EU 2007 11 19 TRAX200701702 1 20071107 A 5260 STEP AEROSP ATR72 ATR72 EU AIRSTAIR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 TOP STEP OF AIRSTAIR DOOR BROKEN. 2 H 7 2 4T RT 2007111900086 20071119 00086 EA 2007 11 19 TRAX200701704 1 20071108 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 878AS 7590 FLIGHT ATTENDANT FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007111900089 20071119 00089 EU 2007 11 19 USAA920071105 1 20071108 A 2910 HYDRAULIC SYSTEM AIRBUS 320 A320214 3930316 EU GREEN SYSTEM LOW A USAA O OTHER J WARNING INDICATION CR CRUISE 1 EA 19 110UW 1112 FLT 1162 - SAN - PHX - EMERGENCY LANDING - CREW REPORTED ACARS 80 MILES OUT OF PHX LOSS OF GREEN HYDRAULIC SYSTEM RENDER ING NOSE WHEEL STEERING INOP. CREW DECLARED AN EMERGENCY. AIRCRAFT WAS TOWED TO GATE. OPEN 2 L 7 2 4F RT A28NM 2007111900090 20071119 00090 SO 2007 11 19 C2XA07IA230 1 20071030 A 3150 WARNING LIGHT EMB 145 EMB145LR 3260212 SO CARGO BAY FALSE ACTIVATION A C2XA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 27 13964 145123 CXO - FLIGHT 4945, THE CREW REPORTED THAT THE BAGGAGE EXT LIGHT ILLUMINATES IN FLIGHT. THE AIRCRAFT LANDED IN CXO WITHO UT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE SMOKE DETECTORS WITH NO DEFECTS NOTED, A ND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007111900091 20071119 00091 NM 2007 11 19 USAA920071100 1 20071024 A 5320 65479738 SHEAR WEB BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED SHEAR WEB, BS 578, RBL 70.53, WL 208. REPLACED SHEAR WEB, BS 578, RBL 70.53, W L 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007111900093 20071119 00093 NM 2007 11 19 USAA920071102 1 20071023 A 5312 65163005 BULKHEAD BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FORWARD PRESSURE BULKHEAD WEB, BS 178, LBL 12, WL 234. REPAIRED FORWARD PRESS URE BULKHEAD WEB, BS 178, LBL 12, WL 234 IAW B737 SRM 53-10-08-2R9. 2 L 7 2 4F RT A16WE 2007111900094 20071119 00094 NM 2007 11 19 USAA920071103 1 20071024 A 5312 651758345 BULKHEAD BOEING 737 7373B7 1384580 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FORWARD PRESSURE BULKHEAD WEB, BS 178, LBL 5.7, WL 178. REPAIRED FORWARD PRESS URE BULKHEAD WEB, BS 178, LBL 5.7, WL 178 IAW B737 SRM 53-10-08-2R12. 2 L 7 2 4F RT A16WE 2007111900096 20071119 00096 NM 2007 11 19 USAA920071108 1 20071107 A 5754 114N4003186 PANEL BOEING 757 7572B7 1384964 NM NR 9 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 933UW 27199 PIT - MAJOR REPAIR - C4 CHECK - RIGHT WING NR 9 SLAT INBOARD COVE PANEL CRACKED, SS 605.30. REPAIRED RIGHT WING NR 9 SL AT INBOARD COVE PANEL CRACKED, SS 605.30 IAW USAIRWAYS EA 110231. 2 L 7 2 4F RT A2NM 2007111900098 20071119 00098 NM 2007 11 19 SWAA075625 1 20071108 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 203WN 32483 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007111900099 20071119 00099 2007 11 19 SWAA075639 4 20071108 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 216WR 32488 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007111900101 20071119 00101 NM 2007 11 19 SWAA075627 1 20071108 A 3350 3071BPEGPL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007111900103 20071119 00103 NM 2007 11 19 SWAA075629 1 20071108 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP MISSING AT ROW 1 DEF. INSTALLED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007111900104 20071119 00104 NM 2007 11 19 SWAA075630 1 20071108 A 5753 6573271 TORQUE TUBE BOEING 737 7373H4 1384600 NM MLG WW WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED C3 CHECK, FOUND LEFT WING T/E FLAP, FLAP DRIVE MOTOR TORQUE TUBE WORN. REMOVED AND REPLACED TORQUE TUB E PER MM. 2 L 7 2 4F RT A16WE 2007111900107 20071119 00107 NM 2007 11 19 SWAA075632 1 20071108 A 3350 3071BPEGPL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 5 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007111900108 20071119 00108 NM 2007 11 19 SWAA075633 1 20071108 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM BS 769 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 769, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007111900109 20071119 00109 NM 2007 11 19 SWAA075634 1 20071108 A 5330 6545768 SKIN BOEING 737 7375H4 138449D NM BS 387 S14R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 387, STR 14R. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007111900110 20071119 00110 NM 2007 11 19 SWAA075635 1 20071108 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111900111 20071119 00111 NM 2007 11 19 SWAA075636 1 20071108 A 5753 6546435278 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 618WN 28034 DURING SCHEDULED C2 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD CORNER. REMOVED AND REPLACED F LAP PER MM. 2 L 7 2 4F RT A16WE 2007111900113 20071119 00113 NM 2007 11 19 SWAA075638 1 20071108 A 5755 SKIN BOEING 737 7373Y0 1384671 NM NR 9 SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW MA8171 23826 RIGHT WING NR 9 GROUND SPOILER DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007111900120 20071119 00120 NM 2007 11 19 USAA920071099 1 20071105 A 3350 321454 BATTERY PACK BOEING 737 7373B7 1384580 NM EMERGENCY LIGHTS FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 531AU 24478 BDL - FLT 1724 - EEL - AFT LEFT EMERGENCY LIGHT BATTERY PACK INOP. MX REPLACED THE BATTERY PACK IAW AMM 33-51-51. OPER ATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2007111900124 20071119 00124 NM 2007 11 19 KCSA071514 1 20071110 A 5320 SHEAR WEB BOEING 747 747246F 1384850 NM BS 820 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 FUSELAGE TENSION TIE SLOPING SHEAR WEB IS CRACKED (.5 INCH) AT STA 820, BETWEEN STR 10L & 10AL. 2 L 7 4 4F RT A20WE 2007111900125 20071119 00125 NM 2007 11 19 UPS07451115 1 20071107 A 2410 GENERATOR BOEING 747 747123 1384873 NM NR 3 INOPERATIVE A IPXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 676UP 20101 INSPECTION TYPE:N/A ATB FOR NR 3 BUSS TIE ON WITH FEEDER FAULT LT & CONST SPEED LIGHT. FIVE MIN LATER, CONST SPD LIGHT GEN 2 & GEN 4 W/LOSS OF BOOST PUMP IN TANKS 2 AND 3, NR 2 AFT, NR 3 FWD. NR 3 FAULT ANNUNCIATOR SHOWED GEN/FEEDER. INS PECTED FEEDERS IN PYLON. REPLACED NR 3 GEN PER MM. CHECKED FOR VOLTAGE DROP & VOLTAGES AT BTR & GCR AND ALL CHECKED GO OD. 2 L 7 4 4F RT A20WE 2007111900127 20071119 00127 NM 2007 11 19 UPS07551126 1 20071103 A 5230 SKIN BOEING 757 75724APF 1384969 NM CARGO DOOR DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 406UP 23728 INSPECTION TYPE:C REPAIR DENT IN LOWER EXTERNAL SKIN SURFACE OF AFT CARGO DOOR. REPAIRED DENT IN LOWER EXTERNAL SKIN AF T CARGO DOOR IAW SRM 52-30-01- 2R4. THIS IS A CATEGORY B REPAIR PER SRM 52-30-01-2R4. REINSPECTION PER SRM 52-30-01-2R 4 TABLE IV FIGURE 201 PAGE 1 SHEET 4. 2 L 7 2 4F RT A2NM 2007111900129 20071119 00129 WP 2007 11 19 UPS07851117 1 20071024 A 5514 WEB DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 LT HORIZONTAL STAB AFT WEB ACCESS HOLES HAVE CRACKS AT FASTENER HOLE ON NR 5, 9, 10, AND 12. STOP D RILLED ALL CRACKS, FABBED DOUBLERS, AND INSTALLED DOUBLERS IAW DC8 SRM 55-03-00, 51-1-8, AND 55-02-00. 2 L 7 4 4F RT 4A25 2007111900132 20071119 00132 NM 2007 11 19 BB07088 1 20071111 A 2497 AS2080N010 CONNECTOR BOEING 757 75723N 1384973 NM RT GENERATOR UNSECURE A USAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 EA 19 205UW 30887 FLIGHT 752, SEA-PHL: AFTER TAKEOFF, RIGHT GENERATOR OFF LIGHT ILLUMINATED FOLLOWED BY APU GENERATOR OFF LIGHT. FLIGHT RETURNED TO FIELD. MAINTENANCE RE-SEATED THE ENGINE FIREWALL CONNECT PLUG AS2080N010. NO FURTHER FAULTS. 2 L 7 2 4F RT A2NM 2007111900133 20071119 00133 EU 2007 11 19 YENA2007097 1 20071108 A 2781 WARNING LIGHT EMB ERJ190 ERJ190100IGW 3260408 EU SLATS ILLUMINATED A YENA O OTHER J WARNING INDICATION AP APPROACH 1 EA 15 231JB 19000033 UPON ARRIVAL/APPROACH INTO BUF SLAT FAILURE ILLUMINATED, QRC PROCEDURES FOLLOWED LANDED SLAT 0 FLAP 2. TROUBLESHOT PER FIM TASK 27-81-00-810-015A, BLOCKS 1-2 AND 9-11. TRIP INDICATORS RESET. OPS CHECK GOOD. 2 L 7 2 4F RT A57NM 2007111900138 20071119 00138 EU 2007 11 19 YENA2007098 1 20071109 A 2780 170286A SENSOR EMB ERJ190 ERJ190100IGW 3260408 EU SLAT SKEW MALFUNCTIONED A YENA O OTHER J WARNING INDICATION AP APPROACH 1 EA 15 247JB 3437 19000042 SLAT FAIL INFLIGHT, NO SLATS AT ALL, APPROACH SLAT 0/FLAP 2, FLAPS OPERATED NORMALLY. UPON TROUBLESHOOTING THROUGH CMC, FOUND FAULT CODE 27811013ACE, L WING OUTBD SLAT PANEL SKEW, REMOVED & REPLACED LEFT OUTBOARD SLAT SKEW SENSOR 3/4 IAW E MB 190 AMM 27-83-01 AND PERFORMED OPERATIONAL TEST PER EMB 190 AMM 27-83-01-710-801-A/500. OPS CHECK GOOD AND MESSAGE C LEARED AT THIS TIME. A/C IS OK FOR RETURN TO SERVICE. 2 L 7 2 4F RT A57NM 2007111900140 20071119 00140 NM 2007 11 19 SWAA075643 1 20071110 A 3350 417A5703 LIGHT BOEING 737 7377H4 1384404 NM ROW 1 ABC LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 227WN 34450 EEPLS LIGHT ASSY LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007111900141 20071119 00141 NM 2007 11 19 SWAA075644 1 20071110 A 3350 767 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 285WN 32536 DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007111900143 20071119 00143 NM 2007 11 19 SWAA075652 1 20071111 A 5340 6557463 FITTING BOEING 737 7373H4 1384600 NM L1 DOOR GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FIT TING PER SRM. 2 L 7 2 4F RT A16WE 2007111900144 20071119 00144 NM 2007 11 19 SWAA075645 1 20071110 A 5753 655292546 TORQUE TUBE BOEING 737 7373H4 1384600 NM TE FLAPS WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED BRDG CHECK, FOUND LEFT WING OUTBOARD TORQUE TUBE WORN. REMOVED AND REPLACED TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007111900146 20071119 00146 NM 2007 11 19 SWAA075663 1 20071111 A 5330 6516352 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD CARGO DOOR CUTOUT LOWER AFT CORNER. REPAIRED SKIN PER S WA EA. 2 L 7 2 4F RT A16WE 2007111900147 20071119 00147 NM 2007 11 19 SWAA075661 1 20071111 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM BS 410 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, BL 0. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007111900148 20071119 00148 2007 11 19 SWAA075646 4 20071110 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 432WN 33715 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007111900149 20071119 00149 NM 2007 11 19 SWAA075647 1 20071110 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 433LV 33716 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007111900150 20071119 00150 NM 2007 11 19 SWAA075648 1 20071110 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 464WN 32468 EEPLS LENS MISSING AT ROW 3 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007111900151 20071119 00151 NM 2007 11 19 SWAA075649 1 20071110 A 3040 57176146 WINDOW BOEING 737 7375H4 138449D NM COCKPIT ARCED A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 515SW 25154 FLIGHT DECK R1 WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2007111900152 20071119 00152 NM 2007 11 19 SWAA075654 1 20071111 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 380 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007111900153 20071119 00153 NM 2007 11 19 SWAA075656 1 20071111 A 5311 6546558 FRAME BOEING 737 7375H4 138449D NM BS 907 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111900154 20071119 00154 2007 11 19 SWAA075655 4 20071111 A 2565 6949956 CABLE BOEING 737 7375H4 138449D NM L2 DOOR SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM. 2 L 7 2 4F RT A16WE 2007111900155 20071119 00155 2007 11 19 SWAA075650 4 20071111 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007111900157 20071119 00157 NM 2007 11 19 SWAA075658 1 20071111 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 756SA 27872 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 26 TO LBL 45. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007111900159 20071119 00159 NM 2007 11 19 SWAA075660 1 20071111 A 5320 141A5750 FLOOR SUPPORT BOEING 737 7377H4 1384404 NM BS 281-285 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 759GS 30544 DURING SCHEDULED 8Y CHECK, FOUND FLOOR SUPPORT CORRODED BETWEEN BS 281 AND BS 285, RBL 13. REPAIRED FLOOR BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007111900160 20071119 00160 2007 11 19 SWAA075651 4 20071111 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 788SA 30603 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007111900161 20071119 00161 EU 2007 11 19 USAA920071106 1 20071108 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHTS DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 636AW 54128 10621 98 FLT 170, JFK-PHX - EEL - FAA RAMP CHECK FOUND EMERGENCY LIGHT INOP ROWS 9 & 11. REMOVED AND REPLACED POWER SUPPLY UNIT AT RIGHT OVERWING, MFG P/N 3214-54, S/N 449, OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 2007111900162 20071119 00162 NM 2007 11 19 UPS07451134 1 20071111 A 3350 BATTERY PACK BOEING 747 747212B 1384886 NM BS 420 DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:N/A EMERGENCY LIGHT ON MCD AT STA 420 LT DOES NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT/BATTERY AS SY WITH REF TO MM 33-51 51-07. OPS CHECK GOOD PER SAME. 2 L 7 4 4F RT A20WE 2007111900163 20071119 00163 NM 2007 11 19 UPS07551131 1 20071017 A 5412 311N3271 BULKHEAD BOEING 757 75724APF 1384969 NM NR 1 NACELLE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 406UP 23728 INSPECTION TYPE:C NR 1 PYLON AFT ENG MOUNT BULKHEAD LWR O/B CORNER OUTER SURFACE IS CHAFED. COMPLIED WITH FINAL EA 757- 5453-27-A1757 AND EO B757-5410- 27988-A. 2 L 7 2 4F RT A2NM 2007111900164 20071119 00164 2007 11 19 UPS07651135 4 20071110 A 2564 LIFE RAFT BOEING 767 76734AF 1385212 NM COCKPIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 308UP 27761 INSPECTION TYPE:ETOP LIFE RAFT INOP - M362002 ASSGNED. STOWAGE BIN LATCH REPLACED ON LP 797292/3. THIS CLEARS M362002. 2 L 7 2 4F RT A1NM 2007111900165 20071119 00165 WP 2007 11 19 UPS07851132 1 20071008 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C SEAT TRACK STA 65 RBL 48 HAS BROKEN LUGS. REMOVED, FABRICATED AND INSTALLED REPAIR SEAT TRACK AT STA 50 - 130 RBL 48 IAW SRM 53-21-02-4, SRM 51-3-00, AND DWG S2400463. 2 L 7 4 4F RT 4A25 2007111900167 20071119 00167 NM 2007 11 19 CALA0700668 1 20071109 A 5310 6520723U66 DOOR FRAME BOEING 737 737524 1384721 NM BS 440-460 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 52616 27329 INSPECTION FOUND A .25 INCH CRACK IN FORWARD CARGO DOOR AFT FRAME AT LOWER DOOR STOP AREA, STA 440-460, S14R TO S27R. T HE AFT FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007111900171 20071119 00171 NM 2007 11 19 CALA0700672 1 20071111 A 5230 6547952U133 DOOR FRAME BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR UPPER FRAME AT SPLICE POINT. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007111900172 20071119 00172 NM 2007 11 19 CALA0700673 1 20071111 A 5230 65C2518022 DOOR FRAME BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR FRAME AT FORWARD LOWER SEGMENT AT PULLEY BOLT HOLE. THE FRAME WAS RE MOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007111900175 20071119 00175 SO 2007 11 19 LR7A07121 1 20071106 A 5350 SKIN LKHEED 382 382G 526414U SO FAIRING CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 618 4606 DURING SCHEDULED B-2 CHECK PER JOB CARD HB5301 FOUND LT BOTTOM WHEEL WELL FAIRING SKIN CRACKED AT BELLY ATTACH POINT, FS 517, WL 130, LBL 45. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-12 USING 2024T3 .040". 2 H 7 4 4T A1SO 2007111900179 20071119 00179 SO 2007 11 19 LR7A07125 1 20071106 A 5330 SKIN LKHEED 382 382G 526414U SO FS 885-890 DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 618 4606 DURING SCHEDULED B-2 CHECK PER JOB CARD HB5301 FOUND LT AFT FUSELAGE EXTERIOR SKIN DENT & NICK AT SKIN LOWER EDGE, FS 88 5 & 890, WL 202. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-12 USING 2024T3 .063". 2 H 7 4 4T A1SO 2007111900180 20071119 00180 SO 2007 11 19 LR7A07126 1 20071106 A 5230 SKIN LKHEED 382 382G 526414U SO FS 1003 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 618 4606 DURING SCHEDULED B-2 CHECK PER JOB CARD HB5301 FOUND CARGO DOOR PRESSURE SAFETY VALVE ATTACHMENT INNER SKIN CRACKED, FS 1003, LBL 50. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-12 USING 7075T6 .080". 2 H 7 4 4T A1SO 2007111900184 20071119 00184 NM 2007 11 19 USAA920071111 1 20071027 A 5320 654797321 CUSP WEB BOEING 737 7373B7 1384580 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CORROSION FOUND ON CABIN CUSP WEB, BS 616-BS 639, S17L, WL 208. REPLACED CABIN CUSP WE B, BS 616-BS 639, S17L, WL 208 IAW BOEING DRAWING 65-47973-21. 2 L 7 2 4F RT A16WE 2007111900185 20071119 00185 NM 2007 11 19 USAA920071112 1 20071102 A 5230 SKIN BOEING 737 7373B7 1384580 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - AFT CARGO DOOR INNER SKIN CRACKED 2 PLACES AT LIGHTENING HOLE IN FORWARD LOWER CORNER, BS 819 - BS 844, S24R. REPAIRED AFT CARGO DOOR INNER SKIN AT LIGHTENING HOLE IN FORWARD LOWER CORNER, BS 819 - BS 844, S24R IAW B737 SRM 51-70-013. 2 L 7 2 4F RT A16WE 2007111900186 20071119 00186 EU 2007 11 19 USAA920071113 1 20071108 A 5320 D53480048207 SILL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 657AW 1083 SAL - MAJOR REPAIR - BC6 CHECK - CORROSION ON THE L2 DOOR CUTOUT LOWER SILL SHAPE SILL FITTING, BS 3158 / FR 66 - BS 320 7 /FR 67. REPLACED THE L2 DOOR CUTOUT LOWER SILL SHAPE SILL FITTING, BS 3158 / FR 66 - BS 3207 /FR 67 IAW A320 SRM 51-7 2-11. 2 L 7 2 4F RT A28NM 2007111900188 20071119 00188 EA 2007 11 19 COMA0770063 1 20071112 A 5340 SH670321493 MOUNT CNDAIR CL600 CL6002C10 1390015 EA GALLEY CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 391CA 11332 10108 AFT INBOARD MOUNT FOR GALLEY NR 1 IS CORRODED. REPLACED MOUNT IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 2007111900190 20071119 00190 EA 2007 11 19 COMA0770065 1 20071112 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 391CA 10108 FS 280 BULKHEAD AND CROSSBEAM CORRODED. BLENDED OUT CORROSION IAW SRM 53-21-43, 51-21-11, 51-25-06, 51-42-13 AND 53-11- 10. 2 L 7 2 4F RT A21EA 2007111900191 20071119 00191 EA 2007 11 19 COMA0770066 1 20071112 A 5753 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA TE FLAPS DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 391CA 10108 RIGHT I/B FLAP HAS A 1 INCH DENT. REPAIRED FLAP IAW SRM 57-52-01. 2 L 7 2 4F RT A21EA 2007111900192 20071119 00192 EA 2007 11 19 COMA0770067 1 20071112 A 5320 SH670318257 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 391CA 11332 10108 PAX DOOR SURROUND MID CAP FLOOR EXTRUSION CORRODED. REPLACED FLOOR SUPPORT MID CAP EXTRUSION IAW SRM 51-21-33. 2 L 7 2 4F RT A21EA 2007111900194 20071119 00194 EA 2007 11 19 COMA0760631 1 20071108 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 SO 01 592SW 7279 FLIGHT 5308 - EN ROUTE CVG-LGA RECEIVED FLAP FAIL MESSAGE. DIVERTED TO JFK, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT . COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C) FL AP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2007111900196 20071119 00196 EA 2007 11 19 COMA0760633 1 20071109 A 3010 ANTI-ICE SYSTEM CNDAIR CL600 CL6002B19 1900309 EA WARNING MESSAGE A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 969CA 7141 FLIGHT 4945 - AFTER SETTING T/O THRUST FOR T/O, WING AND COWL ANTI-ICE SYSTEM ON, RECEIVED RIGHT WING ANTI-ICE CAUTION M ESSAGE. ABORTED TAKEOFF BELOW 80 KTS. TRANSFERRED TO DEFERRED LIST PER MEL 30-12-03-1. 2 L 7 2 4F RT A21EA 2007111900197 20071119 00197 EA 2007 11 19 COMA0760634 1 20071109 A 5610 NP1393219 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA O OTHER O OTHER CR CRUISE 1 SO 01 783CA 16717 7315 FLIGHT 5129 - EN ROUTE CVG - TUL PILOT'S WINDSHIELD CRACKED. LANDED TUL WITHOUT INCIDENT. REPLACED PILOT'S WINDSHIELD. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007111900198 20071119 00198 EA 2007 11 19 COMA0760635 1 20071109 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 815CA 7397 FLIGHT 5006 - FLAPS FAILED AT 0 DEGREES ON APPROACH INTO LGA. AIRCRAFT LANDED SAFELY. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C) FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2007112000001 20071120 00001 EU 2007 11 20 TRAX200701624 1 20071029 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 RIGHT SEAT TRACK BETWEEN FR 39 & 40 CORRODED. RT SEAT TRACK BTW FR 39-40 CORROSION REMOVED IAW SRM 51-21-42 BUT IT IS O UT OF LIMIT AS PER SRM 53-00-00 FIG 304 NEW SEAT TRACK FABRICATED COVER ON W/C 2000-171 INSTALLED ON RT BTW FR 39 AND 40 IAW SRM 51-25-04 MATERIAL THICKNESS: 0.083 MATERIAL REMOVED: 0.023 OUT OF LIMITS AS PER SRM: 53-00-00 FIG 304. 2 H 7 2 4T RT 2007112000002 20071120 00002 EU 2007 11 20 TRAX200701626 1 20071029 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 SEAT TRACK RIGHT O/B BETWEEN FR 29 & 39 CORRODED. CORROSION REMOVED IAW SRM 51-21-42 AND IT IS WITHIN LIMIT AS PER SRM 53-00-00 FIG 304 MATERIAL THICKNESS: 0.053 MATERIAL REMOVED: 0.008 WITHIN LIMITS AS PER SRM: 53-00-00 FIG 304. 2 H 7 2 4T RT 2007112000003 20071120 00003 EU 2007 11 20 TRAX200701628 1 20071029 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 SEAT TRACK LEFT O/B BETWEEN FR 29 & 39 CORRODED. REMOVED CORROSION ON SEAT TRACK LT O/B BTW FR 29+39 AS PER SRM 51-21-4 2 AND IS WITHIN LIMITS AS PER SRM 53-00-00 MATERIAL THICKNESS: 0.083 MATERIAL REMOVED: 0.013 WITHIN LIMITS AS PER SRM: 5 3-00-00 FIG 304. 2 H 7 2 4T RT 2007112000004 20071120 00004 EU 2007 11 20 TRAX200701630 1 20071029 A 5711 SPAR AEROSP ATR72 ATR72 EU LT WING CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 LEFT WING FROM SPAR UPPER ANGLE TOP SURFACE CORRODED AT RIB 13. CORROSION REMOVED IAW SRM 51-21-42 REPAIR DETERMINED NO T TO BE A MAJOR REPAIR MATERIAL THICKNESS: 0.200 MATERIAL REMOVED: 0.003. WITHIN LIMITS AS PER SRM: 51-10-10. 2 H 7 2 4T RT 2007112000005 20071120 00005 EU 2007 11 20 TRAX200701634 1 20071029 A 5210 STEP AEROSP ATR72 ATR72 EU PAX DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 ON STAIR CASE OF PAX DOOR CORROSION FOUND ON STEP NR 2. REMOVED CORROSION ON STEP NR 2 ON STAIR CASE OF PAX DOOR AS PE R SRM 51-21-42 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR A CCOMPLISHED IN ACCORDANCE WITH 51-21-42 MATERIAL THICKNESS: 0.050 MATERIAL REMOVED: 0.002 WITHIN LIMITS AS PER SRM: 52- 11-00 FIG 301. 2 H 7 2 4T RT 2007112000006 20071120 00006 EU 2007 11 20 TRAX200701636 1 20071029 A 5210 STEP AEROSP ATR72 ATR72 EU PAX DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 ON STAIR CASE OF PAX DOOR CORROSION FOUND ON STEP NR 5. REMOVED CORROSION ON STEP NR 5 ON STAIR CASE OF PAX DOOR AS P ER SRM 51-21-42 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH 51-21-42 MATERIAL THICKNESS: 0.043 MATERIAL REMOVED: 0.002 WITHIN LIMITS AS PER SRM: 52- 11-00 FIG 301. 2 H 7 2 4T RT 2007111500050 20071115 00050 NM 2007 11 15 SWAA075509 1 20071102 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007111500060 20071115 00060 NM 2007 11 15 ZZDA2007295 1 20071101 A 5330 SKIN BOEING 717 717200 1383700 NM BS 237 L17-18L DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 978AT 55037 DENT IN FUSELAGE BS 237 BETWEEN LONG L17 AND L18. CUT OUT DAMAGED AREA, FABRICATED DOUBLERS, PER SRM 53-00-01. INSTALL ED REPAIR DOUBLERS, PER 717 SRM 53-00-01 REPAIR 6. 2 L 7 2 4F TR A6WE 2007111500067 20071115 00067 NM 2007 11 15 USAA920071095 1 20071029 A 5712 654544555 RIB BOEING 737 7373G7 1384595 NM ZONE 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, LEFT WING RIB CRACKED, WBL 135.5. REPAIRED LEFT WING RIB, WBL 135.5 IAW USAIRWAYS EA 98 937. 2 L 7 2 4F RT A16WE 2007111500071 20071115 00071 NM 2007 11 15 2007UALA04521 1 20071102 A 2120 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 312UA 23673 CREW REPORT: F/A REPORTS FAINT ODOR OF SMOKE COMING FROM OVERHEAD VENT AT DOOR 2L. AFTER ARRIVAL FLT CREW WENT BACK TO CHECK AND NO ODORS NOTICED. OPERATED APU BLEED WITH PACKS, TURNED ON AFT GALLEY CHILLERS, CM AND LIGHTS NO UNUSAL ODORS NOTED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007111500092 20071115 00092 NM 2007 11 15 SWAA075565 1 20071105 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 460 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007111500094 20071115 00094 NM 2007 11 15 SWAA075563 1 20071105 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 520 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007111500105 20071115 00105 NM 2007 11 15 SWAA075543 1 20071105 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111500111 20071115 00111 NM 2007 11 15 SWAA075550 1 20071105 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM BS 482B S14L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 482B, STR 14L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007111500112 20071115 00112 NM 2007 11 15 SWAA075551 1 20071105 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM BS 783 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 783, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007111500128 20071115 00128 NM 2007 11 15 CALA0700656 1 20071107 A 5330 6518420 SKIN BOEING 737 737524 1384721 NM BS 219.8-227.8 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 52616 27329 INSPECTION FOUND A .75 INCH CRACK IN EXTERIOR FUSELAGE SKIN AT CAPTAIN'S WINDSHIELD O/B CORNER, STA 219.8-227.8, S9L. T HE SKIN WAS REPAIRED IAW SRM 53-10-01, FIGURE 201, REPAIR 10. 2 L 7 2 4F RT A16WE 2007111500134 20071115 00134 NM 2007 11 15 ASAA0792199 1 20071101 A 5347 146A750129 CARGO TRACK BOEING 737 737990 NM BS 787-847 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 307AS 30015 AFT CARGO PIT RIGHT TIEDOWN TRACK CORRODED BS 787 TO BS 847 UPPER & LWR SURFACES. CORRODED SECTION REPLACED WITH SERVIC EABLE REPAIR PART IAW B737 900 SRM B3 00 53 REPAIR 3. 2 L 7 4 4F RT A16WE 2007111500137 20071115 00137 NM 2007 11 15 ASAA0792202 1 20071102 A 5321 146A940121 BUTTSTRAP BOEING 737 737990 NM FLOOR PANEL CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 307AS 30015 AFT CARGO PIT STA 887 FLOOR PANEL BUTT STRAP CORROSION FOUND BETWEEN LBL 8.1 TO RBL 21. AFT CARGO PIT STA 887 FLOOR PAN EL BUTT STRAP REPLACED WITH NEW PART AT LBL 8.1 TO RBL 21 IAW B737 900 SRM 51-40-05. 2 L 7 4 4F RT A16WE 2007111500151 20071115 00151 NM 2007 11 15 SWAA075576 1 20071106 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 360 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007111500154 20071115 00154 NM 2007 11 15 SWAA075573 1 20071106 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM BS 826-1006 CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE UPPER SKIN CHAFING BETWEEN BS 826 AND BS 1006, BELOW DORSAL FIN. REPAIRED SK IN PER SRM. 2 L 7 2 4F RT A16WE 2007111500157 20071115 00157 NM 2007 11 15 SWAA075568 1 20071106 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 1 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007111500168 20071115 00168 EA 2007 11 15 COMA0760621 1 20071102 A 3610 CLAMP CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE LOOSE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 436CA 7482 FLIGHT 5628- EN ROUTE MCO-GSP, RECEIVED RIGHT 10TH STAGE DUCT WARNING FOLLOWED BY RIGHT JET PIPE OVERHEAT MESSAGE. DECL ARED EMERGENCY, RETURNED TO MCO AND LANDED WITHOUT INCIDENT. PERFORMED OPS CHECK ON RIGHT ENGINE FIRE LOOP SYSTEM. NO DEFECTS NOTED. TIGHTENED LOOSE CLAMP ON RIGHT 14TH STAGE SHUTOFF VALVE. PERFORMED LEAK CHECK. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007111500178 20071115 00178 EA 2007 11 15 COMA0760627 1 20071106 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 589SW 29762 7072 FLAPS FAIL CAUTION MESSAGE. FLAPS FAILED AT 45 DEGREES ON APPROACH. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED LEFT BPSU. 2 L 7 2 4F RT A21EA 2007111500180 20071115 00180 EA 2007 11 15 COMA0760629 1 20071106 A 2750 860D10018ABCD COMPUTER CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 446CA 18781 7546 FLIGHT 5026 - FLAPS FAIL CAUTION MESSAGE CAME ON WHILE BRINGING THE FLAPS TO ZERO DEGREES ON THE GROUND. REMOVED AND RE PLACED FECU. 2 L 7 2 4F RT A21EA 2007111500182 20071115 00182 SO 2007 11 15 C2XA07RI095 1 20071105 A 3350 LIGHT EMB 135 EMB135ER 3260203 SO CABIN MALFUNCTIONED A C2XA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 27 17507 145215 FLT 3085 - YOW - CREW REPORTED EMERGENCY LIGHTS ON WHEN NOT ARMED. MX POWER DOWN THE ACFT AND POWER UP AGAIN. NO DEFEC TS FOUND THIS TIME. ACFT AS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007111500189 20071115 00189 NM 2007 11 15 2007UALA04582 1 20071106 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY EXIT EEL LIGHT INOP JUST FWD OF LAV 104 BELOW CLOSET. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007111500194 20071115 00194 NM 2007 11 15 2007UALA04587 1 20071106 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 324 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 MAIN CABIN FLOORBEAM CORRODED AT STA 324 RBL 40 TO RBL 60. 2 L 7 2 4F 4 F RT A2NM E17NE 2007111500197 20071115 00197 NM 2007 11 15 2007UALA04590 1 20071105 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 667UA 29239 SEAT 21H, EEL LIGHT BROKE OFF SIDE OF SEAT. REPLACED LIGHT ASSY, LIGHT CKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007111500198 20071115 00198 NM 2007 11 15 2007UALA04591 1 20071105 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 673UA 29241 SEATS 2B AND 3B BOTH HAVE ONE SEAT MOUNTED EMERGENCY EXIT LIGHT INOP, THE SECONDARY LIGHT ON BOTH SEATS DO OPERATE SATIS FACTORILY. REPLACED EEL STRIPS AT SEATS 1B & 2B. 2 L 7 2 4F 4 F RT A1NM E24NE 2007111500200 20071115 00200 EU 2007 11 15 2007UALA04593 1 20071106 A 3150 STEERING SYS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG WARNING MESSAGE A UALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 469UA 1409 NOSE WHEEL STEERING FAULT DISPLAYED, UNABLE TO TAXI. BSCU & SERVO CNTL 6GC REPLACED 2 L 7 2 4F 4 F RT A28NM E40NE 2007111500201 20071115 00201 NE 2007 11 15 2007UALA04594 2 20071106 A 7261 OIL SYSTEM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 1 ENGINE FLUCTUATES A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 127UA 28813 727899 FLIGHT DIVERTED DUE TO FLUCTUATIONS WITH OIL PRESSURE, QUANTITY & TEMPERATURES ON NR 1 ENGINE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007111900007 20071119 00007 NM 2007 11 19 SWAA075581 1 20071107 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111900013 20071119 00013 NM 2007 11 19 SWAA075586 1 20071107 A 3350 3071BPEGPL LAMP BOEING 737 7373H4 1384600 NM ROW 12 ABC INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED MV1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 12 ABC. REMOVED AND REPLACED LIGHT BULB PE R MM. 2 L 7 2 4F RT A16WE 2007111900025 20071119 00025 NM 2007 11 19 SWAA075597 1 20071107 A 5310 6547976 CREASE BEAM BOEING 737 7375H4 138449D NM BS 947-995 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CHORD CORRODED BETWEEN BS 947 AND BS 995, RBL 50. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2007111900036 20071119 00036 NM 2007 11 19 SWAA075603 1 20071107 A 5311 6546549 FRAME BOEING 737 737317 138447P NM BS 767 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111900050 20071119 00050 NM 2007 11 19 BB07086 1 20071109 A 3350 LIGHT BOEING 757 7572G7 1384963 NM ROW 10L BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 909AW 24522 MAINTENANCE FOUND THE EMERGENCY LIGHT AT ROW 10L INOPERATIVE. REPLACED LIGHT ASSEMBLY. NO FURTHER FAULTS. 2 L 7 2 4F RT A2NM 2007111900055 20071119 00055 NM 2007 11 19 SB07097 1 20071109 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM EMERGENCY LIGHTS DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 453UW 24980 PIT - MAINTENANCE REPORTED THE AFT EMERGENCY DOOR EMERGENCY LIGHTS INOPERATIVE, RIGHT-HAND SIDE. MAINTENANCE REMOVED AN D REPLACED THE BATTERY PACK IN AFT CEILING, RIGHT-HAND SIDE. OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD. 2 L 7 2 4F RT A16WE 2007111900059 20071119 00059 NM 2007 11 19 CALA0700665 1 20071101 A 2520 SHADE BOEING 757 757224 1384958 NM CABIN BURNED A CALA O OTHER O OTHER NR NOT REPORTED 1 SW 27 34137 30229 THERE WAS A REPORT THAT THE WINDOW AREA AT THE LT FORWARD OVERWING EXIT GOT HOT ENOUGH TO SCORCH THE SHADE AND PILLOW AT THE PASSENGER SEAT. NO SMOKE, FIRE, OR ODOR WAS OBSERVED. THE LEFT OVERWING HATCH AREA WAS INSPECTED AND SOME BROWN DI SCOLORATION WAS FOUND. THERE WAS A SPOT AFT OF THE EXIT ON FUSELAGE INTERIOR THAT GOT EXCEPTIONALLY HOT. THE HATCH HEA TERS CHECKED NORMAL. THE WINDOW SHADE WAS REMOVED AND REPLACED IAW MM 52-22-02. THE OVERTEMPERATURE THERMOSTATS WERE A LSO CHECKED AND FOUND NORMAL IAW MM 21-45-00. OPEN 2 L 7 2 4F RT A2NM 2007111900063 20071119 00063 SO 2007 11 19 RAIA00711004 1 20071105 A 3350 78241 INVERTER EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS NO TEST A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 819HK 145062 PRE FLT NR 5584 - RIC - EMERGENCY LIGHT AT FLIGHT/ATTENDANT STATION INOP. MAINTENANCE REMOVED AND REPLACED NR 1 INVERTE R, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007111900064 20071119 00064 SO 2007 11 19 RAIA00711005 1 20071105 A 3397 WIRE EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 804HK 145082 PRE FLT NR 3511 - PIT - FLOOR PROXIMITY LIGHT INOP. MAINTENANCE REPAIRED BROKEN WIRE AND OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007111900070 20071119 00070 SO 2007 11 19 C2XA07TY066 1 20071027 A 3230 LANDING GEAR EMB 135 EMB135ER 3260203 SO MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 19503 176 L/G WILL NOT RETRACT. OPS CHECKED PROX SWITCHES ON GEAR IAW EMB 135MM 32-63-05-700-802-A PERFORMED GEAR SWINGS IAW EMB 135 MM 32-30-00. COULD NOT DUPLICATE, OPS CHECKED GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007111900097 20071119 00097 NM 2007 11 19 USAA920071109 1 20071107 A 5330 144N321121 SKIN BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 933UW 27199 PIT - MAJOR REPAIR - C4 CHECK - CORROSION ON FUSELAGE WINDOW BELT SKIN INNER SURFACE, BS 920 - BS 960, S13L. REPAIRED F USELAGE WINDOW BELT SKIN INNER SURFACE, BS 920 - BS 960, S13L IAW USAIRWAYS EA 110213. 2 L 7 2 4F RT A2NM 2007111900100 20071119 00100 NM 2007 11 19 SWAA075626 1 20071108 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 293WN 36612 R2 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007111900102 20071119 00102 NM 2007 11 19 SWAA075628 1 20071108 A 3350 3071BPEGPL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007111900112 20071119 00112 NM 2007 11 19 SWAA075637 1 20071108 A 5311 6546549 FRAME BOEING 737 737317 138447P NM BS 767 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007111900114 20071119 00114 NM 2007 11 19 SWAA075640 1 20071108 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 987 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 759GS 30544 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, LBL 22 TO LBL 41. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007111900116 20071119 00116 NM 2007 11 19 ASAA0752211 1 20071108 A 3610 32144464 VALVE BOEING 737 737890 1384527 NM NR 1 ENGINE DEFECTIVE A ASAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 02 570AS 35185 DUCT PRESSURE SPLIT DURING CLIMBOUT AT 6000. RT=45 LT=12. AT FL390 RT=40 LT=40. AT TOP OF DESCENT RT=23 LT=20. REPLAC ED NR 1 HIGH STAGE VALVE & NR 1 HIGH STAGE REGULATOR. 2 L 7 2 4F RT A16WE 2007111900117 20071119 00117 NM 2007 11 19 ASAA0742213 1 20071109 A 5340 6517688168 ATTACH ANGLE BOEING 737 7374Q8 138447Q NM BS 312-328 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 MAIN CABIN FS 316 328 LBL 60 CUSP WEB ATTACH ANGLE HAS CORROSION. REMOVED CORROSION FROM ANGLE ORG MATERIAL .090, REMOV ED MATERIAL .020 REMAINING .070, FOUND OUT OF LIMITS. OBTAINED DRILLED AND INSTALLED NEW ANGLE IAW B737 400 SRM 51-40-2 . 2 L 7 2 4F RT A16WE 2007111900118 20071119 00118 NM 2007 11 19 ASAA0742214 1 20071109 A 5340 6517688167 ATTACH ANGLE BOEING 737 7374Q8 138447Q NM BS 328-344 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 MAIN CABIN FS 328 344 LBL 60 CUSP WEB ATTACH ANGLE HAS CORROSION. FABRICATED AND INSTALLED NEW ANGLE IAW BAC DWG 65 176 88 AND BAC 737 400 SRM 51-40-2. 2 L 7 2 4F RT A16WE 2007111900121 20071119 00121 NM 2007 11 19 KCSA071511 1 20071110 A 5330 SKIN BOEING 747 747246F 1384850 NM BS 2190 S44-45L CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 EXTERNAL FUSELAGE SKIN HAS PILLOWING SKIN AROUND FASTENERS AND 1 FASTENER WITH A POPPED HEAD AT STA 2190, STR 44L TO 45L . 2 L 7 4 4F RT A20WE 2007111900122 20071119 00122 NM 2007 11 19 KCSA071512 1 20071110 A 5311 FRAME BOEING 747 747246F 1384850 NM BS 434 S26-27L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 FUSELAGE FRAME HAS A CRACK (.5 INCH) AT STA 434, BETWEEN STR 26L & 27L. 2 L 7 4 4F RT A20WE 2007111900123 20071119 00123 NM 2007 11 19 KCSA071513 1 20071110 A 5320 SHEAR WEB BOEING 747 747246F 1384850 NM BS 820-840 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 FUSELAGE TENSION TIE SLOPING SHEAR WEB IS CRACKED IN 2 AREAS (.5 INCH) BETWEEN STA 820 TO 840, STR 10R & 10AR. 2 L 7 4 4F RT A20WE 2007111900126 20071119 00126 NM 2007 11 19 UPS07551125 1 20071016 A 5311 70750080C FRAME BOEING 757 75724APF 1384969 NM BS 1340 S25-26R DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 406UP 23728 INSPECTION TYPE:C DENT IN AFT CARGO COMPARTMENT FUSELAGE FRAME STA 1340 APPROX BETWEEN S25R AND S26R. REPAIR ACCOMPL PE R SRM 53-00-07 REPAIR S DETAIL III FIG 201 SHEET 8 OF 15. THIS IS A CATEGORY B REPAIR PER SRM 53-00-07. REINSPECTION P ER SRM 53-00-07 DETAIL V FIG 201 SHEET 12 OF 15 ZONE 1 TABLE II FIG 201 SHEET 10 OF 15. 2 L 7 2 4F RT A2NM 2007111900128 20071119 00128 NM 2007 11 19 UPS07551127 1 20071107 A 3350 LAMP BOEING 757 75724APF 1384969 NM EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 471UP 28842 EMERGENCY EGRESS LIGHT INOP. RELAMPED EMERGENCY EGRESS LIGHT PER MM 33-51-06-2. 2 L 7 2 4F RT A2NM 2007111900135 20071119 00135 2007 11 19 BB07089 4 20071109 A 3454 285T05545 CONTROL PANEL BOEING 767 7672B7 1385107 NM VOR/DME FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 251AY 84440 490 24764 FLIGHT 811, PHL-CUN: AFTER TAKEOFF, CREW REPORTED LOSS OF L-NAV. RETURNED TO FIELD. MAINTENANCE REPLACED THE VOR/DME CONTROL PANEL. NO FURTHER FAULTS. 2 L 7 2 4F RT A1NM 2007111900142 20071119 00142 NM 2007 11 19 SWAA075653 1 20071111 A 5340 6557463 FITTING BOEING 737 7373H4 1384600 NM L1 DOOR GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FIT TING PER SRM. 2 L 7 2 4F RT A16WE 2007111900158 20071119 00158 NM 2007 11 19 SWAA075659 1 20071111 A 5315 141A5504 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 759GS 30544 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 44. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007111900166 20071119 00166 NM 2007 11 19 CALA0700667 1 20071109 A 5514 6547505 STRUCTURE BOEING 737 7373T0 1384582 NM HORIZONTAL STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND A .5 INCH CRACK IN LT HORIZONTAL STABILIZER UPPER O/B CHORD AT STAB STA 101.90. THE CRACKED AREA OF CH ORD WAS REMOVED AND A REPAIR WAS INSTALLED IAW IAW SRM 51-70-12. 2 L 7 2 4F RT A16WE 2007111900177 20071119 00177 SO 2007 11 19 LR7A07123 1 20071106 A 5320 33147913 FITTING LKHEED 382 382G 526414U SO FS 792 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 618 4606 DURING SCHEDULED B-2 CHECK PER JOB CARD HB5302 FOUND CABIN STRUT UPPER FITTING CRACKED AT FS 792 WL 256 RBL 62. REPAIR ACCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70 USING 7075T6 .250". 2 H 7 4 4T A1SO 2007111900181 20071119 00181 SO 2007 11 19 LR7A07127 1 20071106 A 5320 STIFFENER LKHEED 382 382G 526414U SO FS 896 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 618 4606 DURING SCHEDULED B-2 CHECK PER JOB CARD HB5301 FOUND AFT FUSELAGE INTERIOR STIFFENER CRACKED AT FS 896 WL 202 LBL 63. R EPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-21 USING 301 1/2H .063". 2 H 7 4 4T A1SO 2007111900182 20071119 00182 NM 2007 11 19 USAA920071107 1 20071110 A 5753 65C6321512 SPINDLE BOEING 737 7373G7 1384595 NM TE FLAP CARRIAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, CORROSION ON RIGHT WING OUTBOARD MID FLAP INBOARD CARRIAGE SPINDLE. REMOVED AND REPLACE D SPINDLE. 2 L 7 2 4F RT A16WE 2007111900183 20071119 00183 NM 2007 11 19 USAA920071110 1 20071110 A 5313 STRINGER BOEING 757 757225 1384959 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918UW 22196 CLT - MAJOR REPAIR - CORROSION ON STRINGER, BS 457, S25R. REPAIRED STRINGER, BS 457, S25R IAW USAIRWAYS EA 100010. 2 L 7 2 4F RT A2NM 2007111900187 20071119 00187 NM 2007 11 19 USAA920071114 1 20071014 A 5720 STRUCTURE BOEING 737 7373G7 1384595 NM ZONE 600 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, RIGHT WING LOWER WING CHORD CRACKED, WS 135.5. REPAIRED RIGHT WING LOWER CHORD, WS 135. 5 IAW USAIRWAYS EA 98943. 2 L 7 2 4F RT A16WE 2007111900189 20071119 00189 EA 2007 11 19 COMA0770064 1 20071112 A 5330 SKIN PANEL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE GOUGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 391CA 10108 FUSELAGE SKIN GOUGED BELOW SERVICE DOOR. REPAIRED DAMAGED AREA IAW REO 670-53-21-312. 2 L 7 2 4F RT A21EA 2007111900195 20071119 00195 EA 2007 11 19 COMA0760632 1 20071108 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 675BR 7635 FLIGHT 5620 - EN ROUTE CVG-YUL RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C) FLAP SYSTEM WAS RES ET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2007112000007 20071120 00007 EU 2007 11 20 TRAX200701637 1 20071029 A 5714 INTERCOSTAL AEROSP ATR72 ATR72 EU WING BOX BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 WING BOX INTERCOSTAL ANGLE BROKEN AT FR 23D RIGHT STR 2R. A NEW ANGLE HAS BEEN FABRICATED IAW SRM 53-91-72 FIG 101 AND INSTALLED IAW SRM 51-25-01. 2 H 7 2 4T RT 2007112000008 20071120 00008 EU 2007 11 20 TRAX200701642 1 20071030 A 5210 SKIN AEROSP ATR72 ATR72 EU PAX DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 ON INNER SKIN OF PAX DOOR CORROSION FOUND AT MANY PLACES AROUND ANCHOR NUT. CORROSION FOUND ON PAX DOOR INNER SKIN HAS BEEN BLENDED AND FOUND WIHTIN LIMITS IAW SRM 51-21-42 AND SRM 52-11-00 FIG 301 MATERIAL THICKNESS: 0.050 MATERIAL REMOV ED: 0.002. WITHIN LIMITS AS PER SRM: 53-00-00 . 2 H 7 2 4T RT 2007112000009 20071120 00009 NM 2007 11 20 2007UALA04535 1 20071101 A 5347 SEAT TRACK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 844UA 1581 LT INBD AND OTBD AND RT INBD AND OTBD OVERWING SEAT TRACKS ARE WORN OUT OF LIMITS FROM WHERE FWD SEAT LUGS LOCK INTO TRA CKS BETWEEN FRAMES 41 AND 47 MAJOR REPAIR ACCOMPLISHED. DURING HMV VISIT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112000010 20071120 00010 NM 2007 11 20 2007UALA04538 1 20071103 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 802UA 690 02 LOW REQUIRES SERVICING. SERVICED CREW O2 SYSTEM 2 L 7 2 4F 4 F RT A28NM E40NE 2007112000011 20071120 00011 NM 2007 11 20 2007UALA04540 1 20071103 A 2700 3945128102 COMPUTER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE ELAC2 FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 823UA 952 ELAC 2 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. ELAC2 FAULTY-NFF. REPLACED ELAC2 - ALL TESTS PASSED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112000012 20071120 00012 NM 2007 11 20 2007UALA04569 1 20071102 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 842UA 1569 CREW OXYGEN SYSTEM-LOW, RECORD PRESSURE PRIOR TO SERVICING. CREW COMMENTS: 02 AT 1200 PSI. SERVICED CREW O2 SYSTEM. N O REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112000038 20071120 00038 EU 2007 11 20 2007UALA04620 1 20071109 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 423UA 504 EMERGENCY ESCAPE PATH LIGHTING AT SEAT 25C IS INOP. REPAIRED WIRE ON LIGHT CONNECTOR, OPS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112100013 20071121 00013 NM 2007 11 21 CALA0700678 1 20071110 A 5313 6552988Y609 STRINGER BOEING 737 7373T0 1384582 NM BS 960-980 S25L CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND STRINGER 25L CORRODED AT STA 960-980. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 53-00-03, REPAIR 1 . 2 L 7 2 4F RT A16WE 2007112100017 20071121 00017 NM 2007 11 21 CALA0700682 1 20071112 A 5330 65516242 SKIN BOEING 737 7373T0 1384582 NM BS 967 S27L/R CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND SKIN CORRODED AT RIVET ROW, STA 967 BETWEEN STRINGERS 27R AND 27L. A REPAIR WAS INSTALLED IAW ECRA 531 1-01377. 2 L 7 2 4F RT A16WE 2007112100018 20071121 00018 NM 2007 11 21 CALA0700683 1 20071112 A 5340 6916970501 STRINGER CLIP BOEING 737 7373T0 1384582 NM BS 348.2 S15L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND A .5 INCH CRACK IN ATTACHMENT CLIP (BROKEN FASTENER HEADS TOO) ON STRINGER 15L AT STA 348.2. THE ATTAC HMENT CLIP WAS REPLACED IAW ECRA 5311-01375. 2 L 7 2 4F RT A16WE 2007112100019 20071121 00019 NM 2007 11 21 CALA0700685 1 20071112 A 5320 69265553 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 348.2 S16L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND A 5 INCH CRACK AND MISSING FASTENER HEAD IN INTERCOSTAL WEB ON STRINGER 16L AT STA 348.2. THE INTERCOS TAL WEB WAS REPLACED IAW ECRA 5311-01375. 2 L 7 2 4F RT A16WE 2007112100024 20071121 00024 NM 2007 11 21 SWAA075666 1 20071112 A 5753 SKIN BOEING 737 7377H4 1384404 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 757LV 29850 DURING SCHEDULED 8Y CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED INBOARD AFT CORNER. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007112100025 20071121 00025 NM 2007 11 21 HNAA0700268 1 20071112 A 2910 DSC252A40230 LINE DHAV DHC8 DHC8102 2809003 NM HYDRAULIC SYS LEAKING A HNAA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 EA 07 837EX 217 DURING TAXI AWAY FROM GATE, FLUID WAS SEEN LEAKING FROM THE NR 1 MAIN LANDING GEAR ASSEMBLY. IMMEDIATELY AFTER, THE NR 2 HYDRAULIC SYSTEM WENT INTO ISOLATION MODE. BOTH HYDRAULIC SYSTEMS STILL HAD QUANTITIES DISPLAYED. AIRCRAFT WAS TOWED TO GATE WHERE THE LEFT O/B FLEXIBLE BRAKE LINE WAS FOUND TO BE LEAKING. REPLACED FLEXIBLE LINE AND WAS CHECKED AS GOOD WITH NO LEAKS. BOTH HYDRAULIC SYSTEMS WERE SERVICED. 2 H 7 2 4T RT A13NM 2007112100027 20071121 00027 NM 2007 11 21 KPVA200721 1 20071109 A 2750 FLAP SYSTEM DHAV DHC8 DHC8103 1386005 NM TE FLAPS MALFUNCTIONED A KPVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 13 829EX 146 (PIREP) ON TAKEOFF ROLL RECEIVED THE TAKEOFF WARNING HORN. NOTICED FLAP INDICATOR WAS ON THE HIGH SIDE OF THE 5 DEGREE ARC (BETWEEN 0 AND 5 DEGREES). RETRACTED (CYCLED) FLAPS TO 15 DEGREES THEN BACK TO 5 DEGREES. FLAP INDICATOR SHOWED IT TO BE CENTERED WITH 5 DEGREES FLAPS. RETURNED TO TAXIWAY L TO ATTEMPT ANOTHER TAKEOFF. NO PROBLEMS THERE ON. NOTE: FLIGHT CREW WAS ABLE TO CORRECT THE DISCREPANCY AND NO LOG ENTRY WAS MADE. 2 H 7 2 4T RT A13NM 2007112100029 20071121 00029 NM 2007 11 21 SB07099 1 20071112 A 3350 20121 POWER SUPPLY BOEING 737 737401 1384701 NM EMERGENCY LIGHTS INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 ALB - WITH AIRCRAFT POWER DISCONNECTED, EMERGENCY EXIT LIGHTS AT SEAT ROWS 12 THROUGH 19 DID NOT ILLUMINATE. ALSO, FOUR BULL NOSE LIGHTS AND THE EMERGENCY LIGHT AT THE L2 DOOR DID NOT ILLUMINATE. MAINTENANCE REPLACED EMERGENCY LIGHT POWER SUPPLIES M1136 AND M1137 IN ASSOCIATION WITH MM 33-51-51 AND REPLACED MATING BATTERIES FOR LOW CAPACITY. RELAMPED EMER GENCY LIGHTS AND REPLACED SEVERAL MISSING LENSE. OPERATIONAL TEST OF EMERGENCY LIGHTS CHECKED GOOD PER MM 33-51-02. 2 L 7 2 4F RT A16WE 2007112100032 20071121 00032 EA 2007 11 21 TRAX200701703 1 20071108 A 7830 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 883AS 7504 AAR - LEFT T/R BLOCKER DOOR NR 7 LINK ATTACH LUG CRACKED. DUPLICATE ENTRY (SEE DEFECT 119411-1) SUPPLEMENTAL - SDR CLO SED 11/13/07. 2 L 7 2 4F RT A21EA 2007112100033 20071121 00033 EA 2007 11 21 TRAX200701708 1 20071109 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 830AS 7236 F/A FLASHLIGHT IS INOP. 2 L 7 2 4F RT A21EA 2007112100034 20071121 00034 2007 11 21 C2XA07RI096 2 20071108 A 7320 14530503403 CONTROL MODULE EMB 145 EMB145ER 3260211 SO ENGINE INOPERATIVE A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 11535 14295 3032 145518 FLT 3158 - EWR - CREW REPORTED THAT ENGINE NR 1 WOULD NOT SHUT-DOWN, E1 NO DISPATCH ON EICS. CREW USED T-HANDLE TO SHUT DOWN THE ENGINE. EWR MX REMOVED AND REPLACED POWER PLANT CONTROL MODULE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007112100035 20071121 00035 EA 2007 11 21 TRAX200701709 1 20071109 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 970EV 7527 MIDDLE AFT CEILING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007112100036 20071121 00036 NM 2007 11 21 ZZDA2007297 1 20071109 A 2120 6411211 OVERHEAT SENSOR BOEING 737 7377BD 1384511 NM MALFUNCTIONED A ZZDA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 37 286AT 34480 FUMES IN COCKPIT ON TAKEOFF ABORTED T/O PERFORMED QRH DUCT (LEFT) OVERHEAT ON TAXI OUT ASSOCIATED WITH AIR CONDITIONING / ABORTED TO SP:115 WT:138. REMOVED AND REPLACED LT DUCT OVERTEMP SENSOR, REF B737 AMM 21-61 RAN ENGINE AT TAKEOFF POWE R, NO UNUSUAL SMELL NOTED "DUCT OVERTEMP" LIGHT EXTINGUISHED DID NOT ILLUMINATED AT T/O POWER. 2 L 7 2 4F RT A16WE 2007112100037 20071121 00037 NM 2007 11 21 ZZDA2007298 1 20071105 A 5320 J060228U3 PAN BOEING 717 717200 1383700 NM CARGO DOOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 940AT 55004 FWD CARGO DOOR LOWER PAN, CUT OUT HAS CORROSION. INSTALLED LOWER SECTION OF JAMB PAN BETWEEN STA 370 & 427 AND SPLICED REPAIR PER SRM 53-20-15 REPAIR 6. 2 L 7 2 4F TR A6WE 2007112100038 20071121 00038 EU 2007 11 21 USAA920071115 1 20071101 A 5321 D5361060500000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 657AW 1083 SAL - MAJOR REPAIR - BC6 CHECK - CORROSION ON CABIN FLOORBOARD 221FF, BS 709 / FR 16 - BS 808 / FR 20, +Y1292 TO +Y1732. REPLACED CABIN FLOORBOARD 221FF, BS 709 / FR 16 - BS 808 / FR 20, +Y1292 TO +Y1732 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007112100040 20071121 00040 NM 2007 11 21 USAA920071118 1 20071009 A 5315 6545834107 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 328 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, CRACKED FLOOR SUPPORT STRAP, BS 328, LBL 30. REPLACED FLOOR SUPPORT STRAP, BS 328, LBL 30 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007112100042 20071121 00042 NM 2007 11 21 USAA920071120 1 20071110 A 5322 SHEAR TIE BOEING 757 757225 1384959 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918UW 22196 CLT - MAJOR REPAIR - CORROSION ON SHEAR TIE, BS 480, S23R - S24R. REPLACED SHEAR TIE, BS 480, S23R - S24R IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007112100043 20071121 00043 NM 2007 11 21 USAA920071121 1 20071110 A 5322 SHEAR TIE BOEING 757 757225 1384959 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918UW 22196 CLT - MAJOR REPAIR - CORROSION ON SHEAR TIE, BS 480, S24R - S25R. REPLACED SHEAR TIE, BS 480, S24R - S25R IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007112100044 20071121 00044 EU 2007 11 21 USAA920071122 1 20071110 A 5315 D5347217220400 FLOORBEAM AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 658AW 1110 PIT - MAJOR REPAIR - BC6 CHECK, CORROSION ON CABIN FLOORBEAM, BS 3158 / FR 66 - BS 3257 / FR 68. REPLACED CABIN FLOORBE AM, BS 3158 / FR 66 - BS 3257 / FR 68 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007112100045 20071121 00045 NM 2007 11 21 USAA920071125 1 20071003 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, CRACKED FLOOR SUPPORT, BS 540, RBL 2. REPLACED FLOOR SUPPORT, BS 540, RBL 2 IAW B737 SR M 51-10-02. 2 L 7 2 4F RT A16WE 2007112100046 20071121 00046 NM 2007 11 21 USAA920071126 1 20071003 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, CRACKED FLOOR SUPPORT, BS 540, LBL 2. REPLACED FLOOR SUPPORT, BS 540, LBL 2 IAW B737 SR M 51-10-02. 2 L 7 2 4F RT A16WE 2007112100047 20071121 00047 NM 2007 11 21 USAA920071127 1 20071003 A 5753 65C2591118A SKIN BOEING 737 7373G7 1384595 NM ZONE 600 DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, RIGHT WING AILERON UPPER LEADING EDGE HAS EXPOSED CARBON FIBLER. REPLACED RIGHT WING AI LERON IAW TASK CARD R3M27015. 2 L 7 2 4F RT A16WE 2007112100048 20071121 00048 NM 2007 11 21 USAA920071128 1 20071004 A 5751 SKIN BOEING 737 7373G7 1384595 NM ZONE 500 DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, LEFT WING AILERON OUTBOARD UPPER SURFACE HAS EXPOSED COMPOSITE. REPAIRED LEFT WING AILE RON OUTBOARD UPPER SURFACE IAW USAIRWAYS EA 98940. 2 L 7 2 4F RT A16WE 2007112100050 20071121 00050 NM 2007 11 21 USAA920071130 1 20071003 A 5322 6948204505 SHEAR TIE BOEING 737 7373G7 1384595 NM BS 348 S13L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, CRACKED SHEAR TIE, BS 348, S13L. REPLACED SHEAR TIE, BS 348, S13L IAW 737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007112100051 20071121 00051 NM 2007 11 21 USAA920071131 1 20071107 A 5753 SKIN BOEING 757 7572B7 1384964 NM RT WING TE FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 933UW 27199 PIT - MAJOR REPAIR - C1 CHECK, RIGHT WING OUTBOARD AFT FLAP DELAMINATED, WS 78.30 AND WS 223.40. REPAIRED RIGHT WING OU TBOARD AFT FLAP, WS 78.30 AND WS 223.40 IAW USAIRWAYS EA 110229. 2 L 7 2 4F RT A2NM 2007112100052 20071121 00052 EU 2007 11 21 USAA920071132 1 20071109 A 5320 SILL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 658AW 1110 PIT - MAJOR REPAIR - BC6 CHECK, CORROSION ON DOOR SILL, BS 3257 / FR 68. REPAIRED DOOR SILL, BS 3257 / FR 68 IAW A320 S RM 53-41-14. 2 L 7 2 4F RT A28NM 2007112100054 20071121 00054 WP 2007 11 21 ASAA0782227 1 20071112 A 5322 995301629 SHEAR TIE DOUG DC9 DC983 3022083 WP BS 1437 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 977AS 53453 AFT ACCESSORY COMPT SHEAR TIE CRACKED AT AFT SIDE OF FRAME STA 1437 I/B OF LONGERON 3L. REMOVED DAMAGED SHEAR TIE RECEI VED A REPLACEMENT SHEAR TIE LOCATED DRILLED AND INSTALLED IAW MD80 SRM 51-10-4 PG 1 AND FIG 3A SHEET 1 AND 51-30-5 PG 12 AND 13. 2 L 7 2 4F RT A6WE 2007112100055 20071121 00055 WP 2007 11 21 ASAA0782228 1 20071112 A 5322 995301630 SHEAR TIE DOUG DC9 DC983 3022083 WP BS 1437 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 977AS 53453 AFT ACCESSORY COMPT SHEAR TIE CRACKED AT AFT SIDE OF FRAME STA 1437 I/B OF LONGERON 3R. REMOVED DAMAGED SHEAR TIE RECEI VED A REPLACEMENT SHEAR TIE, LOCATED, DRILLED AND INSTALLED IAW MD80 SRM 51-10-4 PG 1 AND FIG 3A SHEET 1 AND 51-30-5 PG 12, 13. 2 L 7 2 4F RT A6WE 2007112100056 20071121 00056 WP 2007 11 21 ASAA0782216 1 20071108 A 5321 99365833 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 769-807 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 977AS 53453 CABIN FLOOR PANEL DELAMINATED STA 769 TO STA 807 RBL 22 TO RBL 44. FABRICATED A REPLACEMENT FLOOR PANEL IAW MD80 SRM 53 -05 PAGES 251 THRU 257 AND DAC DRAWINGS S4932106. 2 L 7 2 4F RT A6WE 2007112100058 20071121 00058 WP 2007 11 21 ASAA0782218 1 20071108 A 5321 99365833 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 826-866 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 977AS 53453 CABIN FLOOR PANEL DELAMINATED STA 826 TO STA 866 RBL 22 TP RBL 44. FABRICATED A REPLACEMENT PANEL IAW MD80 SRM 53-05 PA GES 251 THRU 257 AND DAC DRAWING S4932106. 2 L 7 2 4F RT A6WE 2007112100061 20071121 00061 WP 2007 11 21 ASAA0782221 1 20071108 A 5321 99366403 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 887-927 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 977AS 53453 CABIN FLOOR PANEL DELAMINATED STA 887 TO STA 927 LBL 22 TO LBL 44. FABRICATED A REPLACEMENT FLOOR PANEL IAW MD80 SRM 53 -05 PAGES 251 THRU 257 AND DAC DRAWING S4932106. 2 L 7 2 4F RT A6WE 2007112100062 20071121 00062 WP 2007 11 21 ASAA0782223 1 20071108 A 5321 99365833 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 826-866 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 977AS 53453 CABIN FLOOR PANEL DELAMINATED STA 826 TO STA 866 LBL 22 TO LBL 44. FABRICATED A REPLACEMENT FLOOR PANEL IAW MD80 SRM 53 -05 PAGES 251 THRU 257 AND DAC DRAWING S4932106. 2 L 7 2 4F RT A6WE 2007112100063 20071121 00063 WP 2007 11 21 ASAA0782224 1 20071108 A 5321 995792118 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 826-928 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 977AS 53453 CABIN FLOOR PANEL HAT STIFFENER CREASED ON AFT SIDE AND PANEL HAS 1 INCH CRACK IN CENTER AREA STA 826 TO STA 928 RBL 44 TO RBL 54. REMOVED DAMAGED HAT CHANNEL, INSTALLED A REPLACEMENT CHANNEL IAW MD80 SRM 51-10-4 PG 1 & 51-30-2 PG 1. REPA IRED CRACK IAW MD80 SRM 53-01 PG 12 FIG 2. 2 L 7 2 4F RT A6WE 2007112100066 20071121 00066 WP 2007 11 21 ASAA0782229 1 20071108 A 5751 5955401503 SKIN DOUG DC9 DC983 3022083 WP LT AILERON DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 977AS 53453 LEFT AILERON IS DENTED APPROX 2 INCHES FORWARD OF TRIM TAB O/B HINGE LOWER SURFACE. PREPARED DAMAGED AREA IAW MD80 SRM 51-90-0 PG 9, APPLIED LAYER OF MIL C 9084 FIBERGLASS BONDED REPAIR IAW MD80 SRM 51-90-0 PG 44. 2 L 7 2 4F RT A6WE 2007112100068 20071121 00068 NM 2007 11 21 ASAA0752230 1 20071109 A 2410 5910292 COUPLING BOEING 737 737890 1384527 NM NR 2 IDG DEFECTIVE A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 557AS 35176 FOLLOW UP TO FREQUENT NR 2 IDG SERVICING. FOUND IDG PERFECTLY SERVICED TO TOP OF THE BAND. PERFORMED LEAK CHECK NO DEF ECTS. REPLACED SERVICE COUPLING. LEAK CHECKED GOOD. 2 L 7 2 4F RT A16WE 2007112100069 20071121 00069 NM 2007 11 21 NOCA16607 1 20071114 A 3350 BPS73 BATTERY PACK BOEING 767 767324 1385203 NM EMERGENCY LIGHT INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 767NA 27569 EMERGENCY EXIT LIGHT INOP AT 20GH. REPLACED BATTERY PACK PER MM 33-51-07. 2 L 7 2 4F RT A1NM 2007112100070 20071121 00070 NM 2007 11 21 NOCA16707 1 20071113 A 3350 417N5058005 SIGN BOEING 757 75728A 1384976 NM CABIN MALFUNCTIONED A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 756NA 32448 EMERGENCY EXIT SIGN ABOVE R-1 FADING STILL READABLE. REPLACED EMERGENCY EXIT SIGN PER MM 33-51-09. 2 L 7 2 4F RT A2NM 2007112100071 20071121 00071 NM 2007 11 21 KCSA071520 1 20071114 A 5315 FLOORBEAM BOEING 747 747246F 1384850 NM BS 840 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 FWD PIT FLOORBEAM UPPER CHORD DAMAGED AT BS 840, RBL 53. 2 L 7 4 4F RT A20WE 2007112100073 20071121 00073 NM 2007 11 21 ASAA0772232 1 20071110 A 5320 143A75014 CHANNEL BOEING 737 737790 13844CN NM BS 500A-500D CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 648AS 30662 FWD CARGO RT ZEE CHANNEL AT BS 500A 500D RBL 21 CORRODED. ZEE CHANNEL REPLACED. 2 L 7 2 4F RT A16WE 2007112100075 20071121 00075 NM 2007 11 21 ASAA0772235 1 20071108 A 5320 143A750124 CHANNEL BOEING 737 737790 13844CN NM BS 500A CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 648AS 30662 FWD CARGO LT ZEE CHANNEL BS 500 A+6 TO 500 A+10 LBL 21 CORRODED. ZEE CHANNEL REPLACED. 2 L 7 2 4F RT A16WE 2007112100076 20071121 00076 NM 2007 11 21 ASAA0772236 1 20071108 A 5320 143A750124 CHANNEL BOEING 737 737790 13844CN NM BS 480-520D CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 648AS 30662 FWD CARGO LT ZEE CHANNEL BS 500+14 LBL 21 CORRODED. ZEE CHANNEL REPLACED. 2 L 7 2 4F RT A16WE 2007112100080 20071121 00080 2007 11 21 ABXA070367 4 20071109 A 3460 4052500962 FMC BOEING 767 767232 1385132 NM E/E BAY DEFECTIVE A ABXA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 23 744AX 3085 22221 AFTER LIFT OFF AT KIX, GOT LAND TERRAIN WARNING THROUGH 3000 FEET, 50 MILE (APPROX) MAP SHIFT OCCURRED. LOST VOR UPDATI NG - FMC MSG "PURGE UPDATE POS 2" CAME ON, COULD NOT RESET LNAV, RETURNED TO KIX. SWAPPED NR 1 ATC ANTENNA AND NR 1 DME ANTENNA REPLACED NR 1 FMC IAW B767 MM 34-61-01. 2 L 7 2 4F RT A1NM 2007112100085 20071121 00085 NM 2007 11 21 ASAA0772242 1 20071110 A 5347 146 CARGO TRACK BOEING 737 737790 13844CN NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 648AS 30662 AFT CARGO PIT BS 767+6 RBL 14 TIEDOWN TRACK CORRODED. AFT CARGO PIT RT TIEDOWN TRACK AT BS 767+6 RBL 14 REPAIRED IAW EA 5330 02743. 2 L 7 2 4F RT A16WE 2007112100090 20071121 00090 NM 2007 11 21 ASAA0772247 1 20071110 A 5315 146A94014 FLOORBEAM BOEING 737 737790 13844CN NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 648AS 30662 AFT CARGO PIT BS 767+6 LBL 21 TO RBL 21 FLOOR SUPPORT TEE CORRODED. AFT CARGO PIT BS 767+6 LBL 21 TO RBL 21 FLOOR SUPPO RT TEE REPLACED WITH NEW PART IAW B737 700 AMM 25 52 10. 2 L 7 2 4F RT A16WE 2007112100091 20071121 00091 NM 2007 11 21 ASAA0772248 1 20071110 A 5347 146A75011 CARGO TRACK BOEING 737 737790 13844CN NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 648AS 30662 AFT CARGO PIT BS 767+6 LBL 17.24 TIE DOWN TRACK CORRODED. AFT CARGO PIT LT TIEDOWN TRACK AT BS 767+6 LBL 17.24 REPAIRED IAW ASA EA 5330 02743. 2 L 7 2 4F RT A16WE 2007112100092 20071121 00092 NM 2007 11 21 ASAA0772249 1 20071105 A 5320 146A75024 CHANNEL BOEING 737 737790 13844CN NM BS 727-907 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 648AS 30662 AFT CARGO BS 907 TO BS 727 RBL 21 ZEE CHANNEL CORRODED. ZEE CHANNEL REPAIRED IAW B737 700 SRM 53-00-53 REPAIR 5. 2 L 7 2 4F RT A16WE 2007112100093 20071121 00093 NM 2007 11 21 UPS07651160 1 20071113 A 2150 A/C PACK BOEING 767 76734AF 1385212 NM ODOR A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 327UP 27753 INSPECTION TYPE:ETOP HEAVY ODOR OF BURNING RUBBER IN COCKPIT UPON LANDING. FAINT SMELL BEFORE TAKEOFF - PREVIOUS CREW C OMMENT. RAN BOTH ENGINES TO FLIGHT IDLE. ISOLATED LEFT AND RIGHT BLEEDS AND RAN BOTH PACKS TO FULL. COULD NOT DUPLICA TE ODOR, A/C OK FOR CONTINUED SERVICE. 2 L 7 2 4F RT A1NM 2007112100094 20071121 00094 NM 2007 11 21 UPS07651162 1 20071114 A 2150 A/C PACK BOEING 767 76734AF 1385212 NM ODOR A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 01 327UP 27753 INSPECTION TYPE:ETOP MOMENTARY ODOR OF BURNING RUBBER IN COCKPIT WHILE IN DESCENT THROUGH 263000 FT. FLT IDLE, EAI ON A ND BOTH PACKS ON. UPON LEVEL OFF AT 24000 FT ODOR WENT AWAY AND DID NOT RETURN. VERIFIED DURING ENGINE RUNS, NO ODOR D ETECTED. DISCUSSED WITH AMC AND W/CREW, NO DEFECTS NOTED. A/C OK TO CONTINUE. 2 L 7 2 4F RT A1NM 2007112100095 20071121 00095 WP 2007 11 21 UPS07851154 1 20071113 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01-2. OPS CHE CK GOOD. 2 L 7 4 4F RT 4A25 2007112100096 20071121 00096 NM 2007 11 21 UPS07M51136 1 20071029 A 5754 ARB2850505 RIB DOUG MD11 MD11F 3023600 NM NR 16 SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP 48575 INSPECTION TYPE:3C LEFT WING NR 16 SLAT TRACK I/B FIXED L/E RIB IS CRACKED. REMOVED AND REPLACED LEFT WING NR 16 SLAT T RACK I/B FIXED L/E RIB IAW MD-11 SRM 51-33-01. 2 L 7 3 4F RT A22WE 2007112100097 20071121 00097 NM 2007 11 21 UPS07M51139 1 20071029 A 5754 SKIN DOUG MD11 MD11F 3023600 NM NR 14 SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP 48575 INSPECTION TYPE:3C LEFT FIXED L/E SKIN HAS A 12 INCH CRACK AT APPROX 16 INCHES O/B OF NR 14 SLAT TRACK. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER & INTERNAL STRAP IAW MD-11 SRM 57-10-00 FIG 41. 2 L 7 3 4F RT A22WE 2007112100098 20071121 00098 2007 11 21 UPS07M51148 4 20071112 A 2565 SLIDE DOUG MD11 MD11F 3023600 NM R1 DOOR NO TEST A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 279UP 48573 INSPECTION TYPE:N/A R1 SLIDE WILL NOT PRESS TO TEST. DEFERRED IAW MEL 25-61-2 PLACARD INSTALLED. DEF 362353. 2 L 7 3 4F RT A22WE 2007112100099 20071121 00099 NM 2007 11 21 UPS07M51149 1 20071031 A 5754 SKIN DOUG MD11 MD11F 3023600 NM NR 1 SLAT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP 48575 INSPECTION TYPE:3C RIGHT NR 1 SLAT O/B END UPPER T/E IS DAMAGED. TRIMMED DAMAGED AREA. FABRICATED REPAIR FILLER AND DO UBLER AND INSTALLED IAW SAA EA 011-2780-01A1223, UPS RAA ENG FILE NUMBER MD11-27-20025 DATED 11/13/2007 AND FAA FORM 810 0-9 APPROVED. 2 L 7 3 4F RT A22WE 2007112100100 20071121 00100 NM 2007 11 21 UPS07M51157 1 20071113 A 2910 HYDRAULIC SYSTEM DOUG MD11 MD11F 3023600 NM NR 2 LEAKING A IPXA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 01 252UP 48768 THREE AND ONE HALF HOURS AFTER TAKEOFF AT FL310, LOST ALL FLUID IN HYD SYSTEM 2. HYD 3 ELEV OFF ALERT NOT DISPLAYED. R EPLACED RIGHT AND LEFT PUMPS PER MM 29-11-20-4-1 AND CASE DRAIN FILTERS. 2 L 7 3 4F RT A22WE 2007112100101 20071121 00101 NM 2007 11 21 2007UALA04613 1 20071108 A 5330 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 941UA 26676 DENT FOUND ON EDGE OF FORWARD PIT PERIMETER. DAMAGE IS APPROX 29.5 INCHES FROM TOP OF DOOR FRAME CUTOUT FWD EDGE, 3 INC H VERTICAL DEFORMATION OUTWARDS .25 INCH AT PEAK WITH .375 INCH TEAR. DRESSED OUT DAMAGE PER SRM 53-00-01. TREATED , PR IMED AND PAINTED TO MATCH. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112100107 20071121 00107 NM 2007 11 21 2007UALA04619 1 20071108 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1503 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 MAIN CABIN FLOORBEAM, ATTACH VERTICAL CHANNEL CRACKED AT BS 1503 LBL 67. MAJOR REPAIR ACCOMPLISHED. REMOVED & REPLACED CHANNEL LBL 67. 2 L 7 2 4F 4 F RT A1NM E24NE 2007112100109 20071121 00109 NE 2007 11 21 2007UALA04624 2 20071109 A 7200 UNKNOWN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT ENGINE VIBRATION A UALA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 WP 29 769UA 26921 222027 ON STARTING LEFT ENGINE, LOUD RUMBLING NOISE AND HEAVY VIBRATION FELT IN CABIN. RAN NUMEROUS DIAGNOSTIC TESTS ON LT EN GINE. NO ENGINE PROBLEM NOTED. DURING DRY MOTORING, AIR SURGES THROUGH ENG CORE, SIMILAR TO PREVIOUS APU SURGE CONTR OL VALVE FAULT, ACCOMPLISHED NR 2 ENG START. ACCOMPLISHED DUAL ENG START FROM OUTSIDE AIR SOURCE, UNABLE TO DUPLICATE P ROBLEM. ALL OPS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007112100111 20071121 00111 NM 2007 11 21 2007UALA04626 1 20071110 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 303UA 23644 EEL FLOOR LIGHT STRIP INOP AT SEAT 3C (1 LIGHT). REPLACED 1 EA LIGHT STRIP, OP CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112100113 20071121 00113 NM 2007 11 21 2007UALA04628 1 20071111 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 EMERGENCY PATH LIGHTING PULLED OUT FROM FLOOR AT SEAT 1AB. 2 L 7 2 4F 4 F RT A2NM E17NE 2007112100114 20071121 00114 NM 2007 11 21 2007UALA04629 1 20071111 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 579UA 26697 EMERGENCY LIGHT STRIP LOOSE AT 12C. 2 L 7 2 4F 4 F RT A2NM E17NE 2007112100118 20071121 00118 NM 2007 11 21 2007UALA04637 1 20071111 A 2432 CHARGER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE MAIN BATTERY FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 786UA 26938 AFTER BLOCKING OUT -MAIN BATTERY DISCHARGE- ADVISORY MESSAGE DISPLAY, WITH A -12 AMP DISCHARGE ON MAIN BATTERY. CYCLED STBY POWER SW ON OVERHEAD AND DISCHARGE DECREASED TO -2 AMP WITH 24 VDC ON MAIN BATTERY. REPLACED MAIN BATTERY CHARGER, OP CHECKED OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007112100119 20071121 00119 NM 2007 11 21 2007UALA04639 1 20071110 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 AFT CREW REST CEILING EMERGENCY LIGHT IS INOP. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112100120 20071121 00120 NM 2007 11 21 2007UALA04640 1 20071110 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 DOOR 5 LEFT SILL (2EA) AND DOOR 2R SILL EMERGENCY LIGHTS ARE INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112100122 20071121 00122 NM 2007 11 21 2007UALA04645 1 20071111 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 181UA 69436 25278 EXTERNAL FUSELAGE IS DENTED. INSTALLED EXTERNAL DOUBLER REF SRM 53-00-01 FIG 201. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112100123 20071121 00123 NM 2007 11 21 2007UALA04646 1 20071111 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 DOOR 4L DOOR MOUNTED EMERGENCY EXIT LIGHT DIM. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112100126 20071121 00126 NM 2007 11 21 2007UALA04650 1 20071111 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 ALL SEAT EEL INOP LEFT B-ZONE. SECURED LOOSE CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112100131 20071121 00131 SO 2007 11 21 C2XA07RI098 1 20071111 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13975 1145163 FLT 3035 - EWR - CREW REPORTED 3 AFT EMERGENCY LIGHT STRIPS INOPERATIVE. EWR MX FOUND BROKEN WIRE AT EMERGENCY LIGHT NR 8. ME REPAIRED WIRING AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007111500183 20071115 00183 NM 2007 11 15 USAA920071097 1 20071021 A 5754 SKIN BOEING BOEING 737 7373B7 1384580 NM NR 2 SLAT DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 0294 23384 MCN - MAJOR REPAIR - C20 CHECK - LEFT WING NR 2 SLAT WEDGE ASSEMBLY HAS AREA OF DISBOND, SS 124.53 - SS 129.03. REPAIRE D LEFT WING NR 2 SLAT WEDGE ASSEMBLY, SS 124.53 - SS 129.03 IAW B737 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 2007111500186 20071115 00186 NM 2007 11 15 2007UALA04248 1 20071015 A 3830 158000122 TOILET BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LAVATORY INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 FOUR OUT OF EIGHT LAVS INOP THE 4 GOOD LAVS FLUSH CLEAR FLUID. *S/D* AFTER 10 DAYS & CONSIDERABLE TROUBLESHOOTING & TA NK SERVICING, DETERMINED LEFT AFT TOILET HAD VALVE PROBLEM WITH CONTINUOUS FLUSHING PROBLEM. REPLACED TOILET ASSEMBLY. LAV SYSTEM CHECKED OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007111500202 20071115 00202 NM 2007 11 15 2007UALA04596 1 20071106 A 2913 3268792 PUMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE HYD SYSTEM LEAKING A UALA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 WP 29 651UA 25389 CTR ADP HAS HYDRAULIC LEAK. REPLACED AIR DRIVEN PUMP PER MM29-11-03. DURING OPS CHECK OF ADP FOUND PRESSURE REGULATOR V ALVE FAILED. OPS CHECK NORMAL. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007111500211 20071115 00211 NM 2007 11 15 2007UALA04607 1 20071107 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SEAT 26HJ MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 665UA 29237 EEL STRIP AT 26HJ MISSING. REPLACED LIGHT STRIP. 2 L 7 2 4F 4 F RT A1NM E24NE 2007111500213 20071115 00213 NE 2007 11 15 2007UALA04609 2 20071108 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 1 FLAMED OUT A UALA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 WP 29 664UA 29236 724637 NR 1 ENGINE FLAMEOUT IN FLIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007111900005 20071119 00005 NM 2007 11 19 SWAA075620 1 20071107 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 277 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007111900020 20071119 00020 NM 2007 11 19 SWAA075593 1 20071107 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 807 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007111900027 20071119 00027 NM 2007 11 19 SWAA075601 1 20071107 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM ROW 17 DEF WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 17 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007111900042 20071119 00042 NM 2007 11 19 SWAA075609 1 20071107 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM BS 406 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 406, RBL 3. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007111900057 20071119 00057 NM 2007 11 19 CALA0700663 1 20070829 A 5330 147A31103 SKIN BOEING 737 737824 13844BZ NM BS 907-927 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12221 28930 CORROSION WAS FOUND IN FUSELAGE SKIN AT LT AFT FUSELAGE AT VACUUM WASTE EXHAUST, STA 907-927, S21L TO S22L DURING A WALK AROUND. THE SKIN WAS REPAIRED IAW ECRA 5330-03715 AND A DIP WAS INITIATED TO PERFORM A PERMANENT REPAIR WITHIN 12 MONTH S. 2 L 7 2 4F RT A16WE 2007111900060 20071119 00060 NM 2007 11 19 CALA0700666 1 20071018 A 5330 UNK SKIN BOEING 767 767224 1385170 NM BS 1132 DAMAGED A CALA O OTHER O OTHER NR NOT REPORTED 1 SW 27 76153 30432 INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN AT STA 1132, S8R. THE SKIN WAS REPAIRED IAW ECRA 5330-03744. 2 L 7 2 4F RT A1NM 2007111900075 20071119 00075 EA 2007 11 19 TRAX200701686 1 20071105 A 5210 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 883AS 7504 DOUBLER INSIDE PAX DOOR AT FS 333 IS CRACKED. REMOVED CRACKED UN-SERVICEABLE DOUBLER FROM INSIDE PAX DOOR AT FS 333. L OCATED NEW SERVICEABLE DOUBLER P/N 601R318094-2 AT PAX DOOR FS 355 IAW CRJ 200 SRM 51-42-06, 51-42-10 AND 51-42-21. 1421 2 2 L 7 2 4F RT A21EA 2007111900079 20071119 00079 EA 2007 11 19 TRAX200701692 1 20071106 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 883AS 7504 AAR - FS 484 I/B OF LBL 36 ANGLE IS CRACKED. 2 L 7 2 4F RT A21EA 2007111900080 20071119 00080 EA 2007 11 19 TRAX200701695 1 20071106 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 880AS 7606 GLOW IN THE DARK "EXIT" STICKER ON AIR STAIR DOOR STEP IS MISSING FIRST THREE LETTERS. 2 L 7 2 4F RT A21EA 2007111900081 20071119 00081 EA 2007 11 19 TRAX200701696 1 20071106 A 5240 LATCH CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 920EV 7810 SERVICE DOOR OUTER LATCH INOP. 2 L 7 2 4F RT A21EA 2007111900092 20071119 00092 NM 2007 11 19 USAA920071101 1 20071025 A 5320 6517684634 INTERCOSTAL BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED INTERCOSTAL, BS 294.5, S16L. REPLACED INTERCOSTAL, BS 294.5, S16L IAW BOEING DRAWING 65-17684-634. 2 L 7 2 4F RT A16WE 2007111900095 20071119 00095 NM 2007 11 19 USAA920071104 1 20071025 A 5312 651758243 BULKHEAD BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FORWARD PRESSURE BULKHEAD WEB, BS 178, LBL 17, WL 224. REPAIRED FORWARD PRESS URE BULKHEAD WEB, BS 178, LBL 17, WL 224 IAW B737 SRM 53-10-08-2R12. 2 L 7 2 4F RT A16WE 2007111900105 20071119 00105 NM 2007 11 19 SWAA075641 1 20071108 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 727C S14R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 727C, STR 14R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007111900130 20071119 00130 WP 2007 11 19 UPS07851118 1 20071024 A 5320 MOUNT DOUG DC8 DC873F 302199F WP MLG DOOR SWITCH ELONGATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 RIGHT MAIN GEAR DOOR SWITCH MOUNT HOLES ELONGATED. FABBED AND INSTALLED DOUBLER ON RIGHT MAIN GEAR D OOR SWITCH MOUNT IAW DWG 5653490 AND SRM 51-0-20-D, 51-1-8. 2 L 7 4 4F RT 4A25 2007111900131 20071119 00131 NM 2007 11 19 KCSA071515 1 20071112 A 5347 SEAT TRACK BOEING 747 747246F 1384850 NM BS 1895 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 MAIN DECK SEAT TRACK CORRODED AT BS 1895, LBL 11. 2 L 7 4 4F RT A20WE 2007111900134 20071119 00134 NM 2007 11 19 HNAA0700265 1 20071110 A 3397 TB146D PIN DHAV DHC8 DHC8102 2809003 NM CONNECTOR LOOSE A HNAA O OTHER O OTHER CL CLIMB 1 EA 07 810EX 308 EMERGENCY LIGHTS COME ON DURING CLIMBOUT FOR 10 SECONDS. FOUND LOOSE PIN AT TB14-6D, REMOVED AND REPLACED PIN ON WIRE 3 352-2A20 OPS CHECK GOOD. SUBJECT TO EVALUATION FLIGHT. EVALUATION FLIGHT WAS SATISFACTORY. 2 H 7 2 4T RT A13NM 2007111900139 20071119 00139 NM 2007 11 19 SWAA075642 1 20071110 A 3350 W4142001220 WIRE BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 204WN 29855 EEPLS INOP BETWEEN ROW 3 ABC AND 6 ABC. FOUND LOOSE WIRE. SECURED WIRE PER MM. 2 L 7 2 4F RT A16WE 2007111900145 20071119 00145 NM 2007 11 19 SWAA075662 1 20071111 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM BS 430 S28L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, STR 28L. REPAIRED SK IN PER SWA EA. 2 L 7 2 4F RT A16WE 2007111900156 20071119 00156 NM 2007 11 19 SWAA075657 1 20071111 A 5330 6545766 SKIN BOEING 737 7373A4 1384585 NM BS 517D S12R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 517D, STR 12R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007111900169 20071119 00169 NM 2007 11 19 CALA0700670 1 20071111 A 5330 6545775 SKIN BOEING 737 7373T0 1384582 NM BS 727C-727E CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17326 23456 INSPECTION FOUND A 4.7 INCH CRACK IN FUSELAGE SKIN AT EMERGENCY LIGHT, STA 727C TO 727E, S21R TO S24R. THE SKIN WAS REP AIRED IAW ECRA 5331-01362. 2 L 7 2 4F RT A16WE 2007111900170 20071119 00170 NM 2007 11 19 CALA0700671 1 20071111 A 5314 65C385022 KEELBEAM BOEING 737 7373T0 1384582 NM BS 540 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND A .5 INCH CRACK IN KEEL BEAM IN RIGHT A/C BAY AT STA 540. THE KEEL BEAM SECTION WAS REMOVED AND REPLAC ED IAW SRM 53-60-12, FIGURE 201, PAGE 201. 2 L 7 2 4F RT A16WE 2007111900178 20071119 00178 SO 2007 11 19 LR7A07124 1 20071106 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FS 477 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 618 4606 DURING SCHEDULED B-2 CHECK PER JOB CARD HB3200 FOUND LT BHD WEB CRACKED AT FS 477 WL 182 LBL 72. REPAIR ACCOMPLISHED IA W SMP583 FIG 53-40-10. 2 H 7 4 4T A1SO 2007111900193 20071119 00193 EA 2007 11 19 COMA0770068 1 20071112 A 5730 SKIN CNDAIR CL600 CL6002C10 1390015 EA WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 391CA 10108 WORKING RIVETS AND DAMAGED TOP WING SKIN O/B OF LEFT MULTI-FUNCTION SPOILERS. REPAIRED DAMAGED AREA IAW REO 670-51-73-0 02 AND EA 70-5557-01885. 2 L 7 2 4F RT A21EA 2007111900199 20071119 00199 WP 2007 11 19 DXTA200702586 2 20071101 A 7200 ENGINE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP LEFT FOD E DXTA E ENGINE SHUTDOWN C F.O.D. TX TAXI/GRND HDL 1 GL 07 858QS 258691 UPON START-UP, LT ENGINE BEGAN TO VIBRATE AND SHUDDER. LT ENGINE START ABORTED. REMOVED RAG FROM FAN. CLEANED FAN BLADE S AND INLET OF TOWEL DEBRIS. A VISUAL INSPECTION OF INLET/BYPASS STATOR AND FAN ASSY. NO DAMAGE VISIBLE. BOROSCOPE OF 1S T STAGE L.P.C. ROTOR & STATOR SHOWED NO DAMAGE. ALL WORK DONE IAW HONEYWELL 731 LMM 72-00-00 72-30-04 72-70-03. RAN ENGI NE OPS CHECKED GOOD. IAW HONEYWELL 731 LMM 72-00-00 2 L 7 2 4F 4 F RT A3EU E6WE 2007111900200 20071119 00200 CE 2007 11 19 DXTA200702587 1 20071101 A 3243 9536718 MASTER CYLINDER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE RT BRAKES BYPASSING E DXTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 394QS 711 5600394 CO-PILOTS RT BRAKE PEDAL NEEDS TO BE DEFLECTED OR PUSHED APPROXIMATELY 30 PERCENT MORE TRAVEL THAN LT PEDAL. REMOVED AN D REPLACED CO-PILOT'S MASTER CYLINDERS AND SOFT LINES IAW CE560 M/M 32-42-02, OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F 4 F RT A22CE E25EA 2007111900201 20071119 00201 NM 2007 11 19 DXTA200702588 1 20071101 A 2435 23291006 STARTER GEN GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE RT ENGINE INOPERATIVE E DXTA C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 GL 07 718QS 950 950 136 RT GENERATOR FAILED AFTER TAKEOFF POWER , R/T GEN WOULD NOT STAY RESET NOR HOLD AMP LOAD NOR VOLTS, TO ABORTED. REMO VED AND REPLACED RH STARTER GEN PER G200 MM 24-30-06. OPS CHECK GOOD PER G200 MM 24-30-00 2 L 7 2 4F 4 F RT A53NM E35NE 2007111900202 20071119 00202 CE 2007 11 19 AMWA88211 1 20071026 A 5270 1013840841179 ANNUNCIATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA COCKPIT FALSE INDICATION A AMWA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 07 163YV 26272 UE163 CABIN DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. AIRCRAFT LANDED AND MAINTENANCE VERIFIED DOOR WAS SECURED AND PROBLEM WAS A FAULTY ANNUNCIATOR. ANNUNCIATOR PLACED IN DEFERRED STATUS. REMAINS DEFERRED AS OF 10/29/07. 2 L 7 2 4T 3 T RT A24CE E2NE 2007111900203 20071119 00203 EU 2007 11 19 TRAX200701617 1 20071029 A 5311 FRAME AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 FR 38 BETWEEN STR 20-21L CORRODED. REMOVED CORROSION ON FR38 BTW STR 20-21L AS PER SRM 51-21-42 AND WITHIN LIMITS AS PE R SRM 53-61-00 MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.003 WITHIN LIMITS AS PER SRM: 53-61-00 FIG 301. 2 H 7 2 4T RT 2007111900204 20071119 00204 EU 2007 11 19 TRAX200701618 1 20071029 A 5315 FLOORBEAM AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 FLOORBEAM 38 CORRODED. FLOORBEAM 38 CORROSION REMOVED IAW SRM 51-21-42 AND IT IS WITHIN AS PER SRM 53-61-00 FIG 301. MAT ERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.003 WITHIN LIMITS AS PER SRM: 53-61-00 FIG 301. 2 H 7 2 4T RT 2007111900205 20071119 00205 EU 2007 11 19 TRAX200701620 1 20071029 A 5315 FLOORBEAM AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 FLOORBEAM 40 CORRODED. FLOORBEAM 40 CORROSION REMOVED IAW SRM 51-21-42 AND IT ISW WITHIN LIMIT AS PER SRM 53-61-00 FIG 301. MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.002 WITHIN LIMITS AS PER SRM: SRM 53-61-00 FIG 301. 2 H 7 2 4T RT 2007111900206 20071119 00206 EU 2007 11 19 TRAX200701621 1 20071029 A 5313 STRINGER SPLICE AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 SPLICE STR 17L BETWEEN FR 38 & 39 CORRODED. REMOVED CORROSION ON SPLICE LOCATED ON STR 17L BTW FR 38939 AS PER SRM 51-2 1-42 AND IS WITHIN LIMIT AS PER SRM 53-61-00 MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.001 WITHIN LIMITS AS PER SR M: SRM 53-61-00 FIG 301. 2 H 7 2 4T RT 2007111900207 20071119 00207 EU 2007 11 19 TRAX200701622 1 20071029 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 RIGHT SEAT TRACK BETWEEN FR 41 & 44 CORRODED. RT SEAT TRACK BTW FR 41-44 CORROSION REMOVED IAW SRM 51-21-42 AND IT IS W ITHIN LIMIT AS PER SRM 3-00-00 FIG 304 MATERIAL THICKNESS: 0.083 MATERIAL REMOVED: 0.007 WITHIN LIMITS AS PER SRM: 53-0 0-00 FIG 304. 2 H 7 2 4T RT 2007112000013 20071120 00013 EU 2007 11 20 2007UALA04574 1 20071104 A 2700 3945128102 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ELAC FAULTY A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 444UA 824 ELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. F-CTL CREW COMMENTS: IN CLIMB SLIGHT BUMP, THEN F-CLT ELAC1 FAULT. CYCLED SWITCH ONCE PER ECAM. NO HELP. FOUND ELAC1 FAULTY/BAD CPU. REPLACED ELAC1 COMPUTER - CHECKS OK, NO REPEATS SINCE O RIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112000026 20071120 00026 NM 2007 11 20 2007UALA04578 1 20071105 A 2700 3945128102 COMPUTER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 ELAC MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 804UA 759 ELAC 2 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. PERFORMED RESET AND OPERATIONAL TEST OF ELAC2. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112000027 20071120 00027 NM 2007 11 20 2007UALA04580 1 20071105 A 3350 58791 JUMPER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 310UA 23671 EMERGENCY ESCAPE PATH LIGHTS INOP FROM ROW 12 TO ROW 16. REPLACED POWER CABLE JUMPER 2 L 7 2 4F 4 F RT A16WE E21EU 2007112000029 20071120 00029 NM 2007 11 20 2007UALA04610 1 20071108 A 3510 OXYGEN MASK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FIRST OFFICER'S MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 827UA 1022 FIRST OFFICER'S O2 MASK LEAKING. FOUND CREW O2 MASK (FO) WAS NOT PROPERLY STOWED. RESTOWED FO MASK- NO LEAKING- SERVICE D CREW O2 SYSTEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112000030 20071120 00030 EU 2007 11 20 07FDEA04752 1 20071108 A 2133 OUTFLOW VALVE AIRBUS 310 A310203 3930313 EU CABIN PRESSURE MALFUNCTIONED A FDEA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 SO 25 427FE 362 ON TAKEOFF, SHORTLY AFTER GEAR RETRACTION ECAM SHOWED NO PRESSURIZATION. PRESS PAGE SHOWED BOTH NR 2 FWD AND AFT OUTFLO W VALVES FULL OPEN AND CABIN V/S PEGGED IN CLIMB. TURNED OFF NR 2 REG NO EFFECT. TRIED TURNING OFF BOTH REG AND USING MANUAL PRESS WITH V/S CONTROL, NO EFFECT. RETURNED TO KIAH. PERFORMED ADJ. AND TEST PER M/M 21-31-00-5 01, ALL SYSTE M TEST GOOD. ALSO CHECKED WIRING, ALL CHECKED GOOD. 2 L 7 2 4F RT A35EU 2007112000039 20071120 00039 EU 2007 11 20 2007UALA04621 1 20071110 A 3350 32145410 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 423UA 504 EPSU FWD L MESSAGE, BATTERY PACK FAILS TEST. REPLACED BATTERY PACK. FUNCTIONS FINE FOR FURTHER FLIGHT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112000040 20071120 00040 EU 2007 11 20 2007UALA04622 1 20071110 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 426UA 510 EMERGENCY LIGHT TEST FAILS WITH ASSOC MSG 'INT LOADS EMER R' AND 'EXT LOADS EMER R'. REPLACED POWER SUPPLY AND BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112000041 20071120 00041 NM 2007 11 20 2007UALA04630 1 20071109 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LAVATORY INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 LEFT MID LAV EEL LIGHT BAR IS INOPERATIVE. REPLACED LIGHT BAR. 2 L 7 2 4F 4 F RT A1NM E24NE 2007112000042 20071120 00042 NM 2007 11 20 2007UALA04632 1 20071111 A 3350 60243 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE AFT GALLEY IMPROPER PART A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 653UA 25391 AFT GALLEY (G4) SHORT LIGHT BAR IS WRONG TYPE. INSTALLED CORRECT PART, OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007112000043 20071120 00043 NM 2007 11 20 2007UALA04635 1 20071111 A 3350 20131A BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 EMERGENCY LIGHTING ON LEFT SIDE OF ECONOMY FLASHES ON AND OFF DURING FLIGHT. REPLACED BATTERY SUPPLY AT 17A. OPS CHECK ED OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007112100004 20071121 00004 NM 2007 11 21 KCSA071516 1 20071112 A 5330 SKIN BOEING 747 747246F 1384850 NM BS 1800 S37R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 STA 1800 AT STR 37R SKIN DAMAGED. 2 L 7 4 4F RT A20WE 2007112100005 20071121 00005 NM 2007 11 21 KCSA071517 1 20071112 A 5330 SKIN BOEING 747 747246F 1384850 NM BS 2190 S44-45L BULGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 STA 2190 STR 44L TO STR 45L PILLOWING SKIN AROUND FASTENERS. 2 L 7 4 4F RT A20WE 2007112100006 20071121 00006 NM 2007 11 21 KCSA071518 1 20071112 A 5347 SEAT TRACK BOEING 747 747246F 1384850 NM BS 2155 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 STA 2155 LBL 11 SEAT TRACK DAMAGED AT CENTER GUIDE LOCKDOWN PIN HOLE. 2 L 7 4 4F RT A20WE 2007112100007 20071121 00007 NM 2007 11 21 KCSA071519 1 20071112 A 5347 SEAT TRACK BOEING 747 747246F 1384850 NM BS 2095 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 STA 2095 LBL 11 SEAT TRACK DAMAGED AT CENTER GUIDE LOCKDOWN PIN HOLE. 2 L 7 4 4F RT A20WE 2007112100008 20071121 00008 NM 2007 11 21 WRLA2007121 1 20071109 A 5714 SKIN DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE RT CENTER WING CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING C-CHECK INSPECTION CORROSION FOUND ON RIGHT CENTER WING TANK UPPER SKIN AT XCW=110S1. ACCOMPLISHED ENGINEERING I NSTRUCTION NO.W2007A57B-668 REV.00, REPAIR CORROSION ON CENTER WING UPPER SKIN UPPER SURFACE AT XCW=110 S1. REF EGAT NRC U05027. 2 L 7 3 4F 4 F RT A22WE E24NE 2007112100009 20071121 00009 NM 2007 11 21 WRLA2007120 1 20071109 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING C-CHECK INSPECTION FOUND CORROSION AFT CABIN FLOOR CURVED SEAT TRACK AT STA Y=2007 X =107.25. REF EGAT NRC U05001 . REPLACED THE DAMAGED AREA PER MD11 SRM 53-70-00 VOL.I FIGURE 8 REV.40. REF EGAT NRC U05028. 2 L 7 3 4F 4 F RT A22WE E24NE 2007112100010 20071121 00010 NM 2007 11 21 CALA0700675 1 20071112 A 5414 311A1450 SKIN BOEING 737 7373T0 1384582 NM NR 2 NACELLE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND A .5 INCH CRACK IN NR 2 PYLON ACCESS PANEL 5824 CUTOUT ON UPPER FORWARD CORNER, NAC STA 258. THE CRACK WAS STOP DRILLED AND A PERMANENT REPAIR WAS INSTALLED IAW ECRA 5430-01204. 2 L 7 2 4F RT A16WE 2007112100011 20071121 00011 NM 2007 11 21 CALA0700676 1 20071112 A 5311 6545801512 FRAME BOEING 737 7373T0 1384582 NM BS 227.8 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND FRAME AND SUPPORTS CORRODED AT STA 227.8, LBL 5.7 TO RBL 5.7, S28L. THE AREA WAS REPAIRED IAW ECRA 531 1-01373. 2 L 7 2 4F RT A16WE 2007112100020 20071121 00020 NM 2007 11 21 CALA0700687 1 20071112 A 5315 BAC1505100849 FLOORBEAM BOEING 737 737524 1384721 NM BS 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 52616 27329 INSPECTION FOUND LIGHT SURFACE CORROSION AROUND FASTENER HOLES ALONG FLOORBEAM AT STA 986.5, LBL 55 TO RBL 55. 2 L 7 2 4F RT A16WE 2007112100026 20071121 00026 SO 2007 11 21 C2XA07TY068 1 20071113 A 3222 STRUT EMB 145 EMB145LR 3260212 SO NLG UNDERSERVICED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16981 145208 L/G AIR GROUND FAIL & ENG 1, 2 REV DISAGREE AFTER T/O. SERVICED NLG STRUT IAW EMB 145 MM 32-20-01, AIRCRAFT RELEASED AN D RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007112100028 20071121 00028 NM 2007 11 21 SB07098 1 20071109 A 2611 PU90461R3 SMOKE DETECTOR BOEING 737 7374B7 1384702 NM AFT RIGHT LAV INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 PHL - PILOT REPORTED THE AFT RIGHT LAVATORY SMOKE DETECTOR WAS INOPERATIVE AS GREEN LIGHT WAS EXTINGUISHED. MAINTENANCE REMOVED AND REPLACED AFT RIGHT LAVATORY SMOKE DETECTOR. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A16WE 2007112100041 20071121 00041 NM 2007 11 21 USAA920071119 1 20071004 A 5754 SKIN BOEING 737 7373G7 1384595 NM NR 5 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, RIGHT WING NR 5 SLAT TRAILING EDGE OUTBOARD END DELAMINATED. REPLACED RIGHT WING NR 5 SLAT IAW B737 AMM 27-81-00. 2 L 7 2 4F RT A16WE 2007112100049 20071121 00049 NM 2007 11 21 USAA920071129 1 20071006 A 5230 6546921528A DOOR FRAME BOEING 737 7373G7 1384595 NM ZONE 800 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 CLT - MAJOR REPAIR - C20 CHECK, FORWARD CARGO DOOR FORWARD LOWER FRAME CRACKED BETWEEN THE LOWER 2 CROSS BEAMS. REPLACE D FORWARD CARGO DOOR IAW 737 MM 52-31-00-404-022. 2 L 7 2 4F RT A16WE 2007112100060 20071121 00060 WP 2007 11 21 ASAA0782220 1 20071108 A 5321 99365859 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 927-1003 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 977AS 53453 CABIN FLOOR PANEL DELAMINATED STA 927 TO STA 1003 LBL 22 TO LBL 44. FABRICATED A REPLACEMENT FLOOR PANEL IAW MD 80 SRM 53-05 PAGES 251 THRU 257 AND DAC DRAWING S4932106. 2 L 7 2 4F RT A6WE 2007112100065 20071121 00065 WP 2007 11 21 ASAA0782226 1 20071109 A 5321 99366405 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 866-887 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 977AS 53453 CABIN FLOOR PANEL DELAMINATED AT STA 866 TO STA 887 RBL 22 TO RBL 44. FABRICATED A REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05 PAGES 251 THRU 257 AND DAC DRAWING S4932106. 2 L 7 2 4F RT A6WE 2007112100067 20071121 00067 NM 2007 11 21 ASAA0752231 1 20071112 A 2160 32149721 MODULATOR BOEING 737 737890 1384527 NM TRIM VALVE FAULTY A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 587AS 35684 MASTER CAUTION ON RECALL FOR ZONE TEMP CABIN. NR 2 FLT DECK TRIM VALVE FAULTED ON BITE TEST. REPLACED NR 2 CONTROL CAB IN TRIM AIR VALVE. OPS NORMAL. 2 L 7 2 4F RT A16WE 2007112100072 20071121 00072 NM 2007 11 21 KCSA071521 1 20071114 A 5311 FRAME BOEING 747 747246F 1384850 NM BS 1900 S12R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 FUSELAGE FRAME I/B FLANGE DAMAGED AT BS 1900, STR-12R. 2 L 7 4 4F RT A20WE 2007112100074 20071121 00074 NM 2007 11 21 ASAA0772234 1 20071108 A 5320 143A750124 CHANNEL BOEING 737 737790 13844CN NM BS 495-520D CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 648AS 30662 FWD CARGO LT ZEE CHANNEL BS 500C + 10 TO 500D LBL 21.80 CORRODED. ZEE CHANNEL REPLACED. 2 L 7 2 4F RT A16WE 2007112100084 20071121 00084 NM 2007 11 21 ASAA0772241 1 20071105 A 5320 146A81279 SHIELD BOEING 737 737790 13844CN NM BS 792-767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 648AS 30662 AFT CARGO PIT BS 792 TO BS 767 RBL 21 SHIELD CORRODED ON TOP AND BOTTOM SURFACES. REPLACED SHIELD WITH MADE REPAIR PART AT AFT CARGO PIT BS 792 TO BS 767 AND RBL 21 IAW B737 700 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007112100087 20071121 00087 NM 2007 11 21 ASAA0772244 1 20071110 A 5320 146A75032 CHANNEL BOEING 737 737790 13844CN NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 648AS 30662 AFT CARGO PIT BS 767+6 RBL 3 CHANNEL CORRODED. AFT CARGO PIT FLOOR CHANNEL AT BS 767+6 RBL 3 REPAIRED IAW EA 5330 02743 . 2 L 7 2 4F RT A16WE 2007112100088 20071121 00088 NM 2007 11 21 ASAA0772245 1 20071110 A 5320 146A75031 CHANNEL BOEING 737 737790 13844CN NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 648AS 30662 AFT CARGO PIT BS 767+6 LBL 3 CHANNEL CORRODED. AFT CARGO PIT FLOOR CHANNEL AT BS 767+6 LBL 3 REPAIRED IAW EA 5330 02743 . 2 L 7 2 4F RT A16WE 2007112100102 20071121 00102 NM 2007 11 21 2007UALA04614 1 20071108 A 3397 58791 FEEDER CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 302UA 23643 AFT CABIN EEL LIGHTS INOP. REPLACED POWER CABLE JUMPER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112100104 20071121 00104 NM 2007 11 21 2007UALA04616 1 20071108 A 5512 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZONTAL STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 306UA 23667 RIGHT HORIZONTAL STAB LOWER SKIN 63 INCHES FROM I/B EDGE 1 INCH FWD OF AFT SPAR CRACKED. REMOVED DAMAGE. FABRICATED AND INSTALLED EXTERNAL DOUBLER REPAIR. REFERENCE MM55-10-94 PG 801-806. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112100105 20071121 00105 2007 11 21 2007UALA04617 4 20071109 A 3497 CONNECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU ADI BURNED A UALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 305UA 23666 F/O ADI BENCH CONNECTOR D2425 PIN 7 IN BURNED. REPLACED EADI AND BENCH CONNECTOR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112100108 20071121 00108 NM 2007 11 21 2007UALA04623 1 20071110 A 3010 VALVE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE ANTI-ICE SYSTEM MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 219UA 30551 FLIGHT DIVERTED DUE TO A WING ANTI-ICE PROBLEM THAT DEVELOPED EN ROUTE AND ASSOCIATED NON-ICING RESTRICTION WHICH PRECLU DED LANDING AT PLANNED DESTINATION. AFTER TROUBLESHOOTING FOUND BAD WING ANTI-ICE VALVE. SUSPECT DEBRIS PREVENTED FULL VALVE OPERATION. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007112100112 20071121 00112 NM 2007 11 21 2007UALA04627 1 20071111 A 3350 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 506UA 24627 DOOR 3L OUTSIDE EMERGENCY EXIT LIGHT INOP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007112100117 20071121 00117 NM 2007 11 21 2007UALA04634 1 20071110 A 2897 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT WING ARCED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 LEFT WING O/B SURGE TANK WIRES HAS SIGNS OF ARCING AT TERMINAL BLOCK, HARDWARE RUSTED O/B SIDE OF RIB 31. REPLACED LEVE L SENSOR AND TERMINAL BLOCK. AC OK FOR SERVICE 2 L 7 2 4F 4 F RT A1NM E24NE 2007112100125 20071121 00125 NM 2007 11 21 2007UALA04649 1 20071111 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 WALL EELS INOP AFT OF DR1L, FWD OF LAV 104 AND ON LT SIDE & AFT OF LAV 110 ARE INOPERATIVE. SECURED LOOSE CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112100128 20071121 00128 NE 2007 11 21 2007UALA04653 2 20071109 A 7200 DRIVE ASSY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 1 ENGINE FAILED A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 673UA 29241 727574 REPORTS OF SPARKS COMING FROM NR 1 ENGINE ON START. NR 1 ENGINE DAMAGED EXTENSIVELY FROM STARTER DISINTEGRATION. REPLAC ED STARTER. STARTER DRIVE SPLINE IN GEARBOX SHEARED. REPLACED NR 1 ENGINE. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007112100129 20071121 00129 NM 2007 11 21 2007UALA04657 1 20071111 A 3500 OXYGEN BOTTLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 803UA 748 THE O2 BOTTLE AT 24C LOW. REPLACED THE LONG O2 BOTTLE UNDER SEAT 24C WITH A NEW ONE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112100133 20071121 00133 NM 2007 11 21 WRLA2007126 1 20071107 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING C-CHECK INSPECTION CORROSION FOUND ON AFT FUSELAGE FLOOR SUPPORT AT STA Y=1990 X=27.5. REPLACED DAMAGE SUPPORT P ER MD11 SRM VOL.1 51-31-01 REV.40 REF EGAT NRC U05024. 2 L 7 3 4F 4 F RT A22WE E24NE 2008010400095 20080104 00095 NM 2008 1 4 CALA0700754 1 20071210 A 5311 6546532 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 FUSELAGE FRAME CRACKED STA480 B/W STR 8/9 RT. REPAIRED PER EA5310-04498. 2 L 7 2 4F RT A16WE 2007112100139 20071121 00139 NM 2007 11 21 USAA920071134 1 20071113 A 5330 6545775 SKIN BOEING 737 7374B7 1384702 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - MAJOR REPAIR - CRACKED FUSELAGE SKIN, BS 727E, S24R. REPAIRED FUSELAGE SKIN, BS 727E, S24R IAW USAIRWAYS EA 10002 5. 2 L 7 2 4F RT A16WE 2007112100141 20071121 00141 NM 2007 11 21 USAA920071137 1 20071019 A 5743 654948823 ATTACH FITTING BOEING 737 7373B7 1384580 NM ZONE 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK, CRACKED LEFT WING LANDING GEAR BEAM ATTACH FITTING, WS 224.14. REPAIRED LEFT WING LANDI NG GEAR BEAM ATTACH FITTING, WS 224.14 IAW EA 98986. 2 L 7 2 4F RT A16WE 2007112100149 20071121 00149 NM 2007 11 21 SWAA075671 1 20071113 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 235WN 34630 EEPLS LENS LOOSE AT ROW 3 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007112100151 20071121 00151 NM 2007 11 21 SWAA075700 1 20071113 A 5414 310A1050 SKIN BOEING 737 7373H4 1384600 NM LT NACELLE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED SPV CHECK, FOUND NR 1 ENGINE UPPER PYLON T-CROWN CRACKED. REPAIRED PYLON PER ER. 2 L 7 2 4F RT A16WE 2007112100154 20071121 00154 NM 2007 11 21 SWAA075687 1 20071113 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM BS 380 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007112100155 20071121 00155 NM 2007 11 21 SWAA075688 1 20071113 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 486 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 486, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007112100157 20071121 00157 NM 2007 11 21 SWAA075676 1 20071113 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 455WN 32462 DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007112100158 20071121 00158 2007 11 21 SWAA075689 4 20071111 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 480WN 33998 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007112100159 20071121 00159 NM 2007 11 21 SWAA075677 1 20071113 A 3350 MS155721 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 490WN 32476 DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007112100161 20071121 00161 NM 2007 11 21 SWAA075679 1 20071113 A 5754 65C26601 SKIN BOEING 737 7375H4 138449D NM NR 1 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED C3 CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT LOWER T/E. REPAIRED SLAT PER SWA EA. 2 L 7 2 4F RT A16WE 2007112100163 20071121 00163 2007 11 21 SWAA075681 4 20071113 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 635SW 27708 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007112100165 20071121 00165 NM 2007 11 21 SWAA075684 1 20071113 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM BS 360 S23R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER 23R CORRODED AT BS 360. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007112100167 20071121 00167 NM 2007 11 21 SWAA075690 1 20071113 A 5311 6546526 FRAME BOEING 737 737317 138447P NM BS 400 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007112100168 20071121 00168 NM 2007 11 21 SWAA075691 1 20071113 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM BS 515 S20R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER 20R CRACKED AT BS 515. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007112100169 20071121 00169 NM 2007 11 21 SWAA075692 1 20071113 A 5553 6546568 FITTING BOEING 737 7373A4 1384585 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND RT VERTICAL STABILIZER FITTING BODY FRONT SPAR CLEVIS AFT LUG FACE CORRODED. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007112100170 20071121 00170 NM 2007 11 21 SWAA075686 1 20071113 A 5311 6546558 FRAME BOEING 737 7373A4 1384585 NM BS 907 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007112100173 20071121 00173 NM 2007 11 21 SWAA075695 1 20071113 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM BS 500D S28R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007112100174 20071121 00174 NM 2007 11 21 SWAA075685 1 20071113 A 5310 571773 WINDOW FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND L1 WINDOW UPPER FRAME CRACKED AT OUTBOARD END. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007112100175 20071121 00175 NM 2007 11 21 SWAA075696 1 20071113 A 5743 115A5211 TRUNNION BOEING 737 7377H4 1384404 NM RH WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 712SW 27846 DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2007112100178 20071121 00178 NM 2007 11 21 SWAA075699 1 20071113 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 796SW 27889 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 5 ABC INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007112100180 20071121 00180 SO 2007 11 21 FDKA200707340 1 20070717 A 3350 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FDM 6133 MCO-FLL (1015 PHX LCL). ROW 3 BULKHEAD EMERGENCY LIGHT INOP, RT ROW 12 EMERGENCY AND RT ROW 12 EMERGENCY LOCAT OR SIGN INOP. MX RESET THE EMERGENCY LIGHTS, OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2007112100182 20071121 00182 SO 2007 11 21 FDKA200707342 1 20070720 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 16815 145416 FDM 6166 JFK. EMERGENCY LIGHT INOP. MX REPLACED 3 BATTERIES, OPS GOOD. 2 L 7 2 4T RT T00011AT 2007112100185 20071121 00185 SO 2007 11 21 FDKA200707345 1 20070723 A 3350 SG9341 LIGHT EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 829MJ 145228 FDM 6153 MCO (1319 PHX LCL). LEFT HAND CENTER FLOOR EMERGENCY STRIP UNSECURE. MX RE-SECURED STRIP COVER AND INSTALLED NEW PHOTO ILLUMINESCENT STRIP. 2 L 7 2 4T RT T00011AT 2007112100186 20071121 00186 SO 2007 11 21 FDKA200707348 1 20070725 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6155 MCO (0624 PHX LCL). TWO EMERGENCY FLOOR LIGHT STRIPS INOP. MX RESET EMERGENCY LIGHT SYSTEM, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007112100187 20071121 00187 SO 2007 11 21 FDKA200707349 1 20070727 A 3350 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 847MJ 145517 FDM 6146 GPT (0710 PHX LCL). EMERGENCY LIGHT INOP. MX PERFORMED OPS CHECKS, OPS GOOD. 2 L 7 2 4T RT T00011AT 2007112100188 20071121 00188 SO 2007 11 21 FDKA200707353 1 20070731 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DISCONNECTED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FDM 6091 FLL (0759 PHX LCL). ROW 12 EMERGENCY LOCATOR SIGN INOP. MX DISCONNECTED AND RE-CONNECTED LOCATOR SIGN CONNECT ORS, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007112100189 20071121 00189 SO 2007 11 21 FDKA200708354 1 20070801 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 FDM 6001 PWM (0233 PHX LCL). EMERGENCY EXIT AISLE LIGHT DOESN'T ILLUMINATE AND IS LOOSE. MX REMOVED AND REPLACED EMERG ENCY LIGHT ASSY, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007112100190 20071121 00190 NM 2007 11 21 FDKA200708359 1 20070802 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 803LR 322 ASH 6208 JFK-SYR (1713 PHX LCL). PILOT REPORTED THAT THE EMERGENCY LIGHTS WILL NOT GO OFF WHEN SELECTED OFF. EMERGENCY LIGHTS SYSTEM WAS RESET WITH NO FURTHER ACTION REQUIRED. 2 H 7 2 4T RT A13NM 2007112100191 20071121 00191 NM 2007 11 21 KCSA071523 1 20071114 A 5415 ATTACH ANGLE BOEING 747 747246F 1384850 NM NR 4 NACELLE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 NR 4 PYLON STA - 221 UPPER ATTACH ANGLE ON I/B SIDE IS CRACKED .5 INCH LONG. 2 L 7 4 4F RT A20WE 2007112100193 20071121 00193 SO 2007 11 21 RAIA00711010 1 20071112 A 3010 M535366022M RELAY EMB 145 EMB145 3260210 SO ANTI ICE SYSTEM MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 814HK 145046 FLT NR 5489 - STL - WING ICE FAIL MESSAGE IN ICING CONDITION. MAINTENANCE PERFORMED OPS CHECK OF WING ANTI-ICE SYSTEM. REMOVED AND REPLACED WING ANTI-ICE COMMAND RELAY, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007112100194 20071121 00194 SO 2007 11 21 RAIA00711009 1 20071112 A 5210 DOOR EMB 145 EMB145 3260210 SO LACK OF LUBE A RAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 03 843HK 14500822 POST FLT NR 7958 - ORD - PAX DOOR HARD TO OPEN. MAINTENANCE LUBED PAX DOOR AND OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007112100197 20071121 00197 SO 2007 11 21 RAIA00711008 1 20071109 A 3350 744437 LIGHT EMB 145 EMB145 3260210 SO CABIN BURNED OUT A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 833HK 145240 PRE FLT NR 7979 - MLI - EMERGENCY EXIT LIGHT LEFTHAND OVERWING EXIT MARKER INOP. MAINTENANCE REMOVED AND REPLACED EMERG ENCY LIGHT, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007112100198 20071121 00198 NM 2007 11 21 CALA0700688 1 20071113 A 5330 654577683 SKIN BOEING 737 7373T0 1384582 NM BS 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND CORROSION ON BONDED DOUBLER AT STA 986.5 BELOW S27L. THE AREA WAS REPAIRED IAW ECRA 5311-01372. 2 L 7 2 4F RT A16WE 2007112100199 20071121 00199 NM 2007 11 21 CALA0700689 1 20071114 A 5313 6517685 STRINGER BOEING 737 737524 1384721 NM BS 360 S16L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 52616 27329 INSPECTION FOUND STRINGER 16L CHANNEL CRACKED AT FASTENER HOLE COMMON TO WEB AND CLIP AT STA 360. MULTIPLE CRACKS WERE FOUND IN THE SAME LOCATION, REPAIRED IAW ECRA 5311-01378. 2 L 7 2 4F RT A16WE 2007112100200 20071121 00200 NM 2007 11 21 SWAA075701 1 20071114 A 5752 6546455 TAB BOEING 737 7373H4 1384600 NM RT AILERON DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED BRDG CHECK, FOUND RT WING AILERON TAB DELAMINATED. REPAIRED TAB PER SRM. 2 L 7 2 4F RT A16WE 2007112600005 20071126 00005 NM 2007 11 26 NWAA073726301 1 20071108 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 661US 23719 DURING OVERNIGHT CHECK, FOUND 2 AFT RIGHT SIDE EXTERIOR EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED POWER S UPPLY AND BATTERY PACK. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007112600006 20071126 00006 NM 2007 11 26 KNNA200700042 1 20071008 A 5330 SKIN BOEING 737 7372L9 1384497 NM PWA JT8 JT8D9 52048 NE BS 951 CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 464AT 21278 CRACK ON FUSELAGE SKIN AT LWR HINGE CUTOUT DOOR-R2 STA 951. REPAIRED AREA BY CUTTING OUT THE DAMAGE AND INSTALLING A RE PAIR IAW SRM 53-30-3 FIG 45 AND ACO-0753104. 2 L 7 2 4F 4 F RT A16WE E2EA 2007112600007 20071126 00007 NM 2007 11 26 KNNA200700041 1 20070902 A 2910 BACH6M0194AAR HOSE BOEING BOEING 737 737232 1384475 NM PWA JT8 JT8D5 52046 NE HYDRAULIC SYS LEAKING A KNNA B EMER. DESCENT K FLUID LOSS DE DESCENT 1 WP 25 332D 23104 WHILE EN ROUTE TO ATLANTA HARTSFIELD AIRPORT (KATL) FROM TUNICA, MISSISSIPPI (KUTA) AS SKY KING FLT (SGB332) THE CREW NO TICED A SLOW LOSS OF SYSTEM “A” HYDRAULIC FLUID. AFTER DECLARING AN IN-FLIGHT EMERGENCY, AN UNEVENTFUL LANDING WAS MADE , THE CREW TAXI THE AIRCRAFT UNTIL THE SYSTEM A LOW PRESSURE LIGHT CAME ON, AND THE SYSTEM WAS SHUTDOWN AND THE AIRCRAFT WAS TOWED THE REST OF THE WAY TO THE GATE. 2 L 7 2 4F 4 F RT A16WE E2EA 2007112600008 20071126 00008 NM 2007 11 26 QXEA200701657 1 20071101 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - FUSELAGE SKIN IS GOUGED 12" AFT OF FRONT AND 14" UNDER LOWER EDGES OF AFT CARGO DOOR CUTOUT. REPAIRED IAW SRM 53-40-31, 51-25-10. 2 H 7 2 4T RT A13NM 2007112600010 20071126 00010 NM 2007 11 26 QXEA200701656 1 20071101 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - FUSELAGE SKIN IS GOUGED IN 2 PLACES, 20" AFT OF FRONT AND 2" UNDER LOWER EDGES OF AFT CARGO DOOR CUTOUT. REPAI RED IAW RD8/4-53-666 AND SRM 51-25-00, 51-21-10. 2 H 7 2 4T RT A13NM 2007112600011 20071126 00011 NM 2007 11 26 QXEA200701654 1 20071101 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - CHAFE MARK ON AFT CARGO DOOR FUSELAGE CUTOUT AT CENTER OF RADIUS AT TOP AFT CORNER. REPAIRED IAW SRM 51-14-00, 51-21-10, 51-25-15. 2 H 7 2 4T RT A13NM 2007112600012 20071126 00012 SW 2007 11 26 WGEA200700023 1 20071108 A 3230 LANDING GEAR ECLIPS EA500 ECLIPSEEA500 3350000 SW RIGHT MALFUNCTIONED E WGEA O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 110DJ 000007 DURING EVALUATION FLIGHT, RIGHT MAIN GEAR INDICATED UNSAFE IN TRANSITION-TOOK APPROXIMATELY 20 SECONDS TO INDICATE GREEN . FIRST EXTENSION NORMAL, SECOND EXTENSION WAS WHEN GEAR INDICATED UNSAFE AND 20 SECONDS TO GREEN, DOWN AND LOCKED. PE RFORMED EXTENSION AND RETRACTION TEST OF MLG SYSTEM IAW EA500 AMM 32-30-00, NO DEFECTS NOTED WITH GREEN INDICATIONS AND TIMING. 1 L 7 2 4J RT A00002AC 2007112600013 20071126 00013 SW 2007 11 26 WGEA200700024 1 20071109 A 2620 FIRE BOTTLE ECLIPS EA500 ECLIPSEEA500 3350000 SW RT NACELLE LEAKING E WGEA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 EA 27 115DJ 190 000020 EVIDENCE OF FIRE SUPPRESSION AGENT LEAKING INTO RIGHT ENGINE. SUPPLEMENTAL INFORMATION, CLEANED ENGINE IAW PWC EMM 71-0 0-00-108-808 AND PWC FSR RECOMMENDATION LETTER. 1 L 7 2 4J RT A00002AC 2007112600016 20071126 00016 EA 2007 11 26 SIMA200731603 1 20071107 A 2150 23438123 ACM CNDAIR CL600 CL6002C10 1390015 EA LEFT SMOKE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 517AE 10124 LEFT PACK AUTO FAIL AND VISUAL SMOKE FROM AIRCRAFT VENTS IN COCKPIT. REMOVED AND REPLACED LEFT ACM IAW CRJ AMM 21-51-08 . OPERATIONAL TEST GOOD MEL ITEM RESTORED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007112600017 20071126 00017 EA 2007 11 26 SIMA200731604 1 20071110 A 5230 DOOR CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY UNSECURE A SIMA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 SW 21 516AE 10123 CREW NOTED DURING CLIMB OUT THAT COULD NOT PRESSURIZE A/C AND NO WARNING INDICATION, THEY RETURNED TO BNA FOR MTX. AFTE R LANDING FOUND THE AFT CARGO DOOR AFT SECTION WAS NOT CLOSED ALL THE WAY. RESECURED CARGO DOOR PERFORMED GVI OF CARGO DOOR AND PERFORMED. OPS CHECK OF DOOR IAW CRJ MM 52-31-00, OPS CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SER VICE. 2 L 7 2 4F RT A21EA 2007112600018 20071126 00018 SO 2007 11 26 SIMA200731602 1 20071111 A 2720 15793101 PRESSURE SWITCH EMB 135 EMB135LR 3260305 SO RUDDER MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 733KR 145368 RUDDER SYS 1-2 INOPERATIVE ON GROUND DURING TAXI. REMOVE AND REPLACE NR 2 RUDDER PRESSURE SWITCH IAW EMB 135 AMM 27-23- 04. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007112600019 20071126 00019 NM 2007 11 26 NWAA073735515 1 20071109 A 3397 WIRE BOEING 757 757251 1384970 NM EMERGENCY LIGHTS DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 515US 23203 DURING OVERNIGHT CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOP FROM ROW 23 TO AFT LAVS. MAINTENANCE REPAIRED BAD WIR E SPLICE. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007112600020 20071126 00020 EA 2007 11 26 QXEA200701600 1 20071021 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 C4 PDX - 280 FLOORBEAM HAS CORROSION AREAS ON TOP SURFACE OF BEAM RIGHT SIDE AT 13-18, 19-33, 34-46 CENTERLINE AS MEASUR ED FROM RIGHT SIDEWALL FUSELAGE SKIN TO CENTERLINE LOCATION. REPAIRED IAW REO670-53-11-047, REO670-53-11-052. 2 L 7 2 4F RT A21EA 2007112600021 20071126 00021 EA 2007 11 26 QXEA200701599 1 20071020 A 5510 PIVOT ASSY CNDAIR CL600 CL6002C10 1390015 EA HORIZONTAL STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 C4 PDX - RIGHT HORIZONTAL STAB PIVOT POINT HAS ROTATED INTO THE ANTI ROTATION TAB. REPAIRED IAW REO670-55-11-110. 2 L 7 2 4F RT A21EA 2007112600023 20071126 00023 EA 2007 11 26 QXEA200701603 1 20071027 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 485-541 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 C4 PDX - CENTER SEAT TRACK NR 15 HAS CORROSION IN CENTER AND EDGES OF TRACK AT STATION FS 485, 493, 509, 525, AND 541. REPAIRED IAW AMM 53-00-49-000-0801-A01. 2 L 7 2 4F RT A21EA 2007112600025 20071126 00025 EA 2007 11 26 QXEA200701601 1 20071021 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 C4 PDX - 280 FLOORBEAM RIGHT SIDE BULKHEAD HAS CORROSION ON AFT SIDE OF BULKHEAD NEXT TO 18-24, 26-35, AS MEASURED FROM RIGHT SIDE WALL FUSELAGE SKIN LOCATION. REPAIRED IAW REO670-53-052. 2 L 7 2 4F RT A21EA 2007112600026 20071126 00026 EA 2007 11 26 QXEA200701602 1 20071018 A 5414 SKIN CNDAIR CL600 CL6002C10 1390015 EA RT NACELLE DEBONDED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 C4 PDX - RIGHT ENGINE PYLON TRAILING EDGE ASSEMBLY LOWER SKIN IS DISBONDED AND TORE. REPAIRED IAW SRM 54-53-01, 51-75-0 0, AND 51-42-13. 2 L 7 2 4F RT A21EA 2007112600027 20071126 00027 EA 2007 11 26 QXEA200701606 1 20071023 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 C4 PDX - LEFT CENTER CABIN SEAT TRACK NR 9 STATION X370 TO X379 HAS PITTING CORROSION, CHAFE, SCRATCHES. REPAIRED IAW A MM 53-00-49-000-801-A01. 2 L 7 2 4F RT A21EA 2007112600029 20071126 00029 EA 2007 11 26 QXEA200701605 1 20071023 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 370-485 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 C4 PDX - RIGHT CENTER CABIN SEAT TRACK NR 14 STATION X370 TO X485 HAS NUMEROUS AREAS OF PITTING CORROSION NICKS AND SCRA TCHES. REPAIRED IAW AMM 53-00-49-000-801-A01. 2 L 7 2 4F RT A21EA 2007112600031 20071126 00031 EA 2007 11 26 REXA200700062 1 20071110 A 2100 ECS CNDAIR CL600 CL6002B19 1900309 EA CONTAMINATED A REXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 8747B 7747 ON CLIMB-OUT, RECEIVED SMOKE TOILET MESSAGE, RETURNED TO AIRPORT. INDICATION CAUSED BY DE-ICE FLUID INTO ECS SYSTEM. 2 L 7 2 4F RT A21EA 2007112600033 20071126 00033 EA 2007 11 26 QXEA200701616 1 20071024 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 C4 PDX-280 FLOORBEAM HAS CORROSION ON TOP SURFACE OF BEAM LEFT SIDE AT 6-8, 13-18, 19-25, AND 29-46 MEASURED FROM LEFT S IDE FUSELAGE SKIN TO CENTERLINE. REPAIRED IAW REO670-53-11-047 AND SRM 51-42-10. 2 L 7 2 4F RT A21EA 2007111900077 20071119 00077 EA 2007 11 19 TRAX200701688 1 20071105 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 CAPTAIN`S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007111900078 20071119 00078 EA 2007 11 19 TRAX200701689 1 20071105 A 7830 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSERS ILLUMINATED A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 839AS 7284 R THRUST REVERSER UNLOCK MESSAGE IN FLIGHT EMER STOW BUTTON WAS USED, NO INDICATION CHANGE TOOK PLACE. EN ROUTE TO ATL A/C DIVERTED TO CVG DUE TO MTC. EMERGENCY DECLARED. THRUST REVERSER SYSTEMS. 2 L 7 2 4F RT A21EA 2007111900087 20071119 00087 NM 2007 11 19 ZZDA2007296 1 20070701 A 5330 SKIN BOEING 717 717200 1383700 NM BS 550 L21R DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 996AT 55140 BAG CART DAMAGE ON RT FUSELAGE APPROX STA 550 AT LONGERON 21 AFT OF FWD BB DOOR AND FWD OF RT WING TO BODY FAIRING HIDDE N DAMAGE INSPECTION REQUIRED REF: RFE 07-0665 / PEA 17- 53-00518IR. INSTALLED PERMANENT REPAIR AT SKIN DAMAGE AND LONGE RON DAMAGED IAW B717 SRM 53-00-01 FIG 201 REPAIR 1 AND 5300-05 REPAIR 2 FIG 201. 2 L 7 2 4F TR A6WE 2007111900088 20071119 00088 NM 2007 11 19 CALA0700662 1 20071108 A 3350 RPS1B CHARGER BOEING 737 7373TO 138447G NM EMERGENCY LIGHTS INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16339 23577 THE EMERGENCY EXIT LIGHTS FROM ROW 21-25 LEFT WERE FOUND INOPERATIVE. THE AFT BATTERY PACK AND CHARGER WERE REMOVED AND REPLACED IAW AMM 33-51-51 PG 201. 2 L 7 2 4F RT A16WE 2007111900106 20071119 00106 NM 2007 11 19 SWAA075631 1 20071108 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500C S27R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 27R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007111900115 20071119 00115 NM 2007 11 19 ASAA0752212 1 20071108 A 2131 CONTROLLER BOEING 737 737890 1384527 NM CABIN PRESSURE MALFUNCTIONED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 585AS 35683 ON PRE FLIGHT PRESSURIZATION CONTROLLER CRUISE ALTITUDE WILL NOT SET. STUCK ON 37,000 THEN 38,000. CYCLED AIRCRAFT POW ER CABIN PRESSURE CONTROL PANEL ALTITUDE WINDOW, OP CHECKS GOOD. 2 L 7 2 4F RT A16WE 2007111900119 20071119 00119 NM 2007 11 19 ASAA0742215 1 20071109 A 5320 6517688126 CUSP WEB BOEING 737 7374Q8 138447Q NM BS 312-332 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 MAIN CABIN LEFT STA 312 332 LBL 56 CUSP WEB HAS CORROSION AT L1 DOOR CUTOUT. REMOVED CORROSION FOUND OUT OF LIMITS. FA BRICATED NEW CUSP WEB USING MATERIAL 7075 T6.40. INSTALLED NEW CUSP WEB IAW BAC DWG 65 17688 AND SRM 737 400 51-40-2. 2 L 7 2 4F RT A16WE 2007111900136 20071119 00136 EA 2007 11 19 HNAA0700266 1 20071111 A 3350 SW593 SWITCH DHAV DHC8 DHC8311 1386006 EA EMERGENCY LIGHTS INOPERATIVE A HNAA O OTHER L NO TEST TX TAXI/GRND HDL 1 EA 07 328EN 281 THE EMERGENCY LIGHTS SWITCH ON FLIGHT ATTENDANTS PANEL IS INOP. FERRIED A/C TO MDT. REMOVED AND REPLACED THE FLIGHT AT TENDANTS EMERGENCY LIGHT SWITCH ASSEMBLY. THE OPS CHECK WAS GOOD. 2 H 7 2 4T RT A13NM 2007111900137 20071119 00137 NM 2007 11 19 HNAA0700267 1 20071110 A 3350 MODULE DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS INOPERATIVE A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 975HA 176 FIRST RED LIGHT ON FLOOR INOP. REMOVED AND REPLACED THE MODULE, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007111900168 20071119 00168 NM 2007 11 19 CALA0700669 1 20071110 A 5320 INTERCOSTAL BOEING 737 737524 1384721 NM BS 348.2-360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 52616 27329 INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL BETWEEN BS 348.2 AND BS 360.0, S16L. THE INTERCOSTAL WAS REMOVED AND REP LACED IAW SRM 53-10-04, REPAIR 2, FIGURE 201. 2 L 7 2 4F RT A16WE 2007111900173 20071119 00173 NM 2007 11 19 CALA0700674 1 20071111 A 5311 651630364 FRAME BOEING 737 7373T0 1384582 NM BS 203 S28L/R CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND FRAME AND SUPPORT CORRODED AT STA 203.8, S28L TO S28R, RBL 5.7 TO LBL 5.7. THE FRAME CHORD AND SUPPORT WERE REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007111900174 20071119 00174 SO 2007 11 19 LR7A07120 1 20071106 A 5230 SKIN LKHEED 382 382G 526414U SO CARGO DOOR CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 618 4606 DURING SCHEDULED B-2 CHECK PER JOB CARD HB5301 FOUND 1 INCH LONG CRACK AT CARGO DOOR EXTERIOR SKIN PRESSURE SAFETY VALVE CUTOUT AREA FS 1003 LBL 50. REPAIR ACCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70. 2 H 7 4 4T A1SO 2007111900176 20071119 00176 SO 2007 11 19 LR7A07122 1 20071106 A 5350 SKIN LKHEED 382 382G 526414U SO BS 537-577 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 618 4606 DURING SCHEDULED B-2 CHECK PER JOB CARD HB5301 FOUND RT BOTTOM WHEEL WELL FAIRING SKIN CRACKED AT BELLY ATTACHMENT AREA FS 537 & FS 577, WL 132, RBL 45. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-12 USING 2024T3 .040". 2 H 7 4 4T A1SO 2007112000014 20071120 00014 CE 2007 11 20 DXTA200702599 1 20071106 A 3230 LANDING GEAR BEECH MU300 400A 1155402 CE MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 138QS RK492 RED LIGHT IN MLG HANDLE STAYS ON AFTER GEAR RETRACTION. JACKED ACFT & INSTALLED HYD MULE. CHECKED MLG UPLOCK ASSY'S & ADJUSTED RT MLG UPLOCK IAW MM 32-30-00. ACCOMPLISHED GEAR SWINGS WHILE SLOWLY REDUCING HYD PRESSURE. AT 1200 PSI RED H ANDLE MLG LIGHT STAYED ON & BOTH MLG DOORS REMAINED OPEN. WITH HYD PRESSURE STILL APPLIED BOTH MLG REMAINED RETRACTED W ITH MLG DOORS OPEN. PULLED ON NLG DOORS & NLG EXTENDED. CHECKED RIGGING OF NLG UPLOCK ASSY & ADJUSTED PER MM 32-30-00. POWERED UP HYD SYS & ACCOMPLISHED MLG FUNCTIONAL TEST PER MM 32-00-00. POWERED UP HYD SYS & ACCOMPLISHED MLG FUNCTION AL TEST PER MM 32-00-00 NO DEFECTS NOTED. REMOVED ACFT FROM JACKS & REMOVED HYD MULE. CHECKED SERVICE OF HYD RESERVOI 2 H 7 2 4F RT A16SW 2007112000015 20071120 00015 CE 2007 11 20 DXTA200702600 1 20071106 A 3243 991205015 MASTER CYLINDER CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE BRAKES BYPASSING E DXTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 639QS 174 174 5605139 LT BRAKE PEDAL ON CAPTAINS SIDE GOES NEARLY TO THE FLOOR. COPILOTS SIDE NORMAL. GAINED ACCESS AND REMOVED PILOT SIDE L T BRAKE MASTER CYLINDER AND INSTALLED AN OVERHAULED UNIT AND SECURED BLED SYST. AS REQUIRED OPS CHECKED SATISFACTORY I.A .W CE-560XL M/M CHAPTERS 32-42-02 AND 32-42-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007112000016 20071120 00016 CE 2007 11 20 DXTA200702601 1 20071106 A 2170 COALESCER BAG CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CABIN AIR DIRTY E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 956QS 7500156 VERY STRONG PUNGENT ODOR COMMING FROM THE AIR CONDITION SYSTEM. REMOVED & CLEANED WATER SOCKS. INSTALLED WATER SOCKS AN D LEAK CHECK. OPS CHECKED. WORK DONE IAW CITATION 750 AMM 12-10-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007112000017 20071120 00017 CE 2007 11 20 DXTA200702602 1 20071107 A 3620 1153P0104 PRESSURE SWITCH CESSNA 680 680CE 2076811 CE PWA JT15 JT15D5 52112 NE AFT SERVICE BAY INOPERATIVE E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 313QS 361 6800140 ABORTED TAKE OFFDUE TO HP FAIL LT CAUTION LIGHT. INSTALLED NEW LEFT HP DIFFERENTIAL PRESSURE SWITCH (SD001). PERFORMED OPERATIONAL CHECK AND LEAK CHECK IAW CE-680 MM 36-10-00. CHECKED GOOD. 2 L 7 2 4F 4 F RC T00012WI E25EA 2007112000018 20071120 00018 NM 2007 11 20 UPS07551108 1 20071107 A 5610 WINDOW BOEING 757 75724APF 1384969 NM COCKPIT BINDING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 438UP 25469 R2 WINDOW BINDING DURING OPERATION. COMPLETED REMOVAL OF RT WINDOW CRANK AND INSTALLED NEW SERVICEABLE GEARBOX AND (4) MOUNT BOLTS. REFERENCE MM 56-11-04-4. INSTALLED NR 2R WINDOW SHROUD AND CRANK HANDLE PANEL. OPENED & CLOSED WINDOW SEVE RAL TIMES. CHECKS GOOD W/REF TO MM 56-11-04-4. 2 L 7 2 4F RT A2NM 2007112000019 20071120 00019 SO 2007 11 20 CHQA200700069 1 20071104 A 2750 FLAP SYSTEM EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL TE FLAPS MALFUNCTIONED A CHQA O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 262SK 145168 CAE312351 CXR TO CLE - ON APPROACH TO CLE THE FLAPS WERE SELECTED FROM THE 0 TO 9 POSITION AND AS SOON AS THE LEVER WAS MOVED, THE FLAP FAIL MESSAGE WAS DISPLAYED ON EICAS WITH A FLAP 0 POSITION INDICATION. THE QRH WAS FOLLOWED FOR FLAP FAILURE, AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE CMC FOR FAULT CODES AND FOUND ONE OCCURRENCE OF FLA P JAMMING. MAINTENANCE THEN INSPECTED THE FLAPS AND FLAP TRACKS BUT DID NOT FIND ANY DEFECTS. THE FLAP SYSTEM WAS RESE T AND THE FLAPS WERE CYCLED SEVERAL TIMES WITHOUT FAULTS, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007112000020 20071120 00020 SO 2007 11 20 C2XA07TY065 1 20071031 A 3234 HANDLE EMB 145 EMB145LR 3260212 SO MLG FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14953 145071 LANDING GEAR FAILED TO RETRACT. REPLACED LANDING GEAR HANDLE IAW EMB 145 MM 32-32-02, OPS CHECK GOOD. AIRCRAFT RELEASE D AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007112100001 20071121 00001 EU 2007 11 21 TRAX200701623 1 20071029 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 LEFT SEAT TRACK BETWEEN FR 36 & 37 CORRODED. 2 H 7 2 4T RT 2007112100022 20071121 00022 NM 2007 11 21 SWAA075667 1 20071112 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM BS 500C S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 21L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007112100031 20071121 00031 EA 2007 11 21 TRAX200701698 1 20071107 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 883AS 7504 AAR - PILOTS BULKHEAD AT FS 280.0 AND LBL 9.0 IS CRACKED IN LOWER RADIUS. PERFORMED REPAIR TO PILOT'S BULKHEAD AT FS 28 0.0 AND LBL 9.0, PER: REO 601R-53-11-171, REV D. SUPPLEMENTAL - SDR CLOSED 11/13/07. 2 L 7 2 4F RT A21EA 2007112100053 20071121 00053 EU 2007 11 21 USAA920071133 1 20071110 A 5320 D5347112420000 SHEAR PLATE AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 658AW 1110 PIT - MAJOR REPAIR - BC6 CHECK, CORROSION ON LEFT HAND SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70. REPLACED LEFT HA ND SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007112100057 20071121 00057 WP 2007 11 21 ASAA0782217 1 20071108 A 5321 99365859 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 927-1003 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 977AS 53453 CABIN FLOORBOARD CRACKED OUT CORNER AND DELAMINATED STA 927 TO STA 1003 RBL 22 TO RBL 44. FABRICATED A REPLACEMENT PANE L IAW MD80 SRM 53-05 PAGES 251 THRU 257 AND DAC DRAWINGS S4932106. 2 L 7 2 4F RT A6WE 2007112100078 20071121 00078 EU 2007 11 21 ASAA0742237 2 20071108 A 7320 1459M27P07 MEC BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU LT ENGINE MALFUNCTIONED A ASAA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 NM 02 797AS 42361 5698 28892 ON ROUTE LAX TO YVR LEFTHAND ENGINE FLAMED OUT IN CRUISE AT FL340. DESCENDED TO FL200 PERFORMED AIR RESTART THEN DIVERT ED TO SEA WHERE AIRCRAFT CHANGE WAS MADE BEFORE CONTINUING ON TO YVR. REPLACED ENGINE FUEL PUMP AND MEC (MAIN ENGINE CO NTROL). AFTER ENGINE BORESCOPE REVEALED NO DAMAGE, AIRCRAFT AND ENGINE WERE DECLARED SERVICEABLE. SUSPECT MEC WAS CAUS E. FOLLOW-UP ASSESSMENT IS BEING SCHEDULED WITH VENDOR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112100079 20071121 00079 SO 2007 11 21 C2XA07RI097 1 20071109 A 3350 20131A INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13949 3603 3603 145057 EWR - DURING ROUTINE MAINTENANCE, MX FOUND GALLEY SERVICE LIGHT INOPERATIVE. MX REMOVED AND REPLACED NR 2 EMERGENCY LIG HT INVERTER AND PERFORMED OPERATIONAL SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007112100083 20071121 00083 NM 2007 11 21 ASAA0772240 1 20071110 A 5347 146A750125 CARGO TRACK BOEING 737 737790 13844CN NM BS 761-887 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 648AS 30662 AFT CARGO RT TIE DOWN TRACK BS 792 TO 847 RBL 13 IS CORRODED. AFT CARGO RT TIEDOWN TRACK CORRODED SECTION FROM BS 76 TO 887 REPLACED WITH MADE REPAIR PARTS IAW B737 700 SRM 53 00 53 FIG 201 REPAIR 3. 2 L 7 2 4F RT A16WE 2007112100086 20071121 00086 NM 2007 11 21 ASAA0772243 1 20071110 A 5320 146A75036 FLOOR SUPPORT BOEING 737 737790 13844CN NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 648AS 30662 AFT CARGO PIT BS 767+6 RBL 8.1 CHANNEL CORRODED. AFT CARGO PIT FLOOR CHANNEL AT BS. 767+6 RBL 8.0 REPAIRED IAW ASA EA 5 330 02743. 2 L 7 2 4F RT A16WE 2007112100089 20071121 00089 NM 2007 11 21 ASAA0772246 1 20071110 A 5320 146A75039 CHANNEL BOEING 737 737790 13844CN NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 648AS 30662 AFT CARGO PIT BS 767+6 LBL 12.5 CHANNEL CORRODED. AFT CARGO PIT FLOOR CHANNEL AT 767+6 LBL 12.5 REPAIRED IAW ASA EA 533 0 02743. 2 L 7 2 4F RT A16WE 2007112100121 20071121 00121 NM 2007 11 21 2007UALA04642 1 20071111 A 5230 65B04250330 STRUCTURE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE AFT CARGO DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 181UA 25278 MAJOR REPAIR: AFT CARGO DOOR INSIDE LWR AFT AREA CORROSION, 6 PLACES. INSTALLED DOUBLER REF SRM 51-70-13 FIG 201. AC O K FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112100124 20071121 00124 NM 2007 11 21 2007UALA04648 1 20071111 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 DOOR 2R BOTH EMERGENCY EXIT SILL LIGHTS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112100130 20071121 00130 NM 2007 11 21 2007UALA04658 1 20071108 A 5330 65B07618 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 174UA 69238 24381 FUSELAGE DAMAGED 4 FEET BELOW F/O'S NR 2 WINDOW, INLINE WITH WINDOW AND AOA SENSOR. DENT IS 2.5" LONG AXIS AN D .125" I N DEPTH. CTR HAS CREASE OR GOUGE. DAMAGE IS APPROX STA 297 BETWEEN RT STRINGER 14 & S14-D WITH NO FRAME CONTACT. REPAI RED PER SRM 53-00-01 REPAIR 7 TIME LIMITED EXTERNAL REPAIR. MF1596 CREATED TO MONITOR. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112100134 20071121 00134 NM 2007 11 21 WRLA2007123 1 20071109 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING C-CHECK INSPECTION CORROSION FOUND RIGHT HAND SEAT TRACK STA Y=555 X=75.25. REPLACED DAMAGED SEAT TRACK PER MD11 SRM 51-33-01 VOL.II REV.40. 2 L 7 3 4F 4 F RT A22WE E24NE 2007112100140 20071121 00140 NM 2007 11 21 USAA920071135 1 20071113 A 5320 141N842241 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 200UU 27809 MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON CABIN FLOOR ANGLE, BS 310.5 - BS 326, S17R, WL 208. REPLACED CABIN FLOOR A NGLE, BS 310.5 - BS 326, S17R, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007112100145 20071121 00145 NM 2007 11 21 USAA920071141 1 20071110 A 5320 ANGLE BOEING 767 767201 1385125 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 245AY 23897 CLT - MAJOR REPAIR - CORROSION ON AFT LAVATORY DUMP CUTOUT ANGLE. REPLACED AFT LAVATORY DUMP CUTOUT ANGLE IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2007112100146 20071121 00146 NM 2007 11 21 SWAA075668 1 20071113 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 203WN 32483 EEPLS END CAP LOOSE AT ROW 1 ABC. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 2007112100153 20071121 00153 2007 11 21 SWAA075674 4 20071113 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007112100166 20071121 00166 NM 2007 11 21 SWAA075683 1 20071113 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM BS 360 S22R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER 22R CORRODED AT BS 360. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007112100171 20071121 00171 NM 2007 11 21 SWAA075693 1 20071113 A 5314 6562125 KEELBEAM BOEING 737 7373A4 1384585 NM BS 500D S28R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND KEEL BEAM CHORD CORRODED AT BS 500D, STR 28R. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2007112100183 20071121 00183 SO 2007 11 21 FDKA200707343 1 20070722 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 15182 145359 FDM 6129 RDU (0356 PHX LCL). ALL EMERGENCY LIGHTS INOP. MX REPLACED ALL EMERGENCY BATTERY PACKS. 2 L 7 2 4T RT T00011AT 2007112100201 20071121 00201 NM 2007 11 21 SWAA075717 1 20071114 A 5512 SKIN BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRDG CHECK, FOUND RT HORIZONTAL STABILIZER LOWER T/E SKIN CRACKED AT STA 179. REMOVED AND REPLACED HOR IZONTAL STABILIZER PER MM. 2 L 7 2 4F RT A16WE 2007112100202 20071121 00202 2007 11 21 SWAA075702 4 20071114 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007112100203 20071121 00203 NM 2007 11 21 SWAA075703 1 20071113 A 3260 1899 SENSOR BOEING 737 7373H4 1384600 NM NLG DOOR DIRTY A SWAA O OTHER J WARNING INDICATION CL CLIMB 1 SW 29 361SW 26572 DURING GEAR RETRACTION NLG RED LIGHT REMAINED ILLUMINATED. CYCLED GEAR ALL INDICATIONS NORMAL. RESEATED LOGIC CARDS M1 214, N1215AND M983 AND CLEANED NLG POSITION SENSOR PER MM. 2 L 7 2 4F RT A16WE 2007112600001 20071126 00001 SW 2007 11 26 WGEA200700020 1 20071106 A 3240 30266B BRAKE ECLIPS EA500 ECLIPSEEA500 3350000 SW MLG WEAK E WGEA O OTHER O OTHER LD LANDING 1 EA 27 145DJ 14 000057 LT BRAKE PEDAL WENT TO THE FLOOR ON LANDING. RAPID PUMPING RESULTED IN SLIGHT BRAKE EFFECTIVENESS. DID NOT TO FULL PED AL UNTIL ON RAMP. SUPPLEMENTAL INFORMATION, REPLACED LT BRAKE WITH NEW BRAKE. PERFORMED SATISFACTORY BLEED, LEAK, AND O P'S CHECK. SERVICED BRAKE RESERVOIR I/A/W EA 500 M/M 32-41-15 AND EA SEM 500-0063 REV A. 1 L 7 2 4J RT A00002AC 2007112600014 20071126 00014 SO 2007 11 26 SIMA200731605 1 20071111 A 2610 UNKNOWN EMB 135 EMB135KL 3260302 SO CABIN SMOKE A SIMA B A EMER. DESCENT UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 807AE 145506 CREW FOLLOWED UP WITH CALL ABOUT 500' AFTER TAKEOFF 'LAV SMOKE' WARNING ILLUMINATED. WARNING LIGHT WENT OFF ON FINAL AP PROACH. FA REPORTED SMOKE IN CABIN. OVERWEIGHT LANDING: LANDING WEIGHT 42320, SINK RATE 200 FT PER MIN TOUCHDOWN WAS SOFT. 2 L 7 2 4F RT T00011AT 2007112600032 20071126 00032 EA 2007 11 26 QXEA200701612 1 20071022 A 5320 INTERCOSTAL CNDAIR CL600 CL6002C10 1390015 EA BS 283 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 C4 PDX - FORWARD NUTPLATE HOLE IN THE FLOOR LEVEL INTERCOSTAL AT STATION 283 IS CORRODED. REPAIRED IAW SRM 53-21-43, 51 -21-16, AND REO670-53-21-302. 2 L 7 2 4F RT A21EA 2007112600034 20071126 00034 EA 2007 11 26 QXEA200701617 1 20071022 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 484 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 C4 PDX - CORROSION FOUND ON BEAM UNDER SEAT TRACK NR 9 AT STATION FS 484.0. REPAIRED IAW SRM 51-26-06, REO670-53-31-088 . 2 L 7 2 4F RT A21EA 2007112600036 20071126 00036 EA 2007 11 26 QXEA200701610 1 20071021 A 5330 DOUBLER CNDAIR CL600 CL6002C10 1390015 EA BS 304 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 C4 PDX - INTERNAL FUSELAGE SKIN DOUBLER ABOVE LOWER TCAS ANTENNA HAS CORROSION AT FS304 AT STRINGER 0. REPAIRED IAW SRM 51-21-06. 2 L 7 2 4F RT A21EA 2007112600037 20071126 00037 EA 2007 11 26 QXEA200701609 1 20071021 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 492 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 C4 PDX - CORROSION ON FLANGE UNDER RIGHT INBOARD SEAT RAIL NR 15 AT STATION X492. REPAIRED IAW SRM 51-21-06, REO670-53- 31-088. 2 L 7 2 4F RT A21EA 2007112600040 20071126 00040 NM 2007 11 26 QXEA200701664 1 20071031 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - RIGHT INBOARD SEAT TRACK NR 10 HAS CORROSION AT STATION 1.00. REPAIRED IAW RD8/4-53-884 AND SRM 51-42-05. 2 H 7 2 4T RT A13NM 2007112600041 20071126 00041 NM 2007 11 26 QXEA200701662 1 20071105 A 5753 FLAP TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - THE NR 4 FLAP TRACK ON THE LEFT SIDE HAS WEAR DAMAGE ON INBOARD SIDE OF TRACK. REPAIRED IAW RD8/4-57-87811. 2 H 7 2 4T RT A13NM 2007112600045 20071126 00045 NM 2007 11 26 QXEA200701672 1 20071103 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 713 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - AFT CARGO BAY, LEFT SEAT TRACK 7" LONG SECTION OF SEAT TRACK AT STATION X713 - Z100 HAS CORROSION. REPAIRED IA W SRM 51-40-07, 51-42-05, 51-40-15. 2 H 7 2 4T RT A13NM 2007112600047 20071126 00047 NM 2007 11 26 QXEA200701674 1 20071103 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - AFT CARGO BAY, LEFT SEAT TRACK HAS CORROSION FASTENER HOLE AT STATION 733-Z100 OUTBOARD SIDE. REPAIRED IAW SRM 51-40-10, 51-42-05, 51-40-15. 2 H 7 2 4T RT A13NM 2007112600048 20071126 00048 NM 2007 11 26 QXEA200701675 1 20071103 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX-AFT CARGO BAY, LEFT SEAT TRACK HAS CORROSION FASTENER HOLE 6" FROM AFT END OUTBOARD SIDE. REPAIRED IAW SRM 51-42 -05, 51-40-10, 51-40-15. 2 H 7 2 4T RT A13NM 2007112600050 20071126 00050 NM 2007 11 26 QXEA200701669 1 20071031 A 5320 FLOOR SUPPORT BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - THE FORWARD FLOOR SUPPORT FLANGE FOR FLOOR PANEL 131CZ/131BZ HAS CORROSION. REPAIRED IAW SRM 51-21-00, 51-14-0 0. 2 H 7 2 4T RT A13NM 2007112600051 20071126 00051 NM 2007 11 26 QXEA200701667 1 20071101 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - NR 2 SEAT TRACK HAS PITTING CORROSION AT STATION X388. REPAIRED IAW RD8/4-53-884, SRM 51-40-15, 51-42-05, AND 51-42-45. 2 H 7 2 4T RT A13NM 2007112600052 20071126 00052 NM 2007 11 26 QXEA200701668 1 20071101 A 5320 FLOOR SUPPORT BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - THE MAIN CABIN DOOR THRESHOLD FLOOR PANEL LANDING HAS CORROSION AT SCREW HOLES AND RIVETS. REPAIRED IAW RD8/4- 53-1660. 2 H 7 2 4T RT A13NM 2007112600053 20071126 00053 NM 2007 11 26 QXEA200701671 1 20071031 A 5310 STRUCTURE BOMBDR DHC8 DHC8402 1390042 NM CARGO DOORWAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - AFT CARGO BAY CORROSION FASTENER HOLES INBOARD OF CARGO DOOR LIP. REPAIRED IAW SRM 51-14-00, 51-21-10. 2 H 7 2 4T RT A13NM 2007112600054 20071126 00054 NM 2007 11 26 QXEA200701676 1 20071031 A 5320 SUPPORT ANGLE BOMBDR DHC8 DHC8402 1390042 NM BS 783 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - AFT CARGO BAY, STATION 783, 7" IN FROM DOOR LIP AFT END HAS A CHAFE ON ANGLE SUPPORT. REPAIRED IAW SRM 51-14-0 0, 51-25-10. 2 H 7 2 4T RT A13NM 2007112600055 20071126 00055 NE 2007 11 26 REXA200700063 2 20071111 A 7230 5022T04P02 CARBON SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENGINE LEAKING A REXA E ENGINE SHUTDOWN B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 8390A 15165 7390 872951 CREW REPORTED A LAV SMOKE WARNING WHICH WAS CONFIRMED BY FLIGHT ATTENDANT. ENGINE WAS SHUT DOWN AT THE GATE AND MAINTEN ANCE WAS CALLED. MAINTENANCE TROUBLESHOT LAV SMOKE DETECTOR AND FOUND NO DISCREPANCIES. FURTHER INVESTIGATION LED TO A BOROSCOPE OF THE LT ENGINE WHICH REVEALED A LEAKING NUMBER THREE BEARING CARBON SEAL. AIRCRAFT WAS FERRIED TO A MAINTE NANCE BASE FOR CARBON SEAL REPLACEMENT. 2 L 7 2 4F 4 F RT A21EA E15NE 2007112600058 20071126 00058 NM 2007 11 26 QXEA200701681 1 20071031 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - RIGHT INBOARD SEAT TRACK NR 11 HAS CORROSION AT STATION +32.400. REPAIRED IAW SRM 51-42-05, 51-40-20. 2 H 7 2 4T RT A13NM 2007112600059 20071126 00059 NM 2007 11 26 QXEA200701682 1 20071101 A 5320 THRESHOLD BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - MAIN CABIN DOOR THRESHOLD CHANNEL HAS CORROSION ON LOWER SURFACE AT FIVE NUTPLATE LOCATIONS. REPAIRED IAW RD8/ 4-53-2117, RD8/4-53-1660. 2 H 7 2 4T RT A13NM 2007112600060 20071126 00060 NM 2007 11 26 QXEA200701680 1 20071102 A 5313 STRINGER BOMBDR DHC8 DHC8402 1390042 NM BS 258-286 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - THERE ARE SEVERAL RIVET BUCKTAILS CORRODED BETWEEN X258.5 AND X286.5 ON STRINGER 31L OUTBOARD SIDE. REPAIRED I AW SRM 51-42-00, 51-21-00, 51-14-00. 2 H 7 2 4T RT A13NM 2007112600062 20071126 00062 NM 2007 11 26 QXEA200701677 1 20071102 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 783 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - AFT CARGO BAY, 3" INBOARD FROM AFT END OF LEFT SEAT TRACK STATION 783 HAS CORROSION FASTENER HOLE AND ANGLE SUP PORT. REPAIRED IAW SRM 51-21-00, 51-21-10, 51-42-05. 2 H 7 2 4T RT A13NM 2007112600064 20071126 00064 NM 2007 11 26 QXEA200701679 1 20071102 A 5320 FLOOR SUPPORT BOMBDR DHC8 DHC8402 1390042 NM BS 664-685 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - CABIN FLOOR SUPPORT BETWEEN X664 AND X685, Y30L, Z100 IS CORRODED. REPAIRED IAW SRM 51-21-00, 51-40-07, 51-42- 35. 2 H 7 2 4T RT A13NM 2007112600065 20071126 00065 NM 2007 11 26 QXEA200701686 1 20071031 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 230-235 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION IN CHANNEL AND ON TOP OF RAILS BETWEEN X230 AND X235. REPAIRED IAW RD8 /4-83-884. 2 H 7 2 4T RT A13NM 2007112600068 20071126 00068 NM 2007 11 26 QXEA200701689 1 20071031 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 321 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION IN BOTTOM OF CHANNEL AND ON TOP OF RAILS AT STATION X321. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007112600069 20071126 00069 NM 2007 11 26 QXEA200701687 1 20071031 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 290 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION IN BOTTOM OF CHANNEL AND ON TOP OF RAILS AT STATION X290. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007112600074 20071126 00074 NM 2007 11 26 QXEA200701693 1 20071031 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 372-374 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION IN CHANNEL BETWEEN STATION X372 AND X374. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007112600078 20071126 00078 NM 2007 11 26 QXEA200701710 1 20071111 A 3297 473901 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM MLG SENSOR DAMAGED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 406QX 4048 GEG FLIGHT NR 2371: AFTER TAKEOFF, HAD A RED NOSE AND HANDLE LIGHT ILLUMINATED. DID ALTERNATE GEAR EXTENSION. HAD NO G REEN WITH RED NOSE AND HANDLE STILL ILLUMINATED. ALTERNATE INDICATOR WAS SHOWING GREEN (3). AIRCRAFT RETURNED TO FIELD . MAINTENANCE INTEROGATED PSEU AND NOTED PRESENT FAULT NGLK1 PROX SENSOR OPEN. REMOVED SENSOR NGLK1 HARNESS ONLY IAW 3 2-21-11-000-801. INSTALLED NEW HARNESS IAW 32-21-11-400-801, NGLK1 SENSOR ONLY, UP TO AND INCLUDING 5.H. OPS CHECK OF PRIMARY EXTENSION AND RETRACTION SYSTEM CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007112600082 20071126 00082 NM 2007 11 26 QXEA200101697 1 20071031 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 433-435 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION IN CHANNEL AND ON TOP OF RAIL BETWEEN STATION X433 AND X435. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007112600083 20071126 00083 NM 2007 11 26 QXEA200701698 1 20071031 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 558 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION IN CHANNEL AT STATION X558. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007112600084 20071126 00084 NM 2007 11 26 QXEA200701700 1 20071102 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 664 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - LEFT OUTBOARD SEAT TRACK HAS CORROSION AT STATION X664.5. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007112600085 20071126 00085 NM 2007 11 26 QXEA200701699 1 20071031 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 479 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION IN CHANNEL AND ON TOP OF RAIL AT STATION X479. REPAIRED IAW RD8/4-53-8 84. 2 H 7 2 4T RT A13NM 2007112600086 20071126 00086 NM 2007 11 26 QXEA200701718 1 20071112 A 7160 TCCAPDANIH949 ACTUATOR DHAV DHC8 DHC8202 2809007 NM NR 2 BYPASS DOOR MALFUNCTIONED A QXEA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 09 350PH 8699 488 PDX FLIGHT NR 2119, NR 2 ENGINE BYPASS DOOR DOES NOT INDICATE OPEN (LIGHT TEST OK) FROM CRUISE (FL230/-20'C) TO PARKING (+10"C). REPAIRED CHAFFED WIRES AND REPLACED NR 2 ENGINE INTAKE BYPASS DOOR LINEAR ACTUATOR. OPERATION CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007112600087 20071126 00087 NM 2007 11 26 07FDEA04775 1 20071113 A 5330 2024T3100C SKIN BOEING 727 727227 1384078 NM BS 480 S28L CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 479FE 21461 FWD CARGO BILGE 3" FWD OF STA 480 S-28L AT REPAIR SPLICE OTBD SIDE HAS CORROSION. CUT OUT DAMAGE, FABRICATED REPAIR PAR TS STR T7/710940. FABRICATED DOUBLER, FILLER, MAT 2024 T3.100C, AND 7075-T6.071C IAW SRM 53-10-3, 53-30-3. INSTALLED R EPAIR STRINGER AND FILLER/DOUBLER IAW SRM 53-10-3FIG 1, 53-30-3 FIG 3A, FS 480, S-28L. REPAIR IS CLASSIFIED AS MINOR RE PAIR. 2 L 7 3 4F A3WE 2007112600089 20071126 00089 NM 2007 11 26 DHLA200700059 1 20071025 A 7930 ST104Z TRANSMITTER BOEING 727 7272B7 138407L NM OIL PRESSURE MALFUNCTIONED A DHLA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 05 770AT 21953 NR 2 ENG OIL TEMP GAGE REDUCED TO 0 DEG ENG OIL PRESS REDUCED TO 20 PSI OIL QUALITY GOOD COMPLETED APPROPRIATE PRECAUTIO NARY ENG SHUT DOWN ENG OIL PRESSURE LIGHT FORWARD PANEL DID NOT ILLUMINATE. CK WIRING ON NR 2 ENG OIL TEMP AND OIL PRES SURE, CK WIRING FROM FIRE WALL FWD TO INDICATOR CK'S-GOOD. SUSPECTED WEEK C/B REMOVED AND REPLACED NR 2 ENG OIL TEMP A ND OIL PRESSURE BREAKER (P/N BACC18Z3R). REMOVED AND REPLACCED 32 PRESSURE TRANS PER 79-32-1, OPS CK LEAK CK OK. 2 L 7 3 4F A3WE 2007112600093 20071126 00093 NM 2007 11 26 DHLA200700063 1 20071031 A 3350 LAMP BOEING 727 727223 1384074 NM EMERGENCY LIGHTS INOPERATIVE A DHLA O OTHER O OTHER NR NOT REPORTED 1 GL 05 754DH 22008 EMERG EXIT LTS UNARMED LIGHT INOP. RELAMPED EMERG EXIT LTS. UNARMED LIGHT (P/N 313). OPS CHECKS NORMAL IAW MM CH 33-5 0-01. 2 L 7 3 4F A3WE 2007112600094 20071126 00094 NM 2007 11 26 QXEA200701717 1 20071106 A 5753 SKIN BOMBDR DHC8 DHC8402 1390042 NM TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - LEFT OUTBOARD FLAP HAS CHAFE ON THE INBOARD UPPER SKIN SURFACE, FROM THE UPPER FLAP SHROUD. REPAIRED IAW RD8/4 -57-016, SRM 51-52-30, 51-25-05. 2 H 7 2 4T RT A13NM 2007112600095 20071126 00095 NM 2007 11 26 AALA20072161 1 20071106 A 3350 D71701001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 756AM 30264 JFK - EMERGENCY LIGHTS AT LOWER RIGHT NUMBER TWO GALLEY WALL INOPERATIVE. REPLACED BATTERY PACK M33097 FOR EMERGENCY LI GHTS AT LOWER RIGHT NUMBER TWO GALLEY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007112600097 20071126 00097 NM 2007 11 26 AALA20072159 1 20071105 A 2750 PSEU BOEING 767 767223 1385123 NM TE FLAPS INOPERATIVE A AALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 21 323AA 22324 JFK INFLIGHT T2/05NOV - DURING INITIAL APPROACH CREW RECEIVED LEADING EDGE SLAT ASYMMETRY. CAPTAIN EXECUTED A MISSED AP PROACH AND LANDED ON SECOND APPROACH WITHOUT INCIDENT. AIRCRAFT TAXIED TO GATE. FOUND PROXIMITY SENSOR ELECTRONICS UNI T CARD FAULTED. REPLACED PROXIMITY SENSOR ELECTRONICS UNIT CARD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007112600098 20071126 00098 NM 2007 11 26 AALA20072160 1 20071106 A 3350 BPS73 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 319AA 22320 LAX - EMERGENCY LIGHT AT OVERHEAD SEAT 36B INOPERATIVE. REPLACED BATTERY PACK M379 FOR EMERGENCY LIGHT AT OVERHEAD SEAT 36B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007112600104 20071126 00104 NM 2007 11 26 AALA20072151 1 20071105 A 3350 0L3071BPEGPL LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 790AN 30251 MIA - EMERGENCY LIGHT AT SEAT 20C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007112600105 20071126 00105 NM 2007 11 26 AALA20072152 1 20071105 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 790AN 30251 MIA - EMERGENCY LIGHT AT SEAT 20C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007112600106 20071126 00106 NM 2007 11 26 AALA20072163 1 20071106 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 JFK - EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK M33401 FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007112600108 20071126 00108 NM 2007 11 26 AALA20072156 1 20071104 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 790AN 30251 MIA - EMERGENCY LIGHT AT SEAT 24C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007112600109 20071126 00109 EU 2007 11 26 F3LA200700315 1 20071113 A 5210 FE240004 CYLINDER DAMPER AIRBUS A318 A318111 3940019 EU R2 DOOR LOW PRESSURE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 812FR 1295 3163 FLIGHT CREW REPORTED R2 DOOR DAMPER CYLINDER WOULD NOT HOLD PRESSURE. MAINTENANCE FOUND L2 DOOR DAMPER ASSIST BOTTLE PR ESSURE LOW AND WOULD NOT TAKE NITROGEN CHARGE. REMOVED AND REPLACED L2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IAW AMM 52-13-14-PB401. 2 L 7 2 4F RT 2007112600110 20071126 00110 EA 2007 11 26 SWIA200718836 1 20070727 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA BS 235 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 CRACK IN FUSELAGE SKIN AT BS 235 AND RBL6, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS PER REO 601R 53-11-048 REV B. 2 L 7 2 4F RT A21EA 2007112600111 20071126 00111 EA 2007 11 26 SWIA200718837 1 20070727 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 480 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 CRACK FOUND ON SUPPORT ANGLE UNDER FLOOR PANEL 262DRF AT FS480, DISCOVERED AT C-CHECK. INSTALLED NEW SUPPORT AT FS484 A ND RBL36 PER CRJ200 SRM 51-23-00, 51-42-06 AND 51-42-21. 2 L 7 2 4F RT A21EA 2007112600112 20071126 00112 EA 2007 11 26 SWIA200718838 1 20070727 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 CRACKED VERTICAL STIFFENER AT FS 280.0 AND LBL27, DISCOVERED AT C-CHECK. INSTALLED NEW FABRICATED ANGLE AT FS280 AND LB L 27 IAW CRJ200 SRM 51-42-06 PG 11. 2 L 7 2 4F RT A21EA 2007112600113 20071126 00113 EA 2007 11 26 SWIA200718839 1 20070727 A 5310 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 338 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 PAX DOOR FRAME IS CRACKED STA 338, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS ON PAX DOOR PER REO 601R-52-11-402 REV G. 2 L 7 2 4F RT A21EA 2007112600114 20071126 00114 EA 2007 11 26 SWIA200718840 1 20070727 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 559 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 CARGO FLOOR SUPPORT STRUCTURE IS CRACKED AT FS 559 + 90 AND RBL27 ON INBD SIDE, DISCOVERED AT C-CHECK. COMPLIED WITH RE PAIR PER CRJ200 SRM 53-00-43. 2 L 7 2 4F RT A21EA 2007112600115 20071126 00115 EA 2007 11 26 SWIA200718841 1 20070727 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 RIGHT ENGINE AFT MOUNT THRUST FITTING BALL RACE IS CORRODED, DISCOVERED AT C-CHECK. REPLACED RIGHT ENGINE AFT MOUNT THR UST FITTING ASSEMBLY IAW CRJ200 AMM 71-22-01-000-801 AND 71-22-01-400-801. 2 L 7 2 4F RT A21EA 2007112600116 20071126 00116 EA 2007 11 26 SWIA200718842 1 20070727 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 LEFT ENGINE AFT MOUNT FITTING BALL BEARING IS CORRODED, FOUND AT C-CHECK. REPLACED LEFT ENGINE AFT MOUNT FITTING PER CR J200 AMM 71-22-01-000-801. 2 L 7 2 4F RT A21EA 2007112600117 20071126 00117 EA 2007 11 26 SWIA200718843 1 20070727 A 7120 BOLT CNDAIR CL600 CL6002B19 1900309 EA ENGINE MOUNT SCORED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 RIGHT ENGINE FORWARD MOUNT BOLTS SHOW SIGNS OF SHANK SCORING BELOW HEAD OF BOLT, FOUND AT C-CHECK. REPLACED FORWARD ENG INE MOUNT BOLTS PER CRJ200 AMM SUBTASK 71-00-00-420-001 PARA A ITEMS 15-20. 2 L 7 2 4F RT A21EA 2007112600120 20071126 00120 EA 2007 11 26 SWIA200718846 1 20071104 A 3350 20131A POWER SUPPLY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 461SW 16110 14814 7811 FLT 3820 - EXIT ROW EMERGENCY LIGHT IS INOP. REPLACED ELBP NR 3. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007112600122 20071126 00122 SO 2007 11 26 SWIA200718848 1 20071106 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 308SW 120326 FLT 5561 - RED EMERGENCY LIGHTS ON FLOOR ARE INOP. REPAIRED WIRES AT RED EMERGENCY LIGHT FIXTURE. 2 L 7 2 4T RT A31SO 2007112600123 20071126 00123 EA 2007 11 26 SWIA200718849 1 20071105 A 3230 750005000 VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG SELECTOR MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 952SW 7805 FLT 6386 - ON APPROACH, GOT A "GEAR DISAGREE" WARNING MESSAGE AND MAIN GEAR WERE NOT SHOWING GREEN. PERFORMED A MANUAL EXTENSION. REPLACED MAIN LANDING GEAR SELECTOR VALVE IAW CRJ MM 32-32-10. 2 L 7 2 4F RT A21EA 2007112600124 20071126 00124 EA 2007 11 26 SWIA200718850 1 20071110 A 2613 WIRE CNDAIR CL600 CL6002B19 1900309 EA OVERHEAT OUT OF POSITION A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 928SW 7701 FLT 6723 - ANTI-ICE DUCT WARNING MESSAGE APPEARED AND WOULD NOT CLEAR. REPOSITIONED SENSOR WIRE. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007112600126 20071126 00126 2007 11 26 SWIA200718852 2 20071108 A 7261 ENGINE CNDAIR CL600 CL6002B19 1900309 EA RIGHT LEAKING A SWIA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 07 457SW 7773 AFTER LIFT OFF GOT "SMOKE TOILET" CAUTION MESSAGE ALONG WITH SMOKE IN THE CABIN. FOUND ENGINE OIL LEAKING INTO BLEED SY STEM. REPLACED RIGHT ENGINE IAW AMM 71-00-00. OPS AND LEAK CHECK GOOD, P/N: CF34-3B1, S/N OFF: 872864. 2 L 7 2 4F RT A21EA 2007112600127 20071126 00127 EA 2007 11 26 SWIA200718853 1 20071109 A 2913 6619003 PUMP CNDAIR CL600 CL6002C10 1390015 EA HYD SYSTEM LEAKING A SWIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 340CA 145 145 10062 FLT 4035 - HYDRAULIC SYSTEM NR 2 QUANTITY INDICATION SHOWS 0 PERCENT. REPLACED NR 2 ENGINE DRIVEN PUMP IAW AMM 29-11-01 . 2 L 7 2 4F RT A21EA 2007112600129 20071126 00129 2007 11 26 SWIA200718855 2 20071105 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA RIGHT LEAKING A SWIA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 07 452SW 7716 FLT 3909 - AFTER ROTATION, RECEIVED A "SMOKE TOILET" MESSAGE ALONG WITH SMOKE IN THE CABIN. FOUND ENGINE OIL MIGRATING INTO THE BLEED SYSTEM. REPLACED RIGHT ENGINE WITH SERVICEABLE UNIT IAW CRJ 200 MM 71-00-00. ALL OPS CHECK AND LEAK CHE CKS GOOD, PN CF34-3B1, SN/OFF 873574. 2 L 7 2 4F RT A21EA 2007112600130 20071126 00130 EA 2007 11 26 SWIA200718856 1 20071104 A 5210 CONTROL ROD CNDAIR CL600 CL6002B19 1900309 EA DOOR VENT BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 408SW 7055 PAX DOOR OUTER HANDLE WILL NOT CLOSE FROM INSIDE AIRPLANE. (FLIGHT #3810) ADJUSTED PRESSURE VENT FLAP CONTROL ROD IAW 5 2-11-15. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007112600131 20071126 00131 NM 2007 11 26 F3LA200700316 1 20071101 A 5330 SKIN AIRBUS A319 A319111 3930336 NM FUSELAGE DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 946FR 2763 DURING C-1 CHECK, INSPECTION REPORTED COMPLIANCE WITH RW0000967, "DENT ABOVE LT COCKPIT WINDSHIELD". REMOVED DAMAGED AR EA, PERFORMED HFEC INSPECTION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-11-11 AND EA A9-53R-12248. 2 L 7 2 4F RT A28NM 2007112600133 20071126 00133 NM 2007 11 26 QXEA200701719 1 20071113 A 3222 STRUT BOMBDR DHC8 DHC8402 1390042 NM NLG LEAKING A QXEA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 405QX 4047 RNO FLIGHT NR 2258: DURING TAXI OUT TO THE DEPARTURE RUNWAY, COMPANY ADVISED THAT FLUID WAS FOUND WHERE THE NOSE GEAR WA S PARKED EARLIER AT THE GATE. UPON RETURN TO THE GATE, THE NOSE GEAR WAS FOUND FULLY COMPRESSED AND A TRACE AMOUNT OF F LUID WAS FOUND LEAKING NEAR THE NOSE GEAR/TUG HOOK UP. MAINTENANCE C/W NITROGEN SERVICE IAW Q400 MM TASK 12-10-32-610-8 01. NO LEAKS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007112600134 20071126 00134 NM 2007 11 26 2007UALA04655 1 20071111 A 2800 UNKNOWN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE UNKNOWN A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 325UA 23957 AT 0145Z FLT CREW REPORTED POTENTIAL FUEL LEAK WITH NO FLUID VISIBLE TO THE CREW. CAPTAIN DECLARED AN EMERGENCY WITH AT C. AMBER ALERT DECLARED BY DISPATCHER. FOUND NR 2 DTCU OUT OF ADJUSTMENT. READJUSTED. 2 L 7 2 4F 4 F RT A16WE E2GL 2007112600135 20071126 00135 NM 2007 11 26 2007UALA04656 1 20071110 A 2750 ACTUATOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FLAPERON NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 781UA 26945 RAN RT FLAPERON POSITION TEST AND RESULT WAS FAILURE OF RT OTBD FLAPERON ACTUATOR TO ACHIEVE COMMANDED POSITION. RAN R IGHT FLAPERON POSITION TEST AND RESULT WAS FAILURE OF RH OTBD FLAPERON ACTUATOR TO ACHIEV E COMMANDED POSITION. INSTALLE D NEW FLAPERON ACTUATOR AND SYSTEM CHECKED OK FOR SERVICE. SUSPECT STICKING DUE TO DEBRIS BUILDUP. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007112600136 20071126 00136 EA 2007 11 26 TRAX200701710 1 20071110 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 875AS 7559 LT 1ST EMERGENCY LIGHT ON FUSELAGE INOP. 2 L 7 2 4F RT A21EA 2007112600141 20071126 00141 SO 2007 11 26 SIMA200731804 1 20071114 A 3320 BR900022 BALLAST EMB 135 EMB135KL 3260302 SO LAVATORY LIGHTS SMOKE A SIMA B A EMER. DESCENT UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 807AE 145506 ABOUT 500' AFTER TAKEOFF 'LAV SMOKE' WARNING ILLUMINATED. WARNING LIGHT WENT OFF ON FINAL APPROACH, FA REPORTED SMOKE I N CABIN. TOUCHDOWN WAS SOFT. REMOVE AND REPLACED BOTH LAVATORY BALLAST IAW 140 AMM 33-28-02. OPS CHECK GOOD. AIRCRAF T RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007112600142 20071126 00142 SO 2007 11 26 SIMA200731805 1 20071114 A 5320 14521700001 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 669MB 145788 DURING IMBV INSPECTION, FOUND LEFT OMEGA BEAM CORRODED AT FRAME 24-25 CROSSMEMBER. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007112600145 20071126 00145 SO 2007 11 26 SIMA200731807 1 20071114 A 5320 14521725013 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 669MB 145788 DURING IMBV INSPECTION, FOUND AFT SVC DOOR SILL IS CORRODED BETWEEN FR 21-22. REPAIRED SILL IAW SRM 53-21-10. A/C RETU RNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007112600146 20071126 00146 SO 2007 11 26 SIMA200731806 1 20071114 A 5320 14521725013 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 669MB 145788 DURING IMBV INSPECTION, FOUND FWD SERVICE DOOR SILL BETWEEN FR 18-20. CORRODED REPAIRED FWD SILL IAW SRM 53-21-10. A/C RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007112600147 20071126 00147 EU 2007 11 26 07FDEA04778 1 20071113 A 5343 TRUNNION AIRBUS 310 A310203 3930313 EU RT MLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 RT MLG TRUNNION RIB 5 FWD LUG AFT FACE APPEARS TO BE CRACKED. SPOT FACE AND CHAMFERED ON E.O. 6-5710-7-5010 PT8 - NO C RACKS FOUND. 2 L 7 2 4F RT A35EU 2007112600149 20071126 00149 NM 2007 11 26 07FDEA04780 1 20071113 A 5754 STRUCTURE DOUG MD11 MD11F 3023600 NM NR 4 SLAT DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 RIGHT WING NR 4 SLAT LEADING EDGE FOUND DENT. REPAIR CARRIED OUT AT RIGHT HAND WING NR 4 SLAT LEADING EDGE DENTED AREA AS PER SRM 57-10-00 FIGURE 5 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007112600150 20071126 00150 NM 2007 11 26 07FDEA04781 1 20071113 A 5730 ACCESS PANEL DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 RIGHT WING LEADING EDGE ACCESS PANEL 619CB INBOARD FORWARD CUTOUT FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 57-10-0 0 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007112600151 20071126 00151 NM 2007 11 26 07FDEA04782 1 20071113 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM NLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 LEFT NOSE LANDING GEAR TRUNNION FITTING FWD LOWER CORNER FOUND CRACKED. REPAIRED AS PER SRM 53-40-00 FIGURE 23 VOLUME I . REPETITIVE INSPECTION REQUIRED FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS. REPAIR CLASSIFIED AS MAJOR PE R GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007112600154 20071126 00154 NM 2007 11 26 07FDEA04786 1 20071114 A 5230 65C80736690 CASTING BOEING 727 727225 1384077 NM CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 MAIN DECK 1L DR CUT OUT LWR HINGE UPPER STOP PLATE SUPPORT CASTING IS CORRODED AT FASTENER HOLE, BS 307, STR 13R, WL 238 . REMOVED FITTING RER SRM 51-30-2, SENT TO HAVE NEW CASTING MATCHED DRILLED UP FOR BEARING PLATED AND INTO PLACE PER S RM 51-30-5 PG 1,2. INSTALLED FITTING PER SRM 51-30-2. 2 L 7 3 4F A3WE 2007112600155 20071126 00155 NM 2007 11 26 07FDEA04787 1 20071114 A 5320 53FX1285 TENSION TIE BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 FOUND CLIP CRACKED AT FS 480 AND STR 2. REMOVED FASTENERS IN LOWER WEB. REMOVED CRACKED TENSION CLIP, FABRICATED NEW T ENSION CLIP AND INSTALLED NEW TENSION CLIP AND FASTENERS IN LOWER WEB. REFERENCE DRAWING NR 53FX1285 AND SRM 51-30-02 C LASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007112600156 20071126 00156 NM 2007 11 26 07FDEA04788 1 20071114 A 5320 6525579252 SUPPORT BOEING 727 727225 1384077 NM BS 720C CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 BODY FAIRING FRAME SUPPORT LOCATED RIGHT OF AIR CONDITION HOOK UP IS CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIM ITS, ORIGINAL .040". REMOVED .023", REMAINING .014 IAW 53-101, TOOL AAR 10274 CAL DUE 12-27-07. REMOVED FAIRING AND BR ACE. FABRICATED, DRILLED, AND TREATED AND PRIMED NEW BRACE. REINSTALLED FAIRING AND BRACE IAW SRM 51-30-2, 51-10-2, A ND BOEING DRAWING 65-22579. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2007112600160 20071126 00160 EA 2007 11 26 A6WA200740588 1 20071014 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 469AW 7917 LT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT 510AB, WS 12.245, HOLE NR 2 HAS PITTING CORROSION AT INBOARD AND OUTBOA RD ENDS IN NON-CRITICAL AREA MEASURES APPROX 9.5 INCH LONG BY .25 INCH WIDE BY .005 INCH DEEP AND 3.5 INCH LONG BY .20 I NCH WIDE BY .007 INCH DEEP. MAINTENANCE REPAIRED IAW AWAC EO E06/021/457 AND BOMBARDIER REO 601R-57-030 REV F. (M) 2 L 7 2 4F RT A21EA 2007112600162 20071126 00162 EA 2007 11 26 A6WA200740590 1 20071015 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 469AW 7917 RIGHT WING LOWER PLANK FUEL ACCESS DOOR CUTOUT 650BB, WS 54.897, HOLE NR 1, HAS PITTING CORROSION ON INBOARD AND OUTBOAR D ENDS IN NON-CRITICAL AREA MEASURES APPROX 10.5 INCH LONG BY .25 INCH WIDE BY .009 INCH DEEP AND 5.5 INCH LONG BY .25 I NCH WIDED BY .006 INCH DEEP. MAINTENANCE REPAIRED IAW AWAC EO E06/021/457 AND BOMBARDIER REO 601R-57-21-030 REV F. (M) 2 L 7 2 4F RT A21EA 2007112600163 20071126 00163 EA 2007 11 26 A6WA200740591 1 20071017 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA RIGHT ODOR A A6WA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 445AW 7804 ODOR AND HAZE DETECTED IN CABIN, SMOKE TOILET CASS MESSAGE NO VISIBLE SIGN OF SMOKE IN LAV. TURNED OFF RIGHT PACK AND C ASS MESSAGE WENT AWAY AS DID HAZE AND ODOR. TROUBLESHOT PER FIM, 79-20-0. REMOVED AND REPLACED COALESCER SOCKS ON LT A ND RT SIDE. OPS CHECK OF PACK GOOD. NO ODOR OR HAZE NOTED. (M) 2 L 7 2 4F RT A21EA 2007112600165 20071126 00165 EU 2007 11 26 USAA920071117 1 20071112 A 3397 CONNECTOR AIRBUS A321 A321211 3930370 EU EMERGENCY LIGHTS UNSECURE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 173US 1481 TPA - EEL - AFT LEFT EMERGENCY EXIT POWER SUPPLY FAILED DURING SYSTEM TEST DURING WEEKLY CHECK. MAINTENANCE RESECURED M ISALIGNED PIN IN ATTACH CONNECTOR AT AFT EPSU. TEST SEVERAL TIMES, SHOWED "TEST OK" MESSAGE EACH TIME. 2 L 7 2 4F RT A28NM 2007112600166 20071126 00166 EA 2007 11 26 A6WA200740598 1 20071104 A 2700 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA FLT CONTROLS MALFUNCTIONED A A6WA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 31 434AW 7322 ABORTED TAKEOFF PRIOR TO 80 KNOTS DUE TO TAKEOFF WARNING FOR CONFIG TRIM, CONFIG SPOILERS AT WEIGHT OF APPROXIMATELY 46, 000 LBS. WHEN MESSAGE CLEARED AILERON AND RUDDER TRIM INDICATIONS FLUTTERED FROM WHITE TO GREEN. PERFORMED NUMEROUS, O PS CHECKS OF FLIGHT CONTROLS, PERFORMED TAXI RUN, NO DEFECTS NOTED AT THIS TIME, ALL INDICATIONS NORMAL. (M) 2 L 7 2 4F RT A21EA 2007112600169 20071126 00169 EA 2007 11 26 A6WA200740595 1 20071024 A 2800 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA FUEL SYSTEM MALFUNCTIONED A A6WA O OTHER O OTHER DE DESCENT 1 GL 31 467AW 7900 AFTER TAKEOFF RT TRANSFER SHUT OFF VALVE CAUTION MESSAGE ILLUMINATED AS WELL AS FUEL CHANNEL 1 STATUS MESSAGE. LOST RT ANF AND TOTAL FUEL IND (AMBER DASHES) CENTER TANK INDICATED 0 DURING FLIGHT AUTO CROSSFLOW INHIBIT STATUS MSG ILLUMINATE D DURING FINAL APPROACH R X-FLOW SOV CAUTION AND CROSSFLOW/APU PUMP MESSAGE ILLUMINATED AND ALL FUEL QTY READOUTS DASHED AMBER ON GROUND CHECK AUTO CROSSFLOW INHIBIT SWITCH WAS IN NORMAL POSITION AND EMERGENCY WAS DECLARED. REMOVED AND REP LACED FUEL SYSTEM COMPUTER IAW CRJ200 AMM 28-41-16. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007112600170 20071126 00170 EU 2007 11 26 TRAX200701629 1 20071029 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 ETNRC-200-120 SEAT TRACK LT I/B BTW FR 29 AND 39 CORRODED, (RESOLVED ON W/O: 74559 TASKCARD: N/R-0018). REMOVED CORROSI ON ON SEAT TRACK LT I/B BTW FR 29 AND FR 39 AS PER SRM 53-00-00. FABRICATION COVERED ON W/C 2000-203 SEAT TRACK. REPLA CED IAW SRM 51-25-04, MATERIAL THICKNESS: 0.083 MATERIAL REMOVED: 0.027 OUT OF LIMITS AS PER SRM: 53-00-00 FIG 304. 2 H 7 2 4T RT A53EU 2007112600171 20071126 00171 EU 2007 11 26 TRAX200701714 1 20071025 A 5310 SEAL AEROSP ATR72 ATR72212 8680945 EU TAIL BUMPER CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 TAIL BUMPER SURROUND SEAL (DOUBLER) CORRODED. 2 H 7 2 4T RT A53EU 2007112600172 20071126 00172 NM 2007 11 26 QXEA200701720 1 20071112 A 5210 85217555003 SEAL BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR LOOSE A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 424QX 4006 RDD FLIGHT: AFT PAX DOOR HARD TO OPERATE WITH DOOR SEAL PROTRUDING. MAINTENANCE PERFORMED DOOR ADJUSTMENT AND REMOVED A ND REPLACED THE DOOR SEAL. AFT PAX DOOR OPERATES AND PRESSURE CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007112600173 20071126 00173 NM 2007 11 26 QXEA200701721 1 20071108 A 2931 9669951 PRESSURE SWITCH BOMBDR DHC8 DHC8402 1390042 NM NR 1 HYD SYSTEM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 423QX 1471 2 4153 RNO FLIGHT NR 2447: NR 1 ENGINE HYD PUMP ILLUMINATED ON CLIMB AFTER TAKEOFF. ALL HYD QTY/PRESSURE INDICATES NORMAL AFTE R RUNNING CHECKLIST. MAINTENANCE REMOVED AND REPLACED NR 1 ENG HYD WARNING PRESSURE SWITCH IAW AMM 29-30-16-400-801. O PS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007112600175 20071126 00175 EU 2007 11 26 USAA920071142 1 20071110 A 5320 D5347218820400 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 658AW 1110 PIT - MAJOR REPAIR - BC6, CORROSION ON CABIN FLOOR SUPPORT, BS 3158/FR 66 - BS 3257/FR 68. REPLACED CABIN FLOOR SUPPORT , BS 3158/FR 66 - BS 3257/FR 68 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007112600176 20071126 00176 NM 2007 11 26 USAA920071143 1 20071107 A 5320 146N52468 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 200UU 27809 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR CHANNEL, BS 1640 - BS 1660, RBL 58, WL 208. REPLACED C ABIN FLOOR CHANNEL, BS 1640 - BS 1660, RBL 58, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007112600178 20071126 00178 NM 2007 11 26 USAA920071146 1 20071107 A 5320 146N52421 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 200UU 27809 MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON CABIN FLOOR CHANNEL, BS 1640 - BS 1660, BL 0, WL 208. REPLACED CABIN FLOOR SUPPORT, BS 1640 - BS 1660, BL 0, WL 208 IAW 757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007112000021 20071120 00021 NM 2007 11 20 07FDEA04737 1 20071107 A 2571 65298685 BATTERY BOX BOEING 727 727225 1384077 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 E/E COMPARTMENT CRADLE (TRAY ASSY) IS CRACKED AT FWD RT CORNER REMOVED AND REPLACED BATTERY TRAY ASSY REF SRM 51-30-2, T HIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2007112000022 20071120 00022 NM 2007 11 20 WRLA2007119 1 20071031 A 5245 SKIN DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE ACCESS DOOR CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING C CHECK INSPECTION FOUND CRACK IN RIGHT HAND NR 3 AIR CONDITION COMPARTMENT DOOR OUTER UPPER SKIN L=4". REF EGAT NRC U05001. REPAIRED RIGHT NR 3 AIR CONDITION COMPARTMENT DOOR OUTER UPPER SKIN PER MD-11 SRM VOL 1 52-10-00 FIG 1 REV 40. 2 L 7 3 4F 4 F RT A22WE E24NE 2007112000023 20071120 00023 CE 2007 11 20 110607N336CS1 1 20071106 A 3230 615101 BYPASS VALVE CESSNA 500 550 2076604 CE PWA 530 PW530A NE TAILCONE FAULTY E Z5FA O OTHER J WARNING INDICATION AP APPROACH 1 EA 63 336CS 2898 5501095 WHEN LANDING GEAR WAS EXTENDED, NO LT GEAR DOWN INDICATION OBSERVED. CREW FOLLOWED EMERGENCY PROCEDURES AND BLEW GEAR DO WN AND DECLARED EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. PRIOR TO LANDING, THE LT MAIN GEAR GREEN DOWN INDICATION I LLUMINATED. AIRCRAFT CURRENTLY IN MAINTENANCE FOR TROUBLESHOOTING. MAINTENANCE PERSONNEL FOUND OPEN CENTER BYPASS VALVE TO BE THE CAUSE OF LEFT MAIN GEAR EXTENTION DELAY. REPLACED VALVE, PERFORMED GEAR RETRACTION TEST SATISFACTORILY. AIRCR AFT RETURNED TO SERVICE. 1 L 7 2 4F 4 F A22CE E00053EN 2007112000024 20071120 00024 SO 2007 11 20 CHQA200700070 1 20071105 A 2750 FLAP SYSTEM EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL TE FLAPS MALFUNCTIONED A CHQA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 GL 11 262SK 145168 CAE312351 CLE TO MSP - ON APPROACH TO MSP, THE FLAPS WERE EXTENDED TO 9 DEGREES AND A MASTER CAUTION APPEARED EICAS MESSAGE APPEAR ED STATING FLAP FAIL. AFTER RUNNING THROUGH THE QRH THE AIRCRAFT LANDED WITHOUT INCIDENT AND WAS TURNED OVER TO MAINTEN ANCE. MAINTENANCE RESET THE FLAP SYSTEM AND PERFORMED SEVERAL OPERATIONAL CHECKS OF THE FLAP SYSTEM AND FOUND NO DEFECT S. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007112000025 20071120 00025 SO 2007 11 20 CHQA200700071 1 20071106 A 2750 3631001005 ELECTRONIC UNIT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL TE FLAPS MALFUNCTIONED A CHQA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 GL 11 262SK 18146 3057 145168 CAE312351 PHL TO CLE - UPON STARTING APPROACH INTO CLE, THE FLAP HANDLE WAS MOVED TO 9 DEGREE POSITION AND A FLAP FAIL EICAS MESSA GE WAS DISPLAYED. THE FLAPS HAD FAILED AT THE 0 DEGREE POSITION. THE APPLICABLE QRH PROCEDURES WERE PERFORMED AND THE AIRCRAFT PROCEEDED TO LAND AT CLE. ON LANDING ONLY ONE THRUST REVERSER DEPLOYED AND THE EICAS MESSAGE "ENG 2 REV DISAGR EE" WAS DISPLAYED. THE AIRCRAFT WAS STOPPED ON THE RUNWAY AND TAXIED BACK TO THE GATE UNEVENTFULLY.MAINTENANCE INTERRO GATED THE CMC FOR FAULT MESSAGES AND FOUND NO CMC MESSAGES RELATING TO THE FLAP SYSTEM. MAINTENANCE THEN REPLACED THE L EFT HAND FLAP VELOCITY SENSOR, THE FLAP ELECTRONIC CONTROL UNIT, AND PLACED THE THRUST REVERSER ON MEL. THE AIRCRAFT WA 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007112000031 20071120 00031 2007 11 20 07FDEA04754 4 20071108 A 2230 K151AEM0 AUTOTHRUST SYS AIRBUS 300 A300B4622R 3930312 EU FAILED A FDEA E ENGINE SHUTDOWN S AFFECT SYSTEMS TO TAKEOFF 1 SO 25 721FD 477 ON TAKEOFF ROLL LIMC 17R ACCELERATED TO 120KTS CAPTS PFD WENT TOTALLY BLANK, FOLLOWED BY BOTH ATS SWITCHES DISENGAGING. HIGH SPEED ABORT FOLLOWED BY RTO V LIST. TAXI BACK TO GATE. ACN RELEASED FOR SERVICE PER MEL/CDL: 22-30-01-C ATS 1 A ND 2 - INOP. ALL THRUST SETTINGS MUST BE MANUALLY SET. NO OPS WITHIN METRIC AIR. SWAPPED CAPTAIN'S PFD WITH RT ECAM DISPLAY AS PER MM 34-74-22-4. ALL TEST PASSED. R&R AS REQUESTED FAC/ATS ENGAGE UNIT AS PER AMM: 22-25-12-4.AFS/LAND TES T PERFORMED. ALL PASSED. STICKER REMOVED. 2 L 7 2 4F RT A35EU 2007112000032 20071120 00032 2007 11 20 UPS07851138 4 20071109 A 2565 SLIDE DOUG DC8 DC871F 302199D WP DISLODGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:N/A SLIDE FELL OUT OF CASE ON DOOR OPENING. DEFERRED PER MEL 52-7-4. PLACARD INSTALLED. SLIDE IS REMO VED. REINSTALLED FORWARD ENTRANCE DOOR ESCAPE SLIDE PER MM 25-60-01-2. OPS CHECKS NORMAL. 2 L 7 4 4F RT 4A25 2007112000033 20071120 00033 EU 2007 11 20 07FDEA04759 1 20071109 A 5311 FRAME AIRBUS 310 A310203 3930313 EU ZONE 200 GOUGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 402FE 201 MAIN CABIN FR55 AT APPROX L15L HAS A PUNCTURE IN FLANGE OF FRAME. CUTOUT DAMAGE AND REPAIRED WITH REINFORCING PLATE/REP AIR DOUBLER IAW A310 SRM 53-10-13 PAGE 206-209 FIGURE 202. 2 L 7 2 4F RT A35EU 2007112000034 20071120 00034 EU 2007 11 20 07FDEA04770 1 20071111 A 5311 FRAME AIRBUS 310 A310203 3930313 EU DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 FWD E/E BAY FRAME 14 RT VERTICAL LEG HOLE LABELED "A" DAMAGED FABRICATED AND INSTALLED 2. REPAIR BUSHINGS IAW FED EX EA 6-5310-109224 "FUSELAGE-MAINFRAME-O.S. HOLES IN NLG WHEEL WELL CROSSMEMBER-REPAIR" BY TIMCO EMP NR 110294/QC254. 2 L 7 2 4F RT A35EU 2007112000044 20071120 00044 NM 2007 11 20 2007UALA04636 1 20071112 A 3350 S479W2302 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE AFT GALLEY BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 219UA 30551 EEL LIGHT STRIP IS BROKEN IN AFT GALLEY BY CART 400. REPLACED BROKEN LIGHT STRIP. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007112000045 20071120 00045 NM 2007 11 20 2007UALA04638 1 20071110 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 SEATS 4A FWD & 58 EMERGENCY LIGHTS ARE INOPERATIVE. RELAMPED EMERGENCY LIGHTS, CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112000046 20071120 00046 NM 2007 11 20 2007UALA04641 1 20071110 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 ZONE-B CEILING EMERGENCY LIGHT IS INOP. RELAMPED EMERGENCY LIGHT, CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112000047 20071120 00047 NM 2007 11 20 2007UALA04644 1 20071111 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 181UA 25278 AFT CARGO DOOR CUTOUT UPPER FWD CORNER, 1 EACH FASTENER HOLE CRACKED. MAJOR REPAIR ACCOMPLISHED: INSTALLED EXTERNAL DO UBLER, TRIPLER & QUADRUPLER REPAIRS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112000049 20071120 00049 NM 2007 11 20 KCSA071522 1 20071114 A 5720 ANGLE BOEING 747 747246F 1384850 NM RT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 RIGHT WING L/E CAVITY I/B OF FS-1318 HAS CORROSION ON ANGLE AT L/E WEB DOUBLER LOWER AT ATTACH POINT. 2 L 7 4 4F RT A20WE 2007112000050 20071120 00050 WP 2007 11 20 07FDEA04798 1 20071115 A 5420 777119105 BOLT DOUG MD10 MD1010F 3022112 WP NR 3 NACELLE SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68049 47803 DURING B CHECK, RT WING NR 3 ENGINE PYLON TOMBSTONE FITTING, FOUND 2(EA)3/8 DIAMETER BOLTS AT LOWER SPHERICAL BEARING SH EARED OFF. REMOVED AND REPLACED QTY (6) 77711-9-105 INCONEL BOLTS,AUB7125-1 PLATE ASSY AND AUB7126-501 RETAINER ASSY PER MM 54-00-01 AND GMM 1-1-600. 2 L 7 3 4F RT A22WE 2007112100014 20071121 00014 NM 2007 11 21 CALA0700679 1 20071110 A 5313 6551628Y29 STRINGER BOEING 737 7373T0 1384582 NM BS 980-996 S27L CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND STRINGER 27L CORRODED AT STA 980-996. THE CORRODED SECTION OF STRINGER WAS CUT OUT AND A REPAIR WAS IN STALLED IAW SRM 53-00-03, REPAIR 1. 2 L 7 2 4F RT A16WE 2007112100021 20071121 00021 NM 2007 11 21 SWAA075664 1 20071111 A 3350 767 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 285WN 32536 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007112100023 20071121 00023 2007 11 21 SWAA075665 4 20071112 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007112100030 20071121 00030 EA 2007 11 21 TRAX200701693 1 20071106 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 883AS 7504 AAR - FS 280 FLOOR SUPPORTS CRACKED O/B OF RBL 9.0. PERFORMED REPAIR TO FS 280.0 BULKHEAD AT RBL 9.0 PER: REO 601R-53-1 1-171, REV D, IAW EO 600-53-0090. SUPPLEMENTAL - SDR CLOSED 11/13/07. 2 L 7 2 4F RT A21EA 2007112100039 20071121 00039 NM 2007 11 21 USAA920071116 1 20071021 A 5753 SKIN BOEING 737 7373B7 1384580 NM ZONE 500 DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - LEFT WING OUTBOARD FOREFLAP HAS AREA DEBONDED, WS 206.5 - WS 214.5. REPAIRED LEFT WIN G OUTBOARD FOREFLAP, WS 206.5 - WS 214.5 IAW B737 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 2007112100059 20071121 00059 WP 2007 11 21 ASAA0782219 1 20071108 A 5321 99366403 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 887-927 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 977AS 53453 CABIN FLOOR PANEL DELAMINATED STA 887 TO STA 927 RBL 22 TO RBL 44. FABRICATED A REPLACEMENT FLOOR PANEL IAW MD80 SRM 53 -05 PAGES 251 THRU 257 AND DAC DRAWING S4932106. 2 L 7 2 4F RT A6WE 2007112100064 20071121 00064 WP 2007 11 21 ASAA0782225 1 20071109 A 5321 995792117 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 826-927 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 977AS 53453 CABIN FLOOR PANEL PUNCTURED DENTED APPROX IN MIDDLE OF PANEL STA 826 TO STA 927 LBL 44 TO LBL 54. REMOVED DAMAGED AREA, FABRICATED LOCATED DRILLED AND INSTALLED A REPAIR DOUBLER IAW MD80 SRM 53 01 FIG 4 SHEET 4. 2 L 7 2 4F RT A6WE 2007112100077 20071121 00077 NM 2007 11 21 ASAA0772233 1 20071110 A 5330 147A31103 SKIN BOEING 737 737790 13844CN NM BS 1008 S14L GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 648AS 30662 GOUGE ON FUSELAGE SKIN AT BS 1008 JUST BELOW STR 14 LT. GOUGE ON LT FUSELAGE SKIN AT BS 1008 JUST BELOW STR 14L REPAIRE D IAW CASCADE ERD 7455 AND ASA EA5330 02256. 2 L 7 2 4F RT A16WE 2007112100081 20071121 00081 NM 2007 11 21 ASAA0772238 1 20071110 A 5320 146A75023 CHANNEL BOEING 737 737790 13844CN NM BS 227-847 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 648AS 30662 AFT CARGO LT ZEE CHANNEL BS 847 TO 727 LBL 21 IS CORRODED. AFT CARGO LT ZEE CHANNEL BS 727 TO 847 LBL 21 REPAIRED IAW B 737 700 SRM 53-00-53 REPAIR 5. 2 L 7 2 4F RT A16WE 2007112100082 20071121 00082 NM 2007 11 21 ASAA0772239 1 20071106 A 5320 1434948535 SUPPORT BOEING 737 737790 13844CN NM BS 500D CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 648AS 30662 FWD CARGO AFT BLKHD SUPPORT RAIL CORRODED BS 500D RBL 21 TO LBL 21. REPLACED WITH NEW PART IAW B737 700 SRM 51-40-02, 5 1-40-05. 2 L 7 2 4F RT A16WE 2007112100103 20071121 00103 NM 2007 11 21 2007UALA04615 1 20071109 A 3397 TERMINAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LV2 TRANSFORMER DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 336UA 24240 LV2 TERMINAL AT MAIN TRANSFORMER NR 1 BURNED AND DAMAGED. FOUND GROUND STUD LOCATED AT T36 TRANSFORMER BURNT. UNKNOWN AS TO EXACT CAUSE OF BURN. REPLACED GROUND STUD AT T36 AND ASSOCIATED WIRING. REINSTALLED J5 BOX AND OPS CHECK TRIM SYSTEM DUE TO REMOVAL OF BOX. ALL LIGHTS NORMAL AT THIS TIME. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112100106 20071121 00106 NM 2007 11 21 2007UALA04618 1 20071108 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 246 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 STA 246, LBL 26, FLOORBEAM VERTICAL STIFFENER IS CRACKED. REMOVED & REPLACED VERTICAL STIFFENER. 2 L 7 2 4F 4 F RT A1NM E24NE 2007112100110 20071121 00110 EU 2007 11 21 2007UALA04625 1 20071109 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN ODOR A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 486UA 1620 F/A REPORTS STRONG ELECTRICAL ODOR ROW 13. TURNED OFF VIDEO LIGHTS, ODOR GONE. COULD DUPLICATE ON GROUND. TURNED ON VIDEO AND ALL CABIN AND READING LIGHTS, AND CHECKED UNDERSEAT AREAS AT ROW 13 NO DEFECTS OR ODORS NOTED. CHECKED AVIONIC S EQUIPMENT BAYS ALSO AND NO ELECTRICAL ODORS FOUND. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112100135 20071121 00135 NM 2007 11 21 WRLA2007122 1 20071106 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING C-CHECK INSPECTION FOUND CORROSION AFT FUSELAGE FLOOR SUPPORT AT STA Y=2007 X=23.5. REPLACED DAMAGED FLOOR SUP PORT PER SRM 51-31-01. 2 L 7 3 4F 4 F RT A22WE E24NE 2007112100136 20071121 00136 SO 2007 11 21 C2XA07RI099 1 20071113 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13964 14767 719 145123 FLT 2882 - EWR - CREW REPORTED EMERGENCY FLOOR STRIPS INOPERATIVE. EWR MX REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATT ERY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007112100142 20071121 00142 EU 2007 11 21 USAA920071138 1 20071110 A 5540 D5537131800000 HINGE FITTING AIRBUS 320 A320232 3930326 EU ZONE 300 WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 657AW 1083 SAL - MAJOR REPAIR - BC6 CHECK - RUDDER HINGE FITTING NR 1 WORN, VERTICAL STABILIZER STATION 780 / RIB 2. REPLACED RUDD ER HINGE FITTING NR 1, VERTICAL STABILIZER STATION 780 / RIB 2 IAW A320 AMM 55-36-41. 2 L 7 2 4F RT A28NM 2007112100143 20071121 00143 EU 2007 11 21 USAA920071139 1 20071110 A 5540 D5537131800200 HINGE FITTING AIRBUS 320 A320232 3930326 EU ZONE 300 WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 657AW 1083 SAL - MAJOR REPAIR - BC6 CHECK - RUDDER HINGE FITTING NR 4 WORN, VERTICAL STABILIZER STATION 2632 / RIB 6. REPLACED RUD DER HINGE FITTING NR 4, VERTICAL STABILIZER STATION 2632 / RIB 6 IAW A320 AMM 55-36-41. 2 L 7 2 4F RT A28NM 2007112100144 20071121 00144 NM 2007 11 21 USAA920071140 1 20071022 A 5311 6545871132A FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, FORWARD SERVICE DOOR CUTOUT AFT FRAME CRACKED, BS 344. REPAIRED FORWARD SERVICE DOOR CU TOUT AFT FRAME, BS 344 IAW USAIRWAYS EA 100022. 2 L 7 2 4F RT A16WE 2007112100147 20071121 00147 NM 2007 11 21 SWAA075669 1 20071113 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 208WN 29856 DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS BROKEN AT ROW 3 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007112100148 20071121 00148 NM 2007 11 21 SWAA075670 1 20071113 A 3350 8100022605 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 232WN 32500 EEPLS ASSY LOOSE AT ROW 1 ABC. SECURED ASSY PER MM. 2 L 7 2 4F RT A16WE 2007112100156 20071121 00156 NM 2007 11 21 SWAA075675 1 20071113 A 5754 65C26602 SKIN BOEING 737 7373H4 1384600 NM NR 6 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED 14Y CHECK, FOUND RT WING NR 6 L/E SLAT OUTBOARD END DELAMINATED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007112100160 20071121 00160 NM 2007 11 21 SWAA075678 1 20071113 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM BS 801 S19L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 801, STR 19L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007112100162 20071121 00162 NM 2007 11 21 SWAA075680 1 20071113 A 5330 6545866 PANEL BOEING 737 7375H4 138449D NM BS 717 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED 16Y CHECK, FOUND RT KEEL BEAM PANEL CRACKED AT BS 717. REPAIRED PANEL PER SRM. 2 L 7 2 4F RT A16WE 2007112100172 20071121 00172 NM 2007 11 21 SWAA075694 1 20071113 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM BS 520 S27R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007112100176 20071121 00176 NM 2007 11 21 SWAA075697 1 20071113 A 5743 115A5211 TRUNNION BOEING 737 7377H4 1384404 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 712SW 27846 DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2007112100177 20071121 00177 NM 2007 11 21 SWAA075698 1 20071113 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 774SW 27882 DURING SCHEDULED MV3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007112100179 20071121 00179 NM 2007 11 21 FDKA200707333 1 20070709 A 3350 BULB DHAV DHC8 DHC8101 2809002 NM NLG INDICATOR BURNED OUT A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 808LR 073 FDM 6180 ALB-JFK. DURING GEAR EXTENSION INTO JFK, NLG DOWN AND LOCKED INDICATOR DID NOT ILLUMINATE. MX FOUND INDICATOR BULB BURNED OUT AND REPLACED. 2 H 7 2 4T RT A13NM 2007112100181 20071121 00181 SO 2007 11 21 FDKA200707341 1 20070719 A 3350 1317 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6203 ATL-CAE (0525 PHX LCL). OVERHEAD EMERGENCY LIGHT AT ROW 8 AND ROW 16 INOP. MX RELAMPED BOTH LIGHTS, OPS GOOD. 2 L 7 2 4T RT T00011AT 2007112100184 20071121 00184 SO 2007 11 21 FDKA200707344 1 20070722 A 3350 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 FDM 6021 ATL. ROW 12 EMERGENCY EXIT SIGN LOOSE. MX RE-SECURED SIGN. 2 L 7 2 4T RT T00011AT 2007112100192 20071121 00192 SO 2007 11 21 C2XA07TY069 1 20071114 A 3350 2013BR BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14923 145318 NR 3 EMERGENCY LIGHT BATTERY INOP. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY IAW EMB 145MM 33-50-04. OPS CHECK GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007112100195 20071121 00195 SO 2007 11 21 RAIA00711007 1 20071108 A 3350 BULB EMB 145 EMB145 3260210 SO EMERGENCY LIGHT BURNED OUT A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 809HK 145187 PRE FLT NR 3558 - PIT - AIRSTAIR EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED EMERGENCY LIGHT AND OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007112100196 20071121 00196 SO 2007 11 21 RAIA00711006 1 20071108 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS UNSECURE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 833HK 145240 PRE FLT NR 7967 - ORD - EMERGENCY LIGHT BEHIND OVERWING EXIT LEFT SIDE INOP. MAINTENANCE RE-SECURED LIGHT SIGN CONNECTO R AND ACCOMPLISHED EMERGENCY LIGHT TEST. 2 L 7 2 4F RT T00011AT 2007112100204 20071121 00204 SW 2007 11 21 WGEA200700019 1 20071101 A 3233 EM411511 ACTUATOR ECLIPS EA500 ECLIPSEEA500 3350000 SW MLG MALFUNCTIONED E WGEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 109DJ 292 000006 LANDING GEAR FAIL AMBER CAS MESSAGE ILLUMINATED ON TAXI IN. FLASHED NUMEROUS TIMES AND CUTOUT NUMEROUS TIMES. REMOVED AND REPLACED RIGHT MLG ACTUATOR WITH A NEW UNIT IAW EA500 AMM 32-30-20. PERFORMED NORMAL EXTENSION AND RETRACTION CHECK , AND EMERGENCY EXTENSION CHECK, ALL CHECKED GOOD IAW EA500 AMM 32-30-00. 1 L 7 2 4J RT A00002AC 2007112600015 20071126 00015 SO 2007 11 26 SIMA200731601 1 20071110 A 2750 3631001011 FCU EMB 135 EMB135LR 3260305 SO TE FLAPS MALFUNCTIONED A SIMA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 21 736DT 145388 FLAPS FAIL EICAS MESSAGE WITH FLAPS STUCK AT 0 DEG. CAPT DECLARE EMERGENCY AND LANDED WITH NO PROBLEMS. REMOVED AND RE PLACED FECU IAW EMB AMM 27-53-02. FLAP OPERATIONAL CHECK IAW AMM 27-53-00 IS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007112600024 20071126 00024 EA 2007 11 26 QXEA200701574 1 20071017 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 C4 PDX - RIVET ROW NEXT TO RECEIVER ANTENNA 1 HAS CORROSION OUTBOARD SIDE. REPAIRED IAW SRM 51-42-06, 51-25-01. 2 L 7 2 4F RT A21EA 2007112600038 20071126 00038 EA 2007 11 26 QXEA200701607 1 20071023 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 379-421 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 C4 PDX - LEFT CENTER CABIN SEAT TRACK NR 9 STATION X379 TO X421 HAS PITTING CORROSION, CHAFE, SCRATCHES. REPAIRED IAW A MM 53-00-49-400-801-A01, 53-00-49-000-801-A01. 2 L 7 2 4F RT A21EA 2007112600044 20071126 00044 NM 2007 11 26 QXEA200701665 1 20071031 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - RIGHT INBOARD SEAT TRACK NR 11 HAS CORROSION AT STATION 47.975. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007112600061 20071126 00061 NM 2007 11 26 QXEA200701685 1 20071031 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 137-141 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - RIGHT OUTBOARD SEAT TRACK HAS LIGHT CORROSION IN BOTTOM OF CHANNEL BETWEEN STATION X137 AND X141. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007112600063 20071126 00063 NM 2007 11 26 QXEA200701678 1 20071102 A 5320 SUPPORT ANGLE BOMBDR DHC8 DHC8402 1390042 NM BS 783 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - AFT CARGO BAY, ANGLE SUPPORT CORRODED AT STATION 783 10" FROM CARGO DOOR LIP. REPAIRED IAW SRM 51-14-00, 51-21 -10, 51-42-05. 2 H 7 2 4T RT A13NM 2007112600067 20071126 00067 NM 2007 11 26 QXEA200701708 1 20071110 A 3010 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM DE ICE SYS UNKNOWN A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 414QX 4061 SEA FLIGHT NR 2321: DEICE PRESSURE CAUTION LIGHT ILLUMINATED. RAN CHECKLIST. LIGHT EXTINGUISHED THEN CAME ON AGAIN. NO TED THAT THE SECOND INDICATOR LIGHT ON THE RIGHT WING WAS SLOW TO ILLUMINATE AND WOULD FLICKER WHEN ILLUMINATED. ALL OT HER INDICATIONS WERE NORMAL. MAINTENANCE PERFORMED FUNCTIONAL TEST OF THE AIRFRAME PNEUMATIC DEICING SYSTEM IAW Q400 AM M 30-11-00-720-801. RAN ALL CYCLES IN MANUAL, ISO, NORM WITH BOTH ENGINES AND NR 1 AND NR 2 INDEPENDENTLY. DEICE PRESS CAUTION DID NOT RETURN. ALL BOOT INDICATIONS AND INFLATION CYCLES CHECK NORMAL. ALL OPS CHECK GOOD AT THIS TIME. NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007112600072 20071126 00072 NM 2007 11 26 QXEA200701691 1 20071031 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 342 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION IN CHANNEL AND ON TOP OF RAILS AT STATION X342. REPAIRED IAW RD8/4-53- 884. 2 H 7 2 4T RT A13NM 2007112600073 20071126 00073 NM 2007 11 26 QXEA200701692 1 20071031 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 350-359 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION IN CHANNEL AND ON RAIL BETWEEN STATION X350 AND X359. REPAIRED IAW RD8 /4-53-884. 2 H 7 2 4T RT A13NM 2007112600075 20071126 00075 NM 2007 11 26 QXEA200701694 1 20071031 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 385-389 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION WITH PITS IN CHANNEL AND LIGHT CORROSION ON TOP OF RAIL BETWEEN STATION X385 AND X389. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007112600088 20071126 00088 NE 2007 11 26 HALA0700485 2 20071112 A 7261 PACKING BOEING 767 7673G5 1385126 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE LEAKING A HALA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 WP 13 584HA 24258 ETOPS SIGNIFICANT SYSTEM, FOUND NR 1 ENGINE LEAKING OIL ON ETOPS CHECK. T/S ENG OIL LEAK PER FIM 71-05-00, FOUND OIL LE AKING FROM FUEL/OIL COOLER BYPASS VLV SOLENOID. REMOVED AND REPLACED "O RINGS" ON BYPASS VALVE SOLENOID PER AMM 79-21-0 3, LEAK CHK GOOD ON GRD ENG RUN, SERVICED ENG OIL TO FULL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007112600096 20071126 00096 NM 2007 11 26 AALA20072164 1 20071106 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 794AN 30256 ORD - EMERGENCY LIGHT AT RIGHT AISLE SEAT ROW 38 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RIGHT HAND AISLE SE AT ROW 83. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007112600099 20071126 00099 NM 2007 11 26 AALA20072162 1 20071106 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 JFK - EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK M33400 FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007112600119 20071126 00119 EA 2007 11 26 SWIA200718845 1 20070727 A 5340 NUT PLATE CNDAIR CL600 CL6002B19 1900309 EA LAV MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 LAVATORY FLOOR NUTPLATES ARE CORRODED, FOUND AT C-CHECK. REPLACED NUTPLATES ON LAVATORY FLOOR. 2 L 7 2 4F RT A21EA 2007112600125 20071126 00125 EA 2007 11 26 SWIA200718851 1 20071108 A 5210 CABLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 958SW 7833 CREW REPORTS PAX DOOR IS HARD TO OPEN AND CLOSE. REPLACED ICE BREAKER CABLE AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007112600128 20071126 00128 EA 2007 11 26 SWIA200718854 1 20071108 A 7120 BUSHING CNDAIR CL600 CL6002C10 1390015 EA ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 613SK 10038 RIGHT ENGINE FORWARD MOUNT LINK BUSHING IS CORRODED. REPLACED LINK AND BUSHING IAW CRJ 700 MM 71-00-00. 2 L 7 2 4F RT A21EA 2007112600148 20071126 00148 NM 2007 11 26 07FDEA04779 1 20071113 A 5410 311N505822 BUSHING BOEING 757 7572B7 1384964 NM NR 1 NACELLE MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 NR 1 PYLON LOWER SPAR FITTING 311N5024-3 ASSY HAS 2, 311N5058-22 BUSHINGS WITH THE INTERNAL BORE NOT PERPENDICULAR TO TH E FITTING. REMOVED BUSHINGS 2 PER SRM 54-50-90. CHECKED LUG PER NTM 51-00-13, NO DAMAGE FOUND. LUG HOLE DIAMETER 1.53 1". FABRICATED 2 NEW BUSHINGS PER SRM 54-50-90, ON MAE TRAVELER NR T7/711482. INSTALLED NEW BUSHINGS 2, PER SRM 54-50- 90. REPAIR NR 5, MACHINED THE INNER DIAMETER OF THE BUSHINGS TO 1.313" PER SRM 54-50-90, REPAIR NR 5. AIRPLANE MANUFAC TURED FEB 1993, LESS THAN 15 YEARS AGO. 2 L 7 2 4F RT A2NM 2007112600159 20071126 00159 NM 2007 11 26 USAABB07090 1 20071114 A 3350 LIGHT BOEING 767 767201 1385125 NM COCKPIT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 246AY 23898 MAINTENANCE FOUND THE COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. NO FURTHER PROBLEMS. 2 L 7 2 4F RT A1NM 2007112600161 20071126 00161 EA 2007 11 26 A6WA200740589 1 20071015 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 469AW 7917 FOUND INTERCOSTAL AT FS 484 IS CRACKED. MAINTENANCE REMOVED CRACKED UNSERVICEABLE INTERCOSTAL CLIP AT FS 484 RBL 27 AND REPLACED WITH NEW SERVICEABLE CLIP, P/N 601R31171-9, IAW BSC 601R-53-0029B AND CRJ SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2007112600179 20071126 00179 NM 2007 11 26 USAA920071147 1 20071113 A 5320 146N53235 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 200UU 27809 MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON CABIN FLOOR CHANNEL, BS 1660 - BS 1681, BL 0, WL 208. REPLACED CABIN FLOOR SUPPORT, BS 1660 - BS 1681, BL 0, WL 208 I/A/W 757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007112600181 20071126 00181 EU 2007 11 26 USAA920071149 1 20071108 A 5344 D5348011900000 HINGE FITTING AIRBUS 320 A320232 3930326 EU R2 DOOR WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 657AW 1083 SAL - MAJOR REPAIR - BC6 CHECK - R2 DOOR LOWER HINGE FITTING WORN ALLOWING THE BEARING TO MIGRATE. REPLACED THE R2 DOOR LOWER HINGE FITTING, BEAM 2-3 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007112600182 20071126 00182 NM 2007 11 26 754002 1 20071112 A 2730 940005013 CONTROL SYSTEM BOEING 747 747228F 1384895 NM ELEVATOR UNSTABLE A Q2SA J A DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 63 754SA 21576 DURING CLIMB-OUT, THE VERTICAL SPEED WHEEL MOVED TO FULL NOSE UP POSITION WITH "B" AUTOPILOT SELECTED. IN CRUISE AUTO S TAB "B" LIGHT ILLUMINATED SEVERAL TIMES. AT FL 340 WITH ALTITUDE HOLD SELECTED, VERTICAL SPEED VARIED +/- 2000 FPM. WIT H AUTOPILOT OFF, THE AIRCRAFT WAS UNSTABLE IN PITCH AXIS. REPLACED INBOARD ELEVATOR CONTROL UNIT AND OPERATIONALLY CHEC KED GOOD. 2 L 7 4 4F RT A20WE 2007112600184 20071126 00184 EA 2007 11 26 SWIA200718858 1 20070823 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT WW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 978SW 7953 BRAKE TRANSDUCER IN LEFT WHEEL WELL IS CRACKED, FOUND AT C-CHECK. INSTALLED BRAKE TRANSDUCER BRACKET PER CRJ200 SRM 51- 42-06 PG 1-18. 2 L 7 2 4F RT A21EA 2007112600185 20071126 00185 EA 2007 11 26 SWIA200718859 1 20070820 A 5320 THRESHOLD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 934SW 7722 ANGLE BELOW CARGO DOOR THRESHOLD HAS EVIDENCE OF CRACKING, FOUND AT C-CHECK. REPLACED ANGLE BELOW CARGO DOOR THRESHOLD PER CRJ200 SRM 51-42-06 PAGE 18. 2 L 7 2 4F RT A21EA 2007112600186 20071126 00186 EA 2007 11 26 SWIA200718860 1 20070820 A 5340 NUT CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 934SW 7722 STA 280 AT RBL 9 INBOARD AND OUTBOARD CLIPS ARE CRACKED, FOUND AT C-CHECK. REPLACED CLIPS AT STA 280 RBL9 PER CRJ200 SR M 51-42-21 PG 17. 2 L 7 2 4F RT A21EA 2007112600187 20071126 00187 EA 2007 11 26 SWIA200718861 1 20070820 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 934SW 7722 STA280 AT LBL9 UPPER BEAM IS CRACKED, FOUND AT C-CHECK. REPAIRED UPPER BEAM CRACK PER CRJ200 REO 601R-53-11-138. 2 L 7 2 4F RT A21EA 2007112600189 20071126 00189 EA 2007 11 26 SWIA200718863 1 20071111 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 443SW 7638 FLT 3751 - EMERGENCY LIGHT PODS AT ROWS 5 AND 10 ARE INOP. RELAMPED AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007112600190 20071126 00190 EA 2007 11 26 SWIA200718864 1 20071106 A 5240 ROLLER CNDAIR CL600 CL6002B19 1900309 EA GALLEY DOOR BINDING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 954SW 7815 GALLEY SERVICE DOOR IS DIFFICULT TO OPEN. CLEANED DOOR SEAL AND LUBRICATED DOOR ROLLER TRACKS. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007112600192 20071126 00192 SO 2007 11 26 SWIA200718866 1 20071108 A 3520 OXYGEN MASK EMB 120 EMB120ER 3260203 SO CABIN UNWANTED DEPLOY A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 576SW 120345 FLT 5441 - OXYGEN MASKS DEPLOYED IN THE CABIN. RESTOWED ALL O2 MASKS. 2 L 7 2 4T RT A31SO 2007112600193 20071126 00193 SO 2007 11 26 SWIA200718867 1 20071111 A 2197 WIRE EMB 120 EMB120ER 3260203 SO COOLING FAN BURNED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 583SW 15260 15260 120351 FLT 5522 - SMOKE IN THE FLIGHT DECK AND CABIN WITH LEFT PACK ON. REPLACED RCCB, WIRE W206-0051-10 AND LEFT GROUND COOLI NG FAN. CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007112600194 20071126 00194 EA 2007 11 26 QXEA200701712 1 20071112 A 2612 47388904 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA FIRE DETECTION MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 616QX 11995 1715 10128 DEN - FLIGHT 4324 - RECEIVED A FIRE SYSTEM FAULT MESSAGE. MAINTENANCE PLACED THE SYSTEM ON MEL 26-00-1. AIRCRAFT RETUR NED TO SERVICE. REPLACED THE FIDEEX CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007112600198 20071126 00198 EA 2007 11 26 QXEA200701711 1 20071111 A 3010 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA ANTI ICE SYS FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 614QX 10049 PDX - FLIGHT 2571 - RIGHT WING ANTI ICE CAUTION MESSAGE RECEIVED WITH CHECKLIST ACCOMPLISHED, MESSAGE DID NOT RE-APPEAR. MAINTENANCE PLACED THE SYSTEM ON MEL 30-12-4B. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007112600199 20071126 00199 EA 2007 11 26 QXEA200701724 1 20071109 A 2612 47388904 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA FIRE DETECTION MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 612QX 7226 10042 PDX - FLIGHT 2586 - INTERMITTENT FIRE SYSTEM FAULT MESSAGE. PLACED ON MEL 26-00-1. AIRCRAFT RETURNED TO SERVICE. MAIN TENANCE REPLACED THE FIDEEX CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007112600201 20071126 00201 WP 2007 11 26 07FDEA04777 1 20071113 A 3010 ARM0620 DUCT DOUG MD10 MD1010F 3022112 WP ANTI ICE SYS CRUSHED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 393FE 46627 DURING C CHECK MAINT, FOUND NR 4 LT L/E SLAT CRUSHED ANTI ICE DUCT IN L/E OF SLAT. REMOVED AND REPLACED NR 4 LT NR 4 SL AT PICCOLO TUBE PER BOEING DRAWING NRM 6061. 2 L 7 3 4F RT A22WE 2007112600203 20071126 00203 NM 2007 11 26 07FDEA04790 1 20071115 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 MAIN DECK CARGO COMPARTMENT AT ABOUT STA 889 LBL 8 SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLAC EMENT FROM STA 869 TO STA 909 LBL 8 AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007112600204 20071126 00204 NM 2007 11 26 07FDEA04791 1 20071115 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 900 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 MAIN DECK COMPARTMENT AT ABOUT STA 900 RBL 47 SEAT TRACK FOUND DAMAGED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007112700001 20071127 00001 EA 2007 11 27 TRAX200701716 1 20071111 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. 2 L 7 2 4F RT A21EA 2007112700002 20071127 00002 WP 2007 11 27 ASAA0782250 1 20071114 A 5313 591143289 LONGERON DOUG DC9 DC983 3022083 WP BS 1418 L2R CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 977AS 53453 AFT ACCESSORY COMPT LONGERON 2R CRACKED AT AFT SIDE OF FRAME STA 1418. REMOVED DAMAGED SECTION OF LONGERON, LOCATED, DR ILLED AND INSTALLED REPAIR EXTRUSION AND REPAIR SPLICE IAW MD80 SRM 53-02 FIG 18. 2 L 7 2 4F RT A6WE 2007112700003 20071127 00003 WP 2007 11 27 ASAA0782251 1 20071114 A 5313 591143289 LONGERON DOUG DC9 DC983 3022083 WP BS 1418 L2L CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 977AS 53453 AFT ACCESSORY COMPT LONGERON 2L CRACKED AT AFT SIDE OF FRAME 1418. REMOVED DAMAGED SECTION OF LONGERON LOCATED DRILLED AND INSTALLED REPAIR EXTRUSION AND REPAIR SPLICE IAW MD80 SRM 53-02 FIG 18. 2 L 7 2 4F RT A6WE 2007112700004 20071127 00004 WP 2007 11 27 ASAA0782252 1 20071115 A 5753 5930196509 SKIN DOUG DC9 DC983 3022083 WP TE FLAP VANE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 977AS 53453 LEFT WING O/B FLAP I/B VANE REPAIR DOUBLER GOUGED. REMOVED DAMAGED REPAIR DOUBLER, FABRICATED, LOCATED, DRILLED AND BON DED IAW MD80 SRM 51-70-2 PAR 18B PG 91 AND MD80 SRM 57-03 FIG 11 PG 27. 2 L 7 2 4F RT A6WE 2007112700005 20071127 00005 WP 2007 11 27 ASAA0782253 1 20071115 A 5753 5930496 SKIN DOUG DC9 DC983 3022083 WP TE FLAP VANE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 977AS 53453 RIGHT WING O/B FLAP I/B VANE PREVIOUS REPAIR GOUGED. REMOVED DAMAGED DOUBLER. FABRICATED, LOCATED, DRILLED AND BONDED REPAIR DOUBLER AND FILLER IAW MD80 SRM 51-70-2 PAR 18B AND 57-03 FIG 11 PG 27. 2 L 7 2 4F RT A6WE 2007112700007 20071127 00007 NM 2007 11 27 SWAA075705 1 20071114 A 3097 MB10P1 CONNECTOR BOEING 737 7377H4 1384404 NM WINDOW HEAT ARCED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 405WN 27893 FLIGHT DECK L2 WINDOW HEAT CONNECTOR ARCING AT CONNECTOR. REMOVED AND REPLACED CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2007112700008 20071127 00008 NM 2007 11 27 SWAA075706 1 20071114 A 5753 6552925 TORQUE TUBE BOEING 737 7375H4 138449D NM LT WING TE FLAP WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED SERVICE CHECK, NR 4 FLAP TRANSMISSION TO 90 DEGREE GEARBOX TORQUE TUBE WORN. REMOVED AND REPLACED TORQ UE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007112700009 20071127 00009 NM 2007 11 27 SWAA075707 1 20071114 A 5753 6552925 TORQUE TUBE BOEING 737 7375H4 138449D NM TE FLAP WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED SERVICE CHECK, NR 4 FLAP TRANSMISSION TO 120 DEGREE GEARBOX TORQUE TUBE WORN. REMOVED AND REPLACED TOR QUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007112700011 20071127 00011 2007 11 27 SWAA075716 2 20071112 A 7320 8063214 MEC BOEING 737 7373H4 1384600 NM NR 2 ENGINE FAULTY A SWAA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SW 29 619SW 28035 INFLIGHT SHUTDOWN / DIVERSION. AT FL 340, NR 2 ENGINE FAILED. NO FUEL BALANCE IN PROGRESS, ABLE TO RESTART ENGINE. RE MOVED AND REPLACED MEC AND FUEL PUMP PER MM. 2 L 7 2 4F RT A16WE 2007112700013 20071127 00013 NM 2007 11 27 SWAA075711 1 20071114 A 5712 6545445 RIB BOEING 737 7373A4 1384585 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT STA 135, STR 2. REPAIRED RIB PER ACO. 2 L 7 2 4F RT A16WE 2007112700015 20071127 00015 NM 2007 11 27 SWAA075712 1 20071114 A 5311 6545807 FRAME BOEING 737 7373A4 1384585 NM BS 291 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 291, STR 16R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007112700016 20071127 00016 NM 2007 11 27 SWAA075713 1 20071114 A 5311 6546543 FRAME BOEING 737 7373A4 1384585 NM BS 706 S8L/R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007112700017 20071127 00017 NM 2007 11 27 SWAA075714 1 20071114 A 3350 3071BPEGPL LAMP BOEING 737 7373G7 1384595 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007112700019 20071127 00019 NM 2007 11 27 ZZDA2007299 1 20070916 A 5310 STRUCTURE BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 936AT 55058 WHILE DOWNJACKING A/C AFT JACK FAILED AND DAMAGED A/C. INSTALLED REPAIR DOUBLER, TRIPLER, FILLER AND FINGER DOULBER. 2 L 7 2 4F TR A6WE 2007112700022 20071127 00022 EA 2007 11 27 COMA0760639 1 20071111 A 2752 854D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA RT WING TE FLAP FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 991CA 12448 7216 FLIGHT 5474 - FLAPS FAILED AT 0 DEGREES ON APPROACH INTO BGR. AIRCRAFT LANDED SAFELY. RIGHT SIDE NR 4 FLAP ACTUATOR FA ILED TORQUE CHECK. REMOVED AND REPLACED RIGHT SIDE NR 4 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2007112700023 20071127 00023 2007 11 27 C2XA07IA231 4 20071112 A 2300 7511001939 AUDIO PANEL EMB 145 EMB145XR 3260214 SO COCKPIT BURNED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 11109 18808 5373 145657 IAH - FLIGHT 2470, DURING CLIMB THE CREW REPORTED A STRONG ELECTRICAL ODOR IN THE COCKPIT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PILOTS DIGITAL AUDIO PANEL, OPERATIONALLY CHECK ED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007112700024 20071127 00024 NM 2007 11 27 KCSA071524 1 20071115 A 5347 SEAT TRACK BOEING 747 747246F 1384850 NM BS 1730-1800 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 CORROSION ON SEAT TRACK AT RBL-76 AT AT BS-1780 TO 1800. 2 L 7 4 4F RT A20WE 2007112700027 20071127 00027 EU 2007 11 27 TRAX200701706 1 20071025 A 5730 PANEL AEROSP ATR72 ATR72 EU FUEL PANEL DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 PANEL 623GT UPPER SURFACE SCRATCHED AND FLANGE CORRODED. CORROSION REMOVED. FUEL PANEL REPLACED BY NEW. 2 H 7 2 4T RT 2007112700028 20071127 00028 EA 2007 11 27 TRAX200701707 1 20071109 A 7830 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BLOCKER DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 883AS 7504 LEFT T/R BLOCKER DOOR NR 7 LINK ATTACH LUG CRACKED. 2 L 7 2 4F RT A21EA 2007112700029 20071127 00029 EA 2007 11 27 TRAX200701715 1 20071108 A 5520 HINGE CNDAIR CL600 CL6002B19 1900309 EA LT ELEVATOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 883AS 7504 LT ELEVATOR CENTER HINGE BEARING HAS AXIAL AND RADIAL PLAY AND CORROSION. CORROSION REMOVED. 2 L 7 2 4F RT A21EA 2007112700030 20071127 00030 EU 2007 11 27 07FDEA04797 1 20071115 A 5312 R538106796 BULKHEAD AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 FWD PIT, 3 INCHES AFT FRAME 39 LEFT, 3 INCHES ABOVE STRINGER 30 LEFT, HORIZONTAL BULKHEAD LT FWD CORNER, SEVERE EXFOLIAT ION CORROSION. COMPLIED WITH EA 6-5310-109221 2 L 7 2 4F RT A35EU 2007112700031 20071127 00031 CE 2007 11 27 HYIA13568752 1 20071108 A 2720 51152604 TORQUE TUBE CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO RUDDER PEDAL BROKEN E HYIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NE 01 68752 11100 1 402C0518 ON APPROACH, RT RUDDER PEDAL WENT TO FLOOR. APPROACH WAS CONTINUED, LANDING UNEVENTFUL. MAINTENANCE FOUND RUDDER PEDAL ATTACH BRACKET HAD FAILED. REMOVED AND REPLACE TORQUE TUBE AND RELEASED AIRCRAFT BACK TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2007112700032 20071127 00032 EU 2007 11 27 HYIA8344171 1 20071101 A 3350 3011180 POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE EMERGENCY LIGHTS FAILED A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 14834 193 EMREGENCY AISLE PATH AND LOWER EXIT SIGNS FOR THE PASSENGER AND SERVICE DOORS ILLUMINATE DIMMLY WHEN EMERGENCY EXIT LIGH TS ARE ARMED. REMOVED AND INSTALLED EMER. LIGHT POWER SUPPLY THERE WERE NO ENGINE SHUTDOWNS, NO PROPELLER FEATHERINGS , NO DELAYS AND NO CANCELLATIONS DUE TO THIS PROBLEM. 2 H 7 2 4T 4 T RT A53EU E20NE 2007112700033 20071127 00033 WP 2007 11 27 UPS07851186 1 20071118 A 5522 SKIN DOUG DC8 DC871F 302199D WP RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:N/A RIGHT ELEVATOR UPPER SKIN HAS A CRACK 3.75 INCH LONG, JUST AFT OF I/B ELEVATOR HINGE. ACCOMPLISHED INTERIM REPAIR AS SPECIFIED IN PARAGRAPH 6A. LOG PAGE 812958. PERMANENT REPAIR IS REQUIRED AT OR BEFORE NEXT C CHECK (1 1/08) 2 L 7 4 4F RT 4A25 2007112700034 20071127 00034 CE 2007 11 27 13583111807 1 20071118 A 3243 19105471 MASTER CYLINDER CESSNA 402 402C 207590R CE BRAKES FAILED E HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 83PB 402C0350 DURING TAXI OUT FOR REPOSITIONING FLIGHT, PILOT FELT A PULSE FROM THE LEFT RUDDER PEDAL AND THEN A UNCONTROLLABLE TURN T O THE RIGHT. PILOT USED MAXIMUM BRAKING AND THROTTLES TO IDLE TO STOP AIRCRAFT. MAINTENANCE REBUILT, SERVICED, AND BLE D THE LEFT BRAKE MASTER CYLINDER, NO FURTHER DEFECTS REPORTED. 1 L 7 2 3O A7CE 2007112700035 20071127 00035 WP 2007 11 27 07FDEA04860 1 20071119 A 5300 ACA3799501 FITTING DOUG DC10 DC1010 3022110 WP 100 CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), VANE AIR CONDITION LT SIDE BAY JAMB STRUCTURE FRAME TO STA 528 DEFORMED CORROSION AND CRACK LONG 2" ON SUPPORT FITTING. REPLACED FRAME ACA3347-3 AND FITTING ACA3799-501 FOR S RM 51-35-01 VOL II. 2 L 7 3 4F A22WE 2007112700036 20071127 00036 NM 2007 11 27 USAA920071166 1 20071117 A 5711 69620146 STIFFENER BOEING 737 7373G7 1384595 NM BS 663.75 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 MAJOR REPAIR - CRACKED CENTER WING REAR SPAR VERTICAL STIFFENER, BS 663.75, RBL 6.15, WL 170, IN RT MLG WHEEL. REPAIRED IAW USAIRWAYS EA 120397. 2 L 7 2 4F RT A16WE 2007112700037 20071127 00037 2007 11 27 07FDEA04865 4 20071119 A 3160 DISPLAY AIRBUS 300 A300F4605R 3930327 EU RIGHT MALFUNCTIONED A FDEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 654FE 738 ON RUNWAY WHEN POWER WAS ADVANCED NR 1 REV PRESSURIZED ON ECAM. REMOVED AND REPLACED NR 1 ENGINE RT CDU SWITCH PER MM 78-31-04-4-07. T/R OPS GOOD PER JRH CHAPTER 7. 2 L 7 2 4F RT A35EU 2007112700039 20071127 00039 SO 2007 11 27 C2XA07CL097 1 20071114 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN SMOKE A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 13965 145125 EWR FLIGHT 2261 THE CREW REPORTED SMOKE IN CABIN AFTER TAKEOFF. THE AIRCRAFT RETURNED TO EWR AND LANDED WITHOUT INCIDEN T. MAINTENANCE INSPECTED AND PERFORMED FAULT ISOLATION PROCEDURES IAW 21-20-00-810-801A. RAN ENGINES, PACKS AND APU AT TAKEOFF POWER AND AT VARIOUS SETTINGS. CHECKED LIGHTING AND CABIN ELECTRICAL COMPONENTS AND NO DEFECTS WERE FOUND. TH E AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007112700040 20071127 00040 NM 2007 11 27 SWAA075718 1 20071115 A 3397 W4142001220 WIRE BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 220WN 32491 EEPLS INOP BETWEEN ROW 5 ABC AND ROW 7 ABC. FOUND LOOSE WIRE. SECURED WIRE PER MM. 2 L 7 2 4F RT A16WE 2007112700044 20071127 00044 NM 2007 11 27 SWAA075723 1 20071115 A 3350 101114 COVER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED C4 CHECK, FOUND AFT CABIN EMERGENCY EXIT SIGN COVER CRACKED. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007112700045 20071127 00045 NM 2007 11 27 SWAA075722 1 20071115 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM BS 390 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 390, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007112700046 20071127 00046 NM 2007 11 27 SWAA075725 1 20071115 A 5512 182A4401 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 430WN 33659 DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007112700070 20071127 00070 EA 2007 11 27 HNAA0700270 1 20071113 A 3211 YOKE DHAV DHC8 DHC8311 1386006 EA LANDING GEAR BINDING A HNAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 07 335EN 375 ON APPROACH TO AIRFIELD, LANDING GEAR DOWN WAS SELECTED AND NR 1 GEAR DOOR AMBER LIGHT ALONG WITH RED GEAR UNSAFE LIGHT ILLUMINATED. UPON VERIFYING THE CONDITION INDICATED, THE CREW THEN DECLARED AN EMERGENCY AND PROCEEDED TO EXTEND THE LA NDING GEAR USING THE ALTERNATE EXTENSION SYSTEM. MAINTENANCE FOUND THE UPPER LANDING GEAR YOKE ASSEMBLY WAS BINDING. Y OKE SHIMS WERE REMOVED, RE-MEASURED AND ASSEMBLY WAS RE-SHIMMED TO PROPER SPECS. OPS CHECKS WERE GOOD IAW MM 32-10-13. 2 H 7 2 4T RT A13NM 2007112700071 20071127 00071 EA 2007 11 27 HNAA0700269 1 20071114 A 2510 HA1555 MASTER CAUTION DHAV DHC8 DHC8311 1386006 EA COCKPIT UNKNOWN A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 333EN 221 DURING CREW SWAP IN CLT, ARRIVING CREW FOUND A FISH ODOR IN COCKPIT AREA. MAINTENANCE CHECKED OVERHEAD PANELS IN COCKPIT . SLIGHT ODOR WAS NOTICED COMING FROM MASTER CAUTION PANEL. REMOVED AND REPLACED CAUTION PANEL AND OPS CHECKED GOOD PE R AMM 33-12-01. SMELL DISSIPATED AFTERWARDS AND AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 2007112700072 20071127 00072 WP 2007 11 27 MWEA070294 1 20071115 A 2611 CGAB140000 SMOKE DETECTOR DOUG DC9 DC982 3022082 WP LAVATORY INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 809ME 48071 RIGHT LAVATORY SMOKE DETECTOR BRIEFLY SOUNDS WITH RED LIGHT THEN TESTS NORMAL AGAIN, NO FIRE. REMOVED AND REPLACED RIGH T LAVATORY SMOKE DETECTOR. 2 L 7 2 4F A6WE 2007112700073 20071127 00073 NM 2007 11 27 MWEA070295 1 20071115 A 5347 5936663505 CARGO TRACK DOUG MD88 MD88 3023688 NM BS 1212-1322 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 701ME 49760 AFT CARGO COMPARTMENT, BETWEEN FUSELAGE STATION 1212 & 1322 STRINGER 28 RIGHT TIE DOWN TRACK HAS SEVERAL SPOTS OF CORROS ION. REMOVED CORROSION. FABRICATED AND INSTALLED NEW TIE DOWN TRACK. 2 L 7 2 4F RT A6WE 2007112700074 20071127 00074 NM 2007 11 27 MWEA070297 1 20071116 A 5280 DOOR FRAME BOEING 717 717200 1383700 NM MLG DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 923ME 55185 LEFT MAIN LANDING GEAR DOOR JAM HAS A CRACK 3.5 INCHES BELOW THE PROXMITY SENSOR. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2007112700075 20071127 00075 NM 2007 11 27 MWEA070296 1 20071115 A 5347 593663509 CARGO TRACK DOUG MD88 MD88 3023688 NM BS 1231-1322 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 701ME 49760 AFT CARGO COMPARTMENT BETWEEN FUSELAGE STATION 1231 & 1322 STATION 28 LEFT TIE DOWN TRACK HAS SEVERAL SPOTS OF CORROSION . FABRICATED AND INSTALLED NEW TIE DOWN TRACK. 2 L 7 2 4F RT A6WE 2007112700076 20071127 00076 NM 2007 11 27 CALA0700692 1 20071119 A 5230 6547952182 SKIN BOEING 737 7373T0 1384582 NM AFT CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 THE RAMP FOUND A 3.5 INCH CRACK IN AFT CARGO DOOR SKIN ABOVE FORWARD DOOR CUTOUT. DOUBLERS WERE INSTALLED IAW ECRA 5232 -01096. A DIP WAS INITIATED TO ACCOMPLISH A PERMANENT REPAIR WITHIN SIX MONTHS. 2 L 7 2 4F RT A16WE 2007112800002 20071128 00002 NM 2007 11 28 ASAA0792263 1 20071114 A 5315 143A9485Y3 FLOORBEAM BOEING 737 737990 NM BS 500L CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 309AS 30857 FWD CARGO PIT FLOORBEAM ANGLE AT BS 500L RBL 21 TO LBL 21 FOUND CORRODED. FLOOR SUPPORT ANGLE IN FWD CARGO PIT AT BS 50 0L LBL 21 TO RBL 21 REPLACED WITH NEW PART IAW B737 900 SRM 51-40-02. 2 L 7 4 4F RT A16WE 2007112800006 20071128 00006 NM 2007 11 28 ASAA0792269 1 20071114 A 5320 146A750221 ANGLE BOEING 737 737990 NM BS 727I-847 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 309AS 30857 AFT CARGO PIT LEFT ZEE ANGLE FOUND CORRODED AT BS 727I+6 TO BS 847 LBL 21 LEFT. ZEE ANGLE IN AFT CARGO PIT ON 727I+6 TO BS 847 LBL 21 REPLACED, MADE REPAIR PART IAW B737 950 SRM 53-00-53. 2 L 7 4 4F RT A16WE 2007112800007 20071128 00007 NM 2007 11 28 ASAA0792271 1 20071114 A 5320 146A750218 ANGLE BOEING 737 737990 NM BS 727-727D CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 309AS 30857 AFT CARGO PIT RIGHT ZEE ANGLE FOUND CORRODED AT BS 727 TO 727D. AFT CARGO PIT RIGHT ZEE ANGLE REPLACED AT BS 727 TO 727 D RBL 21. 2 L 7 4 4F RT A16WE 2007112800008 20071128 00008 NM 2007 11 28 ASAA0792273 1 20071115 A 5320 146A750222 ANGLE BOEING 737 737990 NM BS 727I-767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 309AS 30857 AFT CARGO PIT RIGHT ZEE ANGLE AT BS 727 I+B TO 767 RBL 21 FOUND CORRODED. AFT CARGO PIT RIGHT ZEE ANGLE AT BS 727 I+B T O 767 RBL 21 REPLACED IAW B737 900 SRM 53-00-53. 2 L 7 4 4F RT A16WE 2007112800009 20071128 00009 NM 2007 11 28 ASAA0792274 1 20071114 A 5315 BUTTSTRAP BOEING 737 737990 NM BS 773 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 309AS 30857 AFT CARGO PIT FLOOR BUTTSTRAP "TEE" CORRODED BS 767+6 RBL 21 TO LBL 21. BUTT STRAP "TEE" REPLACED. 2 L 7 4 4F RT A16WE 2007112800010 20071128 00010 WP 2007 11 28 ASAA0782257 1 20071118 A 5753 5930495508 SKIN DOUG DC9 DC983 3022083 WP TE FLAP VANE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 977AS 53453 RIGHT WING I/B FLAP O/B VANE MULTIPLE DENTS ON LWR I/B SURFACE. PREPARED DAMAGED AREA IAW MD 80 SRM 51-70-2 PG 11. FAB RICATED DOUBLER AND BONDED IAW MD 80 SRM 51-70-2 PGS 23 AND 91. 2 L 7 2 4F RT A6WE 2007112800018 20071128 00018 NM 2007 11 28 CALA0700693 1 20071118 A 5310 141A81121 DOOR FRAME BOEING 737 737724 13844BY NM BS 291.5-360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24702 28763 INSPECTION FOUND L-1 DOOR CHORD CORRODED AT STA 291.5-360, LBL 43. THE CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND GMM 10-900-02. 2 L 7 2 4F RT A16WE 2007112800020 20071128 00020 NM 2007 11 28 ABXA070368 1 20071118 A 5753 BACB30LJ6U74 BOLT BOEING 767 767232 1385132 NM TE FLAP FAIRING MISSING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 750AX 22227 AT STA SJO, DURING MAINTENANCE WALKAROUND, FOUND RIGHT INBOARD TRAILING EDGE FLAP FAIRING PANEL 196HR MISSING BOLT ON FO RWARD HINGE POINT. INSTALLED BOLT, BUSHINGS, NUT AND TORQUED IAW B767 MM 27-51-15-4. CYCLED FLAPS SEVERAL TIMES, OPS C HECKED GOOD. 2 L 7 2 4F RT A1NM 2007112800021 20071128 00021 NM 2007 11 28 SWAA075730 1 20071116 A 3350 MS155721 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 239WN 34714 L1 DOOR EMERGENCY EXIT LIGHT BULB INOP. REMOVED AND REPLACED BULB PER MM. 2 L 7 2 4F RT A16WE 2007112800022 20071128 00022 NM 2007 11 28 SWAA075731 1 20071117 A 5330 6518420 SKIN BOEING 737 7373H4 1384600 NM BS 259 S19L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259.5, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007112800023 20071128 00023 NM 2007 11 28 SWAA075732 1 20071117 A 5753 SKIN BOEING 737 7373H4 1384600 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 2123 23333 DURING SCHEDULED BRIDGE CHECK, FOUND RIGHT WING INBOARD T/E FLAP DELAMINATED. REMOVED AND REPLACED RIGHT INBOARD T/E FL AP PER MM. 2 L 7 2 4F RT A16WE 2007112100137 20071121 00137 NM 2007 11 21 USAA920071123 1 20071112 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 PHX - MAJOR REPAIR - CRACKED FUSELAGE BS 727E, S23L. REPAIRED FUSELAGE SKIN BS 727E, S23L IAW B737 SRM 53-00-01-2R-31. 2 L 7 2 4F RT A16WE 2007112100138 20071121 00138 NM 2007 11 21 USAA920071124 1 20071112 A 5330 6545774 SKIN BOEING 737 7373S3 1384711 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 PHX - MAJOR REPAIR - CRACKED FUSELAGE BS 727E, S18L. REPAIRED FUSELAGE SKIN BS 727E, S18L IAW B737 SRM 53-00-01-2R-31. 2 L 7 2 4F RT A16WE 2007112100150 20071121 00150 NM 2007 11 21 SWAA075672 1 20071112 A 3350 417A5700 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 252WN 34973 EEPLS ASSY LOOSE AT ROW 5 ABC. SECURED ASSY PER MM. 2 L 7 2 4F RT A16WE 2007112100152 20071121 00152 2007 11 21 SWAA075673 4 20071113 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007112100164 20071121 00164 NM 2007 11 21 SWAA075682 1 20071113 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED MV1 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP P ER MM. 2 L 7 2 4F RT A16WE 2007112600002 20071126 00002 SW 2007 11 26 WGEA200700021 1 20071108 A 2731 TRIM SYSTEM ECLIPS EA500 ECLIPSEEA500 3350000 SW PITCH MALFUNCTIONED E WGEA O OTHER O OTHER CL CLIMB 1 EA 27 135DJ 000036 NORMAL TAKEOFF GNV, ELECTRIC PITCH TRIM INOP ON CLIMB-OUT ( NO CAS MESSAGE). USED ALTERNATE PITCH TRIM FOR LANDING (FLAP S T/O POSITION). PERFORMED FLIGHT CONTROLS ADJUSTMENT. TEST FOR ELEVATOR AND ELEVATOR TRIM IAW EA 500 MM 27-00-00. AL L TEST CHECK GOOD. PERFORMED MFD (FLCS) FLIGHT CONTROL SYNOPTIC PAGE TRIM SYSTEM TEST IAW EA500 AMM 31-10-00 WITH PILOT S AND COPILOTS SIDE STICK WITH FLAPS AT TAKEOFF, LANDING, AND THROTTLES AT MAX. SYSTEM CHECK GOOD. NO DEFECTS NOTED. 1 L 7 2 4J RT A00002AC 2007112600003 20071126 00003 SW 2007 11 26 WGEA200700022 1 20071107 A 3230 LANDING GEAR ECLIPS EA500 ECLIPSEEA500 3350000 SW LEFT MALFUNCTIONED E WGEA O OTHER J WARNING INDICATION LD LANDING 1 EA 27 110DJ 000007 UPON EXTENSION, LEFT MAIN LANDING GEAR REMAINS IN TRANSIT 15 SECONDS AFTER EXTENSION ( LONGER THAN OTHER TWO GEAR). PER FORMED 10 GEAR CYCLES IAW EA500 AMM 32-30-00. SYSTEM OPERATES SATISFACTORY WITH NO DEFECTS NOTED. ALSO TIMED GEAR DURIN G 10 CYCLES AND AVERAGED 9.5 SECONDS ON DOWN TRAVEL. PERFORMED ADJUSTMENT TEST OF MAIN GEAR/DOORS IAW EA500 AMM 32-10-0 0 ALL CLEARANCES AND ADJUSTMENT FOUND TO BE WITH IN LIMITS. 1 L 7 2 4J RT A00002AC 2007112600004 20071126 00004 NE 2007 11 26 070176 2 20071107 A 7200 JT8D219 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 1 FAILED A WX0A A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 WP 19 869GA 53294 708516 ALLEGIANT AIR FLIGHT 722 FROM CID (CEDAR RAPIDS, IOWA) TO SFB (SANFORD, FLORIDA), FLIGHT CREW REPORTED THE NR 1 (LEFT) ENGINE FAILURE ON CLIMB-OUT. PERFORMED EMERGENCY QRH ITEMS AND RETURNED TO CID. AIRCRAFT LANDED NORMALLY, MAINTENANCE DEPARTMENT PERSONNEL HAVE INSPECTED AND COMMENCED REPLACEMENT OF THE LEFT ENGINE. THIS WILL REMAIN AN OPEN ITEM UNTIL C OMPLETION OF ENGINE REPLACEMENT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007112600009 20071126 00009 NM 2007 11 26 QXEA200701655 1 20071102 A 5246 STRUCTURE BOMBDR DHC8 DHC8402 1390042 NM LAV SERV ACCESS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - LAV SERVICE DOOR HAS CORROSION UNDER BOTTOM EDGE RUBBER SEAL. REPAIRED IAW SRM 51-21-00, 51-00-04, 51-42-05. 2 H 7 2 4T RT A13NM 2007112600022 20071126 00022 EA 2007 11 26 QXEA200701575 1 20071016 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 605-645 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 C4 PDX - RIGHT CENTER SEAT TRACK NR 16 HAS CORROSION ON CENTER AND EDGES OF TRACK AT STATION FS 605, 645, 688. REPAIRED IAW AMM 53-00-49. 2 L 7 2 4F RT A21EA 2007112600028 20071126 00028 EA 2007 11 26 QXEA200701604 1 20071023 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 550-581 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 C4 PDX - RIGHT CENTER SEAT TRACK NR 15 HAS CORROSION ON CENTER AND EDGES OF TRACK AT STATIONS FS 550, 555, 573, AND 581. REPAIRED IAW AMM 53-00-49-000-801-A01. 2 L 7 2 4F RT A21EA 2007112600030 20071126 00030 EA 2007 11 26 REXA200700061 1 20071008 A 2612 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY MALFUNCTIONED A REXA F ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SO 25 8946A 7946 RECEIVED SMOKE TOILET INDICATION ON CLIMB-OUT BITTER HAZE SMOKE IN CABIN TO FLIGHT COMPARTMENT. REMOVED AND REPLACED LA V SMOKE DETECTOR IAW AMM 26-10-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007112600046 20071126 00046 NM 2007 11 26 QXEA200701673 1 20071103 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - AFT CARGO BAY, LEFT HAD SEAT TRACK 2" LONG SECTION AT STATION 746-Z100 HAS CORROSION. REPAIRED IAW SRM 51-40-1 0, 51-40-15, 51-42-05. 2 H 7 2 4T RT A13NM 2007112600057 20071126 00057 NM 2007 11 26 QXEA200701683 1 20071101 A 5320 THRESHOLD BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - MAIN CABIN DOOR THRESHOLD CHANNEL HAS CORROSION ON UPPER SURFACE AT FIVE NUTPLATE LOCATIONS. REPAIRED IAW RD8/ 4-53-1660. 2 H 7 2 4T RT A13NM 2007112600066 20071126 00066 NM 2007 11 26 QXEA200701684 1 20071031 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 127 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION IN BOTTOM OF CHANNEL AT STATION X127. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007112600071 20071126 00071 NM 2007 11 26 QXEA200701690 1 20071031 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 323-327 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION IN BOTTOM OF CHANNEL BETWEEN STATION X323 AND X327. REPAIRED IAW RD8/4 -53-884. 2 H 7 2 4T RT A13NM 2007112600076 20071126 00076 NM 2007 11 26 QXEA200701695 1 20071031 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 403-405 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION IN CHANNEL AND ON TOP OF RAIL BETWEEN STATION X403 AND X405. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007112600080 20071126 00080 NM 2007 11 26 QXEA200701703 1 20071106 A 5415 ATTACH FITTING BOMBDR DHC8 DHC8402 1390042 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - LEFT ENGINE NACELLE INBOARD FORWARD SPINE COWL CLIP HAS A CRACK. REPAIRED IAW RD8/4-71-032. 2 H 7 2 4T RT A13NM 2007112600081 20071126 00081 NM 2007 11 26 QXEA200701702 1 20071101 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM BS 295-292 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - TWO DENTS LOCATED AT FS-X295.5 AND FS-X292 BETWEEN STRINGER 20R AND 21R. REPAIRED IAW RD8/4-53-0666, SRM 51-25 -10, 51-25-15. 2 H 7 2 4T RT A13NM 2007112600100 20071126 00100 NM 2007 11 26 AALA20072153 1 20071105 A 3350 0L3071BPEGPL LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 790AN 30251 MIA - EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007112600101 20071126 00101 NM 2007 11 26 AALA20072154 1 20071105 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 790AN 30251 MIA - EMERGENCY LIGHT AT SEAT 22C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007112600102 20071126 00102 2007 11 26 AALA20072158 4 20071105 A 2565 100505201 SLIDE DOUG DC9 DC983 3022083 WP L2 DOOR WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9628W 53598 MSP - LEFT NUMBER TWO DOOR EMERGENCY SLIDE HANDLE VELCRO IN POOR CONDITION. REPLACED EMERGENCY SLIDE AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007112600103 20071126 00103 NM 2007 11 26 AALA20072157 1 20071105 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 345AN 33084 MIA - EMERGENCY LIGHTS AT SEAT ROWS 5HJ TO 13HJ INOPERATIVE. SECURED CONNECTOR AT SEAT 5H FOR EMERGENCY LIGHTS AT SEAT ROWS 5HJ TO 13HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007112600107 20071126 00107 NM 2007 11 26 AALA20072155 1 20071105 A 3350 0L3071BPEGPL LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 790AN 30251 MIA - EMERGENCY LIGHT AT SEAT 24C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007112600121 20071126 00121 EA 2007 11 26 SWIA200718847 1 20071101 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 492SW 7168 FLT 3882 - FOUND SEVERAL FLOOR EMERGENCY LIGHTS DON'T WORK. REPLACED TRACK LIGHT CONNECTOR. 2 L 7 2 4F RT A21EA 2007112600132 20071126 00132 NM 2007 11 26 QXEA200701716 1 20071107 A 2760 3960001005 VALVE BOMBDR DHC8 DHC8402 1390042 NM SPOILERS MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 418QX 11904 59 4143 GTF FLIGHT: DURING CLIMB-OUT FROM HLN, SPOILER OUTBOARD CAUTION LIGHT ILLUMINATED. RAN CHECKLIST, NO ADDITIONAL/ASSOCIAT ED LIGHTS. THIS CAUTION LIGHT CAME ON BETWEEN 185-185 KNOTS. MAINTENANCE REMOVED AND REPLACED NR 2 UNLOAD VALVE IAW Q4 00 AMM 27-61-26-000-801/400-801. OPS CHECK GOOD. NO LEAKS NOTED. THE VALVE WAS CHANGED FOR PRECAUTIONARY MEASURE. AI RCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007112600137 20071126 00137 EA 2007 11 26 TRAX200701711 1 20071110 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 884AS 7513 ON SHORT FINAL, FLIGHT CREW SMELLED SOMETHING BURNING. CONTINUED DURING LANDING AND TAXI (AIR CONDITIONING PACK, LT SID E). 2 L 7 2 4F RT A21EA 2007112600144 20071126 00144 2007 11 26 SIMA200731801 4 20071111 A 3416 INDICATOR EMB 145 EMB145LR 3260212 SO ALTIMETER INOPERATIVE A SIMA D RETURN TO BLOCK P NO WARNING INDICATION TO TAKEOFF 1 SW 21 673AE 145797 STANDBY ALTIMETER GAUGE INOP AFTER TO. A/C RETURNED TO FIELD. NO OVERWEIGHT LANDING. 2 L 7 2 4T RT T00011AT 2007112600153 20071126 00153 NM 2007 11 26 07FDEA04784 1 20071113 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1280 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 MAIN DECK CARGO COMPARTMENT AT ABOUT STA 1280 LBL 47 SEAT TRACK FOUND DAMAGED. REPAIRED BY SECTIONAL SEAT TRACK REPLA CEMENT FROM STA 1249 TO STA 1331 LBL 47 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100. 2 L 7 3 4F RT A22WE 2007112600158 20071126 00158 EA 2007 11 26 A6WA200740587 1 20071014 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 469AW 7917 LT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT 540BB, WS 54.897, HOLE NR 1, HAS PITTING CORROSION AT INBOARD AND OUTBO ARD ENDS IN NON-CRITICAL AREA. MEASURES APPROX .3 INCH LONG BY .20 INCH WIDE BY .005 INCH DEEP EACH. MAINTENANCE REPAI RED IAW AWAC EO E06/02/457 AND REO 601R-57-21-030 REV F. (M) 2 L 7 2 4F RT A21EA 2007112600164 20071126 00164 EA 2007 11 26 A6WA200740597 1 20071101 A 2697 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA FIRE BOTTLE DIRTY A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 456ZW 7849 CARGO BOTTLE LOW MESSAGE ILLUMINATED. CLEANED FIRE BOTTLE EXT CONNECTOR LEFT AND RIGHT, OPS CHECK GOOD IAW CRJ AMM 26-2 5-01 PER MAINTENANCE CONTROL CHANGED CARGO FIRE EXT LEFT BOTTLE. (M) 2 L 7 2 4F RT A21EA 2007112600167 20071126 00167 EA 2007 11 26 A6WA200740599 1 20071105 A 2740 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA STAB MALFUNCTIONED A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 453AW 7838 STAB CHANNEL 1 DIS-ENGAGED NUMEROUS TIMES IN FLIGHT. REMOVED AND REPLACED MCU IAW 27-42-05, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007112600168 20071126 00168 EA 2007 11 26 A6WA200740596 1 20071030 A 5350 SEAL CNDAIR CL600 CL6002B19 1900309 EA FAIRING MISSING A A6WA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 31 411ZW 7569 DURING CRUISE INTERMITTENT VIBRATION AT 280 KNOT FOR APPROX 5 SECONDS. ALL ENGINE PARAMETERS WERE NORMAL. APPLIED SEAL ANT TO WING TO FUSELAGE FAIRING AS REQUIRED IAW CRJ AMM 51-23-00 AS REQUIRED. (M) 2 L 7 2 4F RT A21EA 2007112600180 20071126 00180 NM 2007 11 26 USAA920071148 1 20071021 A 5754 STRUCTURE BOEING 757 7572B7 1384964 NM NR 6 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 423 23384 MCN - MAJOR REPAIR - C4 CHECK - RIGHT WING NR 6 SLAT CRACKED, SS 338.5 - SS 340 AND SS 373.5 - SS 379. REPAIRED IAW B7 57 SRM 57-43-01-2R6, FIGURE 201. 2 L 7 2 4F RT A2NM 2007112600191 20071126 00191 EA 2007 11 26 SWIA200718865 1 20071113 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 762SK 10226 FLT 6690 - CEILING EMERGENCY FLOOD LIGHT IS INOP. RELAMPED CEILING FLOOD LIGHT IAW CRJ 700 AMM 33-51-09. OPS CHECK GOO D. 2 L 7 2 4F RT A21EA 2007112600196 20071126 00196 EA 2007 11 26 QXEA200701723 1 20071112 A 8012 32913393 VALVE CNDAIR CL600 CL6002C10 1390015 EA STARTER FAILED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 614QX 4251 10049 DEN - FLIGHT 2507 - DURING ENGINE START AFTER PUSHBACK RECEIVED A LEFT ENGINE STARTER VALVE CAUTION. RETURNED TO THE GA TE. MAINTENANCE PLACED THE SYSTEM ON MEL 80-11-3. AIRCRAFT RETURNED TO SERVICE. REPLACED THE STARTER CONTROL VALVE. OPERATIONAL CHECKS GOOD MEL CLOSED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007112600202 20071126 00202 NM 2007 11 26 07FDEA04789 1 20071115 A 5300 LOCK FASTENER DOUG MD11 MD11F 3023600 NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 EMPENNAGE AFT FUSELAGE COMPARTMENT UPPER DOG HOUSE AT STA 2102 FRAME CLIP AROUND 1 LOCK FASTENER FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007112700077 20071127 00077 NM 2007 11 27 KCSA071526 1 20071119 A 5320 FITTING BOEING 747 747246F 1384850 NM BS 962 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 FWD PIT, AFT PALLET STOP FITTING CRACKED AT BS 962, LBL 24. 2 L 7 4 4F RT A20WE 2007112700078 20071127 00078 NM 2007 11 27 KCSA071527 1 20071119 A 5320 SUPPORT BRACKET BOEING 747 747246F 1384850 NM BS 560 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 FWD PIT, SIDE RAIL SUPPORT BRACKET CRACKED AT BS 560, RBL 65. 2 L 7 4 4F RT A20WE 2007112700079 20071127 00079 SO 2007 11 27 C2XA07CL098 1 20071116 A 3233 21180100401 ACTUATOR EMB 145 EMB145LR 3260212 SO NLG FAULTY A C2XA O OTHER J WARNING INDICATION DE DESCENT 1 SW 27 16571 15257 145633 FLT 2966, OKC - CLE. INBOUND TO CLE, AN AIR/GROUND FAIL MESSAGE ILLUMINATED DURING GEAR EXTENSION. THE RIGHT NOSE LAND ING GEAR DOOR ACTUATOR WAS REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2007112700080 20071127 00080 SO 2007 11 27 C2XA07TY070 1 20071116 A 5330 14520571001 SKIN EMB 145 EMB145LR 3260212 SO FUESLAGE PUNCTURED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 DENT AND PUNCTURE UNDERNEATH SERVICE DOOR. REPAIRED DAMAGE TO AIRCRAFT IAW EC 5330-01752. PRESSURE CHECK GOOD. AIRCRA FT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007112700081 20071127 00081 NM 2007 11 27 UPS07551174 1 20071116 A 3040 CONTROL UNIT BOEING 757 75724APF 1384969 NM WINDSHIELD HEAT OVERHEATED A IPXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 443UP 27388 FLIGHT CONTROL WAS NOTIFIED BY MCI CENTER THAT THE CREW REPORTED SMOKE IN COCKPIT WHEN APPROXIMATELY 120NM WEST OF BUM V OR AND AT FL300 AND WERE DECLARING AN EMERGENCY. AFTER CLOCK IN, CAPT WINDSHIELD CRACKED. ISOLATED FUMES TO OVERHEATED WINDSHIELD. REMOVED AND REPLACED LEFT WINDOW HEAT CONTROL UNIT PER 757 AMM 30-41-01-4 TESTS OK. REMOVED AND REPLACED CAPTAINS WINDSHIELD PER AMM 56-11-01-4. 2 L 7 2 4F RT A2NM 2007112700082 20071127 00082 NM 2007 11 27 UPS07551185 1 20071116 A 3350 BULB BOEING 757 75724APF 1384969 NM EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 457UP 25478 EMERGENCY EXIT EGRESS LIGHT FAILED TO TEST. REMOVED AND REPLACED GE767 BULBS. OPS CHECK PER MM 33-51-06-2. 2 L 7 2 4F RT A2NM 2007112700083 20071127 00083 2007 11 27 UPS07651170 2 20071114 A 7200 ENGINE BOEING 767 76734AF 1385212 NM NR 1 ODOR A IPXA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 01 327UP 27753 INSPECTION TYPE:ETOP SMELL OF BURNING RUBBER AFTER T/O. BOTH PACKS SMELLED OF PAINT BEFORE T/O. REMOVED AND REPLACED N R 1 ENGINE PER T/C 6002. NO ODD ODOR BEFORE, DURING OR AFTER ENGINE RUN. 2 L 7 2 4F RT A1NM 2007112700084 20071127 00084 NM 2007 11 27 UPS07651179 1 20071113 A 5751 RIB BOEING 767 76734AF 1385212 NM LT WING AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 311UP 27741 INSPECTION TYPE:SEG2 LEFT WING I/B AILERON I/B HINGE SUPPORT RIB IS CRACKED AT UPPER AFT O/B BOLTS COMMON TO UPPER T/E P ANEL SUPPORT WS 445. REPAIRED PER UPS RAA FILE 767-57-20084 AND GOODRICH EO 07-3840. 2 L 7 2 4F RT A1NM 2007112700085 20071127 00085 NM 2007 11 27 UPS07651180 1 20071117 A 2400 MS25306222 SWITCH BOEING 767 76734AF 1385212 NM COCKPIT OVERHEAD MELTED A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 01 327UP 27753 INSPECTION TYPE:ETOP CREW REPORTED, DURING LOWERING THE LANDING GEAR, THERE WAS A BURNING RUBBER LIKE ODOR WITH BOTH PAC KS ON. FOUND RT RUNWAY TURNOFF TOGGLE SWITCH SMOKING WHEN TURNED ON. REMOVED AND REPLACED THE TOGGLE SWITCH IN REF TO 767 M/M 20-11-00 AND OPS CHECKED IN REF 767 M/M 33-43-01-2. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A1NM 2007112700086 20071127 00086 2007 11 27 UPS07851177 4 20071115 A 2565 SLIDE DOUG DC8 DC873F 302199F WP EMERGENCY EXIT DISLODGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:N/A THE MAIN ENTRY DOOR EMERGENCY ESCAPE SLIDE NEEDS TO BE ADJUSTED IN THE HOLDING CASE AS IT APPEARS TO BE SLIDING OUT AND IT IS DIFFICULT TO READ SLIDE PRESSURE. REPOSITIONED MAIN ENTRY DOOR EVACUATION SLIDE IN CONTAINER AND RE-INSTALLED W/REF TO MM 25-60-01-2. SLIDE IS SECURE. 2 L 7 4 4F RT 4A25 2007112700087 20071127 00087 NM 2007 11 27 UPS07B51181 1 20071118 A 3350 LAMP BOEING 747 74744AF 13848B2 NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 570UP 35667 INSPECTION TYPE:N/A EMERGENCY LIGHT IN CEILING AT L1 DOOR DOES NOT ILLULMINATE WHEN TESTED. RELAMPED EMERGENCY LIGHT WI TH REF TO MM 33-51-07-2. CHECKED GOOD PER SAME. 2 L 7 4 4F RT A20WE 2007112700088 20071127 00088 EA 2007 11 27 TRAX200701736 1 20071114 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 926EV 7843 FLAPS FAIL AT 0 DEGREES ON APPROACH WHEN SELECTED TO 8 DEGREES. EMERGENCY EQUIPMENT ON STANDBY. 2 L 7 2 4F RT A21EA 2007112700089 20071127 00089 NM 2007 11 27 200711191 1 20071115 A 2780 SLAT SYSTEM EMB ERJ170 ERJ170100SE 3260406 NM LE SLATS FAILED A UHLA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 11 857RW 17000079 FLIGHT 6462 MDW TO LGA ON APPROACH CREW EXPERIENCED A SLAT FAIL. CREW DIVERTED TO JFK, DECLARED EMERGENCY AND LANDED WI THOUT INCIDENT. MAINTENANCE WAS ABLE TO RESET SLATS AND ACCOMPLISHED A RETURN TO SERVICE TEST. 2 L 7 2 4F RT A56NM 2007112700090 20071127 00090 SO 2007 11 27 C2XA07IA232 1 20071118 A 2612 3601133500230 FIRE LOOP EMB 145 EMB145LR 3260212 SO LEFT NACELLE INOPERATIVE A C2XA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 27 12540 14289 14289 145537 IAH - FLIGHT 2713, THE CREW REPORTED THE ENGINE 1 FIRE DETECTOR FAIL CAUTION MESSAGE ON EICAS IN FLIGHT. THE CREW COMPL ETED THE QRH WITH THE MESSAGE NOT CLEARING, AND NO OTHER ISSUES NOTED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHER E MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE FIRE LOOP, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCR AFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007112700091 20071127 00091 SO 2007 11 27 C2XA07IA233 1 20071118 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO CABIN ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 13202 14500962 IAH - FLIGHT 409, THE CREW REPORTED A BURNING ACRID ODOR ON TAKEOFF IN THE CABIN. THE AIRCRAFT LANDED AT IAH WITHOUT IN CIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE ENGINE WITH NO DEFECTS NOTED, AND THE AIRCRAF T WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007112700092 20071127 00092 NM 2007 11 27 ASAA0752272 1 20071118 A 3110 LIGHT BOEING 737 737890 1384527 NM GLARESHIELD INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 584AS 35682 MODE CONTROL PANEL BACKGROUND LIGHTING INOP. REPLACED MODE CONTROL PANEL. OP CHECKS GOOD. BITE TEST PASS. 2 L 7 2 4F RT A16WE 2007112700093 20071127 00093 NM 2007 11 27 ASAA0752268 1 20071116 A 3610 62144464 VALVE BOEING 737 737890 1384527 NM ENG HIGH STAGE FAULTY A ASAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 02 579AS 35187 BLEED TRIP OFF LIGHT ILLUMINATED ON DEPARTURE FROM LIH. FOLLOWED QRH AND PROBLEM CLEARED. PERFORMED FIM 36 10 TASK 801 . REPLACED NR 2 ENGINE HIGH STAGE VALVE. PERFORMED REPAIR CONFIRMATION PER FIM 36 10 TASK 801. REPAIR CONFIRMED. 2 L 7 2 4F RT A16WE 2007112700094 20071127 00094 WP 2007 11 27 ASAA0782260 1 20071118 A 5311 591359577 FRAME DOUG DC9 DC983 3022083 WP BS 1418 S2L/R CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 977AS 53453 AFT ACCESSORY COMPT FRAME STA 1418 CRACKED IN RADIUS AT LONG 2R AND LONG 2L. TWO EACH CRACKS PREPARED DAMAGED AREA, STO P DRILLED CRACKS, VERIFIED CRACK TERMINATION IAW MD80 SRM 51-01 PG 9. RECEIVED REPLACEMENT REPAIR PARTS LOCATED, DRILLE D AND INSTALLED IAW MD80 SRM 53-03 FIG 31A. 2 L 7 2 4F RT A6WE 2007112700095 20071127 00095 NM 2007 11 27 ASAA0792261 1 20071111 A 5320 ANGLE BOEING 737 737990 NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 309AS 30857 FWD CARGO PIT LEFT ZEE ANGLE FOUND CORRODED AT BS 500F+12 TO BS 500L. LEFT ZEE ANGLE AT BS 500F+12 TO BS 500L LBL 21 RE PLACED WITH NEW PART IAW B737 950 SRM 53-00-53. 2 L 7 4 4F RT A16WE 2007112800003 20071128 00003 NM 2007 11 28 ASAA0792264 1 20071115 A 5320 143A750315 INTERCOSTAL BOEING 737 737990 NM BS 500K-500L CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 309AS 30857 FWD CARGO PIT FLOOR SUPPORT INTERCOSTAL FOUND CRACKED AT BS 500K TO 500L LBL 21. FLOOR SUPPORT INTERCOSTAL IN FWD CARGO AT BS 500K TO 500L LBL 21 REPLACED WITH MADE REPAIR PART IAW B737 900 SRM 51-40-02 AND 51-30-01. 2 L 7 4 4F RT A16WE 2007112800004 20071128 00004 NM 2007 11 28 ASAA0792265 1 20071114 A 5320 143A81225 SILL BOEING 737 737990 NM BS 440-500 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 309AS 30857 FWD CARGO PIT LWR SILL WEB FOUND CORRODED AT BS 440 BS 446 RBL 22-26. LWR SILL WEB IN FWD CARGO PIT AT 440 TO 500 RBL 2 2-26 REPLACED WITH MADE REPAIR PART IAW B737 900 SRM 51-30-01 AND 51-40-02. 2 L 7 4 4F RT A16WE 2007112800012 20071128 00012 WP 2007 11 28 ASAA0782259 1 20071118 A 5753 5930494509 VANE DOUG DC9 DC983 3022083 WP TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 977AS 53453 RIGHT I/B FLAP I/B VANE DENTED AT TOP SURFACE IN MIDDLE SECTION OF VANE. REMOVED DAMAGED AREA, FABRICATED FILLER AND RE PAIR DOUBLER PREPARED AREA BAND AREA AND FASTENERS IAW MD80 SRM 51-70-2 PGS 11, 23, 43, 45, 59 AND 63. 2 L 7 2 4F RT A6WE 2007112800014 20071128 00014 SO 2007 11 28 RAIA00711014 1 20071118 A 3222 STRUT EMB 145 EMB145 3260210 SO NLG LOW A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 834HK 145269 FLT NR 8018 - STL - GEAR FAILED TO RETRACT/LANDING GEAR GROUND FAIL MESSAGE. MAINTENANCE INSPECTED FOUND NOSE LANDING G EAR NEEDS SERVICED, PERFORMED LANDING GEAR EXTENSION RETRACTION TEST, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007112800015 20071128 00015 SO 2007 11 28 RAIA00711011 1 20071115 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 822HK 145069 POST FLT NR 5542 - STL - EMERGENCY LIGHT AT EMERGENCY EXITS LOOSE. MAINTENANCE RE-SECURED LIGHT STRIP, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007112800016 20071128 00016 SO 2007 11 28 RAIA00711012 1 20071117 A 3350 MS25231316 BULB EMB 145 EMB145 3260210 SO FLOOD LIGHT BURNED OUT A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 830HK 145313 POST FLT NR 5505 - STL - MAIN DOOR EXTERIOR FLOOD LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007112800027 20071128 00027 NM 2007 11 28 SWAA075735 1 20071117 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM RT OVRWING LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED 14Y CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY EXIT LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007112800028 20071128 00028 NM 2007 11 28 SWAA075736 1 20071117 A 3397 BR2013 WIRE BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 425LV 29829 EEPLS WIRE FOUND LOOSE BETWEEN ROW 12 TO ROW 14. RECONNECTED LOOSE WIRE PER MM. 2 L 7 2 4F RT A16WE 2007112800032 20071128 00032 NM 2007 11 28 SWAA075741 1 20071116 A 5230 6547952 DOOR FRAME BOEING 737 7375H4 138449D NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED SPECIAL VISIT, FOUND AFT CARGO DOOR FRAME LOWER FWD CORNER CRACKED. REMOVED AND REPLACED AFT CARGO DOO R PER MM. 2 L 7 2 4F RT A16WE 2007112800038 20071128 00038 2007 11 28 SWAA075744 4 20071116 A 2565 6557463 GIRT BAR BOEING 737 7373G7 1384595 NM R2 DOOR SLIDE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR AFT GIRT BAR ATTACH FITTING LOOSE. SECURED AFT GIRT BAR ATTACH FITTING PER MM . 2 L 7 2 4F RT A16WE 2007112800039 20071128 00039 NM 2007 11 28 SWAA075746 1 20071117 A 5315 6546811 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 757LV 29850 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 47 TO LBL 47. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2007112800041 20071128 00041 EA 2007 11 28 TRAX200701727 1 20071113 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA ACCESS PANEL CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 883AS 7504 AAR - FUEL ACCESS CUTOUT 640BB HAS CORROSION ON O/B SIDE. CORROSION AT CUTOUT 540BB REMOVED PER REO 601R-57-21-030 ON E LITE STRUCTURAL SERVICER. SUPPLEMENTAL - SDR CLOSED 11/20/07. 2 L 7 2 4F RT A21EA 2007112800042 20071128 00042 EA 2007 11 28 TRAX200701734 1 20071115 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 761ND 10213 LEFT LOWER FS 280 WEB IS CORRODED. BLENDED MINOR SURFACE CORROSION WITHIN LIMITS TO MAX DEPTH OF.004, TREATED, PRIMED A ND PAINTED BLEND OUT IAW REO 670-53-11-052. 2 L 7 2 4F RT A21EA 2007112800043 20071128 00043 EU 2007 11 28 YENA2007099 1 20071116 A 2782 1703909 ACTUATOR EMB ERJ190 ERJ190100IGW 3260408 EU SLATS FAILED A YENA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 EA 15 231JB 3922 19000033 SLAT FAIL ON APPROACH, TROUBLESHOOT OF SLAT FAIL/SLAT SYS FOUND SLAT ACTUATOR NR 5 AT SLAT TRACK NR 6, TORQUE LIMITER TR IP INDICATOR PLASTIC HOUSING BROKEN. REMOVED AND REPLACED NR 5 SLAT ACTUATOR AT SLAT TRACK NR 6 PER AMM 27-81-01-420-00 5-A. PERFORMED SLAT CTL SYSTEM RIGGING PER AMM 27-80-00-710-801. OPS CHECK GOOD. 2 L 7 2 4F RT A57NM 2007112800044 20071128 00044 EA 2007 11 28 TRAX200701738 1 20071116 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA DOOR STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 ASD OUTER HANDLE IS HARD TO OPEN. FLT 4918 DEL 80 MINS. 2 L 7 2 4F RT A21EA 2007112800051 20071128 00051 EU 2007 11 28 USAA920071168 1 20071015 A 5315 D53472172205 FLOORBEAM AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3158 / FR 66, -Y1292. REPAIRED CABIN FLOORBEAM, BS 31 58 / FR 66, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007112800055 20071128 00055 NM 2007 11 28 USAA920071172 1 20071116 A 5314 KEELBEAM BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, CRACKED LEFT HAND KEEL BEAM ANGLE, BS 685 INSIDE LEFT MAIN LANDING GEAR WHEEL WELL. REP AIRED LEFT HAND KEEL BEAM ANGLE, BS 685 INSIDE LEFT MAIN LANDING GEAR WHEEL WELL IAW B737 SRM 51-70-11. 2 L 7 2 4F RT A16WE 2007112800056 20071128 00056 EU 2007 11 28 USAA920071173 1 20071119 A 5320 DAN2001T79511 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 625AW 64 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOOR SUPPORT, BS 3158 / FR 66 - BS 32157 / FR 68, +Y1292. REPLACED CABIN FLOOR SUPPORT, BS 3158 / FR 66 - BS 32157 / FR 68, +Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007112800057 20071128 00057 EU 2007 11 28 USAA920071174 1 20071119 A 5320 D5311208720009 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 625AW 64 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 605 / FR 12 - BS 950 / FR 24, +Y254. REPLACED CABIN FL OORBEAM, BS 605 / FR 12 - BS 950 / FR 24, +Y254 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007112800058 20071128 00058 NM 2007 11 28 USAA920071175 1 20071117 A 5320 149N755319 CHANNEL BOEING 757 757225 1384959 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 921UW 22201 PIT - MAJOR REPAIR - C3 CHECK, CRACKED CANTED FRAME CHANNEL, BS 1068. REPAIRED CANTED FRAME, BS 1068 IAW B757 SRM 53-00 -07. 2 L 7 2 4F RT A2NM 2007112800059 20071128 00059 NM 2007 11 28 USAA920071176 1 20071116 A 5753 SKIN BOEING 737 737301 1384611 NM ZONE 500 DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 591US BN743 23936 CLT - MAJOR REPAIR - C6 CHECK, LEFT WING OUTBOARD AFT FLAP LOWER SURFACE DELAMINATED, WS 395. REPLACED LEFT WING OUTBOA RD AFT FLAP IAW B737 AMM 27-51-39. 2 L 7 2 4F RT A16WE 2007112800060 20071128 00060 NM 2007 11 28 2007UALA03192 1 20070815 A 5210 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU TORQUE TUBE CTOT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 AFT ENTRY DOOR TORQUE TUBE HINGE CUTOUT UPPER FWD CORNER CRACKED. ROUTED OUT DAMAGE, WITHIN LIMITS. ACCOMPLISHED NDT I NSPECTION, NO DEFECTS NOTED. ALODINE, PRIME & PAINTED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112800067 20071128 00067 NM 2007 11 28 2007UALA04703 1 20071115 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 380 MISREPAIRED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 301UA 23642 BS 380 AT E&E COMPARTMENT EXHAUST OUTLET LOWER EXTERNAL FUSELAGE SKIN EXISTING REPAIR IS INSUFFICIENT. REMOVED PREVIOU S REPAIR. INSTALLED NEW LARGE AREA DOUBLER AND PREVENTATIVE RAIDO ALTIMETER CUTOUT DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112800068 20071128 00068 NM 2007 11 28 2007UALA04704 1 20071115 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 440 S24R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 301UA 23642 FWD CARGO DOOR CUTOUT, FWD FRAME CRACKED AT INNER CHORD RADIUS ABOVE LWR DOOR STOP FITTING, AT BS 440 STR 24R. REMOVED DAMAGE. INSTALLED ANGLE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112800069 20071128 00069 NM 2007 11 28 2007UALA04705 1 20071115 A 5730 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RT WING LE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 301UA 23642 RIGHT LEADING EDGE SKIN UPPER SURFACE CRACKED AND SEPARATED, AND GOUGED ABOVE NR 4 SLAT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112800070 20071128 00070 NM 2007 11 28 2007UALA04707 1 20071115 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 DOOR R2 FWD UPPER HINGE CUTOUT CRACKED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007112800073 20071128 00073 NM 2007 11 28 2007UALA04710 1 20071116 A 5754 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 12 SLAT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 795UA 26927 NR 12 L/E SLAT LOWER SKIN NEAR MID HAS 6 INCH LONG CREASE. CUT OUT DAMAGE ON EXT SKIN AND INTERIOR NOSE BEAM, FABRICATE D FILLER AND DOUBLER. INSTALLED REPAIR. AC OK FOR SERVICE 2 L 7 2 4F 4 F RT T0001SE E46NE 2007112800074 20071128 00074 NM 2007 11 28 2007UALA04711 1 20071116 A 5753 WEDGE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RT TE FLAP DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 795UA 26927 RIGHT MID FLAP TRAILING EDGE WEDGE IS CRUSHED AND CUT THROUGH. SUSPECTED TRAILING EDGE DAMAGED DURING GROUND MAINTENAN CE. CATEGORY A REPAIR OF ACCOMPLISHED. NO FUTURE INSPECTION REQUIRED. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007112800075 20071128 00075 NM 2007 11 28 2007UALA04712 1 20071115 A 3320 BD10007001 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE GALLEY LIGHT SHORTED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 107UA 26900 BC GALLEY WHEN CEILING LIGHTS ARE TURNED ON SMOKE AND ELECT ODOR IS PRESENT. FOUND SHORTED LIGHT ASSEMBLY. REPLACED LI GHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112800076 20071128 00076 NM 2007 11 28 2007UALA04713 1 20071116 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 36 ABC INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY LIGHTS INOP AT 4A FWD AND 36 ABC. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112800077 20071128 00077 NM 2007 11 28 2007UALA04714 1 20071116 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY LIGHT INOP AT 48 HJK. FOUND CONNECTOR UNSECURE. RECONNECTED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112800078 20071128 00078 NE 2007 11 28 2007UALA04715 2 20071115 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 2 FIRE A UALA D RETURN TO BLOCK A J FLAME/FIRE WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 206UA 30212 222257 NR 2 ENG FAILED TO START. FIRE NOTED IN TAILPIPE DURING ATTEMPT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007112800079 20071128 00079 2007 11 28 2007UALA04718 4 20071106 A 2565 62510101 ASPIRATOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE ESCAPE SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 778UA 0107 26940 LOWER TUBE ASPIRATORS ARE LEAKING. REPLACED ASPIRATOR DURING SLIDE OVERHAUL. SUSPECT ASPIRATOR CRUSHED DURING ASSEMBLY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007112800088 20071128 00088 NM 2007 11 28 2007UALA04728 1 20071117 A 5542 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE RUDDER DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 846UA 1600 RUDDER T/E HAS AN AREA OF DELAMINATION 7" BY 80", TOP OF DAMAGE IS 90" BELOW TIP AND BOTTOM OF DAMAGE IS 79" FROM BOTTOM OF RUDDER. REPLACED RUDDER & OP CHK'D ON NR G7263I. INSTALLED RUDDER IS TS1274. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112800090 20071128 00090 NM 2007 11 28 2007UALA04730 1 20071118 A 3510 OXYGEN SYSTEM BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 927UA 26649 CREW O2 LOW READS 575 PSI. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112800092 20071128 00092 NM 2007 11 28 2007UALA04735 1 20071118 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 SEATS 4J FWD, 47ABC & 50ABC EMERGENCY LIGHTS ARE INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112800093 20071128 00093 NM 2007 11 28 2007UALA04736 1 20071118 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 DOOR 2 LEFT SILL FWD EMERGENCY LIGHT IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112800094 20071128 00094 NM 2007 11 28 2007UALA04737 1 20071118 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 UPPER DECK CEILING EMERGENCY LIGHT 2 EA IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112800095 20071128 00095 NM 2007 11 28 2007UALA04738 1 20071117 A 3397 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 4R SLIDE MISWIRED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 522UA 24931 DOOR 4R, "SLIDE" SIGN ABOVE DOOR INOP. ARMING DOOR POPS C-B. 2 L 7 2 4F 4 F RT A2NM E17NE 2007112800096 20071128 00096 NM 2007 11 28 2007UALA04739 1 20071118 A 3350 SOCKET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS CORRODED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 586UA 26710 EXTERIOR EMERGENCY LIGHTS AT DOORS 1R & 4R ARE INOP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007112800097 20071128 00097 NM 2007 11 28 2007UALA04740 1 20071117 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 653UA 25391 FLOOR EEL LIGHTS INOPERATIVE AT 10E. FOUND TERMINAL CONNECTOR LOOSE, SECURED AND OPS CK NOW OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007112800100 20071128 00100 NM 2007 11 28 2007UALA04743 1 20071117 A 3350 1317 LAMP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 223UA 30224 DOOR 4R EXTERIOR EMERGENCY LIGHT IS INOP. RELAMPED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007112800101 20071128 00101 NM 2007 11 28 2007UALA04744 1 20071118 A 3350 SIGN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU RT OVERWING UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 932UA 26658 EMERGENCY EXIT SIGN OVER RIGHT SIDE OVERWING HAS FALLEN OFF. SECURED SIGN. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112800104 20071128 00104 NM 2007 11 28 SCNA07012 1 20071120 A 3350 LIGHT BOEING 737 737800* NM CABIN LOOSE A SCNA O OTHER O OTHER CR CRUISE 1 GL 15 PHHZV 30650 FLIGHT CREW REPORTED ROWS 11-12 EMERGENCY TRACK LIGHTING STICKING UP OFF THE FLOOR. MAINTENANCE RESECURED TRACK LIGHTIN G AT ROWS 11-12 AS REQUIRED. 2 L 7 2 4F RT A16WE 2007112800106 20071128 00106 SO 2007 11 28 C2XA07CL099 1 20071120 A 3350 7287100507 CONTROL PANEL EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14148 145751 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT SWITCH AT THE FORWARD FLIGHT ATTENDANT STATION WAS INOPERATIVE. MAINTENA NCE INSPECTED AND REPLACED THE ATTENDANT CONTROL PANEL. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2007112800107 20071128 00107 EA 2007 11 28 TRAX200701743 1 20071117 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR SEPARATED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 903EV 7621 PAX DOOR BOTTOM STEP SEPARATING AT ATTACH POINT. 2 L 7 2 4F RT A21EA 2007112800109 20071128 00109 EA 2007 11 28 TRAX200701745 1 20071117 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA ROWS6CD-12CD INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 921EV 7819 CABIN FLOOR EMERGENCY LIGHTS AT ROWS 6CD THRU 12CD ARE INOP. 2 L 7 2 4F RT A21EA 2007112800110 20071128 00110 EA 2007 11 28 TRAX200701746 1 20071117 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 PAX DOOR HANDLE DIFFICULT TO OPERATE. 2 L 7 2 4F RT A21EA 2007112800111 20071128 00111 EA 2007 11 28 TRAX200701747 1 20071117 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 BOTH OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. CABIN INTERIOR LIGHTS. 2 L 7 2 4F RT A21EA 2007112800112 20071128 00112 EA 2007 11 28 TRAX200701748 1 20071117 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 920EV 7810 MAIN DOOR EXIT SIGN PLACARD AND DOOR "OPEN" PLACARD IN EXIT WAY NEEDS TO BE REPLACED. 2 L 7 2 4F RT A21EA 2007112800113 20071128 00113 EA 2007 11 28 TRAX200701749 1 20071117 A 5240 HANDLE CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 390CA 10106 F/A REPORTS SERVICE DOOR HANDLE DIFFICULT TO OPEN FULLY. 2 L 7 2 4F RT A21EA 2007112800115 20071128 00115 EA 2007 11 28 TRAX200701751 1 20071118 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA WINGS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 933EV 8022 LT AND RT WING LEADING EDGE EMERGENCY LIGHTS INOP. 2 L 7 2 4F RT A21EA 2007112800116 20071128 00116 EA 2007 11 28 TRAX200701752 1 20071118 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 880AS 7606 CAPT'S FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2007112800117 20071128 00117 EA 2007 11 28 TRAX200701753 1 20071118 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS UNKNOWN A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 971EV 7528 FLAP FAIL AT 0. EMERGENCY EQUIPMENT ON STANDBY. FLT 4693 CX. 2 L 7 2 4F RT A21EA 2007112800119 20071128 00119 EA 2007 11 28 TRAX200701756 1 20071119 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 MAIN CABIN DOOR VERY DIFFICULT TO OPEN FROM THE OUTSIDE. 2 L 7 2 4F RT A21EA 2007112800120 20071128 00120 EA 2007 11 28 TRAX200701757 1 20071119 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA CABIN WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 971EV 7528 THE "EXIT" PLACARD ON ASD WORN. 2 L 7 2 4F RT A21EA 2007112800121 20071128 00121 EU 2007 11 28 TRAX200701758 1 20071119 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 F/A REPORTS TRACK LIGHTING AT 8AB BROKEN. 2 H 7 2 4T RT 2007112800122 20071128 00122 EA 2007 11 28 TRAX200701759 1 20071120 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 970EV 7527 EMERGENCY FLOOR TRACK LIGHTING FROM 1CD-5CD INOP. 2 L 7 2 4F RT A21EA 2007112800123 20071128 00123 NM 2007 11 28 USAA920071180 1 20071109 A 5320 141N516076 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 200UU 27809 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR STRUCTURE ANGLE, BS 310 - BS 324, RBL 45.50. REPLACED CABIN FLOOR STRUCTURE ANGLE, BS 310 - BS 324, RBL 45.50 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007112800125 20071128 00125 NM 2007 11 28 USAA920071182 1 20071107 A 5320 141N5160 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 200UU 27809 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR STRUCTURE CHANNEL, BS 310 - BS 324, RBL 45.50. REPLACE D CABIN FLOOR STRUCTURE CHANNEL, BS 310 - BS 324, RBL 45.50 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007112800126 20071128 00126 NM 2007 11 28 USAA920071177 1 20071116 A 5755 SKIN BOEING 737 737301 1384611 NM SPOILER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 591US MA11473 23936 CLT - MAJOR REPAIR - C6 CHECK, LEFT WING SPOILER NUMBER 0 UPPER AND LOWER SURFACES DELAMINATED, WS 447 - WS 499. REPLAC ED LEFT WING SPOILER NUMBER 0, IAW B737 AMM 27-62-91. 2 L 7 2 4F RT A16WE 2007112800127 20071128 00127 EU 2007 11 28 SA07076 1 20071118 A 2120 UNKNOWN AIRBUS A319 A319112 3930323 EU CABIN ODOR A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 722US 1097 MCI FLT 1609 MCI - CLT. A STRONG ODOR WAS NOTED IN THE CABIN. MAINTENANCE ACTION PENDING. 2 L 7 2 4F RT A28NM 2007112800128 20071128 00128 NM 2007 11 28 SA07077 1 20071120 A 3350 BATTERY PACK AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 802AW 0924 ATL - THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE IN THE FORWARD CABIN. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY LIG HTS. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2007112800129 20071128 00129 NM 2007 11 28 USAA920071184 1 20071118 A 2612 FIRE WARNING BOEING 737 7373G7 1384595 NM APU BAY ACTIVATED A USAA O OTHER J WARNING INDICATION DE DESCENT 1 EA 19 306AW 24633 LAS - SMF - FLT 226 - CREW REPORTED DURING DESCENT TRIED TO START APU. APU FIRE WARNING HORN SOUNDED, CREW DISCHARGED F IRE BOTTLE, FIRE WARNING INDICATION EXTINGUISHED. THE CREW DECLARED AN EMERGENCY AND THE CABIN WAS PREPPED IN CASE FURT HER EMERGENCY ACTION WAS NECESSARY. THE LANDING WAS UNEVENTFUL AND THE AIRCRAFT TAXIED TO THE GATE. MX PLACED THE APU ON MEL. OPEN 2 L 7 2 4F RT A16WE 2007112800130 20071128 00130 NM 2007 11 28 USAA920071183 1 20071119 A 3350 321454 BATTERY PACK BOEING 737 7373B7 1384580 NM EMERGENCY LIGHTS FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 529AU 24411 BDL - FLT 1724 - MX REPORTED SEVERAL EMERGENCY LIGHTS IN AFT CABIN ARE INOP. MX REPLACED BATTERY PACK. OPERATIONAL CHE CK WAS GOOD. 2 L 7 2 4F RT A16WE 2007112800131 20071128 00131 NM 2007 11 28 SWAA075762 1 20071115 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727E S22L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727E, STR 22L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007112800132 20071128 00132 NM 2007 11 28 SWAA075768 1 20071115 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 767 S25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 767, STR 25R. REMOVED AND REPLACED CLIP PER S RM. 2 L 7 2 4F RT A16WE 2007112800133 20071128 00133 NM 2007 11 28 SWAA075767 1 20071115 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 767 S22L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 767, STR 22L. REMOVED AND REPLACED CLIP PER S RM. 2 L 7 2 4F RT A16WE 2007112800134 20071128 00134 NM 2007 11 28 SWAA075766 1 20071115 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 787 S20L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 787, STR 20L. REMOVED AND REPLACED CLIP PER S RM. 2 L 7 2 4F RT A16WE 2007112800135 20071128 00135 NM 2007 11 28 SWAA075765 1 20071115 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727E S20L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727E, STR 20L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007112800136 20071128 00136 NM 2007 11 28 SWAA075763 1 20071115 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 767 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 767, STR 21L. REMOVED AND REPLACED CLIP PER S RM. 2 L 7 2 4F RT A16WE 2007112800137 20071128 00137 NM 2007 11 28 SWAA075769 1 20071115 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 887 S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 887, STR 24L. REMOVED AND REPLACED CLIP PER S RM. 2 L 7 2 4F RT A16WE 2007112800140 20071128 00140 NM 2007 11 28 SWAA075759 1 20071115 A 5753 SKIN BOEING 737 7373H4 1384600 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRIDGE CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED RIGHT WING O UTBOARD AFT FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007112800144 20071128 00144 NM 2007 11 28 SWAA075764 1 20071115 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 787 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 787, STR 21L. REMOVED AND REPLACED CLIP PER S RM. 2 L 7 2 4F RT A16WE 2007112800146 20071128 00146 NM 2007 11 28 SWAA075771 1 20071115 A 5330 6518420 SKIN BOEING 737 7373H4 1384600 NM BS 258 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 258, WL 181.5, LEFT SIDE. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007112800148 20071128 00148 NM 2007 11 28 SWAA075784 1 20071119 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 727E S22R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 2, STR 22R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007112800150 20071128 00150 NM 2007 11 28 SWAA075787 1 20071119 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 727E S22-23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727E + 2 TO BS 727E + 3, BETWEEN STR 22L TO STR 2 3L. REPAIRED SKIN PER SWA EA & SRM. 2 L 7 2 4F RT A16WE 2007112600035 20071126 00035 EA 2007 11 26 QXEA200701608 1 20071023 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 385-421 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 C4 PDX - LEFT CENTER CABIN SEAT TRACK NR 9 STATION X421 TO X385 HAS PITTING CORROSION, NICKS, SCRATCHES. REPAIRED IAW A MM53-00-49-000-801-A01. 2 L 7 2 4F RT A21EA 2007112600039 20071126 00039 EA 2007 11 26 QXEA200701613 1 20071022 A 5320 INTERCOSTAL CNDAIR CL600 CL6002C10 1390015 EA BS 280-295 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 C4 PDX -THE TRIANGLER DOUBLER IN THE FLOOR LEVEL INTERCOSTAL BETWEEN BEAMS 280 AND 295 RIGHT SIDE HAS SURFACE CORROSION BETWEEN STATION 280 AND 284 ALONG THE INBOARD RIVET. REPAIRED IAW SRM 53-21-43, 51-25-06. 2 L 7 2 4F RT A21EA 2007112600042 20071126 00042 NM 2007 11 26 QXEA200701666 1 20071102 A 5230 ANGLE BOMBDR DHC8 DHC8402 1390042 NM CARGO BAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - FOUND CORROSION UNDER FORWARD BAG DOOR ANGLE/KICK PLATE. REPAIRED IAW SRM 53-20-25, 51-21-10, 51-25-10. 2 H 7 2 4T RT A13NM 2007112600043 20071126 00043 NM 2007 11 26 QXEA200701663 1 20071106 A 5210 ROD END BOMBDR DHC8 DHC8402 1390042 NM DOOR HANDLE BENT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - MAIN CABIN DOOR AFT HANDLE RAIL ASSY UPPER STRUT ROD END BENT. ROD END WEARING ON LOWER STRUT AT ATTCH POINT. REPAIRED IAW AMM 52-11-00. 2 H 7 2 4T RT A13NM 2007112600049 20071126 00049 NM 2007 11 26 QXEA200701670 1 20071102 A 5320 CHANNEL BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - THE OUTBOARD HAT CHANNEL SUPPORT FOR COAT CLOSET PAN HAS CORROSION AT THE INBOARD END, STARTING FROM THE PANEL EDGE, AFT. REPAIRED IAW SRM 51-14-00, 51-42-05, 51-42-35. 2 H 7 2 4T RT A13NM 2007112600056 20071126 00056 EU 2007 11 26 NWAA073743303 1 20071102 A 5712 RIB AIRBUS 330 A330323 3930335 EU LT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 803NW 0542 DURING INSPECTION PER AD 2006-22-14, FOUND CRACK IN RIB 6 RT AND RIB 6 LT. REPAIRED PER EA 33-211191. 2 L 7 2 4F RT A46NM 2007112600070 20071126 00070 NM 2007 11 26 QXEA200701688 1 20071031 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 292-296 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION IN BOTTOM OF CHANNEL BETWEEN STATION X292 AND X296. REPAIRED IAW RD8/4 -53-884. 2 H 7 2 4T RT A13NM 2007112600077 20071126 00077 NM 2007 11 26 QXEA200701696 1 20071031 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 417-420 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION IN CHANNEL BETWEEN STATION X417 AND X420. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007112600079 20071126 00079 NM 2007 11 26 QXEA200701701 1 20071101 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 722-777 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 417QX 4086 C2 PDX - LIGHT SURFACE CORROSION ON AFT CARGO PIT FLOOR ADJACENT TO SEAT TRACK NR 9 AT STATIONS X777, 775, 769, 762, 733 , AND 722. REPAIRED IAW SRM 51-21-00, 51-21-10. 2 H 7 2 4T RT A13NM 2007112600090 20071126 00090 WP 2007 11 26 NWAA073759929 1 20071104 A 2780 CONTROL SYSTEM DOUG DC9 DC931 3022065 WP SLATS OUT OF RIG A NWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 01 8923E 45838 WHEN THE SLATS WERE SELECTED TO EXTEND DURING THE APPROACH FOR LANDING, THE BLUE "SLAT DISAGREE" LIGHT ILLUMINATED AND W AS ACCOMPANIED BY AN AIRCRAFT ROLL TO THE RIGHT. THE FLAP/SLAT COMBINATION WAS RECYCLED AND THE FIRST OFFICER VISUALLY VERIFIED FLAPS HAD EXTENDED. AFTER A 5 MINUTE PAUSE THE SLATS EXTENDED EQUALLY, FULLY, AND ALL COCKPIT INDICATIONS WE RE NORMAL. THE FLIGHT CREW PERFORMED AN UNEVENTFUL LANDING AT MBS. AIRCRAFT WAS FERRIED TO DTW WHERE MAINTENANCE REPLA CED SLAT CONTROL CABLES AND PULLEYS, RIGGED THE CONTROL SYSTEM, AND FUNCTIONALLY CHECKED ALL WING DEVICES. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2007112600091 20071126 00091 SO 2007 11 26 CHQA200700076 1 20071110 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LAVATORY MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 266SK 145241 CAE311208 CLE TO RDU - DURING CLIMB-OUT AT APPROXIMATELY 800 FT, CREW RECEIVED A LAV SMOKE EICAS MESSAGE. THE FLIGHT ATTENDANT CH ECKED THE LAVATORY AND REPORTED NO SIGNS OF SMOKE, FIRE OR HEAT. THE APPROPRIATE CHECKLISTS WERE FOLLOWED AND THE AIRCR AFT LANDED BACK AT CLE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO DEFECTS. THE LAVATORY SMOKE D ETECTOR WAS REPLACED, AND THE AIRCRAFT WAS RELEASED BACK TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007112600092 20071126 00092 GL 2007 11 26 CHQA200700077 2 20071111 A 7200 AE3007A1P ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 ODOR A CHQA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 11 266SK 17549 9614 145241 CAE311208 CLE TO DCA - AFTER ROTATION DEPARTING CLE, CREW RECEIVED "LANDING GEAR AIR/GND FAIL" EICAS MESSAGE. ONCE POSITIVE CLIMB RATE WAS ESTABLISHED, THE LANDING GEAR WOULD NOT RETRACT. THE LANDING GEAR HANDLE WOULD NOT MOVE, SO THE GEAR WAS LEFT DOWN AND LOCKED. ONCE CLIMB THRUST WAS APPLIED A "LAV SMOKE" EICAS MESSAGE APPEARED ACCOMPANIED BY THE LAVATORY SMOKE ALARM IN THE CABIN. THE FLIGHT ATTENDANT REPORTED SMELLING AN ODOR OF SOMETHING HOT. AT THIS POINT AN EMERGENCY WAS DE CLARED AND THE AIRCRAFT PREPARED TO RETURN TO FIELD. AFTER THREE OR FOUR MINUTES THE EICAS MESSAGE AND SMOKE ALARM STOP PED AND THE ODOR DISAPPEARED. THE APPROPRIATE QRH CHECKLISTS WERE FOLLOWED FOR AIR/GROUND FAIL AND CABIN SMOKE. THE AI 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007112600118 20071126 00118 EA 2007 11 26 SWIA200718844 1 20070727 A 5310 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 LEFT EMERGENCY EXIT DOOR SURROUND HAS CORRODED HINGE PINS, FOUND AT C-CHECK. REPLACED PINS ON LEFT EMERGENCY EXIT DOOR SURROUND PER CRJ200 AMM 20-24-00-910-801. 2 L 7 2 4F RT A21EA 2007112600138 20071126 00138 EA 2007 11 26 TRAX200701712 1 20071110 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 843AS 7310 MAIN CABIN DOOR OUTER HANDLE WOULD NOT STOW FROM INSIDE OF A/C, HAD TO GET GROUND PERSONEL TO CLOSE FROM OUTSIDE. THAT STILL TOOK SEVERAL ATTEMPTS. 2 L 7 2 4F RT A21EA 2007112600139 20071126 00139 EA 2007 11 26 TRAX200701713 1 20071110 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 920EV 7810 CABIN FLOOR EMERG LIGHTS AT ROWS 4CD THRU 8CD ARE INOP. 2 L 7 2 4F RT A21EA 2007112600143 20071126 00143 EU 2007 11 26 SIMA200731803 1 20071112 A 3260 387 BULB SAAB SF340 340B 7860101 EU MLG INDICATOR INOPERATIVE A SIMA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SW 21 298AE 340B298 CREW REPORTED ON APPROACH AFTER LANDING GEAR SELECTED TO THE DOWN POSITION. CREW DID NOT GET LEFT LANDING GEAR DOWN AND LOCK INDICATION ON THE CONTROL PANEL. CREW ABORTED APPROACH. CREW FOLLOWED AOM PROCEDURES. CREW DECLARED AN EMERGENC Y. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENT. REMOVED AND REPLACED LIGHT BULB. OPS CHECK GOOD IAW SAAB 340 AMM 32-12-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007112600152 20071126 00152 NM 2007 11 26 07FDEA04783 1 20071113 A 5753 STOP FITTING DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 RIGHT WING OUTBOARD FLAP SECONDARY UP STOP FITTING FOUND CRACKED. RIGHT HAND WING OUTBOARD FLAP ASSEMBLY REMOVED AND R EPLACED AS PER AMM 27-50- 30-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM N00654 FOR WORK DETAILS. 2 L 7 3 4F RT A22WE 2007112600174 20071126 00174 NM 2007 11 26 QXEA200701722 1 20071115 A 2930 9604417 SWITCH BOMBDR DHC8 DHC8402 1390042 NM HYD TEMP MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 423QX 1513 4153 SEA FLIGHT NR 2490: NR 1 HYD PUMP FAILED AND CAUTION LIGHT DURING CLIMB-OUT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE F OUND GOOD QUANTITY LEVEL IN NR 1 HYD SYSTEM. FOUND ALL 3 DPI'S AND IN AND ON THE NR 1 HYD SYSTEM. UNABLE TO DUPLICATE PROBLEM. SUSPECT NR 1 HYD RESERVOIR LOW LIMIT SWITCH. REPLACED THE NR 1 HYD RESERVOIR AND THE RESERVOIR 225 DEG F TEMP SWITCHES IAW D8-400 MM 29-11-16-000-801 AND 29-11-16-400-801 AND 29-11-00-710-807. OPS CHECK GOOD. NO LEAKS NOTED. A IRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007112600177 20071126 00177 NM 2007 11 26 USAA920071144 1 20071107 A 5320 6055199 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 200UU 27809 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 1660 - BS 1681, RBL 58, WL 208. REPLACED C ABIN FLOOR SUPPORT, BS 1660 - BS 1681, RBL 58, WL 208 IAW 757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007112600183 20071126 00183 EA 2007 11 26 SWIA200718857 1 20070823 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA TRANSDUCER CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 978SW 7953 BRAKE TRANSDUCER IN RIGHT WHEEL WELL IS CRACKED, FOUND AT C-CHECK. INSTALLED BRAKE TRANSDUCER BRACKET PER CRJ200 SRM PG S 4-14. 2 L 7 2 4F RT A21EA 2007112600188 20071126 00188 EA 2007 11 26 SWIA200718862 1 20070820 A 5320 THRESHOLD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 934SW 7722 SERVICE DOOR THRESHOLD SHOWS SIGNS OF CORROSION, FOUND AT C-CHECK. REPLACED SERVICE DOOR THRESHOLD PER CRJ200 SRM 51-41 -02 PG 1-7. 2 L 7 2 4F RT A21EA 2007112600197 20071126 00197 EA 2007 11 26 QXEA20071714 1 20071110 A 2612 47388904 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA FIRE DETECTION FAULTED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 601QX 12703 12679 10009 DEN - RECEIVED A FIRE SYSTEM FAULT MESSAGE. MAINTENANCE REPLACED THE FIDEEX CONTROL UNIT. OPERATIONAL CHECKS GOOD. AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007112700006 20071127 00006 NM 2007 11 27 SWAA075704 1 20071114 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007112700010 20071127 00010 NM 2007 11 27 SWAA075708 1 20071114 A 3350 417N5212 CAP BOEING 737 73776Q 13845AA NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 550WN 30279 EEPLS END CAP LOOSE AT ROW 1 ABC. SECURED END CAP PER MM. 2 L 7 2 4F RT A16WE 2007112700018 20071127 00018 NM 2007 11 27 SWAA075715 1 20071114 A 2560 PH22300L GLOWSTRIP BOEING 737 7373G7 1384595 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007112700026 20071127 00026 NM 2007 11 27 CALA0700690 1 20071115 A 5320 655584311 CHANNEL BOEING 737 7373T0 1384582 NM BS 967-986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND AFT DRAIN MAST MOUNTING CHANNEL CORRODED FROM STA 967-986.5 BETWEEN S24L AND S25L. THE DRAIN MAST CHAN NEL WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND BAC DRAWING 65-55843. 2 L 7 2 4F RT A16WE 2007112700041 20071127 00041 2007 11 27 SWAA075720 4 20071115 A 2565 57463 GIRT BAR BOEING 737 7373H4 1384600 NM L1 DOOR SLIDE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FIT TING PER SRM. 2 L 7 2 4F RT A16WE 2007112700042 20071127 00042 NM 2007 11 27 SWAA075719 1 20071115 A 5312 6545819 PRESSURE PANEL BOEING 737 7373H4 1384600 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED BRDG CHECK, FOUND NLG W/W RIGHT CEILING PANEL CUTOUT WEB CRACKED AT INBOARD CORNER. REPAIRED WEB PER A CO. 2 L 7 2 4F RT A16WE 2007112700043 20071127 00043 NM 2007 11 27 SWAA075721 1 20071115 A 5330 6545770 SKIN BOEING 737 7373H4 1384600 NM BS 678 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 678, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007112700047 20071127 00047 NM 2007 11 27 SWAA075724 1 20071115 A 5512 182A4401 SKIN BOEING 737 7377H4 1384404 NM HORIZONAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 430WN 33659 DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007112700048 20071127 00048 NM 2007 11 27 SWAA075729 1 20071115 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM BS 492 S17R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED SPV CHECK, FOUND BELTFRAME CRACKED AT BS 492, STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007112700049 20071127 00049 NM 2007 11 27 SWAA075726 1 20071115 A 5753 SKIN BOEING 737 7373Q8 1384670 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 2216 23256 DURING SCHEDULED MV2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007112700050 20071127 00050 2007 11 27 SWAA075727 4 20071115 A 2565 D31354 SLIDE BOEING 737 7373T5 1384608 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007112700051 20071127 00051 2007 11 27 SWAA075728 4 20071115 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 786SW 29811 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007112700052 20071127 00052 NM 2007 11 27 ASAA0752256 1 20071115 A 2133 71231997302 CONTROLLER BOEING 737 737890 1384527 NM CABIN PRESSURE MALFUNCTIONED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 585AS 35683 AUTO FLIGHT ALTITUDE WINDOW NUMBERS WILL NOT CHANGE. ACCOMPLISHED BITE CHECK ON NR 1 AUTO PRESSURE CONTROLLER. LOGGED FAULT "AIRCRAFT RATE HI". ACCOMPLISHED FIM 21 31 TASK 815. SYSTEM RE-SET. OP CHECK GOOD. 2 L 7 2 4F RT A16WE 2007112700053 20071127 00053 2007 11 27 ASAA0752255 4 20071115 A 3442 6225135202 ANTENNA BOEING 737 737890 1384527 NM WX RADAR INTERMITTENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 583AS 35681 WITH WX SELECTED WEATHER RADAR DISPLAYS RETURN ON LEFT SIDE OF SCREEN WITH GREATER INTENSITY THAN ON RIGHT SIDE AS IF TH E ANTENNA IS TILTED TO LEFT. ALSO TWO GHOST RETURNS ABOUT 2 MILES LEFT AND RIGHT AHEAD OF ACFT POSTION. ALL GAIN LEVEL S. ACCOMPLISHED WXR SYSTEM OPERATIONAL TEST NO DISCREPANCIES. ACCOMPLISHED FIM 34 43 TASK 814, NO FAULTS. REPLACED WX R ANTENNA ASSY PRECAUTIONARY. 2 L 7 2 4F RT A16WE 2007112700054 20071127 00054 NM 2007 11 27 ASAA0752254 1 20071109 A 7720 TC29603 PROBE BOEING 737 737890 1384527 NM NR 2 ENGINE TEMP DIRTY A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 559AS 35178 ENGINE TREND DATA SHOWS AN INCREASE IN CRUISE DELTA EGT ALONG WITH A DECREASE IN TAKEOFF EGT HOT DAY MARGIN. NR 2 ENGIN E S/N 894227. ALL OTHER PARAMETERS ARE STABLE. INDICATION ERRORS ARE SUSPECT. ACCOMPLISHED FMC CDU FAULT TASKCARD NO FAULTS NOTED. ACCOMPLISHED EGT INDICATING CLEANING IAW MMS77 21 00. ACCOMPLISHED EEC TEST, NO FAULTS FOUND. 2 L 7 2 4F RT A16WE 2007112700055 20071127 00055 EA 2007 11 27 TRAX200701717 1 20071101 A 7830 TRACK CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 759EV 10211 AS REPORTED BY MAINTENANCE, LEFT UPPER O/B SLIDER TRACK SCREWS SHEARED AND SLIDER TRACK BROKEN. 2 L 7 2 4F RT A21EA 2007112700056 20071127 00056 EA 2007 11 27 TRAX200701718 1 20071112 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 872AS 7542 NR 1 EMERGENCY LIGHTING BATTERY PACK IS INOP. 2 L 7 2 4F RT A21EA 2007112700057 20071127 00057 EA 2007 11 27 TRAX200701719 1 20071112 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 878AS 7590 FLAPS FAIL MSG AT FL240 FOLLOWED QRH AND TALKED WITH MCC AND DISPATCH. FLAPS WHERE AT 0 DEG. EMERGENCY DECLARED. EMER GENCY EQUIPMENT ON STANDBY. SKEW DETECTION SYSTEM 2 L 7 2 4F RT A21EA 2007112700058 20071127 00058 EA 2007 11 27 TRAX200701720 1 20071112 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA LEFT ODOR A ASOA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 884AS 7513 LEFT PACK MAKING ABNORMAL NOISE AND ODOR. A/C RETURNED TO ATL AFTER T/O. FLTS 4771, 4910 CX. 2 L 7 2 4F RT A21EA 2007112700059 20071127 00059 EA 2007 11 27 TRAX200701721 1 20071112 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA LT OVERWING INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 LEFT FWD EXTERIOR EMERGENCY OVERWING EXIT LIGHT INOP. 2 L 7 2 4F RT A21EA 2007112700060 20071127 00060 EA 2007 11 27 TRAX200701722 1 20071112 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 837AS 7271 CLIMBING OUT 26,000FT GOT FLAP FAIL, FLAPS AT 0. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. FLTS 4573, 4860 C X. 2 L 7 2 4F RT A21EA 2007112700061 20071127 00061 EU 2007 11 27 TRAX200701723 1 20071112 A 2750 FLAP SYSTEM AEROSP ATR72 ATR72 EU TE FLAPS MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 630AS 336 FLAP UNLOCK ON APPROACH. EMERGENCY DECLARED. FLTS 4415, 4821 CX. 2 H 7 2 4T RT 2007112700062 20071127 00062 EA 2007 11 27 TRAX200701724 1 20071113 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA RT OVERWING INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 RIGHT SIDE EXTERNAL OVERWING AFT EMERGENCY EXIT LIGHT IS INOP. 2 L 7 2 4F RT A21EA 2007112700063 20071127 00063 EA 2007 11 27 TRAX200701725 1 20071113 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 682BR 7691 FOUND INDICATION OF CRACK DURING REAR PRESSURE BULKHEAD INSPECTION. CRACK INDICATION IS AT THE LINTEL FITTING REF: NDT M PART 6 53-61-153 PG 8 & 9. 2 L 7 2 4F RT A21EA 2007112700064 20071127 00064 EA 2007 11 27 TRAX200701730 1 20071114 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT NO TEST A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 877AS 7579 RIGHT EMERGENCY EXIT FAILED PULL TEST. 2 L 7 2 4F RT A21EA 2007112700065 20071127 00065 EA 2007 11 27 TRAX200701731 1 20071114 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 878AS 7590 FLAPS FAILED CLIMBING OUT OF CVG, FAILURE OCCURRED AT FL 26800. EMERGENCY DECLARED. EMERGENCY EQUIPMENT ON STANDBY. 2 L 7 2 4F RT A21EA 2007112700066 20071127 00066 EA 2007 11 27 TRAX200701732 1 20071114 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS STUCK A ASOA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 971EV 7528 FLAP FAIL MSG DURING CRUISE FLT AT 320 SAT 47. FLAPS STUCK AT 0 DEGREES. RAN QRH AND LANDED NO FLAP. EMERGENCY DECLAR ED. 2 L 7 2 4F RT A21EA 2007112700067 20071127 00067 NM 2007 11 27 ZZDA2007301 1 20071113 A 5310 STRUCTURE BOEING 717 717200 1383700 NM BS 219-299 L16L DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 942AT 55005 DENT AT AFT OF L1 DOOR STA 219 - 229 L16L. CUT OUT DAMAGED AREA IAW B717 SRM 53-00-01, INSPECTED CUTOUT WITH HFEC IAW N DTSPM PART 6 10-01-001. NO CRACKS NOTED, INSTALLED NEW SKIN SECTION IAW B717 SRM 53-00-01. 2 L 7 2 4F TR A6WE 2007112700068 20071127 00068 EA 2007 11 27 TRAX200701733 1 20071115 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 761ND 10213 FS 280 FLOORBEAM IS CRACKED AND CORRODED. WORK DONE IAW IS670-53-11-0026 REFER TO M-234 MAINTENANCE CONTINUATION LOG ST EPS 2-26 FOR WORK ACOMPLISHED. 2 L 7 2 4F RT A21EA 2007112700069 20071127 00069 EA 2007 11 27 TRAX200701735 1 20071115 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 761ND 10213 RIGHT LOWER FS 280 WEB IS CORRODED. REMOVED AND REPLACED RT LOWER 280 WEB IAW REO670-53-11-052 REFER TO M-234 MAINTENAN CE CONTINUATION LOG STEPS 2-7 FOR WORK ACOMPLISHED. 2 L 7 2 4F RT A21EA 2007112800005 20071128 00005 NM 2007 11 28 ASAA0792266 1 20071114 A 5320 146A81271 INTERCOSTAL BOEING 737 737990 NM BS 847-867 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 309AS 30857 AFT CARGO PIT FLOOR ZEE INTERCOSTAL AT BS 847 867 RBL 25 FOUND CORRODED FLOOR ZEE INTERCOSTAL AT BS 847 TO 867 RBL 25. REPLACED WITH NEW PART MADE REPAIR PART IAW B737 900 SRM 51-40-05 AND 51-40-02. 2 L 7 4 4F RT A16WE 2007112800013 20071128 00013 NE 2007 11 28 ASAA0752270 2 20071117 A 7261 CFM567B27 ENGINE BOEING 737 737890 1384527 NM CFMINT CFM567 CFM567B2US 13802 NE NR 2 OVERSERVICED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 02 579AS 35187 NR 1 ENGINE HIGH OIL CONSUMPTION, 8 QTS PER HOUR. ACCOMPLISHED HPC BORO STAGES 1&2 FOR OIL CONTAMINATION. NO OIL NOTED IN HPC. RAN MOTOR, NO LEAKS NOTED. FOUND ENGINE TO BE OVERSERVICED BY 0.5 QTS. DRAINED 0.5 QTS FROM ENGINE. SIGHT G LASS SHOWS FULL. 2 L 7 2 4F 4 F RT A16WE E2GL 2007112800019 20071128 00019 NM 2007 11 28 ASAA0742275 1 20070919 A 5320 6517688165 ANGLE BOEING 737 7374Q8 138447Q NM BS 312-332 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 MAIN CABIN STA 312 - 332 LBL 56 SHEAR WEB ANGLE HAS CORROSION. REMOVED CORROSION. ORIGINAL MAT'L .090 REMOVED .028. B EYOND SERVICE LIMITS. REPLACED SHEAR WEB ANGLE IAW B737 400 SRM 51-40-02 & BAC DWG 65 17688. 2 L 7 2 4F RT A16WE 2007112800025 20071128 00025 NM 2007 11 28 SWAA075745 1 20071116 A 5230 6547952 FRAME BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED BRIDGE CHECK, FOUND AFT CARGO DOOR FWD LOWER FRAME CRACKED. REMOVED AND REPLACED AFT CARGO DOOR PER MM . 2 L 7 2 4F RT A16WE 2007112800029 20071128 00029 NM 2007 11 28 SWAA075737 1 20071117 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 431WN 29845 EEPLS COVER LOOSE AT ROW 1. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2007112800033 20071128 00033 NM 2007 11 28 SWAA075739 1 20071116 A 5310 6520722 DOOR FRAME BOEING 737 7375H4 138449D NM BS 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED SPECIAL VISIT, FOUND FWD CARGO DOOR CUTOUT, FWD FRAME CRACKED AT BS 440, LOWER STOP FITTING. REMOVED A ND REPLACED FWD CARGO DOOR FWD FRAME PER SWA ACO. 2 L 7 2 4F RT A16WE 2007112800034 20071128 00034 NM 2007 11 28 SWAA075747 1 20071116 A 3040 5893543129 WINDOW BOEING 737 7373G7 1384595 NM COCKPIT ARCED A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 671SW 23785 L1 COCKPIT WINDOW ARCED IN FLIGHT. REMOVED AND REPLACED L1 COCKPIT WINDOW PER MM. 2 L 7 2 4F RT A16WE 2007112800046 20071128 00046 EU 2007 11 28 TRAX200701740 1 20071116 A 5714 STRUCTURE AEROSP ATR72 ATR72 EU WING BOX CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 WING BOX RIGHT FR 28 FACE PLATE CRACKED. 2 H 7 2 4T RT 2007112800049 20071128 00049 NM 2007 11 28 USAA920071165 1 20071117 A 5330 6545766 SKIN BOEING 737 7373B7 1384580 NM BS 520 S10R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 PIT - MAJOR REPAIR - CRACKED FUSELAGE SKIN, BS 520, S10R. REPAIRED FUSELAGE SKIN, BS 520, S10R IAW B737 SRM 53-00, FIGU RE 31. 2 L 7 2 4F RT A16WE 2007112800061 20071128 00061 NM 2007 11 28 2007UALA04697 1 20071115 A 2700 WARNING LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE STAB TRIM ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 526UA 24994 STAB TRIM LIGHT ILLUMINATED AFTER T/O,TRIM FELT LIKE REDUCED RATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007112800062 20071128 00062 NM 2007 11 28 2007UALA04698 1 20071115 A 3350 58781 LIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 906UA 25006 EEL LIGHTS AT THE AFT SECTION OF THE CABIN INOP. REPLACED LIGHT ASSEMBLY 2 L 7 2 4F 4 F RT A16WE E21EU 2007112800065 20071128 00065 NM 2007 11 28 2007UALA04701 1 20071115 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 360 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 CABIN BS 360 INTERCOSTAL AT RBL 1 FLOOR LEVEL CRACKED AT WL 208. REMOVED AND REPLACED CRACKED INTERCOSTAL WITH NEW UNIT . 2 L 7 2 4F 4 F RT A16WE E21EU 2007112800066 20071128 00066 NM 2007 11 28 2007UALA04702 1 20071115 A 5340 ATTACH ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 291 S13R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 INTERCOSTAL WEB ATTACH ANGLE CRACKED BELOW STRINGER 13R FORWARD OF DOOR 1R CUTOUT APPROX BS 291.5. REMOVED AND REPLACED CRACKED ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112800080 20071128 00080 NM 2007 11 28 2007UALA04719 1 20071116 A 5340 6545807U3 ATTACH ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 291 S12R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 FUSELAGE INTERCOSTAL WEB ATTACH ANGLE CRACKED BELOW STR 12R FWD OF DOOR 1R AT APPROX BS 291.5. MAJOR REPAIR ACCOMPLISHE D: INSTALLED NEW ATTACH ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112800081 20071128 00081 NM 2007 11 28 2007UALA04720 1 20071116 A 5347 SEAT TRACK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 847UA 1627 LEFT INBOARD SEAT TRACK Y765 FROM FR41 TO FR 47-51 HAS WEAR AT LUGS. REPLACED SEAT TRACK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112800082 20071128 00082 NM 2007 11 28 2007UALA04721 1 20071116 A 3397 FEEDER CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 330UA 24191 AFT FLOOR EMERGENCY LIGHTS ON AIRCRAFT LEFT DO NOT TEST. POWER CABLE SHORTED UNDER WET CARPET. CLEANED IMMEDIATE AREA AND DRIED THE CONNECTION . 2 L 7 2 4F 4 F RT A16WE E21EU 2007112800084 20071128 00084 EU 2007 11 28 2007UALA04724 1 20071117 A 2520 SEAT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ROW 9 ABC LOOSE A UALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 29 449UA 851 ROW 9ABC SEATS CAME OUT OF ATTACHMENT TRACK ON TAKEOFF. SEAT ROW 9ABC RE-SECURED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112800091 20071128 00091 NM 2007 11 28 2007UALA04733 1 20071116 A 2621 FIRE BOTTLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU APU BAY READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 APU FIRE BOTTLE PRESSURE LOW. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112800098 20071128 00098 NM 2007 11 28 2007UALA04741 1 20071116 A 3350 BULB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 647UA 25284 AT ROW 29AB LEFT OVERHEAD CEILING LIGHT EMERGENCY EXIT IS OUT. REPLACED LIGHT BULB. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007112800102 20071128 00102 SO 2007 11 28 C2XA07ON028 1 20071118 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL ZONE 400 ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 13202 4035 4035 1450962 CAE312917 FLT 216 - SAT TO SMF - FLIGHT CREW REPORTED BURNING ACRID ODOR ON TAKEOFF IN CABIN. NORTH AMERICA AIRCRAFT CONTRACT MAI NTENANCE WAS DISPATCHED AND PERFORMED ENGINE RUNS AND COULD NOT DUPLICATE ACRID ODOR . MX ADDED 6 PTS OF OIL TO BOTH EN GINES. OPERATIONALLY CHECKED GOOD AND AIRCRAFT WAS RELEASE TO RETURN FOR SERVICE IN AIRWORTHY CONDITIONS. 2 L 7 2 4F 4 F RT TE6CH 2007112800114 20071128 00114 EA 2007 11 28 TRAX200701750 1 20071118 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 F/A AND GROUND PERSONNEL HAD DIFFICULTY OPENING BOARDING DOOR. 2 L 7 2 4F RT A21EA 2007112800138 20071128 00138 NM 2007 11 28 SWAA075761 1 20071115 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 847 S23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 847, STR 23L. REMOVED AND REPLACED CLIP PER S RM. 2 L 7 2 4F RT A16WE 2007112800141 20071128 00141 NM 2007 11 28 SWAA075758 1 20071115 A 5330 6552880 SKIN BOEING 737 7373H4 1384600 NM BS 988 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 988, AFT UPPER CORNER L2 DOOR CUTOUT. REPAIRED SKIN PE R SRM. 2 L 7 2 4F RT A16WE 2007112800143 20071128 00143 NM 2007 11 28 SWAA075756 1 20071115 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 400 S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 400, STR 24L. REMOVED AND REPLACED CLIP PER S RM. 2 L 7 2 4F RT A16WE 2007112800145 20071128 00145 NM 2007 11 28 SWAA075772 1 20071115 A 5330 6518420 SKIN BOEING 737 7373H4 1384600 NM BS 258 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 258, WL 170.5, LEFT SIDE. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007112800147 20071128 00147 NM 2007 11 28 SWAA075770 1 20071117 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 1040 S13L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 1040, STR 13L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007112800151 20071128 00151 NM 2007 11 28 SWAA075786 1 20071119 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 727D S22-24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727D + 16 TO BS 727D + 17, BETWEEN STR 22L TO STR 24L. REPAIRED SKIN PER SWA EA & SRM. 2 L 7 2 4F RT A16WE 2007112800153 20071128 00153 NM 2007 11 28 SWAA075750 1 20071119 A 5523 65C26384 STRUCTURE BOEING 737 7373H4 1384600 NM LT ELEVATOR TAB DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED 14Y CHECK, FOUND LEFT ELEVATOR TAB DISBONDED AT OUTBOARD END. REPAIRED LEFT ELEVATOR TAB PER SRM. 2 L 7 2 4F RT A16WE 2007112800154 20071128 00154 NM 2007 11 28 SWAA075749 1 20071119 A 5523 65C26384 STRUCTURE BOEING 737 7373H4 1384600 NM RT ELEVATOR TAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED 14Y CHECK, FOUND RIGHT ELEVATOR TAB CRACKED AT NR 2 HINGE. REPAIRED RIGHT ELEVATOR TAB PER SRM. 2 L 7 2 4F RT A16WE 2007112800156 20071128 00156 2007 11 28 SWAA075751 4 20071119 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007112800158 20071128 00158 NM 2007 11 28 SWAA075774 1 20071115 A 3397 WIRE BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 460WN 32464 EEPLS WIRE FOUND LOOSE BETWEEN ROW 5 TO ROW 7. RECONNECTED LOOSE WIRE PER MM. 2 L 7 2 4F RT A16WE 2007112800159 20071128 00159 2007 11 28 SWAA075753 4 20071119 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007112800167 20071128 00167 2007 11 28 SWAA075782 4 20071114 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED L2 DOOR EMERGENCY EV AC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007112800168 20071128 00168 NM 2007 11 28 SWAA075781 1 20071114 A 3350 65C27028 LIGHT BOEING 737 7373G7 1384595 NM MID CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED HC1 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LEFT OVERWING EM ERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2007112800169 20071128 00169 NM 2007 11 28 SWAA075780 1 20071114 A 3350 6042221 LENS BOEING 737 7373G7 1384595 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR LOWER EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED R2 DOOR LOWER E MERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2007112800170 20071128 00170 NM 2007 11 28 SWAA075779 1 20071114 A 3350 6042221 LIGHT BOEING 737 7373G7 1384595 NM R2 DOOR INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED R2 DOOR LOWER EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2007112800171 20071128 00171 2007 11 28 SWAA075778 4 20071114 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REPOSITIONED R1 DOOR EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007112800172 20071128 00172 NM 2007 11 28 SWAA075755 1 20071114 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS NO TEST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 720WN 27854 DURING SCHEDULED HC2 CHECK, FOUND CABIN EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PAC KS PER MM. 2 L 7 2 4F RT A16WE 2007112800174 20071128 00174 NM 2007 11 28 MWEA070298 1 20071120 A 5330 5910157107 SKIN BOEING 717 717200 1383700 NM FUSELAGE PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 918ME 55180 PUNCTURED ON SKIN AT AFT SIDE NEAR STOP NR 3. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2007112800176 20071128 00176 NM 2007 11 28 ASAA0752276 1 20071118 A 2160 3989083 VALVE BOEING 737 737890 1384527 NM CABIN PRESSURE FAULTY A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 557AS 35176 AFTER ENGINE START ON RECALL THE CONTROL CABIN ZONE TEMP LIGHT ILLUMINATED. REPLACED ZONE TRIM AIR MODULATING VALVE. O PS BITE CHECKED GOOD. 2 L 7 2 4F RT A16WE 2007112800177 20071128 00177 NM 2007 11 28 ASAA0752277 1 20071119 A 2160 412A160041 FILTER BOEING 737 737890 1384527 NM CABIN AIR DIRTY A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 577AS 35186 AFT TEMP CONTROLLER EXTREMELY SENSITIVE TO SMALL ADJUSTMENTS. BITE TEST BOTH ZONE TEMP CONTROLLERS. ALL GOOD NO FAULTS NOTED. FOUND AIR FILTERS DIRTY AT FLIGHT COMPT FWD & AFT COMPARTMENTS. CLEANED AIR FILTERS. OP CHECKS GOOD. 2 L 7 2 4F RT A16WE 2007112800179 20071128 00179 SO 2007 11 28 C2XA07SH093 1 20071122 A 5751 14569009410SD ATTACH FITTING EMB 145 EMB145LR 3260212 SO RT AILERON DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 131 SHV - DURING C-CHECK RIGHT AILERON PCA BRACKET HAT BUSHING HOLES ELONGATED. MX REMOVED AND REPLACED RIGHT AILERON PCA B RACKET IAW EC5750-01177. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007112800180 20071128 00180 SO 2007 11 28 C2XA07SH094 1 20071122 A 5751 14569009409SD ATTACH FITTING EMB 145 EMB145LR 3260212 SO LT AILERON DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 131 SHV - DURING C-CHECK LEFT AILERON PCA BRACKET HAT BUSHING HOLES ELONGATED. MAINTENANCE REMOVED AND REPLACED LEFT AILERO N PCA BRACKET IAW EC5750-01177. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007112800183 20071128 00183 EU 2007 11 28 YENA2007100 1 20071116 A 3320 LIGHT AIRBUS 320 A320232 3930326 EU SEAT 12E INOPERATIVE A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 656JB 3091 FLT 309, IAD-SAN, APPROX BETWEEN 13:30Z-15:09Z SEAT 12E READING LIGHT OUT. PAX OBSERVED SMOKE AS LIGHT WENT OUT. REMOV ED OVERHEAD PANEL 12 DEF, INSP WIRING AND CIRCUIT BOARD, FOUND NO EVIDENCE OF ELECT BURNING, RESECURED PANEL. RE-SET CI DS, PERFORMED OPERATIONAL TEST OF THE PASSENGER READING LIGHT SYSTEM PER AMM 33-25-00-710-001. OPS CHECK OK. 2 L 7 2 4F RT A28NM 2007112800184 20071128 00184 EU 2007 11 28 USAA920071187 1 20071122 A 3350 321431 BATTERY AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHTS FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 622AW 54 ATL - EEL - MX REPORTED EMERGENCY LIGHT AT ROW 9 AND 11 LT AND RT INOP. MX REPLACED THE RIGHT BATTERY. OPERATIONAL CHE CK WAS GOOD. 2 L 7 2 4F RT A28NM 2007112800185 20071128 00185 NM 2007 11 28 HNAA0700271 1 20071115 A 7931 OIL SYSTEM DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE NR 1 ENGINE LOW PRESSURE A HNAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 07 914HA 30342 2369 53 120219 ON CLIMBOUT NR 1 ENG OIL PRESSURE GAUGE FLUX, FOLLOWED BY NR 1 ENGINE OIL WARNING LIGHT. CREW REDUCED POWER AND LEVELED OFF, OIL PRESSURE STABILIZED AND NR 1 ENG OIL WARNING LIGHT EXTINGUISHED. NR 1 OIL PRESSURE FLUX BETWEEN 60 AND 30 PSI FOR APPROX 5 MIN. 2 H 7 2 4T 4 T RT A13NM E20NE 2007112800186 20071128 00186 NM 2007 11 28 USAA920071178 1 20071120 A 5720 69520145 STIFFENER BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 175AW 23634 CLT - MAJOR REPAIR - CRACKED CENTER WING REAR SPAR VERTICAL STIFFENER, BS 663.75, RBL 6.15. REPAIRED CENTER WING REAR S PAR VERTICAL STIFFENER, BS 663.75, RBL 6.15 IAW USAIRWAYS TYPICAL REPAIR 57-10-03B AND EA 110301. 2 L 7 2 4F RT A16WE 2007112800190 20071128 00190 NM 2007 11 28 USAA920071188 1 20071119 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 502UW 23232 CLT - MAJOR REPAIR - CRACKED FUSELAGE SKIN, BS 727E, S20L. REPAIRED FUSELAGE SKIN, BS 727E, S20L IAW B737 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2007112800191 20071128 00191 NM 2007 11 28 USAA920071189 1 20071108 A 5311 FRAME BOEING 737 737301 1384611 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 591US 23936 CLT - MAJOR REPAIR - C6 CHECK, FORWARD CARGO DOOR CUTOUT AFT FRAME CRACKED, BS 492.4, S24R. REPAIRED FORWARD CARGO DOOR CUTOUT AFT FRAME, BS 492.4, S24R IAW USAIRWAYS EA 100014. 2 L 7 2 4F RT A16WE 2007112800192 20071128 00192 NM 2007 11 28 USAA920071190 1 20071110 A 5330 6545769 SKIN BOEING 737 737301 1384611 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 591US 23936 CLT - MAJOR REPAIR - C6 CHECK, CRACKED FUSELAGE SKIN, BS 460, S26R. REPAIRED FUSELAGE SKIN, BS 460, S26R IAW USAIRWAYS EA 100015. 2 L 7 2 4F RT A16WE 2007112800195 20071128 00195 EU 2007 11 28 USAA920071193 1 20071112 A 5320 D53472189202 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 625AW 64 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON FLOORBEAM, BS 3257 / FR 68, -Y1165. REPLACED FLOORBEAM, BS 3257 / FR 68 - BS 3310 / FR 69, -Y1165 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007112800196 20071128 00196 EU 2007 11 28 USAA920071194 1 20071119 A 5347 D53112092202 SEAT TRACK AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 625AW 64 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON SEAT TRACK, BS 808 / FR 20 - BS 843 / FR 21, +Y1292. REPLACED SEAT TRACK, BS 808 / FR 20 - BS 843 / FR 21, +Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007112800198 20071128 00198 NM 2007 11 28 USAA920071196 1 20071116 A 5340 6935352U14 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CRACKED STRINGER TIE CLIP, BS 578, S4R. REPLACED STRINGER TIE CLIP, BS 578, S4R IAW B73 7 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007112800200 20071128 00200 NM 2007 11 28 USAA920071198 1 20071116 A 5340 6935352U14 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CRACKED STRINGER TIE CLIP, BS 616, S4L. REPLACED STRINGER TIE CLIP, BS 616, S4L IAW B73 7 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007112800201 20071128 00201 NM 2007 11 28 USAA920071199 1 20071116 A 5340 6953207U501 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CRACKED STRINGER TIE CLIP, BS 663, S4L. REPLACED STRINGER TIE CLIP, BS 663, S4L IAW B73 7 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007112800204 20071128 00204 NM 2007 11 28 USAA920071202 1 20071017 A 3350 SIGN BOEING 737 7373G7 1384595 NM EMERGENCY LIGHTS WEAK A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 307AW 24634 CLT - EEL - C16 CHECK, EMERGENCY EXIT SIGNS ON FIRST CLASS CURTAIN HEADER FAILED BETA LIGHT COMPARATOR TEST. REPLACED E MERGENCY EXIT SIGNS ON FIRST CLASS CURTAIN HEADER IAW B737 AMM 33-51-14-2. 2 L 7 2 4F RT A16WE 2007112900004 20071129 00004 EU 2007 11 29 XV6A200700003 1 20071116 A 2612 D3894120 FIRE LOOP DORNER DO228 DO228202 2992030 EU GARRTT TPE331 TPE33110 01514 WP HARTZL HCB4T HCB4TN5 GL LT NACELLE WORN E XV6A A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 19 404VA 8120 LEFT FIRE HANDLE LIGHT AND MASTER WARNING WENT OFF IN FLIGHT FOR ONE SECOND (TWICE). REMOVED AND REPLACED FIRE WARNING LOOP DETECTOR IAW 26-10-05. LEFT ENGINE FIRE LOOP TEST OPS CHECK GOOD. AIRCRAFT APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T 4 T RT A16EU E4WE 6 C P40EA 2007112900005 20071129 00005 EA 2007 11 29 COMA0780001 1 20071111 A 3230 895304 PSEU CNDAIR CL600 CL6002D24 1390016 EA AVIONICS BAY FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 691CA 99 15136 FLIGHT 5543 - ON CLIMBOUT FROM LGA TO CVG, RECEIVED GEAR DISAGREE MESSAGE DURING GEAR RETRACTION. AIRCRAFT DIVERTED TO JFK AND LANDED SAFELY. REMOVED AND REPLACED PSEU. 2 L 7 2 4F RT A21EA 2007112900006 20071129 00006 EA 2007 11 29 COMA0760640 1 20071113 A 2131 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA CABIN PRESSURE FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 956CA 7105 FLIGHT 5219 - AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF FROM BOS. AIRCRAFT RETURNED TO BOS AND LANDED SAFELY. FOUND C ABIN PRESSURE CONTROLLER FAULTY. DEFERRED PER MEL 21-31-01-1. 2 L 7 2 4F RT A21EA 2007112900008 20071129 00008 EA 2007 11 29 COMA0760642 1 20071114 A 2750 860D10018ABCD COMPUTER CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 443CA 8874 7539 FLIGHT 5086 - FLAPS FAIL ON TAXI OUT. AIRCRAFT RETURNED TO GATE. REMOVED AND REPLACED FECU. 2 L 7 2 4F RT A21EA 2007112900009 20071129 00009 EA 2007 11 29 COMA0760643 1 20071114 A 2752 852D10021 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA LT TE FLAP FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 443CA 3497 7539 FLIGHT 5089 - FLAPS FAILED AT 8 DEGREES ON APPROACH INTO MSP. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED LEFT I/B FL AP I/B ACTUATOR. 2 L 7 2 4F RT A21EA 2007112900014 20071129 00014 EA 2007 11 29 COMA0760648 1 20071115 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 629BR 7251 FLIGHT 5592 - AFTER T/O FLAPS FAIL MESSAGE. FOLLOWED QRH AND RETURNED TO BNA AND LANDED SAFELY. FOUND SKEW DETECTION S YSTEM TO BE CAUSE OF FLAP FAIL. DEFERRED THE SKEW DETECTION SYSTEM PER MEL 27-51-03-1. FLAP SYSTEM OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007112900016 20071129 00016 EA 2007 11 29 COMA0760650 1 20071115 A 2760 SPOILER SYS CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 798CA 7348 FLIGHT 5303 - ON T/O ROLL RECEIVED SPOILERON AND CONFIG MESSAGES. ABORTED T/O. PERFORMED SPOILER SYSTEM RESET, OPS CHE CK GOOD. 2 L 7 2 4F RT A21EA 2007112900017 20071129 00017 EA 2007 11 29 COMA0760651 1 20071116 A 5210 601R386493 CONTROL ROD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR VENT FAULTY A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 716CA 7250 FLIGHT 5109 - AFTER TAKEOFF FROM CLE AIRCRAFT WOULD NOT PRESSURIZE, FLIGHT RETURNED TO CLE. REPLACED THE CABIN DOOR VEN T VALVE CONTROL ROD. 2 L 7 2 4F RT A21EA 2007112900018 20071129 00018 EA 2007 11 29 COMA0760652 1 20071117 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 924CA 7026 FLIGHT 4950 - EN ROUTE ATL-YYZ RECEIVED A FLAP FAIL MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EV ENT- MAINTENANCE ACTION PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007112900019 20071129 00019 EA 2007 11 29 COMA0760653 1 20071117 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 446CA 7546 FLIGHT 5028 - PRIOR TO TAXI-OUT RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION ME SSAGES. 2 L 7 2 4F RT A21EA 2007112900020 20071129 00020 EA 2007 11 29 COMA0760654 1 20071119 A 3241 140153 TRANSDUCER CNDAIR CL600 CL6002B19 1900309 EA WHEEL SPEED FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 436CA 17844 7482 FLIGHT 5066 - RECEIVED ANTI-SKID CAUTION MESSAGE. ABORTED TAKEOFF, RETURNED TO GATE. PERFORMED RTO INSPECTION AND REPL ACED LEFT I/B WHEEL SPEED TRANSDUCER. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007112900021 20071129 00021 EA 2007 11 29 COMA0760655 1 20071119 A 3241 140153 TRANSDUCER CNDAIR CL600 CL6002B19 1900309 EA WHEEL SPEED FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 436CA 17844 7482 FLIGHT 5066 - RECEIVED ANTI-SKID CAUTION MESSAGE. ABORTED TAKEOFF, RETURNED TO GATE. PERFORMED RTO INSPECTION AND REPL ACED RIGHT I/B WHEEL SPEED TRANSDUCER. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007112900022 20071129 00022 EA 2007 11 29 COMA0760656 1 20071120 A 3010 ANTI-ICE SYSTEM CNDAIR CL600 CL6002B19 1900309 EA WINGS MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 960CA 7117 FLIGHT 5181 - DURING TAKEOFF ROLL RECEIVED A WING OVERHEAT WARNING MESSAGE, ABORTED T/O AND RETURNED TO THE GATE. DEFER RED WING ANTI-ICE SYSTEM PER MEL 30-12-03. 2 L 7 2 4F RT A21EA 2007112900023 20071129 00023 EA 2007 11 29 COMA0760657 1 20071120 A 3230 46193 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG FAULTY A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 594SW 4543 7285 FLIGHT 5467 - DURING CLIMBOUT UPON GEAR RETRACTION TEMPORARILY RECEIVED A LANDING GEAR DISAGREE MESSAGE. REPLACED THE M LG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2007112900025 20071129 00025 EA 2007 11 29 COMA0760660 1 20071120 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 446CA 7546 FLIGHT 4953 - EN ROUTE DTW-CVG RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOU T INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007112900026 20071129 00026 NM 2007 11 29 KCSA071528 1 20071123 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM BS 570-590 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 FORWARD BILGE SEAT TRACK IS DAMAGED AT STA 570 TO 590, LBL 45. 2 L 7 4 4F RT A20WE 2007112900027 20071129 00027 NM 2007 11 29 2007UALA02270 1 20070627 A 2612 FIRE WARNING AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE APU BAY FALSE ACTIVATION A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 842UA 1569 APU FIRE DISCHARGE LIGHT ILLUMINATED. REPLACED APU FIRE BOTTLE AND CLEANED APU COMPARTMENT. NO FURTHER REPEATS SINCE T HE ORIGINAL. UNKNOWN AS WHAT CAUSED THE BOTTLE TO FIRE IN THE FIRST PLACE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112900030 20071129 00030 NM 2007 11 29 2007UALA04747 1 20071119 A 5241 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 FWD GALLEY DOOR AFT FRAME WEB HAS 4 EA CRACKS AT OUTBOARD FASTENER HOLES FOR LOWER STOP FITTING. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112900031 20071129 00031 NM 2007 11 29 2007UALA04748 1 20071119 A 5241 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 FWD GALLEY DOOR, NR 4 STOP FITTING FROM TOP CRACKED IN CUTOUT, CRACK PREVIOUSLY STOP DRILLED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112900034 20071129 00034 NM 2007 11 29 2007UALA04753 1 20071119 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1460 S25-26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 AFT PIT STA 1460 BETWEEN STR 25L AND 26L FRAME DENTED. REMOVED DAMAGED AREA, FABRICATED REPAIR, AND INSTALLED A NEW DOU BLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007112900036 20071129 00036 EU 2007 11 29 2007UALA04755 1 20071119 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 427UA 512 EMERGENCY LIGHTS FAIL 3SVC TEST, INT LOADS EMER L. FOUND INTERNAL ELECTRICAL FAULT/FAILURE OF LT OVERWING SLIDE ASSY. REPLACED LT OVERWING SLIDE ASSY- OPS CHECKED GOOD. NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112900038 20071129 00038 NM 2007 11 29 2007UALA04757 1 20071119 A 3350 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LT WING INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 325UA 23957 LEFT EXTERIOR EMERGENCY LIGHT AFT OF THE WING INOP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112900040 20071129 00040 NM 2007 11 29 2007UALA04759 1 20071119 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 534UA 25129 EXTERIOR EMERGENCY LIGHT AT R4 DOOR INOP. REPLACED LAMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007112900042 20071129 00042 NM 2007 11 29 2007UALA04761 1 20071120 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 NEAR DOOR 3R CEILING EMERGENCY LIGHT IS INOP. REPLACED LAMP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112900043 20071129 00043 NM 2007 11 29 2007UALA04762 1 20071120 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 SEAT 1A FWD EMERGENCY LIGHT & SEAT 3J AFT ARE INOP. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112900044 20071129 00044 2007 11 29 2007UALA04763 4 20071119 A 2565 O-RING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SLIDE BOTTLE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 196UA 28715 LEFT UPPER DECK SLIDE AFT BOTTLE PRESSURE READING 1500 PSI NOT WITHIN GREEN BAND. THE O-RING THAT SEALS THE SPOOL WAS LEAKING. REPLACED O-RING. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112600195 20071126 00195 EA 2007 11 26 QXEA200701715 1 20071109 A 3610 GG67080027 SHUTOFF VALVE CNDAIR CL600 CL6002C10 1390015 EA LT ENG BLEED SYS FAILED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 611QX 6321 47 10041 PDX - RECEIVED A LEFT ENGINE BLEED CAUTION. RETURNED TO THE GATE. MAINTENANCE REPLACED THE LEFT PRSOV. MDC SHOWED A FA IL WORD 352 BIT A & B. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007112600200 20071126 00200 EA 2007 11 26 QXEA200701713 1 20071111 A 2612 FIRE LOOP CNDAIR CL600 CL6002C10 1390015 EA MALFUNCTIONED A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 612QX 10042 PDX - FLIGHT 2555 - AFTER ENGINE START RECEIVED A INTERM FIRE SYSTEM FAULT MESSAGE. RETURNED TO THE GATE, MAINTENANCE P LACED THE SYSTEM ON MEL 26-00-1. AIRCRAFT RETURNED TO SERVICE. TROUBLESHOOTING SHOWED A SHORT IN LOOP "A" ON THE LEFT SIDE MEL CONTINUED. REPLACED LOOP ELEMENT "A". OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007112700012 20071127 00012 NM 2007 11 27 SWAA075709 1 20071114 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED MV2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007112700014 20071127 00014 NM 2007 11 27 SWAA075710 1 20071114 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM BS 444-454 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BETWEEN BS 444 AND BS 454, RBL 4 AND LBL 3. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007112700020 20071127 00020 NM 2007 11 27 ZZDA2007300 1 20071114 A 2120 UNKNOWN BOEING 717 717200 1383700 NM AFT CABIN ODOR A ZZDA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 37 979AT 55038 ODOR OF SMOKE FROM AFT OF AC BY F/A JUMPSEAT. INSPECTED AFT F/A HANDSET AND CRADLE FOR DEFECTS AS WELL AS THE TAIL CONE AREA AS WELL AS BOTH LAVS FOR OBVIOUS DEFECTS NONE NOTED, RAN A/C AT 1.3 EPR IN NORMAL CONFIG FOR 10-15 MIN. NO DEFECTS CND ON GROUND. 2 L 7 2 4F TR A6WE 2007112700021 20071127 00021 EA 2007 11 27 COMA0760638 1 20071110 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 991CA 7216 FLIGHT 5218 - FLAPS FAILED AT 0 DEGREES ON APPROACH INTO BDL. AIRCRAFT LANDED SAFELY. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTH ER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007112700025 20071127 00025 NM 2007 11 27 KCSA071525 1 20071115 A 5330 SKIN BOEING 747 747246F 1384850 NM BS 748 S41-42R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 STA 748 AT S41R TO S42R SKIN DAMAGED. 2 L 7 4 4F RT A20WE 2007112700038 20071127 00038 NM 2007 11 27 CALA0700691 1 20071115 A 5320 654578140 BRACKET BOEING 737 7373T0 1384582 NM BS 986.5-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND INTERGRANULAR CORROSION ON AFT LAV SERVICE SUPPORT HAT BRACKET AT STA 986.5-1016, S24R TO 25R. THE BRA CKET ASSEMBLY WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND BAC DRAWING 69-36677. 2 L 7 2 4F RT A16WE 2007112800001 20071128 00001 NM 2007 11 28 ASAA0792262 1 20071114 A 5320 143A7501162 ANGLE BOEING 737 737990 NM CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 309AS 30857 FWD CARGO PIT RIGHT ZEE FOUND CORRODED AT BS 500F+12 TO BS 500L. RIGHT ZEE IN FWD CARGO PIT AT BS 500F+12 TO BS 500L RB L 21 REPLACED WITH NEW PART IAW B737 900 SRM 53-00-53. 2 L 7 4 4F RT A16WE 2007112800011 20071128 00011 WP 2007 11 28 ASAA0782258 1 20071118 A 5753 5930494509 SKIN DOUG DC9 DC983 3022083 WP TE FLAP VANE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 977AS 53453 RIGHT FLAP I/B SIDE I/B FLAP VANE MULTIPLE DENTS ON LWR. REMOVED DAMAGED AREA, FABRICATED FILLER AND REPAIR DOUBLER, PR EPARED AREA BOND AREA AND FASTENER IAW MD80 SRM 51-70-2 PG 11, 23, 43, 45, 59 AND 63. 2 L 7 2 4F RT A6WE 2007112800017 20071128 00017 SO 2007 11 28 RAIA00711013 1 20071118 A 3397 WIRE EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 813HK 145044 PRE FLT NR 5507 - STL - EXIT ROW LIGHTS INOP. MAINTENANCE RE-SECURED WIRING TO LOWER EMERGENCY LIGHT, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007112800030 20071128 00030 NM 2007 11 28 SWAA075738 1 20071116 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 480WN 33998 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 1 TO ROW 12. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2007112800031 20071128 00031 NM 2007 11 28 SWAA075740 1 20071116 A 5310 6520723 DOOR FRAME BOEING 737 7375H4 138449D NM BS 492 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED SPECIAL VISIT, FOUND FWD CARGO DOOR CUTOUT, AFT FRAME CRACKED AT BS 492, LOWER STOP FITTING. REMOVED A ND REPLACED FWD CARGO DOOR AFT FRAME PER SWA ACO. 2 L 7 2 4F RT A16WE 2007112800040 20071128 00040 EA 2007 11 28 TRAX200701726 1 20071113 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA ACCESS PANEL CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 883AS 7504 FUEL ACCESS CUTOUT 550BB HAS CORROSION ON I/N SIDE. CORROSION AT CUTOUT 65000 REMOVED PER REO 601R-57-21-030-07 ELITE S TRUCTURAL SERVICES WO 50237 5000-0064. SUPPLEMENTAL - SDR CLOSED 11/20/07. 2 L 7 2 4F RT A21EA 2007112800045 20071128 00045 EU 2007 11 28 TRAX200701739 1 20071116 A 5313 STRINGER AEROSP ATR72 ATR72 EU 16R CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 STR 16R CORRODED BETWEEN FR 35-37. 2 H 7 2 4T RT 2007112800047 20071128 00047 EA 2007 11 28 TRAX200701741 1 20071116 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 902EV 7620 PASSENGER DOOR EXIT PLACARD IS WORN. 2 L 7 2 4F RT A21EA 2007112800048 20071128 00048 EA 2007 11 28 TRAX200701742 1 20071116 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS LOOSE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 846AS 7328 EXIT SIGN ABOVE SERVICE DOOR IS LOOSE AND ABOUT TO COME OFF. 2 L 7 2 4F RT A21EA 2007112800050 20071128 00050 NM 2007 11 28 USAA920071167 1 20071116 A 5753 SKIN BOEING 737 7373G7 1384595 NM ZONE 500 DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 01014 24711 PHX - MAJOR REPAIR - LEFT WING OUTBOARD TRAILING EDGE FOREFLAP DELAMINATED, WS 202.69 - WS 413.61. REPLACED LEFT WING O UTBOARD TRAILING EDGE FOREFLAP, WS 202.69 - WS 413.61 IAW USAIRWAYS TASK CARD R3M27022. 2 L 7 2 4F RT A16WE 2007112800052 20071128 00052 EU 2007 11 28 USAA920071169 1 20071015 A 5320 D53472188204 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3257 / FR 68 - BS 3310 / FR 69, +Y1162. REPAIRED CABI N FLOORBEAM, BS 3257 / FR 68 - BS 3310 / FR 69, +Y1162 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007112800053 20071128 00053 EU 2007 11 28 USAA920071170 1 20071019 A 5347 D53112815202 SEAT TRACK AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 668AW 1764 SAL - MAJOR REPAIR - BC4 CHECK - CORROSION ON CABIN SEAT TRACK, BS 605 / FR 12 - BS 950 / FR 24, +Y1292. REPAIRED CABIN SEAT TRACK, BS 605 / FR 12 - BS 950 / FR 24, +Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007112800054 20071128 00054 NM 2007 11 28 USAA920071171 1 20071116 A 5330 6545774 SKIN BOEING 737 737401 1384701 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 CLT - MAJOR REPAIR - 4214397, CRACKED FUSELAGE SKIN, BS 727E, S24L. REPAIRED FUSELAGE SKIN, BS 727E, S24L IAW B737 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2007112800063 20071128 00063 NM 2007 11 28 2007UALA04699 1 20071115 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 500B-500C CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 LEFT CABIN CREASE BEAM WEB ADJACENT TO STRINGER 17L IS CORRODED ON UPPER SURFACE BETWEEN BS 500B & S 500C WL 208. BLE NDED OUT CORROSION. FABRICATED AND INSTALLED A TYPICAL WEB REPAIR ON UPPER SURFACE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112800071 20071128 00071 NM 2007 11 28 2007UALA04708 1 20071115 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR E LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 527UA 24995 THE 1L & 4L EXTERIOR EMERGENCY LIGHTS ARE OUT. RELAMPED LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007112800083 20071128 00083 NM 2007 11 28 2007UALA04723 1 20071119 A 3320 WIRE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LIGHT BALLAST BURNED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 217UA 30550 CREW REPORTED AN ELECTRICAL ODOR FROM REAR GALLEY AREA. RECIRC FANS AND GALLEY POWER TURNED OFF AND ODOR DISSIPATED. G ALLEY AREA CHECKED AND NO OBVIOUS FAULTS FOUND. CHECKED FOR ODOR IN GALLEY CEILING AREA, UNDER FLOOR AND CHECKED WIRIN G IN AREA AND NO FAULTS FOUND. CHECK GALLEY COMPONENTS AND ALL WERE OK. FOUND CEILING LIGHT BALLAST HAD BURNED WIRE TO P IN AT CONNECTOR. REPLACED BALLAST AND LAMPS ON BOTH FWD OVERHEAD LIGHT ASSYS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007112800089 20071128 00089 NM 2007 11 28 2007UALA04729 1 20071118 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1520 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 AFT PIT FRAME STA 1520 STR 26L DENTED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED & INSTALLED REPAIR ANGLE . 2 L 7 2 4F 4 F RT A2NM E17NE 2007112800103 20071128 00103 GL 2007 11 28 C2XA07ON029 2 20071119 A 7261 CARBON SEAL EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL NR 4 ENGINE LEAKING A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 14171 8842 8842 1450859 CAE312681 FLT 7827 - LAX TO SFO - FLIGHT CREW REPORTED SMOKE IN CABIN. AIRCRAFT WAS FERRY FLIGHT TO ONT MX HANGER WHERE MX PERSON NEL REMOVED AND REPLACED NR 1 ENG, OPERATIONALLY CHECKED GOOD AND AIRCRAFT WAS RETURNED FOR SERVICE IN AIRWORTHY CONDITI ONS. NR 4 ENGINE CARBON SEAL EXHIBITED SIGNS OF HEAVY LEAKAGE(SEGMENTS FULLY WETTED WITH OIL AND COCKING ON THE EXTERIOR OF HOUSING). NR 4 CARBON SEAL WAS REPLACED WITH POST SB72-348 STANDARD. 2 L 7 2 4F 4 F RT TE6CH 2007112800105 20071128 00105 NM 2007 11 28 SB07101 1 20071121 A 3350 20131ASMI BATTERY PACK BOEING 737 737401 1384701 NM EMERGENCY LIGHTS DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 PVD - MAINTENANCE REPORTED THE RIGHT REAR CABIN SERVICE DOOR EMERGENCY EXIT LIGHT BATTERY WAS DEAD. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007112800108 20071128 00108 EA 2007 11 28 TRAX200701744 1 20071117 A 5240 LATCH CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 903EV 7621 EXTERNAL SERVICES DOOR HAS (1) BROKEN LATCH. 2 L 7 2 4F RT A21EA 2007112800118 20071128 00118 EA 2007 11 28 TRAX200701754 1 20071119 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA RT OVERWING INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 933EV 8022 RIGHT WING FWD OVERWING FORWARD EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007112800124 20071128 00124 NM 2007 11 28 USAA920071181 1 20071107 A 5315 141N5160102 FLOORBEAM BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 200UU 27809 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON FLOORBEAM, BS 327, RBL 24.75 - RBL 37.50, WL 208. REPLACED FLOORBE AM, BS 327, RBL 24.75 - RBL 37.50, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007112800139 20071128 00139 NM 2007 11 28 SWAA075760 1 20071115 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727E S25L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727E, STR 25L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007112800142 20071128 00142 NM 2007 11 28 SWAA075757 1 20071115 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 420 S23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 420, STR 23L. REMOVED AND REPLACED CLIP PER S RM. 2 L 7 2 4F RT A16WE 2007112800149 20071128 00149 NM 2007 11 28 SWAA075788 1 20071119 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 727E S23-24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727E + 2.5 TO BS 727E + 17, BETWEEN STR 23L TO ST R 24L. REPAIRED SKIN PER SWA EA & SRM. 2 L 7 2 4F RT A16WE 2007112800155 20071128 00155 NM 2007 11 28 SWAA075773 1 20071114 A 5753 SKIN BOEING 737 7373H4 1384600 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED 14Y CHECK, FOUND LEFT WING OUTBOARD AFT FLAP OUTBOARD T/E DELAMINATED. REMOVED AND REPLACED LEFT WING AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2007112800160 20071128 00160 NM 2007 11 28 SWAA075754 1 20071119 A 5311 6546558 FRAME BOEING 737 7375H4 138449D NM BS 907 S8-9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SWA EA . 2 L 7 2 4F RT A16WE 2007112800161 20071128 00161 2007 11 28 SWAA075783 4 20071119 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF LIMITS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 L2 DOOR EMERGENCY EVAC SLIDE OUT OF LIMITS. REMOVED AND REPLACED L2 DOOR EMERGENCY EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007112800162 20071128 00162 NM 2007 11 28 SWAA075789 1 20071119 A 5330 6545765 SKIN BOEING 737 737301 1384611 NM BS 500D S12L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 17, STR 12L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007112800163 20071128 00163 NM 2007 11 28 SWAA075790 1 20071119 A 5330 6545775 SKIN BOEING 737 737301 1384611 NM BS 867 S24R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 867 + 17, STR 24R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007112800165 20071128 00165 NM 2007 11 28 SWAA075776 1 20071113 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM BS 420 S26R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CORRODED AT BS 420, STR 26R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007112800166 20071128 00166 2007 11 28 SWAA075777 4 20071118 A 2565 6557463 BRACKET BOEING 737 7373Y0 1384671 NM R1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR BRACKET LOOSE. REMOVED AND REPLACED GIRT BAR BRACKET PER MM. 2 L 7 2 4F RT A16WE 2007112800173 20071128 00173 NM 2007 11 28 SWAA075791 1 20071117 A 2170 21BC126 COALESCER BAG BOEING 737 7377H4 1384404 NM A/C PACK ODOR A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 29 782SA 29808 AIR TURNBACK. SMOKE ODOR ALONG WITH BURNING ODOR IN COCKPIT DURING TAKEOFF AND CLIMB. RETURNED TO BASE. REMOVED AND R EPLACED A/C COALESCER BAGS PER MM. 2 L 7 2 4F RT A16WE 2007112800178 20071128 00178 SO 2007 11 28 C2XA07IA234 1 20071120 A 3200 LANDING GEAR EMB 135 EMB135LR 3260305 SO MALFUNCTIONED A C2XA O OTHER E VIBRATION/BUFFET LD LANDING 1 SW 27 27523 145389 IAH - FLIGHT 2843, THE CREW REPORTED THAT WHEN THE GEAR COMES DOWN THE AIRCRAFT OSCILLATES AGRESSIVELY TO THE RIGHT AND LEFT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE LANDING GEAR AND DOORS, AND OPERATION ALLY CHECKED THE AUTOPILOT SYSTEM ALL WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007112800182 20071128 00182 EU 2007 11 28 YENA2007101 1 20071116 A 2120 UNKNOWN EMB ERJ190 ERJ190100IGW 3260408 EU CABIN ODOR A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 178JB 19000004 FLT 1016, JFK-, EXPERIENCED DUSTY/HAZY/BURNING ODOR IN CABIN ON TAKEOFF ROLL. ENTIRE CABIN HAZY, WARM RUSH OF AIR ON FL T DECK, LIGHTS ON FLT ATTENDANT WERE INOP. PERFORMED VISUAL INSPECTION OF NR 1 & 2 ENGINE BLEED AIR LINES. FOUND 1 BLA NKING CAP MISSING FROM NR 1 ENGINE NAPRSOV. INSTALLED NEW BLANKING CAP PER AMM 36-11-031, NO OTHER DEFECTS FOUND ON NR 1 AND 2 ENGINE BLEED AIR LINES. PERFORMED VISUAL INSPECTION OF SPDA 1 PER AMM 24-61-01. NO DEFECTS NOTED, REMOVED ACCE SS PANELS 191 EL AND 191 AR AND PERFORMED GENERAL VISUAL INSPECTION OF LT AND RT COOLING PACKS PER AMM 21-51-00. LEAK C HECK OF LT AND RT COOLING PACKS PER AMM 21-51-00, NO DEFECTS NOTED. REINSTALLED ACCESS PANELS 191 EL AND 191 AR PER AMM 2 L 7 2 4F RT A57NM 2007112800194 20071128 00194 NM 2007 11 28 USAA920071192 1 20071115 A 5340 141N5160252 ATTACH ANGLE BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 200UU 27809 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL OUTBOARD ATTACH ANGLE, BS 324 BL 0, WL 208. REPLACED I NTERCOSTAL OUTBOARD ATTACH ANGLE, BS 324 BL 0, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007112800205 20071128 00205 NE 2007 11 28 2007UALA02230 2 20070625 A 7200 5R185TYP ACOUSTIC PANEL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE DEBONDED A UALA C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 WP 29 456UA 39347 7379 1128 V10059 FLIGHT RETURNED TO FIELD DUE TO LEFT ENGINE FAILURE ON TAKEOFF. LT ENGINE WAS REMOVED FROM AIRCRAFT, POSITION 1, DUE T O FAN ATTRITION LINER DAMAGE. THE ENGINE WAS SHIPPED TO MANUFACTURER FOR INVESTIGATION AND REPAIR. THE LAST TWO SHOP V ISITS WERE IN 2005 AND 2004 WERE FOR FAN CASE LINER PROBLEMS. AT THE LSV, THE FOLLOWING LEVELS OF MAINTENANCE WERE PERF ORMED: L3 ON THE FAN, L2 ON THE FAN CASE THE REASON FOR REMOVAL WAS VERIFIED BASED ON THE CONDITION OF THE ATTRITION LIN ERS AND MISSING ACOUSTIC LINERS FROM 3 TO 9 O`CLOCK POSITION. SIX OF TWELVE ACOUSTIC LINERS SEPARATED FROM THE FAN CASE AND LODGED IN THE FEGVÕS. SUBSEQUENTLY, A FULL FAN CASE LINER / PANEL REPLACEMENT OCCURRED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112900013 20071129 00013 EA 2007 11 29 COMA0760647 1 20071115 A 3230 601R751461 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 969CA 25247 7141 FLIGHT 9484 - GEAR DISAGREE ON FINAL APPROACH NOSE GEAR WOULD NOT COME DOWN. FOLLOWED QRH, LOWERED GEAR MANUALLY AND LA NDED SAFELY. REMOVED AND REPLACED NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2007112900024 20071129 00024 EA 2007 11 29 COMA0760658 1 20071120 A 3230 4622 VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 798CA 14638 7314 FLIGHT 5604 - DURING CVG APPROACH RECEIVED A LANDING GEAR DISAGREE CAUTION. CREW DECLARED AN EMERGENCY AND ABORTED APPR OACH, THEN LANDED WITHOUT INCIDENT ON SECOND APPROACH. REPLACED NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2007112900035 20071129 00035 NM 2007 11 29 2007UALA04754 1 20071119 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 610 S16-17L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 REPAIR DOUBLER AT BS 610 IS DENTED BETWEEN STR 16L-STR 17L. REMOVED DAMAGED AREA, FABRICATED REPAIR, AND INSTALLED A NE W DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007112900046 20071129 00046 NM 2007 11 29 2007UALA04765 1 20071120 A 5754 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 6 SLAT DELAMINATED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 533UA 25073 RTFL WITH A DELAMINATING NR 6 SLAT. POSSIBLE BIRD STRIKE. THE RT WING LE AREA INBOARD OF THE ENGINE DELAMINATION AND M ISSING MATERIAL. AREA OF DAMAGE IS APPROX 1 FOOT LONG BY 6" WIDE. THIS DAMAGE IS TO THE NR 6 SLAT. REPLACED THE NR 6 LE SLAT 2 L 7 2 4F 4 F RT A2NM E17NE 2007112900051 20071129 00051 EU 2007 11 29 2007UALA04771 2 20071119 A 7200 ENGINE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LEAKING A UALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 399UA 24674 725210 ON TAKEOFF AND CLIMB; MUSTY, DIRTY SOCK ODOR IN COCKPIT. FOUND EVIDENCE OF INTERNAL OIL LEAK AT HPC STAGE 1, 2, & 3. R EPLACED ENGINE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112900054 20071129 00054 NM 2007 11 29 2007UALA04776 1 20071120 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 294-360 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 CABIN FLOOR CREASE BEAM HAS SPOTS OF CORROSION AT BS 294-360, RBL 49". REMOVED AND REPLACED CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112900055 20071129 00055 NM 2007 11 29 2007UALA04777 1 20071120 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 500C S10L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 331UA 24192 FUSELAGE UPPER INTERNAL SKIN CHEM MILLED HAS CRACK, BS 500C+17" JUST ABOVE STR 10L SKIN LAP. FABRICATED AND INSTALLED EXTERNAL DOUBLER AND FILLERS REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112900057 20071129 00057 NM 2007 11 29 2007UALA04779 1 20071120 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 596UA 28749 CEILING EEL EXIT LIGHT OUT AT OVERWING POSITION. FOUND BATTERY PACK LOOSE. SECURED LOOSE BATTERY PACK AT SEAT 23DEF. 2 L 7 2 4F 4 F RT A2NM E17NE 2007112900061 20071129 00061 NM 2007 11 29 2007UALA04784 1 20071120 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 246 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 662UA 27159 ON THE FORWARD FACE OF FLOORBEAM LOCATED AT BS 246 LBL 22L AT STIFFENER IS CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED STIFFENER. 2 L 7 2 4F 4 F RT A1NM E24NE 2007112900062 20071129 00062 2007 11 29 2007UALA04785 4 20071120 A 2565 767 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE R3 DOOR SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 773UA 26929 DOOR 3R EXTERIOR SLIDE LIGHT INOPERATIVE. DOOR 3R EXTERIOR SLIDE LIGHT INOPERATIVE , REPLACED BULB OK FOR SERVICE 2 L 7 2 4F 4 F RT T0001SE E46NE 2007112900065 20071129 00065 SO 2007 11 29 C2XA07CL100 1 20071124 A 3350 2013BR BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16976 145171 DURING ROUTINE MAINTENANCE THE LEFT AND RIGHT EXTERNAL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REP LACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2007112900066 20071129 00066 EU 2007 11 29 YEAN2007102 1 20071119 A 2121 EVT3454H FAN AIRBUS 320 A320232 3930326 EU CABIN AIR BURNED OUT A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 556JB 22238 13563 1904 FLT 411, BOS-SAN, APPROX BETWEEN 12:00Z-15:00Z, LOUD NOISE AND STRANGE/ELECTRICAL ODOR FOLLOWED BY BLOWER FAN FAULT, RAN ECAM SET BLOWER TO OVERRIDE-SOUND AND ODOR CEASED. REMOVED AND REPLACED BLOWER FAN, NO MESSAGES REMAINED, OPS CHECK OK . 2 L 7 2 4F RT A28NM 2007112900068 20071129 00068 WP 2007 11 29 ASAA0782280 1 20071124 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 235 S17-18L DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 982AS 53473 TWO DENTS ON FUSELAGE SKIN AT STA 235 BETWEEN LEFT L 17 & 18. REPLACED FORMER & REPAIRED SKIN PER SRM 53-04 FIG 12B & E A 5330 02266. 2 L 7 2 4F RT A6WE 2007112900071 20071129 00071 EA 2007 11 29 TRAX200701762 1 20071116 A 5510 FITTING CNDAIR CL600 CL6002B19 1900309 EA CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 883AS 7504 HORIZONTAL ANTI-ROTATION FITTING CORRODED. 2 L 7 2 4F RT A21EA 2007112900074 20071129 00074 EA 2007 11 29 TRAX200701765 1 20071121 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 FS 280 LBL 9 ANGLES CRACKED I/B AND O/B. FS 280LBL 9 O/B CLIP ANGLE WAS REPLACED PER REO 601R-53-21-787. 2 L 7 2 4F RT A21EA 2007112900078 20071129 00078 NM 2007 11 29 SWAA075803 1 20071121 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 239WN 34714 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007112900079 20071129 00079 2007 11 29 SWAA075804 4 20071120 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 256WN 32514 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007112900080 20071129 00080 NM 2007 11 29 SWAA075805 1 20071121 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 261WN 32517 R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007112900081 20071129 00081 NM 2007 11 29 SWAA075831 1 20071120 A 3350 65C27028 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 275WN 36153 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 22 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007112900082 20071129 00082 NM 2007 11 29 SWAA075809 1 20071121 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM BS 360 S11L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007112900085 20071129 00085 NM 2007 11 29 SWAA075807 1 20071121 A 5311 6546538 FRAME BOEING 737 7373H4 1384600 NM BS 597 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007112900086 20071129 00086 NM 2007 11 29 SWAA075806 1 20071121 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007112900088 20071129 00088 NM 2007 11 29 SWAA075811 1 20071123 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM BS 259 S19-23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259.5, BETWEEN STR 19L AND STR 23L. REPAIRED SKIN PER SRM . 2 L 7 2 4F RT A16WE 2007112900090 20071129 00090 NM 2007 11 29 SWAA075794 1 20071119 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM BS 380 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007112900091 20071129 00091 NM 2007 11 29 SWAA075796 1 20071119 A 5330 6545777 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007112900092 20071129 00092 NM 2007 11 29 SWAA075795 1 20071119 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 520 S13L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 13L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007112900094 20071129 00094 NM 2007 11 29 SWAA075798 1 20071119 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 727E S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007112900095 20071129 00095 NM 2007 11 29 SWAA075834 1 20071120 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 967 S27L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED 14Y CHECK, FOUND STRINGER 27L CORRODED AT BS 967. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007112900096 20071129 00096 NM 2007 11 29 SWAA075812 1 20071124 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 430 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, BL 0. REPAIRED SKIN P ER ACO. 2 L 7 2 4F RT A16WE 2007112900098 20071129 00098 NM 2007 11 29 SWAA075814 1 20071123 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM R2 DOOR INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 409WN 27896 R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007112900100 20071129 00100 NM 2007 11 29 SWAA075835 1 20071119 A 5610 141A481014 WINDOW BOEING 737 7377H4 1384404 NM FLIGHT DECK ARCED A SWAA O OTHER O OTHER NR NOT REPORTED 1 SW 29 439WN 29834 FLIGHT DECK L2 WINDOW ARCED. REMOVED AND REPLACED WINDOW AND CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 2007112900103 20071129 00103 2007 11 29 SWAA075817 4 20071122 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 481WN 29853 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007112900104 20071129 00104 NM 2007 11 29 SWAA075818 1 20071124 A 2560 P4010021 BATTERY BOEING 737 7375H4 138449D NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED MV1 CHECK, FOUND AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2007112900106 20071129 00106 NM 2007 11 29 SWAA075820 1 20071120 A 3350 3071BPEGPL LAMP BOEING 737 7375H4 138449D NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 5 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007112900107 20071129 00107 NM 2007 11 29 SWAA075800 1 20071120 A 5610 5717623122 WINDOW BOEING 737 7375H4 138449D NM COCKPIT ARCED A SWAA O OTHER O OTHER NR NOT REPORTED 1 SW 29 509SW 24186 FLIGHT DECK R2 WINDOW ARCED. REMOVED AND REPLACED WINDOW AND CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 2007112900108 20071129 00108 2007 11 29 SWAA075821 4 20071125 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007112900112 20071129 00112 NM 2007 11 29 SWAA075823 1 20071123 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007112900114 20071129 00114 2007 11 29 SWAA075825 4 20071120 A 2565 6949956 CONTROL CABLE BOEING 737 7373H4 1384600 NM R2 DOOR SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 619SW 28035 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM. 2 L 7 2 4F RT A16WE 2007112900115 20071129 00115 2007 11 29 SWAA075836 4 20071119 A 2565 D31354418 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007112900116 20071129 00116 NM 2007 11 29 SWAA075801 1 20071119 A 5753 SKIN BOEING 737 7373H4 1384600 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 2181 27719 DURING SCHEDULED MV2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP LOWER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PE R MM. 2 L 7 2 4F RT A16WE 2007112900117 20071129 00117 NM 2007 11 29 SWAA075837 1 20071119 A 5330 6545766 SKIN BOEING 737 737301 1384611 NM BS 517D S12L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 517D, STR 12L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007112900118 20071129 00118 NM 2007 11 29 SWAA075838 1 20071119 A 5330 6545776 SKIN BOEING 737 737301 1384611 NM BS 984 S24R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 984, STR 24R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007112900119 20071129 00119 NM 2007 11 29 SWAA075826 1 20071125 A 3350 1619 LAMP BOEING 737 7373G7 1384595 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007112900120 20071129 00120 NM 2007 11 29 SWAA075827 1 20071121 A 5755 HINGE BOEING 737 7373Q8 1384670 NM NR 4 SPOILER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW MA4581 23254 DURING SCHEDULED MV1 CHECK, FOUND LT WING NR 4 GROUND SPOILER INBOARD HINGE BROKEN. REMOVED AND REPLACED SPOILER PER MM . 2 L 7 2 4F RT A16WE 2007112900121 20071129 00121 NM 2007 11 29 SWAA075828 1 20071121 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 770SA 30589 DURING SCHEDULED MV2 CHECK, FOUND LT MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGE R PER MM. 2 L 7 2 4F RT A16WE 2007112900122 20071129 00122 NM 2007 11 29 SWAA075829 1 20071123 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 783SW 29809 EEPLS LENS LOOSE AT ROW 8 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007112900123 20071129 00123 NM 2007 11 29 SWAA075830 1 20071121 A 3350 6556633 LIGHT BOEING 737 7377H4 1384404 NM RT OVERWING INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 797MX 27890 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007112900128 20071129 00128 EU 2007 11 29 07FDEA04796 1 20071115 A 4990 OIL SYSTEM AIRBUS 300 A300F4605R 3930327 EU APU LEAKING A FDEA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 661FE 760 DURING TAXI OUT MAIN DECK CARGO SMOKE DETECTOR "B" LOOP INDICATED SMOKE. ECAM INDICATED SMOKE IN AFT COMPARTMENT. STOP PED AIRCRAFT AND COMPLIED WITH ECAM. WARNING EXTINGUISHED WHEN NR 2 PACK VALVE TURNED OFF. RETURNED TO GATE. MAIN DEC K CARGO DETECTOR AFT LOOP A INOP-PREV-MEL. AFTER BLOCK IN FOUND APU LEAKING OIL INTO APU INTAKE CAUSING SMOKE IN CABIN DURING PACK OPERATION. REMOVED AND REPLACED NR 1 AND 2 PACK COALESCER BAGS, REF MM 21-51-16-3. MEL'D APU SEE WRI 49-10 /0023. RAN ENGINES AT POWER TO CLEAR PNEUMATIC DUCTS OF OIL RESIDUE PER MM 21-51-00-3. NOW BOTH AIR-CONDITIONING PACKS WORK AND SMELL NORMAL. 2 L 7 2 4F RT A35EU 2007112900130 20071129 00130 NM 2007 11 29 07FDEA04785 1 20071114 A 5410 65195086 FLANGE BOEING 727 727225 1384077 NM NR 1 NACELLE DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 NR 1 ENGINE UPPER COWL T/E FLANGE IS CHIPPED AND DISBONDED REMOVED NR 1 ENGINE UPPER COWL T/E FLANGE, LOCATED AND DRILLE D NEW FLANGE. INSTALLED NEW FLANGE, REF SRM 51-30-2 PG 1-4 REF DWG 65-19508. 2 L 7 3 4F A3WE 2007112900131 20071129 00131 NM 2007 11 29 TSAA0777061 1 20071112 A 7700 UNKNOWN BOEING 737 737210C 1384459 NM EPR INDICATIONS UNKNOWN A TSAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 13 834AL 20917 NON-ETOPS CARGO FLIGHT 909 HNL-LIH - DURING TAKE OFF, THE CREW NOTED ERRONEOUS EPR INDICATIONS FROM BOTH ENGINES. THE C REW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE RESET BOTH EPR CIRCUIT BREAKERS PER AMM 77-11-0 PG 501 AND RAN THE ENGINES WITH ALL OPERATIONAL CHECKS SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVI CE. 2 L 7 2 4F A16WE 2007112900132 20071129 00132 EU 2007 11 29 MALA070181 1 20071114 A 3020 HEATER SAAB SF340 340B 7860101 EU LT INTAKE SPARKS A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 452XJ 340B452 LEFT INTAKE HEAT SPARKING. AIR-TURN-BACK, SLIGHT SMOKE ODOR IN CABIN DUE TO INTAKE SMOKE INGESTION INTO BLEED SYSTEM. REMOVED AND REPLACED LOWER DUCT. 2 L 7 2 4T RT A52EU 2007112900135 20071129 00135 NM 2007 11 29 07FDEA04801 1 20071116 A 5753 HINGE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 RIGHT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FORWARD INBOARD NR 2 BOLT HOLE, FOUND CORROSION. REMOVED AND R EPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRIED OUT FOUND 'SATIS' AS PER AMM 27-50-00-5. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007112900136 20071129 00136 NM 2007 11 29 07FDEA04802 1 20071116 A 5753 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM RT WING TE FLAPS CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 RIGHT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FORWARD OUTBOARD NR 2 BOLT HOLE, FOUND CORROSION. REMOVED AND R EPLACED AS PER AMM 27-50-30-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007112900140 20071129 00140 NM 2007 11 29 07FDEA04806 1 20071116 A 5730 ACCESS DOOR DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 2 EACH CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA X ORS 683 AND STA XORS 713 FASTENER HOLES. REPAIRED AS PER FEDEX EA 1-5710-117059. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100. 2 L 7 3 4F RT A22WE 2007112900141 20071129 00141 NM 2007 11 29 07FDEA04807 1 20071116 A 5730 ACCESS DOOR DOUG MD11 MD11F 3023600 NM BS 683-713 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 1 EACH FASTENER HOLE FOUND DAMAGED DURING HFEC OPEN HOLE INSPECTION ON LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN S TA XORS 683 AND STA 713. REPAIRED AS PER FEDEX EA 1-5710-117058, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007112900143 20071129 00143 EU 2007 11 29 07FDEA04809 1 20071116 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT PIT, BILGE AREA, STRINGER 51R CORRODED, FR 54.1 TO 54.3 (STA X 2984 - 3090). CUT OUT CORRODED SECTION AND SPLICED IN NEW SECTION IAW A310-200 SRM 53-10-14. 2 L 7 2 4F RT A35EU 2007112900144 20071129 00144 EU 2007 11 29 07FDEA04810 1 20071116 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 BULK CARGO PIT, STRINGER 55 CORRODED AT FRAME 65 (STA X 3514). REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-10-00. INSTALLED STRINGER REPAIR IAW A310 SRM 53-10-14 FIGURE 201. 2 L 7 2 4F RT A35EU 2007112900145 20071129 00145 EU 2007 11 29 07FDEA04811 1 20071116 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT PIT, STRINGER 57L CORRODED BETWEEN FR 54.2 AND FR 54.3 (STA X 3037 - 3090). ALL CORRECTIVE ACTION COMPLIED WITH ON EA 6-5310-113000. 2 L 7 2 4F RT A35EU 2007112900146 20071129 00146 EU 2007 11 29 07FDEA04812 1 20071116 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT CARGO PIT BILGE AREA, STRINGER 56L CORRODED BETWEEN FR 60 T0 FR 61 (STA X 3249 - X3302). REMOVED CORROSION IAW A31 0 SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-10-00. CUT OUT DAMAGE SECTION IAW A310 SRM 53-10-14. LOCATED AND DRILLED NEW STRINGER IAW A310 SRM 51-40-44. FABBED TWO REPAIR SPLICES IAW A310 SRM 53-10-44. ALODINED IAW A310 SRM 5 1-21-10, PRIMED AND TOP COATED IAW A310 SRM 51-23-10. INSTALLED STRINGER AND REPAIR PARTS IAW A310 SRM 53-10-14 REINSTAL LED SHEAR TIE. 2 L 7 2 4F RT A35EU 2007112900150 20071129 00150 EU 2007 11 29 07FDEA04816 1 20071116 A 5315 A5381293420000 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 MAIN DECK FLOOR, ADAPTER TRACK ( CROSS BEAM ) CRACKED, FR 50 ( STA X2718 ) BL 17L TO 37L ( Y430 - Y940 ). REMOVED AND REPLACED CROSS BEAM, REF: A310-200 SRM 51-40-21 PAR 5. LOCATED AND DRILLED NEW CROSS BEAM REF: A310-200 SRM 51-40-44 PA R 2. 2 L 7 2 4F RT A35EU 2007112900151 20071129 00151 EU 2007 11 29 07FDEA04817 1 20071116 A 5315 A5381293420000 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 MAIN DECK FLOOR, ADAPTER TRACK ( CROSSBEAM ) CRACKED, FR 50 ( STA X2718 ) BL 17L TO 37L ( Y430 - Y940 ). REMOVED AND R EPLACED CROSSBEAM, REF: A310-200 SRM 51-40-21 PAR 5. LOCATED AND DRILLED NEW CROSSBEAM REF: A310-200 SRM 51-40-44 PAR 2 . 2 L 7 2 4F RT A35EU 2007112900152 20071129 00152 EU 2007 11 29 07FDEA04818 1 20071116 A 5315 A5381293420000 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 MAIN DECK FLOOR, ADAPTER TRACK (CROSS BEAM) CRACKED AT FR 53 ( Z2878 ), BL 17L TO BL 37L ( Y430 - Y940 ). REMOVED AND REPLACED CROSSBEAM, REF: A310-200 SRM 51-40-21 PAR 5. LOCATED AND DRILLED NEW CROSS BEAM REF: A310-200 SRM 51-40-44 PAR 2. 2 L 7 2 4F RT A35EU 2007112900153 20071129 00153 EU 2007 11 29 07FDEA04819 1 20071116 A 5315 A5381293420000 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 MAIN DECK FLOOR, CARGO TIE DOWN ADAPTER (CROSS BEAM) CRACKED, AT FR 50 (STA Z2718 ) BL 36R ( -Y 480 TO -Y920 ). REMOVE D AND REPLACED CROSSBEAM, REF: A310-200 SRM 51-40-21 PAR 5. LOCATED AND DRILLED CROSSBEAM REF: A310-200 SRM 51-40-44 PA R 2. 2 L 7 2 4F RT A35EU 2007112900155 20071129 00155 NM 2007 11 29 QXEA200701725 1 20071115 A 2121 011749500 COOLING FAN BOMBDR DHC8 DHC8402 1390042 NM E/E BAY INOPERATIVE A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 400QX 16761 16761 4030 SEA FLIGHT NR 2279: SEA TO RDM FLIGHT - AFTER TAKEOFF, FANS FAIL ED MESSAGE. MESSAGE WENT AWAY UPON WOW. AIRCRAFT WAS DIVERTED TO PDX. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF AVIONICS COOLING FANS IAW Q400 AMM TASK 21-25-00-710-801 . FLAGGED NR 1 AVIONICS FAN INOP. REMOVED AND REPLACED NR 1 AVIONICS COOLING FAN WITH SERVICEABLE FROM STOCK IAW TASK 21-25-04-400-801 AND TASK 21-25-04-000-801. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007112900157 20071129 00157 NM 2007 11 29 DL738071479 1 20071113 A 2130 365701064 SENSOR BOEING 737 737832 13844CF NM NR 1 NACELLE OPEN A DALA B EMER. DESCENT G MULTIPLE FAILURE CR CRUISE 1 SO 27 3730B 30538 AT FL 390 AND .77M ATC REQUESTED TO SLOW TO .75M. ALMOST IMMEDIATELY GOT NR 1 LEFT BLEED TRIP. LOST CABIN PRESS CABIN WENT UP TO 12'000 TO 12'200. BEFORE BLEED RESET WORKED AT APPROX 29'000. LEVELED AT FLT 250 AND KEPT AS STABLE AS POSS IBLE. NO FURTHER TRIPS OCCURRED. MTC IN PROGRESS DNTC. REPLACED 390 DEG TEMP SENSOR ON NR 1 ENG PYLON. REPLACED 390 DEG TEMP SENSOR NR 2 ENG PYLON. CKS GOOD PER M/M. 2 L 7 2 4F RT A16WE 2007112900160 20071129 00160 NM 2007 11 29 DLM90071484 1 20071113 A 3260 833703 SENSOR DOUG MD90 MD9030 3023690 NM LT MLG OUT OF LIMITS A DALA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 915DN 53395 UNSAFE LEFT MAIN GEAR INDICATION. INSPECTED LT GEAR AREA FOR DAMAGE, CKS GOOD. FOUND LT GEAR DOWN AND LOCKED PROXIMITY SENSOR ON OUTER RANGE LIMIT. ADJUSTED PER MM 32-61-02-420-802-CK'D PSEU NOW SHOWS NEAR AND INDICATION IS NORMAL, PSEU SHOWS NO ADDITIONAL FAULTS. SENSOR SHOWS PASS AND CLOSE. 2 L 7 2 4F RT A6WE 2007112900161 20071129 00161 NM 2007 11 29 DL76G071485 1 20071112 A 5315 BAC1505100393 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 645 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 156DL 25354 FWD CARGO STATION 645+110 LBL 41 CARGO FLOOR BEAM UPPER CHORD CORRODED. REPAIRED ON NR APP509288 PER 53-00-07D FIGURE 8 01DAT HMV3/PSV17. 2 L 7 2 4F RT A1NM 2007112900162 20071129 00162 NM 2007 11 29 DL76G071486 1 20071113 A 5315 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 720 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 152DL 24984 FWD CARGO STATION 720 LBL 41 CARGO FLOORBEAM UPPER CHORD FWD BOTTOM SIDE CORRODED. REPAIRED PER 53-00-07D FIGURE 801D O N NR APP509228 AT HMV3/PSV 17. 2 L 7 2 4F RT A1NM 2007112900165 20071129 00165 NM 2007 11 29 DL76G071489 1 20071113 A 5315 LS50337075 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 1197 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 152DL 24984 AFT CARGO STATION 1197+132 LBL 41 CARGO FLOORBEAM FWD FACE UPPER CHORD NUT SIDE CORRODED. REPAIRED ON APP514981 PER 53- 00-07D FIGURE 801D AT HMV3/PSV17. 2 L 7 2 4F RT A1NM 2007112900168 20071129 00168 NM 2007 11 29 DL76G071492 1 20071113 A 5315 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 1197 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 152DL 24984 AFT CARGO STATION 1197+88 RBL 41 CARGO FLOORBEAM FWD FACE UPPER SURFACE AND BOTTOM SURFACE CORRODED. REPAIRED PER 53-00 -07 REPAIR 4 FIGURE 201 ON NR APP515160 AT HMV3/PSV17. 2 L 7 2 4F RT A1NM 2007112900169 20071129 00169 NM 2007 11 29 DL76G071493 1 20071112 A 5311 FRAME BOEING 767 7673P6 1385105 NM BS 1809 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 152DL 24984 BS 1809 OUTER FRAME FOUND CRACKED AT FRAME RADIUS BETWEEN STRINGER 7R AND 8 R APPROX 3/4 INCH. REPAIRED PER SRM 53-80-0 8 FIGURE 201 REPAIR 9 ON APP 502887 ON HMV 3/ PSV17. 2 L 7 2 4F RT A1NM 2007112900170 20071129 00170 NM 2007 11 29 DLM88071494 1 20071113 A 5414 SKIN DOUG MD88 MD88 3023688 NM NR 2 NACELLE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 969DL 53172 DUE SPLSKD SRM REPAIR 53-04 DENT/GOUGE NR 2 PYLON ABOVE LGN 19R FWD OF STA 1309. REPAIRED PER SRM 53-04D FIG 12B CLASS 2. REINSPECT DUE AT 15000 CYCLES. DATA RETRIEVAL SENT. 2 L 7 2 4F RT A6WE 2007112900171 20071129 00171 NE 2007 11 29 DLM88071496 2 20071115 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 STALLED A DALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SO 27 965DL 40068 49984 725997 LT ENGINE COMPRESSOR STALL AT FLT LEVEL 290, NO POWER EPR WOULD NOT INCREASE. ALL OTHER INDICATIONS NORMAL. REPLACED N R 1 ENG. 2 L 7 2 4F 4 F RT A6WE E9NE 2007112900173 20071129 00173 NM 2007 11 29 USAA920071145 1 20071114 A 5755 65C2525121SP SKIN BOEING 737 7373G7 1384595 NM SPOILER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 PHX - MAJOR REPAIR - RIGHT WING NR 6 SPOILER PANEL DISBONDED UPPER SURFACE, WS 290.07 - WS 342.53. REPLACED THE NR 6 SP OILER, WS 290.07 - WS 342.53 IAW B737 AMM 27-61-11-4. 2 L 7 2 4F RT A16WE 2007112900174 20071129 00174 NM 2007 11 29 USAA920071150 1 20071110 A 5330 6545769 SKIN BOEING 737 7373G7 1384595 NM BS 527 S27L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, CRACKED FUSELAGE SKIN, BS 527, S27L. REPAIRED FUSELAGE SKIN, BS 527, S27L IAW USAIRWAYS EA 98963. 2 L 7 2 4F RT A16WE 2007112900175 20071129 00175 NM 2007 11 29 USAA920071151 1 20071102 A 5531 6552490 SPAR BOEING 737 7373G7 1384595 NM VERTICAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, CRACKED VERTICLE STABILIZER LEFT AFT SPAR CHORD, RUDDER STATION 18. REPLACED VERTICLE S TABILIZER LEFT AFT SPAR CHORD, RUDDER STATION 18 I/A/W B737 SRM 55-30-13. 2 L 7 2 4F RT A16WE 2007112900176 20071129 00176 NM 2007 11 29 USAA920071152 1 20071115 A 5320 69432331 ANGLE BOEING 737 7373B7 1384580 NM BS 794 S25R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED ANGLE, BS 794, S25R. REPLACED ANGLE, BS 794, S25R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007112900177 20071129 00177 NM 2007 11 29 USAA920071154 1 20071023 A 5311 65465252 FRAME BOEING 737 7373B7 1384580 NM BS 380 S8-9R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - CRACKED FRAME, BS 380, S8R - S9R. REPAIRED FRAME, BS 380, S8R - S9R IAW USAIRWAYS EO 5311-01019. 2 L 7 2 4F RT A16WE 2007112900178 20071129 00178 NM 2007 11 29 USAA920071155 1 20071023 A 5311 654653211 FRAME BOEING 737 7373B7 1384580 NM BS 480 S8-9R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 480, S8R - S9R. REPAIRED FRAME, BS 480, S8R - S9R IAW USAIRWAYS EO 5 311-01019. 2 L 7 2 4F RT A16WE 2007112900179 20071129 00179 NM 2007 11 29 USAA920071156 1 20071025 A 5311 90526911 FRAME BOEING 737 7373B7 1384580 NM BS 787 S8-9R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 787, S8R - S9R. REPAIRED FRAME, BS 787, S8R - S9R IAW USAIRWAYS EO 5 311-01019. 2 L 7 2 4F RT A16WE 2007112900181 20071129 00181 NM 2007 11 29 USAA920071158 1 20071024 A 5311 654655211 FRAME BOEING 737 7373B7 1384580 NM BS 827 S8-9R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 827, S8R - S9R. REPAIRED FRAME, BS 827, S8R - S9R IAW USAIRWAYS EO 5 311-01019. 2 L 7 2 4F RT A16WE 2007112900184 20071129 00184 NM 2007 11 29 USAA920071161 1 20071024 A 5311 90526911 FRAME BOEING 737 7373B7 1384580 NM BS 807 S8-9L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - CRACKED FRAME, BS 807, S8L - S9L. REPAIRED FRAME, BS 807, S8L - S9L IAW USAIRWAYS EO 5311-01019. 2 L 7 2 4F RT A16WE 2007112900185 20071129 00185 NM 2007 11 29 USAA920071162 1 20071024 A 5311 654655211 FRAME BOEING 737 7373B7 1384580 NM BS 827 S8-9L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 827, S8L - S9L. REPAIRED FRAME, BS 827, S8L - S9L IAW USAIRWAYS EO 5 311-01019. 2 L 7 2 4F RT A16WE 2007112900186 20071129 00186 NM 2007 11 29 USAA920071163 1 20071024 A 5311 6546555 FRAME BOEING 737 7373B7 1384580 NM BS 867 S8-9L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 867, S8L - S9L. REPAIRED FRAME, BS 867, S8L - S9L IAW USAIRWAYS EO 5 311-01019. 2 L 7 2 4F RT A16WE 2007112900188 20071129 00188 NM 2007 11 29 AALA20072173 1 20071108 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 776AN 29582 DFW - EMERGENCY LIGHT AT SEAT ROW 24C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 24C. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007112900189 20071129 00189 NM 2007 11 29 AALA20072174 1 20071108 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 776AN 29582 DFW - EMERGENCY LIGHT AT SEAT ROW 24C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 24C. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007112900190 20071129 00190 GL 2007 11 29 HEEA117612 2 20070925 A 7321 0164548640 FUEL CONTROL SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30 03013 GL NR 2 ENGINE MALFUNCTIONED D HEEA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION HO HOVERING 1 SW 03 776P 595 760275 NR 2 ENGINE DECAYED FROM HOVER POWER TO IDLE APPROXIMATELY 60 N1 DURING HOVER. LANDING AND SHUTDOWN UNEVENTFUL. MAINTE NANCE REPLACED NR 2 FUEL CONTROL. 1 G 7 2 3U 3 U H1NE E1GL 2007112900191 20071129 00191 2007 11 29 QMLA7216 4 20071022 A 2213 7004206901 COMPUTER BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101* NE ROLL CHANNEL BURNED E QMLA H DEACTIVATE SYST/CIRCUITS B F SMOKE/FUMES/ODORS/SPARKS FLT CONT AFFECTED NR NOT REPORTED 1 NM 03 330SL 7216 THE AIRCRAFT ROLLED VERY SLIGHTLY TO THE RT AND THEN TO THE LT. THE ROLL RATE WAS CASUAL, AND SINCE WE WERE FLYING IN SL IGHTLY GUSTY CONDITIONS I TOOK ALMOST NO NOTICE OF IT. THEN THE AIRCRAFT DID IT AGAIN. THIS TIME THE ROLLS WERE ACCOMPAN IED BY THE STRONG ODOR OF HOT ELECTRICAL INSULATION. PUNCHED OFF THE CSAS SYSTEM, THEN RE-ENGAGED THE PITCH AND YAW CHAN NELS AND COMPLETED THE FLIGHT. ROLL CHANNEL WAS MEL'D AND PLACARDED INOP. 1 G 7 2 3U 3 U H13EU E5NE 2007112900194 20071129 00194 NM 2007 11 29 AMTA200700507 1 20071014 A 2840 3012803 PROCESSOR BOEING 737 73783N 13844HI NM FUEL QTY IND UNSERVICEABLE A AMTA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 308TZ 28244 NO FUEL QUANTITY INDICATION ON FMC. REMOVED AND REPLACED FQIS PROCESSOR IAW AMM 28-41-81-4. 2 L 7 2 4F RT A16WE 2007112800036 20071128 00036 NM 2007 11 28 SWAA075742 1 20071116 A 5330 6552988 SKIN BOEING 737 7373G7 1384595 NM BS 960 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 960, R2 DOOR LOWER FWD CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007112800037 20071128 00037 NM 2007 11 28 SWAA075743 1 20071116 A 5330 6550570 SKIN BOEING 737 7373G7 1384595 NM BS 960 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 960, R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007112800072 20071128 00072 NM 2007 11 28 2007UALA04709 1 20071115 A 3350 8200008815ATS LENS BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 654 MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 RIGHT MID CABIN (STA 654) AISLE EXIT LENS IS MISSING. SUSPECT LENS LOST DURING NORMAL OPERATIONS. REPLACED LENS OPS CHEC KED OK. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007112800085 20071128 00085 NM 2007 11 28 2007UALA04725 1 20071117 A 5313 655169810 STRINGER SPLICE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 907 S24R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 FUSELAGE STRINGER END SPLICE DAMAGED, BS 907 STR 24R. MAJOR REPAIR ACCOMPLISHED: REMOVED & INSTALLED NEW STRINGER END SPLICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112800086 20071128 00086 NM 2007 11 28 2007UALA04726 1 20071117 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 360 S14-15R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 FRAME SHEAR TIE IS CRACKED BS 360 BETWEEN STRINGERS 14R-15R. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED SHEAR TIE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112800099 20071128 00099 NM 2007 11 28 2007UALA04742 1 20071116 A 8012 START VALVE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE LEFT ENGINE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 676UA 30028 LEFT ENG START VALVE WON`T OPEN. REPLACED NBR 1 ENG STARTER PER AMM 80-11-01 AND REPLACED STARTER CONTROL VALVE PER AMM 80- 11-02. GRD OPERATION CHECKED GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007112800157 20071128 00157 NM 2007 11 28 SWAA075752 1 20071119 A 5753 SKIN BOEING 737 7373H4 1384600 NM TE FOREFLAP DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 2484 27693 DURING SCHEDULED HC1 CHECK, FOUND LEFT WING OUTBOARD FOREFLAP INBOARD T/E DISBONDED. REMOVED AND REPLACED FOREFLAP PER MM. 2 L 7 2 4F RT A16WE 2007112800164 20071128 00164 NM 2007 11 28 SWAA075775 1 20071113 A 5311 6546537 FRAME BOEING 737 737317 138447P NM BS 727 S13L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 727, STR 13L. REPAIRED CHORD PER BFG ER. 2 L 7 2 4F RT A16WE 2007112800175 20071128 00175 NM 2007 11 28 MWEA070299 1 20071120 A 5320 99576657 CHANNEL BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 918ME 55180 T-CHANNEL DAMAGED AT AFT SIDE NEAR STOP NR 3. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2007112800193 20071128 00193 EU 2007 11 28 USAA920071191 1 20071110 A 5320 D53112224200 FITTING AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 657AW 1083 SAL - MAJOR REPAIR - C3 CHECK - CORROSION ON L2 DOOR CUTOUT LOWER CORNER FITTING, BS 808 / FR 20, S23L. REPLACED L2 DO OR CUTOUT LOWER CORNER FITTING, BS 808 / FR 20, S23 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007112800203 20071128 00203 NM 2007 11 28 USAA920071201 1 20071116 A 5340 6935352U14 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CRACKED STRINGER TIE CLIP, BS 597, S4R. REPLACED STRINGER TIE CLIP, BS 597, S4R IAW B73 7 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007112900001 20071129 00001 CE 2007 11 29 N87SF 1 20070531 A 3260 602EN166B SWITCH DECOTO CESSNA 500 550 2076604 CE ACTUATOR INTERMITTENT E SFOA O OTHER N FALSE WARNING AP APPROACH 1 EA 23 87SF DA22 5500096 UPON APPROACH TO DESTINATION AIRPORT THE GEAR WAS SELECTED DOWN. THE PILOT NOTED THAT THE LT GEAR DOWN & LOCKED ANNUNCI ATOR WAS NOT ILLUMINATED. THE PILOT RECYCLED THE GEAR BUT THE LIGHT STILL WOULD NOT ILLUMINATE. FOLLOWING PROCEDURES, THE EMERGENCY GEAR EXTENSION SYSTEM WAS ENGAGED AND A SAFE LANDING WAS MADE. AFTER TAXI TO THE RAMP, IT WAS NOTED THAT THE DOWN AND LOCKED ANNUNCIATOR HAD ILLUMINATED. A FERRY PERMIT WAS OBTAINED AND THE AIRCRAFT WAS FLOWN TO HOME BASE GE AR DOWN, WHERE AN UNEVENTFUL LANDING WAS MADE. INVESTIGATION INTO THE PROBLEM REVEALED THAT THE LT GEAR DOWNLOCK SWITCH HAD FAILED. THE SWITCH WAS REPLACED, THE EMERGENCY GEAR SYSTEM WAS RESET, AND THE GEAR WAS CYCLED NUMEROUS TIMES WITHO 1 L 7 2 4F A22CE 2007112900003 20071129 00003 EU 2007 11 29 XV6A200700002 1 20070924 A 5522 FABRIC DORNER DO228 DO228202 2992030 EU GARRTT TPE331 TPE33110T WP HARTZL HCB4T HCB4TN5 GL ELEVATOR TORN E XV6A O OTHER E VIBRATION/BUFFET CR CRUISE 1 WP 19 403VA 2356 1171 8171 DURING CRUISE FLIGHT, PILOT FELT A BUMP IN THE CONTROL COLUMN. CONTROL COLUMN MOVED UNCOMMANDED FORWARD AND AFT. POWER REDUCTION RESULTED IN NORMAL FLIGHT CHARACTERISTICS. AFTER NORMAL LANDING FOUND LEFT ELEVATOR UPPER SURFACE FABRIC TOR N OFF. DURING INVESTIGATION FOUND A 5 INCH SECTION WHERE GLUE WAS NOT PRESENT. POSSIBLE GLUE WAS WEAK AT THIS POINT. 2 H 7 2 4T 4 T RT A16EU E4WE 6 C P40EA 2007112900007 20071129 00007 EA 2007 11 29 COMA0760641 1 20071113 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 443CA 7539 FLIGHT 5641 - FLAPS FAIL CAUTION MESSAGE CAME ON AT FLIGHT LEVEL 320 WITH FLAPS AT 0 DEGREES. COMPLIED WITH AD 2006-12- 21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH N O FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007112900015 20071129 00015 EA 2007 11 29 COMA0760649 1 20071115 A 2760 SPOILER SYS CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 629BR 7251 FLIGHT 5592 - ON T/O ROLL RECEIVED WARNING CONFIG SPOILERS MESSAGE. ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORME D RESET OF SECU'S NR 1 AND NR 2, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007112900029 20071129 00029 NM 2007 11 29 2007UALA04746 1 20071119 A 5241 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 FWD GALLEY DOOR, LOWER AFT CORNER FRAME CRACKED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112900032 20071129 00032 NM 2007 11 29 2007UALA04749 1 20071119 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 R2 DOOR UPPER HINGE CUTOUT REQUIRES DOUBLER CRACKED. PERFORMED HFEC PER NDT MANUAL. FOUND 1 EA CRACK. REMOVED DAMAGED AREA AND INSTALLED DOUBLER IN THE AREA. 2 L 7 2 4F 4 F RT A2NM E17NE 2007112900033 20071129 00033 NM 2007 11 29 2007UALA04750 1 20071119 A 5210 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 R1 DOOR WEB GOUGED BY UPPER HINGE ARM CUTOUT INTERCOSTAL STRUCTURE OF DOOR. REMOVED DAMAGED AREA, FABRICATED AND INSTAL LED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007112900041 20071129 00041 NM 2007 11 29 2007UALA04760 1 20071120 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 53ABC INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 SEAT 53ABC EMERGENCY LIGHT IS INOP. REPLACED LIGHT STRIP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112900048 20071129 00048 NM 2007 11 29 2007UALA04768 1 20071121 A 5330 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 843UA 1573 PUNCTURE HOLE IN SKIN JUST FWD AND BELOW DOOR 1L. REMOVED DAMAGED AREA AND PERFORMED HFEC AROUND CUTOUT, NO CRACKS NOT ED. PERFORMED A TEMP REPAIR, PERMANENT REPAIR TO BE INSTALLED WITHIN 3000 FH. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112900052 20071129 00052 EU 2007 11 29 2007UALA04774 1 20071120 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 430UA 568 DURING 3 SVC FOUND EMERGENCY LIGHT FAULT. FOUND EPSU FAILED. REPLACED FWD LT EPSU..OPS CHECKED GOOD-NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112900059 20071129 00059 NM 2007 11 29 2007UALA04782 1 20071120 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 4L UPPER CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 L4 DOOR UPPER GATE CORRODED. REMOVED & REPLACED GATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007112900063 20071129 00063 NM 2007 11 29 2007UALA04786 1 20071121 A 2910 UNKNOWN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE HYD SYSTEM UNKNOWN A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 195UA 26899 EMERGENCY DECLARED DUE TO NR 4 HYDRAULIC SYSTEM ISSUE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112900064 20071129 00064 EU 2007 11 29 2007UALA04787 1 20071121 A 2910 LINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYD SYSTEM BURST A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 432UA 587 GREEN RESERVOIR LOW LEVEL DISPLAYED ON UPPER ECAM SCREEN. EMERGENCY DECLARED. FOUND LT ENGINE HYDRO FLEX LINE TO TRA NSMITTER, BURST. REPLACED LINE,LEAK CHECKED AND SVCD HYD. TO FULL 2 L 7 2 4F 4 F RT A28NM E40NE 2007112900072 20071129 00072 EU 2007 11 29 TRAX200701763 1 20071120 A 5210 PIN AEROSP ATR72 ATR72 EU ASD HANDLE BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 REF DEF 086935 ASD HANDLE HAS BROKEN PIN. 2 H 7 2 4T RT 2007112900075 20071129 00075 EA 2007 11 29 TRAX200701769 1 20071121 A 5740 ATTACH BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 LEFT WING CENTER L/E INBOARD ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED ATTACH BRACKET WITH SERVICEABLE BRACKET PN 600-12045-11 IAW CRJ MM 20-21-00. 2 L 7 2 4F RT A21EA 2007112900077 20071129 00077 2007 11 29 SWAA075802 2 20071121 A 7230 3400018050 COMPRESSOR WHEEL BOEING 737 7377H4 1384404 NM NR 2 ENGINE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 227WN 34450 DURING SCHEDULED HC1 CHECK, FOUND NR 2 ENGINE BLADE PLATFORM CRACKED. REMOVED AND REPLACED PLATFORM PER MM. 2 L 7 2 4F RT A16WE 2007112900083 20071129 00083 NM 2007 11 29 SWAA075832 1 20071122 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 360 S5L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007112900087 20071129 00087 NM 2007 11 29 SWAA075810 1 20071120 A 5753 6573731 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED BRDG CHECK, FOUND RT WING INBOARD T/E FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007112900089 20071129 00089 NM 2007 11 29 SWAA075793 1 20071119 A 5330 6545777 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007112900097 20071129 00097 2007 11 29 SWAA075813 4 20071120 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007112900102 20071129 00102 NM 2007 11 29 SWAA075799 1 20071120 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 478WN 33989 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007112900105 20071129 00105 NM 2007 11 29 SWAA075819 1 20071120 A 3350 3071BPEGPL LAMP BOEING 737 7375H4 138449D NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 3 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007112900126 20071129 00126 EU 2007 11 29 07FDEA04794 1 20071114 A 2420 9612660321 GENERATOR AIRBUS 300 A300F4605R 3930327 EU NR 2 INOPERATIVE A FDEA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 SO 25 685FE 803 REJECTED T/O ON 18L KMEM DUE TO F/O'S PFD AND NAV DISPLAY SHOWING DIAGONAL LINES. ABORTED AT 60 KTS. ALL CHECKLISTS C OMPLETED AND PERFORMED SECOND UNEVENTFUL TAKEOFF. PERFORMED EFIS BITE AND DISPLAYS TEST ON SYSTEM, ALL CHECKS NORMAL. SWAPPED NR 3 SGU AND NR 2 SGU AS PRECAUTIONARY, PERFORMED OPS CHECK PER MM 34-71-00-5. ALL SYSTEMS CHECK NORMAL AT TH IS TIME. NO HISTORY FOR 30 DAYS SGU NR 2 P/N 9612660321, S/N 1626 SGU NR 3, P/N 9612660321 S/N 1973. SWAPPED UNITS PRE CAUTIONARY 4 GOOD LEGS. 2 L 7 2 4F RT A35EU 2007112900129 20071129 00129 WP 2007 11 29 07FDEA04799 1 20071115 A 5512 ALC74392 SKIN DOUG MD10 MD1010F 3022112 WP HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 RT HORIZONTAL STAB UPPER REAR SKIN PANEL HAS APPROXIMATELY A I/2 INCH LONG CRACK INDICATION. REPAIRED RIGHT HAND HORIZO NTAL STAB SKIN PANEL IN REFERENCE TO EA 8-5510-109228. 2 L 7 3 4F RT A22WE 2007112900138 20071129 00138 NM 2007 11 29 07FDEA04804 1 20071116 A 5753 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 RIGHT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING AFT STRUT FORWARD BOLT HOLE, FOUND CORROSION. REMOVED AND REPLA CED AS PER AMM 27-50-30-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007112900139 20071129 00139 NM 2007 11 29 07FDEA04805 1 20071116 A 5730 ACCESS DOOR DOUG MD11 MD11F 3023600 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 3 EACH CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XO RS 683 AND STA XORS 713 FASTENER HOLES. REPAIRED AS PER FEDEX EA 1-5710-117058, REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100. 2 L 7 3 4F RT A22WE 2007112900142 20071129 00142 NM 2007 11 29 07FDEA04808 1 20071116 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1485-1520 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 MAIN DECK CARGO COMPARTMENT AT ABOUT STA 1485 TO STA 1520 RBL 75 SEAT TRACK SUPPORT FLOOR PANEL FLANGE FOUND CORRODED. AREA REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM BS 1451-1531 RBL 75 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAI R CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007112900147 20071129 00147 EU 2007 11 29 07FDEA04813 1 20071116 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT CARGO PIT, STRINGER 52R CORRODED AT FR 62 ( STA X 3355 ). REPAIRED IAW A310 SRM 53-10-14 2 L 7 2 4F RT A35EU 2007112900148 20071129 00148 EU 2007 11 29 07FDEA04814 1 20071116 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT CARGO PIT, STRINGER 52R CORRODED BETWEEN FR 54.2 AND FR 54.3 (STA X 3037 - 3090). FOUND CORROSOIN TO BE OUT OF LIMI TS IAW A310-200 SRM 51-10-00 CUT OUT DAMAGED SECTION, FABBED ALL REPAIR PARTS IAW A310 SRM 53-10-14 FIG 201A. ALODINED A ND PRIMED IAW A310 SRM 51-21-10. PAINTED PARTS IAW A310 SRM 51-21-23. INSTALLED REPAIR AND REPLACED STRINGER SECTION IAW A310 SRM 53-10-14 FIG 201A 2 L 7 2 4F RT A35EU 2007112900156 20071129 00156 NM 2007 11 29 DL76G071478 1 20071113 A 5315 LS50337075T6511 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 1197 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 152DL 24984 AFT CARGO STATION 1197+22 RBL 41 FLOORBEAM UPPER CHORD FWD SIDE CORRODED. REPAIRED PER 53-00-07D FIGURE 801 ON NR APP51 5053 AT HMV3/PSV17. 2 L 7 2 4F RT A1NM 2007112900158 20071129 00158 NM 2007 11 29 DL757071480 1 20071112 A 3350 LIGHT BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 658DL 24420 EMERGENCY PATH LIGHT AT 6 C/D INOP. REPLACED LIGHT ASSY AT 6 C/D, LIGHTS OP NORMAL. 2 L 7 2 4F RT A2NM 2007112900167 20071129 00167 NM 2007 11 29 DL76G071491 1 20071112 A 5315 AND101331401 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 1502 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 152DL 24984 BULK CARGO STATION 1502 CABIN FLOORBEAM LOWER SURFACE CORRODED FROM RBL 7 TO RBL 42. REPAIRED PER 53-00-51D FIGURE 101 ON APP504362. 2 L 7 2 4F RT A1NM 2007112900192 20071129 00192 NM 2007 11 29 AMTA200700485 1 20071009 A 4940 1152464265 POWER UNIT BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE APU INOPERATIVE A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 301TZ 20579 20579 28239 APU WILL NOT START WITH BATTERY POWER ON. REMOVED AND REPLACED APU START POWER UNIT IAW AMM 49-41-71-4. OPS CHECK GOOD . (K) 2 L 7 2 4F 4 F RT A16WE E2GL 2007112900195 20071129 00195 2007 11 29 AMTA200700508 4 20071014 A 3418 0861FL1 SENSOR BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE AOA UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 308TZ 18382 18382 28244 LT ALPHA VANE LT ILLUM IN FLIGHT WILL NOT EXTINGUISH. REMOVED AND REPLACED AOA VANE IAW 34-21-05-4. OPS CHECK GOOD. ( K) 2 L 7 2 4F 4 F RT A16WE E2GL 2007112900198 20071129 00198 WP 2007 11 29 AMTA200700523 1 20071015 A 3350 LIGHT LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE CABIN INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 163AT 1229 FWD GALLEY ESCAPE PATH LIGHTING INOPERATIVE. REMOVED AND REPLACED FWD GALLEY LIGHT STRIP. OPS CHECK NORMAL. (K) 2 L 7 3 4F 4 F A23WE E12EU 2007112900199 20071129 00199 NM 2007 11 29 AMTA200700526 1 20071017 A 3150 WARNING LIGHT BOEING 737 73783N 13844HI NM ILLUMINATED A AMTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 11 301TZ 28239 NR 2 BLEED TRIP OF LIGHT ILL DURING DESCENT FL390 ABLE TO RE-SET. (K) 2 L 7 2 4F RT A16WE 2007112900200 20071129 00200 2007 11 29 AMTA200700527 4 20071017 A 3460 1762000101 COMPUTER BOEING 737 73783N 13844HI NM FLT MANAGE UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 308TZ 28244 LT FMC FAILED. REMOVED AND REPLACED LT FMC IAW REF AMM 34-61-02-4. PERFORMED OPERATIONAL TEST IAW REF AMM 34-61-00-5. OPS CHECK GOOD. (K) 2 L 7 2 4F RT A16WE 2007112900201 20071129 00201 NM 2007 11 29 AMTA200700550 1 20071020 A 3610 32144464 VALVE BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE RT HIGH STAGE UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 11 301TZ 28239 RT BLEED TRIP OFF DURING HIGH ALTITUDE DESCENT RESET, OK. REMOVED AND REPLACED HIGH STAGE VALVE IAW AMM 36-11-06-4. (K ) 2 L 7 2 4F 4 F RT A16WE E2GL 2007112900202 20071129 00202 NM 2007 11 29 AMTA200700551 1 20071019 A 3350 S417N5101009 LENS BOEING 737 73783N 13844HI NM EMERGENCY LIGHTS BROKEN A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 315TZ 28245 L2 DOOR EMERGENCY EXIT SIGN COVER (LENS) BROKEN. REPLACED EMERGENCY LIGHT ASSY, OPS CHECK GOOD. (K) 2 L 7 2 4F RT A16WE 2007112900206 20071129 00206 NM 2007 11 29 Z6WR200700002 1 20071128 A 7830 315W17021 ACOUSTIC PANEL BOEING 777GE9094B BOEING 777 777 UTILUSE NM THRUST REVERSER CRACKED B Z6WR K NONE O OTHER IN INSP/MAINT 1 CE 07 EIDBK 18630 000195 32783 THE 315W1702-1 INNER WALL HAS AN 18 INCH LONG CRACK STARTING 6 INCHES FROM THE AFT END OF THE WALL EXTENDING 18 INCHES F ORWARD AND CENTERED 6 INCHES FROM THE UPPER END. THIS REPAIR IS BEING PERFORMED FOR THE MANUFACTURER WHO DISCOVERED THE DEFECT WITH THEIR AOG TEAM. WE WERE UNABLE TO DETERMINE THAT THEY HAD REPORTED THE DEFECT UNDER THEIR 145 CERTIFICATE S O A REPORT WAS SUBMITTED IN CASE OF OMISSION. 2 L 7 2 4F RT T00001SE 2007113000001 20071130 00001 NM 2007 11 30 AALA20072165 1 20071106 A 2910 HYDRAULIC LINE BOEING 757 757223 1384957 NM RT MLG WW LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 619AA 24577 JFK INFLIGHT T1444/06NOV - LEFT HYDRAULIC QUANTITY INDICATION AND RESERVOIR LIGHT ILLUMINATED DURING CLIMB. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED RIGHT WHEEL WELL DOWNLOCK ACTUATOR PRESSURE AND RETURN HOSES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007113000004 20071130 00004 2007 11 30 AALA20072166 4 20071101 A 2565 BACR13CE2 RELAY BOEING 767 767223 1385123 NM EVAC SLIDE INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 323AA 22324 JFK - LEFT OVERWING SLIDE GREEN SQUIB INOPERATIVE. REPLACED RELAY FOR LEFT OVERWING SLIDE GREEN SQUIB. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007113000005 20071130 00005 NM 2007 11 30 AALA20072171 1 20071108 A 3350 CM1317 LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 323AA 22324 JFK - EMERGENCY LIGHT AT OVERWING ON RIGHT SIDE AFT BULB INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERWING ON RIGHT SIDE AFT POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007113000007 20071130 00007 NM 2007 11 30 AALA20072167 1 20071107 A 5610 WINDSHIELD BOEING 737 737823 13844BZ NM COCKPIT CRACKED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 964AN 30093 DFW INFLIGHT T1181/07NOV - CAPTAINS WINDSHIELD ARCED AND SHATTERED WHEN WINDOW HEAT WAS TURNED ON. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED CAPTAINS WINDSHIELD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007113000008 20071130 00008 NM 2007 11 30 AALA20072168 1 20071108 A 3320 LIGHT BOEING 757 757223 1384957 NM CABIN MISINSTALLED A AALA F A ACTIVATE FIRE EXT. UNSCHED LANDING B A SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE CL CLIMB 1 SW 21 650AA 24608 MIA INFLIGHT T2160/08NOV - FLIGHT ATTENDANTS REPORTED FIRE IN OVERHEAD ROW 11. FLIGHT ATTENDANTS USED HALON EXTINGUISH ER WHICH CREATED SMOKE IN CABIN. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FLUORESCENT L IGHT AT RIGHT SEAT ROW 11. INSTALLED INCORRECTLY WITH PRONGS BENT. ACCOMPLISHED DETAILED INSPECTIONS AND REPLACED LIGH T ASSEMBLY BALLAST AT SEAT ROW 11 AND 12. MAINTENANCE REPORTED NO EVIDENCE OF FIRE. SYSTEM GROUND CHECKED NORMAL OPERA TION. 2 L 7 2 4F RT A2NM 2007113000011 20071130 00011 NM 2007 11 30 2007UALA04378 1 20071025 A 5751 113T710042SP AILERON BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT WING DAMAGED A UALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 29 656UA 63147 25394 RETURN TO GATE DUE TO WING TO WING CONTACT. SUPPLEMENTAL DATA UPDATE RIGHT OUTBOARD AILERON DAMAGED DUE TO RT WING CONT ACT WITH LT WING OF 6672. 2 L 7 2 4F 4 F RT A1NM E24NE 2007113000012 20071130 00012 NM 2007 11 30 2007UALA04470 1 20071029 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 2A FWD LIGHT ASSY. SUPPLEMENTAL DATA UPDATE RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007113000013 20071130 00013 CE 2007 11 30 DJFA2007119 1 20071018 A 3213 STRUT BEECH MU300 400A 1155402 CE MLG OVERSERVICED E DJFA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 EA 23 470LX RK478 ON LANDING CREW REPORTED LOSS OF BRAKING BELOW 40 KTS. ADDITIONALLY THE TR AND SPEEDBRAKES FAILED TO DEPLOY. MAINTENAN CE DISCOVERED THE MAIN STRUTS WERE OVERSERVICED WITH N2 AND WERE NOT ACTUATING THE SQUAT SWITCH. STRUTS WERE PROPERLY S ERVICED AND ALL OPERATIONAL CHECKS WERE SATISFACTORY. 2 H 7 2 4F RT A16SW 2007113000015 20071130 00015 EU 2007 11 30 COEA0719821 1 20070827 A 5310 S53371290202 CREASE BEAM AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. FOUND LEVEL 2 CORROSION LT CREASE BEAM CORD ANGLES UPPER SURFACE. REPLACED CREASE BEAM ANGLE S. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007113000016 20071130 00016 EU 2007 11 30 COEA0720821 1 20070914 A 5230 S52376633202 SKIN AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE CARGO DOOR CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. FOUND LEVEL 2 CORROSION ON PREVIOUS REPAIR TO MAIN CARGO DOOR INNER SKIN. REPLACED INNER SKI N REPAIR. WO NR 72241/ NR 800015. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007113000017 20071130 00017 EU 2007 11 30 COEA0721821 1 20070921 A 5311 FRAME AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. FOUND LEVEL 2 CORROSION, FRAME 36 LT DOUBLER. REMOVED AND REPLACED DOUBLER. WO NR 72242/ NR 200111. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007113000018 20071130 00018 NM 2007 11 30 2007UALA04481 1 20071030 A 2570 CURTAIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE E&E BAY OUT OF POSITION A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 339UA 24243 CREW DESCENDED TO FL240 AND TURNED OFF RT PACK. WHEN OPERATING JUST ON LT PACK, AIRCRAFT WOULD NOT MAINTAIN PRESSURIZAT ION. CABIN ALT WARNING HORN WENT OFF AND DIVERTED. SUPPLEMENTAL DATA UPDATE CAUSE: E/E RAIN CURTAIN HAD BECOME LOOSE AND FELL ON TOP OF AUTO PRESSURE CONTROL CAUSING HEAT AND BLOCKAGE OF AMBIENT AIR. SECURED RAIN CURTAIN AND REPLACED TH E AUTO PRESS CONTROLLER AND REPLACED RT MIX VALVE AS PRECAUTIONARY. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2007113000019 20071130 00019 EU 2007 11 30 COEA0722821 1 20070913 A 5313 S53671200218 STRINGER AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE S16L CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. MAJOR REPAIR, FOUND LEVEL 2 CORROSION STRINGER 16 LT. REMOVED, FABRICATED AND SPLICED IN REP LACED STRINGER SECTIONS. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007113000022 20071130 00022 EU 2007 11 30 COEA0724821 1 20070824 A 5210 S52176205208 INTERCOSTAL AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE PAX DOOR CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. FOUND LEVEL 2 CORROSION, PASSENGER DOOR BEAM NR 5. REMOVED AND REPLACED NEW INTERCOSTAL. (K ) 2 H 7 2 4T 4 T RT A53EU E20NE 2007113000023 20071130 00023 EU 2007 11 30 COEA0725821 1 20070828 A 5315 S53372411240 FLOORBEAM AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. FOUND LEVEL 2 CORROSION. COCKPIT INTERIOR FLOORBEAM 13 HAS NUMEROUS AREAS OF CORROSION FROM S TRINGER 14L TO 14R. REMOVED AND SPLICED IN FABRICATED LT FLOOR BEAM SECTION. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007113000025 20071130 00025 EU 2007 11 30 COEA0714821 1 20070827 A 5310 S53575112214 CREASE BEAM AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE DAMAGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK, MAJOR REPAIR, FOUND TOOLING DAMAGE ONE PLACE ON UPPER SURFACE OF CREASE BEAM WEB. FABRICATED REPLACEMENT CREASE BEAM WEB. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007113000026 20071130 00026 EU 2007 11 30 COEA0715821 1 20070926 A 5310 S53673000207 CREASE BEAM AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE DAMAGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. MAJOR REPAIR, FOUND TOOLING DAMAGE 4 PLACES ON UPPER SURFACE OF CREASE BEAM WEB. FABRICATED REPLACEMENT CREASE BEAM WEB. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007113000028 20071130 00028 EU 2007 11 30 COEA0717821 1 20070828 A 5200 HINGE AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE DOOR CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. FOUND LEVEL 2 CORROSION ON PANEL 531BB HINGE. REPLACED DOOR HINGE. WO NR 72241/ NR 601032. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007113000030 20071130 00030 EU 2007 11 30 BAQA200700037 1 20071023 A 6230 4ZF4649305050 NUT UROCOP EC135 EC135T1 5620026 EU MAST LOOSE E BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 135KY 1239 0444 WHILE TROUBLESHOOTING MAST MOMENT INDICATION PROBLEM, HAD TO REMOVE MAIN ROTOR SHAFT ASSEMBLY, WHILE REMOVING SHAFT FOUN D MAST NUT LOOSE. REMOVED NUT BY HAND. ALL LOCKING HARDWARE WAS FOUND TO BE INTACT AND SECURED AS REQUIRED. UPON FURT HER INSPECTION, FOUND MAST PROPERLY SEATED IAW EC135 MM 62-31-00-4-3 DIMENSION X WAS .590. ATTACHED HOIST TO MAST AND NO TENSION WAS NEEDED TO REMOVE MAST. AWAITING INSTRUCTIONS FROM MFG. 1 G 7 2 3U H88EU 2007113000031 20071130 00031 2007 11 30 2007UALA04661 4 20071112 A 2565 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 565UA 26669 NR 2 RT MED SLIDE BOTTLE PRESSURE READING AT LOW PRESSURE EDGE OF GREEN BAND AFTER CONSTANT FOR MORE THAN 2 HRS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007113000032 20071130 00032 NM 2007 11 30 2007UALA04662 1 20071112 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 585UA 26709 DOOR 1R WON'T DISARM AND SLIDE LT IS ON. 2 L 7 2 4F 4 F RT A2NM E17NE 2007113000035 20071130 00035 NM 2007 11 30 2007UALA04665 1 20071113 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 FOUND SEATS 2A FWD, 44 ABC AND 46 ABC EMERGENCY LIGHTS ARE INOP. RELAMPED, CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007113000036 20071130 00036 NM 2007 11 30 2007UALA04666 1 20071113 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 ZONE B CEILING EMERGENCY LIGHT IS INOP (2 EA). RELAMPED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007113000039 20071130 00039 NM 2007 11 30 2007UALA04669 1 20071112 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INTERMITTENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 181UA 25278 DOOR 1L EMERGENCY EXIT LIGHT INTERMITTENT. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007113000041 20071130 00041 NM 2007 11 30 2007UALA04671 1 20071112 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN MISSING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 179UA 25158 FOUND SEAT 4J IS MISSING THE EMERGENCY LIGHT STRIP. REPLACED DAMAGED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007113000045 20071130 00045 NM 2007 11 30 2007UALA04676 1 20071113 A 5512 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZ STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 301UA 23642 RT HORIZ STAB LOWER SURFACE SKIN CRACKED AT STAB STA 125, JUST FWD OF REAR SPAR. REMOVED CRACK. FABRICATED 2 ACCESS HOL ES AND COVERS TO FACILITATE REPAIR. FABRICATED AND INSTALLED EXTERNAL DOUBLER ON LOWER STAB SKIN NEAR REAR SPAR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007113000047 20071130 00047 NM 2007 11 30 2007UALA04678 1 20071113 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 L2 DOOR UPPER HINGE CUT OUT ROUTED BEYOND LIMITS. NDT CONFIRMED CRACK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007113000049 20071130 00049 NM 2007 11 30 2007UALA04680 1 20071113 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 DOOR 2L NEEDS PREP DOUBLER AT UPPER HINGE CUT OUT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007113000050 20071130 00050 NM 2007 11 30 2007UALA04681 1 20071113 A 2611 SMOKE DETECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LAVATORY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 505UA 24626 FWD LAV SMOKE DETECTOR INOP. GREEN LED LIGHT NOT ON. 2 L 7 2 4F 4 F RT A2NM E17NE 2007113000051 20071130 00051 NM 2007 11 30 2007UALA04682 1 20071114 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 UPPER DECK EMERGENCY EXIT CEILING LIGHT AT ROW 13 AND EMERGENCY EXIT STAIRS CEILING LIGHT LEADING TO UPPER DECK ARE INOP ERATIVE. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007113000052 20071130 00052 NM 2007 11 30 2007UALA04683 1 20071114 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT CEILING LIGHTS INOP. ALL IN FIRST CLASS AND FROM ROW 6 THRU 8 LEFT AND RIGHT. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007113000053 20071130 00053 NM 2007 11 30 2007UALA04684 1 20071114 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT EEL LIGHTS INOP FROM ROWS 32 THRU 34 LEFT AND AT ROW 49 LEFT. RESECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007113000054 20071130 00054 NM 2007 11 30 2007UALA04687 1 20071114 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 L2 DOOR HANDLE BOX CRACKED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007113000055 20071130 00055 NM 2007 11 30 2007UALA04688 1 20071114 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 301UA 23642 FWD CARGO DOOR, AFT FRAME LWR OF CUTOUT, HAS TEMP REPAIR PER EVA. SUPPLEMENTAL DATA UPDATE:REPLACED FWD CARGO DOOR AFT FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2007113000056 20071130 00056 CE 2007 11 30 ZED2007F00000 1 20071011 A 2612 FIRE WARNING LEAR 35 35A 5170602 CE GARRTT TFE731 TFE7312 01518 WP RT ENGINE FALSE ACTIVATION A ZEDA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 11 394PA 462 89267 STILL TROUBLESHOOTING, DISCREPANCY WRITTEN UP BY PILOT, RT ENGINE FIRE LIGHT ILLUMINATED DURING FLIGHT. TEMPS/PRESSURES NORMAL. LIGHT EXTINGUISHED AFTER REDUCING POWER 10 PERCENT. CHECKED ENGINE PARAMETERS, ALL NORMAL, DIMMED COCKPIT LIG HTING AND LOOKED AT RT WING FROM REFLECTION, REDUCED POWER LIGHT EXTINGUISHED 10 PERCENT. (K) 2 L 7 2 4F 4 F A10CE E6WE 2007113000058 20071130 00058 NM 2007 11 30 2007UALA04691 1 20071114 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 529UA 25019 EMERGENCY EXIT SIGN LIGHT OUT AT 15A OVERWING LOCATION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007113000059 20071130 00059 NM 2007 11 30 2007UALA04692 1 20071114 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 541UA 25253 MULTIPLE EEL STRIP LIGHTS OUT. RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007113000063 20071130 00063 NM 2007 11 30 2007UALA04696 1 20071114 A 3350 LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 778UA 26940 FOUND SEAT 2F AFT EMERGENCY LIGHT OUT. REPLACED LAMP ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007113000065 20071130 00065 NE 2007 11 30 AALA20072175 2 20071109 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LEFT BIRD INGESTION A AALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 21 7519A 49896 725475 ORD INFLIGHT T405/09NOV - AIRCRAFT EXPERIENCED NUMBER ONE ENGINE STALLS AT APPROXIMATELY 2000 FEET DURING CLIMB. ENGINE STALLS STOPPED WHEN NUMBER ONE ENGINE AT IDLE. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. FOUND EVIDENCE OF BIRD ST RIKE. REPLACED ENGINE ON 10 NOV 2007 AT ORD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007113000070 20071130 00070 NM 2007 11 30 AALA20072180 1 20071110 A 3350 LIGHT BOEING 757 757223 1384957 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 172AJ 32400 DFW - AFT EXTERIOR EMERGENCY LIGHT AT LEFT AFT ENTRY DOOR INOPERATIVE. REPLACED LAMP FOR AFT EXTERIOR EMERGENCY LIGHT A T LEFT AFT ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007113000071 20071130 00071 NM 2007 11 30 AALA20072181 1 20071110 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 172AJ 32400 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 27C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROW 27C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007113000072 20071130 00072 SO 2007 11 30 LR7A07128 1 20071110 A 3297 WIRE HARNESS LKHEED 382 382G 526414U SO BRAKE SYSTEM CHAFED A LR7A O OTHER O OTHER TX TAXI/GRND HDL 1 AL 03 406LC 681 4676 FLIGHT CREW REPORTED NORMAL BRAKE SYSTEM FAILURE ON GROUND TAXI PANC. MAINTENANCE FOUND LT AFT ANTI-SKID TRANSDUCER HAR NESS WIRE CHAFED AND SHORTED TO GROUND. REPAIRED IAW SMP581 32-42. 2 H 7 4 4T A1SO 2007113000074 20071130 00074 NM 2007 11 30 HALA0700487 1 20071110 A 7160 COWLING BOEING 767 7673G5 1385126 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE DENTED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM - NR 2 ENG INLET COWL DENTED AT APPROX 5:30 POSITION AS VIEWED LOOKING FWD DENT MEASURE APPROX: 28"L, 2.5"W, 0.042" DEPTH. REPAIRED PER M105 FILE NR 585114 AND TRANSFERED TO DPM P98977. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007113000075 20071130 00075 NM 2007 11 30 HALA0700488 1 20071116 A 3350 LIGHT BOEING 767 76733A 1385209 NM CABIN INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 591HA 33423 EMERGENCY FLOOR TRACK LIGHTING INOP FROM 20HJ-29HJ. REPLACED CONNECTOR STRIP AT 29HJ, OPS CK NML. 2 L 7 2 4F RT A1NM 2007113000077 20071130 00077 EU 2007 11 30 SIMA200731902 1 20071114 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 317AE 340B317 CREW REPORTED THAT 5 OF 6 AFT FLOOR EMERGENCY LIGHTS NOT WORKING. REMOVED AND REPLACED NR 5 EMERGENCY POWER SUPPLY IAW SAAB 340B AMM 33-50-10. PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTING SYSTEM IAW SAAB 340 AMM 33-50-10. AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007113000079 20071130 00079 2007 11 30 SIMA200732301 4 20071118 A 3416 C16221GC03 ALTIMETER EMB 135 EMB135KL 3260302 SO COCKPIT MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 803AE 145483 ABORTED TAKEOFF, DURING TAKEOFF ROLL AT 50 KNOTS THE STAND BY ALTIMETER INDICATOR WENT TO CAGE. REPLACED STAND BY ATT INDICATOR AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007113000081 20071130 00081 2007 11 30 BB07092 4 20071115 A 2565 101630305 SLIDE BOEING 767 7672B7 1385107 NM LT OVERWING DEPLOYED A USAA K NONE Z SIGNIFICANT FAILURE REPORT IN INSP/MAINT 1 EA 19 252AU 29355 2697 24765 MAINTENANCE CAME ONBOARD AIRCRAFT AND FOUND LEFT OVERWING ESCAPE SLIDE PARTIALLY DEPLOYED. REPLACED ESCAPE SLIDE. 2 L 7 2 4F RT A1NM 2007113000082 20071130 00082 NM 2007 11 30 BB07093 1 20071117 A 3232 ACTUATOR BOEING 757 7572S7 1384962 NM LT MLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 901AW 23321 FLIGHT 146, PHX-LIH: AFTER TAKEOFF AND GEAR SELECTED TO 'UP' POSITION, RECEIVED GEAR DISAGREE LIGHT. SELECTED GEAR DOWN AND RECEIVED DOWN AND LOCKED INDICATIONS. FLIGHT RETURNED TO PHX. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR RET RACTION ACTUATOR. 2 L 7 2 4F RT A2NM 2007113000084 20071130 00084 NM 2007 11 30 SB07100 1 20071117 A 3397 CONNECTOR BOEING 737 737401 1384701 NM CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 425US 23992 DFW - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 12 AND 16, LEFT SIDE, INOPERATIVE. MAINTENANCE FOUND THE CONNECTOR DISCONNECTED AT SEAT 16. RECONNECTED CONNECTOR AT SEAT 12. MAINTENANCE FOUND THE WIRE DISCONNECTED. RECONNE CTED WIRE/BUTT SPLICE PER SWP CHAPTER 20. OPERATIONAL CHECK OF LIGHTS GOOD. 2 L 7 2 4F RT A16WE 2007113000085 20071130 00085 NM 2007 11 30 DHLA200700064 1 20071118 A 3350 BATTERY BOEING 727 727223 1384074 NM CABIN DISCHARGED A DHLA K NONE L NO TEST UK UNKNOWN 1 GL 05 749DH 22013 EMERGENCY EXIT LIGHTS ILLUMINATE THEN IMMEDIATELY EXTINGUISH WHEN TURNED ON AND DURING STAND BY POWER CHECK. REMOVED AN D REPLACED BOTH EMERGENCY EXIT LIGHT BATTERIES, OPS CHECK GOOD PER MM 33-50-01 P/N MISC062 QTY 4. 2 L 7 3 4F A3WE 2007113000086 20071130 00086 NM 2007 11 30 DHLA200700065 1 20071118 A 2560 PANEL BOEING 727 727223 1384074 NM COCKPIT DEFECTIVE A DHLA O OTHER O OTHER NR NOT REPORTED 1 GL 05 749DH 22013 ESCAPE ROPE ACCESS PANEL ON CAPT SIDE WILL NOT CLOSE. SECURED ESCAPE ROPE PANEL ON CAPT SIDE, OPS CHECK GOOD PER MM 25- 60-00. 2 L 7 3 4F A3WE 2007113000088 20071130 00088 EU 2007 11 30 MALA070182 1 20071016 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 416XJ 340B416 SEVERAL DENTS WERE FOUND IN THE RT FUSELAGE SKIN, IN THE ICE GUARD AREA LOCATED FROM STA 313 AND STA 321, BETWEEN STRING ERS SL1615 AND SL 1622. DOUBLER/TRIPLER INSTALLED IAW EO NR S53494. 2 L 7 2 4T RT A52EU 2007113000089 20071130 00089 NM 2007 11 30 070179 1 20071109 A 3350 BATTERY PACK DOUG MD80 MD83 3023681 NM CABIN DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 892GA 49826 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT 2007113000090 20071130 00090 WP 2007 11 30 070177 1 20071111 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 862GA 49556 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007113000092 20071130 00092 NM 2007 11 30 070178 1 20071109 A 3350 BATTERY PACK DOUG MD80 MD83 3023681 NM CABIN DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 892GA 49826 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT 2007113000094 20071130 00094 SO 2007 11 30 GUUA10220701 1 20071022 A 3260 20700 SPRING EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE MLG INOPERATIVE A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 29 268AS 120202 FLIGHT:5401, DURING APPROACH WITH LANDING GEAR SELECTED DOWN, NOSE GEAR HAD NO GREEN LIGHTS. BOTH MAIN GEARS SHOWED DOW N AND LOCKED. REPLACED NOSE GEAR LOCKING SPRING . OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2007113000096 20071130 00096 NM 2007 11 30 QXEA200701728 1 20071117 A 3040 M39016105L RELAY DHAV DHC8 DHC8202 2809007 NM WINDSHIELD HEAT FAILED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 347PH 480 BOI-ON FLIGHT 2192, RETURNED TO GATE. RIGHT WINDSHIELD HOT CAUTION ILLUMINATED VERY SOON AFTER SELECTING WINDSHIELD HEA T TO NORM, OAT 10 C. MAINTENANCE REMOVED AND REPLACED K6 AND K8 RELAYS. PERFORMED OPERATIONAL TEST OF WINDSHIELD HEAT SYSTEM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007113000097 20071130 00097 EU 2007 11 30 TRBA2007101 1 20071119 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU CABIN FAILED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 270AT 270 EMERGENCY LIGHTS FROM CABIN STAY ON ALL THE TIME (HALF OF THEM). REPLACED AND TESTED EMERGENCY BATTERY POWER SUPPLY 73W L AS PER MM 33-51-21 AND FOUND WORKING PROPERLY. 2 H 7 2 4T RT A53EU 2007113000100 20071130 00100 NM 2007 11 30 HALA0700492 1 20071117 A 4990 OIL SYSTEM BOEING 767 7673CB 1385187 NM APU LOW A HALA K NONE O OTHER TX TAXI/GRND HDL 1 WP 13 588HA 33466 ETOPS SIGNIFICANT SYSTEM, UPON ARRIVAL, APU WOULD NOT START, OIL QUANT .75 QT. SERVICED APU OIL QTY (1 PINT) BITE CK. NO DEFECTS NOTED. LK CK OK. OPS CK GOOD. 2 L 7 2 4F RT A1NM 2007113000101 20071130 00101 WP 2007 11 30 07FDEA04417 1 20071001 A 5754 NRB6023 DOUBLER DOUG DC10 DC1010F 3022111 WP L/E SLAT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 RT WING NR 1 SLAT EXTERNAL SKIN EXISTING DOUBLER. REPAIRED AREA IAW SRM 57-10-00 FIG 84 VOL I. 2 L 7 3 4F A22WE 2007113000102 20071130 00102 NM 2007 11 30 07FDEA04824 1 20071117 A 5350 655850421 FRAME BOEING 727 727225 1384077 NM FAIRING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 BODY FAIRING FRAME LOCATED BETWEEN PANELS 3358 AND 3458, FORWARD END HAS CORROSION. REPLACED FAIRING FRAME, REF BOEING DWG 65-59318 AND SRM 51-30-2, TREATED AND PRIMED REF MM 51-20-021-7, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2007113000104 20071130 00104 NM 2007 11 30 07FDEA04826 1 20071118 A 5753 HINGE BRACKET DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 RIGHT WING OUTBOARD FLAP OUTBOARD HINGE BRACKET OUTBOARD NR 3 BOLT HOLE FOUND CORROSION. CORROSION REMOVED AS PER BOEIN G SOPM 20-11-02, REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-117054. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007113000106 20071130 00106 NM 2007 11 30 07FDEA04828 1 20071118 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 MAIN DECK CARGO COMPARTMENT AT ABOUT STA 1280 TO 1321 RBL 8 SEAT TRACK FLOOR PANEL SUPPORT FLANGE FOUND CORRODED. REPA IRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007113000107 20071130 00107 NM 2007 11 30 07FDEA04829 1 20071118 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 MAIN DECK CARGO COMPARTMENT, AFTER FLOOR PANEL REMOVAL SEAT TRACK FLOOR SUPPORT FLANGE AT STA 1741 TO 1821 RBL 47 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100. 2 L 7 3 4F RT A22WE 2007113000108 20071130 00108 EU 2007 11 30 07FDEA04830 1 20071118 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT PIT STRINGER 52R CORRODED AT FRAME 58 TO 59. REMOVED CORROSION PER SRM 51-74-10. CHECKED LIMITS ORIG MATERIAL .110 . REMAINING MATERIAL .097. REMOVED .013 FOUND TO OUT OF LIMITS PER SRM 53-10-00. REMOVED DAMAGED STRINGER AND REPLAC ED WITH NEW REPAIR PER SRM 53-10-14. JOGGLED NEW STRINGER PER SRM 51-26-20. LOCATED AND DRILLED PER SRM 51-40-44. AL ODINED PRIMED AND PAINTED PER SRM 51-23-10-AND 51-21-10. 2 L 7 2 4F RT A35EU 2007113000109 20071130 00109 EU 2007 11 30 07FDEA04831 1 20071118 A 5347 R538D104820200 ADAPTER AIRBUS 310 A310203 3930313 EU SEAT TRACK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 MAIN CABIN AT FRAME 45(X2506) LBL-36 (Y-910) SEAT TRACK ADAPTER IS CRACKED. REMOVED AND REPLACED ADAPTOR TRACK IAW A310 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007113000112 20071130 00112 EU 2007 11 30 07FDEA04833 1 20071118 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT PIT STRINGER 45R , FRAME 58 HAS CORROSION ON STRINGER. REMOVED CORROSION IAW A310 SRM 51-74-10. CORROSION OUT OF L IMITS PER A310 SRM 53-10-00 PG 106. REMOVED WEB FR54.3 TO 58 STRINGER 45R FOR ACCESS PER A310 51- 40-21 PG 15. CUT O UT DAMAGED SECTION OF STRINGER 45R, FABBED NEW SECTION OF STRINGER 45R, FABBED PLICE DOUBLER PER A310 SRM 53-10-14 FIG 201, INSTALLED NEW SECTION OF STRINGER 45R SPLICE AND WEB FRAME 54.3 TO FRAME 58 PER A310 SRM 53-10-14 FIG 201, A310 SRM 51-40-21 PAGE 36 AND A310 SRM 51-40-21 PAGE 9, STATION 3090 TO 3143. 2 L 7 2 4F RT A35EU 2007113000113 20071130 00113 EU 2007 11 30 07FDEA04834 1 20071118 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FOUND AFT PIT STRINGER 47R AT FRAME 58, CORRODED. REMOVED CORROSION IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW S RM 53-10-00. CUT OUT DAMAGED SECTION IAW SRM 53-14-00 FIG 201. LOCATED AND DRILLED NEW SECTION OF STRINGER IAW SRM 51-40 -44. FABBED COUPLING IAW SRM 53-10-14. ALODINED, PRIMED AND PAINTED IAW SRM 51-21-10, 51-23-10. INSTALLED REPAIR IAW SRM 53-14-10 FIG 201. 2 L 7 2 4F RT A35EU 2007113000114 20071130 00114 CE 2007 11 30 GUUA10200701 1 20071020 A 3243 903800133 MASTER CYLINDER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT BRAKES MALFUNCTIONED A GUUA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 29 81533 UE137 FLIGHT:9250, AFTER LANDING DISCOVERED RT BRAKE NOT HOLDING. REPLACED CAPTAIN RT BRAKE MASTER CYLINDER. OPERATIONAL CHE CK GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2007113000115 20071130 00115 SO 2007 11 30 GUUA10230701 1 20071023 A 3230 12038594001 CONTROL BOX EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE MLG MALFUNCTIONED A GUUA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 29 282AS 120226 FLIGHT: 9273, AFTER DEPARTURE FROM FPO LANDING GEAR WOULD NOT RETRACT UNTIL RECYCLED. REPLACED LANDING GEAR CONTROL BOX . OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 2007113000117 20071130 00117 CE 2007 11 30 AMWA223904 1 20071016 A 5330 12943006413 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A6 52043 EA BS 213-243 CORRODED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 161YV 21146 UE161 SURFACE TYPE CORROSION FOUND ON INTERIOR SURFACE OF FUSELAGE SKIN IN AIRCRAFT BELLY. FS213.25, 228.25, AND 243.25 ALONG STRINGER 16. INSPECTED, CLEANED AND REPAIRED IAW DER SUPPLIED REPAIR DATA. 2 L 7 2 4T 3 T RT A24CE E4EA 2007113000118 20071130 00118 EA 2007 11 30 N6WA0071003 1 20071025 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE EMERGENCY LIGHTS BURNED OUT A N6WA K NONE L NO TEST IN INSP/MAINT 1 CE 03 151GJ 10216 LT INTERIOR LOWER OVERWING EMERGENCY EXIT SIGN HAS ONE LAMP INOP. REPLACED BULB. 2 L 7 2 4F 4 F RT A21EA E00063EN 2007113000119 20071130 00119 EU 2007 11 30 07FDEA04835 1 20071118 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT PIT STRINGER 48R CORRODED AT FRAME 58. REMOVED CORROSION IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW SRM 53-1 0-00. CUTOUT DAMAGE IAW SRM 53-10-14. LOCATED AND DRILLED NEW STRINGER SECTION IAW SRM 51-40-44. FABBED COUPLING IAW 53-10-14. ALODINED IAW SRM 51-21-10. PRIMED AND PAINTED IAW SRM 51-23-10. INSTALLED REPAIR IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007113000120 20071130 00120 SO 2007 11 30 GUUA10140701 1 20071014 A 3150 WARNING LIGHT EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE ANTI SKID SYS FALSE ACTIVATION A GUUA O OTHER J WARNING INDICATION LD LANDING 1 SO 29 285AS 120265 FLIGHT:253, DURING LANDING ROLL RT ANTI-SKID ANNUNCIATOR ILLUMINATED AND A TEMPORARY LOSS OF BRAKING. INSPECTED ANTI S KID SYSTEM ON GROUND NO DEFECTS NOTED. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2007113000121 20071130 00121 EU 2007 11 30 07FDEA04836 1 20071118 A 5330 SKIN AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FUSELAGE SKIN/INTERIOR SURFACE BETWEEN FRAME 78 AND 79 AT STRINGER 50R HAS CORROSION. REMOVED CORROSION ON INTERNAL DO UBLER IAWA310 SRM 51-74-10 FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-10-00 REPLACED INTERNAL DOUBLER FROM FRAME 78-80 ST RINGER 45R IAW A310 SRM 51-40-21, 51-26-00, 51-27-00, 51-40-44, 51-21-10. REMOVED AND REINSTALLED STRINGER 45R FROM FRAM E 78 TO 80, STRINGER 47AND 48R FROM FRAME 79-80 STRINGER 50R FROM FRAME 78-80, SHEAR TIE ON FRAME 79 FROM FRAME 50R TO 45R, PAN FROM FRAME 78 TO 79 STRINGER 45R TO 50R, DRAIN MAST IAW A310 SRM 51-40-21, 51-21-10, WDM30-71-02, AMM 30-71-1 1-4 TO FOM, 2 L 7 2 4F RT A35EU 2007113000123 20071130 00123 CE 2007 11 30 DJFA2007121 1 20071021 A 2170 COALESCER BAG BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE A/C PACKS DIRTY E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 478LX RK387 CREW REPORTED ODOR OF SMOKE IN THE LAV AREA WITH WING HEAT ON IN ICING CONDITIONS. ODOR DISAPATED AFTER WING A/I WAS SH UTOFF. MAINTENANCE DISCOVERED THE COALESCER SOCK DIRTY. THE COALESCER SOCK WAS REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007113000124 20071130 00124 NE 2007 11 30 DJFA2007122 2 20071023 A 7321 COMPUTER BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE OUT OF ADJUST E DJFA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 EA 23 476LX RK376 PCEJA0531 CREW REPORTED ENGINE ROLL BACK OF 5 PERCENT N1 ON THE RT ENGINE FOLLOWED BY A FLUXUATION OF 3-4 PERCENT. ENGINE STABILI ZED AFTER ENGINE HEAT WAS TURNED ON. MAINTENANCE ADJUSTED THE EFC AUTHORITY. 2 H 7 2 4F 4 F RT A16SW E25EA 2007113000128 20071130 00128 EU 2007 11 30 07FDEA04838 1 20071118 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT PIT STRINGER 49R CORRODED BETWEEN FRAME 60 AND 62. FABRICATED REPAIR STRINGER SECTION AND COUPLING, AND REMOVED AND REPLACED CORRODED STRINGER SECTION IAW A310-200 SRM 53-10-14 PG 203 / 204, & SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007113000131 20071130 00131 WP 2007 11 30 07FDEA04843 1 20071119 A 5320 S4929251 CHANNEL DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK) FOUND IN LOWER FWD CARGO LIGHT CORROSION ON CHANNEL FROM STA 759 TO STA 879 X= 59. REMOVED CORROSION FOR SRM 51-21-01 VOL 2. PERFORMED CHECK LIMIT THICKNESS IS OUT LIMITS. RE PLACED CHANNEL FOR SRM 53-70-00 FIG 7 VOL I. 2 L 7 3 4F A22WE 2007112800181 20071128 00181 SO 2007 11 28 C2XA07SH095 1 20071122 A 5330 14540330403 PANEL EMB 145 EMB145LR 3260212 SO FUSELAGE DELAMINATED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 131 SHV - DURING C-CHECK PANEL 191 RIGHT FWD UPPER SIDE HAS AN AREA OF DELAMINATION ON INTERNAL AND EXTERNAL SIDE AND LEFT F WD EDGE FOUND TO HAVE COMPOSITE DAMAGE. MAINTENANCE REPAIRED RIGHT FWD UPPER SIDE AND LEFT FWD EDGE IAW EC5350-01101. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2007112800187 20071128 00187 NM 2007 11 28 USAA920071179 1 20071120 A 5720 69620146 STIFFENER BOEING 737 7373S3 1384711 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 PHX - MAJOR REPAIR - CRACKED CENTER WING REAR SPAR VERTICAL STIFFENER, BS 663.75, RBL 6.15. REPAIRED CENTER WING REAR S PAR VERTICAL STIFFENER, BS 663.75, RBL 6.15 IAW USAIRWAYS TYPICAL REPAIR 57-10-03B AND EA 120412. 2 L 7 2 4F RT A16WE 2007112800188 20071128 00188 NM 2007 11 28 USAA920071185 1 20071122 A 5330 6552988 SKIN BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 PHX - MAJOR REPAIR - CRACKED FUSELAGE SKIN, BS 927, S23L. REPAIRED FUSELAGE SKIN, BS 927, S23L IAW USAIRWAYS EA 120405. 2 L 7 2 4F RT A16WE 2007112800189 20071128 00189 NM 2007 11 28 USAA920071186 1 20071122 A 5330 6552988 SKIN BOEING 737 7373B7 1384580 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 532AU 24479 PIT - MAJOR REPAIR - CRACKED FUSELAGE SKIN, BS 947.5, S10L AT THE L2 DOOR UPPER HINGE CUTOUT. REPAIRED FUSELAGE SKIN, B S 947.5, S10L AT THE L2 DOOR UPPER HINGE CUTOUT IAW B737 SRM 53-60-01-2R5. 2 L 7 2 4F RT A16WE 2007112800197 20071128 00197 NM 2007 11 28 USAA920071195 1 20071116 A 5340 6935352U14 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CRACKED STRINGER TIE CLIP, BS 578, S4L. REPLACED STRINGER TIE CLIP, BS 578, S4L IAW B73 7 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007112800199 20071128 00199 NM 2007 11 28 USAA920071197 1 20071116 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CRACKED STRINGER TIE CLIP, BS 616, S4R. REPLACED STRINGER TIE CLIP, BS 616, S4R IAW B73 7 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007112800202 20071128 00202 NM 2007 11 28 USAA920071200 1 20071116 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CRACKED STRINGER TIE CLIP, BS 639, S4L. REPLACED STRINGER TIE CLIP, BS 639, S4L IAW B73 7 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007112900002 20071129 00002 CE 2007 11 29 SFO57SF 1 20071116 A 3246 31418 WHEEL CESSNA 500 550 2076604 CE NLG BROKEN E SFOA O OTHER O OTHER LD LANDING 1 EA 23 57SF 63 63 5500402 ON LANDING, ENCOUNTERED SEVERE CROSSWIND GUSTS CAUSING ACFT TO YAW ON TOUCHDOWN. AFTER A SUCCESSFUL LANDING, NOTED A SE VERE SWAYING OF THE NLG & VIBRATION FELT IN RUDDER PEDALS. ACFT STOPPED & DISCOVERED THE NLG TIRE BLOWN & RIMS BROKEN O FF. AT THE HANGER NOTED A SMALL DENT/SCRATCH ON EACH INBOARD HEATED LEADING EDGE. BOTH ENGINES WERE INSPECTED. RT ENG INE FOUND TO HAVE DAMAGE TO ROUGHLY HALF OF THE FAN BLADES FROM PIECES OF WHEEL RIM ENTERED. LT ENGINE NO DAMAGE. RT E NGINE DAMAGE LIMITED TO FAN BLADES, FAN SHROUD, FAN STATOR, AND ITT SENSOR. NO DAMAGE FOUND IN THE CORE. SOME SHEET ME TAL DAMAGE NOTED ON AFT EDGE OF INLET. FURTHER INSPECTION MADE ON REMAINDER OF ACFT & MINOR DAMAGE NOTED ON BOTH HEATED 1 L 7 2 4F A22CE 2007112900010 20071129 00010 EA 2007 11 29 COMA0760644 1 20071114 A 2752 852D10021 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA LT TE FLAP FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 443CA 1676 7539 FLIGHT 5089 - FLAPS FAILED AT 8 DEGREES ON APPROACH INTO MSP. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED LEFT I/B FL AP O/B ACTUATOR. 2 L 7 2 4F RT A21EA 2007112900011 20071129 00011 EA 2007 11 29 COMA0760645 1 20071115 A 5240 051940 SEAL CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR TORN A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 963CA 7127 FLIGHT 5326 - LOUD NOISE AT ALTITUDE FROM BOTTOM OF SERVICE DOOR EN ROUTE FROM OKC TO CVG. AIRCRAFT DIVERTED TO STL AND LANDED SAFELY. FOUND PAX DOOR SEAL TORN. REMOVED AND REPLACED PAX DOOR SEAL. 2 L 7 2 4F RT A21EA 2007112900012 20071129 00012 EA 2007 11 29 COMA0760646 1 20071115 A 5241 CD1398503 REDUCER CNDAIR CL600 CL6002B19 1900309 EA GALLEY DOOR CLOGGED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 963CA 7127 FLIGHT 5326 - LOUD NOISE AT ALTITUDE FROM BOTTOM OF SERVICE DOOR EN ROUTE FROM OKC TO CVG. AIRCRAFT DIVERTED TO STL AND LANDED SAFELY. FOUND GALLEY DRAIN NOISE REDUCER CLOGGED. REMOVED AND REPLACED NOISE REDUCER. 2 L 7 2 4F RT A21EA 2007112900039 20071129 00039 NM 2007 11 29 2007UALA04758 1 20071119 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE AFT CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 534UA 25129 AFT CABIN EEL LIGHT INOPERATIVE. REPLACE LAMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007112900047 20071129 00047 NM 2007 11 29 2007UALA04766 1 20071117 A 3213 CYLINDER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LT MLG STRUT CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 826UA 989 LEFT MAIN LANDING GEAR, OUTER CYLINDER, FOUND CORROSION ON INNER SURFACE. REPLACED THE LT GEAR AND SENT UNIT TO SHOP FO R COMPLETE OVERHAUL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112900069 20071129 00069 SO 2007 11 29 C2XA07TY071 1 20071118 A 3350 276005 FUSE EMB 145 EMB145XR 3260214 SO POWER SUPPLY FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17138 145727 EMERGENCY LIGHTS OVERWING INOP. REMOVED AND REPLACED FUSES IN NR 4 POWER SUPPLY IAW EMB 145 VCMM 33-21-70. OPS CHECKED GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT 2007112900070 20071129 00070 EU 2007 11 29 TRAX200701761 1 20071029 A 5714 FAIRING AEROSP ATR72 ATR72 EU WING BOX CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 RIGHT WING BOX FAIRING PLATE CRACKED AT FR 28A. 2 H 7 2 4T RT 2007112900073 20071129 00073 EA 2007 11 29 TRAX200701764 1 20071121 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 FS 280 AFT ANGLE CRACKED O/B OF LBL 9 AND RBL 9. CUT AWAY DAMAGED SECTION OF FS280 AFT ANGLE IAW REO 601R-53-11-136. P ERFORMED LPI PER NDTM 51-20-08 ON LT & RT CUT LINES TO ENSURE DAMAGE REMOVAL IAW REO 601R-53-11-136 (NO DEFECTS NOTED AT THIS TIME). FABRICATED REPAIR FILLER ANGLE FROM P/N 600-34017-595 AND SPLICE ANGLE IAW REO 601R-53-11-136. OK TO ALODIN E PRIME AND TOPCOAT. APPLIED FINISH IAW CRJ 200 SRM 51-21-16. OK TO INSTALL. INSTALLED REPAIR FILLER ANGLE, AND SPLICE ANGLE IAW REO 601R-53-11-136. OK TO TOPCOAT FASTENERS . APPLIED TOPCOAT TO FASTENERS AND REPAIRED AREA IAW CRJ 200 SRM 5 1-25-16. COMPILED WITH EC/TC EO 600-53-91. 2 L 7 2 4F RT A21EA 2007112900101 20071129 00101 NM 2007 11 29 SWAA075816 1 20071124 A 3350 285A178010 CIRCUIT CARD BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 467WN 33830 EMERGENCY EXIT LIGHTS ILLUMINATED IN THE ARMED POSITION. REMOVED AND REPLACED PC CARD AT AFT F/A PANEL PER MM. 2 L 7 2 4F RT A16WE 2007112900109 20071129 00109 NM 2007 11 29 SWAA075822 1 20071121 A 3350 1619 LAMP BOEING 737 7375H4 138449D NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007112900111 20071129 00111 NM 2007 11 29 SWAA075792 1 20071116 A 5610 5893543139 WINDOW BOEING 737 7375H4 138449D NM COCKPIT FAILED A SWAA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SW 29 528SW 26570 DIVERSION - FLIGHT DECK L1 WINDOW SHATTERED AND ARCED. REMOVED AND REPLACED L1 WINDOW PER MM. 2 L 7 2 4F RT A16WE 2007112900113 20071129 00113 NM 2007 11 29 SWAA075824 1 20071121 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007112900125 20071129 00125 NM 2007 11 29 07FDEA04793 1 20071115 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1821 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 MAIN DECK CARGO COMPARTMENT AT ABOUT STA 1821 RBL 75 SEAT TRACK FOUND CORROSION. REPAIRED BY REPLACEMENT AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007112900133 20071129 00133 NM 2007 11 29 BB07091 1 20071115 A 3397 WIRE HARNESS BOEING 757 7572S7 1384962 NM EMERGENCY LIGHTS UNKNOWN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 902AW 23322 MAINTENANCE FOUND FLOOR LEVEL LIGHT AT ROW 33L INOPERATIVE. REPLACED WIRE HARNESS TO LIGHT ASSEMBLY. NO FURTHER FAULTS . 2 L 7 2 4F RT A2NM 2007112900134 20071129 00134 2007 11 29 07FDEA04800 4 20071116 A 3414 PITOT TUBE AIRBUS 300 A300F4605R 3930327 EU CLOGGED A FDEA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 SO 25 679FE 793 ON TAKEOFF ROLL AT 80KNOT CALL F/O AIRSPEED INDICATOR SHOWED 40KTS, REF MM 34-11-15-6/34-10-00-5. INSPECTED F/O'S PITOT TUBE. DISCOVERED SLIGHT BLOCKAGE. CLEANED PITOT TUBE, PERFORMED AIRSPEED ADJUSTMENT AND TEST. TESTED BOTH CAPT'S AND F/O'S INDICATION OF 200KTS WITH TEST SET. BOTH INDICATIONS CHECK GOOD. ACFT OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2007112900137 20071129 00137 NM 2007 11 29 07FDEA04803 1 20071116 A 5753 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 RIGHT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FORWARD OUTBOARD NR 3 BOLT HOLE, FOUND CORROSION. REMOVED AND RE PLACED AS PER AMM 27-50-30-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007112900154 20071129 00154 EU 2007 11 29 07FDEA04820 1 20071116 A 5320 A53974259200 FLOOR SUPPORT AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 BULK CARGO PIT FLOOR SUPPORT (LONGITUDINAL PROFILE) CORRODED, FR 60 TO FR 65 ( X3514 TO X3567), BL 4L (Y100). REMOVED A ND REPLACED CORRODED FLOOR SUPPORT SECTION IAW A310-200 SRM 51-40-21 PAR 9, & SRM 51-40-44 PG 9 2 L 7 2 4F RT A35EU 2007112900172 20071129 00172 EU 2007 11 29 USAA920071153 1 20071115 A 2611 PPA120100 SMOKE DETECTOR AIRBUS A321 A321211 3930370 EU LAVATORY DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 161UW 14436 179 1403 FLT NR 1521 - CLT-DEN - EMERGENCY EQUIPMENT, SMOKE LAV + CRG DET FAULT DURING PREFLIGHT. MAINTENANCE REPLACED FORWARD L AV SMOKE DETECTOR. BITE CHECK SMOKE DETECTOR CONTROL UNIT. SYSTEM OPS NORMAL. MESSAGE CLEARED. 2 L 7 2 4F RT A28NM 2007112900180 20071129 00180 NM 2007 11 29 USAA920071157 1 20071023 A 5311 6545815560 FRAME BOEING 737 7373B7 1384580 NM BS 344 S8-9R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 344, S8R - S9R. REPAIRED FRAME, BS 344, S8R - S9R IAW USAIRWAYS EO 5 311-01019. 2 L 7 2 4F RT A16WE 2007112900187 20071129 00187 NM 2007 11 29 USAA920071164 1 20071024 A 5311 6546558 FRAME BOEING 737 7373B7 1384580 NM BS 907 S8-9L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 907, S8L - S9L. REPAIRED FRAME, BS 907, S8L - S9L IAW USAIRWAYS EO 5 311-01019. 2 L 7 2 4F RT A16WE 2007113000002 20071130 00002 CE 2007 11 30 GUUA10190702 1 20071019 A 3297 CONTACT BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG ANNUNCIATOR LOOSE A GUUA O OTHER N FALSE WARNING AP APPROACH 1 SO 29 81556 UE239 FLIGHT: 9238 EYW/TPA DURING APPROACH LOWER LANDING GEAR LIGHTS INOPERATIVE. SECURED LOOSE CONTACTS ON LANDING GEAR ANNU NCIATOR. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007113000003 20071130 00003 SO 2007 11 30 GUUA10190701 1 20071019 A 3260 12038594004 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE MLG INOPERATIVE A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 29 282AS 120226 FLIGHT: 5400, DURING APPROACH THE LANDING GEAR RT (B) LIGHT NOT ILLUMINATED WITH GEAR FULLY EXTENDED. REPLACED LANDING GEAR CONTROL. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2007113000020 20071130 00020 EU 2007 11 30 COEA0723821 1 20070824 A 5420 S5711224520101 SKATE ANGLE AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE RT NACELLE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. FOUND LEVEL 2 CORROSION, RT NACELLE OB SKATE ANGLE. REMOVED AND REPLACED WITH NEW SKATE ANGL E. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007113000024 20071130 00024 EU 2007 11 30 COEA0726821 1 20070827 A 5310 S53575112203 CREASE BEAM AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE DAMAGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. FOUND TOOL DAMAGE TO CREASE BEAM WEB ON UPPER SURFACE BETWEEN FR 28B, 28C. REMOVED AND INSTA LLED NEW FABRICATED WEB. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007113000027 20071130 00027 EU 2007 11 30 COEA0716821 1 20070824 A 5313 S53673000207 STRINGER AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE S18L CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. MAJOR REPAIR, FOUND LEVEL 2 CORROSION ON STRINGER 18L. FABRICATED REPLACEMENT STRINGER SECTI ON. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007113000034 20071130 00034 NM 2007 11 30 2007UALA04664 1 20071113 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 674UA 29242 EEL STRIP DAMAGED AT SEAT 5A. REPLACED EEL STRIP, TEST OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007113000038 20071130 00038 NM 2007 11 30 2007UALA04668 1 20071112 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 DOOR 5L EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007113000044 20071130 00044 2007 11 30 2007UALA04675 4 20071112 A 2565 5A29011B ASPIRATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE UNSERVICEABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA PK0195 27112 ASPIRATOR LEAKING. REPLACED ASPIRATOR AND SLIDE. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007113000048 20071130 00048 NM 2007 11 30 2007UALA04679 1 20071113 A 5210 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 DOOR 2R FRAME IS CRACKED AT UPPER HINGE CUTOUT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007113000057 20071130 00057 NM 2007 11 30 2007UALA04689 1 20071114 A 3510 HOSE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE O2 SYSTEM FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 202UA 24717 CREW REPORT: CAPT O2 HOSE CAME APART SAMC TEXT: IT LOOKS LIKE THE END OF BAYONNET ATTACHMENT FOR THE HOSE ON THE ACFT S IDE BLEW OFF AND IS MISSING. PLASTIC FITTING IN THE BOX IS BROKEN. 2 L 7 2 4F 4 F RT A16WE E2GL 2007113000062 20071130 00062 NM 2007 11 30 2007UALA04695 1 20071114 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 653UA 25391 FWD PARTITION LIGHT BAR INOP, EEL . REMOVED AND REPLACED LIGHT BAR. 2 L 7 2 4F 4 F RT A1NM E24NE 2007113000066 20071130 00066 NM 2007 11 30 AALA20072177 1 20071110 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 786AN 30250 MIA - EMERGENCY LIGHT AT SEAT ROW 24C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 24C. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007113000069 20071130 00069 NM 2007 11 30 AALA20072182 1 20071110 A 3350 LIGHT BOEING 757 757223 1384957 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 172AJ 32400 DFW - AFT EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP FOR AFT EXTERIOR EMERGENCY LIG HT AT RIGHT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007113000073 20071130 00073 NM 2007 11 30 HALA0700486 1 20071112 A 7722 INDICATION SYS BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE RT EGT FLUCTUATES A HALA K NONE O OTHER DE DESCENT 1 WP 13 594HA 23275 580314 ETOPS SIGNIFICANT SYSTEM, RIGHT ENGINE EGT FLUCTUATED ERRATICALLY DURING DESCENT WITH POWER LEVER RETARDED BELOW CRUISER POWER BETWEEN 600 DEGREES AND 55 DEGREES. PERFORMED FIM 77-21-00 FIG 103. NO DAMAGE OR FAULTS FOUND. OPERATED ENGINE S. NO FLUCTUATIONS OF EGT NOTED, LT AND RT ENGINES EGT REMAINED SIMILAR AT ALL POWER SETTINGS. NOTIFIED MOC OF WORK AC COMPLISHED AND FINDINGS. 2 L 7 2 4F 4 F RT A1NM E13NE 2007113000099 20071130 00099 NE 2007 11 30 HALA0700489 2 20071116 A 7200 BR700715A130 ENGINE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE NR 1 MALFUNCTIONED A HALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 13 486HA 7733 7733 55131 13241 ATO - AFTER TAKEOFF, THRUST SET AND PRIOR TO 80 KTS CREW HEARD LOUD BAG. TOT OVERTEMP TO 1064 DEG AND COMPRESSOR STALL ALERT ILLUMINATED. ABORTED T/O AND RETURNED TO GATE. REMOVED ENG PER HAL M144-717. INSTALLED NR 1 ENG PER HAL M143-71 7. GRD RUN-UP AND LEAK CHECK OK. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007113000103 20071130 00103 NM 2007 11 30 07FDEA04825 1 20071117 A 5311 BAC1503100183 FRAME BOEING 727 727225 1384077 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 FWD PIT BODY FRAME, UPPER CHORD ANGLE, DOUBLER IS CRACKED, BS 720B, STR 26L-27L. REMOVED DAMAGE, FORMED REPAIR ANGLE AN D FILLER, HEAT TREATED TO T-6 CONDITION, DRILLED AND TRIMMED REPAIR PARTS, ALODINED AND PRIMED. INSTALLED REPAIR REF S RM 51-40-3, 51-20-021, 8130-3 TRACKING NR 2007-11-087. REPAIR IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007113000105 20071130 00105 NM 2007 11 30 07FDEA04827 1 20071118 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 MAIN DECK CARGO COMPARTMENT AT ABOUT STA 1280 TO 1321 LBL 8 SEAT TRACK FLOOR PANEL SUPPORT FLANGE FOUND CORRODED. REP AIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. NEW SEAT TRACK AND SPLICES REWORKED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007113000116 20071130 00116 CE 2007 11 30 AMWA88127 1 20071020 A 2820 1183890065 TRANSFER PUMP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FUEL SYSTEM INOPERATIVE A AMWA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 CE 07 162ZV 635 UE162 AFTER LANDING, CREW REPORTED ODOR OF FUEL IN THE CABIN AND COCKPIT. MAINTENANCE REPLACED RT AUX TRANSFER PUMP AND CHECK VALVE AND SEALED AUX TANK. VERIFIED LEAK CHECK OK AND RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A24CE E26NE 2007113000122 20071130 00122 NM 2007 11 30 CO1Y200700008 1 20071027 A 5410 AUB7717AUB7719 HINGE DOUG MD11 MD11 3023602 NM NACELLE DOOR OUT OF LIMITS B CO1Y K NONE O OTHER IN INSP/MAINT 1 EA 33 702BC 48504 ON FWD AND AFT CORE COWLS HINGES HAVE BEEN FOUND HOLES OUT OF DWG LIMITS. 2 L 7 3 4F RT A22WE 2007113000126 20071130 00126 EU 2007 11 30 HEER117995 1 20071024 A 5330 L524M1003102 SKIN UROCOP EC135 EC135P2 5620027 EU FUSELAGE SEPARATED B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 327PH 789 0445 FIBERGLASS OUTER SKIN AND ALUMINUM DOUBLER ARE SEPARATING AT CUT OUT FOR LANDING LIGHT. REPAIRED FORWARD ACCESS PANEL I AW EMAIL PHI-921-E-070917-01R. 1 G 7 2 3U H88EU 2007113000130 20071130 00130 EU 2007 11 30 07FDEA04840 1 20071118 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT PIT STRINGER 50R CORRODED I/B SIDE AT FRAME 58. REMOVED CORROSION IAW A310-200 SRM 51-74-10. FOUND TO BE OUT OF LIM ITS IAW SRM 53-10-00 STRINGER REPLACEMENT ACCOMPLISTED ON FED EX NON ROUTINE N00357. 2 L 7 2 4F RT A35EU 2007113000132 20071130 00132 WP 2007 11 30 07FDEA04844 1 20071119 A 5313 AGA70471 STRINGER DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), VANE AIR CONDITION LT SIDE FROM STA 561 TO STA 587 STRI NGER 48 WITH CRACK AND SEVERAL CORROSION REPAIRED WITH REFERENCE SRM 53-10-00 FIG 6 VOL I. 2 L 7 3 4F A22WE 2007113000136 20071130 00136 WP 2007 11 30 07FDEA04848 1 20071119 A 5521 NLC60391 SKIN DOUG DC10 DC1030 3023501 WP LT ELEVATOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 LT INBD ELEVATOR OUTER RIB UPPER SKIN WITH .25 INCH CRACK. REPAIRED SKIN IAW SRM 55-10-00 FIG 8 VOL I. 2 L 7 3 4F A22WE 2007113000139 20071130 00139 NM 2007 11 30 AMTA200700557 1 20071024 A 3097 CONNECTOR BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE ANTI-ICE VALVE DAMAGED A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 560TZ 33525 (R ENG ANTI ICE) EICAS MSG, ENF ANTI ICE (VALVE) LIGHT ON W/SWITCH SELECTED FROM ON TO OFF. FAULT CODE 30-21-11-02. FO UND PIN PUSHED BACK IN CONNECTOR FOR VALVE, RESEATED PIN SYSTEM OPS CHECKED NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007113000140 20071130 00140 NM 2007 11 30 AMTA200700558 1 20071027 A 5514 STRAP BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE HORIZONTAL STAB CRACKED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 522AT 29330 STABILIZER STRAP CRACKED AT STA 365.25, WL 208, LBL 25. FABRICATED REPAIR IAW SRM 53-10-51-2R-1, TREATED AND PRIMED IAW SRM 51-20-01, INSTALLED REPAIR AT STA 365.25, WL 208, LBL IAW SRM 51-40-02. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007113000156 20071130 00156 SO 2007 11 30 GUUA10280701 1 20071028 A 3397 WIRE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE EMERGENCY LIGHTS LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 266AS 120188 AT SCHEDULED ROUTINE MAINTENANCE DISCOVERED EMERGENCY LIGHTS NEAR THE REAR OF THE AIRCRAFT INOPERATIVE. RESECURED LOOSE WIRE ON TRACK LIGHTING. 2 L 7 2 4T 4 T RT A31SO E20NE 2007113000158 20071130 00158 WP 2007 11 30 07FDEA04849 1 20071119 A 5314 APB70781 FITTING DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), CTR SECTION BOX WHEEL WELL AREA STA 1370 LT SIDE XCW 31. 500 KEEL FITTING APB7078-1 WITH CRACK 5" LONG REPLACED KEEL FITTING FOR SRM 51-33-01 AND SRM 51-32-01. 2 L 7 3 4F A22WE 2007113000160 20071130 00160 WP 2007 11 30 07FDEA04851 1 20071119 A 5730 ARB23122 SKIN DOUG DC10 DC1010 3022110 WP RT WING WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 RT WING DROOPED FOUND DEEP WEAR ON LWR EXTERNAL SKIN. REPAIRED SKIN IAW SRM 57-10-00 VOL I FIG 39. 2 L 7 3 4F A22WE 2007113000161 20071130 00161 WP 2007 11 30 07FDEA04852 1 20071119 A 5320 AFA71321 FITTING DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING THE HOLES OF T HE BOLTS WITH CORROSION. PERFORMED CORROSION REWORK REAMED HOLES, PERFORMED INSPECT HFEC AND INSTALLED BUSHINGS FOR SRM 53-50-00 FIG 17. 2 L 7 3 4F A22WE 2007113000162 20071130 00162 WP 2007 11 30 07FDEA04853 1 20071119 A 5730 ARB23121 SKIN DOUG DC10 DC1010 3022110 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 LT WING DROOPED FOUND CRACK AND DEEP WEAR ON EXT SKIN OUTBOARD SIDE DROOPED. REPAIRED SKIN IAW SRM 57-10-00 VOL I FIG 1 5 SHT 1. 2 L 7 3 4F A22WE 2007113000164 20071130 00164 WP 2007 11 30 07FDEA04855 1 20071119 A 5730 ARC1959U27 SKIN PANEL DOUG DC10 DC1010 3022110 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), LT WING T/E ON UPPER SKIN OUTBOARD FLAP XOF 620 FOUND DEN T 1" BY 1" AND A TEE ANGLE WITH CRACK 1 INCH LONG REPLACED PANEL ARC 1959U27 FOR SRM 51-35-01 VOL II. 2 L 7 3 4F A22WE 2007113000166 20071130 00166 WP 2007 11 30 07FDEA04857 1 20071119 A 5311 ADA71183 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), AVIONIC COMPT AT STA 449 RT AND X= -10 FRAME WITH HOLE OV ALIZED PERFORMED REPAIR FOR SRM 53-30-00 FIG 4 VOL I. 2 L 7 3 4F A22WE 2007113000167 20071130 00167 WP 2007 11 30 07FDEA04858 1 20071119 A 5312 AEA0161187 BULKHEAD DOUG DC10 DC1010 3022110 WP CLG WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 CLG WW CENTER CRACKS ON VERTICAL RT BULKHEAD. REPAIRED AREA IAW SRM 53-00-01 FIG 10 VOL I. 2 L 7 3 4F A22WE 2007113000168 20071130 00168 WP 2007 11 30 07FDEA04859 1 20071119 A 5753 ARC2735 SKIN DOUG DC10 DC1010F 3022111 WP T/E FLAP LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 LT WING I/B FLAP UPPER SKIN EXISTING REPAIR. REPAIRED SKIN IAW SRM 57-10-00 FIG 86 VOL I. 2 L 7 3 4F A22WE 2007113000171 20071130 00171 EU 2007 11 30 07FDEA04863 1 20071119 A 5210 A53610639202 BEAM AIRBUS 310 A310203 3930313 EU PAX DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 NR 3 HOLE ON FIGURE 8, AREA ON RT PAX DOOR INDICATED AS CRACKED WHEN CHECKED BY BHEC IAW NDT MANUAL 53-30-53 USING MACHI NE T8209A. REAMED HOLE IN REF TO SRM 51-40-51. PERFORMED BHEC IAW NTM 53-30-53-NO CRACKS FOUND. FABRICATED REPAIR BUS HING, PRIMED, PAINTED AND INSTALLED REPAIR BUSHING AND FASTENER IN REF TO EA 6-5310-112988 PT1, "FUSELAGE-AD2007-11-12, SB A310-53-2037, SB A310-53-2017, EO 6-5310-7-3318, RI DOOR UPPER HEADER AT FR14C-REPAIR" 2 L 7 2 4F RT A35EU 2007113000173 20071130 00173 NM 2007 11 30 SA07075 1 20071120 A 3350 32145410 BATTERY PACK AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 802AW 0924 MAINTENANCE FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. 2 L 7 2 4F RT A28NM 2007113000174 20071130 00174 EU 2007 11 30 NWAA073773304 1 20071110 A 5712 RIB AIRBUS 330 A330323 3930335 EU WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 804NW 0549 DURING INSPECTION PER AD 2006-22-14, FOUND CRACK IN RIB 6 RT AND RIB 6 LT. REPAIRED PER EA 33-211276. 2 L 7 2 4F RT A46NM 2007113000178 20071130 00178 SO 2007 11 30 SIMA200732405 1 20071119 A 3620 14540214409 HOSE EMB 145 EMB145LR 3260212 SO LT PYLON CRACKED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 933JN 14500918 AFTER TAKEOFF "LAV SMOKE WARNING" SMELL OF SMOKE IN COCKPIT AND CABIN NO FIRE IN LAV BUT COULD STILL SMELL SMOKE. FOUND CRACKED HOSE ASSY IN LEFT PYLON REMOVED AND REPLACED HOSE IAW EMB 135 AMM 20-10-03. OPS CK SATISFACTORY IAW AMM 36-00- 00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007113000188 20071130 00188 EU 2007 11 30 N820NA103107 1 20071031 A 6420 109013505101 SCISSOR LINK AGUSTA A109 A119 0261102 EU PWA PT6 PT6* 52043 EA TAIL ROTOR BROKEN E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 820NA 14011 UPON THE PILOTS DAILY INSPECTION, HE FOUND THE SUSPECT PART APPEARED TO BE CRACKED. THE MECHANIC REMOVED THE PART FROM A IRCRAFT AND PART CAME APART AT ONE OF THE MOUNTING EARS. 1 G 7 2 3U 3 T H7EU E2NE 2007113000189 20071130 00189 EU 2007 11 30 SMIA200732402 1 20071113 A 5347 7253725191 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 307AE 21265 5000 340B307 DURING MBV INSPECTION, THE SEAT TRACK AT BL 0 WAS FOUND TO BE CORRODED BEYOND MANUAL LIMITS. REPLACED SEAT TRACK IAW SA AB SRM CHAPTER 53-70-60. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4T RT A52EU 2007113000193 20071130 00193 NM 2007 11 30 ANCF200700028 1 20071029 A 2922 271N20403 FILTER BOEING 757 757236 1384971 NM RROYCE RB211 RB211535E4 54555 NE PTU CRACKED W ANCF O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 23 521NA 230 230 25592 PILOT REPORT: AIRPLANE RETURN TO RAMP DUE TO TECHNICAL PROBLEMS ( HYD SYS QTY). DURING INSPECTION FOUND THE POWER TRANS FER UNIT PRESSURE FILTER MODULE WITH LEAKAGE. REMOVED AND REPLACED THE PTU PRESSURE FILTER MODULE IAW AMM 29-22-02 PAGE 401. OPS TEST OK. 2 L 7 2 4F 4 F RT A2NM E12EU 2007113000194 20071130 00194 WP 2007 11 30 ASMF20071008 1 20071028 A 3213 733A9FT9874780 SEAL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE STRUT DAMAGED W ASMF A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 23 838AM 49397 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT HMO DUE TO CAPTAIN REPORTED THAT DURING NOSE LANDING GEAR RETRACTION, STRON G VIBRATION WAS FELT, BURNED RUBBER ODOR WAS DETECTED AND RED WARNING LIGHT TURNED ON ALL THE TIME. MAINTENANCE PERSONNE L VERIFIED THE NOSE LANDING GEAR STEERING SYSTEM IAW MM 32-51-00 NO DAMAGES WERE FOUND. NOSE LANDING GEAR CYLINDER WAS D ISASSEMBLED AND THE O-RING SEALS WERE FOUND DAMAGED, SO THEM WERE REPLACED IAW MM 32-21-02, NO MORE INTERNAL DAMAGES WER E FOUND. ADDITIONALLY, NOSE LANDING GEAR EXTENSION / RETRACTION TEST WAS PERFORMED IAW MM 32-30-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007113000196 20071130 00196 SO 2007 11 30 GUUA10240702 1 20071024 A 5330 SKIN EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE BS 6842 CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 285AS 120265 DURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED LT FUSELAGE BELLY EXFOLIATION AT F.S 6842.6. REMOVED DAMAGED AREA AND INSTALLED FILLER AND EXTERNAL REINFORCEMENT DOUBLER OVER NEW AND PREVIOUS REPAIR IAW CTA DER RCE 2001C12-24 DOCUMENT NR IC2007-120/07449. 2 L 7 2 4T 4 T RT A31SO E20NE 2007113000199 20071130 00199 NM 2007 11 30 DL757071497 1 20071116 A 3350 21007 SWITCH BOEING 757 757232 1384965 NM CABIN WORN A DALA K NONE O OTHER CR CRUISE 1 SO 27 661DN 24972 CABIN EMERGENCY LIGHTS ILLUMINATE INTERMITTENTLY DURING FLIGHT WHEN NOT COMMANDED. REPLACED TEST SWITCH S10295. 2 L 7 2 4F RT A2NM 2007113000202 20071130 00202 NM 2007 11 30 DL764071500 1 20071110 A 3350 BATTERY PACK BOEING 767 767432ER 1385134 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 836MH 29709 EMERGENCY LIGHTS AT SEATS 30 GF THRU 37GF ARE INOP. REMOVED AND REPLACED BATTERY PACK IAW B767-400 MM 33-51-07-022-005. OPS CHECKS GOOD IAW B767-400 MM 33-51-07-022-05. 2 L 7 2 4F RT A1NM 2007113000203 20071130 00203 NM 2007 11 30 DL764071501 1 20071110 A 3520 RELAY BOEING 767 767432ER 1385134 NM CABIN O2 FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 836MH 29709 A/C FAILS AUTO O2 DEPLOYMENT. REMOVED AND REPLACED RELAY K455 IAW B767-400 WDM 35-51-21-11. PERFORMED OPS CHECK OF AUT O DEPLOY O2 SYSTEM IAW B767-400 MM 35-21-00-705-054. PROCEDURE F OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2007113000204 20071130 00204 NM 2007 11 30 DLM90071502 1 20071110 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 RT CUSP WEB CORRODED OUT OG LIMITS- FS 693-769. REMOVED AND REPLACED WEB IAW MD-88 SRM 5305D FIG 828D ON N/R 2400-0232 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007113000206 20071130 00206 NM 2007 11 30 DLM90071504 1 20071110 A 5311 FRAME DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 AFT PIT FRAME AT STA 1363 CORRODED ON AFT SIDE LONGERON 28L-28R. REPAIRED FRAME IAW MD-90 SRM 53-10-02 FIG 2 ON N/R 160 0-0201 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007113000207 20071130 00207 NM 2007 11 30 DLM90071505 1 20071028 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 LT SEAT TRACK CORRODED 1255-1364 LBL 24. REPAIRED SEAT TRACK IAW MD-90 SRM 53-40-01 VOL I ON N/R 2000-0238 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007113000209 20071130 00209 NM 2007 11 30 DLM90071508 1 20071118 A 5753 5910042511 VANE DOUG MD90 MD9030 3023690 NM T/E FLAP CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 LEFT WING OUTBOARD FLAP MID VANE CHAFED APPROX 18 INCHES FROM NR 3 FLAP FAIRING. REPAIRED DAMAGED AREA OF THE LEFT WING O/B FLAP MID VANE IAW MD-90 SRM 51-10-02D PG 18B. INDENTIFIED PER DELTA PS 900-5-1 NR 4 ON N/R 5400-0002 AT HMV-2 IN O KC. 2 L 7 2 4F RT A6WE 2007113000210 20071130 00210 NM 2007 11 30 DL757071510 1 20071118 A 5610 141T480013 WINDOW BOEING 757 757232 1384965 NM COCKPIT CRACKED A DALA K NONE O OTHER CR CRUISE 1 SO 27 635DL 23762 1L WINDOW CRACKED AT FL370 M .78. REPLACED 1L WINDOW AND CONTROLLER. RETORQUE OF WINDOW AND TERMINAL CONTACTS FWD TO M CO PER M/M. 2 L 7 2 4F RT A2NM 2007113000213 20071130 00213 NM 2007 11 30 DL764071513 1 20071115 A 3320 LAMP BOEING 767 767432ER 1385134 NM R1 SLIDE INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 836MH 29709 RI DOOR SLIDE LIGHT INOP. RELAMP LIGHT INDICATOR IAW DALB767-400 MM 33-13-00. OPS CHECK GOOD IAW DAL B767-400 MM 52-73 -00 STEP E1-E9. 2 L 7 2 4F RT A1NM 2007113000215 20071130 00215 NM 2007 11 30 DL764071515 1 20071113 A 3397 WIRE BOEING 767 767432ER 1385134 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 836MH 29709 LEFT WING EMERGENCY EXIT LIGHT IN COCKPIT. TROUBLESHOOT FOUND BROKEN WIRE NR 916-222R-20 IN CROWN OF CABIN IAW DAL B767 -400 WDM 52-71-15, SPLICED WIRE W916-222R-20 IAW BSWPM 20-10-13. OPS CHECK GOOD IAW DAL B767-400 MM 52-71-00. 2 L 7 2 4F RT A1NM 2007113000217 20071130 00217 NM 2007 11 30 NWAA073786624 1 20071117 A 3350 LIGHT BOEING 747 747251B 1384892 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 624US 21706 DURING OVERNIGHT CHECK, EMERGENCY LIGHTS INOP AT DOOR 1L AND 1R. MAINTENANCE REMOVED AND REPLACED BATTERY SUPPLY, LIGHT ASSEMBLY, AND REPAIRED BROKEN WIRES. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007113000218 20071130 00218 NM 2007 11 30 NWAA073796624 1 20071116 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 624US 21706 DURING OVERNIGHT CHECK, FOUND EMERGENCY LIGHTS MAIN DECK RIGHT SIDE AISLE EXIT SIGNS IN AISLE JUST FORWARD AND AFT OF DO OR 2R INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVI CE. 2 L 7 4 4F RT A20WE 2007113000219 20071130 00219 NM 2007 11 30 NWAA073805644 1 20071118 A 3350 PIN BOEING 757 757251 1384970 NM CONNECTOR DEFECTIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 544US 26491 DURING OVERNIGHT CHECK, FOUND SEAT MOUNTED EMERGENCY LIGHTS INOP FROM ROW 17ABC TO 30ABC. MAINTENANCE INSTALLED NEW PIN IN CONNECTOR. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007113000220 20071130 00220 NM 2007 11 30 TSAA0752062 1 20071117 A 5210 6070283 CONTROL ROD BOEING 737 73776N 13844CH NM PAX DOOR OUT OF ADJUST A TSAA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 13 742AL 30830 NON-ETOPS FLIGHT 376 OAK-RNO - DURING CLIMB, THE AIRCRAFT FAILED TO PRESSURIZE. THE CREW RETURNED TO OAK WITHOUT FURTHE R INCIDENT. MAINTENANCE ADJUSTED THE FORWARD ENTRY DOOR HORIZONTAL CONTROL ROD PER AMM 52-11-00-5 AND PRESSURIZED THE A IRCRAFT ON THE GROUND WITH ALL CHECKS SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE AND PASSED A FLIGHT VERIFICATI ON ON THE NEXT FLIGHT LEG. 2 L 7 2 4F RT A16WE 2007113000221 20071130 00221 WP 2007 11 30 07FDEA04866 1 20071120 A 5347 NEA6022 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 DURING PERFORMING OK TO CLOSE FLOOR PANELS WITH J/C MD10-53210290-1J FOUND SEAT TRACK CRACK ON MAIN CABIN. 2 L 7 3 4F A22WE 2007113000222 20071130 00222 WP 2007 11 30 07FDEA04867 1 20071120 A 5320 AFJ70021 CHANNEL DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 CTR CARGO COMPT SEVERE CORROSION WITH EXFOLIATION ON CHANNEL. REPAIRED CHANNEL IAW SRM 53-70-00 VOL I FIG 5 SHT 5. 2 L 7 3 4F A22WE 2007113000223 20071130 00223 WP 2007 11 30 07FDEA04868 1 20071120 A 5347 NCA602225 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 ENTRY WAY ZONE AFTER REMOVAL FLOOR PANEL WITH OAN J/C MD10-600C220-1JR FOUND CRACK ON SEAT TRACK LUG LT SIDE. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1 SHT 1 AND 3 VOL I. 2 L 7 3 4F A22WE 2007113000226 20071130 00226 WP 2007 11 30 07FDEA04882 1 20071120 A 5310 TORQUE BOX DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 317FE 46835 R-3 DOOR FWD JAMB TORQUE BOX WEB CRACKED AT FLOOR LINE REPAIRED WEB IAW SRM 53-50-00 FIG 19 SHEET 1. 2 L 7 3 4F RT A22WE 2007113000228 20071130 00228 WP 2007 11 30 07FDEA04884 1 20071120 A 5320 SILL DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 317FE 46835 FWD PIT DOOR LOWER SILL AFT AND FWD ENDS BELOW OMNI ROLLERS SUPPORT IS CORRODED REWORKED AREAS AS REQUIRED IAW SRM 53-50 -00 FIGURE 15. 2 L 7 3 4F A22WE 2007113000229 20071130 00229 EU 2007 11 30 07FDEA04885 1 20071120 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT CARGO BILGE CORROSION ON STR - 52L, FR 58 TO FR -59. REMOVED CORROSION IAW A310 SRM 51-74-10 FOUND TO BE OUT OF LIM ITS IAW A310 SRM 53-10-00. 2 L 7 2 4F RT A35EU 2007113000233 20071130 00233 EU 2007 11 30 AALA20072223 1 20071115 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80057 465 JFK - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007113000235 20071130 00235 EU 2007 11 30 AALA20072221 1 20071115 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80057 465 JFK - EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007113000237 20071130 00237 WP 2007 11 30 AALA20072199 1 20071113 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 563AA 49345 LGA - EMERGENCY LIGHTS AT FORWARD OVERHEAD AISLE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD OVE RHEAD AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007113000238 20071130 00238 WP 2007 11 30 AALA20072187 1 20071111 A 3260 INDICATOR DOUG DC9 DC982 3022082 WP COCKPIT FAULTY A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 7544A 53026 ORD INFLIGHT T2045/11NOV - RED NOSE GEAR UNSAFE LIGHT ILLUMINATED DURING CLIMB. CYCLED GEAR AND RED NOSE GEAR LIGHT REM AINED ILLUMINATED WITH GEAR DOWN. SECONDARY GEAR INDICATOR WAS NORMAL. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. R EPLACED INDICATOR D1 32. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007113000240 20071130 00240 NE 2007 11 30 AALA20072188 2 20071112 A 7230 COMPRESSOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT ENGINE STALLED A AALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 21 970TW 53620 728213 SAT INFLIGHT T1303/12NOV - NUMBER TWO ENGINE HAD COMPRESSOR STALLS ON INITIAL CLIMB-OUT PASSING 3500 FEET. CREW HEARD T HREE OR FOUR BANGS. ENGINE WAS BROUGHT TO IDLE UNTIL LANDING. RETURNED TO SAT AND LANDED WITHOUT INCIDENT. FOUND INTE RNAL DAMAGE TO 12 AND 13 STAGE. REPLACED NUMBER TWO ENGINE ON 13 NOV 2007 AT SAT. SYSTEM GROUND CHECKED NORMAL OPERATI ON. 2 L 7 2 4F 4 F RT A6WE E9NE 2007120300001 20071203 00001 NM 2007 12 3 DL76L071447 1 20071111 A 5270 SENSOR BOEING 767 767332 1382001 NM LT SLIDE DOOR OBSTRUCTED A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 187DN 27582 L WING SLIDE MSG ON EICAS W/EMERG DOORS LIGHT ON OVERHEAD PANEL INTERMITTENT ON TAXI. FWD TO MCO/PLAC PER MEL 52-71-01. LT OVERWING SLIDE DOOR VERIFIED CLOSED AND FAIRED. DISARMED EMERGENCY EVAC SYSTEM PER AMM. REMOVED LT FWD AND A OVER WING HATCHES. REMOVED DEBRIS FROM SENSORS. PERFORMED ESCAPE HATCH INDICATION CIRCUIT CK, CKS GOOD. OVERWING SLI DOOR LATCH AND ACTUATORS WERE REPLACED IN ANOTHER LOG ENTRY PERFORMED LT SLIDE DOOR SENSOR CK. CHECKED GOOD. MCO AND PLACAR D REMOVED. 2 L 7 2 4F RT A1NM 2007120300002 20071203 00002 NM 2007 12 3 07FDEA04869 1 20071120 A 2810 SKIN DOUG MD11 MD11F 3023600 NM AUX TANK CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 CABIN, AT ABOUT STA 1228 LBL 8 TO RBL 8 UPPER AUX TANK UPPER SKIN FOUND CORRODED. REPAIRED AS PER FEDEX EA 1-5710-11706 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007120300003 20071203 00003 NM 2007 12 3 07FDEA04870 1 20071120 A 2810 SKIN DOUG MD11 MD11F 3023600 NM AUX TANK CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 CABIN, AT ABOUT STA 1228 RBL 40 TO RBL 54 UPPER AUX TANK UPPER SKIN FOUND CORRODED. REPAIRED AS PER FEDEX EA 1-5710-1 17062, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007120300010 20071203 00010 WP 2007 12 3 07FDEA04878 1 20071120 A 5330 ADA3139501 DOUBLER DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON EXTERNAL SKIN AT FWD CARGO DOOR AFT JAMB WAS FOUND DAMAGED. REPA IR AS BEEN REPLACED WITH A NEW ONE IAW SRM 53-50-00 FIG 9. 2 L 7 3 4F A22WE 2007120300011 20071203 00011 WP 2007 12 3 07FDEA04879 1 20071120 A 5730 ARB23121 SKIN DOUG DC10 DC1010 3022110 WP LT WING MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON LT DROOPED L/E SKIN WAS FOUND NOT IN COMPLIANCE WITH APPROVED DAT A REPAIR HAS BEEN REPLACED WITH A NEW ONE IAW SRM 57-10-00, FIG 55, VOL I. 2 L 7 3 4F A22WE 2007120300012 20071203 00012 WP 2007 12 3 07FDEA04880 1 20071120 A 5311 ADA00105 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON FRAME CAP AT STA 840 BETWEEN LONG NR 50R AND 50L WAS FOUND NOT IN COMPLIANCE WITH APPROVED DATA. REPAIR HAS BEEN REPLACED WITH A NEW ONE IAW SRM 53-30-00, FIG 5, VOL I. 2 L 7 3 4F A22WE 2007120300015 20071203 00015 NM 2007 12 3 AALA20072186 1 20071111 A 3350 LENS BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 668AA 25333 DFW - EMERGENCY LIGHT AT SEAT 14D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007120300016 20071203 00016 NM 2007 12 3 AALA20072197 1 20071113 A 3397 CONNECTOR BOEING 767 767323 1385205 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 343AN 33082 MIA - EMERGENCY LIGHTS AT SEAT ROWS 38B TO 41B INOPERATIVE. RECONNECTED CONNECTORS AT SEAT ROW 38 FOR EMERGENCY LIGHTS AT SEAT ROWS 38B TO 41B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007120300018 20071203 00018 NM 2007 12 3 AALA20072212 1 20071115 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 954AN 30089 MIA - EMERGENCY LIGHT AT LEFT FORWARD OVERWING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT FORWARD OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007120300019 20071203 00019 NM 2007 12 3 AALA20072216 1 20071115 A 3350 LENS BOEING 737 737823 13844BZ NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 975AN 29549 LGA - EMERGENCY LIGHT AT SEAT 20D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007120300020 20071203 00020 NM 2007 12 3 AALA20072217 1 20071115 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 603AA 27054 DFW - EMERGENCY LIGHT AT SEAT 34D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 34D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007120300023 20071203 00023 EU 2007 12 3 AALA20072220 1 20071115 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80057 465 JFK - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007120300026 20071203 00026 WP 2007 12 3 AALA20072207 1 20071114 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 955U 49427 LGA - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 8 INOPERATIVE. SECURED LOOSE BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD SE AT ROW 8. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007120300027 20071203 00027 NM 2007 12 3 AALA20072208 1 20071114 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 649AA 24607 DFW - EMERGENCY LIGHT AT BULL NOSE OVERHEAD SEATS 1AB AND 2EF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT BULL NOSE OVERHEAD SEATS 1AB AND 2EF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007120300030 20071203 00030 NM 2007 12 3 AALA20072192 1 20071112 A 3350 12653 BEZEL BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 352AA 24033 SFO - EMERGENCY LIGHT AT RIGHT AFT GALLEY INOPERATIVE. REPLACED BEZEL FOR EMERGENCY LIGHT AT RIGHT AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007120300032 20071203 00032 NM 2007 12 3 AALA20072209 1 20071114 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 679AN 29589 DFW - EMERGENCY LIGHT AT AFT LEFT OVERWING EXIT DOOR FORWARD HATCH HANDLE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGH T AT AFT LEFT OVERWING EXIT DOOR FORWARD HATCH HANDLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007120300033 20071203 00033 WP 2007 12 3 AALA20072201 1 20071113 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7535A 49989 DFW - EMERGENCY LIGHT AT SEAT 9D INOPERATIVE. REPLACED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007120300034 20071203 00034 WP 2007 12 3 AALA20072202 1 20071113 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7535A 49989 DFW - EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F A6WE 2007120300036 20071203 00036 WP 2007 12 3 AALA20072204 1 20071113 A 3350 SHROUD DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7535A 49989 DFW - EMERGENCY LIGHT AT SEAT 13D HAD DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007120300037 20071203 00037 NM 2007 12 3 AALA20072205 1 20071113 A 3350 LIGHT BOEING 777 777223 1385213 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 DFW EXTERNAL EMERGENCY LIGHT AT RIGHT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT RIG HT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120300038 20071203 00038 EA 2007 12 3 SWIA200718868 1 20070802 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 906SW 7510 FOUND AT C-CHECK, FS480 AT LBL36 CLIP IS CRACKED. INSTALLED CLIP PER REO:601R-53-41-059 REV. 2 L 7 2 4F RT A21EA 2007120300039 20071203 00039 EA 2007 12 3 SWIA200718869 1 20070802 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 906SW 7510 FS 480 AT RBL36 CLIP IS CRACKED, FOUND AT C-CHECK. INSTALLED CLIP PER REO 601R 53-41-059. 2 L 7 2 4F RT A21EA 2007120300042 20071203 00042 EA 2007 12 3 SWIA200718872 1 20070802 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 906SW 7510 PAX DOOR AFT DRAG ANGLE IS CRACKED, FOUND AT C-CHECK. INSTALLED UPPER AND LOWER AFT ANGLE SPLICES PER CRJ200 SRM 51-42- 06 PAGE 4. 2 L 7 2 4F RT A21EA 2007120300051 20071203 00051 EA 2007 12 3 SWIA200718881 1 20071116 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN DAMAGED A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 906SW 7510 AFT FLOOR EMERGENCY LIGHTS ARE INOP, FLIGHT NR 6523. REPAIRED WIRING IAW WM 20-10-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2007120300053 20071203 00053 EA 2007 12 3 SWIA200718883 1 20071114 A 3350 POWER STRIP CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 963SW 7865 FLT 5966 - BACK HALF OF EMERGENCY LIGHTS ARE INOP. REPLACED AFT FLOOR EMERGENCY LIGHTS POWER STRIP IAW CRJ AMM 33-51-00 . OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007120300058 20071203 00058 SO 2007 12 3 SWIA200718888 1 20071117 A 3397 WIRE EMB 120 EMB120ER 3260203 SO CABIN BROKEN A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 297SW 120327 ROW 9 EMERGENCY EXIT LIGHTS ARE INTERMITTENT, FLIGHT NR 5708. REPAIRED BROKEN WIRE BEHIND EXIT SIGN. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007120300060 20071203 00060 NM 2007 12 3 QXEA200701730 1 20071117 A 4950 HOUSING BOMBDR DHC8 DHC8402 1390042 NM APU CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 C4 PDX - APU FLOW CONTROL SOV HOUSING IS CHAFING AGAINST TOP OF FRAME AT STATION 920.916 ON VERTICAL WEB AT 11:00 POSITI ON ON FORWARD SIDE. REPAIRED IAW SRM 51-14-00, RD8/4-55-358. 2 H 7 2 4T RT A13NM 2007120300062 20071203 00062 NM 2007 12 3 QXEA200701736 1 20071116 A 5320 FLOOR SUPPORT BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 C4 PDX - AFT PASSENGER DOOR AIRSTAIR TROLLY FLOOR SUPPORT FLANGE HAS CORROSION AT THE SCREW. REPAIRED IAW SRM 51-42-05, 51-42-35. 2 H 7 2 4T RT A13NM 2007120300063 20071203 00063 NM 2007 12 3 QXEA200701733 1 20071114 A 5320 THRESHOLD BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 C4 PDX - MAIN CABIN DOOR ENTRY THRESHOLD LANDING FOR THE FLOOR PANEL 131CZ IS CORRODED IN SPOTS ALONG ITS LENGTH. REPAI RED IAW SRM 51-42-05, RD8/4-53-1660. 2 H 7 2 4T RT A13NM 2007120300066 20071203 00066 NM 2007 12 3 QXEA200701732 1 20071113 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 C4 PDX - LEFT INBOARD SEAT TRACK NR 5 HAS CORROSION BETWEEN STATION X-18 TO X30. REPAIRED IAW RD8/4-53-884, AND SRM 51- 42-05. 2 H 7 2 4T RT A13NM 2007112900045 20071129 00045 NM 2007 11 29 2007UALA04764 1 20071119 A 2150 A/C PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 514UA 24839 726597 ACRID ODOR FROM AIR CONDITIONING SYS ON DEPARTURE. CREW ISOLATED LT PACK OFF AND ODOR DISSIPATED. CREW STATED IT SMELL ED LIKE HYD FLUID. LT PACK INOP. ENGINE HISTORY SHOWS THAT ENGINE WAS REMOVED DUE TO OIL PUDDLE AT NR 3 BEARING AREA, ACCOMPLISHED BORESCOPE OF THE ENGINE NR 1, LOOKING FOR EVIDENCE OF OIL IN THE NR 3 BEARING COMPARTMENT. NO OIL FOUND BU T STREAKING PRESENT COMING FROM HOLES ON HUB & ON IGV'S AND HPC BLADES. REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007112900053 20071129 00053 NM 2007 11 29 2007UALA04775 1 20071120 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 FWD ENTRY DOOR LOWER FWD CORNER HAS CRACK IN FRAME. REPLACED LOWER FORWARD FRAME. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112900058 20071129 00058 NM 2007 11 29 2007UALA04780 1 20071120 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 580UA 26698 DOOR 2 LEFT EXTERIOR EMERGENCY LIGHT INOP. REPLACE LAMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700091 20080107 00091 NM 2008 1 7 200712211 1 20071221 A 3350 340022 BATTERY EMB ERJ170 ERJ170100SE 3260406 NM CABIN DISCHARGED A UHLA K NONE L NO TEST IN INSP/MAINT 1 GL 11 657RW 17000115 DURING EMERGENCY LIGHT POWER UNIT FUNCTIONAL TEST THE EXIT LOCATER SIGN AT CENTER FUSELAGE IN AFT GALLEY CENTER CEILING PANEL DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT POWER UNIT. 2 L 7 2 4F RT A56NM 2007112900067 20071129 00067 WP 2007 11 29 ASAA0782279 1 20071125 A 5260 9915570101 SKIN DOUG DC9 DC983 3022083 WP AIRSTAIR DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 961AS 53075 A 9 INCH J-SHAPED CREASE ON EXTERIOR OF AFT STAIRWAY DOOR LEFT SIDE OF AIRPLANE JUST FORWARD OF EXTERNAL TAIL CONE ACCES S DOOR. CUT OUT DAMAGED SECTION OF SKIN, FABRICATED LOCATED AND INSTALLED A REPLACEMENT SKIN AND DOUBLER IAW MD80 SRM 5 2-05 FIG 56. 2 L 7 2 4F RT A6WE 2007112900076 20071129 00076 EA 2007 11 29 TRAX200701770 1 20071121 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 683BR 7692 RIGHT EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007112900084 20071129 00084 NM 2007 11 29 SWAA075808 1 20071121 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM BS 380 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007112900093 20071129 00093 NM 2007 11 29 SWAA075833 1 20071120 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 729E S22L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 729E, STR 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007112900099 20071129 00099 NM 2007 11 29 SWAA075815 1 20071124 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM LT OVERWING INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 436WN 32456 DURING SCHEDULED MV2 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007112900110 20071129 00110 NM 2007 11 29 SWAA075797 1 20071123 A 2121 6454051 FAN BOEING 737 7375H4 138449D NM E&E BAY FAULTY A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 526SW 26568 F/A REPORTED A BURING ODOR IN CABIN. FOUND RECIRC FAN C/B TRIPPED. ODOR WENT AWAY. REMOVED AND REPLACED RECIRC FAN PE R MM. 2 L 7 2 4F RT A16WE 2007112900124 20071129 00124 NM 2007 11 29 07FDEA04792 1 20071115 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1059 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 MAIN DECK CARGO COMPARTMENT AT ABOUT STA 1059 RBL 47 SEAT TRACK FOUND DAMAGED. REMOVED AND REPLACED AS PER SRM 53-70-00 . NEW SEAT TRACK REWORKED AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007112900127 20071129 00127 EU 2007 11 29 07FDEA04795 1 20071115 A 5711 FRAME AIRBUS 310 A310203 3930313 EU ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 FRAME 47 FASTENER HOLE INSPECTION, NR 4 RT HOLE HAS INDICATION OF DEFECT. REAMED HOLE TO TRANSITION FITTING IAW FED EX A310-200 SRM 51-40-40 PG14. INSTALLED FASTENER IAW A310-200 SRM 51-40-21 PG 24. BHEC NR 4 HOLE REF EA 6-5710-112994. N O CRACK INDICATION NOTED 2 L 7 2 4F RT A35EU 2007112900149 20071129 00149 EU 2007 11 29 07FDEA04815 1 20071116 A 5315 A5381293420000 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 MAIN DECK FLOOR, ADAPTER TRACK ( CROSS BEAM ) CRACKED, FR 52 ( X2825 ) BL 17L TO BL 37L ( Y430 - Y940 ). REMOVED AND R EPLACED CROSS BEAM, REF: A310-200 SRM 51-40-21 PAR 5. LOCATED AND DRILLED NEW CROSS BEAM REF: A310-200 SRM 51-40-44 PAR 2. 2 L 7 2 4F RT A35EU 2007112900163 20071129 00163 NM 2007 11 29 DL76G071487 1 20071112 A 5315 150531237075 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 434 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 152DL 24984 FWD CARGO STATION 434 RBL 4 CARGO FLOORBEAM UPPER CHORD RIVET ADJACENT TO SCREW HOLE. UPPER CORD REPAIRED PER 53-00-07 REPAIR 4 FIGURE 201 ON NR APP523636. 2 L 7 2 4F RT A1NM 2007112900164 20071129 00164 NM 2007 11 29 DL76G071488 1 20071112 A 5315 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 1197 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 152DL 24984 AFT CARGO STATION 1197+88 RBL 27 TO RBL 33 FLOORBEAM TOP SURACE CORRODED. REPAIRED PER 53-00-07 REPAIR 4 FIGURE 201 ON NR APP5155574 AT HMV3/PSV17. 2 L 7 2 4F RT A1NM 2007112900166 20071129 00166 NM 2007 11 29 DL76G071490 1 20071112 A 5315 LS50337075 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 1197 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 152DL 24984 AFT CARGO STATION 1197+44 RBL 41 CARGO FLOORBEAM UPPER CHORD CORRODED. REPAIRED ON NR APP515129 PER 53-00-07D FIGURE 80 1D ON HMV3/ PSV17. 2 L 7 2 4F RT A1NM 2007112900182 20071129 00182 NM 2007 11 29 USAA920071159 1 20071023 A 5311 65465292 FRAME BOEING 737 7373B7 1384580 NM BS 440 S8-9L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 440, S8L - S9L. REPAIRED FRAME, BS 440, S8L - S9L IA W USAIRWAYS EO 5311-01019. 2 L 7 2 4F RT A16WE 2007112900183 20071129 00183 NM 2007 11 29 USAA920071160 1 20071023 A 5311 90526911 FRAME BOEING 737 7373B7 1384580 NM BS 480 S8-9L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 480, S8L - S9L. REPAIRED FRAME, BS 480, S8L - S9L IAW USAIRWAYS EO 5 311-01019. 2 L 7 2 4F RT A16WE 2007112900193 20071129 00193 NM 2007 11 29 AMTA200700486 1 20071009 A 3610 S212N10145 CONTROLLER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 520AT 27976 EICAS MSG L ENG BLEED OFF DISPLAYED. LT ENGINE BLEED AIR OFF LGT ILLUM WITH ENG RUNNING ADN SW ON. DUCT PRES ZERO. T/ S IAW FIM 36-10-00. REMOVED AND REPLACED THE LT ENG REVERSE FLOW CONTROLLER IAW MM 36-11-18-4. SYSTEM CHECKS OK. AC OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007112900196 20071129 00196 NM 2007 11 29 AMTA200700509 1 20071015 A 2610 CIRCUIT CARD BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 11 519AT 27975 RT ENGINE O/H LP1 DISPLAYED DURING DECENT. AFTER 4 MINUTES THEN OUT, THEN CAME ON INTERMITTENTLY AFTER THAT OFF AT LAND ING. RT ENGINE O/H LB1 TESTS NORMALLY. SWAPPED LT ENG AFOLTS CARD (M10224) WITH RT ENGINE AFOLTS CARD (M10274) FOR T/S MPN 285N0028-36 LT ENGINE SN NOW D10996, RT ENGINE SN NOW D11126. BOTH SYS TEST NORMAL IAW AMM 26-10-01-4. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007112900197 20071129 00197 NM 2007 11 29 AMTA200700520 1 20071017 A 5313 LONGERON BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE BS 133 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 550TZ 32584 AFT CARGO PIT LOWER BILGE CORROSION AT STA 1330, RBL 7.55 ON LONGERON. REMOVED CORROSION MATERIAL LOSS .027 OUT OF LIMI TS. REPAIRED IAW SRM 53-60-53, 53-00-53. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007112900204 20071129 00204 SO 2007 11 29 GUUA10210701 1 20071021 A 3250 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE NLG STEERING CONTAMINATED A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 29 268AS 120202 FLIGHT:9218 MIA/TPA DURING APPROACH NOSEWHEEL (A) DISAGREEMENT RED LIGHT ILLUMINATED AT LANDING GEAR EXTENSION. AFTER LA NDING (6) GREEN LIGHTS ILLUMINATED. CLEANED WATER RESIDUE FROM NOSE WHEEL STEERING CONNECTOR. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2007112900205 20071129 00205 2007 11 29 CLCA304NOV28 4 20071128 A 3400 20704100101 RECEIVER DOUG DC10 DC1030 3023501 WP WX RADAR SYS MALFUNCTIONED A CLCA J A DUMP FUEL UNSCHED LANDING G MULTIPLE FAILURE NR NOT REPORTED 1 SO 29 304SP N46540 BOTH WEATHER RADARS NR 1 AND NR 2 PAINT NO RETURN EITHER CAPTAINS OR FIRST OFFICERS SCREEN. REPLACED TR UNIT LISTED BELO W IN ADDITION TO RADAR ANTENNA P/N 2070409-0101 S/N 2927 FOR TROUBLE SHOOTING PURPOSES. 2 L 7 3 4F A22WE 2007113000006 20071130 00006 NM 2007 11 30 AALA20072172 1 20071108 A 3350 CM1317 LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 323AA 22324 JFK - EMERGENCY LIGHT AT OVERWING ON LEFT SIDE FORWARD BULB INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERWING ON LEFT SIDE FORWARD POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007113000009 20071130 00009 NM 2007 11 30 AALA20072169 1 20071108 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 921AN 29522 LGA - EMERGENCY LIGHTS AT OVERHEAD LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVER HEAD LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007113000021 20071130 00021 NM 2007 11 30 2007UALA04660 1 20071112 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 507UA 24743 EXTERIOR EMERGENCY LIGHTS AT DOOR 2R, 4L, 4R AND AFT CARGO DOOR INOP WHEN EMERG LT TEST SW ON NOSE GEAR PUT IN MOM POSIT ION. RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007113000029 20071130 00029 EU 2007 11 30 COEA0727821 1 20070828 A 5711 S57112081200 SPAR CAP AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE RT WING CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. MAJOR REPAIR, LEVEL 2 CORROSION. CORROSION ON RT WING AFT SPAR UPPER CAP SLAT STRIP BETWEEEN RIBS 4 AND 7. REMOVED CORROSION AND DAMAGE BLENDED IAW DO/TS-4073/07-9281 REPAIR INSTRUCTIONS. WO NR 72241/ NR602018. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007113000033 20071130 00033 NM 2007 11 30 2007UALA04663 1 20071112 A 3350 POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT INTERMITTENT A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 655UA 25393 EEL LIGHTS FLICKER ON AND OFF AT LEFT SIDE OF FIRST CLASS. SUSPECT BAD PWR PACK. PREVIOUS HISTORY. REPLACED BATTERY POWER SUPPLY PACK. TEST FLOOR EEL LIGHTS. OP CHKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007113000046 20071130 00046 NM 2007 11 30 2007UALA04677 1 20071113 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 CREW REPORTED SEAT 4A EMERGENCY EVACUATION LIGHT INOP. REPLACED LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007113000061 20071130 00061 NM 2007 11 30 2007UALA04694 1 20071114 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R3 DOOR OUT OF ADJUST A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 577UA 26693 FOUND DOOR 3R DIFFICULT TO ARM. 2 L 7 2 4F 4 F RT A2NM E17NE 2007113000064 20071130 00064 NM 2007 11 30 AALA20072183 1 20071110 A 3350 SWITCH BOEING 757 757223 1384957 NM EXTERIOR LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 172AJ 32400 DFW - EXTERNAL EMERGENCY LIGHT SWITCH BY NOSE STRUT IS LOOSE. TIGHTENED EXTERNAL EMERGENCY LIGHT SWITCH BY NOSE STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007113000067 20071130 00067 NM 2007 11 30 AALA20072178 1 20071110 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 786AN 30250 MIA - EMERGENCY LIGHT AT SEAT ROW 40G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 40G. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007113000068 20071130 00068 NM 2007 11 30 AALA20072179 1 20071110 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 786AN 30250 MIA - EMERGENCY LIGHT AT SEAT ROW 40G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 40G. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007113000076 20071130 00076 SO 2007 11 30 SIMA200731901 1 20071114 A 3150 80069425 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 641AE 145191 ON TAKEOFF ROLL, GOT TAKEOFF CONFIG WARNING SPOILERS 60 KTS. TROUBLESHOOT IAW FIM REMOVED AND REPLACED THE AURAL WARNIN G UNIT IAW 31-51-01. OP CHECK GOOD. ALSO, PERFORMED HIGH SPEED TAXI TO CONFIRM PROPER OPERATION. OPS GOOD AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007113000078 20071130 00078 SO 2007 11 30 SIMA200732302 1 20071116 A 7931 23078098 PRESSURE SWITCH EMB 135 EMB135KL 3260302 SO OIL SYSTEM DEFECTIVE A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 825AE 145589 ENGINE 2 OIL PRESS FLUX EN ROUTE TO GDL ELECTED TO RETURN TO DFW DISC. REMOVED AND REPLACED LOW OIL PRESSURE SWITCH IAW RR MM 79-33-10. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007113000080 20071130 00080 EU 2007 11 30 TRBA2007100 1 20071118 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU CABIN DISCHARGED A TRBA O OTHER O OTHER UK UNKNOWN 1 SO 29 426AT 426 2ND CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY UNIT IAW JIC 33-51-21. PERFORMED O PERATIONAL CHECK AND FOUND WORKING PROPERLY AT THIS TIME. 2 H 7 2 4T RT A53EU 2007113000083 20071130 00083 NM 2007 11 30 NWAA073766624 1 20071116 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 624US 21706 DURING OVERNIGHT CHECK, FOUND 2 EMERGENCY LIGHTS OUTSIDE OF AIRCRAFT ON LEFT SIDE WING ROOT FAIRING INOP. MAINTENANCE R EMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007113000110 20071130 00110 EU 2007 11 30 07FDEA04832 1 20071118 A 5347 R538D104820200 ADAPTER AIRBUS 310 A310203 3930313 EU CABIN SEAT TRACK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FLOORBEAM ADAPTER BETWEEN SEAT TRACK AT LBL17 AND LBL 37 AT FRAME 46 IS CRACKED. REMOVED AND REPLACED ADAPTER IAW A310 SRM 51-40-21 PAR 6. 2 L 7 2 4F RT A35EU 2007113000133 20071130 00133 WP 2007 11 30 07FDEA04845 1 20071119 A 5411 AUB71242 FRAME DOUG DC10 DC1010 3022110 WP NR 3 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK) PYLON NR 3 FOUND INTERNAL SIDE FRAME BROKEN AND DEFORMED. REPLACED STRAP P/N AVB7123-3, ANGLE P/N AUB7123-5, ZEE P/N AUB7123-7, CLIP P/N AUB7124-2 FOR SRM 51-33-01 VOL II. 2 L 7 3 4F A22WE 2007113000134 20071130 00134 WP 2007 11 30 07FDEA04846 1 20071119 A 5310 ACA33473 DOOR FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE DEFORMED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), VANE AIR CONDITION COMPT LT SIDE BAY JAMB STRUCTURE FRA ME AT STA 486 DEFORMED REPAIRED FOR SRM 53-30-00 FIG 5 VOL I. 2 L 7 3 4F A22WE 2007113000149 20071130 00149 SO 2007 11 30 GLBA20061021 1 20071029 A 5712 RIB EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT WING CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 96ZK 120096 RIB CRACKED AT LT WS YA 6285. MX REPAIRED CRACKED RIB AT WS 6285 IAW SRM 57-20-07. CRACK APPROXIMATELY .375. RII INSPE CTION COMPLIED WITH PER TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A31SO E20NE 2007113000153 20071130 00153 CE 2007 11 30 GUUA10240701 1 20071024 A 3297 CONTACT BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NLG ANNUNCIATOR DIRTY A GUUA O OTHER O OTHER LD LANDING 1 SO 29 231YV UE231 FLIGHT: 9188, DURING LANDING NOSE LANDING GEAR ANNUNCIATOR FAILED TO ILLUMINATE. CLEANED ANNUNCIATOR CONTACTS. OPERATIO NAL CHECK GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2007113000163 20071130 00163 EU 2007 11 30 07FDEA04854 1 20071119 A 5313 FX5310141N310 STRINGER AIRBUS 310 A310324 3930206 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FWD CARGO BETWEEN FR 38.1 AND FR 38.2 STGR 48 RT HAS CORROSION. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53- 10-14. CUT OUT DAMAGE AREA STR 48 RT FR 37-38.1 IAW SRM 53-10-14. REMOVED SHEAR TIE TR 37 STR 47 RT. FAB STRINGER D OUBLER IAW MAE TRAVELER NR T2 / 711754. FAB STRINGER COUPLING IAW SRM 53-10-14. LOCATED AND DRILLED STRINGER DOUBLER A ND STRINGER COUPLING IAW SRM 51-40- 43. INSTALLED STRINGER DOUBLER, STRINGER COUPLING, AND SHEAR TIE IAW SRM 53-10-14. 2 L 7 2 4F RT A35EU 2007113000165 20071130 00165 WP 2007 11 30 07FDEA04856 1 20071119 A 5512 ALC72081 SKIN PANEL DOUG DC10 DC1010F 3022111 WP HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 DURING STB INSP FOUND PANEL P/N 7206-1 AND P/N 7207-1 OF CONSTANT SECTION SKIN PANEL PLANKS, SEE ATTACHED SHEET FOR BEST DETAIL. CRACK IS IN FLYABLE LIMITS. ACCOMPLISHED EA NR 8-5510-99384. 2 L 7 3 4F A22WE 2007113000169 20071130 00169 WP 2007 11 30 07FDEA04861 1 20071119 A 5512 ALC72051 SKIN DOUG DC10 DC1010 3022110 WP HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 DURING U/S INSP OF HORIZ STB, FOUND TWO PANEL WITH CRACK IN FLYABLE LIMITS. ACCOMPLISHED EA NR 8-5510-111533. 2 L 7 3 4F A22WE 2007113000176 20071130 00176 NM 2007 11 30 QXEA200701729 1 20071119 A 2434 31708001A GENERATOR DHAV DHC8 DHC8202 2809007 NM NR 1 MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION UK UNKNOWN 1 NM 09 346PH 1381 1381 477 SEA-ON FLIGHT 2199, RETURNED TO GATE NR 1 DC GENERATOR HOT CAUTION. MAINTENANCE REMOVED AND REPLACED NR 1 DC GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007113000177 20071130 00177 EU 2007 11 30 SIMA200732409 1 20071113 A 5320 7253621501 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 391AE 340B391 DURING A HMBV INSPECTION, THE GALLEY FLOOR SUPPORT ON FRAME 225 WAS FOUND TO BE CORRODED. REPAIRED FLOOR SUPPORT ON FRA ME 225 PER SAAB SRM CHAPTER 53-70-30. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007113000185 20071130 00185 SO 2007 11 30 SIMA200732406 1 20071117 A 3097 CONNECTOR EMB 135 EMB135KL 3260302 SO WINDSHIELD HEAT BURNED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 808AE 145519 ELECTRICAL ODOR IN COCKPIT AND FLT ATTENDANT REPORTED SMOKE/HAZE AT ROWS 10 AND 11. UPON INSPECTION FOUND BURNT CONNECT OR AT THE F/O WINDSHIELD POWER CONNECTOR. REPLACED BURNT CONNECTOR IAW EMB 140 WM 20-00-0. REATTACHED CONNECTOR TO FO WINDSHIELD IAW EMB 30-43-04. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007113000186 20071130 00186 SO 2007 11 30 SIMA200732407 1 20071117 A 3620 14540214409 HOSE EMB 135 EMB135LR 3260305 SO LT PYLON CRACKED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 713AE 145249 ON CLIMB-OUT OF LGA, GOT BLEED 1 OVER TEMP EICAS MESSAGE. DIVERTED TO BOS. DID NOT HAVE OVER WEIGHT LANDING. FOUND CR ACKED HOSE ASSEMBLY IN LEFT PYLON REMOVED AND REPLACED HOSE IAW EMB 135 AMM 20-10-03. OPS CHECK SATISFACTORY IAW AMM 36 -00-00 EMB 30-43-04. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007113000190 20071130 00190 NE 2007 11 30 HEEA118029 1 20071028 A 5302 9220306301107 DOUBLER SKRSKY S92 S92A NE TAILBOOM CRACKED B HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 392PH 2430 920015 DURING ROUTINE INSPECTION NOTED CRACK IN TAILBOOM TO PYLON TRANSITION AREA, UPPER LEFT SIDE IN SADDLE STRAP DOUBLER. RE PAIRED SADDLE STRAP PER SIKORSKY DRAWING 92203-06301-011. 2 G 7 2 4U R00024BO 2007113000191 20071130 00191 EU 2007 11 30 SIMA200732401 1 20071116 A 5347 7253725193 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 307AE 21265 5000 340B307 DURING MBV INSPECTION, THE SEAT TRACK AT B.L. 18.3 LEFT WAS FOUND TO BE CORRODED. REPLACED SEAT TRACK WITH PN 7253725- 193 IAW SAAB SRM 53-70-60. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007113000192 20071130 00192 EU 2007 11 30 SIMA200732410 1 20071106 A 5347 7253742407 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 307AE 21265 5000 340B307 DURING A MBV INSPECTION, THE LEFT AFT THREE 36L SEAT TRACK WEBS WERE FOUND TO BE DAMAGED. REPAIRED THE LEFT AFT THREE 3 6L SEAT TRACK WEBS PER SAAB SRM CHAPTER 51-70-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007113000201 20071130 00201 NM 2007 11 30 DL764071499 1 20071110 A 3520 CONNECTOR BOEING 767 767432ER 1385134 NM CABIN NOT SEATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 836MH 29709 PSU AT SEAT 46CDE FAILS O2 DEPLOYMENT. RESEATED LOOSE CONNECTOR. PERFORMED OPS TEST OF PASSENGER OXYGEN SYSTEM IAW B767 -400 MM 35-21-00-705-054. OPS TEST GOOD. 2 L 7 2 4F RT A1NM 2007113000205 20071130 00205 NM 2007 11 30 DLM90071503 1 20071113 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 CABIN SEAT TRACK CORRODED OUT OF LIMITS FS 455-520 RBL 54. REPAIRED DAMAGED SEAT TRACK FROM FS 332-864 RBL 54 IAW MD-90 SRM 53-40-01 FIG 6 ON N/R 2700-0199 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007113000208 20071130 00208 NM 2007 11 30 DL738071507 1 20071117 A 5610 141A48107 WINDOW BOEING 737 737832 13844CF NM COCKPIT CRACKED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 395DN 30773 CLIMBING THROUGH 12,000 CAPT SIDE NR 2 WINDOW CRACKED. PRESS WAS NOT LOST. REPLACED CAPT NR 2 SLIDING WINDOW PER MM. PRESSURIZED A/C, NO LEAKS. WINDOW HEAT CONTROLLER REPLACED AND CKS OK PER MM. PARTS HELD IN QUARANTINE CVG. 2 L 7 2 4F RT A16WE 2007113000224 20071130 00224 NM 2007 11 30 07FDEA04874 1 20071120 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 MAIN DECK CARGO COMPARTMENT, AFTER FLOOR PANEL REMOVAL AT ABOUT STA 1661 TO STA 1701 SEAT TRACK FLOOR PANEL SUPPORT FLAN GE FOUND CORRODED. REPAIRED AS PER FEDEX EA 1-5310-117060. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007113000230 20071130 00230 EU 2007 11 30 07FDEA04886 1 20071120 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 CORROSION ON STR-56R, FR-59 TO FR-60 -AFT CARGO BILGE. REMOVED CORROSION IAW SRM 51-74-10. FOUND TO OUT OF LIMITS IAW SRM 53-10-00. CUT OUT DAMAGE SECTION OF STRINGER IAW SRM 53-10-74. LOCATED AND DRILLED NEW SECTION OF STRINGER IAW SRM 51-40-44, FABBED SPLICE REPAIR IAW SRM 53-10-14. ALODINED REPAIR PARTS IAW SRM 51-21-10, PRIMED AND TOP COATED REPAI R PARTS IAW SRM 51-23-10. INSTALLED NEW STRINGER SECTION AND SPLICE IAW SRM 53-10-14. 2 L 7 2 4F RT A35EU 2007113000232 20071130 00232 NM 2007 11 30 AALA20072214 1 20071115 A 3350 LENS BOEING 737 737823 13844BZ NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 975AN 29549 LGA - EMERGENCY LIGHT AT SEAT 9D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A16WE 2007113000239 20071130 00239 NM 2007 11 30 AALA20072194 1 20071113 A 3350 LENS BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 664AA 25298 MIA - EMERGENCY LIGHT AT OVERHEAD SEAT 5F MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD SEAT 5F. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007113000241 20071130 00241 NM 2007 11 30 AALA20072189 1 20071112 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 652AA 24610 JFK - EMERGENCY LIGHTS AT SEAT ROWS 16 TO 25 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 16 TO 25. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007113000244 20071130 00244 WP 2007 11 30 AALA20072184 1 20071111 A 3230 CABLE DOUG DC9 DC982 3022082 WP COCKPIT DAMAGED A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 246AA 49258 MCI INFLIGHT T2406 - LANDING GEAR WOULD NOT RETRACT. RETRACT HANDLE WOULD NOT RETURN TO RETRACT POSITION. RETURNED TO MCI AND LANDED WITHOUT INCIDENT. REPLACED DAMAGED ANTI-MAGNETIC CABLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007120300005 20071203 00005 NM 2007 12 3 07FDEA04872 1 20071120 A 2810 SKIN DOUG MD11 MD11F 3023600 NM AUX TANK CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 CABIN, AT ABOUT STA 1228 LBL 30 TO LBL 75 UPPER AUX TANK UPPER SKIN FOUND CORRODED. REPAIRED AS PER FEDEX EA. 1-5710-1 17064, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007120300006 20071203 00006 NM 2007 12 3 07FDEA04873 1 20071120 A 2810 SKIN DOUG MD11 MD11F 3023600 NM AUX TANK CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 CABIN, AT ABOUT STA 1234 LBL 18 UPPER AUX TANK UPPER SKIN FOUND CORRODED. REMOVED CORROSION AS PER SRM 51-21-01. 2 L 7 3 4F RT A22WE 2007120300021 20071203 00021 EU 2007 12 3 AALA20072218 1 20071115 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80057 465 JFK - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DO OR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007120300028 20071203 00028 NM 2007 12 3 AALA20072210 1 20071114 A 3350 LENS BOEING 757 757223 1384957 NM CABIN WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 679AN 29589 DFW - EMERGENCY LIGHT AT FLIGHT DECK ENTRY AREA EXIT SIGN DOUBLE ARROW LENS HAD WRITING WORN OFF. REPLACED LENS FOR EME RGENCY LIGHT AT FLIGHT DECK ENTRY AREA EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007120300029 20071203 00029 NM 2007 12 3 AALA20072191 1 20071112 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 352AA 24033 SFO - EMERGENCY LIGHT AT RIGHT AFT GALLEY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT AFT GALLEY. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007120300035 20071203 00035 WP 2007 12 3 AALA20072203 1 20071113 A 3350 LENS DOUG DC9 DC982 3022082 WP CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7535A 49989 DFW - EMERGENCY LIGHT AT SEAT 11D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F A6WE 2007120300043 20071203 00043 EA 2007 12 3 SWIA200718873 1 20071114 A 3350 CHARGER CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 920SW 7660 OVERHEAD, RIGHT SIDE AND FORWARD GALLEY EMERGENCY LIGHTS ARE INOP. REPLACED NR 2 EMERGENCY LIGHT CHARGER ASSEMBLY IAW A MM 33-52-04. 2 L 7 2 4F RT A21EA 2007120300045 20071203 00045 EA 2007 12 3 SWIA200718875 1 20071113 A 3350 RELAY CNDAIR CL600 CL6002C10 1390015 EA CABIN MALFUNCTIONED A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 760SK 10223 EMERGENCY LIGHTS FLASH ON AND OFF IN THE ARMED POSITION, FLIGHT NR 6632. INSTALLED RELAY K135 IN JB11 PER MM 24-06-00. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007120300046 20071203 00046 EA 2007 12 3 SWIA200718876 1 20071115 A 3350 RELAY CNDAIR CL600 CL6002C10 1390015 EA CABIN MALFUNCTIONED A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 750SK 10207 EMERGENCY LIGHTS CYCLE ON AND OFF WHEN SWITCH IS IN THE "ARM" POSITION. REPLACED RELAY K135. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007120300047 20071203 00047 2007 12 3 SWIA200718877 4 20071113 A 2360 BONDING STRAP EMB 120 EMB120ER 3260203 SO AILERON DAMAGED A SWIA O OTHER F FLT CONT AFFECTED UK UNKNOWN 1 NM 07 586SW 120354 FLT 5543 - AILERON MOVEMENT DOES NOT FEEL CORRECT. REPLACED RIGHT AILERON BONDING STRAP. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007120300052 20071203 00052 EA 2007 12 3 SWIA200718882 1 20071115 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY MALFUNCTIONED A SWIA O OTHER N FALSE WARNING UK UNKNOWN 1 NM 07 939SW 7742 CARGO SMOKE TRIPLE CHIME WARNING. REPLACED FORWARD CARGO SMOKE DETECTOR IAW CRJ 200 MM, PN: 473597-19 S/N OFF: 3245. 2 L 7 2 4F RT A21EA 2007120300055 20071203 00055 SO 2007 12 3 SWIA200718885 1 20071116 A 3397 WIRE EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 218SW 120287 FORWARD FLOOR EMERGENCY LIGHTS ARE INOP. REPAIRED WIRING AT FORWARD FLOOR LIGHTING STRIP. 2 L 7 2 4T RT A31SO 2007120300057 20071203 00057 SO 2007 12 3 SWIA200718887 1 20071116 A 3350 SIGN EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 290SW 120317 FORWARD EMERGENCY EXIT SIGN IS INOP, FLIGHT NR 5424. REPLACED EMERGENCY EXIT SIGN. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007120300064 20071203 00064 NM 2007 12 3 QXEA200701734 1 20071118 A 5320 THRESHOLD BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 C4 PDX - CORROSION UNDER THE EMERGENCY EXIT DOOR THRESHOLD IN THE AREAS OF THE LOWER DOOR LATCH PLATES. REPAIRED IAW SR M 51-40-07, 51-42-15. 2 H 7 2 4T RT A13NM 2007120300065 20071203 00065 NM 2007 12 3 QXEA200701731 1 20071120 A 5320 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 C4 PDX - SMALL NICK ON EXTERNAL FUSELAGE LOCATED AT STATION 3.00 JUST BELOW STRINGER 31L. REPAIRED IAW RD8/4-53-505, RD 8/4-53-2136. 2 H 7 2 4T RT A13NM 2007120300068 20071203 00068 NM 2007 12 3 QXEA200701738 1 20071117 A 5320 TIE CLIP BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 C4 PDX - FUSELAGE FRAME X196.000 TIE CLIP TO STRINGER 24R AT AFT SIDE OF FRAME IS CORRODED. REPAIRED IAW SRM 53-20-43, 51-42-05, AND 53-20-15. 2 H 7 2 4T RT A13NM 2007120300069 20071203 00069 NM 2007 12 3 QXEA200701739 1 20071116 A 5320 TIE CLIP BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 C4 PDX - FUSELAGE FRAME X489.500 TIE CLIP TO FUSELAGE SKIN AT FORWARD SIDE IS CORRODED. REPAIRED IAW SRM 51-42-05, 53-2 0-15, 51-21-10. 2 H 7 2 4T RT A13NM 2007120300070 20071203 00070 NM 2007 12 3 QXEA200701740 1 20071115 A 5320 TIE CLIP BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 C4 PDX - SUSPECTED CORROSION AROUND LOWER RIVET OF TIE CLIP ON BACK SIDE OF FRAME X216.000 TO FUSELAGE JUST ABOVE STRING ER 24P. REPAIRED IAW SRM 51-42-05, 53-20-15, 51-25-10. 2 H 7 2 4T RT A13NM 2007120300071 20071203 00071 NM 2007 12 3 QXEA200701742 1 20071115 A 5240 HINGE FITTING BOMBDR DHC8 DHC8402 1390042 NM AFT SERVICE DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 C4 PDX - AFT SERVICE DOOR APETURE MAIN HINGE FITTINGS HAVE CHAFING ON OUTBOARD EDGES. REPAIRED IAW SRM 51-21-10, 51-25- 65. 2 H 7 2 4T RT A13NM 2007120300072 20071203 00072 NM 2007 12 3 QXEA200701737 1 20071115 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 C4 PDX - RIGHT INBOARD SEAT TRACK NR 16 HAS CORROSION ON THE TOP SURFACES STATIONS X670 TO X700. REPAIRED IAW RD8/4-53- 884 AND SRM 51-40-15. 2 H 7 2 4T RT A13NM 2007120300073 20071203 00073 NM 2007 12 3 QXEA200701743 1 20071115 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 C4 PDX - POSSIBLE SURFACE CORROSION AND PAINT MISSING ON EXTERNAL FUSELAGE JUST AFT AND BELOW LAV SERVICE DOOR. REPAIRE D IAW SRM 51-14-00, 51-25-10, 51-25-15. 2 H 7 2 4T RT A13NM 2007120300074 20071203 00074 NM 2007 12 3 QXEA200701744 1 20071115 A 5320 STRUCTURE BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 C4 PDX - CORROSION FOUND AT LAV SERVICE COMPARTMENT LOWER AFT INTERNAL LIP. REPAIRED IAW RD8/4-53-347. 2 H 7 2 4T RT A13NM 2007120300076 20071203 00076 NM 2007 12 3 QXEA200701746 1 20071115 A 5320 STRAP BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 C4 PDX - TIE STRAP HAS LIGHT CORROSION AT STATION X89.0 ON TOP OF INTERCOSTAL STRINGER 24R. REPAIRED IAW SRM 51-14-00, 51-21-00, AND 51-42-05. 2 H 7 2 4T RT A13NM 2007120300078 20071203 00078 NM 2007 12 3 QXEA200701748 1 20071115 A 5320 STRAP BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 C4 PDX - TIE STRAP HAS LIGHT CORROSION AT STATION X77 ON TOP OF INTERCOSTAL STRINGER 24R. REPAIRED IAW SRM 51-42-05. 2 H 7 2 4T RT A13NM 2007120300079 20071203 00079 WP 2007 12 3 UPS07851189 1 20071116 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 811UP 46089 FOUND EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK AND OPS CK IAW MM 33-50-01. 2 L 7 4 4F RT 4A25 2007120300080 20071203 00080 2007 12 3 UPS07851190 4 20071119 A 2565 SLIDE DOUG DC8 DC873F 302199F WP PAX DOOR UNWANTED DEPLOY A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 GROUND CREW OPENED ENTRY DOOR FROM OUTSIDE REMOVING ESCAPE SLIDE FROM COVER NEEDS REPACKING. REINSTALLED SLIDE IAW DC8 MM 25-60-01-2. 2 L 7 4 4F RT 4A25 2007120300081 20071203 00081 NM 2007 12 3 UPS07M51191 1 20071120 A 2560 BATTERY DOUG MD11 MD11F 3023600 NM EVAC SLIDE DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 251UP 48744 LT ENTRY DOOR SLIDE BOTTLE TEST BUTTON DIM WHEN TESTED. REMOVED AND REPLACED LT ENTRY DOOR SLIDE PUSH TO TEST BATTERY A ND OPS CHECKS OK PER MM 25-61-06. A/C OK TO CONTINUE SERVICE. 2 L 7 3 4F RT A22WE 2007120300082 20071203 00082 SW 2007 12 3 WGEA200700025 1 20071119 A 3243 1094 MASTER CYLINDER ECLIPS EA500 ECLIPSEEA500 3350000 SW COPILOT BRAKE MALFUNCTIONED E WGEA K NONE O OTHER LD LANDING 1 EA 27 145DJ 000057 UPON LANDING IN BOCA, COPILOTS (RIGHT SIDE) LEFT BRAKE PEDAL HAD NO PRESSURE OR BRAKING, EVEN AFTER 2 OR 3 PUMPS. SOME BRAKING WAS RESTORED AFTER 5-7 PUMPS ON CAPTAINS LEFT BRAKE PEDAL. SUPPLEMENTAL INFORMATION, REPLACED COPILOTS LT MASTE R CYLINDER WITH A NEW CYLINDER. RETORQED PRESSURE B-NUT IN PEDESTAL FWD AREA. PERFORMED SATISFACTORY BLEED, LEAK, OP' S CHECK OF BRAKE SYSTEM IAW EA 500 M/M 32-41-11, 20-05-00, 32-40-00. 1 L 7 2 4J RT A00002AC 2007120300083 20071203 00083 NM 2007 12 3 07FDEA04729 1 20071107 A 5753 ARC24441 SKIN DOUG MD11 MD11F 3023600 NM T/E FLAP MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 591FE 48527 LEFT WING : INBOARD FLAP OUTBOARD SEGMENT LOWER SURFACE FOUND WITH TWO EACH EXTERNAL EXISTING DOUBLER NOT IN ACCORDANCE WITH SRM REPAIR. LEFT HAND WING : INBOARD FLAP OUTBOARD SEGMENT LOWER SURFACE WITH TWO EACH EXTERNAL EXISTING DOUBLER CARRIED OUT SKIN REPAIR AS PER SRM 57-10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007120300087 20071203 00087 NM 2007 12 3 P5CA0701539 1 20071113 A 5347 ROLLER TRAY BOEING 747 74747UF 1384812 NM CABIN DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 416MC 32838 ROLLER TRAY AND SEAT TRACK DAMAGE M/D STA 1650-1800. REPAIR ROLLER TRAYS AND SEAT TRACK PER XEO NR 53-111407 SRM 51-70- 12 SOYM 20-44-04 2 L 7 4 4F RT A20WE 2007120300088 20071203 00088 NM 2007 12 3 NWAA073815639 1 20071119 A 2612 FIRE LOOP BOEING 757 757251 1384970 NM RT ENGINE MALFUNCTIONED A NWAA F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 539US 26486 AFTER SELECTING CLIMB HAD THRUST R ENGINE FIRE INDICATION, COMPLIED WITH COM PROCEDURE. SHUT DOWN ENGINE, DISCHARGED BO TH FIRE BOTTLES AND INDICATION WENT OUT ON SHORT FINAL. ALL ENGINE INDICATIONS WERE NORMAL. RETURNED TO NRT AND LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED ENGINE FIRE LOOP AND BAD WIRE. OPERATIONAL CHECKED GOOD AND AIRCRAFT HAS RETURNE D TO SERVICE. 2 L 7 2 4F RT A2NM 2007120300089 20071203 00089 NM 2007 12 3 QXEA200701754 1 20071120 A 5210 85217008101 SEAL BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR DEFECTIVE A QXEA K NONE O OTHER CL CLIMB 1 NM 09 405QX 4047 SEA - ON FLIGHT 2392, ON INITIAL CLIMB CABIN WOULD NOT PRESSURIZE. CHECKLIST LED TO THE MANUAL MODE, WHICH WORKED. CAB IN PRESSURE RETURNED TO NORMAL. FLIGHT ATTENDANT IN THE AFT CABIN REPORTED LOUD SQUEAL FROM THE AFT PASSENGER DOOR, WHI CH EVENTUALLY WENT AWAY. MAINTENANCE REMOVED AND REPLACED THE AFT PASSENGER DOOR SEAL. OPERATIONAL CHECK GOOD. AIRCRA FT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007120300092 20071203 00092 NM 2007 12 3 QXEA200701756 1 20071120 A 5230 HANDLE BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR NOT SEATED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 431QX 4164 SMF - ON FLIGHT 2384, DIVERTED FLIGHT, CLIMBING THRU FL220 MASTER WARNING ANNUNCIATED SHOWING FUSELAGE DOOR R1 SHOWED UP ON DOOR PAGE MASTER WARNING INTERMITTENTLY KEPT CYCLING WITH NO CHANGE IN CABIN PRESSURE. MAINTENANCE FOUND CARGO DOOR HANDLE NOT FULLY SEATED IN LOCKED POSITION UPON ARRIVAL. PERFORMED OPERATIONAL TEST OF DOOR AND DOOR WARNING SYSTEM. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007120300093 20071203 00093 NM 2007 12 3 QXEA200701749 1 20071109 A 3233 468305 ACTUATOR BOMBDR DHC8 DHC8402 1390042 NM MLG MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 425QX 7 7 4039 PDX - ON FLIGHT 2431, RETURNED TO GATE, DURING TAKEOFF UPON GEAR RETRACTION, THE RIGHT GEAR DOOR AMBER LIGHT REMAINED IL LUMINATED. THE AMBER LIGHT EXTINGUISHED ON ITS OWN. NORMAL GEAR EXTENSION AND LANDING IN PDX. MAINTENANCE REMOVED AND REPLACED UPLOCK ASSY, UPLOCK PROX SENSORS, MLG DOOR ACTUATOR, MLG AFT DOOR MECHANICAL SEQUENCE VALVE, SOLENOID VALVE, IN LINE RESTRICTORS. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007120300094 20071203 00094 NM 2007 12 3 QXEA200701752 1 20071118 A 2897 WIRE BOMBDR DHC8 DHC8402 1390042 NM FUEL SYSTEM CHAFED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 403QX 4037 SEA - ON FLIGHT 2490, ON TAXI OUT NR 1 FUEL AUX PUMP CIRCUIT BREAKER TRIPPED. MAINTENANCE FOUND WIRES CHAFED. REPAIRED WIRES AND NR 1 AND NR 2 AUX PUMP. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007120300095 20071203 00095 NM 2007 12 3 QXEA200701753 1 20071118 A 5210 DOOR SEAL BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR DIRTY A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 424QX 4006 BOI-ON FLIGHT 2338, AFT PASSENGER DOOR HARD TO OPEN AND CLOSE. MAINTENANCE CLEANED AFT PASSENGER DOOR SEAL. OPERATIONA L CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007120300098 20071203 00098 NM 2007 12 3 748002 1 20071122 A 3220 65B0798785 ACCESS PANEL BOEING 747 747206B 1384856 NM NLG LOOSE A Q2SA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 63 748SA 21110 NOSE LANDING GEAR DOOR OPEN LIGHT ILLUMINATED IN FLIGHT. COMPLETED DOOR OPEN LIGHT PROCEDURES IAW QRH. FOUND LOOSE ACC ESS PANEL AND PARTS BAG OBSTRUCTING RIGHT HAND DOOR HINGE. SECURED PANEL AND OPERATIONALLY CHECKED NOSE GEAR DOOR SYSTE M WITH NO FURTHER DISCREPANCIES NOTED. 2 L 7 4 4F RT A20WE 2007120300099 20071203 00099 NE 2007 12 3 MALA070183 2 20071118 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT OVERTEMP A MALA E A ENGINE SHUTDOWN UNSCHED LANDING M OVER TEMP CL CLIMB 1 GL 15 435XJ 340B435 CREW DID NOT SHUT OFF CTOT BEFORE PULLING POWER LEVERS BELOW 64 DEGREE SWITCH AND ENGINE OVERTORQUED/FEATHERED. CREW DEC LARED EMERGENCY AND RETURNED TO PIR. REMOVED AND REPLACED RT ENGINE. 2 L 7 2 4T 4 T RT A52EU E8NE 2007120300100 20071203 00100 SO 2007 12 3 FDKA200708362 1 20070802 A 2560 SIGN EMB 145 EMB145LR 3260212 SO CABIN DETERIORATED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FDM 6051 MCO (1337 PHX LCL) - ROW 12 OVER HEAD AFT EMERGENCY SIGN FALLING APART. MX RESECURED SIGN OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2007120300101 20071203 00101 SO 2007 12 3 FDKA200708364 1 20070802 A 2560 744424 SIGN EMB 145 EMB145LR 3260212 SO CABIN OUT OF POSITION A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FDM 6024 MCO (1757 PHX LCL) - ROW 12 OVERHEAD EMERGENCY EXIT SIGN AFT SIDE FELL OUT. MX REPLACED THE SIGN AND OPS CHECK ED. 2 L 7 2 4T RT T00011AT 2007120300102 20071203 00102 SO 2007 12 3 FDKA200708366 1 20070802 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 852MJ 145567 FDM 6206 ATL (1823 PHX LCL), ROW 16 CEILING EMERGENCY LIGHT WAS INOPERATIVE. MX RELAMPED AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2007120300103 20071203 00103 NM 2007 12 3 FDKA200708367 1 20070803 A 3350 6038443 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 803LR 1773 322 FDM 6208 JFK (1315 PHX LCL) - ALL EMERGENCY LIGHTS WILL NOT SHUT OFF. MX REMOVED AND REPLACED FWD EMERGENCY LIGHT BATTE RY. 2 H 7 2 4T RT A13NM 2007120300104 20071203 00104 NM 2007 12 3 FDKA200708370 1 20070804 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 803LR 1766 322 FDM 6076 JFK-PHL (1447 PHX LCL) - ALL EMERGENCY LIGHTS WILL NOT SHUT OFF. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIE S (8). 2 H 7 2 4T RT A13NM 2007120300109 20071203 00109 SO 2007 12 3 FDKA200708384 1 20070814 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 838MJ 145384 FDM 6036 CLT (0945 PHX LCL) - EMERGENCY EXIT OVERHEAD LIGHT AT ROW 12 INOP. MX RESECURED WIRE. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007120300110 20071203 00110 SO 2007 12 3 FDKA200708386 1 20070814 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6054 ATL-NAS (1742 PHX LCL). RT EMERGENCY LIGHT INOP. MX RELAMPED OPS GOOD. 2 L 7 2 4T RT T00011AT 2007120300112 20071203 00112 SO 2007 12 3 FDKA200708391 1 20070816 A 3350 AD20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 847MJ 914 145517 FDM 6125 MCO (0515 PHX LCL) - ALL EMERGENCY LIGHTS INOP. MX REMOVED AND REPLACED ALL EMERGENCY BATTERY PACKS OPS CK GOO D. 2 L 7 2 4T RT T00011AT 2007120300113 20071203 00113 SO 2007 12 3 FDKA200708392 1 20070816 A 2560 744424 FRAME EMB 145 EMB145LR 3260212 SO EXIT SIGN MISSING A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 842MJ 145457 FDM 6074 ATL (1036 PHX LCL) - RT AND LT ROW 12 EMERGENCY SIGN FRAMES LOOSE/MISSING. MX INSTALLED LIGHT FRAMES. 2 L 7 2 4T RT T00011AT 2007120300114 20071203 00114 SO 2007 12 3 FDKA200708393 1 20070816 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 838MJ 145384 FDM 6172 ATL (1540 PHX LCL) - OVERHEAD EMERGENCY LIGHT AT ROW 12 INOPERATIVE. MX CYCLED LIGHTS AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2007120300115 20071203 00115 SO 2007 12 3 FDKA200708395 1 20070817 A 3350 FRAME EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FDM 6086 MCO (1405 PHX LCL) - RT EMERGENCY LIGHT FRAME LOOSE. MX RE-SECURED FRAME SCREWS. 2 L 7 2 4T RT T00011AT 2007120300117 20071203 00117 SO 2007 12 3 FDKA200708394 1 20070816 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 855MJ 145614 FDM 6029 MCO (1540 PHX LCL) - 12 A EMERGENCY LIGHT INOPERATIVE. MX RELAMPED AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2007120300118 20071203 00118 SO 2007 12 3 FDKA200708416 1 20070821 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 FDM 6093 ROC (1415 PHX LCL) - EMERGENCY EXIT SIGN AFT OF LT EXIT INOP. MX CAN NOT DUPLICATE DISCREPANCY. OPS CHECK GOO D. 2 L 7 2 4T RT T00011AT 2007120300119 20071203 00119 NM 2007 12 3 HALA0700495 1 20071122 A 2913 66180 PUMP BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE RT ENGINE MALFUNCTIONED A HALA K NONE K FLUID LOSS CR CRUISE 1 WP 13 480HA 7607 7607 55125 13320 AIRBORNE - RT HYD QTY LOW LIGHT, WILL BE LANDING ON 8R. WILL DO AN ALT GEAR EXTENSION AND WAIT FOR MAINT AND LINE SERVI CE OUT THERE. CREW DECLARED AN EMERGENCY. LANDED AT HNL, WHERE AN UNEVENTFULL LANDING WAS MADE. T/S RT HYD SYSTEM. R EMOVED AND REPLACED RT ENG HYD PUMP PER AMM 29-11-01. REMOVED AND REPLACED HYD FILTERS PER AMM29-12-12 AS PRECAUTIONARY STEP. OK FOR SERVICE. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007120300120 20071203 00120 NM 2007 12 3 HALA0700496 1 20071122 A 2841 ELECTRONIC UNIT BOEING 767 76733A 1385209 NM FUEL SYSTEM MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM , FUEL QUANTITY MESSAGE DISPLAYED ON EICAS FUEL QTY BITE MAINT MESSAGE. REMOVED AND REPLACED D ENSIOMETER ELECTRONICS UNIT PER AMM28-41-03. OPS AND SECURITY CK AND BITE CK OK. 2 L 7 2 4F RT A1NM 2007120300121 20071203 00121 NM 2007 12 3 HALA0700498 1 20071122 A 3350 BATTERY PACK BOEING 767 76733A 1385209 NM CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 591HA 33423 EMERGENCY FLOOR TRACK LIGHT INOP ROW 20 - 29. REPLACED BATTERY PACK PER MM 33-51-07-022-003-002. FLOOR TRACK LIGHTING ROWS 20-29 LEFT OPS CKS NORMAL. ALL FLOOR "E" PATH LIGHTING OP CKS NORMAL. 2 L 7 2 4F RT A1NM 2007120300122 20071203 00122 2007 12 3 HALA0700497 4 20071122 A 2310 TRANSCEIVER BOEING 767 7673G5 1385126 NM NR 1 HF COMM MALFUNCTIONED A HALA K NONE O OTHER NR NOT REPORTED 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, NR 1 HF INOP. REPLACED LT TRANSCEIVER PER MM 23-11-03-424 CKS GOOD. XMIT AND RECEIVE "LOUD A ND CLEAR " SFO 5.574. 2 L 7 2 4F RT A1NM 2007120300124 20071203 00124 SO 2007 12 3 135632112407 2 20071124 A 8500 TSIO520VB ENGINE CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO RIGHT FAILED E HYIA O OTHER T Y ENGINE CASE PENETRATION ENGINE STOPPAGE CL CLIMB 1 EA 61 26632 340 402C0404 832076R ON TAKEOFF FROM MAZ, AT 2400 FEET AND CLIMBING TO 3500 FEET, PILOT HEARD LOUD BOOM WITH RIGHT ENGINE SHUT DOWN AND PROPE LLER FEATHERING. THE PILOT PERFORMED ENGINE FAILURE FLOW CHECK LIST AND RETURNED TO MAZ. PRELIMINARY INSPECTION SHOWS CATASTROPHIC FAILURE OF THE RIGHT ENGINE. MAINTENANCE WILL BE REMOVING AND REPLACING THE ENGINE. ENGINE WILL BE SENT T O TCM FOR TEARDOWN AND INSPECTION. 1 L 7 2 3O 3 O A7CE E8CE 2007120300127 20071203 00127 EU 2007 12 3 1218342112107 1 20071004 A 2611 FR3212 SMOKE DETECTOR AEROSP ATR42 ATR42320 8680930 EU CARGO ABY FAILED A HYIA K NONE L NO TEST IN INSP/MAINT 1 EA 61 14834 193 AFT CARGO SMOKE LIGHT REMAINED OFF DURING SMOKE DETECTION TEST. REMOVED AND REPLACED SMOKE DETECTOR. 2 H 7 2 4T RT A53EU 2007120300128 20071203 00128 EU 2007 12 3 1218343112107 1 20070916 A 3350 3011180A BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A HYIA K NONE L NO TEST IN INSP/MAINT 1 EA 61 14834 193 ALL EMERGENCY LIGHTING DID NOT WORK IN THE ARM POSITION. REMOVED AND REPLACED EMERGENCY BATTERY PACK. EMERGENCY LIGHTI NG TESTED SATISFACTORY 2 H 7 2 4T RT A53EU 2007120300130 20071203 00130 EU 2007 12 3 1218345112107 1 20070821 A 5753 S5751067000400 FITTING AEROSP ATR42 ATR42320 8680930 EU T/E FLAP CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 14834 193 FOUND LEFT WING FLAP ARM AT RIB 23 IS CORRODED. REPLACED LEFT WING FLAP ARM AT RIB 23. 2 H 7 2 4T RT A53EU 2007120300131 20071203 00131 EU 2007 12 3 1218346112107 1 20070821 A 5753 S5751066000400 FITTING AEROSP ATR42 ATR42320 8680930 EU T/E FLAP CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 14834 193 LEFT WING OUTBOARD FLAP RIB 1O ARM CORRODED. REMOVED AND REPLACED LEFT WING OUTBOARD FLAP ARM AT RIB 10. 2 H 7 2 4T RT A53EU 2007120300132 20071203 00132 EU 2007 12 3 1218347112107 1 20070821 A 5753 S5751065400400 FITTING AEROSP ATR42 ATR42320 8680930 EU T/E FLAP CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 14834 193 LEFT WING INBOARD FLAP RIB 9 ARM CORRODED. REMOVED AND REPLACED LEFT INBOARD FLAP ARM AT RIB 9. 2 H 7 2 4T RT A53EU 2007120300135 20071203 00135 EU 2007 12 3 TRBA2007103 1 20071123 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU CABIN DISCHARGED A TRBA K NONE O OTHER UK UNKNOWN 1 SO 29 322AC 320 EMERGENCY LIGHT OUT LEFT EXTERIOR FORWARD OF EMERGENCY EXIT. REMOVED AND REPLACED EMERGENCY EXIT POWER SUPPLY AS PER MM 33-51-21. 2 H 7 2 4T RT A53EU 2007120300136 20071203 00136 SO 2007 12 3 2000SIMA33008 1 20071121 A 2120 P1163 HOSE EMB 135 EMB135KL 3260302 SO A/C BAY DEFECTIVE A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 837AE 145647 PACK 1 FAIL EICAS MSG DID NOT HAVE ENOUGH FUEL TO CONTINUE ON TO CVG ELECTED TO DO AN AIR RETURN TO DFW DISC-SHORTLY AFT ER TAKEOFF, NR 2 BLEED AND PACK VALVE CLOSED ANNUNCIATED ON THE EICAS. PER AOM; CYCLED BLEED VALVE AND PACK SEVERAL TIM ES. UNSUCCESSFULLY. NR 2 PACK VALVE WOULD NOT STAY OPEN. REMOVED AND REPLACED BLEED HOSE AT DUAL TEMP CONTROL VALVE P ACK OPS CK GOOD IAW EMB 140 AMM 21-20-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007120300137 20071203 00137 SO 2007 12 3 SIMA200733009 1 20071125 A 3412 102AU1AF SENSOR EMB 135 EMB135KL 3260302 SO NR 1 TAT FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 21 835AE 145634 TAT 1 HEAT INOP AFTER TAKEOFF. REMOVED AND REPLACED NR 1 TAT SENSOR IAW EMB 140 AMM 34-45-03. OPS CK GOOD AT THIS TIME . AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT T00011AT 2007120300138 20071203 00138 2007 12 3 SWAA075840 4 20071125 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 272WN 32527 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007120300143 20071203 00143 NM 2007 12 3 SWAA075851 1 20071126 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM EVAC SLIDE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FIT TING PER MM. 2 L 7 2 4F RT A16WE 2007120300144 20071203 00144 NM 2007 12 3 SWAA075852 1 20071126 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM EVAC SLIDE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FIT TING PER MM. 2 L 7 2 4F RT A16WE 2007120300148 20071203 00148 NM 2007 12 3 SWAA075865 1 20071126 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007120300149 20071203 00149 NM 2007 12 3 SWAA075866 1 20071122 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007120300150 20071203 00150 NM 2007 12 3 SWAA075868 1 20071120 A 5755 654645262A SKIN BOEING 737 7373H4 1384600 NM NR 4 SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED C2 CHECK, FOUND LT WING NR 4 GROUND SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PE R MM. 2 L 7 2 4F RT A16WE 2007120300151 20071203 00151 NM 2007 12 3 DHL2007765001 1 20071124 A 5320 WEB BOEING 727 727264 138408M NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 A-8 CHECK REF N/R 054239 AFT AIRSTAIR AREA LT TORQUE BOX AT STA 1263 LWR LIGHTING HOLE SKIN HAS 1 INCH CRACK AT 11:00 PO SITION. CUT OUT DAMAGED AREA AT AFT AIRSTAIRS AREA LT TORQUE BOX STA 1263 LWR LIGHTING HOLE SKIN DIMENSION 3/4" BY 1/4" IAW B727 SRM 51-40-2 FIG 1. FABRICATED WEB REPAIR MATERIAL USED 7075-T6 .032 PO NR 9006027 DIM 4" BY 2 1/2" IAW B727 S RM 53-10-2 FIG 6 AND 51-40-2 FIG 1 AND 51-30-5. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED NEW WEB REPAIR AT S TA 1263 LIGHTING HOLE IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2007120300152 20071203 00152 GL 2007 12 3 SIMA200733010 2 20071125 A 7200 CAE3007A1 ENGINE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL RIGHT MALFUNCTIONED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 808AE 145519 CAE312533 AFTER DEPARTURE OBSERVED SMELL OF BURNING RUBBER IN THE COCKPIT AND F/A VERIFIED SMELL IN GALLEY PASSENGER COMPARTMENT. CREW RETURNED TO THE BLOCK. REMOVED AND REPLACED RIGHT ENG IAW EMB WCNR 71-000-00 AND OPS CHECK WAS DONE PER WORK CAR D NR 72-700-00. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007112900203 20071129 00203 NM 2007 11 29 AMTA200700552 1 20071021 A 3350 D71702001 POWER SUPPLY BOEING 737 73783N 13844HI NM EMERGENCY LIGHTS UNSERVICEABLE A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 319TZ 30643 RT SIDE AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT, NO HELP REMOVED AND REPLACED POWE R SUPPLY AT SEAT ROW 19DEF CARPET RISER. OPS CHECK NORMAL IAW MM 33-55-1-06-2. (K) 2 L 7 2 4F RT A16WE 2007113000010 20071130 00010 NM 2007 11 30 AALA20072170 1 20071108 A 3350 102160036 CAPACITOR BOEING 767 767223 1385123 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 327AA 22327 JFK - EMERGENCY LIGHT AT MID GALLEY MISSING CAPACITOR. REPLACED CAPACITOR FOR EMERGENCY LIGHT AT MID GALLEY. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007113000014 20071130 00014 CE 2007 11 30 DJFA2007120 1 20071019 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 417LX 7110 RK230 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THI S AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. MAINTENANCE REPLACED BOTH RIB ASSEMBLIES WITH THE IMPROVED ASSEMBLIES. 2 H 7 2 4F 4 F RT A16SW E25EA 2007113000037 20071130 00037 NM 2007 11 30 2007UALA04667 1 20071113 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 DOOR 4 RIGHT SILL EMERGENCY LIGHT FWD IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007113000040 20071130 00040 NM 2007 11 30 2007UALA04670 1 20071112 A 5311 FRAME BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 181UA 25278 DOORWAY 5L FWD FRAME TORQUE TUBE COVER FRAME CRACKED AT STR 23L-25L. MAJOR REPAIR ACCOMPLISHED: REPLACED FRAME SECTION . 2 L 7 4 4F 4 F RT A20WE E24NE 2007113000042 20071130 00042 NE 2007 11 30 2007UALA04673 2 20071111 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 SHUTDOWN A UALA D RETURN TO BLOCK Y ENGINE STOPPAGE TX TAXI/GRND HDL 1 WP 29 215UA 30221 777012 NR 1 ENGINE JUST SHUT DOWN ON TAXI OUT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007113000060 20071130 00060 NM 2007 11 30 2007UALA04693 1 20071114 A 3520 DOOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE PAX O2 SYSTEM MALFUNCTIONED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 521UA 24891 DURING AUTO DEPLOYMENT OF PASS O2 SYSTEM THE FOLLOWING DOORS DID NOT OPEN 14ABC, 14DEF, AND 16 DEF. 2 L 7 2 4F 4 F RT A2NM E17NE 2007113000095 20071130 00095 EU 2007 11 30 10252007 1 20071024 A 5302 SKIN BOLKMS BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE TAILBOOM CRACKED E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 1140H 7078 7078 DURING DAILY INSPECTION, A 1 INCH LONG CRACK WAS DISCOVERED ON A TAIL BOOM SHEET METAL DOUBLER, LT SIDE, JUST AFT OF THE HORIZONTAL STABILIZER. 1 G 7 2 3U 3 U H13EU E5NE 2007113000127 20071130 00127 EU 2007 11 30 07FDEA04837 1 20071118 A 5347 R538D104820200 ADAPTER AIRBUS 310 A310203 3930313 EU SEAT TRACK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 CARGO TIE DOWN ADAPTER CRACKED AT FRAME 44 (STA 2824) BL36R (-Y900) REMOVED CRACKED TIE DOWN ADAPTER IAW A310-200 SRM 51 -40-21 PAR 5. RECIEVED NEW CUSTOMER FURNISHED PART NR R538D104820200 P/O NR 597285.1. INSTALLED NEW CARGO TIE DOWN A DAPTER IAW A310-200 SRM 51-40-21 PAR 5. 2 L 7 2 4F RT A35EU 2007113000129 20071130 00129 EU 2007 11 30 07FDEA04839 1 20071118 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT PIT STRINGER 50R CORRODED AT FRAME 59. REMOVED CORROSION IAW A310 SRM 51-74-10 FOUND TO BE OUT OF LIMITS IAW A310 S RM 53-10-00 UT GUAGE T 8225B. REMOVED DAMAGED SECTION OF STRINGER IAW A310 SRM 53-10-14 FIG 201. FABRICATED REPAIR COUPL ING AND LOCATED AND DRILLED STRINGER SECTION IAW A310 SRM 53-10-14 FIG 201. ALODINED REPAIR PARTS IAW A310 SRM 51-23-1 0. PRIMED REPAIR PARTS IAW A310 SRM 51-23-10 PAINTED REPAIR PARTS IAW A310 SRM 51-23-10. INSTALLED REPAIR AND STRING ER SECTION IAW A310 SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007113000135 20071130 00135 WP 2007 11 30 07FDEA04847 1 20071119 A 5522 NLC60391 SKIN DOUG DC10 DC1030F 3023504 WP LT ELEVATOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 LT INBD ELEVATOR OUTER RIB WITH 1/4" CRACK ON RIB AND LOWER SKIN. 2 L 7 3 4F RT A22WE 2007113000150 20071130 00150 SO 2007 11 30 GLBA20061019 1 20071029 A 5712 RIB EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT WING CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 96ZK 120096 MAJOR REPAIR RIB CRACKED AT LWS YA 6750. MX REPAIRED CRACKED RIB AT WS 6750 IAW EMB 120 SRM 57-20-07. CRACK APPROXIMAT ELY .375 RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A31SO E20NE 2007113000154 20071130 00154 CE 2007 11 30 GUUA10270701 1 20071027 A 5520 1016200111BM HINGE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 53545 UE185 REPORT: DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLAC ED LT OB ELEVATOR HINGE BRACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 2007113000159 20071130 00159 WP 2007 11 30 07FDEA04850 1 20071119 A 5511 ALC73081 SPAR CAP DOUG DC10 DC1030 3023501 WP HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 308FE 48297 DURING SPAR CAP INSP, FOUND 1 1/2 INCH CRACK. ACCOMPLISHED EA 8-5510-111624. 2 L 7 3 4F A22WE 2007113000182 20071130 00182 EU 2007 11 30 SIMA200732403 1 20071112 A 5347 7253743407 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 307AE 21265 5000 340B307 DURING MBV, THE SEAT TRACK AT BL36L WAS FOUND TO BE CORRODED. REPLACED SEAT TRACK IAW SAAB SRM 53-70-60. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007113000187 20071130 00187 CE 2007 11 30 JAS2007F00000 1 20071012 A 2913 MS287786 PACKING RAYTHN 390 390 7150030 CE WILINT FJ44 FJ442A GL HYD PUMP FAILED A JASA O OTHER J WARNING INDICATION CR CRUISE 1 WP 09 408J RB193 (CONTROL NR JAS-SDR-OO1) FLUCTION OF HYDRAULIC PRESSURE. DEFECTIVE/DAMAGED PN MS28778-6 PACKING. FLIGHT CREW COMPLETED ABNORMAL CHECKLIST. UPON INSPECTION, FOUND THAT PACKING AT HYDRAULIC PUMP PRESSURE OUTLET FITTING HAD FAILED. THIS CO MPONENT WAS WORKED ON IAW COMMUNIQUE 280, ON JULY 9, 2007. AFT 49.9 HRS 68 CYCLES 1 L 7 2 3F 4 F RT A00010WI E3GL 2007113000200 20071130 00200 NM 2007 11 30 DL764071498 1 20071110 A 3350 BATTERY PACK BOEING 767 767432ER 1385134 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 836MH 29709 FUSELAGE EXT SURFACE, EMERGENCY EXIT LIGHT INOP AT R1, R2, L2 AND AFT OF LT/RT. RESTORED EMERG LIGHT BATT PACKS IAW B76 7-400 MM 33-51-07-612-003. LIGHTS AT R1, R2, L2 AND AFT OF LT/RT WING. OPS CHECKS GOOD B767-400 MM 33-51-07-612-003. 2 L 7 2 4F RT A1NM 2007113000236 20071130 00236 EU 2007 11 30 AALA20072222 1 20071115 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80057 465 JFK - EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007120300009 20071203 00009 WP 2007 12 3 07FDEA04877 1 20071120 A 5311 ADA007617 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON FRAME CAP AT STA 879 BETWEEN LONG NR 47R AND 47L WAS FOUND NOT IN COMPLIANCE WITH APPROVED DATA. REPAIR HAS BEEN REPLACED WITH A NEW IAW SRM 53-30-00, FIG 5, VOL I. 2 L 7 3 4F A22WE 2007120300013 20071203 00013 NE 2007 12 3 AALA20072198 2 20071113 A 7230 COMPRESSOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LT ENGINE STALLED A AALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 21 458AA 49563 725910 LAX INFLIGHT T458/13NOV - AIRCRAFT RETURNED TO LAX DUE TO NUMBER ONE ENGINE COMPRESSOR STALLS. NUMBER ONE ENGINE REDUCE D TO IDLE. OIL TEMPERATURE WAS IN YELLOW BAND. LANDED LAX WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE ON 13 NOV AT L AX. REPLACED LEFT ENGINE ISOLATORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007120300017 20071203 00017 WP 2007 12 3 AALA20072200 1 20071113 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7535A 49989 DFW - EMERGENCY LIGHT AT SEAT 8D INOPERATIVE. REPLACED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 8D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007120300022 20071203 00022 EU 2007 12 3 AALA20072219 1 20071115 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80057 465 JFK - EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007120300031 20071203 00031 WP 2007 12 3 AALA20072193 1 20071112 A 3350 GUARD DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 560AA 53090 DFW - EMERGENCY LIGHT AT SEAT 17D LENS GUARD DAMAGED. REPLACED LENS GUARD FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007120300044 20071203 00044 EA 2007 12 3 SWIA200718874 1 20071112 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DIRTY A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 957SW 7829 REAR HALF OF THE EMERGENCY LIGHTS DON'T WORK, FLIGHT NR 6505. CLEANED AND SECURED EMERGENCY STRIP CONNECTION. OPS CHEC K GOOD. 2 L 7 2 4F RT A21EA 2007120300048 20071203 00048 SO 2007 12 3 SWIA200718878 1 20071112 A 5210 ROLLER EMB 120 EMB120ER 3260203 SO PAX DOOR OUT OF ADJUST A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 295UX 120295 FLT 5584 - MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN. ADJUSTED UPPER AFT ROLLER ON PAX DOOR FRAME. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007120300061 20071203 00061 NM 2007 12 3 QXEA200701735 1 20071115 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 C4 PDX - LEFT OUTBOARD SEAT TRACK IS CORRODED AT THE SHIM/STOP LOCATIONS BETWEEN X644 AND X688. REPAIRED IAW SRM 51-42- 05, 51-40-15, AND RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007120300075 20071203 00075 NM 2007 12 3 QXEA200701745 1 20071118 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 C4 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 17 CORRODED ON UPPER SURFACE NEAR STATION X712. REPAIRED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 2007120300116 20071203 00116 NM 2007 12 3 FDKA200707339 1 20070717 A 3320 BALLAST DHAV DHC8 DHC8101 2809002 NM CABIN MALFUNCTIONED A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 809LR 083 FDM 6023 JFK-BWI (1544 PHX LCL) - CAPTAIN REPORTED BURNING SMELL IN REAR CABIN. REMOVED AND REPLACED ROW 7DF SIDEWALL BALLAST AND OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2007120300139 20071203 00139 NM 2007 12 3 SWAA075839 1 20071125 A 2560 6557463 FITTING BOEING 737 7377H4 1384404 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 272WN 32527 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2007120300140 20071203 00140 NM 2007 12 3 SWAA075871 1 20071126 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 384, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007120300141 20071203 00141 NM 2007 12 3 SWAA075870 1 20071126 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259, STR 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007120300146 20071203 00146 NM 2007 12 3 SWAA075863 1 20071126 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, STR 17L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007120300147 20071203 00147 NM 2007 12 3 SWAA075872 1 20071126 A 5312 6545819 PRESSURE PANEL BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED MV2 CHECK, FOUND LT NLG W/W CEILING PANEL CRACKED AT BS 257.8. REPAIRED PANEL PER SWA EA. 2 L 7 2 4F RT A16WE 2007120300153 20071203 00153 SO 2007 12 3 SIMA200733012 1 20071124 A 3610 8166101 VALVE EMB 145 EMB145LR 3260212 SO BLEED AIR SYS MALFUNCTIONED A SIMA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 SW 21 640AE 145183 IN ICE CONDITION, NR 1 BLEED OVER TEMP WARNING. REMOVED AND REPLACED NR 1 FAN AIR VALVE IAW EMB 145 AMM 36-11-03. OPS GOOD AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007120300154 20071203 00154 SO 2007 12 3 SIMA200733004 1 20071123 A 4920 M4504113A APU EMB 145 EMB145LR 3260212 SO FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 643AE 145200 EXPERIENCED SMOKE IN THE CABIN AND COCKPIT. IT OCCURRED AFTER A COUPLE OF MINUTES OF STARTING THE APU CREW TURNED ON NR 2 PACK AND CROSS BLEED OPEN. WITHIN 30 SECONDS SMOKE APPEARED IN THE CABIN AND COCKPIT. THE FO TURNED OFF THE PACK AN D CROSS BLEED. SMOKE IMMEDIATELY DISSIPATED. SOON AFTER THE SMOKE APPEARED THE APU FAILED AND SHUT DOWN. ON APU/OPS C HECKED PACKS, NO SMOKE. REMOVED AND REPLACED APU IAW AEWC 49-800-05 LEAK AND OPS CHECK GOOD IAW CMM 49-00-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007120300157 20071203 00157 SO 2007 12 3 SIMA200733007 1 20071119 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LAVATORY SMOKE A SIMA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 933JN 14500918 AFTER TAKEOFF "LAV SMOKE WARNING" ODOR OF SMOKE IN COCKPIT AND CABIN FLIGHT ATTENDANT VERIFIED NO FIRE IN LAV BUT COULD STILL ODOR SMOKE. CW GVI OF LAV SIDE WALL AND IN THE LAV GVI OF ENGINE AND RAN BOTH ENGINE TO TAKE POWER. ALL CHECK GO OD AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007120300159 20071203 00159 NM 2007 12 3 QXEA200701757 1 20071119 A 2434 23088008 GENERATOR DHAV DHC8 DHC8202 2809007 NM NR 2 INOPERATIVE A QXEA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 346PH 1381 1381 477 SEA - ON FLIGHT 2199, NR 2 DC GENERATOR HOT CAUTION LIGHT ILLUM. DURING TAXI, FLICKERING ON AND OFF THE ENTIRE TIME. C ONDUCTED CHECKLIST AND UPON TURNING OFF THE DC GENERATOR SWITCH, THE CAUTION LIGHT WENT OUT. MAINTENANCE REMOVED AND RE PLACED NR 2 DC GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007120400001 20071204 00001 EU 2007 12 4 TRBA2007104 1 20071123 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHTS INOPERATIVE A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 550LL 550 AFTER ENGINE START, TESTED EMERGENCY LIGHT/CAPT REPORTED HALF OF SYSTEM NOT ILLUMINATING. REMOVED AND REPLACED BATTERY PACK AT EMERGENCY LIGHT POWER SUPPLY FIN 73WL IAW JIC 33-50-00. OPT CK GOOD IAW JIC 33-50-00. 2 H 7 2 4T RT A53EU 2007120400002 20071204 00002 NE 2007 12 4 DHLA200700066 2 20071120 A 7200 ENGINE BOEING 727 7272Q9 138448M NM PWA JT8 JT8D17 52049 NE NR 2 MALFUNCTIONED A DHLA E ENGINE SHUTDOWN J E WARNING INDICATION VIBRATION/BUFFET CR CRUISE 1 GL 05 741DH 43288 1885 21931 702653 FLT 594 IN CRUISE FL 320 CLEAR CONDITIONS NR 2 ENGINE PARAMETERS STARTED TO FLUCTUATE ALONG WITH SEVERE VIBRATION, PERFO RMED ABNORMAL PROCEDURE OBSERVED NR 2 OIL QTY GO TO ZERO AND PERFORMED ENG SHUTDOWN ABNORMAL PROCEDURE UPON LANDING OIL QTY RETURNED TO NORMAL AFTER ENG SHUTDOWN OIL PRESS WAS AT REDLINE. REMOVED AND REPLACED NR 2 ENG PER MTM 71.2, RAN ENG PER JRH. PERFORMED MPA AND RUN SHEET NR 2 ENG, OK FOR SERVICE. AIRCRAFT WAS GROUNDED 2 L 7 3 4F 4 F RT A3WE E2EA 2007120400007 20071204 00007 EA 2007 12 4 CHQA200700080 1 20071121 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE WING MALFUNCTIONED A CHQA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 GL 11 645BR 7383 GEE872681 CLE TO MSP - ON APPROACH FLAPS FAILED AT ZERO DEGREES. CREW RAN QRH WHILE RECEIVING VECTORS FROM ATC AND THE AIRCRAFT L ANDED WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE FECU FOR MESSAGES, FOUND NONE, AND RESET THE FLAP SYSTEM. AFTER R ESETTING, THE FLAP SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2007120400013 20071204 00013 SO 2007 12 4 CHQA200700082 1 20071123 A 7722 23073461125 CLAMP EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 ENGINE MISSING A CHQA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 GL 11 263SK 145199 CAE311771 IAH TO STL - DURING CLIMB-OUT WHILE PASSING THROUGH 9,000 FT, THE FLIGHT CREW NOTICED THE NR 2 ENGINE ITT WAS AMBER WITH AN INDICATION OF 905C AND CLIMBING. THE POWER WAS REDUCED IMMEDIATELY AND THE QRH WAS EMPLOYED FOR TROUBLESHOOTING. A S A RESULT THE POWER WAS REDUCED TO MAINTAIN ITT AT AN ACCEPTABLE LEVEL. IT WAS ALSO NOTED THAT THE ENGINE NR 2 FUEL FL OW WAS SIGNIFICANTLY HIGHER THAN ENGINE NR 1. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NR 2 ENGINE AND FOUND THE V-BAND DISCHARGE CLAMP MISSING FROM THE DISCHARGE TUBE. MAINTENANCE REPLACED T HE MISSING V-BAND CLAMP AND RAN THE ENGINES WITH NO FURTHER DEFECTS NOTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007120400016 20071204 00016 NM 2007 12 4 UPS07551197 1 20071124 A 3350 LIGHT BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 401UP 23723 NUMEROUS EMERGENCY EXIT LIGHT BULBS INOP. RELAMPED PER AMM 33-51-01-2. OPS CHECK NORMAL. 2 L 7 2 4F RT A2NM 2007120400017 20071204 00017 NM 2007 12 4 UPS07M51200 1 20071122 A 2560 GIRT BAR DOUG MD11 MD11F 3023600 NM ENTRY DOOR DETACHED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 279UP 48573 RIGHT SIDE ENTRY DOOR GIRT BAR NEED TO BE REATTACHED FORWARD END. REATTACHED RIGHT SIDE DOOR GIRT BAR AS REQUIRED PER M M 25-61-01-42-00. OPS CHECK NORMAL. 2 L 7 3 4F RT A22WE 2007120400018 20071204 00018 NM 2007 12 4 UPS07M51201 1 20071123 A 3350 6044115 BATTERY DOUG MD11 MD11F 3023600 NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 276UP 48579 EMERGENCY LIGHT TEST GIVES BAT 1 LOW FAULT. T/S CARRIED OUT IAW FIM 33-51-02-00. REPLACED BATTERY 1 IAW MM 33-51-01. C/O MSC RTS TEST IAW MM 31-42-01. EMERGENCY LIGHT TEST PASS. 2 L 7 3 4F RT A22WE 2007120400019 20071204 00019 NM 2007 12 4 QXEA200701762 1 20071123 A 2434 GENERATOR BOMBDR DHC8 DHC8402 1390042 NM NR 1 MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 418QX 4143 SJC FLIGHT NR 2452: NR 1 DC GEN CAUTION LIGHT ILLUMINATED AFTER START. EXTERNAL POWER KICKED OFF DURING START. AIRCRAF T RETURNED TO BLOCK. MAINTENANCE POWERED A/C DOWN AND REPOWERED/RESTARTED GEN. ALL OPERATE NORMALLY AS PER MTX CONTROL . NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007120400020 20071204 00020 NM 2007 12 4 DU4R2007187 1 20071116 A 5230 RIB BOEING 757 757232 1384965 NM CARGO DOOR DENTED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 6715C 30486 C-2 DOOR FORMER RIB DENTED, NR 5 AFT TO FWD, LWR INBD SECTION AT LINER SNAP. CUT OUT DENTED RIB, FABRICATED AND INSTALL ED REPAIR RIB 8-1/2 BY 4-1/2 FROM 0775-T6 .050 IAW B757 SRM 51-10-02, PARA 8, 51-40-02, 52-40-02 FIG 1 AND 51-20-01. 2 L 7 2 4F RT A2NM 2007120400021 20071204 00021 NM 2007 12 4 HALA0700499 1 20071124 A 3010 3003654 ANTI-ICE VALVE BOEING 767 767332 1382001 NM LT WING MALFUNCTIONED A HALA K NONE J WARNING INDICATION CR CRUISE 1 WP 13 598HA 39722 39722 23278 ETOPS SIGNIFICANT SYSTEM, WITH WING ANTI-ICE SW ON EICAS MSG L WING ANTI ICE DISPLAYED. RESPECTED VALVE LIGHT ILLUMINAT ED. REMOVED AND REPLACED LT WING TAI VALVE PER AMM 30-11-02-404. OPS CHECKS GOOD. 2 L 7 2 4F RT A1NM 2007120400022 20071204 00022 NM 2007 12 4 HALA0700502 1 20071124 A 4920 APU BOEING 767 76733A 1385209 NM MALFUNCTIONED A HALA K NONE J WARNING INDICATION NR NOT REPORTED 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM, APU FAILED TO START. FAULT LIGHT ILLUM AND EICAS MSG APU FAULT DISP ADDITIONAL START ATTEMPTS UNSUCCESSFUL. PERFORM BIT CHECK ON ECU. NO FAULTS NOTED. RUN APU OP CHECK NORMAL. NO DEFECTS NOTED. PER FIM 49-11- 00. 2 L 7 2 4F RT A1NM 2007120400024 20071204 00024 2007 12 4 HALA0700501 4 20071125 A 3421 CONNECTOR BOEING 767 76733A 1385209 NM ATTITUDE IND DIRTY A HALA K NONE O OTHER CR CRUISE 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM, ATTITUDE INDICATION OF STANDBY ATTITUDE INDICATION IS ABNORMAL IN PITCH ROLL GYRO FLAG IS RETR ACTED. CLEANED CONNECTORS ON STANDBY ATT IND GRND CHK NML, IAW 34-20-00. 2 L 7 2 4F RT A1NM 2007120400026 20071204 00026 NM 2007 12 4 DXTA200702555 1 20071019 A 3240 50128891 BRAKE GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE NR 1 WORN E DXTA O OTHER O OTHER LD LANDING 1 GL 07 703QS 2222 060 NORMAL BRAKES INEFFECTIVE ON LANDING ROLLOUT. FOUND NR 1 BRAKE ASSY WORN. REMOVED AND REPLACED NR 1 BRAKE ASSY WITH REP AIRED UNIT IAW G-200 CMP CARD NR: 324301. PERFORMED NORMAL BRAKE SYSTEM BLEEDING IAW G-200 MM CHAPTER 32-40-20. OPS CHEC K AND LEAK CHECK SATISFACTORY. 2 L 7 2 4F 4 F RT A53NM E35NE 2007120400027 20071204 00027 WP 2007 12 4 ARWA20071102 1 20071120 A 7830 898980X3 VALVE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE THRUST REVERSER ERRATIC A ARWA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 19 524MD 46999 455452 ON INITIAL TAKEOFF ROLL, UPON ADVANCING THE POWER LEVERS TO MAX TAKEOFF THRUST NR 1 ENGINE REVERSER PRESSURE LIGHT ILLUM INATED; CANCELLED THE TAKEOFF. LIGHT WENT OUT WHEN POWER WAS REDUCED TO IDLE. REVERSER NR 1 PREVIOUS DEACTIVATED AND S ECURED LOCK, TRANSFERRED TO DMI NR 21213; RE-CHECKED FOUND LOCKED; DEACTIVATED "LIGHT" IN ACCORDANCE WITH M/M 78-00-22 A ND DDG 78-1. ON T/S, FOUND NR 1 ENGINE THRUST REVERSER OVER PRESSURE INLET S/O VALVE AND PRESSURE REGULATOR VALVE WORKI NG ERRATIC. REMOVED AND REPLACED BOTH VALVES OVER PRESSURE AND REGULATOR. OPERATIONAL CHECK FOUND NORMAL IN ACCORDANCE WITH DC-10 M/M 78-31-09/78-31-05. DMI NR 21213 CLEARED (SEE LOG PAGE NR 120797). 2 L 7 3 4F 4 F A22WE E23EA 2007120400028 20071204 00028 NM 2007 12 4 USAA920071204 1 20071015 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK , CRACKED FRAME, BS 747, S8R - S9R. REPAIRED FRAME, BS 747, S8R - S9R IAW USAIRWAYS TYPI CAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2007120400029 20071204 00029 NM 2007 12 4 USAA920071205 1 20071012 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, CRACKED FRAME, BS 867, S8L - S9L. REPAIRED FRAME, BS 867, S8L - S9L IAW USAIRWAYS TYPIC AL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2007120400030 20071204 00030 NM 2007 12 4 USAA920071206 1 20071012 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, CRACKED FRAME, BS 867, S8R - S9R. REPAIRED FRAME, BS 867, S8R - S9R IAW USAIRWAYS TYPIC AL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2007120400032 20071204 00032 NM 2007 12 4 USAA920071208 1 20071016 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, CRACKED FRAME, BS 784, S8L - S9L. REPAIRED FRAME, BS 784, S8L - S9L IAW USAIRWAYS TYPIC AL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2007120400033 20071204 00033 NM 2007 12 4 USAA920071209 1 20071116 A 5312 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, CRACKED BULKHEAD WEB, BS 727, LBL 19, WL 161. REPAIRED BULKHEAD WEB, BS 727, LBL 19, WL 161 IAW USAIRWAYS EA 98972. 2 L 7 2 4F RT A16WE 2007120400034 20071204 00034 NM 2007 12 4 USAA920071210 1 20071115 A 5755 65C252421A SKIN BOEING 737 7373G7 1384595 NM SPOILER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, LEFT WING NR 4 GROUND SPOILER UPPER SURFACE HAS DELAMINATION. REPAIRED LEFT WING NR 4 G ROUND SPOILER IAW B737 SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007120400035 20071204 00035 NM 2007 12 4 USAA920071211 1 20071123 A 5753 6546481149 CARRIAGE BOEING 737 7373G7 1384595 NM T/E FLAP CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, CORROSION ON LEFT WING OUTBOARD MIDFLAP NR 1 CARRIAGE ASSEMBLY. REPLACED LEFT WING OUTB OARD MIDFLAP NR 1 CARRIAGE ASSEMBLY IAW B737 AMM 27-51-44. 2 L 7 2 4F RT A16WE 2007120400036 20071204 00036 NM 2007 12 4 USAA920071212 1 20071123 A 5753 6546481150 CARRIAGE BOEING 737 7373G7 1384595 NM T/E FLAP CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, CORROSION ON RIGHT WING OUTBOARD MIDFLAP CARRIAGE ASSEMBLY. REPLACED RIGHT WING OUTBOAR D MIDFLAP CARRIAGE ASSEMBLY IAW B737 AMM 27-51-44. 2 L 7 2 4F RT A16WE 2007120400037 20071204 00037 NM 2007 12 4 AALA20072234 1 20071104 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 976AN 30099 TUL - EMERGENCY LIGHT AT RIGHT FORWARD WING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIGHT FORWAR D WING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007120400038 20071204 00038 WP 2007 12 4 AALA20072224 1 20071116 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7549A 53031 BOS - EMERGENCY LIGHT AT SEAT 6E INOPERATIVE. REPAIRED EMERGENCY LIGHT AT SEAT 6E. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F A6WE 2007120400039 20071204 00039 NM 2007 12 4 AALA20072235 1 20071104 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 976AN 30099 TUL - EMERGENCY LIGHT AT RIGHT AFT OF FIRST CLASS DIVIDER INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIG HT AFT OF FIRST CLASS DIVIDER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007120400040 20071204 00040 NM 2007 12 4 AALA20072227 1 20071116 A 3040 CONTROLLER BOEING 737 737823 13844BZ NM WINDOW HEAT OVERHEATED A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 901AN 29503 STL INFLIGHT T1252/16NOV - OVERHEAD INDICATION FOR LEFT FRONT WINDOW ILLUMINATED FOLLOWED BY MULTIPLE CRACKS IN LEFT FR ONT WINDOW. LANDED STL WITHOUT INCIDENT. REPLACED WINDOW AND WINDOW HEAT CONTROLLER. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F RT A16WE 2007120400042 20071204 00042 NM 2007 12 4 AALA20072230 1 20071104 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 976AN 30099 TUL - EMERGENCY LIGHT AT FORWARD LEFT WING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD LEFT WING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007120400043 20071204 00043 NM 2007 12 4 AALA20072228 1 20071104 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 976AN 30099 TUL - EMERGENCY LIGHT AT LEFT WING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT WING EXIT. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007120400044 20071204 00044 NM 2007 12 4 AALA20072231 1 20071104 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 976AN 30099 TUL - EMERGENCY LIGHT AT LEFT OVERHEAD ENTRY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT OVERHEAD EN TRY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007120400047 20071204 00047 NM 2007 12 4 DXTA200702556 1 20071019 A 2921 ACCUMULATOR AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE THRUST REVERSER LEAKING E DXTA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 07 229QS 129 DURING CLIMBOUT THE NR 1 HYDRAULIC SYSTEM INDICATION DROPPED TO 10 PERCENT ON QUANTITY AND PRESSURE DROPPED AS WELL. NOT ED LEAK FROM LT T/R ACCUMULATOR TO FILTER ASSY. REPAIRED LEAK AND SERVICED SYSTEM 1 RESERVOIR. PERFORMED SYSTEM 1 HYDRAU LIC OPERATION TEST WITH NO DEFECTS NOTED. OPS AND LEAK CHECKED GOOD. WORK DONE IAW AMM 29-100. 2 L 7 2 4F 4 F RT A50NM E44NE 2007120400052 20071204 00052 NM 2007 12 4 PIDR07014 1 20071022 A 5330 SKIN BOEING 737 737301 1384611 NM BS 727C-727E CRACKED B PIDR K NONE O OTHER IN INSP/MAINT 1 SO 05 XAVIV 23560 DURING C-CHECK, NOTED A CRACK IN THE FUSELAGE SKIN AT BS 727E AT APX. STR 22LT IN CLOSE PROXIMITY TO AN EXISTING REPAIR. REMOVED EXISTING REPAIR AND REPAIRED SKIN FROM BS 727C +14 TO BS 727E +10 FROM STR 22LT TO STR 24LT PER EA NR 53-287. 2 L 7 2 4F RT A16WE 2007120400054 20071204 00054 CE 2007 12 4 DXTA200702558 1 20071021 A 3240 BRAKE ASSY CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE RIGHT MALFUNCTIONED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 630QS 5605130 THE TOE BRAKES ON RT PEDAL GOES TO THE FLOOR. PERFORMED BRAKE BLEED IAW AMM 32-42-01. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007120400056 20071204 00056 CE 2007 12 4 DXTA200702560 1 20071022 A 2916 RESERVOIR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE HYD SYSTEM UNDERSERVICED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 394QS 5600394 SIDE BRAKES ARE EXTREMELY MUSHY. LT PEDAL GOES ALMOST TO THE FLOOR. ACCOMPLISHED BRAKE BLEED ON LT AND RT BRAKES AND S ERVICED RESERVOIR WITH HYDRAULIC FLUID. BRAKING SYSTEM FUNCTIONS NORMALLY AT THIS TIME COMPLIED. WORK IAW CITATION. 5 60 MM CHAPTER 32-42-00 2 L 7 2 4F 4 F RT A22CE E25EA 2007120400059 20071204 00059 CE 2007 12 4 DXTA200702562 1 20071023 A 3260 WARNING LIGHT CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE MLG UNLOCK FALSE INDICATION E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 308QS 6800116 GEAR UNLOCK LIGHT REMAINED ILLUMINATED. CYCLED GEAR ONE TIME. PERFORMED VISUAL INSPECTION OF LANDING GEAR UPLOCK SYSTEM. NO DEFECTS NOTED. VERIFIED PROPER ENGAGMENT OF ALL (3) UPLOCK SWITCHES WITH GEAR IN THE WELL. CYCLED GEAR SEVERAL TIMES AND PERFORMED INDICATOR TEST IAW MM 32-00-00. NO DEFECTS NOTED AT THIS TIME. COULD NOT DUPLICATE. BOTH NOSE GEAR INDIC ATOR BULBS ARE WORKING AT THIS TIME. 2 L 7 2 4F 4 F RC T00012WI E35NE 2007120400060 20071204 00060 EU 2007 12 4 AALA20072240 1 20071117 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7076A 610 MIA - EMERGENCY LIGHT AT SEAT ROW 25H INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 25H. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007120400065 20071204 00065 NM 2007 12 4 AALA20072225 1 20071116 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 780AN 29956 JFK - EMERGENCY LIGHTS AT OVERHEAD FROM LEFT NUMBER TWO DOOR TO SEAT ROW 13D INOPERATIVE. REPLACED BATTERY PACK FOR EME RGENCY LIGHTS AT OVERHEAD FROM LEFT NUMBER TWO DOOR TO SEAT ROW 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120400066 20071204 00066 NM 2007 12 4 AALA20072232 1 20071104 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 976AN 30099 TUL - EMERGENCY LIGHT AT RIGHT AFT WING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIGHT AFT WING E XIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007120400067 20071204 00067 EU 2007 12 4 363011032007 1 20071103 A 6730 SC5083 SERVO SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B1 60056 NE FAILED E QMLA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 NM 03 902CF 5653 380 3630 AIRCRAFT WAS IN STRAIGHT AND LEVEL FLIGHT 10 MINUTES FROM T/O AT 7000 FT AGL. CYCLIC STICK JUMPED TO THE STOP AT THE 3 O ’CLOCK POSITION. A/C ENTERED A RT BANK (APPROX. 10 DEGREES). IMMEDIATE RECOVERY WAS MADE. FELT CONTINUOUS FEEDBACK IN TH E RT QUADRANT. SLOWED THE A/C TO 65 KTS TO REDUCE FEEDBACK ON THE CYCLIC. ABORTED THE MISSION AND TURNED THE A/C BACK T OWARDS THE LOCAL AIRPORT AND CONTACTED TOWER. ELECTED TO DECLARE A (PAN) AND SET UP FOR A NORMAL APPROACH. MADE MINIMU M CONTROL INPUTS AND LANDED WITHOUT DELAY AND NO HOVERING. DID NOT CONDUCT A "RUN ON" BECAUSE HAD NO PRESSURE ON THE CO NTROLS AT THE REDUCED SPEED. MAINT CALLED AND A HYDRAULIC TEST CONDUCTED WITH NO FURTHER PROBLEMS. MECHANIC PLANNED TO S 1 G 7 1 3U 3 U H9EU E00054EN 2007120400068 20071204 00068 NM 2007 12 4 AALA20072233 1 20071104 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 976AN 30099 TUL - EMERGENCY LIGHT AT RIGHT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIGHT AFT CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007120400071 20071204 00071 CE 2007 12 4 110407N420CS1 1 20071104 A 3260 MS25237327 BULB CESSNA 525 525 2076601 CE WILINT FJ44 FJ441A GL MLG INDICATOR BURNED OUT E Z5FA O OTHER P NO WARNING INDICATION AP APPROACH 1 EA 63 420CS 525B0115 DURING APPROACH CREW NOTICED NO RT GEAR DOWN INDICATION. CREW FOLLOWED EMERGENCY PROCEDURES, BLEW GEAR DOWN AND DECLARE D AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT . MAINTENANCE PERSONNEL FOUND CAUSE TO BE BURNED OUT BULB. BULB REPLACE D, SYSTEM OPS CHECKED GOOD AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 4F 4 F RT A1WI E3GL 2007120400074 20071204 00074 EU 2007 12 4 07FDEA04891 1 20071121 A 5320 A5377364420000 FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FWD LWR CARGO COMP AT FR STA 34 LT FRAME TO FLOORBEAM CONNECTION FITTING CORRODED, FITTING FOUND TO BE CRACKED ALSO. R EMOVED AND REPLACED FITTING IAW A310-200 SRM 51-72-10 PG 2. 2 L 7 2 4F RT A35EU 2007120400075 20071204 00075 EU 2007 12 4 07FDEA04892 1 20071121 A 5340 A5377364420000 ATTACH FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FWD LWR CARGO COMP AT FR STAT 38.2 LT FRAME TO FLOORBEAM CONNECTION FITTING CRACKED. REMOVED FITTING IAW SRM 51-72-10 PG 2 PARAG 5A LOCATED AND DRILLED NEW FITTING IAW SRM 51-72-10 PG 2 PARAG 8 .6A INSTALLED NEW FITTING IAW SRM 51-40-30. 2 L 7 2 4F RT A35EU 2007120400079 20071204 00079 EU 2007 12 4 07FDEA04897 1 20071121 A 5320 A5377364420100 FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FOUND FWD LWR CARGO COMP AT FR STAT 33 RT FRAME TO FLOORBEAM CONNECTION FITTING CRACKED. CRACKED REMOVED AND REPLACED F ITTING IAW A310-200 SRM`S 51-72-10 AND 51-40-30. 2 L 7 2 4F RT A35EU 2007120400082 20071204 00082 NM 2007 12 4 07FDEA04899 1 20071122 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 MAIN DECK CARGO COMPARTMENT, AFTER FLOOR PANEL REMOVAL AT ABOUT STA 1558 LBL 8 SEAT TRACK FLOOR PANEL SUPPORT FLANGE FOU ND CORRODED. REPAIRED AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007120400083 20071204 00083 WP 2007 12 4 07FDEA04900 1 20071122 A 5313 NCA6014 LONGERON DOUG DC10 DC1010F 3022111 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 FWD CARGO COMPT BILGE AREA FOUND CRACK ON LONGERON, SEE NRC N00293, N00294, N00295, N00297. REPAIRED LONGERON IAW SRM 5 3-10-00 VOL I FIG 1-2. 2 L 7 3 4F A22WE 2007120400085 20071204 00085 EA 2007 12 4 N6WA0071102 1 20071102 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE EMERGENCY LIGHT BURNED OUT A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 160GJ 10239 AFT EMERGENCY CEILING LIGHT OUT. REPLACED BULB. 2 L 7 2 4F 4 F RT A21EA E00063EN 2007120400086 20071204 00086 EA 2007 12 4 N6WA0071103 1 20071103 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE EMERGENCY LIGHT BURNED OUT A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 164GJ 10256 CEILING EMERGENCY FLOOD LIGHT INOP AT ROW 2. REPLACED BULB. 2 L 7 2 4F 4 F RT A21EA E00063EN 2007120400087 20071204 00087 EA 2007 12 4 N6WA0071104 1 20071103 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE EMERGENCY LIGHT BURNED OUT A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 165GJ 10257 EMERGENCY EXIT SIGN AT ROW 12A INOP. REPLACED BULB. 2 L 7 2 4F 4 F RT A21EA E00063EN 2007120400088 20071204 00088 WP 2007 12 4 07FDEA04901 1 20071123 A 5720 ARB24083 INTERCOSTAL DOUG DC10 DC1010F 3022111 WP LT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 LT WING L/E INTERNAL STRUCTURE ON HORIZONTAL INTERCOSTAL EXISTING ANGLE REPAIR. REPLACED INTERCOSTAL IAW DWG ARB2408 AN D ARB1333. 2 L 7 3 4F A22WE 2007120400091 20071204 00091 CE 2007 12 4 GLBA20061022 1 20071104 A 5260 1295140591 CABLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE AIRSTAIR DOOR BROKEN A GLBA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 03 184UX UE184 EES SYSTEM - PILOTS REPORTED DIFFICULTY WITH THE AIRSTAIR DOOR NOT LOCKING PROPERLY. MAINTENANCE DISCOVERED THE DOOR CAB LE WAS BROKEN ON THE INSIDE. MAINTENANCE REMOVED AND REPLACED THE AIRSTAIR DOOR CABLE IAW MM 52-10. OPERATIONAL CHECK GO OD. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007120400093 20071204 00093 WP 2007 12 4 07FDEA04905 1 20071123 A 5310 AFA71321 DOOR FRAME DOUG MD10 MD1010F 3022112 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 MAIN CARGO DOOR LOWER JAMB AT NR 2 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A, B,C,D TO REMOVE CORROSION AND INSTALLED REPAIR BUSHINGS. FOUND REPAIR BUSHINGS WOULD NOT MEET THE LIMITS STATED IN MD/D C10-10 SRM 53-50-00 FIG 17 VOL I. REPLACED NR 2 FITTING AFA7132-1 IN REF TO MD/DC10-10 SRM 51-33-01 VOL II AND DAC DW G ACA7224 REV G. 2 L 7 3 4F RT A22WE 2007120400094 20071204 00094 WP 2007 12 4 07FDEA04906 1 20071123 A 5310 AFA71321 DOOR FRAME DOUG MD10 MD1010F 3022112 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 MAIN CARGO DOOR LOWER JAMB AT NR 4 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B ,C TO .460 TO REMOVE CORROSION. WITHIN LIMITS OF MD/DC10-10 SRM 53- 50-00 FIG 17 VOL I. HOLE D REAMED TO REMOVE CORRO SION AND INSTALLED BUSHING IN REF TO MD/DC10-10 SRM 53-50-00 FIG 17 VOL I. NDT FOR CRACKS HOLES A,B,C,D, NO DEFECTS N OTED IAW NTSPM 06-10-01-003. TOOL T8203A MEASURING TOOL T8723K 2 L 7 3 4F RT A22WE 2007120400096 20071204 00096 WP 2007 12 4 07FDEA04907 1 20071123 A 5310 AFA71321 DOOR FRAME DOUG MD10 MD1010F 3022112 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 MAIN CARGO DOOR LOWER JAMB AT NR 5 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A, B,D TO .517 AND HOLE D TO .484 TO REMOVE CORROSION IN REF TO MD/DC10-10 SRM 53-50-01 FIG 17 VOL I. ACCOMPLISHED BHEC IN REF TO NTSPM 06-10-01-003 AND FOUND HOLES A,B,D WITH CRACK INDICATION. REPLACED NR 5 FITTING IAW SRM 51-33-01 VOL II PG 1 AND DAC DWG ACA 7224 REV G. 2 L 7 3 4F RT A22WE 2007120400097 20071204 00097 WP 2007 12 4 07FDEA04908 1 20071123 A 5310 AFA71321 DOOR FRAME DOUG MD10 MD1010F 3022112 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 MAIN CARGO DOOR LOWER JAMB AT NR 6 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A, B,C TO 0517 AND HOLE D TO .484 TO REMOVE CORROSION IN REF TO MD/DC10-10 SRM 53-50-00 FIG 17 VOL I. ACCOMPLISHED BHEC IN REF TO NTSPM 06-10-01-003 AND FOUND HOLES B AND C WITH CRACK INDICATION. REPLACED NR 6 FITTING IN REF TO MD/DC10-10 SRM 51-33-01 VOL II PG 1 AND DAC DWG ACA 7224 REV G. 2 L 7 3 4F RT A22WE 2007120400098 20071204 00098 SW 2007 12 4 HEEA118059 1 20071102 A 5620 206202301 WINDOW BELL 206 206L3 1182108 SW ALLSN 250C 250C30 03013 GL CABIN DEPARTED B HEEA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 SW 03 4180F 51469 SUSPECT TAIL ROTOR BLADE STRIKE CAUSED FROM PASSENGER SLIDING WINDOW EXITING THE AIRCRAFT IN FLIGHT. SUSPECT PASSENGER POSSIBLY DAMAGED WINDOW PRIOR IT DEPARTING AIRCRAFT. 1 G 7 1 3U 3 U H2SW E1GL 2007120400101 20071204 00101 NM 2007 12 4 ASMF200711001 1 20071102 A 2160 39811611 MIXING VALVE BOEING 737 737* NM CFMINT CFM567 CFM567B22 13802 NE CABIN TEMP FAILED W ASMF O OTHER O OTHER CR CRUISE 1 SW 23 857AM 9213 33793 CAPTAIN REPORTED AIR CONDITIONED TEMPERATURE CONTROL OUT OF SERVICE, MAINTENANCE PERSONNEL PERFORMED FIM PROCEDURE 21-61 TASK 847, CLEANED AND RECONNECTED THE RT MIX VALVE CONNECTOR, TESTED CORRECT. LATER, DURING OVERNIGHT CHECK, THE RT SID E AIR MIX VALVE WAS REPLACED IAW MM 21-61-02, TESTED CORRECT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007120400105 20071204 00105 NM 2007 12 4 07FDEA04912 1 20071124 A 5320 65295675 PAN BOEING 727 727225 1384077 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 DITCHING PAN IS CRACKED, LOCATED AT STA 1183, WL 20/8, LBL 27. REMOVED DITCHING PAN, STA 1183, LBL 27 REF SRM 51-30-02. FABRICATED DITCHING PAN REF BOEING DRAWING 65-29567-5 DITCHING PAN. HEAT TREATED REF BOEING DRAWING 65-29567-5. TREA TED AND PRIMED DITCHING PAN REF SRM 51-10-2. IDENTIFIED DITCHING PAN WITH FX65-29567-5, REF FED EX GMM 7-0-1001. INSTA LLED DITCHING PAN AT STA 1183 LBL27 REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2007120400108 20071204 00108 2007 12 4 AMTA200700568 4 20071027 A 3460 1741010301 CDU BOEING 737 73783N 13844HI NM NR FMC UNSERVICEABLE A AMTA J A DUMP FUEL UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 GL 11 321TZ 28249 NR 1 FMC SCREEN BLANK. REMOVED AND REPLACED NR 1 FMC CDU IAW MM 34-61-01. OPS CHECK GOOD. (K) 2 L 7 2 4F RT A16WE 2007120400109 20071204 00109 2007 12 4 AMTA200700569 4 20071029 A 3460 FMC BOEING 737 73783N 13844HI NM FAILED A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 318TZ 28247 DUAL FMC FAILURE AT CRUISE ALTITUDE, LOST ALL STORED DARA, NAV DISPLAY RESTORED ITSELF AND FLIGHT CREW REPROGRAMMED FMC DATA. PERFORMED FMC SYSTEM BITE CHECK IAW 34-61-00-810-801, NO FAULTS NOTED ON FMC NR 1 AND NR 2 SYS OPS OK. (K) 2 L 7 2 4F RT A16WE 2007120400112 20071204 00112 NM 2007 12 4 AMTA200700573 1 20071030 A 5753 SKIN BOEING 737 73783N 13844HI NM RT WING TE FLAP NICKED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 308TZ 28244 RT WING IB AFT FLAP LOWER SURFACE HAS MULTIPLE NICKS AND DINGS IN MLG TIRE PATHWAYS. REPAIRED IAW SAA EA 737-5753-09-A1 149 AND SRM 57-53-02-DI REF ATA ERA 737-57R-6170 FOR REPETITIVE REINSPECTION EVERY B3500, FLT CYCLES OR 24 MONTHS CLASS MAJOR. (K) 2 L 7 2 4F RT A16WE 2007120400114 20071204 00114 NM 2007 12 4 07FDEA04914 1 20071124 A 5320 65295675 PAN BOEING 727 727225 1384077 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 DITCHING PAN AT STA 1183 BETWEEN RBL46 TO 49, WL 208 IS CRACKED, ALONG WITH AFT SUPPORT CLIP. REMOVED GILLINER SUPPORT PLUS DITCHING PAN SRM 51-30-20 PG 16. FABBED NEW DITCHING PAN REF DWG 65-29567. TREATED AND PRIMED REPAIR PARTS 51-10- 02 PG 7. INSTALLED REPAIR PARTS SRM 51-40-3 PG 1-6. INSTALLED DITCHING PANS SRM 51-30-2 PG 1- 16. INSTALLED GILLINER SUPPORT SRM 51-30-2. 2 L 7 3 4F A3WE 2007120400115 20071204 00115 NM 2007 12 4 07FDEA04915 1 20071124 A 5311 651633925 FRAME BOEING 727 727225 1384077 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 AFT PIT BODY FRAME WEB IS CRACKED AT TOOLING HOLE BS 970, STR 26L - 27L REMOVED ASSOCIATED PARTS TO FRAME 970 SECTION, R EMOVED DAMAGE SECTION OF FRAME FROM STR 27R TO STR 24L AND 25L. FABRICATED NEW FRAME SECTION, HEAT TREATED, ALODINED AN D PRIMED, PAINTED AND INSTALLED. INSTALLED REMOVED ASSOCIATED PARTS TO FRAME REF BOEING DOCUMENT NUMBER 65-16339 AND SR M 51-30-02. REPAIR IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007120400117 20071204 00117 CE 2007 12 4 AMWA88382BC 1 20071103 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER MALFUNCTIONED A AMWA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 146ZV 9664 68 UE146 BATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT MULTIPLE TIMES. BATTERY WAS REPLACED BY MAINTENANCE AND DISCREPANCY CLE ARED. 2 L 7 2 4T 4 T RT A24CE E26NE 2007120400118 20071204 00118 CE 2007 12 4 AMWA88376BC 1 20071102 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER MALFUNCTIONED A AMWA O OTHER N FALSE WARNING CL CLIMB 1 CE 07 174YV 5696 34 UE174 BATTERY CHARGE ANNUNCIATOR ILLUMINATED TWICE IN FLIGHT. 1ST TIME IN CLIMB A FEW SECONDS AFTER GEAR RETRACTION AND CONTIN UING THROUGH FL100 ALL AT ~10A. 2ND TIME WAS A FEW MINUTES INTO CRUISE FOR 2-3 MINUTES AT APPROXIMATELY 8A. MAINTENANCE REPLACED BATTERY AND CLEARED DISCREPANCY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007120400120 20071204 00120 NM 2007 12 4 07FDEA04918 1 20071124 A 5320 65295675 PAN BOEING 727 727225 1384077 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 DITCHING PAN IS CRACKED LOCATED AT RBL 27 STA 1183, WL 208 REMOVED GILL LINER SUPPORT PLUS DITCHING PAN REF SRM51-30-2 PG 1-16. FABRICATED NEW DITCHING PAN REF DWG 65-29567. TREATED AND PRIMED DITCHING PAN SRM 51-30-02. REMOVED FLAPPER VALVE SRM 51-30-2. INSTALLED NEW FLAPPER VALVE. 2 L 7 3 4F A3WE 2007120400121 20071204 00121 2007 12 4 AMTA200700574 4 20071031 A 3460 4052506955 COMPUTER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE E&E COMPT UNSERVICEABLE A AMTA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 517AT 27973 DURING ENGINE START LT FMC FAIL ILLUMINATED. (K) PERFORMED BITE OF FMC IAW FIM 34-61-00. NO FAULTS NOTED. REPLACED L. FMC AS PRECAUTIONARY MEASURE. OPS CK GOOD REF MM 34-61-01-4. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007120400122 20071204 00122 NM 2007 12 4 07FDEA04919 1 20071124 A 5320 BAC15171508 FLOOR SUPPORT BOEING 727 727225 1384077 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 FWD PIT FLR SPPT Z-CHANNEL IS CORRODED BS 720B TO 720C PLUS 10, LBL 20, WL 156 BLENDED CORROSION ON FLOOR SUPPORT. MATE RIAL OF .025" OF .063' ORIG "T" FOUND TO BE OUT OF LIMITS REF 53-10-1 PG 2. FABRICATED NEW FLOOR SUPPORT Z-CHANNEL FROM EXTRUSION BAC1517-1508 7075-T6. FABRICATED REPAIR SPLICE AT BS 720 PLUS 8 REF SRM 51-40-4 PG 1-9. INSTALLED Z-CHANNEL FLOOR SUPPORT FROM BS 720 PLUS 8 TO BS 720D, LBL 20, REF 51-30-2, SRM 51-40-4, 51-10-2. 2 L 7 3 4F A3WE 2007120400124 20071204 00124 NM 2007 12 4 07FDEA04920 1 20071124 A 5320 6517506125 BRACKET BOEING 727 727225 1384077 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 2" CRACK THROUGH FASTENER ON ANGLE BRACKET, FS 1303, LBL 20, WL 273, ON FWD SIDE OF BULKHEAD, ABOVE S-DUCT, BRACKET CON NECTS BULKHEAD TO FUSELAGE SKIN. REMOVED AND INSTALLED NEW BRACKET AT FS 1303, LBL 20, WL 273 ON FWD SIDE OF BULKHEAD A BOVE S-DUCT REF 51-30-02 PG 1-12. LEAK CHECKED TAI DUCT REF W/C 73C015-00. LEAK CHECK GOOD. THIS IS CLASSIFIED AS A M INOR REPAIR. 2 L 7 3 4F A3WE 2007120400125 20071204 00125 NM 2007 12 4 07FDEA04921 1 20071124 A 5320 6946373 FLOOR SUPPORT BOEING 727 727225 1384077 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 FWD PIT FLOOR SUPPORT PNL IS CORRODED BS 480-720D, LBL 20-26, WL 157. BLENDED CORROSION AT BS 480 TO 720C +10. MAX MAT ERIAL LOSS OF 16 PERCENT OF .050 ORIG "T". WITHIN LIMITS REF SRM 53-10-1 PG 31. BLENDED CORROSION AT BS 720C+10 TO BS 720D. MATERIAL LOSS OF 30 PERCENT OF .050" ORIG "T" FOUND TO BE OUT OF LIMITS REF SRM 53-10-1. FABRICATED AND REPLACE D Z- ANGLE PANEL AT BS 720C+10 TO 720D, REF 51-30-2, 51-10-2 AND BOEING DWG 69-46373 THIS IS CLASSIFIED AS A MINOR REPAI R. 2 L 7 3 4F A3WE 2007120400127 20071204 00127 NM 2007 12 4 AMTA200700582 1 20071103 A 2822 SWITCH BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE FUEL BOOST MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 11 550TZ 32584 DURING CLIMB, RT AFT FUEL BOOST PUMP SWITCH CAME UNLATCHED. FUEL PUMP OPS OK. SWITCH WILL NOT STAY IN HOUSING CONTINUO USLY (LATCHED IN). REMOVED AND REPLACED RT AFT FUEL BOOST PUMP SWITCH OPS CHECK, OK. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007120400128 20071204 00128 NE 2007 12 4 AMTA200700583 2 20071103 A 7532 BLEED VALVE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 518AT 27974 EICAS MSG R ENG BLEED OFF DISPLAYED. RT ENG BLEED AIR OFF LGT ILLUM W/ENG RUNNING AND SW ON DUCT PRESS WAS ZERO. REMOV ED AND REPLACED PSROV IAW MM CH 36-11-09-2. PERFORMED TEST NR 3, COMPRESSOR AIRFLOW CTRL. TEST OPS CHECK GOOD, OK FOR S ERVICE.(K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007120400131 20071204 00131 EU 2007 12 4 07FDEA04923 1 20071126 A 5313 A53970014 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 CORROSION ON STRINGER 56R FROM FRAME 60 TO 61 ALSO ON FRAME SHEAR TIE IN AFT PIT. REMOVED SHEAR TIE IAW A310-200 SRM 5 3-10-14 PARA. 4.A (2) (A) AND DAMAGE STRINGER AT FRAME 60-61 S56R IAW A310-200SRM 53-10-14 PARA. 4.A (2) (A). REMOVED CO RROSION IN SHEAR TIE, NO MATERIAL LOSS IAW A310-200 SRM 51-74-10. INSTALLED REPAIR SPLICES, STRINGER AND SHEAR TIE IAW A 310-200 SRM 53-10-14 PARA. 4.A (2) (A). 2 L 7 2 4F RT A35EU 2007120400134 20071204 00134 EA 2007 12 4 A6WA200740601 1 20071108 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 426AW 7669 FOUND CRACK ON 2 BRACKETS FS 625.0 STRINGER 14R AND STRINGER 14L. BRACKETS REPLACED 2X AT FS 625 STRINGER 14R AND STRIN GER 14L IAW SRM 51-42-20. (M) 2 L 7 2 4F RT A21EA 2007120400138 20071204 00138 EA 2007 12 4 A6WA200740603 1 20071108 A 5242 RETAINER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 426AW 7669 FOUND CORROSION EXIST ON FORWARD DOOR SEAL RETAINER OF MAIN AVIONICS DOOR. FORWARD MAIN AVIONICS DOOR SEAL RETAINER REP LACED IAW CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007120400140 20071204 00140 EA 2007 12 4 A6WA200740604 1 20071102 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 426AW 7669 FOUND CRACK EXIST ON FLOORBEAM AT FUSELAGE STATION 280 RBL 9. REPAIR PERFORMED IAW REO 601R-53-11-171 REV D. (M) 2 L 7 2 4F RT A21EA 2007120400144 20071204 00144 EA 2007 12 4 A6WA200740606 1 20071107 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 426AW 7669 HYDRAULIC SUPPORT BRACKET OF MLG BAY FOUND CRACKED. REPLACED HYD SUPPORT BRACKET OF MLG BAY LT FS 529.50 LBL 31 IAW CR J 200 SRM 51-42-06 ML 1617. (M) 2 L 7 2 4F RT A21EA 2007120400146 20071204 00146 EA 2007 12 4 A6WA200740609 1 20071103 A 7830 TRACK CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 426AW 7669 RIGHT ENGINE THRUST REVERSER MAIN TRACK AT 7 O’CLOCK FOUND CRACKED. REPLACED IAW CRJ 200 AMM 78-34-11-801. OP CHECK OF T/R TRANSFERRED TO MWC 115431-208. (M) 2 L 7 2 4F RT A21EA 2007120400148 20071204 00148 EA 2007 12 4 A6WA200740611 1 20071107 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 426AW 7669 FOUND CRACK EXIST ON FORWARD AND AFT EDGE MEMBER OF PAX DOOR. FORWARD AND AFT EDGE MEMBER OF PAX DOOR REPAIRED IAW REO 601R-52-11-279. (M) 2 L 7 2 4F RT A21EA 2007120400149 20071204 00149 EA 2007 12 4 A6WA200740612 1 20071108 A 2611 47359719 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY MALFUNCTIONED A A6WA K NONE N FALSE WARNING NR NOT REPORTED 1 GL 31 458AW 7861 RECEIVED SMOKE CARGO WARNING MESSAGE FOR 5-10 SECONDS. INSPECTED CARGO COMPARTMENT AND FOUND NO EVIDENCE OF SMOKE OR FI RE. REMOVED AND REPLACED BOTH CARGO SMOKE DETECTORS IAW 26-15-01, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007120400154 20071204 00154 EA 2007 12 4 A6WA200740619 1 20071108 A 5753 GUIDE CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 470ZW 7927 FOUND RIGHT OUTBOARD FLAP MID HINGE FAIRING, INBOARD GUIDE CRACKED. REPAIRED IAW SRM 51-24-16, 51-21-16, 51-25-16. (M) 2 L 7 2 4F RT A21EA 2007120400155 20071204 00155 CE 2007 12 4 1356813112207 1 20071122 A 2140 AN8164D FITTING STWARNER CESSNA 402 402C 207590R CE HEATER LEAKING E HYIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 61 6813J 402C0641 PILOT NOTICED FUEL SMELL IN COCKPIT DURING HEATER START UP AND SHUT DOWN, WHEN BRINGING AIRCRAFT TO FLEET CENTER AT END OF NIGHT. MAINTENANCE FOUND PUMP OUTLET FITTING LEAKING. MAINTENANCE TIGHTENED FUEL PUMP OUTLET FITTING AND AS A PRECA UTIONARY MEASURE REMOVED AND REPLACED HEATER FUEL LINE. LEAK CHECKED AND OPERATIONALLY CHECKED GOOD. 1 L 7 2 3O A7CE 2007120400157 20071204 00157 WP 2007 12 4 ABXA070372 1 20071019 A 5310 99578607 ANGLE DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 45596 DURING COCKPIT WINDSHIELD FRAME MOD, FOUND ANGLE CRACKED IN RADIUS. REPLACED ANGLE IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 2007120400160 20071204 00160 WP 2007 12 4 ABXA070375 1 20071111 A 5310 99115056 WINDOW FRAME DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 DURING COCKPIT WINDSHIELD FRAME MOD, FOUND LOWER SILL RIGHT SIDE FRAME CRACKED. FRAME REPAIRED IAW DC9 SRM 53-03, FIGUR E 34. 2 L 7 2 4F A6WE 2007120400161 20071204 00161 WP 2007 12 4 ABXA070378 1 20071023 A 5311 9919619505N FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 LEFT AFT MAIN FRAME STA 775, HAD A CRACK IN THE FORWARD FLANGE AT POINT J. REPAIRED MAIN FRAME IAW DC9 SRM. 2 L 7 2 4F A6WE 2007120400168 20071204 00168 CE 2007 12 4 AMWA88439BC 1 20071106 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER FAILED A AMWA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 176YV 1967 126 UE176 DURING FLIGHT THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED THEN WENT OUT. MAINTENANCE REMOVED AND REPLACED BATTERY AND CLE ARED DISCREPANCY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007120400170 20071204 00170 CE 2007 12 4 AMWA88451BC 1 20071107 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER FAILED A AMWA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 07 166YV 8326 32 UE166 AFTER TAKEOFF THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED. AIRCRAFT RETURNED TO FIELD AND BATTERY WAS REPLACED AND DISCRE PANCY CLEARED. 2 L 7 2 4T 4 T RT A24CE E26NE 2007120400172 20071204 00172 CE 2007 12 4 GLBA20061024 1 20071107 A 5210 LATCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE PAX DOOR FAILED A GLBA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 NM 03 247GL UE247 EES - FLIGHT 5041 (DEN) PILOTS REPORTED THE MAIN CABIN DOOR COULD NOT BE OPENED FROM THE INSIDE. MAINTENANCE CLEANED THE PUSH BUTTON SWITCH AND OPERATIONALLY CHECKED THE DOOR. OPS GOOD IAW MM 52-10-00. 2 L 7 2 4T 4 T RT A24CE E26NE 2007113000137 20071130 00137 EU 2007 11 30 711510292007 1 20071029 A 7603 POWER LEVER BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE DISLODGED E QMLA A UNSCHED LANDING C R J F.O.D. PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 NM 03 118NY 7115 2EA HELICOPTER STUCK SEVERAL GEESE. 1 PENETRATED THE WINDOW ON RT SIDE BEHIND THE SLIDING DOOR NEXT TO PARAMEDIC & LODGED IT SELF BETWEEN THE WALL & AIRFRAME. ANOTHER BROKE THROUGH PILOT'S UPPER LT MAIN WINDSCREEN, LEAVING A HOLE APPROXIMATELY 1 2 X 12 INCHES. GOOSE THEN STRUCK BOTH THROTTLES (PCLS) DISLODGING THEM FROM THE FLY POSITION AND INTO THE IDLE POSITION. AT THAT TIME, IT WAS UNKNOWN THAT THIS HAD OCCURRED. AN IMMEDIATE VIBRATION WAS PICKED UP WITH SUBSEQUENT SLOWING OF TH E ACFT. DURING THE RADIO CALL TO FLT OPS DESCRIBING OUR SITUATION, IT WAS QUICKLY REALIZED THAT THE ACFT AT A POWER LOSS WITH LOW ENGINE LIGHTS & AURAL LOW ROTOR WARNING HORN SOUNDING. AN IMMEDIATE AUTOROTATION ENTERED, MAYDAY MADE TO TOWER 1 G 7 2 3U 3 U H13EU E5NE 2007113000138 20071130 00138 NM 2007 11 30 AMTA200700556 1 20071024 A 3150 WARNING MESSAGE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211* 54555 NE FALSE ACTIVATION A AMTA O OTHER N FALSE WARNING CR CRUISE 1 GL 11 560TZ 33525 STATUS MSG (R TURB OH DET2) DISPLAYED. TROUBLESHOOT IAW FIM 26-13-00, FIG 103 AND 104, OPS CHECK NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM A12EU 2007113000148 20071130 00148 SO 2007 11 30 GLBA20061020 1 20071029 A 5712 RIB EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT WING CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 96ZK 120096 10/29/07-RIB CRACKED AT LT WS YA 5825. MAINTENANCE REMOVED DAMAGED AREA AND INSTALLED REPAIR PIECE I.A.W. EMB-120 SRM 5 7-20-07. ALSO REFERENCE EMB LETTER 1C2007-120/08000 DATED NOVEMBER 8TH, 2007. RII INSPECTION COMPLIED WITH PER GLA TASKC ARD 8.2.1. 2 L 7 2 4T 4 T RT A31SO E20NE 2007113000151 20071130 00151 CE 2007 11 30 K452007F00001 1 20071026 A 7830 20200481 SUPPORT BRACKET NORD CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE THRUST REVERSER MISSING E K45A K NONE O OTHER IN INSP/MAINT 1 GL 25 103BG 2366 5600091 DURING ROUTINE INSPECTION, THE LT OB THRUST REVERSER STANG FOUND DISPLACED .2500 INCH OB FROM NORMAL POSITION. REMOVAL OF STANG REVEALED THE LOWER FWD SUPPORT WAS MISSING THE UPPER FWD SUPPORT SHEARED OFF. THE ATTACHING RIVETS HAD FAILED. FURTHER INSPECTION REVEALED THE UPPER AFT MOUNTING LUG OF OB (BIRDCAGE) WAS CRACKED DUE TO STRESSES IMPOSED DUE TO MIS SING FWD SUPPORT. THRUST REVERSER WAS REMOVED AND SENT TO MFG FOR REPAIR. AS PREVENTIVE MEASURE, THE RT OB THRUST REVE RSER STANG WAS REMOVED AND THE LOWER FWD SUPPORT WAS FOUND LOOSE WITH ONE SHEARED ATTACHING RIVET. THE UNIT WAS REMOVED FOR REPAIR. CAUSE MAY HAVE BEEN ACCUMULATED AGE AND VIBRATION. (K) 2 L 7 2 4F 4 F RT A22CE E25EA 2007113000170 20071130 00170 WP 2007 11 30 07FDEA04862 1 20071119 A 5713 ARB09441 STRINGER DOUG DC10 DC1010 3022110 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 AT ACCESS 534 AT FOUND CRACK, ACCOMPLISHED EA NR 8-5710-111526. 2 L 7 3 4F A22WE 2007113000172 20071130 00172 EU 2007 11 30 SA07074 1 20071118 A 3350 NSA937901M2004 TERMINAL BLOCK AIRBUS A319 A319112 3930323 EU CABIN FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 700UW 0885 MAINTENANCE FOUND EMERGENCY LIGHTS INTERMITTENT. REPLACED TERMINAL BLOCK 7222VT MODULE 3. NO FURTHER FAULTS. 2 L 7 2 4F RT A28NM 2007113000175 20071130 00175 NM 2007 11 30 QXEA200701727 1 20071118 A 2611 PU90461R2 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY ACTIVATED A QXEA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 09 357PH 504 PDX - ON FLIGHT 2093 RETURNED TO FIELD, RIGHT AFTER TAKEOFF THROUGH 3000, THE SMOKE ALARM IN THE BATHROOM WENT OFF. LAS TED FOR 2-3 MINUTES AND THEN STOPPED AFTER IT EXTINGUSHED. THE FLIGHT ATTENDANT SAID THE GREEN LIGHT CAME BACK ON. ON THE ALARM THE FLIGHT ATTENDANT SAID HE HAD SMELLED SMOKE IN THE BATHROOM. MAINTENANCE REMOVED AND REPLACED THE SMOKE DET ECTOR AS A PRECAUTIONARY MEASURE. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007113000180 20071130 00180 SO 2007 11 30 SIMA200732408 1 20071115 A 4920 APU EMB 145 EMB145LR 3260212 SO APU BAY FAILED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 643AE 145200 EXPERIENCED SMOKE IN THE CABIN AND COCKPIT. IT OCCURRED AFTER A COUPLE OF MINUTES OF STARTING THE APU, TURNED ON NR 2 P ACK AND CROSS BLEED OPEN. WITHIN 30 SECONDS SMOKE APPEARED IN THE CABIN AND COCKPIT. THE FO TURNED OFF THE PACK AND CR OSS BLEED. SMOKE IMMEDIATELY DISSIPATED. SOON AFTER THE SMOKE APPEARED THE APU FAILED AND SHUT DOWN. ISSUED MEL ON AP U/OPS CHECKED PACKS, NO SMOKE. 2 L 7 2 4T RT T00011AT 2007113000183 20071130 00183 EU 2007 11 30 SIMA200732404 1 20071113 A 5347 7253742409 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 307AE 21265 500 340B307 DURING MBV INSPECTION, THE SEAT TRACK AT BL36R WAS FOUND TO BE CORRODED. REPLACED SEAT TRACK WITH PN 7253742-409 IAW S AAB SRM CHAPTER 53-70-60. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007113000195 20071130 00195 NM 2007 11 30 ASMF200710012 1 20071030 A 3240 50078983 BRAKE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE LEFT FAILED W ASMF D RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 169PL 19002 3134 53175 CAPTAIN REPORTED THAT DURING TAXING AT RUNWAY THRESHOLD, THE TEMPERATURE OF THE MAIN LANDING GEAR BRAKE NR 1 REACHED 45 0 CELSIUS DEGREES, SO IT WAS NECESSARY TO STOP THE AIRCRAFT. MAINTENANCE PERSONNEL REPLACED THE LT BRAKE ASSY AND THE MA IN LANDING GEAR WHEEL NR 1 IAW MM 32-42-01 AND 32-40-01 RESPECTIVELY. 2 L 7 2 4F 4 F RT A6WE E9NE 2007113000197 20071130 00197 CE 2007 11 30 GUUA10110701 1 20071011 A 5540 10164001415 HINGE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RUDDER CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 16540 UE172 REPORT: DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED UPPER RUDDER HINGE ASSEMBLY EXFOLIATED. REPLACED UPPER RUDDER H INGE ASSEMBLY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007113000211 20071130 00211 2007 11 30 DL76L071511 4 20071118 A 3442 20414440401 TRANSCEIVER BOEING 767 767332 1382001 NM WEATHER RADAR FAILED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 196DN 6170 28453 WX RADAR FAILED IN FLT WITH ANT FAULT. REPLACED TRANSCEIVER AND ANTENNA CHECKS OK. 2 L 7 2 4F RT A1NM 2007113000212 20071130 00212 2007 11 30 DL76L071512 4 20071118 A 3442 20414440401 ANTENNA BOEING 767 767332 1382001 NM WEATHER RADAR FAILED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 196DN 28453 WX RADAR FAILED IN FLIGHT WITH ANT FAULT. REPLACED TRANSCEIVER AND ANTENNA. CKS OK. 2 L 7 2 4F RT A1NM 2007113000214 20071130 00214 NM 2007 11 30 DL764071514 1 20071114 A 3320 LIGHT BOEING 767 767432ER 1385134 NM L1 SLIDE INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 836MH 29709 SLIDE LIGHT AT 1L DOOR INTERMITENT. RELAMP SLIDE LIGHT IAW DAL B767-400 33-13-00. OPS CHECK GOOD IAW B767-400 MM 52-73 -00 STEP E1-E9. 2 L 7 2 4F RT A1NM 2007113000216 20071130 00216 NM 2007 11 30 DL764071516 1 20071115 A 3350 CHARGER BOEING 767 767432ER 1385134 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 836MH 29709 RT EMERGENCY LIGHTS ROW 30-37 OUT. REMOVED AND REPLACED BATTERY CHARGER AT ROW 37 RIGHT. OPS CHECK GOOD IAW B767-400 M M 33-51-04. 2 L 7 2 4F RT A1NM 2007113000225 20071130 00225 WP 2007 11 30 07FDEA04881 1 20071120 A 5310 7075T6063CW WEB DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 317FE 46835 R-3 DOOR AFT JAMB TORQUE BOX WEB CRACKED AT FLOOR LINE REPAIRED WEB IAW SRM 53-50-00 FIG 19 SHEET 2. 2 L 7 3 4F RT A22WE 2007113000227 20071130 00227 WP 2007 11 30 07FDEA04883 1 20071120 A 5330 7075T3071C SKIN DOUG DC10 DC1030F 3023504 WP FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 317FE 46835 FUSELAGE SKIN AFT OF CENTER PIT DOOR HAS 3 EACH DENTS REPAIRED AREA AS REQUIRED IAW SRM 53-20-00 FIG 13. 2 L 7 3 4F RT A22WE 2007113000234 20071130 00234 NM 2007 11 30 AALA20072215 1 20071115 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 975AN 29549 LGA - EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A16WE 2007113000242 20071130 00242 NE 2007 11 30 AALA20072190 2 20071112 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RIGHT MAKING METAL A AALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 7528A 49920 717304 IAD INFLIGHT T731/12NOV LGA TO DFW. NUMBER TWO ENGINE LOST OIL PRESSURE. NUMBER TWO ENGINE OIL INDICATION ILLUMINATED. REDUCED POWER AND OIL TEMPERATURE DROPPED. SHUT DOWN NUMBER TWO ENGINE. LANDED IAD WITHOUT INCIDENT. SINGLE ENGINE TIME 12 TO 15 MINUTES. FOUND METAL IN OIL FILTER. REPLACED NUMBER TWO ENGINE ON 13 NOV 2007 AT IAD. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007113000243 20071130 00243 2007 11 30 AALA20072211 4 20071114 A 2565 SLIDE BOEING 757 757223 1384957 NM L1 DOOR DISLODGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7667A 25301 SXM - EMERGENCY SLIDE AT LEFT NUMBER ONE DOOR DISLODGED FROM SLIDE STORAGE PACK AND WAS SUPPORTED BY JETBRIDGE NOT ACTIV ATING INFLATION SEQUENCE. SLIDE DID NOT DEPLOY. REPLACED EMERGENCY SLIDE AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007120300004 20071203 00004 NM 2007 12 3 07FDEA04871 1 20071120 A 2810 SKIN DOUG MD11 MD11F 3023600 NM AUX TANK CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 CABIN, AT ABOUT STA 1228 RBL 65 TO RBL 80 UPPER AUX TANK UPPER SKIN FOUND CORRODED. REPAIRED AS PER FEDEX EA 1-5710-11 7063. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007120300007 20071203 00007 WP 2007 12 3 07FDEA04875 1 20071120 A 5311 ADA00757 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON FRAME CAP AT STA 859 BETWEEN LONG NR 50R AND 50L WAS FOUND NOT IN COMPLIANCE WITH APPROVED DATA REPAIR HAS BEEN REPLACED WITH A NEW ONE IAW SRM 53-30-00, FIG 5, VOL I. 2 L 7 3 4F A22WE 2007120300008 20071203 00008 WP 2007 12 3 07FDEA04876 1 20071120 A 5311 ADA00105 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON FRAME CAP AT STA 824 BETWEEN LONG NR 50R AND 50L WAS FOUND NOT IN COMPLIANCE WITH APPROVED DATA. REPAIR HAS BEEN REPLACED WITH A NEW ONE IAW SRM 53-30-00, FIG 5, VOL I. 2 L 7 3 4F A22WE 2007120300014 20071203 00014 NM 2007 12 3 AALA20072185 1 20071111 A 3350 8200037401 SIGN BOEING 777 777223 1385213 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 798AN 30797 JFK - EMERGENCY EXIT SIGN LIGHT AT OVERHEAD LEFT NUMBER FOUR DOOR DISCONNECTED. REPLACED EXIT SIGN AT OVERHEAD LEFT NUM BER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120300024 20071203 00024 NM 2007 12 3 AALA20072213 1 20071115 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 975AN 29549 LGA - EMERGENCY LIGHT AT SEAT 9D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT A16WE 2007120300025 20071203 00025 WP 2007 12 3 AALA20072206 1 20071114 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 955U 49427 LGA - EMERGENCY LIGHT AT OVERHEAD FORWARD GALLEY INOPERATIVE. SECURED LOOSE BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEA D FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007120300040 20071203 00040 EA 2007 12 3 SWIA200718870 1 20070802 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 906SW 7510 FS 280 FORWARD FLOOR SUPPORT IS CRACKED WITH SHEARED FASTENERS, FOUND AT C-CHECK. REPLACED FASTENERS AND FLOOR SUPPORT PER CRJ200 SRM 51-41-00, 51-40-11 AND 51-42-06. 2 L 7 2 4F RT A21EA 2007120300041 20071203 00041 EA 2007 12 3 SWIA200718871 1 20070802 A 5210 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 906SW 7510 PAX DOOR INTERCOSTAL IS CRACKED, FOUND AT C-CHECK. INSTALLED NEW INTERCOSTAL IAW CRJ200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007120300049 20071203 00049 SO 2007 12 3 SWIA200718879 1 20071115 A 5753 FLAP TRACK EMB 120 EMB120ER 3260203 SO T/E FLAP CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 288SW 120316 RIGHT INBOARD FLAP TRACK IS CRACKED. REPLACED FLAP TRACK WITH A SERVICEABLE UNIT IAW 57-53-02. 2 L 7 2 4T RT A31SO 2007120300050 20071203 00050 EA 2007 12 3 SWIA200718880 1 20071117 A 5610 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA O OTHER O OTHER DE DESCENT 1 NM 07 764SK 10229 RIGHT SIDE WINDSHIELD CRACKED ON DESCENT, FLIGHT NR 6105. REPLACED WINDSHIELD PER AMM 56-11-01, PN: NP-13932-003, SN OF F: 05157H1939. 2 L 7 2 4F RT A21EA 2007120300054 20071203 00054 EA 2007 12 3 SWIA200718884 1 20071116 A 3234 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA O OTHER O OTHER TO TAKEOFF 1 NM 07 405SW 7029 NOSE GEAR WILL NOT RETRACT, FLIGHT NR 3940. REPLACED NOSE LANDING GEAR SELECTOR VALVE AND PRIORITY VALVE IAW MM 32-33-1 5. NO DEFECTS NOTED, PN: 4622 SN ON: 440A SN OFF: 420. 2 L 7 2 4F RT A21EA 2007120300056 20071203 00056 EA 2007 12 3 SWIA200718886 1 20071117 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE DENTED A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 715SK 10179 FOUND DENT ON FUSELAGE ABOUT 10 FEET AFT OF GALLEY SERVICE DOOR, FLIGHT NR 6599. REPAIRED RIGHT SIDE FUSELAGE SKIN PER REO 670-53-00-0135. 2 L 7 2 4F RT A21EA 2007120300059 20071203 00059 EA 2007 12 3 SWIA200718889 1 20071118 A 3242 QUICK DISCONNECT CNDAIR CL600 CL6002B19 1900309 EA NR 1 BRAKE LOOSE A SWIA O OTHER O OTHER LD LANDING 1 NM 07 909SW 7558 ON LANDING ROLL, THE AIRPLANE SEEMED TO VEER TO THE RIGHT WHEN BRAKES WERE APPLIED, FLIGHT NR 6472. FOUND NR 1 BRAKE QU ICK DISCONNECT TO BE LOOSE. SECURED THE QUICK DISCONNECT FITTING IAW CRJ 200 AMM 32-41-05. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007120300067 20071203 00067 NM 2007 12 3 QXEA200701741 1 20071117 A 5320 ANGLE BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 C4 PDX - ANGLE PIECE ON BACKSIDE OF FRAME X196.000 TO TOP OF STRINGER 24P CORRODED AROUND FORWARD RIVET. REPAIRED IAW S RM 53-20-43, 51-42-05, 51-25-10. 2 H 7 2 4T RT A13NM 2007120300084 20071203 00084 EU 2007 12 3 07FDEA04887 1 20071120 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT CARGO BILGE, CORROSION ON STR-56R, FR-58 TO FR-59. STRINGER WAS REPLACED. 2 L 7 2 4F RT A35EU 2007120300085 20071203 00085 EU 2007 12 3 07FDEA04888 1 20071120 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FOUND AFT PIT STR 54R CORRODED AT FRAME 58 -59. REPAIRED IAW SRM 53-10-14 FIG 210. 2 L 7 2 4F RT A35EU 2007120300090 20071203 00090 NM 2007 12 3 QXEA200701750 1 20071117 A 2731 3994001013 ACTUATOR BOMBDR DHC8 DHC8402 1390042 NM ELEVATOR TRIM MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 400QX 3395 3395 4030 SEA - DURING CLIMB-OUT, THE PITCH TRIM CAUTION ILLUMINATED, ALSO PFD AUTO TRIM FAIL MESSAGE DISPLAYED. COMPLETED PITCH TRIM CAUTION CHECKLIST. MAINTENANCE REMOVED AND REPLACED ELEVATOR PITCH TRIM ACTUATORS. OPERATIONAL CHECK GOOD. AIRCR AFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007120300091 20071203 00091 NM 2007 12 3 QXEA200701751 1 20071117 A 3620 WARNING SYSTEM BOMBDR DHC8 DHC8402 1390042 NM BLEED AIR SYS MALFUNCTIONED A QXEA K NONE N FALSE WARNING UK UNKNOWN 1 NM 09 408QX 4050 SEA - NR 1 BLEED HOT MASTER CAUTION ILLUMINATED ON DESCENT DUCT TEMPS WERE NORMAL. TURNED BLEEDS OFF PER CHECKLIST LIGH T WENT OUT AFTER A COUPLE MINUTES. MAINTENANCE GROUND RAN BOTH ENGINES, TURNED BLEED AIR ON INDIVIDUALLY AND TOGETHER O PERATED BLEEDS AT MIN AND MAX FLOW. NO FAULTS FOUND. ALL INDICATIONS NORMAL. CHECKS GOOD. AIRCRAFT RETURNED TO SERVI CE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007120300096 20071203 00096 EU 2007 12 3 DHLA200700067 1 20071123 A 3350 LIGHT AIRBUS 300 A300B4203 3930306 EU CABIN INOPERATIVE A DHLA K NONE O OTHER NR NOT REPORTED 1 GL 05 363DH 085 EMERGENCY EXIT LIGHT DISARM WARNING DOES NOT ILLUMINATE. REPLACED LIGHT BULBS ON DISARM CAPSULE PER MM 33-51-00. OPS T EST OK. 2 L 7 2 4F RT A35EU 2007120300105 20071203 00105 NM 2007 12 3 FDKA200708378 1 20070809 A 3350 78812 LIGHT DHAV DHC8 DHC8101 2809002 NM CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 926HA 114 FDM 6175 ALB-JFK (0459 PHX LCL) - 2 FLOOR EMERGENCY STRIP LIGHTS INOP. MX RELAMPED LIGHT STRIPS. 2 H 7 2 4T RT A13NM 2007120300108 20071203 00108 SO 2007 12 3 FDKA200708383 1 20070812 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 838MJ 145384 FDM 6132 MCO (1540 PHX LCL) - EMERGENCY EXIT OVERHEAD LIGHT AT ROW 12 INOP. MX OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007120300111 20071203 00111 NM 2007 12 3 FDKA200708388 1 20070815 A 3397 WIRE DHAV DHC8 DHC8101 2809002 NM CABIN DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 926HA 114 FDM 6014 JFK-SYR (0951 PHX LCL) - OVERHEAD CEILING ENERGENCY LIGHT INOP. MX REPAIRED WIRING TO LIGHT ASSY. 2 H 7 2 4T RT A13NM 2007120300123 20071203 00123 NM 2007 12 3 HALA0700494 1 20071119 A 3350 ADAPTER BOEING 767 7673CB 1385187 NM CABIN DEFECTIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 588HA 33466 EMERGENCY FLOOR LIGHTING EXTINGUISHED DURING TEST, BETWEEN SEAT 25AB TO 26 AB. REMOVED AND REPLACED LIGHTING STRIP ADAP TER, OPS CHK EMERGENCY LTS ALL CHK OK. 2 L 7 2 4F RT A1NM 2007120300142 20071203 00142 NM 2007 12 3 SWAA075869 1 20071126 A 5753 65C30462 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED BRDG CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED INBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007120300145 20071203 00145 NM 2007 12 3 SWAA075864 1 20071126 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED MV2 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007120400008 20071204 00008 CE 2007 12 4 AMWA88325BC 1 20071031 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MASTER MALFUNCTIONED A AMWA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 146ZV 9638 43 UE146 BATTERY CHARGE ANNUNCIATOR ILLUMINATED MULTIPLE TIMES DURING FLIGHT. MAINTENANCE REPLACED BATTERY AND CLEARED DISCREPANC Y. THIS TYPE DISCREPANCY IS CONSIDERED A DISTRACTION TO THE CREW AND A NUISANCE ITEM. 2 L 7 2 4T 3 T RT A24CE E2NE 2007120400011 20071204 00011 EA 2007 12 4 S9BA200700025 1 20071202 A 3246 13000 FLOAT DHAV DHC6 DHC6* 2802606 EA PWA PT6 PT6A27 52043 EA MLG TORN A S9BA K NONE O OTHER TX TAXI/GRND HDL 1 SO 29 888PV 620 HOLE IN LT FLOAT ABOVE WATER LINE. THE HOLE WAS LOCATED BETWEEN BAYS 4 AND 5 LT FLOAT OB. AIRCRAFT WAS FERRIED FROM SP B TO SSB. REMOVED AND REPLACED FLOAT ASSY IAW SBA WC 32.01 1 H 7 2 3T 4 T A9EA E4EA 2007120400041 20071204 00041 NM 2007 12 4 AALA20072229 1 20071104 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 976AN 30099 TUL- EMERGENCY LIGHT AT LEFT AFT CABIN OVERHEAD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT AFT CABI N OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007120400046 20071204 00046 NM 2007 12 4 AALA20072237 1 20071117 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 692AA 26972 SFO - EMERGENCY LIGHTS FROM SEAT ROW 26 TO AFT OF CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT FROM SEA T ROW 26 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007120400049 20071204 00049 NM 2007 12 4 AALA20072241 1 20071117 A 2120 UNKNOWN BOEING 777 777223 1385213 NM COCKPIT ODOR A AALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 776AN 29582 EICAS SMOKE CREWREST FLIGHT DECK ANNUNCIATED SHORTLY AFTER TAKEOFF WITH CORRESPONDING SMOKE ALARM IN THE FLIGHT DECK CRE WREST AREA. THERE WAS A PUNGENT ODOR BUT NO VISIBLE SMOKE. THE ALARM WENT OFF AFTER APPROXIMATELY TWO MINUTES. THE OD OR RETURNED DURING DESCENT WITH NO ALARM. LANDED NRT WITHOUT INCIDENT. OPERATED AIR CONDITIONING SYSTEM AND SMOKE DETE CTORS WITH NO FAULTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120400053 20071204 00053 CE 2007 12 4 DXTA200702557 1 20071019 A 2150 73838433 ACM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL A/C BAY LEAKING E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 946QS 2463 2463 7500195 CABIN FILLED WITH ENGINE EXHAUST ODOR INSTALLED REPAIRED ACM IAW 750MM 21-51-00. OPS CHECKED GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007120400055 20071204 00055 CE 2007 12 4 DXTA200702559 1 20071022 A 2730 6223260 FUSE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP AFT SERVICE BAY OPEN E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 895QS 3497 258606 ELECTRIC ELEVATOR TRIM FAILED IN FLIGHT. REMOVED AND REPLACED ELEVATOR E-TRIM SERVO FUSE ZL-F24 PN:622-3260 SN:1CKYC AN D PN: 5920-99-012-0075. PERFORMED SYSTEM FUNCTIONAL CHECK IAW AMM 27-30-00. 2 L 7 2 4F 4 F RT A3EU E6WE 2007120400064 20071204 00064 SO 2007 12 4 GLBA2006017 1 20071028 A 2150 A/C PACK EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LEFT ODOR A GLBA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 NM 03 297UX 120297 SMOKE/SMELL - FLIGHT 4961 ENROUTE, THE PILOTS REPORTED THAT THE LT PACK EMITTED A BURNING ODOR WHICH SET OFF THE SMOKE A LARM. MAINTENANCE PLACED THE ISSUE ON MEL 21-50-2 CATEGORY C. MAINTENANCE TROUBLESHOT THE LT PACK SYSTEM AND OPERATION AL CHECKS WERE GOOD IAW MM 21-00. NO FAULTS FOUND. 2 L 7 2 4T 4 T RT A31SO E20NE 2007120400077 20071204 00077 EU 2007 12 4 07FDEA04895 1 20071121 A 5340 A5377364420100 FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FWD PIT FRAME STA 38.2 RT FRAME TO FLOORBEAM CONNECTION FITTING CORRODED. REMOVED ALL SUBSTRUCTURE AND CARGO SYS COMPON ENTS COMMON TO FRAME FITTING AREAS FROM FR 33 - 38.2 RT IAW A310-200 AMM 25-52-48-4,44-4,26-4 AND A310-200 AMM 25-52-4 8-4 AND A310-200-SRM 51-40-21. REMOVED AND REPLACED FRAME FITTING AT FR 38.2 RT IAW A310-200-SRM 51-72-10. REINSTALLED A LL PREVIOUSLY REMOVED SUBSTRUCTURE AND CARGO SYS COMPONENTS IAW A310-200-AMM 25-52-48-4, AND A310-200 SRM 51-40-21. A310 - 200 AMM 25-52-44-4, A310-200 AMM 25-52-26-4. MAJOR REPAIR. 2 L 7 2 4F RT A35EU 2007120400078 20071204 00078 EU 2007 12 4 07FDEA04896 1 20071121 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FOUND AFT PIT STR 51R , FRAME 54.3-58 STRINGER CORRODED. CUT OUT CORRODED SECTION AND SPLICED IN NEW SECTION IAW SRM 53 -10-14 AND SRM 51-40-44. 2 L 7 2 4F RT A35EU 2007120400080 20071204 00080 NM 2007 12 4 07FDEA04898 1 20071122 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 MAIN DECK, SEAT TRACK BELOW FLOOR PANEL NR 281CS LOWER SURFACE FOUND CORROSION AT STA 5-83 AND STA 1531. REPAIRED AS PE R SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007120400119 20071204 00119 NM 2007 12 4 07FDEA04917 1 20071124 A 5330 6554575 SKIN BOEING 727 727225 1384077 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 RT FUSELAGE SKIN UNDER WING TO BODY TO FAIRING 3442 HAS CORROSION AROUND NUTPLATE HOLES AND FRETTING ALONG MATING SURFAC E REMOVED CORROSION REF SRM 51-10-6, ORIGINAL MATERIAL THICKNESS "T" .060" AFTER BLENDING, REMAINING MATERIAL THICKNESS IS .043" AND IS OUT OF LIMITS REF 53-30-3 FIG 5. INSTALLED REPAIR REF SRM 53-30-3 FIG 5. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2007120400123 20071204 00123 NM 2007 12 4 AMTA200700575 1 20071101 A 5320 INTERCOSTAL BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE BS 1661-1681 BROKEN A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 522AT 29330 INTERCOSTAL UPPER ANGLE BROKEN IN 3 AREAS AROUND FASTENER HOLES IN MAIN CABIN AFT FLOOR STRUCTURE BETWEEN FS 1661-1681, RBL 10. REMOVED DAMAGED ANGLE AND FABRICATED NEW IAW SRM 53-00-01. TREATED PRIMED IAW SRM 51-21-01. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007120400141 20071204 00141 EA 2007 12 4 A6WA200740605 1 20071107 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 426AW 7669 FOUND CRACK EXIST ON ANGLE CLIP FS 280 LBL 9 INBOARD CLIP AND RBL 9 INBOARD CLIP. REPLACED IAW CRJ 200 SRM 51-42-06. ( M) 2 L 7 2 4F RT A21EA 2007120400147 20071204 00147 EA 2007 12 4 A6WA200740610 1 20071107 A 5751 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT AILERON DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 426AW 7669 RIGHT AILERON, UPPER LEADING EDGE SKIN BTW WS 389 TO WS 285, ABRASION EXIST. ABRASION FOUND OUT OF LIMITS IAW REO 601R- 57-60-013. LEADING EDGE SKIN ON RIGHT AILERON (UPPER) REPLACED IAW CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007120400158 20071204 00158 WP 2007 12 4 ABXA070373 1 20071019 A 5310 99578606 ANGLE DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 45596 DURING COCKPIT WINDSHIELD FRAME MOD, FOUND ANGLE AT INBOARD TIP OF FRAME CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-2 AN D 51-30-5. 2 L 7 2 4F A6WE 2007120400163 20071204 00163 CE 2007 12 4 DJFA2007123 1 20071103 A 2910 AE2847G0536180 HOSE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HYD SYSTEM RUPTURED E DJFA O OTHER K FLUID LOSS AP APPROACH 1 EA 23 413LX 11514 RK209 ON APPROACH CREW EXPERIENCED COMPLETE HYDRAULIC FAILURE AT 4000' ON APPROACH INTO KDAL, LOST ALL HYDRAULIC PRESSURE WITH IN ABOUT 20 SEC. AFTER FIRST INDICATION OF A PROBLEM, DECLARED AN EMERGENCY, RAN THE EMERGENCY CK LIST FOR GEAR EXTENSIO N, ZERO FLAP LANDING, AND EMERGENCY BRAKING. LANDED AND USED EMERGENCY BRAKING. CREW FOUND HYDRAULIC RESERVOIR COMPLET ELY EMPTY. MAINTENANCE DISCOVERED HYDRAULIC PUMP PRESSURE HOSE RUPTURED. THERE WAS NO EVIDENCE OF CHAFFING OR OTHER DAM AGE TO THE HOSE AT THE POINT WHERE IT RUPTURED HOSE WAS REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007120400176 20071204 00176 CE 2007 12 4 DJFA2007125 1 20071108 A 5522 SKIN RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP ELEVATOR CORRODED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 831LX 258510 DURING POST FLIGHT INSPECTION CREW NOTED EVIDENCE OF CORROSION ON THE ELEVATOR LEADING EDGES. MAINTENANCE DISCOVERED TH E CORROSION TO BE MODERATE AND OUT OF REPAIRABLE LIMITS. MAINTENANCE REPLACED THE LEADING EDGE. 2 L 7 2 4F 4 F RT A3EU E6WE 2007120400179 20071204 00179 WP 2007 12 4 ABXA070370 1 20071019 A 5310 99115056 WINDOW FRAME DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 45596 DURING COCKPIT WINDSHIELD FRAME MOD, FOUND FRAME 9911505-6 CRACKED AT INBOARD END. REPAIRED FRAME IAW DC9 SRM 53-03, FI GURE 34. 2 L 7 2 4F A6WE 2007120400180 20071204 00180 WP 2007 12 4 ABXA070371 1 20071019 A 5310 99115057 WINDOW FRAME DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 45596 DURING COCKPIT WINDSHIELD FRAME MOD, FOUND FRAME 9911505-7 CRACKED AT BOTH ENDS. REPAIRED FRAME IAW DC9 SRM 53-03, FIGU RE 34. 2 L 7 2 4F A6WE 2007120400185 20071204 00185 NM 2007 12 4 USAA920071215 1 20071124 A 5312 PRESSURE PANEL BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - C6 CHECK, CRACKED PRESSURE PANEL, BS 663, LBL 31, WL 208.1. REPAIRED PRESSURE PANEL, BS 663, LBL 3 1, WL 208.1 IAW USAIRWAYS TYPICAL REPAIR 53-60-04. 2 L 7 2 4F RT A16WE 2007120400186 20071204 00186 EU 2007 12 4 USAA920071216 1 20071112 A 5347 D53371110001 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 625AW 64 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON SEAT TRACK, BS 1810/FR 41 - BS 2136/FR 47, -Y765. REPLACED SEAT TRACK, BS 1810/FR 41 - BS 2136/FR 47, -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007120400189 20071204 00189 EU 2007 12 4 USAA920071219 1 20071112 A 5320 D53471123200 PLATE AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 625AW 64 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON SUPPORT PLATE, BS 3310/FR 69 - BS 3366/FR 70, S23R. REPLACED SUPPORT PLATE , BS 3310/FR 69 - BS 3366/FR 70, S23R IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007120400192 20071204 00192 EU 2007 12 4 USAA920071222 1 20071119 A 5320 D53480020342 SHEAR PLATE AIRBUS 320 A320231 3930325 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 625AW 64 SAL - MAJOR REPAIR - CRACKED SHEAR PLATE, BS 3257/FR 68 - BS 3310/FR 69, S23L. REPLACED SHEAR PLATE, BS 3257/FR 68 - BS 3310/FR 69, S23L IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007120400194 20071204 00194 NM 2007 12 4 USAA920071224 1 20071123 A 5753 6546481105 CARRIAGE BOEING 737 7373G7 1384595 NM T/E FLAP CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, CORROSION ON LEFT WING OUTBOARD MIDFLAP NR 2 CARRIAGE ASSEMBLY. REPLACED LEFT WING OUTB OARD MIDFLAP NR 2 CARRIAGE ASSEMBLY IAW B737 AMM 27-51-44. 2 L 7 2 4F RT A16WE 2007120400196 20071204 00196 WP 2007 12 4 07FDEA04924 1 20071126 A 5347 S4929147 SEAT TRACK DOUG MD10 MD1010F 3022112 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 MAIN CABIN FLOOR TRACK SCALLOP BROKEN OUT AT STA 814 LBL 29. CHECKED LIMITS ON SEAT TRACK SCALLOPS. SCALLOPS TO SCALL OPS IS .510 OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21. DIAL CALIPERS USED T8278D. REMOVED SEAT TRACK IA W DC/MD10-10 SRM 51-31-01 VOL II PG 1. DRILLED NEW SEAT TRACK IAW DC/MD10-10 SRM 51-31-01 VOL I I PG 1. ALODINED AND PRIMED SEAT TRACK IAW DC/MD10-10 SRM 51-21-01 VOL II PG 21. INSTALLED SEAT TRACK IAW DC/MD10-10 SRM 51-31-01 VOL II PG 1. 2 L 7 3 4F RT A22WE 2007120400197 20071204 00197 WP 2007 12 4 07FDEA04925 1 20071126 A 5420 ANGLE DOUG MD10 MD1010F 3022112 WP NR 1 PYLON CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 NR 1 PYLON THRUST LINK RUBBING AGAINST WING O/B THRUST ANGLE, STA YN348 CENTERED THRUST LINK, CLEANED AREA AROUND ATTACH MENT PIN & BUSHING, INSPECTED AREA OF BEARING & BUSHING IAW FEDEX WORK CARD 54X1201ALI-P1 LUBED THRUST LINK BEARING I AW FEDEX MM 12-21-02-3, NO DISCREPANCIES NOTED 2 L 7 3 4F RT A22WE 2007120400198 20071204 00198 WP 2007 12 4 07FDEA04926 1 20071126 A 5347 4929150 SEAT TRACK DOUG MD10 MD1010F 3022112 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 FOUND MAIN CABIN, BS 1085, RBL 28, SEAT TRACK SCALLOP CHIPPED. BLENDED AREA; CHECKED LIMITS. GAP BETWEEN SCALLOPS IS.5 20 MAX ALLOWED IS .500 OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21. REMOVED DAMAGED TRACK SECTION AND INSTAL LED NEW SECTION IAW DC/MD10-10 SRM 51-31-01 VOL II PG 1. MAT ID NEW TRACK SECTION FABED NEW TRACK IAW DC/MD10-10 SRM 53-70-00 VOL I FIG 1. ALODINED AND PRIMED NEW SECTION IAW DC/MD10-10 SRM 51-21-01 VOL II PG 1-24, REMOVED AND REINSTA LLED FLOOR PANELS IAW DC/MD10-10 M/M 53-21-01-2 2 L 7 3 4F RT A22WE 2007120400201 20071204 00201 WP 2007 12 4 07FDEA04929 1 20071126 A 5347 S4929405 SEAT TRACK DOUG MD10 MD1010F 3022112 WP FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 CABIN FLOOR TRACK GOUGED AT STA 1119 RBL 48 2 EACH SCALLOPS. 2 L 7 3 4F RT A22WE 2007120400202 20071204 00202 WP 2007 12 4 07FDEA04930 1 20071126 A 5347 S4929405 SEAT TRACK DOUG MD10 MD1010F 3022112 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 CABIN FLOOR TRACK SCALLOP BROKEN OUT AT STA 1059 LBL 48. FOUND TO BE OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 PGS 21 & 22 VOL I REMOVED TRACK IAW DC/MD10-10 SRM 51-31-01 VOL II PGS 1-10. IAW DC/MD10-10 SRM 53-42-01 VOL III PGS 13 & 14 . FABRICATED SEAT TRACK IAW DC/MD10-10 SRM 53-70-00 VOL I PGS 3 & 6A. ALODINED AND PRIMED IAW DC/MD10-10 SRM 51-31-01 VOL II PGS 1-10 STA 989-1109 LBL 48 REMOVED AND INSTALLED FLOORBOARDS STA 979-1159 LBL 26-76 IN REF TO MD10 AMM 53-21- 01-2 2 L 7 3 4F RT A22WE 2007120400204 20071204 00204 EU 2007 12 4 07FDEA04932 1 20071126 A 5340 A5377364420000 ATTACH FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FWD LWR CARGO COMP, FR 38.1 LT FRAME TO CROSS BEAM CONNECTION FITTING CRACKED. CLEANED AREA IAW AMM12-21-2, REMOVED, LOCATED & INSTALLED FITTING IAW SRM 51-72-10 PG 2 PARA 5. 2 L 7 2 4F RT A35EU 2007120400205 20071204 00205 EU 2007 12 4 07FDEA04934 1 20071126 A 5320 A5377364420000 FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FWD LWR CARGO COMP, FR 37 LT FRAME TO CROSS BEAM CONNECTION FITTING CRACKED. CLEANED AREA IAW A310-200 SRM 51-72-10 LOC ATED & DRILLED NEW FITTING P/N 5377364420000 PO# 598020.3 IAW A310-200 SRM 51-72-10 INSTALLED FITTING IAW A310-200 SRM 51-72-00 CORROSION LEVEL MISTAKENLY CHECKED THIS ITEM NOT CORROSION. 2 L 7 2 4F RT A35EU 2007120400207 20071204 00207 EU 2007 12 4 07FDEA04936 1 20071126 A 5320 A5377364420300 FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FWD LWR CARGO COMP, FR 38.1 RT FRAME TO CROSS BEAM CONNECTION FITTING CORRODED. REMOVED FITTING IAW A310-200 SRM 51- 72-10 PG 2 PARAG 5A LOCATED AND DRILLED NEW FITTING P/N A5377364420100 PO 598232.3 IAW A310-200 SRM 51-72-10 PG 2 PARAG 6A INSTALLED NEW FITTING IAW A310-200 SRM 51-40-30 2 L 7 2 4F RT A35EU 2007120400209 20071204 00209 EU 2007 12 4 07FDEA04938 1 20071126 A 5320 A5377364420100 FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FWD LWR CARGO COMP, FR 38 RT FRAME TO CROSS BEAM CONNECTION FITTING CRACKED. REMOVED FITTING IAW A310-200 SRM 51-72-10 PG 2 PARAG 5A LOCATED AND DRILLED NEW FITTING P/N AS5377364420100 PO 598232.1 IAW A310-200 SRM 51-72-10 PG 2 PARAG. 6A INSTALLED FITIING IAW A310-200 SRM 51-40-30 2 L 7 2 4F RT A35EU 2007120400210 20071204 00210 EU 2007 12 4 07FDEA04940 1 20071126 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FOUND AFT PIT STR 47R AT FRAME 59 IS GOUGED ON UPPER SURFACE. REMOVED GOUGE ON STRINGER 47R IAW FEDEX A310 SRM 51-73- 10, STRINGER 47R OUT OF LIMITS IAW A310 SRM 53-10-00. REMOVED IEA SHEAR TIE AT FRAME 59 BETWEEN STRINGER 47R AND 48R I AW A310 SRM 51-40-21 PG 23-27. REMOVED DAMAGE STRINGER SECTION IAW A310 SRM 52-10-14 203/204 FIG201. LOCATED AND DRILL ED NEW STRINGER SECTION IAW A310 FABBED REPAIR COUPLING IAW A310 53-10-14PG 203/204 FIG 201 ALODINED REPAIR PARTS I AW A310 SRM 51-21-10 PRIMED AND TOP COATED REPAIR PARTS IAW A310 SRM 51-23- 10 INSTALLED NEW STRINGER SECTION AND COUPL ING IAW A310 53-10-14 PG203/204 FIG201. INSTALLED SHEAR TIE IAW A310 SRM 51-40-21 PG 23-27. 2 L 7 2 4F RT A35EU 2007120400211 20071204 00211 EU 2007 12 4 07FDEA04941 1 20071126 A 5320 A5377364420100 FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FWD LWR CARGO COMP, AT FR STAT 36 RT FRAME TO FLOORBEAM CONNECTION FITTING CRACKED. REMOVED FITTING IAW A310-200 SRM 51 -72-10. LOCATED AND DRILLED NEW FITTING P/N A5377364420100 IAW A310-200 SRM 51-72-10 PG 2 PARAG 6A INSTALLED NEW FITTING IAW A310-200 SRM 51-40-30 2 L 7 2 4F RT A35EU 2007120400212 20071204 00212 EU 2007 12 4 07FDEA04942 1 20071126 A 5320 AS377364420100 FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FWD LWR CARGO COMP AT FR 35 RT FRAME TO FLOORBEAM CONNECTION FITTING CRACKED. REMOVED FITTING IAW A310-200 SRM 51-72-10 PG 2 PARAG. 5A LOCATED AND DRILLED NEW FITTING P/N AS377364420100 PO3 598232.2 IAW A310-200 SRM 51-72-10 PG 2 PARAG. 6A ISTALLED FITTING IAW A310- 200SRM 51-40-30. 2 L 7 2 4F RT A35EU 2007120400213 20071204 00213 NM 2007 12 4 07FDEA04943 1 20071127 A 3260 WARNING SYSTEM DOUG MD11 MD11F 3023600 NM COCKPIT ACTIVATED A FDEA O OTHER J WARNING INDICATION DE DESCENT 1 SO 25 603FE 48459 AFTER SELECTING GEAR DOWN RECEIVED ANTI-SKID R FAIL AND RT MAIN GEAR RED UNSAFE LIGHT. EXECUTED GO-AROUND. RECYCLED MA IN GEAR ONLY TO HAVE BOTH ALERTS APPEAR AGAIN. COMPLIED WITH QRH PROCEDURES AND LANDED ON LONGEST RWY FLAPS 50 WITHOUT INCIDENT. REMOVED AND REPLACED FWD RT MLG DOWN AND LOCKED SENSOR (D1-43). 2 L 7 3 4F RT A22WE 2007120400215 20071204 00215 CE 2007 12 4 DXTA200702590 1 20071103 A 2910 RESERVOIR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE HYD SYSTEM LOW E DXTA O OTHER O OTHER LD LANDING 1 GL 07 398QS 5600522 CO-PILOT'S RT BRAKE IS SPONGY, WILL PUMP UP AFTER SEVERAL APPLICATIONS. INSPECTED RESERVOIR, PUMP/MOTOR, ACCUMULATOR, AN TISKID VALVES FITTINGS, (4) MASTER CYLINDERS RT BRAKE AND ASSOCIATED PLUMBING NO LEAKS FOUND, THOROUGHLY BLED RT BRAKE M M 32-42-00. SERVICED RESERVOIR COMPLETED TAXI CHECK NO DISCREPANCIES OPERATING GOOD AT THIS TIME. 2 L 7 2 4F 4 F RT A22CE E25EA 2007120400219 20071204 00219 CE 2007 12 4 DXTA200702592 1 20071103 A 3240 38771 RELAY BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE POWER BRAKE INOPERATIVE E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 161QS 144 144 RK435 WHEEL BRAKES FAILED DURING TAXI OUT. REPLACED POWER BRAKE RELAY VALVE ASSY IAW 32-40-00. OPS CK GOOD. 2 H 7 2 4F 4 F RT A16SW E25EA 2007120400222 20071204 00222 NM 2007 12 4 DXTA200702595 1 20071104 A 3010 861CAU2 TRANSMITTER AMD FALC50 FALCON2000 2730170 NM PWC PW308 PW308C 52182 NE AOA HEAT INOPERATIVE E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 221QS 1928 54 AT THE INITIATION OF THE TAKEOFF ROLL AND AT APPROXIMATELY 60 KTS THE YELLOW CAS MESSAGE AOA HEAT NR 2 ILLUMINATED. REMO VED AND REPLACED ANGLE OF ATTACK TRANSMITTER WITH REPAIRED UNIT AS REQUIRED. OPS CHECK GOOD. HEAT TEST GOOD AT THIS TIME . WORK IAW MM 27-804, 30-300. 2 L 7 2 4F 4 F RT A50NM E00065EN 2007120400226 20071204 00226 CE 2007 12 4 DXTA200702597 1 20071104 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG LEAKING E DXTA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 GL 07 382QS 5600382 ON TAXI OUT, BRAKES PULLED HARD TO THE RT FROM BOTH CAPT AND FO POSITION. FOUND LEAK IN LT HAND BRAKE ASSY. TIGHTEN AND BLED SYSTEM, LEAK CHECKS GOOD TAXI CHECKS GOOD IAW 560MM 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007120400227 20071204 00227 EA 2007 12 4 SWIA200718890 1 20071126 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 417SW 7400 FLT 2509 - MAIN CABIN DOOR HANDLE WOULD NOT OPEN FROM THE OUTSIDE. INSPECTED, CLEANED AND LUBED DOOR. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2007120400228 20071204 00228 CE 2007 12 4 DXTA200702598 1 20071105 A 7500 S101816PG SENSOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL BLEED SYS INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 915QS 142 7500015 WING BLEED LEAK R CAS MESSAGE CAME ON DURING CRUISE, REDUCED PWR AND MESSAGE EXTINGUISHED. REMOVED AND REPLACED RT SENSO R TR020 DUE TO FAILED CALIBRATION CHECK. SYSTEM THEN OPS CHECKED GOOD AT ALL POWER SETTINGS- NO CAS MESSAGES. ALL WORK D ONE IAW THE CE750 MM CHAP 30-16-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007120400229 20071204 00229 EA 2007 12 4 SWIA200718891 1 20071125 A 5753 FLAP CNDAIR CL600 CL6002B19 1900309 EA LT WING DAMAGED A SWIA O OTHER F FLT CONT AFFECTED UK UNKNOWN 1 NM 07 961SW 7857 LEFT OUTBOARD FLAP IS DAMAGED ALONG TRAILING EDGE. REPLACED FLAP PER 27-54-05. 2 L 7 2 4F RT A21EA 2007120400230 20071204 00230 CE 2007 12 4 110507N542CS1 1 20071105 A 3010 BOOT CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE TAIL LEAKING E Z5FA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 63 542CS 5605523 TAIL DEICE INOP IN ICING CONDITIONS. CREW REQUESTED EMERGENCY DECENT TO GET OUT OF ICING CONDITIONS. AT LOWER ALTITUDE S YSTEM STARTED WORKING PROPERLY, SYSTEM WAS CHECKED AGAIN ON THE GROUND SATISFACTORILY. AS A RESULT OF THE WAY THE SYSTEM WAS OPERATING, THE CREW DID NOT WRITE UP ANY DISCREPANCIES. MAINTENANCE PERSONNEL FOUND SEVERAL PIN HOLES IN TAIL BOOTS AND PATCHED AS REQUIRED. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007120400236 20071204 00236 EA 2007 12 4 SWIA200718894 1 20071121 A 3520 OXYGEN MASK CNDAIR CL600 CL6002B19 1900309 EA CABIN UNWANTED DEPLOY A SWIA G O2 MASK DEPLOYED O OTHER LD LANDING 1 NM 07 405SW 7029 FLT 5889 - OXYGEN MASKS ABOVE SEATS 7A AND 7B DEPLOYED INADVERTANTLY ON LANDING. REPACKED OXYGEN MASKS IAW 35-21-09. 2 L 7 2 4F RT A21EA 2007120400243 20071204 00243 EU 2007 12 4 420611112007 1 20071111 A 2612 FIRE WARNING SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B1 60056 NE FALSE ACTIVATION E QMLA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 03 544AM 4206 SECOND OCCURRENCE OF A FALSE ENGINE FIRE WARNING ON THIS AIRCRAFT IN THE LAST THREE DAYS. ONE FLIGHT OCCURRED BETWEEN TH E TWO INCIDENTS. ARRIVED AT HOSPITAL TO PICK UP PATIENT TO TRANSPORT TO ANOTHER HOSPITAL. WHEN THE TWIST GRIP WAS PLACED IN THE IDLE POSITION, THE (ENG FIRE) WARNING LIGHT ON THE CWP CAME ON. CREW MEMBERS WERE ASKED TO CONFIRM IF THERE WAS FIRE OR SMOKE. NONE WAS OBSERVED. SHUTDOWN THE ENGINE AND DID A VISUAL INSPECTION OF THE ENGINE AND ENGINE COMPARTMENT. NO EVIDENCE OF FIRE WAS APPARENT. CONTACTED DISPATCH AND ADVISED THE AIRCRAFT WAS OUT OF SERVICE. THE PILOT CONTACTED HI S SUPERVISOR AND THE BASE MECHANIC. THE BASE MECHANIC WAS TROUBLESHOOT THE WARNING AND THE MECHANICAL INSPECTION AGAIN R 1 G 7 1 3U 3 U H9EU E00054EN 2007120400244 20071204 00244 EA 2007 12 4 SWIA200718898 1 20071121 A 3350 INVERTER CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 967SW 7872 FLT 6045 - EMERGENCY FLOOR LIGHTING INOP FROM ROW 9 AND BACK. REPLACED INVERTER IAW CRJ MM 33-51-07. 2 L 7 2 4F RT A21EA 2007120400245 20071204 00245 EA 2007 12 4 SWIA200718899 1 20071121 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 430SW 7523 FLT 3810 - FIRST OFFICERS WINDSHIELD SHATTERED IN FLIGHT. REPLACED THE RIGHT WINDSHIELD IAW CRJ AMM 56-11-01, PN: NP139 321-14, SN OFF: 01058H2081. 2 L 7 2 4F RT A21EA 2007120400246 20071204 00246 EU 2007 12 4 350611102007 1 20071110 A 3150 UNKNOWN UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE UNKNOWN E QMLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 03 130LN 3506 UPON COMPLETION OF REFUELING, PILOT AND CREW PERFORMED WALK-AROUND AND NORMAL ENGINE START. AFTER CLEARANCE FROM TOWER D EPARTED FOR A SCENE FLIGHT. TWO MILES OUT OF AIRPORT, MGB PRESSURE LIGHT STARTED TO FLICKER WITH AUDIO WARNING (GONG). WARNING LIGHT THEN ILLUMINATED STEADY (ON) AND AIRCRAFT WAS RETURNED TO THE AIRPORT WITHOUT INCIDENT. LIGHT EXTINGUISHED AFTER LANDING. POST-FLIGHT REVEALED NORMAL OIL LEVEL. BASE MECHANIC CLEANED ALL ELECTRICAL CONNECTORS AND CHECKED OIL Q UANTITY. STARTED ENGINE AND GROUND RUN AT 100 PERCENT FOR FIVE MINUTES WITH NO FAULTS NOTED. AIRCRAFT WAS FLOWN ON FUNCT IONAL CHECK FLIGHT FOR 20 MINUTES WITH NO FAULTS. MECHANIC CHECKED ALL TRANSMISSION CONNECTORS AND FLUID LEVELS AND RETU 1 G 7 2 3U 3 U H9EU E00054EN 2007120400247 20071204 00247 SO 2007 12 4 GUUA11020703 1 20071102 A 3234 HANDLE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE MLG DAMAGED A GUUA O OTHER J WARNING INDICATION CR CRUISE 1 SO 29 282AS 120226 FLIGHT: 9166 NAS/FLL, DURING FLIGHT LT AND NOSE LANDING GEAR RED LIGHT ILLUMINATED. REPLACED LANDING GEAR SELECTOR HAND LE. LANDING GEAR OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2007120400248 20071204 00248 CE 2007 12 4 GUUA11020702 1 20071102 A 3240 BRAKE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG WEAK A GUUA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 29 190YV UE190 FLIGHT: 9188 VPS/TPA, DURING TAXI BRAKES FEEL NORMAL BUT WILL NOT STOP THE AIRCRAFT, NEED TO APPLY STRONG PRESSURE. BLE D ALL FOUR BRAKES. 2 L 7 2 4T 4 T RT A24CE E26NE 2007120400250 20071204 00250 CE 2007 12 4 DXTA200702605 1 20071111 A 5270 SWITCH CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE PAX DOOR MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 373QS 5600373 CABIN DOOR LIGHT ILLUMINATED IN FLIGHT. REMOVED CABIN DOOR SWITCH P/N P18M30 S/N 1020. INSTALLED NEW PART P/N P18M30 S /N 4317. OPERATIONAL AND LEAK CHECK GOOD. WORK DONE IAW CESSNA MAINTENANCE MANUAL 560 36-11-02. 2 L 7 2 4F 4 F RT A22CE E25EA 2007120400251 20071204 00251 CE 2007 12 4 DXTA200702606 1 20071111 A 3150 WARNING LIGHT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 987QS 7500087 DURING T/O ROLL, THE RED NO TAKEOFF CAS MESSAGE ILLUMINATED. T/O WAS ABORTED. CENTRAL COMPUTER MESSAGE HISTORY WAS RE VIEWED BY CREW AND HIGH SPEED TAXI WAS PERFORMED. CREW WAS UNABLE TO DUPLICATE DISCREPANCY. INSPECTED AIRCRAFT AND FLI GHT CONTROL FOR NORMAL POSITION. ALL SYSTEMS APPEAR TO BE WORKING IN SATISFACTORY CONDITION. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007120400254 20071204 00254 EA 2007 12 4 SWIA200718901 1 20071119 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 430SW 7523 FLT 3942 - CLIMBING THROUGH 32,400 HEARD A POP AND SAW THE PILOT WINDSHIELD CRACK. REPLACED PILOT'S WINDSHIELD, PN NP-1 39321-13, SN OFF 01162H9560. 2 L 7 2 4F RT A21EA 2007120400255 20071204 00255 CE 2007 12 4 DXTA200702603 1 20071110 A 2820 TUBE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL FUEL VENT DAMAGED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 962QS 7500126 IN LEVEL CRUISE FLIGHT, (RT WING O' FULL) CAS MESSAGE ILLUMINATED. FUEL WAS SEEN VENDING FROM RT WING. TOTAL FUEL 6470 N R- RT TANK 3240 NR TURNED OFF CTR WING X-FER. MSG EXTINGUISHED AND FUEL STOPPED VENDING AT 3200 LBS. COMPLETED SB750-28 -18 INBD CLIMB VENT TUBE REPLACEMENT. OPS AND LEAK CHECKED GOOD. WORK DONE IAW SB750-28-18. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007120400256 20071204 00256 NM 2007 12 4 F3LA200700318 1 20071111 A 5420 STRUCTURE AIRBUS A319 A319111 3930336 NM RT PYLON CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED CRACK EMANATING FROM RT PYLON (OTBD UPPER, ABOVE TR) SCREW HOLE. CUT OUT DAMAGE D AREA, FABRICATED REPAIR FILLER AND SPLICE, AND INSTALLED REPAIR IAW SRM 54-52-11, REPAIR E, STEP 2C; 54-52-12, FIG. 20 5; AND EA A9-54R-12271. 2 L 7 2 4F RT A28NM 2007120400259 20071204 00259 NE 2007 12 4 DHLA200700058 2 20071109 A 7200 ENGINE DOUG DC8 DC873 302199C WP GE CFM56 CFM562C1 13802 NE NR 2 SHUTDOWN A DHLA E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION TX TAXI/GRND HDL 1 GL 05 805DH 46125 WHILE FOR PARKING, NR 2 ENG FAILED, RESTARTED ENGINE AND TAXIED TO GATE NR 2. INSPECTED NR 2 ENG INLET AND EXHAUST, NO DEFECT NOTED. RUN ENG IAW JRH CAP 12.6., WORKING NORMAL. 2 L 7 4 4F 4 F RT 4A25 E2GL 2007120400262 20071204 00262 CE 2007 12 4 DXTA200702609 1 20071112 A 2840 SWITCH CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL FUEL SYSTEM MALFUNCTIONED E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 987QS 7500087 DURING T/O ROLL THE RED NO TAKEOFF CAS MESSAGE ILLUMINATED . TAKEOFF ABORTED. INSTALLED NEW LT AND RT LOW FUEL SWITCHES IAW CE-750 M/M 28-20-07. OPS AND LEAK CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007120400263 20071204 00263 2007 12 4 COEA0719908 4 20071117 A 3416 959960712326 ANTENNA AEROSP ATR42 ATR42300 8680920 EU RADAR ALTIMETER CORRODED A COEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 13 908FX 023 AIR TURN BACK, FLT 8813 - ON CLIMB-OUT AT CPR, THE RADAR ALTIMETER WAS VERY ERRATIC WITH MULTIPLE TERRAIN AHEAD WARNINGS . PILOT ELECTED TO RETURN TO CPR. AIRCRAFT LANDED WITHOUT INCIDENT. (M) 2 H 7 2 4T RT A53EU 2007120400264 20071204 00264 GL 2007 12 4 DXTA200702610 2 20071112 A 7320 FADEC CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MALFUNCTIONED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 989QS 7500089 FADEC BUSS FAIL LB , FAULT LB, FADEC LA CAS MESSAGE ON TAKEOFF, TAKEOFF ABORTED. TROUBLESHOT TO FAULTY LT "B" FADEC. RE PLACED WITH REPAIRED UNIT I.A.W CE-750 MM CHAP 70-12-00 & 71-00-04. OPS CHECK WAS GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007120400267 20071204 00267 SO 2007 12 4 GUUA11090701 1 20071109 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN INOPERATIVE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 268AS 120202 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT AFT EMERGENCY EGRESS LIGHT INOPERATIVE. REPLACED EMERGENCY EGRESS LI GHT ASSEMBLY. SYSTEM OPERATIONAL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2007120400268 20071204 00268 CE 2007 12 4 GUUA11090702 1 20071109 A 3240 BRAKE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT MLG WEAK A GUUA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 29 178YV UE178 FLIGHT: 9180 FPO/MIA, DURING TAXI LT BRAKE WILL NOT STOP AIRCRAFT WHEN DEPRESSED FULLY. PERFORMED LT BRAKE BLEEDING. O PERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2007120400269 20071204 00269 CE 2007 12 4 GUUA11090703 1 20071109 A 3240 BRAKE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LEFT MLG WEAK A GUUA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 29 178YV UE178 FLIGHT: 9171 MHH/MIA, DURING TAXI LT BRAKE WILL NOT STOP AIRCRAFT WHEN FULLY DEPRESSED. INSPECTED UNDER FLOOR FOR LEAKS . BLED LT BRAKE ASSEMBLIES. OPEARATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2007120400270 20071204 00270 2007 12 4 COEA0711911 4 20071114 A 3497 7003360946 CONNECTOR AEROSP ATR42 ATR42300 8680920 EU NR 2 AHRS DIRTY A COEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 NM 13 911FX 1228 045 FLT 7202 - ABORTED APPROACH, OVERFLYING KTN AND SIT, WHILE ON APPROACH INTO KTN FROM SEA, NR 2 AHRS WITH EFIS COMP ALERT ED ON THE CREW ALERT PANEL. APPROACH WAS TERMINATED AND THE AIRCRAFT CONTINUED ON TO JNU, OVERFLYING KTN AND SIT. AHRS CONNECTIONS CLEANED AND RESECURED. (M) 2 H 7 2 4T RT A53EU 2007120400272 20071204 00272 NE 2007 12 4 N425CT0003 2 20071031 A 7321 311949003 HYDROMECH UNIT BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE ENGINE RESTRICTED E T17A A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 17 425CT 250 RK523 PCEJG0033 PARTIAL POWER LOSS FROM RT ENGINE AT FL 390 POWER SURGED DURING APPROACH AND LANDING. 2 H 7 2 4F 4 F RT A16SW E25EA 2007120400277 20071204 00277 EA 2007 12 4 A6WA200740630 1 20071117 A 5230 HOUSING CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 470ZW 7927 FOUND CARGO DOOR HOUSING CRACK. (M) CARGO DOOR HOUSING REPLACED IAW CRJ SRM 51-42-21. (K) 2 L 7 2 4F RT A21EA 2007120400278 20071204 00278 EA 2007 12 4 A6WA200740632 1 20071115 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 427ZW 7685 FOUND SERVICE DOOR CUT-OUT LOWER SILL PLATE CORRODED P/N NR 601R38957-19. NEW SERVICEABLE LOWER SILL PROTECTIVE PLATE I NSTALLED IAW CRJ 200 SRM 51-41-02. (M) 2 L 7 2 4F RT A21EA 2007120400282 20071204 00282 NE 2007 12 4 AC2A118178 2 20071111 A 7200 250C40B ENGINE BELL 430 430 1182150 SW ALLSN 250C 250C40B 03032 NE NR 2 WARNING LIGHT E AC2A O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 07 430CF 49188 DURING FLIGHT THE NR 2 ENGINE CHIP SCAV CAUTION LIGHT BEGAN TO FLICKER. NO FLUCTUATIONS IN EITHER ENGINE TEMP OR PRESSUR E WERE NOTED. CONTINUED FLIGHT TO VENICE MONITORING ENGINE PARAMETERS. 1 G 7 2 3U 3 U RT H9SW E1GL 2007120400287 20071204 00287 CE 2007 12 4 GUUA11100701 1 20071110 A 3246 BEARING BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA NR 2 WHEEL FAILED A GUUA O OTHER S AFFECT SYSTEMS LD LANDING 1 SO 29 47542 UE198 FLIGHT: 9171, AFTER LANDING ROLL OUT LOST ALL BRAKE PRESSURE ON LT TOE BRAKES. DETERMINED NR TWO MAIN WHEEL ASSEMBLY BE ARING FAILED,REPLACED NR ONE AND TWO MAIN WHEEL ASSEMBLIES AND LT MAIN LANDING GEAR ASSEMBLY. 2 L 7 2 4T 3 T RT A24CE E2NE 2007120400288 20071204 00288 NM 2007 12 4 F3LA200700319 1 20071113 A 5321 FLOORBOARD AIRBUS A319 A319111 3930336 NM CABIN CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED BOTTOM OF FLOORBOARD 221FF CORRODED. REMOVED AND REPLACED FLOOR PANEL 221FF IAW MM 53-12-12-401 AND 53-12-12-400-001. 2 L 7 2 4F RT A28NM 2007120400289 20071204 00289 NM 2007 12 4 F3LA200700320 1 20071113 A 5321 FLOORBOARD AIRBUS A319 A319111 3930336 NM CABIN CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED BOTTOM OF FLOORBOARD 222FF CORRODED. REMOVED AND REPLACED FLOOR PANEL 222FF IAW MM 53-12-12-PB401 AND 53-12-12-400-001. 2 L 7 2 4F RT A28NM 2007120400291 20071204 00291 CE 2007 12 4 GUUA11110701 1 20071111 A 3230 1013880083 VALVE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG INTERMITTENT A GUUA O OTHER J WARNING INDICATION CL CLIMB 1 SO 29 69549 UE194 FLIGHT: 9276 EYW/FLL AFTER TAKEOFF THE LANDING GEAR REQUIRED RECYCLING FOUR TIMES TO RETRACT. REPLACED THE LANDING GEAR SERVICE VALVE. LANDING GEAR OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007120400298 20071204 00298 SO 2007 12 4 SIMA200733203 1 20071124 A 5240 14527605005 SKIN EMB 145 EMB145LR 3260212 SO COMM DOOR DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 667GB 9629 500 145784 DURING MBV INSPECTION, A DENT BEYOND MANUAL LIMITS WAS FOUND UNDER THE COMM DOOR ON THE FORWARD FUSELAGE. REPAIRED DENT ON FORWARD FUSELAGE UNDER COMM DOOR PER EMB SRM -145/1142 REV 38 CHAPTER 53-11-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007120400302 20071204 00302 2007 12 4 COEA0701819 4 20071030 A 3416 INDICATOR AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE NR 2 AIRSPEED MALFUNCTIONED A COEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 13 819FX 359 FLIGHT 8080 - ABORTED TAKEOFF, DURING TAKEOFF ROLL PILOT NOTICED NR 2 AIRSPEED INDICATOR READ ZERO, FOLLOWED BY (DACD DA TA INVALID) ON AFCS CONTROL PANEL. PILOT RETURNED TO RAMP AT OAK. REMOVED AND REPLACED ASI. AIRCRAFT RETURNED TO SERV ICE. DISCREPANCY RETURNED NEXT FLIGHT. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2007120400303 20071204 00303 EU 2007 12 4 COEA0709902 1 20071031 A 2797 E0052R10B6NSE CONNECTOR AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE TE FLAPS CONTAMINATED A COEA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 13 902FX 175 FLT 8788 -WHILE PERFORMING TAXI CHECKS AFTER A/C DEICING, CREW OBSERVED THAT THE FLAPS WOULD NOT EXTEND. THE CREW RETUR NED TO RAMP. CLEANED CONNECTORS, DEICE FLUID CONTAMINATION. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2007120400304 20071204 00304 EU 2007 12 4 COEA0702913 1 20071031 A 2150 ACM AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NR 1 SMOKE A COEA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 13 913FX 250 FLT 7693, DURING TAXI TO RUNWAY CREW NOTED SMOKE IN COCKPIT. ELECTRIC SMOKE CAP LIGHT ILLUMINATED AND NR 1 PACK VALVE F AULTED ON CAP. CREW RETURNED AIRCRAFT TO RAMP. REPLACED NR 1 AIR COOLING TURBINE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2007120400307 20071204 00307 EU 2007 12 4 COEA0709911 1 20071025 A 2497 411VC WIRE HARNESS AEROSP ATR42 ATR42300 8680920 EU NR GEN SHORT A COEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 13 911FX 045 FLT 100 - WHILE ENROUTE, NR 1 ACW GENERATOR FAULT AFTER TAKEOFF. RETURNED GEG. REPAIRED (3) CHAFED WIRES ON 411VC HARN ESS NR 2422-2525, 2526, AND 2527. (M) 2 H 7 2 4T RT A53EU 2007120400309 20071204 00309 CE 2007 12 4 AMWA88513BC 1 20071110 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER DISCHARGED A AMWA O OTHER J WARNING INDICATION CL CLIMB 1 CE 07 146ZV 27915 33 UE146 AFTER TAKEOFF, HAD BRIEF BATTERY CHARGE ANNUNCIATOR ILLUMINATION. THEN, AFTER NEXT TAKEOFF ANNUNCIATOR REMAINED ILLUMINA TED AND WAS ACCOMPANIED BY BATTERY AMMETER AND BOTH GENERATOR LOAD METERS CYCLING. AMMETER CYCLED FROM 0 TO 30A AND LOAD METERS CYCLED FROM 20 TO 35 PERCENT UNTIL BATTERY MASTERSWITCH WAS TURNED OFF. PROCEEDED TO NEXT LANDING AND MAINTENAN CE CLEANED BATTERY AMMETER SHUNT, BATTERY TERMINALS, REPLACED BATTERY AND PERFORMED EXTENSIVE OPERATIONAL CHECK BEFORE C LEARING DISCREPANCY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007120400311 20071204 00311 CE 2007 12 4 AMWA1001010A 1 20071109 A 5711 1141200229 SPAR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT WING DAMAGED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 244YV 23091 UE244 AT RT WING WS 54.75 FOUND 0.50 INCH HOLE THROUGH SUB SPAR. HOLE HAD EVIDENCE OF POSSIBLE ELECTRICAL ARCING AT WIRING GRO UNDING ATTACHMENT. REPAIRED IAW APPROVED DATA AND CLEARED DISCREPANCY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007120400313 20071204 00313 EA 2007 12 4 SIMA200733213 1 20071112 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 513AE 10114 LEFT EMERGENCY EXIT OVERWING FLOOR LEVEL SIGN IS OUT. REMOVED AND REPLACED NR 3 BATTERY (EMERGENCY) IN IAW CRJ 700 MM 3 3-51-17. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007120400315 20071204 00315 NM 2007 12 4 BB07094 1 20071126 A 3232 161N40011 ACTUATOR BOEING 757 757225 1384959 NM LT MLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 914AW 72796 30443 22208 FLT 304 PHX - CLT AFTER TAKEOFF FROM PHX, THE FLT CREW GOT A LANDING GEAR DISAGREE INDICATION AND A LANDING GEAR DOOR OP EN INDICATION. CYCLED GEAR AND STILL HAD INDICATION. RETURNED TO PHX. AN EMERGANCY WAS DECLARED, FLIGHT LANDED WITHOU T INCIDENT. MAINTENACE REPLACED LEFT MLG RETRACTION ACTUATOR. 2 L 7 2 4F RT A2NM 2007120400316 20071204 00316 EU 2007 12 4 TRBA2007105 1 20071126 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 538AT 538 CABIN EMERGENCY AFT LIGHTS INOPERATIVE. REMOVED AND REPLACED AFT BATTERY PACK IAW JIC NR 33-51-21. 2 H 7 2 4T RT A53EU 2007120300077 20071203 00077 NM 2007 12 3 QXEA200701747 1 20071116 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 C4 PDX - RIGHT OUTBOARD SEAT TRACK NR 19 HAS CORROSION PITTING IN PREVIOUS BLENED AREA LOCATED ST STATION X358.0. REPAI RED IAW SRM 51-40-15, 51-42-05. 2 H 7 2 4T RT A13NM 2007120300086 20071203 00086 NE 2007 12 3 C8GA20070012 2 20071120 A 7260 HELICOIL BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE NR 3 GEARBOX DAMAGED A C8GA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 29 713AA 22469 708395 FLT 708 FROM TOL TO MCI - DURING CRUISE OPERATION AT FLT LEVEL 320, THE NR 3 ENGINE LOW OIL PSI LIGHT ILLUMINATED. OIL QUANTITY WAS OBSERVED TO BE DECREASING FOLLOWED BY A DECREASE IN OIL PSI. THE NR 3 ENGINE WAS SHUT DOWN AND THE AIRCRAF T DIVERTED TO STL WHERE AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEAL ED THAT A FITTING FOR THE OIL FILTER BYPASS SWITCH WAS LEAKING ON THE GEARBOX. THE GEARBOX HELI COIL WAS REPLACED, OPS AND LEAK CHECK WERE PERFORMED WITH NO DEFECTS. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2007120300097 20071203 00097 2007 12 3 754003 4 20071122 A 3417 HG480C2 CADC BOEING 747 747228F 1384895 NM E&E BAY MALFUNCTIONED A Q2SA J A DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 EA 63 754SA 21576 AUTOPILOT B ALTITUDE HOLD WOULD NOT CAPTURE OR HOLD ALTITUDE. VERTICAL SPEED COMMAND UNUSABLE AND MANUAL PITCH WHEEL CON TROL UNUSABLE. AUTOPILOT A PREVIOUSLY DEFERRED. REMOVED AND REPLACED CADC TO CORRECT AUTOPILOT B. REMOVED AND REPLACE D P10 PANEL TO RESOLVE THE AUTOPILOT A DISCREPANCY. 2 L 7 4 4F RT A20WE 2007120300106 20071203 00106 SO 2007 12 3 FDKA200708380 1 20070812 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 852MJ 13497 145567 FDM 6034 CLT (0337 PHX LCL) - AFT EMERGENCY ESCAPE PATH LIGHTING ROW 17 THRU 18 INOP. MX REPLACED NR 3 AND NR 4 EMERGEN CY BATTERY PACKS. OPS GOOD. 2 L 7 2 4T RT T00011AT 2007120300107 20071203 00107 SO 2007 12 3 FDKA200708381 1 20070812 A 3350 BA50933901 CHARGER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 704 145626 FDM 6053 TPA (0360 PHX LCL) - CABIN EMERGENCY ESCAPE PATH LIGHTING ROW 17 THRU 18 INOP. MX REPLACED NR 4 EMERGENCY BATT ERY PACKS CHARGER. OPS GOOD. 2 L 7 2 4T RT T00011AT 2007120300125 20071203 00125 CE 2007 12 3 135106112107 1 20071121 A 2460 CM358950 MASTER SWITCH CESSNA 402 402C 207590R CE COCKPIT FAILED E HYIA K NONE O OTHER NR NOT REPORTED 1 EA 61 106CA 989 989 402C1020 AVIONICS WOULD NOT COME ON WHEN MASTER SWITCH SWITCHED TO ON POSITION. MAINTENANCE REMOVED AND REPLACED AVIONICS MASTER . 1 L 7 2 3O A7CE 2007120300126 20071203 00126 EU 2007 12 3 1218341112107 1 20070916 A 3350 3011180 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A HYIA K NONE L NO TEST IN INSP/MAINT 1 EA 61 14834 193 ALL EMERGENCY LIGHTING DID NOT WORK IN THE ARM POSITION. REMOVED AND REPLACED EMERGENCY BATTERY PACK. EMERGENCY LIGHTI NG TESTED SATISFACTORY. 2 H 7 2 4T RT A53EU 2007120300129 20071203 00129 EU 2007 12 3 1218344112107 1 20070928 A 5753 S5701407900200 BEAM AEROSP ATR42 ATR42320 8680930 EU T/E FLAP CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 14834 193 CORROSION ON LEFT WING FLAP BEAM AT RIB 8, FOUND TO BE BEYOND LIMITS. LEFT WING FLAP BEAM RIB 8 REPLACED. 2 H 7 2 4T RT A53EU 2007120300133 20071203 00133 EU 2007 12 3 1218348112107 1 20070820 A 5753 S575156650000 FITTING AEROSP ATR42 ATR42320 8680930 EU T/E FLAP CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 14834 193 RIGHT WING OUTBOARD FLAP ARM RIB 14 CORRODED. REPLACED RIGHT WING OUTBOARD FLAP ARM AT RIB 14. 2 H 7 2 4T RT A53EU 2007120300155 20071203 00155 GL 2007 12 3 SIMA200733003 2 20071120 A 7200 CAE3007A1 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL RIGHT MALFUNCTIONED A SIMA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 933JN 14500918 DURING CLIMB-OUT GOT "LAV SMOKE" WARNING, FLIGHT ATTENDANT CALLED SAID LOTS OF SMOKE IN CABIN. REMOVED AND REPLACED RIG HT ENGINE IAW WC NR 71-000-00. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007120400006 20071204 00006 CE 2007 12 4 DXTA200702553 1 20071019 A 2170 COUPLING CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE WATER SEPARATOR DISCONNECTED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 699QS 5605199 LOSS OF NORMAL CABIN PRESSURIZATION OCCURRED IN FLIGHT. FOUND THE FWD COUPLING AT THE WATER SEPARATOR ASSY, TO HAVE COM E DISCONNECTED FROM THE AIR DUCT ASSY PN 6615073-7 FOUND NO DAMAGES TO THE AIR DUCT ASSY AND THE COUPLING ASSY AT THIS P OINT IN TIME 10-19-07. RECONNECTED THE COUPLING AT SLATED LOCATION WITH THE SAME WORN CLAMP ASSY. PERFORMED PRESSURIZATI ON TESTED IAW 560XL MM REV 24 FOUND NO AIR LEAKS AT THIS POINT IN TIME 10-17-07. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007120400014 20071204 00014 NM 2007 12 4 QXEA200701760 1 20071120 A 3040 MS2416601 RELAY BOMBDR DHC8 DHC8402 1390042 NM WINDSHIELD HEAT FAILED A QXEA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 09 402QX 4032 SEA FLIGHT NR 2285: LEFT WINDSHIELD HEAT CIRCUIT BREAKER ON AC BUS POPPED. AIRCRAFT DIVERTED TO GEG. MAINTENANCE REMOV ED AND REPLACED RELAY 3041-K1 IAW AMM 30-41-01, PAGES 407-412. OPS CHECK GOOD IAW AMM 30-41-00-710-801. NO OTHER DEFEC TS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007120400023 20071204 00023 2007 12 4 HALA0700500 4 20071124 A 3414 4039891906 INDICATOR BOEING 767 76733A 1385209 NM AIRSPEED FAILED A HALA K NONE O OTHER AP APPROACH 1 WP 13 582HA 16885 16885 28139 ETOPS SIGNIFICANT SYSTEM, CAPT A/S INDICATOR FAILED ON FINAL APPROACH. REPLACED CAPT A/S IND OPS CHECK OK PER MM 34-13- 01. 2 L 7 2 4F RT A1NM 2007120400051 20071204 00051 NM 2007 12 4 PIDR07015 1 20071018 A 5310 STRUCTURE BOEING 737 737301 1384611 NM BS 178-182 CRACKED B PIDR K NONE O OTHER IN INSP/MAINT 1 SO 05 XAVIV 23560 DURING C-CHECK, NOTED CRACK BETWEEN FASTENERS AT BS 178 RT AT WL 190. REPAIRED DAMAGE FROM BS 178 TO BS 182 AT WL 190 I AW EA NR 53-286. 2 L 7 2 4F RT A16WE 2007120400069 20071204 00069 NM 2007 12 4 AALA20072226 1 20071116 A 2750 FSEU BOEING 737 737823 13844BZ NM T/E FLAP INOPERATIVE A AALA A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 SW 21 969AN 29546 MEX INFLIGHT T2115/16NOV - ON APPROACH FLAPS REMAINED IN UP POSITION. LANDED MEX WITHOUT INCIDENT. TAXIED TO GATE WITH NO FURTHER PROBLEMS. REPLACED FLAP SLAT ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007120400076 20071204 00076 EU 2007 12 4 07FDEA04893 1 20071121 A 5340 A5377364420000 FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FWD PIT FRAME STA 35 LT FRAME TO FLOORBEAM CONNECTION FITTING CORRODED. REMOVED ALL SUBSTRUCTURE AND CARGO SYS COMPONEN TS FROM FR 24 -38.2 L/H TO FACILITATE FITTING REPLACEMENTS IAW A310-200 AMM25-52-44-4,26-4,21-4, AND A310-200 SRM 51 -20--41. REMOVED AND REPLACED FRAME FITTING AT FR 35 L/H IAW A310-200 SRM 51-72- 10.REINSTALLED ALL PREVIOUSLY REMOVED SUBSTRUCTURE AND CARGO SYS COMPONENTSIAW A310-200 AMM 25-52-44-4,26-4,21-4 AND A310 -200 SRM 51-20-41 MAJOR REPAIR. 2 L 7 2 4F RT A35EU 2007120400089 20071204 00089 WP 2007 12 4 07FDEA04902 1 20071123 A 5311 AEA01591 FRAME DOUG DC10 DC1010F 3022111 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 INT CAC CRACK ON FRAME. PERFORMED FRAME REPAIR IAW SRM 53-30-00 VOL I FIG 7. 2 L 7 3 4F A22WE 2007120400095 20071204 00095 SW 2007 12 4 HEEA118058 1 20071031 A 3340 12225310 FILTER BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL STROBE SMOKE B HEEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 03 8593X 51509 SMOKE IN COCKPIT. TURNED OFF LANDING LIGHT AND SMOKE REDUCED. LANDED IN A BACKYARD. REPLACED NOISE FILTER IN PULSE LIG HT SYSTEM. 1 G 7 1 3U 3 U H2SW E1GL 2007120400102 20071204 00102 NM 2007 12 4 07FDEA04911 1 20071124 A 5230 655720493 BRACKET BOEING 727 727225 1384077 NM CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 AFT LOWER CARGO DOOR, LOWER AFT CORNER WEB CORRODED INSTALLED NEW BRACKET PER DWG 65-57204 AND APPLIED LEVELING COMPOUND TO THE LOWER AREA AROUND BRACKET PER BOHM 52-36-22 PG 407. 2 L 7 3 4F A3WE 2007120400116 20071204 00116 NM 2007 12 4 07FDEA04916 1 20071124 A 5311 651766450 FRAME BOEING 727 727225 1384077 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 FWD PIT, PREVIOUS UNREPAIRED DAMAGE FRAME CRACKED AT BS 700 AND BETWEEN STR 18R AND 19R REPAIRED FRAME 700 AT STRINGER 1 8 TO19 RT REF FED EX EA NR 7-5310-113118 AND BOEING DWG 65-15938, 65-82614-9, 65-17664-50. TREATED AND PRIMED PARTS REF SRM 51-10-2. IDENTIFIED PARTS FX 65-82614-9 REF FED EX GMM 7-0-1001 PG 1 SEC 7B. HFEC INSP FOR CRACK REMOVAL REF 727 NDT MAN, PART 6, 51-00-00 FIG 23. NO DEFECTS NOTED. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007120400126 20071204 00126 NM 2007 12 4 AMTA200700581 1 20071104 A 2613 579601 DETECTOR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT OVERHEAT INOPERATIVE A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 519AT 27975 RT ENGINE OVERHEAT LP1 EICAS MESSAGE DISPLAYED. REMOVED AND REPLACED NR 2 ENG LP1 OVERHEAT DETECTOR IAW MM 26-11-01-4, MSG ERASED, OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007120400133 20071204 00133 CE 2007 12 4 CVG2007F00000 1 20071004 A 3040 660393003 DEFOG SYSTEM LEAR 35 31A 5170531 CE GARRTT TFE731 TFE7312B WP COCKPIT WINDOW FAILED E CVGA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 05 431DA 2464 163 (DAE ID NR 07-277) ON DESCENT, AFTER TURNING ON WINDSHIELD DEFOG IAW CHECKLIST, WINDSHIELD BEGAN TO VISIBLY ARC AND ELEC TRICAL ODOR FILLED COCKPIT. AFTER TURNING WINDSHIELD DEFOG OFF, ARCING STOPPED AND ODOR DISSIPATED. LT WINDSHIELD ELEC TRICAL ELEMENT FAILED. REPLACED LT WINDSHIELD. (K) 2 L 7 2 4F 4 F RT A10CE E6WE 2007120400150 20071204 00150 EA 2007 12 4 A6WA200740613 1 20071109 A 3320 BALLAST CNDAIR CL600 CL6002B19 1900309 EA CABIN FAULTY A A6WA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 31 449AW 7818 ELECTRICAL SMOKE ODOR IN AREA OF ROW 3, AT GATE NO PASSENGERS ONBOARD. IDENTIFIED BAD BALLAST FOR 4DF CEILING LIGHT. R EMOVED AND REPLACED CEILING LIGHT 4DF POWER UNIT/DIMMER (111B) IAW CRJ200 AMM 33-21-04. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007120400153 20071204 00153 EA 2007 12 4 A6WA200740618 1 20071108 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 470ZW 7927 FOUND INTERCOSTAL ANGLES AT FS 484 LBL 36 AND LBL 27 ARE CRACKED. REPAIRED IAW REO 601R-53-41-059 REV A. (M) 2 L 7 2 4F RT A21EA 2007120400156 20071204 00156 WP 2007 12 4 U2RA872LP2801 1 20071125 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 872SJ 46040 DURING INSPECTION, FOUND CORROSION AT AFT CARGO COMPARTMENT AREA STATION 1440 LONGERON 36 RT EXTERNAL LOWER SKIN. 2 L 7 4 4F RT 4A25 2007120400162 20071204 00162 WP 2007 12 4 ABXA070377 1 20071111 A 5310 99115057 WINDOW FRAME DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 DURING COCKPIT WINDSHIELD FRAME MOD, FOUND LOWER SILL CENTER FRAME CRACKED AT LEFT AND RIGHT ENDS. REPAIRED FRAME IAW D C9 SRM 53-03, FIGURE 34. 2 L 7 2 4F A6WE 2007120400175 20071204 00175 CE 2007 12 4 DJFA2007124 1 20071104 A 5511 45A21086004 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 484CW 1124 RK334 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER IB RIB AND BRACKET ASSEMBLIES, THE RT SIDE ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF T HIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. THE LT AND RT RIB AND BRACKET ASSEMBLIES WERE REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007120400178 20071204 00178 WP 2007 12 4 ABXA070369 1 20071019 A 5310 99115055 WINDOW FRAME DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 47596 DURING COCKPIT WINDSHIELD FRAME MOD, FOUND FRAME 9911505-5 CRACKED AT INBOARD END. REPAIRED FRAME IAW DC9 SRM 53-03, FI GURE 34. 2 L 7 2 4F A6WE 2007120400187 20071204 00187 EU 2007 12 4 USAA920071217 1 20071112 A 5315 D53112621200 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 625AW 64 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON FLOORBEAM, BS 605/FR 12 - BS 709/FR 16, -Y81. REPLACED FLOORBEAM, BS 605 F R 12 - BS 709 FR 16, -Y81 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007120400188 20071204 00188 EU 2007 12 4 USAA920071218 1 20071112 A 5315 D53472284002 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 625AW 64 SAL - MAJOR REPAIR - C7 CHECK - 6016788, CORROSION ON FLOORBEAM, BS 3101/FR 65 - BS 3207/FR 67, -Y464. REPLACED FLOORBE AM, BS 3101/FR 65 - BS 3207/FR 67, -Y464 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007120400190 20071204 00190 EU 2007 12 4 USAA920071220 1 20071113 A 5315 D53112712200 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 625AW 64 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON FLOORBEAM, BS 657/FR 14, -Y25 TO -Y81. REPLACED FLOORBEAM, BS 657/FR 14, - Y25 TO -Y81 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007120400199 20071204 00199 WP 2007 12 4 07FDEA04927 1 20071126 A 5347 4929150 SEAT TRACK DOUG MD10 MD1010F 3022112 WP FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 FOUND MAIN CABIN AT STA 1441 RBL 48 SEAT TRACK WORN. BLENDED SEAT TRACK, WIDTH OF SCALOP HAS .200 REMAINING MIN IS .2 60 OUT OF LIMITS IAW DC 10 SRM 53-70-00 VOL I PG 21". REMOVED AND REPLACED DAMAGED SECTION OF TRACK IAW DC/MD10 51-31-0 1. ALODINED & PRIMED TRACK AND SPLICE HAT & PLATE IAW DC 10 SRM 51-21-01. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2007120400200 20071204 00200 WP 2007 12 4 07FDEA04928 1 20071126 A 5347 S4929405 SEAT TRACK DOUG MD10 MD1010F 3022112 WP FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 CABIN FLOOR TRACK GOUGED AT STA 1119 RBL 48 2 EACH SCALLOPS. BLENDED AREA .500 MAX LIMIT GAP .510 REMAIN. OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21 & 22. MAT ID TRACK, SPLICE HAT & PLATE. REMOVED DAMAGED TRACK INSTALLED NEW S ECTION IAW DC/MD10-10 SRM 51-31-01 PG 1 VOL II. ALODINED AND PRIMED PARTS IAW DC/MD10-10 SRM 51-21-01 VOL II PG 1-24, R EMOVED AND REISTALLED FLR PANELS IAW MD10-10 AMM 53-21-01-2. FABED PARTS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 3 & 4 2 L 7 3 4F RT A22WE 2007120400206 20071204 00206 EU 2007 12 4 07FDEA04935 1 20071126 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT PIT STR 51R CORRODED AT FRAME 59. REPAIRED STRINGER PER SRM 53-10-14 FIG 201. REMOVED CORROSION PER SRM 51-74-10. CHECKED LIMITS FOUND OUT OF LIMITS. LOCATED AND DRILLED PER SRM 51-40-44. FABBED COUPLING SPLICE PER SRM 53-10-14. AL ODINED, PRIMED AND PAINTED PER SRM 51-21-10 AND 53-23-10. 2 L 7 2 4F RT A35EU 2007120400218 20071204 00218 CE 2007 12 4 DXTA200702591 1 20071103 A 3310 46380191 LAMP CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE CHART LIGHT SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 301QS 2615 6800010 CAPTAINS YOKE MOUNTED CHART LIGHT SMOKES WHEN TURNED OFF. REPLACED CAPTAINS YOKE MOUNTED (CHART) MAP LIGHT ASSY WITH A NEW LIGHT ASSY IAW MM 27-13-00. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RC T00012WI E35NE 2007120400223 20071204 00223 EU 2007 12 4 07FDEA04946 1 20071127 A 5320 A5327828920000 ADAPTER AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 MAIN DECK, ADAPTER TRACK CRACKED, FR 66 (STA X3567) BL 0 TO BL 7L (Y0 TO Y180). REMOVED AND REPLACED ADAPTER IAW A310- 200 SRM 51-40-21 PAR 7, AND SRM 51-40-44 PAR 2. 2 L 7 2 4F RT A35EU 2007120400225 20071204 00225 EU 2007 12 4 07FDEA04947 1 20071127 A 5313 A53970713204 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT CARGO PIT BILGE AREA, STR 52L CORRODED FROM FR 54.2 TO FR 58. ( X3037 TO X3143). REMOVED CORROSION IAW A310 SRM 51- 74-10 ,OUT OF LIMITS IAW A310 SRM 53-10-00, REMOVED FSATENERS TO SUB STRUCTURE COMMON TO THE REPAIR AREA, REMOVED STR INGER SECTION FROM FRAME 54.1 TO FRAME 60, FABBED NEW STRINGER AND ALL REPAIRE PARTS IAW A310 SRM 53-10-14 201/201A, ALO DINED IAW A310 SRM 51-21-10 PRIMED AND PAINTED IAW A310 SRM 51-23-10, INSTALLED STRINGER AND REPAIR PARTS IAW A310 SRM 53-10-14 FIG 201/201A REINSTALLED ALL FASTERNERS AND SUBFRAME PREVIOUSLY REMOVED IAW A310 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007120400240 20071204 00240 EA 2007 12 4 SWIA200718896 1 20071120 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 752SK 10209 FLT 6716 - NR 2 CEILING EMERGENCY FLOOD LIGHT IS INOP. REPLACED NR 2 CEILING FLOOD LIGHT BULB IAW AMM 33-51-09. 2 L 7 2 4F RT A21EA 2007120400241 20071204 00241 EU 2007 12 4 420611092007 1 20071109 A 2612 WARNING LIGHT SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B1 60056 NE FIRE WARING FALSE ACTIVATION E QMLA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 03 544AM 4206 PERFORMED AIRCRAFT STOPPING ENGINE ITEMS AS OUTLINED IN CHECK LIST. WHEN TWIST GRIP WAS PLACED IN THE IDLE POSITION, THE (ENG FIRE) WARNING LIGHT ON THE CWP CAME ON. CREW MEMBER OUTSIDE THE AIRCRAFT WAS ASKED IF SMOKE OR FLAMES WERE PRESENT . HE ADVISED THEY WERE NOT. SHUTDOWN THE ENGINE AND DID A VISUAL INSPECTION OF THE ENGINE AND ENGINE COMPARTMENT. NO EVI DENCE OF A FIRE WAS APPARENT. CONTACTED DISPATCH ADVISED THE AIRCRAFT WAS OUT OF SERVICE. THE MEDICAL CREW HAD NOT LOADE D THE PATIENT ON THE AIRCRAFT. ANOTHER AIRCRAFT WAS DISPATCHED TO PERFORM THE PATIENT TRANSPORT. THE PILOT CONTACTED HIS SUPERVISOR AND THE BASE MECHANIC. THE BASE MECHANIC WAS DISPATCHED THE AIRCRAFT LOCATION. HE INSPECTED THE AIRCRAFT. PR 1 G 7 1 3U 3 U H9EU E00054EN 2007120400242 20071204 00242 SO 2007 12 4 SWIA200718897 1 20071119 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN BROKEN A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 289YV 120289 AFT EMERGENCY FLOOR LIGHT IS BROKEN. REPLACED AFT FLOOR WHITE EMERGENCY LIGHT ASSEMBLY. 2 L 7 2 4T RT A31SO 2007120400252 20071204 00252 SO 2007 12 4 SWIA200718900 1 20071114 A 2460 RCCB EMB 120 EMB120ER 3260203 SO COCKPIT NOISY A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 237SW 120314 FLT 5740 - RCCB BEGAN TO CHATTER IN FLIGHT WITH A BURNING SMELL. INSPECTED AND OPERATED ALL RCCB'S IN LEFT SIDE PANEL. NO DEFECTS NOTED. 2 L 7 2 4T RT A31SO 2007120400253 20071204 00253 CE 2007 12 4 DXTA200702608 1 20071111 A 3246 WHEEL CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE NLG OUT OF BALANCE E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 345QS 5600445 AT APPROX 50 KTS ON TAKE OFF ROLL, NOSE WHEEL SHIMMIES AND STAYS AT A STEADY STATE OF OSCILLATION UNTIL STOPPED. REMOV ED NOSE SHIMMY DAMPER AND INSTALLED OVERHAULED UNIT. REMOVED NOSE WHEEL AND FOUND BALANCE TO BE OUT. REINSTALLED REPAIRE D NOSE WHEEL BALANCED BY DUNCAN AVIATION WORK PERFORMED IAW CESSNA 560 M/M 32-21-02. 2 L 7 2 4F 4 F RT A22CE E25EA 2007120400260 20071204 00260 NM 2007 12 4 DHL2007763001 1 20071110 A 5320 WEB BOEING 727 727264 138408M NM PWA JT8 JT8D17A 52049 NE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 A-6 CHECK, DISCREPANCY: AFT AIR STAIRS RT FWD LWR LIGHTING HOLE TORQUE BOX SKIN AREA IS CRACKED. ROUTED OUT CRACK IAW SR M 51-10-1 FABRICATED REPAIR DOUBLER FROM 7075-T6 .025 X 2 INCH X 4 INCH IAW SRM 51-40-2 AND 53-10-2, PN 9003505 ALODINED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR IAW SRM 51-30-2 SEALED REPAIR IAW SRM 51-20-4. 2 L 7 3 4F 4 F A3WE E2EA 2007120400261 20071204 00261 SW 2007 12 4 U0GA118168 1 20071110 A 2612 70265341902 FIRE WARNING AGUSTA AB139 AB139 0260110 SW PWA PT6 PT6* 52043 EA NR 2 NACELLE FALSE ACTIVATION B U0GA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SW 03 428NE 201 41001 DURING A TRAINING MISSION, THE PILOT REPORTED THAT DURING A MISSED APPROACH THE AUDIO ALERT, NR 2 ENGINE FIRE, SOUNDED T WICE JUST AS IT DOES IN A TEST OF THE SYSTEM. NO WARNING/CAUTION LIGHTS OR CAS MESSAGES WERE OBSERVED. THE PILOT LANDE D AT HUM AS SOON AS POSIBLE. VISUAL INSPECTION FOUND NO SIGNS OF FIRE OR OVERHEATING. 2 G 7 2 4U 3 T R00002RD E2NE 2007120400271 20071204 00271 EU 2007 12 4 714311122007 1 20071112 A 2140 ECU BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101* NE DIRTY E QMLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 03 105VU 7143 PIC AND MED CREW SMELLED SMOKE AND RETURNED TO, AND LANDED AT THE HOSPITAL. A MECHANIC HAS TROUBLESHOT ANY SYSTEM THAT COULD PRODUCE THE ODOR. PERFORMED A MAINTENANCE OPERATIONAL CHECK FLIGHT AND FOUND NO REOCCURRENCE OF THE ODOR. DECIDED THAT THE ECU HAD BEEN USED FOR THE FIRST TIME THIS SEASON AND THE BURNING ODOR POSSIBLY WAS FROM THE DUST THAT HAD ACCU MULATED DURING THE HEATERS NON-USE. 1 G 7 2 3U 3 U H13EU E5NE 2007120400280 20071204 00280 EA 2007 12 4 A6WA200740634 1 20071116 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 427ZW 7685 FOUND CRACK ON AFT DRAG ANGLE OF PASSENGER DOOR AIRSTAIRS. JOB PERFORMED ON AFT DRAG ANGLE OF PASSENGER DOOR AIRSTAIRS IAW REO 601R-57-11-513. (M) 2 L 7 2 4F RT A21EA 2007120400283 20071204 00283 EA 2007 12 4 A6WA200740623 1 20071113 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 470ZW 7927 FOUND PAX DOOR OUTER HANDLE CRACKED. REPLACED IAW AMM 52-11-03-400-802. (M) 2 L 7 2 4F RT A21EA 2007120400292 20071204 00292 SO 2007 12 4 SIMA200733201 1 20071123 A 5320 EPNEM53EP54701 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 667GB 145784 DURING MBV INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND MANUAL LIMITS AT FRAME 20. REMOVED CORRODED AREA AND REPLACED PER. EMB SRM CHAPTER 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007120400299 20071204 00299 EU 2007 12 4 COEA0710911 1 20071024 A 2420 243211 CONTROL UNIT AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NR 1 ENGINE SHORTED A COEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 13 911FX 045 WHILE ENROUTE, NR 1 ACW GENERATOR FAULT WOULD NOT RESET. SMELLED ELECTRICAL SMOKE FOR 30 SECONDS THEN WENT AWAY. REMOV ED AND REPLACED NR 1 ACW GENERATOR AND ACW GENERATOR CONTROL UNIT. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2007120400306 20071204 00306 NE 2007 12 4 COEA0701788 2 20071024 A 7261 ENGINE CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE ENGINE OIL SYS LOW PRESSURE A COEA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 NM 13 788FE 208B0286 PCE17132 ENROUTE- PILOT NOTICED OIL PRESSURE LOSS. PILOT SECURED THE ENGINE AND COMPLETED EMERGENCY CHECK LIST. EMERGENCY CREWS WERE CALLED. AIRCRAFT LANDED IN EUG WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED ENGINE. OPS CHECKED GOOD. AI RCRAFT RETURNED TO SERVICE. (M) 1 H 7 1 3T 3 T A37CE E4EA 2007120400308 20071204 00308 EU 2007 12 4 E3MA071115001 1 20071018 A 6510 BB1B649616B BEARING UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE TAIL ROTOR DRIVE ROUGH E E3MA O OTHER O OTHER NR NOT REPORTED 1 EA 03 639ME 23 23 0563 DURING A DAILY CHECK OF THE AIRCRAFT A GRINDING NOISE WAS DETECTED FROM THE TAIL ROTOR DRIVESHAFT COVER, AFTER AN INVEST IGATION THE GRINDING NOISE WAS FOUND TO BE COMING FROM THE 2 AFT TAIL ROTOR DRIVESHAFT HANGAR BEARINGS. THE BEARING PN: BB1B649616B, SN: N1899 AND N1828. THE BEARINGS WERE STAMPED (ITALY V) ON THE SIDE. THERE IS NO VISIBLE LOT NUMBER. 1 G 7 2 3U 3 U H88EU E34NE 2007120400312 20071204 00312 CE 2007 12 4 AMWA1001016 1 20071108 A 5730 11412002933 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT WING DENTED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 155ZV 22879 UE155 RT CENTER LEADING EDGE AT APPROXIMATELY WS 54.45 HAD BIRD STRIKE DAMAGE EXCEEDING STRUCTURAL REPAIR MANUAL LIMITS. OBTAI NED APPROVED DATA, REPAIRED LEADING EDGE AND CLEARED DISCREPANCY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007120400318 20071204 00318 NM 2007 12 4 UPS07451203 1 20071126 A 3350 S1356B37 BATTERY PACK BOEING 747 747121 1384871 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 683UP 20353 AF L1 DOOR ENTRY EMERGENCY LIGHT WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT/BATTERY PACK ASSY WITH REF TO MM 33-51-07. OPS CHECK GOOD PER SAME. 2 L 7 4 4F RT A20WE 2007120400319 20071204 00319 NM 2007 12 4 UPS07451218 1 20071126 A 7331 ELECTRONIC UNIT BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE FUEL FLOW SMOKE A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 683UP 20353 FUEL FLOW ELECTRONICS UNIT SMOKING. REMOVED AND REPLACED FUEL FLOW ELECTRONICS UNIT PER MM 73-31-02. OPS CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E20EA 2007120400321 20071204 00321 NE 2007 12 4 ASMF200711002 2 20071113 A 7200 JT8D219 ENGINE DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE RIGHT FAILED W ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 838AM 41126 13180 49397 725620 AIRCRAFT REJECTED TAKEOFF AT 130 KNOTS DUE TO RT ENGINE HAS LOSS OF POWER AND BRAKES REACHED 350 DEGREE C. DURING MAINTE NANCE CHECK, T4 STAGE WAS DETECTED WITH LOSS OF MATERIAL, THEREFORE, RT ENGINE WAS REPLACED AND TESTED IAW MPSM 71-00-02 AND 71-00-01. HIGH ENERGY STOP INSPECTION WAS PERFORMED IAW MM 05-57-00, ALL CORRECT. 2 L 7 2 4F 4 F RT E9NE 2007120400324 20071204 00324 CE 2007 12 4 GUUA11130701 1 20071113 A 3260 DOWNLOCK SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG LOOSE A GUUA O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 29 218YV UE218 FLIGHT: 9200, DURING APPROACH LANDING GEAR UNSAFE LIGHTS DID NOT ILLUMINATE (3) GREEN INDICATION DID NOT ILLUMINATE WHEN GEAR HANDLE PLACED IN THE DOWN POSITION. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. REPLACED CIRCUIT BREAKER 16 AN D RESECURED LT MAIN LANDING GEAR DOWNLOCK SWITCH. 2 L 7 2 4T 4 T RT A24CE E26NE 2007120400326 20071204 00326 SW 2007 12 4 AWTR118188 1 20071114 A 6210 407015001117 BLADE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL MAIN ROTOR CRACKED B AWTR K NONE O OTHER IN INSP/MAINT 1 WP 25 110AL 1237 53469 BLADE LEADING EDGE CAP CRACKED. 1 G 7 1 3U 3 U O H2SW E1GL 2007120400330 20071204 00330 CE 2007 12 4 DXTA200702612 1 20071115 A 3260 SQUAT SWITCH CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 388QS 6800113 AFTER TAKEOFF AND UPON RAISING THE GEAR HANDLE, THE GEAR WOULD NOT COME UP. FOUND NOSE GEAR SQUAT SWTICH OUT OF ADJUST, READJUSTED SQUAT SWITCH, OPS CHECK GOOD AT THIS TIME IAW CE-680 MM 32-60-00. 2 L 7 2 4F 4 F RC T00012WI E35NE 2007120400331 20071204 00331 GL 2007 12 4 2007F00067 2 20071106 A 7323 SHAFT HUGHES 369 369E 4470707 WP ALLSN 25OC 250C20R GL GOVERNOR SHEARED E B EMER. DESCENT O OTHER CR CRUISE 1 NM 01 400MB 336 HR47618 CAE295301 ENGINE EXPERIENCED AN N2 OVERSPEED IN FLIGHT. PILOT REGAINED CONTROL WITH THROTTLE AND LANDED AIRCRAFT WITHOUT FURTHER I NCIDENT. REMOVAL OF GOVERNOR FOUND INPUT SHAFT SHEARED WITH AN APPARENT INTERNAL CONTACT OF THE FLYWEIGHT TO THE GOV HO USING. 1 G 7 1 3U 3 U H3WE E4CE 2007120400332 20071204 00332 CE 2007 12 4 GLBA20061028 1 20071116 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 156-164 DENTED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 254GL UE254 DENT ON FUSELAGE ABOVE AIRSTAIR DOOR FROM STA. 156-164 AND BL 10L TO BL18 APPROXIMATLEY .2500 INCH DEEP. MAINTENANCE REP AIRED DAMAGED FRAME AT F.S. 163.975 I.A.W. BEECH 1900D E.O. 07-UE254-02. REPAIR AREA APPROXIMATELY 17" LONG. RII C/W PER GLA TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007120400333 20071204 00333 CE 2007 12 4 GLBA20061029 1 20071116 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 212 CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 254GL UE254 EXFOLIATION REPORTED ON BELLY OF THE AIRCRAFT AT STA. 212 AT BL3.5L TO BL 8.0L APPROXIMATELY 3 INCHES. MAINTENANCE REPL ACED STRINGER 15L BETWEEN F.S. 183.25 TO F.S. 258.25 I.A.W. BEECH 1900D E.O. 07-UE254-01. MATERIAL APPROXIMATELY 5" LONG OF 2014 T6511 EXTRUSION. RII COMPLIED PER TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007120400334 20071204 00334 CE 2007 12 4 ZESA877RF01 1 20071012 A 2731 6660013435 CABLE ASSY CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE ELEVATOR TRIM LOOSE E ZESA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 03 877RF 1517 5243 ELEVATOR TRIM WAS JAMMED AFTER TAKEOFF, RETURNED TO AIRPORT OF DEPARTURE WITH OUT INCIDENT. INSPECTION REVEALED THE ELEV ATOR TRIM CABLE WAS EXCESSIVELY LOOSE. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007120400339 20071204 00339 NM 2007 12 4 UPS07M51204 1 20071027 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48579 INSPECTION TYPE:C CABIN, CORROSION ON SEAT TRACK FLANGE FROM STA 806-840 X=-75. REMOVED PER SRM 51-21-01VIIR35. ORG THK :0.100", MATL REMN: 0.040", EXCEED LMT PER SRM 53-70-00VI FIG 3 R35. CORROSION SEAT TRACK REMOVED PER SRM 51-31-01VIIR3 5. NEW SEAT TRACK REWK USING EXTRUSION P/N:S4929147-7075T 6511 PER SRM 51-70-00VIR35 FIG 1R35. NEW SEAT TRACK INSTALLE D PER SRM 53- 70-00 FIG 1 VIR35. 2 L 7 3 4F RT A22WE 2007120400340 20071204 00340 NM 2007 12 4 UPS07M51205 1 20070917 A 5744 HINGE FITTING DOUG MD11 MD11F 3023600 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C RHW O/B FLAP I/B HINGE (WING SIDE) LWR MOUNT I/B BORE SPOT FACE FOUND CORRODED. RT FWD OB FLP I/B HIN GE LWR MOUNT I/B HOLE SPOTFACE CORROSION REMOVED FOUND EXCEED LMT PER CMM 57-44-08 PG 602-607 R.58. FPI C/O IAW DAC NDT SPM R.13 PART 8 AND FOUND NO CRACK AND CORROSION EVIDENT. REWORKED AREA INSP AND FOUND SATIS PER BSOPM 20-11-02R.58. F LAP PEENING C/O PER BSOPM20-11-02R.58. REWORKED AREA PAINTED PER SRM 51-21-01. 2 L 7 3 4F RT A22WE 2007120400341 20071204 00341 NE 2007 12 4 ANCF200700029 2 20071114 A 7230 BLADES BOEING 757 757236 1384971 NM RROYCE RB211 RB211535E437 54555 NE ENGINE FAN DAMAGED W ANCF A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 23 521NA 25592 30855 N1 ENGINE VIBRATION HIGH, READS 3.0. ENGINE INDICATIONS NORMAL. VIBRATION RETUNED BELOW 2.5 WITH THRUST LEVER RETARDED. ENGINE WAS NOT SHUTDOWN. ON THE LT ENGINE FAN BLADE NR 17 WAS REPLACED CHOCKING PAD IAW AMM 72-31-73 PAGE 401, IAW AMM 71-00-00 PAGE 548, TEST NR 7 FAN TRIM BALANCE WAS ACCOMPLISHED WITH THE 3 TRIAL WEIGHT METHOD AND IAW AMM 71-00-00 PAGE 544 TEST NR 6, VIBRATION SURVEY WAS ACCOMPLISHED SATISFACTORILY. 2 L 7 2 4F 4 F RT A2NM E12EU 2007120400344 20071204 00344 NM 2007 12 4 DXTA200702614 1 20071117 A 5730 SKIN GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE RT WING DAMAGED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 701QS 141 DURING LANDING AND AFTER TOUCHDOWN, THE AIRCRAFT DEPARTED THE LT SIDE OF THE RUNWAY. DAMAGE NOTED ON THE LOWER IB SECTIO N OF THE RT WING, DAMAGE NOTED ON THE RT WING IB LEADING EDGE, AND DAMAGE NOTED ON THE RT KRUEGER FLAP. 2 L 7 2 4F 4 F RT A53NM E35NE 2008041100148 20080411 00148 CE 2008 4 11 DXTA200702616 1 20071117 A 5210 PIN CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE PAX DOOR OUT OF ADJUST E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 834QS 5600669 MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN FROM INSIDE AFTER FLIGHT. FOUND LOWER AFT DOOR PIN OUT OF ADJUSTMENT, ADJUST ED AFT LOWER DOOR PIN IAW CE560 M/M CH 52-10-00. OPS CK GOOD. CHECKED WARM AIR DUCT FOR PROPER INSTALLATION AND DOOR SEA L VALVE. NO DEFECTS NOTED. PRESSURIZED A/C AND DE-PRESSURIZED, DOOR OPS CK GOOD. REF CE560 M/M CH 21-32-00. 2 L 7 2 4F 4 F RT A22CE E00053EN 2007120400345 20071204 00345 NM 2007 12 4 ASAA0752281 1 20071121 A 4990 38809381 FILTER BOEING 737 737890 1384527 NM APU DIRTY A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 570AS 35185 WHILE PERFORMING "A" CHECK WORKCARD FOUND LUBE FILTER HOUSING DELTA P POPPED. REPLACED LUBE FILTER ELEMENT. RAN APU OP S NORMAL, LEAK CHECK GOOD. 2 L 7 2 4F RT A16WE 2007120400346 20071204 00346 CE 2007 12 4 DXTA200702613 1 20071116 A 3260 UPLOCK SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 873QS 258573 RT MAIN GEAR (RED INDICATION) STAYED ILLUMINATED AFTER GEAR RETRACTION. ALL GREEN INDICATORS WERE EXTINGUISHED. GEAR DEP LOYED NORMALLY WITH ALL INDICATIONS IN THE GREEN. REPLACED RIGHT HAND DOOR UP LOCK SWITCH "KN" PER WIRING DIA. 32-60-10 -05, 34-13-01-10 AND ADJUSTED PER XP 32-60-00-501. 2 L 7 2 4F 4 F RT A3EU E6WE 2007120400347 20071204 00347 NE 2007 12 4 ASAA0752282 2 20071124 A 7200 CFM567B27 ENGINE BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE NR 1 OIL CONSUMPTION A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 559AS 35178 ENGINE NR 1 OIL CONSUMPTION = 0.74QPH, OUT OF ETOPS LIMITS. ENGINE NR 1 RE-CALCULATED RATE = 0.06QPH. INSPECTED INLET & EXHAUST, NO DEFECTS NOTED. AIRCRAFT IS NOW ETOPS QUALIFIED. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007120400350 20071204 00350 NM 2007 12 4 SWAA075912 1 20071129 A 3350 1619 LIGHT BOEING 737 7375H4 138449D NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED HC1 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB P ER MM. 2 L 7 2 4F RT A16WE 2007120400351 20071204 00351 NM 2007 12 4 CALA0700700 1 20071120 A 3350 29335130013 BATTERY PACK BOEING 737 737824 13844BZ NM CABIN FAILED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 36207 30579 BOTH RIGHT AND LEFT ADT GALLEY EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY CHECK. REMOVED AND REPLACED BOTH PACKS. 2 L 7 2 4F RT A16WE 2007120400352 20071204 00352 NM 2007 12 4 CALA0700711 1 20071127 A 5320 6546568519520 CHANNEL BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 CORROSION ON FWD SIDE OF APB LWR VERTICAL CHANNEL STIFFENER AND SKIN AT BL 0 STA 1016. FABRICATED AND INSTALLED ALL REP AIR PARTS, REPAIRED STIFFENER PER EA 5310-04045 REV B. 2 L 7 2 4F RT A16WE 2007120400354 20071204 00354 NM 2007 12 4 SWAA075911 1 20071129 A 3350 MS155721 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007120400360 20071204 00360 NM 2007 12 4 NWAA073836304 1 20071116 A 5311 FRAME BOEING 747 747451 1384940 NM FUSELAGE DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 664US 23819 DURING "L" CHECK FRAME WEB AT BS 400 S11R WAS DAMAGED DURING SKIN REPAIR/INSPECTION. REPAIRED PER EA 63-210887. 2 L 7 4 4F RT A20WE 2007120500002 20071205 00002 NM 2007 12 5 1119200701 1 20071119 A 3244 TIRE BOEING 747 747200B 1385021 NM RROYCE RB211 RB211524* NE MLG FAILED A OZYA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 29 361FC 22442 ON TO ROLL, AIRCRAFT AIRFRAME SHUDDERED AT 155KTS. CONTINUED TAKEOFF, REPORTED TO TOWER POSSIBLE BLOWN TIRE. DEBRIS CO NFIRMED ON RUNWAY. ALL SYSTEMS INCLUDING BRAKE TEMPS GOOD, CONTINUED. (25) MINUTES INTO FLIGHT, NR 1 HYDRAULIC SYSTEM FAILURE - RETURNED TO DEPARTURE, JETTISON FUEL, LANDED WITHOUT INCIDENT. 2 L 7 4 4F 4 F RT A20WE E12EU 2007120500004 20071205 00004 2007 12 5 AMTA200700590 4 20071111 A 2210 285T0013126 MODULE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE YAW DAMPER UNSERVICEABLE A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 514AT 27971 RT YAW DAMPER EICAS MSG DISPLAYED. REMOVED AND REPLAYED YDM IAW MM CTL: 22-21-04, OPS CHECK GD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007120500006 20071205 00006 NM 2007 12 5 AMTA200700592 1 20071112 A 3610 1074925 REGULATOR BOEING 737 73783N 13844HI NM BLEED SYS UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 11 310TZ 28243 RT BLEED TRIP OFF LIGHT ILLUMINATED DURING CLIMB OUT. TRIP RESET BUTTOM EXTINGUISHED BLEED TRIP PFF OFF LIGHT. AFTER 1 MIN BLEED TRIP OFF LIGHT REILLUMINATED. REMOVED AND REPLACED RT ENGINE BLEED AIR REGULATOR IAW AMM 36-11-03-04 PERFORM ED RT ENGINE BLEED AIR SYSTEM HEALTH CHECK NO DEFECTS NOTED. (K) 2 L 7 2 4F RT A16WE 2007120500013 20071205 00013 NM 2007 12 5 AMTA200700588 1 20071108 A 3246 31558 WHEEL BOEING 737 73783N 13844HI NM NR 3 UNSERVICEABLE A AMTA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 11 318TZ 28247 AT 130 KTS, HEARD A POPPING NOISE AND AIRCRAFT STARTED PULLING TO THE RT, REJECTED TAKEOFF. FOUND NR 3 MLG TIRE TREAD S EPARATED. REMOVED AND REPLACED NR 3 MLG WHEEL ASSY IAW 32-45-11-4 AMM, NO DEFECTS NOTED. (K) 2 L 7 2 4F RT A16WE 2007120500014 20071205 00014 CE 2007 12 5 DXTA200702618 1 20071119 A 3260 WARNING LIGHT RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG MALFUNCTIONED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 873QS 258573 RT MAIN GEAR RED INDICATION STAYED ILLUMINATED AFTER GEAR RETRACTION. ALL GREEN INDICATION WERE EXTINGUSHED. CHECKED RE SISTANCE AND VOLTAGE ON MAIN GEAR DOWN LOCK AND DOOR UPLOCK SWITCHES. CHECKED GOOD. CHECKED RIGGING ON REVERSING VALVE A ND SEQUENCE VALVE CHECKED GOOD. ADJUSTED DOOR UPLOCK SWITCH FOR MORE ENGAGEMENT. CYCLED GEAR APPROX 20 TIMES WITH NO DEF ECTS IAW MM 32-60-00. 2 L 7 2 4F 4 F RT A3EU E6WE 2007120500015 20071205 00015 EA 2007 12 5 DJFA2007133 1 20071102 A 2430 ADG CNDAIR CL601 CL6012A12 1900303 EA GE CF34 CF341A 30033 NE GENERATOR BURNED E DJFA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 EA 23 664CW 266 3064 DURING POST MAINTENANCE CHECK FLIGHT, CREW TESTED THE AIR DRIVEN GENERATOR SYSTEM (ADG). DURING THE TEST THE ADG FAILED LEAVING THE CREW IN COMPLETE ELECTRICAL BLACKOUT. ENGINE DRIVEN SYSTEM WAS BROUGHT BACK ON-LINE AND AIRCRAFT LANDED SA FELY. MAINTENANCE FOUND ADG FAILED INTERNALLY. THE ADG WAS REPLACED. 2 L 7 2 4F 4 F RT A21AE E15NE 2007120500025 20071205 00025 CE 2007 12 5 ZED2007F00001 1 20071029 A 2612 FIRE WARNING LEAR 35 35A 5170602 CE GARRTT TFE731 TFE7312 01518 WP NACELLE INTERMITTENT E ZEDA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 11 394PA 462 P89267 FALSE ENGINE FIRE LIGHT. THIS IS AN INTERMITTENT DISCREPANCY; WE HAVE ALREADY SENT A SDR EARLIER THIS MONTH. COULD NOT DUPLICATE. CHECKED FIRE LOOPS, WIRING, CHECKED FOR BLEED AIR LEAKS, GROUND RAN, AND SWAPPED ENGINE FIRE DETECT CONTROL . (SUSPECT ENGINE EXHAUST FIRE LOOP) WE THINK IT IS MAKING CONTINUITY PREMATURELY. PULLED BACK THRUST LEVER, LIGHT EXT INGUISHED, LANDED. (K) 2 L 7 2 4F 4 F A10CE E6WE 2007120500048 20071205 00048 CE 2007 12 5 GUUA11180701 1 20071118 A 3260 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MLG OUT OF ADJUST A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 29 190YV UE190 FLIGHT: 9237, DURING FLIGHT LANDING GEAR UNSAFE LIGHT FLASHES INTERMITTENTLY. ADJUSTED LT MAIN LANDING GEAR UPLOCK SWI TCH. 2 L 7 2 4T 3 T RT A24CE E2NE 2007120500062 20071205 00062 SO 2007 12 5 20071101 1 20071126 A 3150 8005575 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE AUTOFEATHER FALSE INDICATION E HSYA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 05 210AS 570 120006 FLT 8110- AFTER APPROXIMATELY 10 SECONDS INTO TAKEOFF ROLL, THE CREW REPORTED AN AUTOFEATHER AURAL WARNING. THE CREW ABO RTED THE TAKEOFF AND RETURNED TO THE RAMP WITHOUT FURTHER INCIDENT. THE CREW INFORMED MX THAT THE AUTOFEATHER SWITCH WAS IN THE ARMED POSITION WITH A GREEN LIGHT INDICATION AND THAT ALL ENGINE PARAMETERS WERE NORMAL. MX REMOVED AND REPLACED THE AURAL WARNING UNIT AND THE FLIGHT CREW PERFORMED A HIGH SPEED TAXI WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2007120500063 20071205 00063 CE 2007 12 5 AMWA88571 1 20071113 A 3242 1143880241 BRAKE GOODYEARAERO BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NR1 WEAK A AMWA K NONE O OTHER TX TAXI/GRND HDL 1 CE 07 163YV 12751 27 JUL962183 UE163 AFTER LANDING THE CAPTAIN REPORTED THAT THE LT BRAKE WAS SPONGY AND MUSHY. REPLACED NR 1 AND NR 2 BRAKE ASSEMBLIES AND CLEARED DISCREPANCY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007120500064 20071205 00064 CE 2007 12 5 AMWA88632 1 20071117 A 3260 1293800161 CONTROL PANEL BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG FAILED A AMWA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 CE 07 242YV 9388 9270 UE242 ALL (3) BUSS TIE ENUNCIATORS ILLUMINATED IN FLIGHT, REQUIRING MANUAL EXTENSION OF LANDING GEAR AND EMERGENCY LANDING. MA INTENANCE REPLACED LT DC POWER PANEL AND CLEARED DISCREPANCY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007120500065 20071205 00065 CE 2007 12 5 AMWA88588 1 20071114 A 3097 GROUND WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE WINDSHIELD LOOSE A AMWA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 CE 07 161YV 9611 UE161 AFTER LANDING AND SHUTDOWN, CREW STATED THEY SMELLED AN ELECTRICAL ODOR IN THE COCKPIT. MAINTENANCE INSPECTED COCKPIT WI RING AND PERFORMED GROUND RUNS AT SEVERAL POWER SETTINGS AND TIGHTENED CAPTAIN'S SIDE WINDSHIELD HEAT GROUNDING SCREW AN D CLEARED DISCREPANCY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007120500067 20071205 00067 CE 2007 12 5 GUUA11240701 1 20071124 A 2620 ANNUNCIATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT FIRE DISCHARG WARNING LIGHT A GUUA O OTHER J WARNING INDICATION CR CRUISE 1 SO 29 218YV UE218 FLIGHT: 9269, DURING FLIGHT, RT FIRE DISCHARGE ANUNCIATOR ILLUMINATED. REPLACED TERMINAL ON RT FIRE EXTINGUISHER. 2 L 7 2 4T 4 T RT A24CE E26NE 2007120500071 20071205 00071 CE 2007 12 5 DXTA200702623 1 20071121 A 5270 SWITCH CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE PAX DOOR OUT OF ADJUST E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 678QS 5605616 CRUISING AT FL 270 AND 270 KIAS, THE CABIN DOOR LIGHT ILLUMINATED. ADJUSTED SWITCH. LIGHT EXTINGUISHES WHILE PRESSURIZE D AND UNPRESSURIZED. IAW CE560 XL MM 52-70-00. & 21-30-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007120500077 20071205 00077 CE 2007 12 5 J00A2007N27VP 1 20071125 A 3250 S3128B0166000G FLEX LINE CESSNA CE750 CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG STEERING FAILED E J00A B J EMER. DESCENT DUMP FUEL K F J FLUID LOSS FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 01 27VP 4404 2 7500027 FLT CREW REPORTED THE FOLLOWING: SOON AFTER TAKEOFF HYDRAULIC QUANTITY A EICAS MESSAGE FOLLOWED SHORTLY BY HYDRAULIC PR ESSURE A EICAS MESSAGE. CREW DECLARED AN EMERGENCY WITH LOSS OF HYDRAULIC A SYSTEM AND LANDED AIRCRAFT MOMENTS AFTER TA KEOFF. THE HYDRAULIC A SYSTEM AFFECTED GEAR EXTENSION, FLIGHT CONTROLS, AND BRAKING AFTER LANDING. THE LANDING GEAR WA S EXTENDED BEFORE HYDRAULIC RESERVOIR A WAS DEPLETED. CREW HAD TO BRAKE AIRCRAFT WITH EMERGENCY PNEUMATIC BRAKES. AIRC RAFT WAS IMMEDIATELY INSPECTED WITH THE FOLLOWING OBSERVATIONS NOTED FROM THE FLIGHT CREW AND A MECHANIC, EMPLOYED WITH MFG FBO; THERE IS HYDRAULIC FLUID STREAKING FROM THE NOSE LANDING GEAR TO THE EMPENNAGE. FURTHER INVESTIGATION FROM MEC 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007120500079 20071205 00079 CE 2007 12 5 DJFA2007126 1 20071108 A 5511 45A21146005 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 744TA 5976 RK245 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER INBOARD RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS ARE A ARE OUTLINED IN COMMUNIQUE' NR 70. MAINTENANCE REPLACED BOTH RIBS WITH IMPROVED PART (RIGHT RIB WAS REPLACED TO PREV ENT FUTURE CRACKS). 2 H 7 2 4F 4 F RT A16SW E25EA 2007120500080 20071205 00080 SO 2007 12 5 DJFA2007128 1 20071108 A 5300 UNKNOWN EMB 135 EMB135BJ 3260306 SO ALLSN AE3007 AE3007C GL FUSELAGE VIBRATION E DJFA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 23 906LX 14500825 AIR TURN BACK TO DEPARTURE DUE TO A LOUD VIBRATION FELT ON CLIMB OUT. THE AIRCRAFT LANDED OVERWEIGHT. ALTHOUGH NO EMER GENCY WAS DECLARED THE AIRCRAFT WAS MET BY AIRPORT EMERGENCY CREW. MAINTENANCE COULD NOT IDENTIFY THE SOURCE OF THE VIB RATION BUT ADJUSTED R/H ELECTRONIC BAY VENT VALVE AND TIGHTENED CLAMP ON R/H RAM AIR VALVE DUCT FOR PRECAUTIONARY PURPO SES. 2 L 7 2 4F 4 F RT TE6CH 2007120500081 20071205 00081 CE 2007 12 5 DJFA2007129 1 20071110 A 5511 45A21146005 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 441LX 954 RK292 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER INBOARD RIB AND BRACKET ASSEMBLIES, THE LT AND RT IB RIBS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF T HIS AREA ARE OUTLINED IN COMMUNIQUÉ' NR 70. MAINTENANCE REPLACED THE RIB ASSEMBLIES WITH IMPROVED PART. 2 H 7 2 4F 4 F RT A16SW E25EA 2007120500082 20071205 00082 NM 2007 12 5 2007UALA04685 1 20071114 A 3260 SENSOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE MLG MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C CL CLIMB 1 WP 29 826UA 989 GEAR HANDLE WOULD NOT GO UP AFTER TAKEOFF UNTIL ABOVE ABOUT 150 FEET. FOUND SENSOR 22GA OUT OF ADJUSTMENT/TOLERANCE. AD JUSTED SENSOR 22GA AND ADJUSTED UPPER TORQUE LINKS. FAC1 AND FAC2 WERE ALSO REPLACED AS PRECAUTIONARY. NO REPEATS,, 2 L 7 2 4F 4 F RT A28NM E40NE 2007120500083 20071205 00083 NM 2007 12 5 2007UALA04686 1 20071113 A 3240 BRAKE ASSY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE MLG DRAGGING A UALA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 WP 29 850UA 1653 HARD RIGHT RUDDER NEEDED TO MAINTAIN STRAIGHT TAKEOFF AND LANDING. REPLACED BOTH NOSE TIRES, PERFORMED A FNC OF STEERI NG SYSTEM- NO FAULTS FOUND, JACKED EACH MAIN TIRE AND SPUN TO CHECK FOR WHEEL BEARINGS DRAGGING/BRAKES DRAGGING--NONE FO UND. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007120500084 20071205 00084 NM 2007 12 5 2007UALA04690 1 20071114 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 805UA 783 EXIT LIGHT AT FLOOR LEVEL OF DOOR 1R BROKEN OFF OF MOUNT. REPLACED EXIT LIGHT ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007120500085 20071205 00085 NE 2007 12 5 AALA20072176 2 20071109 A 7320 8061865 CONTROL UNIT BOEING 767 767323 1385205 NM GE CF6 CF680C2B6 30025 NE RT ENGINE INOPERATIVE A AALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SW 21 368AA 25195 690267 GRU INFLIGHT T942/09NOV - RIGHT ENGINE FUEL SHUTOFF VALVE CIRCUIT BREAKER POPPED AFTER LEVEL OFF. RETURNED TO GRU AND L ANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE MAIN FUEL CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A1NM E13NE 2007120500086 20071205 00086 EU 2007 12 5 07FDEA04821 1 20071116 A 5751 SKIN AIRBUS 300 A300B4622 3930401 EU AILERONS MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 718FD 365 PREVIOUS EXTERNAL REPAIR DOUBLER ON LEFT WING AILERON LOWER TRAILING EDGE SKIN BETWEEN RIBS 1 TO 6 MEASURES 21 INCH BY 14.5 INCH AT THE AFT INBD EDGE. REMOVED AND REPLACED 3 BLIND FASTENERS TO CORRECT REPAIR PER A300-600 SRM 51-40-21 AND REFERENCE FEDEX EA 6-5761-70314 AND AIRBUS RAS/FOK/0651 2003 ISSUE A. 2 L 7 2 4F RT A35EU 2007120500087 20071205 00087 EU 2007 12 5 07FDEA04822 1 20071116 A 5753 SKIN AIRBUS 300 A300B4622 3930401 EU TE FLAP MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 718FD 365 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING INBOARD TRAILING EDGE LOWER SURFACE BETWEEN RIBS 11 AND 15 MEASURE S 5.2 INCH BY 13.1 INCH. REMOVED AND REPLACED 5 EACH BLIND FASTENERS TO CORRECT REPAIR PER A300-600 SRM 51-40-21 AND FE DEX EA 6-5750-70315. REPAIR IS CLASSIFIED AS A MAJOR REPAIR PER FEDEX GMM 6-2-100. 2 L 7 2 4F RT A35EU 2007120500088 20071205 00088 EU 2007 12 5 07FDEA04823 1 20071116 A 5753 SKIN AIRBUS 300 A300B4622 3930401 EU TE FLAP MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING INBOARD FLAP TRAILING EDGE LOWER SURFACE AT RIBS 9 AND 10 MEASURES 13.3 INCH BY 24 INCH. REMOVED AND REPLACED 3 EACH BLIND FASTENERS TO CORRECT THE REPAIR PER A300-600 SRM 51-40-21 AND REF FEDEX EA 6-5750-70315. THIS REPAIR IS CLASSIFIED AS A MAJOR PER FEDEX GMM 6-2-100. 2 L 7 2 4F RT A35EU 2007120500089 20071205 00089 EU 2007 12 5 07FDEA04841 1 20071118 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 671FE 778 MAIN CABIN LT SEAT TRACK NR 2 HAS THREE AREAS OF CORROSION INSIDE SCALOPE HOLES ON FOLLOWING; FR 42 = 2 IN LONG, FR 43 A FT 3 SQ IN, FR44- 45 2.5 SQ IN. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-72-10, DUE BEYOND LIMITS. 2 L 7 2 4F RT A35EU 2007120500090 20071205 00090 EU 2007 12 5 07FDEA04842 1 20071118 A 5347 A53832020400 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 671FE 778 MAIN CABIN LT NR 5 SEAT TRACK HAS 3 AREAS OF CORROSION INSIDE/TOP SCALOPE HOLES WITH APPROXIMATE MEASUREMENTS AS FOLLOWS ; BETWEEN FR 44 -45 = 4 SQ IN, AFT OF FR 42 =4 SQ IN FR 41 = 3.5 SQ IN. REMOVED SEAT TRACK L5 FR 40 TO FR 45, AND REINS TALLED NEW PART PER A300-600 SRM 51-72-10, AS FOUND BEYOND LIMIT. 2 L 7 2 4F RT A35EU 2007120500091 20071205 00091 EU 2007 12 5 07FDEA04864 1 20071119 A 5347 A5383202020400 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 671FE 778 MAIN CABIN LT NR 3 SEAT TRACK HAS 3 EACH AREAS OF CORROSION INSIDE/TOP OF SCALOPE HOLES WITH APPROX MEASUREMENTS FR 43= 3-SQ IN, BETWEEN FR 44-45 =3 SQ IN ,FR 45- 46= 1 SQ IN. REMOVED AND REPLACED SEAT TRACK PER A300-600 SRM 51-40-21 AS F OUND BEYOND LIMIT PER A300-600 SRM 53-10-16. 2 L 7 2 4F RT A35EU 2007120500092 20071205 00092 CE 2007 12 5 DJFA2007134 1 20071116 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 794TA RK282 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER IB RIB AND BRACKET ASSEMBLIES, THE RT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. MAINTENANCE REPLACED BOTH RIBS WITH IMPROVED PART (LEFT RIB WAS REPLACED TO PREVENT FUTU RE CRACKS). 2 H 7 2 4F 4 F RT A16SW E25EA 2007120500096 20071205 00096 EA 2007 12 5 TRAX200701737 1 20071116 A 7830 TRACK CNDAIR CL600 CL6002C10 1390015 EA THRUST REVERSER BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 761ND 10213 LEFT ENG UPPER INBOARD T/R SLIDER TRACK BROKEN. INSTALLED NEW LT ENG UPPER INBD T/R SLIDER TRACK IAW REO 670-78-34-029 3. 2 L 7 2 4F RT A21EA 2007120500097 20071205 00097 NM 2007 12 5 2007UALA04716 1 20071116 A 2820 UNKNOWN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUEL XFER VALVE UNKNOWN A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 835UA 1426 LEFT OUTER FUEL TRANSFER VALVE AMBER HALF CLOSED. NO STATUS MSG. VALVE WAS FOUND TO BE OPERATING NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007120500098 20071205 00098 NM 2007 12 5 2007UALA04717 1 20071115 A 3510 OXYGEN MASK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 834UA 1420 CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. CREW COMMENTS: CURRENT PRI 830. O2 AT 1600 PSI AT START O F FLIGHT. FOUND MASK LEAKING. REPLACED THE F OBS MASK AND SERVICED THE CREW O2 SYSTEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007120500099 20071205 00099 NM 2007 12 5 2007UALA04722 1 20071116 A 3260 SENSOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE MLG OUT OF ALIGNMENT A UALA O OTHER N FALSE WARNING CL CLIMB 1 WP 29 813UA 858 ON GEAR RETRACTION, LANDING GEAR NOT UPLOCKED, DISPLAYED WITH ASSOCIATED ANTI-ICE STDY PITOT HEAT MESSAGE. CREW CYCLED GEAR AND ALL FAULTS CLEARED. FOUND SENSORS 24GA AND 25GA NOT ALIGNED. RE-ALIGNED SENSORS 24GA AND 25GA. PERFORMED GE AR SWING WITH SATISFACTORY RESULTS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007120500100 20071205 00100 2007 12 5 2007UALA04732 4 20071116 A 2565 SLIDE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE DOOR 2R FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 846UA 1600 R2 DOOR ARM HANDLE FAILS PUSH-PULL TEST. REMOVED SLIDE PACK AND PERFORMED OPS CHECK AND TENSION CHECK OF ARM HANDLE- A LL CHECKED GOOD. REINSTALLED SLIDE AND PUT BACK INTO SERVICE--NO REPEATS SINCE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007120500101 20071205 00101 WP 2007 12 5 UPS07851194 1 20071121 A 2497 BUSS DOUG DC8 DC871F 302199D WP NR 1 FAILED A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 755UP 46055 LOST NUMBER ONE ELECTRICAL BUS. CREW REQUESTED SPECIAL PRIORITY TO REMAIN IN RVSM AIRSPACE AND A LONG DESCENT INTO IAH. CREW DID NOT DECLARE EMERGENCY, BUT TOWER REQUESTED CFR TO STANDBY. R&R NR 1 GEN. PER MM 24-20-01-4, R&R NR 1 VOLT RE G & GEN CONT PANEL PER MM 24-20-06-2. R&R GEN FEEDER WIRE T3-T6 & TRANSFORMER. RAN ALL ENGINES. A/C SYSTEM OPS CHECK GOO D. 2 L 7 4 4F RT 4A25 2007120500102 20071205 00102 EU 2007 12 5 07FDEA04889 1 20071121 A 7720 60253301 THERMOCOUPLE AIRBUS 310 A310203 3930313 EU GE CF6 CF680 30025 NE NR 2 EGT MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 429FE 1306 1306 364 585167 DURING CLIMB, NR 2 EGT (POINTER/DIGITAL) WERE FLUCTUATING +/- 50C. ALL OTHER ENGINE PARMS NML. NO YAW NOTED. PULL NR 2 THROTTLE BACK TO ABOUT 10 PERCENT, NO CHANGE. HIGHEST EGT WAS APPROX 860C. AFTER ABOUT 10 MINS EGT STAB AT ABOUT 800 C AND NML REST OF FLIGHT. FLUX STARTED AGAIN AFTER LNDG. ON GND FLUX WAS ABOUT +/ - 10C. AGAIN, REMOVED AND REPLACED NR 2 ENG EGT IND PRECAUT REF AMM 77-21-21-4. RAN ENG PER JRH AT VARIOUS LOW POWER SETTINGS FOR APPROX 15 MINS. NO FLU CTUATION NOTED. FOUND WIRE HARNESS J3 FWD OF J BOX THAT UPPER AND LOWER T/C HARNESSES CONNECT HAS VISUAL DMG AND WHEN S HOOK GAVE FLUX TO EGT IND. REMOVED AND REPLACED FWD THERMOCOUPLE CABLE IAW MM 77-21-02-4-04. 2 L 7 2 4F 4 F RT A35EU E13NE 2007120300156 20071203 00156 EA 2007 12 3 SIMA200733005 1 20071125 A 3250 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA STEERING SYS MALFUNCTIONED A SIMA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 21 523AE 10152 EMERGENCY DECLARED ON ARRIVAL, STEERING INOP CAUTION DURING GEAR RETRACTION. PERFORMED BITE CHECK OF NWS IAW AMM II CH 32-50-00. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007120300158 20071203 00158 GL 2007 12 3 SIMA200733011 2 20071122 A 7200 AE3007A13 ENGINE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL NR 1 MALFUNCTIONED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 21 808AE 145519 CAE312812 IN ICE CONDITION GOT STRONG BURNING RUBBER SMELL IN COCKPIT AND CABIN. REMOVED AND REPLACED NR 1 ENGINE IAW WC NR 71-00 0-00. NO BURNING SMELL NOTED DURING OPS CHECK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007120400003 20071204 00003 SO 2007 12 4 CHQA200700079 1 20071120 A 2612 14534156401 CONTROL PANEL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL COCKPIT FAULTY A CHQA O OTHER N FALSE WARNING AP APPROACH 1 GL 11 279SK 16923 145379 CAE311424 GSP TO LGA - UPON REACHING 10,000 FT DURING DESCENT, THE APU WAS STARTED DUE TO AN MEL'D NR 3 GENERATOR. SHORTLY AFTER STARTING APU, CREW RECEIVED A FIRE WARNING EICAS MESSAGE. AFTER TAKING THE APPROPRIATE ACTION THE APU FIRE INDICATION W ENT AWAY. THE AIRCRAFT LANDED WITHOUT INCIDENT, AND WAS INSPECTED BY FIRE CREWS AND MAINTENANCE AND NO TRACES OF FIRE D AMAGE WERE FOUND. MAINTENANCE TROUBLESHOT THE FAULT TO THE APU FIRE CONTROL OVERHEAD PANEL. THE PANEL WAS REPLACED AND THE APU FIRE CONTROL SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007120400009 20071204 00009 EA 2007 12 4 S9BA200700024 1 20071112 A 2497 WIRE DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA ZONE 200 SHORTED A S9BA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 29 562CP 562 LT GENERATOR WOULD NOT COME ON-LINE AFTER START. FERRIED AC BACK TO BASE SSB. FOUND SHORTED WIRE ON GEN. FIELD RELAY D UE TO LACK OF HEAT SHRINK TUBING ON SOLDERED TERMINAL JOINT. 1 H 7 2 3T 4 T RT A9EA E4EA 2007120400012 20071204 00012 EA 2007 12 4 CHQA200700081 1 20071121 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LAVATORY ODOR A CHQA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 11 647BR 7399 GEE872717 DFW TO IAH - AFTER TAKEOFF, WHILE CLIMBING THROUGH 6,000FT, CREW RECEIVED "SMOKE TOILET" MESSAGE. THE FLIGHT ATTENDANT CHECKED THE LAV AND SMELLED SMOKE AND HEARD THE ALARM GOING OFF. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCI DENT. EMERGENCY CREWS INSPECTED THE AIRCRAFT AND FOUND NO SIGNS OF FIRE. MAINTENANCE INSPECTED AIRCRAFT AND RESET THE FIRE DETECTION SYSTEM AND FOUND NO FURTHER FAULTS. 2 L 7 2 4F 4 F RT A21EA E15NE 2007120400015 20071204 00015 EU 2007 12 4 UPS07151195 1 20071121 A 2750 MECHANISM AIRBUS A300 A300F4622R 3930360 EU COCKPIT OBSTRUCTED A IPXA K NONE F FLT CONT AFFECTED AP APPROACH 1 SO 01 125UP 0809 DURING FINAL APPROACH, CREW DECLARED AND EMERGENCY DUE TO THE SLATS/FLAPS WERE STUCK IN THE 15/0 POSITION. CREW EXECUTE D A NO FLAP LANDING AND WAS ABLE TO LAND WITHOUT FURTHER INCIDENT. REMOVED DEBRIS FROM SLAT/FLAP CONTROL HANDLE LEVER M ECHANISM. ACCOMPLISHED SLAT/FLAP BITE TEST PER AMM 27-51-00-05. OPERATIONAL TEST NORMAL. 2 L 7 2 4F RT A35EU 2007120400025 20071204 00025 2007 12 4 DXTA200702554 4 20071019 A 2210 4006719906 CONTROL SERVO CESSNA 750 750 2076810 CE ALLSN 250C 250C30S 03013 GL ELEVATORS INOPERATIVE E DXTA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 07 989QS 7154 7500089 (B) HYDRAULIC VOLUME LOW AND ILLUMINATED IN FLIGHT. REMOVED AND REPLACED THE ELEVATOR SERVO. OPS CHECKS GOOD IAW MM 22- 10-01. 2 L 7 2 4J 3 U RT T00007WI E1GL 2007120400031 20071204 00031 NM 2007 12 4 USAA920071207 1 20071016 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 CLT - MAJOR REPAIR - C16 CHECK, CRACKED FRAME, BS 727D, S8L - S9L. REPAIRED FRAME, BS 727D, S8L - S9L IAW USAIRWAYS TYP ICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2007120400045 20071204 00045 EU 2007 12 4 AALA20072238 1 20071117 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80057 465 JFK - EMERGENCY EXIT SIGN LIGHT AT OVERHEAD LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVER HEAD LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007120400058 20071204 00058 EU 2007 12 4 AALA20072239 1 20071117 A 3350 2510771 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80057 465 JFK - EMERGENCY EXIT SIGN LIGHT AT OVERHEAD LEFT NUMBER TWO DOOR LENS INOPERATIVE. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007120400062 20071204 00062 NM 2007 12 4 AALA20072236 1 20071104 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 976AN 30099 TUL - EMERGENCY LIGHT AT RIGHT FORWARD OVERHEAD ENTRY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIGHT F ORWARD OVERHEAD ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007120400073 20071204 00073 NM 2007 12 4 07FDEA04890 1 20071121 A 3210 TRIM CYLINDER DOUG MD11 MD11F 3023600 NM LEFT CONTAMINATED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 609FE 48549 AFTER TAKEOFF LANDING GEAR HANDLE WOULD NOT MOVE TO UP POSITION. FOLLOWED QRH GEAR HANDLE REMAINED IN DOWN POSITION. PROBLEM DUPLICATED BY VISUAL CHECK MLG TRIM INTERLOCK CYLINDER, FOUND IT FAILED TO EXTEND AND CAUSED L/G CONTROL LEVEL UNABLE LIFT TO FULLY UP POSITION, WITH HYD SYS PRESSURIZED. PER MM 32-37-01-4, RESET UPSTREAM HYD FUSE NO HELP, BLEED RT TRIM CYLINDER HYD FLUID STILL NO HELP. BLEED LT TRIM CYLINDER, INTERLOCK CYLINDER FUNCTION BACK NORMAL, LANDING GEA R CONTROL LEVEL LIFT UP NORMAL. FOR PRECAUTION, ALSO REMOVED AND REPLACED TRIM CYLINDER FUSE ASSY AS PER MM 32-37-06-4, LEAK CHECK PASSED AND L/G CONTROL LEVEL FUNCTION TEST OK. A/C OK FOR CONTINUE SERVICE. 2 L 7 3 4F RT A22WE 2007120400084 20071204 00084 EA 2007 12 4 N6WA0071101 1 20071102 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE EMERGENCY LIGHT BURNED OUT A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 165GJ 10257 OVERHEAD EMERGENCY LIGHT IN CABIN INOP. REPLACED BULB 2 L 7 2 4F 4 F RT A21EA E00063EN 2007120400090 20071204 00090 WP 2007 12 4 07FDEA04903 1 20071123 A 5310 ACA72261 BEAM DOUG MD10 MD1010F 3022112 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 MAIN CARGO DOOR JAMB TOP SURFACE UNDER CENTERING GUIDE HAS SURFACE CORROSION, STA 660. REMOVED AND REPLACED BEAMS ACA7 225-1 AND ACA7226-1 IN REF TO DAC DRAWING ACA7224 REV G AND DC/MD10-10 SRM 51-31-01 VOL II PG 1, MD/DC10-10 SRM 51-33-01 VOL II PG 1 AND DC/MD10-10 SRM 51-35-01 VOL II PG1 2 L 7 3 4F RT A22WE 2007120400092 20071204 00092 WP 2007 12 4 07FDEA04904 1 20071123 A 5310 AFA71321 DOOR FRAME DOUG MD10 MD1010F 3022112 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 MAIN CARGO DOOR LOWER JAMB AT NR 1 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A, B,C,D TO REMOVE COROSION AND INSTALLED REPAIR BUSHINGS. FOUND REPAIR BUSHINGS WOULD NOT MEET THE LIMITS STATED IN MD/DC 10-10 SRM 53-50-00 FIG 17 VOL I. REPLACED FITTINGAFA7132-1 IN REF TO MD/DC10-10 SRM 51-33-01 VOL II PG 1 AND DAC DWG AC A7224 REV G. 2 L 7 3 4F RT A22WE 2007120400099 20071204 00099 WP 2007 12 4 07FDEA04909 1 20071123 A 5310 AFA71321 DOOR FRAME DOUG MD10 MD1010F 3022112 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 MAIN CARGO DOOR LOWER JAMB AT NR 7 SPOOL LOCATION, ALL FOUR HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,D TO .517 AND HOLE D TO .484 TO REMOVE CORROSION IN REF TO MD/DC10-10 SRM 53-50-01 FIG 17 VOL I. ACCOMPLISHED BHEC IN REF TO NTSPM 06-10-01-003 AND FOUND HOLES A,B,D WITH CRACK INDICATION. REPLACED NR 7 FITTING IN REF TO MD/DC10-10 SRM 51-33-01 VOL II PG 1 AND DAC DWG ACA7224 REV G. 2 L 7 3 4F RT A22WE 2007120400100 20071204 00100 NM 2007 12 4 07FDEA04910 1 20071124 A 5311 651766450 FRAME BOEING 727 727225 1384077 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 FWD PIT, PREVIOUS UNREPAIRED DAMAGE FRAME CRACKED AT BS 720, STR 19R REPAIRED FRAME 720 BTW STR 18R AND 19R REF FED EX EA 7-5310-113119, SRM 51-40-3 FIG 1 SRM 51-30-2 PG 2 51-30-5 PG 1 BOEING DWG 65-82614-12, 65-17664-50. TREATED AND PRIM ED REF SRM 51-10-2 PG 7 PG 6. IDENTIFIED PART AS FX 65-82614-12 REF GMM 7-0-1001 PG 1. HFEC FOR DAMAGE REMOVAL, IAW 72 7 NDT MAN PART 6 51-00-00 FIG 23 TOOL NR IDM -0031 CAL DATE DUE 11-30-07. NO DEFECTS NOTED, THIS IS CLASSIFIED AS A MAJ OR REPAIR. 2 L 7 3 4F A3WE 2007120400113 20071204 00113 NM 2007 12 4 07FDEA04913 1 20071124 A 5311 651633926 ANGLE BOEING 727 727225 1384077 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 AFT CARGO BS 970 LOWER FRAME ANGLE CRACKED BETWEEN STR 26L-27L REMOVED LOWER FRAME ANGLE. FABRICATED REPAIR ANGLE AND R EINSTALLED LOWER FRAME REPAIR AND INSTALLED LOWER REPAIR ANGLE. REF SRM 51-40-3/ FIG NR 1/ PAGES 1-6 AND SRM 51-30-02 . REPAIR IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007120400129 20071204 00129 NM 2007 12 4 07FDEA04922 1 20071125 A 7931 21SN04334 PRESSURE SWITCH DOUG MD11 MD11F 3023600 NM GE CF6 CF680 30025 NE OIL SYSTEM MALFUNCTIONED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 603FE 48459 702867 DURING CRUISE FLIGHT, GOT A LEVEL 2 ALERT "ENG 2 OIL FILTER". THIS ALERT DID NOT GO AWAY, EVEN WITH THROTTLE IDLE. ENG INE SHUT DOWN IAW QRH NO OTHER ABNORMAL INDICATIONS. REPLACED OIL FILTER DIFFERENTIAL PRESSURE SWITCH PER MM 79-35-01-4 . REFLUSH NR 2 ENG OIL SYS PER MM 12-12-01-3 AND INSPECTION MASTER CHIP DETECTOR PER MM 79-36-01-6. REPLACED NR 2 ENG OIL SCAVENGE FILTER PER MM 79-22-04-4. ALL NO DSIC FOUND PER MM 79-22-04-6. RAN NR 2 ENG PER MD-11 JRH ALL PARAMETER NORMALLY. 2 L 7 3 4F 4 F RT A22WE E13NE 2007120400132 20071204 00132 EA 2007 12 4 A6WA200740600 1 20071107 A 5320 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 426AW 7669 CHANNEL SUPPORT CRACK, FRAME FS 574 STRINGER LT. CHANNEL ON FRAME 574 STRINGER 16L. REPLACED IAW CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007120400135 20071204 00135 EA 2007 12 4 A6WA200740602 1 20071108 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 426AW 7669 FOUND CRACK EXIST ON BRACKET ON INTERCOSTAL FS 484 RBL 27. REPLACED IAW REO 601R-53-41-059 REV A. (M) 2 L 7 2 4F RT A21EA 2007120400145 20071204 00145 EA 2007 12 4 A6WA200740607 1 20071108 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 426AW 7669 HYDRAULIC SUPPORT BRACKET OF MLG BAY FS 529.50 RT FS 523, RBL 31 IS CRACKED. HYD SUPPORT BRACKET OF MLG BAY FS 529.50 AN D FS 523 RBL 31. REPLACED IAW CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007120400151 20071204 00151 EA 2007 12 4 A6WA200740616 1 20071107 A 5320 PLATE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 426AW 7669 FOUND SERVICE DOOR LOWER SILL PROTECTOR PLATE IS CORRODED. FOUND OUT OF LIMITS IAW SRM 53-21-27. SERVICE DOOR LOWER SI LL PROTECTIVE PLATE REPLACED IAW CRJ 200 SRM 51-41-04. (M) 2 L 7 2 4F RT A21EA 2007120400152 20071204 00152 EA 2007 12 4 A6WA200740617 1 20071108 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 470ZW 7927 FOUND INTERCOSTAL ANGLES AT FS 484 RBL 36 AND RBL 27 ARE CRACKED. REPAIRED IAW REO 601R-53-059 REV A. (M) 2 L 7 2 4F RT A21EA 2007120400159 20071204 00159 WP 2007 12 4 ABXA070374 1 20071111 A 5310 99115055 WINDOW FRAME DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 DURING COCKPIT WINDSHIELD FRAME MOD, FOUND COCKPIT WINDOW LOWER SILL LEFT SIDE FRAME CRACKED AT UPPER INBOARD END. FRAM E REPAIRED IAW DC9 SRM 53-03, FIGURE 34. 2 L 7 2 4F A6WE 2007120400169 20071204 00169 CE 2007 12 4 AMWA88437BC 1 20071106 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER FAILED A AMWA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 127ZV 2364 140 UE127 DURING FLIGHT THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED THEN WENT OUT. MAINTENANCE REPLACED BATTERY AND CLEARED DISCREP ANCY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007120400171 20071204 00171 NM 2007 12 4 C77A200700003 1 20071107 A 2700 70265421901 MODULE EMB ERJ170 ERJ170100LR 3260401 NM POWER LOSS A C77A O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 606CZ 4413 4413 17000188 DURING FLIGHT PILOT SENT ACARS MESSAGE WAS AS FOLLOWS: DSP/MX ADS 1 FAIL MSG. RAN QRH. ALSO SPLR FLT MSG. ARE LANDING DS T AFFECT. ONCE A/C LANDED IN GRB A/C WAS TOWED TO GATE. MECHANIC PERFORMED A POWER RESET, IAW AMM FIM 31-42-00-811-808A WHICH CLEARED (AVNX MAU 1A FAIL) MESSAGE. FROM THAT POINT, HAD THE MECHANIC PERFORM A FLIGHT CONTROL RETURN TO SERVICE T EST, IAW AMM 27-00-00, WHICH CLEARED (SPLR FAULT) MESSAGE, (FLT CTRL NO DISPATCH) MESSAGE, AND (ADS 1 FAIL) MESSAGE. FUR THER TROUBLESHOOTING SHALL BE PERFORMED PENDING THE RESULTS OF FAULT HISTORY DATABASE DOWNLOAD. 2 L 7 2 4F RT A56NM 2007120400182 20071204 00182 NM 2007 12 4 USAA920071203 1 20071124 A 5755 654645170A SPOILER BOEING 737 7373G7 1384595 NM LT WING DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 PHX - MAJOR REPAIR - LEFT WING NR 2 SPOILER HAS LARGE AREA OF DISBOND. REPLACED LEFT WING NR 2 SPOILER IAW B737 AMM 27 -61-11-4. 2 L 7 2 4F RT A16WE 2007120400191 20071204 00191 EU 2007 12 4 USAA920071221 1 20071118 A 5320 D53480020437 SHEAR PLATE AIRBUS 320 A320231 3930325 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 625AW 64 SAL - MAJOR REPAIR - C7 CHECK - CRACKED SHEAR PLATE, BS 3257/FR 68 - BS 3310/FR 69, S23R. REPLACED SHEAR PLATE, BS 3257 /FR 68 - BS 3310/FR 69, S23R IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007120400195 20071204 00195 EU 2007 12 4 F3LA200700317 1 20071122 A 3350 LIGHT AIRBUS A318 A318111 3940019 EU CABIN INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 804FR 2051 MAINTENANCE REPORTED SEAT-MOUNTED EMERGENCY LIGHTS AT ROW 22 ABC INOPERATIVE. REMOVED AND REPLACED SEAT-MOUNTED EMERGEN CY LIGHTS AT ROW 22 ABC IAW AMM 33-51-19, PB401. OPS CHECK GOOD. 2 L 7 2 4F RT 2007120400208 20071204 00208 EU 2007 12 4 07FDEA04937 1 20071126 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT PIT, BETWEEN FR 64/3461 AND 63/3408 STR 52R CORRODED. REMOVED CORROSION IAW A310-200 SRM 51-74-10. FOUND TO BE OU T OF LIMITS IAW A310- 200 SRM 51-10-00. REMOVED AND REPLACED STRINGER SECTION IAW A310-200 SRM 53-10- 14 PG 203/204 2 L 7 2 4F RT A35EU 2007120400216 20071204 00216 CE 2007 12 4 GUUA11020701 1 20071102 A 3260 SQUAT SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RT MLG OUT OF ADJUST A GUUA O OTHER N FALSE WARNING CL CLIMB 1 SO 29 69549 UE194 FLIGHT: 9128 AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. RETURNED TO DEPARTURE. LANDED WITH OUT INCIDENT. READJU STED RT MAIN LANDING GEAR SQUAT SWITCH. 2 L 7 2 4T 3 T RT A24CE E2NE 2007120400217 20071204 00217 CE 2007 12 4 GUUA11040701 1 20071104 A 3230 VALVE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MLG MISRIGGED A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 29 69549 UE194 FLIGHT: 9279 DURING APPROACH, LANDING GEAR WOULD NOT EXTEND. MANUALLY EXTENDED LANDING GEAR. LANDED WITHOUT INCIDENT. F OUND LANDING GEAR GROUND SERVICE VALVE IN THE UP POSITION PLACED IN THE DOWN POSITION. LANDING GEAR EXTENSION AND RETRAC TION OPERATIONAL CHECK GOOD. 2 L 7 2 4T 3 T RT A24CE E2NE 2007120400220 20071204 00220 CE 2007 12 4 DXTA200702593 1 20071103 A 2150 73838433 ACM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL AFT SERVICE BAY LEAKING E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 926QS 4842 7500026 THERE IS A BURNED OIL SMELL COMING FROM AIR SYSTEM. REMOVED FAULTY AIR CYCLE MACHINE. INSTALLED REPAIRED UNIT. PERFORM ED LEAK AND OPS CHECK GOOD. IAW MM. 21-50-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007120400224 20071204 00224 CE 2007 12 4 DXTA200702596 1 20071104 A 3240 BRAKE ASSY CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG MALFUNCTIONED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 639QS 5605139 LT BRAKE PEDAL ON CAPTAINS SIDE GOES NEARLY TO THE FLOOR BEFORE ENGAGING. T/S. FOUND BRAKE SYSTEM NEEDED BLED. BLED LT B RAKE SYSTEM MULTIPLE TIMES IAW MM CH 32-42-00. BRAKE SYSTEM OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007120400233 20071204 00233 EA 2007 12 4 SWIA200718893 1 20071123 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY MALFUNCTIONED A SWIA O OTHER N FALSE WARNING CL CLIMB 1 NM 07 479CA 7675 FLT 2500 - RECEIVED "SMOKE TOILET" CAUTION MESSAGE AFTER TAKEOFF. REPLACED LAV SMOKE DETECTOR. OPS CHECK GOOD IAW AMM 26--16-01. 2 L 7 2 4F RT A21EA 2007121800018 20071218 00018 CE 2007 12 18 DXTA200702604 1 20071111 A 3240 AHA1897 BRAKE RAYTHN DH125 HAWKER800XP 7150012 CE MLG DRAGGING E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 832QS 2395 258683 AFTER LANDING, AIRCRAFT BRAKES WERE APPLIED AT SLOW SPEED, AIRCRAFT VEERED LEFT DUE TO LEFT BRAKE GRABBING AND NOT RELEA SING. LEFT BRAKE RELEASED AFTER REPEATEDLY PUSHING THE PEDALS AND PULLING PARKING BRAKE LEVER. HAPPENED AGAIN ON RAMP OF FBO AT SLOW TAXI SPEED. 2 L 7 2 4F RT A3EU 2007120400257 20071204 00257 EA 2007 12 4 A6WA200740620 1 20071114 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 470ZW 7927 FOUND FLOOR SUPPORTS IN CARGO COMPARTMENT AT FS 621 RBL 38 CRACKED. REPAIRED IAW CRJ 200 REO 601R-53-61-117 REV C. (M) 2 L 7 2 4F RT A21EA 2007120400258 20071204 00258 EU 2007 12 4 TRBA2007096 1 20071109 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE EMERGENCY LIGHTS FAILED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 426AT 426 EMERGENCY LIGHTS STAY ON WITH ENGINE RUNNING. REPLACED EMERGENCY POWER SUPPLY 61WL IAW MM 37-51-21, OPT CK NORMAL. 2 H 7 2 4T 4 T RT A53EU E20NE 2007120400266 20071204 00266 EU 2007 12 4 TRBA2007098 1 20071112 A 3350 3011162 SIGN AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE SERVICE DOOR INOPERATIVE A TRBA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 448AM 448 SERVICE DOOR EMERGENCY EXIT SIGN INOPERATIVE. RAI SERVICE DOOR EMERGENCY EXIT SIGN IAW JIC 33-51-00. OPT OK IAW JIC 33- 50-00. 2 H 7 2 4T 4 T RT A53EU E20NE 2007120400279 20071204 00279 SW 2007 12 4 AC2A118174 1 20071111 A 2560 5016612 SEAT BELT BELL 206 206L1 1182107 SW ALLSN 250C 250C* GL FAILED D AC2A O OTHER O OTHER CR CRUISE 1 SW 31 39LR 45654 DEPARTED HELIPORT THE 0821 WITH 2 CPL PASSENGERS. ONE PASSENGER WAS IN THE LT FRONT SEAT WITH THE REMAINING PASSENGER IN THE RT REAR FORWARD FACING SEAT. ARRIVED AT SWP24 AT 0821 AND THE REAR PASSENGER DEPARTED THE AIRCRAFT. AFTER THE PASS ENGER DEPARTED THE PAD THE NEXT DESTINATION WAS SP 75. ARRIVED AT SP 75 NR 0833 WERE THE FRONT PASSENGER DEPARTED THE AI RCRAFT. AFTER THE PASSENGER DEPARTED THE DECK, RETURNED WITH AN ARRIVAL TIME OF 0854. DURING POST FLIGHT, NOTICED PAINT MISSING FROM AREA JUST AFT OF RT PASSENGER DOOR. UPON FURTHER INVESTIGATION, NOTICED THE RT REAR PASSENGER SEAT BELT WAS WEDGED BETWEEN THE AFT CROSS TUBE AND FLOAT INFLATION HOSE. NO NOISE WAS NOTICED. 1 G 7 1 3U 3 U H2SW E4CE 2007120400290 20071204 00290 CE 2007 12 4 GUUA11100702 1 20071110 A 3234 1013841377 CONTROL HANDLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG INTERMITTENT A GUUA O OTHER O OTHER TO TAKEOFF 1 SO 29 69549 UE194 FLIGHT: 9131, AFTER TAKEOFF LANDING GEAR DID NOT RETRACT WHEN LANDING GEAR SELECTED UP. RETURNED TO TPA. LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR CONTROL HANDLE . LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007120400300 20071204 00300 SO 2007 12 4 SIMA200733202 1 20071112 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 664MS 9613 5000 145779 DURING MBV INSPECTION, THE BAGGAGE DOOR LOWER SILL WAS FOUND TO BE CORRODED. REPLACED BAGGAGE DOOR LOWER SILL PER EMB S RM 145/1142 REV 38 CHAPTER 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007120400301 20071204 00301 EU 2007 12 4 COEA0702819 1 20071031 A 3411 PITOT HEAD AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE OBSTRUCTED A COEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 13 819FX 359 FLT 8080 - ABORTED TAKEOFF, DURING TAKEOFF ROLL PILOT NOTICED NR 2 AIRSPEED INDICATOR READ ZERO, FOLLOWED BY (DACD DATA INVALID) ON AFCS CONTROL PANEL. PILOT RETURNED TO RAMP AT OAK. MAINTENANCE FOUND AND REMOVED DEBRIS IN PITOT PROBE, TW O INSECTS. AIRCRAFT RETURNED TO SERVICE. REPEAT OF DISCREPANCY FROM CONTROL NR COEA 0701819. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2007120400310 20071204 00310 SO 2007 12 4 SIMA200733209 1 20071127 A 3320 BR900022 BALLAST EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 21 616AE 145092 STRONG PLASTIC MELTING OR BURNING SMELL COMING FROM GALLEY AREA. FOUND BALLAST OVER GALLEY GOING OUT REMOVED AND REPLAC ED BALLAST IAW EMB AMM 33-28-07. OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007120400317 20071204 00317 EA 2007 12 4 N6WA0071105 1 20071115 A 3397 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE EMERGENCY LIGHTS UNSECURE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 152GJ 10218 (2) OF THE AFT EMERGENCY LIGHTS INOP. RESECURED CONNECTOR TO NR 4 POWER SUPPLY. 2 L 7 2 4F 4 F RT A21EA E00063EN 2007120400322 20071204 00322 CE 2007 12 4 DJFA2007130 1 20071111 A 2910 AE1011889G0166 LINE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL HYD SYSTEM RUPTURED E DJFA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 EA 23 706LX 5887 7500073 THE CREW REPORTED THAT THEY LOST A-SYSTEM HYDRAULICS, THE CREW DECLARED AN EMERGENCY AND DIVERTED. MX INVESTIGATED AND FOUND NOSE WHEEL SYSTEM CENTERING PRESSURE HOSE TO RUPTURED. MX REPLACED HOSE AND BLED NWS SYSTEM. OPS AND LEAK CHECK GO OD. AIRCRAFT FERRIED TO A MFG MX FACILITY WITH THE GEAR DOWN AND LOCKED FOR A TOTAL A-SYSTEM HYDRAULIC BLEED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007120400323 20071204 00323 CE 2007 12 4 DJFA2007131 1 20071113 A 2120 UNKNOWN BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE CABIN ODOR E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 708TA RK178 THE CREW REPORTED HOT ODOR FROM CABIN DUCTING. RT SIDE TABLE FELT HOT AFTER SHUTDOWN. MAINTENANCE REMOVED THE SIDEWALL PANEL AND INSPECTED DUCTING. THE AIRCRAFT WAS RUN IN FULL HOT. NO DEFECTS OR LEAKS WERE NOTED. NO (HOT) OR BURNING O DOR NOTED DURING GROUND RUN. 2 H 7 2 4F 4 F RT A16SW E25EA 2007120400337 20071204 00337 WP 2007 12 4 UPS07851222 1 20071127 A 2560 ESCAPE ROPE DOUG DC8 DC873F 302199F WP COCKPIT OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 CAPTAIN'S ESCAPE ROPE COVER FELL OFF, ROPE UNCOILED. REPACKED AND STOWED ESCAPE TAPE AND REINSTALLED AND RESECURED ACCE SS DOOR ON CAPTAIN'S ESCAPE ROPE, REF MM 25-60-02-2. 2 L 7 4 4F RT 4A25 2007120400353 20071204 00353 NM 2007 12 4 SWAA075900 1 20071128 A 3350 D7170230 CHARGER BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 436WN 32456 DURING SCHEDULED HC1 CHECK, FOUND LT FWD CABIN EMERGENCY BATTERY CHARGER INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007120400355 20071204 00355 NM 2007 12 4 SWAA075945 1 20071202 A 5311 6546530 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007120500052 20071205 00052 WP 2007 12 5 AMTA200700594 1 20071113 A 2910 HYDRAULIC SYSTEM DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL MALFUNCTIONED A AMTA O OTHER K FLUID LOSS AP APPROACH 1 GL 11 705TZ 46915 ON FINAL AFTER SELECTING GEAR DOWN THE HYD SYS 3 ELEV OFF LIGHT CAME ON. NR 3 QUANTITY DROPPED TO 19 QTS. TAXIING IN A T ETAR THE QUANTITY CAME BACK UP TO 12 GALLONS AND LIGHT WENT OUT SERVICED AND BLED NR 3 HYD SYSTEM IAW MM 12-13-01. NR 3 QTY AND SYSTEM PSI GOOD. (K) 2 L 7 3 4F 4 F A22WE A23EA 2007120500066 20071205 00066 CE 2007 12 5 112207N336CS1 1 20071122 A 3233 99124655 ACTUATOR CESSNA 500 550 2076604 CE PWA 530 PW530A NE LT MLG FAILED E Z5FA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 63 336CS 2921 5501095 LT MLG DOWN INDICATION FAILED TO ILLUMINATE WHEN GEAR WAS EXTENDED. PERFORMED AFM ABNORMAL PROCEDURES. DECLARED EMERGENC Y, BLEW GEAR DOWN AFTER A SHORT TIME, GREEN DOWN INDICATION DID ILLUMINATE AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTE NANCE STAFF REPLACED GEAR ACTUATOR. OPS CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 2 4F 4 F A22CE E00053EN 2007120500069 20071205 00069 CE 2007 12 5 DXTA200702625 1 20071121 A 7700 MOTOR CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE ENGINE TORQUE INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 643QS 5605588 AFTER T/O, EEC MANUAL R ANNUNCIATOR ILLUMINATED, RAT DIGITS DISAPPEARED TO BE REPLACED BY AMBER DASHES, AND R ENGINE N1 RPM DECREASED BY APPROX 10 PERCENT. REMOVED INOP RIGHT ENGINE BOV TORQUE MOTOR AND INSTALLED AN OVERHAULED TORQUE MOTOR . INSTALLED A NEW ORIFICE SIZE. ALL RUN CHECKS GOOD PER EMM 75-30-01. NEW ORIFICE SIZE-30J1296CL48. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007120500072 20071205 00072 CE 2007 12 5 DXTA200702628 1 20071125 A 3260 SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG DOOR OUT OF RIG E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 873QS 258573 RT MAIN GEAR RED INDICATION REMAINED ILLUMINATED AFTER GEAR RETRACTION AND ALL GREEN INDICATORS WERE EXTINGUISHED. PER FORMED NUMEROUS OPS CHECKS OF GEAR WITHOUT ANY DISCREPANCIES, CHECK RIGGING OF GEAR UPLOCK DOOR SWITCH IAW AMM 32-60-00 & RAC DWGS. 25-8NA5-616A ISS 1 & 149-349531, REV R. REF HBS-LIT WO 19-1425 SQK 1.21 2 L 7 2 4F 4 F RT A3EU E6WE 2007120500103 20071205 00103 NM 2007 12 5 NWAA073825816 1 20071119 A 3320 BALLAST BOEING 757 757351 1384991 NM CABIN LIGHTS SMOKE A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 596NW 32996 DURING FLIGHT THE LAV AT DOOR 3 LEFT A PASSENGER NOTICED THAT THE LIGHTS FLICKERED AND WENT OUT. THIS WAS FOLLOWED BY S OME SMOKE FROM OVERHEAD THE SMELL OF BURNING PLASTIC. FLIGHT CONTINUED ON AND LANDING WAS UNEVENTFUL. MAINTENANCE REMO VED AND REPLACED LAV BALLAST. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007120500104 20071205 00104 CE 2007 12 5 135762112207 1 20071122 A 2140 W31X2M1G15 SWITCH CESSNA 402 402C 207590R CE HEATER FAILED E HYIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 61 762EA 402C0061 HEATER INOPERATIVE, SMOKE CAME FROM SWITCH. MAINTENANCE INSPECTED AND FOUND THE HEATER SWITCH TO BE BAD. MAINTENANCE R EMOVED AND REPLACED SWITCH, OPERATIONALLY TESTED HEATER AND SWITCH SATISFACTORY WITH NO OTHER DEFECTS NOTED. 1 L 7 2 3O A7CE 2007120500106 20071205 00106 2007 12 5 SIMA200733006 4 20071124 A 3497 SSPD11338 COUPLER CNDAIR CL600 CL6002C10 1390015 EA VOR SYSTEM MALFUNCTIONED A SIMA L ABORTED APPROACH N FALSE WARNING LD LANDING 1 SW 21 520DC 10140 WHILE ON ILS APPROACH A/C WOULD NOT TRACK LOCALIZER. SECOND APPROACH ILS OPERATIONAL. REMOVED AND REPLACED VOR/ILS COU PLER WITH SERVICEABLE COUPLER IAW CRJ 700 AMM 34-51-04 OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT A21EA 2007120500108 20071205 00108 NM 2007 12 5 2007UALA04788 1 20071121 A 5330 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU LT FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 903UA 25003 LEFT FUSELAGE SKIN GOUGED JUST AFT OF NR 2 AFT MED. GENERAL FUSELAGE SKIN REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007120500109 20071205 00109 NM 2007 12 5 2007UALA04789 1 20071121 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 860-908 WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 EXTERNAL FUSELAGE SKIN HAS SEVERAL AREAS OF WEAR UNDER DORSAL FIN LANDING FROM BS 860-908. BLENDED WORN AREAS. FABRICAT ED AND INSTALLED EXTERNAL DOUBLER, INTERNAL STRAPS, AND FILLERS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007120500110 20071205 00110 NM 2007 12 5 2007UALA04790 1 20071121 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 331UA 24192 FUSELAGE LOWER SKIN CRACKED AT FWD E&E EXHAUST OUTLET. MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED EXTERNAL AND INTERNAL REPAIR DOUBLERS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007120500111 20071205 00111 NM 2007 12 5 2007UALA04793 1 20071124 A 5313 STRINGER SPLICE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU S15R BS 360 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 STR 15R SPLICE IS CRACKED BS 360. MAJOR REPAIR: REPLACED STRINGER SPLICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007120500112 20071205 00112 NM 2007 12 5 2007UALA04794 1 20071124 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 807 S26-27L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 LOWER FUSELAGE HAS A DENT ALONG FRAME SHEAR TIE BETWEEN STR 26L-27L BS 807. MAJOR REPAIR: FABRICATED AND INSTALLED E XTERNAL FUSELAGE SKIN DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007120600001 20071206 00001 EA 2007 12 6 TRAX200701772 1 20071121 A 5310 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA BS 349 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 PAX DOOR CUTOUT FRAME FS 349.00 HAS CORROSION. REMOVED MINOR SURFACE CORROSION FROM FWD BRACKET. IAW CRJ SRM 51-21-06. ASSEMBLED BRACKETS TO ANGLES REPLACING CORRODED PART. 2 L 7 2 4F RT A21EA 2007120600002 20071206 00002 CE 2007 12 6 J00A200727001 1 20071125 A 3250 S3128B0166000G FLEX LINE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG STEERING FAILED E J00A B A EMER. DESCENT UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 01 27VP 4404 2 7500027 FLT CREW REPORTED THE FOLLOWING: SOON AFTER TAKEOFF HYDRAULIC QUANTITY A EICAS MESSAGE FOLLOWED SHORTLY BY HYDR PRESSUR E A EICAS MESSAGE. CREW DECLARED AN EMERGENCY WITH LOSS OF HYDRAULIC A SYSTEM AND LANDED AIRCRAFT MOMENTS AFTER TAKEOFF . HYDRAULIC A SYS AFFECTED GEAR EXTENSION, FLIGHT CONTROLS, AND BRAKING AFTER LANDING. LANDING GEAR WAS EXTENDED BEFOR E HYD RESERVOIR A WAS DEPLETED. CREW HAD TO BRAKE AIRCRAFT WITH EMERGENCY PNEUMATIC BRAKES. AIRCRAFT WAS IMMEDIATELY I NSPECTED WITH FOLLOWING OBSERVATIONS NOTED FROM FLIGHT CREW AND MECHANIC; THERE IS HYDRAULIC FLUID STREAKING FROM NOSE L ANDING GEAR TO EMPENNAGE. FURTHER INVESTIGATION FROM MECHANIC; FOUND NWS CENTERING LINE TO HAVE FAILED AT BEND IN FLEXI 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007120600004 20071206 00004 GL 2007 12 6 DHLA200700070 2 20071129 A 7200 ENGINE DOUG DC8 DC873 302199C WP GE CFM CFM562 GL NR 3 SHUTDOWN A DHLA O OTHER E Y J VIBRATION/BUFFET ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 GL 05 801DH 46033 693493 IN CRUISE FL 360 FELT A/C SHUDDER AND VIBRATION FOUND NR 3 ENGINE SPOOLING DOWN ATTEMPTED RELIGHT EGT 565 ENGINE N1 WOUL D NOT ACCELERATE N2 MAX 70. VIBRATION NOTED DURING DECELERATION AND ADVANCE OF THRUST LEVER PRECAUTIONARY SHUTDOWN ACCO MPLISHED A WINDMILLING OIL PRESSURE 4 PSI 13 PERCENT N2 FUEL CONTROL CYCLED FOR EACH HOUR ENG WAS SLOW TO ACCELERATE FRO M GND IDLE TO T/O THRUST. R&R NR 3 ENG. PER DC-8 MAINTENANCE TASK MANUAL 71.1. OPS CK SDRVICEABL 2 L 7 4 4F 4 F RT 4A25 E2GL 2007120600007 20071206 00007 EU 2007 12 6 SIMA200733215 1 20071126 A 7620 6068T72P22 HMU SAAB SF340 340B 7860101 EU LT ENGINE MALFUNCTIONED A SIMA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SW 21 313AE 340B313 CREW REPORTED THAT SHORTLY AFTER TAKEOFF LEFT ENGINE POPPED THEN SHUT DOWN WITH AUTO FEATHER RETURNED TO FIELD. REMOVE D AND REPLACED LEFT HMU LEAK CHECK AND OPERATIONAL CHECK GOOD AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4T RT A52EU 2007120600008 20071206 00008 NM 2007 12 6 07FDEA04996 1 20071204 A 5270 BLOCKER DOOR BOEING 727 727200 138407E NM CARGO DOOR OUT OF ADJUST A FDEA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 258FE 20940 MAIN CARGO DOOR "A" OPEN LIGHT ILLUMINATED INFLIGHT, PRESSURIZATION NORMAL INITIALLY, FLICKERED AT FL 200 THEN REMAINE D ON STEADY IN DESCENT UNTIL SHORT FINAL THEN WENT OUT. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-15-01 CATEGORY: C EXPI RATION: 14DEC07 "MEL 52-15-01: MAIN CARGO DOOR WARNING LIGHT SYSTEM (A ) INOP. VERIFY DOOR CLOSED AND LOCKED PRIOR TO E ACH BLOCK OUT. "A" OPEN LIGHT C/0340477. T/S TO CABLE GOING TO AFT BLOCKER ASSY NEEDS ADJ.AND IS CAUSING SWITCH S9058 TO BE ON THE EDGE OF MAKE OR BREAK. ADJ AFT BLOCKER ASSY CABLE IAW NASI MM 52-30-00 PG 504. 2 L 7 3 4F RT A3WE 2007120600010 20071206 00010 EA 2007 12 6 SIMA200733211 1 20071126 A 2150 CG670950093 ACM CNDAIR CL600 CL6002C10 1390015 EA RIGHT SMOKE A SIMA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 521AE 10142 LAV SMOKE WARNING INDICATION AND RT PACK AUTO FAIL MSGS ON TAXI OUT. ISSUED MEL 2113 FOR RT PACK. REMOVED AND REPLACED RIGHT HAND ACM IAW CRJ 700 AMM 21-51-08 OPS CHECK AN LEAK CHECK GOOD AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT A21EA 2007120600011 20071206 00011 EU 2007 12 6 07FDEA04967 1 20071129 A 3260 141FL01D3 SWITCH AIRBUS 310 A310 EU N/A FAILED A FDEA L ABORTED APPROACH N S FALSE WARNING AFFECT SYSTEMS AP APPROACH 1 SO 25 412FE 360 RECEIVED AN AUDIBLE "TOO LOW-GEAR" WNG ON SHORT FINAL. ALL GEAR INDS SHOWED GREEN/DOWN, SWITCHED TO POS1, REATTEMPT LAN DING ALL SYS WORK NORMAL. ACN RELEASED FOR SVC. BRIEF INCREASED ALTITUDE AND TERRAIN AWARENESS." R&R MICROSWITCH 7 9GB IN REF TO MM 32-00-00-4 ,PERFORMED OPS ON THE NR 2 INDICATION SYSTEM ,CHECKED NORAML. ITEM CLOSED,A/C OK TO CONT S VC. 2 L 7 2 4F RT A35EU 2007120600012 20071206 00012 EU 2007 12 6 WRNA200700061 1 20070118 A 3150 WARNING MESSAGE AIRBUS 300 A300B4203 3930306 EU FALSE ACTIVATION A WRNA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 05 821SC 211 DURING TAKEOFF, RECEIVED A CONFIGURATION DEVIATION WARNING, TAKEOFF ABORTED. UNABLE TO DUPLICATE CONFIGURATION DEVIATIO N WARNING. PREPARED A/C FOR TEST FLIGHT, TEST FLIGHT COMPLETED SATISFACTORY 11-26-07. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A35EU 2007120600013 20071206 00013 2007 12 6 USAA920071227 2 20071127 A 7230 V2527A5 ENGINE AIRBUS 320 A320232 3930326 EU RT PYLON STALLED A USAA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 EA 19 667AW 30930 15364 1710 ENG NR 2 COMPRESSOR VANE FAULT, COMPRESSOR STALLED AND ENG NR 2 SHUTDOWN. MAINTENANCE PERFORMED BORESCOPE INSPECTION OF HPT STAGES THROUGH 8 HPC AND 1ST STAGE BLADES AND VANES. SUBSTANTIAL WEAR OBSERVED THROUGHOUT ALL AREAS INSPECTED AS W ELL AS MODERATE HEAT DAMAGE DUE TO OVERTEMP. NO MISSING MATERIALS OR CATASTROPHIC FAILING OBSERVED. THE AIRCRAFT WAS M AINTENANCE FERRIED BACK TO PHX. MAINTENANCE REMOVED AND REPLACED THE #2 ENGINE IAW TASK CARD R5M71302. LEAK AND OPERA TIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 2007120700002 20071207 00002 NE 2007 12 7 U2RA872LP2804 2 20071128 A 7200 CFM562C1 ENGINE DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C1 13802 NE NR 1 FLAMED OUT A U2RA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 GL 23 872SJ 39908 5315 46040 693372 NR 1 ENGINE FLAMED OUT TOP OF DESCENT AT IDLE. RELIGHT PERFORMED IAW INFLIGHT ENGINE START PROCEDURES, OBSERVED NORMAL START AND INDICATION. 2 L 7 4 4F 4 F RT 4A25 E2GL 2007120700003 20071207 00003 NM 2007 12 7 DL75A071506 1 20071117 A 7920 CARBON SEAL BOEING 757 757212 1384951 NM PWA 2037 PW2037 NE NR 1 ENGINE DAMAGED A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 750AT 65624 23126 716391 LEFT ENGINE OIL QTY WENT TO ZERO FOLLOWED BY OIL PRESS FLUX. AS CREW WAS FOLLOWING CHECKLIST LEFT ENGINE OIL PRESSURE I NDICATION STARTED FLASHING RED CREW THEN SHUT ENGINE DOWN. THIS OCCURED AT CRUISE FLT. REMOVED AND REPLACED NR 1 ENGIN E PRECOOLER CARBON SEAL AND OIL PUMP. RAN NR 1 ENGINE FOUND EXCESSIVE OIL LEAK IN TAILPIPE. REPLACED NR 1 ENGINE PER T RANS 6T103. 2 L 7 2 4F 4 F RT A2NM E17NE 2007120700014 20071207 00014 NM 2007 12 7 DLM90071526 1 20071119 A 5753 5930496 VANE DOUG MD90 MD9030 3023690 NM TE FLAP GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 LEFT WING O/B FLAP O/B VANE GOUGED TOP SIDE ABOVE I/B ATTACH POINT. REPAIRED LEFT O/B FLAP VANE IAW MD-90 SRM 51-10-02D PG 84 ON N/R 5400-0052 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007120700015 20071207 00015 NM 2007 12 7 DL76S071527 1 20071120 A 2761 252T13012 ACTUATOR BOEING 767 767332 1382001 NM NR 5 SPOILER CRACKED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 136DL 23146 DURING TAXI C HYD LOW PRESS LIGHT ILLUM AND QTY WENT TO 0. A/C TOWED BACK TO GATE. FOUND NR 5 SPOILER ACT HOUSING CRAC KED. REPLACED SAME, OP CHK AND LEAKS NORMAL. 2 L 7 2 4F RT A1NM 2007120700016 20071207 00016 NM 2007 12 7 DL76S071528 1 20071121 A 5311 FRAME BOEING 767 767332 1382001 NM FS 1725 S7R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 121DE 23435 FATIGUE CRACKS IN SKIN AND BULKHEAD CHORD STRAP AT FS 1725.5 AND S-7R. CUT OUT CRACKED MATERIAL AND INSTALLED DOUBLERS. 2 L 7 2 4F RT A1NM 2007120700018 20071207 00018 NM 2007 12 7 DLM88071531 1 20071027 A 5315 FLOORBEAM DOUG MD88 MD88 3023688 NM BS 650 S25-26R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 CRACK ON FLOOR SUPPORT STA Y=650 BTWN LONGERON 25 RT AND 26 RT REPAIRED PER ERA 413029-14MA. 2 L 7 2 4F RT A6WE 2007120700019 20071207 00019 NM 2007 12 7 DLM88071532 1 20071011 A 5320 WEB DOUG MD88 MD88 3023688 NM BS 1140 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 CORROSION ON WEB AT STA Y=1140 AND X=54. REPAIR PER SRM 51-30-5. 2 L 7 2 4F RT A6WE 2007120700021 20071207 00021 NM 2007 12 7 DLM88071537 1 20071028 A 5340 ATTACH FITTING DOUG MD88 MD88 3023688 NM BULKHEAD BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 BROKEN CLIP ON O/B END OF P-DOME LT NR 3 STIFFENER. REPLACED CLIP PER DOUGLAS DWG 9915558. 2 L 7 2 4F RT A6WE 2007120700023 20071207 00023 NM 2007 12 7 DLM88071539 1 20071103 A 5712 RIB DOUG MD88 MD88 3023688 NM LWS 453 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 CRACK ON LT WING FIXED LEADING EDGE RIB STA XFS=453. REPLACED RIB PER DWG 9919329-9. 2 L 7 2 4F RT A6WE 2007120700026 20071207 00026 NM 2007 12 7 DLM88071542 1 20071031 A 5320 ANGLE DOUG MD88 MD88 3023688 NM FUSELAGE WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 WORN LT LWR ANGLE AT AFT ENTRY DOOR, REPLACED ANGLE PER DWG 9915565. 2 L 7 2 4F RT A6WE 2007120700028 20071207 00028 2007 12 7 DLM88071544 4 20071015 A 2565 SUPPORT DOUG MD88 MD88 3023688 NM R1 DOOR SLIDE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 CORROSION RT AFT SLIDE SUPPORT AT R1 DOOR. REPLACED SUPPORT PER SRM 51-30-1, 51-10-4. 2 L 7 2 4F RT A6WE 2007120700029 20071207 00029 2007 12 7 DLM88071545 4 20071022 A 2565 SUPPORT DOUG MD88 MD88 3023688 NM L2 DOOR SLIDE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 CORROSION ON FWD SLIDE SUPPORT AT L2 DOOR. REPLACED SUPPORT PER SRM 51-30-50, 51-10-4. 2 L 7 2 4F RT A6WE 2007120700030 20071207 00030 2007 12 7 DLM88071546 4 20071022 A 2565 SUPPORT DOUG MD88 MD88 3023688 NM L2 DOOR SLIDE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 CORROSION ON AFT SLIDE SUPPORT AT L2. REPLACED SUPPORT PER SRM DWG 9930612. 2 L 7 2 4F RT A6WE 2007120700033 20071207 00033 NM 2007 12 7 DLM88071549 1 20071013 A 5320 THRESHOLD DOUG MD88 MD88 3023688 NM R1 DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 CORROSION ON WEB THRESHOLD AT R1. REPLACED THRESHOLD PER DWG 9957828. 2 L 7 2 4F RT A6WE 2007120700034 20071207 00034 NM 2007 12 7 DLM88071550 1 20071023 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 984-1003 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 CORROSION ON RT CUSP WEB AT STA Y=984 TO Y=1003. REPLACED WEB PER DWG 9930612. 2 L 7 2 4F RT A6WE 2007120700035 20071207 00035 NM 2007 12 7 DLM88071551 1 20071013 A 5320 THRESHOLD DOUG MD88 MD88 3023688 NM R1 DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 FOUND CORROSION ON PLATE THRESHOLD AT R1. REPLACED PLATE THRESHOLD PER DWG 9957828. 2 L 7 2 4F RT A6WE 2007120700038 20071207 00038 NM 2007 12 7 DL757071554 1 20071125 A 2530 252010508 CHILLER BOEING 757 757232 1384965 NM GE CF6 CF680C2B6F 30025 NE NR 2 GALLEY OVERHEATED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 617DL 370 22907 704806 DURING FLIGHT, BURNING ODOR DETECTED IN FORWARD GALLEY. ALL CIRCUIT BREAKERS WERE PULLED. FOUND INSULATION INSIDE CHIL LER/FREEZER MELTED AND BURNED. CHECKED POWER TO UNIT ALL 3 PHASES CHECK OK. REPLACED CHILLER/FREEZER. CHECKS GO OD. OK TO CLEAR PER MCO AND PLACARD REMOVED. 2 L 7 2 4F 4 F RT A2NM E13NE 2007120700039 20071207 00039 NE 2007 12 7 DL76G071556 2 20071126 A 7310 FUEL FILTER BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 ENGINE UNKNOWN A DALA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 27 175DZ 29696 706110 LEFT AND RIGHT ENG FUEL FILTER STATUS MSG. REPLACED LT AND RT FUEL FILTERS PER MM 73-11-03. RAN LT AND ENGINES. LEAK CHECK OK. OPERATION NORMAL. TANKS SUMPED NO CONTAMINATION FOUND. 2 L 7 2 4F 4 F RT A1NM E13NE 2007120700041 20071207 00041 NM 2007 12 7 DLM90071560 1 20071126 A 5310 DOOR FRAME DOUG MD90 MD9030 3023690 NM BS 1211-1268 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 AFT CARGO COMPT LOWER JAMB OUTER SURFACE HAS CORROSION STA 1211 TO 1268. REPAIRED AFT CARGO DOOR CUTOUT LOWER JAMB IAW MD-80 53-05D FIG 63 ON N/R 1000-0074, AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007120700042 20071207 00042 NM 2007 12 7 DL738071561 1 20071124 A 3244 TIRE BOEING 737 737832 13844CF NM NR 3 FAILED A DALA C ABORTED TAKEOFF D INFLIGHT SEPARATION TO TAKEOFF 1 SO 27 3744D 29662 ON T/O OUT OF PHX, NR 3 TIRE LOST RECAP. TIRE DEBRIS DAMAGED FLAPS/HYD LINES/WIRES IN WHEEL WELL LEADING EDGE OF RT STA B. FLIGHT DIVERTED TO DENVER DUE TO LOSS OF A SYSTEM HYD QTY. REPLACED BROKEN HYD LINES AND DOWN/LOCK HARNESS AND ANT I-SKI HARNESS. LK CKD AND PERF A/S, A/B CK OUT, DOWN AND LOCK IN OK. 2 L 7 2 4F RT A16WE 2007120700043 20071207 00043 NM 2007 12 7 DL757071562 1 20071127 A 2120 UNKNOWN BOEING 757 757232 1384965 NM CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 624DL 22914 AFTER DESCENT, PILOTS SMELLED ELECTRICAL ODOR IN COCKPIT. RAN ENGINES TO TAKEOFF POWER WITH FULL ELECTRICAL LOAD. NO O DORS NOTED, RELAMP SWITCH LIGHTS RT ENG BLEED AND RT RECIR FAN. ALL CKS NML. 2 L 7 2 4F RT A2NM 2007120700044 20071207 00044 NM 2007 12 7 DL757071563 1 20071126 A 2910 251124217 LINE BOEING 757 757232 1384965 NM LT HYD SYS BROKEN A DALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 634DL 23615 ON TAXI OUT, LT HYD QTY DROPPED TO .18 ASSOC LT HYD SYS PRESS EICAS LT ENG HYD PRESS AND LT ELEC HYD PRESS LIGHTS ALL CA ME ON. FOUND RT OUTBD AILERON PCA PRESS LINE CRACKED. INST TEMP LINE PER AMM 20-10-09-801-001. NEEDS MFG P/N 2511242- 17. TEMP LINE NEEDS TO BE INSP WITHIN 175 HRS AND REPLACED WITHIN 350 HRS. SERVICED LT HYD SYS TO FULL. LEAK CK AND OPS CK GOOD. 2 L 7 2 4F RT A2NM 2007120700046 20071207 00046 NM 2007 12 7 DLM88071565 1 20071126 A 2910 HYDRAULIC SYSTEM DOUG MD88 MD88 3023688 NM LOW PRESSURE A DALA O OTHER J WARNING INDICATION LD LANDING 1 SO 27 977DL 53258 AFTER EXTENDING SLATS BOTH LT AND RT HYD PRESS DROPPED TO ZERO. AFTER RESETTING C/B H17 PRESS RETURNED TO NML. FOUND A IR IN BOTH LT AND RT SYS BED AIR. SERVICED TO FULL. FOUND A 4 ACCUM LOW LT T/R LEAKING. NO BYPASS PINS POPPED. SERV LT/RT BRAKE ACCUM AND RT THRUST REV ACCUM TO PLACARD. RAN ENG PRESS CKS GOOD. ECLECTIC PUMPS CKS GOOD. PRESS CK GOOD. CHECK SYS AGAIN FOR AIR. NO SYS HYD LEAKS NOTED. PRECAUTION CHANGED BOTH ENG HYD PUMPS. ALSO CHANGED LT THRUST REV ACCUM LEAKING. REPLACED LT THRUST REV ACCUM. ALSO, REPLACED BOTH CASE DRAIN FILTERS AND NR 1 GARLOCK SEAL. 2 L 7 2 4F RT A6WE 2007120700047 20071207 00047 NM 2007 12 7 DL757071566 1 20071127 A 2910 NAS161212 O-RING BOEING 757 757232 1384965 NM HYD SYSTEM FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 27 631DL 23612 ON FINAL, CREW REPORTED LOSS A LEFT HYD FLUID. FOUND CONNECTOR ON FLAP/SLAT DEPRESSURIZATION MODULE IN LEFT WHEELWELL W ITH O-RING BLOWN OUT. REPLACED O-RING. LEAK CKS GOOD. SVCD LEFT HYD SYS QTY TO FULL. 2 L 7 2 4F RT A2NM 2007120700048 20071207 00048 2007 12 7 FFKA119 4 20071123 A 6122 F411B GOVERNOR PIPER PA32 PA32R300 7103213 SO LYC 0540 IO540K1G5D 41532 SO HARTZL HCC2Y CHCC2YF2 GL MALFUNCTIONED B FFKA O OTHER J WARNING INDICATION CL CLIMB 1 SO 05 6291J 1134 32R7680350 L1456448A CH34693B PILOT REPORTED THAT THE TACHOMETER WAS INDICATING 100 RPMS HIGHER THEN RECOMMENDED BY THE ENGINE MANUFACTURE AFTER TAKEO FF BUT STILL HAD CONTROL OF THE PROPELLER GOVERNOR. REMOVED GOVERNOR FROM SERVICE AND SENT OFF FOR EVALUATION, THIS EVA LUATION DETERMINED THAT THERE WAS INTERNAL OIL LEAKAGE OF OIL PRESSURE CAUSING THE UN-COMMANDED PROPELLER RPM FLUCTUATIO N. 1 L 7 1 3O 3 O A3SO 1E4 5 C P920 2007120700050 20071207 00050 2007 12 7 FFKA120 4 20071121 A 6122 F44A GOVERNOR PIPER PA32 PA32300 7103212 SO LYC O540 IO540K1A5 41532 EA HARTZL HCC2Y HCC2YK2 GL PROPELLER MALFUNCTIONED B FFKA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 05 833WC 836 327640059 L319548A CH36545B PILOT REPORTED THAT THE TACHOMETER WAS INDICATING 100 RPMS HIGHER THEN RECOMMENDED BY THE ENGINE MANUFACTURE AFTER TAKEO FF PILOT HAD NO CONTROL OF THE PROPELLER GOVERNOR. PILOT REDUCED ENGINE POWER TO KEEP RPMS BELOW REDLINE AND THEN COULD NOT MAINTAIN ALTITUDE. REMOVED GOVERNOR FROM SERVICE AND SENT OFF FOR EVALUATION, THIS EVALUATION DETERMINED THAT THER E WAS INTERNAL OIL LEAKAGE OF OIL PRESSURE CAUSING THE UN-COMMANDED PROPELLER RPM FLUCTUATION. 1 L 7 1 3O 3 O A3SO 1E4 5 C P920 2007120700051 20071207 00051 NM 2007 12 7 F3LA200700321 1 20071113 A 5320 PLATE AIRBUS A319 A319111 3930336 NM FUSELAGE LOOSE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED SHEARED RIVETS ON SILL PLATE AT FRAME 68, AFT AND OTBD OF +Y1292 BEAM. REMOVED SHEARED RIVETS THAT CONNECT PLATE TO FLOOR BEAM IAW SRM 51-42-11. REPLACED THE FOUR SHEARED BLIND RIVETS THAT ATTACH TH E SHEAR PLATES TO THE LONGITUDINAL BEAMS WITH HL11VF6 LOCK FASTENERS. REPLACED THE SHEARED SOLID RIVETS THAT ATTACH THE JOINT SHEETS TO THE LONGITUDINAL BEAMS WITH HL11VF6 LOCK FASTENERS. ABOVE WORK ACCOMPLISHED IAW EA A9-53R-12267. 2 L 7 2 4F RT A28NM 2007120700054 20071207 00054 NM 2007 12 7 F3LA200700322 1 20071113 A 5320 PLATE AIRBUS A319 A319111 3930336 NM FUSELAGE LOOSE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED SHEARED RIVETS ON SILL PLATE AT FRAME 69, -Y1292 FLOORBEAM. REMOVED SHEARED RIV ETS ON WEB PLATE AFT OF FR68 FLOORBEAM AT -Y1292 IAW SRM 51-42-11, PARA. 6. INSTALLED LOCK FASTENER THROUGH WEB PLATE A FT OF FR68 THAT ATTACHES TO -Y1292 BEAM IAW EA A9-53R-12267. 2 L 7 2 4F RT A28NM 2007120700057 20071207 00057 2007 12 7 746004 4 20071127 A 2565 SLIDE BOEING 747 747206B 1384856 NM LEFT UNWANTED DEPLOY A Q2SA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 EA 63 746SA 21111 UPPER DECK LEFT ESCAPE SLIDE INADVERTENTLY DEPLOYED. REMOVED SLIDE ASSEMBLY AND TRANSFERRED TO DEFERRED ITEM. 2 L 7 4 4F RT A20WE 2007120700058 20071207 00058 NM 2007 12 7 AALA20072246 1 20071118 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 795AN 30257 DFW - EMERGENCY LIGHT AT SEAT 22G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120700059 20071207 00059 WP 2007 12 7 AALA20072254 1 20071119 A 3350 0201804001 LENS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 975TW 53625 MSP - EMERGENCY LIGHT AT SEAT 12D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A6WE 2007120700061 20071207 00061 NM 2007 12 7 AALA20072248 1 20071118 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 774AN 29581 DFW - EMERGENCY LIGHT AT SEAT 21C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120700062 20071207 00062 WP 2007 12 7 AALA20072243 1 20071118 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 447AA 49473 SFO - EMERGENCY LIGHTS AT SEAT ROWS 28 TO 32 INOPERATIVE. REPLACED BATTERY PACK AND REPAIRED WIRING BETWEEN SEAT ROWS 2 7 AND 28 FOR INOPERATIVE EMERGENCY LIGHTS AT SEAT ROWS 28 TO 32. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007120700063 20071207 00063 WP 2007 12 7 AALA20072242 1 20071118 A 2910 HOSE DOUG DC9 DC983 3022083 WP HYD SYSTEM LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 588AA 53251 AUS INFLIGHT T1960/18NOV, RIGHT HYDRAULIC SYSTEM LOST FLUID AT CRUISE. NORMAL GEAR EXTENSION WAS USED. LANDED AUS WITH OUT INCIDENT. FOUND RIGHT HYDRAULIC RETURN LINE LEAKING AT AFT CARGO RIGHT WALL. REPLACED RIGHT HYDRAULIC RETURN LINE A T AFT CARGO RIGHT WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007120700064 20071207 00064 NM 2007 12 7 AALA20072249 1 20071118 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 774AN 29581 DFW - EMERGENCY LIGHT AT SEAT 22C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120700065 20071207 00065 NM 2007 12 7 AALA20072244 1 20071118 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 795AN 30257 DFW - EMERGENCY LIGHTS AT SEAT ROWS 26 TO 28 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 26 TO 28. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120700067 20071207 00067 WP 2007 12 7 AALA20072251 1 20071119 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 976TW 53626 SFO - EMERGENCY LIGHTS AT OVERWING LEFT AND RIGHT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERWING L EFT AND RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007120700068 20071207 00068 WP 2007 12 7 AALA20072252 1 20071119 A 3397 TERMINAL DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 976TW 53626 SFO - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 8 TO 16 INOPERATIVE. CLEANED BATTERY PACK TERMINALS FOR EMERGENCY LIGHTS A T OVERHEAD SEAT ROWS 8 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007120700069 20071207 00069 WP 2007 12 7 AALA20072253 1 20071119 A 3350 OL1098BPEGPL LAMP DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 975TW 53625 MSP - EMERGENCY LIGHT AT SEAT 12D MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007120700070 20071207 00070 WP 2007 12 7 AALA20072255 1 20071119 A 3350 0202226001 SHROUD DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 975TW 53625 MSP - EMERGENCY LIGHT AT SEAT 12D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007120700071 20071207 00071 NM 2007 12 7 AALA20072256 1 20071119 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 966AN 30094 MIA - EMERGENCY LIGHT AT SEAT ROW 14DEF DOOR SIDE WALL INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEA T ROW 14DEF DOOR SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007120700072 20071207 00072 NM 2007 12 7 AALA20072261 1 20071119 A 3350 SHROUD BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 910AN 29512 DFW - EMERGENCY LIGHT AT SEAT ROW 8DEF SHROUD BROKEN. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 8DEF. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007120700074 20071207 00074 NM 2007 12 7 AALA20072259 1 20071119 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 647AM 24605 JFK - EMERGENCY LIGHTS AT SEAT ROW 27 TO AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROW 27 TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007120700076 20071207 00076 NM 2007 12 7 AALA20072258 1 20071119 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 647AM 24605 JFK - EMERGENCY EXIT LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT NUMBE R ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007120700077 20071207 00077 NM 2007 12 7 AALA20072245 1 20071118 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 795AN 30257 DFW - EMERGENCY LIGHT AT SEAT 22G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120700080 20071207 00080 EU 2007 12 7 07FDEA04949 1 20071127 A 5347 R5307008820000 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 671FE 778 MCC SEAT TRACK SECTION 2L HAS CORROSION AT FRAMES 77 AND 78. REMOVED AND INSTALLED SEAT TRACK IAW A300-600 SRM 53-1-16 AND 51-40-21. 2 L 7 2 4F RT A35EU 2007120700087 20071207 00087 EU 2007 12 7 07FDEA04956 1 20071128 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT CARGO PIT, STRINGER 53L CORRODED, FR 58 TO FR 59 (STA X3143 TO STA X3196). REMOVED COUPLING AND STRINGER SECTION. REMOVED SHEAR TIE. FABBED COUPLING AND STRINGER SECTION IAW SRM 53-10-14. ALODINED IAW SRM 51-21-10. PRIMED & PAINTED IAW SRM 51-23-10. INSTALLED COUPLING AND STRINGER SECTION AND SHEAR TIE IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007120700089 20071207 00089 EU 2007 12 7 07FDEA04958 1 20071128 A 5320 A532782620700 TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 MAIN DECK FLOOR, ADAPTER TRACK CRACKED, STA X3143, BL -Y685 TO -Y910. REMOVED AND REPLACED ADAPTER TRACK IAW A310-200 SRM 51-40-21 PAR 6, AND 51-40-44 PAR 2. 2 L 7 2 4F RT A35EU 2007120700092 20071207 00092 NM 2007 12 7 QXEA200701765 1 20071126 A 3010 DEICE SYSTEM BOMBDR DHC8 DHC8402 1390042 NM RT ENGINE INTAKE MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 424QX 4006 SEA FLIGHT NR 2340: RIGHT ENGINE INTAKE DEICE BOOT FAILS TO SHOW GREEN LIGHT INFLATION ON DEICE PANEL. BULB TEST OK AND DEICE PRESSURE NORMAL. DEICE PRESSURE CAUTION WOULD ILLUMINATE ON EVERY 2ND TO 3RD CYCLE. AIRCRAFT RETURNED TO SEA. MAINTENANCE C/W FUNCTIONAL TEST OF THE AIRFRAME DEICE SYSTEM IAW Q400 AMM 30-11-00-720-801. NO DEFECTS NOTED. CHECKED CDS FOR FAULTS. NO FAULTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007120700093 20071207 00093 NM 2007 12 7 QXEA200701766 1 20071128 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 418QX 4143 BOI FLIGHT NR 2399: CABIN DUCT HOT CAUTION. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE C/W Q400 FIM TASK 21-60-00-810-804 . NO CABIN DUCT HOT CAUTION MESSAGE NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007120700094 20071207 00094 NM 2007 12 7 F3LA200700324 1 20071113 A 5321 D5361076400000 SPLICE AIRBUS A319 A319111 3930336 NM FLOOR PANEL CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 221LF SPLICE PLATE CORRODED, AFT END. REPLACED AFT SPLICE PLATE ON FLOOR PANEL 221LF IAW AMM 53-12-12-PB401 AND WORK CARD CP753-12. 2 L 7 2 4F RT A28NM 2007120400177 20071204 00177 WP 2007 12 4 ABXA070376 1 20071111 A 5310 99578608 ANGLE DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 DURING COCKPIT WINDSHIELD FRAME MOD, FOUND RIGHT ANGLE CRACKED AT AFT END. REPLACED ANGLE IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 2007120400181 20071204 00181 EA 2007 12 4 CHQA200700083 1 20071125 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE T/E FLAP BINDING A CHQA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 GL 11 645BR 1882 7383 GEE872681 IAH TO AMA - DURING APPROACH TO AMA, THE FLAPS FAILED AT ZERO DEGREES WHEN SELECTED TO 8 DEGREES. ATC WAS NOTIFIED AND THE QRH WAS FOLLOWED. THE AIRCRAFT LANDED WITHOUT INCIDENT AND WAS INSPECTED BY EMERGENCY PERSONNEL BEFORE TAXING TO TH E GATE. MAINTENANCE WAS ABLE TO DUPLICATE THE FLAP FAIL ON THE GROUND. MAINTENANCE TROUBLESHOT THE FLAP SYSTEM AND DUR ING THE COURSE OF TROUBLESHOOTING, THE FLAP POWER DRIVE UNIT, FLAP ELECTRONIC CONTROL UNIT, AND THE FLAP LEVER WERE REPL ACED, ALL NO FIX. THE RIGHT INBOARD FLAP ACTUATOR WAS FOUND TO BE BINDING WHEN MAINTENANCE WAS RE-RIGGING THE FLAP SYST EM. THE RIGHT INBOARD FLAP ACTUATOR WAS REPLACED AND THE FLAP SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2007120400183 20071204 00183 NM 2007 12 4 USAA920071213 1 20071126 A 5330 6545766 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 PHX - CRACKED FUSELAGE SKIN, BS 500A, S10R. REPAIRED FUSELAGE SKIN, BS 500A - BS 500B, S10R IAW B737 SRM 53-00-01. 2 L 7 2 4F RT A16WE 2007120400184 20071204 00184 NM 2007 12 4 USAA920071214 1 20071125 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS 727E, S8L - S9L. REPAIRED FRAME, BS 727E, S8L - S9L IAW USAIRWAYS TYP ICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2007120400193 20071204 00193 EU 2007 12 4 USAA920071223 1 20071121 A 5347 D53112092205 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 625AW 64 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON SEAT TRACK, BS 808/FR 20, -Y765. REPLACED SEAT TRACK, BS 808/FR 20, -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007120400203 20071204 00203 WP 2007 12 4 07FDEA04931 1 20071126 A 5347 S4929405 SEAT TRACK DOUG MD10 MD1010F 3022112 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 MAIN CABIN FLOOR TRACK SCALLOP BROKEN OUT AT STA 792 LBL 49. CHECK LIMITS AND IS OUT OF LIMITS IAW DC/MD10-10 SRM 53-7 0-00 VOL I PG 21. REMOVED SEAT TRACK IAW DC/MD10-10 SRM 51-31-01 VOL II PG 1. FABRICATED SPLICE PLATE AND SPLICE HAT IAW DC/MD10-10 SRM 53-70-00 PG 4 FIG 1 VOL I. DRILLED NEW SEAT TRACK IAW DC/MD10-10 51-31-01 VOL II PG 1. INSTAL LED SEAT TRACK, SPLICE PLATE AND SPLICE HAT IAW DC/MD10-10 SRM 51-31-01 VOL II PG 1. REPAIR CLASSIFIED AS MAJOR REPAIR . 2 L 7 3 4F RT A22WE 2007120400214 20071204 00214 CE 2007 12 4 DXTA200702589 1 20071102 A 3222 STRUT BEECH MU300 400A 1155402 CE NLG LOW E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 138QS RK492 AFTER GEAR RETRACTION, RED IN TRANSIT LIGHT REMAINED ILLUMINATED. JACKED ACFT, REMOVED LT HYDRAULIC PUMP & INSTALLED ON HYDRAULIC POWER UNIT. CYCLED GEAR 30 TIMES WITH NO FAILURES NOTED. ACCESSED CONNECTORS P271 & P272 IN LT & RT GEAR WELL S. OHMED OUT UPLOCK SWITCHED & DOOR SWITCHES NO DEFECTS WERE NOTED. REINSTALLED ALL PREVIOUSLY REMOVED CONNECTORS AND PA NELS. ACCESSED PCB A162 AND CHECKED CONNECTOR P162 FOR LOOSE OR DAMAGED PINS NO DEFECTS WERE NOTED. ACCESSED RELAY K1 ON PCB A162 & OHMED OUT RELAY CONTACTS NO DEFECTS WERE NOTED. REINSTALLED PCB A162 AND CONNECTOR, ACCOMPLISHED MAIN GEAR L UBRICATION PER 400XP MM 12-20-00. ACCOMPLISHED 25 GEAR SWINGS WITH NO DEFECTS NOTED. REMOVED LT HYDRAULIC PUMP FROM HYDR 2 H 7 2 4F RT A16SW 2007120400232 20071204 00232 EA 2007 12 4 SWIA200718892 1 20071125 A 2131 21197688 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA CABIN PRESSURE MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 459SW 7782 FLT 3757 - CLIMBING-OUT OF 11,000 FEET, CABIN WOULD NOT PRESSURIZE. RETURNED TO SLC. REPLACED CABIN PRESSURE CONTROLLE R IAW CRJ 200 MM 21-31-16. 2 L 7 2 4F RT A21EA 2007120400237 20071204 00237 CE 2007 12 4 DJFA2007127 1 20071008 A 5512 SKIN BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CORRODED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 746TA 8170 RK146 DURING A SCHEDULED MAINTENANCE INSPECTION, TECHNICIANS FOUND MODERATE CORROSION ON BOTH HORIZONTAL STABILIZER LEADING ED GES. CORROSION WAS BEYOND REPAIRABLE LIMITS. BOTH LEADING EDGES WERE REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007120400238 20071204 00238 SO 2007 12 4 SWIA200718895 1 20071122 A 2611 SMOKE DETECTOR EMB 120 EMB120ER 3260203 SO LAVATORY ACTIVATED A SWIA O OTHER J WARNING INDICATION UK UNKNOWN 1 NM 07 218SW 120287 FLT 5541 - LAV SMOKE DETECTOR SOUNDED WHEN APU WAS STARTED. OPERATED BOTH PACKS WITH NO DEFECTS NOTED. 2 L 7 2 4T RT A31SO 2007120400239 20071204 00239 CE 2007 12 4 AMWA88479BC 1 20071108 A 2432 10136457217 CIRCUIT BOARD BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA BATTERY CHARGER INOPERATIVE A AMWA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 146ZV 7724 4355 UE146 DURING FLIGHT BATTERY CHARGE ANNUNCIATOR ILLUMINATED. MAINTENANCE REPLACED A-130 PC BOARD AND CLEARED DISCREPANCY. 2 L 7 2 4T 3 T RT A24CE E2NE 2007120400249 20071204 00249 CE 2007 12 4 DXTA200702607 1 20071111 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 351QS 5600451 CAPTAIN'S BRAKES ON TAXI OUT WERE EXTREMELY SPONGY. BLED BOTH CO-PILOTS & PILOTS BRAKES IAW CE-560 ULTRA AMM CHAPTER 3 2-40-00, TAXIED AIRCRAFT AND BRAKES OPS CHECKED GOOD ON BOTH PILOTS & COPILOTS SIDE. 2 L 7 2 4F 4 F RT A22CE E25EA 2007120400265 20071204 00265 EU 2007 12 4 TRBA2007097 1 20071112 A 3350 3011210 LIGHT AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW124B NE CABIN BURNED OUT A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 288AM 288 PASSENGER ENTRY STAIRS EMERGENCY LIGHT OUT. REMOVED AND REPLACED PAX/CREW DOOR EMERGENCY LIGHT IAW JIC 33-51-25. PERFO RMED OPT CHK FOUND WORKING PROPERLY AT THIS TIME. 2 H 7 2 4T 4 T RT A53EU E2ONE 2007120400273 20071204 00273 2007 12 4 01 4 20070516 A 3418 SLZ7695 COMPUTER CESSNA 500 S550 2076607 CE STALL WARNING DEFECTIVE E T17A O OTHER J WARNING INDICATION CL CLIMB 1 GL 17 408CT 6392 S5500055 STICK SHAKER DID NOT ACTIVATE WHEN DOING STALL RECOGNITION/RECOVERY TRAINING. 1 L 7 2 4F RT A22CE 2007120400274 20071204 00274 2007 12 4 COEA0720908 4 20071120 A 3497 1312321 CONNECTOR AEROSP ATR42 ATR42300 8680920 EU RADAR ALTIMETER DEFECTIVE A COEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 13 908FX 023 AIR TURN BACK, FLT 8788 - ON CLIMB-OUT AT CPR, THE CREW RECEIVED MULTIPLE RADAR ALTIMETER WARNINGS AS WELL AS GROUND PRO XIMITY WARNING SYSTEM AND TERRAIN AHEAD WARNING SYSTEM ERRORS. PILOT ELECTED TO RETURN TO CPR. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE COAX CABLE CONNECTOR TO THE TRANSMISSION ANTENNA. (M) 2 H 7 2 4T RT A53EU 2007120400275 20071204 00275 EA 2007 12 4 A6WA200740628 1 20071116 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING SCRATCHED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 470ZW 7927 SCRATCH ON LT WING UPPER PLANK AT WS 162-49. (M) SCRATCH REWORKED IAW REO 601R-57-21-887. (K) 2 L 7 2 4F RT A21EA 2007120400276 20071204 00276 EA 2007 12 4 A6WA200740629 1 20071116 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 470ZW 7927 FOUND PAX DOOR AFT DRAG ANGLE CRACK, LENGTH 1 INCH. (M) PAX DOOR AFT DRAG ANGLE REPAIRED IAW REO 601R-52-11-513, REV A . (K) 2 L 7 2 4F RT A21EA 2007120400281 20071204 00281 EA 2007 12 4 A6WA200740635 1 20071116 A 5260 HINGE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 427ZW 7685 FOUND PAX DOOR FOLDING STEP (UPPER) HINGE CORRODED. PAX DOOR FOLDING STEP HINGE INSTALLED IAW SRM 51-41-00. (M) 2 L 7 2 4F RT A21EA 2007120400284 20071204 00284 CE 2007 12 4 DXTA200702611 1 20071113 A 2711 INDICATION SYS CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE TRIM SYS MALFUNCTIONED E DXTA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 GL 07 631QS 5605131 EXTREME FORWARD FORCE, ON YOKE, USED TO KEEP AIRCRAFT CONTROL ON TAKEOFF. FOUND TRIM POINTER MIS-INDEXED IN TRIM WHEEL . RE-INDEXED POINTER TO PROPER POSITION. ELEVATOR TRIM SYSTEM OPS CHECKS GOOD AT THIS TIME. WORK DONE IAW CE-560XL M/M 2 7-32-01 2 L 7 2 4F 4 F RT A22CE E00059EN 2007120400285 20071204 00285 EA 2007 12 4 A6WA200740624 1 20071114 A 5753 FITTING CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP GOUGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 470ZW 7927 FOUND RIGHT OUTBOARD FLAP ALIGNMENT FITTING GOUGE AT WS 170, WEAR DEPTH .060 INCH. OUT OF LIMIT IAW REO 601R-57-51-143. FLAP ALIGNMENT FITTING REPLACED IAW SRM 51-42-06 AND 51-42-20. OPS CHECK C/O IAW CRJ 200 AMM 27-54-00-710-801. (M) 2 L 7 2 4F RT A21EA 2007120400286 20071204 00286 CE 2007 12 4 111007N541CS 1 20071110 A 3241 99124894 VALVE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE ANTI SKID FAILED E Z5FA O OTHER G MULTIPLE FAILURE LD LANDING 1 EA 63 541CS 3085 5605521 AFTER LANDING LT BRAKE LOCKED UP AND THE LT TIRE BLEW. APPROXIMATLY 500 FEET LATOR THE RT BRAKE LOCKED UP WITH THE SAME RESULTS, A BLOWN RIGHT TIRE. AIRCRAFT SKIDDED TO A STOP. CREW EXTINGUISHED TIRE FIRES. BOTH WHEELS AND BRAKES GROUND DOWN. AIRCRAFT CURRENTLY IN MAINTENANCE, WILL FOLLOW-UP WITH FINAL REPAIR. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007120400294 20071204 00294 CE 2007 12 4 102207N338CS1 1 20071022 A 5311 65111312 FRAME CESSNA 500 550 2076604 CE PWA 530 PW530A NE BS 263 CRACKED E Z5FA K NONE O OTHER IN INSP/MAINT 1 EA 63 338CS 3108 5501084 FUSELAGE FRAME CRACKED AT FS 263.4 -- LBL 15.35 TO RBL 15.35. FRAME P/N 6511131-2. NOTE: FIVE OTHER AIRCRAFT IN FLEET CHECKED AND FOUR HAD CRACKS AT THE SAME LOCATION. THIS SDR IS A REVISION TO SDR 102207N338CS 1 L 7 2 4F 4 F A22CE E00053EN 2007120400295 20071204 00295 SO 2007 12 4 SIMA200733205 1 20071125 A 3412 102AU1AF SENSOR EMB 135 EMB135KL 3260302 SO NR 1 TAT INOPERATIVE A SIMA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 21 853AE 145742 TAT 1 HEAT INOP AFTER TAKEOFF. REMOVED AND REPLACED NR 1 TAT SENSOR IAW EMB 140 AMM 34-45-03. OPS CK GOOD AT THIS TIME . AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007120400296 20071204 00296 CE 2007 12 4 102207N338CS2 1 20071022 A 5311 65111362 FRAME CESSNA 500 550 2076604 CE PWA 530 PW530A NE BS 275 CRACKED E Z5FA K NONE O OTHER IN INSP/MAINT 1 EA 63 338CS 3108 5501084 FUSELAGE FRAME CRACKED AT FS 275.6, LBL 15.35 AND RBL 15.35. FRAME P/N 6511136-2. NOTE: FIVE OTHER AIRCRAFT IN FLEET C HECKED AND FOR HAD CRACKS AT THE SAME LOCATION. THIS SDR IS A REVISION TO SDR 102207N338CS. 1 L 7 2 4F 4 F A22CE E00053EN 2007120400305 20071204 00305 SO 2007 12 4 SIMA200733206 1 20071125 A 3020 C1460094 ANTI-ICE VALVE EMB 135 EMB135KL 3260302 SO ANTI-ICE SYSTEM FAULTY A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 836AE 145635 ON T/O ROLL GOT E2 A/ICE FAIL MESSAGE. ABORTED TAKEOFF SPEED BELOW 100KTS APU WAS OFF T/O THRUST WAS 84. 2N1 MESSAGE DI SAPPEARED AFTERWARDS TO IDLE. REMOVED AND REPLACED ANTI-ICE VALVE IAW MM 30-21-01 AND REMOVED AND REPLACED DELIVERY TUB E IAW AMM 36-11-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007120400314 20071204 00314 EU 2007 12 4 BAQA200700038 1 20071113 A 6210 709010301109 BLADE AGUSTA A109 A109E 0260119 EU PWC PW206C PW206C NE MAIN ROTOR SEPARATED E BAQA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 EA 03 1UW 4109 529 11034 DURING NORMAL FLIGHT PILOT EXPERIENCED ABNORMAL VIBRATIONS. THE PILOT INITIATED AN EMERGENCY LANDING AND LANDED WITH THE GEARS UP IN A FIELD. MAINTENANCE PERSONNEL INSPECTED THE AIRCRAFT AND FOUND THE TIP CAP UPPER SKIN ON MAIN ROTOR BLADE P/N 709-0103-01-109 S/N A5-1641 SEPARATED FROM THE LEADING EDGE TO THE TRAILING EDGE. THE AIRCRAFT WILL BE TRANSPORTED T O MFG FIELD ON A FLAT BED TRUCK. 1 G 7 2 3U 3 U RT H7EU E42NE 2007120400325 20071204 00325 NE 2007 12 4 ASMF200711003 2 20071112 A 7230 815431 BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE LT COMPRESSOR DAMAGED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 501AM 49188 709834 DURING TRANSIT CHECK, FIVE BLADES WERE DETECTED DAMAGED DUE TO A FOD IN LT ENGINE. (4) BLADES WERE DETECTED WITH NICKS O N BLADES LEADING EDGE AND WERE REWORKED IAW MM 72-33-21 BEING WITHIN LIMITS. ONE BLADE WAS DETECTED WITH DENT WITH DEPTH OF 0.135 INCHES AND 5 INCHES FROM BLADE LEADING EDGE TO BLADE ROOT AND WAS REWORKED IAW MM 72-33-21 PARAGRAPH B-3B, CON DITIONED TO 24 FLIGHT HOURS. A BOROSCOPE INSPECTION TO 6TH AND 7TH STAGE COMPRESSOR WERE PERFORMED IAW MM 72-00-00, PAGE 635, NO DAMAGES WERE FOUND. (2) BLADES SETS OF FAN STAGE WERE REPLACED IAW MM 72-33-21 AND LT ENGINE WAS TESTED IAW 71 -00-00, ALL CORRECT. 2 L 7 2 4F 4 F A6WE E9NE 2007120400329 20071204 00329 WP 2007 12 4 BKAA200710004 2 20071115 A 7261 8960621 OIL TANK MTSBSI MU2 MU2B35 5780411 CE GARRTT TPE331 TPE331* 01514 WP ENGINE CRACKED E BKAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 13 21JA 614 P20176C OIL TANK CRACKED. 1 H 7 2 3T 3 T RT A10SW E2WE 2007120400338 20071204 00338 2007 12 4 717311162007 4 20071116 A 2211 7004206901 COMPUTER BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101650B1 41560 NE CSAS FAILED E QMLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 155SC 7173 DURING FLIGHT, YAW CSAS CAUTION LIGHT ILLUMINATED. DIVERTED LANDING FROM HELIPAD TO AIRPORT 4 MILES AWAY. COMPLETED APPR OPRIATE EMERGENCY PROCEDURE IAW AFM. 1 G 7 2 3U 3 U H13EU E5NE 2007120400349 20071204 00349 SO 2007 12 4 RAIA00711015 1 20071123 A 2913 971808 PUMP EMB 145 EMB145 3260210 SO HYDRAULIC SYS MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 801HK 9682 9682 145053 FLT NR 3514 - PIT - NR 2 HYDRAULIC SYSTEM FAILED. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYDRAULIC PUMP, O PS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007120400356 20071204 00356 NM 2007 12 4 SWAA075949 1 20071202 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007120500001 20071205 00001 NM 2007 12 5 DXTA200702617 1 20071118 A 3610 WARNING LIGHT GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE RT BLEED ILLUMINATED E DXTA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 07 706QS 131 PCECC0282 "RT BLEED AIR LEAK" WOULD NOT EXTINGUISH INFLIGHT AND RT ENGINE SHUTDOWN INFLIGHT. "RT BLEED AIR LEAK" MESSAGE REMAINED ON AFTER ENGINE SHUTDOWN. R & R RT FWD & AFT LEAK DETECTION ELEMENTS IAW MM 21-61-60. OPS CHECKED SATISFACTORY. 2 L 7 2 4F 4 F RT A53NM E35NE 2007120500009 20071205 00009 NE 2007 12 5 AMTA200700585 2 20071105 A 7250 3360261010 PLUG BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE ENGINE MISSING A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 310TZ 28243 FOUND THE S16 HIGH PRESSURE TURBINE BORESCOPE PLUG NOT INSTALLED. REINSTALLED NEW PN 336-026-101-0 PLUG (S16) IAW MM 72 -00-00 AND W/C 342I7202. OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A16WE E2GL 2007120500032 20071205 00032 CE 2007 12 5 DXTA200702621 1 20071120 A 3297 CONNECTOR CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE MLG DOWNLOCK DIRTY E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 809QS 5600698 LT MAIN MOUNT DID NOT LOCK DOWN WITH OTHER GEAR. GREEN LIGHT STAYED OFF AND RED UNSAFE INDICATOR LIGHT ILLUMINATED FOR 1 5+ SECONDS. JACKED A/C PERFORMED GEAR SWING IAW CE560E M/M 32-01-00. LANDING GEAR HYD SYSTEM ADJ/TEST. GEAR SWING OPS CHECKED GOOD. SUSPECTED MOISTURE IN GEAR DOWN LOCK SWITCH. CLEANED DOWN LOCK SWITCH CONNECTOR PER CESSNA TECH REP. GEAR TRAVEL TIMES WITHIN LIMITS. 5 SECONDS AND 4 SECONDS EXTEND. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A22CE E00053EN 2007120500059 20071205 00059 CE 2007 12 5 290ASEAS1 1 20071121 A 5610 101384002523 WINDSHIELD BEECH B300 B300 1159232 CE PWA PT6 PT6* 52043 EA COCKPIT CRACKED E E07A A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 CE 07 290AS FL296 LT WINDSHIELD INNER PANE CRACKED. 2 L 7 2 4T 3 T RT A24CE E2NE 2007120500073 20071205 00073 CE 2007 12 5 DXTA200702626 1 20071121 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA 545 PW545A NE MLG WEAK E DXTA O OTHER O OTHER LD LANDING 1 GL 07 351QS 5600451 CAPTAIN'S SIDE BRAKE PEDALS ARE SOFT, SPONGY, AND REQUIRE ABNORMAL AMOUNT OF TRAVEL FOR BRAKING. BLED BRAKES AND PRESS URIZED BRAKES SYSTEM IAW MM 32-42-00, BRAKES FELT FIRM, AND NO LEAKS NOTED AT THIS TIME. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007120500076 20071205 00076 2007 12 5 HEER118264 4 20071125 A 3160 C19267VG11 DISPLAY UROCOP EC135 EC135P2 5620027 EU FAULTY B HEER O OTHER O OTHER NR NOT REPORTED 1 SW 03 325PH 16 0576 PILOT ND SMD45 INDICATED FAULT DURING BIT TEST, ALTERNATING F WITH T. REPLACED DISPLAY. FUNCTION CHECKED GOOD. 1 G 7 2 3U H88EU 2007120500078 20071205 00078 CE 2007 12 5 DJFA2007137 1 20071123 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORISONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 750TA RK226 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. MAINTENANCE REPLACED BOTH RIBS WITH THE NEW IMPROVED ASSEMBLY. RIGHT SIDE REPLACED TO A VOID FUTURE CRACKS. 2 H 7 2 4F 4 F RT A16SW E25EA 2007120500093 20071205 00093 CE 2007 12 5 DJFA2007135 1 20071118 A 2433 UC2814 CONVERTER BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE DC FAILED E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 23 454LX RK327 AFTER LANDING CREW REPORTED BURNING ODOR COMING FROM AREA AROUND PAX TABLE. MAINTENANCE FOUND THE DC TO DC CONVERTOR FA ILED. THE COMPONENT WAS REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007120500094 20071205 00094 CE 2007 12 5 DJFA2007136 1 20071119 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 709TA 7759 RK180 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER IB RIB AND BRACKET ASSEMBLIES, THE RT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE O UTLINED IN COMMUNIQUE' NR 70. MAINTENANCE REPLACED THE RIB WITH IMPROVED PART. 2 H 7 2 4F 4 F RT A16SW E25EA 2007120500095 20071205 00095 EU 2007 12 5 TRBA2007102 1 20071119 A 5610 NP1588014 WINDSHIELD AEROSP ATR72 ATR72212 8680945 EU COCKPIT CRACKED A TRBA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 29 447AM 447 F/O WINDSHIELD CRACKED IN FLIGHT AT CRUISE. ORIGINAL FLIGHT SJU-EIS, DIVERTED TO STT. REMOVED AND REPLACED RH WINDSHIE LD IAW JIC 53-11-10. PERFORMED OPERATIONAL AND LEAK CHECK AND FOUND SATISFACTORY. 2 H 7 2 4T RT A53EU 2007120600003 20071206 00003 NM 2007 12 6 DHLA200700069 1 20071127 A 3350 BATTERY BOEING 727 727223 1384074 NM EMERGENCY LIGHTS INOPERATIVE A DHLA O OTHER O OTHER NR NOT REPORTED 1 GL 05 753DH 22468 FWD ENTRY DOOR ESCAPE SLIDE LIGHT REMAINS ILLUMINATED. DEFERRED IAW MEL 33-16-2A CAT-B PLACARD INSTALLED. REMOVED AND REPLACED BATTERY ASSY OPS CHECK GOOD IAW MM 33-50-01 THIS CLEARS DMI 30900 PLACARD REMOVED PN 60-1321-1 2 L 7 3 4F A3WE 2007120700001 20071207 00001 2007 12 7 754004 4 20071127 A 2211 2590623907 COMPUTER BOEING 747 747228F 1384895 NM AUTO PILOT NO TEST A Q2SA J A DUMP FUEL UNSCHED LANDING F G FLT CONT AFFECTED MULTIPLE FAILURE CR CRUISE 1 EA 63 754SA 21576 AUTOPILOT A WILL NOT ENGAGE AND AUTOPILOT B IS ALREADY DEFERRED. DUMPED FUEL AND DIVERTED INTO RKSI. AUTOPILOT A ROLL COMPUTER DOES NOT PASS SELF TEST. REPLACED AUTOPILOT A ROLL COMPUTER AND AUTOPILOT B MONITOR LOGIC UNIT. 2 L 7 4 4F RT A20WE 2007120700007 20071207 00007 NM 2007 12 7 DL76S071519 1 20071119 A 5330 143T351112 SKIN BOEING 767 767332 1382001 NM FS 650 S21R GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 121DE 23435 SKIN GOUGE AT FS 650 AND STR 21R. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F RT A1NM 2007120700010 20071207 00010 NM 2007 12 7 DLM90071522 1 20071116 A 5753 5930496507 VANE DOUG MD90 MD9030 3023690 NM TE FLAPS DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 LT WING O/B FLAP I/B VANE WAS A DENT IN L/E BETWEEN NR 2 AND NR 3 SUPPORTS. INSTALLED METAL BOND REPAIR DOUBLER IAW MD- 90 SRM 51-10-02D PARA 17 PAGE 84 ON N/R 5400-0003 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007120700011 20071207 00011 NM 2007 12 7 DLM90071523 1 20071116 A 5753 5930496507 VANE DOUG MD90 MD9030 3023690 NM LT TE FLAP DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 LT O/B FLAP I/B VANE DENTED ON TOP O/B END. INSTALLED BONDED REPAIR DOUBLER IAW MD-90 SRM 51-10-02D PARA 17 P84 ON N/R 5400-0077 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007120700012 20071207 00012 NM 2007 12 7 DLM90071524 1 20071116 A 5753 5930496507 VANE DOUG MD90 MD9030 3023690 NM TE FLAP GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 LT O/B FLAP VANE GOUGED ON TOP SIDE I/B END. INSTALLED HOT BOND REPAIR DOUBLER IAW MD-90 SRM 51-10-02D PARA 17 PG 83 ON N/R 5400-0076 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007120700013 20071207 00013 NM 2007 12 7 DLM90071525 1 20071119 A 5322 SHEAR TIE DOUG MD90 MD9030 3023690 NM FS 1344 26L-28R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 AFT PIT SHEAR TIE CORRODED AT FS 1344 BETWEEN LONGERONS 27R-29L. REPAIRED AFT PIT SHEAR TIE AT STA 1344 BETWEEN LG 26L AND 28R IAW MD-90 SRM 53-10-02D FIG 3 ON N/R 1600-0204 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007120700020 20071207 00020 NM 2007 12 7 DL76L071533 1 20071121 A 2750 MODULE 7321870015 BOEING 767 767332 1382001 NM TE FLAPS/SLATS FAILED A DALA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 185DN 12470 27961 TE FLAP DISAGREE MESSAGE WHEN FLAPS SELECTED FROM 1 TO 5 POSITION. REPLACED FLAP/SLAT SOV MODULE PER MM. 2 L 7 2 4F RT A1NM 2007120700024 20071207 00024 NM 2007 12 7 DLM88071540 1 20071103 A 5320 ANGLE DOUG MD88 MD88 3023688 NM BS 1003 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 CRACK ON ANGLE AT STA Y=1003 BTWN X=7 AND X=-7 KEEL BEAM AREA. REPLACED ANGLE PER DWG 5936395 AND SRM 51-30-1/51-30-2/5 1-30-5. 2 L 7 2 4F RT A6WE 2007120700027 20071207 00027 2007 12 7 DLM88071543 4 20071015 A 2565 SUPPORT DOUG MD88 MD88 3023688 NM R1 DOOR SLIDE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 CORROSION ON FWD SLIDE SUPPORT AT R1, REPLACE SUPPORT PER SRM 51-30-1, 51-10-4. 2 L 7 2 4F RT A6WE 2007120700036 20071207 00036 NM 2007 12 7 DLM88071552 1 20071020 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 1041-1022 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 CORROSION ON LT CUSP WEB BETWEEN STA Y=1041 TO Y=1022. REPLACED SECTION OF WEB PER DWG 9930612. 2 L 7 2 4F RT A6WE 2007120700040 20071207 00040 NM 2007 12 7 DLM90071559 1 20071126 A 2420 1B1903A TRANSFORMER DOUG MD90 MD9030 3023690 NM RT GENERATOR INOPERATIVE A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 27 916DN 53396 INFLIGHT RT ENG GEN OFF AND RT AC PWR FAULT. RT ENG GEN TRANSFORMER UNIT INOP. REPLACED TRANSFORMER UNIT. 2 L 7 2 4F RT A6WE 2007120700045 20071207 00045 NM 2007 12 7 DL757071564 1 20071126 A 2910 LINE BOEING 757 757232 1384965 NM HYD SYS RUPTURED A DALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 633DL 23614 LT SYS HYD QUANITY MSG FOUND LEAK IN LEFT WW. INSPECTED AND FOUND LT ELEC HYD PUMP HAS RUPTURED HOSE. REMOVED AND REPL ACED RUPTURED HOSE. SERVICED AND LEAK CK IAW AMM12-12-01. NO LEAKS, NO DEFECTS NOTED. 2 L 7 2 4F RT A2NM 2007120700052 20071207 00052 NM 2007 12 7 C1HA200778002 1 20071126 A 2497 WIRE BOEING 727 727225 1384077 NM FUSELAGE CHAFED A C1HA H K DEACTIVATE SYST/CIRCUITS NONE B G M SMOKE/FUMES/ODORS/SPARKS MULTIPLE FAILURE OVER TEMP IN INSP/MAINT 1 GL 15 678MG 22555 WHILE WAITING FOR PASSENGER AIRCRAFT HAD SOME SORT OF POWER SURGE OR INTERRUPTION IN POWER. GASPER FAN CIRCUIT BREAKER POPPED, COOLING DOOR BREAKER POPPED, LEFT PACK FAN CIRCUIT BREAKER POPPED, LEFT DUCT OVERHEATED, FOLLOWED BY LEFT PACK T RIP. NR 1 GENERATOR SHOWED A FIELD RELAY TRIP, FAULTS SHOWED A "GROUND FAULT" ALL POWER WAS SHUTDOWN BATTERY TURNED OFF BY MECH SMOKE IN CABIN (SMELLED ELECTRICAL SMOKE). CREW WAS SENT OFF AIRCRAFT AND CFR WAS CALLED IN. REPORTED CHAFED WIRING AT THE J-4 ELECTRICAL JUNCTION BOX. REPLACED AFFECTED WIRING B727 WIRING MANUAL 91-01-03. SYSTEM OPS CHECK GOOD . 2 L 7 3 4F A3WE 2007120700055 20071207 00055 NM 2007 12 7 NWAA070385563 1 20071125 A 2910 O-RING BOEING 757 757251 1384970 NM HYD SYSTEM LEAKING A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 539US 26486 DURING FLIGHT THERE WAS A LEFT HYDRAULIC FAILURE LOSS OF FLUID FOLLOWED BY PRESSURE LOSS AFTER PTU FAILED. FLIGHT CONTI NUED ON TO NGO. EMERGENCY WAS DECLARED AND LANDING WAS UNEVENTFUL. RUNWAY WAS CLOSED FOR 20 MINUTES, A/C HAD TO BE TOW ED OFF OF RUNWAY. MAINTENANCE REMOVED AND REPLACED LEAKING O-RING. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007120700056 20071207 00056 NM 2007 12 7 F3LA200700323 1 20071114 A 5321 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 221FF. REMOVED AND REPLACED FLOOR PANEL 221FF IAW AMM 53-12-12-PB40 1, AMM 53-12-12-400-001, AND FRONTIER WORK CARD CP753-12. 2 L 7 2 4F RT A28NM 2007120700060 20071207 00060 NM 2007 12 7 AALA20072247 1 20071118 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 DFW - EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120700066 20071207 00066 NM 2007 12 7 AALA20072250 1 20071118 A 3397 P10400705001 WIRE HARNESS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 DFW - EMERGENCY LIGHT AT SEAT 3G INOPERATIVE. REPAIRED HARNESS FOR EMERGENCY LIGHT AT SEAT 3G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120700081 20071207 00081 EU 2007 12 7 07FDEA04950 1 20071127 A 5347 R5307008820200 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 671FE 778 MCC FR 72 SEAT TRACK 3R HAS CORROSION I PLACE. REMOVED AND REPLACED SEAT TRACK SECTION BETWEEN FR 71 TO FR 73 IAW A300- 600 SRM 53-10-16 AND 51-40-21. 2 L 7 2 4F RT A35EU 2007120700090 20071207 00090 NM 2007 12 7 07FDEA04959 1 20071128 A 5313 655848825 STRINGER BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 RT EXT FUSELAGE SKIN STRINGER IS CRACKED, BS 940-946, STR 18A R REMOVED DAMAGE SECTION OF STR 18A RT. DRILLED UP REPAIR ANGLES, RADIUS FILLERS AND AND SHIMS, AND NEW STR SECTION. INSTALLED ALL REPAIR PARTS AND INSTALLED W/B PLN NR 3118 AN D 3116. REF FED EX EA NR 7-5310-113120, SRM 51-30-02, BOEING DWG 65C29069. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2007120700091 20071207 00091 EU 2007 12 7 07FDEA04960 1 20071121 A 5610 NP1752014 WINDSHIELD AIRBUS 310 A310203 3930313 EU ZONE 200 FAILED A FDEA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 25 424FE 241 AT FL 360, IN THE CLEAR, F/O'S WINDSCREEN SHATTERED. HAD BRIGHT FLASH OUT OF LOWER RIGHT CORNER, SPARKING AND ARCING. ALSO HAD LOUD POPPING NOISE. TURNED OFF F/O WINDOW HEAT AND ARCING AND SPARKING STOPPED AFTER ABOUT ONE MINUTE. MADE E MERGENCY LANDING AT BUF. REMOVED AND REPLACED F/O'S WINDSCREEN PER M/M 56-11-11-4. ALSO, REPLACED F/O'S WINDSCREEN R EGULATOR AND CONTROLLER, CKS GOOD PER M/M 30-42-00-5. 2 L 7 2 4F RT A35EU 2007120700096 20071207 00096 NM 2007 12 7 NWAA073855639 1 20071125 A 2910 O-RING BOEING 757 757251 1384970 NM HYD SYSTEM LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 GL 01 539US 26486 DURING FLIGHT THERE WAS A LEFT HYDRAULIC FAILURE LOSS OF FLUID FOLLOWED BY PRESSURE LOSS AFTER PTU FAILED. FLIGHT CONTI NUED ON TO NGO. EMERGENCY WAS DECLARED AND LANDING WAS UNEVENTFUL, RUNWAY WAS CLOSED FOR 10 MINUTES, A/C HAD TO BE TOWE D OFF OF RUNWAY. MAINTENANCE REMOVED AND REPLACED A LEAKING O-RING. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007120700097 20071207 00097 NM 2007 12 7 DHLA200700071 1 20071129 A 2780 40174 POSITION SWITCH BOEING 727 727227 1384078 NM NR 5 LE FLAP FAILED A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 782DH 21998 DURING DEPARTURE AT 300 FEET AGL, LE FLAPS LIGHT WENT FROM GREEN TO YELLOW S/O CONFIRMED SLATE NR 5 YELLOW THEN LIGHT WE NT BACK TO GREEN ON BOTH FRONT AND SO PANEL. REMOVED AND REPLACED NR 5 L/E FLAP POSITION SWITCH IAW M/M 27-82-01, CK'S NORMAL. 2 L 7 3 4F A3WE 2007120700098 20071207 00098 NM 2007 12 7 QXEA200701767 1 20071128 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHTS INOPERATIVE A QXEA O OTHER O OTHER CL CLIMB 1 NM 09 353PH 23282 23282 496 PDX - ON FLIGHT 2139, EMERGENCY LIGHTS IN CABIN FLICKER AFTER TAKEOFF. TURNING OFF THEN ON, ARM STOPS THE FLICKERING. LIGHTS FLICKERING ARE THE EXIT SIGNS AND OVERHEAD. MAINTENANCE REMOVED AND REPLACED PS3 AND PS4 POWER SUPPLIES AND BATT ERY PACKS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007120700101 20071207 00101 NM 2007 12 7 QXEA200701769 1 20071128 A 2420 11522184 GENERATOR BOMBDR DHC8 DHC8402 1390042 NM NR 1 MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 403QX 13683 1711 4037 SEA/EUG FLIGHT NR 2333: NR 1 AC GEN CAUTION LIGHT CAME ON IN FLIGHT. COMPLIED WITH CHECKLIST, DID NOT RESET. FLIGHT DI VERTED TO PDX. MAINTENANCE REMOVED AND REPLACED NR 1 AC GEN IAW Q400 TASK CARD NR 6242101. PERFORMED LEAK CHECK. NO L EAKS NOTED. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007120700102 20071207 00102 WP 2007 12 7 IXXA070055O 1 20071129 A 5270 STRIKER DOUG DC8 DC871F 302199D WP MLG DOOR WORN A IXXA O OTHER N FALSE WARNING CL CLIMB 1 SW 11 829BX 92552 2879 45994 DURING CLIMB FROM KRFD TO KTOL, THE LANDING GEAR DOORS LIGHT REMAINED ILLUMINATED AFTER GEAR WAS RETRACTED. THE CREW CY CLED THE GEAR AND THE LIGHT REMAINED ON. THE CREW CONTINUED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE LEFT MAIN LANDING GEAR DOOR STRIKER, THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RE TURNED TO SERVICE IAW DC8 MM 32-12-1. 2 L 7 4 4F RT 4A25 2007120700103 20071207 00103 NM 2007 12 7 07FDEA04961 1 20071128 A 5330 146N35317 SKIN BOEING 757 7572B7 1384964 NM ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 LOWER FUSELAGE SKIN AT BS 1503, LBL 4 HAS A GOUGE NEXT TO RIVET. GOUGE MEASURED .017" DEEP IN .060 THICK SKIN. DAMAGE OUT OF LIMITS PER SRM 53-00-01, DETAIL II. UPON REMOVAL OF DAMAGED SKIN, FOUND CORROSION ON BOTTOM OF WEB. REMOVED AND REPLACED WEB IAW SRM 51-40-02. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-00-01, REPAIR NR 16. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-00-01, REPAIR NR 16, FIG 201. THIS IS A CATEGORY "B" MAJOR REPAIR REQUIRING REPEAT INSP ECTIONS IN 29,000 FLIGHT CYCLES PER SRM 53-00-01, REPAIR NR16, FIG 201, TABLE V. 2 L 7 2 4F RT A2NM 2007120700105 20071207 00105 WP 2007 12 7 07FDEA04963 1 20071129 A 5720 ARB22172 LUG DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 AT ACCESS 634 AT FOUND LOWER CHORD LUG CRACKED. REPAIRED AREA IAW EA NR 8-5710-111525A. 2 L 7 3 4F A22WE 2007120700106 20071207 00106 WP 2007 12 7 07FDEA04964 1 20071129 A 5720 ARB22171 LUG DOUG DC10 DC1010 3022110 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 FOUND LOWER CHORD LUG CRACKED. REPAIRED AREA IAW EA NR 8-5710-111524A. 2 L 7 3 4F A22WE 2007120700107 20071207 00107 WP 2007 12 7 07FDEA04965 1 20071129 A 5320 NCA604463 ANGLE DOUG DC10 DC1010 3022110 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 LOWER FWD COMPT CRACK ON TEE ANGLE. REPAIRED TEE CAP IAW EA NR 8-5310-111463. 2 L 7 3 4F A22WE 2007120700110 20071207 00110 NM 2007 12 7 HALA0700503 1 20071126 A 3241 42977 CONTROL UNIT BOEING 717 717200 1383700 NM ANTI SKID SYS MALFUNCTIONED A HALA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 WP 13 478HA 55123 ATB - AFTER GEAR EXTENSION IN LIH, R ANTI-SKID FAIL ILLUMINATED. DISPATCH ADVISE RTN HNL. UPON LANDING HNL ANTISKID FA IL LT REMAINED OFF. BRAKES NORMAL ON LANDING. BITE CHECK BCU PER FIM 32-45-00 FOUND BCU INTERNAL FAULT. REMOVED AND R EPLACED BCU PER AMM 32-45-01, ANTI-SKID RTS TEST PASSED. OK FOR SERVICE. 2 L 7 2 4F TR A6WE 2007120700112 20071207 00112 NE 2007 12 7 HALA0700507 2 20071128 A 7200 UNKNOWN BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE ENGINE UNKNOWN A HALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 13 581HA 28140 ETOPS SIGNIFICANT SYSTEM, LEFT AND RIGHT ENGINES ARE OUT OF SYNC DURING CLIMB AND DESCENT. RIGHT ENGINE IS 1 PERCENT HI GHER THAN LEFT ENGINE. PER HAL ENGINEERING PERF DATA ALL NORMAL ACCOMP BITE CK, NO DEFECTS NOTED. TELEX SVC TO GENERAT E TSI TO MONITOR. REQUEST FOR MORE CREW EVALUATIONS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007120700113 20071207 00113 NM 2007 12 7 HALA0700508 1 20071128 A 8011 S332T00117 STARTER BOEING 767 767300 1385204 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE LEAKING A HALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 582HA 28141 ETOPS SIGNIFICANT SYSTEM, DURING ENGINE MOTORING FOUND NR 1 ENG STARTER LEAKING. REPLACED NR 1 ENG STARTER ASSY IAW B76 7 AMM 80-11-01-004. OPS AND LEAK CHECKS NORMAL, STARTER SERVICED TO FULL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007120700116 20071207 00116 EU 2007 12 7 MALA070185 1 20071124 A 3020 INTAKE DUCT SAAB SF340 340B 7860101 EU LEFT BURNED A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 15 417XJ 340B417 AIR RETURN DUE TO A LT LOWER DUCT THAT BURNED AND HAD AN ODOR. REMOVED AND REPLACED IAW JCN NR 7160-301. RAN ENGINE 15 MINUTES, OPS CHECK GOOD, PN ON/OFF: NH24668-165; SN OFF: L169247; SN ON: L197714. 2 L 7 2 4T RT A52EU 2007120700117 20071207 00117 EU 2007 12 7 MALA070186 1 20071125 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU LAVATORY FALSE ACTIVATION A MALA O OTHER N FALSE WARNING DE DESCENT 1 GL 15 420XJ 340B420 INBOUND TO DTW, CREW RECEIVED A LAV SMOKE WARNING AND VERIFIED INDICATION ONLY. CLEANED AND OPS CHECKED GOOD. REMOVED S MOKE DETECTOR. INSPECTED SMOKE DETECTOR AND WIRING HARNESS. NO DEFECTS NOTED. REINSTALLED SMOKE DETECTOR IAW MAL AMM 26-13-10-04. OPS CHECK GOOD IAW MAL AMM 26-13-00. 2 L 7 2 4T RT A52EU 2007120700121 20071207 00121 NM 2007 12 7 DU4R2007188 1 20071128 A 5711 654532421 SPAR BOEING 737 737322 1384676 NM CRACKED B DALA K NONE O OTHER IN INSP/MAINT 1 SO 15 401TZ 24663 REPAIRED VERTICAL CRACK FROM HOLE C-DOWN TO EDGE OF CUT OUT OF LT REAR SPAR UPPER CHORD BY OVERSIZING HOLE, FABRICATING AND INSTALLING BUSHING IAW REO-L0152 REV IR DATED 11-21-07 FAA FORM 8100-9. THIS IS A TIME LIMITED REPAIR, REPEAT INSPE CTION REQUIRED AT 4500 AIRCRAFT CYCLES. 2 L 7 2 4F RT A16WE 2007120700124 20071207 00124 SO 2007 12 7 SIMA200733402 1 20071129 A 3350 66368 LIGHT EMB 135 EMB135KL 3260302 SO CABIN INOPERATIVE A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 815AE 145545 EMERGENCY LIGHTNING STRIP ON ROW 7/8 IS INOP. REMOVED AND REPLACED EMERGENCY FLOOR LIGHT STRIP BETWEEN SEAT RO 7/8 AND OPS CHECK GOOD IAW EMB 140 MM 33-50-12. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007120700126 20071207 00126 NM 2007 12 7 AMTA200700651 1 20071127 A 3411 RELAY BOEING 757 75723N 1384973 NM PITOT SYS MALFUNCTIONED A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 514AT 27971 AFTER ENGINE START, "CAPT PITOT" WARNING ON EICAS AND OVERHEAD ILLUMINATED. T/S PER FIM 30-31-00 FIG 103. REMOVED AND REPLACED K243 RELAY, RAN ENGINES, OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A2NM 2007120700128 20071207 00128 NM 2007 12 7 DHLA200700072 1 20071130 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 GL 05 749DH 22013 RE INSTALL EMERG EXIT LIGHT. REINSTALLED COCKPIT EMERGENCY LIGHT ASSY OVER DOOR PER MM 33-50-71, OPS CKS GOOD. 2 L 7 3 4F A3WE 2007120700130 20071207 00130 SO 2007 12 7 SWIA200718903 1 20071122 A 2150 A/C PACK EMB 120 EMB120ER 3260203 SO RIGHT SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 223SW 120291 FLT 5706 - RIGHT PACK FAIL LIGHT CAME ON INFLIGHT AND LAV SMOKE ALARM SOUNDED WITH ASSOCIATED SMELL OF SMOKE. RAN AIRCR AFT AND RIGHT PACK ON BOTH ENGINE AND APU BLEEDS AND IN AUTO AND MANUAL MODES. NO DISCREPANCIES NOTED. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007120700131 20071207 00131 SO 2007 12 7 SWIA200718904 1 20071119 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 296SW 120325 FLT 3687 - FORWARD FLOOR EMERGENCY LIGHT SIGN BROKEN. REPLACED LIGHT ASSEMBLY. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007120700132 20071207 00132 SO 2007 12 7 SWIA200718905 1 20071124 A 3246 WHEEL EMB 120 EMB120ER 3260203 SO NR 2 BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 393SW 120330 FLT 5552 - DURING POST FLIGHT, NOTICED NR 2 MAIN WHEEL ASSEMBLY APPEARED TO BE BROKEN. REPLACED BOTH LEFT WHEEL ASSEMBL IES, PN 3-1446-1 SN OFF 0538PN 3-1446-1 SN OFF 777. 2 L 7 2 4T RT A31SO 2007120700133 20071207 00133 EA 2007 12 7 SWIA200718906 1 20070819 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 728SK 10192 STA 280 FLOORBEAM IS CRACKED AT LBL11, FOUND AT C-CHECK. REPLACED FS280 BEAM PER CRJ7/9 SRM 51-23-00. 2 L 7 2 4F RT A21EA 2007120700134 20071207 00134 EA 2007 12 7 SWIA200718907 1 20070819 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSLEAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 728SK 10192 AFT COCKPIT FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. INSTALLED NEW FLOOR SUPPORT PER CRJ7/9 SRM 51-42-06/51-23-00. 2 L 7 2 4F RT A21EA 2007120700136 20071207 00136 EU 2007 12 7 CPCP20070118 1 20071024 A 5320 CHANNEL AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 355AT 355 RT Z FLOOR FRAME 39-41 FOUND CORRODED. RT Z FLOORFRAME 39-41 REPLACED IAW SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007120700139 20071207 00139 NM 2007 12 7 F3LA200700325 1 20071126 A 5751 ATTACH BOLT AIRBUS A319 A319111 3930336 NM AILERON CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED RT AILERON NR 3 HINGE SUPPORT FRAME ATTACHMENT BOLTS (ATTACHES TO BRACKET ON WIN G) WORN AND CORRODED. REPLACED RT AILERON NR 3 HINGE SUPPORT BRACKET MOUNTING BOLTS IAW AMM 57-51-31-400-0001. 2 L 7 2 4F RT A28NM 2007120700140 20071207 00140 EU 2007 12 7 CPCP2007120 1 20071024 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 355AT 355 RT SEAT TRACK FRAME 39-40 CORRODED AROUND NUTPLATE HOLES. RT SEAT TRACK FRAME 39-40 REPLACED IAW SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007120700143 20071207 00143 NM 2007 12 7 F3LA200700327 1 20071114 A 5320 SILL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON L2 DOOR SILL AT AFT INBD END AT NUT PLATE HOLES, APPROX 1-4 INCHES FWD OF FR 68. DETERMINED DAMAGE TO BE OUT OF LIMITS IAW SRM 53-41-14. REMOVED AND REPLACED L2 DOOR SILL IAW SRM 52-42- 11. 2 L 7 2 4F RT A28NM 2007120700147 20071207 00147 WP 2007 12 7 UPS07851227 1 20071129 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA O OTHER O OTHER CR CRUISE 1 SO 01 840UP 46140 AT CRUISE, THE DOME LIGHT AND PEANUT LIGHTS CAME ON BY THEMSELVES NO SWITCHES WERE THROWN, NO ABNORMAL INDICATIONS OF F/ E PANEL WHEN WENT TO DC TIE WITH THE FREQ SELECTOR, THE LIGHTS WENT OUT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY P ACK IAW MM 33-50-01-2. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2007120700150 20071207 00150 NM 2007 12 7 UPS07M51226 1 20071129 A 5320 SPRING DOUG MD11 MD11F 3023600 NM CEILING PANEL BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 256UP 48405 L1 DOOR UPPER SLIDING CEILING PANEL RETRACTION SPRING BROKEN. EMERGENCY EXIT SIGN INTERFERES WITH DOOR. A/C FERRIED TO SDF NR 9048 FOR REPAIR REPLACED RETRACTION SPRING PER MM 52-11-08-4. L1 DOOR OPS CHECKS NORMAL PER MM 52-10-01-2. 2 L 7 3 4F RT A22WE 2007120700153 20071207 00153 NM 2007 12 7 USAA920071225 1 20071127 A 5330 6545774 SKIN BOEING 737 737401 1384701 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 CLT - MAJOR REPAIR - CRACKED FUSELAGE SKIN, BS 727D, S23R. REPAIRED FUSELAGE SKIN, BS 727D, S23R IAW USAIRWAYS TYPICAL REPAIR 53-60-03A. 2 L 7 2 4F RT A16WE 2007120700154 20071207 00154 NM 2007 12 7 USAA920071229 1 20071121 A 5720 69520145 STIFFENER BOEING 737 7373B7 1384580 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED CENTER WING REAR SPAR VERTICAL STIFFENER, BS 663.75, RBL 6.15, WL 176, IN RIGHT MAIN LANDING GEAR WHEEL. REPAIRED CENTER WING REAR SPAR VERTICAL STIFFENER, BS 663.75, RBL 6.15, WL 176, IN RIGHT MAIN LANDING GEAR WHEEL IAW USAIRWAYS TYPICAL REPAIR 57-10-03B 2 L 7 2 4F RT A16WE 2007120700157 20071207 00157 NM 2007 12 7 USAA920071232 1 20071130 A 5315 6545812 FLOORBEAM BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CRACKED CABIN FLOOR STRUCTURE ANGLE, BS 328, LBL 30. REPLACED CABIN FLOOR STRUCTURE, BS 328, LBL 30 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007120700158 20071207 00158 NM 2007 12 7 USAA920071233 1 20071130 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CRACKED STRINGER CLIP, BS 727E, S4L. REPLACED STRINGER CLIP, BS 727E, S4L IAW B737 SRM 51-20-02. 2 L 7 2 4F RT A16WE 2007120700159 20071207 00159 NM 2007 12 7 USAA920071234 1 20071117 A 5340 6545807U30 ATTACH ANGLE BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CRACKED INTERCOSTAL ATTACH ANGLE, BS 289, S12R - S13R. REPLACED INTERCOSTAL ATTACH ANGL E, BS 289, S12R - S13R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007120700160 20071207 00160 NM 2007 12 7 USAA920071235 1 20071118 A 5311 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS 807, S8L - S9L. REPAIRED FRAME, BS 807, S8L - S9L IAW USAIRWAYS EA 100 048 AND TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2007120700162 20071207 00162 NM 2007 12 7 USAA920071237 1 20071127 A 5340 6916970 ATTACH FITTING BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CRACKED CLIP ANGLE, BS 344, S15L. REPLACED CLIP ANGLE, BS 344, S15L I/A/W BOEING DRAWING 69-16970. 2 L 7 2 4F RT A16WE 2007120700163 20071207 00163 NM 2007 12 7 USAA920071238 1 20071127 A 5315 65528941 FLOORBEAM BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CRACKED FLOOR SUPPORT, BS 540, BL 0 - LBL 24. REPLACED FLOOR SUPPORT, BS 540, BL 0 - LB L 24 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007120700164 20071207 00164 NM 2007 12 7 USAA920071239 1 20071127 A 5340 6935350 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C16 CHECK, CRACKED STRINGER CLIP, BS 500A, S16R. REPLACED CRACKED STRINGER CLIP, BS 500A, S16R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007120700165 20071207 00165 NM 2007 12 7 USAA920071240 1 20071123 A 5311 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C16 CHECK, CRACKED FRAME, BS 847, S8L - S9L. REPAIRED FRAME, BS 847, S8L - S9L IAW USAIRWAYS EA 10 0048 AND TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2007120700170 20071207 00170 NM 2007 12 7 USAA920071245 1 20071116 A 5340 6935352U14 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C16 CHECK, CRACKED STRINGER CLIP, BS 616, S4R. REPLACED STRINGER CLIP, BS 616, S4R IAW B737 SRM 51 -40-02. 2 L 7 2 4F RT A16WE 2007120700172 20071207 00172 NM 2007 12 7 USAA920071247 1 20071129 A 5340 6545807 ATTACH ANGLE BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CRACKED ATTACH ANGLE, BS 289, S12R - S13R. REPLACED ATTACH ANGLE, BS 289, S12R - S13R I AW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007120700173 20071207 00173 NM 2007 12 7 F3LA200700333 1 20071114 A 5315 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM NUTPLATE HOLES AT +Y1292 (LT), 4 INCHES FWD OF FR68-69. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM'S 51-74-00, 51-42-11, 53-00-14, 51-44-11, 51-75-12 AND EA A9-53R-12267 (STEP S 1 AND 2). 2 L 7 2 4F RT A28NM 2007120700174 20071207 00174 NM 2007 12 7 F3LA200700334 1 20071114 A 5315 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSLEAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED MAIN CABIN FLOORBEAM AT FR16, +Y254, CORRODED. DETERMINED CORROSION TO BE OUT O F LIMITS IAW SRM 53-11-14. CUT OUT CORRODED AREAS, AND FABRICATED AND INSTALLED FILLER AND REPAIR ANGLES IAW SRM 53-11- 14 AND 51-75-12. 2 L 7 2 4F RT A28NM 2007120700175 20071207 00175 NM 2007 12 7 F3LA200700335 1 20071114 A 5320 D5311282600101 DUMMY RAIL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED MAIN CABIN FLOOR DUMMY RAIL AT +Y503.2 BETWEEN FR 12 AND 16 CORRODED. REMOVED A ND INSTALLED CORRODED DUMMY RAIL IAW SRM 51-42-11, 51-44-11 AND DWG D531 12825. 2 L 7 2 4F RT A28NM 2007120700176 20071207 00176 NM 2007 12 7 F3LA200700336 1 20071114 A 5320 D5347112420000 SHEAR PLATE AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED LT AFT SHEAR PLATE CORRODED AT FR 69-70 AT BEAM +1732 (APPROX). REMOVED AND INS TALLED LT AFT SHEAR PLATE IAW SRM'S 51-72-11 AND 51-42-11. 2 L 7 2 4F RT A28NM 2007120700177 20071207 00177 NM 2007 12 7 AALA20072292 1 20071125 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 770AN 29578 DFW - EMERGENCY LIGHT AT LEFT WALL AFT GALLEY MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LEFT WALL AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120700178 20071207 00178 NM 2007 12 7 AALA20072284 1 20071124 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 ORD - EMERGENCY LIGHT AT RIGHT OVERHEAD SEAT ROW 17 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT OVERHEAD SE AT ROW 17. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007120700179 20071207 00179 NM 2007 12 7 AALA20072293 1 20071125 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 193AN 32387 SFO - EMERGENCY LIGHT IDENTIFIER AT SEAT 15D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IDENTIFIER AT SEAT 15D. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007120700180 20071207 00180 WP 2007 12 7 AALA20072263 1 20071120 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9628W 53598 SFO - EMERGENCY LIGHTS AT OVERHEAD FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD F ORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007120700181 20071207 00181 NM 2007 12 7 AALA20072283 1 20071124 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHTS AT LEFT AND RIGHT AFT COACH INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT AND RIGHT AFT COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120700182 20071207 00182 NM 2007 12 7 AALA20072264 1 20071120 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 766AN 32880 DFW - EMERGENCY LIGHT AT SEAT ROW 30 CDEF INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 30 CDEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120700183 20071207 00183 WP 2007 12 7 AALA20072273 1 20071122 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 76200 53290 SFO - EMERGENCY LIGHTS AT MID COACH CABIN SEATS INOPERATIVE. REPLACED BATTERY PACK B5104 FOR EMERGENCY LIGHTS AT MID CO ACH CABIN SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007120700184 20071207 00184 NM 2007 12 7 AALA20072285 1 20071124 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 ORD - EMERGENCY LIGHT AT RIGHT OVERHEAD SEAT ROW 37 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT OVERHEAD SE AT ROW 37. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007120700186 20071207 00186 NM 2007 12 7 AALA20072286 1 20071124 A 3350 LAMP BOEING 767 767223 1385123 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 325AA 22326 LAX - EXTERNAL EMERGENCY LIGHT AT LEFT AFT WING INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT LEFT AFT WIN G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007120700187 20071207 00187 NM 2007 12 7 AALA20072278 1 20071123 A 3350 8039001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 JFK - EMERGENCY LIGHTS AT SEAT ROWS 20 TO 22 INOPERATIVE. REPLACED BATTERY PACK AT RIGHT NUMBER THREE DOOR FOR EMERGENC Y LIGHTS AT SEAT ROWS 20 TO 22. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120700188 20071207 00188 NM 2007 12 7 AALA20072279 1 20071123 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 797AN 30012 DFW - EMERGENCY LIGHT AT SEAT 21G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120700189 20071207 00189 WP 2007 12 7 AALA20072276 1 20071123 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 553AA 53083 LGA - EMERGENCY LIGHT AT SEAT 13D MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F A6WE 2007120700191 20071207 00191 2007 12 7 AALA20072267 4 20071122 A 2565 100504205 SLIDE DOUG DC9 DC982 3022082 WP L1 DOOR DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 258AA 49288 RDU - EMERGENCY EVACUATION SLIDE AT LEFT NUMBER ONE DOOR HAD INFLATION CABLE PULLED FROM PINS. REPLACED EMERGENCY EVACU ATION SLIDE AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007120700194 20071207 00194 NE 2007 12 7 AALA20072265 2 20071121 A 7230 FAN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LEFT ENGINE FOD A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 955U 49427 728200 ORD INFLIGHT - NUMBER ONE ENGINE LOST POWER DURING CLIMB. CREW HEARD LOUD POPS. PULLED THROTTLE TO IDLE AND LEFT NUMBE R ONE ENGINE AT IDLE FOR LANDING. NUMBER ONE ENGINE PARAMETERS WERE NORMAL. LANDED ORD WITHOUT INCIDENT. REPLACED NUM BER ONE ENGINE AND ISOLATORS ON 22 NOV AT ORD DUE TO COMPRESSOR STALL DUE TO FAN FOREIGN OBJECT DAMAGE. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007120700195 20071207 00195 NM 2007 12 7 AALA20072268 1 20071122 A 3397 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 BOS - EMERGENCY LIGHTS AT LEFT AND RIGHT FORWARD COACH INOPERATIVE. REINSERTED PIN FOR EMERGENCY LIGHTS AT LEFT AND RIG HT FORWARD COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120700196 20071207 00196 WP 2007 12 7 AALA20072274 1 20071122 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 76200 53290 SFO - EMERGENCY LIGHTS AT AFT CABIN SEATS INOPERATIVE. REPLACED BATTERY PACK B5107 FOR EMERGENCY LIGHTS AT AFT CABIN SE ATS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007120700198 20071207 00198 NM 2007 12 7 AALA20072269 1 20071122 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 175AN 32394 SFO - EMERGENCY LIGHTS AT FLOOR SEAT ROWS 14D TO 25D INOPERATIVE. REPLACED BATTERY PACK AT M10953 FOR EMERGENCY LIGHTS AT FLOOR SEAT ROWS 14D TO 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007120700201 20071207 00201 NM 2007 12 7 AALA20072288 1 20071125 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 779AN 29955 MIA - EMERGENCY LIGHT AT SEAT 23G INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 23G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120700203 20071207 00203 NM 2007 12 7 AALA20072290 1 20071125 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 377AN 25446 MIA - EMERGENCY LIGHT AT SEAT 25B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25B. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007120700204 20071207 00204 NM 2007 12 7 AALA20072281 1 20071123 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 797AN 30012 DFW - EMERGENCY LIGHT AT SEAT 31G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 31G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120700206 20071207 00206 WP 2007 12 7 AALA20072262 1 20071120 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9628W 53598 SFO - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 3 TO 7 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 3 TO 7. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007120400320 20071204 00320 NM 2007 12 4 UPS07551214 1 20071126 A 3350 LIGHT BOEING 757 75724APF 1384969 NM EXTERIOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 473UP 28846 OUTSIDE EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM 33-51-06-2. 2 L 7 2 4F RT A2NM 2007120400328 20071204 00328 2007 12 4 BKAA200710003 4 20071016 A 3497 TERMINAL BLOCK MTSBSI MU2 MU2B36 5780412 CE GARRTT TPE331 TPE331* 01514 WP STICK SHAKER DAMAGED E BKAA A UNSCHED LANDING P S NO WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 13 535WM 11798 655 PITCH CONTROL JAMMED IN FLIGHT. SLIGHT MOVEMENT UP ABOUT 1 INCH CONTROL TRAVEL. A/C TRIED A FEW TIMES TO PITCH DOWN. A/P AND AVIONICS SWITCH OFF. LANDED WITH POWER CONTROLLING PITCH. T/S FOUND STICK SHAKER ON YOKE GETTING HUNG UP BY TERMINA L BOARD. RESECURED TERMINAL BOARD, OPS CHECK GOOD. 1 H 7 2 3T 3 T RT A10SW E2WE 2007120400335 20071204 00335 NM 2007 12 4 UPS07551221 1 20071127 A 3350 M00043 LIGHT BOEING 757 75724APF 1384969 NM CONTROL PANEL DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 451UP 27739 EMERGENCY EXIT LIGHT CONTROL PANEL ANNUNCIATOR LIGHT DAMAGED. REMOVED AND REPLACED ANNUNCIATOR LIGHT UNIT. OPS CHECK O K IAW MM -33-51-01. 2 L 7 2 4F RT A2NM 2007120400336 20071204 00336 CE 2007 12 4 BB1402111207 1 20071112 A 3397 D25K10R0 RESISTOR BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE YOKE LOOSE E QMLA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NM 03 791DC BB1402 DURING APPROACH TO LANDING PILOT NOTICED SPARKING TWICE UNDER THE COPILOTS YOKE, AND NOTICED A BURNING SMELL. LANDED WIT HOUT INCIDENT. THE MECHANIC FOUND A DIMMING RESISTOR LOOSE IN SUBPANEL. HE REPAIRED THE ITEM AND APPROVED THE A/C FOR RE TURN TO SERVICE. 1 L 7 2 4T 4 T A24CE E4EA 2007120400342 20071204 00342 CE 2007 12 4 DJFA2007132 1 20071114 A 3243 MASTER CYLINDER RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP BRAKES WEAK E DJFA O OTHER O OTHER LD LANDING 1 EA 23 791TA 258291 CREW REPORTED BRAKES FELT SPONGY AND TRAVELED A GREAT DISTANCE BEFORE BRAKING WAS FELT ON LANDING. THE BRAKE MASTER CYL INDERS WERE BLED. THE MAIN AND EMERGENCY SYSTEMS WERE BLED. THE MAIN HYDRAULIC SYSTEM WAS SERVICED TO FULL. 2 L 7 2 4F 4 F RT A3EU E6WE 2007120400348 20071204 00348 CE 2007 12 4 DXTA200702615 1 20071117 A 3260 BULB CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG INDICATOR INOPERATIVE E DXTA O OTHER P NO WARNING INDICATION LD LANDING 1 GL 07 607QS 5605340 ON APPROACH, LT MAIN LANDING GEAR (GREEN) DOWN AND LOCKED INDICATOR FAILED TO ILLUMINATE. FOLLOWED CHECKLIST AND DISCHAR GED BOTTLE. INDICATOR STILL INOP. FOUND BULBS BLOWN IN THE LT DOWN & LOCKED GREEN INDICATOR. REPLACED BULBS. INDICATOR OPS CHECK GOOD. JACKED AIRCRAFT. C/W RESET OF EMER GEAR N2 BOTTLE & SERVICED. C/W GEAR SWINGS & PURGED SYSTEM OF NITROGE N GEAR INDICATION OPS CHECK GOOD. ALL WORK IAW CE560XL MM 32-01-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007120400357 20071204 00357 NE 2007 12 4 UPS07851217 2 20071127 A 7200 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 3 FLAMED OUT A IPXA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 SO 01 802UP 46100 NR 3 ENGINE FLAME OUT. INFLIGHT RESTART ACCOMPLISHED AFTER DESCENT TO FL220. NORMAL ENGINE INDICATIONS AFTER RESTART. A/C IS CURRENTLY OUT OF SERVICE. PERFORMED DC8 MM71-00-00-1, FIG 139 AS REQUIRED. REF LP 887083/1,2,3 LOG PAGE 887084 ITEM 1,2,3. NR 3 ENGINE PERFORMANCE WAS NORMAL WITH MIN. FUEL PRESSURES MET. NO PREVIOUS FLAME OUT HISTORY. A/C OK F OR CONTINUED SERVICE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2007120400358 20071204 00358 NM 2007 12 4 UPS07M51208 1 20070928 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C MAIN DECK: BS 1029, ALONG -X=76 (RBL76) SEAT TRACK CROWN AREA FOUND CRACKED (ABOUT ONE INCH LENGTH OF CRACK), SEAT TRACK AT STA 1009 RBL 76" TRIMMED OFF PER SRM 53-70-00D FIG 1R.35. HFEC INSP C/OUT PER DAC NDT SPM R.13 06 -10-01.001. NO CRACK EVIDENT REP SPLICE HAT AND PLATE REWORK PER SRM53-70-00D FIG1V 1R.35. NEW SEAT TRACK REP PARTS HO LES P/UP AND PROTECTED PER SRM51-31-01 AND 51-21-01V.2R.35. NEW SEAT TRACK PAINTED PER SRM 51-21-01 V.2R.35. OK TO INS TALL. 2 L 7 3 4F RT A22WE 2007120400359 20071204 00359 NM 2007 12 4 UPS07M51209 1 20070920 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C MAIN DECK: FROM BS 820 TO BS 835 (LOCATION :NR 2 DOOR AREA), LT MOST O/B SEAT TRACK FLANGE AREAS FOUND CORRODED. CORROSION AT M/DECK FR BS 820-BS 835 OB SEAT TRACK FLANGE REMOVED PER SRM 51-21-01V.2R.35. FOUND EXCEED LIM IT PER SRM 53-70-00D FIG.3V.1R.35. CORRODED SEAT TRACK AT STA 869 TRIMMED OFF PER SRM 53-70-00D FIG.1V.1R.40. HFEC C/O UT PER DACNDT SPM R.13 PART 06-10-01-001. FOUND NO CRACK EVIDENT NEW SEAT TRACK AND REP PARTS REWORKED PER SRM 53-70-00 D FIG.1V.1R.40. 2 L 7 3 4F RT A22WE 2007120500005 20071205 00005 NM 2007 12 5 AMTA200700591 1 20071111 A 3610 106200825 SENSOR BOEING 737 73783N 13844HI NM PRECOOLER VALVE UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 11 308TZ 28244 LT BLEED TRIP OFF LIGHT ON, LT ENG IS THE BLEED SOURCE. REMOVED AND REPLACED PRE-COOLER CONTROL VALVE SENSOR IAW AMM 36 -12-03-4. OPS CHECK NORMAL. (K) 2 L 7 2 4F RT A16WE 2007120500007 20071205 00007 2007 12 5 AMTA200700593 4 20071112 A 3460 1762000101 COMPUTER BOEING 737 73783N 13844HI NM NR 2 FMC UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 319TZ 30643 F/O FMC FAIL. REMOVED AND REPLACED NR 2 FMC IAW AMM 34-61-02-4 AND PERFORM ADJUSTMENT/ TEST IAW AMM 34-61-00-5. (K) 2 L 7 2 4F RT A16WE 2007120500008 20071205 00008 NM 2007 12 5 AMTA200700584 1 20071105 A 2120 UNKNOWN BOEING 737 73783N 13844HI NM CABIN SMOKE A AMTA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 11 304TZ 30675 ON APPROACH SMOKE AND FUMES ENTER THE CABIN AND FLT DECK. T/S IAW FIM 21-00-00-810-802, NO FAULTS FOUND, OK FOR SERVICE . (K) 2 L 7 2 4F RT A16WE 2007120500010 20071205 00010 NM 2007 12 5 AMTA200700586 1 20071106 A 4900 WARNING MESSAGE BOEING 737 73783N 13844HI NM APU FALSE ACTIVATION A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 317TZ 28246 AFTER BOTH ENG STARTED W/MASTER CAUTION RECALL APU LIGHT STAYED ILLUMINATED. COMPLIED WITH APU BITE CHECK FOUND FAULT 4 9-11019 COMPLIED WITH FIM TASK 49-10 TASK 801 FAULT CLEARED. OPS CHECK NORMAL. (K) 2 L 7 2 4F RT A16WE 2007120500012 20071205 00012 NM 2007 12 5 AMTA200700576 1 20071104 A 5320 STRUCTURE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE BS 620 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 522AT 29330 FWD CARGO COMPARTMENT RT SIDE WALL TO FLOOR TRANSITION PANEL STRUCTURE, BLOWN OUT CORROSION, STA 620, RBL 30. CUT OUT D AMAGE FROM BS620, RBL 30, NO CORROSION ON FITTING OR DOUBLER IAW SRM 51-70-13, FIG 1, REMOVED CRACKED T-BRACKET FABRICAT ED FILLER AND DOUBLER IAW SRM 51-70-13, FIG 1, INSTALLED T BRACKET AND FILLER AND DOUBLER IAW SRM 51-70-13, 51-40-01. ( K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007120500017 20071205 00017 CE 2007 12 5 CIEA200700009 1 20071120 A 2721 505245799 SPINDLE BEECH B300 B300 1159232 CE PWA PT6 PT6* 52043 EA RUDDER BROKEN E CIEA O OTHER O OTHER NR NOT REPORTED 1 NM 03 350JB 3510 FL213 DURING TAKEOFF THE PILOT NOTICED THAT IT WAS NECESSARY TO PUT APPROX 4 DEGREES OF RT RUDDER TRIM IN ORDER TO HAVE THE AI RPLANE FLY STRAIGHT DURING TAKEOFF WITH MINIMAL APPLICATION OF RUDDER. THE PILOT THEN NOTICED AFTER LANDING THAT WHEN T HE RUDDER TRIM WAS INDICATING 4 DEGREES OF RT RUDDER TRIM, THE RUDDER TRIM APPEARED TO BE IN THE NEUTRAL POSITION. THE PILOT REQUESTED THAT MAINT CHECK AND VERIFY THE RUDDER TRIM WAS RIGGED PROPERLY. MAINTENANCE VERIFIED THAT THE RUDDER T RIM TRAVEL WAS PROPER FOR BOTH THE LT AND RT DEFLECTION, BUT NOTICED THAT THE INDICATOR WAS SHOWING AN INCORRECT VALUE. FURTHER TROUBLESHOOTING RESULTED IN FINDING THE SHAFT THAT INTERFACES WITH THE TRIM INDICATOR HAD BROKEN. DUE TO THE F 2 L 7 2 4T 3 T RT A24CE E2NE 2007120500070 20071205 00070 CE 2007 12 5 DXTA200702627 1 20071122 A 3230 MANIFOLD CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG VIBRATION E DXTA O OTHER E VIBRATION/BUFFET DE DESCENT 1 GL 07 905QS 7500105 ON DESCENT THRU 18000 FT, HEARD 2 LOUD BANGS FOLLOWED BY VIBRATION FELT BY THE CREW. THE VIBRATION WAS CENTER IN THE FL OOR AREA OF THE COCKPIT. COMPLIED WITH 750 GEAR BUMP TROUBLESHOOTING INSTRUCTION IAW 750 MM 32-30-00. COMPLIED WITH SB7 50-32-47. REMOVED AND REPLACED MLG CONTROL MANIFOLD ASSY IAW SB750-32-47. LEAK AND OPS CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007120500074 20071205 00074 NE 2007 12 5 HEER118215 1 20071116 A 5350 ANGLE SKRSKY S92 S92A NE GE CT7TS CT78A 30136 NE TAILCONE CRACKED B HEER O OTHER O OTHER NR NOT REPORTED 1 SW 03 192PH 3211 920006 FWD LT CAP ANGLE CRACKED. REPORTED PROBLEM TO MFG. 2 G 7 2 4U 4 U R00024BO E8NE 2007120500075 20071205 00075 NE 2007 12 5 HEER118259 1 20071120 A 2434 7655009006106 CONTROL UNIT SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL2S2 60036 NE NR 1 DC GEN UNKNOWN B HEER O OTHER O OTHER NR NOT REPORTED 1 SW 03 796P 16 760681 NR 1 DC GENERATOR DROPS OFF LINE. 1 G 7 2 3U 4 U NC H1NE E00054EN 2007120500105 20071205 00105 EU 2007 12 5 SIMA200733002 1 20071123 A 2750 FLAP SYSTEM SAAB SF340 340B 7860101 EU TE FLAPS OUT OF RIG A SIMA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SW 21 304AE 340B304 AT FL230, THE A/C BEGAN OSCILLATING PITCH UP/DOWN. THIS OCCURRED AT CRUISE FLT. PITCH UP AND DOWN WENT FROM +2.5 TO -2 .5 ABV AND BELOW HORIZON. THIS OCCURRED WITH ALL PAX AND FA SEATED. NO CG CHANGES CONDITION OCCURRED WITH AUTO PILOT O N AND OFF AND YAW DAMPER OFF. LEVEL FLT AT 7K AND 10K ON CLIMB-OUT NO ISSUES. ON DESCENT FL 6K NO ISSUES, ONLY ALT WIT H OSCILLATIONS FL230 LEVEL FLIGHT. RERIGGED FLAP ELECTRICAL SYSTEM AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4T RT A52EU 2007120500107 20071205 00107 EU 2007 12 5 SIMA200733001 1 20071123 A 2750 FLAP SAAB SF340 340B 7860101 EU TE FLAPS CHAFED A SIMA O OTHER J F WARNING INDICATION FLT CONT AFFECTED LD LANDING 1 SW 21 250AE 340B250 EMERGENCY DECLARED, FLAP WOULD NOT EXTEND AT ALL FOR LANDING, HAD TO LAND 0 DEGREE FLAPS. NO FLAP CWP. INSPECTED AND F OUND FLAP CHAFING ON LT AND RT ENG DOVE TAIL AND ALSO FOUND AIR IN THE HYD SYSTEM. BLEED SYSTEM AND TRIMMED DOVE TAIL. F CF CHECK GOOD. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4T RT A52EU 2007120700004 20071207 00004 NM 2007 12 7 DLM88071509 1 20071118 A 2497 TRANSFORMER DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE CABIN BURNED A DALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 922DL 14664 49646 P80508 SMOKE AND FUMES IN CABIN. FOUND VARIABLE TRANSFORMER FOR LOWER SIDE WALL PANEL BAD AT AFT F/A PANEL. REMOVED AND REPLA CED ON ITEM 5 TRANSFORMER HAD STRONG BURNED ELECTRICAL ODOR PERFORMED ALT DUCT BURN ON ITEM 7. 2 L 7 2 4F 4 F RT A6WE E9NE 2007120700005 20071207 00005 NE 2007 12 7 DL757071517 2 20071120 A 7297 WIRE HARNESS BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE DAMAGED A DALA E ENGINE SHUTDOWN X J ENGINE FLAMEOUT WARNING INDICATION AP APPROACH 1 SO 27 696DA 48344 29728 716591 ON FINAL APPROACH CREW REPORTED THE LEFT ENGINE HAD A FLAME OUT AND SHUT DOWN BY ITSELF. CREW DID NOT NOTICE ANYTHING A BNORMAL BEFORE IT SHUTDOWN. INSPECTED INLET EXHAUST ON ENG, ALL NORMAL. FOUND WIRES OFF PRIMARY AND SECONDARY CHANNEL S OFF PMA ORANGE WIRES BROKEN. PERFORMED ENG WIRE HARNESS REPAIR TIME LIMITED 10 DAY REPAIR PER ERA 46-465241-14. ALSO , REPLACED LT EEC AND PMA, ENGINE RUN NORMAL. OK FOR SERVICE, ALSO REPLACED PMA ROTOR - OFF 1092- ON UNE00434. 2 L 7 2 4F 4 F RT A2NM E17NE 2007120700009 20071207 00009 NM 2007 12 7 DLM90071521 1 20071120 A 5322 SHEAR TIE DOUG MD90 MD9030 3023690 NM FS 1288 S29L/R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 AFT SHEAR TIE CORRODED AT FS 1288 LONGERON 29L TO 29R. REPAIRED AFT PIT SHEAR TIE AT STA 1288 BETWEEN LONGERON 29L TO L ONGERON 29R IAW MD-90 SRM 53-10-02D ON N/R 1600-0178 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007120700017 20071207 00017 NM 2007 12 7 DL76P071529 1 20071120 A 2910 AS11708K0165 LINE BOEING 767 767332 1382001 NM HYD SYSTEM FAILED A DALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 140LL 25988 DURING PUSHBACK RIGHT HYD SYS WENT TO ZERO RETURNED TO GATE FOR REPAIRS. REPLACED ACMP HYD PRESSURE LINE. 2 L 7 2 4F RT A1NM 2007120700037 20071207 00037 NM 2007 12 7 DLM90071553 1 20071124 A 5754 SKIN DOUG MD90 MD9030 3023690 NM NR 2 SLAT DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 RIGHT WING NR 2 SLAT DENTED LEADING EDGE NEAR CENTER. REPAIRED RT WING NR 2 SLAT L/E IAW MD-90 SRM 57-20-05D FIG 4 VOL 1, ON N/R 6600-0002 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007120700053 20071207 00053 2007 12 7 FFKA121 4 20071126 A 6122 F44A GOVERNOR PIPER PA32 PA32300 7103212 SO LYC O540 IO540K1A5 41532 EA HARTZL HCC2Y HCC2YK1 GL PROPELLER MALFUNCTIONED B FFKA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 05 87619 1729 3240752 L455148 CH33319B PILOT REPORTED THAT THE TACHOMETER WAS INDICATING 100 RPMS HIGHER THEN RECOMMENDED BY THE ENGINE MANUFACTURE AFTER TAKEO FF AND HAD NO CONTROL OF THE PROPELLER GOVERNOR. PILOT REDUCED ENGINE POWER TO KEEP RPMS BELOW REDLINE AND THEN COULD N OT MAINTAIN ALTITUDE. REMOVED GOVERNOR FROM SERVICE AND SENT OFF FOR EVALUATION. THIS EVALUATION DETERMINED THAT THERE WAS INTERNAL OIL LEAKAGE OF OIL PRESSURE CAUSING THE UN-COMMANDED/UN-CONTROLLABLE PROPELLER RPM FLUCTUATION. 1 L 7 1 3O 3 O A3SO 1E4 5 C P920 2007120700073 20071207 00073 NM 2007 12 7 AALA20072260 1 20071119 A 3350 CM767 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 399AN 29606 SFO - EMERGENCY EXIT LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DO OR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007120700075 20071207 00075 NM 2007 12 7 AALA20072257 1 20071119 A 3350 FUSE BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 647AM 24605 JFK - EMERGENCY LIGHT AT OVERHEAD SEAT 16C INOPERATIVE. REPLACED FUSE AT M10770 FOR EMERGENCY LIGHT AT OVERHEAD SEAT 1 6C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007120700078 20071207 00078 EU 2007 12 7 07FDEA04894 1 20071121 A 3230 BDM3003 PROCESSING UNIT AIRBUS 300 A300F4605R 3930327 EU MLG INOPERATIVE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 664FE 768 GEAR FAILED TO RETRACT ON TAKEOFF. INDICATION 3 GREEN, 3 RED "UNLKD" ON LOWER AND UPPER PANEL. MAX AIRSPEED 225 KIAS T HE DET SYS 2 WAS UNABLE TO RETRACT THE GEAR. DID NOT TRY THE DET SYS 1. REMOVED BOOGIE BEAM PROX SENSOR PROX MOUNT REM OVED FOR ACCESS OF 12GA. ALSO FOUND 8GA PROX (SYS 1) CONNECTOR CORRODED. INSTALLED BOOGIE BEAM POSITION PROX SENSORS 12 GA AND 8 GA RT STRUT, REMOVED AND REPLACED PROXIMITY DETECTOR PROCESSING UNIT. OPS CHECK IS NORMAL, OFF MFG BDM300-3, SRL 585 ON MFG BDM300-3, SRL 203. WORK IS COMPLETE, ACFT IS OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2007120700083 20071207 00083 EU 2007 12 7 07FDEA04952 1 20071127 A 5315 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 671FE 778 FWD CARGO COMPT FR 29 BETWEEN SEAT TRACKS 3R-2R APPROX 3/4 INCH CRACK IN FLOORBEAM REPAIRED CROSSBEAM AT FR 29 BETWEEN SEAT TRACK RT 2-3 IAW A300-600 FSRM 53-10-15. 2 L 7 2 4F RT A35EU 2007120700085 20071207 00085 EU 2007 12 7 07FDEA04954 1 20071128 A 5313 A53970713210 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT CARGO PIT BILGE AREA, STRINGER 55L CORRODED, FR 54.3 T0 FR 58 (STA X3090 TO STA X3143). REMOVED COROSION ON STRINGE R 55L BETWEEN FRAMES 54.3 AND 58 IAW SRM 51-74-10 AND CHECKED LIMITS STRINGER 52L FOUND TO BE OUT OF LIMITS IAW SRM 53-1 0-00. CUT OUT DAMAGED SECTION OF STRINGER 52L BETWEEN FRAME 54.1 TO 58 IAW SRM 51-40-40. FABBED REPAIR COUPLINGS IAW SRM 53-10-14 FIG 201 A. ALODINED STRINGER AND REPAIR PARTS IAW SRM 51-21-10, TOPCOAT AND PRIMED STRINGER AND REPAIR PARTS I AW SRM 51-23-10. INSTALLED NEW STRINGER SECTION AND REPAIR PARTS IAW SRM 53-10-14 PG 204A/204B. 2 L 7 2 4F RT A35EU 2007120700086 20071207 00086 EU 2007 12 7 07FDEA04955 1 20071128 A 5313 A5390192200 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT CARGO PIT BILGE AREA, STRINGER 57L CORRODED, FR 54.2 TO FR 54.3 (STA X3037 TO STA X3090). COMPLIED WITH EA 6-5310-1 13000. 2 L 7 2 4F RT A35EU 2007120700095 20071207 00095 WP 2007 12 7 NWAA073869752 1 20071016 A 5330 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 752NW 47116 DURING "M" CHECK, FOUND CRACK IN FUSELAGE SKIN AT THE AFT LOWER CORNER OF FORWARD CARGO DOOR JAMB. REPAIRED PER EA 97-2 10194. 2 L 7 2 4F A6WE 2007120700109 20071207 00109 NE 2007 12 7 KNNA200700064 2 20071122 A 7200 BALL JOINT BOEING 737 7372L9 1384497 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE LEAKING A KNNA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION DE DESCENT 1 WP 25 465AT 21528 P665721 WHILE EN ROUTE, THE CREW WAS ALERTED BY A NR 1 ENGINE FIRE WARNING ALARM BELL/LIGHTS. DECLARING AN IN-FLIGHT EMERGENCY, AND SHUTTING DOWN NR 1 ENGINE, AND A SINGLE ENGINE LANDING WAS MADE. THE CREW WAS TOLD TO WAIT AT THE END OF THE RUNWA Y AND WAS MET BY THE FIRE DEPARTMENT. THE FIRE DEPARTMENT REPORTED SEEING A PUFF OF SMOKE AND REQUESTED THE FIRE EXTING UISHER BOTTLE BE ACTIVATED 2 L 7 2 4F 4 F RT A16WE E2EA 2007120700118 20071207 00118 NM 2007 12 7 UIEA200700478 1 20071128 A 5410 2242301521 COWLING BOEING 747 74747UF 1384812 NM NR 3 NACELLE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 492 29253 NR 3 ENG I/B CORE COWL UPPER AFT EDGE WHERE COWL SITS AGAINST FIRE SEAL FINGERS, 5 INCHES LONG CRACK WITH 4 PULLED FASTE NERS. UNDERSIDE GOUGED. 2 L 7 4 4F RT A20WE 2007120700119 20071207 00119 NM 2007 12 7 UIEA200700479 1 20071128 A 5280 DOOR BOEING 747 74747UF 1384812 NM MLG DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 492 29253 RT WING LANDING GEAR UPPER STRUT DOOR, IMPACT DAMAGE ON LEADING EDGE OF DOOR 7.5 INCH LONG BY 2.5 INCH WIDE ASSOCIATED D ELAM AND SLIGHT DEFORMATION OF OUTSIDE SKIN OF DOOR. 2 L 7 4 4F RT A20WE 2007120700123 20071207 00123 SO 2007 12 7 SIMA200733401 1 20071125 A 2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY UNKNOWN A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 918AE 14500902 LAV SMOKE CAME ON DURING CLIMB. PULLED CB'S E11 AND E12 PER PROCEDURES. ALSO LAV SMOKE SYSTEM TEST PER PROCEDURE DID N OT TEST PROPERLY. PURGED OF DEICING FLUID ODOR IAW AE3007A FIM 72-00-00-810-814 AND AE3007A MM 72-00-00 BY RUNNING ENGI NES AT HIGH POWER. PERFORMED OPS CHK OF LAV SMOKE DETECTION SYSTEM IAW EMB145 AMM 26-14-00. OPS CHK GOOD. AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007120700125 20071207 00125 SO 2007 12 7 SIMA200733403 1 20071128 A 7500 40303920 O-RING EMB 145 EMB145LR 3260212 SO BLEED SYSTEM BROKEN A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 635AE 145158 CREW GOT A BLEED 1 LEAK MESSAGE IN FLIGHT WHILE PASSING THROUGH 10,000 FEET. CREW FOLLOWED AOM PROCEDURES AND MESSAGE W ENT AWAY. CREW DECIDED TO RETURN TO ORD. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. FOUND O-RING IN CARG O AREA, BOTTOM PANEL BY DOOR WAS BROKEN. REMOVED AND REPLACED O-RINGS IAW EMB 145 AMM 36-11-10, OPS CHECK GOOD. NO FUR THER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007120700135 20071207 00135 EA 2007 12 7 SWIA200718908 1 20070819 A 5220 HANDLE CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 728SK 10192 RIGHT EMERGENCY EXIT DOOR HANDLE RELEASE REQUIRES EXCESSIVE FORCE TO OPEN, FOUND AT C-CHECK. REPLACED CORRODED MOUNTING BOLTS AND CLEANED AND LUBED PINS PER CRJ700/900 AMM 52-21-00-820-802-A01. 2 L 7 2 4F RT A21EA 2007120700141 20071207 00141 NM 2007 12 7 F3LA200700326 1 20071114 A 5320 SHEAR PLATE AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED SHEAR PLATE AT FR 69-70, -Y1732, CORRODED. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11, PARA 6,7,14, AND EA A9-53R-12267. 2 L 7 2 4F RT A28NM 2007120700148 20071207 00148 NM 2007 12 7 UPS07M51223 1 20071027 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 830-909 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C CABIN, CORROSION ON SEAT TRACK CROWN AND CHANNEL AT STA 902 X=27. CORROSION ON SEAT TRACK SECTIONAL T RIM OUT BTWN STA830 - 909, X=27 AND REMOVED PER SRM 51-31-01 VIIR 35. HFEC INSP C/O PER DAC NDTSPM R13 06-10-01.001 ON TRIM OUT AREA AND FOUND NO CRACK. NEW SEAT TRACK AND REPAIR SPLICE REWK AND FAB PER SRM 53-70-00 FIG 7 VIR 35. NEW SE AT TRACK AND SPLICE INSTALLED PER SRM 53-70-00 FIG 1 VIR 35 AND SRM 51-31-01 VIIR 35. 2 L 7 3 4F RT A22WE 2007120700152 20071207 00152 NM 2007 12 7 F3LA200700332 1 20071112 A 5340 FITTING AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR FITTING UNDER CABINET SECTION OF AFT GALLEY CORRODED. REMOVED AND REPLACE D CORRODED FITTING IAW AMM 25-33-41-400-002. 2 L 7 2 4F RT A28NM 2007120700155 20071207 00155 NM 2007 12 7 USAA920071230 1 20071119 A 5753 113N280096SP SKIN BOEING 757 7572B7 1384964 NM RT WING TE FLAP DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 200UU 27809 MCN - MAJOR REPAIR - C4 CHECK - RIGHT WING INBOARD AFT FLAP HAS AREA OF DISBOND, WS 300.83 - WS 328.83. REPAIRED RIGHT WING INBOARD AFT FLAP, WS 300.83 - WS 328.83 IAW B757 SRM 51-70-04. 2 L 7 2 4F RT A2NM 2007120700167 20071207 00167 NM 2007 12 7 USAA920071242 1 20071123 A 5311 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C16 CHECK, CRACKED FRAME, BS 787, S8R - S9R. REPAIRED FRAME, BS 787, S8R - S9R IAW USAIRWAYS EA 10 0048 AND TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2007120700168 20071207 00168 NM 2007 12 7 USAA920071243 1 20071119 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C16 CHECK, CORROSION ON FLOORBEAM, BS 320, RBL 18. REPAIRED FLOORBEAM, BS 320, RBL 18 IAW B737 SRM 53-10-51. 2 L 7 2 4F RT A16WE 2007120700171 20071207 00171 NM 2007 12 7 USAA920071246 1 20071116 A 5340 6935352U14 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C16 CHECK, CRACKED STRINGER CLIP, BS 639, S4L. REPLACED STRINGER CLIP, BS 639, S4L IAW B737 SRM 51 -40-02. 2 L 7 2 4F RT A16WE 2007120700200 20071207 00200 NM 2007 12 7 AALA20072291 1 20071125 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120700209 20071207 00209 NM 2007 12 7 F3LA200700337 1 20071115 A 5320 D5347112320203 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED FRAME SUPPORT CORRODED AT FR 69-70, -Y1732. REMOVED AND INSTALLED REPLACEMENT F RAME SUPPORT IAW SRM 51-42-11. 2 L 7 2 4F RT A28NM 2007120700213 20071207 00213 NM 2007 12 7 KNNA200700065 1 20071129 A 2150 A41905533505 RELAY BOEING 737 737291 138448W NM A/C PACK BINDING A KNNA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 25 977UA 21508 PRIOR TO TAKEOFF, THE SENIOR FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. MECHANIC’S INVESTIGATION DETERMINED THE SMOK E IN THE CABIN WAS DUE TO AN ELECTRICAL MALFUNCTION CAUSING BOTH PACKS TO TRIP OFF. CABIN THEN FILLED WITH ENGINE BLEED AIR BYPASSING BOTH AIR-CYCLE MACHINES. 2 L 7 2 4F A16WE 2007120700214 20071207 00214 NM 2007 12 7 F3LA200700341 1 20071127 A 5554 D5537002021000 ATTACH BOLT AIRBUS A319 A319111 3930336 NM RUDDER ATTACH CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED RUDDER ATTACH FITTING NR 7 ATTACHMENT BOLT CRACKED AROUND CENTER CIRCUMFERENCE A REA. REMOVED AND REPLACED HARDWARE IAW AMM 27-21-41-420-051. 2 L 7 2 4F RT A28NM 2007120700218 20071207 00218 NM 2007 12 7 F3LA200700344 1 20071114 A 5347 STRAP AIRBUS A319 A319111 3930336 NM CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C-4/S1 CHECK, INSPECTION REPORTED PANEL 262EF TIE-DOWN STRAP CORRODED. REPLACED AFT TIE-DOWN STRAP ON PANEL 262E F IAW AMM 53-32-12-400-002. 2 L 7 2 4F RT A28NM 2007120700219 20071207 00219 NM 2007 12 7 F3LA200700345 1 20071113 A 5321 FLOORBOARD AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED BOTTOM OF FLOORBOARD 261FF CORRODED. REMOVED AND REPLACED FLOOR 261FF IAW AMM 5 3-32-12-400-002. 2 L 7 2 4F RT A28NM 2007121100001 20071211 00001 EA 2007 12 11 TRAX200701779 1 20071126 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 FS 280 RBL 36 I/B ANGLE IS CRACKED. 2 L 7 2 4F RT A21EA 2007121100002 20071211 00002 EA 2007 12 11 TRAX200701781 1 20071126 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 FLOOR SUPPORT AFT OF CARGO DOOR HAS CORROSION. 2 L 7 2 4F RT A21EA 2007121100003 20071211 00003 EA 2007 12 11 TRAX200701782 1 20071126 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 MAIN PAX DOOR WILL NOT LATCH FROM INSIDE OR OUTSIDE A/C. JAMMED ITSELF TRYING TO STOW OUTER HANDLE. 2 L 7 2 4F RT A21EA 2007121100006 20071211 00006 EU 2007 12 11 TRAX200701784 1 20071127 A 5320 BRACKET AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 RT BELLY , LWR INTERNAL BTW FR 24-25 FWD L BRACKET CRACKED. 2 H 7 2 4T RT A53EU 2007121100008 20071211 00008 EA 2007 12 11 TRAX200701816 1 20071127 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 761ND 10213 RT LWR EMERGENCY LIGHT AT RT EMERGENCY DOOR DOES NOT COME ON. 2 L 7 2 4F RT A21EA 2007121100009 20071211 00009 EU 2007 12 11 TRAX200701786 1 20071127 A 5320 INTERCOSTAL AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 WHEEL WELL RT INTERCOSTAL ON FR 27 CRACKED (193AL). 2 H 7 2 4T RT A53EU 2007121100011 20071211 00011 EU 2007 12 11 TRAX200701787 1 20071127 A 5311 FRAME AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 FOUND FR 23B CORRODED ON LWR FLANGE BTW STR 21L-21R. FR 23B ON LWR FLANGE BTW STR 21L - 21R CORROSION IS REMOVED IAW SR M 51-21-42 AND FOUND OUT OF LIMITS SRM 53-51-00 U/T PERFORMED BY HEATHAIR AMO46-90 W/O 37934 IAW NTM MIN = 0.035" FRAME 23B ON LWR FLANGE BTW STR 21L - 21R REPAIRED IAW SRM 53-00-00 FIG 430 SHEET 1FABRICATION COVER ON W/C 2000-232 MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.028 WITHIN LIMITS AS PER SRM: 53-51-00 FIG 301. 2 H 7 2 4T RT A53EU 2007121100012 20071211 00012 EA 2007 12 11 TRAX200701818 1 20071128 A 5414 SKIN CNDAIR CL600 CL6002B19 1900309 EA ENGINE SUPPORT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 826AS 7210 ENGINE SUPPORT BOX BEAM UPPER SKIN HAS 17/32 INCH CRACK AT AFT CENTER SECTION JUST I/B OF RBL 9.500 SEE AFDL 311351 ITEM 2. 2 L 7 2 4F RT A21EA 2007121100014 20071211 00014 EU 2007 12 11 TRAX200701819 1 20071128 A 5720 BRACKET AEROSP ATR72 ATR72212 8680945 EU LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 LT WING, (3) OMEGA BRACKET CRACKED ON FLAP BEAM RIB 8. 2 H 7 2 4T RT A53EU 2007121100015 20071211 00015 EU 2007 12 11 TRAX200701789 1 20071127 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 DOUBLER CORRODED ON FLOORBEAM L/O, AT LBL 10. 2 H 7 2 4T RT A53EU 2007121100016 20071211 00016 EU 2007 12 11 TRAX200701790 1 20071127 A 5313 STRINGER AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 CORROSION FOUND ON STRINGER 21L (FORMER) BTW FR 40-41. CORROSION ON STRINGER 21 LT BTW FR 40-41 REMOVED AS PER SRM 51-2 1-42 STR 21 LT BTW 40-41 REMOVED FOR ACCESS AS PER SRM 51-25-01STR 21 LT BTW FR 40-41 INSTALLED AS PER SRM 51-25-01 REPA IR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORD ANCE WITH SRM 51-21-42 MATERIAL THICKNESS: 0.063MATERIAL REMOVED: 0.003 WITHIN LIMITS AS PER SRM: 53-61-00 FIG 301. 2 H 7 2 4T RT A53EU 2007121100017 20071211 00017 EU 2007 12 11 TRAX200701791 1 20071127 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 RT I/B SEAT TRACK CORRODED BTW FR 36-40. 2 H 7 2 4T RT A53EU 2007121100018 20071211 00018 EU 2007 12 11 TRAX200701822 1 20071128 A 5755 SHIELD AEROSP ATR72 ATR72212 8680945 EU SPOILER CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 THUNDER SHIELD BLADE OF RT SPOILER FOUND CORRODED. BLADE REMOVED IAW SRM 51-21-42 AMD OUT OF LIMIT IAW SRM 51-10-10 T HUNDER SHIELD BLADE BONDED AS PER SRM 57-71-10 THUNDER SHIELD BLADE INSTALLED IAW SRM 51-25-01 THUNDER SHIELD BLADE OF RT SPOILER PAINTED AS PER SRM 51-21-27 MATERIAL THICKNESS: 0.024 MATERIAL REMOVED: 0.006 OUT OF LIMITS AS PER SRM: 51 -10-10. 2 H 7 2 4T RT A53EU 2007121100019 20071211 00019 EU 2007 12 11 TRAX200701823 1 20071128 A 3350 LIGHT AEROSP ATR72 ATR72212 8680945 EU CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 EMERGENCY LIGHT 21WL ON PAX DOOR DON'T WORK. 2 H 7 2 4T RT A53EU 2007121100020 20071211 00020 EU 2007 12 11 TRAX200701824 1 20071128 A 5210 INTERCOSTAL AEROSP ATR72 ATR72212 8680945 EU PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 AFT INTERCOSTAL BTW BEAM 6 AND 7 CRACKED OF PAX DOOR. REPLACED IAW SRM 51-25-01 REPAIR DETERMINED NOT TO BE A MAJOR R EPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007121100023 20071211 00023 EU 2007 12 11 TRAX200701795 1 20071127 A 5313 STRINGER AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 CORROSION FOUND ON STRINGER 17R, BOTH SIDE OF FR 37. CORROSION ON STRG 17 RT ARROUND FR 37 REMOVED AS PER SRM 51-21-42 STRINGER 17R ARROUND FR 37 REPAIRED IAW SRM 53-00-00 FIG 428 MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.013 OUT OF LIMITS AS PER SRM: 53-61-00 FIG 301. 2 H 7 2 4T RT A53EU 2007121100026 20071211 00026 EU 2007 12 11 TRAX200701799 1 20071127 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 RT O/B SEAT TRACK CORRODED BETWEEN FR 29-36 AT FR 36, CORROSION HAS BEEN REMOVED IAW SRM 51-21-42, AND FOUND OUT OF LIM ITS SRM 53-00-00 FIG 301ON RT O/B SEAT TRACK HAS BEEN REPLACED IAW SRM 51-25-04 MATERIAL THICKNESS: 0.146 MATERIAL REMO VED: 0.026 OUT OF LIMITS AS PER SRM: 53-00-00 FIG 304. 2 H 7 2 4T RT A53EU 2007121100027 20071211 00027 EU 2007 12 11 TRAX200701834 1 20071129 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 FLOORBEAM FR 40 FOUND CORRODED OUT OF LIMIT ONE W/C 100-55 NEEDS SPLICE PARTS TO BE FABRICATED. 2 H 7 2 4T RT A53EU 2007121100029 20071211 00029 EU 2007 12 11 TRAX200701801 1 20071127 A 5714 INTERCOSTAL AEROSP ATR72 ATR72212 8680945 EU LT WING BOX CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 WING BOX LT INTERCOSTAL BTW FR 23D AND 24 L BRACKET CRACKED (291AL) BTW STR 2-3-4. 2 H 7 2 4T RT A53EU 2007121100030 20071211 00030 EU 2007 12 11 TRAX200701802 1 20071127 A 5714 INTERCOSTAL AEROSP ATR72 ATR72212 8680945 EU RT WING BOX CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 WING BOX RT INTERCOSTAL BTW FR 23D AND 24 L BRACKET CRACKED (291AL) BTW STR 2-3-4. 2 H 7 2 4T RT A53EU 2007121100031 20071211 00031 EU 2007 12 11 TRAX200701803 1 20071127 A 5740 ATTACH BRACKET AEROSP ATR72 ATR72212 8680945 EU WING BOX CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 FOUND WING BOX AT BLO ATTACHING BRACKET OF PANEL 291AL CRACKED. 2 H 7 2 4T RT A53EU 2007121100032 20071211 00032 EU 2007 12 11 TRAX200701804 1 20071127 A 5714 FRAME AEROSP ATR72 ATR72212 8680945 EU RT WING BOX CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 FOUND RT WING BOX FR 284 FACE PLATE CRACKED. REPLACED AS PER SRM 51-25-01REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACOMPLISHED IN ACCORDANCE WITH SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007121100035 20071211 00035 EU 2007 12 11 TRAX200701808 1 20071127 A 5340 ANCHOR FITTING AEROSP ATR72 ATR72212 8680945 EU WINDSHIELD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 RT SIDE WINDSHIELD , 3 ANCHOR NUTS MISSING 2, RT SIDE WINDSHIELD, ONE ANCHOR NUT IS CRACKED. 2 H 7 2 4T RT A53EU 2007121100037 20071211 00037 NM 2007 12 11 F3LA200700347 1 20071114 A 5320 D5348004320501 SILL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON R2 DOOR SILL, INBD AFT TWO NUTPLATE HOLES AND NUTPLATE HOLE LOCATED OTBD AND AFT OF FWD GIRT BAR FITTING ON SILL. REPAIRED CORRODED AREAS IAW SRM 53-41-14, PRINCIPAL 5 REPAIR. 2 L 7 2 4F RT A28NM 2007121100038 20071211 00038 NM 2007 12 11 F3LA200700348 1 20071114 A 5320 SILL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED R2 DOOR SILL CORRODED IN TWO AREAS AFT OF INBD AFT NUTPLATE HOLE LOCATED 1.5 INC HES AND 2.5 INCHES AFT. REPAIRED CORRODED AREAS IAW SRM 53-41-14, FIG 101, PAGES 103/104. 2 L 7 2 4F RT A28NM 2007121100039 20071211 00039 NM 2007 12 11 F3LA200700349 1 20071114 A 5315 D5347217220400 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED NUTPLATE HOLES CORRODED ON FLOORBEAM +Y1292 (LT), 4 INCHES FWD OF FR68. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11, PARA 7. 2 L 7 2 4F RT A28NM 2007121100040 20071211 00040 NM 2007 12 11 HALA0700510 1 20071012 A 3520 11900311 OXYGEN GEN BOEING 767 7673CB 1385187 NM PBE FIRE A HALA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 WP 13 592HA 17470 17470 33468 PBE (S/N 302362) WAS REMOVED FOR TIME, AND NEEDED TO BE SCRAPED. THE OXYGEN GENERATOR NEEDED TO BE DEPLOYED AND SENT TO HAZMAT FOR DISPOSAL. OPENED THE SEALED WRAP AND PEELED OPEN THE HOOD MASK. DEPLOYED THE OXYGEN GENERATOR AND WITHIN TW O (2) SECONDS, THE MASK STARTED TO BURN. HEARD SMALL (POP) NOISE AFTER DEPLOYMENT AND FLAMES STARTED TO SHOOT OUT FROM THE OXYGEN GENERATOR CANISTER. THE SMALL TUBE (CANDLE) SEPARATED FROM THE MAIN CANISTER. 2 L 7 2 4F RT A1NM 2007121100041 20071211 00041 NM 2007 12 11 HALA0700509 1 20071130 A 3222 537213 STRUT BOEING 767 7673G5 1385126 NM NLG BINDING A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 586HA 24259 EICAS STATUS MSG: LDG GEAR MONITOR. PERFORMED FIM 32-61-00. FOUND RT NLG FWD DOOR BINDING AT STRUT ASSY FOR GROUND REL EASE HANDLE. REMOVED AND REPLACED RT FWD NOSE GEAR DOOR'S STRUT. GEAR SWING CKS OK PER AMM 32-22-02. 2 L 7 2 4F RT A1NM 2007121100042 20071211 00042 NM 2007 12 11 F3LA200700350 1 20071114 A 3220 FITTING AIRBUS A319 A319111 3930336 NM NLG CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 1759 DURING C4/S1 CHECK, INSPECTION REPORTED CRACK IN HOLE H4 ON THE NLG FITTING MOD (EO NR A0-53EO-20373, REV. B). UPSIZED HOLE FROM .277 TO .309 AND RE-INSPECTED HOLE. NO DEFECTS NOTED. INSTALLED NEW FASTENER IAW EA NR A9-53R-12284 AND SRM 51-49-00, TABLE 18. 2 L 7 2 4F RT A28NM 2007121100044 20071211 00044 NM 2007 12 11 F3LA200700352 1 20071113 A 5320 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON NUT PLATE HOLES OF FLOORBEAM -Y1292 BETWEEN FR 66 AND 70. REMOVED AND REPLACED FLOORBEAM -Y1292 IAW SRM 51-42-11. 2 L 7 2 4F RT A28NM 2007121100045 20071211 00045 NM 2007 12 11 F3LA200700353 1 20071114 A 5320 BLANKING PLATE AIRBUS A319 A319111 3930336 NM GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION AROUND L2 DOOR FWD GIRT BAR ATTACH BRACKET MOUNTING HOLES. REMOVED AN D REPLACED GIRT BAR BLANKING PLATE IAW AMM 52-11-31-000-005 AND 52-11-31-400-005. 2 L 7 2 4F RT A28NM 2007121100046 20071211 00046 NM 2007 12 11 F3LA200700354 1 20071114 A 5320 D5348015800400 BLANKING PLATE AIRBUS A319 A319111 3930336 NM GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED L2 DOOR AFT GIRT BAR BRACKET CORRODED AROUND ATTACH POINTS. REMOVED AND REPLACE D GIRT BAR BLANKING PLATE IAW AMM 52-11-31-000-005 AND 52-11-31-400-005. 2 L 7 2 4F RT A28NM 2007121100048 20071211 00048 GL 2007 12 11 UIEA200700441 2 20071015 A 7250 1538M90P12 BLADES GE BOEING 747 74747UF 1384812 NM GE CF6 CF680C2* GL HPT ROTOR CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 492MC 33524 18522 53X04890 29253 704890 ESN 704890 - HPT STAGE 1 BLADES 71 EA FOUND WITH UNDER PLATEFORM CORROSION AND CRACKS. 2 L 7 4 4F 4 F RT A20WE E23EA 2007121100049 20071211 00049 GL 2007 12 11 UIEA200700439 2 20071015 A 7250 1538M90P12 BLADE GE BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL HPT ROTOR CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 454PA 30007 17972 53X04272 30812 704330 ESN 704330 - HPT STAGE 1 BLADES 68EA FOUND WITH UNDER PLATEFORM CORROSION AND CRACKS. 2 L 7 4 4F 4 F RT A20WE E23EA 2007121100050 20071211 00050 NM 2007 12 11 UIEA200700442 1 20071010 A 5730 SKIN BOEING 747 74747UF 1384812 NM LT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 415MC 32837 DURING LEFT WING LIGHT REPLACEMENT THE PLATFORM SUDDENLY LOWERED AND HIT THE LEADING EDGE SKIN. THE PLATFORM MOVEMENT CA USED A 15 INCH VERTICAL CRACK. A TIME LIMITED REPAIR WAS ACCOMPLISHED AS PER XEO 57-101007 PART 1 AND SRM 57-41-01 REPA IR 4. PERMANENT REPAIR IS TO BE ACCOMPLISHED WITHIN 6 MONTH. NO ADDITIONAL DAMAGE FOUND. 2 L 7 4 4F RT A20WE 2007121100052 20071211 00052 NM 2007 12 11 UIEA200700444 1 20071001 A 5312 BULKHEAD BOEING 747 747228F 1384895 NM BS 260 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 RIGHT SIDE NOSE WHEEL WELL BULKHEAD WEB CRACKED AT STATION 260, WL 182 RBL 38. WEB REPAIRED AS PER BOEING MESSAGE 1-636 527780-4. 2 L 7 4 4F RT A20WE 2007121100053 20071211 00053 NM 2007 12 11 UIEA200700445 1 20070926 A 5350 FAIRING BOEING 747 747228F 1384895 NM FUSELAGE DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 FUSELAGE FAIRING 193C AREA OF DELAMINATION. DELAMINATED AREA REPAIRED AS PER SRM 51-40-12 2 L 7 4 4F RT A20WE 2007121100055 20071211 00055 NM 2007 12 11 UIEA200700447 1 20070930 A 5755 SKIN BOEING 747 747228F 1384895 NM NR 8 SPOILER CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 NR 8 SPOILER AREA OF UPPER SKIN AND REAR SPAR HAS AREA OF CORROSION. REPAIRED AS PER BOEING MESSAGE 1--638467931-2. 2 L 7 4 4F RT A20WE 2007121100057 20071211 00057 NM 2007 12 11 UIEA200700449 1 20070929 A 5711 SPAR CAP BOEING 747 747228F 1384895 NM RT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 RIGHT WING FRONT SPAR LOWER CHORD AREA BETWEEN FSSO 1322 AND 1340 CORRODED. CORROSION REMOVED AS PER SRM 51-10-01 AND B OEING MESSAGE 1-638497220-2. 2 L 7 4 4F RT A20WE 2007121100060 20071211 00060 NM 2007 12 11 UIEA200700455 1 20071019 A 5755 SKIN BOEING 747 7472D7B 1384803 NM NR 11 SPOILER DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 RT WING NR 11 SPOILER TRAILING EDGE HAS A 1.0 INCH BY 2.0 INCH AREA OF DELAMINATION. PERMANENT REPAIR WAS ACCOMPLISHED AS PER B747-200 SRM 51-40-06 FIG 3 AND 4, SHEET 1 AND SRM 51-40-20. ALSO, REFERENCE ATLAS EO NR 4757A399. 2 L 7 4 4F RT A20WE 2007121100067 20071211 00067 NM 2007 12 11 UIEA200700467 1 20071102 A 5730 65B145967 PANEL BOEING 747 7472D3B 1384805 NM LWS 170-630 DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 LT WING UPPER L/E FIXED PANEL BETWEEN AISLES 170.0 TO AISLES 630.72 HAS AN AREA DELAMINATION, AREA IS 58.0 INCH LONG BY 50.0 INCH WIDE. INTERIM REPAIR WAS ACCOMPLISHED AS PER B747-200 SRM 51-40-16 AND ATLAS AIR EO NR 4757A402 PART 4. PER FAA FORM 8110-3 REQUIRES DETAIL VISUAL INSPECTIONS AT EVERY "C" CHECK PER PART 5 OF EO NR 4757A402. 2 L 7 4 4F RT A20WE 2007121100068 20071211 00068 NM 2007 12 11 UIEA200700464 1 20071027 A 7830 DRIVE SYSTEM BOEING 747 7472D7B 1384803 NM THRUST REVERSER BROKEN A UIEA O OTHER P NO WARNING INDICATION LD LANDING 1 EA 15 523MC 21782 NR 3 REVERSER DID NOT DEPLOY DURING LANDING. NO AMBER THRUST REVERSER LIGHT. REVERSER WOULD NOT GO PAST INTERLOCK. IN SPECTED AND FOUND BROKEN DRIVE CABLE ON THE OUTBOARD SIDE OF NR 3 ENGINE. ITEM TRANSFERRED TO DMI M07-241 PER MEL 78-1- 5 CAT C LOCKED OUT PER DDPG. 2 L 7 4 4F RT A20WE 2007121100070 20071211 00070 NM 2007 12 11 UIEA200700463 1 20071024 A 5414 SKIN BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE NR 4 NACELLE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 21784 NR 4 PYLON LT SKIN WAS FOUND A CRACK AT THE 483 AL ACCESS PANEL CUTOUT LOWER AFT CORNER. DEFECTIVE CRACK AREA INTERIM R EPAIRED AS PER BOEING MESSAGE NR 1-656345659-3 AND ATLAS XEO NR 54-102307. 2 L 7 4 4F 4 F RT A20WE E23EA 2007121100072 20071211 00072 NM 2007 12 11 UIEA200700474 1 20071122 A 2750 65B1565111 PUSHROD BOEING 747 7472D7B 1384803 NM TE FLAP BROKEN A UIEA O OTHER O OTHER LD LANDING 1 EA 15 524MC 21784 AIRCRAFT EXPERIENCED HARD LANDING. PERFORMED HARD LANDING PHASE I INSPECTION. NOTED DEFECTS LISTED ON FOLLOWING LOG PA GES PER AMM 5-51-05, FOUND LEFT INBOARD FLAP NR 4 PUSH ROD BROKEN. REPLACED AND ADJUST PUSH ROD ASSY. ACCOMPLISHED PAR TS OF PHASE II INSPECTION AND DEFERRED REMAINDER OF THE PHASE II AFTER SPECIAL MAINTENANCE FERRY FLIGHT TO PIK TO COMPLE TE THE PHASE II INSPECTION. 2 L 7 4 4F RT A20WE 2007121100074 20071211 00074 NM 2007 12 11 UIEA200700469 1 20071109 A 5347 BAC15201566 SEAT TRACK BOEING 747 74747UF 1384812 NM BS 1850-1920 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 496MC 29257 MAIN DECK CARGO SIDE DOOR AREA, SEAT TRACK DAMAGED AND CRACKED AT STA 1850 AND 1920, LBL 99.0. PERMANENT REPAIR ACCOMPL ISHED AS PER B747-400 SRM 53-00-52 FIG 201, REPAIR 6. REFERENCE ATLAS AIR XEO NR 53-110607. 2 L 7 4 4F RT A20WE 2007121100075 20071211 00075 NM 2007 12 11 UIEA200700470 1 20071109 A 5310 65B1795118 SUPPORT BEAM BOEING 747 74747UF 1384812 NM CARGO DOOR CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 496MC 29257 MAIN DECK CARGO SIDE DOOR AREA, SUPPORT BEAM BETWEEN STA 1820-1840 AND 1840-1860 LBL 102.250, CRACKED AND DENTED. PERMA NENT REPAIR ACCOMPLISHED AS PER ATLAS AIR XEO 53-110607, BOEING DRAWING 65B17951 AND FAA FORM 8100-9. 2 L 7 4 4F RT A20WE 2007121100076 20071211 00076 NM 2007 12 11 UIEA200700461 1 20071022 A 2120 UNKNOWN BOEING 747 747243B 1384830 NM GALLEY AREA SMOKE A UIEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 517MC 23300 AT FL 380 (6.50 HOURS INTO FLIGHT) SMELLED ELECTRICAL SMOKE FROM UPPER DECK. COMPLETED ELECTRICAL SMOKE CHECKLIST LOCA TED ODOR FROM GALLEY AREA. REMOVED POWER FROM GALLEY SMOKE ODOR WENT AWAY. INSPECTED GALLEY AREA FOR DEFECTS PERFORMED DETAILED WIRING INSPECTION PER 20-60-00. TURNED ON GALLEY EQUIPMENT FOR 2 HOURS AND WAS UNABLE TO DUPLICATE. ALL GALL EY EQUIPMENT OPERATED NORMAL. 2 L 7 4 4F RT A20WE 2007121100078 20071211 00078 NM 2007 12 11 UIEA200700475 1 20071116 A 5315 FLOORBEAM BOEING 747 747243B 1384830 NM BS 620 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 AFTER REMOVAL OF MCD CEILING PANEL AT STA 620 FOUND UPPER FLOORBEAM LOWER CHORD AT BS 620 LBL 52 WL 300.8 HAS IMPACT DEN T. 4.5" LONG 1.5" WIDE. HFEC ACCOMPLISHED TO DAMAGED AREA PER NDT PARA 6 51-00-00 FIG 23. NO CRACK INDICATION FOUND. LOWER CHORD REPAIRED PER ATLAS AIR XEO 53-111607. 2 L 7 4 4F RT A20WE 2007121100081 20071211 00081 CE 2007 12 11 1357141120307 1 20071203 A 8120 4066109028 TURBOCHARGER CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO LT ENGINE FAILED E HYIA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NE 01 2714M 1907 1907 402C0211 832084R PILOT LOG READS THE FOLLOWING: LEFT ENG SMOKES ON APPROACH. MAINTENANCE INSPECTED AND FOUND TURBO TO HAVE FAILED. MAIN TENANCE REMOVED AND REPLACED THE TURBO. 1 L 7 2 3O 3 O A7CE E8CE 2007121100084 20071211 00084 NM 2007 12 11 HALA0700512 1 20071130 A 5280 SEAL BOEING 767 7673G5 1385126 NM NLG DOOR OUT OF ADJUST A HALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 586HA 24259 LDG GEA MONITOR, STATUS MESSAGE DISPLAYED IN FLIGHT. PERFORMED FIM 32-61-00 ADJUSTED LEFT FWD NOSE LANDING GEAR DOOR SE AL AND RIGHT FWD NOSE LANDING GEAR DOOR SEAL PER AMM 32-22-02. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007121100089 20071211 00089 2007 12 11 UPS07M51237 4 20071202 A 2565 SLIDE DOUG MD11 MD11F 3023600 NM R1 DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 279UP 48573 R1 SLIDE DAMAGED, R1 SLIDE DEACTIVATION PIN INSTALLED. REF TO WAN 1300451 REMOVED AND REPLACED SLIDE ON R1 DOOR IAW AM CH 25-61-15 & TC 8033. REMOVED DEACTIVATION PIN. 2 L 7 3 4F RT A22WE 2007121100090 20071211 00090 WP 2007 12 11 ASAA0782295 1 20071201 A 5311 591359577 FRAME DOUG DC9 DC983 3022083 WP BS 1418 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 961AS 53075 AFT A C BAY FRAME 1418 CRACKED AT LONGERON 2 RIGHT REPAIRED AFT A C BAY FRAME 1418 IAW MD80 SRM 53 03 FIG 31A. STOP DRI LLED CRACK, INSTALLED REPAIR ANGLES. LOCATED AND DRILLED 2 EACH 37 AND 1 EA 35. REPAIR ANGLES AND STRAP INSTALLED PER FIG 31A. 2 L 7 2 4F RT A6WE 2007121100092 20071211 00092 EA 2007 12 11 TRAX200701840 1 20071129 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 826AS 7210 F/A STATION EXIT LIGHT ASSY IS CRACKED AND BROKEN. 2 L 7 2 4F RT A21EA 2007121100097 20071211 00097 NM 2007 12 11 SA07078 1 20071201 A 3350 321454 BATTERY AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 826AW 1534 ATL - THE LEFT EMERGENCY LIGHTS FORWARD BATTERY WAS INOPERATIVE. MAINTENANCE REPLACED THE LEFT FORWARD EMERGENCY BATTER Y. 2 L 7 2 4F RT A28NM 2007121100098 20071211 00098 NM 2007 12 11 F3LA200700357 1 20071110 A 3350 321430 BATTERY AIRBUS A319 A319111 3930336 NM EMERGENCY LIGHTS FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 908FR 1759 DURING C4/S1 CHECK, INSPECTION REPORTED LT OVERWING EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED EMERGENCY BA TTERY FROM POWER SUPPLY UNIT 11WL IAW AMM 33-51-38-000-002. INSTALLED SERVICEABLE BATTERY IAW AMM 33-51-38-400-002. PE RFORMED OPERATIONAL CHECK IAW AMM 33-51-00-710-001. OPS CHECK NORMAL. 2 L 7 2 4F RT A28NM 2007121100099 20071211 00099 NM 2007 12 11 F3LA200700358 1 20071110 A 3350 321430 BATTERY AIRBUS A319 A319111 3930336 NM EMERGENCY LIGHTS FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 908FR 1759 DURING C4/S1 CHECK, INSPECTION REPORTED FWD LT EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED EMERGENCY BATTERY FROM POWER SUPPLY UNIT 10WL IAW AMM 33-51-38-000-002. INSTALLED SERVICEABLE BATTERY IAW AMM 33-51-38-400-002. PERFORM ED OPERATIONAL TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00-710-001. OPS TEST NORMAL. 2 L 7 2 4F RT A28NM 2007121100103 20071211 00103 2007 12 11 MALA070189 2 20071124 A 7297 WIRE HARNESS SAAB SF340 340B 7860101 EU RT ENGINE UNKNOWN A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 435XJ 340B435 DURING LANDING IN DTW, WHEN THE POWER LEVERS WERE RETARDED, THE RT PROP AUTOCOARSENED. CREW CONTINUED THE LANDING AND P OWER RETURNED TO RT ENGINE DURING TAXI. REMOVED AND REPLACED RT ENGINE RT AIRFRAME HARNESS, PN: 7292533-681 AND STARTER GEN, PN: 23080-031, SN OFF: 3486, SN ON: 2680 IAW SAAB TASK CARD 243103 AND SAAB 340B POWERPLANT BUILDUP MANUAL. SEE M M 409 286623 FOR FURTHER DETAILS. 2 L 7 2 4T RT A52EU 2007121100105 20071211 00105 NM 2007 12 11 ASAA0792299 1 20071129 A 5320 146A750218 ANGLE BOEING 737 737990 NM BS 727-727I CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 302AS 30017 AFT CARGO PIT RT 'Z' ANGLE HAS CORROSION FROM BS 727+4 TO 727I+8 AFT CARGO PIT. RT 'Z' ANGLE REPLACED AT BS 727+4 TO 72 7I+8 RBL 21 IAW B 737 900 SRM 53 00 53. 2 L 7 4 4F RT A16WE 2007121100106 20071211 00106 NM 2007 12 11 ASAA0792300 1 20071129 A 5320 146A750219 ANGLE BOEING 737 737990 NM BS 727-847 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 302AS 30017 AFT CARGO PIT LT 'Z" ANGLE AT BS 727+4 TO BS 847 LBL 21 HAS CORROSION ON VARIOUS LOCATION AFT CARGO PIT LT "Z' ANGLE AT BS 727 +4 TO BS 847. REPLACED IAW B 737 900 SRM 53 00 53. 2 L 7 4 4F RT A16WE 2007121100107 20071211 00107 NM 2007 12 11 ASAA0792301 1 20071130 A 5320 143A7501161 ANGLE BOEING 737 737990 NM BS 500-500L CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 302AS 30017 FWD CARGO PIT RT SIDE FLOOR SUPPORT 'Z' ANGLE FOUND CORROSION FROM BS 500-500L FWD CARGO PIT RT SIDE FLOOR SUPPORT 'Z' A NGLE REPLACED AT BS 500-500L IAW B 737 900 SRM 53 00 53. 2 L 7 4 4F RT A16WE 2007121100108 20071211 00108 NM 2007 12 11 ASAA0792302 1 20071130 A 5320 143A7501134 ANGLE BOEING 737 737990 NM BS 500-500L CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 302AS 30017 FWD CARGO PIT LT SIDE FLOOR SUPPORT 'Z' ANGLE FOUND CORROSION FROM BS 500 TO 500 L FWD CARGO PIT LT SIDE 'Z' ANGLE AT BS 500 TO 500D FOUND TO BE WIITHIN ALLOWABLE LIMITS IAW B 737 900 SRM 53 00 53 ALLOWABLE LIMITS DAMAGE 1 AND BS 500 D TO B S 500 L. REPLACED IAW B 737 900 SRM 53 00 53. 2 L 7 4 4F RT A16WE 2007121100110 20071211 00110 NM 2007 12 11 ASAA0792304 1 20071130 A 5320 143A75101 FLOOR SUPPORT BOEING 737 737990 NM BS 500G-500H BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 302AS 30017 FWD CARGO PIT FLOOR SUPPORT INTERCOSTAL AT BS 500G TO 500H RBL 24 FOUND BROKEN FWD CARGO PIT FLOOR SUPPORT INTERCOSTAL A T BS 500G TO 500H RBL 24. REPLACED WITH MADE REPAIR PART IAW B 737 900 SRM 53 30 53. 2 L 7 4 4F RT A16WE 2007121100111 20071211 00111 NM 2007 12 11 ASAA0792305 1 20071130 A 5320 143A75101 FLOOR SUPPORT BOEING 737 737990 NM BS 500H-500I CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 302AS 30017 FWD CARGO PIT FLOOR SUPPORT INTERCOSTAL AT BS 500 H TO BS 500I LBL 24 FOUND CRACKED FWD CARGO PIT FLOOR SUPPORT INTERCOS TAL AT BS 500H TO BS 500I LBL 24. REPLACED WITH MADE REPAIR PART IAW B 737 900 SRM 53 30 53. 2 L 7 4 4F RT A16WE 2007121100114 20071211 00114 NM 2007 12 11 ASAA0772313 1 20071128 A 5347 CARGO TRACK BOEING 737 737790 13844CN NM BS 767-847 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 AFT CARGO CORROSION ON CARGO TIEDOWN TRACK RBL 13.84 BS 767 TO 847 TIE DOWN TRACK REPLACED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2007121100116 20071211 00116 NM 2007 12 11 ASAA0772315 1 20071123 A 5320 146A75022 FLOOR SUPPORT BOEING 737 737790 13844CN NM BS 727-767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 AFT CARGO PIT CORROSION ON FLOOR SUPPORT ZEE CHANNEL RBL 22 BS 727+4 TO 767 ZEE CHANNEL REPLACED. 2 L 7 2 4F RT A16WE 2007121100119 20071211 00119 NM 2007 12 11 ASAA0772318 1 20071120 A 5320 143A75011 CHANNEL BOEING 737 737790 13844CN NM BS 438-500D CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 FWD CARGO PIT LT ZEE CHANNEL BS 500D TO 438 LBL 21 REPLACED CORRODED SECTION FROM BS 438 TO 500D WITH MADE REPAIR PART I AW B737 700 SRM 53 00 53 REPAIR E FIG 202. 2 L 7 2 4F RT A16WE 2007121100121 20071211 00121 NM 2007 12 11 ASAA0772320 1 20071120 A 5321 146A94014 FLOOR PANEL BOEING 737 737790 13844CN NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 AFT CARGO PIT FLOOR PANEL SPLICE TEE CORRODED BS 767+6 SPLICE TEE REPLACED. 2 L 7 2 4F RT A16WE 2007121100124 20071211 00124 NM 2007 12 11 ASAA0772323 1 20071130 A 5347 146A750125 CARGO TRACK BOEING 737 737790 13844CN NM BS 747 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 AFT CARGO PIT CORROSION ON CARGO TIE DOWN TRACK BS 747 RBL I5 REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2007121100125 20071211 00125 NM 2007 12 11 ASAA0772324 1 20071121 A 5347 146A75036 CARGO TRACK BOEING 737 737790 13844CN NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 AFT CARGO PIT CORROSION ON FLOOR SUPPORT RAIL AT EXISTING REPAIR BS 767 + 8 RBL 8 FLOOR SUPPORT RAIL REPLACED. 2 L 7 2 4F RT A16WE 2007121100126 20071211 00126 NM 2007 12 11 ASAA0772325 1 20071129 A 5347 146A75031 CARGO TRACK BOEING 737 737790 13844CN NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 AFT CARGO PIT CORROSION ON FLOOR SUPPORT RAIL BS 767+6 LBL 3 REPAIRED WITH MADE REPAIR PARTS. 2 L 7 2 4F RT A16WE 2007121100127 20071211 00127 NM 2007 12 11 ASAA0772311 1 20071130 A 5320 453A26112 PLATE BOEING 737 737790 13844CN NM BS 867 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 AFT CARGO PIT AFT TIEDOWN SCUFF PLATE BS 867 CORRODED REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2007121100129 20071211 00129 NM 2007 12 11 ASAA0792297 1 20071201 A 5753 113A37008 SKIN BOEING 737 737990 NM RT WING TE FLAP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 302AS 30017 RT OUTBD AFT FLAP INBD T C CORNER DELAM RT O/B AFT FLAP REPAIRED IAW B737 900 SRM CH 51 70 10 RT O/B AFT FLAP, INSTALLED AND RIGGED ON A C 617 MIG NR 5. 2 L 7 4 4F RT A16WE 2007121100130 20071211 00130 NM 2007 12 11 ASAA0792298 1 20071201 A 5753 113A37007 SKIN BOEING 737 737990 NM LT WING TE FLAP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 302AS 30017 LT OUTBD AFT FLAP INBD T C CORNER DELAM LT O/B AFT FLAP REPAIRED IAW B737 900 SRM CH 51 70 10. 2 L 7 4 4F RT A16WE 2007121100131 20071211 00131 NM 2007 12 11 ASAA0792307 1 20071124 A 5750 SUPPORT BOEING 737 737990 NM LT WING TE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 302AS 30017 LT FIXED TRAILING EDGE AFT OF NACELLE CENTER SUPPORT IS CRACKED WS 278.5 LT WING FIXED TRAILING EDGE AFT OF NACELLE CENT ER SUPPORT WEB REPLACED IAW B737 900 SRM 51 40 02. 2 L 7 4 4F RT A16WE 2007121100132 20071211 00132 NM 2007 12 11 ASAA0792308 1 20071124 A 5750 SUPPORT BOEING 737 737990 NM RT WING TE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 302AS 30017 RT WING FIXED TRAILING EDGE AFT OF NACELLE CENTER SUPPORT IS CRACKED WS 278.5 (FWD AND AFT) RT WING FIXED TRAILING EDGE AFT OF NACELLE FWD AND AFT CENTER WEB SUPPORTS REPLACED IAW 737 900 SRM 51 40 02. 2 L 7 4 4F RT A16WE 2007121100134 20071211 00134 NM 2007 12 11 NWAA073876302 1 20071108 A 5330 SKIN BOEING 747 747451 1384940 NM BS 2285 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 662US 23720 DURING "L" CHECK FOUND CRACK IN FUSELAGE SKIN AT UPPER AFT CUTOUT FOR NR 5 RT DOOR AT BS 2285. REPAIRED PER EA 63-21088 4. 2 L 7 4 4F RT A20WE 2007120700006 20071207 00006 NM 2007 12 7 DL76S071518 1 20071120 A 5512 SKIN BOEING 767 767332 1382001 NM HORIZONTAL STAB DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 121DE 23435 TOOLING DAMAGE TO UPPER HORIZONTAL STAB SKIN AND FRONT SPAR UPPER CHORD AT SPAR STA 27. DAMAGE WAS CUTOUT AND REPAIR DO UBLER INSTALLED. 2 L 7 2 4F RT A1NM 2007120700008 20071207 00008 NM 2007 12 7 DL757071520 1 20071119 A 5330 146N333014 SKIN BOEING 757 757232 1384965 NM FS 1338 S26L DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 6713Y 30777 LIGHTNING STRIKE TO LAP JOINT UPPER SKIN AT FS 1338, STR 26L. CUT OUT DAMAGE AND INSTALLED DOUBLER. 2 L 7 2 4F RT A2NM 2007120700022 20071207 00022 NM 2007 12 7 DLM88071538 1 20071103 A 5712 RIB DOUG MD88 MD88 3023688 NM LWS 446 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 CRACK ON LT WING FIXED LEADING EDGE RIB STA XFS=446. RIB REPLACED PER DWG 9919329-7. 2 L 7 2 4F RT A6WE 2007120700025 20071207 00025 NM 2007 12 7 DLM88071541 1 20071108 A 5320 SCUFF PLATE DOUG MD88 MD88 3023688 NM CARGO BAY BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 WEAR DEFORMED AND BROKEN SCUFF PLATE OF AFT CARGO BIN. REPLACED SCUFF PLATE PER DWG 5936070. 2 L 7 2 4F RT A6WE 2007120700031 20071207 00031 NM 2007 12 7 DLM88071547 1 20071022 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 508 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 CORROSION ON RT CUSP WEB AT STA Y=508, REPLACED SECTION OF WEB PER DWG 9930538. 2 L 7 2 4F RT A6WE 2007120700032 20071207 00032 NM 2007 12 7 DLM88071548 1 20071102 A 5340 ATTACH FITTING DOUG MD88 MD88 3023688 NM BS 1155 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 CORROSION ON STRUCTURE AT STA 1155 BTWN LONGERON 29 AND 28 RT. REPLACED CLIP PER DWG 9936073. 2 L 7 2 4F RT A6WE 2007120700049 20071207 00049 EA 2007 12 7 MALA070184 1 20071122 A 3350 2013BR BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 905XJ 15137 DURING OTHER MAINTENANCE NOTED EMERGENCY LIGHT SWITCH WAS LEFT ON BY FLIGHT CREW AND EMERGENCY LIGHTS DIM/INOPERATIVE BA TTERY PACKS REQUIRE REPLACEMENT. REMOVED AND REPLACED ALL 5 BATTERY PACKS. 2 L 7 2 4F RT A21EA 2007120700079 20071207 00079 EU 2007 12 7 07FDEA04948 1 20071127 A 5347 R5307008820200 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 671FE 778 MCC SEAT TRACK SECTION 3 R HAS CORROSION AT FRAMES FR 64.5 , 65.5 , AND 66. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 53-10-16. INSTALLED NEW SEAT TRACK, SECTION AND REPAIR SPLICES IAW A300-600 SRM 53-10-16 FROM FR 64 TO FR 68. 2 L 7 2 4F RT A35EU 2007120700082 20071207 00082 EU 2007 12 7 07FDEA04951 1 20071127 A 5310 CROSSBEAM AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 671FE 778 FWD CARGO COMPT MAIN CABIN CROSSBEAM C-27 BETWEEN RT SEAT TRACK 2-3 CRACKED ON VERTICAL STIFFENER UPPER CONTOUR APPROX 1 /4 IN LONG. REPAIRED CROSSBEAM C-27 BETWEEN RT SEAT TRACK 2-3 IAW A300-600 FSRM 53-10-15. 2 L 7 2 4F RT A35EU 2007120700084 20071207 00084 EU 2007 12 7 07FDEA04953 1 20071128 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT CARGO PIT BILGE AREA, STR 54L CORRODED BETWEEN FR 58 AND 59 ( X3143 TO X3196 ). REMOVED COUPLING AND STRINGER. REM OVED ATTACH ANGLE. FABBED STRINGER SECTION IAW SRM 53-10-14. FABBED COUPLING IAW SRM 53-10-14. ALODINED COUPLING AND STRINGER IAW SRM 53-21-10. PRIMED AND PAINTED IAW SRM 51-23-10 INSTALLED COUPLING AND STRINGER IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007120700088 20071207 00088 EU 2007 12 7 07FDEA04957 1 20071128 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT CARGO PIT, STRINGER 53L CORRODED BETWEEN FRAME 54.3 AND FRAME 58 (STA X3090 TO STA X3143 ). REPAIRED STRINGER 53L A T FRAME 54.3 TO FRAME 58 IAW A310 SRM 53-10-14 PG 204A/204B FIG 201A. 2 L 7 2 4F RT A35EU 2007120700100 20071207 00100 NM 2007 12 7 QXEA200701768 1 20071128 A 5310 DOOR FRAME BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 416QX 4083 YVR FLIGHT: A HOLE IN THE REAR CARGO DOOR JAM WAS FOUND BEHIND THE DOOR SUPPORT BRACE FIXTURE. MAINTENANCE REPAIRED THE HOLE PER QX SUPPLEMENT 25-52-19: 'GILLPATCH III INSTALLATION'. FUNCTIONAL CHECK OF THE AFT BAGGAGE DOOR AND ROD WAS GO OD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007120700104 20071207 00104 WP 2007 12 7 07FDEA04962 1 20071129 A 5730 ARB23122 SKIN DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 RT WING DROOPED FOUND CRACK ON UPPER EXTERNAL SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 55 VOL I. 2 L 7 3 4F A22WE 2007120700108 20071207 00108 EU 2007 12 7 TRBA2007106 1 20071127 A 2913 8210308 PUMP AEROSP ATR72 ATR72212 8680945 EU HYD SYSTEM FAILED A TRBA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SO 29 348AE 349 NR 1 ENGINE OIL PRESSURE FLUCTUATING BETWEEN 50 AND 40 PSI. PRECAUTIONARY ENGINE SHUT DOWN PERFORMED. EMERGENCY DECLAR ED AND AIRCRAFT LANDED UNEVENTFULLY AT RSW. REMOVED AND REPLACED HYDRAULIC PUMP AND OVERSPEED GOVERNOR IAW MM NR 61-12- 63 AND NR 61-23-61. PERFORMED OPS RUN CHECK. OPS CHECK GOOD. 2 H 7 2 4T RT A53EU 2007120700114 20071207 00114 NM 2007 12 7 HALA0700504 1 20071126 A 2612 89873202 CIRCUIT CARD BOEING 767 7673G5 1385126 NM FIRE DECTECTION MALFUNCTIONED A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 585HA 24257 STATUS MESSAGE APU FIRE LP 2. REPLACED NR 2 APU FIRE DETECTION CARD PER FIM 26-15-00 FIGURE 103, OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007120700115 20071207 00115 NM 2007 12 7 HALA0800504 1 20071126 A 2612 89873202 CIRCUIT CARD BOEING 767 7673G5 1385126 NM FIRE DETECTION MALFUNCTIONED A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, STATUS MESSAGE APU FIRE LP 2. REPLACED NR 2 APU FIRE DETECTION CARD PER FIM 26-15-00 FIGURE 1 03, OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007120700122 20071207 00122 2007 12 7 SIMA200733404 4 20071129 A 3418 SENSOR EMB 145 EMB145LR 3260212 SO AOA BROKEN A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 633AE 145148 ABORTED TAKEOFF AT 80 KTS FOR WARNING SPS 1 INOP MESSAGE. ON POST FLIGHT INSPECTION, FOUND AOA 1 VANE BROKEN. REMOVED AND REPLACED NR 1 AOA SENSOR IAW EMB145 AMM 27-36-00 BECAUSE VANE ON AOA SENSOR DAMAGED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007120700127 20071207 00127 NM 2007 12 7 AMTA200700652 1 20071127 A 2150 CONTROLLER BOEING 757 75723N 1384973 NM RT A/C PACK MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 517AT 27973 EICAS MSG R PACK OFF AND PACK TEMP DISPLAYED. R INOP AND PACK OFF LIGHTS ILLUMINATED. LIGHTS EXTINGUISHED WHEN PACK RE SET SWITCH IN STANDBY. OPS NORMAL IN STUDY. PERFORMED BITE CHECK ON RIGHT PACK CONTROLLER PER FIM 21-51-14-745-001 FIG 501. NO FAULTS NOTED. OPS CHECK NORMAL. VERIFICATION FLT REQ`D. (M) 2 L 7 2 4F RT A2NM 2007120700129 20071207 00129 EA 2007 12 7 SWIA200718902 1 20071126 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 755SK 10220 FLT 5909 - FLOOR LEVEL FLOOD LIGHT IN GALLEY IS INOP. REPLACED FLOOR LEVEL FLOODLIGHT ASSEMBLY IAW CRJ 700 MM 33-51-11. 2 L 7 2 4F RT A21EA 2007120700142 20071207 00142 EU 2007 12 7 MALA070188 1 20071130 A 3350 330151 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS NO TEST A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 450XJ 340B450 DURING TASK 335003, POWER SUPPLY 24LN FAILED CAP TEST. REPLACED POWER SUPPLY 24LN, P/N 3301-51; S/N 2062. 2 L 7 2 4T RT A52EU 2007120700146 20071207 00146 NM 2007 12 7 F3LA200700330 1 20071114 A 5320 BLANKING PLATE AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED R2 DOOR AFT GIRT BAR BRACKET CORRODED AROUND ATTACH POINTS. REMOVED AND REPLACE D R2 DOOR AFT BLANKING PLATE IAW AMM 52-11-31-400-005. 2 L 7 2 4F RT A28NM 2007120700151 20071207 00151 NM 2007 12 7 F3LA200700331 1 20071114 A 5320 BLANKING PLATE AIRBUS A319 A319111 3930336 NM FUSLEAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED R2 DOOR FWD GIRT BAR BRACKET CORRODED AROUND ATTACH POINTS. REMOVED AND REPLACE D R2 DOOR GIRT BAR BLANKING PLATE IAW AMM 52-11-31-400-005. 2 L 7 2 4F RT A28NM 2007120700161 20071207 00161 NM 2007 12 7 USAA920071236 1 20071127 A 5340 6926555 ATTACH FITTING BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CRACKED FRAME CHANNEL CLIP, BS 344, S16L. REPLACED FRAME CHANNEL CLIP, BS 344, S16L IAW BOEING DRAWING 69-26555. 2 L 7 2 4F RT A16WE 2007120700185 20071207 00185 NM 2007 12 7 AALA20072287 1 20071125 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 779AN 29955 MIA - EMERGENCY LIGHT AT SEAT 32C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 32C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120700192 20071207 00192 WP 2007 12 7 AALA20072275 1 20071122 A 3350 LENS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 76200 53290 SFO - EMERGENCY LIGHT AT OVERHEAD SEAT 9D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007120700197 20071207 00197 NM 2007 12 7 AALA20072266 1 20071122 A 2560 BATTERY BOEING 777 777223 1385213 NM FLASHLIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 LHR - EMERGENCY FLASHLIGHT AT LEFT NUMBER TWO DOOR FORWARD INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT LE FT NUMBER TWO DOOR FORWARD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120700202 20071207 00202 NM 2007 12 7 AALA20072289 1 20071125 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 198AA 32392 MIA - EMERGENCY LIGHT AT SEAT 30C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 30C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2007120700205 20071207 00205 NM 2007 12 7 AALA20072282 1 20071124 A 3350 0201984002 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 360AA 24041 JFK - EMERGENCY LIGHT AT MID GALLEY MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT MID GALLEY. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007120700208 20071207 00208 NM 2007 12 7 AALA20072272 1 20071122 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 760AN 31477 DFW - EMERGENCY LIGHT AT SEAT 22C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120700216 20071207 00216 NM 2007 12 7 F3LA200700343 1 20071115 A 5315 STRUCTURE AIRBUS A319 A319111 3930336 NM FLOORBEAM CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED CONNECTING SECTION ASSY (BROWN PIECE THAT GOES UNDER THE FLOOR PANEL AND UP THE SIDE OF THE FLOOR PANEL) CORRODED AT FR66. INSTALLED REPLACEMENT SECTION ASSY IAW SRM 51-42-11, PARA 5. 2 L 7 2 4F RT A28NM 2007121100010 20071211 00010 EA 2007 12 11 TRAX200701817 1 20071128 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 978EV 7723 ASD LOWER BOTTOM STEP CRACKED. 2 L 7 2 4F RT A21EA 2007121100013 20071211 00013 EU 2007 12 11 TRAX200701788 1 20071127 A 5313 STRINGER AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 FOUND STRINGER 17L CORRODED BTW FR 36-38. REPAIR ACOMPLISHED IN ACCORDANCE WITH SRM 51-21-42 2 H 7 2 4T RT A53EU 2007121100024 20071211 00024 EU 2007 12 11 TRAX200701796 1 20071127 A 5300 UNKNOWN AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 RT FR 37 CORRODED AT FLOOR LEVEL. RT FR 37 AT FLOOR LEVEL CORROSION REMOVED AS PER SRM 51-21-42 FABRICATION OF FR 37 R EPAIERD PARTS COVER ON W/C 2000-245 FR 37 REPAIRED IAW SRM 53-67-70 FIG 402 MATERIAL THICKNESS: 0.080 MATERIAL REMOVE D: 0.030 OUT OF LIMITS AS PER SRM: 53-61-00 FIG 301. 2 H 7 2 4T RT A53EU 2007121100036 20071211 00036 EU 2007 12 11 TRAX200701809 1 20071127 A 5320 BRACKET AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 ON RT SIDE AT FR 37 BTW STGR 14R-13R OMEGA BRACKET FOUND CRACKED. 2 H 7 2 4T RT A53EU 2007121100051 20071211 00051 NM 2007 12 11 UIEA200700443 1 20070929 A 5415 BRACE BOEING 747 747228F 1384895 NM NACELLE CHAFED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 NR 4 STRUT DIAGONAL BRACE FORWARD END CHAFED. CHAFING AREA DAMAGE BLENDED AS PER BOEING MESSAGE 1-636565614-4. 2 L 7 4 4F RT A20WE 2007121100054 20071211 00054 NM 2007 12 11 UIEA200700446 1 20071001 A 5340 FITTING BOEING 747 747228F 1384895 NM BS 230 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 BS 230 RBL 1 BILGE AREA BEAM WEB SUPPORT FITTING CORRODED. REPLACED FITTING AS PER SRM 51-10-01 AND BOEING MESSAGE 1-63 7033946-3. 2 L 7 4 4F RT A20WE 2007121100061 20071211 00061 NM 2007 12 11 UIEA200700456 1 20071019 A 5730 PANEL BOEING 747 7472D7B 1384803 NM RT WING DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 RT WING UPPER SURFACE L/E FIXED PANEL AT WING STA 526.0 HAS A 3.0 INCH BY 4.0 INCH AREA OF DELAMINATION. PERMANENT REPA IR WAS ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18, SHEETS 1 THRU 5 AND SRM 51-40-12. ALSO, REFERENCE ATLAS AIR EO NR 4757A400. 2 L 7 4 4F RT A20WE 2007121100065 20071211 00065 NM 2007 12 11 UIEA200700472 1 20071116 A 5730 65B144604 PANEL BOEING 747 7472D3B 1384805 NM RWS 199-263 DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 21252 RT WING LEADING EDGE, INBOARD OF LANDING LIGHTS, INTERIOR AREA OF LEADING EDGE, COMPOSITE SKIN IS DELAMINATED. AREA IS 64.0 INCH BY 20.0 INCH. INTERIM REPAIR WAS ACCOMPLISHED AS PER B747-200 SRM 57-30-02, FIG 10 AND SRM 51-40-09, FIG 18, REFERENCE ATLAS AIR XEO NR 57-111607 AND FAA FORM 8110-3. 2 L 7 4 4F RT A20WE 2007121100069 20071211 00069 NM 2007 12 11 UIEA200700465 1 20071026 A 5730 PANEL BOEING 747 7472D3B 1384805 NM LT WING DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 UPPER SURFACE OF LEFT WING INBOARD NR 2 ENGINE FIBERGLASS HAS HOLE AND DENT. REPAIRED PER XEO 57-102607 TRANS TO NON ME L N07-126. REINSPECTED IN ORD AND ACCOMPLISHED XEO 57-102607 PART 3 IAW SRM 51-40-16. REPAIRED AND TO BE INSPECTED EVE RY 10 FLIGHT CYCLES UNTIL PERM REPAIR IS ACCOMPLISHED AT THE NEXT "A" CHECK. 2 L 7 4 4F RT A20WE 2007121100073 20071211 00073 NM 2007 12 11 UIEA200700468 1 20071109 A 5410 STRUCTURE BOEING 747 74747UF 1384812 NM LT NACELLE ERODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 496MC 29257 NR 2 ENGINE LT FAN COWL L/E HAS 78.0 INCH AREA OF EROSION AT L/E. PERMANENT REPAIR ACCOMPLISHED AS PER B747-400 SRM 54- 21-01, REPAIR 6. REFERENCE ATLAS EO NR 4471A009. 2 L 7 4 4F RT A20WE 2007121100077 20071211 00077 NM 2007 12 11 UIEA200700480 1 20071128 A 5753 SKIN BOEING 747 74747UF 1384812 NM TE FLAPS DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 492MC 29253 THREE SEPARATE ITEMS OF DAMAGE TO LT IB AFT FLAP AND MID FLAP: A) TEAR IN LT IB MID FLAP AFT PANEL 0.800" LONG BY 0.500 HIGH. ALLOWABLE DAMAGE PER SRM 51-70-02. TEAR IN ALUM SKIN UPPER SURFACE RUB STRIP LT IB AFT FLAP 0.600 INCH TEAR WITH CRACKS EMANATING FROM EITHER END 0.200" OB END AND 0.150" IB END. IMPACT DAMAGE TO T/E OF LT IB AFT FLAP 0.650" LONG B Y 0.200" HIGH. 2 L 7 4 4F RT A20WE 2007121100080 20071211 00080 CE 2007 12 11 1352714120307 1 20071126 A 8011 642085A15R ADAPTER CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO STARTER FAILED E HYIA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 61 2714B 1027 1027 402C0210 832024R PILOT DISCREPANCY OF RIGHT ENGINE DOES NOT SPIN ON START. AIRCRAFT WAS AT GATE IN SJU. MAINTENANCE FOUND A STARTER ADA PTER GEAR TOOTH AND ENGINE START GEAR TOOTH FAILURE. MAINTENANCE REMOVED AND REPLACED THE ENGINE. 1 L 7 2 3O 3 O A7CE E8CE 2007121100085 20071211 00085 EU 2007 12 11 UPS07151228 1 20071129 A 2560 GIRT BAR AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DETACHED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 140UP 0823 EMERGENCY SLIDE GIRT BAR BECAME DETACHED AT FORWARD POINT. DEFERRED SLIDE PER MM 52-11-01-3. SECURED GIRT BAR UNDER DO OR WITH SAFETY WIRE. FORWARD SLIDER IN PFM BOX. REINSTALLED DOOR SLIDE REF MM 25-61-21. OPS CHECKS GOOD. THIS CLEARS D363555. 2 L 7 2 4F RT A35EU 2007121100091 20071211 00091 WP 2007 12 11 ASAA0782293 1 20071129 A 5751 SKIN DOUG DC9 DC983 3022083 WP AILERON DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 961AS 53075 RT AILERON IS DELAMINATED AT THE O/B ATTACH POINT LOWER SURFACE PREPPED AREA. FABRICATED AND BONDED REPAIR PLIES IAW MD 80 SRM 51 90 0 8N PG 72. 2 L 7 2 4F RT A6WE 2007121100096 20071211 00096 NM 2007 12 11 SB07102 1 20071203 A 3350 7003661 BALLAST BOEING 737 737401 1384701 NM OVERWING LIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 THE AFT LEFT OVER-WING EXIT LIGHT ASSEMBLY IS INOPERATIVE. MAINTENANCE REPLACED THE AFT LEFT OVERWING EXIT LIGHT ASSEMB LY. OPS CHECK OK. 2 L 7 2 4F RT A16WE 2007121100100 20071211 00100 NM 2007 12 11 F3LA200700355 1 20071111 A 5310 FASTENER AIRBUS A319 A319111 3930336 NM WINDOW CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 1759 DURING C4/S1 CHECK, INSPECTION REPORTED SCREWS RUSTY AROUND THE OUTSIDE OF THE FIRST OFFICER'S RT AFT FIXED COCKPIT WIND OW. REMOVED FIXED WINDOW IAW AMM 56-11-12-000-001. INSTALLED FIXED WINDOW IAW AMM 56-11-12-000-002. PERFORMED OPS TES T OF WINDOW HEAT SYSTEM IAW 30-42-00-710-001. OPS CHECKED NORMAL. 2 L 7 2 4F RT A28NM 2007121100101 20071211 00101 NM 2007 12 11 F3LA200700356 1 20071110 A 3350 321430 BATTERY AIRBUS A319 A319111 3930336 NM EMERGENCY LIGHTS FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 908FR 1759 DURING C4/S1 CHECK, INSPECTION REPORTED RT OVERWING EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED EMERGENCY BA TTERY FROM POWER SUPPLY UNIT 12WL IAW AMM 33-51-38-000-002. INSTALLED SERVICEABLE BATTERY IAW AMM 33-51-38-400-002. PE RFORMED OPERATIONAL TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00-710-001. OPS TEST NORMAL. 2 L 7 2 4F RT A28NM 2007121100102 20071211 00102 NM 2007 12 11 F3LA200700359 1 20071110 A 3350 321430 BATTERY AIRBUS A319 A319111 3930336 NM EMERGENCY LIGHTS FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 908FR 1759 DURING C4/S1 CHECK, INSPECTION REPORTED AFT EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED EMERGENCY BATTERY FR OM POWER SUPPLY UNIT 13WL IAW AMM 33-51-38-000-002. INSTALLED SERVICEABLE BATTERY IAW AMM 33-51-38-400-002. PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00-710-001. OPS TEST NORMAL. 2 L 7 2 4F RT A28NM 2007121100104 20071211 00104 NM 2007 12 11 ASAA0792309 1 20071127 A 5320 141A851218 WEB BOEING 737 737990 NM BS 3237-3512 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 302AS 30017 GOUGE FOUND ON E/E EQUIPMENT COMPT ACCESS DOOR SURROUND WEB BETWEEN STA 323.7 TO 351.2 AND LBL 24. GOUGE FOUND ON E/E E QUIPMENT COMPT ACCESS DOOR SURROUND WEB BETWEEN STA 323.7 TO 351.2 LBL 6.74 BEYOND LIMITS. REPLACED WITH MADE REPAIR PA RT IAW B737 900 SRM 51 40 05 AND 51 40 02 AND 53 10 15 FIG 104 TABLE 3 LINE 8. 2 L 7 4 4F RT A16WE 2007121100113 20071211 00113 NM 2007 12 11 ASAA0772312 1 20071130 A 5320 146A75021 FLOOR SUPPORT BOEING 737 737790 13844CN NM BS 727-847 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 AFT CARGO PIT CORROSION ON FLOOR SUPPORT ZEE CHANNEL AT LBL 22 BS 727+4 847, REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2007121100120 20071211 00120 NM 2007 12 11 ASAA0772319 1 20071120 A 5321 146A94018 FLOOR PANEL BOEING 737 737790 13844CN NM BS 727D CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 AFT CARGO PIT FLOOR PANEL SPLICE TEE BS 727D+6 CORRODED SPLICE TEE REPLACED. 2 L 7 2 4F RT A16WE 2007121100137 20071211 00137 EA 2007 12 11 A6WA200740621 1 20071114 A 2910 DRAIN LINE CNDAIR CL600 CL6002B19 1900309 EA NR 2 HYD SYS CHAFED A A6WA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 31 437AW 7744 HYD 2 LOW PRESSURE CAUTION MESSAGE WITH ZERO QUANTITY AND ZERO PRESSURE. COMPLIED WITH QRH. DECLARED EMERGENCY, NORMAL LANDING. SHUT DOWN ENGINE NR 2 AFTER LANDING. TOTAL TIME AT ZERO QUANTITY 23 MINUTES. APU BAY LEAKING FLUID. FOUND NR 2 HYDRAULIC CASE DRAIN LINE P/N 601R75286-51 CHAFED. REMOVED AND REPLACED LINE IAW 29-10. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007121100138 20071211 00138 EA 2007 12 11 A6WA200740625 1 20071114 A 2750 FITTING CNDAIR CL600 CL6002B19 1900309 EA FLAP ALIGNMENT WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 470ZW 7927 WEAR MARK ON OUTBOARD FLAP ALIGNMENT FITTING LT SIDE OUT OF LIMIT IAW REO 601R-57-51-143, .060 INCH DEPTH. REPLACED IAW SRM 51-42-06 AND 51-42-20. OPS CHECK C/O IAW CRJ 200 AMM 27-54-00-710-801. (M) 2 L 7 2 4F RT A21EA 2007121100140 20071211 00140 EA 2007 12 11 A6WA200740627 1 20071116 A 5280 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT MLG DOOR GOUGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 470ZW 7927 FOUND LT MLG DOOR GOUGED AT LOWER FORWARD CORNER LOADING EDGE. (M) DAMAGED REPLACED IAW REO 601R-52-82-034. 2 L 7 2 4F RT A21EA 2007121100141 20071211 00141 GL 2007 12 11 SIMA200733703 2 20071129 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 SMOKE A SIMA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 632AE 145143 CAE311225 AFTER LIFTOFF LAV SMOKE ON EICAS. SMOKE CONFIRMED BY FLIGHT ATTENDANT DECLARED EMERGENCY AND RETURNED FOR LANDING. FOL LOWED AOM PROCEDURES LANDED BELOW MAX LANDING WEIGHT. REMOVED AND REPLACED ENG 1 IAW W.C. 71-000-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007121100142 20071211 00142 SO 2007 12 11 SIMA200733701 1 20071125 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO CARGO DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 667GB 9629 5000 145784 DURING IMBV INSPECTION, THE CARGO DOOR SILL WAS FOUND TO BE CORRODED BEYOND MANUAL LIMITS. REPLACED SILL WITH PN 145-25 480-603 IAW SRM 51-40-02, 51-40-06, 51-40-06, 51-40-10. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007121100143 20071211 00143 EA 2007 12 11 SIMA200733706 1 20071201 A 2130 GG6700980051 VALVE CNDAIR CL600 CL6002C10 1390015 EA NR 1 MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 514AE 10119 CREW REPORTED THAT AUTO PRESS HALF FAIL IN CLIMB. REMOVED AND REPLACED NUMBER 1 SAFETY VALVE IAW AMM 21-32-03. OPS CH ECK IAW AMM 21-32-03. NO DEFECTS NOTED PRESSURIZED AIRCRAFT IAW AMM 21-31-00. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007121100145 20071211 00145 SO 2007 12 11 SIMA200733708 1 20071201 A 2797 GROUND STUD EMB 145 EMB145LR 3260212 SO LOOSE A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 619AE 145101 CREW ABORTED T/O AT 30 KNTS FOR UNCOMMANDED SPOILER DEPLOYMENT. TROUBLESHOT PER EMB 145FIM27-63-00. FOUND LOOSE GROUND STUD. TIGHTENED. GROUND STUD IAW EMB AMM 20-10-01. OPS CK GOOD OF SPOILER SYSTEM IAW AMM27-62-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007121100149 20071211 00149 EU 2007 12 11 SIMA200733804 1 20071202 A 5347 7253742409 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 232AE 23550 5000 340B232 DURING MBV INSPECTION, THE SEAT TRACK AT B.L. 36R WAS FOUND TO BE CORRODED. REPLACED SEAT TRACK WITH NEW IAW SAAB SRM ( 72LKS 3079 REV 49) CHAPTERS 51-40-21 AND 51-40-22. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007121100150 20071211 00150 SO 2007 12 11 SIMA200733805 1 20071201 A 5220 SEAL EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT UNSECURE A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 925AE 14500908 DV WINDOW SEAL HANGING OUT IN FLIGHT MADE VERY LOUD SQUEALING NOISE. SECURED COCKPIT EMERGENCY EXIT RUBBER TRIM SEAL ON FIRST OFFICERS DV WINDOW IAW EMB145 AMM 56-11-02. PERFORMED PRESSURIZATION CHECK IAW EMB145 AMM 21-31-00. PRESSURE CH ECK GOOD. LEAK CHECK GOOD AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007121100152 20071211 00152 SO 2007 12 11 SIMA200733802 1 20071201 A 2720 15793101 PRESSURE SWITCH EMB 135 EMB135LR 3260305 SO RUDDER SYS INOPERATIVE A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 703MR 145173 RUDDER SYSTEM NR 1 INOP MSG ON EICAS DURING START OF TAKEOFF ROLL. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. REMO VED AND REPLACED RUDDER SYSTEM 1 PRESSURE SWITCH PER EMB AMM 27-23-04. OPERATIONAL CHECK GOOD AT THIS TIME AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007121100154 20071211 00154 2007 12 11 SIMA200733702 2 20071129 A 7230 COMPRESSOR CNDAIR CL600 CL6002C10 1390015 EA LT ENGINE STALLED A SIMA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 518AE 10126 CREW HAD SEVERAL E1 COMPRESSOR STALLS IMMEDIATELY AFTER TAKEOFF, FLEX THRUST WAS USED FOR TAKEOFF. SHUT DOWN LEFT ENGI NE IN FLT PER CHECKLIST. REMOVED AND REPLACED LT ENGINE ASSEMBLY IAW EC 71-002. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007121100155 20071211 00155 SO 2007 12 11 SIMA200733704 1 20071130 A 2730 3621001013 CONTROL UNIT EMB 145 EMB145LR 3260212 SO HORIZONTAL STAB MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 908AE 14500897 PITCH TRIM INOP. REMOVED AND REPLACED HSCU IAW AMM 27-10-01-000-801-A AND 27-40-01-400-801-A. OPS CHECKED GOOD. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007121100156 20071211 00156 EA 2007 12 11 RU3A0710 1 20071203 A 5610 6003303026 WINDSHIELD CNDAIR CL600 CL6002B16 1900305 EA COCKPIT CRACKED E RU3A O OTHER O OTHER CR CRUISE 1 SW 15 87 5190 FLYING AT FL340 1.5 HOURS INTO FLIGHT THE CO-PILOTS WINDSHIELD OUTER PLY CRACKED. COMING INTO THE TERMINAL AREA WITH -3 DEGREE C AND MOISTURE IN THE AIR, RAIN STARTED TO GET INSIDE THE CRACK. ON A 14 MILE ILS FINAL TO RWY 28 AT ABOUT 3000 ' HEARD A LOUD POP AND A 1/4 OF THE CO-PILOT'S WINDSHIELD OUTER PLY BROKE OFF. AFTER LANDING, RIGHT SIDE OF AIRCRAFT TO INCLUDE THE NR 2 ENGINE WAS INSPECTED WITH NO VISIBLE DAMAGE NOTICED. 2 L 7 2 4F RT A21EA 2007121100159 20071211 00159 EU 2007 12 11 MALA070193 1 20071204 A 5210 SKIN SAAB SF340 340B 7860101 EU PAX DOOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 412XJ 340B412 MAIN ENTRANCE DOOR HINGE, INNER CLOSING SKIN HAS A DENT. REPAIRED IAW EO NR S52093. 2 L 7 2 4T RT A52EU 2007121100160 20071211 00160 NM 2007 12 11 AMTA200700658 1 20071129 A 5753 113A93521 FAIRING BOEING 737 737800* NM NR 3 FLAP TRACK DAMAGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 310TZ 28243 ATTACHING SCREWS PULLING THROUGH ON LEFT WING FLAP SUPPORT FAIRING NR 3. ACCOMPLISHED REPAIR IAW SAA EA 737-5753-09-A11 03. (M) 2 L 7 2 4F RT A16WE 2007121100161 20071211 00161 2007 12 11 COEA0701850 4 20071130 A 3497 CONNECTOR CESSNA 208 208B 2073701 CE HSI LOOSE A COEA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 NM 13 850FE 208B0164 AIR TURN BACK, FLT 8673 PDX-MFR - DURING TAKEOFF, THE HORIZONTAL SITUATION INDICATOR FLAGGED. PILOT COULD NOT RESET. P ILOT ELECTED TO RETURN TO PDX. AIRCRAFT LANDED SAFELY. RECONNECTED LOOSE CONNECTOR TO HSI UNIT. (M) 1 H 7 1 3T A37CE 2007121100162 20071211 00162 NM 2007 12 11 NWAA073896301 1 20071130 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 661US 23719 DURING OVERNIGHT CHECK, FOUND 2 EMERGENCY OUTSIDE AFT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY OV ER DOOR 3R. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007121100163 20071211 00163 NM 2007 12 11 NWAA073886301 1 20071129 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 661US 23719 DURING OVERNIGHT CHECK, UPPER DECK FORWARD HALF EMERGENCY FLOOR TRACK LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED POW ER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007121100164 20071211 00164 EA 2007 12 11 TRAX200701766 1 20071121 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 FS 280 RBL 9 ANGLES CRACKED IB AND OB, RESOLVED ON W/O: 75509 TASKCARD: N/R-00248). REMOVED 280 RBL 9 CRACKED ANGLE CLI PS I/B AND O/B. FABRICATED SERVICEABLE CLIP ANGLES. REFER TO FORM 412 IAW CRJ 200 SRM 53-21-43 AND 51-24-21. OK TO TOP COAT FASTENERS APPLIED TOPCOAT TO FASTENERS AND REPAIR AREA IAW CRJ 200 SRM 51-25-16. INSTALLED DRIP TRAY (REF 409A) IAW CRJ 200 SRM 51-42-13 USING CR 3552-4-2. 2 L 7 2 4F RT A21EA 2007121100165 20071211 00165 EA 2007 12 11 TRAX200701767 1 20071121 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 FS 280 LBL 27 ANGLE CRACKED OB, RESOLVED ON W/O: 75509 TASKCARD: N/R-00249. REMOVED AND FABRICATED ANGLE CLIP FOR FS 28 0LBL 20 OB SIDE IAW CRJ 200 SRM 53-21-43 AND 51-24-21. OK TO TOPCOAT TO FASTENERS AND REPAIR AREA IAW CRJ 200 SRM 51-25 -16. INSTALLED PANEL REF 409A IAW CRJ 200 SRM 51-42-13, USING CR3552-4-B AND 4-7 RIVETS. 2 L 7 2 4F RT A21EA 2007121100166 20071211 00166 EA 2007 12 11 TRAX200701780 1 20071126 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 AAR-1049, FS 280 LBL 27 O/B ANGLE CRACKED. RESOLVED ON W/O: 75509 TASKCARD: N/R-00333, REMOVED DAMAGED ANGLE FROM FS 28 0 LBL 27. FS 280 LBL 27 O/B CLIP ANGLE WAS REPLACED ON W/C 1000/0050 PER REO 601R-53-11-1290. 2 L 7 2 4F RT A21EA 2007121100167 20071211 00167 EU 2007 12 11 TRAX200701785 1 20071127 A 5320 FLANGE AEROSP ATR72 ATR72212 8680945 EU MLG WW CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 WHEEL WELL FR 27 LOWER FLANGE CENTER SECTION CORRODED UNDER NUT PLATE. RESOLVED ON W/O: 75891 TASKCARD: N/R-00016 , WHE EL WELL FR 27 LOWER FLANGE CENTER SECTION CORROSION REMOVED AS PER SRM 51-21-42. RT NUT PLATE REPLACED AS PER SRM 51-25 -01. UNDER 3RD NUT PLATE AT FR 27 LWR FLANGE CENTER SECTION, LT, CORROSION REMOVED AS PER SRM 51-21-42. FOUND OUT OF L IMITS IAW SRM 51-10-10. REWORKED AS PER ANA/YUL07/276/362/003 1-MATERIAL THICKNESS: 0.050 MATERIAL REMOVED: 0.002 WITHI N LIMITS AS PER SRM: 51-10-10 2-MATERIAL THICKNESS: 0.050 MATERIAL REMOVED: 0.040 OUT OF LIMITS AS PER SRM: 51-10-10. 2 H 7 2 4T RT A53EU 2007121100170 20071211 00170 EU 2007 12 11 TRAX200701807 1 20071127 A 5320 ANGLE AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 CRACK FOUND ON RT ANGLE FR 26 STRG 5R, RESOLVED ON W/O: 75891 TASKCARD: N/R-00169. ON RT FR 26 STRG 5R, ANGLE REPLACED IAW SRM 51-25-01 AND IAW TECHNICAL INSTRUCTION 57-01-91F FABRICATION COVER ON W/C 2000-233. 2 H 7 2 4T RT A53EU 2007121100171 20071211 00171 EA 2007 12 11 TRAX200701821 1 20071128 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 FS 280 FWD ANGLE CORRODED, RESOLVED ON W/O: 75509 TASKCARD: N/R-00399. REMOVED AND LOCATED NEW ANGLE P/N 600-34017-351 IAW CRJ SRM 51-40-11. OK TO INSTALL. INSTALLED ANGLE IAW CRJ 200 SRM 51-42-06. OK TO TOPCOAT FASTENERS. APPLIED TOPCO AT TO FASTENERS AND REPAIR AREA IAW CRJ 200 SRM 51-25-16. 14212. 2 L 7 2 4F RT A21EA 2007121100172 20071211 00172 EU 2007 12 11 TRAX200701842 1 20071130 A 3211 LANDING GEAR AEROSP ATR72 ATR72212 8680945 EU LEFT INOPERATIVE A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 636AS 375 LEFT MAIN GEAR WILL NOT RETRACT, EMERGENCY DECLARED. EMERGENCY EQUIPMENT ON STANDBY. 2 H 7 2 4T RT A53EU 2007121100173 20071211 00173 EU 2007 12 11 EPUA120107 1 20071201 A 5711 SPAR REIMS 406 F406 7535723 EU LT WING CRACKED E EPUA K NONE O OTHER IN INSP/MAINT 1 AL 03 6590Y F4060052 DURING ROUTINE SCHEDULED MAINTENANCE, A CRACK WAS DISCOVERED APPROX 6.5" LONG IN A U-SHAPED PATTERN ON THE LT WING MAIN SPAR AT LT CWS 51.00 TO CWS 48.00, EMANATING FROM THE UPLOCK BRACKET ATTACHMENT POINT TO THE MAIN SPAR. THE UPLOCK BRAC KETS WERE ALSO BROKEN AND BENT INDICATING POSSIBLE FORCE FROM MAIN GEAR EXTENSION, NOT CORROSION WERE THE CAUSE OF DAMAG E. 1 L 7 2 3T RT A54EU 2007121100176 20071211 00176 EA 2007 12 11 SWIA200718912 1 20071128 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN SMOKE A SWIA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 07 943SW 7762 FLT 6017 - AFTER TAKEOFF ROTATION, CAUTION MESSAGE "SMOKE TOILET" APPEARED AND FLIGHT ATTENDANT REPORTED SEEING AND DETE CTING SMOKE. INSPECTED LAVATORY, BOTH LEFT AND RIGHT PACKS AND DUCT SYSTEM, AND BOTH LEFT AND RIGHT ENGINES. COULD NOT DUPLICATE PROBLEM AT THIS TIME. 2 L 7 2 4F RT A21EA 2007121100179 20071211 00179 EA 2007 12 11 SWIA200718915 1 20071129 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 865AS 7507 FLT 3879 - EMERGENCY EXIT SIGN BY MAIN CABIN DOOR IS INOP. REPLACED LAMP IN EXIT SIGN AS NEEDED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007121100181 20071211 00181 NM 2007 12 11 HALA0700514 1 20071203 A 2612 WARNING MESSAGE BOEING 767 7673G5 1385126 NM APU FIRE ILLUMINATED A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, APU FIRE LOOP 2 MSG DISPLAYED. PERFORMED FIM 26-15-00 FIGURE 103 MESSAGE CLEARED TEST OKAY. 2 L 7 2 4F RT A1NM 2007121100183 20071211 00183 NM 2007 12 11 ASAA0752347 1 20071203 A 2410 IDG BOEING 737 737890 1384527 NM NR 2 LEAKING A ASAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 02 557AS 35176 FOLLOW UP TO FREQUENT NR 2 IDG SERVICING. LEAK CHECK HAS BEEN ACCOMPLISHED HOWEVER FREQUENT SERVICING CONTINUES. REPLA CED IDG. 2 L 7 2 4F RT A16WE 2007121100185 20071211 00185 NM 2007 12 11 ASAA0752340 1 20071201 A 4990 38809381 FILTER BOEING 737 737890 1384527 NM APU OIL SYS CLOGGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 577AS 35186 APU OIL FILTER CLOGGED. REPLACED APU OIL FILTER. 2 L 7 2 4F RT A16WE 2007121100186 20071211 00186 NM 2007 12 11 ASAA0772331 1 20071114 A 5315 147A55047 FLOORBEAM BOEING 737 737790 13844CN NM BS 947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 AFT CABIN CORROSION FOUND ON BS 947 FLOORBEAM LBL 53 AROUND CLIP NOT HOLE LOCATION REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2007121100187 20071211 00187 NM 2007 12 11 ASAA0772337 1 20071116 A 5315 141A55052 FLOORBEAM BOEING 737 737790 13844CN NM BS 344 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 CABIN FLOORBEAM BS 344 LBL 12 CORRODED REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2007121100188 20071211 00188 NM 2007 12 11 ASAA0772326 1 20071113 A 5320 146A75035 FLOOR SUPPORT BOEING 737 737790 13844CN NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 AFT CARGO PIT CORROSION ON FLOOR SUPPORT RAIL BS 767+6 LBL B REPAIRED WITH MADE REPAIR PART. 2 L 7 2 4F RT A16WE 2007121100189 20071211 00189 NM 2007 12 11 ASAA0772327 1 20071114 A 5320 SHEAR WEB BOEING 737 737790 13844CN NM BS 1016 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 AFT CABIN CORROSION FOUND ON SHEAR WEB RBL 33 BS 1016+3. REPLACED WITH MADE REPAIR PART IAW BOEING ENG DWG 147A15712 AN D B737 700 SRM 51 40 02. 2 L 7 2 4F RT A16WE 2007121100190 20071211 00190 NM 2007 12 11 ASAA0772328 1 20071114 A 5320 147A57124 SHEAR WEB BOEING 737 737790 13844CN NM BS 1016 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 AFT CABIN DENT FOUND ON SHEAR WEB AT RBL 33.5 BS 1016+5. REPLACED WITH MADE REPAIR PART FOR BOEING ENG DWG 147A5712 AND B737 700 SRM 51 40 02. 2 L 7 2 4F RT A16WE 2007121100192 20071211 00192 NM 2007 12 11 ASAA0772330 1 20071114 A 5320 147A566021 INTERCOSTAL BOEING 737 737790 13844CN NM BS 947-967 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 AFT CABIN CORROSION FOUND ON INTERCOSTAL LBL 50 BS 947 TO 967. INTERCOSTAL REPLACED WITH NEW PART. 2 L 7 2 4F RT A16WE 2007121100193 20071211 00193 NM 2007 12 11 ASAA0772332 1 20071115 A 5320 141A541012 INTERCOSTAL BOEING 737 737790 13844CN NM BS 312-328 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 FWD CABIN INTERCOSTAL CRACKED BS 312 TO 328 RBL 31. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2007121100195 20071211 00195 NM 2007 12 11 ASAA0772334 1 20071115 A 5320 141A541012 INTERCOSTAL BOEING 737 737790 13844CN NM BS 312-328 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 FWD CABIN INTERCOSTAL CRACKED BS 312 TO 328 LBL 46. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2007121100196 20071211 00196 NM 2007 12 11 ASAA0772335 1 20071115 A 5320 141A541012 INTERCOSTAL BOEING 737 737790 13844CN NM BS 328-344 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 FWD CABIN INTERCOSTAL CRACKED BS 328 TO 344 LBL 46, REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2007121100199 20071211 00199 NM 2007 12 11 ASAA0772344 1 20071118 A 5320 143A524010 FLOOR SUPPORT BOEING 737 737790 13844CN NM BS 540 BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 FLOORBOARD SUPPORT CHANNEL BROKEN AT BS 540 WL 208 RBL 2. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2007121100200 20071211 00200 NM 2007 12 11 ASAA0772346 1 20071113 A 5321 453A261018 FLOOR PANEL BOEING 737 737790 13844CN NM BS 767-887 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 AFT CARGO PIT FLOOR PANEL FROM STA 767+6 TO 887 CORRODED ALONG PANEL EDGES AND CRACKED AT STA 792. REPLACED WITH MADE R EPAIR PART IAW B737 700 SRM 53 60 53 KG1 AND 51 40 05 AND BOEING ENG DWG 453A2610. 2 L 7 2 4F RT A16WE 2007121100201 20071211 00201 SO 2007 12 11 RAIA00711016 1 20071123 A 3240 38793500 SHUTOFF VALVE EMB 145 EMB145 3260210 SO NR 1 BRAKE UNKNOWN A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 812HK 17493 17493 145373 FLT 5468 - STL - INTERMITTENT OUTBOARD BRAKE INOP MESSAGE DURING TAXI. MAINTENANCE REMOVED AND REPLACED NR 1 BRAKE SHUT OFF VALVE, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007121200001 20071212 00001 EA 2007 12 12 VNAA0711004 1 20071107 A 5242 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE E&E BAY DAMAGED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 209PS 7874 CREW REPORTED A BIRD STRIKE FORWARD OF THE AVIONICS NOSE COMPARTMENT. MAINTENANCE INSPECTED AND FOUND DAMAGE TO THE LEF T HAND FORWARD AVIONICS DOOR. MAINTENANCE COMPLIED WITH THE BIRD STRIKE INSPECTION 05-51-25-210-801. MAINTENANCE REPAI RED ALL DAMAGE TO THE LEFT HAND FUSELAGE NOSE AREA IN ACCORDANCE WITH THE AIRCRAFT STRUCTURE REPAIR MANUAL 53-11-31. AI RCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007121200003 20071212 00003 NM 2007 12 12 ASAA0772338 1 20071113 A 5330 143A32334 DOUBLER BOEING 737 737790 13844CN NM BS 500-500A CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 FWD CARGO PIT RADIO ANTENNA DOUBLER FOUND CORRODED AT BS 500 BS 500A BL 0, FWD CARGO RADIO ANTENNA DOUBLER REPLACED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2007121200006 20071212 00006 NE 2007 12 12 ASAA0752345 2 20071202 A 7397 3906605010 CONNECTOR BOEING 737 737890 1384527 NM CFMINT CFM567 CFM567B2US 13802 NE EEC DAMAGED A ASAA O OTHER O OTHER CR CRUISE 1 NM 02 587AS 35684 WHILE TROUBLESHOOTING NR 2 IDENTIFICATION PLUG FOUND NR 1 IDENTIFICATION PLUG CONFIGURED WRONG. REPINNED ID PLUG PER 73 21 61 PG 501. EEC OPERATES NORMALLY. 2 L 7 2 4F 4 F RT A16WE E2GL 2007121200007 20071212 00007 WP 2007 12 12 07FDEA03319 1 20070903 A 5330 ADA3763 SKIN DOUG DC10 DC1010F 3022111 WP BS 427 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 R1 PASSENGERS DOOR DEFORMATION OLD REPAIR ON UPPER FWD CORNER EXTERNAL SKIN. REPAIRED AREA IAW SRM 52-10-00 FIG 12A VOL I. 2 L 7 3 4F A22WE 2007121200009 20071212 00009 NM 2007 12 12 07FDEA04968 1 20071130 A 5347 AFA77407 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 MAIN DECK, SEAT TRACK BELOW FLOOR PANEL NR 281HF LOWER SURFACE FOUND CORROSION AROUND FASTENER HOLE AT STA 1731 LBL 75. MAIN DECK, SEAT TRACK BELOW FLOOR PANEL NR 281HF LOWER SURFACE CORROSION AROUND FASTENER HOLE AT STA 1731 LBL 75 REPA IRED AS PER FEDEX EA NR 1-5310-117060, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007121200010 20071212 00010 EU 2007 12 12 07FDEA04969 1 20071201 A 5340 A5377259904091 FITTING AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 FWD CARGO COMPARTMENT DOOR LOCK FITTING AT NR 1 POSITION CORRODED. REMOVED AND REPLACED FWD CARGO COMPARTMENT DOOR NR 1 LOCK FITTING IAW A310-200 SRM 51-40-20. 2 L 7 2 4F RT A35EU 2007121200012 20071212 00012 EU 2007 12 12 07FDEA04971 1 20071201 A 5320 A5378193620200 TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 MAIN DECK FLOOR, ADAPTER TRACK GOUGED AT FR37, (STA X2029) BL 44L (Y1120). REMOVED AND REPLACED ADAPTER REF: A301-200 S RM 51-40-21 PAR 6 AND 7. 2 L 7 2 4F RT A35EU 2007121200013 20071212 00013 EU 2007 12 12 07FDEA04972 1 20071201 A 5320 A5378193620200 TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 MAIN CABIN FLOOR ADAPTER TRACK GOUGED AT FR38.1 (STA X2135) BL 44L (Y1120) REMOVED AND REPLACED ADAPTER REF: A310-200 SR M 51-40-21 PAR 6 AND 7. 2 L 7 2 4F RT A35EU 2007121200015 20071212 00015 EU 2007 12 12 07FDEA04973 1 20071201 A 5340 ATTACH FITTING AIRBUS 310 A310203 3930313 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FWD LOWER CARGO COMPARTMENT, FLOORBEAM FITTING CRACKED AT FR 34 (X1870) BL 60L (Y1520). REMOVED FITTING IAW A310 SRM 5 1-72-10 PG 2 PARAGRAPH 5A LOCATED AND DRILLED NEW FITTING PN A5377364420100 IAW A310 SRM 51-72-10 PG 2 PARAGRAPH 6A. I NSTALLED NEW FITTING IAW A310 SRM 51-40-30. 2 L 7 2 4F RT A35EU 2007121200016 20071212 00016 EU 2007 12 12 07FDEA04974 1 20071201 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FWD LOWER CARGO COMPARTMENT, FLOORBEAM FITTING CRACKED AT FR 34 (X1870) BL 60L (Y1520). 2 L 7 2 4F RT A35EU 2007121200020 20071212 00020 EA 2007 12 12 COMA0760662 1 20071122 A 2611 SMOKE WARNING CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY ACTIVATED A COMA F ACTIVATE FIRE EXT. J WARNING INDICATION LD LANDING 1 SO 01 784CA 17766 7319 FLIGHT 5539 - CARGO SMOKE MESSAGE ILLUMINATED. DISCHARGED NORMAL AND STANDBY BOTTLES. DECLARED EMERGENCY, LANDED WITHO UT INCIDENT. REMOVED AND REPLACED RIGHT CARGO FIRE EXTINGUISHER BOTTLE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007121200022 20071212 00022 EA 2007 12 12 COMA0760664 1 20071122 A 2612 47259702 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A COMA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 784CA 22476 7319 FLIGHT 5218 - BOTH CARGO FIRE LIGHTS ILLUMINATED UPON LANDING. COMPLIED WITH QRH PROCEDURE, BOTH BOTTLES DISCHARGED. R EMOVED AND REPLACED CARGO FIRE CONTROL PANEL. 2 L 7 2 4F RT A21EA 2007121200023 20071212 00023 EA 2007 12 12 COMA0760665 1 20071122 A 3297 TR17300600000 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA RT MLG BROKEN A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 436CA 7482 FLIGHT 5180 - RECEIVED ANTI-SKID CAUTION MESSAGE ON TAKEOFF. ABORTED TAKEOFF, RETURNED TO GATE WITHOUT INCIDENT. REPLA CED RIGHT O/B BROKEN HARNESS SEGMENT. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007121200024 20071212 00024 EA 2007 12 12 COMA0760666 1 20071122 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION CR CRUISE 1 SO 01 443CA 11990 7539 FLIGHT 5345 - RECEIVED FLAP FAIL CAUTION MESSAGE DURING CRUISE. LANDED CVG WITHOUT INCIDENT. REPLACED LEFT BPSU. NO F URTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007121200025 20071212 00025 WP 2007 12 12 07FDEA04975 1 20071201 A 3230 CONTROL VALVE DOUG MD10 MD1010F 3022112 WP MLG MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION DE DESCENT 1 SO 25 386FE 46620 ON INITIAL GEAR EXTENSION GOT ALL RED AND NO GREEN ON LIGHTS AND CONFIG PAGE. SAME ON SECOND ATTEMPT. NO WIND NOISE ON 1ST AND SECOND TIME, THIRD TIME ALL GREEN INDICATIONS. CHECKED MECHANICAL CONTROL TO LANDING GEAR CONTROL VALVE NO FA ULTS FOUND. CHECKED CABLE TENSION ON CABLES 109,110,111,112A FOUND OK PER MD10-10 MM 32- 31-01-5. REMOVED AND REPLACED LANDING GEAR CONTROL VALVE REF MD10-10 M/M 32-31-03-2. RIGGED VALVE PER MD10-10 PERFORMED FUNCTIONAL TEST REF MD10- 10 M/M 32-30-00- 5. LEAK AND OPS CHECK GOOD, NEEDS PLUMB BOB REMOVED AFTER A/C IS DOWN JACKED. 2 L 7 3 4F RT A22WE 2007121200032 20071212 00032 EA 2007 12 12 COMA0760670 1 20071124 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 779CA 7306 FLIGHT 5580 - FLAPS FAIL CAUTION MESSAGE WHEN GOING FROM 45 DEGREES TO 20 DEGREES FLAP SETTING AFTER LANDING. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007121200033 20071212 00033 EA 2007 12 12 COMA0760671 1 20071124 A 3222 161201 PISTON CNDAIR CL600 CL6002B19 1900309 EA NLG LEAKING A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 811CA 13562 7380 FLIGHT 9450 - NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED BACK TO JFK AND LANDED SAFELY. UPON INSPECTION FOUND NLG LEAKING AND NOT FULLY EXTENDING. REMOVED AND REPLACED PISTON ASSEMBLY. 2 L 7 2 4F RT A21EA 2007121200035 20071212 00035 NM 2007 12 12 WRLA2007128 1 20071107 A 5320 S292916914400 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING C-CHECK INSPECTION CORROSION FOUND AFT FUSELAGE FLOOR SUPPORT AT STA Y=2007 X=-23.5. REPLACED DAMAGED SUPPORT PE R MD11 SRM VOL II 51-31-01 REV 40. REF EGAT NRC U05025. 2 L 7 3 4F 4 F RT A22WE E24NE 2007121200037 20071212 00037 NM 2007 12 12 2007UALA04791 1 20071123 A 5330 65B04107 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 199UA 41609 28717 FUSELAGE SKIN SCRATCHED AND DENTED IN 2 AREAS BETWEEN STATION 590 & 603 AT STR 45R 46R. INSTALLED EXTERNAL DOUBLER REF SRM 53-00-01 REPAIR 1 FIG.A CATEGORY "B" REPAIR. ACF ITEM WILL BE GENERATED FOR REINSPECTIONS PER SRM. AC OK FOR SERVICE . 2 L 7 4 4F 4 F RT A20WE E24NE 2007121200038 20071212 00038 NE 2007 12 12 2007UALA04792 2 20071123 A 7200 LINER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE CRACKED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 540UA 25252 RTFL DUE TO NR 1 ENGINE HIGH OIL TEMPERATURE INDICATIONS. BOROSCOPE SHOWS A CRACK IN THE CRACK OF INNER LINER NR 4 PANE L. AIR/OIL HEAT EXCHANGER ALSO BELIEVED TO BE FAULTY. REMOVED ENGINE AND REPLACED WITH A NEW ENGINE. ENG 726661 SENT TO SHOP FOR OVERHAUL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121200039 20071212 00039 NE 2007 12 12 2007UALA04795 2 20071123 A 7421 IGNITER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LT ENGINE FAILED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 224UA 30225 222020 IGNITOR L1 FAILED TO START LEFT ENG. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121200040 20071212 00040 EU 2007 12 12 2007UALA04796 1 20071124 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT LOW A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 480UA 1555 PILOTS O2 SHOWING AMBER. SERVICED FROM 1700 TO 1900 PSI. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121200041 20071212 00041 2007 12 12 2007UALA04797 4 20071125 A 2210 AUTOPILOT SYS BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 924UA 26645 RTFL DUE TO INABILITY TO ENGAGE AP1 & AP2, CURRENT WEATHER & TURBULENCE IN THE AREA. FOUND FAULTY AUTOPILOT FLIGHT CONT ROL PANEL. REPLACED AUTOPILOT FLIGHT CONTROL PANEL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121200043 20071212 00043 EU 2007 12 12 2007UALA04799 1 20071126 A 3510 OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 412UA 465 CAPTAIN'S OXYGEN FACE SHIELD IS DAMAGED. REPLACED DAMAGED O2 FACE SHIELD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121200044 20071212 00044 EU 2007 12 12 2007UALA04800 1 20071126 A 3500 OXYGEN BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE 27L LOW PRESSURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 412UA 465 OXYGEN BOTTLE LOW AT 27L. REPLACED O2 BOTTLE AT LOCATION 27L. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121200045 20071212 00045 EU 2007 12 12 2007UALA04801 1 20071122 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 451UA 865 EMERGENCY LIGHT TEST FAIL RIGHT SIDE POWER SUPPLY. FOUND EPSU FAILURE. REPLACED RT EPSU, NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121200046 20071212 00046 NM 2007 12 12 2007UALA04802 1 20071124 A 3350 362624 LIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 927UA 26649 EEL LIGHTS INOP IN FWD AFT CABIN. REPLACED EEL LIGHT STRIP. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121200051 20071212 00051 WP 2007 12 12 07FDEA04980 1 20071203 A 5347 NFA622239 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 CTR CARGO COMPT DURING PERFORMED J/C MD10-2552-C180 FOUND SEVERE EXFOLIATION CORROSION ON SEAT TRACK. REPAIRED SEAT TRA CK IAW SRM 53-70-00 FIG 1 SHT 1-2 VOL I. 2 L 7 3 4F RT A22WE 2007121200053 20071212 00053 NM 2007 12 12 2007UALA04805 1 20071122 A 3350 6500994001 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 596UA 28749 DOOR 3R LIGHT BULB INSERT NEXT TO EXIT LIGHT MISSING. INSTALLED NEW LIGHT ASSY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121200054 20071212 00054 WP 2007 12 12 07FDEA04982 1 20071203 A 5313 ADA3064529 LONGERON DOUG DC10 DC1010F 3022111 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 FWD CARGO COMPT BILGE AREA FOUND SEVERE CORROSION ON LONGERON. REPAIRED AREA IAW SRM 53-30-00 FIG 10 VOL I. 2 L 7 3 4F A22WE 2007121200056 20071212 00056 WP 2007 12 12 07FDEA04983 1 20071203 A 5713 ARB07431 STRINGER DOUG DC10 DC1010 3022110 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 FOUND LOWER CHORD LUGS CRACKED. REPAIRED AREA IAW SRM 57-20-00 FIG 27 SHT 2 VOL I. 2 L 7 3 4F A22WE 2007121200057 20071212 00057 WP 2007 12 12 07FDEA04984 1 20071203 A 5740 ARB07432 LUG DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 FOUND LOWER CHORD LUG CRACKED. REPAIRED AREA IAW SRM 57-20-00 FIG 27 SHT 2 VOL I. 2 L 7 3 4F A22WE 2007121200058 20071212 00058 WP 2007 12 12 07FDEA04985 1 20071203 A 5313 ACA3032507 LONGERON DOUG DC10 DC1010F 3022111 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 FWD CARGO COMPT BILGE AREA FOUND CORROSION WITH EXFOLIATION ON LONGERON, REPAIRED LONGERON IAW SRM 53-10-00 VOL I FIG 5. 2 L 7 3 4F A22WE 2007121200062 20071212 00062 WP 2007 12 12 07FDEA04988 1 20071203 A 5347 S4929150 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 CABIN FLOOR TRACK SCALLOP BROKEN OUT AT STA 1139 LBL 48 EVALUATED SEAT TRACK, FOUND BROKEN SCALLOP, OUT OF LIMITS IAW DC /MD10 SRM 53-70-00 VOL I PG 21 AND 22. REMOVED AND REPLACED OUT OF LIMIT SECTION IAW DC/MD10 SRM 51-31-01 VOL II PG 1 AND DC/MD10 SRM 51-33-01 VOL II PG 1. MAT ID SEAT TRACK, SPLICE HAT AND PLATE. SCALLOPED SEAT TRACK. FAB`D SEAT TRAC K AND SPLICE HAT AND PLATE IAW DC/MD10 SRM 53-70-00 VOL I PG 3 AND 4. ALODINED AND PRIMED SEAT TRACK, SPLICE HAT AND PL ATE IAW DC/MD10 SRM 51-21-01 VOL II PG 1 AND 21, MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2007121200064 20071212 00064 NM 2007 12 12 2007UALA04809 1 20071121 A 3350 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 661UA 27158 EMERGENCY EXIT PATH LIGHTS ON FLOOR IN AFT PART ECONOMY ON LEFT SIDE ONLY ARE FLASHING ON AND OFF. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121200065 20071212 00065 EU 2007 12 12 07FDEA04990 1 20071203 A 5347 A5327541120300 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 MAIN CABIN SEATTRACK ADAPTER AT FR 60/61, Y - 1456 IS CRACKED REMOVED ADAPTER IAW A310-200 SRM 51-40-21 PARA 7. LOCATED AND DRILLED NEW ADAPTER REF A310-200 SRM 51-40-44 PARA 2. INSTALLED NEW ADAPTER REF A310-200 SRM 51-40-21 PARA 7. 2 L 7 2 4F RT A35EU 2007121200066 20071212 00066 NM 2007 12 12 2007UALA04810 1 20071122 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INTERMITTENT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 661UA 27158 EMERGENCY PATH LIGHT STRIP AT ROW 28 LEFT SIDE FLICKERING ON & OFF. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121200067 20071212 00067 NM 2007 12 12 07FDEA04992 1 20071204 A 5320 25FX1253 SUPPORT ANGLE BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 CABIN UPPER LOBE, STA 1110, AND STR 6R, SIDE WALL SUPPORT ANGLE IS CRACKED IN HALF. REMOVED DAMAGED ANGLE ANGLE REF SRM 51-30-2, FABRICATED REPLACEMENT REF DWG 25FX. TREATED AND PRIMED REF SRM 51-10-02. INSTALLED NEW ANGLE REF SRM 51-30 -2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007121200068 20071212 00068 NM 2007 12 12 2007UALA04811 1 20071124 A 3350 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 RIGHT EXTERNAL EMERGENCY LIGHTS ARE INOPERATIVE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121200070 20071212 00070 EU 2007 12 12 07FDEA04995 1 20071204 A 5315 LN9497A420 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 AT FRAME 26 FLOOR SUPPORT T-CAP HAS CORROSION AT RBL 59. CUT DAMAGE IAW A310 SRM 53-10-15. MATERIAL ID LN 9497-420 AND LN 9496-310 IAW A310 SRM 53-10-15. FABRICATED REPAIR PARTS IAW A310 SRM 53-10-15, ALODINED AND PRIMED IAW A310 SRM 51- 21-10. PAINTED IAW A310 SRM 51-23-10 AND INSTALLED IAW A310 SRM 53-10-15. 2 L 7 2 4F RT A35EU 2007121200071 20071212 00071 2007 12 12 2007UALA04812 4 20071121 A 2565 SLIDE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SERVICE DOOR DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 662UA 27159 RIGHT AFT SERVICE DOOR SLIDE FABRIC TORN ON TOP AND IS MISSING YEAR OVERHAULED STICKER BY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007120700099 20071207 00099 NM 2007 12 7 QXEA200701763 1 20071125 A 2420 GENERATOR BOMBDR DHC8 DHC8402 1390042 NM APU INOPERATIVE A QXEA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 NM 09 428QX 4160 PDX FLIGHT NR 2354: APU GEN DROPPED OFF LINE DURING ENGINE START. APU FAILED TO START. AIRCRAFT RETURNED TO BLOCK. PL ACED ON MEL IAW MEL REF 49-00-1, RSI NR 358894. 2 H 7 2 4T RT A13NM 2007120700111 20071207 00111 NM 2007 12 7 HALA0700505 1 20071128 A 4940 106170756 EXCITER BOEING 767 7673CB 1385187 NM APU MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 590HA 251 251 33467 ETOPS SIGNIFICANT SYSTEM, APU WILL NOT START. BITE ON APU ECU FAULTS NO LIGHT OFF. T/S PER FIM 49-11-00 FIG 107. REPL ACED IGNITER PLUG, LEAD AND EXCITER BOX. APU STARTS NORMAL AND BITE CHECKS NORMAL. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007120700120 20071207 00120 NM 2007 12 7 AMTA200700382 1 20070812 A 5320 STRUCTURE BOEING 757 75723N 1384973 NM FLOOR BROKEN A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 FOUND FLOOR STRIP BROKEN IN LT TUNNEL BESIDE NLG BOX STATION 377, LBL 24. REMOVED FLOOR STRIP DAMAGED IAW SRM 51-70-11 FIG 1 FROM STATION 367 TO 377. FABRICATED NEW FLOOR STRIP IAW SRM 51-70-11 FIG 1. TREATED AND PRIMED IAW SRM 51-20-01. INSTALLED REPAIR IAW 51-70-11 AND 51-40-02 STATION 367 TO 377. (M) 2 L 7 2 4F RT A2NM 2007120700137 20071207 00137 EU 2007 12 7 CPCPC2007119 1 20071024 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSLEAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 355AT 355 LT SEAT TRACK FRAME 36-39 CORRODED. LT SEAT TRACK FRAME 36-39 REPLACED IAW SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007120700138 20071207 00138 EU 2007 12 7 MALA070187 1 20071125 A 2150 7769106 ACM SAAB SF340 340B 7860101 EU LEFT ODOR A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 15 449XJ 340B449 RIGHT BLEED CLOSED LIGHT ILLUMINATED DURING DESCENT PRECEDED BY BURNED POPCORN ODOR IN FLIGHT DECK. ODOR WENT AWAY AFTE R VALVE CLOSED. REPLACED LT ACM P/N 776910-6, S/N OFF 921197; S/N ON 9807109. ALSO REPLACED RT LP BLEED VALVE P/N ON/O FF 785802-3; S/N OFF 910619 S/N ON 9707098. 2 L 7 2 4T RT A52EU 2007120700144 20071207 00144 NM 2007 12 7 F3LA200700328 1 20071127 A 5320 BOLT AIRBUS A319 A319111 3930336 NM LAVATORY MOUNT CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED ONE BOLT FOR FLOOR HOLD DOWN ON LAVATORY E CORRODED. REMOVED AND REPLACED CORRO DED BOLT IAW AMM 25-43-42-100-001. 2 L 7 2 4F RT A28NM 2007120700145 20071207 00145 NM 2007 12 7 F3LA200700329 1 20071114 A 5320 BLANKING PLATE AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED R2 GIRT BAR CORRODED. REMOVED AND REPLACED R2 DOOR BLANKING PLATE IAW AMM 52-11 -31-400-005. 2 L 7 2 4F RT A28NM 2007120700149 20071207 00149 NM 2007 12 7 UPS07M51225 1 20071105 A 5313 LONGERON DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C CTR CARGO AT STATION 5-32 TO STA 5-52 LONGERON 46L 14 EACH FASTENERS FOUND WITH RUSTY NUT AS MARK. CE NTER CARGO STA 5-32 TO 5-52 LONGERON 46 LT RUSTY NUTS 14 EA REMOVED PER SRM 51-33-01VIIR35. NEW NUTS 3D0006-3 (14 EA). INSTALLED AT CTR CARGO STA 5-32 TO 5-52 L46 LT PER SRM 51-33-01 VIIR35. 2 L 7 3 4F RT A22WE 2007120700156 20071207 00156 NM 2007 12 7 USAA920071231 1 20071117 A 5315 654654039 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C18 CHECK, CRACKED FLOORBEAM ATTACH ANGLE, BS 639, RBL 45. REPLACED FLOORBEAM ATTACH ANGLE, BS 639 , RBL 45 IAW 737 SRM 51-40-03. 2 L 7 2 4F RT A16WE 2007120700166 20071207 00166 NM 2007 12 7 USAA920071241 1 20071121 A 5311 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C16 CHECK, CRACKED FRAME, BS 827, S9R. REPAIRED FRAME, BS 827, S9R IAW USAIRWAYS EA 100048 AND TYP ICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2007120700169 20071207 00169 NM 2007 12 7 USAA920071244 1 20071120 A 5311 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C16 CHECK, CRACKED FRAME, BS 663, S1R. REPAIRED FRAME, BS 663, S1R IAW USAIRWAYS EA 100046. 2 L 7 2 4F RT A16WE 2007120700190 20071207 00190 WP 2007 12 7 AALA20072277 1 20071123 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 553AA 53083 LGA - EMERGENCY LIGHT AT SEAT 13D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F A6WE 2007120700193 20071207 00193 NM 2007 12 7 AALA20072280 1 20071123 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 797AN 30012 DFW - EMERGENCY LIGHT AT SEAT 40G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 40G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120700199 20071207 00199 NM 2007 12 7 AALA20072270 1 20071122 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 760AN 31477 DFW - EMERGENCY LIGHT AT FORWARD GALLEY RIGHT MIDDLE EMERGENCY EXIT SIGN MISSING LENS. REPLACED LENS FOR EMERGENCY LIGH T AT FORWARD GALLEY RIGHT MIDDLE EMERGENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120700207 20071207 00207 NM 2007 12 7 AALA20072271 1 20071122 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 760AN 31477 DFW - EMERGENCY LIGHT AT SEAT 22C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007120700211 20071207 00211 NM 2007 12 7 F3LA200700339 1 20071127 A 5414 D5463083700100 FAIRING AIRBUS A319 A319111 3930336 NM NR 1 ENGINE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED NR 1 ENGINE FAN OUTLET FAIRING INSTALLATION HAD CRACKS AT THE 7 O'CLOCK AND 9 O' CLOCK POSITIONS. REMOVED AND REPLACED NR 1 ENGINE FAN OUTLET FAIRING IAW SRM 51-44-11, 51-42-11 AND AMM 51-75-12-300-00 3. 2 L 7 2 4F RT A28NM 2007120700212 20071207 00212 NM 2007 12 7 F3LA200700340 1 20071127 A 5320 D5348004320601 SILL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED L2 DOOR SILL CORRODED AT NUTPLATE HOLES UNDER FWD L2 GIRT BAR FITTING/PLATE AREA , JUST AFT OF FR66. CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED L2 DOOR SILL IAW SRM 52-42-11. 2 L 7 2 4F RT A28NM 2007120700220 20071207 00220 NM 2007 12 7 F3LA200700346 1 20071114 A 5321 D5367180500500 FLOORBOARD AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBOARD 261FF CORRODED. REMOVED AND REPLACED FLOORBOARD 261FF IAW AMM 53-32- 12-400-002. 2 L 7 2 4F RT A28NM 2007121100021 20071211 00021 EU 2007 12 11 TRAX200701825 1 20071128 A 5210 BEAM AEROSP ATR72 ATR72212 8680945 EU PAX DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 FOUND BEAM 8 OF PAX DOOR CORRODED AROUND AFT INTERCOSTAL. CORROSION REMOVED IAW SRM 51-21-42 WITHIN LIMIT AS PER SRM 5 2-11-10 FIG 301MATERIAL THICKNESS: 0.047MATERIAL REMOVED: 0.002 WITHIN LIMITS AS PER SRM:52-11-10 FIG 301. 2 H 7 2 4T RT A53EU 2007121100022 20071211 00022 EU 2007 12 11 TRAX200701794 1 20071127 A 5320 INTERCOSTAL AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 CORROSION FOUND ON INTERCOSTAL BTW FR 38-39 LT, UNDER A/N AT FLOOR LEVEL. 2 H 7 2 4T RT A53EU 2007121100028 20071211 00028 EU 2007 12 11 TRAX200701800 1 20071127 A 5313 STRINGER AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 FOUND STR 17L CORRODED AT FR 39. CORROSION REMOVED AS PER SRM 51-21-42 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42 MATERIAL THICKNES S: 0.063 MATERIAL REMOVED: 0.003 WITHIN LIMITS AS PER SRM: 53-61-00 FIG 301. 2 H 7 2 4T RT A53EU 2007121100043 20071211 00043 NM 2007 12 11 F3LA200700351 1 20071115 A 5320 SILL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON R2 DOOR SILL, FWD SPLICE JUST FWD OF FR66. REMOVED SPLICES AND RE- MEASURED AREA. SUBMITTED EAR FOR APPROVAL OF MATERIAL LOSS. ROTOPROBED HOLES AND REINSTALLED SPLICES AND NEW COUPLING IAW EA A9-53R-12290. 2 L 7 2 4F RT A28NM 2007121100056 20071211 00056 NM 2007 12 11 UIEA200700448 1 20070929 A 5712 SPAR CAP BOEING 747 747228F 1384895 NM RT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 RIGHT WING FRONT SPAR LOWER CHORD AREA FSSO 1356 CORRODED. CORROSION REMOVED AS PER SRM 51-10-01 AND BOEING MESSAGE 1-6 38497220-2. 2 L 7 4 4F RT A20WE 2007121100059 20071211 00059 NM 2007 12 11 UIEA200700451 1 20071003 A 5245 ACCESS PANEL BOEING 747 747228F 1384895 NM A/C BAY DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 AIR CONDITION ACCESS PANEL 192ER EXTERNAL SURFACE IS DELAMINATED. REPAIRED AS PER SRM 51-40-17 AND BOEING MESSAGE 1-638 498164-2. 2 L 7 4 4F RT A20WE 2007121100064 20071211 00064 NM 2007 12 11 UIEA200700477 1 20071115 A 7160 NOSE COWL BOEING 747 747271C 1384869 NM GE CF6 CF650E2 30018 NE NR 2 ENGINE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 530388 NR 2 ENGINE NOSE COWL HAS 3 EACH CRACKS. ONE CRACK AT 7 O'CLOCK POSITION IS 15" LONG. NEXT CRACK AT 6 O'CLOCK POSITION IN 6 INCH LONG AND THE NEXT CRACK AT 6.45 O'CLOCK POSITION IS 11 INCH LONG. REPAIRED NR 2 ENGINE NOSE COWL IAW SRM 51 -43-01 AND XEO 71-111707. 2 L 7 4 4F 4 F RT A20WE E23EA 2007121100079 20071211 00079 NM 2007 12 11 UIEA200700476 1 20071116 A 5315 FLOORBEAM BOEING 747 747243B 1384830 NM ZONE 200 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 ON REMOVAL OF MCD CEILING PANELS AROUND STA 600 FOUND UPPER FLOORBEAM LOWER CHORD AT BS 620 RBL 52 HAS SUSTAINED IMPACT DENT OF 5" LONG 1.5" WIDE 0.187" DEEP. STRUCTURAL DISCREPANCY RAM PART 1 COMPLETED. HFEC ACCOMPLISHED TO DAMAGED AREA PER NDT PARA 6 51-00-00 FIG 23. NO CRACK INDICATION FOUND. LOWER CHORD STA 620 RBL 52 WL 300.8 REPAIRED PER ATLAS AIR XEO 53-111607. 2 L 7 4 4F RT A20WE 2007121100083 20071211 00083 CE 2007 12 11 1356911120307 1 20071202 A 3230 99101397 ACTUATOR CESSNA 402 402C 207590R CE UPLOCK INTERMITTENT E HYIA O OTHER P NO WARNING INDICATION AP APPROACH 1 NE 01 36911 7478 7478 402C0314 NOSE GEAR DOWN AND LOCKED LIGHT CAME ON AND THEN WENT OFF DURING FINAL APPROACH. BLEW GEAR DOWN TESTED GEAR DOWN INDICA TION WITH FLAP HANDLE, LANDED. MAINTENANCE FOUND UPLOCK ACTUATOR TO BE BAD REMOVED AND REPLACED ACTUATOR. 1 L 7 2 3O A7CE 2007121100086 20071211 00086 NM 2007 12 11 UPS07551232 1 20071202 A 2910 TUBE BOEING 757 75724APF 1384969 NM HYD SYSTEM LEAKING A IPXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 457UP 25478 APPROX 20 MINUTES AFTER DEPARTURE CREW INDICATED LOST LEFT HYDRAULIC SYSTEM AND WERE RETURNING BACK TO PTY. DECLARED AN EMERGENCY. INSPECTED AND FOUND TUBE PRESS ASSY BROKEN. REMOVED AND REPLACED TUBE PRESS ASSY AND ELBOW MOTORIZED ENGINE . NO LEAK NOTED. A/C BACK TO SERVICE. ALL THIS REMOVED ACCORDING TO MM 29-10-09-04. 2 L 7 2 4F RT A2NM 2007121100088 20071211 00088 NM 2007 12 11 UPS07M51231 1 20070926 A 5410 AUB7564 WEB DOUG MD11 MD11 3023602 NM NR 3 PYLON SCRATCHED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C PYLON NR 3 WIRING SUPPORT WEB WITH SCRATCHES ABOVE PRECOOLER. REMOVAL C/OUT TO ACCESS SCRATCHES MARK MENTIONED ABOVE, FOUND EXCEEDED LIMIT PER SRM 54-00-01,F1A, V1, .ORI THK 0.032", REMAIN THK 0.012". NEW WEB AT NR 3 PY LON FAB PER P/N AUB7564-7,USING MAT 2219-0-0.032". INSTALLATION C/OUT ON NEW WEB PER SRM 51-31-01, V2, R40. PYLON NR 3 WIRING SUPT CLAMPS AT AFFECTED AREAS. INSTALLED PER AMM20-30-01, R53 AFTER REPAIR. 2 L 7 3 4F RT A22WE 2007121100109 20071211 00109 NM 2007 12 11 ASAA0792303 1 20071130 A 5315 FLOORBEAM BOEING 737 737990 NM BS 500L CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 302AS 30017 FWD CARGO PIT RBL 25 LBL25 STA 500L FOUND CORROSION ON FLOOR SUPPORT ANGLE FWD CARGO PIT AT BS 500L RBL 25 TO LBL 25 RAI L ASSY REPLACED IAW B 737 900 SRM 51 40 02. 2 L 7 4 4F RT A16WE 2007121100112 20071211 00112 NM 2007 12 11 ASAA0792306 1 20071128 A 5320 143A812630 SHIELD BOEING 737 737990 NM BS 492-500A CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 302AS 30017 FWD CARGO PIT RT RBL 21 STA 492 500A SUPPORT ANGLE SHIELD WEB FOUND CORROSION FWD CARGO PIT RT FLOOR SUPPORT SHIELD AT B S 492 TO BS 500A RBL 21. REPLACED WITH MADE REPAIR PART IAW B 737 900 SRM 53 30 15 AND 51 40 02. 2 L 7 4 4F RT A16WE 2007121100117 20071211 00117 NM 2007 12 11 ASAA0772316 1 20071130 A 5320 146A81271 SHIELD BOEING 737 737790 13844CN NM BS 767-794 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 AFT CARGO PIT CORROSION ON WEB RBL 20 BS 767 TO 794.3 REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2007121100123 20071211 00123 NM 2007 12 11 ASAA0772322 1 20071123 A 5320 146A81233 WEB BOEING 737 737790 13844CN NM BS 794-847 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 AFT CARGO PIT CORROSION ON WEB UPPER FLANGE UNDER ANCHOR NUTS AT RBL 20 BETWEEN BS 847 AND 794. REPLACED WITH MADE REPA IR PART IAW BOEING ENG DWG 146AB123 AND B737 700 SRM 51 30 01 51 40 05 AND 51 40 02. 2 L 7 2 4F RT A16WE 2007121100128 20071211 00128 NM 2007 12 11 ASAA0772310 1 20071120 A 5512 186A10018 SKIN BOEING 737 737790 13844CN NM HORIZONTAL STAB DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 RT HORIZONTAL STAB L E STA 46.00 DENTED REPAIRED CUT OUT FILM AND DOUBLER. 2 L 7 2 4F RT A16WE 2007121100133 20071211 00133 EU 2007 12 11 TRBA2007107 1 20071202 A 3320 EO38711 BULB AEROSP ATR72 ATR72212A 8680902 EU CABIN LIGHTS BURNED OUT A TRBA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 29 536AT 536 BURNING ODORIN FWD PORTION OF CABIN. FOUND LIGHT BULBS BURNT AT ROW 1AB AND 6CD. REMOVED LIGHT BULBS (CEILING) IAW ATR 72 JIC 33-10-00. 2 H 7 2 4T RT A53EU 2007121100146 20071211 00146 SO 2007 12 11 SIMA200733710 1 20071201 A 3150 WARNING MESSAGE EMB 145 EMB145LR 3260212 SO ILLUMINATED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 679AE 14500814 CAPT REPORTED, GOT WING A/I FAIL MESSAGE. FOLLOWED AOM PROCEDURES AND COULD NOT GET MESSAGE TO CLEAR. DUE TO WEATHER E LECTED TO DIVERT TO CMH. 2 L 7 2 4T RT T00011AT 2007121100147 20071211 00147 SO 2007 12 11 SIMA200733709 1 20071201 A 3350 2013BR BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 667GB 145784 EMERGENCY LIGHTS AT ROW 12-18 INOP, FOUND DURING MORNING PREFLIGHT. SFP TO DFW FOR EMERGENCY BATTERY PACK. AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007121100151 20071211 00151 2007 12 11 SIMA200733801 4 20071201 A 2310 ANTENNA EMB 145 EMB145LR 3260212 SO COMMS DEBONDED A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 696AE 14500874 IN CLOUDS COMM 1 AND 2 BECOMES UNREADABLE AND UNLINK GOES NO COMM CREW ELECTED TO RETURN TO MQT. FOUND COMM 3 ANTENNA U NBOUNDED REBOUNDED COMM 3 ANTENNA. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007121100169 20071211 00169 EU 2007 12 11 TRAX200701806 1 20071127 A 5320 BRACKET AEROSP ATR72 ATR72212 8680945 EU CARGO BAY CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 ON RT FWD CARGO COMPT BRACKET AT FR 15 FOUND CRACKED, RESOLVED ON W/O: 75891 TASKCARD: N/R-00167. ON RT FWD CARGO COMPT BRACKET AT FR 15 BTW STRG 14R REPLACED AS PER SRM 51-25-01. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE W ITH SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007121100177 20071211 00177 EA 2007 12 11 SWIA200718913 1 20071201 A 5210 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 367CA 10069 PAX DOOR AFT DRAG ANGLE IS CRACKED NEAR CABLE PULLEY BRACKET. REPAIRED CRACK IAW REO 670-52-11-0054. 2 L 7 2 4F RT A21EA 2007121100194 20071211 00194 NM 2007 12 11 ASAA0772333 1 20071115 A 5320 141A5410V3 INTERCOSTAL BOEING 737 737790 13844CN NM BS 294-277 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 FWD CABIN INTERCOSTAL CRACKED BS 294 TO 277 BL 0. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2007121200002 20071212 00002 WP 2007 12 12 ASAA0782349 1 20071203 A 5330 5924802517 SKIN DOUG DC9 DC983 3022083 WP BS 229-264 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 960AS 53074 DENT IN FUSELAGE APPROX 4' FROM L1 DOOR AND 2' BELOW WINDOW BELT REMOVED DAMAGED AREA OF SKIN. FABRICATED AND INSTALLED REPAIR SECTION OF SKIN FINGER DOUBLERS SKIN SPLICE STRAP STRAPS IAW MD80 SRM 53 04 FIG 12C. 2 L 7 2 4F RT A6WE 2007121200008 20071212 00008 EU 2007 12 12 07FDEA04760 1 20071109 A 5330 A53811049200 SKIN AIRBUS 310 A310203 3930313 EU FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 402FE 201 AGING AIRCRAFT DETERMINATION OF EXTERNAL DOUBLER ON FUSELAGE SKIN AT FRAME 40 STRINGER 16 TO 18 RT REQUIRE EVALUATION FO R MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED REPAIR FOUND NOT TO B E WITHIN SRM REQUIREMENTS. REMOVED DOUBLER, REPAIRED HOLES AND INSTALLED FASTENERS IAW EA 6-5330-112990 FUSELAGE-SKIN P ANEL AT FR 40 AND S-17R- REPAIR. REMOVED AND REPLACED STRINGER SPLICE AT FS 2294- S-17R IAW A310 SRM 51-40-21 PG 22 AND PG 24. 2 L 7 2 4F RT A35EU 2007121200026 20071212 00026 WP 2007 12 12 07FDEA04976 1 20071201 A 3297 WIRE HARNESS DOUG MD10 MD1010F 3022112 WP MLG UNSECURE A FDEA O OTHER J WARNING INDICATION DE DESCENT 1 SO 25 570FE 47829 UNSAFE GEAR DOWN INDICATIONS X2 BOTH PRIMARY AND SECONDARY, CYCLED GEAR VIA RED TABS QRH GOT SAFE INDICATIONS ON 3RD TRY . FOUND WIRE BUNDLE FOR THE GEAR INDICATION LIGHTS INTERFERRING WITH GEAR HANDLE. FOUND NO DAMAGE ON WIRE BUNDLE. SEC URED WIRE BUNDLE AS PER WIRING STANDARD PRACTICES 20-10-01. CLEANED LANDING GEAR CONTROL MECHANISM PER MM 32-31-02-7. JACKED A/C PER MM 07-11-00-2 AND RETRACTED GEAR NUMEROUS TIMES PER MM 32-30-00-5. NOW GEAR RETRACTS AND EXTENDS NORMA LLY WITH CORRECT INDICATION. 2 L 7 3 4F RT A22WE 2007121200029 20071212 00029 NM 2007 12 12 WRLA2007127 1 20071110 A 5350 SUPPORT BEAM DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FAIRING CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING C-CHECK INSPECTION CORROSION FOUND RT WING TO BODY FAIRING SUPPORT BEAM AT STA Y=1348 Z=-20. REPAIRED THE RT WIN G TO BODY FAIRING SUPPORT BEAM AT STA Y=1348 Z-20 PER SRM VOL 1 53-00-01 FIG 9 REV 40. REF EGAT NRC U05030. 2 L 7 3 4F 4 F RT A22WE E24NE 2007121200060 20071212 00060 WP 2007 12 12 07FDEA04987 1 20071203 A 5347 S492914727700 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 MAIN CABIN APPROX AT STA 1531 LBL 27 SEAT TRACK HAS CORROSION. REMOVED AND REPLACED SEAT TRACK AT STA 1490 TO 1531 LBL 27 IAW DC-10/MD-10 SRM 53-70-00, VOL I, FIG 1. 2 L 7 3 4F RT A22WE 2007121200069 20071212 00069 EU 2007 12 12 07FDEA04994 1 20071204 A 5320 A5377364420100 SUPPORT ANGLE AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 AT FRAME 26 SUPPORT ANGLE UNDERNEATH T-CAP AT RBL59 HAS CORROSION. REMOVED GUIDE AND FITTING IAW A310 SRM 51-40-02 PG 7. RECIEVED NEW FITTING P/N A5377364420100. DRILLED AND LOCATED FITTING IAW A310 SRM 51-40-44 PG 16 AND INSTALLED FITT ING AND GUIDE IAW A310 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007121200074 20071212 00074 EU 2007 12 12 USAA920071248 1 20071126 A 5347 SEAT TRACK AIRBUS 330 A330323 3930335 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 278AY 388 BFM - MAJOR REPAIR - C2 CHECK - NR 6048974, CORROSION ON SEAT TRACK, BS 4470/FR 55 - BS 4842/FR 58, -Y450. REPLACED SEA T TRACK, BS 4470/FR 55 - BS 4842/FR 58, -Y450 IAW A330 SRM 53-00-15. 2 L 7 2 4F RT A46NM 2007121200077 20071212 00077 NM 2007 12 12 USAA920071251 1 20071026 A 5320 65535953 REVEAL BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED R1 DOOR CUT OUT REVEAL, BS 312, S9R. REPLACED R1 DOOR CUT OUT REVEAL, BS 312, S9R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007121200078 20071212 00078 NM 2007 12 12 USAA920071252 1 20071025 A 3211 65827681 LINK BOEING 737 7373B7 1384580 NM LT MLG CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CORROSION ON LEFT MAIN LANDING GEAR SUPPORT BEAM SWING LINK. REPLACED LEFT MAIN LANDIN G GEAR SUPPORT BEAM SWING LINK IAW B737 AMM 57-15-00-4. 2 L 7 2 4F RT A16WE 2007121200079 20071212 00079 NM 2007 12 12 USAA920071253 1 20071023 A 5320 655829312 ANGLE BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED VERTICLE ANGLE, BS 967, S1R. REPLACED VERTICLE ANGLE, BS 967, S1R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007121200080 20071212 00080 NM 2007 12 12 2007UALA04814 1 20071125 A 2612 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FIRE DETECTION INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 667UA 29239 LEFT CUTOUT SWITCH LIGHT DOES NOT ILLUMINATE DURING FIRE TEST. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121200081 20071212 00081 NM 2007 12 12 USAA920071254 1 20071024 A 5311 65458076 FRAME BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED STUB FRAME, BS 294 S7R. REPLACED STUB FRAME, BS 294 S7R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007121200082 20071212 00082 EU 2007 12 12 F3LA200700360 1 20071201 A 2910 TUBE AIRBUS A318 A318111 3940019 EU HYD SYSTEM DAMAGED A F3LA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 NM 03 806FR 2218 FLIGHT CREW REPORTED YELLOW HYDRAULIC RESERVOIR LOW LEVEL INDICATION IN COCKPIT. REF TSM 52-36-00-810-805, FOUND YELLOW SYSTEM LOW PRESSURE SWITCH TUBE DAMAGED. REMOVED AND REPLACED LOW PRESSURE SWITCH TUBE IAW AMM 29-13-49-000-005 AND 29 -13-49-400-005. PERFORMED LEAK CHECK. NO LEAKS NOTED. 2 L 7 2 4F RT 2007121200083 20071212 00083 NM 2007 12 12 2007UALA04815 1 20071125 A 2520 CONSOLE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN SEAT LOOSE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 667UA 29239 ARMREST- CONSOLE LOOSE (ROCKS) AT SEAT 6H. CREW COMMENTS: SIDE TRIM LOOSE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121200085 20071212 00085 NM 2007 12 12 2007UALA04817 1 20071124 A 2611 SMOKE DETECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE AFT CARGO BAY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 675UA 29243 NR 1 AFT CARGO COMPARTMENT SMOKE DETECTOR INOPERATIVE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121200088 20071212 00088 NM 2007 12 12 2007UALA04820 1 20071126 A 3397 CONNECTOR BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 WALL EEL INOP LEFT SIDE AFT GALLEY. SECURED LOOSE CONTACT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121200090 20071212 00090 NM 2007 12 12 2007UALA04822 1 20071126 A 3350 1317 LAMP BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EEL LIGHTS INOP AT SEATS 39 ABC & 56 HJK. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121200091 20071212 00091 NM 2007 12 12 2007UALA04823 1 20071126 A 3350 1317 LAMP BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHT INOPERATIVE DOOR 5L SLIDE ILLUM. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121200092 20071212 00092 NM 2007 12 12 2007UALA04825 1 20071124 A 5610 WINDOW BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT OUT OF TRACK A UALA C ABORTED TAKEOFF W INADEQUATE Q C TO TAKEOFF 1 WP 29 531UA 25042 ABORTED T/O AT 110KTS. COPILOT'S BACK WINDOW CAME OPEN AND WAS OFF TRACK. COULD NOT GET IT TO CLOSE. AUTOBRAKES DID E NGAGE. SECURED FO WINDOW BACK IN TRACK AND CLOSED IT PROPERLY, NO REPEATS SINCE ORIGINAL INCIDENT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121200095 20071212 00095 NM 2007 12 12 2007UALA04828 1 20071123 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY EXIT LIGHTS INOP AT UPPER DECK CEILING ROWS 13, 17, 41L AND AT TOP OF STAIRS. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121200096 20071212 00096 NM 2007 12 12 2007UALA04829 1 20071123 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY EXIT EEL LIGHT INOP. JUST FWD OF LAV 102 BELOW CLOSET. REPLACED LIGHT ASSEMBLY 2 L 7 4 4F 4 F RT A20WE E24NE 2007121200099 20071212 00099 NM 2007 12 12 2007UALA04831 1 20071124 A 2560 GIRT BAR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L5 DOOR OBSTRUCTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 179UA 25158 THE 5L WILL NOT ARM. FOUND HEAD SET OBSTRUCTING GIRT BAR. REMOVED OBSTRUCTION SLIDE ARMED NORMALLY. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121200102 20071212 00102 NM 2007 12 12 2007UALA04834 1 20071123 A 3350 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT LOOSE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 548UA 25396 EMERGENCY EXIT SWITCH LOOSE. FOUND DAMAGE TO THE SWITCH ASSY BY IMPACT. SECURED THE SWITCH & INSTALLED A NEW SWITCH GUA RD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121200104 20071212 00104 NM 2007 12 12 QXEA200701780 1 20071124 A 3150 WARNING MESSAGE BOMBDR DHC8 DHC8402 1390042 NM PUSHER SYS ILLUMINATED A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 420QX 4147 PDX - AFTER LANDING AND TAXI TO THE GATE, THE PUSHER SYSTEM FAIL CAUTION ILLUMINATED. AFTER RUNNING CHECKLIST, LIGHT CO NTINUED TO BE ON. MAINTENANCE PERFORMED FIM TASK 27-33-00-810-829. CHECKS GOOD, LIGHT DID NOT RETURN. AIRCRAFT RETURN ED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007121200105 20071212 00105 NM 2007 12 12 QXEA200701783 1 20071129 A 3150 WARNING MESSAGE BOMBDR DHC8 DHC8402 1390042 NM FLAP POWER ILLUMINATED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 422QX 4150 SEA- FLIGHT 2431 - AFTER ENGINE START, RECEIVED A FLAP POWER CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENANCE RESET THE CIRCUIT BREAKER AND COMPLIED WITH SERVICE LETTER 27-002. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPL ACED. 2 H 7 2 4T RT A13NM 2007121200106 20071212 00106 SO 2007 12 12 C2XA07IA236 1 20071124 A 2611 SMOKE WARNING EMB 145 EMB145XR 3260214 SO COCKPIT FALSE ACTIVATION A C2XA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING UK UNKNOWN 1 SW 27 24103 145645 BRO - FLIGHT 2196, THE CREW REPORTED BAGGAGE SMOKE INDICATION INTERMITTENTLY DURING FLIGHT, THE CREW DISCHARGED THE BAGG AGE FIRE BOTTLES AND LANDED IN BRO WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT WITH NO EVIDENCE OF FIRE OR SMO KE FOUND. REPLACED THE FIRE BOTTLES, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007121200107 20071212 00107 NM 2007 12 12 QXEA200701772 1 20071202 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 415QX 4081 YVR- ON TAXI, TAKEOFF WARNING TEST ACTIVATES WITH ALL ITEMS APPEARING TO BE SET CORRECTLY. RETURNED TO THE GATE. MAINT ENANCE RESET THE ELEVATOR TRIM IAW SERVICE LETTER 27-006. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PA RTS REPLACED. 2 H 7 2 4T RT A13NM 2007121200111 20071212 00111 SO 2007 12 12 C2XA07IA237 1 20071121 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO CABIN SMOKE A C2XA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 13202 14500962 SAT - FLIGHT 998, THE CREW REPORTED AN ACRID SMOKE IN THE REAR OF THE AIRCRAFT WITH LAV SMOKE ALARM WHEN SWITCHING FROM APU TO ENGINE BLEEDS. MAINTENANCE INSPECTED THE AIRCRAFT, PERFORMED OPERATIONAL CHECKS OF THE ENGINE/APU BLEED SYSTEMS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007121200115 20071212 00115 CE 2007 12 12 135375120507 1 20071204 A 3260 SWITCH CESSNA 402 402C 207590R CE NLG CONTAMINATED E HYIA O OTHER N FALSE WARNING LD LANDING 1 EA 61 375R 402C0468 ON LANDING AT ACK, NOSE LANDING GEAR FAILED. PILOT HAD 3 GREEN DOWN AND LOCKED INDICATIONS PRIOR TO AND AFTER LANDING. AFTER SECURING GEAR DOWN AND LOCKED, REMOVING AND REPLACING BOTH PROPELLERS, AN ENGINE RUN UP, AND INSPECTION, AIRCRAFT FERRY FLOWN TO MAINTENANCE BASE FOR FURTHER INVESTIGATION. PART WAS INSPECTED AND OVERHAULED. UPON INITIAL INSPECTION NO DAMAGE WAS NOTED. UPON TEARDOWN EVIDENCE OF WATER WAS FOUND IN COVER. SUSPECT FREEZE UP OF TOWER AND SWITCH MECHANISM . UNIT HAS BEEN RETURNED TO SERVICE. 1 L 7 2 3O A7CE 2007121200116 20071212 00116 EA 2007 12 12 REXA200700064 1 20071204 A 3310 RHEOSTAT CNDAIR CL600 CL6002B19 1900309 EA FLOOD LIGHT SMOKE A REXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 8969A 7969 FIRST OFFICERS FLOOD LIGHT RHEOSTAT SMOKING AND LIGHT BLINKING. 2 L 7 2 4F RT A21EA 2007121200117 20071212 00117 EA 2007 12 12 TRAX200701771 1 20071119 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 AAR - ALL PLACARDS ON CREW ESCAPE HATCH EXTERIOR ARE WORN. 2 L 7 2 4F RT A21EA 2007121200118 20071212 00118 NM 2007 12 12 NWAA073905518 1 20071120 A 5330 SKIN BOEING 757 757251 1384970 NM BS 418 S17L GOUGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 518US 23206 DURING LINE CHECK, FOUND DENTS AND GOUGES IN FUSELAGE SKIN AT BS 418 S17L. REPAIRED PER EA 55-210494 SECT I SECTION II P ERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 100 HOURS AND 50 CYCLES FROM ORIGINAL DATE OF DISCREPANCY. 2 L 7 2 4F RT A2NM 2007121200121 20071212 00121 EU 2007 12 12 TRBA2007108 1 20071202 A 3246 WHEEL AEROSP ATR72 ATR72212 8680945 EU NR 3 DAMAGED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 308AE 309 POST FLIGHT INSPECTION REVEALED NR 3 WHEEL TIRE AT ODD ANGLE AND BRAKE DISC OUT OF POSITION. REMOVED AND REPLACED RT ML G AS PER JIC 32-11-00. 2 H 7 2 4T RT A53EU 2007121200126 20071212 00126 WP 2007 12 12 UPS07851240 1 20071203 A 5740 BRACKET DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:SP BRACKET CRACKED AT 3 BOLT HOLES L/WING FRONT SPAR UPPER INBD CORNER STA 680. REMOVED, FABRICATED, AN D INSTALLED REPAIR BRACKET AT L/WING FRONT SPAR STA 680 IAW SRM 51-1-21, AND DWG 5615800. 2 L 7 4 4F RT 4A25 2007121200127 20071212 00127 2007 12 12 UPS07M51233 4 20071202 A 2565 SLIDE DOUG MD11 MD11F 3023600 NM L1 DOOR UNWANTED DEPLOY A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 285UP 48457 L1 DOOR SLIDE BLOWN. REMOVED AND REPLACED SLIDE PER AMM 25-61-15-4. SERVICE PAX DOOR PNEU BOTTLE PER AMM 12-25-04-3. OPERATIONAL CHECK OF L1 DOOR PER AMM 52-11-02-2. FOUND OK. ARM/DISARM LEVER CHECKED NORMAL. 2 L 7 3 4F RT A22WE 2007121200131 20071212 00131 NM 2007 12 12 UPS07M51246 1 20071018 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C RT HORIZ STAB NR 20 BARREL NUT HOLE FOUND CORRODED CORROSION AT BARREL NUT REMOVED PER SRM 51-21-0 1V.2R.35.10X MAGNIFICATION DETAILED VISUAL INSP C/OUT FOUND NO CORROSION EVIDENT. BARREL NUT BORE BLEND OUT VOID AND B OTTOM PERIPHERY RADIUS SMOOTHEN AND PROTECTED PER SRM 51 -21-01 V.2R.35. REP SLEEVE BUSHING FAB AND PROTECTED PER EO MD 11-5510-19409 -L. REP C/OUT AT BARREL NUT BORE NR 20 RT IS ACCEPTABLE PER EN 1696-07. 2 L 7 3 4F RT A22WE 2007121200133 20071212 00133 NM 2007 12 12 UPS07M51248 1 20071028 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C LT HORIZ STAB NR 7 BARREL NUT HOLE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED PER SRM 51-21 -01V.2R.40.10X MAGNIFICATION DETAILED VISUAL INSP FOUND NO CORROSION EVIDENT. BARREL NUT BORE BLEND OUT VOIDS AND BOTTO M PERIPHERY RADIUS SMOOTHENED AND PROTECTED PER SRM 5 1-21-01V2R.40. REP SLEEVE BUSHING FAB AND PROTECTED PER EO MD11-5 510-19409- L FIG 5. REP C/OUT AT NR 7 LT BORE IS ACCEPTABLE PER EN 1712-07. 2 L 7 3 4F RT A22WE 2007121200136 20071212 00136 NM 2007 12 12 UPS07M51250 1 20071010 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C LT HOR STAB NR 1 BARREL NUT HOLE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED PER SRM 51-21-0 1V.2R.35. 10X MAGNIFICATION DETAILED VISUAL INSP C/OUT AND FOUND NO CORROSION EVIDENT. BARREL NUT BORE BOTTOM AND BLEND OUT PERIPHERY RADIUS SMOOTHED AND PROTECTED PER SRM 51-21-01V.2R.35. REP SLEEVE BUSHING FAB AND PROTECTED PER EO MD11- 5510-19409 -L FIG 5. REP C/OUT AT NR 1 LT BORE IS ACCEPTABLE PER EN179-07. 2 L 7 3 4F RT A22WE 2007121200140 20071212 00140 NM 2007 12 12 UPS07M51253 1 20071019 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C RT HORIZ STAB NR 17 BARREL NUT HOLE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED PER SRM 51-2 1-01V.2R.35. REAM BORE FURTHER TO 1.089:DIAM PER EN1704-07. REAM B/NUT BORE FURTHER TO 1.12 1"DIA PER EN 1704-07. B/N UT BORE BLEND OUT VOIDS AND BOTTOM PERIPHERY RADIUS SMOOTHED AND PROTECTED PER SRM 51-21-01V.2R.40. REP SLEEVE BUSHING FAB AND PROTECTED PER EO MD11-5510-19409-L FIG 5. REP C/OUT IS ACCEPTABLE PER EN1704-07. 2 L 7 3 4F RT A22WE 2007121200144 20071212 00144 EA 2007 12 12 TRAX200701844 1 20071201 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 659CA 10153 G4 GALLEY EMERGENCY LIGHT HAS SEVERAL INOP BULBS. 2 L 7 2 4F RT A21EA 2007121200147 20071212 00147 NM 2007 12 12 SWAA075841 1 20071126 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121200149 20071212 00149 NM 2007 12 12 SWAA075842 1 20071126 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121200150 20071212 00150 EA 2007 12 12 TRAX200701852 1 20071201 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 PAX DOOR OUTER HANDLE IS CRACKED. REMOVED CRACKED UNSERVICEABLE OUTER HANDLE ASSY IAW AMM 52-11-03. OBTAINED NEW SERVI CEABLE OUTER HANDLE ASSY PN 601R31704-7. INSTALLED NEW SERVICEABLE HANDLE ASSY PN 601R31704-7, PERFORMED FUNCTIONAL TE ST OF PAX-DOOR OUTER HANDLE AS PER CRJ 200 AMM 52-11-03. NO-DEFECTS. PERFORMED OPERATIONAL TEST OF PAX-DOOR OUTER HANDLE AS PER AMM 52-11-03, NO DEFECTS. 2 L 7 2 4F RT A21EA 2007121200153 20071212 00153 EA 2007 12 12 TRAX200701853 1 20071201 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 PAX DOOR TOP STEP CRACKED ON THE AFT SIDE. REPAIRED IAW REO 601R-52-11-1401. COMPLIED WITH EO 600-52-43 NO DEFECTS NOTE D. 2 L 7 2 4F RT A21EA 2007121200154 20071212 00154 EA 2007 12 12 TRAX200701854 1 20071201 A 5210 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 PAX DOOR FWD SUPPORT CRACKED UNDER STEP 832CT. COMPLIED WITH REO 601R-52-11-702 FOR REPAIR OF PAX DOOR FWD SUPPORT UND ER STEP 832CT. 2 L 7 2 4F RT A21EA 2007121200156 20071212 00156 NM 2007 12 12 SWAA075855 1 20071126 A 5311 65C22910 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 22R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007121200157 20071212 00157 EA 2007 12 12 TRAX200701855 1 20071201 A 7830 TRACK CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 LT ENG T/R BOTTOM O/B TRACK CRACKED CLOSE TO MOUNTING BOLT. REMOVED UNSERVICEABLE LT ENGINE T/R BOTTOM O/B TRACK IAW S HORTS CMM 78-30-00-040-002-A01. INSTALLED NUTPLATES P/N MS21059L3 AND MS 21061L3 USING MS 20426AD3 RIVETS ON NEW SERVICE ABLE TRACK ASSY P/N 228-50809-803 IAW CRJ 200 SRM 51-45-00. OK TO INSTALL. INSTALLED LT ENGINE T/R BOTTOM O/B TRACK IAW SHORTS CMM 78-30-440-010-A01. REFER TO FORM 409D FOR OPERATIONAL CHECK. TRACK INSTALLATION . 2 L 7 2 4F RT A21EA 2007121200159 20071212 00159 NM 2007 12 12 SWAA075857 1 20071126 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND STRINGER 24R CORRODED AT BS 363. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2007121200160 20071212 00160 NM 2007 12 12 SWAA075858 1 20071126 A 5330 6545776 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 902, STR 23R. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007121200161 20071212 00161 EA 2007 12 12 TRAX200701858 1 20071201 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 FS 280 UPPER AFT ANGLE IS CRACKED O/B OF LBL 9. REPAIRED UPPER AFT ANGLE F.S. 280.00 O/B OF LBL 9.00 IAW REO 601R-53-1 1-138 REQUIRES FILLET SEAL / TOPCOAT. FILLET SEALED. IAW SRM 51-23-00 AND TOPCOATED. IAW SRM 51-25-16. 2 L 7 2 4F RT A21EA 2007121200163 20071212 00163 NM 2007 12 12 SWAA075854 1 20071126 A 5330 6545767 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 413, LBL 2. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2007121200164 20071212 00164 2007 12 12 ASAA0752351 4 20071204 A 2210 8221567102 KNOB BOEING 737 737890 1384527 NM ALTITUDE SELECT LOOSE A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 583AS 35681 SELECTOR KNOB ON ALTITUDE SELECT MCP IS LOOSE. TIGHTENED LOOSE KNOB. 2 L 7 2 4F RT A16WE 2007121200165 20071212 00165 NM 2007 12 12 SWAA075860 1 20071126 A 5553 6546568 FITTING BOEING 737 7373A4 1384585 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED 20Y CHECK, FOUND LT VERTICAL STABILIZER FITTING LUG FACES CORRODED. REPAIRED FITTING PER ER. 2 L 7 2 4F RT A16WE 2007121200168 20071212 00168 NM 2007 12 12 SWAA075848 1 20071125 A 2560 10107451 SIGN BOEING 737 737317 138447P NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 L1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007121200171 20071212 00171 NM 2007 12 12 SWAA075850 1 20071126 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 720WN 27854 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS INOP BETWEEN ROW 9 ABC AND ROW 11 ABC. REMOVED AND REP LACED BATTERY AND BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007121200172 20071212 00172 NM 2007 12 12 SWAA075861 1 20071121 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 757LV 29850 DURING SCHEDULED 8Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007121200173 20071212 00173 NE 2007 12 12 USAA920071255 2 20071201 A 7321 FMU500MK4 METERING UNIT AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 2 ENG FUEL FAULTY A USAA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 EA 19 637AW 39036 3597 99 V0091 FLT NR 9205 - TPA-PHX - IFSD - LEVEL OFF AT 5000' ON APPROACH TO PHX, RIGHT ENG DID NOT RESPOND TO AUTOTHRUST. ENGINE I NDICATIONS WERE LESS THAN IDLE. PERFORMED ECAM ACTIONS TO SHUT DOWN NR 2 ENGINE. FUEL CONTROL DID NOT RESPOND TO NR 2 ENG MASTER. PUSHED NR 2 FIRE P/B TO SHUTDOWN ENGINE. POST-FLIGHT REPORT FAULTS THE NR 2 FMU/HC/EEC. MAINTENANCE REMOV ED AND REPLACED THE NR 2 FUEL METERING UNIT. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E311NE 2007121200174 20071212 00174 EU 2007 12 12 07FDEA04998 1 20071204 A 5320 A5377145421600 SILL AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 FWD CARGO COMPARTMENT DOOR SILL LOWER/AFT CORNER CORRODED. REMOVED NR 10 LATCH FITTING AND ANGLE IN AFT CORNER. REMOVE D CORROSION IAW A310-200 SRM 51-74-10-8. MAT THICKNESS .243 LOWEST SPOT REMOVED 0.110 FOUND TO BE OUT OF LIMITS. FAB RICATED REPAIR IAW A310-200 SRM 53-13-83 FIG 203 SHEET 1. ALODINED REPAIR PARTS AND SILL AREA IAW A310-200 SRM 51-21-10 . PRIMED AND PAINTED REPAIR PARTS AND DOOR SILL AREA IAW A310-200 SRM 51-23-10. INSTALLED NEW CORNER ANGLE IAW A310-20 0 SRM 51-40-21. INSTALLED DOUBLER AND NR 10 DOOR LATCH FITTING IAW A310-200 SRM 53-13-83 FIG 203 SHT.1 2 L 7 2 4F RT A35EU 2007121200176 20071212 00176 EU 2007 12 12 07FDEA04999 1 20071204 A 5340 A5377293500200 FITTING AIRBUS 310 A310203 3930313 EU ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 FWD CARGO COMPARTMENT DOOR LOCK FITTING AT NR 1 POS GOUGED ON BOTH LUGS. RECEIVED NEW DOOR LOCK FITTING P/N A5377293500 200 PO NR 597399.1. INSTALLED FITTING IAW A310-200 SRM 51-40 20 AND 53-13-83 PARA 5 SHT 1. FITTING WAS INSTALLED ON FE DEX JOB CARD NON-ROUTINE N00900. 2 L 7 2 4F RT A35EU 2007121200177 20071212 00177 NM 2007 12 12 07FDEA05000 1 20071204 A 5320 141N511153 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 SHORT SECTION OF FLOOR SUPPORT BS 333.45 I/B OF LBL 45.5 HAS CORROSION. REMOVED CORRODED SUPPORT BEAM AT STA 333 - 335, LBL 45.5 IAW SRM 51-40-02. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS PER SRM 53-00-51, FIG 101. FABRICATED NEW SUPPORT BEAM ON NR T7/705498. LOCATED AND DRILLED BEAM IAW SRM 51-40-05. TREATED AND PRIMED BEAM IAW SR M 51-20-01. TOP COATED BEAM IAW MM 51-20-00. INSTALLED BEAM IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007121200178 20071212 00178 NM 2007 12 12 HALA0700515 1 20071204 A 4900 APU BOEING 767 76733A 1385209 NM SHUTDOWN A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 581HA 28139 ETOPS SIGNIFICANT SYSTEM, APU SHUT DOWN ON TAXI IN, PER FIM 49-11-01. BITE ECU NO FAULTS OPS CK GOOD APU OK TO CONTINUE . 2 L 7 2 4F RT A1NM 2007121200180 20071212 00180 NM 2007 12 12 HALA0700516 1 20071201 A 4900 APU BOEING 767 76733A 1385209 NM UNKNOWN A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, APU FAILED TO START. FAULT LGT ILLUM AND EICAS MSG APU FAULT DISPLAYED. BITE CK ECU, NO FAUL TS NOTED. CHECKED APU OIL QTY OK. STARTED APU ON GRD 2X, NORMAL STARTS OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007121200182 20071212 00182 EA 2007 12 12 SIMA200733905 1 20071203 A 2840 COMPUTER CNDAIR CL600 CL6002C10 1390015 EA FUEL QTY MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 500AE 10025 CREW REPORTED IN CRUISE FUEL QUANTITY INDICATION WENT TO DASHES IN ALL TANKS ELECTED TO RETURN TO DFW. REMOVED AND REPL ACED THE FUEL QUANTITY GAUGING COMPUTER IAW CRJ 700 AMM 28-41-22. OPS CHECK GOOD. NO CURRENT FAULTS NOTED. AIRCRAFT R ETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007121200184 20071212 00184 EU 2007 12 12 SIMA200733902 1 20071202 A 5347 7253799459 SEAT TRACK SAAB SF340 340B 7860101 EU BS 619-686 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 232AE 23550 5000 340B232 DURING A HMBV INSPECTION, THE SEAT TRACK AT BL 18.3L WAS FOUND TO BE CORRODED BETWEEN FS 619.0 AND FS 686.0. REPLACED S EAT TRACK AT BL 18.3L BETWEEN FS 619.0 AND FS 686.0 PER SAAB SRM (79LKS 3079 REV 49) CHAPTER 53-70-60. AIRCRAFT RETURNE D TO SERVICE. 2 L 7 2 4T RT A52EU 2007121200185 20071212 00185 EU 2007 12 12 SIMA200733904 1 20071203 A 2120 UNKNOWN SAAB SF340 340B 7860101 EU COCKPIT SMOKE A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 323AE 340B323 CREW REPORTED AIRCRAFT DID A AIR TURN BACK FOR SMOKE IN THE COCKPIT. 2 L 7 2 4T RT A52EU 2007121200186 20071212 00186 EU 2007 12 12 SIMA200733903 1 20071202 A 5311 7253621501 FRAME SAAB SF340 340B 7860101 EU FS 225 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 307AE 21265 5000 340B307 DURING MBV INSPECTION THE FRAME AT FS 225.0 WAS FOUND TO BE CORRODED. REPAIRED FRAME AT FS 225.0 PER SAAB SRM (72LKS 30 79 REV49) CHAPTER 53-70-30. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007121200187 20071212 00187 SO 2007 12 12 SIMA200733906 1 20071201 A 2760 SPOILER SYS EMB 145 EMB145LR 3260212 SO UNWANTED DEPLOY A SIMA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SW 21 619AE 145101 CREW ABORTED T/O AT 30 KNTS FOR UNCOMMENTED SPOILER DEPLOYMENT. 2 L 7 2 4T RT T00011AT 2007121200188 20071212 00188 EU 2007 12 12 SIMA200733901 1 20071130 A 5311 7253721439 FRAME SAAB SF340 340B 7860101 EU FS 258 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 307AE 21265 5000 340B307 DURING MBV, THE FRAME AT FS 258.0 WAS FOUND TO BE CORRODED. REPAIRED FRAME AT FS 258.0 PER SAAB SRM (72LKS 3079 REV 49) CHAPTER 53-70-30. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007121200190 20071212 00190 SO 2007 12 12 SIMA200733910 1 20071204 A 7810 NOZZLE EMB 145 EMB145LR 3260212 SO ENGINE DIRTY A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 619AE 145101 WHEN THRUST LEVERS PUSHED FWD, SMOKE FILLED COCKPIT AND WHEN THRUST LEVERS PULLED BACK SMOKE STARTED TO DISSIPATE. AIR CRAFT RETURNED TO SERVICE. CLEANED EXHAUST NOZZLE NR 1. OPERATIONAL CHECK GOOD IAW EMB 145 AMM 36-10-00 AIRCRAFT RETUR NED TO SERVICE 2 L 7 2 4T RT T00011AT 2007121200191 20071212 00191 EU 2007 12 12 AALA20072294 1 20071125 A 3241 ANTI-SKID SYS AIRBUS 300 A300B4605R 3930308 EU MLG FAILED A AALA O OTHER M A OVER TEMP FLAME/FIRE AP APPROACH 1 SW 21 90070 513 SDQ - FLIGHT LANDED WITH ONLY ONE BRAKE SYSTEM FUNCTIONAL. BRAKES REACHED EXCESSIVE TEMPERATURE CAUSING REPORTED FIRE. FIRE WAS EXTINGUISHED BY FIRE DEPARTMENT. REPLACED NUMBER FOUR BRAKES, WHEEL SLEEVE, COOLING MOTORS, FANS, ANTI-SKID T RANSDUCER AND NUMBER THREE AND FOUR TIRES. CLEANED NUMBER SEVEN TRANSDUCER CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPE RATION. FERRIED TO TUL FOR FURTHER EVALUATION. REPLACED RIGHT MAIN LANDING GEAR AXLE/BOGIE BEAM AND NUMBER EIGHT BRAKE SELECTOR VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121200193 20071212 00193 NM 2007 12 12 AALA20072300 1 20071127 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 767AJ 33539 EMERGENCY LIGHT AT FIRST CLASS LEFT COAT CLOSET INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FIRST CLASS LEFT COAT CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121200194 20071212 00194 EU 2007 12 12 AALA20072301 1 20071127 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 JFK - SEAT MOUNTED EMERGENCY LIGHTS AT AFT MID CABIN LEFT INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT AFT MID CABIN LEFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121200195 20071212 00195 EU 2007 12 12 AALA20072302 1 20071127 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 JFK - EMERGENCY LIGHTS AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT NUMBER O NE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121200198 20071212 00198 WP 2007 12 12 AALA20072296 1 20071126 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 968TW 53618 LGA - EMERGENCY LIGHT AT SEAT ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 20. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007121200200 20071212 00200 NM 2007 12 12 AALA20072297 1 20071126 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 795AN 30257 JFK - EMERGENCY LIGHTS AT SEAT ROWS 20 TO 26 RIGHT AND LEFT INOPERATIVE. REPLACED BATTERY PACK AT RIGHT NUMBER THREE DO OR FOR EMERGENCY LIGHTS AT SEAT ROWS 20 TO 26 RIGHT AND LEFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121200201 20071212 00201 EU 2007 12 12 AALA20072303 1 20071127 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 JFK - EMERGENCY LIGHTS AT RIGHT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121200202 20071212 00202 EU 2007 12 12 AALA20072305 1 20071127 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 JFK - EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIGHT NUMBER T WO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121200206 20071212 00206 EU 2007 12 12 YENA2007105 1 20071123 A 2750 WARNING SYSTEM EMB ERJ190 ERJ190100IGW 3260408 EU T/E FLAP ACTIVATED A YENA O OTHER J WARNING INDICATION AP APPROACH 1 EA 15 190JB 19000011 WHEN SELECTING FLAPS 1 RECEIVED FLAP FAIL EICAS. RAN QRH. LANDED WITH FLAPS/SLATS 0. PERFORMED FIM TASK 27-51-00-810- 802-A, VERIFIED ALL FLAP ACTUATOR TORQUE LIMITERS ARE NOT TRIPPED. FAULT CLEARED. FLAP OPERATIONAL CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A57NM 2007121200208 20071212 00208 SO 2007 12 12 C2XA07CL101 1 20071127 A 3030 CS500060D4A RELAY EMB 145 EMB145XR 3260214 SO COCKPIT BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 27 34110 145658 CLE - FLIGHT 2986 - THE CREW REPORTED A ELECTRICAL BURNING SMELL IN CABIN AROUND ROW 7 AND SMALL AMOUNT OF SMOKE AFTER B EGINNING DESCENT. TEMPORARILY RECEIVED PITOT 2 INOPERATIVE ON THE EICAS PRIOR TO ODOR. MAINTENANCE INSPECTED AND REPLA CED RELAY K0054 AND SOCKET K0054 OF PITOT NR 2. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2007121200209 20071212 00209 NM 2007 12 12 HNAA0700274 1 20071126 A 5270 864202 SENSOR DHAV DHC8 DHC8102 2809003 NM CARGO DOOR FAILED A HNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 07 941HA 47919 47919 161 BAG DOOR WARNING LIGHT ILLUMINATED AFTER TAKEOFF, WENT OUT AT 6000 FEET AND CAME BACK ON AT 7500 FEET AND THEN BACK OFF AT 6000 FEET. MAINTENANCE CONFIRMED THAT THE FORWARD BAG DOOR SENSOR IS BAD AND NEEDS TO BE REPLACED. SENSOR WAS REPLA CED, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2007121200213 20071212 00213 NM 2007 12 12 UPS07M51211 1 20071023 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C CABIN ALONG STA 1721, ALONG LBL 28 (X=28), SEAT TRACK CROWN AREA FOUND CRACKED. DAMAGED SEAT TRACK AT STA 1671 & STA 1771 LBL 28", TRIMMED OFF PER SRM 53-70-00D FIG 1V1 R35. HFEC INSP C/OUT PER DAC NDTSPM R.13 PART06-10- 01.001, NO CRACK EVIDENT. NEW SEAT TRACK & REP PARTS HOLES P/UP & PROTECTED PER SRM 51-31-01 & 51-21-01 V2 R35. NEW SE AT TRACK PAINTED PER SRM 51-21-01V2 R35. OK TO INSTALL. PARTS INSTALLED PER SRM 51-31-01 & 51-33-01 V2 R40. 2 L 7 3 4F RT A22WE 2007121200214 20071212 00214 EA 2007 12 12 TRAX200701774 1 20071124 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 907EV 7648 ASD FWD ANCHOR FITTING CRACKED. FLT 4673 DEL 206 MINS. 2 L 7 2 4F RT A21EA 2007121200216 20071212 00216 EA 2007 12 12 TRAX200701776 1 20071124 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 902EV 7620 AFT PRESSURE BULKHEAD CRACKED AT LINTEL FITTING. REF; NDTM PART 6 53-61-153. 2 L 7 2 4F RT A21EA 2007121200218 20071212 00218 EA 2007 12 12 125ST11 1 20071125 A 3260 6015778853 PROXIMITY SWITCH CNDAIR CL600 CL6002B16 1900305 EA NLG FAILED E DBCA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 13 125ST 5052 AFTER TAKEOFF NOSE GEAR DID NOT RETRACT. CREW MADE UNEVENTFUL LANDING AT FLL. BOMBARDIER SERVICE CENTER DETERMINED THE NOSE GEAR CENTERING PROXIMITY SWITCH HAD FAILED. BOMBARDIER SERVICE CENTER REPLACED NOSE GEAR CENTERING PROXIMITY SWIT CH. OPERATIONS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2007121200220 20071212 00220 NM 2007 12 12 SWAA075873 1 20071127 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 267WN 32525 DURING SCHEDULED MV1 CHECK, FOUND EEPLS END CAP BROKEN AT ROW 1 ABC. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 2007121200222 20071212 00222 NM 2007 12 12 SWAA075891 1 20071127 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FIT TING PER MM. 2 L 7 2 4F RT A16WE 2007121200223 20071212 00223 NM 2007 12 12 SWAA075890 1 20071127 A 5311 6546560 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 947 STR 18R AND STR 18L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007121200224 20071212 00224 NM 2007 12 12 SWAA075893 1 20071127 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007121200225 20071212 00225 NM 2007 12 12 SWAA075874 1 20071127 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121200227 20071212 00227 NM 2007 12 12 SWAA075876 1 20071127 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 473WN 33832 DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS CRACKED AT ROW 5 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007121200228 20071212 00228 NM 2007 12 12 SWAA075877 1 20071127 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 775 AND BS 786, STR 18L AND STR 19L. REPAIRED SKIN P ER SRM. 2 L 7 2 4F RT A16WE 2007121200229 20071212 00229 NM 2007 12 12 SWAA075878 1 20071127 A 2560 65C16820 HOOK BOEING 737 7375H4 138449D NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2007121200230 20071212 00230 NM 2007 12 12 SWAA075882 1 20071127 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007120700215 20071207 00215 NM 2007 12 7 F3LA200700342 1 20071127 A 5347 D5347219021000 SEAT TRACK AIRBUS A319 A319111 3930336 NM CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED SEAT TRACK FLOORBEAM +Y1292 FROM FR 64 TO 4 INCHES AFT OF FR 66 CORRODED AT NUTP LATE HOLES. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11 AND 51-44-11. 2 L 7 2 4F RT A28NM 2007120700217 20071207 00217 NM 2007 12 7 TSAA0734063 1 20071128 A 3411 PITOT HEAD BOEING 737 737236 1384476 NM OBSTRUCTED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 836AL 23225 NON-ETOPS FLIGHT 275 HNL-LIH. DURING TAKEOFF, THE NR 2 AIRSPEED INDICATOR AND THE NR 2 ALTIMETER FAILED TO OPERATE PROP ERLY. THE CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE CLEARED DEBRIS FROM THE FIRST OFFICER’S PITOT/STA TIC SYSTEM. AS A PRECAUTION, MAINTENANCE ALSO REPLACED THE NR 2 AIR DATA COMPUTER CIRCUIT BREAKER. SYSTEM OPERATIONAL CHECK PER AMM 34-12-0, WITH ALL CHECKS SATISFACTORY. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007121100004 20071211 00004 EA 2007 12 11 TRAX200701783 1 20071127 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 826AS 7210 PAX DOOR STEP "EXIT" PLACARD IS WORN. 2 L 7 2 4F RT A21EA 2007121100005 20071211 00005 EU 2007 12 11 TRAX200701810 1 20071127 A 5320 BRACKET AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 ON RT SIDE AT FR 39 STRG14R-13R OMEGA BRACKET FOUND CRACKED. 2 H 7 2 4T RT A53EU 2007121100007 20071211 00007 EA 2007 12 11 TRAX200701815 1 20071127 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 681BR 7680 IN CLIMB-OUT AT FL280 W/FLAPS SELECTED 0 RECIEVED A FLAPS FAIL CAUTION MESSAGE. THE FLAP SELECTOR WAS NOT USE, EMERGENC Y DECLARED. 2 L 7 2 4F RT A21EA 2007121100025 20071211 00025 EU 2007 12 11 TRAX200701798 1 20071127 A 5313 STRINGER SPLICE AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 STRINGER 17R, SPLICE CORRODED BTW FR 34-35. STR 17 RT SPLICE BTW FR 34-35 CORROSION REMOVED AS PER SRM 51-21-42 MATER IAL THICKNESS: 0.063 MATERIAL REMOVED: 0.003 WITHIN LIMITS AS PER SRM: 53-61-00 FIG 301. 2 H 7 2 4T RT A53EU 2007121100033 20071211 00033 EA 2007 12 11 TRAX200701838 1 20071129 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 826AS 7210 FOUND LT SIDE FS 484 INTERCOSTAL INBD CLIP CRACKED. 2 L 7 2 4F RT A21EA 2007121100034 20071211 00034 EA 2007 12 11 TRAX200701839 1 20071129 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 820AS 7188 FOUND LT SIDE AFT EMERGENCY LIGHT BULB BURNED OUT. 2 L 7 2 4F RT A21EA 2007121100058 20071211 00058 NM 2007 12 11 UIEA200700450 1 20070929 A 5415 BRACE BOEING 747 747228F 1384895 NM NR 1 PYLON LOOSE A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 NR 1 PYLON DIAGONAL BRACE UNDERWING FITTING TENSION FASTENER HEAD SHEARED. REMOVED AND INSTALLED FASTENER AS PER 51-30- 02. 2 L 7 4 4F RT A20WE 2007121100062 20071211 00062 NM 2007 12 11 UIEA200700457 1 20071019 A 5347 BAC15201566 SEAT TRACK BOEING 747 7472D7B 1384803 NM BS 1880 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 SEAT TRACK AT MAIN DECK STA 1880L AND LBL 99 HAS WORN AND TORN CROWN LUGS. PERMANENT REPAIR ACCOMPLISHED AS PER B747-20 0 SRM 53-10-05 FIG 1A, SHEETS 1 THRU 4. ALSO, REFERENCE ATLAS AIR EO NR 4753B098. 2 L 7 4 4F RT A20WE 2007121100063 20071211 00063 NM 2007 12 11 UIEA200700460 1 20071022 A 3510 10622381 TRANSMITTER BOEING 747 747243B 1384830 NM CREW O2 MALFUNCTIONED A UIEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 15 540MC 22508 DIVERSION, DUE TO LOSS OF CREW O2. REPLACED UPPER AND LOWER CREW O2 BOTTLES IAW AMM 12-15-08. REPLACED UPPER AND LOWER CREW O2 PRESS XMITTERS, LEAK CHECKED OKAY. 2 L 7 4 4F RT A20WE 2007121100066 20071211 00066 NM 2007 12 11 UIEA200700471 1 20071115 A 5753 SKIN BOEING 747 7472D7B 1384803 NM LT WING FOREFLAP DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 527MC 22471 LEFT WING INBOARD T/E FOREFLAP HAS SIGNS OF DELAMINATION 15" FROM OUTBOARD EDGE. PERFORMED WING TRAILING EDGE REPAIR AS PER SRM 51-40-09 AND 51-40-06 AND XEO 57-110707. 2 L 7 4 4F RT A20WE 2007121100082 20071211 00082 EA 2007 12 11 TRAX200701768 1 20071121 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 LT OBLIQUE ANGLE ON FS 625 CRACKED, RESOLVED ON W/O: 75509 TASKCARD: N/R-00281. REMOVED CRACKED ANGLE, LOCATED IAW CRJ SRM. 2 L 7 2 4F RT A21EA 2007121100087 20071211 00087 WP 2007 12 11 UPS07851236 1 20071130 A 3350 BULB DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INTERMITTENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 EMERGENCY EXIT LIGHTS DISARM IS INTERMITTENT. RELAMPED LIGHT BULB ON EMERGENCY EXIT LIGHT BULB IAW 33-10-00. OPS CHECK S GOOD. 2 L 7 4 4F RT 4A25 2007121100093 20071211 00093 EA 2007 12 11 TRAX200701841 1 20071129 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 885AS 7521 GALLEY DOOR EMERGENCY SIGN HAS BULBS INOP. 2 L 7 2 4F RT A21EA 2007121100094 20071211 00094 NM 2007 12 11 TSAA0753064 1 20071129 A 5300 6552988 SKIN BOEING 737 737230 1384401 NM BS 973 S21-22L CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 823AL 23154 WHILE PERFORMING INSPECTIONS TO COMPLY WITH AD 03-14-06 A CRACK APPROXIMATELY 1.5 LONG WAS DISCOVERED 1 BELOW STR 21L AT BS 967+6. 2 L 7 2 4F RT A16WE 2007121100095 20071211 00095 NM 2007 12 11 DHLA200700073 1 20071202 A 3350 BATTERY BOEING 727 727223 1384074 NM EMERGENCY LIGHT INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 GL 05 749DH 22013 COCKPIT EMERGENCY EXIT LIGHT INOP WITH EMERGENCY EXIT LIGHT SWITCH ON AND DURING STANDBY POWER CHECK. REMOVED AND REPLA CED COCKPIT EMERGENCY LIGHT BATTERIES PER MM 33-50-101 CK GOOD, P/N MISC062 (2 EACH). 2 L 7 3 4F A3WE 2007121100115 20071211 00115 NM 2007 12 11 ASAA0772314 1 20071123 A 5320 146A81212 WEB BOEING 737 737790 13844CN NM BS 794-847 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 AFT CARGO PIT CORROSION ON WEB RBL 25 794.3 TO 847 REPLACED WITH MADE REPAIR PART IAW BOEING ENG DWG 146A 8120 AND B737 700 SRM 51 40 05 AND 51 40 02. 2 L 7 2 4F RT A16WE 2007121100118 20071211 00118 NM 2007 12 11 ASAA0772317 1 20071130 A 5320 146A81275 WEB BOEING 737 737790 13844CN NM BS 847-867 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 AFT CARGO PIT CORROSION ON WEB RBL 20 BS 847 TO 867 REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2007121100122 20071211 00122 NM 2007 12 11 ASAA0772321 1 20071120 A 5321 146A940121 FLOOR PANEL BOEING 737 737790 13844CN NM BS 887 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 AFT CARGO PIT FLOOR PANEL SPLICE TEE CORRODED BS 887 SPLICE TEE REPLACED. 2 L 7 2 4F RT A16WE 2007121100144 20071211 00144 GL 2007 12 11 SIMA200733707 2 20071202 A 7200 ENGINE EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL NR 1 POWER LOSS A SIMA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SW 21 612AE 145079 CREW REPORTED DURING CRUISE AT FL360, NR 1 ENG EXPERIENCED A SUDDEN LOSS OF RPM BOTH N1 AND N2 INDICATIONS DROPPED APPRO X 70 PERCENT N1, BUT AUTO RELIGHT OCCURRED WITHIN IN 3-5 SECONDS. REST OF THE FLIGHT NORMAL. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007121100148 20071211 00148 SO 2007 12 11 SIMA200733803 1 20071201 A 3260 852701 DOWNLOCK SWITCH EMB 135 EMB135KL 3260302 SO LT MLG DEFECTIVE A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 828AE 145604 CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. ALSO HAD A LANDING GEAR AIR/GND FAIL ON EICAS. CAPT DIVERTED TO LGA. AIRCRAFT LANDED SAFELY WITH NO OTHER PROBLEMS. FOUND MAIN LEFT DOWNLOCK PROXIMITY SWITCH DEFECTIVE. REMOVED AND REPLACED LEFT MAIN PROX SWITCH IAW EMB140 AMM 32-61-02. ALSO, PERFORMED MULTIPLE GEAR SWINGS IAW EMB 140 AMM 32-30-00. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007121100158 20071211 00158 EU 2007 12 11 MALA070192 1 20071204 A 5230 SKIN SAAB SF340 340B 7860101 EU CARGO DOOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 412XJ 340B412 DENTS LOCATED IN CARGO DOOR, ONE AT 23 INCH CARGO DOOR LOWER EDGE, 9 INCHES FROM AFT EDGE. THE OTHER AT 14 INCHES FROM LOWER EDGE, 10 INCHES FROM AFT EDGE. REPAIRED IAW EO NR S52028. 2 L 7 2 4T RT A52EU 2007121100168 20071211 00168 EU 2007 12 11 TRAX200701797 1 20071127 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 RT SIDE FR 36 CORROSION AT FLOORBEAM JUNCTION, RESOLVED ON W/O: 75891 TASKCARD: N/R-00066. RT SIDE, FR 36 AT FLOOR BEAM JUNCTION, CORROSION REMOVED AS PER SRM 51-21-42. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42 MATERIAL THICKNESS: 0.080 MATERIAL REMOVED: 0.003 WITHIN LIMITS AS PER SRM: 53-61-00 FIG 301. 2 H 7 2 4T RT A53EU 2007121100182 20071211 00182 NM 2007 12 11 HALA0700513 1 20071126 A 2612 89873202 CIRCUIT CARD BOEING 767 7673G5 1385126 NM APU FIRE DETECT MALFUNCTIONED A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, STATUS MESSAGE APU FIRE LP 2. REPLACED NR 2 APU FIRE DETECTION CARD PER FIM 26-15-00 FIGURE 1 03. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007121100184 20071211 00184 NM 2007 12 11 ASAA0752341 1 20071202 A 3097 BACC45FT105P CONNECTOR BOEING 737 737890 1384527 NM WINDOW HEAT DAMAGED A ASAA O OTHER O OTHER AP APPROACH 1 NM 02 559AS 35178 ON APPROACH WINDOW HEAT "OVERHEAT" ILLUMINATED FOR RIGHT SIDE WINDOW. FOUND PUSHED PINS ON WINDOW PIGTAIL. REPLACE SAM E. SYSTEM OP CHECKS NORMALLY. 2 L 7 2 4F RT A16WE 2007121100191 20071211 00191 NM 2007 12 11 ASAA0772329 1 20071114 A 5320 147A57102 CHANNEL BOEING 737 737790 13844CN NM BS 992 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 AFT CABIN CORROSION FOUND ON ZEE CHANNEL BS 992 RBL 37, REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2007121100202 20071211 00202 SO 2007 12 11 RAIA00711017 1 20071125 A 3350 1317 BULB EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS BURNED OUT A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 846HK 14500855 PRE FLT 8043 - RIC - LEFT AFT WING/FUESLAGE FAIRING EXTERIOR FLOOD LIGHT INOP. MAINTENANCE REMOVED AND REPLACED NR 1 SI DE EMERGENCY LIGHT, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007121200004 20071212 00004 NM 2007 12 12 ASAA0772342 1 20071119 A 3340 3025053 HOUSING BOEING 737 737790 13844CN NM COLLISION LIGHT CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 UPPER FUSELAGE ANTI COLLISION LIGHT HOUSING SCREW HOLES CRACKED REPLACED UPPER FUSELAGE ANTI COLLISION LIGHT HOUSING WIT H REPLACEMENT PART NR 30 2505 3 PO NR 113319 IAW B737 700 SRM 51 40 02. 2 L 7 2 4F RT A16WE 2007121200005 20071212 00005 NE 2007 12 12 ASAA0752343 2 20071202 A 7321 2044M16P02 EEC BOEING 737 737890 1384527 NM CFMINT CFM567 CFM567B2US 13802 NE NR 2 ENGINE FAULTY A ASAA O OTHER O OTHER CR CRUISE 1 NM 02 587AS 35684 AUTO THROTTLES OPERATING IN "A T LIM" MODE DURING CRUISE. ENGINE BITE SHOWS FAULTS 73 10772 9 (PS3 SIGNAL OUT OF RANGE) AND 73 11282 (EEC CHANNEL NOT ENERGIZED WITH ALTERNATOR VOLTAGE). REPLACED NR 2 EEC. EEC INSTALLATION TEST AT SYSTEM TESTS NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2007121200014 20071212 00014 EA 2007 12 12 VNAA0711006 1 20071115 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT WING DAMAGED A VNAA O OTHER O OTHER LD LANDING 1 GL 05 244PS 7912 CREW REPORTED WHILE LANDING IN CLT, THE LEFT WING STRUCK THE RUNWAY UPON TOUCHDOWN. THE AIRCRAFT TAXIED SAFELY TO THE G ATE WHERE MAINTENANCE INSPECTED AND FOUND DAMAGE TO THE LEFT HAND WINGTIP AND LEFT HAND OUTBOARD FLAP. MAINTENANCE COMP LIED WITH AN EDDY CURRENT INSPECTION FOR THE DAMAGE. MAINTENANCE REPAIRED ALL DAMAGE PER REO 601R-57-00-055. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007121200017 20071212 00017 EA 2007 12 12 VNAA0711009 1 20071118 A 5242 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE EXTERNAL POWER OPEN A VNAA O OTHER O OTHER CL CLIMB 1 GL 05 716PS 10171 CREW REPORTED A LOUD WHINE OR SCREECH FROM THE RIGHT SIDE OF THE COCKPIT AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT A ND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE GPU POWER DOOR OPEN. MAINTENANCE CLOSED THE DOOR AND F OUND NO DEFECTS. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 2007121200019 20071212 00019 EA 2007 12 12 COMA0760661 1 20071122 A 2110 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT TRIPPED A COMA G A O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 973CA 7146 FLIGHT 5057 - RECEIVED LEFT PACK OFF STATUS MESSAGE WITH UNPRESSURIZED FLIGHT AND PASSENGER O2 MASKS DEPLOYED. RETURNED TO JFK, LANDED WITHOUT INCIDENT. RESET C/B 1J1 FOR LEFT PACK. RESTOWED PAX O2 MASKS. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007121200021 20071212 00021 EA 2007 12 12 COMA0760663 1 20071122 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY ACTIVATED A COMA F ACTIVATE FIRE EXT. J WARNING INDICATION LD LANDING 1 SO 01 784CA 27632 7319 FLIGHT 5539 - CARGO SMOKE MESSAGE ILLUMINATED. DISCHARGED NORMAL AND STANDBY BOTTLES. DECLARED EMERGENCY, LANDED WITHO UT INCIDENT. REMOVED AND REPLACED LEFT CARGO FIRE EXTINGUISHER BOTTLE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007121200030 20071212 00030 EA 2007 12 12 COMA0760668 1 20071123 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 659BR 7509 FLIGHT 5217 - FLAPS FAIL CAUTION MESSAGE INTO BNA. AIRCRAFT LANDED SAFELY. COMPLIED WITH AD 2006-12-21 FLAP CAUTION ME SSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAU TION MESSAGES. 2 L 7 2 4F RT A21EA 2007121200034 20071212 00034 EA 2007 12 12 COMA0760672 1 20071126 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 933CA 7040 FLIGHT 5239 - DURING TAXI OUT FLAPS FAIL CAUTION MESSAGE ILLUMINATED. AIRCRAFT RETURNED BACK TO GATE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RES ET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007121200048 20071212 00048 NM 2007 12 12 2007UALA04804 1 20071123 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR DETACHED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 548UA 25396 THE 3R GIRT BAR INOP. ITEM ROLLED FORWARD. DOOR POSITION IS DOOR 4L, GIRT BAR IS DETACHED AND LAYING ON THE FLOOR. ON E SLIDER HAS SPRING CLIP BROKEN OFF. REINSTALLED GIRT BAR/CLIPS. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121200049 20071212 00049 WP 2007 12 12 07FDEA04978 1 20071203 A 5330 NGA6312507 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 308FE 48297 LOWER EXT FUS FOUND DENT .50" BY .50" DEPTH .04" ON SKIN. REPAIRED AREA IAW SRM 53-20-00 FIG 13 VOL I. 2 L 7 3 4F RT A22WE 2007121200050 20071212 00050 WP 2007 12 12 07FDEA04979 1 20071203 A 5347 NFA622239 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 CTR CARGO COMPT DURING PERFORMED J/C MD10-2552-C180 FOUND SEVERE EXFOLIATION CORROSION ON SEAT TRACK. 2 L 7 3 4F RT A22WE 2007121200052 20071212 00052 WP 2007 12 12 07FDEA04981 1 20071203 A 5313 ADA3065501 LONGERON DOUG DC10 DC1010F 3022111 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 FWD CARGO COMPT SUMP AREA FOUND CORROSION WITH EXFOLIATION, SEE NRC N00315, N00316, N00294, N00253. REPAIRED LONGERON I AW SRM 53-10-00 VOL I FIG 5 SHEET 1. 2 L 7 3 4F A22WE 2007121200059 20071212 00059 EU 2007 12 12 07FDEA04986 1 20071203 A 5347 A25213126204 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 CABIN SEAT TRACK CORRODED FROM STATION 1240CM TO 1280 CM, Y 5.0CM. BLENDED AREA IAW A310-200 SRM 51-74-10 AND FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 51-10-16 FIG 101. REMOVED AND REPLACED SEAT TRACK IAW A310-200 SRM 51-40-21 PARA 6 AN D 7. 2 L 7 2 4F RT A35EU 2007121200072 20071212 00072 EU 2007 12 12 07FDEA04997 1 20071204 A 5313 A53980057200201 LONGERON AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 RT LONGERON 11 HAS DEFECT INDICATION ON INNER FLANGE BETWEEN 2 RIVETS AT APPROXIMATE STA 4051. REMOVED COVER PLATE TO G AIN ACCESS TO INNER FLANGE. REMOVED DAMAGE, REPAIRED AREA AND INSTALLED DOUBLE FILLER AND COVER PLATE IAW SRM AB310/200 53-18-18 FIG 205C PAGE 235. 2 L 7 2 4F RT A35EU 2007121200086 20071212 00086 NM 2007 12 12 2007UALA04818 1 20071126 A 3350 78961 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 104UA 26902 SEAT 4A AFT EMERGENCY LIGHT ON ARMREST IS BROKEN. REPLACED LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121200100 20071212 00100 NM 2007 12 12 2007UALA04832 1 20071125 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EXIT LIGHTS FLASHING 57H-61H. CONNECTED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121200101 20071212 00101 NM 2007 12 12 2007UALA04833 1 20071123 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 DOOR 4L, DOOR MOUNTED EMERGENCY EVACUATION LIGHT INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121200109 20071212 00109 NM 2007 12 12 QXEA200701774 1 20071202 A 2420 DH103024600C511B INVERTER DHAV DHC8 DHC8202 2809007 NM 2NDRY FAILED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 347PH 480 PDX - FLIGHT 2050, ON TAXI RECEIVED A SECONDARY INVENTER CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENANCE PLACED THE SYSTEM ON MEL 24-8. AIRCRAFT RETURNED TO SERVICE. REPLACED THE SECONDARY INVERTER. OPERATIONAL CHECKS GOOD. AIRCRAFT R ETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007121200120 20071212 00120 WP 2007 12 12 NWAA073919864 1 20071115 A 5311 FRAME DOUG DC9 DC951 3022051 WP BS 1209 L8L CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 773NC 47775 DURING "H" CHECK, FOUND CRACK IN FRAME INNER CHORD AT BS 1209 L8L. REPAIRED PER EA 98-211041. 2 L 7 2 4F RT A6WE 2007121200122 20071212 00122 NM 2007 12 12 UPS07451230 1 20071201 A 3060 60B500651 HOSE BOEING 747 747123 1384873 NM WATER DRAIN BURNED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:A CK DURING INSPECTION OF EO FOUND WATER DRAIN TUBE CRUSHED AND BURNED. ALSO, FOUND EVIDENCE OF BURNED INSULATION BLANKET REF EO B747-3670-27749B. ORDERED NEW HOSE ON REQ A940808. WORKING WITH ENG ON INSULATION. REPLACE HOSE ASSY PER B747-3070-27749. 2 L 7 4 4F RT A20WE 2007121200124 20071212 00124 EA 2007 12 12 TRAX200701773 1 20071123 A 3250 STEERING SYS CNDAIR CL600 CL6002C10 1390015 EA NLG MALFUNCTIONED A ASOA K NONE J WARNING INDICATION CL CLIMB 1 SO 27 760EV 10212 AFTER TAKEOFF RECEIVED NWS INOP CAUTION MSG. FOLLOWED QRH. AFTER LANDING RESET SYS USING CIRCUIT BREAKERS. MSG EXTING UISHED. EMERGENCY EQUIPMENT ON STANDBY. 2 L 7 2 4F RT A21EA 2007121200125 20071212 00125 WP 2007 12 12 UPS07851239 1 20071202 A 5320 BRACKET DOUG DC8 DC873F 302199F WP FUSELAGE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:SP BROKEN BRACKET ON FUSELAGE ABOVE LEADING EDGE AUX TANK, L/WING. REMOVED, FABRICATED AND INSTALLED RE PAIR BRACKET ON L/WING AUX TANK STA XCW 69.500 IAW SRM 51-3-00-01, AND DWG 5769482. 2 L 7 4 4F RT 4A25 2007121200128 20071212 00128 NM 2007 12 12 UPS07M51243 1 20071018 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C LT HORIZ STAB NR 17 BARREL NUT HOLE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED PER SRM 51-2 1-01V.1R.35.10X MAGNIFICATION DETAILED VISUAL INSPECTION C/OUT AND FOUND NO CORROSION EVIDENT. BARREL NUT BORE BLEND OU T VOIDS AND BOTTOM PERIPHERY RADIUS, SMOOTHEN AND PROTECTED PER SRM 51-21-01V.2R.40. REP SLEEVE BUSHING FAB AND PROTECT ED PER EO MD11-5510-19409-L. REP C/OUT AT NR 17 LT BORE ACCEPTABLE PER EN 1706-07. 2 L 7 3 4F RT A22WE 2007121200129 20071212 00129 NM 2007 12 12 UPS07M51244 1 20071028 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C RT HORIZ STAB NR 25 BARREL NUT HOLE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED PER SRM 51-2 1-01V.2R.40.10 BY MAGNIFICATION DET VISUAL INSP C/OUT FOUND NO CORROSION EVIDENT. BARREL NUT BORE BLEND OUT VOID AND BO TTOM PERIPHERY RADIUS SMOOTHEN AND PROTECTED PER SRM5 -21-01V.2R.40. REP SLEEVE BUSHING FAB AND PROTECTED PER EO MD11-5 510-19409- L FIG 5. REP C/OUT AT RT NR 25 BORE IS ACCEPTABLE PER EN 1710-07. 2 L 7 3 4F RT A22WE 2007121200132 20071212 00132 NM 2007 12 12 UPS07M51247 1 20071018 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C LT HORIZ STAB NR 36 BARREL NUT HOLE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED PER SRM 51-2 1-01V.2R.35. BARREL NUT BORE BOTTOM MACHINE DOWN 0.050" DEEPER AND BORE REAM FURTHER TO2.586" DIA PER EN1697-07. B/NUT BORE BLEND OUT VOIDS AND BOTTOM PERIPHERY RADIUS SMOOTHEN AND PROTECTED PER SRM 1-21-01V.2R.35. REP SLEEVE BUSHING FAB AND PROTECTED PER EO MD11-5510-19409-L. REPAIR C/OUT IS ACCEPTABLE PER EN 1697-07. 2 L 7 3 4F RT A22WE 2007121200134 20071212 00134 EU 2007 12 12 YENA2007104 1 20071126 A 2560 D5211052200000 GIRT BAR AIRBUS 320 A320232 3930326 EU L1 DOOR MALFUNCTIONED A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 519JB 24679 17134 1398 ON C-2 CHECK, TRIGGER OF GIRT BAR DOES NOT GO TO THE UNLOCKED POSITION WHEN PUSHED AT L1 PASSENGER/CREW DOOR 831. THE G IRT BAR ASSY AT PASSENGER/CREW DOOR 831 WAS REPLACED IAW 25-62-44. OPERATIONAL TEST WAS ACCOMPLISHED IAW AMM 52-11-00-2 00-050. OPS TEST OK. 2 L 7 2 4F RT A28NM 2007121200138 20071212 00138 NM 2007 12 12 UPS07M51252 1 20071013 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C LT HORIZ STAB NR 21 BARREL NUT HOLE FOUND CORRODED. CORROSION REMOVED AT BARREL NUT BORE PER SRM 51-2 1-01V.2R.35.10X MAGNIFICATION DETAILED VISUAL INSP C/OUT FOUND NO CORROSION EVIDENT. BARREL NUT BORE BLEND OUT VOIDS AN D BOTTOM PERIPHERY RADIUS SMOOTHEN AND PROTECTED PER SRM51-21-01V.2R.35. REP SLEEVE BUSHING FAB AND PROTECTED PER EO MD 11-5510 -19409-L FIG 5. REP C/OUT AT NR 21 LT BORE IS ACCEPTABLE PER EN 1684-07. 2 L 7 3 4F RT A22WE 2007121200146 20071212 00146 NM 2007 12 12 SWAA075843 1 20071126 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121200148 20071212 00148 EA 2007 12 12 TRAX200701851 1 20071201 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 760EV 10212 FOUND STA 280 FWD FLOOR SUPPORT ANGLE CORRODED AT BL 0. 2 L 7 2 4F RT A21EA 2007121200179 20071212 00179 NM 2007 12 12 LYNX00001 1 20071120 A 3234 AR2674 LATCH BOMBDR DHC8 DHC8402 1390042 NM COCKPIT BROKEN A 3LYA K NONE O OTHER IN INSP/MAINT 1 NM 21 501LX 81 81 4165 DISCOVERED NOSE LANDING GEAR ALTERNATE EXTENSION DOOR WILL NOT OPEN ON PREFLIGHT INSPECTION. FOUND THE LATCH WAS BROKEN WHICH LOCKS THE DOOR IN THE CLOSED POSITION. MAINTENANCE REPLACED THE LATCH. 2 H 7 2 4T RT A13NM 2007121200192 20071212 00192 WP 2007 12 12 AALA20072295 1 20071126 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 968TW 53618 LGA - EMERGENCY LIGHT AT SEAT 25B INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT 25B. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007121200196 20071212 00196 EU 2007 12 12 AALA20072304 1 20071127 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 JFK - EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121200205 20071212 00205 NM 2007 12 12 HNAA0700272 1 20071118 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM CARGO BAY MALFUNCTIONED A HNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 07 824EX 11153 219 387 SMOKE WARNING LIGHT ILLUMINATED ON TAXI OUT SEVERAL TIMES. THE FLIGHT ATTENDANT DID NOT NOTICE THE SMELL OF SMOKE ON TA XI OUT. THE FLIGHT ATTENDANT DID AN INSPECTION OF THE BAG BAY DURING TAXI BACK TO GATE, NO SMOKE WAS DETECTED. INSPECT ED BAG BAY AREA, EVIDENCE OF FIRE OR SMOKE WAS DETECTED. REPLACED BOTH SMOKE DETECTORS S/N: 0555 AND 0772. S/N 0772 H AS HAD PREVIOUS HISTORY OF THIS DISCREPANCY. 2 H 7 2 4T RT A13NM 2007121200217 20071212 00217 2007 12 12 ASAA0752188 4 20071029 A 2210 721101A1 SWITCH BOEING 737 737890 1384527 NM AUTOPILOT SYS FAULTY A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 583AS 35681 THE "A" AUTO PILOT WILL NOT ENGAGE. FFR SHOWS CHANNEL AAP DISCONNECT SWITCH INPUT INVALID. REPLACED S231 SWITCH IAW 22- 11-41. 2 L 7 2 4F RT A16WE 2007121200219 20071212 00219 EU 2007 12 12 YENA2007106 1 20071123 A 2750 5914868 CONTROL UNIT EMB ERJ190 ERJ190100IGW 3260408 EU T/E FLAP MALFUNCTIONED A YENA O OTHER J WARNING INDICATION CR CRUISE 1 EA 15 236JB 3404 19000035 FLT 1052, JFK-PIT, IN CRUISE SLAT FAIL MESSAGE NOT ASSOCIATED WITH MOVEMENT OF THE FLAP HANDLE. FLAP HANDLE WAS IN 0 DE TENT AND SLATS FLAPS DID NOT DEPLOY. SLATS DID NOT DEPLOY WHEN COMMANDED, FLAPS DROVE TO SELECTED DETENT. FAULT FOUND AS TRANSITORY CONDITION OF SUFACE OPERATION TEST OF FLAPS AND SLATS NORMAL. SLAT FLAP HANDLE WAS REPLACED AS PRECAUTION ARY. 2 L 7 2 4F RT A57NM 2007121200232 20071212 00232 NM 2007 12 12 SWAA075881 1 20071127 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121200233 20071212 00233 NM 2007 12 12 SWAA075880 1 20071127 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121200234 20071212 00234 NM 2007 12 12 SWAA075884 1 20071127 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121200237 20071212 00237 NM 2007 12 12 SWAA075886 1 20071127 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING BROKEN. REMOVED AND REPLACED FITTIN G PER MM. 2 L 7 2 4F RT A16WE 2007121200240 20071212 00240 NM 2007 12 12 SWAA075889 1 20071127 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 784SW 29810 DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 7 ABC. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007121200241 20071212 00241 NM 2007 12 12 USAA920071226 1 20071022 A 5311 654795946 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CORROSION ON FRAME, BS 794.30, S23R. REPLACED FRAME, BS 794.30, S23R IAW USAIRWAYS EA 98994. 2 L 7 2 4F RT A16WE 2007121200244 20071212 00244 NM 2007 12 12 ASAA0752284 1 20071126 A 4910 MF530493 FASTENER BOEING 737 737890 1384527 NM APU INLET DAMAGED A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 557AS 35176 APU AIR INLET CHAMBER HAS A LOOSE FASTENER. REMOVED & REPLACED DAMAGED NUT PLATE. SECURED FASTENER. 2 L 7 2 4F RT A16WE 2007121200246 20071212 00246 EA 2007 12 12 TRAX200701777 1 20071125 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 682BR 7691 EMERGENCY EXIT SIGNS AT BOTTOM OF BOTH OVERWING EXIT DOORS INOP. FLT 4828 CX. 2 L 7 2 4F RT A21EA 2007121200247 20071212 00247 EA 2007 12 12 TRAX200701778 1 20071125 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 EXIT PLACARD MISSING AT PAX STAIRWAY DOOR. 2 L 7 2 4F RT A21EA 2007121200248 20071212 00248 NM 2007 12 12 CALA0700694 1 20071121 A 5330 SKIN BOEING 737 737724 13844BY NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24702 28763 LOWER FUSELAGE STA 500 CORRODED AT VERIZON ANT FOOTPRINT. REPAIRED PER SRM 53-00-01 REPAIR 3. 2 L 7 2 4F RT A16WE 2007121200250 20071212 00250 EA 2007 12 12 QXEA200701785 1 20071201 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002C10 1390015 EA ILLUMINATED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 609QX 10031 GEG - FLIGHT 2518 - INTERMITTENT FIRE SYSTEM FAULT MESSAGE. PLACED THE SYSTEM ON MEL 26-00-1. AIRCRAFT RETURNED TO SER VICE. 2 L 7 2 4F RT A21EA 2007121200251 20071212 00251 NM 2007 12 12 CALA0700695 1 20071123 A 5420 311N50052 FITTING BOEING 757 757224 1384958 NM NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12109 27299 REF EA 5440-01234 REV B OP 11 FASTENER 20 HAS CRACK INDICATION, NR 1 PYLON AFT BULKHEAD FITTING. REPAIRED PER ECRA 5450 -01724. 2 L 7 2 4F RT A2NM 2007121200253 20071212 00253 NM 2007 12 12 CALA0700696 1 20071125 A 5210 6552878U124 ANGLE BOEING 737 7373T0 1384582 NM L2 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 SURFACE CORROSION ON L-2 DOOR Z-ANGLE FROM STA 942 TO 993. REMOVED AND REPLACED Z-ANGLE FROM STA 913-1010 REF SRM 51-40 -02. 2 L 7 2 4F RT A16WE 2007121200254 20071212 00254 EA 2007 12 12 QXEA200701793 1 20071203 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002C10 1390015 EA FIRE SYS ILLUMINATED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 601QX 10009 SEA - RECEIVED A FIRE SYSTEM FAULT STATUS MESSAGE. MAINTENANCE PLACED THE SYSTEM ON MEL 26-00-1. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007121200255 20071212 00255 EA 2007 12 12 QXEA200701758 1 20071120 A 8012 START VALVE CNDAIR CL600 CL6002C10 1390015 EA MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 609QX 10031 PDX - FLIGHT 2533 - LEFT START VALVE FAILED TO OPEN DURING CROSS BLEED START. RETURNED TO THE GATE. MAINTENANCE PERFOR MED TWO CROSS BLEED STARTS WITH NO DEFECTS, COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007121200256 20071212 00256 NM 2007 12 12 QXEA200701788 1 20071202 A 3150 WARNING MESSAGE BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS ILLUMINATED A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 416QX 4083 LAX - FLIGHT 2446 - WHEN SELECTING FLAPS FROM 15 TO 35, RECEIVED A FLAP POWER CAUTION MESSAGE. COMPLIED WITH THE EMERGE NCY/ABNORMAL CHECKLIST, NO HELP. AIRCRAFT LANDED WITH FLAPS 15. AFTER LANDING FLAPS WOULD NOT RETRACT. MAINTENANCE CL EARED THE CAUTION BY SERVICE LETTER DH8-400-SL-27-002A. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007121200258 20071212 00258 NM 2007 12 12 CALA0700697 1 20071125 A 5347 BAC1520792 SEAT TRACK BOEING 757 757324 1384930 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 75853 32812 CABIN SEAT TRACK CORRODED AT STA 1320 AND LBL 24.75. REPAIRED PER SRM 53-00-52. 2 L 7 2 4F RT A2NM 2007121200262 20071212 00262 NM 2007 12 12 QXEA200701787 1 20071201 A 3150 WARNING MESSAGE BOMBDR DHC8 DHC8402 1390042 NM STICK PUSHER FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING LD LANDING 1 NM 09 418QX 4143 SEA - DURING LANDING ROLL OUT, RECEIVED A PUSHER SYSTEM FAIL MESSAGE. PER THE CHECKLIST PERFORMED A PUSHER TEST. LIGHT STAYS ON. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE ELEVATOR PUSHER SYSTEM, CHECKS GOOD WITH NO DEFECTS. AIRCR AFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007121200266 20071212 00266 WP 2007 12 12 DHLA200700074 1 20071205 A 7830 UNKNOWN DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C1 13802 NE THRUST REVERSER UNKNOWN A DHLA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 05 805DH 46125 69341 DURING CRUISE, NR 2 ENG REVERSER THRUST LIGHT STARTED FLASHING CREW PERFORMED EMERGENCY AND ABNORMAL PROCEDURES AND SHUT DOWN NR 2 ENGINE. INSPECTED NR 2 TR PER M/M 78-30-0. FOUND NORMAL, T/S NR 2 THR/RVS PER 78-00. CHK AND CLEANED ELECT POS SENSORS PER 78-35-3. CYCLED NR 2 T/R VARIOUS TIMES FLT NODE AND GROUND MODE. ALL NORMAL. RAN NR 2 ENG PER JRH GR OUND IDLE AND FLT IDLE. DID NOT DUPLICATE. OPS NORMAL PER DC8 M/M 78-30-0. 2 L 7 4 4F 4 F RT 4A25 E2GL 2007121200273 20071212 00273 NM 2007 12 12 CALA0700705 1 20071127 A 5320 654580733 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 CABIN FWD ENTRY INTERCOSTAL BETWEEN STRINGER 10R AND 11R O/B SUPPORT ANGLE CRACKED. REMOVED AND REPLACED INTERCOSTAL RE F SRM 53-00-04 AND 53-00-01, 51-40-02. 2 L 7 2 4F RT A16WE 2007121200274 20071212 00274 NM 2007 12 12 CALA0700706 1 20071127 A 5320 654580730 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 CABIN FWD ENTRY INTERCOSTAL WEB FWD OF R-1 DOOR CUTOUT BETWEEN STRINGERS 12R AND 13R O/B SUPPORT CRACKED. REMOVED AND R EPLACED INTERCOSTAL WEB PER SRM 53-00-04, 53-00-01, 51-40-02. 2 L 7 2 4F RT A16WE 2007121200277 20071212 00277 NM 2007 12 12 CALA0700709 1 20071127 A 3350 29335130013 BATTERY PACK BOEING 737 737824 13844BZ NM CABIN FAILED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 24224 28933 EMERGENCY LIGHT BATTERY PACK AT ROW 19ABC FAILED CAPACITY CHECK. REMOVED AND REPLACED LIGHT BATTERY PACK. 2 L 7 2 4F RT A16WE 2007121200278 20071212 00278 NM 2007 12 12 CALA0700712 1 20071128 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 RIGHT I/B SEAT TRACK CORRODED FROM STA 913 TO 936. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK AND REPAIRED STA 887, 947 RIGHT I/B TRACK PER SRM 53-00-52 FIG 201. 2 L 7 2 4F RT A16WE 2007121200279 20071212 00279 NM 2007 12 12 CALA0700713 1 20071128 A 5310 6546561Y509 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 R2 FWD FUSELAGE DOOR FRAME CRACKED BETWEEN S-10R AND S-11R. REMOVED DAMAGED FRAME AND INSTALLED NEW FRAME PER SRM 51-40 -02 PARAGRAPH 4 AND 7. 2 L 7 2 4F RT A16WE 2007121200280 20071212 00280 NM 2007 12 12 HNAA0700275 1 20071127 A 3350 AML91LA85 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST NR NOT REPORTED 1 EA 07 908HA 57185 57185 015 FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH LIGHTING IS INOP. REMOVED AND REPLACED SWITCH LIGHT BULB, OPERATIONAL CHECK GO OD. 2 H 7 2 4T RT A13NM 2007121200281 20071212 00281 EU 2007 12 12 TRAX200701805 1 20071127 A 5714 STRUCTURE AEROSP ATR72 ATR72212 8680945 EU WING BOX CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 RT WING BOX FR 28 CRACKED, RESOLVED ON W/O: 75891 TASKCARD: N/R-00126. ON RT WING BOX FR 28 CRACK REMOVED IAW SRM 51-10 -10 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-10-10. 2 H 7 2 4T RT A53EU 2007121200283 20071212 00283 EU 2007 12 12 TRAX200701814 1 20071127 A 5313 STRINGER AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 AFT AVIONIC COMPARTMENT, BTW FR 44-45 STRINGER 21R CORRODED, RESOLVED ON W/O: 75891 TASKCARD: N/R-00244. AFT AVIONIC CO MPT BTW FR 44-45 STRINGER 21R REPLACED IAW 51-25-01. 2 H 7 2 4T RT A53EU 2007121200285 20071212 00285 EU 2007 12 12 TRAX200701835 1 20071129 A 5311 FRAME AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 FR 23B FOUND CORRODED OUT OF LIMIT ON W/C 100-15 NEEDS SPLICE PART TO BE FABRICATED, RESOLVED ON W/O: 75891 TASKCARD: N/ R-00651. FABRICATION SPLICE PARTS ON FRAME 23B IAW SRM 53-00-00 FIG 430 (SHEET 1). INSTALLATION COVER ON W/C 100-15. 2 H 7 2 4T RT A53EU 2007121200287 20071212 00287 EU 2007 12 12 TRAX200701837 1 20071129 A 5755 SHIELD AEROSP ATR72 ATR72212 8680945 EU RT SPOILER CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 RT SPOILER THUNDER SHIELD FOUND CORRODED OUT OF LIMIT ON WC 600-19 NEEDS TO BE FABRICATED, RESOLVED ON W/O: 75891 TASKCA RD: N/R-00666. RT SPOILER THUNDER SHIELD FABRICATED IAW SRM 51-24-01. INSTALLATION COVERED ON W/C 600-19. 2 H 7 2 4T RT A53EU 2007121200289 20071212 00289 NM 2007 12 12 KCSA07088 1 20071115 A 3310 LIGHT BOEING 747 747249F 1384849 NM COCKPIT NOT SEATED A KCSA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 706CK 21827 DURING CRUISE STRONG ACRID SMELL IN COCKPIT TURNED OFF PILOT FLUORESCENT & SMELL WENT AWAY. FOUND ONE OF THE CAPTAIN`S FLUORESCENT LIGHT BULBS NOT COMPLETELY SEATED IN LIGHT SOCKET. REMOVED AND REPLACED CAPTAIN'S FLUORESCENT LIGHT BULBS I AW B747 MM CHAPT 33-11-11. OPS CHECKED SYSTEM FOR 7 HRS. NO DEFECTS OR ABNORMAL ODORS NOTED. SYSTEM OPS CHECKS GOOD I AW B747 MM CHAPT 33-11-00. 2 L 7 4 4F RT A20WE 2007121200290 20071212 00290 EU 2007 12 12 TRAX200701830 1 20071129 A 5510 BRACKET AEROSP ATR72 ATR72212 8680945 EU HORIZONTAL STAB CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 CORROSION FOUND ON LT MID BRACKET JUNCTION BTW HORIZONTAL AND VERT STAB, RESOLVED ON W/O: 75891 TASKCARD: N/R-00514. ON LT MID BRACKET T-JUNCTION BTW HORIZONTAL AND VERTICAL STAB CORROSION IS REMOVED IAW SRM 51-21-42 MATERIAL THICKNESS: 0. 250 MATERIAL REMOVED: 0.003 WITHIN LIMITS AS PER SRM: 51-10-10. 2 H 7 2 4T RT A53EU 2007121200293 20071212 00293 WP 2007 12 12 DHL2007801532 1 20071109 A 5542 5654883 SKIN DOUG DC8 DC873F 302199F WP RUDDER DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 RUDDER TIP SKIN BROKEN AT STA ZR 335.250 (DAMAGE CAUSED BY SEMAN). REMOVED BROKEN TIP IAW SRM 51-1-21. CLEANED, TREATE D AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TIP IAW SRM 51-1-21A. REFER TO JC EC-00592-001 (WO 2624) FOR FABRICAT ION AND NR 101137 FOR RUDDER BALANCING. 2 L 7 4 4F RT 4A25 2007121200294 20071212 00294 WP 2007 12 12 DHL2007801534 1 20071112 A 5330 STRUCTURE DOUG DC8 DC873F 302199F WP BS 280 S29R DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 INSPECT REPAIR AT FUSELAGE STA 280 LONGERON 29R PER INSPECTION REQUIREMENTS OF DC8 SRM 53-2-1 CLASS II TYPE REPAIR. REP AIR ACCOMPLISHED AUG 94. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 11-12-07, ENGINEERING VARIATION AUTHORIZATI ON NR D853-00023 REV IR DATED 11-05-07. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR FILLER AND REPAIR DOUBLER IAW DWG NR ESD85300023-001-D REV IR. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. NO CRACK NOR CORROSION FOUND AT CUT OUT AREA AND REPAIR PARTS. ENCLOSED SMN FORM 242- 4. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW ASTAR DWG NR ESD85300 2 L 7 4 4F RT 4A25 2007121200298 20071212 00298 WP 2007 12 12 DHL2007801538 1 20071114 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 LT WING MAIN TANK NR 1 LWR SIDE CRACKED 1" STA XRS 84.000 S-59. PERFORMED MAJOR REPAIR IAW MSG NR 1-654248500-2 DATED 1 0-19-07, SRM 57-2-2 FIG 3D SHEET 1, 2, 3, TR NR 57-86 DATED 05-15-01. REMOVED EXISTING CLIPS AND CUT OUT DAMAGED STRING ER SEGMENT IAW MSG NR 1-654248500-2, SRM 57-2-2 FIG 3D SHEET 1, 2, 3, TR NR 57-86. FABRICATED NEW STRINGER SEGMENT IAW BOEING MSG 1-654248500-2, SRM 57-4-3 FIG. 7 ITEM "C" SRM 51-2-0 FIG 50 SHEET 55 SPLICE FITTINGS IAW SRM 57-2-2 FIG 3D SH EET 1, 2, 3, CLIPS IAW MSG NR 1-662905218-2 DATED 10-26-07, DOUGLAS DWG 3642239 AND SPACER5S IAW SRM 57-2-2 FIG 3F SHEET 4. HEAT TREATED SPACER IAW SRM 51-1-1 PG 1-13-17, NDT INSPECTED NEW CLIPS IAW NDT SPM PART 08-00-02 TO 07. NO CRACK/C 2 L 7 4 4F RT 4A25 2007121200299 20071212 00299 WP 2007 12 12 DHL2007801515 1 20071106 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 490 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 INSPECT REPAIR AT FUSELAGE STA 490 L-23R PER INSPECTION REQUIREMENTS OF DC8 SRM 53-2-1 CLASS II TYPE REPAIR. REPAIR ACC OMPLISHED AT AIR CANADA AUG 94. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1, 2. REMOVED EXISTING REPAIR DOUB LER IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER INTERNAL FINGER DOUBLER AND FILLER IAW SRM 5 3-2-1 FIG 7 SHEET 1, 2, SRM 53-4-1 FIG 5C ITEM D, SRM 51-9-0 FIG. 68A. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART S IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 53-2-1 FIG 7 SHEET 1, 2, SRM 51-1-11, SRM 51-1-21, SRM 51-1-26, SRM 5 1-1-20D, SRM 51-3-1. THIS IS A CLASS I TYPE REPAIR (INITIAL INSP AT 4000, REPETITIVE AT 4000, REPLACEMENT N/A) IAW SRM 2 L 7 4 4F RT 4A25 2007121200300 20071212 00300 WP 2007 12 12 DHL2007801523 1 20071109 A 5542 SKIN DOUG DC8 DC873F 302199F WP RUDDER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 LT RUDDER SKIN CRACKED 5" AT STA ZR 335.000 MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1 PG 2. REMOVED DA MAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21, SRM 51-1-21A. FABRICATED PLATING AND BONDED DOUBLER BOTH FROM AL 2024T3 0.016" IAW SRM 55-6-1 FIG 1, PG 2 ITEM "A". BONDED BOTH PARTS IAW SRM 51-1-9, SRM 51-1-9A. CLEANED, TREATED AND PRIMED AREA AND PANEL PLATING IAW SRM 51-1-8B. INSTALLED NEW PANEL PLATING IAW SRM 51-1-21, SRM 51-1-21A. PERFORMED W EIGHT AND BALANCE IAW SRM 51-4-6 PG 1-6. FOUND WITHIN TOLERANCE 2563,8 INCH-LBS. 2 L 7 4 4F RT 4A25 2007121200301 20071212 00301 NE 2007 12 12 ZZDA2007302 2 20071126 A 7200 BR700715A130 ENGINE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE NR 1 MALFUNCTIONED A ZZDA E ENGINE SHUTDOWN O OTHER CL CLIMB 1 SO 37 969AT 55030 DURING CLIMB IN THE MID TO HIGH TEENS, OBSERVED LOUD BANG FROM THE LEFT ENGINE. ENGINE ROLLED BACK AND TGT REMAINED STE ADY BUT ROSE TO 974 DURING CALLING CHECK LIST. EMERGENCY RETURN TO PBI, LANDING NORMAL. NR 1 (LEFT) ENG HAS BEEN REMOV ED AND REPLACED IAW TC 603 REF SP 8140.2, ALL LEAK OPS AND RTS PASS (NORMAL). 2 L 7 2 4F 4 F TR A6WE E00061EN 2007121200308 20071212 00308 WP 2007 12 12 DHL2007801524 1 20071107 A 5751 5646601501 SUPPORT DOUG DC8 DC873F 302199F WP AILERON HINGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 NR 7 LT AILERON HINGE SUPPORT CRACKED. REMOVED AND REPLACED NR 7 LT AIL HINGE SUPPORT IAW MM 20-16-0 PG 201-207, OHM 27 -2-3A. REFER TO NR 130478 FOR OPS CHECK AND NR 130141 FOR LT OUTBD AIL REMOVAL/REINSTALLATION. 2 L 7 4 4F RT 4A25 2007121200309 20071212 00309 NM 2007 12 12 SWAA075898 1 20071128 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 436WN 32456 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007121200311 20071212 00311 NM 2007 12 12 SWAA075901 1 20071128 A 5311 65C34355 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121200313 20071212 00313 WP 2007 12 12 DHL2007801529 1 20071108 A 5240 9755586 FITTING DOUG DC8 DC873F 302199F WP SERVICE DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 MAIN CARGO COMPT SERVICE DOOR JAMB FITTING CRACKED 1" AT STA 1118.528 L11R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-0, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007121200316 20071212 00316 WP 2007 12 12 DHL2007801528 1 20071111 A 5754 STRUCTURE DOUG DC8 DC873F 302199F WP LT WING LE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 LT INNER WING OUTBD EXTENDED LEADING EDGE SLOT LWR PLATING ELONGATED HOLES AT STA XILD 42.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 11-12-07, ENGINEERING VARIATION AUTHORIZATION NR D857-00020 REV IR DATED 10-20-0 7. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER AND REPAIR FILLER IAW ASTAR DWG ES-D85700020-001-D REV IR. NDT INSPECTED CUT OUT AREA AND REPAIR PARTS IAW DC8 NDT SPM PART 08-00-02 TO 07. NEITHER C RACK OR CORROSION FOUND. ENCLOSED SMN FORM 242-4. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. IN STALLED REPAIR PARTS IAW ASTAR DWG NR ES-D85700020-001-D, SRM 51-1-21, SRM 51-3-0, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007121200319 20071212 00319 WP 2007 12 12 DHL2007801526 1 20071114 A 5730 5611016502 SKIN DOUG DC8 DC873F 302199F WP BS 409-456 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 RT WING LWR T/E PANEL INTERNAL/EXTERNAL SKIN DELAMINATED (STA XF 409.000 - XRS 456.000). REMOVED AND REPLACED RT WING T /E LWR PANEL (STA XF 409.000 - XRS 456.000) IAW SRM 51-3-0, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007121200320 20071212 00320 WP 2007 12 12 ABXA070380 1 20071106 A 5230 99234847 PAN DOUG DC9 DC941 302207N WP FWD CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 FORWARD LOWER CARGO DOOR CRACKED IN RADIUS (LOWER FORWARD AT LOCK MECHANISM ON INNER PAN). REPAIRED FORWARD LOWER CARGO DOOR IAW DC9 SRM 52-05. 2 L 7 2 4F A6WE 2007121200323 20071212 00323 WP 2007 12 12 IXXA070057O 1 20071206 A 3260 STRIKER DOUG DC8 DC871F 302199D WP MLG DOOR OUT OF ADJUST A IXXA O OTHER N FALSE WARNING CL CLIMB 1 SW 11 829BX 92575 2903 45994 DURING CLIMB-OUT FROM KPHL TO KTOL, AFTER GEAR RETRACTION THE DOOR LIGHT REMAIN ON. THE CREW CYCLED THE GEAR AND THE LI GHT REMAINED ON. THE CREW CONTINUED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CLEANED UPLATCH SWI TCHES AND ADJUSTED DOOR STRIKER. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE IAW DC8 MAINTE NANCE MANUAL 32-12-1. 2 L 7 4 4F RT 4A25 2007121200324 20071212 00324 WP 2007 12 12 ABXA070383 1 20071115 A 5315 992348421 FLOORBEAM DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 FLOORBEAM STA 180, LEFT BUTT LINE 22 WAS CRACKED ON OUTBOARD SIDE OF INTERCOSTAL. REPAIRED FLOOR IAW REA D953-56651. 2 L 7 2 4F A6WE 2007121200326 20071212 00326 WP 2007 12 12 ABXA070382 1 20071106 A 5320 59101419 INTERCOSTAL DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 INTERCOSTAL CRACKED FS 180 AT LEFT BUTT LINE 22. REPAIRED INTERCOSTAL IAW DC9 SRM 53-01 FIGURE 2. 2 L 7 2 4F A6WE 2007121200328 20071212 00328 WP 2007 12 12 ABXA070384 1 20071115 A 5315 992348421 FLOORBEAM DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 FLOORBEAM ANGLE AT STA 180 CRACKED AT BUTT LINE 0, AFT SIDE OF FLOORBEAM, LEFT SIDE OF INTERCOSTAL. REMOVED AND REPLACE D ANGLE IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2007121200329 20071212 00329 NM 2007 12 12 200711291 1 20071126 A 3350 340022 BATTERY PACK EMB ERJ170 ERJ170100SE 3260406 NM CABIN DISCHARGED A UHLA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 11 863RW 17000100 FLIGHT 6492 MDW CREW REPORTS ON PREFLIGHT FOUND AN EMERGENCY CEILING LIGHT ABOVE ROW 5 INOP. MAINTENANCE REMOVED AND RE PLACED LT FORWARD EMERGENCY LIGHT BATTERY PACK. 2 L 7 2 4F RT A56NM 2007121200330 20071212 00330 NM 2007 12 12 200711292 1 20071127 A 2782 1702885C ACTUATOR EMB ERJ170 ERJ170100SE 3260406 NM L/E SLAT MALFUNCTIONED A UHLA O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 869RW 17000133 FLIGHT 6498 ATL TO IND ON APPROACH CREW RECEIVED THE EICAS CAUTION MESSAGE FOR SLAT FAILURE. FLAPS AND SLATS WERE AT ZE RO LANDED THE AIRCRAFT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RT NR 4 SLAT ACTUATOR. 2 L 7 2 4F RT A56NM 2007121200336 20071212 00336 NM 2007 12 12 07FDEA05002 1 20071206 A 5754 SKIN DOUG MD11 MD11F 3023600 NM RT WING LE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 524FE 48480 RIGHT WING, LEADING EDGE UPPER SURFACE FOUND DEEP GOUGE AT XIS 247. REPAIRED AS PER SRM 57-10-00 FIGURE 24 VOLUME I. R EPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007121200337 20071212 00337 NM 2007 12 12 CALA0700716 1 20071129 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16618 27331 CABIN STA 787 BETWEEN LT S8 AND S9 FRAME CRACKED AT BRACKET ATTACHED TO PSU MOUNT RAIL MARKED. INSTALLED DOUBLERS PER E CRA 5310-04677. 2 L 7 2 4F RT A16WE 2007121200346 20071212 00346 EA 2007 12 12 CHQA200700085 1 20071203 A 2750 855D1009 SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BRAKE POSITION MALFUNCTIONED A CHQA L ABORTED APPROACH O OTHER DE DESCENT 1 GL 11 645BR 14278 7383 GEE872681 SDF TO IAH - DURING DESCENT TO IAH. THE CREW RECEIVED A FLAP FAIL MESSAGE. THE APPROACH WAS ABORTED AND THE CREW RAN TH E QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE FECU AND FOUND CODES FOR THE LEFT BRAKE POSITION SENSIN G UNIT. THE BRAKE POSITION SENSING UNIT WAS REPLACED, AND THE FLAP SYSTEM, OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2007121200348 20071212 00348 SO 2007 12 12 CHQA200700084 1 20071203 A 3260 8005701 PROXIMITY SWITCH EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL LT MLG FAULTED A CHQA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 11 377SK 145579 CAE312152 BWI TO STL - ON APPROACH TO STL, WHEN THE GEAR WAS SELECTED DOWN, THE CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL EICAS MESSAGE. THE AIRCRAFT DID A GO AROUND IN ORDER TO RUN THE QRH AND AS A PRECAUTION THE LANDING GEAR WAS LEFT DOWN. ON THE SECOND APPROACH THERE WERE NO FURTHER INDICATIONS OF GEAR MALFUNCTIONS, AND THE AIRCRAFT LANDED WITHOUT INCIDENT. M AINTENANCE INTERROGATED THE CMC FOR FAULT MESSAGES AND FOUND A PROXIMITY SWITCH FAULT, AND WAS TROUBLESHOT DOWN TO THE L EFT MAIN LANDING GEAR PROXIMITY SWITCH. BOTH OF THE LEFT MAIN LANDING GEAR PROXIMITY SWITCHES WERE CHANGED, AND THE WEI GHT ON WHEELS SYSTEM OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007121200351 20071212 00351 NM 2007 12 12 AALA20072316 1 20071127 A 3350 SOCKET BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 198AA 32392 ORD - EMERGENCY LIGHTS AT SEAT ROW 16D INOPERATIVE. REPLACED SOCKET AT SEAT ROW 16 FOR EMERGENCY LIGHTS AT SEAT ROWS 16 D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007121200352 20071212 00352 NM 2007 12 12 AALA20072333 1 20071130 A 2560 P4010021000 BATTERY BOEING 777 777223 1385213 NM FLASHLIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 795AN 30257 LHR - EMERGENCY FLASHLIGHT AT RIGHT NUMBER THREE DOOR INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT RIGHT N UMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121200353 20071212 00353 NM 2007 12 12 AALA20072334 1 20071130 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 795AN 30257 LHR - EMERGENCY LIGHT AT SEAT 2D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 2D. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121200354 20071212 00354 NM 2007 12 12 AALA20072320 1 20071128 A 3350 P4010051112 MODULE BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 175AN 32394 LGA - EMERGENCY LIGHTS AT SEAT ROW 16 INOPERATIVE. REPLACED CONTROL MODULE FOR EMERGENCY LIGHTS AT SEAT ROW 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007121200356 20071212 00356 NM 2007 12 12 AALA20072322 1 20071128 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 952AA 30088 MIA - EMERGENCY LIGHT AT LEFT AFT EXIT DOOR WINDOW INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LEFT AFT EXIT DOOR WINDOW. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007121200359 20071212 00359 WP 2007 12 12 AALA20072337 1 20071130 A 1100 PLACARD DOUG DC9 DC982 3022082 WP EMERGENCY EXIT TORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7544A 53026 LGA - EMERGENCY EXIT PLACARD AT AFT LEFT TAIL CONE TORN. REPLACED EMERGENCY EXIT PLACARD AT AFT LEFT TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121200362 20071212 00362 NM 2007 12 12 AALA20072332 1 20071130 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 779AN 29955 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121200363 20071212 00363 NM 2007 12 12 AALA20072342 1 20071201 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 789AN 30252 JFK - EMERGENCY LIGHT AT SEAT 21G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121200364 20071212 00364 NM 2007 12 12 AALA20072343 1 20071201 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 789AN 30252 JFK - SEAT MOUNTED EMERGENCY LIGHTS AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK M33094 FOR SEAT MOUNTED EMERGENCY LIGHTS AT FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121200367 20071212 00367 2007 12 12 AALA20072340 2 20071130 A 7261 FILTER DOUG DC9 DC983 3022083 WP NR 2 ENGINE OIL DIRTY A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 9618A 53565 DFW INFLIGHT T1874/30NOV - NUMBER TWO ENGINE OIL FILTER CLOG LIGHT ILLUMINATED IN FLIGHT. CAPTAIN SHUT DOWN NUMBER TWO ENGINE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME 48 MINUTES. FOUND NUMBER TWO ENGINE OIL FILT ER DIRTY WITH CARBON. REPLACED OIL FILTER AND SERVICED NUMBER TWO ENGINE OIL TO FULL. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F RT A6WE 2007121200371 20071212 00371 NM 2007 12 12 AALA20072345 1 20071201 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 789AN 30252 JFK - EMERGENCY LIGHT AT SEAT 25C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121200372 20071212 00372 NM 2007 12 12 AALA20072346 1 20071201 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 789AN 30252 JFK - EMERGENCY LIGHT AT SEAT 26C MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121200373 20071212 00373 NM 2007 12 12 AALA20072353 1 20071201 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 960AN 29542 DFW - EMERGENCY EXIT IDENTIFIER LIGHT AT SEAT 14F INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT IDENTIFIER LIGHT AT SEA T 14F. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007121200375 20071212 00375 NM 2007 12 12 AALA20072341 1 20071201 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 789AN 30252 JFK - EMERGENCY LIGHT AT SEAT 38G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 38G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121200378 20071212 00378 NM 2007 12 12 CALA0700719 1 20071130 A 5315 BAC1490100246 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 CABIN FWD ENTRY FLOORBEAM STA 344 TOP AND AROUND CORRODED FROM RBL 10 LBL 10. INSTALLED SECTION "T" CHORD & SPLICE PER SRM 53-10-51. 2 L 7 2 4F RT A16WE 2007121200390 20071212 00390 NM 2007 12 12 AALA20072312 1 20071127 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 638AA 24596 DFW - EMERGENCY LIGHT AT SEAT 38D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 38D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007121200391 20071212 00391 NM 2007 12 12 ASAA0752289 1 20071127 A 7722 TC29603 PROBE BOEING 737 737890 1384527 NM NR 1 ENGINE DIRTY A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 579AS 35187 NR 1 ENGINE TREND DATA SHOWS AND INCREASE IN CRUISE DELTA EGT ALONG WITH A DECREASE IN TAKEOFF EGT HOT DAY MARGIN. ACCO MPLISHED CLEANING PER MM 77-21-00 PGS 201-202. ALL CONTACTS LOOK GOOD. NOTE: S1 &S2 VALUES ARE NEAR 35 DEGREE DIFF LIM IT. 2 L 7 2 4F RT A16WE 2007121200394 20071212 00394 SO 2007 12 12 C2XA07RI100 1 20071125 A 3234 7455503 CONTROL LEVER EMB 145 EMB145LR 3260212 SO COCKPIT DEFECTIVE A C2XA K NONE O OTHER CL CLIMB 1 SW 27 12567 13464 9429 145623 FLT 2490 - EWR - CREW REPORTED THAT LANDING GEAR WILL NOT RETRACT AFTER TAKEOFF. CREW PROCEEDED WITH AIR RETURN AND LAN DED UNEVENTFULLY. EWR MX REMOVED AND REPLACED LANDING GEAR CONTROL LEVER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007121200395 20071212 00395 EU 2007 12 12 YENA2007107 1 20071120 A 2752 791A000006 ACTUATOR AIRBUS 320 A320232 3930326 EU T/E FLAP CONTAMINATED A YENA K NONE F FLT CONT AFFECTED AP APPROACH 1 EA 15 503JB 16217 1123 FLT 352, BUR-JFK. DURING CONFIGURATION FROM FLAPS 1 TO 2 F/CTL FLAPS LOCKED ECAM. WING TIP BRAKE ON. REMOVED AND REPL ACED NR 1 & 2 RT WING FLAP ACTUATORS, RIG/ADJUST OF RT FLAP OPERATIONAL TEST GOOD IAW 27-54-49 AND 27-54-00-05. 2 L 7 2 4F RT A28NM 2007121100135 20071211 00135 EA 2007 12 11 A6WA200740614 1 20071110 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA DIRTY A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 31 437AW 7744 MEDIUM TO STRONG ODOR OF FUEL NOTICED FLIGHT DECK AND FORWARD CABIN AREA. REMOVED AND REPLACED COALESCER BAGS IAW CRJ A MM 21-51-13, RAN PACKS USING BOTH APU AND ENGINE AIR. NO DEFECTS NOTED. VISUAL INSPECTION FOR LEAKS, NO LEAKS NOTED. (M) 2 L 7 2 4F RT A21EA 2007121100136 20071211 00136 2007 12 11 A6WA200740622 4 20071115 A 3140 6229820009 DCU CNDAIR CL600 CL6002B19 1900309 EA NR 2 MALFUNCTIONED A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 433AW 7289 RIGHT ENGINE N2 FLUCTUATION INFLIGHT. COMPLIED WITH QRH. N2 SPIKE OVER 104 PERCENT AT LEAST TWO TIMES WITH POWER REDUC ED. OAT -6. NO VIBE GAUGE INDICATION. DIVERTED TO ORF. FOUND DCU NR 2 CAUSING N2 FLUCTUATING INDICATION. REMOVED AN D REPLACED DCU NR 2 IAW AMM 31-41-04. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007121100139 20071211 00139 EA 2007 12 11 A6WA200740626 1 20071114 A 5230 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA ROLLER TRACK CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 470ZW 7927 FOUND CRACK ON SUPPORT BRACKET AT LOWER ROLLER CARGO DOOR TRACK IS 574 WL 82. REMOVED AT LOWER ROLLER TRACK CARGO DOOR IAW CRJ 200 SRM 51-42-06. BRACKET FABRICATED IAW CRJ 200 SRM 51-24-21, BRACKET INSTALLED IAW SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007121100153 20071211 00153 SO 2007 12 11 SIMA200733705 1 20071130 A 2730 3622001015 ACTUATOR EMB 145 EMB145LR 3260212 SO HORIZONTAL STAB FAILED A SIMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 908AE 14500897 MAIN PITCH TRIM FAILED. CAPT ELECTED TO RETURN TO THE FIELD IAW AMM 27-40-02 REF NRWC 2004864. REMOVED AND REPLACED HO RIZONTAL STABILIZER ACTUATOR IAW AMM 27-40-03-000-801. OPS CHECK GOOD AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007121100157 20071211 00157 EU 2007 12 11 MALA070191 1 20071204 A 5330 SKIN PANEL SAAB SF340 340B 7860101 EU BS 300-319 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 412XJ 340B412 DENTS LOCATED UNDER ICE SHIELD NR 7 AT FS 300.5 - FS 319.5, SL1615-SL1618. INSTALLED DOUBLER TRIPLER REPAIR IAW EO NR S 53009. 2 L 7 2 4T RT A52EU 2007121100174 20071211 00174 EA 2007 12 11 SWIA200718909 1 20071119 A 2421 820465 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA ADG MALFUNCTIONED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 948SW 7789 FLT 6388 - AFTER STARTING ENGINE NR 2 AND TURNING ON GENERATOR 2, THE ADG DEPLOYED. REPLACED ADG AUTO DEPLOY PANEL IAW RJ 200 MM 24-23-15. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007121100175 20071211 00175 EA 2007 12 11 SWIA200718910 1 20071128 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 447SW 7677 FLT 3872 - SECOND TO LAST EMERGENCY LIGHT POD ON CEILING OF CABIN INOP. REPLACED LAMP IN CEILING EMERGENCY POD LIGHT AS NEEDED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007121100178 20071211 00178 2007 12 11 SWIA200718914 4 20071126 A 2360 BONDING STRAP EMB 120 EMB120ER 3260203 SO LT ENGINE BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 227SW 120304 FLT NR 565 - LEFT CONDITION LEVER IS BECOMING DIFFICULT TO MOVE. REPLACED BONDING STRAP ON LT ENGINE CONDITION LEVER BE LLCRANK. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007121100180 20071211 00180 EA 2007 12 11 SWIA200718916 1 20071129 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 614SK 10051 FLT 4065 - SECOND EMERGENCY LIGHT FROM THE BACK IS BROKEN. RELAMPED LIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007121100197 20071211 00197 NM 2007 12 11 ASAA0772336 1 20071113 A 5320 ANGLE BOEING 737 737790 13844CN NM BS 500A-500D CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 FWD CARGO PIT ZEE ANGLE FOUND CORRODED AT BS 500A TO 500D RBL21 FWD CARGO PIT ZEE ANGLE BS 500D RBL21. REPAIRED IAW B73 7 700 SRM 53 30 53 AND SRM 53 00 53 REPAIR 5. 2 L 7 2 4F RT A16WE 2007121100198 20071211 00198 NM 2007 12 11 ASAA0772339 1 20071113 A 5320 FLOOR SUPPORT BOEING 737 737790 13844CN NM BS 500-500A CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 617AS 30542 CORROSION FOUND ON TOP AND BOTTOM OF FWD CARGO PIT FLOOR SUPPORT INTERCOSTAL AT BS 500 TO BS 500A RBL 21.00. CORROSION BLENDED OUT AND FOUND TO BE BEYOND ALLOWABLE LIMITS IAW B737 700 SRM 53 00 53. MADE AND INSTALLED REPAIR PART IAW B737 200 SRM 51 40 05 AND 51 40 02. 2 L 7 2 4F RT A16WE 2007121200011 20071212 00011 EU 2007 12 12 07FDEA04970 1 20071201 A 5320 A5378193620300 ADAPTER AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 MAIN DECK CARGO TIE-DOWN ADAPTER CRACKED AT FR54.3, (STA X3090) RBL -Y685. REMOVED AND REPLACED ADAPTER REF: A310-200 SRM 51-40-21 PAR 6 AND PAR 7. 2 L 7 2 4F RT A35EU 2007121200018 20071212 00018 EA 2007 12 12 COMA0760659 1 20071120 A 3230 46193 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 798CA 17590 7314 FLIGHT 5604 - DURING CVG APPROACH RECEIVED A LANDING GEAR DISAGREE CAUTION. CREW DECLARED AN EMERGENCY AND ABORTED APPR OACH, THEN LANDED WITHOUT INCIDENT ON SECOND ATTEMPT. REPLACED THE MLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2007121200027 20071212 00027 WP 2007 12 12 07FDEA04977 1 20071203 A 5310 AFA00395 BEAM DOUG DC10 DC1010F 3022111 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 FWD CARGO COMPT BILGE AREA FOUND CRACK ON BEAM. REPAIRED BEAM IAW SRM 53-60-01 VOL I FIG 3. 2 L 7 3 4F A22WE 2007121200028 20071212 00028 EA 2007 12 12 COMA0760667 1 20071123 A 2120 DUCT CNDAIR CL600 CL6002B19 1900309 EA HEAT EXCHANGER DISCONNECTED A COMA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 01 966CA 7132 FLIGHT 5473 - CABIN ALT CAUTION MESSAGE FOLLOWED BY CABIN ALT WARNING MESSAGE AFTER LEVELING OFF AT FS 240. QRH FOLLOWE D FOR BOTH MSGS, CONTINUED DESCENT INTO MCO AND LANDED SAFELY. FOUND RIGHT DUAL HEAT EXCHANGER PRIMARY INLET DUCT DISCO NNECTED. RECONNECTED DUCT WITH SERVICEABLE CLAMP. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007121200031 20071212 00031 EA 2007 12 12 COMA0760669 1 20071124 A 2750 860D10018ABCD COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS BAY FAULTY A COMA K NONE J WARNING INDICATION DE DESCENT 1 SO 01 916CA 12046 7014 FLIGHT 5043 - FLAPS FAIL CAUTION MESSAGE INFLIGHT DURING DESCENT/APPROACH PHASE. AIRCRAFT LANDED SAFELY. REMOVED AND R EPLACED FECU. 2 L 7 2 4F RT A21EA 2007121200042 20071212 00042 2007 12 12 2007UALA04798 4 20071125 A 2565 LANYARD AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR OUT OF POSITION A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 421UA 500 CREW REPORT: DOOR 2L HAS GREEN CHORD HANGING OUT BELOW SLIDE PACK. RESECURED MOORING LINE BACK INTO SLIDE PACK. NO R EPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121200055 20071212 00055 NM 2007 12 12 2007UALA04806 1 20071124 A 3350 78941 LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 769UA 26921 EEL LIGHTING AT SEAT 1E BROKEN. INSTALLED LAMP 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121200061 20071212 00061 NM 2007 12 12 2007UALA04808 1 20071125 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN MISSING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 228UA 30556 EMERGENCY ESCAPE PATH LIGHT (AFT) ON SEAT 2E IS MISSING. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121200063 20071212 00063 WP 2007 12 12 07FDEA04989 1 20071203 A 5347 S4929150 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 MAIN CABIN APPROX AT STA 1256 AND STA 1264 SEAT TRACK SCALLOPS (3EA) ELONGATED (N7513) AT LBL 48 EVALUATED SEAT TRACK FO UND TO BE OUT OF LIMITS IAW DC/MD10 SRM 53-70-00 VOL I PG 21 AND 22. MAT ID S4929150 PO NR 595343.1 IAW DC/MD10 SRM 53- 42-01 FIG 5 VOL III. FABRICATED SEAT TRACK IAW DC/MD10 SRM 53-70-00 PG 4 VOL I FIG 1. ALODINED AND PRIMED IN REF TO DC /MD10 SRM 51-21-01 VOL II PG 5. 2 L 7 3 4F RT A22WE 2007121200073 20071212 00073 NM 2007 12 12 2007UALA04813 1 20071125 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN OUT OF POSITION A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 673UA 29241 FLIGHT REPORTS STRANGE WIRE STICKING OUT OF SEAT 40B. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121200075 20071212 00075 EU 2007 12 12 USAA920071249 1 20071126 A 5347 SEAT TRACK AIRBUS 330 A330323 3930335 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 278AY 388 BFM - MAJOR REPAIR - C2 CHECK - NR 6048975, CORROSION ON SEAT TRACK, BS 4842/FR 58 - BS 5372/FR 68, -Y450. REPLACED SEA T TRACK, BS 4842/FR 58 - BS 5372/FR 68, -Y450 IAW A330 SRM 53-41-15. 2 L 7 2 4F RT A46NM 2007121200084 20071212 00084 NM 2007 12 12 2007UALA04816 1 20071123 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 675UA 29243 SEAT 14H SIDE SEAT EEL LIGHT PULLED OUT AND ON SEAT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121200089 20071212 00089 NM 2007 12 12 2007UALA04821 1 20071126 A 3397 WIRE BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHT INOPERATIVE SEAT 3J FWD SECTION. REPAIRED BROKEN WIRE ASSEMBLY 2 L 7 4 4F 4 F RT A20WE E24NE 2007121200108 20071212 00108 SO 2007 12 12 C2XA07IA235 1 20071125 A 2131 92185A010200 CONTROLLER EMB 145 EMB145XR 3260214 SO CABIN PRESSURE MALFUNCTIONED A C2XA O OTHER O OTHER UK UNKNOWN 1 SW 27 16112 13329 13329 145660 IAH - FLIGHT 2953, THE CREW REPORTED THAT CABIN PRESSURE WAS LOST IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDEN T. MAINTENANCE REMOVED AND REPLACED THE PRESSURIZATION SYSTEM DIGITAL CONTROLLER, OPERATIONALLY CHECKED WITH NO DEFECTS , AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007121200110 20071212 00110 NM 2007 12 12 QXEA200701775 1 20071202 A 3246 BEARING BOMBDR DHC8 DHC8402 1390042 NM MLG N21 WHEEL FAILED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 426QX 9903 9 4154 HLN- FLIGHT 2321, RECEIVED A ANTI-SKID MESSAGE ON THE TAKEOFF. ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENAN CE PLACED THE SYSTEM ON MEL 32-40-2. AIRCRAFT RETURNED TO SERVICE. 12/3 REPLACED THE WHEEL SPEED TRANSDUCER (NR 1), LT MLG AXLE, AND NR 1 WHEEL ASSEMBLY (BEARING FAILURE). MEL CLEARED AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007121200112 20071212 00112 NM 2007 12 12 QXEA200701778 1 20071202 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM NR 2 BLEED ILLUMINATED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 405QX 4047 LAX - FLIGHT 2421, IN CRUISE FLIGHT RECEIVED A NR 2 BLEED HOT CAUTION LIGHT. COMPLIED WITH THE CHECKLIST AND TURNED THE BLEED OFF, AND THE CAUTION LIGHT WENT OUT. MAINTENANCE PERFORMED A OPERATIONAL TEST AND COULD NOT DUPLICATE THE PROBLE M. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007121200113 20071212 00113 NM 2007 12 12 QXEA200701779 1 20071128 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM NR 2 BLEED ILLUMINATED A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 405QX 4047 RNO - FLIGHT 2259, ON APPROACH RECEIVED A NR 2 BLEED HOT CAUTION LIGHT. AFTER COMPLETING THE CHECKLIST, THE LIGHT WENT OUT. MAINTENANCE CLEANED THE CONNECTOR TO THE NR 2 OVERTEMP SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SER VICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007121200114 20071212 00114 EA 2007 12 12 TRAX200701755 1 20071119 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 AAR - O/B 280 CLIP AT LBL 9 ON FLOORBEAM HAS A SUSPECTED CRACK. DUPLICATE, REFER TO W/O: 50229 W/C 1000-0041 FOR CORREC TIVE ACTION. SUPPLEMENTAL - SDR CLOSED 11/27/07. 2 L 7 2 4F RT A21EA 2007121200119 20071212 00119 EU 2007 12 12 MALA070194 1 20071205 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 655 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 420XJ 340B420 FUSELAGE DENTS BELOW CARGO DOOR STA 655 NOTED DURING W/A. COMPLETED PERMANENT REPAIR TO AREA BELOW CARGO DOOR AT FS 655 IAW SDS 013700. REFERENCE MM04 318251 AND CONT CARD 092042 AND 092043 FOR DETAILS OF WORK PERFORMED. 2 L 7 2 4T RT A52EU 2007121200130 20071212 00130 NM 2007 12 12 UPS07M51245 1 20071016 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C RT HORIZ STAB NR 28 BARREL NUT HOLE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED PER SRM 51-2 1-01 V2.R.35.10X MAGNIFICATION DETAILED VISUAL INSP C/OUT FOUND NO CORROSION EVIDENT. BARREL NUT BORE BLEND OUT VOID AN D BOTTOM PERIPHERY RADIUS SMOOTHEN AND PROTECTED PER SRM 51-21-01V.2R.35. REP SLEEVE BUSHING FAB AND PROTECTED PER EO M D11-5510-19 409-L FIG 5. REP C/OUT AT RT NR 28 BORE IS ACCEPTABLE PER EN 1698-07. 2 L 7 3 4F RT A22WE 2007121200135 20071212 00135 NM 2007 12 12 UPS07M51249 1 20071010 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C RT HORIZ STAB NR 27 BARREL NUT HOLE FOUND CORRODED. CORROSION REMOVED AT BARREL NUT BORE PER SRM 51-2 1-01V.2R35.10X MAGNIFICATION DETAILED VISUAL INSP C/OUT FOUND NO CORROSION EVIDENT. BARREL NUT BORE BOTTOM AND BLEND OU T PERIPHERY RADIUS SMOOTHEN AND PROTECTED PER SRM 51-21 -01V.2R.35. REP SLEEVE BUSHING FAB AND PROTECTED PER EO MD11-55 10-19409-L FIG 5. REP C/OUT AT NR 27 RT BORE IS ACCEPTABLE PER EN1678-07. 2 L 7 3 4F RT A22WE 2007121200141 20071212 00141 NM 2007 12 12 SWAA075853 1 20071126 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121200142 20071212 00142 EA 2007 12 12 TRAX200701843 1 20071201 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 820AS 7188 FOUND FWD CEILING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2007121200143 20071212 00143 NM 2007 12 12 SWAA075845 1 20071126 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121200145 20071212 00145 NM 2007 12 12 SWAA075844 1 20071126 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121200155 20071212 00155 NM 2007 12 12 SWAA075856 1 20071126 A 5310 6547956 DOOR FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER ACO. 2 L 7 2 4F RT A16WE 2007121200166 20071212 00166 NM 2007 12 12 ASAA0742352 1 20071130 A 5330 65C329541 SKIN BOEING 737 7374Q8 138447Q NM BS 867-877 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 RIVET HEADS BROKEN OFF AND POSSIBLE CORROSION ON HOLES OF PREVIOUS REPAIR DOUBLER AT STA867 STR 26R. REPAIRED IAW B737 400 SRM 53 00 01 REPAIR 31. 2 L 7 2 4F RT A16WE 2007121200170 20071212 00170 EU 2007 12 12 USAA920071257 1 20071129 A 3350 32145410 PSU AIRBUS 320 A320231 3930325 EU ZONE 200 NO TEST A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 625AW 64 SAL - EEL - C7 CHECK - L FWD DOOR EMERGENCY LIGHT EPSU FAILED DURING OPERATIONAL TEST. REMOVED AND REPLACED L FWD DOOR EMERGENCY LIGHT EPSU AND PERFORMED OPERATIONAL TEST GOOD. 2 L 7 2 4F RT A28NM 2007121200183 20071212 00183 SO 2007 12 12 SIMA200733909 1 20071203 A 3350 20131A BATTERY EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHTS INOPERATIVE A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 708AE 145205 FORWARD SECTION OF EMERGENCY STRIP LIGHTS INOP. REMOVED AND REPLACED NUMBER 1 AND 2 BATTERY’S AIRCRAFT RETURNED TO SER VICE. 2 L 7 2 4F RT T00011AT 2007121200189 20071212 00189 SO 2007 12 12 SIMA200733908 1 20071203 A 2720 15H0048PH PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO RUDDER SYSTEM MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 661JA 145766 AIR TURN BACK FOR RUDDER SYSTEM 2 INOP MESSAGE. AIRCRAFT WAS BEING REPOSITIONED TO XNA. REMOVED AND REPLACED NR 2 RUDD ER PRESSURE SWITCH IAW AMM27-73-04. LEAK AND OPS CHECK GOOD IAW AMM 27-23-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007121200197 20071212 00197 NM 2007 12 12 AALA20072298 1 20071126 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 795AN 30257 JFK - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 25 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD SEAT R OW 25. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121200207 20071212 00207 NM 2007 12 12 HNAA0700273 1 20071119 A 3320 BV033001248 SOCKET DHAV DHC8 DHC8102 2809003 NM CABIN BURNED A HNAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 826EX 30538 30538 389 STRONG ELECTRICAL ODOR IN CABIN WITH SMOKE. INSPECTED CABIN AND FOUND THE OVERHEAD LIGHT AT ROW 8DF LIGHT SOCKET BURNT. PERFORMED HIDDEN DAMAGE INSPECTION NO OTHER DAMAGE NOTED. REPLACED LAMP HOLDER SOCKET. 2 H 7 2 4T RT A13NM 2007121200210 20071212 00210 WP 2007 12 12 UPS07851213 1 20071127 A 3350 5708458503 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:N/A EMERGENCY LIGHTS DO NOT TEST. REPLACED EMERGENCY BATTERY PACK. OPS CHECK GOOD PER MM 33-50-01-2. 2 L 7 4 4F RT 4A25 2007121200215 20071212 00215 EA 2007 12 12 TRAX200701775 1 20071124 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 902EV 7620 L-ANGLE PART NUMBER 601R35050-109 CRACKED. 2 L 7 2 4F RT A21EA 2007121200221 20071212 00221 NM 2007 12 12 SWAA075892 1 20071127 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FIT TING PER MM. 2 L 7 2 4F RT A16WE 2007121200239 20071212 00239 NM 2007 12 12 SWAA075888 1 20071127 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 784SW 29810 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007121200242 20071212 00242 NM 2007 12 12 USAA920071228 1 20071108 A 5532 175N2001 PANEL BOEING 757 7572B7 1384964 NM VERTICAL STAB DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 200UU 27809 MCN - MAJOR REPAIR - C4 CHECK - DELAMINATION ON VERTICAL STABILIZER LEFT HAND SIDE, FSS 131.25. REPAIRED VERTICAL STABI LIZER LEFT HAND SIDE, FSS 131.25 IAW B737 SRM 51-70-10. 2 L 7 2 4F RT A2NM 2007121200243 20071212 00243 2007 12 12 ASAA0752285 4 20071126 A 3460 1714970501 COMPUTER BOEING 737 737890 1384527 NM FLT MANAGEMENT FAULTY A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 587AS 35684 F/O'S "MAP" FLAG NO "VSPDS" "ALT DIS" FLAG. SWITCHED FMC BOTH TO LEFT, 1 MINUTE LATER BACK TO FMC NORMAL. ALL MODES NO RMAL. UPON ARRIVAL @ ACFT BOTH IRS SWITCHED OFF. REALIGNED BOTH IRS'S. ALL DISPLAYS NORMAL. NO HISTORY. ACFT REQUIRES ETOPS VERIFICATION FLIGHT. VERIFICATION FLIGHT SATISFACTORY. 2 L 7 2 4F RT A16WE 2007121200252 20071212 00252 NM 2007 12 12 QXEA200701791 1 20071204 A 5220 SEAL BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY EXIT OBSTRUCTED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 424QX 4006 BOI - FLIGHT 2385 - AFT EMERGENCY DOOR HARD TO OPEN FROM INSIDE THE CABIN. MAINTENANCE CLEANED DEBRIS FROM THE SEAL. O PERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007121200259 20071212 00259 EA 2007 12 12 QXEA200701759 1 20071124 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002C10 1390015 EA FALSE ACTIVATION A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 602QX 10010 DEN - RECEIVED A PITCH FEEL CAUTION AND A SSCU 1 FAULT STATUS MESSAGE. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENT FUL LANDING. MAINTENANCE COMPLIED WITH FIM TASK 27-31-00-810-804-A01 AND 27-61-05-810-825-A01. FAULT DID NOT COME BACK . CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007121200260 20071212 00260 NM 2007 12 12 CALA0700698 1 20071125 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 CABIN FWD ENTRY FLOORBEAM STA 328 AT LBL 10 2 AT HOLES ELONGATED. REMOVED AND REPLACED PER SRM 53-10-51 REPAIR 5. 2 L 7 2 4F RT A16WE 2007121200265 20071212 00265 NM 2007 12 12 CALA0700699 1 20071125 A 5330 2024T3 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 CRACK IN FUSELAGE SKIN 10 INCHES ABOVE LAP JOINT AND 11 INCHES AFT OF AFT UPPER BODY FAIRING RIGHT SIDE AT STATION 727A AND STRINGER S-19R. REPAIRED FUSELAGE SKIN PER SRM 53-00-01. 2 L 7 2 4F RT A16WE 2007121200267 20071212 00267 NM 2007 12 12 CALA0700701 1 20071126 A 5320 6545834523 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 CABIN FWD ENTRY INTERCOSTAL WEB BETWEEN STA 294.5 AND 312 BL 0 TOP ANGLE AFT END CRACKED. REMOVED AND REPLACED PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007121200268 20071212 00268 NM 2007 12 12 F3LA200700361 1 20071204 A 5210 D5211013320000 ROLLER AIRBUS A319 A319111 3930336 NM DOOR HANDLE BROKEN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 933FR 2260 MAINTENANCE REPORTED BROKEN ROLLER BEARING ON L2 SERVICE DOOR OUTER HANDLE/LATCH. REMOVED AND REPLACED CRANK ON THE OUT ER CONTROL HANDLE IAW AMM 52-13-21-400-001. OPS CHECK NORMAL. 2 L 7 2 4F RT A28NM 2007121200269 20071212 00269 NM 2007 12 12 CALA0700702 1 20071127 A 5330 6545775 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 FUSE SKIN CRACK INDICATION RT SIDE 39 INCHES AFT OF AFT BIN DOOR FRAME & 30 INCHES ABOVE LAP SEAM. COMPLETED SKIN REPAI R 31 PER SRM 53-00-01 AND REPAIR DEVIATION PER ECRA 5331-01365. 2 L 7 2 4F RT A16WE 2007121200270 20071212 00270 WP 2007 12 12 IXXA070056O 1 20071205 A 3260 UPLOCK SWITCH DOUG DC8 DC871F 302199D WP ZONE 700 DIRTY A IXXA O OTHER N FALSE WARNING CL CLIMB 1 SW 11 829BX 92574 2902 45994 DURING CLIMB-OUT FROM KTOL TO KPHL, GEAR LANDING DOOR LIGHT REMAINED ON AFTER GEAR WAS RETRACTED, THE CREW CYCLED THE GE AR AND THE LIGHT REMAINED ON. THE CREW CONTINUED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE SYSTEM AND CLEANED GLYCOL FROM UPLATCH SWITCHES. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE IAW DACO MAINTENANCE MANUAL 32-12-1. 2 L 7 4 4F RT 4A25 2007121200286 20071212 00286 EU 2007 12 12 TRAX200701836 1 20071129 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 RT O/B SEAT TRACK FOUND OUT OF LIMIT BTW FR 29-36 ON W/C 100-64, NEEDS SEAT TRACK TO BE FABRICATED, RESOLVED ON W/O: 758 91 TASKCARD: N/R-00653. ON RT O/B SEAT TRACK BTW FR 29-36, FABRICATION IAW SRM 53-63-00 FIG 101. INSTALLATION COVERED ON W/C 100-64. 2 H 7 2 4T RT A53EU 2007121200288 20071212 00288 EA 2007 12 12 TRAX200701850 1 20071201 A 5340 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 RIGHT SIDE INBOARD BATHTUB FITTING CRACKED, RESOLVED ON W/O: 75508 TASKCARD: N/R-00108. REMOVED CRACKED RT INBOARD BATH TUB FITTING. LOCATED SERVICEABLE FITTING P/N 600-3106-19 IAW CRJ SRM 51-40-11. OK TO INSTALL. INSTALLED NEW SERVICEABLE FITTING IAW CRJ SRM 51-42-21. OK TO TOPCOAT FASTENERS. AAR 349. APPLIED TOPCOAT TO FASTENERS PER CRJ 200 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2007121200302 20071212 00302 2007 12 12 SWAA075896 4 20071128 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007121200303 20071212 00303 2007 12 12 SWAA075895 4 20071128 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007121200304 20071212 00304 2007 12 12 SWAA075894 4 20071128 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007121200305 20071212 00305 NM 2007 12 12 SWAA075897 1 20071128 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 428WN 29844 EEPLS ASSY BROKEN AT ROW 5 ABC. REMOVED AND REPLACED EEPLS ASSY PER MM. 2 L 7 2 4F RT A16WE 2007121200306 20071212 00306 WP 2007 12 12 DHL2007801516 1 20071105 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 160 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 INSPECT REPAIR AT FUSELAGE STA 160 LONGERON 31R PER INSPECTION REQUIREMENTS OF DC8 SRM 53-2-1 CLASS II TYPE REPAIR. REP AIR ACCOMPLISHED AUG 94. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1, 5. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED REPAIR DOUBLER FILLER AND INTERNAL FINGER DOUBLER IAW SRM 53-2-1 FIG 7 SHEET 1, 5 SRM 53-4-1 FIG 5C PG 10 ITEM A, SRM 51-9-0 FIG 68A. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B . INSTALLED REPAIR PARTS IAW SRM 53-2-1 FIG 7 SHEET 1, 5 SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1. THIS IS A CLASS I TYPE REPAIR (INITIAL INSP AT 4000, REPETITIVE AT 4000, REPLACEMENT N/A) IAW SRM 53-2-1 FIG 5, TR NR 53-190 DAT 2 L 7 4 4F RT 4A25 2007121200307 20071212 00307 NM 2007 12 12 SWAA075899 1 20071128 A 3350 D7170230 CHARGER BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 436WN 32456 DURING SCHEDULED HC1 CHECK, FOUND RT FWD CABIN EMERGENCY BATTERY CHARGER INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007121200315 20071212 00315 NM 2007 12 12 ASAA0752288 1 20071128 A 2460 115195214 CONTROL UNIT BOEING 737 737890 1384527 NM E&E BAY MALFUNCTIONED A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 557AS 35176 THE "ELEC" LIGHT ON. BITE PROCEDURE SHOWED SPCU 1 INOP. CLEARED FAULT REF FIM 24 34 TASKS 801 802. NO REOCCURRENCE NO TED. 2 L 7 2 4F RT A16WE 2007121200317 20071212 00317 WP 2007 12 12 DHL2007801507 1 20071029 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1749 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 RT AFT FUSELAGE EXTERNAL SKIN CRACKED 2" STA 1749.000 L-15R TO L-16R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53- 2-1 FIG 7 SHEET 1, 4. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER INTERNA L FINGER DOUBLER AND FILLER IAW SRM 53-2-1 FIG 7 SHEET 1, 4, SRM 53-5-3 FIG 1 ITEM D. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 53-2-1 FIG 7 SHEET 1, 4, SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1. THIS IS A CLASS I TYPE REPAIR (INITIAL INSP 4.000, REPETITIVE 4.000, REPLACEMENT N/A) IAW SRM 53- 2-1 FIG. 5, TR NR 53-190 DATED 09-20-03. REINSPECTION AT 36570 LANDING CYCLES. 2 L 7 4 4F RT 4A25 2007121200327 20071212 00327 WP 2007 12 12 ABXA070379 1 20071106 A 5320 99234843 PANEL DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 SUBFLOOR PANEL 1B WAS CORRODED. FABRICATED AND INSTALLED NEW PANEL IAW DC9 SRM 51-10-4. 2 L 7 2 4F A6WE 2007121200334 20071212 00334 NM 2007 12 12 CALA0700715 1 20071129 A 5315 6546812 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 CORROSION UNDER FLOORBEAM FLANGE AT STA 1016 FROM LBL 9 - LBL 17. PRIMED AND INSTALLED NEW FLOORBEAM CAP IN REF TO ECRA 5310-03851. 2 L 7 2 4F RT A16WE 2007121200345 20071212 00345 EU 2007 12 12 07FDEA05010 1 20071206 A 5347 A5361164020000 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 CABIN, SEAT TRACK CORRODED STA X1240 TO X1340 LBL Y450. REMOVED AND REPLACED SEAT TRACK IAW A310-200 SRM 51-40-21 PAR 6 AND 7. 2 L 7 2 4F RT A35EU 2007121200368 20071212 00368 WP 2007 12 12 AALA20072349 1 20071201 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISLODGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 289AA 49301 LGA - EMERGENCY LIGHTS AT SEAT ROWS 30AC TO 32A INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 30 AC TO 32A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121200369 20071212 00369 EU 2007 12 12 AALA20072351 1 20071201 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70074 517 MIA - EMERGENCY LIGHT AT SEAT 11C BROKEN. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 11C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121200370 20071212 00370 NM 2007 12 12 AALA20072344 1 20071201 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 789AN 30252 JFK - EMERGENCY LIGHT AT SEAT 25C MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121200374 20071212 00374 NM 2007 12 12 AALA20072355 1 20071201 A 3350 SHROUD BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 908AN 29510 MIA - EMERGENCY LIGHT AT SEAT 28D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007121200392 20071212 00392 NE 2007 12 12 ABXA070385 2 20071123 A 7200 JT8D9A ENGINE DOUG DC9 DC933F 302207A WP PWA JT8 JT8D9A 52048 NE RIGHT MALFUNCTIONED A ABXA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 935AX 192 47413 674459 RIGHT OIL STRAINER CLOGGING LIGHT ILLUMINATED ON CLIMBOUT AT REDUCED THRUST. AT IDLE, THE LIGHT STAYED ILLUMINATED. SH UT DOWN RIGHT ENGINE. RIGHT ENGINE WINDMILLED FOR LESS THAN 30 MINUTES. OIL PRESSURE OBSERVED AT ZERO. REPLACED NR 2 ENGINE IAW ABX JOB CARD 9090010. 2 L 7 2 4F 4 F A6WE E2EA 2007121200393 20071212 00393 WP 2007 12 12 ABXA070386 1 20071127 A 2130 CIRCUIT BREAKER DOUG DC9 DC941 302207N WP CABIN PRESSURE DEFECTIVE A ABXA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 23 956AX 47620 COULD NOT PRESSURIZE AIRCRAFT IN AUTO OR MANUAL. FOUND CABIN PRESSURE CONTROL 2 AMP CIRCUIT BREAKER WOULD NOT RESET. R EPLACED 2 AMP CIRCUIT BREAKER. PRESSURIZED AIRCRAFT TO 6 PSI, AIRCRAFT PRESSURIZED NORMALLY PER AMM CHAPTER 21. 2 L 7 2 4F A6WE 2007121200397 20071212 00397 NM 2007 12 12 SWAA075904 1 20071129 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 228WN 32496 DURING SCHEDULED HC1 CHECK, LT FWD EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007121200400 20071212 00400 NM 2007 12 12 SWAA075921 1 20071129 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 275WN 36153 EELPS ASSY LOOSE AT ROW 2 ABC. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007121200402 20071212 00402 NM 2007 12 12 SWAA075908 1 20071129 A 2730 6545166 PUSHROD BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED BRDG CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED PUSH ROD PER MM. 2 L 7 2 4F RT A16WE 2007121200403 20071212 00403 NM 2007 12 12 SWAA075909 1 20071129 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007121200405 20071212 00405 NM 2007 12 12 SWAA075922 1 20071129 A 5610 5717623001 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT ARCED A SWAA K NONE O OTHER NR NOT REPORTED 1 SW 29 348SW 24375 FLIGHT DECK R1 WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2007121200406 20071212 00406 NM 2007 12 12 SWAA075914 1 20071129 A 5330 6545765 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 952, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007121200407 20071212 00407 2007 12 12 SWAA075913 4 20071129 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007121200409 20071212 00409 NM 2007 12 12 SWAA075924 1 20071129 A 5311 6546548 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121200410 20071212 00410 NM 2007 12 12 SWAA075916 1 20071129 A 5311 6546536 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121200411 20071212 00411 NM 2007 12 12 SWAA075917 1 20071129 A 5311 65C33509 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300001 20071213 00001 WP 2007 12 13 DHL2007801508 1 20071105 A 5280 56489331 SKIN DOUG DC8 DC873F 302199F WP LT MLG DOOR DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 LT MLG MID DOOR EXTERNAL SKIN DELAMINATED. REMOVED AND REPLACED LT MLG MID DOOR IAW MM 32-12-1 PG 401. REFER TO JC BZ5 A32376 FOR OPS CHECK. 2 L 7 4 4F RT 4A25 2007121300003 20071213 00003 WP 2007 12 13 DHL2007801512 1 20071107 A 5730 57624434 SKIN DOUG DC8 DC873F 302199F WP RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 RT WING ACCESS DOOR NR 577B INTERNAL SKIN DELAMINATED (STA XA 650.000 - 670.000). REMOVED AND REPLACED DOOR ASSY IAW SR M 51-3-0, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007121300005 20071213 00005 NM 2007 12 13 SWAA075918 1 20071129 A 5311 6546220 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300006 20071213 00006 NM 2007 12 13 SWAA075923 1 20071129 A 5311 6546550 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300007 20071213 00007 NM 2007 12 13 SWAA075919 1 20071129 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED BRDGH CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 3 DEF. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007121300008 20071213 00008 NM 2007 12 13 SWAA075920 1 20071129 A 5330 6545776 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 951, STR 26L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007121300009 20071213 00009 2007 12 13 2007UALA04835 4 20071126 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 478UA 1533 DOOR 1L ESCAPE SLIDE PRESSURE APPEARS LOW. UNKNOWN PRESSURE LEAK WITHIN THE THE SLIDE ASSY. REPLACED THE 1L SLIDE ASS Y. SLIDE WAS SENT TO SHOP FOR OVERHAUL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121300013 20071213 00013 NM 2007 12 13 2007UALA04837 1 20071126 A 3510 VALVE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW REST O2 FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 171UA 24322 UPPER AFT CREW REST FWD LWR BUNK, O2 MASK DOOR WILL NOT OPEN, WITH OPS CK OF THE FLOW CONTROL UNITS. SUSPECT FAULTY VAL VE ASSEMBLY. REPLACED UNITIZED VALVE ASSEMBLY. REF MM 35-21-36. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121300014 20071213 00014 NM 2007 12 13 DHL2007784 1 20071109 A 5755 ANGLE BOEING 727 727227 1384078 NM NR 7 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 LEFT WING BELOW NR 7 SPOILER HAS FALSE SPAR LOWER CHORD ANGLE REPAIR DOUBLER CRACKED AND WITH GAP UNDER DOUBLER. REPAIR MADE PER BOEING SERVICE BULLETIN 727-57-158 REV 1 DATED MARCH 30, 1989. 2 L 7 3 4F A3WE 2007121300018 20071213 00018 NM 2007 12 13 2007UALA04841 1 20071126 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 664UA 29236 LEFT FWD LAV AND FWD X AISLE EEL LIGHTS INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121300021 20071213 00021 WP 2007 12 13 DHL2007801541 1 20071118 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 AFT CARGO COMPT SKIN CORRODED STA 1200.000 L-36 TO L-35L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DAT ED 11-15-07, EVA D853-00021 REV "B" DATED 11-15-07. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED EXISTING EXTERNAL REPAIR DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER (AL7075T6 0.160") REPAIR TRIPLER (AL7075T6 0.100") AND (2EA) FILLERS (AL7075T6 0.125"/0.100") IAW ASTAR DWG NR ESD85300021-001. TAPERED REPAIR DOUBLER FROM 0.160" TO 0.085" AND FILLER FROM 0.125" TO 0.080" IAW AS TAR DWG ESD85300021-001. NDT INSPECTED CUT OUT AREA AND REPAIR PARTS IAW NDT SPM PART 08-00-02 TO 07. NO CRACK NOR COR 2 L 7 4 4F RT 4A25 2007121300024 20071213 00024 NM 2007 12 13 2007UALA04845 1 20071126 A 3350 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT LOOSE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 531UA 25042 EMERGENCY LIGHTING STRIP ON FLOOR AT ROW 29-30 HAS BROKEN PLASTIC AND BULB OUT OF SOCKET. INSTALLED BULB AND RE ASSEMB LED LIGHT. OPERATES PROPERLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121300026 20071213 00026 NM 2007 12 13 2007UALA04847 1 20071126 A 2560 58791 CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU GIRT BAR DEFECTIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 331UA 24192 GIRT BAR FOR DOOR 1R FALLS OUT OF BRACKET. REPLACED POWER LEAD AT ROW 12. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300027 20071213 00027 NM 2007 12 13 2007UALA04851 1 20071127 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 EEL LIGHTS INOP ROWS 11-16. FOUND POWER LEAD DAMAGE. REPLACED POWER LEAD AT ROW 12. EEL LIGHTS OPERATE CORRECTLY. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300028 20071213 00028 NM 2007 12 13 2007UALA04852 1 20071127 A 5210 DOOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE L2 MALFUNCTIONED A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 660UA 27115 DOOR 2L WILL NOT ARM. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121300030 20071213 00030 NM 2007 12 13 2007UALA04854 1 20071127 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 DOOR 2L EXTERIOR EMERGENCY EXIT LIGHT IS INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121300031 20071213 00031 NM 2007 12 13 2007UALA04855 1 20071127 A 5420 FITTING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 662UA 27159 NR 2 PYLON OUTBD MID SPAR FITTING AS SEEN FROM LWR INSIDE TORQUE BOX CRACKED AT 3 - 8INCHES BOLT I/B POSITION. MAJOR RE PAIR ACCOMPLISHED: REMOVED FASTENER FROM CLOSEOUT ANGLE. VERIFIED CRACK BY HFEC. STOP DRILLED END OF CRACK. FABRICAT ED & INSTALLED A REPAIR SPLICE STRAP & FILLER. ANGLE TO BE REPLACED AT C-12. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121300033 20071213 00033 NM 2007 12 13 2007UALA04856 1 20071128 A 5512 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZ STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 RIGHT HORZ STAB LOWER SKIN IS CRACKED, JUST FWD OF FIRST BALANCE PANEL BAY. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF LWR SKIN. INSTALLED A SINGLE .063 THICK DOUBLER. CUT 2EA ACCESS HOLES IN LWR SKIN & INSTALLED REPAIR DOUBL ERS & ACCESS PLATES. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300034 20071213 00034 WP 2007 12 13 DHL2007801521 1 20071108 A 5414 SKIN DOUG DC8 DC873F 302199F WP NR 2 NACELLE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 NR 2 ENG NACELLE INLET COWL UPPER SKIN WORN AT 12 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN (AL2024T3 0.080") A ND SPLICE (STEEL TYPE 17-7PH 0.050") IAW SRM 71-5-2 FIG 2 SHEET 1, 2. HEAT TREATED SPLICE FROM 17-7 PH TO H1050 IAW SRM 51-1-6. CLEANED, TREATED AND PRIMED NEW SKIN IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 71-5-2 FIG 2 SHEET 1, 2, SRM 51-1-21A. 2 L 7 4 4F RT 4A25 2007121300038 20071213 00038 NM 2007 12 13 2007UALA04857 1 20071128 A 5315 STIFFENER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 663UA 27160 BS 246 FLOORBEAM STIFFENER CRACKED RBL 26. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED STIFFENER. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121300039 20071213 00039 NM 2007 12 13 DHL2007770 1 20071206 A 5730 6521655476 SKIN BOEING 727 7272B7 138407L NM RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 770AT 21953 RT WING UPPER SURFACE HAS PANEL O/B OF APU EXH WITH 2 LARGE AREAS OF DELAMINATION APPROX W/S 224 TO 330. TWO AREAS EQUA L TO ABOUT 120 SQ IN. 2 L 7 3 4F A3WE 2007121300041 20071213 00041 NM 2007 12 13 AALA20072309 1 20071127 A 3350 0201804002 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 184AN 29594 ORD - EMERGENCY LIGHT AT SEAT 18D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 18D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007121300043 20071213 00043 NM 2007 12 13 AALA20072310 1 20071127 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 383AN 26995 DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007121300044 20071213 00044 NM 2007 12 13 AALA20072318 1 20071127 A 3350 0201804001 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 391AA 27451 JFK - EMERGENCY LIGHT AT SEAT ROW 33HJ MISSING LENS INOPERATIVE. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 33HJ. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007121300046 20071213 00046 WP 2007 12 13 AALA20072324 1 20071129 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISLODGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 432AA 49350 LGA - EMERGENCY LIGHTS AT OVERHEAD COCKPIT INOPERATIVE. SECURED BATTERIES AT BATTERY CHARGER B5 23 FOR EMERGENCY LIGHTS AT OVERHEAD COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121300048 20071213 00048 WP 2007 12 13 AALA20072314 1 20071127 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISLODGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 417AA 49328 LGA - EMERGENCY LIGHTS AT TAIL COMPARTMENT INOPERATIVE. RESET BATTERIES IN BATTERY PACK FOR EMERGENCY LIGHTS AT TAIL CO MPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121300049 20071213 00049 NM 2007 12 13 AALA20072315 1 20071127 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 198AA 32392 ORD - EMERGENCY LIGHTS AT SEAT ROWS 16D TO 25D INOPERATIVE. REPLACED BATTERY PACK AT M10800 FOR EMERGENCY LIGHTS AT SEAT ROWS 16D TO 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007121300051 20071213 00051 WP 2007 12 13 AALA20072328 1 20071129 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISLODGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 432AA 49350 LGA - EMERGENCY LIGHT AT OVERHEAD SEAT 11A INOPERATIVE. SECURED BATTERIES IN CHARGER B5 101 FOR EMERGENCY LIGHT AT OVER HEAD SEAT 11A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121300053 20071213 00053 EU 2007 12 13 MALA070195 1 20071130 A 3297 WIRE SAAB SF340 340B 7860101 EU MLG DAMAGED A MALA B EMER. DESCENT N FALSE WARNING AP APPROACH 1 GL 15 436XJ 340B436 CREW DECLARED AN EMERGENCY WITH NO MAIN GEAR LIGHT AND INTRANSIT LIGHT REMAINED ON. RT MAIN LANDING GEAR DOWN GREEN IND ICATION INOP. COMPLETED 409 CARD JC NR 201649. REPLACED LANDING GEAR CONTROL HANDLE. OPS CHECKED NO GOOD. REPAIRED W IRE DG604-22 IAW SAAB AMM CH 20. F/C OF GEAR SWINGS OK. ALL CHECKS GOOD, REF 409 CARDS 302068, 201649, 114135, 114136, 113656. 2 L 7 2 4T RT A52EU 2007121300054 20071213 00054 NM 2007 12 13 2007UALA04858 1 20071128 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 MAIN CABIN FLOORBEAM UPPER CHORD CORRODED BS 324 RBL 50 TO 62 WL 207. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED T-CHO RD. FABRICATED & INSTALLED NEW T-CHORD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121300056 20071213 00056 EU 2007 12 13 2007UALA04860 1 20071129 A 5754 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L/E SLAT DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 472UA 1435 DENT IN NR 1 SLAT LEFT INBOARD WING LOWER SURFACE ABOUT 14 INCHES FROM INBOARD EDGE OF SLAT. PANEL JUST AFT OF NR 1 SLA T LOWER SURFACE HAS A CRACK ABOUT 1.5 INCHES LONG AND AREA OF DENT AROUND CRACK IS ABOUT 2.5 INCH DIAMETER. DENT ON LOW ER PANEL BEGINS ABOUT 12 INCHES FROM INBOARD EDGE OF PANEL. REPLACED PANEL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121300057 20071213 00057 NM 2007 12 13 2007UALA04861 1 20071129 A 3350 CHARGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 RIGHT OVERWING FWD TWO EACH EMERGENCY LIGHTS ASSY IS INOP. REPLACED EMERGENCY BATTERY CHARGER. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121300058 20071213 00058 NM 2007 12 13 QXEA200701770 1 20071201 A 3080 4100S01907 DETECTOR BOMBDR DHC8 DHC8402 1390042 NM ICE DETECTION FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 428QX 4617 11 4160 SEA - DURING CLIMB RECEIVED A ICE DETECTOR FAIL CAUTION LIGHT. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LAND ING. MAINTENANCE REPLACED THE LT ICE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007121300059 20071213 00059 NM 2007 12 13 2007UALA04862 1 20071129 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 CEILING EMERGENCY LIGHT NEAR SEAT 53HJK IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121300060 20071213 00060 2007 12 13 QXEA200701782 4 20071129 A 3418 C16177AC TRANSDUCER BOMBDR DHC8 DHC8402 1390042 NM AOA MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 421QX 1313 4149 PDX- FLIGHT 2466 - ON PUSHBACK WITH THE PROPS COMING OUT OF FEATHER, THE STALL PUSHER SYSTEM LIGHT ILLUMINATED. RETURNE D TO THE GATE. MAINTENANCE REPLACED THE AOA TRANSDUCER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007121300062 20071213 00062 EU 2007 12 13 SIMA200734106 1 20071203 A 5311 FRAME SAAB SF340 340B 7860101 EU BS 272 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 307AE 340B307 DURING MBV INSPECTION, THE FRAME AT FS 294.0 WAS FOUND CORRODED. CUT OUT CORRODED AREA OF THE FRAME INSTALLED NEW FRAME IAW SAAB SRM 53-70-30. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4T RT A52EU 2007121300063 20071213 00063 SO 2007 12 13 SIMA200734104 1 20071204 A 2720 9850575793101 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO RUDDER FAILED A SIMA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SW 21 664MS 145779 EMERGENCY DECLARED, RUDDER 1/2 INOP IN FLIGHT LANDED SAFELY. REMOVED AND REPLACED NR 1 RUDDER PRESSURE SWITCH IAW EMB 1 45 AMM 27-23-04. OPS CHECK AND LEAK CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007121300065 20071213 00065 SO 2007 12 13 SIMA200734103 1 20071204 A 2720 RUDDER CONTROL EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A SIMA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SW 21 667GB 145784 EMERGENCY DECLARED, RUDDER 1/2 INOP IN FLIGHT. 2 L 7 2 4T RT T00011AT 2007121300066 20071213 00066 NM 2007 12 13 KNNA200700043 1 20071113 A 5754 114A71213 SLAT TRACK BOEING BOEING 737 737232 1384475 NM PWA JT8 JT8D15 52051 NE ZONE 500 JAMMED A KNNA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 25 326DL 56515 681 BN68 231098 AFTER TAKEOFF, LT LEADING EDGE SLAT DID NOT RETRACT, AIRCRAFT DIVERTED FROM KGNV TO KJAX. PILOT DECLARED IN FLIGHT EMER GENCY FOR FLAPS UP LANDING. AFTER REMOVAL AND INSPECTION, FOUND OUTBD AUXILIARY TRACK JAMMED, WHICH CAUSED THE SLAT TO SHIFT AND THE TRAILING EDGE TO REACH THE UPPER STOP. THUS CAUSING THE DAMAGE TO THE STAT ASSY. 2 L 7 2 4F 4 F RT A16WE E2EA 2007121300068 20071213 00068 NE 2007 12 13 DL76G071530 2 20071122 A 7200 CF680C2B6F ENGINE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 BIRD INGESTION A DALA A UNSCHED LANDING C J F.O.D. WARNING INDICATION CL CLIMB 1 SO 27 1611B 40378 2329 704806 30595 704806 200-300 FT AGL NR 2 ENGINE INGESTED BIRD/BIRDS. ATB INITIATED. ENGINE WAS NOT SHUT DOWN. REMOVED AND REPLACED NR 2 EN G PER TRANS 1T161. 2 L 7 2 4F 4 F RT A1NM E13NE 2007121300069 20071213 00069 NM 2007 12 13 DLM90071567 1 20071128 A 5330 SKIN DOUG MD90 MD9030 3023690 NM BS 210 PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 HOLE PUNCTURED IN FUSELAGE SIDE BELOW L-1 DOOR AIRSTAIR CUT OUT STA 210. REPAIRED FUSELAGE SKIN IAW DELTA ERA 464537-14 REV ORG DATE NOV 20 2007 ON N/R 1000-0009 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2007121300072 20071213 00072 NM 2007 12 13 DL757071570 1 20071109 A 2121 7313674 FAN BOEING 757 757232 1384965 NM GE CF6 CF680C2B6F 30025 NE NR 1 INOPERATIVE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 674DL 25979 704806 RECIEVED EQUIP OVERHEAT EICAS MSG IN FLT SMELLED SMOKE HEARD EQUIP FAN C/B POP. FOUND FAN 1 INOP REPLACED NR 1 FWD EQUI PMENT COOLING SUPPLY, CLEARED MSG CKS GOOD. 2 L 7 2 4F 4 F RT A2NM E13NE 2007121300073 20071213 00073 NM 2007 12 13 DL757071571 1 20071129 A 3097 WIRE HARNESS BOEING 757 757232 1384965 NM L1 WINDOW SPARKS A DALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 624DL 22914 CLIMBING THROUGH 17000 FEET NOTICED A STRONG ELEC SMELL. CAPT NOTICED SPARKING IN LOWER LEFT SIDE OF WINDOW L1. FOUND L1 WINDOW J5 WINDOW HEAT CONNECTION LOOSE. REPLACED J5 WIRE HARNESS AND HARDWARE. 2 L 7 2 4F RT A2NM 2007121300074 20071213 00074 NM 2007 12 13 DLM88071572 1 20071129 A 2916 RESERVOIR DOUG MD88 MD88 3023688 NM HYD SYSTEM AERATED A DALA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 935DL 49722 LEFT HYD SYS PRESS READ ZERO/QTY READ 16QTS WHILE, AIRBORNE 19QTS AT TAXI IN PRESS DROPPED TO ZERO SHORTLY AFTER SLATS W ERE EXTENDED. ON ARRIVAL, BLED LT SYS HYD FOUND ABNORMAL AMOUNT OF AIR IN SYS. EXERCISED FLT CONTROLS AND BLED MORE AI R FROM LT SYS. RAN ENG AND PRESSURIZED LT AND RT HYD SYS. LT ENG PUMP PRESS NORMAL. RAN FLT CONTROLS AND CK OK. 2 L 7 2 4F RT A6WE 2007121300080 20071213 00080 2007 12 13 DL76S071577 4 20071130 A 2565 101656306 SLIDE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE RT OVERWING UNWANTED DEPLOY A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 139DL PDO392 25984 704806 RIGHT OVERWING SLIDE DEPLOYMENT, C/W OP 7838 AND REPLACE OFF WING SLIDE AFTER DEPLOYMENT. 2 L 7 2 4F 4 F RT A1NM E13NE 2007121300085 20071213 00085 NM 2007 12 13 2007UALA04865 1 20071128 A 5210 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 531UA 25042 DOOR 4L DOOR ASSIST BOTTLE READS 2300 AT 70 DEGREES NEEDS SERVICE TO 3000. DUE TO UNKNOWN LEAKAGE. REPLACED BOTTLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121300086 20071213 00086 NM 2007 12 13 2007UALA04866 1 20071128 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 663UA 27160 B-ZONE LEFT SIDE FWD 2 EA EEL LIGHT STRIPS ARE INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121300087 20071213 00087 NM 2007 12 13 2007UALA04867 1 20071128 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 663UA 27160 EMERGENCY EXIT LIGHT AT LEFT AND RIGHT AFT DOORS, LWR PORTION OF LIGHT (DOOR HANDLE ILLUMINATION) IS INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121300090 20071213 00090 NM 2007 12 13 2007UALA04870 1 20071128 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 788UA 26942 AFT GALLEY LT AFT CEILING LIGHT BLINK. RELAMPED LIGHT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121300092 20071213 00092 NE 2007 12 13 DL757071588 2 20071206 A 7260 CHIP DETECTOR BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE LOOSE A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 642DL 44857 726714 23996 726714 AT CRUISE ALT NR 2 ENGINE OIL PRESS WAS IN THE RED AND HAD A LOSS OF OIL QTY, CREW WENT THRU CHECKLIST AND SHUT ENGINE D OWN. OPENED RT ENG FAN COWL. FOUND NR 5 CHIP DETECTOR NOT COMPLETELY SEATED IN CHIP DETECTOR HOUSING. CREW FILLED OUT LOSS OF FLAME REPORT LOG IN LOGBOOK. VERIFIED OIL IN SYSTEM FDR READOUT SHOWED POSITIVE PRESS 3 PSI DURING WINDMILL. PERFORMED INSPECTION PER AMM. REPLACED NR 5 CHIP DETECTOR HOUSING. REPLACED MAIN OIL FILTER. ENG RUN AND LEAK CHKS G O. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121200076 20071212 00076 NM 2007 12 12 USAA920071250 1 20071125 A 5311 6546541504 FRAME BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 663, S3L - S3R. REPAIRED FRAME, BS 663, S3L - S3R IAW B737 SRM 53-00 -07-2R-9 FIGURE 201. 2 L 7 2 4F RT A16WE 2007121200087 20071212 00087 NM 2007 12 12 2007UALA04819 1 20071126 A 2612 P4100822 SWITCH BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE FIRE DETECTION DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 FIRE EXT SQUIB TEST PANEL FAILS TO ILLUM ENG 1 WITH TEST SW 1. SUSPECT DIRTY SWITCH CONTACTS. CLEANED CONTACTS OPS CHEC K NORMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121200094 20071212 00094 NM 2007 12 12 2007UALA04827 1 20071125 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY LIGHT INOP AT 37 ABC. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121200098 20071212 00098 EA 2007 12 12 QXEA200701764 1 20071127 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002C10 1390015 EA ANTI ICE SYS INTERMITTENT A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 611QX 10041 GEG - FLIGHT 2597 - RECEIVED A RIGHT ENGINE DEGRADE CAUTION MESSAGE WHEN TURNING ON THE WING ANTI-ICE. RETURNED TO THE GATE, MAINTENANCE CHECKED THE MDC FAULT HISTORY AND NOTED T2 A/I RELAY FAILED CLOSED. COMPLIED WITH FIM TASK 72-00-00-8 01-804-A01. CHECKS GOOD, MESSAGE DID NOT COME BACK. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007121200103 20071212 00103 EU 2007 12 12 YENA2007103 1 20071122 A 3097 19019566401 WIRE HARNESS EMB ERJ190 ERJ190100IGW 3260408 EU WING FAULTY A YENA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 197JB 4707 19000020 FLT 1604, JFK-PWM, DIVERTED TO BOS DUE A-I WING 2 LEAK EICAS WARNING MSG DISPLAYED DURING CLIMBOUT 11,000 FT OCCURED DUR ING A-I WING TEST. HARD FAULT WARNING ON EICAS, RT TEMP SENSOR SLAT 4 INBOARD (FAULT CODE 301142021 AM1). REMOVED AND REPLACED SLAT HARNESS W612 AND TEMP SENSOR PER AMM 27-83-07, AMM 30-11-02 AI OPERATION CHECKS NORMALLY. OK FOR SERVICE. 2 L 7 2 4F RT A57NM 2007121200123 20071212 00123 NM 2007 12 12 UPS07551255 1 20071204 A 3350 LAMP BOEING 757 75724APF 1384969 NM EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 415UP 23855 EMERGENCY LIGHTS UNARMED LIGHT INOP. RELAMPED IAW MM 33-116-02-2. OPS CKS GOOD. 2 L 7 2 4F RT A2NM 2007121200137 20071212 00137 NM 2007 12 12 UPS07M51251 1 20071013 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C RT HORIZ STAB NR 15 BARREL NUT HOLE FOUND CORRODED. CORROSION AT BARREL BORE REMOVED PER SRM51-21-01 V.2R.35.10X MAGNIFICATION DETAILED VISUAL INSP C/OUT FOUND NO CORROSION EVIDENT. BARREL NUT BORE BLEND OUT VOIDS AND BO TTOM PERIPHERY RADIUS SMOOTHED AND PROTECTED PER SRM 51-21-01V.2R.35. REP SLEEVE BUSHING FAB AND PROTECTED PER EO MD11- 5510-1940 9-L FIG 5. REP C/OUT AT NR 15 RT BORE IS ACCEPTABLE PER EN1685-07. 2 L 7 3 4F RT A22WE 2007121200139 20071212 00139 NM 2007 12 12 SWAA075867 1 20071120 A 5752 SPH46A1502 BEARING BOEING 737 7373H4 1384600 NM AILERON TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED C2 CHECK, FOUND LT WING AILERON TAB INBOARD HINGE HAS EXCESSIVE PLAY. REMOVED AND REPLACED NR 1 BEARIN G PER MM. 2 L 7 2 4F RT A16WE 2007121200151 20071212 00151 NM 2007 12 12 SWAA075846 1 20071126 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121200152 20071212 00152 NM 2007 12 12 SWAA075847 1 20071126 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121200158 20071212 00158 EA 2007 12 12 TRAX200701857 1 20071201 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 FS 280 LBL 9 I/B AND O/B ANGLES ARE CRACKED. DUPLICATED NEW CLIPS. INSTALLED IAW REO 601R-53-11-171. COMPLIED WITH ASA EO 600-53-0090 RII 5000528. 2 L 7 2 4F RT A21EA 2007121200162 20071212 00162 NM 2007 12 12 SWAA075859 1 20071126 A 5322 6546569 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 947, STR 25R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007121200167 20071212 00167 NM 2007 12 12 SWAA075849 1 20071125 A 3350 6128251 CHARGER BOEING 737 737317 138447P NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 693SW 23174 FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2007121200169 20071212 00169 NM 2007 12 12 ASAA0752350 1 20071204 A 8012 332A230017 START VALVE BOEING 737 737890 1384527 NM NR 1 ENG UNKNOWN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 570AS 35185 NO N2 ROTATION. START SWITCH WAS ENGAGED FOR NR 1 ENGINE. OPENED COWL CHECKED CONNECTORS ON START VALVE AND CONDITION OF STARTER. FOUND ALL SECURE. RAN ENGINE OPS NORMAL. OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2007121200175 20071212 00175 NM 2007 12 12 SWAA075862 1 20071121 A 5315 147A5501 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 757LV 29850 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM WEB CORRODED BETWEEN BS 986 AND BS 1006, LBL 45. REMOVED AND REPLACED WEB PE R SRM. 2 L 7 2 4F RT A16WE 2007121200181 20071212 00181 EU 2007 12 12 MAC110701 1 20071018 A 5311 S53672408200 FRAME AEROSP ATR72 ATR72202 8680940 EU FUSLEAGE CORRODED A MTNA K NONE O OTHER IN INSP/MAINT 1 SO 33 810FX 220 DURING INSPECTION, CORROSION WAS FOUND ON FRAME 39 AT BL 0 REQUIRING A FRAME REPAIR. THE CORROSION ORIGINATED FROM A BL UE WATER SPILL AT SOMETIME IN THE PAST. THE LAV WAS PREVIOUSLY REMOVED DURING A RECONFIGURATION OF THE A/C. THIS IS AN ISOLATED CASE AND HAS NOT BEEN FOUND ON OTHER A/C IN OUR FLEET. REPAIR REF: ATR 72 SRM 53-61-40 FIG 110 SHEET 1. 2 H 7 2 4T RT A53EU 2007121200199 20071212 00199 WP 2007 12 12 AALA20072299 1 20071126 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 287AA 49299 LGA - EMERGENCY LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS CABI N. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121200203 20071212 00203 EU 2007 12 12 AALA20072306 1 20071127 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 JFK - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIGHT NUMBER O NE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121200204 20071212 00204 EU 2007 12 12 AALA20072307 1 20071127 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 JFK - EMERGENCY LIGHTS AT LEFT AFT CABIN SEAT MOUNTED AND LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR E MERGENCY LIGHTS AT LEFT AFT CABIN SEAT MOUNTED AND LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121200211 20071212 00211 WP 2007 12 12 UPS07851215 1 20071126 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, SYSTEM OPS CHECKS GOOD PER MM 3 3-50-01-2. 2 L 7 4 4F RT 4A25 2007121200212 20071212 00212 NM 2007 12 12 UPS07M51210 1 20070921 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C MAIN DECK: FROM BS 879 TO BS 899, LT MOST O/B SEAT TRACK CROWN & FLANGE AREAS FOUND CORRODED. CORROSI ON ON M/DECK FR BS 879 TO 899 REMOVED PER SRM 51-21-01V.2R.35. FOUND EXCEEDED LIMT PER SRM 53-70-00D FIG 3 V1 R35. COR RODED SEAT TRACK AT STA 869 & STA 909 LBL 107", TRIMMED OFF PER SRM 53-70-00D FIG 1V1 R40. HFEC INSP C/OUT PER DACNDT S PM R.13 PART06-10-01 FOUND NO CRACK EVIDENT. NEW SEAT TRACK & REP PARTS HOLES P/UP & PROTECTED PER SRM 51-31-01 & 51-21 -01V2 R40. 2 L 7 3 4F RT A22WE 2007121200226 20071212 00226 NM 2007 12 12 SWAA075875 1 20071127 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 409WN 27896 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LOOSE AT RT MID CABIN. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2007121200231 20071212 00231 NM 2007 12 12 SWAA075879 1 20071127 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121200238 20071212 00238 NM 2007 12 12 SWAA075887 1 20071127 A 2560 101114 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 632SW 27707 DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT SIGN COVER MISSING. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007121200261 20071212 00261 NM 2007 12 12 QXEA200701786 1 20071129 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 348PH 484 LMT- SHORTLY AFTER TAKEOFF, THE LAVATORY SMOKE DETECTOR STARTED BEEPING. THE FLIGHT ATTENDANT CHECKED THE LAVATORY AND TRASH BIN FOR SIGNS OF SMOKE OR FIRE. NONE FOUND. FLIGHT ATTENDANT RESET THE SMOKE DETECTOR, THE BEEPING STOPPED, BUT THE FLASHING LIGHT STAYED ON. MAINTENANCE CLEANED THE SMOKE DETECTOR ELEMENT AND PERFORMED TEST PER 26-16-00-710-801. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007121200263 20071212 00263 NM 2007 12 12 NWAA073936316 1 20071203 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 676NW 33002 DURING OVERNIGHT CHECK FOUND RIGHT SIDE E-ZONE EMERGENCY PATH LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PAC K AND POWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007121200272 20071212 00272 NM 2007 12 12 CALA0700704 1 20071127 A 5311 6546539 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 MAIN FRAME CRACKED STA 616 LT JUST BELOW MAIN DECK FLOOR INSTALLED STIFFENING ANGLE AND FILLER PER ECRA 5311-01158. 2 L 7 2 4F RT A16WE 2007121200275 20071212 00275 NM 2007 12 12 CALA0700707 1 20071127 A 5320 65458078 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 CABIN FWD ENTRY INTERCOSTAL WEB LOWER SIDE OF R-1 DOOR LOWER HINGE CRACKED AT FWD I/B CORNER. REMOVED AND REPLACED INTE RCOSTAL WEB PER SRM 53-00-04, 53-00-01, AND 51-40-02. 2 L 7 2 4F RT A16WE 2007121200276 20071212 00276 NM 2007 12 12 CALA0700708 1 20071127 A 5320 654580731 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 CABIN FWD ENTRY WEB FWD OF R-1 DOOR CUTOUT BETWEEN STRINGERS 11R AND 12R O/B SUPPORT CRACKED. REMOVED AND REPLACED WEB PER SRM 53-00-04, 53-00-01, AND 51-40-02. 2 L 7 2 4F RT A16WE 2007121200292 20071212 00292 EU 2007 12 12 TRAX200701811 1 20071127 A 5313 STRINGER AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 ON RT SIDE AT FR 39 STGR 14R DOUBLER OF FR FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-42 WITHIN LIMITS AS PER SRM 53-61-00 FIG 301 MATERIAL THICKNESS: 0.063MATERIAL REMOVED: 0.001 WITHIN LIMITS AS PER SRM: 53-61-00 FIG 301. 2 H 7 2 4T RT A53EU 2007121200296 20071212 00296 WP 2007 12 12 DHL2007801535 1 20071114 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 240 S20-21R CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 MAIN CARGO COMPT FRAME SEGMENT CRACKED 5" STA 240.000 L20R TO L21R. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG. 2 SHEET 2.6. REMOVED DAMAGED FRAME SEGMENT, SPLICES AND EXISTING ANGLES IAW SRM 51-1-20D. FABRICATED NEW FRAME SEGMENT P/N S25 37716 IAW SRM 53-2-0 FIG. 2, SRM 53-2-0 FIG 2 SHEET 1-6 SHEET 8 TR NR 53-110 DATED 11-10-200, SRM 53-4-1 FIG 40 SHEET 7, 9 ITEM "C", SRM 51-2-0 FIG. 50 SHEET 49. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED NEW FRAME SEGMENT AND REINSTALLED SPLICES AND EXISTING ANGLES IAW SRM 53-2-0 FIG 2 SHEET 2 6, SRM 51-1-20D, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007121200312 20071212 00312 NM 2007 12 12 SWAA075903 1 20071128 A 2560 PH22300L GLOWSTRIP BOEING 737 7373G7 1384595 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED C2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP CRACKED AT ROW 1 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007121200318 20071212 00318 NM 2007 12 12 ASAA0742101 1 20071012 A 5311 65465292 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 MAIN CABIN STA 440 BETWEEN STR 8R AND 9R FRAME CRACKED AT HAT BIN ATTACH BRACKET POINT. CUT OUT DAMAGE AREA IAW SRM 53- 00-7 NOT VERIFIED CRACKED CONTAINED IAW 737 NDT MANUAL PART 6 CH 51 00 00 FIG 23. REPAIRED IAW B737 400 SRM 53-00-7 DET AIL II. 2 L 7 2 4F RT A16WE 2007121200325 20071212 00325 WP 2007 12 12 ABXA070381 1 20071106 A 5311 5911448503 FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 AFT LOWER CARGO FRAME PUNCTURED AND CRACKED AT FS 927, BETWEEN LONGERON 29 - 30. REPAIRED FRAME AT FS 927, LONGERON 29 - 30 IAW DC9 SRM 53-03, FIGURE 5. 2 L 7 2 4F A6WE 2007121200333 20071212 00333 EA 2007 12 12 VNAA0711010 1 20071124 A 3244 18X44 TIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NLG FAILED A VNAA O OTHER O OTHER LD LANDING 1 GL 05 245PS 4 7919 CREW REPORTED THE RIGHT NOSE TIRE SHREDDED UPON LANDING IN CLT. MAINTENANCE INSPECTED AND FOUND THE TIRE SHREDDED, DAMA GE TO THE NLG FOLLOW UP DOOR AND A DENT IN THE FUSELAGE. MAINTENANCE REMOVED AND REPLACED BOTH NOSE TIRES. MAINTENANCE REMOVED AND REPLACED THE NLG REAR FOLLOW UP DOOR IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL AND ISSUED A TEMP R EPAIR REO NR 10926 FOR THE DAMAGE TO THE FUSELAGE. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007121200339 20071212 00339 EU 2007 12 12 07FDEA05004 1 20071206 A 5315 A5397422122400 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 BULK PIT FLOORBEAM CORRODED AT FR 65 ( X3514 ) BL 21L TO 35L ( -Y530 TO -Y890) REMOVED AND REPLACED FLOORBEAM IAW A310- 200 SRM 51-40-21 PG 26 & 39, AND A310-200 SRM 51-40-44 PG 7. 2 L 7 2 4F RT A35EU 2007121200342 20071212 00342 EU 2007 12 12 07FDEA05007 1 20071205 A 7830 SWITCH AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D7R4E1 52054 NE THRUST REVERSER LOOSE A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 453FE 267 715410 DURING TAKEOFF ROLL WITH POWER ADVANCING TO TAKEOFF POWER (MAX), THE NR 2 REV UNLOCK LIGHT ILLUMINATED. TAKEOFF WAS RE JECTED. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 15DEC07, SFS BKK/06 T/S FOUND ENG NR 2 RT STOW SWITCH S303 CAME LOOSE. RE-ADJUSTED AND SECURED PER AMM 78-31-18-4, NR 2 T/R. OPS CKD PER AMM 78-32-11-5, FOUND NORMAL. 2 L 7 2 4F 4 F RT A35EU E3NE 2007121200349 20071212 00349 WP 2007 12 12 NWAA073939868 1 20071203 A 3240 836SD620 FUSE DOUG DC9 DC951 3022051 WP NR 4 BRAKE BROKEN A NWAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 01 777NC 67147 67147 47787 THE RIGHT HYDRAULIC SYSTEM FLUID QUANTITY DROPPED TO ZERO DURING TAXI FOR TAKEOFF. COM PROCEDURES WERE COMPLIED WITH. DUE TO A POSSIBLE LOSS OF BRAKING ACTION THE AIRCRAFT WAS TOWED BACK TO THE GATE. MAINTENANCE FOUND THAT THE NR 4 POSIT ION UPPER BRAKE FUSE WAS BROKEN AND HAD COME APART. THE FUSE WAS REPLACED AND LEAK CHECKED. THE ELECTRIC HYDRAULIC PUM P, THE ENGINE DRIVEN HYDRAULIC PUMP, THE HYDRAULIC FLUID QUANTITY LIMITER, AND THE FILTERS FOR THE RIGHT HYDRAULIC SYSTE M WERE ALL REPLACED. ASSORTED HYDRAULIC LINES WERE ALSO REPLACED. FUNCTIONAL CHECKS WERE GOOD AND THE AIRCRAFT HAS RET URNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007121200350 20071212 00350 NM 2007 12 12 AALA20072308 1 20071127 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 908AN 29510 MIA - EMERGENCY LIGHTS AFT ROW 22D INOPERATIVE. REPLACED BATTERY PACK M1672 FOR EMERGENCY LIGHTS AFT ROW 22D. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007121200357 20071212 00357 NM 2007 12 12 AALA20072335 1 20071130 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 795AN 30257 LHR - EMERGENCY LIGHT AT SEAT 39G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 39G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121200361 20071212 00361 NM 2007 12 12 AALA20072331 1 20071130 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 779AN 29955 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121200379 20071212 00379 CE 2007 12 12 112607N458F 1 20071126 A 3260 1EN329R DOWNLOCK SWITCH TEIJINSEIKI CESSNA 500 550 2076604 CE NLG INTERMITTENT E T6FA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 09 458F 1451 0706 5500986 THE GEAR HANDLE WAS MOVED TO THE EXTEND SELECTION DURING APPROACH TO GRR, THE GREEN INDICATOR FOR THE NLG DID NOT ILLUM. PERFORMED THE EMERGENCY PROCEDURES TO ENSURE THE NLG WAS DOWN AND LOCKED. THE NLG INDICATOR FAILED TO ILLUM. FLY-BY OF THE TOWER, TO VISUALLY CHECK THE NLG. IT APPEARED TO BE DOWN, A/C LANDED. THE GROUND FIRE AND RESCUE SYSTEM WAS IN PLACE DURING THE LANDING AND THE NLG DID NOT COLLAPSE. IT WAS DISCOVERED THE INTERNAL SWITCH OF THE NLG ACTUATOR FAILED . THE UNIT WAS REMOVED FROM SERVICE AND SENT OUT FOR REPAIR. AFTER FURTHER RESEARCH IT WAS DISCOVERED THE NLG ACTUATOR WAS REPLACED PER CESSNA SB550-32-48 R2 ON 10/12/2004 (1653.8 TT 1233 CYCL), AND WAS VERIFIED REPLACED PER SB550-32-48 1 L 7 2 4F A22CE 2007121200380 20071212 00380 WP 2007 12 12 AALA20072348 1 20071201 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISLODGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 289AA 49301 LGA - EMERGENCY LIGHTS AT LEFT NUMBER TWO DOOR AND SEAT ROW 28A INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT NUMBER TWO DOOR AND SEAT ROW 28A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121200381 20071212 00381 WP 2007 12 12 AALA20072350 1 20071201 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 289AA 49301 LGA - EMERGENCY LIGHTS AT COCKPIT FORWARD ENTRY INOPERATIVE. REPLACED BATTERY PACK AT B5 23 FOR EMERGENCY LIGHTS AT COC KPIT FORWARD ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121200396 20071212 00396 EU 2007 12 12 YENA2007108 1 20071120 A 2752 792A000007 ACTUATOR AIRBUS 320 A320232 3930326 EU T/E FLAP CONTAMINATED A YENA K NONE F FLT CONT AFFECTED AP APPROACH 1 EA 15 503JB 16217 1123 FLT 352, BUR-JFK. DURING CONFIGURATION FROM FLAPS 1 TO 2 F/CTL FLAPS LOCKED ECAM. WING TIP BRAKE ON. REMOVED AND REPL ACED NR 1 & 2 RT WING FLAP ACTUATORS. RIG/ADJUST FLAP OPERATIONAL TEST GOOD IAW 27-54-49 AND 27-54-00-05. 2 L 7 2 4F RT A28NM 2007121200401 20071212 00401 NM 2007 12 12 SWAA075907 1 20071129 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED 14Y CHECK, FOUND LT WING NR 2 L/E SLAT CRACKED AT T/E. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007121200408 20071212 00408 NM 2007 12 12 SWAA075915 1 20071129 A 5311 6546558 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300012 20071213 00012 WP 2007 12 13 DHL2007801510 1 20071106 A 5730 56110011 SKIN DOUG DC8 DC873F 302199F WP LT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 LT WING UPPER PANEL EXTERNAL SKIN DELAMINATED (STA XW 0 - 33.000). REMOVED AND REPLACED LT WING UPPER PANEL ASSY IAW SR M 51-3-0, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007121300025 20071213 00025 EU 2007 12 13 2007UALA04846 1 20071127 A 2910 HYDRAULIC LINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN SYSTEM MALFUNCTIONED A UALA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 408UA 457 GREEN RESERVOIR LOW LEVEL DISPLAYED ON UPPER ECAM SCREEN. LOSS OF GREEN HYD SYSTEM ON TAXI IN. A/C TOWED TO THE GATE. FOUND LT LOCKING STAY SUPPLY HOSE LEAKING. REPLACED LT LOCKING STAY HOSE. RESERVICED GREEN HYD SYSTEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121300029 20071213 00029 NM 2007 12 13 2007UALA04853 1 20071127 A 2120 UNKNOWN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE GALLEY ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 204UA 28713 SMOKE ODOR IN AREA OF AFT GALLEY. CREW DEBRIEF STATED ODOR PREVELANT THROUGHOUT CABIN , INSPECTED E&E COMPARTMENT , OVE RHEAD AREA AT FWD GALLEY AND LAVS , AFT AND MID GALLEYS WITH ALL ELECTRICAL EQUIPMENT POWERED. TOOK AIRCRAFT TO PAD FOR HIGH POWER RUN WITH ALL PACKS ON FULL - NO ANOMOLOUS ODORS WHERE GENERATED. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121300032 20071213 00032 WP 2007 12 13 DHL2007801518 1 20071102 A 5740 5644972 FITTING DOUG DC8 DC873F 302199F WP NR 4 ALT TANK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 NR 4 ALT TANK FITTING CRACKED 0.500" AT STA XRS 408.000 S-58 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW JC EC-00590-001 , DOUGLAS DWG 5644972. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-11, SRM 51-1-23 (PLI WASHER) SRM 51-1-20D, SRM 51-3-1 (TORQUE). REFER TO JC EC-00590-001 (WO 2624) FOR FABRICATION AND NR 130482 FOR LEAK CHECK (FUEL). 2 L 7 4 4F RT 4A25 2007121300037 20071213 00037 WP 2007 12 13 DHL2007801539 1 20071114 A 5414 SKIN DOUG DC8 DC873F 302199F WP NR 4 NACELLE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 NR 4 ENG NACELLE INLET COWL LT EXTERNAL SKIN CRACKED 1" STA YN 132.000 AT 9 O'CLOCK POS. (MAJOR REPAIR). PERFORMED MAJO R REPAIR IAW FAA FORM 8110-3 DATED 10-16-07, EVA B271-00015 REV IR DATED 10-12-07. REMOVED FASTENERS IAW SRM 51-1-21, S RM 51-1-21A, CUT OUT DAMAGED SECTION IAW ASTAR DWG ESD87100013-001-D REV IR DATED 10-16-07. PERFORMED NDT INSPECTION IA W DC8 NDT SPM PART 06-10-01-001. NO CRACK NOR CORROSION FOUND AT CUT OUT AREA. ENCLOSED SMN FORM 242-2. FABRICATED FI LLER (AL2024"0" 0.080") AND DOUBLER (AL2024"0" 0.090") IAW ASTAR DWG NR ES-D87100013-001-D. HEAT TREATED FILLER AND DOU BLER FROM 2024"0" TO 2024T62 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1- 2 L 7 4 4F RT 4A25 2007121300045 20071213 00045 NM 2007 12 13 AALA20072319 1 20071128 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 792AN 30253 DFW - EMERGENCY LIGHT AT SEAT 41G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 41G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121300047 20071213 00047 WP 2007 12 13 AALA20072325 1 20071129 A 3397 TERMINAL DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 432AA 49350 LGA - EMERGENCY LIGHTS AT TAIL CONE INOPERATIVE. REPAIRED BROKEN TERMINAL FOR EMERGENCY LIGHTS AT TAIL CONE. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121300055 20071213 00055 NM 2007 12 13 2007UALA04859 1 20071128 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 MAIN CABIN INTERCOSTAL APPEARS TO BE CRACKED 1.5 INCH AT BS 680 STRINGER 12L. MAJOR REPAIR ACCOMPLISHED: REPLACED INTE RCOSTAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121300061 20071213 00061 NM 2007 12 13 QXEA200701776 1 20071129 A 3350 31708001A GENERATOR DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHTS MALFUNCTIONED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 353PH 120 496 RDM - EMERGENCY LIGHTS IN THE CABIN FLICKER SOMETIMES THROUGH THE DURATION OF THE FLIGHT. SOME LIGHTS ARE ON UP TO 5 SE CONDS. THE LIGHTS THAT FLICKER ARE THE EXIT SIGNS AND OVERHEAD. MAINTENANCE REPLACED THE NR 2 AC GENERATOR. OPERATION AL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007121300064 20071213 00064 EU 2007 12 13 SIMA200734105 1 20071203 A 5311 FRAME SAAB SF340 340B 7860101 EU BS 272 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 307AE 21265 5000 340B307 DURING MBV INSPECTION THE FRAME AT F.S. 272.0 WAS FOUND CORRODED. CUT OUT CORRODED ON FRAME INSTALLED NEW FRAME IAW SAA B SRM 53-70-30 AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4T RT A52EU 2007121300070 20071213 00070 NM 2007 12 13 DL757071568 1 20071128 A 4920 353N40141 BELLMOUTH BOEING 757 757232 1384965 NM APU CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 628DL 22918 APU AIR INTAKE PLENUM BELLMOUTH CRACKED. MODIFED BELLMOUTH PER SERVICE BULLETIN 757-49-0011. 2 L 7 2 4F RT A2NM 2007121300075 20071213 00075 2007 12 13 DL76L071573 4 20071130 A 3416 LK352 ALTIMETER BOEING 767 767332 1382001 NM INSTRUMENT PANEL INACCURATE A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 1201P 28458 RTB, DUE TO STBY ALTIMETER SHOWED 45000 FT. REPLACED STBY ALT, OPS CK GD. 2 L 7 2 4F RT A1NM 2007121300076 20071213 00076 NM 2007 12 13 2007UALA04863 1 20071128 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 509UA 24763 FLOOR EEL LIGHT INOP AT MID LAV. REPLACED MID LAV EEL STRIP, OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121300077 20071213 00077 NM 2007 12 13 2007UALA04864 1 20071128 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 531UA 25042 EXTERIOR EMERGENCY LIGHT INOP AT MED 4L. FOUND LAMP BURNED OUT. RELAMPED ASSY- OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121300091 20071213 00091 NM 2007 12 13 2007UALA04871 1 20071129 A 5754 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE L/E SLAT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 NR 8 SLAT LOWER SKIN CRACKED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121300093 20071213 00093 2007 12 13 DLM88071589 4 20071206 A 2565 D29982125 SLIDE DOUG MD88 MD88 3023688 NM R1 DOOR UNWANTED DEPLOY A DALA K NONE W INADEQUATE Q C TX TAXI/GRND HDL 1 SO 27 954DL 49885 R1 DOOR SLIDE WAY DEPLOYED WHEN DOOR WAS OPENED BY GATE GROMMET. THE DOOR WAS UNLATCHED AND THE GIRT BAR WAS NOT LOCKED IN THE CLIPS. GIRT/SLIDE WAS HANGING ON THE LOWER DOOR FRAME CUT OUT. REMOVED AND REPLACED R1 DOOR SLIDE PER OP 7035. 2 L 7 2 4F RT A6WE 2007121300094 20071213 00094 NE 2007 12 13 DL76S071590 2 20071205 A 7200 CF680A2 ENGINE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 FAILED A DALA C ABORTED TAKEOFF Y J ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 SO 27 137DL 44511 4540 25306 580209 ADVANCED THROTTLES ON T/O AND GOT A LOUD POP FROM RT ENGINE REMOVED AND REPLACED NR 2 ENG IAW TRANS 1T145. 2 L 7 2 4F 4 F RT A1NM E13NE 2007121300096 20071213 00096 NM 2007 12 13 07FDEA05011 1 20071207 A 5710 STRUCTURE DOUG MD11 MD11F 3023600 NM LT WING LE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 524FE 48480 LEFT WING LEADING EDGE AT STA XOS 774 CAVITY EDGE FOUND CRACKED. REPAIRED AS PER SRM 57-10 -00 FIGURE 21 VOLUME I. REP AIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007121300100 20071213 00100 SO 2007 12 13 CHQA200700088 1 20071204 A 2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LAVATORY DIRTY A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 285SK 145435 CAE311920 RDU TO CLE - AFTER TAKEOFF AT 1,500FT, THE CREW RECEIVED A LAV SMOKE EICAS MESSAGE. THE CREW PERFORMED THE CHECKLIST IT EMS FOR LAVATORY SMOKE AND PREPARED FOR A RETURN TO FIELD. THE FLIGHT ATTENDANT CONFIRMED THAT THERE WAS NO VISIBLE SMO KE NOR ODOR OF SMOKE. THE LAVATORY SMOKE INDICATION WENT AWAY ON FINAL APPROACH AND THE AIRCRAFT LANDED WITHOUT INCIDEN T. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO SIGNS OF FIRE, BUT DID FIND THAT THE LAVATORY SMOKE DETECTOR WAS DIR TY. THE LAVATORY SMOKE DETECTOR WAS CLEANED AND THE ENGINES WERE RUN UP TO HIGH POWER WITH NO FURTHER INDICATIONS. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007121300101 20071213 00101 GL 2007 12 13 CHQA200700089 2 20071204 A 7200 AE3007A1P ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 LEAKING A CHQA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 11 285SK 14746 5245 145435 CAE311920 RDU TO CLE - AFTER TAKEOFF WHILE CLIMBING THROUGH 1,500FT, THE CREW RECEIVED A LAV SMOKE EICAS INDICATION. THE CREW PER FORMED THE CHECKLIST ITEMS FOR LAVATORY SMOKE AND PREPARED TO RETURN TO FIELD. THE FLIGHT ATTENDANT CONFIRMED THAT THER E WAS VISIBLE SMOKE AND A STRONG ODOR OF SMOKE IN THE FORWARD CABIN. THERE WAS NO SMOKE OR ODOR IN THE COCKPIT. THE AI RCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THAT THE NUMBER 1 ENGINE FAN HAD SIGNS OF OIL ON IT. DURING ENGINE RUNS IT WAS CONFIRMED THAT SMOKE WAS ONLY VISIBLE WHILE RUNNING OFF THE NUMBER ONE BLEED SYSTE M. THE AIRCRAFT WAS THEN FERRIED TO STL WERE THE NUMBER 1 ENGINE WAS REPLACED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007121300104 20071213 00104 NE 2007 12 13 761001 2 20071205 A 7200 CF650E2 ENGINE BOEING 747 7472F6B 1384807 NM GE CF6 CF650E2 30018 NE NR 3 FLAMED OUT A Q2SA A UNSCHED LANDING R X J PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 EA 63 761SA 71673 21832 517591 NON-RECOVERABLE STALL ON NR 3 ENGINE AT FL 330. ACCOMPLISHED QRH AND COULD NOT RECOVER STALL AT LEVEL CRUISE. ENGINE F LAME OUT AND IN-FLIGHT ENGINE SHUTDOWN. DIVERTED TO KORD. METAL FOUND IN TAIL PIPE. REPLACING NR 3 ENGINE. 2 L 7 4 4F 4 F RT A20WE E23EA 2007121300108 20071213 00108 WP 2007 12 13 AALA20072360 1 20071202 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 969TW 53619 LGA - EMERGENCY LIGHT AT SEAT ROW 12DEF INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 12DEF. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007121300113 20071213 00113 NE 2007 12 13 AALA20072362 2 20071202 A 7250 BLADES DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LEFT ENGINE FAILED A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 443AA 49469 717880 DFW INFLIGHT T1382/02DEC - DURING CLIMB CREW HEARD A LOUD BANG ON LEFT SIDE OF AIRCRAFT AND NUMBER ONE ENGINE PRESSURE R ATIO ROLLED BACK. REDUCED NUMBER ONE ENGINE TO IDLE. ALL INDICATIONS NORMAL AT IDLE POWER. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE DUE TO TURBINE BLADE FAILURE AND OVER ENGINE GAS TEMPERATURE ON 04 DEC AT DFW. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007121300114 20071213 00114 NM 2007 12 13 AALA20072373 1 20071204 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 902AN 29504 DFW - EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007121300115 20071213 00115 WP 2007 12 13 AALA20072391 1 20071206 A 3260 PSEU DOUG DC9 DC982 3022082 WP MLG INOPERATIVE A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 21 7550 53032 DFW INFLIGHT T2422/06DEC - CREW REPORTED MAIN LANDING GEAR INDICATION ON APPROACH TO DFW. TOWER CONFIRMED GEAR DOWN. LANDED DFW WITHOUT INCIDENT. REPLACED PROXIMITY SWITCH ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121300116 20071213 00116 WP 2007 12 13 AALA20072369 1 20071204 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 400AA 49311 LGA - EMERGENCY LIGHT AT SEAT ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 20. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121300117 20071213 00117 EU 2007 12 13 AALA20072371 1 20071204 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70074 517 MIA - EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS CABI N. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121300118 20071213 00118 NM 2007 12 13 AALA20072380 1 20071204 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 776AN 29582 DFW - EMERGENCY LIGHT AT SEAT 44G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 44G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121300119 20071213 00119 NM 2007 12 13 AALA20072363 1 20071203 A 2781 849704 PSEU BOEING 767 767323 1385205 NM SLATS INOPERATIVE A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 383AN 26995 LAX INFLIGHT T5/03DEC DFW TO HNL - LEADING EDGE SLAT ASYMMETRY MESSAGE ILLUMINATED WITH AURAL WARNING HORN. LANDED LAX WITHOUT INCIDENT. REPLACED PROXIMITY SWITCH ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007121300121 20071213 00121 NM 2007 12 13 AALA20072370 1 20071204 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 368AA 25195 SFO - EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007121300124 20071213 00124 WP 2007 12 13 AALA20072385 1 20071205 A 3222 STRUT DOUG DC9 DC982 3022082 WP NOSE GEAR INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7521A 49898 ORD INFLIGHT T755/05DEC - NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO ORD AND LANDED WITHOUT INCIDEN T. ACCOMPLISHED NOSE STRUT REPACK AND REPLACED SCHRADER VALVE AND SERVICED WITH DRY NITROGEN. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F A6WE 2007121300127 20071213 00127 EU 2007 12 13 AALA20072376 1 20071204 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 40064 507 JFK - EMERGENCY EXIT SIGN LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMPS FOR EMERGENCY EXIT SIGN LIGHT AT LE FT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121300128 20071213 00128 EU 2007 12 13 AALA20072377 1 20071204 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 40064 507 JFK - EMERGENCY EXIT SIGN LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMPS FOR EMERGENCY EXIT SIGN LIGHT AT R IGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121300129 20071213 00129 EU 2007 12 13 AALA20072378 1 20071204 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 40064 507 JFK - EMERGENCY EXIT SIGN LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN LI GHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121300130 20071213 00130 NM 2007 12 13 AALA20072379 1 20071204 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 776AN 29582 DFW - EMERGENCY LIGHT AT SEAT 21C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121300131 20071213 00131 WP 2007 12 13 AALA20072381 1 20071204 A 8012 9794104 START VALVE DOUG DC9 DC982 3022082 WP RIGHT ENGINE INOPERATIVE A AALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 459AA 49564 DFW INFLIGHT T732/04DEC - NUMBER TWO ENGINE START VALVE OPEN LIGHT ILLUMINATED. CAPTAIN SHUT DOWN NUMBER TWO ENGINE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME 20 MINUTES. REPLACED STARTER AND START VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121300134 20071213 00134 WP 2007 12 13 AALA20072384 1 20071205 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 450AA 49476 LGA - EMERGENCY LIGHT AT OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERWING EXIT. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121300135 20071213 00135 WP 2007 12 13 AALA20072389 1 20071206 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 492AA 49730 LGA - EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS CABI N. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121300136 20071213 00136 WP 2007 12 13 AALA20072390 1 20071206 A 2560 SEAL DOUG DC9 DC982 3022082 WP FLASHLIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 44503 49797 LGA - EMERGENCY FLASHLIGHT SECURITY SEAL AT LEFT NUMBER ONE DOOR BROKEN. REPLACED SECURITY SEAL FOR EMERGENCY FLASHLIGH T AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121300137 20071213 00137 NM 2007 12 13 AALA20072386 1 20071206 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 652AA 24610 DFW - EMERGENCY EXIT LIGHT AT SEAT 17A INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT LIGHT AT SEAT 17A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007121300138 20071213 00138 NM 2007 12 13 AALA20072387 1 20071206 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 789AN 30252 MIA - EMERGENCY LIGHT AT SEAT 24G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 24G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121300139 20071213 00139 NM 2007 12 13 2007UALA04872 1 20071129 A 2497 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE E & E BAY DAMAGED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 210UA 30216 RIGHT UTILITY BUSS NO POWER. FOUND PIN "A1" DAMAGED ON M24211 & ON RECEPTICAL. REPLACED P200 PANEL. ACCOMPLISHED P200 PANEL OP CHECK. A/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121300140 20071213 00140 NM 2007 12 13 2007UALA04874 1 20071129 A 2910 HYDRAULIC SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LEFT MALFUNCTIONED A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 644UA 25094 LOSS OF LEFT HYDRAULIC SYSTEM ON ENGINE START. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121300142 20071213 00142 NE 2007 12 13 2007UALA04877 2 20071127 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 MALFUNCTIONED A UALA O OTHER K A FLUID LOSS FLAME/FIRE TX TAXI/GRND HDL 1 WP 29 438UA 678 V10513 RAMP REPORTS NR 2 ENGINE TAILPIPE FIRE ON SHUTDOWN AT GATE. OIL OBSERVED LAST STAGE AFT TURBINE SECTION. CAUSE WAS AN OIL COKE FIRE. PERFORMED MAINTENANCE TIP TO CLEAN, REPLACE COMPONENTS IN AFT TAILCONE. AFTER THIS MTC WAS PERFORMED, T HERE WERE NO FURTHER REPORTS FOR THE NR 2 ENG RELATED TO THIS EVENT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121300145 20071213 00145 NM 2007 12 13 QXEA200701789 1 20071129 A 3010 4100S00503 VALVE BOMBDR DHC8 DHC8402 1390042 NM DEICE SYS INOPERATIVE A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 432QX 982 6 4166 SEA- DEICE PRESSURE LIGHT ILLUMINATED FOUR TIMES ON APPROACH. RAN CHECKLIST EACH TIME AND THE LIGHT WENT OUT, BUT THEN LATER CAME BACK. MAINTENANCE REPLACED THE NR 2 DDV. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007121300146 20071213 00146 SO 2007 12 13 C2XA07TY073 1 20071201 A 5532 RIVET EMB 145 EMB145XR 3260214 SO VERTICAL STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11121 145683 TYS - DURING A CURRENT 3C INSPECTION THE RIGHT AFT FUSELAGE AT FR 76 WAS FOUND WITH SOME CRACKED RIVETS ON THE CONTOUR F LANGE OF THE VERTICAL STAB. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT FUSELAGE CONTOUR FLANGE DRAG ANGLE AT FR 76. ALL WORK WAS ACCOMPLISHED IAW EMB 145 XR SRM 51-46-02, 51-20-03 AND CPM 51-21-07. AIRCRAFT WILL BE RELEASED AT THE EN D OF THE CHECK. 2 L 7 2 4F RT 2007121300147 20071213 00147 NM 2007 12 13 ZZDA2007303 1 20071130 A 5320 PAN BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 946AT 55009 FWD CARGO THRESHOLD CUTOUT HAS AREAS OF CORROSION IN PAN. REPAIR LOWER DOOR JAMB PAN SECTION AT FWD CARGO COMP IAW B717 SRM 53-70-15 REPAIR 6. 2 L 7 2 4F TR A6WE 2007121300148 20071213 00148 NM 2007 12 13 QXEA200701781 1 20071130 A 2760 25ET1TF SWITCH BOMBDR DHC8 DHC8402 1390042 NM TAXI BROKEN A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 409QX 4051 SEA - FLIGHT TAXI SWITCH BROKE OFF. RETURNED TO THE GATE. MAINTENANCE REPLACED THE SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007121300149 20071213 00149 NM 2007 12 13 ZZDA2007304 1 20071128 A 3350 8039251 POWER SUPPLY BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 910AT 55086 EMERGENCY LIGHTS INOPERATIVE ON SEAT ROWS 20 FED TO 25 FED. REPLACED BATTERY SUPPLY ASSY'S. 2 L 7 2 4F TR A6WE 2007121300150 20071213 00150 NM 2007 12 13 QXEA200701777 1 20071202 A 3411 PH11001DH PITOT HEAD DHAV DHC8 DHC8202 2809007 NM DAMAGED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 365PH SEA - NR 2 AIRSPEED INDICATION FAILED FOR ABOUT 3 MINUTES DURING A SEVERE ICING ENCOUNTER. MAINTENANCE REPLACED THE RT PITOT HEAD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007121300151 20071213 00151 NM 2007 12 13 CALA0700720 1 20071202 A 3232 161N50017 ACTUATOR BOEING 757 757224 1384958 NM MLG MALFUNCTIONED A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 17104 27294 GEAR DISAGREED WITH EICAS AIR RETURN. ACTUATOR CHANGED PER FIM 32-30-00. 2 L 7 2 4F RT A2NM 2007121300152 20071213 00152 NM 2007 12 13 CALA0700721 1 20071128 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 LEFT I/B CABIN SEAT TRACK CORRODED STA 827 TO STA 913. REMOVED AND REPLACED FROM STA 827 TO STA 907 PER SERM 53-00-52. 2 L 7 2 4F RT A16WE 2007121300153 20071213 00153 EU 2007 12 13 DHLA200700075 1 20071207 A 3260 PROXIMITY SENSOR AIRBUS 300 A300B42C 3930106 EU LANDING GEAR MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION CL CLIMB 1 GL 05 366DH 249 LANDING GEAR FAILED TO RETRACT (LOCKED OUT) IN WARNING SYSTEM NR 1 PERFORMED ABNORMAL PER AOM RETRACTED IN SYSTEM 2. RE MOVED AND REPLACED PROX SENSORS 63GB AND 65 GB. OPS CK GOOD PER M/M 32-61-00 AND 32-00-00 P/N DSF00201-1. 2 L 7 2 4F RT A35EU 2007121300154 20071213 00154 NM 2007 12 13 CALA0700722 1 20071128 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 SURFACE CORROSION ON LEFT I/B SEAT TRACK AT STA 927. REMOVED AND REPLACED FROM STA 927 TO 947.5 LEFT, TREATED AND PRIME D PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 2007121300155 20071213 00155 NM 2007 12 13 CALA0700723 1 20071201 A 5210 65C807351 ANGLE BOEING 737 7373T0 1384582 NM R2 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 SURFACE CORROSION ON R2 DOOR Z-ANGLE FROM STA 967 TO 993. REMOVED AND REPLACED PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007121300156 20071213 00156 NM 2007 12 13 CALA0700724 1 20071201 A 5311 6554892 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 STA 320 BETWEEN S-20L AND 2-21L CRACK IN FRAME. CUTOUT DAMAGED AREA, INSTALLED REPAIR DOUBLER AND FILLER REF SRM 51-70- 11. 2 L 7 2 4F RT A16WE 2007121300158 20071213 00158 NM 2007 12 13 CALA0700726 1 20071203 A 5313 6545800122 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 STR 27 RT CORRODED AT APPROX STA 320. REMOVED AND REPLACED STRINGER 27 RIGHT STA 320 PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007121300160 20071213 00160 SO 2007 12 13 C2XA07TY074 1 20071202 A 3350 GE1317 LIGHT EMB 135 EMB135LR 3260305 SO EXTERIOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27506 206 LEFT AFT EXTERNAL EMERGENCY LIGHT INOP. REMOVED AND REPLACED LEFT AFT EMERGENCY LIGHT BULB IAW EMB 135 AMM 33-50-10. O PS CKED GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007121300161 20071213 00161 NM 2007 12 13 KPVA200722 1 20071126 A 2761 A44700009 ACTUATOR DHAV DHC8 DHC8103 1386005 NM LT SPOILER CRACKED A KPVA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 WP 13 979HA 29648 373 (PIREP) HYDRAULIC FLUID LEAKING FROM LEFT WING. (MX) REMOVED AND REPLACED LT OUTBOARD SPOILER ACTUATOR IAW DHC-8 MM 27- 14-05 PG 201-203. UPON INSPECTION IT IS NOTED THAT THE ACTUATOR HOUSING CRACKED AND FAILED AT THE PISTON END CAP. THE END CAP SEPARATED FROM THE ACTUATOR UNIT. 2 H 7 2 4T RT A13NM 2007121300165 20071213 00165 WP 2007 12 13 ASAA0782291 1 20071129 A 5313 591143289 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 961AS 53075 LONGERON 2 LEFT CRACKED AT STA 1418. REMOVED CRACKED SECTION OF LONGERON, FABRICATED AND INSTALLED REPLACEMENT SECTION ON LONGERON AND SPLICE IAW MD80 SRM 53-02 FIGURE 18. 2 L 7 2 4F RT A6WE 2007121300166 20071213 00166 NM 2007 12 13 DHLA200700078 1 20071208 A 2720 RUDDER CONTROL BOEING 727 7272M7 138407S NM MALFUNCTIONED A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 750DH 21951 LOWER RUDDER MOVED ON ITS OWN FAR TO THE LEFT AS COMPARED WITH THE UPPER RUDDER AS SEEN ON THE RUDDER POSITION INDICATOR S DURING TAKEOFF ROLL. ACFT PULLED TO THE LEFT, UPPER RUDDER IND FAR RT. TRANSFERRED RUDDER POS IND TO DMI 31029 PER M EL 27-8 CAT C DDD12-18-07 COMPLIED WITH SPECIAL PROCEDURES 27-8 ENTERED IN DMI LOG. 2 L 7 3 4F A3WE 2007121300167 20071213 00167 EU 2007 12 13 DHLA200700079 1 20071208 A 3230 A25280 SEQUENCE VALVE AIRBUS 300 A300B4203 3930306 EU MLG MALFUNCTIONED A DHLA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 364DH 49665 659 141 UPON GEAR RETRACTION, RT MAIN GEAR WOULD NOT RETRACT. UNSAFE LIGHT AND GEAR DOOR LIGHTS BOTH ILLUMINATED. PERFORMED LA NDING GEAR UNSAFE INDICATION ABNORMAL PROCEDURE. LOWERED GEAR. GOT ALL 3 GREEN. CONTACTED MAINT AND FLIGHT CONTROL. RETURNED TO JFK. 2 L 7 2 4F RT A35EU 2007121300168 20071213 00168 WP 2007 12 13 ASAA0782292 1 20071129 A 5313 591143289 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 961AS 53075 LONGERON 2 RIGHT CRACKED AT STA 1418. REMOVED CRACKED SECTION OF LONGERON, FABRICATED AND INSTALLED REPLACEMENT SECTION OF LONGERON AND SPLICE IAW MD80 SRM 53-02 FIGURE 18. 2 L 7 2 4F RT A6WE 2007121300169 20071213 00169 NM 2007 12 13 DHLA200700080 1 20071208 A 7930 SWITCH BOEING 727 7272B7 138407L NM PWA JT8 JT8D17 52049 NE NR 3 ENG OIL SYS MALFUNCTIONED A DHLA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 05 762AT 22162 666312 APPROXIMATLY 35 MIN, AFTER TAKEOFF NR 3 ENG OIL PRESSURE/BYPASS LIGHT ILLUMINATED. ABNORMAL PROCEDURE ACCOMPLISHED, DET ERMINED THAT BYPASS MODE WAS RESPONSIBLE AND ENGINE WAS SHUT DOWN AT 0835Z. PRESSURE AND QUANTITY WAS NORMAL PRIOR TO S HUT DOWN. WINDMILL TIME 1+28. REMOVED AND REPLACED NR 3 ENG OIL FILTER PER JT-8 B/M 71-02-01. REMOVED AND REPLACED NR 3 ENG L/P OIL SWITCH IAW B727 M/M 79-33-1. REMOVED AND REPLACED NR 3 ENG OIL BYPASS SWITCH IAW B727 M/M 79-33-2, CKS G OOD,JRH 5.2 P/N 7578678. 2 L 7 3 4F 4 F A3WE E2EA 2007121300170 20071213 00170 NM 2007 12 13 DHLA200700076 1 20071207 A 5210 DOOR BOEING 727 727233 138408A NM MAIN PAX LACK OF LUBE A DHLA O OTHER O OTHER NR NOT REPORTED 1 GL 05 753DH 22468 FWD ENTRY DOOR WOULD NOT CLOSE ALL THE WAY AND THEN COULD NOT OPEN. FREED FWD ENTRY DOOR. CYCLED DOOR MANY TIMES. DOO R OPERATES NORMALLY PER B727 MM 52-11-22. LUBED DOORS ALL POINTS. 2 L 7 3 4F RT A3WE 2007121300171 20071213 00171 WP 2007 12 13 IXXA07SMN229S 1 20071109 A 5753 SKIN DOUG DC8 DC873F 302199F WP TE FLAP MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP UPPER PLATING HAD IMPROPER REPAIR AT STATION XF 213.000. RE MOVED EXISTING REPAIR. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. I NSTALLED REPAIR PARTS IAW DC8 SRM 57-7-1 FIGURE 4 T/R 5794 ITEM "C", DATED 10-01-02, DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007121300172 20071213 00172 WP 2007 12 13 IXXA07SMN230S 1 20071110 A 5753 SKIN DOUG DC8 DC873F 302199F WP LT WING TE FLAP DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOIND LEFT HAND WING INBOARD FLAP HAS A DENT ON UPPER PANEL PLATING BETWEEN STATION X W 115.000 AND STATION XW 122.000.REMOVED FASTNERS AS NEEDED. REMOVED DAMAGEDAREA. FABRICATED NEW SKIN AND INTERNAL DOUB LER. BONDED REPAIR PARTS WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND RE PAIR PARTS IAW DC8 SRM 51-1-21, DC8 SRM 57-7-1 FIGURE 1 PAGE 2 ITEM "D", "M" AND "K", DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51- 1-9A T/R NUMBER 51-141 DATED 04-05-06, DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007121300173 20071213 00173 WP 2007 12 13 IXXA07SMN231S 1 20071110 A 5753 SKIN DOUG DC8 DC873F 302199F WP LT WING TE FLAP MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER PLATING HAS IMPROPER REPAIR AND DENT BETWEEN STATION XW 104.000 AND XW 115.000. REMOVED FASTENER AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. APPLIED SEAL TO FAYING SURFACE. INSTALLED NEW FAS TENERS AND REPAIR PARTS IAW DC8 SRM 57-7-1 FIGURE 1 PAGE 2 ITEM "D",DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-8B , DC8 SRM 51-1-11, 51-3-0, AND 51-3-1. 2 L 7 4 4F RT 4A25 2007121300174 20071213 00174 EU 2007 12 13 MALA070196 1 20071201 A 3350 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS NO TEST A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 422XJ 340B422 20 LN FAILED BATTERY CAPACITY CHECK IN JC NR 335003. REPLACED EMERGENCY POWER SUPPLY 20LN IAW SAAB 340 AMM 33-50-10, PN 3301-51; SN OFF: 1445; SN ON: 2054. EMERGENCY POWER SUPPLY SYSTEM, OPS CHECKS GOOD IAW MAL JC#335003. 2 L 7 2 4T RT A52EU 2007121300175 20071213 00175 WP 2007 12 13 IXXA07SMN232S 1 20071110 A 5753 SKIN DOUG DC8 DC873F 302199F WP LT WING TE FLAP MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT HAND INBOARD FLAP UPPER PLATING HAS A IMPROPER REPAIR AT STATION XW 71.000 AND STATION XW 91.000.REMOVED FASTNER AS NEEDED TO PERFORM REPAIR.REMOVED EXISTING REPAIR.FABRICATED NEW SKIN AND INTER NAL DOUBLRE. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTNERS AND REPAIR PARTS AT STATION XW 2. 000 TO STATION XW 91.000 IAW 51-3-1, DC8 SRM 57-7-1 FIGURE 1 PAGE 2, ITEM "D", DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, 51-3- 0, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007121300176 20071213 00176 WP 2007 12 13 IXXA07SMN234S 1 20071110 A 5313 LONGERON DOUG DC8 DC873F 302199F WP ZONE 100 MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 97.000 LONGERON 34.5 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NET INSPECTION. NO CRACK NOR CORROSION FOUND. FABRICATED EXTERNAL AND INTERNAL FINGER DOUBLER. CLEANED, TREATED AND PRIMED AREA, AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SEMAN DRAWING NUMBER ED-4642, SRM 51-1-11, 51-3-1, FAA FORM 8110-3 NUMBER 07569 DATED 11-27-07, SEMAN D RAWING NUMBER ED-4642 DATED 11-12-07, DC8 SRM 51-1-21, 51-1-20D, DC8 NDT SPM PART 08-00-02 TO 07, DC8 SRM 51-1-8B, AND A TTACHED FORM SEMAN 242-4. 2 L 7 4 4F RT 4A25 2007121300177 20071213 00177 EU 2007 12 13 07FDEA05018 1 20071208 A 5320 STRUCTURE AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FWD LOWER CARGO PIT "T" CAP CORRODED FR 38.2 (X2187) BL 56R ( -Y1420) UNDER NUT PLATE. REMOVED AND REPLACED "T" CAP ( EXTRUSION ) IAW A310-200 SRM 53-10-15 PAGE 237-242. 2 L 7 2 4F RT A35EU 2007121300179 20071213 00179 EU 2007 12 13 07FDEA05020 1 20071208 A 5410 A54612112600602 WEB AIRBUS 300 A300F4605R 3930327 EU ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 656FE 745 NR 2 FWD PYLON INSIDE ACCESS HOLE JUST FWD OF BLOW-OUT DOORS 2.5 IN CRACK EXIST IN OVAL CUT OUT AT DECK LEVEL REPAIRED C RACKED WEB IAW A300-600 SRM 54-52-12. CUT OUT DAMAGED PORTION OF WEB AND INSTALLED FILLER AND REPAIR DOUBLER IAW A300-6 00 SRM 54-52-21 WITH DEVIATION APPROVED BY EA 6-5450-113392. 2 L 7 2 4F RT A35EU 2007121300180 20071213 00180 EU 2007 12 13 07FDEA05021 1 20071209 A 7830 VALVE AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2* GL THRUST REVERSER MALFUNCTIONED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 667FE 771 ECAM DISPLAYED NR 2 ENG REVERSER PRESSURIZED ON TAKEOFF ROLL. WARNING WENT AWAY WHEN POWER WAS RETARDED. RTO LESS THAN 80KTS. MEL 09DEC07 15:05. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A. THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION." REMOVED AND REPLACED NR 2 ENG. PRSOV VALVE IAW MM 78-31-05. PERFORMED THR UST REV. SYS. CHECK IAW JRH 7-17. PERFORMED POWER ASSURANCE RUN IAW JRH 7-10. NO ECAM WARNINGS WERE NOTED DURING POWER A SSURANCE RUNS. 2 L 7 2 4F 4 F RT A35EU E23EA 2007121300182 20071213 00182 WP 2007 12 13 IXXA07SMN235S 1 20071110 A 5330 SKIN DOUG DC8 DC873F 302199F WP ZONE 100 MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT FS 1518 LONGERON 32.5 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED EXTERNAL DOUBLER AND INTERNAL FINGER DOUBLE R. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACE. INSTALLED NEW FASTENER AND R EPAIR PARTS IAW DC8 SRM 53-2-1 FIGURE 7 SHEET 1,4,5, DC8 SRM 51-1-21, 51-1-20D, SRM 53-4-1 FIGURE 17A SHEET 2 ITEM "B", DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND 51-3-1. 2 L 7 4 4F RT 4A25 2007121300183 20071213 00183 EA 2007 12 13 SWIA200718917 1 20071207 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 929SW 7703 FLT 3937 - NR 3 EMERGENCY FLOOD LIGHT ON CEILING IS INOP. REPLACED LAMP IN NR 3 LIGHT WITH SERVICEABLE UNIT. 2 L 7 2 4F RT A21EA 2007121300184 20071213 00184 EA 2007 12 13 SWIA200718918 1 20071129 A 3310 LIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT SHORTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 961SW 7857 FLT 6436 - MAP LIGHTS INOP. FIRST OFFICERS MAP LIGHT POPS THE CIRCUIT BREAKER. SECURED LOOSE HARDWARE ON MAP LIGHT. 2 L 7 2 4F RT A21EA 2007121300185 20071213 00185 EA 2007 12 13 SWIA200718919 1 20071129 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 340CA 10062 SERVICE DOOR OVERHEAD EMERGENCY LIGHT IS BROKEN. REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F RT A21EA 2007121300186 20071213 00186 SO 2007 12 13 SWIA200718920 1 20071129 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 292SW 120319 EMERGENCY LIGHT OVER PAX DOOR IS INOP. REPLACED EMERGENCY LIGHT. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007121300187 20071213 00187 2007 12 13 SWIA200718921 2 20071201 A 7497 CONNECTOR CNDAIR CL600 CL6002D24 1390016 EA BURNED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 817SK 15107 LEFT AND RIGHT IGNITION A FAULT STATUS MESSAGES. REPLACED CONNECTOR IAW WM CHAPTER 20. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007121300189 20071213 00189 SO 2007 12 13 SWIA200718922 1 20071009 A 5752 TAB EMB 120 EMB120ER 3260203 SO AILERON CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 223SW 120291 LEFT AILERON TRIM TABS HAVE SURFACE CORROSION. REPLACED LEFT AILERON TRIM TAB OUTBOARD CONTROL ROD IAW EMB 120 MM 27-12 -02. 2 L 7 2 4T RT A31SO 2007121300190 20071213 00190 SO 2007 12 13 SWIA200718923 1 20071009 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 223SW 120291 LEFT FORWARD SMALL SEAT TRACK SECTION IS CORRODED. REPLACED SEAT TRACK IAW AMM 53-01-05. 2 L 7 2 4T RT A31SO 2007121300191 20071213 00191 EA 2007 12 13 SWIA200718924 1 20071206 A 3233 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 405SW 7029 FLT 6083 - NOSE GEAR DISAGREE SHORTLY AFTER GEAR RETRACTION. RETURNED TO FIELD. REPLACED NLG ACTUATOR IAW MM 32-33-01. 2 L 7 2 4F RT A21EA 2007121300192 20071213 00192 EA 2007 12 13 SWIA200718925 1 20071205 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR STUCK A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 427SW 7497 SERVICE DOOR OUTER HANDLE WILL NOT RELEASE. REPLACED OUTER HANDLE IAW CRJ SRM 51-40-11, 51-42-06 AND 51-42-21. 2 L 7 2 4F RT A21EA 2007121300193 20071213 00193 SO 2007 12 13 SWIA200718926 1 20071206 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DISCHARGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 229SW 12029 12029 120305 FLT 5714 - TWO SECTIONS OF FLOOR EMERGENCY LIGHT TRACK ARE INOP. REPLACED FORWARD EMERGENCY BATTERY WITH SERVICEABLE UN IT. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007121300194 20071213 00194 EA 2007 12 13 SWIA200718927 1 20071206 A 3350 AD20131A BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS DISCHARGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 812SK 4661 4661 15098 FLT 4000 - OVERHEAD EMERGENCY LIGHT AT ROW 13 IS INOP. REPLACED NR 3 EMERGENCY LIGHT BATTERY AS NEEDED PER CRJ MM 33-50 -00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007121300195 20071213 00195 WP 2007 12 13 IXXA07SMN236S 1 20071110 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 240 S29L DAMAGED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, AT F/S STATION 240 LEFT FRAME HAS DOUBLE DRILLED HOLE BETWEEN LONGERON 29 LEFT AND LO NGERON 30 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PLUGGED MISDRILLED HOLE WITH RIVET. PERFORMED NDT INSP ECTION. NO CRACK, NO CORROSION. FABRICATED REPAIR ANGLE. CLEANED, TREATED AND PRIMED AREA AND REPAIR ANGLE. INSTALLE D NEW FASTENERS AND REPAIR ANGLE IAW SRM 51-1-11, 51-3-1, FAA FORM 8110-3 NUMBER 07529 DATED 11-09-07, SEMAN DRAWING NUM BER ED-4646 DATED 11-08-07, DC8 SRM 51-1-20D, DC8 NDT SPM PART 08-00-02 TO 07, ATTACHED FORM SMN 242-4, AND DC8 SRM 51-1 -8B, 2 L 7 4 4F RT 4A25 2007121300196 20071213 00196 WP 2007 12 13 IXXA07SMN237S 1 20071110 A 5753 VANE DOUG DC8 DC873F 302199F WP RT WING TE FLAP ELONGATED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INTERNAL VANE WITH ELONGATED HOLES AT STATION XS 247.000. REMOVED F ASTENERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER AN D INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA, AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW D C8 SRM 51-1-11, 51-1-20D, 51-3-1, FORM FAA 8110-3 NUMBER 07532 DATED 11-08-07 SEMAN DRAWING NUMBER ED-4649 DATED 11-07-0 7, DC8 SRM 51-1-21, 51-3-0, DC8 NDT SPM PART 08-00-02 TO 07, FORM SMN 242-4, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007121200235 20071212 00235 NM 2007 12 12 SWAA075885 1 20071127 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121200236 20071212 00236 NM 2007 12 12 SWAA075883 1 20071127 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121200245 20071212 00245 NM 2007 12 12 ASAA0742283 1 20071126 A 5210 65867841 GUIDE ARM BOEING 737 7374Q8 138447Q NM L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 765AS 25102 CANNOT CLOSE L1 DOOR. ADJUSTED UPPER GUIDE ARM (REF 52 11 00). DOOR OPS NORMAL. 2 L 7 2 4F RT A16WE 2007121200249 20071212 00249 NM 2007 12 12 QXEA200701784 1 20071201 A 3150 WARNING LIGHT DHAV DHC8 DHC8202 2809007 NM MULTIPLE IND A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 345PH 476 PDX - AFTER STARTING THE NR 1 ENGINE THE START LIGHT REMAINED ILLUMINATED. AFTER MOVING THE START SELECTOR SWITCH MANUA LLY BACK TO CENTER THE LIGHT WENT OUT. THE NR 1 DC GENERATOR CAUTION WAS ILLUMINATED. AFTER FOLLOWING THE CHECKLIST, A LL INDICATIONS WENT TO NORMAL. MAINTENANCE CYCLED THE FAULT RESET SWITCH ON THE DC CONTROL PANEL. FUNCTIONAL TESTS GOO D. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007121200257 20071212 00257 NM 2007 12 12 QXEA200701794 1 20071203 A 2497 CONNECTOR BOMBDR DHC8 DHC8402 1390042 NM BATTERY CONTAMINATED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 400QX 4030 GEG - FLIGHT 2393 - DURING TAXI, THE LOAD ON THE STANDBY BATTERY REMAINS STEADY AT .03 TO .45. RETURNED TO THE GATE. M AINTENANCE CLEANED THE BATTERY INDICATION CONNECTOR AND REMOVED MOISTURE FROM THE STANDBY BATTERY SHUNT AREA. BATTERY I NDICATION RETURNED TO NORMAL AND BATTERY SYSTEM TESTS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007121200264 20071212 00264 NM 2007 12 12 NWAA073925636 1 20071204 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 536US 26483 DURING OVERNIGHT CHECK FOUND DOOR L1 EMERGENCY EXIT SIGN ABOVE DOOR DIMS OUT IN 10 SECONDS. MAINTENANCE REMOVED AND REP LACED BATTERY PACK. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007121200271 20071212 00271 NM 2007 12 12 CALA0700703 1 20071127 A 5311 6546539 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 RIGHT MAIN FRAME CRACKED STA 616 JUST BELOW MAIN DECK FLOOR INSTALLED STIFFENING ANGLE AND FILLER PER ECRA 5311-01158. 2 L 7 2 4F RT A16WE 2007121200282 20071212 00282 EU 2007 12 12 TRAX200701813 1 20071127 A 5313 STRINGER AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 AFT AVIONIC COMPARTMENT, BTW 44-45, STRINGER 21L CORRODED, RESOLVED ON W/O: 75891 TASKCARD: N/R-00243. AFT AVIONIC COMP T, BTW FR 44-45, STRINGER 21L REPLACED IAW 51-25-01. 2 H 7 2 4T RT A53EU 2007121200284 20071212 00284 EU 2007 12 12 TRAX200701820 1 20071128 A 5755 SHIELD AEROSP ATR72 ATR72212 8680945 EU SPOILER CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 THUNDER SHIELD BLADE OF LT SPOILER FOUND CORRODED, RESOLVED ON W/O: 75891 TASKCARD: N/R-00327. CORROSION ON THUNDER SHI ELD BLADE OF LT SPOILER REMOVED IAW SRM 51-21-42 AND WITHIN LIMIT IAW SRM 51-10-10. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42 MATERIAL THICKNESS: 0.024 MATERIAL REMOVED: 0.002 WITHIN LIMITS AS PER SRM: 51-10-10. 2 H 7 2 4T RT A53EU 2007121200291 20071212 00291 EU 2007 12 12 TRAX200701828 1 20071129 A 5720 ANGLE AEROSP ATR72 ATR72212 8680945 EU LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 LT WING STRG 4L PRESSURE DECK ANGLE AT FR 27 CRACKED IN X AXIS 1.625 LONG, RESOLVED ON W/O: 75891 TASKCARD: N/R-00435. FABRICATION NOT REQUIRED PART IN ORDER ON W/C 100-5. 2 H 7 2 4T RT A53EU 2007121200295 20071212 00295 WP 2007 12 12 DHL2007801536 1 20071113 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1690-1700 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 AFT ACCY COMPT SKIN CORRODED STA 1690.000 - 1700.000 L-30L TO L-32R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 1 1-13-07, ENGINEERING VARIATION AUTHORIZATION NR D853-00024 REV IR DATED 11-06-07. REMOVED FASTENERS IAW SRM 51-1-21, SR M 51-1-20D. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT DAMAGED SECT ION AND FABRICATED DOUBLER FILLER AND FINGER DOUBLER IAW DWG NR AE46-53-101 REV IR DATED 10-31-07. NDT INSPECTED CUT OU T AREA AND REPAIR PARTS IAW NDT SPM PART 08-00-02 TO 07. NO CRACK NOR CORROSION FOUND. ENCLOSED SMN FORM 242-4. CLEAN ED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DWG NR AE46-53-101, SRM 51-1- 2 L 7 4 4F RT 4A25 2007121200297 20071212 00297 WP 2007 12 12 DHL2007801522 1 20071109 A 5542 SKIN DOUG DC8 DC873F 302199F WP RUDDER DEFORMED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 RT RUDDER SKIN DEFORMED AT STA ZR 335.000 MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1 PG 2. REMOVED DAMA GED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21, SRM 51-1-21A. FABRICATED PLATING AND BONDED DOUBLER BOTH FROM IAW S RM 55-6-1 FIG 1 PG 2 ITEM "A". BONDED BOTH PARTS IAW SRM 51-1-9, SRM 51-1-9A. CLEANED, TREATED AND PRIMED AREA AND PAN EL PLATING IAW SRM 51-1-8B. INSTALLED PANEL PLATING IAW SRM 51-1-21, SRM 51-1-21A. REFER TO NR 101137 FOR WEIGHT AND B ALANCE AND NR 130177 FOR PAINTING. 2 L 7 4 4F RT 4A25 2007121200310 20071212 00310 NM 2007 12 12 SWAA075902 1 20071128 A 5311 6546558 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121200314 20071212 00314 WP 2007 12 12 DHL2007801525 1 20071105 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 40 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 INSPECT REPAIR AT FUSELAGE 40 LONGERON 28L PER INSTRUCTIONS REQUIREMENTS OF SRM 53-2-1 CLASS II TYPE REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 13 SHEET 3,5. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-20D. FABRICATED REPAIR DOU BLER IAW SRM 53-2-0 FIG 13 SHEET 3,5. SRM 53-2-0 FIG 13 SHEET 5, TR NR 53-169 DATED 09-20-03, SRM 53-3-3 FIG 1 ITEM "C". CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER IAW SRM 51-1-8B. INSTALLED REPAIR DOUBLER IAW SRM 53-2-0 FIG.13 SH EET 3,5, SRM 53-2-0 FIG. 13 SHEET 5 TR NR 53-169, SRM 51-1-11, SRM 51-3-0 SRM 51-1-20D, SRM 51-3-1. THIS IS A CLASS I T YPE REPAIR IAW SRM 51-1-0A FIG 1 TR NR 51-144 MAR 2007, INITIAL INSP AT 4000, REPETITIVE AT 4000, REPLACEMENT N/A, NEXT 2 L 7 4 4F RT 4A25 2007121200321 20071212 00321 EU 2007 12 12 TRAX200701860 1 20071127 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 RT INB SEAT TRACK BTW FR 13 TO 17 CORROSION FOUND. 2 H 7 2 4T RT A53EU 2007121200322 20071212 00322 EA 2007 12 12 TRAX200701861 1 20071202 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 916EV 7757 FLOOR EMERGENCY LIGHTING STRIP IN FWD CABIN DOES NOT ILLUMINATE. 2 L 7 2 4F RT A21EA 2007121200331 20071212 00331 EA 2007 12 12 VNAA0711012 1 20071127 A 7160 INLET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT ENGINE DAMAGED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 218PS 7885 CREW REPORTED MULTIPLE BIRD STRIKES TO THE FUSELAGE, WING AND BOTH ENGINES. MAINTENANCE INSPECTED FOUND DAMAGE TO THE L EFT ENGINE INLET, FORWARD EQUIPMENT BAY DOOR AND BULKHEAD, AND THE RIGHT WING LEADING EDGE. MAINTENANCE REMOVED AND REP LACED THE DAMAGED LEFT ENGINE INLET. MAINTENANCE PERFORMED TEMPORARY REPAIRS. AIRCRAFT WAS FERRIED FOR PERMANENT REPAI RS TO BE ACCOMPLISHED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007121200332 20071212 00332 NM 2007 12 12 CALA0700714 1 20071129 A 5320 6562276 FITTING BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16618 27331 ATTACHMENT CLIP CRACKED AT STA 360 STRINGER 11L. REMOVED AND REPLACED CLIP PER ECRA 5311-01379. 2 L 7 2 4F RT A16WE 2007121200335 20071212 00335 NM 2007 12 12 07FDEA05001 1 20071203 A 5610 WINDSHIELD BOEING 727 7272S2F 1384O81 NM COCKPIT CRACKED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 213FE 8207 8207 22935 AT APPROX 27000' ON CLIMB-OUT, CAPT'S L-1 WINDOW CRACKED/SHATTERED AND BEGAN ARCING. COMPLIED WITH RED TABS PROCEDURES. RETURNED TO MEMPHIS. REMOVED CAPT'S NR 1 WINDOW AND COMPLIED WITH PREPARATION FOR INSTALL IAW B727-200 AMM 56-11-011- 4. COMPLETED INSTALLATION OF WINDSHIELD AND APPLIED AERODYNAMIC SEALANT REF 727-200 AMM 56-11-011-4. REINSTALLED GLARE SHIELD PER 7272-200 AMM 25-10-062-4. 2 L 7 3 4F A3WE 2007121200338 20071212 00338 NM 2007 12 12 07FDEA05003 1 20071206 A 5753 SKIN DOUG MD11 MD11F 3023600 NM LT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 524FE 48480 LEFT WING INBOARD FLAP SURFACE FOUND DENTS (3 EACH). REPAIRED AS PER SRM 57-10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007121200340 20071212 00340 EU 2007 12 12 07FDEA05005 1 20071206 A 5315 A5397422024000 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT CARGO PIT FLOORBEAM CORRODED, FR 64 ( STA. X3461) BL 32 R ( -Y810 ) REMOVED AND REPLACED FLOORBEAM IAW A310-200 SRM 51-40-21 PG 7, 15, & 26, AND A310- 200 SRM 51-40-44 PG 9. 2 L 7 2 4F RT A35EU 2007121200341 20071212 00341 EU 2007 12 12 07FDEA05006 1 20071206 A 5320 A5397426020200 STRAP AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT CARGO PIT FLOOR SUPPORT STRAP CORRODED AT FR 64 ( STA X3461) BL 32R (-Y810). REMOVED AND REPLACED FLOOR SUPPORT STR AP, FR 64 TO FR 67, (STA X3461 - X3620 ) BL 32R ( -Y810 ) IAW A310-200 SRM 51-40-21 PG 7, 15 & 26, AND A310-200 SR M 51-40-44 PG 9. 2 L 7 2 4F RT A35EU 2007121200343 20071212 00343 EU 2007 12 12 07FDEA05008 1 20071206 A 5310 A5377263600000 DOOR FRAME AIRBUS 310 A310222 3930315 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 FORWARD CARGO DOOR JAMB AT FRAME 20 AND 20A/STRINGER 38, RT FERRY F COMPLY WITH EA 6-5310-117514 REV NR POS P. MAJOR R EPAIR ACCOMPLISHED REF: EA NR 6-5310-117520 P1. 2 L 7 2 4F RT A35EU 2007121200344 20071212 00344 EU 2007 12 12 07FDEA05009 1 20071206 A 5311 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 718FD 365 PREVIOUS REPAIR LOCATED IN BULK CARGO ON FRAME 64 UNDER FLOOR BETWEEN STRINGER 46 AND 48 RT HAS 2 EACH REPAIR ANGLES O N THE AFT SIDE MEASURING 14.4" BY 2.9" AND 13.6" BY 2.2" PREVIOUS INSTALLED REPAIR WAS DETERMINED NOT TO BE IAW FEDEX EA 6-5310-68347, DUE TO 15 EACH INCORRECT FASTENERS INSTALLED, BASED ON A VISUAL EVALUATION. REMOVED 15 EACH MS20470DD6 RI VETS, REAMED HOLES TO 1ST OVERSIZE AND INSTALLED 15 EACH LOCK FASTENER IAW A300-600 SRM 51-40-21 AND REF FEDEX EA6-5310- 68347. REPAIR IS CLASSIFIED AS A MAJOR PER FED EX GMM 6-2-100. 2 L 7 2 4F RT A35EU 2007121200347 20071212 00347 EA 2007 12 12 CHQA200700086 1 20071203 A 2750 601R93106505 FLEX DRIVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS DAMAGED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 645BR 7383 GEE872681 IAH TO MAF - AFTER TAKEOFF, THE FLAP LEVER WAS MOVED TO 0 AND THE FLAPS STOPPED RETRACTING AT 6. THE QRH WAS FOLLOWED A ND SUFFICIENT FUEL WAS BURNED OFF TO ALLOW FOR A LANDING BELOW STRUCTURAL LANDING WEIGHT. THE AIRCRAFT LANDED WITHOUT I NCIDENT WITH THE FLAPS AT 6. IAH MAINTENANCE RESET THE FLAP SYSTEM WITH NO FAIL MESSAGES SHOWN AT THE TIME AND THE AIRC RAFT WAS FERRIED TO SDF. SDF MAINTENANCE TROUBLESHOT THE FLAP SYSTEM AND FOUND 3 FLEX SHAFTS THAT WERE BAD. THE NR 3 L EFT, NR 5 LEFT, AND THE NR 5 RIGHT SIDE FLEX SHAFTS WERE REPLACED. AFTER THE REPLACEMENT OF THE FLEX SHAFTS THE FLAPS W ERE RE-RIGGED, THE AIRCRAFT WAS TEST FLOWN SUCCESSFULLY, AND RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007121200355 20071212 00355 2007 12 12 AALA20072321 4 20071128 A 2565 100505201 SLIDE DOUG DC9 DC982 3022082 WP L2 DOOR DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 487AA 49680 MSP - EMERGENCY SLIDE AT LEFT NUMBER TWO DOOR HANDLE VELCRO MISSING. REPLACED SLIDE AT LEFT NUMBER TWO DOOR. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121200358 20071212 00358 NM 2007 12 12 AALA20072336 1 20071130 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 795AN 30257 LHR - EMERGENCY LIGHT AT SEAT 21G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121200360 20071212 00360 NM 2007 12 12 AALA20072338 1 20071130 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 677AN 29427 MIA - EMERGENCY LIGHT AT SEAT 30C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 30C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2007121200365 20071212 00365 NM 2007 12 12 AALA20072347 1 20071201 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 789AN 30252 JFK - EMERGENCY LIGHT AT SEAT 26C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121200366 20071212 00366 EU 2007 12 12 AALA20072339 1 20071130 A 2720 COMPUTER AIRBUS 300 A300B4605R 3930308 EU RUDDER SYSTEM INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 80052 460 MIA INFLIGHT T377/30NOV - BOTH NUMBER ONE AND TWO RUDDER SYSTEM FAILURE DURING CLIMB. RETURNED TO MIA AND LANDED WITHOU T INCIDENT. REPLACED NUMBER ONE AND TWO FEEL LIMITATION COMPUTERS, NUMBER ONE AND TWO SLAT FLAT CONTROL COMPUTERS, AND NUMBER ONE AND TWO FAULT WARNING CONTROL SYSTEM AND VARIABLE STOP ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121200376 20071212 00376 NM 2007 12 12 CALA0700717 1 20071129 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16618 27331 CABIN STA 867 BETWEEN S8 AND S9 FRAME CRACKED AT BRACKET ATTACH TO PSU, OUT RAIL LT SIDE. INSTALLED DOUBLER PER ECRA 53 10-04677. 2 L 7 2 4F RT A16WE 2007121200377 20071212 00377 NM 2007 12 12 CALA0700718 1 20071129 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16618 27331 CABIN STA 907 BETWEEN LT S8 AND S9 FRAME CRACKED WHERE IT ATTACHED TO PSU RAIL SUPPORT. INSTALLED DOUBLERS PER ECRA 531 0-04677. 2 L 7 2 4F RT A16WE 2007121200382 20071212 00382 NM 2007 12 12 AALA20072352 1 20071201 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 960AN 29542 DFW - EMERGENCY EXIT IDENTIFIER LIGHT AT SEAT 14A INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT IDENTIFIER LIGHT AT SEA T 14A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007121200383 20071212 00383 NM 2007 12 12 AALA20072354 1 20071201 A 3350 SHROUD BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 960AN 29542 DFW - EMERGENCY LIGHT AT SEAT 26D SHROUD BROKEN. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 26D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007121200384 20071212 00384 NM 2007 12 12 AALA20072356 1 20071201 A 3350 BALLAST BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 908AN 29510 MIA - EMERGENCY LIGHT AT SEAT 13F INOPERATIVE. REPLACED BALLAST ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 13F. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007121200385 20071212 00385 NM 2007 12 12 AALA20072357 1 20071201 A 3350 D71701100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 928AN 29528 MIA - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 14 AFT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD SE AT ROW 14 AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007121200386 20071212 00386 SO 2007 12 12 C2XA07TY072 1 20071129 A 4920 M4509113A APU EMB 145 EMB145LR 3260212 SO APU BAY MALFUNCTIONED A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 14991 145278 SMOKE SMELL IN COCKPIT. REMOVED AND REPLACED APU IAW EMB 145 MM 49-14-01. OPS AND LEAK CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007121200387 20071212 00387 WP 2007 12 12 AALA20072326 1 20071129 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISLODGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 432AA 49350 LGA - EMERGENCY LIGHT AT OVERHEAD SEAT 7A INOPERATIVE. SECURED BATTERIES IN CHARGER FOR EMERGENCY LIGHT AT OVERHEAD SEA T 7A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121200388 20071212 00388 WP 2007 12 12 AALA20072330 1 20071129 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISLODGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 432AA 49350 LGA - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 30AC INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROW 30AC. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121200389 20071212 00389 NM 2007 12 12 AALA20072311 1 20071127 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 638AA 24596 DFW - EMERGENCY LIGHT AT SEAT 38D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 38D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007121200398 20071212 00398 2007 12 12 SWAA075905 4 20071129 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 250WN 34972 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007121200404 20071212 00404 NM 2007 12 12 SWAA075910 1 20071129 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 6R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2007121300002 20071213 00002 WP 2007 12 13 DHL2007801511 1 20071105 A 5753 5701446502 SKIN DOUG DC8 DC873F 302199F WP TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 NR 3 RT FLAP VANE LWR SKIN DELAMINATED (STA XF 160.000 - 213.000). REMOVED AND REINSTALLED NR 3 RT FLAP VANE (REPAIRED CONDITION) IAW MM 27-51-14 PG 201-202. REFER TO NR 130478 FOR OPS CHECK. 2 L 7 4 4F RT 4A25 2007121300010 20071213 00010 EU 2007 12 13 2007UALA04836 1 20071126 A 5347 SEAT TRACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 486UA 1620 RIGHT INBOARD AND OUTBOARD SEAT TRACKS BETWEEN FRAMES 41AND 47 WORN BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED: REPLACED SEAT TRACKS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121300016 20071213 00016 NM 2007 12 13 2007UALA04839 1 20071126 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN MISLOCATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 662UA 27159 EEL AT LEFT C-ZONE AISLE MIS-LOCATED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121300035 20071213 00035 WP 2007 12 13 DHL2007801533 1 20071114 A 5742 SKIN DOUG DC8 DC873F 302199F WP RUDDER TE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 ITEM REF. NR. 101138: UPPER RUDDER T/E BROKEN AT STA ZR 335.250 (FIBERGLASS) DAMAGE CAUSED BY SEMAN. STAGGERED CUT BACK BY A/2" TO A INCH PER PLY FROM THE CRACK THROUGH ALL DAMAGED PLIES OF THE CLOTH IAW SRM 51-1-19 PG 3. REPLACED THE CUT OUT CLOTH WITH A NEW CLOTH IAW SRM 51-1-9 PG 4 FIG 19. PRESSURIZED THE PATCHED AREAS AND CURED (HYSOL) IAW SRM 51-1-9A , SRM 51-1-19 PAR 4 PG 5. ENCLOSED HEATING PARAMETERS. 2 L 7 4 4F RT 4A25 2007121300052 20071213 00052 WP 2007 12 13 AALA20072329 1 20071129 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISLODGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 432AA 49350 LGA - EMERGENCY LIGHT AT OVERHEAD SEAT 28A INOPERATIVE. RESET BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD SEAT 28A. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121300071 20071213 00071 NM 2007 12 13 DL76G071569 1 20071127 A 2780 UNKNOWN BOEING 767 7673P6 1385105 NM SLATS WARNING LIGHT A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 153DL 24985 EICAS MSG LE SLAT DISAGREE DISPLAYED. LEADING EDGE LIGHT ILLUM WITH THE FLAP LEVER IN 1, BOTH FLAP POINTERS. FSEU CHEC KED, NO FAULT EPSU CHECKED FOUND SENSOR 302. FAULTY TARGET FOUND FULL OF GREASE, CLEANED SYSTEM. OPERATED SEVERAL TIME S, OP`S OK. 2 L 7 2 4F RT A1NM 2007121300078 20071213 00078 NM 2007 12 13 DL76G071574 1 20071130 A 2130 3964621 VALVE BOEING 767 767332 1382001 NM FLOW CONTROL MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 1603 29695 ATL - SVO DIVERTED DUE TO RT PACK WENT INOP. PACK OFF LIGHT ILLUMN. RT ZONE TEMP AND PACK CONTROLLER SHOWS NO FAULTS. AIR SUPPLY BITE MODULE SHOWS NO FAULTS. CREW REPORTED PACK BEGAN WORKING PASSING THRU FL120. REMOVED AND REPLACED RT PACK COMP OUTLET OVHR SW. REMOVED AND REPLACED RT PACK FLOW CTL VALVE. 2 L 7 2 4F RT A1NM 2007121300105 20071213 00105 2007 12 13 AALA20072361 4 20071202 A 2297 WIRE DOUG DC9 DC982 3022082 WP RUDDER SYS CHAFED A AALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 553AA 53083 PHX INFLIGHT T1658/02DEC PSP-DFW - DURING CLIMB AIRCRAFT EXPERIENCED AN UNCOMMANDED RUDDER INPUT. LANDED PHX WITHOUT IN CIDENT. FOUND CHAFED WIRE FOR RIGHT POSITION SENSOR IN AFT TAIL COMPARTMENT. REPAIRED WIRE FOR RIGHT DUEL SERVO RUDDER POSITION SENSOR IN AFT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121300120 20071213 00120 WP 2007 12 13 AALA20072367 1 20071203 A 2560 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 475AA 49650 LGA - EMERGENCY FLASHLIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT AT FORWARD ENTRY DOOR. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121300133 20071213 00133 EU 2007 12 13 AALA20072382 1 20071205 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14077 612 MIA - EMERGENCY LIGHT AT RIGHT FORWARD CABIN. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121300143 20071213 00143 EU 2007 12 13 2007UALA04878 2 20071129 A 7261 CARBON SEAL BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU NR 2 ENGINE LEAKING A UALA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 WP 29 914UA 25381 722251 NR 2 ENGINE SHUT DOWN DUE TO LOSS OF ENGINE OIL. LANDED UNDER AMBER ALERT AND TAXIED TO GATE. FOUND STARTER CARBON SE AL FAILED WITH AN INTERNAL LEAK ON STARTER. REPLACED NR 2 ENGINE STARTER DRIVE CARBON SEAL. RAN ENGINE, NO FURTHER LE AKS NOTED, ALL QUANTITIES, AND PRESSURES NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300198 20071213 00198 SO 2007 12 13 C2XA07IA239 1 20071130 A 2610 WARNING SYSTEM EMB 145 EMB145XR 3260214 SO COCKPIT MALFUNCTIONED A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 27 12160 145799 IAH - FLIGHT 2186, THE CREW REPORTED BAGGAGE WARNING LIGHT ILLUMINATED IN FLIGHT WITH NO INDICATIONS IN EICAS. THE AIRC RAFT LANDED IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007121300199 20071213 00199 SO 2007 12 13 C2XA07IA240 1 20071128 A 3350 20131A BATTERY PACK EMB 145 EMB145XR 3260214 SO CABIN DISCHARGED A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 11107 145654 IAH - FLIGHT 2556 THE CREW REPORTED THAT THE OVERWING EMERGENCY EXIT LIGHTS ILLUMINATED IN FLIGHT WITH ALL OTHERS OFF, A ND FINALLY EXTINGUISHED AFTER APPROXIMATELKY 20 MINUTES. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMO VED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2007121300201 20071213 00201 NM 2007 12 13 SWAA075939 1 20071129 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 202WN 33999 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007121300202 20071213 00202 NM 2007 12 13 SWAA075925 1 20071130 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 232WN 32500 EEPLS ASSY LOOSE AT ROW 3 ABC. SECURED EEPLS ASSY PER MM. 2 L 7 2 4F RT A16WE 2007121300203 20071213 00203 NM 2007 12 13 SWAA075926 1 20071130 A 2560 100031 SIGN BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 247WN 32508 FWD RT CABIN EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2007121300204 20071213 00204 NM 2007 12 13 SWAA075927 1 20071201 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 253WN 32511 L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007121300205 20071213 00205 NM 2007 12 13 SWAA075928 1 20071202 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007121300207 20071213 00207 NM 2007 12 13 SWAA075956 1 20071202 A 5311 6546540 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17L. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2007121300208 20071213 00208 NM 2007 12 13 SWAA075959 1 20071202 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED BRDG CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER MM. 2 L 7 2 4F RT A16WE 2007121300209 20071213 00209 NM 2007 12 13 SWAA075958 1 20071202 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007121300210 20071213 00210 NM 2007 12 13 SWAA075957 1 20071202 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007121300214 20071213 00214 NM 2007 12 13 SWAA075944 1 20071202 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300215 20071213 00215 NM 2007 12 13 SWAA075943 1 20071202 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300216 20071213 00216 NM 2007 12 13 SWAA075930 1 20071201 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 401WN 29813 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 5 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007121300217 20071213 00217 NM 2007 12 13 SWAA075931 1 20071130 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 411WN 29821 DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007121300218 20071213 00218 NM 2007 12 13 SWAA075932 1 20071130 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 411WN 29821 DURING SCHEDULED HC2 CHECK, FOUND EEPLS LIGHT LENS CRACKED AT ROW 5 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007121300220 20071213 00220 NM 2007 12 13 SWAA075934 1 20071130 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 427WN 29831 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007121300226 20071213 00226 NM 2007 12 13 SWAA075960 1 20071202 A 2710 6937290 CONTROL ROD BOEING 737 7373H4 1384600 NM LT AILERON WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED BRDG CHECK, LT AILERON FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD PER MM. 2 L 7 2 4F RT A16WE 2007121300228 20071213 00228 NM 2007 12 13 SWAA075952 1 20071202 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300230 20071213 00230 NM 2007 12 13 SWAA075950 1 20071202 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300234 20071213 00234 NM 2007 12 13 SWAA075954 1 20071129 A 3350 20131A BATTERY PACK BOEING 737 7373Q8 1384670 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007121300237 20071213 00237 NM 2007 12 13 SWAA075938 1 20071202 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 786SW 29811 DURING SCHEDULED MV2 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2007121300238 20071213 00238 SO 2007 12 13 C2XA07ON031 1 20071130 A 2611 K0630 RELAY EMB 145 EMB145XR 3260214 SO SMOKE DETECTOR FAILED A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 11194 6020 145940 FLT 524 - MCI TO RDU - WHILE FLIGHT CREW WAS PERFORMING PRE-FLIGHT WALK AROUND AND SYS CHECKS, ENCOUNTER THAT THE BAGGAG E SMOKE DETECTOR TEST FAIL. MX PERSONNEL REMOVED AND REPLACED RELAY K0630 AND OPERATIONALLY CHECKED SATISFACTORY AND AI RCRAFT WAS RELEASE TO RETURN FOR SERVICE IN AIRWORTHY CONDITIONS. 2 L 7 2 4F RT 2007121300239 20071213 00239 SO 2007 12 13 C2XA07ON032 1 20071202 A 5730 14569685901 SEAL EMB 145 EMB145XR 3260214 SO LT WING SWOLLEN A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 14186 6814 145924 FLT 519 - AUS TO MSY - WHILE FLIGHT CREW WAS PERFORMING A PRE-FLIGHT WALK AROUND ENCOUNTER LT WING FUEL LEAK. MX PERSON NEL REMOVED AND REPLACED FUEL PANEL SEAL AND PERFORMED LEAK CHECK GOOD AND A/C WAS RELEASED TO RETURN FOR SERVICE IN AIR WORTHY CONDITIONS. 2 L 7 2 4F RT 2007121300240 20071213 00240 SO 2007 12 13 C2XA07RI101 1 20071121 A 2611 M83726316002P RELAY EMB 145 EMB145ER 3260211 SO SMOKE DETECTION FAILED A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 14943 145040 FLIGHT 2929 - EWR - CREW REPORTED BAGG SMOKE LIGHT ON, BUT NO VISUAL SMOKE IN CARGO BAY. EWR MX REMOVED AND REPLACED BA GG SMOKE TEST RELAY AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007121300241 20071213 00241 EA 2007 12 13 HNAA0700277 1 20071125 A 2421 31708001A GENERATOR DHAV DHC8 DHC8311 1386006 EA NR 1 FAILED A HNAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 07 343EN 40028 8003 340 NR 1 AC GENERATOR FAILED IN FLIGHT. THE FLIGHT RETURNED TO CLT. THE NR 1 AC GENERATOR AND AC GENERATOR CONTROL UNIT WE RE REPLACED, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2007121300242 20071213 00242 EA 2007 12 13 HNAA0700276 1 20071116 A 3350 LIGHT DHAV DHC8 DHC8311 1386006 EA CABIN INTERMITTENT A HNAA K NONE O OTHER CR CRUISE 1 EA 07 337EN 284 CABIN EMERGENCY LIGHTS CYCLING ON AND OFF IN FLIGHT. PROP HEAT WAS SELECTED ON AT THE TIME. GROUND RAN AIRCRAFT WITH P ROP HEAT ON AND OFF, NO DEFECTS NOTED. COULD NOT DUPLICATE CONDITION. NO FURTHER REPORTS OF EMERGENCY LIGHTS CYCLING O N AND OFF REPORTED SINCE. 2 H 7 2 4T RT A13NM 2007121300246 20071213 00246 NM 2007 12 13 CALA0700727 1 20071203 A 2120 DUCT BOEING 737 737524 1384721 NM AC SYSTEM CONTAMINATED A CALA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 37615 27328 AFTER TAKEOFF SMOKE ENTERED FLIGHT DECK AND CABIN AT APPROX 1000FT MSL. RETURNED TO FIELD. CABIN AND FLT DECK BEGAN TO CLEAR ON FINAL. FOUND DE-ICING FLUID CONTAMINATION IN AC SYSTEM AFTER DE-ICING. SMOKE BURN OUT OF PNEUMATIC SYSTEM AN D REPLACEMENT OF COALESCER BAGS. RAN ENGINES AT VARIOUS POWER SETTING, NO SMOKE. 2 L 7 2 4F RT A16WE 2007121300247 20071213 00247 NE 2007 12 13 HNAA0700280 2 20071129 A 7320 78639114 HMU PWA PW120A DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE DEFECTIVE A HNAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 07 839EX 38055 10729 120776 226 120776 NR 2 ENGINE SURGED DURING CLIMB, TORQUE, FUEL FLOW, AND AIRCRAFT SURGED. A 3.5 TO 4 INCH KNOB SPLIT WITH NR 2 ADVANCED DURING APPROACH. REPLACED NR 2 HMU, OPERATIONAL AND LEAK CHECKS GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2007121300248 20071213 00248 EU 2007 12 13 YENA2007111 1 20071127 A 2797 WIRE HARNESS EMB ERJ190 ERJ190100IGW 3260408 EU L/E SLAT DEFECTIVE A YENA K NONE F FLT CONT AFFECTED DE DESCENT 1 EA 15 190JB 19000011 SLAT FAIL EICAS MESSAGE AFTER SELECTING FLAPS 1. SLAT POSITION SHOWED LOCKED SOMEWHERE BETWEEN THE 0 AND 1 POSITION WIT H - DISPLAYED IN THE SLAT POSITION BOX. FURTHER MOVEMENT OF FLAP HANDLE HAD NO EFFECT ON SLAT POSITION. MESSAGE OCCURE D AROUND 210 KTS DURING FIRST MOVEMENT OF HANDLE. REMOVED AND REPLACED RT OLD STANDARD SLAT HARNESSES (W611) AND (W612) PER EO E2707138 PART II, CLEARED SLAT FAIL MESSAGE IAW 27-83-00. ALL EICAS MSG CLEAR. 2 L 7 2 4F RT A57NM 2007121300249 20071213 00249 EA 2007 12 13 546611232007 1 20071123 A 5210 GUARD CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF343B 30069 NE PAX DOOR LOOSE E J7SA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 05 327FX 5466 (CABIN ALT FAIL) CAS MESSAGE ILLUMINATED AT FL372. CREW DECLARED EMERGENCY TO DESCEND TO FL100. AIRCRAFT DIVERTED WITH UNEVENTFUL LANDING NAD TAXI. MAINTENANCE FOUND A LOCK FASTER GUARD DISPOSITIONED FROM PASSENGER DOOR, WHICH KEPT THE DO OR SEAL FROM PROPER SEATING. REATTACHED GUARD AND PERFORMED AN OPERATIONAL CHECK FLIGHT TO CONFIRM PRESSURIZATION SYSTEM OPERATION. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A21EA E15NE 2007121300250 20071213 00250 2007 12 13 200712042 4 20071129 A 2565 4A40302 SLIDE EMB ERJ170 ERJ170100SE 3260406 NM L1 DOOR MALFUNCTIONED A UHLA K NONE O OTHER IN INSP/MAINT 1 GL 11 870RW 4398 4398 17000138 DURING A SCHEDULED EMERGENCY EVACUATION SLIDE SYSTEM OPERATIONAL CHECK OF THE L1 DOOR AND SLIDE THE OPERATIONAL CHECK FA ILED. THE AIRCRAFT DOOR OPERATED NORMALLY BUT THE SLIDE PARTIALLY DEPLOYED IN A BALL SHAPE AND REMAINED IN THAT SHAPE. 2 L 7 2 4F RT A56NM 2007121300251 20071213 00251 EA 2007 12 13 546611232007A 1 20071123 A 5210 GUARD CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF343B 30069 NE PAX DOOR LOOSE E J7SA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 05 327FX 5466 (CABIN ALT FAIL) CAS MESSAGE ILLUMINATED AT FL372. CREW DECLARED EMERGENCY TO DESCEND TO FL100. AIRCRAFT DIVERTED WITH U NEVENTFUL LANDING NAD TAXI. MAINTENANCE FOUND A HYLOC FASTER GUARD DISPOSITIONED FROM PASSENGER DOOR, WHICH KEPT THE DO OR SEAL FROM PROPER SEATING. REATTACHED GUARD AND PERFORMED AN OPERATIONAL CHECK FLIGHT TO CONFIRM PRESSURIZATION SYSTEM OPERATION. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A21EA E15NE 2007121300252 20071213 00252 2007 12 13 200712041 4 20071128 A 2565 4A40302 SLIDE EMB ERJ170 ERJ170100SE 3260406 NM L1 DOOR MALFUNCTIONED A UHLA K NONE O OTHER IN INSP/MAINT 1 GL 11 640RW 5704 5704 17000058 DURING THE BEGINNING OF THE OPERATIONAL CHECK THE L1 DOOR STARTED TO OPEN, TRANSLATED FORWARD ABOUT 8 INCHES AND THEN ST OPPED. THE SLIDE ACTED AS IF IT BECAME JAMMED AND THE MECHANIC WAS UNABLE TO PULL THE DOOR CLOSED DUE TO THE FORCE BEIN G APPLIED BY THE POWER ASSIST. THE MECHANIC PUSHED THE DOOR OPEN THE SLIDE FELL OUT OF THE BUSTLE BUT DID NOT INFLATE. WHILE STILL HANGING BY THE GIRT THE MECHANIC PULLED MANUAL INFLATION HANDLE AND THE SLIDE INFLATED NORMALLY. 2 L 7 2 4F RT A56NM 2007121300256 20071213 00256 NM 2007 12 13 ZZDA2007306 1 20071127 A 5347 5971207503 SEAT TRACK BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 946AT 55009 COPILOT'S AFT I/B SEAT TRACK CORRODED BEYOND LIMITS. FABRICATED SEAT TRACK FROM RAW STOCK AND REPLACED TRACK. 2 L 7 2 4F TR A6WE 2007121300257 20071213 00257 EA 2007 12 13 COMA0770069 1 20071130 A 5310 DOOR FRAME CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 376CA 10092 LOWER COAMING AFT CARGO DOOR SURROUND FRAME IS GOUGED BEYOND LIMITS. REPAIRED IAW EA 70-5361-01934. 2 L 7 2 4F RT A21EA 2007121300258 20071213 00258 2007 12 13 AMTA200700616 4 20071117 A 2310 RADIO BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE HF SYSTEM MALFUNCTIONED A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 522AT 29330 RT HF RADIO WILL NOT CHANNELIZE ON ANY FREQ. RE-RACKED RT HF RT, OPS CK NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007121300264 20071213 00264 EA 2007 12 13 COMA0760673 1 20071127 A 3297 TC601935S CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA MLG BROKEN A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 956CA 7105 FLIGHT 5594 - RECEIVED ANTI-SKID OUTBOARD CAUTION MESSAGE ON TAKEOFF ROLL. ABORTED TAKEOFF, RETURNED TO GATE WITHOUT IN CIDENT. REPLACED BROKEN CONNECTOR ON WHEEL SPEED TRANSDUCER. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007121300274 20071213 00274 NE 2007 12 13 E0X2007F00000 2 20071119 A 7261 31B167801 SCAVENGE PORT BRAERO 1000 BAE1251000 1500287 EU PWA 305 PW305 NE NR 3 BEARING WORN E E0XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 39 515LR NA1006 DEPARTED, ENROUTE, AT 22,000FT THE FLIGHT CREW DECLARED AN EMERGENCY WHEN THE NR 1 (LT) ENGINE OIL PRESSURE STARTED FLUC TUATING AND ALL LOW PRESSURE LIGHT CAME ON. FLIGHT CREW SHUTDOWN NR 1 ENGINE AND MADE AN EMERGENCY LANDING. THE LANDIN G WAS UNEVENTFUL WITH NO INJURIES. UPON INVESTIGATION, IT WAS NOTED THAT THE NR 1 ENGINE HAD AN OIL LEAK FROM THE NR 3 BEARING SCAVENGE OIL LINE. THE ENGINE HAS BEEN REMOVED FOR REPAIR AND INSPECTION AT THIS LINE. (K) 2 L 7 2 4F 4 F RT A3EU E35NE 2007121300275 20071213 00275 EA 2007 12 13 COMA0760683 1 20071130 A 5755 SPOILER CNDAIR CL600 CL6002C10 1390015 EA WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 376CA 10092 MULTI FUNCTION SPOILER SURROUND STRUCTURE HAS WORKING RIVETS. REMOVED RIVETS AND PERFORMED HOT BOND REPAIR TO DAMAGED A REA IAW EA 70-5751-01925. 2 L 7 2 4F RT A21EA 2007121300276 20071213 00276 NM 2007 12 13 SWAA075964 1 20071201 A 3350 6556633 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 207WN 34012 RT OVERWING EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007121300277 20071213 00277 2007 12 13 SWAA075965 4 20071202 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR UNWANTED DEPLOY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 223WN 32492 R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007121300287 20071213 00287 EU 2007 12 13 14011OCT3107 1 20071031 A 6420 109013505101 SCISSOR LINK AGUSTA A109 A119 0261102 EU PWA PT6 PT6* 52043 EA TAIL ROTOR BROKEN E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 820NA 14011 UPON THE PILOTS DAILY INSPECTION HE FOUND THE SUSPECT PART APPERARED TO BE CRACKED. THE MECHANIC REMOVED THE PART FROM A IRCRAFT AND PART CAME APART AT ONE OF THE MOUNTING EARS. 1 G 7 2 3U 3 T H7EU E2NE 2007121300288 20071213 00288 NM 2007 12 13 SWAA075992 1 20071203 A 5311 6546557 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300289 20071213 00289 NM 2007 12 13 SWAA075991 1 20071203 A 5311 6546554 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300290 20071213 00290 NM 2007 12 13 SWAA075990 1 20071203 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300291 20071213 00291 NM 2007 12 13 SWAA075989 1 20071203 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300292 20071213 00292 EU 2007 12 13 14011NOV2907 1 20071129 A 7110 109034217103 STIFFENER AGUSTA A109 A119 0261102 EU COWLING CRACKED E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 820NA 1004 300 14011 ENGINE COWLING STIFFENER CRACKED AT APPROX. STA. 4960, WL 1979, BL 510. THE CRACK RUNS COMPLETELY THROUGH THE STIFFENER IN THE AREA OF THE CUTOUT FOR THE OIL BREATHER TUBE INSTALLED ONTO THE ENGINE. 1 G 7 2 3U H7EU 2007121300293 20071213 00293 CE 2007 12 13 N772PT112707 1 20071127 A 2822 99144251 PUMP CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LT ENGINE BROKEN E AWKA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 WP 25 772P 440 7500272 CAE330571 AT LEVEL AT FL430 JUST PRIOR TO DECENT THE AMBER FUEL BOOST ON-L MESSAGE ILLUMINATED, WHICH WAS FOLLOWED BY AN AMBER FUE L LOW PRESS-L MESSAGE. AFTER LANDING AND WITH ONLY THE APU RUNNING, THE PILOTS WITNESSED A LARGE AMOUNT OF FUEL LEAKING FROM THE LT ENGINE COWING. AFTER SHUTTING DOWN THE APU AND SECURING THE AIRCRAFT, THE LT ENGINE COWLING WAS OPENED. A V ISUAL INSPECTION DETERMINED THE LT ENGINE MOTIVE FLOW FUEL PUMP HAD AN INTERNAL FAILURE THAT CAUSED THE HOUSING TO BREAK WITH AN APPROXIMATELY ONE INCH HOLES. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007121300294 20071213 00294 NM 2007 12 13 SWAA075968 1 20071203 A 5310 6547980 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM CHORD CORRODED BETWEEN BS 947 AND BS 1006, RBL 49. REMOVED AND REPLACED C HORD PER SRM. 2 L 7 2 4F RT A16WE 2007121300295 20071213 00295 NM 2007 12 13 SWAA075969 1 20071201 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 401WN 29813 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 5 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007121300296 20071213 00296 NM 2007 12 13 SWAA075970 1 20071203 A 2560 65C16820 HOOK BOEING 737 7377H4 1384404 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 406WN 27894 L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM. 2 L 7 2 4F RT A16WE 2007121300298 20071213 00298 NM 2007 12 13 SWAA075972 1 20071203 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 418WN 29823 DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007121300300 20071213 00300 NM 2007 12 13 SWAA075981 1 20071203 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 460, BL 0. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007121300302 20071213 00302 NM 2007 12 13 SWAA075977 1 20071203 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300303 20071213 00303 NM 2007 12 13 SWAA075976 1 20071203 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300304 20071213 00304 NM 2007 12 13 SWAA075975 1 20071203 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300306 20071213 00306 NM 2007 12 13 SWAA075995 1 20071203 A 5753 65C30462 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED BRDG CHECK, FOUND RT WING FOREFLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007121300307 20071213 00307 CE 2007 12 13 DXTA200702636 1 20071129 A 2770 LAMP CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE INDICATOR INOPERATIVE E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 837QS 5600685 YAW DAMPNER WOULD NOT ENGAGE ON DEPARTURE. PERFORMED AND CHECK AND FOUND BOTH LAMP IN THE SWITCH/IND BURNED. RELALMPED AND PERFORMED A GOOD OPERATIONAL CHECK REF CESSNA 560 MM 22-11-00 AND 33-10-00 2 L 7 2 4F 4 F RT A22CE E00053EN 2007121300309 20071213 00309 NM 2007 12 13 SWAA075982 1 20071203 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300311 20071213 00311 CE 2007 12 13 DXTA200702637 1 20071129 A 3260 DOWNLOCK SWITCH CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE MLG INTERMITTENT E DXTA A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 GL 07 809QS 5600698 GEAR UNSAFE INDICATION ON LT MAIN. RECYCLED GEAR IAW ACP REQUEST STILL UNSAFE. DIVERTED, VISUAL FLY BY INSPECTION INDIC ATED OK. LANDED WITH NO INCIDENT. COULD NOT CONFIRM DISCREPANCY. PERFORMED MULTIPLE GEAR SWINGS WITH ALL NORMAL INDIC ATIONS. SUSPECT INTERMITANT LT MLG ACTUATOR DOWN LOCK SWITCH. REMOVED AND REPLACED NR 1 MLG ACTUATOR WITH SERVICABLE UNI T IAW CE-560 M/M CHAP 32-31-10. PERFORMED GEAR SWINGS. OPS CHECK AND LEAK CHECK SATISFACTORY. 2 L 7 2 4F 4 F RT A22CE E00053EN 2007121300313 20071213 00313 NM 2007 12 13 SWAA075985 1 20071202 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300316 20071213 00316 NE 2007 12 13 363011292007 2 20071129 A 7320 0292928370 HYDROMECH UNIT SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B 60037 NE ENGINE LEAKING E QMLA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 902CF 3630 22351 DURING PATIENT TRANSFER FLIGHT FROM OUTLYING HOSPITAL TO MAIN HOSPITAL, FUEL FUMES NOTED BY ALL CABIN OCCUPANTS. VENTS A ND HEATER DUCTS MANIPULATED WITH NO DISCERNABLE EFFECT. SMELL OF FUEL FUMES INCREASED IN INTENSITY TO UNPLEASANT LEVELS UPON REDUCTION OF COLLECTIVE DURING APPROACH TO LANDING PHASE. SUBSEQUENT INVESTIGATION BY DUTY MECHANIC REVEALED FAULTY HMU. MECHANIC FOUND FUEL LEAKING INTO ENGINE FROM THE P2 SENSE LINE. 1 G 7 1 3U 3 U H9EU E00054EN 2007121300318 20071213 00318 NM 2007 12 13 SWAA075987 1 20071201 A 5743 115A5211 FITTING BOEING 737 7377H4 1384404 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 715SW 27849 DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION FITTING MOUNT LUG CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300319 20071213 00319 NM 2007 12 13 SWAA075988 1 20071201 A 5743 115A5211 FITTING BOEING 737 7377H4 1384404 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 715SW 27849 DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION FITTING MOUNT LUG CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300321 20071213 00321 NM 2007 12 13 SWAA075980 1 20071202 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 762SW 27876 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300322 20071213 00322 SO 2007 12 13 GLBA20061032 1 20071129 A 5230 DOOR FRAME EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CARGO DOOR CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 96ZK 120096 DURING C-CHECK INSPECTION, A CARGO DOOR FRAME WAS FOUND CRACKED UNDERNEATH FORWARD UPPER STEP. MAINTENANCE REPAIRED CRAC K ON OUTER CARGO DOOR FRAME BENEATH THE FORWARD UPPER STOP I.A.W. EMB120 SRM 52-30. REPAIR APPROXIMATELY 9". RII INSPECT ION COMPLIED PER GLA TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A31SO E20NE 2007121300323 20071213 00323 2007 12 13 SWAA075979 4 20071202 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 762SW 27876 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007121300325 20071213 00325 NM 2007 12 13 2007UALA03189 1 20070815 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 AFT LAV AREA FLOORBEAM CORRODED BS 1016 BL 4R-8R. MAJOR REPAIR: REMOVED DAMAGED SECTION OF STA 1016 FLOORBEAM CAP LBL 10 TO RBL 21 AND REPAIRED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300326 20071213 00326 CE 2007 12 13 GUUA11290701 1 20071129 A 3230 LANDING GEAR BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA STUCK A GUUA O OTHER J WARNING INDICATION CL CLIMB 1 SO 29 87550 UE205 AFTER TAKEOFF LANDING GEAR GOT STUCK ON THE DOWN POSITION TOOK (2) CYCLES TO BRING IT BACK UP. PERFORMED LANDING GEAR E XTENSION AND RETRACTION. COULD NOT DUPLICATE. 2 L 7 2 4T 3 T RT A24CE E2NE 2007121300331 20071213 00331 NM 2007 12 13 2007UALA03879 1 20070924 A 5320 654654417 ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LT MLG WW CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 LEFT MLG WHEEL WELL BS 695 FRAME FWD CHORD ANGLE CRACK INDICATION IN RADIUS. MAJOR REPAIR: REMOVED AND REPLACED CRACKE D ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300336 20071213 00336 CE 2007 12 13 DXTA200702642 1 20071202 A 2150 ACM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CABIN SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 933QS 7500133 AFTER LANDING DURING TAXI IN, A SLIGHT BURNING RUBBER ODOR WAS NOTICEABLE. ( BOTH ENGINES AND APU RUNNING) AFTER ENGINE SHUTDOWN, APU STILL ON, THE ODOR GOT VERY STRONG AND CABIN STARTED TO FILL WITH SMOKE. ODOR AND SMOKE CLEARED AFTER COM PLETE SHUTDOWN. REMOVED AND REPLACED CABIN ACM WITH A REPAIRED UNIT. PERFORMED OPERATIONAL TEST OF THE ECU. OPS CHEC K GOOD. ALL WORK DONE IAW MM 21-51-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007121300337 20071213 00337 NM 2007 12 13 2007UALA03931 1 20070925 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 305UA 23666 RIGHT EXT FUSELAGE STA 320, 1-2 INCHES ABOVE STR 18R, ABOUT 10 INCHES BELOW FWD GALLEY DOOR, A .093" DEEP 2" WIDE DENT. MAJOR REPAIR: PERMANENT DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121200399 20071212 00399 NM 2007 12 12 SWAA075906 1 20071129 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 250WN 34972 DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007121300004 20071213 00004 WP 2007 12 13 DHL2007801513 1 20071106 A 5740 FITTING DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 LT WING CTR L/E UPPER INTERNAL SPLICE FITTING CRACKED 3" AT STA XOLDI 6.2246. REMOVED SPLICE FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 5 1-1-21, SRM 51-1-20D, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007121300011 20071213 00011 WP 2007 12 13 DHL2007801509 1 20071029 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1620 S20-21R CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 FUSELAGE AFT SVC DOOR CRACKED 0.750" STA 1620.000 L-20R TO L-21R AT LWR FWD JAMB CORNER (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD200-20-08 S/B DC8-53-075, DRAWING DOUGLAS SR08530021. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0 AND S RM 51-1-20D. CUT OUT DAMAGED AREA IAW DRAWING DOUGLAS SR08530021. PERFORMED NDT INSPECTION IAW DC8 NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK, NO CORROSION AFTER CUT. ATTACHED FORM SMN 242-2. FABRICATED REPAIR DOUBLER F ROM AL7075T6 0.090" AND REPAIR TRIPLER FROM AL7075T6 0.125" AND FILLER FROM AL7075T6 0.080" IAW DRW DOUGLAS SR08530021. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DRAWING DOUGLAS SR085300 2 L 7 4 4F RT 4A25 2007121300015 20071213 00015 NM 2007 12 13 2007UALA04838 1 20071126 A 3397 CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 585UA 26709 DURING ENGINE START ELECTRICAL POWER WAS LOST AND FLT ATTENDANT REPORTED THAT SEVERAL EEL FLOOR STRIPS WERE NOT ILLUMINA TED WHEN EMERGENCY LIGHTS CAME ON. AFTER POWER UP STRIPS NEAR ROWS 9-13 AND 24-31 WERE INOP. REPLACED BROKEN POWER EX T AT ROW 14 AND SYSTEM CHECKS NORMALLY, 2 L 7 2 4F 4 F RT A2NM E17NE 2007121300017 20071213 00017 NM 2007 12 13 2007UALA04840 1 20071126 A 3350 CHARGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 EMERGENCY LIGHTS ABOVE OVERWING DOORS ARE INOP. REMOVED & REPLACED BATTERY CHARGER & BATTERY ASSY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121300019 20071213 00019 WP 2007 12 13 DHL2007801540 1 20071121 A 5710 SPAR CAP DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 LT LWR WING FRONT SPAR CAP CRACKED 1.250" APPROXIMATELY AT STA XFS 520.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW F AA FORM 8100-9 DATED 11-20-07, BOEING MSG NR 1-653039342-4 DATED 10-22-07, BOEING SKETCH JO060232, JCT04316, EVA D857-00 022 REV IR DATED 10-27-07. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICATED FILLER (AL7075T73 51) DOUBLER (AL7075 T7351) (4EA) ANGLES (7075"0" 0.071") IAW BOEING SKETCH J060232. NDT INSPECTED CUT OUT AREA. NO CRA CK NO CORROSION FOUND IAW NDT SPM PART 08-00-02 TO 07. ENCLOSED SMN FORM 242-4. HEAT TREATED ANGLES FROM 7075"0" TO 7 075T6 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR P 2 L 7 4 4F RT 4A25 2007121300020 20071213 00020 NM 2007 12 13 2007UALA04842 1 20071126 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 664UA 29236 SEAT 26B EEL LIGHT INOPERATIVE. REPLACED LIGHT ASSY. OPS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121300022 20071213 00022 NM 2007 12 13 2007UALA04843 1 20071126 A 2611 SMOKE DETECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE E&E BAY FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 664UA 29236 FWD EQUIP COOLING TEST FAILED. NO SMOKE ILLUMINATED, NO NW HORN. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121300036 20071213 00036 WP 2007 12 13 DHL2007801520 1 20071108 A 5414 SKIN DOUG DC8 DC873F 302199F WP NR 1 NACELLE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 85401 46033 NR 1 ENG NACELLE INLET COWL UPPER SKIN WORN STA YN 150.000 AT 12 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION. FABRICATED NEW SKIN (AL2024 T3 0.080") AND SPLICE (STEEL TYPE 17-7PH 0.050") IAW SRM 71-5-2 FIG 2 SHEET 1, 2. HEAT TREATED SPLICE FROM 17-7 PH TO H 1050 IAW SRM 51-1-6. CLEANED, TREATED AND PRIMED NEW SKIN IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 71-5-2 FIG 2 SHEET 1, 2, SRM 51-1-21A. 2 L 7 4 4F RT 4A25 2007121300040 20071213 00040 WP 2007 12 13 AALA20072313 1 20071127 A 3350 CONTACT DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 417AA 49328 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 28 TO 30 INOPERATIVE. CLEANED CONTACTS ON BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 28 TO 30. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121300042 20071213 00042 NM 2007 12 13 AALA20072317 1 20071127 A 3350 0201804001 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 391AA 27451 JFK - EMERGENCY LIGHT AT SEAT ROW 37AB MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 37AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007121300050 20071213 00050 WP 2007 12 13 AALA20072327 1 20071129 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISLODGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 432AA 49350 LGA - EMERGENCY LIGHT AT OVERHEAD SEAT 9ABC INOPERATIVE. SECURED BATTERIES IN CHARGER B5 107 FOR EMERGENCY LIGHT AT OVE RHEAD SEAT 9ABC. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121300067 20071213 00067 WP 2007 12 13 IXXA070058O 1 20071206 A 3297 CONNECTOR DOUG DC8 DC873F 302199F WP SQUAT SWITCH DIRTY A IXXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 11 605AL 98397 1839 46106 DURING CLIMB-OUT FROM KTOL, WHEN LEFT AIR CONDITIONER PACK MADE A LOUD BANG, TURNED ON AND MADE EXCESSIVE NOISE WHILE TU RNED ON. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIR CONDITIONER PACK AND FOU ND LEFT GROUND CONTROL RELAY STUCK VIA LEFT SQUAT SWITCH CLEANED ELECTRICAL CONNECTOR AND RESEATED TO LEFT SWITCH. OPER ATIONAL CHECK WAS GOOD IAW DC8 MAINTENANCE MANUAL 21-55-5. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2007121300079 20071213 00079 2007 12 13 DL757071575 4 20071130 A 3454 6225220103 RECEIVER BOEING 757 757232 1384965 NM RT VOR FAILED A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 633DL 23614 CREW REPORTED ELECTRICAL FUMES IN FLIGHT. RIGHT VOR C/B WAS FOUND POPPED AND WOULD NOT RESET. RT VOR RECEIVER WAS FOUN D TO HAVE STRONG ELECTRICAL SMELL AND SIGNS OF FAILURE. 2 L 7 2 4F RT A2NM 2007121300081 20071213 00081 NM 2007 12 13 DL764071580 1 20071201 A 2530 250007390 OVEN BOEING 767 767432ER 1385134 NM GALLEY UNSERVICEABLE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 825MH 29696 FAS REPORTED A SCREECHING SOUND WHEN STARTING FWD NR 1 OVEN. SUBSEQUENT HOT ELECTRICAL SMELL IN FWD GALLEY. FWD OVENS WERE SHUT OFF AND SMELL DISSIPATED. NR 1 OVEN IS BELIEVED TO BE SOURCE OF ODOR. PULLED FWD GALLEY U-33 CIRCUIT BREAKER AS PRECAUTION. RESET U-33 BREAKER FWD TO MCO NR 1 OVEN PER MEL 25-20-01H. NIS HNL - NDS 250007390. W/GALLEY PWR ON, ELECTRICAL SMELL NOTED. REPLACED NR 1 OVEN FWD GALLEY FOR PRECAUTION DUE TO HOT ELECTRIC SMELL AND SCRATCHING SOUND WHE N OVEN WAS TURNED ON OVEN CKS OK. MCO/PLAC REMOVED. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS. 2 L 7 2 4F RT A1NM 2007121300083 20071213 00083 NE 2007 12 13 DL757071585 2 20071204 A 7261 O-RING BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 6714Q 59022 716506 30485 716506 RT ENG OIL QTY0 / FLUX OIL PRESS, ON ARRIVAL FOUND NR 2 ENG MAIN OIL SCREEN O-RING CUT. REPLACED OIL SCREEN AND O-RING, RAN ENG. NO LKS NOTED, OK FOR SVC. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121300084 20071213 00084 NM 2007 12 13 DLM90071587 1 20071204 A 2910 B-NUT DOUG MD90 MD9030 3023690 NM HYD LINE LOOSE A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 906DA 53386 ACFT DECLARED EMERGENCY FOR LOW LEFT SYSTEM HYDRAULIC QTY. TIGHTENED B NUT TO BRAKE ACCUMULATOR. SERVICED HYDRAULIC SY STEM LEAK CHECK OK. 2 L 7 2 4F RT A6WE 2007121300089 20071213 00089 NM 2007 12 13 2007UALA04869 1 20071128 A 2530 3010000801 OVEN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE GALLEY FAULTY A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 776UA 26937 OVEN R-52 WILL NOT TURN OFF. OVEN WAS SMOKING AND C/B WAS PULLED BY CREW PER SAM. POWER SWITCH STAYS IN ALL THE TIME, REPLACED OVEN. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121300095 20071213 00095 WP 2007 12 13 IXXA070059O 1 20071206 A 3231 MECHANISM DOUG DC8 DC871F 302199D WP RT MLG DOOR OUT OF ADJUST A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 829BX 92576 2904 45994 DURING CLIMB-OUT FROM KTOL, MAIN LANDING GEAR DOOR LIGHT STAYED ILLUMINATED. THE CREW CYCLED THE GEAR AND THE LIGHT STA YED ON. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED RIGHT MAIN GEAR DOOR AND ADJUSTED RIGHT GEAR DOOR FOLLOWUP MECHANISM, OPERATIONAL CHECK WAS GOOD IAW DACO DC8 MAINTENANCE MANUAL 32-30-0, AND 32-31-5. A IRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2007121300097 20071213 00097 NM 2007 12 13 07FDEA05012 1 20071207 A 5720 DUCT DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 524FE 48480 RT WING, NR 3 LEADING EDGE SLAT TELESCOPIC DUCT CUTOUT OUTBOARD CORNER FOUND CRACKED. FOUND CRACKED. COMPLIED WITH FED EX EA 1-5710-117087. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007121300099 20071213 00099 EU 2007 12 13 07FDEA05014 1 20071207 A 5753 A57660300002 SKIN AIRBUS 300 A300F4605R 3930327 EU LT WING TE FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 657FE 748 LT WING CENTER FLAP T/E UPPER SKIN 6" UP FROM T/E 3" INBD OF OTBD EDGE 2 EA GOUGES 1ST = .3 X .059 X .010 2ND = .5" X .3" X .013" REPAIRED DAMAGE IAW EA 6-5730-110528 REF PART 1 ITEM 3 REPAIR OF DAMAGE AERAS 1 AND 2 BLENDED AREAS AND CHEC KED FOR CRACKS, NO CRACKS INDICATED. RESTORED TOPCOAT AND ORIGINAL FINISH IAW A300-600 SRM 51-21-10, AND EA 6-5730-1105 28 PART 1 ITEM 3 AND TD FOK/181/2007 REPAIR OF DAMAGE AREAS 1 AND 2. 2 L 7 2 4F RT A35EU 2007121300102 20071213 00102 SO 2007 12 13 CHQA200700087 1 20071204 A 5210 14590091001 SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL PAX DOOR OUT OF TOLERANCE A CHQA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 11 265SK 145226 CAE312169 CLE TO MCI - DURING CLIMB THE MAIN DOOR BEGAN SQUEALING AROUND 14,000 TO 16,000FT. THE AIRCRAFT CONTINUED TO CLIMB TO 3 0,000FT, ACCELERATED TO CRUISE SPEED AND THE DOOR CONTINUED TO SQUEAL. AS A PRECAUTION THE CREW DECIDED TO DIVERT TO ST L WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE DOOR FRAME SEAL BEYOND AMM LIMITS AND HAD TO BE REP LACED. AFTER REPLACING THE SEAL, THE AIRCRAFT WAS PRESSURE TESTED ON THE GROUND AND NO LEAKS WERE NOTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007121300103 20071213 00103 SO 2007 12 13 CHQA200700090 1 20071205 A 3150 WARNING MESSAGE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL BLEED SYS FALSE ACTIVATION A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 572RP 145828 CAE311959 IND TO CVG - DURING CLIMB-OUT OF IND IN ICING CONDITIONS THE CREW RECEIVED A BLEED 1 LEAK EICAS MESSAGE WITH LEAK ILLUMI NATED ON THE ENGINE BLEED VALVE SELECTOR SWITCH. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENAN CE PERFORMED ENGINE RUNS AND COULD NOT DUPLICATE THE BLEED LEAK. ALL THE BLEED DUCTS WERE CHECKED FOR LEAKS AND NONE WE RE FOUND AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007121300106 20071213 00106 WP 2007 12 13 AALA20072358 1 20071201 A 2910 HOSE DOUG DC9 DC982 3022082 WP HYD SYSTEM LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 7514A 49891 RIC INFLIGHT 1180/01DEC - RIGHT LOW HYDRAULIC PRESSURE LIGHT ILLUMINATED. RIGHT HYDRAULIC QUANTITY AND PRESSURE ZERO. LANDED RIC WITHOUT INCIDENT. FOUND HYDRAULIC PRESSURE LINE ON RIGHT WHEEL LOOSE. TIGHTENED RIGHT HYDRAULIC PRESSURE LI NE AND REPLACED HYDRAULIC PUMP AND FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121300109 20071213 00109 WP 2007 12 13 AALA20072364 1 20071203 A 3222 STRUT DOUG DC9 DC983 3022083 WP NOSE GEAR INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 565AA 49347 YYC INFLIGHT T1166/03DEC - NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO YYC AND LANDED WITHOUT INCIDENT. ACC OMPLISHED NOSE STRUT REPAIR AND GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007121300110 20071213 00110 WP 2007 12 13 AALA20072365 1 20071203 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 477AA 49652 LGA - EMERGENCY LIGHTS AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121300112 20071213 00112 NM 2007 12 13 AALA20072368 1 20071204 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 345AN 33084 DFW - EMERGENCY LIGHTS AT SEAT ROWS 5HJ TO 14HJ INOPERATIVE. RESEATED CONNECTOR AT SEAR ROW 11HJ FOR EMERGENCY LIGHTS A T SEAT ROWS 5HJ TO 14HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007121300123 20071213 00123 WP 2007 12 13 AALA20072383 1 20071205 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 450AA 49476 LGA - EMERGENCY LIGHTS AT SEAT ROWS 16AB TO 25AB INOPERATIVE. RESEATED CONNECTOR PLUG AT SEAT ROW 16AB FOR EMERGENCY LI GHTS AT SEAT ROWS 16AB TO 25AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121300144 20071213 00144 NM 2007 12 13 2007UALA04879 1 20071129 A 2750 FLAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU WING STUCK A UALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 29 328UA 24148 RTFL DUE TO STUCK FLAPS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300159 20071213 00159 EU 2007 12 13 YENA2007109 1 20071126 A 2150 10007004 ACM EMB ERJ190 ERJ190100IGW 3260408 EU NR 2 CONTAMINATED A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 178JB 4959 19000004 FLT 1047, JFK-BNA, AT APRX 21:40 PM RETURNED TO JFK, SMOKE/FUMES/HAZE IN CABIN & COCKPIT PASSING 8K FEET, GOT WORSE AS C LIMB CONTINUED. LANDED ASAP. FUMES SEEMED TO CLEAR A BIT DESCENDING THROUGH 2K FEET ON DESCENT. PERFORMED SMOKE/ABNOR MAL SMELL IN PASSENGER, CABIN AND COCKPIT PER AMM 21-20-00-810-801A. NO FAULTS FOUND, NO SMELL PRESENT IN A/C. REPLACE D NR 2 AIR CYCLE MACHINE & TURBINE BYPASS VALVE DUE TO COFFEE CONTAMINATION. OPS CHECK OK. 2 L 7 2 4F RT A57NM 2007121300162 20071213 00162 NM 2007 12 13 KPVA200723 1 20071129 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8103 1386005 NM FALSE ACTIVATION A KPVA K NONE N FALSE WARNING CR CRUISE 1 WP 13 808WP 026 (PIREP) SMOKE WARNING LIGHT ILLUMINATED BRIEFLY INFLIGHT. NO SMOKE DETECTED. PAX IN REAR OF PLANE HAD CELL PHONE ON. (MX) OPS CHECK GOOD. IT WAS DETERMINED CELL PHONE IN BACK SEAT IN FLIGHT WITNESSED BY OFF DUTY WP PILOT. 2 H 7 2 4T RT A13NM 2007121300212 20071213 00212 NM 2007 12 13 SWAA075941 1 20071202 A 5524 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED 8Y CHECK, RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BEARING PER MM. 2 L 7 2 4F RT A16WE 2007121300213 20071213 00213 NM 2007 12 13 SWAA075942 1 20071202 A 5753 65C34812 BOLT BOEING 737 7373H4 1384600 NM FLAP TRACK CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED 8Y CHECK, FOUND RT WING NR 7 FLAP TRACK BOLT CORRODED. REPAIRED FLAP TRACK PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300227 20071213 00227 NM 2007 12 13 SWAA075962 1 20071202 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300235 20071213 00235 2007 12 13 SWAA075936 4 20071202 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 706SW 27840 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007121300244 20071213 00244 NM 2007 12 13 HNAA0700278 1 20071129 A 3260 MS2452333 SWITCH DHAV DHC8 DHC8102 2809003 NM COCKPIT LOOSE A HNAA O OTHER N FALSE WARNING AP APPROACH 1 EA 07 912HA 56027 56027 040 WHEN THE GEAR WAS SELECTED DOWN, THE CREW GOT THREE RED LIGHTS. PERFORMED EMERGENCY EXTENSION AND GOT THREE GREEN LIGHT S. THE LANDING GEAR SELECTOR VALVE WAS REPLACED. ON 1 DECEMBER WHEN THE GEAR WAS SELECTED DOWN, THE CREW GOT THREE RED LIGHTS, AFTER LEVELING OFF, THE GEAR EXTENDED. FOUND RING TERMINAL ON THE LANDING GEAR INHIBIT SWITCH VERY LOOSE. TIG HTENED SCREWS, SWUNG THE GEAR SEVERAL TIMES, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2007121300259 20071213 00259 EA 2007 12 13 COMA0770074 1 20071130 A 5320 CC670341757 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 376CA 10092 THE 280 BULKHEAD AND CROSSBEAM ARE CORRODED. REPAIRED DAMAGE IAW REO 670-53-11-047 AND SRM 51-40-11. 2 L 7 2 4F RT A21EA 2007121300269 20071213 00269 CE 2007 12 13 DXTA200702631 1 20071128 A 3010 WARNING LIGHT BEECH MU300 400A 1155402 CE STAB DE ICE ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 141QS RK498 WHEN HORIZONTAL STAB DE ICE WAS TURNED OFF AFTER CLIMB OUT THE RED STAB ANTI-ICE FAIL LIGHT ILLUMINATED STEADY. EMERGENC Y ACTION TAKEN. CANNOT DUPLICATE SQUAWK. INSPECTED COMPONENTS IN TAIL AND NOSE BAYS. MEASURED SENSOR & HEATER RESISTA NCES. CHILLED LEFT LOADING EDGE WHILE MEASURING RESISTANCE. NO DEFECTS NOTED. RESET CIRCUIT BREAKERS. SYSTEM HAS PAS SED 15 OPERATIONAL TESTS WITHOUT FAULT. NO FURTHER ACTION. 2 H 7 2 4F RT A16SW 2007121300270 20071213 00270 CE 2007 12 13 DXTA200702633 1 20071128 A 2731 LIMIT SWITCH CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE STAB OUT OF ADJUST E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 679QS 5605279 HORIZONTAL STAB MOVED NORMALLY UPON FLAP RETRACTION AFTER TAKEOFF. AT 16000 FT AND LEVEL FLIGHT 280 KNOTS, "STAB MISCOMP ARE" AND "HYD PRESS" ANNUNCIATORS CAME ON. ADJUSTED UP AND DOWN LIMIT SWITCHES IAW 560XL MM CHP. 27-40-00. PERFORMED T/ O WARNING SYS AND HORIZONTAL STAN OPS CHECKS IAW MM CHP 27-40-00. ALL SYSTEMS OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007121300271 20071213 00271 CE 2007 12 13 DXTA200702634 1 20071128 A 2720 PUSHROD CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE RUDDER LOOSE E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 690QS 5605090 RACHETING FEELING IN YOLK WHILE TURNING LT OR RT. MORE NOTICABLE DURING LT TURNS. MUCH MORE NOTICEABLE AT HIGH SPEEDS. OCCASIONALLY FEELS LIKE CONTROLS ARE STICKING WHEN INITIATING A TUR FROM NEUTRAL ON WINGS LEVEL POSITION. FOUND A WON /RUDDER INTERCONNECT PUSHROD TO HAVE EXCESSIVE PLAY. REMOVED AND REPLACED PUSHROD WITH NEW. OPS CK GOOD. I/A/W CE 560 XL MM 27-10-02. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007121300272 20071213 00272 CE 2007 12 13 DXTA200702635 1 20071128 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE UNKNOWN E DXTA O OTHER O OTHER LD LANDING 1 GL 07 331QS 5600331 ON ROLL OUT, F/O LT BRAKE PEDAL WENT TO THE FLOOR. CAPTAIN`S BRAKES WORK NORMALLLY. BLEED LEFT AND RIGHT BRAKES IAW 32- 42-00. OPS CK GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2007121300297 20071213 00297 NM 2007 12 13 SWAA075971 1 20071202 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 409WN 27896 EEPLS END CAP LOOSE AT ROW 1 ABC. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 2007121300299 20071213 00299 2007 12 13 SWAA075973 4 20071203 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 477WN 33988 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007121300305 20071213 00305 NM 2007 12 13 SWAA075994 1 20071203 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300310 20071213 00310 NM 2007 12 13 SWAA075983 1 20071202 A 3350 101114 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 FWD CABIN EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007121300312 20071213 00312 NM 2007 12 13 SWAA075984 1 20071202 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 23R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300314 20071213 00314 NM 2007 12 13 SWAA075986 1 20071202 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 981, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300338 20071213 00338 NM 2007 12 13 2007UALA04850 1 20071127 A 5310 DOOR FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 936UA 26667 FWD CARGO DOOR CUTOUT, AFT FRAME IS CRACKED IN UPPER RADIUS. MAJOR REPAIR: FABRICATED AND INSTALLED EXTERNAL NESTED AN GLES DOUBLER AND TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300350 20071213 00350 NE 2007 12 13 HCM2007F00002 2 20071116 A 7260 CHIP DETECTOR UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ENGINE FAULTY E HCMA O OTHER N FALSE WARNING CR CRUISE 1 WP 13 11QM 3751 23265 APPROX 1 HR AFTER TAKEOFF ON A TOUR FLIGHT, THE ENGINE CHIP LIGHT ILLUMINATED. THE PILOT MADE A PRECAUTIONARY LANDING. UPON INSPECTION BY MAINT, NO METAL WAS FOUND ON THE ENGINE ELECTRICAL CHIP PLUGS OR ON THE ENGINE MAGNETIC PLUGS. SMAL L CARBON DEPOSIT WAS EVIDENT ON FULL FLOW PLUG. C/W GROUND RUNS AND HOVER CHECKS AND AC MAINT FLIGHT PERFORMED. UPON A RRIVAL AT AIRPORT. DURING MAINTENANCE CHECK FLIGHT CHIP LIGHT ILLUMINATED AGAIN. INSPECTION BY MAINTENANCE REVEALED NO METAL CHIPS ON ANY ELECTRICAL PLUGS OR MAGNETIC PLUGS, OIL FILTER INSPECTED AND NO METAL FOUND. FURTHER INVESTIGATION REVEALED FAULTY CHIP DETECTOR WAS THE CAUSE, ELECTRICAL CHIP DETECTOR REPLACED AND NO FURTHER PROBLEMS EVIDENT. (K) 1 G 7 2 3U 3 U H9EU E00054EN 2007121300351 20071213 00351 NM 2007 12 13 2007UALA04886 1 20071129 A 3350 58674 INVERTER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 333UA 24228 EMERGENCY EXIT MARKER INOP AT LEFT OVERWING EXIT. REPLACED INVERTER MODULE, M1581. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300354 20071213 00354 CE 2007 12 13 DXTA200702647 1 20071203 A 2731 INDICATOR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE NOSE TRIM OUT OF ADJUST E DXTA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 07 366QS 5600466 DURING TAKEOFF, AIRCRAFT REQUIRED SIGNIFICANT FOWARD PRESSURE DURING CLIMBOUT. ALL OTHER INDICATIONS WERE NORMAL EXCEP T NOSE TRIM WHEEL INDICATOR WAS BEYOND THE FORWARD WHITE ARC. FOUND TRIM INDICATOR OUT OF ADJUSTMENT. RE-POSITIONED I NDICATOR TO SHOW CORRECT POSITION OF ELEVATOR TABS. OPERATIONAL CHECK AND RIGGING CHECK SATISFACTORY. ALL WORK IAW MM 27-31-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007121300356 20071213 00356 CE 2007 12 13 120207N549CS 1 20071202 A 2910 AE6209H0300130 HOSE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE HYD SYSTEM RUPTURED E Z5FA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 EA 63 549CS 2583 5605546 DURING APPROACH THE HYDRAULIC FLUID LOW LEVEL LIGHT ILLUMINATED FOLLOWED SHORTLY THEREAFTER BY THE HYDRAULIC LOW FLOW LI GHT. THE LANDING GEAR WAS LOWERED, HOWEVER THE FLAPS WOULD ONLY EXTEND TO 15 DEGREES. THE AIRCRAFT MADE AN UNEVENTFUL LA NDING. TROUBLESHOOTING REVEALED A RUPTURED HYDRAULIC PRESSURE HOSE ON THE ENGINE. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007121300357 20071213 00357 CE 2007 12 13 113007N423CS 1 20071130 A 2611 47359717 SMOKE DETECTOR CESSNA 525 525 2076601 CE WILINT FJ44 FJ44 66000 GL CARGO BAY FALSE INDICATION E Z5FA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 63 423CS 964 525B0121 DURING CLIMB AT 15,000 FT, THE BAGGAGE SMOKE LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO HPN AND MADE AN UNEVENTFUL LANDING. THE SYSTEM WAS TROUBLESHOT AND THE PROBLEM COULD NOT BE DUPLICATED. THE AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 2 4F 4 F RT A1WI E3GL 2007121300358 20071213 00358 NM 2007 12 13 2007UALA04889 1 20071129 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 LIGHTNING STRIKE STA 1480 STRINGER 3L. REPLACED BLIND RIVET WITH SOLID RIVET. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121300359 20071213 00359 CE 2007 12 13 DJFA2007138 1 20071202 A 2140 HEATER RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP CABIN SMOKE E DJFA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 733TA 258337 AT FL 400 CREW REPORTED SMOKE AND FUMES IN THE COCKPIT APPROX 3 MINS AFTER ACTIVATING/OPENING FLIGHT DECK HEAT VALVE. SM OKE WENT AWAY AFTER HEAT VALVE WAS CLOSED. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY. DUCTS WERE CHECKED FOR EV IDENCE OF CONTAMINATION BUT NONE WAS FOUND. MAINTENANCE PERFORMED HIGH POWER ENGINE RUNS AND A CHECK FLIGHT WITH NO FUR THER DISCREPANCIES. 2 L 7 2 4F 4 F RT A3EU E6WE 2007121300360 20071213 00360 NM 2007 12 13 2007UALA04890 1 20071129 A 5320 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 LIGHTNING STRIKE STA 418 BETWEEN S7L AND S8L. REPLACED BLIND FASTENER WITH SOLID RIVET. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121300361 20071213 00361 CE 2007 12 13 112707N508CS 1 20071127 A 3233 99124913 ACTUATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE NLG MALFUNCTIONED E Z5FA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 63 508CS 5188 5605294 AFTER TAKEOFF NOSE LANDING GEAR DID NOT RETRACT. CREW ELECTED TO USE EMERGENCY BLOW DOWN. AIRCRAFT RETURNED AND MADE AN UNEVENTFUL LANDING. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007121300362 20071213 00362 NM 2007 12 13 2007UALA04891 1 20071129 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR UNRELIABLE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 579UA 26697 DOOR 2L WILL NOT ARM. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121300363 20071213 00363 EU 2007 12 13 BAQA200700040 1 20071204 A 6320 4649205010 SPACER UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE MAIN GEAR BOX CRACKED B BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 911TS 2980 0167 PILOT REPORTED AT 11 PERCENT TORQUE A VIBRATION WAS FELT AND A CLUNK WAS HERD. INSPECTED MAIN ROTOR SYSTEM. LIFTED MAS T AND FOUND .35 INCHES OF AXIAL PLAY. DISASSEMBLED MAST ASSEMBLY AND FOUND THE SPACER TUBE CRACKED IN (2) PLACES AND TH E KEYS OF THE SPACER TUBE WORN. REPLACED SPACER TUBE, BEARING AND NUT IAW MFG. 1 G 7 2 3U 3 U O H88EU E42NE 2007121300365 20071213 00365 CE 2007 12 13 DXTA200702648 1 20071204 A 3230 ARM CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE BLOWDOWN BOTTLE OUT OF RIG E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 371QS 5600471 AFTER TAKEOFF GEAR WOULDN'T RETRACT. SECURED GEAR AND FOUND BLOW DOWN BOTTLE ARM AND HANDLE/CABLE OUT OF PROPER RIG. RE-RIGGED AND SERVICED BOTTLE. COMPLETED SEVERAL GEAR OPS CHECKS AND GEAR BLOW DOWN. ALL CHECKS GOOD PER CE560 M.M. 3 2-31-08. 2 L 7 2 4F 4 F RT A22CE E25EA 2007121300367 20071213 00367 CE 2007 12 13 DXTA200702649 1 20071204 A 2700 UNKNOWN CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE UNKNOWN E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 580QS 5605741 A LARGE AMOUNT OF FORWARD ELEVATOR TRIM WAS REQUIRED AFTER TAKEOFF. ALSO DURING DESCENT THE TRIM WAS ALL THE WAY FORWARD AGAINST THE STOP. INSPECTED SYSTEM. FOUND HARDWARE FOR ELEV TRIM CONTROL WHEEL BACKED 3/4 OF THE WAY OUT, ALLOWING EL EV TRIM INDICATOR DRIVE TO JUMP OF OUT GROOVE IN CONTROL WHEEL. PROPERLY INSTALLED TRIM IND DRIVE AND CONTROL WHEEL ASS Y AS REQUIRED. OPS CHECK GOOD. IAW MM 27-32-01. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007121300368 20071213 00368 2007 12 13 DXTA200702650 4 20071204 A 3197 CONNECTOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE DAMAGED E DXTA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 07 608QS 5605308 AT FL350 RED CABIN ALT LIGHT ILLUMINATED. VERIFIED CABIN WAS AT 10000 FT, INITIATED EMER DESCENT. TROUBLESHOT ELECTRI CAL AND FOUND AND CORRECTED WIRING AT PIN "A" OF CONNECTOR PC042 AND PC003 OPS CHECKS GOOD IAW MM 21-30-00 AND SB560XL-2 1-19 (AS REFERENCE) OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007121300369 20071213 00369 CE 2007 12 13 DXTA200702651 1 20071204 A 5597 WIRE BEECH MU300 400A 1155402 CE HORIZONTAL STAB DAMAGED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 153QS RK490 H-STAB FAIL ANNUNCIATOR LIGHT ILLUMINATED IN FLIGHT. TROUBLESHOT SYSTEM FOUND TOO LARGE OF AN OHM SPLIT AT C/P 473 OF CONTROLLER, TRACED WIRING BACK TO TB061 STILL HAD LARGE SPLIT OHM DIFFERENCE. REMOVED LT STAB LEADING EDGE, REPAIRED CON NECTIONS AT TB060 AND OHMED FROM C/P 473 NOW 198.4 ON BOTH SENSE WIRES AT 67.5 DEGREES. REINSTALLED LT STAB LEADING EDGE AND VERTICAL STAB KNEE CAP PANEL. OPERATED SYSTEM SEVERAL TIMES. OPERATES NORMAL. ALL WORK DONE PER 400XP MM 30-12-00 2 H 7 2 4F RT A16SW 2007121300370 20071213 00370 EU 2007 12 13 12052007 1 20071204 A 5302 1173025451 FRAME BOLKMS BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101750B1 41560 NE TAILBOOM CRACKED E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 217MC 11112 7195 7195 DURING A SCHEDULED INSPECTION , A CRACK WAS DISCOVERED ON THE RT SIDE OF TAILBOOM FRAME 10L. THE CRACK EXTENDS FROM THE CENTER OPENING OF FRAME 10L TO THE OMEGA CUTOUT AT THE RT OUTER EDGE OF FRAME 10L. 1 G 7 2 3U 3 U NC H13EU E5NE10 2007121300371 20071213 00371 CE 2007 12 13 AMWA1019019 1 20071108 A 5711 11412004465 SPAR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE WING CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 155ZV 22879 165 UE155 DURING DETAIL INSPECTION, RT AFT SPAR FLANGE AT WS117.5 WAS FOUND TO BE CRACKED FROM RIVET TO EDGE OF FLANGE. MAINTENANC E OBTAINED APPROVED DATA, PERFORMED REPAIR AND CLEARED DISCREPANCY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007121300373 20071213 00373 CE 2007 12 13 AMWA88803BC 1 20071127 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER DISCHARGED A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 127ZV 14152 126 UE127 BATTERY CHARGE ANNUNCIATOR ILLUMINATED FOR A SHORT TIME. MAINTENANCE REPLACED BATTERY AND CLEARED DISCREPANCY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007121300374 20071213 00374 CE 2007 12 13 AMWA88820BC 1 20071128 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER DISCHARGED A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 162ZV 2037 76 UE162 DURING FLIGHT THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED. MAINTENANCE CHARGED BATTERY AND CLEARED DISCREPANCY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007121300375 20071213 00375 SO 2007 12 13 GUUA12030701 1 20071203 A 3350 1317 LAMP EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE EMERGENCY LIGHTS INOPERATIVE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 261AS 120141 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT AFT EMERGENCY LIGHT INOPERATIVE. REPLACED RT AFT EMERGENCY LIGHT. 2 L 7 2 4T 4 T RT A31SO E20NE 2007121300377 20071213 00377 CE 2007 12 13 ACE120407 1 20071204 A 3245 G195X6758 TUBE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA NLG TIRE FAILED E YADA O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 AL 03 113AX 58 UC41 PILOT STOPPED AIRCRAFT ON TAXIWAY DUE VIBRATION FROM NOSE TIRE. MAINTENANCE REPLACED FLAT TIRE. INSPECTION OF TIRE AND TUBE IDENTIFIED A NAIL IN TIRE (UNDETERMINED IF THIS WAS CAUSE OF FAILURE) ADDITIONAL INSPECTION OF TUBE INDICATED POS SIBLE PROBLEM WITH TUBE CONSTRUCTION IN THAT TUBE SHOWS INDICATION OF FAULTY MATERIAL (TUBE TEARS EASILY BY HAND) AND WA LL THICKNESS ABOUT HALF OF THAT OF A DIFFERENT TUBE OF THE SAME MFG (AND ABOUT HALF THE WEIGHT). THIS WAS THE LATEST OF A RECENT STRING OF FLAT TIRES FOR UNDETERMINED REASONS. MANUFACTURER NOTIFIED OF FINDINGS. QUESTIONABLE TUBE INDICATE D FABRICATION IN EUROPE (HEAVIER TUBE CONSTRUCTED IN CANADA). 2 L 7 2 4T 4 T RT A24CE E4EA 2007121300379 20071213 00379 NM 2007 12 13 2007UALA04895 1 20071129 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 663UA 27160 RIGHT FUSELAGE EVACUATION (EMERGENCY) LIGHT LOOSE STA 1230, STR 23R. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121300381 20071213 00381 NM 2007 12 13 2007UALA04897 1 20071203 A 3350 RETAINER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 833UA 1401 FORWARD ENTRY DOOR EXIT LIGHT PANEL, AT FLOOR LEVEL, INNER RETAINERS DAMAGED. REPLACED THREE RETAINERS ON DOOR EXIT LIG HT PANEL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121300383 20071213 00383 EU 2007 12 13 2007UALA04899 1 20071202 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 481UA 1559 CORROSION ON L2 DOOR SILL FR 66. PERFORMED A MAJOR REPAIR AFTER BLENDING BROUGHT AREA OUT OF LIMITS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121300385 20071213 00385 NM 2007 12 13 2007UALA04902 1 20071202 A 5610 WINDSHIELD BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT CRACKED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 366UA 24535 RTFL- CAPTS WINDSHIELD CRACKED ON CLIMBOUT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300388 20071213 00388 NM 2007 12 13 2007UALA04906 1 20071201 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 FUSELAGE FORWARD ENTRY DOOR CUTOUT LOWER HINGE CUTOUT BEAR STRAP HAS CRACK OUT OF FASTENER HOLES ABOVE & BELOW GUIDE PLA TES. MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED EXTERNAL FUSELAGE SKIN DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300389 20071213 00389 2007 12 13 2007UALA04907 4 20071201 A 3160 DISPLAY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT FAILED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 548UA 25396 RTFL DUE TO A FAILED COMPUTER DISPLAY UNIT. HAD TO RESOLDER SEVERAL JOINTS AND A5 CARD WAS REPLACED DUE TO A BURNT CARD . REPLACED CAPT CDU 2 L 7 2 4F 4 F RT A2NM E17NE 2007121300390 20071213 00390 NM 2007 12 13 2007UALA04908 1 20071201 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 FWD GALLEY DOOR CUTOUT, LWR AFT CORNER IS CRACKED. MAJOR REPAIR; REMOVED DAMAGE, FABRICATED AND INSTALLED EXTERNAL FUSE LAGE SKIN DOUBLER-TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300394 20071213 00394 NM 2007 12 13 2007UALA04913 1 20071130 A 3350 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 313UA 23674 EXTERIOR EMERGENCY LIGHT OUT AT RT EMERGENCY EXIT DOOR. FOUND LAMP BURNED OUT. RELAMPED FIXTURE, TESTED OK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300395 20071213 00395 NM 2007 12 13 2007UALA04914 1 20071201 A 3350 1317 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT DEFECTIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 COCKPIT EMERGENCY DOME LIGHT EXTREMELY DIM AND FLICKERING. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300396 20071213 00396 NM 2007 12 13 2007UALA04916 1 20071201 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 DOOR 4L EMERGENCY SILL LIGHT FWD INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121300397 20071213 00397 NM 2007 12 13 2007UALA04917 1 20071201 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY CEILING LIGHTS FROM ROW 35 TO 44 LT & RT ARE INOP. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121300399 20071213 00399 NM 2007 12 13 2007UALA04919 1 20071201 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 UPPER DECK EMERGENCY LIGHT ABOVE ROW 17 INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121300400 20071213 00400 NM 2007 12 13 2007UALA04920 1 20071202 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EXIT LIGHT INOP AT UPPER DECK CEILING AT TOP OF STAIRS. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121300401 20071213 00401 NM 2007 12 13 2007UALA04921 1 20071202 A 3350 9F19948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EXIT EEL LIGHT INOP JUST FWD OF LAV 104 BELOW COAT CLOSET. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121400002 20071214 00002 NM 2007 12 14 HALA0700523 1 20071209 A 7714 889313 PROBE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE N2 SHAFT SPEED MALFUNCTIONED A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 479HA 55124 BTB - ENG L SYS FAIL SW TAXI OUT ALERT. INTERROGATED MCDU PER FIM TASK 77-12-00-810-802. REMOVED AND REPLACED N2 SHAFT SPEED HPC PROBE. OPS AND LEAK CHECK OK. OK FOR SERVICE. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007121400003 20071214 00003 NE 2007 12 14 HALA0700521 2 20071209 A 7320 112E9321G2 EEC BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE LT ENGINE FAULTED A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 479HA 55124 ENG L SYS FAIL DISPLAYED. FOUND 10P BOX FAULT ON EEC FAULT REVIEW AND CURRENT FAULT REMOVED AND REPLACED 10P PER MM 73- 21-11, COND SAME. REMOVED AND REPLACED NR 1 EEC ASSY PER AMM 73-21-01. NO FAIL NOTED ON ENG RUN. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007121400004 20071214 00004 EA 2007 12 14 DATA200700009 2 20071117 A 7320 3033265 LINE STBROS SD3 SD360200 8100607 EU PWA PT6 PT6A65R 52043 EA ENGINE BROKEN E DATA K NONE R PARTIAL RPM/PWR LOSS LD LANDING 1 GL 13 601A SH3623 PCE97170 WITH ABOUT 500' TO TOUCHDOWN THE LEFT ENGINE WENT INTO FEATHER (NO INDICATION ON CWP). ALL ENGINE INSTRUMENTS WERE NORM AL EXCEPT TORQUE AT 0 LBS. TORQUE WAS SET BETWEEN 500-1000 LBS. UPON TOUCHDOWN, LEFT ENGINE CAME OFF FEATHER AND RETU RNED TO NORMAL. AFTER EXITING THE RUNWAY, PILOT NOTICED OIL PRESSURE DROPPING. AS THE PILOT SHUTDOWN THE LEFT ENGINE O N THE TAXIWAY THE "OIL L" ANNUNCIATOR LIGHT INDICATED ON THE CWP. 2 H 7 2 4T 4 T RT A41EU E4EA 2007121400005 20071214 00005 NE 2007 12 14 DATA200700010 2 20071127 A 7320 3033265 LINE STBROS SD3 SD360300 8100610 EU PWA PT6 PT6A67A 52043 NE ENGINE BROKEN E DATA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 13 136LR SH3752 PCE106075 ENGINE FAILED APPROX 15 MILES SSW OF NEW HOPE VA. LEFT ENGINE INSTRUMENTS DECREASING. INFORMED FO TO CONFIRM LEFT ENGI NE FAILURE. COMPLETED PROCEDURE ACCORDING TO ACC SOP. DECLARED EMERGENCY AND ADVISED ATC. CLEARED TO LAND ON ILS 35L. LANDED SAFELY NO FIRE ASSOCIATED WITH FAILURE. 2 H 7 2 4T 4 T RT A41EU E26NE 2007121400006 20071214 00006 NM 2007 12 14 2007UALA04922 1 20071202 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EXIT EEL LIGHT INOP AT ROW 61 LT. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121400007 20071214 00007 NM 2007 12 14 2007UALA04923 1 20071130 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 528UA 25018 EEL LIGHT INOP AT MID LAV THRESHOLD. FOUND EEL LIGHT ASSY DAMAGED. REPLACED EEL LIGHT ASSY AT MID LAV THRESHOLD. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121400012 20071214 00012 NM 2007 12 14 CALA0700729 1 20071205 A 5320 AND101362402 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 CABIN FWD ENTRY FLOOR SUPPORT STA 294.5 AND RBL 31.5 PREVIOUS REPAIR STRAP HAS CORROSION UNDER, AROUND NUT PLATE HOLE. INSTALLED SECT "T" CHORD AND REINSTALLED STRAP PER SRM 53-10-51. 2 L 7 2 4F RT A16WE 2007121400013 20071214 00013 EA 2007 12 14 COMA0760674 1 20071129 A 2131 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA CABIN PRESSURE MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 956CA 7105 FLIGHT 4953 - A/C WILL NOT PRESSURIZE IN FLIGHT. TRIED BOTH CONTROLLERS AND MANUAL MODE WITH NO AFFECT. A/C RETURNED T O DTW AND LANDED SAFELY. TRANSFERRED TO DEFERRED LIST PER MEL 21-31-01-2. 2 L 7 2 4F RT A21EA 2007121400015 20071214 00015 NM 2007 12 14 HALA0700518 1 20071208 A 3610 79275516 CONTROLLER BOEING 767 7673CB 1385187 NM PWA 4060 PW4060 52119 NE PRV MALFUNCTIONED A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 590HA 33467 ETOPS SIGNIFICANT SYSTEM, BTB R ENG PRV STATUS MESSAGE AFTER RIGHT ENGINE STARTED. REPLACED PRV CONTROLLER PER M/M 36-1 1-19. REPLACED PRV VALVE PER M/M 36-11-18. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121400016 20071214 00016 EA 2007 12 14 COMA0760676 1 20071129 A 2752 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 408CA 7440 FLIGHT 5526 - RECEIVED FLAP FAIL CAUTION MESSAGE AFTER LANDING. PERFORMED EO 27-046 AD, INCLUDING FLEX DRIVE REJUVE. N O FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007121400017 20071214 00017 EA 2007 12 14 COMA0760677 1 20071129 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 446CA 7546 FLIGHT 5449 - FLAPS DEGRADED STATUS MESSAGE, FOLLOWED BY FLAPS FAIL CAUTION MESSAGE. FLAPS FAILED AT 0 DEGREES. COMPLI ED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYST EM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2007121400019 20071214 00019 NM 2007 12 14 KCSA071529 1 20071205 A 5311 FRAME BOEING 747 747259B 1384804 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 DAMAGED STRUCTURE BEHIND LT COUNTER BALANCE WHEEL FOR FLIGHT DECK STAIRS AT STA 460 TO 480, WL 305, LBL 35. 2 L 7 4 4F RT A20WE 2007121400024 20071214 00024 NM 2007 12 14 SWAA075996 1 20071204 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 235WN 34630 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007121400025 20071214 00025 2007 12 14 SWAA075997 4 20071204 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007121400028 20071214 00028 NM 2007 12 14 SWAA076011 1 20071204 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 390, RBL 1.5. REPAIRED SKI N PER EA. 2 L 7 2 4F RT A16WE 2007121400029 20071214 00029 2007 12 14 SWAA076000 4 20071204 A 2565 63562101 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 423WN 29827 R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007121400030 20071214 00030 NM 2007 12 14 SWAA076001 1 20071204 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 464WN 32468 EEPLS END CAP LOOSE AT ROW 1 ABC. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 2007121400031 20071214 00031 2007 12 14 SWAA076002 4 20071204 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 477WN 33988 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007121400032 20071214 00032 NM 2007 12 14 SWAA076003 1 20071204 A 3350 1619 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 495WN 33869 DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007121400033 20071214 00033 NM 2007 12 14 SWAA076015 1 20071204 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007121400035 20071214 00035 NM 2007 12 14 SWAA076013 1 20071204 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121400036 20071214 00036 NM 2007 12 14 SWAA076012 1 20071204 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121400037 20071214 00037 NM 2007 12 14 SWAA076004 1 20071204 A 5514 6549863 FITTING BOEING 737 7373H4 1384600 NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED BRDG CHECK, FOUND RT HORIZONTAL STABILIZER NR 6 HINGE FITTING CORRODED. REPAIRED FITTING PER ER. 2 L 7 2 4F RT A16WE 2007121400040 20071214 00040 NM 2007 12 14 SWAA076007 1 20071204 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 792, STR 19L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007121400041 20071214 00041 NM 2007 12 14 SWAA076008 1 20071204 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 723SW 27855 DURING SCHEDULED MV2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 DEF. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007121400043 20071214 00043 NM 2007 12 14 SWAA076010 1 20071204 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 762SW 27876 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007121400044 20071214 00044 EA 2007 12 14 COMA0760681 1 20071130 A 2752 1104SD100201 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP LEAKING A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 735CA 7267 FLIGHT 5394 - RECEIVED FLAP FAIL MESSAGE ON TAXI IN. REPLACED NR 2 FLAP FLEX SHAFT ON LEFT SIDE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007121400046 20071214 00046 NM 2007 12 14 HALA0700519 1 20071209 A 2697 CONNECTOR BOEING 767 7673G5 1385126 NM APU FIRE LOOP DIRTY A HALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 13 585HA 24257 BTB - APU FIRE LP 2 STATUS MESSAGE ILLUMINATED. CLEANED CONNECTORS FOR LOOP 2 ON APU. FIRE LOOP TEST OK FOR APU. WDM 26-15-11 AND FIM 26-15-00. 2 L 7 2 4F RT A1NM 2007121400048 20071214 00048 NM 2007 12 14 HALA0700520 1 20071208 A 3080 0087000200002 DETECTOR BOEING 717 717200 1383700 NM ICE DETECTION FAILED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 478HA 55123 WING ICE R FAIL ALERT. REMOVED AND REPLACED RT WING ICE DETECTOR PER AMM 30-81-02 RTS NO FAULTS NOTED, OK FOR SERVICE M IC SHEET CLEARED. 2 L 7 2 4F TR A6WE 2007121400049 20071214 00049 SO 2007 12 14 SIMA200734102 1 20071130 A 3230 CONTROL UNIT EMB 135 EMB135KL 3260302 SO NLG MALFUNCTIONED A SIMA O OTHER J WARNING INDICATION LD LANDING 1 SW 21 837AE 145647 DISC-LND AIR/GND FAIL MESSAGE ON EICAS DURING GEAR EXTENSION. REMOVED AND REPLACED LGEU IAW EMB 140 AMM 32-21-01. RESE CURED CONNECTOR ON LEFT MLG DOWN LOCK FWD PROX SWITCH 32-61-02. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007121400050 20071214 00050 GL 2007 12 14 SIMA200734101 2 20071204 A 7200 AE3007A1 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 SMOKE A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 619AE 145101 RETURN TO GATE DUE TO SMOKE IN COCKPIT. REMOVED AND REPLACED NR 1 ENG IAW W/C 71-000-00. OPS CHECKS, LEAK CHECK GOOD. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007121400052 20071214 00052 SO 2007 12 14 C2XA07SH097 1 20071205 A 5730 14540329009 PLATE EMB 145 EMB145XR 3260214 SO FAIRING CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17115 145666 SHV - DURING C-CHECK 191 WING TO FUSELAGE FAIRING HAS CORRODED BONDING PLATE ON LOWER TRAILING EDGE. MAINTENANCE REPAIR ED 191 PNL LOWER TRAILING EDGE BONDING PLATE IAW EC5750-01315 REV-E. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2007121400053 20071214 00053 SO 2007 12 14 C2XA07SH098 1 20071205 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17115 145666 SHV - DURING C-CHECK LEFT OMEGA BEAM HAS CORROSION BETWEEN FR 19-21. MAINTENANCE REPAIRED LEFT OMEGA BEAM BETWEEN FRS 1 9-21 IAW EC 5320-01229. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2007121400054 20071214 00054 SO 2007 12 14 C2XA07SH099 1 20071205 A 5310 14525480003 BEAM EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17115 145666 SHV - DURING C-CHECK BAGGAGE DOOR CUTOUT LOWER CENTER BEAM HAS CORROSION. MAINTENANCE REMOVED AND REPLACED LOWER BEAM F OR BAGGAGE DOOR CUTOUT IAW EMB 145 SRM 51-40-02. INSTALLED NUT PLATES IAW EC 5320-01137. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2007121400056 20071214 00056 SO 2007 12 14 C2XA07SH100 1 20071205 A 3213 23092029001 AXLE EMB 145 EMB145XR 3260214 SO LT MLG CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17115 145666 SHV - DURING C-CHECK LT MLG STRUT LOWER ATTACH AXLE CORRODED. MAINTENANCE REMOVED AND REPLACED LT MLG STRUT LOWER ATTAC H AXLE IAW EMB 145XR AMM 32-10-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2007121400057 20071214 00057 SO 2007 12 14 C2XA07SH102 1 20071205 A 5751 14569009410SD ATTACH FITTING EMB 145 EMB145XR 3260214 SO RT AILERON DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17115 145666 SHV - DURING C-CHECK RIGHT AILERON PCA HAS PLAY WHEN HYD ARE PRESSURIZED. MAINTENANCE REMOVED AND REPLACED RIGHT AILERO N PCA FITTING AND PAINTED IAW EC5750-01179. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2007121400061 20071214 00061 WP 2007 12 14 ABXR070392 1 20071002 A 5320 39164112 ANGLE DOUG DC9 DC915 3022036 WP RT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 784TW 47014 ANGLE CRACKED AT INBOARD END OF SLANT PANEL. REMOVED AND REPLACED INBOARD END OF SLANT PANEL IAW DC9 SRM. 2 L 7 2 4F A6WE 2007121400063 20071214 00063 WP 2007 12 14 ABXR070393 1 20071003 A 5320 99579123 INTERCOSTAL DOUG DC9 DC915 3022036 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 784TW 47014 STA 389, LONGERON 29 LEFT, INTERCOSTAL CRACKED AT UPPER RADIUS. REMOVED AND REPLACED INTERCOSTAL AT LONGERON 29 LEFT, S TA 370 - 389 IAW DC9 SRM 51-10-3. 2 L 7 2 4F A6WE 2007121400065 20071214 00065 SO 2007 12 14 SIMA200734402 1 20071209 A 3600 4800112 BUTTON EMB 145 EMB145LR 3260212 SO BLEED SYS FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 900AE 14500885 EMERGENCY DECLARED, RIGHT AFTER TAKEOFF AT ABOUT 2000 FEET WING AND STAB FAIL CAUTION CAME ON FOLLOWED BY ICE CONDITION A/I INOP WARNING ON EICAS. RETURNED FOR LANDING AT ORD. VISUALLY INSPECTED PRESSURE SWITCH MANIFOLD, WING ANTI ICE VAL VES, AND SENSE LINES AT WING TO FUSE FAIRING FOR SECURITY AND ABNORMALITIES. NO DEFECTS NOTED. REMOVED AND REPLACED BO TH ENGINE BLEED PUSHBUTTONS IAW EMB 145 20-13-04. OPS CHECK NUMEROUS TIMES IAW EMB 145 30-00-00. OPS CHECK GOOD, NO DE FECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007121400067 20071214 00067 WP 2007 12 14 ABXR070394 1 20071004 A 5312 5910130363 BULKHEAD DOUG DC9 DC915 3022036 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 784TW 47014 AFT PRESSURE BULKHEAD LEFT VENTRAL DOOR CORNER (FORWARD SIDE) WAS CRACKED IN THE RADIUS OF THE FORWARD MOST FORMED SECTI ON. REPAIRED CRACK IAW DC9 SSRM DWG K05159. 2 L 7 2 4F A6WE 2007121400068 20071214 00068 EU 2007 12 14 SIMA200734401 1 20071206 A 7930 1PTR119100007 SENSOR SAAB SF340 340B 7860101 EU PROP OIL PRESS FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 384AE 340B384 RIGHT PROP PSI INDICATIONS PEGGED IN RED. FLUCTUATES WHEN IN FEATHER. OTHER ENGINE INDICATIONS NORMAL. REMOVED AND RE PLACED RIGHT PROP OIL PRESSURE SENSOR ON THE PGB IAW SAAB 340B AMM 79-30-05. OPS CHK GOOD. OIL PRESSURE SENSOR. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007121400069 20071214 00069 WP 2007 12 14 ABXR070395 1 20071005 A 5544 5912103501 HINGE BRACKET DOUG DC9 DC915 3022036 WP RUDDER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 784TW 47014 UPPER RUDDER HINGE BRACKET CRACKED RIGHT SIDE. REMOVED AND REPLACED BRACKET IAW DC9 MM 27-20-1 AND DAC DWG 5910254. 2 L 7 2 4F A6WE 2007121400070 20071214 00070 WP 2007 12 14 ABXR070396 1 20071005 A 5320 99574472 PANEL DOUG DC9 DC915 3022036 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 784TW 47014 RIGHT TRAP PANEL CRACKED AT AFT ATTACH HOLES NR 1 AND 2. REPAIRED TRAP PANEL WITH REPAIR ANGLE IAW DC9 SRM 51-09. 2 L 7 2 4F A6WE 2007121400072 20071214 00072 WP 2007 12 14 ABXR070398 1 20071005 A 5311 99118589 FRAME DOUG DC9 DC915 3022036 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 784TW 47014 FRAME CRACKED AT STA 897, LONGERON 12 RIGHT. REPAIRED FRAME AT STA 897, LONGERON 12 RIGHT IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 2007121400075 20071214 00075 NM 2007 12 14 MWEA070300 1 20071205 A 3350 6011779 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 923ME 55185 OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE ON EXTERIOR. REPLACED BATTERY PACK. 2 L 7 2 4F TR A6WE 2007121400078 20071214 00078 EU 2007 12 14 YENA2007112 1 20071206 A 2782 1703911 ACTUATOR EMB ERJ190 ERJ190100IGW 3260408 EU L/E SLAT MALFUNCTIONED A YENA B EMER. DESCENT F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 EA 15 228JB 4450 19000030 FLIGHT 1264, AUS-BOS, SLAT FAIL EICAS MESSAGE ON APPROACH TO BOSTON. FOUND NR 3, 6 AND 8 SLAT ACTUATORS ON LEFT WING WI TH TRIPPED TORQUE LIMITERS. REPLACED NR 3 AND 8 ACTUATORS PER 27-81-01. RESET NR 6 ACTUATOR, RAN SLAT SEVERAL TIMES, C HECK NORMAL PER 27-81-01. INSP CK ALL RIGGING, ELECTRIC CHECKS AND OPS CHECK NORMAL. 2 L 7 2 4F RT A57NM 2007121400080 20071214 00080 WP 2007 12 14 FX7A200700006 1 20071106 A 4920 3812761 APU DOUG DC9 DC982 3022082 WP SHUTDOWN A FX7A K NONE O OTHER DE DESCENT 1 SO 19 905TA 49905 APU SHUT DOWN AT TOP OF DESCENT. 2 L 7 2 4F A6WE 2007121300098 20071213 00098 NM 2007 12 13 07FDEA05013 1 20071207 A 5310 STRUCTURE DOUG MD11 MD11F 3023600 NM BS 1741 L12L CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 524FE 48480 MAIN DECK CARGO, LEFT SIDEWALL STRUCTURE FRAME AT STA 1741 LONGERON 12L FOUND CRACKED. REPAIRED AS PER SRM 53-30-00 F IGURE 1 VOLUME I. DUE TO CATEGORY B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES AND REPETITIVE INSPECTIONS EVER Y 9,500 CYCLES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007121300107 20071213 00107 NM 2007 12 13 AALA20072359 1 20071202 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 784AN 29588 NRT - EMERGENCY LIGHT AT FIRST CLASS CLOSET LENS BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FIRST CLASS CLO SET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121300111 20071213 00111 EU 2007 12 13 AALA20072366 1 20071203 A 3260 DSB11021 SENSOR AIRBUS 300 A300B4605R 3930308 EU MLG INOPERATIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 14056 463 JFK INFLIGHT T635/03DEC - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. R EPLACED RIGHT STRUT SENSORS 64GB AND 62GB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121300122 20071213 00122 EU 2007 12 13 AALA20072372 1 20071204 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70074 517 MIA - EMERGENCY LIGHTS AT SEAT ROWS 30G TO 37G INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 30G TO 37G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121300125 20071213 00125 NM 2007 12 13 AALA20072374 1 20071204 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 902AN 29504 DFW - EMERGENCY LIGHT AT SEAT 7D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT A16WE 2007121300126 20071213 00126 NM 2007 12 13 AALA20072375 1 20071204 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 902AN 29504 DFW - EMERGENCY LIGHT AT FORWARD EXIT OVERWING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT FORWARD EXIT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007121300132 20071213 00132 WP 2007 12 13 AALA20072388 1 20071206 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 492AA 49730 LGA - EMERGENCY LIGHTS AT FORWARD EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121300157 20071213 00157 NM 2007 12 13 CALA0700725 1 20071202 A 5330 65C35794 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 L2 DOOR CUTOUT CRACKED AT LOWER HINGE LWR AREA. REPAIRED AND INSTALLED PER ECRA 5331-01364. 2 L 7 2 4F RT A16WE 2007121300163 20071213 00163 WP 2007 12 13 ASAA0782296 1 20071201 A 5230 59101413 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 961AS 53075 RAMP REPORTS DENT IN AFT CARGO DOOR EXTERIOR SKIN JUST BELOW THE HANDLE CUTOUT. DAMAGED AREA OF SKIN FABRICATED REPAIR DOUBLERS AND INSTALLED IAW ASA EA 5230 01392. 2 L 7 2 4F RT A6WE 2007121300164 20071213 00164 WP 2007 12 13 ASAA0782290 1 20071129 A 5311 591359581 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 961AS 53075 FUSELAGE FRAME STA 1418 FROM LONGERON 5L TO 5R FAILSAFE CHORD IS CRACKED. REMOVED CRACKED CHORD RECEIVED DRILLED AND IN STALLED NEW CHORD IAW MD80 SRM 51-10-4, 51-30-5. 2 L 7 2 4F RT A6WE 2007121300178 20071213 00178 NM 2007 12 13 SCNA07013 1 20071202 A 3350 BATTERY PACK BOEING 737 7378Q8 13844BX NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 801SY 30332 MAINTENANCE FOUND THE L1 DOOR EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE THEN REPLACED THE EMERGENCY LIGHT BATTERY PACK. 2 L 7 2 4F RT A16WE 2007121300206 20071213 00206 NM 2007 12 13 SWAA075929 1 20071202 A 5755 6573735 SPOILER BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 2 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007121300211 20071213 00211 NM 2007 12 13 SWAA075940 1 20071202 A 5524 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED 8Y CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BEARING PER MM. 2 L 7 2 4F RT A16WE 2007121300219 20071213 00219 NM 2007 12 13 SWAA075933 1 20071130 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 411WN 29821 DURING SCHEDULED HC2 CHECK, FOUND EEPLS LIGHT LENS CRACKED AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007121300222 20071213 00222 NM 2007 12 13 SWAA075947 1 20071202 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CRACKED AT BS 500C, STR 8R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007121300232 20071213 00232 NM 2007 12 13 SWAA075953 1 20071128 A 5312 6546568 BULKHEAD BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED MV2 CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6L. REPAIRED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300253 20071213 00253 SO 2007 12 13 C2XA07SH096 1 20071129 A 2910 AE71379016 HYDRAULIC LINE EMB 145 EMB145 3260210 SO HYDRAULIC SYS RUPTURED A C2XA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 27 14930 011 SHV - FLT 2395, DURING CLIMB AND UPON MOVING THE LANDING GEAR SELECTOR TO RETRACT THE CREW OBSERVED A HYDRAULIC SYSTEM 1 ADVISORY. THE CREW MOVED THE LANDING GEAR SELECTOR BACK TO EXTEND AND PERFORMED THE ABNORMAL INDICATION PROCEDURES. T HE AIRCRAFT MADE AN UNEVENTFUL LANDING BACK TO JAN. UPON INSPECTION MAINTENANCE FOUND A RUPTURED HYDRAULIC PRESSURE LIN E. MAINTENANCE REMOVED AND REPLACED THE PRESSURE LINE; AS A PRECAUTIONARY REMOVED AND REPLACED THE NR 1 ENGINE HYDRAULI C PUMP IAW EMB 145 AMM 29-10-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2007121300254 20071213 00254 CE 2007 12 13 420CT010 1 20071127 A 2160 1325501301 SENSOR BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE COCKPIT CONTAMINATED E T17A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 17 420CT 359 RK517 DURING CLIMB NOTICED COCKPIT VERY WARM TO HOT. BETWEEN 12000' AND 18000' IT APPEARED A THIN LAYER OF SMOKE WAS PRESENT IN THE COCKPIT. ABOUT 30 SECONDS LATER THE FIRST OFFICER VERIFIED THERE WAS SMOKE IN THE COCKPIT AND THICKER. EMERGENC Y DESCENT AND LANDING AT DEPARTURE POINT. FOUND EXCESSIVE AMOUNTS OF CARPET FIBERS TRAPPED IN FAN ON TEMPERATURE SENSIN G UNIT FOR COCKPIT. CLEANED FAN, OPERATION CHECKED GOOD. 2 H 7 2 4F 4 F RT A16SW E25EA 2007121300255 20071213 00255 NM 2007 12 13 ZZDA2007305 1 20071203 A 2910 HYDRAULIC SYSTEM BOEING 717 717200 1383700 NM RIGHT LOW A ZZDA O OTHER O OTHER AP APPROACH 1 SO 37 952AT 55014 RIGHT HYDRAULIC QUANTITY LOW. SERVICED RIGHT HYD SYSTEM TO FULL, BLEED HYD SYSTEM AND INSPECTED A/C FOR HYD LEAKS. NO LEAKS NOTED IAW B-717 AMM 12-13-01, A/C OK FOR SERVICE. 2 L 7 2 4F TR A6WE 2007121300262 20071213 00262 EA 2007 12 13 COMA0770071 1 20071130 A 5414 COWL DOOR CNDAIR CL600 CL6002C10 1390015 EA RT ENGINE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 376CA 10092 RIGHT ENGINE LOWER FAN COWL DOOR I/B AFT CORNER IS DAMAGED. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 54-14-00 AN D 51-14-00. 2 L 7 2 4F RT A21EA 2007121300279 20071213 00279 NM 2007 12 13 SWAA075966 1 20071203 A 3350 MS155721 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 235WN 34630 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007121300286 20071213 00286 NM 2007 12 13 SWAA075993 1 20071203 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 500A, STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007121300301 20071213 00301 NM 2007 12 13 SWAA075974 1 20071202 A 3350 20131A BATTERY PACK BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK AND CHARG ER PER MM. 2 L 7 2 4F RT A16WE 2007121300328 20071213 00328 NM 2007 12 13 DXTA200702645 1 20071202 A 3230 LANDING GEAR AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 269QS 169 GEAR WOULD NOT EXTEND NORMALLY, WITH GEAR HANDLE DOWN, ONLY MAIN GEAR DOORS OPENED. 2 CYCLES SAME RESULT. GEAR CAME DOWN WITH EMERGENCY GEAR HANDLE PULLED. INSP, FAULT CODE 435 PRESENT DURING GEAR SWING. REMOVED LANDING GEAR SELECT HANDLE P/N 307-39. S/N 212 AND REPLACED WITH INSPECTED GEAR HANDLE P/N 12-337-39, S/N 206 IN ACCORDANCE WITH F2000 MM 32-315. REMOVED AND REPLACED GEAR DOOR PROX DETECTORS L50GA1/R50GA1M P/N 84799031 (2EA) AND INSTALLED NEW DETECTORS, S/NS 2106 AND 2110. OPERATIONAL CHECK GOOD 2 L 7 2 4F 4 F RT A50NM E44NE 2007121300329 20071213 00329 CE 2007 12 13 DXTA200702640 1 20071201 A 3230 INDICATION SYS RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG MALFUNCTIONED E DXTA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 GL 07 871QS 258763 AFTER TAKEOFF DURING GEAR RETRACTION, GEAR INDICATORS SHOWED 3 GREEN AND 3 RED . SELECTED GEAR BACK DOWN AND GOT 3 GREEN . FOUND AUXILLIARY PUMP HANDLE IN UP POSITION AND AUX HANDLE PULLED. JACKED ACFT, CYCLED GEAR SEVERAL TIMES WITH SATIS FACTORY RESULTS. GEAR OPS CHECKS GOOD IAW MM 32-30-00. 2 L 7 2 4F 4 F RT A3EU E6WE 2007121300330 20071213 00330 CE 2007 12 13 DXTA200702641 1 20071201 A 3230 BOTTLE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG AUX EXTEND DISCHARGED E DXTA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 GL 07 670QS 5605170 ON TAKEOFF THE LANDING GEAR WILL NOT RETRACT. FOUND AUX GEAR BOTTLE HAD BEEN BLOWN AND NEVER RESET, RESET N2 BOTTLE SE RVICED AND SAFTIED GEAR BLOWDOWN CONTROL VALVE, ACCOMPLISHED FULL HYDRAULICS SYSTEM BLEED. VERIFIED NO HYD CONTAMINATION IN N1 BOTTLE, IAW MM CHAP 32-30-00. OPERATIONAL AND LEAK CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007121300332 20071213 00332 CE 2007 12 13 DXTA200702644 1 20071202 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE RIGHT UNKNOWN E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 306QS 5600266 RT BRAKE PEDAL ON CO-PILOT SIDE IS SOFT. CAPTAIN SIDE BRAKES ARE GOOD. REMOVED LT MASTER CYLINDER, INSTALLED NEW UNIT . REMOVED RT CO-PILOTS MASTER CYLINDER & INSTALLED NEW UNIT. REMOVED PUMP RELAY AND INSTALLED NEW RELAY. BLED BRAKES IAW C560 MM 32-42-00 FOR ALL OTHER WORK REF C560 MM 32-42-02 BRAKE SYSTEM OPERATES NORMALLY. 2 L 7 2 4F 4 F RT A22CE E25EA 2007121300333 20071213 00333 CE 2007 12 13 DXTA200702638 1 20071130 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE COPILOT INADEQUATE E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 354QS 5600356 COPILOT'S BRAKES TEND TO REQUIRE MORE THAN NORMAL PRESSURE FOR EVEN BRAKING. TROUBLESHOT BRAKE SYSTEM. FOUND CO-PILOT'S BRAKES (BOTH PEDALS) FIRM. SERVICED BRAKE RESERVOIR TO FULL AND BLED BOTH LT AND RT BRAKE SYSTEM AS REQUIRED. CO-PILOTS BRAKES OPS NML NOW. RESERVICED BRAKE RESERVOIR SYSTEM TO FULL. ALL WORK PERFORMED IAW CE-560 AMM 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007121300334 20071213 00334 CE 2007 12 13 DXTA200702639 1 20071130 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE PWA 545 PW545A NE INADEQUATE E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 306QS 5600266 WHEN BOTH BRAKE PEDALS ARE DEPRESSED, THE RT ONE IS MUCH SOFTER THAN THE LT. THIS HOLDS FOR BOTH THE CAPTAIN AND FIRST OFFICER RESPECTIVE SIDES. VISUALLY INSPECTED RT BRAKE ASSY AND LINES. PERFORMED BRAKE BLEED ON RT SIDE IAW MM 32-42-00. TAXIED ACFT AND BRAKE SYSTEM PERFORMED NORMAL. NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007121300335 20071213 00335 CE 2007 12 13 DXTA200702643 1 20071202 A 3260 EN1EN114N119 SQUAT SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG MALFUNCTIONED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 867QS 258576 AFTER T/O, LANDING GEAR WOULD NOT RETRACT, SQUAT AND STALL IDENT WARNING LIGHTS CAME ON. REPLACED LT & RT MLG WOW SWITC H . ROUTED WIRE TO TERMINAL BLOCKS "JK" AND "KK" AND TERMINATED. PERFORMED OPERATIONAL CHECKS AS REQUIRED WITH NO DEFECT S NOTED. ALL WORK PERFORMED IN ACCORDANCE WITH THE WDM 32-60-03 AND AMM 32-10-12. 2 L 7 2 4F 4 F RT A3EU E6WE 2007121300347 20071213 00347 NM 2007 12 13 2007UALA04883 1 20071129 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 FRAME CORRODED ON FWD AND AFT SIDE OF BS 380 AND ON SKIN ADJACENT TO FWD SIDE OF FRAME, IN FWD PIT BILGE RBL 2"- LBL 2". MAJOR REPAIR: REMOVED CORROSION AND ACCOMPLISHED REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300366 20071213 00366 NM 2007 12 13 2007UALA04892 1 20071129 A 5320 DOUBLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 AFT PIT AT BS 1440 BETWEEN STR 27R AND STR 28R, ANGLE DOUBLER IS CORRODED UNDER TRANSITION PANEL. MAJOR REPAIR ACCOMPLI SHED: REMOVED SPLICE, FABRICATED & INSTALLED A NEW SPLICE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121300382 20071213 00382 NM 2007 12 13 2007UALA04898 1 20071201 A 3350 BR964422 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 849UA 1649 EMERGENCY LIGHT AISLE PATHWAY LIGHT AT ROW 11 OUT. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121300386 20071213 00386 NM 2007 12 13 2007UALA04904 1 20071201 A 5320 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 AFT ENTRY DOOR LOWER HINGE CUTOUT IN FUSELAGE CRACKED AT THE LOWER FORWARD CORNER. MAJOR REPAIR: REMOVED DAMAGE. FABR ICATED AND INSTALLED EXTERNAL SKIN DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300387 20071213 00387 NM 2007 12 13 2007UALA04905 1 20071201 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 BS 517 TO 519 AT STRINGER 12L, FUSELAGE INTERIOR SKIN CRACKED AT CHEM MILLED STEP BELOW STRINGER. MAJOR REPAIR: REMOVE D DAMAGE. FABRICATED AND INSTALLED EXTERNAL FUSELAGE SKIN DOUBLER-TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300391 20071213 00391 NM 2007 12 13 2007UALA04909 1 20071202 A 5313 STRINGER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 FUSELAGE STRINGER CORRODED JUST BELOW FWD LAV SERVICE PANEL - RT NOSE TUNNEL STR 21R. MAJOR REPAIR: REMOVED DAMAGED PA RT OF STRINGER. REMOVED CORROSION FROM SKIN. FABRICATED AND INSTALLED U-CHANNEL, HAT CHANNEL AND J-ANGLES STRINGER REP AIRS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300398 20071213 00398 NM 2007 12 13 2007UALA04918 1 20071201 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY CEILING LIGHT ABOVE ROW 53 LT INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121400011 20071214 00011 NM 2007 12 14 CALA0700728 1 20071204 A 5320 6916970501 FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 CABIN FWD ENTRY INTERCOSTAL 15L AFT OF L1 DOOR CUTOUT WEB FWD SUPPORT CLIP CRACKED. INSTALLED CLIP PER SRM 53-40-02. 2 L 7 2 4F RT A16WE 2007121400014 20071214 00014 EA 2007 12 14 COMA0760675 1 20071129 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP WORN A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 716CA 23466 7250 FLIGHT 5053 - FLAPS FAIL CAUTION MESSAGE, FLAPS FAILED AT 12 DEGREES ON DESCENT. AIRCRAFT LANDED SAFELY IN JFK. REMOVE D AND REPLACED PDU. 2 L 7 2 4F RT A21EA 2007121400021 20071214 00021 EA 2007 12 14 COMA0760679 1 20071130 A 3230 46193 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 969CA 14912 7141 RECEIVED NOSE GEAR DISAGREE MESSAGE DURING RETRACTION. DECLARED EMERGENCY, RETURNED TO FSD, LANDED WITHOUT INCIDENT. R EPLACED MAIN GEAR PRIORITY VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007121400023 20071214 00023 EA 2007 12 14 TRAX200701845 1 20071201 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 AAR - PILOTS BULKHEAD AT FS 280 RBL 9.0 IS CRACKED. 2 L 7 2 4F RT A21EA 2007121400038 20071214 00038 NM 2007 12 14 SWAA076005 1 20071204 A 5754 65C26602312 SLAT BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT AFT CORNER DELAMINATED. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 2007121400042 20071214 00042 2007 12 14 SWAA076009 4 20071204 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 762SW 27876 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007121400059 20071214 00059 WP 2007 12 14 ABXR070390 1 20071002 A 5755 3923254503N SUPPORT BRACKET DOUG DC9 DC915 3022036 WP SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 784TW 47014 LEFT INBOARD FLIGHT SPOILER INBOARD TORQUE TUBE SUPPORT BRACKET (REACTION ARM) CRACKED. REMOVED AND REPLACED SUPPORT IA W DC9 SRM. 2 L 7 2 4F A6WE 2007121400064 20071214 00064 SO 2007 12 14 SIMA200734409 1 20071206 A 3220 14524475003 CAP EMB 145 EMB145LR 3260212 SO NOSE GEAR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 664MS 9613 5000 145779 DURING MBV, THE NOSE LANDING GEAR WAS INSPECTED (CPC CARD NUMBER 53-200-06) AND FOUND CORROSION ON THE LANDING GEAR CAP. REMOVED AND REPLACED WITH NEW IAW EMB AMM AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007121400066 20071214 00066 GL 2007 12 14 SIMA200734403 2 20071207 A 7200 AE3007A13 ENGINE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL RIGHT SMOKE A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 819AE 145566 CAE311013 CREW NOTED ON CLIMB-OUT SMOKE IN CABIN. CREW GOT THE LAV SMOKE DETECTOR, FOLLOWED MANUAL AND DECLARED EMERGENCY AND RET URNED TO SDF FOR MTX. LANDED SAFELY WITH NO OTHER PROBLEMS. REMOVED AND REPLACED RT ENGINE. OPERATION CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007121400071 20071214 00071 WP 2007 12 14 ABXR070397 1 20071005 A 5411 9911840125 SPAR DOUG DC9 DC915 3022036 WP RT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 784TW 47014 RIGHT AFT PYLON SPAR WEB CRACKED FORWARD SIDE. REPAIRED CRACKED WEB IAW DC9 SRM 54-01. 2 L 7 2 4F A6WE 2007121400076 20071214 00076 SO 2007 12 14 SIMA200734407 1 20071207 A 2797 GROUND STUD EMB 145 EMB145LR 3260212 SO SPOILERS SHORTED A SIMA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 SW 21 619AE 145101 ON TAKEOFF ROLL AT 10 KTS IN THRUST SET POSITION GOT NO TAKEOFF CONFIGURING EICAS SPOILER SHOWED OPEN. GOT NO SPOILER A URAL WARNING. ABORTED TAKEOFF AND SPOILER CLOSED AT IDLE THRUST. FOUND GROUND BLOCKS GS0163 DC AND GS 0186 DC TO HAVE HIGH OHMS TO GROUND. CLEANED AND REINSTALLED PER WM 20-10-01. SPOILERS OPS CHECK GOOD PER EMB 145 AMM 27-63-01. BOTH STATIC AND DURING GROUND TAXI CHECK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007121400082 20071214 00082 NM 2007 12 14 SWAA076032 1 20071205 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121400083 20071214 00083 NM 2007 12 14 QXEA200701845 1 20071204 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM MAIN PAX LACK OF LUBE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 424QX 4006 BOI - AFT PASSENGER DOOR HARD TO OPEN. MAINTENANCE CLEANED AND LUBED THE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETU RNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007121400084 20071214 00084 NM 2007 12 14 SWAA076033 1 20071205 A 5310 6545834 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 268 AND BS 360, RBL 70. REPAIRED CREASE BEAM PER SRM . 2 L 7 2 4F RT A16WE 2007121400085 20071214 00085 NM 2007 12 14 QXEA200701792 1 20071204 A 2750 C1486742003 SWITCH BOMBDR DHC8 DHC8402 1390042 NM TE FLAPS MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 415QX 4081 SEA - FLAP DRIVE CAUTION MESSAGE DURING TAXI. FLASHES OFF AND ON 5 TO 6 TIMES. RETURNED TO THE GATE. DURING TAXI BACK TO THE GATE, DID NOT FLASH. AIRCRAFT FERRIED TO PDX FOR REPAIRS. MAINTENANCE REPLACED THE FLIGHT/TAXI SWITCH. OPERAT IONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007121400086 20071214 00086 NM 2007 12 14 SWAA076016 1 20071205 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2007121400087 20071214 00087 2007 12 14 SWAA076017 4 20071205 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007121400089 20071214 00089 NM 2007 12 14 QXEA200701796 1 20071204 A 5270 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR FALSE ACTIVATION A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 400QX 4030 SEA - FLIGHT 2276 - CARGO DOOR OPEN INDICATION AT ROTATION. RETURNED TO THE FIELD AND ACCOMPLISHED A OVERWEIGHT LANDING OF 62,200 LBS ACCORDING TO THE FMS. DESCENT RATE WAS 100 TO 200 FPM. MAINTENANCE ACCOMPLISHED A OVERWEIGHT LANDING IN SPECTION WITH NO DEFECTS NOTED. PERFORMED OPERATIONAL TEST OF THE CARGO DOOR WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007121400092 20071214 00092 NM 2007 12 14 SWAA076020 1 20071205 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007121400094 20071214 00094 NM 2007 12 14 SWAA076021 1 20071205 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 433LV 33716 EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 7 DEF. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007121400095 20071214 00095 WP 2007 12 14 IXXA07SMN240S 1 20071110 A 5330 SKIN DOUG DC8 DC873F 302199F WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT FUSELAGE NOSE SECTION ACS MODIFICATION DOUBLER HEAT INTERCHARGER COMPARTM ENT LOWER AFT JAMB CORNER DAMAGE AT STATION FS 12.000 LONGERON 27 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED EXTERNAL DOUBLER AND EXTER NAL REPAIR TRIPLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW FORM FAA 8110-3 NUM BER 07529 DATED 11-09-07 SEMAN DRAWING NUMBERED-4645 DATED 11-08-07, SRM 51-1-21, DC8 51-3-0, DC8 NDT SPM PART 08-00-02 TO 07, FORM SEMAN 242-4, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, 51-3-0, 51-1-20D, AND 51-3-1. 2 L 7 4 4F RT 4A25 2007121400096 20071214 00096 2007 12 14 SWAA076022 4 20071204 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007121400097 20071214 00097 WP 2007 12 14 IXXA07SMN241S 1 20071110 A 5330 SKIN DOUG DC8 DC873F 302199F WP ZONE 200 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, EXTERNAL SKIN SHOWS CRACK AT STATION FS 1750.000 LONGERON 15 LEFT. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER INTERNAL FINGER DOUBLER. PERFORMED NDT INSPECTION. NO CRACK NO CORROSION FOUND. CLEANE D, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-1 FIGURE 7 SHEET 1 AND 4, SRM 53-5 -3 FIGUE 1 ITEM "D", DC8 NDT SPM PART 08-00-02 TO 07, FORM SEMAN 242-4, DC8 SRM 51-1-8B, SRM 51-1-21, 51-1-20D, AND 51-3 -1. 2 L 7 4 4F RT 4A25 2007121400098 20071214 00098 NM 2007 12 14 SWAA076037 1 20071205 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007121400100 20071214 00100 NM 2007 12 14 KNNA200700066 1 20070813 A 5330 SKIN BOEING 737 7372L9 1384497 NM PWA JT8 JT8D9 52048 NE STA 907 25R BULGED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 464AT 21258 PREVIOUS REPAIR ON FUSELAGE SKIN AT STA 907 AND STR-25R. REPAIRED BY REMOVING EXISTING REPAIR AND CUTTING OUT THE DAMAGE D AREA, THEN FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-30-03 FIG 48 AND SKYKING ACO-0753116 2 L 7 2 4F 4 F RT A16WE E2EA 2007121400103 20071214 00103 WP 2007 12 14 IXXA07SMN244S 1 20071110 A 5340 37552221 FITTING DOUG DC8 DC873F 302199F WP BS 702 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND IN MAIN CARGO COMPARTMENT A CRACKED FITTING AT STATION 702.875 RIGHT BOTTOM LIN E 25". REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-3-0, DC8 SRM 5 1-1-8B, DC8 SRM 51-1-20D, AND 51-3-1. 2 L 7 4 4F RT 4A25 2007121400104 20071214 00104 NM 2007 12 14 SWAA076025 1 20071205 A 5753 6546430129 SKIN BOEING 737 7373H4 1384600 NM FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED HC1 CHECK, FOUND LT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM . 2 L 7 2 4F RT A16WE 2007121400109 20071214 00109 WP 2007 12 14 IXXA07SMN246S 1 20071115 A 5340 36408870 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND IN MAIN CARGO COMPARTMENT A CRACKED FITTING BETWEEN STATION 960.000 AND STATION 980.000 RIGHT BOTTOM LINE 25". REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, AND DC8 SRM 51-3- 1. 2 L 7 4 4F RT 4A25 2007121400110 20071214 00110 WP 2007 12 14 IXXA07SMN248S 1 20071115 A 5512 SKIN DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, LEFT HORIZONTAL STABILIZER LEADING EDGE UPPER SKIN SHOWS CORROSION AT STATION XFS 177 .750. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION AFTER INSPECTION. FABRICATED NEW SKIN, INTERNAL, AND EXTERNAL DOUBLER S. CLEANED, TREATED AND PRIMED AREA REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FORM FAA 8110-3 NUMBER 07529 DATED 11-09-07 SEMAN DRAWING NUMBER ED-4647 DATED 11-08-07, DC8 SRM 51-1-21, 51-3-0, DC8 SRM 51-1-8 PAGE 17-18, DC 8 SRM 55-2-0 PAGE 12, DC8 NDT SPM PART 08-00-0 TO 07, FORM SMN 242-4, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND 51-3-1. 2 L 7 4 4F RT 4A25 2007121400111 20071214 00111 NM 2007 12 14 SWAA076026 1 20071205 A 2750 655292552 TORQUE TUBE BOEING 737 7373H4 1384600 NM T/E FLAP WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED BRDG CHECK, FOUND LT WING TORQUE TUBE WORN AT NR 1 TRANSMISSION. REMOVED AND REPLACED TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2007121400113 20071214 00113 NM 2007 12 14 SWAA076034 1 20071205 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121400114 20071214 00114 WP 2007 12 14 IXXA07SMN250S 1 20071115 A 5330 S1616757 SKIN DOUG DC8 DC873F 302199F WP ZONE 200 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, AFT FUSELAGE FOUND A CRACK AT LONGERON 17 RIGHT AT STATION 1769.000. REMOVED CRACKED LONGERON. FABRICATED LONGERON. CLEANED, TREATED AND PRIMED AREA AND NEW LONGERON. INSTALLED NEW LONGERON IAW DC8 SRM 51-1-11, 51-3-1, DC8 SRM 53-5-3 FIGURE 5 SHEET 1 ITEM "B", DC8 SRM 53-1-0 PAGE 1, SRM 51-1-21 AND 51-1-20D, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007121400116 20071214 00116 NM 2007 12 14 SWAA076035 1 20071205 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121400117 20071214 00117 2007 12 14 TRBA2007109 4 20071207 A 6113 AN8143DL SCREW AEROSP ATR72 ATR72212A 8680902 EU PROPELLER DOME LOOSE A TRBA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SO 29 548AT 548 LOST NR 2 OIL PRESSURE IN FLIGHT. INDICATION ON CAP AND OIL PRESSURE SWITCH. NR 2 ENGINE SHUT DOWN IN FLIGHT AS PER AO M VOL 1. POST FLIGHT INSPECTION REVEALED OIL DRIPPING FROM ENGINE IN LARGE PUDDLE AND COVERING SIDE OF A/C. FOUND ACTU ATOR ASSEMBLY PLUG AND BLEEDER SCREW LOOSE; LOSING OIL THRU PLUG. RE-ATTACHED PLUG AND BLEEDER SCREW IAW HAMILTON SUNDS TRAND MM NR 61-13-12. COMPLIED WITH ENGINE OIL CONSUMPTION CHECK IAW PRATT AND WHITNEY MM NR 05-50-00 AND AE WORK CARD NR 055007-CS-20000-002. ALL PARAMETERS NORMAL. ALSO CLEANED SIDE FUSELAGE AND NR 2 ENGINE IAW JIC NR 12-21-11. 2 H 7 2 4T RT A53EU 2007121400120 20071214 00120 NM 2007 12 14 SWAA076028 1 20071205 A 5754 65C26601 SLAT BOEING 737 7373G7 1384595 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED C3 CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT INBOARD END. REPAIRED SLAT PER SWA EA. 2 L 7 2 4F RT A16WE 2007121400121 20071214 00121 WP 2007 12 14 ARWA20071201 1 20071210 A 5520 PIN DOUG DC10 DC1030 3023501 WP ELEVATOR INSTALLED A ARWA D RETURN TO BLOCK W INADEQUATE Q C TX TAXI/GRND HDL 1 SO 19 524MD 46999 DURING FLIGHT CONTROL CHECK UNABLE TO MOVE CONTROL COLUMN FORE AND AFT. FOUND ELEVATOR LOCKING PIN ON ELEVATOR POSITION P-6. REMOVED AS REQUIRED IN ACCORDANCE WITH DC-10 M/M 27-31-00. OPERATIONAL CHECK OK IN ACCORDANCE WITH DC-10 M/M 27- 31-00 2 L 7 3 4F A22WE 2007121400123 20071214 00123 WP 2007 12 14 IXXA07SMN253S 1 20071115 A 5311 2537716 FRAME DOUG DC8 DC873F 302199F WP ZONE 100 DENTED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD CARGO COMPARTMENT FRAME WITH DENT AND MISDRILLED AT STATION 200.000 LON GERON31 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED FRAME SEGMENT. FABRICATED FRAME SEGMENT ANGLE AND SPLICE. PERFORMED HEAT TREATMENT TO REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTAL LED REPAIR PARTS AND NEW FASTENERS IAW DC8 SRM 53-2-0 FIG 2, SHEET 2 AND 6, 51-1-11, 51-3-1, IAW DC8 SRM 53-2-0 FIGURE 2 SHEET 2 AND 6, DC8 SRM 51-1-20D, DC8 SRM 53-2-0 FIGURE 2 SHEET 1, 51-2-0 FIGURE 50 SHEET 49 T/R NUMBER 51-106 DATED 01- 29-99, SRM 53-4-1 FIGURE 40 SHEET 5 AND 6, DC8 SRM 53-2-0 FIGURE 2 SHEET 7 AND 8 T/R NUMBER 53-110 DATED 11-10-2000, DC8 2 L 7 4 4F RT 4A25 2007121400124 20071214 00124 WP 2007 12 14 IXXA07SMN254S 1 20071115 A 5330 SKIN DOUG DC8 DC873F 302199F WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, NOSE SECTION FUSELAGE FREON EXHAUST SYSTEM FORWARD UPPER CORNER CRACKED AT STATION FS 40.000 L27L. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR.REMOVED DAMAGED AREA.FABRICATED EXTERNAL REPAIR DOUBLER , A ND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS AND NEW FASTNERS IAW SRM 51-1-21, 5 1-3-1, DC8 SRM 53-2-0 FIGURE 13 SHEET 1, SRM 53-2-0 FIGURE 13 SHEET 5 TR NUMBER 53-169 DATED 09-20-03, SRM 53-3-3 FIGUR E 1 ITEM "C", DC8 SRM 51-1-20D, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007121400125 20071214 00125 WP 2007 12 14 IXXA070060S 1 20071115 A 5330 SKIN DOUG DC8 DC873F 302199F WP ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, NOSE SECTION FUSELAGE FREON EXHAUST SYSTEM FORWARD UPPER CORNER CRACKED AT STATION FS 40.000 LONGERON 28 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED EXTERNAL RE PAIR DOUBLER, AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW SRM 51-1-21, 51-3-1, DC8 SRM 53-2-0 FIGURE 13 SHEET 1, SRM 53-2-0 FIGURE 13 SHEET 5 TR NUMBER 53-169 DATED 09-20-03, SRM 53-3-3 FIGURE 1 ITEM "C", DC8 SRM 51-1-20D, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007121400126 20071214 00126 2007 12 14 SWAA076027 4 20071205 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007121400127 20071214 00127 NM 2007 12 14 SWAA076030 1 20071205 A 5330 65C381921 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 511D, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007121400128 20071214 00128 2007 12 14 SWAA076031 4 20071205 A 2565 D31354 SLIDE BOEING 737 7373T5 1384608 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 696SW 23064 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007121400130 20071214 00130 EU 2007 12 14 07FDEA05022 1 20071211 A 3150 WARNING LIGHT AIRBUS 310 A310203 3930313 EU A/C PACKS FALSE ACTIVATION A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 409FE 273 DURING CLIMB AT APPROX FL 260, GOT PACK 1 AND PACK 2 FAULT, WOULD NOT RESET. DESCENDED TOWARDS 10.000, PACKS RESET AT ABOUT 14,000. CLIMBED BACK TOWARDS FL 340, BUT BOTH PACKS FAULTED AGAIN AT APPROX FL260. DIVERTED INTO BOS. PERFORME D CABIN PRESS CONTROL AND MONITORING TEST IAW AMM 21-31-00-5. OP CKS GOOD. RAN NR 1 AND NR 2 ENGINES PER JRH. ENG BL EED VALVES AND PRESS NORMAL. A/C HAS NO HISTORY IN ATA 21 OR 36 FOR PRESSURIZATION. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2007121400132 20071214 00132 WP 2007 12 14 IXXA07SMN255S 1 20071115 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 604BX 46046 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT HAS A IMPROPER REPAIR AND DENT ON FRAME AT STATION 240.0 00 LONGERON 20 RIGHT. REMOVED FASTENER AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED FRAME SEGMENT , SPLICE AND ANGLE. PERFORMED HEAT TREATMENT TO FRAME SEGMENT, SPLICE AND ANGLE. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW 51-1-11, 51-3-1, DC8 SRM 53-2-0 FIGURE 2 SHEET 2 AND 6, DC8 SRM 51-1-20D, DC8 SRM 53-4-1 FIGURE 40 SHEET 7-9 ITEM "C", SRM 53-2-0 FIGURE 2 SHEET 1, SRM 51-2-0 FIGURE 50 SHEET 49A, DC8 SRM 53-2-0 FIGURE 2 SHEET 8 T/R 53-110 DATED 11-10-2000, SRM 53-2-0 FIGURE 2 SHEET 7 T/R 53-110 DATED 11-10-2000, D 2 L 7 4 4F RT 4A25 2007121400134 20071214 00134 NM 2007 12 14 NWAA073956745 1 20071208 A 3350 BATTERY PACK BOEING 747 747222B 1384904 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 645NW 23736 DURING OVERNIGHT CHECK, FOUND EMERGENCY LIGHT "EXIT" LOCATED OVER UPPER DECK EMERGENCY DOOR INOP. MAINTENANCE REMOVED A ND REPLACED BATTERY PACK. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007121400135 20071214 00135 NM 2007 12 14 NWAA073966745 1 20071208 A 3350 BATTERY PACK BOEING 747 747222B 1384904 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 645NW 23736 DURING OVERNIGHT CHECK, FOUND EMERGENCY LIGHT IN UPPER DECK CEILING APPROX STA 560 (NEAR GALLEY) INOP. MAINTENANCE REMO VED AND REPLACED BATTERY PACK. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007121400137 20071214 00137 NM 2007 12 14 2007UALA04652 1 20071108 A 3010 8106012 ANTI-ICE VALVE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RT WING FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 784UA 26951 ICING WING PRIMARY ICE DETECTION SYSTEM (LEFT OR RIGHT ICE DETECTORS) DETECTS ICE, AND THE WING ANTI-ICING (WAI) SWITCH IS OFF. *S/D* REPLACED RIGHT WING ANTI-ICE VALVE PER MM 30-11-03 & ACCOMPLISHED OPS CHECKS PER MM 30-11-00, ALL OPS & INDICATIONS NOW NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121400138 20071214 00138 NM 2007 12 14 NWAA073986740 1 20071209 A 2612 CONNECTOR BOEING 747 747251F 1384898 NM FIRE DETECTOR DIRTY A NWAA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 01 640US 23888 MAIN DECK CARGO SMOKE DETECTOR ZONE 4 LIGHT CAME ON ALONG WITH THE CARGO FIRE LIGHT AND BELL. AFTER 20 MINUTES THE LIGH TS WENT OUT. TESTED SYSTEM AND TEST OK. MAINTENANCE CLEANED PLUG ON DETECTOR AND TEST OK. OPERATIONAL CHECKED GOOD AN D AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007121400141 20071214 00141 EU 2007 12 14 2007UALA04928 1 20071130 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 469UA 1409 PER 3SVC TESTED EMERGENCY LIGHTS TEST FAILED EPSU RT SIDE. FOUND EPSU FAILED. REPLACED EPSU, OPS CHECK NORMAL, NO REP EATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121400143 20071214 00143 NM 2007 12 14 2007UALA04929 1 20071203 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 MAIN CABIN AT STA 700, LBL 24, FLOORBEAM CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA. FABRICATED & INS TALLED NEW T-CAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121400144 20071214 00144 EU 2007 12 14 CPCP20070122 1 20071119 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 342AT 29282 LT SEAT TRACK BETWEEN FRAME 36-39 CORRODED. LT SEAT TRACK BETWEEN FRAME 36-39, REPLACED IAW SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007121400149 20071214 00149 NM 2007 12 14 2007UALA04931 1 20071203 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 CABIN FLOORBEAM UPPER FLANGE CRACKED AT RADIUS AT BS 700 LBL 25. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121400151 20071214 00151 NM 2007 12 14 2007UALA04932 1 20071203 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 DOOR L2 UPPER HINGE CUTOUT HAS DAMAGE. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121400152 20071214 00152 NM 2007 12 14 2007UALA04933 1 20071204 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 DOOR 1 LEFT FWD SILL & DOOR 5R SILL 2EA EMERGENCY LIGHTS ARE INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121400153 20071214 00153 NM 2007 12 14 2007UALA04934 1 20071204 A 3350 80541 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 SEAT 32 HJK EMERGENCY LIGHT IS INOP. REPLACED LIGHT STRIP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121400154 20071214 00154 NM 2007 12 14 2007UALA04935 1 20071204 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 SEAT 4J AFT EMERGENCY LIGHT IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121400155 20071214 00155 EU 2007 12 14 F3LA200700363 1 20071205 A 7120 LOCK TAB AIRBUS A319 A319112 3930323 EU NR 2 ENG MOUNT FAILED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 901FR 5849 1488 DURING C-5 CHECK, INSPECTION REPORTED NR 2 ENG AFT MOUNT INBD LWR LOCKING TAB THAT SECURES BOLT FROM ROTATING BLOWN OUT OF ITS SECURING POSITION TO PREVENT BOLT FROM ROTATING. REMOVED AND REPLACED BEARING AT RIB 10 IAW MM 54-51-17-000-003 AND MM 54-51-17-400-003, STEPS 1-4. 2 L 7 2 4F RT A28NM 2007121400156 20071214 00156 EU 2007 12 14 F3LA200700365 1 20071207 A 5322 D5391379020002 SHEAR PLATE AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 901FR 5849 1488 DURING C-5 CHECK, INSPECTION REPORTED CORROSION ON FWD CARGO COMPARTMENT FLOORBEAM AT FR 28, AND ON THE AFT DOOR SILL. CORROSION WAS CLASSIFIED AS EXFOLIATION. REMOVED AND REPLACED PROFILE PLATE IAW SRM 51-42-11-PAR 2A1. 2 L 7 2 4F RT A28NM 2007121400157 20071214 00157 NM 2007 12 14 2007UALA04936 1 20071204 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 UPPER DECK CEILING EMERGENCY LIGHT IS INOP NEAR CENTER WING DOORS (1 EA). RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121400158 20071214 00158 NM 2007 12 14 NWAA074005505 1 20071102 A 5321 PLATE BOEING 757 757251 1384970 NM BS 1720 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 505US 23194 DURING "M" CHECK, FOUND CORROSION ON AFT DECK PLATE AT BS 1720 LBL 20-26. REPAIRED PER EA 55-210439. 2 L 7 2 4F RT A2NM 2007121400160 20071214 00160 NM 2007 12 14 DL757071591 1 20071119 A 5522 183N20012 SKIN BOEING 757 757232 1384965 NM RT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 SMALL CRACK IN RT ELEVATOR UPPER SKIN FOUND DURING PAINT. CRACK FALLS IN CRITICAL AREA MAKING MAJOR REPAIR. REPAIRED E R SRM 55-20-01. 2 L 7 2 4F RT A2NM 2007121400161 20071214 00161 NM 2007 12 14 2007UALA04938 1 20071203 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 536UA 25156 NR 2R DOOR EMERGENCY LIGHT BURNED OUT. REPLACED BURNED OUT LAMP. SYSTEM OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121400162 20071214 00162 NM 2007 12 14 DL757071594 1 20071201 A 2597 W0624001420 WIRE HARNESS BOEING 757 757232 1384965 NM RT OVRWG SLIDE BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 645DL 24216 RIGHT OVERWING SLIDE DID NOT DEPLOY DURING SAMPLING EVENT. TROUBLESHOT PER WD 25-65-21. FOUND WIRE HARNESS W0624 ON P7 9 PANEL TIED TOO TIGHT CAUSING WIRE COMING FROM RELAY BASE K10536 TO BE VERY TAUGHT. THIS CAUSED WIRE TO BREAK FROM PIN B1. REPLACED B1 PIN IN RELAY BASE K10536. TESTED FOR 28 VOLTS DC AT RIGHT OVERWING SLIDE PRESSURE BOTTLE SQUIB. TES T GOOD. 2 L 7 2 4F RT A2NM 2007121400168 20071214 00168 2007 12 14 DL76P071602 4 20071210 A 3120 066500011001 INDICATOR BOEING 767 767332 1382001 NM COCKPIT ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 144DA 27584 CAPTAINS VSI WENT BLANK. DETECTED FAINT ELECTRICAL ODOR. PULLED VSI CIRCUIT BREAKER. ODOR DISSIPATED. REPLACED CAPTS VSI, OPS TESTS GOOD. 2 L 7 2 4F RT A1NM 2007121400169 20071214 00169 NM 2007 12 14 DL764071604 1 20071210 A 5330 SKIN BOEING 767 767432ER 1385134 NM BS 1395-1439 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 839MH 29712 FOUND DEBRIS STUCK FUSELAGE AT FS 1395-1439. INSTALLED SKIN REPAIR DOUBLER. 2 L 7 2 4F RT A1NM 2007121400172 20071214 00172 EU 2007 12 14 F3LA200700366 1 20071209 A 5415 D5463009200000 HINGE FITTING AIRBUS A319 A319112 3930323 EU NR 2 NACELLE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 901FR 5849 1488 DURING C-5 CHECK, INSPECTION REPORTED NR 2 PYLON T/R COWL FITTINGS AT RIB 1 AND RIB 2 CORRODED. REMOVED AND REPLACED NR 2 PYLON OTBD T/R COWL FITTINGS AT RIBS 1 AND 2 IAW AMM 54-57-17-000-003 AND 54-57-17-420-053. 2 L 7 2 4F RT A28NM 2007121400174 20071214 00174 WP 2007 12 14 IXXA07SMN233S 1 20071110 A 5330 SKIN DOUG DC8 DC873F 302199F WP ZONE 100 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND LOWER FUSELAGE NOSE SECTION HAS IMPROPER REPAIR AT STATION 165.000 TO STATION 7 0.000 LONGERON 31 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKINS AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 53-3-3 FIGURE 1, DC8 SRM 53-1-0 PAGE 1 AND SRM 51-1-21, DC8 SRM 51-1-8B, 51-1-20D, AND 51-3-1. 2 L 7 4 4F RT 4A25 2007121400175 20071214 00175 WP 2007 12 14 IXXA070062S 1 20071110 A 5330 SKIN PANEL DOUG DC8 DC873F 302199F WP ZONE 100 MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND LOWER FUSELAGE NOSE SECTION HAS IMPROPER REPAIR AT STATION 165.000 TO STATION 7 0.000 LONGERON 31 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKINS AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 53-3-3 FIGURE 1, DC8 SRM 53-1-0 PAGE 1 AND SRM 51-1-21, DC8 SRM 51-1-8B, 51-1-20D, AND 51-3-1. 2 L 7 4 4F RT 4A25 2007121400176 20071214 00176 EU 2007 12 14 AALA20072403 1 20071208 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70079 619 JFK - EMERGENCY LIGHTS AT SEAT MOUNTED LEFT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT M OUNTED LEFT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121400177 20071214 00177 WP 2007 12 14 AALA20072404 1 20071208 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 569AA 49351 LGA - EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS CABI N. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007121400178 20071214 00178 EU 2007 12 14 AALA20072393 1 20071207 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7062A 474 JFK - EMERGENCY LIGHTS AT SEAT 22G INOPERATIVE. REPAIRED BENT PIN ON CONNECTOR FOR EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121400179 20071214 00179 NM 2007 12 14 AALA20072395 1 20071207 A 5610 141W74001 WINDOW BOEING 777 777223 1385213 NM COCKPIT CRACKED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 799AN 30258 LGW INFLIGHT T173/07DEC - CAPTAINS LEFT NUMBER ONE WINDSHIELD ARCED AND CRACKED. RETURNED TO LGW AND LANDED WITHOUT INC IDENT. REPLACED WINDOW AND REPLACED HEAT CONTROLLER AS PRECAUTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121400191 20071214 00191 NM 2007 12 14 AALA20072408 1 20071210 A 3350 LIGHT BOEING 767 767323 1385205 NM GALLEY DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 391AA 27451 JFK - EMERGENCY LIGHT AT LEFT MID GALLEY DAMAGED. REPLACED LIGHT ASSEMBLY BASE FOR EMERGENCY LIGHT AT LEFT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007121400192 20071214 00192 NM 2007 12 14 AALA20072412 1 20071210 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 972AN 30097 MIA - EMERGENCY LIGHT AT SEAT 27D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 27D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A16WE 2007121400193 20071214 00193 NM 2007 12 14 AALA20072409 1 20071210 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 391AA 27451 JFK - EMERGENCY LIGHT AT LEFT MID GALLEY DAMAGED. REPLACED LENS FOR EMERGENCY LIGHT AT LEFT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007121400194 20071214 00194 NM 2007 12 14 AALA20072411 1 20071210 A 3397 WIRE BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 972AN 30097 MIA - EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. FOUND BROKEN WIRE AT CONNECTOR. REPLACED LIGHT ASSEMBLY FOR EMERGENCY L IGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007121400195 20071214 00195 NM 2007 12 14 AALA20072413 1 20071210 A 3350 0201984002 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 793AN 30255 JFK - EMERGENCY LIGHT AT SEAT 23G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121400196 20071214 00196 NM 2007 12 14 AALA20072410 1 20071210 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 972AN 30097 MIA - EMERGENCY LIGHT AT SEAT 10D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A16WE 2007121400200 20071214 00200 EU 2007 12 14 F3LA200700371 1 20071204 A 3350 321430 BATTERY PACK AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHTS NO TEST A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 901FR 1488 DURING C-5 CHECK, INSPECTION REPORTED AFT EMERGENCY BATTERY EPSU FAILED CAPACITY TEST. REMOVED AND REPLACED EPSU BATTER Y AND PERFORMED OPS CHECK IAW AMM 33-51-38-400-002. CHECKED GOOD. 2 L 7 2 4F RT A28NM 2007121400207 20071214 00207 NM 2007 12 14 2007UALA04939 1 20071203 A 3397 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 502UA 24623 EMERGENCY ESCAPE LIGHT INOP 26C, SEAT MOUNTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121400208 20071214 00208 NM 2007 12 14 07FDEA05034 1 20071212 A 5330 6540150 SKIN BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 LWR FUSE SKIN CRACKED JUST AFT OF TAIL SKID CUT REMOVED DAMAGED SKIN FILLER PLUS DOUBLER, INSTALLED REF SRM 51-10-2 PG2 FOR TREAT AND PRIME REF 53-30-3 FIG 25 FOR REPAIR. THIS IS A CATAGORY "C" REPAIR. THIS IS CLASSIFIED AS A MINOR REPAIR . 2 L 7 3 4F RT A3WE 2007121400209 20071214 00209 NM 2007 12 14 07FDEA05035 1 20071212 A 5754 651622193 SKIN BOEING 727 727233 138408A NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 LEFT WING, INBOARD LEADING EDGE, INNER PANEL AT LEADING EDGE. STATION 106 TO 130 HAS RIVETS PULLED THROUGH AND CRACKS I N SKIN AT 3 LOCATIONS STOP DRILLED CRACKS. HFEC INSP AROUND STOP DRILLED HOLED. FABRICATED REPAIR DOUBLERS, PRIMED AND PAINTED AND INSTALLED. REF FED EX DWG SR27-57-009 AND SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007121400212 20071214 00212 EU 2007 12 14 07FDEA05038 1 20071212 A 5347 A53274005200 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 671FE 778 MCC SEAT TRACK 2R HAS CORROSION AT FR75, 77, AND 78. INSTALLED SECTION OF SEAT TRACK AND 2 EA SPLICE AT 2 RT FR 75-77- AND 78 IAW A300 SRM 53-10-16. 2 L 7 2 4F RT A35EU 2007121400213 20071214 00213 EU 2007 12 14 07FDEA05039 1 20071212 A 5347 A53274005200 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 671FE 778 MCC SEAT TRACK SECTION 3R HAS CORROSION AT FR'S 57.1, 57.3 AND 57.5 REMOVED CORROSION IAW A300 SRM 51-74-10. ALODINED A ND PRIMED IAW A300 SRM 51-75-10. AREA WAS FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK IAW A300 SRM 53-10-16. REPAIRED AND INSTALLED NEW SEAT TRACK IAW A300 SRM 53-10-16 AND A300 SRM 51-75-10. 2 L 7 2 4F RT A35EU 2007121400214 20071214 00214 NM 2007 12 14 07FDEA05040 1 20071212 A 5330 6554577 SKIN BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 LWR FWD CARGO PIT, INNER SKIN IN BILGE HAS PITTING CORROSION UNDER LEVELING COMPOUND, STA 680 PLUS 5, LBL 8". CUT OUT DAMAGE, FABRICATED DOUBLER AND INSTALLED DOUBLER, REF SRM 53-30-3 FIG 1. REPAIR IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007121400215 20071214 00215 NM 2007 12 14 07FDEA05041 1 20071212 A 5330 6572702 SKIN BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 EXT FUSELAGE SKIN IS GOUGED AT BS 990, STR S-23L PLUS 6" REMOVED DAMAGE REF SRM 53-30-3 FIG, INSTALLED DOUBLER AND FILLE R REF SRM 53-30-3 FIG 1. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007121400221 20071214 00221 NM 2007 12 14 2007UALA04942 1 20071203 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 663UA 27160 EXTERIOR EMERGENCY LIGHT AT L-1 DOOR IS INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121400222 20071214 00222 NM 2007 12 14 2007UALA04943 1 20071203 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 663UA 27160 EEL EXTERIOR DOOR 1R AND 2L INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121400223 20071214 00223 GL 2007 12 14 SIMA200734607 2 20071210 A 7200 AE3007A13 ENGINE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL NR 1 SMOKE A SIMA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 819AE 145566 CAE312899 ON TAKEOFF ROLL, APU OFF, ENG BLDS ON, PACKS ON (NORMAL CONFIG) SMOKE IN CKPT. NO SMOKE OBSERVED IN CABIN. ABORTED T/O WITH NORMAL BRAKING. REMOVED AND REPLACED NR 1 ENGINE IAW MTX WORK CARD 71-000-00, OPS CHECK GOOD AND LEAK CHECK GOOD. NO DEFECTS NOTED. RAN ENGINE IAW WC 72-700-00. NO SMOKE DETECTED IN CABIN AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007121400229 20071214 00229 NM 2007 12 14 2007UALA04945 1 20071203 A 2421 SEAL BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 1 IDG DAMAGED A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 218UA 30222 DURING A-CHECK SERVICE OF NR 1 IDG, FOUND IDG LEVEL LOW. FOUND EVIDENCE OF INPUT SHAFT SEAL OF IDG LEAKING. INPUT SHAF T SEAL OF IDG LEAKING. REPLACED IDG. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121400230 20071214 00230 EA 2007 12 14 A6WA200740655 1 20071104 A 3000 PICCOLO TUBE CNDAIR CL600 CL6002B19 1900309 EA RIGHT DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 426AW 7669 RIGHT SIDE INTERNAL LEADING EDGE WS 163, BAY 630AZ 1 DENT EXIST ON DEICING TUBE (PICCOLO TUBE) DYE PENETRANT PERFORMED O N DENT, ONE CRACK FOUND. PICCOLO TUBE REPLACED IAW CRJ 200 AMM 30-11-41-000-801. (M) 2 L 7 2 4F RT A21EA 2008010700199 20080107 00199 NM 2008 1 7 UIEA200700493 1 20071212 A 5730 PANEL BOEING 747 7472D7B 1384803 NM ZONE 500 DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 LT WING UPPER SURFACE LEADING EDGE TO FRONT SPAR PANEL (BEHIND NR 8 LEADING EDGE FLAP WS 917) HAS EVIDENCE OF DELAMINATI ON. PANEL REPAIRED IAW SRM 51-40-9 AND 51-40-12. 2 L 7 4 4F RT A20WE 2007121400231 20071214 00231 EA 2007 12 14 A6WA200740656 1 20071107 A 5342 HANDLE CNDAIR CL600 CL6002B19 1900309 EA E/E BAY DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 426AW 7669 MAIN AVIONICS DOOR HANDLE CRACK MAIN AVIONIC DOOR HANDLE REPLACED IAW CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2007121400233 20071214 00233 EU 2007 12 14 2007UALA04948 1 20071204 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 481UA 1559 DENT IN A-C SKIN, LOWER FORWARD LEFT OF DOOR 2L, APPROX 3 INCHES IN DIAMETER X .25 INCH DEEP. MAJOR REPAIR ACCOMPLISHED : INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121400235 20071214 00235 NM 2007 12 14 2007UALA04950 1 20071204 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 INNER FUSELAGE STRUCTURE AT ENTRY DOOR CUTOUT FOR 1-L. INTERCOSTAL HAS CRACK, AFT SIDE OF STA 294.5, STR 12-L. MAJOR R EPAIR ACCOMPLISHED: REPLACED INTERCOSTAL WEB AT STRINGER 12L STA 294.5. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300221 20071213 00221 NM 2007 12 13 SWAA075935 1 20071201 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 433LV 33716 EEPLS LIGHT ASSY DISCONNECTED AT ROW 1 ABC. RECONNECTED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007121300223 20071213 00223 NM 2007 12 13 SWAA075946 1 20071202 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300224 20071213 00224 NM 2007 12 13 SWAA075948 1 20071202 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300225 20071213 00225 NM 2007 12 13 SWAA075961 1 20071202 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300229 20071213 00229 NM 2007 12 13 SWAA075951 1 20071202 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300231 20071213 00231 NM 2007 12 13 SWAA075963 1 20071202 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121300233 20071213 00233 NM 2007 12 13 SWAA075955 1 20071202 A 2824 61163 VALVE BOEING 737 7373T5 1384608 NM RT WING DISCONNECTED A SWAA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SW 29 667SW 23063 DIVERSION / DECLARED EMERGENCY. EN ROUTE TO LAS CROSSFEED VALVE STUCK IN OPEN POSITION. FUEL USED FROM NR 1 TANK ONLY. INSPECTED AND FOUND CROSSFEED VALVE DISCONNECTED. RECONNECTED VALVE PER MM. 2 L 7 2 4F RT A16WE 2007121300236 20071213 00236 2007 12 13 SWAA075937 4 20071202 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 717SA 27851 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007121300245 20071213 00245 NE 2007 12 13 HNAA0700279 2 20071129 A 7321 7898426009 ECU PWA PW120A DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE DEFECTIVE A HNAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 07 825EX 36157 1014 121348 388 121348 NR 2 ENGINE MANUAL CAUTION LIGHT ILLUMINATED AFTER ENGINE START. MEL'D NR 2 ECU. ON 30 NOVEMBER 2007, NR 2 ECU WAS REP LACED. OPERATIONAL CHECK GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2007121300263 20071213 00263 EA 2007 12 13 COMA0770072 1 20071130 A 5210 SEAL CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 376CA 10092 PAX DOOR SEAL NIB PREVIOUS REPAIR APPEARED DAMAGED BY SHOOT BOLT. REMOVED PREVIOUS REPAIR, STRIPPED PAINT, LPI INSPECTE D REPAIR PART AND FOUND NO DAMAGE. REINSTALLED REPAIR PART AND RE-PAINTED IAW REO 670-53-22-001. 2 L 7 2 4F RT A21EA 2007121300265 20071213 00265 EU 2007 12 13 705211272007 1 20071127 A 3310 1179203103 CONTROLLER BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101* NE COCKPIT LIGHT BURNED E QMLA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 NM 03 952CJ S7052 AT APPROXIMATELY 1930, THE PILOT HAD A CIRCUIT BREAKER (POP) AND WAS SHORTLY FOLLOWED BY A BURNING ODOR. ABORTED THE TA KEOFF AND IMMEDIATELY SHUT THE AIRCRAFT DOWN. NOTIFIED THE PROGRAM MAINTENANCE MANAGER WHO INFORMED THE NEXT RUNG ON TH E INFORMATION LADDER. APPROPRIATE INTERCOMPANY REPORTS WERE FILED AND THE FAILURE OF THE COMPONENT WAS LOGGED IN THE MA INTENANCE LOG. THE FLIGHT WAS A TRAINING MISSION. MECHANIC TROUBLESHOT PROBLEM TO LIGHT CONTROLLER. 1 G 7 2 3U 3 U H13EU E5NE 2007121300266 20071213 00266 NE 2007 12 13 HEER118276 1 20071126 A 5311 9220906316 SPAR CAP SKRSKY S92 S92A NE GE CT7TS CT78A 30136 NE FUSELAGE CRACKED B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 192PH 3211 920006 FORWARD SPAR CAP ANGLE AT TOP OF THE DRIVESHAFT TUNNEL IS CRACKED AT TOP OF THE LAST LARGE HL64-8 PIN. CONTACTED MFG FO R 8110 REPAIR. 2 G 7 2 4U 4 U R00024BO E8NE 2007121300267 20071213 00267 EU 2007 12 13 RMXA10282007 1 20071028 A 5302 1173010615 DOUBLER BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101* NE TAILBOOM CRACKED E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 1140H 7078 LT TAILBOOM DOUBLER (FASTENER) HAS A 1.5 INCH LONG CRACK IN THE DOUBLER ONLY. 1 G 7 2 3U 3 U H13EU E5NE 2007121300268 20071213 00268 EU 2007 12 13 RMXA11092007 1 20071109 A 5302 SKIN UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIU2F NE TAILBOOM CRACKED E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 135NP 1860 0068 LADDER FELL OVER AND HIT AGAINST THE RT TAILBOOM SHROUD AND CAUSED A 0.5 INCH LONG CRACK IN THE COMPOSITE STRUCTURE. 1 G 7 2 3U 3 U H88EU E34NE 2007121300278 20071213 00278 EU 2007 12 13 4006 1 20071120 A 2133 14640113 OUTFLOW VALVE AMD FALC20 FALCON20F5 2730105 EU GE CF700 CF7002D2 30010 NE AIR CONDITIONING FAILED E CX0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 15SL 1427 256 AIR CONDITIONING VALVE CIRCUIT BREAKER POPPED AFTER TAKEOFF AND WOULD NOT RESET WHICH PREVENTED THE AIRCRAFT FROM PRESSU RIZING. THE PILOTS REMAINED AT LOWER ALTITUDE WHILE FOLLOWING PROPER PROCEDURES AND LANDED AT THE NEXT AIRPORT. THE PART WAS REPLACED AND THE SYSTEM CHECKED GOOD. WE ARE PRESENTLY WAITING ON A TEARDOWN REPORT OF THE UNIT. TSO 3474.5 2 L 7 2 4F 4 F RT A7EU E7EA 2007121300284 20071213 00284 NM 2007 12 13 SWAA075967 1 20071203 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 380, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007121300308 20071213 00308 NM 2007 12 13 SWAA075978 1 20071203 A 5751 DAS520A1509 BEARING BOEING 737 7373H4 1384600 NM LT AILERON WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED BRDG CHECK, LT AILERON FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BEARING AND BUSHING PE R MM. 2 L 7 2 4F RT A16WE 2007121300352 20071213 00352 NM 2007 12 13 2007UALA04887 1 20071129 A 5320 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 LIGHTNING STRIKE DAMAGE AT STATIONS 490, 520 & 550 STR 6L. REPLACED BLIND FASTENERS WITH SOLID FASTENERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121300355 20071213 00355 NM 2007 12 13 2007UALA04888 1 20071129 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 LIGHTNING STRIKE STA 1530 STRINGER 3L & STA 1163 BTWEEN STRINGERS 5&6 MIDDLE OF FIELD. REPLACED FASTENERS WITH SOLID RI VETS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121300376 20071213 00376 NM 2007 12 13 2007UALA04894 1 20071129 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN UNSECURE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 661UA 27158 EMERGENCY LIGHTS GO ON AND OFF ROW 16 AND 22. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121300392 20071213 00392 NM 2007 12 13 2007UALA04910 1 20071130 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 SKIN DENT AT STA 334, BETWEEN STR 24 AND 25R. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121400001 20071214 00001 NM 2007 12 14 HALA0700517 1 20071204 A 3010 DETECTOR BOEING 717 717200 1383700 NM ICE DETECTION MALFUNCTIONED A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 478HA 55123 WING ICE RT FAIL INDICATION. CLEANED WATER OUT OF RIGHT WING ICE DETECTOR, OPS CHECK GOOD, CLEARED MIC SHEET, REMOVED P LACARD. 2 L 7 2 4F TR A6WE 2007121400026 20071214 00026 NM 2007 12 14 SWAA075998 1 20071204 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730D, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007121400039 20071214 00039 2007 12 14 SWAA076006 4 20071204 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007121400045 20071214 00045 EA 2007 12 14 COMA0760682 1 20071130 A 3397 59465 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN FAULTY A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 436CA 7482 FLIGHT 5286 - EMERGENCY LIGHTS INOP FROM ROW 8, ALL THE WAY AFT. REPLACED AFT EEL PATH FEEDER WIRE. NO FURTHER DEFECTS . 2 L 7 2 4F RT A21EA 2007121400051 20071214 00051 2007 12 14 ZZDA2007307 4 20071203 A 2565 D29982225 SLIDE BOEING 717 717200 1383700 NM R1 DOOR DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 955AT 55017 R-1 GALLEY DOOR EVAC SLIDE ARMING STRIP LOOSE STICKING OUT OF SLIDE PACK (LANYARD ASSY). REMOVED AND REPLACED R1-DOOR S LIDE PER MM 25-61. 2 L 7 2 4F TR A6WE 2007121400060 20071214 00060 WP 2007 12 14 ABXR070391 1 20071002 A 5320 39164111 ANGLE DOUG DC9 DC915 3022036 WP LT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 784TW 47014 ANGLE CRACKED AT INBOARD END OF SLANT PANEL. REMOVED AND REPLACED FITTING INBOARD END OF SLANT PANEL IAW DC9 SRM. 2 L 7 2 4F A6WE 2007121400093 20071214 00093 WP 2007 12 14 IXXA07SMN239S 1 20071110 A 5330 SKIN DOUG DC8 DC873F 302199F WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT FUSELAGE NOSE SECTION ACS MODIFICATION DOUBLER HEAT INTERCHARGER COMPARTME NT LOWER AFT JAMB CORNER CRACKED AT STATION FS 12.000 LONGERON 27 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED EXTERNAL AND INTERNAL DOUBL ER CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-11, 51-1-20D, 51-3-1, FOR M FAA 8110-3 NUMBER 07569 DATED 11-27-07 SEMAN DRAWING NUMBER ED-4644 DATED 11-09-07, DC8 SRM 51-1-21, 51-3-0, DC8 NDT S PM PART 08-00-02 TO 07, FORM SMN 242-4, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007121400106 20071214 00106 NM 2007 12 14 SWAA076024 1 20071205 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT E&E EXHAUST PORT BS 378, LBL 2.8. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007121400115 20071214 00115 WP 2007 12 14 IXXA07SMN251S 1 20071115 A 5340 4772397U1 FITTING DOUG DC8 DC873F 302199F WP ZONE 200 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE A CRACK AT SPLICE FITTING AT STATION 1766.000 LONGERON17 LEFT. RE MOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-3-0, 51-3-1. 2 L 7 4 4F RT 4A25 2007121400129 20071214 00129 WP 2007 12 14 NWAA073949868 1 20071203 A 2910 836SD620 FUSE DOUG DC9 DC951 3022051 WP HYD EDP LEAKING A NWAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 01 777NC 67147 67147 47787 THE RIGHT HYDRAULIC SYSTEM FLUID QUANTITY DROPPED TO ZERO DURING TAXI FOR TAKEOFF. COM PROCEDURES WERE COMPLIED WITH. DUE TO A POSSIBLE LOSS OF BRAKING ACTION THE AIRCRAFT WAS TOWED BACK TO THE GATE. MAINTENANCE FOUND THAT THE NR 4 POSIT ION UPPER BRAKE FUSE WAS BROKEN AND HAD COME APART. THE FUSE WAS REPLACED AND LEAK CHECKED. THE ELECTRIC HYDRAULIC PUM P, THE ENGINE DRIVEN HYDRAULIC PUMP, THE HYDRAULIC FLUID QUANTITY LIMITER, AND THE FILTERS FOR THE RIGHT HYDRAULIC SYSTE M WERE ALL REPLACED. ASSORTED HYDRAULIC LINES WERE ALSO REPLACED. FUNCTIONAL CHECKS WERE GOOD AND THE AIRCRAFT HAS RET URNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007121400142 20071214 00142 EU 2007 12 14 CPCP20070121 1 20071119 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 342AT 345 RT SEAT TRACK BETWEEN FRAME 39-40 CORRODED. NEW RT SEAT TRACK BETWEEN FRAME 39-40 IS INSTALLED IAW SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007121400145 20071214 00145 EU 2007 12 14 CPCP20070123 1 20071119 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 345 345 RT SEAT TRACK BETWEEN FRAME 36-39 CORRODED. NEW RT SEAT TRACK BETWEEN FRAME 36-39. INSTALLED IAW SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007121400147 20071214 00147 EU 2007 12 14 CPCP20070124 1 20071119 A 5320 PLATE AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 342AT 345 LT GUTTER PLATE ON FORWARD CARGO DOOR THRESHOLD BETWEEN FRAME 14 TO 17 IS CORRODED. LT GUTTER PLATE ON FORWARD CARGO DO OR THRESHOLD BETWEEN FRAME 14 TO 17, REPLACED AS PER SRM 51-25-01 AND SRM 51-25-03. 2 H 7 2 4T RT A53EU 2007121400170 20071214 00170 NM 2007 12 14 DLM88071605 1 20071209 A 5512 5922578517 SKIN DOUG MD88 MD88 3023688 NM HORIZONTAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 920DL 49644 MISSING TAB ON REPLACEMENT LT LOWER AFT SKIN PANEL ON HORIZ STAB. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F RT A6WE 2007121400173 20071214 00173 2007 12 14 F3LA200700367 4 20071210 A 2565 D5211009820000 HOOK AIRBUS A319 A319112 3930323 EU R2 DOOR SLIDE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 901FR 5849 1488 DURING C-5 CHECK, INSPECTION REPORTED UPON INSTALLATION OF R2 DOOR SLIDE, OPEN/CLOSE HANDLE COULD BE OPERATED BEFORE DOO R WAS IN HOLE. REMOVED AND REPLACED HOOK ON DOOR LOCKING MECHANISM AND PERFORMED OPS CHECK AND RIG CHECK IAW AMM 52-13- 21-400-001. 2 L 7 2 4F RT A28NM 2007121400202 20071214 00202 EU 2007 12 14 07FDEA05026 1 20071211 A 5313 FX5310141N311 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 805FD 456 FWD PIT BETWEEN FR 39 AND FR 38.2 STGR 53 LT HAS CORROSION REMOVED CORROSION FOUND TO BE OUT OF LIMIT IAW SRM 53-10-14. FAB`D STRINGER DOUBLER IN T7/711755. REMOVED AND REPLACED STRG DOUBLER AND COUPLING IAW 51-40-44. 2 L 7 2 4F RT A35EU 2007121400210 20071214 00210 NM 2007 12 14 07FDEA05036 1 20071212 A 5510 65727961 PIVOT BOEING 727 727233 138408A NM STAB DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 RT AFT PIVOT POINT ON STAB HAS PLAY. REMOVED HORIZONTAL STAB. REPLACED HORIZONTAL STAB HINGE PINS IAW MM 55-10-001-4. REINSTALLED, ADJUSTED & OPS CHECKED HORIZONTAL STAB & ELEVATOR CONTROL SYS. IAW MM 55-10-001-4 & MM 27-30-000-5. STABI LIZER HINGE BUSHINGS REPLACED ON EA 7-5510-113960, HORIZONTAL STAB TRIM & ELEVATER CONTROL SYS CHECKED GOOD. REPAIR C LASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007121400211 20071214 00211 NM 2007 12 14 07FDEA05037 1 20071212 A 5720 652811521 FAIRING BOEING 727 727233 138408A NM LT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 LT WING FLAP O/B TRACK FAIRING O/B ATTACH FLANGE HAS CRACK JUST AFT OF TRACK AFT MOUNT POINT. REMOVED ATTACHED FLANGE , FABRICATED, LOCATED AND DRILLED NEW ATTACH FLANGE, ALODINED AND PRIMED AND INSTALLED REF SRM 51-30-2, DWG 65-28115, AN D SRM 51-10-2 PG 7, 11-12. 2 L 7 3 4F RT A3WE 2007121400220 20071214 00220 NM 2007 12 14 2007UALA04941 1 20071203 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 502UA 24623 DOOR 3R SLIDE LIGHT WILL NOT ILLUMINATE. FOUND BATTERY PACK WEAK AND NOT CHARGING. REPLACED BATTERY PACK AND CHARGER. ALL SYSTEMS FUNCTION/TEST NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121400225 20071214 00225 SO 2007 12 14 SIMA200734601 1 20071207 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO ZONE 200 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 670AE 9594 5000 145790 DURING INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND TO HAVE TWO SMALL AREAS CORRODED BEYOND MANUAL LIMITS. REMOVED CORROSION IAW EMB SRM PERFORMED EDDY CURRENT WITH NO REJECTABLE INDICATIONS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007121400226 20071214 00226 2007 12 14 2007UALA04944 4 20071203 A 2565 CYLINDER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 663UA 27160 RIGHT OVERWING SLIDE CYLINDER BOTTLE BALL IS BELOW THE SPRING FORCE MECHANISM. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121400227 20071214 00227 2007 12 14 SIMA200734609 4 20071210 A 3430 7510100831 INU EMB 145 EMB145LR 3260212 SO NR 1 MALFUNCTIONED A SIMA A UNSCHED LANDING O OTHER AP APPROACH 1 SW 21 625AE 145115 RMU 1 NAV 1 FREQUENCY WINDOW DASHES ONLY FREQUENCY NOT SELECTABLE. REMOVED AND REPLACED NR 1 INERTIAL NAVIGATION UNIT I AW EMB MM 34-32-01. OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007121400228 20071214 00228 EA 2007 12 14 A6WA200740608 1 20071102 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 426AW 7669 BRACKET CRACK AT JUNCTION OF NET POST AND AFT PRESSURE BULKHEAD FORWARD FACE, FS 621, CARGO BAY AREA. BRACKET FABRIATED IAW CRJ SRM 53-61-23 AND SRM 51-24-16, AND INSTALLED IAW CRJ 20 SRM 51-42-20. (M) 2 L 7 2 4F RT A21EA 2007121400234 20071214 00234 NM 2007 12 14 2007UALA04949 1 20071204 A 5320 ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 INNER FUSELAGE STRUCTURE AT DOOR CUTOUT 1L, L-ANGLE UNDER INTERCOSTAL WEB IS CRACKED STA 294.5+7 INCHES AT STR 13-L. MA JOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED LWR HINGE BOX DOUBLER BS 294. REINFORCEMENT CLIPS, AUX INTERCOSTAL & R EPLACEMENT 'H' STRAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121400236 20071214 00236 NM 2007 12 14 2007UALA04951 1 20071204 A 5320 ATTACH ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 MED 1L, BS 294 UPPER HINGE BOX LOWER AUX INTERCOSTAL ATTACH ANGLE CRACKED DURING FASTENER REMOVAL. MAJOR REPAIR ACCOMPL ISHED: FABRICATED & INSTALLED UPPER HINGE BOX LWR AUX INTERCOSTAL ATTACH ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121400238 20071214 00238 NM 2007 12 14 2007UALA04953 1 20071204 A 5320 ATTACH BRACKET BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 INNER FUSELAGE STRUCTURE AT FWD ENTRY DOOR CUTOUT INTERCOSTAL ATTACH BRACKET CRACKED AFT SIDE OF BS 294.5 AT STRINGER 11 L. MAJOR REPAIR ACCOMPLISHED: REPAIRED INTERCOSTAL ATTACH BRACKET. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121400240 20071214 00240 WP 2007 12 14 NWAA074019995 1 20071211 A 5230 DOOR DOUG DC9 DC931 3022065 WP CARGO DOOR OUT OF RIG A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 8978E 47327 ABORTED TAKEOFF SAFELY AT APPROXIMATELY 100 KNOTS DUE TO A COCKPIT WARNING THAT THE AFT CARGO DOOR WAS OPEN. COM PROCED URES WERE COMPLIED WITH AND THE AIRCRAFT TAXIED BACK TO THE GATE UNDER ITS OWN POWER. MAINTENANCE INSPECTED THE AFT CAR GO DOOR AND FOUND IT TO BE SECURELY CLOSED AND THAT THERE WERE NO DISCREPANCIES WITH THE DOOR WARNING INDICATOR SYSTEM. MSP MAINTENANCE INSPECTED AFT CARGO DOOR, OPENED AND CLOSED OK. DISCOVERED AFT CARGO DOOR INDICATION SWITCH LOOSE, RES ECURED SWITCH AND DEFERRED PER MEL 52-7E. AIRCRAFT WAS RETURNED TO SERVICE. FURTHER INSPECTION FOUND DOOR HARD TO OPEN AND CLOSE AND OUT OF RIG. RERIGGED DOOR AND PRESSURIZED AIRCRAFT TO ADJUST DOOR STOPS PER AMM 52-31-00. CLEARED MEL A 2 L 7 2 4F A6WE 2007121400241 20071214 00241 WP 2007 12 14 07FDEA05024 1 20071211 A 5311 FRAME DOUG DC10 DC1010 3022110 WP ZONE 200 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 371FE 46609 MAIN CABIN FOUND 1 CRACK ON FRAME STA 1741 STR 14 RT REPAIRED IAW SRM 53-30-00 FIG 5 VOL I AND EA NR 8-5380-111563. 2 L 7 3 4F A22WE 2007121400247 20071214 00247 NM 2007 12 14 2007UALA04955 1 20071204 A 5320 ATTACH BRACKET BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 INNER FUSELAGE STRUCTURE AFT OF DOOR CUTOUT FOR 1-L, INTERCOSTAL WEB ATTACH BRACKET IS CRACKED, FWD SIDE OF STA 360, STR 11-L. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKED INTERCOSTAL & ACCMP NDT OF OPEN HOLES. FABRICATED & INSTALLED NEW I NTERCOSTAL (P/N 69-45985-6). 2 L 7 2 4F 4 F RT A16WE E21EU 2007121400248 20071214 00248 NM 2007 12 14 AMTA200700602 1 20071116 A 5320 FLOOR SUPPORT BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE BS 1660-1675 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 522AT 29330 CABIN FLOOR STRUCTURE UPPER SURFACE HAS CORROSION AT STA 1660 TO 1675, LBL 48. REMOVED CORROSION ON FLOOR SUPPORT STRUC TURE STA 1660-1675, LBL48 IAW SSRM 51-20-01 ORG=IG. MAT .071, CORROSION 100 PERCENT THRU OUT OF LIMITS IAW SRM 53-00-51, FIG 101, FLOOR SUPPORT, REMOVED AND REPLACED FLOOR SUPPORT STA 1660-1675, IAW SRM 51-40-00. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007121400250 20071214 00250 NM 2007 12 14 2007UALA04956 1 20071204 A 5712 RIB BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 NR 1 MAIN FUEL TANK LT RIB LOWER CHORD CRACKED WBL135.5 BETWEEN WING STRINGERS S2 AND S3. CRACK IS APPROXIMATELY 1 INCH LONG & ORIGINATES IN THE CUTOUT RADIUS OF THE LOWER RIB CHORD. MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT DAMAGE. FABRIC ATED & INSTALLED REPAIR TEE, VERTICAL STIFFENER & FILLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121400252 20071214 00252 NM 2007 12 14 2007UALA04958 1 20071204 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 STA 365.25 FLOORBEAM CORRODED FROM LBL 24 .75 TO RBL 45.5. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGED T-CAP. FABRICATE D & INSTALLED NEW CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121400253 20071214 00253 NM 2007 12 14 2007UALA04959 1 20071204 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 AFT PIT BS 1360 FRAME HAS DENT AND MINOR SURFACE CORROSION AT STR 25L. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SECT ION OF FRAME. FABRICATED & INSTALLED A REPAIR ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121400254 20071214 00254 NM 2007 12 14 2007UALA04960 1 20071204 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 R-4 DOOR LOWER GATE MATING SURFACE WORN AND CORRODED IN SEVERAL AREAS ALONG EDGES. INSTALLED NEW GATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121400257 20071214 00257 NM 2007 12 14 2007UALA04963 1 20071204 A 2560 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FLASHLIGHT DISCHARGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 802UA 690 AFT JUMP SEAT EMERGENCY FLASH LIGHT RED STS LIGHT DOES NO BLINK. FOUND RECHARGEABLE BATTERY INOPERATIVE. REPLACED FLA SH LIGHT BATTERY, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121400261 20071214 00261 NM 2007 12 14 AMTA200700608 1 20071118 A 5345 SUPPORT FITTING BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 552TZ 32586 BEAM BOX AND LAV SUPPORT FITTING CORRODED BETWEEN STA 334 AND 345, WL 208, LBL 20. REMOVED 2 EA SUPPORT STIFFENERS AT S TA 345, REMOVED FLOOR SUPPORT FITTING, FABRICATED NEW FITTING. INSTALLED NEW FITTING AND STIFFENERS, APPLIED CIC PROTEC TION IAW 51-40-02, SO OPM 20-41-05, 51-40-05. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007121400262 20071214 00262 NM 2007 12 14 2007UALA04966 1 20071204 A 3350 COVER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS MISSING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY EXIT LIGHT SWITCH COVER MISSING AT DOOR L1 STATION. SWITCH GUARD BROKEN REMOVED GUARD FROM DR 2L GRD SVC SW & INSTALLED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121400263 20071214 00263 NM 2007 12 14 2007UALA04967 1 20071204 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 669UA 30025 EMERGENCY ESCAPE PATH LIGHT AT SEATS 10HJ AND 16AB MISSING. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121400264 20071214 00264 CE 2007 12 14 DXTA200702630 1 20071127 A 2120 UNKNOWN CESSNA 560 560XL 2076702 CE CABIN ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 592QS 5605706 WHILE ON GROUND WITH APU RUNNING AND BLEED AIR ON HAD BURNING ODOR COMING THRU COCKPIT DUCTS. REMOVED & REPLACED DEFECT IVE TEMP CONTROLLER OPERATIONAL CHECK OF ECS SYSTEM NORMAL. WORK PERFORMED IAW MM 21-61-00 & 21-51-00. 2 L 7 2 4F RT A22CE 2007121400267 20071214 00267 CE 2007 12 14 M001095 1 20071205 A 2121 1013841001 MOTOR AEROSPACECMP 50041 BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A60A 52043 NE BLOWER SEIZED E VQMA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 NM 03 725MC 185 185 1617 BB169 ON NOVEMBER 30, AC WAS SIXTY MILES OUT ENROUTE AND THE CREW NOTICED AN ODOR IN THE CABIN. ON FINAL APPROACH, SMOKE BEGAN COMING OUT OF THE CABIN HEAT VENTS AND THE CREW EXPEDITED TO LANDING. UPON LANDING THE SMOKE DISSIPATED WITH WINDOW VEN TS OPENED, BUT AS A PRECAUTION THEY CALLED TOWER AND REQUESTED FIRE EQUIPMENT, AND EVACUATED THE PASSENGERS THRU THE MAI N DOOR. THE AIRCRAFT WAS GROUNDED UNTIL MAINTENANCE ARRIVED. WHEN MAINTENANCE ARRIVED THEY DISCOVERED THE FORWARD CABIN VENT BLOWER SEIZED. A OVERHAULED UNIT WAS INSTALLED, FUNCTIONAL TESTED AND THE AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 4T 4 T A24CE E4EA 2007121400268 20071214 00268 NM 2007 12 14 2007UALA04968 1 20071203 A 5610 141W74001 WINDOW BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE COCKPIT FAULTY A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 219UA 30551 STATUS MSG, `WINDOW HEAT L FWD` DISPLAYED MAINT MSG 30-21031. FOUND OPEN CIRCUITS ON PRIMARY AND SPARE SENSORS ON WIND OW. REPLACED WINDOW PER 56-11- 01. AC OK FOR SERVICE 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121400270 20071214 00270 EU 2007 12 14 2007UALA04970 1 20071205 A 3350 LAMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 421UA 500 EMERGENCY LIGHT TEST FAILS WITH MESSAGE EXT LOAD. FOUND SEVERAL LAMPS BURNT OUT ON O/W EXITS (EXTERIOR). RELAMPED ASSY S- SYSTEM TESTED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121400272 20071214 00272 NM 2007 12 14 2007UALA04972 1 20071205 A 3350 LAMP BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY SIGN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 923UA 26643 RIGHT LOWER EMERGENCY EXIT SIGN ROW 9 INOPERATIVE. RELAMPED 2 L 7 2 4F 4 F RT A16WE E21EU 2007121400275 20071214 00275 NM 2007 12 14 2007UALA04975 1 20071205 A 3350 1619 LIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 923UA 26643 ROW 12 BULLNOSE LIGHT INOPERATIVE. REPLACED LIGHT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121400276 20071214 00276 NM 2007 12 14 2007UALA04976 1 20071205 A 5241 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 50961 24640 FWD GALLEY DOOR FWD CUTOUT CRACKED BETWEEN STR 12R & STR 13R. MAJOR REPAIR ACCOMPLISHED BY REPLACING WEB ANGLE. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121400277 20071214 00277 NM 2007 12 14 2007UALA04977 1 20071205 A 5313 STRINGER SPLICE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 360 S15L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 50961 24640 STRINGER SPLICE CRACKED AT STR 15L ON LOWER FLANGE AT BS 360. SUSPECT NORMAL AC OPERATION. MAJOR REPAIR ACCOMPLISHED BY REPLACING STRINGER SPLICE. AC OK FOR SERVICE 2 L 7 2 4F 4 F RT A16WE E21EU 2007121400278 20071214 00278 NM 2007 12 14 2007UALA04978 1 20071205 A 5320 ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 FWD GALLEY DOOR FWD CUTOUT AT BS 294.5 INTERCOSTAL WEB ANGLE CRACKED BETWEEN STRINGER S9R & S10R. SUSPECT NORMAL AC OPE RATION. REMOVED & REPLACED ANGLE. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121400284 20071214 00284 NM 2007 12 14 2007UALA04984 1 20071205 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 577UA 26693 EEL LIGHT STRIP SEGMENT AFT OF SEAT 6B INOPERATIVE. FOUND LAMP ASSY BURNED OUT. REPLACED LIGHT ASSY (RELAMPED). 2 L 7 2 4F 4 F RT A2NM E17NE 2007121400285 20071214 00285 NM 2007 12 14 2007UALA04985 1 20071205 A 5210 SPRING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR BROKEN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 577UA 26693 DOOR 4R MODE SELECTOR GUARD FOR SLIDE HAS BROKEN SPRING. REPLACED SELECTOR GUARD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121400286 20071214 00286 NM 2007 12 14 2007UALA04986 1 20071205 A 5210 GUARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 577UA 26693 DOOR 4L MODE SELECTOR GUARD DOES NOT PREVENT SLIDE HANDLE FROM BEING MOVED. FOUND SELECTOR GUARD OUT OF ADJUSTMENT. A DJUSTED SELECTOR GUARD, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121400288 20071214 00288 NM 2007 12 14 2007UALA04988 1 20071204 A 3510 HOSE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT DEFECTIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 568UA 26674 OXYGEN MASK HOSE DEFECTIVE AT 1(1=CAPT, 2=1ST OF, 3= 1ST OBS). CREW COMMENTS: CAPT O2 MASK DOES NOT FIT SNUG OR HOSE C OMPLETELY INFLATE WHEN PUT ON. FOUND DIAPHRAGM STIFFENED PER SHOP FINDINGS. REPLACED MASK ASSY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121400289 20071214 00289 NM 2007 12 14 ASAA0742353 1 20071205 A 5210 MS166241037 RETAINING RING BOEING 737 7374Q8 138447Q NM L1 DOOR OUT OF POSITION A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 L1 DOOR HARD TO OPEN. FOUND RETAINING RING OFF PIN. RE-ATTACHED RING TO PIN. OP CHECKS GOOD. REF ILLUSTRATION FROM M M 52-11-21 PG 402. 2 L 7 2 4F RT A16WE 2007121400291 20071214 00291 SO 2007 12 14 C2XA07ON033 1 20071205 A 2810 2770138101 FLAPPER VALVE EMB 145 EMB145XR 3260214 SO FUEL SYSTEM WORN A C2XA D RETURN TO BLOCK K FLUID LOSS UK UNKNOWN 1 SW 27 11547 145563 FL 0060 - TUS TO OMA - FLIGHT CREW REPORTED FUEL LEAK ON LT WING. FLIGHT CREW RETURNED TO BLOCK AND MX PERSONNEL IAH RE COVERY REMOVED AND REPLACED FLAPPER VALVE, OPERATIONALLY AND LEAK CHECK SATISFACTORY. A/C WAS RELEASE TO RETURN FOR SER VICE IN AIRWORTHY CONDITIONS. 2 L 7 2 4F RT 2007121400294 20071214 00294 NM 2007 12 14 HNAA0700282 1 20071202 A 2611 PU90461S SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM LAVATORY MALFUNCTIONED A HNAA O OTHER N FALSE WARNING UK UNKNOWN 1 EA 07 805EX 41993 41993 228 LAVATORY SMOKE DETECTOR WAS SOUNDING OFF WITH OUT BEING SMOKE SEEN. REMOVED AND REPLACED SMOKE DETECTOR. 2 H 7 2 4T RT A13NM 2007121400295 20071214 00295 NM 2007 12 14 HNAA0700283 1 20071201 A 7600 JV5 SWITCH DHAV DHC8 DHC8102 2809003 NM COCKPIT OUT OF RIG A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 807EX 40106 40106 292 TAKEOFF WARNING HORN SOUNDED DURING TAKEOFF ROLL, ABORTED TAKEOFF, CYCLED ALL APPROPRIATE SWITCHES AND LEVERS, NO FIX. FOUND NR 1 CONDITION LEVER SWITCH OUT OF RIG. RIGGED SWITCH AND LUBED. GROUND RAN AIRCRAFT, SYSTEM OPERATIONAL CHECK G OOD. 2 H 7 2 4T RT A13NM 2007121400296 20071214 00296 NM 2007 12 14 HNAA0700284 1 20071202 A 3350 1013075 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A HNAA K NONE O OTHER NR NOT REPORTED 1 EA 07 809EX 40005 40005 302 FLOOR LEVEL EMERGENCY LIGHTING AT ROW 4 IS BROKEN. REINSTALLED ONE RED EMERGENCY FLOOR LIGHT CAPTION. OPERATIONAL CHEC K GOOD. 2 H 7 2 4T RT A13NM 2007121400297 20071214 00297 NM 2007 12 14 SCNA07014 1 20071205 A 3350 BATTERY PACK BOEING 737 7378Q8 13844BX NM CABIN FAILED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 801SY 30332 DURING A FUNCTIONAL CHECK MAINTENANCE FOUND THE EMERGENCY LIGHT BATTERY BACKS AT R1, R2, AND L2 DOORS FAILED CAPACITY CH ECK. MAINTENANCE THEN REPLACED THE BATTERY PACKS AT THE R1, R2, AND L2 DOOR. 2 L 7 2 4F RT A16WE 2007121400298 20071214 00298 NM 2007 12 14 SCNA07015 1 20071205 A 3350 BATTERY PACK BOEING 737 7378Q8 13844BX NM CABIN FAILED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 801SY 30332 DURING A FUNCTIONAL CHECK MAINTENANCE FOUND THE EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY CHECK AT DOORS L1, L2, AND R2. MAINTENANCE REPLACED THE BATTERY PACKS AT THE L1, R1, R2 DOORS. 2 L 7 2 4F RT A16WE 2007121400299 20071214 00299 NM 2007 12 14 SWAA076038 1 20071206 A 5753 6546430129 SKIN BOEING 737 7375H4 138449D NM FOREFLAP DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED C2 CHECK, FOUND LT WING FORE FLAP UPPER SURFACE DISBONDED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007121400300 20071214 00300 NM 2007 12 14 SWAA076039 1 20071206 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121400303 20071214 00303 NM 2007 12 14 ZZDA2007309 1 20071207 A 5320 PAN BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 957AT 55019 FWD CARGO COMP LOWER PAN CORRODED BEYOND LIMITS. REPAIR FWD CARGO COMP LOWER SECTION OF JAMB PAN IAW B717 53-20-15 REP 6. 2 L 7 2 4F TR A6WE 2007121400305 20071214 00305 NM 2007 12 14 ASAA0742354 1 20071204 A 5330 6551626418 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 760AS 25098 WATER SERVICE TRUCK PULLED AWAY FROM AIRCRAFT WITH THE HOSE CONNECTED TO SERVICE PANEL RIPPING OUT NIPPLE AND PAN ATTACH MENT. REMOVED AND REPLACED PAN AND ASSOCIATED FITTING IAW SRM 51-40-02 & EA5330 02272. 2 L 7 2 4F RT A16WE 2007121400306 20071214 00306 EU 2007 12 14 TRAX200701862 1 20071203 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 635AS 372 CABIN FLOOR EMERGENCY LIGHT TRACK HAS A LIGHT OUT AT SEAT 17B. 2 H 7 2 4T RT 2007121400308 20071214 00308 EA 2007 12 14 TRAX200701864 1 20071203 A 5220 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 CREW ESCAPE HATCH FRAME AT FS 276.00 HAS CRACK AT LBL 8.5 FROM CREW ESCAPE HATCH HINGE ARM. REPAIRED IAW REO 601R-53-11 -1296. COMPLIED WITH ASA EC/TC REO 601R-53-11-1296. 2 L 7 2 4F RT A21EA 2007121400309 20071214 00309 EA 2007 12 14 TRAX200701865 1 20071203 A 5320 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 905EV 7632 CARGO DOOR SUPPORT BEAM ANGLE THAT ATTACHES TO REAR PRESSURE BULKHEAD IS CRACKED APPROX .2 INCH IN LENGTH. 2 L 7 2 4F RT A21EA 2007121400310 20071214 00310 EA 2007 12 14 TRAX200701866 1 20071203 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 900EV 7608 FLAPS FAILED AT ZERO WHEN SELECTING 8 ON DESCENT. EMERGENCY EQUIPMENT ON STANDBY. FLT 4257 DEL 115 MINS. 2 L 7 2 4F RT A21EA 2007121400312 20071214 00312 EA 2007 12 14 TRAX200701870 1 20071205 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 826AS 7210 NR 1 EMERGENCY LIGHT BATTERY WILL NOT TURN ON LIGHTS. 2 L 7 2 4F RT A21EA 2007121400313 20071214 00313 EA 2007 12 14 TRAX200701871 1 20071205 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 826AS 7210 NR 2 EMERGENCY LIGHT BATTERY WILL NOT TURN ON LIGHTS. 2 L 7 2 4F RT A21EA 2007121400314 20071214 00314 EA 2007 12 14 TRAX200701872 1 20071205 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 826AS 7210 NR 3 EMERGENCY LIGHT BATTERY WILL NOT TURN ON LIGHTS. 2 L 7 2 4F RT A21EA 2007121400317 20071214 00317 EA 2007 12 14 TRAX200701875 1 20071205 A 3260 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA COCKPIT ACTIVATED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 719EV 10099 EXTENDED GEAR HANDLE IN THE DOWN POSITION, GOT A GEAR DISAGREE WARNING MSG, FOLLOWED QRH FOR MANUAL EXTENSION. LANDED W ITHOUT FURTHER INCIDENT. EMERGENCY DECLARED. EMERGENCY EQUIPMENT ON STANDBY. FLT 4646 CX. 2 L 7 2 4F RT A21EA 2007121400318 20071214 00318 EA 2007 12 14 TRAX200701876 1 20071206 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 879AS 7600 CENTER EMERGENCY EXIT LIGHT HAS 4 BULBS INOP. 2 L 7 2 4F RT A21EA 2007121400319 20071214 00319 EA 2007 12 14 TRAX200701877 1 20071206 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 681BR 7680 RECEIVED FLAPS FAIL MESSAGE AT 0 DEGREES IN FLIGHT. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007121400320 20071214 00320 EA 2007 12 14 TRAX200701878 1 20071206 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 900EV 7608 FLAPS FAILED AT 0 DEGREES, LANDED IN MOBILE 0 DEGREES FLAPS 165KTS, 42000 LBS, HIGHEST BREAK TEMP 05. EMERGENCY DECLARE D. EMERGENCY EQUIPMENT ON STANDBY. 2 L 7 2 4F RT A21EA 2007121400321 20071214 00321 NM 2007 12 14 PIDA07055 1 20071205 A 5320 TIE CLIP BOEING 737 737228 13844AG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 252TR 23001 DURING MAINTENANCE CHECK, NOTED STRINGER TIE CLIP CRACKED AT BS 787 AT STR 9RT. REPLACED TIE CLIP PER SRM 51-30-2. 2 L 7 2 4F RT A16WE 2007121400322 20071214 00322 NM 2007 12 14 PIDA07056 1 20071205 A 5320 TIE CLIP BOEING 737 737228 13844AG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 252TR 23001 DURING MAINTENANCE CHECK, NOTED STRINGER TIE CLIP CRACKED AT BS 767 AT STR 9RT. REPLACED TIE CLIP PER SRM 51-30-2. 2 L 7 2 4F RT A16WE 2007121400323 20071214 00323 NM 2007 12 14 PIDA07044 1 20071204 A 5320 TIE CLIP BOEING 737 737228 13844AG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 252TR 23001 DURING MAINTENANCE INSPECTION, NOTED CRACK IN STRINGER TIE CLIP AT BS 597 AT STR 8RT. REPLACED TIE CLIP PER SRM 51-30-2 . 2 L 7 2 4F RT A16WE 2007121400325 20071214 00325 NM 2007 12 14 PIDA07045 1 20071204 A 5320 TIE CLIP BOEING 737 737228 13844AG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 252TR 23001 DURING MAINTENANCE CHECK, NOTED CRACK IN STRINGER TIE CLIP AT BS 639 AT STR 3RT. REPLACED TIE CLIP PER SRM 51-30-2. 2 L 7 2 4F RT A16WE 2007121400327 20071214 00327 NM 2007 12 14 PIDA07050 1 20071205 A 5320 TIE CLIP BOEING 737 737228 13844AG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 252TR 23001 DURING MAINTENANCE CHECK, NOTED STRINGER TIE CLIP CRACKED AT BS 787 AT STR 9LT. REPLACED TIE CLIP PER SRM 51-30-2. 2 L 7 2 4F RT A16WE 2007121400329 20071214 00329 CE 2007 12 14 DXTA200702652 1 20071205 A 2751 SENSOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS DIRTY E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 900QS 7500123 ON FLAP RETRACTION AFTER T/O FLAPS AND SLATS CAME UP BUT AMBER FLAP FAIL LIGHT CAME ON - WOULD NOT RESET. REMOVED FLAP SELECTOR AND REMOVED LINT FROM OPTICAL SENSORS. IAW MM 27-50-00. OPS CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007121400330 20071214 00330 NM 2007 12 14 PIDA07053 1 20071205 A 5320 TIE CLIP BOEING 737 737228 13844AG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 252TR 23001 DURING MAINTENANCE CHECK, NOTED STRINGER TIE CLIP CRACKED AT BS 827 AT STR 5LT. REPLACED TIE CLIP PER SRM 51-30-2. 2 L 7 2 4F RT A16WE 2007121400331 20071214 00331 NM 2007 12 14 PIDA07054 1 20071205 A 5320 TIE CLIP BOEING 737 737228 13844AG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 252TR 23001 DURING MAINTENANCE CHECK, NOTED STRINGER TIE CLIP CRACKED AT BS 827 AT STR 10LT. REPLACED TIE CLIP PER SRM 51-30-2. 2 L 7 2 4F RT A16WE 2007121400333 20071214 00333 NM 2007 12 14 PIDA07047 1 20071205 A 5320 TIE CLIP BOEING 737 737228 13844AG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 252TR 23001 DURING MAINTENANCE CHECK, NOTED STRINGER TIE CLIP CRACKED AT BS 706 AT STR 4LT. REPLACED TIE CLIP PER SRM 51-30-2. 2 L 7 2 4F RT A16WE 2007121400334 20071214 00334 NM 2007 12 14 PIDA07048 1 20071205 A 5320 TIE CLIP BOEING 737 737228 13844AG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 252TR 23001 DURING MAINTENANCE CHECK, NOTED STRINGER TIE CLIP CRACKED AT BS 639 AT STR 2LT. REPLACED TIE CLIP PER SRM 51-30-2. 2 L 7 2 4F RT A16WE 2007121400336 20071214 00336 NM 2007 12 14 PIDA07049 1 20071205 A 5320 TIE CLIP BOEING 737 737228 13844AG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 252TR 23001 DURING MAINTENANCE CHECK, NOTED STRINGER TIE CLIP CRACKED AT BS616 AT STR 4LT. REPLACED TIE CLIP PER SRM 51-30-2. 2 L 7 2 4F RT A16WE 2007121400338 20071214 00338 EU 2007 12 14 UPS07151262 1 20071207 A 2120 A/C PACK AIRBUS A300 A300F4622R 3930360 EU COCKPIT SMOKE A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 150UP 0833 INSPECTION TYPE:N/A DURING LOADING, LOADING CREW REPORTED SMOKEY HAZE IN THE CARGO AREA NO SMOKE DETECTION WAS SENSED BY SYSTEM. THERE WAS AN ODOR PRESENT FROM THE PACKS. TEMPS AT MIX VALVES WERE NORMAL EXCEPT MID 138. A/C HAD 380 (PLUS) LBS OF DRY ICE ON BOARD ACFT UNLOADED. CFR INSPECTED A/C NO DEFECTS NOTED AT THIS TIME. PACKS OPS CHECKS GOOD IAW MM 21-00-00. 2 L 7 2 4F RT A35EU 2007121400350 20071214 00350 SO 2007 12 14 GLBA20061034 1 20071205 A 2120 12046207002 RAM AIR DOOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE BROKEN A GLBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 108UX 120108 SMOKE SMELL - AIR RETURN FLIGHT 5005 ENROUTE FROM DEN - EAR PILOTS REPORTED SMOKE IN THE COCKPIT CLIMBING THROUGH 12000. LANDING UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED THE LT RAM IAW DOOR IAW MM 21-26-01. OPERATIONAL CHECK GOOD ON GR OUND. 2 L 7 2 4T 4 T RT A31SO E20NE 2007121400352 20071214 00352 NE 2007 12 14 HALA0700511 2 20071130 A 7200 BR700715A130 ENGINE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE NR 1 OVERHEATED A HALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 WP 13 481HA 8994 8994 55126 13248 ENGINE SEVERE DAMAGE AT 1200' AGL ON TO TGT AT 1014 C. PERFORMED ENG FIRE SEVERE DAMAGE CHECK LIST AND RETURN TO AIRPOR T (ITO) WITHOUT FURTHER INCIDENT. REMOVED NR 1 ENG PER HALM144 12-2-07 INSTALLED NR 1 ENG PER HAL M143 GRD RUN-UP AND L EAK CHECK OKAY. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007121400353 20071214 00353 WP 2007 12 14 UPS07851256 1 20071105 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK. OPS CHECK GOO D REF MM 33-50-01. 2 L 7 4 4F RT 4A25 2007121400354 20071214 00354 NM 2007 12 14 UPS07M51257 1 20071104 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C CABIN - CORROSION ON SEAT TRACK CROWN, CHANNEL & FLANGE AT STA 1289 TO STA 1381 X=-75. CORROSION REMO VED PER SRM 51-21-01 VII R35. ORG THK: 0.080", MATL REMN: 0.035" (CHANNEL). FOUND EXCEED LIMIT. DAMAGED SEAT TRACK SE CTIONAL CUT OUT & REMOVED BETWEEN 1285-1411 X=-75 PER SRM 51-31-01 VII R35. HFEC INSP C/O PER DAC NDTSPM R13 06-10-01.0 01, FOUND NO CRACK. NEW SEAT TRACK SECT & REPAIR SPLICE FABRICATED & INSTL SRM 51-31-01 VII R35 & SRM 53-70-00 VI FIG 1 R35. 2 L 7 3 4F RT A22WE 2007121400355 20071214 00355 NM 2007 12 14 UPS07M51258 1 20071029 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C CABIN - CORROSION ON SEAT TRACK CROWN & CHANNEL AT STA 999-1079. CORROSION REMOVED PER SRM 51-21-01 V II R35. ORG THK: 0.100", MATL REMN: 0.047" (CHANNEL). FOUND EXCEED LIMIT. DAMAGED SEAT TRACK SECTIONAL CUT OUT BETWEE N STA 969 - STA 1089 X=-8 & REMOVED PER SRM 51-31-01 VII R35. HFEC INSP C/O PER DAC NDTSPM R13 06-10-01.001 ON CUT OUT AREA FOUND NO CRACK. NEW SEAT TRACK & SPLICE FAB, INSTL SRM 51-31-01 VII R35 & SRM 53-70-00 VI FIG 1R35. 2 L 7 3 4F RT A22WE 2007121400358 20071214 00358 NM 2007 12 14 USAA920071258 1 20071204 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 23876 CLT - MAJOR REPAIR-RON-NR 4217632, LEFT FUSELAGE HAS A SKIN CRACK 7 INCHES AFT OF FRAME 727E ALONG TOP SIDE OF STRINGER 24L. REPAIRED IAW SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2007121400359 20071214 00359 NM 2007 12 14 USAA920071259 1 20071203 A 5420 FITTING BOEING 757 7572B7 1384964 NM NR 1 NACELLE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 942UW 27807 CLT - MAJOR REPAIR-RON- NR 4214235/EO5407R146, CRACK AT NR 2 FASTENER HOLE (AFT INBD) OF NR 1 ENGINE DIAGONAL BRACE FITT ING INSIDE PYLON EO 547R146. REPAIRED IAW EA100041. 2 L 7 2 4F RT A2NM 2007121700001 20071217 00001 EU 2007 12 17 UPS07151264 1 20071206 A 2120 UNKNOWN AIRBUS A300 A300F4622R 3930360 EU COCKPIT SMOKE A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 159UP 0848 INSPECTION TYPE:N/A STARTED APU N2 GOT TO 25% - 30%. THE AVIONICS SMOKE LIGHT Y BELLS CAME ON AND SMOKE ENTERED THE FLT DECK. SHUTDOWN APU AND BATTERY SMOKE STOPPED. REF TSM 21-20-00. OPERATED A/C ELECTRICAL SYSTEM ON GROUND. ENG NOT R UNNING. A/C AND DC OPS GOOD. RAN APU AND PNEUMATICS. COULD NOT DULICATE CONDITION. SUSPECT EXTERNAL FUME INGESTION. 2 L 7 2 4F RT A35EU 2007121700002 20071217 00002 NM 2007 12 17 UPS07551266 1 20071206 A 2120 UNKNOWN BOEING 757 75724APF 1384969 NM COCKPIT ODOR A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 01 409UP 23731 INSPECTION TYPE:N/A STRONG BURNT RUBBER SMELL IN COCKPIT AFTER TOUCHDOWN AND THROUGHOUT LANDING ROLL. INSPECTED PACK BA YS, NOSE, MAIN TIRES AND BRAKES. ENGINE OIL AND HYDRAULICS PROPERLY SERVICED. RAN PACKS WITH THE APU AND ENGINES OPERA TING IN FORWARD AND REVERSE THRUST, FLAPS UP AND POSITION 5, NO DEFECTS NOTED. 2 L 7 2 4F RT A2NM 2007121700004 20071217 00004 NM 2007 12 17 USAA920071261 1 20071204 A 5315 D531114620201 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 810AW 1116 PIT - MAJOR REPAIR - BC6 CHECK, CORROSION ON CABIN FLOORBEAM, BS 683 / FR 15 - BS 709 / FR 16, -Y254. REPLACED CABIN FL OORBEAM, BS 683 / FR 15 - BS 709 / FR 16, -Y254 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007121700005 20071217 00005 NM 2007 12 17 USAA920071262 1 20071205 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR-C-18-NR I1C53034/10, FRAME 827 LEFT CRACKED AT RIVET FOR BIN RAIL ATTACHMENT. INSTALLED REPAIR IAW E A100048, TR53-10-20E. 2 L 7 2 4F RT A16WE 2007121700006 20071217 00006 NM 2007 12 17 USAA920071263 1 20071205 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR-C-18-NR I1C53034/13, FRAME 807 RIGHT IS CRACKED AT RIVET FOR BIN RAIL ATTACHMENT. REPAIRED IAW EA100 048, TR53-10-20E. 2 L 7 2 4F RT A16WE 2007121700007 20071217 00007 NM 2007 12 17 USAA920071264 1 20071205 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR-C-18-NR I1C53034/11, FRAME 847 LEFT IS CRACKED AT RIVET FOR BIN RAIL ATTACHMENT. REPAIRED IAW EA1000 48, TR53-10-20E. 2 L 7 2 4F RT A16WE 2007121700008 20071217 00008 NM 2007 12 17 USAA920071265 1 20071205 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR-C-18-NR I1C53034/12, FRAME 787 RIGHT IS CRACKED AT RIVET FOR BIN RAIL ATTACHMENT. REPAIRED IAW EA100 048, TR53-10-20E. 2 L 7 2 4F RT A16WE 2007121700009 20071217 00009 NM 2007 12 17 USAA920071266 1 20071205 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR-C-18-NR I1C53034/14, FRAME 827 RIGHT IS CRACKED AT RIVET FOR BIN RAIL ATTACHMENT. REPAIRED IAW EA100 048, TR53-10-20E. 2 L 7 2 4F RT A16WE 2007121300339 20071213 00339 NE 2007 12 13 2007UALA04880 2 20071130 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 BIRD INGESTION A UALA E A ENGINE SHUTDOWN UNSCHED LANDING C F.O.D. CL CLIMB 1 WP 29 520UA 24890 717942 RTFL UNDER AMBER ALERT DUE TO BIRD INJESTION IN THE NR 2 ENGINE. ENGINE SHUT DOWN AFTER LANDING. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121300340 20071213 00340 NM 2007 12 13 2007UALA04881 1 20071126 A 2560 GIRT BAR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU PAX DOOR FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 936UA 26667 FWD ENTRY DOOR EMERGENCY SLIDE GIRT HAS EXCESS MATERIAL OUT OF COVER AT AFT END AND THE PULL HANDLE COVER FLAP IS STUCK UP UNDER COVER. REPOSITIONED SLIDE CONTENTS AND REINSTALLED THE SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300345 20071213 00345 SO 2007 12 13 O5W2007F00000 2 20071120 A 8510 641909 LOCK PLATE CESSNA 421 421B 2076014 CE CONT O520 GTSIO520H 17032 SO CRANKSHAFT DESTROYED E O5WA K NONE O OTHER IN INSP/MAINT 1 SO 15 707DT 149 421B0468 218370R THIS ENGINE WAS REMOVED ON AUG 31, 2007, HOBBS TIME 1523.9 DUE TO A CRACKED ENGINE CASE. THE ENGINE WAS SENT FOR REPAIR . REPAIRED THE ENGINE ON SEPT 20, 2007. THIS ENGINE WAS REINSTALLED ON AIRCRAFT. DURING A NIGHT FLIGHT ON NOV 20, 200 7 THE PILOT HAD AN ALTERNATOR FAILURE. REPORTED PROBLEM THE NEXT DAY. UPON INSPECTION OF THE ALTERNATOR, IT WAS FOUND IN PIECES, WITH THE MOUNT HOUSING STILL ATTACHED TO THE ENGINE. THE INSIDE OF THE ALTERNATOR INSTALLATION HOLE WAS INSP ECTED. THE INSPECTION REVEALED THAT THE ATTACH BOLTS ON THE ALTERNATOR FACE GEAR HAD NO TAB LOCK PLATES INSTALLED. THE ATTACH BOLTS CAME LOOSE AND DAMAGED THE ENGINE AND ALTERNATOR. RAM AC WAS NOTIFIED OF THE PROBLEM. IT IS RECOMMENDED 1 L 7 2 3O 3 O A7CE E7CE 2007121300348 20071213 00348 NM 2007 12 13 2007UALA04884 1 20071129 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 FUSELAGE CROWN DENT AT BS 360 BETWEEN STR 2R & 3R AND HAS A CRACK AT STR 2 AT RIVET, DENT IS IN COMMON TO BUTT JOINT. M AJOR REPAIR: DENT ALLEVIATED WHEN STRINGER SPLICE REPLACED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300349 20071213 00349 NM 2007 12 13 2007UALA04885 1 20071129 A 3397 FEEDER CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 333UA 24228 FWD GALLEY EEL STRIP INOPERATIVE. FOUND DAMAGE TO POWER CABLE FOR EEL. ACCOMPLISHED REPAIR TO POWER CABLE. EEL LIG HTS OPERATE CORRECTLY. NO REPEATS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300372 20071213 00372 NM 2007 12 13 2007UALA04893 1 20071129 A 5320 CUSP WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 CABIN AT BS 1020, RBL 69, CUSP WEB CORRODED. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121300380 20071213 00380 NM 2007 12 13 2007UALA04896 1 20071130 A 3350 COVER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN MISSING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 216UA 30549 THE 37C EMERGENCY EXIT COVER IS MISSING. REPLACED LIGHT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121400009 20071214 00009 NM 2007 12 14 2007UALA04925 1 20071130 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 528UA 25018 EMERGENCY EXIT LIGHT INOP AT AFT RT BULLNOSE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121400020 20071214 00020 EA 2007 12 14 COMA0760678 1 20071130 A 3250 16735109 POTENTIOMETER CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 967CA 7134 FLIGHT 5439 - ON LANDING, RECEIVED NOSE WHEEL STEERING INOP MESSAGE. DECLARED EMERGENCY, TOWED TO GATE WITHOUT INCIDENT . REPLACED NOSE GEAR RVDT. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007121400022 20071214 00022 EA 2007 12 14 COMA0760680 1 20071130 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 969CA 17967 7141 FLIGHT 5690 - RECEIVED NOSE GEAR DISAGREE MESSAGE DURING RETRACTION. DECLARED EMERGENCY, RETURNED TO FSD, LANDED WITHOU T INCIDENT. REPLACED NOSE GEAR PRIORITY VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007121400027 20071214 00027 NM 2007 12 14 SWAA075999 1 20071204 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007121400034 20071214 00034 NM 2007 12 14 SWAA076014 1 20071204 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121400047 20071214 00047 NM 2007 12 14 HALA0700522 1 20071210 A 2897 RELAY BOEING 767 76733A 1385209 NM BOOST PUMP MALFUNCTIONED A HALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, AT 3+30 IN CRUISE LEFT FORWARD FUEL BOOST PUMP CIRCIUT BREAKER TRIPPED. REPLACED K-00188 LEFT FWD BOOST PUMP RELAY PER FIM767 28-22-00. GRND OPS CK OK. 2 L 7 2 4F RT A1NM 2007121400055 20071214 00055 SO 2007 12 14 C2XA07SH101 1 20071205 A 3213 23092029001 AXLE EMB 145 EMB145XR 3260214 SO RT MLG CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17115 145666 SHV - DURING C-CHECK RT MLG SHOCK STRUT LOWER ATTACH AXLE CORRODED. MAINTENANCE REMOVED AND REPLACED RT MLG SHOCK STRUT LOWER ATTACH AXLE IAW EMB AMM 32-10-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2007121400058 20071214 00058 WP 2007 12 14 ABXR070388 1 20071002 A 5420 59132626 ATTACH ANGLE DOUG DC9 DC915 3022036 WP RT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 784TW 47014 RIGHT LOWER PYLON ATTACH WAS CRACKED AND MISSING MATERIAL AT THE FORWARD OUTBOARD CORNER ATTACH POINT LOCATION FOR PANEL 8212A. REPAIRED AREA IAW ABX DC9 SSRM DGW K05683. 2 L 7 2 4F A6WE 2007121400062 20071214 00062 SO 2007 12 14 SIMA200734406 1 20071208 A 3010 ANTI-ICE SYSTEM EMB 145 EMB145LR 3260212 SO NO TEST A SIMA A UNSCHED LANDING L NO TEST CL CLIMB 1 SW 21 622AE 145108 AIR TURN BACK DUE TO WING A/I FAIL AND EXPECTING ICE CONDITIONS REROUTE. PERFORMED ICE TEST AIRBORNE ALL OK EXCEPT WING A/ICE FAIL. PERFORMED OPS CHECK WING A/ICE SYSTEM IAW EMB 145 AMM 30-10-00. COULD NOT DUPLICATE THIS PROBLEM AT THIS TIME. NO PARTS CHANGED, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007121400073 20071214 00073 WP 2007 12 14 ABXA070387 1 20071124 A 3260 RELAY DOUG DC9 DC932 3022066 WP LANDING GEAR INTERMITTENT A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 986AX 47543 UPON SELECTING GEAR DOWN, NO GREEN NOSE GEAR LIGHT WAS OBSERVED. RECYCLED GEAR, GOT 3 GREEN LIGHTS. CHECKED OPERATION OF NOSE GEAR UP AND DOWN LIMIT SWITCHES. NO FAULT FOUND. VERIFIED INTERMITTENT CONTACT BETWEEN A2 AND A3 OF RELAY R2-2 5. REPLACED RELAY, OPS CHECK GOOD IAW DC9 AMM 32-60-001. 2 L 7 2 4F A6WE 2007121400074 20071214 00074 WP 2007 12 14 ABXR070389 1 20071002 A 5755 3923255U503N SUPPORT BRACKET DOUG DC9 DC915 3022036 WP SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 784TW 47014 LEFT INBOARD FLIGHT SPOILER OUTBOARD TORQUE TUBE SUPPORT BRACKET (REACTION ARM) CRACKED. REMOVED AND REPLACED OUTBOARD FITTING IAW DC9 SRM. 2 L 7 2 4F A6WE 2007121400077 20071214 00077 EU 2007 12 14 SIMA200734408 1 20071207 A 5311 FRAME SAAB SF340 340B 7860101 EU BS 686 BENT A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 232AE 23551 5000 340B232 DURING H-MBV INSPECTION, FRAME 686.888 WAS FOUND BENT ABOVE THE FLOOR ON THE RIGHT SIDE OF ACFT. INSPECTED FRAME IAW SA AB SRM EDDY CURRENT WAS USED TO DETECT A CRACK, NO CRACK FOUND. REMOVED AND REPAIRED FRAME IAW SAAB SRM. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007121400079 20071214 00079 SO 2007 12 14 SIMA200734405 1 20071208 A 2121 4611028900 FAN EMB 145 EMB145LR 3260212 SO CABIN BURNED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 691AE 14500860 PAX COMPLAINING OF NOXIOUS VAPORS LOCATED MID CABIN. VERIFIED BY DEAD HEADING CREW MEMBERS. UNABLE TO LOCATE SOURCE. REMOVED AND REPLACED BOTH RECIRCULATION FANS THAT WERE FOUND TO HAVE BURNED, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007121400091 20071214 00091 NM 2007 12 14 SWAA076019 1 20071205 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED 14Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007121400099 20071214 00099 WP 2007 12 14 IXXA07SMN242S 1 20071110 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 798 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOIND IN MAIN CARGO COMPARTMENT A CRACKED FITTING AT STATION 798.000 LEFT BOTTOM LINE 25". REMOVED CRACKED FITTING. FABRICATED FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND FITTING. INSTALLED FITTING IAW DC8 SRM 51-1-20D, 51-3-1, DC8 SRM 51-1-20D, ATI REPAIR SPEC IFICATION NUMBER 2003-05 DRAWING DOUGLAS NUMBER 3755222, DC8 NDT SPM PART 08-00-02 TO 07, FORM SEMAN 242.4, AND SRM 51-1 -8B. 2 L 7 4 4F RT 4A25 2007121400101 20071214 00101 NM 2007 12 14 SWAA076023 1 20071205 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121400102 20071214 00102 WP 2007 12 14 IXXA07SMN243S 1 20071110 A 5340 37552221 FITTING DOUG DC8 DC873F 302199F WP BS 822 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND IN MAIN CARGO COMPARTMENT A CRACKED FITTING AT STATION 822.500 RIGHT BOTTOM LIN E 25". REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, 51-3-1, DC8 SRM 51-1-20D, SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007121400112 20071214 00112 WP 2007 12 14 IXXA07SMN249S 1 20071115 A 5330 S1616757 SKIN DOUG DC8 DC873F 302199F WP ZONE 200 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, AFT FUSELAGE FOUND A CRACK AT LONGERON 17 LEFT AT STATION 1769.000. REMOVED CRACKED LONGERON. FABRICATED NEW LONGERON. CLEANED, TREATED AND PRIMED AREA AND NEW LONGERON. INSTALLED NEW LONGERON IAW DC8 SRM 51-1-11, 51-1-21, 51-1-20D, 51-3-1, DC8 SRM 53-5-3 FIGURE 5 SHEET 1, DC8 SRM 53-1-0 PAGE 1,SRM 51-1-21 AND 51-1-20D, DC8 SRM 53-5-3 FIGURE 5 SHEET 1 ITEM "B", AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007121400118 20071214 00118 WP 2007 12 14 IXXA07SMN252S 1 20071115 A 5340 4772397 FITTING DOUG DC8 DC873F 302199F WP ZONE 200 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE SPLICE FITTING CRACKED AT STATION 1766.000 LONGERON 17 RIGHT. REM OVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, 51-3-0, 51-3-1. 2 L 7 4 4F RT 4A25 2007121400131 20071214 00131 EU 2007 12 14 07FDEA05025 1 20071211 A 5310 A53611517200 GUSSET AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 LT FWD ENTRY DOOR OPENING, LWR FWD CORNER HAS DEFECT INDICATION FROM EDDY CURRENT INSPECTION, IN CORNER STRAP EDGE. REM OVED AND REPLACED CORRODED CORNER STRAP (GUSSET) IAW A310-200 SRM 51-40-21 PAR 7. MACHINED CORNER STRAP, AND FORMED TO CONTOUR, IAW AIRBUS DWG NR 12A 53611517, REV "D" AND ABS 5032. 2 L 7 2 4F RT A35EU 2007121400136 20071214 00136 NM 2007 12 14 NWAA073976745 1 20071208 A 3350 LIGHT BOEING 747 747222B 1384904 NM CABIN INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 645NW 23736 DURING OVERNIGHT CHECK, FOUND EMERGENCY LIGHT ON CEILING ON MAIN CARGO DECK AT STA 590 INOP. MAINTENANCE REMOVED AND RE PLACED LIGHT ASSEMBLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007121400148 20071214 00148 EU 2007 12 14 CPCP20070125 1 20071120 A 5753 RIB AEROSP ATR72 ATR72212 8680945 EU TE FLAP CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 342AT 345 FLAP ARM AT FLAP RIB 18 RT CORRODED FORWARD ATTACH POINT. RT FLAP AT FLAP RIB 18 REPLACED IAW JIC 57-53-00 RAI 10000. OPERATIONAL TEST OF FLAP TRANSFERED TO NRWC 197237. 2 H 7 2 4T RT A53EU 2007121400159 20071214 00159 NM 2007 12 14 2007UALA04937 1 20071203 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 DOOR R1 LWR GATE CRACKED AND CORRODED. REMOVED & REPLACED GATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121400164 20071214 00164 2007 12 14 DLM90071597 4 20071209 A 2330 RDAV980501 VIDEO MONITOR DOUG MD90 MD9030 3023690 NM CABIN SMOKE A DALA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 902DA 53382 VIDEO MONITOR AT 19 A/B BEGAN SMOKING. REPLACED MONITOR AT 19AB CKS OK. INSPECTED AREA, NO ABNORMAL CONDITIONS NOTED. 2 L 7 2 4F RT A6WE 2007121400166 20071214 00166 NM 2007 12 14 DL76S071600 1 20071128 A 5330 141T3211 SKIN BOEING 767 767332 1382001 NM FS 1286 S32L DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 125DL 24075 FUSELAGE SKIN BLENDS AT FS 1286.5 AND 32L DUE TO GROUND DAMAGE PER ER/A 459209-14 REV A. 2 L 7 2 4F RT A1NM 2007121400167 20071214 00167 NM 2007 12 14 DL76L071601 1 20071210 A 2131 CONTROLLER BOEING 767 767332 1382001 NM CABIN PRESSURE MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 179DN 25144 RTB - AUTO PRESS 1 AND 2 EICAS STATUS MSG, PRESS CONT 1 AND 2 BITE FAULTED CONTROLLER 1 AND 2. CONTROL 1 2 RESET. CON T 12 NOW SHOW NO FAULT. 2 L 7 2 4F RT A1NM 2007121400184 20071214 00184 WP 2007 12 14 AALA20072392 1 20071206 A 3222 SEAL DOUG DC9 DC982 3022082 WP NLG STRUT INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 552AA 53034 MSP INFLIGHT T1085/06DEC - NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REP LACED NOSE LANDING GEAR SHOCK STRUT SEALS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121400185 20071214 00185 EU 2007 12 14 AALA20072400 1 20071208 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70079 619 JFK - EMERGENCY LIGHTS AT SEAT MOUNTED RIGHT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT S EAT MOUNTED RIGHT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121400186 20071214 00186 WP 2007 12 14 AALA20072405 1 20071208 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT MOUNT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 420AA 49332 LGA - EMERGENCY FLASHLIGHT AT FORWARD ENTRY DOOR HAS DAMAGED STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121400187 20071214 00187 NM 2007 12 14 AALA20072406 1 20071208 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 766AN 32880 DFW - EMERGENCY LIGHT AT SEAT 21C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121400188 20071214 00188 NM 2007 12 14 AALA20072407 1 20071208 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 766AN 32880 DFW - EXTERNAL EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121400189 20071214 00189 EU 2007 12 14 AALA20072401 1 20071208 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70079 619 JFK - EMERGENCY LIGHTS AT SEAT MOUNTED RIGHT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT MOUNTED RIGHT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121400190 20071214 00190 EU 2007 12 14 AALA20072402 1 20071208 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70079 619 JFK - EMERGENCY LIGHTS AT SEAT MOUNTED RIGHT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT MOUNTED RIGHT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121400197 20071214 00197 EU 2007 12 14 AALA20072394 1 20071207 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7062A 474 JFK - EMERGENCY LIGHTS AT SEAT 24G INOPERATIVE. REPAIRED BROKEN PIN ON CONNECTOR FOR EMERGENCY LIGHT AT SEAT 24G. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121400199 20071214 00199 EU 2007 12 14 F3LA200700369 1 20071204 A 3350 321431 BATTERY PACK AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHTS NO TEST A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 901FR 1488 DURING C-5 CHECK, INSPECTION REPORTED FWD EMERGENCY BATTERY EPSU FAILED CAPACITY TEST. REMOVED AND REPLACED FWD EPSU BA TTERY AND PERFORMED OPS CHECK IAW 33-51-38-000-002. CHECKED GOOD. 2 L 7 2 4F RT A28NM 2007121400203 20071214 00203 EU 2007 12 14 07FDEA05027 1 20071211 A 5330 A5377862720000 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 403FE 230 FUSELAGE FLUSH REPAIR DOUBLER AT FR 34-35 STR 43/45 LT. REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED FLUSH REPAIR AT FR 34/35 STGR 43/45 LT. FOUND NOT TO BE WITHIN F AA APPROVED DATA. REMOVED REPAIR AND ACCOMPLISHED EXTERNAL REPAIR IAW A310 SRM 53-10-12 FIG 225. 2 L 7 2 4F RT A35EU 2007121400216 20071214 00216 EU 2007 12 14 F3LA200700372 1 20071204 A 3350 321431 BATTERY PACK AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHTS NO TEST A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 901FR 1488 DURING C-5 CHECK, INSPECTION REPORTED RT OVERWING EMERGENCY BATTERY EPSU FAILED CAPACITY TEST. REMOVED AND REPLACED EPS U BATTERY AND PERFORMED OPERATIONAL CHECK IAW AMM 33-51-38-PB401. CHECKED GOOD. 2 L 7 2 4F RT A28NM 2007121400224 20071214 00224 SO 2007 12 14 SIMA200734606 1 20071210 A 2120 UNKNOWN EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 21 853AE 145742 CREW REPORTED A OIL ODOR ON DESCENT APU OFF PACKS ON. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007121400245 20071214 00245 EU 2007 12 14 DELA200700009 1 20071125 A 7330 FUEL FILTER BRAERO DH125 BAE125800A 1500285 EU GARRTT TFE731 TFE7315R 01518 WP NR 2 ENGINE UNKNOWN E DELA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 904JR 258018 P91137 ENG 2 FUEL LIGHT. ABORTED TAKEOFF DUE TO ENGINE 2 FUEL LIGHT ON. REPLACED FILTER WITH NEW, PERFORMED GROUND ENGINE RUN, NO LEAKS NOTED, (ENG 2 FUEL) ENUNCIATOR DID NOT ILLUMINATE. 2 L 7 2 4F 4 F RT A3EU E6WE 2007121400255 20071214 00255 NM 2007 12 14 2007UALA04961 1 20071204 A 2560 ATTACH BRACKET BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L1 DOOR DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 193UA 26890 DOOR 1R SLIDE ATTACH BRACKET DAMAGED. DAMAGED CAUSE UNKNOWN. REPLACED DOOR 1R SLIDE PER MM 25-69-01. AND REPLACED AT TACH BRACKET ACCOMPLISHED INSPECTION. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121400273 20071214 00273 NM 2007 12 14 2007UALA04973 1 20071205 A 3350 1619 LAMP BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 923UA 26643 DOOR 2L EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121400274 20071214 00274 NM 2007 12 14 2007UALA04974 1 20071205 A 3350 767 LAMP BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 923UA 26643 RIGHT EXTERIOR OVERWING EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121400281 20071214 00281 NE 2007 12 14 2007UALA04981 2 20071205 A 7250 BLADES BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT ENGINE FAILED A UALA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 WP 29 772UA 26930 777021 FLIGHT CANCELLED DUE TO RT ENGINE VIBRATION AND METAL CHIPS FOUND ON DETECTOR. ENGINE REPLACED AT LHR. SHOP TEARDOWN RE VEALED ONE STAGE-2 HP TURBINE BLADE FRACTURED AT THE AIRFOIL MID-SPAN. THE FRACTURE WAS THE RESULT OF INTERNAL SULFIDAT ION RESULTING FROM TURBO TIP CONTAMINATION. THIS WAS THE RESULT OF A REPAIR/ MANUFACTURE PROCESS ERROR THAT HAS SINCE B EEN CORRECTED BY PRATT & WHITNEY. UA IS REPLACING SUSPECT CONTAMINATED BLADES AT SHOP VISIT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121400287 20071214 00287 NM 2007 12 14 2007UALA04987 1 20071205 A 2913 PUMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE HYDRAULIC SYS MALFUNCTIONED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 663UA 27160 NR 1 ACMP DOES NOT COME ON LINE WHEN IN AUTO MODE AND EDP IS SWITCHED OFF. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121400302 20071214 00302 NM 2007 12 14 ZZDA2007308 1 20071130 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 957AT 55019 DENT IN FUSELAGE BS 214L LONGERON 17. INSTALLED INTERNAL DOUBLER PER 717 SRM 51-10-02 AND 53-00-01. 2 L 7 2 4F TR A6WE 2007121400307 20071214 00307 EA 2007 12 14 TRAX200701863 1 20071203 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 FS 280 FWD FLOOR SUPPORT IS CRACKED I/B OF RBL 9. INSTALLED NEW ANGLE IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007121700011 20071217 00011 NM 2007 12 17 USAA920071268 1 20071205 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR-C-18-NR I1C53034/15, FRAME 847 RIGHT IS CRACKED AT RIVET FOR BIN RAIL ATTACHMENT. REPAIRED IAW EA100 048, TR53-10-20E. 2 L 7 2 4F RT A16WE 2007121700014 20071217 00014 NM 2007 12 17 USAA920071271 1 20071206 A 5313 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR-C-18-NR CIC25009/1, CRACK ON STRINGER AT BS 940, S4L. REPAIRED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007121700017 20071217 00017 NM 2007 12 17 USAA920071274 1 20071129 A 5311 69374024 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR -C-18- NR I1D25012, CRACK ON FRAME AT BS 291.5 - 294.5, S17L. REPAIRED IAW BOEING DWG 69-37402, SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007121700019 20071217 00019 NM 2007 12 17 USAA920071276 1 20071204 A 5320 ATTACH ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR-C-18- NR I1C53037/3, CRACK ON STRINGER ATTACH ANGLE AT BS 500D,13R. REPAIRED IAW SRM 53-00-07-2R FIG 201. 2 L 7 2 4F RT A16WE 2007121700020 20071217 00020 NM 2007 12 17 USAA920071277 1 20071130 A 5313 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C-18- NR I2D53012/7, CORROSION ON CARGO FLOOR STRINGER AT BS 727D+5", LBL 10. REPAIRED IAW EA10006 1, TR 53-10-06B. 2 L 7 2 4F RT A16WE 2007121700021 20071217 00021 NM 2007 12 17 USAA920071278 1 20071130 A 5313 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR-C-18- NR I2D53012/6, CORROSION ON CARGO FLOOR STRINGER AT BS 727D+5", LBL 2. REPAIRED IAW EA100061, TR 53-10-06B. 2 L 7 2 4F RT A16WE 2007121700022 20071217 00022 NM 2007 12 17 USAA920071279 1 20071130 A 5313 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR-C-18- NR I2D53012/5, CORROSION ON CARGO FLOOR STRINGER AT BS 727D+5", RBL 2. REPAIRED IAW EA100061, TR 53-10-06B. 2 L 7 2 4F RT A16WE 2007121700024 20071217 00024 NM 2007 12 17 USAA920071281 1 20071127 A 5320 6545807037 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR-C-18- NR 03-0553-8-0303/2, ANGLE CRACKED AT BS 290, S11R - S12R. REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2007121700028 20071217 00028 NM 2007 12 17 USAA920071285 1 20071120 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR-C-18- NR I1D25007/2, CRACK ON FLOORBEAM T-CAP AT BS 294.5, S17L, LBL 54. REPAIRED IAW 53-10-51-2R5 F IG 201. 2 L 7 2 4F RT A16WE 2007121700032 20071217 00032 NM 2007 12 17 USAA920071292 1 20071124 A 5542 173N21011 SKIN BOEING 757 7572B7 1384964 NM RUDDER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 200UU 27809 MCN - MAJOR REPAIR - C4 CHECK - NR 6055223, DELAMINATION ON RUDDER SKIN LEFT HAND SIDE, RUDDER STATION 332. REPAIRED RU DDER SKIN LEFT HAND SIDE, RUDDER STATION 332 IAW B757 SRM 51-70-04 FIGURE 5. 2 L 7 2 4F RT A2NM 2007121700033 20071217 00033 NM 2007 12 17 USAA920071293 1 20071107 A 5753 113N23412 RIB BOEING 757 7572B7 1384964 NM T/E FLAP CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 200UU 27809 MCN - MAJOR REPAIR - C4 CHECK - NR 6055159, RIGHT WING INBOARD FLAP INBOARD RIB CRACKED, FS 76.8. REPLACED RIGHT WING I NBOARD FLAP INBOARD RIB, FS 76.8 IAW B757 SRM 51-40-05. 2 L 7 2 4F RT A2NM 2007121700038 20071217 00038 SO 2007 12 17 C2XA07TY076 1 20071204 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16571 145633 TYS - DURING ACCOMPLISHMENT OF EA5310-01061 (LR WEIGHT INCREASE), THE SKIN WAS MISDRILLED BETWEEN FRAMES 45 AND 46, STRI NGERS 4R & 5R. THE DAMAGED AREAS OF SKIN AND SKIN SPLICE STRAP WERE CUT OUT. A NEW SPLICE STRAP, FILLER, AND DOUBLER W ERE FABRICATED AND THE PARTS WERE ALODINED AND PRIMED. THE FILLER AND DOUBLER WERE INSTALLED WET WITH SEALANT AND THE R EPAIR AREA WAS PRIMED AND PAINTED IAW EC5330-01757, AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007121700039 20071217 00039 NM 2007 12 17 NOCA16807 1 20071130 A 5270 SWITCH BOEING 757 75728A 1384976 NM R4 DOOR DIRTY A NOCA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING TX TAXI/GRND HDL 1 EA 15 752NA 28174 R4 DOOR EICAS AND OVERHEAD STATUS LIGHT NOT ON WHEN DOOR IS OPEN. PLUNGER STUCK CLOSED WITH DEBRIS REMOVED DEBRIS, OPS CHECK OK PER MM 52-71-00. 2 L 7 2 4F RT A2NM 2007121700041 20071217 00041 NM 2007 12 17 CALA0700731 1 20071209 A 5330 65C27755 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 R-2 DOOR CUTOUT CRACKED AT UPPER HINGE UPPER AREA. REPAIR COMPLETED IAW SRM 53-60-01 FIG 201. 2 L 7 2 4F RT A16WE 2007121700042 20071217 00042 NM 2007 12 17 PIDA07057 1 20071205 A 5340 STRINGER CLIP BOEING 737 737228 13844AG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 252TR 23001 DURING MAINTENANCE CHECK, NOTED STRINGER TIE CLIP CRACKED AT BS 616 AT STR 5LT. REPLACED TIE CLIP PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007121700043 20071217 00043 NM 2007 12 17 WRLA2007133 1 20071206 A 3232 ACG7075501 BRACKET DOUG MD11 MD11 3023602 NM LANDING GEAR BROKEN A WRLA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 11 273WA 48519 AT GEAR RETRACTION SEVERE VIBRATION AND NOISE BELOW FLIGHT DECK. REPLACED BRACKET P/N ACG7075-501 AND NOSE LANDING GEAR AFT DOOR DRIVE LINKAGE P/N ACG7326-1 IAW MM 32-36-02. GEAR SWING ACCOMPLISHED IAW MM 32-31-00-700-801. 2 L 7 3 4F RT A22WE 2007121700044 20071217 00044 EU 2007 12 17 UPS07151269 1 20071209 A 2510 3A2180007011 SEAT AIRBUS A300 A300F4622R 3930360 EU COCKPIT DEFECTIVE A IPXA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 138UP 0821 INSPECTION TYPE:N/A DURING TAKEOFF ROLL IN MIAMI, CAPTS SEAT UNLATCHED AND SLID TO REAR STOP. REJECTED TAKEOFF SPEED LE SS THAN 50 KTS. REMOVED AND REPLACED CAPT'S SEAT ASSY IAW A300 MM 25-11-11-04-01. 2 L 7 2 4F RT A35EU 2007121700047 20071217 00047 WP 2007 12 17 UPS07851275 1 20071208 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD PER MM 33-50-02-2. 2 L 7 4 4F RT 4A25 2007121700048 20071217 00048 NM 2007 12 17 UPS07M51268 1 20071107 A 5320 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C CTR CARGO DOORWAY AREA STA 1745 TO STA 1764 FOUND SUPPORT FITTING WITH ELONGATED MOUNTING HOLES. 02EA DISCREPANT HOLES AT CTR CARGO DOORWAY REAMED TO 0.465" & 0.425" DIA RESPECTIVELY PER EN1721-07. HFEC INSP CUTOUT PER D AC NDTSPM R.13 06-10-0 1.003 FOUND NO CRACK EVIDENT. REP BUSHING USING MATL 7075-T6 & REP STRAP 01 USING MATL 7075T6-0. 190" FABRICATED PER EN1721-07. 02EA BUSHINGS & 01EA REPAIR STRAP INSTALLED PER EN1721-07 ON SUPPORT FITTING. 2 L 7 3 4F RT A22WE 2007121700049 20071217 00049 2007 12 17 UPS07M51271 4 20071207 A 2565 SLIDE DOUG MD11 MD11F 3023600 NM R1 DOOR LOW PRESSURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:N/A CREW PREFLIGHT - RIGHT (R1) DOOR SLIDE LOW PRESSURE. REMOVED AND REPLACED R1 DOOR SLIDE. REF MM 25 -61-15-4. 2 L 7 3 4F RT A22WE 2007121700051 20071217 00051 SO 2007 12 17 RAIA00712002 1 20071204 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 816HK 145055 POST FLT 5526 - STL - EMERGENCY FLOOR LIGHT STRIP LOOSE AT 1A. MAINTENANCE RESECURED FLOOR LIGHT STRIP, OPS CHECK NORMA L. 2 L 7 2 4F RT T00011AT 2007121700052 20071217 00052 GL 2007 12 17 RAIA00711018 2 20071127 A 7261 4252070 GARLOCK SEAL EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL NR 2 ENGINE WORN A RAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 03 842HK 14500830 FLT 8006 - IAD - NR 2 ENG OIL PRESSURE WENT INTO RED/QUANTITY AT 3 QTS. ENGINE WAS SHUT DOWN. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE GENERATOR GARLOCK SEAL AND RETAINING RING PERFORMED LEAK CHECK AND GROUND RUN CHECKS GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007121700053 20071217 00053 SO 2007 12 17 RAIA00711020 1 20071128 A 3350 LIGHT EMB 145 EMB145 3260210 SO EXTERIOR INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 847HK 14500857 PRE FLT 7891 - SYR - EMERGENCY LIGHT LEFTHAND FORWARD EXTERIOR LIGHT INOP. MAINTENANCE DEFERRED AS PER MEL. 2 L 7 2 4F RT T00011AT 2007121700056 20071217 00056 EU 2007 12 17 YENA2007113 1 20071208 A 3411 0851HL PITOT TUBE AIRBUS 320 A320232 3930326 EU PITOT/STATIC SYS PLUGGED A YENA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 EA 15 583JB 16753 2150 FLT 411, BOS-SAN, RETURNED TO BOS DUE ON TAKEOFF F/O AIR SPEED, AUTO THRUST WENT AWAY, ALSO RUDDER TRAVEL LIM ECAM AND L OSS OF AUTOPILOTS. REMOVED AND REPLACED F/O PITOT PROBE IAW MM 34-11-15. OPS CHECK OK. PRECAUTIONARY REMOVED AND REPL ACED ADIRU 2 IAW 34-12-64, REMOVED AND REPLACED PRECAUTIONARY F/O ADM 2 REF 34-13-00, OPS CHECK GOOD. AFT TEST IAW 22-4 5-00 LAND TEST REF 22-97-00, OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 2007121700058 20071217 00058 NE 2007 12 17 SWAA076094 2 20071205 A 7200 CFM567B24G22 ENGINE BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B22 13802 NE RIGHT FAILED A SWAA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SW 29 234WN 32502 874875 AIR TURNBACK / DECLARED EMERGENCY. NR 2 ENGINE FAILED DURING CLIMB AT 1400'. REMOVED AND REPLACED NR 2 ENGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007121700060 20071217 00060 NM 2007 12 17 SWAA076068 1 20071207 A 2560 65C16820 HOOK BOEING 737 7377H4 1384404 NM L2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 251WN 32510 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2007121700061 20071217 00061 NM 2007 12 17 SWAA076041 1 20071209 A 5754 65C26601 SLAT BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2007121700062 20071217 00062 NM 2007 12 17 SWAA076069 1 20071209 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700064 20071217 00064 NM 2007 12 17 SWAA076071 1 20071209 A 5315 65C33941 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 12. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007121700067 20071217 00067 NM 2007 12 17 SWAA076072 1 20071207 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007121700068 20071217 00068 NM 2007 12 17 SWAA076074 1 20071209 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12L. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2007121700070 20071217 00070 NM 2007 12 17 SWAA076044 1 20071209 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 417WN 29822 DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007121700072 20071217 00072 NM 2007 12 17 SWAA076046 1 20071209 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 474WN 33861 DURING SCHEDULED MV2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP CRACKED AT ROW 5 ABC. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007121700073 20071217 00073 NM 2007 12 17 SWAA076047 1 20071209 A 2560 65C16820 HOOK BOEING 737 7377H4 1384404 NM R1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 497WN 32479 R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2007121700074 20071217 00074 2007 12 17 SWAA076075 4 20071207 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007121700075 20071217 00075 NM 2007 12 17 SWAA076076 1 20071206 A 5755 654645170A SKIN BOEING 737 7375H4 138449D NM NR 8 SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 RIGHT WING NR 8 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007121700076 20071217 00076 NM 2007 12 17 SWAA076077 1 20071206 A 5755 654645170A SKIN BOEING 737 7375H4 138449D NM NR 9 SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 RIGHT WING NR 9 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2007121700079 20071217 00079 NM 2007 12 17 SWAA076048 1 20071207 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700081 20071217 00081 NM 2007 12 17 SWAA076049 1 20071207 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700082 20071217 00082 NM 2007 12 17 SWAA076081 1 20071206 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 803, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700084 20071217 00084 NM 2007 12 17 SWAA076084 1 20071209 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700086 20071217 00086 NM 2007 12 17 SWAA076083 1 20071209 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700087 20071217 00087 NM 2007 12 17 SWAA076086 1 20071209 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 390, LBL 1.5. REPAIRED SK IN PER EA. 2 L 7 2 4F RT A16WE 2007121700088 20071217 00088 NM 2007 12 17 SWAA076087 1 20071209 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700090 20071217 00090 NM 2007 12 17 SWAA076050 1 20071209 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700091 20071217 00091 NM 2007 12 17 SWAA076051 1 20071209 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700094 20071217 00094 NM 2007 12 17 SWAA076088 1 20071206 A 5755 654645262A HINGE FITTING BOEING 737 7373A4 1384585 NM NR 2 SPOILER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 2 GROUND SPOILER INBOARD HINGE FITTING BROKEN. REMOVED AND REPLACED SPOILE R PER MM. 2 L 7 2 4F RT A16WE 2007121700096 20071217 00096 NM 2007 12 17 SWAA076093 1 20071209 A 5310 6547967 DOOR FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND AFT CARGO DOOR FWD FRAME CORRODED AT LOWER FWD CORNER. REPAIRED FRAME PER ACO. 2 L 7 2 4F RT A16WE 2007121700099 20071217 00099 NM 2007 12 17 SWAA076091 1 20071209 A 5340 65C27314 STRINGER CLIP BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700100 20071217 00100 NM 2007 12 17 SWAA076092 1 20071209 A 5340 65C27314 STRINGER CLIP BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700102 20071217 00102 NM 2007 12 17 SWAA076057 1 20071207 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 716SW 27850 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007121700104 20071217 00104 NM 2007 12 17 SWAA076059 1 20071207 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 716SW 27850 DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007121700105 20071217 00105 NM 2007 12 17 SWAA076060 1 20071207 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 716SW 27850 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PA CKS PER MM. 2 L 7 2 4F RT A16WE 2007121700107 20071217 00107 NM 2007 12 17 SWAA076062 1 20071209 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 781WN 30601 DURING SCHEDULED HC1 CHECK, FWD CABIN EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK S PER MM. 2 L 7 2 4F RT A16WE 2007121700110 20071217 00110 NM 2007 12 17 SWAA076065 1 20071209 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 781WN 30601 DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 133.15. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007121700111 20071217 00111 NM 2007 12 17 SWAA076064 1 20071209 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 781WN 30601 DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 13 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007121700114 20071217 00114 NM 2007 12 17 USAA920071297 1 20071201 A 5320 FITTING BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 921UW 22201 PIT - MAJOR REPAIR - C3 CHECK, LEVEL 2 CORROSION ON AFT CARGO COMPARTMENT SKIN CLIP, BS 1320, S27R - S28R. REMOVED AND REPLACED AFT CARGO COMPARTMENT SKIN CLIP, BS 1320, S27R - S28R IAW B757 SRM 53-00-53. 2 L 7 2 4F RT A2NM 2007121700115 20071217 00115 NM 2007 12 17 USAA920071298 1 20071208 A 5330 6545766 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 PHX - MAJOR REPAIR - NR 4297359, CRACKED FUSELAGE SKIN, BS 380 - BS 400, S10R. REPAIRED FUSELAGE SKIN, BS 380 - BS 400, S10R IAW B737 SRM 530--001-2R. 2 L 7 2 4F RT A16WE 2007121700118 20071217 00118 NM 2007 12 17 USAA920071301 1 20071205 A 5340 69353521 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C16 CHECK - NR 6052386, CRACKED STRINGER TIE CLIP, BS 887, S6R. REPLACED STRINGER TIE CLIP, BS 887 , S6R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007121700119 20071217 00119 NM 2007 12 17 USAA920071302 1 20071205 A 5753 6546435277 SKIN BOEING 737 7374B7 1384702 NM T/E FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 459UW 25023 CLT - MAJOR REPAIR - C6 CHECK, LEFT WING OUTBOARD AFT FLAP LOWER SURFACE HAS AREA OF DELAMINATION. REPLACED LEFT WING O UTBOARD AFT FLAP IAW B737 AMM 27-51-39. 2 L 7 2 4F RT A16WE 2007121700120 20071217 00120 NM 2007 12 17 USAA920071303 1 20071205 A 5753 6546435278 SKIN BOEING 737 7374B7 1384702 NM T/E FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 459UW 25023 CLT - MAJOR REPAIR - C6 CHECK, RIGHT WING OUTBOARD AFT FLAP LOWER SURFACE HAS AREA OF DELAMINATION. REPLACED RIGHT WING OUTBOARD AFT FLAP IAW B737 AMM 27-51-39. 2 L 7 2 4F RT A16WE 2007121700121 20071217 00121 NM 2007 12 17 USAA920071304 1 20071205 A 5753 6546431279 SKIN BOEING 737 7374B7 1384702 NM FOREFLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 459UW 25023 CLT - MAJOR REPAIR - C6 CHECK, LEFT WING OUTBOARD FORE FLAP LOWER SURFACE HAS AREA OF DELAMINATION. REPLACED LEFT WING OUTBOARD FORE FLAP IAW B737 AMM 27-51-37. 2 L 7 2 4F RT A16WE 2007121700125 20071217 00125 NM 2007 12 17 USAA920071308 1 20071205 A 5754 65C26602224SP SLAT BOEING 737 7373G7 1384595 NM RT WING DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C16 CHECK - NR 6049364, RIGHT WING NR 5 SLAT HAS AREA OF DISBOND, SS 124.53 - SS 129.53. REPAIRED RIGHT WING NR 5 SLAT IAW B737 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 2007121700126 20071217 00126 NM 2007 12 17 USAA920071309 1 20071205 A 5340 6935321 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C16 CHECK - NR 6049347, CRACKED STRINGER TIE CLIP, BS 727B, S25L. REPLACED STRINGER TIE CLIP, BS 7 27B, S25L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007121700127 20071217 00127 NM 2007 12 17 USAA920071310 1 20071203 A 5340 6935352U14 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK, CRACKED STRINGER TIE CLIP, BS 663, S10R. REPLACED STRINGER TIE CLIP, BS 663, S10R IAW B 737 SRM 51-00-00. 2 L 7 2 4F RT A16WE 2007121700128 20071217 00128 NM 2007 12 17 USAA920071311 1 20071205 A 5340 69366001 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK, CRACKED STRINGER TIE CLIP, BS 277, S10R. REPLACED STRINGER TIE CLIP, BS 277, S10R IAW B 737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007121700129 20071217 00129 NM 2007 12 17 USAA920071312 1 20071124 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK, CRACKED STRINGER TIE CLIP, BS 663, S10L. REPLACED STRINGER TIE CLIP, BS 663, S10L IAW B 737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007121700132 20071217 00132 NM 2007 12 17 USAA920071315 1 20071207 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK, CRACKED FRAME WEB BS 787, S9L. REPAIRED FRAME WEB, BS 787, S9L IAW USAIRWAYS TYPICAL RE PAIR 53-10-25. 2 L 7 2 4F RT A16WE 2007121700133 20071217 00133 NM 2007 12 17 ASAA0752365 1 20071204 A 2160 3983083 MODULATING VALVE BOEING 737 737890 1384527 NM CABIN TEMP MALFUNCTIONED A ASAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 587AS 35684 CONTROL CABIN `ZONE TEMP` LIGHT CAME ON DURING RECALL. GOES OUT ON RESET. REPLACED CONTROL CABIN TRIM AIR MODULATION V ALVE. OP AND BITE CHECKS OK. 2 L 7 2 4F RT A16WE 2007121700134 20071217 00134 EA 2007 12 17 COMA0770076 1 20071205 A 5610 NP1393226 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 398CA 8426 10112 FLIGHT 5419 - F/O SIDE WINDOW CRACKED IN FLIGHT PASSING 7000FT. NO IMPACT WITH ANY OUTSIDE OBJECT NOTED. AIRCRAFT RETU RNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED F/O'S SIDE WINDOW. 2 L 7 2 4F RT A21EA 2007121700135 20071217 00135 EA 2007 12 17 COMA0770075 1 20071206 A 2750 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA NR 1 AND 2 MALFUNCTIONED A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 625CA 10113 FLIGHT 4957 - DURING TAXI, RECEIVED FLAP FAIL MESSAGE. RETURNED TO GATE. RESET NR 1 AND NR 2 SFECU. GROUND CHECKS GOO D. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007121700136 20071217 00136 NM 2007 12 17 BB07096 1 20071207 A 3350 893003 CHARGER BOEING 767 7672B7 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 256AY 26847 MAINTENANCE FOUND FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE FROM ROW 19AB REARWARD, AND FROM ROW 3FG TO 5FG. REPLACED CH ARGER AND REPAIRED WIRING. 2 L 7 2 4F RT A1NM 2007121700137 20071217 00137 SO 2007 12 17 RAIA00712004 1 20071206 A 5210 ROLLER EMB 145 EMB145 3260210 SO PAX DOOR OUT OF POSITION A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 831HK 145232 POST FLT 7886 - IAD- PAX DOOR WILL NOT OPEN FULLY. MAINTENANCE REPOSITIONED LOWER AFT MAIN DOOR GUIDE ROLLER CHECK GOOD . 2 L 7 2 4F RT T00011AT 2007121700138 20071217 00138 SO 2007 12 17 RAIA00712003 1 20071206 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN NOT SEATED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 830HK 145313 POST FLT NR 5526-STL- NR 1 EMERGENCY LIGHT ON STAIRS INTERMITTENT. MAINTENANCE RESEATED SAID LIGHT, OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007121400081 20071214 00081 NM 2007 12 14 QXEA200701790 1 20071203 A 7160 TCCAPDANIH949 ACTUATOR BOMBDR DHC8 DHC8402 1390042 NM BYPASS DOOR MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 412QX 7220 4059 SEA- FLIGHT 2287 - ENGINE INTAKE SWITCH ON THE NR 2 SIDE FLICKERING ON AND OFF WHILE SWITCH IS IN CLOSED POSITION. RETU RNED TO THE GATE. MAINTENANCE REPLACED THE INTAKE BYPASS DOOR ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007121400088 20071214 00088 NM 2007 12 14 SWAA076018 1 20071205 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM R2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2007121400090 20071214 00090 WP 2007 12 14 IXXA07SMN238S 1 20071110 A 5753 VANE DOUG DC8 DC873F 302199F WP ZONE 600 DAMAGED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING EXTERNAL VANE WITH ELONGATED HOLES AT STATION XOLDO 67.000. REMOVED FASTENERS AS NEEDED TP PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED REPAIR DOUBLER AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA, AND REPAIR PART. INSTALLED NEW FAST ENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, 51-3-1, FORM FAA 8110-3 NUMBER 07532 DATED 11-08-07 SEMAN DRAWING NUMBER ED- 4648 DATED 11-07-07, DC8 SRM 51-1-21, 51-3-0, 51-1-20D, DC8 NDT SPM PART 08-00-02 TO 07, FORM SEMAN 242-4, AND DC8 SRM 5 1-1-8B. 2 L 7 4 4F RT 4A25 2007121400105 20071214 00105 NM 2007 12 14 KNNA200700067 1 20070813 A 5330 SKIN BOEING 737 7372L9 1384497 NM PWA JT8 JT8D9 52048 NE BS 410-445 DENTED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 464AT 21258 SEVERAL DENTS IN FUSELAGE SKIN AT STA 410 TO STA 445. REPAIRED AREA BY CUTTING OUT THE DAMAGE AND FABRICATING THEN INST ALLING REPAIR PARTS IAW SRM 53-30-3-FIG 46 AND SKYKING ACO-0753104. 2 L 7 2 4F 4 F RT A16WE E2EA 2007121400107 20071214 00107 WP 2007 12 14 IXXA07SMN245S 1 20071110 A 5340 37552221 FITTING DOUG DC8 DC873F 302199F WP BS 781 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND IN MAIN CARGO COMPARTMENT A CRACKED FITTING AT STATION 781.500 LEFT BOTTOM LINE 25". REMOVED CRACKED FITTING.CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-3-0, 51-1-20D, 51-3 -1, DC8 SRM 51-3-0, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007121400108 20071214 00108 WP 2007 12 14 ARWA20071103 1 20071107 A 3297 WIRE DOUG DC10 DC1030F 3023504 WP PROX SENSOR BROKEN A ARWA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 478CT 47819 AFTER GEAR RETRACTION, NOSE GEAR RED LIGHTS REMAINED ILLUMINATED ON BOTH THE FORWARD AND F/E PANELS, CYCLED GEAR ONCE AS PER CHECK LIST, BUT NO HELP. PERFORMED ELECTRICAL TROUBLE SHOOTING, SYSTEM FOUND BROKEN WIRE AT NOSE GEAR PROXIMITY SE NSOR; REPAIRED WIRING IN ACCORDANCE WITH M/M 20-31-00; CHECKED ON GROUND IN ACCORDANCE WITH M/M 32-30-00. 2 L 7 3 4F RT A22WE 2007121400119 20071214 00119 NM 2007 12 14 SWAA076036 1 20071205 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121400122 20071214 00122 NM 2007 12 14 SWAA076029 1 20071205 A 3350 65C27093 LIGHT BOEING 737 7373G7 1384595 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT ASSY CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007121400133 20071214 00133 WP 2007 12 14 IXXA070061S 1 20071115 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 240 MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 604BX 46046 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT HAS A IMPROPER REPAIR AND DENT ON FRAME AT STATION 240.0 00 LONGERON-21 RIGHT. REMOVED FASTNER AS NEEDED TO PERFORM REPAIR.REMOVED EXISTING REPAIR.FABRICATED FRAME SEGMENT, SPLI CE AND ANGLE.PERFORMED HEAT TREATMENT TO FRAME SEGMENT, SPLICE AND ANGLE. CLEANED, TREATED AND PRIMED AREA AND REPAIR PA RTS.INSTALLED REPAIR PARTS AND NEW FASTNERS IAW 51-1-11, 51-3-1, DC8 SRM 53-2-0 FIGURE 2 SHEET 2 AND 6, DC8 SRM 51-1-20D , DC8 SRM 53-4-1 FIGURE 40 SHEET 7-9 ITEM "C", SRM 53-2-0 FIGURE 2 SHEET 1, SRM 51-2-0 FIGURE 50 SHEET 49A, DC8 SRM 53-2 -0 FIGURE 2 SHEET 8 T/R 53-110 DATED 11-10-2000, SRM 53-2-0 FIGURE 2 SHEET 7 T/R 53-110 DATED 11-10-2000, DC8 SRM 51-1- 2 L 7 4 4F RT 4A25 2007121400139 20071214 00139 NM 2007 12 14 2007UALA04927 1 20071130 A 2560 131W18201101 GIRT BAR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE L4 DOOR DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 772UA 26930 DOOR 4L WILL NOT ARM. REMOVED FOREIGN OBJECT. LT SIDE OF GIRT BAR, OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121400140 20071214 00140 NM 2007 12 14 NWAA073996740 1 20071209 A 2611 SMOKE DETECTOR BOEING 747 747251F 1384898 NM CARGO BAY FALSE INDICATION A NWAA O OTHER N FALSE WARNING CR CRUISE 1 GL 01 640US 23888 DURING FLIGHT, MAIN DECK CARGO SMOKE DETECTOR ZONE 4 WARNING LIGHT WITH CARGO FIRE LIGHT CAME ON. COM PROCEDURE COMPLIE D WITH. NO VISUAL SIGN OF SMOKE OR OTHER SUBSTANCES. MAINTENANCE REPLACED 4A SMOKE DETECTOR. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2007121400146 20071214 00146 NM 2007 12 14 2007UALA04930 1 20071203 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 MAIN CABIN AFT SECTION AT STA 1640, RBL 20 TO RBL 40, FLOORBEAM CORRODED ON UPPER T-CAP. MAJOR REPAIR ACCOMPLISHED: RE MOVED DAMAGE, FABRICATED & INSTALLED NEW FLOORBEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121400163 20071214 00163 NM 2007 12 14 DLM88071596 1 20071208 A 2750 FLAP SYSTEM DOUG MD88 MD88 3023688 NM MALFUNCTIONED A DALA A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 SO 27 911DL SEM1888 49542 IRR/FLAPS WOULD NOT DEPLOY BEYOND 11 DEGREES DURING APPROACH. COMPLIED WITH QRH DIVERT TI JFK SOFT TOUCHDOWN. LEFT FLA PS AT 11 DEGREE POSITION FOR SHUTDOWN. CYCLED FLAPS TO UP THEN TO 28 FLAPS OPERATE NORMAL. RAN BOTH ENGINES FOR 15 MINS WITH FLAPS UP. ALL FLAP ACTUATORS COLD. PERFORMED BYPASS TEST ON ALL FLAP ACT. ALL OPS NML. OK FOR SVC. ALL RII CK S OK. 2 L 7 2 4F RT A6WE 2007121400165 20071214 00165 NM 2007 12 14 DL76G071598 1 20071204 A 5330 146T32112 SKIN BOEING 767 767324 1385203 NM FS 1300 S26-36L NICKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 394DL 27394 MINOR NICKS IN SKIN BLENDED IN STA 1219 - 1307/STR 26L - 36L. 2 L 7 2 4F RT A1NM 2007121400171 20071214 00171 EU 2007 12 14 F3LA20700364 1 20071205 A 3220 D64433 PIN AIRBUS A319 A319112 3930323 EU NLG CENTERING CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 901FR 5849 1488 DURING C-5 CHECK, INSPECTION REPORTED PITTING ON SHOULDER OF NLG TORQUE LINK CENTER PIN. REMOVED AND REPLACED NLG TORQU E LINK CENTER PIN IAW 32-21-27-420-050. PERFORMED FUNCTIONAL CHECK OF THE NORMAL EXTENSION AND RETRACTION OF THE NOSE L AND GEAR IAW AMM 32-31-00-720-003. CHECKED GOOD. PERFORMED FUNCTIONAL TEST OF THE NOSE WHEEL STEERING IAW AMM 32-51-00 -720-003. CHECKED GOOD. 2 L 7 2 4F RT A28NM 2007121400180 20071214 00180 NM 2007 12 14 AALA20072396 1 20071207 A 3350 0202365001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 795AN 30257 NRT - EMERGENCY LIGHTS AT RIGHT MID GALLEY MISSING LENS. REPLACED LIGHT ASSEMLY FOR EMERGENCY LIGHT AT RIGHT MID GALLEY . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121400181 20071214 00181 EU 2007 12 14 AALA20072397 1 20071207 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 8067A 510 MIA - EMERGENCY LIGHT AT SEAT 32G INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 32G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121400182 20071214 00182 EU 2007 12 14 AALA20072398 1 20071207 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 8067A 510 MIA - EMERGENCY LIGHT AT SEAT 19G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 19G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121400183 20071214 00183 EU 2007 12 14 AALA20072399 1 20071207 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 8067A 510 MIA - EMERGENCY LIGHT AT SEAT 1G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 1G. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT A35EU 2007121400198 20071214 00198 EU 2007 12 14 F3LA200700368 1 20071207 A 5321 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CABIN BROKEN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 901FR 5849 1488 DURING C-5 CHECK, INSPECTION REPORTED FLOOR PANEL 151PE IN AFT CARGO COMPARTMENT BROKEN INTERNALLY. REMOVED PANEL 151PE IAW SRM 51-42-11. DETERMINED PANEL TO BE BROKEN IN HALF (FULL LENGTH OF PANEL) AND OUT OF LIMITS IAW SRM 53-02-00, FIG 206, SHEET 2. REPLACED FLOOR PANEL 151PE IAW SRM 53-42-14-400-001. 2 L 7 2 4F RT A28NM 2007121400201 20071214 00201 EU 2007 12 14 07FDEA05023 1 20071211 A 3230 837101A ELECTRONIC UNIT AIRBUS 310 A310203 3930313 EU MLG INOPERATIVE A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 429FE 2455 2455 364 LANDING GEAR WOULD NOT RETRACT ON EITHER SYSTEM ATTEMPTED TO INTERROGATE THE PROXIMITY ELECTRONIC UNIT. UNIT WOULD NOT TEST NOT EVEN LIGHT TEST. REMOVED AND REPLACED PROX ELEC UNIT IAW 32-31-71-4, CHECKS GOOD. MOCC REQUESTS ALT LDG GEAR RELAY TEST. R/I. PREMATURE REMOVAL/INSTALLATION OFF MFG 8-371-01A. PERFORMED FUNCTION TEST IAW M/M 32-31-00-5, STE P 3(D)(5). TEST CHECKS GOOD. PERFORMED FUNCTION TEST IAW M/M 32-31-00-5, STEP 3(D)(5). TEST CHECKS GOOD. REMOVED AND REPLACED LT MLG PITCH DAMPER PER AMM. 2 L 7 2 4F RT A35EU 2007121400204 20071214 00204 WP 2007 12 14 07FDEA05029 1 20071211 A 5347 S4929150 SEAT TRACK DOUG MD10 MD1010F 3022112 WP BS 1229-1286 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 MAIN CABIN, BS 1240, LBL 48, SEAT TRACK SCALLOP CHIPPED AND WORN RE-EVALUATED TRACK. TRACK HAS CHIPPED/BROKEN AREAS. O UT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21 AND 22. REMOVED DAMAGED SECTION AND INSTALLED FABED/NEW SECTION IA W DC/MD10-10 SRM 51-31-01 VOL II PG 1, DC/MD10-10 SRM 51-33-01 VOL II PG 1. MAT ID NEW TRACK. FABED NEW SECTION IAW DC /MD10-10 SRM 53-70-00 VOL I PG 4. ALODINED AND PRIMED TRACK IAW DC/MD10-10 SRM 51-21-01 VOL II PGS 1-24. REMOVED AND R EINSTALLED FLOOR PANELS IAW MD10-10 M/M 53-21-01-2. 2 L 7 3 4F RT A22WE 2007121400205 20071214 00205 NM 2007 12 14 07FDEA05030 1 20071211 A 2820 VALVE BOEING 727 727247 138408F NM FUEL CROSSFEED MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 237FE 21331 NR 2 FUEL TANK CROSS FEED WOULD NOT OPEN UP IN FLIGHT. ACN RELEASED FOR SERVICE. CLEANED AND RESEATED NR 2 FUEL CROSSF EED MAINIFOLD VALVE CONNECTOR PER SMP. TRANSFERED FUEL FROM NR 2 INTO 1&3 TANKS. PERFORMED TEST OF VALVE PER AMM 28-22-0 11-4. SYS CHECKS NORMAL. 2 L 7 3 4F A3WE 2007121400206 20071214 00206 EU 2007 12 14 07FDEA05033 1 20071211 A 5320 A53611517200 GUSSET AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 LT FWD ENTRY DOOR OPENING LOWER AFT CORNER HAS DEFECT INDICATION FROM EDDY CURRENT CORNER STRAP EDGE. CLEANED AREA IAW FEDEX A310-200 SRM 51-74-10. AREA WAS FOUND TO HAVE SEVERE INTERGRANULAR CORROSION REQUIRING COMPONENT REPLACEMENT. RE MOVED STRAP IAW FED EX A310-200 SRM 51-40-21 PAR 7. MAT ID 2024 T351 IAW AIRBUS DWG 12A536101516 REV D AND ABS 5032. M ACHINED CORNER STRAP IAW AB DWG 12A536 11576 REV D. FORMED CORNER STRAP IAW AB DWG 12A53611516 REV D. ALODINED, PRIMED AND PAINTED CORNER STRAP IAW FED EX A310-200 SRM 51-75-10. INSTALLED CORNER STRAP IAW FED EX A310-200 SRM 51-40-21 PAR A 7. 2 L 7 2 4F RT A35EU 2007121400217 20071214 00217 NM 2007 12 14 2007UALA04940 1 20071203 A 3350 SOCKET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 502UA 24623 EMERGENCY ESCAPE LIGHT INOP 18C, SEAT MOUNTED. FOUND DAMAGED SOCKET. REPAIRED SOCKET, RELAMPED OPS CHECK NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121400218 20071214 00218 EU 2007 12 14 F3LA200700370 1 20071204 A 3350 321431 BATTERY PACK AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHTS NO TEST A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 901FR 1488 DURING C-5 CHECK, INSPECTION REPORTED LT OVERWING EMERGENCY BATTERY EPSU FAILED CAPACITY TEST. REMOVED AND REPLACED EPS U BATTERY AND PERFORMED OPS CHECK IAW AMM 33-51-38-000-002. CHECKED GOOD. 2 L 7 2 4F RT A28NM 2007121400232 20071214 00232 NE 2007 12 14 2007UALA04947 2 20071203 A 7250 BLADE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 2 ENGINE DAMAGED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 218UA 30222 222034 NR 2 ENG HAS HPT STG 1 BLADE TRAILING EDGE BREAKTHROUGH INTO INTERNAL CAVITY. 1 BLADE TRAILING EDGE BREAKTHROUGH INTO I NTERNAL CAVITY. REPLACED WITH ESN 222175 IN POS 02. PER TOD AMM 71-00-02 CONFIG 2 FIG 422. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121400237 20071214 00237 NM 2007 12 14 2007UALA04952 1 20071204 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 FUSELAGE FORWARD ENTRY DOOR (1L) CUTOUT UPPER HINGE CUTOUT BEAR STRAP IS CRACKED OUT OF FASTENER HOLE BELOW LOWER GUIDE PLATE. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE & ACCMP'D NDT FOR CRACK CONTAINMENT. ACCMP'D INSURANCE CUT. FABRICA TED & INSTALLED EXTERNAL DOUBLER & FILLER REPAIRS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121400239 20071214 00239 NM 2007 12 14 2007UALA04954 1 20071204 A 5313 STRINGER SPLICE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 FWD ENTRY DOOR CUTOUT STRINGER SPLICE CHANNEL CRACKED AT BS 360 AND STRINGER 16L. MAJOR REPAIR ACCOMPLISHED: REPLACED STRINGER SPLICE CHANNEL AT BS 360 STR 16L. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121400258 20071214 00258 NM 2007 12 14 2007UALA04964 1 20071204 A 5210 ACCUMULATOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE L2 & R2 DOORS LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 845UA 1585 EMERGENCY CYLINDER ACCUMULATOR PRESSURE IS LOW AT DOORS 2L & 2R. FOUND LEAKAGE FROM PRESSURE CYLINDER. SERVICED ACCU MULATOR, ABLE TO HOLD PRESSURE WITH NO DECAY. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121400266 20071214 00266 2007 12 14 AMTA200700615 4 20071117 A 3197 CIRCUIT CARD BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LOOSE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 518AT 27974 BOTTOM EICAS SCREEN FLICKEERS/ FAILS WHEN COMPUTER IN AUTO/ OPERATES NORMAL WHEN RT COMPUTER SELECTED. FOUND EICAS SWIT CHING MODULE CARD NOT PROPERLY SEATED SWAPPED CARDS AND ALL SCREENS CHECKED GOOD FROM BOTH COMPUTERS. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007121400271 20071214 00271 EU 2007 12 14 2007UALA04971 1 20071205 A 3397 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 433UA 589 EMERGENCY LTS TEST FAILS WITH `AFT L EXT LTS` FAILURE MSG. FOUND DIRTY CONNECTION INSIDE SLIDE RAFT. REMOVED SLIDE AND CLEANED CONNECTOR- ALL OPS CHECK OK. NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121400282 20071214 00282 NM 2007 12 14 2007UALA04982 1 20071205 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 198UA 28716 E-ZONE EMERGENCY LIGHTS RIGHT SIDE WILL NOT TURN OFF. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121400293 20071214 00293 NM 2007 12 14 HNAA0700281 1 20071202 A 3230 83200506003 CABLE DHAV DHC8 DHC8102 2809003 NM COCKPIT BROKEN A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 931HA 49566 49566 132 MAIN LANDING ALTERNATE RELEASE CABLE BROKE IN FLIGHT DECK AT T-HANDLE. REMOVED AND REPLACED THE CABLE, OPERATIONAL CHEC K GOOD. 2 H 7 2 4T RT A13NM 2007121400301 20071214 00301 WP 2007 12 14 ABXA070414 1 20071123 A 3350 60030451 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 984AX 117 47258 EMERGENCY POWER LIGHTING INOPERATIVE, NO P-NUT BULB ILLUMINATION. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW DC-9 AMM 33 -53-02-4. 2 L 7 2 4F A6WE 2007121400304 20071214 00304 SO 2007 12 14 C2XA07TY075 1 20071204 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12921 145354 CARGO DOOR SILL CORRODED. REMOVED AND REPLACED SILL IAW EMB 135/145 SRM 51-40-02, 51-20-03. ALODINED, PRIMED & PAINTED IAW EMB 135/145 CPM 51-21-04, 05, 06. AIRCRAFT STILL IN C-CHECK. 2 L 7 2 4T RT T00011AT 2007121400311 20071214 00311 EU 2007 12 14 TRAX200701868 1 20071204 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 633AS 344 RIGHT SIDE FUSELAGE EMERGENCY LIGHT INOP. 2 H 7 2 4T RT 2007121400315 20071214 00315 EA 2007 12 14 TRAX200701873 1 20071205 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 826AS 7210 NR 4 EMERGENCY LIGHT BATTERY WILL NOT TURN ON LIGHTS. 2 L 7 2 4F RT A21EA 2007121400316 20071214 00316 EA 2007 12 14 TRAX200701874 1 20071205 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 27 827AS 7212 ON APPROACH AT 170 KNOTS WITH FLAPS SELECTED AND INDICATING 20 DEG, SELECTED FLAPS TO 30 DEG, RECEIVED FLAPS FAIL AT 20 DEG. EN ROUTE TO SCE A/C DIVERTED TO MDT DUE TO MTC. EMERGENCY EQUIPMENT ON STANDBY. 2 L 7 2 4F RT A21EA 2007121400328 20071214 00328 NM 2007 12 14 PIDA07051 1 20071205 A 5320 TIE CLIP BOEING 737 737228 13844AG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 252TR 23001 DURING MAINTENANCE CHECK, NOTED STRINGER TIE CLIP CRACKED AT BS 727B AT STR 6RT. REPLACED TIE CLIP PER SRM 51-30-2. 2 L 7 2 4F RT A16WE 2007121400340 20071214 00340 EU 2007 12 14 UPS07151263 1 20071206 A 3230 CONTROL MODULE AIRBUS A300 A300F4622R 3930360 EU LANDING GEAR FAULTY A IPXA K NONE O OTHER TO TAKEOFF 1 SO 01 165UP 0005 INSPECTION TYPE:N/A ON TAKEOFF LANDING GEAR WOULD NOT GO UP PAST NEUTRAL. LEVER PUT BACK DOWN; GEAR DOWN 3 GREEN ALL NO RMAL. DEFERRED IAW MEL 32-30-01. DMI 364010 REMOVED AND REPLACED LANDING GEAR CONTROL MODULE PER MM 32-31-11-04 PARA 2. PERFORMED OPS CHECK IAW MM 32-31-11-04 AND 32-00-00-05. ALL OPS NORMAL. DEFERRAL CLEARED, PLACARD REMOVED. 2 L 7 2 4F RT A35EU 2007121400342 20071214 00342 CE 2007 12 14 DXTA200702654 1 20071206 A 3297 WIRE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG DAMAGED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 639QS 5605139 AFTER TAKEOFF AND POSITIVE RATE LANDING GEAR WAS SELECTED UP, THE (3) GEAR LIGHTS EXTINGUISHED BUT THE RED UNLOCK LIGHT ILLUMINATED. REMOVED AND REPLACED WIRE EPR002-APR034 BETWEEN PLUGS PR002 AND PR034 IAW WIRING MANUAL 20-10-01. OPS CHE CK GOOD IAW 32-61-00 AND 32-01-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007121400356 20071214 00356 NM 2007 12 14 UPS07M51259 1 20070921 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C MAIN DECK: ALONG BS 1966, ALONG X=107 (LBL 107), LT MOST O/B SEAT TRACK CROWN AREAS FOUND CORRODED. C ORROSION ON SEAT TRACK CROWN AREAS REMOVED PER SRM 51-21-01V.2.R.35. CORRODED SEAT TRACK AT STA 1821 LBL 107 TRIMMED OF F PER SRM 53-700-00D.FIG.1 V.1.R.40. NEW REP PARTS REWORKED PER SRM 53-70-00D FIG.1V.1R.40. NEW SEAT TRACK & REP PARTS HOLES PICK UP & REPROTECTED PER SRM 51-31-01&V.2R.40. NEW SEAT TRACK FR STA 1821 TO STA 2007 LBL 107" & REP PART INSTA LLED PER SRM 51-31-01V2. 2 L 7 3 4F RT A22WE 2007121400357 20071214 00357 NM 2007 12 14 UPS07M51261 1 20071008 A 5514 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:C RT HOR STAB NR 36 BARREL NUT HOLE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED PER SRM 51-21- 01 V.2.R35. BARREL NUT BORE REAM FURTHER TO 2.586" DIA & BOTTOM MACHINE DOWN TO 0.075" PER EN168 9-07. BARREL NUT BORE BOTTOM & BLEND OUT PERIPHERY RADIUS, SMOOTHEN & PROTECTED PER SRM 51-21-01V.2R.35. REP SLEEVE BUSHING FAB & PROTECTED PER EO MD1 1-5510-19409-L. REP C/OUT AT NR 36RT BORE IS ACCEPTABLE PER EN1689-07. 2 L 7 3 4F RT A22WE 2007121700003 20071217 00003 NM 2007 12 17 USAA920071260 1 20071204 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 24781 PIT - MAJOR REPAIR - A- NR 03-0553-8-0349-6, CRACK ON FWD PRESS BLKD AT BS 178, WL 218, LBL 11.750. REPAIRED IAW SRM 53 -10-08 REPAIR 9. 2 L 7 2 4F RT A16WE 2007121700018 20071217 00018 NM 2007 12 17 USAA920071275 1 20071202 A 5313 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR -C-18- NR I2B53003/1, CORROSION ON STRINGER AT BS 535, S26L. REPAIRED IAW SRM 53-00-03-2 FIG 201 DET AIL VII. 2 L 7 2 4F RT A16WE 2007121700027 20071217 00027 NM 2007 12 17 USAA920071284 1 20071204 A 5314 KEELBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR-C-18- NR I2B53003/4, CORROSION ON KEEL BEAM LOWER CHORD AT BS 500D, S28R. REPAIRED IAW 53-30-12-2R, REPAIR 2. 2 L 7 2 4F RT A16WE 2007121700030 20071217 00030 NM 2007 12 17 USAA920071287 1 20071114 A 5330 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR-C-18- NR I1A53039/1, CRACK ON FUSELAGE SKIN AT BS 292, S13R - S14R. REPAIRED IAW SRM 53-00-01A. 2 L 7 2 4F RT A16WE 2007121700031 20071217 00031 NM 2007 12 17 USAA920071288 1 20071130 A 5320 65C264594 FLOOR SUPPORT BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR-C-18- NR I2D53012/4, CORROSION ON FLOOR SUPPORT (STRAP) AT BS 727D+5", S17R. REPLACED IAW SRM 51-10- 02. 2 L 7 2 4F RT A16WE 2007121700034 20071217 00034 NM 2007 12 17 USAA920071294 1 20071107 A 5315 141N293217 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 200UU 27809 MCN - MAJOR REPAIR - C4 CHECK - NR 6051873, CORROSION ON CABIN FLOORBEAM CHORD, BS 324, RBL 45.75 - RBL 58, WL 208. REP AIRED CABIN FLOORBEAM CHORD, BS 324, RBL 45.75 - RBL 58, WL 208 IAW B757 SRM 51-70-12. 2 L 7 2 4F RT A2NM 2007121700035 20071217 00035 NM 2007 12 17 SA07079 1 20071205 A 3350 321454 BATTERY AIRBUS A319 A319132 3930340 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 802AW 0924 PHX - DURING THE EMERGENCY LIGHTS TEST, THE FORWARD LEFT EMERGENCY LIGHT BATTERY FAILED. MAINTENANCE REPLACED THE FORWA RD LEFT EMERGENCY LIGHT BATTERY. OPERATIONALLY TEST OK. 2 L 7 2 4F RT A28NM 2007121700036 20071217 00036 NM 2007 12 17 HNAA0700286 1 20071205 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM CARGO BAY DEFECTIVE A HNAA K NONE N FALSE WARNING DE DESCENT 1 EA 07 982HA 17841 17841 380 BAG BAY SMOKE WARNING AND MASTER WARNING LIGHT ILLUMINATED SEVERAL TIMES ON DESCENT TO HTS STARTING AT 6000 FEET THROUGH TOUCHDOWN. REMOVED AND REPLACED BOTH SMOKE DETECTORS IN THE BAG BAY, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2007121700037 20071217 00037 NM 2007 12 17 HNAA0700285 1 20071206 A 3150 WARNING SYSTEM DHAV DHC8 DHC8102 2809003 NM COCKPIT MALFUNCTIONED A HNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 07 805EX 228 AIRCRAFT TAKEOFF WAS ABORTED DUE TO WARNING HORN SOUNDING IN COCKPIT. AIRCRAFT WAS GROUND RUN AND TAKEOFF WARNING SYSTE M WAS CHECKED IN DIFFERING CONFIGURATIONS IAW MAINTENANCE MANUAL PROCEDURES. NO DEFECTS WERE FOUND AND AIRCRAFT WAS REL EASED FOR SERVICE. 2 H 7 2 4T RT A13NM 2007121700040 20071217 00040 NM 2007 12 17 NOCA16907 1 20071209 A 2781 211C223521 SWITCH BOEING 757 75728A 1384976 NM L/E SLAT FAULTY A NOCA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 750NA 26277 LEADING EDGE SLAT DISAGREE EICAS MSG WHILE RETRACTING FLAPS 1 TO 0 AIR TURNBACK TO JFK. T/S PER FIM TASK 27-51-00 FIG 1 04B AND 115 FOUND SWITCH S1 CONNECTOR AT FAULT. REMOVED AND REPLACED S1 SWITCH AS PER MM 27-51-29 ACOMP REQ, OPS CHECKS OK. 2 L 7 2 4F RT A2NM 2007121700045 20071217 00045 EU 2007 12 17 UPS07151270 1 20071207 A 3350 SIGN AIRBUS A300 A300F4622R 3930360 EU CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 148UP 0831 INSPECTION TYPE:N/A ENTRY DOOR EXIT MARKING SIGN HAS 3 INOP BULBS. RELAMPED AND TESTED IAW 33-51-05. OPS CHECKS GOOD. 2 L 7 2 4F RT A35EU 2007121700055 20071217 00055 NM 2007 12 17 SB07104 1 20071209 A 2751 2061141 INDICATOR BOEING 737 7374B7 1384702 NM COCKPIT FAULTY A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 441US 3336 3336 24812 PIT FLT 1512 - ON APPROACH TO PIT, AS CREW SELECTED FLAPS PAST 5 UNITS, A SPLIT FLAPS CONDITION OCCURRED AND THE FLAPS S TOPPED MOVING. CREW RETURNED FLAP LEVER TO 5 UNITS AND FLAPS CAME BACK TO A SYMMETRICAL POSITION. FLIGHT LANDED WITHOU T FURTHER INCIDENT AT 5 UNITS. AN EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FLAP POSITION INDICATOR PER MM 27-58-41-4. OPERATIONAL CHECK NORMAL. ALSO, REMOVED AND REPLACED A WORN RIGHT-HAND INBOARD FOREFLAP AND TOGGLE ASSEMBLY. OPERATIONAL CHECK OF FLAPS NORMAL. 2 L 7 2 4F RT A16WE 2007121700063 20071217 00063 NM 2007 12 17 SWAA076070 1 20071209 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 742C, STR 14R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700097 20071217 00097 NM 2007 12 17 SWAA076090 1 20071206 A 2121 215101 GASPER FAN BOEING 737 7373Q8 1384670 NM E&E BAY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 29 695SW 23506 ON APPROACH CREW REPORTED AN ELECTRICAL ODOR IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2007121700098 20071217 00098 NM 2007 12 17 SWAA076055 1 20071209 A 5311 6546532 FRAME BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700101 20071217 00101 NM 2007 12 17 SWAA076056 1 20071208 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 713SW 27847 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER M M. 2 L 7 2 4F RT A16WE 2007121700117 20071217 00117 NM 2007 12 17 USAA920071300 1 20071207 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C16 CHECK - NR 6050280, CRACKED STRINGER TIE CLIP, BS 727A, S10L. REPLACED STRINGER TIE CLIP, BS 7 27A, S10L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007121700130 20071217 00130 NM 2007 12 17 USAA920071313 1 20071129 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK, CRACKED STRINGER TIE CLIP, BS 706, S11L. REPLACED STRINGER TIE CLIP, BS 706, S11L IAW B 737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007121700131 20071217 00131 NM 2007 12 17 USAA920071314 1 20071203 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK, CRACKED FRAME BS 480, S8R. REPAIRED FRAME, BS 480, S8R IAW USAIRWAYS TYPICAL REPAIR 53- 10-25. 2 L 7 2 4F RT A16WE 2007121700140 20071217 00140 SO 2007 12 17 RAIA00712006 1 20071207 A 3610 O-RING EMB 145 EMB145 3260210 SO BLEED AIR SYS BLOWN A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 812HK 145373 FLT 5511 - STL - DUAL BLEED LEAK WHILE CLIMBING DURING SECOND HALF OF ICE TEST ACCOMPANIED BY A GOOD `POP`. MAINTENANCE FOUND BLOWN O-RING ON BLEED LINE IN BELLY. REMOVED AND REPLACED O-RING, OPS TESTED AND LEAK CHECK GOOD. 2 L 7 2 4F RT T00011AT 2007121700141 20071217 00141 2007 12 17 SB07106 4 20071211 A 2565 D17978113 BOTTLE AIRCRUISERS BOEING 737 7374B7 1384702 NM L2 DOOR LOW PRESSURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 000765 24781 PIT - MAINTENANCE REPORTED THE AFT LEFT ENTRY DOOR EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE WAS LOW. MAINTENANCE REMOVED AND REPLACED THE SLIDE ASSEMBLY PER MM 25-61-35. 2 L 7 2 4F RT A16WE 2007121700142 20071217 00142 EU 2007 12 17 Y2LA200700005 1 20071210 A 2120 UNKNOWN AIRBUS A319 A319112 3930323 EU COCKPIT SMOKE A Y2LA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 07 522VA 2811 AFTER LANDING THE COCKPIT AND CABIN FILLED WITH SMOKE. 2 L 7 2 4F RT A28NM 2007121700144 20071217 00144 NM 2007 12 17 SWAA076116 1 20071210 A 5311 6546549 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700145 20071217 00145 NM 2007 12 17 SWAA076126 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700147 20071217 00147 NM 2007 12 17 SWAA076124 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700150 20071217 00150 NM 2007 12 17 SWAA076119 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700151 20071217 00151 NM 2007 12 17 SWAA076127 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700153 20071217 00153 NM 2007 12 17 SWAA076122 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007121700154 20071217 00154 NM 2007 12 17 SWAA076115 1 20071210 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700158 20071217 00158 NM 2007 12 17 SWAA076111 1 20071210 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700159 20071217 00159 NM 2007 12 17 SWAA076110 1 20071210 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700161 20071217 00161 NM 2007 12 17 SWAA076108 1 20071210 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 14R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700162 20071217 00162 NM 2007 12 17 SWAA076118 1 20071210 A 5311 6546557 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700163 20071217 00163 NM 2007 12 17 SWAA076143 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007121700164 20071217 00164 NM 2007 12 17 SWAA076146 1 20071210 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 12L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007121700165 20071217 00165 NM 2007 12 17 SWAA076120 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700166 20071217 00166 NM 2007 12 17 SWAA076144 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007121700167 20071217 00167 NM 2007 12 17 SWAA076128 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700168 20071217 00168 NM 2007 12 17 SWAA076142 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007121700173 20071217 00173 NM 2007 12 17 SWAA076136 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007121700175 20071217 00175 NM 2007 12 17 SWAA076134 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007121700179 20071217 00179 NM 2007 12 17 SWAA076130 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007121700181 20071217 00181 NM 2007 12 17 SWAA076137 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700183 20071217 00183 NM 2007 12 17 SWAA076096 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 22R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007121700184 20071217 00184 NM 2007 12 17 SWAA076097 1 20071210 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700185 20071217 00185 NM 2007 12 17 SWAA076098 1 20071210 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700186 20071217 00186 NM 2007 12 17 SWAA076099 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700187 20071217 00187 NM 2007 12 17 SWAA076106 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 270, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700188 20071217 00188 NM 2007 12 17 SWAA076107 1 20071210 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 436, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700190 20071217 00190 NM 2007 12 17 SWAA076148 1 20071210 A 5753 6546435273 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PE R MM. 2 L 7 2 4F RT A16WE 2007121700192 20071217 00192 NM 2007 12 17 SWAA076101 1 20071210 A 2560 PH22300L GLOWSTRIP BOEING 737 7375H4 138449D NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED MV4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 2 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007121700193 20071217 00193 NM 2007 12 17 SWAA076102 1 20071210 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700194 20071217 00194 NM 2007 12 17 SWAA076103 1 20071210 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007121700195 20071217 00195 NM 2007 12 17 SWAA076104 1 20071210 A 5311 6546552 FRAME BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700196 20071217 00196 NM 2007 12 17 SWAA076105 1 20071210 A 2560 65C16820 HOOK BOEING 737 7377H4 1384404 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 755SA 27871 L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2007121700197 20071217 00197 EU 2007 12 17 TRAX200701879 1 20071127 A 5310 DOOR FRAME AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 FR 45 AFT SIDE CORRODED AT AFT AVIONIC DOOR HOLE. 2 H 7 2 4T RT 2007121700199 20071217 00199 EU 2007 12 17 TRAX200701881 1 20071128 A 5220 BRACKET AEROSP ATR72 ATR72 EU EMERGENCY EXIT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 RIGHT EMERGENCY DOOR BONDING BRACKET CRACKED. 2 H 7 2 4T RT 2007121700201 20071217 00201 EU 2007 12 17 TRAX200701885 1 20071207 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN INTERMITTENT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 ASD DOOR LOWER EMERGENCY LIGHT INTERMITTENT. 2 H 7 2 4T RT 2007121700202 20071217 00202 EA 2007 12 17 TRAX200701887 1 20071208 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 722EV 10127 EXIT LIGHT AT 1A + B IS OUT. 2 L 7 2 4F RT A21EA 2007121800001 20071218 00001 EU 2007 12 18 YENA2007110 1 20071122 A 3397 WIRE AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS DAMAGED A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 632JB 2647 EMERGENCY LIGHTING A ROW 7 INOP. WIRES PULLED FROM CONNECTOR. ITEM IS (OPEN) PLACED ON MEL 33-50-03, CAT C UNDER CONTRO L NUMBER L01907. 2 L 7 2 4F RT A28NM 2007121800002 20071218 00002 EU 2007 12 18 07FDEA04991 1 20071204 A 5610 NP1752012 WINDSHIELD AIRBUS 310 A310324 3930206 EU COCKPIT CRACKED A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 806FD 2770 458 A/C HAS DIVERTED INTO CUN DUE F/O WINDSHIELD HAS SHATTERED. REMOVED AND REPLACED F/O WINDSHIELD A310-300 M/M 56-11-1 1-4, OPN CHECK IS GOOD. OK FOR SVC. REPLACED WINDSHIELD TEMP REGULATOR AS A PRECAUTION AMM 30-42-11-4 REPLACED WINDOW HEAT PROTECTION CONTROLLER AS A PRE AUTION AMM 30-42-51-4 2 L 7 2 4F RT A35EU 2007121800003 20071218 00003 EU 2007 12 18 07FDEA04993 1 20071204 A 5730 SKIN AIRBUS 310 A310203 3930313 EU LT WING MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 402FE 201 LEFT WING EXTERNAL REPAIR DOUBLER ON TRAILING EDGE END RIB, APPROXIMATE WING STATION 1278 BETWEEN WING RIBS 20 AND 21 RE AR SPAR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVAL UATED REPAIR, FOUND NOT TO BE WITHIN APPROVED DATA. REMOVED DAMAGED RIB AND REPLACED WITH NEW PART. FABED ON FEDEX NR N01216 AND N01215. INSTALLED I/A/W A310- 200 SRM 51-40-21 PG. 25. 2 L 7 2 4F RT A35EU 2007121800004 20071218 00004 EU 2007 12 18 UPS07151241 1 20071204 A 3610 VALVE AIRBUS A300 A300F4622R 3930360 EU NR 1 ENGINE OPEN A IPXA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 01 131UP 0815 DIVERSION, NR 1 HP VALVE UNCOMMANDED OPEN. DEFERRED PER MEL. D363807 ASSIGNED. R&R NR 1 ENGINE HP BLEED CONTROL VALVE PER MM 36-11-17-04. DMI CLEARED. 2 L 7 2 4F RT A35EU 2007121800005 20071218 00005 NM 2007 12 18 WRLA2007130 1 20071201 A 5753 SKIN DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE LT WING TE FLAP DEBONDED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 803DE 48474 DURING C-CHECK INSPECTION FOUND LEFT OUTBOARD FLAP TRAILING EDGE OUTBOARD EDGE SKIN DISBOND 33 X 4.5 INCHES. REPAIRED D AMAGE AS PER EGAT EI NO.W2007A57B-710 REV.1 REF EGAT NRC U07001. 2 L 7 3 4F 4 F RT A22WE E24NE 2007121800006 20071218 00006 NM 2007 12 18 WRLA2007131 1 20071201 A 5310 DOOR FRAME DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE CARGO DOORWAY DAMAGED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 803DE 48474 DURING C-CHECK INSPECTION FOUND CENTER CARGO DOOR JAMB LOWER AFT EDGE DAMAGED. REPAIRED DAMAGE PER MD11 SRM 53-50-00 FI G.17 VIEW B REF WOA ERA 7-53-62. 2 L 7 3 4F 4 F RT A22WE E24NE 2007121800007 20071218 00007 NM 2007 12 18 WRLA2007132 1 20071201 A 5343 TRUNNION DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NLG CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 803DE 48474 DURING C-CHECK INSPECTION FOUND NOSE LANDING GEAR LEFT HAND TRUNNION FITTING CRACKED. REPAIRED LT NOSE LANDING GEAR FIT TING PER MD11 SRM VOL.1 53-40-00 REV.40 REF EGAT NRC U05005. 2 L 7 3 4F 4 F RT A22WE E24NE 2007121800008 20071218 00008 EU 2007 12 18 AALA20072195 1 20071113 A 2780 COMPUTER AIRBUS 300 A300B4605R 3930308 EU FLAP/SLATS INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SW 21 34078 615 SJU INFLIGHT - JFK TO SDQ - SLAT POSITION INDICATION REMAINS AT ZERO WHEN SLAT FLAP HANDLE IS MOVED. LANDED SJU WITHOUT INCIDENT. CHECKED AND LUBRICATED ALL RIGHT AND LEFT SLAT JACKSCREWS. RESET BOTH SLAT FLAP CONTROL COMPUTERS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121800009 20071218 00009 GL 2007 12 18 SIMA200733911 2 20071202 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN 501D 501D22A 03006 GL RIGHT ODOR A SIMA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 918AE 14500902 CAE312297 ON TAKEOFF APPROX 500 ', LAV SMOKE ILLUMINATED WITH ODOR OF SMOKE. FLIGHT ATTENDANT REPORTS HAZE BY LAV, AT 5000' LIGHT EXTINGUISHED. ODOR SUBSIDED. A/C RETURNED TO ORD. REMOVED AND REPLACED RT ENGINE ASSY IAW W/C 71-000-00 OPERATIONA L AND LEAK CHECK GOOD COMPLETED A FCF AND PASSED. AIRCRAFT RETURN TO SERVICE 2 L 7 2 4T 4 T RT T00011AT E282 2007121800010 20071218 00010 CE 2007 12 18 GLBA20061035 1 20071206 A 5260 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE AIRSTAIR DOOR DELAMINATED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 254GL AIRSTAIR DOOR SKIN DELAMINATED AROUND EXTERIOR DOOR HANDLE. MAINTENANCE REMOVED CORROSION AROUND DOOR HANDLE AREA AND ACCOMPLISHED MINIMUM DAMAGE REPAIR I.A.W. B1900D SRM 52-10. RII C/W PER GLA TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007121800011 20071218 00011 SO 2007 12 18 N93A04122007 1 20071204 A 3231 1159SCH23133 VALVE GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE NLG DOOR FAULTY E N93A O OTHER J WARNING INDICATION AP APPROACH 1 SO 13 506QS 623 NOSE LANDING GEAR DID NOT EXTEND NORMALLY AFTER GEAR WAS SELECTED DOWN, AFTER ABOUT 45 SECONDS GEAR EXTENDED NORMALLY, F OUND NOSE LANDING GEAR DOOR CONTROL VALVE AT FAULT. 2 L 7 2 4F 4 F RT A12EA E00057EN 2007121800012 20071218 00012 EA 2007 12 18 TRAX200701869 1 20071204 A 5220 HINGE FITTING CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 RT HINGE CRACKED ON CREW ESCAPE HATCH. REMOVED CRACKED RT. HINGE FITTING ON CREW ESCAPE HATCH AND REPLACED WITH NEW S ERVICEABLE HINGE FITTING P/N 600-33217-1001 IAW CRJ AMM 20-21-00. PAINTED RT. HINGE FITTING IAW CRJ SRM 51-25-16. REFER TO W/C 50246/2000/0005 FOR OPS CHECK. 2 L 7 2 4F RT A21EA 2007121800013 20071218 00013 NM 2007 12 18 HNAA0700287 1 20071206 A 2910 65960 SPOILER SYS DHAV DHC8 DHC8102 2809003 NM NR 2 FAILED A HNAA O OTHER K FLUID LOSS CR CRUISE 1 EA 07 930HA 49691 49691 126 DURING FLIGHT, NR 2 HYDRAULIC SYSTEM BEGAN LOOSING FLUID. AT 1/2 QT LOSS, SYSTEM ISOLATION VALVE CLOSED TO PREVENT FURT HER LOSS OF FLUID. LANDING GEAR WAS CYCLED DOWN BEFORE ISOLATION VALVE CLOSED AS A PRECAUTION. MAINTENANCE FOUND NR 2 ROLL SPOILER UNLOADING VALVE UNSERVICEABLE. REMOVED AND REPLACED VALVE. SERVICED HYDRAULIC SYSTEM AND OPS CHECKED AIRC RAFT IAW MAINTENANCE MANUAL PROCEDURES. CHECKS WERE GOOD. 2 H 7 2 4T RT A13NM 2007121800016 20071218 00016 EU 2007 12 18 07FDEA05017 1 20071208 A 5320 A5361079723400 FLOOR SUPPORT AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 MAIN CABIN, FLOOR SUPPORT CORRODED FROM FR12 TO FR 16A, (STA X1067 TO X1285) BL 56L (Y1456 ), REMOVED AND REPLACED FL OOR SUPPORT IAW A310-200 SRM 51-40-21 PAR 6 AND 7. 2 L 7 2 4F RT A35EU 2007121800017 20071218 00017 EU 2007 12 18 07FDEA05019 1 20071208 A 5320 A5361060720200 FITTING AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AVIONICS COMPARTMENT FLOOR, FR 17 ( X1315 ) STR 43L, FITTING CORRODED. REMOVED AND REPLACED STRINGER END FITTING IAW A3 10-200 SRM 51-40-21, 51-24-00 AND 51-43-00 TABLE 1. 2 L 7 2 4F RT A35EU 2007121800019 20071218 00019 NE 2007 12 18 DJFA2007140 2 20071207 A 7220 45A35022222 INLET BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE RT ENGINE CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 449LX 3316 RK257 PCEJA0469 DURING POSTFLIGHT, CREW REPORTED CRACKS ON THE NR2 INLET RING. MAINTENANCE CONFIRMED THE DISCREPANCY AND REPLACED THE I NLET RING. 2 H 7 2 4F 4 F RT A16SW E25EA 2007121800020 20071218 00020 GL 2007 12 18 SIMA200734404 2 20071207 A 7200 AE3007A13 ENGINE EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL NR 2 SURGES A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 21 733KR 145368 CAE311013 OIL ODOR FROM AIR CONDITIONING SYSTEM IN COCKPIT AND CABIN DURING CLIMB AND DESCENT IT CLEARS DURING CRUISE. REMOVED AN D REPLACED NR 2 ENGINE IAW WC 71-000-00 PASSED FCF. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007121800021 20071218 00021 NM 2007 12 18 SB07105 1 20071210 A 3397 WIRE BOEING 737 737401 1384701 NM EMERGENCY LIGHTS SHORTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 MAINTENANCE REPORTED THE R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPAIRED SHORTED WIRE AT LAST ROW OF SEAT MOUNTED EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007121800022 20071218 00022 EA 2007 12 18 TRAX200701883 1 20071201 A 5751 HINGE CNDAIR CL600 CL6002B19 1900309 EA AILERONS CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 OUTBOARD RT AILERON WING ATTACH HINGE CORRODED, TOP OF WING HINGE. AFTER FURTHER INVESTIGATION, THE DAMAGE ON THE OUTB OARD RT AILERON WING ATTACH HINGE HAS MINOR SURFACE CORROSION. REMOVED SURFACE CORROSION IAW CRJ 200 SRM 51-21-06. APPLI ED PROTECTIVE FINISH TO REPAIR AREA IAW CRJ 200 SRM 51-25-16. 2 L 7 2 4F RT A21EA 2007121800023 20071218 00023 EU 2007 12 18 TRAX200701884 1 20071206 A 5210 ATTACH ANGLE AEROSP ATR72 ATR72 EU PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 FWD ATTACHMENT ANGLE CRACKED ON PAX DOOR FWD SIDE PANEL. FWD ATTACHMENT ANGLE REPLACED IAW SRM 51-25-01. REPAIR DETERM INED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01. 2 H 7 2 4T RT 2007121800024 20071218 00024 EA 2007 12 18 TRAX200701886 1 20071207 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA RT WING INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 RIGHT WING FLOOR EMERGENCY EXIT LIGHT INOP. REMOVED INOP. RT WING FLOOR EMERGENCY EXIT LIGHT AND INSTALLED SERVICEABLE LIGHT P/N 5020-5 IAW CRJ 200 33-51-10. REQUIRES OPS CHECK. OPS CHECK GOOD IAW CRJ 200 AMM 33-51-01. 2 L 7 2 4F RT A21EA 2007121800025 20071218 00025 NM 2007 12 18 NOCA17007 1 20071212 A 2780 ELECTRONIC UNIT BOEING 757 75728A 1384976 NM FLAP/SLATS MALFUNCTIONED A NOCA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 750NA 26277 LEADING EDGE SLAT DISAGREE MESSAGE AIR TURNBACK INTO KWI. FLAP/SLAT ELECTRONIC UNIT BITE (FSEU) PER FIM 27-51-00 FIG 10 4B UNABLE TO DUPLEATE SWAPPED FSEU NR 1 BOX P/N 285N0011-40 S/N D02243 TO NR 3 BOX POSITION S/N 2244 PER BLOCK NR 16 ALS O ACCOMPLISHED FIM 27-81-00 FIG 104 UNABLE TO DUPLICATED MSG PERFORMED THE ROLLERS LUBICATION PER MM 12-21-08/301 AND OP ERATE THE SLATS AND LUBEICATED THE ROLLERS AGAIN NO CAUTION MGS DISPLAY SYSTEM TEST OK 2 L 7 2 4F RT A2NM 2007121800027 20071218 00027 2007 12 18 07FDEA05051 4 20071213 A 3413 C6646120 PIN AIRBUS 300 A300F4605R 3930327 EU SHEARED A FDEA A UNSCHED LANDING J G S WARNING INDICATION MULTIPLE FAILURE AFFECT SYSTEMS CR CRUISE 1 SO 25 650FE 726 F/O TAT FAILED, CAUSING SECONDARY LOSS OF NR 2 PITCH TRIM, NR 2 CABIN PRESS REGULATOR 34-62 0508. NR 2 INTERMITTENT FOU ND PROX SYS FAULTING SENSOR. REF:MDIS 32 10 0511, BOLT/PIN BROKEN ON RT MLG AT DRAG LINK ATTACHMENT FOR GEAR SENSORS. REMOVED AND REPLACED 62GB SENSOR PER AMM 32-61-00. CLEARED FAULT CODES AND BITE TEST ON PROX BOX SHOWS NO FAULTS.GRO UND SCAN AUTOPILOT SYSTEM PASSED WITH NO FAULTS. 2 L 7 2 4F RT A35EU 2007121900001 20071219 00001 NM 2007 12 19 QXEA200701846 1 20071206 A 2130 CABIN PRESSURE BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 429QX 4161 RDM - CABIN PRESSURE WARNING LIGHT ILLUMINATED. CABIN NOT PRESSURIZING. MAINTENANCE PLACED ON MEL 21-30-5B. AIRCRAFT R ETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007121900002 20071219 00002 EA 2007 12 19 QXEA200701848 1 20071205 A 2612 446648 ELEMENT CNDAIR CL600 CL6002C10 1390015 EA FIRE DETECTION MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 601QX 10009 SEA- FLIGHT 2904 - RECEIVED A FIRE SYSTEM FAULT STATUS MESSAGE. MAINTENANCE REPLACED THE FIRE SENSING ELEMENT. OPERATI ONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007121900003 20071219 00003 EA 2007 12 19 QXEA200701851 1 20071207 A 2612 22402820 FIRE LOOP CNDAIR CL600 CL6002C10 1390015 EA LT NACELLE INTERMITTENT A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 609QX 10031 PDX - FIRE SYSTEM FAULT MESSAGE DISPLAYED. PLACED ON MEL 26-00-1. FOUND LEFT ENGINE LOOP "A" INTERMITTENT, OPEN OR SHO RTED. MEL CONTINUED, FURTHER TROUBLESHOOTING REQUIRED. REPLACED THE FIRE LOOP A. OPERATIONAL CHECKS GOOD. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007121900005 20071219 00005 NM 2007 12 19 QXEA200701795 1 20071204 A 2612 101098 ELEMENT BOMBDR DHC8 DHC8402 1390042 NM NR 2 FIRE LOOP MALFUNCTIONED A QXEA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 NM 09 406QX 4048 RNO - FLIGHT 2551 - ON DESCENT, RECEIVED A NR 2 FIRE WARNING. SHUT DOWN THE ENGINE AND DISCHARGED BOTH FIRE BOTTLES. C FR CALLED. ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF A FIRE OR DAMAGE. REPLAC ED THE NR 2 PEC FIRE LOOP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007121900006 20071219 00006 NM 2007 12 19 QXEA200701773 1 20071202 A 2820 956A15BG62362 SWITCH BOMBDR DHC8 DHC8402 1390042 NM AUX FUEL TANK FAILED A QXEA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 09 417QX 4086 SEA - FUEL TANK 2 AUX PUMP SWITCH WILL NOT ENGAGE. RETURNED TO THE GATE. MAINTENANCE REPLACED THE SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007121900008 20071219 00008 WP 2007 12 19 ARWA20071202 1 20071213 A 7332 FUEL SYS DOUG DC10 DC1030 3023501 WP NR 2 ENGINE LOW PRESSURE A ARWA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 524MD 46999 DURING TAXI, NR 2 ENGINE FUEL PRESSURE INITIALLY INDICATING 20 PSI, THEN DROPPED TO ZERO, AS PER MEL 73-4 CATEGORY "C". REMOVED AND REPLACED # 2 ENGINE FUEL INTERSTAGE PRESSURE TRANSMITTER IAW MM 73-33-01. FUEL PRESSURE INDICATION NORMAL; CLEARED DMI 21297. 2 L 7 3 4F A22WE 2007121900013 20071219 00013 NM 2007 12 19 2007UALA05050 1 20071210 A 3510 OXYGEN SYSTEM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CREW READS LOW A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 938UA 26671 CREW O2 IS INDICATING 650 PSI, LEFT SFO WITH 1400 PSI. SERVICED TO 1750 PSI. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007121900016 20071219 00016 EU 2007 12 19 1214834312170 1 20070920 A 5740 S5721060500103 BRACKET AEROSP ATR42 ATR42320 8680930 EU RT WING CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 14834 193 RIGHT WING AT RIB 17 OF LOWER REAR SPAR SIDE STAY BRACKET CORRODED. REMOVED AND REPLACED FITTING IN ACCORDANCE WITH SRM 51-25-04. 2 H 7 2 4T RT A53EU 2007121900017 20071219 00017 NM 2007 12 19 2007UALA04997 1 20071207 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 FOUND SEATS 2J AFT, 4E FWD, 6GH FWD, 37ABC, 42ABC, AND 61ABC EMERGENCY LIGHTS ARE INOPERATIVE. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121400242 20071214 00242 NM 2007 12 14 NWAA074025638 1 20071212 A 3150 WARNING LIGHT BOEING 757 757251 1384970 NM LT ENG BLEED FALSE ACTIVATION A NWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 01 538US 26485 REJECTED TAKEOFF AT DUS LESS THAN 120 KNOTS FOR FAULTY LEFT ENGINE BLEED AIR LIGHT. A/C EXITED RUNWAY, RECYCLED SWITCH AND REMOVED ITS LIGHT, TAXIED BACK FOR TAKEOFF. TAKEOFF WAS NORMAL, NO FURTHER INCIDENTS. CLIMB-OUT WAS NORMAL. MAINT ENANCE DID A COMPLETE PNEUMATIC OPS CHECK ON BOTH ENGINES. ALL CHECKS GOOD AT THIS TIME, OPERATIONAL CHECKED GOOD, AND A IRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007121400243 20071214 00243 EU 2007 12 14 U30A200700004 1 20071126 A 3150 UNKNOWN AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE WARNING MESSAGE A U30A O OTHER N FALSE WARNING CR CRUISE 1 EA 17 268AV 2175 IN CRUISE, EXPERIENCED ECAM WARNING APU FIRE DET FAULT, & BOTH CARGO BOTTLES DISC LIGHTS ILLUMINATED ON THE P/B SWITCHES , WITH NO ASSOCIATED ECAM, OR WARNINGS. UPON LANDING, AND AFTER ENGINE SHUTDOWN AT GATE, NO POWER ON AC BUSS 2, NO POWER ON TRANSFORMER RECTIFIER NR 2, & APU WOULD NOT CRANK OR START. MAINTENANCE FOUND C/B FIN 30WF POPPED AND THEN RESET IT , WHICH CLEARED THE APU FIRE DET FAULT. THE AC POWER LOSS WAS CLEARED BY FURTHER TROUBLESHOOTING, WHICH LOCATED THAT C/B FIN 11PB HAD POPPED. IT WAS RESET AND TR 2 WAS RESET, A SUCCESSFUL APU WAS C/W, AND ALL AC BUSSES CK'D OK.TESTED APU FI RE DET SYS IAW AMM 26-13-00-PB501, TESTED CARGO SMOKE DET SYS IAW AMM 26-16-00PB501, C/W TSM 24-32-00-810-806 AND 24-32- 2 L 7 2 4F 4 F RT A28NM E38NE 2007121400244 20071214 00244 WP 2007 12 14 AMTA200700598 1 20071115 A 2910 31801312 ACCUMULATOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL NR 3 UNSERVICEABLE A AMTA O OTHER K FLUID LOSS DE DESCENT 1 GL 11 705TZ 46915 SYS 3 HYD FLUID QTY SLOWLY DECREASED TO .5 GALS. PRESS STAYED AT 2800 PSI, TEMP STAYED AT 33 DEGREES. REMOVED AND REPL ACED NR 3 HYD SYS TRANSMITTER FOUND LEAKING IAW 29-12-01. REPLACED SYSTEM ACCUMULATOR. (K) 2 L 7 3 4F 4 F A22WE A23EA 2007121400246 20071214 00246 NM 2007 12 14 AMTA200700601 1 20071115 A 3150 WARNING MESSAGE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE WX RADAR FALSE ACTIVATION A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 522AT 29330 (WXR SYS) STATUS MESSAGE DISPLAYED. WX RADAR OPERATES NORMALLY WITH NO FAULTS INDICATED. MSG CLEARED IAW FIM 34- EICAS MESSAGES, WXR SYS OPS NORMALLY. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007121400249 20071214 00249 NM 2007 12 14 AMTA200700603 1 20071116 A 5320 FLOOR SUPPORT BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE BS 1650-1680 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 522AT 29330 CABIN FLOOR SUPPORT STRUCTURE UPPER SURFACE HAS CORROSION FROM STA 1650 TO 1680, RBL 48. REMOVED CORROSION STA 1650-168 0, RBL 48 IAW SRM 51-20-01, STA 1652-1661, RBL 48 ORIG MAT .071 CORROSION OUT OF LIMITS, STA 1661-1680. CORROSION REMOV ED .005, ORIG MAT .071 WITHIN LIMITS IAW SRM 53-00-51, FIG 101, STA 1652, FLOOR SUPPORT REPAIR. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007121400256 20071214 00256 2007 12 14 2007UALA04962 4 20071204 A 2565 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE LIGHT UNKNOWN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 593UA 28144 SLIDE LIGHT AT DOOR 1R INOP. REARMED TARGET SWITCH AND SYSTEM OPERATES/TESTS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121400259 20071214 00259 NM 2007 12 14 2007UALA04965 1 20071204 A 2697 W3506503506 WIRE BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE NR 3 FIRE LOOP FAILED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 105UA 26473 F-C REPORTED FIRE LOOP A 3 ENG. REPLACED WIRES W3506-503 AND 506 REF SWP 20-30-11, CHECKED ROUTING OF WIRES ON AC 8174 ENG 3-4, AC 8105 ENG NR 3, WIRES ROUTED DIFFERENTLY, REROUTED REPLACED WITH CORRECT CLAMPS. ACCOMP TEST REF MM26-11-00, OPS CHECK PASSED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121400260 20071214 00260 NM 2007 12 14 AMTA200700605 1 20071118 A 5345 FITTING BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE BS 1686 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 552TZ 32586 CORROSION ON FLOOR FITTING GALLEY ATTACHMENT, LOCATED AT STA 1686, BL 0. FOUND CORROSION OUT OF LIMITS IAW SRM 53-00-51 -1A, DETAIL III. REMOVED AND REPLACED FITTING IAW SRM 51-40-02. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007121400265 20071214 00265 2007 12 14 AMTA200700613 4 20071118 A 3460 1762000101 COMPUTER BOEING 737 73783N 13844HI NM FLT MANAGE UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 319TZ 30643 SINGLE FMC OPERATION DISPLAYED IN SCRATCH PAD AND MAP. DISPLAYED ON FO CDU (RIGHT FMC INOP). REMOVED AND REPLACED NR 2 FMC COMPUTER IAW AMM 34-61-02-4. PERFORMED FMC SYS ADJUSTMENT AND TEST IAW AMM 34-61-00-5. OPS CK NORMAL. (K) 2 L 7 2 4F RT A16WE 2007121400269 20071214 00269 2007 12 14 2007UALA04969 4 20071204 A 2565 5A29011B ASPIRATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 649UA PF0174 25286 LEAKING ASPIRATOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121400283 20071214 00283 NM 2007 12 14 2007UALA04983 1 20071205 A 3350 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 577UA 26693 EMERGENCY LIGHT AT OVERHEAD BIN SEAT 5C. FOUND BURNED OUT BULB. REPLACED BULB ASSY FOR OVERHEAD BIN 5C. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121400324 20071214 00324 NM 2007 12 14 PIDA07046 1 20071204 A 5320 TIE CLIP BOEING 737 737228 13844AG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 252TR 23001 DURING MAINTENANCE CHECK, NOTED CRACK IN STRINGER TIE CLIP AT BS 747 AT STR 6RT. REPLACED TIE CLIP PER SRM 51-30-2. 2 L 7 2 4F RT A16WE 2007121400326 20071214 00326 NM 2007 12 14 PIDA07052 1 20071205 A 5320 TIE CLIP BOEING 737 737228 13844AG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 252TR 23001 DURING MAINTENANCE CHECK, NOTED STRINGER TIE CLIP CRACKED AT BS 807 AT STR 10LT. REPLACED TIE CLIP PER SRM 51-30-2. 2 L 7 2 4F RT A16WE 2007121400332 20071214 00332 CE 2007 12 14 DXTA200702653 1 20071205 A 2150 ACM CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE CABIN ODOR E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 640QS 5605240 WHAT SEEMED TO BE AN ELECTRICAL BURNING ODOR DEVELOPED IN THE COCKPIT DURING LEVEL FLIGHT WITH THE ANTIICE SYSTEM (ON) L ASTING APPROXIMATELY 2 MINUTES. FOUND BAD ACM AND HEAT EXCHANGER ASSY. REMOVED THE ECU ACM S/N AND HEAT EXCHANGER AND INSTALLED NEW HEAT EXCHANGER AND AN OVERHAULED ACM WITH A NEW PLENUM. PERFORMED AN OPERATIONAL CHECK OF THE ECS SYSTEM. OPS CHECKS AND LEAK CHECKS PASS. ALL WORK ACCOMPLISHED IAW MM 21-51-00 AND THE OPERATION AND MAINTENANCE SOURCE DATA REP ORT 4-401 ECU. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007121700012 20071217 00012 NM 2007 12 17 USAA920071269 1 20071202 A 5347 SEAT TRACK BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C-18-NR I1C53043/15, SEAT TRACK CRACKED AT BS 663, LBL 24. REPAIRED IAW EA1000040. 2 L 7 2 4F RT A16WE 2007121700015 20071217 00015 NM 2007 12 17 USAA920071272 1 20071206 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR-C-18- NR I1C53037/7, CRACK ON FRAME AT BS 400 BETWEEN S8R & S9R. REPAIRED IAW EA10048. 2 L 7 2 4F RT A16WE 2007121700016 20071217 00016 NM 2007 12 17 USAA920071273 1 20071202 A 5310 CREASE BEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR -C-18-NR I1C53043/16, LT CREASE BEAM WEB CRACKED AT BS 616-639, LBL 70. REPLACED IAW BOEING DRWG 65C 3473, SRM 51-40-03. 2 L 7 2 4F RT A16WE 2007121700023 20071217 00023 NM 2007 12 17 USAA920071280 1 20071129 A 5320 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR-C-18- NR I2D53012/1, CORROSION ON WEB AT BS 787, S25R. REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007121700026 20071217 00026 NM 2007 12 17 USAA920071283 1 20071203 A 5340 6935352014 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23777 CLT - MAJOR REPAIR-C-18- NR I1C53040/3, CRACK ON STRINGER TIE CLIP AT BS 663, S10R. REPLACED IAW 51-00-00. 2 L 7 2 4F RT A16WE 2007121700029 20071217 00029 NM 2007 12 17 USAA920071286 1 20071121 A 5320 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR-C-18- NR 03-0553-8-0105/2, CRACK ON BEAM (WEB) AT BS 178, LBL 17, WL 184. REPAIRED IAW SRM 70-13-0G. 2 L 7 2 4F RT A16WE 2007121700046 20071217 00046 NE 2007 12 17 UPS07551267 2 20071208 A 7200 PWA2040 ENGINE BOEING 757 75724APF 1384969 NM PWA 2037 PW2040 NE NR 1 MALFUNCTIONED A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 01 409UP 23731 INSPECTION TYPE:AS/E NOTICED PREVIOUSLY NOTED SMELLS ON T/O AND LANDING, BUT SMELLS WERE NOT STRONG AND LASTED FOR A VER Y SHORT TIME. CHANGED ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121700050 20071217 00050 SO 2007 12 17 RAIA00712001 1 20071202 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 817HK 145058 POST FLT 5576 - STL- PAX KICKED EMERGENCY EXIT LIGHT AT ROW 13 LOOSE. MAINTENANCE SECURED WIRES TO LIGHT, OPS CHECK GOO D. 2 L 7 2 4F RT T00011AT 2007121700054 20071217 00054 NM 2007 12 17 SB07103 1 20071207 A 2750 FLAP BOEING 737 7374B7 1384702 NM WING MALFUNCTIONED A USAA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 EA 19 441US 24812 JAX - FLT 1652 - ON APPROACH TO JAX, CREW REPORTED WHEN SELECTING FLAPS TO 15 UNITS, FLAPS STAYED AT 10 UNITS. CREW ACC OMPLISHED GO-AROUND AND QUICK REFERENCE HANDBOOK PROCEDURES. WHEN CREW PLACED FLAP SELECTOR BACK TO 10 UNITS, FLAP INDI CATOR WAS NOW IN AGREEMENT. CREW THEN SELECTED FLAPS TO 15 UNITS AND FLAPS OPERATED NORMALLY. FLIGHT LANDED WITHOUT FU RTHER INCIDENT. MAINTENANCE CHECKED FLAPS, TORQUE TUBES AND CABLES WITH NO DISCREPANCIES FOUND. OPERATED FLAPS SEVERAL TIMES. FLAPS OPERATED NORMAL. 2 L 7 2 4F RT A16WE 2007121700059 20071217 00059 NM 2007 12 17 SWAA076040 1 20071209 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 236WN 34631 R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007121700065 20071217 00065 NM 2007 12 17 SWAA076043 1 20071209 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 966, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700066 20071217 00066 NM 2007 12 17 SWAA076042 1 20071209 A 5753 65C30462 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED 22Y CHECK, FOUND LT WING OUTBOARD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007121700069 20071217 00069 NM 2007 12 17 SWAA076073 1 20071209 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505D, STR 14R. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2007121700077 20071217 00077 2007 12 17 SWAA076078 4 20071206 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007121700083 20071217 00083 NM 2007 12 17 SWAA076082 1 20071206 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700089 20071217 00089 NM 2007 12 17 SWAA076054 1 20071209 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700092 20071217 00092 NM 2007 12 17 SWAA076052 1 20071209 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700095 20071217 00095 NM 2007 12 17 SWAA076089 1 20071206 A 5312 6545409 PRESSURE PANEL BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED MV2 CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, LBL 33 TO LBL 36. REPAIRED PRESSURE WEB PER SW A EA. 2 L 7 2 4F RT A16WE 2007121700109 20071217 00109 NM 2007 12 17 SWAA076066 1 20071209 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 781WN 30601 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 133.15. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007121700112 20071217 00112 NM 2007 12 17 USAA920071295 1 20071203 A 5311 146N103028 FRAME BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 921UW 22201 PIT - MAJOR REPAIR - C3 CHECK, CRACKED FRAME CHORD, BS 1580, S26L - S27L. REPAIRED FRAME CHORD, BS 1580, S26L - S27L IA W USAIRWAYS EA 110324. 2 L 7 2 4F RT A2NM 2007121700113 20071217 00113 NM 2007 12 17 USAA920071296 1 20071120 A 5320 140N2002 FITTING BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 921UW 22201 PIT - MAJOR REPAIR - C3 CHECK, LEVEL 2 CORROSION ON AFT CARGO COMPARTMENT SKIN CLIP, BS 1460, S28R. REMOVED AND REPLACE D AFT CARGO COMPARTMENT SKIN CLIP, BS 1460, S28R IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007121700116 20071217 00116 NM 2007 12 17 USAA920071299 1 20071207 A 5753 6546435278 SKIN BOEING 737 7373S3 1384711 NM T/E FLAP DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 PHX - MAJOR REPAIR - NR 4306637 AND 4306638, RIGHT WING OUTBOARD AFT FLAP INBOARD CORNER LOWER SURFACE DISBONDED. REPLA CED RIGHT WING OUTBOARD AFT FLAP IAW TASK CARD R3M27304. 2 L 7 2 4F RT A16WE 2007121700123 20071217 00123 NM 2007 12 17 USAA920071306 1 20071208 A 5330 6545774 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 PHX - MAJOR REPAIR - WEEKLY - NR 4257110, CRACKED FUSELAGE SKIN, BS 727E, S23L. REPAIRED FUSELAGE SKIN, BS 727E, S23L I AW USAIRWAYS EA 120454. 2 L 7 2 4F RT A16WE 2007121700124 20071217 00124 NM 2007 12 17 USAA920071307 1 20071201 A 5753 6546435278 FLAP BOEING 737 7373G7 1384595 NM RT WING DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C16 CHECK - NR 6053647, RIGHT WING OUTBOARD AFT FLAP HAS AREA OF DISBOND, WBL 407.88 - WBL 409.38. REPAIRED RIGHT WING OUTBOARD AFT FLAP, WBL 407.88 - WBL 409.38 IAW B737 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 2007121700139 20071217 00139 SO 2007 12 17 RAIA00712005 1 20071206 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 839HK 14500829 POST FLT 7880 - ORD - EMERGENCY FLOOR STRIP LIGHT IS LOOSE. MAINTENANCE RESECURED EMERGENCY EXIT FLOOR STRIP, CHECK GOO D. 2 L 7 2 4F RT T00011AT 2007121700157 20071217 00157 NM 2007 12 17 SWAA076112 1 20071210 A 5311 6546554 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700160 20071217 00160 NM 2007 12 17 SWAA076109 1 20071210 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700169 20071217 00169 NM 2007 12 17 SWAA076141 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700174 20071217 00174 NM 2007 12 17 SWAA076135 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007121700176 20071217 00176 NM 2007 12 17 SWAA076133 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007121700177 20071217 00177 NM 2007 12 17 SWAA076132 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007121700178 20071217 00178 NM 2007 12 17 SWAA076131 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007121700180 20071217 00180 NM 2007 12 17 SWAA076129 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700198 20071217 00198 EU 2007 12 17 TRAX200701880 1 20071128 A 5720 CHANNEL AEROSP ATR72 ATR72 EU RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 CRACK FOUND ON ANCHOR NUT CHANNEL ON UPPER HANGER OF REAR SPAR OF RT WING JUST BESIDE THE INBOARD FITTING OF SPOILER. 2 H 7 2 4T RT 2007121800026 20071218 00026 EU 2007 12 18 07FDEA05032 1 20071211 A 5320 A5377364420100 FITTING AIRBUS 310 A310203 3930313 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FWD LOWER CARGO COMP, FR 37 RT FRAME TO CROSSBEAM CONNECTION FITTING CRACKED. REMOVED FITTING IAW A310-200 SRM 51-72-10 PG 2 PARA 5A LOCATED AND DRILLED NEW FITTING P/N 5377364420100 P.O. NO 598023.1 IAW A 310-200 SRM 51-72-10 PG 2 PARA 6A. INSTALLED NEW FITTING IAW A 310-200 SRM 51-40-30. 2 L 7 2 4F RT A35EU 2007121900004 20071219 00004 NM 2007 12 19 QXEA200701852 1 20071208 A 3240 BRAKE DHAV DHC8 DHC8202 2809007 NM MLG STIFF A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - BRAKE PEDALS ARE STIFF ON APPLICATION AND BRAKING ACTION NOT SMOOTH. MAINTENANCE COMPLIED WITH A HIGH SPEED TAXI AT ABOUT 40 KNOTS (WITH CREW). APPLIED BRAKES AND FOUND ACTION TO BE NORMAL WITH NO DEFECTS NOTED. AIRCRAFT RETURNED T O SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007121900007 20071219 00007 NM 2007 12 19 DHL2007763002 1 20071218 A 5730 6521657253 PANEL BOEING 727 727264 138408M NM NR 1 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 7 BY 5 INCH AREA OF DELAMINATION ON PANEL JUST O/B OF NR 1 SPOILER. DELAMINATION LOCATED JUST ABOVE JACKSCREW GEAR BOX, PANEL NR 8155. 2 L 7 3 4F A3WE 2007121900012 20071219 00012 NM 2007 12 19 2007UALA05049 1 20071210 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 727B S20L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 50961 24640 BS 727B STRINGER CLIP AT S20L CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED AND REPLACED STRINGER CLIP. AC OK FOR SERVIC E. 2 L 7 2 4F 4 F RT A16WE E2GL 2007121900014 20071219 00014 EU 2007 12 19 2007UALA05051 1 20071210 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 416UA 479 AFT LEFT DOOR FAILED EMERGENCY LIGHT TEST. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121900018 20071219 00018 NM 2007 12 19 2007UALA04998 1 20071207 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 FOUND DOOR 1L AFT SILL EMERGENCY LIGHT IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121900019 20071219 00019 NM 2007 12 19 2007UALA05005 1 20071205 A 5532 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE VERTICAL STAB DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 791UA 26933 RIGHT SIDE OF THE VERTICAL STABILIZER IS DELAMINATED. BLISTER ON VERTICAL FIN BETWEEN STATIC PORTS RT PANEL REMOVED F OR REPAIR. SENT TO SHOP 273. R&R R30639. REINSTALLED PANEL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121900020 20071219 00020 2007 12 19 2007UALA05006 4 20071206 A 2565 DISC AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE L1 SLIDE BOTTLE RUPTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 832UA 1321 L1 DOOR SLIDE HAS A LOW BOTTLE. FOUND RUPTURE DISC LEAKING. REPLACED RUPTURE DISC, SERVICED SYSTEM TO PROPER OPERATI NG LEVEL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121900021 20071219 00021 EU 2007 12 19 2007UALA05007 1 20071210 A 5512 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HORIZONTAL STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 464UA 1290 DENT IN LT FWD STAB TIP. SAMC TEXT: FOUND DENT AND SCRATCHES ON LT HORIZ STAB TO BE 8" WIDE BY 4" LONG BY 1-2" DEEP. TH ERE APPEARS TO BE A SMALL CRACK AT THE INBD END OF DENT, WHERE DENT MEETS SCAB PATCH. DUE TO UNKNOWN DAMAGE. REPLACED THE LT STAB TIP WITH NEW ASSY AND SEALED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121900022 20071219 00022 EU 2007 12 19 2007UALA05008 1 20071209 A 7540 SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 BLEED TEMP FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 405UA 452 V10484 RTFL DUE TO NR 2 ENGINE AIR BLEED FAULT. FOUND RT HEAT EXCHANGER OUTLET TEMP SENSOR FAULTY. REPLACED THE RT HEAT EXCH ANGER OUTLET TEMP SENSOR AND REPLACE NR 2 FAN AIR VALVE CONTROL THERMOSTAT DUE TO NR 2 BLEED AIR OVERHEAT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121900023 20071219 00023 EU 2007 12 19 TRBA2007111 1 20071212 A 3246 WHEEL AEROSP ATR72 ATR72212A 8680902 EU NR 2 DAMAGED A TRBA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 545AT 545 LT LANDING GEAR, NR 2 TIRE ASSEMBLY POSSIBLE BEARING DAMAGES. REPLACED LT MAIN LANDING GEAR SWINGING LEVEL AS PER JIC 3 2-11-00. FUNCTIONAL CHECK GOOD. 2 H 7 2 4T RT A53EU 2007121900028 20071219 00028 NM 2007 12 19 2007UALA05020 1 20071209 A 3350 9F19948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 WALL EEL INOP DOOR 5R AFT CROSS AISLE. REPLACED LIGHT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121900030 20071219 00030 NM 2007 12 19 KNNA200700068 1 20071210 A 5522 SKIN BOEING 737 737232 1384475 NM PWA JT8 JT8D15 52051 NE LT ELEVATOR DAMAGED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 326DL 23098 WHILE PERFORMING AN A-7 CHECK, A LIGHTNING STRIKE WAS FOUND ON THE LT ELEVATOR AT THE OUTBOARD TRAILING EDGE LOWER SIDE, UNDER I/B STATIC WICK, SPECIAL INSPECTION WAS PERFORMED IAW SKY KING GMM SECTION 4.03 AND AMM 05-51-151-201 WITH NO OTH ER DAMAGE NOTED. ELEVATOR WAS REPAIRED IAW SRM51-40-12, REPAIR 14, DAMAGED AREA WAS APPROX 3/16 OF AN INCH. 2 L 7 2 4F 4 F RT A16WE E2EA 2007121900031 20071219 00031 EU 2007 12 19 1214834612170 1 20070929 A 7120 S5421020001000 MOUNT AEROSP ATR42 ATR42320 8680930 EU NR 2 ENGINE CHAFED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 14834 193 NR 2 ENGINE "Z" MOUNT TUBE 7 CHAFED. REPAIRED BY BLENDING AND FOUND TO BE WITHIN LIMITS PER ATR SRI DO/TS-3777/07-9189. 2 H 7 2 4T RT A53EU 2007121900034 20071219 00034 NM 2007 12 19 AALA20072422 1 20071211 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 668AA 25333 MIA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 13D MISSING LENS. REPLACED LENS FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 13D . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007121900035 20071219 00035 WP 2007 12 19 AALA20072431 1 20071213 A 3350 LENS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9617R 53564 DFW - EMERGENCY LIGHT AT SEAT ROW 8 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 8. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007121900036 20071219 00036 WP 2007 12 19 AALA20072432 1 20071213 A 3350 SHROUD DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9617R 53564 DFW - EMERGENCY LIGHT AT SEAT ROW 30 MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 30. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007121900037 20071219 00037 WP 2007 12 19 AALA20072433 1 20071213 A 3350 SHROUD DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9617R 53564 DFW - EMERGENCY LIGHT AT SEAT ROW 31 MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 31. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007121900038 20071219 00038 WP 2007 12 19 AALA20072434 1 20071213 A 3350 SHROUD DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9617R 53564 DFW - EMERGENCY LIGHT AT SEAT ROW 32 MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 32. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007121900039 20071219 00039 NM 2007 12 19 AALA20072442 1 20071213 A 3260 FRF0327S03 SENSOR BOEING 757 757223 1384957 NM NLG INOPERATIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 182AN 29592 MIA INFLIGHT T973/13DEC - RECEIVED NOSE LANDING GEAR AIR GROUND SWITCH DISAGREE MESSAGE. RETURNED TO MIA AND LANDED WIT HOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. REPLACING SENSOR. 2 L 7 2 4F RT A2NM 2007121900040 20071219 00040 WP 2007 12 19 AALA20072424 1 20071212 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISLODGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 494AA 49732 LAS - OVERHEAD EMERGENCY LIGHT AT SEAT ROW 20 INOPERATIVE. SECURED BATTERIES IN BATTERY PACK FOR OVERHEAD EMERGENCY LIG HT AT SEAT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121900041 20071219 00041 WP 2007 12 19 AALA20072425 1 20071212 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISLODGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 494AA 49732 LGA - OVERHEAD EMERGENCY LIGHT AT SEAT ROW 29 INOPERATIVE. SECURED BATTERIES IN BATTERY PACK FOR OVERHEAD EMERGENCY LIG HT AT SEAT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121900042 20071219 00042 NM 2007 12 19 AALA20072417 1 20071211 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT SEAT 31C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 31C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121900043 20071219 00043 WP 2007 12 19 AALA20072414 1 20071211 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 451AA 49477 LGA - EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS CABI N. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121900044 20071219 00044 NM 2007 12 19 AALA20072415 1 20071211 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT SEAT 24C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHTS AT SEAT 24C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121900047 20071219 00047 SO 2007 12 19 2007F00068 2 20071211 A 7414 10682016 GEAR D6LN3000 PIPER PA32 PA32R300 7103213 SO LYC 0540 IO540K1G5D 41532 SO HARTZL HCC2Y HCC2YK1 GL MAGNETO FAILED G D RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 AL 05 8493C 650 G06KA103 32R7680118 L1075148A CH39289B PILOT REPORTED PARTIAL POWER/ROUGH-RUNNING ENGINE PRIOR TO TAKEOFF, RETURNED TO MAINTENANCE HANGAR. MAINTENANCE PERSONN EL REMOVED D6LN-3000 DUAL MAGNETO AND DISCOVERED SEVERAL DOZEN TEETH MISSING BOTH DISTRIBUTOR GEARS. MAGNETO INSTALLED NEW ON 28 MAY, 2007. 1 L 7 1 3O 3 O A3SO 1E4 5 C P920 2007121900048 20071219 00048 EU 2007 12 19 2007UALA05052 1 20071210 A 3350 MR33131 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 426UA 510 EMERGENCY EXIT LIGHTS AT SEATS ON LEFT SIDE NEXT TO THE OVERWING EMERGENCY DOORS FAIL TO TEST. FOUND EPSU FAILED. REPL ACED EPSU ON LT SIDE. OPS CHECKED GOOD, NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121900049 20071219 00049 NM 2007 12 19 DHLA200700085 1 20071217 A 5210 LATCH BOEING 727 7272M7 138407S NM PAX DOOR LACK OF LUBE A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 750DH 21951 FWD ENTRY DOOR WILL NOT LOCK IN OPEN POSITION. CLEANED AND LUBED FWD ENTRY DOOR LATCH ASSY. OPS CHECK NORMAL IAW AMM 5 2-11-01. 2 L 7 3 4F A3WE 2007121900050 20071219 00050 WP 2007 12 19 IXXA07SMN260S 1 20071115 A 5340 3355841U501 FITTING DOUG DC8 DC873F 302199F WP BS 1180 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND AFT BELLY PIT INTERNAL STRUCTURE FITTING UNDER CROSS SLIDE DOOR CRACKED AT STAT ION 1180.000 AROUND LONGERON-33 RIGHT. REMOVED CRACKED INTERNAL STRUCTURE FITTING. INSTALLED NEW FITTING IAW DC8 SRM 5 1-1-20D, AND 51-3-1. 2 L 7 4 4F RT 4A25 2007121900051 20071219 00051 WP 2007 12 19 IXXA070064S 1 20071115 A 5340 3355841U501 FITTING DOUG DC8 DC873F 302199F WP BS 1180 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND AFT BELLY PIT INTERNAL STRUCTURE FITTING UNDER CROSS SLIDE DOOR CRACKED AT STAT ION 1180.000 AROUND LONGERON-34 RIGHT. REMOVED CRACKED INTERNAL STRUCTURE FITTING. INSTALLED NEW FITTING IAW DC8 SRM 5 1-1-20D, AND 51-3-1. 2 L 7 4 4F RT 4A25 2007121900054 20071219 00054 NM 2007 12 19 NWAA074076307 1 20071120 A 5320 ANGLE BOEING 747 747451 1384940 NM BS 480 S10R CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 667US 24222 DURING "M" CHECK WHILE ACCOMPLISHING SB 747-53A2484, FOUND CRACK IN ANGLE AT BS 480 S10R. REPAIRED PER EA 63-211354. 2 L 7 4 4F RT A20WE 2007121900056 20071219 00056 NM 2007 12 19 NWAA074096307 1 20071204 A 5322 SHEAR WEB BOEING 747 747451 1384940 NM BS 1120 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 667US 24222 DURING "M" CHECK, FOUND CRACK IN TENSION TIE AREA GUSSET AND SHEAR WEB AT BS 1120. REPAIRED PER EA 63-211013. 2 L 7 4 4F RT A20WE 2007121900057 20071219 00057 NE 2007 12 19 NACA20070022 2 20071214 A 8560 GEAR PWA CB3 DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE ENGINE BLOWER STRIPPED A NACA C ABORTED TAKEOFF Y J ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 AL 03 2907F 1342 1342 31026 533265 31026 NR 2 ENGINE SHUT DOWN, QUIT ON TAKEOFF. BLOWER GEARS STRIPPED. REPLACED NR 2 ENGINE. 2 L 7 4 4R 4 R A781 5E8 2007121900058 20071219 00058 EU 2007 12 19 TRBA2007112 1 20071214 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS FAILED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 440AM 440 EMERGENCY LIGHTS STAYS STAY ON WHEN THE SWITCH IS ON THE ARM POSITION. REMOVED AND REPLACED THE EMERGENCY LIGHT POWER S UPPLY AT 73WL, THE EMERGENCY BATTERY LIGHT PACK AT 62WL, OPS CHECK NORMAL IAW MM 33-51-00. OPS CHECKS NORMAL AS PER MM 25-60-00. 2 H 7 2 4T RT A53EU 2007121900059 20071219 00059 NM 2007 12 19 2007UALA05053 1 20071211 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY LIGHT ALONG UPPER DECK WALL ACROSS ROW 18 INOP. RELAMPED WALL UNIT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121900062 20071219 00062 NM 2007 12 19 2007UALA05057 1 20071211 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 CABIN 'B' ZONE LT SIDE EEL'S AND 'D' ZONE RT SIDE EEL'S DO NOT STAY ON REQUIRED LENGTH OF TIME. REPLACED BATTERY PACKS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121900063 20071219 00063 NM 2007 12 19 2007UALA05058 1 20071211 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 516UA 24860 FOUND FWD EEL LAMP AT FWD CLOSET INOP. REPLACED LAMP ASSY, OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121900064 20071219 00064 NM 2007 12 19 2007UALA05059 1 20071210 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 670UA 29240 FOUND 6B EEL LIGHT MISSING ON SIDE PANEL. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121900065 20071219 00065 NM 2007 12 19 2007UALA05060 1 20071210 A 3260 INDICATOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE RT MLG INOPERATIVE A UALA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 WP 29 670UA 29240 RT MLG INDICATION LIGHT INOPERATIVE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121900066 20071219 00066 WP 2007 12 19 IXXA07SMN270S 1 20071116 A 5542 SKIN DOUG DC8 DC873F 302199F WP RUDDER MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT RUDDER RIGHT SKIN AT STATION ZR 253.000 TO STATION ZR 271.00 0. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, INTERNAL, AND EXTERNA L DOUBLER, BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. PERFORMED BALANCE TO RUDDER FOUND MOMENT WITHIN TOLERANCE. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, 51-1-21, DC8 SRM 51 -4-6 PAGES 1-6, IAW DC8 SRM 55-6-1 FIGURE 1, DC8 SRM 55-1-0 PAGE 1 AND SRM 51-1-21, DC8 SRM 55-6-1 FIGURE 1, ITEM "A", D C8 SRM 51-1-9, T/R NUMBER 51-142 DATED 04-05-06, SRM 51-1-9A T/R 51-141 DATED 04-03-06, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007121900069 20071219 00069 NM 2007 12 19 2007UALA05028 1 20071208 A 5210 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 FOUND DOOR 2R UPPER HINGE ARM CUTOUT HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121900070 20071219 00070 EA 2007 12 19 REXA200700065 1 20071211 A 3350 MS277891A SWITCH CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS MALFUNCTIONED A REXA K NONE L NO TEST IN INSP/MAINT 1 SO 25 825AY 8025 EMERGENCY LIGHTS WOULD NOT SHUTOFF ON ONE LOCATION. ANOTHER TIME EMERGENCY LIGHTS WOULD NOT TURN ON. 2 L 7 2 4F RT A21EA 2007121900072 20071219 00072 EU 2007 12 19 TRAX200701898 1 20071210 A 5280 BRACKET AEROSP ATR72 ATR72212 8680945 EU NLG DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 NLG FWD LT DOOR, FWD STOP BRACKET CRACKED. 2 H 7 2 4T RT A53EU 2007121900073 20071219 00073 NM 2007 12 19 2007UALA05061 1 20071211 A 2120 UNKNOWN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN SMOKE A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 913UA 25291 LIGHT SMOKE IN THE CABIN WITH PACKS ON. 2 L 7 2 4F 4 F RT A16WE E2GL 2007121900075 20071219 00075 NM 2007 12 19 2007UALA05063 1 20071212 A 2150 A/C PACK BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RIGHT LEAKING A UALA O OTHER O OTHER AP APPROACH 1 WP 29 675UA 29243 LOUD AIR LEAK RIGHT PACK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121900076 20071219 00076 NM 2007 12 19 2007UALA05064 1 20071211 A 5340 131W18372402 BRACKET BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE R2 DOOR GIRT BAR MISINSTALLED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 781UA 26945 IMPROPERLY INSTALLED GIRT BAR RESULTING IN SLIDE DEPLOYMENT WHEN SLIDE LEVER IN DISARMED POSITION. FWD FLAG BRACKET BRO KEN. REPLACED FLAG BRACKET SLIDE AND BOTTLE. GIRT BAR ENGAGES NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121900077 20071219 00077 NM 2007 12 19 2007UALA05065 1 20071212 A 2560 GIRT BAR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE R1 DOOR MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 797UA 26924 1R DOOR SLIDE-RAFT GIRT BAR IN INSTALLED INCORRECTLY. GIRT BAR IS INSTALLED INCORRECTLY. INSTALLED GIRT BAR AND SLIDE. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121900081 20071219 00081 EU 2007 12 19 1218341121707 1 20070918 A 5210 S5367139028602 STRUCTURE AEROSP ATR42 ATR42320 8680930 EU SERVICE DOOR CRACKED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 14834 193 LOWER FORWARD CORNER OF SURROUND STRUCTURE ON RIGHT SERVICE DOOR CRACKED. REMOVED AND REPLACED STRUCTURE IN ACCORDANCE WITH SRM 51-25-01. 2 H 7 2 4T RT A53EU 2007121900085 20071219 00085 EU 2007 12 19 SIMA200734804 1 20071212 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 236AE 340B236 CREW REPORTED DURING PRE FLIGHT SEVERAL FLOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED AFT EMERGENCY BATTERY POWER S UPPLY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007121900088 20071219 00088 EA 2007 12 19 TRAX200701892 1 20071205 A 5510 FITTING CNDAIR CL600 CL6002B19 1900309 EA CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 HORIZ TAB ANTI ROTATION FITTING CORRODED. 2 L 7 2 4F RT A21EA 2007121900089 20071219 00089 EA 2007 12 19 TRAX200701893 1 20071209 A 2130 CABIN PRESSURE CNDAIR CL600 CL6002B19 1900309 EA FAILED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 874AS 7551 CREW REPORTS LOSS OF PRESSURIZATION AT 20000 FT. ALL MASK DEPLOYED. A/C RETURNED TO ATL AFTER T/O, EMERGENCY DECLARED. EMERGENCY EQUIPMENT ON STANDBY, FLT 4368 DEL 132 MINS. 2 L 7 2 4F RT A21EA 2007121900090 20071219 00090 NM 2007 12 19 GTIA200700033 1 20071202 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSLEAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 520NK 2784 FLOORBEAM AT APPROX Y+400 SHOWS SIGNS OF CORROSION AT FRAME 68. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2007121900091 20071219 00091 NM 2007 12 19 12170701 1 20071212 A 2150 8021709 SHUTOFF VALVE BOEING 767 76723B 1385112 NM RT PACK FAULTY A L43A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 260MY 23973 AFTER TAKEOFF FROM STN WITH THE RT PACK DEFERRED PER THE MEL, A LEFT HPSOV EICAS MSG WITH ASSOCIATED LIGHT ILLUMINATED. THE CREW FOLLOWED THE QRH PROCEDURE FOR INOPERATIVE BLEED AND RETURNED TO STN DUE TO RT PACK DEFERRAL AND LT HPSOV EICA S MESSAGE. THE AIRCRAFT MADE AN UNEVENTFUL OVERWEIGHT LANDING AND AN OVERWEIGHT LANDING INSPECTION WAS CARRIED OUT WITH NO FINDINGS. THE HPSOV WAS FAULTED, REMOVED AND REPLACED AND OPS CHECKED NORMAL. 2 L 7 2 4F RT A1NM 2007121900095 20071219 00095 EU 2007 12 19 TRAX200701831 1 20071129 A 5420 ANGLE AEROSP ATR72 ATR72212 8680945 EU FIREWALL CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 ANGLE CRACKED UPPER PORT FIREWALL, RESOLVED ON W/O: 75891 TASKCARD: N/R-00584. ANGLE AT UPPER PART OF FIREWALL ON O/B S IDE OF RT ENGINE FABRICATED AS PER SRM 51-24-01 ANGLE AT UPPER PART OF FIREWALL ON O/B SIDE OF RT ENGINE REPLACED AS PER SRM 51-25-02. 2 H 7 2 4T RT A53EU 2007121900096 20071219 00096 NM 2007 12 19 AALA20072426 1 20071212 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 347AN 33086 SFO - EXTERNAL EMERGENCY LIGHT AT AFT LEFT WING INOPERATIVE. REPLACED LAMPS FOR EXTERNAL EMERGENCY LIGHT AT AFT LEFT WI NG. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007121900098 20071219 00098 WP 2007 12 19 AALA20072429 1 20071213 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 448AA 49474 LGA - EMERGENCY LIGHT AT AFT OVERWING EXIT LOWER SIDE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT OVE RWING EXIT LOWER SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121900101 20071219 00101 NM 2007 12 19 AALA20072419 1 20071211 A 3520 MASK BOEING 737 737823 13844BZ NM CABIN UNWANTED DEPLOY A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 964AN 30093 DFW - FOUND CABIN OXYGEN MASKS DEPLOYED WHEN AIRCRAFT WAS PARKED. REPACKED AND STOWED CABIN OXYGEN MASKS. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2007121900102 20071219 00102 WP 2007 12 19 AALA20072420 1 20071211 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 482AA 49675 LGA - EMERGENCY LIGHTS AT SEAT ROWS 29 TO 30 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 29 TO 30. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121900104 20071219 00104 EA 2007 12 19 TRAX200701888 1 20071208 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 722EV 10127 FOUND EXIT LIGHT AT 1 A + B IS OUT. 2 L 7 2 4F RT A21EA 2007121900105 20071219 00105 EU 2007 12 19 1218345121707 1 20070928 A 7120 S5421020001000 MOUNT AEROSP ATR42 ATR42320 8680930 EU NR 2 ENGINE CHAFED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 14834 193 NR 2 ENGINE AFT "Z" MOUNT TUB NR 2 CHAFED. CHAFE REPAIRED BY BLENDING OUT IN ACCORDANCE WITH ATR SRT DO/TS-3777/07-918 9 SRAS 4238. BLEND OUT WITHIN LIMITS. 2 H 7 2 4T RT A53EU 2007121900106 20071219 00106 WP 2007 12 19 07FDEA05042 1 20071212 A 3234 ROD END DOUG MD10 MD1010F 3022112 WP MLG HANDLE LOOSE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 375FE 46613 AFTER ROTATION GEAR HANDLE DID NOT MOVE TO UP POSITION COMPLIED WITH QRH. GEAR HANDLE DID MOVE UP WITH HANDLE RELEASE BUTTON PUSHED. LANDED AT KLCK, FOUND ROD END AS DESCRIBED IN AMM 32-24-01-2 FIGURE 201 SHEET 1 AS ITEM "G" TO HAVE LOWE R END DISCONNECTED FROM THE LINKAGE IT IS NORMALLY ATTACHED. ALL ATTACH HARDWARE WAS MISSING. FOLLOWING AMM 32-24-01-2 INSPECTED AND REATTACHED ROD END WITH NEW HARDWARE DESCRIBED IN THE ORIGINAL WRITE UP. INSPECTED THE GROUND SENSE MECH ANISM AND SURROUNDING AREA PER THE DESCRIPTIONS IN AMM 32-24-01-2. ALL CHECKS NORMAL. 2 L 7 3 4F RT A22WE 2007121900107 20071219 00107 WP 2007 12 19 07FDEA05043 1 20071212 A 5246 ARB1101508 DOOR DOUG MD10 MD1010F 3022112 WP RT WING SEPARATED A FDEA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 SO 25 367FE 46605 POST FLIGHT WALK AROUND, DISCOVERED RT WING FUEL DOOR MISSING FROM A/C. INSTALLED RT WING REFUELING ACCESS PANEL DOOR I AW SMP. OPS CHECKS NORMAL. OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2007121900109 20071219 00109 NM 2007 12 19 07FDEA05045 1 20071213 A 5347 6519601508 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 MAIN DECK FLOOR SEAT TRACK IS CRACKED/CORRODED, BS 950-950A, RBL 45, WL 208 REMOVED CORRODED SEAT TRACK FROM STA 870 T O 950, 9". FABRICATED NEW SECTION REF BAC DWG 65-19601. TREATED AND PRIMED NEW SECTION. INSTALLED NEW SEAT TRACK. T HIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007121900110 20071219 00110 WP 2007 12 19 07FDEA05047 1 20071213 A 5320 AJC7013 WEB DOUG DC10 DC1030F 3023504 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 308FE 48297 LOWER AFT FUSELAGE COMPT CRACK ON WEB, UPPER TORQUE BOX PLANE. REPAIRED WEB IAW SRM 51-40-00 FIG 41 VOL I. 2 L 7 3 4F RT A22WE 2007121900112 20071219 00112 WP 2007 12 19 07FDEA05049 1 20071213 A 5320 AGA7081509 FLOOR SUPPORT DOUG DC10 DC1030F 3023504 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 308FE 48297 AFTER REMOVAL CEILING PANELS WITH J/C "2552C180-3JR" AFT CARGO COMPT BELOW CHANNEL SUPPORT FLOOR FOUND SEVERE EXFOLIAT ION CORROSION. REPAIRED AREA IAW SRM 53-70-00 VOL I FIG 13. 2 L 7 3 4F RT A22WE 2007121900113 20071219 00113 EU 2007 12 19 AALA20072435 1 20071213 A 3350 82400 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14056 463 JFK - EMERGENCY EXIT SIGN LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SIGN LIGHT AT R IGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121900114 20071219 00114 NM 2007 12 19 2007UALA05035 1 20071207 A 2560 TRACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE DOOR 2L DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 FOUND DOOR 2L WON'T ARM. FOUND TRACK DIRTY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121900116 20071219 00116 NM 2007 12 19 2007UALA05037 1 20071208 A 3350 5661373 LENS BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 216UA 30549 FOUND EMERGENCY EXIT PATH LIGHT BROKEN AT ROW 37G. REPLACED BROKEN LENS 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121900117 20071219 00117 NM 2007 12 19 2007UALA05038 1 20071207 A 3350 SIGN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 792UA 26934 FOUND EMERGENCY EXIT SIGN ABOVE DOOR 4L IS LOOSE. SECURED SIGN. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121900119 20071219 00119 NM 2007 12 19 2007UALA05040 1 20071209 A 2721 INDICATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RUDDER TRIM MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 CREW REPORT RUDDER TRIM INDICATOR IS HESITANT WHEN TRIM SELECTED PRIOR TO DEPARTURE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121900120 20071219 00120 EU 2007 12 19 TRBA2007113 1 20071216 A 3350 3011210 LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS FAILED A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 369AT 369 PASSENGER STAIR EMERGENCY FLOOD LIGHT IS INOP. REMOVED AND INSTALLED ENTRANCE DOOR EMERGENCY LIGHT AS PER MM 33-51-00. 2 H 7 2 4T RT A53EU 2007121900121 20071219 00121 NM 2007 12 19 ANCF200700031 1 20071210 A 2497 CONNECTOR BOEING 757 757236 1384971 NM GENERATOR DAMAGED W ANCF A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 23 506NA 24771 AFTER TAKEOFF, GEN OFF EICAS MESSAGE WAS PRESENTED. ALSO LEFT BUSS ISOLATED MESSAGE WAS PRESENTED AND SEVERAL CAPTAIN I NSTRUMENTS WERE LOST. THERE WAS NOT FLIGHT INSTRUMENT TRANSFER AND THE AUTOPILOT AUTOMATICALLY DISCONNECTED. GEN OFF C HECK LIST WAS ACCOMPLISHED WAS PERFORMED AND GENERATOR WAS RECOVERED, HOWEVER, L BUS ISOLATED WAS STILL PRESENTED. IAW SWPM 20-61-19 CONNECTOR D1116P WAS REPLACED IN LEFT ENGINE GENERATOR SYSTEM THIS ITEM IS DEFERRED TO DMI-628 MEL 24-00-1 CAT B IAW SWM 20-61-19 CONNECTOR D116P WAS REPLACED LT ENG GEN SYSTEM IAW AMM 24-11-01 PAGE 401. THE IDG WAS REPLACED , THE CABLES IDG FROM D116P WERE REPLACED IAW WDM24-21-14 P/N ON AND OFF LJ34975. 2 L 7 2 4F RT A2NM 2007121900122 20071219 00122 EU 2007 12 19 AALA20072436 1 20071213 A 3350 82400 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14056 463 JFK - EMERGENCY EXIT SIGN LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SIGN LIGHT AT RI GHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121900123 20071219 00123 2007 12 19 AALA20072441 4 20071213 A 2250 ACTUATOR AIRBUS 300 A300B4605R 3930308 EU YAW DAMPER INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 18066 509 MIA INFLIGHT T377/13DEC - NUMBER ONE YAW DAMPER PADDLE TRIPPED ON TAKEOFF. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED AUTO PILOT YAW ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121900125 20071219 00125 EU 2007 12 19 AALA20072438 1 20071213 A 3350 82400 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14056 463 JFK - EMERGENCY EXIT SIGN LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SIGN LIGHT AT LEF T NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121900126 20071219 00126 NM 2007 12 19 AALA20072428 1 20071213 A 3397 WIRE BOEING 767 767323 1385205 NM EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 359AA 24040 JFK - EMERGENCY LIGHT AT SEAT 40H INOPERATIVE. RECONNECTED WIRE UNDER SEAT FOR EMERGENCY LIGHT AT SEAT 40H. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2007121900128 20071219 00128 WP 2007 12 19 07FDEA05050 1 20071213 A 5347 ADA7321503 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 308FE 48297 AFTER REMOVAL CEILING PANELS WITH J/C "2552C120-2JR" FWD CARGO COMPT BELOW SEAT TRACK FOUND CRACK. REPAIRED SEAT TRACK I AW SRM 53-70-01 FIG 1 VOL I. 2 L 7 3 4F RT A22WE 2007121900129 20071219 00129 EU 2007 12 19 AALA20072439 1 20071213 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14056 463 JFK - SEAT MOUNTED EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENC Y LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121900130 20071219 00130 NM 2007 12 19 2007UALA05032 1 20071207 A 3510 OXYGEN SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 CREW OXYGEN LOW. SERVICED CREW O2- NO NOTED LEAKS PRESENT AT THIS TIME. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121900131 20071219 00131 NM 2007 12 19 2007UALA05033 1 20071207 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 LT GRND ILLUM EMERGENCY LIGHT INOPERATIVE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121900132 20071219 00132 NM 2007 12 19 2007UALA05034 1 20071207 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 FOUND ROW 25 RT CEILING EMERGENCY LIGHT INOPERATIVE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121900134 20071219 00134 WP 2007 12 19 07FDEA05052 1 20071213 A 5315 601068718 FLOORBEAM DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 563FE 46948 AFT CARGO COMPARTMENT FLOORBEAM AND FLOOR SUPPORT ARE EXFOILIATED ARROUND NUMEROUS NUTPLATES ON UPPER CHORDS ALONG ENTIR E LENGTH AT F/S 1841 BLENDED WORN AREAS IAW SRM 51-21-01 CHECKED LIMITS ORIGINAL MAT. .094 AFTER REWORK .078 WITHIN LIMI TS ON FLOORBEAM, ON FLOOR SUPPORT ORIG MAT. .063 AFTER REWORK .054 WITHIN LIMITS IAW SRM 53-00-01 FIG 1A. FOUND SECTION OF FLOORBEAM BETWEEN LBL 12 TO RBL 50 OUT OF LIMITS SPLICED NEW SECTION OF FLOORBEAM IAW SRM 53-00-01 FIG 9 VOL 1. 2 L 7 3 4F RT A22WE 2007121900135 20071219 00135 WP 2007 12 19 07FDEA05053 1 20071213 A 5315 601068718 FLOORBEAM DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 563FE 46948 AFT CARGO COMPARTMENT FLOORBEAM AND FLOOR SUPPORT ARE EXFOILIATED AROUND NUMERIOUS NUTPLATES ON UPPER CHORDS ALONG ENTIR E LENGTH AT F/S 1841 BLENDED WORN AREAS IAW SRM 51-21-01 CHECKED LIMITS ORIGINAL MAT. .094 AFTER REWORK .078 WITHIN LIMI TS ON FLOORBEAM, ON FLOOR SUPPORT ORIG MAT .063 AFTER REWORK .054 WITHIN LIMITS IAW SRM 53-00-01 FIG 1A. FOUND SECTION OF FLOORBEAM BETWEEN LBL 12 TO RBL 50 OUT OF LIMITS SPLICED NEW SECTION OF FLOORBEAM IAW SRM 53-00-01 FIG 9 VOL 1. 2 L 7 3 4F RT A22WE 2007121900136 20071219 00136 WP 2007 12 19 07FDEA05054 1 20071213 A 5347 SEAT TRACK DOUG MD10 MD1010F 3022112 WP BS 1957 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 563FE 46948 AFT CARGO COMPT SEAT TRACK F/S 1957 RBL 20 IS EXFOLIATED ON LWR SURFACE. BLENDED SEAT TRACK CORROSION AT STA 1957 RBL 20 AND FOUND TO BE OUT OF LIMITS, IAW SRM 53-70-00 FIG 5. REMOVED SECTION OF SEAT TRACK IAW SRM 51-31-01 AND SRM 53-70-00 FIG 1. FAB SEAT TRACK IAW SRM 53-70-00 FIG 1 FROM 60-11393/18 BATCH NR 826186, SPLICE CAP FROM 60-71581 BATCH 1336047 AND INSTALLED SEAT TRACK IAW SRM 53-70-00 FIG 1 AND SRM 51-31-01. 2 L 7 3 4F RT A22WE 2007121700010 20071217 00010 NM 2007 12 17 USAA920071267 1 20071205 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR-C-18-NR I1C53034/6, FRAME 727E CRACKED AT RIVET FOR BIN RAIL ATTACHMENT. REPAIRED IAW EA100048, TR53 -10-20E. 2 L 7 2 4F RT A16WE 2007121700013 20071217 00013 NM 2007 12 17 USAA920071270 1 20071203 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR-C-18-NR I1D25012/15, CORROSION ON FLOORBEAM T-CAP AT BS 328, RBL 18. REPAIRED IAW SRM 53-10-51 FIG 1 01. 2 L 7 2 4F RT A16WE 2007121700025 20071217 00025 NM 2007 12 17 USAA920071282 1 20071205 A 5320 69770651 FITTING BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR- C-18 -NR I1D25012/10, CORROSION ON FLOOR FITTING MOUNT AT BS 303, LBL 12. REPAIRED IAW SRM 53-10-51 -A, SRM 51-10-02. 2 L 7 2 4F RT A16WE 2007121700057 20071217 00057 2007 12 17 SWAA076067 4 20071207 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 200WN 32482 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007121700071 20071217 00071 NM 2007 12 17 SWAA076045 1 20071209 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 442WN 32459 EEPLS PHOTOLUMINESCENT STRIP MISSING AT ROW 10 DEF. INSTALLED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007121700078 20071217 00078 NM 2007 12 17 SWAA076079 1 20071206 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 751 AND BS 781, STR 18L AND STR 19L. REPAIRED SKIN PE R SRM. 2 L 7 2 4F RT A16WE 2007121700080 20071217 00080 NM 2007 12 17 SWAA076080 1 20071209 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700085 20071217 00085 NM 2007 12 17 SWAA076085 1 20071209 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700093 20071217 00093 NM 2007 12 17 SWAA076053 1 20071209 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007121700103 20071217 00103 NM 2007 12 17 SWAA076058 1 20071207 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 716SW 27850 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138.7. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007121700106 20071217 00106 NM 2007 12 17 SWAA076061 1 20071207 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 716SW 27850 DURING SCHEDULED HC1 CHECK, RT OVERWING EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK S PER MM. 2 L 7 2 4F RT A16WE 2007121700108 20071217 00108 NM 2007 12 17 SWAA076063 1 20071209 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 781WN 30601 DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK S PER MM. 2 L 7 2 4F RT A16WE 2007121700122 20071217 00122 NM 2007 12 17 USAA920071305 1 20071205 A 5755 654645170A PANEL BOEING 737 7374B7 1384702 NM NR 3 SPOILER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 459UW 25023 CLT - MAJOR REPAIR - C6 CHECK, LEFT WING NR 3 SPOILER PANEL AREA OF DELAMINATION. REPLACED LEFT WING NR 3 SPOILER PANEL IAW B737 AMM 27-61-11. 2 L 7 2 4F RT A16WE 2007121700143 20071217 00143 NM 2007 12 17 SWAA076095 1 20071210 A 3397 W4142001220 WIRE BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 225WN 34333 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 3 ABC. FOUND BROKEN WIRE. REPAIRED WIRE PER MM. 2 L 7 2 4F RT A16WE 2007121700148 20071217 00148 NM 2007 12 17 SWAA076123 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700156 20071217 00156 NM 2007 12 17 SWAA076113 1 20071210 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700170 20071217 00170 NM 2007 12 17 SWAA076140 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700171 20071217 00171 NM 2007 12 17 SWAA076139 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700172 20071217 00172 NM 2007 12 17 SWAA076138 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700189 20071217 00189 NM 2007 12 17 SWAA076100 1 20071210 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700200 20071217 00200 EU 2007 12 17 TRAX200701882 1 20071128 A 5220 BRACKET AEROSP ATR72 ATR72 EU EMERGENCY EXIT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 LEFT EMERGENCY DOOR BONDING BRACKET CRACKED. 2 H 7 2 4T RT 2007121800014 20071218 00014 WP 2007 12 18 07FDEA05015 1 20071207 A 5310 ACA72261 DOOR FRAME DOUG MD10 MD1010F 3022112 WP MAIN CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 MAIN CARGO DOOR LOWER JAMB TOP SURFACE MOST AFT PART OF JAMB AT STA 766 HAS SURFACE CORROSION. REMOVED CORROSION AND FO UND TO BE OUT OF LIMITS IN REF TO MD/DC10-10 SRM 53-00-01 VOL I. ORIGIONAL .100, REMOVED.027, REMAINING .073. LOCATION OF DAMAGE STA 766, LBL 117. UPPER JAMB ACA7226-1 WAS REPLACED ON NON- ROUTINE N00665 2 L 7 3 4F RT A22WE 2007121800015 20071218 00015 WP 2007 12 18 07FDEA05016 1 20071207 A 5310 ACA72261 DOOR FRAME DOUG MD10 MD1010F 3022112 WP MAIN CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 MAIN CARGO DOOR JAMB TOP SURFACE UNDER NR 5 SPOOL FITTING HAS EXFOLIATION, STA 712. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IN REF TO MD/DC10-10 SRM 53-00-01 FIG 1 VOL I. ORIGIONAL .100, REMOVED .047, REMAINING .053. LOCATION OF DAMAGE AT STA 712, LBL 117. UPPER JAMB ACA7226-1 WAS REPLACED ON NON-ROUTINE N00665. 2 L 7 3 4F RT A22WE 2007121900009 20071219 00009 WP 2007 12 19 IXXA07SMN268S 1 20071116 A 5720 5770409502 SUPPORT DOUG DC8 DC873F 302199F WP ZONE 600 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE INTERNAL PART SUPPORT CRACKED AT STATION XFS 430 .000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SUPPORT. FABRICATED SUPPORT CLEANED, TREATED AND PRIMED AREA AND NEW SUPPORT. INSTALLED NEW FASTENERS AND NEW SUPPORT IAW BOEING MESSAGE NUMBER 1-680003043-2 DATED 12- 11-07, DRAWING NUMBER 5770409, DC8 SRM 57-1-0 PAGE 1, SRM 51-1-20D, DC8 SRM 51-1-8B, DC8 SRM 57-2-1 FIGURE 12 SHEET 1, 2 , AND 3, SRM 51-9-0 T/R 51-108, 51-126 DATED 04-03-00 AND 01-08-03, SRM 51-3-0, 51-1-20D, AND SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007121900015 20071219 00015 CE 2007 12 19 20071202 1 20071210 A 3260 SQUAT SWITCH CESSNA 680 680CE 2076811 CE MLG OUT OF ADJUST E CWQA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 05 305EJ 6800105 AFTER LANDING, GEAR RETRACTION CREW REPORTED AN IMMEDIATE VIOLENT SHAKING THROUGHOUT THE AIRCRAFT. GEAR INDICATION SHOW ED RED LIGHT ONLY. GEAR WAS EXTENDED AND SHAKING STOPPED AND INDICATED THREE GREEN, DOWN AND LOCKED. CREW DECLARED EME RGENCY AND LANDED AIRCRAFT. MAINTENANCE INSPECTED AND FOUND NOSE LANDING GEAR SQUAT SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH AND PERFORMED DANGEROUS TURBULENCE INSPECTION. NO DISCREPANCIES WERE NOTED 2 L 7 2 4F RC T00012WI 2007121900024 20071219 00024 NM 2007 12 19 2007UALA05016 1 20071207 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 338UA 24242 AFT SECTION EMERGENCY FLOOR LIGHTS INOPERATIVE. REPLACED POWER STRIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2007121900025 20071219 00025 NM 2007 12 19 2007UALA05017 1 20071207 A 3350 LIGHT BOEING 737 737322 1384676 NM ROW 6 BUCKLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 338UA 24242 FOUND EMERGENCY LIGHTS AT ROW 6 BUCKLED. STRAIGHTENED LIGHT AT ROW 6. 2 L 7 2 4F RT A16WE 2007121900027 20071219 00027 NM 2007 12 19 2007UALA05019 1 20071210 A 3350 78961 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 4E LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EEL STRIP AISLE OF SEAT 4E HANGING LOOSE. REPLACED EEL STRIP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121900053 20071219 00053 NM 2007 12 19 NWAA074066307 1 20071123 A 5313 STRINGER BOEING 747 747451 1384940 NM BS 500 S10L CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 667US 24222 DURING "M" CHECK WHILE ACCOMPLISHING BS 747-53A2484, FOUND CRACK IN STRINGER 10L AT BS 500. REPAIRED PER EA 63-211355. 2 L 7 4 4F RT A20WE 2007121900068 20071219 00068 NM 2007 12 19 2007UALA05027 1 20071207 A 5210 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 DOOR 4L INTERNAL WEBBING PUNCTURED AT UPPER HINGE ASSY AREA. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121900074 20071219 00074 NM 2007 12 19 2007UALA05062 1 20071211 A 3097 WIRE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE WINDSHIELD HEAT DAMAGED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 217UA 30550 F/O WINDSHIELD OVERHEATED AND STARTED TO SMOKE AT THE WINDOW TERMINAL LUGS. FWD WINDOW HEAT WAS TURNED OFF AND WINDOW DO ES NOT SHOW SIGNS OF CRACKING OR DELAMINATION PER CREW. REPLACED WINDOW AND SPLICED IN NEW WIRE TO WIRE HARNESS. SUSPEC T WIRE CRACK OR OPEN LEADING TO A OVERHEAT CONDITION. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121900078 20071219 00078 NM 2007 12 19 2007UALA05066 1 20071211 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 87UA 26713 EVACUATION DOOR LIGHT AT DOOR 4R INOP. FOUND LAMP INOP. RELAMPED ASSY-OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121900079 20071219 00079 WP 2007 12 19 IXXA07SMN267S 1 20071111 A 5542 SKIN DOUG DC8 DC873F 302199F WP ZONE 300 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT RUDDER RIGHT AT STATION ZR 87.000 TO STA ZR 115.000. REMOVE D FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING PAIR. FABRICATED NEW SKIN, INTERNAL, AND EXTERNAL DOUBLER. B ONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS PERFORMED BALANCE TO RUDDER. FOUND MOMENT WITHIN TOLERANCE MOMENT 2455 INCH/LB. INSTALLED NEW FASTENERS AND REPAIR PARTS DC8 SRM IAW 51-1-11, 51-1-21, DC8 SRM 51-4-6 PAGES 1-6, DC8 SRM 55-1-0 PAGE 1 AND SRM 51-1-21, DC8 SRM 55-6-1 FIGURE 1, ITEM "A", DC8 SRM 51-1-9, T/R 51- 142 DATED 04-05-06 AND DC8 SRM 51-1-9A T/R 51-141 DATED 04-03-06, DC8 AND SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007121900094 20071219 00094 EU 2007 12 19 TRAX200701829 1 20071129 A 5720 ANGLE AEROSP ATR72 ATR72212 8680945 EU RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 RT WING PRESSURE DECK ANGLE AT FR 27 STRG 4R CRACKED IN X AXIS 1.375 LONG, RESOLVED ON W/O: 75891 TASKCARD: N/R-00436. E/C PERFORMED IAW AMO 46-90 W/O 37934 IAW NTM CRACK CONFIRMED RT WING PRESSURE DECK ANGLE AT FR 27 STRG 4R, CRACK IN X A XIS IS SEALED IAW DO/TS-4923/07-9527 COMPLIED WITH EC/TC DO/TS-4923/07. 2 H 7 2 4T RT A53EU 2007121900099 20071219 00099 WP 2007 12 19 AALA20072423 1 20071212 A 3222 SEAL DOUG DC9 DC983 3022083 WP STRUT FAILED A AALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 21 437AA 49455 DFW INFLIGHT T616/12DEC - UNABLE TO RETRACT NOSE GEAR AFTER TAKEOFF. FLEW GEAR DOWN TO DFW AND LANDED WITHOUT INCIDENT . FOUND STRUT FLAT. REPLACED NOSE GEAR SEALS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2007121900100 20071219 00100 EU 2007 12 19 AALA20072440 1 20071213 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14056 463 JFK - SEAT MOUNTED EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENC Y LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121900133 20071219 00133 NM 2007 12 19 GTIA200700032 1 20071202 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 520NK 2784 FLOORBEAM Y-400 SHOW SIGNS OF CORROSION AT FRAME 68. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2007121900139 20071219 00139 NM 2007 12 19 2007UALA05041 1 20071206 A 2560 BRACKET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GIRT BAR DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 CANNOT ARM DOOR 1R. FOUND BRACKET DIRTY. CLEANED AREA AROUND GIRT BAR BRACKETS, DOOR OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121900140 20071219 00140 EU 2007 12 19 2007UALA05042 1 20071208 A 2560 LEVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE DOOR 2R STUCK A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 437UA 655 UNABLE TO ARM 2R. ARMING LEVER STUCK. DOOR LEVER WAS FREED UP AFTER NUMEROUS ATTEMPTS. NO DEFECTS WERE NOTED AND DOO R CLOSED/ARMED WITHOUT EFFORT AFTERWARD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121900142 20071219 00142 NM 2007 12 19 2007UALA05044 1 20071210 A 5400 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COWL UNKNOWN A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 663UA 27160 724657 FLIGHT DIVERTED DUE TO RIGHT ENGINE CORE COWL PROBLEM. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121900145 20071219 00145 EA 2007 12 19 QXEA200701853 1 20071209 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 601QX 10009 LAX - WITH EXTERNAL POWER PLUGGED IN, THE AC GREEN POWER LIGHT CYCLES OFF AND ON AND A BURN ODOR IS NOTICED. MAINTENANC E PLUG IN EXTERNAL POWER AND APPLIED POWER FOR OVER 15 MINUTES. LIGHT WAS STEADY GREEN AND THERE WAS NO BURN ODOR NOTIC ED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007121900148 20071219 00148 NM 2007 12 19 2007UALA04992 1 20071206 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 S11-12R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 50961 24640 FWD GALLEY DOOR FWD CUTOUT INTERCOSTAL ANGLE BETWEEN STRINGERS S11R AND S12R CRACKED AT BS 294.5. SUSPECT NORMAL AC OP ERATION. REMOVED CRACKED ANGLE AND REPLACED WITH NEW ANGLE. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007121900149 20071219 00149 NM 2007 12 19 2007UALA04993 1 20071206 A 3150 WARNING MESSAGE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE ILLUMINATED A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 671UA 30026 717695 NR 2 ENG OIL FLTR EICAS MSG AFT ENG START. TEMP UP TO 74C AND MSG STILL WOULD NOT ERASE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121900152 20071219 00152 SO 2007 12 19 SIMA200734605 1 20071211 A 2150 8152403 ACM EMB 145 EMB145LR 3260212 SO NR 2 SMOKE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 622AE 145108 PACK NR 2 FED BY APU CAUSED SMOKE IN CABIN AND COCKPIT. REMOVED AND REPLACED NR 2 ACM IAW 21-51-03, OPS CHK GOOD. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007121900155 20071219 00155 EU 2007 12 19 AALA20072446 1 20071214 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 JFK - EMERGENCY LIGHT AT RIGHT NUMBER THREE DOOR EXIT SIGN INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT RIGHT NUM BER THREE DOOR EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121900159 20071219 00159 EA 2007 12 19 QXEA200701850 1 20071208 A 4997 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA ECU DAMAGED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 605QX 10022 PDX - AFTER ENGINE START, THE APU FAULT CAUTION ILLUMINATED FOLLOWED BY A APU SHUTDOWN. COMPLIED WITH CHECKLIST AND MES SAGE WENT AWAY. MAINTENANCE FOUND A UNDERSPEED FAULT AND ECU BUSS FAULT IN THE MDC. RESEATED AND CLEANED THE ECU PINS. OPERATIONAL CHECKS GOOD AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007121900160 20071219 00160 SO 2007 12 19 SWIA200718928 1 20071207 A 3350 SIGN EMB 120 EMB120ER 3260203 SO CABIN UNSECURE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 567SW 120342 FLT 3720 - EXIT SIGN AT ROW 6 IS UNSECURE. REPLACED LIGHT ASSEMBLY. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007121900162 20071219 00162 EA 2007 12 19 SWIA200718930 1 20071210 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS UNSECURE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 963SW 7865 FLT 6693 - FLOOR LEVEL "EMERGENCY LIGHTING" STRIPS INOPERATIVE AFT OF ROW NR 9. SECURED CONNECTIONS TO AFT POWER STRIP IAW AMM 33-50-00. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2007121900164 20071219 00164 EA 2007 12 19 SWIA200718932 1 20071208 A 5270 STRIKER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY DOOR OUT OF ADJUST A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 771SK 10244 FLT 5830 - RIGHT EMERGENCY DOOR CAUTION ON THE GROUND. ADJUSTED DOOR SENSOR STRIKER PLATE. OP CHECKS GOOD IAW MM 52-70 -00. 2 L 7 2 4F RT A21EA 2007121900165 20071219 00165 EA 2007 12 19 SWIA200718933 1 20071207 A 3520 OXYGEN MASK CNDAIR CL600 CL6002C10 1390015 EA ROW 1 UNWANTED DEPLOY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 763SK 10228 FLT 6274 - O2 MASKS DROPPED ON RIGHT SIDE OF ROW 1. SECURED RIGHT SIDE O2 MASKS IAW MM 35-21-05. OPS CHECK GOOD AT THI S TIME. 2 L 7 2 4F RT A21EA 2007121900166 20071219 00166 EU 2007 12 19 20071201 1 20071211 A 5753 54147 BOLT AMD FALC90 FALCON900EX 2730009 EU FLAP ROD MISSING E CWQA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 05 88ND 19 AFTER T/O FLT CREW EXPERIENCED A FLAP ASYMMETRY UPON FLAP RETRACTION. FLAPS WERE HELD AT 14 DEGREES & WOULD NOT MOVE. CREW DECIDED TO DIVERT. UPON LANDING, MX INSPECTED & FOUND THE RT WING, 2ND OUTBOARD FLAP ROD, UNIVERSAL JOINT DISCONNE CTED & BOLT MISSING. FOUND NO OTHER DAMAGE. MX REINSTALLED NEW BOLT, RIGGED PER AFM & OPS TESTED OK. BOLT HOLDING THE RT WING 2ND OUTBOARD FLAP DRIVE TUBE SPLINE TO UNIVERSAL JOINT TIGHTENING FORK MAY NOT HAVE BEEN INSTALLED AFTER MAINTEN ANCE ON A PREVIOUS "C" CHECK INSPECTION. BOLT & LOCKING DEVICE WERE NOT FOUND. THE CONCLUSION THAT BOLT MOST LIKELY NOT INSTALLED WAS REACHED BY LACK OF WITNESS MARKS ON WING STRUCTURE LOCATED CLOSE TO FLAP CONTROL ROD UNIVERSAL JOINT. 2 L 7 3 4F RT A46EU 2007121900167 20071219 00167 NM 2007 12 19 NWAA074035641 1 20071207 A 5313 STRINGER BOEING 757 757251 1384970 NM BS 1680-1681 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 541US 26488 DURING "M" CHECK, FOUND CRACK IN STRINGER AT BS 1680-1681 S15L. REPAIRED PER EA 56-210582. 2 L 7 2 4F RT A2NM 2007121900171 20071219 00171 EA 2007 12 19 SWIA200718934 1 20071203 A 7120 MOUNT CNDAIR CL600 CL6002C10 1390015 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 708SK 10156 LEFT ENGINE FORWARD YOKE ENGINE MOUNT IS CORRODED. REPLACED LEFT YOKE ENGINE MOUNT WITH SERVICEABLE PART IAW MM 71-21-0 1, P/N: BA670-37070-13, S/N OFF: 230. 2 L 7 2 4F RT A21EA 2007121900174 20071219 00174 EA 2007 12 19 SWIA200718936 1 20071203 A 7120 MOUNT CNDAIR CL600 CL6002C10 1390015 EA ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 708SK 10156 CORROSION PITTING FOUND ON UPPER AND LOWER FORWARD ENGINE MOUNT PINS. INSTALLED SERVICEABLE PINS IAW MM 71-21-01, P/N: MM670-37011-003. 2 L 7 2 4F RT A21EA 2007121900176 20071219 00176 EA 2007 12 19 SWIA200718938 1 20071210 A 3230 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 903SW 7425 FLT 6650 - NOSE GEAR DISAGREE ON FINAL. REPLACED NLG PRIORITY VALVE IAW AMM 32-33-00. OPS AND LEAK CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007121900177 20071219 00177 EA 2007 12 19 TRAX200701894 1 20071210 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 903EV 7621 AAR-2011 - LT WINDSCREEN EMERGENCY EXIT SIGN HAS 3 INOP LAMPS. 2 L 7 2 4F RT A21EA 2007121900178 20071219 00178 NM 2007 12 19 2007UALA05021 1 20071209 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 FOUND EEL LIGHTS INOP AT 35 ABC. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121900179 20071219 00179 NM 2007 12 19 2007UALA05030 1 20071207 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 FOUND DOOR R1 UPPER GATE HAS 2 CRACKS, ONE AT EACH END. REMOVED AND REPLACED UPPER GATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121900180 20071219 00180 EA 2007 12 19 TRAX200701895 1 20071210 A 5510 PIVOT ASSY CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB GOUGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 903EV 7621 HORIZONTAL STABILIZER RT OUTER PIVOT PIN HAS GOUGE, POSSIBLE CRACK ON I/B END NEXT TO ANTI-ROTATION TAB. 2 L 7 2 4F RT A21EA 2007121900182 20071219 00182 NM 2007 12 19 2007UALA05045 1 20071210 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 677UA 30029 EMERGENCY LIGHTS OVER L OVERWING EXIT ROWS 15-22 ARE INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121900190 20071219 00190 EA 2007 12 19 SWIA200718940 1 20071207 A 2740 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 975SW 7951 RECEIVED STAB TRIM RUNAWAY AURAL WARNING IN FLIGHT. REPLACED PITCH FEEL CONTROL UNIT, MOTOR CONTROL UNIT AND AUTO PILOT FLIGHT CONTROL PANEL. OPS CHECK GOOD, PN 30000-09 SN OFF 04-1033, PN 7062-3 SN OFF 1374PN 822-0044-001 SN OFF HG5W. 2 L 7 2 4F RT A21EA 2007121900192 20071219 00192 EA 2007 12 19 SWIA200718942 1 20071210 A 3233 16520101 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 903SW 18433 18433 7425 FLT 6675 - ON APPROACH, RECEIVED NOSE GEAR DISAGREE AND NOSE GEAR DOOR OPEN WARNING MESSAGES BEFORE NOSE GEAR LOCKED DOW N IN PLACE WITH THREE GREENS. REPLACED NLG EXTEND/RETRACT ACTUATOR IAW CRJ 200 MM 32-33-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007121900194 20071219 00194 SO 2007 12 19 SWIA200718944 1 20071023 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 290SW 120317 FOUND AT C-CHECK, LEFT FORWARD SEAT TRACK IS CORRODED. REPLACED SEAT TRACK IAW AMM 53-01-05. 2 L 7 2 4T RT A31SO 2007121900196 20071219 00196 SO 2007 12 19 SWIA200718946 1 20071205 A 5610 WINDOW EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 561SW 120335 FLT 3716 - CAPTAINS SIDE WINDOW IS CRACKED. REPLACED CAPTAINS SIDE DIRECT VISION WINDOW IAW AMM 56-11-01. 2 L 7 2 4T RT A31SO 2007121900198 20071219 00198 EA 2007 12 19 CHQA200700094 1 20071210 A 2752 601R93106309 SHAFT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS FAILED A CHQA L ABORTED APPROACH O OTHER AP APPROACH 1 GL 11 645BR 7383 GEE872681 IAH TO HRL - ON APPROACH TO HRL, THE FLAPS FAILED AT 20 DEGREES WHEN SELECTED TO 30 DEGREES. THE QRH WAS FOLLOWED AND T HE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE WAS ABLE TO RESET THE FLAP SYSTEM AND OPERATE THE FLAPS IN ORDER TO FE RRY THE AIRCRAFT TO SDF. SDF MAINTENANCE TROUBLESHOT THE FLAP SYSTEM AND PERFORMED A TORQUE CHECK ON THE FLAP SYSTEM AN D FOUND THE NR 3 LT FLEX SHAFT FAILING THE TORQUE CHECK AND THE FLAP SYSTEM WAS OUT OF RIG. MAINTENANCE REPLACED THE FL EX SHAFT AND COMPLETELY RE-RIGGED THE FLAP SYSTEM. THE TEST FLIGHT THAT FOLLOWED WAS SUCCESSFUL AND NO FURTHER DEFECTS WERE NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 2007121900199 20071219 00199 WP 2007 12 19 IXXA07SMN257S 1 20071115 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 879 L21L DAMAGED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT MISSDRILLED HOLE ON FLANGE OF FRAME FITTING AT STATION 8 79.000 LONGERON-21 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PLUGGED MISDRILLED HOLE WITH RIVET. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION NOTED. FABRICATED REPAIR ANGLE. CLEANED, TREATED AND PRIMED AREA AND REPAIR A NGLE. INSTALLED NEW FASTENERS AND REPAIR ANGLE IAW FAA FORM 8110-3 NUMBER 07529 DATED 11-09-07, SEMAN DRAWING NUMBER ED -4655 DATED 11-07-07, DC8 SRM 51-1-20D, DC8 SRM 51-1-21,DC8 NDT SPM PART 08-00-02 TO 07, FORM 242-4, DC8 SRM 51-1-8B, AN D 51-3-1. 2 L 7 4 4F RT 4A25 2007121900200 20071219 00200 WP 2007 12 19 IXXA07SMN256S 1 20071115 A 5311 FRAME DOUG DC8 DC873F 302199F WP ZONE 200 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT HAS A IMPROPER REPAIR AND DENT ON FRAME AT STATION 1580. 000 LONGERON-20 RIGHT REMOVED FASTENER AS NEEDED TO PERFORM REPAIR. REMOVED FRAME SEGMENT WITH EXISTING REPAIR. FABRIC ATED FRAME SEGMENT, ANGLES. PERFORMED HEAT TREATMENT. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NE W FASTENERS, AND REPAIR PARTS IAW DC8 SRM 53-2-0 FIGURE 2 SHEET 4 AND 6, DC8 SRM 51-1-20D, DC8 SRM 53-4-1 FIGURE 51 SHEE T 21 ITEM "A", SRM 53-2-0 FIGURE 2 SHEET 7 AND 8 T/R 53-110 DATED 11-10-2000, DC8 SRM 51-1-1 PAGES 1, 13, 17, DC8 SRM 51-1-8B, AND 51-3-1. 2 L 7 4 4F RT 4A25 2007122000002 20071220 00002 WP 2007 12 20 IXXA07SMN274S 1 20071126 A 5330 SKIN DOUG DC8 DC873F 302199F WP ZONE 100 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT FORWARD FUSELAGE ACM AFT LOWER CORNER, SPACING TOO LARGE, AT STATION FS 8. 000 LONGERON-30 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK NO CORROSION NOTED. FABRICATED NEW SKIN, INTERNAL, AND EXTENAL DOUBLERS. CLEANED, TREATED AND PRIMED AREA REPAIR PARTS. INSTALLED NEW FASTENERS, AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 07578 DATED 12-06-07, SEMAN DRAWING NUMBER ED-4660 DATED 11-22-07, DC8 SRM 51-1-21, 51-1-20D, DC8 NDT SPM PART 08-00-02 TO 07, FORM SEMAN 242-4, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007122000003 20071220 00003 WP 2007 12 20 IXXA07SMN275S 1 20071126 A 5330 SKIN DOUG DC8 DC873F 302199F WP ZONE 100 MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT FORWARD FUSELAGE BELOW AND AFT OF ACM, SPACING TOO LARGE AT STATION FS 8. 000 LONGERON-30 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK NO CORROSION NOTED. FABRICATED NEW SKIN, INTERNAL, AND EXTERNAL DOUBLERS. CLEANED, TREATED AND PRIMED AREA REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 07569 DATED 11-27-07, SEMAN DRAWING NUMBER ED-4663 DATED 11-24-07, DC8 SRM 51-1-21, 51-1-20D, DC8 NDT SPM PART 08-00-02 TO 07, FORM SEMAN 242-4, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007122000005 20071220 00005 NM 2007 12 20 QXEA200701919 1 20071218 A 3097 697071272 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM DE ICE SYSTEM BROKEN A QXEA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 NM 09 400QX 4030 SEA- FLIGHT 2397 - PROP DE-ICE CAUTION LIGHT ILLUMINATED FOR ABOUT 10 SECONDS WHILE NR 2 ENGINE PROP GREEN LIGHT ILLUMIN ATED. THIS HAPPENED SEVERAL TIMES. TURNING THE DE-ICE OFF PER THE CHECKLIST THE CAUTION WENT OUT. MAINTENANCE REPLACE D A BROKEN DE-ICE LEAD ON THE NR 2 PROP, NR 3 BLADE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007122000006 20071220 00006 EU 2007 12 20 AALA20072450 1 20071215 A 3350 1009821 SIGN AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 50051 459 JFK - EMERGENCY EXIT SIGN AT OVERHEAD RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED EXIT SIGN ASSEMBLY FOR EMERGENCY EXIT SIGN AT OVERHEAD RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007122000007 20071220 00007 NM 2007 12 20 AALA20072454 1 20071215 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 697AN 26977 JFK EMERGENCY LIGHTS AT SEAT 13D INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHTS AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007122000008 20071220 00008 NM 2007 12 20 AALA20072455 1 20071215 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 697AN 26977 JFK - EMERGENCY LIGHTS AT SEAT 13D INOPERATIVE. REPLACED LENS FOR EMERGENCY LIGHTS AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007122000009 20071220 00009 WP 2007 12 20 AALA20072451 1 20071215 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 485AA 49678 LGA - EMERGENCY LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007122000011 20071220 00011 WP 2007 12 20 AALA20072453 1 20071215 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 501AA 49738 LGA - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 32 INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROW 32. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007122000012 20071220 00012 SO 2007 12 20 SWIA200718956 1 20071208 A 5210 BUSHING EMB 120 EMB120ER 3260203 SO PAX DOOR TQ TUBE BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 232SW 120306 FLT 3664 - MAIN CABIN DOOR HANDLE IS VERY DIFFICULT TO OPEN AND CLOSE. REPLACED CENTER ROD TORQUE TUBE BUSHINGS. OPS C HECK GOOD IAW MM 52-11-05. 2 L 7 2 4T RT A31SO 2007122000013 20071220 00013 EA 2007 12 20 SWIA200718957 1 20071211 A 3350 FIXTURE CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 703SK 10139 FLT 6048 - EMERGENCY LIGHT ON THE GALLEY WALL IS BROKEN. REPLACED FLOOR LEVEL FLOOD LIGHT FIXTURE IN GALLEY IAW CRJ AMM 33-51-11. 2 L 7 2 4F RT A21EA 2007122000017 20071220 00017 NM 2007 12 20 2007UALA02361 1 20070702 A 2420 693731575 MODULE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE A/C POWER BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 370UA 24539 A-C FAILS STANDBY POWER TEST WHEN SWITCH PLACED FROM OFF TO AUTO POSITION. REPLACED P5-5 MODULE, GEN DRIVE AND STBY PWR MODULE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122000019 20071220 00019 NM 2007 12 20 2007UALA05067 1 20071211 A 3350 58674 INVERTER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 913UA 25291 CABIN FLOOR MOUNTED EEL LIGHTS INOP FROM ROW 4 TO 9. REPLACED BATTERY PACK AND INVERTER. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122000022 20071220 00022 SO 2007 12 20 SIMA200734803 1 20071213 A 5610 SEAL EMB 145 EMB145LR 3260212 SO COCKPIT WINDOW LEAKING A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 689EC 14500853 CREW REPORTED DURING CLIMB A AIR LEAK COMING FROM THE FO'S DV WINDOW. CREW ELECTED TO RETURN TO DFW. AIRCRAFT LANDED A ND RETURNED TO THE GATE SAFELY. REMOVED AND REINSTALLED REPAIRED SEAL IN RT DV WINDOW, IAW EMB145 AMM 56-10-02. PERFOR MED PRESSURIZATION CHECK IAW EMB 145-AMM 21-51-00 PRESSURE CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007122000024 20071220 00024 NM 2007 12 20 2007UALA05070 1 20071212 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 171UA 24322 UPPER DECK EMERGENCY EXIT SIGN INOP AT LEFT CEILING DOOR SIGN. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007122000027 20071220 00027 NM 2007 12 20 2007UALA05073 1 20071212 A 3260 WARNING LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE MLG FALSE ACTIVATION A UALA O OTHER N FALSE WARNING CL CLIMB 1 WP 29 367UA 24536 NOSE LANDING GEAR RED LIGHT WAS ILLUMINATED AFTER TAKEOFF, AND CONTINUED TO BE ILLUMINATED. CREW VERIFIED NOSE GEAR WAS UP. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122000029 20071220 00029 NM 2007 12 20 2007UALA05075 1 20071213 A 3150 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 676UA 30028 FLIGHT DIVERTED DUE A LE SLAT ASSY INDICATION AT FL360. 2 L 7 2 4F 4 F RT A1NM E24NE 2007122000032 20071220 00032 NM 2007 12 20 2007UALA02953 1 20070801 A 2910 O-RING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HYD PUMP MISINSTALLED A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 336UA 24240 CREW REPORTS 'A' RESERVOIR QUANTITY DECREASED TO ROUGHLY 25 PERCENT. IMPROPER O-RING INSTALLATION. REPLACED O-RING AT EDMP PUMP-SERVICED SYSTEM-LEAKED CHECKED-NONE NOTED. OK FOR SERVICE. FOUND O-RING DISLODGED BETWEEN UNION AND PUMP POR T DUE TO MISSING STEEL BACKUP WASHER. REPLACED BOTH STEEL WASHER AND O-RING TO REPAIR THIS LEAK. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122000033 20071220 00033 NM 2007 12 20 2007UALA05078 1 20071212 A 3150 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 671UA 30026 RTFL DUE TO EICAS "R GEN OFF" DISPLAYED AT LIFT - OFF, WILL NOT RESET. 2 L 7 2 4F 4 F RT A1NM E24NE 2007122000039 20071220 00039 NM 2007 12 20 2007UALA05079 1 20071212 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 50961 24640 CABIN FLOORBEAM CORRODED ON UPPER CHORD, BS 986 RBL 45". SUSPECT NORMAL AC OPERATION. MAJOR REPAIR ACCOMPLISHED. REPAIR ED FLOOR UPPER BEAM T-CAP.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122000040 20071220 00040 NM 2007 12 20 2007UALA05080 1 20071212 A 5415 FITTING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 NR 2 PYLON CROSS TIE FITTING HAS A CRACK ON THE OUTBOARD ATTACH FASTENER LOCATION AT NAC STA 107.7. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007122000042 20071220 00042 NM 2007 12 20 2007UALA05084 1 20071213 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 5E EMERGENCY EXIT LIGHTS INOPERATIVE. RESECURED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007122000043 20071220 00043 NM 2007 12 20 2007UALA05085 1 20071212 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 L-2 DOOR UPPER GATE CRACKED. INSTALLED NEW GATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010800039 20080108 00039 EU 2008 1 8 07FDEA05135 1 20071224 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS STRINGER REPAIR LOCATED IN BULK CARGO ON STRINGER 53 RT BETWEEN FRAMES 63 TO 65, HAS 1 EACH REPAIR SECTION ME ASURING 32.1" LONG AND 1 EACH REPAIR SPLICE MEASURING 7.9" LONG PREVIOUSLY INSTALLED REPAIR LOCATED AT BULK CARGO ON STR INGER 53 RT BETWEEN FRAMES 63 TO 65 WAS DETERMINED NOT TO BE IAW A310 SRM 53-10-14 FIG 201, DUE TO INCORRECT REPAIR SPLI CE MATERIAL INSTALLED, BASED ON A VISUAL EVALUATION WITH THE REPAIR INSTALLED. REMOVED EXISTING REPAIR SPLICE AND REPAI RED PER A310 SRM 53-10-14 FIG 201. THIS IS A REPAIR WITH NO AIRBUS ISSUED PART NUMBER, REPAIR IDENTIFIED BY THE AGING AIRCRAFT INSPECTION PROGRAM. 2 L 7 2 4F RT A35EU 2007122000045 20071220 00045 WP 2007 12 20 IXXA07SMN276S 1 20071126 A 5330 SKIN DOUG DC8 DC873F 302199F WP ZONE 200 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT FORWARD FUSELAGE FORWARD GALLEY VENT ABOVE R-1 DOOR, RIVET SPACING TOO SM ALL AT STATION FS 183.000, LONGERON-10.5 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR . REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION NO CRACK, NO CORROSION NOTED. FABRICATED INTERNAL, AND EXTERNAL DOUB LERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8100-9 DATED 12-10-07, BOEING MESSAGE NUMBER 704498313-4 DATED 10-12-07 AND 1-689890784-4 DATED 11-21-07 AD-2000-20-08, S/B DC8 -53-075, DRAWING DOUGLAS SR08530021 AND 5750776, DC8 SRM 51-1-21, 51-1-20D, DC8 SRM 51-1-8B, BOEING MESSAGE NUMBER 1-689 2 L 7 4 4F RT 4A25 2007122000046 20071220 00046 EU 2007 12 20 F3LA200700376 1 20071215 A 3350 LIGHT AIRBUS A318 A318111 3940019 EU CABIN INOPERATIVE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 808FR 3038 MAINTENANCE REPORTED ONE LIGHT IN EMERGENCY SEAT MOUNTED LIGHT ASSY AT ROW 5ABC INOP. REMOVED AND REPLACED ROW 5ABC EME RGENCY SEAT MOUNTED LIGHT ASSY IAW AMM 33-51-11-PB401. OPS CHECK GOOD. 2 L 7 2 4F RT 2007122000048 20071220 00048 NM 2007 12 20 QXEA200701910 1 20071215 A 3297 471515 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM MLG MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 406QX 4048 BOI- FLIGHT 2422 - DEPARTING BOI SELECTED GEAR UP, BUT GEAR REMAINED DOWN. HANDLE WAS ILLUMINATED AND GREEN LIGHTS AND R ED UNSAFE LIGHTS STAYED ON. MOVED HANDLE TO DOWN POSITION AND LIGHT WENT OUT. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE WOW 2 CENTERING HARNESS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007122000049 20071220 00049 EA 2007 12 20 QXEA200701908 1 20071216 A 2612 22402820 FIRE LOOP CNDAIR CL600 CL6002C10 1390015 EA ILLUMINATED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 608QX 10026 PSP- FLIGHT 2625 - FIRE SYSTEM FAULT MESSAGE RECEIVED. MAINTENANCE PLACED ON MEL 26-00-1. REPLACED FIRE LOOP "A" AT TH E RIGHT ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007122000053 20071220 00053 EU 2007 12 20 07FDEA05076 1 20071218 A 5230 A52378014202 SKIN AIRBUS 310 A310203 3930313 EU CARGO DOOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FOUND BULK PIT DOOR SKIN DENTED AT FWD LOWER EDGE. DENT FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 52-30-00 PAGE 108. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW A310-200 SRM 52-30-00 FIG 206, AND SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007122000054 20071220 00054 EU 2007 12 20 07FDEA05077 1 20071218 A 5280 A5281005220000 HINGE FITTING AIRBUS 310 A310203 3930313 EU NLG DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 LT AFT NLG DOOR, AFT HINGE CRACKED. REMOVED AND REPLACED LT AFT NLG AFT HINGE FITTING IAW A310-200 CMM 52-82-12 P 204. 2 L 7 2 4F RT A35EU 2007122000059 20071220 00059 NM 2007 12 20 HALA0700526 1 20071213 A 4920 S351T02018 ECU BOEING 767 7673CB 1385187 NM APU FAILED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 592HA 33468 ETOPS SIGNIFICANT SYSTEM, APU FAILED AFTER PARKING. APU T/S PER FIM 49-11-00. REMOVED AND REPLACED ECU IAW AMM APU, OP S CHKD NML. 2 L 7 2 4F RT A1NM 2007122000062 20071220 00062 EA 2007 12 20 SWIA200718949 1 20071208 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCONNECTED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 905SW 7437 FLT 5872 - EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPAIRED WIRING ON AFT EMERGENCY LIGHT AS REQUIRED. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007122000064 20071220 00064 EA 2007 12 20 SWIA200718951 1 20070814 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 738SK 10195 FOUND AT C-CHECK, FS 280 FLOORBEAM IS CRACKED AT LBL12 AND RBL12. INSTALLED FS280 BEAM AS PER CRJ7/9 SRM 51-42-06 AND 51-42-13 AND LIGHTNING DIVERTER PANELS PER CRJ7/9 SRM 51-41-02. 2 L 7 2 4F RT A21EA 2007122000065 20071220 00065 EA 2007 12 20 SWIA200718952 1 20070814 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 738SK 10195 FS 280 FORWARD FLOORBEAM IS CRACKED AT LBL10 AND RBL10 RADIUS OF UPPER FLANGE, FOUND AT C-CHECK. INSTALLED FLOOR SUPPOR T FOR COCKPIT AT FS 280 PER CRJ7/9 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2007122000066 20071220 00066 EA 2007 12 20 SWIA200718953 1 20070822 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 429SW 7518 AREAS OF CORROSION FOUND AT BOTTOM OF LEFT OVERWING EMERGENCY EXIT DOOR, FOUND AT C-CHECK. REMOVED CORROSION PER CRJ200 SRM 52-00-00 FIG 102. 2 L 7 2 4F RT A21EA 2007122000068 20071220 00068 EA 2007 12 20 SWIA200718955 1 20070826 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 730SK 10193 COCKPIT FLOORBEAM ANGLE IS CRACKED AT RBL9 AND LBL9 AT FS 280 BEAM, FOUND AT C-CHECK. INSTALLED NEW COCKPIT FLOORBEAM AT FS 280 PER SB670BA-53-026. 2 L 7 2 4F RT A21EA 2007122000069 20071220 00069 NM 2007 12 20 GITA200700034 1 20071203 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 520NK 2784 FLOORBEAM Y-512.2 AT APPROX FRAME 69 CORRODED. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2007122000072 20071220 00072 EA 2007 12 20 TRAX200701918 1 20071211 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 683BR 7692 A/S/D SFT ANCHOR FITTING HAS SUSPECTED CRACK. 2 L 7 2 4F RT A21EA 2007122000073 20071220 00073 EA 2007 12 20 TRAX200701920 1 20071212 A 5310 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA RT OVERWING CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 903EV 7621 AAR-8020 - RT OVERWING EMERGENCY EXIT HAS CORROSION INSIDE LOWER ACCESS HOLE ON AFT SIDE. 2 L 7 2 4F RT A21EA 2007122000075 20071220 00075 NM 2007 12 20 2007UALA05014 1 20071208 A 5310 6545875U70 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294-328 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 PASSENGER CABIN FLOOR, DOOR 1 RIGHT INBD CREASE BEAM CORRODED BETWEEN BS 294-328 WL 208. MAJOR REPAIR ACCOMPLISHED: RE MOVED AND REPLACED DAMAGED FLOOR CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122000076 20071220 00076 NM 2007 12 20 2007UALA05015 1 20071208 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 280 S2L SCRATCHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 UPPER FUSELAGE HAS DEEP SCRATCHES AT BS 280 AND STRINGER S2L, N-R 12941-2000-0007. MAJOR REPAIR ACCOMPLISHED: FABRICATE D AND INSTALLED EXTERNAL FUSELAGE SKIN DOUBLER TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122000082 20071220 00082 NM 2007 12 20 2007UALA05093 1 20071214 A 5312 STIFFENER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT MLG WW CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 59770 23671 RIGHT MAIN WW FWD BULKHEAD HAS CRACKED STIFFENER. SUSPECT NORMAL AC OPERATION. MANUFACTURED AND HEAT TREATED REPAIR AN GLE PER MM57-12-96, INSTALLED STIFFENER RETURNED AC TO ORIGINAL CONFIGURATION. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122000083 20071220 00083 NM 2007 12 20 2007UALA05094 1 20071213 A 5310 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 328UA 24148 LOWER NOSE AREA HAS DAMAGE. ACFT OK FOR CONTINUES SERVICE PER EVA 60175A UNTIL 15MAY2007 OR 24 MONTHS. PERMANENT REPAIR ACCOMPLISHED BY REPLACING EXTERNAL DOUBLER PER EA I070906. INSPECTION COMPLETE. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122000084 20071220 00084 EU 2007 12 20 2007UALA05095 1 20071214 A 3510 B-NUT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE OXYGEN SYS LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 463UA 1282 CREW OXYGEN PRESSURE IS 1310 PSI ON ECAM. FOUND LEAKING B-NUT AT CAPT LOCATION. TIGHTENED B-NUT AND CHECKED ALL LOCAT IONS IN COCKPIT. NO LEAKS NOTED. SERVICED 02 SYSTEM TO FULL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007122000085 20071220 00085 NM 2007 12 20 2007UALA04751 1 20071119 A 5210 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 L2 DOOR UPPER HINGE CUTOUT REQUIRES DOUBLER (NOT CRACKED). PRECAUTIONARY MAJOR REPAIR ACCOMPLISHED. PERFORMED HFEC PER NDT MANUAL. NO DEFECT NOTED. INSTALLED DOUBLER IN THE AREA. 2 L 7 2 4F 4 F RT A2NM E17NE 2007122000089 20071220 00089 EU 2007 12 20 AALA20072447 1 20071214 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 JFK - SEAT MOUNTED EMERGENCY LIGHTS AT LEFT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT M ID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007122000090 20071220 00090 WP 2007 12 20 IXXA07SMN264S 1 20071115 A 5753 VANE DOUG DC8 DC873F 302199F WP LT WING TE FLAP DAMAGED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE OUTBOARD VANE WITH ELONGATED HOLES AT STATION XOL DO 67.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION NOTED. FABRICATED REPAIR DOUBLER. INTERNAL DOUBLER CLEANED, TREATED AND PRIMED AREA, REPAIR PARTS. INSTA LLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 07532 DATED 11-08-07, SEMAN DRAWING NUMBER ED-4654 DATED 11-05-07, DC8 SRM 51-1-21, 51-3-0, DC8 NDT SPM PART 08-00-02 TO 07, FORM SEMAN 242-4, DC8 SRM 51-1-8B, SRM 51-1-11, 51-1 -20D, AND 51-3-1. 2 L 7 4 4F RT 4A25 2007122000091 20071220 00091 WP 2007 12 20 IXXA07SMN263S 1 20071115 A 5730 SKIN DOUG DC8 DC873F 302199F WP ZONE 500 DAMAGED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE UPPER SKIN WITH MISDRILLED HOLES AT STATION XW 40 8.343. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AN D PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, 51-1-21, 51-3-0, 51-3-1, DC8 SRM 57-3-3 FIGURE 4 SHEET 1 ITEM "F", DC8 SRM 57-1-0 PAGE 1 AND SRM 51-1-21, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007122000095 20071220 00095 SO 2007 12 20 SIMA200734604 1 20071209 A 3010 ANTI-ICE SYSTEM EMB 145 EMB145LR 3260212 SO WING FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 900AE 14500885 WING ANTI ICE SYSTEM FAILED ON CLIMB-OUT. CREW CALLED MOC AND ELECTED TO RETURN BACK TO ORD DUE TO WEATHER. 2 L 7 2 4T RT T00011AT 2007122000096 20071220 00096 EA 2007 12 20 TRAX200701922 1 20071212 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 903EV 7621 PASSENGER DOOR HAS A CRACK IN FWD SKIN OF DOOR STEP SUPPORT, UNDER RAIL STOP BRACKET IN STEP RADIUS. REPAIRED DAMAGE T O PAX DOOR STEP SUPPORT FWD SIDE IAW ASA EC/T/C REO 601R-52-11-702. 2 L 7 2 4F RT A21EA 2007122000098 20071220 00098 EA 2007 12 20 TRAX200701924 1 20071212 A 3150 SMOKE WARNING CNDAIR CL600 CL6002C10 1390015 EA CARGO ILLUMINATED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 923EV 7826 SMOKE CARGO EICAS WARNING MSG ON SHORT FINAL. COMPLIED W/QRH AND MSG OUT. BOTTLES NOT BLOWN, EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2007122000099 20071220 00099 EA 2007 12 20 TRAX200701926 1 20071213 A 5530 ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 758EV 10210 LT VERTICAL STAB TO FUSELAGE ANGLE T/E CRACKED. NEEDS PAINT REMOVED FOR FURTHER EVALUATION. 2 L 7 2 4F RT A21EA 2007122000101 20071220 00101 NM 2007 12 20 2007UALA04752 1 20071119 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1480 S25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 AFT PIT STA 1480 STR 25L DENTED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED AREA, FABRICATED REPAIR, AND INSTALLED A N EW DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007122000102 20071220 00102 2007 12 20 2007UALA05097 4 20071213 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR SLIDE OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 585UA 26709 DOOR 1R UNABLE TO ARM SLIDE. FOUND GIRT BAR LANYARD INTERFERENCE. REPOSITIONED GIRT BAR LANYARD. DOOR FUNCTIONS NOR MALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007122000103 20071220 00103 EA 2007 12 20 TRAX200701928 1 20071213 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 838AS 7276 PASSENGER DOOR WILL NOT OPEN OR CLOSE. 2 L 7 2 4F RT A21EA 2007122000105 20071220 00105 EU 2007 12 20 TRAX200701792 1 20071127 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 FLOORBEAM 40 CORRODED AT SEVERAL PLACES (SEE UNDER A/N)(RESOLVED ON W/O: 75891 TASKCARD: N/R-00059 ) FLOORBEAM 40 CORRO SION REMOVED IAW SRM 51-21-42, OUT OF LIMIT AS PER SRM 53-00-00 TABLE 1. FLOORBEAM REPAIRED AS PER SRM 53-00-00 FIG 450 FLOORBEAM FLANGE. FABRICATED ON W/C 2000-231MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.016OUT OF LIMITS AS PER SRM: 53-00-00. 2 H 7 2 4T RT A53EU 2007122000106 20071220 00106 NM 2007 12 20 UPS07651304 1 20071216 A 2560 SEAT BELT BOEING 767 76734AF 1385212 NM SEAT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 323UP 27749 LEFT SUPERNUMARY SEAT INTERTIAL RESTRAINT INOP. REMOVED AND REPLACED RESTRAINT IAW MM 25-11-00-6. OPS CK NORMAL. 2 L 7 2 4F RT A1NM 2007122000109 20071220 00109 NM 2007 12 20 UPS07M51299 1 20071215 A 2612 FIRE LOOP DOUG MD11 MD11F 3023600 NM NR 1 NACELLE INOPERATIVE A IPXA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 01 284UP 48541 ATB-IFSD--DURING CLIMB-OUT AT FLT LEVEL 200; ENGINE 1 FIRE INDICATION AURAL WARNINGS SOUNDED. FIRE HANDLE RED LIGHT DID NOT ILLUMINATE. NO MASTER WARNING ANNUNCIATION. FIRE MSG ON EAD. ATB TO PHL - IFSD OF NR 1 ENGINE. REMOVED AND REPL ACED NR 1 ENGINE FIRE LOOP WIRING IAW MM CH 20 STD PRACTICES. REF LT T/R ELEC HARNESS WIRES 148001 THRU 148004 - 16BL A ND 16RD ACCOMPLISHED ALL FIRE DET TESTS IAW 26-11-02-5 CKS NORMAL. 2 L 7 3 4F RT A22WE 2007122000111 20071220 00111 NM 2007 12 20 2007UALA05099 1 20071213 A 3520 OXYGEN BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN READS HIGH A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 544UA 25322 O2 BOTTLES OVER 15ABC LOW PSI. REPLACED O2 BOTTLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007122000112 20071220 00112 EU 2007 12 20 MALA070190 1 20071204 A 5311 FRAME SAAB SF340 340B 7860101 EU MISREPAIRED A MALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 15 412XJ 340B412 PREVIOUS REPAIR TO UNDERFLOOR FRAME STA 258 CENTER FUSELAGE REQUIRES ADDITIONAL WORK. REPAIRED SECTION IAW EO NR S53108 . 2 L 7 2 4T RT A52EU 2007122000113 20071220 00113 NM 2007 12 20 07FDEA05056 1 20071214 A 5230 655720493 RIB BOEING 727 727233 138408A NM ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 C-2 PIT FWD CARGO DOOR HAS 2ND, 5TH AND 6TH LOWER EDGE FORMER RIBS CRACKED IN INSIDE OF DOOR REMOVED DAMAGE RIBS 3. FOR MED 3 RIBS FROM 7075-0 .050". HEAT TREATED TO T-6, 3EA. TRANSFERRED FASTENERS HOLES, APPLIED ALODINE, PRIMER AND PAIN T. INSTALLED 3 RIBS REF DWG 65-57204-93, SRM 51-30-2, 51-10-2 51-20-3, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007122000114 20071220 00114 NM 2007 12 20 UPS07M51276 1 20071211 A 2910 HYDRAULIC SYSTEM DOUG MD11 MD11F 3023600 NM NR 2 LEAKING A IPXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 275UP 48774 2 HOURS AFTER DEPARTURE, CREW REPORTED A LEAK ON THE NR 2 HYDRAULIC SYSTEM. T/S PER FIM 29-10-00-1. RAN NR 2 ENGINE PER AMM 71-00-00-51. NO LEAKS FOUND. RAN ALL 3 ENGINES FOR MIGRATION CHECK OF HYD FLUID FROM SYS 2 TO 1 AND 3. UNABLE TO FI ND LEAK OR MIGRATION OF HYD FLUID ON GROUND. FOB BEFORE ENG RUN 62.6, AFTER 62.0. HYD PRESS NR 2 3020, NR 1 3060, NR 3 3 020 PSI RESPECTIVELY. 2 L 7 3 4F RT A22WE 2007122100001 20071221 00001 SO 2007 12 21 C2XA07TY077 1 20071210 A 3350 276005 FUSE EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 21130 145704 FWD RIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED FUSES ON NR 2 EMERGENCY LIGHT BATTERY HOLDER IAW EMB VCMM 25-60-03. OPS CHECK GOOD. 2 L 7 2 4F RT 2007122100003 20071221 00003 NM 2007 12 21 USAA920071316 1 20071208 A 5313 6561277505 STRINGER SPLICE BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 24781 PIT - MAJOR REPAIR - FPBH, CRACKED STRINGER SPLICE, BS 360, S14L. REPLACED STRINGER SPLICE, BS 360, S14L IAW EO 5305V20 3. 2 L 7 2 4F RT A16WE 2007122100004 20071221 00004 NM 2007 12 21 USAA920071317 1 20071208 A 5313 69265552 STRINGER BOEING 737 7374B7 1384702 NM ZONE 200 - FUSEL CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 24781 PIT - MAJOR REPAIR - FPBH, CRACKED STRINGER, BS 348 - BS 351, S16L. REPLACED STRINGER, BS 348 - BS 351, S16L IAW EO 530 5V203. 2 L 7 2 4F RT A16WE 2007122100005 20071221 00005 NM 2007 12 21 USAA920071318 1 20071208 A 5322 6948204505 SHEAR TIE BOEING 737 7374B7 1384702 NM BS 360 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 24781 PIT - MAJOR REPAIR - FPBH, CRACKED SKIN CLIP, BS 360, S13L - S14L. REPLACED SKIN CLIP, BS 360, S13L - S14L IAW EO 5305V 203. 2 L 7 2 4F RT A16WE 2007122100006 20071221 00006 NM 2007 12 21 ASAA0742371 1 20070922 A 5320 6517684642 INTERCOSTAL BOEING 737 7374Q8 138447Q NM BS 294-303 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 FWD SIDE OF L1 DOOR CUTOUT STR 7L BS 294 INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW BAC DWG 65 17684 PEM CO EA PD 37 53 987 AND ALASKA EA 5310 02747. 2 L 7 2 4F RT A16WE 2007122100007 20071221 00007 NM 2007 12 21 ASAA0742372 1 20070922 A 5340 66142101 ATTACH FITTING BOEING 737 7374Q8 138447Q NM BS 294-303 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 FWD SIDE OF L1 DOOR CUTOUT STR 11L BS 294 ATTACH CLIP CRACKED. REMOVED AND REPLACED ATTACH CLIP IAW BAC DWG 66 14210 PE MCO EA PD 37 53 987 AND ALASKA EA 5310 02747. 2 L 7 2 4F RT A16WE 2007121700146 20071217 00146 NM 2007 12 17 SWAA076125 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700149 20071217 00149 NM 2007 12 17 SWAA076121 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007121700152 20071217 00152 NM 2007 12 17 SWAA076117 1 20071210 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700155 20071217 00155 NM 2007 12 17 SWAA076114 1 20071210 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121700182 20071217 00182 NM 2007 12 17 SWAA076145 1 20071210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 24L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007121700191 20071217 00191 NM 2007 12 17 SWAA076147 1 20071210 A 5311 6546552 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007121900010 20071219 00010 WP 2007 12 19 IXXA07SMN269S 1 20071116 A 5710 STRUCTURE DOUG DC8 DC873F 302199F WP ZONE 600 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING. NUMBER 4 STUB WING LEADING EDGE LOWER PART DOUBLER HAS A CRACK AT S TATION XFS 529.000. REMOVED FASTENERS AS NEEDED TP PERFORM REPAIR. REMOVED CRACKED DOUBLER. FABRICATED EXTERNAL, INTE RNAL REPAIR DOUBLER. PERFORMED HEAT TREATMENT TO REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INS TALLED NEW FASTENERS AND REPAIR PARTS IAW 51-1-20D, 51-3-1 DC8 SRM 57-2-1A FIGURE 1, DC8 SRM 51-1-21, DC8 SRM 51-1-1 PAG ES 1, 13, 17, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007121900011 20071219 00011 NM 2007 12 19 2007UALA05048 1 20071211 A 7711 EPR SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 ENGINE FAULTED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 824UA 965 V10394 FLIGHT DIVERTED WITH NR 2 ENGINE EPR MODE FAULT AND NR 2 ENG N1 UNRATED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121900029 20071219 00029 NM 2007 12 19 F3LA200700374 1 20071212 A 3350 32146210 EPSU AIRBUS A319 A319111 3930336 NM EMERGENCY LIGHTS INOPERATIVE A F3LA O OTHER O OTHER LD LANDING 1 NM 03 939FR 2448 FLIGHT CREW REPORTED AFT OVERHEAD EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE WITH GEAR EXTENSION. REPLACED EPSU 13WL IAW AMM 33-51-38-PB401. OPS TEST GOOD IAW AMM 33-51-38-740-040 AND CIDS EPSU TEST IAW 23-73-00-710-010. 2 L 7 2 4F RT A28NM 2007121900033 20071219 00033 EU 2007 12 19 1218344121707 1 20070921 A 5751 S5761009800101 TAB HINGE AEROSP ATR42 ATR42320 8680930 EU RT AILERON CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 14834 193 RT AILERON INBOARD TAB HINGE CORRODED. REMOVED AND REPLACED INBOARD HINGE. 2 H 7 2 4T RT A53EU 2007121900045 20071219 00045 NM 2007 12 19 AALA20072416 1 20071211 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT SEAT 26C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHTS AT SEAT 26C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121900046 20071219 00046 NM 2007 12 19 AALA20072418 1 20071211 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT SEAT 32G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 32G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121900061 20071219 00061 NM 2007 12 19 2007UALA05055 1 20071211 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY LIGHT AFT GALLEY RT BOTTOM WALL INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121900071 20071219 00071 WP 2007 12 19 IXXA07SMN266S 1 20071115 A 5542 SKIN DOUG DC8 DC873F 302199F WP RUDDER MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT RUDDER RIGHT HAND SKIN AT STATION ZR 115.000 TO STATION ZR 1 50.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKINS AND INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. PERFORMED BA LANCE TO RUDDER FOUND MOMENT WITHIN TOLERANCE MOMENT 2455 INCH/LB. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 55-6-1 FIGURE 1, DC8 SRM 55-1-0 PAGE 1 AND SRM 51-1-21, DC8 SRM 55-6-1 FIGURE 1 ITEM "A", DC8 SRM 51-1-9 T/R 51-142 DAT ED 04-05-06 AND DC8 SRM 51-1-9A T/R 51-141 DATED 04-03-06, DC8 SRM 51-1-8B, DC8 SRM 51-4-6 PAGES 1-6. DC8 SRM 51-1-11, A 2 L 7 4 4F RT 4A25 2007121900080 20071219 00080 NM 2007 12 19 NWAA074045657 1 20071213 A 3350 SIGN BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 557NW 33393 DURING OVERNIGHT CHECK, FOUND MID GALLEY LOWER EMERGENCY SIGN INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OPE RATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2007121900082 20071219 00082 NM 2007 12 19 2007UALA05029 1 20071208 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 FOUND DOOR 2L UPPER HINGE ARM CUTOUT HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED: INSTALLED STEEL DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121900087 20071219 00087 EA 2007 12 19 TRAX200701891 1 20071203 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 FS 280 WEB UNDER LBL 9 IS CRACKED UNDER THE PARKING BRAKE CABLE FITTING. REPAIRED CRACKED AREA OF FS 280.00 WEB UNDER L BL 9.00 REQUIRES FILLET SEAL/TOPCOAT FILLET SEALED IAW CRJ MM 51-23-00. REAPPLIED TOPCOATED IAW CRJ SRM 51-25-16 ALL WO RK ACCOMPLISHED IAW REO 601R-53-11-171 COMPLIED W/ ASA EO600-53-90. 2 L 7 2 4F RT A21EA 2007121900092 20071219 00092 NM 2007 12 19 NACA20070021 1 20071207 A 5310 DOOR FRAME BOEING 737 737232 1384475 NM BS 500B DAMAGED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 320DL 23092 DAMAGE TO MCD DOOR FRAME APPROXIMATELY 12-18 INCHES UP FROM AFT LOWER CORNER, MAIN CARGO DOOR AFT FRAME STA 500B+9 STRGR 15L-16L. HFEC AFFECTED AREA, NO FURTHER CRACKS. FABRICATED DOUBLERS AND REPAIRED PER NAC DRAWING NAC2007-320-02, FAA 8110-3 DATED 12-07-07. 2 L 7 2 4F RT A16WE 2007121900097 20071219 00097 NM 2007 12 19 AALA20072427 1 20071213 A 2560 BATTERY BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 775AN 29584 LT EMERGENCY FLASHLIGHT AT RIGHT NUMBER THREE DOOR JUMPSEAT INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT R IGHT NUMBER THREE DOOR JUMPSEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007121900108 20071219 00108 NM 2007 12 19 07FDEA05044 1 20071213 A 5330 65545789 SKIN BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 AFT CARGO COMPARTMENT, BODY STATION 1010 TO 1011, STRINGER 30, WATER LINE 139, BOTH SIDES OF STRINGER, FUSELAGE SKIN COR RODED. REMOVED CORROSION IAW SRM 51-10-6. AFTER CORROSION MATERIAL WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1 FIG 1 . CUT OUT DAMAGE AREA IAW SRM 53-30-3 FIG 1. FAB REPAIR DOUBLER IAW SRM 53-30-3 FIG 1. INSTALLED REPAIR DOUBLER AFTER TREATING AND PRIMING IAW 51-10-6 PG 1. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007121900124 20071219 00124 EU 2007 12 19 AALA20072437 1 20071213 A 3350 82400 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14056 463 JFK - EMERGENCY EXIT SIGN LIGHT AT LEFT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SIGN LIGHT AT L EFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121900127 20071219 00127 WP 2007 12 19 AALA20072430 1 20071213 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 448AA 49474 LGA - EMERGENCY LIGHT AT AFT OVERWING EXIT TOP INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 20 FOR EMERGENCY LIGHT AT AFT OVERWING EXIT TOP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007121900138 20071219 00138 NM 2007 12 19 F3LA200700375 1 20071214 A 3350 LIGHT AIRBUS A319 A319111 3930336 NM R2 DOOR INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 939FR 2448 FLIGHT CREW REPORTED EMERGENCY EXIT SIGN OVER R2 DOOR WOULD NOT ILLUMINATE. RESEATED CONNECTOR ON 32WL AND OPS CHECKED NORMAL IAW AMM 33-51-00-PB501. 2 L 7 2 4F RT A28NM 2007121900141 20071219 00141 EU 2007 12 19 2007UALA05043 1 20071208 A 3150 WARNING MESSAGE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ILLUMINATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 418UA 485 ELAC 2 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. ELAC 2 COMPUTER FAULT. REPLACED ELAC2, NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121900143 20071219 00143 WP 2007 12 19 IXXA07SMN262S 1 20071115 A 5753 VANE DOUG DC8 DC873F 302199F WP LT WING TE FLAP DAMAGED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE OUTBOARD VANE WITH ELONGATED HOLES AT STATION XOL DI 6.224. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, N O CORROSION NOTED. FABRICATED REPAIR DOUBLER INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA, REPAIR PART. INSTALL ED NEW FASTENERS AND REPAIR PARTS IAW 8110-3, DRAWING ED-4652 DATED 11-05-07, DC8 SRM 51-1-21, 51-3-0, DC8 NDT SPM PART 08-00-02 TO 07, FORM SMN 242-4, 51-1-20D, 51-3-1, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007121900144 20071219 00144 EA 2007 12 19 QXEA200701849 1 20071208 A 7710 M210D4N RELAY CNDAIR CL600 CL6002C10 1390015 EA LT ENGINE UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 612QX 10042 BOI - FLIGHT 2592 - ON TAXI RECEIVED A ENGINE DEGRADE CAUTION FOR THE LEFT ENGINE. RETURNED TO THE GATE. MAINTENANCE RE PLACED THE K19 AND K21 RELAYS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007121900146 20071219 00146 NM 2007 12 19 2007UALA04989 1 20071207 A 5520 BEARING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HINGE FITTING WORN A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 331UA 24192 RTFL DUE TO ELEVATOR VIBRATION. FOUND HORIZONTAL STAB LEFT CENTER SECTION HINGE BEARING WORN. REPLACED HINGE FITTING. 2 L 7 2 4F 4 F RT A16WE E2GL 2007121900154 20071219 00154 EU 2007 12 19 AALA20072443 1 20071214 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 JFK - EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR EXIT SIGN INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121900161 20071219 00161 EA 2007 12 19 SWIA200718929 1 20071212 A 3320 INVERTER CNDAIR CL600 CL6002B19 1900309 EA CABIN LIGHT INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 963SW 7865 FLT 6681 - AFT FLOOR LEVEL LIGHT STRIP IS INOP. REPLACED AFT INVERTER. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007121900163 20071219 00163 SO 2007 12 19 SWIA200718931 1 20071204 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 290SW 120317 RIGHT FORWARD EMERGENCY EXIT SIGN ASSEMBLY IS BROKEN. REPLACED EMERGENCY EXIT SIGN AS REQUIRED. OPS CK GOOD. 2 L 7 2 4T RT A31SO 2007121900169 20071219 00169 NM 2007 12 19 2007UALA05009 1 20071208 A 2150 A/C PACK BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 937UA 26668 UNUSUAL ELECTRICAL ODOR IN COCKPIT. EMERGENCY DECLARED. UNABLE TO DUPLICATE ODOR ON THE GROUND, SUSPECT PACK VALVE CON TAMINATION ISSUE. REPLACED CABIN TEMP MODULE AND BOTH PACK MODULES. NO REPEATS OF ODOR IN COCKPIT. 2 L 7 2 4F 4 F RT A16WE E2GL 2007121900170 20071219 00170 NM 2007 12 19 2007UALA05010 1 20071208 A 2612 6937307149 MODULE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 2 FIRE HANDLE FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 938UA 26671 NR 2 FIRE HANDLE WILL NOT TEST USING MASTER-DIM TEST SWITCH. SUSPECT FAULTY FIRE CONTROL MODULE. ENGINE & APU FIRE CON TROL MODULE REPLACED AND TESTED NORMAL PER MM 26-21-51-401. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007121900173 20071219 00173 EA 2007 12 19 SWIA200718935 1 20071203 A 7120 MOUNT CNDAIR CL600 CL6002C10 1390015 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 708SK 10156 LEFT ENGINE FORWARD MOUNT UPPER LINK AND BUSHINGS ARE CORRODED. REPLACED LEFT ENGINE FORWARD MOUNT UPPER LINK ASSEMBLY IAW MM 71-21-01. 2 L 7 2 4F RT A21EA 2007121900184 20071219 00184 NM 2007 12 19 2007UALA05047 1 20071207 A 3260 SENSOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE MLG DOOR MALFUNCTIONED A UALA O OTHER J WARNING INDICATION LD LANDING 1 WP 29 834UA 1420 LANDING GEAR NOT DOWN AND LOCKED ECAM MSG. LANDING GEAR DISAGREE AFTER LANDING. LANDING GEAR DOOR NOT CLOSED ECAM. F OUND EXCESSIVE GAP ON NLG LEFT DOOR SENSOR 39GA. REPLACED NLG LT DOOR SENSOR 39GA, PERFORMED GEAR SWINGS, OPERATING NO RMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121900187 20071219 00187 NM 2007 12 19 2007UALA05023 1 20071208 A 2120 UNKNOWN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN ODOR A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 194UA 26892 717603 HAZE AND ODOR IN CABIN WITH NR 3 ENGINE RUNNING. ONE QUART OF OIL ADDED DUE CREW REQUEST FOR OIL SERVICE PRIOR DEPT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121900189 20071219 00189 EA 2007 12 19 SWIA200718939 1 20071204 A 3350 RELAY CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 707SK 10003 EMERGENCY LIGHTING TURNS ON AND OFF WITH COCKPIT SWITCH IN THE ARM POSITION. REPLACED RELAY K135 ON PCB5 IN JB11. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2007121900193 20071219 00193 EA 2007 12 19 SWIA200718943 1 20071207 A 3230 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 903SW 7425 FLT 5851 - "GEAR DISAGREE" ON TAKEOFF AFTER SELECTING GEAR UP. NO PROBLEMS WITH GEAR ON EXTENSION. REPLACED MLG PRIORI TY VALVE IAW CRJ 200 MM 32-32-15. 2 L 7 2 4F RT A21EA 2007121900195 20071219 00195 SO 2007 12 19 SWIA200718945 1 20071207 A 5210 TORQUE TUBE EMB 120 EMB120ER 3260203 SO PAX DOOR CORRODED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 576SW 120345 FLT 3724 - CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. REPLACED CORRODED CABIN DOOR LOCKING TORQUE TUBE AND BUSHINGS IAW MM 52-1105. DOOR OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2007121900197 20071219 00197 SO 2007 12 19 CHQA200700093 1 20071210 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL MLG MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 296SK 145514 CAE311464 LGA TO CMH - DURING TAKEOFF AFTER A POSITIVE RATE WAS ESTABLISHED THE LANDING GEAR WOULD NOT RETRACT WITH A LANDING AIR/ GROUND FAIL ECIAS MESSAGE. CREW FOLLOWED QRH, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE CMC FOR FAULT CODES AND RETRIEVED CODES FOR LG PROX SWITCH AND LG AIR/GROUND LGEU FAIL. THE PROXIMITY SYSTEM WAS TR OUBLESHOT AND THE FAULT WAS FOUND WITH THE NOSE LANDING GEAR WEIGHT OFF WHEELS SWITCH. MAINTENANCE REPLACED THE SWITCH AND PERFORMED A COMPLETE SERVICE OF THE NOSE LANDING GEAR STRUT, PERFORMED GEAR SWINGS AND FOUND NO FURTHER FAULTS. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007122000014 20071220 00014 NM 2007 12 20 TSAA0721065 1 20071214 A 2120 CONTROLLER BOEING 737 7372X6C 1384552 NM RAM AIR DOOR MALFUNCTIONED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 841AL 059C1613 23123 FLIGHT 48 HNL-ITO - DURING CLIMB THE CREW NOTED THE RIGHT SUPPLY DUCT PRESSURE READING 100 PSI (FULL SCALE). THE CREW L ANDED IN HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT RAM AIR DOOR CONTROL AND PERFORMED AN ENGINE RUN WITH ALL OPERATIONAL CHECKS SATISFACTORY PER AMM 36-11-00. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2007122000035 20071220 00035 2007 12 20 UPS07551313 2 20071207 A 7200 ENGINE BOEING 757 75724APF 1384969 NM LEFT ODOR A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 409UP 23731 EXTREMELY HOT ODOR ON TAKEOFF ROLL AND AFTER TAKEOFF. ODOR INCREASED WITH BOTH PACKS AND DISSIPATED AFTER APPROX 15 MIN UTES AT CRUISE. FOR T/S RAN ENGINES, PRESSURIZED A/C, ISOLATED LT AND RT PACKS, COULD NOT DUPLICATE ODOR. ALSO WITH COC KPIT WINDOWS COLD, TURNED ON WINDOW HEAT AND NO ODOR NOTICED IN C/P. SUSPECT DEICE FLUID INGESTION. SEE SAME LP ITEM 3 . 2 L 7 2 4F RT A2NM 2007122000037 20071220 00037 WP 2007 12 20 IXXA07SMN273S 1 20071126 A 5312 56119433 BULKHEAD DOUG DC8 DC873F 302199F WP ZONE 100 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND BULKHEAD CAP ANGLES HAS IMPROPER REPAIR AT STATION 70.000 LONGERON-32.5LEFT. R EMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED FORWARD FRAME SEGMENT. FABRICATED FRAME S EGMENT, AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 07578 DATED 12-06-07, SEMAN DRAWING NUMBER ED-4659 DATED 12-01-07, DC8 SRM 51-3-0, 51-1-21, DRAWING DOUGLAS SR08538006 SRM 53-2-5 FIGURE 2 8C-2 SHEETS 1-2, T/R 53-176 FIG 8C-2 SHEET 2,3,4,5 DATED 09-30-03, DC8 SR M 51-1-8B, AND 51-3-1. 2 L 7 4 4F RT 4A25 2007122000038 20071220 00038 WP 2007 12 20 IXXA070065S 1 20071126 A 5312 56119433 BULKHEAD DOUG DC8 DC873F 302199F WP ZONE 100 MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND BULKHEAD CAP ANGLES HAS IMPROPER REPAIR AT STATION 70.000 LONGERON-32.5 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED FORWARD FRAME SEGMENT. FABRICATED FR AME SEGMENT, AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 07578 DATED 12-06-07, SEMAN DRAWING NUMBER ED-4659 DATED 12-01-07, DC8 SRM 51-3-0, 51- 1-21, DRAWING DOUGLAS SR08538006 SRM 53-2-5 FIGURE 2 8C-2 SHEETS 1-2, T/R 53-176 FIG 8C-2 SHEET 2,3,4,5 DATED 09-30-03, DC8 SRM 51-1-8B, AND 51. 2 L 7 4 4F RT 4A25 2007122000051 20071220 00051 EA 2007 12 20 QXEA200701920 1 20071218 A 3150 FIRE WARNING CNDAIR CL600 CL6002C10 1390015 EA ILLUMINATED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 601QX 10009 SMF - FLIGHT 2560 - RECEIVED A FIRE SYSTEM FAULT MESSAGE. MAINTENANCE PLACED THE SYSTEM ON MEL 26-00-1. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F RT A21EA 2007122000055 20071220 00055 EU 2007 12 20 07FDEA05078 1 20071218 A 2550 ROLLER TRAY AIRBUS 300 A300B4622 3930401 EU CARGO BAY MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 PREVIOUS ANGLE REPAIR LOCATED ON AFT CARGO ROLLER TRACK NR 1 RT -Y140 BETWEEN FRAME 57.3 AND 58 HAS 2 REPAIR ANGLES MEAS URING 7.7" L , 1 REPAIR SECTION MEASURING 8.3" L AND 1 REPAIR DOUBLER ON BOTTOM SURFACE MEASURING 8.3" BY 6.3" PREVIOUS REPAIR FOUND NOT TO BE IAW A300-600 SRM 53-10-15 PARA 5 PAGE 207-212 FIG 203. REMOVED AND REPLACED REPAIR WITH CORRECT REPAIR IAW A300-600 SRM 53-10-15 PARA 5 FIG 203 PAGE 207-212. THIS IS A REPAIR WITH NO AIRBUS ISSUED PART NUMBER, REPAI R IDENTIFIED BY THE AGING AIRCRAFT INSPECTION PROGRAM. 2 L 7 2 4F RT A35EU 2007122000057 20071220 00057 NM 2007 12 20 HALA0700525 1 20071212 A 3020 2790583108 ANTI-ICE VALVE BOEING 767 767332 1382001 NM RT ENGINE MALFUNCTIONED A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, EICAS MSG 'R ENG ANTI-ICE' DISP AND ENG ANTI-ICE VALVE LIGHT ILLUMINATED INTERMITTENTLY WITH R T SWITCH ON. REPLACED RT ENGINE ANTI-ICE VALVE PER AMM 30-31-03. 2 L 7 2 4F RT A1NM 2007122000058 20071220 00058 NM 2007 12 20 HALA0700524 1 20071213 A 3240 BRAKE ASSY BOEING 767 76733A 1385209 NM MLG FIRE A HALA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 WP 13 587HA 33421 NR 6 TIRE AND WHEEL AND TIRE CAUGHT FIRE AFTER PARKING. REMOVED NR 6 TIRE FOUND EXCESSIVE GREASE ON THE AXLE. REPLACED NR 5 AND NR 6 TIRE PER AMM 32-45-01 INSPECTED AXLE AND BRAKE. LATER REPLACED NR 6 BRAKE AND PERFORMED AXLE OVER TEMPER ATURE INSPECTION PRECAUTIONARY. NO FINDINGS OF HEAT DAMAGE. NOTE FUSE PLUGS DID NOT RELEASE. 2 L 7 2 4F RT A1NM 2007122000061 20071220 00061 EA 2007 12 20 SWIA200718948 1 20071208 A 3244 TIRE CNDAIR CL600 CL6002B19 1900309 EA NR 4 MLG FAILED A SWIA O OTHER O OTHER LD LANDING 1 NM 07 492SW 7168 NR 4 MAIN TIRE BLEW OUT ON LANDING, DAMAGING THE RIGHT INBOARD FLAP. REPLACED FLAP ASSEMBLY IAW CRJ 200 AMM 27-54-01, P /N: 601R14002-2, S/N OFF: SB/RJ/784. 2 L 7 2 4F RT A21EA 2007122000067 20071220 00067 EA 2007 12 20 SWIA200718954 1 20070826 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 730SK 10193 FS 280 BEAM IS CRACKED AT LBL9, FOUND AT C-CHECK. REPLACED FLOORBEAM PER SRM 51-42-06-001-001. 2 L 7 2 4F RT A21EA 2007122000071 20071220 00071 EA 2007 12 20 TRAX200701917 1 20071211 A 5210 HINGE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 683BR 7692 A/S/D AFT SUPPORT HINGE HAS SUSPECTED CRACK. 2 L 7 2 4F RT A21EA 2007122000078 20071220 00078 NM 2007 12 20 2007UALA05088 1 20071213 A 5320 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 996 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 PASSENGER CABIN STA 996 RBL41 HAS CORROSION ON WEB JUST INBOARD OF I-B CREASE BEAM BY DOOR 2R AT WL 208. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122000079 20071220 00079 NM 2007 12 20 2007UALA05089 1 20071213 A 5340 ATTACH ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 291 S12R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 FUSELAGE INTERCOSTAL ATTACH ANGLE IS CRACKED, BS 291.5 BELOW STR 12R. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122000086 20071220 00086 EU 2007 12 20 AALA20072445 1 20071214 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 JFK - EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR EXIT SIGN INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT RIGHT NUMBE R TWO DOOR EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007122000092 20071220 00092 NM 2007 12 20 2007UALA05096 1 20071213 A 3510 MC1025154 OXYGEN MASK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE 1ST OFFICER'S LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 CREW O2 PRESS GAGE READING 0. SAMC TEXT: FOUND 1ST OFFFICER'S MASK LEAKING, SWAPPING THE OBS MASK POSITION TO FO'S POSIT ION. OBS POSITION IS INOP. SUSPECT DAMAGE DUE TO PRE FLIGHT CHECKS. REPLACED OBSERVERS O2 MASK REF MM-35-12-86 LEAK A ND OPS CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122000097 20071220 00097 EA 2007 12 20 TRAX200701923 1 20071212 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 903EV 7621 PASSENGER DOOR HAS A CRACK IN AFT SKIN OF DOOR STEP SUPPORT, UNDER RAIL STOP BRACKET IN STEP RADIUS. REPAIRED DAMAGE TO PAX DOOR STEP SUPPORT AFT SIDE IAW ASA EC/TC REO 601R-52-11-702. 2 L 7 2 4F RT A21EA 2007122000100 20071220 00100 EA 2007 12 20 TRAX200701927 1 20071213 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 758EV 10210 FOUND FS 280 FWD FLOORBEAM ANGLE IN CORRODED. 2 L 7 2 4F RT A21EA 2007122000104 20071220 00104 SO 2007 12 20 CHQA200700092 1 20071209 A 3610 CA33020 CLAMP EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL BLEED DUCT BROKEN A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 288SK 145461 CAE312717 STL TO CLE - DURING CLIMB AT APPROXIMATELY 17,000 FT WHILE ENTERING ICING CONDITIONS THE AIRCRAFT EXPERIENCED A BLEED NR 2 LEAK. THE QRH PROCEDURES WERE FOLLOWED AND THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE BLEED LEAK AND FOUND A BROKEN CLAMP AND SEPARATED MANIFOLD AT JOINT 8 IN THE FECU COMPARTMENT. AFTER RE PLACING THE O-RING, CLAMP AND RESECURING THE JOINT THE BLEED SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007122000107 20071220 00107 NM 2007 12 20 UPS07651306 1 20071214 A 2910 O-RING BOEING 767 76734AF 1385212 NM NR 9 SPOILER FAILED A IPXA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 01 331UP 27757 C HYD QTY EICAS MSG, TURNED INTO A C HYD FLUID TOTAL LOSS. CREW TURNED CENTER PUMPS OFF TO SEE IF FLUID WOULD STILL BE LOST. THE FLUID QTY CONTINUED TO GO DOWN. THIS STARTED ABOUT 75 MILES FROM SDF. FOUND NR 9 SPOILER FILTER PLUG O-RING BLOWN, SEE IPC 27-61-02 AS PER MM 27-91-02-4. REMOVED PLUG AND REPLACED O-RING AND TIGHTENED, LEAK CHECKS OK. RAN AL L FH. CONTROLS THROUGH SEVERAL TIMES. 2 L 7 2 4F RT A1NM 2007122000108 20071220 00108 WP 2007 12 20 UPS07851305 1 20071216 A 3350 LAMP DOUG DC8 DC871F 302199D WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 ONE EMERGENCY EXIT LIGHT IN COCKPIT INOP. RELAMPED COCKPIT DOME LIGHT IAW DC8 MM 33-50-02-2. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2007122100008 20071221 00008 NM 2007 12 21 ASAA0742373 1 20070922 A 5320 6517684638 INTERCOSTAL BOEING 737 7374Q8 138447Q NM BS 294 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 FWD SIDE OF L1 DOOR CUTOUT STR 12L BS 294 INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW PEMCO EA PD 37 53 9 87 AND ALASKA EA 5310 02747. 2 L 7 2 4F RT A16WE 2007122100009 20071221 00009 NM 2007 12 21 ASAA0742374 1 20070922 A 5320 6517684634 INTERCOSTAL BOEING 737 7374Q8 138447Q NM BS 294 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 FWD SIDE OF L1 DOOR CUTOUT STR 16L BS 294 INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW BAC DWG 65 17684 PE MCO EA PD 37 53 987 AND ALASKA EA 5310 02747. 2 L 7 2 4F RT A16WE 2007122100010 20071221 00010 NM 2007 12 21 ASAA0742375 1 20071004 A 5320 66142083 WEB BOEING 737 7374Q8 138447Q NM BS 294 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 FWD MAIN CABIN STA 294 STG 11L WEB CRACKED. REMOVED AND REPLACED INTERCOSTAL WEB IAW BAC DWG 65 17684 PEMCO EA PD 37 53 987 AND ALASKA EA 5310 02747. 2 L 7 2 4F RT A16WE 2007122100013 20071221 00013 SO 2007 12 21 FDKA200708422 1 20070825 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 FDM 6184 JFK. LEFT ROW 12 EMERGENCY LOCATOR SIGN INOP. MX RESECURED LIGHT CONNECTOR, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007122100016 20071221 00016 SO 2007 12 21 FDKA200710279 1 20071027 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 FDM 6011 JFK (1005 PHX LCL). SEAT 12A EMERGENCY EXIT LIGHT INOP. MX RESET THE EMERGENCY LIGHTS, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007122100017 20071221 00017 SO 2007 12 21 FDKA200711305 1 20071102 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 FRL RON CAE (0330 PHX LCL). LEFT WING EMERGENCY EXIT SIGN INOP. RESET, OPS GOOD. 2 L 7 2 4T RT T00011AT 2007122100022 20071221 00022 SO 2007 12 21 FDKA200708428 1 20070828 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 10760 145214 FDM RON MCO (0444 PHX LCL). EMERGENCY EXIT FLOOR LIGHTING NR 2 & 3 INOP. MX REPLACED NR 2 BATTERY AND CHARGER. OPS CH ECK GOOD. 2 L 7 2 4T RT T00011AT 2007122100026 20071221 00026 SO 2007 12 21 FDKA200709460 1 20070910 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM FLT 6124 JFK. TWO EMERGENCY FORWARD LIGHT STRIPS INOP. MX RESET EMERGENCY LIGHTING SYSTEM, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007122100030 20071221 00030 SO 2007 12 21 FDKA200711339 1 20071119 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6082 ATL (0516 PHX LCL). SERVICE DOOR EMERGENCY LIGHT INOP. MX RE-SECURED CONNECTOR ON LIGHT ASSY, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007122100031 20071221 00031 NM 2007 12 21 ZZDA2007310 1 20071207 A 5347 SEAT TRACK BOEING 717 717200 1383700 NM COCKPIT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 947AT 55010 FIRST OFFICER'S I/B SEAT TRACK CORRODED BEYOND LIMITS. REPLACED SEAT TRACK, FABRICATED FROM RAW STOCK. 2 L 7 2 4F TR A6WE 2007122100033 20071221 00033 NM 2007 12 21 ZZDA2007312 1 20071101 A 5330 SKIN BOEING 717 717200 1383700 NM STA 160 L24-25R DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 947AT 55010 FOUND DENT ON A/C 708 RIGHT SIDE FUSELAGE AT STATION 160 BETWEEN L24 AND L25 DENT MEASURED .141 X 1.5 X 1.4. INSTALLED DOUBLER REPAIR AND FILLER AT RT SIDE FUSELAGE AT STA 160 BETWEEN L24 AND L25. 2 L 7 2 4F TR A6WE 2007122100035 20071221 00035 WP 2007 12 21 ABXA070410 1 20071020 A 5347 SEAT TRACK DOUG DC9 DC941 302207N WP BS 996-1021 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 SEAT TRACK CORRODED AT LEFT BUTT LINE 9.88, STATION 996-1021. REMOVED AND REPLACED TRACK IN ACCORDANCE WITH DC9 SRM 51- 30-5 AND 51-30-1. 2 L 7 2 4F A6WE 2007122100037 20071221 00037 WP 2007 12 21 ABXA070412 1 20071022 A 5755 3957149503 BRACKET DOUG DC9 DC941 302207N WP SPOILER CONTROL CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 SPOILER CONTROL TORQUE TUBE BRACKET CORRODED. REMOVED AND REPLACED SPOILER TORQUE TUBE BRACKET IN ACCORDANCE WITH DC9 M AINTENANCE MANUAL 20-16-00-2-0001. 2 L 7 2 4F A6WE 2007122100040 20071221 00040 WP 2007 12 21 ABXA070416 1 20071122 A 5315 992348487 FLOORBEAM DOUG DC9 DC941 302207N WP BS 180 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 FLOORBEAM CRACKED ON BOTH SIDES OF INTERCOSTAL AT STATION 180, LEFT BUTT LINE 20-23. REPAIRED FLOORBEAM IN ACCORDANCE W ITH DC9 SRM. 2 L 7 2 4F A6WE 2007122100043 20071221 00043 WP 2007 12 21 ABXA070402 1 20071019 A 5340 991073749 SUPPORT ANGLE DOUG DC9 DC941 302207N WP MLG DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 LEFT MAIN LANDING GEAR DOOR ACTUATOR SUPPORT ANGLE CRACKED FORWARD SIDE. REMOVED AND REPLACED IN ACCORDANCE WITH DC9 SR M. 2 L 7 2 4F A6WE 2007122100047 20071221 00047 WP 2007 12 21 ABXA070419 1 20071114 A 5230 3914025502 ATTACH FITTING DOUG DC9 DC941 302207N WP AFT CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 AFT LOWER CARGO DOOR BEAM NR 2 AFT FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IN ACCORDANCE WITH DC9 SRM 51-30-5 . 2 L 7 2 4F A6WE 2007122100050 20071221 00050 NM 2007 12 21 ABXA070423 1 20071119 A 5320 284T0350 INTERCOSTAL BOEING 767 767281 1385109 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 792AX 23142 AFT CARGO COMPARTMENT RIGHT SIDE WALL INTERCOSTAL CRACKED. FABRICATED NEW INTERCOSTAL AND INSTALLED IN ACCORDANCE WITH B767 SRM 51-40-2. 2 L 7 2 4F RT A1NM 2007122100052 20071221 00052 WP 2007 12 21 ABXA070422 1 20071114 A 5230 3914025501 ATTACH FITTING DOUG DC9 DC941 302207N WP AFT CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 AFT LOWER CARGO DOOR BEAM NR 3 AFT FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IN ACCORDANCE WITH DC9 SRM 51-30-5 . 2 L 7 2 4F A6WE 2007122100053 20071221 00053 WP 2007 12 21 ABXA070418 1 20071113 A 5320 99101515 CUSP WEB DOUG DC9 DC941 302207N WP BS 636-655 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 LEFT CUSP WEB CRACKED TWO (2) PLACES BETWEEN FS 636-655. REPAIRED CRACKS IN ACCORDANCE WITH DC9 SRM 53-01, FIGURE 2. 2 L 7 2 4F A6WE 2007122100055 20071221 00055 WP 2007 12 21 ABXA070415 1 20071109 A 5330 59114065 SKIN DOUG DC9 DC941 302207N WP PAX DOOR CUTOUT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 MAIN ENTRY DOOR CUTOUT UPPER AFT CORNER WAS DAMAGED AND CRACKED. REPAIRED UPPER AFT CORNER IN ACCORDANCE WITH DC9 SRM 5 3-05, FIGURE 114 AND 117. 2 L 7 2 4F A6WE 2007122100056 20071221 00056 WP 2007 12 21 ABXA070408 1 20071020 A 5313 S27779225 LONGERON DOUG DC9 DC941 302207N WP BS 1041 L16R CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 LONGERON 16 RIGHT CRACKED AT UPPER FRAME ATTACH HOLE AT STATION 1041. REMOVED AND REPLACED SECTION IN ACCORDANCE WITH D C9 SRM 53-02. 2 L 7 2 4F A6WE 2007122100057 20071221 00057 WP 2007 12 21 ABXA070409 1 20071020 A 5313 S27779225 LONGERON DOUG DC9 DC941 302207N WP BS 1041-1056 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 LONGERON 17 LEFT CRACKED AT FRAME ATTACH POINTS AT STATION 1041 AND 1056. REMOVED AND REPLACED LONGERON SECTION IN ACCO RDANCE WITH DC9 SRM. 2 L 7 2 4F A6WE 2007122100058 20071221 00058 WP 2007 12 21 ABXA070401 1 20071019 A 5311 5911448503 FRAME DOUG DC9 DC941 302207N WP BS 598 L30 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 FORWARD LOWER CARGO AFT SIDE AND LOWER LEG OF FRAME CORRODED FS 598 AT LONGERON 30. BLENDED AREA IN ACCORDANCE WITH DC9 SRM. 2 L 7 2 4F A6WE 2007122100059 20071221 00059 SO 2007 12 21 C2XA07TY079 1 20071207 A 3350 BA50933901 CHARGER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 26545 145558 BOTH AFT OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGER IAW EMB 145 MM 33-50 -04. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007122100060 20071221 00060 NM 2007 12 21 SWAA076149 1 20071211 A 3350 3071BPEGPL LAMP BOEING 737 737705 13844SC NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 271LV 29090 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 20 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007122100061 20071221 00061 NM 2007 12 21 SWAA076150 1 20071211 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 294WN 32540 EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2007122100062 20071221 00062 NM 2007 12 21 SWAA076151 1 20071211 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727C S22R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 22R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007122100063 20071221 00063 NM 2007 12 21 SWAA076152 1 20071211 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727E S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 2007122100064 20071221 00064 NM 2007 12 21 SWAA076153 1 20071211 A 5311 66546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122100067 20071221 00067 NM 2007 12 21 SWAA076155 1 20071211 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM BS 503D S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007122100068 20071221 00068 NM 2007 12 21 SWAA076178 1 20071211 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM BS 374 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 374, S4L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007122100069 20071221 00069 NM 2007 12 21 SWAA076156 1 20071211 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM ROW 5 DEF INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 404WN 27892 EEPLS INOP AT ROW 5 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007122100070 20071221 00070 NM 2007 12 21 SWAA076157 1 20071211 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 487WN 33854 EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007122100073 20071221 00073 NM 2007 12 21 SWAA076159 1 20071211 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122100075 20071221 00075 NM 2007 12 21 SWAA076171 1 20071211 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 338 S20L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 338, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007122100077 20071221 00077 NM 2007 12 21 SWAA076169 1 20071211 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 318 S20L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 318, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007122100079 20071221 00079 NM 2007 12 21 SWAA076162 1 20071211 A 3350 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007122100080 20071221 00080 2007 12 21 SWAA076172 4 20071211 A 2565 D31354 SLIDE BOEING 737 7373L9 1384470 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007122100081 20071221 00081 NM 2007 12 21 SWAA076163 1 20071211 A 3350 MS155721 LAMP BOEING 737 7373G7 1384595 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007122100082 20071221 00082 NM 2007 12 21 SWAA076165 1 20071211 A 5311 6546558 FRAME BOEING 737 7373TO 138447G NM BS 907 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122100083 20071221 00083 NM 2007 12 21 SWAA076173 1 20071211 A 5340 65C27314 STRINGER CLIP BOEING 737 7373TO 138447G NM BS 360 S5L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007122100085 20071221 00085 NM 2007 12 21 SWAA076175 1 20071211 A 5340 65C27314 STRINGER CLIP BOEING 737 7373TO 138447G NM BS 887 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007122100086 20071221 00086 NM 2007 12 21 SWAA076176 1 20071211 A 5340 65C27314 STRINGER CLIP BOEING 737 7373TO 138447G NM BS 907 S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007122100087 20071221 00087 NM 2007 12 21 SWAA076177 1 20071211 A 5330 6545776 SKIN BOEING 737 7373TO 138447G NM BS 931 S22R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 931, STR 22R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007122100088 20071221 00088 NM 2007 12 21 SWAA076164 1 20071211 A 5340 65C27314 STRINGER CLIP BOEING 737 7373TO 138447G NM BS 400 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007122100089 20071221 00089 NM 2007 12 21 SWAA076166 1 20071211 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 760SW 27874 DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007122100093 20071221 00093 NM 2007 12 21 CALA0700732 1 20071205 A 5730 114N2106 SKIN BOEING 757 757224 1384958 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12114 27556 LEFT WING FIXED L/E TOP SURFACE CRACKED BW WSS380 TO WSS420. REPAIR PER EA 5731-01010 OP 4 AND SRM 51-70-07. 2 L 7 2 4F RT A2NM 2007122100094 20071221 00094 NM 2007 12 21 CALA0700733 1 20071208 A 5311 6546551 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 FUSELAGE FRAME CRACKED AROUND RIVET ABOVE S-9L. REPAIRED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2007122100095 20071221 00095 NM 2007 12 21 CALA0700734 1 20071208 A 5311 65C25230 FRAME BOEING 737 7373T0 1384582 NM BS 727E S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 STA 727E FUSELAGE FRAME CRACKED AROUND RIVET ABV S-9L. REPAIRED PER EA5310-04498. 2 L 7 2 4F RT A16WE 2007122100096 20071221 00096 NM 2007 12 21 CALA0700735 1 20071208 A 5311 6546555 FRAME BOEING 737 7373T0 1384582 NM BS 867 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 STA 867 FUSELAGE FRAME CRACKED AROUND RIVET ABOVE S-9L. REPAIRED FUSELAGE FRAME STA 867 ABOVE S-9L PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2007122100097 20071221 00097 NM 2007 12 21 CALA0700736 1 20071208 A 5311 6546549 FRAME BOEING 737 7373T0 1384582 NM BS 767 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 STATION 767 FUSELAGE FRAME CRACKED AROUND RIVET ABOVE S-9L. REPAIRED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2007122100099 20071221 00099 NM 2007 12 21 CALA0700738 1 20071208 A 5311 6546558 FRAME BOEING 737 7373T0 1384582 NM BS 907 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 FRAME CRACKED STA 907 BETWEEN S8L AND S9L. REPAIRED PER ECRA 5310-04498. 2 L 7 2 4F RT A16WE 2007122100100 20071221 00100 NM 2007 12 21 200712121 1 20071210 A 3250 17073205903 ELEMENT EMB ERJ170 ERJ170100SE 3260406 NM NLG FEEDBACK DIRTY A UHLA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 11 650RW 17000104 FLIGHT 7665 ATL TO ORD. ON FINAL APPROACH WHEN THE GEAR WAS LOWERED THE CREW RECEIVED AN EICAS CAUTION MESSAGE STEER FA IL. CREW EXECUTED A GO-AROUND, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND INSPECTED TH E FEEDBACK SENSOR. 2 L 7 2 4F RT A56NM 2007122100103 20071221 00103 SO 2007 12 21 C2XA07RI102 1 20071207 A 5210 STRUCTURE EMB 145 EMB145LR 3260212 SO DOOR HANDLE BOX LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13994 145291 FLT 2289 - EWR - CREW REPORTED DOOR DIFFICULT TO OPEN AND CLOSE. EWR MX RE-SECURED HANDLE BOX BOLTS AND APPLIED LUBE TO DOOR SEAL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2007122100105 20071221 00105 SO 2007 12 21 C2XA07RI104 1 20071208 A 3397 WIRE EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHTS CHAFED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14943 145040 FLT 2616 - RIC - CREW REPORTED PAX DETECTED ELECTRIC TYPE OF SMOKE. RIC MX FOUND ELECTRIC EMERGENCY SIGN AT ROW 3BC WIT H BARE WIRE EXPOSED. MX REPAIRED WIRE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SER VICE. 2 L 7 2 4F RT T00011AT 2007122100108 20071221 00108 NM 2007 12 21 CALA0700739 1 20071208 A 5311 6546554 FRAME BOEING 737 7373T0 1384582 NM BS 847 S8-9 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 FRAME CRACKED AT STA 847 BETWEEN STR 8 & 9. REPAIRED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2007122100109 20071221 00109 NM 2007 12 21 CALA0700740 1 20071208 A 5311 6546552 FRAME BOEING 737 7373T0 1384582 NM BS 827 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 FUSELAGE FRAME CRACKED AT STA 827 AROUND RIVET ABOVE S-9L. REPAIRED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2007122100111 20071221 00111 NM 2007 12 21 CALA0700742 1 20071211 A 5330 6545774 SKIN BOEING 737 7373T0 1384582 NM BS 747-767 S19R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59302 23353 ON WALK AROUND FOUND 2 INCH CRACK IN FUSELAGE SKIN BETWEEN RT SIDE BETWEEN STA 747 AND 767 ON STR 19R. REPAIRED PER SRM 53-00-01 REPAIR 31 DETAIL 10. 2 L 7 2 4F RT A16WE 2007122100112 20071221 00112 NM 2007 12 21 CALA0700743 1 20071212 A 5230 PAN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 C2 DOOR FWD SIDE PAN, UPPER AND LOWER HALVES CRACKED AT SPLICE. INSTALLED NEW PANS ON DOOR ASSY. 2 L 7 2 4F RT A16WE 2007122100113 20071221 00113 NM 2007 12 21 CALA0700744 1 20071212 A 5322 0567075O SHEAR TIE BOEING 737 7373T0 1384582 NM BS 500D S28L CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 FBB BELT FRAME HAS CORROSION STA 500D AT S28L. REWORKED AND REPLACES SHEAR TIE REF SRM 53-00-01 & 51-40-02. 2 L 7 2 4F RT A16WE 2007122100114 20071221 00114 NM 2007 12 21 CALA0700745 1 20071213 A 5320 WEB BOEING 737 7373T0 1384582 NM BS 787 S27R CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 ABB WEB CORRODED AT STA 787 STR 27R. REMOVED AND REPLACED WEB REF SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007122100120 20071221 00120 WP 2007 12 21 ABXA070425 1 20071211 A 3350 60030451 BATTERY PACK DOUG DC9 DC932F 3022067 WP EMERGENCY LIGHTS DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 1010 47040 EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY PACK IAW DC9 AMM CHAPTER 33. 2 L 7 2 4F A6WE 2007122100121 20071221 00121 WP 2007 12 21 ABXA070426 1 20071211 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP EMERGENCY LIGHTS DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 EMERGENCY LIGHTING WOULD NOT TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00-8. 2 L 7 2 4F A6WE 2007122100122 20071221 00122 NM 2007 12 21 SWAA076181 1 20071213 A 3350 6556633 LIGHT BOEING 737 7377H4 1384404 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 210WN 34162 DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007122100123 20071221 00123 NM 2007 12 21 SWAA076182 1 20071213 A 2560 P4010021 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 261WN 32517 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2007122100124 20071221 00124 NM 2007 12 21 SWAA076197 1 20071213 A 5311 6546592 FRAME BOEING 737 7373H4 1384600 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD FITTING CHORD CORRODED AT BS 1016, RBL 29. REPAIRED CHORD PER ER. 2 L 7 2 4F RT A16WE 2007122100125 20071221 00125 NM 2007 12 21 SWAA076198 1 20071213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 706 S11L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007122100130 20071221 00130 NM 2007 12 21 SWAA076183 1 20071213 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 500C-500D CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 500C AND BS 500D, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007122100131 20071221 00131 NM 2007 12 21 SWAA076224 1 20071213 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 518D S12R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518D, STR 12R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007122100132 20071221 00132 NM 2007 12 21 SWAA076244 1 20071213 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 518D S12R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518D, STR 12R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007122100135 20071221 00135 NM 2007 12 21 SWAA076240 1 20071213 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 423WN 29827 DURING SCHEDULED MV3 CHECK, FOUND EEPLS INOP AT ROW 3 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007122100137 20071221 00137 NM 2007 12 21 SWAA076227 1 20071213 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 452WN 29846 DURING SCHEDULED HC2 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007122100139 20071221 00139 NM 2007 12 21 SWAA076228 1 20071213 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 483WN 32472 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2007122100140 20071221 00140 NM 2007 12 21 SWAA076186 1 20071213 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 487WN 33854 EEPLS COVER MISSING AT ROW 3 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007122700001 20071227 00001 EU 2007 12 27 USAA920071322 1 20071212 A 3397 CONNECTOR AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 657AW 1083 FLT 158 - PHX - STL - EEL - FAA RAMP CHECK, ROW 9 DEF EMERGENCY LIGHT INOP. MAINTENANCE RECONNECTED EMERGENCY LIGHT CON NECTOR 5157VC AT ROW 9DEF. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT A28NM 2007122700003 20071227 00003 NM 2007 12 27 USAA920071323 1 20071210 A 5320 65516983 CHANNEL BOEING 737 7373Y0 1384671 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - CORROSION ON CHANNEL, BS 907, S26L. REPLACED CHANNEL, BS 907, S26L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007121900026 20071219 00026 NM 2007 12 19 2007UALA05018 1 20071208 A 3510 MC1025154 OXYGEN MASK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 FO'S O2 MASK MIC DOES NOT WORK. SUSPECT DAMAGE DUE TO PRE FLIGHT CHECKS. REPLACED ASSEMBLY, CHECKS OK. AC OK FOR SERVICE . 2 L 7 2 4F 4 F RT A16WE E2GL 2007121900032 20071219 00032 EU 2007 12 19 1218342121707 1 20070927 A 5753 S5751565000000 FITTING AEROSP ATR42 ATR42320 8680930 EU TE FLAP CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 14834 193 RIGHT INBOARD FLAP, FLAP ARM AND FLAP BEAM CORRODED AT FLAP RIB 5. RIGHT INBOARD FLAP BEAM, FLAP, FLAP ARM REPLACED AT RIB 5. 2 H 7 2 4T RT A53EU 2007121900052 20071219 00052 EU 2007 12 19 NWAA074053216 1 20071216 A 5320 BUTTSTRAP AIRBUS 320 A320211 3930320 EU FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 316US 192 DURING "M" CHECK, FOUND CORROSION ON BUTT STRAP AT FR 64 BETWEEN S43R-S44R. REPAIRED PER EA 32-211424. 2 L 7 2 4F RT A28NM 2007121900055 20071219 00055 NM 2007 12 19 NWAA074086307 1 20071203 A 5320 INTERCOSTAL BOEING 747 747451 1384940 NM BS 1940 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 667US 24222 DURING "M" CHECK, FOUND CORROSION IN BULK CARGO SIDEWALL PANEL INTERCOSTAL AT BS 1940. REPAIRED PER EA 63-211343. 2 L 7 4 4F RT A20WE 2007121900067 20071219 00067 WP 2007 12 19 IXXA07SMN271S 1 20071116 A 5550 ATTACH ANGLE DOUG DC8 DC873F 302199F WP STAB TO FUSELAGE CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE TO STABILIZER LEFT ATTACH ANGLE SHOWS CORROSION AT STATION 1754.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGES AREA. FABRICATED ANGLE. PERFORMED HEAT TREATMENT TO ANGLE. CLEANED, TREATED AND PRIMED AREA, AND REPAIR PARTS. INSTALLED REPAIR PARTS SRM IAW 51-1-20D, 51-3-1 DC8 SRM 53-2-5 FIGU RE 16A SHEET 1-2, DC8 SRM 51-1-8 PAGE 17-18, DC8 SRM 53-2-0 PAGE 2P, DC8 SRM 53-2-5 FIGURE 16A SHEET 1-2, DC8 SRM 51-1-6 , DC8 SRM AND SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2007121900083 20071219 00083 SO 2007 12 19 SIMA200734801 1 20071213 A 3233 211010040 ACTUATOR EMB 135 EMB135KL 3260302 SO NLG MALFUNCTIONED A SIMA O OTHER E VIBRATION/BUFFET AP APPROACH 1 SW 21 831AE 145616 IN FLT VIBRATION WENT AWAY WHEN GEAR SELECTED DOWN. REMOVED AND REPLACED LT DOOR (NOSE) ACTUATOR IAW EMB 140 AMM 32-3 3-03. ALSO PERFORMED LANDING GEAR EXTENSION AND RETRACTION IAW EMB 140 AMM 32-32-00. OPS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT T00011AT 2007121900084 20071219 00084 SO 2007 12 19 SIMA200734802 1 20071212 A 2720 15H0048PH SWITCH EMB 145 EMB145LR 3260212 SO RUDDER PRESSURE FAILED A SIMA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 690AE 14500858 RUDDER SYS 1 AND 2 INOP DURING FLIGHT. REMOVED AND REPLACED NUMBER 2 RUDDER PRESSURE SWITCH IAW EMB 145 AMM 27-23-04. OPS CHECK GOOD IAW EMB 145 AMM 27-23-00, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007121900093 20071219 00093 WP 2007 12 19 IXXA07SMN261S 1 20071115 A 5340 FITTING DOUG DC8 DC873F 302199F WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND AFT BELLY PIT CRACKED FITTING AT STATION 1230.000 LONGERON-32 RIGHT. REMOVED C RACKED FITTING. FABRICATED FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION NOTED. CLEANED, TREATED AND PRI MED AREA AND FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, ATI REPAIR SPECIFICATION NUMBER 2003-05 DRAWING DOUGL AS NUMBER 4758514, DC8 NDT SPM PART 08-00-02 TO 07, FORM SEMAN 242-4,DC8 SRM 51-1-8B, AND 51-3-1. 2 L 7 4 4F RT 4A25 2007121900103 20071219 00103 NM 2007 12 19 AALA20072421 1 20071211 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 668AA 25333 MIA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007121900111 20071219 00111 WP 2007 12 19 07FDEA05048 1 20071213 A 5320 AGA7081509 SUPPORT DOUG DC10 DC1030F 3023504 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 308FE 48297 AFTER REMOVAL CEILING PANELS WITH J/C "2552C180-3JR" AFT CARGO COMPT BELOW CHANNEL SUPPORT FLOOR FOUND SEVERE EXFOLIAT ION CORROSION. REPAIRED AREA IAW SRM 53-70-00 FIG 13 VOL I. 2 L 7 3 4F RT A22WE 2007121900118 20071219 00118 NM 2007 12 19 2007UALA05039 1 20071209 A 2560 D71701100 BATTERY BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FLASHLIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 795UA 26927 FOUND EMERGENCY FLASH LIGHT USED AT DOOR 3R. REPLACED BATTERY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121900153 20071219 00153 WP 2007 12 19 IXXA07SMN247S 1 20071115 A 5230 SKIN DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD CARGO COMPARTMENT "B" DOOR OUTER SKIN HAS A CRACK, WEAR DAMAGE, AND SEV ERAL DENTS AT STATION 480.000 TO STATION 560.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA, AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IA W BOEING MESSAGE NUMBER 1-674365491-2 DATED 11-07-07, DC8 SRM 52-1-0 PAGE 1 AND SRM 51-1-21,SRM 52-4-1 FIGURE 3 ITEM "K" , DC8 SRM 51-1-8B, AND DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007121900158 20071219 00158 NM 2007 12 19 QXEA200701771 1 20071201 A 3310 MS327 LAMP DHAV DHC8 DHC8202 2809007 NM HEATER INOPERATIVE A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 355PH 500 PDX - FLIGHT 2011 - HEATER LIGHT ON LEFT ENGINE INTAKE BYPASS DOOR DOES NOT TEST. RETURNED TO THE GATE. MAINTENANCE RE PLACED THE LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007121900175 20071219 00175 EA 2007 12 19 SWIA200718937 1 20071208 A 3340 BEACON CNDAIR CL600 CL6002B19 1900309 EA SHORTED A SWIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 416SW 7089 FLT 3948 - ELECTRICAL ARCING IN CEILING AREA ABOVE ROW 3. REPLACED UPPER BEACON IAW MM 33-41-00. OPS CHECKED GOOD, P/N 2LA002760-70, S/N OFF 361847. 2 L 7 2 4F RT A21EA 2007121900181 20071219 00181 EA 2007 12 19 TRAX200701896 1 20071210 A 5753 BRACKET CNDAIR CL600 CL6002B19 1900309 EA TE FLAP BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 903EV 7621 RT O/B FLAP, O/B HINGE ARM CENTER BRACKET FOR ATTACHING FLAP FAIRING 697BB, I/B END IS BROKEN OFF. REMOVED CRACKED BRAC KET FOR FLAP FAIRING DUPILCATED PART & TOPCOATED. INSTALLED PART IAW CRJ SRM 51-42-13. 2 L 7 2 4F RT A21EA 2007121900186 20071219 00186 NM 2007 12 19 2007UALA05022 1 20071209 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 FOUND WALL EEL INOP FWD WALL OF MID GALLEY. REPLACED FEEDER WIRE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121900188 20071219 00188 NM 2007 12 19 2007UALA05024 1 20071210 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 'E' ZONE RT FWD EEL'S DO NOT REMAIN ON. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007122000001 20071220 00001 NM 2007 12 20 QXEA200701916 1 20071215 A 7710 30005000056 TSCU DHAV DHC8 DHC8202 2809007 NM NR 2 ENGINE MALFUNCTIONED A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 09 379PH 18281 454 530 OTH - FLIGHT 2031 - DURING TAKEOFF ROLL (AT VR), HEARD A SOUND WHICH SOUNDED LIKE A TORQUE SURGE OR PROP SPEED PROBLEM. NO ABNORMAL PROBLEMS NOTICED ON GAUGES, NO CAUTION LIGHTS, NO YAW NOTICED. ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE RAN BOTH ENGINES WITH NO DEFECTS NOTED. FDR DOWNLOAD SHOWS THAT NR 2 ENGINE TORQUE REACHED 136.5 FOR LESS T HEN 20 SECONDS IAW PRATT AND WHITNEY MANUAL 05-20-00 PAGE 5 NO MAINTENANCE REQUIRED. NR 2 PROP REQUIRES REPLACEMENT WIT HIN 10 FERRY FLIGHT HOURS IAW HAMILTON SUNDSTRAND MANUAL 61-10-00 PAGE 513. CAUSE OF OVER TORQUE REQUIRES FURTHER TROUB LESHOOTING. AIRCRAFT FERRIED TO PDX FOR REPAIRS. IN PDX, REPLACED NR 2 TORQUE PROBE AND TSCU. OPERATIONAL CHECKS GOOD 2 H 7 2 4T RT A13NM 2007122000004 20071220 00004 EA 2007 12 20 QXEA200701915 1 20071215 A 5240 DOOR CNDAIR CL600 CL6002C10 1390015 EA AC POWER OPEN A QXEA O OTHER E VIBRATION/BUFFET CL CLIMB 1 NM 09 612QX 10042 PDX - FLIGHT 2586 - LOUD NOISE HEARD FROM LOWER FLIGHT DECK AREA JUST AFTER TAKEOFF ON RIGHT SIDE. MAINTENANCE FOUND TH E A/C POWER DOOR LEFT OPEN. INSPECTED DOOR AND FOUND NO DEFECTS AND CLOSED DOOR. CHECKS GOOD. AIRCRAFT RETURNED TO SER VICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007122000016 20071220 00016 NM 2007 12 20 2007UALA02275 1 20070627 A 7830 STRUCTURE BOEING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE THRUST REVERSER DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 000354 24193 NR 1 ENGINE INBOARD REVERSER IS DELAMINATED. RIGHT REVERSER CENTER CORE INNER AREA WAS FOUND DELAMINATED. REVERSER WAS REPAIRED. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122000020 20071220 00020 NM 2007 12 20 2007UALA05068 1 20071211 A 3397 WIRE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 913UA 25291 EXIT SIGN WITH TWO ARROWS AT CENTER OF CABIN IS INOP. REPAIRED BROKEN WIRE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122000021 20071220 00021 WP 2007 12 20 IXXA07SMN272S 1 20071116 A 5740 5770409501 SUPPORT DOUG DC8 DC873F 302199F WP ZONE 500 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE INTERNAL PART SUPPORT HAS A CRACK AT STATION XFS 430.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SUPPORT. CLEANED, TREATED AND PRIMED AREA INS TALLED NEW SUPPORT IAW BOEING MESSAGE NUMBER1-680003043-2 DATED 11-12-07, DRAWING NUMBER 5770409, DC8 SRM 57-1-0 PAGE 1, SRM 51-3-0, 51-1-20D, DC8 SRM 51-1-8B, DC8 SRM 57-2-1 FIGURE 12 SHEET 1,2,3, 51-3-0, 51-9-0 T/R NUMBER 51-108, 51-9-0 T /R NUMBER 51-126, AND SRM 51-3-1. 2 L 7 4 4F RT 4A25 2007122000023 20071220 00023 NM 2007 12 20 2007UALA05069 1 20071212 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 171UA 24322 UPPER DECK EMERGENCY EXIT SIGN INOP BETWEEN DOORS CEILING AFT SIGN. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007122000026 20071220 00026 NE 2007 12 20 2007UALA05072 2 20071212 A 7230 COMPRESSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE STALLED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 29 423UA 504 V10928 NR 2 ENGINE COMPRESSOR STALL REPORTED. IFSD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007122000034 20071220 00034 2007 12 20 UPS07151310 4 20071217 A 2565 WARNING LIGHT AIRBUS A300 A300F4622R 3930360 EU DOOR SLIDE INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 170UP 0005 SLIDE ARMED WARNING LIGHT ON ENTRY DOOR DOES NOT ILLUMINATE WHEN TESTED. DEFERRED LIGHT ASSY PER MEL 52-73-01-1. OK TO C ONTINUE. REF AMM A300 52-10-11-05 ADJ/TEST RECONNECTED FWD ENTRY DOOR SLIDE ARM CONTROL BOX. OPS CHKS OF FWD ENTRY DOO R ARM CONTROL NORMAL OK FOR SERVICE. THIS CLEARS M364950 PLACARD REMOVED. 2 L 7 2 4F RT A35EU 2007122000036 20071220 00036 WP 2007 12 20 UPS07851307 1 20071218 A 5610 ACCESS PANEL DOUG DC8 DC871F 302199D WP DISLODGED A IPXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 718UP 46018 AFTER T/O LOUD NOISE COMING FROM LEFT FORWARD WINDOW AREA. NOISE WAS SO LOUD DIFFICULT TO COMMUNICATE IN COCKPIT. PRES SURE HELD IN COCKPIT UP TO 11,000 FT FOUND CAPTS CLEARVIEW WINDOW EMERGENCY ACCESS PANEL POPPED IN. RESET CAPTS WINDOW EMERGENCY ACCESS PANEL IAW MM 56-10-03-6. OP CHECK GOOD ON CAPTS CLEARVIEW WINDOW. 2 L 7 4 4F RT 4A25 2007122000044 20071220 00044 NM 2007 12 20 UPS07M51282 1 20071104 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1911-1964 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C AFT CABIN, CORROSION ON SEAT TRACK CROWN AT STA1911 AND STA1964 X=107. DAMAGED SEAT TRACK FOUND OUT O F LIMIT PER SRM 53-70-00 FIG 3 (ORG MAT'L: 0.145", REMVD: 0.090") AND REMOVED FROM STA1831 - 2007 X=107 PER SRM 51-31. - 01VIIR35. NEW SEAT TRACK FASTENER HOLES PICKED UP AND INSTALLED PER SRM 51-31-01 VIIR35. NEW SEAT TRACK REWORKED AREA PAINTED PER SRM 51-21-0 1VIIR 35. 2 L 7 3 4F RT A22WE 2007122000047 20071220 00047 NM 2007 12 20 QXEA200701914 1 20071214 A 3610 8209076 SWITCH BOMBDR DHC8 DHC8402 1390042 NM NR 1 BLEED MALFUNCTIONED A QXEA O OTHER O OTHER AP APPROACH 1 NM 09 413QX 4060 YVR - FLIGHT 2276 - ON FINAL APPROACH (6 MILES OUT), THE NR 1 BLEED HOT CAUTION LIGHT CAME ON. RAN THE CHECKLIST AND IT STAYED ON THROUGH THE APPROACH LANDING AND TOUCHDOWN. MAINTENANCE REPLACED THE NR 1 BLEED OVERTEMP SWITCH. OPERATIONA L CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007122000056 20071220 00056 NM 2007 12 20 2007UALA03682 1 20070910 A 2722 ACTUATOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE RUDDER OUT OF ADJUST A UALA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 929UA 26652 IN MANUAL REVERSION THE AIRCRAFT ROLLS LEFT REQUIRING HARD RIGHT YOKE JO MAINTAIN LEVEL. STANDBY RUDDER ACTUATOR OUT OF ADJUSTMENT (A/C FLOWN IN MANUAL REVERSION DUE TO FLIGHT CONTROL WORK ACCOMPLISHED AT HMV). DURING ATTEMPT AT LEVEL FLI GHT IN MANUAL REVERSION, PILOTS HAD TO APPLY 3.5 UNITS RUDDER TO DO SO. STANDBY RUDDER ACTUATOR WAS NOT ABLE TO BE ADJU STED. REPLACED AND ALSO RE-RIGGED AILERON CABLES. FOLLOWING TEST FLIGHT WAS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122000063 20071220 00063 2007 12 20 SWIA200718950 4 20071205 A 2350 6229852106 TUNING UNIT CNDAIR CL600 CL6002B19 1900309 EA RADIO SMOKE A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 454SW 14377 14377 7749 FLT 3981 - JUST AFTER LIFTOFF, SMOKE APPEARED IN THE COCKPIT. INSPECTED CENTER PEDESTAL WITH NO EVIDENCE OF DAMAGED WIR ES. INSPECTED ALL ELECTRICAL COMPONENTS AND RELAY CONTACTORS IN AVIONICS BAY WITH NO DISCREPANCIES NOTED. REPLACED NR 2 RTU FOR PRECAUTIONS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007122000070 20071220 00070 EA 2007 12 20 TRAX200701916 1 20071211 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 758EV 10210 ASD EXTERNAL HANDLE CRACKED. REMOVED AND REPLACED ASD EXTERNAL HANDLE. PERFORMED ASD HANDLE OPS CK IAW CRJ 700 AMM 52-1 1-03-701-801. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007122000088 20071220 00088 NM 2007 12 20 AALA20072448 1 20071214 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 751AN 30798 JFK - EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS INOPERATIVE. RESET EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS CABIN. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007122000094 20071220 00094 SO 2007 12 20 SIMA200734603 1 20071209 A 3010 APS71000 TRANSDUCER EMB 145 EMB145LR 3260212 SO ANTI ICE SYS MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 902BC 14500887 WING ANTI ICE FAIL ON CLIMB-OUT. ELECTED TO RETURN BACK TO ORD DUE TO WEATHER. REPLACED NUMBER 2 PRESS TRANSDUCER IAW EMB 145 MM 30-11-11. OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007122000110 20071220 00110 EU 2007 12 20 2007UALA04767 1 20071120 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 455UA 1105 FUSELAGE DAMAGE TO AFT FUSELAGE. FUSELAGE DAMAGED AT APPROX FRAME 57 BTWN STRINGERS 40-42 LT. SUPPLEMENTAL DATA UPDATE CAUSE: BELT LOADER CONTACTING LOWER SKIN UNDER FRAME 57. PERFORMED MAJOR REPAIR OF SKIN UNDER FRAME 57, BETWEEN STRIN GERS 40-42 LT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007122100002 20071221 00002 NM 2007 12 21 KPVA200724 1 20071208 A 3150 SMOKE WARNING DHAV DHC8 DHC8103 1386005 NM FALSE INDICATION A KPVA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 829EX 146 (PIREP) BAG SMOKE LIGHT IN FLIGHT. (MX) PERFORMED SMOKE DETECTION SYSTEM TEST IAW DHC-8 MM 26-12-00 PG 201. NO DEFECTS NOTED. SMOKE DETECTORS INSTALLED ARE NR 1) P/N 30-231-43 S/N 182 AND NR 2) P/N 473054 S/N 0285. BOTH DETECTORS HAVE T HE EMI/RFI COPPER SHIELDING TAPE AS PER DEHAVILLAND SB8-26-17. 2 H 7 2 4T RT A13NM 2007122100012 20071221 00012 SO 2007 12 21 FDKA200708421 1 20070824 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 FDM 6044 RIC. LEFT EMERGENCY DOOR LIGHT INOPERATIVE. MX RESECURED CONNECTOR AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2007122100018 20071221 00018 SO 2007 12 21 FDKA200711318 1 20071105 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO LT OVERWING INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 FDM 6038 CLT (1503 PHX LCL). LEFT OVERWING EMERGENCY INTERIOR LIGHT OUT. RESET EMERGENCY LIGHTING SYSTEM, OPS GOOD. 2 L 7 2 4T RT T00011AT 2007122100023 20071221 00023 SO 2007 12 21 FDKA200708431 1 20070829 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6122 MCO (0335 PHX LCL). EMERGENCY EXIT LIGHTING AT GALLEY DOOR WILL NOT COME ON. MX RESET. 2 L 7 2 4T RT T00011AT 2007122100024 20071221 00024 SO 2007 12 21 FDKA200708436 1 20070831 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 EMERGENCY FLOOR LIGHTING INOP IN 2 ADJACENT ROWS. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007122100025 20071221 00025 SO 2007 12 21 FDKA200709459 1 20070910 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM FLT 6175 JFK (0557 PHX LCL). FWD TWO EMERGENCY FLOOR STRIPS WILL NOT ILLUMINATE. MX RESET EMERGENCY LIGHTS, OPS CH ECK GOOD. 2 L 7 2 4T RT T00011AT 2007122100034 20071221 00034 SO 2007 12 21 C2XA07TY078 1 20071209 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO SERVICE DOORWAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12921 145354 SERVICE DOOR SILL CORRODED. REMOVED AND REPLACED SERVICE DOOR SILL IAW EMB 135/145 SRM 51-40-02, 51-20-03 & 51-40-06. ALODINED, PRIMED AND PAINTED IAW EMB CPM 51-21-04, 05, 06. AIRCRAFT STILL IN C-CHECK. 2 L 7 2 4T RT T00011AT 2007122100036 20071221 00036 WP 2007 12 21 ABXA070399 1 20071019 A 5755 99574657 ATTACH FITTING DOUG DC9 DC941 302207N WP LT WING SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 LEFT WING OUTBOARD SPOILER, OUTBOARD SPOILER ATTACH FITTING CRACKED. REMOVED AND REPLACED FITTING IN ACCORDANCE WITH DC 9 SRM. 2 L 7 2 4F A6WE 2007122100038 20071221 00038 WP 2007 12 21 ABXA070404 1 20071012 A 5520 5919752505 COUNTERBALANCE DOUG DC9 DC941 302207N WP RIGHT ELEVATOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 RIGHT ELEVATOR COUNTERBALANCE HEIGHT RUSTY IN SEVERAL AREAS. REPAIRED AREA IN ACCORDANCE WITH REA D955-56583. 2 L 7 2 4F A6WE 2007122100039 20071221 00039 WP 2007 12 21 ABXA070406 1 20071020 A 5320 2913044501 GUSSET DOUG DC9 DC941 302207N WP BS 206 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 FS 206.00, APPROXIMATE LONGERON 11 LEFT, GUSSET CRACKED. REMOVED AND REPLACED GUSSET IN ACCORDANCE WITH DC9 SRM. 2 L 7 2 4F A6WE 2007122100045 20071221 00045 WP 2007 12 21 ABXA070411 1 20071020 A 5315 9958186 FLOORBEAM DOUG DC9 DC941 302207N WP BS 1011 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 FLOORBEAM AT STATION 1011 LOWER FORWARD FLANGE CORRODED AT APPROXIMATELY RIGHT BUTT LINE 15 UNDER NUT PLATES. REPAIRED FLOORBEAM IN ACCORDANCE WITH DC9 SSRM K07411. 2 L 7 2 4F A6WE 2007122100048 20071221 00048 WP 2007 12 21 ABXA070417 1 20071122 A 5330 59248763 SKIN DOUG DC9 DC941 302207N WP BS 813 L29R CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 CORROSION ON SKIN FS 813 AT LONGERON 29 RIGHT TO LONGERON 28 LEFT. REPAIRED BLENDED AREA IN ACCORDANCE WITH DC9 SRM 53- 04, FIGURE 38. 2 L 7 2 4F A6WE 2007122100049 20071221 00049 WP 2007 12 21 ABXA070421 1 20071114 A 5230 59101573 SKIN DOUG DC9 DC941 302207N WP AFT CARGO DOOR GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 AFT LOWER CARGO DOOR SKIN WAS GOUGED FORWARD LOWER CORNER. REPLACED SKIN IN ACCORDANCE WITH DC9 SRM 51-10-4. 2 L 7 2 4F A6WE 2007122100054 20071221 00054 WP 2007 12 21 ABXA070413 1 20071029 A 5311 5911448503 FRAME DOUG DC9 DC941 302207N WP BS 579 L30 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 FORWARD LOWER CARGO FRAME AT STATION 579 WAS CORRODED AT LONGERON 30. REPAIRED FRAME IN ACCORDANCE WITH DC9 SRM 53-03. 2 L 7 2 4F A6WE 2007122100065 20071221 00065 NM 2007 12 21 SWAA076154 1 20071211 A 5311 66546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122100071 20071221 00071 NM 2007 12 21 SWAA076179 1 20071211 A 5312 6546568 BULKHEAD BOEING 737 7375H4 138449D NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, BETWEEN 10 O'CLOCK POSITION AND 3 O'CLO CK POSITION. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007122100072 20071221 00072 NM 2007 12 21 SWAA076158 1 20071211 A 3350 101114 LENS BOEING 737 7375H4 138449D NM EMERGENCY LIGHTS CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 RT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007122100074 20071221 00074 NM 2007 12 21 SWAA076170 1 20071211 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 328 S20L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007122100084 20071221 00084 NM 2007 12 21 SWAA076174 1 20071211 A 5340 65C27314 STRINGER CLIP BOEING 737 7373TO 138447G NM BS 706 S2L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007122100092 20071221 00092 NM 2007 12 21 USAA920071320 1 20071208 A 2700 UNKNOWN BOEING 737 7373B7 1384580 NM FLT CONTROLS MALFUNCTIONED A USAA O OTHER F FLT CONT AFFECTED CR CRUISE 1 EA 19 505AU 23380 FLT 1985 - BUF-CLT - UNCOMMANDED ROLL - AT FL 370 AUTO PILOT NR 1 KICKED OFF WITH AIRCRAFT ROLL LEFT AT 5 DEG. MANUALLY CONTROLLED A/C. ENG PARAMETERS NORMAL, YAW DAMPER NORMAL, RUDDER FREE AND CENTERED. TRIED BOTH AUTO PILOTS TO NO AVAIL . HAD CW/PITCH STEERING. AUTO PILOTS RESTORED AT 4000FT. SPEED BRAKE DID NOT APPEAR AS AUTHORITATIVE. MAINTENANCE AC TION PENDING. 2 L 7 2 4F RT A16WE 2007122100126 20071221 00126 NM 2007 12 21 SWAA076222 1 20071213 A 3350 MS155721 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007122700002 20071227 00002 NM 2007 12 27 USAA920071321 1 20071210 A 5311 654957411 FRAME SPLICE BOEING 737 7373Y0 1384671 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - CORROSION ON FRAME SPLICE ANGLE, BS 1016, S26R - S27R. REPLACED FRAME SPLICE ANGLE, BS 1016, S26R - S27R IAW B737 SRM 53-80-08-2R6. 2 L 7 2 4F RT A16WE 2007122700004 20071227 00004 NM 2007 12 27 SA07081 1 20071211 A 3260 664700500A4D INTERFACE UNIT AIRBUS A319 A319132 3930340 NM MLG FAILED A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 828AW 21987 9748 1552 PHX FLT 0132 EN ROUTE LAS TO PHX. ON TAKEOFF, WITH THE GEAR HANDLE SELECTED UP, A RED ECAM MESSAGE FOR GEAR UNSAFE, G EAR NOT DOWN WAS GENERATED. THE GEAR WAS RECYCLED AND THE MESSAGE CLEARED. THE FLIGHT CONTINUED WITHOUT FURTHER INCIDE NT. MAINTENANCE REPLACED LGCIU 1 AND 2. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2007122700006 20071227 00006 NM 2007 12 27 USAA920071136 1 20071024 A 5311 651630153 FRAME BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 188, RBL 28, WL 208. REPAIRED FRAME, BS 188, RBL 28, WL 208 IAW B737 SRM 53-00-07-2R11, FIGURE 201. 2 L 7 2 4F RT A16WE 2007122700008 20071227 00008 EA 2007 12 27 A6WA20070651 1 20071129 A 2410 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 2 UNDERSERVICED A A6WA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 31 438AW 7748 TAKEOFF ABORTED DUE TO RIGHT IDG CAUTION AND THEN RIGHT GENERATOR DROPPING OFF LINE. TAKEOFF ABORTED AT 70 KNOTS, MINIM AL BRAKING. BTMS BRAKE TEMPS READ 2-1-1-2. SERVICED IDG NR 2 IAW CRJ AMM 12-13-24. RAN ENGINE WITH OPS CHECK OF IDG N R 2. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007122700010 20071227 00010 EA 2007 12 27 A6WA200740643 1 20071202 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA COCKPIT SMOKE A A6WA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 447AW 7812 SMOKE AND ELECTRICAL FIRE ODOR COMING FROM F/O`S SIDE PANEL NEAR WINDSHIELD. FOUND FLOOD LIGHT ON F/O`S SIDE INOPERATIV E AND CIRCUIT BREAKER FOR FLOOD LIGHT POPPED. INSPECTED WIRE HARNESS, NO DEFECTS NOTED. (M) 2 L 7 2 4F RT A21EA 2007122700013 20071227 00013 EA 2007 12 27 A6WA200740645 1 20071114 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA ODOR A A6WA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 31 434AW 7322 NOTICED A STRONG FUEL ODOR FROM EWR, CONTINUED TO DETECT A FUEL OR EXHAUST ODOR DURING CLIMB. DIVERTED TO PHL. NO SMOK E, HOWEVER FLIGHT ATTENDANT AND PASSENGER NOTICED ODOR. REMOVED AND REPLACED APU INLET BELLOWS ASSEMBLY IAW AMM 49-10-0 0, OPS CHECK GOOD. NO EVIDENCE OF FORWARD FUEL ODOR. (M) 2 L 7 2 4F RT A21EA 2007122700015 20071227 00015 EA 2007 12 27 A6WA200740653 1 20071130 A 5242 HANDLE CNDAIR CL600 CL6002B19 1900309 EA E/E BAY DOOR DISLODGED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 418AW 7618 AFTER ROTATION AVIONICS BAY CAUTION MESSAGE CAME ON, RAN QRH AND RETURNED TO ORF. CREW FOUND HANDLE OUT, RESTOWED HANDL E. AVIONICS BAY DOOR INDICATION GREEN AS PER AMM 52-40-00. (M) 2 L 7 2 4F RT A21EA 2007122700018 20071227 00018 EA 2007 12 27 A6WA200740637 1 20071119 A 3220 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA NOSE ICED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 444ZW 7788 ON GEAR RETRACTION AFTER TAKEOFF, GEAR DISAGREE WARNING AND NLG DOOR OPEN WARNING, COMPLIED WITH QRH. IN ICING AFTER TA KEOFF FROM CONTAMINATED RUNWAY AT LESS THAN 200 KNOTS. VISUALLY CHECKED MLG AND NLG COMPONENTS, FOUND AND REMOVED ICE A ND SNOW FROM NLG COMPONENTS AND SENSORS. PERFORMED LANDING GEAR EXTENSION AND RETRACTION IAW 32-30-00, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007122700019 20071227 00019 NM 2007 12 27 SWAA076242 1 20071213 A 5523 65C2638427A TAB BOEING 737 7375H4 138449D NM LT ELEVATOR DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRDG CHECK, FOUND LT ELEVATOR TAB DELAMINATED. REMOVED AND REPLACED TAB PER MM. 2 L 7 2 4F RT A16WE 2007122700020 20071227 00020 NM 2007 12 27 SWAA076187 1 20071213 A 2560 PH22300L GLOWSTRIP BOEING 737 7375H4 138449D NM ROW 20 DEF LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED SPV CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 20 DEF. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007122700021 20071227 00021 2007 12 27 SWAA076199 4 20071213 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007122700023 20071227 00023 NM 2007 12 27 SWAA076188 1 20071213 A 5340 6545819 ATTACH FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 DURING SCHEDULED BRDG CHECK, FOUND NLG W/W SNUBBER ATTACHMENT FITTING CRACKED AT RBL 7.75. REPAIRED FITTING PER ACO. 2 L 7 2 4F RT A16WE 2007122700026 20071227 00026 NM 2007 12 27 SWAA076234 1 20071213 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM BS 867 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700028 20071227 00028 NM 2007 12 27 SWAA076229 1 20071213 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM BS 500C S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700029 20071227 00029 NM 2007 12 27 SWAA076231 1 20071213 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM BS 727D S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700030 20071227 00030 NM 2007 12 27 SWAA076230 1 20071213 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM BS 727B S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700035 20071227 00035 NM 2007 12 27 SWAA076193 1 20071213 A 2560 PH22300L GLOWSTRIP BOEING 737 7373Y0 1384671 NM ROW 10 DEF WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 10 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2007122700036 20071227 00036 NM 2007 12 27 SWAA076180 1 20071213 A 3260 1899 LOGIC CARD BOEING 737 7373G7 1384595 NM NLG FAULTY A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 29 683SW 24008 AIR TURNBACK / DECLARED EMERGENCY. DURING CLIMB FROM HOU NLG WARNING LIGHTS ILLUMINATED. CYCLED GEAR, NO HELP. REMOVE D AND REPLACED LOGIC CARD PER MM. 2 L 7 2 4F RT A16WE 2007122700037 20071227 00037 2007 12 27 SWAA076236 4 20071213 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007122700039 20071227 00039 NM 2007 12 27 SWAA076214 1 20071213 A 5311 6546538 FRAME BOEING 737 7373TO 138447G NM BS 597 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700040 20071227 00040 NM 2007 12 27 SWAA076202 1 20071213 A 5311 6546529 FRAME BOEING 737 7373TO 138447G NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700042 20071227 00042 NM 2007 12 27 SWAA076213 1 20071213 A 5311 65C22909 FRAME BOEING 737 7373TO 138447G NM BS 500C S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700044 20071227 00044 NM 2007 12 27 SWAA076237 1 20071213 A 5330 6545767 SKIN BOEING 737 7373TO 138447G NM BS 480 S28L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 480, STR 28L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007122700045 20071227 00045 NM 2007 12 27 SWAA076221 1 20071213 A 5310 6547979 CREASE BEAM BOEING 737 7373TO 138447G NM BS 752 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 752, LBL 70. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007122700048 20071227 00048 NM 2007 12 27 SWAA076218 1 20071213 A 5311 6546557 FRAME BOEING 737 7373TO 138447G NM BS 887 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700049 20071227 00049 NM 2007 12 27 SWAA076217 1 20071213 A 5311 6546550 FRAME BOEING 737 7373TO 138447G NM BS 787 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700050 20071227 00050 NM 2007 12 27 SWAA076212 1 20071213 A 5311 6546593 FRAME BOEING 737 7373TO 138447G NM BS 500A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700052 20071227 00052 NM 2007 12 27 SWAA076203 1 20071213 A 5311 6546549 FRAME BOEING 737 7373TO 138447G NM BS 767 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700053 20071227 00053 NM 2007 12 27 SWAA076211 1 20071213 A 5311 6546532 FRAME BOEING 737 7373TO 138447G NM BS 480 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700054 20071227 00054 NM 2007 12 27 SWAA076210 1 20071213 A 5311 6546529 FRAME BOEING 737 7373TO 138447G NM BS 440 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700057 20071227 00057 NM 2007 12 27 SWAA076207 1 20071213 A 5311 6546554 FRAME BOEING 737 7373TO 138447G NM BS 847 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700059 20071227 00059 NM 2007 12 27 SWAA076205 1 20071213 A 5311 6546551 FRAME BOEING 737 7373TO 138447G NM BS 887 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700060 20071227 00060 NM 2007 12 27 SWAA076204 1 20071213 A 5311 6546550 FRAME BOEING 737 7373TO 138447G NM BS 787 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700063 20071227 00063 NM 2007 12 27 SWAA076195 1 20071213 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 712SW 27846 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007122700064 20071227 00064 NM 2007 12 27 SWAA076196 1 20071213 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 792SW 27887 DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007122700065 20071227 00065 2007 12 27 SWAA076239 4 20071213 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007122700067 20071227 00067 EU 2007 12 27 USAA920071325 1 20071210 A 5315 D53472193200 FLOORBEAM AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 649AW 803 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3158 / FR 66 - BS 3366 / FR 70, -Y765. REPLACED CABIN FLOORBEAM, BS 3158 / FR 66 - BS 3366 / FR 70, -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007122700069 20071227 00069 SO 2007 12 27 C2XA07SH106 1 20071215 A 5320 14529495004 SILL EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18120 145681 SHV - DURING C-CHECK RIGHT FLOOR SILL HAS CORROSION FR 52-59. MAINTENANCE REPAIRED RIGHT FLOOR SILL BETWEEN FR 52-59, R EMOVED AND REPLACED CORRODED SECTION OF SILL IAW EC 5320-01394 AND IAW ENB 145 SRM 51-40-02 AND IAW EMB 145 CPM 51-21-06 . THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2007122700070 20071227 00070 NM 2007 12 27 HNAA0700289 1 20071212 A 2913 570347 PUMP DHAV DHC8 DHC8102 2809003 NM HYD SYSTEM MALFUNCTIONED A HNAA O OTHER J WARNING INDICATION CR CRUISE 1 EA 07 943HA 48987 15816 167 DURING CRUISE FLIGHT, CREW NOTED THAT ISO VALVE CAUTION LIGHT ILLUMINATED. HYDRAULIC QUANTITY OF NR 1 SYSTEM HAD DROPPE D TO 1 QUART. CREW ADVISED MAINTENANCE CONTROL AND DECISION WAS MADE TO DIVERT TO MDT. AIRCRAFT LANDED WITH 0 DEGREE F LAP SETTING, TAXIED TO RAMP AREA AND WAS THEN TOWED TO GATE. MAINTENANCE DISCOVERED PROBLEM WITH NR 1 ENGINE DRIVEN HYD RAULIC PUMP AND REPLACED THAT UNIT. OPS AND LEAK CHECKED PUMP IAW MM PROCEDURES. ALL CHECKS GOOD. AIRCRAFT RETURNED T O SERVICE. 2 H 7 2 4T RT A13NM 2007122700071 20071227 00071 NM 2007 12 27 HNAA0700288 1 20071203 A 3260 864202 PROXIMITY SENSOR DHAV DHC8 DHC8102 2809003 NM LT MLG OUT OF ADJUST A HNAA O OTHER N FALSE WARNING CR CRUISE 1 EA 07 839EX 41395 41395 226 AFTER TAKEOFF, LEFT GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. WHEN GEAR WAS EXTENDED, THE LEF T GEAR SHOWED AN UNSAFE CONDITION. CREW DID NOT NOTE POSITION OF L/G DOORS AT THIS TIME. CREW CHECKED ALTERNATE EXTENS ION SYSTEM AND IT ALSO INDICATED AN UNSAFE CONDITION ON THE LEFT GEAR. ALTERNATE EXTENSION PROCEDURES WERE FOLLOWED AND AIRCRAFT LANDED SAFELY. MAINTENANCE INSPECTED LEFT GEAR AND DOORS AND NOTED NO OBVIOUS DEFECTS. PROXIMITY SENSOR ON F ORWARD GEAR DOOR ACTUATOR WAS FOUND TO BE OUT OF ADJUSTMENT. SENSOR WAS ADJUSTED AND GEAR WAS SWUNG ON GROUND IAW MM PR OCEDURES. CHECKS WERE GOOD. HYDRAULIC SYSTEM WAS BLED AND SERVICED. AIRCRAFT WAS RELEASED FOR EVALUATION FLIGHT. EVA 2 H 7 2 4T RT A13NM 2007122700073 20071227 00073 NM 2007 12 27 BB07097 1 20071214 A 7700 3301KGAMS1 TACH GENERATOR BOEING 757 7572S7 1384962 NM RROYCE RB211 RB211535E4 54555 NE FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 906AW 47330 3871 23568 FLT 146 PHX-LIH CREW STATES, CLIMBING FROM FL280 TO FL340, N3 BEGAN TO FLUCTUATE FROM 10% TO 93%, RIGHT DUCT PRESSURE FL UCTUATED FROM 0 TO 35, CABIN RATE FLUCTUATED BETWEEN 1000 UP AND 1000 DOWN, RIGHT CENTER FUEL PUMP PRESSURE LIGHT ILLUMI NATED INTERMITTENTLY. ALL OTHER INDICATIONS NORMAL. MAINTENANCE REMOVED AND REPLACED N3 TACH GENERATOR, REMOVED AND RE PLACED RT SPEED CARD. 2 L 7 2 4F 4 F RT A2NM E12EU 2007122700075 20071227 00075 NM 2007 12 27 USAA920071326 1 20071214 A 5311 652072270 FRAME BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 458UW 25022 CLT - MAJOR REPAIR - FPBH - A .375 X .375 INCH L SHAPED CRACK ON FWD FRAME LOWER STOP FITTING OF FWD CARGO DOOR OPENING AT BS 440, S24R. REMOVED DAMAGE, INSTALLED DOUBLER AND TRIPLER. A 4000 FC REPETITIVE INSPECTION REQUIRED IAW US AIRWA YS EA-100077. 2 L 7 2 4F RT A16WE 2007122700077 20071227 00077 NM 2007 12 27 USAA920071328 1 20071212 A 5753 SKIN BOEING 737 737301 1384611 NM FORE FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 23742 CLT - MAJOR REPAIR - C-4 CHECK, DELAMINATION ON UPPER SKIN OF RIGHT OUTBOARD FORE FLAP AT TRAILING EDGE 15 INCHES FROM O UTBOARD TO INBOARD END. REMOVED AND REPLACED RIGHT OUTBOARD TRAILING EDGE FORE FLAP IAW B737-300 AMM 27-51-37. 2 L 7 2 4F RT A16WE 2007122700085 20071227 00085 2007 12 27 SWAA076247 4 20071215 A 2565 65C16820 HOOK BOEING 737 7377H4 1384404 NM R1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 256WN 32514 R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2007122700086 20071227 00086 NM 2007 12 27 SWAA076248 1 20071214 A 3350 417N5212 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 261WN 32517 DURING SCHEDULED MV1 CHECK, FOUND EEPLS END CAP BROKEN AT ROW 1 ABC. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 2007122700087 20071227 00087 NM 2007 12 27 SWAA076271 1 20071216 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727E S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007122700088 20071227 00088 NM 2007 12 27 SWAA076272 1 20071216 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727E S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007122700092 20071227 00092 NM 2007 12 27 SWAA076249 1 20071216 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 737E S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737E, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700097 20071227 00097 NM 2007 12 27 SWAA076255 1 20071216 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM LT OVERWING EXIT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 409WN 27896 DURING SCHEDULED 6Y CHECK, FOUND EEPLS ASSY MISSING AT LT OVERWING EMERGENCY EXIT. INSTALLED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007122700098 20071227 00098 NM 2007 12 27 SWAA076254 1 20071216 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 409WN 27896 DURING SCHEDULED 6Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 141.65. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007122700099 20071227 00099 NM 2007 12 27 SWAA076256 1 20071214 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 419WN 29824 DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 166. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007122700100 20071227 00100 NM 2007 12 27 SWAA076257 1 20071216 A 3350 417A5601 LIGHT BOEING 737 7377H4 1384404 NM RT OVERWING EXIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 422WN 29826 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007122700101 20071227 00101 NM 2007 12 27 SWAA076258 1 20071214 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM R2 DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 425LV 29829 R2 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007122700102 20071227 00102 NM 2007 12 27 SWAA076259 1 20071214 A 3350 417N5212 LIGHT BOEING 737 7377H4 1384404 NM ROW 1 ABC BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 427WN 29831 EEPLS END CAP BROKEN AT ROW 1 ABC. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 2007122700103 20071227 00103 NM 2007 12 27 SWAA076260 1 20071215 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM ROW 3 ABC MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 452WN 29846 EEPLS MISSING LENS AT ROW 3 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007122700107 20071227 00107 NM 2007 12 27 SWAA076264 1 20071216 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 360 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007122700108 20071227 00108 NM 2007 12 27 SWAA076265 1 20071216 A 5520 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM LT ELEVATOR FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED BRDG CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BEARING PER MM. 2 L 7 2 4F RT A16WE 2007122700112 20071227 00112 NE 2007 12 27 HNAA0700292 2 20071210 A 7261 OIL SYSTEM DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE LOW A HNAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 936HA 145 120418 ACFT YAWED TO THE LEFT ON CLIMBOUT, CREW NOTED NR 1 ENG TQ WAS AT 30 PERCENT. ALL OTHER ENG INST APPEARED NORMAL. CREW SHUTDOWN AND DECLARED AN EMERGENCY AND RETURNED TO PHL. MX INSPECTED NR 1 ENG AND ONLY DEFECT NOTED WAS ENG 2 QTS LOW ON OIL. SERVICED ENG AND CREW PERFORMED 3 HIGH POWER RUNS WITH NO DEFECTS NOTED. ACFT FERRIED FROM PHL TO ROA. ROA RE MOVED AND REPLACED NR 1 HMU AND FUEL PUMP; REMOVED AND REPLACED EEC. 2 H 7 2 4T 4 T RT A13NM E20NE 2007122700113 20071227 00113 NM 2007 12 27 HNAA0700293 1 20071216 A 5610 8SC0043011 WINDSHIELD DHAV DHC8 DHC8102 2809003 NM COCKPIT CRACKED A HNAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 07 806EX 2080 263 FLT 4280 FROM PHL TO IPT. WEATHER WENT BELOW MINS AND CAPTAINS WINDSHIELD CRACKED. ACFT DIVERTED TO MDT. LANDED WITHO UT INCIDENT. MDT REMOVED AND REPLACED CAPT WINDSHIELD. 2 H 7 2 4T RT A13NM 2007122700115 20071227 00115 NM 2007 12 27 HNAA0700295 1 20071217 A 2530 180140 GALLEY DHAV DHC8 DHC8102 2809003 NM ODOR A HNAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 982HA 380 ELECTRICAL ODOR IN CABIN. FLIGHT 4165, LGA TO ROA. LGA MNT PERFORMED HIDDEN DAMAGE INSPECTION AND FOUND HOT JUG IN NR 1 POSITION OVERHEATED AND CAUSING ODOR. REMOVED HOT JUG AS PRECAUTION, ITEM PLACED ON MEL. ROA MTN REMOVED AND REPLACE D HOT JUG. 2 H 7 2 4T RT A13NM 2007122700116 20071227 00116 NM 2007 12 27 HNAA0700296 1 20071215 A 3350 82410162005 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS INTERMITTENT A HNAA O OTHER N FALSE WARNING CR CRUISE 1 EA 07 810EX 308 EMERGENCY FLOOR LIGHTS AND LOWER FORWARD EXIT LIGHT ILLUMINATED IN-FLIGHT. CLT MTN REMOVED AND REPLACED EMERGENCY LIGHT CONTROL BOX, OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2007122700117 20071227 00117 NM 2007 12 27 USAA920071333 1 20071214 A 5340 69265552 ATTACH ANGLE BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 23742 CLT - MAJOR REPAIR - C-4 CHECK - 1A CRACK FOUND ON ATTACH ANGLE AT BS 348, S16L. REMOVED AND INSTALLED ATTACH ANGLE AT BS 348, S16L IAW B737-300 SRM 51-20-01 AND BOEING DRAWING 69-26555. 2 L 7 2 4F RT A16WE 2007122700118 20071227 00118 NM 2007 12 27 USAA920071334 1 20071215 A 5330 SKIN BOEING 737 737301 1384611 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 23742 CLT- MAJOR REPAIR - C-4 CHECK, A CRACK FOUND ON FUSELAGE SKIN AT BS 942, S24R. FABRICATED AND INSTALLED DOUBLER AT BS 9 42, S24R IAW B737 SRM 53-00-01. 2 L 7 2 4F RT A16WE 2007122700120 20071227 00120 NM 2007 12 27 USAA920071336 1 20071215 A 5313 655162825 STRINGER BOEING 737 7373Y0 1384671 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - CORROSION FOUND STRINGER S26L AT BS 907 - BS 936. REMOVED AND REPLACED STRINGER S26L AT BS 907 - B S 936 IAW B737-300 SRM 53-00-03-2R1 FIG 201 AND 51-40-20-0G FIG 3 AND 12. 2 L 7 2 4F RT A16WE 2007122700121 20071227 00121 NM 2007 12 27 USAA920071337 1 20071217 A 5330 6545774575 SKIN BOEING 737 7373Y0 1384671 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - CRACKS ON FUSELAGE SKIN AT BS 727D - BS 756+5", S19L - S23L. REPAIRED FUSELAGE SKIN AT BS 727D - B S 756+5", S21L - S23L IAW USAIRWAYS EA 100093. 2 L 7 2 4F RT A16WE 2007122700123 20071227 00123 NM 2007 12 27 SWAA076289 1 20071217 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 845 S23L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 23L CORRODED AT BS 845. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2007122700124 20071227 00124 NM 2007 12 27 SWAA076326 1 20071217 A 5753 65C34812 FLAP TRACK BOEING 737 7373Q8 1384670 NM NR 7 FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED BRDG CHECK, FOUND RT WING NR 7 OUTBOARD FLAP INBOARD TRACK FITTING CORRODED. REPAIRED FLAP TRACK PER S WA EA. 2 L 7 2 4F RT A16WE 2007122700125 20071227 00125 NM 2007 12 27 SWAA076325 1 20071217 A 5753 65C34812 FLAP TRACK BOEING 737 7373Q8 1384670 NM NR 2 FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 2 OUTBOARD FLAP INBOARD TRACK FITTING CORRODED. REPAIRED FLAP TRACK PER S WA EA. 2 L 7 2 4F RT A16WE 2007122700129 20071227 00129 NM 2007 12 27 SWAA076321 1 20071217 A 5311 6546526 FRAME BOEING 737 7373Q8 1384670 NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700130 20071227 00130 NM 2007 12 27 SWAA076320 1 20071217 A 5311 6546593 FRAME BOEING 737 7373Q8 1384670 NM BS 500A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700131 20071227 00131 NM 2007 12 27 SWAA076302 1 20071215 A 5743 6552235 FITTING BOEING 737 7373H4 1384600 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD HANGER FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM. 2 L 7 2 4F RT A16WE 2007122700132 20071227 00132 NM 2007 12 27 SWAA076301 1 20071215 A 5743 6552235 FITTING BOEING 737 7373H4 1384600 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED MV2 CHECK, FOUND RT MLG AFT HANGER FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM. 2 L 7 2 4F RT A16WE 2007122700134 20071227 00134 NM 2007 12 27 SWAA076275 1 20071214 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 513B S19R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 513B, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007122700135 20071227 00135 NM 2007 12 27 SWAA076273 1 20071214 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 503D S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007122700137 20071227 00137 2007 12 27 SWAA076291 4 20071216 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007122700140 20071227 00140 NM 2007 12 27 SWAA076278 1 20071213 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 420WN 29825 DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147.23. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700141 20071227 00141 NM 2007 12 27 SWAA076279 1 20071213 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 420WN 29825 DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.24. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700142 20071227 00142 NM 2007 12 27 SWAA076292 1 20071216 A 3350 417A5601 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 422WN 29826 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007122700143 20071227 00143 NM 2007 12 27 SWAA076280 1 20071214 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 430WN 33659 DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS MISSING AT ROW 13 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007121900137 20071219 00137 WP 2007 12 19 07FDEA05055 1 20071213 A 5347 SEAT TRACK DOUG MD10 MD1010F 3022112 WP BS 1351 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 563FE 46948 MAIN CARGO DECK STA 1351 RBL 28 SEAT TRACK IS DAMAGED BLENDED AREA OUT OF LIMITS IAW SRM 53-70-00 VOL 1. REMOVED SEAT T RACK IAW SRM 53-70-00. FABBED NEW SEAT TRACK ON TRAVELER NR T7/713046. INSTALLED SEAT TRACK IAW SRM 53- 70-00 FIG 1 V OL.1 2 L 7 3 4F RT A22WE 2007121900147 20071219 00147 NE 2007 12 19 2007UALA04990 2 20071207 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 2 BURNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 677UA 30029 729034 NR 2 ENGINE IS BURNED AND CRACKED AT COMBUSTION CHAMBER BULKHEAD FWD OF AP-8 PLUG AT 7:00 POS. DAMAGE IS BEYOND LIMITS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121900150 20071219 00150 NM 2007 12 19 2007UALA02220 1 20070625 A 2612 5604154 DETECTOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO BAY FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 341UA 24245 CARGO FIRE DETECTION FAIL LIGHTS ALL 4 ARE ILLUMINATED. REPLACED 3 DETECTORS IN AFT PIT A SYSTEM AND 3 IN FWD PIT 2 EAC H FOR B SYSTEM AND 1 FOR A SYSTEM. 2 L 7 2 4F 4 F RT A16WE E2GL 2007121900151 20071219 00151 NM 2007 12 19 QXEA200701855 1 20071210 A 3297 WIRE DHAV DHC8 DHC8202 2809007 NM ANTI SKID SYS CHAFED A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 358PH 506 PDX - UPON GEAR EXTENSION THE ANTI SKID CAUTION LIGHT ILLUMINATED. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE PERFORMED A TEST OF THE SYSTEM, TEST FAILS. FOUND A CHAFED WIRE AT THE LEFT OUTBOARD TRANSDUCER ( WHEEL SPEED). REPAIRED WIRE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2007121900156 20071219 00156 EU 2007 12 19 AALA20072444 1 20071214 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 JFK - EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR EXIT SIGN INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT LEFT NUMBE R THREE DOOR EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2007121900157 20071219 00157 WP 2007 12 19 IXXA070063S 1 20071115 A 5311 FRAME DOUG DC8 DC873F 302199F WP ZONE 200 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT HAS A IMPROPER REPAIR AND DENT ON FRAME AT STATION 1580. 000 LONGERON-21RIGHT REMOVED FASTENER AS NEEDED TO PERFORM REPAIR. REMOVED FRAME SEGMENT WITH EXISTING REPAIR. FABRICA TED FRAME SEGMENT, ANGLES. PERFORMED HEAT TREATMENT. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS, AND REPAIR PARTS IAW DC8 SRM 53-2-0 FIGURE 2 SHEET 4 AND 6, DC8 SRM 51-1-20D, DC8 SRM 53-4-1 FIGURE 51 SHEET 21 ITEM "A", SRM 53-2-0 FIGURE 2 SHEET 7 AND 8 T/R 53-110 DATED 11-10-2000, DC8 SRM 51-1-1 PAGES 1, 13, 17, DC8 SRM 51 -1-8B, AND 51-3-1. 2 L 7 4 4F RT 4A25 2007121900168 20071219 00168 NM 2007 12 19 2007UALA04999 1 20071207 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 FOUND SEATS 55-56-57-58-59 ABC EMERGENCY LIGHTS IS INOP. SECURED LOOSE CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121900183 20071219 00183 NM 2007 12 19 2007UALA05046 1 20071210 A 2560 65B549299 GIRT BAR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE DOOR 2L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 194UA 26892 AIRCRAFT SETTLED ON JETBRIDGE AND DAMAGED DOOR 2L GIRT BAR FITTINGS. DOOR DAMAGED DUE TO GROUND EQUIPMENT. REPLACED FW D AND AFT DOOR GIRT BAR BRACKET AND LOWER GATE TIE ROD. ACCOMPLISHED INSTALLATION AND OPERATION INSPECTION OF DOOR AND S LIDE. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121900185 20071219 00185 EU 2007 12 19 TRAX200701897 1 20071210 A 5330 DOUBLER AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 DOUBLER CORRODED AT LWR FUSELAGE AREA (ANTENNA DOUBLER) FR 16-17 (SEE W/C 2000-18 FOR FABRICATION) SEE STICKER 200. 2 H 7 2 4T RT A53EU 2007121900191 20071219 00191 2007 12 19 SWIA200718941 4 20071207 A 2210 6229815904 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA FLIGHT CONTROL MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 975SW 9411 9411 7951 FLT 6389 - RECEIVED STAB TRIM RUNAWAY AURAL WARNING IN FLIGHT. REPLACED NR 2 FCC UNIT, OPS CHECKS GOOD ON AUTO PILOT AN D TRIM FUNCTIONS, IAW 22-10-00. 2 L 7 2 4F RT A21EA 2007122000010 20071220 00010 WP 2007 12 20 AALA20072452 1 20071215 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 501AA 49738 LGA - EMERGENCY LIGHTS AT TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007122000015 20071220 00015 NM 2007 12 20 2007UALA02267 1 20070623 A 5740 BOLT BOEING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE SLAT ACTUATOR INCORRECT A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 376UA 0533 24641 NR 1 LEADING EDGE SLAT INTRANSIT LIGHT IS ILLUMINATED WITH FLAPS UP. ROOT CAUSE UNKNOWN. FOUND INCORRECT LEADING EDGE SLAT ACTUATOR ROD END BOLT. REPLACED NR 1 LEADING EDGE SLAT ACTUATOR AND ROD END BOLT. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122000018 20071220 00018 NM 2007 12 20 UPS07M51287 1 20071211 A 3245 4305890022 TRANSMISSION DOUG MD11 MD11F 3023600 NM MLG NO INDICATION A IPXA O OTHER P NO WARNING INDICATION CL CLIMB 1 SO 01 278UP 48577 AFTER T/O CREW REPORTED RECEIVING ALERT FOR NR 5 AND NR 6 TIRE HAD FAILED. FLT CONTINUED TO CGN. CREW DECLARED AN EMER GENCY UPON LANDING. MX REMOVED NR 5 TIRE PRESSURE TRANSDUCER AND DEFERRED THE NR 6 TIRE PRESSURE INDICATION M364436 ASS IGNED. T/S IAW FIM 32-40-00-1 FIG 119 AND WDM 32-46-02 MEASURED WIRING FROM BTM/TPI UNIT PIN 6A AND 6B THRU THERMAL PLU P1-3649 PIN 1 AND 2. ALL SATIS. REMOVED AND REPLACED TRANSMISSION UNIT IAW AMM 32-46-08. REMOVED AND REPLACED TIRE P RESSURE TRANSDUCER OF NR 6 MAIN WHEEL. 2 L 7 3 4F RT A22WE 2007122000025 20071220 00025 NM 2007 12 20 2007UALA05071 1 20071211 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 S10-11R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 50961 24640 FWD GALLEY DOOR FWD CUTOUT BETWEEN STR 10R AND STR 11R WEB AT BS 294.5 CRACKED AT ANGLE. SUSPECT NORMAL AC OPERATION. R EMOVED & REPLACED CRACKED INTERCOSTAL WEB ANGLE. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122000028 20071220 00028 NE 2007 12 20 2007UALA05074 2 20071213 A 7230 COMPRESSOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE STALLED A UALA A UNSCHED LANDING C J F.O.D. WARNING INDICATION CL CLIMB 1 WP 29 662UA 27159 717590 RTFL DUE TO NR 1 ENGINE SURGE (COMPRESSOR STALL) AS A RESULT OF A BIRDSTRIKE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007122000030 20071220 00030 NM 2007 12 20 2007UALA05076 1 20071213 A 2421 767146A IDG BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 1 ENGINE FAILED A UALA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 WP 29 220UA 30223 LT GENERATOR FAILURE ON TAKEOFF ROLL. DISCONNECTED GENERATOR AND CONTINUED TO ORD AFTER PHONE PATCH WITH SAMC AND DISPAT CH. NR 1 ENGINE INTEGRATED DRIVE GENERATOR FREQUENCY IS LOW. REPLACED NR 1 IDG. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007122000031 20071220 00031 2007 12 20 2007UALA05077 4 20071212 A 3440 INDICATOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE INCORRECT A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 813UA 858 RTFL DUE TO NAVIGATION PROBLEMS HEADING SYSTEM NOT WORKING, POSITION NOT CORRECT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007122000050 20071220 00050 EA 2007 12 20 QXEA200701921 1 20071218 A 7830 SLEEVE CNDAIR CL600 CL6002C10 1390015 EA THRUST REVERSER MISSING A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 614QX 10049 BIL- FLIGHT 2549 - ON TAXI OUT, CYCLING THE THRUST REVERSERS RESULTED IN A REVERSER UNLOCKED CAUTION MESSAGE. RETURNED TO THE GATE. AFTER PARKING THE REVERSER APPEARS TO BE FULLY DEPLOYED. MAINTENANCE FOUND THE INBOARD TRANS COWL SLIDING SLEEVE TO BE HALF MISSING AND TWISTED, PREVENTING RETRACTION OF THE RIGHT THRUST REVERSER. ADJUSTED REMAINING PORTION OF SLEEVE AND REINSTALLED THE TRANS COWLS. LOCKED OUT THE RIGHT THRUST REVERSER AND PLACED ON MEL 78-33-01. ACFT RETUR NED TO SERVICE. REPLACED THE NR 2 ENGINE UPPER TRANSCOWL NYLON INSERT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4F RT A21EA 2007122000052 20071220 00052 2007 12 20 QXEA200701918 4 20071217 A 3418 STICK SHAKER CNDAIR CL600 CL6002C10 1390015 EA MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 616QX 10128 BOI - FLIGHT 2572 - APPROACHING TOP OF CLIMB RECEIVED A STALL WARNING CAUTION MESSAGE. TURNED STALL PUSHER SWITCH OFF P ER CHECKLIST. MAINTENANCE FOUND ON THE MDC, NO POWER TO THE STICK PUSHER. CYCLED THE CIRCUIT BREAKER AND PERFORMED A O PERATIONAL TEST. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2007122000060 20071220 00060 EA 2007 12 20 SWIA200718947 1 20071209 A 2760 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILERS LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 442SW 7609 FLT 3984 - HYDRAULIC 2 LOW PRESS CAUTION IN FLIGHT. REPLACED RIGHT FLIGHT SPOILER OUTBOARD PCU IAW AMM 27-62-01. OPS C HECK AND LEAK CHECKS GOOD, P/N 2700-7, S/N OFF MAL5571. 2 L 7 2 4F RT A21EA 2007122000074 20071220 00074 EA 2007 12 20 TRAX200701921 1 20071212 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 903EV 7621 CORROSION ON 2 ANGLES ON BOTTOM OF LT EMERGENCY EXIT (FLAGGED). 2 L 7 2 4F RT A21EA 2007122000077 20071220 00077 NM 2007 12 20 2007UALA05087 1 20071213 A 5312 PRESSURE PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 664 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 PRESSURE DECK CRACKED STA 664 AT LBL 32 WL 203 JUST FWD OF AILERON QUADRANT. MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT DA MAGE. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122000087 20071220 00087 NM 2007 12 20 AALA20072449 1 20071215 A 2910 HOSE BOEING 757 757223 1384957 NM HYD SYSTEM LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 21 692AA 26972 MCO INFLIGHT T1034/15DEC - RIGHT MAIN LANDING GEAR DOOR AMBER LIGHT ILLUMINATED DURING APPROACH. CAPTAIN FLEW BY TOWER FOR COMFIRMATION. LANDED MCO WITHOUT INCIDENT. REPLACED RIGHT MAIN LANDING HEAR DOOR INBOARD EXTENSION/RETRACTION RETUR N HYDRAULIC LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007122000093 20071220 00093 SO 2007 12 20 SIMA200734602 1 20071207 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO SERVICE DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 670AE 9594 5000 145790 DURING INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND TO HAVE TWO SMALL AREAS CORRODED BEYOND MANUAL LIMITS. REMOVED CORROSION IAW EMB SRM PERFORMED EDDY CURRENT WITH NO REJECT ABLE INDICATIONS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007122100011 20071221 00011 NM 2007 12 21 ASAA0742376 1 20070922 A 5320 654580734 INTERCOSTAL BOEING 737 7374Q8 138447Q NM BS 294 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 MAIN CABIN AT FWD SERVICE DOOR CUTOUT BS 294 BETWEEN STG 9R AND 10R HAS CRACK AT AFT END OF INTERCOSTAL ANGLE. REMOVED AND REPLACED INTERCOSTAL ANGLE IAW BAC DWG 65 45807 AND 51 40 1 BOEING 737 400 SRM. 2 L 7 2 4F RT A16WE 2007122100021 20071221 00021 SO 2007 12 21 FDKA200711346 1 20071125 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 FDM 6041 JFK-RIC (1615 PHX LCL). LEFT WING EMERGENCY EXIT SIGN INOP. MX RESET, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007122100029 20071221 00029 SO 2007 12 21 FDKA200710541 1 20071010 A 3350 SGEMBF145 LIGHT EMB 145 EMB145 3260210 SO ROW 12 INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FRL FLT 6063 MCO-CHS. EMERGENCY LIGHT INOP ROW 12. MX REMOVED AND REPLACED PATH LIGHTING, OPS GOOD. 2 L 7 2 4F RT T00011AT 2007122100041 20071221 00041 WP 2007 12 21 ABXA070403 1 20071019 A 5313 591140617 LONGERON DOUG DC9 DC941 302207N WP BS 160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 LONGERON 4 LEFT CRACKED AT FRAME ATTACH POINTS AT STATION 160. SPLICED IN NEW LONGERON IN ACCORDANCE WITH DC9 SRM. 2 L 7 2 4F A6WE 2007122100044 20071221 00044 WP 2007 12 21 ABXA070407 1 20071020 A 5415 59132626 ATTACH ANGLE DOUG DC9 DC941 302207N WP RT NACELLE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 LOWER PYLON LEADING EDGE ATTACH ANGLE CRACKED. REMOVED AND REPLACED FORWARD SECTION OF PYLON LOWER ATTACH ANGLE IN ACCO RDANCE WITH DC9 SRM 54-04. 2 L 7 2 4F A6WE 2007122100046 20071221 00046 WP 2007 12 21 ABXA070405 1 20071020 A 5320 2913044501 GUSSET DOUG DC9 DC941 302207N WP BS 206 L16L CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 FS 206.00, LONGERON 16 LEFT GUSSET CRACKED. REMOVED AND REPLACED GUSSET IN ACCORDANCE WITH DC9 SRM. 2 L 7 2 4F A6WE 2007122100091 20071221 00091 EU 2007 12 21 USAA920071319 1 20071208 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHTS INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 625AW 24956 24956 64 FLT 350 - MSP-PHX - EEL - ROW 9 & 11 ABC & DEF EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY RIGHT MID IAW A320 AMM 33-51-38. 2 L 7 2 4F RT A28NM 2007122100098 20071221 00098 NM 2007 12 21 CALA0700737 1 20071208 A 5311 6546557 FRAME BOEING 737 7373T0 1384582 NM BS 887 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 FUSELAGE FRAME CRACKED STA 887 BETWEEN STA 8 & 9 RT. REPAIRED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2007122100101 20071221 00101 NM 2007 12 21 SA07080 1 20071209 A 3350 32145410 EPSU AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 829AW 1563 PHX - THE LEFT HAND, FORWARD POWER SUPPLY UNIT FAILED OPS TEST. MAINTENANCE REPLACED THE LEFT HAND, FORWARD EMERGENCY P OWER SUPPLY UNIT. OPS TEST OK. 2 L 7 2 4F RT A28NM 2007122100104 20071221 00104 SO 2007 12 21 C2XA07RI103 1 20071207 A 2611 SMOKE WARNING EMB 145 EMB145XR 3260214 SO LAVATORY FALSE ACTIVATION A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 27 21129 145703 FLT 2596 - EWR - CREW REPORTED EICAS LAV SMOKE MESSAGE, NO CABIN FIRE OR SMOKE NOTICED. EWR MX PERFORMED OPERATIONAL CH ECK IAW EMB 145 AMM SUCCESSFULLY AND COULD NOT DUPLICATE THE PROBLEM. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2007122100117 20071221 00117 WP 2007 12 21 ASAA0782378 1 20071210 A 5313 591143289 LONGERON DOUG DC9 DC983 3022083 WP BS 1407-1421 S2R CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 944AS 53019 AFT ACCESSORY COMPT LONGERON 2R CRACKED JUST AFT OF 1418 FRAME. REMOVED DAMAGED SECTION OF LONGERON LOCATED DRILLED AND INSTALLED A REPLACEMENT SECTION AND REPAIR SPLICE IAW MD80 SRM 53-02 PG 50 AND 52. 2 L 7 2 4F RT A6WE 2007122100118 20071221 00118 EA 2007 12 21 COMA0760685 1 20071202 A 3150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE DUCT FALSE ACTIVATION A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 938CA 7046 FLIGHT 5591 - RECEIVED ANTI-ICE DUCT WARNING MESSAGE ON TAKEOFF. ABORTED TAKEOFF, RETURNED TO GATE WITHOUT INCIDENT. P ERFORMED RUNS WITH CREW, OPS CHECK OF ANTI-ICE SYSTEM IN NORMAL MODE. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2007122100133 20071221 00133 NM 2007 12 21 SWAA076184 1 20071213 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 727E S24R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007122100138 20071221 00138 NM 2007 12 21 SWAA076185 1 20071213 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 452WN 29846 DURING SCHEDULED HC2 CHECK, FOUND EEPLS INOP AT ROW 7 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007122700012 20071227 00012 EA 2007 12 27 A6WA200740644 1 20071114 A 2700 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA FLT CONTROLS UNKNOWN A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 460AW 7867 DURING APPROACH TO MHT, NOSE UP TRIM OF 9.2 UNITS REQUIRED TO MAINTAIN NORMAL GLIDE PATH. FLIGHT CONTROLS HEAVIER THAN NORMAL, ESPECIALLY ELEVATOR. AILERONS FEEL HEAVY ALSO. NO UNUSUAL WEATHER CONDITIONS. ALL HYDRAULIC NORMAL. ELEVATOR TRIM ON GO AROUND OPERATED NORMALLY. OPS CHECKED FLIGHT CONTROL PANEL, COMPLIED WITH SERVO ELEVATOR TEST, PERFORMED CO NTROL COLUMN FEEL FORCE CHECK, AND CENTERING CHECK, DETAILED INSPECTION OF MECHANICAL CONTROL PATH. ALL OPS CHECK GOOD. ALSO, AILERON, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007122700024 20071227 00024 NM 2007 12 27 SWAA076233 1 20071213 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700031 20071227 00031 NM 2007 12 27 SWAA076189 1 20071213 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700032 20071227 00032 NM 2007 12 27 SWAA076192 1 20071213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 440 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007122700033 20071227 00033 NM 2007 12 27 SWAA076191 1 20071213 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700034 20071227 00034 NM 2007 12 27 SWAA076200 1 20071213 A 3350 65C27028 LIGHT BOEING 737 737317 138447P NM EMERGENCY EXIT DISCONNECTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SERVICE CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 1 DEF. FOUND LIGHT ASSY DISCONNECTED. RECONNECTED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2007122700043 20071227 00043 NM 2007 12 27 SWAA076238 1 20071213 A 5322 6546569 SHEAR TIE BOEING 737 7373TO 138447G NM BS 907 S27R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 907, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2007122700062 20071227 00062 NM 2007 12 27 SWAA076241 1 20071213 A 2820 61162 VALVE BOEING 737 737317 138447P NM NR 2 ENGINE FAULTY A SWAA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SW 29 698SW 23176 INFLIGHT SHUTDOWN / DECLARED EMERGENCY/DIVERSION. NR 2 ENGINE ROLLED BACK AND SHUTDOWN, RESTARTED NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE SPAR VALVE PER MM. 2 L 7 2 4F RT A16WE 2007122700074 20071227 00074 NM 2007 12 27 USAABB07098 1 20071215 A 3397 WIRE BOEING 757 7572S7 1384962 NM EMERGENCY LIGHTS BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 906AW 23568 MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT ROW 19LH INOP. REPAIRED WIRING. 2 L 7 2 4F RT A2NM 2007122700076 20071227 00076 NM 2007 12 27 USAA920071327 1 20071215 A 5313 655162829 STRINGER BOEING 737 7373Y0 1384671 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - CORROSION ON BOTTOM SIDE OF STRINGER 27L, AT BS 986 - BS 1006. REMOVED AND REPLACED STRINGER 27L, AT BS 986 - BS 1006 IAW B737-300 SRM 51-40-02-0G, PAR 7D FIG 8 & 12. 2 L 7 2 4F RT A16WE 2007122700080 20071227 00080 NM 2007 12 27 USAA920071331 1 20071210 A 5340 69489853 STRINGER CLIP BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 23742 CLT - MAJOR REPAIR - C-4 CHECK, A CRACK FOUND ON FRAME TO STRINGER ATTACHED CLIP AT BS 360, S19L. REMOVED AND REPLACED FRAME TO STRINGER ATTACHED CLIP AT BS 360, S19L IAW B737-300 SRM 51-10-02, 51-40-02, AND BOEING DRAWING 69-48985-3. 2 L 7 2 4F RT A16WE 2007122700081 20071227 00081 NM 2007 12 27 USAA920071332 1 20071210 A 5340 69489854 STRINGER CLIP BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 23742 CLT - MAJOR REPAIR - C-4 CHECK, A CRACK FOUND ON FRAME TO STRING ATTACHED CLIP AT BS 360, S10L. REMOVED AND REPLACED FR AME TO STRING ATTACHED CLIP AT BS 360, S10L IAW B737-300 SRM 51-10-02, 51-40-02, AND BOEING DRAWING 69-48985-4. 2 L 7 2 4F RT A16WE 2007122700089 20071227 00089 NM 2007 12 27 SWAA076268 1 20071216 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 597 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007122700105 20071227 00105 NM 2007 12 27 SWAA076262 1 20071216 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 496WN 32478 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 2 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007122700110 20071227 00110 NM 2007 12 27 SWAA076267 1 20071215 A 3350 3071BPEGPL LAMP BOEING 737 7373Q8 1384670 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007122700114 20071227 00114 NM 2007 12 27 HNAA0700294 1 20071217 A 5270 PROXIMITY SWITCH DHAV DHC8 DHC8102 2809003 NM CARGO DOOR DIRTY A HNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 07 937HA 148 DURING TAKEOFF ROLL AT 85 KTS THE BAG BAY DOOR LIGHT ILLUMINATED. THE AIRCARFT REJECTED TAKEOFF AND RETURNED TO THE GAT E. THE CARGO DOOR WAS RE-OPENED AND CLOSED BY THE CREW TO VERIFY THAT IT WAS PROPERLY CLOSED. THE LIGHT WAS EXTINGUISH ED. MTN MEL'ED CARGO DOOR/ INDICATION. MDT MNT CLEANED AND LUBED PROX SWITCHES. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2007122700126 20071227 00126 NM 2007 12 27 SWAA076324 1 20071217 A 5520 REP4HEB BEARING BOEING 737 7373Q8 1384670 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED BRDG CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BEARING PER MM. 2 L 7 2 4F RT A16WE 2007122700127 20071227 00127 NM 2007 12 27 SWAA076323 1 20071217 A 5520 REP4HEB BEARING BOEING 737 7373Q8 1384670 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED BRDG CHECK, RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BEARING PER MM. 2 L 7 2 4F RT A16WE 2007122700138 20071227 00138 NM 2007 12 27 SWAA076276 1 20071213 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 420WN 29825 DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS BROKEN AT ROW 3 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2007122700144 20071227 00144 NM 2007 12 27 SWAA076281 1 20071214 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 430WN 33659 DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007122700145 20071227 00145 NM 2007 12 27 SWAA076296 1 20071217 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 488WN 33853 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACK AT ROW 16ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PAC K PER MM. 2 L 7 2 4F RT A16WE 2007122700147 20071227 00147 NM 2007 12 27 SWAA076294 1 20071217 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 488WN 33853 DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK P ER MM. 2 L 7 2 4F RT A16WE 2007122700148 20071227 00148 NM 2007 12 27 SWAA076295 1 20071217 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 488WN 33853 DURING SCHEDULED HC1 CHECK, MID CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK P ER MM. 2 L 7 2 4F RT A16WE 2007122700149 20071227 00149 NM 2007 12 27 SWAA076318 1 20071217 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 277 S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BDRG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007122700156 20071227 00156 NM 2007 12 27 SWAA076298 1 20071217 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED BRDG CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007122700158 20071227 00158 NM 2007 12 27 SWAA076314 1 20071217 A 5312 6545409 PRESSURE PANEL BOEING 737 7373G7 1384595 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND NLG W/W VERTICAL WEB CRACKED AT FWD TEE CHORD. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007122700159 20071227 00159 NM 2007 12 27 SWAA076310 1 20071217 A 5310 6547977 CREASE BEAM BOEING 737 7373G7 1384595 NM BS 660 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM CORRODED AT BS 660, LBL 70. REMOVED AND REPLACED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2007122700164 20071227 00164 NM 2007 12 27 SWAA076312 1 20071217 A 5553 6547450 FITTING BOEING 737 7373G7 1384595 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND LT VERTICAL STABILIZER LUG FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700165 20071227 00165 NM 2007 12 27 SWAA076285 1 20071217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373TO 138447G NM BS 663 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007122700166 20071227 00166 NM 2007 12 27 SWAA076288 1 20071217 A 5311 6546551 FRAME BOEING 737 7373TO 138447G NM BS 807 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700167 20071227 00167 NM 2007 12 27 SWAA076286 1 20071217 A 5311 6546526 FRAME BOEING 737 7373TO 138447G NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700169 20071227 00169 NM 2007 12 27 SWAA076303 1 20071217 A 5751 69764421 CONTROL ROD BOEING 737 7373TO 138447G NM RT AILERON WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, RT WING AILERON FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT AILERON CONTROL ROD PER MM. 2 L 7 2 4F RT A16WE 2007122700170 20071227 00170 NM 2007 12 27 SWAA076309 1 20071217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373TO 138447G NM BS 460 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007122700171 20071227 00171 NM 2007 12 27 SWAA076308 1 20071217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373TO 138447G NM BS 440 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007122700172 20071227 00172 NM 2007 12 27 SWAA076307 1 20071217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373TO 138447G NM BS 420 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007122700173 20071227 00173 NM 2007 12 27 SWAA076306 1 20071217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373TO 138447G NM BS 400 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007122700174 20071227 00174 NM 2007 12 27 SWAA076300 1 20071217 A 5310 6547978 CREASE BEAM BOEING 737 7373TO 138447G NM BS 700 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 700, RBL 70. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2007122700175 20071227 00175 NM 2007 12 27 SWAA076305 1 20071217 A 5753 SKIN BOEING 737 7373TO 138447G NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2007122700176 20071227 00176 NM 2007 12 27 SWAA076304 1 20071217 A 5313 6551698 STRINGER SPLICE BOEING 737 7373TO 138447G NM BS 907 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER S RM. 2 L 7 2 4F RT A16WE 2007122700179 20071227 00179 2007 12 27 SWAA076328 4 20071215 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 773SA 27881 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007122700182 20071227 00182 SO 2007 12 27 C2XA07TY083 1 20071218 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 29906 145472 NR 3 EMERGENCY LIGHT FLOOR STRIP HAS BROKEN WIRE. REMOVED AND REPLACED LIGHT STRIP IAW EMB 145 AMM 33-50-12 OPS CHECK G OOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007122700183 20071227 00183 SO 2007 12 27 C2XA07TY084 1 20071218 A 3350 276005 FUSE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BLOWN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 26545 145558 LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED FUSES IAW VCMM 33-21-70, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007122700185 20071227 00185 EU 2007 12 27 USAA920071343 1 20071213 A 2782 830A000002 ACTUATOR AIRBUS 320 A320232 3930326 EU TE FLAPS FAULTY A USAA A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 EA 19 619AW 40446 527 FLT 598 - PHL - LAS - EL - FLIGHT CONTROL SLATS FAULT/LOCKED ON APPROACH. FLAP LEVER RECYCLE PER ECAM UNSUCCESSFUL. CR EW DECLARED AN EMERGENCY. PASSENGERS DID NOT BRACE. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED SLAT ACTUATOR ASSY PER AIRBUS AMM 27-84-49 PG 401 RIGHT HAND ACTUATORS 6079CM, OPERATIONAL CHECK OF SLATS OK PER AIRBUS AMM 27-84-00-710-001. 2 L 7 2 4F RT A28NM 2007122700186 20071227 00186 NM 2007 12 27 USAA920071339 1 20071208 A 5753 6546486129 WEDGE BOEING 737 7373Y0 1384671 NM LT WING TE FLAP DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - A DENT FOUND ON LEFT WING INBOARD MID FLAP TRAILING EDGE WEDGE AT WBL 75.01. REPAIRED LEFT WING IN BOARD MID FLAP TRAILING EDGE WEDGE AT WBL 75.01 IAW B737-300 SRM 51-70-10-2R, FIG 202. 2 L 7 2 4F RT A16WE 2007122700187 20071227 00187 NM 2007 12 27 USAA920071340 1 20071110 A 5753 6546435278 WEDGE BOEING 737 7373G7 1384595 NM RT WING TE FLAP DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT- MAJOR REPAIR - C-18 CHECK - A DEBOND FOUND ON 2 INCHES OUT OF INBOARD EDGE OF RIGHT OUTBOARD FLAP TRAILING EDGE WED GE. REMOVED DAMAGE AND REPAIRED ON RIGHT OUTBOARD FLAP TRAILING EDGE WEDGE IAW B737-300 SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007122700188 20071227 00188 NM 2007 12 27 USAA920071344 1 20071205 A 5754 SKIN BOEING 737 7373G7 1384595 NM NR 2 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C-16 CHECK - THREE CRACKS FOUND ON LOW LEADING EDGE SKIN OF NR 2 SLAT AT NR 2 SLAT STATION 213.25 - 215.75, AND 161. REPAIRED CRACKS IAW B737-300 SRM 57-43-01-2R6, FIG 201. 2 L 7 2 4F RT A16WE 2007122700189 20071227 00189 NM 2007 12 27 USAA920071345 1 20071206 A 5311 651630220 FRAME BOEING 737 7373G7 1384595 NM BS 188 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C-16 CHECK- A CRACK FOUND AT BS 188, RBL 31 WL 207. REMOVED DAMAGE AND INSTALLED FILLERS IAW B737 -300 SRM 53-00-07-2R11. 2 L 7 2 4F RT A16WE 2007122700191 20071227 00191 NM 2007 12 27 USAA920071348 1 20071218 A 5330 6545800745 SKIN BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C-16 CHECK - A CRACK ON FUSELAGE SKIN AT R1 DOOR LOWER HINGE CUTOUT, BS 291.5, WL 233.5. INSTALLED DOUBLER AND REPAIRED CRACK ON FUSELAGE SKIN AT R1 DOOR LOWER HINGE CUTOUT, BS 291.5, WL 233.5 IAW B737-300 SRM 53-10-01 -2R, FIG 201. 2 L 7 2 4F RT A16WE 2007122700195 20071227 00195 NM 2007 12 27 USAA920071349 1 20071217 A 5330 654576987 SKIN BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 PHX - MAJOR REPAIR - A CRACK FOUND ON FUSELAGE SKIN AT BS 380, S28L - S28R. REPAIRED CRACK IAW US AIRWAYS EA 12067. 2 L 7 2 4F RT A16WE 2007122700196 20071227 00196 NM 2007 12 27 USAA920071350 1 20071218 A 5330 SKIN BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 23381 CLT - MAJOR REPAIR - A CRACK FOUND ON FUSELAGE SKIN AT BS 520 S10L. INSTALLED REPAIR ON FUSELAGE SKIN AT BS 520, S10L. 2 L 7 2 4F RT A16WE 2007122700198 20071227 00198 NM 2007 12 27 USAA920071352 1 20071217 A 5340 69353522 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C-16 CHECK - STRINGER CLIP CRACKED AT BS 727D, S20R. REMOVED AND REPLACED STRINGER CLIP AT BS 727D , S20R IAW B737-300 SRM 51-40-02-0G FIG 8 AND 12. 2 L 7 2 4F RT A16WE 2007122700199 20071227 00199 NM 2007 12 27 USAA920071354 1 20071218 A 5754 SKIN BOEING 757 7572B7 1384964 NM NR 5 SLAT DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU A1884 27810 MCN - MAJOR REPAIR - C-4 CHECK - DENTS FOUND ON UPPER AND OUTBOARD END SKIN OF NR 5 SLAT TRAILING EDGE WEDGE AT NR 5 SLA T STA 267.10. REPAIRED DENTS ON NR 5 SLAT TRAILING EDGE WEDGE AT NR 5 SLAT STA 267.10 IAW B757-200 SRM 51-70-10, REPAIR Z, FIG 203. 2 L 7 2 4F RT A2NM 2007122800001 20071228 00001 NM 2007 12 28 07FDEA05089 1 20071219 A 5320 65607899 BRACKET BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 LT WING TO BODY FAIRING ATTACH BRACKET AT STR S-18A, BS 937 IS CRACKED REMOVED CRACKED BRACKET. FABRICATED NEW BRACKET, P/N 65-60789-9, FROM 2024T3 - .063". A TAG A 59659/ PO 1026484. TREATED AND PRIMED AND INSTALLED NEW BRACKET REF SRM 51-30-2 PG 2 AND 8 SRM 51-10-2 PG 1 AND 2/ BOEING DWG 65-60789 THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007122800002 20071228 00002 2007 12 28 HALA0700546 4 20071225 A 3416 4039892904 INDICATOR BOEING 767 76733A 1385209 NM ALTIMETER MALFUNCTIONED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 587HA 33421 ETOPS SIGNIFICANT SYSTEM, OFF FLAG IN VIEW ON CAPT'S ALTM WITH BOTH NORM AND ALT AIR DATA SW SELECTED. REPLACED CAPT'S ALTIMETER INDICATOR. OPS CK OK PER MM 34-13-01. 2 L 7 2 4F RT A1NM 2007122800005 20071228 00005 NM 2007 12 28 07FDEA05090 1 20071219 A 5347 BAC15201257 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 CORROSION AROUND SEAT TRACK ATTACH SCREW, BS 720E, RBL 64, WL 208. REMOVED DAMAGE SECTION OF SEAT TRACK, REF SRM 51-30- 2 FROM STA 720-750, RBL 64. REMOVED CREASE BEAM FROM STA 720C-740, RBL 64 REF SRM 51-30-2. FABRICATED SEAT TRACK, REPA IR PARTS, REF SRM 53-10 FIG 1. FABRICATED CREASE BEAM REF BOEING DRAWING 65-23359. TREATED AND PRIMED SEAT TRACK, REPA IR PARTS AND CREASE BEAM. REF SRM 53-10-2 AND 51-30-2. THIS IS CLASSIFIED AS MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007122800006 20071228 00006 NM 2007 12 28 07FDEA05091 1 20071219 A 5220 500797869 RETAINER BOEING 727 727233 138408A NM ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 LT FWD OVERWING PRESSURE SEAL CORNER RETAINER ANGLE IS CRACKED. FABRICATED ANGLE REF BAC DWG 50-07978, HEAT TREATED, TR EATED AND PRIMED REF SRM 51-10-2. INSTALLED RETAINER REF SRM 51-30-2, THIS IS CLASSIFIED AS A MINOR. 2 L 7 3 4F RT A3WE 2007122800007 20071228 00007 NM 2007 12 28 07FDEA05092 1 20071219 A 5320 65579966 WEB BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 CORROSION ON DITCHING WEB FRAMES AT BS 720E AND BS 720F, RT OF MAIN CARGO BAY, WL 208, RBL 67. BLENDED CORROSION ON DIT CHING WEB, FOUND TO BE OUT OF LIMITS. ORIGINAL .040", REMOVED .010 " REF SRM 53-10-1 DISPLACED SEAT TRACK FROM STA 720 B - 745, RBL 67 REF SRM 51-30-2. REMOVED DITCHING WEB. RECEIVED FABRICATED WEB ON N/R N00390 AND HEAT TREATED REF 8130 -200-7-12-043. DRILLED AND TRIMMED WEB REF DWG 65-57996. TREATED AND PRIMED WEB REF SRM 51-10-2. INSTALLED DITCHING W EB RE-INSTALLED DISPLACED SEAT TRACK FROM 720B - 745. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007122800008 20071228 00008 EU 2007 12 28 07FDEA05093 1 20071218 A 3260 BDM3003 PROXIMITY SENSOR AIRBUS 300 A300F4605R 3930327 EU MLG FAILED A FDEA G O2 MASK DEPLOYED N FALSE WARNING CL CLIMB 1 SO 25 661FE 11879 11879 760 AFTER T/O GEAR WOULD NOT RETRACT. SELECTED SYSTEM NR 2 STILL NO RETRACTION. HANDLE WOULD NOT GO PAST NEUTRAL POSITION. JACKED A/C REF A300-600 M/M 07-11-00-0, PERFORMED GEAR SWING AND RETRACTION REF 32-30-00-6. FOUND FAULT ON PROX BOX. REMOVED AND REPLACED PROX BOX REF A300-600 M/M 32-31-71-4. PERFORMED GEAR SWING AND RETRACTION AGAIN OPS CHECK NORMAL REF A300-600 32-30-00-6. PER MOCC REQUEST: LUBED ALL (3) LANDING GEAR AS REQUIRED PER A300-600 M/M 12-22-32-0, SWUNG TH E LANDING GEAR SEVERAL TIMES USING BOTH LANDING GEAR POSITION SYSTEMS, ONE AND TWO. A/C NOW ON 4TH LEG. 2 L 7 2 4F RT A35EU 2007122800011 20071228 00011 NM 2007 12 28 HALA0700531 1 20071219 A 2150 11518641 CONTROLLER BOEING 767 76733A 1385209 NM A/C PACK TEMP FAULTED A HALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, RIGHT PACK "INOP LIGHT ON IN AUTO POSITION. FOUND PACK TEMPERATURE CONTROLLER, "CONTROLLER FA ULT LIGHT ON." REPLACED RIGHT PACK TEMPERATURE CONTROLLER PER AMM 21-51-14. OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2007122800014 20071228 00014 NM 2007 12 28 HALA0700529 1 20071218 A 3150 WARNING LIGHT BOEING 767 76733A 1385209 NM LT FUEL PUMP FALSE ACTIVATION A HALA O OTHER N FALSE WARNING DE DESCENT 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, LT FWD FUEL PUMP EICAS LIGHT ILLUMINATED ON DESCENT. CHECKED AND PERFORMED OPERATIONAL TEST O F THE ENGINE FUEL FEED SYSTEM PER MM 28-22-00-715-001 OF THE LT FWD FUEL PUMP. PUMP OPS CHECK OK. A/C OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007122800015 20071228 00015 NM 2007 12 28 HALA0700532 1 20071218 A 3150 WARNING LIGHT BOEING 767 7673G5 1385126 NM FALSE ACTIVATION A HALA O OTHER N FALSE WARNING DE DESCENT 1 WP 13 584HA 24258 ETOPS SIGNIFICANT SYSTEM, ON DESCENT R IDG VALVE STATUS MESSAGE ILLUMINATED. CLEARED DISCREPANCY WORK DONE IAW AMM31-41 -00. ACCOMP FIM T/S PROCEDURES PER FIM24-20-00 FIG 102, CKS NORMAL. 2 L 7 2 4F RT A1NM 2007122800017 20071228 00017 NM 2007 12 28 HALA0700534 1 20071219 A 4990 SEAL BOEING 767 7673G5 1385126 NM APU OIL CAP TORN A HALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 584HA 24258 ETOPS SIGNIFICANT SYSTEM, PRIOR TO WALKAROUND FOUND OIL ON APU DOOR. FOUND APU OIL CAP SEAL TORN. REPLACED OIL CAP SEA L. NO LEAKS OK TO CONTINUE SERVICED APU WITH 4 PINTS. 2 L 7 2 4F RT A1NM 2007122800018 20071228 00018 GL 2007 12 28 SIMA200735501 2 20071218 A 7261 23073567 CARBON SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL RT ENGINE LEAKING A SIMA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 686AE 14500843 ON FLIGHT 4111, CREW REPORTED LAV SMOKE DETECTOR AND SMOKE ODOR DURING CLIMB-OUT. REMOVED AND REPLACED "0" CARBON SEAL ON RT ENG IAW MM 72-25-25. PERFORMED SEVERAL HIGH POWER RUN IAW MM 72-00-00. RAN PACKS NR 1 AND 2 OFF BLEED ALL CHECK GOOD. NO SMOKE OR ODOR WITNESSED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007122800019 20071228 00019 EA 2007 12 28 SIMA200735503 1 20071218 A 3222 STRUT CNDAIR CL600 CL6002C10 1390015 EA NLG UNDERSERVICED A SIMA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 SW 21 523AE 10152 ON FLIGHT 4342, CREW REPORTED A STEERING INOP MESSAGE AFTER TAKEOFF DECLARED EMERGENCY IN CMH. MTX SERVICED NLG SHOCK S TRUT PER WORKCARD 32-014. PERFORMED GROUND TAXI, NO DEFECTS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2007122800020 20071228 00020 SO 2007 12 28 SIMA200735502 1 20071215 A 2150 A/C PACK EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 OVERHEATED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 622AE 145108 CAE312757 ON FLIGHT 3475, NUMBER ONE PACK OVERHEATED SMOKE IN CABIN AND COCKPIT. SMOKE LASTED 20 SECONDS. PACK OVERHEAT LASTED 3 SEC. REMOVED AND REPLACED NUMBER TWO ENGINE PER AE W/C 71-000-00, OPS AND LEAK CHECK GOOD. RELEASED FROM TRIAD. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007122800021 20071228 00021 NM 2007 12 28 HALA0700550 1 20071224 A 3600 UNKNOWN BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE RT ENG BLEED UNKNOWN A HALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 13 598HA 23278 ETOPTS SIGNIFICANT SYSTEM, RT ENG BLEED OFF LIGHT ON AFTER START UNTIL POWER IS APPLIED (APPX 60 PERCENT N1) THEN OPERAT ED NORMALLY FOR REST OF FLIGHT. BIT AIR SUPPLY MODULE AS PRECAUTIONARY. NO FAULTS NOTED. OKAY FOR SVC. REFERENCE AMM 36-23-00-715-001. 2 L 7 2 4F 4 F RT A1NM E24NE 2007122800022 20071228 00022 NM 2007 12 28 HALA0700527 1 20071217 A 2841 LG1136AA01 DEU BOEING 767 76733A 1385209 NM FUEL QTY IND MALFUNCTIONED A HALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, LEFT TANK FUEL QUANTITY INDICATOR BLANK. EICAS MSG 'FUEL QTY IND' PRESENT. FUEL QUANTITY BIT E TEST SHOWS HARD FAULT CODES '63' AND 'D5'. CLEANED AND RESEATED LEFT TANK HI-Z AND LO-Z CONNECTORS, NO HELP. REMOVED AND REPLACED RT DEU PER AMM 28-41-03. OPS CHECK GOOD PER AMM 28-41-03-404-012. RESET FQP4, FAULT CLEARED. VERIFY GOOD RESET FUEL QTY PROCESSOR FAULT D5 CLEARED. INSULATION RESISTANCE TEST PER AMM 28-41-00-765-151-001, SHOWED LOW RESISTA NCE ON HI-Z TO SHIELD. CLEANED HI-Z BUSSING PLUG AND CONNECTORS AND LO-Z CONNECTOR AT LT MAIN SPAR. TEST OK FOR REMAIN ING LT MAIN UNITS. 2 L 7 2 4F RT A1NM 2007122800024 20071228 00024 NM 2007 12 28 07FDEA05097 1 20071219 A 5340 6072322 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 STRINGER CLIP IS CRACKED AT STATION 680, STRINGER 10 RIGHT REMOVED, FABRICATED, TREATED AND PRIMED, IDENTIFIED AND INSTA LLED STRINGER CLIP IAW SRM 51-10-2, 51-20-1PG 11, 51-30-2 PG4 BAC DWG 60-7232-2 AND FED EX GMM 7-0-1001 P1 ITEM 7B. 2 L 7 3 4F RT A3WE 2007122800025 20071228 00025 NM 2007 12 28 07FDEA05098 1 20071219 A 5531 65174843 SPAR BOEING 727 727233 138408A NM VERTICAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 VERTICAL STAB TIP L/E SPAR, CLOSER WEB HAS CRACK RUNNING THROUGH UPPER MOST FASTENER HOLE OF RIGHT SIDE TERMINAL FITTING LOCATION, 4.5" RBL. FABED DOUBLER, APPLIED ALODINE AND PRIMER AND INSTALLED REF DWG 65-17484, SRM 51- 10-2. CLASSIFI ED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007122800026 20071228 00026 NM 2007 12 28 07FDEA05099 1 20071219 A 5311 FX6616439 FRAME BOEING 727 727233 138408A NM BS 1166 S8L DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 MAIN CABIN FRAME HAS DEEP WEAR AT STA 1166 AND STR 8L REMOVED DAMAGE SECTION OF FRAME STA 1166 AT STR 8L. FABRICATED AND INSTALLED REPAIR DOUBLER, REF SRM 51-40-3 FIG 1. TREATED AND PRIMED REPAIR PARTS AND AREA. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007122800027 20071228 00027 NM 2007 12 28 07FDEA05100 1 20071219 A 5347 BAC1520792 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 MAIN CABIN FLOOR STRUCTURE, LEFT SIDE STA 560 TO 580, LBL 24 SEAT TRACK, INBOARD FLANGE CORRODED ON UPPER SURFACE, FOUND CORROSION TO BE OUT OF LIMITS. NO CORROSION ALLOWED, IAW P-F SRM 53-10-1, FIG 3A PG 3. REPAIRED SEAT RAIL DAMAGE SECT ION, STA 560 TO 670, LBL 24, IAW SRM 53-10-5 FIG 1 53-10-2. TREATED AND PRIMED IAW SRM 51-10-2, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007122800028 20071228 00028 NM 2007 12 28 07FDEA05101 1 20071219 A 5313 651842043 STRINGER BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 STR 5L CRACKED ON LOWER SIDE UP RIGHT AT ATTACH RIVET AT STA 353 FABRICATED NEW STINGER, TREATED AND PRIMED REF SRM 51-3 0-2 AND 51-10-2. INSTALLED STRINGER THIS IS CLASSIFIED AS A MAJOR REPAIR 2 L 7 3 4F RT A3WE 2007122800029 20071228 00029 NM 2007 12 28 07FDEA05102 1 20071219 A 5320 65C1703843 FLOOR SUPPORT BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 LWR FWD CARGO PIT, FLOOR SUPPORT Z-ANGLE HAS WIDE SPREAD CORROSION WITH A CRACK AT STA 720 RBL 25" CORROSION FROM 710-72 0D REMOVED Z-ANGLE AT FWD CARGO PIT STA 720, RBL 25" FROM 710 TO 720D REF SRM 51-30-2. LOCATED AND DRILLED HOLES ON NEW "Z" ANGLE P/N 65C17038-43, A 78432, REF 51-30-5. INSTALLED NEW Z- ANGLE, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007122800031 20071228 00031 SO 2007 12 28 SIMA200735301 1 20071215 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 21 658AE 145760 FLT 3483 SMOKE IN COCKPIT (NOT VISIBLE) ALSO DETECTED BY FLT ATTENDANT NEAR FWD CABIN AT COCKPIT DOOR. DISSIPATED WITHI N ABOUT 3 MINUTES. NO OTHER PROBLEMS NOTED. DECLARED EMERGENCY AND LANDED ASAP. NO SYSTEM OR BREAKER ABNORMALITIES NO TED. PERFORMED CABIN/COCKPIT ODOR EVENT TROUBLESHOOTING CHECKLIST AS PER ETN NR EM-72-034, ALSO PERFORMED ABNORMAL SMEL L IN THE CABIN/COCKPIT TROUBLESHOOTING PROCEDURE AS PER EMB-FIM 21-20-00-810-801A, INSPECTED ALL ELECTRICAL BUSSES, RELA Y, FUSES, AND W/S'S CONTROLLERS, PERFORMED ELEC SYSTEM TEST USING ALL ELECTRICAL SOURCES. ALL OPER TESTS GOOD. NO SMOK E/ODOR NOTED. PERFORMED FCF AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007122800033 20071228 00033 SO 2007 12 28 SIMA200735308 1 20071216 A 5320 14529063007 SUPPORT ANGLE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 662EH 145777 DURING MBV INSPECTION FOUND, ANGLE SUPPORT AT FRAME 23 RIGHT SIDE FOR AFT GALLEY SUPPORT IS CORRODED. REMOVED AND REPLA CED ANGLE SUPPORT IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007122800035 20071228 00035 SO 2007 12 28 SIMA200735306 1 20071216 A 5320 14522460009 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 662EH 145777 DURING MBV INSPECTION FOUND, FORWARD GALLEY FLOOR-SUPPORT CORRODED AT FRAME 20, NEAR CENTER OMEGA BEAM AND CARBON CROSS- MEMBER. REMOVED AND REPLACED SUPPORT IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007122800037 20071228 00037 SO 2007 12 28 SIMA200735305 1 20071217 A 5320 14522461011 DOUBLER EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 668HH 145785 DURING MBV INSPECTION FOUND, DOUBLER PLATE BETWEEN RIGHT HAT BEAM AND FLOORBEAM 21 IS CORRODED. REPLACED DOUBLER PLATE IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007122800039 20071228 00039 SO 2007 12 28 SIMA200736001 1 20071224 A 3242 98505158561 PRESSURE SWITCH EMB 135 EMB135KL 3260302 SO MLG BRAKES MALFUNCTIONED A SIMA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 842AE 145673 ON FLIGHT 3485, FLIGHT CREW NOTICED BRAKE ON LIGHT. CREW DECLARED EMERGENCY AND LANDED SAFELY IN SJT. REMOVED AND REP LACED PARK BRAKE PRESS SWITCH AND CLEANED CONNECTOR, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007122800040 20071228 00040 SO 2007 12 28 SIMA20073602 1 20071223 A 3234 7455501 CONTROL LEVER EMB 145 EMB145LR 3260212 SO MLG MALFUNCTIONED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 647AE 145222 ON FLIGHT 3619, THE CREW NOTED AFTER TAKEOFF WHEN SELECTED GEAR HANDLE UP GEAR SHOWS IN TRANSIT LIGHT LONGER THAN NORMAL . LANDING GEAR DISAGREE AND CREW NOTED THAT IT SOUNDED LIKE THE GEAR DID NOT RAISE. CREW SELECT GEAR HANDLE DOWN 3 GR EEN CREW ELECTED TO RETURN TO DFW. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW EMB 145 AMM 32-32-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007122800042 20071228 00042 2007 12 28 HALA0700536 4 20071220 A 2310 9640452011 COUPLER BOEING 767 7673CB 1385187 NM HF TRANSCEIVER DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 590HA 33467 ETOPS SIGNIFICANT SYSTEM, LEFT HF TRANSMISSION/RECEPTION INOP, ALSO DATALINK FUNCTION. REPLACED RIGHT HF COUPLER. GRD CHECK OK PER 23-11-00 BOTH NR 1 AND NR 2 HF. 2 L 7 2 4F RT A1NM 2007122800048 20071228 00048 NM 2007 12 28 AALA20072462 1 20071216 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 921AN 29522 DFW - EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A16WE 2007122800049 20071228 00049 NM 2007 12 28 HALA0700540 1 20071223 A 4990 CONTROL VALVE BOEING 767 767332 1382001 NM APU OIL TEMP MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, APU AUTO SHUTDOWN. ACCOMPLISHED ECU BITE PER FIM 49-11-00 FIG 103. REPLACED TEMP BULB, CONDI TION SAME, HIGH OIL TEMP DISPLAYED. REPLACED OIL TEMP CONTROL VALVE PER AMM 49-27-10, APU OPS CK OK. 2 L 7 2 4F RT A1NM 2007122800052 20071228 00052 SO 2007 12 28 SIMA20073603 1 20071224 A 3230 355022002 ELECTRONIC UNIT EMB 145 EMB145LR 3260212 SO MLG MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 647AE 145222 ON FLIGHT 3719, THE CREW NOTED AFTER TAKEOFF AFTER LANDING GEAR HANDLE SELECTED UP GEAR NEVER MOVED. LANDING GEAR LEVER DISAGREE ON EICAS AT APPROX 700' AGL FOLLOWED ALL AOM PROCEDURES SEVERAL TIMES GEAR WOULD NOT COME UP LANDED OVER WEIGH T AT 44,600 LBS RATE OF DESCENT LESS THAN 50'/MIN NORMAL ROLL OUT NO PROBLEMS WITH GEAR AFTER LANDING. DOWNLOADED CMC A ND FOLLOWED FIM 32-61-00-810-807. FOUND PROBLEM IN LGEU REMOVED AND REPLACED LGEU IAW EMB 145 AMM 32-32-01. PERFORMED LDG GEAR EXTENSION/RETRACTION IAW EMB 145 AMM EMB 145 AMM 32-30-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007122800055 20071228 00055 NM 2007 12 28 07FDEA05114 1 20071220 A 5347 53FX20535 CARGO TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 MAIN DECK FLOOR TIE DOWN FITTING ASSY IS CORRODED BS 950, RBL 57, WL 208 REMOVED CORROSION ON TIE DOWN FITTING, AND IS O UT OF LIMITS. DRILLED HOLES IN NEW TIE DOWN FITTING AND INSTALLED, REF SRM 51-30-2 AND SRM 51-30-5 THIS IS CLASSIFIED A S A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007122800057 20071228 00057 WP 2007 12 28 07FDEA05075 1 20071218 A 2612 HANDLE DOUG MD10 MD1010F 3022112 WP NR 1 FIRE INOPERATIVE A FDEA O OTHER O OTHER CR CRUISE 1 SO 25 393FE 46627 DURING 'C' CHK TEST FLIGHT OF ALL A/C SYSTEMS AND FUNCTION CHECKS, NR 1 FIRE HANDLE WOULD NOT OPERATE. SEQ 18 WORK ORDE R 39794 PDIS 393, 26-10 0005670 17DEC07. NR 1 ENG FIRE HANDLE WOULD NOT MOVE. SUSPECT MOISTURE AT ALTITUDE. REPLACE D NR 1 ENGINE FUEL SHUTOFF VALVE IAW MM 28-22-05-2. INSPECTED NR 1 ENG EMERGENCY SHUTDOWN SYS IAW MM 20-21-00-0. CLEAN ED AND LUBED NR 1 ENG LEADING EDGE HYD AND FUEL CABLES. REPLACED GROMMETS IAW MM 20-21-00-0. OPS CHECK PERFORMED IAW M M 28-22-05-2. CLOSED PANELS IAW MM 20-00-00. 2 L 7 3 4F RT A22WE 2007122800060 20071228 00060 WP 2007 12 28 AALA20072461 1 20071216 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 586AA 53249 DFW - EMERGENCY LIGHT AT SEAT 7D SHROUD DAMAGED. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007122800061 20071228 00061 NM 2007 12 28 AALA20072457 1 20071216 A 2740 285T0015117MODD MODULE BOEING 757 757223 1384957 NM STAB TRIM INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 666A 25300 DEN INFLIGHT T2209/16DEC DFW TO EGE, HORIZONTAL STABILIZER ASYMMETRY STATUS MESSAGE ILLUMINATED AT CRUISE. LANDED DEN W ITHOUT INCIDENT. REPLACED STABILIZER TRIM AILERON CONTROL MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007122800062 20071228 00062 NM 2007 12 28 HALA0700544 1 20071223 A 2697 CONNECTOR BOEING 767 7673G5 1385126 NM APU FIRE LOOP DIRTY A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, APU FIRE LP 2 DISPLAYED. NO APU FIRE LP 2 EICAS MSG ON INITIAL CHECK. RAN RESISTANCE CHECK. W/TEST CARD PIN 20-21-13.8 OHMS. PIN 20 TO GROUND .341 OHMS PIN 21 TO GROUND .343 M OHMS. CLEANED AND RESECURED CONNE CTORS RAN FIM, OPS CHK OK PER FIM 26-15-00. NO MSGS NOTED. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007122800063 20071228 00063 NM 2007 12 28 HALA0700541 1 20071224 A 3150 WARNING LIGHT BOEING 767 767332 1382001 NM FALSE ACTIVATION A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, BTB, R REV ISLN VALVE ILLUMINATED. ACCOMPLISHED FIM 78-34-00 FIG 113. NO FAULTS NOTED. OK F OR SERVICE. 2 L 7 2 4F RT A1NM 2007122800066 20071228 00066 2007 12 28 HALA0700547 4 20071223 A 3417 3404220 ADI BOEING 767 767332 1382001 NM COCKPIT INOPERATIVE A HALA O OTHER P NO WARNING INDICATION CR CRUISE 1 WP 13 596HA 23276 ETOPS SIGNIFICANT SYSTEM, AIRSPEED INDICATOR ON CAPT'S ADI IS INOP THE YELLOW CAUTION BAND JUMPS UP AND DOWN TO THE RED OVERSPEED BAND IN FLIGHT. REMOVED AND REPLACED CAPT'S ADI PER AMM 34-22-03-004-001 AND 34-22-03-404-026, CHECKS OK. 2 L 7 2 4F RT A1NM 2007122800067 20071228 00067 NM 2007 12 28 HALA0700548 1 20071225 A 3150 UNKNOWN BOEING 767 767332 1382001 NM UNKNOWN A HALA O OTHER N FALSE WARNING CR CRUISE 1 WP 13 598HA 23278 ETOPS SIGNIFICANT SYSTEM, 3,200 DIFFERENCE BETWEEN FUEL QUANTITY AND TOTALIZER. NO EVIDENCE OF FUEL LEAK. FUEL QTY ERR OR-PROG 2/2 ALE RT MSG DISPLAYED ON CDU AND EICAS MSG FMC DISPLAY. FUEL FLOW WAS NORMAL TOTAL 30.0/CALCULATED 26.8. RE F FRM FAULT CODE DIAGRAM CH 28 PG 14 NOTE 2. DIFFERENCE LESS THAN 4500 LBS WITHIN SYSTEM TOLERANCE. OK TO CONTINUE. 2 L 7 2 4F RT A1NM 2007122800070 20071228 00070 NM 2007 12 28 2007UALA05100 1 20071213 A 3397 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 FOUND DOOR 2L EMERGENCY LIGHT JIFFY SPLICE IS BROKEN. REMOVED AND REPLACED JIFFY SPLICE, OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007122800071 20071228 00071 NM 2007 12 28 2007UALA05101 1 20071214 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY EXIT EEL LIGHTS INOPERATIVE AT SEAT ROWS 41 RIGHT AND 42 LEFT. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007122800072 20071228 00072 NM 2007 12 28 2007UALA05102 1 20071214 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY EXIT CEILING LIGHTS INOPERATIVE FROM DOORS 3L AND 3R THRU DOORS 4L AND 4R. REPLACED BATTERY UNIT FOR BATTERY CHARGER. 2 L 7 4 4F 4 F RT A20WE E24NE 2007122800073 20071228 00073 NM 2007 12 28 2007UALA05103 1 20071213 A 3350 8100133801 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 3E INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 768UA 26919 FOUND SEAT 3E AND SEAT 2F (1 OF 2) EMERGENCY PROX LIGHTS INOPERATIVE. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007122800074 20071228 00074 NM 2007 12 28 2007UALA05104 1 20071213 A 3040 SWITCH BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE WINDSHIELD HEAT FAULTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 774UA 26936 LEFT FWD WINDSHIELD HEAT INOPERATIVE. FOUND FAULTY SWITCH. REPLACED LT FWD SWITCH CAP AND MODULE, OPERATIONAL CHECK GO OD. A/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007122100014 20071221 00014 SO 2007 12 21 FDKA200709512 1 20070930 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 FDM 6089 MCO (0630 PHX LCL). SIDEWALL EMERGENCY DOOR EXIT LIGHT INOPERATIVE. MX RESET LIGHT, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2007122100015 20071221 00015 SO 2007 12 21 FDKA200710551 1 20071015 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 FDM 6093 ROC (0515 PHX LCL). LEFT WING EMERGENCY EXIT SIGN INOP. MX RESET LIGHT, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007122100019 20071221 00019 SO 2007 12 21 FDKA200711329 1 20071109 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO LT OVERWING INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 FDM 6127 FLL (0455 PHX LCL). LEFT WING EMERGENCY EXIT SIGN INOP. MX RE-SEATED CONNECTOR. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007122100020 20071221 00020 SO 2007 12 21 FDKA200711334 1 20071113 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 FDM 6179 JFK (0655 PHX LCL). LEFT DOOR EMERGENCY LIGHT INOP AT ROW 12. MX RESET EMERGENCY LIGHT SYSTEM, OPS CHECK GOOD . 2 L 7 2 4T RT T00011AT 2007122100027 20071221 00027 SO 2007 12 21 FDKA200709486 1 20070924 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO ROW 3 INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6118 MCO (0738 PHX LCL). ROW 3 BULKHEAD EMERGENCY LIGHT INOP. RESET EMERGENCY LIGHTS, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007122100028 20071221 00028 SO 2007 12 21 FKDA200710517 1 20071002 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6074 JFK (1445 PHX LCL). FWD BULKHEAD EMERGENCY EXIT LIGHT INOP. MX CLEANED AND RE-SECURED CONNECTORS ON LIGHT ASS Y, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007122100032 20071221 00032 NM 2007 12 21 ZZDA2007311 1 20071207 A 5230 J060228J3 PAN BOEING 717 717200 1383700 NM FWD CARGO DOOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 947AT 55010 FWD CARGO DOOR THRESHOLD CORRODED BEYOND LIMITS. REPLACED THRESHOLD PAN IAW B717 SRM 53-20-15. 2 L 7 2 4F TR A6WE 2007122100042 20071221 00042 WP 2007 12 21 ABXA070400 1 20071019 A 5755 3923255504 SUPPORT DOUG DC9 DC941 302207N WP RT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 RIGHT INBOARD SPOILER TORSION BAR CENTER SUPPORT CRACKED IN THREE (3) PLACES. REPLACED SUPPORT ASSEMBLY IN ACCORDANCE W ITH DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2007122100066 20071221 00066 NM 2007 12 21 SWAA076168 1 20071211 A 5752 6546455 TAB BOEING 737 7373H4 1384600 NM RT WING AILERON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED 22Y CHECK, FOUND RT WING AILERON TAB CRACKED. REMOVED AND REPLACED TAB PER MM. 2 L 7 2 4F RT A16WE 2007122100076 20071221 00076 NM 2007 12 21 SWAA076160 1 20071211 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122100078 20071221 00078 NM 2007 12 21 SWAA076161 1 20071211 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007122100090 20071221 00090 2007 12 21 SWAA076167 4 20071211 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR READS LOW A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 784SW 29810 L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007122100102 20071221 00102 NM 2007 12 21 WRLA2007134 1 20071210 A 2530 2510003205 OVEN DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE GALLEY FAULTY A WRLA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 276WA 48632 DURING OVEN OPERATIONS, ELECTRICAL BURNING ODOR DETECTED. OVEN SHUT OFF AND BREAKERS PULLED. ODOR WENT AWAY. REMOVED AND REPLACED OVEN IAW MM 25-35-10. OPS CHECK GOOD. 2 L 7 3 4F 4 F RT A22WE E24NE 2007122100106 20071221 00106 SO 2007 12 21 C2XA07TY080 1 20071210 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO CABIN ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13118 145675 BURNING ELECTRIC ODOR IN COCKPIT AND FRONT OF GALLEY AREA IN FRONT OF SEAT 1A. DETECTED ODOR AFTER LANDING AND INCREASE D ON THE WAY TO THE GATE. MX INSPECTED AREA AND RELAYS. NO DEFECTS FOUND. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT 2007122100107 20071221 00107 SO 2007 12 21 C2XA07CL103 1 20071212 A 3260 8005701 PROXIMITY SWITCH EMB 135 EMB135ER 3260203 SO NLG CORRODED A C2XA O OTHER N FALSE WARNING CL CLIMB 1 SW 27 17507 145215 CLE FLIGHT 2419 - THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. MAINTENANCE INSPECTED AND REP LACED THE NOSE LANDING GEAR WOW PROXIMITY SWITCH AND HARNESS. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT T00011AT 2007122100110 20071221 00110 NM 2007 12 21 CALA0700741 1 20071208 A 5311 6546555 FRAME BOEING 737 7373T0 1384582 NM BS 867 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 FUSELAGE FRAME CRACKED AT STA 867 BETWEEN STR 8 & 9 RIGHT. REPAIRED PER EA5310-04498. 2 L 7 2 4F RT A16WE 2007122100115 20071221 00115 2007 12 21 ASAA0752379 4 20071212 A 2397 8220987004 COUPLER BOEING 737 737890 1384527 NM HF ANTENNA DAMAGED A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 584AS 35682 NR 1 HF FAILED TO TRANSMIT. CONFIRMED FAILURE ON GROUND. REPLACED NR 1 HF ANTENNA COUPLER. OP CHECK & FVF GOOD. 2 L 7 2 4F RT A16WE 2007122100116 20071221 00116 WP 2007 12 21 ASAA0782377 1 20071212 A 5311 591359577 FRAME DOUG DC9 DC983 3022083 WP BS 1418 S2R CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 944AS 53019 AFT ACCESSORY COMPT FRAME STA 1418 CRACKED AT LONGERON 2R. REMOVED DAMAGED SECTION OF FRAME LOCATED DRILLED AND INSTALL ED A REPLACEMENT FRAME SECTION IAW MD 80 SRM 51-30-2 PG 1 AND 51-30-5 PG 1 AND ASA EA 5310 02749. 2 L 7 2 4F RT A6WE 2007122100119 20071221 00119 WP 2007 12 21 ABXA070424 1 20071208 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932F 3022067 WP EMERGENCY LIGHTS DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 905AX 47147 CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-02-4. 2 L 7 2 4F A6WE 2007122100127 20071221 00127 NM 2007 12 21 SWAA076223 1 20071213 A 3350 3071BPEGPL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED BRDG CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2007122100128 20071221 00128 NM 2007 12 21 SWAA076245 1 20071213 A 5311 6546526 FRAME BOEING 737 7373Q8 1384670 NM BS 400 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122100129 20071221 00129 NM 2007 12 21 SWAA076246 1 20071213 A 5311 6545808 FRAME BOEING 737 7373Q8 1384670 NM BS 294 S17R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED BRDG CHECK, FOUND STUB FRAME CRACKED AT BS 294.5, STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2007122100134 20071221 00134 NM 2007 12 21 SWAA076225 1 20071213 A 5753 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW BN961 26590 DURING SCHEDULED HC2 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED AT LOWER SURFACE. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007122100136 20071221 00136 NM 2007 12 21 SWAA076226 1 20071213 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 435WN 32455 EEPLS COVER MISSING AT ROW 11 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2007122100141 20071221 00141 NM 2007 12 21 SWAA076243 1 20071213 A 5523 SKIN BOEING 737 7375H4 138449D NM RT ELEVATOR TAB DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 3779001 24185 DURING SCHEDULED BRDG CHECK, FOUND RT ELEVATOR TAB DELAMINATED. REMOVED AND REPLACED TAB PER MM. 2 L 7 2 4F RT A16WE 2007122700005 20071227 00005 2007 12 27 USAASA07082 4 20071211 A 2211 3945123506 COMPUTER AIRBUS A319 A319112 3930323 EU AUTOPILOT INTERMITTENT A USAA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CR CRUISE 1 EA 19 769US 27167 320 1391 CLT - FLT 1480 EN ROUTE MSP TO CLT. DURING THE FLIGHT, AUTOPILOT 2 DISENGAGED. THE CREW RE-ENGAGED THE AUTOPILOT, AND IT DISCONNECTED AGAIN, ALONG WITH AUTOPILOT 1. AFTER HAND FLYING FOR ABOUT 20 SECONDS, THE STAB TRIM WHEEL JERKED WHIL E AUTO-TRIMMING, THEN JAMMED IN ONE POSITION. THE FLIGHT CONTINUED TO CLT. AFTER LANDING, THE STABILIZER UNJAMMED AND CENTERED ITSELF. MAINTENANCE PERFORMED A SYSTEM TEST OF THE THS SYSTEM. NO FAULTS WERE NOTED. THE ELAC 1 WAS THEN REP LACED AS A PRECAUTION. A LAND VERIFY TEST WAS PERFORMED AND THE AIRCRAFT WAS CERTIFIED FOR CAT 111 STATUS. 2 L 7 2 4F RT A28NM 2007122700011 20071227 00011 EA 2007 12 27 A6WA200740647 1 20071202 A 2752 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA O OTHER J WARNING INDICATION LD LANDING 1 GL 31 458AW 7861 DURING MISSED APPROACH WHEN FLAP HANDLE MOVED TO 8 DEGREES, FLAP FAIL CAS MESSAGE ILLUMINATED AND FLAP STAYED AT 45 DEGR EES. ALL 8 FLAPS ACTUATORS REPLACED ALSO RIGHT BPSU UNIT. REPLACED UE TO FLUCTUATION CAUSING JAMMING. FLAP SYSTEM. O PS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007122700014 20071227 00014 EA 2007 12 27 A6WA200740652 1 20071130 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA ILLUMINATED A A6WA O OTHER N FALSE WARNING CR CRUISE 1 GL 31 402AW 7281 FLAP FAIL CAUTION MESSAGE IN FLIGHT AT FLT LEVEL 260 AND FLAPS AT 0. COMPLIED WITH QRH. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4, FLAP SYSTEM RESET OK. (M) 2 L 7 2 4F RT A21EA 2007122700022 20071227 00022 NM 2007 12 27 SWAA076190 1 20071213 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700046 20071227 00046 NM 2007 12 27 SWAA076220 1 20071213 A 5311 6546595 FRAME BOEING 737 7373TO 138447G NM BS 727A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700047 20071227 00047 NM 2007 12 27 SWAA076219 1 20071213 A 5311 6546558 FRAME BOEING 737 7373TO 138447G NM BS 907 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700051 20071227 00051 NM 2007 12 27 SWAA076215 1 20071213 A 5311 65C25229 FRAME BOEING 737 7373TO 138447G NM BS 727D S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700055 20071227 00055 NM 2007 12 27 SWAA076209 1 20071213 A 5311 6546525 FRAME BOEING 737 7373TO 138447G NM BS 380 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700056 20071227 00056 NM 2007 12 27 SWAA076208 1 20071213 A 5311 6546554 FRAME BOEING 737 7373TO 138447G NM BS 867 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700058 20071227 00058 NM 2007 12 27 SWAA076206 1 20071213 A 5311 6546552 FRAME BOEING 737 7373TO 138447G NM BS 827 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700078 20071227 00078 NM 2007 12 27 USAA920071329 1 20071213 A 5754 SKIN BOEING 737 737301 1384611 NM NR 2 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 23742 CLT - MAJOR REPAIR - C-4 CHECK, DELAMINATION AT INBOARD AND OUTBOARD ENDS OF NR 2 SLAT. REMOVED AND REPLACED NR 2 SLAT IAW US AIRWAYS JOB CARD J3-11-27300, STEP A-B. 2 L 7 2 4F RT A16WE 2007122700079 20071227 00079 NM 2007 12 27 USAA920071330 1 20071214 A 5313 6517685 STRINGER SPLICE BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 23742 CLT - MAJOR REPAIR - C-4 CHECK, A CRACK FOUND ON STRINGER SPLICE AT BS 360, S15L. REMOVED AND REPLACED STRINGER SPLICE AT BS 360, S15L IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2007122700082 20071227 00082 NM 2007 12 27 ZZDA2007313 1 20071212 A 5347 5971207503 SEAT TRACK BOEING 717 717200 1383700 NM COCKPIT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 948AT 55011 FIRST OFFICER'S AFT LOWER I/B SEAT TRACK CORRODED. FABRICATED SEAT TRACK FROM RAW STOCK, P/N IDI774T PER DRAWING 597120 7 AND EA 17-53-008951R, REPLACED PER B717 SRM 51-41-01. 2 L 7 2 4F TR A6WE 2007122700083 20071227 00083 NM 2007 12 27 ZZDA2007314 1 20071213 A 5321 FLOOR PANEL BOEING 717 717200 1383700 NM COCKPIT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 948AT 55011 FLIGHT COCKPIT RIGHT HAND FLOOR PANEL NR 211 AMF HAS CORROSION AT I/B AFT CORNER - CORROSION OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOULBERS 2" X 2.5" .040 AND FILLER (1 X 1 X.032) IAW B717 SRM 53-10-50. RO 046561 2024T3.040, PO 0 46316 2024T3 .032 AT I/B AFT OF PANEL 211AMF. 2 L 7 2 4F TR A6WE 2007122700090 20071227 00090 NM 2007 12 27 SWAA076270 1 20071216 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727B S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007122700091 20071227 00091 NM 2007 12 27 SWAA076269 1 20071216 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 597 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2007122700104 20071227 00104 NM 2007 12 27 SWAA076261 1 20071215 A 3350 8200037740 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 472WN 33831 R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007122700109 20071227 00109 NM 2007 12 27 SWAA076266 1 20071216 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM BS 380 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700111 20071227 00111 NE 2007 12 27 HNAA0600292 2 20071210 A 7261 OIL SYSTEM DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE LOW A HNAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 936HA 145 120418 ACFT YAWED TO THE LEFT ON CLIMBOUT, CREW NOTED NR 1 ENG TQ WAS AT 30 PERCENT. ALL OTHER ENG INST APPEARED NORMAL. CREW SHUTDOWN AND DECLARED AN EMERGENCY AND RETURNED TO PHL. MX INSPECTED NR 1 ENG AND ONLY DEFECT NOTED WAS ENG 2 QTS LOW ON OIL. SERVICED ENG AND CREW PERFORMED 3 HIGH POWER RUNS WITH NO DEFECTS NOTED. ACFT FERRIED FROM PHL TO ROA. ROA RE MOVED AND REPLACED NR 1 HMU AND FUEL PUMP AND REMOVED AND REPLACED EEC. 2 H 7 2 4T 4 T RT A13NM E20NE 2007122700128 20071227 00128 NM 2007 12 27 SWAA076322 1 20071217 A 5311 6546558 FRAME BOEING 737 7373Q8 1384670 NM BS 907 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700133 20071227 00133 NM 2007 12 27 SWAA076274 1 20071214 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 934 S22R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 22R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007122700146 20071227 00146 NM 2007 12 27 SWAA076293 1 20071217 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 488WN 33853 DURING SCHEDULED HC1 CHECK, LT FWD CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PAC K PER MM. 2 L 7 2 4F RT A16WE 2007122700150 20071227 00150 NM 2007 12 27 SWAA076317 1 20071217 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 277 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BDRG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2007122700155 20071227 00155 NM 2007 12 27 SWAA076282 1 20071217 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8L/R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700163 20071227 00163 NM 2007 12 27 SWAA076319 1 20071217 A 5753 65C348124 FLAP TRACK BOEING 737 7373G7 1384595 NM NR 7 TE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND RT WING NR 7 OUTBOARD FLAP INBOARD TRACK FITTING CORRODED. REPAIRED FLAP TRACK PER S WA EA. 2 L 7 2 4F RT A16WE 2007122700177 20071227 00177 NM 2007 12 27 SWAA076327 1 20071214 A 5753 SKIN BOEING 737 7377H4 1384404 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 708SW 27842 DURING SCHEDULED SPV CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP INBOARD LOWER CORNER DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007122700192 20071227 00192 NM 2007 12 27 BB07100 1 20071217 A 3610 312N53217 DUCT BOEING 757 757225 1384959 NM BLEED SYSTEM LEAKING A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 918UW 14085 979 22196 FLIGHT 790, CLT-BOS: AIRCRAFT DIVERTED TO PHL DUE TO A NUMBER 2 ENGINE OVERHEAT MESSAGE. CREW REDUCED THROTTLE TO IDLE AND WARNING WENT AWAY. MAINTENANCE REPLACED THE HP2 AND HP6 BLEED DUCTS. NO FURTHER FAULTS. 2 L 7 2 4F RT A2NM 2007122700194 20071227 00194 NM 2007 12 27 USAA920071347 1 20071206 A 5313 65516981 STRINGER BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C-16 CHECK - STRINGER CRACKED AT BS 907, S4L. REMOVED AND REPLACED STRINGER SPLICE AT BS 907, S4L IAW B737-300 SRM 51-40-02-0G FIG 8, 3, AND 12. 2 L 7 2 4F RT A16WE 2007122800012 20071228 00012 NM 2007 12 28 HALA0700528 1 20071219 A 2920 PACKING BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE HYD PUMP LEAKING A HALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, DURING WALKAROUND, NOTICE HYD FLUID LEAKING FROM NR 1 ENG. FOUND HYD FLUID LEAKING FROM HYD E NG PUMP PACKING AT PRESSURE PORT REPLACED PACKING, SERVICED NR 1 SYSTEM. SYSTEM OPS CHECK LEAK CHECK GOOD. OK FOR SERV ICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007122800013 20071228 00013 NM 2007 12 28 HALA0700530 1 20071219 A 2822 5006003D PUMP BOEING 767 767332 1382001 NM FUEL BOOST MALFUNCTIONED A HALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, L FWD FUEL PUMP MSG AND PRESS LIGHT ON SWITCH WITH SWITCH IN. REPLACED L FWD BOOST PUMP PER A MM 28-22-03. OPS CHECK GOOD. LEAK CK GOOD. 2 L 7 2 4F RT A1NM 2007122800032 20071228 00032 SO 2007 12 28 SIMA200735307 1 20071216 A 5320 14522459003 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 662EH 145777 DURING MBV INSPECTION FOUND RAMP FLOOR SUPPORT CORRODED AT FRAME 20 NEAR CARBON CROSS MEMBER. REMOVED AND REPLACED SUPP ORT IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007122800034 20071228 00034 SO 2007 12 28 SIMA200735303 1 20071218 A 5320 14525480 SILL EMB 145 EMB145LR 3260212 SO CARGO DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 673AE * 5000 145797 DURING IMBV INSPECTION, THE CARGO DOOR CUT OUT CENTER SILL WAS FOUND TO BE CORRODED. REPLACED THE CARGO DOOR CUT OUT CE NTER SILL PER EMBRAER SRM (SRM-145/1142 REV 38) CHAPTER 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007122800043 20071228 00043 NE 2007 12 28 HALA0700537 2 20071220 A 7230 BLADE BOEING 767 767300 1385204 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 582HA 28139 729024 ETOPS SIGNIFICANT SYSTEM, NR 1 ENG NR 1 BLADE HAS TEAR ON LEADING EDGE APPROX 3/4 INCH FROM TIP, APPROX 1/8 INCH DEEP AN D 1/8 INCH WIDE, AREA A. BLENDED BLADE ON NR 1 ENG PER AMM 72-31-02. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007122800044 20071228 00044 WP 2007 12 28 ARWA20071205 1 20071218 A 2130 SNAP RING DOUG DC8 DC863F 302198F WP NR 2 TC DEFUSER LOOSE A ARWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 784AL 46135 DURING CLIMB-OUT, UNABLE TO CONTROL THE CABIN PRESSURIZATION, NEITHER WITH AUTO OR MANUAL (WITH 4 T.C. ON). FOUND NR 2 TC DISFUSER SNAP RING LOOSE. REINSTALLED SNAP RING AT NR 2 TC IN ACCORDANCE WITH DC-8 M/M 21-10-6. PRESSURIZATION CHEC K FOUND NORMAL IN ACCORDANCE WITH DC-8 M/M 21-31-0. 2 L 7 4 4F 4A25 2007122800045 20071228 00045 WP 2007 12 28 AALA20072459 1 20071216 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 586AA 53249 DFW - EMERGENCY LIGHT AT SEAT 12D SHROUD DAMAGED. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007122800047 20071228 00047 WP 2007 12 28 AALA20072460 1 20071216 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 586AA 53249 DFW - EMERGENCY LIGHT AT SEAT 10D SHROUD DAMAGED. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007122800050 20071228 00050 2007 12 28 HALA0700539 4 20071221 A 2310 9460453011 COUPLER BOEING 767 7673CB 1385187 NM HF TRANSCEIVER DAMAGED A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 590HA 33467 ETOPS SIGNIFICANT SYSTEM, LEFT SIDE HF EICAS MESSAGE HF DATA LINK DISPLAYED, UNABLE TO CHANNEL. REPLACED NR 1 HF COUPLE R PER AMM 23-11-00. GRD OPS CHECK AND TEST OKAY. 2 L 7 2 4F RT A1NM 2007122800064 20071228 00064 NM 2007 12 28 HALA0700545 1 20071223 A 3150 WARNING LIGHT BOEING 767 76733A 1385209 NM INTERMITTENT A HALA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 WP 13 587HA 33421 ETOPS SIGNIFICANT SYSTEM, RIGHT PACK OFF LIGHT DOES NOT COME ON WHEN RIGHT PACK SELECTED OFF. LIGHT TEST OK PACK DOES S HUT DOWN. CYCLED RT PACK SW 3X OPS CHK OK NO DEFECTS NOTED CAN NOT DUPLICATE WRITE UP, OK FOR SVC, RT PACK OPS CHK (NOR MAL) OPS CK OK PER AMM 21-52-00. OK FOR SVC. 2 L 7 2 4F RT A1NM 2007122800068 20071228 00068 EU 2007 12 28 07FDEA05059 1 20071214 A 2410 IDG AIRBUS 300 A300B4605R 3930308 EU NR 2 UNDERSERVICED A FDEA B EMER. DESCENT W INADEQUATE Q C CL CLIMB 1 SO 25 733FD 715 ON TAKEOFF ROLL AT IND, ABOUT 50 KTS NR 2 GENERATOR FAULTED, ACCOMPLISHED RTO CK LIST, AND RESET GEN, AFTER RESET WORKED OK. FOUND IDG UNDER SERVICED, SERVICED PER AB MM 24-11-00-3-02, RAN ENG OPS CK OK. FOUND IDG UNDER SERVICED, SERVICED PER AB MM 24-11-00-3-02, RAN ENG OPS CK OK. 2 L 7 2 4F RT A35EU 2007122800075 20071228 00075 NM 2007 12 28 2007UALA05105 1 20071213 A 3397 8100035701 TERMINAL BLOCK BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 215UA 30221 SIDE EEL LIGHTS OF MID GALLEY, 3 EA, INOP. FOUND TERMINAL BLOCK BROKEN. REPLACED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007122800079 20071228 00079 NM 2007 12 28 P5CA0701540 1 20071118 A 5410 ACCESS DOOR BOEING 747 74747UF 1384812 NM NR NACELLE INFLT SEPARATION A P5CA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 EA 15 416MC 32838 NR 4 ENGINE STRUT I/B ACCESS DOOR PARTIALLY LOST IN FLIGHT AND NR 4 ENGINE STRUT O/B ACCESS DOOR PEELED BACK IN FLIGHT. MAJOR REPAIR AND PARTS REPLACEMENT ACCOMPLISHED PER XEO-51-120607, P/N: 323U2304-84, 323U2303-72. 2 L 7 4 4F RT A20WE 2007122800080 20071228 00080 EU 2007 12 28 SIMA200735103 1 20071216 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 263AE 340B263 CREW REPORTED FWD EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED FWD BATTERY PACK 2LA. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007122800082 20071228 00082 SO 2007 12 28 SIMA200735102 1 20071215 A 3150 WARNING LIGHT EMB 145 EMB145 3260210 SO ILLUMINATED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 613AE 145081 CREW REPORT LANDING GEAR AIR GROUND FAIL MSG ON TAKEOFF AND GEAR WOULD NOT INITIALLY RETRACT. CREW DID GET GEAR UP. AL SO RECEIVED BLEED 2 CLOSED MESSAGE. AC LANDED WITHOUT INCIDENT. 2 L 7 2 4F RT T00011AT 2007122800083 20071228 00083 SO 2007 12 28 SIMA200735104 1 20071214 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO BS 236 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 673AE 9225 5000 145797 DURING MBV INSPECTION, THE FRAME AT FS 236.5 WAS FOUND TO BE CORRODED. REPAIRED FRAME AT FS 236.5 PER SAAB SRM (72LKS 3 079 REV 49) CHAPTER 53-70-30. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007122800085 20071228 00085 SO 2007 12 28 SIMA200735106 1 20071212 A 3350 110049 POWER SUPPLY EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHTS INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 808AE 145519 CREW REPORTED PART OF THE EMERGENCY LIGHTS NOT WORKING. REMOVED AND REPLACED NR 1, NR 2, NR 3, NR 4 BATTERY POWER SUPPL IES IAW EMB 140 AMM 33-50-04. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007122800087 20071228 00087 NM 2007 12 28 UPS07M51288 1 20071105 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1381-1501 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C CABIN, CORROSION ON SEAT TRACK CROWN AND CHANNEL AT STA1381 - 1501 X=-8. CORROSION REMOVED FOUND EXCE EDED LMT PER SRM 53-70-00 FIG3 VIR 35. DAMAGED SEAT TRACK SECTIONAL CUT-OUT AND REMOVED BTW STA 1411-1531 PER SRM 51-3 1-01 VIIR 35. HFEC INSP C/O PER DAC NDT SPM, R13,PT06-10-01.001 ON CUT-OUT AREA, FOUND NO CRACK EVIDENT. REPAIR SEAT T RACK AND SPLICE FABRICATED AND INSTALLED PER SRM 51-31-01VIR 35. 2 L 7 3 4F RT A22WE 2007122800088 20071228 00088 NM 2007 12 28 UPS07M51289 1 20071105 A 5313 LONGERON SPLICE DOUG MD11 MD11 3023602 NM BS 1535 L40L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C CTR CARGO/AT STATION 1535 LONGERON 40 LT FOUND DOUBLER WITH SUSPICIOUS CRACKED AS MARKED. HFEC C/O IA W DAC NDT SRM R13, PT06-10-01.001 ON CRACKED AREA. CRACK CONFIRMED APPROX 1 INCH LONG. CRACKED LONGERON SPLICE REMOVED . NEW SPLICE FAB FROM EXTRUSION 1D1104-T150-T61511 PER SRM 53-15-01VIIIR 35 AND SRM 51-1 0-01 VIIR 35. FPI C/O ON NEW SPLICE, FOUND NO CRACK EVIDENT. NEW LONGERON SPLICE INSTALLED PER SRM 51-33-01 VIIR 35. 2 L 7 3 4F RT A22WE 2007122800089 20071228 00089 NM 2007 12 28 UPS07M51290 1 20071030 A 5753 SKIN DOUG MD11 MD11 3023602 NM TE FLAP DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C LT WING I/B FLAP O/B LOWER SEGMENT LOWER SURFACE FOUND NUMEROUS DENTS. LT I/B FLAP O/B SEGMENT REMOVE D PER CMM 51-52-03R59. LHW I/B FLAP O/B LOWER SEGMENT SKIN REMOVED PER SRM51-35-01VIIR 35. NEW SKIN FAB USING 2024T3-0 .040" MAT'L PER DOUGLAS DWG ARC2444, REV J. FASTENER HOLES DRILLED ON NEW SKIN AND REPROTECTED. NEW SKIN INSTL PER SRM 51-35-01 VIIR 35. LHW I/B FLAP O/B SEGMENT INSTALLED PER CMM 57-52-03 REV 59. 2 L 7 3 4F RT A22WE 2007122800090 20071228 00090 NM 2007 12 28 UPS07M51291 1 20071030 A 5753 SKIN DOUG MD11 MD11 3023602 NM LT WING TE FLAP DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C LT WING I/B FLAP I/B LOWER SEGMENT LOWER SURFACE FOUND NUMEROUS DENTS. LT I/B FLAP I/B SEGMENT REMOVE D AND SKIN REMOVED PER SRM 51-35-01VIIR 35. NEW SKIN FAB USING 2.24-T3 0.040" MAT'L PER DOUGLAS DWG ARC2736 REV B. FAS TENER HOLES DRILLED ON NEW SKIN AND REPROTECTED PER SRM 51-21-01VIIR 3. 5. NEW SKIN INSTALLED PER SRM 51-35-01 VIIR35. LHW I/B FLAP I/B SEGMENT INSTALLED AS PER CMM57-52-03 REV59. 2 L 7 3 4F RT A22WE 2007122800091 20071228 00091 NM 2007 12 28 UPS07M51295 1 20071119 A 5730 SKIN DOUG MD11 MD11 3023602 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C LHW L/E LOWER ACCESS STA XORS 538 AT O/B REFUELING RECEPTACLE TOP FOUND CORRUGATED SKIN CRACKED AS MAR KED. LHW L/E LWR CAVITY BEADED SKIN FASTENERS AT DAMAGED AREA AND ATTACH PARTS REMOVED. DAMAGED AREA ON BEADED DOUBLER TRIMMED OFF PER SRM 57-10-0 0 FIG 27R40VI. HFEC C/O ON TRIMMED EDGE, FOUND NO CRACK EVIDENT. REPAIR DOUBLER, FILLER A ND ANGLES FABRICATED. REPAIR PARTS REPROTECTED/PAINTED SRM 51-21-01VIIR35. REPAIR PARTS INSTALLED PER SRM 57-10-00 FI G 27 VIR 40. 2 L 7 3 4F RT A22WE 2007122800096 20071228 00096 NM 2007 12 28 2007UALA05000 1 20071207 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 LT OVERWING EMERGENCY EXIT LIGHT INOP, 2ND FROM AFT. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007122800097 20071228 00097 NM 2007 12 28 2007UALA05001 1 20071207 A 3397 794640 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 FOUND GALLEY G5B OUTBOARD WALL EEL INOP. REPAIRED EEL CABLE 2 L 7 4 4F 4 F RT A20WE E24NE 2007122800098 20071228 00098 NM 2007 12 28 2007UALA05002 1 20071206 A 3350 1317 LAMP BOEING 727 727222 1384073 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 769UA 26921 SEAT 1E AFT EMERGENCY LIGHT ON ARMREST BROKEN OFF. RELAMPED. 2 L 7 3 4F 4 F A3WE E46NE 2007122800099 20071228 00099 NM 2007 12 28 2007UALA05003 1 20071206 A 3350 5661373 LENS BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 775UA 26947 FOUND SEAT 3F EEL LIGHT COVER IS MISSING. REPLACED LENS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007122800104 20071228 00104 NM 2007 12 28 2007UALA05110 1 20071216 A 2611 21198356 SMOKE DETECTOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE AFT CARGO BAY FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 223UA 30224 DET ZONE 1 CARGO AFT AFT CARGO COMPARTMENT SMOKE DETECTOR ZONE FAILURE, SUSPECT SMOKE DETECTOR AT FAULT. REPLACED AFT PI T SMOKE DETECTOR. OPS CHECKED GOOD. AC OK FOR SERVICE 2 L 7 2 4F 4 F RT T0001SE E46NE 2007122800106 20071228 00106 NM 2007 12 28 2007UALA05112 1 20071214 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 271 S20L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 FUSELAGE EXT SKIN IS DENTED AT APPROX BS 271, JUST BELOW STR 20L. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007122800110 20071228 00110 NM 2007 12 28 2007UALA05116 1 20071215 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 1006 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 CABIN DIAGONAL FLOOR SUPPORT CORRODED BS 1006 LBL 1" - 6". MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW FLOOR SUPPORT. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122800112 20071228 00112 NM 2007 12 28 2007UALA01692 1 20070526 A 2782 6544551 ACTUATOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE SLAT BROKEN A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 933UA 26659 LEADING EDGE TRANSIT LIGHT ON AFTER RETRACT. REPLACED ACTUATOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122800113 20071228 00113 NM 2007 12 28 2007UALA05026 1 20071207 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 DOOR R4 HANDLE BOX HAS CORROSION AROUND AND IN INSERTS AND IN SHAFT FOR HANDLE MECHANISM. INSTALLED NEW HANDLE BOX. 2 L 7 2 4F 4 F RT A2NM E17NE 2007122800118 20071228 00118 NM 2007 12 28 2007UALA05124 1 20071217 A 2780 SLAT SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LOCKED A UALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 WP 29 812UA 850 AIRCRAFT LANDED WITH SLATS LOCKED-FLAPS 3 IAW ECAM. REPLACED SFCC 2, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2007122800119 20071228 00119 NM 2007 12 28 2007UALA05125 1 20071217 A 4900 APU BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SHUTDOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 771UA 26932 APU SHUT DOWN AT GATE FOR NO APPARENT REASON. REPLACE APU OIL CLUSTER, OPS CHECKED NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007122800121 20071228 00121 NM 2007 12 28 2007UALA05127 1 20071216 A 3397 WIRE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 850UA 1653 WIRES THAT SUPPLY POWER TO THE EMERGENCY LIGHTS AT ROW 16ABC ARE PULLED UP. REPLACED AND RESECURED EEL LIGHT WIRING AT SEAT LOCATIONS 15,16 ABC. 2 L 7 2 4F 4 F RT A28NM E40NE 2007122800125 20071228 00125 NM 2007 12 28 07FDEA05105 1 20071220 A 3260 LIGHT BOEING 727 727233 138408A NM MLG INDICATOR INOPERATIVE A FDEA A UNSCHED LANDING P NO WARNING INDICATION DE DESCENT 1 SO 25 266FE 21672 UNSAFE NOSE GEAR INDICATION. NO GREEN NOSE GEAR LIGHT WHEN GEAR HANDLE DOWN. FOLLOW CHECKLIST TO LOWER NOSE GEAR MANUA LLY, THAT WAS UNSUCCESSFUL. NO GREEN LIGHT. GREEN LIGHT TESTED GOOD WHEN DEPRESSING LENS CAP BUT WOULD NOT TEST GOOD WHEN USING APD TEST LIGHT SWITCH. RED GEAR LIGHT REMAINED OUT. REMOVED AND REPLACED NOSE LANDING GEAR GREEN LIGHT CAPS ULE ASSY IAW B727-200 SMP. PERFORMED OP'S CK OF NLG LIGHTS IAW MM 32-61-071-5. NLG POSITION LIGHTS, OP'S CK'D GOOD. 2 L 7 3 4F RT A3WE 2007122800127 20071228 00127 EU 2007 12 28 TRAX200701900 1 20071210 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 FOUND FLOORBEAM 36 CORRODED. 2 H 7 2 4T RT A53EU 2007122800128 20071228 00128 EU 2007 12 28 TRAX200701901 1 20071210 A 5320 INTERCOSTAL AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 CRACK FOUND ON RT O/B INTERCOSTAL BTW FUSELAGE FAIRING FR 23D TO FUSELAGE. 2 H 7 2 4T RT A53EU 2007122800130 20071228 00130 EU 2007 12 28 TRAX200701903 1 20071210 A 5753 BRACKET AEROSP ATR72 ATR72212 8680945 EU LT WING TE FLAP CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 LT I/B FLAP O/B FLAP ARM OMEGA BRACKET CRACKED. 2 H 7 2 4T RT A53EU 2007122800131 20071228 00131 EA 2007 12 28 TRAX200701904 1 20071210 A 2150 BLEED AIR SYS CNDAIR CL600 CL6002B19 1900309 EA ODOR A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 977EV 7720 OIL/GAS/GREASE ODOR ON DESCENT AND WHEN SWAPPING BLEEDS FROM APU TO ENGINES. OILY AND MOLDY ODOR WHEN TRANSFERRING BLEE D TO APU, FLT 4373 DEL 42 MINS. 2 L 7 2 4F RT A21EA 2007122800132 20071228 00132 EA 2007 12 28 TRAX200701907 1 20071211 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 905EV 7632 DURING OPS TEST OF EMERG LIGHTING SYSTEM, THE FLOOR LEVEL EXIT LIGHTS AT THE LT/RT OVERING EXITS, FWD OF THE SERVICE DOO R, AND ON THE AFT FACE OF THE GALLEY ARE INOP, 4 LIGHTS TOTAL. 2 L 7 2 4F RT A21EA 2007122800135 20071228 00135 NM 2007 12 28 QXEA200701906 1 20071216 A 2133 88060B010002 OUTFLOW VALVE BOMBDR DHC8 DHC8402 1390042 NM CABIN PRESSURE MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 418QX 2455 2 4143 GEG - FLIGHT 2371 - CLIMBING OUT OF 8000 FEET, PRESSURIZATION WAS RAPIDLY INCREASING, AND 12000 GOT A MASTER WARNING. A IRCRAFT WOULD NOT DEPRESSURIZE IN MANUAL MODE, DESCENDING OUT OF 10000 MANUAL MODE STARTED TO OPERATE. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE AFT OUTFLOW VALVE. OPERATIONAL CHECKS GOOD. AIR CRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007122800137 20071228 00137 CE 2007 12 28 DXTA200702664 1 20071209 A 3246 315381 WHEEL CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG VIBRATES E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 944QS 423 423 7500144 EXTREMELY VIOLENT NOSEWHEEL SHIMMY ON TAKEOFF AT 70 KIAS. SHIMMY BROKE BOTH FILLAMENTS IN THE TAXI LIGHTS AND FLUID IS LEAKING FROM THE STRUT, AND YAW DAMPER AMBER CAS MESSAGE ILLUMINATED. FOUND NOSE WHEEL TIRES TO HAVE LARGE FLAT SPOTS. R EMOVED AND REPLACED LT & RT NOSE WHEEL ASSYS IAW 750 M/M CH 32-41-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007122800138 20071228 00138 CE 2007 12 28 DXTA200702657 1 20071207 A 3200 UNKNOWN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE UNKNOWN E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 393QS 5600393 AFTER TAKEOFF, RED LANDING GEAR NOT LOCKED AND AMBER HYD SYS PRESS LIGHTS REMAINED ILLUMINATED FOR APPROXIMATELY 2 MINUT ES. AT THAT TIME A THUMP WAS HEARD AND FELT COMING FROM THE AREA OF THE NOSE GEAR. LIGHTS WENT OUT. GEAR CYCLED DOWN NO RMALLY FOR LANDING. PERFORMED 10 GEAR SWING CYCLES. CHECKED FULL LOCK RET. TIME (4.5 SEC MAX) AND FULL LOCK EXT. TIME (5.0 SEC MAX). EXT. AND RET. TIMES WERE WITHIN LIMITS DURING ALL 10 CYCLES. GEAR INDICATION FUNCTIONED NORMAL DURING AL L CYCLES. OPS CHECK GOOD. WORK PERFORMED IAW CE-560 MM 32-01-00. REF. FAS W.O. 07-2988. 2 L 7 2 4F 4 F RT A22CE E25EA 2007122800139 20071228 00139 CE 2007 12 28 DXTA200702658 1 20071207 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG WEAK E DXTA O OTHER O OTHER LD LANDING 1 GL 07 324QS 5600423 COPILOT RT BRAKE IS MUSHY. BLED RT BRAKE SYSTEM IAW CE-560 M/M 32-42-00. PERFORMED TAXI CHECK. R/H BRAKE SYSTEM OPS C HECK GOOD AT THIS TIME. 2 L 7 2 4F 4 F RT A22CE E25EA 2007122800140 20071228 00140 CE 2007 12 28 DXTA200702660 1 20071207 A 3260 1EN115BN111 DOWNLOCK SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP MLG INTERMITTENT E DXTA O OTHER N FALSE WARNING CL CLIMB 1 GL 07 893QS 7448 258393 DURING T/O AS THE NLG LEAVES THE GRD, A NOSE LIKE SHIMMY OR A TIRE IMBALANCE IS HEARD FOR APPROX. 3 SEC. THEN DURING RET RACTION THE NLG LIGHTS DIMLY FLICKER (BOTH RED & GREEN) UNTIL THE GEAR IS RETRACTED FULLY. MLG LIGHT ARE NORMAL. ALSO AT APPROX 20 MIN INTO THE FLIGHT DURING CLIMB WE NOTICED THE NLG LIGHTS FLICKER LIKE BEFORE. REMOVED & REPLACED NOSE WHE EL DOWN LOCK SWITCH WITH NEW SWITCH OPS CHECKS GOOD PER 800XP MM 32-60-00 & WD 32-60-10-04. 2 L 7 2 4F 4 F RT A3EU E6WE 2007122800141 20071228 00141 CE 2007 12 28 DXTA200702665 1 20071209 A 2131 CONTROLLER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE CABIN PRESSURE OBSTRUCTED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 330QS 5600329 ON TAKE-OFF CABIN CONTROLLER FAILED TO MAINTAIN CABIN PRESSURIZATION. TROUBLESHOT TO VENT BLOCKAGE ON CONTROLLER. CLEAR ED BLOCKAGE AND PERFORMED OPS CHECK. OPS CHECK GOOD. IAW CE 560 MM CH 21-31-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007122800142 20071228 00142 CE 2007 12 28 DXTA200702666 1 20071209 A 5532 EROSION SHIELD CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE VERTICAL STAB LOOSE E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 399QS 5600510 EROSION TAPE CAME LOOSE FROM VERTICAL STAB AND WEDGED IN RUDDER. RUDDER ONLY MOVES ONE DIRECTION. REMOVED LOOSE EROSI ON TAPE FOUND IN VERTICAL STAB. AND PERFORMED RUDDER SYSTEM OPS CHECK, OPS CHECK NORMAL. WORK DONE IAW CESSNA 560 M/M C H 27-30-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007122800143 20071228 00143 CE 2007 12 28 DXTA200702667 1 20071209 A 3010 99145192 OVERHEAT SENSOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE WING INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 663QS 1364 5605263 IN CRUISE FLT WITH WING + ENGINE ANTI-ICE ON, MASTER CAUTION FLICKERED THEN LATER CAME ON AND RT (WING OVERHEAT) ANNUNCI ATOR FLASHED. REPLACED TEMP SENSOR TT02 WITH NEW. LEAK & OPERATIONAL CHECK NORMAL IAW 560XL MM 36-11-01. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007122800144 20071228 00144 CE 2007 12 28 DXTA200702661 1 20071208 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D1 52060 NE MLG WEAK E DXTA O OTHER O OTHER LD LANDING 1 GL 07 348QS 5600348 BRAKES PULL AIRCRAFT NOSE HARD LT WHEN EQUAL PRESSURE IS APPLIED TO BOTH BRAKE PEDALS DURING LANDING ROLLOUT. BLED BRAK ES IAW C560 M/M 32-42-00. TAXI CHECKED/BRAKE CHECKED A/C. OPS CHECKS NORM. 2 L 7 2 4F 4 F RT A22CE E1NE 2007122800145 20071228 00145 CE 2007 12 28 DXTA200702662 1 20071208 A 3240 AC61518 METERING VALVE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP BRAKE ASSY BYPASSING E DXTA O OTHER O OTHER LD LANDING 1 GL 07 858QS 2398 258691 BRAKES ARE VERY MUSHY, LT BRAKE ALMOST GOES TO THE FLOOR. REMOVED MAIN REDUCING VALVE & INSTALLED OVERHAULED MAIN REDU CING VALVE & BLED FULL BRAKE SYSTEM, OPS CHECKS GOOD. IAW 800XP MM CH 32-40-00. 2 L 7 2 4F 4 F RT A3EU E6WE 2007122800146 20071228 00146 CE 2007 12 28 DXTA200702668 1 20071209 A 3260 41EN496 SQUAT SWITCH CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG WORN E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 324QS 9242 5600423 LANDING GEAR WILL NOT RETRACT. GEAR INDICATES DOWN AND 3 GREEN . GEAR HANDLE WILL NOT RAISE AS IF LOCKED DOWN. JACKED AIRCRAFT AND FOUND LH SQUAT SWITCH TO BE IN GROUND MODE. WITH SLIGHT SIDE LOAD TO THE SCISSOR LINK MOVES SWITCH SHAFT LA TERALLY BACK INTO FLIGHT. SWITCH SHAFT SHOULD NOT HAVE A LATERAL WIGGLE TRIGGERING GROUNF FROM FLIGHT AND VISE VERSA. WA S ABLE TO NUDGE SHAFT TO TRIGGER GROUND AND FLIGHT MODE. SWITCH FAULTY FROM STOCK. REMOVED LH SQUAT SWITCH AND INSTALLED NEW. RIGGED AND TESTED THROUGHLY. PERFORMED GEAR SWINGS. GEAR SWINGS OPS CHECKED GOOD. RAN ENGINES AND PRESSURIZED AIR CRAFT ON GROUND AND IN FLIGHT MODE. LH SQUAT SWITCH OPERATES NORMALLY AT THIS TIME IAW CE560 MM 32-61-00 AND 21-31-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007122800147 20071228 00147 2007 12 28 DXTA200702669 4 20071209 A 3440 IRS CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NR 2 UNKNOWN E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 908QS 7500108 DURING CRUISE FLT AT FL410, NR2 IRS FAILED. WE WERE ABLE TO REVERT AND USE NR1 IRS INFO. CHECKED FAULTS AND FAULTS FOR PREVIOUS LEG CALL FOR RETURN TO SERVICE & MONITOR PER HONEYWELL FAULT ISOLATION MANUAL. NO PREVIOUS HISTORY OF IRS FAUL TS. SYSTEM OPERATIONAL CHECKED NORMALLY WITH NO FAULTS OR DEFECTS AT THIS TIME IAW CE750 MM CHAPTER 34-43-01 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007122800148 20071228 00148 CE 2007 12 28 DXTA200702663 1 20071209 A 2130 UNKNOWN RAYTHN DH125 HAWKER800XP 7150012 CE CABIN PRESSURE UNKNOWN E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 891QS 258788 CABIN WOULD NOT PRESSURIZE. DIFFERENTIAL STAYED AT ZERO. TRIED MANUAL AND STILL WOULD NOT PRESSURIZE. PERFORMED CABIN P RESSURE CONTROL SYSTEM TROUBLESHOOTING IAW HAWKER 800XP MM CHP 21-30-00-101. NO DEFECTS NOTED. FUNCTIONALLY TESTED PRE SSURIZATION SYSTEM IAW HAKER 800XP 21-30-00-501. NO DEFECTS NOTED. PERFORMED PRSOV TEST AND MAIN AIR VALVE TEST IAW HA WKER 800XP MM CHP 21-10-76-501. NO DEFECTS NOTED. SYSTEM OPS CHECK NORMAL. 2 L 7 2 4F RT A3EU 2007122800149 20071228 00149 CE 2007 12 28 DXTA200702670 1 20071210 A 3260 41EN496 SQUAT SWITCH CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG ERRATIC E DXTA B EMER. DESCENT N FALSE WARNING CL CLIMB 1 GL 07 374QS 8441 5600475 PRESSURIZATION INOP ON CLIMBOUT CABIN RATE HAD NO CONTROL OF RATE OF CLIMB. AT ALTITUDE CONTROLLER HAD NO EFFECT ON CABI N ALT. ON DESCENT PRESSURIZATION FAILED (CABIN ALT) LIGHT CAME ON O2 MASKS WERE DONNED EMERGENCY DECLARED UNTIL REACHING A SAFE ALT. REMOVED LT MLG SQUAT SWITCH DUE TO ERRATIC READINGS INSTALLED NEW SWITCH AND RIGGED. OPS CHECK GOOD . PRESSURIZATION CHECK GOOD. IAW C560 MM 32-61-00 2 L 7 2 4F 4 F RT A22CE E25EA 2007122800150 20071228 00150 CE 2007 12 28 DXTA200702671 1 20071211 A 4990 OIL SYSTEM CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE APU OVERSERVICED E DXTA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 389QS 6800149 AFTER STARTING APU AND TURN-ON BLEED AIR CABIN BEGAN TO FILL WITH AN OILY ODOR. SHUTDOWN APU AND STARTED BOTH ENGINES A ND SMOKE DISSIPATED AND DID NOT RETURN. RE-ENABLED APU. VISUALLY INSPECTED APU EXAUST AND EXTERNAL COMPONENTS. NO LEA K OR DEFECTS NOTED. CHECKED OIL LEVEL FOUND TO BE OVERSERVICED TO TOP OF FILLER NECK. CLEANED AND INSPECTED COALESCER IAW CE680 MM 12-11-03 AND HONEYWELL RE100 (CS) MM 49-20-00. RAN FOR 30 MIN. NO DEFECTS OR ODOR NOTED. 2 L 7 2 4F 4 F RC T00012WI E35NE 2007122800151 20071228 00151 NM 2007 12 28 UPS07M51286 1 20071212 A 2710 2A4204A ACTUATOR DOUG MD11 MD11F 3023600 NM AILERONS WARNING LIGHT A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 271UP 48572 ATB - AILERON DEFLECT DISAGREE ALERT ON FLAP RETRACTION. A/C ROLLED RT WITH FLAPS UP. NO EMERGENCY DECLARED. R&R RH I /B AILERON DEFLECT ACTUATOR PER AMM 27-16-01-4 AND FUNCTION TEST C/W PER AMM 27-16-00-5. RESULT NORMAL. 2 L 7 3 4F RT A22WE 2007122800152 20071228 00152 CE 2007 12 28 DJFA2007141 1 20071212 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 775TA RK276 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE O UTLINED IN COMMUNIQUE' NR 70. BOTH RIBS WERE REPLACED WITH UPGRADED ASSEMBLIES TO PREVENT FUTURE FAILURES. 2 H 7 2 4F 4 F RT A16SW E25EA 2007122800153 20071228 00153 2007 12 28 DXTA200702672 4 20071212 A 2210 702800901 ACTUATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL YAW DAMPER INOPERATIVE E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 945QS 9082 7500029 DURING T/O ROLL PRIOR TO 80KTS WE HAD THE FOLLOWING: RED NO T/O MESSAGE. Y/D NOT CENTERED. FGC FAIL. REMOVED AND REP LACED YD LINEAR ACTUATORS. PERFORMED OPERATIONAL CHECK SATISFACTORY. WORK DONE IAW 750 MM CHAP 27-24-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007122800154 20071228 00154 CE 2007 12 28 DXTA200702673 1 20071212 A 2913 99144603 PUMP CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LT ENGINE INOPERATIVE E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 916QS 4264 4264 7500116 AMBER CAS MESSAGER: HYD PUMP FAIL, A. HYD O'TEMP, FUEL BOOST N-L AND HYD VOLUME LOW, A ILLUMINATED IN FLIGHT. THE CHECKL IST PROCEDURES WERE PERFORMED. THE LANDING GEAR WAS BLOWN DOWN. THE EMERGENCY BRAKE HANDLE USED TO STOP THE AIRCRAFT ON THE RUNWAY. REPLACED LT HYD PUMP IAW 29-10-02. REPLACED LT MOTIVE FLOW PUMP IAW 750 MM 73-10-00. FLUSHED AND OPS CHEKC ED IAW 750 MM 28-20-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007122800155 20071228 00155 NE 2007 12 28 DXTA200702674 2 20071212 A 7532 31J285704 BLEED ACTUATOR CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE LT ENGINE INOPERATIVE E DXTA E ENGINE SHUTDOWN E VIBRATION/BUFFET DE DESCENT 1 GL 07 693QS 1343 5605657 DURING DESCENT FROM CRUISE ALTITUDE, CREW EXPERIENCED ENGINE VIBRATION ACCOMPANIED BY EEC MANUAL L ADVISORY WITH NO ENG VIB ANNUNCIATOR. THROTTLE AY IDLE ITT= 650. EEC CHECKLIST DID NOT EFFECT VIBRATION. PERFORMED PRECAUTIONARY S/D. VISU ALLY INSPECTED CHIP DETECTOR AND OIL FILTER ON LH ENGINE. PERFORMED BOROSCOPE ON LH ENGINE COMPRESSOR AND HP TURBINE. INSTALLED MODIFIED BLEED VALVE TORQUE MOTOR ON LH ENGINE I.A.W. P&W MM 75-30-01. COMPLETED 5 POINT ENGINE PERFORMANCE R UN I.A.W. P&W MM 71-00-00. ALL CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007122800156 20071228 00156 NM 2007 12 28 NOCA17107 1 20071214 A 2780 667604 ACTUATOR BOEING 757 75728A 1384976 NM SLATS MALFUNCTIONED A NOCA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 750NA 26277 ON TAKEOFF OUT OF YQX HAD `L/E SLAT DISAGREE` EICAS CAUTION MESSAGE. AIR TURNBACK TO YQX. ITEM REMAINS OPEN, MX FERRY BACK TO JFK. REPLACED NR 10 L/E ROTARY ACTUATOR PER MM 27-81-18 FLIGHT TEST OK ITEM CLOSED 2 L 7 2 4F RT A2NM 2007122800157 20071228 00157 CE 2007 12 28 DXTA200702675 1 20071213 A 3260 UPLOCK SWITCH CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG OUT OF ADJUST E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 330QS 5600329 AFTER RETRACTING THE GEAR, THE HYD PRESS ON LIGHT AS WELL AS THE GEAR UNLOCKED LIGHTS WERE ON. WE RAN THE CHECKLISTS BR OUGHT THE GEAR DOWN AND USED THE BLOW DOWN AS A PRECAUTION. INSPECTED AND ADJUSTED UP-LOCK SWITCH. OPS CHECKED GOOD IAW CESSNA 560 MM 32-31-05 2 L 7 2 4F 4 F RT A22CE E25EA 2007122800158 20071228 00158 EU 2007 12 28 TRAX200701905 1 20071211 A 7120 MOUNT AEROSP ATR72 ATR72212 8680945 EU RT ENGINE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 RT ENG LT FWD LATERAL SHOCKMOUNT CRACKED. RT ENG LT FWD LATERAL SHOCKMOUNT AFT MOLDED CUSHION REPLACED IAW AMM 71-20-2 2 AND JIC 71-21-61 RAI 10 000. 2 H 7 2 4T RT A53EU 2007122800159 20071228 00159 EU 2007 12 28 TRAX200701906 1 20071211 A 5280 BRACKET AEROSP ATR72 ATR72212 8680945 EU NLG DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 PAX DOOR SURROUND 255DW, 255EW IN CRACKED. NLG FWD LT DOOR FWD STOP BRACKET REPLACED IAW SRM 51-25-01REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR CCOMPLISHED IN ACCORDANCE WITH SRM 5 1-25-01. 2 H 7 2 4T RT A53EU 2008010200002 20080102 00002 EA 2008 1 2 COMA0760687 1 20071203 A 3234 555406 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 588SW 29952 7069 FLIGHT 5391 - AFTER TAKEOFF RECEIVED GEAR DISAGREE AND NOSE DOORS OPEN MESSAGES. DECLARED EMERGENCY LANDED CHS WITHOUT INCIDENT. REPLACED NOSE GEAR SELECTOR VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008010200005 20080102 00005 NM 2008 1 2 ASAA0752380 1 20071211 A 7722 TC29604 PROBE BOEING 737 737890 1384527 NM NR 1 ENGINE DIRTY A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 579AS 35187 ENGINE TREND DATA SHOWS EGT HOT DAY MARGIN HAS NOT RECOVERED FROM CONNECTOR CLEANING. REPLACE T49.5 PROBE. REPLACED T49 .5 PROBE. OP TEST GOOD. 2 L 7 2 4F RT A16WE 2008010200006 20080102 00006 EA 2008 1 2 COMA0760689 1 20071204 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 SO 01 806CA 7359 FLIGHT 5236 - FLAPS FAIL CAUTION MESSAGE DURING FLAP DEPLOYMENT. AIRCRAFT LANDED SAFELY IN JFK. COMPLIED WITH AD 2006- 12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WI TH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2008010200007 20080102 00007 NE 2008 1 2 COMA0760690 2 20071205 A 7200 CF343A1QR ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* 30015 NE NR 2 VIBRATES A COMA E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 SO 01 708CA 17201 7235 807658 FLIGHT 5201 - IN CRUISE RECEIVED NR 2 N2 VIBE CAUTION MESSAGE. FOLLOWED QRH, SHUTDOWN NR 2 ENGINE. DECLARED EMERGENCY, DIVERTED TO ATL AND LANDED WITHOUT INCIDENT. REPLACED NR 2 ENGINE. NO FURTHER DEFECTS. 2 L 7 2 4F 4 F RT A21EA 2008010200008 20080102 00008 EA 2008 1 2 COMA0760691 1 20071205 A 2611 PU9042R3 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 917CA 7017 FLIGHT 5603 - IMMEDIATELY AFTER TAKEOFF, SMOKE TOILET CAUTION MESSAGE DISPLAYED. FOLLOWED QRH PROCDEDURE. AFT PAX REPO RTED SMOKE SMELL. AIRCRAFT RETURNED BACK TO JFK AND LANDED SAFELY. REMOVED AND REPLACED LAV SMOKE DETECTOR. 2 L 7 2 4F RT A21EA 2008010200015 20080102 00015 EA 2008 1 2 COMA0770078 1 20071210 A 2150 A/C PACK CNDAIR CL600 CL6002C10 1390015 EA RIGHT MALFUNCTIONED A COMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 391CA 10108 FLIGHT 5420 - DURING TAXI OUT IN DFW PASSENGERS WERE EVACUATED DUE TO SMOKE IN CABIN ROWS 8.9 AND 10. FOUND RIGHT PACK TO BE THE CAUSE OF THE SMOKE. DEFERRED TIGHT PACK PER MEL 21-51-04-2. 2 L 7 2 4F RT A21EA 2008010200022 20080102 00022 NE 2008 1 2 ASAA0752384 2 20071214 A 7321 2042M67P02 EEC BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE NR 1 ENGINE FAULTY A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 583AS 35681 NR 1 ENGINE SHOWS EEC FAULT CODE 73 20011 AS A CURRENT SHORT TERM FAULT. REPLACED EEC AND UPLOADED NEW SOFTWARE. NR 1 ENGINE EEC SYSTEM TEST PASSED. 2 L 7 2 4F 4 F RT A16WE E00055EN 2008010200023 20080102 00023 EA 2008 1 2 COMA0760697 1 20071207 A 3020 22856480801 RELIEF VALVE CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE FAULTY A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 812CA 7381 FLIGHT 5137 - ON CLIMBOUT FROM CVG TO YYZ RECEIVED LEFT COWL ANTI-ICE INOP MESSAGE. CREW DECLARED EMERGENCY AND RETURNE D BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED LEFT ENGINE COWL ANTI-ICE PRESSURE RELIEF VALVE. 2 L 7 2 4F RT A21EA 2008010200026 20080102 00026 EA 2008 1 2 COMA0760700 1 20071208 A 3350 362624 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 931CA 7037 CABIN EMERGENCY FLOOR LIGHTS AT ROWS 9 THROUGH 12 INOP. REMOVED AND REPLACED LAMP ASSEMBLY. 2 L 7 2 4F RT A21EA 2008010200029 20080102 00029 EA 2008 1 2 COMA0760703 1 20071210 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 779CA 7306 FLIGHT 5354 - AFTER LANDING IN CVG, SELECTED FLAPS TO 0 DEGREES AND RECEIVED FLAPS FAIL CAUTION MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2008010200030 20080102 00030 EA 2008 1 2 COMA0760704 1 20071210 A 3020 5399001 ANTI-ICE VALVE CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 807CA 8334 7364 FLIGHT 5643 - EN ROUTE FROM BOS TO CMH RECEIVED RIGHT COWL ANTI-ICE MESSAGE WITH ANTI-ICE SELECTED OFF. COMPLIED WITH Q RH, CREW THEN DECLARED AN EMERGENCY AND DIVERTED TO GSO AND LANDED SAFELY. REMOVED AND REPLACED RIGHT COWL ANTI-ICE VAL VE. 2 L 7 2 4F RT A21EA 2008010200031 20080102 00031 EA 2008 1 2 COMA0760705 1 20071210 A 3020 12681 PRESSURE SWITCH CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 807CA 6349 7364 FLIGHT 5643- EN ROUTE FROM BOS TO CMH RECEIVED RIGHT COWL ANTI-ICE MESSAGE WITH ANTI-ICE SELECTED OFF. COMPLIED WITH QR H, CREW THEN DECLARED AN EMERGENCY AND DIVERTED TO GSO AND LANDED SAFELY. REMOVED AND REPLACED RIGHT COWL ANTI-ICE PRES SURE SWITCH. 2 L 7 2 4F RT A21EA 2008010200033 20080102 00033 WP 2008 1 2 ASAA0782387 1 20071215 A 5210 HANDLE DOUG DC9 DC983 3022083 WP PAX DOOR OBSTRUCTED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 943AS 53018 CANNOT OPEN MAIN PAX (L10) DOOR FROM INSIDE, HAD TO OPEN FROM OUTSIDE. REMOVED EXCESS PAINT ON OUTSIDE OF DOOR WHICH PR EVENTED OUTSIDE HANDLE FROM MOVING TO OPEN POSITION WHEN ATTEMPTING OPENING FROM INSIDE. INSIDE HANDLE THEN OPENED DOOR PROPERLY. 2 L 7 2 4F RT A6WE 2008010200039 20080102 00039 EA 2008 1 2 COMA0760710 1 20071211 A 5315 601R3111357 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 712CA 23431 7244 LONGITUDINAL FLOORBEAM ATTACH CLIP CRACKED FS 280, LBL 10 OUTBOARD SIDE OF BEAM. REMOVED AND REPLACED CLIP IAW CRJ SRM 51-42-21. 2 L 7 2 4F RT A21EA 2008010200048 20080102 00048 EA 2008 1 2 COMA0760719 1 20071213 A 5313 STRINGER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 779CA 7670 BAGGAGE CART STRUCK AIRCRAFT JUST AFT OF APU EXHAUST. SPLICED STRINGER 15 FROM STA 682 TO STA 688. 2 L 7 2 4F RT A21EA 2007122700007 20071227 00007 EA 2007 12 27 A6WA200740651 1 20071129 A 2410 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 2 UNDERSERVICED A A6WA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 438AW 7748 TAKEOFF ABORTED DUE TO RIGHT IDG CAUTION AND THEN RIGHT GENERATOR DROPPING OFF LINE. TAKEOFF ABORTED AT 70 KNOTS, MINIM AL BRAKING. BTMS BRAKE TEMPS READ 2-1-1-2. SERVICED IDG NR 2 IAW CRJ AMM 12-13-24. RAN ENGINE WITH OPS CHECK OF IDG N R 2. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007122700009 20071227 00009 EA 2007 12 27 A6WA200740654 1 20071130 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA ILLUMINATED A A6WA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 31 438AW 7748 ABORTED TAKEOFF AT 80 KNOTS FOR YELLOW "ICE" CAS MESSAGE, BRAKE TEMPS 7-5-4-7. OPS CHECK OF ICE DETECTION IAW 30-81-01 . OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2007122700016 20071227 00016 EA 2007 12 27 A6WA200740646 1 20071124 A 2750 DRIVE ASSY CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS UNKNOWN A A6WA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 31 458AW 7861 WHEN FLAP HANDLE SELECTED FROM 20 DEGREES TO 8 DEGREES IN FLIGHT, FLAP FAIL CAS MESSAGE STAYED AT 20 DEGREES. REMOVED A ND REPLACED FLEX DRIVE NR 5 PER CRJ AMM 27-50-00, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007122700017 20071227 00017 EA 2007 12 27 A6WA200740648 1 20071127 A 2710 272007 PCU CNDAIR CL600 CL6002B19 1900309 EA AILERONS UNKNOWN A A6WA O OTHER F FLT CONT AFFECTED LD LANDING 1 GL 31 441ZW 7777 EXCESSIVE LEFT DOWN AILERON TRIM REQUIRED FOR LEVEL FLIGHT, REQUEST INSPECTION. REMOVED AND REPLACED NR 1 AILERON PCU P ER AMM 27-14-01, OPS AND LEAK CHECK GOOD. RIG CHECK PER AMM 27-11-00, RIG CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2007122700025 20071227 00025 NM 2007 12 27 SWAA076235 1 20071213 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700027 20071227 00027 NM 2007 12 27 SWAA076232 1 20071213 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM BS 747 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700038 20071227 00038 NM 2007 12 27 SWAA076194 1 20071213 A 5551 6552857 ATTACH FITTING BOEING 737 7373TO 138447G NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STABILIZER FWD AND AFT LUG FITTING CORRODED. REMOVED AND REPLACED FITTI NG PER MM. 2 L 7 2 4F RT A16WE 2007122700041 20071227 00041 NM 2007 12 27 SWAA076201 1 20071213 A 5311 6558280 FRAME BOEING 737 7373TO 138447G NM BS 360 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700061 20071227 00061 NM 2007 12 27 SWAA076216 1 20071213 A 5311 6546548 FRAME BOEING 737 7373TO 138447G NM BS 747 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700066 20071227 00066 EU 2007 12 27 USAA920071324 1 20071209 A 5320 D53480048203 FITTING AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 624AW 55 SAL - MAJOR REPAIR - C6 CHECK - CORROSION ON THE R2 DOOR CUTOUT LOWER SILL CENTER SHAPE SILL FITTING, BS 3158 / FR 66 - BS 3257 / FR 68. REPLACED THE R2 DOOR CUTOUT LOWER SILL CENTER SHAPE SILL FITTING, BS 3158 / FR 66 - BS 3257 / FR 68 IA W A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2007122700068 20071227 00068 SO 2007 12 27 C2XA07SH105 1 20071215 A 5320 14529495001 SILL EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18120 145681 SHV - DURING C-CHECK LEFT FLOOR SILL HAS CORROSION FR 52-59. MAINTENANCE REPAIRED LEFT FLOOR SILL BETWEEN FR 52-59, REM OVED AND REPLACED CORRODED SECTION OF SILL IAW EC5320-01394 AND IAW EMB 145 SRM 51-40-02 AND EMB 145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2007122700084 20071227 00084 2007 12 27 SA07083 4 20071213 A 2565 LANYARD AIRBUS A319 A319112 3930323 EU DOOR SLIDE MISROUTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 724UW 1122 PIT - THE RIGHT HAND, FORWARD AND LEFT HAND AFT DOOR SLIDES HAVE IMPROPERLY ROUTED LANYARDS. MAINTENANCE ROUTED THE LAN YARDS PROPERLY. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2007122700093 20071227 00093 NM 2007 12 27 SWAA076252 1 20071214 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 430 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, RBL 3. REPAIRED SKIN PER ACO. 2 L 7 2 4F RT A16WE 2007122700094 20071227 00094 NM 2007 12 27 SWAA076251 1 20071214 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 450 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, RBL 1.5. REPAIRED SKI N PER ACO. 2 L 7 2 4F RT A16WE 2007122700095 20071227 00095 NM 2007 12 27 SWAA076250 1 20071214 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 410 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, RBL 2. REPAIRED SKIN PER ACO. 2 L 7 2 4F RT A16WE 2007122700096 20071227 00096 NM 2007 12 27 SWAA076253 1 20071214 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 408WN 27895 EEPLS LIGHT LENS LOOSE AT ROW 7 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2007122700106 20071227 00106 NM 2007 12 27 SWAA076263 1 20071216 A 3350 417A5701 LENS BOEING 737 7375H4 138449D NM EMERGENCY LIGHTS BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2007122700119 20071227 00119 NM 2007 12 27 USAA920071335 1 20071215 A 5313 655162823 STRINGER BOEING 737 7373Y0 1384671 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - A CRACK FOUND ON STRINGER S25R AT BS 907 - BS 1016. REMOVED AND REPLACED STRINGER S25R AT BS 907 - BS 1016 IAW B737-300 SRM 51-40-02-0G, PAR 7D, FIG 8 &12. 2 L 7 2 4F RT A16WE 2007122700122 20071227 00122 NM 2007 12 27 USAA920071338 1 20071217 A 5330 6545776Y55 SKIN PANEL BOEING 737 7373Y0 1384671 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - CORROSION FOUND BETWEEN SKIN AND INTERNAL DOUBLER AT BS 908 - BS 1006, S27L - S27R. REMOVED AND RE PLACED FUSELAGE SKIN AT BS 908 - BS 1006, S27L - S27R IAW B737-300 SRM 51-40-02-0G FIG 3, 8 AND 12. 2 L 7 2 4F RT A16WE 2007122700136 20071227 00136 NM 2007 12 27 SWAA076290 1 20071217 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT FORE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2007122700139 20071227 00139 NM 2007 12 27 SWAA076277 1 20071213 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 420WN 29825 DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138.8. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700154 20071227 00154 NM 2007 12 27 SWAA076283 1 20071217 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007122700160 20071227 00160 NM 2007 12 27 SWAA076311 1 20071217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM BS 727B S14L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 2007122700178 20071227 00178 NM 2007 12 27 SWAA076329 1 20071215 A 3230 273A1101 ACTUATOR BOEING 737 7377H4 1384404 NM NLG FAULTY A SWAA O OTHER O OTHER CL CLIMB 1 SW 29 713SW 27847 NLG SLOW TO RETRACT, CYCLED GEAR, NLG TOOK 30 SECONDS TO RETRACT. REMOVED AND REPLACED NLG RETRACT ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2007122700184 20071227 00184 NM 2007 12 27 SB07107 1 20071217 A 3297 WIRE BOEING 737 737401 1384701 NM RT MLG BROKEN A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 420US 23987 CLT FLT 1570 - AFTER TAKEOFF AND DURING CLIMBOUT FROM CLT, CREW RECEIVED A RIGHT MAIN LANDING GEAR RED UNSAFE LIGHT AFTE R GEAR RETRACTION. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MA INTENANCE REPAIRED A BROKEN WIRE AT THE RIGHT MAIN LANDING GEAR UPLOCK SENSOR. ACCOMPLISHED TEST PER MM 32-61-21. OPER ATIONAL TEST GOOD. 2 L 7 2 4F RT A16WE 2007122700193 20071227 00193 NM 2007 12 27 SB07108 1 20071220 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM EMERGENCY LIGHTS DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 453UW 24980 CLT - MAINTENANCE REPORTED A SECTION OF AFT CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE AFT LEFT EMERGENCY LIGHT BATTERY ASSEMBLY LOCATED IN AFT GALLEY CEILING. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2007122700197 20071227 00197 NM 2007 12 27 USAA920071351 1 20071205 A 5754 SKIN BOEING 737 7373G7 1384595 NM NR 1 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 968 25400 MCN - MAJOR REPAIR - C-16 CHECK - 3 CRACKS ON NR 1 SLAT SKIN AT NR 1 SLAT STA 166.5 - 171.75. INSTALLED DOUBLER AND REP AIRED IAW B737-300 SRM 57-43-01-2R4. 2 L 7 2 4F RT A16WE 2007122800003 20071228 00003 NM 2007 12 28 HALA0700542 1 20071224 A 2820 S343T00314 ACTUATOR BOEING 767 76733A 1385209 NM FUEL CROSSFEED MALFUNCTIONED A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM, SINGLE FUEL CROSSFEED VALVE LGT REMAINED ILLUM WHEN "CLOSE" SELECTED. EICAS MSG "FUEL CROSSFE ED" DISPLAYED. REMOVED AND REPLACED FUEL CROSSFEED VALVE ACTUATOR PER AMM 28-22-12. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2007122800010 20071228 00010 NM 2007 12 28 07FDEA05095 1 20071219 A 5410 B277101901 FAIRING BOEING 727 727233 138408A NM ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 NR 1 ENG INBOARD COWLING IS CRACKED THROUGH AT 3RD LATCH FROM THE FRONT (TOP SIDE). REMOVED DAMAGE AND REPAIRED WITH DO UBLER, APPLIED ALODINE AND PRIMER REF SRM 54-10-03, DWG SR27-71-007, 51-10-02, CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2007122800016 20071228 00016 2007 12 28 HALA0700533 4 20071219 A 2330 1301273107 AUDIO VIDEO UNIT BOEING 767 76733A 1385209 NM CABIN ODOR A HALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 13 591HA 33423 ELECTRICAL SMOKE ODOR AROUND SEATS 14HJ (NO VISIBLE SMOKE). POWERED OFF ENTERTAINMENT SYSTEM ODOR DIMINISHED. FOUND BA D AVU AT SEAT 14HJ REPLACED AVU AND ORCHESTRATED ENTERTAINMENT SYSTEM OPS CKS NORMAL. 2 L 7 2 4F RT A1NM 2007122800023 20071228 00023 NM 2007 12 28 07FDEA05096 1 20071219 A 5411 651950759 LONGERON BOEING 727 727233 138408A NM NR 1 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 NR 1 ENG LWR COWL DOOR OB LONGERON IS CRACKED AT AFT HINGE CUT OUT. REMOVED, FABRICATED NEW INTERCOSTAL, SENT TO HEAT T REAT ON SNR NR N00829. TREATED AND PRIMED, COMPLETED INSTALLATION, REF SRM 51-30-2, 51-10-2 AND BAC DWG 65-19507. 2 L 7 3 4F RT A3WE 2007122800030 20071228 00030 NM 2007 12 28 07FDEA05103 1 20071219 A 5313 BAC1498146 STRINGER BOEING 727 727233 138408A NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 EXT FUSELAGE SKIN 2 RIVETS HAVE LIGHTING STRIKES AT STR S-8R BS 510 AND 513 REMOVED LIGHTNING STRIKE DAMAGE TO SKIN AND STR 8R. INSTALLED SKIN DOUBLER USING .050"2024 T-3 FILLER .040 2024 T-3, REF 53-30-2 FIG 20 STR 8. REPAIRED USING BAC 1598-146 REF SRM 53-30-3 FIG 3. 2 L 7 3 4F RT A3WE 2007122800036 20071228 00036 SO 2007 12 28 SIMA200735304 1 20071217 A 5320 14522460009 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 668HH 145785 DURING MBV INSPECTION, FOUND GUSSET ON CENTER HAT BEAM BETWEEN FRAMES 20 TO 23 HAS SPOTS OF CORROSION. REPLACED GUSSET IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2007122800038 20071228 00038 SO 2007 12 28 SIMA200735302 1 20071215 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145 3260210 SO NLG MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 613AE 145081 FLT 4105 - CREW CALLED TO REPORT LANDING GEAR AIR GROUND FAIL MSG ON TAKEOFF AND GEAR WOULD NOT INITIALLY RETRACT. CREW DID GET GEAR UP. ALSO RECEIVED BLEED 2 CLOSED MESSAGE. AC LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR PROX SWITCH AN D FUNCTIONAL CHECK OF PROX SWITCH IAW EMB 145 32-63-00 AND PERFORMED EXTENSION RETRACTION TEST IAW EMB AMM 32-30-00. AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2007122800053 20071228 00053 NM 2007 12 28 HALA9700444 1 20071223 A 2697 CONNECTOR BOEING 767 7673G5 1385126 NM APU FIRE LOOP DIRTY A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, APU FIRE LP 2 DISPLAYED. NO APU FIRE LP 2 EICAS MSG ON INITIAL CHECK. RAN RESISTANCE CHECK. W/TEST CARD PIN 20-21-13.8 OHMS. PIN 20 TO GROUND .341 OHMS PIN 21 TO GROUND .343 M OHMS. CLEANED AND RESECURED CONNE CTORS, RAN FIM OPS CHK OK PER FIM 26-15-00. NO MSGS NOTED. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2007122800054 20071228 00054 WP 2007 12 28 ARWA20071204 1 20071216 A 7897 WIRE DOUG DC10 DC1030F 3023504 WP THRUST REVERSER DAMAGED A ARWA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 19 450ML 47831 DURING INITIAL TAKEOFF ROLL SPOOLING UP NR 1 ENGINE REVERSER PRESSURE LIGHT CAME ON. TRANSFERRED TO DMI NR 21307, MEL 7 8-1 CAT "C", INSTALLED PLACED AND DEACTIVATED FAN REVERSER IAW DDG. REPAIRED WIRES AT THRUST REVERSER LOCK SWITCH CAM ASSEMBLY THROTTLE MODULE IAW MM 20-30-01; OPS CHECK IAW M/M 78-30-00, OPERATIONAL CHECK NORMAL. 2 L 7 3 4F RT A22WE 2007122800065 20071228 00065 NM 2007 12 28 HALA0700549 1 20071225 A 3150 WARNING SYSTEM BOEING 767 767332 1382001 NM MALFUNCTIONED A HALA O OTHER N FALSE WARNING CR CRUISE 1 WP 13 598HA 23278 ETOPS SIGNIFICANT SYSTEM, FMC MESSAGE: "FUEL DISAGREE-PROG 2" TOTALIZER: 30.8 CALCULATED: 27.3 FUEL QTY IND TOTAL QTY: 3 0.7. ACCOMPLISHED FIM 34-61-00 FIG 106, NO FAULTS INDICATED. ACCOMPLISHED FIM INDEX 34-63-20 STEP 2. CURRENT DATE ACT IVE. DIFFERENCE WITHIN SYSTEM TOLERANCE. 2 L 7 2 4F RT A1NM 2007122800076 20071228 00076 NM 2007 12 28 2007UALA05106 1 20071213 A 3350 8100133801 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 33R BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 215UA 30221 FOUND SEAT 33R, SEAT EEL LIGHT BROKEN. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007122800084 20071228 00084 EU 2007 12 28 SIMA200735105 1 20071204 A 5320 SILL SAAB SF340 340B 7860101 EU BS 236 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 307AE 21265 5000 340B307 DURING IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REPAIRED SERVICE DOOR CENTER SILL PER EM BRAER SRM (SRM-145/1142 REV 38) CHAPTER 53-21-02 PARAGRAPH 2. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007122800092 20071228 00092 NM 2007 12 28 2007UALA04994 1 20071206 A 2612 LAMP AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FIRE HANDLE INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 826UA 989 NR 1 ENGINE FIRE HANDLE HAS FOUR OUT OF EIGHT LIGHTS INOP. RELAMPED AND SWAPPED LGCIU AND ENG/APU FIRE IND PANEL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007122800094 20071228 00094 NM 2007 12 28 2007UALA04996 1 20071206 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 EMERGENCY LIGHT STRIP IS COMING LOOSE AT 7C. RESECURED EEL STRIP, PERFORMED OPS CHECK - FUNCTIONS NORMALLY. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122800107 20071228 00107 NM 2007 12 28 2007UALA05113 1 20071214 A 2913 PUMP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE HYD SYS LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 671UA 30026 RT HYD PUMP LEAKING. 2 L 7 2 4F 4 F RT A1NM E24NE 2007122800108 20071228 00108 NM 2007 12 28 2007UALA05114 1 20071216 A 2130 UNKNOWN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE UNKNOWN A UALA B EMER. DESCENT O OTHER NR NOT REPORTED 1 WP 29 349UA 24253 FLIGHT LOST CABIN PRESSURE, DESCENDED TO FL 100. FLT ABLE TO PRESS, CABIN CLIMB TO FL240. UNABLE TO CLIMB HIGHER. CON TINUED FLIGHT TO PLANNED DESTINATION. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122800117 20071228 00117 EU 2007 12 28 2007UALA05122 1 20071216 A 2121 VD3920 FAN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EXTRACT VENT SEIZED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 493UA 1821 EMERGENCY DECLARED DUE TO SMOKE IN THE CABIN. FAILED VENT FAN BEARING. REPLACED OUTBOARD VENT FAN. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010200004 20080102 00004 2008 1 2 ASAA0752381 4 20071213 A 2310 8220990004 TRANSCEIVER BOEING 737 737890 1384527 NM HF COMM INTERMITTENT A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 584AS 35682 NO SIDETONE ON HF1 FROM EITHER SEAT. HF1 RECEIVES OK. VOICE & SELCAL OTHER RADIOS WORK OK. ON CAPT'S SIDE VHF & F/O'S SIDE HF2 WORK OK. REPLACED NR 1 HF TRANSCEIVER. GROUND VERIFICATION TEST GOOD, VERIFICATION FLIGHT SATISFACTORY. 2 L 7 2 4F RT A16WE 2008010200010 20080102 00010 2008 1 2 COMA0760693 4 20071205 A 3420 6229336400 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAILED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 784CA 18123 7319 FLIGHT 5452 - AHC NR 1 FAILED EN ROUTE, CVG TO ABE. AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLA CED NR 1 AHC. 2 L 7 2 4F RT A21EA 2008010200049 20080102 00049 EA 2008 1 2 COMA0760720 1 20071213 A 5313 601R35004101 STRINGER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 779CA 7670 BAGGAGE CART STRUCK AIRCRAFT JUST AFT OF APU EXHAUST. REPLACED STRINGER 15 FROM STA 688 TO STA 736 PER SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008010200058 20080102 00058 NM 2008 1 2 SWAA076333 1 20071218 A 3350 20121A CHARGER BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED 14Y CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2008010200059 20080102 00059 NM 2008 1 2 SWAA076332 1 20071218 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010200060 20080102 00060 2008 1 2 SWAA076335 4 20071218 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008010200062 20080102 00062 NM 2008 1 2 SWAA076336 1 20071218 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 445WN 29841 DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS CRACKED AT ROW 4 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008010200063 20080102 00063 NM 2008 1 2 SWAA076337 1 20071218 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 485WN 32473 DURING SCHEDULED HC1 CHECK, LT FWD CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PAC K PER MM. 2 L 7 2 4F RT A16WE 2008010200064 20080102 00064 NM 2008 1 2 SWAA076340 1 20071218 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 485WN 32473 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PA CK PER MM. 2 L 7 2 4F RT A16WE 2008010200067 20080102 00067 NM 2008 1 2 SWAA076341 1 20071218 A 5330 6545768 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 487B, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008010200068 20080102 00068 NM 2008 1 2 SWAA076350 1 20071218 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008010200075 20080102 00075 2008 1 2 SWAA076344 4 20071218 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008010200077 20080102 00077 NM 2008 1 2 SWAA076353 1 20071218 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008010200080 20080102 00080 NM 2008 1 2 SWAA076356 1 20071218 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008010200082 20080102 00082 2008 1 2 ASAA0752389 4 20071219 A 3460 1714970501 FMC BOEING 737 737890 1384527 NM E&E BAY MALFUNCTIONED A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 587AS 35684 LEFT FMC FAILED. COULD NOT DUPLICATE LEFT FMC FAILURE. PERFORMED FMCS SYS TEST IAW MM 34-61-00. OPS NORMAL. 2 L 7 2 4F RT A16WE 2008010200083 20080102 00083 2008 1 2 SWAA076359 4 20071219 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT SKIRT FRAYED. REMOVED AND REPLACED VAC SLIDE PER MM . 2 L 7 2 4F RT A16WE 2008010200089 20080102 00089 NM 2008 1 2 SWAA076363 1 20071219 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008010200100 20080102 00100 NM 2008 1 2 SWAA076374 1 20071219 A 3350 65C27093 LIGHT BOEING 737 7373Y0 1384671 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008010200102 20080102 00102 NM 2008 1 2 SWAA076382 1 20071219 A 5530 6546872 FITTING BOEING 737 7373G7 1384595 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND RT VERTICAL STABILIZER AFT INBOARD FAIL SAFE FITTING CORRODED. REMOVED AND REPLACED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008010200110 20080102 00110 NM 2008 1 2 SWAA076397 1 20071220 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 23L CORRODED AT BS 375. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008010200111 20080102 00111 NM 2008 1 2 SWAA076398 1 20071220 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 22L CORRODED AT BS 737. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008010200116 20080102 00116 NM 2008 1 2 SWAA076409 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200117 20080102 00117 NM 2008 1 2 SWAA076430 1 20071220 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008010200119 20080102 00119 NM 2008 1 2 SWAA076412 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200125 20080102 00125 NM 2008 1 2 SWAA076405 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200127 20080102 00127 NM 2008 1 2 SWAA076406 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200130 20080102 00130 NM 2008 1 2 SWAA076426 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200135 20080102 00135 NM 2008 1 2 SWAA076414 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200136 20080102 00136 NM 2008 1 2 SWAA076429 1 20071220 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 887, STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008010200139 20080102 00139 NM 2008 1 2 SWAA076416 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200143 20080102 00143 NM 2008 1 2 SWAA076420 1 20071220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010200152 20080102 00152 NM 2008 1 2 SWAA076392 1 20071220 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 486WN 33852 DURING SCHEDULED HC1 CHECK, LT FWD CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PAC K PER MM. 2 L 7 2 4F RT A16WE 2008010200155 20080102 00155 NM 2008 1 2 SWAA076396 1 20071220 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 732SW 27864 EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008010200164 20080102 00164 NM 2008 1 2 ASAA0772397 1 20071205 A 5320 146A75032 FLOOR SUPPORT BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT FLOOR SUPPORT RAIL BS 767+5 RBL 3 CORRODED. REPAIR WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008010200167 20080102 00167 NM 2008 1 2 ASAA0772401 1 20071205 A 5321 453A261013 FLOOR PANEL BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 AFT CARGO PIT FLOOR PANEL AT STA 727D TO 767 CORRODED ALONG EDGES. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008010200171 20080102 00171 NM 2008 1 2 ASAA0772405 1 20071205 A 5330 143A32335 DOUBLER BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 FWD CARGO PIT RADIO ANT INTERNAL DBLR BS 500 TO 500A BL 0 CORRODED. FWD CARGO PIT RADIO ANTENNA INTERNAL DOUBLER AT BS 500 TO BS 500A BL 0 WAS BLENDED OUT AND FOUND TO BE BEYOND ALLOWABLE LIMITS IAW B737 700 SRM 53 00 53. DOUBLER REPLACED WITH REPAIR PART IAW B DRWG 143A3233 & B737 700 SRM 51 30 01. 2 L 7 2 4F RT A16WE 2008010200172 20080102 00172 NM 2008 1 2 AMTA200700614 1 20071117 A 3010 ANTI-ICE VALVE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LT WING MALFUNCTIONED A AMTA K NONE J WARNING INDICATION CR CRUISE 1 GL 11 518AT 27974 EICAS MSG L WING ANTI-ICE DISPLAYED AND WING ANTI-ICE VALVE LIGHT REMAINED ILLUMINATED WITH SWITCH ON. REMOVED AND REPL ACED LT WING ANTI-ICE VALVE. LEAK AND OPS CHECK GOOD REM MM 30-11-02-4. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010200173 20080102 00173 2008 1 2 AMTA200700617 4 20071117 A 2310 9640452022 TRANSCEIVER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE HF COMM UNSERVICEABLE A AMTA K NONE L NO TEST CR CRUISE 1 GL 11 522AT 29330 RT HF TRANSMISSION AND RECEPTION INOP AT ALL CREW STATIONS. REPLACED RT HF RT BITE CHECK GOOD. CONTACT, RADIO CHECK GO OD. REM MM 23-11-03. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010200174 20080102 00174 WP 2008 1 2 AMTA200700618 1 20071117 A 2120 UNKNOWN DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL CABIN ODOR A AMTA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 705TZ 46915 STRONG ELECTRICAL SMELL NEAR 3R EXIT DOOR. INSP AREA AND CONNECTORS OP DOOR SEVERAL TIMES NO ODOR, SMELL. OK FOR SERVI CE. (K) 2 L 7 3 4F 4 F A22WE A23EA 2008010200177 20080102 00177 EA 2008 1 2 TRAX200701889 1 20071208 A 3350 CHARGER CNDAIR CL600 CL6002C10 1390015 EA CABIN READS LOW A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 722EV 10127 EMERGENCY BATTERY CHARGER NR 1 READING LOW VOLTAGE. 2 L 7 2 4F RT A21EA 2008010200184 20080102 00184 EA 2008 1 2 A6WA200740639 1 20071116 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 427ZW 7685 CRACK EXIST ON FLOORBEAM FS 280 RBL 9 OUTBOARD CRACK ON FLOORBEAM .750 INCH. FLOORBEAM REPAIRED IAW CRJ 200 REO 601R-53 -11-1171. (M) 2 L 7 2 4F RT A21EA 2008010200187 20080102 00187 EA 2008 1 2 A6WA200740691 1 20071210 A 5280 SKIN CNDAIR CL600 CL6002B19 1900309 EA MLG DOOR DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 432AW 7257 ON MLG DOOR RIGHT INNER SKIN, ABRASION EXIST ON FORWARD SIDE OF DOOR, LOWER AND UPPER. (M) REPAIRED IAW REO 601R-52-8 2-016 AND REO 601R-52-82-102. (K) 2 L 7 2 4F RT A21EA 2008010200192 20080102 00192 EA 2008 1 2 A6WA200740671 1 20071130 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 433AW 7289 CRACK FOUND ON 4 BRACKET FS 280 LBL 9 AND RBL 9 CRACK LENGTH IS 1 INCH. (M) 3 BRACKETS REPLACED ON FS 280, LBL 9, OB A ND IB AND RBL 9 OB IAW REO 601R-53-11-171 REV-D. BRACKET REPLACED ON FS 280, RBL 9, IB IAW CRJ 200, SRM 51-42-06. (K) 2 L 7 2 4F RT A21EA 2008010200196 20080102 00196 SO 2008 1 2 C2XA07RI108 1 20071224 A 3397 CONNECTOR EMB 145 EMB145XR 3260214 SO CABIN LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11113 145662 RIC: DURING A ROUTINE MX INSPECTION, SEAT 12A LOWER SIDEWALL EMERGENCY EXIT LIGHT FOUND INOP. REPAIR SECURED SEAT 12A L OWER SIDEWALL EMERGENCY EXIT LIGHT CONNECTOR IAW EMB145XR AMM 33-50-13. OPS CHECK GOOD. A/C APPROVED FOR RETURN TO SER VICE. 2 L 7 2 4F RT 2008010300020 20080103 00020 NM 2008 1 3 07FDEA05069 1 20071217 A 5320 ACJ703212 CHANNEL DOUG MD11 MD11F 3023600 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 524FE 48480 FORWARD CARGO COMPARTMENT: STA 615 X = 40 CHANNEL DOLLY ASSEMBLY END STOP MOUNTING AREA FOUND DAMAGED. COMPLIED WITH FE DEX E.A.# 1-5340-117080. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008010300021 20080103 00021 NM 2008 1 3 07FDEA05070 1 20071217 A 5320 ACJ703212 CHANNEL DOUG MD11 MD11F 3023600 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 524FE 48480 FORWARD CARGO COMPARTMENT: STA 615 X = -40 CHANNEL DOLLY ASSEMBLY END STOP MOUNTING ANCHOR NUT MOUNTING AREA FOUND DAMAG ED. COMPLIED WITH FEDEX E.A.1-5340-117080. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008010300022 20080103 00022 NM 2008 1 3 07FDEA05071 1 20071217 A 5320 ADJ70982 CHANNEL DOUG MD11 MD11F 3023600 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 524FE 48480 FORWARD CARGO COMPARTMENT: STA 899 TO STA 919 X = -40 CHANNEL DOLLY ASSEMBLY RETRACTOR MOUNTING HOLE FOUND ELONGATED. C OMPLIED WITH FEDEX E.A. 1-5340-117082, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008010300023 20080103 00023 NM 2008 1 3 07FDEA05072 1 20071217 A 5320 ADJ70901 CHANNEL DOUG MD11 MD11F 3023600 NM ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 524FE 48480 FORWARD CARGO COMPARTMENT: STA 859 TO STA 899 X = -35 CHANNEL FOUND CHAFED. COMPLIED WITH FEDEX E.A. 1-5340-117085, RE PAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008010300024 20080103 00024 NM 2008 1 3 07FDEA05073 1 20071217 A 5320 ADJ70901 CHANNEL DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 524FE 48480 FORWARD CARGO COMPARTMENT: STA 979 TO STA 1019 X = -35 CHANNEL FOUND CRACKED. COMPLIED WITH FEDEX E.A. 1-5340-117084, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008010300025 20080103 00025 EU 2008 1 3 07FDEA05074 1 20071217 A 3150 UNKNOWN AIRBUS 300 A300F4605R 3930327 EU UNKNOWN A FDEA C E ABORTED TAKEOFF ENGINE SHUTDOWN J WARNING INDICATION TO TAKEOFF 1 SO 25 671FE 778 IMMEDIATELY AFTER SELECTING TOGA ON THE RUNWAY GOT A CHIME AND ECAM MESSAGE. INITIATED AN ABORT THEN SAW AN ECAM MESSAG E INDICATING FMS DISAGREE. TAXIED CLEAR AND RELOADED THE RUNWAY IN THE FMS. ON THE SECOND TAKEOFF ATTEMPT THE TOGA LE VERS WOULD NOT ENGAGE WHEN SELECTED. CYCLED ALL FCC, FAC, AND TCC C/B'S REALIGNED ALL 3 IRU'S AND PERFORMED AFS LAND TE ST IAW A300-600 MM 22-40-00. OP'S GOOD TOGA SYSTEM OP'S GOOD IAW A300-600 MM 22-30-00-5-01. GOOD LEG INTO YMX, 2:47 FL T TIME. 2 L 7 2 4F RT A35EU 2008010300026 20080103 00026 NM 2008 1 3 DXTA200702685 1 20071217 A 3260 D233360001 PROXIMITY SENSOR AMD FALC50 FALCON2000 2730170 NM PWC PW308 PW308C 52182 NE MLG INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 232QS 439 115 LT MAIN GEAR FAILED TO RETRACT. TROUBLESHOT, FAULT CD 000315 PRESENT ON BSCU1 DURING GEAR SWING. REMOVED PROX SENSOR 40 GAA P/N D23336000-1, S/N 02551 AND INSTALLED REPAIRED PROX SENSOR 40GAA P/N D23336000-1, S/N 02555 IN ACCORDANCE WITH F2 000EX EASY MM 32-315. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A50NM E00065EN 2008010300027 20080103 00027 CE 2008 1 3 DXTA200702687 1 20071217 A 2170 7464513 COALESCER BAG CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL A/C PACK DIRTY E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 983QS 7500083 BAD SMELL IN CABIN 7 LARGE ANOUNTS OF MOISTURE COMING FROM WEEMACS AND FLOOR VENTS. REMOVED AND REPLACED BOTH ACM FILTE R SOCKS WITH NEW SOCKS, RAN APU OPS AND LEAK CHECK GOOD AT THIS TIME IAW CE-750 MM 21-51. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008010400001 20080104 00001 EA 2008 1 4 TRAX200701929 1 20071212 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 903EV 7621 EXTERNAL DECALS ON CREW ESCAPE HATCH REQUIRE REPLACEMENT. 2 L 7 2 4F RT A21EA 2008010400005 20080104 00005 CE 2008 1 4 DXTA200702676 1 20071213 A 3150 WARNING SYSTEM CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE ROLL SYSTEM FALSE INDICATION E DXTA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 GL 07 365QS 6800057 AMBER (ROLL SYSTEM CONTROL FAULT) APPEARED SEVERAL TIMES ON DESCENT, WITH AUTOPILOT ON AND OFF. TESTED SEVERAL TIMES WI THOUT DUPLICATING THE DISCREPANCY. VIEWED MAINTENANCE DIAGNOSTICS AND FOUND FIVE OCCURENCES OF THE "ROLL SYSTEM CONTR OL FAULT" DURING ONE LEG OF FLIGHT. NONE OF THESE MESSAGES CORRELATED TO A HARDWARE FAILURE. RETURNED AIRCRAFT TO AN A IRWORTHY CONDITION. 2 L 7 2 4F 4 F RC T00012WI E35NE 2008010400009 20080104 00009 EA 2008 1 4 TRAX200701935 1 20071214 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 882AS 7503 FLT 4822, UNABLE TO OPEN ASD. 2 L 7 2 4F RT A21EA 2008010400010 20080104 00010 EA 2008 1 4 TRAX200701936 1 20071214 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 874AS 7551 SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. 2 L 7 2 4F RT A21EA 2008010400012 20080104 00012 EA 2008 1 4 TRAX200701938 1 20071215 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 856AS 7404 EMERGENCY EXIT CEILING LIGHT INOP. 2 L 7 2 4F RT A21EA 2008010400017 20080104 00017 SO 2008 1 4 C2XA07RI109 1 20071225 A 3350 110049 POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 26545 145558 EWR: DURING A ROUTINE MX INSPECTION, MX FOUND "LT AND RT EXTERIOR OVERWING EMERGENCY LIGHTS INOP". REPAIR MX "REMOVED A ND REPLACED NR 4 BATTERY POWER SUPPLY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE . 2 L 7 2 4T RT T00011AT 2008010400020 20080104 00020 SO 2008 1 4 C2XA07IA250 1 20071217 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13992 145284 IAH - FLIGHT 2802, DURING PREFLIGHT INSPECTION, THE CREW REPORTED SOME EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 6 EMERGENCY LIGHT INVERTER. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008010400023 20080104 00023 SO 2008 1 4 C2XA07IA251 1 20071219 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 13975 145163 FLIGHT 2875 IAH-MFE, THE CREW REPORTED A BURNING ELECTRICAL SMELL IN THE COCKPIT. THE AIRCRAFT RETURNED TO IAH AND LAND ED WITHOUT INCIDENT. MAINTENANCE PERFORMED AN INSPECTION AND SYSTEM CHECKS. THE BURNING SMELL COULD NOT BE DUPLICATED AND THE DISCREPANCY WAS CLEARED. 2 L 7 2 4T RT T00011AT 2008010400024 20080104 00024 NE 2008 1 4 DXTA200702683 2 20071215 A 7200 30500005 ENGINE AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE RIGHT FAILED E DXTA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 GL 07 226QS 5489 126 P105430 HAD AN UNCOMMANDED NR 2 ENGINE FAILURE AT FL430. WE OBSERVED A FADEC 2 MWP LIGHT AND THEN AN UNCOMMANDED SHUTDOWN OF THE ENGINE. REPLACED A FAILED RT ENGINE PER THE MM 54-010, 54-104, 54-106, 54-107, 71-000, 71-015 AND THE ENGINE LMM 72-00 -00, 72-00-08, 72-70-06 AND 79-30-02. ENGINE SERVICED WITH TURBINE OIL. GROUND OPERATIONAL AND LEAK CHECK SATISFACTORY ( POWER ASSURANCE RUN) SATISFACTORY. 2 L 7 2 4F 4 F RT A50NM E44NE 2008010400025 20080104 00025 CE 2008 1 4 DXTA200702684 1 20071217 A 3260 69481013 UPLOCK SWITCH CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE MLG FAILED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 380QS 1081 6800089 AFTER TAKEOFF, RETRACTED LANDING GEAR, THE UNLOCK LIGHT REMAINED ON. FOUND RIGHT HAND LANDING GEAR UPLOCK SWITCH FAILED .REPLACED RIGHT HAND LANDING GEAR UPLOCK SWITCH WITH NEW SWITCH PER MM 32-60-00. PERFORMED GEAR SWINGS. OPERATIONAL CHE CK GOOD. 2 L 7 2 4F 4 F RC T00012WI E35NE 2008010400026 20080104 00026 CE 2008 1 4 DXTA200702686 1 20071217 A 2750 67183281 CONTROLLER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS FAILED E DXTA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 07 919QS 4039 7500224 AFTER TAKE-OFF, RETRACTED THE FLAP, THE FLAPS FAILED. TROUBLESHOT TO AN INTERNALLY FAILED FLAP CONTROLLER. REPLACED CON TROLLER WITH AN INSPECTED UNIT. FUNCTIONAL CHECK GOOD. ALL WORK IAW CH 27-50-00 OF THE CE-750 M.M. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008010400031 20080104 00031 SO 2008 1 4 C2XA07RI105 1 20071207 A 3412 102AU1AF TAT PROBE EMB 145 EMB145XR 3260214 SO NR 2 INOPERATIVE A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 25134 13423 13423 145714 FLT 2993 - EWR - CREW REPORTED TAT 2 HEAT INOP MESSAGE ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY . EWR MX REMOVED AND REPLACED NR 2 TAT PROBE IAW EMB145XR AMM 34-15-03 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. 2 L 7 2 4F RT 2008010400032 20080104 00032 EU 2008 1 4 2007UALA05130 1 20071215 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GALLEY ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 470UA 1427 ELECTRICAL ODOR NOTICED IN AFT GALLEY. SELECTED GALLEY POWER OFF AN D RECONFIGURED AVIONICS FAN SYSTEM. RETURNED POWER AND AEVC SYS TO NORMAL. TURNED ON ALL LIGHTS AND GALLEY EQUIP IN AFT GALLEY AREA, OPERATED EQUIP AND NO ODORS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010400034 20080104 00034 SO 2008 1 4 C2XA07ON037 1 20071209 A 2621 346000731 EXTINGUISHER EMB 145 EMB145LR 3260212 SO BAGGAGE DISCHARGED A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 14570 16988 4070 145632 FLT 7756 - LAX TO LAX - DURING GROUND HANDLING BY TOWING CREW BOTH BAGGAGE FIRE BOTTLES WERE DISCHARGED. MX AT LAX REMO VED AND REPLACED BOTH FIRE BOTTLE AND AIRCRAFT WAS RETURN FOR SERVICE IN AIRWORTHY CONDITIONS. 2 L 7 2 4T RT T00011AT 2008010400035 20080104 00035 SO 2008 1 4 C2XA07ON034 1 20071205 A 2611 473559713 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO CARGO BAY INOPERATIVE A C2XA K NONE O OTHER UK UNKNOWN 1 SW 27 15555 13523 13523 145594 FLT 0108 - ONT TO BOI - DURING FLIGHT, FLIGHT CREW REPORTED BAG SMOKE MESSAGE DID NOT APPEAR ON EICAS. MX AT LAX REMOVE D AND REPLACED NR 1 BAGGAGE BIN SMOKE DETECTOR, OPERATIONALLY CHECK GOOD AND A/C WAS RELEASE TO RETURN FOR SERVICE IN AI RWORTHY CONDITIONS. 2 L 7 2 4T RT T00011AT 2008010400055 20080104 00055 SO 2008 1 4 C2XA07SH107 1 20071218 A 3697 SPLICE EMB 145 EMB145EP 3260221 SO BLEED AIR SYS DAMAGED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 16927 145006 SHV - FLIGHT 2249 - DIVERTED INTO SHV DUE TO A BLEED 2 VALVE FAIL MESSAGE ON DEPARTURE. MAINTENANCE REPAIRED SPLICE SP 11183 IAW EMB 145 SWPM 20-21-00. OPS CHECK GOOD IAW EMB 145 AMM II 36-00-00-700-803-A. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008010400056 20080104 00056 SO 2008 1 4 C2XA07CL108 1 20071226 A 3350 66361 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13995 145295 DURING ROUTINE MAINTENANCE, THE AISLE PATH EMERGENCY LIGHT STRIP WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLA CED THE NR 3 AISLE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008010400061 20080104 00061 SO 2008 1 4 C2XA07IA242 1 20071211 A 3097 S010498987 SOCKET EMB 135 EMB135LR 3260305 SO COCKPIT BURNED A C2XA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 28529 145512 XNA - FLIGHT 2413, THE CREW REPORTED PITOT HEAT FAIL MESSAGE FOLLOWED BY SMOKE IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED RELAY SOCKET TXK0054 WHICH WAS FOUND TO BE BURNT, AND RELAY K0054 AS A PRECAUTION, OP ERATIONALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008010400062 20080104 00062 SO 2008 1 4 C2XA07IA244 1 20071210 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO CABIN ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16151 145758 IAH - FLIGHT 2680, THE CREW REPORTED THAT AFTER STARTING THE APU ON THE GROUND, AND OPENING APU BLEED AIR, THERE WAS A S TRONG ODOR OF JET FUEL IN THE CABIN. THE AIRCRAFT CONTINUED TO THE GATE WHERE MAINTENANCE OPERATIONALLY CHECKED THE APU WITH NO DEFECTS, OR ODORS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008010400075 20080104 00075 NM 2008 1 4 CALA0700768 1 20071218 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17619 27332 CABIN STA 400 BETWEEN RIGHT STRINGER 8 AND PUS RAIL ATTACH BRACKET TO FRAME CRACKED. REPIARED PER ECRA 5310-04684. 2 L 7 2 4F RT A16WE 2008010400076 20080104 00076 NM 2008 1 4 CALA0700769 1 20071218 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17619 27332 CABIN STATION 440 BETWEEN STRINGER 8 AND 9 PSU RAIL ATTACH BRACKET TO FRAME CRACKED LEFT SIDE. REPAIRED PER ECRA 5310-0 4684. 2 L 7 2 4F RT A16WE 2008010400084 20080104 00084 NM 2008 1 4 CALA0700746 1 20071208 A 5311 6546532 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 FUSELAGE CRACKED AT STA480 B/W STR 8 AND 9. REPAIRED PER EA 5310-04498 2 L 7 2 4F RT A16WE 2008010400092 20080104 00092 NM 2008 1 4 SB07109 1 20071220 A 7797 GROUND WIRE BOEING 737 737401 1384701 NM NR 1 ENGINE DAMAGED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 422US 23989 FLT 1803 DURING CRUISE, EN ROUTE FROM PHL TO PIT, THE NR 1 ENGINE EGT INDICATED 1,800. CREW DECLARED AN EMERGENCY AND R ETURNED TO FIELD AT PHL. FLIGHT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND TWO BROKEN S HIELDED WIRE GROUNDS AT CONNECTOR DISCONNECT FOR THE NR 1 ENGINE. REPLACED SHIELDED WIRE PAIRS W3760-220-20W/-219-20R AN D W3760-218-20W/-217-20R PER WM 77-31-11 AND SWPM. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2008010400098 20080104 00098 NM 2008 1 4 CALA0700757 1 20071214 A 5230 6547952162 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 C2 DOOR OUTER SKIN CRACKED AT DOOR HANDLE CUT-OUT. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 52-00-01 FIG 201 REPAIR NR 3 2 L 7 2 4F RT A16WE 2008010400100 20080104 00100 NM 2008 1 4 CALA0700759 1 20071215 A 5310 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 FWD BAG BIN FWD DOOR FRAME CRACKED AT LWR STOP PAD INSTALLED DOOR FRAME REF SRM 51-40-02 AND EA 5310-04443. 2 L 7 2 4F RT A16WE 2008010400101 20080104 00101 NM 2008 1 4 CALA0700760 1 20071215 A 5310 654795978 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 AFT CARGO DOOR FWD FRAME CRACKED AT LOWER STOP PAD REMOVED AND REPLACED AFT CARGO FWD FRAME PER DWG 65-47959 AND SRM 51- 40-02. 2 L 7 2 4F RT A16WE 2008010400106 20080104 00106 NM 2008 1 4 DLM90071622 1 20071214 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 RT CUSP WEB CORRODED FS 1155-1193. REPAIRED RT CUSP WEB FS 1155-1193 IAW EA 398191-14MA ON N/R 2700-0196 AT HMV-2 IN OK C. 2 L 7 2 4F RT A6WE 2008010400113 20080104 00113 NM 2008 1 4 DL764071629 1 20071216 A 5330 143T35218 SKIN BOEING 767 767432ER 1385134 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 844MH 29717 SKIN DENTED AT FS 654A+110 TO FS 654 S29R TO 30R. DAMAGE CUTOUT AND A REPAIR DOUBLER INSTALLED. 2 L 7 2 4F RT A1NM 2008010400117 20080104 00117 NM 2008 1 4 DLM90071634 1 20071215 A 5320 5930961 FLOOR SUPPORT DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 AFT PAX CABIN FLOOR SUPPORT BEAM AT STA 1307 LT SIDE HAS CORROSION ON LT END. FABRICATED AND INSTALLED NEW FLOOR SUPPOR T IAW MD-90 SRM 51-30-05 ON N/R 2000-0201 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2008010400119 20080104 00119 NE 2008 1 4 07FDEA05112 2 20071220 A 7200 ENGINE DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE NR 2 POWER LOSS A FDEA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 25 620FE 48791 DURING CLIMB FROM FL320 TO FL340 NOTICED A/C DETERIORATION. NR 2 ENG EPR READ .40 LESS THAN NR 1 AND NR 3. N1 READIN G 20 PERCENT LESS THAN 1 AND 3, N2 20 PERCENT LESS AS WELL. ENG 2 THROTTLE, MOVEMENTS RESULTED IN SLUGGISH RESPONSE W/M AX EPR OUTPUT OF 1.08 AND AT 80 PERCENT N1. SECONDARY ENG PARAMETER READINGS NORMAL FF NR 2 AT 1.00 EPR, N1 76.5, EGT 3 70, N2 86 WAS 4000LB/HR FL 310 OAT-32 DEG C TARGET EPR WAS 1.27 M.830 IAS 309 KTS TAT +1 DEG C. DIVERTED TO SIN. FOUND 9 FAN BLADES DAMAGED ON ENGINE NR 2. REMOVED AND REPLACED FAN BLADES IN PAIR TOTAL 18EA. REMOVED AND REPLACED FUEL ME TERING UNIT. REMOVED AND REPLACED NR 2 ENG EEC. 01-2008 REPLACED NR 2 ENGINE. 2 L 7 3 4F 4 F RT A22WE E24NE 2008010400120 20080104 00120 NE 2008 1 4 DL76L071636 2 20071219 A 7597 79275516 TERMINAL BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE HPSOV BROKEN A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 176DN 25061 724638 DURING CLIMB-OUT FROM JFK, THE LEFT ENGINE BLEED/BLEED LIGHT AND AURAL WARNING KEPT CYCLING. HAD THEM RESET C/B P11S11 FOR THE LEFT ENGINE BLEED CONTROL WHICH FIXED FOR A SHORT PERIOD AND THEN THE PROBLEM RETURNED. DUE TO PREV HISTORY, OP TED TO RETURN THE AIRCRAFT TO JFK AND SWAP EQUIP. FOUND NR 2 TERMINAL BROKEN OFF ON HPSOV VALVE AS PRECAUTION RE-TER MINATED ALL 3 TERMINALS ON VLV PER MM. RAN ENG, OPS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010400126 20080104 00126 NM 2008 1 4 DLM90071632 1 20071218 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 LT CABIN CUSP WEB CORRODED ENTIRE LENGTH 598-655. REMOVED AND REPLACED LT CABIN CUSP WEB FS 598-655 PER MD-90 51-30-01 ON N/R 2700-0143 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2008010400129 20080104 00129 2008 1 4 DL76G071608 4 20071212 A 2565 251706365 BOTTLE BOEING 767 767332 1382001 NM PWA JT8 JT8D219 52053 NE EVAC SLIDE EMPTY A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1608 30573 726047 LEFT OVERWING SLIDE BOTTLE FOUND EMPTY DURING ROUTINE CHECK BOTTLE REPLACED. 2 L 7 2 4F 4 F RT A1NM E9NE 2008010400135 20080104 00135 NM 2008 1 4 DLM90071617 1 20071214 A 5320 991015199 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 LT CUSP WEB OUT OF LIMITS FS 924-962. REPAIRED LT CUSP WEB FS 924-962 IAW MD-80 DRD 53-05D FIG 827D ON N/R 2400-0163 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2008010400142 20080104 00142 NM 2008 1 4 DHL2007746001 1 20071220 A 5752 652172630 TAB BOEING 727 727224 1384076 NM RT AILERON DEBONDED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 UPON WALK AROUND INSPECTION, FOUND RIGHT OUTBOARD AILERON TAB OUTBOARD DISBONDED ON UPPER SKIN APPROX 20 INCHES LONG. P ART REPLACED. 2 L 7 3 4F A3WE 2008010400151 20080104 00151 NM 2008 1 4 F3LA200700381 1 20071214 A 5320 D534711242001 SHEAR PLATE AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED SHEAR PLATE AT BS -Y1292 BETWEEN FR 69 AND FR 70 CORRODED. CORROSION FOUND TO B E OUT OF LIMITS IAW SRM 53-41-14-101. REMOVED AND INSTALLED REPLACEMENT SHEAR PLATE IAW SRM 51-42-11, SRM 51-44-11 AND EA A9-53R-12329. 2 L 7 2 4F RT A28NM 2008010400152 20080104 00152 NM 2008 1 4 F3LA200700382 1 20071213 A 2540 NAS130431 BOLT AIRBUS A319 A319111 3930336 NM LAVATORY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED LAV "D" MOUNT BOLTS CORRODED. REMOVED AND REPLACED CORRODED MOUNT BOLTS IAW AMM 25-43-41-PB401. 2 L 7 2 4F RT A28NM 2008010400177 20080104 00177 NM 2008 1 4 F3LA200700390 1 20071216 A 5320 D5348015900700 PLATE AIRBUS A319 A319111 3930336 NM GIRT BAR LATCH CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED R2 DOOR AFT GIRT BAR LATCH FILLER CORRODED. REMOVED AND REPLACED R2 DOOR AFT GI RT BAR LATCH FILLER PANEL IAW AMM 53-42-12-PB401. 2 L 7 2 4F RT A28NM 2008010400191 20080104 00191 NM 2008 1 4 F3LA200700394 1 20071214 A 5315 D53472090010 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT Y1292, FR66, CORRODED AT NUTPLATE HOLES. REMOVED AND REPLACED FLOO RBEAM AT Y1292, FR66, IAW SRM 51-42-11. 2 L 7 2 4F RT A28NM 2008010800381 20080108 00381 2008 1 8 AMTA200700672 4 20071204 A 3425 SYMBOL GENERATOR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RIGHT MALFUNCTIONED A AMTA K NONE O OTHER TX TAXI/GRND HDL 1 GL 11 522AT 29330 R SYMBOL GENERATOR FAILED AFTER LANDING. UNABLE TO LOCATE FIRM CODE REASONABLE TIME. RESET AC POWER. OPS CHECKS OK ON GROUND. OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010800391 20080108 00391 CE 2008 1 8 DJFA2007143 1 20071213 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZ STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 743TA RK271 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER INBOARD RIB AND BRACKET ASSEMBLIES, THE RIGHT INBOARD RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF TH IS AREA ARE OUTLINED IN BEECHJET COMMUNIQUE' NR 70. MAINTENANCE REPLACED BOTH RIBS WITH IMPROVED ASSEMBLIES. 2 H 7 2 4F 4 F RT A16SW E25EA 2008010900009 20080109 00009 NM 2008 1 9 070181 1 20071228 A 4930 360231033 FUEL CONTROL DOUG MD80 MD83 3023681 NM APU LEAKING A WX0A D RETURN TO BLOCK K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 19 892GA 49826 FLIGHT 705 AT GSP (GREENVILLE,SC), FLIGHT CREW REPORTED DURING TAXI TO THE GATE UPON APU START THE SMELL OF FUEL AND SMO KE FILLED THE CABIN. ON CALL MTX INSPECTED THE AIRCRAFT AND APU AND DETERMINE THAT THE FUEL CONTROL WAS LEAKING FUEL IN TO THE AIR DUCT. APU WAS DEFERRED AND REPAIR WAS ACCOMPLISHED BY ALLEGIANT AIR MAINTENANCE DEPARTMENT PERSONNEL BY REPL ACING THE APU FUEL CONTROL. OPERATIONAL CHECK OF THE APU WAS NORMAL AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT 2008010900010 20080109 00010 NM 2008 1 9 070180 1 20071230 A 2150 A/C PACK DOUG MD80 MD83 3023681 NM LEFT SMOKE A WX0A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 19 865GA 49998 FLIGHT 603 FROM BLI, THE FLIGHT CREW DETECTED SMOKE IN THE CABIN, DECLARED AN EMERGENCY AND RETURN TO BLI. ON CALL MX PERSONNEL WERE DISPATCHED TO THE ACFT BY MX CONTROLLER. AIR CONDITIONING SYSTEM WAS INSPECTED AND IT WAS DETERMINED THA T THE LT AIR CONDITIONING SYSTEM WAS AT FAULT AND THE SYSTEM WAS DEFERRED. ADDITIONALLY IAW GMM PROCEDURES AN AIRBORNE SYSTEM TEST WAS ACCOMPLISHED WITH THE LT AIR CONDITIONING SYSTEM "OFF", NO SMOKE WAS DETECTED IN THE CABIN. THE LT AC S YSTEM DEFERRAL WAS CORRECT BY INSPECTING AND CLEANING THE LT PACK CABIN DUCT SENSOR. ACCOMPLISHMENT OF THE OPERATIONAL CHECK IAW AMM 21-61-00. CHECKED NORMAL AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT 2008010900021 20080109 00021 EU 2008 1 9 2007UALA05228 1 20071223 A 3510 D9231026600060 REGULATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LEAKING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 493UA 1821 CAPT OXYGEN MASK - PRESS TO TEST AND RESET- BUTTON NOT TESTING OK. LEAKING REGULATOR AT BOX. REPLACED O2 BOX AT CAPT P OSITION. TESTED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010900024 20080109 00024 EU 2008 1 9 2007UALA05239 1 20071223 A 3230 664700500A4C CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 FAULTY A UALA O OTHER J W WARNING INDICATION INADEQUATE Q C AP APPROACH 1 WP 29 424UA 506 LANDING GEAR DID NOT EXTEND WHEN HANDLE LOWERED, GOT ECAM WARNING. GEAR LOWERED AFTER 45 SECONDS. TROUBLE SHOOTING FAU LTED LGCIU 1 F120. REPLACED LGCIU1. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010900027 20080109 00027 WP 2008 1 9 NWAA074359946 1 20071221 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8926E 45863 DURING "H" CHECK, FOUND CRACKS IN SKIN AT FORWARD PASSENGER ENTRY DOOR CUTOUT AT AFT DOOR STOPS NR 3 AND NR 4. REPAIRED PER EA 99-211049. 2 L 7 2 4F A6WE 2008010900072 20080109 00072 WP 2008 1 9 AALA20072471 1 20071218 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 455AA 49560 LGA - EMERGENCY LIGHT AT TAIL COMPARTMENT INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008010900075 20080109 00075 WP 2008 1 9 AALA20072473 1 20071218 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 480AA 49655 LGA - EMERGENCY LIGHT AT OVERHEAD LEFT SEAT ROW 19 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD LEFT SEA T ROW 19. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008010900090 20080109 00090 EA 2008 1 9 SWIA200719016 1 20071230 A 3350 AD20131A POWER SUPPLY CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 746SK 2099 2099 10202 FLT 6710 - OVERHEAD EMERGENCY LIGHT POD IS INOP. REPLACED NR 4 ELBP IAW CRJ AMM 33-51-17. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008010900110 20080109 00110 EA 2008 1 9 MASA200700810 1 20071120 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17175 7175 FLT 7182, PHL - GEAR DISAGREE, NLG WOULD NOT COME DOWN. INSPECTED NOSE AREA, NO NOTICEABLE DAMAGE FOUND. REMOVED AND R EPLACED PRIORITY VALVE, GEAR SWINGS GOOD. 2 L 7 2 4F RT A21EA 2008010900122 20080109 00122 2008 1 9 2007UALA05316 4 20071227 A 2565 B14056112 O-RING AIRCRUISERS BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EVAC SLIDE DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 912UA 0322A 25290 LOW BOTTLE PRESSURE. FOUND PISTON O-RING LEAKING. REPLACE O-RING. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010900123 20080109 00123 NE 2008 1 9 2007UALA05318 2 20071228 A 7200 ENGINE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 1 MALFUNCTIONED A UALA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 WP 29 823UA 952 V10367 FLIGHT DIVERTED UNDER AMBER DUE TO NR 1 ENGINE PROBLEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010900124 20080109 00124 NM 2008 1 9 2007UALA05319 1 20071227 A 5313 STRINGER SPLICE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 STRINGER SPLICE 14L LOWER FLANGE IS CRACKED JUST FWD OF STA 360. REPLACED STRINGER SPLICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010900125 20080109 00125 EA 2008 1 9 MASA200700734 1 20071024 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75998 7336 ASH FLT 7369 LGA - FLAPS FAIL AT 34 DEGREES ON GO AROUND. CONTRACT MX COMPLIED WITH PART A. 2 L 7 2 4F RT A21EA 2008010900127 20080109 00127 NM 2008 1 9 2007UALA05320 1 20071227 A 5320 SUPPORT ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 DOOR 1L CUTOUT, AFT SIDE SUPPORT ANGLE CRACKED BS 348, SECOND DOOR STOP FITTING FROM BOTTOM. INSTALLED NEW "L" ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010900128 20080109 00128 NM 2008 1 9 2007UALA05321 1 20071227 A 2560 D31354437 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L2 DOOR OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 366UA 24535 CREW REPORTED DOOR 2L NOT CLOSING. FOUND SLIDE GIRT HANGING DOWN. REPLACED L2 DOOR SLIDE. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010900129 20080109 00129 NM 2008 1 9 2007UALA05322 1 20071227 A 2612 JKL737 BULB BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU APU FIRE HANDLE INOPERATIVE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 904UA 25004 BULB BURNED OUT IN APU FIRE HANDLE. SAMC TEXT: CREW REPORTS 3 OF THE 4 BULBS ARE OPERATIONAL. SUSPECT BURNED OUT LIGH T BULB. REPLACED LAMP. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010900130 20080109 00130 NM 2008 1 9 2007UALA05323 1 20071227 A 2612 JKL737 BULB BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 2 FIRE HANDLE INOPERATIVE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 NR 2 FIRE HANDLE ONE LIGHT BULB BURNED OUT. SUSPECT BURNED OUT LIGHT BULB. REPLACED LAMP. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010900131 20080109 00131 NM 2008 1 9 2007UALA05324 1 20071227 A 4920 APU BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FLAMED OUT A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 665UA 29237 APU FLAMED OUT AND WOULD NOT RESTART. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010900132 20080109 00132 NM 2008 1 9 2007UALA05325 1 20071227 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R3 DOOR OBSTRUCTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 546UA 25367 DOOR 3R WILL NOT ARM. FOUND DEBRIS ON/AROUND GIRT BAR FITTINGS PREVENTED POSITIVE ENGAGEMENT, CLEANED AREA AROUND GIRT BAR FITTINGS, DOOR ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010900170 20080109 00170 EA 2008 1 9 MASA200700789 1 20071110 A 2760 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA SPOILERS UNKNOWN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75993 7372 ASH FLT 7376 ORD - SPOILER AND SPOILERON FAULT. PERFORMED RESET OF SYSTEM, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008010900176 20080109 00176 EA 2008 1 9 MASA200700866 1 20071208 A 3244 TIRE CNDAIR CL600 CL6002B19 1900309 EA NLG FLAT A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 649BR 3886 7414 ASH 7168 IAD - STRONG VIBE IN NOSE GEAR AFTER GEAR WAS RETRACTED. MX FOUND NOSE TIRE WITH A FLAT SPOT AND THEY CHANGED BOTH NOSE TIRES. 2 L 7 2 4F RT A21EA 2008010900202 20080109 00202 EA 2008 1 9 MASA200700838 1 20071203 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 75995 7361 PILOTS BULKHEAD FS 280.0 BETWEEN RBL 9.0 AND LBL 9.0 CORROSION IS IN THE WEB AND CORROSION IN THE FLOOR ANGLE, REPAIRED. 2 L 7 2 4F RT A21EA 2008010900204 20080109 00204 NM 2008 1 9 SB07111 1 20071229 A 3350 1012721 LIGHT BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 440US 24811 PIT - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 4, LEFT-HAND SIDE, INOPERATIVE. MAINTENANCE REP AIRED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2008010900208 20080109 00208 NM 2008 1 9 KCSA07102 1 20071204 A 2697 WIRE BOEING 747 7472B4B 138481B NM FIRE DETECTOR CHAFED A KCSA K NONE N FALSE WARNING CL CLIMB 1 GL 23 713CK 21099 NR 1 ENG FIRE DETECTOR LOOP "B" FLUCTUATED AND FAULT LIGHT CAME ON DURING CLIMB. REPAIRED CHAFED WIRE JUST AFT OF LWR F WD LOOP IAW BSWP MM 20-10-13. SYSTEM OPS CHECKS GOOD IAW B747 AMM 26-11-00 PG 504. 2 L 7 4 4F RT A20WE 2008010900209 20080109 00209 EA 2008 1 9 MASA200700832 1 20071130 A 2750 860D10018ABCD FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27314 15768 7314 ASH RON ORD - FLAPS FAIL. REMOVED AND REPLACED FECU. 2 L 7 2 4F RT A21EA 2008010900210 20080109 00210 2008 1 9 BB07095 4 20071206 A 3460 98346190002 FMC BOEING 767 7672B7 1385107 NM LEFT FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 253AY 24894 FLT 798 PHL - AMS RETF - CREW REPORTED, "FMC WON'T ENTER THE IRS (3) DME MODE. PROGRESS PAGE 2 INDICATES BLANK. MAINTE NANCE REMOVED AND REPLACED LT FMC. 2 L 7 2 4F RT A1NM 2008010900235 20080109 00235 SO 2008 1 9 RAIA00712029 1 20071226 A 3350 RPS1B BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 834HK 145269 PRE FLT NR 7904 - ROA - EMERGENCY LIGHTS SERVICE DOOR FLOOD LIGHT, SERVICE DOOR EXIT IDENTIFIER, SERVICE DOOR EXIT MARKE R, GALLEY WALL EXIT LOCATOR, AISLE FLOOD LIGHT AND FLOOR PROXIMITY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED NR 1 E MERGENCY BATTERY, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008010900236 20080109 00236 SO 2008 1 9 RAIA00712030 1 20071226 A 3350 LIGHT EMB 145 EMB145 3260210 SO EXTERIOR INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 805HK 145096 PRE FLT NR 3568 - BDL - MAIN DOOR EXTERIOR FLOOD LIGHT INOP. MAINTENANCE DEFERRED PER MEL. 2 L 7 2 4F RT T00011AT 2008010900237 20080109 00237 SO 2008 1 9 RAIA00712031 1 20071226 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN MALFUNCTIONED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 806HK 145112 PRE FLT NR 3535 - RIC - EMERGENCY LIGHT LEFTHAND AND RIGHTHAND OVERWING EXIT IDENTIFIER INOP. MAINTENANCE PERFORMED OPS CHECK OF EMERGENCY LIGHT, NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F RT T00011AT 2008010900238 20080109 00238 SO 2008 1 9 RAIA00712032 1 20071227 A 3350 1317 LIGHT EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 827HK 145021 PRE FLT NR 5452 - IND - EMERGENCY LIGHT AISLE FLOOD LIGHTS INOP. MAINTENANCE RELAMPED AISLE EMERGENCY LIGHT, OPS CHECK NORMAL. 2 L 7 2 4F RT T00011AT 2008010900239 20080109 00239 SO 2008 1 9 RAIA00712033 1 20071228 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN DIRTY A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 818HK 145059 PRE FLT NR 5452 - IND - EMERGENCY LIGHTS FWD CEILING EXIT LOCATOR AND COCKPIT STEP IDENTIFIER APPEAR TO BE OUT. MAINTEN ANCE CLEANED AND RESEATED CONNECTOR ON EMERGENCY LIGHT INVERTOR, OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2008010900240 20080109 00240 SO 2008 1 9 RAIA00712034 1 20071228 A 5210 ARM EMB 145 EMB145LR 3260212 SO PAX DOOR OUT OF SEQUENCE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 844HK 14500838 PRE FLT NR 7885 - EWR - PAX DOOR HARD TO OPEN. MAINTENANCE FOUND DOOR LOCK ARMS OUT OF SEQUENCE, RELEASED ARMS OPERATED DOOR 3 TIMES LOCK MECHANISM, OPS CHECK NORMAL. 2 L 7 2 4T RT T00011AT 2008010900241 20080109 00241 SO 2008 1 9 RAIA00712035 1 20071229 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN NOT SEATED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 811HK 145256 PRE FLT NR 5587 - STL - FWD SIDE AFT CEILING EXIT LOCATOR LIGHT INOP. MAINTENANCE RESEATED CONNECTOR FOR EMERGENCY LIGH T, TEST GOOD. 2 L 7 2 4T RT T00011AT 2008010900242 20080109 00242 SO 2008 1 9 RAIA00712036 1 20071230 A 3350 100865 BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 814HK 145046 POST FLT NR 5505 - STL - EMERGENCY LIGHT COCKPIT FLOOD LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK IN FWD CLOSET, CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008010900243 20080109 00243 SO 2008 1 9 RAIA00712037 1 20071230 A 3150 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 830HK 145313 FLT NR 5503 - JAX - ELECTRICAL EMERGENCY ABNORMAL IN FLIGHT. MAINTENANCE RESET POWER, MESSAGE CLEARED AND DID NOT RETUR N. 2 L 7 2 4T RT T00011AT 2008010900245 20080109 00245 EA 2008 1 9 MASA200700796 1 20071112 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7305V 7305 ASH FLT 2773 PHX - CABIN EMERGENCIES OVERHEAD LIGHT AT ROW 5 INOP, RELAMPED. 2 L 7 2 4F RT A21EA 2008010900291 20080109 00291 EA 2008 1 9 MASA200700907 1 20071221 A 2170 7506622 WATER SEPARATOR CNDAIR CL600 CL6002B19 1900309 EA CONTAMINATED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 649BR 7414 FLT 7350 - ORD - SMOKE IN THE CABIN. THE AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED BOTH WATER SEPARATOR B AGS AND CLEARED THE WATER SEPARATOR DRAIN TUBE. 2 L 7 2 4F RT A21EA 2008010900292 20080109 00292 EA 2008 1 9 MASA200700908 1 20071221 A 2170 7506622 WATER SEPARATOR CNDAIR CL600 CL6002B19 1900309 EA CONTAMINATED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 649BR 7414 FLT 7350, ORD - SMOKE IN CABIN, TOILET SMOKE CAUTION. REMOVED AND REPLACED BOTH WATER SEPARATOR BAGS AND UNPLUGGED WATE R SEPARATOR DRAIN LINE, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008010900294 20080109 00294 EA 2008 1 9 MASA200700735 1 20071023 A 3150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAP ILLUMINATED A MASA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 154SF 7154 ASH FLT 7200 CWA - FLAPS FAIL CAUTION ON TAXI IN. CONTRACT MX COMPLIED WITH PART A AND RESET, OPS NORMAL. 2 L 7 2 4F RT A21EA 2008010900295 20080109 00295 EA 2008 1 9 MASA200700694 1 20071014 A 5210 CAM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27172 7172 ASH 7319 - IAD - REPORTED HAVING TROUBLE CLOSING THE PAX DOOR. MX LUBED THE CAMS AND ROLLERS, AND WERE ABLE TO CLOSE TH E DOOR NORMALLY. 2 L 7 2 4F RT A21EA 2008010900309 20080109 00309 EA 2008 1 9 MASA200700713 1 20071018 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 593ML 7465 ASH FLT 7237 ORD - EMERGENCY FLOOR LIGHTS AT ROWS 2, 3, 4 AND 5 INOP. RESECURED CONNECTOR PLUG, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008010900333 20080109 00333 EA 2008 1 9 MASA200700581 1 20070915 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 651ML 7139 ASH FLT 7240 DSM - EXTERIOR EMERGENCY LIGHT NR 8, RIGHT AFT, INOP. MX RELAMPED, OPS NORMAL. 2 L 7 2 4F RT A21EA 2008010900335 20080109 00335 EA 2008 1 9 MASA200700620 1 20070921 A 3350 587387221 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27191 7191 ASH 2721 - PHX - REPORTED 2 FLOOR PATH LIGHTING STRIPS INOP. MX REPLACED THE LIGHTING STRIPS. 2 L 7 2 4F RT A21EA 2008010900339 20080109 00339 EA 2008 1 9 MASA200700653 1 20070928 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75993 7372 ASH FLT 7240 DSM - OVERNIGHT, NR 2 EXTERNAL EMERGENCY LIGHT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2008010900342 20080109 00342 EA 2008 1 9 MASA200700666 1 20071004 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17231 7231 ASH FLT 2872 SBP - PILOT REPORTED ONE CEILING LEVEL EMERGENCY FLOOD LIGHT INOPERATIVE. RELAMPED, OPS GOOD. 2 L 7 2 4F RT A21EA 2008010900346 20080109 00346 EA 2008 1 9 MASA200700675 1 20071007 A 3350 BC10066003 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17337 7337 ASH 2750 - PHX-DRO - CEILING FLOOD LIGHT INOP. REPLACED LIGHT ASSY. 2 L 7 2 4F RT A21EA 2008010900350 20080109 00350 EA 2008 1 9 TRAX200701992 1 20071227 A 5720 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 AAR - DRAG ANGLE CRACKED INBOARD OF RT BATT RIB (FLAGGED). REMOVED RT MLG HYDRAULIC LINES COVER SHIELD TO GAIN ACCESS T O REPAIR AREA. REMOVED CRACKED DRAG ANGLE I/B OF RT BATT RIB. LOCATED FASTENER HOLES IN SERVICEABLE DRAG ANGLE (P/N 60 0-10204-28) IAW CRJ-200 SRM 51-40-11. 13367. 01-02-08. AAR-338. OK TO INSTALL SERVICEABLE DRAG ANGLE. AAR-338. INS TALLED SERVICEABLE DRAG ANGLE IAW CRJ-200 SRM 51-42-21. 13367. 01-02-08. AAR-338. OK TO INSTALL HYDRAULIC LINES COVE R SHIELD. AAR-338. REINSTALLED RT MLG HYDRAULIC LINES COVER SHIELD IAW CRJ-200 SRM 51-41-02. 13367. 01-02-08. AAR- 338. SUPPLEMENTAL SDR CLOSED 1/3/08. 2 L 7 2 4F RT A21EA 2008010900351 20080109 00351 CE 2008 1 9 DXTA200702692 1 20071219 A 3240 556560913 BRACKET CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE BRAKE PEDAL CRACKED E DXTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 351QS 8938 5600451 PILOT SIDE BRAKES ARE VERY SOFT AND MORE THAN NORMAL TRAVEL FOR BRAKES TO GRAB. FOUND PILOT'S RUDDER PEDAL SUPPORT BRAC KET ASSY CRACKED. REMOVED AND REPLACED BRACKET ASSY WITH NEW I/A/W CE560 S/R/M 51-30-03. PERFORMED BLEEDING PROCEDURE OF ANTI-SKID SYSTEM. PERFORMED TAXI CHECK. BRAKE PEDALS OPERATE NORMALLY AT THIS TIME. ALL I/A/W CE560 M/M 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2008010900352 20080109 00352 EA 2008 1 9 TRAX200701974 1 20071222 A 5210 COVER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DENTED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 AAR - PAX DOOR AFT CORNER COVER IS DENTED. REMOVED DAMAGED PAX DOOR AFT CORNER COVER. LOCATED, DRILLED & DEBURRED NEW CORNER COVER P/N 600-31902-287 IAW CRJ 200 SRM 51-40-11 MF 13871 01/01/08 (AAR357) OK TO INSTALL CORNER COVER GL 14531. INSTALLED COVER PLATE IAW CRJ SRM 51-42-13. SUPPLEMENTAL SDR CLOSED 1/3/08. 2 L 7 2 4F RT A21EA 2008010900353 20080109 00353 EA 2008 1 9 TRAX200701966 1 20071220 A 5230 SCUFF PLATE CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR DENTED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 AAR - CARGO DOOR SCUFF PLATE DENTED IN SEVERAL PLACES. REQ EVAL. REFER TO 50275-1000-0035 FOR REMOVAL AND REPLACEMENT OF CARGO SCUFF PLATE. SUPPLEMENTAL SDR CLOSED 1/3/08. 2 L 7 2 4F RT A21EA 2008010900354 20080109 00354 EA 2008 1 9 TRAX200701955 1 20071218 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 840AS 7290 AAR - SERVICE DOOR BETA LIGHT REQUIRES REPLACEMENT. REMOVED SERVICE DOOR BETA LIGHT P/N 601R38774-3 AND REPLACED WITH N EW SERVICEABLE BETA LIGHT P/N 601R38774-7 IAW CRJ 200 AMM 20-21-00. TORQUED SCREWS WITH TORQUE WRENCH AARHOT 1047 IAW C RJ 200MM 20-21-00. SUPPLEMENTAL SDR CLOSED 1/3/08. 2 L 7 2 4F RT A21EA 2008010900355 20080109 00355 SO 2008 1 9 C2XA07ON048 1 20071217 A 2720 15H0048PH PRESSURE SWITCH EMB 145 EMB145XR 3260214 SO RUDDER FAULTY A C2XA K NONE O OTHER CL CLIMB 1 SW 27 17185 6479 6479 14500922 FLT 7652 - LAX TO LAX - FLIGHT CREW REPORTED RUDDER OVERBOOST ON CLIMBOUT OF ONT. MX PERSONNEL REMOVED AND REPLACED NR 1 RUDDER PRESSURE SWITCH. OPERATIONALLY CHECKED GOOD AND A/C WAS RETURNED FOR SERVICE IN AIRWORTHY CONDITIONS. 2 L 7 2 4F RT 2008010900356 20080109 00356 2008 1 9 C2XA07ON049 4 20071217 A 3417 14532708403 HOSE EMB 145 EMB145XR 3260214 SO E&E BAY BROKEN A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 14188 6767 6767 14500929 FLT 54 - MCI TO MCI - FLIGHT CREW REPORTED ADC 2 FAIL AND F/O ALT RED X'S. MX PERSONNEL REMOVED AND REPLACED THE TOTAL PRESSURE HOSE ON THE RIGHT ADC, OPERATIONALLY CHECKED SATISFACTORY AND A/C WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008010900357 20080109 00357 SO 2008 1 9 C2XA07ON050 1 20071221 A 2120 8166041 VALVE EMB 145 EMB145 3260210 SO A/C PACK MALFUNCTIONED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 19554 3213 3213 14500587 FLT 421 - SMF TO GEG - FLIGHT CREW REPORTED PACK 1 VALVE FAILED TO CLOSED NUMEROUS TIMES ON CLIMB. MX PERSONNEL REMOVED AND REPLACED NR 1 PACK VALVE, OPERATIONALLY CHECKED SATISFACTORY AND A/C WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 2008010900358 20080109 00358 SO 2008 1 9 C2XA07ON051 1 20071224 A 3610 54722250 DUCT CLAMP EMB 145 EMB145XR 3260214 SO NR 2 ENGINE LOOSE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 11199 4873 14500953 FLT 210 - SMF TO ONT - FLIGHT CREW REPORTED E2 ITT JUMPED 110 DEGREES AFTER T/O WITH WF INCREASE & N1 DROP-BLEED SELECTI ON ONLY 10 DEGREES. MX PERSONNEL RE-ADJUSTED AND TORQUED V-BAND CLAMP OPERATIONALLY CHECKED SATISFACTORY AND A/C WAS RE LEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008010900359 20080109 00359 SO 2008 1 9 C2XA07ON052 1 20071225 A 3234 7455503 SELECTOR VALVE EMB 145 EMB145 3260210 SO LANDING GEAR NOISY A C2XA K NONE O OTHER CL CLIMB 1 SW 27 12569 20967 20967 14500630 FLT 7803 - LAX TO LAX - FLIGHT CREW REPORTED KNOCKING SOUND WHEN GEAR RETRACTED - FERRY TO ONT, CHANGED SEVERAL COMPONEN TS E.I BCU, RELAY K0273 AND FINALLY REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE. OPERATIONALLY, TEST FLEW CHECKED SATISFACTORY AND AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 2008010900360 20080109 00360 GL 2008 1 9 C2XA07ON053 2 20071228 A 7261 AE3007A1P ENGINE EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL NR 1 OIL CONSUMPTION A C2XA C ABORTED TAKEOFF K FLUID LOSS TO TAKEOFF 1 SW 27 22909 11758 11758 14500459 CAE312223 FLT 7825 - PDX TO LAX - FLIGHT CREW REPORTED E1 LOW OIL ON TAKEOFF. CONTRACT MX SERVICED NR 1 ENGINE, OPERATIONALLY CHE CKED SATISFACTORY AND A/C WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2008010900361 20080109 00361 SO 2008 1 9 C2XA07ON054 1 20071228 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT & CABIN SMOKE A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 11184 14500917 FLT 7672 - SLC TO SLC - FLIGHT CREW REPORTED SMOKE IN CABIN AND COCKPIT. MX PERSONNEL PERFORMED OPERATIONAL CHECK OF TH E ENGINE TO DUPLICATED, BUT COULD NEVER DUPLICATE FAULT AGAIN. SUSPECTED DEICING FLUID. A/C WAS RELEASED TO RETURN FOR SERVICE IN AIRWORTHY CONDITIONS. 2 L 7 2 4F RT 2008010900362 20080109 00362 2008 1 9 C2XA07ON055 4 20071231 A 3416 7001840937 ALTIMETER EMB 145 EMB145 3260210 SO COCKPIT INOPERATIVE A C2XA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 27 10575 12586 12586 14500640 FLT 7803 - SLC TO EUG - FLIGHT CREW REPORTED RA 1 INOP IN FLIGHT. MX PERSONNEL REMOVED AND REPLACED RA 1, OPERATIONALLY CHECKED SATISFACTORY AND A/C WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 2008010900363 20080109 00363 2008 1 9 C2XA07ON056 4 20071231 A 3460 7021170951 CONTROLLER EMB 145 EMB145XR 3260214 SO FLIGHT GUIDANCE MALFUNCTIONED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 11164 13029 13029 14500817 FLT 421 - SAN TO ONT - EN ROUTE FROM SAN TO GEG FLIGHT CREW REPORTED TOTAL NAV 1 AND 2 FAILURE. DIVERTED TO ONT AN EMER GENCY WAS NOT DECLARED; A/C LANDED SAFELY IN ONT WHERE MX PERSONNEL REMOVED AND REPLACED FLIGHT GUIDANCE CONTROLLER. OP ERATIONALLY CHECKED SATISFACTORY AND A/C WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008010900365 20080109 00365 NM 2008 1 9 CALA0800001 1 20071217 A 5534 65474505 BUSHING BOEING 737 7373T0 1384582 NM VERTICAL STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 VERTICAL FIN FED RIGHT FITTING HAVE CORROSION IN BUSHING. REPLACED PER ECRA 5530-01493. 2 L 7 2 4F RT A16WE 2008010900369 20080109 00369 EA 2008 1 9 TRAX200800011 1 20071228 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 724EV 10138 FS 280 FWD FLOOR SUPPORT ANGLE IS CORRODED. 2 L 7 2 4F RT A21EA 2008010900370 20080109 00370 EU 2008 1 9 TRAX200800012 1 20071231 A 2560 PBE AEROSP ATR72 ATR72 EU COCKPIT UNSERVICEABLE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 PBE BEHIND CAPTAIN LOST VACUUM. 2 H 7 2 4T RT 2008010900371 20080109 00371 EA 2008 1 9 TRAX200800013 1 20071231 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 682BR 7691 PAX DOOR HAS EMERGENCY LIGHT BROKE OFF. 2 L 7 2 4F RT A21EA 2008010900372 20080109 00372 EA 2008 1 9 TRAX200800014 1 20071231 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 931EV 8015 SERVICE DOOR WILL NOT CLOSE. 2 L 7 2 4F RT A21EA 2008010900373 20080109 00373 EA 2008 1 9 TRAX200800015 1 20071231 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 933EV 8022 RIGHT FWD OVERWING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2008010900379 20080109 00379 EA 2008 1 9 TRAX200800005 1 20071228 A 5310 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 724EV 10138 FS 280 CROSSBEAM IS CORRODED. BLENDED CORROSION ON RT SIDE CROSSBEAM WITHIN LIMITS OF REO 670-53-11-046, RESTORED SURFA CE FINISH PER CRJ700 SRM 51-25-00. REMOVED AND REPLACED LT SIDE 280 CROSSBEAM DUE TO OUT OF LIMITS CORROSION AS PER IS6 7053110026. ALL WORK ACCOMPLISHED ON ATTACHED M-234 PGS 1 THRU 4. SUPPLEMENTAL SDR CLOSED 1/4/08. 2 L 7 2 4F RT A21EA 2008010900394 20080109 00394 CE 2008 1 9 B8M2007F00000 1 20071207 A 5610 NH2401692 WINDSCREEN RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP INCORRECT E B8MA K NONE O OTHER IN INSP/MAINT 1 NM 07 890SP 258530 RECEIVED NEW WINDSCREEN RT (B) SCREEN PN NH24016-92, SN L366293. WHILE DOING OUR INCOMING PARTS INSPECTION WE DISCOVERE D THAT THE TERMINAL BLOCK LAYOUT PLACARD FOR THE WINDOW WAS INCORRECT. IT WAS LAYED OUT FOR THE LT WINDOW ASSY PN NH240 16-81 OR NH24016-91. REORDERED ANTOHER WINDSCREEN AND IT HAD THE CORRECT TERMINAL LAYOUT PLACARD. (K) 2 L 7 2 4F 4 F RT A3EU E6WE 2008011000005 20080110 00005 NM 2008 1 10 ASAA0842446 1 20071231 A 5210 652892586 FITTING BOEING 737 7374Q8 138447Q NM L2 DOOR DEFECTIVE A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 765AS 25102 FLIGHT ATTENDANT REPORTS L2 DOOR DIFFICULT TO OPEN & MAKES A SQUEAKING SOUND ON OPENING. REPLACED LOWER TORQUE TUBE SPR OCKET UPPER DOOR FITTING AND UPPER GUIDE ARM & PIN. DOOR OP CHECKS GOOD & NO SQUEAKING NOISES ON DOOR. 2 L 7 2 4F RT A16WE 2008011000007 20080110 00007 NM 2008 1 10 UPS07M51349 1 20071113 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C RT WING FUEL TANK STRINGER NR 10 END SUSPECT CRACKED. HFEC INSP C/O AT STR NR 10 END FOUND CRACK OF A PPROX 11 INCHES LONG. STR NR 10 SPLICE END & HI-LOKS AT REPAIR AREA REMOVED. CRACK AT STR NR 10 SLOT OUT PER SRM 57-20 -00 FIG 10 VI R35. HFEC INSP C/O ON SLOT OUT AREA & FOUND NO CRACK EVIDT. REPAIR ANGLES FAB, HEAT-TREATED, REPROTECTED & PRIMED. REPAIR ANGLES INSTALLED. CAP SEAL C/O ON REPAIR AREA. LEAK CHECK SATIS. 2 L 7 3 4F RT A22WE 2008011000009 20080110 00009 2008 1 10 UPS08M51359 4 20071226 A 2565 LIGHT DOUG MD11 MD11F 3023600 NM EVAC SLIDE INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:N/A R1 SLIDE PRESSURE PRESS TO TEST LIGHT INOP. DEFERRED M365742. REMOVED R1 SLIDE, REPLACED R1 SLIDE S/N ON 0169 IAW 25-61-15-4. THIS CLEARS M365742. OPS CHECKS NORMAL. 2 L 7 3 4F RT A22WE 2008011000011 20080110 00011 EU 2008 1 10 USAA920071374 1 20071224 A 2611 PPA120100 SMOKE DETECTOR AIRBUS 320 A320232 3930326 EU LAVATORY FALSE ACTIVATION A USAA K NONE N FALSE WARNING IN INSP/MAINT 1 EA 19 659AW 1166 FLT 0025 - FFW - PHX - CREW REPORTED LAVATORY SMOKE DETECTOR FAULT LIGHT ILLUMINATED. MX REPLACED THE LAVATORY SMOKE DE TECTOR IAW 26-16-15. OPERATIONAL CHECK WAS GOOD. A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2008011000013 20080110 00013 EU 2008 1 10 USAA920071375 1 20071222 A 2810 L95F50603 DISK AIRBUS A321 A321211 3930370 EU CENTER FUEL TANK BROKEN A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 174US 1492 FLT 1433 - CLT - LAX - ATB - CREW REPORTED DURING CLIMB, EXPERIENCED A FUEL TRANSFER PROBLEM WITH THE LEFT TANK CAUSING A FUEL IMBALANCE CONDITION THE LEFT ENGINE WAS REDUCED TO IDLE, CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. THE C ABIN WAS NOT PREPPED, EMERGENCY EQUIPMENT WAS DISPATCHED AND THE A/C LANDED OVERWEIGHT. THE LANDING WAS UNEVENTFUL AND THE A/C TAXIED TO THE GATE. MX INSPECTED CENTER FUEL TANK AND DISCOVERED THE FUEL CENTER TANK OVERPRESSURE PROTECTOR (9 6QM) DISK BROKEN. MX REPLACED THE OVERPRESSURE PROTECTOR (96QM). OPERATIONAL TEST OF CENTER TANK FUEL TRANSFER SYSTEM AND VENT SYSTEM WAS GOOD. A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2008011000051 20080110 00051 EA 2008 1 10 COMA0770082 1 20071228 A 3230 SERVO VALVE CNDAIR CL600 CL6002C10 1390015 EA LANDING GEAR NOISY A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 374CA 10090 FLIGHT 5654 - LOUD SQUEAL NOISE HEARD ON TAKEOFF. RETURNED TO JAX, LANDED WITHOUT INCIDENT. PERFORMED INSPECTION OF NO SE AREA, ALL ACCESS PANELS AND DOOR SEALS. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008011000053 20080110 00053 NM 2008 1 10 QXEA200702015 1 20071224 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA FALSE ACTIVATION A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 09 422QX 4150 MASTER CAUTION STICK PUSHER FAIL, ILLUMINATED DURING TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE PERFORMED FIM TASK 27-33-00-810-829. NO RECORDED FAULTS IN CDS SYSTEM. COMPLIED WITH TEST OF STALL PROTECTION SYSTEM. F AULT LIGHT CLEARED. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2008011000054 20080110 00054 CE 2008 1 10 DJFA2007148 1 20071222 A 2121 FAN BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE TEMP SENSOR OVERHEATED E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 EA 23 439LX RK284 ON LANDING CREW REPORTED BURNING ODOR IN THE CABIN. MAINTENANCE FOUND THE CABIN TEMP SENSOR FAN OVERHEATING. THE FAN W AS REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2008011000058 20080110 00058 2008 1 10 HNAA0800003 4 20071231 A 2210 7003652611 PANEL DHAV DHC8 DHC8102 2809003 NM AUTOPILOT SYTSEM FAILED A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 EA 07 981HA 29908 5078 378 CAPTAINS 802 PANEL IS INOP AND SIMUTANEOULSY SMELLED A STRONG ELECTRONIC SMELL. REPLACED CAPTAINS 802 PANEL, OPERATIONA L CHECK GOOD. 2 H 7 2 4T RT A13NM 2008011000060 20080110 00060 NE 2008 1 10 COMA0760727 2 20071214 A 7261 6087T04P05 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30068 NE RT ENGINE FAULTY A COMA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 713CA 72 7245 807512 FLIGHT 9658 - DURING CRUISE FLIGHT RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING MESSAGE, CREW DECLARED AN EMERGENCY, PER FORMED AN I.F.S.D. AND DIVERTED TO MDT. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT ENGINE LUBRICATION AND SCAV ENGE PUMP. 2 L 7 2 4F 4 F RT A21EA E15NE 2008011000061 20080110 00061 EA 2008 1 10 COMA0760728 1 20071214 A 7931 601509199 TRANSDUCER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30068 NE RT ENGINE FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 713CA 87 7245 807512 FLIGHT 9658 - DURING CRUISE FLIGHT RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING MESSAGE, CREW DECLARED AN EMERGENCY, PER FORMED AN I.F.S.D. AND DIVERTED TO MDT. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT ENGINE OIL PRESSURE TRANSDU CER. 2 L 7 2 4F 4 F RT A21EA E15NE 2008011000065 20080110 00065 EA 2008 1 10 COMA0760732 1 20071218 A 2752 853D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 587SW 1912 7062 FLIGHT 5186 - FLAPS FAIL CAUTION MESSAGE WHEN SELECTING FLAPS TO 8 DEGREES. EMERGENCY DECLARED AND AIRCRAFT LANDED SAFE LY IN CVG. REMOVED AND REPLACED RT OUTBOARD FLAP NR 3 ACTUATOR. 2 L 7 2 4F RT A21EA 2008011000069 20080110 00069 EA 2008 1 10 COMA0760735 1 20071218 A 3297 17300110 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA RT MLG FAILED A COMA A UNSCHED LANDING O OTHER AP APPROACH 1 SO 01 409CA 7441 FLIGHT 5512 - ANTI-SKID I/B CAUTION MESSAGE ON APPROACH INTO LGA. AIRCRAFT DIVERTED TO JFK AND LANDED SAFELY. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR INBOARD WIRE HARNESS. 2 L 7 2 4F RT A21EA 2008011000070 20080110 00070 NM 2008 1 10 HNAA0800005 1 20071219 A 3150 06500757 MASTER CAUTION DHAV DHC8 DHC8102 2809003 NM COCKPIT SPARKS A HNAA K NONE B L SMOKE/FUMES/ODORS/SPARKS NO TEST NR NOT REPORTED 1 EA 07 912HA 56104 56104 040 MASTER CAUTION PUSH TO RESET SPARKED WHEN PUSHED AND WILL NOT TEST. REPLACED MASTER CAUTION SWITCH AND CAUTION PANEL. 2 H 7 2 4T RT A13NM 2008011000074 20080110 00074 EA 2008 1 10 COMA0760739 1 20071220 A 7830 4EN886 SWITCH CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 936CA 7043 FLIGHT 5591 - RECEIVED RIGHT T/R REV UNLOCK MESSAGE. FOLLOWED QRH, AFTER EMERGENCY STOW, BUFFETING CONTINUED, SHUTDOWN RIGHT ENGINE. DECLARED EMERGENCY AND LANDED PHL WITHOUT INCIDENT. REPLACED RIGHT T/R STOW SWITCH. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011000075 20080110 00075 EA 2008 1 10 COMA0760740 1 20071221 A 2740 9960013 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 917CA 7017 FLIGHT 5626 - STAB AND MACH TRIM DISENGAGED REPEATEDLY DURING CLIMB. RE-ENGAGED, DIVERTED TO IAD, LANDED WITHOUT INCIDE NT. REPLACED CAPTAIN'S PITCH TRIM DISCONNECT SWITCH. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008010900109 20080109 00109 EA 2008 1 9 MASA200700814 1 20071121 A 3230 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 654BR 189 7454 ASH FLT 1028 HNL - GEAR DISAGREE WITH NOSE DOOR OPEN WARNING MESSAGE. REPLACED PSEU AND RIGGED UPLOCK SENSOR. 2 L 7 2 4F RT A21EA 2008010900114 20080109 00114 EA 2008 1 9 MASA200700924 1 20071228 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77195 7195 ASH 7285 - IAD - ONE FLOOR PATH LIGHTING SEGMENT INOP. RESECURED LIGHT STRIP, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008010900138 20080109 00138 EA 2008 1 9 MASA200700932 1 20071231 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A MASA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 651ML 7139 ASH FLT 7278 IAD-CAK - FLAPS FAILED AT 0 DEGRESS DURING TAXI. C/W PART B, NO FAULTS NOTED. 2 L 7 2 4F RT A21EA 2008010900146 20080109 00146 EA 2008 1 9 MASA200700868 1 20071211 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77181 7181 ASH 7390 ROA - FLOOR EMERGENCY EXIT LIGHTS INOP ROW 1. RESECURED CONNECTOR, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2008010900148 20080109 00148 EA 2008 1 9 MASA200700767 1 20071102 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 651BR 7426 ASH 1034 HNL - LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 2008010900149 20080109 00149 EA 2008 1 9 MASA200700769 1 20071102 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27172 7172 ASH FLT 7483 ORD - MAIN DOOR CABIN WILL NOT OPEN FROM OUTSIDE. MX CND, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008010900150 20080109 00150 EA 2008 1 9 MASA200700896 1 20071217 A 5755 601R10334 FITTING CNDAIR CL600 CL6002B19 1900309 EA SPOILER CHAFED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 75994 7367 DAMAGE TO FUSELAGE. DAMAGE IS CHAFING ON THE LT OB GROUND SPOILER FITTING P/N 601R10334. CHAFING IS 0.5" LONG, .34" WI DE AND .50" DEEP. WEB IS ORIGINALLY .115" THICK. PERM REPAIR IS COMPLETE. 2 L 7 2 4F RT A21EA 2008010900169 20080109 00169 EA 2008 1 9 MASA200700785 1 20071109 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75991 7422 ASH FLT 7279 ROC - FLAPS FAIL AT 28. CONTRACT MX COMPLIED WITH PART A. 2 L 7 2 4F RT A21EA 2008010900199 20080109 00199 EA 2008 1 9 MASA200700824 1 20071128 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A MASA O OTHER O OTHER CR CRUISE 1 SW 07 17175 15616 7175 FLT 7322, BUF - GEAR DISAGREE WARNING, NOSE GEAR WOULDN’T EXTEND. CREW MANUALLY EXTENDED. REMOVED AND REPLACED PARK BR EAK SOV AND NLG DOOR SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2008010900200 20080109 00200 EA 2008 1 9 MASA200700768 1 20071102 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17358 7358 ASH FLT 2802 - CEILING LEVEL EMERGENCY LIGHTS INOP AT ROW 11. RELAMPED 2 L 7 2 4F RT A21EA 2008010900201 20080109 00201 EA 2008 1 9 MASA200700928 1 20071230 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27172 7172 ASH FLT 7209 IAD - PAX DOOR WILL NOT SECURE. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008010900205 20080109 00205 EA 2008 1 9 MASA200700819 1 20071122 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STIFF A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77302 7302 FLT 7353, ORD - CREW REPORTED PAX DOOR HARD TO CLOSE. MX CYCLED DOOR AND OP CHECKED NORMAL. 2 L 7 2 4F RT A21EA 2008010900206 20080109 00206 EA 2008 1 9 MASA200700818 1 20071121 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DIRTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27172 7172 ASH FLT 7308 ORD - MAIN PASSENGER DOOR OUTER HANDLE WILL NOT SECURE. MX REMOVED DEBRIS FROM HANDLE. 2 L 7 2 4F RT A21EA 2008010900211 20080109 00211 GL 2008 1 9 CLCA2007F001 2 20070325 A 7310 AC9227F1638 FUEL FILTER DOUG DC10 DC1030 3023501 WP GE CF6 CF6* 30020 GL NR 2 ENGINE DIRTY A CLCA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 29 68044 46903 NR 3 ENGINE FUEL FILTER PRESSURE DROP LIGHT ON. NR 2 ENGINE FUEL FILTER PRESSURE LIGHT ON AFTER ADDITIONAL ONE AND HALF HOUR AFTER TAKEOFF. DIVERTED TO CLO. REPLACED FILTERS SUMPED TANKS RUN-UP ALL ENGINES. 2 L 7 3 4F 4 F A22WE E23EA 2008010900212 20080109 00212 WP 2008 1 9 CLCA2007F0002 1 20070501 A 3610 BAM7000541 CLAMP DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2B 30018 NE PRECOOL MANIFOLD WORN A CLCA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 29 612GC 47840 517392 AT APPROX 6000 FT NR 2 ENGINE FIRE INDICATION. FOUND CLAMP TO PRECOOLER MANIFOLD WORN. 2 L 7 3 4F 4 F RT A22WE E23EA 2008010900214 20080109 00214 WP 2008 1 9 FX7A200700009 1 20071229 A 2410 696233B CSD DOUG DC9 DC982 3022082 WP RIGHT LOW PRESSURE A FX7A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 905TA 49905 DURING CLIMB THRU FL240 RIGHT HAND CSD OIL PRESSURE LOW AND RIGHT HAND GENERATOR OFF ILLUMINATED. QRH COMPLIED WITH. 2 L 7 2 4F A6WE 2008010900215 20080109 00215 SO 2008 1 9 C2XA07IA255 1 20071228 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 13123 145688 IAH - FLIGHT 2694, THE CREW REPORTED A VERY STRONG FUEL SMELL ON TAKEOFF THAT GOES AWAY AFTER THE APU IS SHUTDOWN. THE AIRCRAFT LANDED AT IOAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND APU, OPERATIONALLY CHECKED THE APU & B LEED SYSTEMS WITH NO SEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008010900216 20080109 00216 SO 2008 1 9 C2XA07IA256 1 20071230 A 5220 14525737401 STRUCTURE EMB 145 EMB145EP 3260221 SO EMERGENCY EXIT OUT OF POSITION A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14938 145029 IAH - DURING A-CHECK INSPECTION THE RIGHT HAND OVERWING EMERGENCY EXIT DOOR WOULD NOT OPEN. THE METAL TRIM AT THE TOP O F THE DOOR WAS FOUND TO BE CATCHING ON THE OPENING. MAINTENANCE RECONTOURED/TRIMMED THE AFFECTED MATERIAL, OPERATIONALL Y CHECKED THE EXIT WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008010900229 20080109 00229 2008 1 9 CALA0700792 4 20071228 A 2564 64356101 LIFE RAFT BOEING 737 737824 13844BZ NM CABIN LOW PRESSURE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14214 216 216 28774 FORWARD CABIN LIFE RAFT PRESSURE GAGE READING ZERO. REMOVED AND INSTALLED SERVICEABLE FORWARD LIFE RAFT. REF B737 AMM 25-64-00. 2 L 7 2 4F RT A16WE 2008010900230 20080109 00230 EA 2008 1 9 TRAX200701993 1 20071227 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 723EV 10132 LEFT EMERGENCY EXIT LOWER EMERGENCY LIGHT HAS SEVERAL INOP BULBS. 2 L 7 2 4F RT A21EA 2008010900231 20080109 00231 EU 2008 1 9 USAA920071390 1 20071228 A 3231 ABS012110 DOWNLOCK SENSOR AIRBUS 320 A320232 3930326 EU NLG FAILED A USAA L ABORTED APPROACH N FALSE WARNING DE DESCENT 1 EA 19 665AW 1644 FLT 80 - BWI - LAS - EL - CREW REPORTED DURING DESCENT RECEIVED AN ECAM WARNING MESSAGE THAT THE LEFT FRONT LANDING GEAR DOOR DID NOT CLOSE WHEN THE GEAR WAS LOWERED FOLLOWED BY A NOSE WHEEL STEERING FAULT. A GO AROUND WAS EXECUTED AND THE CREW REQUESTED LAS TOWER TO CONFIRM GEAR WAS DOWN. TOWER CONFIRMED GEAR WAS DOWN, CREW DECLARED AN EMERGENCY. THE CAB IN WAS NOT PREPPED. THE LANDING WAS UNEVENTFUL. MX PINNED AND INSPECTED THE NOSE GEAR. THE A/C WAS TAXIED TO THE GATE . MX FOUND THE NOSE GEAR DOWN LOCK SENSOR 19GA FAULTED. MX REPLACED 19GA IAW 32-31-73. TEST PASSED. THE A/C WAS RETU RNED TO SERVICE. 2 L 7 2 4F RT A28NM 2008010900232 20080109 00232 2008 1 9 ASAA0752441 4 20071228 A 2397 286A0811043 CONNECTOR BOEING 737 737890 1384527 NM E&E BAY LOOSE A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 559AS 35178 HF NR 1 GRABLED AND UNREADABLE. DUPLICATED PROBLEM. REPLACED COUPLER & TRANSMITTER, NO HELP. REINSTALLED ORIGINALS. PERFORMED FIM 23 4 TASK 806 FOUND HF NR 1 E* COAX RACK CONNECTOR & STANCHION CONNECTOR LOOSE. SECURED CONNECTIONS. HF SYSTEM OPS & BITE CHECKS GOOD. 2 L 7 2 4F RT A16WE 2008010900246 20080109 00246 SO 2008 1 9 C2XA08IA001 1 20071231 A 3260 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO AIR GROUND SYS MALFUNCTIONED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 15980 145202 OMA - FLIGHT 2145, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON TAKEOFF. THE AIRCRAFT RETURNED TO OMA WH ERE IT LANDED WITHOUT INCIDENT. THE CREW SUCCESSFULLY RESET THE AIR GROUND SYSTEM PER MAINTENANCE CONTROL, AND THE AIRC RAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008010900247 20080109 00247 SO 2008 1 9 C2XA08TY001 1 20071228 A 5330 14535010003 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14998 145302 RIGHT FUSELAGE SKIN DAMAGE (GROUND DAMAGE) BETWEEN FRM 67 & 71 BETWEEN STR 20L & 15R. REMOVED AND REPLACED SKIN PANEL I AW EMB 145 SRM 51-20-03, 51.40-06, CPM 51-21-04, 05, 06. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008010900249 20080109 00249 EA 2008 1 9 TRAX200800001 1 20071228 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 682BR 7691 PAX DOOR INTERNAL SKIN HAS EDGE CRACK AT AFT SIDE. 2 L 7 2 4F RT A21EA 2008010900251 20080109 00251 EA 2008 1 9 TRAX200800003 1 20071228 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 682BR 7691 PAX DOOR INNER SKIN HAS EDGE CRACK AT AFT SIDE .500 INCH LONG. 2 L 7 2 4F RT A21EA 2008010900252 20080109 00252 EA 2008 1 9 TRAX200800004 1 20071228 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 724EV 10138 FS 280 FWD FLOOR SUPPORT ANGLE IS CORRODED. 2 L 7 2 4F RT A21EA 2008010900253 20080109 00253 EU 2008 1 9 TRAX200800006 1 20071229 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 634AS 370 EMERGENCY EXIT LIGHT LOCATED AT THE BOTTOM OF SERVICE DOOR INOP. 2 H 7 2 4T RT 2008010900255 20080109 00255 EA 2008 1 9 TRAX200800008 1 20071230 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 873AS 7549 AIRSTAIR DOOR MISSING "EXIT" AND "OPEN" PLACARDS. 2 L 7 2 4F RT A21EA 2008010900293 20080109 00293 EA 2008 1 9 MASA200700909 1 20071225 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA RIGHT CONTAMINATED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 649BR 7007 7414 ASH FLT 7214 ATW - LAV SMOKE CAUTION MESSAGE IN FLIGHT FOLLOWED BY HAZE IN FLIGHT DECK AND CABIN. CAPT AND FO REPORTED THE ODOR OF GLYCOL. MX REMOVED AND REPLACED RT ACM, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008010900306 20080109 00306 EA 2008 1 9 MASA200700711 1 20071018 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 593ML 7465 ASH FLT 7306 BMI - CAPT REPORTS EMERGENCY FLOOR LIGHTS AT ROWS 2, 3, 4 AND 5 INOP. RESECURED CONNECTOR PLUG, OPS CK GOO D. 2 L 7 2 4F RT A21EA 2008010900315 20080109 00315 EA 2008 1 9 MASA200700528 1 20070828 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75995 7361 ASH 7409 IAD - CREW REPORTED A CABIN EMERGENCY EXIT SIGN INOP. MX RESECURED A LOOSE CONNECTOR. 2 L 7 2 4F RT A21EA 2008010900340 20080109 00340 EA 2008 1 9 MASA200700657 1 20071001 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 97325 7325 ASH FLT 2818 DSM - EMERGENCY CEILING FLOOD LIGHT IN AFT CABIN (NR 4) INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2008011000004 20080110 00004 NM 2008 1 10 BB07107 1 20071230 A 3350 LIGHT BOEING 757 7572S7 1384962 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 903AW 23323 PHX - MAINTENANCE REPORTED THE FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17C INOPERATIVE. MAINTENANCE REM OVED AND REPLACED SEAT ROW 17C FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 2008011000062 20080110 00062 2008 1 10 COMA0760729 4 20071214 A 3418 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 807CA 7364 FLIGHT 5682 - RECEIVED A STALL FAIL CAUTION MESSAGE AFTER TAKEOFF, FLIGHT RETURNED TO CVG. CLEARED DEBRIS FROM LEFT AOA CANE AND RESET THE STALL COMPUTER SYSTEM. 2 L 7 2 4F RT A21EA 2008011000063 20080110 00063 EA 2008 1 10 COMA0760730 1 20071217 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 712CA 7244 DURING 559 INSPECTION FOUND .6 INCH CRACK ON INBOARD SIDE AND .8 INCH CRACK AT OUTBOARD SIDE OF VERTICAL STIFFENERS. RE MOVED DAMAGE AND INSTALLED DOUBLERS PER BOMBARDIER REO 601R-53-41-057. 2 L 7 2 4F RT A21EA 2008011000066 20080110 00066 EA 2008 1 10 COMA0760733 1 20071218 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 712CA 7244 DURING 559 EDDY CURRENT INSPECTION FOUND A CRACK ON THE 559 WEB. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW SR10-5341-001 REV A SECTION 1 PERMANENT REPAIR. 2 L 7 2 4F RT A21EA 2008011000067 20080110 00067 EA 2008 1 10 HNAA0800004 1 20071217 A 3320 BA080061 BALLAST DHAV DHC8 DHC8311 1386006 EA CABIN DEFECTIVE A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 EA 07 327EN 28122 28122 261 ELECTRICAL SMELL IN CABIN, MORE NOTICEABLE AT ROW 7. PERFORMED HIDDEN DAMAGE INSPECTION, FOUND OVERHEAD LIGHT ASSEMBLY AT 7C BURNT. REPLACED LAMP HOLDER BV03300-12-150 AND BALLAST, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2008011000068 20080110 00068 EA 2008 1 10 COMA0760734 1 20071218 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 712CA 23431 7244 CABIN FLOOR LATERAL BEAM CRACKED ON LOWER FLANGE. COMPLIED WITH REO601R-53-11-1308 BY CUTTING OUT DAMAGE AND APPLYING D OUBLER. 2 L 7 2 4F RT A21EA 2008011000076 20080110 00076 EA 2008 1 10 COMA0760741 1 20071221 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 712CA 7244 DURING HMV-5 INSPECTION EDDY CURRENT OF AFT PRESSURE BULKHEAD, FOUND 3 CRACKS AROUND LINTEL ATTACHMENT FITTING. REPAIRE D CRACKS TO AFT PRESSURE BULKHEAD AROUND LINTEL FITTING AS PER REO 601R-53-61-1230 AND REO 601R-53-61-2463. 2 L 7 2 4F RT A21EA 2008011000077 20080110 00077 EA 2008 1 10 COMA0760742 1 20071222 A 3040 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 729CA 7265 FLIGHT 5308 - RECEIVED RIGHT WINDOW HEAT MESSAGE. RETURNED TO CVG AND LANDED WITHOUT INCIDENT. PERFORMED OPERATIONAL C HECK OF WINDOW HEAT. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2008011000078 20080110 00078 EA 2008 1 10 COMA0760743 1 20071228 A 3620 356024310 SENSING ELEMENT CNDAIR CL600 CL6002B19 1900309 EA AFT BAY FAULTY A COMA K NONE N FALSE WARNING CR CRUISE 1 SO 01 916CA 7014 FLIGHT 5699 - RECEIVED ANTI-ICE DUCT MESSAGE WITH RED INDICATING ON RIGHT FUSELAGE. C/W QRH, MESSAGE WENT AWAY AFTER AB OUT 1 MINUTE. DECLARED EMERGENCY, LANDED BHM WITHOUT INCIDENT. REPLACED AFT BAY SENSING ELEMENT. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011000079 20080110 00079 EA 2008 1 10 COMA0760745 1 20071228 A 3020 5399001 ANTI-ICE VALVE CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 739CA 7273 FLIGHT 5008 - RECEIVED LEFT COWL ANTI-ICE CAUTION. DIVERTED TO AVP, LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE COWL ANTI-ICE VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011000080 20080110 00080 EA 2008 1 10 COMA0760746 1 20071229 A 3610 14467102 DUCT CNDAIR CL600 CL6002B19 1900309 EA BLEED AIR SYS DAMAGED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 938CA 7046 FLIGHT 5205 - RECEIVED ANTI-ICE WARNING MESSAGE. RIGHT FUSELAGE SHOWING RED. MESSAGE CLEARED WHEN SYSTEM SELECTED FF, DID NOT GO INTO STANDBY. DECLARED EMERGENCY, RETURNED TO CVG, LANDED WITHOUT INCIDENT. REPAIRED RIGHT NR 2 DUCT (REO60 1-36-10-002). NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011000087 20080110 00087 EU 2008 1 10 TRAX200800010 1 20071230 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 632AS 338 ASD EMERGENCY LIGHT INOP. 2 H 7 2 4T RT 2008011000112 20080110 00112 NM 2008 1 10 USAA920080004 1 20071219 A 5312 651758243 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C16 CHECK - CRACKED VERTICAL BEAM WEB, BS 178, RBL 17, WL 224 - WL 234. REPAIRED VERTICAL BEAM WEB , BS 178, RBL 17, WL 224 - WL 234 IAW B737 SRM 53-10-08-2R12. 2 L 7 2 4F RT A16WE 2008011000114 20080110 00114 NM 2008 1 10 USAA920080006 1 20071227 A 5320 655162618 PAN BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C16 CHECK - CORROSION ON POTABLE WATER SERVICE PAN, BS 947 - BS 967, S24L - S24R. REPLACED POTABLE WATER SERVICE PAN, BS 947 - BS 967, S24L - S24R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008011000115 20080110 00115 NM 2008 1 10 USAA920080007 1 20071228 A 5330 655298874 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C16 CHECK - CRACKED FUSELAGE SKIN, BS 943 S24L. REPAIRED FUSELAGE SKIN, BS 943, S24L IAW USAIRWAYS EA 100084. 2 L 7 2 4F RT A16WE 2008011000117 20080110 00117 NM 2008 1 10 USAA920080009 1 20071206 A 5311 6546555 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C16 CHECK - CRACKED FRAME, BS 867, S8L - S9L. REPAIRED FRAME, BS 867, S8L - S9L IAW USAIRWAYS EA 1 00111. 2 L 7 2 4F RT A16WE 2008011000118 20080110 00118 NM 2008 1 10 USAA920080010 1 20071206 A 5311 6546552 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C16 CHECK - CRACKED FRAME, BS 827, S8L - S9L. REPAIRED FRAME, BS 827, S8L - S9L IAW USAIRWAYS EA 1 00111. 2 L 7 2 4F RT A16WE 2008011000119 20080110 00119 NM 2008 1 10 USAA920080011 1 20071206 A 5311 6546550 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C16 CHECK - CRACKED FRAME, BS 787, S8L - S9L. REPAIRED FRAME, BS 787, S8L - S9L IAW USAIRWAYS EA 1 00111. 2 L 7 2 4F RT A16WE 2008011000120 20080110 00120 NM 2008 1 10 USAA920080012 1 20071206 A 5311 6546548 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C16 CHECK - CRACKED FRAME, BS 747, S8L - S9L. REPAIRED FRAME, BS 747, S8L - S9L IAW USAIRWAYS EA 1 00111. 2 L 7 2 4F RT A16WE 2008011000121 20080110 00121 NM 2008 1 10 USAA920080013 1 20071206 A 5311 6525229 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C16 CHECK - CRACKED FRAME, BS 727D, S8L - S9L. REPAIRED FRAME, BS 727D, S8L - S9L IAW USAIRWAYS EA 100111. 2 L 7 2 4F RT A16WE 2008011000122 20080110 00122 NM 2008 1 10 USAA920080014 1 20071206 A 5311 6546596 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C16 CHECK - CRACKED FRAME, BS 727B, S8L - S9L. REPAIRED FRAME, BS 727B, S8L - S9L IAW USAIRWAYS EA 100111. 2 L 7 2 4F RT A16WE 2008011000123 20080110 00123 NM 2008 1 10 USAA920080015 1 20071206 A 5311 6546555 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C16 CHECK - CRACKED FRAME, BS 867, S8R - S9R. REPAIRED FRAME, BS 867, S8R - S9R IAW USAIRWAYS EA 1 00111. 2 L 7 2 4F RT A16WE 2008011000125 20080110 00125 NM 2008 1 10 USAA920080017 1 20071205 A 5311 6546548 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C16 CHECK - CRACKED FRAME, BS 747, S8R - S9R. REPAIRED FRAME, BS 747, S8R - S9R IAW USAIRWAYS EA 1 00111. 2 L 7 2 4F RT A16WE 2008011000126 20080110 00126 NM 2008 1 10 USAA920080055 1 20071220 A 5330 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FUSELAGE SKIN, BS 948, S14L - S15L. REPAIRED FUSELAGE SKIN, BS 948, S14L - S15 L IAW B737 SRM 53-00-01-10. 2 L 7 2 4F RT A16WE 2008011000128 20080110 00128 NM 2008 1 10 USAA920080057 1 20071229 A 5751 65C2591118A SKIN BOEING 737 7373G7 1384595 NM RT AILERON DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - RIGHT WING AILERON UPPER SURFACE HAS DELAMINATION. REPAIRED RIGHT WING AILERON UPPER S URFACE IAW USAIRWAYS EA 100087. 2 L 7 2 4F RT A16WE 2008011000129 20080110 00129 SW 2008 1 10 H9X2007F00000 1 20071201 A 6510 2040107553 HOUSING BELL 204 UH1B 1181410 SW LYC T53 T53* 41549 NE TAIL ROTOR QUILL DAMAGED E H9XA B EMER. DESCENT F FLT CONT AFFECTED CR CRUISE 1 WP 25 198HM 1400 621996 AIRCRAFT WAS RETURNING HOME FROM FLIGHT AND PILOT NOTICED THE PEDALS WERE NOT OPERATING NORMALLY. HE THEN BEGAN CIRCLIN G THE AIRPORT UNTIL WE DETERMINED THAT THE PROBLEM WAS A PARTIALLY LT STUCK TAIL ROTOR PEDAL, AT WHICH TIME HE DECLARED AN EMERGENCY AND LANDED THE AIRCRAFT WITH NO DAMAGE TO THE AIRCRAFT. UPON INSPECTION, REMOVED THE T/R QUILL HOUSING AN D FOUND THE SPLINE PORTION OF THE HOUSING STRIPED IN THE MIDDLE PORTION OF THE SPLINE. (K) 1 G 7 1 4U 4 U EXPA1G71 E1EA 2008011000134 20080110 00134 CE 2008 1 10 DJFA2007145 1 20071216 A 3240 AHA1897 BRAKE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG ERRATIC E DJFA O OTHER O OTHER LD LANDING 1 EA 23 839LX 258657 ON LANDING CREW REPORTED BRAKES DO NOT APPLY WHEN BRAKE PEDALS ARE DEPRESSED IN A NORMAL FASHION BRAKE PEDALS MUST BE DE PRESSED MUCH FURTHER DOWN THAN NORMAL BEFORE BRAKING OCCURS WHEN BRAKES DO APPLY THEY GRAB OR SUDDENLY OVER APPLY DIRECT IONAL CONTROL DIFFICULT TO MAINTAIN DURING LANDING ROLL ONE THRU PATCHY ICE. MAINTENANCE REPLACED THE NR 3 AND NR 4 BRA KES. 2 L 7 2 4F 4 F RT A3EU E6WE 2008011000135 20080110 00135 CE 2008 1 10 DJFA2007147 1 20071218 A 2612 7013348943 DAU CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NR 1 FALSE INDICATION E DJFA O OTHER J WARNING INDICATION CR CRUISE 1 EA 23 704LX 19 19 7500091 IN CRUISE CREW REPORTED INTERMITTENT NR 1 ENGINE AND APU FIRE EICAS WARNINGS ALONG WITH A DAU NR 1 MISCOMPARE MESSAGE ON THE EICAS. MAINTENANCE REVIEWED A RECENTLY REPLACED DAU; ON REVIEW OF THE TEARDOWN REPORT IT WAS NOTED THAT THE UNIT W AS RETURNED TO SERVICE AS A NO-FAULT-FOUND FROM THE BENCH - PREVIOUS FAILURE WAS FALSE WARNINGS ON A DIFFERENT AIRCRAFT. MAINTENANCE REPLACED THE NR 1 DAU. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008011000138 20080110 00138 NM 2008 1 10 ZZDA2007315 1 20071231 A 5610 5912290508 WINDOW BOEING 717 717200 1383700 NM COCKPIT FAILED A ZZDA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 37 952AT 55014 ON TAXI OUT F/O WINDOW FWD HAD ARCING AND ELEC SMOKE RT UPPER CORNER. TURNED OFF HEAT, ARCING AND SMOKE STOPPED. REPLA CED F/O WINDSHIELD PER MM 56-11. OPS CHECK GOOD. 2 L 7 2 4F TR A6WE 2008011000141 20080110 00141 NM 2008 1 10 USAA920080061 1 20071219 A 5320 6546877 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED HORIZONTAL WEB, BS 727 - BS 727A, S18AL. REPLACED HORIZONTAL WEB, BS 727 - BS 727A, S18AL IAW USAIRWAYS EA 100057. 2 L 7 2 4F RT A16WE 2008011000143 20080110 00143 NM 2008 1 10 USAA920080063 1 20071217 A 5315 STRAP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FLOORBEAM STABILIZER STRAP, BS 328, RBL 48. REPAIRED FLOORBEAM STABILZER STRAP , BS 328, RBL 48 IAW B737 SRM 53-10-51. 2 L 7 2 4F RT A16WE 2008011000149 20080110 00149 EU 2008 1 10 2007UALA05274 1 20071225 A 3350 100865 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 406UA 454 EMERGENCY LIGHT TEST FAILS LEFT FORWARD DOOR BATTERY. BATTERY FAULTY. REPLACED DOOR LIGHT BATTERY AT DOOR 1L. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011000152 20080110 00152 EU 2008 1 10 2007UALA05276 1 20071224 A 3397 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 495UA 1842 ROW 24C, 25C & 26C EMERGENCY LIGHTS OUT. LOOSE CONNECTOR AT 24C. RESECURED CONNECTOR AT SIDEWALL. OPS CHECKED NORMALL Y. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011000154 20080110 00154 NM 2008 1 10 2007UALA05336 1 20071227 A 3350 BR964421 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 821UA 944 EMERGENCY LIGHT AT AISLE SEAT 15C IS INOPERATIVE. FAULTY LIGHT ASSY. REPLACED LIGHT ASSY. OPS CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011000158 20080110 00158 NM 2008 1 10 2007UALA05347 1 20071228 A 3510 A300812OMO TRANSDUCER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CREW O2 FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 203UA 24718 CREW OXYGEN CYLINDER IN PIT READING 500 TO 600 LBS LESS THAN AT FILL STATION AND IN FLIGHT DECK. SUSPECT PRESSURE TRANS DUCER FAULTY. REPLACED PRESSURE TRANSDUCER PER MM 35-12-21. OPS AND LEAK CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011000161 20080110 00161 NM 2008 1 10 2007UALA05348 1 20071228 A 5310 ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C 13802 EU DOOR FRAME CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 FWD ENTRY DOOR AFT CUTOUT AT BS 360 WEB AT STR 11L CRACKED AT ANGLE. INSTALLED NEW ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011000163 20080110 00163 NM 2008 1 10 2007UALA05349 1 20071228 A 5313 STRINGER SPLICE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 FUSELAGE STRINGER SPLICE CHANNEL WAS FOUND CRACKED AT BS 360 STR 15L. REPLACED STRINGER SPLICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011000166 20080110 00166 NM 2008 1 10 2007UALA05350 1 20071228 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 FWD ENTRY DOOR UPPER HINGE CUTOUT HAS 1 EA FASTENER SHOWING CRACK INDICATION FROM NDT. FABRICATED AND INSTALLED EXTERNA L FUSELAGE SKIN DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011000167 20080110 00167 NM 2008 1 10 2007UALA05351 1 20071228 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 375UA 24640 TWO EMERGENCY EXTERIOR LIGHTS ARE INOP, AFT OF DOOR 1L AND AFT OF LEFT INBOARD FLAP. SECURED STRIP SOCKET. OPS CHECKS G OOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011000170 20080110 00170 NM 2008 1 10 2007UALA05352 1 20071228 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 ONE SMALL DENT LOCATED LT SIDE OF A-C STA 251 JUST BEHIND RT PITOT TUBE MEASURING 1"L X 1"D X .045 DEEP. A-Y IS 22. FA BRICATED AND INSTALLED EXTERNAL FUSELAGE SKIN DOUBLER-TRIPLER REPAIR IN THE RVSM AREA. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011000171 20080110 00171 NM 2008 1 10 2007UALA05353 1 20071228 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 908 WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 UPPER FUSELAGE DORSAL FIN AREA AT BS 908 HAS WEAR MARKS ON BOTH LT AND RT SIDES. FABRICATED AND INSTALLED SINGLE EXTERN AL FUSELAGE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011000173 20080110 00173 NM 2008 1 10 2007UALA05355 1 20071228 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C 13802 EU BS 907-1006 WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 UPPER FUSELAGE CROWN SKIN HAS WEAR DAMAGE AT RT DORSAL FIN LANDING AREA FROM STA 907 TO 1006. FABRICATED AND INSTALLED SINGLE EXTERNAL FUSELAGE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011000175 20080110 00175 NM 2008 1 10 2007UALA05356 1 20071228 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 FWD ENTRY DOOR FWD CUTOUT AT BS 294.5 WEB AT STR 8L CRACKED AT ANGLE. INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011000176 20080110 00176 NM 2008 1 10 2007UALA05357 1 20071228 A 5320 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 FWD NOSE COMPARTMENT STA 227 LWR CHORD CORRODED LBL 0 TO LBL 4. INSTALLED REINFORCING REPLACEMENT REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011000178 20080110 00178 NM 2008 1 10 2007UALA05359 1 20071229 A 3350 REFLECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 375UA 24640 TEST FLIGHT, EMERGENCY EXIT LIGHT INOP, DOOR 1L. REPLACED REFLECTOR ASSEMBLY. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011000182 20080110 00182 NM 2008 1 10 2007UALA05363 1 20071231 A 3510 A300812OMO TRANSDUCER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CREW O2 FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 THE O2 BOTTLE PRESS AT 1400 PSI WITH A-C GAUGES AT 1700 PSI. SUSPECT FAULTY PRESSURE TRANSDUCER. REPLACED PRESSURE TRA NSDUCER LEAK CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011000183 20080110 00183 NM 2008 1 10 2007UALA05364 1 20071231 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EEL INOP SEAT 3J FWD SECTION. SECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011000189 20080110 00189 NM 2008 1 10 2007UALA05369 1 20071229 A 5420 FITTING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 PYLON DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 532UA 25072 NR 2 PYLON STRUT FITTING (DELTA FITTING) NEEDS TO BE FABRICATED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008011000191 20080110 00191 NE 2008 1 10 DXTA200702714 2 20071225 A 7300 ENGINE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15* 52060 NE RIGHT POWER LOSS E DXTA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 07 341QS 5600341 ON TAKEOFF, UNABLE TO MAKE TAKEOFF, N1OF 95.5 PERCENT UNLESS THE POWER LEVER ON RT ENGINE WAS AT THE FIREWALL STOP. OPS CHECK GOOD ON ENGINE RUN. ALL NUMBERS WITHIN SPECS IAW MM 72-00-00. THROTTLE KNOB SPLIT WITHIN LIMITS. 2 L 7 2 4F 4 T RT A22CE E1NE 2008011000192 20080110 00192 CE 2008 1 10 DXTA200702715 1 20071225 A 2720 199409271 ACCUMULATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL E/E BAY LEAKING E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 941QS 7267 7500141 RUD STBY SYS FAIL (AMBER) ILLUMINATED 2 TIMES DURING FLIGHT. FOUND RUDDER STBY ACCUMULATOR GAGE TO BE LEAKING INTERNALL Y. REMOVED AND REPLACED GAGE WITH NEW IAW CE-750 M/M CHAP 29-10-04. SERVICED ACCUMULATOR TO 2000 PSI OAW CE-750 M/M CHAP 12-10-16. NO LEAKS DETECTED. OPS CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008011000193 20080110 00193 NM 2008 1 10 2007UALA05372 1 20071230 A 2841 PROCESSOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUEL QTY IND MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 783UA 26950 FUEL QUANTITY INDICATION ON EICAS DISPLAY FLUCTUATES. CREW COMMENTS: RIGHT FUEL QUANTITY INTERMITTENT. FUEL QUANTI TY PROCESSOR UNIT FAULTY.REPLACED FUEL QTY PROCESSOR UNIT. PERFORMED OPERATIONAL CHECK OK. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008011000194 20080110 00194 NM 2008 1 10 2007UALA05373 1 20071230 A 2120 UNKNOWN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN ODOR A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 783UA 26950 ROWS 11-13 RIGHT AISLE AREA HAD BURNING ODOR. CLEARED UP AFTER 5 MINUTES. PERFORMED ALL CABIN'S LIGHT AND BALLAST OPN AND EVIDENCE OF SMOKE AND BURNING ODOR-FOUND NONE, CHECKED DOOR 2 GALLEY'S ALL EQUIPMENT OPERATION-ALL GALLEY 'S EQUIPME NT OPERATION NORMAL. NO BURNING ODOR CONDITION NOTED WITH BOTH PACK'S ON AND ALL CABIN EQUIPMENT SYSTEM TURNED ON. UNAB LE TO DUPLICATE PROBLEM. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008011000195 20080110 00195 2008 1 10 DXTA200702716 4 20071227 A 3197 TERMINAL BLOCK AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE CONFIG WARNING DAMAGED E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 251QS 202 UPON POWER APPLICATION FOR TAKEOFF, TAKEOFF CONFIGURATION ANNUNICATOR ILLUMINATED ACCOMPANIED BY ORAL WARNING. CONFIRME D DISCREPANCY. T/S PROBLEM TO INTERMITTENT GROUND AT JUNCTION BLOCK 4JM. RESEALED ALL PINS. PERFORMED FUNCTIONAL TEST OF TAKE-OFF SAFETIES ALARM TEST AND INDICATION LOGIC I/A/W FALCON 2000 MM 31-301 AND 31-300. NO FURTHER DEFECTS NOTED. 2 L 7 2 4F 4 F RT A50NM E44NE 2008011000196 20080110 00196 NM 2008 1 10 2007UALA05374 1 20071229 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 MID LAV FWD RIGHT EEL LIGHT INOPERATIVE. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011000197 20080110 00197 NM 2008 1 10 2007UALA05375 1 20071229 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 CEILING EEL LIGHT INOPERATIVE AT ROW 16 UPPER DECK. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011000199 20080110 00199 NM 2008 1 10 2007UALA05377 1 20071229 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EXIT SIGN AFT DOOR 3R INOPERATIVE. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011000200 20080110 00200 CE 2008 1 10 DXTA200702717 1 20071227 A 3260 UPLOCK SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP RT MLG CONTAMINATED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 870QS 258732 RT MAIN GEAR UNSAFE LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF CLIMBING THRU 17000 FT. FOUND RT GEAR DOOR UPLOCK SWITCH WA TER SOAKED - CLEANED & LUBED SWTICH - COLD SOAKED SWITCH NO DEFECTS NOTED & PERFORMED GEAR SWINGS PER 800XP MM 32-30-01. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A3EU E6WE 2008011000201 20080110 00201 NM 2008 1 10 2007UALA05378 1 20071229 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 RIGHT SIDE SEATS 32, 33 & 34 EEL LIGHTS ARE INOPERATIVE. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011000202 20080110 00202 NM 2008 1 10 2007UALA05379 1 20071229 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 SEAT 2J FWD AND AFT EEL LIGHT INOPERATIVE. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011000203 20080110 00203 CE 2008 1 10 DXTA200702718 1 20071227 A 2750 MP50G4 DRIVE UNIT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS INOPERATIVE E DXTA A UNSCHED LANDING F FLT CONT AFFECTED DE DESCENT 1 GL 07 997QS 5118 7500208 UPON APPROACH, SELECTED FLAPS TO 5 DEGREES AND RECEIVED EICAS (FLAP FAIL) AMBER MESSAGE. TROUBLESHOT TO BAD PDU CLUTCH. REMOVED AND REPLACED PDU IAW 750 MM 27-52-00. ALSO CHECKED RESOLVERS OPERATION DURING FUNCTIONAL CHECK AND RESOLVERS CHECK GOOD. FLAPS OPS CHECK GOOD IAW 750 MM 27-50-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008011000204 20080110 00204 NM 2008 1 10 2007UALA05380 1 20071229 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 RIGHT SIDE FWD CLOSET EEL LIGHT INOPERATIVE. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010900207 20080109 00207 EA 2008 1 9 MASA200700831 1 20071130 A 2750 766359A PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 75998 7336 ASH FLT 7294 SPI-IAD - FLAPS FAILED AT 35 DEGREES ON TAXI IN. REMOVED AND REPLACED THE FLAP PDU, OPS NORMAL. 2 L 7 2 4F RT A21EA 2008010900234 20080109 00234 NM 2008 1 9 ASAA0752443 1 20071230 A 2432 893003 CHARGER BOEING 737 737890 1384527 NM E&E BAY MALFUNCTIONED A ASAA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 NM 02 577AS 35186 WHILE TAXIING OVERHEAD "ELEC" LIGHT ILLUMINATED. RAN FIM 24 31 TASK 801. ELECTRICAL MODULE SHOWED "BATTERY CHARGER INO P". CLEARED FAULT RERAN FIM TASK. NO FAULTS SHOWING. ALSO VISUALLY CHECKED BATTERY CHARGER INDICATION LIGHTS IAW FIM 24 31 TASK 824. BOTH LAMPS GREEN. 2 L 7 2 4F RT A16WE 2008010900299 20080109 00299 EA 2008 1 9 MASA200700513 1 20070821 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27185 7185 ASH IAD 7421 - EMERGENCY EXIT LIGHT ON LT FUSELAGE ASSY LOOSE. MX RESECURED LIGHT ASSY. 2 L 7 2 4F RT A21EA 2008010900305 20080109 00305 EA 2008 1 9 MASA200700706 1 20071017 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 593ML 7465 ASH FLT 7251 - LT EMERGENCY EXIT LIGHT INOP. MX INSPECTED, OPS CHECK GOOD NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2008010900308 20080109 00308 EA 2008 1 9 MASA200700712 1 20071018 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37178 7178 ASH FLT 2872, PHX - EMERGENCY LIGHTS ON WITH SWITCH IN ARMED POSITION. MX FOUND C/B POPPED, RESET AND OPS GOOD. 2 L 7 2 4F RT A21EA 2008010900318 20080109 00318 EA 2008 1 9 MASA200700544 1 20070902 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 591ML 7388 PAX DOOR EMERGENCY EXIT LIGHT INOP. REPAIRED BROKEN WIRE ON LIGHT. 2 L 7 2 4F RT A21EA 2008010900323 20080109 00323 EA 2008 1 9 MASA200700561 1 20070908 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7305V 7305 ASH FLT 2864 PHX - CABIN CEILING EMERGENCY EXIT LIGHT AT OVERWING EXITS INOP. MAINTENANCE RELAMPED, OPS NORMAL. 2 L 7 2 4F RT A21EA 2008010900337 20080109 00337 EA 2008 1 9 MASA200700643 1 20070926 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH FLT 2872 - PHX - CREW REPORTED THAT THE AFT EMERGENCY FLOOR LIGHT STRIPS WERE INOP. MX RESECURED LIGHT STRIP. 2 L 7 2 4F RT A21EA 2008010900344 20080109 00344 EA 2008 1 9 MASA200700667 1 20071004 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17358 7358 ASH 2818 PHX-DSM - MX REPORTED NR 6 EXTERNAL EMERGENCY LIGHT INOPERATIVE ON OVERNIGHT MAINTENANCE. RELAMPED, OPS GOOD. 2 L 7 2 4F RT A21EA 2008011000002 20080110 00002 NM 2008 1 10 ASAA0852445 1 20071231 A 4990 38809381 FILTER BOEING 737 737890 1384527 NM APU CLOGGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 585AS 35683 WHILE PERFORMING PDC FOUND APU OIL FILTER CLOGGED INDICATOR POPPED. REPLACED APU OIL FILTER AS REQUIRED. RAN APU. NO LEAKS, NO POPPED INDICATOR. 2 L 7 2 4F RT A16WE 2008011000006 20080110 00006 NM 2008 1 10 UPS07M51348 1 20071113 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C LT WING UPPER FUEL TANK STRINGER NR 12 END SUSPECT CRACKED. HFEC INSP C/O AT STR NR 12 END FOUND CRAC K OF APPROX 10.5 INCHES LONG. STR 12 SPLICE END & HI-LOKS REMOVED. CRACK AT LT WING STR NR 12 SLOT OUT PER SRM 57-2 0- 00 FIG 10 VI R35. HFEC INSP C/O ON SLOT OUT AREA & FOUND NO CRACK EVIDT. REPAIR ANGLES FAB, HEAT-TREATED, REPROTECTED & PAINTED. REPAIR ANGLES INSTALLED ON STR NR 12 END, CAP SEALING C/O & LEAK CHECK SATISFACTORY. 2 L 7 3 4F RT A22WE 2008011000010 20080110 00010 NM 2008 1 10 USAA920080041 1 20071228 A 5330 6545778 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 23876 PIT - MAJOR REPAIR - RON, CRACKED FUSELAGE SKIN, BS 947, S11R. REPAIRED FUSELAGE SKIN, BS 947, S11R IAW B737 SRM 53-60- 01 REPAIR 5. 2 L 7 2 4F RT A16WE 2008011000018 20080110 00018 CE 2008 1 10 DJFA2007146 1 20071217 A 3240 BRAKE BEECH MU300 400A 1155402 CE MLG MALFUNCTIONED E DJFA O OTHER O OTHER LD LANDING 1 EA 23 470LX RK478 ON LANDING CREW REPORTED NO BRAKES UNTIL (2) OR (3) TIMES NORMAL PRESSURE IS APPLIED TO THE BRAKE PEDDALS THEN THE BRAKE S GRAB EXTREAMLY HARD. MAINTENANCE BLED THE SYSTEM AND TAXIED THE AIRCRAFT WITH NO FURTHER PROBLEMS NOTED. 2 H 7 2 4F RT A16SW 2008011000023 20080110 00023 CE 2008 1 10 122107N540CS1 1 20071221 A 3233 99125373 ACTUATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG FAILED E Z5FA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 63 540CS 3185 5605516 LT MAIN GEAR DOWN INDICATION FAILED ON GEAR EXTENSION. AFM EMERGENCY PROCEDURES DID NOT REMEDY SITUATION. DIVERTED FROM SCHEDULED DESTINATION. DECLARED EMERGENCY AND LANDED AIRCRAFT WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED SUSPECT GEAR ACTUATOR AND OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008011000052 20080110 00052 EA 2008 1 10 COMA0760725 1 20071213 A 2760 FE210304 THROTTLE SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 629BR 7251 FLIGHT 5384 - ABORTED TAKEOFF BELOW 80 KTS FOR SPOILER CONFIG MESSAGE WITH POWER LEVERS ADVANCED. REMOVED AND REPLACED ACSU (THROTTLE POSITION INDICATOR). 2 L 7 2 4F RT A21EA 2008011000064 20080110 00064 EA 2008 1 10 COMA0760731 1 20071218 A 2752 854D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 587SW 12373 7062 FLIGHT 5186 - FLAPS FAIL CAUTION MESSAGE WHEN SELECTING FLAPS TO 8 DEGREES. EMERGENCY DECLARED AND AIRCRAFT LANDED SAFE LY IN CVG. REMOVED AND REPLACED RT OUTBOARD FLAP NR 4 ACTUATOR. 2 L 7 2 4F RT A21EA 2008011000081 20080110 00081 EA 2008 1 10 COMA0760744 1 20071228 A 3020 12681 PRESSURE SWITCH CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 739CA 7273 FLIGHT 5008 - RECEIVED LEFT COWL ANTI-ICE CAUTION. DIVERTED TO AVP, LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE COWL ANTI-ICE PRESSURE SWITCH. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011000110 20080110 00110 NM 2008 1 10 USAA920080002 1 20071204 A 5210 501945272 DOOR FRAME BOEING 737 7373G7 1384595 NM L1 DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C16 CHECK - L1 DOOR AFT EDGE BEAM CRACKED AT 3RD DOOR STOP HOLE FROM BOTTOM. REPAIRED THE L1 DOOR AFT EDGE BEAM AT 3RD DOOR STOP HOLE FROM BOTTOM IAW USAIRWAYS EA 100101. 2 L 7 2 4F RT A16WE 2008011000113 20080110 00113 NM 2008 1 10 USAA920080005 1 20071219 A 5312 6041025 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C16 CHECK - CRACKED VERTICAL BEAM WEB, BS 178, LBL 17, WL 224. REPAIRED VERTICAL BEAM WEB, BS 178, LBL 17, WL 224 IAW B737 SRM 53-10-08-2R12. 2 L 7 2 4F RT A16WE 2008011000124 20080110 00124 NM 2008 1 10 USAA920080016 1 20071205 A 5311 6546552 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C16 CHECK - CRACKED FRAME, BS 827, S8R - S9R. REPAIRED FRAME, BS 827, S8R - S9R IAW USAIRWAYS EA 1 00111. 2 L 7 2 4F RT A16WE 2008011000153 20080110 00153 NM 2008 1 10 2007UALA05335 1 20071227 A 2560 62222101 PANEL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EVAC SLIDE CRACKED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 815UA 867 LEFT OVERWING SLIDE PANEL IS CRACKED AT THE FWD UPPER CORNER (MKD). DELAMINATION OF PANEL. REPLACED SLIDE ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011000205 20080110 00205 NM 2008 1 10 2007UALA05381 1 20071229 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EEL LIGHT FWD OF AFT GALLEY LEFT. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011000206 20080110 00206 NM 2008 1 10 2007UALA05382 1 20071229 A 2621 30903822U1 SQUIB BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FIRE BOTTLE FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 FIRE SQUIB PANEL LIGHT FAILS TO ILLUM TEST SW 1 ENG 4. REPLACED BOTTLE A SQUIB REF MM26 -21-04 TEST OK. AC OK FOR SERVI CE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011000207 20080110 00207 CE 2008 1 10 DXTA200702719 1 20071227 A 3233 15500003 ACTUATOR CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE LT MLG INOPERATIVE E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 618QS 6409 5605506 FAILED TO GET LT MAIN GEAR LIGHT UPON EXTENDING MLG. JACKED A/C, REMOVED NR 2 ENG HYD PUMP TO FACILITATE HYD PWR W/ROBO MULE, REMOVED & REPLACED LT MLG ACTUATOR, SWING GEAR MULTIPLE TIMES NO DEFECT NOTED. DOWNJACKED A/C, REINSTALLED NR 2 E NGINE RAN, OPS & LEAK CHECKED. NO DEFECTS NOTED. ALL WORK DONE IAW CESSNA 560XLS MM 32-30-04, 32-01-00, 29-11-03-01, 7-1 0-01, 12-12-01 2 L 7 2 4F 4 F RT A22CE E00059EN 2008011000208 20080110 00208 NM 2008 1 10 2007UALA05383 1 20071231 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DEFECTIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 193UA 26890 THE "C" ZONE LEFT AFT COLUMN EEL LIGHT DIM. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011000209 20080110 00209 NM 2008 1 10 2007UALA05385 1 20071231 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT ODOR A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 29 537UA 25157 726594 DURING T/O ROLL BAD SMELL IN COCKPIT 30 SECONDS AFTER T/O POWER SET. CEASED AFTER 3 MINUTES. 2 L 7 2 4F 4 F RT A2NM E17NE 2008011000211 20080110 00211 EU 2008 1 10 2007UALA05317 1 20071228 A 2150 345540 GASKET AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT A/C PACK FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 430UA 568 RTFL AFTER LEAK DETECTED FROM ONE OF THE PACKS. CAUSE: FAULTY CLAMP AND PACKING AT DUCT AT LT. PACK OZONE CONVERTER AND FCV. REPLACED CLAMP AND PACKING 2 L 7 2 4F 4 F RT A28NM E40NE 2008011000212 20080110 00212 NM 2008 1 10 2007UALA05327 1 20071228 A 3510 B-NUT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE OXYGEN SYSTEM LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 834UA 1420 OXYGEN SUPPLY LOW 1380 PSI. FOUND SLOW LEAK IN CREW O2 SYSTEM. TIGHTENED B-NUT AT REGULATOR AND RESERVICED CREW O2. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011000213 20080110 00213 NM 2008 1 10 2007UALA05328 1 20071227 A 3510 HARNESS AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CAPTAIN'S OXYGEN LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 834UA 1420 CAPTAIN'S OXYGEN HARNESS FAILS TO INFLATE CAPT O2 MASK SUPPLY SWITCH PINCHED OPEN IN STOWED POSITION. RESTOWED THE MAS K CORRECTLY AND SERVICED CREW O2. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011000214 20080110 00214 2008 1 10 2007UALA05391 4 20071228 A 2312 DMC5017 ANTENNA BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE VHF SYSTEM FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 783UA 26950 VHF RADIO - RECEPTION PROBLEM CREW COMMENTS: GARBLED RECEPTION ON VHF 1. ALL POSITIONS - ALL FREQ. NOT A HEADSET PROB LEM. FOUND CONNECTION AT LT VHF ANTENNA. REPLACED VHF ANTENNA. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008011100001 20080111 00001 NM 2008 1 11 2007UALA05083 1 20071212 A 2150 6240141 SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A/C PACK FAULTY A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 551UA 25399 FLIGHT DIVERTED DUE TO PACK PROBLEM. RIGHT PACK TEMP INDICATOR FAILURE. REPLACED RT PACK TEMP SENSOR NR 2, NO REPEATS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008011100002 20080111 00002 CE 2008 1 11 VUC2007F00001 1 20071126 A 2612 FIRE WARNING LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP RT NACELLE FALSE ACTIVATION E VUCA O OTHER N FALSE WARNING CL CLIMB 1 CE 19 35TJ 137 UPON TAKEOFF, AC CLEARED TO FL410 AND THEN REQUESTED, AND WAS APPROVED FOR FL430. DURING CLIMB TO FL430, RT ENGINE FIRE WARNING LIGHT ILLUMINATED. FLIGHT CREW SLIGHTLY RETARDED THE POWER BACK ON THE RT ENGINE (WHICH WAS AT MAX CONTINUOUS ITT INDICATION) REQUESTED CLEARANCE TO FL390 AND DECLARED AN EMERGENCY. UPON PULLING POWER BACK THE FIRE WARNING LIGHT EXTINGUISHED. ADVANCING POWER ON THE AFFECTED ENGINE DID NOT CAUSE THE LIGHT TO ILLUMINATE AGAIN. NO DIFFERENCES OBSER VED BETWEEN LT AND RT ENGINE INDICATIONS. FLIGHT CREW PERFORMED FIRE WARNING CHECKLIST AND DETERMINED THAT THERE WAS A FALSE FIRE INDICATION. FLIGHT CREW UNDECLARED THE EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. AN EXTENSIVE VISUAL IN 2 L 7 2 4F 4 F A10CE E6WE 2008011100004 20080111 00004 NM 2008 1 11 ASMF200712002 1 20071215 A 5610 8935734 WINDOW BOEING 737 737* NM CFMINT CFM567 CFM567B22 13802 NE COCKPIT BROKEN W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 908AM 9632 9632 30038 DURING TRANSIT CHECK CAPTAIN REPORTED THE UPPER RT SIDE WINDOW NR 4 GOT BROKEN, MAINTENANCE PERSONNEL REPLACED THE WINDO W IAW MM 56-11-31, TESTED CORRECT IAW MM 30-41-31. 2 L 7 2 4F 4 F RT A16WE E00055EN 2008011100007 20080111 00007 EU 2008 1 11 2007UALA05243 1 20071221 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 489UA 1702 CABIN EMERGENCY LIGHTS ARE ON WITH SWITCH IN THE ARMED POSITION. PERFORMED SYSTEM RESET AND ALL LIGHTS ARE NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011100014 20080111 00014 EU 2008 1 11 2007UALA05252 1 20071223 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LOW A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 411UA 464 THE O2 LOW. SERVICED CREW O2 TO FULL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011100016 20080111 00016 EA 2008 1 11 CHQA200700097 1 20071217 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS MALFUNCTIONED A CHQA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 11 701BR 7448 GEE872845 ON APPROACH, THE FLAPS FAILED AT 30 DEGREES. THE AIRCRAFT PERFORMED A GO-AROUND, THE QRH WAS FOLLOWED, AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RESET POWER TO THE AIRCRAFT AND THE FAIL MESSAGE CLEARED, AFTER OPERATING THE FLA P SYSTEM SEVERAL TIMES THE FAIL MESSAGE DID NOT RETURN AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008011100019 20080111 00019 NM 2008 1 11 QXEA200701896 1 20071213 A 2931 INDICATION SYS DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE HYD PRESSURE MALFUNCTIONED A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 365PH FLIGHT 2138, AFTER ENGINE START THE NR 2 STANDBY HYDRAULIC PRESSURE SHOWS ZERO WITH THE SWITCH IN THE NR 2 POSITION. A IRCRAFT RETURNED TO THE GATE. MAINTENANCE RESET THE CIRCUIT BREAKER FOR THE SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 2008011100020 20080111 00020 EA 2008 1 11 QXEA200701881 1 20071213 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE ILLUMINATED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 606QX 10023 FLIGHT 2621, ON TAXI RECEIVED A AFT CARGO SOV MESSAGE. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PLACED THE SYSTEM ON M EL 21-55-4A. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008011100023 20080111 00023 EU 2008 1 11 2007UALA05297 1 20071224 A 3510 MXP401600U OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT LEAKING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 462UA 1272 CAPTAIN'S O2 WILL NOT TEST. CAPT O2 BOX IS LEAKING. REPLACED CAPT O2 STOWAGE BOX ASSY, LEAK CHECKED ALL LINES, OPS CHE CKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011100024 20080111 00024 NM 2008 1 11 QXEA200701899 1 20071213 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA FALSE INDICATION A QXEA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 429QX 4161 FLIGHT 2246, ON LANDING ROLL OUT RECEIVED A PUSHER SYSTEM FAIL CAUTION. RAN THE CHECKLIST AND THE CAUTION STAYED ON. MA INTENANCE COMPLIED WITH SL DH8-400-SL-31-31-005. LIGHT WENT OUT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE . NO PARTS REPLACED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2008011100025 20080111 00025 NM 2008 1 11 2007UALA05312 1 20071227 A 3350 D9239003500060 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 824UA 965 EPSU INT LOAD EMER L 33-51-38 FAULT DURING TEST AFTER ESCAPE SLIDE 2L REPLACEMENT. EMERGENCY LIGHT SYS NEEDS REPAIR. F AULTY POWER SUPPLY FOR EMERGENCY LIGHTS (EPSU). REPLACED EPSU, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011100028 20080111 00028 NM 2008 1 11 2008UALA0006 1 20071231 A 5210 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 DOOR 1L LOWER FWD FRAME CRACKED UNDER STOP FITTING. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011100029 20080111 00029 NM 2008 1 11 2008UALA0007 1 20071231 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 FWD GALLEY DOOR CUTOUT, AFT FRAME IS CRACKED AT 2ND STOP FITTING FROM TOP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011100030 20080111 00030 NM 2008 1 11 2008UALA0008 1 20071231 A 5241 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 FORWARD GALLEY DOOR LOWER FRAME WEB CRACKED AT AFT INBOARD CORNER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011100035 20080111 00035 NM 2008 1 11 2008UALA0013 1 20071231 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EEL INOP BETWEEN MID LAVS. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011100036 20080111 00036 NM 2008 1 11 2008UALA0014 1 20071231 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EEL INOP LT SIDE AFT GALLEY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011100038 20080111 00038 NM 2008 1 11 QXEA200701901 1 20071214 A 2130 PRESSURE SYSTEM BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA CABIN PRESSURE MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 425QX 4039 FLIGHT 2339. ON TAKEOFF ROLL PRESSURIZATION FAULT RECEIVED. SWITCHED TO MANUAL MODE IAW THE CHECKLIST. MAINTENANCE PLACE D THE AUTO PRESSURIZATION SYSTEM ON MEL 21-30-5B. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2008011100041 20080111 00041 NM 2008 1 11 2008UALA0016 1 20071231 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHT INOP DOOR 5L SLIDE ILLUM. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011100042 20080111 00042 NM 2008 1 11 QXEA200701880 1 20071213 A 5270 401020101 PROXIMITY SENSOR BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA PAX DOOR MALFUNCTIONED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 415QX 4081 FLIGHT 2340. AFTER TAKEOFF RECEIVED A FUSELAGE DOOR WARNING FOR THE MAIN CABIN DOOR. THE FLIGHT ATTENDANT REPORTED THAT THE DOOR APPEARED NORMAL, AIRCRAFT PRESSURIZATION WAS NOT AFFECTED. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE DOOR PROX SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2008011100046 20080111 00046 NM 2008 1 11 AMTA200700710 1 20071216 A 5753 SKIN BOEING 737 73783N 13844HI NM TE FLAP DAMAGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 315TZ 28245 LT IB FLAP HAS SEVERAL NICKS LOWER SURFACE. FABRICATED REPAIR SKINS AND STRAP DOUBLERS IAW SRM 51-70-10, REPAIR 4, FIG 203 AND EA NR 737-5753-09-A1234, ERA 737-57R-6181 FOR TRACKING. (K) 2 L 7 2 4F RT A16WE 2008011100047 20080111 00047 2008 1 11 AMTA200700711 4 20071215 A 3160 C16221KA02 DISPLAY BOEING 737 73783N 13844HI NM ISFD UNSERVICEABLE A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 305TZ 30706 ISFD DISPLAYING (SPD), (ALT) AND (HDG) FLAGS. REMOVED AND REPLACED ISDF INDICATOR. GROUND OPS CHECK GOOD IAW 34-24-02- 4. (K) 2 L 7 2 4F RT A16WE 2008011100050 20080111 00050 NM 2008 1 11 AMTA200700713 1 20071217 A 3150 WARNING LIGHT BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE NR 2 ENGINE FALSE INDICATION A AMTA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 308TZ 28244 ENGINE CONTROL LIGHT, LIGHT ON ENGINE NR 2. PERFORMED ACTUATOR TEST IAW AMM 71-00-00-5. NO FAULTS NOTED, OK FOR SERVIC E. (K) 2 L 7 2 4F 4 F RT A16WE E2GL 2008011100053 20080111 00053 NM 2008 1 11 2008UALA0021 1 20071231 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 652UA 25390 FS-3 LAV EMERGENCY LIGHT PATH BAR INOP AT LAV DOOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2008011100054 20080111 00054 EU 2008 1 11 UVV2007F00000 1 20071210 A 3010 FAL1007 HOSE AMD FALC10 FALCON10 2730101 EU GARRTT TFE731 TFE731* 01518 WP ANTI ICE SYS DELAMINATED B UVVR K NONE O OTHER IN INSP/MAINT 1 CE 03 222MU 171 164 THE LT OB SLAT ANTIICING HOSE (PN FAL 1007) WAS INSTALLED ON 9/8/2005 WHILE COMPLYING WITH AD 2005-07-23 AND SB F10-313. AD 2007-18-08 HAS SUPERSEDED AD 2005-07-23. IAW REQURIEMENTS OF THE MOST RECENT AD 2007-18-08, THE SLAT ANTI-ICE HOSE S BEARING PN FAL 1007 MUST BE REPLACED AT INTERVALS NOT TO EXCEED 700 FLIGHT CYCLES. UPON VISUAL INSPECTION, THIS HOSE EXHIBITS SUBSTANTIAL INTERNAL DELAMINATION WHICH COULD LEAD TO INSUFFICIENT AND ICING CAPABILITY. IAW THE AC LOG RECORD S, THIS HOSE HAS ACCUMULATED 405 FLIGHT CYCLES SINCE INSTALLATION. (K) 2 L 7 2 4F 4 F A33EU E6WE 2008011100057 20080111 00057 EU 2008 1 11 JM02007F00000 1 20071129 A 2910 723080171 TUBE ISRAEL 1124 1124A 4500103 EU GARRTT TFE731 TFE731* 01518 WP HYD SYSTEM LEAKING E JM0A O OTHER K FLUID LOSS LD LANDING 1 SW 19 407W 10619 407 APPROX 2 MINUTES AFTER THE LANDING GEAR WAS DEPLOYED AND A FEW SECONDS BEFORE LANDING, FLIGHT CREW REPORTED AN (UNUSUAL SMELL) ON THE FLIGHT DECK. NO OTHER WARNING OR INDICATOR WAS NOTED. LANDING PROCEEDED AS USUAL. ON POST FLIGHT INSPEC TION, HYDRAULIC RESERVOIR WAS FOUND TO BE ABNORMALLY LOW. FLIGHT DECK FLOOR WAS REMOVED AND BELLY WAS FOUND TO BE WET W ITH HYDRAULIC FLUID. VISUAL INSPECTION APPLIED TO SYSTEM, A SEEPAGE WAS FOUND IN A GEAR DOWN PRESSURE LINE, THOUGH NO VI SUAL MECHANICAL DEFECT WAS NOTED. AFTER MANY PRESSURE CYCLES MICROSCOPIC PERFORATIONS IN TUBE AT STA 96.00 BECAME EVIDE NT. REPAIR WAS MADE UNDER OEM EO AND AIRCRAFT RETURNED TO SERVICE. (K) 2 M 7 2 4F 4 F A2SW E6WE 2008011100059 20080111 00059 NM 2008 1 11 C77A200700004 1 20071219 A 3150 WARNING LIGHT EMB ERJ170 ERJ170200LR 3260121 NM MAU 1 FALSE ACTIVATION A C77A B EMER. DESCENT N FALSE WARNING AP APPROACH 1 EA 27 607CZ 176 176 17000192 ON INITIAL APPROACH, CONFIGURATION MESSAGES APPEARED ON EICAS: FLIGHT CONTROL NO DISPATCH, SLAT FAIL AND SHAKER ANTICIPA TED. MAINTENANCE PERFORMED A RETURN TO SERVICE TEST, IAW AMM 27-00-00, CLEARED ALL MESSAGES. 2 L 7 2 4F RT A56NM 2008011100060 20080111 00060 CE 2008 1 11 GUUA12120701 1 20071212 A 2697 CONNECTOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FIRE BOTTLE DIRTY A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 29 69547 UE189 DURING FLIGHT RT FIRE BOTTLE DISCHARGE ANNUNCIATOR ILLUMINATED. CLEANED CONNECTIONS AT RT FIRE BOTTLE SQUIB. 2 L 7 2 4T 4 T RT A24CE E26NE 2008011100061 20080111 00061 CE 2008 1 11 GUUA12130701 1 20071213 A 2697 CONNECTOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FIRE BOTTLE LOOSE A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 29 69547 UE189 DURING FLIGHT RT FIRE BOTTLE DISCHARGE ANNUNCIATOR ILLUMINATED. SECURED LOOSE CONNECTION AT RT FIRE BOTTLE. 2 L 7 2 4T 4 T RT A24CE E26NE 2008011100067 20080111 00067 SO 2008 1 11 GUUA12160701 1 20071216 A 3234 12038594001 CONTROL LEVER EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE MLG INOPERATIVE A GUUA O OTHER J WARNING INDICATION CL CLIMB 1 SO 29 283AS 120236 AFTER TAKEOFF, LT MAIN AND NOSE LANDING GEAR RED (A) LIGHTS ILLUMINATED. REPLACED LANDING GEAR CONTROL LEVER ASSEMBLY. 2 L 7 2 4T 4 T RT A31SO E20NE 2008011100069 20080111 00069 SO 2008 1 11 GUUA12170701 1 20071217 A 3260 922AA2YA692722A PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE LT MLG SHORTED A GUUA O OTHER N FALSE WARNING CL CLIMB 1 SO 29 266AS 120188 AFTER TAKEOFF LT MAIN GEAR RED (A) ANNUNCIATOR ILLUMINATED UPON GEAR RETRACTION AND REMAINS ON. RETURNED TO FLL. REPLAC ED CIRCUIT (A) UPLOCK PROXIMITY SENSOR. 2 L 7 2 4T 4 T RT A31SO E20NE 2008011100071 20080111 00071 NM 2008 1 11 LYNX00002 1 20071212 A 5270 22420179007 PROXIMITY SWITCH BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR SEIZED A 3LYA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 21 506LX 35 4176 DEPARTING, ON CLIMB OUT. AFT CARGO DOOR WARNING INDICATION AND AUTO PRESSURIZATION INOP. AIR RETURN. MAINTENANCE FOUND T HE AFT CARGO DOOR PROX SWITCH STUCK IN THE UP POSITION. MAINTENANCE CLEANED AND LUBED THE FLOATING PROX SWITCH. VERIFIED ON PSEU THAT THE FAULT WAS THE ABDLK PROX SWITCH TO FAR WHICH RENDERED THE AUTO PRESSURIZATION CONTROLLER INOP. PERFORM ED CHECK ON AUTO PRESS CONTROLLER AND AFT BAGGAGE DOOR. OPPS CHECKED GOOD AND RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008011100073 20080111 00073 SO 2008 1 11 CHQA200700098 1 20071217 A 2913 971808MODA PUMP EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 ENGINE INOPERATIVE A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 566RP 13973 13973 145691 CAE312032 DURING CLIMB, THE CREW RECEIVED AN E1 HYDRAULIC PUMP FAIL MESSAGE. THE FLIGHT CREW CONTACTED MAINTENANCE CONTROL AND DI SPATCH AND IT WAS DECIDED THAT THE FLIGHT WOULD DIVERT. THE AIRCRAFT FUNCTIONED NORMALLY ON THE ELECTRIC PUMP AND THE F LIGHT LANDED WITHOUT INCIDENT.MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THAT THE ENGINE 1 HYDRAULIC PUMP WAS NOT FUN CTIONING AND THE DRIVE SHAFT HAD SHEARED. AFTER REPLACING THE HYDRAULIC PUMP AND THE DRIVE SHAFT THE ENGINE 1 HYDRAULIC PUMP WAS LEAK TESTED AND OPS CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008011100074 20080111 00074 WP 2008 1 11 ANCF200700033 1 20071220 A 2751 SWITCH DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE TE FLAPS OUT OF ADJUST W ANCF C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 23 160BS 53463 DURING T/O ROLL, T/O CONFIGURATION FLAP WAS PRESENTED AT SPEED 105 KTS 110.500 LBS. THE FLAP STAT HANDLE POSITION SWITC HES WERE ADJUSTED. IAW AMM 27-80-07 PAG 205 TEST SATISFACTORY. 2 L 7 2 4F 4 F RT A6WE E2EA 2008011100079 20080111 00079 SO 2008 1 11 FFKA123 2 20071217 A 8520 646743 PISTON PIPER PA34 PA34200T 7103406 SO CONT O360 LTSIO360EB 17025 SO NR 2 ENGINE BURNED B FFKA B E A EMER. DESCENT ENGINE SHUTDOWN UNSCHED LANDING E K J VIBRATION/BUFFET FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 05 553DM 706 347670330 807758R PILOT REPORTED A LOSS OF POWER ON THE RT ENGINE AND DECLARED AN EMERGENCY. MAINTENANCE PERFORMED A COMPRESSION CHECK O N THE CYLINDERS AND FOUND ZERO PRESSURE ON (1) OF THE CYLINDERS. UPON REPLACEMENT OF CYLINDER IT WAS FOUND THAT THE PIS TON HAD A (HOLE) DOWN THE SIDE OF THE PISTON. REPLACED PISTON AND NO OTHER DEFECTS WERE NOTED. 1 L 7 2 3O 3 O A7SO E9CE 2008011100081 20080111 00081 NM 2008 1 11 QXEA200702011 1 20071220 A 2430 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA NR 1 GENERATOR ILLUMINATED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 423QX 4153 FLIGHT 2461, NR1 DC GENERATOR CAUTION LIGHT ILLUMINATED. RETURNED TO THE GATE. MAINTENANCE PLACED THE SYSTEM ON MEL 24-3 0-6. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2008011100083 20080111 00083 NM 2008 1 11 QXEA200702013 1 20071220 A 3397 CONNECTOR BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA EMERGENCY LIGHTS DISCONNECTED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 425QX 4039 FLIGHT 2463. FLIGHT ATTENDANT CANNOT ARM THE THE EMERGENCY LIGHTS OR TEST THEM IN THE CABIN. THE F/O CANNOT ARM OR TEST THEM EITHER. THE EMERGENCY LIGHTS DISARM CAUTION LIGHT ALSO FAILS TO ILLUMINATE WITH THE EMERGENCY LIGHTS SWITCH (IN THE COCKPIT) IN EITHER POSTION. MAINTENANCE FOUND THE CONNECTOR PLUG 3351 P2 DISCONNECTED OB OF THE GALLEY CLOSET. CONNECT ED THE PLUG. EMERGENCY LIGHTS SYSTEM CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2008011100084 20080111 00084 NM 2008 1 11 QXEA200702012 1 20071220 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA ELEVATORS ILLUMINATED A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 423QX 4153 ELEVATOR ASSYMMETRY CAUTION LIGHT ILLUMINATED IN A TURN WITH THE AUTOPILOT ENGAGED. NO ASYMMETRY OBSERVED ON PFCS INDICA TOR. COMPLIED WITH CHECKLIST. ON LANDING ROLLOUT, THE LIGHT WENT OUT. MAINTENANCE COMPLIED WITH SL DH8-400-SL-27-001R1. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2008011100085 20080111 00085 EA 2008 1 11 QXEA200702009 1 20071219 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE ILLUMINATED A QXEA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 615QX 10065 FLIGHT 2606. AVIONICS FAN CAUTION DURING TAXI, SELECTED ALTERNATE IAW THE CHECKLIST. AFTER TAKEOFF IT ILLUMINATED AGAIN, SELECTED NORMAL AND IT WENT OUT. DURING TAXI IN, LIGHT DID NOT COME ON. MAINTENANCE PLACED ON MEL 21-24-3. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008011100091 20080111 00091 NM 2008 1 11 ASMF200712003 1 20071218 A 5330 SKIN BOEING 737 737* NM CFMINT CFM567 CFM567B22 13802 NE BS 807 S26-27R DAMAGED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 851AM 29363 DURING TRANSIT CHECK THE AIRCRAFT WAS HIT BY A BAGGAGE CONVEYOR IN THE LOWER FUSELAGE SKIN AT STATION 807 BETWEEN STRING ER 26R AND 27R; CAUSING A DAMAGE OUT OF LIMITS OF 1INCH DIAMETER AND 0.066 INCH DEPTH IAW SRM 53-00-01. MAINTENANCE PER SONNEL REPAIRED THE FUSELAGE SKIN IAW ENGINEERING DWG AMR 3753008 AND SERVICE REQUEST ID1-726119416-4 APPROVED FAA FORM 8100-9 DATED DECEMBER 19TH, 2007. 2 L 7 2 4F 4 F RT A16WE E00055EN 2008011100100 20080111 00100 2008 1 11 AWKA121707 4 20071217 A 3418 COMPUTER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL AOA DEFECTIVE E AWKA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 25 772PT 497 7500272 DURING CLIMB, PASSING FL340, RECEIVED A RED AUTO SLATS FAIL CAS MESSAGE SAME TIME THE STICK SHAKER WENT OFF. DISENGAGED AUTOPILOT & LEVELED OFF TO INCREASE AIRSPEED. TLA’S SET IN CLIMB POWER DETENT. STICK SHAKER REMAINED ON & AOA INDICA TOR SHOWING .2. THROUGHOUT THE EVENT THE CO-PILOT REPORTED THE RED AUTO SLATS FAIL CAS MESSAGE OCCURRED ANOTHER 3-4 TIM ES. NOTICED AN AMBER SLATS FAIL CAS MESSAGE INTERMITTENT. AND A WHITE/AMBER SPEED TAPE FLUCTUATING UP AND DOWN. ALL AIRSPEED INDICATIONS APPEARED NORMAL. STICK SHAKER CONTINUED FOR SEVERAL MINUTES. AFTER LEVEL OFF AT APPROX FL363, & E MERGENCY INDICATIONS STILL PRESENT, RECEIVED A CLEARANCE TO FL350 & BEGAN DESCENT. DURING DESCENT, STICK SHAKER PERSIS 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008011100102 20080111 00102 EA 2008 1 11 QXEA200702020 1 20071223 A 3320 LIGHT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE CABIN ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 608QX 10026 SEAT 4A PSU LENS COVER FELL OFF AND NOTICED A BURNED ODOR COMING FROM THE LIGHT AREA. MAINTENANCE INSPECTED AREA AND NOT ICED NO EVIDENCE OF BURNS OR SMOKE. REINSTALLED THE LIGHT COVER. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008011100104 20080111 00104 NM 2008 1 11 QXEA200702018 1 20071223 A 3010 4100S00503 VALVE BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA DE ICE SYS MALFUNCTIONED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 401QX 9488 1241 4031 DE-ICE PRESSURE CAUTION ILLUMINATED. RAN CHECKLIST AND THE RT OUTER BOOT SEEMS TO BE THE ONE WITH THE PROBLEM. LIGHT ILL UMINATES LATE OR NOT AT ALL. APPEARS TO INFLATE OK FROM OBSERVATION FROM THE FLIGHT DECK. MAINTENANCE REPLACED THE NR 4 DISTRIBUTOR VALVE ON THE RT SIDE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2008011100105 20080111 00105 EA 2008 1 11 QXEA200702017 1 20071221 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE ILLUMINATED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 612QX 10042 FLIGHT 2503. FIRE SYSTEM FAULT MESSAGE RECEIVED. MAINTENANCE PLACED THE SYSTEM ON MEL 26-00-1. AIRCRAFT RETURNED TO SERV ICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008011100106 20080111 00106 NM 2008 1 11 QXEA200702014 1 20071223 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA ILLUMINATED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 402QX 4032 AMBER ICE LIGHT DETECTED ON DISPLAY. CAME ON DURING TAXI OUT. WOULD NOT GO OUT UNTIL PROPS SET TO FEATHER AFTER PARKING . RETURNED TO THE GATE. MAINTENANCE PLACED ON MEL 30-80-2. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2008011100109 20080111 00109 WP 2008 1 11 FX7A200700008 1 20071222 A 2740 95905 ACTUATOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE TRIM INOPERATIVE A FX7A O OTHER E VIBRATION/BUFFET TO TAKEOFF 1 SO 19 905TA 49905 AFTER TAKEOFF, AROUND 2,500 FEET, FLIGHT CREW WAS UNABLE TO TRIM AIRCRAFT WITH CAPTAIN, F/O SUITECASE OR ALTERNATE TRIM. AIRCRAFT WAS FLOWN WITH ELEVATORS ONLY. AROUND 250 KTS VIBRATION WAS FELT THROUGHTOUT THE AIRCRAFT. AFTER LANDING, T RIM SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F A6WE E9NE 2008011100126 20080111 00126 NM 2008 1 11 HNAA0800009 1 20071222 A 3397 6405451 WIRE HARNESS DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A HNAA K NONE L NO TEST UK UNKNOWN 1 EA 07 825EX 32678 32678 388 THE CABIN FLOOR EMERGENCY LIGHTING AT ROW 4 WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND A WIRE BROKEN AND CONTACT PI N PULLED FROM CONNECTOR 3352-P5. WIRE WAS REPAIRED AND CONNECTOR PIN WAS REPLACED. OPS CHECK OF SYSTEM WAS GOOD AND AI RCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 2008011100127 20080111 00127 CE 2008 1 11 AMWA89064BC 1 20071213 A 3150 WARNING LIGHT BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE ILLUMINATED A AMWA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 159YV UE159 BATTERY CHARGE ANNUNCIATOR ILLUMINATED FROM AFTER START TO AFTER TAKEOFF, WHEN CHARGE RATE DECREASED BELOW 7A, MASTER CA UTION FLASHERS W/N REMAIN EXTINGUISHED-TRIPPED MULTIPLE TIMES. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY DURIN G TROUBLESHOOTING ON GROUND. 2 L 7 2 4T 4 T RT A24CE E26NE 2008011100128 20080111 00128 NM 2008 1 11 HNAA0800010 1 20071230 A 2751 44281508010 INDICATOR DHAV DHC8 DHC8102 2809003 NM COCKPIT FAULTY A HNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 07 805EX 17476 288 228 DURING TAKEOFF, T/O WARNING HORN SOUNDED AT APPROXIMATELY 50 KNOTS AND THE TAKEOFF WAS ABORTED. CREW CYCLED FLAPS FROM 0 DEG TO 35 DEG, THEN BACK TO 5 DEG AND SYSTEM OPERATED NORMALLY. MAINTENANCE CHANGED THE FLAP POSITION INDICATOR AND S YSTEM OPS CHECKED GOOD IAW PIEDMONT PROCEDURES. AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 2008011100133 20080111 00133 EU 2008 1 11 TRBA2007115 1 20071223 A 3297 D22701072 WIRE HARNESS AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE MLG FAILED A TRBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 431AT 431 AFTER DEPARTURE LANDING GEAR HANDLE WILL NOT MOVE, FROZEN IN PLACE. REMOVED AND REPLACED NOSE LANDING GEAR HARNESS IAW M M 32-21-11. REMOVED AND REPLACED RT MAIN LANDING GEAR WOW 54GB HARNESS IAW 32-11-51. 2 H 7 2 4T 4 T RT A53EU E20NE 2008011100137 20080111 00137 2008 1 11 HNAA0800012 4 20071225 A 3197 V319 SWITCH DHAV DHC8 DHC8102 2809003 NM COCKPIT DETERIORATED A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 907HA 57163 57163 011 DURING TAKEOFF ROLL, T/O WARNING HORN SOUNDED. CREW ABORTED TAKEOFF. FLAPS WERE CYCLED AND HORN DID NOT SOUND. MAINTE NANCE FOUND CONDITION LEVER MICRO SWITCH 3151-S3 TO HAVE A DETERIORATED SOLDER JOINT AT THE SWITCH. SWITCH WAS RESOLDER ED AND SYSTEM CHECKED IAW PIEDMONT WORK CARD PROCEDURES. OPS CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008011100138 20080111 00138 NM 2008 1 11 HNAA0800013 1 20071229 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN EXPOSED A HNAA K NONE O OTHER UK UNKNOWN 1 EA 07 937HA 148 THE ROW 9 EMERGENCY LIGHTS WIRING WAS FOUND EXPOSED. WIRES WERE REPOSITIONED UNDER PROTECTIVE COVER STRIP. AIRCRAFT WA S RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008011100139 20080111 00139 GL 2008 1 11 HEEA118523 2 20071219 A 7200 ENGINE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 1 FAILED B HEEA O OTHER O OTHER CR CRUISE 1 SW 03 1545K 760047 APPROXIMATELY 30-40 SECONDS AFTER COMPLETION OF CRUISE CHECKLIST AT 2750 FEET NR1 ENGINE FAILED. COMPLETED EMERGENCY CH ECKLIST. DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. 1 G 7 2 3U 3 U H1NE E1GL 2008011100140 20080111 00140 SW 2008 1 11 HEER118528 1 20071216 A 5320 407030450195S SUPPORT BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FUSELAGE CRACKED B HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 741PH 53457 FOUND BOTH LT AND RT SUPPORT CRACKED IN RADIUS AT 7TH SCREW IB ATTACHMENT. BOTH ANGLES CRACKED IN IDENTICAL AREA. REMO VED AND REPLACED BOTH SUPPORT ANGLES. 1 G 7 1 3U 3 U O H2SW E1GL 2008011100142 20080111 00142 NM 2008 1 11 HNAA0800014 1 20071218 A 5210 85321986001 DOOR SEAL DHAV DHC8 DHC8102 2809003 NM PAX DOOR DIRTY A HNAA K NONE O OTHER UK UNKNOWN 1 EA 07 982HA 35045 35045 380 WITH ALL DOOR INDICATIONS NORMAL, DOOR SEAL WOULD NOT INFLATE. MAINTENANCE INSPECTED DOOR SEAL SUPPLY LINES AND PRESSUR IZING VALVE, NOTING NO DEFECTS. DOOR SEAL WAS CLEANED OF DIRT AND GRIME. DOOR SEAL AT THIS TIME INFLATED PROPERLY AND AIRCRAFT WAS CHECKED FOR PRESSURIZATION. SYSTEM CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008011100147 20080111 00147 EU 2008 1 11 Y2LA200700006 1 20071210 A 2120 UNKNOWN AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B1 13000 NE CABIN/COCKPIT ODOR A Y2LA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 07 522VA 2811 AFTER LANDING THE COCKPIT AND CABIN FILLED WITH SMOKE. PERFORMED GEN VISUAL INSPECTION OF OUTSIDE AND CABIN OF AIRCRAFT IAW AMM 05-51-00. RAN APU, ENGINES AND PACKS. FOUND NO EVIDENCE OF SMOKE, ODOR OR OTHER DEFECTS. OK TO CONTINUE. 2 L 7 2 4F 4 F RT A28NM 2008011100148 20080111 00148 EU 2008 1 11 Y2LA200700007 1 20071225 A 5330 SKIN AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE DENTED A Y2LA K NONE O OTHER IN INSP/MAINT 1 GL 07 551SX 1901 DENT ON LT SIDE OF AIRCRAFT, AFT OF L1 DOOR, ABOVE AOA VANE, JUST FORWARD OF SKIN LAP. STILL UNDER INVESTIGATION OF WHAT STATION DAMAGED OCCURRED. INSPECTED DENT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-11-11 AND 53-11-13. SIDEWALL PANELS R E-INSTALLED IAW 25-23-44 AND 25-23-43 IN PREPARATION FOR FERRY FLIGHT. AIRCRAFT WAS FERRIED TO BFM FOR REPAIRS AND THE R EPAIR WAS IAW SRM 53-00-11 FIG 203. 2 L 7 2 4F 4 F RT A28NM E37NE 2008010900381 20080109 00381 CE 2008 1 9 DXTA200702697 1 20071220 A 3040 99120856 CONTROLLER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE WINDSHIELD HEAT INOPERATIVE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 335QS 4007 5600335 WINDSHIELD OVERHEAT ANNUNCIATOR ILLUMINATED WITH WINDSHIELD HEAT SELECTED ON IN THE LOW POSITION. RAN CHECKLIST AND SELE CTED OFF. CONDITION OCCURED ABOUT 30 TO 60 SECONDS AFTER SELECTING ON. HOT BURNING ODOR WAS PRESENT.KSPI-KLAL. TROUBLESH OT PROBLEM DOWN TO A BLOWN FUSE INSIDE OF WINDSHIELD TEMP CONTROLLER. REMOVED CONTROLLER P/N 9912085-6 S/N 9AV134 AND IN STALLED NEW CONTROLLER PIN 9912085-6 S/N 8BC167 IAW CESSNA CITATION 560 AMM SECTION 30-41-02. OPS CHECK SATISFACTORY. 2 L 7 2 4F 4 F RT A22CE E25EA 2008010900382 20080109 00382 CE 2008 1 9 DXTA200702698 1 20071220 A 2170 WATER SEPARATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 695QS 5605293 NOXIOUS FUMES ENTER COCKPIT WHEN COCKPIT TEMPERATURE CONTROL IS RAISED TO HEAT COCKPIT. REMOVED & CLEANED WATER SEPARATO R. REINSTALLED WATER SEPARATOR IAW CESSNA 560XL MM CH 12-19-02. OPS & LEAK CHECK GOOD 2 L 7 2 4F 4 F RT A22CE E00059EN 2008010900383 20080109 00383 CE 2008 1 9 DXTA200702699 1 20071220 A 3260 ROLLER RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG DOOR MALFUNCTIONED E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 873QS 258573 AFTER T/O AND GEAR RETRACTION THE RT MAIN GEAR RED LIGHT STAYED ON. FOUND RT IB GEAR DOOR (MAIN) UPLOCK ROLLER TO BE OU T OF RIG. RIGGED DOOR IAW HAWKER 800XP MM 32-10-41. OPS CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A3EU E6WE 2008010900395 20080109 00395 2008 1 9 DXTA200702712 4 20071221 A 2210 6221019313 COMPUTER BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE FLT CONTROLS INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 117QS RK391 RUDDER BOOST FAIL LIGHT CAME ON AND YAW DAMPNER/AUTOPLOT KICKED OFF AT F230 LEVEL FLIGHT AT THE SAME TIME. REPLACED #1 FGC-4007 WITH OVH. UNIT IAW ROCKEWELL COLLINS MANUAL 523-0225807-0411A REV 9 OCT. 2005. GROUND OPS CHECK GOOD. 2 H 7 2 4F 4 F RT A16SW E25EA 2008011000001 20080110 00001 NM 2008 1 10 ASAA0852444 1 20071231 A 2131 71231997303 CONTROLLER BOEING 737 737890 1384527 NM CABIN PRESSURE DAMAGED A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 577AS 35186 DIGIT BURNED OUT ON PRESSURIZATION CONTROL PANEL "FLT ALT" WINDOW. REPLACED CABIN PRESSURE CONTROL MODULE. OP CHECKS N ORMAL. 2 L 7 2 4F RT A16WE 2008011000003 20080110 00003 EA 2008 1 10 TRAX200701967 1 20071220 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE SCRATCHED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 AAR - A SCRATCH IN SKIN AT FS 645 BETWEEN STR 2R & 3R (MARKED). BLENDED SCRATCH IN SKIN AT FS 645 BETWEEN STR 2R & 3R. BLENDED AREA IS .700 "LX .300" W X .003" D, FOUND TO BE IN LIMITS IAW CRJ 200 SRM 53-00-31. OK TO ALODINE AND PRIME. ALODINED AND PRIMED IAW CRJ 200 SRM 51-21-11. OK TO TOPCOAT. TOPCOATED IAW CRJ 200 SRM 51-21-16. SUPPLEMENTAL SDR CLO SED 1/2/08. 2 L 7 2 4F RT A21EA 2008011000021 20080110 00021 SO 2008 1 10 FFKA122 2 20071214 A 8520 IO550 CONNECTING ROD CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO ENGINE BROKEN B FFKA E B A ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING K E R FLUID LOSS VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 05 401NA 1057 402B0035 826261R PILOT REPORTED A LOSS OF POWER AND DECLARED AN EMERGENCY. MAINTENANCE INVESTIGATED THE LT ENGINE AND FOUND A HOLE IN TH E CASE HALF AT THE BASE OF THE NR 6 CYLINDER. THEY ALSO FOUND THE CONNECTING ROD IN 2 PIECES THE CONNECTING ROD CAP ALM OST FLATTENED AND BOTH CONNECTING ROD BOLTS SHEARED. BROKEN PIECES HAVE BEEN SENT FOR ANALYSIS. 1 L 7 2 3O 3 O A7CE E8CE 2008011000059 20080110 00059 EA 2008 1 10 COMA0760726 1 20071213 A 2760 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA E&E BAY MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 629BR 20463 7251 FLIGHT 5384 - ABORTED TAKEOFF BELOW 80 KTS FOR SPOILER CONFIG MESSAGE WITH POWER LEVERS ADVANCED. REMOVED AND REPLACED PSEU. 2 L 7 2 4F RT A21EA 2008011000071 20080110 00071 EA 2008 1 10 COMA0760736 1 20071219 A 2910 HYDRAULIC LINE CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYSTEM DEFECTIVE A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 964CA 7129 FLIGHT 5483 - RECEIVED HYD 2 LOW PRESSURE CAUTION MESSAGE, FOLLOWED BY ED2 CAUTION. ALL NR 2 FLUID LOST. LANDED IAD WI THOUT INCIDENT. REPLACED RIGHT ENGINE HYDRAULIC CROSSOVER LINE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011000072 20080110 00072 EA 2008 1 10 COMA0760737 1 20071219 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 712CA 23431 7244 DURING HMV-5 INSPECTION, FOUND CRACK AT LOWER END OF VERTICAL STIFFENER. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW BOMBA RDIER REO 601R-53-41-056. 2 L 7 2 4F RT A21EA 2008011000073 20080110 00073 EA 2008 1 10 COMA0760738 1 20071220 A 7931 6229820009 DCU CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAULTY A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 914CA 30271 7012 LOST LEFT ENGINE OIL PRESSURE INDICATION ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED NR 1 DCU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011000116 20080110 00116 NM 2008 1 10 USAA920080008 1 20071228 A 5743 6545324 FITTING BOEING 737 7373G7 1384595 NM RT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C16 CHECK - RIGHT WING AFT GEAR SUPPORT FITTING CRACKED, RSS 224.14. REPAIRED RIGHT WING AFT GEAR SUPPORT FITTING, RSS 224.14 IAW USAIRWAYS EA 100091. 2 L 7 2 4F RT A16WE 2008011100161 20080111 00161 CE 2008 1 11 13552N122707 1 20071226 A 5751 SKIN CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO AILERON DEBONDED E HYIA O OTHER O OTHER NR NOT REPORTED 1 NE 01 4652N 17623 57 402C0011 ON TAXI IN, CREW NOTICED DEBONDING HAD TAKEN PLACE ON RT AILERON UPPER IB SKIN. THE DISPLACEMENT OF SKIN DID NOT AFFECT THE FLIGHT CHARACTERISTICS OF THE AIRCRAFT AS NOTED BY THE CREW. MX REMOVED AND REPLACED AILERON, DISPENSED AILERON FOR REPAIR. 1 L 7 2 3O 3 O A7CE E8CE 2008011100164 20080111 00164 EU 2008 1 11 TRBA2007117 1 20071225 A 2913 4019501 PUMP AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE HYD SYSTEM FAILED A TRBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 414WF 414 AFTER GEAR UP SELECTION, DURING T/O, LOUD BANG HEARD AND UNLOCK INDICATION ON LT MLG. REMOVED AND REPLACED GREEN HYDRAU LIC PUMP. PERFORMED EXTENSION AND RETRACTION OF LANDING GEARS. OPS GOOD IAW JIC 29-10-00. 2 H 7 2 4T 4 T RT A53EU E20NE 2008011100166 20080111 00166 SO 2008 1 11 N93A25122007 1 20071225 A 3250 1159SCL50051 STEERING SYS GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE NLG FAILED E N93A O OTHER J WARNING INDICATION LD LANDING 1 SO 13 502QS 601 DURING GEAR EXTENSION, STEER BY WIRE FAIL MESSAGE ILLUMINATED. NO STEERING ON LANDING. 2 L 7 2 4F 4 F RT A12EA E00057EN 2008011100167 20080111 00167 CE 2008 1 11 12262007 1 20071226 A 2497 700088001 CIRCUIT BREAKER LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP DEFECTIVE E KC8A A UNSCHED LANDING H ELECT. POWER LOSS-50 PC DE DESCENT 1 GL 23 73CK 1376 092 LOSS OF ESSENTIAL BUSS POWER. CAPTAINS ESSENTIAL BUSS CIRCUIT BREAKER POPPED. CO-PILOTS ESSENTIAL BUSS CIRCUIT BREAKER P OPPED WHILE SUPPLYING THE CAPTAINS ESSENTIAL BUSS THROUGH THE BUSS TIE. THE AIRCRAFT LOST COMM, AND NAV. FOUND THE CAPT AINS ESSENTIAL BUSS CIRCUIT BREAKER TO BE WEAK AND REPAIRED WIRING BEHIND THE CAPTAINS ARM REST. PERFORMED ELECTRICAL LO AD CHECK OF THE ESSENTIAL BUSSES AND FOUND TO BE WELL WITHIN LIMITS. ALL WORK PERFORMED IAW THE MM. 2 L 7 2 4F 4 F A10CE E6WE 2008011100220 20080111 00220 EA 2008 1 11 N6WA0071201 1 20071227 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE CABIN INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 152GJ 10218 CEILING LEVEL EMERGENCY LIGHT INOP AT ROW 14. DEFERRED LIGHT IAW MEL-33-51-01-2A. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008011100221 20080111 00221 CE 2008 1 11 DJFA2007150 1 20071226 A 2120 UNKNOWN BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE CABIN ODOR E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 783TA RK234 IN CRUISE, CREW NOTED BURNING ODOR FROM HEAT DUCTS. MAINTENANCE TESTED THE ENVIRONMENTAL SYSTEM BUT WAS UNABLE TO DUPLI CATE THE DISCREPANCY. 2 H 7 2 4F 4 F RT A16SW E25EA 2008011100223 20080111 00223 CE 2008 1 11 CIEA200700011 1 20071227 A 7500 67469 GASKET LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP BLEED LINE FAILED E CIEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 03 717EB 1243 016 DURING CRUISE FLIGHT THE RT ENGINE FIRE WARNING CAME ON. THE FLIGHT CREW REDUCE THE ENGINE POWER AND THE LIGHT WENT OUT AND REMAINED OUT UNTIL LANDING. DURING MAINTENANCE INSPECTION, THE RT ENGINE BLEED AIR LINE GASKET IN THE PYLON WAS FO UND TO BE DEFECTIVE AND ALLOWING HOT BLEED AIR TO SET OFF THE FIRE WARNING SYSTEM. THE GASKET WAS REPLACED AND THE AIRC RAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F A10CE E6WE 2008011100225 20080111 00225 EU 2008 1 11 TRBA2007119 1 20071229 A 3350 3011210 BULB AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE EMERGENCY LIGHTS FAILED A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 408AT 408 EMERGENCY DOOR STAIRLIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT BULB. 2 H 7 2 4T 4 T RT A53EU E20NE 2008011100226 20080111 00226 WP 2008 1 11 ANCF200700034 1 20071228 A 3397 WIRE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LIGHT BURNED W ANCF B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 23 160BS 53463 DURING CRUISE STRONG BURNING ODOR IN COCKPIT DUE TO PREVIOUS REPORTS ON RT PACK THE PACK WAS TURNED OFF AND THE ODOR DIS SIPATED. THE ODOR WAS IN COCKPIT. IAW WDM AND AMM 33-22-07/525 AND 20-50-01 /201 IN LT UPPER SIDE WALL LIGHTING TRANSFO RMER LINE IL 1701F18 WAS FOUND SPLICE BURNED. THE SPLICE WAS REPLACED AND CHECKED DURING SEVERAL TIMES. 2 L 7 2 4F 4 F RT A6WE E9NE 2008011100228 20080111 00228 CE 2008 1 11 DJFA2007151 1 20071228 A 2140 VALVE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP HEAT SMOKE E DJFA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 830LX 258483 IN CRUISE CREW REPORTED SMOKE FILLED THE COCKPIT WITH A BURNING ODOR WHEN THE HEAT VALVE WAS OPENED. SMOKE CLEARED WHEN THE VALVE WAS CLOSED AND THE DUMP PARTIALLY OPENED. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. 2 L 7 2 4F 4 F RT A3EU E6WE 2008011100236 20080111 00236 CE 2008 1 11 JEMA010208001 1 20071201 A 5610 45AS31010022 WINDOW BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE COPILOT SIDE CRACKED E JEMA K NONE O OTHER IN INSP/MAINT 1 CE 01 48MF RK218 WHILE PERFORMING A SCHEDULED A-B INSPECTION FOUND NR 2 (CO-PILOT) SIDE WINDOW CRACKED USING THE PRISM INSPECTION METHOD. THE (D) INSPECTION IS THE ONLY INSPECTION THAT REQUIRES THAT BOTH WINDSHIELDS BE INSPECTED BY REMOVING THE WINDSHIELD RETAINERS OR USING OPTICAL PRISM INSPECTION METHOD. THERE IS NO STATEMENT IN THE AIRCRAFT MAINTENANCE MANUAL OR IN THE A-D INSPECTION CHECKLIST THAT REQUIRES YOU TO INSPECT THE COCKPIT SIDE WINDOWS IN THE SAME MANNER AS THE WINDSHIELDS. A LL OF THE WINDOWS IN THE COCKPIT AREA ARE INSTALLED OR FASTENED IN THE SAME MANNER AS THE WINDSHIELDS. IT IS SUSPECTED THAT THE COPILOT WINDOW CRACKED FROM FATIGUE, OR TT INSTALLED. WOULD RECOMMEND THAT INSP OF ALL COCKPIT WINDOWS WITH A 2 H 7 2 4F 4 F RT A16SW E25EA 2008011100237 20080111 00237 CE 2008 1 11 JEMA010208002 1 20071201 A 5312 45A3940111 BULKHEAD BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE FUSELAGE CRACKED E JEMA K NONE O OTHER IN INSP/MAINT 1 CE 01 48MF RK218 WHILE PERFORMING A SCHEDULED A-B INSPECTION, FOUND RT AND LT AFT FUSELAGE BLEED AIR LINE ATTACH BRACKETS PULLED FROM AFT FUSELAGE BULKHEAD RESULTING IN CRACKS IN THE BULKHEADS AT FRAME STATION 329.92. THIS IS THE 4TH AIRCRAFT IN A ROW THAT THE BULKHEAD HAS BEEN CRACKED. THE CRACK HAS BEEN FOUND ON BOTH SIDES OF THE AIRCRAFT. (K) 2 H 7 2 4F 4 F RT A16SW E25EA 2008011100264 20080111 00264 NE 2008 1 11 HSYA20071201 2 20071203 A 7200 ENGINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE LEFT READS HIGH E HSYA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 NM 05 101UE 17149 5829 UC101 PCE32151 DURING CRUISE, THE CREW REPORTED THAT THE LT ENGINE INDICATED ABNORMALLY HIGH ITT. THE CREW ELECTED TO RETURN DEPARTURE AND LANDED WITH OUT INCIDENT. MX PERFORMED A LT ENGINE ITT THERMOCOUPLE LOOP RESISTANCE CHECK AND ADJUSTED. MX ALSO PE RFORMED AND ITT CALIBRATION CHECK AND WAS FOUND TO BE SATISFACTORY. PERFORMED ENGINE TORQUE INDICATION CALIBRATION CHECK AND WAS FOUND TO BE SATISFACTORY. PERFORMED ENGINE TRIM THERMOCOUPLE TEST AND WAS FOUND TO BE WITHIN LIMITS. MX PERFOR MED LT AND RT ENGINE RIGGING AND ADJUSTMENTS AND PERFORMED AN ENGINE ROCOVERY WASH AND GROUND PERFORMANCE RUN UP AND FOU ND THE ENGINE PARAMETERS TO BE WITH IN LIMITS AT THIS TIME. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 T RT A24CE E4EA 2008011100267 20080111 00267 EA 2008 1 11 MASA200700687 1 20071012 A 3350 8GH00247308 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17275 7275 ASH FLT 2818 DSM - OVERNIGHT - RT NR 2 EXTERIOR EMERGENCY LIGHT INOP. MX REPLACED THE LAMP, OP CHECK GOOD. 2 L 7 2 4F RT A21EA 2008011100268 20080111 00268 EA 2008 1 11 MASA200700689 1 20071012 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37178 7178 ASH FLT 2783 - PHX - EMERGENCY FLOOR LIGHT ROW 2 INOP. MX RESECURED CONNECTION. 2 L 7 2 4F RT A21EA 2008011100269 20080111 00269 NM 2008 1 11 NWAA074365520 1 20071230 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 520US 23208 DURING OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTS FROM ROW 14 TO 23 INOP. MAINTENANCE REMOVED AND REPLACED POWER SUP PLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2008011100273 20080111 00273 NM 2008 1 11 MASA200700647 1 20070926 A 2560 P487220187220021 BATTERY DHAV DHC8 DHC8202 2809007 NM FLASHLIGHT DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 989HA 427 ASH FLT 2859 PHX-FLG - FA FLASHLIGHT INOP. MX REPLACED THE FLASHLIGHT BATTERY, OPS CK GOOD. 2 H 7 2 4T RT A13NM 2008011100282 20080111 00282 EA 2008 1 11 HSYA20071102 2 20071129 A 7320 3244773542 FCU STBROS SD3 SD330 8100602 EU PWA PT6 PT6* 52043 EA ZONE 400 INOPERATIVE E HSYA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 NM 05 331SB 3544 SH3015 PCE84023 DURING CLIMB OUT THE CREW REPORTED THE LT ENGINE LOST POWER. THE LT ENGINE PROP RPM DROPPED TO 1200 AND THE BLUE FINE PI TCH LIGHT BEGAN FLASHING ALONG WITH A DROP IN TORQUE. THE CREW ELECTED TO RETURN TO DEPARTURE AND LANDED WITH OUT INCIDE NT. MX FOUND THE LT ENGINE FCU TO BE INOPERATIVE AND A LOOSE (B)-NUT ON THE PY LINE TO THE FCU. MX REMOVED AND REPLACE D THE FCU AND RESECURED THE PY LINE. GROUND RUN OPERATIONAL CHECKS SATISFACTORY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T 3 T A41EU E2NE 2008011100288 20080111 00288 NM 2008 1 11 DLM90071644 1 20071221 A 5320 9930538U11 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 LT CABIN CUSP WEB CORRODED ENTIRE LENGTH FS 503-579. REMOVED AND REPLACED WEB IAW MD-90 SRM 51-30-01, 51-30-02 AND 51-3 0-05 ON N/R 2700-0139 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2008011100289 20080111 00289 NM 2008 1 11 DLM90071645 1 20071220 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 LT CUSP WEB CRACKED AT STA 870. REPAIRED CUSP WEB IAW MD-88 DRD 53-05D FIG 828 ON N/R 2400-0185 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2008011100291 20080111 00291 NM 2008 1 11 DLM88071648 1 20071221 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 922DL 49646 FUSELAGE SKIN FOUND WITH CORROSION AT STA 620 BETWEEN L-29L AND L-29R. CUTOUT DAMAGED SKIN AND INSTALLED A DOUBLER. 2 L 7 2 4F RT A6WE 2008011100293 20080111 00293 NM 2008 1 11 DL76L071650 1 20071221 A 5320 AND101342009 FLOOR SUPPORT BOEING 767 767332 1382001 NM FUSELAGE CRACKED A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 171DN 24759 CABIN: STATION 927 TO BS 999 FLOOR SUPPORT CRACKED. REPAIRED ON NR511301 AT HMV3/PSV22 PER 53-00-51 REPAIR 3 FIGURE 201 . 2 L 7 2 4F RT A1NM 2008011100295 20080111 00295 NM 2008 1 11 DL76L071651 1 20071221 A 5315 BAC1505101498 FLOORBEAM BOEING 767 767332 1382001 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 171DN 24759 CABIN: STATION 1480 RBL 36 TO 42 FLOORBEAM UPPER CHORD FOUND CORRODED. REPAIRED ON NR515625 AT HMV3/PSV22 PER SRM 53-00 -51D FIG 201. 2 L 7 2 4F RT A1NM 2008011100298 20080111 00298 NM 2008 1 11 DL757071653 1 20071223 A 2510 POWER CABLE BOEING 757 757232 1384965 NM COCKPIT FRAYED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 662DN 24991 F/O SEAT ELECTRICAL ARC AND SEAT UNPOWERED. PWR CORD FRAYED. REMOVED CORD. FWD TO MCO/PLAC MEL 25.11.01A. REPLACED P WR CORD ON F/O SEATS CKS GOOD MCO/PLAC REMOVED. 2 L 7 2 4F RT A2NM 2008011100301 20080111 00301 NM 2008 1 11 DLM88071658 1 20071226 A 3231 BEARING DOUG MD88 MD88 3023688 NM RT MLG DOOR MISSING A DALA L ABORTED APPROACH D INFLIGHT SEPARATION AP APPROACH 1 SO 27 988DL 53339 GEAR DOOR UNSAFE LIGHT ON AFTER EXTENSION. AFTER GO AROUND GEAR WAS RETRACTED AND EXTENDED MANUALLY. A/C LANDED WITH G EAR DOORS OPEN. DOOR BUMPERS WERE GROUND DOWN WITH NO DAMAGE TO THE DOORS. FOUND RT MLG DOOR ROLLER MISSING. 2 L 7 2 4F RT A6WE 2008011100303 20080111 00303 NM 2008 1 11 DL76S071659 1 20071226 A 5711 112T20063 SPAR BOEING 767 767332 1382001 NM LT WING GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 128DL 24078 LT WING FRONT SPAR WEB DENTED/GOUGED. CUTOUT DAMAGE AND INSTALLED A REPAIR DOUBLER. 2 L 7 2 4F RT A1NM 2008011100304 20080111 00304 NM 2008 1 11 ASMF200712006 1 20071229 A 2760 429352 CONTROL UNIT BOEING 737 737* NM CFMINT CFM567 CFM567B22 13802 NE SPEED BRAKES DAMAGED W ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 908AM 9777 9777 30038 AIRCRAFT REJECTED TAKEOFF DUE TO DURING TAKEOFF RUN, THE SPEED BRAKE DO NOT ARM LIGHT TURNED ON. MAINTENANCE PERSONNEL REPLACED THE S651 SPEED BRAKE, TAKEOFF WARNING SWITCH IAW MM 31-51-03 AND THE ANTI SKID/AUTO BRAKE CONTROL UNIT IAW MM 3 2-42-21, TESTED CORRECT IAW MM 32-42-00. ADDITIONALLY, FIM PROCEDURE 27-62 TASK 802 WAS PERFORMED, TESTED CORRECT. THE H IGH ENERGY STOP INSPECTION WAS NOT NECESSARY IAW MM 05-51-07, DUE TO THE AIRCRAFT STOPPED AT 90 KNOTS AND 56500 KG. 2 L 7 2 4F 4 F RT A16WE E00055EN 2008011100308 20080111 00308 NM 2008 1 11 DL76L071662 1 20071228 A 5330 2024T300711N SKIN BOEING 767 767332 1382001 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 171DN 24759 REPAIR AT STA 1418 AND BETWEEN STR L38.8-39.5, 9/22/02 EXHIBITS DAMAGED SKIN BETWEEN STA 1418-1439 AND STR 37R TO 37L. REPAIRED PER SRM 53-00-01. 2 L 7 2 4F RT A1NM 2008011100312 20080111 00312 EU 2008 1 11 TRBA2007120 1 20071230 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE EMERGENCY LIGHTS FAILED A TRBA O OTHER O OTHER CR CRUISE 1 SO 29 355AT 355 IN CRUISE THE AFT GALLEY EMERGENCY LIGHTS CAME ON BY THEMSELVES; TRIED RESETING EMERGENCY LIGHT SWITCH IN COCKPIT AND CA BIN BUT THE LIGHTS STAYED ON. REMOVED AND REPLACE BATTERY PACK FIN NR 62WL IAW JIC NR 33-51-21. 2 H 7 2 4T 4 T RT A53EU E20NE 2008011100314 20080111 00314 NM 2008 1 11 DL76L071669 1 20071231 A 5330 146T32621 SKIN BOEING 767 767332 1382001 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 182DN 25987 CORROSION AND CRACKING OF SKIN AT FS 1219, S-37L. DAMAGE WAS CUT OUT AND REPAIR PARTS WERE INSTALLED. 2 L 7 2 4F RT A1NM 2008011100316 20080111 00316 EU 2008 1 11 NSVA20070070 1 20070320 A 2611 CGAB20101 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A NSVA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 121CQ 121 CARGO SMOKE LIGHT ILLUMINATED. REMOVED AND REPLACED CARGO SMOKE DET IAW AMM 26-13-15, OP'S CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011100317 20080111 00317 EU 2008 1 11 NSVA20070109 1 20070423 A 6120 980871103P0620 SENSOR SAAB SF340 340B 7860101 EU RT ENGINE MALFUNCTIONED A NSVA O OTHER N FALSE WARNING AP APPROACH 1 EA 27 204CJ 204 AUTOCOARSEN LIGHT ILLUMINATED ON FINAL AT 40 PERCENT TQ. REMOVED AND REPLACED P3 SENSOR ON THE RT ENG PART OFF PN 98087 -1103P-0620 SN 0620 PART ON PN 1103P0620 DN 2052 DONE IAW 61-22-10-02. OPS CHECK GOOD 61-22-00-05-2. 2 L 7 2 4T RT A52EU 2008011100322 20080111 00322 EU 2008 1 11 NSVA20070053 1 20070307 A 2612 005WS00 WEU SAAB SF340 340B 7860101 EU MALFUNCTIONED A NSVA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 196CJ 196 TAIL PIPE HOT LIGHT ILLUMINATED IN FLIGHT, CHECK LIST FOLLOWED, LIGHT DID NOT EXTINGUISH, ALL EMERGENCY AND ABNORMAL CHE CK LIST WERE FOLLOWED ENGINE SHUTDOWN. REMOVED AND REPLACED WARNING ELECTRONIC UNIT (WEU) IAW 31-50-00 PN ON/OFF 005WS0 0, SN ON 1251 SN OFF 1376. 2 L 7 2 4T RT A52EU 2008011100323 20080111 00323 EU 2008 1 11 NSVA20070054 1 20070303 A 2612 472326 FIRE LOOP SAAB SF340 340B 7860101 EU RT ENGINE DAMAGED A NSVA O OTHER O OTHER CR CRUISE 1 EA 27 251CJ 251 RIGHT FIRE DETECT FAIL ILLUMINATED INTERMITTENTLY IN FLIGHT. FOUND RT ENG FIRE DETECTION AFT SENSOR LOOP DAMAGED. REMO VED RT AFT SENSOR LOOP IAW SAAB AMM CH 26-11-05 PN: 472326, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011100324 20080111 00324 EU 2008 1 11 NSVA20070084 1 20070405 A 2120 UNKNOWN SAAB SF340 340B 7860101 EU CABIN ODOR A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 198CJ 198 IN FLIGHT F/A SMELLED SMOKE AROUND GALLEY TURNED OFF HOT JUGS AND GALLEY LIGHT. INSPECTED HOT JUGS, WIRING AND LIGHTING . DIDN'T SMELL SMOKE. OP'S CHECK GOOD IAW AMM 25-32-01. 2 L 7 2 4T RT A52EU 2008011400013 20080114 00013 EU 2008 1 14 COEA0754821 1 20070904 A 5320 FLOOR SUPPORT AEROSP ATR72 ATR72202 8680940 EU FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK, LEVEL 2 CORROSION, CABIN FLOOR SUPPORT STRUCTURES CORRODED. FLOOR SUPPORT CHANNEL BETWEEN FLO ORBEAM 38 AND 39L. FLOOR SUPPORT ZEE BETWEEN FRAME 39 AND 40L. FLOOR SUPPORT ZEE BETWEEN FRAME 39 AND 41R. REMOVED AN D REPLACED FLOOR SUPPORT STRUCTURES. CHANNEL P/N S5367800826801, ZEE LT P/N S5367800820002, ZEE RT P/N S5367800821602. (M) 2 H 7 2 4T RT A53EU 2008011400020 20080114 00020 NM 2008 1 14 AMTA200800002 1 20071231 A 3397 WIRE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHTS DISCONNECTED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 520AT 27976 EGRESS TRACK LIGHTING WIRES EXPOSED NR 2L FLOOR. RESECURED EMERGENCY LIGHTING WIRES AT 2L FLOOR. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008011400021 20080114 00021 NM 2008 1 14 AMTA200800001 1 20071228 A 3350 LIGHT BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE CABIN INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 518AT 27974 FLOOR PATH EXIT MARKER AT R-3 DOOR INOPERATIVE. RECONNECTED LIGHT ASSY, OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008011400024 20080114 00024 2008 1 14 DXTA200702619 4 20071119 A 2297 CONNECTOR RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP AUTOPILOT DAMAGED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 836QS 258436 DURING CRUISE AT F300, AIRCRAFT PITCHED UP ABOUT 15 DEGREES AND AUTOPILOT KICKED OFF. RESEATED PIN (C) OF CONNECTOR GND 28 SYSTEM GROUND CHECKS GOOD IAW DWG NR A8-43-100 REV. F AND AMM 34-22-05. REF 19-1415 SQK 1.5 2 L 7 2 4F 4 F RT A3EU E6WE 2008011400029 20080114 00029 SO 2008 1 14 WVBA121807001 1 20071218 A 8011 ERB8011 STARTER PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2A GL LT ENGINE UNSERVICEABLE E WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 4434D 290 290 317552020 L755761A DJ10390A INSTALLED NEW E-DRIVE STARTER ON THE LT SIDE. HAD MULTIPLE DISCREPANCIES WHERE PILOT NOTED THAT THE STARTER WOULD NOT E NGAGE THE SLIP RING. WHEN A MECHANIC WOULD INVESTIGATE THEY COULD NOT DUPLICATE THE PROBLEM. DURING A DETAILED INSPECT ION IT WAS NOTED THAT THE LT ENGINE RING GEAR ON THE SLIP RING WAS SIGNIFICANTLY DAMAGED - RING WAS REPLACED AND WE ATTE MPTED TO CONTINUE TO USE THE STARTER BUT EVENTUALLY HAD TO REPLACE THE PART AS IT DOESN’T SEEM TO MATE CORRECTLY WITH TH E GEAR. THE STARTER ITSELF STILL FUNCTIONS STRONGLY - HOWEVER IT SEEMS THE TEETH OF THE STARTER AND RING GEAR DO NOT LI NE UP OR MESH CORRECTLY. IN LOOKING AT DOCUMENTATION - WE HAVE CONFIRMED THAT WE ARE USING THE CORRECT PITCH (12/14)RIN 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2008011400033 20080114 00033 CE 2008 1 14 GUUA12190703 1 20071219 A 5524 1016200131 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 69547 24915 UE189 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT ELEVATOR CENTER HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR CENTE R HINGE BRACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 2008011400035 20080114 00035 CE 2008 1 14 GUUA12190701 1 20071219 A 5524 1016200131 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 69547 24915 UE189 REPORT: DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT ELEVATOR CENTER HINGE BRACKET EXFOLIATED. REPLACED LT ELEVAT OR CENTER HINGE BRACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 2008011400037 20080114 00037 CE 2008 1 14 GUUA12200701 1 20071220 A 5220 12943004519 DOOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA EMERGENCY EXIT INOPERATIVE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87552 UE216 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT EMERGENCY EXIT DOOR WILL NOT OPEN. ADJUSTED LT EMERGENCY EXIT DOOR. 2 L 7 2 4T 3 T RT A24CE E2NE 2008011400053 20080114 00053 SW 2008 1 14 AC2A118586 1 20071022 A 6420 BEARING BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL TAIL ROTOR WORN B AC2A O OTHER O OTHER NR NOT REPORTED 1 SW 31 17238 1146 CS13921 51492 TAIL ROTOR HAS WORN FEATHERING BEARINGS. 1 G 7 1 3U 3 U H2SW E1GL 2008011400054 20080114 00054 SW 2008 1 14 AC2A118583 1 20071220 A 3212 D24974115 FLOAT BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL MLG LEAKING E AC2A K NONE L NO TEST IN INSP/MAINT 1 SW 31 6533U 52439 LEAKED DURING 6 MONTH INSPECTION. 1 G 7 1 3U 3 U H2SW E1GL 2008011000082 20080110 00082 NE 2008 1 10 HNAA0800006 2 20071217 A 7261 3014397 GARLOCK SEAL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE CUT A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 814EX 46946 3376 318 120372 ON TAKEOFF ROLL, ONE ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED AT 80% TI 90% AND EXTINGUISHED AFTER REDUCING POWER. INSPECTED NR 2 ENGINE AND SERVICED WITH THREE QUARTS OF OIL. GROUND RAN AIRCRAFT, NO LEAKS NOTED. FOLLOWED UP NR 2 EN GINE OIL CONSUMPTION HIGHER THAN NORMAL. FOUND NR 2 STARTER GENERATOR GARLOCK SEAL LEAKING, REPLACED GARLOCK SEAL, LEAK CHECK GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2008011000111 20080110 00111 NM 2008 1 10 USAA920080003 1 20071217 A 5340 69353521 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C16 CHECK - CRACKED STRINGER CLIP, BS 727D, S21R. REPLACED STRINGER CLIP, BS 727D, S21R IAW B737 S RM 51-40-02. 2 L 7 2 4F RT A16WE 2008011000127 20080110 00127 NM 2008 1 10 USAA920080056 1 20071217 A 5230 6547932524A SKIN BOEING 737 7373G7 1384595 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - AFT CARGO DOOR SKIN CRACKED. REPAIRED AFT CARGO DOOR SKIN IAW B737 SRM 52-00-21. 2 L 7 2 4F RT A16WE 2008011500001 20080115 00001 EU 2008 1 15 2007UALA05313 1 20071227 A 3510 REGULATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE OXYGEN MASK FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 464UA 1290 SECOND OBSERVER'S O2 MASK DOES NOT TEST AND STOWAGE BOX ASSY IS MISSING PARTS. FAULTY REGULATOR. REPLACED O2 MASK BOX. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011500003 20080115 00003 CE 2008 1 15 NSVA20070192 1 20070720 A 2750 FLAP SYSTEM BEECH 1900 1900D 1154162 CE TE FLAPS MALFUNCTIONED A NSVA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 27 155CJ UE55 FLAP INOP, WHEN FLAPS WERE SELECTED 35* THEY DID NOT RESPOND. FLAP DID COME UP, HOWEVER THEY DID NOT RESPOND THEREAFTER . RESET C/B PERFORMED OPERATIONAL TEST OF FLAP SYSTEM, IAW BEECH MANUAL 27-00-00, NO FAULTS FOUND. 2 L 7 2 4T RT A24CE 2008011500007 20080115 00007 EU 2008 1 15 NSVA2007170 1 20070630 A 7400 6071T20P16 COMPUTER SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE FAULTED A NSVA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 9CJ 340B224 RETURN TO GATE DUE TO IGNITION LIGHT LT, DURING TAXI, BEFORE TAKEOFF. REMOVED AND REPLACED LT DECU. OPS CK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011500010 20080115 00010 EU 2008 1 15 2007UALA05329 1 20071228 A 2751 D2787002000061 SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE T/E FLAP FAULTY A UALA O OTHER W INADEQUATE Q C AP APPROACH 1 WP 29 472UA 1435 UPPER ECAM F-CTL SLATS LOCKED WING TIP BRK ON DURING 4 MILE FINAL. FPPU FAULTY (FEEDBACK POSITION PICK-OFF UNIT). RANG ALL ASSOCIATED WIRING FROM SFCC1 & SFCC2 TO FPPU 28CV. SWAPPED CONNECTORS ON FPPU 28CV AND IPPU 4CN, WAS ABLE TO RESET WTB AND RUN FLAPS-SLATS, HOWEVER FLAP INDICATION SHOWED IN POSITION AT ANY SETTING AND FLAPS CONTINUED TO RUN INDICATIN G FPPU WAS FAULTY. REPLACED FPPU 28CV, ALL OPS NORMAL AFTER, PERFORMED CAT 3 TEST. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011500012 20080115 00012 NM 2008 1 15 2007UALA05333 1 20071228 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY LIGHT AT 37 ABC INOP. REPLACED WITH NEW LIGHT ASSY. OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011500032 20080115 00032 EU 2008 1 15 NSVA20070048 1 20070226 A 6123 COMPUTER SAAB SF340 340B 7860101 EU AUTOCOARSEN SYS MALFUNCTIONED A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 339CJ 085 339 DURING TAKEOFF ROLL AUTOCOARSEN ILLUMINATED 40 KNOTS, PERFORMED REJECTED TAKEOFF, NO BRAKING REQUIRED. REMOVED AND REPL ACED AUTOCOARSEN COMPUTER IAW SAAM 61-22-00 P/N ON 9302979-04 P/N OFF9302979-001 SN ON 174, SN OFF 085. 2 L 7 2 4T RT A52EU 2008011500037 20080115 00037 SO 2008 1 15 C2XAO8RI007 1 20071226 A 2421 30086011 GENERATOR EMB 145 EMB145ER 3260211 SO NR 1 INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14943 11937 290 145040 FLT 3142 - EWR - CREW REPORTED APU GENERATOR AND GENERATOR NR 1 OFF BUSS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNE VENTFULLY. EWR MX REMOVED AND REPLACED APU GCU AND GENERATOR NR 1 AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008011500038 20080115 00038 SO 2008 1 15 C2XA08RI008 1 20071225 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO LANDING GEAR INOPERATIVE A C2XA B EMER. DESCENT O OTHER LD LANDING 1 SW 27 14904 145477 FLT 2868 - EWR - CREW REPORTED A LOUD NOISE FROM NOSE WHEEL AREA AFTER LANDING GEAR EXTENSION. NORMAL DOWN AND LOCKED I NDICATION. NO MESSAGES ON EICAS. ALTHOUGH ALL INDICATIONS WERE NORMAL, CREW PROCEEDED WITH EMERGENCY DESCENT. ACFT LA NDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED DOWNLOCK PROXIMITY SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008011500040 20080115 00040 EU 2008 1 15 NSVA20070143 1 20070531 A 7797 CONNECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ENGINE DIRTY A NSVA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 350CJ 350 NO TORQUE INDICATION ON LT SIDE DURING TAKEOFF ROLL. CLEANED LT ENG YELLOW ENGINE HARNESS CONNECTORS. OPS CHECK GOOD I AW GE MM 74-00-00. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011500053 20080115 00053 EU 2008 1 15 NSVA20070177 1 20070706 A 2720 8618M16 ACTUATOR SAAB SF340 340B 7860101 EU RUDDER LIMITER MALFUNCTIONED A NSVA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 242CJ 242 RUDDER LIMIT LIGHT ILLUMINATED ON GROUND WHEN GUST LOCK RELEASED, NO RUDDER TRAVEL AVAILABLE. REMOVED AND REPLACED RUDD ER LIMITER ACTUATOR P/N ON 8618M16 SN ON 008028A SN OFF 08009A IAW MM 27-21-53, OPS CHK GOOD. 2 L 7 2 4T RT A52EU 2008011500054 20080115 00054 NE 2008 1 15 NSVA20070141 2 20070529 A 7261 OIL SYSTEM SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE UNDERSERVICED A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 277MJ 277 RIGHT ENGINE OIL PRESSURE LIGHT ILLUMINATED, ABORTED TAKEOFF. SERVICED ENG OIL IAW 12-10-79. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011500055 20080115 00055 CE 2008 1 15 NSVA20070181 1 20070709 A 5230 HANDLE BEECH 1900 1900D 1154162 CE CARGO DOOR LACK OF LUBE A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 124CJ UE24 JUST AFTER BRAKE RELEASE, CARGO DOOR LIGHT ILLUMINATED. LUBED DOOR HANDLE, OP CHECKS GOOD. 2 L 7 2 4T RT A24CE 2008011500056 20080115 00056 EU 2008 1 15 NSVA20070086 1 20070404 A 6123 MS25308232 SWITCH SAAB SF340 340B 7860101 EU AUTOCOARSEN MALFUNCTIONED A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 184CJ 184 AUTO COARSENING LOW LIGHT ILLUMINATES INTERMITTENTLY. DURING OPS CHECK OF AUTO COARSEN SYSTEM IAW AMM 61-22-00-05-2 FOU ND FAULTY AUTO COARSEN SWITCH. SWITCH IS AOG WRITE UP REMAINS OPEN. REMOVED AND REPLACED AUTOCOARSEN SWITCH ON OVERHEA D PANEL IAW AMM 20-10-00. OPS CHK OK, P/N ON AND OFF MS25308-232. 2 L 7 2 4T RT A52EU 2008011500062 20080115 00062 WP 2008 1 15 UPS08851360 1 20071227 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 FWD ACCESSORY COMPT AT L25R INTERCOSTAL HAS 2EA CRACKS AT FASTENER HOLES. REMOVED INTERCOSTAL AT L25 R FWD ACCESSORY BAY IAW SRM 51-01-21, FABRICATED AND INSTALLED REPAIR INTERCOSTAL AT L25R FWD ACCESSORY BAY IAW DWG 5703 478, AND SRM 51-01-21. 2 L 7 4 4F RT 4A25 2008011500068 20080115 00068 2008 1 15 NSVA20070098 4 20070414 A 2210 SWITCH SAAB SF340 340B 7860101 EU YAW DAMPER LACK OF LUBE A NSVA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 171CJ UE71 YAW DAMPER BUTTON STUCK IN ENGAGED POSITION. LUBED AND FREED STUCK SWITCH, SYSTEM OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2008011500071 20080115 00071 EU 2008 1 15 NSVA20070076 1 20070327 A 7603 531706 THROTTLE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LOOSE A NSVA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 27 347CJ 347 FLIGHT IDLE STOP HAS EXCESSIVE UP AND DOWN SLACK AND FLIGHT IDLE LIGHT ON STATUS PANEL IS ON. REMOVED AND REPLACED THRO TTLE QUADRANT IAW SAAB AMM 76-10-05-04 PN 53170-6 SN ON 252 SN OFF 029, OPS CHK IS REQUIRED. OPS CHK IAW 76-10-05. OPS CHK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011500075 20080115 00075 EU 2008 1 15 NSVA20070090 1 20070410 A 6123 CONNECTOR SAAB SF340 340B 7860101 EU AUTOCOARSEN DIRTY A NSVA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 184CJ 184 AUTO COARSEN LOW LIGHT FLICKERING ON AND OFF. CLEANED AND RECONNECTED CONNECTORS ON AUTO COARSEN COMPUTER, OPS CHECK GO OD IAW AMM 61-22-0-05-2. 2 L 7 2 4T RT A52EU 2008011500078 20080115 00078 NM 2008 1 15 USAA920080067 1 20071202 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED INTERCOSTAL OUTER CHORD ANGLE, BS 291, WL 249. REPLACED INTERCOSTAL OUTER CHOR D ANGLE, BS 291, WL 249 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008011500079 20080115 00079 NM 2008 1 15 USAA920080068 1 20071224 A 5320 6545807433 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED INTERCOSTAL OUTER CHORD ANGLE, BS 291, S10R, WL 253. REPLACED INTERCOSTAL OUTE R CHORD ANGLE, BS 291, S10R, WL 253 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008011500081 20080115 00081 NM 2008 1 15 USAA920080070 1 20071130 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 663, S3R. REPAIRED FRAME, BS 663, S3R IAW USAIRWAYS EA 100069. 2 L 7 2 4F RT A16WE 2008011500083 20080115 00083 NM 2008 1 15 USAA920080072 1 20071205 A 5320 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED VERTICAL BEAM WEB, BS 180, LBL 17, WL 228. REPAIRED VERTICAL BEAM WEB, BS 180, LBL 17, WL 228 IAW B737 SRM 51-70-13. 2 L 7 2 4F RT A16WE 2008011500085 20080115 00085 NM 2008 1 15 USAA920080074 1 20071221 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 492, S21R. REPAIRED FRAME, BS 492, S21R IAW USAIRWAYS EA 100079. 2 L 7 2 4F RT A16WE 2008011500086 20080115 00086 NM 2008 1 15 USAA920080075 1 20071128 A 5330 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FUSELAGE SKIN, BS 375, S10L. REPAIRED FUSELAGE SKIN, BS 375, S10L IAW USAIRWAY S EA 100110. 2 L 7 2 4F RT A16WE 2008011500087 20080115 00087 EU 2008 1 15 NSVA20070111 1 20070423 A 2710 7227151621 CENTERING MECH SAAB SF340 340B 7860101 EU LT AILERONS MALFUNCTIONED A NSVA O OTHER O OTHER CR CRUISE 1 EA 27 239CJ 239 CONTROL PRESSURE FOR ROLL IS AT LEAST 2X HIGHER THAN ANY OTHER ACFT PILOT HAS FLOWN. PITCH AND YAW OK. "AIL" FLASHING INTERMITTENTLY. NOTED MORE DURING TURNS. "AIL" WILL STILL FLASH INTERMITTENTLY EVEN IF AILERON TRIM IS NEUTRALIZED. C HECKED PULLEYS UNDER YOKE AT ELECTRICAL BAYS LT AND RT CHECKED AROUND AILERONS LT AND RT PULLEYS, LINKAGES. ALSO BEHIND FLAPS UNDERBELLY OF A/C. CHECKED PULLEYS UNDER FLOORBOARDS. RELUBED LINKAGES, CABLES AND PULLEYS NO OBVIOUS APPARENT DAMAGE TO CONNECTIONS OPS CHECKED AUTO PILOT IAW SAAB MM 22-10-00. OPS CHECK GOOD. REPLACED LT AILERON CENTERING MECHA NISM CAM IAW SAAB MM 27-11-45-04. OPS CHECK GOOD. ALSO LUBRICATED AILERON HINGE POINTS IAW C/W 27-11-07S. OPS CHECK G 2 L 7 2 4T RT A52EU 2008011500088 20080115 00088 NM 2008 1 15 USAA920080076 1 20071219 A 5320 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED WEB ANGLE, BS 303, S10L. REPLACED WEB ANGLE, BS 303, S10L IAW B737 SRM 51-10-0 1. 2 L 7 2 4F RT A16WE 2008011500096 20080115 00096 EU 2008 1 15 NSVA20070150 1 20070607 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 344CJ 344 AFT CABIN EMERGENCY LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED POWER SUPPLY PN ON/OFF 60-1321-1 SN OFF 17275. 2 L 7 2 4T RT A52EU 2008011500099 20080115 00099 EU 2008 1 15 NSVA20070122 1 20070506 A 2612 WEU SAAB SF340 340B 7860101 EU FIRE DETECTION MALFUNCTIONED A NSVA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 194CJ 194 LEFT ENGINE FIRE DETECT INOP. INSPECTED FIRE LAP, NO DEFECTS; CLEANED ENGINE NACELLE CONNECTORS, RERACKED WEU, DID LT E NGINE RUN NO WARNINGS OR FAULTS, REF 26-11-00. 2 L 7 2 4T RT A52EU 2008011500100 20080115 00100 2008 1 15 NSVA20070123 4 20070507 A 2330 4970114012 CRADLE SAAB SF340 340B 7860101 EU ODOR A NSVA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 27 362PX 258 F/A'S PA SYSTEM HAD HOT WIRE ODOR AND IS INOP. FOUND FLIGHT DECK CRADLE SHORTED AND CAUSING HOT WIRE ODOR. REMOVED AND REPLACED FLIGHT DECK CRADLE ASSY, OPS CHECK GOOD IAW 23-30-05. 2 L 7 2 4T RT A52EU 2008011500101 20080115 00101 EU 2008 1 15 NSVA20070136 1 20070524 A 3350 SWITCH SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS MALFUNCTIONED A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 347CJ 347 EMERGENCY LIGHTS NOT TESTING. RESET SWITCH ON F/A'S PANEL, OPS OK AMM 33-50-00. 2 L 7 2 4T RT A52EU 2008011500104 20080115 00104 EU 2008 1 15 NSVA20070209 1 20070809 A 2612 703072 FIRE LOOP SAAB SF340 340B 7860101 EU LT NACELLE SHORTED A NSVA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 194CJ 194 LEFT ENGINE FIRE LIGHT AND BELL CAME ON SHORT FINAL. REMOVED AND REPLACED FIRE LOOP TO LT ENGINE OUTBOARD SECTION IAW 2 6-11-03. OPS CHECK GOOD, PN ON/OFF 703072. 2 L 7 2 4T RT A52EU 2008011500105 20080115 00105 EU 2008 1 15 NSVA20070202 1 20070805 A 3234 D49412001 CONTROL HANDLE SAAB SF340 340B 7860101 EU MLG MALFUNCTIONED A NSVA O OTHER N FALSE WARNING AP APPROACH 1 EA 27 350CJ 350 GEAR UNSAFE INDICATION WHEN SELECTED DOWN, NOSE GEAR DOES NOT ILLUMINATE, JIGGLING HANDLE AND ALL 3 COME ON. REPLACED L ANDING GEAR CONTROL HANDLE IAW SAAB AMM 32-31-05 FUNCTIONAL CHECK OF EXTENSION AND RETRACTION COMPLIED WITH IAW SAAB 340 32-30-00. NO DEFECT NOTED, PN: D494-12-001, SN ON: 300/05-90, SN OFF: 215/07-88. 2 L 7 2 4T RT A52EU 2008011500110 20080115 00110 NM 2008 1 15 USAA920080082 1 20071202 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 867, S9L. REPAIRED FRAME, BS 867, S9L IAW USAIRWAYS TYPICAL REPAIR 5 3-10-25. 2 L 7 2 4F RT A16WE 2008011500111 20080115 00111 NM 2008 1 15 USAA920080083 1 20071212 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 907, S9L. REPAIRED FRAME, BS 907, S9L IAW USAIRWAYS TYPICAL REPAIR 5 3-10-25. 2 L 7 2 4F RT A16WE 2008011500113 20080115 00113 NM 2008 1 15 USAA920080084 1 20071204 A 5320 655287454 ATTACH ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED INTERCOSTAL WEB ATTACH ANGLE , BS 944, S14L. REPLACED INTERCOSTAL WEB ATTACH A NGLE, BS 944, S14L IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008011500114 20080115 00114 EU 2008 1 15 NSVA2007224 1 20070908 A 2897 CONNECTOR SAAB SF340 340B 7860101 EU FUEL FLOW IND DIRTY A NSVA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 344CJ 344 RT FUEL FLOW INDICATOR READS 200 LBS ON TAKEOFF. CLEANED CONNECTOR AND OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011500115 20080115 00115 NM 2008 1 15 USAA920080085 1 20071221 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 787, S9R. REPAIRED FRAME, BS 787, S9R IAW USAIRWAYS TYPICAL REPAIR 5 3-10-25. 2 L 7 2 4F RT A16WE 2008011500116 20080115 00116 EU 2008 1 15 NSVA20070221 1 20070902 A 2750 FLAP SYSTEM SAAB SF340 340B 7860101 EU TE FLAPS MALFUNCTIONED A NSVA O OTHER O OTHER CR CRUISE 1 EA 27 356CJ 340B356 FLAPS DROP TO 7 DEGREES IN FLIGHT MULTIPLE TIMES. OPS CHECK FLAP CONTROL SYSTEM IAW AMM 27-51. OPS CHECK OK. NO FAULT FOUND. 2 L 7 2 4T RT A52EU 2008011500117 20080115 00117 NM 2008 1 15 USAA920080086 1 20071205 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 827, S9R. REPAIRED FRAME, BS 827, S9R IAW USAIRWAYS TYPICAL REPAIR 5 3-10-25. 2 L 7 2 4F RT A16WE 2008011500118 20080115 00118 NM 2008 1 15 USAA920080087 1 20071221 A 5311 9U53261485 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 887, S9R. REPAIRED FRAME, BS 887, S9R IAW USAIRWAYS TYPICAL REPAIR 5 3-10-25. 2 L 7 2 4F RT A16WE 2008011500122 20080115 00122 NM 2008 1 15 USAA920080091 1 20071215 A 5313 STRINGER SPLICE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED STRINGER SPLICE, BS 360, S15L. REPLACED STRINGER SPLICE, BS 360, S15L IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008011500130 20080115 00130 NM 2008 1 15 USAA920080096 1 20071217 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 440, S8R. REPAIRED FRAME, BS 440, S8R IAW USAIRWAYS TYPICAL REPAIR 5 3-10-25. 2 L 7 2 4F RT A16WE 2008011500131 20080115 00131 EU 2008 1 15 NSVA20070200 1 20070802 A 3297 CONNECTOR SAAB SF340 340B 7860101 EU DOWNLOCK SWITCH LOOSE A NSVA O OTHER O OTHER AP APPROACH 1 EA 27 203CJ 203 RIGHT MAIN LANDING GEAR INDICATOR WILL NOT ILLUMINATE IN FLIGHT WITH GEAR DOWN. RESECURED LOCK DOWN SWITCH CONNECTOR AT RT MAIN LANDING GEAR IAW AMM 61-65-02, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011500132 20080115 00132 NM 2008 1 15 USAA920080097 1 20071219 A 5322 SHEAR TIE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED SHEAR TIE, BS 360, S14R - S15R. REPLACED CRACKED SHEAR TIE, BS 360, S14R - S15 R IAW B737 SRM 53-00-07 REPAIR 7. 2 L 7 2 4F RT A16WE 2008011500136 20080115 00136 NM 2008 1 15 USAA920080100 1 20071215 A 5322 6948204503 SHEAR TIE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED SHEAR TIE, BS 360, S13L. REPLACED SHEAR TIE, BS 360, S13L IAW B737 SRM 51-10-0 2. 2 L 7 2 4F RT A16WE 2008011500142 20080115 00142 NM 2008 1 15 USAA920080104 1 20071202 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED STRINGER CLIP, BS 294.5, S12L. REPLACED STRINGER CLIP, BS 294.5, S12L IAW B737 SRM 51-20-00. 2 L 7 2 4F RT A16WE 2008011500143 20080115 00143 NM 2008 1 15 USAA920080105 1 20071219 A 5311 6545807 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FRAME INNER CHORD, BS 312, S7R. REPLACED FRAME INNER CHORD, BS 312, S7R IAW B7 37 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008011500147 20080115 00147 NE 2008 1 15 NSVA20070198 2 20070731 A 7261 GAS GENERATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE ENGINE LEAKING A NSVA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 221CJ UE221 PS0003 SMALL AMOUNT OF SMOKE IN THE COCKPIT, ODOR. LANDED SAFELY. FOUND GAS GENERATOR LEAKING OIL INTO COMPRESSOR SECTION (UN DETERMINED INTERNAL LEAK) LT ENGINE, REQUIRES ENGINE CHANGE. 2 L 7 2 4T 4 T RT A24CE E26NE 2008011500151 20080115 00151 NM 2008 1 15 USAA920080110 1 20071205 A 5320 654654039 ATTACH BRACKET BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED STUB BEAM ATTACH BRACKET, BS 639, LBL 45. REPLACED STUB BEAM ATTACH BRACKET, B S 639, LBL 45 IAW B737 SRM 51-40-03. 2 L 7 2 4F RT A16WE 2008011500152 20080115 00152 2008 1 15 NSVA20070249 4 20071212 A 3421 6226342022 EADI SAAB SF340 340B 7860101 EU COCKPIT DISTORTED A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 350CJ 340B350 DURING CRUISE; FO'S EADI WENT DISTORTED, LOUD POP HEARD SCREEN CAME BACK FULL THEN ELECTRICAL SMOKE DETECTED. 2 L 7 2 4T RT A52EU 2008011500154 20080115 00154 EU 2008 1 15 NSVA20070204 1 20070807 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 233CJ 340B233 FLOOR EMERGENCY LIGHTS 5, 6, 6A, 7, 7DF, 9DF OUT. REMOVED AND REPLACED EMERGENCY BATT PWR SUPPLY NR 3 IAW SAAB 340 AMM 33-50-10P/N OFF/ON: 60-1321-1, S/N OFF: 17778, S/N ON: 16022. 2 L 7 2 4T RT A52EU 2008011500155 20080115 00155 EU 2008 1 15 NSVA20070237 1 20071001 A 7797 6068T54P02 WIRE HARNESS SAAB SF340 340B 7860101 EU LT ENGINE UNKNOWN A NSVA O OTHER N FALSE WARNING CR CRUISE 1 EA 27 350CJ 340B350 LT ENGINE TORQUE AND RMP FLUX/AIR RETURN. REPLACED RT ENGINE YELLOW HARNESS. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011500156 20080115 00156 EU 2008 1 15 NSVA20070244 1 20071130 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 251CJ 251 EMERGENCY LIGHTS FLICKERING DURING MAINTENANCE CHECK. REPLACED POWER SUPPLY. 2 L 7 2 4T RT A52EU 2008011500157 20080115 00157 EU 2008 1 15 NSVA20070250 1 20071221 A 3350 7225280527 CONTROL PANEL SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS MALFUNCTIONED A NSVA O OTHER O OTHER CR CRUISE 1 EA 27 362PX 340B258 ALL INTERIOR EMERGENCY LIGHTS ILLUMINATED, CREW UNABLE TO TURN LIGHTS OFF. REMOVED AND REPLACED FLIGHT ATTENDANTS PANEL . 2 L 7 2 4T RT A52EU 2008011500161 20080115 00161 NM 2008 1 15 USAA920080081 1 20071210 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 847, S9L. REPAIRED FRAME, BS 847, S9L IAW USAIRWAYS TYPICAL REPAIR 5 3-10-20E. 2 L 7 2 4F RT A16WE 2008011500162 20080115 00162 EU 2008 1 15 NSVA20070248 1 20071206 A 3240 BRAKE ASSY SAAB SF340 340B 7860101 EU MLG MALFUNCTIONED A NSVA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 321CJ 340B321 AFTER LANDING ON RW31 LGA, WHILE TAXIING ON ALPHA TO RAMP WAS TOLD TO HOLD SHORT, WHEN PUSHED ON BRAKES THERE WAS NO RES PONSE. HYDRO PRESSURE CHECKED OK, PUT POWER LEVERS TO REVERSE TO STOP. ACFT WAS TOWED IN TO GATE BY GROUND CREW. PILO T HAD BRAKES TO STOP ON RUNWAY AND WHILE TURNING ON TO ALPHA TAXIWAY. INSPECTED ALL 4 BRAKES, HYD QTY, PRESS ACCUMULATO RS. NO LEAKS NOTED IN BRAKE LINES. TAXIED A/C FOR 20 MIN BRAKES, OPS CHECK GOOD AT TAXI SETTINGS AND HYD POWER SETTING S. PARKING BRAKE ALSO OPS CHECK GOOD. COULD NOT DUPLICATE DISCREPANCY AT THIS TIME. 2 L 7 2 4T RT A52EU 2008011500164 20080115 00164 CE 2008 1 15 NSVA20070213 1 20070814 A 6123 UNKNOWN BEECH 1900 1900D 1154162 CE AUTOFEATHER SYS MALFUNCTIONED A NSVA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 27 172MJ UE72 AUTOFEATHER SYSTEM WILL NOT ARM. FOUND CIRCUIT BREAKER POPPED, CLEANED SOLENOID AND LUBRICATED. RAN A/C IAW BEECH MM 6 1-21-00. OPS CHECK GOOD, NO FAULTS NOTED. 2 L 7 2 4T RT A24CE 2008011500165 20080115 00165 NE 2008 1 15 NSVA20070207 2 20070809 A 7510 32248122 ANTI-ICE VALVE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE MALFUNCTIONED A NSVA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 210CJ 210 785548 LT ENGINE COMPRESSOR STALL AT 10,000 FEET MSL DURING CRUISE. NORMAL CRUISE POWER SETTING TEMPS NORMAL, ALL INDICATIONS NORMAL. POPPING SOUND AND DROP IN TORQUE STARTED. ITT WAS HIGH FOR TORQUE SETTING AFTER POPPING SOUND. PERFORMED TROU BLESHOOTING OF ENGINE STALL IAW CT7 M/M TABLE 101. FOUND ANTI-ICE BLEED VALVE STICKING AND HARD TO MOVE. REMOVED AND R EPLACED LT ENGINE ANTI-ICE VALVE FOR TROUBLESHOOTING IAW GE MM 75-00-00. FOUND ACTUATOR BINDING AND ROUGH TRAVEL, PN ON /OFF 3224812-2, SN OFF GRTB5071, SN ON GRTB7045. PERFORMED OPS CHECK OF LT ANTI-ICE BLEED VALVE IAW 72-00-00. NO DEFEC TS NOTED. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011500170 20080115 00170 EU 2008 1 15 NSVA20070215 1 20070815 A 2697 POWER SUPPLY SAAB SF340 340B 7860101 EU SMOKE DETECTION DISCONNECTED A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 299CJ 299 LAVATORY SMOKE DETECTION SYSTEM WILL NOT TEST. RECONNECTED POWER SUPPLY TO THE BACK OF THE LAVATORY SMOKE LIGHT BULB AS SY, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011500171 20080115 00171 EU 2008 1 15 NSVA20070228 1 20070916 A 2917 GPP125012 PRESSURE SWITCH SAAB SF340 340B 7860101 EU HYD SYSTEM MALFUNCTIONED A NSVA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 343CJ 346 HYDRAULIC LIGHT ILLUMINATED AT ALT COMPLETED APPROPRIATE CHECK LIST DETERMINED THAT ATO FUNCTION FAILED MAIN ACCUMULATOR WAS LOW AT RED LINE EMERGENCY ACC INB OUTBOARD NORMAL USED OVERRIDE FUNCTION AS NEEDED FOR REMAINDER OF FLIGHT. SERVIC ED HYD RESERVOIR IAW 12-10-29, REMOVED AND REPLACED HYD PRESSURE SWITCH PN GPP1250-12 SN ON 8506113 SN OFF 0625892IAW 2 9-10*45-04, OPS CHECK OK, LEAK CHECK OK. 2 L 7 2 4T RT A52EU 2008011500172 20080115 00172 EU 2008 1 15 NSVA2007240 1 20071005 A 3251 708572 ACTUATOR SAAB SF340 340B 7860101 EU NLG STEERING MALFUNCTIONED A NSVA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 EA 27 339CJ 340B339 WHILE TAXING CAPTAIN HEARD A CRUNCHING NOISE AND LOST ALL STEERING. AIRCRAFT WAS TOWED BACK TO GATE. INSPECTED NOSE STE ERING CONTROL ASSY, NO DAMAGE NOTED IAW SAAB AMM 32-50-00-00. NOSE STEERING OPERATES NORMALLY TO THE RIGHT BUT STEERS T O FAR TO THE LEFT TILLER OR NOSE DOES NOT RETURN TO CENTER WHEN TILLER RELEASE. VIBRATE NOISE COMING FROM STEERING ACTU ATOR WHEN OPERATED. STEERING BRAKE SWITCH STICK WHEN TILLER WOULD DO THE LT, ABLE TO MOVE STEERING WITHOUT PRESSING DOW N THE TILLER, COULD NOT FIND CAUSE OF OVER STEERING TO THE LEFT. REMOVED AND REPLACED STEERING SERVO ACTUATOR IAW SAAB 32-50-25, ALL CHECKS GOOD NO LEAKS. 2 L 7 2 4T RT A52EU 2008011500174 20080115 00174 EU 2008 1 15 NSVA20070218 1 20070818 A 2913 4018502 PUMP SAAB SF340 340B 7860101 EU HYD SYSTEM INOPERATIVE A NSVA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 352CJ 352 DURING TAXI INTERMITTENT HYDRAULIC PUMP OPERATION IN AUTO OVERRIDE. REMOVED AND REPLACED HYDRAULIC MOTOR DRIVEN PUMP IA W AMM 29-10-10-4. OPS AND LEAKAGE CHECK GOOD IAW AMM 29-10-10-5 PN, ON/OFF 40185-02 SN ON EQ21 OFF EQ23. 2 L 7 2 4T RT A52EU 2008011500175 20080115 00175 2008 1 15 NSVA20070217 2 20070817 A 7320 HMU SAAB SF340 340B 7860101 EU ENGINE OUT OF RIG A NSVA O OTHER E VIBRATION/BUFFET CR CRUISE 1 EA 27 344CJ 344 VIBRATION IN FLIGHT AT LOW POWER/HIGH RPM SETTINGS. REMOVED SPINNER AND INSPECTED PROP AND BLADES FOR SECURITY. INSPEC TED PCU AND HMU FOR SECURITY. NO DEFECTS NOTED. GRD RAN ENGS WITH NO NOTICEABLE VIBRATION. INSPECTED COND LEVERS AND OVERALL CONDITION OF CONTROL CABLES, NO DEFECTS. FOUND RT ENG HMU AND PCU RIG OUT OF ADJUSTMENT. RIGGED RT ENG HMU AND PCU IAW AMM 76-10-00. ENGINE REQUIRES RUN FOR OPS CHECK. ON MX RUNS RT ENGINE OPERATION WAS GOOD. NO DEFECTS NOTED A FTER ENGINE, OPS CK ON MX RUNS. THE VIBRATION IS THE LT ENGINE WHEN TRANSCENDING LEVERS TO IDLE IF PERFORM IN SINGLE OP ERATION LT SIDE VIBES COMING DOWN, REQUIRES TROUBLESHOOTING OF LT ENGINE. C/W RIGGING AND MX RUNS AND OPS CHECK RT ENG 2 L 7 2 4T RT A52EU 2008011500177 20080115 00177 EU 2008 1 15 NSVA20070242 1 20071102 A 2121 EVCTA465 FAN SAAB SF340 340B 7860101 EU RECIRCULATION FAILED A NSVA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 251CJ 251 RIGHT RECIRCULATION FAN LIGHT ILLUMINATED THEN WENT OUT, SMOKE ODOR IN CABIN AND COCKPIT. VISIBLE SMOKE FROM THE CABIN F LOOR BOTH ENGINES RUNNING AT GROUND IDLE. DEFERRED INOPERATIVE BLOWER MOTOR IAW MEL 21-20-1. 2 L 7 2 4T RT A52EU 2008011500179 20080115 00179 EU 2008 1 15 NSVA20070216 1 20070812 A 5220 HANDLE SAAB SF340 340B 7860101 EU EMERGENCY DOOR UNSECURE A NSVA O OTHER O OTHER CR CRUISE 1 EA 27 350CJ 350 FWD EMERG DOOR HANDLE TO OPEN POSITION IN FLIGHT. RESECURED FWD EMERG DOOR HANDLE SAFTIED, A/C OK FOR SERVICE. 2 L 7 2 4T RT A52EU 2008011500182 20080115 00182 EU 2008 1 15 NSVA20070243 1 20071119 A 3240 07750125893 BRAKE SAAB SF340 340B 7860101 EU NR 4 INOPERATIVE A NSVA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 321CJ 340B321 BRAKES INOP DURING TAXI. REMOVED AND REPLACED NR 4 BRAKE ASSY. 2 L 7 2 4T RT A52EU 2008011500183 20080115 00183 EU 2008 1 15 NSVA20070234 1 20070926 A 7500 BLEED AIR SYS SAAB SF340 340B 7860101 EU LT ENGINE UNKNOWN A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 334CJ 340B334 ABORTED TAKEOFF AT 70KTS. LT ENGINE HOT. OPENED MEL FOR BLEED SYSTEM MEL NR 27424, THEN REMOVED AND REPLACED PERI SEAL, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011500189 20080115 00189 EA 2008 1 15 VNAA0712004 1 20071223 A 3250 STEERING SYS CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE NLG MALFUNCTIONED A VNAA O OTHER J WARNING INDICATION LD LANDING 1 GL 05 708PS 10160 CREW REPORTED A STEERING INOP AMBER MESSAGE DURING LANDING. AIRCRAFT WAS TOWED TO THE GATE UPON REQUEST FROM THE CREW. MAINTENANCE INTERROGATED THE MDC AND PERFORMED AN OPS TEST OF THE NOSE WHEEL STEERING IN ACCORDANCE WITH THE AIRCRAFT M AINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008011500209 20080115 00209 EA 2008 1 15 MASA200700424 1 20070713 A 5220 COVER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 515MJ 10117 ASH 7195 IAD - CAPT REPORTED THE EMERGENCY EXIT HANDLE COVER AT SEAT 12A WILL NOT STAY CLOSED. MX RESECURED THE VELCRO STRIP AS REQUIRED. 2 L 7 2 4F RT A21EA 2008011500211 20080115 00211 EU 2008 1 15 WRNA200700066 1 20071011 A 7120 BOLT AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE CORRODED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 510TA 100 DURING ACCOMPLISHMENT OF CPCP C54-400-03-00 AT M96 CHECK LEVEL II CORROSION WAS FOUND ON 4 HORIZONTAL BOLTS OF NR 2 ENGI NE AFT MOUNT. REMOVED AND REPLACED 4 HORIZONTAL MOUNT BOLTS IAW MM 20-21-17 AND MM 70-00-00. 2 L 7 2 4F RT A35EU 2008011500214 20080115 00214 EA 2008 1 15 MASA200700865 1 20071207 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 502MJ 10050 ASH 7154 ORD - CAPTAIN REPORTED EMERGENCY PATH LIGHTING UNSECURED AT ROW 12 D/F. MX RESECURED LIGHTS. 2 L 7 2 4F RT A21EA 2008011500219 20080115 00219 EA 2008 1 15 MASA200700911 1 20071221 A 5210 601R3181273 CABLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR UNKNOWN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 503MJ 10058 ASH 7404 RDU-ORD - CAPTAIN REPORTED THE MAIN PAX DOOR OUTSIDE HANDLE DIFFICULT TO OPEN. CHANGED ICE BREAK CABLE. 2 L 7 2 4F RT A21EA 2008011500221 20080115 00221 EA 2008 1 15 MASA200700497 1 20070809 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 513MJ 12989 10111 ASH 7259 CLT-IAD - EMERGENCY LIGHTS WILL NOT STAY ILLUMINATED WHEN TURNED ON. MX REMOVED AND REPLACED ALL EMERGENCY LIG HT BATTERY PACKS. 2 L 7 2 4F RT A21EA 2008011500233 20080115 00233 EA 2008 1 15 MASA200700523 1 20070826 A 3260 895304 PROXIMITY SENSOR CNDAIR CL600 CL6002C10 1390015 EA MLG MALFUNCTIONED A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 513MJ 6519 10111 ASH 7039 CHS-ORD - CREW DIVERTED TO CLT DUE TO A GEAR DISAGREE AND WOW I/P CAUTION IN FLIGHT. MX REMOVED AND REPLACED S ELECTOR VALVE AND PSECU. 2 L 7 2 4F RT A21EA 2008011500236 20080115 00236 EA 2008 1 15 MASA200700617 1 20070922 A 5230 DOOR CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY OPEN A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 507MJ 10077 ASH FLT 7215 ORD-SAV - FWD CARGO DOOR OPENED AFTER TAKEOFF. MX CHECKED RIG AND OPERATION, NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2008011500237 20080115 00237 EA 2008 1 15 MASA200700629 1 20070924 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA CABIN ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 511MJ 10104 ASH FLT 7367 IAD TO AUS - BURNING ODOR IN CABIN. MX PERFORMED OPERATIONAL CHECKS OF AIR CONDITIONING PACKS AND BLEED SY STEMS. COULD NOT DUPLICATE ODOR. 2 L 7 2 4F RT A21EA 2008011500238 20080115 00238 EA 2008 1 15 MASA200700632 1 20070903 A 5280 CC67010520952 PANEL CNDAIR CL600 CL6002C10 1390015 EA RT MLG DOOR UNKNOWN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 510MJ 10101 RT MLG DOOR LOWER PANEL FAILED INSPECTION. REMOVED AND REPLACED RT MLG DOOR LOWER PANEL. 2 L 7 2 4F RT A21EA 2008011500255 20080115 00255 EA 2008 1 15 MASA200700697 1 20071014 A 2560 SEAL CNDAIR CL600 CL6002C10 1390015 EA MED KIT MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 571ML 7670 7209 ASH FLT 7165 ORD-ATW - EMERGENCY MEDICAL KIT SEAL WAS MISSING. MX REPLACED THE MEDICAL KIT. 2 L 7 2 4F RT A21EA 2008011500256 20080115 00256 EA 2008 1 15 MASA200700702 1 20071009 A 5280 SKIN CNDAIR CL600 CL6002C10 1390015 EA MLG DOOR LOOSE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 502MJ 15016 10050 LT MLG INBOARD DOOR LOWER SKIN RIVETS LOOSE. REMOVED AND REPLACED DOOR P/N CC670-10520-9 S/N 15016. 2 L 7 2 4F RT A21EA 2008011500262 20080115 00262 EA 2008 1 15 MASA200700848 1 20071203 A 5330 SKIN CNDAIR CL600 CL6002D24 1390016 EA BS 437 PUNCTURED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 925FJ 15025 REPAIR TO PUNCTURE IN FUSELAGE SKIN AT FS 437.00 STR 22R. 2 L 7 2 4F RT A21EA 2008011500264 20080115 00264 EA 2008 1 15 MASA200700613 1 20070920 A 2150 GG670950095 ACM CNDAIR CL600 CL6002D24 1390016 EA RIGHT ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 902FJ 9407 15002 ASH FLT 2610 SRQ-CLT - RT PACK AUTO FAIL CAUTION MESSAGE ALONG WITH SMOKE AND ODOR IN THE CABIN. REMOVED AND REPLACED R T ACM, OPS NORMAL. 2 L 7 2 4F RT A21EA 2008011500265 20080115 00265 EA 2008 1 15 MASA200700480 1 20070804 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 654BR 7454 ASH 1019 HNL-OGG - PILOT REPORTED THE FLOOR LEVEL EMERGENCY LIGHT STRIP AT ROW 6 WAS OUT. MX, RELAMPED. 2 L 7 2 4F RT A21EA 2008011500275 20080115 00275 EA 2008 1 15 MASA200700583 1 20070916 A 3350 38672088722607 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 942LR 150042 ASH FLT 2769 - MOST EMERGENCY AFT LIGHTS INOP. MX REPLACED LIGHTS. 2 L 7 2 4F RT A21EA 2008011500276 20080115 00276 EA 2008 1 15 MASA200700363 1 20070626 A 5220 SEAL CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT LEAKING A MASA O OTHER O OTHER CR CRUISE 1 SW 07 932LR 15032 ASH 2633 CLT - LT AFT EMERGENCY EXIT DOOR WHISTLES IN FLIGHT. SECURED SEAL. 2 L 7 2 4F RT A21EA 2008011500280 20080115 00280 EA 2008 1 15 MASA200700701 1 20071016 A 5720 SHROUD CNDAIR CL600 CL6002D24 1390016 EA RT WING LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 906FJ 15006 FOUND 1 MISSING RIVET ON RT WING OUTBOARD MFS SHROUD FITTING AT WING STATION 231.23. PERFORMED PERM REPAIR. 2 L 7 2 4F RT A21EA 2008011500286 20080115 00286 WP 2008 1 15 UPS08851375 1 20071227 A 5320 FLOOR SUPPORT DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 CABIN STA 5 RBL 48 AND RBL 50 FLOORBOARD SUPPORT CRACKED. REMOVED AND REPLACED FLOORBOARD SUPPORT IN MAIN CABIN AT STA 5 RBL 48-50 IAW DWG 5613327, AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 2008011500288 20080115 00288 NM 2008 1 15 UPS08M51354 1 20071230 A 2150 A/C PACK DOUG MD11 MD11F 3023600 NM NR 3 ODOR A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 253UP 48439 INSPECTION TYPE:N/A APU QUIT AND WOULDN'T ACCEPT GROUND POWER. SMELL OF ELECTRICAL FUMES IN COCKPIT. MX STARTED THE AP U, PERFORMED EPCU RTS AND FUMES WERE FROM THE NR 3 PACK. PERFORMED EPCU RTS ALL PASS. INSPECTED CTR ACCESSORY AND FWD E&E NO PROBLEMS NOTED, FUMES OR SMELL FROM NR 3 PACK. WARM STARTED APU. ALL CHECKS OK. 2 L 7 3 4F RT A22WE 2008011500289 20080115 00289 NM 2008 1 15 UPS08M51378 1 20071210 A 5320 A766731 SUPPORT DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C FWD CARGO/AT STATION 6-74, X+44 AND X-36 TEE SUPPORT FOUND CRACKED. CRACK TEE SUPPORT REMOVED AS PER SRM 51-31-01 V II R 35. NEW TEE P/N: AD FAB PER DWG ADA7667. NEW TEE FASTENERS HOLE TRANSFERED PER DWG ADA7667 AND SRM 51-31-01 VII R35. NEW TEE REPROTECTED PER SRM 51-21-01 VII R35. NEW TEE PAINTED PER SRM 51-21-01 VII R35. NEW TEE SUP PORT INSTALLED PER SRM 51-31-01 VII R35. 2 L 7 3 4F RT A22WE 2008011500296 20080115 00296 EA 2008 1 15 MASA200700698 1 20071015 A 2611 47359719 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY MALFUNCTIONED A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 27172 11342 7172 ASH 7271 IAD-MYR - CARGO SMOKE WARNING MESSAGE. THE CREW DEPLANED THE PASSENGERS CONVENTIONALLY, AND BLEW THE FIRE BOTT LES. MX DETERMINED THAT THERE WAS NEVER ANY SMOKE OR FIRE. REPLACED BOTH SMOKE DETECTORS, AND FIRE BOTTLES. 2 L 7 2 4F RT A21EA 2008011000136 20080110 00136 NM 2008 1 10 USAA920080058 1 20071228 A 5754 65C26602218 SLAT BOEING 737 7373G7 1384595 NM L/E SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - RIGHT WING NR 5 SLAT LOWER TRAILING EDGE HAS DELAMINATION. REPLACED RIGHT WING NR 5 SL AT IAW B737 AMM 27-81-21-004-001. 2 L 7 2 4F RT A16WE 2008011000139 20080110 00139 NM 2008 1 10 USAA920080059 1 20071218 A 5753 654643099 SKIN BOEING 737 7373G7 1384595 NM T/E FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - LEFT WING INBOARD FORE FLAP LOWER SURFACE HAS DELAMINATION. REPAIRED LEFT WING INBOARD FORE FLAP LOWER SURFACE IAW B737 SRM 51-70-10. 2 L 7 2 4F RT A16WE 2008011000147 20080110 00147 EU 2008 1 10 2007UALA05212 1 20071222 A 2130 CABIN PRESSURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 415UA 475 RTFL WHEN UNABLE TO PRESSURIZE THE MAIN CABIN. A/C WAS CHECKED OUT AFTER INCIDENT AND CONDITION, COULD NOT BE DUPLICATE D. AIRCRAFT PRESSURIZED NORMALLY AND PASSED ALL TESTS (AEVC, SKIN VALVE). 2 L 7 2 4F 4 F RT A28NM E40NE 2008011000156 20080110 00156 2008 1 10 2007UALA05337 4 20071228 A 2565 65C318435 SLIDE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE L1 DOOR SHORT A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 826UA 989 EMERGENCY LIGHTS TEST FAILS PER 3SVC PAPERWORK. FAULTS EPSU EXT LOAD FWD L. ELECTRICAL SHORT INSIDE SLIDE 1L. REPLACE D SLIDE PACK 1L, OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011000177 20080110 00177 NM 2008 1 10 2007UALA05358 1 20071229 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 AFT PIT INTERCOSTAL AT STA 847-867 BETWEEN STR 25 AND 26 IS CRACKED. REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011000188 20080110 00188 NM 2008 1 10 2007UALA05368 1 20071229 A 3350 LENS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 563UA 26665 EXIT SIGN LENS FELL OFF ROW 16F. 2 L 7 2 4F 4 F RT A2NM E17NE 2008011000198 20080110 00198 NM 2008 1 10 2007UALA05376 1 20071229 A 3350 276005 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BATTERY CHARGER INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 RIGHT SIDE 2 FWD OVERWING LIGHTS INOPERATIVE. REPLACED FUSE ON BATTERY CHARGER 2 L 7 4 4F 4 F RT A20WE E24NE 2008011000210 20080110 00210 NM 2008 1 10 2007UALA05387 1 20071227 A 3213 CYLINDER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT MLG CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 RIGHT MLG HAS EVIDENCE OF CORROSION ABOVE GLAND NUT INSIDE OF MLG INNER CYLINDER. RT MLG OUTER CYLINDER REPLACED AS WEL L AS STRUT SEAL REPLACEMENT TO CORRECT A LEAK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008011000220 20080110 00220 NM 2008 1 10 2008UALA0004 1 20071231 A 5240 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 FORWARD GALLEY DOOR, FWD FRAME IS CRACKED AT LOWER CORNER OUTBOARD FASTENER HOLES. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011100003 20080111 00003 2008 1 11 2007UALA05242 4 20071221 A 2565 65C318435 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 407UA 456 EMERGENCY LIGHT AT DOOR 1L IS INOP. INTERNAL ELECTRICAL FAULT (SLIDE 1L). REPLACED DOOR SLIDE 1L, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011100013 20080111 00013 NM 2008 1 11 2007UALA05251 1 20071223 A 3350 BR964421 LENS AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN MISSING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 834UA 1420 EEPM LIGHT SEAT 22C MISSING LENS. REPLACED LENS AT SEAT 22C (EEPM). 2 L 7 2 4F 4 F RT A28NM E40NE 2008011100021 20080111 00021 EU 2008 1 11 2007UALA05296 1 20071225 A 2612 TEST UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FIRE WARNING MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 420UA 489 APU FIRE TEST NOT WORKING. RESET APU FDU SYSTEM, OPERATES/TESTS NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011100031 20080111 00031 NM 2008 1 11 2008UALA0009 1 20071231 A 5320 ATTACH ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 FWD GALLEY DOOR CUTOUT INTERCOSTAL ATTACH ANGLE CRACKED BETWEEN BS 277 & 294.5 AND BETWEEN STRINGERS 12R & 13R. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011100032 20080111 00032 NM 2008 1 11 2008UALA0010 1 20071231 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 AFT PIT BS 727B STRINGER CLIPS DAMAGED AT STRINGERS S19R & S20R DURING SKIN REPLACEMENT ACTIVITY. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011100055 20080111 00055 SO 2008 1 11 IMP2007F00000 1 20071201 A 5312 45346000 BULKHEAD PIPER PA31T PA31T 7103124 SO PWA PT6 PT6A28 EA FUSELAGE CRACKED E IMPA K NONE O OTHER IN INSP/MAINT 1 WP 11 155CA 11500 31T7820024 FOUND BULKHEAD (NR 45346-000) LOCATED AT STA 46.0 TO HAVE CRACKS IN RADIUS OF VERTICAL FLANGE, EXTENDING APPROXIMATELY . 5 INCH FROM THE TOP. (K) 1 L 7 2 3T 4 T A8EA E4EA 2008011100072 20080111 00072 NE 2008 1 11 C1HA200776001 2 20071218 A 7200 BLADES BOEING 727 727225 1384077 NM PWA JT8 JT8D* NE NR 1 ENGINE DAMAGED A C1HA C ABORTED TAKEOFF C J F.O.D. WARNING INDICATION TO TAKEOFF 1 GL 15 676MG 22554 649698 AFTER 1.4 EPR CHECK, WHICH WAS COMPLETELY NORMAL, POWER WAS ADVANCED ON ALL ENGINES. AT APPROXIMATELY 1.6 EPR AND 60 KTS THE NR 1 PACK TRIP LIGHT ILLUMINATED FOLLOWED BY THE ENGINE FAIL LIGHTS. ABORTED THE TAKEOFF AT THAT POINT THE FLIGHT A TTENDANT HEARD A SERIES OF BANGS AND POPS, WE DIDN'T HEAR ANYTHING. ALL ENGINE INDICATIONS NORMAL. NR 1 ENGINE HAS 4 D AMAGED BLADES: 3 ARE REPAIRABLE AND 1 REQUIRES NO REPAIR. NR1 ENGINE BLADES REPAIRED. NR 3 ENGINE REMOVED AND REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 2008011100080 20080111 00080 SO 2008 1 11 GUUA12180702 1 20071218 A 3350 12036904005 LIGHT EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN DAMAGED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 261AS 120141 FLIGHT: 9227, EMERGENCY LIGHTS NEAR GALLEY ARE DAMAGED AND MISSING RED LIGHT ON THE END. INSTALLED RED EMERGENCY LIGHT AND TRACK. 2 L 7 2 4T 4 T RT A31SO E20NE 2008011100107 20080111 00107 EA 2008 1 11 QXEA200702016 1 20071222 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE ILLUMINATED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 617QX 10130 FLIGHT 2548, RECEIVED A PROX SYSTEM FAULT STATUS MESSAGE. RETURNED TO THE GATE. MAINTENANCE PLACED THE SYSTEM ON MEL 52 -70-5. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008011100130 20080111 00130 CE 2008 1 11 AMWA071130025 1 20071210 A 5720 DOUBLER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE WS 67 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 127ZV 25394 UE127 AFT ACM SCREEN ASSEMBLY CHAFING INTO DOUBLER P/N 114-120022-11 IN RT WING CENTER SECTION AT WS 67.05. REPAIRED IAW SRM 5 1-40-02 AND CLEARED DISCREPANCY. 2 L 7 2 4T 4 T RT A24CE E26NE 2008011100141 20080111 00141 CE 2008 1 11 ACE122407 1 20071224 A 3245 G195X6758 TUBE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA NLG TIRE FAILED E YADA O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 AL 03 111AX 127 UC81 PILOT STOPPED AIRCRAFT ON TAXIWAY DUE NOSE TIE VIBRATION. REPLACED FLAT NOSE TIRE. TEARDOWN INSPECTION OF TIRE INDICAT ED A BURST TUBE AT A INSTALLATION FOLD. INSPECTION OF TUBE MATERIAL AT BURST AREA APPEARED TO RESEMBLE A CRACK MORE THA N A TEAR. THIS IS THIS WAS THE LATEST OF A STRING OF FLAT TIRES FOR UNDETERMINED REASONS. 2 L 7 2 4T 4 T RT A24CE E4EA 2008011100149 20080111 00149 EU 2008 1 11 Y2LA200700002 1 20070911 A 2120 UNKNOWN AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE CABIN SMOKE A Y2LA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 553SX 3171 WHILE STARTING ENG 1 AFTER ENG 2 START ECAM GAVE VENT AVNCS SYST FAULT. AS WE STARTED TO TROUBLESHOOT AND WERE PULLING FCOM UP, FLIGHT ATTENDANTS IN AFT REPORTED DETECTED SMOKE. FIRE DEPARTMENT WAS ASKED TO RESPOND AND PASSENGERS WERE DEPL ANED VIA L1 AND L2 BY AIRSTAIRS. 2 L 7 2 4F 4 F RT A28NM E37NE 2008011100169 20080111 00169 SW 2008 1 11 HKGA269591 1 20071224 A 5100 NONE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL NONE NONE E HKGA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 17 26959 AC662B PILOT REPORTED SMOKEY ODOR IN COCKPIT AND CABIN AREA, (HAZE). AN EMERGENCY WAS DECLARED, AND RETURNED TO DEPARTURE. MX ACCOMPLISHED ENGINE & BLEED SYSTEM AND CHECKS NORMAL, FULL COLD TO FULL HOT, AUTO & MANUAL WITH NO HAZE OR SMOKE NOTED. RT ENGINE & BLEED SYSTEM OPERATIONAL CHECKS WERE NORMAL, FULL COLD TO FULL HOT, AUTO & MANUAL WITH NO HAZE OR SMOKE NOTE D. BOTH ENGINE AND BLEED SYSTEMS WERE CHECKED TOGETHER FROM FULL COLD TO FULL HOT IN AUTO MODE WITH NO HAZE OR SMOKE NOT ED. DURING MANUAL SETTING AT FULL HOT DURING COMBINED SYSTEM CHECKS MAINTENANCE NOTED THAT WHEN THE INTERIOR TEMP OF THE AIRCRAFT WAS APPROACHING (UNBEARABLE), MINOR HAZE OBSERVED. AS THE TEMP ALLOWED TO COOL, THE HAZE DISSIPATED. IT IS SUS 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P61GL 2008011100200 20080111 00200 NM 2008 1 11 ASMF200712004 1 20071223 A 2740 TRIM SYSTEM BOEING 737 737* NM CFMINT CFM567 CFM567B22 13802 NE MALFUNCTIONED W ASMF O OTHER F FLT CONT AFFECTED CL CLIMB 1 SW 23 850AM 33786 CAPTAIN REPORTED THAT THE STABILIZER TRIM DID NOT HOLD ITS POSITION IN FLIGHT (FMR 274-130-00). MAINTENANCE PERSONNEL PE RFORMED A DETAILED VISUAL INSPECTION TO THE STABILIZER TRIM BALL NUT AND JACKSCREW GEARBOX IAW MM 27-41-81, NO DAMAGES W ERE FOUND. ADDITIONALLY, PERFORMED THE TEST TO DIGITAL FLIGHT CONTROL SYSTEM IAW MM 22-11-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2008011100204 20080111 00204 EA 2008 1 11 COMA0760747 1 20071231 A 3040 16591 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 436CA 18100 7482 FLIGHT 5027 - RECEIVED LEFT WINDOW HEAT CAUTION MESSAGE. DIVERTED TO BOS, LANDED WITHOUT INCIDENT. REPLACED LEFT WINDO W HEAT CONTROLLER. 2 L 7 2 4F RT A21EA 2008011100265 20080111 00265 EA 2008 1 11 MASA200700676 1 20071007 A 3350 AE20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27172 7172 ASH 7338 - ORD - REPORTED THE EMERGENCY EXIT LIGHTS WILL NOT ILLUMINATE. MX REPLACED BATTERY PACKS, OPS NORMAL. 2 L 7 2 4F RT A21EA 2008011100266 20080111 00266 EA 2008 1 11 MASA200700681 1 20071011 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27318 7318 ASH FLT 2796, PHX, CREW WROTE UP THAT THE EMERGENCY EXIT SIDEWALL LIGHTS AT ROW 8 WERE INOP. MX WAS CALLED OUT TO PLANE AND PERFORMED OP CHECK, OP CHECK WAS GOOD. 2 L 7 2 4F RT A21EA 2008011100272 20080111 00272 SO 2008 1 11 CHQA200800003 1 20070102 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LAVATORY MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 575RP 145847 CAE312676 CVG TO IND - DURING TAKEOFF A "LAV SMOKE" EICAS MESSAGE WAS DISPLAYED AT APPROXIMATELY 1500 FEET. THE FLIGHT CREW PREP ARED TO RETURN TO FIELD AND PERFORMED THE APPLICABLE QRH CHECK LISTS. THE FLIGHT ATTENDANT REPORTED THAT THERE WAS NO V ISIBLE SMOKE OR ODOR COMING FROM THE LAVATORY. THE AIRCRAFT LANDED WITHOUT INCIDENT AND WAS TURNED OVER TO MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR, RAN BOTH ENGINES AND COULD NOT DUPLICATE THE FAULT. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008011100275 20080111 00275 NE 2008 1 11 MASA200700655 2 20070929 A 7532 311669101 BLEED VALVE DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE NR 1 ENGINE MALFUNCTIONED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 437YV 6644 437 TM123319 ASH FLT 2962 PHX-GYM - AFTER 1 ENGINE START COCKPIT FILLED WITH SMOKE AFTER BLEED ON. REMOVED AND REPLACED HPV, P2.5 SW ITCH VALVE, AND IBV. CLEANED GAS GEN, ICC FITTINGS AND DRAIN. 2 H 7 2 4T 4 T RT A13NM E20NE 2008011100296 20080111 00296 NM 2008 1 11 DLM90071652 1 20071221 A 5330 SKIN DOUG MD90 MD9030 3023690 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 LT FUSELAGE STA 219 LONGERON 17L DENT. REPAIRED DENTS IAW MD-80 SRM 53-14D FIG 12B ON N/R 2000-0040AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2008011100299 20080111 00299 CE 2008 1 11 DJFA2007152 1 20071229 A 2497 TERMINAL BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE BUSS LOOSE E DJFA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 23 783TA RK234 ON CLIMB OUT CREW REPORTED A BURNING ODOR FROM THE PILOT'S CIRCUIT BREAKER PANEL. MAINTENANCE FOUND A LOOSE TERMIAL ON A CIRCUIT BREAKER ON THE NON-ESSENTIAL BUSS. THE TERMIAL APPEARED TO BE OVERHEATED AND WAS REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2008011100306 20080111 00306 NM 2008 1 11 DL76L071661 1 20071227 A 5320 7075T73511 FLOOR SUPPORT BOEING 767 767332 1382001 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 171DN 24759 CABIN BS 999 RBL 33 FLR SUPPORT CRACKED, CABIN BS 910-999 RBL33 FLR SUPPORT REPAIRED PER SRM 53-00-51 FIG 201. REPAIR 3 AND AREA TREAT AND PAINT PER AMM 51-21-10. 2 L 7 2 4F RT A1NM 2008011400019 20080114 00019 NM 2008 1 14 AMTA200800003 1 20071228 A 3397 CONNECTOR BOEING 737 73783N 13844HI NM EMERGENCY LIGHTS LOOSE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 315TZ 28245 FWD ESCAPE SLIDE LIGHT INOPERATIVE (L1 DOOR). T/S IAW WDM 33-51-12 FOUND CONNECTOR D11074 NOT PROPERLY SECURED. SECURE D CONNECTOR LIGHT OPS CHECK NORMAL. (K) 2 L 7 2 4F RT A16WE 2008011400023 20080114 00023 CE 2008 1 14 DXTA200702629 1 20071126 A 3150 WARNING LIGHT CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 681QS 5605181 FLAP OVERSPEED ON DEPARTURE CLIMB. COMPLIED WITH FLAP OVERSPEED INSPECTION IAW MM 5-50-00 NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008011400036 20080114 00036 CE 2008 1 14 GUUA12200702 1 20071220 A 5220 DOOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA EMERGENCY EXIT INOPERATIVE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87552 UE216 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT FWD EMERGENCY EXIT DOOR WILL NOT OPEN. READJUSTED RT FWD EMERGENCY E XIT. 2 L 7 2 4T 3 T RT A24CE E2NE 2008011400040 20080114 00040 EA 2008 1 14 TVMA54181207 1 20071220 A 5610 6003303026 WINDSHIELD CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF34* 30015 NE COCKPIT DELAMINATED E TVMA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 EA 03 604CR 4019 5418 COPILOTS FWD WINDSHIELD DELAMINATED OUTER LAYER APPROXIMATELY 1.5 FT VERTICAL PLANE X 1FT WIDE AND DEPARTED AIRCRAFT. 2 L 7 2 4F 4 F RT A21EA 2008011400063 20080114 00063 EU 2008 1 14 COEA0747821 1 20070824 A 5310 S53575112209 CREASE BEAM AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK, MAJOR REPAIR AND LEVEL 2 CORROSION ON RT CREASE BEAM, IB ANGLE WHERE IT ATTACHES TO FRAME 27. REPLACED WITH NEW, THE FWD END OF THE CORD ANGLE. CUT OFF THE FWD 20 INCHES OF THE ANGLE AND ADDED A SINGLE SPLICE TO THE ANGLE AT THE CUT. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400079 20080114 00079 CE 2008 1 14 AMWA89204 1 20071220 A 3230 1143640681 PCB BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MLG INOPERATIVE A AMWA O OTHER S AFFECT SYSTEMS AP APPROACH 1 CE 07 126YV 20671 308 UE126 LANDING GEAR GAVE NO REACTION WHEN GEAR HANDLE EXTENDED. MOVED FLAPS TO FULL DOWN, LANDING GEAR WARNING HORN SOUNDED. FO LLOWED EMERGENCY CHECKLIST AND MANUALLY EXTENDED THE GEAR AND GOT 3 GEAR SAFE INDICATION LIGHTS AND LANDED SAFELY. MAINT ENANCE REPLACED A316 PC BOARD AND CLEARED DISCREPANCY. 2 L 7 2 4T 3 T RT A24CE E2NE 2008011400093 20080114 00093 SO 2008 1 14 DUFA041007001 2 20070410 A 8530 6461401 STUD CESSNA 404 404 2075901 CE CONT O520 GTSIO520M 17032 SO NR 5 CYLINDER SHEARED E DUFA E ENGINE SHUTDOWN E VIBRATION/BUFFET AP APPROACH 1 GL 27 80BS 641 46 4040048 292223R WHILE ON APPROACH TO AIRPORT, THE PILOT NOTICED MANIFOLD PRESSURE DROPPING AS WELL AS OIL PRESSURE FROM THE RT ENGINE. H E ALSO BEGAN TO FEEL A VIBRATION FROM THE SAME ENGINE. HE ELECTED TO SHUT THE ENGINE DOWN AND MADE AN UNEVENTFUL LANDING . UPON INSPECTION, THE NR 5 CYLINDER HOLD DOWN STUDS HAD SHEARED AND ALLOWED THE CYLINDER TO HAMMER AGAINST THE ENGINE C ASE AND COWLING. THIS IN TURN RIPPED THE RT EXHAUST STACK FROM THE NR 1 AND NR 5 CYLINDERS CAUSING HEAT DISTRESS AT THE COWL DOOR. 1 L 7 2 3O 3 O RT A25CE E7CE 2008011400100 20080114 00100 NM 2008 1 14 AMTA200700726 1 20071228 A 3350 ADD71701100 BATTERY BOEING 737 73783N 13844HI NM EMERGENCY LIGHTS INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 315TZ 28245 FWD LT SIDE EMERGENCY BATTERY PACK IS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06-02 OPS CHECK GOOD . (K) 2 L 7 2 4F RT A16WE 2008011400102 20080114 00102 EU 2008 1 14 COEA0740821 1 20070821 A 5320 S53371316210 INTERCOSTAL AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. MAJOR REPAIR. LEVEL 2 CORROSION ON INTERCOSTAL BETWEEN RT FRAMES 18 AND 19 AT STRINGER 12A. FORMED AND HEAT TREATED REPLACEMENT INTERCOSTAL. WO 72242, NR 200003. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400129 20080114 00129 NE 2008 1 14 NSVA20070126 2 20070506 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT FOD A NSVA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 EA 27 196CJ 196 785217 LT IGNITION LIGHT STAYED ILLUMINATED DURING TAKEOFF ROLL EXTINGUISHED AFTER P/L BROUGHT BACK TO IDLE ABORTED TAKEOFF. F OUND PAPER IN INLET AT 1:00 COVER ABOUT 4 BLADE AT 80 PERCENT. REMOVED AND INSPECTED, NO DAMAGE. PERFORMED OPS CHECK, OPS CHECK NO GOOD IAW GE 72-00-00 SPECIAL PROCEDURES 013 NOTE "C". REMOVED AND REPLACED LT ENGINE IAW COLGAN WC 71-00-0 1, ENGINE MODEL CT7-9B, SN OFF GE-E-785212, SN ON GE-E-785240. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011400132 20080114 00132 EU 2008 1 14 NSVA20070160 1 20070622 A 2842 4000800000105 PROBE SAAB SF340 340B 7860101 EU FUEL QTY MALFUNCTIONED A NSVA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 27 196CJ 340B196 FUEL IMBALANCE, TRIED TO X-FEED BUT IMBALANCE REMAINED. VERIFIED FUEL LOAD IS EQUAL ON BOTH SIDES BY UTILIZING MAGNETIC DIPSTICKS TO ENSURE DISCREPANCY IS INDICATION ONLY. REMOVED AND REPLACED LT WING OUTBD FUEL QUANTITY PROBE. 2 L 7 2 4T RT A52EU 2008011400137 20080114 00137 EU 2008 1 14 NSVA20070055 1 20070302 A 2921 3268 DUMP VALVE SAAB SF340 340B 7860101 EU HYD SYSTEM MALFUNCTIONED A NSVA O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 237MJ 237 EMERGENCY ACCUMULATOR BLEEDING DOWN IN FLIGHT. INSPECTED HYD SYSTEM ACCUM FOR OBVIOUS DAMAGE AND LEAKS. REMOVED AND RE PLACED HYD DUMP VALVE IAW SAAB AMM 29-10-35, OPS CHECK GOOD, NO OTHER DISCREPANCIES NOTED P/N 3268, S/N ON: 267, S/N OFF : UNK. 2 L 7 2 4T RT A52EU 2008011400144 20080114 00144 EU 2008 1 14 NSVA20070144 1 20070531 A 2611 CGA120101 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A NSVA B F EMER. DESCENT ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 EA 27 352CJ 352 CARGO SMOKE FIRE LIGHT CAME ON IN FLIGHT, EXTINGUISHED FIRE, THE LIGHT CAME ON AGAIN AND USED NR 2 EXTRA EXTINGUISHER. REMOVED AND REPLACED CARGO SMOKE DETECTORS IAW AMM 26-13-15. PN ON/OFF CGA1201-01, SN ON 416, SN OFF 0395, AFT SN ON 187 , SN OFF 508. ALSO, REMOVED AND REPLACED LT AND RT FIRE BOTTLES IAW AMM 26-23-10-4, PN OFF/ON 36500007-1, RT SN OFF 201 94D1, RT SN ON 22662D1. LT SN OFF 19257D1, LT SN ON 15263D1. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011400154 20080114 00154 EU 2008 1 14 NSVA20070124 1 20070508 A 6123 1103P0620 PRESSURE SWITCH SAAB SF340 340B 7860101 EU P3 MALFUNCTIONED A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 191MJ 191 AUTO COARSEN WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. REMOVED AND REPLACED RT PRESSURE SWITCH P3 P/N ON AND OFF 1 103P0620 S/N ON 1595 IAW MM 61-22-10-02. REMOVED AND REPLACED LT P3 SWITCH IAW AMM 61-22-10-02. OPS CHECK GOOD, PN ON/ OFF 1103P0620, SN OFF 1545, SN ON 2054. 2 L 7 2 4T RT A52EU 2008011400156 20080114 00156 EU 2008 1 14 NSVA20070058 1 20070311 A 2697 WIRE HARNESS SAAB SF340 340B 7860101 EU TAIL PIPE SENSOR DEFECTIVE A NSVA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 239CJ 239 LEFT TAIL PIPE HOT LIGHT ILLUMINATED. ENGINES WERE NOT STARTED. RESACKED WEU FOUND TAILPIPE SENSOR AT 9 O'CLOCK POSITI ON BAD. REMOVED LT EXHAUST FAIRING, FOUND DEFECTIVE HARNESS. INSTALLED SERVICEABLE LT EXHAUST FAIRING. OPS CHECK SAT PN 7271125-501, NSN REF SAAB AMM 54-30-05, PN: 7271125-501. 2 L 7 2 4T RT A52EU 2008011400159 20080114 00159 CE 2008 1 14 NSVA20070161 1 20070622 A 3297 CONNECTOR BEECH 1900 1900D 1154162 CE MLG HANDLE UNSECURE A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 155CJ UE55 UPPER BULB IN MLG HANDLE INOP. RELAMPED WITH NO HELP. CHECKED AND SECURED CONNECTORS ON PCB AND LDG HANDLE WIRES AND P ERFORMED OPS CHK IAW AMM 32-60-00 GOOD. 2 L 7 2 4T RT A24CE 2008011400176 20080114 00176 EU 2008 1 14 NSVA20070116 1 20070426 A 2697 CONNECTOR SAAB SF340 340B 7860101 EU FIRE LIGHT LOOSE A NSVA O OTHER L NO TEST TX TAXI/GRND HDL 1 EA 27 194CJ 194 LT ENGINE FIRE DETECT SYSTEM FAILED TEST ON FIRST FLIGHT OF THE DAY CHECKS. LT FIRE LIGHTS ON HANDLE AND CWP WILL NOT I LLUMINATE. SECURED LOOSE CONNECTION AT CONTROL BOX. OP CHECKS GOOD IAW SMM. 2 L 7 2 4T RT A52EU 2008011400178 20080114 00178 EU 2008 1 14 NSVA20070072 1 20070323 A 2770 MS253481 SWITCH SAAB SF340 340B 7860101 EU GUST LOCK MALFUNCTIONED A NSVA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 311CE 214 GUST LOCK ANNUNCIATOR ILLUMINATED BEFORE TAKEOFF. REMOVED AND REPLACED GUST LOCK MICRO SWITCH AND ADJUSTED ACTUATOR SPR ING TENSION AND MICRO SWITCH GAP IAW AMM 27-72-15-05, PN ON/OFF MS25348-1. 2 L 7 2 4T RT A52EU 2008011400185 20080114 00185 EU 2008 1 14 NSVA20070050 1 20070227 A 3350 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 350CJ 350 EMERGENCY LIGHTS OPERATING IMPROPERLY. REPLACED NR 1, 2, 3, 4 AND 5 EMERGENCY LIGHTS POWER SUPPLIES IAW W/C 33-50-02S. OPS CHECK GOOD, POS NR 1-21 LN PN: 60-1321-1, SN ON: 18253, SN OFF: 2012, POS NR 2-20 LN, PN: 60-1321-1, SN ON:21036, S N OFF: 16604, POS NR 3-22 LN, PN: 60-1321-1, SN ON: 18219, SN OFF: 19815, POS NR 4-23 LN, PN: 60-1321-1, SN ON: 21548, S N OFF: 20729, POS NR 5-24 LN, PN: 60-1321-1, SN, ON: 12123, SN OFF: 17622. 2 L 7 2 4T RT A52EU 2008011400190 20080114 00190 CE 2008 1 14 NSVA20070051 1 20070227 A 3297 CONNECTOR BEECH 1900 1900D 1154162 CE MLG CORRODED A NSVA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 124CJ UE24 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. CLEARED CORROSION FROM A10881 CONNECTOR, PINS 5/9 P NR ZONE 521, OPS CK G OOD IAW 32-60-05. 2 L 7 2 4T RT A24CE 2008011500011 20080115 00011 EU 2008 1 15 NSVA20070172 1 20070629 A 3297 CIRCUIT BREAKER SAAB SF340 340B 7860101 EU MLG TRIPPED A NSVA O OTHER O OTHER AP APPROACH 1 EA 27 350CJ 340B350 ON APPROACH HAD GEAR UNSAFE INDICATION. CREW NOTICED CB F-7 WAS POPPED. RESET POPPED CB F-7 BREAKER GEAR OPERATED NORM ALLY AIRCRAFT LANDED WITHOUT INCIDENT. NO OTHER PROBLEMS FOUND. 2 L 7 2 4T RT A52EU 2008011500043 20080115 00043 EU 2008 1 15 NSVA20070056 1 20070308 A 7700 N7239060503 CONTROL PANEL SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CTOT MALFUNCTIONED A NSVA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 321CJ 321 LT ENG CAME OFF CTOT/APR ON TAKEOFF, TORQUE FELL FROM 85 PERCENT TO 40 PERCENT. REMOVED AND REPLACED CTOT CONTROL PANEL IAW SAAB AMM 76-10-50-04. OPS CHECK GOOD. P/N7239060503, S/N ON 206244, S/N OFF 0275 A/P 543250726. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011500048 20080115 00048 EU 2008 1 15 NSVA20070196 1 20070725 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 347CJ 347 20NL EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED POWER SUPPLY PN ON/OFF 60-1321-1, SN OFF 9062. OPS CHEC K GOOD. 2 L 7 2 4T RT A52EU 2008011500066 20080115 00066 EU 2008 1 15 NSVA20070108 1 20070420 A 2700 531706 CONTROL QUADRANT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE MALFUNCTIONED A NSVA O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 210CJ 210 "FI STOP OPEN" ILLUMINATED IN FLIGHT UPON GEAR UP. PERFORMED FAULT ISOLATION OF FI STOP AMBER LIGHT ON SHEET 2 FIG 102. FOUND TO FAIL RELAY CONT CHECK. REMOVED AND REPLACED RELAY 20GA STILL NO FIX, CHECKED WIRES AT DOWN LOCK SWITCH HARNE SS, FOUND OPEN GROUND. REMOVED AND REPLACED DOWN LOCK SWITCH HARNESS IAW SAAB MM 32-61-05. OPS CHECK GOOD PN ON/OFF AI R130902 SN ON TALL31212332F SN OFF UNKNOWN. UPON FURTHER TROUBLESHOOTING FOUND QUADRANT POWER LEVERS TO ACTIVATE FI BLU E LIGHT WHEN A/C IS IN FLIGHT MODE AND BY SHACKING LEVERS THE AMBER FI LIGHT ILLUMINATES SUSPECT QUADRANT, SWITCHES IMPR OPERLY FUNCTIONING POD PN 53162-4. REMOVED CONTROL QUADRANT ASSY IAW AMM 76-10-05. INSTALL CONTROL QUADRANT UP TO AND 2 L 7 2 4T 4 T RT A52EU E8NE 2008011500065 20080115 00065 WP 2008 1 15 UPS08851363 1 20071227 A 5512 SKIN DOUG DC8 DC871F 302199D WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 CRACKED FASTENER HOLE ON LT HORIZONTAL STAB T/E LIGHTENING HOLE OUTBOARD OF NR 1 ELEV ATTACH BRACKET. FABRICATED AND INSTALLED REPAIR DOUBLER ON LT HORIZONTAL STAB T/E AT STA XET 21.471 IAW DWG 5652086, AND SRM 55-2-0. 2 L 7 4 4F RT 4A25 2008011500070 20080115 00070 NM 2008 1 15 UPS08M51365 1 20071027 A 5754 RIB DOUG MD11 MD11F 3023600 NM L/E SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C RIGHT WING L/E SLAT TRACK 16, I/B RIB FOUND CRACKED AS MARKED. RIGHT WING 8 SLAT CABLES REMOVED. NR 16 SLAT TRACK, DOOR, BRACKET, PULLEY, HARDWARES, BEARINGS 4EA & I/B RIB REMOVED. NEW RIB INSTALLED PER SRM 51-31-01 VII R35. RIGHT WING 16 SLAT TRACK BEARINGS, BRACKET, PULLEY & ATTACHING HARDWARES INSTALLED. RIGHT WING NR 16 SLAT TRACK & DOOR INSTALLED. NR 8 SLAT CABLES INSTALLED. FUNCTION CHECK ON NR 16 SLAT TRACK, DOOR & CABLE RIGGING SATIS. 2 L 7 3 4F RT A22WE 2008011500076 20080115 00076 CE 2008 1 15 NSVA20070133 1 20070521 A 2750 FLAP SYSTEM BEECH 1900 1900D 1154162 CE TE FLAPS MALFUNCTIONED A NSVA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 EA 27 171CJ UE71 FLAPS WOULD NOT RETRACT AFTER LANDING. MAINTENANCE RETURNED FLAPS TO FULL UP POSITION AND OPENED MEL. 2 L 7 2 4T RT A24CE 2008011500080 20080115 00080 NM 2008 1 15 USAA920080069 1 20071130 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 663, S1. REPAIRED FRAME, BS 663, S1 IAW USAIRWAYS EA 100069. 2 L 7 2 4F RT A16WE 2008011500089 20080115 00089 NM 2008 1 15 USAA920080077 1 20071210 A 5240 6545871523 SKIN BOEING 737 7373G7 1384595 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - FORWARD SERVICE DOOR SKIN CRACKED AT THE 3RD FROM TOP STOP FITTING CUT OUT. REPAIRED T HE FORWARD SERVICE DOOR SKIN AT THE 3RD FROM TOP STOP FITTING CUTOUT IAW B737 SRM 51-70-11. 2 L 7 2 4F RT A16WE 2008011500106 20080115 00106 EU 2008 1 15 NSVA20070208 1 20070809 A 7603 POWER LEVER SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE OUT OF RIG A NSVA O OTHER O OTHER CR CRUISE 1 EA 27 344CJ 344 RT ENG IS SURGING IN FLIGHT ABOUT 590 FLUCTUATION ON TRQ IN FLIGHT AND PROP FLUCTUATES FROM 1230 TO 1250 RPM. REMOVED A ND REPLACED NR 2 ENG PCU IAW AMM 61-20-05 PN ON 782490-52, PN OFF 728490-55, SN ON 901033, SN OFF 960116. RAN RT ENG AN D FOUND TO BE OUT OF RIG PCU LEAK CHECK GOOD RIGGED LEVER FOUND PWR LEVER OUT OF RIG, RE-RIGGED AS WELL IAW AMM 76-10-00 . RAN RT ENG OPS CHK GOOD FOR INSTALLATION, LEAK CHK AND RIGGING OF PCU AND HHU. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011500107 20080115 00107 EU 2008 1 15 NSVA20070201 1 20070805 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 339CJ 338 DURING OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM ON A LINE CHECK, ALL OF THE EMERGENCY LIGHTS WERE FOUND NOT TO BE WORKING. REMOVED AND REPLACED ALL FIVE OF THE EMERGENCY POWER SUPPLY’S, SYSTEM OPS CHECKED GOOD, PN 60-1321-1. 2 L 7 2 4T RT A52EU 2008011500109 20080115 00109 EU 2008 1 15 NSVA20070245 1 20071204 A 3350 7239410802 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 210CJ 340B210 EMERGENCY AISLE LIGHT AT 4DF INOP, FOUND DURING LINE CHECK NR 1. REMOVED AND REPLACED LIGHT ASSEMBLY. SYSTEM OPERATION AL CHECK IS GOOD. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4T RT A52EU 2008011500119 20080115 00119 NM 2008 1 15 USAA920080088 1 20071221 A 5313 6551698 STRINGER SPLICE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED STRINGER SPLICE, BS 907, S4L. REPLACED STRINGER SPLICE, BS 907, S4L IAW B737 S RM 51-10-02. 2 L 7 2 4F RT A16WE 2008011500127 20080115 00127 2008 1 15 NSVA20070231 3 20070923 A 6197 CONNECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE PROP OIL TEMP DIRTY A NSVA D RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 299CJ 299 LT PROP OIL TEMP GAUGE EXCEEDED IT'S LIMITS, SUDDEN FULL SCALE DEFLECTION. CLEANED CONNECTION ON LT PROP OIL/TEMP GAUGE . OP CHECK GOOD 79-30-15. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011500134 20080115 00134 NM 2008 1 15 USAA920080099 1 20071220 A 5320 ATTACH ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED ANGLE, BS 360, S16L. REPAIRED ANGLE, BS 360, S16L IAW B737 SRM 53-10-04-2R. 2 L 7 2 4F RT A16WE 2008011500137 20080115 00137 NM 2008 1 15 USAA920080101 1 20071202 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED INTERCOSTAL, BS 294 - BS 308, S16L. REPLACED INTERCOSTAL, BS 294 - BS 308, S16 L IAW B737 SRM 51-40-03. 2 L 7 2 4F RT A16WE 2008011500138 20080115 00138 NM 2008 1 15 USAA920080102 1 20071213 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED INTERCOSTAL WEB, BS 295, S12L. REPLACED INTERCOSTAL WEB, BS 295, S12L IAW B737 SRM 51-40-03. 2 L 7 2 4F RT A16WE 2008011500145 20080115 00145 NM 2008 1 15 USAA920080106 1 20071206 A 5313 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED STRINGER CLIP, BS 597, S8L. REPLACED STRINGER CLIP, BS 597, S8L IAW B737 SRM 5 1-20-00. 2 L 7 2 4F RT A16WE 2008011500146 20080115 00146 NM 2008 1 15 USAA920080107 1 20071228 A 5322 6624124 SHEAR TIE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED SHEAR TIE, BS 616, S8L - S9L. REPLACED SHEAR TIE, BS 616, S8L - S9L IAW BOEING DRAWING 66-24124. 2 L 7 2 4F RT A16WE 2008011500149 20080115 00149 2008 1 15 NSVA20070199 4 20070729 A 3414 6225353011 INDICATOR SAAB SF340 340B 7860101 EU AIRSPEED FAILED A NSVA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 EA 27 220MJ 220 CAPT AIRSPEED INDICATOR FAILED, ABORTED AT APPROX 3040KTS. REMOVED AND REPLACED CAPT AIRSPEED INDICATOR IAW SMM 34-12-1 5, PN ON /OFF 622-5353-011SN ON 285, SN OFF 20, OPS CHK GOOD. 2 L 7 2 4T RT A52EU 2008011500150 20080115 00150 NM 2008 1 15 USAA920080109 1 20071228 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FLOORBEAM, BS 665 - BS 669, LBL 24. REPAIRED FLOORBEAM, BS 665 - BS 669, LBL 2 4 IAW USAIRWAYS EA 100085. 2 L 7 2 4F RT A16WE 2008011500159 20080115 00159 NM 2008 1 15 USAA920080124 1 20071202 A 5320 66142081 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED INTERCOSTAL WEB, BS 295, S11L. REPAIRED INTERCOSTAL WEB, BS 295, S11L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008011500163 20080115 00163 EU 2008 1 15 NSVA20070246 1 20071205 A 3350 6013212 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 370PX 340B300 FLOOR EMERGENCY LIGHTS ROW 5/6 ARE INOP, 3 CONSECUTIVE. REPLACED POWER SUPPLY. 2 L 7 2 4T RT A52EU 2008011500169 20080115 00169 EU 2008 1 15 NSVA20070241 1 20071014 A 6123 78249055 PCU SAAB SF340 340B 7860101 EU LT ENGINE UNKNOWN A NSVA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 198CJ 340B198 ABORTED TAKEOFF 45KTS, LT ENGINE POSSIBLE AUTOCOARSEN. REMOVED AND REPLACED LT PCU IAW CWC 61-20-06S. PERFORM OPERATIO NAL TEST OF PCU IAW SAAB AMM 71-00-00-05-1, OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011500192 20080115 00192 2008 1 15 VNAA0712001 4 20071215 A 2360 STATIC WICK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE DAMAGED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 207PS 7873 CREW REPORTED A LIGHTNING STRIKE. MAINTENANCE PERFORMED A DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE FOUND TWO DAMAGED STATIC WICKS. MAINTENANCE REPAIRED ALL DAMAGE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008011500231 20080115 00231 EA 2008 1 15 MASA200700516 1 20070822 A 5210 SEAL CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR OBSTRUCTED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 506MJ 10073 ASH 7001 ORD-IAD - AIRCRAFT REJECTED TAKEOFF DUE TO PAX DOOR WARNING MESSAGE. MX CLEANED DEBRIS FROM PAX DOOR SEAL, OPS GOOD. 2 L 7 2 4F RT A21EA 2008011500235 20080115 00235 EA 2008 1 15 MASA200700579 1 20070913 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS BURNED OUT A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 510MJ 10101 ASH FLT 7178 CLT-IAD - PILOT REPORTED THAT THE RIGHT WING EMERGENCY DOOR FLOOR LEVEL EXIT SIGN HAD 2 BULBS BURNT OUT. MX RELAMPED LIGHTS. 2 L 7 2 4F RT A21EA 2008011500254 20080115 00254 EA 2008 1 15 MASA200700651 1 20070928 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 515MJ 17859 10117 SCHEDULED MX, MX REPORTED THE NR 2 EMERGENCY BATTERY PACK INOP. MX REPLACED THE BATTERY PACK, OPS CK GOOD. 2 L 7 2 4F RT A21EA 2008011500258 20080115 00258 EA 2008 1 15 MASA200700863 1 20071207 A 5210 ROD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR HANDLE OUT OF ADJUST A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77302 7302 ASH 7210 IAD - PAX DOOR OUTER HANDLE CAUTION WHEN DOOR CLOSED FROM INSIDE. MX ADJUSTED OUTER HANDLE ROD. 2 L 7 2 4F RT A21EA 2008011500259 20080115 00259 NM 2008 1 15 MASA200700833 1 20071130 A 3350 2431K20 RELAY DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHTS MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 434YV 434 ASH INBD FLT 7374 DEN - PILOT REPORTED THAT IN START FEATHER, EMERGENCY LIGHTS DISARM CAUTION NOT ILLUMATED WHEN EMERGEN CY LIGHTS IN OFF POSITION. REMOVED AND REPLACED UNDER VOLTAGE RELAY 2431K20. 2 H 7 2 4T RT A13NM 2008011500266 20080115 00266 EA 2008 1 15 MASA200700481 1 20070804 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27173 7173 ASH 7212 ORD - REPORTED ONE CELING EXIT LT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2008011500271 20080115 00271 NM 2008 1 15 MASA200700805 1 20071115 A 2131 21178041 CONTROLLER DHAV DHC8 DHC8202 2809007 NM CABIN PRESSURE MALFUNCTIONED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 436YV 13597 436 ASH FLT 7150 COD - PILOT REPORTED A RAPID DEPRESSURIZATION WITH O2 MASK DROP IN FLIGHT. REPLACED THE CABIN PRESSURE CON TROLLER 2 H 7 2 4T RT A13NM 2008011500279 20080115 00279 EA 2008 1 15 MASA200700478 1 20070803 A 3350 BATTERY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75987 7405 ASH 7190 AVP - EMERGENCY PATH LIGHTING INOP. MX RESET AND RECHARGED SYSTEM, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2008011500297 20080115 00297 EA 2008 1 15 MASA200700700 1 20071014 A 5210 PANEL CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR CRACKED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 912FJ 15012 PAX DOOR FWD AND AFT SIDE PANEL CRACKED AT 2ND STEP. 2 L 7 2 4F RT A21EA 2008011000137 20080110 00137 EU 2008 1 10 TRBA2007114 1 20071216 A 2497 AMP2OW TERMINAL AEROSP ATR72 ATR72212A 8680902 EU PWA PW120 PW127 NE RIGHT ENGINE FAILED A TRBA K NONE O OTHER TX TAXI/GRND HDL 1 SO 29 536AT 536 NR 1 LT ENGINE WOULD NOT START, NO NH WHEN STARTER SELECTED ON. REPLACED TERMINAL END AT 429VN GROUND WIRE IAW AWM STAND ARD PRACTICES 20-27-17. 2 H 7 2 4T 4 T RT A53EU E20NE 2008011000140 20080110 00140 NM 2008 1 10 USAA920080060 1 20071214 A 5754 65C26601179 SKIN BOEING 737 7373G7 1384595 NM L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - LEFT WING NR 1 SLAT LOWER SURFACE IS CRACKED AT ACTUATOR ATTACH AREA. REPAIRED LEFT WI NG NR 1 SLAT LOWER SURFACE AT ACTUATOR ATTACH AREA IAW B737 SRM 57-43-01-2R6. 2 L 7 2 4F RT A16WE 2008011000144 20080110 00144 NM 2008 1 10 USAA920080064 1 20071216 A 5315 STRAP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FLOORBEAM STABILIZER STRAP, BS 312, LBL 45. REPLACED FLOORBEAM STABILZER STRAP , BS 312, LBL 45 IAW B737 SRM 53-10-51. 2 L 7 2 4F RT A16WE 2008011000145 20080110 00145 NM 2008 1 10 USAA920080121 1 20071204 A 5751 65C2591128 AILERON BOEING 737 7373G7 1384595 NM RT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 MCN - MAJOR REPAIR - C16 CHECK - RIGHT WING AILERON HAS AREA OF DELAMINATION, SPAR STATION 479. REPLACED RIGHT WING AIL ERON IAW USAIRWAYS EA 100134. 2 L 7 2 4F RT A16WE 2008011000148 20080110 00148 CE 2008 1 10 DXTA200702708 1 20071222 A 3240 CONTROL BOX CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE E/E BAY INOPERATIVE E DXTA O OTHER O OTHER LD LANDING 1 GL 07 319QS 5600519 ON LANDING AND AFTER APPLYING THE BRAKES, THE BRAKES SEEMED TO GRAB AND WE BEGAN TO SKID. THE RT MAIN TIRE BLEW. AIRCRAF T VEERED TO THE RT SKIDDING OFF THE RWY. NO OTHER DAMAGE TO AIRCRAFT OBSERVED ON POST FLIGHT. REMOVED AND REPLACED ELEC TRONIC CONTROL BOX I.A.W CE-560 MM 32-42-08. PERFORMED FUNCTIONAL TEST ON POWER BRAKE ANTISKID SYSTEM. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2008011000150 20080110 00150 EU 2008 1 10 2007UALA05275 1 20071226 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LOW A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 417UA 483 THE O2 NEEDS SERVICE. SERVICED CREW O2. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011000151 20080110 00151 CE 2008 1 10 DXTA200702709 1 20071222 A 3297 WIRE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE BRAKE DAMAGED E DXTA A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 GL 07 628QS 5605305 AFTER GEAR EXTENSION, RT MAIN GEAR DID NOT INDICATE DOWN AND ASSOCIATED UNLOCK LIGHT DID ILLUMINATE. ATTEMPTED MANUAL G EAR EXTENSION VIA CHECKLIST BUT GEAR STILL INDICATED UNSAFE. NORMAL LANDING AFTER GEAR BLOW DOWN BOTTLE WAS USED. TROU BLESHOT TO BRAKE X1 WIRE AT POWER BRAKE MOTOR RELAY. REPAIRED WIRING. SYSTEM OPERATIONAL CHECK GOOD IAW 560XL M.M. CHA P. 32-42-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008011000172 20080110 00172 NM 2008 1 10 2007UALA05354 1 20071228 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 907-1006 WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 UPPER FUSELAGE CROWN SKIN HAS WEAR DAMAGE AT LT DORSAL FIN STA 907 TO 1006. FABRICATED AND INSTALLED AN EXTERNAL FUSELAG E SKIN DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011000187 20080110 00187 NM 2008 1 10 2007UALA05367 1 20071228 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER CL CLIMB 1 WP 29 527UA 24995 L2 DOOR UPPER HINGE ARM ASSY CUTOUT HAS DAMAGE. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008011100011 20080111 00011 NM 2008 1 11 2007UALA05250 1 20071223 A 3510 MF20010 OXYGEN MASK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT UNSERVICEABLE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 834UA 1420 TOP LEFT STRAP ON CAPT O2 MASK NEEDS INSIDE KEEPER-FASTENER. REPLACED CAPT O2 MASK WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011100037 20080111 00037 NM 2008 1 11 QXEA200701882 1 20071213 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA ILLUMINATED A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 410QX 4053 ON TAXI RECEIVED A YAW DAMPER NOT CENTERED MESSAGE ON BOTH DISPLAYS. RETURNED TO THE GATE. MAINTENANCE CYCLED POWER TO T HE AIRCRAFT. MESSAGES WENT AWAY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2008011100049 20080111 00049 NM 2008 1 11 AMTA200700712 1 20071216 A 4900 COMPUTER BOEING 737 73783N 13844HI NM APU MALFUNCTIONED A AMTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 11 315TZ 28245 APU FAULT LIGHT IS ON WHEN ATTEMPTING TO START APU AND WILL NOT START. RELOADED APU SOFTWARE IAW AMM 49-61-00-2, BITE C HECKS GOOD IAW AMM 49-61-00-700-801. APU STARTS NORMALLY IAW AMM 49-11-00-860-801 WITH NO FAULTS. (K) 2 L 7 2 4F RT A16WE 2008011100051 20080111 00051 NM 2008 1 11 2008UALA0020 1 20071231 A 2611 SMOKE DETECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LAVATORY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 642UA 25092 LAVATORY 101 SMOKE DETECTOR INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008011100063 20080111 00063 SO 2008 1 11 GUUA12140701 1 20071214 A 3260 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE LT MLG DIRTY A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 29 283AS 120236 DURING FLIGHT LANDING GEAR DISAGREEMENT LIGHTS (A) RED ON LT MAIN GEAR AND (A) RED ON NOSE GEAR ILLUMINATED. CLEANED LT MAIN LANDING GEAR AND NOSE LANDING GEAR UPLOCK AND DOWNLOCK PROXIMITY SENSORS. 2 L 7 2 4T 4 T RT A31SO E20NE 2008011100065 20080111 00065 NM 2008 1 11 2008UALA0024 1 20071230 A 2760 WARNING MESSAGE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 221UA 30552 SPOILER EICAS AND FLIGHT CONTROL SYS STATUS MSG ON PUSHBACK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008011100068 20080111 00068 SO 2008 1 11 GUUA12180701 1 20071218 A 3234 12038594001 CONTROL LEVER EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE MLG INTERMITTENT A GUUA O OTHER J WARNING INDICATION CL CLIMB 1 SO 29 283AS 120236 AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. REPLACED LANDING GEAR CONTROL LEVER ASSEMBLY. 2 L 7 2 4T 4 T RT A31SO E20NE 2008011100078 20080111 00078 WP 2008 1 11 FX7A200700007 1 20071218 A 2897 CIRCUIT BREAKER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE CENTER TANK TRIPPED A FX7A O OTHER J WARNING INDICATION CL CLIMB 1 SO 19 905TA 49905 FORWARD CENTER TANK CIRCUIT BREAKER POPPED OUT DURING CLIMB. 2 L 7 2 4F 4 F A6WE E9NE 2008011100129 20080111 00129 CE 2008 1 11 AMWA89107BC 1 20071214 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER DISCHARGED A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 161YV 8259 391 UE161 BATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED BATTERY AND CLEARED DISCREPANCY. 2 L 7 2 4T 4 T RT A24CE E26NE 2008011100224 20080111 00224 EU 2008 1 11 TRBA2007118 1 20071228 A 3350 BULB AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE HAMSTD 247 247F1 NE EMERGENCY LIGHTS FAILED A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 451 451 EMERGENCY LIGHT INOPERATIVE IN THE MAIN ENTRANCE PASSENGER DOOR. MAINTENANCE REPLACED LIGHT BULB. 2 H 7 2 4T 4 T RT A53EU E20NE 6 C P1BO 2008011100286 20080111 00286 EU 2008 1 11 QMLA123107001 1 20071231 A 2110 COMPRESSOR UROCOP EC135 EC135P2 5620027 EU PWA PW206 PW206B 0 NE AIR CONDITIONER STALLED E QMLA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NM 03 230AM 540 AIR CONDITIONER COMPRESSOR STARTED TO MAKE A LOUD NOISE WITH THE SMELL OF RUBBER IN THE COCKPIT, WHILE ON LANDING. TUNED THE AIR CONDITIONER OFF, THE SMELL AND NOISE STOPPED. AFTER LANDING, CALLED MAINTENANCE, FILLED OUT THE MEL DEFERRAL, AND PUT THE AIRCRAFT BACK IN SERVICE. DURING THE MAINTENANCE INSPECTION, THE EARLIER LOUD NOISE AND SMELL COULD NOT BE DUPLICATED. 1 G 7 2 3U 3 U H88EU E42NE 2008011100294 20080111 00294 CE 2008 1 11 Z5FA123007001 1 20071230 A 3297 69480912 WIRE HARNESS CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE MLG DEFECTIVE E Z5FA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 EA 63 621CS 462 6800120 AFTER TAKEOFF, GEAR HANDLE WOULD NOT MOVE TO RETRACT POSITION AND FLIGHT HOUR METER WAS NOT WORKING. CREW CIRCLED IN VI CINITY OF AIRPORT, BURNED OFF FUEL FOR PROPER LANDING WEIGHT AND DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT . MAINTENANCE PERSONNEL FOUND NOSE GEAR SQUAWK SWITCH WIRE BUNDLE DEFECTIVE. NOSE GEAR WIRE BUNDLE WAS FABRICATED AND RE PLACED, OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RC T00012WI E35NE 2008011100300 20080111 00300 CE 2008 1 11 DJFA2007153 1 20071231 A 3260 MS243311 DOWNLOCK SWITCH BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE LT MLG INOPERATIVE E DJFA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 23 463LX 1829 RK426 ON APPROACH CREW REPORTED THE LT MAIN GEAR DOWN AND LOCKED LIGHT WOULD NOT ILLUMINATE. GEAR WAS CYCLED 6 TIMES AND ON T HE 6TH ATTEMPT THE DOWN AND LOCKED LIGHT FINALLY ILLUMINTATED. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED SAFELY. MAIN TENANCE FOUND THE LT MLG DOWNLOCK SWITCH INOPERATIVE. THE SWITCH WAS REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2008011100305 20080111 00305 NM 2008 1 11 DL76L071660 1 20071227 A 5320 7075T6511 FLOOR SUPPORT BOEING 767 767332 1382001 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 171DN 24759 CABIN BS 927-999 LBL33 FLR SUPPORT CRACKED, CABIN BS 910-999 LBL 33 FLR SUPPORT REPAIRED PER SRM 53-00-51 FIG 201. REPA IR 3 AREA, TREAT AND PAINT PER AMM 51-211-10. 2 L 7 2 4F RT A1NM 2008011100319 20080111 00319 2008 1 11 NSVA20070162 4 20070623 A 3418 STALL WARNING SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A NSVA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 311CE 214 PUSHER DISARM LIGHT ILLUMINATED ON GROUND. RESET DISARM SYSTEM, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011100320 20080111 00320 EU 2008 1 11 NSVA20070063 1 20070311 A 3350 BATTERY SAAB SF340 340B 7860101 EU CABIN NOT SEATED A NSVA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 27 334CJ 334 EXIT LIGHT OVER MAIN CABIN DOOR DOES NOT ILLUMINATE. RESEATED BATTERY AND CHECKED FUSES, OPS CHECKED GOOD IAW SAAB MM 3 3-50-00. 2 L 7 2 4T RT A52EU 2008011100321 20080111 00321 CE 2008 1 11 NSVA20070129 1 20070515 A 2612 24409015 FIRE LOOP BEECH 1900 1900D 1154162 CE LT ENGINE DEFECTIVE A NSVA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 27 124CJ UE24 T-HANDLE AND FIRE EXTINGUISHER DISCHARGE LIGHTS DO NOT ILLUMINATE DURING TEST. REMOVED AND REPLACED LT ENG AFT FIRE LOO P, OPS CK GOOD IAW 26-10-01 P/N 244-09015 S/N 034119. 2 L 7 2 4T RT A24CE 2008011400032 20080114 00032 CE 2008 1 14 GUUA12190704 1 20071219 A 5524 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 69547 24915 UE189 DURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED RT ELEVATOR OB HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR OB HINGE BRACKET. 2 L 7 2 4T 3 T RT A24CE E2NE 2008011400061 20080114 00061 EU 2008 1 14 COEA0750821 1 20070827 A 5330 S535713032 SKIN AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 29796 253 FOUND DURING HEAVY CHECK. MAJOR REPAIR, LEVEL 2 CORROSION ON FUSELAGE SKIN UNDER ICE SHIELD AT FASTENER HOLES. SRAS, S 535R0234...4328, NOT DO/TS 5570/07. CUT OUT FUSELAGE SKIN AND FUSELAGE SKIN CROWN PANELS FROM FRAMES 23 TO 23C AND STRI NGERS 1A TO 4L. INSTALLED FACTORY NEW SKIN PANELS AND ADDED SINGLE BUTT SPLICES TO PANELS AT CUTOUT. WO 72242, NR 2000 80. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400062 20080114 00062 EU 2008 1 14 COEA0748821 1 20070824 A 5730 S57112378200 SKIN AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE RT WING CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 29796 253 FOUND DURING HEAVY CHECK. CORROSION ON RT WING LOWER EXTERNAL SKIN PANEL AT FUEL PUMP CUT OUT HOLE, BETWEEN RIBS 4 AND 5. BLENDED CORROSION IAW SRAS DO/ TS-806/04, 2754, NOTE DO/TS-4893/ 07. WO 72241, NR 500002. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400064 20080114 00064 EU 2008 1 14 COEA0760821 1 20070823 A 5322 S53572204205 SHEAR TIE AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE GOUGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 29796 253 FOUND DURING HEAVY CHECK. MAJOR REPAIR: FRAME 24R SHEAR TIE FROM STRINGER 12 TO 13R HAS TOOL DAMAGE. DAMAGED SHEAR TIE CUT AWAY AND SPLICED IN NEW SHEAR TIE SECTION. REPAIR PERFORMED IAW SRAS DO/TS-4747, 4418 AND NOTE DO/TS - 5428/ 07. WO 72242, NR 200008. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400065 20080114 00065 EU 2008 1 14 COEA0759821 1 20070824 A 5310 S53671218204 CREASE BEAM AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. LEVEL 2 CORROSION: CORROSION ON SEVERAL ANGLES ALONG SIDE WALLS WHERE THE FLOOR MEETS FRAMES. 1 IN THE COCKPIT AND 2 IN THE CABIN. REMOVED AND REPLACED THE FOLLOWING STRUCTURES. COCKPIT, FR 13R AND STR 14R CREA SE BEAM ANGLE TIE PN S5307020520001. CABIN, FRAME 36 TO 38L AND STRINGER 15L INTERCOSTAL LWR SUPPORT ANGLE PN S53671218 204. FR 43 TO 44R FLOORBOARD SUPPORT ANGLE PN S5307030922501. WO 72242, NR 200024, 40,46, 47, 57. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400069 20080114 00069 EU 2008 1 14 COEA0753821 1 20070824 A 5310 S53373000212 CREASE BEAM AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 29796 253 FOUND DURING HEAVY CHECK. LEVEL 2 CORROSION: FOUND CORROSION ON THE FOLLOWING RT CREASE BEAM SUPPORTS. INNER CORD ANGL E FROM FRAME 16 TO 18R AND IB SUPPORT CHANNEL BETWEEN FRAMES 16 AND 17R FROM FR 36 TO 38R. REPLACED CORD ANGLE PN S5337 3000212 AND CHANNEL PN S5367800826901. WO 72242, NR 200078, 92. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400088 20080114 00088 SW 2008 1 14 DUFA20070003 1 20070417 A 2613 434422122 OVERHEAT SENSOR SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE3311U 01514 WP LT NACELLE DEFECTIVE E DUFA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 GL 27 159MC AC728B SHORTLY AFTER DEPARTURE, THE LT WING OVERHEAT LIGHT ILLUMINATED. FOLLOWING PROCEDURE, THE PILOT SHUTDOWN THE LT GENERATO R, LT BLEED AIR AND EXTENDED THE LANDING GEAR. THE LIGHT REMAINED ILLUMINATED SO THE LT ENGINE WAS SHUTDOWN AS A PRECAUT IONARY MEASURE AND THE PILOT RETURNED TO FSD AND MADE AN UNEVENTFUL LANDING. AN INVESTIGATION BY MAINTENANCE COULD NOT R EVEAL A CAUSE OTHER THAN A POSSIBLE BRAKE HEATING UP DURING TAXI TO THE RUNWAY OR CABIN TEMP CONTROL SET TO MAX HEAT. MA INTENANCE COULD NOT DUPLICATE. 2 L 7 2 4T 3 T RT A8SW E3WE 2008011400092 20080114 00092 CE 2008 1 14 DUFA081607001 1 20070816 A 3710 DRIVE ASSY CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO VACUUM SYS SHEARED E DUFA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 27 3796C PE6539 402B0803 WHILE IN CRUISE FLIGHT, THE PILOT NOTICED OIL STREAMING FROM THE TOP OF THE LT ENGINE COWL. THE OIL PRESSURE WAS STILL I N THE NORMAL OPERATING RANGE AND THE ENGINE APPEARED TO BE OPERATING NORMALLY. AS A PRECAUTION, THE LT ENGINE WAS SHUTDO WN AND SECURED. THE PILOT DEVIATED TO THE NEAREST AIRPORT WHERE HE MADE AN UNEVENTFUL LANDING. UPON INVESTIGATION BY MA INTENANCE, IT WAS DISCOVERED THAT THE WET SYSTEM VACUUM PUMP DRIVE HAD SHEARED AND CAUSED THE GARLOCK SEAL TO DISINTEGRA TE, ALLOWING OIL TO SEEP PAST IT. 1 L 7 2 3O 3 O A7CE E8CE 2008011400097 20080114 00097 NM 2008 1 14 AMTA200700721 1 20071223 A 5210 GUIDE ARM BOEING 737 73783N 13844HI NM PAX DOOR BROKEN A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 321TZ 28249 FWD ENTRY DOOR L1 GUIDE ARM BROKEN OFF REF IPC 52-11-21-01, ITEM NR 240. REMOVED AND REPLACED IAW AMM 52-11-21-4, OPS N ORMAL, REF ITEM 52-10/66 FOR PRESSURIZATION LEAK CHECK OF DOOR. (K) 2 L 7 2 4F RT A16WE 2008011400098 20080114 00098 NM 2008 1 14 AMTA200700720 1 20071221 A 3150 WARNING LIGHT BOEING 737 73783N 13844HI NM ILLUMINATED A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 315TZ 28245 FFMC FAIL LIGHT ILLUMINATED. PERFORMED BITE ON RT AND LT FMC`S IAW FIM 34-61-00-810-801 NO FAULT FOUND. FMC`S OPERATIO N CHECK NORMAL AT THIS TIME. (K) 2 L 7 2 4F RT A16WE 2008011400099 20080114 00099 NM 2008 1 14 AMTA200700718 1 20071221 A 3350 D71701100 BATTERY BOEING 737 73783N 13844HI NM EMERGENCY LIGHTS INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 305TZ 30706 EMERGENCY LIGHTS AT R1 DOOR INOPERATIVE AT EXTERIOR AND INTERIOR. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT FWD RT POSITION IAW MM 33-51-06-2. OPS CHECK NORMAL. (K) 2 L 7 2 4F RT A16WE 2008011400103 20080114 00103 EU 2008 1 14 COEA0739821 1 20070827 A 5310 S536730002 CREASE BEAM AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 29796 253 FOUND DURING HEAVY CHECK. MAJOR REPAIR. LEVEL 2 CORROSION ON LT OB FLOORBOARD ANGLE, COMMON TO CREASE BEAM. SPLICED I N NEW REPLACEMENT ANGLE SECTION FROM FRAME 34L TO FRAME 36L. WO 72242, NR 200056. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400105 20080114 00105 EU 2008 1 14 COEA0736821 1 20070827 A 5320 S53371227222 INTERCOSTAL AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 29796 253 FOUND DURING HEAVY CHECK. CORROSION ON INTERCOSTAL AT STRINGER 17 LT, BETWEEN FRAMES 13 AND 14. REPLACED WITH NEW FORM ED INTERCOSTAL. WO 72242, NR 200077. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400108 20080114 00108 EU 2008 1 14 COEA0741821 1 20070831 A 5330 S53671305206 SKIN AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 29796 253 FOUND DURING HEAVY CHECK. MAJOR REPAIR. LEVEL 2 CORROSION ON EXTERIOR SKIN, UNDER SERVICE DOOR KICK PANEL. BLENDED OU T CORROSION IAW STRUCTURAL REPAIR APPROVAL SHEET REF DO/TS4026/07, 4275, NOTE DO/TS4178/07. WO 72242, NR 200082. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400111 20080114 00111 2008 1 14 COEA0701720 4 20071207 A 3420 06001700 GYRO CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE FAILED A COEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 13 720FX 208B0452 RETURN TO BLOCKS. FLT NR 8677, DURING TAXI OUT TO RUNWAY ARTIFICIAL HORIZON WOULD NOT ERECT. PILOT ELECTED TO RETURN T O RAMP. REPLACED ARTIFICIAL HORIZON INSTRUMENT. (K) 1 H 7 1 3T 3 T A37CE E4EA 2008011400112 20080114 00112 CE 2008 1 14 COEA0703940 1 20071207 A 2430 200SGL119Q2 GENERATOR CESSNA 208 208B 2073701 CE PWA PT6 PT6A114 52043 NE STANDBY FAILED A COEA H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CR CRUISE 1 NM 13 940FE 208B0040 FLIGHT NR 7511,STAND BY POWER LIGHT CAME ON IN FLIGHT, LOSS OF MAIN GENERATOR. PILOT SELECTED STANDBY ALTERNATOR (ON) A ND CONTINUED WITHOUT ANY OTHER MALFUNCTIONS FROM THIS SYSTEM, AIRCRAFT LANDED SAFELY. REPLACED STARTER GENERATOR. (K) 1 H 7 1 3T 3 T A37CE E4EA 2008011400114 20080114 00114 EU 2008 1 14 COEA0704912 1 20071218 A 7500 E0276CC4FN019 SWITCH AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE BLEED SYS FAILED A COEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 13 912FX 047 AIR TURNBACK. FLIGHT NR 7202. DURING CLIMB 12 MILES OUT, THE NR 2 BLEED VALVE WOULD NOT OPEN AND FAULTED. RESET UNSUCC ESSFUL CREW ELECTED TO RETURN TO DEPARTURE. AC LANDED NORMALLY. REPLACED NR 2 ENGINE BLEED PUSH BUTTON SWITCH. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400115 20080114 00115 NM 2008 1 14 AMTA200700719 1 20071221 A 3150 WARNING LIGHT BOEING 737 73783N 13844HI NM ILLUMINATED A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 315TZ 28245 FMC FAIL LIGHT ILLUMINATED. PERFORMED BITE ON RT AND LT FMC`S IAW FIM 34-61-00-810-801. NO FAULT FOUND. FMC`S OPERATI ON CHECK NORMAL AT THIS TIME. (K) 2 L 7 2 4F RT A16WE 2008011400120 20080114 00120 NE 2008 1 14 NSVA20070131 2 20070515 A 7200 6071T48P04 CABLE ASSY SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE UNKNOWN A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 344CJ 344 LT TQ SURGE WHILE SETTING POWER FOR TAKEOFF. REPLACE BLUE CABLE ON LT ENG P/N 6071T48P04 S/N ON BGAC005, S/N OFF CJWU11 5 IAW G/EMM 74-00-00 PAGE 401-402 RAN A/C IAW SAAB AMM 71-00-00. OPS CKS GOOD ON GROUND AT THIS TIME. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011400121 20080114 00121 CE 2008 1 14 NSVA20070156 1 20070618 A 7931 1013990735 TRANSDUCER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE OIL PRESSURE MALFUNCTIONED A NSVA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 171CJ UE71 RETURN TO GATE, LEFT ENGINE OIL PRESSURE DROPPED TO 60 PSI AND REMAINED AT 60 DURING TAXI OUT. OIL PRESSURE NEEDLE BEGA N BOUNCING BETWEEN 60 PSI AND 110 PSI. REMOVED AND REPLACED OIL PRESSURE TRANSDUCER IAW BMM 1900D 79-50-00-207 RAN LT E NG FOR LEAK AND OPS CHK GOOD, NO LEAKS FOUND PN ON/OFF 101-399073-5, SN OFF 4932-1-145. 2 L 7 2 4T 4 T RT A24CE E26NE 2008011400122 20080114 00122 EU 2008 1 14 NSVA20070117 1 20070426 A 2432 POWER SUPPLY SAAB SF340 340B 7860101 EU EMER BATTERY READS LOW A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 321CJ 321 DC EMERGENCY BUSS POWER SUPPLY VOLTAGES APPEAR LOW. TESTED EMERGENCY BATTERY VOLTAGE IAW SAAB AMM 24-35-00, OPS CHECK G OOD EMERGENCY PWR LIGHTS. 2 L 7 2 4T RT A52EU 2008011400123 20080114 00123 EU 2008 1 14 NSVA20070165 1 20070625 A 3150 WARNING LIGHT SAAB SF340 340B 7860101 EU ILLUMINATED A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 242CJ 242 ABORTED TAKEOFF DUE TO "CONFIG" MASTER WARNING. PERFORMED OPERATIONAL CHECK OF TAKEOFF CONFIGURATION WARNING IAW SAAB 3 40 AMM 31-50-00-05 STEP 3, NO DEFECTS NOTED. 2 L 7 2 4T RT A52EU 2008011400125 20080114 00125 EU 2008 1 14 NSVA20070110 1 20070423 A 2770 MS253481 SWITCH SAAB SF340 340B 7860101 EU GUST LOCK MALFUNCTIONED A NSVA O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 202SR 202 GUST LOCK LIGHT ON DURING FLIGHT CONTROL CHECK. REINSTALLED RUDDER GUST LOCK ACTUATOR IAW SAAB 340 AMM 27-72-10-04, OPS CHECK GOOD TS IAW AMM 72-27-00-00. FOUND WARNING SWITCH 3CF STICKING. REMOVED AND REPLACED GUST LOCK WARNING SW PN MS 25348-1 WITH SERVICEABLE UNIT IAW SAAB 340 AMM 27-72-05-04. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011400126 20080114 00126 EA 2008 1 14 NSVA20070137 2 20070524 A 7321 FUEL CONTROL BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA NR 1 ENGINE MALFUNCTIONED A NSVA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 EA 27 172MJ UE72 ABORTED TAKEOFF DUE TO POWER LOSS ON LT ENG. AT APPROX 40 KNOTS, LT ENG APPEARED TO ROLLBACK TO IDLE. INSPECTED NR 1 E NGINE FUEL CONTROL LINKAGES, GROUND RAN AIRCRAFT IAW PW MM 71-00-00, COULD NOT DUPLICATE DISCREPANCY, OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T 3 T RT A24CE E2NE 2008011400130 20080114 00130 CE 2008 1 14 NSVA20070164 1 20070624 A 5297 CONNECTOR BEECH 1900 1900D 1154162 CE PAX DOOR UNSECURE A NSVA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 243CJ UE43 CABIN DOOR ANNUNCIATOR ILLUMINATED WITH DOOR CLOSED DURING TAKEOFF ROLL. ADJUSTED LATCH, REMOVED AND SECURED CONNECTOR ON DOOR HANDLE MICRO SWITCH, MEL NR 25979 CLEARED ON 6/30/2007. 2 L 7 2 4T RT A24CE 2008011400133 20080114 00133 EU 2008 1 14 NSVA20070105 1 20070417 A 7722 9303262002 INDICATOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ITT DAMAGED A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 321CJ 321 RT ENG ITT DIGITAL APPEARED TO READ 947 DURING TAKEOFF. CREW COLD NOT VERIFY IF ANALOG READING SAME. AFTER ABORT FOUND DIGITAL SEGMENT TO BE MISSING. REMOVED AND REPLACED RT ENGINE TEMP INDICATOR, IAW SAAB AMM 39-40-30-04 OPS CHECK GOOD, P/N ON 10227N01T00 P/N OFF 9303262002 S/N ON 527A S/N OFF 310A EMP- 4253. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011400134 20080114 00134 EU 2008 1 14 NSVA20070134 1 20070521 A 2611 CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A NSVA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 27 35SZ 35 CARGO SMOKE LIGHT WILL NOT EXTINGUISH. REPLACED AFT SMOKE DETECTOR. 2 L 7 2 4T RT A52EU 2008011400138 20080114 00138 EU 2008 1 14 NSVA20070149 1 20070604 A 2611 CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A NSVA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 249CJ 249 CARGO SMOKE LIGHT ON WILL NOT EXTINGUISH. REMOVED AND REPLACED FWD CARGO SMOKE DETECTOR IAW AMM 25-13-15, P/N OFF/ON: C GAB1201-01, S/N OFF: 976, S/N ON: 1238. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011400139 20080114 00139 EU 2008 1 14 NSVA20070085 1 20070405 A 5220 COVER SAAB SF340 340B 7860101 EU EMERGENCY EXIT DISLODGED A NSVA O OTHER O OTHER CR CRUISE 1 EA 27 9CJ 224 LT EMERGENCY EXIT HANDLE COVER FELL OFF IN FLIGHT. SECURED AND RELEASED FOR SERVICE IAW AMM 52-22-00. 2 L 7 2 4T RT A52EU 2008011400140 20080114 00140 EU 2008 1 14 NSVA20070062 1 20070309 A 3297 CONNECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ANTI SKID SYS DISCONNECTED A NSVA O OTHER O OTHER LD LANDING 1 EA 27 277MJ 277 FLIGHT IDLE STOP DID NOT OPEN AFTER LANDING. OVERRIDE PULLED. T/S IAW AMM 76-10-60-01 FIG 111 AND FOUND BOTH CONNECTO RS PLUGS ON THE ANTI-SKID CONTROL BOX DISCONNECTED, RECONNECTED CONNECTORS IAW AMM 32-43-05, OPS CHECKED ANTI-SKID SYSTE M IAW AMM 32-40-00-05 PROCEDURE NR 2 OPS CHECKED GOOD. PERFORMED FLIGHT IDLE STOP SOLENOID TEST IAW 76-10-60-05. OPS C HECKED GOOD, RESET F/I STOP IAW 76-10-60-02 AMM. OPS CHECKED GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011400141 20080114 00141 EU 2008 1 14 NSVA20070065 1 20070314 A 7603 STOP SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FLIGHT IDLE OPEN A NSVA O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 343CJ 343 FLIGHT IDLE STOP OPEN IN FLIGHT. RESET FLIGHT IDLE TOP IAW SAAB MM 76-10-60-02 PER OPERATIONAL OK IAW AMM MM 76-10-60-0 5. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011400146 20080114 00146 CE 2008 1 14 NSVA20070083 1 20070402 A 7603 CONTROL CABLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FUEL CONTROL OUT OF ADJUST A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 124CJ UE24 RT COND LEVER FAILS TO REACH HIGH IDLE POSITION INSPECTED CABLE AT FUEL CONTROL NO BINDING NOTED PERFORMED GROUND RUN OP S CHK VERIFIED NR 2 ENG MAKES LOW IDLE AND FUEL CUTOFF FUNCTIONS NORMAL. ADJUSTED ROD END ON RT CONDITION CABLE AT FCU. RESAFTIED ROD END AND RAN A/C OPS CHK GOOD IAW BMM 76-10-00. 2 L 7 2 4T 4 T RT A24CE E26NE 2008011400147 20080114 00147 EU 2008 1 14 NSVA20070169 1 20070630 A 7931 83465 PRESSURE SWITCH SAAB SF340 SF340A 7850100 EU OIL PRESSURE MALFUNCTIONED A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 121CQ 121 OIL PRESSURE ANNUNCIATOR LIGHT CAME ON DURING TAKEOFF ROLL/TAKEOFF ABORTED. REMOVED AND REPLACED RT ENGINE OIL PRESSURE SWITCH. 2 L 7 2 4T RT A52EU 2008011400148 20080114 00148 EU 2008 1 14 NSVA20070151 1 20070602 A 3150 WARNING LIGHT SAAB SF340 340B 7860101 EU ILLUMINATED A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 9CJ 224 ON TAKEOFF PILOT REPORTED THAT CONFIGURATION WARNING LIGHT ILLUMINATED TO DISPATCH AND MAINTENANCE CONTROL. THE PILOT T HEN REALIZED THAT HE DID NOT HAVE THE POWER LEVERS ALL THE WAY UP TO THE TAKEOFF POSITION CONSEQUENTLY; CONFIG WARNING L IGHT ILLUMINATED. 2 L 7 2 4T RT A52EU 2008011400149 20080114 00149 EU 2008 1 14 NSVA20070057 1 20070309 A 2611 7211211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU LAVATORY INTERMITTENT A NSVA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 249CJ 249 LAV SMOKE DETECTOR ILLUMINATES INTERMITTENTLY ON TAXI OUT TO RUNWAY. CLEANED AND INSPECTED LAV SMOKE DETECTOR IAW COLGA N WORKCARD 26-13-025. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011400150 20080114 00150 NE 2008 1 14 NSVA20070097 2 20070412 A 7321 6071T20P18 CONTROL UNIT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE MALFUNCTIONED A NSVA O OTHER J WARNING INDICATION TO TAKEOFF 1 EA 27 344CJ 344 LT ENG TQ 40 PERCENT ON TAKEOFF ROLL AND THEN NORMALIZED. REMOVED AND REPLACED NR 1 DEC PN 6071T20P18, SN ON LMDT2171, SN OFF EMDT3020IAW GEMM 74-00-00. PERFORMED HIG SPEED TAXI TEST, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011400151 20080114 00151 2008 1 14 NSVA20070132 3 20070519 A 6197 WIRE SAAB SF340 340B 7860101 EU PROP CONTROL DAMAGED A NSVA D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 EA 27 252CJ 340B252 P3 TEST FAILED ON BOTH ENGINES. REPAIRED WIRING AT PROPELLER CONTROL UNIT. 2 L 7 2 4T RT A52EU 2008011400152 20080114 00152 CE 2008 1 14 NSVA20070148 1 20070601 A 7603 SPRING BEECH 1900 1900D 1154162 CE THROTTLE BROKEN A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 221CJ UE221 BOTH THROTTLE LEVERS ARE LOOSE. REMOVED LT AND RT POWER LEVERS IAW BEECH 1900D MM 76-10-00, FOUND RT AND LT POWER LEVER ARM ASSY WORN AND GUILD PINS WORN IN POWER LEVERS. P.O.O. AND ONE RETURN SPRING BROKEN. INSTALLED NEW RT AND LT POWER LEVERS IAW BEECH 1900D MM 76-10-00, OPS CHECK WERE GOOD. 2 L 7 2 4T RT A24CE 2008011400153 20080114 00153 EU 2008 1 14 NSVA20070176 1 20070705 A 2611 DETECTION SYS SAAB SF340 340B 7860101 EU RT FIRE DETECT MALFUNCTIONED A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 370PX 300 DURING FIRE SHORT TEST R FIRE DET LT DID NOT ILLUMINATE. PERFORMED OPERATIONAL CHECK, NO DEFECT NOTED IAW AMM 26-10-00. 2 L 7 2 4T RT A52EU 2008011400155 20080114 00155 EU 2008 1 14 NSVA20070079 1 20070329 A 2611 7292328501 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU CARGO BAY MALFUNCTIONED A NSVA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 121CQ 121 AFT CARGO LIGHT SMOKE DETECTOR REMAINS ILLUMINATED AT ALL TIMES. REMOVED AND REPLACED AFT SMOKE DETECTOR IAW SMM 26-13- 00. OP CHECKS GOOD MEL NR 24719. 2 L 7 2 4T RT A52EU 2008011400157 20080114 00157 EU 2008 1 14 NSVA20070168 1 20070626 A 2611 CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A NSVA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 239CJ 239 CARGO SMOKE INDICATION DURING TAXI OUT. REMOVED AND REPLACED CARGO AFT SMOKE DETECTOR IAW 26-13-15. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011400158 20080114 00158 EU 2008 1 14 NSVA20070190 1 20070719 A 2613 WARNING LIGHT SAAB SF340 340B 7860101 EU TAIL PIPE MALFUNCTIONED A NSVA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 237MJ 237 TAILPIPE HOT LIGHTS ILLUMINATED DURING GROUND RUNS. PERFORMED ENGINE RUNS COULD NOT DUPLICATE, NO DEFECTS NOTED. 2 L 7 2 4T RT A52EU 2008011400162 20080114 00162 EU 2008 1 14 NSVA20070138 1 20070523 A 2121 M4401D8A FAN SAAB SF340 340B 7860101 EU E/E BAY UNKNOWN A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 352CJ 352 AVIONICS SMOKE LIGHT ILLUMINATED WITH GROUND POWER. REMOVED AND REPLACED AVIONICS RACK FAN IAW AMM 21-23-10-02, OP'S CH ECK GOOD, PN ON OFF M4401D8A, SN OFF EM81219SN ON 633. 2 L 7 2 4T RT A52EU 2008011400163 20080114 00163 2008 1 14 NSVA20070185 2 20070712 A 7320 6068T72P22 HMU SAAB SF340 340B 7860101 EU ENGINE MALFUNCTIONED A NSVA O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 350CJ 350 LEFT TORQUE INDICATION FLUCTUATED PLUS/MINUS 3-4 PERCENT DURING CRUISE FLIGHT, AS POWER WAS INCREASED FLUCTUATIONS WERE LONGER. ABOUT 1-2 PERCENT AROUND 40-50 PERCENT TORQUE. NO FLUCTUATIONS ON GROUND OR TAKEOFF WITH CTOT ENGAGED. CLIMB POWER SET AND PROP AT 1270 RPM. CHECKED ALL CONNECTORS LT ENGINE ALL FOUND SECURE CHECKED OIL ADDED 1 QT LT ENGINE SWAP PED TORQUE GAUGES RAN ACFT FOUND NO TORQUE FLUCTUATION DURING RUN UP. GAUGE REMAIN SWAPPED. REPLACED LT HMU IAW GE MM 73-00-00, LEAK CHECK AND OPS TEST GOOD. NO FLUCTUATES NOTED DURING ENGINE RUN, P/N 6068T72P22 S/N ON:11432828, S/N OFF: WYG54843. 2 L 7 2 4T RT A52EU 2008011400164 20080114 00164 2008 1 14 NSVA20070128 4 20070513 A 3418 SWITCH SAAB SF340 340B 7860101 EU PUSHER DISARM UNKNOWN A NSVA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 239CJ 239 PUSHER DISARM LIGHTS ILLUMINATED AFTER PUSHBACK. RESET PUSHER DISARM SWITCH, LIGHT EXTINGUISHED IAW SAAB AMM 2735-00-05 , OPS CHECK OK. 2 L 7 2 4T RT A52EU 2008011400166 20080114 00166 EU 2008 1 14 NSVA20070074 1 20070326 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU LAVATORY NO TEST A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 299CJ 299 LAV SMOKE DETECTION SYSTEM DOES NOT TEST. COULD NOT DUPLICATE DISCREPANCY, OPERATIONAL CHECK GOOD IAW SAAB M/M 26-13-00 . 2 L 7 2 4T RT A52EU 2008011400168 20080114 00168 CE 2008 1 14 NSVA20070115 1 20070426 A 2612 70522 FIRE LOOP BEECH 1900 1900D 1154162 CE LT NACELLE OUT OF POSITION A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 124CJ UE24 LT FIRE LOOP WILL NOT TEST. REMOVED AND REPLACED LT ENGINE FIRE LOOP HARNESS FROM FWD FIRE SEAL TO AFT FIRE WALL REF. B EECH 1900D MM 26-10-01. OPS CHECK GOOD, PN ON/OFF 70522. 2 L 7 2 4T RT A24CE 2008011400169 20080114 00169 2008 1 14 NSVA20070175 4 20070704 A 3425 6226190113S COMPUTER SAAB SF340 SF340A 7850100 EU NR 1 AHRS MALFUNCTIONED A NSVA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 35SZ 35 CAPT SIDE EFIS FAILED IN FLIGHT, NO PAX ON BOARD, RETURNED TO ALB, NO OTHER PROBLEMS. REMOVED AND REPLACED NR 1 AHRS CO MPUTER. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011400170 20080114 00170 CE 2008 1 14 NSVA20070183 1 20070713 A 6123 210461 OVRSPEED LIMITER BEECH 1900 1900D 1154162 CE LT PROP GOVERNOR MALFUNCTIONED A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 171CJ UE71 ON TAKEOFF, LT PROP FEATHERED. REMOVED AND REPLACED OVERSPEED GOVERNOR, AND REMOVED AND REPLACED PROP GOVERNOR ON LT SI DE REF 61-20-02, PN:8210-410 SN: 11536603. 2 L 7 2 4T RT A24CE 2008011400171 20080114 00171 EU 2008 1 14 NSVA20070071 1 20070320 A 3040 8103741 WINDSHIELD SAAB SF340 340B 7860101 EU COCKPIT CRACKED A NSVA B EMER. DESCENT O OTHER CR CRUISE 1 EA 27 196CJ 196 LT FRONT WINDSHIELD CRACKED INFLIGHT. REMOVED AND REPLACED PILOT'S WINDSHIELD PN/OFF 81037-41, SN OFF 23834198-PA SN ON SWU1311 IAW AMM 56-10-05-04. 2 L 7 2 4T RT A52EU 2008011400172 20080114 00172 EU 2008 1 14 NSVA20070100 1 20070416 A 7712 6071T20P16 ECU SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE MALFUNCTIONED A NSVA O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 194CJ 194 DURING ALL FLIGHT CONDITIONS RT ENGINE TORQUE FLUX +/- 3 PERCENT ITT FLUX PLUS/MINUS 5 DEGREES ENGINE OIL PRESSURE FLUX PLUS/MINUS10 PSI. REMOVED AND REPLACED THE DECU IAW CHAPTER 76-10-57-04 OF THE SAAB 340-AMM P/N 6071T20P16, P/N ON 6071 T20P18 S/N OFF ECDT1445, S3 ON LMDT 2232. PERFORMED OPS TEST OK. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011400173 20080114 00173 EU 2008 1 14 NSVA20070112 1 20070425 A 3150 WARNING SYSTEM SAAB SF340 340B 7860101 EU ILLUMINATED A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 9CJ 224 LOW SPEED ABORT DUE TO CONFIG WARNING. PERFORMED HIGH SPEED TAXI WITH NEW, COULD NOT DUPLICATE PROBLEM. 2 L 7 2 4T RT A52EU 2008011400179 20080114 00179 EU 2008 1 14 NSVA20070047 1 20070226 A 7603 STOP SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE FLIGHT IDLE MALFUNCTIONED A NSVA O OTHER J WARNING INDICATION LD LANDING 1 EA 27 35SZ 35 FLIGHT IDLE STOP HAD TO BE OVERRIDDEN DURING LANDING ROLL OUT. RESET FLIGHT STOP WITH F1 REST TOOL. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE6 2008011400180 20080114 00180 EU 2008 1 14 NSVA20070049 1 20070227 A 6120 SWITCH SAAB SF340 340B 7860101 EU P3 MALFUNCTIONED A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 339CJ 339 AUTOCOARSEN LIGHT ON DURING TAKEOFF. REMOVED AND REPLACED LEFT P3 SWITCH IAW SAAB AMM 61-22-10, OPS CHECK GOOD. PERFOR MED 3 HIGH SPEED TAXIS IN TAKEOFF CONFIGURATION. RAN ACFT ON GROUND AND PERFORMED MULTIPLE AUTO COARSEN CHECKS ON GROUN D AT 100 PERCENT TORQUE 90 PERCENT TORQUE SYSTEM DID NOT FAIL IAW SAAB AMM 61-22-00. 2 L 7 2 4T RT A52EU 2008011400182 20080114 00182 CE 2008 1 14 NSVA20070154 1 20070610 A 3297 WIRE BEECH 1900 1900D 1154162 CE DOWNLOCK SWITCH CHAFED A NSVA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 155CJ UE55 GEAR UNSAFE LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION, INSPECTED LANDING GEAR FOR ANY OBVIOUS DAMAGE FOUND NO DA MAGE. FOUND RT DOWN SWITCH WITH CHAFED WIRES. REMOVED AND REPLACED SWITCH IAW AMM 32-60-02. OPS CHECK GOOD, P/N ON/OF F H11-1541. 2 L 7 2 4T RT A24CE 2008011400183 20080114 00183 EU 2008 1 14 NSVA20070059 1 20070311 A 7930 005WS00 WEU SAAB SF340 340B 7860101 EU MALFUNCTIONED A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 347CJ 347 CONFIG ANN ILLUMINATED ON TAKEOFF ROLL 100 KIAS. REPLACED WEU REF SAAB AMM 31-50-05, OPS CHECK OK, PN: 005WS00, SN ON: 1196, SN OFF: 1413. 2 L 7 2 4T RT A52EU 2008011400184 20080114 00184 EU 2008 1 14 NSVA20070068 1 20070317 A 2611 72111211T000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E BAY MALFUNCTIONED A NSVA O OTHER K FLUID LOSS CR CRUISE 1 EA 27 210CJ 210 FLT LEFT FROM SCE, SMOKE DETECTOR ILLUMINATED IN FLIGHT. REMOVED AND REPLACED AVIONICS SMOKE DETECTOR IAW SMM 26-13-05. OP CHECKS GOOD, P/N 72-111211T000 ON/OFF SN ON A1482 SN A4982. 2 L 7 2 4T RT A52EU 2008011400187 20080114 00187 EU 2008 1 14 NSVA20070113 1 20070425 A 7603 STOP SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FLIGHT IDLE MALFUNCTIONED A NSVA O OTHER J WARNING INDICATION LD LANDING 1 EA 27 338CJ 338 FLT IDLE STOP PULLED UPON LANDING. RESET FLIGHT IDLE STOP IAW AMM 76-10-60, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011400192 20080114 00192 CE 2008 1 14 NSVA20070095 1 20070409 A 2750 SWITCH BEECH 1900 1900D 1154162 CE FLAP ASYMMETRIC MALFUNCTIONED A NSVA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 60MJ UE60 FLAPS DID NOT EXTEND TO 35 ON APPROACH AND LANDED FLAPS 17 AND WILL NOT RETRACT. ADJUSTED FLAP SAFETY ASYMMETRIC SWITCH , OPS CHECK GOOD IAW BEECHCRAFT 1900D MM 27-50-06-201. 2 L 7 2 4T RT A24CE 2008011400193 20080114 00193 EU 2008 1 14 NSVA20070066 1 20070317 A 2920 INDICATOR SAAB SF340 340B 7860101 EU HYD SYS MALFUNCTIONED A NSVA O OTHER N FALSE WARNING CR CRUISE 1 EA 27 309CE 201 HYDRAULIC EMERGENCY INDICATOR INDICATING ZERO IN FLIGHT. CLEANED ELECTRICAL CONNECTOR ON HYDRAULIC PRESSURE GAUGE AND P ERFORMED OPERATIONAL TEST. WITH ENGINE RUNNING NOTICED NO FAULTS OR FLUCTUATIONS ON BOTH MAIN AND EMERGENCY HYDRAULIC P RESSURE INDICATOR. OPS CHECK GOOD IN REF WITH SAAB AMM 29-30-00 AND 72-00-00. 2 L 7 2 4T RT A52EU 2008011400195 20080114 00195 EU 2008 1 14 NSVA20070052 1 20070227 A 2750 HP14161005 CONTROL VALVE SAAB SF340 340B 7860101 EU TE FLAPS MALFUNCTIONED A NSVA O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 356CJ 356 FLAPS DEPLOY BETWEEN 0 - 7 DEGREES IN FLIGHT. REMOVED AND REPLACED FLAP CONTROL VALUE IAW CHAPTER 27-51-15-04 THE SAAB 340 AMM PN OFF HP1416100-5 PN ON HP1416100-5 SN OFF 1327 SN ON 1435. PERFORMED OPS CHECK AND LEAK CHECK IAW 27-51-00, O PS AND LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011000142 20080110 00142 NM 2008 1 10 USAA920080062 1 20071206 A 5315 6545834 STRAP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FLOORBEAM STABILIZER STRAP, BS 328, RBL 31. REPLACED FLOORBEAM STABILZER STRAP , BS 328, RBL 31 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008011000159 20080110 00159 2008 1 10 DXTA200702706 4 20071222 A 3422 40205773 GYRO CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE E/E BAY INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 322QS 3755 5600421 NR 1 HEADING INDICATOR FAILED. 1 PFD, STANDBY HEADING INDICATOR AND MFD HEADING INDICATOR FAILED. REMOVED & REPLACED NR 1 DG IAW CE560 MM CHAPTER 34-21-05. OPS CHECKS GOOD 2 L 7 2 4F 4 F RT A22CE E25EA 2008011000160 20080110 00160 CE 2008 1 10 DXTA200702701 1 20071223 A 2750 99146153 DRIVE UNIT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 979QS 3500 3500 7500079 FLAP FAIL ANNUCIATION IN FLIGHT AT 3000 FT AND 220 KNOTS, WILL NOT RESET. REPLACED PDU WITH NEW PER THE 750 MM. CH. 27- 52-00. ALL RIG AND OPERATIONAL CHECKS GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008011000162 20080110 00162 CE 2008 1 10 DXTA200702704 1 20071223 A 3240 BRAKE ASSY CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE RIGHT WEAK E DXTA O OTHER O OTHER LD LANDING 1 GL 07 676QS 5605176 RT BRAKE PEDAL SERVING BOTH PILOT STATIONS IS SPONGY. AIRCRAFT EXHIBITS ASSYMETRIC BRAKING DURING LANDING, BRAKE APPLIC ATION YAWS ABRUPTLY. BLED RIGHT BRAKE IN REF. TO CE-560XL MM 32-42-00. OPS AND LEAK CHECK GOOD. TAXIED ACFT. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008011000164 20080110 00164 CE 2008 1 10 DXTA200702707 1 20071222 A 5610 99143798 WINDOW CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL COCKPIT CRACKED E DXTA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 970QS 8442 7500070 DURING FLIGHT, THE RT SIDE, SIDE WINDOW SHATTERED. REMOVED AND REPLACE COPILOTS RIGHT SIDE WINDOW RIG INSTALLED A NEW ( RIGHT SIDE WINDOW RIG) P# 9914379-8, (SEAL) P#6211407-5, (WASHER) P# NAS1149F0363P NEW, (NUTS)P#MS21044H3 NEW, AND (SCRE WS) P# NAS1580C3R14 IAW 750MM 56-12-001 30-41-00 FOUND NO DEFECT/DAMAGED TO AREA AT THIS POINT IN TIME AFTER FT OPERATIO N. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008011000165 20080110 00165 CE 2008 1 10 DXTA200702703 1 20071223 A 3260 UPLOCK HOOK BEECH MU300 400A 1155402 CE NLG OUT OF ADJUST E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 141QS RK498 AFTER LANDING GEAR RETRACTION, LANDING GEAR UNLOCKED/IN-TRANSIT LIGHT REMAINED ILLUMINATED. GEAR EXTENDED NORMALLY, NORM AL LANDING. ADJUSTED NOSE GEAR UPLOCK HOOK TO PROPERLY ENGAGE IAW 400A M/M CH. 32-20-00. SWUNG GEAR MULTIPLE TIMES, OP S CHECK GOOD. 2 H 7 2 4F RT A16SW 2008011000168 20080110 00168 CE 2008 1 10 DXTA200702705 1 20071223 A 5610 99143809 WINDSHIELD CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL COCKPIT FAILED E DXTA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 999QS 5303 7500203 IN CRUISE FLIGHT AT FL390 RECEIVED (WINDSHIELD HEAT L FAIL) CAS MSG FOLLOWED BY THE FRACTURING OF THE OUTER PLY OF THE L T WINDSHIELD. PERFORMED ELECTRICAL HEATED WINDSHIELD FUNCTIONAL TEST IAW CESSNA 750 M/M 30-41-00, REMOVED LT WINDSHIELD . INSTALLED NEW L/H WINDSHIELD. PERFORMED ELECTRICAL HEATED WINDSHIELD FUNCTIONAL TEST IAW CESSNA 750 MM 30-41-00. NO DI SCREPANCIES AT THIS TIME. INSTALATION OF WINDSHIELD WAS PERFORMED IAW CESSNA 750 M/M 56-11-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008011000169 20080110 00169 WP 2008 1 10 DXTA200702710 2 20071221 A 7200 30751604 ENGINE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP SMOKE E DXTA E ENGINE SHUTDOWN B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 07 824QS 5162 258523 P107617 CLIMBING THRU FL310 THE RT ENGINE PRODUCED A LOUD BANG ACCOMPANIED BY VIBRATIONS AND N1/N2 STARTED ROLLING BACK. WITH TH E SMELL OF SMOKE IN COCKPIT THE CREW SHUTDOWN THE ENGINE. REMOVED & REPLACED RIGHT ENGINE WITH INSPECTED UNIT IAW H800X P AMM 71-00-01. LEAK & OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A3EU E6WE 2008011000174 20080110 00174 CE 2008 1 10 DXTA200702711 1 20071221 A 3230 LANDING GEAR BEECH MU300 400A 1155402 CE MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 139QS RK483 RAISED LANDING GEAR AFTER TAKEOFF; ALL THREE GREEN LIGHTS EXTINGUSHED EXCEPT 2 RED LIGHTS IN GEAR HANDLE; SELECTED GEAR DOWN, ALL 3 GEAR LIGHTS ON AND RED EXTINGUSHED; BROUGHT GEAR UP, ALL 3 GREEN LIGHTS EXTINGUSHED AND 2 RED LIGHTS REMAINE D ON IN GEAR HANDLE. BROUGHT GEAR UP, ALL THREE GREEN LIGHTS EXTINGUSHED AND 2 RED LIGHTS REMAINED ON IN GEAR HANDLE. CHECKED CONNECTORS P387, P271 AND P272. RANG OUT LANDING GEAR UPLOCK SWITCHES, DOWN LOCK SWITCHES AND DOOR NOT CLOSED S WITCHES, NO DISCREPANCIES WERE NOTED. REINSTALLED CONNECTORS AND PANELS. JACKED ACFT IAW HAWKER 400XP MM 07-10-00. RETRA CTED AND EXTENDED LANDING GEAR 10 TIMES UTILIZING MOTOR ON A STICK FOR HYDRAULIC POWER, NO DISCREPANCIES WERE NOTED AT T 2 H 7 2 4F RT A16SW 2008011000179 20080110 00179 NM 2008 1 10 2007UALA05360 1 20071229 A 5340 693636Y1 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 FUSELAGE STRINGER CLIP CRACKED, BS 727D, STR 21R. REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011000180 20080110 00180 NM 2008 1 10 2007UALA05361 1 20071229 A 5340 6935352Y1 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 STRINGER CLIP CRACKED ON LOWER RT FUSELAGE BS 787 STR 22R. INSTALLED NEW STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011000181 20080110 00181 2008 1 10 2007UALA05362 4 20071228 A 2565 INDICATOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EVAC SLIDE OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 399UA 24674 DOOR 1R SLIDE PACK PRESS GAUGE DIFFICULT TO READ DUE TO POSITION OF INDICATOR. REPLACED SLIDE PACK. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011000184 20080110 00184 EU 2008 1 10 07FDEA05139 1 20071226 A 7830 32052213 VALVE AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680 30025 NE NR 1 ENGINE FAILED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 683FE 3868 3868 801 705228 ON TAKEOFF ROLL AS POWER WAS ADVANCED TO FLEX POWER LEFT ECAM SHOWED "ENG 1 REV PRESSURIZED", W/MASTER CAUTION. REJECTE D TAKEOFF AT 60KTS. AS THROTTLES REDUCED TO IDLE, LEFT ECAM AND MASTER CAUTION CLEARED. RELEASED FOR SERVICE. FOUND F AULTY DPV. REMOVED AND REPLACED DIRECTIONAL PILOT VALVE . PERFORMED ENGINE RUN TO MAX POWER. OPS CHECKS NORMAL PER MM 78-31- 09-2 2 L 7 2 4F 4 F RT A35EU E13NE 2008011000185 20080110 00185 NM 2008 1 10 2007UALA05365 1 20071229 A 3320 SOCKET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR LIGHT FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 526UA 24994 DOOR 2R ARMED LIGHT FAILS TO ILLUMINATE WHEN DOOR ARMED. LIGHT SOCKET HAD BECOME LOOSE. RESEATED LIGHT SOCKET AND ASS Y CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008011000215 20080110 00215 NM 2008 1 10 2007UALA05392 1 20071229 A 2721 TRIM SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RUDDER OUT OF RIG A UALA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 575UA 26689 RUDDER TRIM OUT OF LIMITS. FOUND RUDDER RIG OFF SLIGHTLY. RE-RIGGED ENTIRE RUDDER SYSTEM AND STANDBY RUDDER LVDT. N O HISTORY SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008011000216 20080110 00216 EA 2008 1 10 TRAX200701991 1 20071222 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 PAX DOOR TOP STEP IS CRACKED AT THE FWD EDGE. REPARIED DAMAGE TO PAX DOOR SKIN UNDER TOP STEP IAW REO 601R-52-11-279. C/W INSP OF CUTOUT FOR PAX DOOR SKIN UNDERNEATH TOP STEP IAW CRJ 200 NDTM 51-20-06. COMPLIED WITH EC-TC EO 600-52-43 C/W . 2 L 7 2 4F RT A21EA 2008011000218 20080110 00218 CE 2008 1 10 DXTA200702721 1 20071230 A 5610 NP1397219 WINDSHIELD CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL COCKPIT BROKEN E DXTA O OTHER O OTHER DE DESCENT 1 GL 07 906QS 4908 7500206 LT WINDSHIELD IS CRACKED. LT WINDSHIELD HEAT INOP ILLUMINATED ON CAS. REMOVED CRACKED L/H WINDSHIELD. INSTALLED NEW WIN DSHIELD. OPERATIONAL CHECK GOOD IAW CE750 56-11-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008011100006 20080111 00006 NM 2008 1 11 B8M2007F00001 1 20071205 A 5320 A3592 SUPPORT ROBSIN R22 R22BETA 7640110 NM LYC O320 O320B2C 41508 EA RT PEDALS BROKEN E B8MA O OTHER O OTHER CR CRUISE 1 WP 17 805EH 13078 1907 L884139A TRAINING FLIGHT, CFI AND STUDENT ONBOARD. CONDUCTING HOVER AUTOROTATION TRAINING. ON THIRD HOVER AUTOROTATION, AS HELI COPTER SETTLED ON GROUND, STUDENT WAS INPUTTING RT PEDAL TO COMPENSATE FOR LOSS OF TORQUE WHEN A LOUD (SNAP) WAS HEARD F ROM THE PILOT SIDE TAIL ROTOR PEDAL AREA. PEDALS BECAME BOUND IN PLACE. SHUTDOWN HELICOPTER AND INSPECTION SHOWED THAT THE BEARING BLOCK SUPPORT FOR THE PILOT SIDE PEDALS HAD BROKEN AND THE SECURING BLOCK WAS NOW FREE AND PEDALS WOULD NOT TRAVEL FREE. (K) 1 G 7 1 3O 3 O H10WE E274 2008011100009 20080111 00009 NE 2008 1 11 OXB2007F00000 2 20071211 A 7200 ENGINE CESSNA 500 S550 2076607 CE PWA JT15 JT15D4 52112 NE NR 2 OVERSPEED E OXBA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 EA 61 711MD S5500066 102151 WHILE CLIMBING THROUGH 13K FEET, THE NR 2 ENGINE UNEXPECTEDLY OVERSPED AND THE ITT EXCEEDED THE LIMIT OF THE INDICATOR. THE PILOT TRIED PULLING THE THROTTLE BACK TO IDLE BUT IT HAD NO EFFECT. THE PILOTS WERE FORCED TO SHUTDOWN THE ENGINE IN FLIGHT. (K) 1 L 7 2 4F 4 F RT A22CE E1NE 2008011100017 20080111 00017 EU 2008 1 11 2007UALA05292 1 20071223 A 3510 REGULATOR VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE OXYGEN MASK DIRTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 442UA 780 CAPTAIN'S O2 MASK REGULATOR STICKY VALVE INTERMITTENT DURING INHALATION. REGULATOR DIRTY, STICKING. REPLACED CAPT O2 M ASK ASSY. NORMAL OPS CHECK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011100022 20080111 00022 NM 2008 1 11 QXEA200701950 1 20071217 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA ILLUMINATED A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 413QX 4060 FLIGHT 2322, ON APPROACH WHEN SELECTING FLAPS TO 15 DEGREES, AT 10 DEGREES THE FLAP POWER CAUTION ILLUMINATED. IAW THE CHECKLIST, RESET THE CIRCUIT BREAKER AND LIGHT WENT OUT AND FLAPS OPERATED NORMALLY. NOTIFIED MAINTENANCE CONTROL OF PRO BLEM. NO FURTHER ACTION REQUIRED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2008011100026 20080111 00026 NM 2008 1 11 QXEA200701949 1 20071218 A 3010 4100S0053 VALVE BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA DE ICE SYS FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 421QX 2449 4149 DURING CRUISE RECEIVED A DE-ICE PRESSURE CAUTION LIGHT. RAN THE CHECKLIST AND THE LIGHT WENT OUT. 15 MINUTES LATER IT RE TURNED. THE ADVISORY LIGHT FOR THE RT BOOT SEGMENT FLICKERED. DE-ICE PRESSURE WAS OK. MAINTENANCE REPLACED THE NR4 DDV V ALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2008011100034 20080111 00034 NM 2008 1 11 2008UALA0012 1 20071231 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EEL(S) INOPERATIVE AT SEATS 2J FWD SECT, 23ABC FWD SECT, 48ABC & 24JK. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011100044 20080111 00044 NM 2008 1 11 AMTA200700709 1 20071216 A 5753 SKIN BOEING 737 73783N 13844HI NM TE FLAP DENTED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 315TZ 28245 RT WING IB AFT FLAP LOWER SURFACE HAS NUMEROUS DENTS. FABRICATED REPLACEMENT SKIN AND REPAIR DOUBLERS IAW SRM 51-70-10 REPAIR 4, FIG 203 AND EA NR 737-5753-090A1235, ATA ERA 73757R-6180 FOR TRACKING. (K) 2 L 7 2 4F RT A16WE 2008011100058 20080111 00058 NM 2008 1 11 2008UALA0022 1 20071231 A 2611 LIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU SMOKE DETECTOR INOPERATIVE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 936UA 26667 AFT RIGHT LAV SMOKE DETECTOR POWER LIGHT NOT ON. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011100062 20080111 00062 CE 2008 1 11 GUUA12130702 1 20071213 A 3260 H111541 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT MLG DAMAGED A GUUA O OTHER N FALSE WARNING CL CLIMB 1 SO 29 81546 UE187 AFTER TAKEOFF LANDING GEAR RETRACTION GEAR HANDLE LIGHT REMAIN ILLUMINATED. REPLACED LT MAIN LANDING GEAR UPLOCK SWITCH . 2 L 7 2 4T 4 T RT A24CE E26NE 2008011100103 20080111 00103 EA 2008 1 11 QXEA200702019 1 20071222 A 3260 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE BRAKE OVERHEAT ILLUMINATED A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 614QX 10049 FLIGHT 2553. EXPERIENCED ON CLIMB, A BRAKE OVERHEAT WARNING MESSAGE. NR 4 BRAKE INDICATED 20. AFTER 1 MINUTE THE INDICAT ION WENT TO GREEN. BTMS RESET. MAINTENANCE COMPLIED WITH SL 32-033. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO P ARTS REPLACED. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008011100132 20080111 00132 NM 2008 1 11 HNAA0800011 1 20071230 A 3350 82410162007 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM CABIN INTERMITTENT A HNAA K NONE O OTHER CR CRUISE 1 EA 07 931HA 49691 49691 132 DURING FLIGHT, THE CABIN EMERGENCY LIGHTING CYCLED ON AND OFF. CREW NOTED THAT THE PROP DEICE SYSTEM WAS NOT SELECTED O N. MAINTENANCE CHANGED THE EMERGENCY LIGHTS SYSTEM CONTROL BOX AND CHECKED OPERATIONS IAW PIEDMONT WORKCARD PROCEDURES. SYSTEM CHECKED GOOD AND AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 2008011100227 20080111 00227 EA 2008 1 11 S9BA200700026 1 20071230 A 3246 13A02030006 ATTACH BRACKET DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA CRACKED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 888PV 81 620 LT AND RT FORWARD STRUT FITTING CRACKED. REMOVED AND REPLACED LOWER STRUT TO FLOAT FITTINGS. 1 H 7 2 3T 4 T RT A9EA E4EA 2008011400022 20080114 00022 NM 2008 1 14 DXTA200702632 1 20071128 A 2910 HYDRAULIC SYSTEM AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE NR 1 READS LOW E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 281QS 81 NR 1 HYDRAULIC SYSTEM QUANTITY INDICATED IN THE RED ZONE FOR QUANTITY DURING TAKEOFF RUN. ABORTED TAKEOFF ENSUED AS A RE SULT OF LOW HYDRAULIC QUANTITY. SERVICED HYD SYSTEM IAW MM CH 29-112. 2 L 7 2 4F 4 F RT A50NM E44NE 2008011400034 20080114 00034 CE 2008 1 14 GUUA12190702 1 20071219 A 5524 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 69547 24915 UE189 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT ELEVATOR OB HINGE BRACKET EXFOLIATED. REPLACED LT ELEVATOR OB HINGE B RACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 2008011400052 20080114 00052 SW 2008 1 14 AC2A118587 1 20071022 A 6420 BEARING BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL TAIL ROTOR WORN E AC2A O OTHER O OTHER NR NOT REPORTED 1 SW 31 17238 1146 CS13707 51492 TAIL ROTOR HAS WORN FEATHERING BEARINGS. 1 G 7 1 3U 3 U H2SW E1GL 2008011400066 20080114 00066 NE 2008 1 14 0101084118 2 20071231 A 7321 430128308 FUEL CONTROL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE NR 2 ENGINE FAILED E RMXA L ABORTED APPROACH X J ENGINE FLAMEOUT WARNING INDICATION AP APPROACH 1 SW 05 117AP 4981 213 7144 LE45665 ON APPROACH TO LANDING AT APPROXIMATELY 300 FEET AGL NR 2 ENGINE FLAMED OUT. THE ENGINE WAS RESTARTED AFTER LANDING AN D GROUND RUNS HAVE BEEN MADE WITHOUT INCIDENT. MAINTENANCE EVALUATION IS UNDERWAY. FUEL CONTROL SYSTEM IS SUSPECT, B UT NOT CONFIRMED. 1 G 7 2 3U 3 U H13EU E5NE10 2008011400077 20080114 00077 EA 2008 1 14 A6WA200740683 1 20071219 A 2740 TY191051A PITCH CONTROL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE PITCH FEEL INOPERATIVE A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 458AW 10152 7861 CONTROL COLUMN BINDS IN PITCH WHEN MOVED FORWARD AND AFT OF NEUTRAL AND FEELS HEAVIER THAN NORMAL THRU WHOLE RANGE OF MO VEMENT IN-FLIGHT AND ON GROUND AT ALL FLAP ANGLES. REMOVED AND REPLACED PITCH FEEL SIMULATOR. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008011400087 20080114 00087 CE 2008 1 14 DUFA20070004 1 20070816 A 3700 DRIVE ASSY CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO VACUUM SYS SHEARED E DUFA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 27 3796C PE6539 402B0803 WHILE IN CRUISE FLIGHT THE PILOT NOTICED OIL STREAMING FROM THE TOP OF THE LT ENGINE COWL. THE OIL PRESSURE WAS STILL IN THE NORMAL OPERATING RANGE AND THE ENGINE APPEARED TO BE OPERATING NORMALLY. AS A PRECAUTION, THE LT ENGINE WAS SHUTDOW N AND SECURED. THE PILOT DEVIATED TO THE NEAREST AIRPORT WHERE HE MADE AN UNEVENTFUL LANDING. UPON INVESTIGATION BY MAI NTENANCE, IT WAS DISCOVERED THAT THE WET SYSTEM VACUUM PUMP DRIVE HAD SHEARED AND CAUSED THE GARLOCK SEAL TO DISINTEGRAT E, ALLOWING OIL TO SEEP PAST. 1 L 7 2 3O 3 O A7CE E8CE 2008011400089 20080114 00089 SO 2008 1 14 DUFA20070002 2 20070410 A 8530 6461401 STUD CESSNA 404 404 2075901 CE CONT O520 GTSIO520M 17032 SO NR 5 CYLINDER SHEARED E DUFA E ENGINE SHUTDOWN E VIBRATION/BUFFET AP APPROACH 1 GL 27 80BS 641 46 4040048 292223R WHILE ON APPROACH TO AIRPORT, THE PILOT NOTICED MANIFOLD PRESSURE DROPPING AS WELL AS OIL PRESSURE FROM THE RIGHT ENGINE . HE ALSO BEGAN TO FEEL A VIBRATION FROM THE SAME ENGINE. HE ELECTED TO SHUT THE ENGINE DOWN AND MADE AN UNEVENTFUL LAND ING. UPON INSPECTION, THE NR 5 CYLINDER HOLD DOWN STUDS HAD SHEARED AND ALLOWED THE CYLINDER TO HAMMER AGAINST THE ENGIN E CASE AND COWLING. THIS IN TURN RIPPED THE RT EXHAUST STACK FROM THE NR 1 AND NR 5 CYLINDERS CAUSING HEAT DISTRESS AT T HE COWL DOOR. 1 L 7 2 3O 3 O RT A25CE E7CE 2008011400094 20080114 00094 SW 2008 1 14 DUFA041707 1 20070417 A 2613 434422122 OVERHEAT SENSOR SWRNGN SA227 SA227AC 8780603 SW LT NACELLE DEFECTIVE E DUFA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 GL 27 159MC AC728B SHORTLY AFTER DEPARTURE, THE LT WING OVERHEAT LIGHT ILLUMINATED. FOLLOWING PROCEDURE, THE PILOT SHUTDOWN THE LT GENERATO R, LT BLEED AIR AND EXTENDED THE LANDING GEAR. THE LIGHT REMAINED ILLUMINATED SO THE LT ENGINE WAS SHUTDOWN AS A PRECAUT IONARY MEASURE AND THE PILOT RETURNED TO FSD AND MADE AN UNEVENTFUL LANDING. AN INVESTIGATION BY MAINTENANCE COULD NOT R EVEAL A CAUSE OTHER THAN A POSSIBLE BRAKE HEATING UP DURING TAXI TO THE RUNWAY OR CABIN TEMP CONTROL SET TO MAX HEAT. MA INTENANCE COULD NOT DUPLICATE. 2 L 7 2 4T RT A8SW 2008011400096 20080114 00096 2008 1 14 AMTA200700723 4 20071225 A 3460 COMPUTER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE FLT MANAGE FAILED A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 518AT 27974 RT FMC FAILED ON TAXI. PERFORMED FIM REF 34-61-00 FIG 108B, RESET C/B`S. RERACKED R FMC PERFORMED BITE CHECK ON RT FMC , NO FAULTS NOTED. OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008011400106 20080114 00106 EU 2008 1 14 COEA0735821 1 20071011 A 5720 S57213012200 SHIM AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE REAR SPAR CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 29796 253 FOUND DURING HEAVY CHECK. MAJOR REPAIR. CORROSION ON RT WING UPPER SPAR SHIM, REPLACED SHIM WITH NEW MACHINED SHIM. WO 72241, NR 602033. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400109 20080114 00109 EU 2008 1 14 COEA0732821 1 20070827 A 5310 S5357511X201 CREASE BEAM AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE GOUGED A COEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 13 821FX 29796 253 FOUND DURING HEAVY CHECK. MAJOR REPAIR: TOOL DAMAGE (DRILL STARTS) 10 PLACES TO RT CREASE BEAM WEB UPPER SIDE. 5 ON PL ACES TO WEBS ON FORWARD SECTION AND 5 PLACES TO WEBS ON AFT SECTION. REMOVED AND REPLACED WEBS. CREASE BEAMS PN FWD S5 3575110201, AFT S53575112201. W/O 72245, NR 2000050, 2000067. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400110 20080114 00110 EU 2008 1 14 COEA0733821 1 20071015 A 5711 S57112036200 SPAR AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE RT WING CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 29796 253 FOUND DURING HEAVY CHECK. MAJOR REPAIR. CORROSION ON RT WING FWD SPAR ON THE LOWER FWD SPAR FLANGE OB OF WING RIB 10 AN D IB OF WING RIB 12. CORROSION REMOVED AND DAMAGES BLENDED IAW REPAIR DO/TS PROCEDURES. SHEET REFERENCE: DO/TS-803/04, 2752 AND JUSTIFICATION DOCUMENTS REF NOTE DO/TS-5023/07. WO 72241, NR 602034, 602026. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400113 20080114 00113 CE 2008 1 14 COEA0701960 1 20071204 A 2420 26185001 CONTROL UNIT CESSNA 208 208B 2073701 CE PWA PT6 PT6A114 52043 NE GENERATOR INOPERATIVE A COEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 13 960FE 208B0075 RETURNED TO BLOCKS: FLIGHT NR 8800, ON TAXI TO RUNWAY IN GEG STANDBY ELECTRIC GENERATOR FAULT LIGHT ILLUMINATED. ATTEMP TED RESET WAS UNABLE TO CLEAR THE FAULT, PILOT ELECTED TO RETURN TO RAMP. MAINTENANCE REMOVED AND REPLACED THE ALTERNAT OR CONTROL UNIT. (K) 1 H 7 1 3T 3 T A37CE E4EA 2008011400131 20080114 00131 2008 1 14 NSVA20070060 2 20070313 A 7261 CAP SAAB SF340 340B 7860101 EU ENGINE OIL UNSECURE A NSVA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 EA 27 9CJ 224 DURING TAKEOFF BEFORE 80 KNOTS LEFT OIL PSI CWP WARNING LIGHT ILLUMINATED. FOUND OIL FILLER CAP OFF. SERVICED LT ENGIN E W/ 2.75 QTS BP2380. SECURED FILLER CAP AND TEST RAN ENGINE. NO FURTHER DISCREPANCIES NOTED. 2 L 7 2 4T RT A52EU 2008011400142 20080114 00142 EU 2008 1 14 NSVA20070067 1 20070317 A 2613 SENSOR SAAB SF340 340B 7860101 EU LT TAIL PIPE DIRTY A NSVA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 277MJ 277 L TAILPIPE HOT LIGHT ILLUMINATED BEFORE TAKEOFF. THOROUGHLY INSPECTED AND CLEANED OVERTEMP SENSORS IAW SAMM 26-12-00, O PS GOOD, NO FAULTS NOTED. 2 L 7 2 4T RT A52EU 2008011400143 20080114 00143 CE 2008 1 14 NSVA20070139 1 20070524 A 5270 SWITCH BEECH 1900 1900D 1154162 CE LOCK SWITCH OUT OF ADJUST A NSVA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 221CJ UE221 MAIN CABIN DOOR LIGHT ILLUMINATED ON PUSHBACK. ADJUSTED AIRSTAIR DOOR LATCH PRESSURE LOCK SWITCH IAW BMM 52-70-02. OPE RATIONAL CHECK SAT. 2 L 7 2 4T RT A24CE 2008011400160 20080114 00160 CE 2008 1 14 NSVA20070195 1 20070722 A 3260 H111541 LIMIT SWITCH BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A NSVA O OTHER N FALSE WARNING CL CLIMB 1 EA 27 243CJ UE43 OUT OF AUG AS GEAR WAS BEING RETRACTED INTRANSIT LIGHT STAYED ILLUMINATED. RECYCLED GEAR INTRANSIT LIGHT, STAYED ILLUMI NATED, CONTINUED FLIGHT WITH GEAR DOWN. AS HANDLE WAS IN UP POSITION INTRANSIT LIGHT STAYED ILLUMINATED. REPLACED LT M LG UPLIMIT SWITCH AND ADJUSTED IAW BE-1900 MM 32-60-00, OPS CHECK GOOD, PN ON/OFF H11-1541. 2 L 7 2 4T RT A24CE 2008011400165 20080114 00165 EU 2008 1 14 NSVA20070087 1 20070405 A 7500 CLAMP SAAB SF340 340B 7860101 EU ENGINE MISSING A NSVA O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 27 299CJ 299 TORQUE DROP 25 PERCENT ON CLIMB-OUT WITH ITT UP TO LOW 900. FOUND CLAMP ON HP VALVE MISSING. REPLACED MISSING CLAMP AN D OP CHECKS GOOD IAW SMM 36-11-00-02. 2 L 7 2 4T RT A52EU 2008011400175 20080114 00175 EU 2008 1 14 NSVA20070046 1 20070225 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 194CJ 194 EMERGENCY LIGHT ABOVE MAIN CABIN DOOR AND JUMPSEAT INOPERATIVE. REMOVED AND REPLACED FWD RT POWER SUPPLY PN ON/OFF 60-1 321-1, SN ON 19500 SN OFF 17955. OPS CHECK GOOD IAW 33-50-10. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011400177 20080114 00177 EU 2008 1 14 NSVA20070073 1 20070325 A 3220 NAS130425D BOLT SAAB SF340 340B 7860101 EU NLG TORQUE LINK SHEARED A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 239CJ 239 NOSE LANDING GEAR TORQUE LINK (UPPER HALF) PIN, CENTER BOLT BROKEN. REMOVED AND REPLACED NOSE LANDING GEAR TORQUE LINK (UPPER HALF) PIN, CENTER BOLT IAW SAAB 340 AMM 32-21-15, P/N NAS1304-25D. 2 L 7 2 4T RT A52EU 2008011400189 20080114 00189 EU 2008 1 14 NSVA20070078 1 20070330 A 7797 WIRE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ENGINE BROKEN A NSVA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 35SZ 35 LEFT TORQUE READS "0" WHEN POWER IS APPLIED. ALSO FLUCTUATES AT TIMES, NOTE: AFTER APPROX 15 MINUTES RUNNING. INSPECTE D LT TORQUE SENSOR AND LT ALTERNATOR UNITS FOR SECURITY AND PROPER INSTALLATION, NO OBVIOUS FAULT FOUND, REJECTED TAKEOF F. INSPECTED AND PERFORMED RESISTANCE CHECKS FOR LEFT ENG TORQUE SPEED SENSOR, ENG DRIVEN ALTERNATOR, ADV AND ASSOCIATE D CONNECTIONS THRU ECU HARNESS IAW GE MM CH 72-00-00. INSPECTED RED/YELLOW HARNESS ALSO. ALL CHECKS OKAY, RAN AC AND L EFT TORQUE IND STILL NOT GOOD GAUGE OKAY, NEEDS FURTHER T/S. REMOVED AND REPLACED LEFT ENGINE ALTERNATOR. DID NOT FIX PROBLEM REFERENCE GE C 77-5 MM 74-00-00. FOUND BROKEN WIRE AT PIN 11 OF CONNECTOR 1G1VP P3, REPAIRED BROKEN WIRE REFERE 2 L 7 2 4T 4 T RT A52EU E8NE6 2008011400197 20080114 00197 EA 2008 1 14 DATA200700012 2 20071228 A 7200 ENGINE STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA RIGHT SHUTDOWN E DATA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 GL 13 336MV SH3018 PCE84172 ALL ENGINE INDICATIONS APPEARED NORMAL. RIGHT LOW FUEL PRESSURE ANNUNCIATOR CAME ON. ABOUT 5-10 SECONDS LATER, RIGHT E NGINE QUIT. ENGINE FAILURE CHECKLIST WAS CARRIED OUT, ENGINE SECURED AND AIRCRAFT DIVERTED TO VAN NUYS. 2 H 7 2 4T 4 T A41EU E4EA 2008011400198 20080114 00198 EA 2008 1 14 DATA200700011 2 20071228 A 7200 ENGINE STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA RIGHT FAILED E DATA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 GL 13 336MV SH3018 PCE84172 ALL ENGINE INDICATIONS APPEARED NORMAL. RIGHT LOW FUEL PRESSURE ANNUNCIATOR CAME ON. ABOUT 5-10 SECONDS LATER, RIGHT E NGINE QUIT. ENGINE FAILURE CHECKLIST WAS CARRIED OUT, ENGINE SECURED AND AIRCRAFT DIVERTED TO VAN NUYS. 2 H 7 2 4T 4 T A41EU E4EA 2008011500002 20080115 00002 EU 2008 1 15 NSVA20070173 1 20070702 A 3150 WARNING LIGHT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ENGINE OIL FALSE INDICATION A NSVA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 121CQ 121 ABORTED TAKEOFF 70KTS, LT ENGINE OIL MASTER WARNING LIGHT ILLUMINATED. RAN LT ENG AT 80 PERCENT TORQUE FOR 30 MIN, AFTE R CHECK OIL LEVEL AND VERIFIED IT WAS FULL. RECHECK OIL AFTER RUN AND OIL LEVEL DID NOT DROP FROM FULL LINE, PRIOR TO F IRST ENG RUNS SERVICED 2 QTS OF OIL TO LT ENG, PERFORMED 2ND ENG RUN OF LT ENG AT 80 PERCENT TORQUE FOR 30 MIN AFTER RUN OIL CONSUMPTION WAS 0. OIL LEVEL OF LT ENGINE REMAINED AT FULL. 2 L 7 2 4T 4 T RT A52EU E8NE6 2008011500036 20080115 00036 SO 2008 1 15 C2XA08RI006 1 20071226 A 2424 51525014A GCU EMB 145 EMB145ER 3260211 SO APU INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14943 7739 107 145040 FLT 3142 - EWR - CREW REPORTED APU GENERATOR AND GENERATOR NR 1 OFF BUSS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNE VENTFULLY. EWR MX REMOVED AND REPLACED APU GCU AND GENERATOR NR 1 AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008011500046 20080115 00046 NM 2008 1 15 0711002 1 20071109 A 2751 1817383 POSITION SENSOR BOEING 737 737230C 1384472 NM T/E FLAP MALFUNCTIONED A MJYA L A ABORTED APPROACH UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SW 07 767TW 20258 FLAP ASYMMETRY LOCKOUT AT 1 UNIT. DIVERTED FROM KLZU TO KATL (RUNWAY TOO SHORT FOR FLAPS 1 LANDING). 2 L 7 2 4F A16WE 2008011500064 20080115 00064 EU 2008 1 15 NSVA20070127 1 20070511 A 2612 89905202 CONTROL UNIT SAAB SF340 340B 7860101 EU FIRE DETECTION MALFUNCTIONED A NSVA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 194CJ 194 ON OR SHORTLY AFTER TAKEOFF, THE LEFT ENGINE NUISANCE FIRE CWP AND LEFT ENGINE "T" HANDLE ILLUMINATED ALONG WITH A TRIPL E CHIME FOR APPROX 3-5 SECONDS. NO OTHER ADVERSE INDICATIONS NOTICED. REMOVED AND REPLACED LT FIRE DETECTOR CNTL UNIT IAW AMM 26-11-10-02, P/N OFF/ON: 899052-02, S/N OFF: 0581, S/N ON: 0798. FURTHER TROUBLESHOT NACELLE FIRE DETECT SYSTEM AT THE FIRE LOOP, AND FOUND NO FAULTS IAW AMM 26-11-00-05. OP'S CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011500067 20080115 00067 NM 2008 1 15 UPS08M51364 1 20071119 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C RIGHT WING FUEL TANK STRINGER NR 9 END SUSPECT CRACKED. HFEC INSP C/O FOUND CRACK APPROX 10.25". STR 9 SPLICE END & HI-LOKS AT REPAIR AREA REMOVED. CRACK AT STR 19 SLOT OUT PER SRM 57-10-00 FIG 10 VI R35. HFEC INSP C/O ON SLOT OUT AREA, NO CRACK EVIDT. REPAIR ANGLES FAB PER SRM 57-20-00 FIG 10 VI R35. REPAIR ANGLES & STR 9 SPLICE END INSTALLED ON RIGHT WING STR 9 END. CAP SEAL C/O ON REPAIR AREA. LEAK CHECK SATIS. 2 L 7 3 4F RT A22WE 2008011500072 20080115 00072 EU 2008 1 15 NSVA20070061 1 20070308 A 2770 3CF SWITCH SAAB SF340 340B 7860101 EU GUST LOCK MALFUNCTIONED A NSVA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 311CE 214 GUST LOCK LIGHT ILLUMINATED, ENSURE GUST LOCK DISENGAGED, PULLED CB G4 DISCONNECTED C/P SWITCH. REMOVED AND REPLACED TH E RUDDER GUST LOCK SWITCH3CF IAW SMM 27-72-15-05, RIGGED AND TESTED SYSTEM OP'S CHECK GOOD IAW SMM 27-72-15-05. RIGGED AND TESTED SYSTEM GOOD IAW SMM 27-72-15-05. 2 L 7 2 4T RT A52EU 2008011500073 20080115 00073 CE 2008 1 15 NSVA20070197 1 20070727 A 6123 AUTOFEATHER SYS BEECH 1900 1900D 1154162 CE RIGHT MALFUNCTIONED A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 152MJ UE52 RT ENGINE WILL NOT AUTOFEATHER. RESET CB9 AND OPS CHECK NORMAL IAW BMM 61-21-00. 2 L 7 2 4T RT A24CE 2008011500077 20080115 00077 NM 2008 1 15 USAA920080066 1 20071219 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FLOORBEAM, BS 328, LBL 12. REPLACED FLOORBEAM, BS 328, LBL 12 IAW B737 SRM 53- 10-51-2R5. 2 L 7 2 4F RT A16WE 2008011500084 20080115 00084 NM 2008 1 15 USAA920080073 1 20071130 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 663, S3R. REPAIRED FRAME, BS 663, S3R IAW USAIRWAYS EA 100069. 2 L 7 2 4F RT A16WE 2008011500098 20080115 00098 EU 2008 1 15 NSVA20070135 1 20070521 A 3297 GROUND WIRE SAAB SF340 340B 7860101 EU LT MLG DOWNLOCK BROKEN A NSVA O OTHER N FALSE WARNING AP APPROACH 1 EA 27 277MJ 277 LT MLG GEAR DOWN LOCK INDICATION ERRATIC. FOUND LT MLG DOWNLOCK GROUND WIRE BROKEN IN WHEEL WELL. REPAIRED BROKEN WIRE BY INSTALLING NEW TERMINAL IAW SAAB WM 20-20-10, FUNCTION TEST OF EXT AND RETRACTION GOOD IAW SAAB MM 32-30-00. 2 L 7 2 4T RT A52EU 2008011500120 20080115 00120 NM 2008 1 15 USAA920080089 1 20071215 A 5322 SHEAR TIE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED SHEAR TIE, BS 360, S14L - S15L. REPLACED SHEAR TIE, BS 360, S14L - S15L IAW B7 37 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008011500124 20080115 00124 NM 2008 1 15 USAA920080093 1 20071216 A 5320 69489854 ATTACH FITTING BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED INTERCOSTAL ATTACH CLIP, BS 360, S10L. REPLACED INTERCOSTAL ATTACH CLIP, BS 36 0, S10L IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008011500129 20080115 00129 NM 2008 1 15 USAA920080095 1 20071221 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 380, S8R. REPAIRED FRAME, BS 380, S8R IAW USAIRWAYS TYPICAL REPAIR 5 3-10-25. 2 L 7 2 4F RT A16WE 2008011500133 20080115 00133 NM 2008 1 15 USAA920080098 1 20071218 A 5340 69353506 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED STRINGER CLIP, BS 500A, S16R. REPLACED STRINGER CLIP, BS 500A, S16R IAW B737 S RM 51-10-00. 2 L 7 2 4F RT A16WE 2008011500191 20080115 00191 EA 2008 1 15 VNAA0712002 1 20071220 A 7830 1267588 PDU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE THRUST REVERSER FAILED A VNAA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 05 262PS 8249 7962 CREW REPORTED A LEFT HAND THRUST REVERSER UNLOCKED AMBER MESSAGE AFTER TAKEOFF. CREW FOLLOWED THE QRH AND RETURNED TO T RI WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE POWER DRIVE UNIT IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008011500195 20080115 00195 EU 2008 1 15 NSVA20070239 1 20071002 A 3231 DOOR SAAB SF340 340B 7860101 EU MLG MALFUNCTIONED A NSVA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 27 370PX 340B300 LT INBD MLG DOOR REMAINED OPENED IN FLIGHT. INSPECTED LT MLG DOOR, CLEANED 5-10 TIMES IAW 32-10-00-00. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011500220 20080115 00220 EA 2008 1 15 MASA200700491 1 20070807 A 3350 1317 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 508MJ 10087 ASH 7454 CLT-IAD - OVHD EMERGENCY FLOOD LIGHT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2008012800120 20080128 00120 SO 2008 1 28 FDKA200711330 1 20071112 A 2611 SMOKE WARNING EMB 145 EMB145LR 3260212 SO CARGO BAY MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 852MJ 145567 FDM 6150 TYS (0330 PHX LCL) - BAG SMOKE WARNING WILL NOT EXTINGUISH. MX RESET OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008011500273 20080115 00273 EA 2008 1 15 MASA200700580 1 20070913 A 3350 587387221 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 931LR 15031 ASH FLT 2876 LAS-ELP - PILOT REPORTED THAT THE SERVICE DOOR AFT SILL LIGHT STRIP MISSING. MX INSTALLED STRIP. 2 L 7 2 4F RT A21EA 2008011500282 20080115 00282 EU 2008 1 15 WRNA200700064 1 20071228 A 3230 C23005302 DAMPER AIRBUS 300 A300B4203 3930306 EU LT MLG MALFUNCTIONED A WRNA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 05 510TA 100 AFTER DEPARTURE WHEN RAISING GEAR, LEVER WOULD NOT GO PAST THE MID POSITION, GEAR POSITION LIGHTS REMAINED 'GREEN'. RET URNED TO FIELD AND MADE A SAFE LANDING. AIRCRAFT MAINTENANCE FERRIED TO CTS IN JAPAN FOR CORRECT ACTION. REPLACED LT G EAR PITCH DAMPER, AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A35EU 2008011500294 20080115 00294 GL 2008 1 15 C2XA08TY002 2 20071228 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 15574 145639 E1 ITT IN AMBER DURING FLT, DIVERTED TO TYS. WAITING FOR LOG PAGE WILL UPDATE SDR. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008011500298 20080115 00298 EA 2008 1 15 MASA200700710 1 20071018 A 2910 601R7528637 LINE CNDAIR CL600 CL6002D24 1390016 EA HYDRAULIC SYS LEAKING A MASA O OTHER K FLUID LOSS CR CRUISE 1 SW 07 919FJ 15019 ASH FLT 2731 LGB - PHX - EMERGENCY DECLARED ON INBOUND TO PHX DUE TO HYDRAULIC SYSTEM NR 2 LOW PRESSURE WARNING WITH INB OARD FLIGHT SPOILERS AND INBOARD SPOILERONS CAUTION MESSAGES. MX REMOVED AND REPLACED NR 2 HYDRAULIC EDP PRESSURE LINE. 2 L 7 2 4F RT A21EA 2008011500302 20080115 00302 EA 2008 1 15 MASA200700373 1 20070628 A 5210 ROLLER CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR OUT OF ALIGNMENT A MASA O OTHER O OTHER LD LANDING 1 SW 07 516LR 10258 ASH 7195 IAD - CAPTAIN REPORTED COULD NOT OPEN MAIN PAX DOOR UPON ARRIVAL IN PIT. CLEANED AND LUBRICATED PAX DOOR ALIGN MENT ROLLERS, OPS CKD GOOD. 2 L 7 2 4F RT A21EA 2008011500304 20080115 00304 EA 2008 1 15 MASA200700777 1 20071106 A 3260 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA MLG ILLUMINATED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 75993 7372 ASH FLT 7322, BUF - LEFT MAIN GEAR DISAGREE IN FLIGHT. MX IS TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 2008011500305 20080115 00305 EA 2008 1 15 MASA200700778 1 20071106 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 938LR 15038 ASH FLT 2645 CLT - AFT CEILING EMERGENCY FLOODLIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 2008011500306 20080115 00306 NM 2008 1 15 MASA200700779 1 20071107 A 2820 601R622911 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007 NM NR 1 FUEL SYS MALFUNCTIONED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 991HA 431 ASH FLT 2760 PHX-CDL. - NR 1 FUEL FILTER BY-PASS CAUTION LIGHT ILLUMINATED IN FLIGHT. REMOVED AND REPLACED FUEL PRESSUR E SWITCH. 2 H 7 2 4T RT A13NM 2008011500307 20080115 00307 EA 2008 1 15 MASA200700678 1 20071009 A 2450 820465 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA ADG MALFUNCTIONED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 592ML 12161 7410 ASH FLT 7276 PHL-IAD - PILOT REPORTED THAT THE ADG DEPLOYED IN FLIGHT AT 150 KNOTS FOR A DURATION OF 45 MINUTES. MX REP LACED ADG CONTROLLER. 2 L 7 2 4F RT A21EA 2008011500309 20080115 00309 SO 2008 1 15 C2XA07ON036 1 20071208 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO CABIN SMOKE A C2XA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 14180 145900 FLT 7682 - SLC TO LAX - DURING TAKEOFF ROLL FLIGHT CREW REPORTED SMOKE IN CABIN. CONTRACT MX PERFORMED RUN-OPS OF AIRCR AFT AND APU AT FULL FLOW PACKS. NO SMOKE FOUND AND NOTED. A/C WAS RETURNED FOR SERVICE IN AIRWORTHY CONDITIONS. PROBL EM WAS CORRECTED WITHOUT EXCHANGING PARTS. 2 L 7 2 4F RT 2008011500334 20080115 00334 WP 2008 1 15 ABXA080009 1 20071213 A 5313 592599225 LONGERON DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 LONGERON 30 CORRODED AT FS 415 AND SPLICE WAS CRACKED. REPLACED DAMAGED SECTION OF LONGERON 30 IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 2008011500335 20080115 00335 WP 2008 1 15 ABXA080016 1 20071213 A 5320 992348487 INTERCOSTAL DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 CEILING INTERCOSTAL STA 180, LEFT BUTT LINE 30 - 54 WAS CRACKED AT INBOARD END. REMOVED DRIP PAN TO FOM, INSTALLED REPA IR DOUBLERS: -05, 015, 017, 021 AND -19 IAW DC9 SRM 53-05, FIGURE 75. 2 L 7 2 4F A6WE 2008011500339 20080115 00339 WP 2008 1 15 ABXA080019 1 20071213 A 5320 99105035 CUSP WEB DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 CUSP WEB HAD 3 CRACKS, FS 1021 TO 1041 LEFT SIDE. REPAIRED CUSP WEB IAW DC9 SRM. CRACK LENGTHS 7/8", 3/4", AND 1". 2 L 7 2 4F A6WE 2008011500340 20080115 00340 WP 2008 1 15 ABXA080020 1 20071215 A 5347 S2914913M24000 SEAT TRACK DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 SEAT TRACK AT STA 180 (APPROXIMATELY) LEFT BUTT LINE 44 WAS CRACKED ON OUTBOARD FLANGE. REMOVED AND REPLACED TRACK SECT ION FROM FS 160 TO 226, LEFT BUTT LINE 44. INSTALLED TRACK IAW DC9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2008011500341 20080115 00341 WP 2008 1 15 ABXA080015 1 20071213 A 5230 3914025502 FITTING DOUG DC9 DC941 302207N WP AFT CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 AFT LOWER CARGO DOOR BEAM 1 AFT END FITTING CRACKED AT FASTENER. REMOVED AND REPLACED AFT LOWER CARGO DOOR BEAM NR 1 AF T FITTING. 2 L 7 2 4F A6WE 2008011100274 20080111 00274 NM 2008 1 11 MASA200700654 1 20070928 A 2120 UNKNOWN DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE COCKPIT & CABIN SMOKE A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 437YV 437 PCEAG0003 ASH FLT 2851 PHX-YUM - PILOT REPORTED SMOKE IN THE FLIGHT DECK AND CABIN AFTER ENGINE START. INSPECTED A/C SYSTEM, OIL LEVEL GOOD, ENGINE RUNS GOOD, NO DEFECTS NOTED. 2 H 7 2 4T 4 T RT A13NM E20NE 2008011100290 20080111 00290 NM 2008 1 11 DLM90071646 1 20071219 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 LT CUSP WEB CRACKED FS 1355 AT LIGHTNING HOLE. REPAIRED CRACKED CUSP WEB IAW MD-90 SRM 51-11-01, ON N/R 2700-0231 AT HM V-2 IN OKC. 2 L 7 2 4F RT A6WE 2008011100313 20080111 00313 NM 2008 1 11 DLM88071668 1 20071230 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 963DL 49982 FUSELAGE SKIN BENT AND TORN AT FORWARD EDGE OF C-1 CARGO DOOR. DAMAGE WAS CUT OUT AND A REPAIR DOUBLER AND TRIPLER WERE INSTALLED. 2 L 7 2 4F RT A6WE 2008011100315 20080111 00315 EU 2008 1 11 NSVA20070157 1 20070619 A 7600 5308216 CONTROL QUADRANT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE DEFECTIVE A NSVA O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 35SZ 35 FI STOP OPEN LIGHT ILLUMINATED IN FLIGHT. REPLACED CONTROL QUADRANT IAW SAAB AMM 76-10-05, NO DISCREPANCIES NOTED, PN O N: 53162-4, SN ON: 074, PN OFF: 53082-16 SN OFF: 187. 2 L 7 2 4T 4 T RT A52EU E8NE6 2008011100318 20080111 00318 EU 2008 1 11 NSVA20070153 1 20070607 A 3697 WIRE SAAB SF340 340B 7860101 EU BLEED AIR SYS SHORTED A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 27 251CJ 251 THE A/C WAS POWERED W/ EXT PWR, ALL LIGHT SWITCHES WERE ON. THE CABIN SMELLED OF SMOKE. THERE WAS A CLOUD OF SMOKE IN THE COCKPIT. TURNED OFF ALL SWITCHES, POWERED DOWN THE A/C AND ORDERED ALL CREW OFF OF THE PLANE. FOUND SHORTED WIRE T O R BLD AIR LEAK C/B P13. REMOVED AND REPLACED ALL BURNED WIRES IAW WBM 20-20-10 AND REMOVED AND REPLACED C/B P13. OPS CHECK GOOD IAW SAAB AMM 36-23-00 P/N MS3320-5. 2 L 7 2 4T RT A52EU 2008011400067 20080114 00067 EU 2008 1 14 COEA0756821 1 20070824 A 5311 S53672408226 FRAME AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. LEVEL 2 CORROSION: CORROSION ON CABIN FRAME 39. FRAME 39 LOWER SEGMENT FROM STRINGER 13L TO 13R. FRAME 39L, FRAME DOUBLER ABOVE CREASE BEAM. FRAME 39R, FRAME DOUBLER AT STRINGER 14R. REMOVED AND REPLACED, LOWE R FRAME SEGMENT PN S53672408200, FRAME DOUBLER PN S53672408226, AND S53672408228. WO 72241, 2, NR 200003, 19, 30. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400071 20080114 00071 EU 2008 1 14 COEA0751821 1 20070823 A 5311 S53572610201 FRAME AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE CRACKED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. MAJOR REPAIR: FUSELAGE RT FRAME 27 IS CRACKED AT UPPER BOX AFT INTERCOSTAL ATTACHMENT. REMOV ED DAMAGED AREA AND STRESS RELIEVED IAW ATR SRAS, DO/TS-3941/07, 4264. REF: NOTE DO/TS 5198/07. WO 72242, NR 200014. ( K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400104 20080114 00104 EU 2008 1 14 COEA0737821 1 20071003 A 5313 S53671200218 STRINGER AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. MAJOR REPAIR: CORROSION LOWER STRINGER 15R, FORWARD OF FRAME 36. SPLICED IN NEW STRINGER SEC TION FROM FRAME 35 TO FRAME 38. WO 72242, NR 200119. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400107 20080114 00107 EU 2008 1 14 COEA0734821 1 20070822 A 5730 S57212438201 PANEL AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE RT WING CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 29796 253 FOUND DURING HEAVY CHECK. MAJOR REPAIR. CORROSION ON RT WING UPPER FIXED PANEL COMMON TO THE AILERON CENTER HINGE FITT ING. REPLACED PANEL WITH NEW FABRICATED PANEL. WO 72245, NR 602006. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400116 20080114 00116 NE 2008 1 14 AMTA200700717 2 20071219 A 7321 1853M56P08 HMU BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE NR 2 ENGINE UNSERVICEABLE A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 308TZ 17095 12866 28244 ENGINE CONTROL LIGHT, LIGHT ON, ENGINE NR 2. REMOVED AND REPLACED NR 2 ENGINE HYDROMECHANICAL UNIT IAW MM 73-21-10-4. OPS CHECK NORMAL. OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A16WE E2GL 2008011400117 20080114 00117 NM 2008 1 14 AMTA200700716 1 20071218 A 2530 8203610000 OVEN BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE FWD GALLEY UNSERVICEABLE A AMTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 552TZ 32586 F/A REPORTED (HEAVY SMOKE IN THE FORWARD GALLEY, OVEN WAS ON, REMOVED POWER) WHITE SMOKE (ELECTRICAL BURNING SMELL PERS ISTED) EMERGENCY DECLARED, RETURNED TO DEPARTURE. SMOKE SLOWLY DISSIPATED. REMOVED AND REPLACED OVEN IAW MM CHAP 25, O PS CHECKS NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008011400124 20080114 00124 EU 2008 1 14 NSVA20070147 1 20070601 A 7720 10227N01 INDICATOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE MALFUNCTIONED A NSVA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 321CJ 321 LEFT ENGINE ITT RED LINED ON TAKE OFF AND DIGITAL PORTION OF GAUGE WENT BLANK. REMOVED AND REPLACED LT ENG ITT GAUGE IA W AMM 77-20-05. OPS GOOD P/N ON/OFF 10227N01 S/N OFF B599A S/N ON 124A, GROUND RUN ENGS AT TAKEOFF PWR ACC IND NORMAL A CC INDICATIONS NORMAL. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011400127 20080114 00127 EU 2008 1 14 NSVA20070182 1 20070712 A 2612 FIRE LOOP SAAB SF340 340B 7860101 EU LT NACELLE DIRTY A NSVA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 210CJ 210 LFT FIRE DET FAIL CAUTION ILLUM IN FLT. INSPECTED SENSOR LOOP ON LT ENGINE REF AMM 26-11-00-06 FOUND SMALL PIECE OF SAF ETY WIRE ON LOOP. REMOVED PIECE OF SAFETY WIRE CLEANED AROUND LOOP CONNECTIONS AND CLEANED FIRE CONTROL REF 26-11-10. PERFORMED OPS CHECK REF 26-11-00-05, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011400128 20080114 00128 EU 2008 1 14 NSVA20070186 1 20070715 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS MALFUNCTIONED A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 321CJ 321 DURING OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM ON A LINE CHECK 3 COVE EMERGENCY LIGHTS WERE FOUND NOT ILLUMINATI NG. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY 20LN AND SYSTEM TESTED SATISFACTORILY, PN 60-1321-1. 2 L 7 2 4T RT A52EU 2008011400135 20080114 00135 EA 2008 1 14 NSVA20070140 2 20070527 A 7261 FITTING BEECH 1900 1900D 1154162 CE PWA PT6 PT6A6 52043 EA OIL LINE LOOSE A NSVA A UNSCHED LANDING K Y FLUID LOSS ENGINE STOPPAGE CR CRUISE 1 EA 27 136MJ UE36 RT ENG OIL PRESS FLUCTUATED BETWEEN 65-70 THEN DROPPED BELOW 60 PSI WITH LOW OIL PRESS LIGHT ILLUMINATED. INFLIGHT SHU TDOWN. TIGHTENED OIL COOLER RETURN LINE FITTING IAW BE1900 MM 71-00-00, GROUND RAN AIRCRAFT 20 MIN IAW CRUISE CONFIGURA TION, ALL ENGINE PARAMETERS NORMAL, NO FURTHER LEAKAGE DETECTED. 2 L 7 2 4T 3 T RT A24CE E4EA 2008011400136 20080114 00136 EU 2008 1 14 NSVA20070069 1 20070318 A 3297 DG505 WIRE SAAB SF340 340B 7860101 EU MLG CHAFED A NSVA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 27 277MJ 277 LANDING GEAR IN-TRANSIT LIGHT ON WHEN ON THE GROUND AND GEAR HANDLE IN DOWN POSITION SHOWING THREE GREEN. INSPECTED IN- TRANSIT CIRCUIT AND FOUND LT MLG DOWNLOCK SWITCH HARNESS WIRE DG505 SLIGHTLY CHAFED INTO GROUND WIRE DG506 AT AN AREA BE LOW CONNECTOR SGAJ1. REPAIRED DAMAGED WIRES WITH NEW SLEEVE AND ALL CONNECTORS IAW SAAB 340 20-20-35A. AIRCRAFT WIRING MANUAL. JACKED A/C PERFORMED EXT/RET CHECKS PER 32-30-00 AMM, OPS CHECK NORMAL. 2 L 7 2 4T RT A52EU 2008011400145 20080114 00145 CE 2008 1 14 NSVA20070082 1 20070402 A 7603 POWER LEVER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67B 52043 NE OUT OF RIG A NSVA O OTHER J WARNING INDICATION LD LANDING 1 EA 27 171CJ UE71 DURING FLARE POWER LEVERS BROUGHT TO FLIGHT IDLE AIRPLANE YAWED VIOLENTLY LEFT. ADJUSTED RIGGING OF LT AND RT ENGINES A ND PROPS IAW BEECH 76-10-00, REQUIRES ENGINE TO BE RUN TO CHECK RIGGING OF ENGINES AND PROPS. RAN ENGINES TO CHECK RIGG ING OF ENGINE AND PROP CONTROLS IAW MM 76-10-00. 2 L 7 2 4T 4 T RT A24CE E26NE 2008011400161 20080114 00161 EU 2008 1 14 NSVA20070120 1 20070502 A 3246 AON506227 WHEEL SAAB SF340 340B 7860101 EU NLG VIBRATION A NSVA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 EA 27 204CJ 204 EXCESSIVE NOSE WHEEL SHIMMY ON TAKEOFF ROLL. REMOVED AND REPLACED NOSE WHEEL IAW AMM 32-41-15-4 PN OFF AND AON 506227 S N RT NOSE AUG 85-0258/SEP890291 SN LT NOSE OCT 880691. 2 L 7 2 4T RT A52EU 2008011400167 20080114 00167 EU 2008 1 14 NSVA20070118 1 20070429 A 3150 WARNING LIGHT SAAB SF340 340B 7860101 EU ILLUMINATED A NSVA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 191MJ 191 AFTER T/O FLIGHT IDLE STOP OPEN LIGHT ILLUMINATED. RESET FLIGHT IDLE STOP IAW AMM 76-10-60. LIGHT EXTINGUISHED, NO FAU LTS NOTED. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011400174 20080114 00174 EU 2008 1 14 NSVA20070114 1 20070425 A 2750 8519M3 CONTROL BOX SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE TE FLAPS MALFUNCTIONED A NSVA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 277MJ 277 FLAPS ANNUNCIATOR LIGHT ON CWP ILLUMINATES REPEATEDLY IN FLIGHT, GREEN LIGHT ON TEST PANEL 1 ILLUMINATES AND FLAP INDICA TOR NEEDLE FLUCTUATES. SERVICED HYDRAULIC ACCUMULATORS IAW SMM 12-10-29. PERFORMED VISUAL INSPECTION OF FLAP CONTROL V ALVE FLAP ACTUATORS. NO LEAKS NOTED REQUIRES FURTHER T/S. VERIFIED FLAP ACTUATORS ARE NOT LEAKING SUSPECT FLAP RIGGING . FLAP CONTROL BOX IAW SAAB MM 27-51-10, P/N OFF/ON: 8519M3S/N OFF: 271, S/N ON: 424. OPERATIONAL CHECK AND RIGGING A RE GOOD IAW SAAB MM 27-51-00. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011400181 20080114 00181 EU 2008 1 14 NSVA20070152 1 20070606 A 7603 POWER LEVER SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE MALFUNCTIONED A NSVA O OTHER O OTHER LD LANDING 1 EA 27 344CJ 344 FLIGHT IDLE STOP HAD TO BE PULLED ON LANDING. ORANGE F1 STOP OPEN LIGHT DID NOT ILLUMINATE. POWER LEVERS DID GO INTO R EVERSE AFTER F1 STOP KNOB PULLED. PERFORMED OYRD SWITCH WARNING AND SYSTEM INDICATION TEST IAW SAAB AMM 76-10-60-05. O PS CHECK GOOD. CHANGED RELAY PN: M83726-28-7001P IN RT ELECTRICAL BAY NO FIX. CONFIRMED PROP LEVERS MOVE INTO REVERSE WITH F1 STOP OVERRIDE PULLED. PILOT'S REPORTED NO DISCREPANCIES DURING FLIGHT FROM LGA - ALB. PERFORMED FLIGHT IDLE ST OP SOLENOID TEST AND OPERATIONAL TEST OF FI STOP MECHANISM IAW SAAB AMM 76-10-60, NO FAULTS FOUND. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011400186 20080114 00186 EU 2008 1 14 NSVA20070155 1 20070612 A 3222 STRUT SAAB SF340 340B 7860101 EU NLG UNDERSERVICED A NSVA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 311CE 214 GEAR UNSAFE LIGHT AFTER T/O. SERVICED NLG STRUT IAW COLGAN WORKCARD 32-21-075, OPS CHECK GOOD, MEL CLEARED. 2 L 7 2 4T RT A52EU 2008011400188 20080114 00188 EU 2008 1 14 NSVA20070075 1 20070326 A 2611 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU E/E BAY MALFUNCTIONED A NSVA O OTHER N FALSE WARNING CR CRUISE 1 EA 27 35SZ 35 AVIONICS SMOKE LIGHT ILLUMINATED IN FLIGHT. DID TEST OF SMOKE DETECTORS IAW SAAB MM 26-13-00-5, OPS CHECK GOOD. DID FA ULT ISOLATION OF AVIONICS SMOKE DETECTOR WITH SMOKE PRESENT AND WITHOUT. ALARM SOUNDED WHEN PRESENT AND EXTINGUISHED WH EN CLEAR, CHECKED PINS IAW SAAB MM 26-13-00-1, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011400194 20080114 00194 EU 2008 1 14 NSVA20070045 1 20070223 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E BAY DIRTY A NSVA K NONE N FALSE WARNING IN INSP/MAINT 1 EA 27 321CJ 321 AVIONICS SMOKE ANNUNCIATOR BRIEFLY ILLUMINATED. CK CONNECTOR ON BACK OF SMOKE DETECTOR, FOUND TO BE TIGHT CLEAN . REIN STALLED PLUG LAMP CK OK AT THIS IME PER 26-11-00. 2 L 7 2 4T RT A52EU 2008011500005 20080115 00005 2008 1 15 NSVA20070174 4 20070702 A 3425 COMPUTER SAAB SF340 SF340A 7850100 EU AHRS MALFUNCTIONED A NSVA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 27 35SZ 439 35 GATE RETURN FO SIDE EAADI WOULD NOT INITIALIZE. REMOVED AND REPLACED NR 2 AHRS COMPUTER WITH SERVICEABLE UNIT, PERFORME D OPS CHECKS. OPS CHECKS NORMAL. 2 L 7 2 4T RT A52EU 2008011500009 20080115 00009 EU 2008 1 15 NSVA20070171 1 20070701 A 3150 WARNING LIGHT SAAB SF340 SF340A 7850100 EU CABIN PRESSURE ILLUMINATED A NSVA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 35SZ 35 AFTER ENGINE START CABIN PRESSURE WARNING ANNUNCIATOR ILLUMINATED. CABIN MAX DIFF READS 7.5 WHEN CABIN NOT PRESSURIZED. PERFORMED SEVERAL STARTS, CABIN PRESS IND DID NOT ILLUMINATE, OPS CHECK GOOD EVERY TIME. COULD NOT DUPLICATE DISCREPA NCY. 2 L 7 2 4T RT A52EU 2008011500014 20080115 00014 CE 2008 1 15 NSVA20070099 1 20070415 A 5220 LATCH BEECH 1900 1900D 1154162 CE EMERGENCY EXIT UNSECURE A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 221CJ UE221 BOTH EMERGENCY EXIT OUTSIDE HANDLES OPEN. INSPECTED DOORS, BOTH DOORS STILL LATCHED WITH HANDLES PUSHED IN TOO FAR. RE SECURED LATCHES ON BOTH DOORS. REF BMM 52-20-00-201, RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2008011500039 20080115 00039 CE 2008 1 15 NSVA20070178 1 20070708 A 3260 SWITCH BEECH 1900 1900D 1154162 CE MLG OUT OF ADJUST A NSVA O OTHER N FALSE WARNING CR CRUISE 1 EA 27 155CJ UE55 WHILE IN CRUISE FLIGHT, RED "IN TRANSIT" INDICATOR ILLUMINATED IN LANDING GEAR HANDLE. GEAR EXTENDED SUCCESSFULLY. JAC K ACFT, RETRACTED GEAR, LIGHT IN HANDLE ILLUMINATED DURING RETRACTION AND WENT OUT AT END OF UP CYCLE. EXTENDED GEAR LI GHT IN HANDLE OPERATED NORMALLY. INSPECTED WIRES, AND SWITCHES, LEFT UP SWITCH APPEARED TO BE SHORTER IN LENGTH THAN RI GHT, LENGTHENED LEFT UP SWITCH PERFORMED GEAR CYCLE. ALL CHECKS NORMAL AT THIS TIME IAW BEECH AMM 32-60-00. 2 L 7 2 4T RT A24CE 2008011500041 20080115 00041 NE 2008 1 15 NSVA20070142 2 20070530 A 7297 7292531 WIRE HARNESS SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE WORN A NSVA O OTHER N FALSE WARNING CL CLIMB 1 EA 27 370PX 300 L/R FUEL FLOW INDICATORS ERRATIC. FOUND BRACKET HOLDING START BLEED VALVE BROKEN. BLEED VALVE WORE THROUGH RT ENGINE " WHITE HARNESS." REMOVED AND REPLACED BRACKET AND HARNESS IAW AMM 71-50-00, PN OFF/ON (BRACKET), 5051T77G02, PN OFF/ON ( HARNESS) 7292531. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011500049 20080115 00049 EU 2008 1 15 NSVA20070188 1 20070717 A 2697 WIRE SAAB SF340 340B 7860101 EU OVERHEAT SYS CHAFED A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 350CJ 350 TAIL PIPE HOT WILL NOT TEST ON LEFT SIDE ALSO NO MASTER WARNING BELL. REPAIRED CHAFED WIRE WG506 IAW WM 20-20, OPS CHEC K GOOD IAW SAAB MM 26-12-00, NO DISCREPANCIES NOTED. 2 L 7 2 4T RT A52EU 2008011500050 20080115 00050 EU 2008 1 15 NSVA20070088 1 20070406 A 2770 531624 SWITCH SAAB SF340 340B 7860101 EU GUST LOCK MALFUNCTIONED A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 202SR 202 GUST LOCK LIGHT ILLUMINATED WHEN GUST LOCK IS RELEASED. TS TO QUADRANT GUST LOCK SWITCH QUADRANT REMOVED AND REPLACED I AW 76-10-05-09 OPS AND RIGGING KS STILL NEED TO BE DONE. CONTROL LEVERS, INSTALLED COTTER PINS ON BOTH CONTROL LEVERS A ND GUST LOCK ROD END IAW AMM 76-10-15-02. PERFORMED OPS AND RIG CHECK IAW 76-10-00, BOTH OPS AND RIG CHECK GOOD PN 5316 2-4 SN OFF 0/8 SN ON 023. 2 L 7 2 4T RT A52EU 2008011500057 20080115 00057 SO 2008 1 15 C2XA08RI011 1 20071221 A 7931 23067667 TRANSDUCER EMB 145 EMB145LR 3260212 SO NR 2 FAULTY A C2XA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 27 19966 145131 FLT 2609 - EWR - CREW REPORTED ENGINE NR 2 OIL PRESS SPIKE TO THE RED RANGE (ABOUT 165) AND PRESSURE STAYED IN THE AMBER FOR MORE THAN 5 MIN. CREW PERFORMED AIR RETURN AND ACFT LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED ENGINE NR 2 OIL PRESS/TEMP TRANSDUCER IAW EMB145 AMM 79-31-01 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RE TURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008011500061 20080115 00061 NM 2008 1 15 UPS08551367 1 20071230 A 3350 LIGHT BOEING 757 75724APF 1384969 NM EXTERIOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 473UP 28846 INSPECTION TYPE:N/A EXTERIOR EMERGENCY EGRESS LIGHT ON AFT LOWER NR 1 DOOR DOES NOT ILLUMINATE. RELAMPED EMERGENCY EXIT EGRESS LIGHT PER MM 33-51-06-2. OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2008011500074 20080115 00074 NM 2008 1 15 USAA920080065 1 20071216 A 5320 6545834 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED INTERCOSTAL, BS 328 - BS 344, LBL 48. REPLACED INTERCOSTAL, BS 328 - BS 344, L BL 48 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008011500094 20080115 00094 NM 2008 1 15 USAA920080080 1 20071210 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 827, S9L. REPAIRED FRAME, BS 827, S9L IAW USAIRWAYS TYPICAL REPAIR 5 3-10-20E. 2 L 7 2 4F RT A16WE 2008011500095 20080115 00095 EU 2008 1 15 NSVA20070146 1 20070601 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 339CJ 339 2ND AND 3RD FLOOR LEVEL EMERGENCY LIGHTS OUT. PERFORMED OPS CK ON 2ND AND 3RD EMERGENCY FLOOR LIGHT IAW SAAB AMM 35-50- 00. OPS CK OK. 2 L 7 2 4T RT A52EU 2008011500108 20080115 00108 EU 2008 1 15 NSVA20070230 1 20070918 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY LOOSE A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 202SR 202 CARGO COMPARTMENT SMOKE DETECTION SYSTEM DOES NOT TEST. FOUND SMOKE DETECTOR LOOSE RESECURED, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011500121 20080115 00121 NM 2008 1 15 USAA920080090 1 20071215 A 5313 656177 STRINGER SPLICE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED STRINGER SPLICE, BS 360, S14L. REPLACED STRINGER SPLICE, BS 360, S14L IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008011500128 20080115 00128 EU 2008 1 15 NSVA20070247 1 20071204 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A NSVA O OTHER O OTHER NR NOT REPORTED 1 EA 27 294CJ 340B294 EMERGENCY LIGHTS, LAST FOUR EMERGENCY LIGHTS INOP, CHANGED OUT NR 5 POWER SUPPLY, OPS CHECKED GOOD. 2 L 7 2 4T RT A52EU 2008011500153 20080115 00153 EU 2008 1 15 NSVA20070203 1 20070806 A 2612 FIRE DETECTOR SAAB SF340 340B 7860101 EU LT NACELLE MALFUNCTIONED A NSVA O OTHER N FALSE WARNING AP APPROACH 1 EA 27 194CJ 194 LEFT FIRE WARNING ILLUMINATED DURING FLIGHT FOR APPROX 3 SECONDS THEN TURNED OFF ALL ENGINE, PARAMETERS REMAINED NORMAL, NO FIRE NOTED. INSPECTED LT ENG FIRE, NO DEFECTS NOTED INSPECTED AND RESECURED ECU PERFORMED OP TST OF ENG FIRE DETECT SYSTEM. OPS CHECK GOOD, NO DEFECTS NOTED PER SAAB AMM 31-50-05-04. 2 L 7 2 4T RT A52EU 2008011500167 20080115 00167 2008 1 15 NSVA20070205 2 20070808 A 7320 6068T72P22 HMU SAAB SF340 340B 7860101 EU NR 2 ENGINE MALFUNCTIONED A NSVA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 338CJ 338 NR 2 ENGINE TORQUE INDICATION INCREASES AND DECREASES 3 PERCENT APPROX EVERY 5-10 SECONDS, ITT, NG AND FUEL FLOW OK SHOW CHANGE AT SAME TIME. REMOVED AND REPLACED NR 2 ENGINE HMU IAW GE MM 73-00-00. OPS CHECK GOOD LEAK CHECK GOOD, P/N OFF 6068T72P22, S/N OFF WY554843, S/N ON WYG41854. 2 L 7 2 4T RT A52EU 2008011500184 20080115 00184 CE 2008 1 15 NSVA20070238 1 20070930 A 3234 1013841377 HANDLE BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A NSVA O OTHER J WARNING INDICATION LD LANDING 1 EA 27 152MJ UE52 LANDING GEAR FAILED TO EXTEND (NO INDICATION WITH GEAR HANDLE DOWN) RE-CYCLED GEAR. EXTENDED NORMALLY. REMOVED AND REP LACED LANDING GEAR CONTROL HANDLE. 2 L 7 2 4T RT A24CE 2008011500190 20080115 00190 EA 2008 1 15 VNAA0712003 1 20071215 A 2750 ECU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE T/E FLAP MALFUNCTIONED A VNAA O OTHER N FALSE WARNING AP APPROACH 1 GL 05 207PS 7873 CREW REPORTED A FLAPS FAIL IN FLIGHT ON FINAL APPROACH. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTE NANCE INTERROGATED THE FECU AND FOUND IT TO BE FLAGGING THE FLAP HANDLE MIS-POSITION. MAINTENANCE RESET THE FECU AND PE RFORMED A SYSTEM OPS CHECK IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008011500210 20080115 00210 EA 2008 1 15 MASA200700488 1 20070806 A 2740 SWITCH CNDAIR CL600 CL6002C10 1390015 EA STAB TRIM MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 506MJ 10073 ASH 7336 ORD-COS - RETURNED TO FIELD DUE TO CAPT STAB TRIM INOP. MX REMOVED AND REPLACED TRIM SWITCH. 2 L 7 2 4F RT A21EA 2008011500240 20080115 00240 EA 2008 1 15 MASA200700640 1 20070925 A 2560 BF18722001887220 PLACARD CNDAIR CL600 CL6002C10 1390015 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 502MJ 10050 ASH FLT 7227 IN ORD, CAPTAIN REPORTED PHOTO ILLUM ARROWS ON FLOOR MISSING AT ROW 12 ON BOTH SIDES OF ACFT. MX RE-INSTA LLED AND SECURED NEW PHOTO ILLUM ARROWS, ACFT CONTINUED OPERATIONS. 2 L 7 2 4F RT A21EA 2008011500253 20080115 00253 EA 2008 1 15 MASA200700650 1 20070927 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 502MJ 10050 ASH FLT 7227 IN IAD, CAPTAIN REPORTED FLOOR EMERGENCY LIGHT STRIP LOOSE. MX SECURED STRIP, ACFT CONTINUED OPERATIONS. 2 L 7 2 4F RT A21EA 2008011500260 20080115 00260 EA 2008 1 15 MASA200700834 1 20071130 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 919FJ 15019 ASH FLT 2632 CLT-EWR - EMERGENCY LIGHTS WILL NOT TURN OFF. MX RESET EMERGENCY LIGHTING SYSTEM. NO FURTHER DEFECTS NOTE D. 2 L 7 2 4F RT A21EA 2008011500263 20080115 00263 EA 2008 1 15 MASA200700798 1 20071113 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA CABIN ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 518LR 10259 ASH FLT 7139 IAD-RDU - UNUSUAL ODOR IN GALLEY DURING FLIGHT. MX PERFORMED OPS CHECKS OF AIR CONDITIONING, GALLEY HEAT, AND RECIRC SYSTEMS. NO UNUSUAL SMELLS NOTED. 2 L 7 2 4F RT A21EA 2008011500267 20080115 00267 EA 2008 1 15 MASA200700618 1 20070922 A 3240 6007300 SENSOR CNDAIR CL600 CL6002D24 1390016 EA BRAKE OVERHEAT MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 932LR 15032 ASH FLT 2667 SYR-CLT - BRAKE OVERHEAT WARNING NR 4 BTMS. MX CHANGED BTMS SENSOR. 2 L 7 2 4F RT A21EA 2008011500268 20080115 00268 2008 1 15 MASA200700808 4 20071118 A 2562 WARNING LIGHT CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS ILLUMINATED A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 934FJ 15034 ASH FLT 2743 PHX-PSP - ELT ON CAUTION MESSAGE WITH ELT SWITCH IN ARM/RESET POSITION. MX RESET THE SYSTEM, OPS CHECK GOO D. 2 L 7 2 4F RT A21EA 2008011500270 20080115 00270 EA 2008 1 15 MASA200700776 1 20071105 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 902FJ 15002 ASH FLT 2821 PHX - EMERGENCY EXIT OVERHEAD FLOOD LIGHT INOPERATIVE. MX RELAMPED. 2 L 7 2 4F RT A21EA 2008011500274 20080115 00274 EA 2008 1 15 MASA200700582 1 20070915 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 907FJ 15007 ASH FLT 2606 CLT - AFT EMERGENCY FLOOD LIGHT INOP. MX RESECURED LIGHT ASSEMBLY. 2 L 7 2 4F RT A21EA 2008011500300 20080115 00300 EA 2008 1 15 MASA200700861 1 20071206 A 5220 LATCH CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT UNKNOWN A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 906FJ 15006 ASH FLT 2884 PHX - RT AFT EMERGENCY EXIT DOOR CAUTION. MX CHANGED LATCH. 2 L 7 2 4F RT A21EA 2008011500308 20080115 00308 EA 2008 1 15 MASA200700522 1 20070825 A 5220 SEAL CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 918FJ 15018 ASH 2978 LAS-RNO - PILOT REPORTED EMERGENCY DOOR, ROW 16 LEFT SIDE, SQUEAKS. MX RESECURED EXIT DR HANDLE SEAL TAPE/NO L EAKS NOTED. 2 L 7 2 4F RT A21EA 2008011500336 20080115 00336 WP 2008 1 15 ABXA080013 1 20071215 A 5320 991555048 INTERCOSTAL DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 47596 AFT LOWER CARGO FLOOR SUPPORT ATTACH BRACKET CRACKED AT FS 1056, RIGHT UNDER TRACK AT 28 RIGHT. REPLACED INTERCOSTAL AN D BRACKET AT STA 1056 RIGHT IAW DC9 SRM. 2 L 7 2 4F A6WE 2008011500343 20080115 00343 WP 2008 1 15 ABXA080011 1 20071213 A 5320 992343512 ATTACH ANGLE DOUG DC9 DC941 302207N WP RT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 47596 ATTACH ANGLE CRACKED AT APPROXIMATELY STA 775 OUTBOARD SIDE OF WHEEL WELL. APPROXIMATELY 18" AFT OF WHEEL WELL MAIN FRA ME. REPLACED ANGLE IAW DC9 SRM 51-30-5 AND DOUGLAS DWG 9923435 PART -12. 2 L 7 2 4F A6WE 2008011500345 20080115 00345 WP 2008 1 15 ABXA080014 1 20071211 A 5320 992348489 ATTACH FITTING DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 FLOORBEAM AND INTERCOSTAL ATTACH CLIP WERE BROKEN AND CRACKED AT FS 180, LEFT BUTT LINE 22. REPAIRED FLOORBEAM AND INTE RCOSTAL ATTACH CLIP IAW DC9 SRM 53-01, FIGURE 2, SHEET 3. 2 L 7 2 4F A6WE 2008011500346 20080115 00346 EA 2008 1 15 MASA200700927 1 20071229 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 924FJ 15024 ASH FLT 2827 PHX-TUS - CEILING LEVEL EMERGENCY FLOODLIGHT THAT WAS LOCATED 2ND FROM AFT IS INOP. RELAMPED, OPS GOOD. 2 L 7 2 4F RT A21EA 2008011500347 20080115 00347 WP 2008 1 15 ABXA080008 1 20071210 A 5730 59205211 PANEL DOUG DC9 DC933F 302207A WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 LEFT WING TRAILING EDGE ASSEMBLY NUMEROUS AREAS OF CORROSION AND DISBONDING AT INTERVAL FINGER DOUBLER AND LEADING EDGE DOUBLER. REMOVED AND REPLACED TRAILING EDGE ASSEMBLY IAW DC9 SRM. 2 L 7 2 4F A6WE 2008011500348 20080115 00348 WP 2008 1 15 ABXA080021 1 20071218 A 5534 99119817 ANGLE DOUG DC9 DC941 302207N WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 ANGLE CRACKED AT FASTENER - LEFT SIDE JUST FORWARD OF TIP FAIRING. REMOVED FORMER, FABRICATED NEW FORMER IAW DWG 991198 1. REINSTALLED FORMER IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 2008011600037 20080116 00037 EU 2008 1 16 NSVA20070064 1 20070314 A 2750 POTENTIOMETER SAAB SF340 340B 7860101 EU TE FLAPS MALFUNCTIONED A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 334CJ 334 FLAPS DO NOT EXTEND FULL 20 DEGREES WHEN SELECTED SETTING OFF GPWS WARNING. SLAVED IN FLAP CONTROL BOX IAW AMM 27-51-10 -04. NO JOY. RETURNED ORIGINAL BOX TO ORIGINAL CONFIGURATION. REMOVED AND REPLACED FLAP CONTROL VALVE IAW AMM 27-51-1 5. NO JOY. P/N ON-OFF HP1416100-5. S/N ON 1033 OFF 1370. BLED HYD SYSTEM IAW AMM 27-51-25-04. OPS CHECKS GOOD. AD JUSTED GAIN FOR FLAP CONTROL LEVER POTENTIOMETER IAW AMM 27-51-00-05. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 2008011600038 20080116 00038 EU 2008 1 16 NSVA20070089 1 20070408 A 2530 38512 RECEPTACLE SAAB SF340 340B 7860101 EU COFFEE MAKER SHORTED A NSVA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 233CJ 233 STRONG BURNING SMELL NEAR GALLEY. FA INFORMED CA OF BURNING SMELL 20 MIN PRIOR TO NORMAL IN GALLEY. CA INFORMED FA TO TURN OFF HOT JUGS. FA 5 MIN LATER SAID SMELL DECEASED CA AND FO DID NOT SMELL UNTIL AFTER LANDING , DURING TAXI. STRON G BANGLITE ODOR NOTED AFTER COCKPIT DOOR WAS OPENED. T/S TO LOOSE CONNECTION TO AFT HOT JUG 4-8-07. FOUND LIFT COFFEE JUG RECEPTACLE SHORTING OUT CAUSING BURNING SMELL IN CABIN REMOVE COFFEE JUG AND DEFERRED IAW MEL 25-60- 5-01 CAT C ID# 24885. REMOVED AND REPLACED AFT HOT JUG AIRFRAME SIDE RECEPTACLE AND INSTALLED REPAIRED HOT JUG PER SAAB CMM 25-31-54, OPS CHECK NORMAL, P/N 38-51-2 (RECEPTACLE) P/N DLH1009-003. 2 L 7 2 4T RT A52EU 2008011600039 20080116 00039 EU 2008 1 16 NSVA20070119 1 20070430 A 3150 WARNING LIGHT SAAB SF340 340B 7860101 EU ILLUMINATED A NSVA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 346CJ 346 PUSHER DISARM LIGHT ILLUMINATED. RESET PUSHER DISARM SWITCH. OPS CHECK GOOD OK FOR SERVICE. 2 L 7 2 4T RT A52EU 2008011600040 20080116 00040 NE 2008 1 16 NSVA20070184 2 20070715 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT UNKNOWN A NSVA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 343CJ 340B343 ITT ON RIGHT ENGINE WAS AT 93 DEGREES FOR 1 SECOND. ABORTED TAKEOFF. EVALUATED WITHIN LIMITS PER MNTC CONTROL REF GE S PECIAL PROCEDURES 72-00-00-023 B4. PERFORMED TAKEOFF POWER RUN AND ENGINE PERFORMED W/IN LIMITS. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011600041 20080116 00041 EU 2008 1 16 NSVA20070103 1 20070416 A 6123 PROPELLER SAAB SF340 340B 7860101 EU FEATHERING MALFUNCTIONED A NSVA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 210CJ 210 LEFT PROPELLER WILL NOT UNFEATHER. SERVICED PGB IAW SAAB 12-10-79. 2 L 7 2 4T RT A52EU 2008011600043 20080116 00043 EU 2008 1 16 NSVA20070077 1 20070328 A 2612 703072 FIRE LOOP SAAB SF340 340B 7860101 EU LT NACELLE NO TEST A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 237MJ 237 LEFT ENGINE FIRE DETECTION WILL NOT TEST. REMOVED AND REPLACED FWD ENGINE NACELLE FIRE SENSOR LOOP ON LT ENGINE IAW AMM 26-11-05, OP'S CHECK GOOD, P/N 703072. 2 L 7 2 4T RT A52EU 2008011600044 20080116 00044 EU 2008 1 16 NSVA20070102 1 20070415 A 3260 UPLOCK SWITCH SAAB SF340 340B 7860101 EU MLG DIRTY A NSVA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 334CJ 334 DURING TAKEOFF GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH. CLEANED OFF LT AND RT MLG UPLOCK SWITCHES AND PERFORMED TEST OF UPLOCK SWITCH REFERENCING 32-61-15-02 PARAGRAPH E. PERFORMED FUNCTIONAL TEST OF EXTENSION AND RETRACTION SYSTEM REF 32-30-00, OPS CHECKED GOOD. 2 L 7 2 4T RT A52EU 2008011600045 20080116 00045 CE 2008 1 16 NSVA20070091 1 20070406 A 5230 1294400497001 HINGE BEECH 1900 1900D 1154162 CE CARGO DOOR UNKNOWN A NSVA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 EA 27 172MJ UE72 CARGO DOOR OPENED IN FLIGHT. NO WARNING FROM CWP OR MASTER WARNING REMOVED COATING PANEL ABOVE CARGO DOOR. OPS CHECK O F WARNING SYSTEM GOOD IAW REPS 52-30-00. REINSTALLED COATING PANEL ABOVE CARGO DOOR IAW AMM 20-08-00, W/O 0300978, CARG O DOOR HINGES ARE DAMAGED. REMOVED CARGO DOOR HINGES IAW AMM 52-30-00. PERFORMED LIQUID PENETRANT INSPECTION OF CARGO DOOR TRAILING EDGE AND UNDER THE CARGO DOOR HINGE ATTACHMENT SKIN AREA IAW STRUCTURAL INSPECTION MANUAL STANDARD PRACTIC ES DOCUMENT DQG069565/JMP/ 0628-07. NO FAULT FOUND. REPLACED HINGE IAW SRM 51-90-01, CARGO DOOR HANDLE HAS EXCESSIVE PLAY REMOVED CARGO DOOR HANDLE IAW MM 52-30-00. REMOVED AND REPLACED CARGO DOOR HANDLE IAW REPS 52-30-00. OPS CHECK GO 2 L 7 2 4T RT A24CE 2008011600047 20080116 00047 CE 2008 1 16 NSVA20070180 1 20070710 A 3260 1003810061 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A NSVA O OTHER N FALSE WARNING DE DESCENT 1 EA 27 155CJ UE55 GEAR IN TRANSIT LIGHT ANNUNCIATOR ILLUMINATED NORMALLY DURING POWER REDUCTION, HOWEVER IT WOULD NOT EXTINGUISH AFTER ADV ANCING POWER AND REMAINED ILLUMINATED UNTIL GEAR WAS EXTENDED FOR LANDING. REMOVED AND REPLACED NOSE GEAR UP LOCK SWITC H, PERFORMED GEAR EXTENSION AND RETRACTION, OPS CHECK SATISFACTORY IAW BEECH 1900 MM 32-60-00 AND 32-30-00 P/N 100-38100 6-1. 2 L 7 2 4T RT A24CE 2008011600049 20080116 00049 EU 2008 1 16 NSVA20070167 1 20070627 A 7797 CONNECTOR SAAB SF340 340B 7860101 EU DECU DIRTY A NSVA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 338CJ 340B338 LT TORQUE SPIKE ON TAKEOFF ROLL TO 101 PERCENT AT 40 KNOTS. CLEANED CONNECTION ON LT DECU, GROUND RAN AIRCRAFT, OPS CHE CK GOOD. 2 L 7 2 4T RT A52EU 2008011600050 20080116 00050 CE 2008 1 16 NSVA20070145 1 20070530 A 2620 WARNING LIGHT BEECH 1900 1900D 1154162 CE UNKNOWN A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 221CJ UE221 NO PUSH TO EXTINGUISH LIGHT DURING AMP TEST ON RIGHT SIDE. REMOVED AND REPLACED RIGHT ENG. FIRE BOTTLE AND SQUIB ASSY. REMOVED AND REPLACED RIGHT FIRE "T" HANDLE ASSY. OPS CHECK GOOD IAW COLGAN WORK CARD NR 26-20-05 AND MM CH 26-00-00. 2 L 7 2 4T RT A24CE 2008011600051 20080116 00051 EU 2008 1 16 NSVA20070094 1 20070411 A 3350 CIRCUIT BREAKER SAAB SF340 340B 7860101 EU TRIPPED A NSVA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 27 343CJ 343 EMERGENCY POWER LIGHT ILLUMINATED. FOUND C/B POPPED, RESET AND OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011600052 20080116 00052 CE 2008 1 16 NSVA20070106 1 20070418 A 3233 11238002223 ACTUATOR BEECH 1900 1900D 1154162 CE NLG CRACKED A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 243CJ UE43 DURING ROUTINE INSPECTION, HYDRAULIC FLUID WAS FOUND TO BE LEAKING FROM NLG ACTUATOR. FURTHER INVESTIGATION REVEALED TH AT THE NLG ACTUATOR END CAP HOUSING ASSEMBLY HAD A CRACK. REMOVED AND REPLACED NLG ACTUATOR IAW 32-21-00 PN ON/OFF 112- 380022-23, SN ON 69, SN OFF 298. PERFORMED GEAR RETRACTION AND EXTENSION IAW 32-30-00. LEAK AND OPS CHECKED GOOD. 2 L 7 2 4T RT A24CE 2008011500004 20080115 00004 EU 2008 1 15 NSVA20070193 1 20070722 A 3244 TIRE SAAB SF340 340B 7860101 EU NLG DAMAGED A NSVA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 194CJ 340B194 LEFT NOSE GEAR TIRE MISSING CHUNK OF THREAD 4" BY 10, ABORTED TAKEOFF. REMOVED AND REPLACED NOSE TIRES PN OFF L AND R 5 006227 SN (L) OCT01-03561 OCT01-0284 (R) FEB94-1617/JUL97-0103 PN ON (L+R) 5006227 SN (L) NOV98-2479 (R) MAY04-3130 DONE IAW 32-41-1S. 2 L 7 2 4T RT A52EU 2008011500006 20080115 00006 EU 2008 1 15 NSVA20070101 1 20070417 A 3020 SM15CXD4 RELAY SAAB SF340 SF340A 7850100 EU ENGINE INTAKE MALFUNCTIONED A NSVA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 121CQ 121 AFTER T/O NOTICED INTENSE BURNING INSULATION SMOKE ODOR IN COCKPIT AND FRONT PORTION OF CABIN, AND RT INTAKE LIGHT ILLUM INATED. REMOVED AND REPLACED ENG INTAKE POWER RELAY 36HE IAW AMM 30-20-10-04. REPLACED TERMINAL IAW WM 20-20-10, P/N S M15CXD4 (NSN) MS 35036/148 INTAKE HEAT OPS CHECK GOOD IAW AMM 30-20-00. 2 L 7 2 4T RT A52EU 2008011500008 20080115 00008 NE 2008 1 15 NSVA20070187 2 20070716 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE POWER LOSS A NSVA D RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 184CJ 184 BOTTOM GOVERNOR ENGAGES NORMALLY DRIVING TAXI BT A/C RAN DROPS OFFLINE PROP RPM FLUCTUATES, BOTTOM GOVERNOR IS UNABLE TO MAINT PROP RPM, PROP RPM DECAYS TO 750 RPM. RETURN TO GATE. OPS CK RT ENGINE RPM AS PER SAAB MM 76-10-00. NO DEFECT WERE NOTED AT THIS TIME, A/C RETURNS TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011500034 20080115 00034 SO 2008 1 15 C2XA08RI005 1 20071228 A 3260 852701 PROXIMITY SWITCH EMB 135 EMB135ER 3260203 SO LANDING GEAR MALFUNCTIONED A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 19503 145176 FLT 2665 - EWR - CREW REPORTED LANDING GEAR AIR/GROUND FAIL INDICATION ON EICAS IN CRUISE. CREW LANDED ACFT UNEVENTFULLY . EWR MX REMOVED AND REPLACED NOSE WEIGHT ON WHEEL PROXIMITY SWITCH IAW EMB135 AMM 32-63-02 AND PERFORMED OPERATIONAL C HECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008011500042 20080115 00042 EU 2008 1 15 NSVA20070107 1 20070419 A 7697 WIRE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CONNECTOR BROKEN A NSVA O OTHER N FALSE WARNING CL CLIMB 1 EA 27 210CJ 210 FLIGHT IDLE STOP OPEN ANNUNCIATOR ILLUMINATED UPON GEAR UP AT TAKEOFF. INSPECTED AND CLEAN SQUAT SW'S AND CONNECTOR FOR OBVIOUS DEFECTS. FOUND BROKEN WIRE AT CONNECTOR 66-A REQUIRED WORK IAW AC 43:13-IB PAGE 11-65, SECT 13 OPS CK GOOD 36- 10-20. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011500045 20080115 00045 EU 2008 1 15 NSVA20070081 1 20070331 A 7710 6071T20P17 CONTROL UNIT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE ERRATIC A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 343CJ 343 RT ENGINE ERRATIC DURING RUN-UP ITT SURGE (+200 DEGREES) AND PROP, RPM SURGE (UP TO 1250 RPM) OBSERVED. REMOVED AND REP LACED DECU IAW 76-10-57, OPS CHECK GOOD, PN ON/OFF 6071T20P17, SN ON ECDT1074, SN OFF ECDT1392. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011500047 20080115 00047 CE 2008 1 15 NSVA20070158 1 20070612 A 3260 RELAY BEECH 1900 1900D 1154162 CE MLG INTERMITTENT A NSVA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 155CJ UE55 GEAR UNSAFE LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION. REMOVED AND REPLACED PCB A406 DUE TO RELAY K3 INTERMITTE NT IAW WD7 91-34-01. OPS CHECK GOOD IAW AMM 32-60-00, PN OFF 112-364021-1, SN ON 11, SN OFF 582892. 2 L 7 2 4T RT A24CE 2008011500052 20080115 00052 EU 2008 1 15 NSVA20070179 1 20070709 A 6123 COMPUTER SAAB SF340 340B 7860101 EU AUTOCOARSEN SYS FAULTED A NSVA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 194CJ 238 194 ON APPROACH AUTOCOARSEN LOW LIGHT WOULD NOT ILLUMINATE LANDING. REMOVED AND REPLACED AUTOCOARSEN SWITCH IAW AMM 61-22-1 5-02 PN ON AND OFF 8581 SN OFF 238 SN ON 251. OPS CHECK OK IAW AMM 61-22-00. 2 L 7 2 4T RT A52EU 2008011500082 20080115 00082 NM 2008 1 15 USAA920080071 1 20071130 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 663, S3L. REPAIRED FRAME, BS 663, S3L IAW USAIRWAYS EA 100069. 2 L 7 2 4F RT A16WE 2008011500090 20080115 00090 EU 2008 1 15 NSVA20070166 1 20070620 A 7797 WIRE HARNESS SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE DECU DAMAGED A NSVA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 350CJ 340B350 TORQUE ITT NG FUEL FLOW NP FUNCTIONS ON CLIMB-OUT AND CRUISE TORQ FLUCT BETWEEN 4-5 PERCENT, ITT 5C, NG 290, FUEL FLOW 2 0 PPH, NP, 100 RPM. CLEANED ELECTRICAL CONNECTOR ON LT TORQUE SENSOR AND BLUE WIRE HARNESS CONNECTOR ON DECU. OPS CHEC K GOOD. NO FLUCTUATIONS NOTED DURING ENGINE RUN. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011500091 20080115 00091 NM 2008 1 15 USAA920080078 1 20071212 A 5240 6545871523 DOOR FRAME BOEING 737 7373G7 1384595 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - FORWARD SERVICE DOOR FRAME CRACKED AT THE 2ND FROM TOP STOP FITTING CUTOUT. REPAIRED T HE FORWARD SERVICE DOOR FRAME AT THE 2ND FROM TOP STOP FITTING CUTOUT IAW B737 SRM 51-70-11. 2 L 7 2 4F RT A16WE 2008011500092 20080115 00092 NM 2008 1 15 USAA920080079 1 20071221 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 807, S9L. REPAIRED FRAME, BS 807, S9L IAW USAIRWAYS TYPICAL REPAIR 5 3-10-25. 2 L 7 2 4F RT A16WE 2008011500093 20080115 00093 EU 2008 1 15 NSVA20070093 1 20070411 A 2434 23080031 GENERATOR SAAB SF340 340B 7860101 EU NR 2 DC MALFUNCTIONED A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 184CJ 184 NO AUTOCOARSEN GREEN STATUS LIGHTS. REMOVED AND REPLACED NR 2 DC GENERATOR IAW COLGAN W/C 2431-045. OPS CHECK AUTO COA RSEN IAW MM 61-22-00. MEL CLEARED. PN ON/OFF 23080-031 SN ON 98275, SN OFF 5353. 2 L 7 2 4T RT A52EU 2008011500097 20080115 00097 EU 2008 1 15 NSVA20070189 1 20070718 A 3150 WARNING LIGHT SAAB SF340 340B 7860101 EU HYD SYSTEM FALSE ACTIVATION A NSVA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 EA 27 346CJ 346 HYDRAULIC QUANTITY AT RED LINE, EMERGENCY DECLARED. SERVICED HYD SYS TO FULL, NO VISIBLE LEAKS NOTED. CYCLED PARKING B RAKE, NORMAL BRAKES AND FLAPS SEVERAL TIMES, NO LEAKS NOTED, NO CHANGE IN HYD QUANTITY NOTED. 2 L 7 2 4T RT A52EU 2008011500112 20080115 00112 EU 2008 1 15 NSVA20070225 1 20070910 A 5101 UNKNOWN SAAB SF340 340B 7860101 EU UNKNOWN A NSVA O OTHER O OTHER CR CRUISE 1 EA 27 191MJ 191 FLIGHT ATTENDANT REPORTING HISSING SOUND COMING FROM AROUND EMERGENCY EXIT ROW 7 PRESSURIZATION NORMAL. OPS CHECK PRESS URIZATION IAW AMM 21-32-00-05. COULD NOT LOCATE A HISSING SOUND AROUND EMERGENCY EXIT DOORS, NO FAULTS FOUND. 2 L 7 2 4T RT A52EU 2008011500123 20080115 00123 NM 2008 1 15 USAA920080092 1 20071129 A 5320 6948085 ATTACH FITTING BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED INTERCOSTAL ATTACH CLIP, BS 360, S9L. REPLACED INTERCOSTAL ATTACH CLIP, BS 360 , S9L IAW BOEING DRAWING 69-48085. 2 L 7 2 4F RT A16WE 2008011500125 20080115 00125 CE 2008 1 15 NSVA20070233 1 20070924 A 3230 LANDING GEAR BEECH 1900 1900D 1154162 CE MALFUNCTIONED A NSVA O OTHER O OTHER AP APPROACH 1 EA 27 152MJ UE52 LANDING GEAR FAILED TO EXTEND NORMALLY. GEAR HANDLE PLACED IN DOWN POSITION, GEAR DID NOT EXTEND. RED LOLLIPOP LIGHTS DID NOT ILLUMINATE, RECYCLED GEAR HANDLE AND GEAR EXTENDED NORMALLY. PERFORMED EXTENSION AND RETRACTION OF THE LANDING GEAR SYSTEM IAW BEECH MM 32-30-00. OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 2008011500126 20080115 00126 NM 2008 1 15 USAA920080094 1 20071221 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 480, S8L. REPAIRED FRAME, BS 480, S8L IAW USAIRWAYS TYPICAL REPAIR 5 3-10-25. 2 L 7 2 4F RT A16WE 2008011500140 20080115 00140 NM 2008 1 15 USAA920080103 1 20071202 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED STRINGER CLIP, BS 294.5, S11L. REPLACED STRINGER CLIP, BS 294.5, S11L IAW B737 SRM 51-20-00. 2 L 7 2 4F RT A16WE 2008011500141 20080115 00141 CE 2008 1 15 NSVA20070232 1 20070924 A 6123 SWITCH BEECH 1900 1900D 1154162 CE POWER LEVER LOOSE A NSVA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 152MJ UE52 DURING TAKEOFF ROLL AUTO FEATHER INITIALLY ARMED WITH SETTING OF TAKEOFF POWER. AT 55 KIAS AUTOFEATHER DISABLE LIGHT IL LUMINATED AND TAKEOFF WAS ABORTED. FOUND LT POWER LEVER AFX SWITCH LOOSE. TIGHTENED SWITCH AND OP CHECKED IAW AMM 61-2 1-00, OPS CHK GOOD. 2 L 7 2 4T RT A24CE 2008011500144 20080115 00144 EU 2008 1 15 NSVA20070219 1 20070827 A 2121 COOLING FAN SAAB SF340 340B 7860101 EU E/E BAY FAILED A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 202SR 340B202 AVIONICS VENT FAN LIGHT ILLUMINATED AND CB G-11 POPPED ACCOMPANIED BY HOT ELECTRICAL ODOR. AVIONICS VENT FAN MEL'D, WIL L BE REPLACED AT NEXT MAINTENANCE BASE VISIT. 2 L 7 2 4T RT A52EU 2008011500148 20080115 00148 NM 2008 1 15 USAA920080108 1 20071216 A 5340 69730563 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED STRINGER CLIP, BS 706, S6R. REPLACED STRINGER CLIP, BS 706, S6R IAW B737 SRM 5 1-10-02. 2 L 7 2 4F RT A16WE 2008011500158 20080115 00158 NM 2008 1 15 USAA920080123 1 20071224 A 5313 STRINGER SPLICE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CLT - MAJOR REPAIR - C18 CHECK - CRACKED STRINGER SPLICE BS 361, S4R. REPAIRED STRINGER SPLICE, BS 361, S4R IAW B737 SR M 51-10-02. 2 L 7 2 4F RT A16WE 2008011500166 20080115 00166 EU 2008 1 15 NSVA20070206 1 20070808 A 2612 89905202 CONTROL UNIT SAAB SF340 340B 7860101 EU FIRE DETECTION MALFUNCTIONED A NSVA O OTHER N FALSE WARNING CR CRUISE 1 EA 27 194CJ 194 LEFT ENGINE FIRE WARNING ILLUMINATED DURING FLIGHT FOR APPROX 3 SECS THEN TURNED OFF. ALL PARAMETERS REMAINED NORMAL, N O FIRE NOTED. REMOVED AND REPLACED FIRE DETECTING CONTROL UNIT IAW AMM 26-11-10-02 PN OFF/ON 899052-02 SN OFF 0788 SN O N 0485, OPS CHECK OK. 2 L 7 2 4T RT A52EU 2008011500168 20080115 00168 EU 2008 1 15 NSVA20070220 1 20070903 A 2910 UNKNOWN SAAB SF340 340B 7860101 EU HYD SYSTEM UNKNOWN A NSVA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 249CJ 340B249 HYD LIGHTS ON IN FLIGHT. MAIN AND EMERGENCY ACCUM LOW, EMERGENCY LANDING DECLARED. INSPECTED FOR EXTERNAL LEAKS. NONE NOTED. FOUND MAIN SYSTEM OVERSERVICED, AND AUX SYSTEM REQUIRED SERVICING. RESERVICED, PERFORMED HYD SYSTEM CHECK, NO FAULTS FOUND. 2 L 7 2 4T RT A52EU 2008011500180 20080115 00180 EU 2008 1 15 NSVA20070223 1 20070904 A 3397 WIRE SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS BROKEN A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 204CJ 340B204 LT EXTERIOR EMERGENCY LIGHT INOP. FOUND BROKEN WIRE ON LIGHT ASSY. REPAIRED, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011500193 20080115 00193 EA 2008 1 15 VNAA0712005 1 20071225 A 2611 4462534 SMOKE DETECTOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE FWD LAVATORY MALFUNCTIONED A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 05 705PS 9155 10144 CREW REPORTED SHORTLY AFTER TAKEOFF THE FORWARD LAVATORY SMOKE DETECTOR HAD INTERMITTENT INDICATION. THERE WAS NO VISIB LE SMOKE OR ODOR DETECTED. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED THE FORWARD SMOKE DETECTOR PER MEL 26-16-01. MAINTENANCE REMOVED AND REPLACED THE SMOKE DETECTOR IN ACCORDANCE WITH THE AIRCRAFT M AINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008011500216 20080115 00216 EA 2008 1 15 MASA200700869 1 20071211 A 3010 CONTROLLER CNDAIR CL600 CL6002C10 1390015 EA MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 522LR 10262 ASH 7236 ORD-MCI - PILOT REPORTED RECEIVING BOTH WING OVHT WARNING MSG. PILOT DECLARED EMERGENCY. CONTRACT MX RESET AN TI ICE CONTROLLER. 2 L 7 2 4F RT A21EA 2008011500222 20080115 00222 EA 2008 1 15 MASA200700514 1 20070821 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA CABIN ODOR A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 503MJ 10058 ASH 7441 CLT-IAD - FUEL ODOR IN CABIN ROWS 10 AND 12. MX RAN ENGINES AND COULD NOT DUPLICATE. 2 L 7 2 4F RT A21EA 2008011500232 20080115 00232 EA 2008 1 15 MASA200700521 1 20070825 A 3230 533407 SELECTOR VALVE CNDAIR CL600 CL6002C10 1390015 EA MLG MALFUNCTIONED A MASA O OTHER J WARNING INDICATION LD LANDING 1 SW 07 505MJ 10949 10070 ASH 7254 ORD - THE LANDING GEAR WOULD NOT EXTEND DURING LANDING. MX REMOVED AND REPLACED L/G SELECTOR VALVE/OPS CK GOOD . 2 L 7 2 4F RT A21EA 2008011500234 20080115 00234 EA 2008 1 15 MASA200700566 1 20070910 A 3350 BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 507MJ 10077 ASH FLT 7407 CLT-ORD - PILOT REPORTED THAT THE EMERGENCY LIGHTS DID NOT COME ON WHEN TESTED AND PERHAPS THE BATTERIES WE RE DEAD. MX RECHARGED BATTERY PACKS, OPS CK GOOD. 2 L 7 2 4F RT A21EA 2008011500242 20080115 00242 EA 2008 1 15 MASA200700641 1 20070925 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 507MJ 10077 ASH FLT 7323 IN IAD, CAPTAIN REPORTED OVERHEAD EMERG LIGHT AT ROW 16 INOP, RELAMPED. 2 L 7 2 4F RT A21EA 2008012400247 20080124 00247 SO 2008 1 24 FDKA200709458 1 20070909 A 5210 12050901001 HANDLE EMB 145 EMB145LR 3260212 SO PAX DOOR DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM FLT RON MCO - PAX DOOR HANDLE GRIP MISSING. MX INSTALLED GRIP HANDLE. 2 L 7 2 4T RT T00011AT 2008011500257 20080115 00257 EA 2008 1 15 FDKA200700504 1 20070815 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 651ML 7139 ASH 7479 IAD - MID CABIN EMERGENCY CALL LIGHT INOP. MX REINSTALLED THE LAMP AND REPLACED THE LENS. 2 L 7 2 4F RT A21EA 2008011500261 20080115 00261 EA 2008 1 15 MASA200700835 1 20071202 A 5210 LATCH CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR STIFF A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 916FJ 15016 ASH 2824 PHX-TUS - PAX DOOR DIFFICULT TO UNLATCH. MX CYCLED DOOR AND DOOR LATCH SEVERAL TIMES. FOUND NO DEFECTS IN THE PROCESS. 2 L 7 2 4F RT A21EA 2008011500269 20080115 00269 NM 2008 1 15 MASA200700774 1 20071105 A 2913 570347 PUMP DHAV DHC8 DHC8202 2809007 NM HYDRAULIC SYS FAILED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 454YV 12074 454 ASH FLT 7193 ASE - DEN - THE CREW DECLARED AN EMERGENCY INTO DEN DUE TO LOSS OF THE NR 1 HYDRAULIC SYSTEM. MX REMOVED AND REPLACED NR 1 EDP. 2 H 7 2 4T RT A13NM 2008011500272 20080115 00272 EA 2008 1 15 MASA200700309 1 20070607 A 5210 DOOR CNDAIR CL600 CL6002D24 1390016 EA MAIN PAX LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 903FJ 15003 ASH 2887 BUR, MAIN PAX DOOR WOULD NOT CLOSE. MAINTENANCE LUBE THE DOOR. 2 L 7 2 4F RT A21EA 2008011500277 20080115 00277 EA 2008 1 15 MASA200700355 1 20070624 A 3020 ANTI-ICE SYSTEM CNDAIR CL600 CL6002C10 1390015 EA INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 521LR 10261 ASH 7195 PIT - CAPTAIN DECLARED AN EMERGENCY, DUE TO ANTI-ICE SYSTEM DID NOT WORK (ANY OF IT). MX INTERROGATED MDC CURR ENT FAULTS AND FAULT HISTORY, NO FAULTS WERE FOUND. 2 L 7 2 4F RT A21EA 2008011500278 20080115 00278 EA 2008 1 15 MASA200700546 1 20070902 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 928LR 15028 CEILING EMERGENCY FLOOD LIGHT ROW 7 INOP. MX RE-LAMPED. 2 L 7 2 4F RT A21EA 2008011500287 20080115 00287 WP 2008 1 15 UPS08851376 1 20071227 A 5511 SPAR DOUG DC8 DC871F 302199D WP LT HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 LT HORIZ STAB REAR SPAR WEB CRACKED 2EA PLACES AT INBOARD LIGHTNING HOLE. REMOVED, FABRICATED, AND I NSTALLED REPAIR WEB ON LT HORIZ STAB REAR SPAR AT INBOARD LIGHTNING HOLE IAE DWG 5652086, AND SRM 51-03-00. 2 L 7 4 4F RT 4A25 2008011500293 20080115 00293 NM 2008 1 15 ABXA080001 1 20071218 A 3297 WIRE BOEING 767 767281 1385109 NM LT MLG WW SHORTED A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 790AX 23140 AT ILN, MAIN LANDING GEAR WHEEL WELL LIGHTS WERE INOPERATIVE. CIRCUIT BREAKER TRIPPED AND WOULD NOT RESET. FOUND WIRE BUNDLE FROM LEFT WHEEL WELL BURNT AND SHORTED UNDER FLOOR PANEL IN UPPER CARGO AREA. REPAIRED WIRE BUNDLE W0628 IN WORK PACK 2007790 PER BOEING STANDARD WIRING PRACTICES MANUAL. MAIN LANDING GEAR WHEEL WELL LIGHTS CHECKED GOOD ON GROUND I AW B767 AMM 33-31-00. 2 L 7 2 4F RT A1NM 2008011500301 20080115 00301 EA 2008 1 15 MASA200700612 1 20070919 A 5210 2R5206B ACTUATOR CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 938LR 6177 15038 ASH FLT 2824 MRY TO PHX - PASSENGER DOOR DIFFICULT TO OPEN. CONTRACT MX FOUND PASSENGER DOOR ASSIST PULLEY OBSTRUCTING DOOR. REMOVED AND REPLACED ASSIST MOTOR. 2 L 7 2 4F RT A21EA 2008011500319 20080115 00319 NM 2008 1 15 MASA200700761 1 20071031 A 6123 30005000056 TSCU DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER MALFUNCTIONED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 988HA 8796 426 ASH FLT 2839 PHX-FLG - AUTO-FEATHER SYSTEM WON'T DISARM IN FLIGHT. REMOVED AND REPLACED NR 1 TSCU AND RELAY K-5. 2 H 7 2 4T RT A13NM 2008011500332 20080115 00332 WP 2008 1 15 ABXA080006 1 20071207 A 5310 59101575 FASTENER DOUG DC9 DC933F 302207A WP FUSELAGE POPPED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 POPPED FASTENER AT LOWER STOP FITTING - DOOR CUTOUT. REPAIRED AREA IAW DC9 SRM 53-05, FIGURE 44. 2 L 7 2 4F A6WE 2008011500333 20080115 00333 WP 2008 1 15 ABXA080007 1 20071209 A 2780 39239322 ATTACH BRACKET DOUG DC9 DC933F 302207A WP L/E SLAT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 RIGHT WING SLAT CABLE, MOST INBOARD PULLEY, UPPER OUTBOARD ATTACH BRACKET CRACKED AT APPROXIMATELY STA 83.534. REMOVED AND REPLACED BRACKET IAW DC9 SRM. 2 L 7 2 4F A6WE 2008011500338 20080115 00338 WP 2008 1 15 ABXA080018 1 20071213 A 5347 S291493M24000 SEAT TRACK DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 SEAT TRACK AT STA 427 CORRODED BETWEEN LONGERON 28 LEFT AND LONGERON 27 LEFT. REMOVED AND REPLACED SECTION OF TRACK AT STA 427, LONGERON 28 LEFT IAW DOUGLAS DWG 5922344, AND DC9 SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 2008011500342 20080115 00342 WP 2008 1 15 ABXA080010 1 20071221 A 3232 9915511501 FITTING DOUG DC9 DC933F 302207A WP LT WHEEL WELL CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 LEFT INBOARD DOOR ACTUATOR ATTACH FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC9 SRM. 2 L 7 2 4F A6WE 2008011600046 20080116 00046 CE 2008 1 16 NSVA20070159 1 20070615 A 3234 CIRCUIT BOARD BEECH 1900 1900D 1154162 CE MLG HANDLE MALFUNCTIONED A NSVA O OTHER O OTHER CL CLIMB 1 EA 27 155CJ UE55 GEAR HANDLE UNSAFE LIGHT REMAINED ILLUMINATED AFTER RETRACTION. REMOVED AND REPLACED PCB LOGIC RELAY BOARD IAW 32-30-00 . PN OFF/ON 112-364021-1, SN OFF 11, SN ON 775-8-85. OPS CHECK GOOD. ALSO, REMOVED AND REPLACED LANDING GEAR CONTROL H ANDLE IAW 32-10-00 PN 101-384137-7, SN OFF 663, SN ON 3231A. OPS CHECK GOOD IAW AMM 32-30-00. 2 L 7 2 4T RT A24CE 2008011600086 20080116 00086 NE 2008 1 16 NSVA20070080 2 20070331 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT FAILED A NSVA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 EA 27 249CJ 249 785323 ABORTED TAKEOFF AT APPROXIMATELY 45KTS DUE TO A LOUD BANG, AND AN OVERTEMP CONDITION OF APPROXIMATELY 1450 CELSIUS ON RT ENGINE. CAPTAIN NOTICED EXCESSIVE YAW TO THE LEFT AND SMOKE COMING FROM RT ENGINE INTAKE. AFTER RETURNING TO GATE, FO UND METAL SHAVINGS IN RT ENGINE TAIL PIPE. REMOVED AND REPLACED RT ENGINE SN 785323 IAW 72-00-00. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011600100 20080116 00100 EU 2008 1 16 NSVA20070211 1 20070814 A 2612 FIRE DETECTOR SAAB SF340 340B 7860101 EU RT NACELLE NO TEST A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 339CJ 339 R FIRE DETECT FAIL LIGHT DOES NOT ILLUMINATE ON FIRE START TEST. PERFORMED RESISTANCE CHECKS OF FIRELOOP SYSTEM VERIFIE D SECURITY OF FIRELOOP CONNECTORS WEU FIRELOOP, OPS CHECK GOOD IAW SAAB AMM CH 26-11-00. 2 L 7 2 4T RT A52EU 2008011600101 20080116 00101 CE 2008 1 16 NSVA20070214 1 20070814 A 2730 101524887611 ACTUATOR BEECH 1900 1900D 1154162 CE ELEVATOR TRIM MALFUNCTIONED A NSVA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 27 60MJ UE60 AIRCRAFT IS PITCHING UP AND DOWN UNCOMMANDED. REQUIRES EXCESSIVE FORCE ON CONTROL WHEEL TO MAINTAIN DESIRED PITCH, EVEN WITH ELECTRIC TRIM DISCONNECTED. REMOVED AND REPLACED ELECTRIC ELEVATOR TRIM TAB ACTUATOR IAW REPS AIRLINER 1900D M/M 27-30-07-201. PERFORMED ELEVATOR ELECTRIC TRIM TAB CABLE RIGGING IAW 27-30-07-201 PAGE 10. PERFORMED ELEVATOR ELECTRIC TRIM OPERATION CHECK PROCEDURE 27-30-09. ALL CHECKS GOOD. 2 L 7 2 4T RT A24CE 2008011600118 20080116 00118 EA 2008 1 16 MASA200700904 1 20071219 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 925FJ 15025 ASH FLT 2937 PHX - 3RD CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 2008011600119 20080116 00119 NM 2008 1 16 MASA200700905 1 20071219 A 3350 SIGN DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 987HA 425 ASH FLT 2907 PHX-GJT - PILOT REPORTED NO LIGHTED EXIT SIGNS IN CABIN. MX COULD NOT DUPLICATE, FUNCTIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2008011600120 20080116 00120 EA 2008 1 16 MASA200700659 1 20071002 A 5270 WARNING LIGHT CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT ILLUMINATED A MASA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 07 932LR 15032 ASH FLT 2864 PHX-MFR - RT FORWARD EMERGENCY EXIT DOOR CAUTION MESSAGE ON TAKE OFF. MX DEFERRED. 2 L 7 2 4F RT A21EA 2008011600121 20080116 00121 EA 2008 1 16 MASA200700859 1 20071205 A 3397 472698 CIRCUIT CARD CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS FAILED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 919FJ 15019 ASH FLT 2692 CLT - EMERGENCY LIGHTS COME ON AND OFF WHEN ARMED. REMOVED AND REPLACED CIRCUIT CARD 5 IN JB11. 2 L 7 2 4F RT A21EA 2008011600122 20080116 00122 EA 2008 1 16 MASA200700871 1 20071213 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 956LR 15056 ASH FLT 2656 CLT-GSO - PASSENGER DOOR WARNING WILL NOT EXTINGUISH WHEN DOOR IS CLOSED. MX OPENED AND CLOSED DOOR, OPS C HECK GOOD. 2 L 7 2 4F RT A21EA 2008011600123 20080116 00123 EA 2008 1 16 MASA200700622 1 20070923 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 927LR 7744 15027 EMERGENCY LIGHTS WILL NOT TURN ON. REMOVED AND REPLACED BATTERIES (5). 2 L 7 2 4F RT A21EA 2008011600124 20080116 00124 NM 2008 1 16 MASA200700880 1 20071207 A 5414 85410627 SKIN DHAV DHC8 DHC8202 2809007 NM NR 2 NACELLE TORN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 987HA 425 FOUND DAMAGE TO THE NR 2 ENGINE NACELLE. DAMAGE IS A TEAR IN THE LOWER SKIN PANEL AND EXCEEDS THE LIMITS. MX PERFORMED REPAIR. 2 H 7 2 4T RT A13NM 2008011600127 20080116 00127 EA 2008 1 16 MASA200700489 1 20070807 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37342 7342 ASH 7342 IAD - EMERGENCY EXIT OVERWING DOOR SIGN WILL NOT ILLUMINATE. MX RELAMPED, OPS NORMAL. 2 L 7 2 4F RT A21EA 2008011600130 20080116 00130 EA 2008 1 16 MASA200700525 1 20070828 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 650ML 7137 ASH 7288 DTW - PILOT REPORTED ALL THE EMERGENCY LIGHTS INOP. MX CHARGED THE BATTERY PACKS. 2 L 7 2 4F RT A21EA 2008011600131 20080116 00131 EA 2008 1 16 MASA200700511 1 20070819 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 651ML 7139 ASH RON DSM - DURING THE SERVICE CHECK, MX FOUND THE EMERGENCY FLOOR PATH LIGHTS FROM ROW 6-8 INOP AND THE RT OVERWING E XIT SIGN INOP. MX RESECURED CONNECTION. 2 L 7 2 4F RT A21EA 2008011600134 20080116 00134 NM 2008 1 16 MASA200700825 1 20071128 A 3350 SIGN DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHTS LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 449YV 449 ASH FLT 2950 PHX, EXIT SIGN AT PAX DOOR LOOSE. SECURED SIGN ASSEMBLY. 2 H 7 2 4T RT A13NM 2008011600135 20080116 00135 EA 2008 1 16 MASA200700506 1 20070816 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 909FJ 15009 ASH 2710 PHX-SNA, CEILING EMERGENCY EXIT LIGHT AT ROW 17 INOP. MX RELAMPED THE EMERGENCY EXIT LIGHT ASSY, OPS CK GOOD. 2 L 7 2 4F RT A21EA 2008011600138 20080116 00138 EA 2008 1 16 MASA200700406 1 20070710 A 2121 GG670950227 FAN CNDAIR CL600 CL6002D24 1390016 EA ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 907FJ 8705 15007 ASH 2675 CLT - EXPERIENCED A ELECTRICAL ODOR FROM THE RECIRC FAN. MX REMOVED AND REPLACED NR 1 FAN AND FILTER. 2 L 7 2 4F RT A21EA 2008011600139 20080116 00139 EA 2008 1 16 MASA200700311 1 20070608 A 5210 LATCH CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR OBSTRUCTED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 903FJ 15003 ASH 2887 BUR - UNABLE TO LATCH MAIN PAX DOOR. MX PUSHED ACFT PACK APPROX 2 FEET AND WAS ABLE TO CLOSE AND LATCH DOOR. 2 L 7 2 4F RT A21EA 2008011600140 20080116 00140 NM 2008 1 16 MASA200700812 1 20071120 A 5210 BOLT DHAV DHC8 DHC8202 2809007 NM PAX DOOR LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 449YV 449 ASH FLT 2960 - PHX - GRINDING NOISE IN THE PAX DOOR WHEN TRYING TO CLOSE IT. RESECURED UPPER OUTER ATTACH BOLT, OPS CHE CK GOOD. 2 H 7 2 4T RT A13NM 2008011600142 20080116 00142 EA 2008 1 16 MASA200700680 1 20071010 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 922FJ 15022 ASH FLT 2608 CLT TO SAV - OVERHEAD EMERGENCY FLOOD LIGHT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2008011600143 20080116 00143 EA 2008 1 16 MASA200700452 1 20070724 A 2150 GG670950095 ACM CNDAIR CL600 CL6002D24 1390016 EA NR 2 SMOKE A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 917FJ 9367 15017 ASH 2647 CLT-MEM - PILOT REPORTED ENVIRONMENTAL SMOKE IN COCKPIT AND CABIN AFTER NR 1 ENGINE SHUTDOWN ON GROUND. MX REM OVED AND REPLACED NR 2 ACM. 2 L 7 2 4F RT A21EA 2008011600147 20080116 00147 NM 2008 1 16 MASA200700910 1 20071221 A 2913 570347 PUMP DHAV DHC8 DHC8202 2809007 NM NR 2 HYD SYSTEM CAVITATES A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 991HA 1843 431 ASH FLT 2953 PHX - LOSS OF NR 2 HYDRUALIC SYSTEM WENT TO ZERO. REMOVED AND REPLACED LINE AND PUMP. 2 H 7 2 4T RT A13NM 2008011600150 20080116 00150 EA 2008 1 16 MASA200700628 1 20070924 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27318 7318 ASH FLT 2751, PHX - CREW REPORTED THAT THE FWD CEILING EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 2008011600161 20080116 00161 EA 2008 1 16 MASA200700787 1 20071109 A 2120 UNKNOWN CNDAIR CL600 CL6002D24 1390016 EA CABIN SMOKE A MASA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 SW 07 909FJ 15009 ASH FLT 2817 OKC-LAS - FWD AND AFT LAV MASTER WARNING WITH ODOR OF SMOKE IN COCKPIT AND CABIN. RESET, OPS CHECK GOOD. RAN ENGINE AND NO SMOKE DETECTED. 2 L 7 2 4F RT A21EA 2008011600162 20080116 00162 EA 2008 1 16 MASA200700794 1 20071111 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN MISINSTALLED A MASA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SW 07 519LR 10260 ASH FLT 7442 ORD - FWD FA FLASHLIGHT INOPERATIVE. MX INSTALLED FLASHLIGHT CORRECTLY. 2 L 7 2 4F RT A21EA 2008011600165 20080116 00165 EA 2008 1 16 MASA200700420 1 20070714 A 2150 ACM CNDAIR CL600 CL6002D24 1390016 EA RIGHT SMOKE A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 938LR 15038 ASH 2691 MDT-CLT - RETURNED TO FIELD DUE TO AFT LAV SMOKE WARNING. FERRIED TO CLT WHERE MX REMOVED AND REPLACED RT ACM. 2 L 7 2 4F RT A21EA 2008011600166 20080116 00166 EA 2008 1 16 MASA200700614 1 20070920 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 904FJ 15004 ASH FLT 2853 PHX-LAX - EMERGENCY FLOOD LIGHT AISLE 20 INOP. MX RELAMPED THE FLOOD LIGHT, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008011600169 20080116 00169 EA 2008 1 16 MASA200700886 1 20071215 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 905J 15005 ASH FLT 2704 PHX - MAIN CABIN DOOR EMERGENCY EXIT LIGHT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2008011500303 20080115 00303 EA 2008 1 15 MASA200700765 1 20071101 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 917FJ 15017 ASH FLT 2660 CLT - ROW 20 OVERHEAD EMERGENCY FLOOD LIGHT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2008011500316 20080115 00316 WP 2008 1 15 ABXA080002 1 20071227 A 3350 60030451 POWER SUPPLY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 968AX 44 47499 EMERGENCY LIGHT INOPERATIVE IN "ON" POSITION. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY PACK IAW DC9 AMM 33-53-00-4 . 2 L 7 2 4F A6WE 2008011500337 20080115 00337 WP 2008 1 15 ABXA080017 1 20071213 A 5320 99581713 INTERCOSTAL DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 INTERCOSTAL ANGLE CRACKED AT STA 237, BUTT LINE 0. STOP DRILLED AND REPAIRED CRACK IAW SSRM K05159. INSTALLED HI-LOKS IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2008011600048 20080116 00048 EU 2008 1 16 NSVA20070121 1 20070502 A 2612 472326 FIRE LOOP SAAB SF340 340B 7860101 EU RT NACELLE MALFUNCTIONED A NSVA O OTHER N FALSE WARNING CR CRUISE 1 EA 27 347CJ 347 INTERMITTENT RIGHT FIRE DETECT FAIL LIGHT ILLUMINATED ON CWP IN FLIGHT. REMOVED AND REPLACED RIGHT ENGINE SENSOR LOOP S ECTION IAW AMM 26-11-05. OPS CHECK GOOD, PN ON-OFF 472326. 2 L 7 2 4T RT A52EU 2008011600094 20080116 00094 EU 2008 1 16 NSVA20070092 1 20070409 A 2731 7255250503 TRIM TAB SAAB SF340 SF340A 7850100 EU LT ELEVATOR VIBRATION A NSVA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 27 35SZ 35 FLIGHT CONTROL VIBRATIONS ON CLIMB-OUT AT VARIOUS AIRSPEEDS. FLIGHT CONTROL VIBRATIONS MAINLY ELEVATOR. INSTALLED LT E LEVATOR TRIM TAB IAW SAAB AMM 27-35-25 PN ON 7255250-503, SN ON 35, SN OFF NSN. 2 L 7 2 4T RT A52EU 2008011600098 20080116 00098 EU 2008 1 16 NSVA20070222 1 20070905 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 184CJ 340B184 THE FOLLOWING EMERGENCY FLOOR AISLE LIGHTS ARE INOP THE LAST 4 AND ONE ON ROW 8. REMOVED AND REPLACED POS NR 5 EMERGENC Y LIGHT POWER SUPPLY IAW AMM 33-50-10-04, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008011600126 20080116 00126 EA 2008 1 16 MASA20700487 1 20070806 A 3411 PITOT SYSTEM CNDAIR CL600 CL6002D24 1390016 EA STANDBY CONTAMINATED A MASA O OTHER C F.O.D. NR NOT REPORTED 1 SW 07 909FJ 15009 ASH 2920 FAT-PHX - REJECTED TAKE OFF DUE TO STALL FAIL CAUTION MESSAGE. MX FOUND WATER IN THE STAND BY PITOT SYSTEM AND DRAINED. NO FURTHER FAULTS NOTED. 2 L 7 2 4F RT A21EA 2008011600128 20080116 00128 2008 1 16 MASA200700679 4 20071009 A 2330 AMPLIFIER CNDAIR CL600 CL6002B19 1900309 EA PA UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77260 7260 ASH FLT 2872 PHX - FA EMERGENCY ALERT ONLY CHIMES ONCE. MX RESECURED PA AMP, OPS CK GOOD. 2 L 7 2 4F RT A21EA 2008011600129 20080116 00129 EA 2008 1 16 MASA200700400 1 20070707 A 2150 A/C PACK CNDAIR CL600 CL6002D24 1390016 EA AN 2 SMOKE A MASA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 07 938LR 15038 ASH 2995 LGB - RETURNED TO FIELD DUE TO AFT LAV SMOKE WARNING W/SMOKE IN CABIN. CONTRACT MX PERFORMED ENGINE RUNS AND O PERATIONAL CHECKS OF AIR CONDITIONING PACKS AND ISOLATED SOURCE OF SMOKE TO NR 2 PACK. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008011600136 20080116 00136 EA 2008 1 16 MASA200700495 1 20070808 A 2150 GG670950095 ACM CNDAIR CL600 CL6002D24 1390016 EA RIGHT OVERTEMP A MASA O OTHER M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 SW 07 910FJ 9014 15010 ASH 2623 EWR-CLT - SMELL OF SMOKE IN CABIN AND RT PACK TEMP UNCONTROLLABLE. MX REMOVED AND REPLACED THE RT ACM, OPS NOR MAL. 2 L 7 2 4F RT A21EA 2008011600141 20080116 00141 NM 2008 1 16 MASA200700888 1 20071216 A 3230 WIRE DHAV DHC8 DHC8202 2809007 NM MLG SWITCH DAMAGED A MASA O OTHER O OTHER AP APPROACH 1 SW 07 447YV 447 ASH FLT 7096 MTJ - GEAR DID NOT EXTEND WHEN SELECTED. EMERGENCY EXTENSION USED. MX REPAIRED WIRING AT LG INHIBIT SWIT CH. 2 H 7 2 4T RT A13NM 2008011600149 20080116 00149 EA 2008 1 16 MASA200700320 1 20070611 A 5220 COVER CNDAIR CL600 CL6002D24 1390016 EA EXIT DOOR HANDLE UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 911FJ 15011 ASH 2791 LAS - 15A EMERGENCY EXIT DOOR HANDLE COVER WILL NOT STAY UPRIGHT. MX SECURED COVER. 2 L 7 2 4F RT A21EA 2008011600171 20080116 00171 2008 1 16 MASA200700423 2 20070715 A 7261 CARBON SEAL CNDAIR CL600 CL6002D24 1390016 EA NR 1 LEAKING A MASA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 938LR 15038 ASH 2698 CLT - PILOT RETURNED TO FIELD DUE TO AN AFT LAV SMOKE DETECTOR INDICATION AND POSSIBLE SMOKE AFTER TAKEOFF. RE MOVED AND REPLACED 1 AND 3 CARBON SEALS, C SUMP SEAL AND PRSOV, NO LEAKS NOTED. OPS CK GOOD. 2 L 7 2 4F RT A21EA 2008011600172 20080116 00172 EA 2008 1 16 MASA200700682 1 20071011 A 2560 SIGN CNDAIR CL600 CL6002D24 1390016 EA CABIN INACTIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 932LR 15032 ASH FLT 2916 PHX-COS - PHOTOLUMINESCENCE SIGN ON FLOOR FORWARD OF LAV WILL NOT GLOW. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008011600223 20080116 00223 EA 2008 1 16 MASA200700731 1 20071023 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002D24 1390016 EA ILLUMINATED A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 935LR 15035 ASH FLT 2674 CLT - RUDDER LIMIT STATUS MESSAGE. MX PERFORMED S POST, OPS CK GOOD. 2 L 7 2 4F RT A21EA 2008011600225 20080116 00225 EA 2008 1 16 MASA200700822 1 20071125 A 5220 SEAL CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT DIRTY A MASA O OTHER O OTHER CR CRUISE 1 SW 07 906FJ 15006 ASH FLT 2885 PHX-IAH. EMERGENCY EXIT DOOR AT 15A SQUEALS IN FLIGHT. MX INSPECTED AND CLEANED THE SEAL. 2 L 7 2 4F RT A21EA 2008011600226 20080116 00226 EA 2008 1 16 MASA200700548 1 20070903 A 5240 BF58722039087229 COVER CNDAIR CL600 CL6002D24 1390016 EA SERVICE DOOR MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 938LR 15038 SERVICE DOOR LOWER EXIT SIGN COVER MISSING. INSTALLED COVER. 2 L 7 2 4F RT A21EA 2008011600228 20080116 00228 EA 2008 1 16 MASA200700573 1 20070912 A 3350 BR92798722013 LIGHT CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 904FJ 15004 ASH FLT 2785 PHX - EMERGENCY EXIT ROW LIGHTS INOP AT ROWS 17 AND 22. MX REPLACED LIGHTS. 2 L 7 2 4F RT A21EA 2008011600230 20080116 00230 EA 2008 1 16 MASA200700914 1 20071222 A 3350 505802 COVER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 503MJ 10058 ASH FLT 7177 IAD - EMERGENCY EXIT LIGHT COVER AT SERVICE DOOR MISSING. INSTALLED COVER. 2 L 7 2 4F RT A21EA 2008011600231 20080116 00231 EA 2008 1 16 MASA200700451 1 20070723 A 5220 COVER CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 909FJ 15009 ASH 2830 LAS-TUS - EMERGENCY EXIT DOOR RT SIDE AT 15 D/F HANDLE COVER WILL NOT STAY SHUT. RESECURED AS REQUIRED. 2 L 7 2 4F RT A21EA 2008011600233 20080116 00233 NM 2008 1 16 MASA200700752 1 20071029 A 2520 10141812 PSU DHAV DHC8 DHC8202 2809007 NM SMOKE A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 988HA 8009 426 ASH FLT 2871 YUM-PHX - ODOR OF SMOKE IN CABIN NEAR OVERHEAD BIN ROW 4. MX REMOVED AND REPLACED PSU. 2 H 7 2 4T RT A13NM 2008011600234 20080116 00234 EA 2008 1 16 MASA200700326 1 20070612 A 5220 SEAL CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT DIRTY A MASA O OTHER O OTHER CR CRUISE 1 SW 07 918FJ 15018 ASH 2806 PHX - AFT OVERWING EMERGENCY EXIT DOOR SQUEALS IN FLIGHT. INSPECTED AND CLEANED SEAL, REINSTALLED DOOR, OPS GO OD. 2 L 7 2 4F RT A21EA 2008011600238 20080116 00238 EA 2008 1 16 MASA200700929 1 20071230 A 5220 SJ3518 HOOK AND LOOP CNDAIR CL600 CL6002D24 1390016 EA HANDLE COVER DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 917FJ 15017 ASH FLT 2682 CLT - ROW 15DF EMERGENCY EXIT HANDLE COVER WILL NOT STAY SECURE. MX REPLACED HOOK AND LOOP. 2 L 7 2 4F RT A21EA 2008011600241 20080116 00241 EA 2008 1 16 MASA200700881 1 20071214 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002D24 1390016 EA ILLUMINATED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 921FJ 15021 ASH FLT 2665 - INBOUND TO CLT, PITCH FEEL CAUTION MESSAGE. MX PERFORMED AN S-POST TEST, FAULTS CLEARED. NO DEFECTS NOT ED. 2 L 7 2 4F RT A21EA 2008011600248 20080116 00248 EA 2008 1 16 MASA200700890 1 20071216 A 5250 LATCH CNDAIR CL600 CL6002D24 1390016 EA COCKPIT DOOR LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 905J 15005 ASH FLT 2724 LAS - COCKPIT DOOR DEAD BOLT STICKEY. MX LUBED LATCH, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008011600249 20080116 00249 NM 2008 1 16 USAA920080020 1 20071210 A 5320 146N871221 ATTACH ANGLE BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON R4 DOOR THRESHOLD FRAME ATTACH ANGLE, BS 1681, RBL 58, WL 208. REP LACED R4 DOOR THRESHOLD FRAME ATTACH ANGLE, BS 1681, RBL 58, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600252 20080116 00252 NM 2008 1 16 USAA920080023 1 20071210 A 5320 141N516046 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL CHANNEL, BS 310 - BS 324, RBL 39, WL 208. REPLACED INT ERCOSTAL CHANNEL, BS 310 - BS 324, RBL 39, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600254 20080116 00254 NM 2008 1 16 USAA920080025 1 20071211 A 5320 141N517048 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL, BS 365 - BS 377, LBL 63, WL 208. REPLACED INTERCOSTAL , BS 365 - BS 377, LBL 63, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600255 20080116 00255 NM 2008 1 16 USAA920080026 1 20071211 A 5320 141N517040 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL, BS 345 - BS 365, LBL 63, WL 208. REPLACED INTERCOSTAL , BS 345 - BS 367, LBL 63, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600257 20080116 00257 NM 2008 1 16 USAA920080028 1 20071211 A 5320 140N250532 ATTACH ANGLE BOEING 757 7572B7 1384964 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - CRACKED INTERCOSTAL ATTACH ANGLE, BS 1620 - BS 1640, BL 0, WL 208. REPLACED INTERCOSTAL ATTACH ANGLE, BS 1620 - BS 1640, BL 0, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600261 20080116 00261 NM 2008 1 16 USAA920080032 1 20071213 A 5320 146N52162 GUSSET BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON AFT CABIN FLOOR SUPPORT ATTACH PLATE / GUSSET, BS 1681, BL 0, WL 20 8. REPLACED AFT CABIN FLOOR SUPPORT ATTACH PLATE / GUSSET, BS 1681, BL 0, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600263 20080116 00263 NM 2008 1 16 USAA920080034 1 20071217 A 5230 146N6603286 INTERCOSTAL BOEING 757 7572B7 1384964 NM CARGO DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON AFT CARGO DOOR LOWER TEE CHORD INTERCOSTAL, BS 1380, S24R - S25R. REPLACED AFT CARGO DOOR LOWER TEE CHORD INTERCOSTAL, BS 1380, S24R - S25R IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600265 20080116 00265 NM 2008 1 16 USAA920080036 1 20071217 A 5230 146N6603286 INTERCOSTAL BOEING 757 7572B7 1384964 NM CARGO DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON AFT CARGO DOOR LOWER TEE CHORD INTERCOSTAL, BS 1430, S24R - S25R. REPLACED AFT CARGO DOOR LOWER TEE CHORD INTERCOSTAL, BS 1430, S24R - S25R IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600269 20080116 00269 NM 2008 1 16 USAA920080040 1 20071219 A 5320 146N876947 FITTING BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON L4 DOOR THRESHOLD SUPPORT CHANNEL CLIP, BS 1671, LBL 58, WL 208. R EPLACED L4 DOOR THRESHOLD SUPPORT CHANNEL CLIP, BS 1671, LBL 58, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600271 20080116 00271 NM 2008 1 16 USAA920080043 1 20071210 A 5320 141N516039 FITTING BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL / FITTING, BS 330, RBL 24 - RBL 45. REPLACED INTERCOST AL / FITTING, BS 330, RBL 24 - RBL 45 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600272 20080116 00272 NM 2008 1 16 USAA920080044 1 20071222 A 5320 146N5318 WEB BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON AFT CABIN FLOOR PRESSURE WEB, BS 1681 - BS 1720, LBL 57 - RBL 57, WL 208. REPAIRED AFT CABIN FLOOR PRESSURE WEB, BS 1681 - BS 1720, LBL 57 - RBL 57, WL 208 IAW B757 SRM 53-60-51. 2 L 7 2 4F RT A2NM 2008011600273 20080116 00273 NM 2008 1 16 USAA920080045 1 20071211 A 5315 141N517031 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON FLOORBEAM SUPPORT, BS 310 - BS 324, LBL 20, WL 208. REPLACED FLO ORBEAM SUPPORT BS 310 - BS 324, LBL 20, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600288 20080116 00288 NM 2008 1 16 MASA200700724 1 20071022 A 5520 STRUCTURE DHAV DHC8 DHC8202 2809007 NM LT ELEVATOR DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 987HA 425 LIGHTNING STRIKE ON LT ELEVATOR TRAILER EDGE. COMPLIED WITH PERMANENT REPAIR AND CHECKED THE BALANCE OF THE ELEVATOR. 2 H 7 2 4T RT A13NM 2008011600289 20080116 00289 EA 2008 1 16 MASA200700512 1 20070820 A 5280 HINGE PIN CNDAIR CL600 CL6002D24 1390016 EA LT NLG DOOR DAMAGED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 902FJ 15002 ASH 2610 CLT-MYR - AIRCRAFT RETURNED TO FIELD DUE TO NLG DOOR WARNING AFTER RETRACTION. MX REMOVED AND REPLACED LT SPAD E DOOR HINGE PIN. 2 L 7 2 4F RT A21EA 2008011600290 20080116 00290 EA 2008 1 16 MASA200700915 1 20071222 A 3297 525063 WIRE HARNESS CNDAIR CL600 CL6002D24 1390016 EA WOW DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 925FJ 15025 ASH FLT 2781 (INBOUND) - PILOT REPORTED A GEAR DISAGREE WARNING ON GEAR RETRACTION. REMOVED AND REPLACED NLG HARNESS AN D SENSOR, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008011600291 20080116 00291 EA 2008 1 16 MASA200700919 1 20071225 A 2730 PULLEY CNDAIR CL600 CL6002D24 1390016 EA ELEVATOR LACK OF LUBE A MASA O OTHER O OTHER LD LANDING 1 SW 07 932LR 15032 ASH FLT 2677 CLT - ON LANDING ROLL OUT, THE ELEVATOR LOCKED UP ON THE CREW. CHECKED AND LUBED PULLEYS TO FO ELEVATOR CO NTROL, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008011600292 20080116 00292 EA 2008 1 16 MASA200700683 1 20071013 A 2840 WARNING LIGHT CNDAIR CL600 CL6002D24 1390016 EA ILLUMINATED A MASA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 07 902FJ 15002 ASH FLT 9701 LAS-LAS - LOW FUEL CAUTION MSG AFTER T/O. MX IS CURRENTLY TROUBLESHOOTING THE SYSTEM. 2 L 7 2 4F RT A21EA 2008011600295 20080116 00295 EA 2008 1 16 MASA200700770 1 20071103 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA SWITCH INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27314 7314 ASH 7323 IAD-SAV - COCKPIT PA, CHIME, AND EMERGENCY SWITCH LIGHTS INOP. MX RELAMPED SWITCH LIGHTS. 2 L 7 2 4F RT A21EA 2008011600296 20080116 00296 EA 2008 1 16 MASA200700771 1 20071103 A 2150 A/C PACK CNDAIR CL600 CL6002D24 1390016 EA ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 932LR 15032 ASH 2781 PHX-BFL - CAPTAIN REPORTED STRONG BURNING ODOR IN CABIN AND COCKPIT. MX INSPECTED AND RAN AIR CONDITIONING PAC KS AND FOUND NO EVIDENCE OF BURNING ODOR IN COCKPIT OR CABIN. SYSTEM OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008011600297 20080116 00297 NM 2008 1 16 USAA920080112 1 20071210 A 5320 141N515081 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL, BS 324 - BS 350, RBL 24. REPLACED INTERCOSTAL, BS 324 - BS 350, RBL 24 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600299 20080116 00299 NM 2008 1 16 USAA920080113 1 20071215 A 5310 141N842241 CREASE BEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON R1 DOOR CUTOUT INNER CREASE BEAM ANGLE, BS 310 - BS 377, RBL 58. R EPLACED R1 DOOR CUTOUT INNER CREASE BEAM ANGLE, BS 310 - BS 377, RBL 58 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600300 20080116 00300 NM 2008 1 16 USAA920080114 1 20071213 A 5320 141N516078 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL / SUPPORT, BS 345 - BS 365, RBL 58, WL 208. REPLACED I NTERCOSTAL / SUPPORT, BS 345 - BS 365, RBL 58, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600304 20080116 00304 NM 2008 1 16 USAA920080050 1 20071222 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 22198 PIT - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION FLOORBEAM, BS 1641, LBL 16. REPAIRED FLOORBEAM, BS 1641, LBL 16 IAW US AIRWAYS TYPICAL REPAIR 53-15-01. 2 L 7 2 4F RT A2NM 2008011600307 20080116 00307 NM 2008 1 16 USAA920080126 1 20071210 A 5320 141N5160102 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION INTERCOSTAL / SUPPORT, BS 324 - BS 345, RBL 40. REPLACED INTERCOSTAL / SUPPORT, BS 324 - BS 345, RBL 40 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600308 20080116 00308 NM 2008 1 16 USAA920080127 1 20071211 A 5320 141N517029 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION INTERCOSTAL / SUPPORT, BS 324 - BS 345, LBL 32. REPLACED INTERCOSTAL / SUPPORT, BS 324 - BS 345, LBL 32 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600309 20080116 00309 EA 2008 1 16 MASA200700649 1 20070926 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 913FJ 15013 ASH FLT 2604 CLT TO ORF - AFT CEILING EMERGENCY FLOODLIGHT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2008011600310 20080116 00310 NM 2008 1 16 USAA920080128 1 20071211 A 5315 141N5160207 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION FLOORBEAM TOP PLATE / FILLER, BS 297 - BS 310, BL 0. REPLACED FLOORBE AM TOP PLATE / FILLER, BS 297 - BS 310, BL 0 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600311 20080116 00311 NM 2008 1 16 USAA920080129 1 20071211 A 5315 141N51232 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION FLOORBEAM, BS 377, LBL 58 - RBL 58. REPLACED FLOORBEAM, BS 377, LBL 5 8 - RBL 58 IAW USAIRWAYS TYPICAL REPAIR 53-15-01. 2 L 7 2 4F RT A2NM 2008011600312 20080116 00312 NM 2008 1 16 USAA920080130 1 20071211 A 5315 141N51314 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION FLOORBEAM, BS 402, RBL 24, WL 208. REPLACED FLOORBEAM, BS 402, RBL 24 , WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600314 20080116 00314 NM 2008 1 16 USAA920080047 1 20071211 A 5320 141N516251 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL / FITTING, BS 365 - BS 377, RBL 58. REPLACED INTERCOST AL / FITTING, BS 365 - BS 377, RBL 58 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600315 20080116 00315 NM 2008 1 16 USAA920080048 1 20071218 A 5320 146N545121 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON INTERCOSTAL, BS 1600 - BS 1620, S29L. REPLACED INTERCOSTAL, BS 1600 - BS 1 620, S29L IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600316 20080116 00316 EA 2008 1 16 MASA200700722 1 20071021 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 905J 15005 ASH FLT 2601 CLT-IAH - AFT EMERGENCY CEILING FLOODLIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 2008011600317 20080116 00317 EA 2008 1 16 MASA200700660 1 20071002 A 3350 BULB CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 936LR 15033 ASH FLT 2716 PHX-FAT - ROW 15DF LOWER EMERGENCY LIGHT HAS 1 BULB INOP. SECURED BULB. 2 L 7 2 4F RT A21EA 2008011600318 20080116 00318 EA 2008 1 16 MASA200700663 1 20071003 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 917FJ 15017 ASH FLT 2811 PHX - EMERGENCY EXIT LIGHT AT ROW 16A, 16F, IN THE GALLEY AND BY THE MAIN CABIN DOOR HAS 1 LIGHT BULB INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2008011600320 20080116 00320 NE 2008 1 16 AALA20072483 2 20071220 A 7261 OIL SYSTEM DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LEFT ENGINE LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 971TW 53621 716770 FAT INFLIGHT T1846/20DEC SJC TO DFW - LEFT ENGINE INDICATIONS OIL QUANTITY ZERO AND OIL TEMPERATURE RISING. CREW SHUT D OWN ENGINE AS PRECAUTION. LANDED FAT WITHOUT INCIDENT. SINGLE ENGINE TIME 46 MINUTES WITH POSITIVE OIL PRESSURE. REPL ACED NUMBER ONE ENGINE ON 22 DEC AT FAT DUE TO OIL LEAK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A6WE E9NE 2008011600321 20080116 00321 NM 2008 1 16 AALA20072481 1 20071220 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 383AN 26995 MIA - EMERGENCY LIGHT AT LEFT AFT DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008011600322 20080116 00322 WP 2008 1 16 AALA20072482 1 20071220 A 3240 BRAKE DOUG DC9 DC982 3022082 WP MLG DAMAGED A AALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 7518A 49895 STL TAXI T1118/20DEC - DURING TAXI SOUNDS AND FEELS LIKE A POSSIBLE DRAGGING BRAKE. AIRCRAFT PULLS TO THE RIGHT. SUSPE CT RIGHT BRAKES DRAGGING BUT HAVE INDICATION OF HIGH TEMPERATURE ON LEFT INBOARD BRAKE. FOUND NUMBER TWO WHEEL ASSEMBLY INNER HUB BROKEN AND DAMAGE TO BRAKE. REPLACED NUMBER TWO BRAKE AND NUMBER TWO MAIN LANDING GEAR TIRES AND WHEEL ASSEM BLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011600324 20080116 00324 WP 2008 1 16 AALA20072486 1 20071220 A 2560 1001191 FLASHLIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9627R 53597 AUS - EMERGENCY FLASHLIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED PORTABLE LIGHT ASSEMBLY AT LEFT NUMBER ONE DOO R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008011600326 20080116 00326 WP 2008 1 16 AALA20072489 1 20071220 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 274AA 49271 DFW - EMERGENCY SEAT MOUNTED LIGHT AT SEAT 14D MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY SEAT MOUNTED LIGHT AT SEAT 1 4D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011600327 20080116 00327 WP 2008 1 16 AALA20072488 1 20071220 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AA 49271 DFW - EMERGENCY SEAT MOUNTED LIGHT AT SEAT 14D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011600328 20080116 00328 WP 2008 1 16 AALA20072487 1 20071220 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 33414 49325 LGA - EMERGENCY FLASHLIGHT AT AFT FLIGHT ATTENDANT SEAT HAS DAMAGED STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT A FT FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011600341 20080116 00341 EU 2008 1 16 SIMA200800802 1 20071215 A 2120 UNKNOWN SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CABIN ODOR A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 394AE 340B394 ON FLIGHT 3063, CREW REPORTED A STRONG ODOR THROUGHOUT THE CABIN WITH BLEEDS ON. CREW DECLARED AN EMERGENCY AND RETURNE D TO LAX. AIRCRAFT WAS REMOVED FROM SERVICE. MAINTENANCE PERFORMED A GENERAL VISUAL INSPECTION OF BOTH ENGINES AND ACM S. NO DEFECTS NOTED. PERFORMED ENGINE COMPRESSOR WASH RUNS IAW WORK CARD 72-4018 STEP 6. PERFORMED FCF. FCF FOUND S ATISFACTORY NO ODOR NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011500344 20080115 00344 WP 2008 1 15 ABXA080012 1 20071215 A 5712 9919305 RIB DOUG DC9 DC941 302207N WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 47596 RIGHT WING LEADING EDGE RIB WAS CRACKED BETWEEN TWO FASTENERS. LOCATED JUST INBOARD OF THE NR 5 SLAT TRACK. REPAIRED R IGHT WING LEADING EDGE RIB JUST INBOARD OF NR 5 SLAT TRACK IAW REA D957-56780. 2 L 7 2 4F A6WE 2008011600042 20080116 00042 CE 2008 1 16 NSVA20070104 1 20070416 A 2612 CIRCUIT BOARD BEECH 1900 1900D 1154162 CE B FIRE LOOP MALFUNCTIONED A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 124CJ UE24 RIGHT TEST B FIRE LOOP INOP. REPLACED PCB P/N 101-364580-1 S/N OFF 672C93 S/N ON 579-M92, REPLACED PCB P/N 129-364079-7 S/N OFF 898J94 S/N ON 743-H-93, ANNUNCIATOR POWER LIGHT AND LT OIL PRESS WARNING LOW, OPS CHECK GOOD IAW MM 31-10-00. 2 L 7 2 4T RT A24CE 2008011600087 20080116 00087 EU 2008 1 16 NSVA20070125 1 20070506 A 3150 WARNING LIGHT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ILLUMINATED A NSVA O OTHER J WARNING INDICATION CL CLIMB 1 EA 27 343CJ 343 AMBER F/I STOP LIGHT ILLUMINATED AFTER TAKEOFF. RESET FLT IDLE STOP OP CHECK IN ACCORDANCE SAAB 340 AMM 76-10-60-02. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011600099 20080116 00099 EU 2008 1 16 NSVA20070229 1 20070917 A 3150 WARNING LIGHT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ILLUMINATED A NSVA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 203CJ 203 RT ITT ILLUMINATED IN FLIGHT UP TO 75 INCREASE FROM ORIGINAL VALUE TORQUE GAINED APPROX PLUS 3-4 PERCENT. RAN ABNORMAL CHECK LIST TORQUE MOTOR KNOCK OUT PERFORMED FLUCTUATIONS INCREASED. PERFORMED FAULT ISOLATION IAW GE MM 72-00-00 REF NO RMAL FLIGHT OPERATIONS FAULT ISOLATION STEP 9&11. ALSO PERFORMED ECU TEST IAW GE MM TR 72-0597 TO ENSURE ALL INPUTS FRO M ECU WERE PROPERLY REPORTING. PERFORMED ENGINE RUNS FOR 10 MIN AT 80 PERCENT TRQ COULD NOT DUPLICATE FAULT AT THIS TIM E. NO FURTHER REASON TO BELIEVE THAT THIS DISCREPANCY IS STILL PRESENT. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011600132 20080116 00132 EA 2008 1 16 MASA200700509 1 20070818 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17358 7358 ASH 2752 PHX - CAPTAIN REPORTED FWD CEILING EMERGENCY LIGHT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2008011600137 20080116 00137 EA 2008 1 16 MASA200700496 1 20070808 A 2150 A/C PACK CNDAIR CL600 CL6002D24 1390016 EA RIGHT SMOKE A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 921FJ 15021 ASH 2615 CLT - CAPTAIN REPORTED SMOKE IN THE CABIN. MX PLACED THE RT PACK ON MEL. 2 L 7 2 4F RT A21EA 2008011600144 20080116 00144 EA 2008 1 16 MASA200700926 1 20071229 A 5220 CUSHION CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 924FJ 15024 ASH FLT 2816 PHX - EMERGENCY EXIT DOOR 15DF HANDLE RUBBER CUSHION MISSING. CHANGED HANDLE. 2 L 7 2 4F RT A21EA 2008011600148 20080116 00148 EA 2008 1 16 MASA200700587 1 20070917 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 942LR 15042 ASH 2926 IN FAT, CAPTAIN REPORTED 3RD BACK CEILING LEVEL EMERGENCY FLOOD LIGHT INOP. RELAMPED CEILING LEVEL EMERGENCY L IGHT, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008011600159 20080116 00159 EA 2008 1 16 MASA200700630 1 20070924 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 934FJ 15034 ASH FLT 2653 CLT TO IAH - AFT CEILING EMERGENCY FLOOD LIGHT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2008011600163 20080116 00163 EA 2008 1 16 MASA200700795 1 20071111 A 1100 S15748 PLACARD CNDAIR CL600 CL6002D24 1390016 EA SEAT MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 928LR 15028 ASH FLT 2606 GSO-CLT - SEAT 15 A EXIT PLACARD MISSING OFF SEATBACK. MX INSTALLED PLACARD. 2 L 7 2 4F RT A21EA 2008011600168 20080116 00168 NM 2008 1 16 MASA200700885 1 20071214 A 6123 3014403 TSCU DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 2 MALFUNCTIONED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 437YV 13575 437 PCEAG0003 ASH FLT 2849 PHX - AUTO FEATHER ON LIGHT ILLUMINATED IN FLIGHT NR 2 NOT FEATHERING. CHANGED NR 2 TSCU. 2 H 7 2 4T 4 T RT A13NM E20NE 2008011600227 20080116 00227 EA 2008 1 16 MASA200700766 1 20071102 A 5754 STRUCTURE CNDAIR CL600 CL6002D24 1390016 EA LT WING LE DENTED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 913FJ 15013 IMPACT DAMAGE TO LT OUTBOARD L/E. COMPLIED WITH REPAIR. 2 L 7 2 4F RT A21EA 2008011600235 20080116 00235 EA 2008 1 16 MASA200700931 1 20071231 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 928LR 15028 ASH FLT 2642 ATL - 2 CEILING EMERGENCY FLOOD LIGHTS INOP (NOT ADJACENT). RELAMPED AND RESET LIGHTING SYSTEM, OPS GOOD. 2 L 7 2 4F RT A21EA 2008011600236 20080116 00236 SO 2008 1 16 MASA200700445 1 20070723 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 860MJ 145773 ASH 7447 CLT - MAIN CABIN DOOR DIFFICULT TO CLOSE. MX CLEANED AND LUBED PAX DOOR. 2 L 7 2 4T RT T00011AT 2008011600237 20080116 00237 EA 2008 1 16 MASA200700864 1 20071207 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7264V 7264 ASH 2825 PHX - CEILING LIGHT ROW 11 INOP. MX RELAMPED, OPS CHECKED NORMAL. 2 L 7 2 4F RT A21EA 2008011600240 20080116 00240 EA 2008 1 16 MASA200700867 1 20071210 A 2150 A/C PACK CNDAIR CL600 CL6002D24 1390016 EA LEFT SMOKE A MASA O OTHER M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 909FJ 15009 ASH 2677 CLT-STL - LT PACK WENT TO 90 DEGREES "C" AND SMOKE CAME FROM THE VENTS. MX PERFORMED, OP CHECKS AND ALL WERE G OOD. 2 L 7 2 4F RT A21EA 2008011600245 20080116 00245 NM 2008 1 16 USAA920080018 1 20071209 A 5230 146N6603183 INTERCOSTAL BOEING 757 7572B7 1384964 NM CARGO DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON AFT CARGO DOOR INTERCOSTAL WEB, BS 1420, S24R - S25R. REPLACED AFT CARGO D OOR INTERCOSTAL WEB, BS 1420, S24R - S25R IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600251 20080116 00251 NM 2008 1 16 USAA920080022 1 20071210 A 5320 146N53235 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON AFT CABIN FLOOR SUPPORT CHANNEL, BS 1661 - BS 1681, BL 0, WL 208. REPLACED AFT CABIN FLOOR SUPPORT CHANNEL, BS 1661 - BS 1681, BL 0, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600259 20080116 00259 NM 2008 1 16 USAA920080030 1 20071213 A 5230 146N6603183 INTERCOSTAL BOEING 757 7572B7 1384964 NM CARGO DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON AFT CARGO DOOR INTERCOSTAL WEB, BS 1440, S25R. REPLACED AFT CARGO DOOR INT ERCOSTAL WEB, BS 1440, S25R IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600264 20080116 00264 NM 2008 1 16 USAA920080035 1 20071217 A 5230 146N6603286 INTERCOSTAL BOEING 757 7572B7 1384964 NM CARGO DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON AFT CARGO DOOR LOWER TEE CHORD INTERCOSTAL, BS 1400, S24R - S25R. REPLACED AFT CARGO DOOR LOWER TEE CHORD INTERCOSTAL, BS 1400, S24R - S25R IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600268 20080116 00268 NM 2008 1 16 USAA920080039 1 20071228 A 5755 113N540045 SPOILER BOEING 757 7572B7 1384964 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEFT WING NR 4 SPOILER CRACKED, WS 460 - WS 472. REPAIRED LEFT WING NR 4 SPOILER, WS 46 0 - WS 472 IAW B757 SRM 51-70-04. 2 L 7 2 4F RT A2NM 2008011600301 20080116 00301 NM 2008 1 16 USAA920080115 1 20071211 A 5320 141N51703 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL / SUPPORT, BS 324 - BS 345, LBL 36, WL 208. REPLACED I NTERCOSTAL / SUPPORT, BS 324 - BS 345, LBL 36, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600356 20080116 00356 EU 2008 1 16 705712212007 1 20071221 A 6210 1171586006 FITTING BOLKMS BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101750B1 41560 NE MAIN ROTOR CRACKED E QMLA K NONE Z SIGNIFICANT FAILURE REPORT IN INSP/MAINT 1 NM 03 990SL 801 3623 7057 WHILE PERFORMING AIRWORTHINESS CK, MECHANIC FOUND CRACK IN OB LOWER END OF MAIN ROTOR BLADE CUFF (BLADE FITTING 0 DEGREE - NEW STYLE) EXTENDING FROM THE BLADE ROOT OPENING TO THE ATTACHMENT BOLT THAT HOLDS THE UPPER AND LOWER CUFF HALVES TO GETHER ON THE SECONDARY BOLT SIDE OF THE CUFF. 1 G 7 2 3U 3 U NC H13EU E5NE10 2008011600357 20080116 00357 SW 2008 1 16 HEER118527 1 20071216 A 5320 407030450197S SUPPORT BELL 407 407 1182206 SW ALLSN 250C 250C47B GL CRACKED B HEER K NONE O OTHER NR NOT REPORTED 1 SW 03 740PH 53435 FOUND BOTH LT AND RT SUPPORT CRACKED IN RADIUS AT 7TH SCREW IB ATTACHMENT. BOTH ANGLES CRACKED IN IDENTICAL AREA. REMO VED AND REPLACED BOTH SUPPORT ANGLES. 1 G 7 1 3U 3 U O H2SW E1GL 2008011600358 20080116 00358 NM 2008 1 16 TSAA0824002 1 20070104 A 2460 MS2452423 SWITCH BOEING 737 7372X6C 1384552 NM P5 PANEL FAILED A TSAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 WP 13 840AL 23124 NON-ETOPS CARGO FLIGHT 945 KOA-HNL - DURING CLIMB, THE LEFT DC BUSS LOST POWER. THE CREW STARTED THE APU TO REESTABLISH ELECTRICAL LOAD TO THE LEFT HAND DC BUSS. THE AIRCRAFT LANDED IN KOA WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE NR 1 GENERATOR ON MEL 24-1-1 AND RETURNED THE AIRCRAFT TO SERVICE. MAINTENANCE REMOVED AND REPLACED THE GENERATOR CONT ROL SWITCH AND REMOVED MEL 24-1-1. 2 L 7 2 4F RT A16WE 2008011600369 20080116 00369 NM 2008 1 16 AALA20072491 1 20071221 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 751AN 30798 DFW - EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER THREE DOO R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011600371 20080116 00371 NM 2008 1 16 AALA20072493 1 20071221 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 751AN 30798 DFW - EMERGENCY LIGHT AT SEAT 33G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 33G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011600372 20080116 00372 WP 2008 1 16 AALA20072494 1 20071221 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 458AA 49563 LGA - EMERGENCY FLASHLIGHT AT AFT FLIGHT ATTENDANT STATION HAS BROKEN STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT FLIGHT ATTENDANT STATION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011600375 20080116 00375 NM 2008 1 16 AALA20072503 1 20071222 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 MIA - EMERGENCY LIGHT AT SEAT 23G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011600377 20080116 00377 NM 2008 1 16 AALA20072505 1 20071222 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 MIA - EMERGENCY LIGHT AT SEAT 25C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011600379 20080116 00379 NM 2008 1 16 AALA20072509 1 20071222 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 DFW - EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011600389 20080116 00389 2008 1 16 COEA0712911 4 20071221 A 3425 7003360947 AHRS AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE E&E BAY FAILED A COEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 13 911FX 045 FLT NR 8202 JUN TO SIT, FLT NR 7203 SEA TO KTN AIR TURN BACKS: NR 2 AHRS (ALTITUDE AND HEADING REF SYSTEM) WITH EFIS CO MP ( ELECTRONIC FLIGHT INSTRUMENTS SYS FAULTED). FLT NR 8203 AHRS CONNECTIONS CLEANED AND RESECURED, SYSTEM OPERATED NO RMALLY FOR 3 STOPS. FLT NR 7203 AHRU REPLACED (ALTITUDE AND HEADING REF UNIT). REF NR 45982, 86. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011600390 20080116 00390 EU 2008 1 16 COEA0742821 1 20071024 A 5310 S53671XXX CREASE BEAM AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. MAJOR REPAIR. LEVEL 2 CORROSION ON RT AND LT AFT CREASE BEAM WEBS. FORMED AND INSTALLED NEW REPLACEMENT WEBS. LT CREASE BEAM PN S53671217, RT CREASE BEAM PN S53671318. WO 72242 NR 200082. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011600392 20080116 00392 EU 2008 1 16 COEA0746821 1 20070907 A 5755 HINGE FITTING AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE RT SPOILER CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 29796 253 FOUND DURING HEAVY CHECK. LEVEL 2 CORROSION ON RT WING SPOILER HINGE ATTACHMENT FITTINGS INNER, CENTER, AND OUTER. REP LACED THE FOLLOWING FITTING. PN INNER S5771201000203, CENTER S5721211520000, OUTER S5771201000003. WO 72245, 42, 41. ( K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011700001 20080117 00001 EA 2008 1 17 MASA200700648 1 20070926 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002D24 1390016 EA LAVATORY INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 956LR 15056 ASH 2691 IN CLT, CAPTAIN REPORTED FWD LAV SMOKE DETECTOR INOP W/N TEST. MX PERFORMED OPS CHECK, OPS CHECK WAS GOOD. 2 L 7 2 4F RT A21EA 2008011700014 20080117 00014 CE 2008 1 17 DXTA200702724 1 20071229 A 2740 55657563 WHEEL CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE TRIM CRACKED E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 635QS 3997 5605358 TRIM INDICATOR IS NOT INDEXED CORRECTLY. TRIM WAS CHECKED AND SET TO TAKEOFF RANGE BEFORE START. JUST PRIOR TO ENGINE ST ART, BOTH PILOTS NOTICED TRIM INDICATOR FULL FORWARD. TRIM WAS RESET TO TAKEOFF RANGE, TAXI AND TAKEOFF WERE BEGUN. DUR ING TAKEOFF, YOKE STARTED MOVING AFT BEFORE FIRST OFFICER STARTED PULLING AFT FOR ROTATION. AFTER TAKEOFF FIRST OFFICER STARTED CALLING FOR FORWARD TRIM, THEN ASKED FOR PITCH TRIM C.B. TO BE PULLED. HE STATED THAT AFTER PITCH TRIM C.B. WAS PULLED, HE DIDN'T FEEL INCREASING AFT PRESSURE ANYMORE. TRIM WAS OPERATED MANUALLY AND NORMAL LANDING FOLLOWED. AFTER L ANDING, TRIM INDEXER SHOWED 1/2 INCH FORWARD OF WHITE ARC WITH FULL NOSE DOWN TRIM AND RIGHT IN THE MIDDLE OF THE TAKEOF 2 L 7 2 4F 4 F RT A22CE E00059EN 2008011700015 20080117 00015 CE 2008 1 17 DXTA200702731 1 20071231 A 3297 WIRE HARNESS CESSNA 500 560CESSNA 2076750 CE MLG CHAFED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 340QS 5600514 LANDING GEAR WILL NOT RETRACT. FOUND WIRE BUNDLE CHAFED IN 2 LOCATIONS JUST AFT OF WHEEL WELL. REPAIRED DAMAGED WIRES IA W CE560 M/M CHAP 32-01-00. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A22CE 2008011700017 20080117 00017 CE 2008 1 17 DXTA200702722 1 20071230 A 2740 CONTROL WHEEL CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE PITCH TRIM DAMAGED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 693QS 5605657 (EMERGENCY DECLARED) ON ROTATION AN UNUSUAL NOSE UP FORCE WAS NOTED REQUIRING FULL NOSE DOWN TRIM. BOTH PILOTS APPLIED NOSE DOWN PRESSURE AND CONDITION WORSENED AS SPEED INCREASED. FOUND PITCH TRIM WHEEL IMPROPERLY CLOCKED & PART OF INDIC ATOR TRACK MISSING. REPLACED PITCH TRIM CONTROL WHEEL WITH A NEW WHEEL & PROPERLY POSITIONED INDICATOR PINS PER CE560XL MM 27-10-05. OPS CHECK GOOD. VERIFIED PITCH TRIM TO OPERATED NORMALLY STOP TO STOP. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008011700018 20080117 00018 CE 2008 1 17 DXTA200702725 1 20071228 A 3230 UNKNOWN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 340QS 5600514 AFTER ESTABLISHING A POSITIVE RATE FOR TAKEOFF, ATTEMPTED TO RETRACT MLG. MLG HANDLE WOULD NOT RETRACT. NOTICED ALL LIGH TS EXTINGUISHED AND CB BREAKER POPPED. MLG CB WOULD NOT RESET, MANUALLY EXTENDED MLG AS A PRECATIONARY MEASURE AND LAND ED SAFELY. RESET CIRCUIT BREAKER AND JACKED ACFT TO PERFORM RETRACTION/ EXTENSION CHECK SERVICED GEAR BLOW DOWN BOTTLE AND RESET HANDLE AND VALVE. CLEANED CONNECTORS IN WHEEL WELLS. INSPECTED ALL WING ACCESSABLE IN WHEEL WELLS AND UNDER I NSTRUMENT PANEL NEAR GEAR HANDLE. REPLACED 4327 BULBS IN GREEN DOWNLOCK ANNUNCIATOR BLOCK AND 2327 BULBS IN GEAR RED UNS AFE ANNUNCIATOR BLOCK. SERVICED HYDRAULIC RESERVOIR TO PROPER LEVEL. PERFORMED WIGGLE TEST ALL HARNESSES IN WHEEL WELLS 2 L 7 2 4F 4 F RT A22CE E25EA 2008011700020 20080117 00020 CE 2008 1 17 DXTA200702727 1 20071228 A 3297 66187046 CIRCUIT BOARD CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE LT MLG INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 658QS 1077 5605665 CLIMBING TO ALTITUDE THE LEFT GREEN INDICATOR LIGHT STARTED FLICKERING ON AND OFF. NO HYDRAULIC OR GEAR UNSAFE LIGHTS WE RE PRESENT. AT FL300 IT CONTINUED TO FLICKER AND STYING ON LONGER AND LONGER, IT DID THIS FOR 1/2 HOUR. AT GEAR EXTENSI ON ALL GREEN LIGHTS. REMOVED LANDING GEAR PCB CARD. INSTALLED NEW PCB CARD. PERFORMED OPS ON LANDING GEAR WITH NO DEFEC TS NOTED AT THIS TIME. WORK DONE IAW CITATION 560XLS MM CH 24-51-01 2 L 7 2 4F 4 F RT A22CE E00059EN 2008011700021 20080117 00021 CE 2008 1 17 DXTA200702728 1 20071228 A 5210 LINE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE DOOR SEAL CONTAMINATED E DXTA G B O2 MASK DEPLOYED EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 07 335QS 5600335 EMERGENCY DECLARED, LOST PRESSURIZATION WHILE IN CRUISE AT FL390. HEARD AUDIBLE "POP" FOLLOWED BY AIR "HISSING" AND CAB IN CLIMBING AT >4000 FPM. CABIN ALT REACHED 10000 FEET. DEPLOYED MASKS MANUALLY FOR ELDERLY PAX. PERFORMED EMER DESCEN T CABIN REMAINED NEAR 10000 FT TILL PASSING FL240 IN THE DESCENT. INSPECTED CABIN PRESS SYSTEM FOUND SMALL AMOUNT OF WAT ER IN DOOR SEAL LINES ALONG WITH TORN DOOR GROMMET. PURGED SYSTEM WITH NITROGEN AND REPLACED GROMMET. COMPLIED WITH PRES SURE CHECK INSIDE. OPS CK GOOD. GROUND RUN AIRCRAFT OPS CK GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2008011700022 20080117 00022 2008 1 17 DXTA200702729 4 20071228 A 3418 861CAU2 PROBE AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE AOA INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 259QS 6149 159 RT AUTO SLAT LIGHT AT ROTATION ALONG WITH STALL EYEBROW. NO OTHER ABNORMAL INDICATIONS. STALL EYEBROW INDICATION UNTIL 200 KTS. AUTO SLAT LIGHT WENT OUT 15 MIN INTO FLIGHT. REMOVED LT AOA PROBE AND INSTALLED A MODIFIED AOA PROBE IAW FAL CON 2000 AMM 27-813. PERFORMED OPERATIONAL TEST OF THE AOA PROBE IAW FALCON 2000 AMM 27-813 AND AOA PROBE ANTI-ICE TOS I AW FALCON 2000 AMM 30-300 AND OPS TESTS CHECKED GOOD. PERFORMED OPS TEST OF THE SLATS SYSTEM AND OPS TEST CHECKED GOOD I AW FALCON 2000 AMM 27-803. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F 4 F RT A50NM E44NE 2008011700029 20080117 00029 CE 2008 1 17 CWQA071203 1 20071212 A 3000 2744148513 BYPASS VALVE LEAR 60 60LEAR 5170707 CE ANTI-ICE SYS INOPERATIVE E CWQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 05 725SC 083 DURING CRUISE FLIGHT BOTH BLEED AIR OVERHEAT LIGHT ILLUMINATED. CREW DIVERTED TO KDEN. DURING MAINTENANCE, LEFT ENGINE A NTI-ICE BYPASS VALVE WAS FOUND DEFECTIVE. VALVE WAS REPLACED IN ACCORDANCE TO AIRCRAFT MAINTENANCE MANUAL AND RETUNED TO SERVICE. 2 L 7 2 4F RT A10CE 2008011700033 20080117 00033 NM 2008 1 17 QXEA200702046 1 20071230 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY MALFUNCTIONED A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 349PH 486 MFR - ON TAXI THE LAV SMOKE DETECTOR WENT OFF. RETURNED TO THE GATE AND RESET THE DETECTOR. MAINTENANCE COULD NOT DUPL ICATE PROBLEM. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008011700097 20080117 00097 NM 2008 1 17 AALA20072538 1 20071228 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 770AN 29578 MIA - EMERGENCY LIGHT AT SEAT 21C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011700098 20080117 00098 NM 2008 1 17 AALA20072539 1 20071228 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 770AN 29578 MIA - EMERGENCY LIGHT AT SEAT 26C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011700099 20080117 00099 NM 2008 1 17 AALA20072536 1 20071228 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 770AN 29578 MIA - EMERGENCY LIGHT AT SEAT 21C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011700100 20080117 00100 NM 2008 1 17 AALA20072537 1 20071228 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 770AN 29578 MIA - EMERGENCY LIGHT AT SEAT 26C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011700101 20080117 00101 NM 2008 1 17 AALA20072543 1 20071229 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 755AN 30263 LHR EMERGENCY LIGHT AT SEAT 24C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011700102 20080117 00102 NM 2008 1 17 AALA20072544 1 20071228 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 761AJ 31478 DFW - EMERGENCY LIGHT AT FIRST CLASS GALLEY RIGHT FORWARD FLOOR BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FIRST CLASS GALLEY RIGHT FORWARD FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011700103 20080117 00103 NM 2008 1 17 AALA20072542 1 20071229 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 755AN 30263 LHR EMERGENCY LIGHT AT SEAT 24C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011700104 20080117 00104 EU 2008 1 17 AALA20072540 1 20071228 A 3240 C20103500 SERVO VALVE AIRBUS 300 A300B4605R 3930308 EU BREAKS INOPERATIVE A AALA O OTHER M J OVER TEMP WARNING INDICATION LD LANDING 1 SW 21 25071 514 JFK INFLIGHT T1892/28DEC - DURING LANDING, BRAKES THREE AND SEVEN REACHED BRAKE TEMPERATURE OF 370 DEGREES. AIRCRAFT TAXIED TO GATE. REPLACED BRAKE SYSTEM CONTROL UNIT AND SERVO VALVE 75GC. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008011700105 20080117 00105 WP 2008 1 17 AALA20072541 1 20071228 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 245AA 49257 LGA - EMERGENCY LIGHTS AT SEAT ROWS 20DEF TO 22DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 20DEF TO 22DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011800012 20080118 00012 NM 2008 1 18 UIEA200800001 1 20071228 A 5753 SKIN BOEING 747 74747UF 1384812 NM RT WING TE FLAP PUNCTURED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 499MC 29260 RIGHT INBOARD TRAILING EDGE FLAP (AFT) COMPOSITE STRUCTURE HAS PUNCTURE IN IT APPROX 1 INCH IN LENGTH ABOUT 13 INCHES IN BOARD OF OUTBOARD FACE OF NR 5 CANOE FAIRING. PERMANENT REPAIR CARRIED OUT IAW SRM 57-53-01 AND XEO 57-122807. 2 L 7 4 4F RT A20WE 2008011800014 20080118 00014 2008 1 18 UIEA200800005 4 20071228 A 2210 2590624933 SELECTOR PANEL BOEING 747 7472D7B 1384803 NM AUTOPILOT FAILED A UIEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 15 522MC 21783 A/P F/D SYSTEM "A" ROLL DC CIRCUIT BREAKER POPPED, PREVIOUSLY DETECTED ELECTRICAL ODOR MOMENTARILY. 2 L 7 4 4F RT A20WE 2008011600091 20080116 00091 EU 2008 1 16 NSVA20070130 1 20070513 A 7712 TORQUE SENSOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE DIRTY A NSVA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 EA 27 350CJ 350 NO TQ INDICATION ON LT ENGINE ON TAKEOFF ROLL. CLEANED AND INSPECTED TORQUE SENSOR IAW SAAB AMM 77-13-10-02. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2008011600097 20080116 00097 EU 2008 1 16 NSVA20070210 1 20070814 A 3246 WHEEL SAAB SF340 340B 7860101 EU NLG VIBRATION A NSVA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 EA 27 210CJ 210 AIRPLANE WOBBLED (SHIMMY) EXCESSIVELY ON TAKEOFF, ABORTED TAKEOFF). RT LT NOSE TIRE IAW WORKCARD 32-41-01S. REMOVED A ND REPLACED RT NOSE TIRE IAW WORKCARD 32-41-01S. 2 L 7 2 4T RT A52EU 2008011600125 20080116 00125 EA 2008 1 16 MASA200700486 1 20070806 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7264V 7264 ASH 2750 PHX - REPORTED AN EMERGENCY FLOOR PATH LIGHTING STRIP LOOSE. MX RESECURED THE LOOSE STRIP. 2 L 7 2 4F RT A21EA 2008011600133 20080116 00133 EA 2008 1 16 MASA200700510 1 20070819 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17337 7337 ASH 2741 PHX REPORTED THE LT AND RT FUSELAGE FWD OVERWING EXIT LT INOP. MX RELAMPED THE LIGHT. 2 L 7 2 4F RT A21EA 2008011600145 20080116 00145 EA 2008 1 16 MASA200700920 1 20071226 A 2731 FE301000002 PITCH CONTROL CNDAIR CL600 CL6002D24 1390016 EA ELEVATOR MALFUNCTIONED A MASA O OTHER J WARNING INDICATION LD LANDING 1 SW 07 932LR 7472 15032 ASH FLT 2671 CLT - ELEVATOR JAMMED ON TOUCH DOWN. REMOVED AND REPLACED PITCH FEEL SIMULATOR. 2 L 7 2 4F RT A21EA 2008011600146 20080116 00146 2008 1 16 MASA200700923 4 20071229 A 3418 501177003 CONTROL UNIT CNDAIR CL600 CL6002D24 1390016 EA STALL WARNING MALFUNCTIONED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 932LR 7472 15032 ASH FLT 9700 (TEST FLIGHT) - ABORT T/O ELEVATOR JAM AT ROTATION. REMOVED AND REPLACED STICK PUSHER. 2 L 7 2 4F RT A21EA 2008011600160 20080116 00160 EA 2008 1 16 MASA200700786 1 20071109 A 3350 BULB CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 912FJ 15012 ASH FLT 2834 PHX - TUS - LOWER LEFT EXIT ROW LIGHT HAS 2 BULBS INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2008011600164 20080116 00164 EA 2008 1 16 MASA200700421 1 20070714 A 3150 UNKNOWN CNDAIR CL600 CL6002D24 1390016 EA UNKNOWN A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 926LR 15026 ASH 2917 LA, RTG DUE TO NR 1 MLG BTMS IS AT 7 WITH ALL THE OTHERS AT 1. MX TROUBLESHOT AND OPS CHECKED NORMAL. 2 L 7 2 4F RT A21EA 2008011600167 20080116 00167 EA 2008 1 16 MASA200700912 1 20071221 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGNECY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 513MJ 10111 ASH FLT 7267 ATL - CEILING EMERGENCY LIGHT INOP ROW 16. RELAMPED, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008011600243 20080116 00243 EA 2008 1 16 MASA200700883 1 20071215 A 3150 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA LT WING A/I ILLUMINATED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 504MJ 12755 ASH FLT 7386 ORD - LT WING ANTI ICE CAUTION IN FLIGHT. RESET, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008011600244 20080116 00244 EA 2008 1 16 MASA200700884 1 20071216 A 5270 SENSOR CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR WARNING MALFUNCTIONED A MASA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SW 07 956LR 15056 ASH FLT 2610 SRQ-CLT - PASSENGER DOOR WARNING MESSAGE ON TAXI (REPEAT). REPAIRED WIRE TO SENSOR (PX47), OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008011600246 20080116 00246 EA 2008 1 16 MASA200700889 1 20071216 A 5270 WARNING MESSAGE CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR ILLUMINATED A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 956LR 15056 ASH FLT 2610 SRQ-CLT - PASSENGER DOOR WARNING MESSAGE WHEN DOOR IS CLOSED. RESET SYSTEM. 2 L 7 2 4F RT A21EA 2008011600247 20080116 00247 NM 2008 1 16 USAA920080019 1 20071210 A 5320 146N52468 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON FLOOR SUPPORT, BS 1640 - BS 1661, RBL 57, WL 208. REPLACED FLOOR S UPPORT, BS 1640 - BS 1661, RBL 57, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600253 20080116 00253 NM 2008 1 16 USAA920080024 1 20071211 A 5320 146N52421 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON MAIN CABIN FLOOR SUPPORT CHANNEL BS 1640 - BS 1661, BL-0, WL 208. REPLACED MAIN CABIN FLOOR SUPPORT CHANNEL BS 1640 - BS 1661, BL-0, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600260 20080116 00260 NM 2008 1 16 USAA920080031 1 20071213 A 5230 146N6603286 TEE FITTING BOEING 757 7572B7 1384964 NM CARGO DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON AFT CARGO DOOR INTERCOSTAL WEB TEE FITTING, BS 1390, S24R - S25R. REPLACED AFT CARGO DOOR INTERCOSTAL WEB TEE FITTING, BS 1390, S24R - S25R IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600293 20080116 00293 2008 1 16 MASA200700830 4 20071130 A 2561 P0640101 LIFE VEST CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 646BR 7392 ASH FLT 1038 HNL-ITO. INFANT LIFE VEST WAS MISSING. 2 L 7 2 4F RT A21EA 2008011600294 20080116 00294 EA 2008 1 16 MASA200700498 1 20070810 A 3230 LANDING GEAR CNDAIR CL600 CL6002D24 1390016 EA NOSE MALFUNCTIONED A MASA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 07 910FJ 15010 ASH 2779 MEM-PHX RETURNED TO FIELD BECAUSE THE NOSE LANDING GEAR WOULD NOT RETRACT. MX DIS-ASSEMBLED AND RE-ASSEMBLED G EAR, RESERVICED AND OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2008011600298 20080116 00298 EA 2008 1 16 MASA200700725 1 20071022 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 929LR 15029 ASH FLT 2661 CLT - ROW 20 CEILING LEVEL EMERGENCY FLOOD LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 2008011600306 20080116 00306 NM 2008 1 16 USAA920080117 1 20071230 A 5320 141N51603 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL / CHANNEL, BS 350 - BS 365, RBL 24, WL 208. REPLACED INTERCOSTAL / CHANNEL, BS 350 - BS 365, RBL 24, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600319 20080116 00319 EA 2008 1 16 MASA200700695 1 20071014 A 2620 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY NO TEST A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 154SF 7154 ASH FLT 7258 ORD-MSN - NR 2 CARGO FIRE BOTTLE WOULD NOT TEST. MX RESET THE TEST SYSTEM AND IT OP CHECKED GOOD. 2 L 7 2 4F RT A21EA 2008011600366 20080116 00366 WP 2008 1 16 AALA20072507 1 20071222 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DISLODGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 291AA 49303 LGA - EMERGENCY LIGHT AT EXTERIOR LEFT INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY LIGHT AT EXTERIOR LEFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011700125 20080117 00125 EA 2008 1 17 SWIA200719034 1 20071230 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA RIGHT SMOKE A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 983SW 7961 SHORTLY AFTER TAKEOFF, RECEIVED A SMOKE TOILET MESSAGE. PERFORMED OPS CHECK OF RIGHT PACK IAW AMM 21-51-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008011800016 20080118 00016 NM 2008 1 18 UIEA200800004 1 20071228 A 5753 SKIN BOEING 747 74747UF 1384812 NM TE FLAP PEELING A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 499MC 29260 LT INBOARD T/E AFT FLAP REPAIR ALUMINUM FOIL (SPEED TAPE) PEELING FROM CENTER OUTWARDS APPROX 12 INCHES OUTBOARD OF THE NR 4 CANOE FAIRING FACE AND 1 INCH FWD OF THE AFT EDGE. ALUMINUM FOIL (SPEED TAPE) REPLACED AS PER PART 2 OF WORK INSTR UCTIONS FOE INITIAL AND REPEAT INSPECTIONS DETAILED IN EO 4457A102. 2 L 7 4 4F RT A20WE 2008011800017 20080118 00017 NM 2008 1 18 UIEA200800003 1 20071228 A 5753 SKIN BOEING 747 74747UF 1384812 NM TE FLAPS DETERIORATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 499MC 29260 RIGHT T/E AFT FLAP REPAIR SIX INCHES FWD OF THE TRAILING EDGE AND 18 INCHES OUTBOARD OF THE OUTBOARD FACE OF NR 5 CANOE FAIRING HAS SIGNS OF DETERIORATION AND WATER INGRESS OVER AN AREA APPROX 1 INCH DIAMETER. PERMANENT REPAIR CARRIED OUT IAW SRM 57-53-01. VACUUM PRESSURE AND HEAT APPLIED AT 26 INCHES OF MERCURY AND 250 DEGREES. 2 L 7 4 4F RT A20WE 2008011800025 20080118 00025 2008 1 18 XXUA200700041 4 20071023 A 2565 D31042205 SLIDE BOEING 757 7572Q8 1384972 NM PWA PW2037 PW2037M 52117 NE R4 DOOR READS LOW A XXUA K NONE O OTHER IN INSP/MAINT 1 EA 15 926JS 24964 DURING DAILY CHECK, FOUND R4 DOOR SLIDE PRESSURE LOW. 2 L 7 2 4F 4 F RT A2NM E17NE 2008011800032 20080118 00032 SO 2008 1 18 LR7A07130 1 20071219 A 5350 33911927 FAIRING LKHEED 382 382G 526414U SO FS 845 WARPED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HC5301 FOUND RAMP DOOR EXTERIOR FWD PEDESTAL FAIRING SKIN WARP AT FS 845 (RAMP STA 10). REPAIR ACCOMPLISHED BY REPLACING FWD FAIRING IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008011800033 20080118 00033 SO 2008 1 18 LR7A07131 1 20071219 A 5350 3391194L FAIRING LKHEED 382 382G 526414U SO FS 845 LBL 24 WARPED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HC5301 FOUND RAMP DOOR EXTERIOR LT SIDE PEDESTAL FAIRING SKIN WARP FS 845 (RAMP STA 10) LBL24. REPAIR ACCOMPLISHED BY REPLACING FAIRING SKIN IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008011800034 20080118 00034 SO 2008 1 18 LR7A07132 1 20071219 A 5230 BRACKET LKHEED 382 382G 526414U SO FS906 BROKEN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HC5302 FOUND CARGO DOOR LOWER SKIN INTERIOR ATTACH BRACKET BROKEN AT FS 906 BL4 2L/42R. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-20. 2 H 7 4 4T A1SO 2008011800035 20080118 00035 SO 2008 1 18 LR7A07133 1 20071219 A 5312 LS3872 BULKHEAD LKHEED 382 382G 526414U SO BS 617 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HC5301 FOUND MULTIPLE CRACKS IN LT UPPER MWW BHD WEB INCLUDING EXISTING PATCH; FS 617 WL200, 212, AND 218 LBL88. REPAIR ACCOMPLISHED BY REPLACING WEB P/N LS3872 IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008011800036 20080118 00036 SO 2008 1 18 LR7A07134 1 20071219 A 5311 FRAME LKHEED 382 382G 526414U SO FS 817 WL257 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HC5302 FOUND AFT FUSELAGE UPPER BHD FORMER CRACKED AT FS 817, WL257. REPAIR AC COMPLISHED IAW SMP583 FIG 53-50-05. 2 H 7 4 4T A1SO 2008011800037 20080118 00037 SO 2008 1 18 LR7A07135 1 20071219 A 5230 DOUBLER LKHEED 382 382G 526414U SO FS 1012 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HC5302 FOUND CARGO DOOR BHD STIFFENER/REINFORCE DOUBLER CRACKED AT FS 1012, RBL 20, RBL 27. REPAIR ACCOMPLISHED BY REPLACING STIFFENER AND REINFORCING DOUBLER IAW SMP583 CHAP 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008011800038 20080118 00038 SO 2008 1 18 LR7A07136 1 20071219 A 5340 3400439R ATTACH ANGLE LKHEED 382 382G 526414U SO FS 477 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HC5316 FOUND UPPER RT WW ATTACH ANGLE (WING TO FUSELAGE FWD FILLET) CRACKED AT FS 477, WL284, RBL63. REPAIR ACCOMPLISHED BY REPLACING ATTACH ANGLE IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008011800039 20080118 00039 SO 2008 1 18 LR7A07137 1 20071219 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FS 597 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER SB382-57-82 R2 FOUND BOLT HOLE CRACKED IN UPPER AFT BHD WEB FOLLOWING REMOVAL OF ATTACH ANGLE AT FS 597, WL253, LBL62. REPAIR ACCOMPLISHED BY REPLACING AFT BULKHEAD WEB IAW SMP583 CHAPTER 53-40-02 AND 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008011800043 20080118 00043 SO 2008 1 18 LR7A07141 1 20071219 A 5712 BULKHEAD LKHEED 382 382G 526414U SO FS 570 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2, FOUND FASTENER HOLE CRACKED IN UPPER CTR BULKHEAD WEB AFTER ATTACH ANGLE REMOVAL AT FS570, WL254, LBL62. REPAIR ACCOMPLISHED BY FABRICATING AND REPLACING CTR UPPER BHD WEB IAW SMP583 CHAPTER 54-40-02 AND 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008011800044 20080118 00044 SO 2008 1 18 LR7A07142 1 20071219 A 5720 37327739 FILLER LKHEED 382 382G 526414U SO FS 495 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2, FOUND LT FUSELAGE ATTACH ANGLE STRAP FILLERS CRACKED AT FS 495 AND 498, WL256.5, LBL60. REPAIR ACCOMPLISHED BY REPLACING STRAP FILLERS P/N 373277-3 AND 373277-9 IAW SMP583 CH 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008011800046 20080118 00046 SO 2008 1 18 LR7A07144 1 20071219 A 7120 330821612 ATTACH FITTING LKHEED 382 382G 526414U SO ENGINE MOUNT DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, WHILE PERFORMING SCHEDULED TRUSS MOUNT CHANGE FOUND ENG NR 4 OBD TRUSS MOUNT RIB CAP ATTACH FTGS (INBD AND OBD), BOLT HOLES BEYOND LIMITS. REPAIR ACCOMPLISHED BY REPLACING FITTINGS P/N 3308216-1 AND 3308216-2 IA W SMP583 CHAP 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008011800047 20080118 00047 SO 2008 1 18 LR7A07145 1 20071219 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FS 597 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2 WHILE PERFORMING ATTACH ANGLE REPLACEMENT FOUND AFT BULKHEAD WEB CRACKED AT FS 597, WL257, RBL62. REPAIR ACCOMPLISHED BY REPLACING WEB IAW SMP583 CHAP 53-40-02, 51-60, AND 51-70. 2 H 7 4 4T A1SO 2008011800048 20080118 00048 SO 2008 1 18 LR7A07146 1 20071219 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FS 479 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2, WHILE PERFORMING ATTACH ANGLE REPLACEMENT FOUND RT FWD BULKHEAD WEB CRAC KED AT FS479, WL255, RBL62. REPAIR ACCOMPLISHED BY REPLACING BULKHEAD WEB IAW SMP583 CH 53-40-02, 51-60, AND 51-70. 2 H 7 4 4T A1SO 2008011800049 20080118 00049 SO 2008 1 18 LR7A07147 1 20071219 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FS 597 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HSP57119 FOUND LT CTR WING INTERIOR STRUCTURE BULKHEAD CRACKED AROUND FASTENER AT FS 597, CWS140L. REPAIR ACCOMPLISHED BY REINFORCING AREA WITH DOUBLER PATCH IAW SMP583 CH 51-140-17. 2 H 7 4 4T A1SO 2008011800050 20080118 00050 SO 2008 1 18 LR7A07148 1 20071219 A 3010 DIFFUSER LKHEED 382 382G 526414U SO ANTI ICE SYS CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HC5712 FOUND RT OUTER WING LEADING EDGE ANTI-ICING DIFFUSER CRACKED AT OWS211. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-070. 2 H 7 4 4T A1SO 2008011800051 20080118 00051 SO 2008 1 18 LR7A07149 1 20071219 A 5310 BEAM LKHEED 382 382G 526414U SO BS 527 BROKEN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HC5301 FOUND LT UPPER MWW BEAM OBD CAP BROKEN AT FS 527. REPAIR ACCOMPLISHED I AW LAC MEA 382-53-07-069. 2 H 7 4 4T A1SO 2008011800052 20080118 00052 SO 2008 1 18 LR7A07150 1 20071219 A 5340 LONGERON CLIP LKHEED 382 382G 526414U SO BS 557 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HC5301 FOUND RT MAIN WHEEL WELL OBD FRAME TO DOOR HINGE LONGERON TEE CLIP EXFOL IATION CORROSION AT FS 557. REPAIR ACCOMPLISHED BY REPLACING TEE CLIP IAW LAC MEA 382-53-07-80. 2 H 7 4 4T A1SO 2008011800053 20080118 00053 SO 2008 1 18 LR7A07151 1 20071219 A 5310 BEAM LKHEED 382 382G 526414U SO BS 527 BROKEN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HC5324 FOUND RT UPPER MAIN WHEEL WELL BEAM OBD CAP BROKEN AT FS 527R, WL230. R EPAIR ACCOMPLISHED IAW LAC MEA 382-53-07-069. 2 H 7 4 4T A1SO 2008011800054 20080118 00054 SO 2008 1 18 LR7A07152 1 20071219 A 5730 SKIN LKHEED 382 382G 526414U SO CENTER WING CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2 FOUND CORROSION ON RT UNDERWING SURFACE NR 1 AND NR 3 WING PLANKS BEHIND NR 3 ENGINE AFT NACELLE AREA CWS178-212 STRINGER 21-24. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-072 AND CORROSION REM OVED AND TREATED IAW SMP583 CH 51-30. 2 H 7 4 4T A1SO 2008011800056 20080118 00056 SO 2008 1 18 LR7A07154 1 20071219 A 5730 PANEL LKHEED 382 382G 526414U SO CENTER WING CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2 FOUND CRACK ON WING PLANK HOLE COMMON TO RT ATTACH ANGLE AT FS 517, CWS72 R, WL256. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-076. 2 H 7 4 4T A1SO 2008011800057 20080118 00057 SO 2008 1 18 LR7A07155 1 20071219 A 5730 PANEL LKHEED 382 382G 526414U SO BS 517 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2 FOUND CORROSION ON WING PLANK HOLE COMMON TO LT ATTACH ANGLE AT FS 517, C WS72L, WL256. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-076. 2 H 7 4 4T A1SO 2008011800058 20080118 00058 SO 2008 1 18 LR7A07156 1 20071219 A 5412 BULKHEAD LKHEED 382 382G 526414U SO BS 410 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HC7201 FOUND NR 3 ENG NACELLE FWD BULKHEAD RT OUTER CAP TEE CRACKED AT FS 410R PPWL10. REPAIR ACCOMPLISHED IAW LAC MEA 382-54-07-081. 2 H 7 4 4T A1SO 2008011800060 20080118 00060 SO 2008 1 18 LR7A07158 1 20071219 A 5712 RIB LKHEED 382 382G 526414U SO CENTER WING CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HSP57119 FOUND LT CENTER WING BULKHEAD FOOT RIB CAP CRACKED AT FS 517, CWS140L, WL256. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-075. 2 H 7 4 4T A1SO 2008011800067 20080118 00067 EA 2008 1 18 SWIA200719043 1 20070910 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 742SK 10197 FOUND AT C-CHECK, FS 280 FLOOR SUPPORT BEAM IS CRACKED IN UPPER RADIUS OF RBL9. REPLACED FS 280 BEAM PER CRJ700/900 SRM 51-92-06. 2 L 7 2 4F RT A21EA 2008011800073 20080118 00073 EA 2008 1 18 SWIA200719049 1 20070910 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 742SK 10197 FOUND AT C-CHECK, COCKPIT FLOOR SUPPORT IS CRACKED AT RBL9 AND LBL9. INSTALLED NEW COCKPIT FLOOR SUPPORT PER CRJ700/900 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008011800075 20080118 00075 EA 2008 1 18 SWIA200719051 1 20070910 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 742SK 10197 WEB AT FS 280 AND RBL 30 IS CORRODED, FOUND AT C-CHECK. INSTALLED WEB REPAIR PARTS IAW CRJ700/900 SRM 51-23-00 P9-10, 5 1-42-06 P7-8, 51-42-21 P9-11 AND REO 670-53-11-052 P1-5. 2 L 7 2 4F RT A21EA 2008011800076 20080118 00076 EA 2008 1 18 SWIA200719052 1 20070910 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 975SW 7951 FS 280 FLOOR SUPPORT ANGLE IS CRACKED AT RBL9 AND LBL9, FOUND AT C-CHECK. REPAIRED FS 280 FLOOR SUPPORT ANGLE BETWEEN R BL9.0 AND LBL9.0 IAW CRJ200 REO:601R-53-11-136. 2 L 7 2 4F RT A21EA 2008011800077 20080118 00077 EA 2008 1 18 SWIA200719053 1 20070910 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 975SW 7951 FS 280 FLOOR SUPPORT BEAM IS CRACKED AT LBL9, FOUND AT C-CHECK. REPAIRED FS 280 LBL9.0 SUPPORT ANGLE IAW CRJ200 REO:601 R-53-11-171 REV D. 2 L 7 2 4F RT A21EA 2008011800078 20080118 00078 EA 2008 1 18 SWIA200719054 1 20070910 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 975SW 7951 FS 280 FLOOR SUPPORT BEAM IS CRACKED AT RBL9, FOUND AT C-CHECK. REPAIRED FS 280 FLOOR SUPPORT BEAM IAW CRJ200 REO:601R- 53-11-171 REV D. 2 L 7 2 4F RT A21EA 2008011800079 20080118 00079 EA 2008 1 18 SWIA200719055 1 20070910 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 975SW 7951 STA 621 FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS IAW REO:601R-53-61-117 REV C. 2 L 7 2 4F RT A21EA 2008011800082 20080118 00082 NM 2008 1 18 AALA20072551 1 20071229 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AA 24589 DFW - EMERGENCY LIGHT AT SEAT 17D MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008011800083 20080118 00083 NM 2008 1 18 AALA20072552 1 20071229 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AA 24589 DFW - EMERGENCY LIGHT AT SEAT 17D MISSING RED LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008011800084 20080118 00084 NM 2008 1 18 AALA20072557 1 20071230 A 3397 WIRE BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 189AN 32383 LAX - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 35D INOPERATIVE. SECURED WIRES AT CONNECTOR FOR EMERGENCY LIGHT AT SEAT 35D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008011800085 20080118 00085 NM 2008 1 18 AALA20072545 1 20071229 A 3241 ANTI-SKID SYS BOEING 757 757223 1384957 NM MLG MULTIPLE FAIL A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 694AN 26974 SJU INFLIGHT T883/29DEC BOS TO STT - ANTI SKID EICAS MESSAGE ILLUMINATED AND REMAINED ON UNTIL LANDING. LANDED SJU WIT HOUT INCIDENT. REPLACED RIGHT MAIN LANDING GEAR UPPER CONDUIT, RIGHT ANTI SKID MODULE AND NUMBER EIGHT TRANSDUCER. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008011800088 20080118 00088 NM 2008 1 18 AALA20072549 1 20071229 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AA 24589 DFW - EMERGENCY LIGHT AT SEAT 9D MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008011800089 20080118 00089 NM 2008 1 18 AALA20072550 1 20071229 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AA 24589 DFW - EMERGENCY LIGHT AT SEAT 9D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A2NM 2008011800095 20080118 00095 EU 2008 1 18 AALA20072556 1 20071230 A 2780 COMPUTER AIRBUS 300 A300B4605R 3930308 EU SLAT/FLAP INOPERATIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 19059 469 SDQ INFLIGHT T423/30DEC - LEADING EDGE SLAT WOULD NOT EXTEND DURING APPROACH. LANDED SDQ WITHOUT INCIDENT. REPLACED NU MBER ONE SLAT FLAP CONTROL COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008011800096 20080118 00096 NM 2008 1 18 AALA20072566 1 20071231 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 773AN 29583 JFK - EMERGENCY LIGHT AT SEAT ROW 41G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 41G. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011800097 20080118 00097 NM 2008 1 18 AALA20072567 1 20071231 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 790AN 30251 JFK - EMERGENCY LIGHT AT SEAT ROW 24C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 24C. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011800098 20080118 00098 NM 2008 1 18 AALA20072568 1 20071231 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 790AN 30251 JFK - EMERGENCY LIGHT AT SEAT ROW 24C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 24C. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011800099 20080118 00099 NM 2008 1 18 AALA20072558 1 20071231 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 792AN 30253 NRT - EMERGENCY LIGHT AT FIRST CLASS COAT CLOSET DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FIRST CLASS C OAT CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011800100 20080118 00100 WP 2008 1 18 AALA20072559 1 20071231 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7506 49800 LGA - EMERGENCY LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD GALLEY. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011800101 20080118 00101 WP 2008 1 18 AALA20072560 1 20071231 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 496AA 49734 LGA - EMERGENCY LIGHT AT SEAT ROW 25DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 25DEF. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011800102 20080118 00102 WP 2008 1 18 AALA20072561 1 20071231 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 496AA 49734 LGA - EMERGENCY LIGHT AT SEAT ROW 13 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 13. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011800103 20080118 00103 WP 2008 1 18 AALA20072562 1 20071231 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 496AA 49734 LGA - EMERGENCY LIGHT AT SEAT ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 20. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011800104 20080118 00104 WP 2008 1 18 AALA20072563 1 20071231 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 496AA 49734 LGA - EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS CABI N. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011800105 20080118 00105 WP 2008 1 18 AALA20072564 1 20071231 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 3515 49892 LGA - EMERGENCY LIGHTS AT AFT LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011800107 20080118 00107 NM 2008 1 18 AALA20072572 1 20071231 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 944AN 29535 DFW - EMERGENCY LIGHT AT SEAT 14A INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 14A. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A16WE 2008011800109 20080118 00109 NM 2008 1 18 AALA20072573 1 20071231 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 626AA 24584 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 9D HAS SHROUD BROKEN. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 9D. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008011800110 20080118 00110 NM 2008 1 18 AALA20072571 1 20071231 A 2750 SENSOR BOEING 737 737823 13844BZ NM TE FLAPS OUT OF TOLERANCE A AALA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SW 21 931AN 30079 JFK INFLIGHT T766/31DEC DFW TO LGA - DURING APPROACH TO LGA FLAPS WOULD NOT EXTEND PROPERLY. LANDED JFK WITHOUT INCIDEN T. FOUND NUMBER SIX SKEW SENSOR OUT OF TOLERANCE. REPLACED NUMBER SIX SKEW SENSOR. SYSTEM GROUND CHECKED NORMAL OPERA TION. 2 L 7 2 4F RT A16WE 2008011800111 20080118 00111 NM 2008 1 18 AALA20072555 1 20071231 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 610AA 24486 JFK - EMERGENCY LIGHT AT SEAT 32D INOPERATIVE. SECURED CONNECTOR ON HARNESS FOR EMERGENCY LIGHT AT SEAT 32D. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008011800120 20080118 00120 EU 2008 1 18 NWAA074223306 1 20071201 A 5712 RIB AIRBUS 330 A330323 3930335 EU LT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 806NW 578 DURING INSPECTION PER AD 2006-22-14, FOUND CRACKS IN LT WING RIB NR 6. REPAIRED PER EA 33-208520. 2 L 7 2 4F RT A46NM 2008011800121 20080118 00121 EU 2008 1 18 NWAA074383306 1 20071201 A 5712 RIB AIRBUS 330 A330323 3930335 EU RT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 806NW 578 DURING INSPECTION PER AD 2006-22-14 FOUND CRACKS IN RT WING RIB NR 6. REPAIRED PER EA 33-208520. 2 L 7 2 4F RT A46NM 2008011800123 20080118 00123 EU 2008 1 18 NWAA074253308 1 20071206 A 5712 RIB AIRBUS A330 A330223 3940031 EU LT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 808NW 591 DURING INSPECTION PER AD 2006-22-14, FOUND CRACKS IN LT WING RIB NR 6. REPAIRED PER EA 33-208521. 2 L 7 2 4F RT A46NM 2008012200003 20080122 00003 EA 2008 1 22 A6WA200740697 1 20071210 A 5340 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BS 718 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 432AW 7257 RT HYDRAULIC SUPPORT BRACKET AT FS 718 IS CRACKED. RT HYDRAULIC SUPPORT BRACKET AF FS 718 IS CRACKED. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008011600170 20080116 00170 2008 1 16 MASA200700791 4 20071111 A 2300 BUTTON CNDAIR CL600 CL6002B19 1900309 EA INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 651ML 7139 ASH FLT 7364 ORD - AFT FA "EMER" PUSH BUTTON INOP. MX FOUND PUSHBUTTON TO WORK NORMALLY. 2 L 7 2 4F RT A21EA 2008011600173 20080116 00173 EA 2008 1 16 MASA200700891 1 20071216 A 3350 BR9279232 LIGHT CNDAIR CL600 CL6002D24 1390016 EA COCKPIT SMOKE A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 925FJ 15025 ASH FLT 2781 TUS - SMOKE ON RIGHT SIDE COCKPIT AT GLARE SHIELD. MX HAS FOUND THE FO FLOODLIGHTING ASSY THE SOURCE OF SM OKE. REPLACED FO FLOODLIGHT ASSY, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008011600195 20080116 00195 CE 2008 1 16 GUUA12280701 1 20071228 A 5520 1016200111 HINGE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87550 UE205 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR HINGE BRACKE T. 2 L 7 2 4T 4 T RT A24CE E26NE 2008011600224 20080116 00224 EA 2008 1 16 MASA200700501 1 20070812 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17358 7358 ASH 2796 LAS REPORTED A CEILING FLOOD LIGHT INOP. MX RELAMPED AND OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2008011600229 20080116 00229 EA 2008 1 16 MASA200700429 1 20070715 A 2120 UNKNOWN CNDAIR CL600 CL6002D24 1390016 EA CABIN ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 930LR 15030 ASH 2649 CLT - PILOT REPORTED A BURNING ODOR WITH HAZE IN CABIN WITH NR 2 ENGINE RUNNING AND NR 2 PACK ONLINE AT THE GAT E. OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2008011600232 20080116 00232 EA 2008 1 16 MASA200700715 1 20071019 A 5220 COVER CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 906FJ 15006 ASH FLT 2626 CLT - EMERGENCY EXIT HANDLE COVER WILL NOT STAY CLOSED AT SEAT 16A. MX RESECURED THE EXIT HANDLE COVER. 2 L 7 2 4F RT A21EA 2008011600242 20080116 00242 NM 2008 1 16 MASA200700882 1 20071215 A 5270 WARNING LIGHT DHAV DHC8 DHC8202 2809007 NM PAX DOOR ILLUMINATED A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 448YV 448 ASH FLT 7090 DRO-DEN - PASSENGER DOOR WARNING WITH ENGINES AT POWER. RESET SYSTEM, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2008011600250 20080116 00250 NM 2008 1 16 USAA920080021 1 20071210 A 5320 146N52467 SUPPORT BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON L4 DOOR CUTOUT SUPPORT, BS 1640 - BS 1661, LBL 56, WL 208. REPLACE D L4 DOOR CUTOUT SUPPORT, BS 1640 - BS 1661, LBL 56, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600256 20080116 00256 NM 2008 1 16 USAA920080027 1 20071211 A 5320 141N517030 SUPPORT BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL SUPPORT, BS 324 - BS 345, LBL 20, WL 208. REPLACED INT ERCOSTAL SUPPORT, BS 324 - BS 345, LBL 20, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600258 20080116 00258 NM 2008 1 16 USAA920080029 1 20071213 A 5230 146N6603183 INTERCOSTAL BOEING 757 7572B7 1384964 NM CARGO DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON AFT CARGO DOOR INTERCOSTAL WEB, BS 1460, S24R - S25R. REPLACED AFT CARGO D OOR INTERCOSTAL WEB, BS 1460, S24R - S25R IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600262 20080116 00262 NM 2008 1 16 USAA920080033 1 20071216 A 5320 141N5160102 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL, BS 324 - BS 365, RBL 58, WL 208. REPLACED AFT INTERCO STAL, BS 324 - BS 365, RBL 58, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600266 20080116 00266 NM 2008 1 16 USAA920080037 1 20071217 A 5320 146N524661 ATTACH ANGLE BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON L4 DOOR CUTOUT STRUCTURE ATTACH ANGLE CLIP, BS 1676, LBL 54, WL 208 . REPLACED L4 DOOR CUTOUT STRUCTURE ATTACH ANGLE CLIP, BS 1676, LBL 54, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600267 20080116 00267 NM 2008 1 16 USAA920080038 1 20071219 A 5320 146N524660 ATTACH ANGLE BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON R4 DOOR CUTOUT STRUCTURE ATTACH ANGLE, BS 1676, RBL 53, WL 208. RE PLACED R4 DOOR CUTOUT STRUCTURE ATTACH ANGLE, BS 1676, RBL 53, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600270 20080116 00270 NM 2008 1 16 USAA920080042 1 20071210 A 5320 146N52466 SUPPORT BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON R4 DOOR CUTOUT SUPPORT, BS 1661 - BS 1681, RBL 57, WL 208. REPLAC ED R4 DOOR CUTOUT SUPPORT, BS 1661 - BS 1681, RBL 57, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600302 20080116 00302 NM 2008 1 16 USAA920080116 1 20071219 A 5320 141N51603 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL / CHANNEL, BS 345 - BS 365, RBL 45, WL 208. REPLACED I NTERCOSTAL / CHANNEL, BS 345 - BS 365, RBL 45, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600303 20080116 00303 NM 2008 1 16 USAA920080049 1 20071213 A 5320 146N545111 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON INTERCOSTAL, BS 1500 - BS 1520, S30L. REPLACED INTERCOSTAL, BS 1500 - BS 1 520, S30L IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008011600305 20080116 00305 NM 2008 1 16 USAA920080051 1 20071226 A 5753 SKIN BOEING 757 757225 1384959 NM T/E FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 22198 PIT - MAJOR REPAIR - C4 CHECK, LEFT WING INBOARD FLAP UPPER SURFACE DELAMINATED. REPAIRED LEFT WING INBOARD FLAP UPPER SURFACE I/A/W USAIRWAYS EA 110418. 2 L 7 2 4F RT A2NM 2008011600313 20080116 00313 NM 2008 1 16 USAA920080046 1 20071211 A 5315 146N51091 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON FLOORBEAM, BS 1640, LBL 58 - RBL 58, WL 208. REPAIRED FLOORBEAM, B S 1640, LBL 58 - RBL 58, WL 208 IAW USAIRWAYS TYPICAL REPAIR 53-15-02. 2 L 7 2 4F RT A2NM 2008011600323 20080116 00323 NE 2008 1 16 AALA20072484 2 20071220 A 7250 BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RIGHT ENGINE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 70529 49921 718527 DFW INFLIGHT T1538/20DEC - NUMBER TWO ENGINE EXPERIENCED CONTAINED TURBINE FAILURE. ENGINE GAS TEMPERATURE SPIKED. CRE W SHUT DOWN NUMBER TWO ENGINE AND RETURNED TO DFW. LANDED WITHOUT INCIDENT. TOTAL WINDMILL TIME APPROXIMATELY 15 MINUT ES. REPLACED NUMBER TWO ENGINE ON 22 DEC AT DFW DUE TO TURBINE BLADE FAILURE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2008011600325 20080116 00325 WP 2008 1 16 AALA20072485 1 20071220 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 962TW 53612 LGA - EMERGENCY LIGHT IN COCKPIT INOPERATIVE. REPLACED BATTERY PACK AT AB5 23 FOR EMERGENCY LIGHTS IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008011600331 20080116 00331 EA 2008 1 16 MASA200700922 1 20071227 A 2910 601R7523567 LINE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A MASA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 07 47202 7202 ASH FLT 7371 LGA- IAD- LOSING ALL HYD 3 FLUID WHILE TRYING TO EXTEND THE GEAR. REMOVED AND REPLACED HYDRAULIC LINE. 2 L 7 2 4F RT A21EA 2008011600359 20080116 00359 EU 2008 1 16 MALA070205 1 20071231 A 2140 HEATER SAAB SF340 340B 7860101 EU ODOR A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 450XJ 340B450 CREW REPORTED A SULFUR ODOR IN CABIN. TURNED OFF AUX HEAT AND ODOR DISSIPATED. DEFERRED AUX HEAT. CLEANED THE HEATERS . 2 L 7 2 4T RT A52EU 2008011700034 20080117 00034 NM 2008 1 17 QXEA200702049 1 20071229 A 3150 WARNING MESSAGE BOMBDR DHC8 DHC8402 1390042 NM NLG STEERING FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 404QX 4046 SEA - FLIGHT 2330 - NOSE STEERING FAILED DURING TAXI. RETURNED TO THE GATE. MAINTENANCE CLEARED THE FAULT MESSAGE AND OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008011700035 20080117 00035 EA 2008 1 17 QXEA200702054 1 20071231 A 2150 SHUTOFF VALVE CNDAIR CL600 CL6002C10 1390015 EA LT A/C PACK FAILED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 616QX 10128 RNO - FLIGHT 9851 - WITH WING AI ON AND COWL A/I ON RECEIVED A LEFT BLEED MASTER CAUTION. LEFT PACK WAS CYCLING ON AND OFF. RETURNED TO THE GATE. MAINTENANCE REPLACED THE NR 1 ENGINE PRSOV. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008011700036 20080117 00036 NM 2008 1 17 QXEA200702053 1 20071231 A 3150 WARNING MESSAGE BOMBDR DHC8 DHC8402 1390042 NM FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 410QX 4053 SEA - FLIGHT 2279 - ON PUSHBACK RECEIVED A FLIGHT COMPARTMENT DUCT HOT CAUTION AND CABIN PACK HOT LIGHTS. RETURNED TO T HE GATE. MAINTENANCE CLEARED THE FAULTS PER FIM 21-60-00-810-801. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008011700037 20080117 00037 NM 2008 1 17 QXEA200702044 1 20071230 A 3150 WARNING LIGHT DHAV DHC8 DHC8202 2809007 NM ILLUMINATED A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 357PH 504 PUW - ON TOP OF DESCENT RECEIVED A NR 2 DC GENERATOR HOT CAUTION. TURNED OFF GENERATOR PER CHECKLIST, LIGHT WENT OUT. MAINTENANCE PLACED ON MEL 24-10. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008011700038 20080117 00038 NM 2008 1 17 QXEA200702045 1 20071230 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 403QX 4037 LAX - FLIGHT 2421 - RIGHT TRU HOT CAUTION ILLUMINATED. RAN CHECKLIST AND PULLED CIRCUIT BREAKER. LIGHT WENT OUT AFTER ABOUT 5 MINUTES. MAINTENANCE PERFORMED A OPERATIONAL CHECK WITH NO DEFECTS NOTED. COULD NOT DUPLICATE. AIRCRAFT RETUR NED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008011700039 20080117 00039 EA 2008 1 17 QXEA200702047 1 20071230 A 2612 FIRE WARNING CNDAIR CL600 CL6002C10 1390015 EA APU BAY ILLUMINATED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 601QX 10009 SEA - FLIGHT 2584 - APU FIRE FAIL CAUTION ILLUMINATED. MAINTENANCE PLACED ON MEL 26-12-1A. AIRCRAFT RETURNED TO SERVIC E. 2 L 7 2 4F RT A21EA 2008011700040 20080117 00040 EA 2008 1 17 QXEA200702048 1 20071230 A 2150 SENSOR CNDAIR CL600 CL6002C10 1390015 EA ACM INLET TEMP MALFUNCTIONED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 608QX 10026 GEG - FLIGHT 2599 - LEFT BLEED CAUTION ILLUMINATED. WENT OFF AFTER SELECTING PACK TO OFF. RETURNED TO THE FIELD AND AC COMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE PACK INLET TEMP SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT R ETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008011700041 20080117 00041 NM 2008 1 17 QXEA200702052 1 20071231 A 2150 SWITCH BOMBDR DHC8 DHC8402 1390042 NM OVERTEMP FAILED A QXEA O OTHER N FALSE WARNING AP APPROACH 1 NM 09 409QX 4051 SEA - FLIGHT 2223. NR 2 BLEED HOT CAUTION ILLUMINATED DURING APPROACH. AFTER COMPLETING CHECKLIST ITEMS THE LIGHT WENT OUT (ABOUT 3 MINUTES). MAINTENANCE FERRIED THE AIRCRAFT TO PDX FOR REPAIRS. IN PDX, THE OVERTEMP SWITCH WAS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008011700049 20080117 00049 NM 2008 1 17 AALA20072510 1 20071222 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 DFW - EMERGENCY LIGHT AT SEAT 26C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011700050 20080117 00050 NM 2008 1 17 AALA20072495 1 20071221 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 692AA 26972 DFW - EMERGENCY LIGHT AT SEAT 25D BROKEN OFF OF SEAT. REPLACED LIGHT ASSEMBLY AND NUT PLATE FOR EMERGENCY LIGHT AT SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008011700051 20080117 00051 NM 2008 1 17 AALA20072498 1 20071222 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 788AN 30011 MIA - EMERGENCY LIGHT AT SEAT 32G INOPERATIVE. REPAIRED LIGHT ASSEMBLY FOR INOPERATIVE EMERGENCY LIGHT AT SEAT 32G. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011700052 20080117 00052 NM 2008 1 17 AALA20072499 1 20071222 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 788AN 30011 MIA - EMERGENCY LIGHT AT SEAT 32G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 32G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011700053 20080117 00053 NM 2008 1 17 AALA20072500 1 20071222 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 788AN 30011 MIA - EMERGENCY LIGHT AT SEAT 25C LENS INOPERATIVE. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011700054 20080117 00054 NM 2008 1 17 AALA20072501 1 20071222 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 788AN 30011 MIA - EMERGENCY LIGHT AT SEAT 37C LENS INOPERATIVE. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 37C. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011700056 20080117 00056 WP 2008 1 17 AALA20072511 1 20071223 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 482AA 49675 LGA - EMERGENCY LIGHTS AT OVERHEAD FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD F ORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011700057 20080117 00057 NM 2008 1 17 AALA20072512 1 20071223 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7667A 25301 MIA - EMERGENCY LIGHT AT SEAT 24D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008011700058 20080117 00058 WP 2008 1 17 AALA20072517 1 20071224 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 427AA 49339 LGA - EMERGENCY LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011700059 20080117 00059 NM 2008 1 17 AALA20072519 1 20071225 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 762AN 31479 MIA - EMERGENCY LIGHT AT SEAT 22C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011700060 20080117 00060 NM 2008 1 17 AALA20072520 1 20071225 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 753AN 30261 JFK - EMERGENCY LIGHT AT SEAT 25G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 25G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011700061 20080117 00061 NM 2008 1 17 AALA20072521 1 20071225 A 3350 SHROUD BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 973AN 29548 DFW - EMERGENCY LIGHT AT SEAT 19D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 19D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008011700062 20080117 00062 NM 2008 1 17 AALA20072523 1 20071226 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 774AN 29581 JFK - EMERGENCY LIGHT AT SEAT 31G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 31G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011700063 20080117 00063 NM 2008 1 17 AALA20072524 1 20071226 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 774AN 29581 JFK - EMERGENCY LIGHT AT SEAT 33G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 33G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011700064 20080117 00064 NM 2008 1 17 AALA20072514 1 20071223 A 3350 COVER BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 MIA - EMERGENCY EXIT SIGN COVER AT AFT SERVICE DOOR FELL OFF. RESECURED EMERGENCY EXIT SIGN COVER AT AFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008011700065 20080117 00065 NM 2008 1 17 AALA20072513 1 20071223 A 3397 WIRE BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 781AN 29586 JFK - EMERGENCY LIGHT AT SEAT 9D INOPERATIVE. REPLACED BROKEN WIRE FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011700066 20080117 00066 NM 2008 1 17 AALA20072515 1 20071223 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 641AA 24599 DFW - EMERGENCY LIGHT AT RIGHT SEAT ROW 25 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT SEAT ROW 25. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008011700067 20080117 00067 NM 2008 1 17 AALA20072516 1 20071223 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 399AN 29606 MIA - EMERGENCY LIGHT AT SEAT 37B INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 37B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008011700068 20080117 00068 NM 2008 1 17 AALA20072518 1 20071225 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 NRT - EMERGENCY LIGHT AT FORWARD GALLEY CLOSET DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FORWARD GALLEY CLOSET DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011700069 20080117 00069 NM 2008 1 17 AALA20072522 1 20071225 A 2560 STRAP BOEING 767 767323 1385205 NM FLASHLIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 378AN 25447 SFO - EMERGENCY FLASHLIGHT AT AFT LEFT CENTER FORWARD FLIGHT ATTENDANT POSITION HAS BROKEN STRAP. REPLACED STRAP FOR EE MRGENCY FLASHLIGHT AT AFT LEFT CENTER FORWARD FLIGHT ATTENDANT POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008011700070 20080117 00070 WP 2008 1 17 AALA20072526 1 20071226 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 466AA 49596 TPA - EMERGENCY AISLE LIGHT AT SEAT 22E HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY AISLE LIGHT AT SEAT 22E. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011700071 20080117 00071 WP 2008 1 17 AALA20072527 1 20071226 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 466AA 49596 TPA - EMERGENCY AISLE LIGHT AT SEAT 22E HAS BROKEN LAMPS. REPLACED LAMPS FOR EMERGENCY AISLE LIGHT AT SEAT 22E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011700072 20080117 00072 WP 2008 1 17 AALA20072528 1 20071226 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 553AA 53083 LGA - EMERGENCY LIGHT AT SEAT ROW 29 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 29. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011700073 20080117 00073 NM 2008 1 17 AALA20072530 1 20071226 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS DISLODGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 779AN 29955 MIA - EMERGENCY LIGHTS AT SEAT ROWS 30CG TO 40CG INOPERATIVE. CLEANED AND RESEATED BATTERY PACK D3210P FOR EMERGENCY LI GHTS AT SEAT ROWS 30CG TO 40CG. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011700074 20080117 00074 WP 2008 1 17 AALA20072525 1 20071226 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 466AA 49596 TPA - EMERGENCY AISLE LIGHT AT SEAT 12D INOPERATIVE. SECURED CONNECTOR PIN AT SEAT 12F FOR INOPERATIVE EMERGENCY AISLE LIGHT AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011700075 20080117 00075 WP 2008 1 17 AALA20072529 1 20071226 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 553AA 53083 LGA - EMERGENCY LIGHTS AT FIRST CLASS GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS GAL LEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011700076 20080117 00076 WP 2008 1 17 AALA20072531 1 20071227 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 560AA 53090 LGA - EMERGENCY LIGHTS AT OVERHEAD MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD MID CA BIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011700077 20080117 00077 NM 2008 1 17 AALA20072533 1 20071212 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 682AA 25339 DFW - EMERGENCY LIGHT AT EXTERNAL LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT EXTERNAL LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008011700078 20080117 00078 WP 2008 1 17 AALA20072532 1 20071227 A 2170 WATER SEPARATOR DOUG DC9 DC982 3022082 WP AIR CONDITIONING INOPERATIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 449AA 49475 STL INFLIGHT T449/27DEC - SMOKE IN AFT CABIN DURING CLIMB. RETURNED TO STL AND LANDED WITHOUT INCIDENT. REPLACED LEFT AND RIGHT WATER SEPARATORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011700079 20080117 00079 NM 2008 1 17 AALA20072535 1 20071228 A 2611 644501 CIRCUIT CARD BOEING 767 767323 1385205 NM FIRE DETECTOR INOPERATIVE A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 351AA 24032 CDG INFLIGHT T065/28DEC ZRH TO JFK - FIRE OVERHEAT SYSTEM WARNING FAILED. NUMBER TWO ENGINE FIRE DETECTION LOOP 2 PREVI OUSLY PLACARDED. CREW UNABLE TO RESET. LANDED CDG WITHOUT INCIDENT. REPLACED FIRE DETECTOR SYSTEM CARD 644501 AND TEM P CONTROL CARD 285T0094-6 AS PRECAUTIONARY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008011700080 20080117 00080 NM 2008 1 17 AALA20072534 1 20071212 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 682AA 25339 DFW - EMERGENCY LIGHT AT SEAT ROW 12ABC INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 12ABC. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008011800041 20080118 00041 SO 2008 1 18 LR7A07139 1 20071219 A 5322 3313868 TENSION TIE LKHEED 382 382G 526414U SO FS477 RBL63 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HC5302 FOUND CRACKED RT TENSION TIE FITTING AT FS 477, RBL63. REPAIR ACCOMPLIS HED BY REPLACING TENSION TIE FITTING P/N 3313868 IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008011800086 20080118 00086 WP 2008 1 18 AALA20072546 1 20071229 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISLODGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 LGA - EMERGENCY LIGHTS AT AFT VENTRAL STAIRS SIDE WALL INOPERATIVE. SECURED BATTERY IN CHARGER FOR EMERGENCY LIGHTS AT AFT VENTRAL STAIRS SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011800108 20080118 00108 WP 2008 1 18 AALA20072569 1 20071231 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG DISCHARGED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 14551 53033 ORD INFLIGHT T1447/21DEC - AFTER TAKEOFF, NOSE LANDING GEAR WOULD NOT RETRACT. RETURNED TO ORD AND LANDED WITHOUT INCID ENT. FOUND STRUT FLAT. PERFORMED STRUT REPACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008012200012 20080122 00012 EA 2008 1 22 A6WA200740657 1 20071208 A 2750 865D1007 DRIVE UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS MALFUNCTIONED A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 458AW 10077 7861 FLAP FAIL CAUTION MESSAGE INFLIGHT. LANDED WITH FLAPS AT 8 DEGREES. LANDING WEIGHT 40,300 LBS. SPEED 150 KNOTS VERTIC AL SPEED LESS THAN 400 FT MINUTE MAX BTMS READING =3. REMOVED AND REPLACED FLAPS POWER DRIVE UNIT IAW AMM 27-52-01. PE RFORMED OPS CHECK IAW AMM 27-54-00, OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200018 20080122 00018 NM 2008 1 22 USAA920080053 1 20071218 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 22198 PIT - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION ON INTERCOSTAL UPPER CHORD, BS 1661 - BS 1681, RBL 9.2. REPLACED INTER COSTAL UPPER CHORD, BS 1661 - BS 1681, RBL 9.2 IAW B757 SRM 53-60-61. 2 L 7 2 4F RT A2NM 2008012200026 20080122 00026 EA 2008 1 22 A6WA200740666 1 20071115 A 5320 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 427ZW 7685 RT MLG WHEEL WELL, AFT HYD SUPPORT BRACKET IS CRACKED. RT MLG WHEEL WELL AFT HYD SUPPORT BRACKET REPLACED IAW CRJ 200, SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200028 20080122 00028 EA 2008 1 22 A6WA200740650 1 20071127 A 2913 887055 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE HYDRAULIC SYS INOPERATIVE A A6WA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 GL 31 434AW 16429 7322 HYD NR 1 LOW PRESS CAUTION MESSAGE IN FLIGH, HYD 1 QUANTITY READ ZERO FOR 35 MINUTES. PERFORMED PRECAUTIONARY SHUTDOWN OF NR 1 ENGINE AFTER LANDING. FOUND NR 1 SUCTION LINE CHAFED THROUGH AND PRESSURE FLEX PERMASWEDGE REPAIR, REMOVED AND REPLACED PRESSURE LINE REF AMM 29-11-52, AND REMOVED AND REPLACED EDP. LINES LEAK CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200030 20080122 00030 EA 2008 1 22 A6WA200740638 1 20071121 A 7797 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE N2 INDICATOR DIRTY A A6WA O OTHER N FALSE WARNING CR CRUISE 1 GL 31 463AW 7878 INFLIGHT, RT N2 GAUGE READS ZERO APPROXIMATELY 30 MINUTES INTO FLIGHT. CLEANED BLUE HARNESS CONNECTOR W8P2 AT RT ALTERN ATOR IAW 73-21-13 AND AWAC SUPP 06-003, OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200031 20080122 00031 NM 2008 1 22 USAA920080119 1 20071228 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 22198 PIT - MAJOR REPAIR - C4 CHECK, R2 DOOR CUTOUT INTERCOSTAL CRACKED, BS 680. REPLACED R2 DOOR CUTOUT INTERCOSTAL CRACKED, BS 680 IAW USAIRWAYS EO 5304R143. 2 L 7 2 4F RT A2NM 2008012200034 20080122 00034 NM 2008 1 22 USAA920080120 1 20071226 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 22198 PIT - MAJOR REPAIR - C4 CHECK, CRACKED FLOORBEAM, BS 1320 - BS 1340, BL 0. REPAIRED FLOORBEAM, BS 1320 - BS 1340, BL 0 IAW B757 SRM 53-00-51. 2 L 7 2 4F RT A2NM 2008012200037 20080122 00037 EA 2008 1 22 A6WA200740664 1 20071119 A 5720 HINGE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 427ZW 7685 RT SIDE BUTE DOOR 694JB PIANO HINGE CRACKED. HINGE REPLACED ON BUTE DOOR 694JB IAW CRJ 200, SRM 51-42-06 AND PAINTED IA W CRJ 200, SRM 51-25-01. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200038 20080122 00038 NM 2008 1 22 USAA920080134 1 20071227 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 22198 PIT - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION ON FLOORBEAM, BS 377, LBL 12. REPAIRED FLOORBEAM, BS 377, LBL 12 IAW U SAIRWAYS TYPICAL REPAIR 53-15-01. 2 L 7 2 4F RT A2NM 2008012200047 20080122 00047 EA 2008 1 22 A6WA200740631 1 20071117 A 5280 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT MLG DOOR GOUGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 470ZW 7927 RT MLG DOOR L/E INNER SKIN GOUGE RT MLG DOOR REPAIRED IAW REO 601R-52-82-034. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200048 20080122 00048 NM 2008 1 22 USAA920080137 1 20071227 A 5320 FLOOR SUPPORT BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 22198 PIT - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION ON FLOOR SUPPORT, BS 1260 - BS 1300, LBL 21, WL 208. REPLACED FLOOR S UPPORT, BS 1260 - BS 1300, LBL 21, WL 208 IAW B757 SRM 53-00-04. 2 L 7 2 4F RT A2NM 2008012200053 20080122 00053 EA 2008 1 22 A6WA200740703 1 20071216 A 2421 755469E IDG CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NR 2 INOPERATIVE A A6WA C ABORTED TAKEOFF H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 GL 31 419AW 7633 ON T/O ROLL RECEIVED (IDG 2) CAUTION MESSAGE FOLLOWED BY (GEN 2 OFF) CAUTION MESSAGE. ABORTED T/O AT APPROXIMATELY 70 K NOTS, MAX BTMS READINGS = 3,3,2,3. FOUND FAULT MESSAGE CHANGED AFTER IDG WAS PREVIOUSLY CHANGED FROM (NR 2 GEN OFF) MESS AGE TO (IDG 2) MESSAGE. RT GEN TO PYLON HARNESS CONTINUITY CHECK GOOD. RT GEN WAS LOW ON OIL, TOOK 24 PUMPS. FOUND SH AFT SEAL DAMAGED. REPLACED IDG IAW CHAP 24. LEAK AND OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008011600367 20080116 00367 WP 2008 1 16 AALA20072508 1 20071222 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 291AA 49303 LGA - EMERGENCY LIGHT AT SEAT 29D LENS BROKEN. REPLACED LENS ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 29D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011600368 20080116 00368 NM 2008 1 16 AALA20072490 1 20071221 A 3397 WIRE HARNESS BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 905AN 29507 DFW - EMERGENCY LIGHTS AT SEAT ROWS 22D TO 28D INOPERATIVE. REPLACED HARNESS AT SEAT ROW 26D FOR EMERGENCY LIGHTS AT SE AT ROWS 22D TO 28D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008011600370 20080116 00370 NM 2008 1 16 AALA20072492 1 20071221 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 751AN 30798 DFW - EMERGENCY LIGHT AT SEAT 20G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011600373 20080116 00373 WP 2008 1 16 AALA20072496 1 20071221 A 3350 0201720003 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 433AA 49451 LGA - EMERGENCY LIGHTS AT SEAT ROWS 5 TO 20 INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 19DEF FOR INOPERATIVE EMERGENC Y LIGHTS AT SEAT ROWS 5 TO 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008011600374 20080116 00374 NM 2008 1 16 AALA20072502 1 20071222 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 MIA - EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. RESEATED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RIG HT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011600376 20080116 00376 NM 2008 1 16 AALA20072504 1 20071222 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 778AN 29587 MIA - EMERGENCY LIGHT AT SEAT 23G LENS BROKEN. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011600378 20080116 00378 WP 2008 1 16 AALA20072506 1 20071222 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISLODGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 291AA 49303 LGA - EMERGENCY LIGHT AT EXTERIOR RIGHT INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY LIGHT AT EXTERIOR RIGHT. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008011600391 20080116 00391 EU 2008 1 16 COEA0743821 1 20070817 A 5543 S2728175600400 SUPPORT AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE RUDDER TRIM TAB CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 29796 253 FOUND DURING HEAVY CHECK. LEVEL 2 CORROSION ON TRIM TAB BELL CRANK SUPPORT. REPLACED BELL CRANK SUPPORT. WO 72242 NR 200082. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011700013 20080117 00013 CE 2008 1 17 DXTA200702723 1 20071230 A 2130 UNKNOWN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE CABIN PRESSURE UNKNOWN E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 335QS 5600335 ACFT DID NOT PRESSURIZE ON DEPARTURE. GROUND RAN AIRCRAFT CK LEFT AND RIGHT ENGINE SEPARATELY FOR PRESSURIZATION. OPS C K GOOD. CHECK PRE PRESS. OP'S CK GOOD. INSPECTED AND OP'S CK WOW SWITCH OP'S CK GOOD. NO DEFECTS NOTED ON GROUND IAW CES SNA 560 MM CH 21-31-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2008011700023 20080117 00023 CE 2008 1 17 DXTA200702730 1 20071227 A 2750 FLAP SYSTEM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 07 929QS 7500129 WHEN FLAPS SELECTED FOR 15 TO 35. FAILED AROUND 20 DEGREES. DID NOT RESET BUT EVENTUALLY CAME BACK TO FLAPS 15 DEGREES. FLAPS CAME TO 0 DEGREES ON GROUND, FLAP MOVEMENT WAS ABNORMALLY SLOW. FOUND NR 3 FLAP BINDING COMPLIED WITH MECHANICAL AND ELECTRICAL RIG IAW 750 MM 27-50-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008011700024 20080117 00024 CE 2008 1 17 DXTA200702732 1 20071231 A 2750 99146152 DRIVE UNIT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS INOPERATIVE E DXTA A UNSCHED LANDING F FLT CONT AFFECTED LD LANDING 1 GL 07 950QS 8196 7500050 WHEN SELECTING FLAPS TO 5 DEGREES, (FLAP FAIL) CAS MSG CAME ON. TROUBLESHOT TO BAD PDU CLUTCH. REMOVED, REPLACED AND OP S CHECK GOOD OF PDU IAW 750 MM 27-52-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008011800031 20080118 00031 SO 2008 1 18 LR7A07129 1 20071219 A 5340 3530597 FITTING LKHEED 382 382G 526414U SO BS 990 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HC5302 FOUND AFT FUSELAGE INTERIOR RT BHD FTG CRACKED AT FWD SIDE FS990 WL260 R BL64. REPAIR ACCOMPLISHED BY REPLACING FWD FTG P/N 353059-7 & AFT FTG P/N 3317807-4 IAW SMP583 CH 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008011800042 20080118 00042 SO 2008 1 18 LR7A07140 1 20071219 A 5320 LS36423 WEB LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HC5211 FOUND INSIDE CARGO RAMP BASE PLATE, FWD WEB BUCKLED AND CRACKED AND 'T' ANGLE ALSO CRACKED AT RAMP STA 10, LBL10 TO RBL 10. REPAIR ACCOMPLISHED BY REPLACING 'T' ANGLE AND WEB IAW SMP583 CHAPT ER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008011800059 20080118 00059 SO 2008 1 18 LR7A07157 1 20071219 A 5412 BULKHEAD LKHEED 382 382G 526414U SO NR 4 NACELLE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HC7201 FOUND NR 4 ENG NACELLE FWD BULKHEAD RT OUTER CAP TEE CRACKED AT FS 410R PPWL10. REPAIR ACCOMPLISHED IAW LAC MEA 382-54-07-081. 2 H 7 4 4T A1SO 2008011800087 20080118 00087 NM 2008 1 18 AALA20072547 1 20071229 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 914AN 29515 MIA - EMERGENCY LIGHT AT LEFT FORWARD WING EXIT SIGN INOPERATIVE. RESET EMERGENCY LIGHTS AT LEFT FORWARD WING EXIT SIGN . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008011800090 20080118 00090 NM 2008 1 18 AALA20072553 1 20071229 A 3350 LIGHT BOEING 757 757223 1384957 NM SEAT 17D MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AA 24589 DFW - EMERGENCY LIGHT AT SEAT 17D MISSING LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 17D. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008011800091 20080118 00091 NM 2008 1 18 AALA20072554 1 20071229 A 3350 SHROUD BOEING 757 757223 1384957 NM SEAT 17D MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AA 24589 DFW - EMERGENCY LIGHT AT SEAT 17D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008011800092 20080118 00092 NM 2008 1 18 AALA20072570 1 20071231 A 3350 0201720001 LIGHT BOEING 767 767323 1385205 NM SEAT 36H INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 366AA 25193 JFK - EMERGENCY LIGHT AT SEAT 36H INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 36H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008011800093 20080118 00093 NM 2008 1 18 AALA20072574 1 20071231 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 388AA 27448 SFO - EMERGENCY LIGHT AT LEFT AFT CABIN INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT AT LEFT AFT CABIN. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008011800106 20080118 00106 NM 2008 1 18 AALA20072565 1 20071231 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754AN 30262 ORD - EMERGENCY LIGHTS AT AFT GALLEY FORWARD WALL INOPERATIVE. REPLACED BATTERY PACK M33409 FOR EMERGENCY LIGHT AT AFT GALLEY FORWARD WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008012200017 20080122 00017 NM 2008 1 22 USAA920080052 1 20071220 A 5210 INTERCOSTAL BOEING 757 757225 1384959 NM R2 DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 22198 PIT - MAJOR REPAIR - C4 CHECK, THE R2 DOOR HAS A CRACKED INTERCOSTAL, BS 660. REPLACED R2 DOOR INTERCOSTAL, BS 660 IAW USAIRWAYS EO 5304R143. 2 L 7 2 4F RT A2NM 2008012200033 20080122 00033 EA 2008 1 22 A6WA200740695 1 20071210 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 432AW 7257 CRACK FOUND ON AFT ATTACH ANGLE OF PAX DOOR (DRAG ANGLE). AFT ATTACH ANGLE OF PAX DOOR REPAIRED IAW REO 61R-52-11-513 R EV A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200059 20080122 00059 SO 2008 1 22 XGN2008F00000 2 20071207 A 8530 TISN712ACA CYLINDER HEAD BEECH 36 36BEECH 1151602 CE CONT O520 IO520BA 17032 SO ENGINE CRACKED E XGNA K NONE O OTHER IN INSP/MAINT 1 SW 05 1194A 993 E159 ENGINE CYLINDER HEAD CRACKED. (K) 1 L 7 1 3O 3 O 3A15 E5CE 2008012200092 20080122 00092 EA 2008 1 22 A6WA200740675 1 20071129 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BS 202 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 433AW 7289 CRACK FOUND ON T FWD PRESSURE BULKHEAD PARKING BRAKE CABLE HOLE APPROX .650 INCH LONG. FWD PRESSURE BULKHEAD AT FS 202. 00, LBL 23.71. REPAIRED IAW REO 601R-53-11-563. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200100 20080122 00100 SO 2008 1 22 GUUA12100701 1 20071210 A 5210 DOOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE MAIN PAX OUT OF ADJUST A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 283AS 120236 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED MAIN CABIN DOOR WILL NOT OPEN FROM THE OUTSIDE AND WILL CLOSE FROM THE I NSIDE OR OUTSIDE.ADJUSTED MAIN CABIN DOOR LOCKING CAMS. 2 L 7 2 4T 4 T RT A31SO E20NE 2008012200101 20080122 00101 2008 1 22 TRAX200800053 4 20071231 A 2360 BONDING STRAP CNDAIR CL600 CL6002B19 1900309 EA LT SPOILERON FRAYED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 880AS 7606 LEFT SPOILERON O/B BONDING STRAP FRAYED. E/C PERFORMED IAW NTM CRACK CONFIRMED IN X AXIS, END OF CRACK MARKED, NO CRAC K FOUND IN Y AXIS. PRC APPLY IAW REF. DO/TS-43/08-9701. COMPLIED WITH EC/TC DO/TS-43/08. 2 L 7 2 4F RT A21EA 2008012200113 20080122 00113 EA 2008 1 22 A6WA200740684 1 20071216 A 5210 CABLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE PAX DOOR INOPERATIVE A A6WA O OTHER O OTHER CL CLIMB 1 GL 31 412AW 7582 LOUD WHISTLING NOISE COMING FROM MAIN CABIN DOOR, LOUDEST JUST AFTER TAKEOFF. REMOVED AND REPLACED ICE BREAK CABLE IN P RESSURE RELIEF DOOR. REF AMM 52-11-15, OPS TEST GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200114 20080122 00114 EA 2008 1 22 A6WA200740688 1 20071210 A 5210 COVER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 432AW 7257 AFT UPPER CORNER COVER CRACK ON PAX DOOR. (K) AFT UPPER CORNER COVER REPLACED IAW SRM 51-42-13. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200122 20080122 00122 EA 2008 1 22 WAI2008F00000 1 20071213 A 5610 603303025 WINDSHIELD CNDAIR CL600 CL600* 1900302 EA LYC ALF502 ALF502* 41580 EA COCKPIT CRACKED E WAIA B EMER. DESCENT O OTHER CR CRUISE 1 SW 09 900LG 1233 1036 ON 28 NOV, 2007 AT 2100, ENROUTE AT FL 330, THE CAPTAIN NOTICED A CRACK IN THE EXTERIOR PANEL OF THE LT FWD WINDSHIELD. THE APPROPRIATE CHECKLIST WAS COMPLETED AND A SPEED REDUCTION AND DECENT REQUESTED. WHILE DESCENDING A LOUD (POP) AND SUBSEQUENT WHISTLING WAS HEARD. A FURTHER SPEED REDUCTION AND DESCENT WAS INITIATED. UPON LANDING, IT WAS DISCOVERED TH AT A PORTION OF THE OUTER WINDSHIELD HAD SEPARATED THE AIRCRAFT. IT IS UNKNOWN WHEN THE FIRST CRACK HAD OCCURRED. (K) 2 L 7 2 4F 4 F RT A21EA E6NE 2008012200127 20080122 00127 EA 2008 1 22 A6WA200740662 1 20071116 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 427ZW 7685 CRACK EXIST ON BRACKET OF INTERCOSTAL, FS 484, LBL 27, CRACK DIMENTION ON BRACKET , 1 INCH. BRACKET OF INTERCOSTAL AT F S 484, LBL 27 REPLACED IAW REO 601R-53-41-059. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200130 20080122 00130 EA 2008 1 22 A6WA200740661 1 20071116 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 427ZW 7685 CRACK EXIST ON INTERCOSTAL AND BRACKET FS 484, RBL 27 AND RBL 36 CRACK DIMENTION OF INTERCOSTAL 1 INCH AND BRACKET .500 INCH. INTERCOSTAL AT FS 484, RBL 36 REPAIRED IAW REO 601R-53-41-059 BRACKET AT FS 484, RBL 27, REPLACED IAW REO 601R-53 -41-059. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200134 20080122 00134 CE 2008 1 22 AMWA88594BC 1 20071115 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER DISCHARGED A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 142ZV 365 UE142 DURING FLIGHT, THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED. MAINTENANCE REPLACED BATTERY AND CLEARED DISCREPANCY. 2 L 7 2 4T 4 T RT A24CE E26NE 2008012200136 20080122 00136 CE 2008 1 22 AMWA88587BC 1 20071114 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER DISCHARGED A AMWA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CE 07 161YV 153 UE161 BATTERY CHARGE ANNUNCIATOR ILLUMINATED 3 TIMES. MAINTENANCE REPLACED BATTERY AND CLEARED DISCREPANCY. 2 L 7 2 4T 4 T RT A24CE E26NE 2008012200142 20080122 00142 EU 2008 1 22 1092008 1 20071222 A 5315 6070141 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A BUEA K NONE O OTHER IN INSP/MAINT 1 GL 23 320NP 6049 6 1494 SEAT TRACK Y-254 BETWEEN FR 20 TO FR 16 HAS 4 EACH AREAS OF CORROSION (AREA 1 1.5 INCH X .5) (AREA 2 .6 INCH X .5) (AREA 3 .5 INCH X .4) ( AREA4 1.5 INCH X .7) 2 L 7 2 4F 4 F RT A28NM E37NE 2008012200143 20080122 00143 CE 2008 1 22 20071227209 1 20071227 A 2720 6587C PRESSURE SWITCH BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE RUDDER CORRODED E I5WA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 05 209CM 5760 BB1613 DURING TAKEOFF ROLL THE RUDDER PEDALS KICKED HARD LT CAUSING LOSS OF DIRECTIONAL CONTROL. ABORTED TAKEOFF AND TAXIED TO RAMP. MX PERFORMED A RUDDER BOOST TEST AND NOTED DURING RUN-UP THAT THE RT ENGINE RUDDER BOOST DID NOT RESPOND. THE L T ENGINE RUN-UP CAUSED THE RUDDER BOOST TO ACTIVATE. REMOVED AND REPLACED RUDDER BOOST DIFFERENTIAL SWITCH MFG PN 658-7 C (P/N 101-384119-1) S/N OFF 4923 - S/N ON 6508. 1 L 7 2 4T 4 T A24CE E4EA 2008012200145 20080122 00145 EA 2008 1 22 A6WA200740685 1 20071210 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 432AW 7257 EDGE MEMBER CRACK ON PAX DOOR AT FOLDING STEP HINGE. (K) PAX DOOR EDGE MEMBER FABRICATED IAW SRM 51-24-26 AND INSTALL I AW SRM 51-42-13. 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200146 20080122 00146 EA 2008 1 22 A6WA200740636 1 20071118 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS FAILED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 31 458AW 7861 AFTER TAKEOFF FLAPS FAILED AT 13 DEGREES OAT +6 DEGREES CELCIUS, WHEN FLAPS BEING RETRACTED FROM 20 DEGREES TO 8 DEGREES . RESET FLAPS IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4 FLAPS RESET, AIRCRAFT RELEASED FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200154 20080122 00154 EA 2008 1 22 A6WA200740680 1 20071216 A 3210 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LEFT COLLAPSED A A6WA O OTHER O OTHER LD LANDING 1 GL 31 470ZW 7927 UPON LANDING, LT MLG COLLAPSED; AIRCRAFT DEPARTED RUNWAY TO THE LT SIDE, CVR AND FDR CIRCUIT BREAKERS HAVE BEEN PULLED, NO FIRE INDICATIONS RECEIVED. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200155 20080122 00155 EA 2008 1 22 A6WA200740681 1 20071216 A 3010 434419882 THERMAL SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT WING INOPERATIVE A A6WA O OTHER J WARNING INDICATION CL CLIMB 1 GL 31 410AW 7490 WING OVERHEAT WARNING MESSAGE ON CLIMBOUT SYNOPTIC PAGE SHOWS LT WING. COMPLIED WITH QRH, MESSAGE CLEARED. IN OFF, AND APPROXIMATELY 1 MINUTE LATER, REAPPEARED IN STANDBY. REMOVED AND REPLACED LT WING STANDBY THERMAL SWITCH IAW AMM 30, O PS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200156 20080122 00156 NM 2008 1 22 07122101 1 20071221 A 2910 A511506K0140 LINE BOEING 757 757231 1384950 NM PWA 2037 PW2040 NE LT HYD SYSTEM LOOSE A BEFA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 19 741PA 24737 DISCREPANCY LP 003727, ITEM 1: LT HYD QUANTITY FELL TO 0.01 SHORTLY AFTER TO PTC PRESS NORMAL. LP 003727, ITEM 1: AFTER INSPECTION FOUND LOOSE HYDRAULIC LINE. TIGHTEN B-NUT SERVICE HYD SYSTEM OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012200157 20080122 00157 NM 2008 1 22 07122102 1 20071221 A 2910 A511506K0140 FITTING BOEING 757 757231 1384950 NM PWA 2037 PW2040 NE LT HYD SYSTEM LOOSE A BEFA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 19 741PA 24737 LP 003727, ITEM 1: LT HYD QUANTITY FELL TO 0.01 SHORTLY AFTER T/O PTC PRESS NORMAL. LP 003727, ITEM 1: AFTER INSPECTION FOUND LOOSE HYDRAULIC LINE. TIGHTEN B-NUT SERVICE HYD SYSTEM OPS CHECK NORMAL 2 L 7 2 4F 4 F RT A2NM E17NE 2008012200173 20080122 00173 EU 2008 1 22 COEA0761821 1 20070824 A 5730 S57112425202 SKIN AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE LT WING CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. MAJOR REPAIR: LEVEL 2 CORROSION AND FRETTING DAMAGE ON LT WING, UPPER WING PLANK. DAMAGE IS LOCATED AT ACCESS DOOR 522CT HOUSING AT DOOR CUTOUT. BLENDED OUT DAMAGE AND REWORKED DOOR STIFFENER IAW SRAS DO/TS 4811 /07..4338 AND NOTE DOT/TS 5605/07. WO 72242, NR 601008. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008012200174 20080122 00174 CE 2008 1 22 7AA2008F00000 1 20071213 A 5510 AN56A BOLT CESSNA 310 310R 2074245 CE CONT O520 IO520* 17032 SO HORIZONTAL STAB SHEARED E 7AAA K NONE O OTHER IN INSP/MAINT 1 EA 07 310SA 310R1565 WHILE PREPARING AIRCRAFT FOR HORIZONTAL STABILIZER REMOVAL, THE 4 BOLTS THAT ATTACH THE HORIZONTAL STABILIZER TO THE AFT FUSELAGE ALL SHEARED WITH MINIMAL EFFORT WHEN THEY WERE BEING REMOVED. THERE ARE STANDARD AIRCRAFT BOLTS, AN5-6A. (K) 1 L 7 2 3O 3 O 3A10 E5CE 2008012200179 20080122 00179 EA 2008 1 22 A6WA200740693 1 20071213 A 5340 NUT CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 432AW 7257 FS 484.0 RT SIDE, CLIP FOUND CRACKED ON FLOOR SUPPORT STRUCTURE AT RBL 27.0, FS 484.00, RBL 27.00, FLOOR SUPPORT CLIP RE PLACED IAW SRM 51-42-16, 51-21-16 AND SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200182 20080122 00182 EU 2008 1 22 COEA0749821 1 20070829 A 5714 SPAR AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE CENTER WING CHAFED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 29796 253 FOUND DURING HEAVY CHECK. MAJOR REPAIR, LEVEL 2 CORROSION ON CENTER WING BOX FRONT AND REAR SPAR UPPER EXTRUSION. CHAF ES, BETWEEN RIBS 4L AND 4R. CORROSION ON AFT SPAR EXTRUSIONS IN SAME AREAS AS CHAFES. BLENDED CHAFES AND CORROSION IAW SRAS DS/ET 603.600/98...1690, NOTE DO/ TS-4936/ 07. WO 72242, NR 200080. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008012200192 20080122 00192 EA 2008 1 22 A6WA200740706 1 20071226 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE SMOKE A A6WA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 31 466AW 7899 TOILET SMOKE CAS MESSAGE IN FLIGHT, COMPIED WITH QRH SMOKE VISIBLE IN COCKPIT, ELECTRICAL SMOKE ODOR IN LAV, SMOKE SUBSI DED WHEN QRH COMPLIED WITH. CORRECTIVE ACTION IN PROGRESS. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200199 20080122 00199 EA 2008 1 22 A6WA200740682 1 20071216 A 2150 FILTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT A/C PACK INOPERATIVE A A6WA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 453AW 7838 RT PACK HIGH PRESS CAUTION MESSAGE ON TAKEOFF ROLL, ABORTED TAKEOFF AT APPROXIMATELY 20 KNOTS, BTMS READINGS=2,2,1,2. R EMOVED AND REPLACED RT ENGINE PRESSURE REGULATING SHUTOFF VALVE FILTER, REF AMM 21-51-43 AND AWAC SUPPLEMENT 06-039. (K ) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200217 20080122 00217 SO 2008 1 22 LR7A07162 1 20071219 A 5714 RIB LKHEED 382 382G 526414U SO FS 517 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HSP57119 FOUND RT CENTER WING BULKHEAD FOOT RIB CAP CRACKED AT FS 517, CWS140R, WL256. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-075. 2 H 7 4 4T A1SO 2008012200218 20080122 00218 SO 2008 1 22 LR7A07163 1 20071219 A 5714 1 RIB LKHEED 382 382G 526414U SO FS 517 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HSP57119 FOUND RT CENTER WING BULKHEAD FOOT RIB CAP CRACKED AT FS 517, CWS140R, WL256. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-075. 2 H 7 4 4T A1SO 2008012200219 20080122 00219 SO 2008 1 22 LR7A07164 1 20071219 A 5714 RIB LKHEED 382 382G 526414U SO FS 517 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HSP57119 FOUND RT CENTER WING BULKHEAD FOOT RIB CAP CRACKED AT FS 517, CWS140R, WL285. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-079. 2 H 7 4 4T A1SO 2008012200220 20080122 00220 SO 2008 1 22 LR7A07165 1 20071219 A 5714 RIB LKHEED 382 382G 526414U SO FS 597 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HSP57119 FOUND RT CENTER WING BULKHEAD FOOT RIB CAP CRACKED AT FS 597, CWS140R, WL256. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-075. 2 H 7 4 4T A1SO 2008012200223 20080122 00223 SO 2008 1 22 LR7A07168 1 20071219 A 5730 PANEL LKHEED 382 382G 526414U SO CENTER WING CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2 FOUND CORROSION LT CTR WING BOTTOM AFT PANEL AT CWS178-208L BETWEEN STRIN GERS 21 TO 24. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-082. 2 H 7 4 4T A1SO 2008012200224 20080122 00224 SO 2008 1 22 LR7A07169 1 20071219 A 5730 PANEL LKHEED 382 382G 526414U SO CENTER WING CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2 FOUND RT LOWER CENTER WING PANEL CORROSION AT CWS190-208R STRINGERS 15-16 . REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-083. 2 H 7 4 4T A1SO 2008012200225 20080122 00225 NM 2008 1 22 AALA20072581 1 20071119 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 977AN 29550 TUL - EMERGENCY LIGHT BATTERY PACK IN AFT CABIN AT STATION 952 FAILED TEST. REPLACED BATTERY PACK M1672 FOR EMERGENCY L IGHTS IN AFT CABIN AT STATION 952. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008012200226 20080122 00226 SO 2008 1 22 LR7A07170 1 20071219 A 5714 RIB LKHEED 382 382G 526414U SO CENTER WING CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2, FOUND CENTER WING LOWER RIB CAP CRACKED AT CWS61R, STGR 24. REPAIR ACCO MPLISHED IAW LAC MEA 382-57-07-085. 2 H 7 4 4T A1SO 2008012200227 20080122 00227 SO 2008 1 22 LR7A07171 1 20071219 A 5741 RIB LKHEED 382 382G 526414U SO CENTER WING CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER SB382-57-85-R2 FOUND CENTER WING LOWER RIB CRACKED AT CWS61L STGR 23-24. REPAIR ACCOMPL ISHED IAW LAC MEA 382-57-07-077. 2 H 7 4 4T A1SO 2008012200230 20080122 00230 SO 2008 1 22 LR7A07173 1 20071219 A 5714 BEAM LKHEED 382 382G 526414U SO FS 517 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2, FOUND BEAM CAP HOLE CRACK COMMON TO WING ATTACH ANGLE AT FS 517, CWS61R, WL256. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-076. 2 H 7 4 4T A1SO 2008012200241 20080122 00241 NM 2008 1 22 AALA20072583 1 20071206 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 942AN 30084 TUL - EMERGENCY LIGHT BATTERY PACK AT RIGHT FORWARD WING EXIT DOOR FAILED TEST. REPLACED BATTERY PACK AT STATION 565 F OR EMERGENCY LIGHTS AT RIGHT FORWARD WING EXIT DOOR CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008012200242 20080122 00242 NM 2008 1 22 AALA20072578 1 20071216 A 3350 CM1317 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 943AN 30599 TUL - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 10ABC INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROW 10 ABC. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008012200243 20080122 00243 NM 2008 1 22 AALA20072584 1 20071206 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 942AN 30084 TUL - EMERGENCY LIGHT BATTERY PACK FOR RIGHT MID TO AFT CABIN FAILED TEST. REPLACED BATTERY PACK AT STATION 727 FOR EME RGENCY LIGHTS IN RIGHT HAND MID TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008011800040 20080118 00040 SO 2008 1 18 LR7A07138 1 20071219 A 5310 388997112 BEAM LKHEED 382 382G 526414U SO FS 577 CHAFED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HC3213 FOUND LT MLG BEAM/INTERCOSTAL CAP CHAFING MARKS AT FS577/588. REPAIR AC COMPLISHED BY REPLACING TRACKS R/N 388997-1 AND -12 IAW SMP583 CHAPTER 51-660 AND 51-70. 2 H 7 4 4T A1SO 2008011800045 20080118 00045 SO 2008 1 18 LR7A07143 1 20071219 A 7120 3706561L1R ATTACH FITTING LKHEED 382 382G 526414U SO ENGINE MOUNT DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, WHILE PERFORMING SCHEDULED TRUSS MOUNT CHANGE FOUND ENG NR 2 OBD TRUSS MOUNT RIB CAP ATTACH FTGS (INBD AND OBD), BOLT HOLES BEYOND LIMITS. REPAIR ACCOMPLISHED BY REPLACING FITTINGS P/N 370656-1L AND 370656-1R IA W SMP583 CHAP 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008011800055 20080118 00055 SO 2008 1 18 LR7A07153 1 20071219 A 5711 SPAR CAP LKHEED 382 382G 526414U SO CENTER WING CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2 FOUND RT LOWER FWD SPAR CAP EYEBOLT HOLE CRACKED AT FS 517, CWS176R, WL25 7. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-076. 2 H 7 4 4T A1SO 2008011800061 20080118 00061 SO 2008 1 18 LR7A07159 1 20071219 A 5712 RIB LKHEED 382 382G 526414U SO CENTER WING CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HSP57119 FOUND LT CENTER WING BULKHEAD FOOT RIB CAP CRACKED AT FS 517, CWS140L, WL285. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-079. 2 H 7 4 4T A1SO 2008011800074 20080118 00074 EA 2008 1 18 SWIA200719050 1 20070910 A 5320 STIFFENER CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 742SK 10197 STIFFENER CRACKED AT FS 280.0 AND RBL26.0, FOUND AT C-CHECK. INSTALLED REPAIR PARTS AT RBL 26.0 IAW CRJ700 SRM 51-42-06 . 2 L 7 2 4F RT A21EA 2008011800080 20080118 00080 EA 2008 1 18 SWIA200719056 1 20070910 A 5210 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 975SW 7951 PAX DOOR INTERCOSTAL IS CRACKED, FOUND AT C-CHECK. INSTALLED INTERCOSTAL PER SRM 51-42-06 AND 51-42-21. 2 L 7 2 4F RT A21EA 2008011800094 20080118 00094 NM 2008 1 18 AALA20072548 1 20071229 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 914AN 29515 MIA - EMERGENCY LIGHTS AT SEAT ROWS 12D AND 14D INOPERATIVE. RESET EMERGENCY LIGHTS AT SEAT ROWS 12D AND 14D. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008011800122 20080118 00122 EU 2008 1 18 NWAA074373308 1 20071206 A 5712 RIB AIRBUS A330 A330223 3940031 EU RT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 808NW 591 DURING INSPECTION PER AD 2006-22-14, FOUND CRACKS IN RT WING RIB NR 6. REPAIRED PER EA 33-208521. 2 L 7 2 4F RT A46NM 2008012200288 20080122 00288 NM 2008 1 22 2007UALA05056 1 20071211 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY LIGHTS INOP. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012200292 20080122 00292 NM 2008 1 22 2007UALA05303 1 20071226 A 2701 CONTROL COLUMN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 WP 29 506UA 24627 CAPTAIN'S ELEVATOR CONTROLS FEEL HEAVY. CREW COMMENTS: VERY HEAVY ELEVATOR AT TAKEOFF ROTATION. GW AT T/O WAS 236.0, VR WAS 158KTS. TRIM 4.6 ANU. FORCE MEASURMENT FOR AILERON WHEEL TRAVEL RT 26 LBS AND LT 27 LBS REF AMM 27-11-00. LIMI TS EXCEEDS MAX OF 21.5. CONTROL COLUMN TRAVEL WITH C & R HYD SYS ON READS 58 LBS. REF AMM 27-31-00. EXCEEDS MAX OF 55. A UTO LAND TESTS ACCOMPLISHED PER AMM 22-10-00-501. NO PREVIOUS AND PRESENT FAULTS NOTED. REF MOP-7-0-5-4. HAVE ACCOMPLIS HED EG CALLOUTS. REF PTT 102003-102012. NEW TEST FLT TO BE ACCOMPLISHED BY EG CREW. CHECKED AILERON FORCES IAW 27-11-00. TEST OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012200293 20080122 00293 NE 2008 1 22 2007UALA05371 2 20071229 A 7321 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE UNKNOWN A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 648UA 25285 NR 2 ENG 'ENG EEC C1' MESSAGE APPEARED ON EICAS. ENGINE OPERATION ABNORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012200294 20080122 00294 NM 2008 1 22 2007UALA05386 1 20071230 A 3200 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE UNKNOWN A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 594UA 28145 ACFT MIGRATED FROM PAVED TAXIWAY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012200296 20080122 00296 NM 2008 1 22 2007UALA04915 1 20071201 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 FUSELAGE FRAME OUT OF LIMITS AT BS 740 STR 27L. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012200297 20080122 00297 2008 1 22 2007UALA05247 4 20071221 A 2565 HOSE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE COLLAPSED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 652UA 25390 RIGHT OVERWING SLIDE INFLATION HOSE COLLAPSED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012200298 20080122 00298 NM 2008 1 22 2007UALA05271 1 20071222 A 3500 CASE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE O2 SYSTEM CRACKED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 652UA 25390 SUPPLEMENTAL - O2 CASE CRACKED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012200317 20080122 00317 NM 2008 1 22 UPS08M51383 1 20071106 A 5712 RIB DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C RIGHT WING L/E CAVITY, L/E RIB LOWER END SUSPECT CRACK AT 6 INCHES I/B OF SLAT TRACK NR 3 AS MARKED. HFEC INSPECTION C/O AT I/B OF SLAT TRACK NR 3, FOUND CRACK AS MARKED APPROX 1 INCH LENGTH. RIGHT WING L/E CAVITY, L/E L OWER RIB REMOVED PER SRM 51-31-01 VII R35. NEW RIB FAB PER BOEING DRW ARB3006. NEW RIB HEAT-TREATED, HOLES PICKED-UP, PROTECTED & PAINTED. NEW RIB INSTALLED PER SRM 51-31-0 1 VII R35. 2 L 7 3 4F RT A22WE 2008012200318 20080122 00318 NM 2008 1 22 UPS08M51384 1 20071106 A 5712 RIB DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C RIGHT WING L/E CAVITY, L/E RIB LOWER END SUSPECT CRACK AT 19 INCHES O/B OF SLAT TRACK NR 3 AS MARKED. HFEC INSP C/O ON O/B OF SLAT TRACK NR 3 FOUND CRACK OF APPROX 1.5 INCH LENGTH. RIGHT WING L/E CAVITY L/E RIB LOWER REM OVED PER SRM 51-31-01 VII R35. NEW RIB FAB PER BOEING DRW ARB1161. RIB HEAT-TREATED, HOLES PICKED-UP, PROTECTED & PAIN TED. NEW RIB INSTALLED PER SRM 51-31-01 VII R35. 2 L 7 3 4F RT A22WE 2008012200319 20080122 00319 NM 2008 1 22 UPS08M51385 1 20071027 A 5712 RIB DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C LEFT WING L/E SLAT TRACK NR 16, I/B RIB FOUND CRACKED AS MARKED. LEFT WING NR 8 SLAT CABLE REMOVED. LEFT WING NR 16 SLAT TRACK DOOR, SLAT TRACK, BRACKET, PULLEY, ATTACHING HARDWARES & 04 EA BEARINGS REMOVED. LEFT WING L /E ELECT WIRING FROM WING TIP TO NR 15 SLAT TRACK REMOVED. LEFT WING L/E SLAT TRACK NR 16 I/ RIB REMOVED. NEW RIB INST ALLED. BEARING, BRACKET, PULLEY, ATTACH H/W, SLAT TRACK & DOOR INSTALLED. NR 8 SLAT CABLE INSTALLED. ELECT WIRING INS TALLED. OPS CHECK OK. 2 L 7 3 4F RT A22WE 2008012300010 20080123 00010 EA 2008 1 23 SWIA200719070 1 20070905 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BRAKE XDUCER CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 976SW 7952 LEFT WHEEL WELL BRAKE TRANSDUCER BRACKET IS CRACKED, FOUND AT C-CHECK. REPLACED LEFT WHEEL BRAKE PRESSURE TRANSDUCER BR ACKET IAW CRJ200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008012300011 20080123 00011 2008 1 23 2007UALA05341 4 20071228 A 2565 D5337047500160 CABLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EVAC SLIDE BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 815UA 867 RIGHT OVERWING EXIT INFLATION RESERVOIR CABLE BROKEN (INSIDE AFT PIT). REPLACED THE RESERVOIR ASSY, INCLUDING CABLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012300022 20080123 00022 EA 2008 1 23 SWIA200719072 1 20070905 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 976SW 7952 RIGHT SIDE FLOORBEAM ANGLE IS CRACKED AT STA 621, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 REO 601R-53-61-11 7 STEP 2, 5, AND 6. 2 L 7 2 4F RT A21EA 2008012300023 20080123 00023 EA 2008 1 23 SWIA200719073 1 20070905 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 976SW 7952 LEFT SIDE FLOORBEAM ANGLE ON OUTBOARD SIDE IS CRACKED AT STA 621, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 R EO 601R-53-61-117. 2 L 7 2 4F RT A21EA 2008012300045 20080123 00045 SO 2008 1 23 FDKA200706307 1 20070628 A 2750 FLAP SYSTEM EMB 145 EMB145LR 3260212 SO TE FLAPS MALFUNCTIONED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 850MJ 145568 FDM 5986 ATL (0914 PHX LCL) - FLAP LOW SPEED. MX RESET FLAP SYSTEM, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012300047 20080123 00047 SO 2008 1 23 FDKA200708379 1 20070810 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAI PAX LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM 6155 MCO (0636 PHX LCL) - PAX DOOR DIFFICULT TO CLOSE. MX LUBED DOOR, OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012300053 20080123 00053 2008 1 23 FDKA200710515 4 20071001 A 3421 501119720 INDICATOR EMB 145 EMB145LR 3260212 SO ATTITUDE UNKNOWN A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 827MJ 10012 145217 FDM 6036 ATL-ORF (1600 PHX LCL) - AILERON SYSTEM 2 INOP MESSAGE CYCLES ON AND OFF WITH HYDRAULIC PRESSURE OFF. MX REMOV ED AND REPLACED STANDBY ATTITUDE INDICATOR AND AILERON SYSTEM 2 MANIFOLD OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012300064 20080123 00064 SO 2008 1 23 FDKA200710562 1 20071021 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 145416 FDM 6008 JFK (0426 PHX LCL) - MAIN CABIN DOOR HARD TO CLOSE. MX LUBED DOOR, OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012300065 20080123 00065 SO 2008 1 23 FDKA200710518 1 20071003 A 2760 14533022409 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO SPOILERS MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 825MJ 11679 145179 FDM 6041 JFK (1554 PHX LCL) - SPOILER FAIL CAUTION MESSAGE IN FLIGHT. MX REMOVED AND REPLACED LT O/B SPOILER PROX SWITC H. 2 L 7 2 4T RT T00011AT 2008012300113 20080123 00113 NM 2008 1 23 DLM90080038 1 20071228 A 5340 SUPPORT FITTING DOUG MD90 MD9030 3023690 NM GIRT BAR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 L-2 DOORWAY GIRT BAR FITTING SUPPORTS, FWD AND AFT CORRODED. REMOVED AND REPLACED FWD FITTING IAW SRM 51-30-05. AFT FI TTING FOUND TO BE IN LIMITS IAW MD90 SRM 53-00-01 FIG 3. 2 L 7 2 4F RT A6WE 20080918 NM 2008 9 18 2008UALA04372 1 20070822 A 5311 FRAME BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BS 460 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA 25158 FOUND CIRC FRAME ABOVE DOORS 1L & 1R, BS 460 STR 14-STR 15 HAS SHORT EDGE MARGIN FOR FASTENER INSTALLATION FOR EXTERNAL DOUBLER. *S/D* MAJOR REPAIR ACCOMPLISHED: MANUFACTURED & INSTALLED STRAPS FWD AND AFT OF FRAMES AT BS 460. ALSO MANU FACTURED & INSTALLED FILLERS FWD AND AFT OF BS 460. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012200001 20080122 00001 NM 2008 1 22 USAA920080131 1 20071222 A 5320 141N515054 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - CRACKED INTERCOSTAL WEB, BS 395 - BS 418, RBL 45, WL 208. REPLACED INTERCOSTAL WEB, BS 395 - BS 418, RBL 45, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008012200004 20080122 00004 NM 2008 1 22 USAA920080111 1 20071210 A 5315 141N51213 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON FLOORBEAM, BS 345, LBL 58 - RBL 58. REPAIRED FLOORBEAM, BS 345, LB L 58 - RBL 58 IAW USAIRWAYS TYPICAL REPAIR 53-15-01. 2 L 7 2 4F RT A2NM 2008012200016 20080122 00016 EA 2008 1 22 TRAX200800009 1 20071220 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 AAR - LEFT PRESSURE BULKHEAD AT FS 202.75 CRACKED WHERE BRAKE ROD GOES THRU BULKHEAD (FLAGGED) THRU NOSE HYDRAULIC COMP. COMPLIED WITH ASA ECTC EO 600-53-217, NO DEFECTS NOTED. REQUIRES OPS AND LEAK CHECK, REFER TO 409A FOR OPS AND LEAK C HECKS (NO FURTHER ACTION REQUIRED). 2 L 7 2 4F RT A21EA 2008012200019 20080122 00019 EA 2008 1 22 A6WA200740674 1 20071206 A 5344 HINGE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 433AW 7289 PAX DOOR UPPER FOLDING STEP, LOWER HINGE IS CRACKED. PAX DOOR UPPER FOLDING STEP, LOWER HINGE REPLACED IAW SRM 51-41-00 . (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200020 20080122 00020 NM 2008 1 22 USAA920080054 1 20071219 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 22198 PIT - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION ON FLOORBEAM, BS 1661, BL 0 - LBL 58.22. REPAIRED FLOORBEAM, BS 1661, BL 0 - LBL 58.22 IAW B757 SRM 53-00-51 REPAIR 5. 2 L 7 2 4F RT A2NM 2008012200023 20080122 00023 EA 2008 1 22 A6WA200740701 1 20071218 A 5240 PLATE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE SERVICE DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 432AW 7257 SERVICE DOOR PLATE FIND CORRODED, OUT OF LIMITS IAW SRM 53-00-00, FIG 101. SERVICE DOOR PLATE REPLACED IAW SRM 51-42-00 , 51-41-02, 51-41-04. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200024 20080122 00024 EA 2008 1 22 A6WA200740642 1 20071116 A 4980 EXHAUST DUCT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE APU CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 427ZW 7685 APU EXHAUST LIPS CRACKED AT 5 O`CLOCK AND 6 O`CLOCK. APU EXHAUST REPLACED IAW AMM 49-81-01-400-801. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200025 20080122 00025 EA 2008 1 22 A6WA200740660 1 20071115 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FS 625 S14L CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 427ZW 7685 CRACK EXIST ON BRACKET FS 625, LT STR 14L. BRACKET AT FS 625, STR 14L REPLACED IAW, SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200065 20080122 00065 EA 2008 1 22 A6WA200740659 1 20071116 A 4900 INTAKE DUCT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE APU CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 427ZW 7685 APU INTAKE DUCT CRACKED. APU INTAKE DUCT REPLACED IAW AMM. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200085 20080122 00085 EA 2008 1 22 A6WA200740673 1 20071130 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 433AW 7289 PAX DOOR STAIR ASSY, AFT DRAG ANGLE IS CRACKED. REPAIRED IAW CRJ200, REO 601R-52-11-513 REV (A). (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200086 20080122 00086 EA 2008 1 22 A6WA200740702 1 20071218 A 3150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS ILLUMINATED A A6WA O OTHER J WARNING INDICATION AP APPROACH 1 GL 31 464AW 7890 FLAPS FAIL MESSAGE ON APPROACH, FAILED AT 20 DEGREES WHEN SELECTING 30 DEGREES. RESET IAW SUPPLEMENT 98-018B. OPS CHEC K NORMAL. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200087 20080122 00087 EA 2008 1 22 A6WA200740686 1 20071210 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE PAX DOOR GOUGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 432AW 7257 FWD PAX DOOR PULL IN LEVEL GOUGED PULL IN LEVEL GOUGED .070 INCH AND ALLOWABLE MAXIMUM .050 INCH IAW REO 601R-52-11-524. (K) FWD PAX DOOR PULL IN LEVER REPAIRED IAW REO 601R-52-11-524. 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200099 20080122 00099 CE 2008 1 22 GUUA11270701 1 20071127 A 5220 DOOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE EMERGENCY EXIT INOPERATIVE A GUUA K NONE L NO TEST IN INSP/MAINT 1 SO 29 87554 UE227 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT AFT EMERGENCY EXIT DOOR WILL NOT OPEN FROM THE OUTSIDE. LUBRICATED D OOR HANDLE MECHANISIM. 2 L 7 2 4T 4 T RT A24CE E26NE 2008012200102 20080122 00102 SO 2008 1 22 GUUA12160702 1 20071216 A 5210 DOOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE MAIN PAX LACK OF LUBE A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 283AS 120236 FLIGHT: 9273, PILOT REPORTED MAIN CABIN DOOR WILL NOT OPEN FROM THE OUTSIDE. LUBRICATED MAIN CABIN DOOR. 2 L 7 2 4T 4 T RT A31SO E20NE 2008012200123 20080122 00123 SW 2008 1 22 EGI2008F00000 1 20071227 A 2700 2060010985 CONTROL TUBE BELL 206 206L3 1182108 SW ALLSN 250C 250C30 03013 GL COCKPIT SHEARED E EGIA K NONE O OTHER IN INSP/MAINT 1 SW 09 255EV 51488 PILOT REPORTED TO MAINTENANCE THAT THE ELEVATOR HAD AN EXCESSIVE AMOUNT OF TRAVEL AND THE CYCLIC SEEMED TO BE SLIGHTLY S TIFF FORE AND AFT. TROUBLESHOOTING PERFORMED BY MAINTENANCE AND FOUND THE ELEVATOR CONTROL TUBE SHEARED AT THE SHEAR PI N WHICH IS LOCATED IN THE PEDESTAL BETWEEN THE PILOT AND CO-PILOT SEATS. A COMPLETE CHECK OF THE ELEVATOR LINKAGE AND C ONTROLS WAS PERFORMED AND FOUND NO BINDING. THE CONTROL TUBE WAS REPLACED AND OPERATIONAL CHECK FLIGHT PERFORMED WITH N O DISCREPANCIES NOTED. THIS AIRCRAFT HAD BEEN OPERATED 29.6 HOURS SINCE MAJOR INSPECTION. DURING THIS INSPECTION, ALL THE FLIGHT CONTROLS HAD BEEN REMOVED FOR REPLACEMENT OF THE FORWARD BELLY TUB. UPON REINSTALLATION OF THE FLIGHT CONTR 1 G 7 1 3U 3 U H2SW E1GL 2008012200129 20080122 00129 EA 2008 1 22 A6WA200740678 1 20071213 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE WING OVERHEAT ILLUMINATED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 410AW 7490 WING OVERHEAT WARNING MESSAGE ON CLIMBOUT, SYNOPTIC PAGE INDICATES LT WING. CORRECTIVE ACTION IN PROGRESS. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200131 20080122 00131 EA 2008 1 22 A6WA200740663 1 20071115 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT WING LE DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 427ZW 7685 RT WING IB L/E FOUND SCRATCHED AND DENTED OVER LIMITS IAW CRJ200 SRM. NEW SKIN INSTALLED IAW CRJ SRM 51-40-11 AND SRM 5 1-41-04. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200135 20080122 00135 EA 2008 1 22 A6WA200740700 1 20071215 A 5230 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE CARGO DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 432AW 7257 CARGO DOOR CONNECTOR BRACKET CRACKED. (K) CARGO DOOR CONNECTOR BRACKET FABRICATED AND INSTALLED IAW SRM 51-24-15 AND 51 -42-06. 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200139 20080122 00139 EA 2008 1 22 A6WA200740698 1 20071212 A 5210 DIAPHRAGM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 432AW 7257 DIAPHRAGM CRACK UNDER FWD UPPER PAX DOOR CORNER COVER. (K) BRACKET CRACKED UNDER FWD UPPER PAX DOOR CORNER COVER REPLA CED IAW SRM 51-42-06. 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200140 20080122 00140 EA 2008 1 22 A6WA200740641 1 20071116 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 427ZW 7685 CRACK EXIST ON BRACKET OF FLOORBEAM, FS 280, LBL 9 AND RBL 9 CRACK ON BRACKET IS 1 INCH. NEW SERVICEABLE BRACKETS INSTA LL AT FS 280.00, LBL 9.0 AND RBL 9.0 IAW SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200161 20080122 00161 EA 2008 1 22 A6WA200740699 1 20071210 A 5321 FLOOR PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BS 280 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 432AW 7257 CORROSION EXIST ON FLOOR STRUCTURE FS 280, LBL 9 TO RBL 9. PERFORMED ON FLOOR STRUCTURE FS 280, LBL 9 TO RBL 9 IAW REO 601R-53-11-926. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200187 20080122 00187 EU 2008 1 22 COEA0758821 1 20070824 A 5347 SEAT TRACK AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. LEVEL 2 CORROSION: CORROSION ON SEVERAL CABIN FLOOR SEAT TRACKS FROM FR 29 TO 44. REMOVED AN D REPLACED THE FOLLOWING FLOOR SEAT TRACK SECTIONS. FR 29 TO 36, LT/OB, PN S53678001224. FRAME 39 TO 41 LT AND RT, L P N S53678001214, R PN S53678001212. FR 41 TO 44 LT AND RT, L PN S53070308202, R PN S53070308200. WO 72242, NR 200024, 4 0, 46, 47, 57. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008012200191 20080122 00191 EU 2008 1 22 COEA0744821 1 20070824 A 5210 S5217600000860 STRUCTURE AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE PAX DOOR CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 29796 253 FOUND DURING HEAVY CHECK. LEVEL 2 CORROSION SEVERAL PLACES ON AFT PASSENGER DOOR. REPLACED THE FOLLOWING PARTS. BEAM S52176205212, INNER SKIN PANEL S52176301200. WO 72242 NR 800025,33. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008012200193 20080122 00193 EA 2008 1 22 A6WA200740677 1 20071130 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 433AW 7289 CRACK FOUND ON FLOOR STRUCTURE FS 621, LBL 45 CRACK LENGTH IS .500 INCH. FLOOR SUPPORT AT FS 621.00 LBL 45 REPAIRED IAW REO 601R-53-61-117, REV C. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200214 20080122 00214 SO 2008 1 22 LR7A07160 1 20071219 A 5714 RIB LKHEED 382 382G 526414U SO FS 597 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HSP57119 FOUND LT CENTER WING BULKHEAD FOOT RIB CAP CRACKED AT FS 597, CWS140L, WL256. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-075. 2 H 7 4 4T A1SO 2008012200216 20080122 00216 SO 2008 1 22 LR7A07161 1 20071219 A 5714 RIB LKHEED 382 382G 526414U SO FS 597 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HSP57119, FOUND LT CENTER WING BULKHEAD FOOT RIB CAP CRACKED AT FS 597, CWS101L , WL256. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-074. 2 H 7 4 4T A1SO 2008012200221 20080122 00221 SO 2008 1 22 LR7A07166 1 20071219 A 5714 RIB LKHEED 382 382G 526414U SO FS 517 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HSP57119 FOUND LT CENTER WING BULKHEAD FOOT RIB CAP CRACKED AT FS517, CWS101L, WL256. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-074. 2 H 7 4 4T A1SO 2008012200222 20080122 00222 SO 2008 1 22 LR7A07167 1 20071219 A 5714 RIB LKHEED 382 382G 526414U SO FS 517 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER JOB CARD HSP57119 FOUND LT CENTER WING BULKHEAD FOOT RIB CAP CRACKED AT FS 517, CWS101L, WL285. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-078. 2 H 7 4 4T A1SO 2008012200229 20080122 00229 SO 2008 1 22 LR7A07172 1 20071219 A 5714 STRINGER LKHEED 382 382G 526414U SO CENTER WING CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2 FOUND HOLE CRACK IN STRINGER LEG COMMON TO WING ATTACH ANGLE AT CWS61L WL 256 STRINGER 20 HOLE 36Y. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-076. 2 H 7 4 4T A1SO 2008012200232 20080122 00232 SO 2008 1 22 LR7A07174 1 20071219 A 5730 SKIN LKHEED 382 382G 526414U SO CENTER WING CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2 FOUND HOLE CRACK IN WING PLANK COMMON TO WING ATTACH ANGLE AT CWS61R, WL2 56, NR 2 LOWER PANEL, HOLE 36X. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-087. 2 H 7 4 4T A1SO 2008012200234 20080122 00234 SO 2008 1 22 LR7A07176 1 20071219 A 5730 SKIN LKHEED 382 382G 526414U SO FS 597 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2 FOUND HOLE CRACK IN WING PLANK COMMON TO WING ATTACH ANGLE AT FS 597, CWS 61R, WL256, NR 1 LOWER PLANK, HOLE 53Y. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-076. 2 H 7 4 4T A1SO 2008012200235 20080122 00235 NM 2008 1 22 AALA20072582 1 20071119 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 977AN 29550 TUL - EMERGENCY LIGHT BATTERY PACK IN MID CABIN FAILED TEST. REPLACED BATTERY PACK M1695 FOR EMERGENCY LIGHTS IN MID CA BIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008012200236 20080122 00236 NM 2008 1 22 AALA20072579 1 20071023 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 939AN 30883 TUL - EMERGENCY LIGHT BATTERY PACK AT LEFT FORWARD EMERGENCY EXIT FAILED TEST. REPLACED BATTERY PACK AT STATION 609 FOR EMERGENCY LIGHTS AT LEFT FORWARD EMERGENCY EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008012200237 20080122 00237 NM 2008 1 22 AALA20072575 1 20071213 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 943AN 30599 TUL - EMERGENCY LIGHT BATTERY PACK IN FORWARD CABIN FAILED TEST. REPLACED BATTERY PACK M1675 FOR EMERGENCY LIGHTS IN FO RWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008012200295 20080122 00295 NM 2008 1 22 2007UALA05388 1 20071228 A 2421 IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 590UA 28708 LEFT IDG TOOK 81 PUMPS, RAN THEN PUMPED 19 MORE. SUSPECT FUEL OIL HEAT EXCHANGER LEAK. REPLACED FUEL OIL HEAT EXCHAN GER AND IDG. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012200339 20080122 00339 NM 2008 1 22 UPS08M51400 1 20071203 A 5330 DOUBLER DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C LWR FUSELAGE STA 1941 LONG 33R FOUND EXISTING REPAIR SIGN OF CORROSION. EXISTING REPAIR DOUBLER CORR EXCEEDS LIMIT. FASTENER REMOVED. HFEC INSP C/O ON EXISTING TRIM OUT AREA, FOUND NO CRACK EVIDENT. RETRIM ON EXISTING TRIMMED AREA. HFEC INSP C/O ON TRIM OFF AREA, FOUND NO CRACK EVIDENT. FAB 2EA NEW REPAIR DOUBLERS & 12 EA FINGER DOUBL ERS. ALL NEW DOUBLERS HOLES PICKED UP, PAINTED & INSTALLED PER SRM 51-31-01 VII R35. 2 L 7 3 4F RT A22WE 2008012300015 20080123 00015 NM 2008 1 23 2007UALA05344 1 20071229 A 3350 D9239003500060 EPSU AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 827UA 1022 EMERGENCY LIGHTS ON WITH SWITCH ARMED. EPSU FAILURE. REPLACED EPSU 13WL. ALL LIGHTS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012300016 20080123 00016 EU 2008 1 23 2007UALA05345 1 20071229 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 431UA 571 COCKPIT O2 1340 PSI, WITH AMBER HALF-BOX. SERVICED CREW O2, CHECKED FOR LEAKS, NONE NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012300018 20080123 00018 NM 2008 1 23 2007UALA05384 1 20071230 A 5754 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE L/E SLAT DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 851UA 1664 BIRD STRIKE ON NR 3 SLAT ON LEFT WING, DENT MEASURES 6 X 3.5 (CHORDWISE), APPROX 0.5 INCH DEEP. LOCATED 0.31 25 INCHES FROM RIB RIVETS. REPAIRED NR 3 L/E SLAT WITH AN INSERT REPAIR AND PERFORMED BIRD STRIKE INSPECTION OF WHOLE A/C, NO FUR THER DAMAGE WAS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012300035 20080123 00035 EA 2008 1 23 SWIA200719074 1 20070905 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 976SW 7952 LBL 9 LOWER FRAME FS 280 AND LBL 9 IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER REO 601R 53-11-171. 2 L 7 2 4F RT A21EA 2008012300063 20080123 00063 SO 2008 1 23 FDKA200710514 1 20071001 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR DISCONNECTED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 842MJ 145457 FDM 6024 BHM (0333 PHX LCL) - MAIN CABIN DOOR WILL NOT OPEN. MX FOUND TOP FORWARD HOOK OVER ROLLER. DISCONNECTED, UNJA MMED DOOR AND RECONNECTED HOOK. OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012300066 20080123 00066 SO 2008 1 23 FDKA200710519 1 20071003 A 2711 TRIM SYSTEM EMB 145 EMB145LR 3260212 SO AILERONS STIFF A FDKA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 SW 07 853MJ 145464 FDM 6041 JFK (1921 PHX LCL) - AILERON MIS TRIM AND AILERON GOT STIFFER WITH SLOWER AIRSPEED DURING APPROACH. MX COULD N OT DUPLICATE 2 L 7 2 4T RT T00011AT 2008012200013 20080122 00013 EA 2008 1 22 A6WA200740658 1 20071208 A 3350 110049 CHARGER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE EMERGENCY LIGHTS INOPERATIVE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 412AW 8474 7582 ENTRY-WAY EMERGENCY FLOODLIGHT INOPERATIVE. REMOVED AND REPLACED CHARGER ASSY NR 2 IAW 33-51-05, OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200029 20080122 00029 NM 2008 1 22 USAA920080118 1 20071230 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 22198 PIT - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION ON FLOORBEAM, BS 1661, BL 0. REPAIRED FLOORBEAM, BS 1661, BL 0 IAW B75 7 SRM 53-00-51 REPAIR 5. 2 L 7 2 4F RT A2NM 2008012200045 20080122 00045 EA 2008 1 22 A6WA200740667 1 20071115 A 5340 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 427ZW 7685 RT MLG WHEEL WELL FWD HYD SUPPORT BRACKET CRACKED. RT MLG WHEEL WELL FWD HYDRAULIC SUPPORT BARCKET REPLACED IAW CRJ 200 SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200088 20080122 00088 EA 2008 1 22 A6WA200740687 1 20071210 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 432AW 7257 FWD UPPER CORNER COVER CRACK ON PAX DOOR. (K) FWD UPPER CORNER COVER OF PAX DOOR REPLACED IAW SRM 51-42-13. 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200097 20080122 00097 EA 2008 1 22 TRAX200800052 1 20071231 A 2910 HYDRAULIC LINE CNDAIR CL600 CL6002B19 1900309 EA LT WING CHAFED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 880AS 7606 LT WING T/E-HYD LINE CHAFING ON WIRE BUNDLE AT WING STA 50 "FLAGGED". E/C PERFORMED IAW NTM CRACK CONFIRMED IN X AXIS , END OF CRACK MARKED. NO CRACK FOUND IN Y AXIS. 2 L 7 2 4F RT A21EA 2008012200198 20080122 00198 EA 2008 1 22 A6WA200740676 1 20071130 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BS 589-621 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 433AW 7289 CORROSION FOUND ON FLOOR SUPPORT FS 589 TO 621, LBL 27. JOB PERFORMED ON FLOOR SUPPORT FS 589 TO 621, LBL 27 IAW REO 60 1R-53-61-2439. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200233 20080122 00233 SO 2008 1 22 LR7A07175 1 20071219 A 5730 SKIN LKHEED 382 382G 526414U SO CENTER WING CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 2633 4676 DURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2 FOUND HOLE CRACK IN WING PLANK COMMON TO WING ATTACH ANGLE AT CWS61R, WL2 56, STRINGER 20, HOLE 37Y. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-087. 2 H 7 4 4T A1SO 2008012200238 20080122 00238 NM 2008 1 22 AALA20072576 1 20071213 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 943AN 30599 TUL - EMERGENCY LIGHT BATTERY PACK AT STATION 322 FAILED TEST. REPLACED BATTERY PACK M1674 FOR EMERGENCY LIGHTS IN FORW ARD CABIN AT STATION 322. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008012200239 20080122 00239 NM 2008 1 22 AALA20072577 1 20071216 A 3350 CM767 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 943AN 30599 TUL - EMERGENCY LIGHT AT RIGHT FORWARD OVERWING EXIT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT FORWARD OV ERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008012200240 20080122 00240 NM 2008 1 22 AALA20072580 1 20071023 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 939AN 30883 TUL - EMERGENCY LIGHT BATTERY PACK AT RIGHT FIRST CLASS DIVIDER FAILED TEST. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT FIRST CLASS DIVIDER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008012200364 20080122 00364 EA 2008 1 22 TRAX200800026 1 20071230 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 880AS 7606 AAR - RIGHT BATT RIB CRACKED. REMOVED CONNECTOR J410 AND J412 ON RIGHT BATT RIB. REMOVED FASTENERS THRU DOUBLER ON O/B SIDE AND REMOVED NUT PLATES ON ANGLE OF RIGHT BATT RIB. REMOVED DOUBLER ON O/B SIDE AND INSIDE SUPPORT ANGLE ON I/B SI DE OF RIGHT BATT RIB. LOCATED AND DRILLED ANGLE DOUBLER (-10) AND FILLER (-12) WITH CUTOUT OF DAMAGE AS IAW BOMBARDIER REO 601R-57-51-046. INSTALL ANGLE DBLR FILLER AND INBOARD SUPPORT ANGLES. INSTALLED ANGLE DOUBLER FILLER I/B SUPPORT A NGLES IAW BOMBARDIER REO 601R-57-51-09. REINSTALLED CONNECTOR J410 AND J412. OPS CHECK GOOD RII 5001196 IAW CRJ 200 AM M 32-01-00. ALL WORK ACCOMPLISHED PER ASA EC/TC 601R-57-51-046. SUPPLEMENTAL SDR CLOSED 1/15/08. 2 L 7 2 4F RT A21EA 2008012200367 20080122 00367 NM 2008 1 22 2007UALA04876 1 20071127 A 3200 257U000228 MODULE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE INSTRUMENT FAULTY A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 182UA 25279 EICAS MSG "GEAR MONITOR" SHOWS PREDEPARTURE. SUSPECT FAULTY GEAR CONTROL MODULE. REPLACED LANDING GEAR CONTROL HANDLE MODULE PER MM 32-31-01 PAGE 414 PAR H(17). COMPLETE OPERATIONAL CHECKS NORMAL AFTER CMC PSEU TESTS FOR PRIMARY AND ALT SENSOR TESTS PASSED. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012300044 20080123 00044 SO 2008 1 23 FDKA200709506 1 20070926 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 851MJ 145572 FDM 6088 MCO (0810 PHX LCL) - PASSENGER DOOR HARD TO OPEN AND CLOSE. MX LUBED PASSENGER DOOR, OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012300046 20080123 00046 SO 2008 1 23 FDKA200711314 1 20071103 A 5210 14534478403 FAIRING EMB 145 EMB145LR 3260212 SO PAX DOOR UNKNOWN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 855MJ 145614 FRL RON PWM (1913 PHX LCL) - MAIN CABIN DOOR WILL NOT OPEN OR CLOSE. MX REPLACED MAIN DOOR FAIRING. 2 L 7 2 4T RT T00011AT 2008012300050 20080123 00050 SO 2008 1 23 FDKA200709511 1 20070930 A 7810 MIXER BOX EMB 145 EMB145LR 3260212 SO NR 1 ENGINE BROKEN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6097 ALB (0001 PHX LCL) - NR 1 ENGINE EXHAUST FORCED AIR MIXER BROKEN. MX REMOVED AND REPLACED MIXER. 2 L 7 2 4T RT T00011AT 2008012300110 20080123 00110 NM 2008 1 23 DLM90080036 1 20071222 A 5310 993653349 DOOR FRAME DOUG MD90 MD9030 3023690 NM R1 DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 FORWARD PAX CABIN AFT SIDE AND I/B OF R1 DOOR LOWER JAMB WEB HAS CORROSION. REPAIRED FWD PAX CABIN AFT SIDE AND I/B OF R1 DOOR LOWER JAMB WEB IAW MD90 SRM 51-11-01 FIG 2. 2 L 7 2 4F RT A6WE 2008012300114 20080123 00114 NM 2008 1 23 DLM90080039 1 20071228 A 5322 SHEAR TIE DOUG MD90 MD9030 3023690 NM BS 1344 S28R&27L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 CORROSION ON AFT PIT SHEAR TIE AFT SIDE STA1344 LONGERON 28R-27L. REPAIRED SHEAR TIE IAW MD90 SRM 53-10-02D FIG 3. 2 L 7 2 4F RT A6WE 2008012300116 20080123 00116 NM 2008 1 23 DLM90080040 1 20071226 A 5347 593054768 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 795 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 SEAT TRACK OUT OF LIMITS AT STA 795 AND RBL 22 IAW MD90 SRM 53-40-01 FIG4. CORROSION TASK 53.21.01/02. REMOVED AND REP LACED SEAT TRACK IAW MD90 SRM 53-40-01 FIG 6 9FS 778 TO 854. 2 L 7 2 4F RT A6WE 2008012300117 20080123 00117 NM 2008 1 23 DLM90080041 1 20071223 A 5320 993053877 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 674-769 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 RT CABIN CUSP WEB CORRODED AND EXFOLIATED ENTIRE LENGTH FS 674-769. REMOVED AND REPLACED RT CABIN CUSP WEB STA 674-769 IAW MD90 SRM 51-30-02. 2 L 7 2 4F RT A6WE 2008012300202 20080123 00202 SO 2008 1 23 FDKA200709440 1 20070902 A 3350 6050961 BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 848MJ 13850 145530 LEFT EXTERIOR EMERGENCY LIGHT INOP. REPLACED NR 2 POWER SUPPLY AND BATTERY PACK, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008012300203 20080123 00203 SO 2008 1 23 FDKA200709449 1 20070907 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 830MJ 145259 FFDM FLT 6097 JFK - CEILING EMERGENCY OVERWING EXIT SIGN FORWARD SIDE INOP. MX RE-SECURED LIGHT ASSY/CONNECTOR, SYSTEM OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012300204 20080123 00204 SO 2008 1 23 FDKA200709472 1 20070917 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FDM 6129 RDU - ROW 12 EXIT SIGN INOP. MX RESET LIGHTS, OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012300206 20080123 00206 SO 2008 1 23 FDKA200709480 1 20070921 A 3350 SOCKET EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BURNED A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 830MJ 145259 FDM 6135 NAS (1206 PHX LCL), BURNING ODOR FROM ROW 1A SIDEWALL LIGHT. MX FOUND 1A SIDEWALL LIGHT SOCKET BURNED AND REMO VED AND REPLACED FIXTURE. 2 L 7 2 4T RT T00011AT 2008012300207 20080123 00207 SO 2008 1 23 FDKA200709482 1 20070923 A 3350 BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DISCHARGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 849MJ 145534 FDM 6206 FLL (0710 PHX LCL) - EMERGENCY EXIT LIGHT INOP, BATTERIES ARE DEAD. REPLACED BATTERIES, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012300208 20080123 00208 SO 2008 1 23 FDKA200709507 1 20070927 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FDM 6067 BHM (0440 PHX LCL) - ROW 12 RIGHT EMERGENCY LIGHT INOP. MX RESET LIGHT, OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012200368 20080122 00368 NM 2008 1 22 2007UALA04873 1 20071129 A 2160 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE UNKNOWN A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 654UA 25392 FIRST CLASS EXTREMELY COLD, CAN'T CONTROL CABIN TEMP. ECONOMY VERY HOT. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012200369 20080122 00369 NE 2008 1 22 2007UALA04824 2 20071125 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA 4084 PW4084 NE NR 2 MAKING METAL A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 795UA 26927 222025 UNABLE TO START NR 2 ENGINE. FOUND METEL ON NR 2 ENG MAIN GEARBOX CHIP DETECTOR. SUSPECT BEARING FAILURE. REPLACED NR 2 ENG. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008012200370 20080122 00370 NM 2008 1 22 2007UALA04807 1 20071125 A 3010 0871DL6 DETECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT ICE DETECTION FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 214UA 30220 ICE DETECTOR R RIGHT ICE DETECTOR FAILURE. FAILED TEST NUMEROUS TIMES. REPLACED RT ICE DETECTOR. TESTED NORMAL AND MES SAGE GONE PER MM 30-81-01. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008012300012 20080123 00012 EA 2008 1 23 SWIA200719071 1 20070905 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT MLG WW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 976SW 7952 RIGHT WHEEL WELL BRAKE PRESSURE TRANSDUCER BRACKET IS CRACKED, FOUND AT C-CHECK. REPLACED RIGHT BRACKET PER CRJ200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008012300013 20080123 00013 NM 2008 1 23 2007UALA05342 1 20071230 A 3397 WIRE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 807UA 798 PASSENGER SEAT ROW 10ABC, EMERGENCY EXIT LIGHT INOP. WIRES DISTURBED BY PASSENGER BAG OR FOOT. RESECURED WIRES, OPS CK 'D GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012300017 20080123 00017 EU 2008 1 23 2007UALA05346 1 20071230 A 3040 66642023 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE WINDOW HEAT FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 493UA 1821 CAPTAIN'S FWD SIDE WINDOW HOT TO THE TOUCH, F/O NORMAL - NO SUN. WINDOW HEAT COMPUTER MALFUNCTION. REPLACED WINDOW HEA T COMPUTER, WINDOW OPERATES NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012300048 20080123 00048 SO 2008 1 23 FDKA200709508 1 20070927 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 851MJ 145572 FDM 6192 BOS (1621 PHX LCL) - MAIN PAX DOOR HARD TO OPEN. MX INSPECTED, CLEANED AND LUBED OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012300049 20080123 00049 SO 2008 1 23 FDKA200710557 1 20071021 A 2760 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO SPOILER OUT OF ADJUST A FDKA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 827MJ 145217 FDM 6125 MCO - RTG ABORT TAKEOFF MASTER CAUTION WHEN THROTTLES ADVANCED. MX ADJUSTED PROX SENSOR ON LEFT OUTBOARD SPOIL ER. OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012300051 20080123 00051 SO 2008 1 23 FDKA200709510 1 20070928 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 830MJ 145259 FDM RON RDU - LOUD SQUEAL FROM MAIN PAX DOOR ON DESCEND. MX RESEATED DOOR SEAL IN TRACK. 2 L 7 2 4T RT T00011AT 2008012300062 20080123 00062 SO 2008 1 23 FDKA200710513 1 20071001 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6153 MCO (0822 PHX LCL) - MAIN CABIN DOOR WILL NOT CLOSE/SEAL ENTIRE TOP. MX COULD NOT DUPLICATE, DOOR OPS CHECKED AND SEALED GOOD. 2 L 7 2 4T RT T00011AT 2008012300067 20080123 00067 SO 2008 1 23 FDKA200710520 1 20071004 A 2750 3631001011 SENSOR EMB 145 EMB145LR 3260212 SO FLAPS DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 6506 145359 FDM 6065 GSO (0610 PHX LCL) - VISUAL INSPECTION OFF FLAP DUE TO EXCEEDANCE OF AIRSPEED WITH FLAP AT 9 DEGREES AND FLAP L OW SPEED. MX PERFORMED VISUAL INSPECTION WITH NO STRUCTURAL DAMAGED FOUND AND REPLACED FLAP VELOCITY SENSOR. 2 L 7 2 4T RT T00011AT 2008012300068 20080123 00068 SO 2008 1 23 FDKA200710521 1 20071004 A 2710 3670001005 ACTUATOR EMB 145 EMB145LR 3260212 SO AILERONS MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 853MJ 12366 145464 FDM 6021 JFK (0920 PHX LCL) AILERON ABNORMAL CONTROL FORCE AND FEEL DURING CHECK. MX REMOVED AND REPLACED ARTIFICIAL FE EL ACTUATOR AND PCA, OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012300111 20080123 00111 NM 2008 1 23 DLM90080037 1 20071230 A 5347 593054769 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 1315 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 AFT LT PAX CABIN SEAT TRACK FROM STA 1315 TO AFT END HAS CORROSION AROUND FASTENER HOLES. REMOVED AND REPLACED SEAT TRA CK IAW MD90 SRM 53-30-01, 51-30-05 AND 53-40-01 FIG 6. 2 L 7 2 4F RT A6WE 2008012300223 20080123 00223 NM 2008 1 23 HNAA0800018 1 20071230 A 3350 1013075 MODULE DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 812EX 39893 39893 312 DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTING WAS BEING ROUTINELY CHECKED WHEN THE THIRD LIGHT AFT ON THE FLOOR LIGHT ING STRIP WAS FOUND TO BE INOPERATIVE. THE MODULE WAS CHANGED AND SYSTEM CHECKED. OPS CHECK WAS GOOD. 2 H 7 2 4T RT A13NM 2008012300224 20080123 00224 NM 2008 1 23 HNAA0800019 1 20071228 A 3350 61047811 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 827EX 2725 160 390 DURING ROUTINE OVERNIGHT MAINTENANCE, THE RED EMERGENCY AISLE MARKERS AT ROW 1 AND 4 WOULD NOT ILLUMINATE. EMERGENCY BA TTERY PACK AT ROW 3 LEFT (3351-PS3) WAS CHANGED. SYSTEM OPERATED NORMALLY AT THAT TIME. 2 H 7 2 4T RT A13NM 2008012300225 20080123 00225 NM 2008 1 23 HNAA0800007 1 20071223 A 2997 MS3476L833S CONNECTOR DHAV DHC8 DHC8102 2809003 NM HYDRAULIC SYS DIRTY A HNAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 07 808EX 39682 39682 299 DURING APPROACH, LANDING GEAR WAS SELECTED DOWN AND PILOTS OBSERVED THREE RED LIGHTS ON THE LANDING GEAR SELECTOR PANEL AND ILLUMINATION OF THE NR 2 HYDRAULIC ISOLATION VALVE CAUTION LIGHT. HYDRAULIC QUANTITIES AND PRESSURES REMAINED STEAD Y. PILOTS DECLARED AN EMERGENCY AND PERFORMED A GO-AROUND THEN PERFORMED AN ALTERNATE GEAR EXTENSION. AIRCRAFT LANDED NORMALLY AND TAXIED TO THE GATE WITH EMERGENCY VEHICLES FOLLOWING. PILOTS REPORTED LOSS OF NOSE WHEEL STEERING AND OUTB OARD SPOILERS. MAINTENANCE FOUND FLUID LEVELS TO BE ADEQUATELY SERVICED. THE NR 2 RESERVOIR VALVE CONNECTOR WAS CLEANE D AND SYSTEM CHECKED IAW PIEDMONT WORK CARD. OPS CHECKS WERE NORMAL. NEW INFORMATION ADDED. 2 H 7 2 4T RT A13NM 2008012300233 20080123 00233 NM 2008 1 23 HNAA0800015 1 20071207 A 5420 8540146 STRUCTURE DHAV DHC8 DHC8102 2809003 NM NACELLE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 53968 53968 53 DURING INSPECTION, FOUND CRACKS IN THE NR 1 FORWARD RADIUS AT ABOUT 2 O’CLOCK AND NR 2 HORSE COLLAR FORWARD RADIUS AT TH E 2 O’CLOCK AND 10 O’CLOCK POSITIONS. REPAIRED ALL THREE CRACKS PER RD8-54-2451 AND RD8-54-1736. 2 H 7 2 4T RT A13NM 2008012300234 20080123 00234 NM 2008 1 23 2007UALA03880 1 20070924 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 AFT CARGO PIT STRINGER CLIP CRACKED AT BS 727D. MAJOR REPAIR: REMOVED AND REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300253 20080123 00253 NM 2008 1 23 UPS08M51399 1 20071113 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C RIGHT WING FUEL TANK STRINGER 11 END SUSPECT CRACKED. HFEC INSP C/O AT STR 11, FOUND CRACK 11 INCHES LONG. RIGHT WING STR 11 SPLICE END, ATTACH BRACKETS & HI-LOKS REMOVED. STR 11 RIGHT WING TRIM OFF. HFEC INSP C/O ON T RIM OFF AREA, FOUND NO CRACK EVIDT. REPAIR STR & 04EA SPLICES FAB FPI C/O ON FAB SPLICES & FOUND NO CRACK EVIDT. STR 1 1 REPAIR PARTS, NEW STR, ST 11 SPLICE END & ATTACH PARTS INSTALLED. LEAK CHECK SATISFACTORY. 2 L 7 3 4F RT A22WE 2008012300255 20080123 00255 NM 2008 1 23 ZZDA2008009 1 20071003 A 3350 SHROUD BOEING 717 717200 1383700 NM AFT CABIN BROKEN A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 954AT 55016 EXIT SIGN SHROUD AT AFT FLIGHT ATTENDANTS HANDSET BROKEN. REPLACED LIGHT ASSY, OPS CHECK GOOD REF MM 33-28. 2 L 7 2 4F TR A6WE 2008012300257 20080123 00257 NM 2008 1 23 ZZDA2008011 1 20070430 A 3350 POWER SUPPLY BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 965AT 55026 EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED OVERWING POWER SUPPLY IAW M/M 33-51-06, OPS CHECK OK. 2 L 7 2 4F TR A6WE 2008012300258 20080123 00258 NM 2008 1 23 ZZDA2008012 1 20070501 A 3350 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 975AT 55035 SERVICE DOOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD, REF MM 33-51. 2 L 7 2 4F TR A6WE 2008012300260 20080123 00260 NM 2008 1 23 ZZDA2008014 1 20070514 A 3350 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 891AT 55043 LOWER WALKWAY TAIL CONE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK AT PER AMM 24-00. OPS CHECK NORMAL. 2 L 7 2 4F TR A6WE 2008012400012 20080124 00012 SO 2008 1 24 FDKA200712389 1 20071207 A 5541 FRAME EMB 145 EMB145LR 3260212 SO RUDDER DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 FDM 6088 RDU (2225 PHX LCL) - RUDDER CABLES DAMAGED FRAME. MX CURRENTLY TROUBLESHOOTING. 2 L 7 2 4T RT T00011AT 2008012400013 20080124 00013 SO 2008 1 24 FDKA200712391 1 20071209 A 5270 WARNING LIGHT EMB 145 EMB145LR 3260212 SO PAX DOOR FALSE ACTIVATION A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 855MJ 145614 FDM 6157 MCO (1110 PHX LCL) - EICAS INDICATION PAX DOOR OPEN WITH DOOR CLOSED. MX TROUBLESHOT AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012400014 20080124 00014 NM 2008 1 24 ZZDA2008015 1 20070726 A 3350 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 896AT 55048 OVERWING EMERGENCY LIGHTS WILL NOT STAY OFF. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT BATTERY PACK. OP'S CHECK GO OD. REF AMM 33-50. 2 L 7 2 4F TR A6WE 2008012400019 20080124 00019 SO 2008 1 24 FDKA200712387 1 20071207 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX LACK OF LUBE A FDKA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SW 07 851MJ 145572 FDM 6148 MCO (0726 PHX LCL) - MAIN CABIN DOOR DIFFICULT TO OPEN FROM THE INSIDE. MX CLEANED AND LUBED DOOR ASSY. OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012400023 20080124 00023 SO 2008 1 24 FDKA200712393 1 20071210 A 2611 SMOKE WARNING EMB 145 EMB145LR 3260212 SO LAVATORY ACTIVATED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 858MJ 145767 FDM 6145 JFK (0913 PHX LCL) - PILOT RETURNED TO FIELD DUE TO A LAV SMOKE WARNING IN FLIGHT. MX PLACED THE ITEM ON MEL. 2 L 7 2 4T RT T00011AT 2008012400036 20080124 00036 SO 2008 1 24 FDKA200710555 1 20071018 A 2731 SWITCH EMB 145 EMB145LR 3260212 SO PITCH TRIM INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FDM 6188 TLH (0339 PHX LCL) - BACKUP PITCH TRIM SWITCH INOP. MX CLEANED TRIM SWITCH OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012400037 20080124 00037 NM 2008 1 24 ZZDA2008020 1 20070510 A 3350 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 934AT 55070 EMERGENCY EXIT LIGHT INOP AT SEAT ROWS 1DF, 2DF, 3DF AND 10DEF. REMOVED & REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSY AT STA 398 PER B717 AMM 33-51, OPS CHECK GOOD. 2 L 7 2 4F TR A6WE 2008012400040 20080124 00040 NM 2008 1 24 ZZDA2008022 1 20070602 A 3350 8039251 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 932AT 55073 EMERGENCY ROW LIGHTS ON SEATS 1AC, 2AC AND 3AC INOPERATIVE. REMOVED & REPLACED POWER SUPPLY ASSYS AT STA 341 B5-118 & S TA 213, B5-235 REF 33-51 M/M. 2 L 7 2 4F TR A6WE 2008012400044 20080124 00044 NM 2008 1 24 ZZDA2008026 1 20070518 A 3350 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 910AT 55086 EMERGENCY LIGHTS INOP AT SEATS 21DEF THROUGH 25DEF. REMOVED AND REPLACED BATTERY PACKS S3-388 AND S3-384, OPS CHECK GOO D. 2 L 7 2 4F TR A6WE 2008012400046 20080124 00046 NM 2008 1 24 ZZDA2008028 1 20070613 A 3350 8039251 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 986AT 55089 SEAT EMERGENCY LIGHTS INOP SEAT ROWS 25-31 FED. REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSY FOR SEAT ROWS 25-31 FED. PER AMM 33-51, OPS CHECK GOOD. 2 L 7 2 4F TR A6WE 2008012400048 20080124 00048 NM 2008 1 24 ZZDA2008030 1 20070914 A 3350 D71702001 BATTERY PACK BOEING 737 73776N 13844CH NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 284AT 32668 EMERGENCY LIGHTS IN ROWS 21ABC & 23ABC INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY REF B737 AMM 33-51, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2008012400050 20080124 00050 NM 2008 1 24 HNAA0800021 1 20071229 A 2760 TDH60505001 RELAY DHAV DHC8 DHC8102 2809003 NM SPOILER SYS DEFECTIVE A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 981HA 30040 30040 378 ABORTED TAKEOFF DUE TO ILLUMINATION OF ROLL SPOILER INBOARD AND ROLL SPOILER OUTBOARD CAUTION LIGHTS ON TAKEOFF ROLL. I NSPPECTED, TESTED, CLEANED AND LUBED 2763 S1, S2, S5 AND S6. CHANGED TIME DELAY RELAY 2761 K1 PER DMM CHAP 27-14-00. T ESTED SYSTEM PER W/C 27-60-05Q AND C/W JOBCARD 27-60-050. NO DEFECTS NOTED. 2 H 7 2 4T RT A13NM 2008012400083 20080124 00083 SO 2008 1 24 FDKA200707325 1 20070706 A 2731 TRIM SYSTEM EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 833MJ 145327 FDM 6103 PNS-MCO (0701 PHX LCL) - PITCH TRIM MAIN INOP. RESET SYSTEM, OP CK GOOD AND NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008012400092 20080124 00092 SO 2008 1 24 FDKA200707328 1 20070707 A 5610 WINDOW EMB 145 EMB145LR 3260212 SO COCKPIT OUT OF RIG A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6085 MCO (0722 PHX LCL) - FO'S DV WINDOW WILL NOT CLOSE. MX ADJUSTED RIGGING ON FO'S DV WINDOW. 2 L 7 2 4T RT T00011AT 2008012400095 20080124 00095 SO 2008 1 24 FDKA200709479 1 20070921 A 2750 3631001011 FCU EMB 145 EMB145LR 3260212 SO FLAPS MALFUNCTIONED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 847MJ 5921 145517 FDM RON RDU (0034 PHX LCL) - LOW FLAP SPEED MESSAGE ON EICAS. MX REMOVED AND REPLACED FECU. 2 L 7 2 4T RT T00011AT 2008012400098 20080124 00098 SO 2008 1 24 FDKA200707331 1 20070708 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO CARGO BAY MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 855MJ 14743 145614 FDM 6064 HSV (0430 PHX LCL) - CARGO SMOKE DETECTION INDICATION. MX REMOVED AND REPLACED SMOKE DETECTOR. 2 L 7 2 4T RT T00011AT 2008012400100 20080124 00100 SO 2008 1 24 FDKA200707332 1 20070708 A 5240 DOOR EMB 145 EMB145LR 3260212 SO LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 FDM RON MCO (1854 PHX LCL) - SERVICE DOOR WAS DIFFICULT TO CLOSE. MX LUBRICATED THE DOOR AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2008012400105 20080124 00105 SO 2008 1 24 FDKA200711317 1 20071105 A 2760 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO SPOILERS DIRTY A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 831MJ 145273 FDM 6149 JFK (1113 PHX LCL) - SPOILER FAIL IN FLIGHT INTERMITTENTLY. MX CLEANED SPOILER PROX SWITCHES, OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012300227 20080123 00227 SO 2008 1 23 FDKA200709509 1 20070928 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6053 TPA - BOTH OVERWING EMERGENCY LIGHTS INOP. MX RESEATED CONNECTOR ON POWER PACK, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012300228 20080123 00228 SO 2008 1 23 FDKA200710525 1 20071005 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 853MJ 145464 FDM 6023 JFK - BOTH OVERWING EMERGENCY EXIT LIGHTS AT ROW 12 WERE INOPERATIVE. MX RESECURED THE CONNECTORS AND OPS CHEC KED. 2 L 7 2 4T RT T00011AT 2008012300229 20080123 00229 SO 2008 1 23 FDKA200710542 1 20071010 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 838MJ 145384 FRL FLT 6004 MCO-DAY - EMERGENCY FLOOR AFT LIGHTS INOP. MX RESECURED LOOSE CONNECTION. OPS GOOD. 2 L 7 2 4F RT T00011AT 2008012300230 20080123 00230 SO 2008 1 23 FDKA200710553 1 20071015 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 FDM 6101 TLH (1240 PHX LCL) - EMERGENCY FLOOR PATH LIGHTING AT ROW 12 INOP. MX FOUND CORROSION AT CONNECTOR. CLEANED A ND RE-SOLDERED. 2 L 7 2 4T RT T00011AT 2008012300231 20080123 00231 SO 2008 1 23 FDKA200710565 1 20071022 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 855MJ 145614 FDM 6091 RDU - EMERGENCY EXIT SIGN LIGHT AT ROW 12 INOPERATIVE. MX RESECURED CONNECTOR, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008012300232 20080123 00232 SO 2008 1 23 FDKA200710273 1 20071025 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 840MJ 145429 FDM 6142 MCO (1000 PHX LCL) - EMERGENCY FLOOR LIGHTING INOP. MX RECONNECTED CONNECTOR. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012300236 20080123 00236 NM 2008 1 23 2007UALA05390 1 20071231 A 2842 COMPUTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUEL QTY MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 589UA 28707 LEFT FUEL QTY IND WAS DECREASING AT A RAPID RATE. BALANCED FUEL PER IRREGULAR CHECKLIST. FUEL DECREASE IN LEFT AND RI GHT FUEL TANKS NORMAL. FUEL IND AT TIME OF MSG: LT TANK 12.4 RT TANK 14.4 CTR 1.0 CHECKED FUEL PROCESSOR, NO FAULTS. RESET FUEL QTY BITE TESTED GOOD. NO HISTORY. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012300242 20080123 00242 WP 2008 1 23 UPS08851404 1 20071230 A 5544 565507765 DOUBLER DOUG DC8 DC871F 302199D WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 INTERNAL DOUBLER CRACKED ON LOWER EYEBOLT ACCESS HOLE ON RUDDER. REMOVED, FABRICATED AND REPLACED IN TERNAL DOUBLER PER DWG 5655077 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2008012300251 20080123 00251 NM 2008 1 23 UPS08M51398 1 20071113 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C LEFT WING UPPER FUEL TANK STRINGER 9 END SUSPECT CRACKED. HFEC INSP C/O AT STR 9 END, FOUND APPROX 15 INCH CRACK. STR 9 SPLICE END & HI-LOKS REMOVED. CRACKED END AT LEFT WING STR 9 TRIMMED OFF. HFEC INSP C/O ON TRIM OF F AREA, FOUND NO CRACK EVIDT. REPAIR STR & SPLICE FAB SHIMS FOR STR 9 STIFFENERS ARB7192 & ARB7193 FAB. NEW STR 9, ATT ACH PARTS & SPLICE END INSTALLED. SEALANT ON REPAIR AREA APPLIED. LEAK CHECK SATISFACTORY. 2 L 7 3 4F RT A22WE 2008012300256 20080123 00256 NM 2008 1 23 ZZDA2008010 1 20071114 A 2560 SIGN BOEING 717 717200 1383700 NM CABIN OUT OF POSITION A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 978AT 55037 EXIT SIGN BETWEEN ROW 1 & 2 FELL DOWN. RESECURED EXIT SIGN. OK FOR SERVICE. REF M/M 33-00. 2 L 7 2 4F TR A6WE 2008012400015 20080124 00015 NM 2008 1 24 ZZDA2008016 1 20070820 A 3350 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 896AT 55048 EMERGENCY LIGHTS WILL NOT DISARM WITH SWITCH IN OFF POSITION. OVERWING EXIT LIGHTS WILL COME ON WITH ALL POWER OFF. DI SCONNECTED EMERGENCY BATTERY PACK IN AFT CARGO CEILING PANEL, REMOVED AND REPLACED OVERWING EVACUATION EMERGENCY BATTERY POWER SUPPLY PER M/M B-717 M/M REF 33-51-06. OPS CHECKS GOOD. 2 L 7 2 4F TR A6WE 2008012400033 20080124 00033 SO 2008 1 24 FDKA200712390 1 20071208 A 2750 3634001019 SHAFT EMB 145 EMB145LR 3260212 SO TE FLAPS FAILED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 11821 145416 FDM RON RIC (1901 PHX LCL) - FLAPS FAILED AT 45 DEGREES. MX REMOVED AND REPLACED RT FLAP FLEX SHAFT. 2 L 7 2 4T RT T00011AT 2008012400185 20080124 00185 NM 2008 1 24 USAA920080152 1 20071220 A 5210 INTERCOSTAL BOEING 757 757225 1384959 NM R2 DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 22198 PIT - MAJOR REPAIR - C4 CHECK - THE R2 DOOR HAS A CRACKED INTERCOSTAL, BS 660, AT THE NR 4 DOOR STOP AREA. REPLACED THE R2 DOOR INTERCOSTAL, BS 660, AT THE NR 4 DOOR STOP AREA IAW USAIRWAYS EO 5304R143. 2 L 7 2 4F RT A2NM 2008012400202 20080124 00202 EU 2008 1 24 USAA920080174 1 20071223 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 624AW * * 55 SAL - EEL - C6 CHECK - ROW 10 EMERGENCY LIGHTS DID NOT ILLUMINATE DURING OPERATIONAL TEST. REPLACED AND FUNCTIONAL CHEC KED MIDDLE POWER SUPPLY IAW A320 AMM 33-51-00. 2 L 7 2 4F RT A28NM 2008012400239 20080124 00239 SO 2008 1 24 FDKA200708355 1 20070801 A 5240 DOOR EMB 145 EMB145LR 3260212 SO LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 FDM 6001 MCO (0601 PHX LCL) - SERVICE DOOR WON'T CLOSE FROM INSIDE. MX LUBED SERVICE DOOR, OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012400240 20080124 00240 SO 2008 1 24 FDKA200708356 1 20070801 A 2697 CONNECTOR EMB 145 EMB145LR 3260212 SO FIRE BOTTLE UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 855MJ 145614 FDM 5993 MCO (0630 PHX LCL) - BAGGAGE FIRE BOTTLE CAUTION MSG. MX CLEANED CONNECTOR AND RE-SECURED ON CARGO FIRE BOTTLE S, OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012400242 20080124 00242 2008 1 24 FDKA200709448 4 20070907 A 2220 4006719906MOD SERVO EMB 145 EMB145LR 3260212 SO AILERONS FAILED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 831MJ 14852 145273 FDM FLT 6201 FLL - YAW DAMP/AUTOPILOT FAIL. REMOVED AND REPLACED AILERON SERVO. 2 L 7 2 4T RT T00011AT 2008012400245 20080124 00245 SO 2008 1 24 FDKA200709457 1 20070909 A 2731 3621001013 CONTROL UNIT EMB 145 EMB145LR 3260212 SO PITCH TRIM INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 7040 145179 FDM FLT RON MCO - PITCH TRIM MAIN AND STANDBY SYSTEM INOPERATIVE. MX REPLACED THE HSCU AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2008012400246 20080124 00246 SO 2008 1 24 FDKA200712392 1 20071210 A 5270 WARNING LIGHT EMB 145 EMB145LR 3260212 SO PAX DOOR FALSE ACTIVATION A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 855MJ 145614 FDM 6057 PNS (0722 PHX LCL) - EICAS INDICATION PAX DOOR OPEN WITH DOOR CLOSED. MX TROUBLESHOT AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012400248 20080124 00248 SO 2008 1 24 FDKA200704163 1 20070401 A 5320 14524131011 THRESHOLD EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 848MJ 145530 ANGLES AT PASSENGER DOOR THRESHOLD ARE CORRODED OUT OF LIMITS. REMOVED AND REPLACED ANGLES WITH NEW PARTS. 2 L 7 2 4T RT T00011AT 2008012400249 20080124 00249 SO 2008 1 24 FDKA200711315 1 20071104 A 2121 011768500 FAN EMB 145 EMB145LR 3260212 SO CARGO BAY FAILED A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 852MJ 145567 FDM FLT 6067 BHM (0725 PHX LCL) - BAG SMOKE TEST LIGHT STAYS ILLUMINATED. REMOVED AND REPLACED BAG FAN AND SMOKE RELAYS . 2 L 7 2 4T RT T00011AT 2008012400250 20080124 00250 SO 2008 1 24 FDKA200708399 1 20070819 A 5320 SILL EMB 145 EMB145LR 3260212 SO PAX DOORWAY LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 837MJ 145367 FDM 6131 MCO (1015 PHX LCL) - MAIN CABIN DOOR HARD TO CLOSE. MX LUBED DOOR SILLS. 2 L 7 2 4T RT T00011AT 2008012400258 20080124 00258 SO 2008 1 24 FDKA200712379 1 20071204 A 5210 DOOR EMB 145 EMB145LR 3260212 SO LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 145416 FDM 6158 RDU - CREW REPORTS THAT THE MAIN CABIN DOOR IS HARD TO OPEN. MX CLEANED AND LUBED. OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012400260 20080124 00260 SO 2008 1 24 FDKA200705246 1 20070525 A 5350 14530398001 LATCH EMB 145 EMB145LR 3260212 SO RADOME CRACKED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 831MJ 145273 RADOME LATCH HOUSINGS ARE CRACKED. THE DAMAGED PARTS HAVE BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2008012400262 20080124 00262 SO 2008 1 24 FDKA200708361 1 20070802 A 3010 3801D2C CONTROLLER EMB 145 EMB145LR 3260212 SO WINDSHIELD HEAT ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 825MJ 46 145179 FDM 6201 FLL-TLH (0528 PHX LCL) - DIVERT TO MCO DUE TO A STRONG ELECTRICAL BURNING ODOR WITH NO VISUAL SMOKE WHEN WINDSH IELD HEAT ON. MX INSPECTED WIRING FOR BURNED WIRES, NO DEFECTS FOUND. MX REMOVED AND REPLACED WINDSHIELD 2 HEAT CONTRO LLER AND CONTACTOR, NO FURTHER ELECTRICAL ODOR. 2 L 7 2 4T RT T00011AT 2008012400263 20080124 00263 SO 2008 1 24 FDKA200708368 1 20070803 A 5320 SILL EMB 145 EMB145LR 3260212 SO PAX DOORWAY LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM 6092 MCO - PAX DOOR DIFFICULT TO CLOSE. MX LUBED DOOR SILL, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012400264 20080124 00264 SO 2008 1 24 FDKA200709455 1 20070907 A 2720 RUDDER CONTROL EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 833MJ 145327 FDM FLT 6190 JFK-ROC - RUDDER HARDOVER PROTECT FAIL. MX PERFORMED ELECTRICAL RESET, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012400265 20080124 00265 SO 2008 1 24 FDKA200709456 1 20070908 A 2730 ELEVATOR EMB 145 EMB145LR 3260212 SO DISCONNECTED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 842MJ 145457 FDM FLT 6129 RDU - ELEVATOR DISCONNECTED. MX RECONNECTED ELEVATORS, OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012400266 20080124 00266 SO 2008 1 24 FDKA200708369 1 20070803 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM RON MCO (1730 PHX LCL) - PAX DOOR DIFFICULT TO CLOSE. MX CLEANED AND LUBED DOOR. 2 L 7 2 4T RT T00011AT 2008012400267 20080124 00267 SO 2008 1 24 FDKA200708371 1 20070804 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM 6157 MCO (1050 PHX LCL) - MAIN CABIN DOOR DIFFICULT TO CLOSE. MX RE-SECURED DOOR SEAL LOOSE AT RT CORNER AND CLEANE D AND LUBED THE DOOR ROLLERS. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012400268 20080124 00268 SO 2008 1 24 FDKA200708372 1 20070804 A 5270 SWITCH EMB 145 EMB145LR 3260212 SO CARGO DOOR OUT OF ADJUST A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 833MJ 145327 FDM 9700 BNC (1226 PHX LCL) - AFT CARGO DOOR WARNING DURING T/O ROLL. MX ADJUSTED AFT CARGO DOOR WARNING SWITCH. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012400269 20080124 00269 SO 2008 1 24 FDKA200708373 1 20070805 A 5210 HINGE EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM 6003 JFK (0550 PHX LCL) - MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. MX ADJUSTED TOP DOOR ROLLERS. LUBED DOOR H INGES. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012400270 20080124 00270 SO 2008 1 24 FDKA200711321 1 20071107 A 2731 TRIM SYSTEM EMB 145 EMB145LR 3260212 SO PITCH INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 835MJ 145353 FDM 6064 BHM (0430 PHX LCL) - PITCH TRIM MAIN INOP. MX RESET SYSTEM, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008012400280 20080124 00280 SO 2008 1 24 FDKA200710522 1 20071005 A 2910 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO NR 2 HYD SYS UNSECURE A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 844MJ 145481 FDM 6201 FLL (0339 PHX LCL) - NO RUDDER SYSTEM 2 INOP MESSAGE WITH HYDRAULIC SYSTEM OFF. MX RE-SECURED RUDDER 2 PRESSUR E SWITCH, OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012400282 20080124 00282 SO 2008 1 24 FDKA200710507 1 20071005 A 3010 DUCT EMB 145 EMB145LR 3260212 SO ANTI ICE SYS FAILED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 853MJ 145464 FDM 6021 JFK (0839 PHX LCL) - AILERON CONTROLS STICKING. MX FOUND BLOWN DUCT ON PACK CAUSING ICE BUILD UP. REMOVED AND REPLACED DUCT, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012400283 20080124 00283 SO 2008 1 24 FDKA200711322 1 20071107 A 2750 3631001011 CONTROL UNIT EMB 145 EMB145LR 3260212 SO TE FLAPS MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 6507 145507 FDM 6074 JFK (1415 PHX LCL) - FLAP LOW SPEED MESSAGE. MX REPLACED FLAP FECU. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012400284 20080124 00284 SO 2008 1 24 FDKA200708434 1 20070830 A 2741 COMPUTER EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 830MJ 145259 SPS 1 AND 2 INOP ON EICAS. RE-RACKED SPS COMPUTER, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012400285 20080124 00285 SO 2008 1 24 FDKA200708435 1 20070831 A 2731 CONTROL CABLE EMB 145 EMB145LR 3260212 SO ELEVATORS OUT OF RIG A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 853MJ 145464 ELEVATOR CABLES BINDING. INSPECTED CABLES AND RIGGING, NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008012400289 20080124 00289 SO 2008 1 24 FDKA200709443 1 20070904 A 2150 8152403 ACM EMB 145 EMB145LR 3260212 SO NR 2 OVERHEATED A FDKA O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 07 830MJ 10823 16529 SMOKE IN THE CABIN AFTER T/O. FOUND PACK 2 TO BE OVERHEATING, REMOVED AND REPLACED NR 2 ACM. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008012400290 20080124 00290 SO 2008 1 24 FDKA200711349 1 20071127 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INTERMITTENT A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6078 FLL - CABIN CENTER EMERGENCY LIGHT INOP. MX PERFORMED, OPS CHECKS UNABLE TO DUPLICATE PROBLEM. 2 L 7 2 4T RT T00011AT 2008012400294 20080124 00294 SO 2008 1 24 FDKA200712370 1 20071202 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 145416 FDM 6055 TPA (1100 PHX LCL) - AFT EMERGENCY LIGHTS INOP AND ALL EXIT SIGNS. MX OPS CHECKED NORMAL, NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008012400297 20080124 00297 2008 1 24 FDKA200709446 2 20070905 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO NR 1 SHUTDOWN A FDKA O OTHER Y ENGINE STOPPAGE NR NOT REPORTED 1 SW 07 838MJ 145384 FDM FLT 6040 FLL - RUDDER HARD OVER FAIL WITH ENGINE 1 ON ENGINE SHUT DOWN. MX PERFORMED RESET AND RAN ENGINE, MESSAGE CLEARED. 2 L 7 2 4T RT T00011AT 2008012400298 20080124 00298 SO 2008 1 24 FDKA200709447 1 20070905 A 3150 WARNING LIGHT EMB 145 EMB145LR 3260212 SO SPEED BRAKE ILLUMINATED A FDKA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 830MJ 145259 FDM FLT 6207 MHT- JFK - SPEED BRAKE DISAGREE IN FLIGHT. RESET, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012400302 20080124 00302 SO 2008 1 24 FDKA200710530 1 20071008 A 2621 GROMMET EMB 145 EMB145LR 3260212 SO FIRE BOTTLE TORN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 FDM 6053 TPA (0341 PHX LCL) - NR 2 ENGINE FIRE BOTTLE T-HANDLE GROMMET TORN. MX REPAIRED. 2 L 7 2 4T RT T00011AT 2008012400303 20080124 00303 SO 2008 1 24 FDKA200709444 1 20070904 A 3150 WARNING MESSAGE EMB 145 EMB145LR 3260212 SO FALSE ACTIVATION A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 835MJ 145353 SPS 1 INOP AND SPS ADVANCED INOPERATIVE EICAS MESSAGE. MX RESET AND FOUND TO BE TRANSITIONING CONDITION. MESSAGE CLEAR ED AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012300249 20080123 00249 SO 2008 1 23 FDKA200711337 1 20071118 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 840MJ 145429 FDM 6054 ATL-NAS (1600 PHX LCL) EMERGENCY FLOOR LIGHTING INOP AFT OF ROW 3. MX PERFORMED, OPS CHECKS OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012300250 20080123 00250 SO 2008 1 23 FDKA200711338 1 20071119 A 3350 1317 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 829MJ 145228 FDM 6106 MCO - EMERGENCY LIGHT AT ROW 11 CENTER AISLE INOP. MX REMOVED AND REPLACED LAMP, OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012300252 20080123 00252 SO 2008 1 23 FDKA200708427 1 20070828 A 5210 21060017001 ROD EMB 145 EMB145LR 3260212 SO PAX DOOR OUT OF RIG A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM 6184 JFK (0457 PHX LCL) - PAX DOOR HARD TO OPEN. MX REMOVED AND REPLACED ROD AND BOLT RIGGED DOOR. 2 L 7 2 4T RT T00011AT 2008012300259 20080123 00259 NM 2008 1 23 ZZDA2008013 1 20070816 A 3350 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 980AT 55039 AFT ACCESSORY COMPT O/H EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY & SUPPLY AT RIGHT AFT LAV R EF MM 33-51. OP'S CHECK NORMAL. 2 L 7 2 4F TR A6WE 2008012400011 20080124 00011 SO 2008 1 24 FDKA200708415 1 20070821 A 2720 K0112 RELAY EMB 145 EMB145LR 3260212 SO RUDDER SYS FAILED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 FDM 6155 MCO (0715 PHX LCL) - RUDDER HARD OVER FAIL. MX REMOVED AND REPLACED RELAY K0112. 2 L 7 2 4T RT T00011AT 2008012400016 20080124 00016 NM 2008 1 24 ZZDA2008017 1 20070603 A 3350 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 923AT 55051 EMERGENCY LIGHTS INOP LOWER NR 2 GALLEY AND 1ST CLASS. REMOVED AND REPLACED POWER PACK ASSY AT STA 341, OPS CHECKED GOO D REF AMM 33-51. 2 L 7 2 4F TR A6WE 2008012400020 20080124 00020 SO 2008 1 24 FDKA200711306 1 20071102 A 3150 WARNING MESSAGE EMB 145 EMB145LR 3260212 SO FALSE ACTIVATION A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 859MJ 145769 FRL FLT 6089 MCO (0635 PHX LCL) - SPS ADVANCE MESSAGE. MX RESET 2 L 7 2 4T RT T00011AT 2008012400034 20080124 00034 2008 1 24 FDKA200709483 4 20070923 A 3418 0020BN4 COMPUTER EMB 145 EMB145LR 3260212 SO STALL WARNING FAILED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 836MJ 12285 145359 FDM 6055 TPA (0930 PHX LCL), STICK PUSHER FAIL MSG. MX REMOVED AND REPLACED SPC. 2 L 7 2 4T RT T00011AT 2008012400035 20080124 00035 NM 2008 1 24 FDKA200707323 1 20070704 A 5210 ARM DHAV DHC8 DHC8101 2809002 NM PAX DOOR BROKEN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 806LR 093 FDM 6023 JFK (1746 PHX LCL) - PASSENGER DOOR LT ARM BROKEN. MX RESECURED. 2 H 7 2 4T RT A13NM 2008012400038 20080124 00038 NM 2008 1 24 ZZDA2008021 1 20070819 A 3350 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 932AT 55073 EMERGENCY LIGHTS AT SEAT 11-19 INOPERATIVE. EMERGENCY LIGHT BATTERY SUPPLY ASSY WAS REMOVED AND REPLACED AS PER AMM 33- 51. OPS CHECK NORMAL. 2 L 7 2 4F TR A6WE 2008012400039 20080124 00039 SO 2008 1 24 FDKA200707324 1 20070706 A 3350 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6146 GPT-ATL (0642 PHX LCL) - EMERGENCY EXIT SIGN LOOSE. MX RESECURED SIGN. 2 L 7 2 4T RT T00011AT 2008012400041 20080124 00041 NM 2008 1 24 ZZDA2008023 1 20070813 A 3350 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 932AT 55073 ROWS 1, 2, 3, 10 EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED NR 4 BATTERY SUPPY PACK IAW MM 33-51. 2 L 7 2 4F TR A6WE 2008012400043 20080124 00043 NM 2008 1 24 ZZDA2008025 1 20071006 A 3350 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 928AT 55076 THE EMERGENCY LIGHT ARE INOP FROM ROW 10 AND ALL OF BUSINESS CLASS, LIGHTS AT FLOOR 2 EA NR 3 GALLEY SIDE WALL AND WALL LIGHTS AT L1-DOOR AND R1 DOOR, THERE'S ONE BULB OUT IN WALL ALL FWD RT OVERWING EXIT. REMOVED AND REPLACED 2 EA EMERGEN CY LIGHT BATTERY PACKS LOCATED AT STA 398 & 803. OPS CHECK GOOD, ALL WORK PERFORMED IAW B717 AMM 33-51. 2 L 7 2 4F TR A6WE 2008012400045 20080124 00045 NM 2008 1 24 ZZDA2008027 1 20070423 A 3350 8039251 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 986AT 55089 FIRST CLASS ROWS 1, 2 AND 3 EMERGENCY LIGHTS OUT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT P-118 PER AMM CH 33-51, OP'S CHECKED GOOD. 2 L 7 2 4F TR A6WE 2008012400054 20080124 00054 NM 2008 1 24 2007UALA05389 1 20071228 A 5532 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE VERTICAL STAB DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 VERTICAL FIN DAMAGED ON CONTACT WITH HANGAR DOOR. PERFORMED A MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012400224 20080124 00224 SO 2008 1 24 FDKA200710534 1 20071009 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6150 TYS-CVG (0250 PHX LCL), EMERGENCY EXIT LIGHTS AT ROW 12 INOP. MX CHECKED CONNECTOR ON EMERGENCY LIGHTS, NO DEF ECTS NOTED. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012400238 20080124 00238 NM 2008 1 24 FDKA200705182 1 20070504 A 3230 841005 ELECTRONIC UNIT DHAV DHC8 DHC8101 2809002 NM MLG MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 808LR 46124 073 FDM 6144 BWI-JFK (1103 PHX LCL) - CREW REPORTED THE NOSE POS IND LIGHT ILLUMINATED GEAR DIS LIGHT CAME ON DURING FLIGHT AND THE WOW FAIL LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED PSEU. 2 H 7 2 4T RT A13NM 2008012400241 20080124 00241 SO 2008 1 24 FDKA200709494 1 20070905 A 5320 SUPPORT EMB 145 EMB145LR 3260212 SO FAIRING CRACKED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 WING TO FUSELAGE FAIRING SUPPORT STRUCTURE ON THE RT FUSELAGE IS CRACKED BETWEEN FRAME NR 48 AND NR 49. REPAIRED DAMAGE . 2 L 7 2 4T RT T00011AT 2008012400259 20080124 00259 SO 2008 1 24 FDKA200709439 1 20070901 A 2731 SWITCH EMB 145 EMB145LR 3260212 SO PITCH TRIM LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 847MJ 145517 BACK UP PITCH TRIM DOWN NOT WORKING. LUBED SWITCH, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008012400278 20080124 00278 SO 2008 1 24 FDKA200708363 1 20070802 A 2760 825701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO SPOILERS MALFUNCTIONED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 832MJ 15533 145310 FDM 6134 MCO (1420 PHX LCL) - SPOILER FAIL MESSAGE IN FLIGHT AND ON LANDING. MX REMOVED AND REPLACED PROX SWITCH. 2 L 7 2 4T RT T00011AT 2008012400291 20080124 00291 SO 2008 1 24 FDKA200712363 1 20071201 A 3350 20131ASMI CHARGER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 82 145217 FDM 6101 CLT (0351 PHX LCL) - LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. MX REMOVED AND REPLACED BATTERY AND C HARGER. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012400325 20080124 00325 2008 1 24 FDKA200712374 4 20071202 A 3418 WARNING LIGHT EMB 145 EMB145LR 3260212 SO STALL WARNING ILLUMINATED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 841MJ 145448 FDM 6118 MCO (1218 PHX LCL) - STICK PUSHER FAIL ON EICAS. MX RESET, SYSTEM OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012400329 20080124 00329 SO 2008 1 24 FDKA200711360 1 20071129 A 2741 CONTROL UNIT EMB 145 EMB145LR 3260212 SO ROLL TRIM MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 833MJ 145327 FDM 5970 ATL (2007 PHX LCL) - ROLL TRIM ON BACKUP PANEL WON’T ROLL TO THE RIGHT. MX REMOVED AND REPLACED PANEL AND RESE T HSCU. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012400341 20080124 00341 SO 2008 1 24 FDKA200711362 1 20071130 A 2760 WARNING LIGHT EMB 145 EMB145LR 3260212 SO SPEED BRAKES ILLUMINATED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 828MJ 145218 FDM 6087 JFK (1122 PHX LCL) - SPEED BRAKE DISAGREE. MX TROUBLESHOT AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012400343 20080124 00343 2008 1 24 FDKA200712366 4 20071202 A 3418 VANE EMB 145 EMB145LR 3260212 SO AOA MALFUNCTIONED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 844MJ 145481 FDM 6040 FLL (0007 PHX LCL). SPS ADVANCED AND FAIL MESSAGES. MX REMOVED AND REPLACED BOTH AOA VANES. 2 L 7 2 4T RT T00011AT 2008012400346 20080124 00346 SO 2008 1 24 FDKA200703143 1 20070320 A 5350 PANEL EMB 145 EMB145LR 3260212 SO OVERWING CRACKED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 847MJ 145517 UPPER FLANGE FOR FUSELAGE OVERWING PANEL NR 194 IS CRACKED. THE DAMAGE HAS BEEN REPAIRED. 2 L 7 2 4T RT T00011AT 2008012400348 20080124 00348 SO 2008 1 24 FDKA200712395 1 20071211 A 2611 DCU EMB 145 EMB145LR 3260212 SO SMOKE DETECTOR MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 847MJ 145517 FDM 6015 JFK-ORF (2100 PHX LCL) - LAV SMOKE INDICATION IN FLIGHT. MX REMOVED AND REPLACED DCU, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012400349 20080124 00349 SO 2008 1 24 FDKA200705224 1 20070526 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6200 NAS-ATL (0726 PHX LCL) - SMELL OF FUEL WITH APU START. MX OPS CHECKED APU, NO FUEL LEAKS OR ODOR FOUND. 2 L 7 2 4T RT T00011AT 2008012400350 20080124 00350 SO 2008 1 24 FDKA200707350 1 20070729 A 3230 K0642 RELAY EMB 145 EMB145LR 3260212 SO MLG MALFUNCTIONED A FDKA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 827MJ 145217 FDM 6147 TLH (1025 PHX LCL) - LANDING GEAR FAILED TO RETRACT ON T/O. FERRY AIRCRAFT TO MCO WHERE MX REMOVED AND REPLACE D K0642 RELAY. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012400352 20080124 00352 SO 2008 1 24 FDKA200707352 1 20070731 A 2560 MXP21000 SMOKE GOGGLES EMB 145 EMB145LR 3260212 SO COCKPIT MISSING A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 848MJ 145530 FDM 6148 MCO (0646 PHX LCL) - OBSERVER SMOKE GOGGLES MISSING. MX INSTALLED OBSERVER SMOKE GOGGLE. 2 L 7 2 4T RT T00011AT 2008012400373 20080124 00373 EU 2008 1 24 USAA920080181 1 20071225 A 5347 D53112815200 SEAT TRACK AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 885 CLT - MAJOR REPAIR - RON, PILOT REPORT - CORROSION ON CABIN SEAT TRACK, BS 605 / FR 12 - BS 950 / FR 24, +Y1292. REPLAC ED CABIN SEAT TRACK, BS 605 / FR 12 - BS 950 / FR 24, +Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008012400375 20080124 00375 NM 2008 1 24 USAA920080183 1 20071219 A 5320 STIFFENER BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 175AW 23634 CLT - MAJOR REPAIR - CRACKED VERTICAL STIFFENER, WING CENTER SECTION, BS 663.75, RBL 6.25. REPAIRED VERTICAL STIFFENER, WING CENTER SECTION, BS 663.75, RBL 6.25 IAW USAIRWAYS EA 110301. 2 L 7 2 4F RT A16WE 2008012500027 20080125 00027 SO 2008 1 25 FDKA200712375 1 20071203 A 3350 BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM RON MCO (0114 PHX LCL). LT AND RT OVERWING LIGHTS INOP. MX REMOVED AND REPLACED NR 4 BATTERY PACK AND CHARGER. 2 L 7 2 4T RT T00011AT 2008012500030 20080125 00030 SO 2008 1 25 FDKA200710298 1 20071030 A 5210 SEAL EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 145416 FDM 6114 RDU (0451 PHX LCL) - MAIN CABIN DOOR HARD TO OPEN AND CLOSE. MX LUBED DOOR SEAL. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012500031 20080125 00031 SO 2008 1 25 FDKA200711323 1 20071107 A 2731 SWITCH EMB 145 EMB145LR 3260212 SO PITCH TRIM INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 832MJ 145310 FDM 6079 TLH (1659 PHX LCL) - CAPT’S PITCH TRIM INOPERATIVE IN UP POSITION. CONTRACT MX CLEANED YOKE SWITCH AND OPS CHE CKED. 2 L 7 2 4T RT T00011AT 2008012500032 20080125 00032 SO 2008 1 25 FDKA200710302 1 20071030 A 2720 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO RUDDER INOPERATIVE A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 837MJ 145367 FDM 6005 MCO (0925 PHX LCL) - RUDDER SYSTEM 1 AND 2 INOP MESSAGE IN FLIGHT. MX REMOVED AND REPLACED NR 2 SYS RUDDER PRE SS SWITCH. 2 L 7 2 4T RT T00011AT 2008012500033 20080125 00033 SO 2008 1 25 FDKA200712369 1 20071202 A 2760 WARNING MESSAGE EMB 145 EMB145LR 3260212 SO SPOILERS FALSE ACTIVATION A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 838MJ 145384 FDM 6021 JFK (0940 PHX LCL) - SPOILER FAIL MESSAGE. MX RESET SYSTEM, MESSAGE CLEARED. 2 L 7 2 4T RT T00011AT 2008012500034 20080125 00034 2008 1 25 FDKA200710301 4 20071030 A 3418 K0031 RELAY EMB 145 EMB145LR 3260212 SO STALL WARNING FAILED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 834MJ 145340 FDM 6142 MCO (0758 PHX LCL) - SPS ADVANCED MSG, AFTER GEAR RETRACTION. MESSAGE STAYS ON UNTIL GEAR EXTENSION. MX REMOV ED AND REPLACED RELAY K0031, K0571, K0026, K0325, K0354, K0572, K0027, K0030. 2 L 7 2 4T RT T00011AT 2008012500040 20080125 00040 SO 2008 1 25 FDKA200708423 1 20070825 A 3250 12302328407 TILLER EMB 145 EMB145LR 3260212 SO NLG STEERING MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 858MJ 145767 FDM 6185 BWI - ABORTED TAKEOFF DUE TO SEVERE UNCOMMANDED SWERVING BETWEEN 50 AND 80 KNOTS. MX REPLACED TILLER AND PERFO RMED HIGH SPEED TAXI, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012500042 20080125 00042 2008 1 25 FDKA200710296 4 20071030 A 3418 111642116 COMPUTER EMB 145 EMB145LR 3260212 SO STALL WARNING FAILED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 860MJ 8739 145773 FDM 6016 JFK (1000 PHX LCL) - SPS INOP/SP FAIL/CDU DATA BUSS FAIL. MX REMOVED AND REPLACED FMS COMPUTER AND UPLOADED DA TA. 2 L 7 2 4T RT T00011AT 2008012500043 20080125 00043 SO 2008 1 25 FDKA200708420 1 20070824 A 3244 31551 TIRE EMB 145 EMB145LR 3260212 SO NLG DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 858MJ 6052 145767 FDM 6038 CLT - ABORTED TAKEOFF DUE TO UNCOMMANDED SWERVING ON TAKEOFF ROLL. MX REPLACED THE NOSE TIRES AND TAXI CHECKED WITH THE CREW. 2 L 7 2 4T RT T00011AT 2008012500049 20080125 00049 SO 2008 1 25 FDKA200709476 1 20070918 A 3150 FADEC EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 838MJ 145384 FDM 6080 MCO (1336 PHX LCL) - RUDDER HARD OVER PROTECTION. RESET FADEC AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2008012800003 20080128 00003 SO 2008 1 28 FDKA200712409 1 20071217 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 FDM 6093 ROC (0620 PHX LCL) - LT WING EMERGENCY EXIT SIGN INOP. MX RESECURED EMERGENCY LIGHT CONNECTOR AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012800005 20080128 00005 GL 2008 1 28 FDKA200709454 2 20070907 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 HUNG START A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 833MJ 145327 FFDM FLT 6190 JFK-ROC RETURNED TO GATE DUE TO ENGINE 1 HUNG START. MX RESET FADEC, OPS CHECK GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008012800006 20080128 00006 SO 2008 1 28 FDKA200707334 1 20070709 A 2750 BRAKE EMB 145 EMB145LR 3260212 SO RT FLAP XMSN FAILED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 830MJ 15243 145259 FDM RON MCO - RT FLAP TRANSMISSION BRAKE FAILED 5A CHECK. MX REPLACED THE RIGHT FLAP TRANSMISSION BRAKE AND OPS CHECKED . 2 L 7 2 4T RT T00011AT 2008012800007 20080128 00007 SO 2008 1 28 FDKA200712386 1 20071207 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 849MJ 145534 FDM 6061 MCO (0640 PHX LCL) - PAX DOOR HARD TO OPEN AND CLOSE. MX CLEANED AND LUBED. OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012800010 20080128 00010 SO 2008 1 28 FDKA200710289 1 20071029 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 848MJ 145530 FDM 6075 MCO (0933 PHX LCL) - MAIN DOOR HARD TO CLOSE. MX LUBED DOOR OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012800011 20080128 00011 SO 2008 1 28 FDKA200710290 1 20071029 A 5210 BUSHING EMB 145 EMB145LR 3260212 SO PAX DOOR DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 853MJ 145464 FDM 6170 MCO (1000 PHX LCL) - MAIN CABIN DOOR BINDING. MX REMOVED AND REPLACED BUSHINGS ON HINGE ARM OF DOOR. 2 L 7 2 4T RT T00011AT 2008012800012 20080128 00012 SO 2008 1 28 FDKA200710546 1 20071013 A 2760 852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO SPOILERS UNKNOWN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 14610 145179 FDM RON MCO - SPOILER FAIL DURING TEST FLIGHT. MX RIGGED LT GROUND SPOILER AND INSTALLED PROX SWITCH AND RT OB SPEED BR AKE HANDLE. 2 L 7 2 4T RT T00011AT 2008012800014 20080128 00014 SO 2008 1 28 FDKA200707335 1 20070710 A 5210 STOP EMB 145 EMB145LR 3260212 SO PAX DOOR LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6081 CAE - MAIN CABIN DOOR WOULD NOT CLOSE. MX FOUND LOOSE DOOR STOP TIGHTENED IT AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2008012800017 20080128 00017 SO 2008 1 28 FDKA200710556 1 20071018 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 FDM 6016 JFK (1229 PHX LCL) MAIN CABIN DOOR STICKS AND IS HARD TO OPEN, MX LUBED DOOR OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012800019 20080128 00019 SO 2008 1 28 FDKA200712424 1 20071229 A 3097 CONNECTOR EMB 145 EMB145LR 3260212 SO PRESSURE SWITCH DIRTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 FDM FLT 6107 ALB (0548 PHX LCL) - ABORTED T/O DUE TO WING/STAB ANTI-ICE FAIL. MX CLEANED AND RESEATED NR 1 AND NR 2 WIN G ANTI-ICE LOW PRESSURE SWITCHES AND OPS CHECKED SYSTEM, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800020 20080128 00020 SO 2008 1 28 FDKA200708382 1 20070812 A 3610 M832481152 O-RING EMB 145 EMB145LR 3260212 SO BLEED DUCT DAMAGED A FDKA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 07 829MJ 145228 FDM 6184 JFK (0745 PHX LCL) - ABORTED T/O DUE TO A BLEED 1 LEAK ON T/O ROLL, X-FEED VALVE OPEN. MX REPLACED BLEED DUCT O-RINGS. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800022 20080128 00022 SO 2008 1 28 FDKA200708389 1 20070815 A 2750 CONTROL UNIT EMB 145 EMB145LR 3260212 SO TE FLAPS MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 852MJ 145567 FDM 6161-ATL-LEX (1541 PHX LCL) - FLAPS FAIL CAUTION AT 41 DEGREES. MX RESET FECU, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012300237 20080123 00237 NM 2008 1 23 2008UALA0025 1 20071230 A 2730 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE UNKNOWN A UALA O OTHER W INADEQUATE Q C TO TAKEOFF 1 WP 29 518UA 24871 FIRST OFFICER'S ELEVATOR CONTROLS FEEL HEAVY. CREW COMMENTS: ELEVATOR VERY HEAVY ON T/O. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012300245 20080123 00245 SO 2008 1 23 FDKA200710281 1 20071027 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6050 CVG (1337 PHX LCL) - ROW 12 OVERHEAD FORWARD EMERGENCY LIGHT INOP. MX RESECURED EMERGENCY LIGHT CONNECTORS, OP S CK GOOD. 2 L 7 2 4T RT T00011AT 2008012300246 20080123 00246 SO 2008 1 23 FDKA200711307 1 20071102 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FDM FLT 6034 MCO (1447 PHX LCL) - EMERGENCY LIGHT AT ROW 12 B/C NOT ILLUMINATED. MX RE-SET LIGHT, OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012300247 20080123 00247 SO 2008 1 23 FDKA200711309 1 20071103 A 3350 B6245 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 829MJ 145228 FDM FLT 6010 MCO (0558 PHX LCL) - ROW 12 OVERHEAD EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED LIGHT ASSY. 2 L 7 2 4T RT T00011AT 2008012300248 20080123 00248 SO 2008 1 23 FDKA200711310 1 20071103 A 3350 7277126503 SWITCH EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 854MJ 145490 FDM FLT 6091 FLL (1104 PHX LCL) - FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH INOP. MX REMOVED AND REPLACED CONTROL PANEL. 2 L 7 2 4T RT T00011AT 2008012400017 20080124 00017 SO 2008 1 24 FDKA200711308 1 20071102 A 5210 SWITCH EMB 145 EMB145LR 3260212 SO PAX DOOR OUT OF ADJUST A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FRL RON MCO (1626 PHX LCL) - MAIN CABIN DOOR DIFFICULT TO OPERATE. ADJUSTED LOCK OPEN SWITCH. 2 L 7 2 4T RT T00011AT 2008012400018 20080124 00018 NM 2008 1 24 ZZDA2008018 1 20070814 A 3350 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 993AT 55137 EPL INOP AT ROWS 1-10. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSY AT POS NR 4 EPL, OPS OK M/M 33-51. 2 L 7 2 4F TR A6WE 2008012400021 20080124 00021 NM 2008 1 24 ZZDA2008019 1 20070426 A 3350 8039251 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 998AT 55142 ON EMERGENCY LIGHT TEST THE LIGHTS ON SIDE WALLS AT L1-DOOR, R1-DOOR AND THE TWO LIGHTS AT FLOOR ON RT GALLEY AND THE LI GHTS ON SEAT ROWS 1D, 2D, 3D, AND 10D ARE ALL INOPERATIVE. REMOVED & REPLACED BATTERY SUPPLY ASSY AND BATTERY REF AMM 3 3-51-03, OPS CHECKED GOOD. 2 L 7 2 4F TR A6WE 2008012400022 20080124 00022 SO 2008 1 24 FDKA200712388 1 20071207 A 2611 SMOKE WARNING EMB 145 EMB145LR 3260212 SO LAVATORY FALSE ACTIVATION A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 858MJ 145767 FDM 6145 JFK - LAV SMOKE WARNING IN FLIGHT. MX TROUBLESHOT AND COULD NOT DUPLICATE. 2 L 7 2 4T RT T00011AT 2008012400042 20080124 00042 NM 2008 1 24 ZZDA2008024 1 20070625 A 3350 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 932AT 55073 EMERGENCY LIGHTS AT R-1 DOOR INOP (CEILING). REMOVED AND REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSEMBLY. OPS CHECKED NORMAL. REF AMM 33-51. 2 L 7 2 4F TR A6WE 2008012400047 20080124 00047 NM 2008 1 24 ZZDA2008029 1 20070801 A 3350 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 986AT 55089 EPLS ON SEATS 25-31 NOT COMING ON. REMOVED AND REPLACED BATTERY SUPPLY ASSY AT B5-119. OPS CHECK GOOD, REF AMM 33-51. 2 L 7 2 4F TR A6WE 2008012400049 20080124 00049 NM 2008 1 24 ZZDA2008031 1 20070922 A 3350 FUSE BOEING 737 7377BD 1384511 NM CABIN BLOWN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 290AT 33925 LEFT EMERGENCY EXIT WINDOW LIGHT INOP. RELAMPED AND REMOVED AND REPLACED FUSE REF AMM 33-21. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2008012400108 20080124 00108 SO 2008 1 24 FDKA200709481 1 20070922 A 5524 BONDING JUMPER EMB 145 EMB145LR 3260212 SO ELEVATOR OUT OF POSITION A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 853MJ 145464 FDM 6041 JFK (1733 PHX LCL) - ELEVATOR FLIGHT CONTROLS BINDING/GRINDING IN FORWARD AND AFT MOVEMENT. MX RE-POSITIONED B ONDING JUMPER UNDER COCKPIT FLOOR ON ELEVATOR CONNECTING ROD. 2 L 7 2 4T RT T00011AT 2008012400109 20080124 00109 NM 2008 1 24 ZZDA2008034 1 20071115 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 958AT 55020 TWO DENTS FOUND AFT OF L1 DOOR APPROXIMATELY STATION 235.5 LONGERON 16L. INSTALLED PERMANENT FLUSH REPAIR AT STA 235.5 AND BETWEEN LONGERON 16 AND 17 LEFT IAW B717 SRM 53-00-01 FIG 204. DIMENSIONS OF REPAIR 8.25 X 7.25 INCH. 2 L 7 2 4F TR A6WE 2008012400220 20080124 00220 SO 2008 1 24 FDKA200710526 1 20071006 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 853MJ 145464 FDM 6023 JFK (0512 PHX LCL) - OVERWING EMERGENCY EXIT FLOOR PROXIMITY LIGHTS STRIP AT ROW 12 INOPERATIVE. MX REPAIRED T HE CONNECTORS WIRE AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2008012400222 20080124 00222 SO 2008 1 24 FDKA200710528 1 20071007 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6011 JFK (6011 PHX LCL) - EMERGENCY EXIT OVERHEAD SIGN AFT FACE LIGHTS INOP. MX RESET, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012400226 20080124 00226 SO 2008 1 24 FDKA200710536 1 20071009 A 3350 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 840MJ 145429 FDM 6031 ATL (1135 PHX LCL) - EMERGENCY LIGHT 2 FLOOR STRIPS, 2 OVERWING SIGNS INOP. MX RESET SYSTEM, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012400252 20080124 00252 GL 2008 1 24 FDKA200709469 2 20070913 A 7320 23076368 METERING UNIT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 ENGINE MALFUNCTIONED A FDKA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SW 07 840MJ 145429 CAE311321 FDM 6072 CAE (1244 PHX LCL) - PILOT REPORTED AT 17000 FT, NR 2 ENGINE SHUT DOWN AND IT WOULD NOT RESTART. MX REMOVED AN D REPLACED FPMU OPS AND LEAK CHECK GOOD AT LOW AND HIGH POWER RUN. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008012400257 20080124 00257 SO 2008 1 24 FDKA200712378 1 20071204 A 2720 RUDDER CONTROL EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 856MJ 145626 FDM 6040 FLL (0851 PHX LCL) - RUDDER SYSTEM 1 INOP. MX RESET SYSTEM, NO FURTHER ACTION REQUIRED. 2 L 7 2 4T RT T00011AT 2008012400261 20080124 00261 SO 2008 1 24 FDKA200705239 1 20070523 A 5310 14524131009 DOOR FRAME EMB 145 EMB145LR 3260212 SO ZONE 800 CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 831MJ 145273 TWO ANGLES ON THE PAX DOOR FRAME, THAT SECURE THE THRESHOLD ARE CORRODED. THE DAMAGED ANGLES HAVE BEEN REMOVED AND REPL ACED. 2 L 7 2 4T RT T00011AT 2008012400281 20080124 00281 SO 2008 1 24 FDKA200710523 1 20071005 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 832MJ 145310 FDM 6000 ATL (0653 PHX LCL) - MAIN CABIN DOOR WILL NOT CLOSE. MX COULD NOT DUPLICATE, OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012400293 20080124 00293 SO 2008 1 24 FDKA200712368 1 20071202 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 9960 MCO (0645 PHX LCL) - EMERGENCY EXIT LIGHTING AT GALLEY DOOR WILL NOT COME ON. MX RESECURED CONNECTOR, OPERATED NORMAL. 2 L 7 2 4T RT T00011AT 2008012400295 20080124 00295 SO 2008 1 24 FDKA200712394 1 20071210 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO GALLEY UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6028 MCO (1435 PHX LCL) - EMERGENCY EXIT LIGHTING AT GALLEY DOOR WILL NOT COME ON. MX RESECURED LIGHT ASSY, OPERATE D NORMAL. 2 L 7 2 4T RT T00011AT 2008012400345 20080124 00345 SO 2008 1 24 FDKA200707338 1 20070715 A 2731 TRIM SYSTEM EMB 145 EMB145LR 3260212 SO PITCH INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 852MJ 145567 FDM 6166 JFK (1219 PHX LCL) - CAPTAIN PITCH TRIM MAIN INOP. MX RESET SYSTEM, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008012400347 20080124 00347 SO 2008 1 24 FDKA200703145 1 20070321 A 5315 14525522001 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CRACKED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 847MJ 145517 FLOORBEAM TEE AT FRAME 65 LT SIDE IS CRACKED. THE DAMAGED CROSS FRAME HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2008012500029 20080125 00029 SO 2008 1 25 FDKA200712365 1 20071201 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 848MJ 145530 FDM RON CAE (1905 PHX LCL) - MAIN CABIN DOOR HARD TO CLOSE AND DOESN’T ALIGN. MX LUBED THE DOOR ROLLERS AND OPS CHECKED . 2 L 7 2 4T RT T00011AT 2008012500044 20080125 00044 SO 2008 1 25 FDKA200712403 1 20071213 A 2797 CONNECTOR EMB 145 EMB145LR 3260212 SO TE FLAPS DIRTY A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 827MJ 145217 FDM 6208 ATL - FLAP LOW SPEED ADVISORY MESSAGE AFTER LANDING DURING FLAP RETRACTION. MX CLEANED AND RESECURED FECU CONN ECTOR, SYS OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012800001 20080128 00001 SO 2008 1 28 FDKA200707402 1 20070718 A 3210 14571035414 CAP EMB 145 EMB145LR 3260212 SO MLG BEARING CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 860MJ 145773 RT AND LT MLG FWD BEARING CAP IS CORRODED OUT OF LIMITS. REPLACED CAP. 2 L 7 2 4T RT T00011AT 2008012800015 20080128 00015 SO 2008 1 28 FDKA200710545 1 20071013 A 2797 CONNECTOR EMB 145 EMB145LR 3260212 SO PROX SWITCH LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 FDM 9963 MCO - SPOILER FAIL EICAS MESSAGE. MX RESECURED SPOILER PROX SWITCH CONNECTOR AND APPLIED HEAT SHRINK. 2 L 7 2 4T RT T00011AT 2008012800016 20080128 00016 SO 2008 1 28 FDKA200711347 1 20071127 A 2797 CONNECTOR EMB 145 EMB145LR 3260212 SO RUDDER SYSTEM DIRTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 841MJ 145448 FDM 6150 TYS. RUDDER SYSTEM NR 1 WILL NOT SHUT OFF. MX CLEANED CONNECTORS ON CONTROL PANEL SWITCH AND NR 1 PRESSURE SW ITCH. OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012800018 20080128 00018 SO 2008 1 28 FDKA200704164 1 20070402 A 5330 14521721009 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 848MJ 145530 BUTT STRAP AT FRAMES 15 AND 16 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED DAMAGED SECTION. 2 L 7 2 4T RT T00011AT 2008012800021 20080128 00021 SO 2008 1 28 FDKA200710554 1 20071017 A 2701 UNKNOWN EMB 145 EMB145LR 3260212 SO YOKE UNKNOWN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 FDM 6031 ATL (1305 PHX LCL) - YOKE CATCHING ON SOMETHING, MOVEMENT NOT SMOOTH. MX FOUND YOKE MOVEMENT SMOOTH. NO CLICK NOTED WHEN GUSTLOCK C/B IS PULLED. 2 L 7 2 4T RT T00011AT 2008012800023 20080128 00023 SO 2008 1 28 FDKA200711358 1 20071126 A 5330 14522226003 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 855MJ 145614 BUTT STRAP FRAME 59 AND Y=0.0 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED BUTTSTRAP. 2 L 7 2 4T RT T00011AT 2008012800024 20080128 00024 SO 2008 1 28 FDKA200708401 1 20070819 A 5210 SILL EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 837MJ 145367 FDM 6131 MCO (1515 PHX LCL) - MAIN CABIN DOOR HARD TO CLOSE. MX LUBED DOOR SILLS. 2 L 7 2 4T RT T00011AT 2008012800025 20080128 00025 SO 2008 1 28 FDKA200708397 1 20070818 A 3234 SELECTOR EMB 145 EMB145LR 3260212 SO MLG MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM 6144 MCO (1206 PHX LCL) - RTF LANDING GEAR WILL NOT RETRACT. MX REMOVED AND REPLACED LANDING GEAR HANDLE AND PUT EM ERGENCY SELECTOR SWITCH IN NORMAL POSITION, OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012800026 20080128 00026 SO 2008 1 28 FDKA200712411 1 20071219 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 851MJ 145572 FDM 6160 CLT (1003 PHX LCL) - MAIN CABIN DOOR DIFFICULT TO OPEN FROM THE INSIDE. MX LUBED DOOR, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012800027 20080128 00027 SO 2008 1 28 FDKA200712415 1 20071223 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DISCONNECTED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FDM FLT 6119 MCO (0423 PHX LCL) - EMERGENCY LIGHT IS OUT AT ROW 12. MX RECONNECTED CONNECTOR. LIGHTS OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800028 20080128 00028 SO 2008 1 28 FDKA200711335 1 20071113 A 2710 3535701001 MANIFOLD EMB 145 EMB145LR 3260212 SO AILERONS MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 847MJ 145517 FDM RON MCO (1903 PHX LCL) - AILERON SYSTEM 2 WON'T DEACTIVATE. MX REMOVED AND REPLACED AILERON MANIFOLD ASSY. 2 L 7 2 4T RT T00011AT 2008012800029 20080128 00029 SO 2008 1 28 FDKA200712419 1 20071225 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 835MJ 145353 FDM FLT RON PHF (1932 PHX LCL) - MAIN CABIN DOOR WILL NOT CLOSE. MX LUBED THE DOOR ROLLERS AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2008012800030 20080128 00030 SO 2008 1 28 FDKA200706309 1 20070628 A 2750 3631001011 CONTROL UNIT EMB 145 EMB145LR 3260212 SO TE FLAPS MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 850MJ 7395 145568 FDM 6050 ATL (1400 PHX LCL) - FLAP LOW SPEED. MX REMOVED AND REPLACED FECU. 2 L 7 2 4T RT T00011AT 2008012800032 20080128 00032 SO 2008 1 28 FDKA200712430 1 20071230 A 2612 3601134480 FIRE DETECTOR EMB 145 EMB145LR 3260212 SO NR 1 NACELLE FALSE ACTIVATION A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 839MJ 2187 145416 FDM FLT 6069 MCO (0543 PHX LCL) - ABORTED T/O DUE TO ENGINE NR 1 FIRE DETECT FAIL ON T/O ROLL. MX REMOVED AND REPLACED ENGINE 1 FIRE DETECTOR LOOP AND PYLON LOOP. 2 L 7 2 4T RT T00011AT 2008012800033 20080128 00033 SO 2008 1 28 FDKA200709495 1 20070905 A 5420 STRUCTURE EMB 145 EMB145LR 3260212 SO NR 2 NACELLE BENT A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 THE METAL LIP ON NR 2 ENGINE NOSE COWL IS BENT/DAMAGED. THE DAMAGED PART WAS REMOVED, FABRICATED AND REPLACED. 2 L 7 2 4T RT T00011AT 2008012800035 20080128 00035 SO 2008 1 28 FDKA200711336 1 20071115 A 5210 HINGE EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 849MJ 145534 FDM 6011 JFK (1315 PHX LCL), MAIN CABIN DOOR HARD TO OPEN. MX LUBED DOOR HINGE, OPS NORMAL. 2 L 7 2 4T RT T00011AT 2008012800036 20080128 00036 SO 2008 1 28 FDKA200710567 1 20071023 A 3010 0020BN4 COMPUTER EMB 145 EMB145LR 3260212 SO ICE DETECTION FAULTED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 1099 145217 FDM 6137 ATL (1350 PHX LCL) - SPS ICE SPEED DISPLAYED ICING NOT ON. MESSAGE FLICKER ONLY DID NOT STAY ON STEADY. MX RE PLACED SPS COMPUTER. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800037 20080128 00037 SO 2008 1 28 FDKA200712432 1 20071231 A 5210 SEAL EMB 145 EMB145LR 3260212 SO PAX DOOR TORN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 831MJ 145273 FDM FLT 6069 MCO (0418 PHX LCL) MAIN CABIN DOOR SEAL TORN. MX REPAIRED DOOR SEAL. 2 L 7 2 4T RT T00011AT 2008012800042 20080128 00042 SO 2008 1 28 FDKA200708390 1 20070816 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 842MJ 145457 FDM 9964 AVL - ALL EMERGENCY LIGHTS INOP. RESET EMERGENCY LIGHTING SYSTEM, OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012800043 20080128 00043 SO 2008 1 28 FDKA200709497 1 20070914 A 5311 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE CRACKED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 THE APU AIR INLET FRAME IS CRACKED. REPAIRED DAMAGE. 2 L 7 2 4T RT T00011AT 2008012800046 20080128 00046 SO 2008 1 28 FDKA200712420 1 20071226 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DISCONNECTED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM FLT 6135 MCO (1700 PHX LCL) - EMERGENCY EXIT LIGHT AT SERVICE DOOR WILL NOT COME ON. REST CONNECTOR, OPS NORMAL. 2 L 7 2 4T RT T00011AT 2008012800051 20080128 00051 SO 2008 1 28 FDKA200709465 1 20070912 A 5210 SEAL EMB 145 EMB145LR 3260212 SO PAX DOOR INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6155 MCO - PAX DOOR UPPER SEAL NOT SEALING. MX COULD NOT DUPLICATE, DOOR, OPS CHECKED AND SEALED GOOD. 2 L 7 2 4T RT T00011AT 2008012800052 20080128 00052 SO 2008 1 28 FDKA200709466 1 20070912 A 2730 CONTROL CABLE EMB 145 EMB145LR 3260212 SO ELEVATORS OUT OF RIG A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 853MJ 145464 FDM RON MCO - CAPTAIN ELEVATOR HARD TO MOVE. MX RE-RIGGED THE ELEVATOR CABLES. 2 L 7 2 4T RT T00011AT 2008012800053 20080128 00053 SO 2008 1 28 FDKA200709471 1 20070915 A 2710 CONTROL CABLE EMB 145 EMB145LR 3260212 SO FLT CONTROLS DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 853MJ 145464 FDM RON MCO - FLIGHT CONTROL YOKE BOTH SIDES HARD TO MOVE WITH GRINDING. MX INSPECTED CABLES AND PULLEYS. MX REMOVED A ND REPLACED PULLEYS IN CARGO COMPARTMENT. 2 L 7 2 4T RT T00011AT 2008012800054 20080128 00054 SO 2008 1 28 FDKA200712377 1 20071203 A 3010 K0435 RELAY EMB 145 EMB145LR 3260212 SO ANTI ICE SYS MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 860MJ 145773 FDM 6199 PWM (0959 PHX LCL) - DECLARED EMERGENCY, ICE CONDITION/ANTI-ICE FAIL, WING ANTI-ICE FAIL, AND BLEED 2 LOW TEM/ OVER TEMP. MX REMOVED AND REPLACED K0435, K0531 RELAYS AND WING A/F VALVE. 2 L 7 2 4T RT T00011AT 2008012800057 20080128 00057 SO 2008 1 28 FDKA200709473 1 20070917 A 2730 BEARING EMB 145 EMB145LR 3260212 SO ELEVATORS BINDING A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 853MJ 145464 FDM RON RDU - ELEVATOR FLIGHT CONTROLS BINDING/GRINDING IN FORWARD AND AFT MOVEMENT. MX REMOVED AND REPLACED TORQUE BEA RINGS AND CABLE TENSIONER. 2 L 7 2 4T RT T00011AT 2008012800058 20080128 00058 SO 2008 1 28 FDKA200709464 1 20070911 A 5210 HANDLE EMB 145 EMB145LR 3260212 SO PAX DOOR LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 851MJ 145572 FDM RON DAY - PAX DOOR WAS DIFFICULT TO OPEN FROM INSIDE. MX FOUND THE DOOR HANDLE WAS LOOSE AND RE-INSTALLED IT AND O PS CHECKED THE DOOR. 2 L 7 2 4T RT T00011AT 2008012800061 20080128 00061 SO 2008 1 28 FDKA200709467 1 20070912 A 5240 DOOR EMB 145 EMB145LR 3260212 SO SERVICE OUT OF ADJUST A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 FDM 6040 RDU - GALLEY DOOR HARD TO CLOSE. MX ADJUSTED SERVICE DOOR, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012800062 20080128 00062 SO 2008 1 28 FDKA200709463 1 20070911 A 2731 SWITCH EMB 145 EMB145LR 3260212 SO PITCH TRIM INTERMITTENT A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 838MJ 145384 FDM FLT 6104 MCO. FO'S SIDE PITCH TRIM SWITCH INTERMITTENT. MX LUBED FO'S YOKE TRIM SWITCH OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012800063 20080128 00063 SO 2008 1 28 FDKA200710275 1 20071026 A 5220 HANDLE EMB 145 EMB145LR 3260212 SO EMERGENCY DOOR MISINSTALLED A FDKA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SW 07 840MJ 145429 FDM 6137 ATL (0926 PHX LCL) - 12A EMERGENCY DOOR GRIP HANDLE INSTALLED WRONG. MX INSTALLED HANDLE PROPERLY. 2 L 7 2 4T RT T00011AT 2008012800065 20080128 00065 2008 1 28 FDKA200708432 2 20070829 A 7297 CONNECTOR EMB 145 EMB145LR 3260212 SO OIL INDICATION DISCONNECTED A FDKA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 07 835MJ 145353 FDM 6195 BUF (0444 PHX LCL) - ABORTED T/O DUE TO E-2 OIL IMPENDING BYPASS MESSAGE. MX FOUND OIL IMPENDING BYPASS INDICA TOR C/P DISCONNECTED. RECONNECTED C/P, RAN ENGINE, NO OIL DEBRIS MESSAGE IN CMC. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800069 20080128 00069 SO 2008 1 28 FDKA200710516 1 20071002 A 3097 WIRE EMB 145 EMB145LR 3260212 SO WINDSHIELD HEAT DAMAGED A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 849MJ 14460 145534 FDM 6086 MCO-RDU (1624 PHX LCL) - AIRCRAFT DIVERTED TO CAE DUE TO ELECTRICAL BURNING ODOR IN COCKPIT WITH WINDOW HEAT ON . MX REMOVED AND REPLACED WINDSHIELD HEAT CONTROLLER AND REPLACED POWER OUT WIRE FROM WINDSHIELD TO CONTROLLER. 2 L 7 2 4T RT T00011AT 2008012800071 20080128 00071 SO 2008 1 28 FDKA200708430 1 20070829 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO CARGO BAY NO TEST A FDKA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 833MJ 15928 145327 FDM 6081 CAE (0335 PHX LCL) - BAG SMOKE WARNING MESSAGE NOT ILLUMINATED ON TEST. MX REMOVED AND REPLACED FWD SMOKE DETE CTOR. 2 L 7 2 4T RT T00011AT 2008012800074 20080128 00074 SO 2008 1 28 FDKA200710271 1 20071024 A 5210 CAM EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 848MJ 145530 FDM 6131 MCO (1254 PHX LCL) - MAIN CABIN DOOR HARD TO CLOSE. MX LUBED INTER-LIPPING CAM. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800075 20080128 00075 NM 2008 1 28 FDKA200708357 1 20070802 A 2750 FLAP SYSTEM DHAV DHC8 DHC8101 2809002 NM TE FLAPS MALFUNCTIONED A FDKA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 802LR 205 FDM 6204 PVD-JFK (0555 PHX LCL) - PILOT ABORTED TAKEOFF DUE TO TAKEOFF CONFIG WANRING HORN ON ROLLOUT. MX RESET SYSTEM AND PERFORMED OPS CK OF FLAPS AND INDICATION SYSTEM; SYSTEM OPS CK GOOD AND NO DEFECTS WERE NOTED. 2 H 7 2 4T RT A13NM 2008012800076 20080128 00076 NM 2008 1 28 FDKA200708358 1 20070802 A 2751 44281508011 INDICATOR DHAV DHC8 DHC8101 2809002 NM TE FLAPS MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 802LR 10619 205 FDM 6205 JFK-PVD (0555 PHX LCL) - PILOT REPORTED THAT THE FLAPS ONLY GO TO 4 DEGREES ON INDICATOR. MX REPLACED THE FLAP INDICATOR. 2 H 7 2 4T RT A13NM 2008012800077 20080128 00077 SO 2008 1 28 FDKA200708360 1 20070802 A 2750 TRANSMISSION EMB 145 EMB145LR 3260212 SO FLAP BRAKE MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 829MJ 15098 145228 FDM RON MCO - NR 1 AND 2 FLAP BRAKE TRANSMISSION FAIL TEST ON "A" CHECK. MX REMOVED AND REPLACED NR 1 AND NR 2 FLAP BRA KE TRANSMISSIONS. 2 L 7 2 4T RT T00011AT 2008012800079 20080128 00079 SO 2008 1 28 FDKA200704167 1 20070405 A 5411 14576631621 FRAME EMB 145 EMB145LR 3260212 SO LT NACELLE CHAFED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 848MJ 145530 THE AFT FORMER ON THE LT LOWER ENGINE COWLING IS CHAFED BEYOND ALLOWABLE LIMITS. THE DAMAGED FORMER WAS REMOVED AND REP LACED. 2 L 7 2 4T RT T00011AT 2008012800080 20080128 00080 SO 2008 1 28 FDKA200707408 1 20070715 A 7830 DOOR EMB 145 EMB145LR 3260212 SO THRUST REVERSER DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 833MJ 145327 THE LEADING EDGE OF THE NR 2 LOWER THRUST REVERSER IS DAMAGED ON THE OUTBOARD SIDE. REPAIRED LOWER T/R DOOR. 2 L 7 2 4T RT T00011AT 2008012800083 20080128 00083 SO 2008 1 28 FDKA200710272 1 20071025 A 2750 FLAP SYSTEM EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 841MJ 145448 FDM 6137 ATL (0857 PHX LCL) - FLAP FAIL STUCK AT 45 DEGREES. MX RESET FLAP SYSTEM. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800084 20080128 00084 SO 2008 1 28 FDKA200712434 1 20071231 A 5210 SEAL EMB 145 EMB145LR 3260212 SO PAX DOOR DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 835MJ 145353 FDM FLT 6022 BWI (0813 PHX LCL) - MAIN CABIN DOOR DIFFICULT TO OPEN/CLOSE. MX REMOVED AND REPLACED AIRFRAME DOOR SEAL, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800086 20080128 00086 SO 2008 1 28 FDKA200711353 1 20071119 A 5720 STRIP EMB 145 EMB145LR 3260212 SO PANEL CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 855MJ 145614 PANEL 6731 HAS CORRODED BONDING STRIP. REMOVED AND REPLACED CORRODED STRIP. 2 L 7 2 4T RT T00011AT 2008012800091 20080128 00091 SO 2008 1 28 FDKA200712433 1 20071231 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DISCONNECTED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 FDM FLT 6081 CAE (0425 PHX LCL) EMERGENCY LIGHT OUT AT ROW 12. MX RESEATED CONNECTOR. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800092 20080128 00092 SO 2008 1 28 FDKA200709487 1 20070901 A 5411 14576631621 FRAME EMB 145 EMB145LR 3260212 SO NACELLE CHAFED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 THE AFT FRAME ON THE LOWER ENGINE COWLING IS CHAFED OUT OF LIMITS. REMOVED AND REPLACED DAMAGED FRAME. 2 L 7 2 4T RT T00011AT 2008012800093 20080128 00093 SO 2008 1 28 FDKA200709489 1 20070904 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 THE RT SILL AT FRAME NR 23 IS CORRODED OUT OF LIMITS. REPAIRED THE DAMAGE. 2 L 7 2 4T RT T00011AT 2008012800094 20080128 00094 SO 2008 1 28 FDKA200710564 1 20071022 A 5210 LATCH EMB 145 EMB145LR 3260212 SO PAX DOOR UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM 6157 MCO (0630 PHX LCL) - MAIN CABIN DOOR DIFFICULT TO LATCH CLOSE. MX RESECURED LUBED AND ADJUSTED. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800095 20080128 00095 SO 2008 1 28 FDKA200712437 1 20071205 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 THE RT O/B FLOOR SUPPORT AT FRAME NR 22, JUST AFT OF THE SERVICE DOOR IS CORRODED OUT OF LIMITS. THE DAMAGE HAS BEEN RE PAIRED. 2 L 7 2 4T RT T00011AT 2008012800096 20080128 00096 SO 2008 1 28 FDKA200712435 1 20071204 A 5413 STRINGER EMB 145 EMB145LR 3260212 SO UPPER COWLING CHAFED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 LT ENGINE, UPPER COWLING, AFT O/B STRINGER IS DAMAGED AT THE AFT END. THE DAMAGED STRINGER HAS BEEN REPAIRED. 2 L 7 2 4T RT T00011AT 2008012800097 20080128 00097 SO 2008 1 28 FDKA200711356 1 20071118 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 855MJ 145614 CARGO DOOR SILL IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED DOOR SILL. 2 L 7 2 4T RT T00011AT 2008012800098 20080128 00098 SO 2008 1 28 FDKA200707406 1 20070721 A 7830 SKIN EMB 145 EMB145LR 3260212 SO T/R DOOR DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 RT THRUST REVERSER UPPER DOOR SKIN DAMAGE. REPAIRED DAMAGE. 2 L 7 2 4T RT T00011AT 2008012800099 20080128 00099 SO 2008 1 28 FDKA200707407 1 20070721 A 5330 14523056003 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 860MJ 145773 CARGO DOOR CUT OUT FUSELAGE SKIN DAMAGE. REPAIRED FUSELAGE SKIN. 2 L 7 2 4T RT T00011AT 2008012800100 20080128 00100 SO 2008 1 28 FDKA200707409 1 20070725 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 833MJ 145327 CARGO DOOR SURROUND SKIN SCRATCHES ARE BLENDED OUT OF LIMITS. REPAIRED SKIN. 2 L 7 2 4T RT T00011AT 2008012800105 20080128 00105 SO 2008 1 28 FDKA200707411 1 20070728 A 5320 SUPPORT ANGLE EMB 145 EMB145LR 3260212 SO PAX DOOR SILL OUT OF LIMITS A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 858MJ 145767 LOWER PAX DOOR SILL SUPPORT ANGLES CORRODED OUT OF LIMITS. REMOVED AND REPLACED ANGLES. 2 L 7 2 4T RT T00011AT 2008012800106 20080128 00106 SO 2008 1 28 FDKA200708387 1 20070814 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO APU ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 834MJ 145340 FDM 6025 ATL-GPT (2059 PHX LCL) - STRONG ODOR OF FUEL ON APU START. INSPECTED NO FUEL LEAK FOUND AND NO FUEL ODOR FOUND . 2 L 7 2 4T RT T00011AT 2008012800107 20080128 00107 SO 2008 1 28 FDKA200707336 1 20070712 A 2720 K0773 RELAY EMB 145 EMB145LR 3260212 SO RUDDER FAILED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 830MJ 145259 FDM 6130 BGM-JFK (1340 PHX LCL) - RUDDER HARDOVER PROTECTION FAIL. MX REPLACED K0773 AND K0059 RELAYS. OPS CHECKED GOO D. 2 L 7 2 4T RT T00011AT 2008012800110 20080128 00110 SO 2008 1 28 FDKA200712436 1 20071205 A 5320 1452172540 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 THE RT O/B FLOOR SUPPORT SILL, BETWEEN FRAME NR 18 AND NR 20 IS CORRODED OUT OF LIMITS. THE DAMAGED SILL HAS BEEN REMOV ED AND REPLACED 2 L 7 2 4T RT T00011AT 2008012800111 20080128 00111 SO 2008 1 28 FDKA200710295 1 20071029 A 2750 HANDLE EMB 145 EMB145LR 3260212 SO TE FLAPS DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 841MJ 145448 FDM RON DAY - FLAPS FAIL ON LANDING. MX REPLACED FLAP SELECT HANDLE, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012800112 20080128 00112 SO 2008 1 28 FDKA200712416 1 20071223 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR OUT OF ADJUST A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 851MJ 145572 FDM FLT 6160 CLT (1254 PHX LCL) - MAIN CABIN DOOR DIFFICULT TO OPEN FROM THE INSIDE. ADJUSTED DOOR ROLLERS, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800113 20080128 00113 SO 2008 1 28 FDKA200707414 1 20070731 A 5200 12037973007 LATCH EMB 145 EMB145LR 3260212 SO GPU DOOR CRACKED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 833MJ 145327 THE GPU DOOR IS CRACKED AT THE LATCH. DAMAGE WAS REPAIRED. 2 L 7 2 4T RT T00011AT 2008012800114 20080128 00114 SO 2008 1 28 FDKA200708398 1 20070819 A 7500 LINE EMB 145 EMB145LR 3260212 SO BLEED SYSTEM DAMAGED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 841MJ 145448 FDM 9961 MCO (0807 PHX LCL) - ABORT T/O DUE TO NR 1 ENGINE OVERTEMP EXCEEDING 915 DEGREE C WITH MASTER WARNING. MX REMO VED AND REPLACED BLEED LINE. 2 L 7 2 4T RT T00011AT 2008012800116 20080128 00116 SO 2008 1 28 FDKA200708400 1 20070819 A 2720 CONTROLLER EMB 145 EMB145LR 3260212 SO RUDDER MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 FDM 6141 ATL (1145 PHX LCL) - RUDDER HARDOVER PROTECTION FAIL. MX RESET RUDDER CONTROLLER. 2 L 7 2 4T RT T00011AT 2008012800118 20080128 00118 SO 2008 1 28 FDKA200711331 1 20071112 A 5210 HANDLE EMB 145 EMB145LR 3260212 SO PAX DOOR MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6095 MCO (0946 PHX LCL) - MAIN DOOR EXTERNAL HANDLE NOT FLUSH WHEN DOOR IS CLOSED. MX OPS CK DOOR, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800119 20080128 00119 SO 2008 1 28 FDKA200711328 1 20071109 A 5210 LATCH EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 FDM 6064 BHM (0407 PHX LCL) - MAIN CABIN DOOR HARD TO OPEN AND CLOSE. MX LUBRICATED DOOR LATCH ASSY. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008012400243 20080124 00243 SO 2008 1 24 FDKA200709451 1 20070907 A 2731 TRIM SYSTEM EMB 145 EMB145LR 3260212 SO PITCH INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 FFDM FLT 6174 SYR - PITCH TRIM INOP. MX RESET SYSTEM WITH CREW. NO FURTHER ACTION REQUIRED. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012400276 20080124 00276 SO 2008 1 24 FDKA200705228 1 20070505 A 5414 COWLING EMB 145 EMB145LR 3260212 SO LT NACELLE CHAFED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 850MJ 145568 LT LOWER COWLING IS CHAFED, OUT OF LIMITS AT FRAME NR 6. THE DAMAGE HAS BEEN REPAIRED. 2 L 7 2 4T RT T00011AT 2008012400277 20080124 00277 SO 2008 1 24 FDKA200711359 1 20071129 A 2120 GASPER FAN EMB 145 EMB145LR 3260212 SO LAVATORY OUT OF POSITION A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 858MJ 145767 FDM RON ALB (1954 PHX LCL) - LAVATORY SMOKE MASTER WARNING IN FLIGHT WITH NO FIRE FOUND. MX INSPECTED AND FOUND GASPER AIR DIRECTED TOWARDS SMOKE DETECTOR AND REDIRECTED THE GASPER AND OPS CHECKED THE DETECTOR. 2 L 7 2 4T RT T00011AT 2008012400279 20080124 00279 SO 2008 1 24 FDKA200708365 1 20070802 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 5996 ATL (1010 PHX LCL) - MAIN CABIN DOOR WON'T SEAL CLOSED. MX LUBED DOOR ROLLERS, OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012400286 20080124 00286 SO 2008 1 24 FDKA200712396 1 20071211 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6042 RDU (0407 PHX LCL). ROW 12 CEILING EMERGENCY LIGHT AFT FACE INOP. MX FOUND CONNECTOR LOOSE, RESET CONNECTOR, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012400287 20080124 00287 SO 2008 1 24 FDKA200712397 1 20071211 A 3150 WARNING MESSAGE EMB 145 EMB145LR 3260212 SO ILLUMINATED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 840MJ 145429 FDM 9960 ATL-MCO (1553 PHX LCL) - SPS INOP WARNING MESSAGE. MX TROUBLESHOT AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012400288 20080124 00288 SO 2008 1 24 FDKA200709442 1 20070904 A 2710 14521333401 CONTROL PANEL EMB 145 EMB145LR 3260212 SO AILERONS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 828MJ 12647 145218 AILERON SYSTEM 1 CUT OUT SWITCH INOP. MX REPLACED FLIGHT CONTROL PANEL. 2 L 7 2 4T RT T00011AT 2008012400292 20080124 00292 SO 2008 1 24 FDKA200712364 1 20071201 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INTERMITTENT A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6083 BHM (1345 PHX LCL) - EMERGENCY SIGN ROW 12 WILL NOT COME ON. MX PERFORMED OPS CHECKS, UNABLE TO DUPLICATE PROB LEM. 2 L 7 2 4T RT T00011AT 2008012400296 20080124 00296 2008 1 24 FDKA200709441 4 20070903 A 3432 7010133 DETECTOR EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 832MJ 15727 145310 ABORTED T/O DUE TO F/O'S HEADING OFF 30 PERCENT. REMOVED AND REPLACED FLUX DETECTOR. 2 L 7 2 4T RT T00011AT 2008012400299 20080124 00299 SO 2008 1 24 FDKA200710527 1 20071007 A 2760 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO SPOILERS DIRTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 FDM 6089 JFK (0620 PHX LCL) - SPOILER FAIL CAUTION MESSAGE IN FLIGHT. MX CLEANED PROX SWITCHES. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012400300 20080124 00300 SO 2008 1 24 FDKA200703142 1 20070317 A 5320 14526437001 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO LAVATORY AREA CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 847MJ 145517 DIGITAL FLOOR SUPPORT IS CORRODED OUT OF LIMITS UNDER THE COMPOSITE SUPPORT MEMBER, LOCATED LAV AREA ON THE RT SIDE OF T HE FUSELAGE. THE DIGITAL HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2008012400301 20080124 00301 SO 2008 1 24 FDKA200710529 1 20071007 A 2760 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO SPOILERS DIRTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 FDM RON JFK (1714 PHX LCL) - SPOILER FAIL CAUTION MESSAGE IN FLIGHT. MX CLEANED PROX SWITCHES, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012400332 20080124 00332 SO 2008 1 24 FDKA200711361 1 20071129 A 2720 PEDAL EMB 145 EMB145LR 3260212 SO RUDDER STIFF A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 855MJ 145614 FDM 6199 JFK (1104 PHX LCL) - RUDDER PEDALS STIFF. MX PERFORMED RUDDER SYSTEM CHECK OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012400344 20080124 00344 SO 2008 1 24 FDKA200712371 1 20071202 A 5100 NONE EMB 145 EMB145LR 3260212 SO NONE NONE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 841MJ 145448 FDM 6118 MCO (1120 PHX LCL) - MAIN CABIN DOOR DIFFICULT TO OPEN FROM INSIDE. MX CANNOT DUPLICATE DISCREPANCY. OPERATED NORMAL. 2 L 7 2 4T RT T00011AT 2008012400353 20080124 00353 SO 2008 1 24 FDKA200712372 1 20071202 A 2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 858MJ 145767 FDM 6145 BUF (1257 PHX LCL) - LAV SMOKE INDICATION IN FLIGHT. MX REMOVED AND REPLACED DETECTOR AND DAU. 2 L 7 2 4T RT T00011AT 2008012500026 20080125 00026 SO 2008 1 25 FDKA200712373 1 20071202 A 2720 CONTROL CABLE EMB 145 EMB145LR 3260212 SO RUDDER BINDING A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 855MJ 145614 FDM 6032 MCO-ORF (1809 PHX LCL) - RUDDER PEDALS BINDING. MX REMOVED AND REPLACED CABLES. 2 L 7 2 4T RT T00011AT 2008012500028 20080125 00028 2008 1 25 FDKA200712376 4 20071203 A 3418 COMPUTER EMB 145 EMB145LR 3260212 SO STALL WARNING FAULTED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 841MJ 145448 FDM 6003 RIC (0502 PHX LCL) - SPS 1/2 INOP MSG AND STICK PUSHER FAIL. MX RE-RACKED SPS COMPUTER, OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012500035 20080125 00035 SO 2008 1 25 FDKA200705226 1 20070526 A 2750 3631001011 CONTROL UNIT EMB 145 EMB145LR 3260212 SO TE FLAPS MALFUNCTIONED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 844MJ 5177 145481 FDM 6002 MCO-NAS (1434 PHX LCL) - FLAP LOW SPEED MESSAGE. MX REPLACED THE FECU. 2 L 7 2 4T RT T00011AT 2008012500041 20080125 00041 SO 2008 1 25 FDKA200710300 1 20071030 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 145416 FDM 6005 MCO (0740 PHX LCL) - MAIN CABIN DOOR HARD TO OPEN AND CLOSE. MX ADJUSTED DOOR ROLLERS AND LUBED. 2 L 7 2 4T RT T00011AT 2008012500045 20080125 00045 SO 2008 1 25 FDKA200708419 1 20070824 A 3010 K0535 RELAY EMB 145 EMB145LR 3260212 SO ANTI ICE SYSTEM MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 853MJ 145464 FDM 6155 MCO - BURNING ODOR DURING 2ND PART OF ANTI-ICE TEST AND ANTI-ICE COMES ON WITH NO ICE VISIBLE. MX REMOVED AND REPLACED RELAYS K0435, K0535, AND K0527. OPS CK GOOD, NO FURTHER BURNING ODOR. 2 L 7 2 4T RT T00011AT 2008012500046 20080125 00046 SO 2008 1 25 FDKA200708418 1 20070823 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 853MJ 145464 FDM 6086 MCO-RDU (1949 PHX LCL) - ODOR OF ELECTRICAL SMOKE WHEN ANTI ICE CAME ON NOT IN ICING CONDITIONS. MX PERFORMED A/I TEST AND COULD NOT DUPLICATE. 2 L 7 2 4T RT T00011AT 2008012800002 20080128 00002 SO 2008 1 28 FDKA200707403 1 20070719 A 3230 MS21154S16 BEARING EMB 145 EMB145LR 3260212 SO NLG DRAG BRACE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 NOSE GEAR DRAG BRACE LOWER BEARING CORRODED. REPLACED BEARING. 2 L 7 2 4T RT T00011AT 2008012800004 20080128 00004 SO 2008 1 28 FDKA200711348 1 20071126 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR OUT OF ADJUST A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 850MJ 145568 FDM 6208 ATL (1432 PHX LCL) - MAIN CABIN DOOR HARD TO CLOSE. MX ADJUSTED THE ROLLERS. 2 L 7 2 4T RT T00011AT 2008012800008 20080128 00008 SO 2008 1 28 FDKA200710548 1 20071014 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 FDM 6073 JFK - MAIN CABIN DOOR HAVE LOUD SQUEAL. MX CLEANED AND LUBED, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012800038 20080128 00038 SO 2008 1 28 FDKA200710540 1 20071010 A 2560 FLASHLIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 834MJ 145340 FRL FLT 6122 MCO- PFN - CAPTAINS EMERGENCY FLASHLIGHT INOP. MX REMOVED AND REPLACED FLASHLIGHT AND CHARGER. 2 L 7 2 4F RT T00011AT 2008012800041 20080128 00041 SO 2008 1 28 FDKA200703114 1 20070228 A 5320 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 849MJ 145534 OMEGA BEAM HAS NUTPLATE HOLE THAT IS CORRODED OUT OF LIMITS AT FRAME 59 Y=0.0, REPAIRED. 2 L 7 2 4T RT T00011AT 2008012800059 20080128 00059 SO 2008 1 28 FDKA200712422 1 20071228 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 841MJ 145448 FDM FLT 6118 MCO (0616 PHX LCL), MAIN CABIN DOOR WILL NOT SEAL WHEN CLOSED. MX CAN NOT DUPLICATE DISCREPANCY, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800060 20080128 00060 SO 2008 1 28 FDKA200712423 1 20071228 A 2731 SWITCH EMB 145 EMB145LR 3260212 SO BACK UP TRIM DIRTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 FDM FLT 6155 MCO (0742 PHX LCL), BACK UP TRIM SWITCH WILL NOT TRIM UP. MX CLEANED SWITCH, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800082 20080128 00082 SO 2008 1 28 FDKA200711355 1 20071122 A 5320 14526437001 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 855MJ 145614 RT FLOOR SUPPORT GUSSET IN THE LAV AREA FROM FRAME NR 59 TO FRAME NR 61 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED DAMAGED GUSSET. 2 L 7 2 4T RT T00011AT 2008012800090 20080128 00090 SO 2008 1 28 FDKA200711352 1 20071117 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 855MJ 145614 RT O/B FLOOR SUPPORT SILL AT FRAME NR 24 IS CORRODED OUT OF LIMITS AT A NUTPLATE. REPAIRED DAMAGE. 2 L 7 2 4T RT T00011AT 2008012800115 20080128 00115 SO 2008 1 28 FDKA200710547 1 20071014 A 5210 SEAL EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 FDM 6073 JFK - MAIN CABIN DOOR HAVE LOUD SQUEAL. MX CLEANED AND LUBED DOOR SEAL. 2 L 7 2 4T RT T00011AT 2008012800121 20080128 00121 SO 2008 1 28 FDKA200711325 1 20071108 A 2710 CONTROL LEVER EMB 145 EMB145LR 3260212 SO GUSTLOCK MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 855MJ 145614 FDM 6127 FLL (0449 PHX LCL) - ELECTRIC GUSTLOCK WILL NOT DIS-ENGAGE. MX MOVED THE CONTROL LEVER AND THE GUSTLOCK UNLOCK ED. 2 L 7 2 4T RT T00011AT 2008012800122 20080128 00122 SO 2008 1 28 FDKA200710566 1 20071023 A 2730 COMPUTER EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM 6137 ATL (0900 PHX LCL) - SPS ICE SPEED NOT DISPLAYED AFTER ICING ON. MESSAGE ONLY FLICKERED AFTER LEVEL AT FL290. DID NOT STAY ON STEADY. MX RE-RACKED SPS COMPUTER. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800123 20080128 00123 SO 2008 1 28 FDKA200711344 1 20071123 A 3350 BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DISCHARGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 851MJ 145572 FDM 6061 RIC (0440 PHX LCL) - EMERGENCY LIGHTS INOP DUE TO ARM SWITCH LEFT IN THE ARM POSITION ALL NIGHT. MX REMOVED AN D REPLACED EMERGENCY BATTERIES. 2 L 7 2 4T RT T00011AT 2008012800127 20080128 00127 SO 2008 1 28 FDKA200709450 1 20070907 A 5297 WIRE EMB 145 EMB145LR 3260212 SO DOOR SWITCH DAMAGED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 837MJ 145367 FFDM FLT 6103 PNS - SERVICE DOOR WARNING MESSAGE. MX REPAIRED WIRE AT MICRO-SWITCH. 2 L 7 2 4T RT T00011AT 2008012800130 20080128 00130 SO 2008 1 28 FDKA200712408 1 20071216 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6062 ORF - EMERGENCY LIGHT OUT AT ROW 12. MX FOUND LOOSE CONNECTOR AT INVERTER. RESECURED AND OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800133 20080128 00133 SO 2008 1 28 FDKA200709438 1 20070901 A 5753 PIN EMB 145 EMB145LR 3260212 SO TE FLAP MIGRATED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 854MJ 145490 LT AND RT FLAP HINGE PINS MIGRATED. MX RESECURED AND SAFETIED THE PINS. 2 L 7 2 4T RT T00011AT 2008012800134 20080128 00134 SO 2008 1 28 FDKA200712398 1 20071212 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN SMOKE A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 838MJ 145384 FDM 6003 RIC (0517 PHX LCL) - SMOKE IN CABIN, APU ON, PACK 2 ON, ENGINES OFF. MX INSPECTED NR 2 PACK AREA, NO DEFECTS F OUND. 2 L 7 2 4T RT T00011AT 2008012800136 20080128 00136 SO 2008 1 28 FDKA200712400 1 20071212 A 5210 SHROUD EMB 145 EMB145LR 3260212 SO PAX DOOR LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 145416 FDM 6054 ATL-NAS - PAX DOOR WOULD NOT OPEN FROM THE INSIDE. MX FOUND THE DOOR CATCHING ON THE LOWER HINGE SHROUD WHICH WAS LOOSE. MX RESECURED THE SHROUD. 2 L 7 2 4T RT T00011AT 2008012800139 20080128 00139 SO 2008 1 28 FDKA200706314 1 20070627 A 5720 STRIP EMB 145 EMB145LR 3260212 SO WING CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 ANTI STATIC STRIPS ON PANELS 5731 AND 5732 ARE CORRODED OUT OF LIMITS. REMOVED AND REPLACED DAMAGED STRIPS. 2 L 7 2 4T RT T00011AT 2008012800141 20080128 00141 2008 1 28 FDKA200707320 2 20070701 A 7200 O-RING EMB 145 EMB145LR 3260212 SO NR 2 ENGINE DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 855MJ 145614 FDM 6025 ATL (2230 PHX LCL) - AFTER NR 2 ENGINE SHUT DOWN CREW HEARD A LOUD POP AND SMOKE COMING OUT OF THE TAILPIPE. M X REMOVED AND REPLACED THE E2 LPT REAR SHAFT PLUG O-RING. 2 L 7 2 4T RT T00011AT 2008012800143 20080128 00143 SO 2008 1 28 FDKA200706315 1 20070628 A 5414 PANEL EMB 145 EMB145LR 3260212 SO LT NACELLE CHAFED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 LT COWLING PANEL 414, HAS CHAFE DAMAGE TO THE FRAMES FROM CONTACT WITH THE FORWARD AND AFT STAY RODS. REPAIRED DAMAGE. 2 L 7 2 4T RT T00011AT 2008012800144 20080128 00144 SO 2008 1 28 FDKA200706317 1 20070629 A 5420 14531653001 BRACKET EMB 145 EMB145LR 3260212 SO LT PYLON CRACKED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 THE LT PRE-COOLER FORWARD MOUNT ANGLE IS CRACKED AT THE TOP RIVET. REMOVED AND REPLACED DAMAGED PART. 2 L 7 2 4T RT T00011AT 2008012800145 20080128 00145 SO 2008 1 28 FDKA200706318 1 20070629 A 4910 COWLING EMB 145 EMB145LR 3260212 SO APU BAY DEFORMED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 APU COWLING 4 LOWER STRINGERS ARE DEFORMED. REPAIRED DAMAGED STRINGERS. 2 L 7 2 4T RT T00011AT 2008012800151 20080128 00151 SO 2008 1 28 FDKA200712417 1 20071223 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM FLT 6051 MCO (1344 PHX LCL) - MAIN CABIN DOOR HARD TO OPEN FROM THE INSIDE. MX INSPECTED AND FOUND DOOR ROLLERS OU T OF ADJUSTMENT. ADJUSTED OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800152 20080128 00152 SO 2008 1 28 FDKA200712412 1 20071219 A 2710 3535701001 SOLENOID VALVE EMB 145 EMB145LR 3260212 SO AILERONS MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 838MJ 15572 145384 FDM 6109 JFK (1105 PHX LCL) - NO AILERON SYSTEM 2 INOP INDICATION WITH SYSTEM OFF. MX REMOVED AND REPLACED SOLENOID VAL VE 2 L 7 2 4T RT T00011AT 2008012800153 20080128 00153 SO 2008 1 28 FDKA200709475 1 20070917 A 5210 SEAL EMB 145 EMB145LR 3260212 SO PAX DOOR UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 847MJ 145517 FDM RON RDU - LOUD SQUEAL IN FLIGHT FROM PAX DOOR. MX RESECURED THE DOOR SEAL, PRESSURIZED THE CABIN AND FOUND NO FURTH ER LEAK. 2 L 7 2 4T RT T00011AT 2008012800158 20080128 00158 SO 2008 1 28 FDKA200710293 1 20071029 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 851MJ 145572 FDM 6016 JFK (1250 PHX LCL) - MAIN CABIN DOOR HARD TO OPEN. MX LUBED DOOR. 2 L 7 2 4T RT T00011AT 2008012800159 20080128 00159 SO 2008 1 28 FDKA200710291 1 20071029 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX OUT OF RIG A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM 6001 MCO (1032 PHX LCL) - MAIN CABIN DOOR DIFFICULT TO CLOSE. MX RIGGED MAIN CABIN DOOR. 2 L 7 2 4T RT T00011AT 2008012800160 20080128 00160 SO 2008 1 28 FDKA200712439 1 20071213 A 5411 14576057622 RIB EMB 145 EMB145LR 3260212 SO RT NACELLE GOUGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 THE AFT FRAME ON THE RT UPPER ENGINE COWLING IS GOUGED OUT OF LIMITS. THE FRAME HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2008012800168 20080128 00168 SO 2008 1 28 FDKA200712426 1 20071229 A 2750 FLAP SYSTEM EMB 145 EMB145LR 3260212 SO TEL FLAPS MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 851MJ 145572 FDM FLT 6064 CVG (0645 PHX LCL) - WHEN FLAPS WERE SELECTED TO 45 THEY STOPPED AT 22. RESET FLAPS 1 AND 2, FLAPS OPS GOO D. 2 L 7 2 4T RT T00011AT 2008012800169 20080128 00169 SO 2008 1 28 FDKA200712427 1 20071229 A 5210 GATE EMB 145 EMB145LR 3260212 SO PAX DOOR STUCK A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 832MJ 145310 FDM FLT 6052 TPA-PNS (0806 PHX LCL) - MAIN DOOR UPPER FLAP WILL NOT CLOSE. MX CLEANED, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800170 20080128 00170 SO 2008 1 28 FDKA200712428 1 20071229 A 2760 SWITCH EMB 145 EMB145LR 3260212 SO SPOILERS DIRTY A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 825MJ 145179 FDM FLT 6042 JFK-ROC (0839 PHX LCL) - SPOILER FAIL CAUTION. MX CLEANED SWITCHES, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800171 20080128 00171 SO 2008 1 28 FDKA200710285 1 20071028 A 2612 HANDLE EMB 145 EMB145LR 3260212 SO NR 2 FIRE MALFUNCTIONED A FDKA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 SW 07 831MJ 145273 FDM 6049 JFK (0450 PHX LCL) - NR 2 FIRE HANDLE DOES NOT ILLUMINATE DURING TEST. MX RESET, SYSTEM OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012800172 20080128 00172 SO 2008 1 28 FDKA200710286 1 20071028 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX OUT OF RIG A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 834MJ 145340 FDM 6169 ATL (1209 PHX LCL) - MAIN CABIN DOOR WILL NOT CLOSE. MX RE-RIGGED DOOR. 2 L 7 2 4T RT T00011AT 2008012800173 20080128 00173 SO 2008 1 28 FDKA200710537 1 20071009 A 2760 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO SPOILERS DIRTY A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 825MJ 145179 FDM 6018 PNS-TPA (1355 PHX LCL) - SPOILER FAIL CAUTION MESSAGE IN FLIGHT. MX CLEANED C/P ON PROX SW, PERFORMED OPS CHEC K, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800182 20080128 00182 WP 2008 1 28 UPS08851411 1 20071230 A 5321 FLOORBOARD DOUG DC8 DC871F 302199D WP CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 FLOORBOARD PNL NR 682A HAS CORROSION ON NR 682 CUT OUT. REPAIRED FLOORBOARD PNL NR 682A PER SRM 53-0 7-01 FIG 1, SRM 51-01-21, AND SRM 53-2-0 FIG 1F. 2 L 7 4 4F RT 4A25 2008012800185 20080128 00185 SO 2008 1 28 FDKA200704172 1 20070418 A 5320 14526437001 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 852MJ 145567 RT DIGITAL BETWEEN FRAME 58 AND 60 IS CORRODED OUT OF LIMITS. THE DAMAGED PART WAS REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2008012800188 20080128 00188 SO 2008 1 28 FDKA200708377 1 20070808 A 2731 SWITCH EMB 145 EMB145LR 3260212 SO PITCH TRIM DIRTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 FDM 6003 RIC (0600 PHX LCL) - BACK UP PITCH TRIM INOP IN DOWN POSITION. MX CLEANED THE BACK UP TRIM SWITCH, OPS CHECK G OOD. 2 L 7 2 4T RT T00011AT 2008012800189 20080128 00189 2008 1 28 FDKA200708375 4 20070806 A 3100 UNKNOWN EMB 145 EMB145LR 3260212 SO UNKNOWN A FDKA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 842MJ 145457 FDM 5999 ATL (1250 PHX LCL) - ABORTED T/O FOR E2 ATTCS NO MARGIN ON T/O ROLL. MX PERFORMED RUNS AND COULD NOT DUPLICAT E. 2 L 7 2 4T RT T00011AT 2008012800190 20080128 00190 GL 2008 1 28 FDKA200712413 2 20071221 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 SMOKE A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 860MJ 145773 CAE312513 FDM FLT 6025 TLH-ATL (1727 PHX LCL) - GROUND CREW REPORTED SMOKE AND FIRE FROM NR 1 ENGINE ON SHUTDOWN. MX PERFORMED EN GINE RUNS SHUTDOWN WAS NORMAL NO EVIDENCE OF FIRE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008012800192 20080128 00192 SO 2008 1 28 FDKA200710283 1 20071027 A 5241 SEAL EMB 145 EMB145LR 3260212 SO GALLEY DOOR DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 834MJ 145340 FDM RON DAY (1806 PHX LCL) - GALLEY DOOR SQUEALING. REPAIRED DOOR SEAL AND LEAK CHECKED THE CABIN. NO LEAKS NOTED. 2 L 7 2 4T RT T00011AT 2008012800194 20080128 00194 SO 2008 1 28 FDKA200709490 1 20070904 A 5320 14522226003 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 THE LT FLOOR SUPPORT GUSSET IN THE LAV AREA IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED GUSSET. 2 L 7 2 4T RT T00011AT 2008012800195 20080128 00195 SO 2008 1 28 FDKA200709493 1 20070905 A 5524 PLATE EMB 145 EMB145LR 3260212 SO LT ELEVATOR CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 SIX BONDING PLATES ARE CORRODED ON THE LT ELEVATOR TIP. REMOVED AND REPLACED CORRODED PLATES. 2 L 7 2 4T RT T00011AT 2008012800196 20080128 00196 SO 2008 1 28 FDKA200709496 1 20070914 A 5320 14526324001 RECEPTACLE EMB 145 EMB145LR 3260212 SO CARGO DOOR CRACKED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 THE CARGO DOOR HOLD OPEN ROD RECEPTACLE IS CRACKED. REMOVED AND REPLACED DAMAGED PART. 2 L 7 2 4T RT T00011AT 2008012800197 20080128 00197 SO 2008 1 28 FDKA200709503 1 20070920 A 5751 FITTING EMB 145 EMB145LR 3260212 SO LT AILERON DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 LT AILERON DAMPER FITTING IS DAMAGED. THE DAMAGED FITTING HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2008012900021 20080129 00021 NM 2008 1 29 WRNA200800001 1 20071223 A 5412 65B903162 BULKHEAD BOEING 747 747212B 1384886 NM NR 1 PYLON CHAFED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING B-CHECK WHILE ACCOMPLISHING AD 2007-19-19, NR 1 PYLON STRUT FORWARD ENGINE MOUNT BULKHEAD CORD WAS FOUND WITH CHA FED RADIUS AT LOWER INBOARD END. FABRICATED AND INSTALLED REPAIR ANGLE IAW BOEING SKETCH SR1-733824930-1. THIS REPAIR IS TEMPORARY AND REQUIRES A REPEAT DETAILED VISUAL INSPECTION EVERY 30 DAYS OR 60 CYCLES, WHICH EVER OCCURS FIRST. PERM ANENT REPAIR MUST BE ACCOMPLISHED BY APRIL 30TH 2008, WITH REPLACEMENT OF BULKHEAD CORD. 2 L 7 4 4F RT A20WE 2008012900022 20080129 00022 NM 2008 1 29 WRNA200800002 1 20071224 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 526UP 21937 DURING B-CHECK INSPECTION, RIGHT FRAME AT STATION 2674.85 WAS FOUND CRACKED AT WL 325. REMOVED DAMAGE SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW 747 SRM 51-40-03 FIG 2. 2 L 7 4 4F RT A20WE 2008012400326 20080124 00326 SO 2008 1 24 FDKA200709477 1 20070919 A 2710 GUST LOCK EMB 145 EMB145LR 3260212 SO INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 830MJ 145259 FDM 6179 JFK (0500 PHX LCL) - GUST LOCK WILL NOT DISENGAGE. MX RESET SYSTEM, OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012400328 20080124 00328 NM 2008 1 24 FDKA200707337 1 20070714 A 2720 WARNING LIGHT DHAV DHC8 DHC8102 2809003 NM RUDDER ILLUMINATED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 804LR 324 FDM 6181 JFK-SYR (0950 PHX LCL) - RUDDER PRESS CAUTION WHEN FLAPS EXTENDED. MX PERFORMED OPS CK AND OPS CK GOOD, NO FAU LTS NOTED. 2 H 7 2 4T RT A13NM 2008012400351 20080124 00351 SO 2008 1 24 FDKA200707351 1 20070729 A 3150 WARNING LIGHT EMB 145 EMB145LR 3260212 SO SPOILERS ILLUMINATED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6172 ATL-ROA (1752 PHX LCL) - SPOILER FAIL CAUTION MESSAGE IN FLIGHT. MX RESET ELECTRICAL POWER, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012400372 20080124 00372 EU 2008 1 24 USAA920080180 1 20071225 A 5320 D5311282600101 DUMMY RAIL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 885 CLT - MAJOR REPAIR - RON, PILOT REPORT - CORROSION ON CABIN DUMMY RAIL, BS 605 / FR 12 - BS 709 / FR 16, +Y503. REPLACE D CABIN DUMMY RAIL, BS 605 / FR 12 - BS 709 / FR 16, +Y503 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008012500039 20080125 00039 SO 2008 1 25 FDKA200710538 1 20071009 A 2760 14533022409 CONTROL UNIT EMB 145 EMB145LR 3260212 SO SPOILERS FAULTED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 825MJ 13228 145179 FDM 6171 TPA-PNS (1732 PHX LCL) - SPOILER FAIL CAUTION MESSAGE IN FLIGHT. MX REMOVED AND REPLACED THE SPOILER CONTROL U NIT. 2 L 7 2 4T RT T00011AT 2008012500048 20080125 00048 SO 2008 1 25 FDKA200712402 1 20071213 A 3240 15851 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO BRAKES MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 15863 145214 FDM 6104 MCO - ABORTED TAKEOFF, ON TAKEOFF AT 10 KNOTS AC FELT LIKE PARKING BRAKE WAS NOT FULLY RELEASED. FOLLOWED BY A URAL WARNING. MX REMOVED AND REPLACED ACCUMULATOR BRAKE LOW PRESSURE SWITCH OPS GOOD. PERFORMED TAKEOFF CONFIG ADJUSTM ENT TEST, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012500050 20080125 00050 SO 2008 1 25 FDKA200708417 1 20070823 A 4930 SOLENOID EMB 145 EMB145LR 3260212 SO APU FUEL ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6025 ATL-DAY (1425 PHX LCL) - STRONG FUEL ODOR ON APU START. REMOVED AND REPLACED FUEL SOLENOID. 2 L 7 2 4T RT T00011AT 2008012800031 20080128 00031 SO 2008 1 28 FDKA200706306 1 20070628 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX OBSTRUCTED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FDM 6000 JFK (0800 PHX LCL) - MAIN CABIN DOOR WILL NOT STAY LOCKED IN OPEN POSITION. MX FOUND OBSTRUCTION IN DOOR, REMO VED BOOK OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012800040 20080128 00040 SO 2008 1 28 FDKA200703113 1 20070302 A 5320 14526437001 STRUCTURE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 849MJ 145534 RT DIGITAL BETWEEN FRAME 59 AND 61 IS CORRODED OUT OF LIMITS. THE PART WAS REPLACED. 2 L 7 2 4T RT T00011AT 2008012800048 20080128 00048 SO 2008 1 28 FDKA200709462 1 20070911 A 2750 3635001001 TRANSMISSION EMB 145 EMB145LR 3260212 SO NR 2 FLAPS NO TEST A FDKA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 844MJ 2262 145481 FDM RON MCO - NR 2 FLAP BRAKE TRANSMISSION FAILED FUNCTIONAL CHECK. MX REMOVED AND REPLACED NR 2 BRAKE TRANSMISSION, OP S CK GOOD. 2 L 7 2 4T RT T00011AT 2008012800073 20080128 00073 SO 2008 1 28 FDKA200710270 1 20071024 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 145416 FDM 6125 MCO (0515 PHX LCL) - FA CAN NOT OPEN MAIN CABIN DOOR. MX LUBED DOOR OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012800081 20080128 00081 SO 2008 1 28 FDKA200711354 1 20071120 A 5320 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 855MJ 145614 LT OMEGA BEAM AT FRAME NR 20 IS CORRODED OUT OF LIMITS. REPAIRED DAMAGE. 2 L 7 2 4T RT T00011AT 2008012800088 20080128 00088 SO 2008 1 28 FDKA200706310 1 20070629 A 2750 3631001011 CONTROL UNIT EMB 145 EMB145LR 3260212 SO TE FLAPS FAILED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 850MJ 7396 145568 FDM 6152 FLL (1153 PHX LCL) - FLAPS FAILED IN FLIGHT. AIRCRAFT FERRIED TO MCO WHERE MX REPLACED FECU AND OPS CHECKED GO OD. 2 L 7 2 4T RT T00011AT 2008012800102 20080128 00102 SO 2008 1 28 FDKA200711341 1 20071121 A 2120 DUCT EMB 145 EMB145LR 3260212 SO CABIN AIR DIRTY A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 837MJ 145367 FDM 6143 SDF - LAVATORY SMOKE WARNING MESSAGE. MX CLEANED AND RESECURED DUCTING TO RECIRC FAN/OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012800103 20080128 00103 2008 1 28 FDKA200708426 4 20070827 A 2210 3085701007 MANIFOLD EMB 145 EMB145LR 3260212 SO NLG STEERING MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 858MJ 5412 145767 FDM 6157 MCO (1208 PHX LCL) - UNCOMMANDED YAW ON T/O ROLL. PULLED TO THE LEFT. MX REMOVED AND REPLACED NOSE STEERING M ANIFOLD. 2 L 7 2 4T RT T00011AT 2008012800104 20080128 00104 SO 2008 1 28 FDKA200711342 1 20071121 A 2710 CONTROL PANEL EMB 145 EMB145LR 3260212 SO AILERON SYS MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 838MJ 145384 FDM 6049 JFK (0612 PHX LCL) - NR 2 AILERON SYSTEM WILL NOT TURN OFF. MX REMOVED AND REPLACED MANIFOLD AND CONTROL PANEL . 2 L 7 2 4T RT T00011AT 2008012800108 20080128 00108 SO 2008 1 28 FDKA200710543 1 20071011 A 2760 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO SPOILERS OUT OF ADJUST A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 825MJ 145179 FDM RON MCO (1613 PHX LCL) - SPOILER FAIL MESSAGE IN FLIGHT. MX ADJUSTED INDICATION PROX SENSORS. 2 L 7 2 4T RT T00011AT 2008012800135 20080128 00135 SO 2008 1 28 FDKA200712399 1 20071212 A 3350 SWITCH EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS FAILED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 842MJ 145457 FDM 6157 MCO (0930 PHX LCL) - OUTSIDE EMERGENCY LIGHT WILL NOT TURN OFF IN ANY SWITCH POSITION. MX RESET SWITCH OPS NOR MAL. 2 L 7 2 4T RT T00011AT 2008012800137 20080128 00137 SO 2008 1 28 FDKA200706312 1 20070625 A 5210 14524355001 BUSHING EMB 145 EMB145LR 3260212 SO PAX DOOR WORN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 14661 145416 BRASS BUSHING WAS WORN 1/16" ON TRACK, CAUSING HARD TO OPEN AND CLOSE MAIN DOOR. REPLACED BUSHING. 2 L 7 2 4T RT T00011AT 2008012800138 20080128 00138 SO 2008 1 28 FDKA200706313 1 20070627 A 5720 STRIP EMB 145 EMB145LR 3260212 SO WING CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 ANTI STATIC STRIPS ON PANELS 6731 AND 6732 ARE CORRODED OUT OF LIMITS. REMOVED AND REPLACED DAMAGED STRIPS. 2 L 7 2 4T RT T00011AT 2008012800175 20080128 00175 SO 2008 1 28 FDKA200712410 1 20071218 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 840MJ 145429 FDM 6095 MCO (0610 PHX LCL) - EMERGENCY LIGHT INOP. MX RESET. 2 L 7 2 4T RT T00011AT 2008012800176 20080128 00176 SO 2008 1 28 FDKA200712429 1 20071229 A 5210 SEAL EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 835MJ 145353 FDM FLT 6131 MCO-FLL (1454 PHX LCL) - MAIN CABIN DOOR HARD TO CLOSE. MX CLEANED AND LUBED DOOR SEAL, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800177 20080128 00177 SO 2008 1 28 FDKA200710278 1 20071027 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM 6075 MCO (0928 PHX LCL) - MAIN CABIN DOOR HARD TO OPEN AND CLOSE. MX LUBED MAIN CABIN DOOR. 2 L 7 2 4T RT T00011AT 2008012800191 20080128 00191 SO 2008 1 28 FDKA200710282 1 20071027 A 5210 GATE EMB 145 EMB145LR 3260212 SO PAX DOOR OUT OF ADJUST A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 832MJ 145310 FDM RON TPA (1533 PHX LCL) - PASSENGER DOOR FLAP WILL NOT CLOSE. MX ADJUSTED DOOR. 2 L 7 2 4T RT T00011AT 2008012900034 20080129 00034 2008 1 29 2008UALA00182 4 20070110 A 2565 O-RING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L5 DOOR SLIDE LEAKING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 118UA GJ1043 28811 DOOR 5 LEFT SLIDE/RAFT PRESSURE LOW. FILL VALVE LEAKING AROUND O-RING. REPLACED O-RING. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012900221 20080129 00221 NM 2008 1 29 USAA920080186 1 20071213 A 5320 146N545112 INTERCOSTAL BOEING 757 7572B7 1384964 NM BS 1500-1520 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 27810 MCN - MAJOR REPAIR - C4 CHECK - NR 6056657, CORROSION ON INTERCOSTAL, BS 1500 - BS 1520, S29R. REPLACED INTERCOSTAL, BS 1500 - BS 1520, S29R IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008012900222 20080129 00222 SO 2008 1 29 FDKA200709488 1 20070902 A 5414 PANEL EMB 145 EMB145LR 3260212 SO NACELLE DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 PANEL 412CL HAS AN ELONGATED HOLE THAT IS BEYOND LIMITS. INSTALLED A DIMPLED WASHER OVER THE DAMAGE. 2 L 7 2 4T RT T00011AT 2008012900223 20080129 00223 SO 2008 1 29 FDKA200711343 1 20071121 A 5241 DOOR EMB 145 EMB145LR 3260212 SO GALLEY LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 860MJ 145773 FDM 6200 GALLEY DOOR WILL NOT CLOSE. MX PERFORMED ADJUSTMENT CHECK AND LUBED DOOR. 2 L 7 2 4T RT T00011AT 2008012900224 20080129 00224 SO 2008 1 29 FDKA200709491 1 20070904 A 5411 FRAME EMB 145 EMB145LR 3260212 SO RT NACELLE CHAFED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 RT LOWER ENGINE COWLING, THIRD FRAME FROM THE AFT END, IS CHAFED OUT OF LIMITS. REPAIRED THE DAMAGE. 2 L 7 2 4T RT T00011AT 2008012900225 20080129 00225 SO 2008 1 29 FDKA200709502 1 20070920 A 5411 14576631622 FRAME EMB 145 EMB145LR 3260212 SO RT NACELLE CHAFED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 RT LOWER ENGINE COWLING AFT FRAME IS CHAFED BEYOND LIMITS. REMOVED AND REPLACED DAMAGED FRAME. 2 L 7 2 4T RT T00011AT 2008012900226 20080129 00226 SO 2008 1 29 FDKA200709492 1 20070902 A 5520 STRUCTURE EMB 145 EMB145LR 3260212 SO RT ELEVATOR BENT A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 THE RT ELEVATOR HAD DAMAGE FROM CONTACT WITH THE HANGAR DOOR. REMOVED AND REPLACED ELEVATOR. 2 L 7 2 4T RT T00011AT 2008012900227 20080129 00227 SO 2008 1 29 FDKA200709499 1 20070918 A 5320 14521725403 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 RT SILL FWD OF SERVICE DOOR IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED SILL. 2 L 7 2 4T RT T00011AT 2008012900228 20080129 00228 SO 2008 1 29 FDKA200709485 1 20070924 A 3244 TIRE EMB 145 EMB145LR 3260212 SO MLG FAILED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 848MJ 8227 145530 FDM 6035 DAY (0747 PHX LCL). DECLARED EMERGENCY. NR 2 MAIN TIRE BLOWN AND LEFT INBOARD FLAP DAMAGED. MX REMOVED AND R EPLACED NR 1 AND 2 WHEEL ASSEMBLIES AND ARE STILL INSPECTING THE DAMAGE. 2 L 7 2 4T RT T00011AT 2008012900229 20080129 00229 SO 2008 1 29 FDKA200709484 1 20070924 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 838MJ 145384 FDM 6061 MCO (0621 PHX LCL) - MAIN CABIN DOOR STICKING. MX LUBED DOOR OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012900230 20080129 00230 SO 2008 1 29 FDKA200709500 1 20070918 A 5415 14531653002 BRACKET EMB 145 EMB145LR 3260212 SO PRECOOLER CRACKED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 PRECOOLER MOUNT BRACKET CRACKED ON THE NR 2 ENGINE. REMOVED AND REPLACED MOUNT BRACKET. 2 L 7 2 4T RT T00011AT 2008012900232 20080129 00232 SO 2008 1 29 FDKA200709501 1 20070914 A 3210 14571035413 CAP EMB 145 EMB145LR 3260212 SO TRUNNION BEARING CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 RT AFT MLG TRUNNION BEARING CAP CORRODED. REMOVED AND REPLACED CAP. 2 L 7 2 4T RT T00011AT 2008012900234 20080129 00234 SO 2008 1 29 FDKA200708424 1 20070827 A 3297 CONNECTOR EMB 145 EMB145LR 3260212 SO LT MLG DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 833MJ 16096 145327 FDM 6168 MCO (0750 PHX LCL) - LEFT MAIN WILL NOT COME UP. CONFIRMED DOWN. MX REMOVED AND REPLACED WOW PROX SWITCH AND CONNECTOR. 2 L 7 2 4T RT T00011AT 2008012900236 20080129 00236 SO 2008 1 29 FDKA200710561 1 20071020 A 2797 CONNECTOR EMB 145 EMB145LR 3260212 SO SPOILER CONTROL UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 829MJ 145228 FDM 9960 BNA (1445 PHX LCL) - FLIGHT SPOILERS FAILED IN FLIGHT. MX RESECURED CONNECTOR ON CONTROLLER, OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012900237 20080129 00237 SO 2008 1 29 FDKA200709453 1 20070907 A 2731 3621001013 CONTROL UNIT EMB 145 EMB145LR 3260212 SO PITCH TRIM INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825J 10690 145179 FFDM FLT6044 JFK - PITCH TRIM MAIN INOP. MX REPLACED HSCU. 2 L 7 2 4T RT T00011AT 2008012800034 20080128 00034 SO 2008 1 28 FDKA200709498 1 20070917 A 5320 14522459003 ANGLE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 RAMP ANGLE AT Y: 0.0 AND FR 19-20 CORRODED BEYOND LIMITS. REMOVED AND REPLACED RAMP ANGLE. 2 L 7 2 4T RT T00011AT 2008012800044 20080128 00044 SO 2008 1 28 FDKA200704174 1 20070420 A 5330 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 852MJ 145567 CENTER BUTT STRAP BETWEEN FRAME 15 TO JUST AFT OF FRAME 16 IS CORRODED BEYOND ALLOWABLE LIMITS. DAMAGE WAS REPAIRED. 2 L 7 2 4T RT T00011AT 2008012800045 20080128 00045 SO 2008 1 28 FDKA200708433 1 20070829 A 2760 852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO SPOILERS MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 834MJ 15723 145340 FDM RON MCO(1719 PHX LCL) - SPOILER FAIL MESSAGE IN FLIGHT. MX MAINTENANCE REMOVED AND REPLACED LT SPOILER CONTROL PROX SWITCH. 2 L 7 2 4T RT T00011AT 2008012800055 20080128 00055 SO 2008 1 28 FDKA200709470 1 20070914 A 5210 SEAL EMB 145 EMB145LR 3260212 SO PAX DOOR LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6155 MCO - PAX DOOR DIFFICULT TO CLOSE. MX RE-SECURED DOOR FRAME SEAL STICKING OUT. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800064 20080128 00064 SO 2008 1 28 FDKA200710539 1 20071010 A 2760 14533022409 CONTROL UNIT EMB 145 EMB145 3260210 SO SPOILERS MALFUNCTIONED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 825MJ 13228 145179 FRL RON TPA - SPOILER FAULT, SPOILER OPEN MESSAGE. REMOVED AND REPLACED SPOILER CONTROL UNIT. 2 L 7 2 4F RT T00011AT 2008012800072 20080128 00072 SO 2008 1 28 FDKA200710269 1 20071024 A 2710 SWITCH EMB 145 EMB145LR 3260212 SO AILERON SYS DIRTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6121 ORF (0341 PHX LCL). AILERON SYSTEM 2 WILL NOT DISCONNECT. MX CLEANED AILERON SHUT OFF SYSTEM 2 SWITCH. OPS C HECK GOOD. 2 L 7 2 4T RT T00011AT 2008012800078 20080128 00078 SO 2008 1 28 FDKA200707405 1 20070714 A 5320 14530644413 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 860MJ 145773 LT INBD FLOOR FLANGE FOUND CORRODED. REMOVED AND REPLACED FLANGE. 2 L 7 2 4T RT T00011AT 2008012800085 20080128 00085 SO 2008 1 28 FDKA200711350 1 20071101 A 3210 14571035413 CAP EMB 145 EMB145LR 3260212 SO MLG BEARING CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 830MJ 145259 RT MLG FWD LOWER BEARING CAP CORRODED. REWORKED AND REINSTALLED RT FWD MIG TRUNNION BEARING CAP. 2 L 7 2 4T RT T00011AT 2008012800087 20080128 00087 SO 2008 1 28 FDKA200711351 1 20071102 A 5524 STRIP EMB 145 EMB145LR 3260212 SO RT ELEVATOR CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 830MJ 145259 RT ELEVATOR TIP HAS CORRODED BONDING STRIPS. REMOVED AND REPLACED CORRODED STRIPS. 2 L 7 2 4T RT T00011AT 2008012800101 20080128 00101 SO 2008 1 28 FDKA200707410 1 20070726 A 5514 14521939006 BRACKET EMB 145 EMB145LR 3260212 SO HORIZONTAL STAB CHAFED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 833MJ 145327 HORIZONTAL STABILIZER, RT HINGE PIN SAFETY STOP BRACKET IS CHAFED OUT OF LIMITS. REMOVED AND REPLACED BRACKET. 2 L 7 2 4T RT T00011AT 2008012800109 20080128 00109 SO 2008 1 28 FDKA200706311 1 20070625 A 5210 14523092403 ROD EMB 145 EMB145LR 3260212 SO PAX DOOR DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 145416 CRANK ROD ASSY WAS FOUND TO HAVE ELONGATED HOLES AND BUSHINGS NOT PROPERLY SEALED CAUSING HARD TO OPEN AND CLOSE MAIN DO OR. REPLACED CRANK ROD ASSY. 2 L 7 2 4T RT T00011AT 2008012800128 20080128 00128 SO 2008 1 28 FDKA200712438 1 20071206 A 5751 14569382610 FITTING EMB 145 EMB145LR 3260212 SO RT AILERON GOUGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 THE LT AILERON DAMPER FITTING IS DAMAGED. THE FITTING HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2008012800142 20080128 00142 SO 2008 1 28 FDKA200707321 1 20070702 A 2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY FALSE ACTIVATION A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 847MJ 145517 FDM 6128 FLL (1735 PHX LCL) - CREW RETURNED TO THE FIELD DUE TO LAV SMOKE WARNING. MX PERFORMED DETAILED GVI OF LAV, CA BIN, CARGO BAY AND AFT EQUIPMENT BAY NO EVIDENCE OF SMOKE OR FIRE. PERFORMED ENGINE RUN WITH BOTH PACKS ON NO EVIDENCE OF SMOKE NOTED. PERFORMED OPS CHECK OF LAV SMOKE DETECTOR, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008012800154 20080128 00154 SO 2008 1 28 FDKA200710294 1 20071029 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX OUT OF ADJUST A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 145416 FDM RON RDU (1832 PHX LCL) - MAIN DOOR REAL HARD TO OPEN. MX ADJUSTED DOOR, CLEANED AND LUBED LATCH POINTS AND OPS CHEC KED. 2 L 7 2 4T RT T00011AT 2008012800157 20080128 00157 SO 2008 1 28 FDKA200710532 1 20071008 A 5210 BEARING EMB 145 EMB145LR 3260212 SO PAX DOOR HANDLE STICKING A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 834MJ 145340 FDM 6085 MCO (0815 PHX LCL) - MAIN CABIN DOOR HANDLE STICKS. MX INSTALLED BEARING ON DOOR. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800167 20080128 00167 SO 2008 1 28 FDKA200710292 1 20071029 A 2750 FCU EMB 145 EMB145LR 3260212 SO TE FLAPS MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 841MJ 145448 FDM 6005 MCO (1036 PHX LCL) - FLAP FAIL. MX REMOVED AND REPLACED FECU. 2 L 7 2 4T RT T00011AT 2008012800174 20080128 00174 SO 2008 1 28 FDKA200709461 1 20070911 A 2731 SWITCH EMB 145 EMB145LR 3260212 SO PITCH TRIM INTERMITTENT A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 828MJ 145218 FDM FLT 6123 RDU - BACKUP PITCH TRIM SWITCH INTERMITTENT. MX LUBED SWITCH AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2008012800198 20080128 00198 SO 2008 1 28 FDKA200708376 1 20070806 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 834MJ 145340 FDM 6163 PNS-FLL (1919 PHX LCL) - FUEL SMELL IN CABIN AFTER LANDING. MX TROUBLESHOT AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012900208 20080129 00208 WP 2008 1 29 UPS08851423 1 20071223 A 5540 BRACKET DOUG DC8 DC871F 302199D WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 RUDDER L/E FAIRING ATTACH BRACKET CRACKED IN 3 EA PLACES, BETWEEN TOP AND 2ND FROM TOP HINGE POINTS. REMOVED, FABRICATED AND INSTALLED REPAIR BRACKET ON RUDDER L/E IAW SRM 51-01-21, AND DWG 5701591. 2 L 7 4 4F RT 4A25 2008012900209 20080129 00209 WP 2008 1 29 UPS08851425 1 20071227 A 5230 STOP FITTING DOUG DC8 DC871F 302199D WP FS 320 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 A-PIT DOOR STOP PAD MOUNT AFT HAS EXFOLIATION CORROSION. REMOVED AND REPLACED A-PIT DOOR STOP PAD MO UNT FITTING AT STA 320 IAW SRM 51-03-00-0 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2008012900212 20080129 00212 WP 2008 1 29 UPS08851432 1 20071227 A 5280 SKIN DOUG DC8 DC871F 302199D WP RT MLG DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 REPAIR DOUBLER CRACKED ON R/MLG INBD DOOR INTERIOR SKIN, BOTTOM. REMOVED CRACKED REPAIR DOUBLER ON R /MLG INBD DOOR INTERIOR SKIN IAW SRM 51-01-21A. FABRICATED AND INSTALLED REPAIR DOUBLER ON R/MLG INBD DOOR INTERIOR IAW SRM 52-06-00 FIG 1. 2 L 7 4 4F RT 4A25 2008012900215 20080129 00215 NM 2008 1 29 UPS08M51415 1 20071228 A 5740 ARB2850505 FITTING DOUG MD11 MD11F 3023600 NM LT SLAT TRACK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 251UP 48744 INSPECTION TYPE:1C LT WING FIXED LE RIB FITTING IB OF NR 16 SLAT TRACK IS CRACKED. REMOVED AND REPLACED RIB FITTING IAW MD-11 SRM 51-35-01 AND 51-33-01. 2 L 7 3 4F RT A22WE 2008012900216 20080129 00216 NM 2008 1 29 UPS08M51416 1 20071228 A 5740 ARB2850506 FITTING DOUG MD11 MD11F 3023600 NM RT SLAT TRACK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 251UP 48744 INSPECTION TYPE:1C RT WING FIXED LE RIB FITTING IB OF NR 16 SLAT TRACK IS CRACKED. REMOVED AND REPLACED RIB FITTING IAW MD-11 SRM 51-35-01 AND 51-33-01. 2 L 7 3 4F RT A22WE 2008012900217 20080129 00217 NM 2008 1 29 UPS08M51417 1 20071228 A 5754 ARB7118 SKIN DOUG MD11 MD11F 3023600 NM RT WING LE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 251UP 48744 INSPECTION TYPE:1C RT FIXED LE STRUCTURE INSIDE PANEL 626FB HAS EXFOLIATION CORROSION. REMOVED CORROSION, FABRICATED, A ND INSTALLED REPAIR DOUBLERS IAW MD-11 SRM 57-10-00. 2 L 7 3 4F RT A22WE 2008012900218 20080129 00218 NM 2008 1 29 UPS08M51418 1 20071107 A 5330 DOUBLER DOUG MD11 MD11 3023602 NM BS 1954 L51R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C AFT CARGO/AT STATION 1954 LONGERON 51 RT, DOUBLER FOUND WITH SURFACE CORROSION. AFT CARGO STA 1954 L5 1 RT LONG END SPLICE FASTENERS REMOVED, END SPLICE CORRODED REMOVED, FOUND EXCEEDED LIMIT PER SRM 53-00-01 FIG1 AVIR35. NEW END SPLICE AGA3092-503N HOLES PICK UP. NEW SPLICE END INSTALLED PER SRM 51-33-01VIIR35. 2 L 7 3 4F RT A22WE 2008012900239 20080129 00239 2008 1 29 FDKA20710563 4 20071022 A 3425 COMPUTER EMB 145 EMB145LR 3260212 SO AHRS MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 838MJ 145384 FDM 6001 MCO (1240 PHX LCL) - SPS ADVANCE EICAS MESSAGE, HEADING/ATTITUDE FAIL ON PFD/MFD2. MX REPLACED AHRS NR 2 COMPU TER. 2 L 7 2 4T RT T00011AT 2008012900240 20080129 00240 SO 2008 1 29 FDKA200710559 1 20071019 A 3260 TRANSDUCER EMB 145 EMB145LR 3260212 SO NR 1 WHEEL LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 835MJ 145353 FDM 6031 ATL (1322 PHX LCL) - I/B SPOILER RAPID FLUTTER DURING TAXIING. MX FOUND NR 1 WHEEL TRANSDUCER WAS LOOSE AND RE SECURED IT AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2008012900242 20080129 00242 SO 2008 1 29 FDKA200710277 1 20071027 A 2731 SWITCH EMB 145 EMB145LR 3260212 SO PITCH TRIM DIRTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 FDM 6201 FLL (0341 PHX LCL) - ROLL TRIM SWITCH INOP. MX REMOVED DEBRIS FROM SWITCH OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012900243 20080129 00243 SO 2008 1 29 FDKA200707346 1 20070724 A 5210 14525311403 SEAL EMB 145 EMB145LR 3260212 SO PAX DOOR LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6104 MCO - SQUEALING FROM TOP OF MAIN CABIN DOOR DURING PRESSURIZATION. MX RE-INSTALLED SEAL ON FRAME, OPS CK AND L EAD CK GOOD. 2 L 7 2 4T RT T00011AT 2008012900245 20080129 00245 SO 2008 1 29 FDKA200707412 1 20070728 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 858MJ 145767 RT FWD SERVICE DOOR SILL CORRODED. REPAIRED FWD SERVICE DOOR SILL. 2 L 7 2 4T RT T00011AT 2008012900246 20080129 00246 SO 2008 1 29 FDKA200711311 1 20071103 A 2731 14534177405 CONTROL PANEL EMB 145 EMB145LR 3260212 SO PITCH TRIM INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 853MJ 12249 145464 FDM FLT 6007 JFK (1251 PXH LCL) - BACK UP PITCH TRIM FAIL. MX REMOVED AND REPLACED CONTROL PANEL. 2 L 7 2 4T RT T00011AT 2008012900249 20080129 00249 SO 2008 1 29 FDKA200711313 1 20071103 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 145416 FDM FLT 6025 ATL (1554 PHX LCL) - MAIN CABIN DOOR HARD TO OPEN AND CLOSE. MX LUBED DOOR SEAL. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012900252 20080129 00252 SO 2008 1 29 FDKA200708396 1 20070818 A 5101 INSULATION EMB 145 EMB145LR 3260212 SO CABIN BURNED A FDKA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 860MJ 145773 FDM 6003 JFK (0920 PHX LCL). CREW RETURNED TO THE FIELD DUE TO A STRONG SMOKE ODOR COMING FROM ROOF OF GALLEY. MX FOUN D INSULATION AGAINST LIGHT ASSY IN GALLEY, REPOSITIONED INSULATION. NO FURTHER SMOKE SMELL FOUND. 2 L 7 2 4T RT T00011AT 2008012900256 20080129 00256 WP 2008 1 29 UPS08851442 1 20071230 A 5344 HINGE DOUG DC8 DC871F 302199D WP FS 1160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 D-PIT DOOR FWD DOOR LINK HINGE WEB CRACKED IN DOUBLER. REMOVED, FABRICATED, AND INSTALLED REPAIR DOU BLER ON D-PIT DOOR FWD LINK HINGE WEB IAW SRM 51-1-21, AND SRM 51-02-00-0, AND DWG 5616673. 2 L 7 4 4F RT 4A25 2008012900257 20080129 00257 WP 2008 1 29 UPS08851443 1 20071226 A 5510 FAIRING DOUG DC8 DC871F 302199D WP FS 1834 DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 RT HORIZONTAL STAB FAIRING IS DELAMINATED. REMOVED DELAMINATED CORE AND SKIN ON R/HORIZ LWR STAB FAR ING IAW SRM 51-1-9A. FABRICATED AND INSTALLED REPAIR CORE PLUG AND DOUBLER IAW SRM 51-1-9A. 2 L 7 4 4F RT 4A25 2008012900258 20080129 00258 WP 2008 1 29 UPS08851444 1 20071227 A 5522 SKIN DOUG DC8 DC871F 302199D WP LT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 2 EA EDGE CRACKS ON INBD LWR EDGE OF LT ELEVATOR. REMOVED AND REPLACED LWR SKIN PANEL AT STA XE 21.4 71-XE 49.143 IAW SRM 51-1-21, AND SRM 55-02-00 FIG 006. 2 L 7 4 4F RT 4A25 2008012900259 20080129 00259 WP 2008 1 29 UPS08851445 1 20071229 A 5321 FLOORBOARD DOUG DC8 DC871F 302199D WP FS -52.000 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 NUMEROUS HAT CHANNELS CRACKED FLT DECK FLOORBOARD NR 678. REMOVED AND REPLACED CRACKED HAT CHANNELS ON FLT DECK PNL NR 678 IAW SRM 51-1-21 AND DWG 3619353. 2 L 7 4 4F RT 4A25 2008012900263 20080129 00263 WP 2008 1 29 UPS08851448 1 20071230 A 5320 FLOOR SUPPORT DOUG DC8 DC871F 302199D WP FS -12.000 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 FLOOR BOARD NR 676F HAT CHANNEL IS GOUGED. REMOVED AND REPLACED HAT CHANNEL ON FLOORBARD PANEL NR 67 6F IAW SRM 53-07-03-0. 2 L 7 4 4F RT 4A25 2008013000015 20080130 00015 EU 2008 1 30 TRBA2007084 1 20071013 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHTS FAILED A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 541AT 541 F/A COULD NOT OPERATE ALL CABIN EMERGENCY LIGHTS USING AFT EMERGENCY LIGHTS PUSH BUTTON. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK FIN NR 62WL IAW JIC NR 33-51-20. 2 H 7 2 4T RT A53EU 2008012800124 20080128 00124 SO 2008 1 28 FDKA200711345 1 20071124 A 2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY DIRTY A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 858MJ 145767 FDM 6181 CLT - LAV SMOKE INDICATION IN FLIGHT. MX FOUND GUNK IN SMOKE DETECTOR. MX CLEANED AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012800125 20080128 00125 SO 2008 1 28 FDKA200711332 1 20071112 A 5210 HANDLE EMB 145 EMB145LR 3260212 SO PAX DOOR LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM 5968 ATL (0955 PHX LCL) - MAIN DOOR OUT SIDE HANDLE WILL NOT CLOSE FULLY. MX TIGHTENED LOOSE HARDWARE ON DOOR. OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012800126 20080128 00126 SO 2008 1 28 FDKA200711333 1 20071112 A 2620 337000271 BOTTLE EMB 145 EMB145LR 3260212 SO EXTINGUISHER UNKNOWN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 852MJ 901 145567 FDM 6150 TYS (0517 PHX LCL) - BAGGAGE EXTINGUISHING BOTTLE CAUTION ILLUMINATED. MX REMOVED AND REPLACED BAGGAGE BOTTLES , OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012800129 20080128 00129 SO 2008 1 28 FDKA200712405 1 20071216 A 7830 THRUST REVERSER EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A FDKA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 07 846MJ 145507 FDM 6041 JFK - E2 T/R DISAGREE MESSAGE ON TAKEOFF ROLL. MX DEFERRED THE REVERSER. 2 L 7 2 4T RT T00011AT 2008012800131 20080128 00131 SO 2008 1 28 FDKA200708425 1 20070827 A 2730 0020BN4AMOD3A COMPUTER EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 830MJ 401 145259 FDM 6118 MCO (0750 PHX LCL) - SPS 1 AND 2 INOP ON EICAS. MX REMOVED AND REPLACED SPS COMPUTER. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008012800132 20080128 00132 SO 2008 1 28 FDKA200708437 1 20070831 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 851MJ 145572 MAIN CABIN DOOR IS HARD TO OPEN. MX LUBED DOOR HATCH, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008012800140 20080128 00140 SO 2008 1 28 FDKA200706316 1 20070628 A 4910 ACCESS PANEL EMB 145 EMB145LR 3260212 SO APU BAY CRACKED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 PANEL 313CL, APU COWLING DOOR IS CRACKED AROUND THE LATCHES. REPAIRED DAMAGE. 2 L 7 2 4T RT T00011AT 2008012800155 20080128 00155 SO 2008 1 28 FDKA200712406 1 20071214 A 5270 SWITCH EMB 145 EMB145LR 3260212 SO CARGO DOOR OUT OF ADJUST A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 854MJ 145490 FDM 6107 ALB (0512 PHX LCL) - ABORTED T/O. BAG DOOR WARNING LIGHT ILLUMINATED. MX CLEANED ADJUSTED MICROSWITCH. 2 L 7 2 4T RT T00011AT 2008012800156 20080128 00156 SO 2008 1 28 FDKA200712407 1 20071215 A 2611 FAU751A4 CONTROL PANEL EMB 145 EMB145LR 3260212 SO SMOKE WARNING MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 847MJ 46 145517 FDM 6022 JFK (0620 PHX LCL) - LAV SMOKE WARNING IN FLIGHT. MX REMOVED AND REPLACED SMOKE DETECTOR PANEL. 2 L 7 2 4T RT T00011AT 2008012800199 20080128 00199 SO 2008 1 28 FDKA200708374 1 20070806 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM 6157 MCO (0650 PHX LCL) - MAIN CABIN DOOR DIFFICULT TO CLOSE. MX LUBED THE DOOR ROLLERS. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008013000046 20080130 00046 NM 2008 1 30 070183 1 20071218 A 3350 6011777 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS NO TEST A WX0A K NONE K FLUID LOSS IN INSP/MAINT 1 WP 19 883GA 49710 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT 2008013000047 20080130 00047 NM 2008 1 30 WX0A070184 1 20071230 A 3350 6011777 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS NO TEST A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 881GA 49708 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT 2008013000132 20080130 00132 EA 2008 1 30 SWIA200719086 1 20070920 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 983SW 7961 FS 280 FLOORBEAM IS CRACKED AT RBL9, FOUND AT C-CHECK. REPAIRED FS 280 FLOORBEAM RBL9 PER REO 601R 53-11-171 REV D. 2 L 7 2 4F RT A21EA 2008013000161 20080130 00161 EA 2008 1 30 SWIA200719088 1 20070920 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 983SW 7961 LEFT FS 621 FLOORBEAM ANGLE IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO 601R-53-61-117. 2 L 7 2 4F RT A21EA 2008013000162 20080130 00162 EA 2008 1 30 SWIA200719089 1 20070920 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 983SW 7961 FS 484 FLOOR SUPPORT INTERCOSTAL IS CRACKED ON OUTBOARD SIDE, FOUND AT C-CHECK. INSTALLED REPAIR ANGLE PER REO 601R-53- 41-059. 2 L 7 2 4F RT A21EA 2008013000124 20080130 00124 NM 2008 1 30 Q2SA746002 1 20070414 A 2197 CONNECTOR BOEING 747 747206B 1384856 NM NR 1 PACK LOOSE A Q2SA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 63 746SA 21111 DEPARTED KLAX AND FOUND NR 1 PACK SYSTEM INOPERATIVE. NO PRESSURIZATION. RETURNED TO KLAX. NO FUEL WAS DUMPED. FOUND NR 1 PACK CONTROL VALVE CONNECTOR LOOSE. SECURED NR 1 PACK CONTROL VALVE CONNECTOR. OPERATIONAL CHECK GOOD IN ACCORDA NCE WITH AMM 21-00-00. 2 L 7 4 4F RT A20WE 2008013100040 20080131 00040 NM 2008 1 31 UPS08M51439 1 20071207 A 5313 LONGERON SPLICE DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C CENTER CARGO/AT STATION 5-120 LONGERON 44RT FOUND SUSPECTED CRACK ON SPLICE DOUBLER. HFEC INSP C/O PE R DAC NDTSPM REV 13, 06-10-01.001 & CRACK FOUND AS MARKED APPROX 2 INCHES IN LENGTH. CRACKED SPLICE REMOVED PER SRM 51- 33-01 VII R35. NEW SPLICE FASTENER HOLES PICKED UP SRM 51-31-01 VII R35. NEW SPLICE INSTALLED PER SRM 51-33-01 VII R35 . ATTACH INNER SUPPORT FASTENERS REINSTALLED PER SRM 51-33-01 VII R35. 2 L 7 3 4F RT A22WE 2008013000037 20080130 00037 EA 2008 1 30 SIMA200802103 1 20070116 A 5610 601R3303320 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SIMA B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 523AE 10152 ON FLIGHT 4468, CREW REPORTED FIRST OFFICERS SIDE WINDOW CRACKED IN FLIGHT. CREW DECLARED EMERGENCY. NO PRESS ISSUES N OTED CREW USED COCKPIT MASKS. MASKS NOT DROPPED IN CABIN AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FIRST OFF ICERS SIDE WINDOW. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008013000057 20080130 00057 2008 1 30 ARWA20071207 4 20071206 A 3417 HG280D80 COMPUTER DOUG DC10 DC1030 3023501 WP NR 2 ADC MALFUNCTIONED A ARWA O OTHER O OTHER CR CRUISE 1 SO 19 526MD 46998 FIRST OFFICER'S (FO) ALTIMETER ERRATIC; READS + 500 FT AT TIMES. REMOVED AND REPLACE NR 2 DIGITAL AIR DATA COMPUTER IN ACCORDANCE WITH M/M 34-16-01. PERFORMED OPERATIONAL CHECK IN ACCORDANCE WITH M/M 34-16-00, FOUND NORMAL. ALSO PERFORMED PITOT STATIC LEAK CHECK IN ACCORDANCE WITH M/M 34-11-00, NO LEAKS NOTED. 2 L 7 3 4F A22WE 2008013000160 20080130 00160 EA 2008 1 30 SWIA200719087 1 20070920 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 983SW 7961 RIGHT FS 621 FLOORBEAM ANGLES ARE CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 REO 601R-53-61-117 REV C . 2 L 7 2 4F RT A21EA 2008013100032 20080131 00032 NM 2008 1 31 UPS08M51436 1 20071227 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C MAIN DECK AFT ZONE, LBL 27.5 SEAT TRACK BADLY CORRODED BETWEEN STA 1671 & STA 1771. CORROSION AT MAIN DECK BETWEEN STA 1671 TO 1771 LBL 27.5 ON SEAT TRACK CROWN BASE & FLANGE AREA. REMOVED PER SRM 51-21-01 VII R35 FOUND EXCEEDS LIMITS PER SRM 53-70-00 FIG 3 VI R35. SEAT TRACK CROWN BASE ORIGINAL THK 0.100" REMAIN 0.050". NEW SEAT TRACK REPAIR SECT & SPLICES FAB & INSTALLED PER SRM 53-70-00 FIG 1 VI R35 & SRM 51-31-01 VII REV 35. 2 L 7 3 4F RT A22WE 2008013100033 20080131 00033 NM 2008 1 31 UPS08M51437 1 20071211 A 5313 LONGERON SPLICE DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C CENTER CARGO AT STATION 1708 TO STATION 1716 LONGERON 48RT, LONGERON SP SPLICE DOUBLER FOUND CORRODED. CORROSION SPLICES REMOVED PER SRM 51-33-01 VII R35. NEW SPLICES P/N: AF A3113-1 2EA FAB PER DWG AFA3113 AND FASTENERS HOLE PICKUP PER SRM 51-31 -01 VII R35. NEW SPLICE REPROTECTED PER SRM 51-21-01 VII R35. NEW SPLICE PAINTED PER SRM 51 -21-01 VII R35. NEW SPLICE INSTALLED AS PER SRM 51-31-01 VII REV 35. 2 L 7 3 4F RT A22WE 2008013100235 20080131 00235 NM 2008 1 31 USAA920071341 1 20071129 A 5320 69374024 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 CLT - MAJOR REPAIR - C-18 CHECK - A CRACK FOUND ON FWD SERVICE DOOR CUTOUT ANGLE AT BS 291.5 - BS 394.5, S17R. REMOVED ANGLE IAW B737-300 SRM 51-70-11 AND BOEING DWG 69-37402. 2 L 7 2 4F RT A16WE 2008013100236 20080131 00236 EU 2008 1 31 USAA920071342 1 20071210 A 5315 D53472094008 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 649AW 803 SAL - MAJOR REPAIR - C-7 CHECK - CORROSION ON CABIN BEAM, BS 3101/FR 65+23" - BS 3158/FR 66+4", Y512. REPLACED CABIN BE AM BS 3101/FR 65+23" - BS 3158/FR 66+4", Y512 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008013000045 20080130 00045 WP 2008 1 30 070182 1 20071212 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 886GA 49931 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2008013000178 20080130 00178 NM 2008 1 30 DLM90080056 1 20071229 A 5530 BUSHING DOUG MD90 MD9030 3023690 NM VERTICAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 VERTICAL STABILIZER RT I/B HORIZONTAL STABILIZER MOUNT LVG/BUSHING CORRODED/PITTED. REPAIRED HORIZONTAL STABILIZER MOUN T LUG IAW MD90 SRM 55-30-05 VOL.I. 2 L 7 2 4F RT A6WE 2008013000179 20080130 00179 NM 2008 1 30 DLM90080057 1 20071229 A 5347 86003 SEAT TRACK DOUG MD90 MD9030 3023690 NM FS 624-826 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 CABIN SEAT TRACK CORRODED OUT OF LIMITS FS 624-826 LBL54. REPAIRED CABIN SEAT TRACK IAW MD90 SRM 53-40-01, VOL.I FIG 6. 2 L 7 2 4F RT A6WE 2008013100036 20080131 00036 NM 2008 1 31 UPS08M51438 1 20071216 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSLEAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C MAIN DECK FLOOR, RBL 75 SEAT TRACK CROWN & FLANGE FOUND CORRODED BETWEEN STA 1341 & STA 1381. CORROSI ON AT MAIN DECK BETWEEN STA 1341 TO STA 1381 RBL ON SEAT TRACK CROWN BASE & FLANGE AREA REMOVED PER SRM 51-21-01 VII R35 & FOUND EXCEED LIMITS PER SRM 53-70-00 FIG 3 VI R35. MAIN DECK RBL 75 DAMAGED SEAT TRACK SECT ATTACHING SPLICES REMOVE D PER SRM 51-31-01 VII R35. FAB AND INSTALLED SEAT TRACK REPAIR SECT PER SRM 53-70-00 VI R35/51-31-01 VII R35. 2 L 7 3 4F RT A22WE 2008013100286 20080131 00286 WP 2008 1 31 UPS08851464 1 20071229 A 5311 36169442 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 HEAVY CORROSION ON STA 834 FRAME BELOW RIGHT CUSP. REPAIRED LOWER FUSELAGE FRAME CENTER TO REAR SPAR FITTING AT STA 834 L21R IAW SAA EA 008-5320-01-A1254, UPS RAA DC8-53-20673, AND FAA FORM 8100-9. 2 L 7 4 4F RT 4A25 2008013100299 20080131 00299 EA 2008 1 31 A6WA200840002 1 20071202 A 2497 755469E TERMINAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE GENERATOR BURNED A A6WA O OTHER J WARNING INDICATION CL CLIMB 1 GL 31 468AW 7916 GENERATOR NR 1 CAUTION RECEIVED AT CRUISE, COMPLIED WITH QRH. FOUND AC GENEATOR BURNED UP AT TERMINALS. REMOVED AND RE PLACED GENERATOR NR 1 ASSY IAW AMM 24. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008013100300 20080131 00300 EA 2008 1 31 A6WA200840003 1 20071202 A 2497 TERMINAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE GENERATOR BURNED A A6WA O OTHER J WARNING INDICATION CL CLIMB 1 GL 31 426AW 9831 7669 GENERATOR NR 1 CAUTION RECEIVED AT CRUISE, COMPLIED WITH QRH. FOUND AC GENERATOR BURNED UP AT TERMINALS. REMOVED AND R EPLACED GENERATOR NR 1 ASSY IAW AMM 24. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008013100307 20080131 00307 EA 2008 1 31 SWIA200719084 1 20070920 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 983SW 7961 FS 280 FLOORBEAM ANGLE IS CRACKED AT LBL9, FOUND AT C-CHECK. REPAIRED FS 280 FLOORBEAM ANGLE AT LBL 9 PER CRJ200 REO 60 1E 53-11-138. 2 L 7 2 4F RT A21EA 2008013100308 20080131 00308 EA 2008 1 31 SWIA200719085 1 20070920 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 983SW 7741 FS 280 FLOORBEAM IS CRACKED AT LBL9, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO 601R-53-11-171 REV D. 2 L 7 2 4F RT A21EA 2008013100352 20080131 00352 EA 2008 1 31 SWIA200719095 1 20070925 A 2710 BEARING CNDAIR CL600 CL6002B19 1900309 EA LT AILERON WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 912EV 7728 LEFT AILERON HINGE BEARINGS ARE WORN, FOUND AT C-CHECK. REPLACED AILERON HINGE BEARINGS PER CRJ200 AMM TASK 20-26-00-91 0-810. 2 L 7 2 4F RT A21EA 2008013100353 20080131 00353 EA 2008 1 31 SWIA200719096 1 20070925 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 912EV 7728 STA 621 LEFT OUTBOARD FRAME IS CRACKED, FOUND AT C-CHECK. REPLACED DAMAGED AREA OF FLOOR SUPPORT ANGLE AT STA 621.00 PE R CRJ200 REO 601R-53-61-117 REV C. 2 L 7 2 4F RT A21EA 2008013100354 20080131 00354 EA 2008 1 31 SWIA200719097 1 20070925 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 912EV 7728 FS 280 FLOOR SUPPORT BEAM IS CRACKED AT LBL9, FOUND AT C-CHECK. REPAIRED DAMAGED SECTION OF FLOOR ANGLE AT STA 280 LBL9 IAW CRJ200 REO 601R-53-11-138 REV NC. 2 L 7 2 4F RT A21EA 2008013100355 20080131 00355 EA 2008 1 31 SWIA200719098 1 20070925 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 912EV 7728 FS 280 FLOOR SUPPORT BEAM IS CRACKED AT LBL 9, FOUND AT C-CHECK. COMPLIED WITH REPAIR OF FLOOR SUPPORT BEAM PER CRJ200 REO 53-11-171 REV D SCHEME B. 2 L 7 2 4F RT A21EA 2008013100356 20080131 00356 EA 2008 1 31 SWIA200719099 1 20070925 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 912EV 7728 FS 280 FLOOR SUPPORT BEAM IS CRACKED AT RBL9, FOUND AT C-CHECK. COMPLIED WITH REPAIR OF FLOOR SUPPORT BEAM PER CRJ200 R EO 53-11-171 REV D SCHEME B. 2 L 7 2 4F RT A21EA 2008013100357 20080131 00357 EA 2008 1 31 SWIA200719100 1 20070925 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 912EV 7728 CARGO COMPARTMENT FRAME HAS SIGNS OF CORROSION UNDER FLOORBOARD 281LLF, FOUND AT C-CHECK. REMOVED MINOR CORROSION ON TH E FRAME PER CRJ200 SRM 5-21-06 PG 1-4. 2 L 7 2 4F RT A21EA 2008013100358 20080131 00358 EA 2008 1 31 SWIA200719101 1 20070914 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 936SW 7726 UPPER FLOOR SUPPORT FRAME IS CRACKED AT RBL9, FOUND AT C-CHECK. INSTALLED REPAIR PARTS AT RBL9 PER CRJ200 SRM 51-42-06 P 11. 2 L 7 2 4F RT A21EA 2008020100004 20080201 00004 WP 2008 2 1 UPS08851471 1 20071230 A 5514 ANGLE DOUG DC8 DC871F 302199D WP HORIZ STAB BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 RIGHT HORIZ STAB 2ND FROM AFT MOVEABLE FAIRING ATTACH "H" ANGLE BROKEN. REMOVED, FABRICATED, AND INS TALLED "H" ANGLE ON RIGHT HORIZ STAB 2ND FROM AFT MOVEABLE FAIRING IAW SRM 51-01-21-0, AND DWG 3702408. 2 L 7 4 4F RT 4A25 2008020100005 20080201 00005 WP 2008 2 1 UPS08851472 1 20071229 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 STA 1580 FRAME BROKEN ABOVE CUSP, LT SIDE L21L. CUT OUT DAMAGED AREA OF FRAME 1580 ABOVE CUSP LT SID E IAW SRM 53-02 -00 FIG 02. FABRICATED AND INSTALLED FRAME SEGMENT AND 2EA REPAIR ANGLES ON FRAME 1580 L21L IAW SRM 53- 02-00 FIG 002. 2 L 7 4 4F RT 4A25 2008020100006 20080201 00006 NM 2008 2 1 UPS08M51475 1 20071119 A 5514 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C LEFT HORZ STAB NR 23 BARREL NUT HOLE FOUND CORROSION. CORR AT B NUT REMOVED. BORE BOTTOM SURFACE CLE ANED & BORE REAM TO 1.067" DIA, REMN BLEND OUT 0.048" DEEP, EXCEEDED LIMITS. 10X MAG-DETAIL VISUA L INSP C/O & FOUND NO CORR EVIDENT. B NUT BORE, BLEND OUT VOIDS & BOTTOM PERIPHERY RADIUS, SMOOTHEN & PROTECTED. REPAIR SLEEVE BUSHING FAB & INSTALLED. REPAIR C/O IS ACCEPTABLE PER EN1726-07. 2 L 7 3 4F RT A22WE 2008020100014 20080201 00014 CE 2008 2 1 BSAASDR0728 1 20071228 A 3610 131823E4M0160 TUBE BEECH 1900 1900D 1154162 CE BLEED AIR SYS DEFECTIVE A BSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 05 173YV UE173 RIGHT BLEED FAIL ILLUMINATED IN FLIGHT. ITEM INITIALLY DEFERRED. REMOVED AND REPLACED EVA TUBING, RAN AIRCRAFT OPERATI ONAL CHECK GOOD. 2 L 7 2 4T RT A24CE 2008020100058 20080201 00058 NM 2008 2 1 CALA0800066 1 20071225 A 3350 78980 BATTERY PACK BOEING 757 757224 1384958 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17133 29282 EMERGENCY EXIT PATH LIGHTS AT ROW 26, AFT RT SIDE OVERHEAD BEZEL AFT CABIN, DOOR 4R EXIT SIGNS AND DOOR 4R EXTERIOR EMER GENCY LIGHTS INOP. FOUND BATTERY PACK THAT CONTROLS EMERGENCY PATH LIGHTS 26-34 ROW, RT SIDE OVERHEAD BEZELS AND DOOR 4 R EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY PACK PER MM 33-51-07. 2 L 7 2 4F RT A2NM 2008020100100 20080201 00100 EA 2008 2 1 SWIA200719102 1 20070914 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 936SW 7726 LOWER FLOOR SUPPORT IS CRACKED AT STA 280 LBL9, FOUND AT C-CHECK. INSTALLED REPAIR PARTS AT LBL9 LOWER FRAME PER CRJ200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008020100101 20080201 00101 EA 2008 2 1 SWIA200719103 1 20070914 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 936SW 7726 FS 280 RBL9 LOWER FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS AT FS 280 RBL 9 LOWER FLOOR SUPPOR T IAW CRJ200 REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 2008020100103 20080201 00103 EA 2008 2 1 SWIA200719105 1 20071223 A 5320 BEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 754SK 10215 STA 280 BEAM IS CRACKED ON LEFT SIDE, FOUND AT C-CHECK. INSTALLED STA 280 BEAM AS PER CRJ700 SRM 51-42-06 AND REO 670-5 3-11-047. 2 L 7 2 4F RT A21EA 2008020100104 20080201 00104 EA 2008 2 1 SWIA200719106 1 20071223 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 754SK 10215 COCKPIT FLOOR SUPPORT AT FS280 IS CRACKED, FOUND AT C-CHECK. REPLACED FLOOR SUPPORT AS PER CRJ700 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008020100107 20080201 00107 EA 2008 2 1 SWIA200719109 1 20070915 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 982SW 7956 FS 621 LEFT FLOOR ANGLE IS CRACKED, FOUND AT C-CHECK. REPAIRED FLOOR SUPPORT ANGLE PER CRJ200 SRM 51-42-06 AND SRM 51-4 2-21. 2 L 7 2 4F RT A21EA 2008020100110 20080201 00110 EA 2008 2 1 SWIA200719112 1 20070915 A 2710 BEARING CNDAIR CL600 CL6002B19 1900309 EA AILERON PCU LINK CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 982SW 7956 RIGHT AILERON INBOARD PCU OUTPUT LINK ASSEMBLY HAS CORRODED BEARING, FOUND AT C-CHECK. REPLACED RIGHT AILERON PCU LINK ASSEMBLY PER CRJ200 AMM 27-14-15-000-801. 2 L 7 2 4F RT A21EA 2008020100111 20080201 00111 EA 2008 2 1 SWIA200719113 1 20070926 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 913EV 7731 LOWER FLOOR SUPPORT FRAME AT STA 280 AT RBL9 IS CRACKED, FOUND AT C-CHECK. MADE REPAIRS IAW CRJ200 REO 601R-53-11-170. 2 L 7 2 4F RT A21EA 2008020100142 20080201 00142 NM 2008 2 1 EIA2007194 1 20071102 A 2133 7242822 ACTUATOR BOEING 747 747230B 1384889 NM OUTFLOW VALVE MALFUNCTIONED A EIAA G O2 MASK DEPLOYED O OTHER CL CLIMB 1 NM 09 487EV 23286 DURING CLIMB-OUT, LEFT OUTFLOW VALVE STOPPED CLOSING IN AUTO. CABIN STARTED CLIMBING AT MAX RATE WENT TO MANUAL IT STIL L DID NOT CLOSE CABIN REACHED 16,000 FT. ALL CREW ON OXYGEN. CONTINUED ATTEMPTING TO CLOSE OUTFLOW VALVE MANUALLY UNTI L IT BEGAN CLOSING TO GET CONTROL OF CABIN. REMOVED AND REPLACED LEFT OUTFLOW VALVE ACTUATOR PER B747 MM 21-31-08, OPS CHECKED NORMAL PER B747 MM 21-31-00. 2 L 7 4 4F RT A20WE 2008020100144 20080201 00144 NM 2008 2 1 EIA2007220 1 20071119 A 5315 FLOORBEAM BOEING 747 747230F 1384829 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 490EV 24138 BS 420 RT UPPER DECK FLOORBEAM 2 DEFECTIVE FASTENER HOLES FOUND DUCTING ACCOMPLISHMENT OF EO-74-1625-01 REV D. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 490-53-014-2 REV A PART I AND II. 2 L 7 4 4F RT A20WE 2008020100145 20080201 00145 NM 2008 2 1 EIA2007221 1 20071121 A 5315 FLOORBEAM BOEING 747 747230F 1384829 NM FUSELAGE DEFECTIVE A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 490EV 24138 BS 340 RT UPPER DECK FLOORBEAM 2EA FASTENER HOLES DEFECTIVE PERE EO 53-747-1625-01 REV D. REMOVED DAMAGE, FABBED AND IN STALLED REPAIR PER ECRA 490-53-010-2. 2 L 7 4 4F RT A20WE 2008020100146 20080201 00146 NM 2008 2 1 EIA2007222 1 20071121 A 5315 FLOORBEAM BOEING 747 747230F 1384829 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 490EV 24138 BS 440 LT UPPER DECK FLOORBEAM 2 OVERSIZED FASTENER HOLES FOUND WHILE ACCOMPLISHING EO 53-747-1625-01 REV D. REMOVED DA MAGE, FABBED AND INSTALLED REPAIR PER ECRA 490-53-012-2. 2 L 7 4 4F RT A20WE 2008020100147 20080201 00147 NM 2008 2 1 EIA2007223 1 20071120 A 5315 FLOORBEAM BOEING 747 747230F 1384829 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 490EV 24138 BS 380 RT UPPER DECK FLOORBEAM 2 EA DEFECTIVE FASTENERS WERE FOUND DURING THE ACCOMPLISHMENT OF EO 53-747-1625 REV D. R EMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRAS 490-53-011-2. 2 L 7 4 4F RT A20WE 2008020100148 20080201 00148 NM 2008 2 1 EIA2007224 1 20071120 A 5310 DOOR FRAME BOEING 747 747230F 1384829 NM FUSELAGE MISREPAIRED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 490EV 24138 MAIN ENTRY DOOR NR 5L FRAME WEB BS 2231 STR 16L-17L IMPROPER EXISTING REPAIR. REMOVED REPAIR DOUBLER, FABBED AND INSTAL LED NEW REPAIR PER B747 SRM 53-10-04 FIGURE 91. 2 L 7 4 4F RT A20WE 2008020100149 20080201 00149 NM 2008 2 1 EIA2007196 1 20071102 A 3350 900835A BATTERY PACK BOEING 747 747230B 1384889 NM CABIN DISCHARGED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487EV 23286 EMERGENCY LIGHT CEILING OF FLIGHT DECK BETWEEN TWO LAVS INOP. REPLACED BATTERY CARTRIDGE EMERGENCY LIGHTS OPS CHECKED G OOD IAW MM 33-51-00 PAGE 201 AND 501. 2 L 7 4 4F RT A20WE 2008020100150 20080201 00150 2008 2 1 EIA2007197 4 20071111 A 2565 7A146721 SLIDE BOEING 747 747409 13848AU NM ENTRY DOOR LOW PRESSURE A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 780BA 24310 LT ENTRY DOOR 31 ESCAPE SLIDE INFLATION BOTTLE PRESSURE IS "0" PSI. REMOVED AND REPLACED SLIDE PER B747 MM 25-69-00. 2 L 7 4 4F RT A20WE 2008020100151 20080201 00151 NM 2008 2 1 EIA2007198 1 20071106 A 5320 WEB BOEING 747 747273C 1384896 NM NLG WW CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 NOSE WHEEL WELL HAS CRACK BS 270 WL 160 NWW WEB LT SIDE. REMOVED DAMAGE, NDT AREA, FABBED AND INSTALLED REPAIR PER B747 SRM 53-10-01 FIG 116 AND FIG 120. 2 L 7 4 4F RT A20WE 2008020100155 20080201 00155 NM 2008 2 1 EIA2007202 1 20071120 A 3350 900835A BATTERY PACK BOEING 747 747230B 1384889 NM EVAC SLIDE DISCHARGED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487EV 23286 RT EMERGENCY ESCAPE SLIDE LIGHT INOP. RT EMERGENCY ESCAPE SLIDE LIGHT POWER PACK REPLACED AND OPERATIONAL CHECKED CARRI ED OUT FOUND NORMAL PER B747 MM 33-51-02. 2 L 7 4 4F RT A20WE 2008020100156 20080201 00156 NM 2008 2 1 EIA2007203 1 20071204 A 5514 65B035634 HINGE FITTING BOEING BOEING 747 747230B 1384889 NM HORIZ STAB CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 489EV 23393 LT HORIZONTAL STABILIZER HINGE FITTING AT UPPER REAR SPAR CRACKED. REPLACED LT HINE FITTING PER R 55-12-35917, SB 747-5 5-2045 ECRA 489-55-011-1. 2 L 7 4 4F RT A20WE 2008020100157 20080201 00157 NM 2008 2 1 EIA2007204 1 20071204 A 5414 SKIN BOEING 747 747230B 1384889 NM NR 3 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 489EV 23393 NUMBER 3 PYLON PRECOOLER EXHAUST LOWER CUTOUT AFT AREA CRACKED. REPAIRED PER 54-50-359, PERFORM DVI PER ECRA 489-54-010 -1. PER HAECO 5192. 2 L 7 4 4F RT A20WE 2008020100159 20080201 00159 2008 2 1 EIA2007206 4 20071204 A 2565 SLIDE BOEING 747 747230B 1384889 NM EVAC SLIDE DISCONNECTED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 489EV 23393 RT EMERGENCY DOOR SLIDE PACK INFLATION BOTTLE DEPLOYMENT CABLE DETACHED. DEPLOYMENT CABLE RE-ATTACHED IAW 25-60-00. 2 L 7 4 4F RT A20WE 2008020100160 20080201 00160 NM 2008 2 1 EIA2007207 1 20071210 A 3350 900835A BATTERY PACK BOEING 747 747121 1384871 NM CABIN DISCHARGED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480EV 20348 CREW EXIT DOOR UPPER DECK SILL LIGHT INOP. BATTERY PACK OF X327 UPPER DECK AT STATION 403 RT REPLACED. 2 L 7 4 4F RT A20WE 2008013100335 20080131 00335 NM 2008 1 31 DL75E080113 1 20071217 A 5313 LONGERON BOEING 757 7572Q8 1384972 NM BS 730-740 L21R CUT A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 713TW 28173 LONGERON R21 BETWEEN STATIONS 730 AND 740 WAS CUT. REPAIRED IN ACCORDANCE WITH SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008013100350 20080131 00350 EA 2008 1 31 SWIA200719093 1 20070925 A 2710 BEARING CNDAIR CL600 CL6002B19 1900309 EA LT AILERON LINK FAILED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 912EV 7728 LT AILERON INBD AND OTBD PCU LINK BEARINGS FAIL BACKLASH CHECK, FOUND AT C-CHECK. REPLACED LEFT AILERON INBOARD AND OUT BOARD PCU LINKS IAW CRJ200 AMM 27-14-15-000-801 AND 27-14-15-400-801. 2 L 7 2 4F RT A21EA 2008020100002 20080201 00002 WP 2008 2 1 UPS08851467 1 20071228 A 5320 WEB DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 AREA ABOVE HORIZ STAB FWD OF RUDDER PCU STA 1810 LBL 30 FLOOR WEB HAS CRACK. STOP DRILLED CRACKED WE B AT STA 1810 LBL 30 IAW SRM 53-02-00 FIG 1B. FABRICATED AND INSTALLED REPAIR DOUBLER AT STA 1810 LBL 30 IAW SRM 53-02- 00 FIG 1B. 2 L 7 4 4F RT 4A25 2008020100063 20080201 00063 NM 2008 2 1 CALA0800071 1 20071228 A 3350 ADD71701100 BATTERY PACK BOEING 737 737724 13844BY NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13750 28941 EMERGENCY LIGHTS AT FIRST CLASS LEFT ROWS AND FIRST CLASS OVERHEAD BINS DO NOT ILLUMINATE. REPLACED BATTERY PACK FOR FI RST CLASS SEATS AND BIN. 2 L 7 2 4F RT A16WE 2008020100064 20080201 00064 NM 2008 2 1 CALA0800072 1 20071229 A 3350 ADD71701100 BATTERY PACK BOEING 737 737724 13844BY NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 23707 28768 R-1 DOOR EMERGENCY INSIDE LIGHT INOP. REPLACED BATTERY PACK PER 33-51-06-960-805. 2 L 7 2 4F RT A16WE 2008020100109 20080201 00109 EA 2008 2 1 SWIA200719111 1 20070915 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 982SW 7956 PAX DOOR HANDLE IS CRACKED, FOUND AT C-CHECK. REPLACED PAX DOOR HANDLE IAW CRJ200 SRM 51-41-02. 2 L 7 2 4F RT A21EA 2008020100161 20080201 00161 NM 2008 2 1 EIA2007208 1 20071208 A 3350 S1356B37 LIGHT BOEING 747 747273C 1384896 NM CABIN INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 470EV 20653 FOUND UPPER DECK AFT EMERGENCY LIGHT INOP. REPLACED AFT EMERGENCY LIGHT ASSY PER B747 MM 33-51-02, SYSTEM OPS CHECKED P ER 33-51-00. 2 L 7 4 4F RT A20WE 2008020100164 20080201 00164 NM 2008 2 1 EIA2007211 1 20071120 A 5320 STRUCTURE BOEING 747 747230F 1384829 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 490EV 24138 MAIN CABIN BS 2320 RBL 39-RBL63 UPPER CHORD HAS DRILL STARTS NEXT TO FASTENER HOLES. REMOVED DAMAGE FABBED AND INSTALLE D REPAIR PER B747 SRM 51-40-04 FIG 1, 51-30-02, 51-30-05 AND 51-10-02. 2 L 7 4 4F RT A20WE 2008020100167 20080201 00167 NM 2008 2 1 EIA2007214 1 20071114 A 5315 FLOORBEAM BOEING 747 747230F 1384829 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 490EV 24138 MAIN DECK BS 2280 RBL 40 FLOORBEAM UPPER CHORD CORRODED AND ENLONGATED HOLES. REMOVED DAMAGE, FABBED AND INSTALLED REPA IR PER B747 SRM 53-10-07 FIGURE 12 AND 53-10-01 FIG 1. 2 L 7 4 4F RT A20WE 2008020100168 20080201 00168 NM 2008 2 1 EIA2007215 1 20071111 A 5315 FLOORBEAM BOEING 747 747230F 1384829 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 490EV 24138 MAIN DECK BS 720 BETWEEN LBL 75 AND LBL 110 FLOORBEAM UPPER CHORD IS CORRODED BOTH LEGS. REMOVED DAMAGE, FABBED AND INS TALLED REPAIR PER B747 SRM 53-10-07 FIG 12 PAGES 51-54. 2 L 7 4 4F RT A20WE 2008020100169 20080201 00169 NM 2008 2 1 EIA2007216 1 20071115 A 5315 FLOORBEAM BOEING 747 747230F 1384829 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 490EV 24138 BS 500 RT UPPER DECK FLOORBEAM 2 DEFECT FASTENER HOLES PER EO 53-747-1625-01 REV D. REMOVED DAMAGE, FABBED AND INSTALLE D REPAIR PER ECRA 490-53-013-2 PART 1. 2 L 7 4 4F RT A20WE 2008020100170 20080201 00170 NM 2008 2 1 EIA2007217 1 20071118 A 5230 SKIN BOEING 747 747230F 1384829 NM CARGO DOOR DENTED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 490EV 24138 DENT AT LWR EDGE OF FWD PIT DOOR SKIN BS 730 2IN ABOVE STR 39R. CUT OUT DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SR M 52-30-06 FIG 1 DETAIL VI. 2 L 7 4 4F RT A20WE 2008020100171 20080201 00171 NM 2008 2 1 EIA2007218 1 20071116 A 5414 SKIN BOEING 747 747230F 1384829 NM NR 2 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 490EV 24138 NR 2 PYLON INBOARD SIDE AFT OF THRUST REVERSER SLEEVE INSPECTION PANEL 463AR. CUTOUT HAS 2 AREAS OF DAMAGE. REMOVED DA MAGE, FABBED AND INSTALLED REPAIR PER ECRA 490-54-005-2. 2 L 7 4 4F RT A20WE 2008020400041 20080204 00041 EA 2008 2 4 SWIA200719116 1 20070924 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 740SK 10196 COCKPIT FLOORBEAM IS CRACKED AT FS 280 AND RBL 9, FOUND AT C-CHECK. INSTALLED COCKPIT FLOORBEA, PER CRJ700/900 SRM 51-4 2-06 AND 51-40-11. 2 L 7 2 4F RT A21EA 2008020400043 20080204 00043 EA 2008 2 4 SWIA200719118 1 20071001 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 745SK 10201 FS 280 COCKPIT FLOORBEAM IS CRACKED AT RBL9 AND LBL9, FOUND AT C-CHECK. INSTALLED NEW COCKPIT FLOORBEAM PER CRJ700/900 SRM 51-40-11-001-801-A01. 2 L 7 2 4F RT A21EA 2008020400044 20080204 00044 EA 2008 2 4 SWIA200719119 1 20071001 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 745SK 10201 FS 280 FLOORBEAM IS CRACKED AT RBL9, FOUND AT C-CHECK. INSTALLED FS 280.0 FLOORBEAM PER CRJ700/900 SRM 51-42-06 AND 51- 42-21. 2 L 7 2 4F RT A21EA 2008020400045 20080204 00045 EA 2008 2 4 SWIA200719120 1 20071007 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BRAKE XDUCER CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 910EV 7727 RIGHT FORWARD BRAKE TRANSDUCER BRACKET IS CRACKED, FOUND AT C-CHECK. REPLACED BRAKE TRANSDUCER BRACKET PER CRJ200 SRM R EF 51-42-06. 2 L 7 2 4F RT A21EA 2008020400046 20080204 00046 EA 2008 2 4 SWIA200719121 1 20071007 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA DOOR FRAME CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 910EV 7727 FORWARD LOWER CARGO DOOR FRAME STIFFENERS ARE CRACKED, FOUND AT C-CHECK. REPLACED FORWARD LOWER CARGO DOOR TRACK CHANNE L AS PER CRJ200 SRM 51-41-02 PGS 1-18 AND 51-40-02 PGS 1-18. 2 L 7 2 4F RT A21EA 2008020400049 20080204 00049 EA 2008 2 4 SWIA200719124 1 20071002 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY NO TEST A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 937SW 7735 LAV SMOKE DETECTOR DOES NOT TEST, FOUND AT C-CHECK. REPLACED LAVATORY SMOKE DETECTOR PER CRJ200 AMM 26-16-01-400-801. OPERATIONAL TEST IS GOOD. 2 L 7 2 4F RT A21EA 2008020400050 20080204 00050 EA 2008 2 4 SWIA200719125 1 20071002 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 937SW 7735 STATION 484 BRACKET IS CRACKED AT LBL 27, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER REO 601R-53-41059. 2 L 7 2 4F RT A21EA 2008020400054 20080204 00054 EA 2008 2 4 SWIA200719129 1 20071006 A 5220 HANDLE CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 915EV 7754 CREW ESCAPE HATCH OUTER HANDLE ASSEMBLY HAS SIGNS OF CORROSION, FOUND AT C-CHECK. REMOVED LIGHT CORROSION ON OUTER HAND LE ASSEMBLY PER SRM CRJ200 51-21-06 PG 1 TO PG 5. 2 L 7 2 4F RT A21EA 2008020400055 20080204 00055 EA 2008 2 4 SWIA200719130 1 20071006 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 915EV 7754 PAX DOOR EXTERIOR HANDLE IS CRACKED, FOUND AT C-CHECK. REPLACED PAX DOOR OUTSIDE HANDLE PER CRJ200 AMM 52-11-03-020-007 . 2 L 7 2 4F RT A21EA 2008020400056 20080204 00056 EA 2008 2 4 SWIA200719131 1 20071006 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 915EV 7754 RIGHT SIDE OF FS 621 FLOOR SUPPORT ANGLE IS CRACKED, FOUND AT C-CHECK. REPLACED FLOOR SUPPORT PER CRJ200 REO 601R-53-61 -117 REV A. 2 L 7 2 4F RT A21EA 2008020400057 20080204 00057 EA 2008 2 4 SWIA200719132 1 20071006 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 915EV 7754 RIGHT SIDE OF STA 280 LOWER FLOORBEAM IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIR ON LOWER BEAM PER CRJ200 REO 6 01R-53-11-171 REV D DATED 13-FEB-07. 2 L 7 2 4F RT A21EA 2008020400059 20080204 00059 EA 2008 2 4 SWIA200719134 1 20071006 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 915EV 7754 RIGHT LOWER WEB AT FORWARD CORNER OF ACCESS OPENING ON ENGINE SUPPORT BEAM IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REO 601R-53-01-358 REV B TO REPAIR WEB. 2 L 7 2 4F RT A21EA 2008020400062 20080204 00062 SO 2008 2 4 SWIA200719137 1 20071201 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 224SW 120294 LEFT FORWARD FLOOR SEAT TRACK IS CORRODED IN SEVERAL SPOTS, FOUND AT C-CHECK. REPLACED SEAT TRACK IAW EMB 120 MM 53-01- 05. 2 L 7 2 4T RT A31SO 2008020400063 20080204 00063 SO 2008 2 4 SWIA200719138 1 20071201 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 224SW 120294 RIGHT FORWARD SEAT TRACK HAS SURFACE CORROSION IN VERIOUS LOCATIONS, FOUND AT C-CHECK. REPLACED WITH NEW SEAT TRACK IAW EMB 120 MM 53-01-05. 2 L 7 2 4T RT A31SO 2008020400065 20080204 00065 SO 2008 2 4 SWIA200719140 1 20071201 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 224SW 120294 CORROSION ON FLOOR CENTER FLOORBEAM BUTT STRAP NEAR PAX ENTRANCE, FOUND AT C-CHECK. REPLACED BUTT STRAP IAW EMB 120 SRM 51-40-02 PG 3 SECTION 3A. 2 L 7 2 4T RT A31SO 2008013100297 20080131 00297 SW 2008 1 31 H5O2008F00000 1 20071205 A 6730 2040012741 LINER BELL 204 UH1B 1181410 SW PILOT COLLECTIVE WORN D H5OL K NONE O OTHER IN INSP/MAINT 1 WP 27 46969 638548 PILOT EXPERIENCED COLLECTIVE BOUNCE ON TAKEOFF. INSPECTION OF COLLECTIVE LINERS SHOWED SUFFICIENT AMOUNT OF LINER REMAI NING IN THE WEAR AREA. WITH FURTHER INSPECTION, THE MINIMUM COLLECTIVE FRICTION WAS TOO LOW. INSPECTION ON NR 3 AND NR 6 PHASE IAW TM 55-1520-219-PMS, PAGE 6 ITEM NR 2.14 REQUIRES TO INSPECT COLLECTIVE FRICTION LINERS FOR WEAR. ADJUSTMEN T OF MINIMUM COLLECTIVE FRICTION SHOULD ALSO BE INCLUDED IN THE PHASE INSPECTION CHECKLIST ALONG WITH VISUAL INSPECTION OF THE LINERS. (K) 1 G 7 1 4U EXPA1G71 2008013100351 20080131 00351 EA 2008 1 31 SWIA200719094 1 20070925 A 2710 BEARING CNDAIR CL600 CL6002B19 1900309 EA AILERON LINK WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 912EV 7728 RIGHT AILERON INBOARD AND OUTBOARD PCU LINK BEARINGS FAIL BACKLASH CHECK, FOUND AT C-CHECK. REPLACED AILERON PCU LINKS PER CRJ200 AMM 27-14-15-00-801/400-801. 2 L 7 2 4F RT A21EA 2008020100001 20080201 00001 WP 2008 2 1 UPS08851466 1 20071227 A 5420 DRAG ANGLE DOUG DC8 DC871F 302199D WP NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 NR 1 PYLON INBOARD DRAG ANGLE CRACKED 1/4" PAST STOP DRILL. STOP DRILLED CRACK ON NR 1 PYLON DRAG AN GLE IAW EO DC8-5740-07164, CRACK DOES NOT EXCEED LIMITS OF 3" PER EO DC8-5740-07164. 2 L 7 4 4F RT 4A25 2008020100062 20080201 00062 NM 2008 2 1 CALA0800070 1 20071230 A 3350 ADD71701100 BATTERY PACK BOEING 737 737824 13844BZ NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 33209 30581 CIRCUIT BREAKER FOR AFT EMERGENCY LIGHT POPPED. REPLACED EMERGENCY CHARGER AND BATTERY PACK PER AMM 33-51-06. 2 L 7 2 4F RT A16WE 2008020100102 20080201 00102 EA 2008 2 1 SWIA200719104 1 20070914 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 936SW 7726 FS 484 AT RBL 27 IS CRACKED AT TOP OF ANGLE, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO 601R 53-41-059 REV A. 2 L 7 2 4F RT A21EA 2008020100108 20080201 00108 EA 2008 2 1 SWIA200719110 1 20070915 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 982SW 7956 FS 621 RIGHT SIDE FLOOR ANGLE IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIR OF FS 621 FLOOR ANGLE PER CRJ200 REO 6 01R 53-61-117 REV C. 2 L 7 2 4F RT A21EA 2008020100143 20080201 00143 NM 2008 2 1 EIA2007195 1 20071101 A 2120 UNKNOWN BOEING 747 747230B 1384889 NM COCKPIT ODOR A EIAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 488EV 23287 DURING CRUISE STARTED SMELLING LIKE BURNING PLASTIC. FLIGHT DECK FAN WAS ON. THE FAN WAS TURNED OFF AND THE ODOR WENT AWAY, CB WAS PULLED. HOLD FOR CORRECTIVE ACTION. 2 L 7 4 4F RT A20WE 2008020100165 20080201 00165 NM 2008 2 1 EIA2007212 1 20071102 A 5315 FLOORBEAM BOEING 747 747230F 1384829 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 490EV 24138 MAIN CABIN FLOORBEAM BS 960 LBL85 HAS EXFOLIATION CORROSION AROUND FLOORBOARD CLIP NUT HOLES. REMOVED DAMAGE, FABBED AN D INSTALLED REPAIR PER B747 SRM 53-10-07 FIG 12. 2 L 7 4 4F RT A20WE 2008020100166 20080201 00166 NM 2008 2 1 EIA2007213 1 20071102 A 5320 STRUCTURE BOEING 747 747230F 1384829 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 490EV 24138 LIGHT SURFACE CORROSION AROUND NUT CLIP HOLES ON UPPER CHORD MAIN DECK BS 2040 LBL 33-75. REMOVED DAMAGE, FABBED AND IN STALLED REPAIR PER B747 SRM 53-10-07 PAGE 51-54. 2 L 7 4 4F RT A20WE 2008020100172 20080201 00172 NM 2008 2 1 EIA2007219 1 20071115 A 5315 FLOORBEAM BOEING 747 747230F 1384829 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 490EV 24138 BS 500 LT UPPER DECK FLOORBEAM 2 DEFECTIVE FASTENER HOLES PER EO 53-747-1625-01 REV B. REMOVED DAMAGE, FABBED AND INSTA LLED REPAIR PER ECRA 490-53-013-2 PART 1. 2 L 7 4 4F RT A20WE 2008020400064 20080204 00064 SO 2008 2 4 SWIA200719139 1 20071201 A 5347 GALLEY TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 224SW 120294 CORROSION ON FLOOR BUTTSTRAP UNDER FORWARD GALLEY ATTACH TRACK, FOUND AT C-CHECK. REPLACED BUTTSTRAP UNDER FORWARD GALL EY ATTACH POINT IAW EMB 120 SRM 51-40-02 PG 3 SECTION 3A. 2 L 7 2 4T RT A31SO 2008020100056 20080201 00056 NM 2008 2 1 CALA0800064 1 20071229 A 3350 ADD71701 LIGHT BOEING 737 737824 13844BZ NM CABIN BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 37252 30583 MID CEILING EMERGENCY LIGHT BROKEN. INSTALLED SERVICEABLE LIGHT ASSY PER AMM 33-51-01. 2 L 7 2 4F RT A16WE 2008020100105 20080201 00105 EA 2008 2 1 SWIA200719107 1 20070915 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 982SW 7956 LBL9 LOWER FLOOR SUPPORT HAS CRACK AT FS 280, FOUND AT C-CHECK. REPAIRED LOWER FLOOR SUPPORT AS PER REO 601R-53-11-171 REV D. 2 L 7 2 4F RT A21EA 2008020100106 20080201 00106 EA 2008 2 1 SWIA200719108 1 20070915 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 982SW 7956 RIGHT LOWER FLOOR SUPPORT HAS CRACK AT RBL9 AND FS 280, FOUND AT C-CHECK. REPAIRED FLOOR SUPPORT AS PER CRJ200 REO 601R -53-11-171 REV D. 2 L 7 2 4F RT A21EA 2008020100112 20080201 00112 EA 2008 2 1 SWIA200719114 1 20070926 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 913EV 7731 LOWER FLOOR SUPPORT FRAME IS CRACKED AT LBL 9 AND STA 280, FOUND AT C-CHECK. REPAIR PARTS INSTALLED IAW CRJ200 REO 601R -53-11-170 REV D. 2 L 7 2 4F RT A21EA 2008020100113 20080201 00113 EA 2008 2 1 SWIA200719115 1 20070926 A 5320 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 913EV 7731 SUPPORT BEAM DOUBLER IS CRACKED AT FS 640, FOUND AT AT C-CHECK. MADE REPAIRS AT STA 640 PER CRJ200 SRM REF 51-42-00 PG 10-12. 2 L 7 2 4F RT A21EA 2008020100152 20080201 00152 NM 2008 2 1 EIA2007199 1 20071114 A 3350 3004185 LIGHT BOEING 747 747273C 1384896 NM CABIN INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 471EV 20651 R5 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED R5 EMERGENCY EXIT GROUND LIGHT ASSY PER B747 MM 33-51-07 PAGE 201, SYSTEM O PS CHECKED NORMAL PER MM 51-00-50. 2 L 7 4 4F RT A20WE 2008020100153 20080201 00153 NM 2008 2 1 EIA2007200 1 20071114 A 3350 20131A BATTERY PACK BOEING 747 747273C 1384896 NM CABIN DISCHARGED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 471EV 20651 R5 EMERGENCY EXIT SIGN INOP. REPLACED DOOR BATTERY PACK PER B747 MM 33-51-20 SYSTEM, OPS CHECKED GOOD PER MM 33-51-00 P G 501. 2 L 7 4 4F RT A20WE 2008020100154 20080201 00154 NE 2008 2 1 EIA2007201 2 20071120 A 7321 8010003 FMU BOEING 747 7474J6 13848BG NM PWA 4056 PW4056 NE NR 4 ENGINE MALFUNCTIONED A EIAA K NONE R J PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 NM 09 747BC 25879 727323 ON FINAL EICAS MSG "ENG 4 FAIL". PERFORMED FAULT ISOLATION MANUAL PROCEDURES TASK 71-00-919 DUE TO NR 4 CONTROL MESSAGE 74077, OPS CHECK GOOD PER FAULT ISO MANUAL. REMOVED AND REPLACED FMU PER B747-400 AMM 73-21-01. ACCOMPLISHED POWER PL ANT TEST NR 3 PER B747-400 AMM 71-00-00, OPS CHECKED GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2008020100158 20080201 00158 NM 2008 2 1 EIA2007205 1 20071204 A 5414 SKIN BOEING BOEING 747 747230B 1384889 NM NR 2 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 489EV 23393 NUMBER 2 PYLON PRECOOLER LOWER SKIN, TWO CRACKS FOUND AT AFT UPPER CORNER. REPAIR PER 54-50-35916. PERFORM DVI PER ECR A 489-54-010-1. 2 L 7 4 4F RT A20WE 2008020400042 20080204 00042 EA 2008 2 4 SWIA200719117 1 20070924 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 740SK 10196 FS 280 FLOORBEAM IS CRACKED AT LBL9, FOUND AT C-CHECK. INSTALLED FLOORBEAM REPAIR PER CRJ700/900 SRM 51-42-21 AND 51-42 -06. 2 L 7 2 4F RT A21EA 2008020400048 20080204 00048 EA 2008 2 4 SWIA200719123 1 20071007 A 7120 BOX BEAM CNDAIR CL600 CL6002B19 1900309 EA CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 910EV 7727 RIGHT SIDE OF ENGINE BOX BEAM SHOWS SIGNS OF CRACK AT ACCESS HOLE, FOUND AT C-CHECK. INSTALLED REPAIR PARTS IAW REO 601 R-53-61-358 PG 1-4 REV A. 2 L 7 2 4F RT A21EA 2008020400053 20080204 00053 EA 2008 2 4 SWIA200719128 1 20071002 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 937SW 7735 LOWER FLOORBEAM IS CRACKED AT BS 280 AND RBL 9, FOUND AT C-CHECK. COMPLIED WITH REPAIRS IAW CRJ200 REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 2008020400058 20080204 00058 EA 2008 2 4 SWIA200719133 1 20071006 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 915EV 7754 STA 280 LEFT UPPER FLOORBEAM ANGLE IS CRACKED AT STA 280 AND LBL9, FOUND AT C-CHECK. COMPLIED WITH REPAIR TO FLOORBEAM ANGLE PER CRJ200 REO 601R-53-11-138. 2 L 7 2 4F RT A21EA 2008020400061 20080204 00061 SO 2008 2 4 SWIA200719136 1 20071201 A 5241 TRACK EMB 120 EMB120ER 3260203 SO GALLEY DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 224SW 120294 FORWARD DOOR GALLEY ATTACH TRACK IS CORRODED, FOUND AT C-CHECK. REPLACED FORWARD GALLEY FLOOR ATTACH TRACK. 2 L 7 2 4T RT A31SO 2008020600048 20080206 00048 NM 2008 2 6 2007UALA03094 1 20070810 A 3150 WARNING MESSAGE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUEL SYS FALSE INDICATION A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 804UA 759 UNEXPLAINED FUEL TRANSFER AND IMBALANCE. COULD NOT DUPLICATE CONDITION ON GROUND. RAN SEVERAL TESTS INCLUDING EXAMININ G AIR RELEASE FLOAT VALVE, DEFUELING ACTUATOR FOR PROPER OPS, FLSS STATUS, ALL NORMAL. TESTED ALL QTY PROBES. ON PREFL IGHT, QTY PROBE 26QT 2 FAULTED TEST, MTC CAME OUT AND ACCOMPLISHED CHECK PER MM AND TEST PASSED. POSSIBLE INTERMITTANT INDICATION ISSUE. AFTER ALL TESTS CLEARED AND DEEMED NORMAL OPS, A/C RELEASED AND FLEW WITHOUT ANY NOTED FUEL ISSUES. THIS PROBLEM HAS NOT SURFACED AGAIN ON THIS A/C AT ALL SINCE ORIGINAL WRITE UP. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020600120 20080206 00120 NM 2008 2 6 UPS08M51608 1 20071218 A 5713 STRINGER DOUG MD11 MD11 3023602 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C LT WING TANK UPPER STRINGER NR 10 SUSPECT CRACK AS MARKED, THRU TANK LOWER ACCESS NR 536CB. HFEC INSP C/O PER DAC NDTSPM REV 13 PT 6 06-10-01.01.001 AND FOUND CRACK APPROX 10 INCHES AS MARKED. LT WING TANK UPPER STRINGER NR 10 ATTACHED SPLICE REMOVED FOR ACCESS PER SRM 51-33-01 V.II R35. CRACKED AREA SLOTTED OUT PER SR M57-20-00 VI FIG R 35. NEW FAB REPAIR ANGLES 02 EA AND ATTACHED SPLICE AT LHW TANK UPPER STRINGER NR 10 PER SRM 57-20-00 FIG 10 VI REV 35. 2 L 7 3 4F RT A22WE 2008020600125 20080206 00125 NM 2008 2 6 MASA200800042 1 20071124 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT WING WORN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 447YV 447 LEFT WING NR 3 UPPER FLAP TRACK LOWER SIDE, OB SIDE OF NACELLE HAS WORN AREA., REPAIRED. 2 H 7 2 4T RT A13NM 2008020600130 20080206 00130 NM 2008 2 6 MASA200800046 1 20071205 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAP CORRODED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 987HA 425 RT NR 1 FLAP TRACK HAS MINOR CORROSION, REPAIRED. 2 H 7 2 4T RT A13NM 2008020600163 20080206 00163 WP 2008 2 6 UPS07850919 1 20070918 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FS 1220 LBL48 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 SEAT TRACK SCALLOP GOUGED AT STA 1220 LBL 48. REMOVED AND REPLACED SEAT TRACK FROM STA 1170-1270 LBL 48 IAW SRM 53-02-03, AND EO DC8-5320-8309-D. 2 L 7 4 4F RT 4A25 2008020600164 20080206 00164 WP 2008 2 6 UPS07851018 1 20070923 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP L-2 DOOR DAMAGED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 TWO LARGE HOLES DRILLED THROUGH L-2 DOOR FRAME JAMB WEB LOWER AFT CORNER. TOP HOLE DOUBLE DRILLED, B OTTOM HAS CUT THROUGH INNER WEB. REPAIRED L-2 DOOR FRAME AND WEB AT LOWER AFT CORNER IAW DWG 9751052, DWG 9751060, SRM 51-1-8, SRM 51-1-20D, SRM 51-1-21 AND SRM 51-03-00. 2 L 7 4 4F RT 4A25 2008020600199 20080206 00199 NM 2008 2 6 UPS08M51483 1 20071122 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C HORIZ STAB CONSTANT SECTION LT NR 1 BARREL NUT BORE FOUND CORROSION. CORROSION AT B-NUT BORE REMOVED. BORE BOTTOM REMAINING BLEND OUT 0.030" DEEP, BORE REAM TO 1.549" DIA REMAINING BLEND OUT 0.052" DEEP, FOUND EXCEED LM T 10X MAG INSP C/O AND FOUND NO CORROSION EVIDENT. REPAIR SLEEVE BUSHING FAB, PROTECTED AND INSTALLED. REPAIR C/O AT LT NR 01 B-NUT BORE IS ACCEPTABLE PER EN1735-07. 2 L 7 3 4F RT A22WE 2008020600213 20080206 00213 NM 2008 2 6 UPS08M51595 1 20071217 A 5330 SKIN DOUG MD11 MD11 3023602 NM CARGO DOORWAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C CENTER CARGO DOOR CUTOUT AFT LWR CORNER FOUND PREVIOUS REPAIR AND WITH RUSTY FASTENERS. PREVIOUS REPA IR DOUBLER REMOVED PER SRM 51-31-01 V.II R35. HFEC INSP C/O PER DAC NDTSPM REV 13 06-10-01.001 ON EXISTING TRIMMED OFF AREA (02EA) AND FOUND NO CRACK EVIDENT. REPAIR FILLER AND DOUBLER FAB PER SRM 53-50-00 FIG 6 VI R35. REPAIR FILLER AND DOUBLER INSTALLED PER SRM 53-50-00 FIG 16 VOL I REV 35. 2 L 7 3 4F RT A22WE 2008020600223 20080206 00223 NM 2008 2 6 UPS08M51510 1 20071214 A 5320 INTERCOSTAL DOUG MD11 MD11 3023602 NM BS 1621-1641 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C CABIN, INTERCOSTAL AT STA 1621-1641,L7 RT FOUND CRACKED AS MARKED. CRACKED INTERCOSTAL AT CABIN STA 1 621 TO 1641 LONGERON L7 AREA. REMOVED PER SRM 51-31-01 V.II R35. NEW INTERCOSTAL FAB PER BOEING DWG AFA7761. FAB INTE RCOSTAL FASTENERS HOLES PICKED UP PER DWG 51-31-01 V.II R35. NEW INTERCOSTAL AT CABIN STA 1621-1641 LONGERON L7 RT AREA INSTALLED PER SRM 51-31-01 V II REV 35. 2 L 7 3 4F RT A22WE 2008020600235 20080206 00235 NM 2008 2 6 UPS08M51512 1 20071115 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C HORIZ STAB CONSTANT SECTION LT NR 36 BARREL NUT BORE FOUND WITH CORROSION. CORROSION AT B-NUT BORE RE MOVED. BORE BOTTOM REMAINING BLEND OUT 0.075" DEEP. BORE REAM TO 2.538" DIA AND REMAINING BLEND OUT 0.080" DEEP, FOUND EXCEED EO MD 11-5510-19409-L, 10X MAG INSP C/O, FOUND NO CORROSION EVDT. REPAIR SLEEVE BUSHING FAB, PROTECTED AND INST ALLED. C/O FR PRIMER TOUCH UP AT REPAIR AREA. REPAIR C/O IS ACCEPTABLE PER EN 1724-07. 2 L 7 3 4F RT A22WE 2008020100162 20080201 00162 NM 2008 2 1 EIA2007209 1 20071206 A 3350 S1356B37 LIGHT BOEING 747 747273C 1384896 NM CABIN INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 471EV 20651 UPPER DECK AFT EMERGENCY LIGHTS INOP WILL NOT TEST. REPLACED UPPER DECK AFT EMERGENCY LIGHT AND UPPER DECK ENTRY LIGHT PER B747 MM 33-51-07. OPS CHECKEED NORMAL. 2 L 7 4 4F RT A20WE 2008020100163 20080201 00163 NM 2008 2 1 EIA2007210 1 20071207 A 3350 900835A BATTERY PACK BOEING 747 747273C 1384896 NM CABIN DISCHARGED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 470EV 20653 UPPER DECK EMERGENCY LIGHT OVER DOOR SLIDE DOES NOT TEST. REPLACED BATTERY PACK PER B747 MM 33-51-04, OPS CHECKED NORMA L. 2 L 7 4 4F RT A20WE 2008020400047 20080204 00047 EA 2008 2 4 SWIA200719122 1 20071007 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 910EV 7727 LEFT SIDE OF FS 280 UPPER FLOORBEAM ANGLE IS CRACKED AT LBL12, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 REO 601R-53-11-138 STEP 7. 2 L 7 2 4F RT A21EA 2008020400051 20080204 00051 EA 2008 2 4 SWIA200719126 1 20071002 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 937SW 7735 UPPER FLOORBEAM ANGLE IS CRACKED AT BS 280 AND LBL9.0, FOUND AT C-CHECK. INSTALLED REPAIR PARTS AT FS 280 AND LBL9 IAW CRJ200 REO 601R-53-11-136. 2 L 7 2 4F RT A21EA 2008020400052 20080204 00052 EA 2008 2 4 SWIA200719127 1 20071002 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 937SW 7735 LOWER FLOORBEAM IS CRACKED AT STN 280 AND LBL 9, FOUND AT C-CHECK. INSTALLED REPAIR PARTS IAW CRJ200 REO 601R-53-11-171 -1 REV D. 2 L 7 2 4F RT A21EA 2008020600116 20080206 00116 WP 2008 2 6 UPS08851538 1 20071230 A 5522 SKIN DOUG DC8 DC871F 302199D WP LT ELEVATOR DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 2 EA CREASED DENTS ON UPPER OUTBD SURFACE OF LT ELEVATOR. CUT OUT DAMAGE AT LT ELEVATOR STA XE 219 I AW SRM 55-02-01-0 FIG 008. FABRICATED AND INSTALLED SKIN SPLICE REPAIR AT LT ELEV UPPER SURFACE AT STA XE 219 IAW SRM 5 5-02-01. 2 L 7 4 4F RT 4A25 2008020600124 20080206 00124 NM 2008 2 6 MASA200800041 1 20071124 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT WING GOUGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 447YV 447 RIGHT WING NR 5 FLAP TRACK IS GOUGED. REPAIRED RIGHT WING NR 5 FLAP TRACK. 2 H 7 2 4T RT A13NM 2008020600204 20080206 00204 NM 2008 2 6 UPS08M51508 1 20071216 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM BS 1841-1900 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C AFT CARGO/AT STATION 1841 TO STATION 1900 RT MOST OUTBOARD FLOOR SUPPORT FOUND WITH SURFACE CORROSION. CORROSION SUPPORT REMOVED PER SRM51-31-01 V.II R35. NEW SUPPORT P/N:AGA 3857-412 FAB PER DWG AGA3857. SUPPORT HEAT T REAT TO T62 COND PER DPS 7 .00-1. HARDNESS OBTAINED HRB 83 IS ACCEPTABLE PER DPS 1.05-3. NEW FASTENERS HOLE PICKUP PER SRM 51-31-01 V.II R35. NEW SUPPORT PROTECTED AND PAINTED PER SRM 51-21-01 V.II R35. NEW SUPPORT INSTALL PER SRM 51-31 -01 V II R35. 2 L 7 3 4F RT A22WE 2008020600205 20080206 00205 NM 2008 2 6 UPS08M51550 1 20071116 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C HORIZ STAB CONSTANT SECTION RT NR 09 BARREL NUT BORE FOUND WITH CORROSION. CORROSION AT B-NUT BORE RE MOVED. BORE BOTTOM REMAINED BLEND OUT 0.030" BORE REAM TO 0.988" DIA, REMAIN BLEND OUT 0.060" FOUND EXCEED LIMITS 10X M AG INSP C/O AND FOUND NO CORROSION EVIDENT. REPAIR SLEEVE BUSHING FAB, PROTECTED AND INSTALLED. C/O FR PRIMER TOUCH UP AT REPAIR AREA. REPAIR C/O IS ACCEPTABLE PER EN1722-07. 2 L 7 3 4F RT A22WE 2008020600233 20080206 00233 NM 2008 2 6 UPS08M51511 1 20071225 A 5320 INTERCOSTAL DOUG MD11 MD11 3023602 NM BS 515-535 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C CABIN, LONGERON L7 RT AT STA 515-535, FOUND INTERCOSTAL CRACK AS MARKED. CRACK INTERCOSTAL AT CABIN L ONGERON L7 RT AT STA 515-535 AREA. REMOVED PER SRM51-31-V.II R35. NEW INTERCOSTAL P/N:AFA3087-17 FAB PER DWG AF A3087. HOLES ON FAB INTERCOSTAL AREA PICKED UP PER SRM 51-31-01 V.II R35. NEW INTERCOSTAL AT CABIN LONGERON L7 RT STA 515-53 5 AREA INSTALLED AS PER SRM 51-31-01 VOL II REV 35. 2 L 7 3 4F RT A22WE 2008020600255 20080206 00255 NM 2008 2 6 UPS08M51513 1 20071121 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C LT HORIZ STAB NR 6 BARREL NUT HOLE FOUND CORROSIONS. CORROSION AT B-NUT BORE REMOVED. BORE BOTTOM RE MAINING BLEND OUT 0.035" DEEP. BORE REAM TO 0.988" DIA REMAIN BLEND OUT DEPTH 0.030" DEEP FOUND EXCEED LMT PER EO MD11- 5510-19409-L. 10X MAG INSP C/O AND FOUND NO CORROSION EVDT. REPAIR SLEEVE BUSHING FAB, PROTECTED AND INSTALLED. C/O FR PRIMER TOUCH UP AT BORE REPAIR AREA. REPAIR C/O IS ACCEPTABLE PER EN 1731-07. 2 L 7 3 4F RT A22WE 2008020600170 20080206 00170 WP 2008 2 6 UPS08851501 1 20071229 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP FS 80 LBL 42 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 FLOOR PNL F-45 CRACKED AT SCREW HOLE AFT RT SIDE OF LAV. FABRICATED AND INSTALLED REPAIR DOUBLER ON FLOOR PNL F-45 IAW SRM 53-02-03 FIG 010. 2 L 7 4 4F RT 4A25 2008020600186 20080206 00186 WP 2008 2 6 UPS08851527 1 20071231 A 5753 377590623 FLAP TRACK DOUG DC8 DC871F 302199D WP LWS 340 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 LT FLAP TRACK MISSING CHROME AT STA 340. REPLACED LT FLAP TRACKS AT STA 340 IAW MM 27-51-9 AND MM 27 -51-3. 2 L 7 4 4F RT 4A25 2008020600189 20080206 00189 WP 2008 2 6 UPS08851530 1 20071230 A 5321 FLOORBOARD DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 FLOORBOARD PNL NR 680 HAT CHANNELS ARE CUT AND GOUGED AS MARKED. FABRICATED AND REPLACED 3 HAT CHANN ELS ON FLOORBOARD NR 680 IAW SRM 53-07-03 FIG 1A SHT1, SRM 51-3-2 AND SRM 51-1-8. 2 L 7 4 4F RT 4A25 2008020700022 20080207 00022 NM 2008 2 7 HNAA0800008 1 20071218 A 3610 82110001001 BLEED AIR SYS DHAV DHC8 DHC8102 2809003 NM CONTAMINATED A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 07 825EX 32658 32658 388 DURING OPERATION, AN ODOR THAT WAS BELIEVED TO BE FUEL WAS DETECTED WHEN NR 1 ENGINE BLEED SYSTEM WAS SELECTED ON. BLEE D SYSTEM FOR NR 1 AND NR 2 ENGINES, ALONG WITH THE APU, WERE INSPECTED AND FOUND TO BE IN ORDER. SYSTEM WAS RUN AT FULL HOT AND FULL COLD. ODOR WAS DETERMINED TO BE DE-ICE FLUID. AIRCRAFT WAS THEN RELEASED AS OK FOR SERVICE. ADDITIONAL INFORMATION ADDED. 2 H 7 2 4T RT A13NM 2008020700023 20080207 00023 NM 2008 2 7 HNAA0700290 1 20071213 A 2730 85520001001 ELEVATOR DHAV DHC8 DHC8102 2809003 NM ICED A HNAA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 EA 07 938HA 49039 49039 152 DURING TAKEOFF ROLL, THE AIRCRAFT REACHED 104 KNOTS AND THE CREW ATTEMPTED TO ROTATE THE AIRCRAFT TO LIFT OFF, BUT WERE UNABLE TO DO SO. THE CAPTAIN IMMEDIATELY ABORTED THE TAKEOFF AND USED THE REMAINDER OF THE RUNWAY FOR STOPPING. CONDIT IONS WERE WET AND SNOWY. THE AIRCRAFT WAS THEN TAXIED BACK TO THE GATE WHERE MAINTENANCE INSPECTED THE AREA OF THE ELEV ATORS AND DISCOVERED ICE IN THIS AREA. ICE WAS REMOVED FROM THIS AREA AND FURTHER INSPECTION SHOWED NO OTHER DISCREPANC IES. AIRCRAFT WAS THEN RELEASED FOR SERVICE. ADDITIONAL INFORMATION ADDED. 2 H 7 2 4T RT A13NM 2008020600112 20080206 00112 EA 2008 2 6 MASA200800032 1 20071126 A 5312 60034017595 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 75995 7361 PILOTS BULKHEAD AT FS280.0, LBL9.0 IS CRACKED/CORRODED. 2 L 7 2 4F RT A21EA 2008020600126 20080206 00126 NM 2008 2 6 MASA200800043 1 20071124 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT WING WORN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 447YV 447 LEFT WING NR 4 FLAP TRACK LOWER SIDE OUTBOARD AND INBOARD SIDE HAVE WORN AREAS, REPAIRED. 2 H 7 2 4T RT A13NM 2008020600149 20080206 00149 NM 2008 2 6 UPS08M51554 1 20071217 A 5330 SKIN DOUG MD11 MD11 3023602 NM BS 1790 L36R DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C CENTER CARGO DOOR CUTOUT AFT AREA STA 1790.0 RT L36 FOUND DENT AS MARKED DENT AREA SMOOTHED OUT PER SR M 51-21-01 V.II R35. DENT MARK MEASURED FOUND BEYOND LIMIT PER SRM 53-20-00 FIG 6 V.I R35. HFEC INSP CARRIED OUT PER D AC NDTSPM R.13 06-10-01.001 ON REWORKED AREA AND FOUND NO CRACK EVIDENT. NEW DOUBLERS AND FILLER FAB AND INSTALLED PER SRM 53-50-00 FIG V.I R35 AND SRM 51-31-01 VII R35. 2 L 7 3 4F RT A22WE 2008020600162 20080206 00162 WP 2008 2 6 UPS07850895 1 20070918 A 5210 WEB DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1 2 HOLES DRILLED THRU LOWER AFT WEB ON L-1 DOOR INTERIOR SKIN. FABRICATED AND INSTALLED REPAIR DOUBLE R ON LWR AFT WEB ON L-1 DOOR INTERIOR SKIN IAW SRM 53-3-0 FIG 1 AND SRM 52-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2008020600185 20080206 00185 WP 2008 2 6 UPS08851526 1 20071230 A 5321 FLOORBOARD DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 FLOORBOARD PANEL NR 680 CRACKED AND BENT AND HAS CORROSION. REPAIRED FLOORBOARD PANEL NR 680 BY FABR ICATION AND INSTALLATION OF SKIN TO 3 HAT CHANNELS IAW SRM 51-1-21, SRM 51-3-02 AND SRM 51- 1-8. 2 L 7 4 4F RT 4A25 2008020600187 20080206 00187 WP 2008 2 6 UPS08851529 1 20071229 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1580 L21R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 RT STA 1580 FRAME CRACKED ABOVE CUSP, MAIN CABIN. REPAIRED RT STA 1580 FRAME ABOVE CUSP IAW SRM 53-0 2-00 FIG 02, SRM 51-1-8, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2008020600198 20080206 00198 NM 2008 2 6 UPS08M51482 1 20071125 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C HORIZ STAB CONSTANT SECTION BARREL NUT BORE NR 36 RT FOUND WITH CORROSION. CORROSION AT B-NUT BORE RE MOVED. BORE BOTTOM REMOVED BLEND OUT 0.110" DEEP, BORE REAM TO 2.538" DIAMETER REMN BLEND OUT 0.065" DEEP FOUND EXCEED LIMIT 10X MAG INSP C/O AND FOUND NO CORROSION EVDT. B-NUT BORE, BOTTOM SURFACE BORE DOW N 0.045" DEEPER. REPAIR SLEEVE BUSHING FAB, PROTECTED AND INSTALLED. REPAIR IS ACCEPTABLE PER EN1761-07. 2 L 7 3 4F RT A22WE 2008020600200 20080206 00200 NM 2008 2 6 2007UALA05248 1 20071221 A 2400 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE UNKNOWN A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 663UA 27160 EICAS MSG R GEN OFF DISPLAYED. GEN OFF LIGHT ILLUM. CREW COMMENTS: A-C DID NOT PICK UP AC BUS AFTER RT ENGINE STARTED . 2 L 7 2 4F 4 F RT A1NM E24NE 2008020800046 20080208 00046 WP 2008 2 8 DHL2007873504 1 20071228 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 600 DAMAGED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 89073 46091 MAIN CARGO COMPT FLOORBEAM MISDRILLED HOLES AT STA 600.000 RBL 32.250 AND RBL 38" (MAJOR REPAIR). PERFORMED MAJOR REPAI R IAW SRM 51-2-1 FIG 1 SHEET 9-12 TR NR 51-30 DATED JAN 26-04. REMOVED FASTENERS IAW SRM 51-1-20D, CUT OUT DAMAGED SECT ION, FABRICATED REPAIR ANGLE, FILLER IAW SRM 51-2-1 FIG 1 SHEET 9-12 TR NR 51-130 SRM 53-7-3 FIG 9 ITEM "C". CLEANED TR EATED PRIMED AREA, REPAIR PART IAW SRM 51-1-8B. INSTALLED REPAIR PART IAW SRM 51-2-1 FIG 1 SHEET 9-12 TR NR 51-130 SRM 51-1-11 SRM 51-1-21 SRM 51-1-20D SRM 51-3-1. 2 L 7 4 4F RT 4A25 2008020800050 20080208 00050 WP 2008 2 8 DHL2007873508 1 20071226 A 5414 SKIN DOUG DC8 DC873F 302199F WP NR 4 NACELLE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 NR 4 ENG RT NOSE COWL UPPER EXTERNAL SKIN WORN AT STA YN 147.534 AT 12 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPA IR IAW SRM 71-5-2 FIG 2 SHEET 1.2. REMOVED FASTENERS IAW SRM 51-1-21, CUT OUT DAMAGE SECTION AND FABRICATED NE SKIN AND SPLICE IAW SRM 71-5-2 FIG 2 SHEET 1-2 SRM 51-1-4. HEAT TREATED SPLICE FROM 17-7PH-ST TO 17-7 PH-TH1050 IAW SRM 51-1-6. CLEANED, TREATED, PRIMED AREA AND NEW SKIN IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 71-5-2 FIG 2 SHEET 1-2 SRM 51-1-11 SRM 51-1-21A. 2 L 7 4 4F RT 4A25 2008020800168 20080208 00168 NM 2008 2 8 ASAA0842507 1 20071218 A 5753 65C3570340 SKIN BOEING 737 737490 1384715 NM FOREFLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 793AS 28888 RIGHT WING O/B AFT FORE FLAP UPPER SURFACE CHAFED IN CENTER AREA. REMOVED DAMAGED AREA OF SKIN, FABRICATED FILLER AND R EPAIR DOUBLER, PREPARED AREA AND BONDED IAW BOEING SRM 51 70 10 PAR 7 8 11 12 AND 20. 2 L 7 2 4F RT A16WE 2008020800171 20080208 00171 NM 2008 2 8 ASAA0842508 1 20071228 A 5753 654643490 SKIN BOEING 737 737490 1384715 NM T/E FLAP DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 793AS 28888 RIGHT I/B TRAILING EDGE FLAP LOWER SKIN HAS A 2" X 1" HOLE TEAR 9.5" FWD OF TRAILING EDGE 16" I/B OF O/B EDGE (TEMPORARY REPAIR). PREPARED DAMAGED AREA, REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, PREPARED AREA AND BONDED IAW B737 SRM 5 1 70 10. PREPARED AND INSTALLED GLASS OVERLAY IAW B737 51 70 70. 2 L 7 2 4F RT A16WE 2008020800047 20080208 00047 WP 2008 2 8 DHL2007873505 1 20071226 A 7110 NOSE COWL DOUG DC8 DC873F 302199F WP NR 3 NACELLE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 NR 3 ENG NOSE COWL WORN BETWEEN STA YN 147.534 AND 156.534 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN AND SPLICE IAW SRM 71-5 -2 FIG 2 SHEET 1, 2, SRM 51-1-4. HEAT TREATED SPLICE FROM 17-7PH-ST TO 17-7 PH-TH1050 IAW SRM 51-1-6. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 71-5-2 FIG 2 SHEET 1, 2, SRM 51-1-11, SRM 51-1-21A. 2 L 7 4 4F RT 4A25 2008020800048 20080208 00048 WP 2008 2 8 DHL2007873506 1 20071226 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 175-185 MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 89073 46091 REPAIR ON FUSELAGE EXTERIOR NOT IN ACCORDANCE WITH SRM (STA 175.000 - 185.000 L-34R TO L-35R) MAJOR REPAIR. PERFORMED M AJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1, 2. REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21. CUT OUT DAMAGED SEC TION AND FABRICATED REPAIR DOUBLER FILLER AND INTERNAL FINGER DOUBLER IAW SRM 53-2-1 FIG 7 SHEET 1, 2 SRM 53-4-1 FIG 5C ITEM "A". CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 53-2-1 FIG 7 SHEET 1, 2, SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2008020800123 20080208 00123 EU 2008 2 8 CPCP20070120 1 20071024 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 355AT 355 RT SEAT TRACK FRAME 39-40 CORRODED AROUND NUTPLATE HOLES. RT SEAT TRACK FRAME 39-40. REPLACED IAW SRM 51-25-04. 2 H 7 2 4T RT A53EU 2008020800166 20080208 00166 NM 2008 2 8 ASAA0842509 1 20071219 A 5753 65C26603202 SKIN BOEING 737 737490 1384715 NM T/E FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 793AS 28888 RIGHT WING NR 4 L/E SLAT LOWER SURFACE OF T/E WEDGE CHAFED IN CENTER AREA. REMOVED DAMAGED AREA, FABRICATED FILLER AND REPAIR DOUBLER, PREPARED AREA AND BONDED IAW B737 SRM 51 70 10 PAR 7 8 11 15 AND 20. 2 L 7 2 4F RT A16WE 2008020800367 20080208 00367 NM 2008 2 8 EIA2008004 1 20071228 A 5330 SKIN BOEING 747 7474J6 13848BG NM BS 2700 DENTED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 747BC 25879 SECTION 48 TAIL CONE STATION 2700 RT SIDE DENTED 2 PLACES JUST AFT OF APU INLET DOOR. REMOVED DAMAGE, FABRICATED AND IN STALLED REPAIR PER B747 SRM 53-00-01 FIGURE 201 SHEET 5 TABLE III. 2 L 7 4 4F RT A20WE 2008021100002 20080211 00002 EA 2008 2 11 SWIA200719151 1 20071013 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT MLG CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 941SW 7750 RIGHT GEAR AFT BRAKE TRANSDUCER BRACKET IS CRACKED, FOUND AT C-CHECK. REPLACED BRACKET IAW CRJ200 SRM REF 51-42-06 PG 1 1. 2 L 7 2 4F RT A21EA 2008021100003 20080211 00003 EA 2008 2 11 SWIA200719166 1 20071016 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 744SK 10200 FS 280 COCKPIT FLOORBEAM IS CRACKED AT RBL9 AND LBL9, FOUND AT C-CHECK. REPLACED COCKPIT FLOORBEAM PER CRJ700 SRM 51-42 -06. 2 L 7 2 4F RT A21EA 2008021100004 20080211 00004 EA 2008 2 11 SWIA200719189 1 20071101 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 430SW 7523 FS 280 FORWARD FLOORBEAM IS CRACKED, FOUND AT C-CHECK. REPLACED CRACKED FLOORBEAM PER CRJ200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008021100006 20080211 00006 EA 2008 2 11 SWIA200719190 1 20071105 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 943SW 7762 RIGHT SIDE OF STA 280 FLOORBEAM IS CRACKED AT RBL 32, FOUND AT C-CHECK. INSTALLED REPAIR IAW CRJ200 REO 601R-53-11-171 REV D AND STANDARD REPAIR 601R-53-0057A. 2 L 7 2 4F RT A21EA 2008021100008 20080211 00008 EA 2008 2 11 SWIA200719192 1 20071105 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 943SW 7762 STA 280 FLOORBEAM IS CRACKED AT APPROXIMATELY LBL34, FOUND AT C-CHECK. COMPLIED WITH THE INSTALLATION OF REPAIR PARTS P ER CRJ200 REO 601R-53-11-138. 2 L 7 2 4F RT A21EA 2008021100009 20080211 00009 EA 2008 2 11 SWIA200719193 1 20071105 A 7120 BUSHING CNDAIR CL600 CL6002B19 1900309 EA ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 943SW 7762 RIGHT ENGINE FORWARD MOUNT LINK BUSHING IS CORRODED, FOUND AT C-CHECK. REPLACED ENGINE MOUNT LINK PER CRJ200 AMM 71-00- 00-400-801, SUBTASK 71-00-00-210-001. 2 L 7 2 4F RT A21EA 2008021100010 20080211 00010 SO 2008 2 11 SWIA200719194 1 20071220 A 5751 PULLEY EMB 120 EMB120ER 3260203 SO RT AILERON CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 583SW 120351 RIGHT AILERON O/B PULLY IS CRACKED, FOUND AT C-CHECK. REPLACED PULLY IAW EMB 120 MM 27-00-00. 2 L 7 2 4T RT A31SO 2008021100013 20080211 00013 SO 2008 2 11 SWIA200719195 1 20071220 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 583SW 120351 LEFT FLOOR SEAT TRACK AFT AREA IS CORRODED, FOUND AT C-CHECK. REPLACED SEAT TRACK AFT PORTION IAW EMB 120 MM 53-01-05. 2 L 7 2 4T RT A31SO 2008020800042 20080208 00042 WP 2008 2 8 DHL2007873502 1 20071228 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 620 DAMAGED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 89073 46091 MAIN CARGO COMPT FLOORBEAM MISDRILLED HOLE AT STA 620.000 RBL 38" (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 51-2-1 FIG 1 SHEET 9-12, TR NR 51-130 DATED JAN 26-04. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRI CATED REPAIR ANGLE AND FILLER BOTH IAW SRM 51-2-1 FIG 1 SHEET 9-12, TR NR 51-130, SRM 53-7-3 FIG 9 ITEM "C". CLEANED, T REATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 51-2-1 FIG 1 SHEET 9-12, TR NR 51-130, SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2008020800043 20080208 00043 WP 2008 2 8 DHL2007873503 1 20071226 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT WING TE FLAPS WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 RT WING INBD FLAP UPPER SKIN WORN AT STA XW 106.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOV ED DAMAGED PANEL PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED PLATING AND BONDED DOUBLER IAW SRM 57-7-1 FIG 1 I TEM "A" "L". BONDED BOTH PARTS WITH HYSOL IAW SRM 51-1-9 TR NR 51-142, SRM 51-1-9A, TR NR 51-141. CLEANED, TREATED AND PRIMED AREA AND NEW PANEL PLATING INNER FACE IAW SRM 51-1-8B. INSTALLED NEW PANEL PLATING IAW SRM 51-1-11, SRM 51-1-21 . 2 L 7 4 4F RT 4A25 2008021100007 20080211 00007 EA 2008 2 11 SWIA200719191 1 20071105 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT MLG WW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 943SW 7762 LEFT MAIN LANDING GEAR WHEEL WELL TRANSDUCER BRACKET IS CRACKED, FOUND AT C-CHECK. REPLACED BRACKET IAW CRJ200 SRM 51-4 2-06 PG 11-18. 2 L 7 2 4F RT A21EA 2008021100025 20080211 00025 EA 2008 2 11 SWIA200719152 1 20071013 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 941SW 7750 UPPER FLOORBEAM IS CRACKED AT STA 280 AND RBL9, FOUND AT C-CHECK. COMPLIED WITH REPAIR OF UPPER FLOORBEAM PER CRJ200 RE O 601R 53-11-136 DATED 10-02-99. 2 L 7 2 4F RT A21EA 2008021100026 20080211 00026 EA 2008 2 11 SWIA200719167 1 20071016 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 744SK 10200 RIGHT LOWER WEB AT FS 280 IS CORRODED, FOUND AT C-CHECK. REPLACED RIGHT LOWER WEB AT FS 280 PER CRJ700 SRM 53-11-10-201 -003-A01. 2 L 7 2 4F RT A21EA 2008021100036 20080211 00036 EA 2008 2 11 SWIA200719153 1 20071013 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 941SW 7750 STA 280 AT LBL9 LOWER FLOORBEAM IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH FLOORBEAM REPAIR PER CRJ200 REO 601R 53-11- 171. SCHEME B DATED 13-02-2007. 2 L 7 2 4F RT A21EA 2008021100037 20080211 00037 EA 2008 2 11 SWIA200719168 1 20071023 A 2720 CONTROL CABLE CNDAIR CL600 CL6002C10 1390015 EA RUDDER FRAYED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 746SK 10202 LEFT OUTBOARD RUDDER CABLE IS WORN, FOUND AT C-CHECK. REPLACED RUDDER CABLE IAW CRJ7/9 AMM 27-21-00-400-801-A02. 2 L 7 2 4F RT A21EA 2008021100046 20080211 00046 EA 2008 2 11 SWIA200719154 1 20071013 A 2742 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA STAB CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 941SW 7750 BASE OF STABILIZER ACTUATOR IS CRACKED, FOUND AT C-CHECK. REPLACED STAB ACTUATOR PER CRJ200 MM CH 27-42-01-400-801, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008021100047 20080211 00047 EA 2008 2 11 SWIA200719183 1 20071029 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 707SK 10003 CRACK IN UPPER FLANGE OF FS 280 FLOORBEAM AT RBL12 AND RBL9, FOUND AT C-CHECK. REPLACED FS 280 FLOORBEAM PER REO 670-53 -11-047 REV D. 2 L 7 2 4F RT A21EA 2008021100050 20080211 00050 EA 2008 2 11 SWIA200719188 1 20071101 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 430SW 7523 FS 280 AT LBL9 FLOORBEAM IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO 601R-53-11-171 AND CRJ200 SRM 51- 42-06. 2 L 7 2 4F RT A21EA 2008021100077 20080211 00077 NM 2008 2 11 EIA2008005 1 20071227 A 5315 FLOORBEAM BOEING 747 7474J6 13848BG NM BS 1800 PUNCTURED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 747BC 25879 FLOORBEAM WEB PUNCTURED BODY STATION 1800, LBL 53, WL 108. REMOVED DAMAGED AREA OF WEB, FABRICATED AND INSTALLED REPAIR PER ENGINEERING DISPOSITION LETTER ITEM 1 AND 2 DATED 12-21-07 AND B747 SRM 53-00-07 PAGES 201-203. 2 L 7 4 4F RT A20WE 2008021100104 20080211 00104 NM 2008 2 11 UPS08M51581 1 20071107 A 5330 SKIN DOUG MD11 MD11F 3023600 NM BS 615 L4R DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:C FWD FUSE CROWN AT STA 615.0 BETWEEN RT L4 AND L7 FOUND PREVIOUS DENT BLENDOUT REPAIR. REMOVED EXISTIN G FASTENER FOR ACCESS AND TRIM OFF DENT AREA PER SRM 53-20-00 VIR35 FIG2. HFEC INSP C/O ON TRIM OFF AREA, FOUND NO CRAC K EVIDENT. FAB NEW REPAIR DOUBLER 2EA AND FINGER DOUBLER 2EA. REPAIR DOUBLERS AND FINGER DOUBLERS HOLES PICK UP, REPRO TECT AND PAINTED. NEW 2EA REPAIR AND 2EA FINGER DOUBLERS INSTALLED. REWORKED AREA PAINTED. 2 L 7 3 4F RT A22WE 2008021100116 20080211 00116 NM 2008 2 11 EIA2008006 1 20071228 A 5315 FLOORBEAM BOEING 747 7474J6 13848BG NM BS 1780 GOUGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 747BC 25879 FLOORBEAM WEB HAS DEEP GOUGE AT BS 1780, LBL 16, WL 105. REMOVED DAMAGED SECTION OF WEB FABRICATED AND INSTALLED REPAIR PER B747 SRM 53-00-07 PAGES 201-202 AND 51-40-02 PAGE 1-3. 2 L 7 4 4F RT A20WE 2008021100124 20080211 00124 NM 2008 2 11 EIA2008001 1 20071228 A 5313 STRINGER BOEING 747 7474J6 13848BG NM BS 296 S30R CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 747BC 25879 BS 296 STRINGER 30R CRACKED. CUTOUT DAMAGE STRINGER SECTION. NDT AREA, FABRICATED AND INSTALLED REPAIR PER B747 SRM 53 -00-03 PAGES 201-202 AND PAGES 206-207. 2 L 7 4 4F RT A20WE 2008021100125 20080211 00125 NM 2008 2 11 EIA2008002 1 20071230 A 5315 FLOORBEAM BOEING 747 7474J6 13848BG NM BS 1780 BENT A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 747BC 25879 BODY STATION 1780, LBL 29, WL 118 FLOORBEAM UPPER CHORD HAS AFT FLANGE BENT. REMOVED DAMAGED FLANGE UPPER CHORD. FABRI CATED AND INSTALLED REPAIR PER B747 SRM 51-70-12 PAGES 201-207 AND 51-40-02 PAGES 1-3. 2 L 7 4 4F RT A20WE 2008021100126 20080211 00126 NM 2008 2 11 EIA2008003 1 20071226 A 5315 FLOORBEAM BOEING 747 7474J6 13848BG NM BS 1780 BENT A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 747BC 25879 BODY STATION 1780, RBL 18, WL 118 FLOORBEAM UPPER CHORD HAS AFT FLANGE BENT. CUT OUT DAMAGED CHORD, FABRICATED AND INST ALLED REPAIR PER B747 SRM 51-70-12 PAGE 202 FIGURE 201, 51-70-12 PAGES 201-206 AND 51-40-02 PAGE 1. 2 L 7 4 4F RT A20WE 2008021100133 20080211 00133 EA 2008 2 11 SWIA200719156 1 20071013 A 7120 BEARING CNDAIR CL600 CL6002B19 1900309 EA ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 941SW 7750 RIGHT ENGINE MOUNT THRUST SHAFT AND INNER BEARINGS ARE CORRODED, FOUND AT C-CHECK. REPLACED RIGHT ENGINE THRUST SHAFT A ND INNER BEARINGS IAW CRJ200 AMM 71-00-00. 2 L 7 2 4F RT A21EA 2008021100134 20080211 00134 EA 2008 2 11 SWIA200719157 1 20071027 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 944SW 7764 LBL 9 AND RBL 9 AT FS 280 IS CRACKED NEAR UPPER FLOORBEAM, FOUND AT C-CHECK. COMPLIED WITH REPAIR PER REO 601R-53-11-13 6. 2 L 7 2 4F RT A21EA 2008021100139 20080211 00139 NM 2008 2 11 UPS08M51531 1 20071218 A 5713 STRINGER DOUG MD11 MD11 3023602 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C RT WING UPPER STRINGER END NR 12 SUSPECT CRACK AS MARKED, THRU TANK ACCESS NR 635BT, RHW UPPER STRINGE R NR 12 ATTACHED SPLICE REMOVED FOR ACCESS. HFEC INSP C/O PER DAC NDT SPM R13, 06-10-01.001 AND FOUND CRACK END APPROX 8". CRACK AREA SLOTTED OUT PER SRM 57-20-00 FIG 10 V.I R35. HFEC INSP C/O PER DAC N DT SPM R13,06-10-01.001 ON SLOTTED OUT AREA AND FOUND NO CRACK EVIDENT NEW REPAIR ANGLES FAB AND INSTALLED PER SRM 51-33-01 AND SRM 57-20-00. 2 L 7 3 4F RT A22WE 2008021100150 20080211 00150 EA 2008 2 11 SWIA200719148 1 20071016 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 986SW 7967 CRACK FOUND ON SUPPORT ANGLE AT FS625 LBL40 AND WL 98, FOUND AT C-CHECK. REPLACED ANGLE AT FS 625 LBL 40 AND WL 98 PER REO 601R-53-61-422. 2 L 7 2 4F RT A21EA 2008021100177 20080211 00177 EA 2008 2 11 SWIA200719161 1 20071027 A 5313 STRINGER CNDAIR CL600 CL6002B19 1900309 EA BS 625 S12R CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 944SW 7764 STA 625 RIGHT SIDE STRINGER 12 IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS AT STA 625 PER CRJ200 SRM 51-77-00 P G 1 AND REO 601R-53-61-422. 2 L 7 2 4F RT A21EA 2008020800339 20080208 00339 WP 2008 2 8 DHL2007873500 1 20071225 A 5753 SKIN DOUG DC8 DC873F 302199F WP LT WING TE FLAP DEFORMED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 LT WING OUTBD FLAP LWR SKIN DEFORMED AT STA XF 306.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 4 TR N R 57-94 DATED 10-01-02. REMOVED DAMAGED PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0. 050") IAW SRM 57-7-1 FIG 4, TR NR 57-94 ITEM "A". CLEANED, TREATED AND PRIMED AREA AND NEW PLATING INNER FACE IAW SRM 5 1-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-11. INSTALLED NEW PLATING IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2008021100048 20080211 00048 EA 2008 2 11 SWIA200719184 1 20071029 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 707SK 10003 PAX DOOR OUTER HANDLE IS CRACKED, FOUND AT C-CHECK. REPLACED OUTER HANDLE ON PASSENGER DOOR PER CRJ700 AMM 52-11-03-400 -801-A01. 2 L 7 2 4F RT A21EA 2008021100135 20080211 00135 EA 2008 2 11 SWIA200719158 1 20071027 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 944SW 7764 RBL 9 AT FS 280 FLOORBEAM IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIR PER CRJ200 REO 601R 53-11-171. 2 L 7 2 4F RT A21EA 2008021100172 20080211 00172 EA 2008 2 11 SWIA200719149 1 20071016 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 986SW 7967 AFT FLOOR SUPPORT CRACKED AT FS 621 AND LBL 41, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO 601R-53-61-117 REV A. 2 L 7 2 4F RT A21EA 2008021100176 20080211 00176 EA 2008 2 11 SWIA200719160 1 20071027 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 944SW 7764 FS 280 FORWARD FLOOR SUPPORT IS CRACKED AT RBL9, FOUND AT C-CHECK. REPLACED CRACKED SUPPORT ANGLE. 2 L 7 2 4F RT A21EA 2008021100186 20080211 00186 NM 2008 2 11 MASA200800047 1 20071208 A 5330 ACCESS PANEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 987HA 425 RT SIDE FUSELAGE ACCESS PANEL FASTENER HOLE AT ST 25 IS DAMAGED AND ELONGATED, REPAIRED. 2 H 7 2 4T RT A13NM 2008021100198 20080211 00198 NM 2008 2 11 ASAA0752058 1 20070919 A 3233 NC243 BEARING BOEING 737 737890 1384527 NM NLG ACTUATOR MIGRATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 562AS 35091 DURING DAILY CHECK, FOUND NLG RETRACT ACTUATOR ATTACH LUG BEARING MIGRATION LEFT OF CENTER OUT OF LIMITS REF EA 3230 010 55. STEP 1 BEARING MIGRATION MEASURES .155 LEFT OF CENTER. PREVIOUSLY ON DEFERRAL REF L P 6264563. BEARING MIGRATION CONDITION WAS REPAIRED REF L P 6351796. BEARING WAS REMOVED AND REPLACED RESWAGED. 2 L 7 2 4F RT A16WE 2008021200034 20080212 00034 EU 2008 2 12 USA2008F00000 1 20070926 A 5320 ASNA2051DKS RIVET AIRBUS A321 A321211 3930370 EU CFMINT CFM56 CFM565B32P 13008 NE CARGO BAY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 186US 20014 1701 CORRODED RIVET TAILS WERE FOUND IN THE FUSELAGE FWD CARGO COMPARTMENT BETWEEN FR 24 TO 35.8, STRINGER 39L TO 39R. APPRO XIMATELY 1492 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD THE PAI NT FLAKING OFF THE RIVET TAILS THAT WERE CLEANED AND HAD PRIMER AND PAINT REAPPLIED. AIRCRAFT WAS MFG 27 FEB 2002. (K) 2 L 7 2 4F 4 F RT A28NM 2008021200122 20080212 00122 NM 2008 2 12 ASAA0842514 1 20071216 A 5755 654645170 SKIN BOEING 737 737490 1384715 NM LT WING SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 793AS 28888 LT WING NR 3 SPOILER DENTED ON UPPER SURFACE PREPARED AREA OF DAMAGE FOR REPAIR 4 IAW SRM 57-70-01 PGS 201 202. FABRICA TED DOUBLER AND BONDED IAW SRM 57-70-01 REPAIR 2. 2 L 7 2 4F RT A16WE 2008021200124 20080212 00124 NM 2008 2 12 ASAA0842515 1 20071216 A 5755 654645170 SKIN BOEING 737 737490 1384715 NM LT WING SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 793AS 28888 LT WING NR 1 SPOILER DENTED ON UPPER SURFACE PREPARED AREA OF DAMAGE FOR REPAIR 4 IAW SRM 57-70-01 PGS 201-202. FABRICA TED DOUBLER AND BONDED IAW SRM 57-70-01 REPAIR 2. 2 L 7 2 4F RT A16WE 2008021200128 20080212 00128 NM 2008 2 12 ASAA0842516 1 20071217 A 5753 65C3570340 SKIN BOEING 737 737490 1384715 NM RT WING FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 793AS 28888 RT WING O/B FOREFLAP LEADING EDGE IS CHAFED AT O/B CORNER REMOVED DAMAGE FROM SKIN ON L/E. FABRICATED DRILLED AND INSTA LLED A REPAIR DOUBLER IAW SRM 57-53-01 FIG 201. 2 L 7 2 4F RT A16WE 2008021200135 20080212 00135 NM 2008 2 12 ASAA0752009 1 20070827 A 5710 STRUCTURE BOEING 737 737890 1384527 NM WINGLET DAMAGED A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 564AS 0104 35103 LT WINGLET DAMAGED DUE CONTACT WITH AIRCRAFT N784 AT GATE. REMOVED AND REPLACED WINGLET ASSY PER AMM 57 20 21. 2 L 7 2 4F RT A16WE 2008020800340 20080208 00340 WP 2008 2 8 DHL2007873501 1 20071225 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT WING TE FLAP DEFORMED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 RT OUTBD FLAP LWR SKIN DEFORMED AT STA XF 306.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 4 TR NR 57- 94 DATE 10-01-02. REMOVED DAMAGED PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.050") I AW SRM 57-7-1 FIG 4 TR NR 57-94 ITEM "A". CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF NEW PLATING IAW SRM 51-1-8 B. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-11. INSTALLED NEW PLATING IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2008021100049 20080211 00049 EA 2008 2 11 SWIA200719187 1 20071101 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 430SW 7523 FS 280 AT RBL9 AND LBL9 UPPER FLOORBEAM IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER REO 601R-53-11-136 REV A AND REO 601R-53-11-1271 REV A. 2 L 7 2 4F RT A21EA 2008021100095 20080211 00095 NM 2008 2 11 UPS08M51509 1 20071214 A 5320 INTERCOSTAL DOUG MD11 MD11 3023602 NM BS 1701-1721 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C CABIN, INTERCOSTAL AT STA 1701-1721, L7 RT FOUND CRACKED AS MARKED. CRACKED INTERCOSTAL AT CABIN STA 1701-1721 LONGERON L7 AREA REMOVED PER SRM51-31-01 V.II R35. NEW INTERCOSTAL P/N:AFA7761-25 FAB PER BOEING DWG AFA7761. FAB INTERCOSTAL FASTENERS HOLES PICKED UP PER SRM 51-31-01 V II R35. NEW INTERCOSTAL AT CABIN STA 1701-1721 LONGERON L7 RT AREA INSTALLED PER SRM 51-31-01 V II R35. 2 L 7 3 4F RT A22WE 2008021100178 20080211 00178 EA 2008 2 11 SWIA200719162 1 20071019 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 938SW 7741 LBL 9 AT FS 280 SHOWS SIGNS OF CRACKING, FOUND AT C-CHECK. COMPLIED WITH REPAIR OF CRACKED ANGLE AT FS 280 AND LBL 9 FL OORBEAM IAW CRJ200 REO 601R-53-11-138 REV NC. 2 L 7 2 4F RT A21EA 2008021100199 20080211 00199 NM 2008 2 11 ASAA0751411 1 20070117 A 5210 141A61506 FRAME BOEING 737 737890 1384527 NM L1 DOOR BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 564AS 35103 AFT INNER FRAME UPPER CORNER OF THE L1 DOOR IS BENT AND CRACKED DUE TO CONTACT WITH JETWAY. ACCOMPLISHED EA5210 01220 R EPAIR ANGLE. 2 L 7 2 4F RT A16WE 2008021100201 20080211 00201 NM 2008 2 11 ASAA0752057 1 20070918 A 5330 143A3232 SKIN BOEING 737 737890 1384527 NM BS 488 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 566AS 35181 RAMP CREW STRUCK FWD PIT SCUFF PLATE WITH BELT LOADER. TWO SMALL SCRATCHES ON EDGE OF SKIN AND BEAR STRAP. BLENDED EDG E OF BEAR STRAP AND SKIN PERFORMED HFEC INSPECTION ARE CRACK FREE. REPLACED DAMAGED FWD AND CTR SCUFF PLATES IAW EA 533 0 02237. 2 L 7 2 4F RT A16WE 2008021200172 20080212 00172 NM 2008 2 12 2008UALA00013 1 20071231 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EEL INOP BETWEEN MID LAVS. RECONNECTED EMERGENCY LIGHTS. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200212 20080212 00212 EA 2008 2 12 A6WA200740707 1 20071220 A 7830 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE THRUST REVERSER MALFUNCTIONED A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 407AW 7424 LT REVERSER UNLOCKED MESSAGE IN FLIGHT. REACTIVATED LT THRUST REVERSER PERFORMED FUNCTIONAL TEST IAW 78-30-00. CHECKS NORMAL THIS TIME PLACARD AND MEL REMOVED. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200213 20080212 00213 NE 2008 2 12 A6WA200740708 2 20071227 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RIGHT LEAKING A A6WA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 31 466AW 7899 SMOKE TOILET CAS MESSAGE INFLIGHT, SMOKE VISIBLE COMPLIED WITH QRH. SMOKE SOURCE APPEARED TO BE FROM ACROSS LAV ROW 13, AREA LOWER AREA. (K) AIRCRAFT WAS TROUBLESHOT TO RT ENGINE INTERNAL LEAK. REMOVED AND REPLACED. (VENDOR FINDINGS: CAR BON SEAL PRESSURIZATION VALVE BODY CRACKED, LRU). (A) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200214 20080212 00214 EA 2008 2 12 A6WA200740710 1 20071224 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 CRACK ON REAR PRESSURE BULKHEAD FWD FACE UNDER LINTER FITTING BRACKET. REPAIR TO REAR PRESSURE CUTOUT IAW REO 601R-53-61 -1230 REV D. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200217 20080212 00217 EA 2008 2 12 A6WA200740712 1 20071227 A 5242 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE ACCESS DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 426AW 7669 AC CONNECTOR LANDING STRUCTURE OF ACCESS DOOR FOUND CRACKED APPROX 2.500 INCH. AC CONNECTOR ACCESS DOOR LANDING REPAIRE D IAW REO 601R-53-11-569, REV A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200222 20080212 00222 EA 2008 2 12 SWIA200719150 1 20071013 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT MLG WW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 941SW 7750 LEFT GEAR AFT BRAKE TRANSDUCER BRACKET IS CRACKED, FOUND AT C-CHECK. REPLACED BRACKET IAW CRJ200 SRM REF 51-42-06 PG 11 . 2 L 7 2 4F RT A21EA 2008021200223 20080212 00223 EA 2008 2 12 SWIA200719164 1 20071019 A 5753 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 938SW 7741 LEFT OUTBOARD FLAP IS CRACKED ALONG TRAILING EDGE, FOUND AT C-CHECK. REPLACED FLAP ASSEMBLY PER CRJ200 AMM 27-54-05-400 -801. 2 L 7 2 4F RT A21EA 2008021200224 20080212 00224 EA 2008 2 12 SWIA200719165 1 20071016 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 744SK 10200 FS 280 CROSS BEAM IS CRACKED AT RBL9 AND LBL9, FOUND AT C-CHECK. COMPLIED WITH REPAIR OF BEAM PER REO 670-53-11-047. 2 L 7 2 4F RT A21EA 2008021100099 20080211 00099 EA 2008 2 11 SWIA200719155 1 20071013 A 5242 RETAINER CNDAIR CL600 CL6002B19 1900309 EA E/E DOOR SEAL CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 941SW 7750 AVIONICS BAY DOOR SEAL RETAINERS ARE CORRODED, FOUND AT C-CHECK. REPLACED RETAINERS ON AVIONICS BAY DOOR PER CRJ200 SRM 51-42-06 PG 1-18. 2 L 7 2 4F RT A21EA 2008021100136 20080211 00136 EA 2008 2 11 SWIA200719159 1 20071027 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 944SW 7764 FS 280 AND LBL 9 LOWER FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 2008021100179 20080211 00179 EA 2008 2 11 SWIA200719163 1 20071019 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 938SW 7741 LBL9 AT FS 280 IS CRACKED AT LOWER RADIUS, FOUND AT C-CHECK. COMPLIED WITH FLOORBEAM REPAIR IAW CRJ200 REO 601R-53-11-1 71 REV C. 2 L 7 2 4F RT A21EA 2008021100200 20080211 00200 NM 2008 2 11 ASAA0752055 1 20070912 A 5230 1036541 HANDLE BOEING 737 737890 1384527 NM CARGO DOOR SCRATCHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 556AS 35175 FWD CARGO DOOR HANDLE HOUSING HAS INTERIOR SCRACHES REPAIRED IAW EA 5230 011213. 2 L 7 2 4F RT A16WE 2008021200003 20080212 00003 NM 2008 2 12 2007UALA03170 1 20070814 A 2612 MODULE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 924UA 26645 ENG APU FIRE MOD NR 2 ENG DISCHARGE FAILS TEST. REPLACED ENGINE APU FIRE MODULE, NO FAULTS NOTED DURING TEST. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021200166 20080212 00166 NM 2008 2 12 2008UALA00016 1 20071231 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHT INOP DOOR 5L SLIDE ILLUM. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200176 20080212 00176 NM 2008 2 12 2007UALA03190 1 20070815 A 5230 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 FWD CARGO DOOR LOWER AFT FRAME CRACKED IN RADIUS OF OUTER CHORD. MAJOR REPAIR ACP'D, REMOVED AND REPLACED FRAME SECTION . 2 L 7 2 4F 4 F RT A16WE E21EU 2008021200246 20080212 00246 EA 2008 2 12 A6WA200740709 1 20071231 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE WING MALFUNCTIONED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 GL 31 438AW 7748 FLAPS FAIL CAUTION MESSAGE AT ZERO ON APPROACH. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4. FLAP SYSTEM RESET, OK. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021300033 20080213 00033 WP 2008 2 13 UPS08851630 1 20071231 A 5720 56139123 WEB DOUG DC8 DC871F 302199D WP WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 NR 1 MAIN WEB CRACK JUST ABOVE CTR SPAR BET XRS255 AND XRS250 L/W. REPAIRED NR 1 MAIN WEB CRACK ABOV E CTR SPAR BET XRS 255 AND XRS 250 PER SRO 8570005 AND EA 008-5710-01-A1259. 2 L 7 4 4F RT 4A25 2008021300035 20080213 00035 NM 2008 2 13 ABXA080036 1 20071227 A 5754 114T41023 SKIN BOEING 767 767281 1385109 NM NR 2 SLAT CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 787AX 23020 NR 2 SLAT HAD A LARGE CORROSION BULGE ON THE LOWER SURFACE OF LEADING EDGE, NEAR THE INBOARD END. REMOVED, REPAIRED AND REINSTALLED NR 2 SLAT ON SHOP TRAVELER ST-2279-01 AND PWS15, AND IAW B767 AMM 27-81-02-4. 2 L 7 2 4F RT A1NM 2008021300037 20080213 00037 NM 2008 2 13 ABXA080038 1 20071228 A 5315 146T82506 FLOORBEAM BOEING 767 767281 1385109 NM BS 1092 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 787AX 23020 FLOORBEAM ANGLE AT RIGHT BUTT LINE 25, STA 1092 WAS CRACKED AT UPPER END. REMOVED AND REPLACED ANGLE IAW B767 SRM 51-40 -02 AND 53-60-07. 2 L 7 2 4F RT A1NM 2008021300039 20080213 00039 NM 2008 2 13 ABXA080039 1 20071228 A 5330 148T32814 SKIN BOEING 767 767281 1385109 NM BS 1832 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 787AX 23020 AFT FUSELAGE SKIN CRACKED FORWARD OF RIGHT APU DOOR APPROXIMATELY STA 1832. REPAIRED CRACK IAW B767 SRM 53-00-01, FIGUR E 207. 2 L 7 2 4F RT A1NM 2008021200004 20080212 00004 NM 2008 2 12 2007UALA03172 1 20070815 A 5320 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FUSELAGE IS GOUGED AT STA 408, BETWEEN STR 6L AND 7L. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021200115 20080212 00115 NM 2008 2 12 ASAA0842510 1 20071216 A 5753 654643018 SKIN BOEING 737 737490 1384715 NM TE FLAPS DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 793AS 28888 LT INBOARD FORE FLAP HAS MULTIPLE DENTS ON LOWER SURFACE. REMOVED DAMAGED AREA,FABRICATED FILLER AND DOUBLER, PREPARED AREA AND BONDED IAW B737 400 SRM 51 70 10 PER 7 8 11 12 AND 20. 2 L 7 2 4F RT A16WE 2008021200116 20080212 00116 NM 2008 2 12 ASAA0842511 1 20071216 A 5753 6546434369 SKIN BOEING 737 737490 1384715 NM LT WING TE FLAPS DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 793AS 28888 LT INBOARD AFT FLAP HAS MULTIPLE DENTS ON INBOARD UPPER SURFACE SMALL AREA PREPARED DAMAGED AREA IAW B737 400 SRM 51 70 10. REPAIR 2 FABRICATED REPAIR DOUBLER PREPARED AND BONDED IAW B737 400 SRM 51 70 10 PAR 11 12 AND 20. 2 L 7 2 4F RT A16WE 2008021200118 20080212 00118 NM 2008 2 12 ASAA0842512 1 20071227 A 5755 654645268 SKIN BOEING 737 737490 1384715 NM LT WING SPOILER DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 793AS 28888 LT WING INBOARD GROUND SPOILER LOWER SURFACE DELAMINATED. REMOVED DAMAGED AREA OF SKIN. FABRICATED FILLER AND EXTERNAL DOUBLER, PREPARED AREA AND BONDED IAW B737 400 PAR 7 8 11 12 AND 20. 2 L 7 2 4F RT A16WE 2008021200121 20080212 00121 NM 2008 2 12 ASAA0842513 1 20071221 A 5755 654645262 SKIN BOEING 737 737490 1384715 NM RT WING SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 793AS 28888 RT WING INBOARD GROUND SPOILER LOWER SURFACE HAS MULTIPLE DENTS PREPARED AREA OF DAMAGE FOR REPAIR 4 IAW SRM 57-70-01 PG S 201-202. FABRICATED DOUBLERS AND BONDED IAW SRM 57-70-01 REPAIR 2. 2 L 7 2 4F RT A16WE 2008021200168 20080212 00168 NM 2008 2 12 2008UALA00014 1 20071231 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EEL INOP LEFT SIDE AFT GALLEY. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021300036 20080213 00036 NM 2008 2 13 ABXA080037 1 20071228 A 5230 140T2603Y3 BEAM BOEING 767 767281 1385109 NM CARGO DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 787AX 23020 FORWARD LOWER CARGO DOOR BEAM HAD EXFOLIATED CORROSION AT SEVERAL NUT-PLATE AREAS. REMOVED AND REPLACED BEAM ON FORWARD LOWER CARGO DOOR IAW B767 SRM. 2 L 7 2 4F RT A1NM 2008021300141 20080213 00141 NM 2008 2 13 DHL2007785009 1 20071017 A 5322 SHEAR TIE BOEING 727 727214 138407R NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 SURFACE CORROSION ON FORWARD PIT SHEAR TIE BS 520 BETWEEN STRINGER 28L AND 28R. REMOVED FASTENERS IN AREA TO GAIN ACCES S IAW B-727 SRM 51-30-2. REMOVED CORROSION IAW B-727 SRM 51-10-6, FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1. FABRICATED SHEAR TIE REPAIR. CUT OUT DAMAGED SHEAR TIE IAW B-727 SRM 53-10-2 FIGURE 3 AND 53-10-4 FIGURE 11. TREATED A ND PRIMED PARTS IAW B-727 SRM 51-10-2. INSTALLED REPAIR SHEAR TIE AT FORWARD PIT BS 520 BETWEEN STRINGER 28 L AND 28R I AW B0727 SRM 51-30-2 AND 53-10-4 FIGURE 11. 2 L 7 3 4F A3WE 2008021300142 20080213 00142 NM 2008 2 13 DHL2007785010 1 20071101 A 5313 STRINGER BOEING 727 727214 138407R NM BS 560 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 SLIGHT BULGING ON INBOARD SIDE OF STRINGER 27R BS 560 TO BS 567. CUT OUT DAMAGED SECTION OF STRINGER APPROXIMATE DIMENS ION 18" LONG IAW B-727 SRM 53-10-3 FIGURE 1. FABRICATED REPAIR STRINGER. FABRICATED REPAIR SPLICES IAW B-727 SRM 51-10 -3 FIGURE 1 AND SRM 53-10-2 FIGURE 9. TREATED AND PRIMED BARE METAL AREA IAW B-727 SRM 51-10-2. INSTALLED STRINGER REP AIR PARTS AT BS 560 STRINGER 27R IAW B-727 SRM 53-10-3 FIGURE 1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2008021300143 20080213 00143 NM 2008 2 13 DHL2007785011 1 20071017 A 5311 FRAME BOEING 727 727214 138407R NM BS 620 S26-27R GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 C-1 DOOR CUT OUT AFT FRAME BS 620, WEB HAS DEEP GOUGE ON THE FORWARD SURFACE BETWEEN STRINGER 26R AND 27R. BLEND OUT AR EA IAW B-727 SRM 51-10-1. OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1 AND 53-10-2 FIGURE 3. REMOVED FASTENERS FROM AR EA IAW B-727 SRM 51-30-2 AND CUT OUT DAMAGED AREA DIMENSION 4" BY 4" IAW B-727 SRM 51-40-2 FIGURE 1. FABRICATED REPAIR DOUBLER. REPAIR FILLERS IAW B-727 SRM 53-10-2 FIGURE 3 AND 51-40-2 FIGURE 1. TREATED AND PRIMED PARTS IAW B-727 SRM 51 -10-2. INSTALLED REPAIR PARTS IAW B-727 SRM 51-30-2 AND 51-40-2 FIGURE 1. 2 L 7 3 4F A3WE 2008021300145 20080213 00145 NM 2008 2 13 DHL2007785013 1 20071023 A 5322 SHEAR TIE BOEING 727 727214 138407R NM BS 720 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 FORWARD PIT RIGHT BS 720 BETWEEN STRINGER 27R AND 28R FRAME CRACKED AT BOTTOM FLANGE. FABRICATED FRAME SHEAR TIE REPAIR FROM 7075-T6 .063" PO NR 9005685 APPROXIMATE DIMENSION 4.375" BY 5.875" IAW B-727 SRM 53-10-4 FIGURE 12 AND SRM 53-10-2 FIGURE 3. CUT OUT DAMAGED AREA APPROXIMATE DIMENSION 4" BY 5.875" IAW B-727 SRM 53-10-4 FIGURE 12. REPAIR PARTS AND B ARE METAL AREAS TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED REPAIR DOUBLER AT FRAME BS 720 BETWEEN STRINGER 27R AND 28R IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008021300153 20080213 00153 NM 2008 2 13 DHL2007785014 1 20071101 A 5313 STRINGER BOEING 727 727214 138407R NM BS 720E CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 INTERGRANULAR CORROSION NOTED ON STRINGER 26R AT BS 720E + 19". CUT OUT DAMAGED SECTION IAW B-727 SRM 53-10-2 FIGURE 1. FABRICATED REPAIR FILLER. FABRICATED REPAIR SPLICE IAW B-727 SRM 53-10-3 FIGURE 1 AND SRM 53-10-2 FIGURE 9. TREATED AND PRIMED REPAIR PARTS IAW B-727 SRM 51-10-2 AND INSTALLED REPAIR PARTS AT BS 720E + 19" STRINGER 26R IAW B-727 SRM 53- 10-3 FIGURE 1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2008021300154 20080213 00154 NM 2008 2 13 DHL200785015 1 20071027 A 5313 STRINGER BOEING 727 727214 138407R NM BS 720F-740 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 FORWARD PIT BS 720F TO BS 740 STRINGER 27R SHOWS CORROSION. REMOVED CORROSION AT BS 720F TO BS 740 STRINGER 27R IAW B-7 27 SRM 51-10-6, CORROSION FOUND OUT OF LIMIT IAW B-727 SRM 53-10-1 FIGURE 1. CUT OUT DAMAGED STRINGER IAW B-727 SRM 53-1 0-3 FIGURE 1, FABRICATED FILLER. FABRICATED REPAIR CHANNEL IAW B-727 SRM 53-10-3 FIGURE 1 AND SRM 53-10-2 FIGURE 9. IN STALLED STRINGER REPAIR AT BS 720F TO BS 740 STRINGER 27R IAW B727 SRM 53-10-3 FIGURE 1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2008021300155 20080213 00155 NM 2008 2 13 DHL2007785015 1 20071027 A 5313 STRINGER BOEING 727 727214 138407R NM BS 720F-740 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 FORWARD PIT BS 720F TO BS 740 STRINGER 27R SHOWS CORROSION. REMOVED CORROSION AT BS 720F TO BS 740 STRINGER 27R IAW B-7 27 SRM 51-10-6, CORROSION FOUND OUT OF LIMIT IAW B-727 SRM 53-10-1 FIGURE 1. CUT OUT DAMAGED STRINGER IAW B-727 SRM 53- 10-3 FIGURE 1. FABRICATED FILLER. FABRICATED REPAIR CHANNEL IAW B-727 SRM 53-10-3 FIGURE 1 AND SRM 53-10-2 FIGURE 9. INSTALLED STRINGER REPAIR AT BS 720F TO BS 740 STRINGER 27R IAW B727 SRM 53-10-3 FIGURE 1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2008021300159 20080213 00159 NM 2008 2 13 DHL2007785019 1 20071106 A 5322 SHEAR TIE BOEING 727 727214 138407R NM BS 1166 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 SURFACE CORROSION BEHIND SHEAR TIE BS 1166 LEFT SIDE STRINGER 30. REMOVED CORROSION AT BS 1166 SHEAR TIE STRINGER 30 IA W B-727 SRM 51-10-6, FOUND CORROSION OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1. CUT OUT DAMAGED AREA IAW B-727 SRM 5 3-10-4 FIGURE 11. FABRICATED REPAIR DOUBLER IAW B-727 SRM 53-10-2 FIGURE 5 AND 53-10-4 FIGURE 11. TREATED AND PRIMED P ART IAW B-727 SRM 51-10-2, INSTALLED REPAIR DOUBLER PER B-727 SRM 53-10-4 FIGURE 11 AND 51-30-2. 2 L 7 3 4F A3WE 2008021300161 20080213 00161 NM 2008 2 13 DHL2007785021 1 20071107 A 5313 STRINGER BOEING 727 727214 138407R NM BS 1172 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 AFT BAG PIT HAS CORROSION WITH EXFOLIATION ON STRINGER 30 RT BS 1172. REMOVED INTERCOSTAL AND FITTING IAW B-727 SRM 51- 30-2, CUT OUT DAMAGED STRINGER 30 SECTION, FABRICATED STRINGER REPAIR SPLICE IAW B-727 SRM 53-10-3 FIGURE 1 AND 53-10-2 FIGURE 5. FABRICATED NEW INTERCOSTAL AND REPLACED, HEAT TREATED MATERIAL IAW ER 2-37153-801 REV A IAW DRAWING 69-17303. INSTALLED NEW FITTING P/N 69-13383-1 PO NR 7308530 AND INSTALLED REPAIR PARTS AT BS 1166 TO BS 1183 STRINGER 30 IAW B- 727 53-10-3 FIGURE 1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2008021300163 20080213 00163 NM 2008 2 13 DHL2007785024 1 20071015 A 5330 SKIN BOEING 727 727214 138407R NM BS 700 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 RIGHT FUSELAGE UPPER SKIN HAS LIGHTNING STRIKE AT BS 700 + 8" STRINGER 9R. BLEND OUT DAMAGE IAW B-727 SRM 53-30-2 FIGUR E 2 AND 53-30-1 FIGURE 1 AND 2. CUT OUT DAMAGED AREA (DIMENSION .875" DIAMETER) AND FABRICATED REPAIR DOUBLER FROM 2024 -T3 0.063" PO NR 9005773 (DIMENSION 5.5" DIAMETER) AND REPAIR FILLER FROM 2024-T3 0.050" PO NR 9005773 (DIMENSION .875" DIAMETER) IAW B-727 SRM 53-30-3 FIGURE 13 AND 53-30-2 FIGURE 2. TREATED AND PRIMED PARTS IAW B-727 SRM 51-10-2 AND INST ALLED REPAIR PARTS AT RIGHT FUSELAGE UPPER SKIN BS 700 + 8 INCH STRINGER 9R IAW B-727 SRM 51-30-2 AND 53-30-3 FIGURE 13. 2 L 7 3 4F A3WE 2008021300164 20080213 00164 NM 2008 2 13 DHL2007785025 1 20071101 A 5330 SKIN BOEING 727 727214 138407R NM BS 510 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 FORWARD PIT SKIN CORRODED AT ANTENNA CUT OUT BS 510 BETWEEN STRINGER 28L AND 28R. REMOVED FASTENERS AND ANTENNA RING IA W B-727 SRM 51-30-2, REMOVED CORROSION FROM SKIN IAW B-727 SRM 51-10-6, CORROSION FOUND OUT OF LIMITS IAW B-727 SRM 53-3 0-1 FIGURE 1. REMOVED PREVIOUS DOUBLER AT BS 480 - 500 IAW B-727 SRM 51-30-2, CUT-OUT AND REMOVED BELLY SKIN AT BS 480 - 520 BETWEEN STRINGER 26L AND 26R IAW B-727 SRM 53-30-3 FIGURE 12 AND 51-10-1. FABRICATED NEW SKIN SECTION AND REPAIR SPLICE IAW B-727 SRM 53-30-2 FIGURE 2 AND 53-30-3 FIGURE 12. TREATED AND PRIMED REPAIR PARTS AND AREA IAW B-727 SRM 51- 10-2 AND INSTALLED REPAIR SKIN AND SPLICE IAW B-727 SRM 51-30-2 AND 53-30-3 FIGURE 12, REINSTALLED ANTENNA RING IAW B072 2 L 7 3 4F A3WE 2008021300165 20080213 00165 NM 2008 2 13 DHL2007785023 1 20071011 A 5330 SKIN BOEING 727 727214 138407R NM BS 1090 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 SCRATCH ON UPPER FUSELAGE SKIN BS 1090 STRINGER 4R TO STRINGER 5R. BLENDED OUT DAMAGE AREA IAW B-727 SRM 51-10-4. FOUN D OUT OF LIMITS IAW B-727 SRM 53-30-2 FIGURE 2 AND 53-30-1 FIGURE 1 AND 2. DISPLACED GILLINER CABIN LINER FOR ACCESS BE TWEEN BS 1030 AND BS 1110 STRINGERS 4R TO 10R IAW B-727 SRM 51-30-2 AND AEI MM CHAPTER 25. CUT OUT DAMAGE AREA DIMENSIO N IAW B-727 SRM 51-10-1 AND 53-30-3 FIGURE 1. FABRICATED REPAIR PART DOUBLER IAW B-727 SRM 53-30-2 FIGURE 1. TREATED A ND PRIMED IAW B-727 SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW B-727 SRM 53-30-1 AND 51-30-2, REINSTALLED GILLINER IAW B -727 SRM 51-30-2 AND AEI MM CHAPTER 25. 2 L 7 3 4F A3WE 2008021300167 20080213 00167 NM 2008 2 13 DHL2007742015 1 20071119 A 5320 INTERCOSTAL BOEING 727 727225 1384077 NM BS 361 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 MAIN CARGO INTERCOSTAL AT BS 361 STRINGER 8R HAS FORWARD EDGE CRACKED. REMOVED CRACKED INTERCOSTAL IAW B-727 SRM 51-30- 2. FABRICATED NEW INTERCOSTAL IAW B-727 SRM 51-20-1 AND 53-10-2 FIGURE 3. TREATED AND PRIMED NEW INTERCOSTAL IAW B-727 SRM 51-10-2 AND INSTALLED NEW INTERCOSTAL AT MAIN CABIN BS 361 STRINGER 8R IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008021300169 20080213 00169 NM 2008 2 13 DHL2007742017 1 20071207 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 740-848.95 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 MAIN CABIN BS 740 TO BS 848.95 RBL 45 SEAT TRACK HAS CORROSION AT INBOARD FLANGE. REMOVED DAMAGED SEAT TRACK IAW B-727 SRM 51-30-2, FABRICATED IAW B-727 SRM 51-30-5 AND SRM 52-10-2 FIGURE 3 AND 5. INSTALLED EXTRUSION SEAT TRACK IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008021300172 20080213 00172 NM 2008 2 13 DHL2007785026 1 20071026 A 5522 SKIN BOEING 727 727214 138407R NM RT ELEVATOR PUNCTURED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 RIGHT ELEVATOR LOWER SKIN PUNCTURED AT ELEVATOR STATION 35.55. REMOVED FASTENERS AT RIGHT ELEVATOR LOWER SKIN STATION 3 5.55 IAW B-727 SRM 51-30-2, CUT OUT SKIN DAMAGED IAW B-727 SRM 55-20-3 FIG 4. FABRICATED REPAIR DOUBLER IAW B-727 SRM 5 5-20-3 FIGURE 4. INSTALLED REPAIR DOUBLER AT RIGHT ELEVATOR LOWER SKIN STATION 35.55 IAW B-727 SRM 55-20-3 FIGURE 4. E LEVATOR REBALANCING NOT REQUIRED IAW B-727 SRM 51-80-7, ELEVATOR MOMENT 120.12, REPAIR MOMENT .48 LBS, NEW ELEVATOR MOME NT 120.6 IS WITHIN LIMIT IAW B-727 SRM 51-80-7. 2 L 7 3 4F A3WE 2008021300179 20080213 00179 NM 2008 2 13 DHL2007785035 1 20071024 A 5313 STRINGER BOEING 727 727214 138407R NM BS 480-520 S28R CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 FOUND CRACK IN TWO PLACES AT STRINGER 28R BETWEEN BS 480 TO BS 520. CUT OUT STRINGER 28R SECTION AND FABRICATED NEW STR INGER SECTION AND REPAIR SPLICE IAW B-727 SRM 53-10-3 FIGURE 1 AND 53-10-2 FIGURE 9. TREATED AND PRIMED REPAIR PARTS I AW B-727 SRM 51-10-2 AND INSTALLED REPAIR PARTS AT STRINGER 28R BETWEEN BS 480 TO BS 520 IAW B-727 SRM 53-10-3 FIGURE 1 AND 53-10-2 FIGURE 9. 2 L 7 3 4F A3WE 2008021300180 20080213 00180 NM 2008 2 13 DHL2007785036 1 20071023 A 5343 TRUNNION BOEING 727 727214 138407R NM NLG CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 RT NLG TRUNNION AND LOWER CAP BORE HAS PITTING CORROSION. CLEANED RT NLG TRUNNION IAW BSOPM 20-30-05 AFTER FURTHER EVAL UATION FOUND CORROSION ON SUPPORT LOWER CAP IAW B-727 SRM 51-10-6 PARA 3A. REWORKED RT TRUNNION IAW B-727 SRM 53-40-1 F IGURE 2. TRUNNION REWORK FOUND WITHIN LIMIT IAW B-727 SRM 53-40-1 FIGURE 2 TABLE 1. ACCOMPLISHED DYE PENETRANT INSPECT ION IAW SORM 20-20-02, NO CORROSION NOTED. TREATED AND PRIMED TRUNNION CAPS IAW B-727 SRM 51-10-2. FABRICATED NEW BEARIN G HALVES IAW B-727 SRM 53-40-1 FIGURE 2 DETAIL III. ACCOMPLISHED DYE PENETRANT INSPECTION ON BEARING HALVES IAW SOPM 20 -20-02, NO DEFECTS NOTED, CADMIUM PLATED NEW BEARING HALVES IAW B-727 SRM 53-40-1 FIGURE 2. 2 L 7 3 4F A3WE 2008021300181 20080213 00181 NM 2008 2 13 DHL2007785037 1 20071023 A 5343 TRUNNION BOEING 727 727214 138407R NM NLG CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 LT NLG TRUNNION AND LOWER CAP BORE HAS PITTING CORROSION. CLEANED LT NLG TRUNNION AS REQUIRED IAW B-727 MM 12-40-0. CO RROSION FOUND, REQUIRES REPAIR IAW B-727 SRM 53-40-1 FIGURE 2. REAMED LT NLG TRUNNION IAW B-727 SRM 53-40-1 FIGURE 2, TRUNNION REWORKED WITHIN LIMITS IAW B-727 SRM 53-40-1 FIGURE 2 TABLE I. ACCOMPLISHED DYE PENETRANT INSPECTION IAW SOPM 20-20-02, NO CORROSION NOTED. TREATED AND PRIMED TRUNNION CAPS IAW B-727 SRM 51-30-2. FABRICATED NEW BEARING HALVES IA W B-727 SRM 53-40-1 FIGURE 2 DETAIL III. ACCOMPLISHED DYE PENETRANT OF NEW BEARING CAPS IAW SOPM 20-20-02, NO DEFECTS N OTED. CADMIUM PLATED NEW BEARING HALVES IAW B-727 SRM 53-40-1 FIGURE 2. 2 L 7 3 4F A3WE 2008021300182 20080213 00182 NM 2008 2 13 DHL2007785038 1 20071017 A 5322 SHEAR TIE BOEING 727 727214 138407R NM BS 500 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 CORROSION WITH SOME EXFOLIATION ON SHEAR TIE BS 500 BETWEEN STRINGER 28R AND STRINGER 28L. REMOVED CORROSION IAW B-727 SRM 51-10-6, FOUND OUT OF LIMITS IAW B-727 SRM 53-40-1 FIGURE 1 AND 53-10-2 FIGURE 3. CUT OUT SHEAR TIE IAW B-727 SRM 5 1-10-1. FABRICATED NEW SHEAR TIE REPAIR IAW B-727 SRM 53-10-4 FIGURE 11 AND 53-10-2 FIGURE 3. TREATED AND PRIMED PARTS IAW B-727 SRM 51-10-2 AND INSTALLED REPAIR PARTS IAW B-727 SRM 51-30-2 AND 53-10-4 FIGURE 11. 2 L 7 3 4F A3WE 2008021300183 20080213 00183 NM 2008 2 13 DHL2007785039 1 20071031 A 5313 STRINGER SPLICE BOEING 727 727214 138407R NM BS 1000-1015 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 SURFACE CORROSION AT STRINGER 28R CHANNEL, FORWARD AND AFT SPLICES BETWEEN BS 1000 TO BS 1015. REMOVED STRINGER SPLICE IAW B-727 SRM 51-30-2, FABRICATED NEW STRINGER SPLICE IAW B-727 SRM 53-10-2 FIGURE 9, 51-30-5 AND 51-20-1. TREATED AND PRIMED NEW SPLICE IAW B-727 SRM 51-10-2 AND INSTALLED NEW STRINGER SPLICE AT STINGER 28R BETWEEN BS 1000 TO BS 1015 IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008021300187 20080213 00187 NM 2008 2 13 DHL2007785044 1 20071106 A 5322 SHEAR TIE BOEING 727 727214 138407R NM BS 1166 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 SURFACE CORROSION BETWEEN STRINGER 30 AND STRINGER 29R SHEAR TIE BS 1166. REMOVED CORROSION FROM SHEAR TIE IAW B-727 SR M 51-10-6, FOUND CORROSION OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1 AND 53-10-2 FIGURE 5. CUT OUT SHEAR TIE IAW B-7 27 SRM 51-10-2. FABRICATED SHEAR TIE DOUBLER. FABRICATED NEW SHEAR TIE AND FABRICATED RADIUS FILLER IAW B-727 SRM 53 -10-4 FIGURE 13 AND 53-10-2 FIGURE 5. TREATED AND PRIMED PARTS IAW B-727 SRM 51-10-2 AND INSTALLED REPAIR PARTS IAW B-7 27 SRM 53-10-4 FIGURE 13 AND 51-30-2. C 2 L 7 3 4F A3WE 2008021300188 20080213 00188 NM 2008 2 13 DHL2007785045 1 20071031 A 5320 ANGLE BOEING 727 727214 138407R NM BS 910 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 LEFT WHEEL WELL APU SCREEN FORWARD VERTICAL ANGLE HAS CORROSION BS 910. REMOVED NUT PLATES TO GAIN ACCESS IAW B-727 SRM 51-30-2, REMOVED CORROSION IAW B-727 SRM 51-10-6. FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1. REMOVED ANGLE ( BEAM) AND ATTACHED ANGLE IAW B-727 SRM 51-30-2. FABRICATED NEW BEAM ANGLE IAW B-727 SRM 51-30-5 AND 53-10-2 FIGURE 4. TREATED AND PRIMED NEW PART IAW B-727 SRM 51-10-2 AND INSTALLED NEW BEAM ANGLE AND ATTACHED ANGLE AT LEFT WHEEL WELL AP U SCREEN FORWARD VERTICAL ANGLE IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008021300189 20080213 00189 NM 2008 2 13 DHL2007785046 1 20071104 A 5311 FRAME BOEING 727 727214 138407R NM BS 1090 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 SURFACE CORROSION AT BS 1090 ABOVE STRINGER 28R. CUT OUT DAMAGED AREA AT BS 1090 ABOVE STRINGER 28R IAW B-727 SRM 51-40 -3 FIGURE 1. FABRICATED NEW FRAME DOUBLER IAW B-727 SRM 53-10-2 FIGURE 5, SRM 51-30-1 FIGURE 3 AND SRM 51-40-2 FIGURE 1 . HEAT TREATED MATERIAL TO T6 CONDITION IAW ER NR 2-371153-801 REV A. TREATED AND PRIMED REPAIR DOUBLER IAW B-727 SRM 51-10-2. INSTALLED REPAIR DOUBLER AT BS 1090 ABOVE STRINGER 28R IAW B-727 SRM 51-40-3 FIGURE 1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2008021300190 20080213 00190 NM 2008 2 13 DHL2007785047 1 20071017 A 5320 ANGLE BOEING 727 727214 138407R NM BS 480-500 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 FOUND SURFACE CORROSION ON FORWARD PIT FUSELAGE SKIN AT BASE OF INTERCOSTAL BS 480-500 STRINGER 28R. REMOVED CORROSION IAW B-727 SRM 51-10-6, FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1. REMOVED INTERCOSTAL ANGLE IAW B-727 SRM 51-3 0-2. FABRICATED NEW ANGLE IAW B-727 SRM 53-10-2 FIGURE 3 AND 51-20-1. TREATED AND PRIMED NEW ANGLE IAW B-727 SRM 51-10 -2 AND INSTALLED NEW ANGLE AT FORWARD PIT INTERCOSTAL BS 480-500 STRINGER 28R IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008021300194 20080213 00194 NM 2008 2 13 DHL2007785031 1 20071102 A 5754 RIB BOEING 727 727214 138407R NM NR 7 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 NR 7 SLAT INBOARD RIB AND OUTBOARD RIB FOR SLAT INBOARD TRACK ARE CRACKED. REMOVED 2 EACH DAMAGED RIBS FROM NR 7 SLAT I AW B-727 SRM 51-30-2. FABRICATED NEW RIBS IAW B-727 SRM 57-50-2 FIGURE 2 AND 51-20-1. HEAT TREATED NEW RIBS IAW FAS EN GINEERING REPORT NR 2-37153-801 REV A. TREATED AND PRIMED NEW RIBS IAW B-727 SRM 51-10-2. INSTALLED 2 EACH RIBS AT NR 7 SLAT INBOARD TRACK IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008021300198 20080213 00198 NM 2008 2 13 DHL2007742020 1 20071222 A 5330 SKIN BOEING 727 727225 1384077 NM BS 950F-990 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 CORROSION WITH EXFOLIATION, AFT PIT BS 950F + 4" STRINGER 29R. CORROSION FOUND OUT OF LIMIT IAW B-727 SRM 53-10-1 FIGUR E 1. FABRICATED REPAIR DOUBLERS, FABRICATED FILLER IAW EDAE59-1 REV B. INSTALLED REPAIR DOUBLERS AT BS 950F TO BS 970 , BS 970 TO BS 990 STRINGER 29R IAW B-727 SRM 51-30-2 AND EDAE59-1 REV B AND 8110-3 DATED 12-20-07. 2 L 7 3 4F A3WE 2008021200173 20080212 00173 NM 2008 2 12 2008UALA00012 1 20071231 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EEL(S) INOPERATIVE AT SEATS 2J FWD SECT, 23ABC FWD SECT, 48 ABC & 24JK. RELAMPED EMERGENCY LIGHTS. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200179 20080212 00179 CE 2008 2 12 JBG2008F00000 1 20071229 A 3231 FITTING LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP LT MLG LOOSE E JBGA K NONE K FLUID LOSS NR NOT REPORTED 1 SW 11 357LJ 357 P89657 HYDRAULIC PRESSURE LOSS DUE TO LEAKS NOTED AT LT MLG DOOR IB UNLATCH ACTUATOR SHUTTLE VALVE FITTINGS, AND THE RT IB MAIN GEAR DOOR ACTUATOR FITTINGS DUE TO INSUFFICIENT TORQUE AND BAD SEALS. A LOOSE FITTING WAS ALSO NOTED ON THE RT MLG ACT UATOR RETRACT LINE. (PIC) DECLARED AN ONBOARD EMERGENCY AND DIVERTED TO NEAREST SUITABLE AIRPORT, WITH NO FURTHER COMPL ICATIONS. (K) 2 L 7 2 4F 4 F A10CE E6WE 2008021200180 20080212 00180 EA 2008 2 12 A6WA200740705 1 20071210 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 432AW 7257 CRACK SUSPECTED ON AC CONNECTOR BOX. CRACK CONFIRMED BY EDDY CURRENT INSPECTION. INTERCOSTAL AND RECEPTACLE SUPPORT RE PLACED IAW SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200215 20080212 00215 EA 2008 2 12 A6WA200740711 1 20071228 A 5240 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE SERVICE DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 MINOR CORROSION UNDER SERVICE DOOR LOWER SEAL RETAINER. CORROSION REMOVED IAW SRM 51-21-06 WITHIN LIMIT SRM 52-00-31, F IG 101. MATERIAL REMOVED .003 INCH ORIGINAL THICKNESS .040. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021300146 20080213 00146 NM 2008 2 13 2007785014 1 20071101 A 5313 STRINGER BOEING 727 727214 138407R NM BS 720E S26R CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 INTERGRANULAR CORROSION NOTED ON STRINGER 26R AT BS 720E + 19". CUT OUT DAMAGED SECTION IAW B-727 SRM 53-10-2 FIGURE 1. FABRICATED REPAIR FILLER. FABRICATED REPAIR SPLICE IAW B-727 SRM 53-10-3 FIGURE 1 AND SRM 53-10-2 FIGURE 9. TREATED AND PRIMED REPAIR PARTS IAW B-727 SRM 51-10-2 AND INSTALLED REPAIR PARTS AT BS 720E + 19" STRINGER 26R IAW B-727 SRM 53- 10-3 FIGURE 1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2008021300149 20080213 00149 NM 2008 2 13 DHL2007785007 1 20071017 A 5322 SHEAR TIE BOEING 727 727214 138407R NM BS 520 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 SURFACE CORROSION ON FORWARD PIT SHEAR TIE BS 520 BETWEEN STRINGER 28L AND 28R. REMOVED FASTENERS IN AREA TO GAIN ACCES S IAW B-727 SRM 51-30-2. REMOVED CORROSION IAW B-727 SRM 51-10-6, FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1. FABRICATED SHEAR TIE REPAIR, CUT OUT DAMAGED SHEAR TIE IAW B-727 SRM 53-10-2 FIGURE 3 AND 53-10-4 FIGURE 11. TREATED AN D PRIMED PARTS IAW B-727 SRM 51-10-2. INSTALLED REPAIR SHEAR TIE AT FORWARD PIT BS 520 BETWEEN STRINGER 28 L AND 28R IA W B0727 SRM 51-30-2 AND 53-10-4 FIGURE 11. 2 L 7 3 4F A3WE 2008021300150 20080213 00150 NM 2008 2 13 DHL2007785008 1 20071017 A 5322 SHEAR TIE BOEING 727 727214 138407R NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 SURFACE CORROSION ON FORWARD PIT SHEAR TIE BS 520 BETWEEN STRINGER 28L AND 28R. REMOVED FASTENERS IN AREA TO GAIN ACCES S IAW B-727 SRM 51-30-2, REMOVED CORROSION IAW B-727 SRM 51-10-6, FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1. F ABRICATED SHEAR TIE REPAIR, CUT OUT DAMAGED SHEAR TIE IAW B-727 SRM 53-10-2 FIGURE 3 AND 53-10-4 FIGURE 11. TREATED AND PRIMED PARTS IAW B-727 SRM 51-10-2. INSTALLED REPAIR SHEAR TIE AT FORWARD PIT BS 520 BETWEEN STRINGER 28 L AND 28R IAW B727 SRM 51-30-2 AND 53-10-4 FIGURE 11. 2 L 7 3 4F A3WE 2008021300157 20080213 00157 NM 2008 2 13 DHL2007785017 1 20071106 A 5320 ANGLE BOEING 727 727214 138407R NM BS 1050 GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 AFT CARGO COMPARTMENT FRAME AT BS 1050 HAS A GOUGE ABOVE STRINGER 27R. CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE IA W B-727 SRM 53-10-2 FIGURE 5 AND SRM 51-40-3 FIGURE 1. HEAT TREATED ANGLE TO T6 CONDITION IAW FAS ENGINEERING REPORT NR 2-37153-801 REV A. TREATED AND PRIMED REPAIR PARTS AND AREA IAW B-727 SRM 51-10-2 AND INSTALLED REPAIR AT FRAME STATIO N 1050 ABOVE STRINGER 27R IAW B-727 SRM 51-40-3 FIGURE 1 AND 51-30-2. 2 L 7 3 4F A3WE 2008021300166 20080213 00166 NM 2008 2 13 DHL2007742014 1 20071120 A 5310 TEAR STRAP BOEING 727 727225 1384077 NM BS 1148 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AFT CARGO COMPARTMENT TEAR STRAP AT BS 1148 AT STRINGER 26R TO 25R IS EXFOLIATED. CUT OUT DAMAGED TEAR STRAP SECTION, F ABRICATED TEAR STRAP REPAIR IAW B-727 SRM 53-30-4 FIGURE 9 AND 51-10-1. TREATED AND PRIMED PART IAW B-727 SRM 51-10-2 A ND INSTALLED REPAIR STRAP AT AFT CARGO COMPARTMENT BS 1148 STRINGERS 26R TO 25R IAW B-727 SRM 53-30-4 FIGURE 9 AND 51-30 -2. 2 L 7 3 4F A3WE 2008021300171 20080213 00171 NM 2008 2 13 DHL2007742019 1 20071204 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 950A-950B CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 FOUND STRINGER 29L BS 950 - 950D CORRODED. REMOVED CORROSION FROM STRINGER 29L BS 950-950D IAW B-727 SRM 51-10-6, OUT B OARD FLANGE BS 950A-950B FOUND OUT OF LIMIT, BS 950B-950D FOUND WITHIN LIMIT, IAW B-727 SRM 53-10-1 FIGURE 1 AND SRM 53- 10-2 FIGURE 5. FABRICATED REPAIR DOUBLER FOR OUTBOARD FLANGE IAW EDAE59-3 REV IR. TRIMMED FRAME SHEAR TIE AT BS 950A A ND 950B FOR REPAIR ACCESS IAW EDAE59-2 REV IR. INSTALLED STRINGER REPAIR AT BS 950A TO 950B IAW EDAE59-2 REV IR. FABRI CATED SHEAR TIE REPAIRS FOR FRAMES BS 950A TO 950B, FABRICATED RADIUS FILLERS. FABRICATED REPAIR SHIMS IAW B-727 SRM 5 3-10-4 FIGURE 15 AND SRM 53-10-2 FIGURE 5. INSTALLED REPAIR IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008021300176 20080213 00176 NM 2008 2 13 DHL2007785032 1 20071105 A 5313 STRINGER BOEING 727 727214 138407R NM BS 1180 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 AFT PIT TAIL PIECE OF STRINGER 25R BS 1180 AT SHEAR TIE CRACKED AND EXFOLIATED. REMOVED STRINGER FITTING AT BS 1183 STR INGER 25R IAW B-727 SRM 51-30-2. CUT OUT STRINGER SECTION AT BS 1160 IAW B-727 SRM 53-10-3 FIGURE 1. FABRICATED NEW ST RINGER SECTION AND REPAIR SPLICE IAW B-727 SRM 53-10-3 FIGURE 1 AND 53-10-2 FIGURE 9. TREATED AND PRIMED AREA IAW B-727 SRM 51-10-2. INSTALLED REPAIR PARTS AT BS 1180 AND STRINGER 25R IAW B-727 SRM 53-10-3 FIGURE 1. REINSTALLED STRINGER FITTING IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008021300177 20080213 00177 NM 2008 2 13 DHL2007785033 1 20071101 A 5320 ANGLE BOEING 727 727214 138407R NM BS 1217 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 AFT AIRSTAIRS CUT OUT AREA, LOWER SPLICE ANGLE AT BS 1217 RBL 10 IS CRACKED. REMOVED CRACKED SPLICE ANGLE IAW B-727 SRM 51-30-2, FABRICATED NEW ANGLE IAW B-727 SRM 53-10-2 FIGURE 2, 51-10-3, AND 51-20-1. TREATED AND PRIMED NEW SPLICE ANGL E IAW B-727 SRM 51-10-2 AND INSTALLED NEW SPLICE ANGLE AT AFT AIRSTAIRS CUTOUT AREA BS 1217 RBL10 IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008021300195 20080213 00195 NM 2008 2 13 DHL2007785040 1 20071030 A 5310 BEAM BOEING 727 727214 138407R NM BS 1183 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 SURFACE CORROSION AT BS 1183 LOWER HORIZONTAL "I" BEAM INBOARD SIDE JUST AFT OF OUT FLOW VALVE, STRINGER 26R. REMOVED C ORROSION IAW B-727 SRM 51-10-6, CORROSION FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1, REMOVED BEAM IAW B-727 SRM 51-30-2, FABRICATED NEW BEAM IAW B-727 SRM 51-30-5 AND 53-10-2 FIGURE 5. TREATED AND PRIMED NEW BEAM IAW B-727 SRM 51- 10-2. INSTALLED NEW BEAM AT BS 1183 LOWER HORIZONTAL STRINGER 26R IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008021400037 20080214 00037 NM 2008 2 14 ZZDA2008065 1 20070817 A 5330 SKIN BOEING 737 7377BD 1384511 NM BS 777 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 286AT 34480 SCRATCH AND DENT FOUND ON LEFT AFT FUSELAGE AFT OF LEFT WING. INSTALLED AN EXTERNAL PERMANENT REPAIR DOUBLER AT STA 777 , LONGERON 21-L, IAW B737-700 SRM 53-00-01 FIG 201 REPAIR NR 1. 2 L 7 2 4F RT A16WE 2008021400059 20080214 00059 NM 2008 2 14 NWAA074396308 1 20071229 A 5320 WEB BOEING 747 747451 1384940 NM BS 940 PUNCTURED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 668US 24223 DURING "M" CHECK, FOUND PUNCTURE IN WEB BELOW UPPER DECK FLOOR AT BS 940 RBL 34. REPAIRED PER EA 63-210899. 2 L 7 4 4F RT A20WE 2008021300156 20080213 00156 NM 2008 2 13 DHL2007785016 1 20071104 A 5311 FRAME BOEING 727 727214 138407R NM BS 1030 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 DENT AT BS 1030 FRAME, JUST OUTBOARD OF STRINGER 27R. REMOVED FASTENERS FROM BS 1030 IAW B-727 SRM 51-30-2, CUT OUT DAM AGED AREAS AND FABRICATED REPAIR ANGLE DOUBLER IAW B-727 SRM 51-40-3 FIGURE 1 AND SRM 53-10-2 FIGURE 5. HEAT TREATED RE PAIR ANGLE TO T6 CONDITION IAW FAS ENGINEERING REPORT NR 2-37153-801 REV A, TREATED AND PRIMED PARTS IAW B-72 SRM 51-10- 2. INSTALLED REPAIR ANGLE AT BS 1030 FRAME STRINGER 27R IAW B-727 SRM 51-30-2 AND 51-40-2 FIGURE 1. 2 L 7 3 4F A3WE 2008021300162 20080213 00162 NM 2008 2 13 DHL2007785022 1 20071029 A 5322 SHEAR TIE BOEING 727 727214 138407R NM BS 1130 S29L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 SURFACE CORROSION AT BS 1130 LEFT OF STRINGER 29L. REMOVED FASTENERS FOR CORROSION REMOVAL AT BS 1130 BETWEEN STRINGER 29L AND 28L AT SHEAR TIE AREA IAW B-727 SRM 51-30-2. REMOVED CORROSION AT FRAME, WITHIN LIMIT IAW B-727 SRM 53-10-1 FIG URE 1, 53-10-2, AND 51-10-6. FOUND SHEAR TIE AFT ANGLE SUPPORT CORROSION OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1. REMOVED SHEAR TIE AFT ANGLE SUPPORT AT BS 1130 BETWEEN STRINGER 29L AND 28L IAW B-727 SRM 51-30-2. FABRICATED SHEAR TI E SUPPORT IAW B-727 SRM 53-10-2 AND 51-30-5. TREATED AND PRIMED PARTS AND AREA IAW B-727 SRM 51-10-2. INSTALLED SHEAR TIE SUPPORT AT BS 1130 BETWEEN STRINGER 29L AND 28L AND FASTENERS IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008021300175 20080213 00175 NM 2008 2 13 DHL2007785030 1 20071012 A 5532 SKIN BOEING 727 727214 138407R NM VERTICAL STAB BULGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 VERTICAL STABILIZER RIGHT SIDE ABOVE UPPER RUDDER HAS BULGING SKIN (FIN WL 168 AT FIN STA 305). CUT OUT DAMAGE AREA AND FABRICATED REPAIR DOUBLER AND REPAIR FILLER IAW B-727 SRM 55-30-3 FIGURE 6 AND 55-30-2 FIGURE 1. TREATED AND PRIMED PA RTS IAW B-727 SRM 51-10-2 AND INSTALLED REPAIR PARTS AT VERTICAL STABILIZER RIGHT SIDE ABOVE UPPER RUDDER TAB IAW B-727 SRM 51-30-2 AND 55-30-3 FIGURE 6. 2 L 7 3 4F A3WE 2008021300191 20080213 00191 NM 2008 2 13 DHL2007785048 1 20071101 A 5313 STRINGER BOEING 727 727214 138407R NM BS 560 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 FOUND CORROSION ON STRINGER 28R BS 560. REMOVED INTERCOSTALS FROM BS 540 TO BS 580 STRINGER 28R FOR ACCESS IAW B-727 SR M 51-30-2. CUT OUT DAMAGED SECTION OF STRINGER DIMENSION 17.75" IAW B-727 SRM 53-10-13 FIGURE 1. FABRICATED NEW STRING ER SECTION IAW B-727 SRM 53-10-3 FIGURE 1 AND 53-10-2 FIGURE 9. TREATED AND PRIMED REPAIR PARTS IAW B-727 SRM 51-10-2 A ND INSTALLED REPAIR PARTS IAW B-727 SRM 51-30-2 AND 53-10-3 FIGURE 1. INSTALLED INTERCOSTALS IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008021500041 20080215 00041 NM 2008 2 15 2007UALA03155 1 20070810 A 3510 OXYGEN SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 CREW OXYGEN SYSTEM LOW. INSPECTED AND LEAK CHECKED ALL 3 MASKS. NOTED OBSERVER MASK INCORRECTLY STOWED AND POSSIBLE TE ST BEING INADVERTENTLY PUSHED. SERVICED O2 TO 1800. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500055 20080215 00055 NM 2008 2 15 2007UALA05299 1 20071219 A 2910 X6719520854 HYDRAULIC SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HMG FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 HMG FAILED TEST. HMG FAILURE (SHOP RECORDS INDICATED NO CLEAR CAUSE, ONLY THAT R22 AND D4 CIRCUITS WERE REPLACED). REP LACED HMG, OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021500056 20080215 00056 NM 2008 2 15 2008UALA00004 1 20071231 A 5210 69694301 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 FORWARD GALLEY DOOR, FWD FRAME IS CRACKED AT LOWER CORNER OTBD FASTENER HOLES. MAJOR REPAIR: REMOVED OLD FRAME AND REP LACED WITH NEW SPLICE FRAME REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500057 20080215 00057 NM 2008 2 15 2008UALA00006 1 20071231 A 5210 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 DOOR 1L LOWER FWD FRAME CRACKED UNDER STOP FITTING. MAJOR REPAIR: REPLACED FRAME, 3 EACH LINER ATTACH BRACKETS, FORWAR D AND AFT STOP FITTINGS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021300144 20080213 00144 NM 2008 2 13 DHL2007785012 1 20071023 A 5313 STRINGER BOEING 727 727214 138407R NM BS 695 DAMAGED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 785AT 21691 MISDRILLED HOLE IN STRINGER 28R BS 695. REMOVED FASTENERS AT BS 695 STRINGER 28R, CUT OUT DAMAGED AREA IAW B-727 SRM 53 -10-3 FIGURE 1. FABRICATED FILLER. FABRICATED SPLICES 2 EACH IAW B-727 SRM 53-10-3 FIGURE 1 AND 53-10-2 FIGURE 9. TRE ATED AND PRIMED NEW PARTS IAW B-727 SRM 51-10-2 AND INSTALLED FILLER AND SPLICES 2 EACH IAW B-727 SRM 53-10-3 FIGURE 1. 2 L 7 3 4F A3WE 2008021300151 20080213 00151 NM 2008 2 13 2007785015 1 20071027 A 5313 STRINGER BOEING 727 727214 138407R NM BS 720F-740 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 FORWARD PIT BS 720F TO BS 740 STRINGER 27R SHOWS CORROSION. REMOVED CORROSION AT BS 720F TO BS 740 STRINGER 27R IAW B-7 27 SRM 51-10-6, CORROSION FOUND OUT OF LIMIT IAW B-727 SRM 53-10-1 FIGURE 1. CUT OUT DAMAGED STRINGER IAW B-727 SRM 53- 10-3 FIGURE 1. FABRICATED FILLER. FABRICATED REPAIR CHANNEL IAW B-727 SRM 53-10-3 FIGURE 1 AND SRM 53-10-2 FIGURE 9. INSTALLED STRINGER REPAIR AT BS 720F TO BS 740 STRINGER 27R IAW B727 SRM 53-10-3 FIGURE 1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2008021300158 20080213 00158 NM 2008 2 13 DHL2007785018 1 20071101 A 5322 SHEAR TIE BOEING 727 727214 138407R NM BS 950B CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 SURFACE CORROSION AT SHEAR TIE, BS 950B LEFT SIDE OF STRINGER 30. REMOVED FASTENERS AT BS 950B LEFT SIDE OF STRINGER 30 IAW B-727 SRM 51-30-2. REMOVED CORROSION AT FRAME SHEAR TIE IAW B-727 SRM 51-10-6. CORROSION FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1 AND SRM 53-10-2 FIGURE 5, CUT OUT DAMAGE AREA IAW B-727 SRM 53-10-4 FIGURE 11. FABRICATED SH EAR TIE REPAIR DOUBLER IAW B-727 SRM 53-10-4 FIGURE 11 AND SRM 53-10-2 FIGURE 5. HEAT TREATED REPAIR DOUBLER TO T6 COND ITION IAW ER NR 2-37153-801 REV A, TREATED AND PRIMED SHEAR TIE REPAIR AND AREA IAW B-727 SRM 51-10-2. INSTALLED SHEAR TIE REPAIR AT BS 950B LEFT SIDE OF STRINGER 30 IAW B-727 SRM 51-30-2 AND SRM 53-10-4 FIGURE 11. 2 L 7 3 4F A3WE 2008021300160 20080213 00160 NM 2008 2 13 DHL2007785020 1 20071106 A 5322 SHEAR TIE BOEING 727 727214 138407R NM BS 1166 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 SURFACE CORROSION AT LEFT STRINGER 29L BS 1166 SHEAR TIE ATTEND. REMOVED CORROSION IAW B-727 SRM 51-10-6, FOUND CORROSI ON OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1 AND 53-10-2 FIGURE 5. CUT OUT SHEAR TIE IAW B-727 SRM 51-10-1 AND 53-10 -4 FIGURE 11. FABRICATED REPAIR DOUBLER IAW B-727 SRM 53-10-4 FIGURE 11 AND 53-10-2 FIGURE 5. TREATED AND PRIMED PARTS IAW B-727 SRM 51-10-2 AND INSTALLED REPAIR PARTS IAW B-727 SRM 53-10-4 FIGURE 11 AND 51-30-2. 2 L 7 3 4F A3WE 2008021300168 20080213 00168 NM 2008 2 13 DHL2007742016 1 20071120 A 5330 SKIN BOEING 727 727225 1384077 NM BS 615 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 EXTERIOR FUSELAGE SURFACE BS 615 ON STRINGER 27L 1 SKIN STRINGER FASTENER HOLE IS CRACKED, VERIFIED WITH HFEC. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND REPAIR FILLER IAW B-727 SRM 53-30-2 FIGURE 2 AND 53-30-3 FIGURE 3. TREATED AND PRIMED REPAIR PART IAW B-727 SRM 51-10-2 AND INSTALLED REPAIR PARTS AT EXTERNAL FUSELAGE BS 615 ON STRINGER 27L IAW B-727 SRM 53-30-3 FIGURE 3 AND 51-30-2. 2 L 7 3 4F A3WE 2008021300170 20080213 00170 NM 2008 2 13 DHL2007742018 1 20071119 A 5311 FRAME BOEING 727 727225 1384077 NM BS 950D DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 DENT AT FRAME BS 950D ABOVE STRINGER 26L AFT PIT. CUT OUT DAMAGE AREA DIMENSION IAW B-727 SRM 53-10-4 FIGURE 1. FABRIC ATED NEW FRAME REPAIR IAW FORM FAS 1115 REV 11. LOCATED AND DRILLED NEW FRAME REPAIR IAW B-727 SRM 53-10-4 FIGURE 1 AND 51-30-5. TREATED AND PRIMED NEW FRAME IAW B-727 SRM 51-10-2 AND INSTALLED NEW FRAME REPAIR AT BS 950D IAW B-727 SRM 51 -30-2. 2 L 7 3 4F A3WE 2008021300173 20080213 00173 NM 2008 2 13 DHL2007785028 1 20071019 A 5754 STRUCTURE BOEING 727 727214 138407R NM KRUEGER FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 NR 4 KRUEGER FLAP LOWER INBOARD END CRACKED WING STATION 131. CUT OUT CRACKED AREA, FABRICATED REPAIR PLATE, REPAIR FIL LER AND REPAIR ANGLE IAW B-727 SRM 57-50-3 FIGURE 3. TREATED AND PRIMED PARTS IAW B-727 SRM 51-10-2 AND INSTALLED REPA IR PARTS AT NR 4 KRUEGER FLAP LOWER INBOARD END WING STATION 131 IAW B-727 SRM 57-50-3 FIGURE 3 AND 51-30-2. 2 L 7 3 4F A3WE 2008021300174 20080213 00174 NM 2008 2 13 DHL2007785029 1 20071105 A 5754 SKIN BOEING 727 727214 138407R NM NR 7 SLAT DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 PROTRUDING DENT ON NR 7 SLAT INBOARD UPPER SURFACE WING STATION 601. EVALUATED DENT AND FOUND OUT OF LIMITS IAW B-727 S RM 57-50-1 FIGURE 2. REMOVED NR 7 SLAT ACCESS PANELS IAW B-727 SRM 51-30-2, CUT OUT DAMAGED AREA AND COVE SKIN IAW B-72 7 SRM 51-10-1. FABRICATED REPAIR DOUBLER. FABRICATED COVE SKIN DOUBLER AND FABRICATED REPAIR SPACERS IAW B-727 SRM 57- 50-3 FIGURE 1 AND 57-50-2 FIGURE 2. TREATED AND PRIMED PARTS IAW B-727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B-727 S RM 57-50-3 FIGURE 1 AND 51-30-2. REINSTALLED NR 7 SLAT ACCESS PANELS IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008021300178 20080213 00178 NM 2008 2 13 DHL2007785034 1 20071102 A 5320 INTERCOSTAL BOEING 727 727214 138407R NM BS 540-560 S28R DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 FORWARD CARGO COMPARTMENT INTERCOSTAL AT STRINGER 28R BETWEEN BS 540 AND BS 560 HAS ELONGATED HOLES AT BOTTOM. REMOVED INTERCOSTAL FROM BS 540 TO BS 560 STRINGER 28R IAW B-727 SRM 51-30-2. FABRICATED NEW INTERCOSTA IAW B-727 SRM 53-10-2 F IGURE 3 AND 51-20-1. TREATED AND PRIMED NEW INTERCOSTAL IAW B-727 SRM 51-10-2 AND INSTALLED NEW INTERCOSTAL AT FORWARD CARGO COMPARTMENT BETWEEN BS 540 AND BS 560 STRINGER 28R IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008021300184 20080213 00184 NM 2008 2 13 DHL2007785041 1 20071105 A 5322 SHEAR TIE BOEING 727 727214 138407R NM BS 1166 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 SURFACE CORROSION AT STRINGER 25R, BS 1166 SHEAR TIE AFT END. REMOVED CORROSION IAW B-727 SRM 51-10-6, FOUND CORROSION OUT OF LIMITS IAW B-727 SRM 53-10-1. REMOVED SHEAR TIE IAW B-727 SRM 51-30-2. FABRICATED NEW SHEAR TIE IAW B-727 SRM 5 3-10-2 FIGURE 5 AND 53-10-4 FIGURE 11. TREATED AND PRIMED NEW SHEAR TIE IAW B-727 SRM 51-10-2. INSTALLED NEW SHEAR TIE IAW B-727 SRM 53-10-4 FIGURE 11 AND 51-30-2. 2 L 7 3 4F A3WE 2008021300185 20080213 00185 NM 2008 2 13 DHL2007785042 1 20071105 A 5340 ATTACH FITTING BOEING 727 727214 138407R NM BS 1183 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 CORROSION WITH EXFOLIATION AT BS 1183, STRINGER 17R ATTACHED FITTING. REMOVED ATTACH FITTING AT STRINGER 17R BS 1183 IA W B-727 SRM 51-30-2. FABRICATED NEW ATTACH FITTING IAW BOEING DRAWING NR 65-24276 AND J C NR EC-00596-001. TREATED AND PRIMED NEW FITTING IAW B-727 SRM 51-10-2 AND INSTALLED NEW FITTING AT BS 1183 STRINGER 17R IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008021300186 20080213 00186 NM 2008 2 13 DHL2007785043 1 20071027 A 5322 SHEAR TIE BOEING 727 727214 138407R NM BS 1166 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 SURFACE CORROSION AT RIGHT STRINGER 27L BS 1166 SHEAR TIE AFT SIDE. REMOVED CORROSION AT BS 1166 STRINGER 27L IAW B-727 SRM 51-10-6 FOUND CORROSION OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1. REMOVED PREVIOUS SHEAR TIE IAW B-727 SRM 51- 30-2. FABRICATED NEW SHEAR TIE IAW B-727 SRM 53-10-4 FIGURE 15, 53-10-2 FIGURE 5 AND INSTALLED NEW SHEAR TIE IAW B-727 SRM 53-10-4 FIGURE 15 AND 51-30-2. 2 L 7 3 4F A3WE 2008021300192 20080213 00192 NM 2008 2 13 DHL2007785049 1 20071016 A 5347 SEAT TRACK BOEING 727 727214 138407R NM BS 480-700 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 MAIN CABIN SEAT TRACKS LBL 45 BS 480-BS 690 HAVE LIGHT CORROSION. REMOVED CABIN FLOOR PANELS BETWEEN BS 480 AND 700 LBL 22 LBL65-LBL22 FOR ACCESS IAW B-727 MM 53-30-11. REMOVED SEAT TRACK OUT OF LIMITS FROM BS 480 TO 700 LBL45 IAW B-727 S RM 51-30-2. FABRICATED NEW SEAT TRACK IAW B-727 SRM 53-10-5 FIGURE 1 AND 53-10-2 FIGURE 7. TREATED AND PRIMED PARTS IA W B-727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B-727 SRM 51-30-2. INSTALLED FLOORBOARD PANELS IAW B-727 MM 53-20-11. 2 L 7 3 4F A3WE 2008021300193 20080213 00193 NM 2008 2 13 DHL2007785027 1 20071029 A 5754 RIB BOEING 727 727214 138407R NM NR 5 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 CRACK INDICATION ON RIGHT WING NR 5 SLAT OUTBOARD AND INBOARD ACTUATOR ROD END MOUNT BRACKET, PREVIOUSLY REPAIRED. REMO VED SLAT ACCESS PANELS TO GAIN ACCESS IAW B-727 SRM 51-30-2. REMOVED CRACKED RIBS IAW B-727 SRM 51-30-2. LOCATED AND D RILLED NEW RIBS IAW B-727 SRM 51-30-5 AND 57-50-2 FIGURE 2. TREATED AND PRIMED BARE METAL AREAS IAW B-727 SRM 51-10-2. INSTALLED NEW RIBS IAW B-727 SRM 51-30-2 AND REINSTALLED ACCESS PANELS AT NR 5 SLAT IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008021400068 20080214 00068 WP 2008 2 14 UPS08851645 1 20071231 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1973 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 TAILCONE LOWER NAV LIGHT CUTOUT HAS POPPED RIVET, CORROSION AND BARE METAL ON FRAME. REPAIRED TAILCO NE FRAME AND DOUBLER AT STA 1973 IAW EA 008-5310-01-A1280 AND RAA DC8-53-20677. 2 L 7 4 4F RT 4A25 2008021400176 20080214 00176 WP 2008 2 14 G60A200800011 1 20070208 A 5730 SKIN DOUG DC10 DC1030F 3023504 WP LT WING CORRODED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 607GC 46978 FOUND CORROSION LEFT WING DROOP LEADING EDGE INBD UPPER SKIN. 2 L 7 3 4F RT A22WE 2008021500046 20080215 00046 NM 2008 2 15 2007UALA03917 1 20070925 A 3350 20131A BATTERY PACK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 302UA 23643 MID CABIN EMERGENCY LIGHTS INOP FROM SEAT ROW 11ABC TO 16ABC. REPLACED BATTERY PACK AND CHARGER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021900033 20080219 00033 NM 2008 2 19 QXEA200801837 1 20071125 A 5720 PANEL BOMBDR DHC8 DHC8402 1390042 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - CORROSION AROUND FASTENER HOLE ON PANEL 524CT APPERATURE OUTBOARD END. BLENDED OUT CORROSION, INSPECT ED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. 2 H 7 2 4T RT A13NM 2008021900036 20080219 00036 NM 2008 2 19 QXEA200801820 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 425-428 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - RIGHT INBOARD SEAT TRACK NR 13 HAS PITTING CORROSION AT APPROXIMATELY STA 425.00 TO 428.00. BLENDED O UT CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. 2 H 7 2 4T RT A13NM 2008021500077 20080215 00077 NM 2008 2 15 QXEA200801808 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 574 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - SEAT TRACK NR 8 IS CORRODED AT APPROXIMATELY X574. REMOVED CORROSION, INSPECTED, WITHIN LIMITS AND NO CRACK NOTED. RESTORED ALODINE TREATMENT TO BLENDED AREA. 2 H 7 2 4T RT A13NM 2008021900124 20080219 00124 NM 2008 2 19 QXEA200801826 1 20071125 A 5310 RIB BOMBDR DHC8 DHC8402 1390042 NM BATTERY BAY CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - BATTERY COMPARTMENT 4TH VERTICAL RIB HAS DAMAGE AND POSSIBLE CRACK COUNT FROM THE FRONT TO AFT. BLENDE D OUT DAMAGED AREA, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. RESTORED FINISH TO BLENDED AREA. 2 H 7 2 4T RT A13NM 2008021500058 20080215 00058 NM 2008 2 15 2008UALA00007 1 20071231 A 5241 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 FWD GALLEY DOOR CUTOUT, AFT FRAME IS CRACKED AT 2ND STOP FITTING FROM TOP. MAJOR REPAIR: REMOVED DAMAGE. INSTALLED RE PAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500060 20080215 00060 NM 2008 2 15 2008UALA00009 1 20071231 A 5320 ATTACH ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 FWD GALLEY DOOR CUTOUT INTERCOSTAL ATTACH ANGLE CRACKED BETWEEN BS 277 & 294.5 AND BETWEEN STRINGERS 12R & 13R. MAJOR R EPAIR: REMOVED DAMAGED ANGLE AND REPLACED WITH NEW ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021900140 20080219 00140 EA 2008 2 19 QXEA200802061 1 20071215 A 5510 LUG CNDAIR CL600 CL6002C10 1390015 EA HORIZONTAL STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT HORIZONTAL STAB HINGE ANTI-ROTATION LUG APPEARS TO HAVE DAMAGE BEYOND PREVIOUS BLEND REPAIR, DUE T O HINGE HARDWARE ROTATION. BLENDED OUT DAMAGE, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. ROTOPEENED AND R ESTORED FINISH TO BLENDED AREA. 2 L 7 2 4F RT A21EA 2008021900142 20080219 00142 NM 2008 2 19 QXEA200801806 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - INSIDE OF SEAT TRACK NR 7 IS CORRODED FROM APPROXIMATELY X452 TO X464. REMOVED CORROSION BY BLENDING. BLENDED AREA INSPECTED AND REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021900143 20080219 00143 NM 2008 2 19 QXEA200801860 1 20071125 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - FUSELAGE SKIN IS CORRODED AT NR 3 COMM ANTENNA. BLENDED OUT CORROSION, INSPECTED BLEND, WITHIN LIMITS NO CRACKS NOTED. RESTORED FINISH TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021900145 20080219 00145 NM 2008 2 19 QXEA200801815 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 261 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 RIGHT INBOARD SEAT TRACK NR 13 HAS GOUGE AT APPROXIMATELY STA 261.00. BLENDED OUT DAMAGE AT GOUGE, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. 2 H 7 2 4T RT A13NM 2008021900148 20080219 00148 NM 2008 2 19 QXEA200801839 1 20071125 A 5260 TRACK BOMBDR DHC8 DHC8402 1390042 NM AIRSTAIR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - LIGHT SURFACE CORROSION FOUND ON TOP SURFACE OF AIRSTAIR TRACK APPROXIMATELY 6 INCHES FROM LEFT OUTBOAR D SEAT TRACK NR 3 STATION X640 TO X643. BLENDED AWAY LIGHT CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS N OTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021900149 20080219 00149 NM 2008 2 19 QXEA200801840 1 20071125 A 5730 SKIN BOMBDR DHC8 DHC8402 1390042 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - CORROSION AROUND FASTENER HOLES ON FUEL PANEL 524AT APPERATURE INBOARD END. BLENDED OUT CORROSION ARO UND FASTENER HOLES. INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. 2 H 7 2 4T RT A13NM 2008021900150 20080219 00150 NM 2008 2 19 QXEA200801817 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 280 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - RIGHT INBOARD SEAT TRACK NR 13 HAS CORROSION AT APPROXIMATELY STA 280.00. REMOVED CORROSION, INSPECTE D, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. 2 H 7 2 4T RT A13NM 2008021900151 20080219 00151 NM 2008 2 19 QXEA200801819 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 401-403 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - RIGHT INBOARD SEAT TRACK NR 13 HAS PITTING AT APPROXIMATELY STA 401.00 TO 403.00. BLENDED OUT CORROSIO N, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. 2 H 7 2 4T RT A13NM 2008021900159 20080219 00159 NM 2008 2 19 QXEA200801809 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 167-169 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - RIGHT INBOARD SEAT TRACK NR 12 HAS PITTING AT APPROXIMATELY STA 167.00 TO 169.00. BLENDED OUT PITTING, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. RESTORED ALODINE TREATMENT TO BLENDED AREA. 2 H 7 2 4T RT A13NM 2008021900161 20080219 00161 NM 2008 2 19 QXEA200801812 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 620 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - SEAT TRACK NR 8 IS CORRODED AT APPROXIMATELY X620. BLENDED OUT CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. RESTORED ALODINE TREATMENT TO BLENDED AREA. 2 H 7 2 4T RT A13NM 2008021900174 20080219 00174 EA 2008 2 19 QXEA200801957 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 661 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT RAIL SEAT TRACK HAS GOUGE AT APPROXIMATELY 661.00. REMOVED GOUGE BY BLENDING SEAT TRACK, INSPECT ED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TO BLENDED AREA. 2 L 7 2 4F RT A21EA 2008021900176 20080219 00176 EA 2008 2 19 QXEA200802065 1 20071215 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - AIRCRAFT EXTERNAL SKIN CORRODED UNDER AFT ANTENNA. BLENDED OUT CORROSION FROM AFFECTED AREA OF SKIN UN DER ADF ANTENNA IAW REO 670-53-31-090. HFEC INSPECTED NO CRACKS NOTED. RESTORED FINISH TO BLENDED AREA. 2 L 7 2 4F RT A21EA 2008021900188 20080219 00188 NM 2008 2 19 QXEA200801821 1 20071125 A 5320 THRESHOLD BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - SUSPECTED CORROSION UNDER AFT PASSENGER ENTRYWAY DOOR THRESHOLD (INBOARD). REMOVED LIGHT SURFACE CORRO SION FROM THRESHOLD, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. RESTORED FINISH TO WORKED AREA. 2 H 7 2 4T RT A13NM 2008021900189 20080219 00189 NM 2008 2 19 QXEA200801838 1 20071125 A 5720 STRUCTURE BOMBDR DHC8 DHC8402 1390042 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - CORROSION AROUND FASTENER HOLE ON PANEL 524CT APERTURE INBOARD END. BLENDED OUT CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. 2 H 7 2 4T RT A13NM 2008021900261 20080219 00261 NM 2008 2 19 QXEA200801831 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - RIGHT HAND INBOARD SEAT TRACK NR 13 HAS SCRATCHES AT SEVERAL LOCATIONS IN CHANNEL FROM STA X445 TO 570. BLENDED OUT SCRATCHES, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. 2 H 7 2 4T RT A13NM 2008021900270 20080219 00270 NM 2008 2 19 QXEA200801816 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 331-341 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX -C4 CHECK - RIGHT INBOARD SEAT TRACK NR 13 HAS PITTING AT APPROXIMATELY STA 331.00 TO 341.00. BLENDED OUT PITTING, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. 2 H 7 2 4T RT A13NM 2008021900121 20080219 00121 NM 2008 2 19 QXEA200801822 1 20071125 A 5320 THRESHOLD BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - SUSPECTED CORROSION UNDER AFT PASSENGER DOORWAY KICKPLATE THRESHOLD (OUTBOARD). REMOVED KICKPLATE AND BLENDED OUT CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. RESTORED FINISH TO BLENDED AREA. 2 H 7 2 4T RT A13NM 2008021900123 20080219 00123 NM 2008 2 19 QXEA200801824 1 20071125 A 5321 FLOOR PANEL BOMBDR DHC8 DHC8402 1390042 NM CARGO BAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - CORROSION ON AFT CARGO BAY DECK UPPER SKIN UNDER PANEL 144HZ. BLENDED OUT CORROSION, INSPECTED, REMAI NED WITHIN LIMITS AND NO CRACKS NOTED. RESTORED FINISH TO BLENDED AREA. 2 H 7 2 4T RT A13NM 2008021900144 20080219 00144 NM 2008 2 19 QXEA200801863 1 20071125 A 2750 CARRIAGE BOMBDR DHC8 DHC8402 1390042 NM NR 5 FLAP BINDING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - DURING ADJUSTMENT OF RIGHT NR 5 FLAP CARRIAGE SIDE ROLLERS TASK 27-52-820-801 STEP 3, A,(3)(A) FLAP FA ILS TO LIFT AT TRAILING EDGE CARRIAGE IS BOUND. BLENDED RIGHT WING NR 5 FLAP TRACK HOOK RD 84-57-899/1. INSPECTED, REM AINED WITHIN LIMITS AND NO CRACKS NOTED. 2 H 7 2 4T RT A13NM 2008021900146 20080219 00146 NM 2008 2 19 QXEA200801827 1 20071125 A 5312 BULKHEAD BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - NOSE COMPARTMENT UNDER FLOOR FRONT PRESSURE BULKHEAD HAS CHAFE DAMAGE ON LEFT SIDE. BLENDED CHAFED ARE A RD 84-53-1224, INSPECTED, REMAINED WITHIN LIMITS, NO CRACKS NOTED. 2 H 7 2 4T RT A13NM 2008021900160 20080219 00160 NM 2008 2 19 QXEA200801818 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 368-373 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - RIGHT INBOARD SEAT TRACK NR 13 HAS PITTING AT APPROXIMATELY STA 368.00 TO 373.00. BLENDED OUT PITTING, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. 2 H 7 2 4T RT A13NM 2008022000011 20080220 00011 NM 2008 2 20 QXEA200801886 1 20071125 A 5320 INTERCOSTAL BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - CORROSION RIGHT SIDE APPROXIMATELY STRINGER 24 AND FRAME AT X72.2 THROUGH STATION X76. REMOVED CORRODE D INTERCOSTAL AND INSTALLED NEW INTERCOSTAL TO EXISTING STRUCTURE IAW SRM. 2 H 7 2 4T RT A13NM 2008021900152 20080219 00152 NM 2008 2 19 QXEA200801834 1 20071125 A 5210 STRUCTURE BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - MAIN CABIN DOOR ENTRY WAY JUST INBOARD OF MAIN CABIN DOOR STEP ASSEMBLY, TOP SKIN HAS CORROSION AROUND NUT PLATE. REMOVED MCD THRESHOLD AND NUTS PLATES FROM SILL PLATE. REMOVED CORROSION, INSPECTED, WITHIN LIMITS AND NO C RACKS NOTED. INSTALLED NUTPLATES AND THRESHOLD TO SILL PLATE. 2 H 7 2 4T RT A13NM 2008021900153 20080219 00153 NM 2008 2 19 QXEA200801829 1 20071125 A 5753 SKIN BOMBDR DHC8 DHC8402 1390042 NM TE FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - RIGHT WING OUTBOARD FLAP INBOARD END UPPER SURFACE NEAR LEADING EDGE APPROXIMATELY YW191.2 TO YW209.01 9 HAS CHAFE DAMAGE. BLENDED OUT DAMAGE AT CHAFED AREA, INSPECTED, REMAINED WITHIN LIMITS, NO CRACKS NOTED. RESTORED FI NISH TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021900154 20080219 00154 NM 2008 2 19 QXEA200801811 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 232 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - RIGHT INBOARD SEAT TRACK NR 12 HAS GOUGE AT APPROXIMATELY STA 232.00. BLENDED OUT DAMAGED AREA, INSPEC TED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. RESTORED ALODINE TREATMENT TO BLENDED AREA. 2 H 7 2 4T RT A13NM 2008021900155 20080219 00155 NM 2008 2 19 QXEA200801813 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 234-244 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - RIGHT INBOARD SEAT TRACK NR 13 HAS PITTING AT APPROXIMATELY STA 234.00 TO 244.00. BLENDED OUT PITTING , INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. RESTORED FINISH AT BLENDED AREA. 2 H 7 2 4T RT A13NM 2008021900158 20080219 00158 NM 2008 2 19 QXEA200801807 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 114-122 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - RIGHT INBOARD SEAT TRACK NR 12 HAS PITTING AT APPROXIMATELY STA 114.00-122.00. BLENDED OUT PITTING, I NSPECTED, WITHIN LIMITS AND NO CRACKS NOTED. 2 H 7 2 4T RT A13NM 2008021900167 20080219 00167 NM 2008 2 19 QXEA200801810 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 608 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - SEAT TRACK NR 8 IS CORRODED AT APPROXIMATELY X608. BLENDED OUT CORROSION, INSPECTED, REMAINED WITHIN L IMITS AND NO CRACKS NOTED. RESTORED ALODINE TREATMENT TO BLENDED AREA. 2 H 7 2 4T RT A13NM 2008021900256 20080219 00256 NM 2008 2 19 QXEA200801814 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 635 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - SEAT TRACK NR 8 IS CORRODED AT APPROXIMATELY X635. REMOVED CORROSION, INSPECTED, REMAINED WITHIN LIMI TS AND NO CRACKS NOTED. RESTORED ALODINE TREATMENT TO WORKED AREA. 2 H 7 2 4T RT A13NM 2008022000013 20080220 00013 NM 2008 2 20 QXEA200801830 1 20071125 A 5753 SKIN BOMBDR DHC8 DHC8402 1390042 NM TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - LEFT OUTBOARD FLAP HAS A CHAFE ON THE UPPER OUTBOARD SURFACE. LOCATED APPROXIMATELY 11 INCHES FORWARD OF THE TRAILING EDGE ON THE FLAP AND AT THE EDGE. BLENDED OUT CHAFE , INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS N OTED. RESTORED FINISH TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008022000096 20080220 00096 NM 2008 2 20 QXEA200801825 1 20071125 A 5321 FLOORBOARD BOMBDR DHC8 DHC8402 1390042 NM BS 783 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - CORROSION SPOT 1/2 INCH BY 1/2 INCH ON AFT CARGO BAY FLOOR BOARD FLANGE AT STATION 783 AFT OF PANEL 144 JZ. BLENDED OUT CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008022000100 20080220 00100 NM 2008 2 20 QXEA200801823 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 703 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - ON SEAT TRACK NR 9 AT FS X703 YL9.5 X100 THERE IS TRACK DAMAGE WHERE WALL HAS BEEN MOUNTED. REMOVED NR 9 SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW SRM. 2 H 7 2 4T RT A13NM 2008022000101 20080220 00101 EA 2008 2 20 QXEA200801978 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 490-492 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT SEAT TRACK HAS GOUGES AND CORROSION AT STATION 490.5 TO 492.5. BLENDED GOUGES AND REMOVED CORROSI ON FROM SEAT TRACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREA. 2 L 7 2 4F RT A21EA 2008022000102 20080220 00102 EA 2008 2 20 QXEA200801980 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 537-539 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX -C4 CHECK - LEFT SIDE SEAT TRACK HAS GOUGES AND CORROSION AT STATION 537 TO 539.5. BLENDED GOUGES AND REMOVED CORRO SION ON SEAT TRACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO THE BLENDED ARE A. 2 L 7 2 4F RT A21EA 2008022000107 20080220 00107 EA 2008 2 20 QXEA200801964 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 761 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT SIDE RAIL SEAT TRACK HAS CORROSION AT APPROXIMATELY STATION 761.00. BLENDED CORROSION FROM TRACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TO REPAIR AREA. 2 L 7 2 4F RT A21EA 2008022000130 20080220 00130 EA 2008 2 20 QXEA200801961 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 813 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT SIDE RAIL SEAT TRACK TOP FLANGE HAS CORROSION AT APPROXIMATELY STATION 813.00. BLENDED OUT CORRO SION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TO REPAIR AREA. 2 L 7 2 4F RT A21EA 2008022000131 20080220 00131 NM 2008 2 20 QXEA200801843 1 20071125 A 5755 HINGE FITTING BOMBDR DHC8 DHC8402 1390042 NM RT SPOILER CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - RIGHT INBOARD SPOILER INBOARD MIDDLE HINGE FITTING HAS CHAFE DAMAGE FROM COTTER PIN. REMOVED WEB BELOW INBOARD SPOILER MIDDLE HINGE FITTING, INSTALLED NEW INBOARD SPOILER FITTING IAW SRM. 2 H 7 2 4T RT A13NM 2008022000135 20080220 00135 EA 2008 2 20 QXEA200801954 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 477-517 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT CENTER SEAT TRACK HAS CORROSION AND SCRATCHES AT STATION 477.40 TO STATION 517.00. BLENDED OUT CO RROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TO BLENDED AREA. 2 L 7 2 4F RT A21EA 2008022000159 20080220 00159 EA 2008 2 20 QXEA200802056 1 20071215 A 5551 LUG CNDAIR CL600 CL6002C10 1390015 EA HORIZONTAL STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT HORIZONTAL STAB ANTI-ROTATION LUG APPEARS TO HAVE DAMAGE BEYOND PREVIOUS BLEND REPAIR, DUE TO HIN GE HARDWARE ROTATION. BLENDED DAMAGED AREA IAW REO 670-55-11-033, HFEC INSPECTED AND NO CRACKS NOTED. ROTOPEENED AND R ESTORED FINISH TO BLENDED AREA. 2 L 7 2 4F RT A21EA 2008022000160 20080220 00160 EA 2008 2 20 QXEA200801963 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 797 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT SIDE RAIL SEAT TRACK SUSPECT CORROSION ON TOP LIP AT APPROXIMATELY STATION 797.00. BLENDED OUT CO RROSION FROM SEAT TRACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TO REPAIR AREA. 2 L 7 2 4F RT A21EA 2008022000165 20080220 00165 NM 2008 2 20 QXEA200801833 1 20071125 A 5260 TRACK BOMBDR DHC8 DHC8402 1390042 NM AIRSTAIR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - CORROSION ON THE MOST INBOARD FLANGE OF THE AIRSTAIRS TRACK APPROXIMATELY AT THE FOLLOWING LOCATIONS: S TATION X664, X688, X650 AND X630 FORWARD END OF FLANGE. REMOVED INBOARD FLANGE AND INSTALLED NEW FLANGE IAW SRM. 2 H 7 2 4T RT A13NM 2008022000191 20080220 00191 EA 2008 2 20 QXEA200801972 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 613 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT SIDE RAIL SEAT TRACK HAS CORROSION AT APPROXIMATELY STATION 613. REMOVED LOCALIZED CORROSION BY BLENDING SEAT TRACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREA. 2 L 7 2 4F RT A21EA 2008022000194 20080220 00194 EA 2008 2 20 QXEA200801966 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 708 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT SIDE RAIL SEAT TRACK HAS CORROSION AT APPROXIMATELY STATION 708.00. BLENDED OUT CORROSION FROM TR ACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TO REPAIR AREA. 2 L 7 2 4F RT A21EA 2008022000202 20080220 00202 EA 2008 2 20 QXEA200801974 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 460 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT SIDE RAIL SEAT TRACK HAS CORROSION AT APPROXIMATELY STATION 460.00. REMOVED LOCALIZED CORROSION BY BLENDING SEAT TRACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED ARE A. 2 L 7 2 4F RT A21EA 2008021900157 20080219 00157 NM 2008 2 19 QXEA200801828 1 20071125 A 5312 BULKHEAD BOMBDR DHC8 DHC8402 1390042 NM NLG WW CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - NOSE COMPARTMENT UNDER FLOOR FRONT PRESSURE BULKHEAD HAS CHAFE DAMAGE ON RIGHT SIDE (INSIDE NOSE WHEEL WELL). BLENDED OUT DAMAGE, BLEND WITHIN LIMITS RD 84-53-2164. NO CRACKS NOTED. RESTORED FINISH TO WORKED AREA. 2 H 7 2 4T RT A13NM 2008021900175 20080219 00175 EA 2008 2 19 QXEA200801971 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 708 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT SIDE RAIL SEAT TRACK HAS CORROSION AT APPROXIMATELY STATION 708. BLENDED OUT CORROSION FROM SEAT TRACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO REPAIR AREA. 2 L 7 2 4F RT A21EA 2008022000012 20080220 00012 NM 2008 2 20 QXEA200801832 1 20071125 A 5260 TRACK BOMBDR DHC8 DHC8402 1390042 NM AIRSTAIR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - CORROSION ON INBOARD FLANGE OF THE AIRSTAIRS TRACK AT STATION X670 - X695. REMOVED INBOARD FLANGE AND INSTALLED NEW INBOARD FLANGE IAW SRM. 2 H 7 2 4T RT A13NM 2008022000098 20080220 00098 NM 2008 2 20 QXEA200801885 1 20071125 A 5311 FRAME BOMBDR DHC8 DHC8402 1390042 NM BS 704 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - CORROSION AROUND RIVET BUCKTAIL ON FORWARD SIDE OF FRAME AT STATION 704 AND Z133 LEFT BAY AFT OF AFT PA SSENGER ENTRYWAY. BLENDED CORRODED AREA, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. RESTORED FINISH TO REP AIR AREA. 2 H 7 2 4T RT A13NM 2008022000104 20080220 00104 EA 2008 2 20 QXEA200801968 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 409 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT CENTER SEAT TRACK IS WORN AND PITTED AT APPROXIMATELY STATION 409.00. BLENDED OUT WEAR AND PITTIN G, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO REPAIR AREA. 2 L 7 2 4F RT A21EA 2008022000105 20080220 00105 EA 2008 2 20 QXEA200801959 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 797 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT SIDE RAIL SEAT TRACK TOP LOWER FLANGE HAS CORROSION AT APPROXIMATELY 797.00. BLENDED AWAY CORROS ION ON SEAT TRACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED, APPLIED ALODINE TO REPAIR AREA. 2 L 7 2 4F RT A21EA 2008022000106 20080220 00106 EA 2008 2 20 QXEA200802957 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 661 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT SIDE SEAT TRACK HAS GOUGE AT APPROXIMATELY 661.00. REMOVED GOUGE BY BLENDING SEAT TRACK. INSPEC TED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TO REPAIR AREA. 2 L 7 2 4F RT A21EA 2008022000132 20080220 00132 NM 2008 2 20 QXEA200801836 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 703 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - ON SEAT TRACK NR 16 THERE IS DAMAGE AT WALL MOUNTING LOCATION AT FS X703 YR9.5 Z100. REMOVED SEAT TRAC K NR 16 AND INSTALLED NEW SEAT TRACK NR 16 IAW SRM. 2 H 7 2 4T RT A13NM 2008022000133 20080220 00133 NM 2008 2 20 QXEA200801842 1 20071125 A 5330 DOUBLER BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - CORROSION ON DOUBLER UNDER NR 3 COMM ANTENNA. REMOVED ANTENNA DOUBLER AND INSTALLED NEW DOUBLER FROM STOCK IAW SRM. 2 H 7 2 4T RT A13NM 2008022000134 20080220 00134 NM 2008 2 20 QXEA200801835 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 667 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - SEAT TRACK NR 15 HAS LIGHT CORROSION AT FS X667 YR9.O Z100 REMOVED NR 15 SEAT TRACK AND INSTALLED NEW SEAT TRACK NR 15 IAW SRM. 2 H 7 2 4T RT A13NM 2008022000136 20080220 00136 EA 2008 2 20 QXEA200801955 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 598 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX -C4 CHECK - LEFT CENTER SEAT TRACK HAS GOUGES AT STATION 598.00. BLENDED OUT DAMAGE FROM SEAT TRACK, INSPECTED, REM AINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TO REPAIR AREA. 2 L 7 2 4F RT A21EA 2008022000158 20080220 00158 EA 2008 2 20 QXEA200801973 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 549 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX -C4 CHECK - RIGHT SIDE RAIL SEAT TRACK HAS CORROSION AT APPROXIMATELY STATION 549.00. REMOVED LOCALIZED CORROSION B Y BLENDING SEAT TRACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREA . 2 L 7 2 4F RT A21EA 2008022000210 20080220 00210 EA 2008 2 20 QXEA200801958 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 677 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT SIDE RAIL SEAT TRACK TOP FLANGE WORN AT APPROXIMATELY 677.00. BLENDED TO REMOVE WEAR ON SEAT TRA CK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TO REPAIR AREA. 2 L 7 2 4F RT A21EA 2008022000220 20080220 00220 EA 2008 2 20 QXEA200801969 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 412 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT CENTER SEAT TRACK HAS PITTING AT APPROXIMATELY STATION 412.00. BLENDED OUT PITTTING, INSPECTED, R EMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TO BLENDED AREA. 2 L 7 2 4F RT A21EA 2008022000234 20080220 00234 EA 2008 2 20 QXEA200801977 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 459-462 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT SIDE SEAT TRACK HAS GOUGES AND CORROSION AT STATION 459.5 TO 462. BLENDED GOUGES AND REMOVED CORR OSION FROM SEAT TRACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREA . 2 L 7 2 4F RT A21EA 2008022000249 20080220 00249 NM 2008 2 20 QXEA200801841 1 20071125 A 5730 SKIN BOMBDR DHC8 DHC8402 1390042 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - CORROSION AROUND FASTENER HOLES ON FUEL PANEL 524AT APPERATURE OUTBOARD END. BLENDED OUT CORROSION, I NSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. 2 H 7 2 4T RT A13NM 2008022000252 20080220 00252 NM 2008 2 20 QXEA200801857 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - RIGHT INBOARD SEAT TRACK NR 11 HAS CORROSION LOCATED APPROXIMATELY STATION 11.00. REMOVED NR 11 SEAT T RACK AND INSTALLED NEW NR 11 SEAT TRACK IAW SRM. 2 H 7 2 4T RT A13NM 2008022000260 20080220 00260 NM 2008 2 20 QXEA200801858 1 20071125 A 5320 WEB BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - PANEL 414AL AFT INTERNAL WEB CRACKED. REPLACED WEB WITH NEW WEB FROM STOCK IAW SRM. 2 H 7 2 4T RT A13NM 2008022000308 20080220 00308 NM 2008 2 20 HNAA0800078 1 20071128 A 5411 85410424105 FRAME DHAV DHC8 DHC8102 2809003 NM LT NACELLE WORN A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 804EX 227 FRAME WORN OUT O/B SIDE OF LT NACELLE. REPLACED WORN OUT FRAME. 2 H 7 2 4T RT A13NM 2008022000310 20080220 00310 NM 2008 2 20 HNAA0800080 1 20071128 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 804EX 227 FRAME CRACKED. REPAIRED IAW EO8-53-07-3450. 2 H 7 2 4T RT A13NM 2008022000014 20080220 00014 EA 2008 2 20 QXEA200801956 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 560 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT CENTER SEAT TRACK NR 15 HAS GOUGES AND CORROSION AT STATION 560. BLENDED OUT CORROSION, INSPECTE D, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TO REPAIR AREA. 2 L 7 2 4F RT A21EA 2008022000097 20080220 00097 NM 2008 2 20 QXEA200801862 1 20071125 A 5415 ATTACH FITTING BOMBDR DHC8 DHC8402 1390042 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - LEFT OUTBOARD FORWARD SPINE COWL CLEAT IS CRACKED AT THE INBOARD BOLT HOLE. REMOVED CRACKED CLIP AND I NSTALLED FABRICATED CLIP IAW RD AND SRM. 2 H 7 2 4T RT A13NM 2008022000103 20080220 00103 EA 2008 2 20 QXEA200801982 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 584-586 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT SIDE SEAT TRACK HAS CORROSION AND GOUGES AT STATION 584 TO 586. BLENDED OUT CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREA. 2 L 7 2 4F RT A21EA 2008022000203 20080220 00203 EA 2008 2 20 QXEA200801975 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 398-400 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT SIDE SEAT RAIL HAS GOUGES AND CORROSION AT STATION 398 TO 400. BLENDED GOUGES AND REMOVED CORROSI ON FROM SEAT RAIL, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREA. 2 L 7 2 4F RT A21EA 2008022000235 20080220 00235 EA 2008 2 20 QXEA200801979 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 522-524 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT SIDE SEAT TRACK HAS GOUGES AND CORROSION AT STATION 522 TO 524. BLENDED GOUGES AND REMOVED CORROS ION FROM SEAT TRACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREA. 2 L 7 2 4F RT A21EA 2008022000281 20080220 00281 SO 2008 2 20 C2XA08IA053 1 20070206 A 2130 CABIN PRESSURE EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A C2XA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 27 16571 145633 ELP - FLIGHT 2311, THE CREW REPORTED AIRCRAFT PRESURIZATION FAILED IN AUTO AND MANUAL AFTER T/O. THE AIRCRAFT RETURNED TO ELP WHERE IT LANDED WITHIOUT INCIDENT. THE CABIN PRESSURIZATION SYSTEM WAS PLACED ON MEL, AND THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. FLIGHT 2311 THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE OPERATIONALLY CHEC KED THE PRESSURIZATION SYSTEM WITH NO DEFECTS. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008022000099 20080220 00099 NM 2008 2 20 QXEA200801861 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 668 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - UPON REMOVING AFT BULKHEAD CLEAT, SEAT TRACK NR 3 AT APPROXIMATELT 668.5 HAS CORROSION PIT MEASURING 1/ 2 INCH BY 2 INCH BY APPROXIMATELY .040 DEEP. REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW SRM. 2 H 7 2 4T RT A13NM 2008022000161 20080220 00161 EA 2008 2 20 QXEA200801981 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 553-554 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT SIDE SEAT TRACK HAS CORROSION AND AT STATION 553 TO 554.5. BLENDED GOUGES AND REMOVED CORROSION F ROM SEAT TRACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREA. 2 L 7 2 4F RT A21EA 2008022000162 20080220 00162 EA 2008 2 20 QXEA200801960 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 747 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT RAIL SEAT TRACK TOP FLANGE WORN AND HAS PITTING APPROXIMATELY STATION 747.00. BLENDED OUT PITTIN G, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TO REPAIR AREA. 2 L 7 2 4F RT A21EA 2008022000163 20080220 00163 EA 2008 2 20 QXEA200801965 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 736 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT SIDE RAIL SEAT TRACK HAS CORROSION AT APPROXIMATELY STATION 736.00. BLENDED OUT CORROSION FROM TR ACK, INSPECTED, REMAINED WITHIN LIMITS. APPLIED ALODINE TO REPAIR AREA. 2 L 7 2 4F RT A21EA 2008022000193 20080220 00193 EA 2008 2 20 QXEA200801962 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 905 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT SIDE RAIL SEAT TRACK LOWER FLANGE HAS GOUGES AT APPROXIMATELY STATION 905.00. BLENDED OUT GOUGES ON TRACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TO REPAIR AREA. 2 L 7 2 4F RT A21EA 2008022000201 20080220 00201 EA 2008 2 20 QXEA200801970 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 761 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT SIDE RAIL SEAT TRACK HAS CORROSION AT APPROXIMATELY STATION 761. BLENDED OUT CORROSION, INSPECTE D, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TO REPAIR AREA. 2 L 7 2 4F RT A21EA 2008022000219 20080220 00219 SO 2008 2 20 SIMA200804901 1 20071121 A 2820 P1163 HOSE EMB 135 EMB135KL 3260302 SO FUEL SYS WORN A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 837AE 145647 ON FLIGHT 3502 PACK 2 FAIL EICAS MESSAGE DID NOT HAVE ENOUGH FUEL TO CONTINUE ON TO CVG ELECTED TO DO AN AIR RETURN TO D FW DISC-SHORTLY AFTER TAKEOFF, NR 2 BLEED AND PACK VALVE CLOSED ANNUNCIATED ON THE EICAS. PER AOM; CYCLED BLEED VALVE A ND PACK SEVERAL TIMES. UNSUCCESSFULLY. NR 2 PACK VALVE WOULD NOT STAY OPEN. AIRCRAFT REMOVED FROM SERVICE. REMOVED A ND REPLACED BLEED HOSE AT DUAL TEMP CONTROL VALVE PACK OPERATION CHECK GOOD IAW EMB 140 AMM 21-20-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008022000233 20080220 00233 EA 2008 2 20 QXEA200801976 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 429-430 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT SIDE SEAT RAIL TRACK HAS GOUGES AND CORROSION AT STATION 429 TO 430.5. BLENDED GOUGES AND REMOVED CORROSION FROM SEAT TRACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREA. 2 L 7 2 4F RT A21EA 2008022000251 20080220 00251 NM 2008 2 20 QXEA200801856 1 20071125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - C4 CHECK - RIGHT INBOARD SEAT TRACK NR 10 HAS CORROSION ON RIGHT FLANGE AROUND FASTENER HOLE AT APPROXIMATELY STAT ION 10.5. REMOVED NR 10 SEAT TRACK AND INSTALLED NEW NR 10 SEAT TRACK IAW SRM. 2 H 7 2 4T RT A13NM 2008022000307 20080220 00307 NM 2008 2 20 HNAA0800077 1 20071128 A 5313 85320300 STRINGER DHAV DHC8 DHC8102 2809003 NM FUSELAGE DEBONDED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 804EX 227 FWD PASS COMP STRINGER RT SIDE STRINGER 28R DISBONDED FROM SKIN. REPAIRED IAW RD8-53-9890. 2 H 7 2 4T RT A13NM 2008022000309 20080220 00309 NM 2008 2 20 HNAA0800079 1 20071128 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 804EX 227 FRAME CRACKED. REPAIRED IAW SRM 53-20-21. 2 H 7 2 4T RT A13NM 2008022100141 20080221 00141 SO 2008 2 21 SWIA200719203 1 20071206 A 2497 BUSS BAR EMB 120 EMB120ER 3260203 SO CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 292UX 120292 BUS BAR ATTACH POINT NEAR K0135 AREA SHOWS SIGNS OF CORROSION. REPLACED FEED PROTECTION RELAY AND ASSOCIATED BUS BARS I AW EMB 120 AMM 24-52-00. 2 L 7 2 4T RT A31SO 2008022100142 20080221 00142 SO 2008 2 21 SWIA200719204 1 20071206 A 2497 TERMINAL EMB 120 EMB120ER 3260203 SO DC GENERATOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 292UX 120292 THE RIGHT DC CONTACTOR TERMINALS ARE CORRODED. REPLACED THE RIGHT DC CONTACTOR IAW MM 24-30-03. 2 L 7 2 4T RT A31SO 2008022100181 20080221 00181 EA 2008 2 21 SWIA200719211 1 20071108 A 5610 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 748SK 10203 PILOTS SIDE WINDOW INNER PLY CRACK LOCATED AT FWD BOTTOM EDGE, FOUND AT C-CHECK. REPLACED PILOTS SIDE WINDOW PER 56-12- 01-400-801-A01. 2 L 7 2 4F RT A21EA 2008022100183 20080221 00183 EA 2008 2 21 SWIA200719213 1 20071108 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 748SK 10203 FS 280 FLOORBEAM IS CRACKED AT LBL9 AND RBL9, FOUND AT C-CHECK. COMPLIED WITH REPAIRS OF FS 280 BEAM PER CRJ7/9 SRM 51- 42-06. 2 L 7 2 4F RT A21EA 2008022200045 20080222 00045 NM 2008 2 22 HALA0800263 1 20070215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1400 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION ON SEAT TRACK CROWN/BASE AT LBL 88.5, STA 1400, AREA HAS BEEN REWORKED BEFORE. SEAT TRACK REPLACE PER SRM. 2 L 7 2 4F RT A1NM 2008022100182 20080221 00182 EA 2008 2 21 SWIA200719212 1 20071108 A 5320 ANGLE CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 748SK 10203 WEB STIFFENER ANGLE IS CRACKED AT FS 280 RBL 26, FOUND AT C-CHECK. INSTALLED WEB STIFFENER ANGLE PER CRJ700 SRM 51-42-0 6/51-42-13. 2 L 7 2 4F RT A21EA 2008022100138 20080221 00138 EU 2008 2 21 07FDEA04945 1 20071127 A 5310 A53610553223 CROSSBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 402FE 201 FWD E/E BAY FRAME 14 RT CROSS MEMBER VERTICAL LEG HOLE LABELED "A" DAMAGED. THIS SDR WAS GENERATED TO REPLACE SDR 07-47 70. THIS SDR IS TO MAKE CORRECTIONS IN THE FOLLOWING BLOCKS 5A, 5C, 5D, 5F. 2 L 7 2 4F RT A35EU 2008022100162 20080221 00162 SO 2008 2 21 SWIA200819205 1 20071206 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 292UX 120292 CORROSION FOUND ON FUSELAGE FLOOR FRAME AT AFT PAX DOOR HINGE. COMPLIED WITH REPAIR OF FLOOR FRAME IAW EMB 120 SRM 51-10 -02 PG 3 SECTION 3B. 2 L 7 2 4T RT A31SO 2008022100188 20080221 00188 SO 2008 2 21 SWIA200719218 1 20071206 A 5311 FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 292UX 120292 LOWER FUSELAGE BELLY FRAME 23 SHOWS SIGNS OF CORROSION. COMPLIED WITH REPAIRS AT FRAME 23 IAW IC2007-120/07298 AND CPM 51-11-0. 2 L 7 2 4T RT A31SO 2008022500058 20080225 00058 NM 2008 2 25 HNAA0800062 1 20071128 A 5220 85326818104 DOOR FRAME DHAV DHC8 DHC8102 2809003 NM EMERGENCY EXIT CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 804EX 227 RIGHT EMERGENCY EXIT BOTTOM FRAME, SURFACE CORROSION. REPLACED FRAME. 2 H 7 2 4T RT A13NM 2008022500060 20080225 00060 NM 2008 2 25 HNAA0800065 1 20071128 A 5320 85520980105SP FITTING DHAV DHC8 DHC8102 2809003 NM LAV SERVICE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 804EX 227 LAVATORY SERVICE BOX UPPER FITTING FOUND WITH SURFACE CORROSION. REPLACED DEFECTIVE FITTING. 2 H 7 2 4T RT A13NM 2008022500061 20080225 00061 NM 2008 2 25 HNAA0800066 1 20071128 A 5313 85320871101 STRINGER DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 804EX 227 STRINGER 26S IN LAVATORY AREA HAS CORROSION DAMAGE. REPLACED DEFECTIVE STRINGER. 2 H 7 2 4T RT A13NM 2008022500062 20080225 00062 NM 2008 2 25 HNAA0800067 1 20071128 A 5320 CHANNEL DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 804EX 227 JOINT CHANNEL IN LAVATORY AREA HAS CORROSION DAMAGE. REPLACED DEFECTIVE JOINT CHANNEL. 2 H 7 2 4T RT A13NM 2008022500063 20080225 00063 NM 2008 2 25 HNAA0800068 1 20071128 A 5320 85320873103 JOINT DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 804EX 227 JOINT ZED IN LAVATORY AREA DAMAGED BY CORROSION. REPLACED DAMAGED JOINT ZED. 2 H 7 2 4T RT A13NM 2008022500064 20080225 00064 NM 2008 2 25 HNAA0800069 1 20071128 A 5320 85321088101 DOUBLER DHAV DHC8 DHC8102 2809003 NM LAVATORY CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 804EX 227 DOUBLER IN LAVATORY AREA DAMAGED BY CORROSION. REPLACED DAMAGED DOUBLER. 2 H 7 2 4T RT A13NM 2008022500065 20080225 00065 NM 2008 2 25 HNAA0800070 1 20071128 A 5320 85321415101 FITTING DHAV DHC8 DHC8102 2809003 NM LAVATORY CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 804EX 227 CLEATS IN LAVATORY AREA DAMAGED BY CORROSION. REPLACED DAMAGED CLEATS. 2 H 7 2 4T RT A13NM 2008022500072 20080225 00072 NM 2008 2 25 HNAA0800075 1 20071128 A 5320 85320686101 THRESHOLD DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 804EX 227 CORROSION FOUND ON PASS DOOR THRESHOLD. REPLACED THRESHOLD. 2 H 7 2 4T RT A13NM 2008022100184 20080221 00184 EA 2008 2 21 SWIA200719214 1 20071108 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 748SK 10203 COCKPIT FLOOR SUPPORT AT FS 280 AND LBL9 IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS ON COCKPIT FLOOR SUPPORT PER CRJ700/900 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008022500070 20080225 00070 NM 2008 2 25 HNAA0800073 1 20071128 A 5330 85320596109 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 804EX 227 SURFACE CORROSION ON SKIN AND STRINGER. REMOVED AND REPROTECTED. 2 H 7 2 4T RT A13NM 2008022500076 20080225 00076 NM 2008 2 25 HNAA0800076 1 20071128 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE DEBONDED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 804EX 227 FUSELAGE SKIN DISBONDED. REPAIRED SKIN. 2 H 7 2 4T RT A13NM 2008022500104 20080225 00104 NM 2008 2 25 2007UALA03915 1 20070926 A 5241 UNKNOWN STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT GALLEY DOOR GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 AFT GALLEY DOOR SN 1795 SNUBBER ATTACH BOLT ACCESS HOLE GOUGED AT INTERCOSTAL. MAJOR REPAIR ACP'D, FABRICATED AND INSTA LLED REPLACEMENT WEB. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022500059 20080225 00059 NM 2008 2 25 HNAA0800064 1 20071128 A 5347 85320490133 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 804EX 227 BOTH FWD SEAT TRACKS CORRODED. REPLACED DEFECTIVE SEAT TRACKS. 2 H 7 2 4T RT A13NM 2008022500066 20080225 00066 NM 2008 2 25 HNAA0800071 1 20071128 A 5330 85320870101 DOUBLER DHAV DHC8 DHC8102 2809003 NM LAV SERVICE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 804EX 227 CORROSION FOUND ON LAVATORY SERVICE PANEL SURROUND. REPLACED DOUBLER (SURROUND). 2 H 7 2 4T RT A13NM 2008022500067 20080225 00067 NM 2008 2 25 HNAA0800072 1 20071128 A 3830 85321086 SERVICE PANEL DHAV DHC8 DHC8102 2809003 NM LAV SERVICE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 804EX 227 CORROSION FOUND ON LAVATORY SERVICE PANEL. REPLACED LAVATORY SERVICE PANEL. 2 H 7 2 4T RT A13NM 2008022500074 20080225 00074 NM 2008 2 25 HNAA0800074 1 20071128 A 5260 85210307101 BRACKET DHAV DHC8 DHC8102 2809003 NM AIRSTAIRS CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 804EX 227 BRACKET AND ANGLE CORRODED ON AIRSTAIR. REPLACED CORRODED BRACKET, ANGLE AND SHIM. 2 H 7 2 4T RT A13NM 2008022500112 20080225 00112 NE 2008 2 25 2007UALA05340 2 20071227 A 7530 CONTROLLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 595UA 28748 FOUND THIN PIECES OF METAL IN HI-STAGE VALVE NR 1 ENGINE. REPLACED HIGH STAGE VALVE AND HIGH STAGE CONTROLLER, ALSO ACC OMPLISHED A BOROSCOPE WITH NO DAMAGE NOTED TO INTERNAL AREAS. NO FURTHER DAMAGE WAS FOUND. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022600005 20080226 00005 NM 2008 2 26 DHL2007742024 1 20071204 A 5322 SHEAR TIE BOEING 727 727225 1384077 NM BS 950C DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 BS 950C BETWEEN STRINGER 28L AND 29L FRAME SHEAR TIE DAMAGED. CUT OUT DAMAGED SECTION APPROXIMATE DIMENSION 6.75" BY 2" IAW B-727 SRM 53-10-4 FIGURE 15 AND SRM 51-10-1. FABRICATED SHEAR TIE REPAIR FROM 7075-O 0.071" APPROXIMATE DIMENSION 6.75" BY 2" IAW B-727 SRM 53-10-4 FIGURE 15 AND SRM 53-10-2 FIGURE 5. HEAT TREATED MATERIAL TO T6 CONDITION IAW FAS ER NR 2-37153-801 REV A. TREATED AND PRIMED PARTS IAW B-727 SRM 51-10-2. INSTALLED SHEAR TIE REPAIR AT STATION 950C STRIN GER 29L IAW B-727 SRM 53-10-4 FIGURE 15 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2008022600006 20080226 00006 NM 2008 2 26 DHL2007742032 1 20071121 A 5330 SKIN BOEING 727 727225 1384077 NM BS 720D S19R CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 RIGHT FUSELAGE CHAFFED AT BS 720D + 10" STRINGER 19R. CUT OUT DAMAGED AREA 6.75" BY 2.75" IAW B-727 SRM 53-30-3 FIGURE 6. FABRICATED DOUBLER REPAIR 2024-T3 0.071" PO NR 9005922 DIMENSION: 15.5" BY 9", STRUCTURAL FILLER 2024-T3 0.063" PO N R 9006027 DIMENSION: 14.5" BY 4.25" AND FILLER 2024-T3 0.063" PO NR 9006027 DIMENSION: 6.75" BY 2.75" IAW B-727 SRM 53-3 0-3 FIGURE 6 AND SRM 53-30-2 FIGURE 2. TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED REPAIR ON RIGHT FUSELAGE BS 720D + 10" STRINGER 19R IAW B-727 SRM 51-30-2, 53-30-3 FIGURE 6 AND 53-30-2 FIGURE 2. 2 L 7 3 4F A3WE 2008022600007 20080226 00007 NM 2008 2 26 DHL2007742050 1 20071124 A 5311 FRAME BOEING 727 727225 1384077 NM BS 1050 S22L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 EXFOLIATED CORROSION AFT PIT FRAME BS 1050 ABOVE STRINGER 22L ALSO ABOVE 21L. CUT OUT DAMAGED AREA (DIMENSION 4.5" BY 3 .5"). FABRICATED REPAIR ANGLE FROM 7075-0 0.071" PO NR 7247111 (DIMENSION 15.25" BY 4.5") AND REPAIR FILLER FROM 7075-T 6 0.063" PO NR 9005922 (DIMENSION 4.5" BY 3.5") OAW B-727 SRM 53-10-2 FIGURE 5 AND 51-40-3 FIGURE 1. HEAT TREATED REPAI R ANGLE TO T6 IAW FAS ENGINEERING REPORT NR 2=37153-801 REV A. TREATED AND PRIMED PARTS IAW B-727 SRM 51-10-2. INSTALL ED REPAIR PARTS AT AFT PIT FRAME BS 1050 ABOVE STRINGER 22L IAW B-727 SRM 51-40-3 FIGURE 1 AND 51-30-2. 2 L 7 3 4F A3WE 2008022600008 20080226 00008 NM 2008 2 26 DHL2007742052 1 20071204 A 5311 FRAME BOEING 727 727225 1384077 NM BS 420 S7-8R DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 FUSELAGE FRAME STATION 420 FRAME AND STRAP HAVE NUMEROUS HOLES DRILLED THROUGH BETWEEN STRINGER 7R AND 8R. REMOVED STRA PS AND FRAME ATTACHED PARTS FOR ACCESS IAW B-727 SRM 51-30-2. CUT OUT DAMAGED SECTION OF FRAME (DIMENSION 40" BY 5") IA W B-727 SRM 51-10-1. FABRICATED NEW FRAME SECTION (DIMENSION 40" BY 5") FROM 7075-0 0.080" PO NR 9005314 AND REPAIR ANG LE FROM 7075-0 0.090" PO NR 71185240 (DIMENSION 10.5" BY 5") IAW B-727 SRM 51-40-3 FIGURE 1 AND 53-10-2 FIGURE 3. HEAT TREATED PARTS TO T6 IAW FAS ENGINEERING REPORT NR 2-37153-801 REV A. TREATED AND PRIMED PARTS IAW B-727 SRM 51-10-2. I NSTALLED REPAIR PARTS IAW B-727 SRM 51-40-3 FIGURE 1 AND 51-30-2. REINSTALLED STRAPS AND FRAME ATTACHED PARTS IAW B-727 2 L 7 3 4F A3WE 2008022600009 20080226 00009 NM 2008 2 26 DHL2007742022 1 20071116 A 5311 STRAP BOEING 727 727225 1384077 NM BS 560 FRAME GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 FRAME INNER CHORD, UPPER STRAP HAS GOUGES FROM STRINGER 27R TO STRINGER 23R BS 560 AFT EDGE C-1 DOOR AREA. CUT OUT DAMA GED AREA APPROXIMATE DIMENSION 13" BY 5" IAW B-727 SRM 51-40-2 FIGURE 1. FABRICATED REPAIR DOUBLER FROM 2024-T3 0.050" PO NR 9005773 APPROXIMATE DIMENSION 3" BY 5". FABRICATED FILLER FROM 2024-T3 0.040" PO NR 9005634 APPROXIMATE DIMENSION 13" BY 5" IAW B-727 SRM 51-10-3 AND SRM 51-40-2 FIGURE 1. TREATED AND PRIMED REPAIR PARTS IAW B-727 SRM 51-10-2. INST ALLED NEW REPAIR PARTS IAW B-727 SRM 51-40-2 FIGURE 1 AT BS 560 STRINGER 275 TO 23R. 2 L 7 3 4F A3WE 2008022600010 20080226 00010 NM 2008 2 26 DHL2007742029 1 20071213 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 950E S29R CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AFT CARGO COMPARTMENT STRINGER 29R IS CORRODED AT STATION 950E + 4". REMOVED FASTENERS AT AFT CARGO COMPARTMENT STRINGE R 29R STATION 950E IAW B-727 SRM 51-30-2. REMOVED CORROSION STRINGER 29R STATION 950E + 4" IAW B-727 SRM 51-10-6. INSP ECTED AREA, ORIGINAL MATERIAL 0.150", MATERIAL REMOVED 0.045", MATERIAL REMAINING 0.105" USING CL3 IAW B-727 NDT M PT 4, 51-00-00 FIGURE 3. MATERIAL LOSS FOUND OUT OF LIMITS IAW B-727 SRM 53-10-4 FIGURE 1. FABRICATED REPAIR DOUBLER USING 7075-T6 0.080" DIMENSION 15.5" BY 2" AND FILLER USING 7075-T6 0.032" DIMENSION 16.5" BY .75" IAW EDAE59-4 REV A. TREATE D AND PRIMED REPAIR PARTS IAW B-727 SRM 51-10-2 AND EDAE59-4 REV A. POSITIONED AND MATCH DRILLED PARTS TO EXISTING FAST 2 L 7 3 4F A3WE 2008022600012 20080226 00012 NM 2008 2 26 DHL2007742039 1 20071203 A 5753 WEDGE BOEING 727 727225 1384077 NM RWS 80 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 RIGHT INBOARD MID FLAP INBOARD TRAILING EDGE DELAMINATED WBL80. FOUND WEDGE OUT OF REPAIRABLE LIMITS IAW B-727 SRM 57-5 0-1 FIGURE 3. REMOVED WEDGE, LOCATED AND INSTALLED NEW WEDGE IAW B-727 SRM 51-30-2 AND 51-30-5. 2 L 7 3 4F A3WE 2008022600013 20080226 00013 NM 2008 2 26 DHL2007742045 1 20071126 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 720F-740 S26R CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 FORWARD CARGO COMPARTMENT STRINGER 26R IS HEAVILY CORRODED BETWEEN STATION 720F TO 740. CUT OUT DAMAGE AREA 9.5" AT STR INGER 26R BETWEEN STATION 720F - 740 IAW B-727 SRM 53-10-3 FIGURE 1. FABRICATED NEW SECTION, MATERIAL USED BAC 1498-147 0.090" 7075-T6 PO NR 7332258 DIMENSION 9.25" AND SPLICED MATERIAL USED BAC 1498-13107075-T6 PO NR 7332231 DIMENSION 11. 25" IAW B-727 SRM 53-10-3 FIGURE 1 AND 53-10-2 FIGURE 5. TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED REPAIR PA RTS IAW B-727 SRM 53-10-3 FIGURE 1 AND 51-30-2. 2 L 7 3 4F A3WE 2008022600014 20080226 00014 NM 2008 2 26 DHL2007742047 1 20071119 A 5754 SKIN BOEING 727 727225 1384077 NM NR 6 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 NR 6 SLAT SKIN CRACKED AT INBOARD SLAT HOOK UPPER MOUNT SCREW. C/W HFEC IAW B-727 NDT PT 6 51-00-00 FIGURE 23. CRACK T ERMINATES IN FASTENER HOLE. FABRICATED DOUBLER REPAIR WITH 7075-T6 0.125" SIZE 7.5" BY 3.25" PO NR 9005685 IAW B-727 SR M 57-50-3 FIGURE 10. TREATED AND PRIMED PART REPAIR IAW B-727 SRM 51-10-2. INSTALLED DOUBLER IAW B-727 SRM 57-50-3 FIG URE 10 AND 51-30-2. 2 L 7 3 4F A3WE 2008022600015 20080226 00015 NM 2008 2 26 DJL2007742048 1 20071115 A 5754 SKIN BOEING 727 727225 1384077 NM NR 7 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 NR 7 SLAT SKIN CRACKED AT OUTBOARD SLAT HOOK UPPER MOUNT SCREW. C/W HFEC IAW B-727 NDTM PT 6 51-00-00 FIGURE 23. CRACK TERMINATES IN FASTENER HOLE. FABRICATED DOUBLER REPAIR USING 7075-T6 0.125 PO NR 9005685 DIMENSION 7.5" BY 3" IAW B-72 7 SRM 57-50-3 FIGURE 10 AND 51-30-5. TREATED AND PRIMED DOUBLER IAW B-727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B- 727 SRM 57-50-3 FIGURE 10 AND 51-30-2. REMOVED AND REINSTALLED HOOK FOR ACCESS IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008022600017 20080226 00017 NM 2008 2 26 DHL2007742025 1 20071128 A 5322 SHEAR TIE BOEING 727 727225 1384077 NM BS 950D S28-29L DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 BS 950D BETWEEN STRINGER 28L AND 29L FRAME SHEAR TIE DAMAGED. CUT OUT DAMAGED SECTION (DIMENSION 6.75" BY 2") IAW B-727 SRM 53-10-4 FIGURE 15 AND SRM 51-10-1. FABRICATED SHEAR TIE REPAIR FROM 7075-0 0.071" PO NR 7247111 (DIMENSION 6.75" B Y 2") IAW B-727 SRM 53-10-4 FIGURE 15 AND 53-10-2 FIGURE 5. HEAT TREATED SHEAR TIE REPAIR FROM 7075-0 TO 7075-T6 IAW FA S ENGINEERING REPORT NR 2-37153-801 REV A. TREATED AND PRIMED PARTS AND AREA IAW B-727 SRM 51-10-2. INSTALLED REPAIR P ARTS IAW B-727 SRM 53-10-4 FIGURE 15 AND 51-30-2. 2 L 7 3 4F A3WE 2008022600018 20080226 00018 NM 2008 2 26 DHL2007742028 1 20071127 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 720F S27L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 FORWARD CARGO COMPARTMENT STRINGER 27L SHOWS CORROSION AT BS 720F + 10". CUT OUT DAMAGED AREA APPROXIMATE DIMENSION 7.3 75" LENGTH IAW B-727 SRM 53-10-3 FIGURE 1. FABRICATED REPAIR FILLER FROM BAC 1498-147 0.090" PO NR 7332258 APPROXIMATE DIMENSION 7.875" LENGTH. FABRICATED REPAIR SPLICE FROM BAC 1498-131 PO NR 7332231 APPROXIMATE DIMENSION 11" LENGTH IAW B-727 SRM 53-10-3 FIGURE 1 AND SRM 53-10-2 FIGURE 9. INSTALLED REPAIR PARTS AT BS 720F + 10" STRINGER 27L IAW B-727 SRM 53-10-3 FIGURE 1. 2 L 7 3 4F A3WE 2008022600019 20080226 00019 NM 2008 2 26 DHL2007742030 1 20071208 A 5330 SKIN BOEING 727 727225 1384077 NM BS 950E S29R CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AFT CARGO COMPARTMENT SKIN EXFOLIATED CORROSION AT STATION 950E BETWEEN STRINGER 29R AND STRINGER 30 AFT SIDE OF FRAME. REMOVED CORROSION AT AFT CARGO COMPARTMENT SKIN STATION 950E BETWEEN STRINGER 29R AND 30 IAW B-727 SRM 51-10-6. INSPEC TED AREA AND FOUND ORIGINAL MATERIAL TO BE 0.0156", MATERIAL REMOVED IS 0.033" AND MATERIAL REMAINING IS 0123" USING CL3 IAW B-727 NDTM PT. 4, AND 51-00-00 FIGURE 23. MATERIAL LOSS FOUND OUT OF LIMITS IAW B-727 SRM 53-30-1 FIGURE 1. CUT O UT DAMAGED AREA (DIMENSION 5.25" BY 2.375") AND FABRICATED REPAIR DOUBLER FROM 2024-T3 0.063" PO NR 9006027 (DIMENSION 1 5.75" BY 12.875") AND TRIPLER FROM 2024-T3 0.071" PO NR 9005773 (DIMENSION 14.375" BY 12.25") IAW ES NR EAAE59-5 REV IR. 2 L 7 3 4F A3WE 2008022600021 20080226 00021 NM 2008 2 26 DHL2007742036 1 20071129 A 5754 ATTACH ANGLE BOEING 727 727225 1384077 NM NR 2 SLAT MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 742DH 21290 NR 2 SLAT LOWER TRAILING EDGE ACCESS PANEL, ATTACH "L" ANGLE REPAIR AT UPSTOP PAD IS IMPROPER. REMOVED ACCESS PANELS AN D IMPROPER REPAIR IAW B-727 SRM 51-30-2. CUT OUT ANGLE DAMAGED SECTION (DIMENSION 26.75 BY 2") AND FABRICATED NEW ANGLE FILLER SECTION FROM BAC 1514-1559 2024-T3 PO NR 7332223 (DIMENSION 26.75" BY 2") AND REPAIR ANGLE FROM 2024-T3 0.063" P O NR 9006027 (DIMENSION 11.125" BY 2") IAW B-727 SRM 51-40-4 FIGURE 1 AND 57-50-2 FIGURE 2. TREATED AND PRIMED PARTS IA W B-727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B-727 SRM 51-40-4 FIGURE AND 51-30-2 AND REINSTALLED ACCESS PANEL AT NR 2 SLAT IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008022600024 20080226 00024 NM 2008 2 26 DHL2007742041 1 20071121 A 5330 SKIN BOEING 727 727225 1384077 NM BS 750E S19L GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 STRINGER 19L HAS GOUGE IN SKIN AT LAP SEAM AT BS 720E. CUT OUT DAMAGE AREA APPROXIMATE 2.75" BY 4.25" ON STRINGER 19L A T BS 720E IAW B-727 SRM 53-30-3 FIGURE 6. FABRICATED REPAIR DOUBLER 2024-T3 0.071" PO NR 9005922 DIMENSION 12.5" BY 9", STRUCTURAL FILLER 2024-T3 0.063" PO NR 9005551 DIMENSION 12" BY 7", AND FILLER 2024-T3 0.063" PO NR 9005551, DIMENSION 2.75" BY 4.25" IAW B-727 SRM 53-30-3 FIGURE 6 AND 53-30-2 FIGURE 2. TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLE D REPAIR IAW B-727 SRM 51-30-2, 53-30-3 FIGURE 6, AND 51-20-4. 2 L 7 3 4F A3WE 2008022600025 20080226 00025 NM 2008 2 26 DHL2007742068 1 20071125 A 5330 SKIN BOEING 727 727225 1384077 NM BS 710 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 BS 710 RIGHT AND LEFT FAIRINGS HAS CORROSION ON NUT PLATES (AC BAY AREA). CUT OUT DAMAGED AREA AT LOWER FUSELAGE BS 710 APPROXIMATE DIMENSION 1.25" BY .75" IAW B-727 SRM 53-30-3 FIGURE 1. REMOVED DAMAGED SHEAR TIE CLIP ON AFT SIDE OF FRAM E BS 710 IAW B-727 SRM 51-30-2. FABRICATED SKIN REPAIR DOUBLER FROM 2024-T3 0.071" PO NR 9005922 APPROXIMATE DIMENSION 8.825" BY 7.75". FABRICATED REPAIR FILLER FROM 2024-T3 0.063" PO NR 9006027 APPROXIMATE DIMENSION 1.25" BY .75" IAW B-7 27 SRM 53-30-3 FIGURE 1 AND SRM 53-30-3 FIGURE 2. FABRICATED NEW SHEAR TIE CLIP FROM 7075-T6 0.040 PO NR 9005892 APPROX IMATE DIMENSION 2" BY 6.75" IAW B-727 SRM 51-10-3 FIGURE 1 AND SRM 51-20-1 FIGURE 7 AND SRM 53-10-2 FIGURE 5. TREATED A 2 L 7 3 4F A3WE 2008022600027 20080226 00027 NM 2008 2 26 DHL2007742070 1 20071120 A 5330 SKIN BOEING 727 727225 1384077 NM BS 460 S20R DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 DENT ON RIGHT FUSELAGE SKIN BS 460 2" ABOVE STRINGER 20R. CUT OUT DAMAGE (DIMENSION 2.25" BY 1.125") IAW B-727 SRM 51-1 0-1 AND 53-30-3 FIGURE 1. FABRICATED REPAIR DOUBLER FROM 2024-T3 0.063" PO NR 9006027 (DIMENSION 10" BY 6.5") AND REPAI R FILLER FROM 2024-T3 0.050" PO NR 9005554 (DIMENSION 2.25" BY 1.125") IAW B-727 SRM 53-30-3 FIGURE 1 AND 53-30-2 FIGURE 2. TREATED AND PRIMED REPAIR PARTS IAW B-727 SRM 51-10-2. INSTALLED REPAIR AT RIGHT FUSELAGE SKIN BS 440 2" ABOVE STR INGER 20R IAW B-727 SRM 53-30-3 FIGURE 1 AND 51-30-2. 2 L 7 3 4F A3WE 2008022600032 20080226 00032 NM 2008 2 26 DHL2007742043 1 20071115 A 5330 SKIN BOEING 727 727225 1384077 NM BS 316 S3L DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 FUSELAGE EXTERNAL BS 316 ON STRINGER 3L HAS SKIN DENTED. EVALUATED DENTS ON BS 316 STRINGER 3L. A:0.9" Y:0.010" A/Y:90 AND A:1.1" Y:0.017" A/Y RATIO 64.71, A/Y RATIO WITHIN LIMITS BUT FOUND DENTS OUT OF LIMITS DUE TO DENTS ARE LOCATED OVER STRINGER IAW B-727 SRM 53-30-1 FIGURE 1. CUT OUT DAMAGED AREA IAW B-727 SRM 53-30-3 FIGURE 3 (DIMENSION 3.5" BY 1.25") . FABRICATED REPAIR DOUBLER FROM 2024-T3 0.050" PO NR 9005554 (DIMENSION 13.5" BY 7") AND REPAIR FILLER FROM 2024-T3 0. 040" PO NR 9005892 (DIMENSION LENGTH 3.5" BY .25" WIDE) IAW B-727 SRM 53-30-3 FIGURE 3 AND 53-30-2 FIGURE 2. TREATED AN D PRIMED PARTS AND AREA IAW B-727 SRM 51-10-2 AND INSTALLED REPAIR AT FUSELAGE SKIN BS 316 STRINGER 3L IAW B-727 SRM 53- 2 L 7 3 4F A3WE 2008022600033 20080226 00033 NM 2008 2 26 DHL2007742049 1 20071123 A 5320 ANGLE BOEING 727 727225 1384077 NM BS 1070 S22L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 EXFOLIATED CORROSION AFT PIT FRAME BS 1070 JUST ABOVE STRINGER 22L. CUT OUT DAMAGED AREA (DIMENSION 2.25" BY 2.25"). F ABRICATED REPAIR ANGLE FROM 7075-0 0.071" PO NR 7247111 (DIMENSION 13" BY 3.5") AND REPAIR FILLER FROM 7075-T6 0.063" PO NR 9005922 (DIMENSION 2.25" BY 2.25") IAW B-727 SRM 53-10-2 FIGURE 5 AND 51-40-3 FIGURE 1. HEAT TREATED REPAIR ANGLE T O T6 IAW FAS ENGINEERING REPORT NR 2-37153-801 REV A. TREATED AND PRIMED PARTS IAW B-727 SRM 51-10-2. INSTALLED REPAIR PART AT AFT PIT FRAME BS 1070 JUST ABOVE STRINGER 22L IAW B-727 SRM 51-40-3 FIGURE 1 AND 51-30-2. 2 L 7 3 4F A3WE 2008022600034 20080226 00034 NM 2008 2 26 DHL2007742064 1 20071117 A 5311 FRAME BOEING 727 727225 1384077 NM BS 1100 S2R5 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 DENTED FRAME AFT PIT BS 1110 ABOVE STRINGER 25R. REMOVED PREVIOUS REPAIR IAW B-727 SRM 51-30-2. CUT OUT DAMAGE (DIMENS ION 1" BY 1") AND FABRICATED REPAIR ANGLE FROM 7075-0 0.071" PO NR 7247111 (DIMENSION 16" NR 4.25") IAW B-727 SRM 51-40- 3 FIGURE 1 AND 53-10-2 FIGURE 5. HEAT TREATED ANGLE FROM 7075-0 TO 7075-T6 IAW FAS ENGINEERING REPORT NR 2-37153-801 RE V A. TREATED AND PRIMED PARTS AND AREA IAW B-727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B-727 SRM 51-30-2 AND 51-40-3 FIGURE 1. 2 L 7 3 4F A3WE 2008022600035 20080226 00035 NM 2008 2 26 DHL2007742067 1 20071219 A 5230 SEAL DEPRESSOR BOEING 727 727225 1384077 NM CARGO DOOR GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 C-1 DOOR SKIN GOUGED ALONG LOWER SURFACE. FOUND GOUGE OUT OF LIMITS IAW B-727 SRM 52-00-2. REMOVED C-1 DOOR LOWER SEAL DEPRESSOR IAW B-727 SRM 51-30-2. FABRICATED NEW DEPRESSOR FROM BAC 1496-383 2024-T3 PONR 7332283 (DIMENSION 44" LONG) IAW B-727 SRM 52-30-1 FIGURE 4, 51-20-1 AND 51-30-5. TREATED AND PRIMED AREA AND PARTS IAW B-727 SRM 51-10-2. INSTALLE D NEW C-1 DOOR LOWER SEAL DEPRESSOR IAW B-727 SRM 51-30-2. APPLIED LEVELING COMPOUND IN AREA IAW B-727 MM 20-60-1. 2 L 7 3 4F A3WE 2008022600037 20080226 00037 NM 2008 2 26 DHL2007742026 1 20071128 A 5322 SHEAR TIE BOEING 727 727225 1384077 NM BS 950E S28-29L DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 BS 950E BETWEEN STRINGER 28L AND 29L FRAME SHEAR TIE DAMAGED. CUT OUT DAMAGED SHEAR TIE (DIMENSION 6.75" BY 2") IAW B-7 27 SRM 53-10-4 FIGURE 15 AND 51-10-1. FABRICATED SHEAR TIE REPAIR FROM 7075-0 0.071" PO NR 7247111 (DIMENSION 6.75" BY 2") IAW B-727 SRM 53-10-4 FIGURE 15 AND SRM 53-10-2 FIGURE 5. HEAT TREATED SHEAR TIE REPAIR FROM 7075-0 TO 7075-T6 IAW FAS ENGINEERING REPORT NR2-37153-801 REV A. TREATED AND PRIMED PARTS IAW B-727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B-727 SRM 53-10-4 FIGURE 15 AND SRM 51-30-2 BS 950E BETWEEN STRINGER 28L AND 29L FRAME SHEAR TIE. 2 L 7 3 4F A3WE 2008022600038 20080226 00038 NM 2008 2 26 DHL2007742034 1 20071119 A 5522 SKIN BOEING 727 727225 1384077 NM RT ELEVATOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 RIGHT ELEVATOR TAB HAS LARGE LIGHTNING STRIKE ON UPPER TRAILING EDGE. CUT OUT LIGHTNING STRIKE DAMAGE 0.5" BY 0.75". F ABRICATED FILLER 0.5" BY 0.75" AND DOUBLER 2" BY 4" FROM 0.010" 2024-T3 PO NR 9003189 IAW B-727 SRM 55-20-2. BONDED FIL LER AND DOUBLER, CLEANED, PRIMED AND SEALED IAW B-727 SRM 51-40-20. TAB WEIGHT BEFORE REPAIR 11.170 LBS, TAB WEIGHT AFT ER REPAIR 11.175 LBS, WITHIN LIMITS IAW B-727 SRM 51-80. PERFORMED A LIGHTNING STRIKE CONDITIONAL INSPECTION OF RIGHT E LEVATOR TAB ASSEMBLY AND ELEVATOR ASSEMBLY. NO OTHER DEFECTS NOTED IAW B-727 ADV M/M 05-51-82. 2 L 7 3 4F A3WE 2008022600041 20080226 00041 NM 2008 2 26 DHL2007742069 1 20071203 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 460-480 S28R CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 E/E BAY, IN FUSELAGE LOWER LOBE STRINGER 28R BETWEEN STATION 460 TO 480 INSIDE HAT CHANNEL OF STRINGER RUNS THE LENGTH O F SURFACE CORROSION. REMOVED DAMAGED STRINGER BS 440 - BS 480 FROM PREVIOUS REPAIR SPLICE IAW B-727 SRM 51-30-2. FABRI CATED NEW STRINGER FILLER FROM BAC 1498-138 7075-T6 PO NR 7332258 APPROXIMATE DIMENSION 29" LONG. FABRICATED REPAIR SPL ICE FROM 7075-T6 0.040" PO NR 9005674 APPROXIMATE DIMENSION 13" BY 5" IAW B-727 SRM 53-10-3 FIGURE 1 AND SRM 53-10-2 FIG URE 9. TREATED AND PRIMED REPAIR PARTS IAW B-727 SRM 51-10-2. INSTALLED REPAIR PARTS AT BS 440 TO BS 480 STRINGER 28R IAW B-727 SRM 51-30-2 AND SRM 53-10-3 FIGURE 1. 2 L 7 3 4F A3WE 2008022500109 20080225 00109 NM 2008 2 25 2007UALA03937 1 20070923 A 5753 CARRIAGE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU T/E FLAP DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 LEFT OUTBOARD FOREFLAP OUTBOARD SEQUENCE CARRIAGE OUTBOARD SLIDER IS DAMAGED AND ATTACH BOLTS INSIDE FAIRING. REPLACED LEFT OUTBOARD FORE FLAP OUTBOARD SLIDER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022500249 20080225 00249 NM 2008 2 25 2007UALA05301 1 20071226 A 2110 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN PRESSURE UNKNOWN A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION DE DESCENT 1 WP 29 302UA 23643 CREW REPORT: LOST CABIN PSI AT 10000 DURING DESCENT. WARNING HORN WENT OFF. LANDED NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022600002 20080226 00002 NM 2008 2 26 DHL2007742066 1 20071203 A 5310 SUPPORT BEAM BOEING 727 727225 1384077 NM BS 1183 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 CRACK AT RIGHT HORIZONTAL SUPPORT "I" BEAM AFT PIT BS 1183 INBOARD WL 196. REMOVED RIGHT HORIZONTAL SUPPORT BEAM BS 118 3 IAW B-727 SRM 51-30-2. FABRICATED NEW "I" BEAM SUPPORT FROM BAC 1518-356 7075-T6 PO NR 7332188 APPROXIMATE DIMENSION 28.5" BY 3" IAW B-727 SRM 53-10-2 FIGURE 5 AND SRM 51-30-5. INSTALLED NEW "I" BEAM AT BS 1183 WL 196 IAW BA-727 SRM 51- 30-2. 2 L 7 3 4F A3WE 2008022600011 20080226 00011 NM 2008 2 26 DHL2007742035 1 20071113 A 5740 BRACKET BOEING 727 727225 1384077 NM NR 2 SLAT ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 NR 2 SLAT ACTUATOR UPPER MOUNT HAS PLAY WITH CRACK INDICATION AT INBOARD UPPER BOLT. VERIFIED BY NDT. REMOVED PREVIOUS DOUBLER AT NR 2 SLAT ACTUATOR MOUNT INBOARD BRACKET IAW B-727 SRM 51-30-2 FIGURE 1. C/W HFEC ON STIFFENER/WEB IAW B-72 7 NDTM PT 6, 51-00-00 FIGURE 23. NO CRACKS NOTED. FABRICATED NEW DOUBLER FROM 301 1/2 HARD 0.100" PO NR 9001425 DIMENS ION 7.675" BY 2.375" IAW SB 727-57-0130 FIGURE 1. PART AND AREA TREATED AND PRIMED IAW SB 727-57-0130 FIGURE 1. DOUBLE R INSTALLED ON NR 2 SLAT ACTUATOR MOUNT INBOARD BRACKET IAW SB 727-57-0130 FIGURE 1. 2 L 7 3 4F A3WE 2008022600023 20080226 00023 NM 2008 2 26 DHL2007742038 1 20071204 A 5740 ATTACH ANGLE BOEING 727 727225 1384077 NM NR 4 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 NR 4 SLAT LOWER TRAILING EDGE ACCESS PANEL ATTACH "L" ANGLE IS CRACKED AT UPSTOP PAD. REMOVED OUTBOARD NR 4 SLAT ACCESS PANEL AND BUMP STOP IAW B-727 SRM 51-30-2. NDT CRACK FOR END VERIFICATION IAW B-727 NDT MANUAL CH. 51-00-0 PT 6 FIGURE 23. CUT OUT 4 INCH SECTION OF ATTACH "L" ANGLE IAW B-727 SRM 51-40-2. FABRICATED NEW ANGLE REPAIR APPROXIMATE DIMENSI ON 27.5" BY 1.5" AND FILLER APPROXIMATE DIMENSION 9" BY 1.5" FROM EXTRUSION BAC 1514-159 2024-T3511 PO NR 7332223 IAW B- 727 SRM 57-50-2 FIGURE 2. TREATED AND PRIMED ANGLE REPAIR AND FILLER IAW B-727 SRM 51-10-2. INSTALLED NEW REPAIR PARTS AT NR 4 SLAT LOWER TRAILING EDGE IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008022600003 20080226 00003 NM 2008 2 26 DHL2007742021 1 20071123 A 5320 INTERCOSTAL BOEING 727 727225 1384077 NM BS 1148-1166 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AFT PIT INTERCOSTAL BETWEEN BS 1148 - 1166 JUST BELOW STRINGER 26R HAS LOWER ANGLE CRACKED AND CORRODED. REMOVED TRANSI TION PANEL SECTION FROM BS 1135 TO 1166 RIGHT, INTERCOSTAL AND CRACKED LOWER ANGLE IAW B-727 SRM 51-30-3. FABRICATED NE W ANGLE FROM 7075-T6 0.063" PO NR 9005922 (DIMENSION 16.75" BY 2.25") IAW B-727 SRM 53-10-2 FIGURE 5 AND 51-20-1. TREATE D AND PRIMED NEW ANGLE IAW B-727 SRM 51-10-2. INSTALLED NEW ANGLE IAW B-727 SRM 51-30-2, REINSTALLED INTERCOSTAL AND TR ANSITION PANEL IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008022600029 20080226 00029 NM 2008 2 26 DHL2007742044 1 20071126 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 720F-740 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 FORWARD CARGO COMPARTMENT STRINGER 27R IS HEAVILY CORRODED BETWEEN STATION 720F AND 740. CUT OUT DAMAGED AREA 10.5" STR INGER 27R BETWEEN STATION 720F-740 IAW B-727 SRM 53-10-3 FIGURE 1. FABRICATED NEW SECTION MATERIAL USED BAC 1498-147 0. 090" 7075-T6 DIMENSION 10.5" AND SPLICED BAC1498-131 7075-T6 PO NR 733223, DIMENSION 11" IAW B-727 SRM 53-10-3 FIGURE 1. TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED REPAIR PARTS IAW B-727 SRM 53-10-3 FIGURE 1 AND 51-30-2. 2 L 7 3 4F A3WE 2008022700020 20080227 00020 NM 2008 2 27 DHL2007748007 1 20070928 A 5311 FRAME BOEING 727 727225 1384077 NM BS 660 S17R DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 FRAME DENTED IN MAIN CABIN BS 660 STRINGER 17R. REMOVED PREVIOUS REPAIR AT MAIN CABIN BS 660 STRINGER 17R IAW B-727 SRM 51-30-2. FABRICATED DOUBLER IAW SRM 51-40-3 FIGURE 1 AND 53-10-2 FIGURE 2. PART AND AREA TREATED AND PRIMED IAW SRM 5 1-10-2. DOUBLER INSTALLED AT BS 660 STRINGER 17R IAW B-727 SRM 51-40-3 FIGURE 1. 2 L 7 3 4F A3WE 2008022700021 20080227 00021 NM 2008 2 27 DHL2007748012 1 20071003 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 720B CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 MAIN CABIN STRINGER 15 CRACKED AT BS 720B. CUT OUT DAMAGE AREA DIMENSION CUT OUT IAW SRM 53-10-3 FIGURE 5. FABRICATED REPAIR CHANNEL, FILLER, & TAPERED FILLER IAW SRM 53-10-3 FIGURE 5 AND 51-30-5. TREATED AND PRIMED PARTS IAW SRM 51-10- 2. INSTALLED REPAIR AT STRINGER 15 BS 720B IAW SRM 53-10-23 FIGURE 5. 2 L 7 3 4F A3WE 2008022700022 20080227 00022 NM 2008 2 27 DHL2007748018 1 20071003 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 590-689.5 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 CABIN SEAT TRACK CORRODED RBL 24 BS 590 TO 689.5. REMOVED SEAT TRACK IAW SRM 53-10-5 FIGURE 1. FABRICATED NEW SEAT TRA CK SECTION. FABRICATED 4 ANGLES AND FABRICATED ONE STRAP IAW SRM 53-10-5 FIGURE 1. PARTS AND AREA TREATED AND PRIMED IA W SRM 51-10-2. SEAT TRACK, STRAP AND 4 ANGLES INSTALLED IAW SRM 53-10-5 FIGURE 1. 2 L 7 3 4F A3WE 2008022700032 20080227 00032 NM 2008 2 27 DHL2007748011 1 20070928 A 5311 FRAME BOEING 727 727225 1384077 NM BS 560 S17R DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 FRAME DENTED IN MAIN CABIN BS 560 STRINGER 17R. REMOVED PREVIOUS REPAIR AT MAIN CABIN BS 560 STRINGER 17R IAW SRM 51-30 -2. FABRICATED NEW DOUBLER IAW SRM 51-40-3 FIGURE 1 AND 53-10-2 FIGURE 2. PART AND AREA TREATED AND PRIMED IAW SRM 51- 10-2 FIGURE 1. DOUBLER INSTALLED IAW SRM 51-40-3 FIGURE 1. 2 L 7 3 4F A3WE 2008022700048 20080227 00048 NM 2008 2 27 DHL2007748020 1 20071009 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 520-690 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 CABIN AREA SEAT TRACK CORRODED AT LBL 25 BS 520 TO 690. REMOVED SEAT TRACK SECTION FROM STATION 480 TO 690 LBL 25 IAW S RM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-5 FIGURE 1 AND 53-10-2 FIGURE 7, SPLICE ANGLE REPAIR INSTALLED AT BS 590 LBL 25 IAW B-727 SRM 53-10-5 FIGURE 1. ALL PARTS AND AREA TREATED AND PRIMED IAW B-727 SRM 51-10-2. 2 L 7 3 4F A3WE 2008022700049 20080227 00049 NM 2008 2 27 DHL2007748021 1 20071004 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 344-480 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 CABIN AREA SEAT TRACK CORRODED AT BS 344-480 LBL 24. REMOVED DAMAGED SEAT TRACK SECTION BS 344-480 LBL 24 IAW SRM 51-30 -2. FABRICATED NEW SEAT TRACK FROM IAW DRAWING NR 2902. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008022700084 20080227 00084 NM 2008 2 27 DHL2007748014 1 20071005 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 950F-1030 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 SEAT TRACK AT STATION 950F-1030 RBL 45 HAS CORROSION. REMOVED SEAT TRACK OUT OF LIMITS IAW SRM 51-30-2. FABRICATED, LO CATED AND DRILLED NEW SEAT TRACK, 2 ANGLES AND 2 STRAP IAW SRM 53-10-5 FIGURE 1 AND 51-30-5. TREATED AND PRIMED PARTS A ND AREA IAW SRM 51-10-2. INSTALLED NEW SEAT TRACK AND PARTS IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008022600004 20080226 00004 NM 2008 2 26 DHL2007742023 1 20071203 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 460-480 S28L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 FUSELAGE LOWER LOBE (E/E BAY) STATION 480-460 STRINGER 28L INSIDE HAT CHANNEL OF STRINGER RUNS THE LENGTH OF LIGHT SURFA CE CORROSION. REMOVED STRINGER FROM BS 460 - BS 480 PREVIOUS SPLICE IAW B-727 SRM 51-30-2. FABRICATED NEW STRINGER FIL LER FROM BAS 1498-138 7075-T6 PO NR 7332258 APPROXIMATE DIMENSION 29" LENGTH. FABRICATED STRINGER SPLICE FROM 7075-T6 0 .040" PO NR 9005634 APPROXIMATE DIMENSION 13" BY 5" IAW B-727 SRM 53-10-3 FIGURE 1 AND SRM 53-10-2 FIGURE 9. INSTALLED NEW STRINGER REPAIR PARTS AT BS 460 TO BS 480 STRINGER 28L IAW B-727 SRM 51-30-2 AND SRM 53-10-3 FIGURE 1. 2 L 7 3 4F A3WE 2008022600022 20080226 00022 NM 2008 2 26 DHL2007742037 1 20071119 A 5754 RIB BOEING 727 727225 1384077 NM NR 3 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 NR 3 SLAT RIB HAS SMALL CRACK ON INBOARD SIDE OF ACTUATOR ATTACHMENT, VERIFIED BY NDT. REMOVED 3 RIBS FROM NR 3 SLAT IA W B-727 SRM 51-30-2. INSTALLED 2 NEW RIBS IN PLACE, LOCATED AND DRILLED IAW B-727 SRM 51-30-5. REINSTALLED 1 RIB (REMO VED FOR ACCESS) IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008022600030 20080226 00030 NM 2008 2 26 DHL2007742046 1 20071201 A 5753 SKIN BOEING 727 727225 1384077 NM LWS 130 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 LEFT WING INBOARD FOREFLAP HAS TWO AREAS OF DELAMINATION ON LOWER SURFACE, WBL 130. CUT OUT DELAMINATED AREA OF LEFT WI NG INBOARD FOREFLAP WBL 130 10" BY 11". REMOVED DAMAGED CORE 10" BY 11". CUT AND TRIMMED NEW CORE PLUG 10" BY 11" FROM PED3.1 3/16 5052 NA 4.0 PO NR 6261123 IAW B-727 SRM 51-40-20. BONDED CORE PLUG AND FABRICATED DOUBLER 15" BY 15" FROM 0.016" 2024-T3 PO NR 9004174 IAW B-727 SRM 57-50-2. BONDED DOUBLER, CLEANED, PRIMED AND SEALED IAW B-727 SRM 51-40-20. 2 L 7 3 4F A3WE 2008022600031 20080226 00031 NM 2008 2 26 DHL2007742033 1 20071109 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 1110 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 SEAT TRACK LBL 48 STATION 1110 DAMAGED. REMOVED SEAT TRACK FROM STATION 1110 TO 1148 LBL 48 IAW B-727 SRM 51-30-2. FAB RICATED SEAT TRACK FROM P/N BAC 1570-792 7075-T6 PO NR 9005692 APPROXIMATE DIMENSION 46" IAW B-727 SRM 53-10-2 FIGURE 7 AND 53-10-5 FIGURE 1. TREATED AND PRIMED PARTS AND AREA IAW B-727 SRM 51-10-2. INSTALLED SEAT TRACK AT STATION 1110 TO 1148 LBL 48 IAW B-727 SRM 51-30-2 AND 53-10-5. 2 L 7 3 4F A3WE 2008022600039 20080226 00039 NM 2008 2 26 DHL2007742051 1 20071204 A 5311 FRAME BOEING 727 727225 1384077 NM BS 380 S10R DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 FUSELAGE FRAME STATION 380, FRAME AND STRAPS HAVE NUMEROUS HOLES DRILLED THROUGH FROM STRINGER 5R TO STRINGER 10R. REMO VED STRAPS AND FRAME ATTACHED PARTS FOR ACCESS IAW B-727 SRM 51-30-2. CUT OUT DAMAGED SECTION OF FRAME (DIMENSION 26" B Y 5") IAW B-727 SRM 51-10-1. FABRICATED NEW FRAME SECTION FROM 7075-0 0.080" PO NR 9005314 (DIMENSION 26.75" BY 5") AND REPAIR ANGLE FROM 7075-0 0.090" PO NR 7185240 (DIMENSION 9.25" BY 3.25") IAW B-727 SRM 51-40-3 FIGURE 1 AND 53-10-2 FIG URE 3. HEAT TREATED PARTS TO T6 IAW FAS ENGINEERING REPORT NR 2-37153-801 REV A. TREATED AND PRIMED PARTS IAW B-727 SR M 51-10-2. INSTALLED REPAIR PARTS AT FRAME STATION 380 STRINGER 5R TO 10R IAW B-727 SRM 51-40-3 FIGURE 1 AND 51-30-2. 2 L 7 3 4F A3WE 2008022700012 20080227 00012 EA 2008 2 27 COMA0860113 1 20070206 A 3010 356024310 SENSING ELEMENT CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYSTEM FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 487CA 7729 FLIGHT 5693 - RECEIVED ANTI-ICE DUCT WARNING MESSAGE WITH RIGHT FUSELAGE ON EICAS SYNOPTIC PAGE. REPLACED RIGHT FUSELAG E SENSING ELEMENT, AFT BAY SECTION. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008022700034 20080227 00034 NM 2008 2 27 DHL2007748028 1 20071018 A 5311 FRAME BOEING 727 727225 1384077 NM BS 348.2 DENTED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 748DH 22440 REWORK DUE TO IMPROPER REPAIR FRAME AT 9G BARRIER BS 348.2 IS DENTED BETWEEN STRINGER 5L AND STRINGER 6L. REMOVED SRM R EPAIR AT FRAME STATION 348 STRINGER 5L - 6L IAW SRM 51-30-2. CUT OUT FRAME SECTION IAW DRAWING NR AE727-2-360. FABRICA TED AND INSTALLED DOUBLER AND REPAIR ANGLE IAW DRAWING NR AE727-2-360. HEAT TREATED TO T6 IAW ENGINEERING REPORT NR 2-3 7153-801 REV A ALL PARTS AND AREA TREATED AND PRIMED IAW SRM 51-10-2. 2 L 7 3 4F A3WE 2008022700083 20080227 00083 NM 2008 2 27 DHL2007748004 1 20071002 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 848.95-870 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 MAIN CABIN STATION 848.95-870 LBL 45 SEAT TRACK FLANGES HAS CORROSION ON BOTH. REMOVED SECTION OF SEAT TRACK IAW SRM 51 -30-2. FABRICATED SECTION SEAT TRACK IAW SRM 53-10-2 FIGURE 7 AND 51-30-5. TREATED AND PRIMED IAW SRM 51-10-2. INSTAL LED SECTION SEAT TRACK IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008022700131 20080227 00131 CE 2008 2 27 U5QA06008 1 20071101 A 3340 2401S CONTROL UNIT LEAR 60 60LEAR 5170707 CE CABIN BURNED E U5QA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 05 198HB 3746 60198 SMELLED ELECTRICAL ODOR, RECOG PULSE BREAKER POPPED, RETURNED TO CMH AIRPORT. UNIT BURNED INTERNALY, REPLACED UNIT, AND OPS CHECK NORMAL. 2 L 7 2 4F RT A10CE 2008022700151 20080227 00151 NM 2008 2 27 DHL2007748029 1 20071008 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 344-480 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 MAIN CARGO CABIN SEAT TRACK CORRODED AT BS 344 TO 480 RBL 24. REMOVED SEAT TRACK SECTION ON MAIN CARGO CABIN BS 344 TO BS 480 RBL 24 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK LOCATED AND DRILLED. MATERIAL USED BAC 1520-792-7178-T6511 PO NR 9005692 DIMENSION 136" LONG IAW DRAWING NR 2902 REV A AND 51-30-5. TREATED AND PRIMED PART AND AREA IAW SRM 51-10-2 . INSTALLED NEW SEAT TRACK IAW DRAWING NR 2902 REV A AND 51-30-2. 2 L 7 3 4F A3WE 2008022700157 20080227 00157 NM 2008 2 27 DHL2007748009 1 20070928 A 5311 FRAME BOEING 727 727225 1384077 NM BS 600 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 FRAME DENTED IN MAIN CABIN BS 600 STRINGER 17R. REMOVED PREVIOUS REPAIR AT MAIN CABIN BS 600 STRINGER 17R IAW B-727 SRM 51-30-2. FABRICATED NEW DOUBLER FROM 7075-T6 0.063" PO NR 9005773 DIMENSION 10" BY 5" IAW B-727 SRM 51-40-3 FIGURE 1 A ND 53-10-2 FIGURE 3. PART AND AREA TREATED AND PRIMED IAW B-727 SRM 51-10-2. DOUBLER INSTALLED AT BS 600 STRINGER 17R IAW B-727 SRM 51-40-3 FIGURE 1. 2 L 7 3 4F A3WE 2008022700158 20080227 00158 NM 2008 2 27 DHL2007748006 1 20071001 A 5311 FRAME BOEING 727 727225 1384077 NM BS 540 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 FRAME DENTED IN MAIN CABIN BS 540 STRINGER 17R. REMOVED PREVIOUS REPAIR AT MAIN CABIN BS 540 STRINGER 17R IAW B-727 SRM 51-30-2. FABRICATED NEW FRAME REPAIR MATERIAL USED 7075-T6 0.063" PO NR 9005713 DIMENSION (9.25 BY 4.875") IAW B-727 S RM 53-10-2 FIGURE 3 AND 51-40-3 FIGURE 1. TREATED AND PRIMED PART AND AREA IAW B-727 SRM 51-10-2. INSTALLED NEW FRAME REPAIR AT MAIN CABIN BS 540 STRINGER 17R IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008022700160 20080227 00160 NM 2008 2 27 DHL2007748010 1 20070929 A 5311 FRAME BOEING 727 727225 1384077 NM BS 580 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 FRAME DENTED IN MAIN CABIN BS 580 STRINGER 17R. REMOVED PREVIOUS REPAIR AT MAIN CABIN BS 580 STRINGER 17R IAW B-727 SRM 51-30-2. FABRICATED NEW DOUBLER FROM 7075-T6 0.063" PO NR 9005773 DIMENSION 10" BY 5" IAW B-727 SRM 51-40-3 FIGURE 1 A ND 53-10-2 FIGURE 3. PART AND AREA TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED NEW PART IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008022700162 20080227 00162 NM 2008 2 27 DHL2007748016 1 20071018 A 5311 FRAME BOEING 727 727225 1384077 NM BS 640 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 FORWARD CARGO COMPARTMENT FRAME 640 AREA SHOW SEVERAL FASTENER HOLES IMPROPERLY PERFORMED. BLENDED DAMAGED AREA OF STUB FRAME AT STATION 638 BETWEEN 23L AND 25L. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SIE EO NR SIE-N748DH-10-16-07 MATERIAL USED 0.100" 7075-0 23.75" BY 1.5" PO NR 6149299. HEAT TREATED TO T6 CONDITION IAW FASI ENGINEERING REPORT NR 2 -37153-801 REV A. ALL PARTS AND AREA TREATED AND PRIMED IAW B-727 SRM 51-10-2. 2 L 7 3 4F A3WE 2008022700163 20080227 00163 NM 2008 2 27 DHL2007748022 1 20071008 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 344 - 480 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 CABIN AREA SEAT TRACK CORRODED AT LBL 45 BS 344 TO 480. REMOVED DAMAGED SECTION OF SEAT TRACK IAW B-727 SRM 51-30-2 FRO M STATION 344 TO 480 LBL 45. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW VENTURA AEROSPACE DRAWING NR 2902 MATE RIAL USED BAC 1520-792 7178-T611 PO NR 9005692 136" LONG. TREATED AND PRIMED PARTS AND AREA IAW B-727 SRM 51-10-2. 2 L 7 3 4F A3WE 2008022700164 20080227 00164 NM 2008 2 27 DHL2007748026 1 20071016 A 5330 SKIN BOEING 727 727225 1384077 NM BS 700 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 POSSIBLE CORROSION ON SHEAR TIE BS 700 INBOARD OF STRINGER 27R. FABRICATED SKIN DOUBLER REPAIR IAW B-727 SRM 53-30-3 FI GURE 3 AND 53-30-2, AND 2 FRAME SHEAR TIE REPAIR DOUBLERS IAW B-727 SRM 53-10-4 FIGURE 13 AND 14 AT BS 700 STRINGER 27R. MATERIAL USED SKIN DOUBLER 0.071" 2024-T3 16" BY 15.125" PO NR 9005773, AFT SHEAR TIE 0.050" 7075-T6 1" BY 1" BY 7.5" PO NR 9005685, FORWARD SHEAR TIE 0.063" 7075-T6 6" BY 4.25" PO NR 9005685. ALL PARTS AND AREA TREATED AND PRIMED IAW B- 727 SRM 51-10-2. INSTALLED SKIN DOUBLER AND SHEAR TIE PARTS IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008022700201 20080227 00201 NM 2008 2 27 DHL2007793007 1 20071204 A 5322 SHEAR TIE BOEING 727 727247 138408F NM BS 344 CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 FRAME AT BS 344 CHAFING AT 9G BARRIER SHEAR TIE STRINGER 3R. REMOVED AND REPLACED ATTACH ANGLE (SHEAR TIE) AT STRINGER 3R P/N 2942-3 PO NR 734151 IAW DRAWING NR 2936 VENTURA AEROSPACE REV B AND AEI BOEING 727-200 FREIGHTER M/M CHAPTER 25 P AGE 20 REV G MARCH 28, 2005 ON 9G BARRIER. 2 L 7 3 4F A3WE 2008022700203 20080227 00203 NM 2008 2 27 DHL2007793008 1 20071204 A 5322 SHEAR TIE BOEING 727 727247 138408F NM BS 344 CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 FRAME AT BS 344 CHAFFING AT 9G BARRIER SHEAR TIE STRINGER 4R. REMOVED AND REPLACED ATTACH ANGLE (SHEAR TIE) AT STRINGER 3R P/N 2942-3 PO NR 734151 IAW DRAWING NR 2936 VENTURA AEROSPACE REV B AND AEI BOEING 727-200 FREIGHTER M/M CHAPTER 25 PAGE 20 REV G MARCH 28, 2005 ON 9G BARRIER. 2 L 7 3 4F A3WE 2008022700204 20080227 00204 NM 2008 2 27 DHL2007793009 1 20071204 A 5322 SHEAR TIE BOEING 727 727247 138408F NM BS 344 CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 FRAME AT BS 344 CHAFING AT 9G BARRIER SHEAR TIE STRINGER 5R. REMOVED AND REPLACED ATTACH ANGLE (SHEAR TIE) AT STRINGER 3R P/N 2942-3 PO NR 734151 IAW DRAWING NR 2936 VENTURA AEROSPACE REV B AND AEI BOEING 727-200 FREIGHTER M/M CHAPTER 25 P AGE 20 REV G MARCH 28, 2005 ON 9G BARRIER. 2 L 7 3 4F A3WE 2008022700205 20080227 00205 NM 2008 2 27 DHL2007793010 1 20071204 A 5322 SHEAR TIE BOEING 727 727247 138408F NM BS 344 CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 FRAME AT BS 344 CHAFING AT 9G BARRIER SHEAR TIE STRINGER 6R. REMOVED AND REPLACED ATTACH ANGLE (SHEAR TIE) AT STRINGER 3R P/N 2942-3 PO NR 734151 IAW DRAWING NR 2936 VENTURA AEROSPACE REV B AND AEI BOEING 727-200 FREIGHTER M/M CHAPTER 25 P AGE 20 REV G MARCH 28, 2005 ON 9G BARRIER. 2 L 7 3 4F A3WE 2008022700207 20080227 00207 NM 2008 2 27 DHL2007793012 1 20071204 A 5322 SHEAR TIE BOEING 727 727247 138408F NM BS 344 CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 FRAME AT BS 344 CHAFING AT 9G BARRIER SHEAR TIE STRINGER 9R. REMOVED AND REPLACED ATTACH ANGLE (SHEAR TIE) AT STRINGER 3R P/N 2942-3 PO NR 734151 IAW DRAWING NR 2936 VENTURA AEROSPACE REV B AND AEI BOEING 727-200 FREIGHTER M/M CHAPTER 25 P AGE 20 REV G MARCH 28, 2005 ON 9G BARRIER. 2 L 7 3 4F A3WE 2008022700208 20080227 00208 NM 2008 2 27 DHL2007793013 1 20070204 A 5322 SHEAR TIE BOEING 727 727247 138408F NM BS 344 CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 FRAME AT BS 344 CHAFING AT 9G BARRIER SHEAR TIE STRINGER 10R. REMOVED AND REPLACED ATTACH ANGLE (SHEAR TIE) AT STRINGER 3R P/N 2942-3 PO NR 734151 IAW DRAWING NR 2936 VENTURA AEROSPACE REV B AND AEI BOEING 727-200 FREIGHTER M/M CHAPTER 25 PAGE 20 REV G MARCH 28, 2005 ON 9G BARRIER. 2 L 7 3 4F A3WE 2008022700210 20080227 00210 NM 2008 2 27 DHL2007793022 1 20071204 A 7160 NOSE COWL BOEING 727 727247 138408F NM NR 3 NACELLE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 NR 3 ENGINE NOSE COWL HAS DENTS ON INBOARD SIDE 3 O'CLOCK POSITION NAC STATION 99.3. CUT OUT DAMAGE AREA AT NR 3 ENGINE NOSE COWL INBOARD SIDE AT 3 O'CLOCK POSITION. FABRICATED DOUBLER OUT 2024-T3 0.040" IAW B-727 SRM 54-30-3 AND 54-30-2. FABRICATED FILLER OUT OF 2024-T3 0.032" IAW B-727 SRM 54-30-3 AND 54-30-2. INSTALLED REPAIR DOUBLER AND FILLER IAW B- 727 SRM 54-30-3. REPAIR DOUBLER 5.5" BY 9.5", FILLER 2.3" BY 3.2", ACCESS DOOR 6" DIAMETER, ACCESS DOOR RING 6.5" DIAME TER, AND ACCESS DOOR RING DOUBLER 4" BY 1.5". 2 L 7 3 4F A3WE 2008022700023 20080227 00023 NM 2008 2 27 DHL2007748023 1 20071005 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 480-680 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 CABIN SEAT TRACK CORRODED AT BS 480 TO 680 LBL 45. REMOVED SEAT TRACK OUT OF LIMITS IAW SRM 51-30-2. FABRICATED, LOCAT ED AND DRILLED 2 NEW SEAT TRACKS, 2 ANGLES AND 1 STRAP IAW SRM 53-10-5 FIGURE 1 AND 51-30-5. TREATED AND PRIMED PARTS A ND SEAT TRACK IAW SRM 51-10-2. INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008022700033 20080227 00033 NM 2008 2 27 DHL2007748019 1 20071008 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 500-690 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 CABIN AREA SEAT TRACK CORRODED AT BS 500 TO 690 RBL 45. REMOVED SEAT TRACK OUT OF LIMITS IAW SRM 51-30-2. FABRICATED N EW SEAT TRACK, FABRICATED TWO ANGLES AND FABRICATED STRAP IAW SRM 53-10-5 FIGURE 1. TREATED AND PRIMED SEAT TRACK PARTS AND AREA IAW SRM 51-10-2. INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008022700154 20080227 00154 NM 2008 2 27 DHL2007748003 1 20070929 A 5311 FRAME BOEING 727 727225 1384077 NM BS 520 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 FRAME DENTED IN MAIN CABIN BS 520 AT STRINGER 17R. REMOVED PREVIOUS REPAIR AT MAIN CABIN BS 520 STRINGER 17R IAW B-727 SRM 51-30-2. FABRICATED NEW REPAIR MATERIAL USED 7075-T6 0.063" PO NR 9005773 DIMENSION 9" BY 5" IAW B-727 SRM 51-40-3 FIGURE 1 AND 53-10-2 FIGURE 3. TREATED AND PRIMED PART AND AREA IAW B-727 SRM 51-10-2. INSTALLED NEW FRAME REPAIR IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008022700156 20080227 00156 NM 2008 2 27 DHL2007748005 1 20071002 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 848-870 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 MAIN CABIN STATION 848.95 TO 870 LBL 24 SEAT TRACK FLANGE HAS CORROSION BOTH SIDES. REMOVED SEAT TRACK SECTION AT MAIN CABIN STATION 848.95 TO 870 LBL 24 IAW B-727 SRM 51-30-2. FABRICATED SECTION SEAT TRACK MATERIAL USED BAC 1520-1466 717 8-T6511 PO NR 730788 DIMENSION 16" LONG IAW B-727 SRM 53-10-2 FIGURE 7 AND 51-30-5. TREATED AND PRIMED IAW B-727 SRM 51 -10-2. INSTALLED SECTION SEAT TRACK STATION 848.95 TO 870 LBL 24 IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008022700217 20080227 00217 NM 2008 2 27 UPS08M51659 1 20071207 A 5320 A5A7114523 SPLICE DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C CENTER CARGO / AT STATION 1538 LONGERON 51RT FOUND SUSPECTED CRACK ON SPLICE DOUBLER. HFEC INSP C/O P ER DAC NDTSPM R.13,06-10-01.001 & FOUND CRACK APPROX 1.5" IN LENGTH. CRACK SPLICE REMOVED PER SRM 51-33-01 V.II R.35. NEW SPLICE P/N:A5A7114-523 FAB PER DWG A5A7114. FPI C/O PER DAC NDTSPM PT 08 E 13 ON FAB SPLICE & FOUND NO CRACK EVIDEN T. NEW SPLICE INSTALLED AS PER SRM 51-33-01 VOL II REV 35. 2 L 7 3 4F RT A22WE 2008022700267 20080227 00267 NM 2008 2 27 DHL2007748015 1 20071003 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 870 - 930 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 MAIN CABIN STATION 870 TO 930 LBL45 SEAT TRACK FLANGE HAS CORROSION. REMOVED SEAT TRACK SECTION AT MAIN CABIN STATION 8 70 TO 930 LBL45 IAW B-727 SRM 51-30-2. FABRICATED NEW SECTION SEAT TRACK MATERIAL USED BAC 1520-792-7178-T6 DIMENSION 9 1" IAW B-727 SRM 53-10-5 FIGURE 1. TREATED AND PRIMED PART IAW B-727 SRM 51-10-2. INSTALLED NEW SEAT TRACK SECTION AT STATION 870 TO 930 LBL45 IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008022700323 20080227 00323 NM 2008 2 27 DHL2007748030 1 20071015 A 5322 SHEAR TIE BOEING 727 727225 1384077 NM BS 720 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 FORWARD PIT FORWARD SIDE OF FRAME BOTTOM FLANGE AT BS 720 HAS CRACK OUTBOARD OF STRINGER 28R. CUT OUT DAMAGED SECTION A T SHEAR TIE (FRAME) IN FORWARD PIT BS 720 OUTBOARD OF STRINGER 28R IAW B-727 SRM 53-10-4 FIGURE 13 5" BY 2". FABRICATED AND INSTALLED SHEAR TIE REPAIR DOUBLER IAW B-727 SRM 53-10-4 FIGURE 13, MATERIAL USED 0.053" 7075-T6 6" BY 4.5" PO NR 9 005682. ALL PARTS AND AREA TREATED AND PRIMED IAW B-727 SRM 51-10-2. 2 L 7 3 4F A3WE 2008022700031 20080227 00031 NM 2008 2 27 DHL2007748008 1 20070928 A 5311 FRAME BOEING 727 727225 1384077 NM BS 640 S17R DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 FRAME DENTED IN MAIN CABIN BS 640 STRINGER 17R. REMOVED PREVIOUS REPAIR AT MAIN CABIN BS 640 STRINGER 17R IAW SRM 51-30 -2. FABRICATED NEW DOUBLER IAW SRM 51-40-3 FIGURE 1 AND 53-10-2 FIGURE 3. PART AND AREA TREATED AND PRIMED IAW SRM 51- 10-2 FIGURE 1. DOUBLER INSTALLED IAW SRM 51-40-3 FIGURE 1. 2 L 7 3 4F A3WE 2008022700047 20080227 00047 NM 2008 2 27 DHL2007748001 1 20071022 A 5312 BULKHEAD BOEING 727 727225 1384077 NM BS 870 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 RIGHT WW BS 870 BELOW LEAD CONTROL VALVE, BULKHEAD HAS 2 INCH CRACK. CUT OUT DAMAGED AREA BELOW APU LEAD CONTROL, CUT OUT 2" BY .75". FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 53-10-9 FIGURE 5. HEAT TREATED TO 150-190 KSI PER SPE C PO NR 7307279. ALL PARTS TREATED AND PRIMED IAW SRM 51-10-2. 2 L 7 3 4F A3WE 2008022700087 20080227 00087 NM 2008 2 27 DHL2007748027 1 20071008 A 5330 SKIN BOEING 727 727225 1384077 NM BS 1342-1354 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 2 EACH DENTS HAVE INDICATION OF CRACKS FROM HFEC INSPECTION. CUT OUT DAMAGED AREA AT RT FUSELAGE SKIN STRINGER 19R BETW EEN BS 1342.4 TO BS 1354.30 IAW SRM 54-30-3 FIGURE 7. FABRICATED DOUBLER REPAIR IAW SRM 54-30-2 FIGURE 4 AND 51-30-2. TREATED AND PRIMED PART AND AREA IAW SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW SRM 54-30-3 FIGURE 7 AND 51-30-2. 2 L 7 3 4F A3WE 2008022700206 20080227 00206 NM 2008 2 27 DHL2007793011 1 20071204 A 5322 SHEAR TIE BOEING 727 727247 138408F NM BS 344 CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 FRAME AT BS 344 CHAFING AT 9G BARRIER SHEAR TIE STRINGER 8R. REMOVED AND REPLACED ATTACH ANGLE (SHEAR TIE) AT STRINGER 3R P/N 2942-3 PO NR 734151 IAW DRAWING NR 2936 VENTURA AEROSPACE REV B AND AEI BOEING 727-200 FREIGHTER M/M CHAPTER 25 P AGE 20 REV G MARCH 28, 2005 ON 9G BARRIER. 2 L 7 3 4F A3WE 2008022700300 20080227 00300 NM 2008 2 27 DHL2007748031 1 20071016 A 5330 SKIN BOEING 727 727225 1384077 NM BS 1342 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 2 EACH DENTS HAVE INDICATION OF CRACK HFEC INSPECTION. REMOVED PREVIOUS REPAIR AT FUSELAGE SKIN RIGHT 1342 STRINGER 19R IAW B-727 SRM 51-30-2. FABRICATED DOUBLER REPAIR MATERIAL USED 2024-T3 0.063" PO NR 9005773 DIMENSION 11.5" BY 5.5" IA W B-727 SRM 54-30-3 FIGURE 7 AND 54-30-2 FIGURE 4. TREATED AND PRIMED PART AND AREA IAW B-727 SRM 51-10-2. INSTALLED N EW DOUBLER IAW B-727 SRM 51-30-2 AND 54-30-3 FIGURE 7. 2 L 7 3 4F A3WE 2008022700209 20080227 00209 NM 2008 2 27 DHL2007793014 1 20071204 A 5322 SHEAR TIE BOEING 727 727247 138408F NM BS 344 CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 FRAME AT BS 344 CHAFING AT 9G BARRIER SHEAR TIE STRINGER 11R. REMOVED AND REPLACED ATTACH ANGLE (SHEAR TIE) AT STRINGER 3R P/N 2942-3 PO NR 734151 IAW DRAWING NR 2936 VENTURA AEROSPACE REV B AND AEI BOEING 727-200 FREIGHTER M/M CHAPTER 25 PAGE 20 REV G MARCH 28, 2005 ON 9G BARRIER. 2 L 7 3 4F A3WE 2008022700211 20080227 00211 NM 2008 2 27 DHL2007793026 1 20071201 A 5311 FRAME BOEING 727 727247 138408F NM BS 1090 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 AFT CARGO COMPARTMENT FRAME AT STATION 1090 UPPER FLANGE IS DENTED BETWEEN STRINGER 27L TO 26L. CUT OUT DAMAGE AREA AT AFT CARGO COMPARTMENT FRAME STATION 1090 BETWEEN STRINGER 27L TO 26L IAW B-727 SRM 51-40-3 FIGURE 1 DIMENSION CUT OUT .7 5" BY .75". FABRICATED FRAME REPAIR MATERIAL USED 7075-0 0.071" PO NR 724711 DIMENSION 10.25" BY 4.25" IAW B-727 SRM 51 -40-3 FIGURE 1 AND 53-10-2 FIGURE 5. HEAT TREATED PART FROM 7075-0 TO 7075-T6 IAW FLIGHTSTAR AIRCRAFT SERVICES FORM NR FAS0115 REV 11. TREATED AND PRIMED PART IAW B-727 SRM 51-10-2. INSTALLED FRAME REPAIR IAW B-727 SRM 51-30-2 AND 53-10- 2 FIGURE 5. 2 L 7 3 4F A3WE 2008022700222 20080227 00222 EU 2008 2 27 MAC120701 1 20071215 A 7603 CONTROL CABLE AEROSP ATR42 ATR42300 8680920 EU NR 2 ENGINE DIRTY A MTNA K NONE O OTHER CR CRUISE 1 SO 33 910FX 277 UPON REACHING FL 210 (RAIN AND ICING TO FL 210) AN ATTEMPT WAS MADE TO ADJUST THE CONDITION LEVERS. AT THIS TIME THE CR EW DISCOVERED THE NR 2 ENGINE LEVER COULD NOT BE MOVED FORWARD OR BACKWARD. IT WAS STUCK AT APPROXIMATELY 56 DEGREES. AFTER LANDING AND REACHING THE GATE DURING ENGINE SHUTDOWN THE LEVER WAS FREE TO SHUT DOWN THE ENGINE. THE CABLES WERE CLEANED AND LUBED REF: ATR 42 MM JIC12-22-76. THE PANEL REMOVED WAS INSTALLED REF: FIG 54-00-00-RAI00130-001-AFT UPPER COWL. ALL CHECKS WERE SATIFACTORY. 2 H 7 2 4T RT A53EU 2008022800125 20080228 00125 NM 2008 2 28 DHL2007742040 1 20071217 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 950E S28R CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 CORROSION WITH EXFOLIATION, AFT PIT BS 950E STRINGER 28R. CUT OUT DAMAGED AREA APPROXIMATE DIMENSION 15.5" LENGTH IAW C OTNEY AEROSPACE, INC DRAWING NR AE59-53-R01 REV A. LOCATED AND DRILLED NEW STRINGER SECTION USING P/N 65-58387-2 PO NR 7332255 APPROXIMATE DIMENSION 15.5" LENGTH IAW B-727 SRM 51-30-5 AND EVA B253-00029. FABRICATED TWO EACH NEW SPLICE CHA NNELS DIMENSION 13.5" LONG AND 13" LONG USING 7075-O 0.090" PO NR 7185240 IAW EVA B253-00029. FABRICATED 2 SPLICE STRAP S APPROXIMATE DIMENSION 14.25" BY .75", 2 EACH SPLICE STRAPS 12.25" BY .75", 2 SPLICE STRAPS APPROXIMATE DIMENSION 16.12 5" BY .75", 2 SPLICE STRAPS APPROXIMATE DIMENSION 13.25" BY .75", 1 EACH STRAP DIMENSION 36" BY 1" AND 1 SPLICE STRAP AP 2 L 7 3 4F A3WE 2008022800127 20080228 00127 NM 2008 2 28 DHL2007742042 1 20071126 A 5344 HINGE BOEING 727 727225 1384077 NM CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 MCD AFT HINGE ON FUSELAGE SIDE HAS AFT LOBE CRACKED. REMOVED DAMAGED SECTION OF MCD HINGE AEI CH 52 REV G FIGURE 5201 B /A. LOCATED AND DRILLED NEW SECTION OF MCD HINGE APPROXIMATE DIMENSION 18" BY 1.75" P/N 14520001-16-7200 PO NR 724546 I AW AEI B-727 MM CH 52 FIGURE 5201 B AND SRM 51-30-5. TREATED AND PRIMED NEW HINGE SECTION IAW B-727 SRM 51-10-2 AND INS TALLED NEW HINGE SECTION IAW B-727 SRM 51-30-2 AND AEI B-727 MM CH 52 FIGURE 5201B. 2 L 7 3 4F A3WE 2008022800129 20080228 00129 NM 2008 2 28 DHL2007742054 1 20071126 A 5311 FRAME BOEING 727 727225 1384077 NM BS 1070 S26R DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 DENT, AFT PIT AT FRAME BS 1070 ABOVE STRINGER 26R. CUT OUT DAMAGED AREA APPROXIMATE DIMENSTION 1: BY 1: IAW B-727 SRM 5 1-40-2 FIGURE 1. FABRICATED FRAME REPAIR DOUBLER FROM 7075-0 0.071" PO NR 724711 APPROXIMATE DIMENSION 10" BY 4.5" IAW B-727 SRM 51-40-2 FIGURE 1 AND 53-10-2 FIGURE 5. HEAT TREATED MATERIAL TO T6 CONDITION IAW FAS ER NR 2-37153-801 REV A. INSTALLED REPAIR DOUBLER AT FRAME BS 1070 ABOVE STRINGER 26R IAW B-727 SRM 51-40-3 FIGURE 1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2008030400014 20080304 00014 NM 2008 3 4 DHL2007793004 1 20071201 A 5410 DUCT BOEING 727 727247 138408F NM BS 1130 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 CRACK AT "S" INSIDE DUCT INLET, 6 O'CLOCK POSITION BS 1130. REMOVED FASTENERS FOR ACCESS IAW SRM 51-30-2 FIGURE 1. CUT OUT DAMAGE AREA 1" BY .75" ON "S" DUCT SKIN. CUT DAMAGE AREA ON STRAP 1" BY 15.25" IAW SRM 54-10-2 FIGURE 10. FABRICA TED FILLER AND FABRICATED DOUBLER. FABRICATED TWO STRAP DOUBLERS IAW SRM 54-10-2 FIGURE 5 AND 54-10-3 FIGURE 10. PARTS AND AREA TREATED AND PRIMED IAW SRM 51-10-2 FIGURE 1. REPAIR AND STRAP INSTALLED IAW SRM 51-40-3 FIGURE 10 AT "S" DUCT INLET 6 O'CLOCK POSITION BS 1130. 2 L 7 3 4F A3WE 2008030400017 20080304 00017 NM 2008 3 4 DHL2007793003 1 20071201 A 5753 STRUCTURE BOEING 727 727247 138408F NM TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 RT INBOARD MID FLAP TRAILING EDGE CRACKED AT INBOARD CONTROL DRUM ROD-END. REMOVED 48 INCH SECTION OF TRAILING EDGE FRO M RT INBOARD MID FLAP. FABRICATED AND INSTALLED NEW SECTION AND SPLICE IAW SRM 51-40-4 FIGURE 1, 51-30-2 AND 51-10-2. 2 L 7 3 4F A3WE 2008030400024 20080304 00024 NM 2008 3 4 DHL2007793021 1 20071208 A 5313 STRINGER BOEING 727 727247 138408F NM BS 1150-1166 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 SURFACE CORROSION ON STRINGER 30 FROM BS 1150 TO 1166. REMOVED CORROSION IAW SRM 51-10-6. AREA FOUND WITH IN LIMITS IA W SRM 53-10-1 FIGURE 1 AND 53-10-2 FIGURE 9. FOUND CORROSION BETWEEN BS 1150-1155 TO BE OUT OF LIMITS IAW SRM 53-10-1 F IGURE 1 AND 53-10-2 FIGURE 9. CUT OUT DAMAGED SECTION OF STRINGER IAW SRM 53-10-3 FIGURE 1. FABRICATED FILLER STRINGER AND 2 EACH SPLICE STRINGER IAW SRM 53-10-3 FIGURE 1. TREATED AND PRIMED PART AND AREA IAW SRM 51-10-2. INSTALLED REPA IR PARTS IAW SRM 53-10-3 FIGURE 1. 2 L 7 3 4F A3WE 2008030400059 20080304 00059 NM 2008 3 4 DHL2007742056 1 20071119 A 5311 FRAME BOEING 727 727225 1384077 NM BS 950D S26L DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 DENT AT FRAME BS 950D ABOVE STRINGER 26L. CUT OUT DAMAGED AREA IAW SRM 53-10-4 FIGURE 1. FABRICATED NEW FRAME REPAIR IAW SRM 53-10-4 FIGURE 1. HEAT TREATED FRAME REPAIR TO T6 CONDITION IAW FORM 1115 REV 11. LOCATED AND DRILLED NEW FRAM E REPAIR IAW SRM 53-10-4 FIGURE 1 AND 51-30-5. TREATED AND PRIMED NEW FRAME IAW SRM 51-10-2. INSTALLED NEW FRAME REPAI R AT BS 950D IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008030400106 20080304 00106 NM 2008 3 4 DHL2007742058 1 20071209 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 680 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 FLOORBEAM SPLICE PLATE AT LBL 65 HAS CRACK FROM SLOT RADIUS BS 680. REMOVED CRACKED FLOORBEAM SPLICE PLATE IAW B-727 SR M 51-30-2 AND AEI DRAWING NR AE727-3-A004. FABRICATED NEW SPLICE PLATE FROM P/N 2024-T3 0.125 PO NR 9005802 APPROXIMATE DIMENSION 10.625" BY 6.75" BY 6.125" BY 4.8125" IAW AEI DRAWING NR AE727-1-042 REV E AND JC EL00670-001. INSTALLED NEW SPLICE PLATE AT FLOORBEAM BS 680 LBL 65 IAW AEI DRAWING NR AE727-2-0004 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2008030400126 20080304 00126 NM 2008 3 4 DHL2007742063 1 20071206 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 620 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 FORWARD CARGO COMPARTMENT STRINGER 27L IS CORRODED AT STATION 620 WITH EXFOLIATION. REMOVED FASTENERS AND EXISTING SPLI CE IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREA (DIMENSION 17.5" LONG) AND FABRICATED REPAIR FILLER FROM BAC 1493-513 70 75-T6 PO NR 7332258 (DIMENSION 17.5" LONG) AND REPAIR SPLICE FROM BAC 1498-1320 7075-T6 PO NR 7308420 (DIMENSION 7.5" LO NG) IAW B-727 SRM 53-10-2 FIGURE 9 AND 53-10-3 FIGURE 1. TREATED AND PRIMED PARTS IAW B-727 SRM 51-10-2 AND INSTALLED R EPAIR PARTS AT FORWARD CARGO COMPARTMENT STRINGER 27L AT STATION 620 IAW B-727 SRM 53-10-3 FIGURE 1 AND 51-30-2. 2 L 7 3 4F A3WE 2008030400163 20080304 00163 SO 2008 3 4 SIMA200805101 1 20070219 A 5320 14529150003 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSLEAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 619AE 145101 DURING MBV INSPECTION, FOUND UPPER FLOOR SUPPORT FRAME 24 RT SIDE CORRODED. INSTALLED NEW UPPER FLOOR SUPPORT BTW FR 23 AND 24 IAW SRM 51-40-02. A/C WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008030500001 20080305 00001 NM 2008 3 5 QXEA200801924 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - RIGHT HAND OUTBOARD SEAT TRACK NR 10 HAS PITTING CORROSION AND SCRATCHES AT STATION X426. REPAIRED IAW RD8-53-1342 AND -8 NDTM 51-00-01 AND -8 200 SRM 51-20-16, 51-20-66. 2 H 7 2 4T RT A13NM 2008030500002 20080305 00002 NM 2008 3 5 QXEA200801944 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 201 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - SEVERE CORROSION FOUND UNDER BOLT HEAD AT TIE FITTING, LOCATED AT FS X201, Z81, FRAME 201 TO NR 4 SEAT TRACK VERTICLE SUPPORT. REMOVED TIE FITTING, INSTALLED NEW TIE FITTING FROM STOCK IAW D8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008030500026 20080305 00026 NM 2008 3 5 QXEA200801869 1 20071204 A 5315 FLOORBEAM DHAV DHC8 DHC8202 2809007 NM BS 600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - POSSIBLE CORROSION ON LOWER BAGGAGE COMPARTMENT FLOOR ANGLE AT STATION X600 WHERE LOWER FLOOR MEET THE VERTICAL RISER, NUMEROUS LOCATIONS ENTIRE LENGTH. REPAIRED -8 200 CPCM CHAP 4 PG 4-25 PARA 9, - 8 200 SRM 51-20-11, 51- 20-36, 51-20-51 AND -8 200 NDTM 51-00-04. 2 H 7 2 4T RT A13NM 2008030500028 20080305 00028 NM 2008 3 5 QXEA200801946 1 20071204 A 5320 SUPPORT DHAV DHC8 DHC8202 2809007 NM BS 569 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - AFT CARGO DOOR THRESHOLD CORROSION ON TAB AND NUTPLATE ON THRESHOLD SUPPORT AT X569. REPAIRED IAW DAS H 8 200 SRM 51-20-11, 51-20-16, 51-20-36, 51-20-51 , 51-40-00 AND NDTM 51-00-01. 2 H 7 2 4T RT A13NM 2008030500032 20080305 00032 NM 2008 3 5 QXEA200801864 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 228 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - RIGHT INBOARD SEAT TRACK NR 7 HAS CORROSION AT APPROXIMATELY STATION 228.0. REMOVED NR 7 SEAT TRACK AN D INSTALLED NEW SEAT TRACK FROM STOCK IAW DH 200 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2008030500033 20080305 00033 NM 2008 3 5 QXEA200801866 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 580 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - RIGHT OUTBOARD SEAT TRACK NR 9 HAS CORROSION ON OUTBOARD AND INBOARD FLANGE NUTPLATE RECEPTACLES AT STA TION X580. REPAIRED IAW RD8-53-784, INSPECTED NO CRACKS NOTED IAW DASH 8 200 NDTM 51-00-01. 2 H 7 2 4T RT A13NM 2008030500043 20080305 00043 NM 2008 3 5 QXEA200801928 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 456 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - RIGHT OUTBOARD SEAT TRACK NR 11 HAS CORROSION AT STATION X456. REPAIRED IAW RD8-53-1342, AND -8 200 ND TM PART6 51-00-01 AND -8 200 SRM 51-20-16, 51-20-66. 2 H 7 2 4T RT A13NM 2008030500047 20080305 00047 CE 2008 3 5 073371 1 20071203 A 2131 13036813 CONTROLLER LEAR 35 35A 5170602 CE CABIN PRESSURE MALFUNCTIONED E CVGA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 123DA 405 AT FL 295 WHILE CLIMBING TO FL 390, CREW OBSERVED 2500 FT/MIN CABIN CLIMB. INITIATED EMERGENCY DESCENT PER AFM. FINAL MAINTENANCE FINDING, REPLACED DIFFERENTIAL PRESSURE CONTROLLER. FLIGHT TEST OK. 2 L 7 2 4F A10CE 2008030500052 20080305 00052 EA 2008 3 5 QXEA200801997 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 429 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT SIDE RIDE SEAT TRACK HAS CORROSION AT APPROXIMATELY STATION 429.00. REMOVED LOCALIZED CORROSION BY BLENDING SEAT TRACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED ARE AS. 2 L 7 2 4F RT A21EA 2008030500053 20080305 00053 EA 2008 3 5 QXEA200801988 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 676-679 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT SEAT TRACK HAS CORROSION AT STATION 676 TO 679. BLENDED OUT CORROSION FROM SEAT TRACK, INSPECTED , REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030500054 20080305 00054 EA 2008 3 5 QXEA200801983 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 615-617 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT SIDE SEAT TRACK HAS CORROSION AT STATION 615 TO 617. BLENDED OUT CORROSION FROM SEAT TRACK, INSPE CTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREA. 2 L 7 2 4F RT A21EA 2008030500055 20080305 00055 EA 2008 3 5 QXEA200801996 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 692-697 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT CENTER SEAT TRACK HAS CORROSION AT STATION 692 TO 697. BLENDED OUT CORROSION FROM SEAT TRACK, INS PECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030500056 20080305 00056 EA 2008 3 5 QXEA200801991 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 569-575 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT HAND CENTER SEAT TRACK HAS CORROSION AT STATION 569.5 TO 575. BLENDED OUT CORROSION FROM SEAT TRA CK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030500061 20080305 00061 EA 2008 3 5 QXEA200801993 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 632-648 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT SEAT TRACK HAS CORROSION AT STATION 632 TO 648. BLENDED AWAY CORROSION FROM SEAT TRACK, INSPECTED , REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030500064 20080305 00064 EA 2008 3 5 QXEA200801984 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 490-493 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT SEAT TRACK HAS CORROSION AT STATION 490 TO 493. BLENDED OUT CORROSION FROM SEAT TRACK, INSPECTED , REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030500065 20080305 00065 EA 2008 3 5 QXEA200801998 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 582 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX -C4 CHECK - RIGHT SIDE RAIL SEAT TRACK HAS CORROSION AT APPROXIMATELY STATION 582.00. REMOVED LOCALIZED CORROSION B Y BLENDING SEAT TRACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREA S. 2 L 7 2 4F RT A21EA 2008030500103 20080305 00103 EA 2008 3 5 QXEA200802000 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 785 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT RAIL SEAT TRACK HAS CORROSION AT APPROXIMATELY STATION 785.00. REMOVED CORROSION BY BLENDING, IN SPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030500104 20080305 00104 EA 2008 3 5 QXEA200801967 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 379 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT CENTER SEAT TRACK HAS PITTING AT APPROXIMATELY STATION 379.00. REMOVED SEAT TRACK NR 14 AND INST ALLED NEW TRACK FROM STOCK. 2 L 7 2 4F RT A21EA 2008030500106 20080305 00106 EA 2008 3 5 QXEA200802064 1 20071215 A 5410 LATCH CNDAIR CL600 CL6002C10 1390015 EA NACELLE DOOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - NR 1 ENGINE HAS WEAR ON LOWER TRANSLATING DOOR WHERE AFT LATCH HOUSING ON FAN COWL ALIGN. WEAR IS BEYO ND LIMITS. REMOVED WORN LATCH AND INSTALLED NEW LATCH PLATE FROM STOCK 2 L 7 2 4F RT A21EA 2008030500107 20080305 00107 EA 2008 3 5 QXEA200802001 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 844 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT SIDE RAIL SEAT TRACK HAS CORROSION AT APPROXIMATELY STATION 844.00. REMOVED CORROSION FROM TRACK BY BLENDING, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030500149 20080305 00149 NM 2008 3 5 QXEA200801947 1 20071204 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM BS 560 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - AFT CARGO DOOR THRESHOLD CORROSION ON NUTPLATES ON THRESHOLD SUPPORT BRACKET AT STATION X560. REPAIRED IAW DASH 8 200 SRM 51-20-11, 51-20-16 51-20-36, 51-20-51, AND 51-40-00. 2 H 7 2 4T RT A13NM 2008030500157 20080305 00157 NM 2008 3 5 QXEA200801935 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 383-392 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - SEAT TRACK NR 1 HAS SCRATCHES ON TOP BETWEEN STATION 383 AND 392. REPAIRED IAW RD8-53-1342 AND -8 200 NDTM PART 6 51-00-01 AND -8 200 SRM 51-20-16, 51-20-66. 2 H 7 2 4T RT A13NM 2008030400114 20080304 00114 NM 2008 3 4 DHL2007742062 1 20071204 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 560 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 FORWARD CARGO COMPARTMENT STRINGER 27R IS CORRODED JUST AFT OF STATION 560 WITH EXFOLIATION. REMOVED SUPPORT FRAMES AT BS 564 AND BS 574 IAW B-727 SRM 51-30-2. CUT OUT DAMAGED SECTION (DIMENSION 18" LONG) AND FABRICATED NEW STRINGER SECTI ON FROM BAC 1498-1478 0.090" 7075-T6 (DIMENSION 18" LONG) PO NR 7332258 AND 2 EACH REPAIR SPLICES FROM BAC 1498-131 7075 -T6 PO NR 7332231 (DIMENSION 13" LONG EACH) IAW B-727 SRM 53-10-3 FIGURE 1 AND 53-10-2 FIGURE 9. TREATED AND PRIMED REP AIR PARTS IAW B-727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B-727 SRM 51-30-2 AND 53-10-3 FIGURE 1. REINSTALLED SUPPOR T FRAMES IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008030500006 20080305 00006 NM 2008 3 5 QXEA200801889 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 358 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - HOLE IN TOP OF FRAME 358 INBOARD OF NR 4 SEAT TRACK. CUT REPLACEMENT SECTION OF BEAM TO SIZE. FABRICA TED SPLICE PLATE SECTIONS. INSTALLED REPAIR SPLICE IAW RD8-53-9904. 2 H 7 2 4T RT A13NM 2008030500009 20080305 00009 NM 2008 3 5 QXEA200801872 1 20071204 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - CORROSION ON TOP AND BOTTOM OF ANGLE BRACKET AT AFT END OF BAG DOOR THRESHOLD. REPAIRED REF Q200 CPM C HAP 4 PG 4-25 PARA 9, AND -8 200 SRM 51-20-11, 51-20-16, 51-20-36 AND NDTM 51-00-01. 2 H 7 2 4T RT A13NM 2008030500012 20080305 00012 EA 2008 3 5 QXEA200802055 1 20071215 A 5751 SKIN CNDAIR CL600 CL6002C10 1390015 EA LT AILERON WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT AILERON TOP SURFACE LEADING EDGE IS WORN FROM CHAFE WITH SEAL INBOARD OF INBOARD HINGE. REMOVED L EFT AILERON TOP SURFACE IAW CRJ SRM. INSTALLED NEW TOP SURFACE TO LEFT AILERON IAW CRJ 700 SRM. 2 L 7 2 4F RT A21EA 2008030500025 20080305 00025 NM 2008 3 5 QXEA200801939 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 477-487 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - SEAT TRACK NR 5 HAS SCRATCHES ON TOP BETWEEN STATION 477 AND 487. REPAIRED IAW RD 8-53-1339 AND -8 200 NDTM PART 6 51-00-01 AND -8 200 SRM 51-20-16, 51-20-66. 2 H 7 2 4T RT A13NM 2008030500027 20080305 00027 NM 2008 3 5 QXEA200801945 1 20071204 A 5320 SUPPORT BRACKET DHAV DHC8 DHC8202 2809007 NM BS 593 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - AFT CARGO DOOR NUT PLATE ON BOTTOM OF THRESHOLD SUPPORT BRACKET CORRODED AT STATION X593. REPAIRED IAW DASH 8 200 SRM 51-20-11, 51-20-16, 51-20-36, 51-20-51, 51-40-00. 2 H 7 2 4T RT A13NM 2008030500057 20080305 00057 EA 2008 3 5 QXEA200801992 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 599-604 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT HAND CENTER SEAT TRACK HAS CORROSION AT STATION 599 TO 604.5. BLENDED AWAY CORROSION FROM SEAT TR ACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030500102 20080305 00102 EA 2008 3 5 QXEA200801989 1 20071215 A 5310 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 538-543 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT CENTER SEAT TRACK HAS CORROSION AT STATION 538 TO 543. BLENDED OUT CORROSION FROM SEAT TRACK, INS PECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030500154 20080305 00154 NM 2008 3 5 QXEA200801931 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 346-349 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - SEAT TRACK 31 HAS CORROSION ON THE TOP BETWEEN STATION 346 AND 349. REPAIRED IAW RD8-53-1342 AND -8 20 0 NDTM PART6 51-00-01 AND -8 200 SRM 51-20-16, 51-20-66. 2 H 7 2 4T RT A13NM 2008030500158 20080305 00158 NM 2008 3 5 QXEA200801922 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 HAS MINOR SCRATCHES AT STATION (X264), (X288), (X289 TO X302), (X342 TO 348), (X394), (X400). REPAIRED PER RD8-53-1342 AND -8 NDTM 51-00-01, AND -8 200 SRM 51-20-16, 51-20-66. 2 H 7 2 4T RT A13NM 2008030600084 20080306 00084 NM 2008 3 6 UPS08M51707 1 20071221 A 5512 PANEL DOUG MD11 MD11 3023602 NM HORIZ STAB DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C EMPENNAGE, LT HORIZONTAL STABILIZER FRONT SPAR, TOP OF ACCESS PANEL 331B Z CUTOUT AREA, UPPER SURFACE MOUNTING HOLES FOR L/E PANEL 331BT, FOUND WITH 01 EA ELONGATED MOUNTING HOLE AS MARKED. GANG CHANNEL ASSY PARTIALLY REM OVED FOR ACCESS PER SRM 51-35-01-V.II R35. QTY 01EA ELONGATED HOLE REAMED TO 0.343"DIA PER EN 1010-08. HFEC OPEN HOLE INSP C/O PER DAC NDTSPM R13 06-10-01.003 ON REWORKED AREA & FOUND NO CRACK EVIDENT. BUSHING INSTALLED PER EN 1010-08. THIS REPAIR IS TIME LIMITED FOR 24 MONTHS PENDING A DAMAGE TOLERANCE ANALYSIS. 2 L 7 3 4F RT A22WE 2008030500034 20080305 00034 NM 2008 3 5 QXEA200801868 1 20071204 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 242 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - CORROSION ON FRAME X242 LOWER CASTELLATION AT STRINGER X222. REPAIRED IAW -8 200 SRM 51-20-91, 51-40-1 1, 51-20-16, 51-20-36, 51-20-57 AND -8 200 CPM CHAPTER 4, NDTM 51-00-01 2 H 7 2 4T RT A13NM 2008030500109 20080305 00109 EA 2008 3 5 QXEA200802002 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 490 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT CENTER SEAT TRACK HAS CORROSION AT STATION 490.00. BLENDED CORROSION FROM SEAT TRACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030700024 20080307 00024 SO 2008 3 7 BSYA200700015 1 20071205 A 8120 LW12463 TURBOCHARGER PIPER PA31 PA31350 7103110 SO LT ENGINE MALFUNCTIONED E BSYA K NONE P NO WARNING INDICATION CR CRUISE 1 GL 07 4079Y 318152079 LEFT ENGINE MANIFOLD PRESSURE DROPPED TO 25" DURING CRUISE, LANDED DTW NO PROBLEMS. MAINTENANCE CHANGED TURBO CHARGER, OPS CHECKS GOOD. 1 L 7 2 3O A20SO 2008030700076 20080307 00076 EA 2008 3 7 QXEA200802005 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 553 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT SEAT TRACK HAS CORROSION AT STATION 553. BLENDED TO REMOVE CORROSION FROM TRACK, INSPECTED, REMA INED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030700078 20080307 00078 EA 2008 3 7 QXEA200801999 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 597 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT SIDE RAIL SEAT TRACK HAS A SCRATCH AND CORROSION AT APPROXIMATELY STATION 597.00. REMOVED SCRATC H AND CORROSION BY BLENDING SEAT TRACK. INSPECTED TRACK, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE T REATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030700079 20080307 00079 EA 2008 3 7 QXEA200802059 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT HAND SIDE RAIL SEAT TRACT HAS WEAR AND GOUGED AT FORWARD END OF SEAT TRACK JUST AFT OF LEFT OVERW ING EXIT. BLENDED OUT GOUGE FROM SEAT TRACK, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TR EATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030700080 20080307 00080 EA 2008 3 7 QXEA200802060 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 700 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT RAIL SEAT TRACK HAS CORROSION AT APPROXIMATELY STATION 700.00. BLENDED SIDE RAIL OF TRACK, INSPEC TED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030700081 20080307 00081 EA 2008 3 7 QXEA200802007 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT CENTER SEAT TRACK HAS CORROSION AT STATION 600.05. BLENDED OUT CORROSION FROM SEAT TRACK, INSPEC TED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030700082 20080307 00082 EA 2008 3 7 QXEA200802057 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 937 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT SIDE RAIL SEAT TRACK HAS GOUGE AT APPROXIMATELY STATION 937.00. REMOVED GOUGE FROM SEAT TRACK BY BLENDING, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2008030700126 20080307 00126 NM 2008 3 7 QXEA200801948 1 20071204 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM BS 576-569 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - AFT CARGO DOOR THRESHOLD CORROSION AROUND RIVETS AND IN BEND RADIUS OF ANGLE BELOW THRESHOLD BETWEEN ST ATION X576 AND 569. REMOVED RIVETS AND BLENDED OUT .002" MATERIAL, OK FOR CONTINUED SERVICE. ALODINED, PRIMED AND PAIN TED IAW SRM 51-20-16, 51-20-36, AND 51-20-51. INSTALL RIVETS IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008030700129 20080307 00129 NM 2008 3 7 QXEA200801887 1 20071204 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM PAX DOORWAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - MAIN CABIN DOOR THRESHOLD SEAL HAS CORROSION UNDER SIDE AROUND NUT PLATES. REPAIRED IAW RD8-53-8921, A ND -8 200 SRM 51-40-11 AND -8 NDTM 51-00-01. 2 H 7 2 4T RT A13NM 2008030700131 20080307 00131 NM 2008 3 7 QXEA200801890 1 20071204 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 202 S30-32R CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX -C5 CHECK - CORROSION ON FORWARD SIDE OF FRAME X202 BETWEEN STRINGER 30R AND 32R. REPAIRED IAW CPM CHAPTER 4 AND -8 200 SRM 51-20-11, 51-20-16, 51-20-36, AND 51-20-51 ALSO -8 200 NDTM 51-00-01. 2 H 7 2 4T RT A13NM 2008030700133 20080307 00133 NM 2008 3 7 QXEA200801923 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 376 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 HAS PITTING CORROSION AND 2 NICKS AT STATION X376. REPAIRED IAW RD8-53 -1342 AND -8 200 NDTM 51-00-01 AND -8 200 SRM 51-20-16, 51-20-66. 2 H 7 2 4T RT A13NM 2008030700134 20080307 00134 NM 2008 3 7 QXEA200801927 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 318-332 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - SEAT TRACK NR 11 HAS SCRATCHES ON TOP BETWEEN STATION 318 - 332. REPAIRED IAW RD 8-53-1342 AND -8 200 NDTM PART 6 51-00-01, AND -8 200 SRM 51-20-16, 51-20-66. 2 H 7 2 4T RT A13NM 2008030700025 20080307 00025 CE 2008 3 7 BSYA200700016 1 20071218 A 7721 100200007 PROBE BEECH 58 58 1152740 CE ENGINE DEFECTIVE E BSYA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 07 3695V TH1183 EN ROUTE FROM TEB TO HFD WHEN PILOT NOTICED HIGH CYL HEAD TEMP AND DIVERTED INTO MAINTENANCE BASE IN BDL. REMOVED AND R EPLACED DEFECTIVE CHT PROBE, OPS CHECKS GOOD. 1 L 7 2 3O 3A16 2008030700027 20080307 00027 CE 2008 3 7 BSYA200700017 1 20071223 A 2450 CM358920 CIRCUIT BREAKER CESSNA 208 208B 2073701 CE NR 1 BUSS MALFUNCTIONED E BSYA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 9448B 208B0121 EN ROUTE FROM SDF TO MDW AIRCRAFT DIVERTED TO DPA BECAUSE OF HIGH WINDS. UPON ARRIVING AT DPA, LOST ALL AVIONICS. TRIE D TO RESET NR 1 & NR 2 CIRCUIT BREAKERS, NO HELP THEN STARTED TO SMELL SMOKE. FOUND NR 1 BUSS CIRCUIT BREAKER BAD AND P 10 CONNECTOR HAD A BAD PIN (BURNT). REMOVED AND REPLACED SWITCH AND PIN OPS CHECKS GOOD. 1 H 7 1 3T A37CE 2008030700128 20080307 00128 NM 2008 3 7 QXEA200801870 1 20071204 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 597 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - SURFACE CORROSION JUST INSIDE AFT LOWER CORNER OF AFT BAG DOOR OPENING FS X597. REPAIRED REF Q200 CPCM CHAPTER 4 PG 4-25 PARA 9, AND -8 200 SRM 51-20-16, 51-20-11, 51-40-11, 51-20-36, 51-20-26 AND NDTM 51-00-01. 2 H 7 2 4T RT A13NM 2008030700136 20080307 00136 NM 2008 3 7 QXEA200801932 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 501 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - RIGHT OUTBOARD SEAT TRACK NR 11 HAS CORROSION AND SCRATCHES AT STATION X501. REPAIRED IAW RD 8-53-1342 AND -8 200 NDTM PART6 51-00-01 AND -8 200 SRM 51-20-16, 51-20-66. 2 H 7 2 4T RT A13NM 2008030700137 20080307 00137 NM 2008 3 7 QXEA200801867 1 20071204 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 566-600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - SEAT TRACK NR 6 HAS CORROSION ON INBOARD FLANGE BETWEEN STATION 566 AND 600. REPAIRED IAW RD8-53-784, NO CRACKS NOTED IAW -8 200 NDTM 51-00-01. 2 H 7 2 4T RT A13NM 2008030700181 20080307 00181 EA 2008 3 7 SWIA200719272 1 20071111 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 945SW 7770 FOUND AT C-CHECK, FS 280 AT RBL9 LOWER FLOOR SUPPORT ANGLE CRACKED. INSTALLED REPAIR PARTS PER CRJ200 REO 601R-53-11-17 1 REV D DATED 11-13-07 REPAIR SCHEME B. 2 L 7 2 4F RT A21EA 2008030700183 20080307 00183 EA 2008 3 7 SWIA200719273 1 20071111 A 3210 BRACKET CNDAIR CL600 CL6002B19 1900309 EA MLG BRAKE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 945SW 7770 FOUND AT CHECK, LEFT WHEEL BRAKE TRANSDUCER BRACKET IS CRACKED. REPLACED WHEEL BRAKE TRANSDUCER BRACKET PER CRJ200 SRM 51-42-06 PG 11. 2 L 7 2 4F RT A21EA 2008030700077 20080307 00077 EA 2008 3 7 QXEA200802008 1 20071215 A 5320 STIFFENER CNDAIR CL600 CL6002C10 1390015 EA BS 280 BULKHEAD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - RIGHT COCKPIT BULKHEAD VERTICLE STIFFENER HAS CRACK LOWER FASTENER HOLE STATION 280. REMOVED AND REPLA CED WITH NEW STIFFENER AT STATION X280 IAW CRJ SRM. 2 L 7 2 4F RT A21EA 2008030700179 20080307 00179 EA 2008 3 7 SWIA200719271 1 20071111 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 945SW 7770 FOUND AT C-CHECK, STN280 LBL9.0 UPPER FLOOR SUPPORT ANGLE CRACKED. INSTALLED REPAIR PARTS AND NEW COCKPIT FLOOR SUPPORT ANGLE PER CRJ200 REO 601R-53-11-136 DATED 02-10-99. 2 L 7 2 4F RT A21EA 2008030700340 20080307 00340 EA 2008 3 7 SWIA200719276 1 20071111 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 945SW 7770 LEFT ENGINE THRUST SHAFT FITTING SHOWS SIGNS OF CORROSION, FOUND AT C-CHECK. REPLACED AFT MOUNT THRUST FITTING PER CRJ2 00 AMM 71-22-01-400-801. 2 L 7 2 4F RT A21EA 2008030700127 20080307 00127 NM 2008 3 7 QXEA200801942 1 20071204 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM RT WING LE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - C5 CHECK - RIGHT WING INBOARD LEADING EDGE LOWER FLANGE HAS FRETTING CORROSION AT APPROXIMATELY STATION YW57. BLE NDED AND REPAIRED IAW RD8-57-811 AND DASH 8 200 SRM 51-00-01, 51-40-11. 2 H 7 2 4T RT A13NM 2008031000038 20080310 00038 EA 2008 3 10 MASA200800175 1 20070228 A 2120 UNKNOWN CNDAIR CL600 CL6002D24 1390016 EA LAVATORY ODOR A MASA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION LD LANDING 1 SW 07 909FJ 15009 ASH FLT 2885 PHX-IAH, SMOKE WARNING IN AFT LAV WITH SMOKE SMELL SHORTLY AFTER LANDING. MX COULD NOT DUPLICATE, OPS GOOD . 2 L 7 2 4F RT A21EA 2008031000188 20080310 00188 NM 2008 3 10 DHL2007793006 1 20071208 A 5344 HINGE BOEING 727 727247 138408F NM BS 640 S4L CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 793DH 21393 MAIN CARGO DOOR AFT HINGE APPEARS TO BE CRACKED, BS 640 STRINGER 4L. HFEC VERIFIED CRACK IAW B-727 NDTM PT 6-51-00-00 F IGURE 23. REMOVED AT MAIN CARGO DOOR AFT HINGE BS 640 STRINGER 4L AS REQUIRED IAW AEI BOEING 727-200 FREIGHTER M/M FIGU RE 5201B REV G. FABRICATED AFT SECTION OF HINGE MATERIAL USED MS21001-16-7200 PO NR 9002527 DIMENSION 17.5 INCHES LONG IAW AEI BOEING 727-200 FREIGHTER M/M FIGURE 5201B REV G. TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED NEW HINGE SEGMENT IAW AEI BOEING B-727 M/M FIGURE 5201 B REV G. OPS CHECK GOOD IAW AEI M/M CHAPTER 52 REV G. 2 L 7 3 4F A3WE 2008030700338 20080307 00338 EA 2008 3 7 SWIA200719274 1 20071111 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BRAKE TRANS CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 945SW 7770 FOUND AT C-CHECK, RIGHT WHEEL BRAKE TRANSDUCER BRACKETS ARE CRACKED. REPLACED BRACKETS PER CRJ200 SRM 51-42-06 PG 11. 2 L 7 2 4F RT A21EA 2008030700339 20080307 00339 EA 2008 3 7 SWIA200719275 1 20071111 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 945SW 7770 FOUND AT C-CHECK, RIGHT ENGINE AFT THRUST MOUNT FITTING BEARING IS CORRODED. REPLACED RIGHT AFT MOUNT THRUST FITTING PE R CRJ200 AMM 71-22-01-400-801. 2 L 7 2 4F RT A21EA 2008031000039 20080310 00039 EA 2008 3 10 MASA200800176 1 20070227 A 5210 WEB CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 914FJ 15014 REPAIRED THE PAX DOOR AFT WEB CRACKS. 2 L 7 2 4F RT A21EA 2008031000081 20080310 00081 NM 2008 3 10 GTIA0800036 1 20070817 A 5320 D5311282600101 FLOOR SUPPORT AIRBUS A321 A321231 3940032 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 583NK 1195 MAIN DECK FLOOR SUPPORT STRUCTURE (BEAM) CORRODED LT Y503.2 BETWEEN FR14 AND FR16. REMOVED AND REPLACED FLOOR SUPPORT B EAM IAW 51-42-11. 2 L 7 2 4F RT A28NM 2008031300030 20080313 00030 NM 2008 3 13 UPS08M51755 1 20071230 A 5730 DOUBLER DOUG MD11 MD11F 3023600 NM RWS 597 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 47473 INSPECTION TYPE:C RT WING FIXED LE COMPT AT STA XORS 597 APPROX, FOUND UPPER DOUBLER CRACKED AS MARKED. CRACKED AREA AT XOS 692 TO XOS 698 AND XOS 700 TO XOS 703 AREA TRIMMED OUT PER EN NR 1016-08. HFEC INSP C/O PER DAC NDTSPM R13,06-10-0 1.001 ON TRIMMED OUT AREA AND FOUND NO CRACK EVIDENT. NEW REPAIR FILLERS 02EA, DOUBLER 01EA AND REPAIR ANGLES 06EA FAB RICATED AND INSTALLED PER EN NR1016-08. 2 L 7 3 4F RT A22WE 2008031300031 20080313 00031 NM 2008 3 13 UPS08M51756 1 20071218 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C LT WING TANK UPPER STRINGER END NR 09 SUSPECT CRACK AS MARKED, THRU TANK LOWER ACCESS NR 538AB, HFEC I NSP C/O PER DAC NDTSPM R13,06-10-01.001 AND FOUND CRACK APPROX 2' INCH AS MARKED. CRACKED PORTION OF LHW TANK UPPER STR INGER NR 9 TRIMMED OFF AS PER EN NR 1005-08. HFEC INSP C/O PER DAC NDTSPM R13,06-10-01.001 ON TRIMMED AREA AND FOUND NO CRACK EVIDENT. REPAIR STRINGER 01EA AND REPAIR STRAPS 03EA FABRICATED AND INSTALLED PER EN NR 1005-08. 2 L 7 3 4F RT A22WE 2008031300180 20080313 00180 EA 2008 3 13 SWIA200719294 1 20071129 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 935SW 7725 FS 280 BEAM IS CRACKED AT APPROX LBL10, FOUND AT C-CHECK. INSTALLED FS 280 AT LBL9.0 REPAIR PARTS IAW CRJ200 REO 601R-5 3-11-171. 2 L 7 2 4F RT A21EA 2008031300183 20080313 00183 EA 2008 3 13 SWIA200719295 1 20071129 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 935SW 7725 FS 280 BEAM IS CRACKED AT APPROX RBL10, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO 601R-53-11-171 REV D, REPAIR S CHEME 13, DATED 2/13/07. 2 L 7 2 4F RT A21EA 2008031300184 20080313 00184 EA 2008 3 13 SWIA200719296 1 20071129 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 935SW 7725 RIGHT SIDE OF RBL 10 UPPER FLOOR SUPPORT AND LEFT SIDE OF LBL 10 UPPER FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. INST ALLED REPAIR PARTS PER CRJ200 SRM 51-42-06 PG 11 PARA 9 AND REO 601R-53-11-1.36 REV A DATED 2007/11/01. 2 L 7 2 4F RT A21EA 2008031300227 20080313 00227 2008 3 13 SWIA200719298 2 20071129 A 7200 SHAFT CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE GOUGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 935SW 7725 RIGHT ENGINE THRUST SHAFT IS GOUGED, FOUND AT C-CHECK. REPLACED ENGINE THRUST SHAFT PER CRJ200 AMM 71-00-00-020-002 PAR A K STEPS 8-9. 2 L 7 2 4F RT A21EA 2008031300229 20080313 00229 EA 2008 3 13 SWIA200719299 1 20071129 A 7120 BEARING CNDAIR CL600 CL6002B19 1900309 EA ENGINE MOUNT WORN A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 935SW 7725 LEFT ENGINE THRUST FITTING BEARING IS WORN, FOUND AT C-CHECK. REPLACED LEFT ENGINE THRUST FITTING PER CRJ200 AMM 71-22- 01-400-801. 2 L 7 2 4F RT A21EA 2008031300231 20080313 00231 EA 2008 3 13 SWIA200719300 1 20071129 A 5751 PANEL CNDAIR CL600 CL6002B19 1900309 EA LT AILERON GOUGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 935SW 7725 LEFT AILERON LEADING EDGE PANEL IS GOUGED, FOUND AT C-CHECK. REPLACED AILERON PANEL PER CRJ200 SRM 51-40-11 PG 2 AND P G 4. 2 L 7 2 4F RT A21EA 2008031300236 20080313 00236 EA 2008 3 13 SWIA200719303 1 20071122 A 7120 BEARING CNDAIR CL600 CL6002B19 1900309 EA ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 946SW 7776 FOUND AT C-CHECK, LEFT ENGINE AFT THRUST FITTING BEARING IS CORRODED. REPLACED LEFT ENGINE AFT THRUST FITTING BEARING P ER CRJ200 AMM 71-22-01-400-801. 2 L 7 2 4F RT A21EA 2008031300239 20080313 00239 EA 2008 3 13 SWIA200719304 1 20071122 A 7120 BEARING CNDAIR CL600 CL6002B19 1900309 EA ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 946SW 7776 RIGHT ENGINE AFT THRUST FITTING BEARING IS CORRODED, FOUND AT C-CHECK. REPLACED ENGINE AFT THRUST FITTING BEARING PER C RJ200 AMM 71-22-01-400-801. 2 L 7 2 4F RT A21EA 2008031300248 20080313 00248 EA 2008 3 13 SWIA200719307 1 20071119 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 453SW 7743 STN 280 AT RBL9.0 LOWER FLOORBEAM IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS IAW CRJ200 REO 601R-53-11-171 RE V D. 2 L 7 2 4F RT A21EA 2008031300252 20080313 00252 EA 2008 3 13 SWIA200719308 1 20071119 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 394 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 453SW 7743 STN 394 AND LBL9.0 INTERCOSTAL IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIRS PER REO 601R-53-21-821 REV, DATED 11-30- 07 STEPS 8-13. 2 L 7 2 4F RT A21EA 2008031300256 20080313 00256 EA 2008 3 13 SWIA200719311 1 20071127 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 752SK 10209 FS 280 BEAM IS CRACKED AT LBL9 AND RBL9, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER CRJ700/900 REO 670-53-11-04 AND CR J700/900 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008031300258 20080313 00258 EA 2008 3 13 SWIA200719312 1 20071121 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 751SK 10208 COCKPIT FLOOR SUPPORT AT FS 280 IS CRACKED AT LBL 9 AND RBL 9, FOUND AT C-CHECK. REPLACED FLOOR SUPPORT AS PER CRJ700/9 00 SRM 51-23-00 PG 9-10 AND 51-42-06 PG 7-8. 2 L 7 2 4F RT A21EA 2008031300284 20080313 00284 EA 2008 3 13 SWIA200719315 1 20071206 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 750SK 7677 COCKPIT FLOOR SUPPORT BEAM HAS CORROSION, FOUND AT C-CHECK. REPLACED COCKPIT FLOOR SUPPORT PER CRJ7/9 SRM 51-23-00- P 1 0-11 AND 51-42-06 P7-8 AND SB670BA-53-026. 2 L 7 2 4F RT A21EA 2008031300309 20080313 00309 NM 2008 3 13 DHLA200800025 1 20071214 A 5753 STRUCTURE BOEING 727 727224 1384076 NM TE FLAPS DAMAGED A DHLA O OTHER D INFLIGHT SEPARATION AP APPROACH 1 GL 05 746DH 2799 549 22252 FLT NR 520, RT WING INBOARD FORE FLAP DAMAGED. REMOVED AND REPLACED RT INBD FORE FLAP. OP CK GOOD IAW AMM 27-51-01. A IRCRAFT WAS GROUNDED. 2 L 7 3 4F A3WE 2008031300327 20080313 00327 NM 2008 3 13 UPS08M51760 1 20071230 A 5730 DOUBLER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C RT WING FIXED LE COMPT AT XORS 538 APPROX FOUND UPPER DOUBLER CRACK AS MARKED CRACK AREAS ON UPPER DOU BLER BET XOS 636 AND 643 AND XOS 644 AND XOS 648 02 EA LOCATIONS TRIMMED OUT INDIVIDUALLY PER EN NR 1016-08. HFEC INSP C/O PER DAC NDTSPM 06-10-01.001 R13 ON REWORKED AREA AND FOUND NO CRACK EVIDENT. NEW REPAIR FILLERS 02EA, DOUBLER 01EA AND REPAIR ANGLES 06EA, FABRICATED AND INSTALLED PER EN NR 1016-08. 2 L 7 3 4F RT A22WE 2008031300233 20080313 00233 EA 2008 3 13 SWIA200719301 1 20071122 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 946SW 7776 CRACK ON COPILOTS BULKHEAD WEB AT STA 280.00 AND WL73.00 RBL11.00, FOUND AT C-CHECK. INSTALLED REPAIR PARTS IAW CRJ200 REO 601R-53-11-1292, DATED 12/03/07. 2 L 7 2 4F RT A21EA 2008031300234 20080313 00234 EA 2008 3 13 SWIA200719302 1 20071122 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 946SW 7776 FS 280 AND LBL9 LOWER SUPPORT ANGLE IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS AT LBL9.0 AND FS 280 LOWER SUP PORT ANGLE IAW CRJ200 REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 2008031300242 20080313 00242 EA 2008 3 13 SWIA200719305 1 20071119 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 453SW 7743 STN 280 AT LBL-RBL9.0 UPPER FLOOR SUPPORT ANGLE IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO 601R 53-11 -136. 2 L 7 2 4F RT A21EA 2008031300118 20080313 00118 NE 2008 3 13 DHLA200070006 2 20071120 A 7200 ENGINE BOEING 727 7272Q9 138448M NM PWA JT8 JT8D17 52049 NE NR 2 MALFUNCTIONED A DHLA E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 GL 05 741DH 43288 1885 21931 702653 FLT NR 594 IN CRUISE FL320, NR 2 ENGINE PARAMETERS STARTED TO FLUCTUATE ALONG WITH SEVERE VIBRATION, PERFORMED ABNORMAL PROCEDURE OBSERVED NR 2 OIL QTY GO TO ZERO AND PERFORMED ENG SHUTDOWN ABNORMAL, PROCEDURE UPON LANDING OIL QTY RETURNED TO NORMAL AFTER ENG SHUTDOWN OIL PRESS WAS AT REDLINE. REMOVED AND REPLACED NR 2 ENG PER MTM 71.2, RAN ENG PER JRH. PE RFORMED MPA AND RUH SHEET NR 2 ENG. OK FOR SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2008031300187 20080313 00187 EA 2008 3 13 SWIA200719297 1 20071129 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 935SW 7725 FORWARD FLOOR SUPPORT IS CRACKED AT LBL 9 AND FS 280, FOUND AT C-CHECK. INSTALLED REPAIR PARTS IAW CRJ200 SRM CH 51-42- 06, PG 11, PARA 9. 2 L 7 2 4F RT A21EA 2008031300253 20080313 00253 EA 2008 3 13 SWIA200719309 1 20071119 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 453SW 7743 STN 621 AT LBL42.0 FLOOR BULKHEAD ANGLE IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIR PER REO601R 53-61-117 REV C DATED 08-25-07. 2 L 7 2 4F RT A21EA 2008031300255 20080313 00255 EA 2008 3 13 SWIA200719310 1 20071119 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 453SW 7743 STN 621 AND RBL42.0 BULKHEAD ANGLE IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO601R 53-61-117 REV C DAT ED 08-25-07. 2 L 7 2 4F RT A21EA 2008031300282 20080313 00282 EA 2008 3 13 SWIA200719314 1 20071206 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 750SK 10207 FS 280 AND LBL9 BEAM IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER CRJ700 SRM 51-42-06-001-001-A01 AND 51-42- 21-001-001-A01. 2 L 7 2 4F RT A21EA 2008031400094 20080314 00094 NM 2008 3 14 2007UALA04773 1 20071120 A 3610 50U23401 LINE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 2 BLEED SYS LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 206UA 30212 222049 NR 2 ENGINE BLEED PROBLEMS. SECURED HPSOV MUSCLE LINE. ALL PRESSURES CHECK NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008031300246 20080313 00246 EA 2008 3 13 SWIA200719306 1 20071119 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 453SW 7743 FS 280 AND LBL9.0 LOWER FLOORBEAM IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS IAW CRJ200 REO 601R-53-11-171 RE V D. 2 L 7 2 4F RT A21EA 2008031300281 20080313 00281 EA 2008 3 13 SWIA200719313 1 20071121 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 751SK 10208 FS 280 BEAM IS CRACKED AT LBL 9 AND RBL 9, FOUND AT C-CHECK. COMPLIED WITH REPAIR AS PER CRJ700 SRM 51-42-06 PG 7-8, 51 -42-13 PG 4 AND REO 670-5-11-265. 2 L 7 2 4F RT A21EA 2008031300328 20080313 00328 NM 2008 3 13 UPS08M51763 1 20071216 A 5330 SKIN DOUG MD11 MD11F 3023600 NM BS 1778 MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 47473 INSPECTION TYPE:C CENTER CARGO/AT STATION 1778 ABOVE AND IN BETWEEN LONGERON 36 TO LONGERON 37 INTERNAL SKIN ON JAMB ARE A FOUND WITH UNAPPROVED SRM REPAIR. UNAPPROVED SRM REPAIR DOUBLER REMOVED PER SRM 51-33-01 V.II R35. REPAIR SKIN CRACK TRIMMED AS PER EN NR 1011-08 SHT 4 OF 4. HFEC INSP C/O PER DAC NDTSPM R13 06-10-01.001 ON TRIMMED OFF AREA AND FOUND N O CRACK EVIDENT. REPAIR SKIN FILLER AND REPAIR SKIN DOUBLER FAB PER EN NR 1011-08. THIS REPAIR IS TIME LIMITED FOR 24 MTHS PENDING A DAMAGE TOLERANCE ANALYSIS. 2 L 7 3 4F RT A22WE 2008031400095 20080314 00095 NM 2008 3 14 2007UALA05119 1 20071215 A 4990 1605361 VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU THERMAL BYPA SHUTDOWN A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 211UA 30217 APU AUTO SHUTDOWN AT DEPARTURE. HIGH OIL TEMP. ALSO, APU OIL PRESSURE -3 PSI. REPLACED LUBE CLUSTER AND THERMAL BYPAS S VALVEA/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008031800097 20080318 00097 NM 2008 3 18 UPS08M51777 1 20071205 A 5320 SCUFF PLATE DOUG MD11 MD11 3023602 NM FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C FWD CARGO DOOR CUTOUT LOWER AFT CORNER DOUBLER UNDERNEATH SCUFF PLATE IS NON-STANDARD REPAIR FORWARD C ARGO DOOR CUTOUT AFT SCUFF PLATE REMOVED PER AMM20-50-00. NON-STANDARD REPAIR DOUBLERS REMOVED PER SRM 51-31-01 V.II R3 5. HFEC INSP C/ O PER DAC NDTSPM R13 06-10-01.001 ON EXISTING TRIMMED OFF AREA AND FOUND NO CRACK EVIDENT. REPAIR FILL ERS AND DOUBLERS FAB AND INSTALL PER SRM 53-50- 00-FIG 6 VOL I REV 35. 2 L 7 3 4F RT A22WE 2008031900104 20080319 00104 CE 2008 3 19 AMWA88346 1 20071101 A 7931 OIL SYSTEM BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RT ENGINE LOW PRESSURE A AMWA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CE 07 161YV 20945 10942 UE161 DURING DESCENT, CREW NOTICED SMOKE IN CABIN AND COCKPIT AND LOSS OF RT ENGINE OIL PRESSURE. ENGINE SHUTDOWN WITHOUT CREW ACTION, CREW DIVERTED AC AND LANDED AC WITHOUT FURTHER INCIDENT. TEARDOWN AT MFG FOUND POWER SECTION S/N 114135 (TSO 65 01.1) OIL NOZZLE FOR NR 3 AND NR 4 BEARINGS COKED. PROBABLE CONTRIBUTING FACTORS NOTED BY MFG WERE INCOMPLETE, CLEANING OF OIL JET LUBRICATING TUBE DURING LAST OVERHAUL AND HIGH BEARING COMPARTMENT TEMP OF NOZZLE. 2 L 7 2 4T 3 T RT A24CE E2NE 2008031900103 20080319 00103 NE 2008 3 19 AMWA89104A 2 20071214 A 7200 PT6A67 ENGINE BEECH 1900 1900D 1154162 CE PWC PT6 PT6A67AG 52211 NE RIGHT COKED A AMWA E ENGINE SHUTDOWN O OTHER AP APPROACH 1 CE 07 174YV 23832 6501 UE174 114283 CREW REPORTED ON APPROACH THE RT LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED AND OIL PRESSURE INDICATED 60 PSI. ENGINE CONT INUED TO SHUT ITSELF DOWN. EMERGENCY DECLARED AND AIRCRAFT LANDED SAFELY. MAINTENANCE CONFIRMED METAL IN OIL FILTER. POW ER SECTION TEARDOWN RESULTS FROM MFG SHOW OIL NOZZLE FOR NR 3 AND NR 4 BEARINGS FOUND COKED. PROBABLE CONTRIBUTING FACTO RS WERE INCOMPLETE CLEANING OF OIL JET LUBRICATING TUBE DURING LAST OVERHAUL AND HIGH BEARING COMPARTMENT TEMPERATURE OF NOZZLE. NOTE: POWER SECTION S/N 114135 AND GAS GENERATOR S/N 114283 WERE SENT TO SHOP AS A UNIT. 2 L 7 2 4T 4 T RT A24CE E26NE 2008032000083 20080320 00083 SO 2008 3 20 2008F00002 1 20070611 A 7820 6751700 MUFFLER PIPER PA32 PA32300 7103212 SO LYC O540 IO540K1G5 41532 EA HARTZL HCC2Y HCC2YR1 GL ENGINE BROKEN G LABA B A EMER. DESCENT UNSCHED LANDING A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 AL 05 6117J 327640095 ON CLIMB AFTER TAKEOFF, PILOT HEARD BANG IN ENGINE COMPARTMENT, SMOKE AND FLAMES ENTERED CABIN AT PILOT'S FEET. AFTER L ANDING AIRCRAFT, AIRCRAFT BURN, TOTAL LOSS. MUFFLER FOUND CRACKED/BROKEN EMITTING HEAT, FLAME, ETC. THROUGH HEATER MUFF INTO CABIN. 1 L 7 1 3O 3 O A3SO 1E4 5 C P920 2008032000094 20080320 00094 EA 2008 3 20 SWIA200719333 1 20071206 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 455SW 7760 FOUND AT C-CHECK, FLOORBEAM STA 280 AND RBL9, LOWER FLOORBEAM IS CRACKED. COMPLIED WITH REPAIR PER REO 601R-53-11-1305 AND REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 2008032000098 20080320 00098 EA 2008 3 20 SWIA200719337 1 20071206 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 455SW 7760 FOUND AT C-CHECK, PASSENGER DOOR EMERGENCY EXIT BETA LIGHT IS BROKEN. REPLACED EMERGENCY EXIT BETA LIGHT PER CRJ200 AMM 33-51-09-400-801. 2 L 7 2 4F RT A21EA 2008032000099 20080320 00099 EA 2008 3 20 SWIA200719338 1 20071206 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS LOOSE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 455SW 7760 FOUND AT C-CHECK, EMERGENCY TRACK LIGHTING CENTER SECTION IS INOP. SECURED CENTER SECTION LIGHT STRIP CONNECTOR PER CRJ WDM 31-51-00. 2 L 7 2 4F RT A21EA 2008031900336 20080319 00336 NM 2008 3 19 DXTA200802817 1 20070131 A 4900 21189882 ECU GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE APU INOPERATIVE E DXTA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 GL 07 725QS 2902 105 DURING APU SHUTDOWN FLAMES WERE COMING OUT OF EXHAUST, NO FIRE WARNING LIGHTS OR MSG OF ANY KIND. OPENED UP APU FIRE SW ITCH AND DISCHARGED RT FIRE BOTTLE INTO APU, FIRE EXTINGUISHED. M2B- INSPECTED APU AND TAIL CONE AREA FOR DAMAGE NONE N OTED. PERFORMED ALERT SB GTCP-36-49-A7967 ON APU SHUT OFF SOLENOID VALVE, NO LEAK DETECTED. REMOVED AND REPLACED FUEL SH UT OFF SOLENOID VALVE WITH A OVERHAULED UNIT AND PERFORMED ALERT. GTCP36-49-A7867 AS WELL IAW MFG REP LOOSE IAW MFG GTCP 36-150 MM CHAPTER 49-24-14. ALSO CHECKED FOR VOLTAGE AT FUEL SHUTOFF SOLENOID VALVE AT CONNECTOR AT BETWEEN PINS A+C NO VOLTAGE. ALSO REMOVED AND REPLACED ECU P/N 2118988-2 OFF S/N 102-00084 AND INSTALLED A MODIFIED ON + P/N2118988-2 S/N 6 2 L 7 2 4F 4 F RT A53NM E35NE 2008032000097 20080320 00097 EA 2008 3 20 SWIA200719336 1 20071206 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 455SW 7760 FOUND AT C-CHECK, BS 280 AT LBL 9 LOWER FLOORBEAM IS CRACKED. COMPLIED WITH REPAIRS PER CRJ200 REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 2008032000095 20080320 00095 EA 2008 3 20 SWIA200719334 1 20071206 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 455SW 7760 FOUND AT C-CHECK, STA 280 RIGHT UPPER FLOORBEAM ANGLE IS CRACKED AT RBL9. COMPLIED WITH REPAIRS IAW REO 601-53-11-136. 2 L 7 2 4F RT A21EA 2008032000096 20080320 00096 EA 2008 3 20 SWIA200719335 1 20071206 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 455SW 7760 FOUND AT C-CHECK, FLOORBEAM IS CRACKED AT BS 280 AND LBL9. INSTALLED REPAIR PARTS IAW REO 601R-53-11-136. 2 L 7 2 4F RT A21EA 2008032000102 20080320 00102 NM 2008 3 20 UPS08M51778 1 20071205 A 5330 SKIN DOUG MD11 MD11 3023602 NM ZONE 100 UNKNOWN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C FWD CARGO DOOR CUTOUT AFT EDGE FROM L36-RT L40 FOUND PREVIOUS EDGE BLEND OUT REPAIRS AS MARKED. REPAI R DOUBLERS REMOVED PER SRM 51-31-01 V II R35. HFEC INSP C/O AS PER DAC NDTSPM R13. 06-10-01.001 ON REWORKED AREA AND FO UND NO CRACK EVIDENT. REPAIR FILLERS AND DOUBLERS FAB PER SRM53-50-00 FIG 16 V.I R35. REPAIR PARTS INSTALLED PER SRM 5 3-50-00 FIG 16 VOL REV 35. 2 L 7 3 4F RT A22WE 2008032400356 20080324 00356 NM 2008 3 24 2008UALA00024 1 20071230 A 2760 B435428 PCU BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 4 SPOILER FAULTY A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 221UA 30552 SPOILER EICAS AND FLIGHT CONTROL SYS STATUS MSSG ON PUSHBACK. REPLACED NR 4 SPOILER PCU, REPLACED ACE L2. ALSO REPLACE D COUPLER (HARNESS) B27122 IN P212. ACE L2 LRU RPL TEST AND PRI FLT CONTROL SELF TEST PASSED. CONFIRMED SPOILER OPS AND INDICATION NORMAL, AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032500017 20080325 00017 NM 2008 3 25 2007UALA04991 1 20071207 A 5330 148W1314 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUSELAGE MISREPAIRED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 797UA 42802 26924 EXTERNAL FUSELAGE HAS 1 EA LARGE TRI-WING FASTENER INSTALLED THROUGH SKIN AT STATION 2200 NEAR STRINGER 32R. SUSPECTED LIGHTNING STRIKE. FASTENER IS SUBSTITUTED FOR RIVET SRM 51-40-03-001 PARA 4. REMOVED FASTENER DID HFEC INSP, NO CRACK. INSTALLED REPAIR 53-00-01 PARA 6, A/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032500018 20080325 00018 NM 2008 3 25 2007UALA05118 1 20071216 A 2421 757183F CONVERTER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RIGHT FAULTY A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 788UA 26942 RIGHT ENGINE GENERATOR OFF LIGHT CAME ON MOMENTARILY AFTER LIFTOFF. RECURRED ON FLT 0935-15JAN08. REPLACED NR 2 IDG PE R MM 24-11-01, RAN ENGINE PER JRH IDG OPS NORMAL GENERATOR OPS LIGHT STILL COMES ON. REPLACED CONVERTER. TEST PASSED. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032500045 20080325 00045 NE 2008 3 25 AMWA89215 2 20071221 A 7250 BEARING BEECH 1900 1900D 1154162 CE PWC PT6 PT6A67AG 52211 NE GAS GENERATOR SPALLED A AMWA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 07 161YV 19796 7396 UE161 114478 DURING LEVEL FLIGHT THE LT ENGINE BEGAN TO SURGE AND THEN STARTED TO FALL OFF LINE. BLUE SMOKE IN CABIN/COCKPIT AND FLAM ES OUT OF THE EXHAUST WERE REPORTED. AIRCRAFT LANDED SAFELY. TEARDOWN REPORT BY MFG INDICATES THAT SHUTDOWN WAS CAUSED B Y DISTRESSED NR1 BEARING DUE TO SPALLING CONDITION OF ONE BALL AND OUTER RACE, WITH FRACTURE OF BEARING CAGE. SPALLING C AUSED BY ELECTRIC DISCHARGE DAMAGE, TYPICAL TO CURRENT LEAKAGE FROM ENGINE STARTER AS DEMONSTRATED BY OBSERVED EDD PITS ON STARTER GEAR, AGB DRIVE GEAR AND NR1 BEARING. 2 L 7 2 4T 4 T RT A24CE E26NE 2008032600168 20080326 00168 EA 2008 3 26 SWIA200719363 1 20071216 A 5320 BEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 753SK 10214 FS 280 BEAM IS CRACKED AT RBL9, FOUND AT C-CHECK. COMPLIED WITH REPAIR OF BEAM PER CRJ7/9 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008032600169 20080326 00169 EA 2008 3 26 SWIA200719364 1 20071216 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 753SK 10214 FS280 COCKPIT FLOOR SUPPORT IS CORRODED, FOUND AT C-CHECK. REPLACED COCKPIT FLOOR SUPPORT PER CRJ700 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008032600188 20080326 00188 CE 2008 3 26 J00A200706001 1 20070809 A 2431 29783003 SENSING ELEMENT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL BATTERY DELAMINATED E J00A B EMER. DESCENT N FALSE WARNING CL CLIMB 1 EA 01 706VP 4215 4215 7500006 AC RETURNED TO DEPARTURE AIRPORT IMMEDIATELY IAW EMERGENCY PROCEDURES. BATTERY OVERTEMP RT EICAS MESSAGE. FOUND THE OVE RTEMP SENSOR FAILED WITH HIGH RESISTANCE SIMULATING OVERTEMP CONDITION AND SENSOR WAS DELAMINATED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032600241 20080326 00241 SO 2008 3 26 265121707A 1 20071217 A 5311 FRAME EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE FUSELAGE CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 285AS 120265 AT SCHEDULED INSPECTION, DISCOVERED (3) SPOTS OF CORROSION ALONG FRAME 23 BETWEEN STRINGERS 20L AND 20R. CORROSION DID N OT PENTRATE TO FRAME 23, OR STRINGERS, REMOVED DAMAGED AREA AS ONE ENCOMPASSING AREA AND INSTALLED EXTERNAL DOUBLER. R EFERENCE MFG ENGINEERING DOCUMENT ICA2007-120/09243. 2 L 7 2 4T 4 T RT A31SO E20NE 2008032700164 20080327 00164 NM 2008 3 27 2007UALA04654 1 20071108 A 2721 658D1005 ACTUATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RUDDER TRIM FAULTY A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 651UA 25389 AIRCRAFT REQUIRES 4 UNITS LEFT RUDDER TRIM DURING CRUISE. L & R FUEL TANKS BALANCED. SUSPECT RUDDER TRIM ACTUATOR. REP LACED RUDDER TRIM ACTUATOR. ALL SYSTEMS CHECK NORMAL. PERFORM SINGLE HYDRAULIC SYSTEM CHECK OF EACH RUDDER POWER CONTR OL ACTUATOR USING EACH HYDRAULIC SYSTEM IN SEQUENCE. TESTED FIVE MORE TIMES BEFORE HMV NO DISCREPANCIES. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040100243 20080401 00243 EU 2008 4 1 SA08020 1 20070327 A 2560 P2070001215 FLASHLIGHT AIRBUS A319 A319112 3930323 EU CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 723UW 1109 RIC - EMERGENCY FLASHLIGHT WEAK IN LEFT FORWARD FLIGHT ATTENDANT POSITION. MAINTENANCE REMOVED AND REPLACED THE EMERGEN CY FLASHLIGHT ASSEMBLY. 2 L 7 2 4F RT A28NM 2008040300165 20080403 00165 EA 2008 4 3 SWIA200719417 1 20071212 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 939SW 7742 FS 280 AT LBL9 UPPER FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS AT UPPER FLOOR SUPPORT FS 280 AN D LBL9 PER REO 601R-53-11-136. 2 L 7 2 4F RT A21EA 2008040300166 20080403 00166 EA 2008 4 3 SWIA200719418 1 20071212 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN DAMAGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 939SW 7742 PAX DOOR ENTRANCE EMERGENCY LIGHT IS INOP, FOUND AT C-CHECK. REPAIRED EMERGENCY LIGHT WIRING IAW CRJ200 AMM TASK 33-51- 13-400-801. 2 L 7 2 4F RT A21EA 2008040300168 20080403 00168 EA 2008 4 3 SWIA200719420 1 20071216 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 908SW 7540 CRACK FOUND ON LEFT SIDE OF STA 280 AT LBL 9, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 REO 601R-53-11-171 RE V D. 2 L 7 2 4F RT A21EA 2008040300169 20080403 00169 EA 2008 4 3 SWIA200719421 1 20071216 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 908SW 7540 CRACKING FOUND AT STA 280 UPPER FLANGE BETWEEN LBL 9 AND RBL 9, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 REO 601R-53-11-136 REV A. 2 L 7 2 4F RT A21EA 2008040300171 20080403 00171 EA 2008 4 3 SWIA200719423 1 20071216 A 5320 FLANGE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 908SW 7540 CRACK FOUND ON LOWER FLANGE OF RBL9 AT STA 280. COMPLIED WITH REPAIRS IAW CRJ200 REO 601R-53-11-171 REV D REPAIR A. 2 L 7 2 4F RT A21EA 2008040300172 20080403 00172 EA 2008 4 3 SWIA200719424 1 20071229 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 951SW 7795 FOUND AT C-CHECK, CARGO BAY FLOOR IS CRACKED AT STA 574 AND LBL42. COMPLIED WITH REPAIRS IAW PER CRJ200 REO601R-53-61-1 741. 2 L 7 2 4F RT A21EA 2008040300173 20080403 00173 EA 2008 4 3 SWIA200719425 1 20071229 A 2740 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 951SW 7795 FOUND AT C-CHECK, HORIZONTAL STABILIZER ACTUATOR CHASSIS IS CRACKED ON RIGHT SIDE. REPLACED HORIZONTAL STABILIZER TRIM ACTUATOR IAW CRJ200 AMM TASK 27-42-01-400-801 AND 27-42-01-000-801. 2 L 7 2 4F RT A21EA 2008040300174 20080403 00174 EA 2008 4 3 SWIA200719426 1 20071229 A 7120 BUSHING CNDAIR CL600 CL6002B19 1900309 EA ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 951SW 7795 FOUND AT C-CHECK, LEFT ENGINE MOUNT HAT BUSHINGS AND FLOATING BUSHINGS SHOW SIGNS OF CORROSION. REPLACED ENGINE MOUNT H AT BUSHINGS AND FLOATING BUSHINGS PER CRJ200 AMM 71-21-01-400-801. 2 L 7 2 4F RT A21EA 2008040300175 20080403 00175 EA 2008 4 3 SWIA200719427 1 20071229 A 7120 LINK CNDAIR CL600 CL6002B19 1900309 EA ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 951SW 7795 FOUND AT C-CHECK, LEFT ENGINE MOUNT FORWARD LINK IS CORRODED. REPLACED LEFT ENGINE FORWARD MOUNT LINK AND BUSHING PER C RJ200 AMM 71-21-01-400-801, P/N 601-37016-5, S/N RJ/SWA/0064. 2 L 7 2 4F RT A21EA 2008040400021 20080404 00021 CE 2008 4 4 ZESA2007002 1 20071227 A 3233 6632201000005 ACTUATOR LEAR 45 45LEAR 5170805 CE MLG BYPASSING E ZESA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 03 70AE 1491 208 227 AFTER TAKE OFF, PILOT SELECTED GEAR UP, NOSE GEAR DID NOT RETRACT. PILOT SELECTED GEAR DOWN, WITH ALL (3) GEAR DOWN AND LOCKED, LANDED BACK AT ORIGINAL AIRPORT. ACTUATOR BYPASSING. 2 L 7 2 4F RT T00008WI 2008040300170 20080403 00170 EA 2008 4 3 SWIA200719422 1 20071216 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 908SW 7540 FOUND AT C-CHECK, FORWARD COCKPIT FLOOR SUPPORT IS CRACKED. REPLACED FORWARD FLOOR SUPPORT PER CRJ200 SRM 51-42-06 PG 1 -18. 2 L 7 2 4F RT A21EA 2008040400022 20080404 00022 CE 2008 4 4 ZESA2007001 1 20071012 A 2731 66001 CONTROL CABLE CESSNA CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE ELEVATOR TRIM LOOSE E ZESA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 03 877RF 1517 13 5219 AFTER TAKEOFF, FOUND ELEVATOR TRIM JAMMED, RETURNED TO ORIGINAL AIRPORT. INSPECTION OF ELEVATOR TRIM SYSTEM REVEALED TRI M CABLES EXCESSIVELY LOOSE. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008040300163 20080403 00163 EA 2008 4 3 SWIA200719415 1 20071212 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 939SW 7742 FOUND AT C-CHECK, LOWER FRAME AT STA 280 AND RBL10 IS CRACKED. COMPLIED WITH REPAIRS AT STA 280 AND RBL10 PER CRJ200 RE O601R 53-11-1314. 2 L 7 2 4F RT A21EA 2008040300164 20080403 00164 EA 2008 4 3 SWIA200719416 1 20071212 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 939SW 7742 FOUND AT C-CHECK, CRACK IN LOWER FRAME AT STA280 AND LBL10. COMPLIED WITH REPAIRS AT STA 280 AND LBL10 PER REO 601R-53- 11-171. 2 L 7 2 4F RT A21EA 2008040300167 20080403 00167 EA 2008 4 3 SWIA200719419 1 20071229 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 951SW 7795 STA 280 BEAM IS CRACKED JUST OUTBOARD OF COCKPIT DOOR OPENING ON RIGHT SIDE, FOUND AT C-CHECK. INSTALLED REPAIR PARTS A T STN 280 AND RBL9.0 PER RJ200 REO 601R-53-11-171 REV D REPAIR SCHEME B. 2 L 7 2 4F RT A21EA 2008040800065 20080408 00065 NM 2008 4 8 HNAA0800115 1 20071128 A 5347 85300132102 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 804EX 227 CTR FLOOR RIGHT SEAT TRACK CORRODED. REPLACED DEFECTIVE SEAT TRACK. 2 H 7 2 4T RT A13NM 2008041000188 20080410 00188 CE 2008 4 10 DELA200700008 1 20071005 A 2840 WARNING LIGHT LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP LOW FUEL; FALSE INDICATION E DELA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 773DL 174 LOW FUEL LIGHT ILLUMINATED WITH 4000 LBS TOTAL FUEL ON AIRPLANE AND 1200 LBS FUEL IN THE WINGS. FUEL READER GAUGE INDICA TED 400 LBS OF FUEL ON RT WING. LATER ON WENT BACK TO INDICATE 1200 LBS ON THE WINGS. TAKE OF (SIC) WITH 4000 LBS TOTAL LANDING WEIGHT WAS 13,800. CLEANED F.Q. C/B CONTACTS, SUMPED FUEL TANKS (NO CONTAMINATION FOUND), PERFORMED GROUND ENGIN E RUN WHILE OBSERVING CKPT INDICATIONS. OPS NORMAL. (MAX LANDING WEIGHT 14300). 2 L 7 2 4F 4 F A10CE E6WE 2008041400032 20080414 00032 CE 2008 4 14 M000999 1 20070824 A 3411 CM29337 STATIC PORT CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP LEAKING E VQMA A UNSCHED LANDING S J AFFECT SYSTEMS WARNING INDICATION CR CRUISE 1 NM 03 650Z 11709 11709 6500108 SPLIT IN ALTIMETERS (RT ALTIMETER INDICATES 400 FOOT HIGHER THAN LT ALTIMETER AT 41,000 FT MSL) VERIFIED SPLITS IN ALTIM ETERS AND PILOTS PITOT/STATIC SYS. INSTALLED NEW CO-PILOTS STATIC PORT FITTING P/N CM2933-7. LEAK CHECK, SAND, FILLED, PRIMED, PAINTED AND RVSM SKIN WAVINESS SATISFACTORY. 2 L 7 2 4F 4 F A9NM E6WE 2008042100089 20080421 00089 EU 2008 4 21 WRNA200700070 1 20071011 A 5320 FITTING AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 510TA 100 DURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STR TIE END ANGLE FITTING AT 38R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40, APPLIED PROTECTIVE COATIN GS IAW SRM 51-40-12, INSTALLED FITTING IAW SRM 51-30-30. 2 L 7 2 4F RT A35EU 2008042300111 20080423 00111 EU 2008 4 23 1218361042108 1 20071210 A 5312 S5387140921401 STIFFENER AEROSP ATR42 ATR42320 8680930 EU AFT BULKHEAD CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 AFT PRESSURE BULKHEAD FORWARD FACE (3) LOWER STIFFENERS CORRODED. CORROSION REMOVED, 2 STIFFENERS FOUND TO BE WITHIN LI MITS, 1 REMOVED AND REPLACED IN ACCORDANCE WITH SRM. 2 H 7 2 4T RT A53EU 2008042300113 20080423 00113 EU 2008 4 23 1218363042108 1 20071203 A 5310 NTA44182 CREASE BEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 LEFT CREASE BEAM INNER CHORD BETWEEN FRAME 17 AND 20 CORRODED. CORROSION REMOVED AND FOUND TO BE WITHIN LIMITS CREASE B EAM INNER CHORD REPAIRED PER SRM. 2 H 7 2 4T RT A53EU 2008042300116 20080423 00116 EU 2008 4 23 1218364042108 1 20071120 A 5347 S5367800120002 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 CORROSION FOUND ON SEAT TRACK LEFT OUTBOARD SIDE BETWEEN FRAME 29 TO 36. CORROSION FOUND TO BE OUT OF LIMITS SEAT TRACK REPLACED PER SRM. 2 H 7 2 4T RT A53EU 2008042300117 20080423 00117 EU 2008 4 23 1218366042108 1 20071121 A 5347 S5367800121202 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 CORROSION FOUND ON SEAT TRACK LEFT SIDE BETWEEN FRAMES 39 TO 41. CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED SEAT TRACK AND REPLACED PER SRM. 2 H 7 2 4T RT A53EU 2008042300153 20080423 00153 EU 2008 4 23 1218361804218 1 20071203 A 5240 S53671390286 SEAL DEPRESSOR AEROSP ATR42 ATR42320 8680930 EU SERVICE DOOR CRACKED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 SERVICE DOOR LOWER FORWARD CORNER SEAL DEPRESSOR CRACKED. SEAL DEPRESSOR REMOVED AND REPLACED PER SRM. 2 H 7 2 4T RT A53EU 2008042300155 20080423 00155 EU 2008 4 23 1218362004218 1 20071122 A 5320 NTA44770 SHIM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 SHIM BETWEEN STRINGER 15 AND SKIN AT FRAME 41 CORRODED. REMOVED AND FABRICATED SHIM IN ACCORDANCE WITH SRM. 2 H 7 2 4T RT A53EU 2008042300156 20080423 00156 EU 2008 4 23 1218362104218 1 20071121 A 5315 NTA44770 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 FLOORBEAM AT FRAME 40 CORRODED. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS. FLOORBEAM REPAIRED IN ACCORDANCE WITH SRM. 2 H 7 2 4T RT A53EU 2008042300157 20080423 00157 EU 2008 4 23 1218363020708 1 20071213 A 5280 S5287660223400 STIFFENER AEROSP ATR42 ATR42320 8680930 EU NLG DOOR CRACKED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 STIFFENER BROKEN ON FORWARD LEFT SIDE OF NOSE LANDING GEAR DOOR. LEFT AFT NOSE LANDING GEAR DOOR STIFFENER REPLACED IN ACCORDANCE WITH SRM. 2 H 7 2 4T RT A53EU 2008042300185 20080423 00185 EU 2008 4 23 1218365020708 1 20071204 A 3350 3011210 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN FAILED A HYIA K NONE L NO TEST IN INSP/MAINT 1 EA 61 42836 200 EMERGENCY LIGHT ON PAX DOOR NOT WORKING. REMOVED AND REPLACED EMERGENCY LIGHT. 2 H 7 2 4T RT A53EU 2008042300201 20080423 00201 EU 2008 4 23 1218362041408 1 20071214 A 5753 S57510096200 FITTING AEROSP ATR42 ATR42320 8680930 EU TE FLAP CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 LEFT OUTBOARD FLAP FORWARD PICK UP FITTING AT FLAP RIB 18 VERTICAL WEB EDGE CORROSION. REPAIRED PER ATR STRUCTURAL REPA IR INSTRUCTIONS. 2 H 7 2 4T RT A53EU 2008042300108 20080423 00108 EU 2008 4 23 1218361020708 1 20071211 A 5230 S25237620120405 PAN AEROSP ATR42 ATR42320 8680930 EU CARGO DOOR CRACKED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 THE LOWER FORWARD CARGO DOOR PAN CRACKED. REPAIRED IN ACCORDANCE WITH ATR DRAWING NR 13S523R0028. 2 H 7 2 4T RT A53EU 2008042300112 20080423 00112 EU 2008 4 23 1218362042108 1 20071203 A 5310 NTA44182 CREASE BEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 FORWARD CARGO RIGHT CREASE BEAM INNER CHORD ANGLE BETWEEN FRAMES 13 AND 23, STRINGER RIGHT 14 CORRODED. CORROSION REMOV ED AND FOUND TO BE WITHIN LIMITS CREASE BEAM CHORD REPAIRED PER SRM. 2 H 7 2 4T RT A53EU 2008042300191 20080423 00191 EU 2008 4 23 1218366020708 1 20071213 A 5210 SKIN AEROSP ATR42 ATR42320 8680930 EU PAX DOOR CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 PASSENGER DOOR INNER SKIN CORRODED AT TOP AFT CORNER. PASSENGER DOOR INNER SKIN REPAIRED AT TOP AFT CORNER AND CORROSIO N REMOVED. 2 H 7 2 4T RT A53EU 2008042300193 20080423 00193 EU 2008 4 23 1218361021008 1 20071210 A 5240 SKIN AEROSP ATR42 ATR42320 8680930 EU SERVICE DOOR CRACKED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 SERVICE DOOR EXTERNAL SKIN CRACKED AT FORWARD LOWER CORNER. SERVICE DOOR SKIN REPAIRED IN ACCORDANCE WITH SRM. 2 H 7 2 4T RT A53EU 2008042300234 20080423 00234 EU 2008 4 23 1218366041408 1 20071205 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU EMERGENCY LIGHTS NO TEST A HYIA K NONE L NO TEST IN INSP/MAINT 1 EA 61 42836 200 EMERGENCY LIGHT POWER SUPPLY BATTERY FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY. 2 H 7 2 4T RT A53EU 2008042300235 20080423 00235 EU 2008 4 23 1218367041408 1 20071205 A 3350 3011151 BATTERY AEROSP ATR42 ATR42320 8680930 EU EMERGENCY LIGHTS NO TEST A HYIA K NONE L NO TEST IN INSP/MAINT 1 EA 61 42836 200 EMERGENCY LIGHT POWER SUPPLY BATTERY FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY. 2 H 7 2 4T RT A53EU 2008042300237 20080423 00237 EU 2008 4 23 1218368041408 1 20071205 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU EMERGENCY LIGHTS NO TEST A HYIA K NONE L NO TEST IN INSP/MAINT 1 EA 61 42836 200 EMERGENCY LIGHT POWER SUPPLY BATTERY FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY. 2 H 7 2 4T RT A53EU 2008042300240 20080423 00240 EU 2008 4 23 1218361004148 1 20071205 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU EMERGENCY LIGHTS NO TEST A HYIA K NONE L NO TEST IN INSP/MAINT 1 EA 61 42836 200 EMERGENCY LIGHT POWER SUPPLY BATTERY FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY. 2 H 7 2 4T RT A53EU 2008042300242 20080423 00242 EU 2008 4 23 121836142008 1 20071205 A 5330 S53371110200 SKIN PANEL AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 EXTERNAL SKIN UNDER TCAS ANTENNA TOP OF FRAME 16-17 HAS CORROSION. CORROSION REMOVED AND FOUND TO BE WITHIN LIMITS IN A CCORDANCE WITH SRM. 2 H 7 2 4T RT A53EU 2008042300245 20080423 00245 EU 2008 4 23 121836042008 1 20071210 A 5311 S538714042001 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 FRAME 44 AFT FACE CORRODED AT JUNCTION OF LEFT AND RIGHT SEAT TRACK, FOUND TO BE OUT OF LIMITS. NEW FRAME SEGMENT WAS S PLICED IN, IN ACCORDANCE WITH SRM. 2 H 7 2 4T RT A53EU 2008042100086 20080421 00086 EU 2008 4 21 WRNA200700067 1 20071011 A 5340 FITTING AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 510TA 100 DURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STR TIE END ANGLE FITTING AT 35R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40, APPLIED PROTECTIVE COATIN GS IAW SRM 51-40-12, INSTALLED FITTING IAW SRM 51-30-30. 2 L 7 2 4F RT A35EU 2008042100087 20080421 00087 EU 2008 4 21 WRNA200700068 1 20071011 A 5320 FITTING AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 510TA 100 DURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STR TIE END ANGLE FITTING AT 36R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40, APPLIED PROTECTIVE COATIN GS IAW SRM 51-40-12, INSTALLED FITTING IAW SRM 51-30-30. 2 L 7 2 4F RT A35EU 2008042100088 20080421 00088 EU 2008 4 21 WRNA200700069 1 20071011 A 5320 FITTING AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 510TA 100 DURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STR TIE END ANGLE FITTING AT 37R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40, APPLIED PROTECTIVE COATIN GS IAW SRM 51-40-12, INSTALLED FITTING IAW SRM 51-30-30. 2 L 7 2 4F RT A35EU 2008042100097 20080421 00097 NM 2008 4 21 CALA0700684 1 20071112 A 5320 69265552 ANGLE BOEING 737 7373T0 1384582 NM BS 348-351 S16L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND A .5 INCH CRACK IN UPPER ANGLE AT S16L BETWEEN STA 348.2 AND 351.2. THE ANGLE WAS REPLACED IAW ECRA 53 11-01375. 2 L 7 2 4F RT A16WE 2008042100099 20080421 00099 NM 2008 4 21 CALA0700686 1 20071112 A 5320 69165096 ANGLE BOEING 737 7373T0 1384582 NM BS 348-351 S16L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 INSPECTION FOUND A .5 INCH CRACK IN ATTACHMENT ANGLE ON STRINGER 16L BETWEEN STA 348.2 AND 351.2. THE ATTACHMENT ANGLE WAS REPLACED IAW ECRA 5311-01375. 2 L 7 2 4F RT A16WE 2008042300109 20080423 00109 EU 2008 4 23 1218362020708 1 20071120 A 5220 S5227750120001 ATTACH FITTING AEROSP ATR42 ATR42320 8680930 EU EMERGENCY EXIT CRACKED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 RIGHT EMERGENCY EXIT, FORWARD ATTACHMENT POINT CRACKED. REMOVED AND REPLACED EMERGENCY EXIT FORWARD ATTACHMENT POINT IN ACCORDANCE WITH SRM. 2 H 7 2 4T RT A53EU 2008042300114 20080423 00114 EU 2008 4 23 1218365042108 1 20071120 A 5347 S5367800121202 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 CORROSION FOUND ON SEAT TRACK RIGHT BETWEEN FRAMES 39 AND 40. CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED AND REPL ACED SEAT TRACK IN ACCORDANCE WITH SRM. 2 H 7 2 4T RT A53EU 2008042300136 20080423 00136 EU 2008 4 23 1218367042108 1 20071121 A 5347 S5367800121002 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 CORROSION FOUND ON SEAT TRACK RIGHT SIDE BETWEEN FRAMES 36 AND 39. CORROSION OUT OF LIMITS, FABRICATED AND REPLACED SEA T TRACK IN ACCORDANCE WITH SRM. 2 H 7 2 4T RT A53EU 2008042300137 20080423 00137 EU 2008 4 23 1218368042108 1 20071213 A 5311 2024T3 FRAME SPLICE AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 CORROSION FOUND ON BELLY FRAME 27. CORROSION REMOVED, FRAME REPAIRED IN ACCORDANCE WITH SRM. 2 H 7 2 4T RT A53EU 2008042300138 20080423 00138 EU 2008 4 23 1218369042108 1 20071214 A 5311 S5397140320102 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 CORROSION AND BARE METAL FOUND AT BELLY FRAME 28. CORROSION REMOVED FROM BELLY FRAME 28 RIGHT AND LEFT WEB. BELLY FRAM E 28 LEFT AND RIGHT WEBS REPLACED IN ACCORDANCE WITH SRM. 2 H 7 2 4T RT A53EU 2008042300139 20080423 00139 EU 2008 4 23 1218361004218 1 20071120 A 5347 S5337500120002 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 CORROSION FOUND ON SEAT TRACK RIGHT SIDE OUTBOARD SIDE BETWEEN FRAMES 13 AND 23. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK IN ACCORDANCE WITH SRM. 2 H 7 2 4T RT A53EU 2008042300140 20080423 00140 EU 2008 4 23 1218361104218 1 20071120 A 5320 S5307030026000 THRESHOLD AEROSP ATR42 ATR42320 8680930 EU FUELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 RIGHT THRESHOLD BETWEEN FRAMES 36 AND 39 CORRODED. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INS TALLED THRESHOLD. 2 H 7 2 4T RT A53EU 2008042300141 20080423 00141 EU 2008 4 23 1218361204218 1 20071210 A 5320 S5307030922501 SUPPORT ANGLE AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 RIGHT BETWEEN FRAMES 41 AND 44 UPPER CHORD CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPL ACED CHORD IN ACCORDANCE WITH SRM. 2 H 7 2 4T RT A53EU 2008042300142 20080423 00142 EU 2008 4 23 1218361304218 1 20071205 A 5320 S53678008216002 FLOOR SUPPORT AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 RIGHT SIDE BETWEEN FRAMES 39 AND 41 ZEE FLOOR SUPPORT CORRODED. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLA CED ZEE FLOOR SUPPORT IN ACCORDANCE WITH SRM. 2 H 7 2 4T RT A53EU 2008042300149 20080423 00149 EU 2008 4 23 1218361404218 1 20071121 A 5315 NTA44770 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 FOUND FLOORBEAM FRAME 40 CORRODED. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM IN ACCORDANCE W ITH SRM. 2 H 7 2 4T RT A53EU 2008042300150 20080423 00150 EU 2008 4 23 1218361504218 1 20071121 A 5347 S5337500120402 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 CORROSION FOUND ON SEAT TRACK LEFT OUTBOARD SIDE BETWEEN FRAMES 13 AND 23. CORROSION REMOVED AND FOUND TO BE OUT OF LIM ITS. SEAT TRACK REPLACED PER SRM. 2 H 7 2 4T RT A53EU 2008042300151 20080423 00151 EU 2008 4 23 1218361604218 1 20071115 A 5315 2024T3 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 FLOORBEAM FRAME 39 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND REPAIRED FLOORBEAM FLANGE IN ACCORDANCE WITH SRM. 2 H 7 2 4T RT A53EU 2008042300152 20080423 00152 EU 2008 4 23 1218361704218 1 20071121 A 5230 S5337128320302 SEAL DEPRESSOR AEROSP ATR42 ATR42320 8680930 EU CARGO DOOR CRACKED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 CARGO DOOR LOWER AFT SEAL DEPRESSOR CRACKED. REMOVED AND REPLACED IN ACCORDANCE WITH SRM. 2 H 7 2 4T RT A53EU 2008042300154 20080423 00154 EU 2008 4 23 1218361904218 1 20071129 A 5240 S5367139028802 SEAL DEPRESSOR AEROSP ATR42 ATR42320 8680930 EU SERVICE DOOR CRACKED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 SERVICE DOOR AFT LOWER CORNER SEAL DEPRESSOR CRACKED. REPLACED SERVICE DOOR SEAL DEPRESSOR IN ACCORDANCE WITH SRM. 2 H 7 2 4T RT A53EU 2008042300158 20080423 00158 EU 2008 4 23 1218364020708 1 20071211 A 5753 S5751002000001 ARM AEROSP ATR42 ATR42320 8680930 EU TE FLAP CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 RIGHT INBOARD FLAP ARM CORRODED AT RIB 5. REMOVED CORROSION AND PERFORMED EDDY CURRENT INSPECTION, NO CRACKS FOUND. RE PAIRED FLAP ARM IN ACCORDANCE WITH ATR STRUCTURAL REPAIR INSTRUCTIONS. 2 H 7 2 4T RT A53EU 2008042300192 20080423 00192 EU 2008 4 23 1218367020708 1 20071127 A 5711 SPAR AEROSP ATR42 ATR42320 8680930 EU WING CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 RIGHT FRONT SPAR AT RIB 12 INBOARD, AND LEFT FRONT SPAR AT RIB 10, BOLTS FOUND CORRODED. REMOVED AND REPLACED BOLTS AT RIB 10 AND 12. 2 H 7 2 4T RT A53EU 2008042300194 20080423 00194 EU 2008 4 23 1218362021008 1 20071120 A 5240 S5247764300200 BOLT AEROSP ATR42 ATR42320 8680930 EU SERVICE DOOR CHIPPED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 SERVICE DOOR LOWER AFT SHOOT BOLT CHIPPED. SERVICE DOOR LOWER SHOOT BOLT REPLACED IN ACCORDANCE WITH AMM. 2 H 7 2 4T RT A53EU 2008042300198 20080423 00198 EU 2008 4 23 1218363021108 1 20071211 A 5753 S5751067000000 ARM AEROSP ATR42 ATR42320 8680930 EU TE FLAP CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 LEFT OUTBOARD FLAP ARM CORRODED AT RIB 18. CORROSION REMOVED FROM LEFT OUTBOARD FLAP ARM RIB 18 IAW SRM. PERFORMED EDD Y CURRENT, NO CRACKS FOUND. LEFT OUTBOARD FLAP ARM AT RIB 18 REPAIRED IN ACCORDANCE WITH ATR STRUCTURAL REPAIR INSTRUCT IONS. 2 H 7 2 4T RT A53EU 2008042300202 20080423 00202 EU 2008 4 23 1218363041408 1 20071205 A 5744 S5741000321000 HINGE AEROSP ATR42 ATR42320 8680930 EU LE FLAP BROKEN A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 LEADING EDGE 511 HINGE BROKEN. REMOVED AND REPLACED HINGE IAW SRM. 2 H 7 2 4T RT A53EU 2008042300203 20080423 00203 EU 2008 4 23 1218364041408 1 20071205 A 3350 3011151 BATTERY AEROSP ATR42 ATR42320 8680930 EU EMERGENCY LIGHT FAILED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 EMERGENCY LIGHT POWER SUPPLY BATTERY FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY. 2 H 7 2 4T RT A53EU 2008042300196 20080423 00196 EU 2008 4 23 1218361021108 1 20071211 A 5230 SUPPORT FITTING AEROSP ATR42 ATR42320 8680930 EU CARGO DOOR CRACKED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 CARGO DOOR PAN CRACKED AT STRUT SUPPORT FITTING LOCATION. CARGO DOOR PAN AT STRUT FITTING LOCATION REPAIRED IN ACCORDAN CE WITH SRM. 2 H 7 2 4T RT A53EU 2008042300197 20080423 00197 EU 2008 4 23 1218362021108 1 20071213 A 5210 S52176204210 PAN AEROSP ATR42 ATR42320 8680930 EU PAX DOOR CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 PASSENGER DOOR UPPER PAN CORRODED NEAR BONDING STRIP. PASSENGER DOOR UPPER PAN CORROSION REMOVED AND REPAIRED IN ACCORD ANCE WITH SRM. 2 H 7 2 4T RT A53EU 2008042300200 20080423 00200 EU 2008 4 23 1218361041408 1 20071207 A 5753 S57510219200 HINGE FITTING AEROSP ATR42 ATR42320 8680930 EU TE FLAP CORRODED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 LEFT OUTBOARD FLAP, HINGE ARE AT FLAP RIB 18 UPPER AFT LUG CORROSION. REPAIRED PER ATR STRUCTURAL REPAIR INSTRUCTIONS. 2 H 7 2 4T RT A53EU 2008042300209 20080423 00209 EU 2008 4 23 1218365041408 1 20071206 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU EMERGENCY LIGHTS NO TEST A HYIA K NONE L NO TEST IN INSP/MAINT 1 EA 61 42836 200 EMERGENCY LIGHT POWER SUPPLY BATTERY FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY. 2 H 7 2 4T RT A53EU 2008042300238 20080423 00238 EU 2008 4 23 1218369041408 1 20071205 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU EMERGENCY LIGHTS NO TEST A HYIA K NONE L NO TEST IN INSP/MAINT 1 EA 61 42836 200 EMERGENCY LIGHT POWER SUPPLY BATTERY FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY. 2 H 7 2 4T RT A53EU 2008042300252 20080423 00252 EU 2008 4 23 1218363042008 1 20071120 A 5210 S5367126822002 INTERCOSTAL AEROSP ATR42 ATR42320 8680930 EU PAX DOOR CRACKED A HYIA K NONE O OTHER IN INSP/MAINT 1 EA 61 42836 200 PASSENGER DOOR SPRING ATTACH POINT LOWER INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL. 2 H 7 2 4T RT A53EU 2008042300254 20080423 00254 EU 2008 4 23 1218364042008 1 20071201 A 5220 S522770100000 DOOR AEROSP ATR42 ATR42320 8680930 EU L EMER EXIT OUT OF TOLERANCE A HYIA K NONE L NO TEST IN INSP/MAINT 1 EA 61 42836 200 LEFT EMERGENCY EXIT DOOR LATCH HANDLE FOUND HARD TO OPEN AND OPENING WEIGHT OUT OF LIMITS. LUBRICATED AND FUNCTIONALLY TESTED AND FOUND TO BE IN SERVICEABLE CONDITION. 2 H 7 2 4T RT A53EU 2008042500254 20080425 00254 NM 2008 4 25 2008UALA00022 1 20071231 A 2697 WIRE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE SMOKE DETECTOR DISCONNECTED A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 936UA 26667 AFT RIGHT LAV SMOKE DETECTOR POWER LIGHT NOT ON. SUPPLEMENT, SUSPECT IMPROPER PIN CONNECTION. RECONNECTED WIRE W2132-0 53 -22 INTO D3736 PIN 5 SMOKE DETECTOR LIGHT CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042800089 20080428 00089 NM 2008 4 28 2007UALA03898 1 20070925 A 3510 60B5008791 BOTTLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CREW 02 LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 306UA 23667 O2 SYSTEM LOSING 100 PSI PER HOUR. SUPPLEMENTAL, FOUND LEAK AT FITTING CREW 02 BOTTLE REF MM 12-15-21, ALSO HOSE RECEPT ACLE AT 1ST OBS SEAT TO BE FAULTY AND LEAKING. REPLACED 02 BOTTLE ALSO RECEPTACLE AT 1ST OBS. LEAK CHECKED GOOD WITH N O PRESSURE DROP IN 3 HOURS. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042800202 20080428 00202 2008 4 28 2007UALA03897 4 20070925 A 2565 D31591478U1 SLIDE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE DOOR 1L FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 306UA 23667 DOOR SLIDE AT 1L FABRIC TOUCHES FLOOR WHEN ARMED. GENERAL WEAR AND TEAR. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042800261 20080428 00261 EA 2008 4 28 SWIA200719539 1 20070502 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 709BR 7850 FLT 2872 - FIRST OFFICERS WINDSHIELD IS SHATTERED. REPLACED FIRST OFFICERS WINDSHIELD IAW CRJ MM 56-11-01, P/N NP-13432 1-14, S/N OFF 03140R4596. 2 L 7 2 4F RT A21EA 2008042800370 20080428 00370 NM 2008 4 28 RYNA200700013 1 20071119 A 5330 SKIN BOEING 757 75728A 1384976 NM FUSELAGE DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753NA 24544 FUSELAGE SKIN HAS A DENT AT BS 1691-1693 & BETWEEN STR 12L - 13L. REPAIRED DENT IAW EO COO-5-53-487-07. 2 L 7 2 4F RT A2NM 2008042800374 20080428 00374 NM 2008 4 28 RYNA200700007 1 20071118 A 5315 FLOORBEAM BOEING 757 757200 1384950 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753 24544 PASSENGER CABIN FLOORBEAM IS CORRODED AT BS 1661 & BETWEEN LBL 55 THRU RBL 58. REPAIRED PER EO C00-5-53-494-07. 2 L 7 2 4F RT A2NM 2008042800375 20080428 00375 NM 2008 4 28 RYNA200700008 1 20071120 A 5315 FLOORBEAM BOEING 757 757200 1384950 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753 24544 PASSENGER CABIN FLOORBEAM IS CORRODED AT BS 355.25 & BETWEEN BL 0 THRU RBL 60. REPAIRED PER EO C00-5-53-497-07. 2 L 7 2 4F RT A2NM 2008042800377 20080428 00377 NM 2008 4 28 RYNA200700005 1 20071122 A 5315 FLOORBEAM BOEING 757 757200 1384950 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753 24544 PASSENGER CABIN FLOORBEAM IS CORRODED AT BS 740 BETWEEN LBL 63 AND LBL 45. REPAIRED CORROSION PER EO C00-5-53-498-07. 2 L 7 2 4F RT A2NM 2008042800378 20080428 00378 NM 2008 4 28 RYNA200700011 1 20071118 A 5315 FLOORBEAM BOEING 757 75728A 1384976 NM FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753NA 24544 PASSENGER CABIN FLOORBEAM IS CORRODED AT BS 1661 & BETWEEN LBL 45 - RBL 58 & WL 208. REPAIRED IAW EO C00-5-53-494-07. 2 L 7 2 4F RT A2NM 2008042800380 20080428 00380 NM 2008 4 28 RYNA200700012 1 20071113 A 5330 SKIN BOEING 757 75728A 1384976 NM FUSELAGE DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753NA 24544 FUSELAGE SKIN HAS A DENT AT BS 620 - 634 & BETWEEN STR 15L - 18L. REPAIRED DENT IAW EO C00-5-53-489-07. 2 L 7 2 4F RT A2NM 2008042800379 20080428 00379 NM 2008 4 28 RYNA200700010 1 20071113 A 5330 SKIN BOEING 757 75728A 1384976 NM FUSELAGE DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753NA 24544 FUSELAGE SKIN HAS A DENT AT BS 620 - 634 & BETWEEN STR 15L - 16L. REPAIRED IAW EO C00-5-53-489-07. 2 L 7 2 4F RT A2NM 2008042800373 20080428 00373 NM 2008 4 28 RYNA200700006 1 20071119 A 5330 SKIN BOEING 757 757200 1384950 NM FUSELAGE DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753NA 24544 UPPER FUSELAGE SKIN HAS "BLEND OUT" AT BS 444.5 & STR 4LT. REPAIRED FUSELAGE SKIN AT BS 444.5 & STR 4LT PER SRM 53-00-0 1 FIGURE 201 SECTION I & II. 2 L 7 2 4F RT A2NM 2008042800376 20080428 00376 NM 2008 4 28 RYNA200700004 1 20071113 A 5330 SKIN BOEING 757 757200 1384950 NM FUSELAGE DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753 24544 EXTERNAL SKIN AT BS 1417 BETWEEN STR 26R AND 27R HAS A DENT OUT OF SRM 53-00-01 LIMIT. REPAIRED DENT PER EO C00-5-53-49 5-07. 2 L 7 2 4F RT A2NM 2008043000023 20080430 00023 NM 2008 4 30 RYNA200700009 1 20071119 A 5330 SKIN BOEING 757 75728A 1384976 NM FUSELAGE DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753NA 24544 FUSELAGE SKIN HAS A OUT OF LIMIT DENT AT BS 596 - 603 & BETWEEN STR 27LT AND 27RT. REPAIRED IAW EO C00-5-53-492-07. 2 L 7 2 4F RT A2NM 2008050200003 20080502 00003 EU 2008 5 2 WRNA200700065 1 20071011 A 5312 BULKHEAD AIRBUS 300 A300B4203 3930306 EU FUSELAGE CRACKED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 510TA 100 DURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD AT STR TIE END ANGLE FITTING AT 35R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40. APPLIED PROTECTIVE CO ATINGS IAW SRM 51-40-12. INSTALLED FITTING IAW SRM 51-30-30. 2 L 7 2 4F RT A35EU 2008050200047 20080502 00047 WP 2008 5 2 WRLA2008046 1 20071123 A 5322 SHEAR TIE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE BS 2123 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 137WA 48282 DURING C CHECK INSPECTION, FOUND UPPER TORQUE BOX AFT BULKHEAD STA 2123 RBL 8, SHEAR TIE CRACKED. REPAIRED PER SRM 53-3 0-00, REF SAA JOB NR 78326260001. 2 L 7 3 4F 4 F A22WE E23EA 2008050100107 20080501 00107 NM 2008 5 1 RYNA200700014 1 20071113 A 5330 SKIN BOEING 757 75728A 1384976 NM BS 541-543 DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753NA 24544 FOUND FUSELAGE SKIN HAS A OUT OF LIMIT DENT AT BS 541-543 AND BETWEEN STG 20R AND 23R. REPAIRED IAW EO C00-5-53-486-07. 2 L 7 2 4F RT A2NM 2008050100108 20080501 00108 NM 2008 5 1 RYNA200700015 1 20071122 A 5330 SKIN BOEING 757 75728A 1384976 NM BS 405 DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753NA 24544 FUSELAGE SKIN HAS AN OUT OF LIMIT DENT AT BS 405 AND BETWEEN STG 24R AND 25R. REPAIRED IAW EO C00-5-53-483-07. 2 L 7 2 4F RT A2NM 2008050100109 20080501 00109 NM 2008 5 1 RYNA200700017 1 20071113 A 5330 SKIN BOEING 757 75728A 1384976 NM BS 1420 DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753NA 24544 FUSELAGE SKIN HAS AN OUT OF LIMIT DENT AT BS 1420 AND BETWEEN STG 26R AND 27R. REPAIRED IAW EO C00-5-53-495-07. 2 L 7 2 4F RT A2NM 2008050100110 20080501 00110 NM 2008 5 1 RYNA200700016 1 20071113 A 5330 SKIN BOEING 757 75728A 1384976 NM BS 1356 DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753NA 24544 FUSELAGE SKIN HAS A OUT OF LIMIT DENT AT BS 1356 AND BETWEEN STG 25R AND 37R. REPAIRED IAW EO C00-5-53-493-07. 2 L 7 2 4F RT A2NM 2008050100111 20080501 00111 NM 2008 5 1 RYNA200700018 1 20071119 A 5330 SKIN BOEING 757 75728A 1384976 NM BS 431 DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753NA 24544 FUSELAGE SKIN HAS A OUT OF LIMIT DENT AT BS 431 AND STG 4L. REPAIRED IAW EO C00-5-53-490-07. 2 L 7 2 4F RT A2NM 2008050100113 20080501 00113 NM 2008 5 1 RYNA200700020 1 20071121 A 5315 FLOORBEAM BOEING 757 75728A 1384976 NM BS 1640 CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753NA 24544 PASSENGER CABIN FLOORBEAM IS CORRODED AT BS 1640 BETWEEN LBL 48 AND LBL 58. REPAIRED IAW EO C00-5-53-507-07. 2 L 7 2 4F RT A2NM 2008050100114 20080501 00114 NM 2008 5 1 RYNA200700021 1 20071119 A 5315 FLOORBEAM BOEING 757 75728A 1384976 NM BS 1640 CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753NA 24544 PASSENGER CABIN FLOORBEAM IS CORRODED AT BS 1640 BETWEEN RBL 38 AND RBL 60, WATER LINE 208. REPAIRED IAW EO C00-5-53-50 2-07. 2 L 7 2 4F RT A2NM 2008050100115 20080501 00115 NM 2008 5 1 RYNA200700019 1 20071121 A 5330 SKIN BOEING 757 75728A 1384976 NM BS 1800 WORN A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753NA 24544 UPPER FUSELAGE SKIN TAIL CONE AREA HAS EVIDENCE OF WEAR AT BS 1800 BETWEEN STR 15L AND 16L. REPAIRED IAW EO C00-5-53-49 9-07. 2 L 7 2 4F RT A2NM 2008050200046 20080502 00046 WP 2008 5 2 WRLA2008048 1 20071127 A 5322 SHEAR TIE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE BS 2123 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 137WA 48282 DURING C CHECK INSPECTION, FOUND BULKHEAD SHEAR TIE CRACKED STA 2123 LBL 8. REPAIRED PER SRM 53-30-00 FIG 2B, REF SAA J OB NR 78326250001. 2 L 7 3 4F 4 F A22WE E23EA 2008050200048 20080502 00048 WP 2008 5 2 WRLA2008047 1 20071127 A 5330 ACA31092 SKIN DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE BS 593 L45R CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 137WA 48282 DURING C CHECK INSPECTION, FOUND FUSELAGE EXTERIOR SKIN PUNCTURED, CRACKED, CREASED AT RT NOSE JACKPAD POINT STA 593 L45 R. REPAIRED PER SAA EA NR 010-5320-11-A1239. 2 L 7 3 4F 4 F A22WE E23EA 2008050700214 20080507 00214 NM 2008 5 7 RYNA200700026 1 20071203 A 5330 SKIN BOEING 757 75728A 1384976 NM BS 510 S26-27R DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753NA 24544 LOWER FUSELAGE HAS EVIDENCE OF LIGHTNING STRIKE AT BS 510 AND BETWEEN STR 26R - 27R. REPAIRED FUSELAGE SKIN IAW B757-20 0 SRM 5I-00-01. 2 L 7 2 4F RT A2NM 2008050700216 20080507 00216 NM 2008 5 7 RYNA200700024 1 20071117 A 5330 SKIN BOEING 757 75728A 1384976 NM BS 1348 S25-26L DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753NA 24544 LOWER FUSELAGE HAS EVIDENCE OF LIGHTNING STRIKE AT BS 1348 AND BETWEEN STR 25L - 26L. REPAIRED FUSELAGE SKIN IAW B757-2 00 SRM 5I-00-01, REPAIR 4. 2 L 7 2 4F RT A2NM 2008050700217 20080507 00217 NM 2008 5 7 RYNA200700025 1 20070117 A 5330 SKIN BOEING 757 75728A 1384976 NM BS 1483 S21-22R DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753NA 24544 LOWER FUSELAGE HAS EVIDENCE OF LIGHTNING STRIKE AT BS 1483 AND BETWEEN STR 21R - 22R. REPAIRED FUSELAGE SKIN IAW B757-2 00 SRM 5I-00-01, REPAIR 6. 2 L 7 2 4F RT A2NM 2008050700218 20080507 00218 NM 2008 5 7 RYNA200700023 1 20071123 A 5320 146N52571 FLOOR SUPPORT BOEING 757 75728A 1384976 NM BS 164-1661 CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753NA 24544 PASSENGER CABIN FLOOR SUPPORT CORRODED AT BS 1640-1661 AND RBL 13, WATER LINE 208. REPLACED CABIN FLOOR SUPPORT BOTH IN TERCOSTALS WHICH ARE FABRICATED FROM BOC1508-240-707ST73511 EXTRUSION PER QQA-200-111. 2 L 7 2 4F RT A2NM 2008050700219 20080507 00219 NM 2008 5 7 RYNA200700022 1 20071123 A 5320 141N51911 FLOOR SUPPORT BOEING 757 75728A 1384976 NM BS 324-344 CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 753NA 24544 PASSENGER CABIN FLOOR SUPPORT CORRODED AT BS 324-377 AND BETWEEN BL 0 AND RBL 3, WATER LINE 208. REPLACED CABIN FLOOR S UPPORT. 2 L 7 2 4F RT A2NM 20080725 2008 7 25 MWE2008F00008 4 20071210 A 2565 100503117 SLIDE DOUG DC9 DC981 3022081 WP TAILCONE INOPERATIVE A MWEA O OTHER O OTHER NR NOT REPORTED 1 GL 13 804ME 48030 TAILCONE SLIDE PRESSURE AT (0). REMOVED AND REPLACED TAILCONE SLIDE. (K) 2 L 7 2 4F A6WE 20080805 EU 2008 8 5 M7K2008F00055 1 20071010 A 7400 975UNO1B4AA5P SWITCH UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ENGINE START FAILED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 805MH 3799 AT END OF FLIGHT, PILOT SELECTED IDLE POSITION AND ENGINE REMAINED IN THE FLIGHT POSITION AND WAS SHUTDOWN FROM FLIGHT P OSITION. A FAULT CODE WAS GENERATED THA THE START STOP SWITCH WAS DEFECTIVE IN SOME MANNER. A NEW ENGINE START STOP/ON OFF SWITCH WAS INSTALLED AND THE PROBLEM WAS CORRECTED. RECORDS INDICATED ATH 11 SWITCHES OF THIS TYPE HAVE BEEN REPLA CED IN OUR FLEET WHICH HAS FLOWN NEARLY 50,000 HOURS TO DATE. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080805 EU 2008 8 5 M7K2008F00059 1 20071030 A 2150 5300273 TENSIONER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE AIR CONDITIONER CRACKED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 803MH 195 3735 DURING COMPRESSOR REPLACEMENT THE COMPRESSOR TENSIONING BRACKET WAS FOUND TO HAVE CRACKED ON ONE OF THE 2 ARMS AND SERVI CEABLE REPLACEMENT PART INSTALLED. CLOSE EXAMINATION REVEALED THAT THE PARTS ARM SLOTS HAD BEEN WATER JETTED DURING MFG WHICH LEAVES A ROUGH SLOT SURFACE THAT SEEMS TO BE THE SOURCE OF THE STRESS RISER WHERE THE CRACK DEVELOPED. SUGGEST T HAT THE MFG DRESSES AND POLISHES THE WATER JETTED SLOTS TO PREVENT CRACK DEVELOPMENT AND INCREASE MATERIAL THICKNESS TO IMPROVE PART SERVICEABILITY. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080805 EU 2008 8 5 M7K2008F00076 1 20071010 A 3150 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE WARNING LIGHT DEFECTIVE E M7KA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 19 804MH 3750 23058 PILOT REPORTS AMBER GOVERNOR LIGHT ILLUMINATED DURING FLIGHT. A FAULT CODE WAS GENERATED INDICATING THE POTENTIOMETER A S THE LIKELY DEFECTIVE UNIT. A NEW PART WAS INSTALLED AND NO FURTHER DEFECTS WERE NOTED. THIS IS A RECURRING PROBLEM FO R THIS PART THAT HAS EFFECTED THE DISPATCH RELIABILITY FOR THIS AC MODEL. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080804 EU 2008 8 4 M7K2008F00058 1 20071030 A 7921 95544576 FAN UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE OIL COOLER FAILED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 814MH 1991 4020 23100 FAN ASSY HAD 3 BLADES MISSING CORNERS WITH 1 BLADE MISSING 40 PERCENT OF ITS DIMENSIONS. NEW FAN ASSY INSTALLED. INITIAL BLADE FAILURE SEEMED TO BE A MATERIAL FAILURE NOT CAUSED BY AN IMPACT. THIS TYPE DEFECT IS PRETTY RARE. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080805 EU 2008 8 5 M7K2008F00060 1 20071010 A 7603 116F2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE DECU DEFECTIVE E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 813MH 217 3967 23183 A FAULT CODE WAS GENERATED AT ENGINE SHUTDOWN INDICATING A DEFECT WITH THE COLLECTIVE POTENTIOMETER. A NEW POTENTIOMETE R WAS INSTALLED. THIS HAS BECOME A VERY COMMON PROBLEM WITH THE LATEST REPLACEMENT PARTS THAT THEY LAST MUCH LESS THAN THE 2000 HOUR SERVICE LIFE LIMIT. THE SAME POTENTIOMETERS ORIGINALLY INSTALLED LASTED AS LONG AS 4000 HOURS WITHOUT FAI LING. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080808 WP 2008 8 8 07FDEA05046 1 20071213 A 5100 NONE DOUG MD10 MD1010F 3022112 WP NONE NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 369FE 46607 MAIN CABIN L4 PASSENGER DOOR UPPER INTERNAL JAMB EXISTING DOUBLER. ACCOMPLISHED EA NR 8-5310-115295A. 2 L 7 3 4F RT A22WE 20080808 EU 2008 8 8 M7K2008F00126 1 20071105 A 5210 677110100 HANDLE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE MAIN DOOR BROKEN E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 807MH 2925 3912 23130 UPON LANDING PILOT FOUND HANDLE TO BE LIMP AND FLOPPING IN THE SLIPSTREAM. DOOR HAD TO BE OPENED UTILIZING THE INSIDE H ANDLE. BELLCRANK LEVER WHICH CONNECTED OUTSIDE HANDLE TO THE DOOR LATCHING MECHANISM HAD BROKEN. A NEW DOOR HANDLE ASS Y WAS INSTALLED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080808 EU 2008 8 8 M7K2008F00109 1 20071105 A 6700 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE COLLECTIVE DEFECTIVE E M7KA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 19 815MH 930 4022 23167 AC HAD SOME SUDDEN YAWING WHEN PASSING THROUGH A SPECIFIC COLLECTIVE POWER SETTING THAT WAS REPEATABLE AND INDICATED A S UDDEN CHANGE OF ENGINE TORQUE SUCH AS ONE MAY EXPERIENCE WITH COMPRESSOR STALLS. NO FAULT CODES WERE GENERATED AD THE E NGINE HAD NO OBSERVABLE DEFECT WHEN EXAMINED. APPARENT THAT A DEAD SPOT HAD DEVELOPED IN THE POTENTIOMETER SIGNAL CONTR OLLING ENGINE ANTICIPATION. NEW POTENTIOMETER WAS INSTALLED WITH NO FURTHER DEFECT. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080808 EU 2008 8 8 M7K2008F00128 1 20071105 A 8000 975UN01B4AA5P SWITCH UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE STARTER FAILED E M7KA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 19 802MH 3521 3707 23128 AMBER GOVERNOR LIGHT ILLUMINATED IN FLIGHT. NO FAULT CODE WAS GENERATED THAT POINTED TO THE SWITCH AS THE PROBLEM AS WO ULD NORMALLY OCCUR WITH THIS TYPE OF FAILURE. NO FURTHER PROBLEMS DEVELOPED FOLLOWING THE INSTALLATION OF A NEW SWITCH. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00116 1 20070919 A 5344 350A58101020 HINGE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE FUSELAGE CRACKED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 801MH 198 3654 23077 CRACK’S DEVELOP IN HINGE 1ST SEGMENT OF LEADING EDGE DURING NORMAL OPERATIONS, REQUIRING REPAIR OR REPLACEMENT EVERY 100 HOURS. TYPICALLY AT MINIMUM A STOP DRILL IS REQUIRED. HINGE MATERIAL IS THIN ALUMINUM AND PERHAPS A CHANGE TO THICKER GAUGE OR ALTERNATE MATERIAL SUCH AS SS IS REQUIRED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 NE 2008 8 11 M7K2008F00129 2 20071030 A 7261 800301 MAGNETIC SEAL UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ENGINE LEAKING E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 814MH 456 4020 23100 SEAL LEAKAGE WAS NOTED TO BE INCREASING OVER TIME AND SEAL WAS CHANGED WHEN OIL BEGAN ACCUMULATING ON THE ENGINE DECK FO LLOWING A DAYS WORTH OF FLIGHTS. THIS SEAL WAS A HISTORY OF LEAK DEVELOPMENT AND USUALLY WILL BE CHANGED SEVERAL TIMES BEFORE ENGINE REACHES ITS NORMAL OVERHAUL INTERVAL. IN SOME CASES THE SEAL NEVER LEAKS. EXAMINATION OF THE SEAL CARBON FACE AND RUNNER RARELY EXHIBITS ANY NOTICEABLE DEFECT. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00080 1 20070919 A 6322 9696 BLOWER MOTOR UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE OIL COOLER SEIZED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 817MH 4125 23292 PILOT REPORTED BLOWER VERY NOISY/GROWLS IN OPERATION. CLOSER EXAMINATION REVEALED VERY ROUGH SHAFT BEARING. A NEW REPL ACEMENT MOTOR WAS INSTALLED. THIS BLOWER MOTOR IS USUALLY VERY RELIABLE IF A BIT NOISY IN NORMAL OPERATION. LIKELY CAU SE IS POOR QUALITY OR INSUFFICIENT GREASING OF THE BEARINGS BY MFG. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00142 1 20071010 A 6220 704A3364088 FREQ ADAPTER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE M/R HUB CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 803MH 19316 M2381 3735 DURING ROUTINE INSP AT THE 30 HOUR INTERVAL, A CRACK IN THE BLUE BLADE FREQ ADAPTER T/E SIDE WAS FOUND TO EXCEED THE MM LIMITATION OF 10 MM FOR CRACKS IN THE ELASTOMER. IAW MFG REQUIREMENTS ALL 3 ADAPTERS RENEWED. THIS IS A VERY COMMON FA ILURE FOR A PART THAT HAS 3000 HOURS SERVICE LIFE LIMIT, SUGGEST REFORMULATION OF ELASTOMER. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00135 1 20070919 A 6410 350A33300232 BLADE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAIL ROTOR FAILED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 814MH 1894 4020 23100 IB SURFACE ADJACENT TO PITCH HORN WORN BEYOND LIMITS DUE TO "TT" STRAP FAILURE, OB LAMINATE OF 20/21 PLATES BREAKS. THIS PROBLEM OCCURS WHEN STRAPS BREAK INTO 2 PIECES AND BROKEN ENDS VIBRATES LIKE A REED, BEYOND THE HEAT SHRINK. SUGGEST M FG THICKENS OB PLATES OR ALTERS DESIGN OR USES LONGER HEAT SHRINK COVER THAN NORMAL. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00086 1 20071010 A 6220 704A33640088 FREQ ADAPTER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE M/R HEAD CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 812MH M2686 3956 23179 DURING SCHEDULED MAINT ONE ADAPTER OF SET OF 3 FOUND TO HAVE INTERNAL/EXTERNAL ELASTOMER CRACK EXCEEDING MM LIMITATIONS OF 10MM. THIS IS A VERY COMMON FAILURE THAT OCCURS AT HALF OR LESS OF THIS PARTS SERVICE LIFE LIMIT OF 3000 HOURS. THE OLDER PN ADAPTERS USED A DIFFERENT ELASTOMER FORMULATION THAT ALMOST ALWAYS LASTED 3000+ HOURS. SUGGEST THIS FORMULATI ON AGAIN BE USED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00087 1 20071010 A 6200 WIRE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TACH SENSOR DAMAGED E M7KA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 19 809MH 1150 4766 3927 23147 PILOT REPORTED NO LOW ROTOR RPM WARNING HORN (HEADSET BEEP) NR GAUGE INDICATIONS WAS NORMAL. SENSOR IS DUAL ELEMENT WIT H ONE PORTION PROVIDING EACH SIGNAL FOR WARNING HORN AND NR INDICATION. INTERNAL WIRES ARE SO FINE THIS UNIT IS FAILURE PRONE, SUGGEST OPTIC SENSOR DESIGN. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00085 1 20071010 A 6220 704A33640088 FREQ ADAPTER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE M/R HEAD FAILED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 816MH 1392 M2765 4038 23096 DURING A PREFLIGHT INSPECTION PILOT, DISCOVERED ONE FREQUENCY ADAPTER WITH A 20MM CRACK IN THE ELASTOMER. MM LIMITATION IS 10MM. THIS IS A COMMON FAILURE WHICH OCCURS AT HALF LIFE OR LESS FOR THIS PART WITH A 3000 HOUR SERVICE LIFE LIMIT. THE OLDER PN ELASTOMER FOR MOLD RARELY FAILED. SUGGEST RETURNING TO THE OLDER FORMULATION. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00136 1 20070919 A 6297 WIRE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TACH SENSOR BROKEN E M7KA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 19 810MH 2837 3943 3949 23209 NR (ROTOR RPM) MAGNETIC SENSING PICKUP LOOP BROKEN CAUSING INTERMITTENT NR INDICATION FLUCTUATIONS DURING FLIGHT. PROBA BLE CAUSE IS THAT WIRE AND FRAGILE COIL WIRE IS HAIR THIN. SUGGEST A STRONGER WIRE HARNESS BE USED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00089 1 20071010 A 2150 5300273 TENSIONER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE A/C COMPRESSOR CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 803MH 5195 3735 23036 DURING ROUTINE COMPRESSOR REMOVAL TO FACILITATE OTHER MAINTENANCE THE CRACKED TENSIONING ARM WAS DISCOVERED AND A NEW RE PLACEMENT PART INSTALLED. SUSPECT METAL FATIGUE BUT THE SECOND TENSIONING ARM MAINTAINED UNIT FUNCTIONALITY HAD NO APPA RENT DEFECT DEVELOPING. SUGGEST INSPECTING SLOTS OF THE TENSIONING ARMS IN DETAIL, WHENEVER REMOVING THE BELT TENSIONER, FOR CRACK DEVELOPMENT BEFORE ARM BREAKS. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00096 1 20070917 A 3300 704A46831016 LIGHT UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE UNKNOWN E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 804MH 4425 3750 23058 THIS LIGHT ASSY HAS BEEN FAIRLY RELIABLE BUT IS A LITTLE DIFFICULT TO WORK ON REQUIRING PIN EXTRACTION TOOLING TO TROUBL ESHOOT OR REPLACE. THE TYPICAL FAILURE IS INSIDE THE SEALED UNIT. THE QUALITY OF CONSTRUCTION IS EXCELLENT. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00088 1 20070919 A 6320 703A53000001 OIL TANK UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE RT M/R G/B LEAKING E M7KA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 19 813MH 2069 3967 23183 OIL LEAK FOUND ON DECK DURING POST FLIGHT INSP. CRACK FOUND AT OIL TANK FILLER NECK EXTERNAL WELD. THIS SIS A COMMON P ROBLEM THAT OCCURS TO THIS COMPONENT AND IS AGGRAVATED BY CAP BEING INSTALLED TOO AGGRESSIVELY DURING OIL SERVICING. SU GGEST MFG IMPROVE EXTERNAL WELD OR INCREASE METAL THICKNESS. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00123 1 20070917 A 3340 6485000 POWER SUPPLY UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE EXTERIOR LIGHT INOPERATIVE E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 815MH 1126 1186 4022 23167 THIS ANTI-COLLISION LIGHT AND POWER SUPPLY ASSY HAS PROVEN TO BE OF LOW QUALITY AS MOST FAIL WITHIN THEIR FIRST 1000 HOU RS OF SERVICE AND ARE NOT REPAIRABLE IAW MFG. AS THIS UNIT IS VERY EXPENSIVE TO REPLACE WE RECOMMEND THAT THE WHEN LED FLASHING ANTI COLLISION LAMP ASSY BE INSTALLED IN ITS PLACE UNDER A FIELD APPROVAL. THIS LIGHT IS VERY BRIGHT WITH A LO NG DURATION FLASH IS LESS THAN .333 THE PRICE AND IS REPAIRABLE BY THE MFG. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 NE 2008 8 11 M7K2008F00119 2 20070917 A 7320 9560170620 SEAL UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE HMU LEAKING E M7KA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 19 822MH 441 ANR776B 4142 23318 SEAL FOUND LEAKING FUEL OVERBOARD WITH FUEL BOOST PUMP PRESSURE APPLIED. FOLLOWING STARTUP AND SHUTDOWN OF THE FUEL BOO ST PUMP FUEL LEAK SLOWED BUT CONTINUED AND WAS BEYOND ALLOWABLE LIMITS OF THE MM. THIS IS A VERY COMMON PROBLEM WITH AL MOST ALL CONTROLS REQUIRING SEAL REPLACEMENT TYPICALLY AROUND 500 HOURS IN SERVICE AND OFTEN EARLIER. THIS IS AGGRAVATE D BY THE FAILURE OF PILOTS TO USE THEIR CHECKLIST AND ENSURE THAT THE FUEL BOOST PUMP IS ON AND SUPPLYING LUBRICATION TO THE SEAL WHENEVER THE ENGINE IS ROTATING. IN 50,000 HOURS OF FLIGHT OPS, WE HAVE AVERAGED A SEAL EVERY 1,000 HOURS. C URRENTLY HAVE BEEN OPERATING WITH THE LATEST SEAL VERSION, TU133A, THAT TO DATE WITH 4500 HOURS SERVICE IN 8 CONTROLS, H 1 G 7 2 3U 3 U H9EU E00054EN 20080808 EU 2008 8 8 M7K2008F00115 1 20070919 A 6700 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE COLLECTIVE INTERMITTENT E M7KA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 19 804MH 43 3750 23183 THIS PART IS THE POSITION INDICATOR FOR BOTH COLLECTIVE AND TAIL ROTOR FADEC CONTROL ACTIONS. IT ALMOST NEVER FAILS TOT ALLY BUT GENERATES A FAILURE CODE THAT REQUIRES THEY BE REPLACED. THESE PARTS CAN LAST THOUSANDS OF HOURS OR LESS THAN FIFTY. ONLY RECENTLY DID THE AIRCRAFT MFG MAKE THIS A TIME CHANGE ITEM AND UP TO THAT POINT THEY VERY RARELY HAD A PROB LEM. DUE TO THE WEEKLY FAILURE OF ONE OF THESE POTENTIOMETERS IN OUR FLEET WHICH WE NEVER EXPERIENCED BEFORE REPLACING THE ORIGINAL PARTS ON OUR OLDER AC AND THE FACT THAT AC DELIVERED ABOUT THE SAME TIME AS THE NEW REPLACEMENT PARTS WERE BEING INSTALLED IN OUR FLEET BEGAN HAVING RELIABILITY PROBLEMS WE ARE SURE THAT A QC ISSUE EXISTS. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080808 EU 2008 8 8 M7K2008F00122 1 20070917 A 3340 6485000 POWER SUPPLY UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE EXTERINAL LIGHT INOPERATIVE E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 813MH 1995 1053 3967 23183 THIS ANTICOLLISION LIGHT AND POWER SUPPLY ASSY HAS PROVEN TO BE OF LOW QUALITY AS MOST FAIL WITHIN THEIR FIRST 1000 HOUR S OF SERVICE AND ARE NOT REPAIRABLE IAW MFG. AS THIS UNIT IS VERY EXPENSIVE TO REPLACE WE RECOMMEND THAT THE WHEN LED F LASHING ANTI COLLISION LAMP ASSY BE INSTALLED IN ITS PLACE UNDER A FIELD APPROVAL. THIS LIGHT IS VERY BRIGHT WITH A LON G DURATION FLASH IS LESS THAN .333 THE PRICE AND IS REPAIRABLE BY THE MFG. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00125 1 20071030 A 5200 C521C2017202 SUPPORT UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE DOOR LOOSE E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 812MH 2767 3956 23179 DURING ROUTINE INSPECTION IT WAS NOTED THAT THE TOP OF THE FLAP DOOR WAS EXCESSIVELY LOOSE. CLOSER INSPECTION REVEALED THAT THE DOOR’S ATTACHMENT HARDWARE HAD LOOSENED ALLOWING THE FITTING TO WEAR AROUND THE SCREW AND ULTIMATELY BREAK THRO UGH THE METAL FLANGE EDGE. A SERVICEABLE PART WAS INSTALLED. RECOMMEND THAT ALL HARDWARE BE CHECKED FOR PROPER TORQUE ON ALL THE DOOR FITTING AS JUST A VISUAL CHECK MAY NOT REVEAL THIS PROBLEM DEVELOPING BEFORE PARTS ARE DAMAGED. PART WA S MADE OF ALUMINUM AND SUGGEST THAT IT BE MADE WITH SS TO BE MORE DURABLE. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00139 1 20071105 A 5302 350A23422220 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAILBOOM CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 818MH 905 4131 23322 DURING ROUTINE PERIODIC INSPECTION THE UPPER RT FITTING WAS FOUND WITH 25 INCH CRACK ON ITS BOTTOM ATTACHMENT FLANGE AND THROUGH ONE OF THE 4 REINFORCEMENT RIBS. A NEW FITTING WAS MATCH DRILLED AND INSTALLED. THIS IS A FAIRLY COMMON DEFEC T THAT OFTEN REPEATS ITSELF ON AN AIRCRAFT BUT HAS BEEN KNOWN NOT TO CRACK ON SOME AC FOR REASONS UNKNOWN. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00137 1 20071010 A 7700 49202 CHIP DETECTOR UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ENGINE BROKEN E M7KA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 19 806MH 995 3833 23220 FOLLOWING ENGINE INSTALLATION A GROUND RUN WAS ABORTED WHEN AN ENGINE CHIP LIGHT ILLUMINATED IN A DIM FLICKERING MANNER ON THE CWP. INVESTIGATION REVEALED THE DETECTOR END HAD BROKEN LOOSE BUT REMAINED ATTACHED BY ITS INTERNAL WIRING. CLO SE EXAMINATION REVEALED THAT A PLASTIC CENTRAL POST HAD FAILED. PERHAPS THE DETECTOR WAS DAMAGED DURING REMOVAL AND INS TALLATIONS. SUGGEST A MORE ROBUST MATERIAL THAN PLASTIC BE USED TO MAKE PART HANDLED AS MUCH AS THESE ARE. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 NM 2008 8 11 HNA2008F00027 1 20071106 A 3350 51001072 SWITCH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE EMERGENCY LIGHTS FAILED A HNAA O OTHER O OTHER CR CRUISE 1 EA 07 810EX 308 THE FLOOR LEVEL EMERGENCY LIGHT FLICKERED IN FLIGHT. TRIED TO RESET FROM FLIGHT DECK. REMOVED AND REPLACED BOTH F/A AN D COCKPIT EMERGENCY LIGHT SWITCHES.. GROUND RAN AC, OPS CHECKED GOOD. (K) 2 H 7 2 4T 4 T RT A13NM E20NE 20080811 EU 2008 8 11 M7K2008F00143 1 20071030 A 5100 350A25040500 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE UNKNOWN CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 804MH 3750 23058 PART FOUND CRACKED DURING ROUTINE INSP IAW AD2004-01-14/SB53A004 REQUIREMENTS AT THE 110 HOURS INTERVAL INSPECTION. A N EW PART OF THE OLD PN WAS INSTALLED. SUGGEST MFG MAKE AVAILABLE THE NEW PN IMPROVED FITTING THAT DO NOT HAVE THE AD REQ UIREMENT TO ALL EC130B4 OPERATORS AS SOON AS POSSIBLE. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00144 1 20071105 A 5302 350A23422220 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAILBOOM CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 815MH 1003 4022 23167 FITTING FOUND CRACKED DURING POST FLIGHT INSP AND A NEW FITTING MATCH DRILLED AND INSTALLED. THIS IS A COMMON DEFECT FO R THIS PART AND OCCURS MULTIPLE TIMES ON SOME AIRCRAFT AND NEVER ON OTHER AIRCRAFT FOR REASONS UNKNOWN. SOME SHIMMING C AN BE REQUIRED AND MATCH DRILLING THE PART MUST BE DONE CAREFULLY. IF THE INSTALLATION IS NOT DONE CAREFULLY THIS MAY B E A FACTOR IN CRACK DEVELOPMENT AS WELL. (K) 1 G 7 2 3U 3 U H9EU E00054EN 2007092700069 20070927 00069 2007 9 27 UIEA200700341 4 20070830 A 3441 46300161300413 INU BOEING 747 747271C 1384869 NM E/E BAY MALFUNCTIONED A UIEA O OTHER F FLT CONT AFFECTED CL CLIMB 1 EA 15 537MC NR 2 INU BECAME COMPLETELY UNREADABLE AFTER ONE HOUR OF FLIGHT, IT HAD DEVIATED MORE THAN 10 MILES RIGHT OF TRACK. TWO HOURS INTO FLIGHT IT WAS MORE THAN 100 MILES OFF ACTUAL AIRCRAFT POSITION AS ESTABLISHED WITH VOR OVERHEAD. REMOVED AND REPLACED INU P/N 463001-6130-0413.OPS CHECKED GOOD, OK FOR CONTINUED SERVICE. 2 L 7 4 4F RT A20WE 20081017 NM 2008 10 17 2008UALA00025 1 20071230 A 2730 ELEVATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FAULTY A UALA O OTHER W F INADEQUATE Q C FLT CONT AFFECTED TO TAKEOFF 1 WP 29 518UA 24871 FIRST OFFICER'S ELEVATOR CONTROLS FEEL HEAVY. CREW COMMENTS: ELEVATOR VERY HEAVY ON TAKEOFF. RECURRED ON FLT 0053-12J AN. THIS A/C WAS A CHRONIC PROBLEM FOR SEVERAL WEEKS. AFTER MANY TESTS AND RIG CHECKS, SEVERAL TEST FLIGHTS BY DIFFERE NT CREWS IT WAS SUSPECTED THAT ELEV FEEL ACTUATOR WAS INTERMITTENTLY FAULTING. REPLACED AND A/C HAS BEEN CLEAN FOR TWO MONTHS. 2 L 7 2 4F 4 F RT A2NM E17NE 20081121 NM 2008 11 21 UALA2008111304879 1 20071129 A 2751 01812996 INDICATOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT FAULTY A UALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 29 328UA 24148 RTFL DUE TO STUCK FLAPS. SUPPLEMENTAL DATA UPDATE CAUSE: FOUND FAULTY RIGHT HAND FLAP POSITION TRANSMITTER.CORRECTIVE AC TION: REPLACED FLAP POSITION TRANSMITTER. SHOP FINDINGS: 'WAITING ON SHOP FINDINGS'. FOUND GRD FROM INDICATOR SHUTTING OFF FLAPS VIA BYPASS VALVE. REPLACED INDICATOR AGAIN WITH ROBBED UNIT 'KNOWN GOOD' FROM 9911. REPLACED R123 RELAY PER W DM 27-53-01. REPLACED FLAP BYPASS VALVE. REPLACED OVERHEAD FLT CNT MODULE. ALL OPS CHECKS GOOD, NOT ABLE TO DUPLICATE AGAIN. ACP'D CABLE SYSTEM RIG CHECK FOR FLAPS, FOUND LOW TENSION & FIXED-WORKED WITH WU 26492. RANG OUT & MEGGERED WI RES FROM INDICATOR D686 PINS 3, 4, 7, 9 TO TRANSMITTER CONNECTORS D275 077485 & D229 PINS 1&2 PER MM 27-52-01. ALL READ 2 L 7 2 4F 4 F RT A16WE E21EU 20081126 WP 2008 11 26 K11A2008112091503 1 20070220 A 5320 STIFFENER DOUG DC9 DC915F 3022037 WP BS 860 CRACKED A K11A O OTHER O OTHER NR NOT REPORTED 1 GL 23 915CK 47086 HORIZONTAL STIFFENER CRACKED AT END FASTENER ON UPPER SKIN SURFACE INSIDE ACCESS PANEL 8204 18 INCHES OTBD OF FUSELAGE A PPROX STA 860. 2 L 7 2 4F A6WE 20081126 WP 2008 11 26 K11A2008112091504 1 20070208 A 5241 ANGLE DOUG DC9 DC915F 3022037 WP GALLEY DOOR CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 915CK 47086 GALLEY SERVICE DOOR HAS CRACK ANGLE FWD OF HINGE TORQUE TUBE. 2 L 7 2 4F A6WE 20081211 NM 2008 12 11 K11A2008120972004 1 20070719 A 5320 FLOOR SUPPORT BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 FLOOR SUPPORT L-ANGLE HAS AREA OF CORROSION AROUND NUT PLATES. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008120972012 1 20070719 A 5322 SHEAR TIE BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 SHEAR TIE HAS AREA OF CORROSION ON AFT SIDE. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008121072003 1 20070719 A 5311 FRAME BOEING 727 7272B6 138407J NM FUSELAGE DENTED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 FRAME DENTED ON UPPER SURFACE IN 2 AREAS. 2 L 7 3 4F A3WE 20081212 NM 2008 12 12 K11A2008121172013 1 20070720 A 5200 SKIN BOEING 727 7272B6 138407J NM DOOR DENTED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 CENTER OF DOOR OUTER SKIN DENTED. 2 L 7 3 4F A3WE 20081212 NM 2008 12 12 K11A2008121172016 1 20070721 A 5330 SKIN BOEING 727 7272B6 138407J NM BS 197 DENTED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SKIN HAS A DENT. 2 L 7 3 4F A3WE 20081212 NM 2008 12 12 K11A2008121172017 1 20070721 A 5330 SKIN BOEING 727 7272B6 138407J NM BS 225 DENTED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SKIN HAS A DENT. 2 L 7 3 4F A3WE 20081212 NM 2008 12 12 K11A2008121172018 1 20070721 A 5330 SKIN BOEING 727 7272B6 138407J NM BS 211 DENTED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SKIN HAS DENT. 2 L 7 3 4F A3WE 20081212 NM 2008 12 12 K11A2008121172019 1 20070721 A 5330 SKIN BOEING 727 7272B6 138407J NM BS 424 DENTED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SKIN HAS DENT. 2 L 7 3 4F A3WE 20081212 NM 2008 12 12 K11A2008112117202 1 20070721 A 5330 SKIN BOEING 727 7272B6 138407J NM BS 424 DENTED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SKIN HAS DENT. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008121072005 1 20070718 A 5313 STRINGER BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 FORWARD BILGE STRINGER HAS CORROSION ON UPPER FLANGE. 2 L 7 3 4F A3WE 20081212 NM 2008 12 12 K11A2008121172012 1 20070720 A 5320 DUCT BOEING 727 7272B6 138407J NM DAMAGED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 AREA OF DAMAGE LOWER LEFT SIDE OF SOUND ATTENUATING MATERIAL TOP OF DUCT BEHIND INLET (S DUCT). 2 L 7 3 4F A3WE 20081212 NM 2008 12 12 DL757081686 1 20070807 A 5310 STRUCTURE BOEING 757 757232 1384965 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 609DL 22816 MAJOR REPAIR ER/A 463313-14. THREE DENTS NEAR A/C NOSE REPAIRED. 2 L 7 2 4F RT A2NM 20081212 NM 2008 12 12 K11A2008121172001 1 20070719 A 5322 SHEAR TIE BOEING 727 7272B6 138407J NM BS 1130 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SHEAR TIE HAS CORROSION ON AFT SIDE. 2 L 7 3 4F A3WE 20081212 NM 2008 12 12 K11A2008121172002 1 20070719 A 5322 SHEAR TIE BOEING 727 7272B6 138407J NM BS 1110 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SHEAR TIE HAS CORROSION ON AFT SIDE. 2 L 7 3 4F A3WE 20081212 NM 2008 12 12 K11A2008121172003 1 20070719 A 5322 SHEAR TIE BOEING 727 7272B6 138407J NM BS 910 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SHEAR TIE HAS CORROSION ON AFT SIDE. 2 L 7 3 4F A3WE 20081212 NM 2008 12 12 K11A2008121172004 1 20070719 A 5311 FRAME BOEING 727 7272B6 138407J NM BS 970 DENTED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 FRAME DENTED ON TOP SIDE. 2 L 7 3 4F A3WE 20081212 NM 2008 12 12 K11A2008121172005 1 20070719 A 5311 FRAME BOEING 727 7272B6 138407J NM BS 1070 DENTED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 FRAME DENTED ON TOP SIDE. 2 L 7 3 4F A3WE 20081212 NM 2008 12 12 K11A2008121172006 1 20070719 A 5320 WEB BOEING 727 7272B6 138407J NM BS 1125 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 MAIN DECK LOWER WEB HAS CORROSION. 2 L 7 3 4F A3WE 20081212 NM 2008 12 12 K11A2008121172007 1 20070719 A 5320 STRUCTURE BOEING 727 7272B6 138407J NM BS 1112 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 CORROSION ON OTBD SIDE VERTICAL FLANGE. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 K11A2008121072007 1 20070722 A 5322 SHEAR TIE BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 720CK 21298 FWD PIT CORROSION ON SHEAR TIE. 2 L 7 3 4F A3WE 20081215 NM 2008 12 15 K11A2008121172009 1 20070719 A 5320 INTERCOSTAL BOEING 727 7272B6 138407J NM BS 985 CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 MAIN DECK FLOORBEAM INTERCOSTAL HAS CRACK AT LIGHTNING HOLE. 2 L 7 3 4F A3WE 20081215 NM 2008 12 15 K11A2008121172010 1 20070719 A 5520 STRUCTURE BOEING 727 7272B6 138407J NM ELEVATOR DENTED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 UPPER L/E DENTED AND BUCKLED, ELEVATOR STA 225.54 TO 136.50. 2 L 7 3 4F A3WE 20081215 NM 2008 12 15 K11A2008121172011 1 20070720 A 5101 DUCT BOEING 727 7272B6 138407J NM UNKNOWN DAMAGED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 AREA OF DAMAGE LOWER RIGHT SIDE JUST AFT OF SOUND ATTENUATING MATERIAL TOP OF DUCT BEHIND INLET (S DUCT). 2 L 7 3 4F A3WE 20081216 NM 2008 12 16 UALA2008111304633 1 20071109 A 5420 STRUCTURE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 NR 2 PYLON FUEL LINE CUTOUT FWD INBOARD ATTACH HOLE CRACKED. SUSPECT ENGINE VIBRATION CAUSE. INSTALLED NEW REPAIR DOUB LER PER REO-G12178 REV B. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081212 NM 2008 12 12 K11A2008121172008 1 20070719 A 5320 STRUCTURE BOEING 727 7272B6 138407J NM BS 1070 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 CORROSION ON INBD SIDE VERTICAL FLANGE. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 UALA2008111303999 1 20071001 A 2730 162500100 COMPUTER BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU ELEVATOR FAULTY A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 907UA 25007 FEEL DIFF PRESS ILLUM AGAIN DURING DESCENT. DEBRIEFED FLT CREW: WAS TOLD THE ELEVATOR FEEL DIFF PRESS CAME ON AT 34,00 0 FT, 12,000 AND ON LANDING. ACCOMPLISHED TROUBLESHOOTING PROCEDURES. FAILED OPS CHECK ITEM Q NR 3 FEEL FORCES CHECK. PULL BACK FORCES HIGH, OUT OF LIMITS. REPLACED ELEVATOR FEEL COMPUTER. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 20081218 NM 2008 12 18 K11A2008121272015 1 20070726 A 5230 SKIN BOEING 727 7272B6 138407J NM CARGO DOOR DAMAGED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 MCD FWD LOWER CORNER INNER SKIN DAMAGED. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121272016 1 20070814 A 5754 STIFFENER BOEING 727 7272B6 138407J NM RT LEADING EDGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 RT LEADING EDGE STIFFENER HAS CORROSION. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121272017 1 20070816 A 5320 STIFFENER BOEING 727 7272B6 138407J NM FUSLEAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 VERTICAL STIFFENER CORROSION, LT W/W KEEL BEAM. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121272018 1 20070826 A 5320 STIFFENER BOEING 727 7272B6 138407J NM FUSELAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 VERTICAL STIFFENER CORROSION, RT W/W KEEL BEAM. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121272019 1 20070906 A 5330 SKIN BOEING 727 7272B6 138407J NM BS 642 DENTED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SKIN HAS DENT, EXTERNAL FUSELAGE. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121272020 1 20070910 A 5330 SKIN BOEING 727 7272B6 138407J NM BS 720 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SKIN HAS CORROSION, LOWER FUSELAGE. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121572006 1 20070920 A 5330 SKIN BOEING 727 7272B6 138407J NM BS 1100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SKIN HAS CORROSION, C2 DOOR CUTOUT LOWER SILL LOWER WEB. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121572007 1 20070927 A 5322 SHEAR TIE BOEING 727 7272B6 138407J NM BS 1183 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SHEAR TIE HAS CORROSION. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121572008 1 20070924 A 5320 FLOOR SUPPORT BOEING 727 7272B6 138407J NM BS 700-720 CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 FLOOR SUPPORT WEB CRACKED. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121572009 1 20070929 A 5414 SKIN BOEING 727 7272B6 138407J NM AIR INTAKE CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 CENTER ENGINE AIR INTAKE DUCT HAS SKIN CRACK, 4 O`CLOCK POSITION. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121572010 1 20070919 A 5230 SKIN BOEING 727 7272B6 138407J NM CARGO DOOR CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 C1 DOOR CRACK AT PREVIOUS REPAIR. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121272010 1 20070724 A 5322 SHEAR TIE BOEING 727 7272B6 138407J NM BS 950A CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 CORROSION AT SHEAR TIE. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121272011 1 20070725 A 5320 STIFFENER BOEING 727 7272B6 138407J NM BS 915 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 CORROSION ON BACK SIDE OF VERTICAL STIFFENER, LT W/W STA 915 54 INCHES BELOW W/W CEILING NET TO KEEL BEAM. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121272012 1 20070725 A 5320 STIFFENER BOEING 727 7272B6 138407J NM BS 930 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 CORROSION ON BACK SIDE OF VERTICAL STIFFENER, LT W/W STA 930 54 INCHES BELOW W/W CEILING NEXT TO KEEL BEAM. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121272013 1 20070726 A 5311 FRAME BOEING 727 7272B6 138407J NM BS 1090 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 CORROSION ON FRAME WEB AFT SIDE. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121272014 1 20070726 A 5230 SKIN BOEING 727 7272B6 138407J NM CARGO DOOR DAMAGED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 MCD AFT UPPER INNER SKIN DAMAGED, MAIN CARGO DOOR. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121572001 1 20070910 A 5322 SHEAR TIE BOEING 727 7272B6 138407J NM BS 1148 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SHEAR TIE HAS CORROSION. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121572002 1 20070911 A 5330 SKIN BOEING 727 7272B6 138407J NM BS 730B CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 EXTERNAL SKIN HAS CORROSION AT ACCESS PANEL. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121572003 1 20070929 A 5330 SKIN BOEING 727 7272B6 138407J NM BS 1090-1110 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SKIN HAS CORROSION, AFT PIT. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2002121572004 1 20070929 A 5330 SKIN BOEING 727 7272B6 138407J NM BS 1120-1110 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SKIN HAS CORROSION, AFT PIT. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121572005 1 20070929 A 5330 SKIN BOEING 727 7272B6 138407J NM BS 1070-1090 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SKIN CORROSION, AFT PIT. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121572011 1 20071004 A 5414 SKIN BOEING 727 7272B6 138407J NM INTAKE DUCT DAMAGED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 CENTER ENGINE AIR INTAKE DUCT HAS SKIN DAMAGE AT AFT EDGE, 9 O’CLOCK POSITION. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121572012 1 20071004 A 5313 STRINGER BOEING 727 7272B6 138407J NM BS 720E CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 STRINGER 24R CORRODED. 2 L 7 3 4F A3WE 20081219 NM 2008 12 19 K11A2008121672001 1 20071004 A 5311 FRAME BOEING 727 7272B6 138407J NM BS 1110 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 FRAME HAS EVIDENCE OF CORROSION. 2 L 7 3 4F A3WE 20081219 NM 2008 12 19 K11A2008121672002 1 20071019 A 5311 FRAME BOEING 727 7272B6 138407J NM BS 1070 DENTED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 FRAME DENTED. 2 L 7 3 4F A3WE 20081219 NM 2008 12 19 K11A2008121672003 1 20071024 A 5322 SHEAR TIE BOEING 727 7272B6 138407J NM BS 950F CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 FRAME SHEAR TIE CORRODED. 2 L 7 3 4F A3WE 20081219 NM 2008 12 19 K11A2008121672005 1 20071115 A 5322 SHEAR TIE BOEING 727 7272B6 138407J NM BS 1110 CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SHEAR TIE CRACKED. 2 L 7 3 4F A3WE 20081219 NM 2008 12 19 K11A200121672006 1 20071031 A 5330 SKIN BOEING 727 7272B6 138407J NM BS 660 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 FUSELAGE SKIN CORROSION. 2 L 7 3 4F A3WE 20081219 NM 2008 12 19 K11A2008121672007 1 20071101 A 5320 WEB BOEING 727 7272B6 138407J NM BS 1165 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 MAIN DECK FLOOR WEB CORRODED AROUND NUT PLATE. 2 L 7 3 4F A3WE 20081219 NM 2008 12 19 K11A2008121672008 1 20071022 A 5220 SKIN BOEING 727 7272B6 138407J NM ESCAPE HATCH CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 LT AFT OVERWING ESCAPE HATCH EXTERNAL SKIN CRACKED, 1/4 INCH ABOVE OPENING. 2 L 7 3 4F A3WE 20081219 NM 2008 12 19 K11A2008121672009 1 20071116 A 5720 STIFFENER BOEING 727 7272B6 138407J NM RT WING CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 RT WING FRONT SPAR VERTICAL STIFFENER CRACKED. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121272007 1 20070721 A 5330 SKIN BOEING 727 7272B6 138407J NM BS 1193 DENTED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SKIN HAS A DENT EXTERNAL FUSELAGE. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121272008 1 20070721 A 5330 SKIN BOEING 727 7272B6 138407J NM BS 1200 DENTED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SKIN HAS DENT EXTERNAL FUSELAGE. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121272001 1 20070721 A 5330 SKIN BOEING 727 7272B6 138407J NM BS 1031 DENTED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SKIN HAS DENT. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121272002 1 20070721 A 5330 SKIN BOEING 727 7272B6 138407J NM BS 1070-1090 DENTED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SKIN HAS A DENT EXTERNAL FUSELAGE. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121272003 1 20070721 A 5330 SKIN BOEING 727 7272B6 138407J NM BS 1063 DENTED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SKIN HAS A DENT EXTERNAL SKIN. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121272004 1 20070721 A 5330 SKIN BOEING 727 7272B6 138407J NM BS 1075 DENTED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SKIN HAS A DENT EXTERNAL FUSELAGE. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121272005 1 20070721 A 5330 SKIN BOEING 727 7272B6 138407J NM BS 1140 DENTED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SKIN HAS A DENT EXTERNAL FUSELAGE. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 K11A2008121272006 1 20070721 A 5330 SKIN BOEING 727 7272B6 138407J NM BS 1180 GOUGED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 SKIN HAS A GOUGE EXTERNAL SKIN. 2 L 7 3 4F A3WE 20081219 NM 2008 12 19 K11A2008121672010 1 20071121 A 5521 SPAR BOEING 727 7272B6 138407J NM RT ELEVATOR CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 RT ELEVATOR REAR SPAR CRACKED FWD OF THE NR 4 TRIM TAB HINGE, ELEVATOR STA 99.79. 2 L 7 3 4F A3WE 20081222 NM 2008 12 22 K11A2008122272309 1 20070106 A 5315 FLOORBEAM BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 723CK 20545 CORROSION ON FLOORBEAM UPPER CHORD AFT SURFACE. 2 L 7 3 4F RT A3WE 20081223 NM 2008 12 23 UALA2008111305114 1 20071216 A 3610 1074923 REGULATOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 2 ENGINE FAULTY A UALA B EMER. DESCENT J WARNING INDICATION NR NOT REPORTED 1 WP 29 349UA 24253 FLIGHT LOST CABIN PRESSURE, DESCENDED TO FL 100. FLT ABLE TO PRESS CABIN CLIMB TO FL240. UNABLE TO CLIMB HIGHER. CONT INUED FLIGHT TO PLANNED DESTINATION. OPENED ENGINE CHECKED REGULATOR AND SENSE LINES FOR DISCREPANCIES. SUPPLY SENSE L INE FOUND BROKEN (90) AND ONE WITH DEEP WEAR (80), REPLACED BOTH. RAN ENGS AT CRUISE POWER WITH NO ENG BLEED OR PACK I SSUES NOTED. HULL LEAKAGE ACCOMPLISHED ON SEPARATE CHECK. REPLACED NR 2 ENG BLEED AIR REGULATOR PRECAUTIONARY DUE TO D AMAGED SUPPLY SENSE LINE. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 NM 2008 12 23 UALA2008111304567 1 20071102 A 3520 60B5C01019 CONTROL UNIT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE 02 PAX SYSTEM LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 196UA 28715 PAX O2 LOW. RECURRED ON FLT 916-22NOV. REPLACED LEAKING PAX O2 FLOW CONTROL UNIT. LEAK FOUND ON PRESSURE LINE CONNECT ED TO THERMAL COMPENSATOR AT CREW O2 BOTTLE. REPLACED VERTICAL LINE AND CONNECTING ELBOW AND SUBSEQUENT THERMAL COMPENS ATOR LINE. NO FURTHER LEAKS NOTED. 2 L 7 4 4F 4 F RT A20WE E24NE 20081222 NM 2008 12 22 K11A2008122272310 1 20070101 A 5340 STRINGER CLIP BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 723CK 20545 STRINGER CLIP CORRODED AT AFT SIDE OF FRAME. 2 L 7 3 4F RT A3WE 20081223 NM 2008 12 23 UALA2008111304772 1 20071119 A 2120 3289562432145525 VALVE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU A/C PACK MALFUNCTIONED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 379UA 24654 DESCENDED TO 24000FT DUE TO SINGLE PACK OPERATION. REPLACED FAN AIR VALVE AND PRSOV. SECURED APU PNEUMATIC DUCTS CLAMP S. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 NM 2008 12 23 UALA2008111304215 1 20071014 A 5730 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU WING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 341UA 24245 FUEL LEAKING AT AFT SPAR JUST OUTBOARD OF LT MAIN GEAR, FROM UPPER REAR SPAR CORD REINFORCEMENT DOUBLER LOCK FASTENER. BEAM LT SUPPORT FTG HAS 6 ELONGATED HOLES IN UPPER SKIN. BEAM LT SUPPORT FTG HAS 6 ELONGATED HOLES IN UPPER SKIN. EG A PPROVAL TO USE LG DIA LOCK FASTENER INSTEAD OF FREEZE PLUG. MACH SHOP DRILLED & CLEANED UP FASTENER HOLES LT SIDE. AC P PERM REPAIR PER EVA 70 629A REF WU B0530A. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 NM 2008 12 23 UALA2008111304249 1 20071015 A 2751 01812996 INDICATOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU TE FLAP FAULTY A UALA O OTHER N FALSE WARNING AP APPROACH 1 WP 29 378UA 24653 UPON SELECTING FLAPS 5 - FLAP INDICATOR NEEDLES SPLIT, BUT NEVER GOT LOCK OUT. CREW USED ALT FLAP EXTENSION. *S/D* FL AP BYPASS VALVE WILL NOT ALLOW FLAPS TO EXTEND WITH HYDRAULICS. REPLACED RELAY 123, NO HELP. UPON SELECTING FLAPS 5 - FLAP INDICATOR NEEDLES SPLIT, BUT NEVER GOT LOCK OUT. CREW USED ALT FLAP EXTENSION. REPAIRED WIRE AT RT TRANSMITTER CO NNECTOR PIN NR 2. BYPASS VALVE OPS CKS NORMAL. TRAILING EDGE FLAP POSITION IND REPLACED. 2 L 7 2 4F 4 F RT A16WE E21EU 20081224 NM 2008 12 24 K11A2008122372304 1 20070103 A 5330 SKIN BOEING 727 7272H3 138368N NM BS 870 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 CORROSION ON FUSELAGE SKIN. 2 L 7 3 4F RT A3WE 20081223 NM 2008 12 23 UALA08111304351A 1 20071023 A 2621 6937307149 MODULE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU ENG FIRE CONTROL FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 924UA 26645 NR 2 FIRE HANDLE DOES NOT ILLUMINATE DURING FIRE TEST. *S/D* NR 2 ENG FIRE TEST INOP BOTH "A" AND "B" TEST FAIL. FOUN D TERM LUG (CORE B-LOOP) UPPER RT BAD, REPLACED SAME. CTR CORE OF DET TO SHELL, A RES INFINITE, B 20 MEG, SHOULD BE MIN OF 40 MEG, REPLACED ENG CORE B LOOP DET (M1122), TEST OK. REPLACED FIRE CONTROL MODULE. QUICK CHECK OF ENG 2 FIRE LOO PS SHOWED NO OBVIOUS PROBLEMS. CLEANED AND CHECKED THE ENG 2 PYLON DISCONNECT. REPEATED FIRE TEST NUMEROUS TIMES WITH OLD PANEL AND NEW PANEL AND WAS NEVER ABLE TO DUPLICATE ANY FAULTS. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 NM 2008 12 23 K11A2008121672004 1 20071026 A 5340 BOLT BOEING 727 7272B6 138407J NM ATTACH FITTING CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 21298 CORROSION AT BULKHEAD FITTING ATTACH BOLTS. 2 L 7 3 4F A3WE 20081223 NM 2008 12 23 UALA2008111305073 1 20071212 A 3260 SENSOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NLG DOWNLOCK FAULTY A UALA O OTHER N FALSE WARNING CL CLIMB 1 WP 29 367UA 24536 NOSE LANDING GEAR RED LIGHT WAS ILLUMINATED AFTER TAKEOFF, AND CONTINUED TO BE ILLUMINATED. CREW VERIFIED NOSE GEAR WAS UP. S845 HAS DAMAGED WIRES IN NOSE WHEEL WELL. REPLACED DOWNLOCK SENSOR S845. SEVERAL GEAR SWINGS PERFORMED, OPS NOR MAL. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 NM 2008 12 23 UALA2008111305209 1 20071220 A 3260 SENSOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU MLG FAULTY A UALA O OTHER N FALSE WARNING CL CLIMB 1 WP 29 310UA 23671 CREW REPORTS ON GEAR RETRACTION THE NLG GREEN AND RED LIGHTS STAYED ON WITH GEAR HANDLE UP OR OFF. CYCLED GEAR AND NO H ELP. NLG APPEARS TO BE UP, NO ABNORMAL NOISE AND CREW HEARD TIRES HIT SPIN PADS. AFTER A FEW MINUTES, THE GREEN LIGHT WENT OUT, BUT RED LIGHT STAYED ON. COULD NOT DUPLICATE ON GROUND, REPLACED S845, M1215 AND M1214 AS A PRECAUTION. ACCO MPLISHED NOSE GEAR SWING. NOSE GEAR AND LIGHTS, OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 NM 2008 12 23 UALA2008111304612 1 20071108 A 3260 94P10 SWITCH BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NLG INOPERATIVE A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 127UA 28813 TAKEOFF ABORTED AT 100KTS ON ACCT NOSE GEAR PRESSURE SWITCH INDICATION. NOSE GEAR PRESSURE SWITCH INOP. STAB TRIM POS IND MUST BE SET PROPERLY BEFORE EACH FLT. REPLACED NOSE GEAR PRESSURE SWITCH. PERFORMED FUNCTIONAL TEST, OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081223 NM 2008 12 23 K11A2008122372310 1 20070110 A 5315 FLOORBEAM BOEING 727 7272H3 138368N NM BS 400 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 MAIN DECK FLOORBEAM UPPER CHORD HAS CORROSION. 2 L 7 3 4F RT A3WE 20081231 WP 2008 12 31 AALA200802472A 1 20071107 A 3350 LAMP DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 596AA 53286 LGA - EMERGENCY LIGHT AT OVERHEAD FORWARD ENTRY DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT FORWARD ENTRY DO OR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20090108 CE 2009 1 8 GUUA93753112707A 1 20071127 A 5330 SKIN BEECH 1900 1900D 1154162 CE FUSELAGE DAMAGED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 38537 UE158 DURING SCHEDULED ROUTINE MX, DISCOVERED EXFOLIATION AT LOWER FUSELAGE SKIN BETWEEN FS 288.00 AND FS 305.00. REMOVED DAM AGED SKIN FABRICATED AND INSTALLED AN EXTERNAL DOUBLER REPAIR. 2 L 7 2 4T RT A24CE 20090112 CE 2009 1 12 GUUA95253052907A 1 20070529 A 5312 BULKHEAD BEECH 1900 1900D 1154162 CE FUSELAGE CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87552 UE216 DURING INSP DISCOVERED RT FWD PRESSURE BULKHEAD CRACKED 2.5 INCHES HORIZONTALLY AND 1.0 INCH VERTICALLY AT STA 89.00. S TOP DRILLED CRACKS AND INSTALLED AN EXTERNAL DOUBLER REPAIR. 2 L 7 2 4T RT A24CE 20090112 CE 2009 1 12 GUUA95253053107A 1 20070531 A 5312 PRESSURE PANEL BEECH 1900 1900D 1154162 CE NLG WW CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87552 UE216 DURING INSP DISCOVERED CRACKED CEILING IN NOSE WHEEL WELL AT FS 89 WL 100.00 AT CENTER BUTT LINE. REMOVED DAMAGED AREA AND INSTALLED SHIM AND EXTERNAL REINFORCEMENT DOUBLER REPAIR. 2 L 7 2 4T RT A24CE 20090112 CE 2009 1 12 GUUA95753101807A 1 20071018 A 5330 SKIN BEECH 1900 1900D 1154162 CE FUSELAGE CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87557 UE246 DURING SCHEDULED ROUTINE INSP DISCOVERED FUSELAGE SKIN EXFOLIATED AT FS 225.250. REMOVED CORRODED SECTION OF FUSELAGE A ND INSTALLED REINFORCEMENT DOUBLER REPAIR. 2 L 7 2 4T RT A24CE 20090112 CE 2009 1 12 GUUA94753020507A 1 20070205 A 5330 SKIN BEECH 1900 1900D 1154162 CE FUSELAGE CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 69547 UE189 DURING SCHEDULED ROUTINE MX DISCOVERED AFT LOWER FUSELAGE SKIN AT AFT COMM ANTENNA FS 400 HAD CRACK. STOP DRILLED CRACK FABRICATED AND INSTALLED AN EXTERNAL REINFORCEMENT DOUBLER REPAIR. 2 L 7 2 4T RT A24CE 20090112 CE 2009 1 12 GUUA95453080607A 1 20070806 A 5330 SKIN BEECH 1900 1900D 1154162 CE FUSELAGE CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87554 UE227 DURING SCHEDULED ROUTINE MX DISCOVERED EXFOLIATION AT LOWER FUSELAGE SKIN AT FS 273.25 AND FS 285.25. REMOVED DAMAGE SK IN FABRICATED AND INSTALLED AN EXTERNAL DOUBLER REPAIR. 2 L 7 2 4T RT A24CE 20090112 CE 2009 1 12 GUUA94771022607A 1 20070226 A 7120 129910032101 TUBE BEECH 1900 1900D 1154162 CE ENGINE TRUSS CHAFED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 69547 S2120 UE189 DURING INSP DISCOVERED ENGINE TRUSS TUBE PN 129-910032-101 HAD CHAFING DAMAGE AT 2.50 INCHES AFT OF FIRE SEAL FLANGE ON INBD SIDE. PERFORMED ENGINE TRUSS REPAIR TO CHAFED AREA, IAW FAA APPROVED DATA. 2 L 7 2 4T RT A24CE 20090120 NM 2009 1 20 JJBA20095330002 1 20071228 A 5330 85320007 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 361PH 516 LAV SERVICING TRUCK BACKED INTO ACFT WHILE PARKED AT GATE. RE AND TORN SKIN IAW REPAIR DOCUMENT 01-12-07 REV 1R. MFG D AMAGE TOLERANCE REVIEW-INSP AT 40,000 FLTS WITH EDDY CURRENT (LOW AND HIGH FREQ). 2 H 7 2 4T RT A13NM 20090205 NM 2009 2 5 UALA2008111305061 1 20071211 A 2120 UNKNOWN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN SMOKE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 913UA 25291 CREW REPORT: LIGHT SMOKE IN THE CABIN WITH PACKS ON. UNABLE TO DUPLICATE. ACCOMPLISHED PACK BURN WITH EXTERNAL AIR CA RT. RAN PACKS FULL WARM FOR APPX 10 MIN EACH AND DISSIPATED SMELLS. PACKS OPERATED WITH NO FUMES OR SMOKE AFTER BURNOU T. OPS NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 20090205 NM 2009 2 5 UALA2008111304745 1 20071119 A 5610 5893543139 WINDSHIELD BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT CRACKED A UALA K NONE O OTHER AP APPROACH 1 WP 29 374UA 24639 CAPTAIN'S WINDSHIELD SHATTERED FOUR MINUTES BEFORE TOUCHDOWN. REPLACED WINDSHIELD. 2 L 7 2 4F 4 F RT A16WE E21EU 20090205 NM 2009 2 5 UALA2008111304902 1 20071202 A 5610 5893543139 WINDSHIELD BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT CRACKED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 366UA 24535 RTFL - CAPTS WINDSHIELD CRACKED ON CLIMBOUT. REPLACED CAPTAIN WINDOW. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071300250 20070713 00250 2007 7 13 AWXA200700798 1 20070705 A 2611 RAI2800M0706 CONTROL UNIT AIRBUS LAV SMOKE FALSE ACTIVATION A AWXA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 28 838AW 6253 6253 2615 PHX - MX REPORTED SMOKE LAV AND CARGO DETECTION FAULT LIGHT ILLUMINATED. MX REMOVED AND REPLACED SDCU IAW MM 26-17-34-4 01. OPERATIONAL CHECK WAS GOOD. 2007090600049 20070906 00049 EA 2007 9 6 2007F00051 2 20070822 A 8530 850991R CYLINDER HEAD LYC O540 IO540C4B5 41532 EA ENGINE SEPARATED G C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 EA 17 1100 50 L4422 CYLINDER HEAD SEPARATED FROM THE BARREL PRIOR TO DEPARTURE. THE ENGINE HAD BEEN SUFFICIENTLY WARMED UP AND THE GROUND RU N UP CHECKS HAD BEEN COMPLETED. 3 O 1E4 2007012200067 20070122 00067 NM 2007 1 22 WRLA2007013 1 20070108 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE BS 630-670 CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 41081 48632 DURING 2C+12A+150M CHECK, EGAT MAINT FOUND CORROSION AT STA 630-670 LONGERON L52. CUT & FABRICATE REPAIR THE DAMAGED AR EA PER MD-11F SRM 53-10-00 REV.38 FIG.1 & FIG.2. 2.CONDITION CHECK NORMAL. 2 L 7 3 4F 4 F RT A22WE E24NE 2007011800138 20070118 00138 NE 2007 1 18 2007UALA00044 2 20070106 A 7230 COMPRESSOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 2 STALLED A UALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 WP 29 223UA 30224 222149 NR 2 ENGINE COMPRESSOR STALL. ENGINE CONTINUES STALLING WHENEVER THROTTLE ADVANCED BEYOND IDLE. ENGINE REPLACED AT KIX. SHOP DISASSEMBLY SHOWED HEAVY HP COMPRESSOR BLADE DAMAGE RESULTING FROM LIBERATION OF 14 BROKEN VARIABLE STATOR VANE IN NER TRUNNION 'BUTTONS'. THE INNER TRUNNION BUSHINGS HAD WORN AWAY, THEREBY ALLOWING METAL-TO-METAL CONTACT BETWEEN THE 'BUTTONS' AND INNER SHROUD. THIS PROBLEM HAS PREVIOUSLY OCCURRED IN THE INDUSTRY. CURRENT FIXES ARE TO RTV THE INNER S HROUD CAVITIES, TO CONTAIN BROKEN BUTTONS, AND PREVENT THEM FROM ENTERING THE GASPATH. THE OTHER FIX IS NEW MATERIAL IN NER TRUNNION BUSHINGS THAT ARE MORE RESISTANT TO WEAR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007012500018 20070125 00018 CE 2007 1 25 DXTA200701866 1 20070119 A 3230 65430087 UPLOCK SWITCH CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 699QS 5605199 UPON RAISING GEAR , GEAR UNLOCK REMAINED ON HYD PRESS REMAINED ON, STAB MISCOMPARE ILLUMINATED . UPON PULLING HYD CONTRO L CB, RT MAIN GEAR LIGHT ILLUMINATED. TROUBLESHOT TO NOSE GEAR UPLOCK SWITCH P/N 65-430087 S/N N/A. INSTALLED NEW SWITC H. OPS CHECK GOOD. WORK DONE IAW CESSNA 560XL MM CH 32-30-05 2 L 7 2 4F 4 F RT A22CE E00059EN 2007020200096 20070202 00096 EU 2007 2 2 BAQA2007005 1 20070130 A 5302 SKIN BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1E 60030 NE TAILBOOM CRACKED E BAQA K NONE E VIBRATION/BUFFET NR NOT REPORTED 1 EA 03 911TG 6737 7506 A CRACK WAS FOUND AT THE TOP OF THE TAILBOOM VERTICAL FIN WHILE TROUBLESHOOTING A TAIL ROTOR VIBRATION ISSUE. THE CRACK WAS FOUND ON THE LT SIDE OF THE ACCESS SIDE OF THE OPENING FOR ACCESS TO THE TAILROTOR GEARBOX MOUNTING HARDWARE. 1 G 7 2 3U 3 U NC H13EU E19EU 2007012300180 20070123 00180 NM 2007 1 23 2007UALA00124 1 20070118 A 5230 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 927UA 26649 RAMP REPORTS AFT CARGO DOOR DAMAGE ON EXTERIOR SKIN. MAJOR REPAIR: FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 52-0 0-01 REPAIR 2. 2 L 7 2 4F 4 F RT A16WE E2GL 2007012600158 20070126 00158 NM 2007 1 26 2007UALA00179 1 20070123 A 2560 FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN LOOSE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 386UA 24661 AFT ENTRY DOOR FWD GIRT BAR FLOOR MOUNT BRACKET FITTING IS LOOSE. IMPROPER SCREWS USED. INSTALLED SCREWS WITH PROP ER LENGTH. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022000348 20070220 00348 EU 2007 2 20 07FDEA00353 1 20070206 A 7830 THRUST REVERSER AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680 30025 NE NR 1 MALFUNCTIONED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 681FE 799 705284 NR 1 T/R PRESSURIZED AS POWER INCREASED THROUGH 75-80 PERCENT N1. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEG ORY: C EXPIRATION: 16FEB07 "MEL 78-30-01-A: ENGINE NR 1 TSI OPENED FOR T/S. 2 L 7 2 4F 4 F RT A35EU E13NE 2007022100011 20070221 00011 NM 2007 2 21 2007UALA00360 1 20070208 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 AFT CABIN FLOORBEAM AT BS 947.5 CAP CORRODED LBL 21 - RBL 7. MAJOR REPAIR. REMOVED DAMAGE. FABRICATED AND INSTALLED T -CAP, SPLICE ANGLE STRAPS AND CLIPS PER MM 53-10-95 REPAIR XIX PAGE 803 AND 817. 2 L 7 2 4F 4 F RT A16WE E21EU 2007022600013 20070226 00013 NM 2007 2 26 ASMF200702007 1 20070218 A 2782 59370215503 ACTUATOR DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE LT LE SLAT LEAKING W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 158PL 49761 DURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE LT SLAT ACTUATOR. THE SLAT ACTUATOR WAS REPLACED IAW MM 27-80 -05, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007022800016 20070228 00016 EU 2007 2 28 2007UALA00497 1 20070216 A 3350 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 436UA 638 CABIN EEL CONNECTORS HAVE BROKEN BACKSHELLS ON FLOOR BY SIDEWALL AT SEAT ROWS 6L, 7L, 15L, 18L AND 26L. [5-1-07] BACKS HELLS REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007030100021 20070301 00021 NM 2007 3 1 2007UALA00509 1 20070217 A 5200 H2052K3833 LATCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE OVERWING DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 LT OVERWING COMPARTMENT DOOR LATCH FAILED INTEGRATOR TORQUE TEST AT 275 INCH-LBS. REPLACED 4 SLIDE LATCHES PER MM25-65- 09. DOOR TORQUE CHECK GOOD. LATCHES CHATTER IN LOCKED POSITION AND A FRET CHANNEL DEVELOPS OVER TIME. 2 L 7 2 4F 4 F RT A1NM E24NE 2007030100086 20070301 00086 NM 2007 3 1 2007UALA00552 1 20070221 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 FOUND EEL 5F AFT INOPERATIVE. REPLACED CONNECTOR ASSEMBLY. OP CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022100010 20070221 00010 NM 2007 2 21 2007UALA00359 1 20070208 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 AFT GALLEY DOOR CUTOUT LWR THRESHOLD AREA CREASE BEAM HAS SEVERAL SPOTS OF CORROSION FROM BS 950-990. MAJOR REPAIR. RE MOVED AND REPLACED CREASE BEAM PER SRM 51-40-02 AND SRM 53-60-15. 2 L 7 2 4F 4 F RT A16WE E21EU 2007031200016 20070312 00016 NM 2007 3 12 AMTA200700052 1 20070202 A 2697 TERMINAL BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE GROUND WIRE LOOSE A AMTA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 560TZ 33525 LT TURB OH DET 2 STATUS MSG DISPLAYED. DURING T/S FOUND LOOSE GROUND AND LOOSE TERMINAL CONNECTION FOR NR 2 TURBINE OVH T SWITCH, TIGHTENED CONNECTIONS. SYSTEM TESTED GOOD IAW AMM. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007031200068 20070312 00068 CE 2007 3 12 DXTA200701953 1 20070217 A 5610 WINDSHIELD CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE COCKPIT FAILED E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 624QS 5605302 CAPT`S WINDSHIELD SHATTERED. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007022600004 20070226 00004 CE 2007 2 26 ACE021607 1 20070216 A 3230 MS24171D1 RELAY BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA MLG CONTAMINATED E YADA O OTHER S J AFFECT SYSTEMS WARNING INDICATION AP APPROACH 1 AL 03 112AX 2571 UC45 MANUAL GEAR EXTENSION DUE NO GREEN LIGHTS AFTER HANDLE DOWN. CONFIRMED HYDRAULIC MOTOR RELAY LOGGED WITH WATER AND DUPL ICATED FAILURE BY FREEZING RELAY, REPLACED RELAY. 2 L 7 2 4T 4 T RT A24CE E4EA 2007032100028 20070321 00028 NM 2007 3 21 2007UALA00768 1 20070315 A 3350 LAMP BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE ROW 32ABC INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHT ROW32 ABC INOPERATIVE. RELAMPED EMERGENCY LIGHTS. OP CHECKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007032300049 20070323 00049 SO 2007 3 23 SWIA200718024 1 20070119 A 5320 SUPPORT EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 221SW 120290 FRAME SUPPORT CRACKED AFT OF FRAME 9 UNDER DV WINDOW BEAM. (DISCOVERED DURING C-CHECK INSPECTION) NEW SUPPORT INSTALLED IAW SRM 120 51-10-02 PG. 3 SEC. 3A ALSO IAW RII CARD 53-800-1000. 2 L 7 2 4T 4 T RT A31SO E20NE 2007032900130 20070329 00130 NE 2007 3 29 2007UALA00856 2 20070322 A 7230 COMPRESSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE STALLED A UALA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 411UA 464 V11043 NR 2 ENGINE HAD A COMPRESSOR STALL WITH AN AUDIBLE BANG. [SUP 06-01-07] INSPECTED ENGINE PER AMM TASK FOR STALL CONDIT ION AND FOUND NO DEFECTS. LUBED VARIABLE STATOR VALVE MECHANISM AND PERFORMED IDLE RUN CHECK. NO FURTHER IRREGULARITIES NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032800211 20070328 00211 EU 2007 3 28 2007UALA00800 1 20070316 A 5311 FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 452UA 955 AFT BULK CARGO COMPT 2ND FRAME FWD OF AFT PRESSURE BULKHEAD [F68] APPROX 12 INCHES INBOARD LEFT FUSE FLOORBEAM ATTACH CR ACKED. [SUP 06-14-07] MAJOR REPAIR ACCOMPLISHED. CUTOUT DAMAGED FLANGE. HFEC TRIMMED SURFACE. FABRICATED AND HEAT T REATED REPAIR ANGLES. INSTALLED REPAIR PARTS WITH SEALANT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032900093 20070329 00093 NM 2007 3 29 2007UALA00845 1 20070321 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 FUSELAGE STR 29R AT STA 1743 HAS 2 SHEARED RIVETS. FUSELAGE FRAME HAS DEEP GOUGES STA 1720 BETWEEN STR 29L TO OUTBOARD OF STR 29R. SKIN GROUND AWAY STA 1720 STR 29L TO JUST OUTBOARD OF STR 29R. [06-14-07] MAJOR REPAIR ACCOMPLISHED. CHO RD REPAIRS 3 EA ARE PERMANENT REPAIRS, AFT SKIN REPLACEMENT WAS A PERMANENT REPAIR. FORWARD SKIN REPAIR WAS CATEGORY B I NTERIM REPAIR PER UA ENGINEERING SPECIFICATIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007033000023 20070330 00023 SO 2007 3 30 FDKA200703108 1 20070311 A 7333 23052613 SENSOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUEL SYSTEM MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 841MJ 10549 145448 FDM 6148 MCO-ATL (1020 PHX LCL). AIRCRAFT RETURNED TO THE FIELD FOR FUEL 2 LOW LEVEL MESSAGE IN FLIGHT. MX REMOVED AND REPLACED FUEL FLOW SENSOR. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007032600165 20070326 00165 CE 2007 3 26 DXTA200702045 1 20070322 A 3230 LANDING GEAR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LEFT UNKNOWN E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 931QS 7500064 WHEN GEAR SELECTED DOWN THE LT MAIN GREEN LIGHT DID NOT ILLUMINATE. THE EMERGENCY GEAR BLOW DOWN WAS PULLED. RESET & S ERVICED GEAR BLOW DOWN SYSTEM & BOTTLE. REMOVED 2 INOP BULBS FROM LT MLG INDICATOR & INSTALLED 2 NEW BULBS, SWUNG GEAR. OPS & INDICATION CHECKS GOOD. ALL WORK PERFORMED IAW CE-750 MM CHPT. 32-30-00, 12-10-36. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007033000357 20070330 00357 NE 2007 3 30 AALA20070543 2 20070324 A 7261 779150 GEARBOX DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RIGHT ENGINE INOPERATIVE A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 218AA 49168 708565 AFTER TAKEOFF FLIGHT ATTENDANT REPORTED HEARING LOUD POP FOLLOWED BY A MODERATE VIBRATION. ALL INSTRUMENTS APPEARED NOR MAL. AT FLIGHT LEVEL 290 RIGHT ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED. CREW SHUT DOWN RIGHT ENGINE AND LANDED DFW WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE AT DFW ON 24 MARCH 2007 DUE TO METAL IN OIL FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2007040400078 20070404 00078 NE 2007 4 4 ASMF200703009 2 20070327 A 7200 JT8D219 ENGINE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE LEFT FLAMED OUT W ASMF A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SW 23 755RA 37529 9922 49727 725856 AIRCRAFT AIR TURNBACK DUE TO A FLAME OUT ON LT ENGINE DURING CLIMB. DURING MAINTENANCE INSPECTION DETECTED THE C1 STUCK AND CONSIDERABLE DAMAGES ON LPT. THE LT ENGINE WAS REPLACED IAW MPCM 71-00-02, TESTED CORRECT IAW 71-00-01. LANDING A IRCRAFT WEIGHT WAS 131000 POUNDS SO OVERWEIGHT INSPECTION WAS PERFORMED IAW AMM 05-51-04, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007041200051 20070412 00051 NE 2007 4 12 CIEA200700003 2 20070406 A 7414 COWLING BEECH 90 E90 1152914 CE PWA PT6 PT6A60A 52043 NE LT NACELLE BENT E CIEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 03 63BV 13450 LW256 DURING TAKEOFF ROLL OF THE AC, AT THE POINT OF LIFTOFF, THE PILOT NOTICED THE LT ENGINE UPPER AFT COWLING HAD COME OPEN. THE TAKEOFF WAS ABORTED AND THE AC CAME TO A SAFE STOP ON THE RUNWAY. THE PILOT SHUTDOWN THE LT ENGINE AND TAXIED BAC K TO THE HANGAR ON THE RT ENGINE. MAINT INSPECTED THE COWLING AND WAS UNABLE TO FIND ANY MECHANICAL REASON FOR THE COWL ING TO HAVE COME OPEN. THERE WAS DAMAGE TO THE LT UPPER AFT COWLING AND TO THE UPPER NACELLE AREA AFT OF THE ENGINE FIR EWALL. THERE WAS DAMAGE TO THE HINGE POINT OF THE ENGINE COWLING ON THE LT SIDE OF THE COWLING; HOWEVER THE COWLING DID NOT DEPART THE AC. THE ENGINE WAS INSPECTED FOR POSSIBLE INGESTION OF DEBRIS AND NONE WAS NOTED. BOTH COWLING LATCHES 1 L 7 2 3T 4 T 3A20 E4EA 2007041200173 20070412 00173 EA 2007 4 12 A6WA200740183 1 20070402 A 7830 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE THRUST REVERSER UNKNOWN A A6WA O OTHER G MULTIPLE FAILURE LD LANDING 1 GL 31 468AW 7916 UPON LANDING THRUST REVERSERS WOULD NOT DEPLOY UNTIL AFTER 3,000 FT ROLLOUT, NEITHER REVERSER WOULD UNLOCK UNTIL BRAKES TOOK EFFECT. PERFORMED BRAKES OPS TEST IAW 32-43-00, PERFORMED ANTI-SKID COMPUTER BITE TEST IAW 32-44-06. INTERROGATED MDC, NO FAULTS FOUND. COMPLIED WITH FDR DOWNLOAD AND DATA ANALYSIS REVEALS ALL SYSTEMS OPS NORMALLY. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041300114 20070413 00114 NM 2007 4 13 2007UALA00981 1 20070401 A 3350 58781 FEEDER CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 336UA 24240 EEL LIGHTS AFT OF ROW 15 INOPERATIVE. DRIED OUT EEL TRACK & REPLACED POWER CABLE. OP CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041600057 20070416 00057 2007 4 16 2007UALA01012 4 20070402 A 2565 FASTENER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GIRT BAR MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 644UA 25094 LEFT FWD ENTRY DOOR, FWD GIRT BAR FITTING MISSING FASTENER, FOUND DURING PRELIMINARY INSPECTION. [SUP 5-1-07] INSTALLE D LT FWD ENTRY DOOR, FWD GIRT BAR FITTING FASTENER RETAINER. A/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007041700171 20070417 00171 EA 2007 4 17 A6WA200740100 1 20070302 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 453AW 7838 FLOOR SUPPORT ANGLE AT FS 621 IS CRACKED (RT). MAINTENANCE REPAIRED RT FLOOR SUPPORT ANGLE IAW REO 601R-53-61-117, REV C. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041900005 20070419 00005 NM 2007 4 19 NOCA08007 1 20070409 A 2613 0205K05600 OVERHEAT LOOP BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE MALFUNCTIONED A NOCA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 15 756NA 32448 EICAS STATUS MESSAGE L TURB OH DET 2. REMOVED AND REPLACED L ENG OVERHEAT DET 2 IAW MM 26-13-01. OPS CK NORMAL. 2 L 7 2 4F 4 F RT A2NM E12EU 2007041900021 20070419 00021 NE 2007 4 19 2007UALA01057 2 20070408 A 7210 BEARING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 GEARBOX FAILED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 538UA 25222 726582 FLIGHT DIVERTED DUE TO IFSD OF NR 1 ENGINE. [SUP 05-24-07] THIS OCCURRENCE WAS DUE TO ANGLE GEARBOX BEARING FAILURE CA USED BY EXCESSIVE VIBRATORY STRESS. THIS IS BELIEVED TO HAVE BEEN THE RESULT OF AN IMPROPER BALANCING OF THE LOWER TOWE R SHAFT WHICH COULD HAVE OCCURRED DURING INITIAL STAGE OF MANUFACTURE BY THE OEM. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041900075 20070419 00075 EU 2007 4 19 2007UALA01137 1 20070412 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 432UA 587 STRINGER 42 LT HAS CORROSION ON THE INNER SURFACE OF THE FLANGE. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION & INSTAL LED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007050300384 20070503 00384 NM 2007 5 3 2007UALA01317 1 20070427 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 195UA 26899 EXIT PATH LIGHTING AT 4F MISSING. REPLACED EEL STRIP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050800043 20070508 00043 NM 2007 5 8 2007UALA01373 1 20070430 A 3350 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 EMERGENCY LIGHTS TEST SW S10295 BY L-4 DOOR HAS BROKEN TERMINALS. [SUP 06-06-07] REPLACED SWITCH. 2 L 7 2 4F 4 F RT A2NM E17NE 2007042400236 20070424 00236 NM 2007 4 24 2007UALA01193 1 20070415 A 3350 INVERTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 506UA 24627 EEL INVERTER AT SEAT 33A LOWER SIDEWALL INOP. [SUP 4-24-07] REPLACED EEL INVERTER MODULE PER MM 33-51-07 AND OPS CHEC K GOOD ON NON ROUTINE Z2503N. 2 L 7 2 4F 4 F RT A2NM E17NE 2007042700016 20070427 00016 GL 2007 4 27 J4PA2095 1 20070402 A 2400 MCU120 CONTROL UNIT CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO HARTZL HCJ3Y PHCJ3YF1 GL MALFUNCTIONED E J4PA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 13 584CD 1011 1652 917889 F7693DFB ALT NR 1 INFLIGHT, COULD NOT RESET, AMMETER FOR ALT NR 1 SHOWED NORMAL CHARGE SOMETIME AND 0 CHARGE OTHER TIMES. ALT NR 2 SHOWED + 100 THEN -100 AFTER NR 1 SHUTOFF. BOTH WARNING LIGHTS CAME ON. AFTER LANDING, SHUT ENGINE COMPLETELY, RESTART ED FOR GROUND RUN UP SHOWED ALT NR1 ON, BUSS VOLT BELOW 28 VOLTS FOR 1 AND 2, AMP METER +50 FOR ALT 1 AND +100 ON ALT 2 . SUSPECTED MOISTURE IN THE MCU. AFTER 4 HOURS, RETURNED TO AIRCRAFT, STARTED ENGINE AND ALL OPERATIONAL CHECKED NORMAL. 1 L 7 1 3O 3 O NT A00009CH E3SO 5 C P36EA 2007052900049 20070529 00049 EU 2007 5 29 2007UALA01630 1 20070523 A 2750 FLAP SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE TE FLAPS MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 WP 29 433UA 589 CREW REPORTS THAT ON APPROACH FLAPS LOCKED OUT AT 1 UNIT, UNABLE TO RESET. AMBER ALERT DECLARED. LANDED WITH LEADING E DGE DEVICES UP AND FLAPS AT 1 DEGREE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061300051 20070613 00051 GL 2007 6 13 SIMA200715803 2 20070603 A 7200 AE3007A1 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 LEAKING A SIMA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 939AE 4922 2762 14500923 CAE312796 CREW NOTICED OIL BURNING ODOR. REMOVED AND REPLACED NUMBER ONE ENGINE IAW AMERICAN EAGLE WORK CARD 72-000-00. LEAK AND OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007062000175 20070620 00175 NM 2007 6 20 2007UALA01990 1 20070613 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 LOWER LEFT FUSELAGE BETWEEN STR 19L AND 23L FROM STA 500B +12 TO STA 500B +14 HAS 6EA DENTS. THESE DENTS ARE WITHIN ADJ ACENT BAYS. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007061400225 20070614 00225 EA 2007 6 14 S9BA0807 1 20070516 A 5710 C6W10057 STRUT DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA LT WING CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 251SA 4831 230 524 LT WING STRUT LOWER MOUNT CORRODED BEYOND LIMITS, REMOVED AND REPLACED LT WING STRUT. 1 H 7 2 3T 4 T RT A9EA E4EA 2007060500257 20070605 00257 NM 2007 6 5 2007UALA01675 1 20070528 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 FWD PIT, LEFT SIDE, STA 660, BETWEEN STR 24 -25L, MAIN FRAME DENTED (RIB). MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE A ND EXISTING PRODUCTION SPLICE. FABRICATED A NEW PRODUCTION SPLICE AND 1 EA -30 STRINGER CLIP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060700021 20070607 00021 EU 2007 6 7 M2L2007F00000 1 20070428 A 8011 DRIVE GEAR BNORM BN2 BN2A20 1520220 EU LYC O540 IO540K1B5 41532 EA HARTZL HCC2Y HCC2YK2 GL STARTER BROKEN E M2LA O OTHER O OTHER NR NOT REPORTED 1 NM 11 634MA 811 464 L1459848A AU11038B RT ENGINE STARTER DRIVE GEAR SHAFT WAS DAMAGED TO THE EXTENT, THAT THE BENDIX COULD NOT RETRACT FROM THE ENGAGED POSITIO N. THUS CAUSING THE GEAR TO REMAIN ENGAGED AFTER START. THIS IN TURN BROKE THE DRIVE GEAR TEETH. THE BROKEN TOOTH THE N LOCKED UP THE RING GEAR CAUSING THE CRANKSHAFT TO STOP ROTATION. THIS CAUSED AN ENGINE FAILURE. 1 H 7 2 3O 3 O A17EU 1E4 5 C P920 2007062800179 20070628 00179 NM 2007 6 28 2007UALA02106 1 20070618 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1420-1440 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 AFT PIT BETWEEN STA 1420-1440, INTERCOSTAL BETWEEN STR 28R TO 29R IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REMOVED CORR OSION. FABRICATED & INSTALLED NEW INTERCOSTAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007070300021 20070703 00021 EA 2007 7 3 A6WA200740257 1 20070515 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 458AW 7861 LT WING LOWER PLANK ACCESS HOLE NR 9 FOR PANEL 550AB HAS FRETTING/ CORROSION DAMAGE 1 INCH AREAS AT IB END NOT IN CRITIC AL AREA. (K) [07-17-07] MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 9 PANEL 550AB IAW BOMBARDIER REO 601R -57-21-030 REV A. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071000425 20070710 00425 NM 2007 7 10 2007UALA02287 1 20070628 A 3350 9F19948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY LIGHTS INOP LEFT OVERWING 2 AFT ASSEMBLIES. REPLACED EXTERIOR OVERWING LIGHT ASSY L1166. LIGHTS OPS CHECK NO RMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071100040 20070711 00040 CE 2007 7 11 AMWA31034C 1 20070620 A 5414 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NACELLE DAMAGED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 138YV UE138 FRICTION CHAFING DURING OPERATION HAS CREATED WORN SEGMENTS ON THE LT AND RT ENGINE NACELLES. DAMAGE WAS ALONG THE ENTI RE LENGTH OF THE NACELLE SHAPE, DEPTH VARIED AS INDICATED ON THE REPAIR AUTHORIZATION. REPAIRED IAW AIRCRAFT ENGINEERIN G INC REPORT NR 6732-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007071100224 20070711 00224 CE 2007 7 11 F222007F00001 1 20070612 A 3230 115380025 MOTOR BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE MLG FAILED E F22A O OTHER O OTHER NR NOT REPORTED 1 SW 15 888ZX 770 BB1140 THE LANDING GEAR MOTOR, PN 115-38002-5, SN 977, GAVE NO INDICATIONS PRIOR TO FAILURE, NO SLUGGISH OR NOISY OPERATION. T HE PART HAD 770.1 HOURS AND 765 CYCLES USED OF ITS 8000 CYCLE TBO. THE MOTOR HAD BEEN REMOVED FROM ANOTHER AC PRIOR TO THE OVERHAUL FOR POOR PERFORMANCE WHICH SHOULD HAVE BEEN ADDRESSED DURING THE OVERHAUL. (K) 1 L 7 2 4T 4 T A24CE E4EA 2007061900225 20070619 00225 NM 2007 6 19 2007UALA01813 1 20070604 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 WALL EEL INOP FWD OF LAV 102. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000045 20070620 00045 NM 2007 6 20 2007UALA01854 1 20070606 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 STA 787 STR 22R STR CLIP IS CRACKED. MAJOR REPAIR ACCOMPLISHED, INSTALLED NEW STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071100035 20070711 00035 CE 2007 7 11 GLBA20060957 1 20070620 A 5330 BLADE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE PROPELLER DAMAGED A GLBA O OTHER O OTHER LD LANDING 1 NM 03 253GL UE253 EXTENDED ROLLOUT, UPON LANDING, PILOTS REPORTED THAT DUE TO LANDING ROLLOUT BEYOND THE END OF THE RUNWAY, THE RT PROP N R 2 ENGINE STRUCK A RECTANGULAR BOX. PRELIMINARY DAMAGE INDICATES PROP BLADE DAMAGE AND HOLE IN FUSELAGE. [08-01-07] MX INSTALLED TEMP REPAIR IN RT FUSELAGE IAW SRM REF 51-70. 2 L 7 2 4T 4 T RT A24CE E26NE 2007071100234 20070711 00234 EU 2007 7 11 2007UALA02191 1 20070623 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 435UA 613 STR 42R BETWEEN FR 27 AND 28 HAD A DRILL MARK BLENDED OUT BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED: INSTALLED A REPAIR ANGLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100340 20070711 00340 NM 2007 7 11 2007UALA02339 1 20070630 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 203UA 24718 LEFT OVERWING ICE DETECTION LIGHT INOP. [07-24-07] REPLACED LAMP. 2 L 7 2 4F 4 F RT A16WE E2GL 2007072400165 20070724 00165 NM 2007 7 24 2007UALA02599 1 20070713 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 EMERGENCY LIGHT INOP AT CEILING ROWS 6 LT & 33 RT. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007072400169 20070724 00169 NM 2007 7 24 2007UALA02603 1 20070713 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 WALL EEL INOP: BETWEEN MID LAVS. [07-27-07] SPLICED FEEDER. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100050 20070731 00050 NM 2007 7 31 2007UALA02724 1 20070719 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 FWD LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED WITH NEW LAMP AND OP CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071100100 20070711 00100 CE 2007 7 11 DXTA200702296 1 20070625 A 3230 LANDING GEAR RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP RIGHT INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 887QS 258387 RT GEAR FAILED TO RETRACT (AFTER TAKEOFF) 3 RED LIGHTS, RT GEAR GREEN ON. [07-13-07] ADJUSTED RT MLG NORMAL DOWN AND L OCK SWITCH IAW H-800XP MM CH 32-60-00. SWUNG GEAR 5 TIMES ALL LIGHTS WORKED PROPERLY AT THIS TIME 2 L 7 2 4F 4 F RT A3EU E6WE 2007071800285 20070718 00285 NM 2007 7 18 2007UALA02423 1 20070705 A 5320 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 FWD ENTRY DOOR UPPER HINGE CUTOUT 5EA FASTENER HOLES ARE CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. INSTALLE D DOUBLER & STRUCTURAL FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007072500115 20070725 00115 EU 2007 7 25 USA2007F00009 1 20070626 A 5310 STRUCTURE AIRBUS A321 A321211 3930370 EU CFMINT CFM56 CFM565B3P 13006 NE FUSLEAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 182UW 21515 1536 CORRODED RIVET TAILS WERE FOUND IN FUSELAGE CARGO COMPARTMENT BETWEEN FRAME 24 TO 35.7 STRINGER 38L TO 38R. APPROXIMATE LY 1070 RIVETS WERE REPLACED. 25 RIVETS WERE REPLACED AT S38 OB. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NU MEROUS OTHER RIVETS HAD THE PAINT FLAKING OFF THE RIVET TAILS THAT WERE CLEANED AND HAD PRIMER AND PAINT REAPPLIED. AC WAS MFG 9 JULY 2001. (K) 2 L 7 2 4F 4 F RT A28NM E37NE 2007070900109 20070709 00109 NE 2007 7 9 KCSA07054 2 20070624 A 7200 ENGINE BOEING 747 747236B 1384804 NM PWA JT9 JT9D7Q 52054 NE NR 4 STALLED A KCSA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 GL 23 701CK 21730 NR 4 ENG SILENT STALLED DURING FLT IDLE DECEL AT 25000FT, C/W ALL APPLICABLE KA QRH PROCEDURES, 2 RESTART ATTEMPTS UNSUC CESSFUL MAX EGT 617 DEGREE, WINDMILL PAR A - 15 MIN DURATION AT 10K, N1 18%, N2 13%, FF 0, OIL QUANTITY FULL, OIL PRESS ABOVE 6 PSI. ACCOMPLISHED WINDMILL INSP IAW BMM 72-00-00 CHECK 682S. INSP AND REPLACED ENG MAIN OIL FILTER IAW BMM 72- 61-05, NO DEFECTS. CHECKED ALL MAG PLUGS IAW 72-61-02, NO DEFECTS. VISUALLY INSPECTED ALL ENG BLEED LINES, TIGHTENED P S3 LINE. RAN ENG IAW BMM 71-00-00 NORM START. ALL ENG PARA NORMAL. LEAK CHECK OF OIL FILTER & MAG PLUGS OK. T/S PER FIM 71-01-00, NO DEFECTS. 2 L 7 4 4F 4 F A20WE E3NE 2007071100343 20070711 00343 NM 2007 7 11 2007UALA02342 1 20070629 A 5210 TORQUE TUBE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD ENTRY DOOR EXCESS PLAY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 FWD ENTERY DOOR UPPER AND LOWER LATCH TORQUE TUBES HAVE EXCESSIVE LATERAL PLAY. INSTALLED SHIMS ON UPPER AND LOWER LATC H TORQUE TUBES. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071800342 20070718 00342 2007 7 18 DXTA200702319 4 20070705 A 3417 7014700607 AIR DATA MODULE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL AVIONICS BAY INTERMITTENT E DXTA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 924QS 1965 7500124 MACH TRIM AND YAW DAMPER DISENGAGED ON TAKEOFF AT 70-75 KTS. (2) ATTEMPTED TAKEOFFS. (M2B) REPLACED NR 2 MADC DUE TO I NTERMITENT SPLITS. IAW MM 34-12-00. IAW FAR 91.411 + 91-413. OLD P/N: 7014700-607, OLD S/N: 0316642. NEW P/N: 701-470 0-607. NEW S/N: 99093109. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007072500108 20070725 00108 NM 2007 7 25 2007UALA02644 1 20070713 A 3350 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 513UA 24810 LEFT & RIGHT FWD EMERGENCY LIGHTS INOP, EXTERIOR. [07-27-07] TROUBLE SHOOT AND REPLACED BATTERY. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071800352 20070718 00352 NM 2007 7 18 2007UALA02464 1 20070706 A 5522 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU RT ELEVATOR PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 924UA 26645 RIGHT ELEVATOR UPPER SURFACE 19 INCHES FROM INBOARD END AND 14 INCHES FWD OF AFT END HAS PUNCTURE. [07-27-07] MAJOR REPAIR: REMOVED DAMAGE AND REPAIRED THE ELEVATOR PER EA REV IR EA I070490 IR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007081000055 20070810 00055 NM 2007 8 10 CALA0700387 1 20070801 A 5313 6545800122 STRINGER BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE BS 294-323 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14308 23359 INSPECTION FOUND STRINGER 28R CORRODED AT STA 294-323. THE STRINGER WAS REPLACED IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080600029 20070806 00029 NM 2007 8 6 2007UALA02779 1 20070722 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 EMERGENCY STRIP LIGHTING IN FIRST CLASS IS LOOSE. [08-14-07] RESECURED STRIP LIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080600030 20070806 00030 NM 2007 8 6 2007UALA02780 1 20070721 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN ILLUMINATED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 FLOOR EMERGENCY EXIT LIGHTS ARE ILLUMINATED ROW 5 THRU 10 RIGHT SIDE ONLY IN CRUISE. [08-14-07] CHECKED WIRING TO BATTE RY PACK, UNABLE TO DUPLICATE, GROUND CHECKED OK PER MM33-51-00. NO REPEAT WRITE-UP IN SUCCEEDING 21 DAYS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080800038 20070808 00038 NM 2007 8 8 DXTA200702343 1 20070717 A 2530 COFFEEMAKER AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE GALLEY SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 227QS 127 BURNING SMELL AND SMOKE COMING FROM THE COFFEE POT. ISOLATED COFFEE POT AREA FROM WALL AND CONTINUED WITHOUT FURTHER INS TANCE. REMOVED AND REPLACED WIRE TERMINALS TO COFFEE POT- CHECK WIRES WITH METER WIRES CHECK GOOD AT THIS TIME- INSTALL ED SAME COFFEE POT- COFFEE POT OPERATES NORMAL AT THIS TIME IAW F2000 M/M'S 25-922, 20-500. THIS CLEARS MEL 25-7. SUSP ECT IMPROPER INSTALLATION OF COFFEE POT RAIL PRIOR TO ARRIVAL. 2 K 7 2 4F 4 F RT A50NM E44NE 2007081000087 20070810 00087 EA 2007 8 10 A6WA200740379 1 20070707 A 5710 PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 461AW 7870 LT FUEL PANEL 510AB HAS CORROSION DAMAGE IN THE NON-CRITICAL AREA COMPLY WITH E06/21/457 (WING PANEL CUTOUT) (K) MAINT ENANCE REPAIRED WING PLANK IAW BOMARDIER REO 601R-57-21-030. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007081700117 20070817 00117 NM 2007 8 17 KNNA200700037 1 20070711 A 5311 SKIN BOEING 737 7372Q8 138448K NM PWA JT8 JT8D17 52049 NE BS 957-966 CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 413JG 23148 SKIN IS CRACKED AT THE LOWER FWD CORNER OF THE L-2 DOOR CUT OUT. ACO NR 075397 REV 0 PROVIDES INSTRUCTIONS ON REPAIR OF L-2 DOOR CRACK SRM 53-30-3 FIGURE 46. 2 L 7 2 4F 4 F RT A16WE E2EA 2007082100082 20070821 00082 NM 2007 8 21 2007UALA02963 1 20070801 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 AFT PIT FRAME DENTED AT STA 1500 AND STR 25L. MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT DAMAGE. INSTALLED ANGLE & REPAIR ANGLE. COLD WORKED HOLES & INSURANCE CUT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082400170 20070824 00170 WP 2007 8 24 AMTA200700369 1 20070726 A 3350 LIGHT LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211535E4 54555 NE CABIN CONTAMINATED A AMTA K NONE C L F.O.D. NO TEST IN INSP/MAINT 1 GL 11 164AT 1238 EGRESS LIGHTING FROM R-1 TO R-2 (FLOOR LIGHTS) INOPERATIVE. FOUND WATER IN EGRESS TRACK. REMOVED LIGHT STRIPS, DRIED O UT WATER, AND REINSTALLED. POWER AND LIGHT STRIPS. OPS CHECK NORMAL. (K) 2 L 7 3 4F 4 F A23WE E12EU 2007090700065 20070907 00065 NM 2007 9 7 2007UALA03160 1 20070811 A 3350 GE1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 ZONE-C LEFT CEILING EMERGENCY LIGHTS 2EA ARE INOP. *S/D* RELAMPED IN TWO POSITIONS. BOTH OP CHECK NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007091000113 20070910 00113 EU 2007 9 10 2007UALA03477 1 20070829 A 3250 SERVO VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG STEERING FAULTY A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 488UA 1680 ACFT RETURNED TO GATE DUE TO EXCESSIVE PULLING TO THE LEFT DURING TAXI. FOUND NOSE GEAR STEERING VALVE FAULT, REPLAC ED NOSE GEAR STEERING VALVE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007090600003 20070906 00003 NM 2007 9 6 TAMF20070016S 1 20070822 A 5330 SKIN BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE BS 456 S31-32R CORRODED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 768QT 23803 DURING INSPECTION OF (C2) CHECK WAS FOUND CORROSION OVER REPAIR DOUBLER AT SKIN STA 456, STR 31-32 -RT. THE DOUBLER NE EDS TO BE REPLACED. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-046 AND SRM 53-00-01 REPAIR 14.THIS REPAIR CONSTITUTES A M AJOR REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2007092000165 20070920 00165 NM 2007 9 20 2007UALA03612 1 20070906 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 502UA 24623 EMERGENCY LIGHT MISSING AT SEAT 15C. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092500178 20070925 00178 CE 2007 9 25 GLBA20060991 1 20070827 A 5311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 177 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 245GL UE245 FRAME CRACKED AT FS 177.35 APPROXIMATELY 1 INCH AT CUTOUT FOR STRINGER 9R. MAINTENANCE REPAIRED CRACK AT STRINGER RELIE F HOLE 9R AT F.S. 177.35 IAW SRM 51-70. REPAIR APPROXIMATELY 5.5 INCH BY 2.5 INCH. 2024 T3, .080. RII COMPLIED WITH IAW TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2007092500025 20070925 00025 NE 2007 9 25 QXEA200701445 2 20070921 A 7200 3038400 ENGINE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 2 MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 379PH 20349 658 530 PCEAG0054 PDX FLIGHT NR 2139 CLIMBING THROUGH ABOUT 14000', RECEIVED A MASTER WARNING NR 2 OIL PRESSURE LIGHT, OIL PRESSURE FLUCTU ATING ERRATICALLY ABOVE AND BELOW 55 PSI. EVENTUALLY WAS STEADILY BELOW 55 PSI. SHUTDOWN NR 1 AS PER CHECKLIST, INITIA LLY LEFT ENGINE IN START FEATHER AS PER CHECKLIST. THEN DROPPED BELOW 55 PSI AND COMPLETELY SHUTDOWN ENGINE NR 2 SPU AU X POWER CAUTION LIGHT DID NOT ILLUMINATE, EMERGENCY CHECKLIST SAYS IT SHOULD. REPLACED NR 2 ENGINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007092600176 20070926 00176 NM 2007 9 26 2007UALA03710 1 20070913 A 2612 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FIRE HANDLE BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 107UA 26900 LIGHT BULB NR 1 ENGINE FIRE HANDLE BURN OUT. 10-9-07 REPLACED LAMPS IN NR 1 ENG FIRE HANDLE. TESTS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700132 20070907 00132 NM 2007 9 7 2007UALA03432 1 20070827 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 52RH INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY LIGHT ROW 52 RIGHT INOP. RELAMPED EMERGENCY LIGHT. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007091700065 20070917 00065 SO 2007 9 17 N93A28082007A 1 20070828 A 5533 1159B2156225 ANGLE GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU VERTICAL STAB CRACKED E N93A K NONE O OTHER IN INSP/MAINT 1 SO 13 495QS 1295 DURING 5000 LANDING INSPECTION FOUND 793 BULKHEAD VERTICAL STAB CAP ANGLE CRACKED. 2 L 7 2 4F 4 F RT A12EA E25NE 2007092500368 20070925 00368 NM 2007 9 25 2007UALA03657 1 20070910 A 3230 TRUCK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MLG FAILED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 503UA 24624 RTFL DUE TO LANDING GEAR RETRACTION FAILURE. 10-11-07 ACTUATOR DID NOT EXTEND WHEN HYDRAULIC LINES MOVED. BLOCK 25 CALLS FOR ACTUATOR REPLACEMENT. REPLACED MLG TRUCK POSITIONER ACTUATOR ASSEMBLY. AUTO SPEED BRAKE EICAS MESSAGE WAS D ISPLAYED WHEN GEAR WAS SELECTED TO DOWN. SUSPECT POSSIBLE TILT PRESSURE SWITCH PROBLEM. AUTO SPEED BRAKE CONTROL SYSTE M FAILED WITH HANDLE IN ARMED POSITION AND REVIEW OF AMIS SHOWS LOTS OF HISTORY AND DUPLICATE PARTS REPLACED. FOUND RH TRUCK POSITION ACTUATOR PARTIALLY JAMMED NOT ALLOWING TRUCK TO FULL POSITION AND ALLOW PROXIMITY SWITCH FOR AUTO SPEED BRAKES TO FUNCTION PROPERLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007100200014 20071002 00014 NM 2007 10 2 AMTA200700413 1 20070903 A 2432 CHARGER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE BATTERY MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 518AT 27974 EICAS MSG APU BAT CHARGER DISPLAYED WITH APU DISCH LGT EXTING. T/S IAW FIN 24-31-00, BLOCKS 1 AND 2, SYSTEM IS OK. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007092800183 20070928 00183 NM 2007 9 28 2007UALA03793 1 20070919 A 5754 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 SLAT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 NR 1 SLAT L/E LOWER SURFACE JUST INBOARD OF SLAT ACTUATOR SKIN AND RIVET HEAD CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRI CATED AND INSTALLED DOUBLER REPAIR TO EXTERIOR LOWER SKIN. 2 L 7 2 4F 4 F RT A16WE E21EU 2007100200111 20071002 00111 NM 2007 10 2 WRLA2007090 1 20070920 A 2497 CONNECTOR DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE CABIN FAILED A WRLA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 278WA 48746 FLT 100 KIAH/FNLU ELECTRICAL ODOR/SMELL EMANATING FROM SEATS 25A-C DURING CRUISE. POWER PLUG SUPPLY PULLED C/B TO AFFEC TED ZONES. 10-18-07 R & R 26A-C SEAT CONTROL BOX, REPAIRED DAL NR 68 & NR 14 REF WOA WO D10106. 2 L 7 3 4F 4 F RT A22WE E24NE 2007100500116 20071005 00116 NM 2007 10 5 2007UALA03972 1 20070928 A 2750 TRANSMITTER BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU TE FLAPS MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 903UA 25003 DURING TROUBLESHOOTING FOR FLAP PROBLEMS, FLAPS CONSISTENTLY STOPPED BETWEEN 1 & 2 DETENTS FOR LENGTHY PERIODS OF TIME & THEN WOULD START AGAIN WITH NO FURTHER INPUTS (BOTH EXTENDING & RETRACTING). REPLACED RT FLAP POSITION TRANSMITTER AND ADJUSTED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007102300191 20071023 00191 WP 2007 10 23 AMTA200700506 1 20071015 A 2720 4031800902 COMPUTER LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211535E4 54555 NE NR 2 UNSERVICEABLE A AMTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 162AT 1220 RUDDER HYDR LIMITER ANNUNCIATION LIGHT ON. RUDDER LIMITER PANEL HYDR PUSH LT OFF. REMOVED AND REPLACED NR 2, CADC IAW MM 34-14-01, OPS CHECK GOOD. (K) 2 L 7 3 4F 4 F A23WE E12EU 2007101600037 20071016 00037 CE 2007 10 16 AMWA0828013B 1 20071002 A 5311 12943003132 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FS 213.25 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 176YV 26646 UE176 REPAIRED LT AND RT FUSELAGE FRAME DAMAGED BY FRICTION CHAFING AT FS 213.25. 2 L 7 2 4T 4 T RT A24CE E26NE 2007102600154 20071026 00154 NM 2007 10 26 2007UALA04249 1 20071015 A 2751 INDICATOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU TE FLAPS MALFUNCTIONED A UALA O OTHER N FALSE WARNING AP APPROACH 1 WP 29 378UA 24653 UPON SELECTING FLAPS 5 - FLAP INDICATOR NEEDLES SPLIT, BUT NEVER GOT LOCK OUT. CREW USED ALT FLAP EXTENSION. 2 L 7 2 4F 4 F RT A16WE E21EU 2007101100213 20071011 00213 NM 2007 10 11 ASMF200709010 1 20070928 A 2720 59140665563 ACTUATOR DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE RUDDER DAMAGED W ASMF O OTHER F FLT CONT AFFECTED CR CRUISE 1 SW 23 169PL 50221 4120 53175 CAPTAIN REPORTED THAT IT WAS NECESSARY TO ADJUST THE RUDDER TRIM COMPENSATOR 7 UNITS TO THE RIGHT IN FLIGHT. AT PLATFOR M, MAINTENANCE PERSONNEL REPLACED THE RUDDER HYDRAULIC POWER PACKAGE AND THE YAW DAMPER ACTUATOR IAW MM 27-20-04 AND 22- 13-01 RESPECTIVELY, TESTED CORRECT. DURING OVERNIGHT CHECK, THE RUDDER TRIM LOAD FEEL SPRING WAS REPLACED IAW MM 27-20-0 7 AND ADJUSTMENT TEST WAS PERFORMED IAW MM 27-20-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007101600038 20071016 00038 CE 2007 10 16 AMWA87659BC 1 20070925 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER DISCHARGED A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 166YV 2300 148 UE166 BATTERY CHARGE ANNUNCIATOR ILLUMINATED DURING FLIGHT. AIRCRAFT CONTINUED TO DESTINATION WITHOUT INCIDENT. BATTERY WAS RE PLACED. THIS TYPE ANNNUNCIATOR WRITEUP IS CONSIDERED A NUISANCE AND DISTRACTION TO THE CREW. 2 L 7 2 4T 4 T RT A24CE E26NE 2007102300151 20071023 00151 CE 2007 10 23 DXTA200702539 1 20071014 A 2130 UNKNOWN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE CABIN PRESSURE UNKNOWN E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 375QS 5600375 AIRPLANE WILL NOT PRESSURIZE. REPLACED PNEUMATIC RELAY WITH OVERHAULED UNIT I.A.W. CESSNA 560 M.M. 21-32-02. 2 L 7 2 4F 4 F RT A22CE E25EA 2007110100125 20071101 00125 NM 2007 11 1 2007UALA04329 1 20071020 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 FORWARD GALLEY DOOR (1R) 4TH STOP FITTING FROM TOP ON AFT FRAME HAS CRACK AT CUTOUT. FABRICATED AND INSTALLED FRAME REP AIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110100168 20071101 00168 EU 2007 11 1 COEA0713821 1 20070827 A 5310 S53673000221 CREASE BEAM AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE DAMAGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. FOUND TOOLING DAMAGE 3 PLACES ON CREASE BEAM WEB. FABRICATED REPLACEMENT CREASE BEAM WEB. W O NR 72242, NR 200063. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007102300144 20071023 00144 NM 2007 10 23 ASMF200710002 1 20071010 A 3222 5920602 STRUT DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NLG LEAKING W ASMF O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 23 160PL 31466 31466 49763 AIRCRAFT AIR TURNED BACK DUE NOSE LANDING GEAR DID NOT RETRACT AND THE CORRESPONDING RED LIGHT TURNED ON. DURING MAINTEN ANCE CHECK, THE NOSE LANDING GEAR STRUT WAS DETECTED COMPRESSED, SO IT WAS SERVICED IAW MM 32-21-02 AND THE NOSE LANDING GEAR PROXIMITY SENSOR WAS CHECKED IAW MM 32-60-05, ALL CORRECT. AS A PRECAUTIONARY ACTION, A TEST FLIGHT WAS PERFORMED TO CHECK THE MECHANISM OPERATING 3 LANDING GEAR CYCLES, ALL CORRECT. AFTER THAT, THE NOSE LANDING GEAR STRUT WAS FOUND IN SERVICEABLE CONDITION IAW MM 32-21-02, PAGE 307. THE OVERWEIGHT LANDING INSPECTION WAS NOT NECESSARY DUE TO THE AIRCR AFT LANDED WITH 132,000 POUNDS AND THE MAXIMUM LANDING WEIGHT IS 139,500 POUNDS. DURING OVERNIGHT CHECK, THE NOSE LANDIN 2 L 7 2 4F 4 F RT A6WE E9NE 2007102600105 20071026 00105 2007 10 26 ANCF200700024 4 20071018 A 3442 WARNING LIGHT BOEING 767 767283ER 1385149 NM PWA 4056 PW4056 NE WX RADAR FALSE ACTIVATION W ANCF A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 23 728CG 24728 WEATHER FAIL DISPLAYED ON HSI, AFTER WXR TEST WEATHER FAIL DISAPPEARS. IAW FIM 34-43-00. FIGURE 103, BLOCKS 1,2 AND 3 T HE WXR BITE PROCEDURE WAS ACCOMPLISHED SATISFACTORY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110500170 20071105 00170 NE 2007 11 5 HNAA0700254 2 20071027 A 7314 311709401 PUMP DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE FUEL SYS FAILED A HNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 07 812EX 312 121354 THE NR 2 ENGINE FAILED AFTER TAKEOFF. AUTOFEATHER WORKED AND TORQUE WENT TO ZERO. FLT CREW COMPLETED NECESSARY CHECK L IST & RETURNED TO THE FIELD. THE CAPTAIN INSPECTED THE NUMBER TWO NACELLE FOR FLUID, NONE WAS FOUND. THE PROP ROTATES WITH OUT BINDING. MX ABLE TO START THE NR 2 ENGINE, HOWEVER FUEL FLOW HUNG UP DURING START SEQUENCE. INSPECTED ENGINE INLET AND EXHAUST FOR DEFECTS, NONE WERE FOUND. THE ENGINE CONDITION PANEL WAS CHECKED FOR FLAGS NONE WERE NOTED. REMO VED AND REPLACED THE HMU AND FUEL PUMP ON THE NR 2 ENGINE. IAW WORK CARD 73-20-01R. RIGGED THE NUMBER ONE AND NR 2 ENGI NE IAW 76-00-01Q. GROUND RAN AIRCRAFT, OPS CHECK GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2007110800064 20071108 00064 CE 2007 11 8 DXTA200702563 1 20071023 A 2750 APTE233A1750300 TRANSDUCER BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE TE FLAPS INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 132QS 1208 RK427 ON CLIMB OUT AFTER FLAP RETRACTION, ACCELERATING THROUGH 160 KIS, (RDR BST FAIL) YELLOW CAUTION LIGHT ILLUMINATED ALONG WITH DISENGAGEMENT OF THE YAW DAMPER. REMOVED NR 1 ENGINE TRANSDUCER PN APTE233A-1750300A SN 7064-16-116, 7064-16-129 AN D NR 2 ENGINE TRANSDUCER S/N 7133-9-539 AND 6932-10-33. INSTALLED NEW TRANSDUCER'S ON NR 1 ENGINE S/N 7133-9-549 AND 711 1-15-64 AND NR 2 ENGINE SN 7180-5-332 AND 7133-9-532. SYSTEM OP'S CHECKS GOOD. ALL WORK PERFORMED IAW MM CHP 27-21. 2 H 7 2 4F 4 F RT A16SW E25EA 2007103100115 20071031 00115 NM 2007 10 31 2007UALA04372 1 20071024 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHT INOP: DOOR 2R SLIDE ILLUM. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110800018 20071108 00018 EU 2007 11 8 2007UALA04415 1 20071028 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 451UA 865 SEAT 26C EMERGENCY LIGHT INOP: MISSING LENS & LIGHT ASSY DAMAGED. REPLACED LIGHT ASSY, OPS CHECK OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112000037 20071120 00037 NE 2007 11 20 TRBA2007099 2 20071112 A 7200 PW127TM ENGINE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE LEFT MAKING METAL A TRBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 29 410AT 1936 410 LT ENGINE OIL PRESURRE DROP WITH ASSOCIATED WARNINGS. REMOVED AND REPLACED LT ENGINE S/N 127056 AS PER WORK CARD 055006 -CS-20000-001. 2 H 7 2 4T 4 T RT A53EU E20NE 2007112600140 20071126 00140 SO 2007 11 26 CHQA200700078 1 20071111 A 3000 8166248 THERMOSTAT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL ANTI ICE SYSTEM FAILED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 833RP 8308 802 145687 CAE311948 CVG TO XNA - DURING CLIMB-OUT, SHORTLY AFTER ANTI-ICE HAD TURNED OFF FROM EXITING ICING CONDITIONS, CREW RECEIVED A "BLE ED 1 OVERTEMP" MESSAGE. THE CREW RAN THROUGH THE APPROPRIATE QRH CHECKLISTS AND IT WAS DECIDED TO RETURN TO CVG. THE A IRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE FAULT TO THE BLEED AIR THERMOSTAT AND REPLACED IT. THE BLE ED SYSTEM OPS CHECKED GOOD AFTER THE BLEED AIR THERMOSTAT WAS REPLACED. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007112600157 20071126 00157 NM 2007 11 26 KNNA200700061 1 20071113 A 5754 114A71213 SLAT TRACK BOEING BOEING 737 737232 1384475 NM PWA JT8 JT8D15 52051 NE NR 2 SLAT JAMMED A KNNA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 25 326DL 56515 681 BN68 231098 AFTER TAKEOFF, LT LEADING EDGE SLAT DID NOT RETRACT, AIRCRAFT DIVERTED FROM KGNV TO KJAX. PILOT DECLARED IN FLIGHT EMER GENCY FOR FLAPS UP LANDING. AFTER REMOVAL AND INSPECTION, FOUND OUTBD AUXILIARY TRACK JAMMED, WHICH CAUSED THE SLAT TO SHIFT AND THE TRAILING EDGE TO REACH THE UPPER STOP. THUS CAUSING THE DAMAGE TO THE STAT ASSY. 2 L 7 2 4F 4 F RT A16WE E2EA 2007112100127 20071121 00127 NM 2007 11 21 2007UALA04651 1 20071111 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 DOOR 2L AFT EEL EXIT SIGN INOPERATIVE. SECURED LOOSE CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007120400111 20071204 00111 NM 2007 12 4 AMTA200700570 1 20071029 A 2613 LOGIC CARD BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE OVERHEAT DETECT MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 11 560TZ 33525 RT STRUT O/H DET 2 DISPLAYED ON EICAS. IAW TECH SERV MEG CK AS REQUIRED WIRE CK GOOD REMOVED S10203 AND S10204 IAW MM 2 6-12-01-4 S10205 IS SWAPPED FIRE OVHT/LOGICIST CARD 5 WITH SPARE SYS, CK NORMAL. OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007120500033 20071205 00033 CE 2007 12 5 DXTA200702622 1 20071120 A 2750 FLAP SYSTEM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS MALFUNCTIONED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED DE DESCENT 1 GL 07 905QS 7500105 FLAPS FAILED 5 DEGREES, SLATS EXTENDED AT 16000 FT. APPLIED POWER. FOUND NO FLAP FAIL INDICATON OR BITE INDICATIONS ON CONTROL BOX. RAN FLAPS THROUGH EACH DETENT AND FULL MOVEMENT. NO FLAP FAIL OR BITE INDICATIONS APPEARED. TROUBLESHOOTIN G DONE IAW CE-750 MM 27-50-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007120500003 20071205 00003 NM 2007 12 5 AMTA200700589 1 20071112 A 3150 WARNING MESSAGE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE EICAS FALSE ACTIVATION A AMTA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 514AT 27971 CAPTAIN PITOT EICAS MSG. PERFORMED FIM 30-31-00, FIG 103. OPS CHECK, OK (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010700264 20080107 00264 NM 2008 1 7 2007UALA05258 1 20071222 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EEL'S INOP AT SEATS 4A (AFT POS), 33L & 53L. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010700304 20080107 00304 NM 2008 1 7 2007UALA05286 1 20071226 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE 3RD FROM FWD LIGHT ASSY. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007122800105 20071228 00105 NM 2007 12 28 2007UALA05111 1 20071214 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 950-990 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 AFT GALLEY DOOR WAY, FLOOR INNER CREASE BEAM CORRODED ON UPPER SURFACE, BS 950-990 RBL 46". MAJOR REPAIR ACCOMPLISHED A T AAR@IND. 2 L 7 2 4F 4 F RT A16WE E2GL 2008010800362 20080108 00362 CE 2008 1 8 GLBA20061033 1 20071206 A 5320 1144300027179 ANGLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FUSELAGE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 254GL UE254 LT HEAVY ANGLE CRACKED AT FUEL BEND RADIUS AT FS 288.0. LENGTH APPROXIMATELY 1.5 INCHES. MAINTENANCE REPAIRED LT HEAVY ANGLE AT FS 288 IAW SRM 53-90. REPAIR AREA APPROXIMATELY 13.5 INCHES. RII INSPECTION COMPLIED IAW GLA TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2008010900011 20080109 00011 NM 2008 1 9 2007UALA05207 1 20071220 A 3397 WIRE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 827UA 1022 AFT PAX CABIN EMERGENCY LIGHTS ILLUMINATE AFTER ENGINE START. NUMEROUS WIRES FOR EPSU SYSTEM FOUND CHAFED AND OPEN. NO STRANDS BROKEN - INSULATION WORN TO BARE WIRE. UNKNOWN ROOT CAUSE. REPAIRED ALL WIRES FOUND DAMAGED, SYSTEM FUNCTIONS NORMALLY DURING TEST AND ENGINE STARTS. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011000157 20080110 00157 2008 1 10 2007UALA05338 4 20071227 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R1 DOOR LOW PRESSURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 468UA 1363 DOOR SLIDE 1R PRESSURE LOW. SERVICED SLIDE RES. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010400163 20080104 00163 NM 2008 1 4 AMTA200700633 1 20071125 A 2410 HEAT EXCHANGER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE UNKNOWN A AMTA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 GL 11 519AT 27975 "GEN DRIVE LGT" ILLUMINATED APPROX 5 MINUTES LATER. DISCONNECTED RT GEN DRIVE BY FOLLOWING QRH CHECKLIST (GENERATOR DRI VE). ADDITIONAL ITEM PART REMOVED FROM ITEM NR 24101320. REMOVED AND REPLACED EXCHANGER- IDG AIR/OIL HEAT IAW AMM 24-11 -04-4. LEAK CHECK OK. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010900384 20080109 00384 CE 2008 1 9 DXTA200702700 1 20071220 A 3260 OL327LSV BULB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE MLG INDICATOR BURNED OUT E DXTA O OTHER P NO WARNING INDICATION LD LANDING 1 GL 07 120QS 1458 RK409 LT MAIN GEAR DOWN AND LOCK INDICATION INOPERATIVE. REPLACED LT MAIN LANDING GEAR DOWN INDICATION BULB. OPS CHECK GOOD I AW HAWKER 400XP MM CH 32-60-00. 2 H 7 2 4F 4 F RT A16SW E25EA 2008012200058 20080122 00058 EA 2008 1 22 A6WA200740694 1 20071210 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 432AW 7257 CRACK FOUND ON INTERCOSTAL FS 484, LBL 27 AND LBL 36, WL 72.00. INTERCOSTAL AT FS 484, LBL 27 AND LBL 36 AT WL 72.00. REPAIRED IAW REO 601R-53-41-059 REV A AND SRM 51-24-16, 51-21-16 AND SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200167 20080122 00167 CE 2008 1 22 COEA0701756 1 20071227 A 3244 02534900 TIRE CESSNA 208 208B 2073701 CE PWA PT6 PT6A45 52043 EA RT MLG FAILED A COEA O OTHER E VIBRATION/BUFFET LD LANDING 1 AL 03 756FX 208B0532 AFTER LANDING, DURING ROLLOUT PILOT OBSERVED A STRONG VIBRATION THAT SUBSIDED AS THE AC SLOWED. GROUND PERSONAL CONFIRM ED THE RT MAIN TIRE WAS FLAT. REPLACED RT MAIN TIRE AND WHEEL ASSY. (K) 1 H 7 1 3T 4 T A37CE E4EA 2008012200064 20080122 00064 GL 2008 1 22 EOYA20080001 1 20071212 A 5330 GD234200011 SKIN BOMBDR BD700 BD7001A11 1390022 GL RROYCE BR700 BR700710A110 NE BS 101 DENTED E E0YA O OTHER O OTHER LD LANDING 1 SO 35 50DS 1065 1065 9140 DURING LANDING APPROACH, AIRCRAFT STRUCK SECURITY FENCE, RESULTING IN DAMAGE TO FUSELAGE SKIN PANEL ON THE LT SIDE OF TH E FUSELAGE. THE LOCATION OF THE DAMAGE IS AT FUSELAGE STATION 101.18, WATER LINE 73.50. DAMAGE SUSTAINED TO SKIN PANEL I S A DENT WITH GOUGES APPROX 2 INCHES LONG. 2 L 7 2 4F 4 F RT T00003NY E00057EN 2008021500043 20080215 00043 NM 2008 2 15 2007UALA03916 1 20070925 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 302UA 23643 FIRST CLASS CABIN EMERGENCY LIGHTS INOPERATIVE. RELAMPED EMERGENCY LIGHTS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022500107 20080225 00107 2008 2 25 2007UALA03929 4 20070926 A 2565 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU GALLEY DOOR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 FWD GALLEY EVACUATION SLIDE GAUGE NOT VISIBLE DUE TO MIGRATION. REMOVED SLIDE AND ADJUSTED SLIDE IN SLIDE COMPARTMENT A ND GAUGE TO BE VISIBLE IN WINDOW. 2 L 7 2 4F 4 F RT A16WE E21EU 2008041000190 20080410 00190 CE 2008 4 10 DELA200720008 1 20071005 A 2840 INDICATION SYS LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP LOW FUEL FALSE INDICATION E DELA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 773DL 174 LOW FUEL LIGHT ILLUMINATED WITH 4000 LBS TOTAL FUEL ON AIRPLANE AND 1200 LBS FUEL IN THE WINGS. FUEL READER GAUGE INDICA TED 400 LBS OF FUEL ON RT WING. LATER ON WENT BACK TO INDICATE 1200 LBS ON THE WINGS. TAKE OF (SIC) WITH 4000 LBS TOTAL LANDING WEIGHT WAS 13,800. MX ACTIONS: CLEANED F.Q. C/B CONTACTS, SUMPED FUEL TANKS (NO CONTAMINATION FOUND), PERFORMED GROUND ENGINE RUN WHILE OBSERVING CKPT INDICATIONS. OPS NML. (MAX LANDING WEIGHT 14300). 2 L 7 2 4F 4 F A10CE E6WE 20080811 NE 2008 8 11 M7K2008F00145 2 20070919 A 7240 0292377910 COMBUSTION LINER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ENGINE CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 816MH 4588 4038 23237 DURING ROUTINE MONITORING OF EXISTING CRACKS WHICH HAD, TO THIS TIME, REMAINED WITHIN MM LIMITATIONS FOR A REDUCED INTER VAL INSP, NO TO EXCEED 150 FLIGHT HOURS. PARALLEL CRACKS HAVE INTERSECTED WITH THE POSSIBILITY FOR A PIECE TO BREAK FRE E AND BE INGESTED BY THE TURBINES DOWN STREAM OF THE COMBUSTION CHAMBER. THE ENG HAS BEEN REJECTED AND A SERVICEABLE EN GINE REPLACEMENT INSTALLED INTO THE AC. THIS DEFECT, FOUND ONLY IN THE LASER DRILLED COMBUSTION LINER SWIRLPLATE AND NO T IN THE OLDER STYLE PLASMA DRILLED SWIRLPLATES HAS CAUSED THE REJECTION OF ALMOST EVERY ENGINE AT OR BEFORE 1500 HOURS OF SERVICE FOR LASER CUT SWIRLPLATES. MFG IS AWARE OF THE PROBLEM BUT REFUSES TO RETURN TO THE PLASMA DRILL MFG PROCESS 1 G 7 2 3U 3 U H9EU E00054EN 2007012300050 20070123 00050 WP 2007 1 23 07FDEA00117 1 20070116 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1781 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 LOWER EXT FUSELAGE, FOUND DEEP DENT 3" BY 1,5" MAX DEPTH .065" AT STA 1781 FROM L 44 LT TO L 45 LT. TRIMMED OUT DAMAGED SKIN, REPAIRED IAW SRM 53-20-00 VOL1 FIG 6 SHT 2A-4. PERFORMED NDT INSPECTION NO CRACK FOUND, FABRICATED PARTS IAW DET AIL PARTS TRAVELER I025223/N00223 IAW SRM 53-20-00 VOL1 FIG 6 SHT 3-4. 2 L 7 3 4F A22WE 2007032900078 20070329 00078 WP 2007 3 29 07FDEA00914 1 20070315 A 5730 SKIN DOUG DC10 DC1010 3022110 WP ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 RIGHT WING L/EDGE FWD OF PRESSURE "REFUEL" PANEL AT XORS 510 TO XORS 538 DENTED 2 AREAS. REMOVED, REPLACED, FABBED AND INSTALLED DOUBLER IAW DC10 SRM 57-00-01 FIG 4 SHEET 2 VOL I . ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL II. 2 L 7 3 4F A22WE 2007073100168 20070731 00168 NM 2007 7 31 SWAA073599 1 20070720 A 5311 6546557 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED RON, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007071300115 20070713 00115 WP 2007 7 13 07FDEA02340 1 20070629 A 3610 PRESSURE SWITCH DOUG MD10 MD1010F 3022112 WP LT WING MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 360FE 46636 PDIS: ENROUTE AFW-LAX WITHIN 10 SECONDS AFTER TURNING WING ANTI-ICE ON, RECEIVED LEVEL 3 AIR MANIFOLD 1 FAILURE. DIVERT TO BOI. CHECKED MANIFOLD FAIL INDICATION PANEL IN CAC FOUND PRESS SWITCH FAULT BALL SET FOR LEFT WING. RESET FAULT IN DICATION PANEL. PERFORMED DECAY CHECK ON NR 1 MANIFOLD PER MM. TEST OK. INSPECTED SLATS FOR LEAKS WITH PRESSURE APPLIE D. FOUND LT WING ANTI ICE VLV O/B CLAMP LEAKING. REPOSITIONED CLAMP AND RESECURED. LEAK CK NORMAL. MEL WING ANTI ICE AS PRECAUTION. LAX/29 REACTIVATED WAI. FUNCTIONAL CHECK NORMAL. 2 L 7 3 4F RT A22WE 2007121400219 20071214 00219 NM 2007 12 14 F3LA200700373 1 20071212 A 3350 32146210 EPSU AIRBUS A319 A319111 3930336 NM EMERGENCY LIGHTS INOPERATIVE A F3LA O OTHER O OTHER NR NOT REPORTED 1 NM 03 939FR 2448 FLIGHT CREW REPORTED AFT EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED POWER SUPPLY UNIT AFT 13WL IAW AMM 33-51-38-PB401. PERFORMED OPS CHECK. CHECKED GOOD. 2 L 7 2 4F RT A28NM 2007053100019 20070531 00019 WP 2007 5 31 ASAA0781721 1 20070530 A 5320 993053867 WEB DOUG DC9 DC983 3022083 WP BS 218-222 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 PASSENGER CABIN FLOOR WEB IS CRACKED. CUT OUT DAMAGED AREA OF WEB, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM 51-70-4 FIG 2. 2 L 7 2 4F RT A6WE 2007082300097 20070823 00097 EU 2007 8 23 07FDEA02936 1 20070816 A 5347 A53612518200 SEAT TRACK AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION ON SEAT TRACK C14-15A. REPAIR PERFORMED IAW SRM 53-12-16 FIG 201. 2 L 7 2 4F RT A35EU 2007082200162 20070822 00162 NM 2007 8 22 AALA20071432 1 20070807 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 187AN 32381 LAX - EMERGENCY EXIT SIGN LIGHT AT LEFT AFT OVERWING INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY EXIT SIGN LIGHT AT LE FT AFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2007101700184 20071017 00184 EU 2007 10 17 07FDEA04559 1 20071010 A 5753 A579600500000 RIB AIRBUS 300 A300F4605R 3930327 EU TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 DURING COMPLIANCE WITH EO NR 6-5750-7-5000 P2, RIB 7 FLANGE WAS FOUND TO BE CRACKED COMPLIANCE WITH EO NR 6-5750-7-5000 P4. REPLACEMENT OF DAMAGED RIB 7. 2 L 7 2 4F RT A35EU 2007091400064 20070914 00064 EU 2007 9 14 07FDEA03455 1 20070907 A 5313 A53974235200 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 FOUND CORROSION ON STRINGER 50, BETWEEN FRAME 55/58-59 LHS, OUT OF LIMIT. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-1 0-14/FIG 201. 2 L 7 2 4F RT A35EU 2007081500039 20070815 00039 NM 2007 8 15 NWAA072756313 1 20070801 A 2612 FIRE DETECTOR BOEING 747 747451 1384940 NM APU BAY MALFUNCTIONED A NWAA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 01 673US 30268 DURING FLIGHT HAD A FALSE EICAS, APU FIRE WARNING. NO OTHER INDICATIONS NOTICED. FLIGHT CONTINUED ON AND LANDING WAS U NEVENTFUL. MAINTENANCE REMOVED AND REPLACED BOTH A&B LOOP DETECTORS AND LUGS ON THE ACCESS DOOR. OPERATIONAL CHECKED G OOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008030500036 20080305 00036 EA 2008 3 5 QXEA200801995 1 20071215 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 676-680 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - C4 CHECK - LEFT CENTER SEAT TRACK HAS CORROSION AT STATION 676 TO 680. BLENDED OUT CORROSION FROM SEAT TRACK, INS PECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE TREATMENT TO BLENDED AREAS. 2 L 7 2 4F RT A21EA 2007030900184 20070309 00184 2007 3 9 DXTA200701968 4 20070226 A 2210 4006719903 MOTOR CESSNA 750 750 2076810 CE AILERONS INOPERATIVE E DXTA O OTHER S AFFECT SYSTEMS CR CRUISE 1 GL 07 978QS 5201 7500187 AIRCRAFT CONTINUOUSLY DUTCH ROLLS, ALL ALTITUDES AND SPEEDS- ONE TO TWO DEGREES LEFT & RIGHT. SWAPPED YAW DAMPERS ON UPP ER RUDDER- STILL NO IMPROVEMENT. REMOVED AND REPLACED AILERON SERVO MOTOR IAW CE750 MM CH 22-10-01. GROUND CHECKED GOOD . 2 L 7 2 4J RT T00007WI 2007071300378 20070713 00378 NM 2007 7 13 F3LA200700168 1 20070628 A 5321 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR PANEL 151ZG DELAMINATED AT RT SIDE OF PANEL AT CARGO D OOR OPENING. REPLACED FLOOR PANEL 151ZG IAW AMM 53-42-14-000-001. 2 L 7 2 4F RT A28NM 2007041300135 20070413 00135 NM 2007 4 13 F3LA200700066 1 20070328 A 5340 FITTING AIRBUS A319 A319111 3930336 NM LAVATORY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED AFT LT LAVATORY, AFT OTBD MOUNTING HOLES IN LAV WALL WORN AND CORRODED. REMOVED AND CLEANED FITTING. REINSTALLED FITTING WITH NEW HARDWARE IAW CMM 25-43-51, PAGES 303, 618 AND 740. 2 L 7 2 4F RT A28NM 2007102200058 20071022 00058 NM 2007 10 22 2007UALA04192 1 20071012 A 3350 LAMP BOEING 747 747422 1384935 NM EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY EXIT LIGHT INOP AT UPPER DECK FWD CEILING DOOR, UPPER DECK CEILING AT ROW 17 AND AT DOOR 5L CEILING ENTRY. 11-01-07 RELAMPED. 2 L 7 4 4F RT A20WE 2007083100042 20070831 00042 WP 2007 8 31 070154 1 20070822 A 3260 TARGET DOUG DC9 DC983 3022083 WP RT MLG DOOR LOOSE A WX0A A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 19 878GA 53487 FLIGHT 428 FROM LAS VEGAS REPORTED GEAR DOOR OPEN LIGHT ILLUMINATED WITH GEAR HANDLE UP. THE LIGHT EXTINGUISHED WITH GE AR HANDLE DOWN AND THE AIRCRAFT RETURN TO LAS VEGAS. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED THE AIRCRAFT AND FOUND THE RIGHT GEAR DOOR TARGET LOOSE. THE TARGET WAS SECURED AND ALIGNED IAW M/M 32-43-02. OPERATION CHECK WAS NORMAL AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2007092700393 20070927 00393 EU 2007 9 27 07FDEA04142 1 20070921 A 5313 A53973678 STRINGER SPLICE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 803FD 378 HEAVY CORROSION ON STRINGER SPLICE 32 RT, BETWEEN FRAME 64-65. REPLACEMENT OF STRINGER SPLICE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007031600060 20070316 00060 NM 2007 3 16 07FDEA00833 1 20070314 A 5312 BULKHEAD BOEING 727 727225 1384077 NM BS 720D CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 FOUND FWD CARGO STA 720D LWR BULKHEAD BEAM HAS CORROSION AT LBL25. REMOVED AND REPLACED ANGLE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2007071200102 20070712 00102 NM 2007 7 12 F3LA200700153 1 20070627 A 5320 TRANSITION PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED HOLES IN AFT CARGO COMPARTMENT TRANSITION PANEL 152BF. REPAIRED HOLES IN TRANSITI ON PANEL 152BF IAW SRM 53-02-00, FIG 204. 2 L 7 2 4F RT A28NM 2007031500047 20070315 00047 NM 2007 3 15 SWAA071319 1 20070311 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM BS 758 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 758, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2007041200115 20070412 00115 SO 2007 4 12 RAIA00703067 1 20070325 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 845HK 14500842 POST FLT NR 8012 - ORD - FLOOR STRIP EMERGENCY LIGHT LOOSE. MAINTENANCE RESECURED EMERGENCY STRIP LIGHTING AT GALLEY, O PS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007082300154 20070823 00154 NM 2007 8 23 HALA0700345 1 20070814 A 4920 ENGINE BOEING 767 76733A 1385209 NM APU OIL CONSUMPTION A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM, APU FAULT DID NOT START AFTER LANDING DUE TO OIL QTY 0. ADDED 3 PINTS OF OIL. NO LEAKS NOTED . FOUND "NO LIGHT OFF" FAULT ON ECU. REPLACED IGNITER PLUG PER FIM 49-11-00 AND M/M 74-21-2. OPS CK LEAK CK GOOD. 2 L 7 2 4F RT A1NM 2007110900229 20071109 00229 EU 2007 11 9 F3LA200700309 1 20071017 A 5321 D5361087600100 FLOOR PANEL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 910FR 5866 1781 DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 222FF CORRODED ON LOWER SURFACE, FWD EDGE. REMOVED AND REPLACED FLO OR PANEL IAW AMM 53-12-12-PB401 AND WORK CARD CP753-12. 2 L 7 2 4F RT A28NM 2007050300318 20070503 00318 NM 2007 5 3 UPS07M49706 1 20070327 A 5320 ROLLER TRAY DOUG MD11 MD11F 3023600 NM BS 1060 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:C FWD CARGO, 02 EA CORROSION FOUND ON ROLLER TRAY TOP SURFACE AT STA 1060, BL 0. CORROSION ON TOP SURFA CE REMOVED PER SRM 51-21-01VOL IIR38. MEASURED THK 0.090", NAT'L REMOVED 0.050" MAT'L REMAIN 0.040" FOUND OUT OF LIMIT PER SRM 53-00 -01 FIG1AR38. ROLLER TRAY REMOVED PER SRM 51-31-01 VOLIIR38. NEW ROLLER TRAY HOLES PICKED UP PER SRM 51 -31-01 AND 51-21-01 VOLIIR38. PAINTED PER SRM 51- 21-01 VOLIIR38. NEW ROLLER TRAY INSTALLED PER SRM 51-31-01VOLIIR38. 2 L 7 3 4F RT A22WE 2007012300104 20070123 00104 NE 2007 1 23 07FDEA00130 2 20070118 A 7200 ENGINE BOEING 727 727200 138407E NM PWA JT8 JT8D17A 52049 NE NR 2 FAILED A FDEA A UNSCHED LANDING R M J PARTIAL RPM/PWR LOSS OVER TEMP WARNING INDICATION CL CLIMB 1 SO 25 280FE 26736 26736 22347 709291 NR 2 ENGINE FAILED DURING CLIMB-OUT AT APPROX 1500 FT ABOVE GROUND. NOTED HIGH EGT (AROUND 780 C), EPR 0, N1 AND N2 WIN DMILLING. OIL QTY 3 GALS ENGINE FAILED WITH A LOUD BANG AND SPARKS REPORTED TRAILING AIRCRAFT BY TOWER. VISUAL INSPEC TION OF ENGINE REVEALED PARTS OF COMPRESSOR BLADES IN TAIL PIPE. TURBINE WHEEL AND C1 FAN BLADES VISUALLY CK OK BUT 2, 3, 4 COMPRESSOR WHEELS ARE BADLY DAMAGED. UNABLE TO TURN FAN BY HAND. WILL REQUIRE NR 2 ENGINE CHANGE. INSPECTION OF INLET DUCT SHOWS NO MISSING VORTEX GENERATORS. THIS WAS A CONTAINED FAILURE, THE ENGINE WAS REMOVED AND REPLACED. 2 L 7 3 4F 4 F RT A3WE E2EA 2007012500206 20070125 00206 NM 2007 1 25 2007UALA00082 1 20070112 A 5330 DOUBLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 STA 600L AT STR 15L PREVIOUS REPAIR DOUBLER-TRIPLER IS DENTED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND REPLACED REPA IR DOUBLER-TRIPLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007012500069 20070125 00069 2007 1 25 RAIA00701008 4 20070105 A 2311 CONTROL MODULE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL RADIOS UNKNOWN A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 823HK 145475 FLT NR 7897-MDT-CAPTAIN AND FO'S RADIO LOCKED UP AND WERE UNABLE TO CHANGE FREQUENCIES. MAINTENANCE REMOVED AND REINSTA LLED THE CMU. RADIOS OPERATED NORMALLY AFTERWARDS. NO OTHER DEFECTS NOTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007021500075 20070215 00075 2007 2 15 2007UALA00304 4 20070203 A 2565 LIFTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GIRT BAR WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 FOUND DOOR 4L AND 4R FWD GIRT BAR LIFTERS HAVE WORN AREAS. WEAR OUT OF LIMITS, REPLACED LIFTER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030600006 20070306 00006 NM 2007 3 6 2007UALA00595 1 20070225 A 2611 SMOKE DETECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CARGO BAY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 536UA 25156 NR 2 AFT CARGO COMPARTMENT SMOKE DETECTOR INOPERATIVE. [SUP 05-08-07] REPLACED AFT CARGO SMOKE DETECTOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007031200028 20070312 00028 SO 2007 3 12 GUUA02100701 1 20070210 A 3350 12021299001 RECEPTACLE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE EMERGENCY LIGHT SHORTED A GUUA K NONE L NO TEST IN INSP/MAINT 1 SO 29 282AS 120226 AT SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT AND RT EMERGENCY LIGHTS INOPERATIVE. REPLACED LT AFT EXTERNAL EMERGENCY LIGHT RECEPTACLE OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 2007031200043 20070312 00043 CE 2007 3 12 EAS21907 1 20070219 A 5610 10138402522 WINDSHIELD BEECH B300 B300B350C CE PWA PT6 PT6A60A 52043 NE COCKPIT BROKEN E E07A O OTHER O OTHER CR CRUISE 1 CE 07 275BT 1993 FL275 AIRCRAFT WAS ENROUTE, AT FL27000 THE RT WINDSHIELD INNER PANE SHATTERED. CREW DESCENDED TO FL18000 AND MAINTAINED CABIN PRESSURE OF 3 PSI. AIRCRAFT RETURNED TO DEPARTURE WITHOUT INCIDENT. 2 L 7 2 4T 4 T RT A24CE E4EA 2007031300173 20070313 00173 EU 2007 3 13 2007UALA00632 1 20070302 A 3697 WIRE HARNESS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE UNSERVICEABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 427UA 512 NR 2 ENG HP VLV FAULT. FOUND DAMAGED CONNECTOR AND BURNED WIRES. [SUP 05-18-07] FOUND THE WIRING HARNESS BACKSHELL C ONNECTOR ON THE HP VALVE WAS STRIPPED. INITIALLY ATTEMPTED TO REPLACE BACKSHELL CONNECTOR, BUT FOUND BURNT WIRES INSIDE CONNECTOR. DETERMINED THAT WIRES WERE NOT REPAIRABLE, SO REPLACED ENTIRE WIRING HARNESS FROM GROUND STUD TO HP VALVE AND FIRE LOOP. PREVIOUS OVER TORQUE OF THE BACKSHELL STRIPPED THE THREADS AND DAMAGED THE WIRES TO THE EXTENT THAT A SHORT OCCURRED AND BURNT THE WIRES. ALSO REPLACED THE HP VALVE AS A PRECAUTION. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022100176 20070221 00176 NM 2007 2 21 2007UALA00262 1 20070131 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY LIGHT ROW 41ABC AND 54ABC INOP. RELAMPED LIGHT, OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007031500127 20070315 00127 NM 2007 3 15 2007UALA00650 1 20070301 A 2611 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SMOKE LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 SMOKE LIGHT FAILED TO ILLUMINATE DURING EQUIPMENT COOLING TEST. ACCOMPLISHED TROUBLESHOOTING PER MM 21-58-00 FIG 116A . FOUND EQUIP COOLING SMOKE DETECTOR LAMP INOPERATIVE, REPLACED LAMP PER MM:21-58-19, DEVICE WORKS FINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007031300158 20070313 00158 NM 2007 3 13 2007UALA00588 1 20070223 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 UPPER DECK LEFT ESCAPE DOOR BATTERY PACK INOP. SWAPPED BAT PACKS AND FOUND BAT PACK INOP. REPLACED BAD BATTERY PACK . SYSTEM OP CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007031500175 20070315 00175 NE 2007 3 15 2007UALA00677 2 20070305 A 7532 BLEED VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE FAULTY A UALA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 WP 29 421UA 500 V11119 A 'THUD' NOISE NOTED ON TAKEOFF, DEADHEADING CAPT ON 23A NOTICED WHAT APPEARED TO BE A FIREBALL FROM ENG 1 EXHAUST. CREW REPORTED NO ABNORMAL PARAMETERS. NO DEBRIS FOUND ON RUNWAY. SUPPLEMENTAL DATA UPDATE CHECKED FOR EVIDENCE OF COMPRESSOR FAILURE WITH NO FINDINGS FOUND. FURTHER TROUBLESHOOTING FOUND THE 7TH AND 10TH STAGE BLEED VALVES SOLENOIDS TO BE FAULT Y AND WERE REPLACED. ALSO PERFORMED A VARIABLE STATOR VANE SYSTEM LUBE AS A PRECAUTIONARY MEASURE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032100035 20070321 00035 2007 3 21 2007UALA00775 4 20070311 A 3497 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FLT MANAGEMENT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 661UA 27158 FMC DOES NOT AUTO-TUNE. PERFORMED EXTENSIVE TROUBLE SHOOTING. FINALLY FOUND PIN 11 (CONNECTION ON 429 DATA BUS WIRE) OF D4821P SHORTED TO GRND BETWEEN CONNECTOR AND RELAY BASE (SHORT TO SHIELD) OF K2066. THIS IS RED, DATA BUSS WIRE LOCAT ED BEHIND THE E2-SHELF. INSTALLED NEW TWISTED SHIELDED PAIR BETWEEN K2066 AND PLUG D4821P. SHORT COULD HAVE BEEN CAUSE D BY RECENT MOD WORK IN THIS AREA. CHECKS OK. VERIFICATION FLIGHT TESTED. RETURNED TO ETOPS FLYING. 2 L 7 2 4F 4 F RT A1NM E24NE 2007032200075 20070322 00075 NM 2007 3 22 2007UALA00730 1 20070311 A 2121 FAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 531UA 25042 IN DESCENT PASSING FL370 CREW DETECTED AN ELECTRICAL BURNING ODOR IN THE COCKPIT WHICH QUICKLY DISSIPATED. [SUP 05-18-0 7] ACCOMPLISHED INSPECTION BEHIND COCKPIT CB PANELS AND E & E COMP. CREW COMMENT ODOR DISSIPATED BY TURNING OFF RIGHT R ECIRCULATION FAN. INSPECTED WIRING FOR RT RECIRC FAN. NO DISCREPANCY FOUND. CAUSE OF ODOR NOT ESTABLISHED. REPLACED RT RECIRC FAN. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032200170 20070322 00170 EA 2007 3 22 VNAA0703002 1 20070303 A 5270 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR FAILED A VNAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 05 244PS 4325 7912 CREW REPORTED A PAX DOOR/SERVICE DOOR CAUTION MESSAGE IN FLIGHT. CREW DIVERTED TO TYS AND LANDED WITHOUT INCIDENT. MAI NTENANCE REMOVED AND REPLACED THE PROX SENSOR ELECTRONIC UNIT IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCR AFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007032800055 20070328 00055 NE 2007 3 28 HNAA0700049 2 20070317 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA PW120 PW123 NE NR 1 DAMAGED A HNAA A UNSCHED LANDING C Y F.O.D. ENGINE STOPPAGE CL CLIMB 1 EA 07 327EN 284 123260 AFTER TAKEOFF ON CLIMB OUT AT ABOUT 4 THOUSAND FEET THE NR 2 ENGINE SHUT DOWN. INSPECTED ENGINE AND FOUND TO BE SERVICE ABLE. FOUND FOD DAMAGE ON NR 1 ENGINE AND IT WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 2007040200144 20070402 00144 NM 2007 4 2 WRLA2007049 1 20070309 A 5712 ARB2850506 RIB DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE RT WING CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271WA 48518 DURING C-04 CHECK IN TPE, FOUND RT WING FIXED LEADING EDGE SLAT TRACK RIB R16 CRACK .5 INCH XORS:885. REPLACED RIB AND FASTENERS PER MD-11 SRM 51-33-01 VOL.II REV.38. 2 L 7 3 4F 4 F RT A22WE E24NE 2007032900317 20070329 00317 EA 2007 3 29 A6WA200740061 1 20070209 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 421ZW 7346 RT MLG BATT RIB CRACKED 1 INCH LONG AT UPPER AFT CORNER.. MAINTENANCE REPAIRED BATT RIB IAW REO 601R-57-51-046. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007040600100 20070406 00100 SO 2007 4 6 N93A03042007 1 20070403 A 2720 1159SCH2385 TORQUE TUBE GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU RUDDER WORN E N93A K NONE O OTHER IN INSP/MAINT 1 SO 13 477QS 7224 1377 RUDDER TORQUE TUBE BOLT HOLES WERE FOUND WORN (ENLARGED) DURING MAINTENACE. 2 L 7 2 4F 4 F RT A12EA E25NE 2007040500126 20070405 00126 NM 2007 4 5 2007UALA00936 1 20070328 A 5520 ROD END AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE ELEVATOR WORN A UALA O OTHER E VIBRATION/BUFFET AP APPROACH 1 WP 29 823UA 952 VIBRATION NOISE ENCOUNTERED IN FLIGHT. [SUP 06-01-07] PERFORMED ELEVATOR FREEPLAY CHECK AND FOUND BOTH LEFT AND RIGHT OUTBOARD ELEVATOR ACTUATOR ROD ENDS TO BE WORN OUT OF COMPLIANCE. REPLACED LEFT AND RIGHT OUTBOARD ELEVATOR ACTUATOR ROD ENDS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007041300126 20070413 00126 NM 2007 4 13 2007UALA00992 1 20070403 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 CABIN C-ZONE LEFT FWD SEAT EEL INOP. REPLACED BATTERY PACK, OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007040600074 20070406 00074 CE 2007 4 6 DXTA200702076 1 20070403 A 3150 UNKNOWN CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE UNKNOWN E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 631QS 5605131 AFTER LOWERING LANDING GEAR (MASTER CAUTION) ALONG WITH (LOW BRAKE PRESS) AND (ANTISKID INOP) ILLUMINATED FLASHING FOR A PPROX 30 SECONDS. LIGHTS EXTINGUISHED PRIOR TO LANDING AND NORMAL BRAKING WAS NOTED. T/S FOUND SYSTEM OPS CHECKS NORMA L. ITEM IS A COLD SOAK ISSUE. REMOVED & REPLACED BRAKE MOTOR. CYCLE TIME SAME AS PREVIOUS MOTOR. REMOVED & REPLACED BRAK E POWER PACK ASSY WITH A NEW ASSY. BLED BRAKE BRAKES. OPS CHECKS GOOD I/A/W CE560 XL M/M 32-42-06 2 L 7 2 4F 4 F RT A22CE E00059EN 2007041900131 20070419 00131 NM 2007 4 19 2007UALA01110 1 20070409 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EEL INOPERATIVE ROW 53L. REPINNED LOOSE WIRE IN SEAT PLUG. OPS CHECKED GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2007042500315 20070425 00315 NE 2007 4 25 DXTA200702123 2 20070420 A 7321 FCU CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE LT ENGINE MALFUNCTIONED E DXTA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 07 844QS 5600629 LT ENGINE WOULD NOT DEVELOP FULL POWER FOR TAKEOFF. MAX POWER DEVELOPED WAS APPROXIMATELY 2 PERCENT N1 LOW, RIGHT ENGINE DEVELOPED FULL POWER. [SUP 05-02-07] VERIFIED DISCREPANCY. REMOVED AND REPLACED FCU WITH SERVICEABLE UNIT, CANNIBALIZ ED FROM OTHER AIRCRAFT. OPS CHECK GOOD. LEAK CHECK GOOD. WORK DONE IAW PNC. 535A M.M. CHAPTER 73-20-01. 2 L 7 2 4F 4 F RT A22CE E00053EN 2007043000081 20070430 00081 NM 2007 4 30 2007UALA01155 1 20070416 A 5720 VENT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LT WING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA 24380 LT WING HAS INTERNAL DAMAGE AT VENT SCOOP AREA (WING TIP). [SUP 05-16-07] REMOVED DAMAGED PARTS AND REPLACED IAW FRR U AL-744-0263. A/C OK FOR SERVICE. SUSPECT VENT DAMAGED BY GROUND SERVICE EQUIPMENT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007043000123 20070430 00123 NM 2007 4 30 2007UALA01235 1 20070419 A 3350 60252 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE AFT GALLEY SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 346UA 24250 AFT 20' OF EMERGENCY ESCAPE PATH LIGHTS ARE INOP. AFT GALLEY EEL STRIP SHORTED OUT FROM GALLEY MOISTURE. REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2007050900202 20070509 00202 NM 2007 5 9 2007UALA01409 1 20070501 A 2612 WARNING SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FIRE WARNING ACTIVATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 828UA 1031 FIRE LOOP B-FAULT DISPLAYED ON UPPER ECAM SCREEN ENG 2. LAST MTC WAS A FDU CHANGE ON 10/24/07. NO REPEATS SINCE THEN. FOUND 2 BAD SPLICES IN 'B' LOOP HARNESS ON PREVIOUS MONTHS REPORTS AND REPAIRED THOSE SLICES. 2 L 7 2 4F 4 F RT A28NM E40NE 2007051400196 20070514 00196 EU 2007 5 14 TRBA2007005 1 20070209 A 5610 NP1588014 WINDSHIELD AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE COCKPIT CRACKED A TRBA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 29 369AT 369 WHILE IN CRUISE AT 11,000 FTS RT WINDSHIELD STARTED CRACKING. RETURNED TO POS FOR CHECK. REPLACED F/O WINDSHIELD IAW J IC 56-11-00, FOUND WORKING PROPERLY WITH NO LEAK. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007051700138 20070517 00138 NM 2007 5 17 2007UALA01452 1 20070509 A 5310 DOOR FRAME BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 921UA 25388 FWD CARGO PIT, FWD FRAME IS CRACKED AT LWR STOP FITTING. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE, FABRICATED & INSTA LLED EXTERNAL NESTED ANGLES. 2 L 7 2 4F 4 F RT A16WE E21EU 2007052300173 20070523 00173 2007 5 23 2007UALA01495 4 20070512 A 2565 COVER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU R1 DOOR LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 DOOR 1R SLIDE COVER LOOSE. [SUP 05-29-07] SECURED COVER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007060600073 20070606 00073 NM 2007 6 6 2007UALA01726 1 20070529 A 5315 STRAP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 CRACKED FLOORBEAM STABILIZING STRAP AT BS 375, LBL 25. MAJOR REPAIR ACCOMPLISHED: REPAIRED & INSTALLED STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300018 20070523 00018 EU 2007 5 23 2007UALA01550 1 20070520 A 5524 TAB AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RH ELEVATOR BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 412UA 465 RIGHT ELEVATOR HINGE FITTING NR 1 LWR ANTI-ROTATION TAB IS BROKEN OFF. MAJOR REPAIR ACCOMPLISHED: INSTALLED T-ANGLE RE PAIR TO REPLACE ANTI-ROTATION TAB. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061300047 20070613 00047 NE 2007 6 13 ANCF200700013 2 20070602 A 7200 ENGINE DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE LEFT DAMAGED W ANCF A UNSCHED LANDING C F.O.D. CL CLIMB 1 SO 23 583AN 53183 P728011D AT TO ABOUT 11000 FT, A BIRD IMPACT OCCURRED ON THE LEFT ENGINE, PARAMETER DROP 1.4 EPR THEN ALL PARAMETERS CAME BACK TO NORMAL. IN ACCORDANCE WITH EWO 83-72-7309 LT ENGINE WAS REPLACED IAW AMM 71-00-00 PAGE 501 WAS PERFORMED ADJUSTMENT/TE ST AND CONDITIONS ARE SATISFACTORY FOR OPTIMUM OPERATION. 2 L 7 2 4F 4 F RT E9NE 2007061400048 20070614 00048 NM 2007 6 14 2007UALA01892 1 20070607 A 5420 SHIM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 PYLON MIGRATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 NR 2 PYLON LOWER AFT SPAR FITTING FOR THE DIAGONAL BRACE HAS SHIM MIGRATION. [08-08-07] REMOVED 4 EACH FASTENERS A T AFT LOWER SPAR FITTING PER SRM 51-40-02. NO GAP OR FURTHER SHIM MIGRATION NOTED. INSTALLED NEW FASTENERS PER MM 54-51- 95 AND SEALED AREA. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007062800166 20070628 00166 NM 2007 6 28 2007UALA02093 1 20070618 A 2910 HYDRAULIC SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 301UA 23642 RTFL DUE TO HYDRAULIC QUANTITY LOSS ON CLIMBOUT. [07-06-07] FOUND RIGHT WING HYDRUALIC LINE GOING TO MAIN GEAR RETRAC TING ACTUATOR LEAKING. REPLACED HYDRAULIC LINE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007061500004 20070615 00004 CE 2007 6 15 DJFA2007058 1 20070528 A 3220 LANDING GEAR BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE NOSE COLLAPSED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 744TA RK245 DURING A ROUTINE MAINTENANCE ENGINE RUN, THE NOSE LANDING GEAR RETRACTED WHEN THE ENGINE STARTED. MAINTENANCE DISCOVERE D THE LANDING GEAR HANDLE WAS IN THE (UP) POSITION. DAMAGE TO THE FUSELAGE SKIN WAS A RESULT OF AN L-BAND ANTENNA BEING PRESSED INTO THE FUSELAGE AS THE AIRCRAFT CAME TO REST ON THE GROUND. ADDITIONAL DAMAGE TO THE NOSE WHEEL WELL AREA WA S NOTED. DAMAGE WAS REPAIRED IN ACCORDANCE WITH HBC REPAIR ORDER FR-BJ-00688. 2 H 7 2 4F 4 F RT A16SW E25EA 2007061500010 20070615 00010 CE 2007 6 15 DXTA200702217 1 20070526 A 3230 99146372 MANIFOLD CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG LEAKING E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 966QS 5811 7500166 NOSE GEAR (BUMPS) IN CRUISE FLIGHT INTERMITTENTLY. NO GEAR UNSAFE LIGHT DURING BUMP. TROUBLESHOT DISCREPANCY TO INTERNAL LEAKAGE OF TIRE LANDING GEAR CONTROL MANIFOLD. REMOVED DEFECTIVE MANIFOLD. INSTALLED A MODIFIED MANIFOLD. OPS CHECK AND LEAK CHECK OF MANIFOLD ARE GOOD. PERFORMED GEAR SWINGS AND BLEED PROCEDURES IAW MM. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007071800263 20070718 00263 NM 2007 7 18 2007UALA02418 1 20070705 A 4990 OIL SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE APU LEAKING A UALA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 816UA 871 CREW REPORT, 280 MILES FROM DESTINATION GOT BURNED AIR COND DUCT OR OVERHEAT ODOR FROM ROW 10 TO COCKPIT. APU OIL LEAKI NG INTO BLEED AIR SYSTEM. APU REMOVED AND REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007073100062 20070731 00062 NM 2007 7 31 2007UALA02682 1 20070716 A 3397 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 674UA 29242 EEL LIGHT ON SEAT 13A IS INOPERATIVE. [08-17-07] REPLACED SEAT CABLE. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071000460 20070710 00460 EU 2007 7 10 2007UALA02315 1 20070629 A 3510 OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 460UA 1248 FIRST OFFICER'S O2 MASK DOESN'T TEST. 2 L 7 2 4F 4 F RT A28NM E40NE 2007080200091 20070802 00091 NM 2007 8 2 2007UALA02811 1 20070724 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE R1 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 DOOR 1R CUTOUT FWD FRAME LOWER INBD CORNER OF FRAME CRACKED OFF THROUGH RIVET HOLES. FABRICATED AND INSTALLED FILLER-DO UBLER REPAIR PER SRM 51-70-11 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2007072700042 20070727 00042 NM 2007 7 27 DL76G070947 1 20070717 A 4930 491080127 FUEL CONTROL BOEING 767 7673P6 1385105 NM GE CFM56 CFM56* 13802 NE APU MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 152DL 24984 888402 APU FAULT LIGHT DURING START 2 ATTEMPTS. RTB, ECU FAULT FUEL CONTROL UNIT. REPLACED FUEL CONTROL UNIT PER M/M. 2 L 7 2 4F 4 F RT A1NM E2GL 2007080700165 20070807 00165 CE 2007 8 7 AMWA86034 1 20070713 A 6120 5038912121 SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA PROPELLER MALFUNCTIONED A AMWA O OTHER O OTHER CR CRUISE 1 CE 07 244YV 244YV DURING FLT LT PROPS WENT INTO AUTOFEATHER. LANDED WITH NO FURTHER INCIDENT. PERFORMED CHECK FLT AND WAS UNSATISFACTORY . REMOVED AND REPLACED LOW AND HIGH TQ SWITCH, A123PCB. TEST FLT SATISFACTORY 2 L 7 2 4T 3 T RT A24CE E2NE 2007080700005 20070807 00005 NM 2007 8 7 2007UALA02825 1 20070725 A 2130 ACTUATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN PRESSURE SEIZED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 381UA 24656 RTFL DUE TO PRESSURIZATION PROBLEM. VALVE-AIR CYCLE DUAL MIXTURE UNIT ACTUATOR SEIZED. VARIABLE RESISTOR OUT OF LIMIT. BEARINGS RUSTY AND ROUGH. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080800086 20070808 00086 CE 2007 8 8 AMWA06032B 1 20070725 A 5410 STRUCTURE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT NACELLE CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 FRICTION CHAFING DURING OPERATION HAS CREATED WORN SEGMENTS ON THE RT ENGINE NACELLE. DAMAGE WAS ALONG THE ENTIRE LENGT H OF THE NACELLE SHAPE: DEPTH VARIED AS INDICATED ON THE REPAIR AUTHENTICATION. REPAIRED IAW ACFT ENGINEERING REPORT 67 99-2 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080900026 20070809 00026 CE 2007 8 9 GUUA07260703 1 20070726 A 3234 SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG HANDLE OUT OF ADJUST A GUUA O OTHER O OTHER CL CLIMB 1 SO 29 81546 UE187 FLIGHT: 9234, AFTER TAKEOFF, LANDING GEAR HANDLE LIGHT REMAINS ILLUMINATED IN THE UP POSITION. ADJUSTED RT MAIN LANDING GEAR UP POSITION SWITCH OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2007082100169 20070821 00169 EU 2007 8 21 2758071607 1 20070716 A 5533 1173040338 SKIN BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE VERTICAL STAB CRACKED E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 117MH 7112 1 INCH LONG SKIN CRACK FOUND ON IB SIDE OF VERTICAL STABILIZER SKIN. 1 G 7 2 3U 3 U H13EU E5NE 2007082300207 20070823 00207 EU 2007 8 23 2007UALA03104 1 20070809 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 438UA 678 LIGHT AT 13 ABC NOT ILLUMINATING WHEN TESTING THE EMERGENCY ESCAPE PATH LIGHTING. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007082300231 20070823 00231 NM 2007 8 23 2007UALA03128 1 20070811 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 AFT CARGO DOOR CUTOUT STA 847 STR 22, PREVIOUS REPAIR REMOVED FOR SKIN REPLACEMENT. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007082400391 20070824 00391 NM 2007 8 24 2007UALA03048 1 20070806 A 7797 WIRE HARNESS BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE ENGINE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 799UA 26926 ENGINE CONTROL SYSTEM IS OPERATING WITH REDUCED REDUNDANCY. FAULTY T3 INDICATION. REPLACED WO636 HARNESS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007082800011 20070828 00011 NM 2007 8 28 2007UALA03217 1 20070816 A 2120 UNKNOWN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 214UA 30220 CREW REPORTS HAD ELECTRICAL ODOR COMING FROM THE CHIME MODULE. 08-31-07 REPLACED FORTRESS DOOR STRIKER ASSY & OP CHECK S OK PER MM 52-51-02 PG401. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007090500212 20070905 00212 NM 2007 9 5 2007UALA03340 1 20070823 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 FOUND CEILING LIGHT INOP ABOVE ROW 26. REPLACED LAMP. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100101 20070831 00101 NM 2007 8 31 2007UALA03285 1 20070820 A 5514 LUG BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZ STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 379UA 24654 LEFT HORIZ STAB CORRODED: CENTER SECTION, AFT SPAR, CENTER FWD CLEVIS HAS CORROSION. REMOVED BUSHINGS FWD & AFT LUGS. REAMED BORE, HFEC, ROTO PEENED, TREAT AND PRIMED. FABRICATED OVERSIZE BUSHINGS, CAD PLATE AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091100205 20070911 00205 WP 2007 9 11 BKAA200710002 2 20070905 A 7200 31021802 ENGINE MTSBSI MU2 MU2B60 5780460 CE GARRTT TPE331 TPE331* 01514 WP ZONE 600 SHUTDOWN E BKAA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 SO 13 610CA 7341 1330 788SA P36192C SUP RT ENGINE SHUT DOWN IN FLIGHT. APPEARS TO BE A GEARBOX FAILURE OF SOME TYPE 1 H 7 2 3T 3 T RT A10SW E2WE 2007091800204 20070918 00204 NM 2007 9 18 2007UALA03575 1 20070904 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN MISLOCATED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 570UA 26678 EMERGENCY AISLE LIGHT LOCATED AT SEAT 2B IS IN WRONG LOCATION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092000281 20070920 00281 NE 2007 9 20 VNAA0708028 2 20070830 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RIGHT BIRD INGESTION A VNAA O OTHER C F.O.D. NR NOT REPORTED 1 GL 05 247JS 7922 CREW REPORTED A BIRD STRIKE TO THE RIGHT ENGINE COWL. MAINTENANCE VISUALLY INSPECTED FOR INGESTION INTO THE ENGINE AND FOUND NO DEFECTS ON FAN BLADES. NO FURTHER DEFECTS NOTED IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007092500107 20070925 00107 GL 2007 9 25 DXTA200702461 2 20070910 A 7200 ENGINE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RIGHT SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 919QS 7500224 RT ENGINE IS SMOKING AFTER SHUTDOWN AND SMELLS LIKE OIL. NO LEAKS OBSERVED. OIL LEVEL 3.5 TO 4 QTS LOW AND ENGINE TEMP O K. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007090600048 20070906 00048 NE 2007 9 6 HEEA116829 2 20070810 A 7200 0292005340 ENGINE SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B 60037 NE MAKING METAL D HEEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 153AE 2075 3829 DEPARTED, ENROUTE, THE AIRCRAFT ENGINE OIL PRESSURE LIGHT STARTED INTERMITTENTLY TO COME ON AND OFF THEN STAYED ON CONTI NOUS WITH A GONG SOUND FOLLOWING. REFERRED TO AS350B3 EMERGENCY GUIDE, REDUCED POWER, AIRSPEED, AND AT 2148 ADVISED OP ERATIONS OF THE SITUATION AND DIVERTED TO AIRPORT. MONITORED THE OIL PRESSURE AND ENGINE TEMPERATURE WHILE DESCENDING, SLOWING DOWN THE AIRCRAFT AND MAINTAINING A SAFE ALTITUDE IN THE EVENT OF AN ENGINE FAILURE. THE OIL PRESSURE WAS SLOW LY DROPPING BUT THE ENGINE TEMPERATURE WAS WITHIN NORMAL RANGE. APPROXIMATELY 2 MINUTES FROM AIRPORT, THE OIL PRESSURE DROPPED TO .5 , LANDED. 1 G 7 1 3U 3 U H9EU E00054EN 2007091000082 20070910 00082 NM 2007 9 10 2007UALA03450 1 20070828 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1554 S24-25L CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 EXTERNAL FUSELAGE, STA 1554 BETWEEN STR 24L AND STR 25L, FWD LAV VENT, SKIN AROUND EXHAUST BULGED AND CORRODED. REPAI RED PER REO G12120 REV A AND EVA-70582. STARTING AT 37,500FC MUST ACP A DETAILED VISUAL INSP EXT AND INTERNAL AND A LFEC EXT SKIN AND MUST CONTINUE EVERY 3000FC THERE AFTER PER EVA70582. REPAIR INSTALLED. AIRCRAFT READY FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092400004 20070924 00004 CE 2007 9 24 DXTA200702437 1 20070831 A 4990 OIL SYSTEM CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE APU LEAKING E DXTA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 07 611QS 5605548 APU AUTOMATICALLY SHUTDOWN IN FLIGHT DUE TO AN OVERHEAT. SMOKE FROM OVER-HEATED APU ENTERED CABIN. UPON VISUAL INSPE CTION OF APU FOUND APU OIL TO BE LOW. ADDED OIL AS REQUIRED IAW 650XLS AMM 12-10-00. RAN APU LOADED WITH ACM FOR APPROX. 20 MIN EGT PEAKED AT 522 DEG AND STABILIZED AT 502 DEG. ALL PARAMETERS IN LIMITS IAW 560XLS AMM 49-10-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007092700258 20070927 00258 NE 2007 9 27 TSAA0773051 2 20070920 A 7321 7436025 FUEL CONTROL BOEING 737 7372P6 1C84609 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAILED A TSAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 13 835AL 21613 P688655 NON-ETOPS FLIGHT 90 HNL-KOA, ON TAKEOFF ROLL, THE CREW NOTED THE NR 2 EGT CLIMBING FASTER THAN THE NR 1 EGT. ABORTED TH E TAKEOFF AT 100 KTS INDICATED AIRSPEED DUE TO NR 2 ENGINE HIGH EGT. THE CREW RETURNED TO THE GATE WITHOUT FURTHER INCI DENT. MAINTENANCE CONDUCTED A HIGH POWER RUN OF THE NR 2 ENGINE AND FOUND EGT AND EPR FLUCTUATIONS. THE NR 2 FUEL CONT ROL UNIT WAS REMOVED AND REPLACED IN ACCORDANCE WITH PRATT AND WHITNEY M/M 73-21-1. A HIGH POWER RUN WAS COMPLETED PER ALOHA MAINTENANCE TASK FORM M-215 WITH ALL CHECKS SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2007092500195 20070925 00195 SO 2007 9 25 GUUA08300702 1 20070830 A 2612 346000731 EXTINGUISHER EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CARGO BAY WARNING LIGHT A GUUA O OTHER J WARNING INDICATION CR CRUISE 1 SO 29 266AS 1024 120188 DURING FLIGHT BAGGAGE SMOKE FIRE EXTINGUISHER LIGHT ILLUMINATED. REPLACED NR 1 CARGO FIRE EXTINGUISHER BOTTLE. 2 L 7 2 4T 4 T RT A31SO E20NE 2007092800057 20070928 00057 NM 2007 9 28 2007UALA03755 1 20070918 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY LIGHTS AT ROWS 1A, 2A AFT & 35ABC ARE INOPERATIVE. 10-19-07 RELAMPED ALL SEAT POSITIONS. ALL OP CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007101600034 20071016 00034 CE 2007 10 16 AMWA0828013C 1 20071002 A 5311 12943003132 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FS 228.25 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 176YV 26646 UE176 REPAIRED LT AND RT FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT FS 228.25. 2 L 7 2 4T 4 T RT A24CE E26NE 2007101600128 20071016 00128 NM 2007 10 16 2007UALA04069 1 20071004 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 LT EXTERNAL FUSELAGE DENT IN SKIN IN RVSM AREA JUST AFT OF CAPTS PITOT STATIC IST AUX STATIC PROBE. MAJOR REPAIR ACP'D, FABRICATED AND INSTALLED EXTERNAL FUSELAGE SKIN DOUBLER AT THE RVSM ZONE, INCLUDING REPLACEMENT OF FRAME OUTER CHORD BS 251.6 & INSTALLED FRAME BS 256.1 WEB DOUBLER REPAIR STR 15L - 16. 2 L 7 2 4F 4 F RT A16WE E2GL 2007101700015 20071017 00015 2007 10 17 2007UALA04113 4 20071005 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR SLIDE UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 588UA 26717 CREW REPORT: DOOR 2L SLIDE RAFT LANYARD UNFASTENED FROM COVER. 10-30-07 SECURED LANYARD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007102300008 20071023 00008 NM 2007 10 23 AMTA200700492 1 20071012 A 5753 PANEL BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE TE FLAP DENTED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 IB REMOVABLE PANEL ON LWR SURFACE OF LT WING IB MAINFLAP IS DENTED (3) AREAS. REPAIRED IAW SAA EA 757-5753-09-A1012. ( K) PRIMED REPAIR AND BONDING SURFACES AS REQUIRED BY EA. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2007100200112 20071002 00112 EU 2007 10 2 2007UALA01934 1 20070611 A 2720 ROD END AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RUDDER WORN A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 494UA 1840 VIBRATION - NOISE ENCOUNTERED IN FLIGHT. SERVO ROD END WORN ON YELLOW HYD RUDDER SYS. REPLACED YELLOW SYSTEM RUDDER SE RVO ROD END. ALSO REPLACED SEALS ON YELLOW SYS HYDRO CONNECT PANEL, LEFT AND RIGHT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007100400082 20071004 00082 NM 2007 10 4 CHQA200700047 1 20070926 A 3213 STRUT BOMBDR CL600 CL6002D15 NM GE CF34 CF343B1 NE MLG UNDERSERVICED A CHQA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 GL 11 642BR 16371 7356 GEE872617 CRP TO IAH - DURING INITIAL CLIMB THE NOSE LANDING GEAR WOULD NOT RETRACT. COMPLETED ALL APPLICABLE CHECKLISTS AND QRH ITEMS, AND DETERMINED TO RETURN TO FIELD AT CRP. LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND SERVICED NOSE LAND ING GEAR STRUT, AIRCRAFT WAS FLOWN ON TEST FLIGHT WITH NO PROBLEMS NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 2007102600096 20071026 00096 EU 2007 10 26 TRBA2007086 1 20071019 A 3350 WIRE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW124B NE EMERGENCY LIGHTS BROKEN A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 288AM 288 ONE OF THE EMERGENCY EXIT LIGHTS IN THE STAIRS IS BURNED OUT. REPAIRED BROKEN WIRE AT PASSENGER CREW DOOR IAW SRM 20-24 -17. PERFORMED OPT CHK IAW JIC 33-50-00 AND FOUND WORKING PROPERLY AT THIS TIME. 2 H 7 2 4T 4 T RT A53EU E2ONE 2007110100189 20071101 00189 EU 2007 11 1 10192007 1 20071018 A 5302 1053040212 FITTING BOLKMS 117 BK117B2 5626013 EU PWA PT6 PT6A42 52043 NE TAILBOOM CRACKED E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 417MC 11372 7150 DURING SCHEDULED INSPECTION THE TAIL ROTOR GEARBOX ATTACHING FITTING WAS FOUND TO BE CRACKED. 1 G 7 2 3U 4 T NC H13EU E4EA 2007110900058 20071109 00058 NM 2007 11 9 2007UALA04494 1 20071030 A 5310 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 R-2 DOOR AT UPPER HINGE CUT-OUT IS DAMAGED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007111500196 20071115 00196 NM 2007 11 15 2007UALA04589 1 20071105 A 3397 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 560UA 26660 SEAT 19ABC EEL LIGHT CONNECTOR IS BROKEN OFF AT EEL LIGHT CONNECTOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007113000043 20071130 00043 2007 11 30 2007UALA04674 4 20071109 A 2565 5A28701 FLAPPER VALVE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ASPIRATOR LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 128UA G1141 30023 ASPIRATOR FLAPPER VALVE LEAKING. REPLACED ASPIRATOR 2 L 7 4 4F 4 F RT A20WE E24NE 2007113000098 20071130 00098 NE 2007 11 30 HALA0700491 2 20071116 A 7261 ENGINE BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE NR 1 OIL CONSUMPTION A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 587HA 33421 ETOPS SIGNIFICANT SYSTEM, ON ETOPS2 CHECK, NR 1 ENG WAS SERVICED W/4 PTS OF ENG OIL. INSPECTED NR 1 ENG NO LEAKS NOTED. A/C OK FOR SERVICE. CONSUMPTION W/I LIMITS, CONFERRED W/MOC. 2 L 7 2 4F 4 F RT A1NM E24NE 2007112100116 20071121 00116 NM 2007 11 21 2007UALA04633 1 20071109 A 5410 STRUCTURE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 NACELLE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 NR 2 PYLON FUEL LINE CUTOUT FWD INBOARD ATTACH HOLE CRACKED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007120400231 20071204 00231 NM 2007 12 4 F3LA200700314 1 20071101 A 5330 SKIN AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 946FR 2763 DURING C-1 CHECK, INSPECTION REPORTED COMPLIANCE WITH RW0000947 - (DENT LT FUSELAGE FR14 20 INCHES DOWN FROM LAP 53-11-1 1-DIA103 INCH). REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW SRM 53-11-11. 2 L 7 2 4F 4 F RT A28NM E37NE 2007120600009 20071206 00009 NE 2007 12 6 ASMF200711004 2 20071125 A 7200 GE9094B ENGINE BOEING 777 777* UTILUSE NM GE GE90 GE9090B NE LEFT DAMAGED W ASMF O OTHER J WARNING INDICATION CR CRUISE 1 SW 23 746AM 7697 7697 32719 900481 CAPTAIN REPORTED THAT AT 39,000 FEET, LEFT ENGINE STALLED, DESCENDING TO 27,000 FEET WITH OSCILLATIONS IN N1 AND N2 WIT H ENG CONTROL L AND ENG EEC C1 L MESSAGES, LANDING AT GRU. AT GRU, TECHNICAL PERSONNEL CONFIRMED THE MESSAGES AND PERFOR MED FIM 71-05 TASK 806 AND FIM 75-21 TASK 822 PROCEDURES, ALL CORRECT. BOROSCOPIC INSPECTION WAS PERFORMED FOUNDING 6 BL ADES OF HPC DAMAGED WITHIN LIMITS AND ONE FIRST STAGE HPT BLADE WITH DAMAGES OUT OF LIMITS. THE PT25 SENSOR AND EEC WERE REPLACED IAW MM 73-21-63 AND ENGINE STALL INSPECTION WAS PERFORMED IAW MM 71-00-00-200-809-G00, TESTED CORRECT. THE AIR CRAFT WAS DISPATCHED AS A FERRY FLIGHT TO CHICAGO STATION IAW GENERAL ELECTRIC CDR CA-07-0490 APPROVING THE ENGINE OPERA 2 L 7 2 4F 4 F RT T00001SE E00049EN 2007121200093 20071212 00093 NM 2007 12 12 2007UALA04826 1 20071125 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 DOOR 1L AFT CILL EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121300324 20071213 00324 NM 2007 12 13 TAMF20070038S 1 20071130 A 5330 SKIN BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE FUSELAGE DAMAGED W TAMF K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 23 770QT 23802 DURING TRANSIT CHECK THE AIRPLANE WAS HIT AT FUSELAGE WITH A STAIRWAY. SECTION 43, STA 347, STRINGER 31 RT. DAMAGED ARE A WAS REPAIRED IAW SRM 53-00-01 REPAIR 1 AND EWO 767-53-061. THIS REPAIR IS CLASSIFIED AS TEMPORARY REPAIR. PERMANENT R EPAIR WAS PERFORMED DURING C2 CHECK: TEMPORARY REPAIR WAS REMOVED AND PERMANENT REPAIR WAS PERFORMED IAW EWO 767-53-061 PART III & SRM 53-00-01 REPAIR 1. 2 L 7 2 4F 4 F RT A1NM E13NE 2007121400018 20071214 00018 WP 2007 12 14 WRLA2001129 1 20071201 A 5210 CABLE ASSY DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE L4 DOOR MISRIGGED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 14075 46922 DURING MAINTENANCE INSPECTION L4 PASSENGER DOOR FAILED PNEUMATIC TEST. RIGGED AIR RESERVOIR AIR RELEASE CABLE PER DC10 AMM 52-12-00 PAGE 534. ADJUSTED L4 DOOR EMERGENCY BACKLOCK PER DC10 AMM 52-12-00 PAGE 530A. PERFORMED PNEUMATIC TEST O F THE L4 DOOR PER DC10 AMM 52-10-01. REF SAA NRC 78379990001. 2 L 7 3 4F 4 F A22WE E23EA 2007122800111 20071228 00111 NM 2007 12 28 2007UALA05013 1 20071207 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 S14L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 FUSELAGE FRAME SHEAR TIE CRACKED, BS 360 JUST BELOW STR 14L. MAJOR REPAIR ACCOMPLISHED: REPLACED FRAME 360 SHEAR TIE BE LOW STR 14L. 2 L 7 2 4F 4 F RT A16WE E2GL 2008010300005 20080103 00005 CE 2008 1 3 DXTA200702681 1 20071215 A 5297 CONNECTOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL SEAL VALVE LOOSE E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 978QS 7500187 AT FL430 BAGGAGE DOOR SEAL EICAS MSG FOLLOWED BY RAPID CABIN ALTITUDE INCREASE. AFTER A FEW MINUTES ISOLATED BAGGAGE AND BELOW FL200 EICAS MSG OFF. FOUND SOFT SPLICE CONNECTION FOR DOOR SEAL VALVE, HEAT BLANKET NOT PROPERLY CONNECTED. REC ONNECTED SPLICE. PURGED DOOR SEAL PLUMBING OF MOISTURE. OPS CK'S AND LEAK CK'S GOOD. MAINT IAW C.C. 750 M.M. CHPT. 52 -31-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008011000132 20080110 00132 SO 2008 1 10 EKI2007F00000 1 20071010 A 8120 LW12088 ELBOW PIPER PA31 PA31P 7103120 SO LYC O541 TIGO541E1A 41539 EA HARTZL HCC3Y HCC3YR2 NE TURBOCHARGER WORN E EKIA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 WP 07 647SC 880 31P7300129 RL36462A DG227 RT ENGINE OIL SUPPLY FITTING TO TURBOCHARGER AND WASTEGATE PULLED OUT OF CASE ALLOWING OIL TO SPRAY ONTO TURBO AND WASTE GATE. THIS CAUSED AN OIL FIRE AFT OF THE EXHAUST PIPE WHICH DAMAGED THE RT FLAP AND RT OB GEAR DOOR. SUSPECT THAT O-RI NG UNDER FITTING RETAINING NUT EXTRUDED OUT OVER TIME AND ALLOWED THE NUT TO LOSE TORQUE WHICH ALLOWED THE FITTING TO VI BRATE THUS WEARING THE THREADS UNTIL THEY DISENGAGED. REPAIRED BY INSTALLING A HELI-COIL AFTER TALKING TO THE MFG REP. (K) 1 L 7 2 3O 3 O A8EA E19EA 5 C P25EA 2008011000190 20080110 00190 NM 2008 1 10 2007UALA05370 1 20071229 A 5210 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 532UA 25072 DOOR 2L UPPER HINGE ARM CUTOUT ON FRAME IS DAMAGED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008011100018 20080111 00018 2008 1 11 HEER118499 4 20071217 A 2210 L221M0002102 TRANSDUCER UROCOP EC135 EC135P2 5620027 EU PWA PW206 PW206B 0 NE COLLECTIVE MALFUNCTIONED B HEER O OTHER O OTHER NR NOT REPORTED 1 SW 03 328PH 768 0450 COLLECTIVE LINK CAUTION ON PFD WITH COLLECTIVE DOWN AND LOCKED WITH ENGINES AT FLY. REPLACED TRANSDUCER. 1 G 7 2 3U 3 U H88EU E42NE 2008011100108 20080111 00108 CE 2008 1 11 DJFA2007149 1 20071224 A 5511 128620022002 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 793TA 1230 373 RK244 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE O UTLINED IN COMMUNIQUE' NR 70. BOTH RIBS WERE REPLACED WITH THE UPGRADED ASSEMBLIES. 2 H 7 2 4F 4 F RT A16SW E25EA 2008011400068 20080114 00068 EU 2008 1 14 COEA0755821 1 20070904 A 5320 S5367800920002 INTERCOSTAL AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. LEVEL 2 CORROSION: CABIN FLOOR SUPPORT STRUCTURES T-CHANNEL INTERCOSTALS ARE CORRODED BETWEEN STRINGERS 16 AND 17L AND STRINGERS 16 AND 17R, BETWEEN FLOOR BEAMS 36 TO 38 LT AND RT. REMOVED AND REPLACED FLOOR SUPP ORT STRUCTURES T-CHANNELS. PN LT S5367800920002, RT S536780920102. WO 72242, NR 200089, 91. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008021500059 20080215 00059 NM 2008 2 15 2008UALA00008 1 20071231 A 5241 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 FORWARD GALLEY DOOR LOWER FRAME WEB CRACKED AT AFT INBOARD CORNER. MAJOR REPAIR: REPLACED LOWER WEB. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500179 20080215 00179 EU 2008 2 15 2007UALA04154 1 20071010 A 3241 ANTI-SKID SYS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MLG MISINSTALLED A UALA O OTHER W INADEQUATE Q C LD LANDING 1 WP 29 431UA 571 UPON LANDING ACFT DEVIATED FROM RUNWAY. PROBLEM WITH ANITSKID SENSING SYSTEM. AFTER INVESTIGATION IT SEEMS THAT DURING HMV LT AND RT SYSTEMS WERE INADVERTENTLY SWITCHED. A/C DOWN SEVERAL WEEKS WHILE REPAIRS WERE COMPLETED. NOTE: 2 NEW ENGINES WERE INSTALLED DUE TO THIS INCIDENT. QA INVESTIGATION ON GOING. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021500182 20080215 00182 NM 2008 2 15 2007UALA04731 1 20071119 A 2830 AV16B1659C VALVE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUEL SYSTEM FAULTY A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 786UA 26938 FLIGHT DIVERTED TO YEG TO REMOVE AN ILL PASSENGER. THE AIRCRAFT DEVELOPED A MECHANICAL PROBLEM AND RETURNED TO SFO. RE PLACED RT JET ISOLATION VALVE. OP CHK'D THRU MAINT ACCESS TERMINAL. PASSED, NO EXISTING FAULT. NO STATUS MSG. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007013100250 20070131 00250 WP 2007 1 31 07FDEA00215 1 20070131 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 1853-1871 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 AFT MAIN CABIN AFT RT OUTBD SEAT TRACK, EXISTING SPLICE REPAIR BETWEEN STA 1853 TO 1871 X= -100 APPROX PERFORMED GVI IAW EO 8-5100-7-5001 P2 CRITERIA, FOUND CORROSION WITH EXFOLIATION AROUND HEADS OF FASTENERS ON SPLICE SEAT TRACK. REMOVED FASTENERS IAW SRM 51-30-00 VOL 2. REMOVED CORROSION AND VERIFIED LIMITS IAW SRM 53-70-00 FIG 5 VOL 1. NOMINAL THK IS .132, RESIDUAL THK IS .122, MTRL REMOVED IS .010, MAT REMOVED IS 7.5 PERCENT. TREATED REWORKED AREA IAW SRM 51-21-01 VO L 2 AND REINSTALLED FASTENERS IAW SRM 53-70-00 FIG 6 VOL1 AND SRM 51-30-00 VOL 2, MAT REMOVED IS WITHIN LIMITS IAW SRM 53-70-00 FIG 5 VOL 1. 2 L 7 3 4F A22WE 2007091100119 20070911 00119 EU 2007 9 11 07FDEA03356 1 20070905 A 5310 A53973085 BEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 727FD 579 FOUND CORROSION SPOTS ON AFT CARGO DOOR SILL BEAM BETWEEN FRAME 59A-60A AND FRAME 63-63A. REPAIR PERFORMED BY SMOOTH BL END OUT, NDT INSPECTION FOR CRACK FREE AND FLAP PEENING IAW EA 6-5317-92211 AND RAS/DAHAM/4020122/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007060100061 20070601 00061 WP 2007 6 1 07FDEA01965 1 20070524 A 5522 ALC742117 WEDGE DOUG MD10 MD1010F 3022112 WP LT ELEVATOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 LEFT INBOARD ELEVATOR TRAILING EDGE DENTED AT MID-SECTION AREA. REMOVED DAMAGED SECTION OF LEFT INBOARD ELEVATOR PER DC /MD10 SRM 51-31-01 VOL 11. RECEIVED NEW TRAILING EDGE WEDGE SECTION, LOCATED AND DRILLED HOLES PER DC/MD10 SRM 51-31-0 1 PARAG 2 VOL11. ALODINED AND PRIMED PER DC/MD10 SRM 51-21-01 PARAG 31, VOL 11; 51-21-01 PARAG 24 VOL 11. INSTALLED TRAILING EDGE PER MD/DC10 SRM 51-31-01 VOL 11. PAINTED WEDGED SURFACE PER MD/DC10 SRM 51-21-02 PARAG 2J VOL11. 2 L 7 3 4F RT A22WE 2007110900074 20071109 00074 EU 2007 11 9 07FDEA04704 1 20071031 A 3230 D226550003 DAMPER AIRBUS 300 A300F4605R 3930327 EU RT MLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 683FE 801 ON TAKEOFF LANDING GEAR WOULD NOT RETRACT ON SYS2. SWITCHED TO SYS 1 AND TRIED AGAIN. GEAR STILL WOULD NOT RETRACT F AULT ON PROX BOX FOR RT GEAR, JACKED A/C. PRIOR TO RETRACTING GEAR NOTICED RT FWD TRUCK WAS NOT AS LOW AS LEFT, STOOD O N GEAR AND GOT IT TO MOVE INTO PROPER POSITION. RETRACTED GEAR IN SYSTEM 1 THEN SYSTEM 2 WITH NO FAULTS. LUBRICATED GE AR PIVOT POINTS AND REPLACED RT BOGIE BEAM PITCH DAMPER PER A300 M/M 32-11-15-4. LOWERED ACFT TO BRING WHEELS LEVEL TH EN JACKED ACFT BACK UP, RT BOGIE BEAM WENT TO NORMAL POSITION. RETRACTED GEAR NORMAL. 2 L 7 2 4F RT A35EU 2007060700063 20070607 00063 NM 2007 6 7 DLM88070640 1 20070527 A 5330 SKIN DOUG MD88 MD88 3023688 NM FS 245 DAMAGED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 943DL 49816 FUSELAGE SKIN DAMAGED AND UNDERLYING STRUCTURE MISDRILLED. SKIN CUT OUT AND DAMAGED HOLES OVERSIZED AND BUSHED. DAMAGE AT FS 229-250 ABOVE L-18L. 2 L 7 2 4F RT A6WE 2007082000015 20070820 00015 EU 2007 8 20 07FDEA02849 1 20070813 A 5330 A53989430201 SKIN AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 732FD 713 CORROSION ON SKIN AT C101-102, P17-20 RT REPAIR PERFORMED BY BLEND OUT THE CORROSION IAW SRM 51-74-10, APPROVED BY EA 6- 5319-106509 AND RAS/DAHAM/4022473/2007 ISS B. 2 L 7 2 4F RT A35EU 2007072700102 20070727 00102 WP 2007 7 27 07FDEA02555 1 20070720 A 2133 27401561 MOTOR DOUG DC10 DC1030F 3023504 WP OUTFLOW VALVE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 304FE 661 661 46992 PDIS: AFTER DEPARTURE, CLIMBING THROUGH 8000 FT RECEIVED "CABIN RATE" ALERT. LEVELED AT 10,000 FT THEN RECEIVED " CABIN ALTITUDE ALERT. REFER TO QRH PROCEDURE, NO CHANGE. A/C PRESSURIZED TO OUTSIDE PRESSURE AT 10,000 FT THROUGH LANDING. OUTFLOW VALVE SHOWED FULL CLOSED. ALL PACKS ON, ECON OFF, NO CHANGE. PERFORMED FAULT REVIEW OF BOTH CPC'S AND FOUND O FV MOTOR LOGGED. REMOVED AND REPLACED OFV DRIVE MOTOR REF M/M. OPS CKS AND R-T-S OF BOTH CPC'S. ALL INDICATIONS NORMA L, OK FOR SERV. PERFORMED ERASE MAINT MEMORY OF BOTH CPC'S. 2 L 7 3 4F RT A22WE 2007071000077 20070710 00077 EU 2007 7 10 07FDEA02308 1 20070628 A 5754 SKIN AIRBUS 300 A300B4605R 3930308 EU NR 2 SLAT MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 731FD 709 OLD FLUSH REPAIR DOUBLER ON RT SLAT NR 2 RT NOT CORRECT INSTALLED REPAIR PERFORMED BY RENEW THE DOUBLER REPAIR IAW SRM 5 7-43-11 FIG 202, APPROVED BY EA 6-5743-106467 AND RAS/FOK/111/2007 ISS A. 2 L 7 2 4F RT A35EU 2007050300175 20070503 00175 NM 2007 5 3 HALA0700186 1 20070422 A 5330 SKIN BOEING 767 767332 1382001 NM BS 261 S33-34R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 FUSELAGE SKIN RT BS 261, BETWEEN STR 33 AND STR 34 HAS LIGHTNING DAMAGE. REPAIRED LIGHTNING STRIKE OF FUSELAGE SKIN AT BS 261 BETWEEN STR 33 AND 34 PER 767 SRM 53-00-01-2R-8 AND HAL M105 597053. 2 L 7 2 4F RT A1NM 2007061200178 20070612 00178 EU 2007 6 12 07FDEA02104 1 20070610 A 5411 FRAME AIRBUS 310 A310203 3930313 EU NR 1 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 PYLON NR 1 AT AFT T/E LOWER SECTION LOWER FARING INNER INNER (A)-FRAME UPPER AND LOWER PORTION SUPPORT HAS CRACK BETWEEN RIB 19 AND 20 AND VISIBLE THRU OPEN ACCESS NR 474CR AND LIGHTING HOLE REMOVED AND REPLACED A FRAME IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2007040200020 20070402 00020 EU 2007 4 2 07FDEA00997 1 20070319 A 5330 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 300 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 748FD 633 CORROSION ON FUSELAGE UPPER SKIN PANEL C78-85, P4RH AND P7 LT REPAIR WAS PERFORMED BY REWORK IN SMOOTH CONTOUR AND FLAP PEENING IAW EA 6-5319-106398 AND RAS/DAHAM/4021681/2006 ISS. B 2 L 7 2 4F RT A35EU 2007101100072 20071011 00072 SO 2007 10 11 SWIA200718743 1 20070927 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 251YV 120251 FLT 5593 - EMERGENCY POD LIGHT AT ROW 3B IS INOP. REPLACED LIGHT FIXTURE AT ROW 3B. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2007052100065 20070521 00065 NM 2007 5 21 QXEA200700749 1 20070424 A 5320 ANGLE BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 C4 PDX - CORROSION ON ANGLE AFT AND 6" INBOARD OF ACCESS 144JZ. REPAIRED IAW SRM 51-21-00 AND 51-14-00, 51-25-10. 2 H 7 2 4T RT A13NM 2007051600011 20070516 00011 NM 2007 5 16 UIEA200700155 1 20070406 A 5347 SEAT TRACK BOEING 747 747243B 1384830 NM BS 685 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 UPPER DECK STATION 685 RBL 27 SEAT TRACK CORRODED AS MARKED. REMOVED CORROSION PER SRM 53-10-05 2 L 7 4 4F A20WE 2007010900078 20070109 00078 NM 2007 1 9 07FDEA00032 1 20070105 A 5311 AFA00273 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 MAIN DECK CARGO COMPARTMENT: MAIN FRAME STA 1661 LONGERON 12L AREA EXISTING REPAIR DOUBLER FOUND DAMAGED. REPAIR CARRI ED OUT AS PER SRM 53-30-00 VOLUME I FIGURE 1. INITIAL INSPECTION REQUIRED AT 14,500 CYCLES AND REPETITIVE INSPECTION REQUIRED EVERY 9,500 CYCLES THEREAFTER AS PER SRM 53-30-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. OIL CONTOL NO.: 304445, WRI: 53-10/5267 2 L 7 3 4F RT A22WE 2008010900029 20080109 00029 EU 2008 1 9 07FDEA05140 1 20071226 A 5610 NP1752013 WINDSHIELD AIRBUS 300 A300F4605R 3930327 EU COCKPIT CRACKED A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 682FE 800 CAPTS FWD WINDSHIELD SHATTERED IN CRUISE. REMOVED AND REPLACED CAPT'S WINDSHIELD PANEL, WINDOW HEAT PROTECTION CONTROLL ER AND WINDSHIELD TEMP REGULATOR. WINDOW INSTALLATION COMPLETED IAW MM 56-11-11-4. 2 L 7 2 4F RT A35EU 2007122700157 20071227 00157 2007 12 27 SWAA076299 4 20071216 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 636WN 27709 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2007031200138 20070312 00138 WP 2007 3 12 07FDEA00655 1 20070305 A 5230 FITTING DOUG MD10 MD1010F 3022112 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 566FE 46989 FOUND MAIN CARGO DOOR NR 2 SPOOL FITTING HAS CRACK INDICATION. REMOVED AND REPLACED FITTING IAW DC/MD10 SRM 51-33-01 V OL.II,DAC AFA 7132 REV J. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2007080200110 20070802 00110 NM 2007 8 2 ZZDA2007227 1 20070605 A 5313 INTERCOSTAL BOEING 717 717200 1383700 NM BS 1022-1043 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT (WASTE TANK AREA) AT INTERCOSTAL LONGERON 25L BETWEEN BS 1022 AND BS 1043. INSTALLED INTERCOSTAL AT AFT CARGO COMPARTMENT LONGERON 25L BETWEEN STA 1022 TO STA 1043. 2 L 7 2 4F TR A6WE 2007050800234 20070508 00234 NM 2007 5 8 DLM88070460 1 20070416 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 945DL 49818 FUSELAGE SKIN REPAIR AT STA 379.5 TO 389 BETWEEN LONGERONS 27R AND 29R - SCRATCH AND TWO CRACKS. PERMANENT REPAIR INSTA LLED PER AMX REPAIR DRAWING AMR0953593 R1 AND ERA 460140-14. 2 L 7 2 4F RT A6WE 2007011700056 20070117 00056 NM 2007 1 17 DL76L070022 1 20070101 A 4920 380029817 TURBINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE APU OIL CONSUMPTION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 171DN 38662 24759 P141 REPLACED APU DUE TO HIGH OIL CONSUMPTION. 2 L 7 2 4F 4 F RT A1NM E24NE 2007012500088 20070125 00088 NE 2007 1 25 ANCF200600043 2 20070121 A 7200 ENGINE BOEING 767 767259 1385136 NM PWA 4056 PW4056 NE RIGHT OVERTEMP W ANCF E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 23 986AN 24835 724385 EICAS MESSAGE (LE SLAT ASSYM) DISPLAYED. LEADING EDGE LIGHT ILLUM WITH FLAP LEVER IN 1 POS. BOTH FLAP POINTERS WERE CO RRECT. RT ENGINE WAS SHUTDOWN DUE A HIGH EGT EXCEEDED. DIGITAL FLIGHT DATA RECORDER WAS REMOVED FOR READING IN SHOP. THE FLAP/SLAT SYSTEMS AND THE RT ENGINE AND SUB-SYSTEMS ARE BEING CHECKED AND INSPECTED BY TROUBLESHOOTING TO CONTINUE T HE INVESTIGATION AND TO ACCOMPLISH THE REPAIR ACTIONS REQUIRED. RT ENGINE WAS REMOVED AND REPLACED. IT WILL BE SENT TO T HE MFG IN ORDER TO CONTINUE THE INVESTIGATION. 2 L 7 2 4F 4 F RT A1NM E24NE 2007012900350 20070129 00350 CE 2007 1 29 AMWA82203BC 1 20070123 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE DISCHARGED A AMWA K NONE J WARNING INDICATION CR CRUISE 1 CE 07 162ZV 4554 438 UE162 BATTERY CHARGE LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE CHARGED THE BATTERY AS NEEDED TO CLEAR DISCREPANCY. THIS BATTE RY CHARGE LIGHT ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS. 2 L 7 2 4T 4 T RT A24CE E26NE 2007020600023 20070206 00023 NM 2007 2 6 UIEA200700048 1 20070202 A 5414 SKIN BOEING 747 747341 13848AM NM GE CF6 CF650E2 30018 NE NR 3 NACELLE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 NR 3 PYLON PRECOOLER EXHAUST CUT-OUT CRACKED AT LOWER AFT SIDE. THE SKIN ASSEMBLY CRACKS WERE REMOVED BY TRIMMING. THE NR 3 STIFFENER WAS REINFORCED WITH A SUPPLEMENTARY STEEL LOWER ANGLE FROM NAC STATION 235 TO 254. THE RIB INSTALLATION AT NAC STATION 248 WAS MODIFIED TO ACCOMMODATE THE STEEL REPAIR ANGLE INSTALLED ON THE NR 3 STIFFENER. REPAIRED AREAS WERE NDT INSPECTED. 2 L 7 4 4F 4 F RT A20WE E23EA 2007012600160 20070126 00160 NM 2007 1 26 2007UALA00180 1 20070123 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 795UA 26927 DOOR 1L EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE. RELAMPED EXT EMERGENCY LIGHT AT DOOR 1L, OP CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007012500260 20070125 00260 NM 2007 1 25 2007UALA00101 1 20070114 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EEL'S INOP AT GALLEY G7 CEILING, UPPER DECK CEILING AT ROW 12, LAV 112 SIDEWALL. RELAMPED, OP CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007013100155 20070131 00155 SO 2007 1 31 GUUA01190701 1 20070119 A 3397 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN LOOSE A GUUA K NONE L NO TEST IN INSP/MAINT 1 SO 29 268AS 120202 AT SCHEDULED ROUTINE MAINTENANCE FOUND LT AND RT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. SECURED LOOSE CONNECTOR AT LT AFT EXTERIOR EMERGENCY LIGHTS OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 2007020500012 20070205 00012 CE 2007 2 5 AMW107001001 1 20070111 A 5730 SKIN PANEL BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RT WING CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 127ZV 23346 UE127 DURING THE INSPECTION PHASE OF A NR 4 DETAILED INSPECTION, A 2.5 INCH SPANWISE CRACK WAS FOUND ON THE UNDERSIDE OF THE R T WING AT WING STATION B.L. 29.06. NO SB OR AD'S APPLY TO THIS AREA OF THE AIRCRAFT. UPON FURTHER INSPECTION OF THIS AI RCRAFT, A REPAIR WAS ACCOMPLISHED AT THE SAME LOCATION ON THE UNDERSIDE OF THE LT WING. CORRECTIVE ACTION: PENDING 2 L 7 2 4T 3 T RT A24CE E2NE 2007021600014 20070216 00014 NM 2007 2 16 2007UALA00328 1 20070205 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 587UA 26713 EXTERIOR EMERGENCY EXIT LIGHTS OUT AT DOORS 1R & 3R. RELAMPED EXTERIOR EMERGENCY EXIT LIGHTS AT DOORS 1R AND 3R AND OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022200045 20070222 00045 NE 2007 2 22 HNAA0700035 2 20070209 A 7261 GARLOCK SEAL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE LEAKING A HNAA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 EA 07 846EX 326 120400 NR 2 ENGINE OIL PRESSURE FLUCTUATED FROM 40 TO 60 PSI IN FLIGHT. ENGINE WAS SERVICED WITH 6 QUARTS OF OIL TO BRING TO B OTTOM OF SIGHT GAUGE. FOUND STARTER GENERATOR GARLOCK SEAL LEAKING. REPLACED ENGINE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007022300131 20070223 00131 NM 2007 2 23 2007UALA00414 1 20070212 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 EMERGENCY LIGHTS ROW 1J AFT & AT 41 ABC ARE INOPERATIVE. RELAMPED BOTH POSITIONS. BOTH OP CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007030900175 20070309 00175 CE 2007 3 9 DXTA200701977 1 20070228 A 3230 9006EN42 SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP LT MLG INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 876QS 3547 258586 WHEN RETRACTING LANDING GEAR AND AFTER GEAR RETRACTION CYCLE WAS COMPLETE, LT GEAR INDICATOR RED NOSE GEAR INDICATOR RE D, RH GEAR INDICATOR GEAR GREEN AND RED. WHEN GEAR EXTENDED, ALL INDICATONS NORMAL.REMOVED AND REPLACED PRIMARY LANDING GEAR SWITCH ON RIGHT LANDING GEAR. ADJUSTED SWITCH AS NECESSARY AND PEFORMED RETRACTING TEST - ALL TESTS GOOD. 2 L 7 2 4F 4 F RT A3EU E6WE 2007031400005 20070314 00005 CE 2007 3 14 AMW070228004 1 20070227 A 5330 1294300651 SKIN PANEL BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FUSELAGE CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 161YV 19796 UE161 4 INCH LONG CRACK NEAR BASE OF NR 2 COMM ANTENNA, IN FUSELAGE SKIN. REPAIRED BY INSTALLING EXTERNAL DOUBLER IAW AERODES IGN ENGINEERING REPORT NR 6586-1 AND BSRM 51-40-02. LT PN 129-430065-1, PANEL ASSY-LT BONDED. 2 L 7 2 4T 4 T RT A24CE E26NE 2007031600086 20070316 00086 CE 2007 3 16 DXTA200702021 1 20070314 A 5100 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL UNKNOWN E DXTA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 07 966QS 7500166 ON CLIMB OUT, GOING THRU FL180 AND LATER FL 240. WE FELT BUMP FROM GEAR RE-RETRACTING. BOTH WERE AUDIABLE THUMPS. FOUN D ALL THREE UP-LOCK SWITCHES OUT OF RIG AND NOSE GEAR EMERGENCY RELEASE CABLE TENSION WAS TOO TIGHT. MADE NECESSARY ADJU STMENT IAW GEAR BUMP TROUBLE SHOOTING CHECKLIST, OPS CHECK GEAR GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007032900150 20070329 00150 NM 2007 3 29 2007UALA00869 1 20070322 A 3260 WARNING SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 543UA 25698 AFTER PUTTING GEAR DOWN GOT GEAR DISAGREE LIGHT & CORRESPONDING EICAS MSG. 4-17-07....SUP. TAPPED OR PUSHED DOWN ON THE LND GR CNTRL HANDLE EICAS MSG WENT AWAY AND DID NOT COME BACK, NO EICAS MSG RECORDED AGAIN. NO FAULTS FOUND ON PROX ELE CT UNIT. DUE TO NO FAULTS ON PSEU ACCOMPLISHED GEAR SWING. NO FAULTS OR DISCREPANCIES RECORDED DURING SWING. BITE TEST PSEU OKAY, BUT LAST FLT FAULT BITE SHOWED FAULT CODE 421-424. FOUND CONTROL LEVEL IS BINDING AGAINS P3-1 PANEL LIGHT PL ATE, AND NOT FULLY DOWN DETENT (CHRONICALLY). REPOSITION LIGHT PLATE. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007040500112 20070405 00112 NM 2007 4 5 2007UALA00913 1 20070327 A 5210 FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU PAX DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 AFT ENTRY DOOR CUTOUT UPPER DOOR FITTING ON TORQUE TUBE HAS PLAY. SECURED UPPER HINGE FITTING. 2 L 7 2 4F 4 F RT A16WE E21EU 2007033000312 20070330 00312 NM 2007 3 30 AMTA200700149 1 20070320 A 3397 WIRE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE CABIN DISCONNECTED E AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 522AT 29330 ROW 6-9 EMERGENCY FLOOR LIGHTING INOPERATIVE. RECONNECTED WIRE TO LIGHT ASSY AT ROW 6, OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007041200061 20070412 00061 EA 2007 4 12 A6WA200740085 1 20070226 A 5340 6013501251 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FS 625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 450AW 7823 AFT EQUIPMENT COMPARTMENT FS 625.00 OBLIQUE ANGLE LT CRACKED 2 INCHES LONG IN AFT RADIUS. MAINTENANCE REMOVED OLD CRACK ED 625 OBLIQUE ANGLE, INSTALLED NEW SERVICEABLE ANGLE PN 601-35012-51 IAW SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041900078 20070419 00078 EA 2007 4 19 COMA0760314 1 20070413 A 3010 6243843 SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT WING FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 816CA 7398 DURING CLIMB WITH WING A-ICE SWITCHES OFF, RECEIVED WING OVERHEAT MSG WITH TRIPPLE AURAL CHIME AND RED INDICATION ON EIC AS. RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. REPLACED THE LT WING OVERHEAT SENSOR. 2 L 7 2 4F 4 F RT A21EA E15NE 2007041600075 20070416 00075 NM 2007 4 16 2007UALA01026 1 20070405 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY EEL LIGHT INOPERATIVE AT SEAT 5A AFT. *S/D* RELAMPED EEL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007041700267 20070417 00267 EU 2007 4 17 2007UALA00954 1 20070330 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 472UA 1435 R2 DOOR SILL PLATE HAS CORROSION BEYOND LIMITS AT FRAME 68. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE & INSTALLED DOUB LER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2007042400201 20070424 00201 NM 2007 4 24 2007UALA01206 1 20070416 A 3397 WIRE HARNESS BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN UNKNOWN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 675UA 29243 EMERGENCY EEL LIGHTS INOPERATIVE AT SEATS 10AB & 16AB. [SUP 05-08-07] REPLACED DAMAGED WIRE HARNESS 2 L 7 2 4F 4 F RT A1NM E24NE 2007041700056 20070417 00056 WP 2007 4 17 ASMF200704005 1 20070409 A 3240 392492 VALVE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D* NE LT BRAKE ASSY LEAKING W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 216AM 17753 14622 49586 DURING TRANSIT CHECK, IT WAS DETECTED THE LT OB DUAL SERVO VALVE LEAKING. VALVE WAS REPLACED IAW M/M 32-43-03, TESTED CO RRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2007042600272 20070426 00272 CE 2007 4 26 41507 1 20070415 A 2435 23080050 STARTER GEN BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE RT ENGINE FAILED E DBCA E H A ENGINE SHUTDOWN DEACTIVATE SYST/CIRCUITS UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 GL 13 311HS 192 RK296 JA0363 FLIGHT CREW NOTICED VIBRATION DURING CRUISE FOLLOWED BY NR 2 GENERATOR AND LOW OIL PRESSURE ANNUNCIATORS. CREW SECURED NR 2 ENGINE AND DIVERTED.. LANDING WAS UNEVENTFUL. UPON INSPECTION IT WAS FOUND THE NR 2 ENGINE STARTER/GENERATOR HAD FAILED INTERNALLY SETTING UP A VIBRATION THAT CAUSED THE OIL FILTER HOUSING TO FAIL AND A SUBSEQUENT LOSS OF OIL.THE NR 2 ENGINE HAS BEEN REMOVED AND SENT FOR INSPECTION DUE TO VIBRATION AND LOSS OF OIL. 2 H 7 2 4F 4 F RT A16SW E25EA 2007052300001 20070523 00001 NM 2007 5 23 2007UALA01532 1 20070518 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EEL LIGHT INOP AT FWD GALLEY LOWER FWD RIGHT WALL. [SUP 06-06-07] SECURED CONNECTOR. OPS. CKS. NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007060500251 20070605 00251 NM 2007 6 5 2007UALA01668 1 20070528 A 5753 65B3901140 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RT FOREFLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 174UA 24381 RIGHT WING INBOARD TRAILING EDGE FOREFLAP LOWER SURFACE CRACKED. REPAIRED WITH WET LAYUP AND BMS8-301 RESIN PER UA-EVA- 70288 AND BOEING TELEX 8100-9. SUSPECT INSTALATION & RIG CAUSED UNUSUAL DYNAMIC LOADING DURING FLIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007060500293 20070605 00293 NM 2007 6 5 2007UALA01712 1 20070528 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 590UA 28708 EMERGENCY LIGHT INOP AT ROW 22ABC. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060800170 20070608 00170 WP 2007 6 8 WRLA2007074 1 20070527 A 5330 DOUBLER DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 14075 46922 DURING B-CHECK INSPECTION, CORROSION FOUND ON FWD LOWER CORNER OF UPPER CUTOUT SUPPORT DOUBLER FOR AFT HINGE ON CENTER G EAR RIGHT FWD DOOR IN CENTER W/W AT FS 1441. REMOVED DOUBLER, FABRICATED DOUBLER AND INSTALLED DOUBLER, TEE STIFFENER A ND SUPPORT FITTING IAW DC10 SRM VOL II 51-33-01 & 53-14-01. 2 L 7 3 4F 4 F A22WE E23EA 2007061300143 20070613 00143 EU 2007 6 13 BMAC07001 1 20070328 A 5620 137169C405 WINDOW BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE331* 01514 WP CABIN DEPARTED A B16A O OTHER D INFLIGHT SEPARATION CR CRUISE 1 SO 35 530PA 732 OUTER PANE BLEW OUT OF WINDOW SEAT 4A. MAINTENANCE REPLACED PASSENGER WINDOW ASSY AT SEAT 4A, PRESSURIZATION CHECK AND LEAK CHECK GOOD. 2 L 7 2 4T 3 T RT A21EU E2WE 2007061300302 20070613 00302 NM 2007 6 13 2007UALA01757 1 20070531 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 S10L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 FWD ENTERY DOOR CUTOUT STRINGER 10L IS CRACKED AT BS 294.5. [06-26-07] MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND IN STALLED STRINGER ANS STRINGER CLIP PER AAR EA REV IR I070359 AND UA-EVA-7030 1. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061400009 20070614 00009 NM 2007 6 14 2007UALA01881 1 20070606 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EEL INOP, SEAT 4F BOTH SECTIONS. [06-22-07] REPLACED AFT EEL AT 4F AND SECURED LOOSE CONNECTOR UNDER SEAT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007061900316 20070619 00316 EU 2007 6 19 2007UALA01836 1 20070605 A 3150 HORN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EVAC INTERMITTENT A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 413UA 470 EVAC HORN INTERMITTENTLY SOUNDING WHILE ACFT AT GATE. NO JOY WITH RESET BUTTON ON F/A PANEL'S. PERFORMED SEVERAL RESE TS OF THE SYSTEM AND PUT A/C BACK INTO SERVICE. THERE HAVE BEEN NO REPEATS OF THIS PARTICULAR ISSUE SINCE THE ORIGINAL . 2 L 7 2 4F 4 F RT A28NM E40NE 2007082400012 20070824 00012 GL 2007 8 24 RAIA00708027 2 20070813 A 7200 AE3007A1 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LEFT MALFUNCTIONED A RAIA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 823HK 16286 2610 145475 311409 FLT 8085 - ROA - COCKPIT FILLED WITH SMOKE AS ENGINE BLEEDS WERE TURNED ON. MAINTENANCE REMOVED AND REPLACED THE NR 1 E NGINE. OPS CHECK AND LEAK CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007061500013 20070615 00013 CE 2007 6 15 DXTA200702241 1 20070605 A 2750 DRIVE ASSY CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS DAMAGED E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 945QS 7500029 FLAP FAIL CAS MESSAGE CAME UP ON SHORT FINAL, FLAPS FALLED AT 30 DEGREES. [06-15-07] FOUND RIGHT WING INBD FLAP FL EX DRIVE CABLE BAD. REMOVED AND REPLACED CABLE IAW CESSNA 750 M/M 27-52-00 PREFORMED FLAP TROUBLESHOOTING IAW CESNA 750 M/M CH 27-50-00 NO DEFECTS NOTED AT THIS TIME OPS CHECKED SATISFACTORY 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007062600191 20070626 00191 NM 2007 6 26 2007UALA02010 1 20070614 A 5300 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 RAMP REPORTED A GOUGE 1FT AFT OF AFT CARGO DOOR. [07-10-07] MAJOR REPAIR ACCOMPLISHED: REPAIRED CRACK PER EVA-70345. 2 L 7 2 4F 4 F RT A16WE E21EU 2007053100086 20070531 00086 EA 2007 5 31 TRAX200700723 1 20070524 A 5410 COWLING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE NR 2 NACELLE DEPARTED A ASOA A UNSCHED LANDING E Y J VIBRATION/BUFFET ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 27 933EV 8022 NR 2 ENG FAILURE AT 32,000 FT, LOUD BAM WAS HEARD NR 2 THRUST LEVER SLAMMED TO IDLE. A/C YAWED TO THE LT, SEVER VIBRATI ON BEGAN IMMEDIATELY, UNABLE TO SECURE ENGINE, EMERGENCY DECLARED. EN ROUTE TO ATL A/C DIVERTED TO TRI DUE TO MTC. UPO N GROUND INSPECTION BOTH UPPER AND LOWER ENGINE COWLINGS WERE FOUND TO HAVE DEPARTED THE AIRCRAFT. FLT 4344 CX. [07-2 3-07] REMOVED AND REPLACED NR 2 ENGINE IN ACCORDANCE WITH CRJ 200 AMM 71-0-00. OPERATIONAL AND LEAK CHECK COMPLIED WIT H. ALL PARAMETERS WITHIN SERVICABLE LIMITS IAW CRJ 200 AMM 71-00-00. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007061500179 20070615 00179 CE 2007 6 15 DXTA200702208 1 20070520 A 3260 MS25237387 BULB CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG INDICATOR BURNED OUT E DXTA O OTHER P NO WARNING INDICATION DE DESCENT 1 GL 07 975QS 5649 7500175 LANDING GEAR WAS LOWERED FOR LANDING AND HAD NO INDICATION OF EXTENSION EXCEPT BY SOUND. GEAR WAS CYCLED UP AND WE HEARD SOME RETRACTION. HANDLE WAS CYCLED DOWN AND NOTHING HAPPENED. GEAR WAS LOWERED MANUALLY. REMOVED LIGHT BULBS AND INSTA LLED NEW BULBS. OPERATIONAL CHECKS GOOD. WORK PERFORMED IAW CH 33-10-00 OF THE MM. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007121200047 20071212 00047 NM 2007 12 12 2007UALA04803 1 20071124 A 3350 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 504UA 24625 EMERGENCY LIGHT OUT, OUTSIDE BY DOOR 1L. FOUND BURNED OUT LAMP. REPLACED LIGHT BULB/SECURED COEVER. OPS CHECKED NOR MAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062700001 20070627 00001 NM 2007 6 27 2007UALA02055 1 20070617 A 2612 FIRE DETECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU APU FAULTY A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 349UA 24253 APU DETECTOR FAULT LIGHT ON AT ALL TIMES. [07-10-07] FOUND FAULTY APU FIRE DETECTOR M334. ALSO FOUND GROUND BROKEN AT LUG ON APU TAIL PIPE FIRE DETECTOR M515. REPLACED FIRE DETECTOR M334 AND M515. 2 L 7 2 4F 4 F RT A16WE E21EU 2007072000181 20070720 00181 NM 2007 7 20 2007UALA02521 1 20070709 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY CEILING LIGHT INOP ROW 6 RT. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071300278 20070713 00278 NM 2007 7 13 2007UALA02371 1 20070702 A 3350 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EMERGENCY EXIT SIGNS INOPERATIVE JUST ABOVE AND AFT OF LAV 102 & ABOVE DOOR 2R. SECURED BATTERY ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007070200108 20070702 00108 NM 2007 7 2 2007UALA02135 1 20070619 A 2612 SQUIB BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2 NACELLE NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 SQUIB TEST FAILED, ENG 2 TEST 1. [07-20-07] REPLACED "SQUIB TEST PANEL" OPS CK'D ALL ENGINES AND APU SQUIB SYSTEMS 1 & 2 -- OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071700102 20070717 00102 NM 2007 7 17 DLM90070863 1 20070628 A 5210 9955763U17 SHEAR TIE DOUG MD90 MD9030 3023690 NM IAE V2525 V2525D5 NE L1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 V20105 L1 DOOR SHEAR TIE BEHIND DOOR INNER HANDLE IS CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW MD-90 SRM 51-30-02, 51-10-0 5 AND 51-30-05. 2 L 7 2 4F 4 F RT A6WE A40NE 2007080800036 20070808 00036 CE 2007 8 8 GLBA230060965 1 20070722 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE COCKPIT ODOR A GLBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 208GL UE208 AIR RETURN, FLIGHT 5069, PILOTS REPORTED A STRONG BURNING ODOR DURING FLIGHT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF BOTH ENGINES ON THE GROUND WITH NO FAULTS FOUND. SUBSEQUENT OPERATIONAL CHECK FLIGHT WAS CONDUCTED WITH NO FURTHER REPORTS. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080800047 20070808 00047 EA 2007 8 8 NW6A00707002 1 20070721 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE CABIN LOOSE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 160GJ 10239 EMERGENCY FLOOR STRIPS LOOSE AT ROW 5 B/C. SECURED EMERGENCY FLOOR STRIP AT 5 B/C. 2 L 7 2 4F 4 F RT A21EA E15NE 2007080800089 20070808 00089 CE 2007 8 8 AMWA06032U 1 20070725 A 5311 1294300321 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 378 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080900001 20070809 00001 NM 2007 8 9 UPS07450335 1 20070703 A 5320 65B0961429 PLATE BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE BS 940 MISINSTALLED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C M/D BS 940 RT TENSION TIE FWD ATT STEEL PLATE UPPER ROW MOST IB FASTENER HOLE FOUND SHORT EDGE MARGIN . M/DECK BS 940 RT TENSION TIE FWD ATTACH STEEL PLATE REPLACED AND INSTALLED IAW HX RS NR R53-25-35824 AND UPS EO NR B7 47-5310-23715-C CONTINUE INSPECTION ARE REQUIRED IAW RS NR R53-25-35824 AND UPS EO NR B747-5310-27295. 2 L 7 4 4F 4 F RT A20WE E3NE 2007081700111 20070817 00111 NM 2007 8 17 2007UALA02907 1 20070728 A 3350 20131A BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 588UA 26717 EEL LIGHTS INOP ROWS 24-30. REPLACED BATTERY FOR POWER SUPPLY M735. 2 L 7 2 4F 4 F RT A2NM E17NE 2007081700296 20070817 00296 NM 2007 8 17 2007UALA02986 1 20070802 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 672UA 30027 AFT GALLEY'S EMERGENCY X-AISLE EEL LIGHT IS INOP. REPLACED EEL STRIP, OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007080900012 20070809 00012 NM 2007 8 9 AMTA200700350 1 20070717 A 5210 PUSHROD BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE L1 DOOR OUT OF ADJUST A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 552TZ 32586 L-1 DOOR DIFFICULT TO CLOSE FROM OUTSIDE AIRCRAFT. REMOVED AND REPLACED 4 EA LATCH CAM ROLLERS. ADJUSTED COCKING PUSHR OD IAW 52-11-13-2. DOOR OPS CHECK NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007082100151 20070821 00151 CE 2007 8 21 DJFA2007082 1 20070728 A 2120 UNKNOWN BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE CABIN ODOR E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 473LX RK518 DURING CRUISE, PAX REPORTED SMOKE ODOR IN THE CABIN. AIRCRAFT DIVERTED AND LANDED SAFELY. MAINTENANCE COULD NOT FIND T HE SOURCE OF THE ODOR AND WAS UNABLE TO DUPLICATE THE ODOR. NO EVIDENCE OF BURNING OR SMOLDERING WAS FOUND. 2 H 7 2 4F 4 F RT A16SW E25EA 2007082400127 20070824 00127 CE 2007 8 24 DXTA200702374 1 20070801 A 3260 INDICATOR BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE MLG INOPERATIVE E DXTA L ABORTED APPROACH P NO WARNING INDICATION LD LANDING 1 GL 07 151QS RK422 WHEN LANDING GEAR WAS EXTENEDED RT GREEN LIGHT DID NOT ILLUMIMINATE, TESTED BULB AND CONFIRMED BULB WAS GOOD. EXECUTED A GO AROUND AND THE RT LANDING GEAR LIGHT ILLUMINATED. JACKED AIRCRAFT AND COMPLIED WITH GEAR SWING; NO DEFECTS FOUND AT THIS TIME. REFERENCE HAWKER BEECHCRAFT 400A MAINTENANCE MANUAL. CHAPTER 32-00-00. 2 H 7 2 4F 4 F RT A16SW E25EA 2007082100075 20070821 00075 NM 2007 8 21 2007UALA02958 1 20070801 A 5512 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZ STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 RIGHT HORIZ STAB LOWER SKIN IS CRACKED AT AFT SPAR 64 INCHES OUTBOAD. MAJOR REPAIR ACCOMPLISHED: INSTALLED EXTERNAL SK IN DOUBLER REPAIR & INSTALLED ACCESS HOLE CUTOUT REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007083100126 20070831 00126 NM 2007 8 31 2007UALA03308 1 20070821 A 5310 CREASE BEAM BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 913UA 25291 AFT CARGO CREASE BEAM AT WL 208 IS DAMAGED. MAJOR REPAIR ACCOMPLISHED: INSTALLED TYPICAL EXTRUDED SECTION REPAIR. CRE ASE BEAM CUT AT STA 776. REPAIRED FROM STA 770-782 STR 17R. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090400040 20070904 00040 NE 2007 9 4 DL76P071142 2 20070825 A 7250 TURBINE WHEEL BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 140LL 38066 25988 727678 SECOND STAGE HPT DAMAGE FOUND DURING DURING BORO OP 5067. REPLACED NR 1 ENG PER RC DECK XMITTER 76X1T148, RAN ENG PER D ECK, OPS AND LEAK CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082300123 20070823 00123 NE 2007 8 23 NOCA14807 2 20070804 A 7314 GP202MK1 PUMP BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE FAILED A NOCA K NONE Y ENGINE STOPPAGE TX TAXI/GRND HDL 1 EA 15 750NA 26277 ON TAXI IN GEO RAMP LEFT ENG SHUT DOWN (UNCOMMANDED) PERFORMED FIM 73-11-00. REMOVED AND REPLACED HP AND LP FUEL PUMP A S PER MM 73-11-01 & 73-11-03 RAN ENG AND PERFORMED RUNUP TEST PER 71-00-00, OPS CHECK OK. 2 L 7 2 4F 4 F RT A2NM E12EU 2007082300181 20070823 00181 NM 2007 8 23 2007UALA03037 1 20070805 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 FOUND SEATS 1A AND 49HJK EMERGENCY LAMP ARE INOPERATIVE. 08-31-07 RELAMPED AT BOTH SEAT POSITIONS. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700040 20070907 00040 NM 2007 9 7 2007UALA03394 1 20070826 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 1F INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 775UA 26947 AFT EMERGENCY LIGHT AT SEAT 1F IS OUT. REPLACED LIGHT ASSY. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007091800081 20070918 00081 CE 2007 9 18 DJFA2007101 1 20070825 A 2910 25SW265159 LINE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP HYD SYSTEM BENT E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 829LX 7621 258466 DURING PREFLIGHT, CREW NOTED CHAFFING ON THE HYDRAULIC BRAKE LINE IN THE LT MLG WHEEL WELL. MAINTENANCE DISCOVERED THE LINE BENT AND MIS-SHAPEN FROM AN UNKNOWN CAUSE. THE LINE APPEARED TO BE ROUTED CORRECTLY BUT AS A RESULT OF THE CONTORT ION, THE LINE WAS CHAFING ON THE MLG STRUT. MAINTENANCE REPLACED THE LINE. 2 L 7 2 4F 4 F RT A3EU E6WE 2007091800172 20070918 00172 EU 2007 9 18 2007UALA03546 1 20070903 A 3150 WARNING SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 488UA 1680 V11158 STALL DISPLAYED ON UPPER ECAM SCREEN DURING POWER DECELERATION. ENGINE NOT SHUTDOWN. ENG 1 CREW COMMENTS: FLT LVL 360 --49C-.77MACH. FOUND NR 1 ENG 7TH STAGE BLEED SOLENOID VALVE 7B FAILED. REPLACED NR 1 ENG 7TH STAGE BLEED SOLENOID VALVE 7B AND PERFORMED CORRESPONDING ENGINE RUNS WITH NORMAL RESULTS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092000182 20070920 00182 EU 2007 9 20 2007UALA03626 1 20070908 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN ODOR A UALA A UNSCHED LANDING W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 474UA 1475 DUE TO STRONG BURNING ODOR IN CABIN FLIGHT WAS DIVERTED. FOUND OVER HEATING BALLAST/LIGHT (PAX READING) ASSY. REPLA CED BALLAST AND PAX READING LIGHT ASSY. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092500238 20070925 00238 NE 2007 9 25 DXTA200702428 2 20070824 A 7200 ENGINE CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE POWER LOSS E DXTA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 07 368QS 6800073 AFTER TAKEOFF, LEVELED OFF AT 2000 FT WHEN REDUCING POWER ON BOTH ENGINES TO 70 PERCENT N1 BOTH ENGINES SURGED +/- 5 TO 10 PERCENT. BOTH ENGINES STABILIZED AFTER APPROXIMATELY 60 TO 90 SECONDS. DOWNLOADED EDU'S IAW MM CH 77-40-01. RAN EN GINES REPRODUCED SQUAWK TOOK SNAPSHOTS DURING OSCILLATIONS. DOWNLOADED EDU'S AGAIN. THESE OSCILLATIONS ARE DESCRIBED I N SIL PW300-081. IAW THIS SL. THE ENGINE IS ALLOWED AN OSCILLATION WITH AN AMPLITUDE OF 6 PERCENT N1 NO FURTHER MAINTEN ANCE ACTION IS REQUIRED. 2 L 7 2 4F 4 F RC T00012WI E35NE 2007092600133 20070926 00133 EA 2007 9 26 TRAX200701349 1 20070914 A 7931 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE ENGINE OIL ILLUMINATED A ASOA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SO 27 901EV 7616 LEFT ENGINE LOW OIL PRESSURE MSG IN FLIGHT AT FL 310, OIL PRESSURE DROPPED TO 0 PSI. C\W QRH, LANDED WITHOUT EVENT. EM ERGENCY DECLARED. 2 L 7 2 4F 4 F RT A21EA E15NE 2007092500357 20070925 00357 EU 2007 9 25 2007UALA02441 1 20070705 A 2150 BELLOWS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE A/C PACK RUPTURED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 417UA 483 UNABLE TO COOL COCKPIT. FULL COLD SUPPLIES 80 DEGREE AIR WITH HOT AIR SWITCH OFF. STILL 80 DEGREES. FOUND LEFT PACK B ELLOWS HAS LARGE RUPTURE BETWEEN AIR PACK 1 OUTLET AND MIXER UNIT. ALSO FOUND DUCTING PARTIALLY CLOGGED WITH LINT. REP AIRED BELLOWS AND REMOVED LINT. REPLACED NR 1 PACK ANTI ICE VLV, ZONE TEMP CONTROLLER, COCKPIT CABIN TEMP SENSOR, LT RE CIRC FILTER, 24HK LT MIXER UNIT TEMPERATURE SENSOR AS PRECAUTIONARY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007100500090 20071005 00090 NM 2007 10 5 2007UALA03834 1 20070922 A 5241 WEB BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 FWD GALLEY DOOR AFT LOWER WEB CRACKED AT LWR STOP FITTING. REMOVED & REPLACED DAMAGED WEB. 2 L 7 2 4F 4 F RT A16WE E21EU 2007101000165 20071010 00165 EU 2007 10 10 07FDEA04371 1 20070928 A 7830 32143306 REGULATOR VALVE AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE THRUST REVERSER FAILED A FDEA F ACTIVATE FIRE EXT. N FALSE WARNING TO TAKEOFF 1 SO 25 657FE 4222 4222 748 DURING TAKEOFF ROLL BELOW APPROX 60 KNOTS ENG NR 1 REV PRESSURIZED AT APPROX 80 PERCENT N1. REJECTED TAKEOFF. RELEASE D FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 08OCT07. REACTIVATED NR 1 REVERSER, PERFORMED OPS CHECK, NO DEFECTS NOTED. REMOVED AND REPLACED NR 1 T/R PRSOV REF M/M 78-31-05-4-07. SYSTEM OPS AND LEAK CHECKS NORMAL ON GROUND. 3 GOOD LEGS SO FAR 2 L 7 2 4F 4 F RT A35EU E13NE 2007100500138 20071005 00138 NM 2007 10 5 2007UALA03849 1 20070922 A 3350 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EEL INOP ROWS 6AB-8AB. 10-19-07 REPLACED POWER SUPPLY UNIT AT DOOR 2 LEFT. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102900158 20071029 00158 EU 2007 10 29 2007UALA04290 1 20071017 A 3350 D9239003500060 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 427UA 512 FWD BATTERY L EPSU BATTERY FAULT ON LIGHT TEST NO GREEN LIGHT AT COMPLETION PER 3 SV. REPLACED L EPSU - NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007102300303 20071023 00303 NM 2007 10 23 2007UALA03890 1 20070925 A 3350 9F19948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L1 DOOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY LIGHT DOOR 1L SLIDE INOP. REPLACED EEL LIGHT ON DOOR 1L SLIDE. OP CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007103000135 20071030 00135 NM 2007 10 30 2007UALA04358 1 20071023 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 598UA 28751 NR 4R EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007103100186 20071031 00186 NM 2007 10 31 2007UALA04307 1 20071018 A 5241 FABRIC BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 330UA 24191 FWD GALLEY DOOR, FABRIC BELOW GIRT BAR IS HANGING SAGGING. SUSPECT SLIDE IMPROPERLY INSTALLED. REMOVED ESCAPE SLIDE, R EPOSITIONED GIRT MATERIAL & REINSTALLED SLIDE. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110800010 20071108 00010 NM 2007 11 8 2007UALA04408 1 20071025 A 2612 WARNING SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE ACTIVATED A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 579UA 26697 EICAS MESSAGE - R ENGINE FIRE LOOP 2. 2 L 7 2 4F 4 F RT A2NM E17NE 2007111300060 20071113 00060 NM 2007 11 13 2007UALA04576 1 20071105 A 2131 CONTROLLER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN PRESSURE MALFUNCTIONED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 937UA 26668 AIRPLANE DEPRESSURIZED AT 6000FT AGL IN "AUTO", VALVE FULL OPEN. WENT TO "STANDBY", PRESSURIZED MOMENTARILY THEN DEPRES SURIZED AGAIN IN "STANDBY", VALVE FULL OPEN. OK IN "MANUAL AC". FOUND VOLTAGE MISMATCH INSIDE THE AUTO PRESSURE CONTR OLLER. REPLACED THE AUTO PRESSURE CONTROLLER AND ADC AND NR 1 DIGITAL AIR DATA COMPUTER. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2007112900049 20071129 00049 EU 2007 11 29 2007UALA04769 1 20071120 A 3234 HANDLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MLG MALFUNCTIONED A UALA O OTHER O OTHER CL CLIMB 1 WP 29 441UA 751 ON DEPARTURE, GEAR HANDLE WAS LOCKED IN DOWN POS FOR APPROX 5 SEC AFTER ACHIEVING POS CLIMB. BROKEN LINK ON UPPER GEA R DOOR CAUSING THE DOOR TO BIND WHEN MOVING TO STOW. REPAIRED BROKEN LINK. SERVICED STRUT ASSY, ACCOMPLISHED GEAR SWING S, ALL SYSTEMS OPERATING NORMALLY. NO REPEAT REPORTS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121100071 20071211 00071 NM 2007 12 11 UIEA200700473 1 20071117 A 5410 ACOUSTIC PANEL BOEING 747 747271C 1384869 NM GE CF6 CF650E2 30018 NE NR 2 NACELLE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 DURING A CHECK INSPECTION, NR 2 ENGINE NOSE COWL, VISUALLY FOUND AFT INNER SKIN OF ACOUSTIC PANEL CRACKED THREE PLACES ( AS VIEWED WITH COWL OPEN): 6 O'CLOCK/8 INCHES LONG; 06:45 O'CLOCK/11 INCHES LONG; 7 O'CLOCK/15 INCHES LONG. APPLIED INT ERIM REPAIR IAW SRM 54-00-02,51-40-09 FIGURE 9 AND XEO 71-111707. VISUAL INSPECTION REQUIRED EVERY FLIGHT CYCLE UNTIL N OSE COWL REPLACED. 2 L 7 4 4F 4 F RT A20WE E23EA 2007120400221 20071204 00221 CE 2007 12 4 DXTA200702594 1 20071104 A 3240 BRAKE ASSY RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG WEAK E DXTA O OTHER O OTHER LD LANDING 1 GL 07 838QS 258338 BOTH PILOT AND COPILOT BRAKES ARE SPONGY. PEDALS TRAVEL HALF WAY BEFORE ANY BRAKING ACTION. PERFORMED OPS CHECK OF BRAK E SYSTEM. NO DISCREPANCIES NOTED IAW 32-40-00. 2 L 7 2 4F 4 F RT A3EU E6WE 2007121300023 20071213 00023 NM 2007 12 13 2007UALA04844 1 20071126 A 5280 DOOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE LT MLG CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 664UA 29236 LEFT MLG STRUT DOOR, HAS A 7 INCH CRACK ON UPPER AFT CORNER. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121400008 20071214 00008 NM 2007 12 14 2007UALA04924 1 20071130 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 528UA 25018 EMERGENCY EXIT FLOODLIGHT INOP AT FWD LT OVERWING HATCH. 2 L 7 2 4F 4 F RT A2NM E17NE 2007121300344 20071213 00344 NM 2007 12 13 2007UALA04882 1 20071129 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 AFT CARGO DOOR CUTOUT, BEAR STRAP REPAIR BS 847 STR 22R NEEDS TO BE REINSTALLED AFTER SKIN REPLACEMENT. MAJOR REPAIR: REPAIRED AFT PIT DOOR CUTOUT BEAR STRAP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121400279 20071214 00279 NM 2007 12 14 2007UALA04979 1 20071206 A 3320 BALLAST BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN LIGHTS FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 351UA 24319 RTFL DUE TO SMOKE IN AFT GALLEY. FOUND FAILED BALLAST. REPLACED BALLAST. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121900060 20071219 00060 NM 2007 12 19 2007UALA05054 1 20071211 A 3397 794640 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY LIGHT AT SIDE OF LAV 111 LT BOTTOM WALL INOP. REPLACED EEL CABLE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010900115 20080109 00115 NM 2008 1 9 2007UALA05314 1 20070307 A 2611 SMOKE DETECTOR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO BAY FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 913UA 25291 AFT CARGO LOOP "A" FAULT LIGHTS ON. POTENTIAL FAULTY SMOKE DETECTORS. REPLACED 3A SMOKE DETECTOR. NO REPEATS SINCE OR IGINAL. THIS SDR CREATED IN RESPONSE TO REJECTION OF SDR # 2007UALA00693 ASKING FOR SEPARATE WRITEUPS FOR SMOKE DETECTO RS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010200188 20080102 00188 EA 2008 1 2 A6WA200740670 1 20071128 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 433AW 7289 ON PAX DOOR, CRACK FOUND ON PASSENGER EDGE MEMBER. (M) PAX DOOR ON PASSENGER EDGE MEMBER REPAIRED IAW REO 601R-52-11-27 9. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008010700037 20080107 00037 NM 2008 1 7 2007UALA05149 1 20071218 A 3397 794640 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY LIGHT ROW 4E INOPERATIVE. REPLACED CABLE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010900002 20080109 00002 NM 2008 1 9 2007UALA05190 1 20071220 A 2560 9531001REV2 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FLASHLIGHT DISCHARGED A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 824UA 965 F/A FLASHLIGHT IS NOT FLASHING. *S/D* BATTERY FAILURE. REPLACED BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011500044 20080115 00044 EU 2008 1 15 NSVA20070096 1 20070411 A 7600 STOP SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FLIGHT IDLE INTERMITTENT A NSVA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 27 193CJ 193 FI IDLE STOP LT INTERMITTENT. PERFORMED ADJUSTMENT TEST OF THE FLIGHT IDLE STEP SYSTEM IAW SAAB 340 AMM 76-10-60. OPER ATIONAL TEST PASSED. 2 L 7 2 4T 4 T RT A52EU E8NE 2008012200163 20080122 00163 EA 2008 1 22 A6WA200740689 1 20071211 A 5210 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 432AW 7257 BRACKET CRACK ON LOWER PAX DOOR EDGE (LOCK MECHANISM AREA) AFT STA 334.00. CRACKED BRACKET ON PAX DOOR BTW FS 329.5 TO F S 338.0 IS REPLACED IAW SRM 51-41-04. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200219 20080212 00219 EA 2008 2 12 A6WA200740713 1 20071227 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 426AW 7699 A/C CONNECTOR BOX STRUCTURE AFT INTERNCOSTAL CRACKED. AC CONNECTOR BOX STRUCTURE AFT INTERCOSTAL REMOVED AND FABRICATED IAW SRM 51-24-16, ALODINE IAW 51-21-11 AND INSTALLED IAW SRM 51-42-06, 51-42-13, 51-42-20. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 20080808 NE 2008 8 8 M7K2008F00127 2 20071105 A 7261 B-NUT UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ENGINE OIL LEAKING E M7KA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 19 816MH 4038 23096 HOSE FOUND TO BE LEAKING NOT FROM THE B-NUT BUT A THE FITTING JUNCTION WITH THE HOSE MATERIAL. NEW REPLACEMENT HOSE INS TALLED AND NO FURTHER LEAKAGE NOTED. IN 55,000 FLIGHT HOURS THIS IS THE ONLY PROBLEM WE HAVE HAD WITH THIS HOSE. LEAK WAS CONSIDERED MINOR. (K) 1 G 7 2 3U 3 U H9EU E00054EN 2007040200235 20070402 00235 EU 2007 4 2 07FDEA01048 1 20070321 A 5320 A53970875201 COVER PLATE AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CHAFED A FDEA O OTHER O OTHER UK UNKNOWN 1 SO 25 748FD 633 TORSION BOX COVER PLATE MARKS AT EMERGENCY EXIT DOOR RT. REWORK WAS PERFORMED BY BLEND OUT, HFEC INSPECTION AND FLAP PE ENING IAW EA 6-5316-106394 AND RAS/DATLS/0003542/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2007071900376 20070719 00376 EU 2007 7 19 F3LA200700177 1 20070712 A 5321 FLOOR PANEL AIRBUS A318 A318111 3940019 EU FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 807FR 5281 2276 DURING C-2 CHECK, INSPECTION REPORTED PUNCTURE ON TOPSIDE OF AFT CARGO COMPARTMENT FLOOR PANEL 161QF. REPAIRED AFT CARG O COMPARTMENT FLOOR PANEL 161QF IAW SRM 53-02-00, FIG 204. 2 L 7 2 4F RT 2007100400091 20071004 00091 EU 2007 10 4 07FDEA04151 1 20070921 A 5310 A53985250204 COUPLING AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 DAMAGED COUPLING AT STRG 4 LT BETWEEN FRAME 87-88. REPLACEMENT OF COUPLING IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007082300290 20070823 00290 EU 2007 8 23 07FDEA02952 1 20070816 A 5313 104163ITL STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 405FE 237 AFT PIT BETWEEN FRAME 66 AND 65 STRINGER 46L CORRODED REMOVED CORRRODED STRINGER. FABBED REPAIR PARTS. INSTALLED REPAI R PARTS PER A310-200 51-40-21, 53-10-14 PG 203, 51-21-10, 51-23-10. 2 L 7 2 4F RT A35EU 2007030700164 20070307 00164 WP 2007 3 7 IXXA07SMN031S 1 20070113 A 5753 SKIN DOUG DC8 DC871F 302199D WP TE FLAP MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 820BX 89079 2994 46065 DURING ROUTINE C CHECK INSPECTION FOUND LEFT HAND OUTBOARD FLAP HAS A NON STANDARD REPAIR FROM STATION XF384.000 TO STAT ION XF390.000. REMOVED EXISTING SKIN PANEL WITH NON STANDARD REPAIR. FABRICATED NEW SKIN PANEL. BONDED BOTH PARTS. WI TH HYSOL. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN PANEL INTERIOR SURFACE. APPLIED SEALANT TO FAYING SURFACES. DC 8 INSTALLED NEW SKIN PANEL IAW DC8 SRM 51-1-21, DC8 SRM 57-7-1 FIGURE 4 TR NUMBER 57-94 DATED 10-01-02, DC8 SRM 57-1-0 P AGE 1, DC8 SRM 57-7-1 FIGURE 4 ITEMS "A" AND "Q", DC8 SRM 51-1-9, DC8 SRM 51-1-8B AND SRM 51-1-11. 2 L 7 4 4F RT 4A25 2007121900086 20071219 00086 EU 2007 12 19 SUP200733001 1 20071123 A 2910 HYDRAULIC SYSTEM SAAB SF340 340B 7860101 EU CONTAMINATED A SIMA O OTHER O OTHER LD LANDING 1 SW 21 250AE 340B250 CREW REPORTED FLAP WOULD NOT EXTEND AT ALL FOR LANDING. CREW LANDED AT 0 DEGREE FLAPS. INSPECTED AND FOUND AIR IN HYDR AULIC SYSTEM. BLEED SYSTEM FCF GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2007071300258 20070713 00258 NM 2007 7 13 AWXA200700803 1 20070708 A 5310 6555074 GUSSET BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 PHX - MAJOR REPAIR - CRACK AT FIRST OFFICERS NR 1 WINDOW POST GUSSET UPPER OUTBOARD CORNER, BS 196.5 - BS 203.8, S9R - S10R. REPAIRED FIRST OFFICERS NR 1 WINDOW POST GUSSET UPPER OUTBOARD CORNER, BS 196.5 - BS 203.8, S9R - S10R IAW B737-3 00 SRM 53-10-01-2R. 2 L 7 2 4F RT A16WE 2007062200112 20070622 00112 NM 2007 6 22 HALA0700252 1 20070611 A 3030 7705401 RELAY BOEING 767 7673CB 1385187 NM PITOT HEAT FAILED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 590HA 33467 ETOPS SIGNIFICANT SYSTEM, EICAS MSG F/O PITOT DISPLAYED F/O PITOT PROBE HEAT LGT ILLUM. REMOVED AND REPLACED RELAY K310 , OPS CHECK OK PER AM 30-31-00. 2 L 7 2 4F RT A1NM 2007042500310 20070425 00310 EU 2007 4 25 07FDEA01425 1 20070411 A 5730 A57150751 SKIN AIRBUS 310 A310324 3930206 EU LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 814FD 534 CORROSION ON PYLON REINFORCING PLATE ON THE LT WING, UNDERNEATH THE SPIGOT FITTING. REPAIR PERFORMED BY BLEND OUT THE C ORROSION IAW EA 6-5720-103303 AND RAS/BAE/1002985/2006 ISSUE "A". 2 L 7 2 4F RT A35EU 2008010900254 20080109 00254 EA 2008 1 9 TRAX200800007 1 20071229 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 882AS 7503 ASD HANDLE CRACKED. 2 L 7 2 4F RT A21EA 2007091400120 20070914 00120 EU 2007 9 14 F3LA200700212 1 20070901 A 5411 SUPPORT ANGLE AIRBUS A319 A319112 3930323 EU RT NACELLE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 909FR 5694 1761 DURING C4/S1 CHECK, INSPECTION REPORTED RT ENGINE PYLON SUPPORT ANGLE THAT ATTACHES PYLON PANELS 423DL AND 424CR AT RIB 5 CRACKED (AREA AROUND AFT SCREW HOLE). REMOVED AND FABRICATED REPLACEMENT SUPPORT ANGLE IAW SRM'S 54-52-12, P28, 51-31 -00, P44,51-44-11, 51-42-11 AND 51-72-11, AND AIRBUS DRAWING S2 D54630462. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-42-11 , P7. 2 L 7 2 4F RT A28NM 2008010800238 20080108 00238 NM 2008 1 8 HALA0700559 1 20071227 A 3000 SWITCH BOEING 767 767332 1382001 NM ANTI ICE SYS UNKNOWN A HALA O OTHER O OTHER CL CLIMB 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, EICAS MSG R ENG ANTI-ICE DISPLAYED AND ENG VALVE LIGHT ILLUM W/SWITCH SEL ON. VALVE LIGHT/EIC AS MSG ON IN CLIMB AFTER SELECTION ON BEFORE T/O. SYS ON FOR 15-20 MIN BEFORE VALVE LIGHT ILLUMINATED, LIGHT MSG INTERM ITTENT AFTER THAT. REPLACED RIGHT ENG ANTI-ICE SWITCH. GND RUN UP, OPS CK OK. 2 L 7 2 4F RT A1NM 2007080200042 20070802 00042 2007 8 2 DL76G070952 4 20070723 A 3140 8221033100 COMPUTER BOEING 767 767332 1382001 NM LT EICAS FAULTED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 175DZ 29696 LT EICAS COMPUTER FAULT ON DEPARTURE. LEFT EICAS COMPUTER REPLACED TESTED IAW 34-41-02-924-001 OK. SOFTWARE INSTALLED IAW AMM 31-41-92-201. 2 L 7 2 4F RT A1NM 2007031500066 20070315 00066 NM 2007 3 15 07FDEA00777 1 20070312 A 5100 SKIN BOEING 727 727225 1384077 NM UNKNOWN A FDEA K NONE O OTHER NR NOT REPORTED 1 SO 25 462FE 22550 THE MAIN CARGO DOOR HAS 4 EXTERNAL DOUBLERS ON ITS INTERNAL SKIN ALONG THE TOP EDGE AT STATIONS 520, 540, 560, AND 580. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR. 2 L 7 3 4F A3WE 2007122100051 20071221 00051 WP 2007 12 21 ABXA070420 1 20071114 A 5312 5910130392 BULKHEAD DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 AFT PRESSURE BULKHEAD TEE NR 2 WAS CRACKED APPROXIMATELY .75 INCHES LONG AT LONGERON 14 RIGHT. REMOVED AND REPLACED TEE CAP IN ACCORDANCE WITH DC9 SRM. 2 L 7 2 4F A6WE 2007013100259 20070131 00259 EU 2007 1 31 07FDEA00206 1 20070131 A 7830 THRUST REVERSER AIRBUS 300 A300F4605R 3930327 EU NR 2 ENGINE INOPERATIVE A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 668FE 772 AT 75 KNOTS, THE NR 2 ENG REV PRESSURE LIGHT CAME ON. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPI RATION: 10FEB07 "MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) NR 2 THRUST REVERSER, INOP. THRUST REVERSER IS DEACTIVATED I N FORWARD THRUST POSITION." REMOVED AND REPLACED NR 2 RT REVERSER CTR DRIVE UNIT IN REFERENCE TO A300-600 M/M 78-31-01- 4-05.OP CHECKED GOOD. 2 L 7 2 4F RT A35EU 2007091900049 20070919 00049 NM 2007 9 19 07FDEA03715 1 20070913 A 5315 652083817 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 262FE 21624 UPPER DECK FLOORBEAM, STA 1130, LBL 18, WL 208, CORROSION AROUND 1 EA FASTENER HOLE REMOVED CORROSION, REF SRM 51-10-6, ORIGINAL MATERIAL .160" AFTER BLENDING, MATERIAL REMAINING .147" AND IS WITHIN LIMITS PER EA NR 7-5310-113090, SHOT PE ENED AREA REF SOP 20-10-3. TREAT AND PRIMED REF SRM 51-10-2. LEVEL 1 CORROSION. 2 L 7 3 4F RT A3WE 2007032900004 20070329 00004 NM 2007 3 29 QXEA200700421 1 20070313 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 528-597 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - SEAT TRACK NR 9 HAS MINOR SCRATCHES AT STATION 528, 540, 597. REPAIRED IAW RD8-53-4936 AND RD8-53-4472, SRM 51 -40-11, 51-20-36. 2 H 7 2 4T RT A13NM 2008010800112 20080108 00112 NM 2008 1 8 SWAA076455 1 20071221 A 3350 101331 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 496WN 32478 EMERGENCY EXIT LIGHT LENS MISSING AT ROW 2. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2007050300331 20070503 00331 EU 2007 5 3 2007UALA01291 1 20070424 A 3350 COVER AIRBUS 320 A320232 3930326 EU CABIN BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 409UA 462 SEAT 3C FWD EEL LAMP COVER BROKEN OFF. [SUP 05-16-07] REPLACED EEL LIGHT ASSY CRUSHED BY FOOD CARTS SUSPECTED, OPS GOO D. 2 L 7 2 4F RT A28NM 2007012200154 20070122 00154 NM 2007 1 22 2007UALA00068 1 20070109 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 171UA 24322 EEL INOP AT SEAT 5E AFT SECTION AND ROW 46L. REPLACED EEL LIGHT ASSY. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007012600276 20070126 00276 NM 2007 1 26 KCSA071012 1 20070115 A 5320 STIFFENER BOEING 747 747209F 1384800 NM PWA JT9 JT9D7R4G2 52054 NE FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 22299 STA 740 LBL24 HAS CRACKED STIFFENER .5 INCH. 2 L 7 4 4F 4 F RT A20WE E3NE 2007013100150 20070131 00150 CE 2007 1 31 DXTA200701875 1 20070123 A 3230 S430087 UPLOCK SWITCH CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE RT MLG MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 372QS 5600372 RT MAIN GEAR UPLOCK FAILED. HAD A GEAR UNLOCK LIGHT ON WITH A HYDRAULIC PTRS ON LIGHT. RAN THE HYDRAULIC PRES ON CK LIS T AND WHEN WE PULLED THE GEAR CONTROL (CB) AS DIRECTED THE RT MAIN GEAR EXTENDED. THE GEAR HANDLE WAS THEN PLACED IN THE GEAR DOWN POS. RESET THE (CB) AND GOT 3 GREEN LIGHTS, NO DIVERT. REMOVED FAULTY RT MAIN GEAR UPLOCK SWITCH P/N S430087 . INSTALLED NEW SWITCH P/N 65430087. OP CHECK GOOD, ALL WORK PERFORMED IAW CESSNA CE-560 MAINT MANUAL CHAP'S 32-61-00 AND 32-60-00, FOR DETAILS REF FAS W/O 07-183 2 L 7 2 4F 4 F RT A22CE E25EA 2007022100207 20070221 00207 NM 2007 2 21 2007UALA00293 1 20070202 A 3350 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BATTERY CHARGER BLOWN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY LIGHTS INOP AT RT OVERWING 2 AFT ASSEMBLIES. REPLACED ONE FUSE ON BATTERY CHARGER. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022300141 20070223 00141 EU 2007 2 23 2007UALA00470 1 20070215 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 430UA 568 STRINGER 41 RT HAS 3 EACH AREAS OF CORROSION AT FRAME 29, UNDER FRAME 32 AND BETWEEN FRAMES 33 & 34. MAJOR REPAIR ACCOM PLISHED: INSTALLED 3 EACH SPLICE REPAIRS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007021600021 20070216 00021 2007 2 16 2007UALA00335 4 20070206 A 2565 LINE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L2 DOOR SLIDE EXPOSED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 DOOR 2L SLIDE MOORING LINE PARTLY EXPOSED. PUT MOORING LINE BACK INTO VELCRO LINER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007030100113 20070301 00113 NM 2007 3 1 2007UALA00566 1 20070221 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 FOUND SEAT 3J AFT EEL CABLE CONNECTOR BROKEN, EEL INOPERATIVE. REPLACED WITH NEW CONNECTOR PLUG. OP CHECKED NORMAL 2 L 7 4 4F 4 F RT A20WE E24NE 2007030600088 20070306 00088 NM 2007 3 6 2007UALA00618 1 20070228 A 5210 HINGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 557UA 26653 DOOR 2R UPPER HINGE CUTOUT IS CRACKED. MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT DAMAGE & ACCMP'D INSURANCE CUT. NO CRACK S FOUND. FABRICATED & INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022600104 20070226 00104 EA 2007 2 26 VNAA0702002 1 20070201 A 2420 755469E IDG CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 1 FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 260JS 6076 7957 CREW REPORTED AN IDG CAS MESSAGE ON TAKEOFF ROLL. CREW REJECTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. MAINTEN ANCE REMOVED AND REPLACED THE NR 1 IDG IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SE RVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007031200154 20070312 00154 NM 2007 3 12 KNNA200700011 1 20070205 A 5311 2024T32 FRAME BOEING 737 737297 1384480 NM PWA JT8 JT8D9 52048 NE BS 178 MISDRILLED A KNNA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 25 147AW 22630 FOUND MISDRILLED HOLE AT SKIN OF SIDE FRAME, WL 212 LT, STA 179. FOUND PROVIDE INSTRUCTIONS ON REPAIR OF MISDRILLED FAS TENER HOLE BS 178 W/L 212. 2 L 7 2 4F 4 F A16WE E2EA 2007031900047 20070319 00047 NE 2007 3 19 COMA0760241 2 20070309 A 7230 COMPRESSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ENGINE CONTAMINATED A COMA A UNSCHED LANDING C B F.O.D. SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 927CA 7031 FLIGHT 5307 - DURING CLIMBOUT OF TUL EVIDENCE OF SMOKE IN CABIN AND COCKPIT, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. PERFORMED ENGINE RUNS TO REMOVE RESIDUAL COMPRESSOR WASH FLUID. 2 L 7 2 4F 4 F RT A21EA E15NE 2007032000091 20070320 00091 CE 2007 3 20 GLBA20060923 1 20070316 A 5520 STRUCTURE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A6 52043 EA RT ELEVATOR CRUSHED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 210GL UE210 RT ELEVATOR TRAILING EDGE DAMAGED APPROXIMATELY 9 INCHES OB OF TRIM TAB. DAMAGED AREA APPROXIMATELY 1 INCH BY 1.2500 INC H. MAINTENANCE REMOVED 2 INCH BY 1.5 INCH AREA OF TRAILING EDGE SKIN AND INSTALLED INSERTION REPAIR PER BEECH 1900D SRM 55-90-03. RII INSPECTION COMPLIED WITH PER T.C. 8.2.1. 2 L 7 2 4T 3 T RT A24CE E4EA 2007032100006 20070321 00006 2007 3 21 2007UALA00746 4 20070312 A 2565 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE ARM LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 523UA 24932 DOOR 3R SLIDE ARMED LIGHT INOPERATIVE. [SUP 05-29-07] RELAMPED. OP CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032600169 20070326 00169 NE 2007 3 26 AWXA200700390 2 20070319 A 7200 V2500A1 ENGINE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE RIGHT FIRE A AWXA F A ACTIVATE FIRE EXT. UNSCHED LANDING A E FLAME/FIRE VIBRATION/BUFFET CL CLIMB 1 WP 28 626AW 41052 8684 65 0041 LAS - ESD - CREW REPORTED DURING CLIMB THEY HEARD A LOUD BANG FOLLOWED BY A RISING EGT INDICATION ON THE RIGHT ENGINE. THE FLIGHT ATTENDANTS REPORTED SPARKS AND FLAMES COMING FROM THE RIGHT ENGINE. THE ENGINE SHUT DOWN AND THE CREW DISCHA RGED THE FIRE BOTTLE. THE CREW DECLARED AN EMERGENCY AND RETURNED TO LAS. THE PASSENGERS DID NOT BRACE. MX REMOVED AN D REPLACED THE RIGHT ENGINE. OPERATIONAL CHECK WAS GOOD DURING ENGINE RUN. 2 L 7 2 4F 4 F RT A28NM E311NE 2007040300010 20070403 00010 EA 2007 4 3 N6WA0070301 1 20070324 A 3350 LENS CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE EMERGENCY LIGHT MISSING A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 163 10255 MX-STL-LENS COVER MISSING NEXT TO SERVICE DOOR NEAR THE FLOOR. DEFERRED LIGHT IAW MEL 33-51-01-2B. 2 L 7 2 4F 4 F RT A21EA E15NE 2007041900030 20070419 00030 NM 2007 4 19 MWEA070086 1 20070411 A 7830 7150922 FRAME BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 914ME 55177 LT THRUST REVERSER LOWER DOOR, ZEE CHANNEL AT STATION 26 CRACKED AT OB END. FABRICATED AND INSTALLED ZEE FRAME. 2 L 7 2 4F 4 F TR A6WE E00061EN 2007050800066 20070508 00066 NM 2007 5 8 2007UALA01359 1 20070427 A 5414 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 NR 2 PYLON INBOARD SKIN IS CRACKED AT THE MOST FWD ACCESS HOLE, 2:00 O'CLOCK POSITION. [SUP 06-06-07] ACCOMPLISHED REP AIR WITH UA ENGINEERING SPECIFICATION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007041900100 20070419 00100 NM 2007 4 19 2007UALA01082 1 20070409 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EEL INOPERATIVE SEAT 5A AFT SECTION. *S/D* REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007050800139 20070508 00139 EU 2007 5 8 PSNA070303 1 20070322 A 7931 PRESSURE SWITCH SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE OIL SYSTEM MALFUNCTIONED A PNSA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 AL 03 109XJ 340A109 GEE367346 PILOT ABORTED TAKEOFF DUE TO ENGINE OIL PRESSURE LOW MASTER WARNING LIGHT RETURNED TO GATE. REMOVED AND REPLACED ENGINE OIL PRESSURE DIFFERENTIAL SWITCH. 2 L 7 2 4T 4 T RT A52EU E8NE6 2007050800055 20070508 00055 NM 2007 5 8 2007UALA01387 1 20070502 A 5210 LEVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR STIFF A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 DOOR 1L DOES NOT ARM, LEVER IS STIFF. [SUP 06-06-07] GIRT BAR LIFT SPRING WAS JAMMED REPLACED LEFT DOOR GIRT BAR AND BAR LOCK AND REPLACED LEFT DOOR ASSIST BOTTLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050900142 20070509 00142 NM 2007 5 9 2007UALA01339 1 20070428 A 2560 SCREW BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 337UA 24241 FWD GALLEY DOOR EVAC SLIDE GIRT BAR FWD STOW BRACKET ON COVER HAS TWO LOOSE SCREWS. ALSO, TOO MUCH MATERIAL IS HANGING OUT OF THE CONTAINER. [SUP 05-16-07] SECURED SCREWS AND ADJUST MATERIAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007051600106 20070516 00106 SW 2007 5 16 0508079100 1 20070508 A 2810 TANK BOLKMS 117 BK117C2 5626002 SW TMECA ARRIEL ARRIEL1E 60030 NE MAIN CONTAMINATED E E3MA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 03 307ME 96 9100 FOUND A -PIG MAT- IN THE MAIN FUEL TANK. 1 G 7 2 3U 3 U H13EU E19EU 2007060700044 20070607 00044 NM 2007 6 7 WRLA2007076 1 20070531 A 2520 CONTROL UNIT DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE SEAT 14G SMOKE A WRLA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 278WA 48746 FNLU/KIAH FLT 101 05/31/07. SEAT 14G CONTROL INOPERATIVE. SMOKE AND ODOR COMING FROM SEAT WHEN SEAT ACTIVATED. ISOLAT ED TO POWER CONTROL UNIT. REMOVED POWER CONTROL UNIT, DEACTIVATED SEAT ELECTRICALLY AS PRECAUTIONARY MEASURE. PLACED S EAT ON DMI M25JU0107-5, MEL 25-22-01-01. [SUP 06-11-07] REMOVED AND REPLACED SEAT CONTROL BOX (SCP) AND LEG REST MOTOR ON SEAT 14DG. OPS CHECK GOOD. THIS CLEARS DMI. SCP P/N:840102-409 S/N:NSN AND LEGREST ACTUATOR P/N:841413-404 S/N:4616. 2 L 7 3 4F 4 F RT A22WE E24NE 2007052900180 20070529 00180 EA 2007 5 29 PNSA070505 2 20070519 A 7314 LW15473 PUMP PIPER PA32 PA32301 7103207 SO LYC O540 IO540K1G5 41532 EA FUEL SYSTEM MALFUNCTIONED E PNSA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 AL 03 8259V 420 420 328006097 LOW FUEL FLOW. REMOVED AND REPLACED FUEL PUMP. 1 L 7 1 3O 3 O A3SO 1E4 2007053000015 20070530 00015 NM 2007 5 30 ASMF200704016 1 20070430 A 2131 CONTROLLER DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE CABIN PRESSURE MALFUNCTIONED W ASMF A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 23 161PL 12144 12144 49764 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, CAPTAIN REPORTED LOSS OF CABIN PRESSURE CONTROL AT 32000 FEET; EMERGENCY DESC ENT PROCEDURE WAS PERFORMED AND OXYGEN MASKS WERE ACTIVATED. DURING MAINTENANCE CHECK, RT AUGMENTATION VALVE LINES WERE REPAIRED IAW MM 20-12-01 AND ADJUSTMENT / TEST CABIN PRESSURE CONTROL WAS PERFORMED IAW MM 21-32-00; THE RT COMPRESSOR D ISCHARGE THERMAL SWITCH CONNECTOR WAS RECONNECTED AND THE LT COMPRESSOR DISCHARGE THERMAL SWITCH WAS RETIGHTEN IAW MM 21 -31-05. NO OVERWEIGHT INSPECTION WAS REQUIRED, THE APPROVED FERRY FLIGHT WAS PERFORMED. DURING OVERNIGHT CHECK, THE CA BIN PRESSURE CONTROL NR 1 WAS REPLACED IAW 21-32-03, TESTED CORRECT; THE RT PRESSURE REGULATOR VALVE WAS REPLACED IAW MM 2 L 7 2 4F 4 F RT A6WE E9NE 2007051700109 20070517 00109 NM 2007 5 17 2007UALA01441 1 20070507 A 5310 STRUCTURE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE BS 285 S2L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 793UA 26946 STA 285.5 STR 2L IS DAMAGED. [SUP 06-01-07] MAJOR REPAIR ACCOMPLISHED DUE TO LIGHTNING STRIKE DAMAGE ON UPPER FUSE STA 285.5 STR 2L. REPAIR ACCOMPLISHED AND INSPECTED. A/C OK FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007060600186 20070606 00186 GL 2007 6 6 LR7A07031 2 20070525 A 7200 501D22A ENGINE LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL NR 4 FLAMED OUT A LR7A K NONE X ENGINE FLAMEOUT DE DESCENT 1 AL 03 403LC 26 4590 550574 FLIGHT CREW REPORTED, THE NR 4 ENGINE FLAMED OUT AND WENT INTO FEATHER ON DESCENT TO LICZ. MAINTENANCE REMOVED AND REPL ACED NR 4 PROPELLER VALVE HOUSING ON FLIGHT LOG PAGE 26683 WITH UNSATISFACTORY RESULTS. AIRCRAFT FERRIED FROM LICZ TO E TAR, LOG PAGE 26684. ENGINE CHANGE ACCOMPLISHED BY MAINTENANCE IN ETAR ON LOG PAGE 26685. SUSPECT FAULTY NTS PLUNGER I N REDUCTION GEARBOX. FAILURE ANALYISIS UNDER INVESTIGATION. 2 H 7 4 4T 4 T A1SO E282 2007052300042 20070523 00042 2007 5 23 2007UALA01577 4 20070520 A 2565 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L3 DOOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 562UA 26664 CREW REPORT: DOOR 3L SLIDE LIGHT WON`T ILLUM WITH DOOR ARMED. [06-20-07] SLIDE LIGHT RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052300054 20070523 00054 EU 2007 5 23 2007UALA01488 1 20070511 A 3350 32145410 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 481UA 1559 EMERGENCY LIGHT TEST FAILED. THE -EPSU INT LOAD EMER L- DISPLAYED. REPLACED BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061900280 20070619 00280 NM 2007 6 19 2007UALA01825 1 20070604 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 FWD PIT DOOR CUTOUT, AFT FRAME CRACKED NEAR LOWER STOP FITTING. MAJOR REPAIR ACCOMPLISHED: REPLACED DAMAGED FRAME AT B S 492 WITH NEW FRAME P/N 65-20723U54. 2 L 7 2 4F 4 F RT A16WE E21EU 2007060500282 20070605 00282 NM 2007 6 5 2007UALA01701 1 20070526 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EMERGENCY LIGHT INOP. UPPER DECK ROW 13 CEILING LIGHT. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062600213 20070626 00213 NM 2007 6 26 2007UALA02037 1 20070615 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1340 S25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 MAIN FRAME, STA 1340 LEFT SIDE BETWEEN STR 25L, FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED -J- ANGLE REPAIR AND NEW SPLICE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062200116 20070622 00116 NM 2007 6 22 HALA0700254 1 20070614 A 3150 WARNING SYSTEM BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE COCKPIT MALFUNCTIONED A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 580HA 28140 ETOPS SIGNIFICANT SYSTEM, L ENG CONTROL ILLUMINATED AFTER START EICAS WARNING. BIT L PIMU PER FIM NO FAULTS RAN ENG OPE RATION NML 73 2100. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071000454 20070710 00454 NE 2007 7 10 2007UALA02308 2 20070626 A 7200 BLADE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A UALA O OTHER M OVER TEMP TO TAKEOFF 1 WP 29 501UA 24622 717999 NR 1 ENG EGT EXCEEDED 645 DEGREES, NOT DURING SURGE. PEAK EGT WAS 659. CREW COMMENTS: MAX TO IN DEN 10 SEC EXCEEDANCE . [08-08-07] ACCOMPLISHED BOROSCOPE INSPECTION. NR 1 ENGINE FAILED BORO; FOUND 1 EA BLADE HAVING SULFIDATION WITH P ARENT METAL CRACK. MEASURED DAMAGE APPROX 0.500 SQ.IN. NR 1 ENGINE REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072300009 20070723 00009 NM 2007 7 23 2007UALA02530 1 20070708 A 2611 SMOKE WARNING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT LAVATORY INTERMITTENT A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 302UA 23643 SMOKE ALARM ON INTERMITTANTLY AFT LAVATORY. [07-27-07] ALL OPERATIONAL CHECKS WERE NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007073100094 20070731 00094 NM 2007 7 31 2007UALA02710 1 20070717 A 3530 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 PBE BY DOOR 2L IS RIPPED OPEN. 09-07-07 REPLACED SMOKE HOOD OF OXYGEN MASK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071000435 20070710 00435 EU 2007 7 10 2007UALA02296 1 20070628 A 3350 CIRCUIT BREAKER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN POPPED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 417UA 483 EXIT PATH LIGHTING DOES NOT ILLUMINATE ROWS 12, 13, 14, 18, 19 & 20. RESET CIRCUIT BREAKER & TESTED EMERGENCY LIGHTS, O PS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071100142 20070711 00142 SO 2007 7 11 N93A26062007 1 20070626 A 3250 716483 TILLER GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE UNKNOWN E N93A K NONE O OTHER TX TAXI/GRND HDL 1 SO 13 516QS 658 ON TOUCHDOWN, CREW RECEIVED NOSE WHEEL STEERING FAIL MESSAGE. 2 L 7 2 4F 4 F RT A12EA E00057EN 2007073100038 20070731 00038 NM 2007 7 31 2007UALA02701 1 20070717 A 3350 8100133801 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 37G BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 214UA 30220 SEAT PROXIMITY EEL LIGHT BROKEN AT SEAT 37G. REPLACED PROXIMITY EEL LIGHT ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007071700036 20070717 00036 EA 2007 7 17 A6WA200740320 1 20070618 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 460AW 7867 FLOOR SUPPORT ANGLE AT FS 621, WL 73, LBL 27 - 45 IS CRACKED .5 INCHES LONG. MAINTENANCE REPAIRED FLOOR SUPPORT ANGLE I AW REO 601R-53-61-117, REV C. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007072300064 20070723 00064 EU 2007 7 23 2007UALA02575 1 20070711 A 2611 SMOKE WARNING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE E/E BAY UNKNOWN A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 429UA 539 FLIGHT DIVERTED DUE TO AVIONICS ECAM MSG SHOWING SMOKE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007072500014 20070725 00014 EU 2007 7 25 SWAA073522 2 20070718 A 7200 3321A1000 ENGINE BOEING 737 7373H4 1384600 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 DISTORTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 857193 DURING SCHEDULED HC1 CHECK, FOUND NR 1 ENGINE 1ST STAGE LPT BLADES DISTORTED. REMOVED AND REPLACED NR 1 ENGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007080800029 20070808 00029 SO 2007 8 8 N93A19072007 1 20070719 A 3250 1159SCH4023 SHUTOFF VALVE GULSTM GIV GIVG400 3980204 SO RROYCE TAY TAY6118 EU NLG STEERING FAILED E N93A O OTHER J WARNING INDICATION DE DESCENT 1 SO 13 413QS 1521 NOSE WHEEL STEERING FAIL MESSAGE, FOUND STEERING SHUTOFF VALVE INOP. 2 L 7 2 4F 4 F RT A12EA E25NE 2007080600014 20070806 00014 NE 2007 8 6 2007UALA02755 2 20070720 A 7261 BEARING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE LEAKING A UALA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 538UA 25222 OIL ODOR IN CABIN. ON TROUBLE SHOOTING FOUND ODOR COMING FROM RT PACK WITH NR 2 ENGINE BLEED ON. SUSPECTED SKYDROL S MELL IN CABIN AFTER FINDING LEFT HYDRAULIC SYSTEM OVER SERVICED., NO OIL FOUND IN DUCTS. AFTER FURTHER TROUBLE SHOOTIN G, CONFIRMED NR 2 ENGINE HAD SMALL AMOUNT OF OIL SEEPAGE FROM NR 3 BEARING COMPARTMENT. ENGINE REMOVED AND ROUTED TO ENG INE SHOP FOR REPAIR. RAN ENGINES AT POWER. ACCOMPLISHED A/C PACK BURNOUT, NO ODOR NOTED AFTER PACK BURNOUT, REPLACED BOTH RECIRCULATION FILTERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080700013 20070807 00013 NM 2007 8 7 2007UALA02834 1 20070724 A 3150 WARNING HORN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE ACTIVATED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 313UA 23674 DURING CLIMB ENCOUNTERED T/O WARNING HORN WITH FLAPS RETRACTED. REPLACED M983 CARD AND ACP CHECKS OF CARDS M983, M989, M990, M991, AND M1110 PER MM32-09-20, ALSO ACP AURAL WARNING SYS, AND CHECKED GAP ON GROUND SAFETY SENSOR, ALL CHECK O K. NOT CONSIDERED A DIVERSION DUE TO NEAREST SUITABLE AIRPORT BEING ACTUAL DESTINATION. 2 L 7 2 4F 4 F RT A16WE E2GL 2007080700028 20070807 00028 NM 2007 8 7 2007UALA02849 1 20070726 A 3350 794640 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 WALL EEL INOP, MID LAV CROSS AISLE. FOUNDED DISCONNECTED. RECONNECTED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080800081 20070808 00081 CE 2007 8 8 AMWA06032S 1 20070725 A 5311 12943003619 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 318 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007082100230 20070821 00230 CE 2007 8 21 DJFA2007091 1 20070810 A 3260 MS243311 DOWNLOCK SWITCH BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE LT MLG INOPERATIVE E DJFA L ABORTED APPROACH P NO WARNING INDICATION LD LANDING 1 EA 23 463LX 1530 RK426 ON LANDING, CREW REPORTED NO GEAR DOWN AND LOCKED INDICATION FOR THE LT MLG. BULB TEST SHOWED THE BULB TO BE FUNCTIONAL . MAINTENANCE FOUND THE LT MLG DOWN LOCK SW INOPERATIVE. THE SWITCH WAS REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007082800009 20070828 00009 NM 2007 8 28 2007UALA03215 1 20070816 A 5320 THRESHOLD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 819 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 327UA 24147 AFT PIT DOOR THRESHOLD CORRODED: WEB IS CORRODED AT STA 819 RLB 21 APPROX 2 IN FROM UPPER FLANGE. MAJOR REPAIR ACP AFT CARGO PIT DOOR THRESHOLD WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2007083100116 20070831 00116 NM 2007 8 31 2007UALA03296 1 20070821 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 CEILING EMERGENCY LIGHTS INOP AT ROWS 13, 17 & 48R. 08-31-07 RELAMPED ALL THREE POSITIONS. ALL OP CHECKOK FOR SERVIC E. 2 L 7 4 4F 4 F RT A20WE E24NE 2007083100087 20070831 00087 NM 2007 8 31 2007UALA03271 1 20070820 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 DOOR 4R EMERGENCY EXIT SLIDE, EXIT LIGHT INOPERATIVE. 08-31-07 RELAMPED, OP CHECKED OK REF MM 33-51-12. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090600016 20070906 00016 NM 2007 9 6 TAMF20070021S 1 20070822 A 5330 SKIN BOEING 767 767200 1385120 NM PWA PT6 PT6A114A 52043 NE BS 1339 S17L DENTED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 768QT 23803 DURING INSPECTION OF (C2) CHECK WAS FOUND A DENT ON LAP SKIN STA 1339 STR 17 - LT. DAMAGE ON LIMITS IAW EWO 767-53-05 A ND BOEING SERVICE REQUEST 1-526586182. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 3 T RT A1NM E4EA 2007091800162 20070918 00162 NM 2007 9 18 2007UALA03544 1 20070903 A 2824 FLOAT VALVE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CTR FUEL TANK STUCK A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 783UA 26950 FUEL IMBALANCE EXIST WHEN CTR TANK FUEL IS PRESENT. RT MAIN RECEIVING EARLY TRANSFER FROM SCAVENGE PUMPS. SUSPECT CTR TANK SCAVENGE FLOAT VLV STUCK IN OPEN POSITION AFTER T/S WITH FLT CREW. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007090700061 20070907 00061 NM 2007 9 7 2007UALA03503 1 20070830 A 5753 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU TE FLAPS DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 304UA 23665 RIGHT WING OUTBOARD TRAILING EDGE FOREFLAP SPLIT AND DELAMINATED AT INBOARD AFT EDGE. LEFT WING OUTBOARD TRAILING EDGE FOREFLAP GOUGED AT OUTBOARD LEADING EDGE. REPLACED THE LT & RT WING T/E FOREFLAPS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007091800217 20070918 00217 EU 2007 9 18 2007UALA03582 1 20070904 A 3510 MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 438UA 678 F/O'S MASK WILL NOT TEST. FOUND IMPROPER STOWAGE OF MASK. RESET THE FO MASK-TESTS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092000180 20070920 00180 NM 2007 9 20 2007UALA03624 1 20070907 A 2621 FIRE BOTTLE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FWD CARGO BAY DISCHARGED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 912UA 25290 DURING PANEL REPLACEMENT FOR POP SPILL FOUND 1ST BOTTLE FOR CARGO FIRE BOTTLE DISCHARGE LIGHT ON. OPENED PANEL IN FWD P IT AND FOUND BOTTLE DISCHARGED. REPLACED BOTH CARGO FIRE BOTTLES, DIVERTER VALVE, METERING VALVE, SQUIBS AND FILTERS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092000107 20070920 00107 NE 2007 9 20 NWAA073025805 2 20070907 A 7321 45100 POWER SUPPLY BOEING 757 757351 1384991 NM PWA 2037 PW2040 NE NR 1 ENGINE UNSERVICEABLE A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 585NW 14865 13422 32985 727173 DURING TAKEOFF ROLL, ENGINE NR 1 EPR "DROPPED OFF" AND L ENG PRIM CONT MSG ANNUNCIATED. TAKEOFF ABORTED AT 110 KNOTS. MAINTENANCE REPLACED THE PMA AND PERFORMED A HIGH ENERGY STOP INSPECTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2007090700056 20070907 00056 NM 2007 9 7 2007UALA03499 1 20070830 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 690 S2-3L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 520UA 24890 EXTERNAL FUSELAGE HAS HOLE IN SKIN AT BS 690 BETWEEN STR 2L-3L. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092500156 20070925 00156 CE 2007 9 25 DXTA200702492 1 20070921 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 348QS 5600348 EXCESSIVE BRAKE PRESSURE WAS REQUIRED TO STOP AIRCRAFT UNDER NORMAL TAXI SPEED. BRAKES WERE VERY SOFT AND SPONGY. BLED BRAKES & SERVICED RESERVOIR I/A/W C560 M.M 32-42-00. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2007092500427 20070925 00427 NM 2007 9 25 2007UALA03679 1 20070912 A 3350 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EEL AT 39 ABC INOPERATIVE. 10-05-07 RELAMPED EMERGENCY LIGHT. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007100200187 20071002 00187 NE 2007 10 2 MASA200700537 2 20070830 A 7200 PW123D ENGINE DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE UNKNOWN A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 991HA 1018 431 TM123333 TAKEOFF WARNING HORN SOUNDED DURING ENGINE POWER UP. REMOVED AND REPLACED ENGINE/ADJUSTED CONDITION LEVER MICROSWITCH. 2 H 7 2 4T 4 T RT A13NM E20NE 2007101100187 20071011 00187 NM 2007 10 11 AMTA200700463 1 20070927 A 3610 32143069 SHUTOFF VALVE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE NR 1 UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 520AT 27976 EICAS MSG L ENG BLD OFF DISPLAYED. LT ENG BLD AIR OFF LGT ILLUM WITH ENG RUNNING AND SW ON. DUCT NORM. JUMPERED RFCC NO HELP, REMOVED AND REPLACED NR 1 ENG PRESSUE REGULATING SHUTOFF VALVE IAW MM 36-11-09-002-008, OPS CHECKS NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007101200079 20071012 00079 NM 2007 10 12 2007UALA03938 1 20070927 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOORWAY DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 FWD CARGO DOOR CUTOUT FWD FRAME IS DAMAGED. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED FWD CARGO PIT DOOR CUTOUT FW D FRAME. 2 L 7 2 4F 4 F RT A16WE E21EU 2007101200167 20071012 00167 CE 2007 10 12 DJFA2007110 1 20070927 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 466CW RK366 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER IB RIB AND BRACKET ASSEMBLIES, BOTH THE RIGHT AND LEFT INBOARD ROLLER BRACKETS WERE FOUND CRACKED. DETAILED INSPE CTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. MAINTENANCE REPLACED BOTH RIB ASSEMBLIES WITH IMPR OVED ASSEMBILES. 2 H 7 2 4F 4 F RT A16SW E25EA 2007101700029 20071017 00029 NM 2007 10 17 2007UALA04127 1 20071007 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 FOUND 2L MED EMERGENCY LIGHTS INOPERATIVE. 11-01-07 REPLACED WITH NEW BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007102300299 20071023 00299 NM 2007 10 23 2007UALA03886 1 20070924 A 3350 1317 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 664UA 29236 LEFT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BULB IN LEFT AFT OVERWING EMERGENCY LIGHT. OP CHECKED OK FOR S ERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007103100168 20071031 00168 NM 2007 10 31 2007UALA04386 1 20071024 A 3500 OXYGEN SYSTEM BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU LOW A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 921UA 25388 THE O2 REQUIRES SERVICING. SERVICED CREW O2 SYSTEM. NO REPEATS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110800047 20071108 00047 NM 2007 11 8 2007UALA04440 1 20071026 A 5320 ANGLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 MAIN CABIN INTERCOSTAL UPPER ANGLE CRACKED BETWEEN STA 1197 + 22 AND 1197 +44, LBL 40. MAJOR REPAIR ACCOMPLISHED: REMO VED CRACKED ANGLE. INSTALLED NEW ANGLE, P/N 140T2540-9. 2 L 7 2 4F 4 F RT A1NM E24NE 2007112900037 20071129 00037 EU 2007 11 29 2007UALA04756 1 20071119 A 2612 FIRE LOOP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE B SYSTEM MALFUNCTIONED A UALA O OTHER N FALSE WARNING CR CRUISE 1 WP 29 456UA 1128 FIRE LOOP-B FAULT DISPLAYED ON UPPER ECAM SCREEN, ENG 2. ECAM ENG 2 LOOP-B FAULT SELF CLEARED. PERFORMED FUNCTIONAL TEST ON FDU-2, TESTED OK. PERFORMED VISUAL CHECK ON ALL WIRING LEADING TO FDU-2, CLEANED CANON PLUG INSIDE REVERSER AN D INSPECTED/CLEANED INSIDE PANEL 424AR. NO FURTHER REPEATS SINCE THIS ACTION. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121300353 20071213 00353 CE 2007 12 13 DXTA200702646 1 20071203 A 3231 AIR485401 SEQUENCE VALVE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 07 873QS 258573 RT MAIN GEAR DOOR REMAINS OPEN WITH GEAR RETRACTED-TOWER VERIFIED GEAR DOOR-RT MAIN INDICATOR HAD RED LIGHT. REMOVED AN D REPLACED RT MLG DOOR SEQUENCE VALVE IAW MM 32-30-41 AND RT MLG DOOR JACK IAW MM 32-10-41 LEAK CHECKED & OPS CHECKED GO OD. 2 L 7 2 4F 4 F RT A3EU E6WE 2007122000041 20071220 00041 EU 2007 12 20 2007UALA05081 1 20071212 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 477UA 1514 IN SEAT AREA 24C 23ABC AN ELECTRICAL BURNING ODOR IS PRESENT WITH NO VISIBLE SMOKE, COMES AND GOES. 2 L 7 2 4F 4 F RT A28NM E40NE 2007121300384 20071213 00384 NM 2007 12 13 2007UALA04901 1 20071201 A 3397 FEEDER CABLE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 922UA 26642 EMERGENCY LIGHTS INOP FROM SEAT 14ABC TO 24ABC. FOUND POWER CABLE INVERTER DAMAGE. REPLACED POWER CABLE INVERTER AND BATTERY PACK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007122000081 20071220 00081 NM 2007 12 20 2007UALA05092 1 20071213 A 5210 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 L-1 DOOR OUTER SKIN GOUGED AT LOWER END OF DOOR PAN. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700024 20080107 00024 NM 2008 1 7 2007UALA05134 1 20071215 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 182UA 25279 SEAT 39H EEL LIGHT ASSY BROKEN OFF. REPLACED LIGHT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121900115 20071219 00115 NM 2007 12 19 2007UALA05036 1 20071207 A 3397 WIRE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 773UA 26929 FOUND COACH SEAT ROWS 17 THRU 26 SEAT MOUNTED EEL LIGHTS ARE INOP. FOUND SHORTED CONNECTION. CLEARED SHORT. REPLACED F USE IN POWER SUPPLY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121400280 20071214 00280 NM 2007 12 14 2007UALA04980 1 20071206 A 2421 GENERATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RIGHT MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 642UA 25092 FLIGHT DIVERTED DUE TO LOSS OF THE RIGHT GENERATOR. EMERGENCY LANDING WAS DECLARED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010700277 20080107 00277 NM 2008 1 7 2007UALA05272 1 20071222 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 217UA 30550 FIRST CLASS SEAT 2E EEL LIGHT AFT SEGMENT IS INOP. REPLACED LIGHT STRIP. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008010900022 20080109 00022 EU 2008 1 9 2007UALA05229 1 20071223 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 493UA 1821 CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. SERVICED CREW O2 SYSTEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011700019 20080117 00019 CE 2008 1 17 DXTA200702726 1 20071228 A 2752 99120071 ACTUATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE TE FLAPS BYPASSING E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 626QS 6803 5605126 EMERGENCY DECLARED. ON POST FLT DISCOVERED LEFT FLAP EXTENDED ABOUT ONE INCH & RT FLAP FULLY RETRACTED FLUSH WITH THE FL AP HANDLE IN THE FULL UP POSITION. ' HYD PRESS' AMBER ANNUNCIATOR REMAINED ILLUMINATED IN FLT AFTER FLAP RETRACTION. PER FORMED 'HYD PRESS' ABNORMAL CHECKLIST. REPLACED LT FLAP ACTUATOR, WITH NEW. OPS AND LEAK CHECK GOOD. DONE IN REF. TO CE- 560XL MM 27-51-04. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008012200095 20080122 00095 EA 2008 1 22 A6WA200740704 1 20071218 A 5100 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE UNKNOWN A A6WA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 31 464AW 7890 ON TAKEOFF ROLL, AC VEERED RT, TOOK ALMOST FULL LT RUDDER TO STAY CENTERED ON RUNWAY. N1 SPEEDS WERE MATCHED. REDUCED POWER TO ABORT T/O AT 60 KNOTS. AIRCRAFT THEN TRAVELED STRAIGHT. BRAKE TEMPS WERE A 7 ON LT MAIN GEAR AND 3 AND 4 ON R T. WINDS 180 AT 5 KNOTS. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008011100082 20080111 00082 NM 2008 1 11 QXEA200702010 1 20071220 A 3097 697071272 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA NR 2 PROP HEAT INTERMITTENT A QXEA O OTHER O OTHER CL CLIMB 1 NM 09 400QX 4030 PROP DE-ICE CAUTION ILLUMINATES INTERMITTENTLY. AFTER SELECTING HEAT OFF IAW THE CHECKLIST, THE CAUTION LIGHT STARTED CY CLING OFF AND ON. MAINTENANCE REPLACED THE HEATER LEAD AT THE NR 3 BLADE OF NR 2 PROP. OPERATIONAL CHECKS GOOD. AIRCRAF T RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2007030900193 20070309 00193 SO 2007 3 9 C2XA07IA050 1 20070227 A 3350 1010861 LIGHT EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14939 145030 DURING SCHEDULED MAINTENANCE THE PASSENGER DOOR EMERGENCY LIGHT DID NOT ILLUMINATE. THE AFFECTED EMERGENCY LIGHT WAS RE MOVED AND REPLACED, THE SYSTEM OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED. 2 L 7 2 4F RT T00011AT 2007041600042 20070416 00042 NM 2007 4 16 F3LA200700075 1 20070329 A 5340 FITTING AIRBUS A319 A319111 3930336 NM LAVATORY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C-4/S-1, INSPECTION REPORTED LT AFT LAV D AFT WALL CORRODED AT OTBD POINT. REMOVED AND CLEANED FITTING. REINSTA LLED FITTING WITH NEW HARDWARE IAW CMM 25-43-51, PAGES 303, 618 AND 740. 2 L 7 2 4F RT A28NM 2008012800009 20080128 00009 SO 2008 1 28 FDKA200710549 1 20071014 A 5210 SEAL EMB 145 EMB145LR 3260212 SO PAX DOOR LEAKING A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 FDM 6014 PWM - MAIN CABIN DOOR SQUEALING IN FLIGHT. MX REPAIRED DOOR SEAL LEAK CHECK GOOD. 2 L 7 2 4T RT T00011AT 2007111400112 20071114 00112 NM 2007 11 14 HALA0700480 1 20071031 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM BS 1102-1439 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 SEAT TRACKS CORRODED IN SECTION 46 RBL 88.5, STA 1102 THRU 1439. REPLACED SEAT TRACK FROM STA 1102 TO STA 1439 RBL 88.5 AND RBL 11, STA 1197+37. 2 L 7 2 4F RT A1NM 2007061400124 20070614 00124 NM 2007 6 14 AWXA200700719 1 20070527 A 5754 114N407633 SKIN BOEING 757 757225 1384959 NM ZONE 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 MCN - LEFT WING NR 2 SLAT COVE SKIN CRACKED, WS 619. REPLACED LEFT WING NR 2 SLAT COVE SKIN, WS 619 IAW B757-200 SRM 5 1-40-02. 2 L 7 2 4F RT A2NM 2007050100040 20070501 00040 EU 2007 5 1 07FDEA01629 1 20070426 A 5343 A53610580203 BUSHING AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 809FD 449 CORROSION AT NLG RH ATTACHMENT LUG (BUSHING A536-10580-203) REPAIR PERFORMED BY BUSHING REMOVAL IAW SB A300-53-0130, APP ROVED BY EA 6-5312-101314 AND RAS 043643/005/2006 ISS A. 2 L 7 2 4F RT A35EU 2007091200097 20070912 00097 EU 2007 9 12 07FDEA03429 1 20070818 A 5315 A53781840200 FLOORBEAM AIRBUS 310 A310222 3930315 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 419FE 345 MDCC CROSSBEAM AT FR33 Y-690 FOUND CRACKED. A REPAIR IN ACCORDANCE WITH SRM SUPP 53-10-15 FIGURE 201 "SHEET A" WAS ACCO MPLISHED. 2 L 7 2 4F RT A35EU 2007100100074 20071001 00074 EU 2007 10 1 07FDEA04328 1 20070927 A 5311 A53989300246 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 CORROSION ON T-SEGMENT FRAME 92, STGR 12 LT TO RT. REPLACEMENT OF T-SEGMENT IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007102200047 20071022 00047 NM 2007 10 22 2007UALA04178 1 20071011 A 4920 38005501 APU BOEING 757 757222 1384956 NM MAKING METAL A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 782UA 26702 CREW REPORTS LOUD NOISE FROM AFT CABIN DURING FLT CONTROL CHECK. LOUD NOISE IN AFT CABIN COMES FROM DEMAND ON APU BLEED AIR SYSTEM WHEN STARTING ENGINES. REPLACED APU MASTER CHIP DETECTOR HAD SILVER CHUNKS. ROUTED SCREEN FOR CLEANING. N O BYPASS EXPERIENCED. ELECTRIC STARTER SCREEN WAS TORN IN TWO QUADRANTS BOROSCOPE PLUG NOT BROKEN. IT WAS MISSING AND R ED DIRT/SAND PACKED IN HOLE. APU REMOVAL WAS NOT REQUIRED. 2 L 7 2 4F RT A2NM 2007052300099 20070523 00099 NM 2007 5 23 SWAA072533 1 20070520 A 5315 140A0346 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 728SW 27860 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 26. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2007013100113 20070131 00113 WP 2007 1 31 07FDEA00204 1 20070130 A 5415 ATTACH ANGLE DOUG MD10 MD1010F 3022112 WP ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 368FE 46606 NR 1 PYLON LT ATTACH ANGLE FOR PANEL 488GL CHAFED. REMOVED, FABRICATED AND INSTALLED NEW DOUBLER IAW AUB7198 REV AN, DC /MD 10 SRM 51-35-01 VOL II. MECH 2891, QC227. 2 L 7 3 4F RT A22WE 2008011400191 20080114 00191 2008 1 14 NSVA20070194 4 20070721 A 3418 501147801 ACTUATOR SAAB SF340 340B 7860101 EU STICK PUSHER MALFUNCTIONED A NSVA O OTHER E VIBRATION/BUFFET CR CRUISE 1 EA 27 339CJ 339 WHEN OVER POWERING STICK PUSHER A HEAVY ABNORMAL VIBRATION OCCURS. INSPECTED A/C AND FOUND MALFUNCTION IN CAPTAINS ASSY AND STILL HAVING FULL TRAVEL ON ALL FLIGHT CONTROLS. REMOVED AND REPLACED STICK PUSHER MECHANISM SERVO ACTUATOR AND CA PTAIN IAW SAAB 340 AMM 27-35-20. OPERATIONAL CHECK GOOD IAW SAAB 340 AMM 27-35-00, SERVO ACTUATOR P/N ON/OFF 501-1478 -01, S/N ON 1041, S/N OFF 1120, CAPTAINS PIN ON/OF 501-1421-01S/N ON 1313, S/N OFF 1103. 2 L 7 2 4T RT A52EU 2008012900251 20080129 00251 SO 2008 1 29 FDKA200708468 1 20070913 A 2797 CONNECTOR EMB 145 EMB145LR 3260212 SO RUDDER DIRTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 838MJ 145384 FDM 6114 RDU - RUDDER HARDOVER PROTECTION FAIL MESSAGE. MX CLEANED FADEC CONNECTOR, RESET AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2007091900091 20070919 00091 EU 2007 9 19 07FDEA03617 1 20070912 A 5330 A53973277210 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 OLD REPAIR DOUBLER ON FUSELAGE SKIN BULK CARGO DOOR CUTOUT AT FRAME 69, STRG 43-45. DOUBLER MATERIAL NOT CONFORM TO RAS /DAHAM/12953/2000 ISSUE B AND SOGERMA CARD 6007 (B24279). DOUBLER REPLACED IAW RAS/DAHAM/12953/2000 ISSUE B AND SOGERMA DR B24279 NR 6007. 2 L 7 2 4F RT A35EU 2007061900292 20070619 00292 NM 2007 6 19 DHL2007740544 1 20070609 A 5313 BAC1498140 STRINGER BOEING 727 7272Q9 138448M NM BS 450-480 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 STRINGER 28R BS 450 CORRODED. REMOVED STR 28R BS 450 TRU BS 480 IAW B727 SRM 51-30-2. FABRICATED NEW STRINGER MATERIAL USED BAC1498-140 7075T6 PO NR 7191256 DIMENSION 28.750" AND FILLER MAT USED BAC1498-132 7075T6 PO NR 7207138 DIMENSION 16" IAW B727 SRM 53-10-3 FIG 1. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED STRINGER IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2007040300150 20070403 00150 EU 2007 4 3 07FDEA01080 1 20070322 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 FORWARD CARGO COMPARTMENT, FLOORBEAM (C25) FORWARD FACE OF BEAM LOCATED BETWEEN R2 AND R3 SEAT TRACK HAS A .400 INCH CRA CK IN VERTICAL STIFFENER. REPAIRED FLOORBEAM IAW A310/200 SRM SUPPLEMENT 53-10-15. REMOVED AND REINSTALLED FLOORBOARD IAW A310/200 AMM SUPPLEMENT 53-10-21-4. 2 L 7 2 4F RT A35EU 2007082200075 20070822 00075 EU 2007 8 22 07FDEA02831 1 20070811 A 2780 9028A000201 POWER UNIT AIRBUS 310 A310324 3930206 EU FLAP/SLATS FAILED A FDEA L ABORTED APPROACH F FLT CONT AFFECTED LD LANDING 1 SO 25 804FD 549 ON APPROACH, SLATS FAULT, BOTH SLATS ON O/H, NO SLATS ON SFPI, PER QRH, CYCLED FLAP/SLAT HANDLE TO 0/0, BACK 15/0 WITH S AME. APPLIED QRH PROCEED, LANDED "0'/40'." CHECKED FAULTS SFCC1 IS 10000 SFCC2 IS 10000, (LT ASYM PPU FAIL FAULT) ISO L 27-80-08 FIG 102 RESET SFCC OPD SEVERAL TIMES NO FAULTS TSM 27-80-08, BOTH SFCC SAME FAULT CODE. SUSPECT ASSY PPU 31C V. REPLACE IS PER M/M 27-86-11-4 OUT ON WING TIP NOT ABLE P/N 9028A0002-01PER MOCC REQUEST CHECKED MOUNT AND C/P OF BOT H PPU'S. ALL PANEL FOR OUTBOARD PPU, REINSTALLED LOOSELY WITH 2 FASTENERS, PARTS ON FXF905. OPD SLATS SEVERAL MORE TIM ES NO FAULTS. REMOVED AND REPLACED LEFT ASYM POS PICK-OFF UNIT/A310-3 M/M 27-86-11-4. OPS CK OK, NO FAULTS. 2 L 7 2 4F RT A35EU 2007030100145 20070301 00145 NM 2007 3 1 UIEA200700083 1 20070222 A 5730 SKIN BOEING 747 7472D3B 1384805 NM RT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 RIGHT WING UPPER SURFACE WS 697, STR28R AT FRONT SPAR FOUND CORROSION. CORROSION REMOVED AND PROTECTED AS PER SRM 51-10 -01 AND 51-10-02. 2 L 7 4 4F RT A20WE 2007052100002 20070521 00002 NM 2007 5 21 07FDEA01780 1 20070514 A 5754 RIB BOEING 727 727233 138408A NM NR 1 KRUEGER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 221FE 20932 LT WINGS, RIB UPPER CORD AT BL 70-5 FASTENER INSP. DURING "B" CHECK, CRACKED INDICATION WITNESSED BETWEEN BOTH HOLES AN D BEYOND. HOLES SHOWN ON FIGURE 1 OF EO 7-5710-7-2308 PT1L . REPAIRED IAW EO 7-5710-7-2308 PT1 AND PT2 AND EA 7-5710-1 02035 REF WRI 57-10/0313. 2 L 7 3 4F RT A3WE 2007020500031 20070205 00031 NM 2007 2 5 DXTA200701899 1 20070201 A 5210 UNKNOWN AMD FALC50 FALCON2000 2730170 NM DOOR UNKNOWN E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 284QS 185 RED DOOR MASTER WARNING CAME ON JUST PRIOR TO V1- ABORTED TAKEOFF AND LIGHT WENT OUT WHILE DECELERATING. ADJUSTED BAGGA GE DOOR MICRO SWITCHES 43MW & 47 MW IN ACCORDANCE WITH F2000 MM 52-700. OPERATIONAL CHECK GOOD. 2 K 7 2 4F RT A50NM 2007050300067 20070503 00067 2007 5 3 F3LA200700099 4 20070424 A 2565 LATCH AIRBUS A318 A318111 3940019 EU L2 GIRT BAR MISSING A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 801FR 4759 1939 DURING C-3 CHECK, INSPECTION REPORTED AFT OTBD NUTPLATE FOR THE AFT FILLER PLATE AROUND THE L2 DOOR GIRT BAR LATCH MISSI NG. REPLACED L2 DOOR SILL IAW SRM 51-42-11, FIG 6 AND 7. 2 L 7 2 4F RT 2007020700011 20070207 00011 NM 2007 2 7 07FDEA00342 1 20070206 A 5230 HINGE DOUG MD11 MD11 3023602 NM CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 529FE 48624 AFT CARGO DOOR HINGE AT FUSELAGE SIDE FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10-00 FIG. 14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.020" REMAINING THK 0.320". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007092500428 20070925 00428 NM 2007 9 25 2007UALA03680 1 20070912 A 3350 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EEL AT AFT GALLEY XAISLE INOP. 10-5-07 RESECURED EMERGENCY LIGHT CONNECTOR. OP CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007100200010 20071002 00010 NM 2007 10 2 AMTA200700439 1 20070911 A 5315 FLOORBEAM BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE BS 377 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 FLOORBEAM STA 377.7, RBL 3, LBL 30, AREAS AROUND 8 EACH NUTPLATES ARE CORRODED. REMOVED CORROSION ON FLOORBEAM STA 377. 7, RBL 3 - LBL 30 IAW SRM 53-00-51. FOUND SECTION AT LBL4 OUT OF LIMITS REPLACED FLOORBEAM UPPER CHORD IAW SRM 52-00-51 , 2R AND SRM 51-40-02, REF SAA NR 77440500001 FOR REPLACEMENT. 2 L 7 2 4F 4 F RT A2NM E12EU 2007100200016 20071002 00016 NM 2007 10 2 AMTA200700415 1 20070902 A 3150 WARNING LIGHT BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE ILLUMINATED A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 304TZ 30675 PSEU LIGHT ON ATTEN ENG START. RESET PSEU, PERFORMED BITE TEST NO FAULTS, OPS CHECKED FLT CONTROL AND RUN ENG NO FAULT FOUND IAW AMM 32-09-00-810-801. (K) 2 L 7 2 4F 4 F RT A16WE E2GL 2007101000175 20071010 00175 NM 2007 10 10 2007UALA03807 1 20070920 A 2560 HANGER ASSY BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU GIRT BAR OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 929UA 26652 AFT GALLEY DOOR SLIDE GIRT BAR WILL NOT REMAIN IN HANGERS. ADJUSTED HANGERS. 2 L 7 2 4F 4 F RT A16WE E21EU 2007101200168 20071012 00168 CE 2007 10 12 DXTA200702506 1 20070928 A 5270 SWITCH CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE DOOR WARN SYS OUT OF ADJUST E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 315QS 5600315 ON TAKEOFF AT ROTATION, "CABIN DOOR" LIGHT CAME ON. ONCE ON THE GROUND WITH THE DOOR OPEN, LIGHT FLICKERED ON AND OFF SE VERAL TIMES. GAINED ACCESS TO THE CABIN DOOR SWITCH. INSPECTED CONDITION AND WIRING FOUND SATISFACTORY; ADJUSTED SWITC H AND TIGHTENED AS REQUIRED. OPS CHECKED SATISFACTOR IAW CE-560 MM CHAPTER 20-00-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007101500212 20071015 00212 NM 2007 10 15 2007UALA04002 1 20071002 A 2700 3945128102 COMPUTER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 FAULTED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 842UA 1569 ELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. 10-19-07 FOUND NR 2 ELAC FAULTY. REPLACED NR 2 ELAC COMPUTER- NO RE PEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007100500181 20071005 00181 EU 2007 10 5 2007UALA03984 1 20070930 A 3350 256302008 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 432UA 587 EMERGENCY FLASHLIGHT IN F/A SEAT 2 IS NOT CHARGING FLASHING. *S/D* FAULTY BATTERY. REPLACED BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007100500166 20071005 00166 NM 2007 10 5 2007UALA03858 1 20070922 A 2760 SPOILER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 6 MALFUNCTIONED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 665UA 29237 BINDING IN NR 6 SPOILER. BINDING OCCURRED ONLY WITH LEFT HYD SYSTEM AND LEFT WING DOWN - SPOILER NR 6 UP. SPOILER WAS CHATTERING WITH ASSOCIATED NOISE. WITH ONLY CENTER OR RIGHT HYD, NO BINDING OR NOISE NOTED. NR 6 SPOILER FAILED TO LIF T WITH LEFT HYD POWER AT ONE POINT DURING TROUBLESHOOTING. 10-19-07 REMOVED NR 6 SPOILER ACTUATOR PER MM 27-61-02 . INSTALLED NR 6 SPOILER ACTUATOR PER MM 27-61-00. OP CHECKS AND LEAK CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007101600106 20071016 00106 NM 2007 10 16 2007UALA04047 1 20071003 A 5311 FAILSAFE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 787 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 AFT PIT FAIL/SAFE FRAME CHORD CORRODED, BS 787, LBL 1" TO RBL 7". REMOVED DAMAGE. FABRICATED AND INSTALLED FAIL SAFE CH ORD REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007103100069 20071031 00069 NM 2007 10 31 2007UALA04363 1 20071020 A 5230 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 FUSELAGE SKIN 16 INCHES FWD OF FWD CARGO DOOR CUTOUT IS DENTED WITH A GOUGE IN MIDDLE OF DENT. MEASURES 3.5" LONG, .25" WIDE, .080" DEPTH AND RUNS THROUGH 2 RIVETS. PERFORMED SRM REPAIR OF AREA. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110800008 20071108 00008 NM 2007 11 8 DXTA200702570 1 20071024 A 3620 6411801 THERMAL SWITCH GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE ENGINE INOPERATIVE E DXTA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 07 702QS 3887 070 JUST AFTER ENGINE RUN-UP GOT LINE PRESSURE HIGH/OVER TEMP WARNING ILLUMINATED. WHEN THROTTLES REDUCED TO IDLE, LIGHT WEN T OUT. PERFORMED ENGINE RUN, NO DEFECTS NOTED. CHECKED HP PRSOV VALVES NR 1 & 2 ENGINE; PRESSURE FROM NR 1 ENG HP PRSO V VALVE 25 PSI AND NR 2 ENG 25 PSI. REMOVED REMOVED S/N 0148 AND REPLACED OVERTEMPERATURE SWITCH FWD P/N 641180-1 S/N 0 369. AFT TEMP SWITCH S/N 0351 REMOVED S/N 0153 IAW G-200 M.M. CH 21-11-07. NO DEFECTS NOTED. OPS CHECK SATISFACTOR Y. 2 L 7 2 4F 4 F RT A53NM E35NE 2007110900082 20071109 00082 NM 2007 11 9 2007UALA04520 1 20071031 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 195UA 26899 SEAT 4J AFT EEL STRIP MISSING. EEL STRIP REPLACED 2 L 7 4 4F 4 F RT A20WE E24NE 2007111300052 20071113 00052 2007 11 13 2007UALA04565 4 20071105 A 3421 H150AKM1 INDICATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE STBY ATTITUDE FAULTY A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 646UA 25283 RTFL DUE TO STANDBY ATTITUDE INDICATOR PROBLEMS. REPLACED STANDBY ATTITUDE INDICATOR WITH BORROWED UNIT. OPERATIONAL T EST CARRIED OUT SUCCESSFULLY. ACFT CATII-III STATUS NOT ALTERED. 2 L 7 2 4F 4 F RT A1NM E24NE 2007112900028 20071129 00028 NM 2007 11 29 2007UALA04745 1 20071119 A 5610 WINDSHIELD BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT FAILED A UALA O OTHER O OTHER AP APPROACH 1 WP 29 374UA 24639 CAPTAIN'S WINDSHIELD SHATTERED FOUR MINUTES BEFORE TOUCHDOWN. 2 L 7 2 4F 4 F RT A16WE E21EU 2007120400010 20071204 00010 NE 2007 12 4 S9BA200700023 2 20071004 A 7240 020258 INLET GUIDE VANE DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27US 52043 NE ENGINE CRACKED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 888PV 400 620 PCE41552 DURING 400 HOUR BORESCOPE INSPECTION, FOUND CRACKS ON CT STATOR THAT ARE BEYOND SERVICEABLE LIMITS. PERFORMED HOT SECTI ON INSPECTION. REPLACED IE DUCT ASSEMBLY. 1 H 7 2 3T 4 T RT A9EA E2NE 2007121100047 20071211 00047 GL 2007 12 11 UIEA200700440 2 20071015 A 7250 1881M52G05 BLADE GE BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL HPT ROTOR CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 454PA 30007 17972 53X04272 30812 704330 ESN 704330 - HPT STAGE 2 BLADES 74EA FOUND WITH UNDER PLATEFORM CORROSION AND CRACKS. 2 L 7 4 4F 4 F RT A20WE E23EA 2007121400343 20071214 00343 CE 2007 12 14 DXTA200702655 1 20071206 A 3260 LANDING GEAR RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MAINS FALSE INDICATION E DXTA O OTHER N FALSE WARNING CL CLIMB 1 GL 07 893QS 258393 UPON GEAR RETRACTION, (3) RED LIGHTS ALONG WITH 1 GREEN FOR THE NOSEWHEEL ARE INDICATED FOR 1 MINUTE AFTER SELECTING GE AR UP. INSPECTED GEAR AND CYCLED SEVERAL TIMES IAW MM 29-10-00-501. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F 4 F RT A3EU E6WE 2007122800101 20071228 00101 NM 2007 12 28 2007UALA05025 1 20071208 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 29C 30C EMERGENCY STRIP LIGHT IN THE FLOOR IS TORN UP. SECURED AND OPS TESTED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700267 20080107 00267 2008 1 7 2007UALA05261 4 20071222 A 2565 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L1 DOOR UNSERVICEABLE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 117UA 28810 DOOR 1L SLIDE LACING VERY LOOSE, SLIDE BULGING AND DIFFICULT TO INSTALL BUSTLE. SUSPECT SLIDE IMPROPERLY PACKED. REPLAC ED SLIDE REF MM 25-6 9-01. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008010400185 20080104 00185 CE 2008 1 4 K5L2007F00002 1 20071125 A 3320 6900042000 POWER SUPPLY BEECH 200 A200 1152921 CE PWA PT6 PT6A41 52043 EA CABIN LIGHTS FAILED E K5LA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 05 636B BC61 AWAITING TAKEOFF, PILOT TURNED ON CABIN LIGHTS AND NOTICED SMOKE FUMES IN COCKPIT AND CABIN. TURNED OFF VENT BLOWED AND CABIN LIGHTS AND RETURNED TO RAMP. IT WAS DETERMINED THAT THE POWER SUPPLY (BALLAST) HAD FAILED AND CAUSED THE SMOKE. POWER SUPPLY WAS RELACED AND LIGHTS OPERATED NORMAL. (K) 1 L 7 2 4T 4 T A24CE E4EA 2008010800369 20080108 00369 CE 2008 1 8 SH073532 1 20071204 A 2422 501166601 INVERTER LEAR 35 31A 5170531 CE GARRTT TFE731 TFE731* 01518 WP NR 2 FAILED E O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 05 314SG 4813 133 AFTER ENGINE START THE PILOT ATTEMPTED TO TURN ON THE NR2 A/C INVERTER WITH NO RESULTS. AFTER SEVERAL ATTEMPTS SMOKE COU LD BE SMELLED IN THE AIRPLANE, AT THAT TIME THE ENGINES WHERE SHUTDOWN AND MAIN BATTERY POWER TURNED OFF. A LINE SERVIC E ASSISTANT NOTIFIED THE PILOT THAT SMOKE WAS COMING FROM THE DORSAL FIN INLET. THE PILOT GOT OUT AND OPENED THE AFT TAI L AREA EQUIPMENT/BATTERY COMPARTMENT TO DISCONNECT THE BATTERIES, THIS AREA WAS ALSO FULL OF SMOKE. AFTER REMOVING THE N R 2 FAILED INVERTER, BLACK DISCOLORATION FROM THE COOLING VENTS COULD BE SEEN AND A BAD SMELL WAS PRESENT. 2 L 7 2 4F 4 F RT A10CE E6WE 2008011400070 20080114 00070 EU 2008 1 14 COEA0752821 1 20070824 A 5310 S53671217334 CREASE BEAM AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. LEVEL 2 CORROSION: FOUND CORROSION ON THE FOLLOWING CREASE BEAM WEBS. LT CREASE BEAM, 2 WEBS FROM FR 39 TO 41. RT CREASE BEAM, 1 WEB FROM FR 39 TO 40. REPLACED WEBS, LT PN S53671217334, AND S53671217316. RT PN S43671318210. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008010900213 20080109 00213 WP 2008 1 9 CLCA2007F0003 1 20070818 A 7830 9057M85602 DUCT DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2B 30018 NE NR 3 ENGINE DAMAGED A CLCA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 SO 29 612GC 47840 455784 ON T/O NR 3 ENGINE EGT WENT TO 987 DEG WITH FIRE WARNING, RETARDED TLT WARNING GOES OUT 15 SEC. FOUND T/R TUBE ASSY AFT AIR SUPPLY DUCT DAMAGED. REMOVED AND REPLACED DUCT ASSY.T 2 L 7 3 4F 4 F RT A22WE E23EA 2008012200044 20080122 00044 EA 2008 1 22 A6WA200740665 1 20071116 A 5210 FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE PAX DOOR GOUGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 427ZW 7685 GOUGE ON FWD PAX DOOR ALIGNMENT FITTING .750 X .200, .020 DEEP. FWD PAX DOOR ALIGNMENT FITTING REPLACED IAW CRJ 200, SR M 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008012300235 20080123 00235 NM 2008 1 23 2007UALA05216 1 20071221 A 5320 INTERCOSTAL BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 914UA 25381 TWO CRACKS DETECTED AT STA 294.5 INTERCOSTAL WEB. MAJOR REPAIR ACCOMPLISHED: REPLACED WITH NEW INTERCOSTALS AT STA 2 94.5 2 L 7 2 4F 4 F RT A16WE E21EU 2008021200005 20080212 00005 NM 2008 2 12 2007UALA03173 1 20070815 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 DENT IN FUSELAGE AFT ABOVE CAPTAIN`S NR 3 WINDOW. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 NM 2008 12 23 UALA2008111304734 1 20071118 A 2611 G718505 CONTROL PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CARGO SMOKE MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 331UA 24192 CARGO SMOKE DETECTION FAILS OPS CHECK. REPLACED FIRE DETECTION CONTROL PANEL. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007012500175 20070125 00175 EA 2007 1 25 ACE011107 2 20070111 A 7314 COUPLING CRANEXXXXXXX BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65* EA FUEL PUMP DISCONNECTED E YADA O OTHER J WARNING INDICATION CR CRUISE 1 AL 03 112AX 187 B1675019 UC45 PILOT REPORTED NR 2 ENGINE LOW FUEL PRESSURE WARNING CAME ON. WARNING EXTINGUISHED AFTER SELECTING ELECTRIC STANDBY PUM P ON. MAINTENANCE REPLACED LOW PSI FUEL PUMP DUE INTERNALLY DISCONNECTED DRIVE SHAFT (SECOND OCCURRENCE OF THIS TYPE FA ILURE ON THIS ENGINE WITHIN 30 DAYS). VERIFIED PUMP DRIVE SHAFT WOULD EASILY DE-COUPLE FROM ROTOR WHEN TURNING SHAFT BY HAND. 2 L 7 2 4T 4 T RT A24CE E4EA 2007012500007 20070125 00007 CE 2007 1 25 DXTA200701840 1 20070106 A 2611 SMOKE DETECTOR RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP LAVATORY MALFUNCTIONED E DXTA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 875QS 258375 RED FIRE ANNUNICATOR ILLUMINATES, FLASHES INTERMITTENTLY IN FLIGHT. VISUALLY INSPECTED ALL BAGGAGE COMPARTMENTS. CLEANE D AND INSPECTED FORWARD, AFT AND LAV SMOKE DETECTORS. REMOVED LINT AND DUST FROM AFT AND LAV SMOKE DETECTORS. OPS CHEC K GOOD IAW MM 26-10-00. 2 L 7 2 4F 4 F RT A3EU E6WE 2007012300159 20070123 00159 NM 2007 1 23 2007UALA00112 1 20070117 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 797 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 AFT CARGO DOOR CUTOUT, AFT FRAME BS 797 CORRODED ON FWD SIDE BTWN STR 24R AND 25R. INSTALLED NEW FRAME SECTION PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2007020700002 20070207 00002 SW 2007 2 7 AWTR113954 1 20070202 A 5302 206031004115 MOUNT BELL 206 206B3 1181506 SW ALLSN 250C 250C20J 03013 GL TAILBOOM CRACKED B AWTR K NONE O OTHER IN INSP/MAINT 1 SW 03 67PJ 6445 3966 FOUND 2.5 IN CRACK FROM LT REAR MOUNT HOLE FWD. 1 G 7 1 3U 3 U H2SW E4CE 2007013100182 20070131 00182 NM 2007 1 31 2007UALA00157 1 20070120 A 2910 LINE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE AIRSPEED SWITCH DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 674UA 29242 RAT FAILS TO AUTO DEPLOY. TROUBLE SHOOTING FOUND RAT AIRSPEED SWITCH PITOT-STATIC LINES DISCONNECTED AT SWITCH. RECONNE CTED PER MM 29-21-24 AND RAT AUTO DEPLOYS & OPS CHECKS NORMALLY. SUSPECT PRIOR INSTALLATION/ HOOK-UP ERROR. 2 L 7 2 4F 4 F RT A1NM E24NE 2007021500077 20070215 00077 NM 2007 2 15 2007UALA00306 1 20070204 A 3397 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 FOUND EMERGENCY LIGHT STRIP ON FLOOR IN FRONT OF FIRST CLASS CLOSET INOP. PROBLEM WAS TRACED TO THE FEEDER CABLE AND BR OKEN PINS ON THE WALL. REPLACED FEEDER CABLE AND LIGHT STRIP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007021500177 20070215 00177 NM 2007 2 15 2007UALA00237 1 20070127 A 3350 POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS UNRELIABLE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 674UA 29242 FLIGHT ATTENDANT REPORTS EXIT PATH LIGHTING ROWS 10-17 LEFT SIDE CAME ON FOR SEVERAL MINUTES IN CRUISE. REPLACED POWER SUPPLY. CHECKS OUT NORMALLY. RETURN TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022100148 20070221 00148 EU 2007 2 21 2007UALA00438 1 20070213 A 5322 SHEAR TIE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 430UA 568 FWD CARGO PIT CORROSION AT FRAME 30 SHEAR TIES BETWEEN STR 43 & 44 LT, 41 & 42 LT, 41 & 42 RT AND 40 & 41 RT. MAJOR REP AIR ACCOMPLISHED: REPLACED SHEAR TIES. 2 L 7 2 4F 4 F RT A28NM E40NE 2007022200055 20070222 00055 NE 2007 2 22 UPS07649205 2 20070215 A 7200 ENGINE BOEING 767 76734AF 1385212 NM GE CF6 CF680C2B7 NE RIGHT BIRD INGESTION A IPXA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 SO 01 320UP 27747 INSPECTION TYPE:ETOP TSLV = 4514 - DIVERSION - POSSIBLE BIRD INGESTION THROUGH RIGHT ENGINE. THE CREW NOTICED AN UNUSUA L VIBRATION & REQUESTED TO SPEAK TO ACMX. DIVERTED TO SJO. PERFORMED FIM 71-05-00/101 AND REPLACED FAN BLADES 15-16-34 PER MM 72-00-00-6. PERFORMED ENGINE TEST 5 & 6 PER MM 71-00-00-5. ALL CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E13NE 2007030600093 20070306 00093 NM 2007 3 6 2007UALA00623 1 20070301 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 DOOR 3L SLIDE ILLUM EMERGENCY LIGHT INOP. REPLACED LT. ASSY. NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022100162 20070221 00162 NM 2007 2 21 2007UALA00248 1 20070115 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY EXIT LIGHTS ON SEATS 2A 2J AND 4J ARE INOP OR TORN. REPLACED WITH NEW EMERGENCY EXIT LIGHTS ON SEATS 2A,2J & 4J. EEL SYS OP' CHECKED NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022300196 20070223 00196 2007 2 23 2007UALA00484 4 20070215 A 2565 B14056904 O-RING AIRCRUISERS BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SLIDE BOTTLE MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 217UA 0037 30550 LOW BOTTLE PRESSURE. REPLACED SLIDE. A/C READY FOR SERVICE. SLIDE PROBLEM ROOT CAUSE: FOUND LOOSE LOCK NUT ON CONNEC TION TO PRESSURE BOTTLE. SUSPECT IMPROPER TORQUING DURING RESTORATION. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007030100069 20070301 00069 EU 2007 3 1 2007UALA00543 1 20070219 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY EXIT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 449UA 851 FOUND DOOR EMERGENCY EXIT LIGHT ON AND WILL NOT EXTINGUISH. [5-1-07] REMOVED AND RESEATED CAM AND ACPD CFDS TEST. LI GHTS ARE EXTINGUISHED & TEST PASSED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007031200030 20070312 00030 SO 2007 3 12 C2XA07IA028 1 20070206 A 3350 MB12R6 CONNECTOR EMB 145 EMB145EP 3260221 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13936 145025 DURING MAINTENANCE INSPECTION THE GALLEY EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE CONNECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2007030100063 20070301 00063 EA 2007 3 1 QXEA200700251 2 20070226 A 7200 ENGINE BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA LEFT MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 402QX 4032 BOI FLIGHT NR 2303: WITH POWER LEVERS AT RATED DETENT ON CLIMB, LEFT TORQUE APPROX 6 PERCENT HIGHER THAN RIGHT TORQUE ON FINAL WITH CONDITION LEVERS AT MAX. NOTICED NR 1 BLEED OFF. MAINTENANCE PER PILOT CONVERSATION, CONFIRMED NR 1 BLEED OFF. INTERROGATED CDS WITH NO FAULTS NOTED. C/W ENGINE RUN. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2007031500157 20070315 00157 EU 2007 3 15 2007UALA00664 1 20070306 A 5347 SEAT TRACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 477UA 1514 FRAME C20, RBL 31 HAS EXFOLIATED CORROSION. MAJOR REPAIR ACCOMPLISHED: REPLACED SEAT TRACK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007030700116 20070307 00116 CE 2007 3 7 DXTA200701951 1 20070216 A 3234 257NF859601 SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG HANDLE INOPERATIVE E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 816QS 6650 258416 WHEN GEAR WAS RETRACTED AFTER TAKEOFF, THE LT MAIN INDICATED BOTH RED AND GREEN LIGHTS AND THE NOSE AND RT MAIN INDICATE D RED LIGHTS. UPON PLACING THE LEVER IN THE DOWN POSITION 3 GREEN AND NO RED LIGHTS WERE OBSERVED. REMOVED U/C HANDLE S WITCH P/N 25-7NF859-601, NSN FOR FAULTY CONTACTS AND INSTALLED NEW UNDERCARRIAGE MICROSWITCH P/N 25-7NF859-601, NSN AND PERFORMED OPERATIONAL CHECK WITH NO FAULTS FOUND I.A.W HAWKER 800XP M/M CH 32-60-00. 2 L 7 2 4F 4 F RT A3EU E6WE 2007031900095 20070319 00095 NE 2007 3 19 UG8A2007PA02O 2 20070307 A 7200 73811B ENGINE AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE NR1 FOD E UG8A A UNSCHED LANDING C F.O.D. CR CRUISE 1 GL 23 218PH 901 218 P105574 FOD DAMAGE TO LT ENGINE IN FLIGHT. COVER FOR FUEL CAP CAME OFF IN FLIGHT AND WAS INGESTED BY THE ENGINE. ENGINE OPERAT ION WAS REPORTED NORMAL. REMOVED DAMAGED ENGINE AND INSTALLED A RENTAL ENGINE. AIRCRAFT RETURNED TO SERVICE. 2 K 7 2 4F 4 F RT A50NM E44NE 2007032800210 20070328 00210 EU 2007 3 28 2007UALA00799 1 20070317 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 404UA 450 CABIN EMERGENCY LIGHTING DOES NOT TEST OK. SEAT FOUND MOUNTED ON TOP OF POWER (RED) WIRE, CAUSING SHORT. RESPLICED ALL THREE SEATS TO POWER AND GROUND WIRE FROM WALL CONNECTOR. ROUTED PROPERLY AND SECURED. ALL LIGHTS TEST NORMAL. EMER LIG HT TEST AT ATTNDT PANEL OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007032800251 20070328 00251 NM 2007 3 28 2007UALA00831 1 20070316 A 2560 WARNING SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN MALFUNCTIONED A UALA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 29 543UA 25698 EVAC ALARM HAS ACTIVATED AT ALL STATIONS ALL BY ITSELF. PRESSED HORN SHUTOFF, NO HELP. [SUP 06-14-07] TESTED EVAC SYST EM PER UA ENGINEERING SPECIFICATIONS. SYSTEM TESTED GOOD. NO DEFECTS NOTED. UNABLE TO ESTABLISH ANY CAUSE FOR THIS IR REGULARITY EVENT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007032900100 20070329 00100 NM 2007 3 29 2007UALA00847 1 20070321 A 3350 20131A BATTERY PACK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 349UA 24253 EEL LIGHT STRIP IN FIRST CLASS AND RIGHT EXIT DOOR LIGHTS INOP. *S/D* REPLACED BATTERY PACK, OP CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032900326 20070329 00326 EA 2007 3 29 A6WA200740111 1 20070302 A 2450 HA4A039 RELAY CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ELECTRICAL SYS FAILED A A6WA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 GL 31 460AW 7872 7867 ON AC ELECTRICAL SYNOPTIC PAGE ADG BUS DISPLAYED IN WHITE. AC1 AND AC2 BUS SHOW WHITE LINES TO ESS BUS, ESS BUS IS GREE N. REMOVED AND REPLACED K2XD RELAY IAW AMM 24-51-31. OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007040200133 20070402 00133 CE 2007 4 2 DXTA200702052 1 20070327 A 3233 ACTUATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 906QS 7500206 AFTER GEAR DOWN SELECTION, NO NOSE GEAR GREEN LIGHT FOR 20-30 SECONDS. REMOVED AND REPLACED NOSE LANDING GEAR ACTUATOR WITH SERVICABLE (INSPECTED) UNIT BY CESSNA AIRCRAFT COMPANY FAA CRS CNQR918C. OPERATIONAL AND LEAK CHECKS SATISFACTORY. WORK WAS ACCOMPLISHED IAW CESSNA CITATION 750 MAINTENANCE MANUAL CHAPTER 32-30-03. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007040900012 20070409 00012 NM 2007 4 9 DL76L070279 1 20070323 A 5410 FITTING BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE LT PYLON ARCED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 191DN 28448 727679 FOUND ARCING TO LT PYLON MID STRUT FITTING OUTBOARD SIDE. REMOVED LT OTBD PYLON PANELS 437 ELX 437 AL. ALSO, REMOVED T OP WING TO PY ACCESS PANEL. REPAIRED WIRE W/SPLICE PER SWPM. PUMP OPS CKS NML. NEEDS CLAMP/PNLS REINSTALLED. INSTAL LED CLAMPS AND CLOSED PANELS. 2 L 7 2 4F 4 F RT A1NM E24NE 2007041200083 20070412 00083 EA 2007 4 12 A6WA200740087 1 20070227 A 5320 S6144A14 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FS484 RBL36 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 450AW 7823 FS 484 INTERCOSTAL CRACKED AT RBL 36. MAINTENANCE DAMAGED FLANGE AND INSTALLED REPAIR ANGLE IAW REO 601R-53-41-059 REV A AND BSC STANDARD REPAIR 601R-53-0030A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041200012 20070412 00012 NM 2007 4 12 2007UALA01044 1 20070405 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 300-303 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 CRACKED INTERCOSTAL SUPPORT ANGLE STA 300 - 303 JUST ABOVE STR 10 FWD OF L1 DOOR. *S/D* MAJOR REPAIR: REMOVED AND REP LACED SUPPORT ANGLE STA 300-303 STR 10L PER AAR EAI070216 AND UA-EVA-70168. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041300042 20070413 00042 EU 2007 4 13 TRAX200700473 1 20070406 A 3350 SWITCH AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 AFT 2 MINET EMERGENCY LIGHT SWITCH DOES NO WORK. 2 H 7 2 4T 4 T RT E20NE 2007040400164 20070404 00164 NM 2007 4 4 2007UALA00927 1 20070328 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 508UA 24744 L-1 DOOR AND R-3 DOOR EXTERIOR EMERGENCY LIGHTS INOP. [SUP 4-17-07] RELAMPED L1 DOOR AND R3 DOOR EXTERNAL EEL LIGHTS. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007040900145 20070409 00145 NM 2007 4 9 KNNA200700026 1 20070311 A 5311 FRAME BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE BS 867 DAMAGED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 326DL 23098 AFT CARGO PIT, INTERIOR BILGE B-STA 867 BETWEEN STR 27 R AND STR 28 L FRAME BOTTOM SIDE, CORRODED. PROVIDE INSTRUCTIONS ON REPAIR OF CORROSION AFT CARGO PIT, INTERIOR BILGE BS 867 BETWEEN STR 27R-27L BOEING SRM 53-10-4 FIGURE 7. 2 L 7 2 4F 4 F RT A16WE E2EA 2007041600037 20070416 00037 EU 2007 4 16 2007UALA01003 1 20070330 A 8011 STARTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE FAULTY A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 474UA 1475 V10957 ON START NR 1 ENG HAD REPORTED SPARKS COMING FROM THE BOTTOM OF THE ENG. [SUP 06-01-07] REPLACED START VALVE AND STARTE R. 2 L 7 2 4F 4 F RT A28NM E40NE 2007043000103 20070430 00103 NM 2007 4 30 2007UALA01179 1 20070413 A 3350 SIGN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY EXIT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 542UA 25276 EXIT SIGN OVER RIGHT SIDE EMERGENCY EXIT WINDOW IS COMING LOOSE. [SUP 05-16-07] SECURED LENSE. 2 L 7 2 4F 4 F RT A2NM E17NE 2007050100112 20070501 00112 2007 5 1 DXTA200702130 4 20070422 A 2210 4006719903 ROLL SERVO CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL AUTOPILOT INOPERATIVE E DXTA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 07 986QS 2971 7500086 AILERON OSCILLATION BACK AND FORTH DURING CRUISE, WORSENING DURING DESENT WITH AUTOPILOT ON. SWITCHING FGC HAD NO EFFEC T. REMOVED AND INSTALLED A NEW POWER SERVO. OPS CHECKS GOOD AT THIS TIME. ALL WORK DONE IAW MM CHAPTER 22-10-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007050100123 20070501 00123 2007 5 1 DXTA200702149 4 20070426 A 3100 MONITOR GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE COCKPIT INOPERATIVE E DXTA K NONE O OTHER IN INSP/MAINT 1 GL 07 705QS 061 DURING POST FLIGHT, EVALUATING INOP VIDEO MONITOR SCREEN. SCREEN WAS MOVED TO VIP STATION TO DETERMINE IF MONITOR CONNEC TOR WAS CONNECTED OR MONITOR ITSELF WAS INOPERATIVE. IMMEDIATELY AFTER MONITOR WAS PLUGGED IN AT VIP SEAT SMOKE WAS NOT ED AT THE CONNECTION. COMPLIED WITH REPLACEMENT OF MONITORS AND CONNECTOR CABLES WHICH WERE ON HAND. REPLACED MISSING MONITOR IN AIRCRAFT. OPS CHECKED THE OTHER FOUR MONITORS BY PLUGGING THEM INTO A WORKING POSITION AND VERIFYING VIDEO. C ONNECTORS ON THE MONITORS AND MATING CONNECTORS ALL CHECKED NORMAL. 2 L 7 2 4F 4 F RT A53NM E35NE 2007041700001 20070417 00001 CE 2007 4 17 AMWA83860 1 20070410 A 5610 10138402523R WINDSHIELD BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE COCKPIT CRACKED A AMWA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 07 166YV 22266 2351 UE166 DURING FLIGHT, THE CAPT'S WINDSHIELD CRACKED. THE PILOT DIVERTED AND LANDED WITH NO FURTHER INCIDENT. REMOVED AND REPL ACED PILOT'S WINDSHIELD. 2 L 7 2 4T 4 T RT A24CE E26NE 2007050800067 20070508 00067 NM 2007 5 8 2007UALA01360 1 20070427 A 3510 OXYGEN SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CREW O2 LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 307UA 23668 CREW O2 APPEARS TO HAVE SLOW LEAK. DEPARTED SFO 1850 PSI DOWN TO 1400 AFTER 1 HOUR. [SUP 05-16-07] SERVICED O2 SYSTEM TO FULL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007050700017 20070507 00017 NM 2007 5 7 AMTA200700180 1 20070331 A 4940 FILTER BOEING 737 73783N 13844HI NM GE CFM56 CFM56* 13802 NE APU START GEN UNKNOWN A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 315TZ 28245 APU FAULT LIGHT ILLUMINATED AND APU SHUTDOWN AFTER ELECTRICAL WAS ON LINE. REMOVED AND REPLACED APU STARTER GENERATOR F ILTER IAW MM 49-91-12-4. (K) 2 L 7 2 4F 4 F RT A16WE E2GL 2007051700063 20070517 00063 2007 5 17 2007UALA01124 4 20070411 A 2565 612321 GAUGE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE SLIDE BOTTLE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 809UA 825 LOW BOTTLE. *S/D* LEAKING THROUGH GAUGE FACE. CHANGED BOTTLE OUT WITH ANOTHER ONE. FIXED BOTTLE WITH BAD GAUGE AND P UT IT IN STOCK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052400168 20070524 00168 NM 2007 5 24 2007UALA01521 1 20070515 A 3260 PROXIMITY SENSOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE MLG MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 846UA 1600 RETURNED TO FIELD DUE TO LANDING GEAR INDICATION. [06-26-07] FAULT TRACED TO A FAULTY PROXIMITY SENSOR. REPLACED PROX IMITY SENSOR 23GA. 2 L 7 2 4F 4 F RT A28NM E40NE 2007052900023 20070529 00023 NM 2007 5 29 2007UALA01603 1 20070522 A 3350 POWER SUPPLY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 772UA 26930 EMERGENCY EXIT LIGHTS ON SEATS ROWS 11-15 BOTH AISLES ARE INOPERATIVE. [SUP 06-06-07] REPLACED POWER SUPPLY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007060700008 20070607 00008 SO 2007 6 7 JU82007F00000 1 20070518 A 2823 1908001 SELECTOR VALVE PIPER PA44 PA44180 7104402 SO LYC O360 O360* 41514 EA FUEL SYS DEFECTIVE D JU8S O OTHER O OTHER NR NOT REPORTED 1 GL 25 644KS 10 4496220 FUEL SELECTOR VALVE WAS REPLACED UNDER WARRANTY IN AIRCRAFT. IMMEDIATELY AFTER INSTALLATION, FUEL SELECTOR FOUND TO OPE RATE NORMALLY. UPON THE ACCUMULATION OF 10.2 HRS. TIS, THE FUEL SELECTOR VALVE WAS FOUND TO STICK AT EACH DETENT, IE; CROSSFEED, OFF AND NORMAL POSITION. THE STICKING WAS SO SEVERE, THAT EVEN THE FORCE OF (2) HANDS ON THE SELECTOR VALVE WOULD NOT MOVE THE VALVE OUT OF THE DETENT POSITION. CAUSE OF PROBLEM IS UNKNOWN, HOWEVER, THIS POSES A SAFETY OF FLIGH T ISSUE DUE TO THE FACT THAT THE VALVE AT TIMES WOULD NOT MOVE OUT OF THE DETENT. IF THIS VALVE WERE TO STICK DURING AN EMERGENCY, THIS COULD CAUSE THE SELECTOR TO BE STUCK IN THE OFF POSITION. THIS COULD RESULT IN THE AC OPERATING WITH O 1 L 7 2 3O 3 O A19S0 E286 2007053100060 20070531 00060 NM 2007 5 31 2007UALA01644 1 20070524 A 3350 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 660UA 27115 EEL LIGHTS ARE INOP FROM ROW 19 TO 26. RT OPS. [SUP 06-06-07] REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007061400228 20070614 00228 CE 2007 6 14 AMWA84592 1 20070511 A 3240 1013880083 BRAKE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MLG BINDING A AMWA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 07 163YV UE163 DURING ROLLING TAKEOFF, CAPT HAD EXCESSIVE BRAKE DRAG AND ABORTED TAKEOFF. RETURNED TO GATE W/O FURTHER INCIDENT. ADJU STED PARKING BRAKE HANDLE AND VALVES. 2 L 7 2 4T 3 T RT A24CE E2NE 2007061400104 20070614 00104 EU 2007 6 14 2007UALA01907 1 20070609 A 5730 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT WING DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 444UA 824 L/E OF LEFT WING BEHIND NR 4 SLAT DAMAGED. WING LEADING EDGE REPAIRED AND NEW NR 4 LE SLAT INSTALLED. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062600224 20070626 00224 NE 2007 6 26 2007UALA02048 2 20070617 A 7230 BLADES BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 2 ENGINE DAMAGED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING A FLAME/FIRE CL CLIMB 1 WP 29 211UA 30217 777103 RTFL DUE TO NR 2 ENGINE COMPRESSOR STALL. [08-21-07] SURGED IN CLB. EGT EXCEEDED RL FOR 2:37; PEAK 733¡C. SHUTDOWN . METAL IN TAILPIPE. ENGINE REPLACED AT ORD. SHOP DISASSEMBLY REVEALED EXTREME DAMAGE INSIDE THE HP COMPRESSOR. ALL BLADES SHOWED SEVERE BMOD AND HEAT DISTRESS, POSSIBLY FROM A RESULTANT TITANIUM FIRE. ONE STAGE-5 BLADE HAD LIBERATED J UST ABOVE THE PLATFORM. THERE IS EVIDENCE OF A CRACK PROGRESSING FROM FATIGUE, BUT DUE TO THE EXTENSIVE NATURE OF THE D AMAGE, THE CRACK ORIGIN COULD NOT BE DETERMINED. THE BLADE WILL BE RETURNED TO PRATT & WHITNEY FOR FURTHER ANALYSIS. T HE HPC ROTOR, SN B77021 HAD 6620 HOURS (1398 CYCLES) SINCE RE-BUILD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007062000148 20070620 00148 NM 2007 6 20 2007UALA01963 1 20070611 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN DETACHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 226UA 30226 EMERGENCY PATH LIGHT AT 3F AFT SIDE CAME OFF. [06-26-07] REPLACED EMERGENCY EVACUATION LIGHT AT 3F AFT SIDE. EMERGENC Y LIGHT SYS TEST OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007062700008 20070627 00008 CE 2007 6 27 DXTA200702267 1 20070615 A 2720 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RUDDER UNKNOWN E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 953QS 7500153 RUD LIMIT FAIL B CAS MESSAGE IN FLIGHT / RUDDER LIMITED TO 20 PERCENT. [07-09-07] REMOVED AND REPLACED LOWER RUDDER LI MITER ACTUATOR IAW CE-750 M/M 27-23-00. OPS CHECKED GOOD IAW CE-750 M/M 27-20-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007070200101 20070702 00101 NM 2007 7 2 2007UALA02128 1 20070619 A 2597 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 1R SLIDE MISINSTALLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 585UA 26709 DOOR 1R SLIDE LIGHT REMAINS ON WHEN DOOR IS DISARMED. [08-07-07] WIRED LIGHT ASSY CORRECTLY. LIGHT OPERATES NORMA LLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071000365 20070710 00365 2007 7 10 VNAA0706013 4 20070619 A 3425 FLIGHT DIR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 710PS 10167 CREW REPORTED A FLIGHT DIRECTOR FAILED IN TAKEOFF MODE DURING TAKEOFF ROLL. MAINTENANCE INSPECTED AND DEFERRED THE FLIG HT DIRECTOR TAKEOFF MODE PER MEL 22-10-02. MAINTENANCE OPS CHECKED THE TAKEOFF MODE FOR THE FLIGHT DIRECTOR IN ACCORDANC E WITH THE AIRCRAFT MAINTENANCE MANUAL 22-11-31-710-801-A01. OPERATIONAL CHECKS GOOD AT THIS TIME, MEL CLEARED. AIRCRA FT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007071000422 20070710 00422 NM 2007 7 10 2007UALA02285 1 20070628 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY LIGHT INOP: DOOR 3L EXIT SIGN BELOW MONITOR. FOUND LOOSE CONNECTION, SECURED, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000118 20070620 00118 NM 2007 6 20 2007UALA01599 1 20070521 A 2432 018550000 BATTERY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE MAIN LOOSE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 672UA 30027 MAIN BATTERY CHARGER STATUS MSG REPORTED BY CREW. INTERCHANGED MAIN BATTERY AND APU BATTERY PER MM 24-31-01 AND MM 24-3 1-04. SUSPECT FAULTY CONNECTION, CHARGER TO MAIN BATTERY. EICAS MSG ERASED AND NOW MAIN BATTERY OPERATES NORMALLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071100341 20070711 00341 2007 7 11 2007UALA02340 4 20070630 A 2565 COVER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE EVAC SLIDE MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 903UA 25003 DOOR 2L MANUAL INFLATION HANDLE EXPOSED (MISSING VELCRO COVER). [07-24-07] REPOSITIONED SLIDE PACK. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071300313 20070713 00313 NM 2007 7 13 2007UALA02394 1 20070704 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 CEILING EMERGENCY LIGHTS INOP AT ROWS 16 & 17. REPLACED LAMPS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071800304 20070718 00304 NM 2007 7 18 2007UALA02432 1 20070706 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY LIGHT DOOR 4R AFT SILL LIGHT INOP. [07-27-07] RELAMPED SILL LIGHT. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071900287 20070719 00287 NM 2007 7 19 2007UALA02477 1 20070706 A 3350 LAMP BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 912UA 25290 STOW BIN 2A EMERGENCY LIGHT IS INOPERATIVE. [07-27-07] RELAMPED. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071100255 20070711 00255 NM 2007 7 11 2007UALA02217 1 20070625 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY CEILING LIGHT INOP AT 26 ABC. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071700009 20070717 00009 WP 2007 7 17 DELA200700005 2 20070627 A 7297 WIRE HARNESS LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP LT ENGINE DAMAGED E DELA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 431AS 431 P89254 LT ENGINE N1 LAGGED BEHIND RT ENGINE N1 ON TAKEOFF ROLL, AND ALSO LT ENGINE COMPUTER LIGHT CAME ON. FOUND (B) SOLENOID OF SERVO VALVE CONNECTOR HAD EXPOSED WIRE. RE-TERMINATED PINS (A) AND (B) OF CONNECTOR PLUG. CREW CONDUCTED HIGH POWER RUN AND HIGH SPEED TAXI, OPS CHECKED GOOD. 2 L 7 2 4F 4 F A10CE E6WE 2007072300026 20070723 00026 NM 2007 7 23 2007UALA02546 1 20070710 A 2432 CHARGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MAIN BATTERY UNKNOWN A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 514UA 24839 MAIN BATTERY CHARGER STATUS MESSAGE DISPLAYED. [08-08-07] REPLACED AC MAIN BATTERY AND CHARGER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007072400178 20070724 00178 2007 7 24 2007UALA02612 4 20070712 A 2565 HOSE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ESCAPE SLIDE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 RIGHT OVERWING SLIDE CYLINDER LWR INFLATION HOSE IS KINKED AND COLLAPSED. [08-07-07] REPLACED HOSE IAW 20-10-10. SL IDE PROBLEM ROOT CAUSE: SLIDE & INFLATION HOSE ARE IN AN AREA CONTAINING MANY HYDRAULIC LINES & SERVICING ACCESS; SUSPE CT HOSE DAMAGED BY SKYDROL CONTAMINATION. SLIDE & AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007073000210 20070730 00210 CE 2007 7 30 DXTA200702350 1 20070719 A 2760 SPOILER SYS BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE OUT OF RIG E DXTA O OTHER F FLT CONT AFFECTED LD LANDING 1 GL 07 115QS RK383 FLIGHT CONTROLS VERY SLACK/SLOPPY ABOUT THE ROLL AXIS. SPOILER BUZZ NOTED IN TURNS TO THE RT. EXECUTIVE CONTROL INPUT R EQUIRED TO INITIATE AND ROLL OUT OF TURNS. ADJUSTED LT AND RT NEUTRAL POINT OF SPOILERS. RIGGED LT SPOILERS DOWN AND R IGGED RT SPOILERS UP TO WITHIN LIMITS LISTED IN MM. INSPECTED CABLE TENSIONS AND FOUND GOOD. INSPECTED TRAVELS AND FOUND GOOD. ALL WORK PERFORMED IAW BEECHJET 400XP MM CH 27-60-00. 2 H 7 2 4F 4 F RT A16SW E25EA 2007073100010 20070731 00010 NM 2007 7 31 2007UALA02657 1 20070715 A 3350 3071BPEGPL LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 773UA 26929 THE 1F FWD, 3E AFT, 9F AFT & 17G EEL LIGHTS ARE INOPERATIVE. RELAMPED. BACK TO NORM, OK FOR SVC. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007080600165 20070806 00165 NM 2007 8 6 2007UALA02793 1 20070723 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 LEFT EEL INOP: SEATS 46-52ABC & 56ABC. *S/D* REPLACED LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080800023 20070808 00023 2007 8 8 ASMF200707012 1 20070716 A 3150 WARNING MESSAGE CFMINT CFM567 CFM567B22 13802 NE COCKPIT MULTIPLE IND W ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 904AM AIRCRAFT REJECTED TAKEOFF AT LESS THAN 60 KNOTS, CONFIGURATION WARNING APPEARED. MAINTENANCE PERSONNEL PERFORMED PSEU TE ST AND OBTAINED THE FAILURE CODES 31-55006 (STAB TRIM GND) 31-5507 (STAB TRIM NOT GND) AND 31-55008 (T.O.WARN INHIBIT). PERFORMED THE REVIEW AND RESET OF SWITCHES P6-3, C-18 (LANDING GEAR TAKE OFF WARNING CUOFF) AND P6-3, D-18 (LANDING G EAR AURAL WARNING) IAW FIM31-51 PROCEDURE TASK 821; ADDITIONALLY, WARNING TAKE OFF ALARM TEST WAS PERFORMED IAW FIM 31- 51 PROCEDURE TASK 801, ALL CORRECT. 4 F E00055EN 2007081000051 20070810 00051 CE 2007 8 10 DXTA200702369 1 20070731 A 3240 PRESSURE SWITCH CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG BRAKES MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 361QS 5600361 ON FINAL APPROACH THE BRAKE LOW PRESSURE AND ANTI SKID INOP LIGHT ANNUNCIATORS ILLUMINATED FOR ABOUT 10 SECONDS AND THEN EXTINGUISHED. DURING TAXI THE LIGHTS ILLUMINATED AGAIN AND BOTH THE CAPTAIN AND F/O BRAKES BECOME EXTREMELY MUSHY. AF TER ABOUT 10 SECONDS THE BRAKE PUMP CYCLED AND BRAKE PRESSURE WAS RESTORED. REMOVE & REPLACE BRAKE SYSTEM HIGH/LOW PRE SSURE SWITCH. OPS & LEAK CHECKS GOOD IAW CE560MM 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007081700239 20070817 00239 NM 2007 8 17 QXEA200701275 1 20070810 A 3150 WARNING LIGHT DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NONE NONE A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 350PH 488 PDX FLIGHT NR 2184 ECU MANUAL CAUTION LIGHT. MAINTENANCE CYCLED BETA LOCKOUT CIRCUIT BREAKER. MANUAL LIGHT EXTINGUISHE D. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2007080800022 20070808 00022 CE 2007 8 8 DJFA2007076 1 20070718 A 2150 73838433 ACM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL SEIZED E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 23 702LX 4843 7500076 TRIP NR 1205032- ON DESCENT CREW NOTED ACM NOT COOLING AND BURNING ODOR IN CABIN. CREW COMPLETED THE APPROACH AND LANDI NG. MAINTENANCE FOUND THE ACM TURBINE SEIZED. THE ACM WAS REPLACED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007081000043 20070810 00043 EA 2007 8 10 A6WA200740355 1 20070625 A 5340 601R3111357 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FS 280, LBL9 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AW 7878 2 EA, CRACKED ANGLES AT FS 280, LBL 9.0. MAINTENANCE REMOVED AND REPLACED ANGLES AT FS280, LBL 9 CRJ 200, SRM 51-42-21 AND BSC SR 601R-53-0057A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007080900166 20070809 00166 NM 2007 8 9 2007UALA02890 1 20070730 A 3350 58807 LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 903UA 25003 EEL LIGHTS ON FLOOR IN AFT GALLEY IS INOPERATIVE. DRIED WATER OUT OF EEL TRACK. 2 L 7 2 4F 4 F RT A16WE E2GL 2007081700215 20070817 00215 NE 2007 8 17 KPVA20079 2 20070803 A 7421 CH34817 IGNITER DHAV DHC8 DHC8103 1386005 NM PWA PW121 PW121 52124 NE NR 2 ENGINE MISSING A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 808WP 026 (PIREP) NR 2 ENGINE INBOARD AIR VENT BURNED OFF 5 OF 9 SLATS & PAINT AROUND THE AREA BURNED AS WELL. (MX) PERFORMED VIS UAL INSPECTION OF NR 2 NACELLE, FOUND INBOARD IGNITER NOT INSTALLED ON ENGINE. RE-INSTALLED IGNITER IAW DHC-8 MM 72-01- 20 SEC 5B PG 402. ALSO FOUND INBOARD NACELLE AFT DOOR BURNED. REMOVED AND REPLACED DOOR IAW DHC-8 MM 71-10-00 PAR 16 P G 206. NOTE: TEMPORARY RD8-54-2383 INITIATED FOR CONTINUED AIRWORTHINESS UP TO 5000 HOURS WITH REPETITIVE INSPECTIONS EVERY 100 HOURS ON INBOARD ENGINE SUPPORT STRUT P/N 85410029-053, S/N 0118. 2 H 7 2 4T 4 T RT A13NM E20NE 2007082300179 20070823 00179 NM 2007 8 23 2007UALA03035 1 20070805 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEATS 4A, 4E & 5 UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 116UA 26908 EEL STRIPS ON SEATS 4A, 4E, 5E FALLING OFF. 08-31-07 SECURED EEL STRIPS AS REQUIRED . SYSTEM CHECKED OKFOR SERVICE 2 L 7 4 4F 4 F RT A20WE E24NE 2007082800033 20070828 00033 NM 2007 8 28 2007UALA03239 1 20070819 A 3350 58781 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 656UA 25394 FLOOR MOUNTED EEL LIGHTS INOP, RT AISLE IN FIRST CLASS. REPLACED POWER STRIP IN FLOOR TRACK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082800036 20070828 00036 NM 2007 8 28 2007UALA03242 1 20070818 A 3350 POWER SUPPLY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 583UA 26705 ALL EMERGENCY EXIT LIGHTS IN L-4 DOOR AREA ARE INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082400239 20070824 00239 EU 2007 8 24 KC82007F00000 1 20070716 A 2840 1317AB TRANSMITTER AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D 30010 NE LT FUEL TANK MALFUNCTIONED E KC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 995CK 95 245274 THE LT FUEL TRANSFER PUMP STOPPED TRANSFERING FUEL TO THE LT FEEDER FUEL TANK ON THE PREVIOUS LEG. THE TRANSFER PUMP WA S DEFERRED IAW THE APPROVED MEL. DURING THE NEXT LEG, THE FEEDER FUEL TANK QUANTITY SENDING UNIT STUCK AT THE HIGH INDI CATED POSITION. EVENTUALLY THE LT ENGINE FUEL PRESSURE LIGHT CAME ON DURING CRUISE AND THE ENGINE SHUTDOWN DUE TO FUEL STARVATION. THE CREW DESCENDED TO A LOWER ALTITUDE. THE ENGINE FUEL SUPPLY WAS TRANSFERED FROM THE RT WING FUEL TANK. THE ENGINE WAS RESTARTED AND THE CREW ELECTED TO DIVERT TO STL FOR FURTHER INVESTIGATION. MAINTENANCE WAS DISPATCHED T O THE AIRCRAFT FOR REPAIRS. THE LT FUEL TRANSFER PUMP WAS REPLACED AND THE LT FEEDER FUEL QUANTITY SENDING UNIT WAS FOU 2 L 7 2 4F 4 F A7EU E7EA 2007090700076 20070907 00076 NM 2007 9 7 2007UALA03187 1 20070815 A 3397 794440 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHT ROW 52 HJK INOP. *S/D* RESECURED CONNECTOR, OP CHECK NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092000153 20070920 00153 NM 2007 9 20 2007UALA03601 1 20070906 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 FWD PIT DOORWAY AFT SIDE FRAME IS CRACKED AT LOWER DOOR STOP FITTING. 2 L 7 2 4F 4 F RT A16WE E21EU 2007092500114 20070925 00114 NE 2007 9 25 HEEA117246 1 20070906 A 3297 WIRE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL CONTROL PANEL LOOSE E HEEA O OTHER O OTHER LD LANDING 1 SW 03 792P 760193 AIRCRAFT WAS PICKED UP AT BASE AND FLOWN TO MAINTENANCE. NORMAL EXTENSION AND RETRACTION. AFTER TAKEOFF, GEAR RETRACTE D NORMALLY. UPON ARRIVAL, GEAR WOULD NOT EXTEND. PERFORMED EMERGENCY PROCEDURE AND BLEW GEAR DOWN AND LANDED LIGHT ON WHEELS, GEAR WAS PINNED AND AIRCRAFT SHUTDOWN. MAINTENANCE REPAIRED LOOSE WIRE AT THE LANDING GEAR CIRCUIT BREAKER AND REPLACED THE LANDING GEAR CONTROL PANEL. 1 G 7 2 3U 3 U H1NE E1GL 2007092500136 20070925 00136 CE 2007 9 25 DXTA200702487 1 20070920 A 2611 SMOKE WARNING CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CARGO BAY FALSE INDICATION E DXTA O OTHER N FALSE WARNING LD LANDING 1 GL 07 915QS 7500015 (P) (BAG SMOKE) CAS ILLUMINATED AFTER LANDING, NO SMOKE WAS DETECTED AFTER INSPECTING THE BAGGAGE COMPARTMENT. 09-28- 07 PERFORMED OPS TEST OF BAGGAGE SMOKE DETECTOR SYSTEM. NO DEFECTS NOTED. ALL WORK PERFORMED IAW CE750/X MM 26-14-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008040800064 20080408 00064 NM 2008 4 8 HNAA0800063 1 20071128 A 5347 85300132101 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 804EX 227 CTR FLOOR LEFT SEAT TRACK CORRODED. REPLACED DEFECTIVE SEAT TRACK. 2 H 7 2 4T RT A13NM 2007092600023 20070926 00023 EU 2007 9 26 07FDEA04037 1 20070919 A 5310 DOOR FRAME AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 DURING LT FWD PAX DOOR FRAMING AFT PANEL REPLACEMENT, A DOUBLE HOLE WAS PERFORMED AT FRAME 18, STRG 26 IN LOWER BEAM W EB AT ITS REAR END AND IN STRG 26 COUPLING. REPAIR PERFORMED BY CUT OUT OF LOWER BEAM WEB IAW EA 6-5312-81117 AND RAS/A S/0017/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007091900085 20070919 00085 EU 2007 9 19 07FDEA03623 1 20070912 A 5313 A53610797234 LONGERON AIRBUS 310 A310324 3930206 EU ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 812FD 467 FOUND SPLICE REPAIR ON EXTRUSION BETWEEN FRAME 12A-14, Y-953 RT, MATERIAL NOT CONFORM TO SRM 53-12-15/FIG 207. SPLICE REPAIR ON EXTRUSION RENEWED IAW SRM 53-12-15/FIG 207. 2 L 7 2 4F RT A35EU 2007042400056 20070424 00056 EU 2007 4 24 07FDEA01441 1 20070411 A 5730 SKIN AIRBUS 310 A310 EU CENTER WING CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 801FD 539 CORROSION FOUND IN CWB UPPER SURFACE BETWEEN FR46/47 AND FR48 BETWEEN Y1555 AND Y1850. PERFORM NDT INSPECTION NTM 51-10- 08, 51-10-01 AND 51-10-04. REPAIRED PER SRM 57-10-12 PG. 201. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. 2 L 7 2 4F RT A35EU 2007032900328 20070329 00328 NM 2007 3 29 07FDEA00922 1 20070316 A 5280 DOOR DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT MLG FLAPPER DOOR FWD CORNER FOUND CRACKED. REPAIR CARRIED OUT AT RIGHT HAND MLG FLAPPER DOOR FWD CORNER AS PER SR M 52-10-00 FIGURE 18 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007041200057 20070412 00057 NM 2007 4 12 07FDEA01368 1 20070406 A 5740 ATTACH FITTING BOEING 727 727225 1384077 NM LT WING TE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 LT WING NR 1 KRUGER FLAP ALL 3 HINGES, HARDWARE HAS RUST CENTER CASTING AT ACTUATOR ATTACH, 1 HOLE IS CORRODED EDGE DAMA GED. REPLACED NR 1 KRUGER FLAP REFERENCE MM 27-81-001-4 ADJUSTMENT AND CHECK PERFORMED REF W/C70C007-00. 2 L 7 3 4F A3WE 2007070200046 20070702 00046 NM 2007 7 2 HALA0700263 1 20070623 A 3350 BPS73 BATTERY PACK BOEING 767 7673G5 1385126 NM EMERGENCY LIGHTS INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 585HA 24257 EMERGENCY ESCAPE SLIDE TEST, NOT TESTING IN TEST 1 RT SIDE. REMOVED AND REPLACED RT ESC SLIDE BATT PACK AND CHARGER PER AMM 33-51-07. OPS TEST NORMAL. 2 L 7 2 4F RT A1NM 2007111300154 20071113 00154 WP 2007 11 13 UPS07851105 1 20071012 A 5340 FITTING DOUG DC8 DC873F 302199F WP FS 70 L27R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 L27R END FITTING CORRODED AT AFT SIDE OF STA 70 FRAME, A-PIT. REMOVED, AND REPLACED LONGERON END FIT TING AT STA 70 L27R IAW SRM 53-2-0 FIG 001, SRM 51-1-24, AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2007091900067 20070919 00067 EU 2007 9 19 07FDEA03696 1 20070913 A 5712 A57242444 RIB AIRBUS 310 A310203 3930313 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 FOUND ON RT MLG FWD LUG INNER BORE RIB 5 THE BUSHING TO BE OUT OF ROUND, AFTER REMOVAL OF BUSHING FOUND CORROSION ON TH E LUG REPAIR PERFORMED BY CORROSION REMOVAL AND REAM UP THE HOLE IAW DRAWING R572-49121, APPROVED BY EA 6-5751-8106 AND RAS/BAE/0979/2004 ISS A. 2 L 7 2 4F RT A35EU 2007061100055 20070611 00055 EU 2007 6 11 07FDEA02048 1 20070602 A 5310 STRUCTURE AIRBUS 310 A310203 3930313 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 401FE 191 2 HOLES ELONGATED AT FS 54 STRINGER 37 LT NR 1 =.187 BY .220 AND NR 2 = .200 BY .239, REPAIRED HOLES IAW EA 6-5330-11046 2. 2 L 7 2 4F RT A35EU 2007091200121 20070912 00121 EU 2007 9 12 07FDEA03444 1 20070907 A 5313 A5397422470 STRINGER AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 808FD 439 CORROSION ON STRINGER 49, BETWEEN FRAME 65-66, OUT OF LIMIT AS PER SRM 53-10-00. STRINGER SPLICE REPAIR PERFORMED IAW S RM 53-10-14/FIG 201. 2 L 7 2 4F RT A35EU 2007102200214 20071022 00214 NM 2007 10 22 2007UALA04183 1 20071011 A 3350 58674 INVERTER BOEING 737 737322 1384676 NM EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 332UA 24193 EMERGENCY FLOOR LIGHTS AFT OF ROW 15, DO NOT WORK. REPLACED INVERTER. 2 L 7 2 4F RT A16WE 2007092000314 20070920 00314 NM 2007 9 20 QXEA200701421 1 20070916 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 424QX 4006 SEA FLIGHT NR 2332: AFTER START 'PUSHER SYSTEM FAIL' MASTER CAUTION ILLUMINATED. AIRCRAFT RETURNED TO BLOCK. MAINTENAN CE INTERROGATED CDS. NO FAULTS FOUND. CYCLED A/C POWER AND CAUTION LIGHT EXTINGUISHED. C/W OPS CHECK OF THE ELEVATOR CONTROL STICK PUSHER SYSTEM IAW Q400 AMM TASK 27-33-00-710-802. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007071200097 20070712 00097 NM 2007 7 12 F3LA200700151 1 20070627 A 5321 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT FLOOR PANEL 131AF DAMAGED. REPAIRED FLOOR PANEL 131AF IAW S RM 53-02-00, FIG 204. 2 L 7 2 4F RT A28NM 2007081700225 20070817 00225 NM 2007 8 17 07FDEA02822 1 20070810 A 5280 SKIN BOEING 727 727233 138408A NM LT MLG DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 254FE 20936 LT MLG FLYING DOOR UPPER MID INNER SKIN EDGE CRACKED REPAIRED IAW SRM 51-40-2. 2 L 7 3 4F RT A3WE 2007092700391 20070927 00391 EU 2007 9 27 07FDEA04140 1 20070921 A 5330 A53778628 SKIN PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORROSION ON INTERNAL SKIN BETWEEN FRAME 37-38, STRG 53 RT - 54 LT. REPAIR PERFORMED BY BLEND OUT, HFEC/ROTOTEST INSPEC TION AND FLAP PEENING IAW EA 6-5314-82916 AND RAS/DATLS/0002629/2005 ISSUE A. 2 L 7 2 4F RT A35EU 2007013100266 20070131 00266 EA 2007 1 31 COMA0760072 1 20070127 A 3297 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA MLG LOOSE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 951CA 7091 FLIGHT 5196 - DEPARTING LGA SELECTED GEAR UP AND RECEIVED GEAR DISAGREE MESSAGE AND NOSE GEAR WAS STILL DOWN. DIVERTED TO JFK. LANDED WITHOUT INCIDENT. FOUND NOSE GEAR SELECTOR VALVE CONNECTOR BACKED OFF. RESECURED CONNECTOR, SWUNG GEAR , NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2007073000064 20070730 00064 NM 2007 7 30 07FDEA02603 1 20070725 A 3230 A20092000001 SOLENOID BOEING 727 727233 138408A NM MLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 275FE 22040 AFTER LIFTOFF AND GEAR RETRACTION LANDING GEAR LEVER WOULD NOT RAISE PAST THE OFF POSITION. THE LEVER LATCH LIGHT CIRC UIT BREAKER IMMEDIATELY OPENED AND THE FORWARD LANDING GEAR ANNUNCIATOR PANEL LIGHTS INDICATED ONLY THE GREEN NOSE GEAR LIGHT. CONSULT QRH FOR "LEVER LATCH FAILED TO RELEASE" AND "MANUAL GEAR EXTENSION PROCEDURES", VERIFIED GEAR DOWN WIT H POINTERS AND LANDED NORMALLY. FOUND LEVER LATCH COIL SHORTED. REMOVED AND REPLACED LEVER LATCH PER MM 32-31-016-4. OPS CKS GOOD. JACKED A/C PER MM 07-11-000-2. SWUNG LDG SEVERAL TIMES PER MM 32-32-000-5. ALL INDICATIONS CK. 2 L 7 3 4F RT A3WE 2007012900101 20070129 00101 NM 2007 1 29 07FDEA00164 1 20070125 A 5330 LAP JOINT BOEING 727 727233 138408A NM BS 1178 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 AFT PIT AT STA 1178, BETWEEN STR 25R TO 26R, WL 149 AT SKIN LAP HAS CORROSION. REPAIRED DAMAGED SKIN LAP REF EA NR 7-53 30-106984 AND AAR EA NR I070056 ATTACHMENT "A" FOR WORK INSTRUCTIONS. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007080300112 20070803 00112 EU 2007 8 3 07FDEA02644 1 20070728 A 5330 20240BARE063 SKIN AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 657FE 748 MDCC FR 24 HAS A DENT 3 IN BY 1 IN BY .032 IN BETWEEN STR 12R AND 13R - ZONE 230 - REF A300 AMM 53-13-11. COMPLIED IAW EA 6-5310-110523. 2 L 7 2 4F RT A35EU 2007070200049 20070702 00049 EU 2007 7 2 AWXA200700767 1 20070623 A 5321 D5367180500300 FLOOR PANEL AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 SAL - MAJOR REPAIR - CORROSION ON CABIN FLOORBOARD 262FF, FR 66 - FR 68, -Y1292 TO -Y1732. REPLACED CABIN FLOORBOARD 26 2FF, FR 66 - FR 68, -Y1292 TO -Y1732 IAW AWA TASK CARD C1C53303. 2 L 7 2 4F RT A28NM 2007040200049 20070402 00049 EU 2007 4 2 07FDEA00967 1 20070316 A 5312 PRESSURE PANEL AIRBUS 310 A310324 3930206 EU NLG WW DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 813FD 500 FASTENER CAN'T BE INSTALLED AT AFT NOSE LANDING GEAR PANEL, C17-18, P52-53 RT. REPAIR WAS PERFORMED BY FASTENER SUBSTIT UTION IAW EA 6-5312-103408 REV A. 2 L 7 2 4F RT A35EU 2007030900228 20070309 00228 2007 3 9 F3LA200700040 4 20070301 A 2565 LATCH AIRBUS A319 A319111 3930336 NM GIRT BAR STUCK A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 931FR 4727 2253 DURING C-2 CHECK INSPECTION, REPORTED GIRT BAR LATCH STUCK IN THE DOWN POSITION - L1 DOOR AFT LATCH. CLEANED GIRT BAR F ITTING IAW AMM 12-21-12-100-006. 2 L 7 2 4F RT A28NM 2008010400195 20080104 00195 NM 2008 1 4 F3LA200700397 1 20071215 A 5315 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 912FR 5942 1803 DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT FR16, STA Y254, CORRODED ON THE TOP CAP. DETERMINED CORROSION TO B E OUT OF LIMITS IAW SRM 53-11-14. REMOVED AND REPLACED FLOORBEAM FROM FR12 THRU FR24, STA 254, IAW SRM 52-42-11 AND 51- 72-11. 2 L 7 2 4F RT A28NM 2007022300063 20070223 00063 NM 2007 2 23 07FDEA00538 1 20070222 A 5310 UNKNOWN DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 CENTER CARGO BETWEEN STA 1561 TO STA 1581 STR 48R FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 53-10- 00 FIG. 2 VOL .I. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080811 EU 2008 8 11 M7K2008F00049 1 20070919 A 5100 350A25040500 ANGLE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE UNKNOWN CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 805MH 2304 3799 23091 FITTING FOUND CRACKED DURING INSP. A NEW FITTING INSTALLED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 2007010800298 20070108 00298 NM 2007 1 8 2007UALA00030 1 20070103 A 2421 IDG AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 MALFUNCTIONED A UALA A UNSCHED LANDING G MULTIPLE FAILURE NR NOT REPORTED 1 WP 29 848UA 1647 AIRCRAFT LOST GENERATOR 2 IDG AND APU GENERATOR. FOUND FOD IN APU INLET. REMOVED DEBRIS, ACCOMPLISHED OP CHECK OF APU, NO DISCREPANCIES NOTED.REPLACED NUMBER 2 ENGINE IDG. INSPECTED IDG PYLON MOUNTED CONNECTOR, NO ARCING NOTED. OPS CHEC K OF IDG NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007012500267 20070125 00267 EU 2007 1 25 2007UALA00126 1 20070118 A 2910 FLUID AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYDRAULIC SYS LEAKING A UALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 WP 29 407UA 456 RTFL WITH GREEN SYSTEM HYD LOSS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007012500316 20070125 00316 SO 2007 1 25 RAIA00701019 1 20070113 A 5210 CONNECTING ROD EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL PAX DOOR OBSTRUCTED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 831HK 145232 PRE FLT NR 7883-TYS-MAIN DOOR WILL NOT CLOSE SHUT. MAINTENANCE FOUND SAFETY WIRE PIGTAIL ON FWD NR 5 CONNECTING ROD INT ERFERING WITH DOOR CLOSING. CONNECTING ROD WAS RESAFTIED AND DOOR CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2007012200161 20070122 00161 NM 2007 1 22 2007UALA00075 1 20070110 A 5542 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RUDDER DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 LEFT SIDE OF THE RUDDER EXTERNAL SURFACE HAS EXPOSED COMPOSITE FIBER STRANDS AT 2 EACH EXISTING REPAIRS BETWEEN NR 4 HIN GE AND COUNTER WEIGHT HORN. MAJOR REPAIR: REPAIRED RUDDER IN SHOP PER SM 95-55-40-01JD AND GNMM 6-0-2-23. 2 L 7 2 4F 4 F RT A16WE E21EU 2007013000070 20070130 00070 CE 2007 1 30 DXTA200701864 1 20070118 A 2720 67184645 LOGIC CARD CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RUDDER LIMITER INOPERATIVE E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 983QS 4941 7500083 RUDDER LIMITER FAIL B EICAS MESSAGE RUDDER LIMIT 90%.GAINED ACCESS TO THE RUDDER LIMITER PCB NK124. REMOVED RUDDER LIMIT ER PCB NK124 AND INSTALLED A NEW RUDDER LIMITER PCB. CONNECTED THE AIR DATA TEST SET AND APPLIED ELECTRICAL POWER. APPLI ED HYDRAULICS AND PERFORMED RUDDER LIMIT TEST SEVERAL TIMES. OPS CHECK GOOD. REMOVED DATA TEST SET. CLOSED LOGIC MODULE AND MAIN "J" BOX COVER WORK DONE IAW CH 24-53-20 AND CH. 27-20-00 OF THE 750 MM 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007013100137 20070131 00137 NM 2007 1 31 2007UALA00210 1 20070126 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EEL'S INOP ON CEILING AT SEAT ROW 56R. EEL BROKEN AT SEAT 1J. RELAMPED BOTH POSITIONS; OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007020600098 20070206 00098 NE 2007 2 6 DL76G070064 2 20070129 A 7261 CF680C2B6F ENGINE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 LEAKING A DALA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 27 1609 38049 38049 704806 30574 704806 ON WALKAROUND, FOUND OIL DRIPPING FROM BOTTOM AFT END OF THRUST REVERSER AND PUDDLING IN COR COWL NR 2 ENG ADDED 5 PINTS . UPON ARRIVAL REMOVED RECOUP DUCTS AT 6 O`CLOCK AND 8 O`CLOCK POS SEE ITEM 10 FOR T/S FINDINGS REQ ENG CHA REPLACED E NGINE IAW TRANSMITTAL 1T161. 2 L 7 2 4F 4 F RT A1NM E13NE 2007022100169 20070221 00169 NM 2007 2 21 2007UALA00255 1 20070129 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 127UA 28813 SEAT 1J EMERGENCY LIGHT STRIP BROKEN. REPLACED LIGHT STRIP. OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022300224 20070223 00224 NM 2007 2 23 2007UALA00391 1 20070210 A 2560 GIRT BAR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE R4 DOOR FROZEN A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 783UA 26950 UPON ARRIVAL FLT ATTENDANT UNABLE TO DISARM DOOR 4R. FOUND GIRT STILL FROZEN TO SILL. WARMED & DRIED OFF AREA, CLEAN ED AND GREASED GIRT BAR MECHANISM AND ARMING MECHANISM. DOOR 0PERATES NORMALLY. REACTIVATED BOTTLE AND SLIDE. CYCLED AR M-DISARM LEVER, OPENED DOOR SEVERAL TIMES. CLEANED GIRT BAR AREA OF MOISTURE PER MT 52-UA4R3. DOOR OPERATES NORMALLY. R ETURN TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007031500117 20070315 00117 NM 2007 3 15 2007UALA00641 1 20070302 A 5512 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RUDDER GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 RUDDER LEFT SIDE - HAS GOUGE WEAR FROM BLADE SEAL NEAR THE BOTTOM. *S/D* MAJOR REPAIR: ACCOMPLISHED COMPOSITE REPAIR PER AAR EA-I070147. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032200027 20070322 00027 CE 2007 3 22 MWA070314020 1 20070315 A 5754 11811004782 STRUCTURE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT WING DAMAGED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 10675 19611 UE229 REPAIRED BIRD STRIKE RT OB WING LEADING EDGE STATION WS 243 REPAIRED IAW AAE REPORT 6620-1 DATED MARCH 15, 2007. 2 L 7 2 4T 4 T RT A24CE E26NE 2007032200061 20070322 00061 NM 2007 3 22 2007UALA00721 1 20070311 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 947 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 364UA 24533 AFT CABIN FLOORBEAM HAS TOOLING MARK 27 INCHES LONG DOWN CENTER OF T-CAP STA 947 LBL 12 RBL 15. MAJOR REPAIR ACCOMPLISH ED: INSTALLED T-CAP SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032300003 20070323 00003 NM 2007 3 23 QXEA200700373 1 20070314 A 6120 697072003 GOVERNOR BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA NR 2 OVERSPEED MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 424QX 411 4006 FLIGHT NR 2300: NR 2 ENGINE TOOK 28 SECONDS TO COME OUT OF FEATHER. AIRCRAFT RETURNED TO BLOCK. MAINTENACE REMOVED AND R EPLACED NR 2 OVERSPEED GOVENOR IAW AMM TASK 61-20-26-000-801 AND 61-20-26-400-801. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2007032900315 20070329 00315 EA 2007 3 29 A6WA200740135 1 20070317 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 415AW 7593 RT WING PLANK ACCESS HOLE AT 640 AB HAS MINOR PITTING IN CRITICAL AND NON-CRITICAL AREA. (K) [SUP 06-05-07] MAINTENA NCE CLEANED EDGE OF FUEL TANK ACCESS DOOR SKIN CUTOUT. BLENDED CORROSION IN DETAIL AREA I AND IV TO DEPTH OF .002 IAW S TEPS 1-4 OF BOMBARDIER REO 601R-57-21-030. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007032800038 20070328 00038 NE 2007 3 28 SWAA071545 2 20070323 A 7200 CFM567B ENGINE BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B22 13802 NE NR 2 FAILED A SWAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 793SA 27888 888141 IN FLT SHUT DOWN / DIVERSION / DECLARED EMERGENCY. NR 2 ENG FAILED, ENGINE SHUTTERED BANGED (FLAME OUT BACK) AND RED AR C LIGHT ILLUMINATED. REMOVED AND REPLACED NR 2 ENG PER MM. 2 L 7 2 4F 4 F RT A16WE E00055EN 2007040300047 20070403 00047 CE 2007 4 3 HSRA3132007 1 20070313 A 5730 SKIN BEECH 90 C90 1152913 CE PWA PT6 PT6A21 52043 EA LT WING CRACKED E HSRA K NONE O OTHER IN INSP/MAINT 1 NM 05 90EJ 11360 LJ749 FOUND CRACKS IN THE WING SKIN ON THE LT WING UPPER CENTER SECTION WHERE IT IS RIVETED TO THE ATTACH FITTING. THE FORWAR D OB FAIRING NEXT TO THE NACELLE MUST BE LIFTED TO SEE THE CRACKS. LIKELY CAUSED BY LANDING CYCLES AND FATIGUE. SUBMIT TER ADVISES THAT MFG HAS A FIX FOR THIS PROBLEM. 1 L 7 2 3T 4 T 3A20 E4EA 2007041000001 20070410 00001 NE 2007 4 10 2007F00025 2 20070322 A 7261 ENGINE BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE LEFT MAKING METAL G A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 209CM 5099 2110 BB1613 PCEPJ0181 SHORTLY AFTER TAKEOFF CLIMBING THROUH 6,000 FEET, THE LT CHIP DETECTOR LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO DEPA RTURE WITHOUT INCIDENT. NO OTHER ABNORMAL ENGINE PARAMETERS WERE NOTED. INVESTIGATION FOUND FERROUS METAL ON THE CHIP DETECTOR AND METAL PARTICLES WERE FOUND IN THE OIL FILTER. THE LT ENGINE WAS REMOVED AND SENT TO A REPAIR FACILITY FOR INSPECTION AND REPAIR. DETAILED FINDINGS NOT AVAILABLE AT THIS TIME. 1 L 7 2 4T 4 T A24CE E4EA 2007032700178 20070327 00178 CE 2007 3 27 DXTA200702047 1 20070324 A 3240 BRAKE ASSY CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG SMOKE E DXTA O OTHER M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 924QS 7500124 DURING TAXI THE BRAKES STARTED TO DRAG AND MAKE A GRINDING NOISE. UPON VISUAL INSPECTION, THE RT OB BRAKE WAS SMOKING AN D ALSO VERY HOT. REMOVED NR 4 MLG WHEEL ASSY. INSPECTED BRAKE FOR DAMAGE AND FOD. NO DEFECTS FOUND. BRAKE SPUN FREELY. BLED NR 4 BRAKE ASSY. REMOVED EXCESSIVE AMOUNT OF AIR FROM BRAKE BLEEDERS. RE-PACKED WHEEL BEARING ON NR 4 WHEEL ASSY. R EINSTALLED WHEEL ASSY. IAW CE750 MM 32-42-00 & 32-41-02. INSPECTED EMERGENCY BRAKE AIR BOTTLE. BOTTLE IS SERVICED CORREC TLY WITH NO LEAKS NOTED. IAW CE750 MM 12-10-16. NO LEAKS OR FURTHER DEFECTS NOTED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007041600002 20070416 00002 NM 2007 4 16 F3LA200700064 1 20070330 A 5315 FLOORBEAM AIRBUS A319 A319111 3930336 NM GE CF700 CF7002D2 30010 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM BETWEEN FR68 AND FR69 AT -Y1162. FOUND TO BE OUT LIMITS IAW A319 SRM 53-00-14, FIG. 101. REMOVED AND INSTALLED FLOORBEAM ASSY IAW A319 SRM 51-42-11. 2 L 7 2 4F 4 F RT A28NM E7EA 2007041900007 20070419 00007 EU 2007 4 19 BAQA20070011 1 20070415 A 2697 355A67801206AB WIRE HARNESS AEROSP AS355 AS355F2 8680812 EU ALLSN 250C 250C20F 03013 GL ZONE 400 FATIGUED E BAQA A UNSCHED LANDING N A FALSE WARNING FLAME/FIRE NR NOT REPORTED 1 EA 03 912KY 7133 41 5500 CAE840418 DURING CRUISE FLIGHT THE RT (NR 2) ENGINE FIRE WARNING LIGHT ILLUMINATED WITH NO SECONDARY INDICATION OBSERVED. AIRCRAF T LANDED SAFELY AT A NEARBY EMS HELIPAD WHERE TECH FOUND A BROKEN WIRE AT ONE OF THE ENGINE DETECTORS. WIRING REPAIRED IAW MFG STANDARD PRACTICES MANUAL. 1 G 7 2 3U 3 U H11EU E4CE 2007041900122 20070419 00122 NM 2007 4 19 2007UALA01101 1 20070410 A 5523 TAB BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU ELEVATOR TRIM MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 905UA 25005 WHILE DOING LEFT & RIGHT ELEVATOR TAB FREE PLAY CHECK, FOUND ON BOTH ELEVATOR TRIM TABS THAT BOLT HEADS ARE FACING INBOA RD NOT OUTBOARD. *S/D* HARDWARE WAS INSTALLED INCORRECTLY. REMOVED AND INSTALLED HARDWARE IN CORRECT CONFIGURATION. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041700253 20070417 00253 NM 2007 4 17 2007UALA00978 1 20070401 A 3350 20131A LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 508UA 24744 EMERGENCY LIGHTS - THE FOLLOWING ARE INOP: EXIT DOOR 2R, SEAT ROWS 2 AND 3 AND STOW BIN LIGHT AFT OF 3AB. REMOVED AND REPLACED LAMPS, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007042300003 20070423 00003 NM 2007 4 23 WRLA2007065 1 20070417 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 274WA 48633 DURING 4C+30/60M CHECK, EGAT MECHANIC FOUND MAIN DECK CARGO SEAT TRACK CRACK AT Y:755, X:78, Z:-18. [SUP 05-02-07] REPL ACED MAIN DECK CARGO SEAT TRACK PER MD-11 SRM 53-70-00 VOL.1 REV 38 FIG.1. 2 L 7 3 4F 4 F RT A22WE E24NE 2007043000104 20070430 00104 NM 2007 4 30 2007UALA01180 1 20070415 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 563UA 26665 EMERGENCY EXTERIOR SLIDE LIGHTS INOP AT DOORS 2R, 2L AND 4L. [SUP 05-08-07] RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2007051700073 20070517 00073 NM 2007 5 17 2007UALA01418 1 20070505 A 4900 APU BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE APU BAY FAULTY A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 117UA 28810 APU AUTO SHUTDOWN & FILLED ENTIRE CABIN WITH SMOKE. ALSO, SAW SMOKE COMING OUT OF TAILPIPE. [SUP 06-01-07] REPLACED A PU. RESTARTED APU NORMALLY, INDICATIONS NORMAL. OPERATED PACKS AND NO FURTHER SMOKE OR ASSOCIATED OIL SMELL IN CABIN. A /C RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007051700078 20070517 00078 NM 2007 5 17 2007UALA01423 1 20070505 A 3397 794640 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY EEL LIGHT INOPERATIVE AT SEAT 5F AFT. SECURED CONNECTOR, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007060500264 20070605 00264 NM 2007 6 5 2007UALA01682 1 20070525 A 5330 RIVET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 RIVET DAMAGED BY LIGHTNING STRIKE STA 590 WL 160 ON LEFT SIDE OF FUSELAGE. REMOVED BLIND RIVET. HFEC REVEALED NO CRACK S. INSTALLED SOLID. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500303 20070605 00303 NM 2007 6 5 2007UALA01724 1 20070529 A 2822 PUMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 589UA 28707 RTFL DUE TO LEFT AFT FUEL BOOST PUMP FAILURE. [06-20-07] LT AFT FUEL BOOST PUMP INOP. AFT FUEL BOOST PUMP PRESSURE S WITCH WAS REPLACED.PLAN TO LAND APPROX 10K OVERGROSS ON RETURN FOR FUEL BOOST PUMP FAILURE. ACCOMPLISHED PHASE 1 ACFT I NSPECTION AND NO DAMAGE FOUND. 2 L 7 2 4F 4 F RT A2NM E17NE 2007061200124 20070612 00124 EA 2007 6 12 VNAA0705008 1 20070529 A 5200 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE GPU OPEN A VNAA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 GL 05 710PS 10167 CREW REPORTED AN EXTERNAL GPU DOOR WAS LEFT OPEN ON INITIAL CLIMBOUT. CREW WAS INSTRUCTED TO RETURN TO CLT AND HAVE THE AIRCRAFT INSPECTED FOR DAMAGE. CREW LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NO DAMAGE. MAINT ENANCE CLOSED THE DOOR. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007061300327 20070613 00327 2007 6 13 2007UALA01780 4 20070603 A 2565 SLIDE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE DOOR 2L UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 936UA 26667 DOOR 2L SLIDE IS HANGING DOWN AND WILL CATCH IN DOOR WHEN CLOSED. [06-26-07] REPACKED SLIDE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007061900125 20070619 00125 SO 2007 6 19 GUUA06070701 1 20070607 A 3260 PROXIMITY SWITCH EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE DIRTY A GUUA O OTHER S AFFECT SYSTEMS LD LANDING 1 SO 29 261AS 120141 FLIGHT:9156 MHH/FLL, AFTER LANDING BOTH IDLE 1 AND IDLE 2 UNLOCK LIGHTS REMAINED ON, NO NOSE STEERING OR BRAKES, USED DI FFERENTIAL POWER AND RUDDERS TO CLEAR THE RUNWAY. CLEANED PROXIMITY SWITCHES AND CHECKED WIRING NO DEFECTS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 2007061900220 20070619 00220 NM 2007 6 19 2007UALA01811 1 20070602 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 20UAÊ 29166 EMERGENCY LIGHT ROW 1A AFT INOP. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000143 20070620 00143 NM 2007 6 20 2007UALA01958 1 20070609 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 UPPER DECK CEILING EMERGENCY LIGHT (2EA) IS INOPERATIVE. RELAMPED EMERGENCY LIGHT. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007062000171 20070620 00171 2007 6 20 2007UALA01986 4 20070613 A 3442 TRANSMITTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WEATHER RADAR FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 537UA 25157 RTFL DUE TO LOSS OF WEATHER RADAR AND EN ROUTE THUNDERSTORMS. [08-07-07] ERRATIC WX RADAR RETURNS AT VARIOUS RANGES F ROM 80, 40 AND 20 MI RANGES, FALSE RETURNS ARE DEPICTED AT AROUND THE 11'O'CLOCK AND 12'O-CLOCK, REPLACED WX RADAR TRAN SMITTER. 2 L 7 2 4F 4 F RT A2NM E17NE 2007060500203 20070605 00203 NM 2007 6 5 2007UALA01464 1 20070510 A 2520 1254171 POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SEAT 5C SHORTED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 659UA 27114 SEAT 5C ARMREST GETTING HOT. *S/D* TROUBLESHOOTING, DISCOVERED PAX HAD SPILLED GLASS OF CHAMPAGNE OVER ARM REST. COND UCTIVE LIQUID CAUSED INTERNAL SHORTING. C/B`S POPPED. DISCONNECTED LUMBAR CONTROL & POWER TO SEAT. REPLACED LUMBAR SW ITCH PCU PCN 560-4142 AND INSEAT POWER SUPPLY PCN 585-5187. OPS CHECK, OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007053000204 20070530 00204 EA 2007 5 30 HNAA0700093 1 20070526 A 2150 78279010 ACM DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE ODOR A HNAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 327 469 469 261 AIRCRAFT DIVERTED EN ROUTE TO ROA WITH SMOKE IN CABIN AND COCKPIT. THE FC DID DROP THE O2 MASK. THE COCKPIT CREW DID S MELL SMOKE, FLIGHT ATTENDANT CHECKED THE LAV AND CARGO BIN. REMOVED AND REPLACED FWD ACM. 2 H 7 2 4T 4 T RT A13NM E20NE 2007061300326 20070613 00326 NE 2007 6 13 2007UALA01779 2 20070603 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 STALLED A UALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 29 482UA 1584 STALL DISPLAYED ON UPPER ECAM SCREEN DURING CLIMB OR CRUISE ACCELERATION. ENGINE NOT SHUTDOWN, ENG 2. A REVIEW OF THE DFDR DATA FOR THIS EVENT SHOWS THAT THE STALL HAPPENED AT MID-POWER DURING DECEL "TOP OF ASCENT" TYPE STALL. THIS IS CLE ARLY DIFFERENT THAN THE REPORTED "STEADY STATE CLIMB STALL" AND REQUIRES QUITE DIFFERENT TROUBLE SHOOTING. EP HAS CREATE D AN EG CALL-OUT TO REPLACE THE HPC BLEED VALVES AND SOLENOID. EVENT RECURRED ON 06/29/07. REPLACED FMU AND FUEL PUMP AS LAST DITCH EFFORT TO AVOID CHANGING THE ENGINE OUT--NO ISSUES SINCE THAT ACTION. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062800177 20070628 00177 NM 2007 6 28 2007UALA02104 1 20070618 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1360 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 AFT PIT AT STA 1360 INTERCOSTAL BETWEEN STR 27R TO 28R IS CORRODED ON BOTTOM. MAJOR REPAIR ACCOMPLISHED: AFTER FURTHER INVESTIGATION NO CORROSION FOUND ON INTERCOSTAL. CORROSION WAS FOUND ON SUPPORT FITTING, SHIMS AND -Z- CLIPS OUT OF LI MITS. FABRICATED & INSTALLED NEW SUPPORT FITTING. REPLACED 2 EA -Z- CLIPS. FABRICATED & INSTALLED NEW SHIM. 2 L 7 2 4F 4 F RT A2NM E17NE 2007070300012 20070703 00012 EA 2007 7 3 A6WA200740248 1 20070514 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 458AW 7861 FS 280, FLOORBEAM CLIP AT IB SIDE OF RBL 9.0 IS CRACKED IN RADIUS APPROX .30 INCH LONG. S/D MAINTENANCE REPLACED CLIP IAW BSC EO 601R-57-0057A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071700047 20070717 00047 EA 2007 7 17 A6WA200740331 1 20070617 A 5230 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CARGO DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 460AW 7867 CARGO DOOR FWD TRACK LOWER CHANNEL CRACKED. MAINTENANCE REMOVED AND REPLACED CHANNEL IAW CRJ 200 SRM 51-40-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007072400192 20070724 00192 NE 2007 7 24 2007UALA02626 2 20070714 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 OVERTEMP A UALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 WP 29 654UA 25392 727698 NR 2 ENGINE EXPERIENCED OVERTEMP DURING CLIMB. [07-27-07] OIL TEMPERATURE IN YELLOW BAND DURING CLIMB. RETURNED T O FIELD IAW FLT MANUAL IRREG PROCEDURE 14.40.17. ORDMM FOUND OIL LEAK AT FUEL OIL COOLER BYPASS VALVE SOLENOID MATING SU RFACE. REPLACED SOLENOID (UA IPC REF: 79-21-00A-005B-255) PER AMM 79-21-03. RAN ENGINE - NO LEAKS! PROBLEM DID NOT R ECUR. 2 L 7 2 4F 4 F RT A1NM E24NE 2007071000001 20070710 00001 EA 2007 7 10 HNAA070122 1 20070626 A 7930 TRANSMITTER DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE OIL PRESSURE FAILED A HNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 07 328EN 281 123154 NR 2 ENGINE OIL PRESSURE WENT TO ZERO ON TAKEOFF ROLL, ALL OTHER ENGINE PERIMETERS NORMAL, NO CAUTION LIGHTS. CHECKED O IL LEVEL, FOUND TO BE ABOVE ADD 1 QT. CLEANED C/P'S ON OIL PRESSURE S/W AND TRANSMITTER, NO FIX. SWAPPED OIL PRESSURE GAUGE IN FLT DECK, NO FIX. INSTALLED BACK IN ORIGINAL POSITION. REMOVED AND REPLACED PRESSURE TRANSMITTER GROUND RAN A/C OPS CHECK AND LEAK CHECK GOOD IAW 71-00-02. PART NUMBER TO FOLLOW. 2 H 7 2 4T 4 T RT A13NM E20NE 2007071800221 20070718 00221 EU 2007 7 18 U30A200700002 1 20070707 A 2120 UNKNOWN AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE CABIN ODOR A U30A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 17 269AV 2187 FLT 703, AFTER PAX BOARDING A F/A NOTICED A BURNING ODOR IN CENTER CABIN OVERHEAD AREA, NO SMOKE VISIBLE. MAINTENANCE I NSPECTED AREA AND TURNED OFF CABIN WINDOW LIGHTS AND SMELL IMMEDIATELY DISSIPATED. THE CABIN WINDOW LIGHTS WERE DEFERRED AND AIRCRAFT RELEASED IAW MEL 33-20-01. ENROUTE, IN CRUISE, AN INTERMITTENT BURNING SMELL WAS AGAIN NOTICED AGAIN NO SM OKE VISIBLE. THE ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND INSP CEILING PANELS, ROWS 17/21/23 A ND C/W CIDS 1 AND 2 BITE TEST. TURNED ALL CABIN ON FULL BRIGHT, WITH ENTERTAINMENT SYS. ON, WITH AC PACKS 1 AND 2 FULL C OLD AND THEN FULL HOT. FWD AND AFT GALLEY EQUIPMENT ON, AND RAN ENGINES AND SYSTEMS FOR 2 HRS, COULD NOT DUPLICATE ODOR. 2 L 7 2 4F 4 F RT A28NM E38NE 2007080900190 20070809 00190 NM 2007 8 9 KNNA200700035 1 20070505 A 5311 T67075 FRAME SPLICE BOEING 737 7372Q8 138448K NM PWA JT8 JT8D217 52053 NE BS 767 S14R ACTIVE A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 413JG 23148 PASSENGER CABIN/CRACKED FRAME AT BS 767 NEAR STRINGER 14R. PROVIDE INSTRUCTIONS ON REPAIR OF CRACKED FRAME AT BS 767 ST R 14R, BOEING SB 737-53A-1261 PART 3 REPAIR. 2 L 7 2 4F 4 F RT A16WE E9NE 2007080800076 20070808 00076 CE 2007 8 8 AMWA06032O 1 20070725 A 5311 1294300321 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 213 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080700160 20070807 00160 EU 2007 8 7 COEA0701703 1 20070702 A 7997 CONNECTOR FOKKER F27 F27MK600 4990706 EU RROYCE AVON AVON532R 54517 EU NR 1 ENGINE OIL LOOSE A COEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 13 703FE 10420 14375 (AIR TURNBACK) TURNING THE TAKEOFF ROLL, THE CREW NOTICED THE NR 1 ENGINE OIL PRESSURE FLUCTUATING BETWEEN YELLOW, RED A ND ZERO, ALL OTHER INDICATIONS WERE NORMAL. A NORMAL TAKEOFF WAS COMPLETED AND THE CREW ELECTED TO RETURN TO BASE. MAI NTENANCE CLEANED AND TIGHTENED A LOOSE CONNECTOR ON THE OIL PRESSURE TRANSMITTER, THE AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 H 7 2 4T 4 J A817 E307 2007081000058 20070810 00058 CE 2007 8 10 GLBA20060968 1 20070730 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 298-300 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 219GL UE219 BELLY SKIN CRACKED ON RT SIDE 8 INCHES AFT OF FWD WING SPAR AT APPROXIMATELY FS 298.00 TO 300.25. CRACK APPROXIMATELY 2. 375 INCHES IN LENGTH. MAINTENANCE INSTALLED A PRESSURIZED COVER PATCH IAW SRM 51-70. RII PROCEDURES COMPLIED IAW TASKCAR D 8.2.1. AIRCRAFT WAS PRESSURIZED AND OPERATIONAL CHECKS OK. 2 L 7 2 4T 4 T RT A24CE E26NE 2007081700314 20070817 00314 NM 2007 8 17 2007UALA02916 1 20070730 A 3350 STRIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN BUCKLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 303UA 23644 EMERGENCY EXIT LIGHT STRIP BUCKLED AT ROW 6 & 7. REPLACED EEL STRIP 2 L 7 2 4F 4 F RT A16WE E21EU 2007082300268 20070823 00268 NM 2007 8 23 2007UALA03062 1 20070806 A 2751 INDICATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE TE FLAPS MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 313UA 23674 LANDED UNDER AMBER ALERT DUE TO NO FLAP MOVEMENT. FOUND FLAP POSITION INDICATOR FAILURE. REPLACED THE FLAP POSITION INDICATOR. FLAPS CYCLED THROUGH SEVERAL TIMES. ALL SYSTEMS NOTED NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2007082300174 20070823 00174 2007 8 23 2007UALA03091 4 20070808 A 2565 5A29011 ASPIRATOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EVAC SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 669UA PK0074 30025 ASPIRATOR IS LEAKING THROUGH ORANGE SEAL. SLIDE WAS DEPLOYED IN FIELD, ASPIRATOR MAY HAVE BEEN DAMAGED. REPLACED ASPIR ATOR. 08-31-07 REPLACED ASPIRATOR. ASPIRATOR DAMAGED DURING IMPROPERLY CONTROLLED DEPLOYMENT. 2 L 7 2 4F 4 F RT A1NM E24NE 2007083000008 20070830 00008 CE 2007 8 30 DXTA200702404 1 20070814 A 3241 991228113 FILTER CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE ANTI SKID ASSY DIRTY E DXTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 812QS 3548 5600628 LOW BRAKE PRESS/ANTISKID INOP, ANNUNICATOR ILLUMINATED AT BEGINNING OF OUR TAXI. CHANGED ANTI-SKID PUMP FILTER. BLEED ANTI-SKID BRAKE SYSTEM. RECONNECTED LOW PRESSURE SWITCH. C/W OPS CHECK, LEAK CHECK, & TAXI CHECK. ALL CHECKS GOOD. WORK C/W IAW 560MM 32-42-00 2 L 7 2 4F 4 F RT A22CE E00053EN 2007090700064 20070907 00064 NM 2007 9 7 2007UALA03159 1 20070811 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEATS 1J AFT, 4A INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 SEATS 1J AFT, 4A FWD, 55HJK & 8ABC EMERGENCY LIGHTS ARE INOPERATIVE. *S/D* RELAMPED SEAT EEL LIGHTS AT EACH SEAT POSIT ION. ALL OP CHECK NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007091800196 20070918 00196 NM 2007 9 18 2007UALA03568 1 20070902 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 SEATS 3J AFT & 4F AFT EEL ARE INOPERATIVE. RELAMPED, OPS CHECK OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092800049 20070928 00049 NM 2007 9 28 2007UALA03748 1 20070917 A 5320 STRUCTURE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE OXYGEN MASK BOX UNSERVICEABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 842UA 1569 OXYGEN BOX ASSY IS UNSERVICEABLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007090700115 20070907 00115 NM 2007 9 7 2007UALA03421 1 20070826 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 UPPER DECK EMERGENCY EXIT CEILING LIGHT AT ROW 13 & CEILING LIGHT AT ROW 2 ARE INOPERATIVE. RELAMPED CEILING LIGHTS IN BOTH POSITIONS. OP CHECKS. NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007092800042 20070928 00042 NM 2007 9 28 2007UALA03737 1 20070914 A 3150 WARNING LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ILLUMINATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 119UA 28812 THE 'RUD RATIO SNGL' EICAS ADVISORY MESSAGE DISPLAYED. UPPER OR LOWER RUDDER RATIO FUNCTION FAIL. 10-9-07 REPLACED WITH NEW RUDDER RATIO CHANGER ACTUATOR PER MM27-21-12. PERFORMED CMC TEST. RUDDER RATIO CHANGER PASSED AND MSG GONE. A /C RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007101100219 20071011 00219 EU 2007 10 11 HAEA200700202 1 20070925 A 2612 MY2063217 CONTROL BOX AMD FALCON FALCON20 2730103 EU GE CF700 CF7002D2 30010 NE FIRE WARNING SHORTED E HAEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 05 699TW 33015 33015 50 AFTER DEPARTURE, CLIMBING THROUGH 3000 FT, REAR COMPARTMENT FIRE WARNING ILLUMINATED. THE FO PEERED THROUGH THE INSPECTI ON GLASS NOTICING NO VISUAL INDICATION OF FIRE. AS A PRECAUTION, THE CAPT DISCHARGED THE FIRE BOTTLES AND DECLARED AN EM ERGENCY, RETURNING TO DEPARTURE WITHOUT INCIDENT. AIRCRAFT WAS SHUTDOWN AND CREW EXITED THE AIRCRAFT. FIRE DEPARTMENT OP ENED REAR COMPARTMENT AND FOUND NO EVIDENCE OF FIRE. MAINTENANCE FOUND FIRE WARNING LIGHT TO BE ON INDICATING A SHORT IN THE SYSTEM. MAINTENANCE FOUND THE FIRE WARNING CONTROL BOX SHORTED INTERNALLY. REPLACED FIRE WARNING CONTROL BOX. S YSTEM OPERATION NORMAL. 2 L 7 2 4F 4 F RT A7EU E7EA 2007101700002 20071017 00002 NM 2007 10 17 2007UALA04100 1 20071007 A 2597 TERMINAL BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE AFT GALLEY DAMAGED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 924UA 26645 FLT ATTENDANTS REPORTED A BURNING ODOR IN THE AFT GALLEY NEAR THE COFFEEMAKERS. SUSPECT COFFEE MAKER HAS LOOSE TERMINAL S. RIGHT AFT COFFEE MAKER HAD 2 LOOSE TERMINAL WIRES AND TERMINALS WERE ELECTRICALLY BURNT BECAUSE NUTS WERE NOT SECUR ED ON STUDS HOLDING THE WIRES AND TERMINAL ENDS, REPLACED COFFEE MAKER. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007100500106 20071005 00106 NM 2007 10 5 2007UALA03961 1 20071001 A 3150 WARNING LIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 907UA 25007 RTFL DUE TO LEFT FUEL FILTER BYPASS LIGHT ILLUMINATION. REPLACED FUEL FILTER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007102300277 20071023 00277 NM 2007 10 23 2007UALA04145 1 20070920 A 2120 UNKNOWN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FWD CARGO BAY ODOR A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 902UA 25002 RAMP REPORTED TO CREW, GOT AN ELECTRICAL-LIKE SMELL IN FORWARD PIT. 2 L 7 2 4F 4 F RT A16WE E21EU 2007101500138 20071015 00138 EA 2007 10 15 VNAA0709015 1 20070930 A 2621 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CARGO BAY LOW A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 05 202PS 7858 CREW REPORTED A CARGO BOTTLE LOW CAS MESSAGE IN FLIGHT. CREW ELECTED TO DIVERT AND LAND IN LYH WITHOUT INCIDENT. MAINT ENANCE MEL'D THE CARGO FIRE BOTTLE PER MEL 26-25-01 -C-. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007101600066 20071016 00066 NM 2007 10 16 ANCF200700022 1 20071006 A 2780 TORQUE TUBE BOEING 767 767283ER 1385149 NM PWA 4056 PW4056 NE SLATS UNKNOWN W ANCF A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 23 728CG 24728 PILOT REPORT EICAS MSG LE SLAT DISAGREE DISPLAYED LEADING EDGE LIGHT ILLUM WITH THE FLAP LEVER IN 1. BOTH FLAP POINTERS WERE ON .5. IAW AMM 27-81-24 PG 401 TO 420 IN RT WING OB SLAT , ONE TORQUE TUBE WAS REPLACED P/N ON AND OFF 256T2800- 105 2 L 7 2 4F 4 F RT A1NM E24NE 2007101700139 20071017 00139 NM 2007 10 17 DL76S071305 1 20071005 A 2150 6806404 ACM BOEING 767 767332 1382001 NM GE CF6 CF680C2B6 30025 NE LEFT FROZEN A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 133DN 24982 695376 LEFT A/C PACK TRIPPED ON TAKEOFF ROLL. RETURNED FOR LANDING DUE TO SMOKE AND FUMES IN THE CABIN AFTER TAKEOFF. FOUND L EFT AIR CYCLE MACHINE SEIZED. REPLACED LT ACM PER M/M 21-51-03-004. LEFT PACK CKS OK, RAN BOTH ENGS. NO SMOKE OR ODOR NOTED. 2 L 7 2 4F 4 F RT A1NM E13NE 2007102300285 20071023 00285 NM 2007 10 23 2007UALA03863 1 20070922 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 672UA 30027 SEAT 2B EEL STRIP DAMAGED. REPLACED DAMAGED EEL LIGHT STRIP. OP CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007110900076 20071109 00076 NM 2007 11 9 2007UALA04519 1 20071101 A 3510 MC1019151 OXYGEN MASK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 171UA 24322 FIRST OFFICERS O2 MASK, WHILE IN EMERGENCY MODE O2 FLOW "CHOO CHOO'S". SUSPECT FAULTY FLOW VALVE. REPLACED MASK PER MM 35-11 -18 OPS CHECKS NORMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110800002 20071108 00002 CE 2007 11 8 DXTA200702565 1 20071023 A 3240 215297 BRAKE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 316QS 1153 1153 5600516 RT BRAKE ON CAPTAIN'S SIDE DEPRESSES FURTHER THAN LT SIDE AND IS SOFT. CO-PILOTS SIDE HAS SIMILAR PROBLEM. REMOVED AND REPLACED RT MAIN BRAKE IAW CE-560 MAINTENANCE MANUAL 32-42-01. 2 L 7 2 4F 4 F RT A22CE E25EA 2007110800027 20071108 00027 NM 2007 11 8 2007UALA04422 1 20071026 A 3520 OXYGEN BOTTLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU PAX UNKNOWN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 310UA 23671 PASSENGER O2 FLUCTUATING FROM 1450 TO 1740 PSI. PERFORMED LEAK CHECKS OF ALL SYSTEMS-GOOD, SERVICED O2 SYS TO PROPER L EVELS AND OBSERVED NO FLUCTUATIONS. GROUND TEMP 54F. 2 L 7 2 4F 4 F RT A16WE E21EU 2007110900021 20071109 00021 NM 2007 11 9 2007UALA04467 1 20071030 A 3350 1317 LAMP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 204UA 28713 EMERGENCY LIGHT ON GALLEY WALL ACROSS FROM DR 4R, AFT LIGHT IS OUT, RELAMPED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007112000028 20071120 00028 EU 2007 11 20 2007UALA04598 1 20071106 A 3397 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE BATTERY PACK UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 426UA 510 EMERGENCY LIGHT TEST FAILED *33-51-38 INT LOADS EMER R*. FOUND LOOSE CONNECTOR. RESECURED CONNECTOR ON BATTERY PACK AT RT OVERWING EXIT -OPS TEST OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007112800087 20071128 00087 NM 2007 11 28 2007UALA04727 1 20071117 A 5312 PRESSURE PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 665 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 LEFT MAIN WHEEL WELL CEILING CRACKED AT BS 665 LBL 32. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED MID CABIN PRE SS DECK REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112900159 20071129 00159 NE 2007 11 29 DL76L071481 2 20071112 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 MAKING METAL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1201P 65140 12167 28458 723834 DURING OPN 4051, FOUND METAL ON THE MASTER CHIP DETECTOR. METAL FOUND TO BE BEARING MATERIAL. REMOVED AND REPLACED LEF T ENG 2 L 7 2 4F 4 F RT A1NM E24NE 2007111500207 20071115 00207 NM 2007 11 15 2007UALA04602 1 20071106 A 3350 8100133801 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 1F INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 781UA 26945 AFT EEL LIGHT AT SEAT 1F INOP. REPLACED LIGHT ASSY AT SEAT 1F AFT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007112000048 20071120 00048 NM 2007 11 20 2007UALA04647 1 20071111 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INTERMITTENT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 THE E-ZONE RT FWD EEL STRIP INTERMITTENT. REPLACED BATTERY PACK. OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112800035 20071128 00035 NE 2007 11 28 SWAA075748 2 20071117 A 7200 ENGINE BOEING 737 7373A4 1384585 NM GE CFM56 CFM563B1 13802 NE RIGHT FAILED A SWAA E A ENGINE SHUTDOWN UNSCHED LANDING E Y J VIBRATION/BUFFET ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SW 29 676SW 46331 13828 23288 857652 AIR TURNBACK / DECLARED EMERGENCY. IN FLIGHT SHUTDOWN EN ROUTE AT ABOUT 25,000 FT, AIRCRAFT BEGAN VIBRATING THEN HEARD EXPLOSION. SECURED NR 2 ENGINE. NR 2 ENGINE REPLACEMENT IN PROGRESS PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2007112800064 20071128 00064 NM 2007 11 28 2007UALA04700 1 20071115 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 727D-727E CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 RIGHT CABIN CREASE BEAM WEB ADJACENT TO STRINGER 17L IS CORRODED ON UPPER SURFACE BETWEEN BS 727D & S 727E WL 208. B LENDED OUT CORROSION. FABRICATED AND INSTALLED A TYPICAL WEB REPAIR ON UPPER SURFACE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112900060 20071129 00060 NM 2007 11 29 2007UALA04783 1 20071120 A 5315 STIFFENER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 246 FLOORBEAM CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 662UA 27159 FLOORBEAM AT FS 246 FORWARD SIDE VERTICAL STIFFENER CRACKED AT LBL 26.39. REMOVED & REPLACED STIFFENER. 2 L 7 2 4F 4 F RT A1NM E24NE 2007121300088 20071213 00088 NM 2007 12 13 2007UALA04868 1 20071129 A 5210 BATTERY PACK BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 4 MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 774UA 26936 NR 4 RT PED EPAS BATTERY HAS BEEN FOUND INSTALLED UPSIDE DOWN, NEW TYPE BATTERY PACK. REINSTALLED CORRECTLY. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007121400251 20071214 00251 NM 2007 12 14 2007UALA04957 1 20071204 A 5712 RIB BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 NR 2 MAIN FUEL TANK LT RIB LOWER CHORD CRACKED WBL 135.5 BETWEEN WING STRINGERS S2 AND S3. CRACK IS APPROXIMATELY 2.5 I NCH LONG & ORIGINATES IN THE CUTOUT RADIUS OF THE LOWER RIB CHORD. MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT DAMAGE, FABR ICATED & INSTALLED REPAIR TEE, VERTICAL STIFFENER & FILLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2007121300393 20071213 00393 NM 2007 12 13 2007UALA04912 1 20071130 A 3350 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 381UA 24656 DOOR TWO RIGHT EXTERIOR EMERGENCY LIGHT INOP. FOUND LAMP NOT SECURED CORRECTLY IN SOCKET. SECURED LAMP IN SOCKET, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A16WE E21EU 2008010400166 20080104 00166 2008 1 4 AMTA200700635 4 20071125 A 2310 9640452022 TRANSCEIVER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE NR 2 HF SYS UNSERVICEABLE A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 522AT 29330 LT HF DOES NOT RECEIVE AT ANY CREW MEMBER STATION. INSTALLED HF TRANSCEIVER LT SIDE. OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008010700088 20080107 00088 NM 2008 1 7 2007UALA05205 1 20071220 A 4940 STARTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU FAILED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 595UA 28748 APU AUTO SHUTDOWN WILL NOT RESTART. REPLACED APU STARTER. ALL OPS CHECKED OK. ECU SHOWED NO FAULT FOR AUTO-SHUTDOWN. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010700302 20080107 00302 NM 2008 1 7 2007UALA05284 1 20071226 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY EXIT LIGHT INOPERATIVE AT DOOR 2L AFT SILL LIGHT. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011000055 20080110 00055 EU 2008 1 10 TRBA2007116 1 20071222 A 7931 1156100 PRESSURE SWITCH AEROSP ATR72 ATR72212A 8680902 EU PWA PW120 PW127 NE ENGINE FAILED A TRBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 29 545AT 545 LOW OIL PRESSURE WARNING ON NR 2 ENG. REMOVED AND REPLACED NR 2 ENG OIL PRESS SWTICH TRANSMITTER IAW JIC 79-33-61. 2 H 7 2 4T 4 T RT A53EU E20NE 2008011500069 20080115 00069 NE 2008 1 15 NSVA20070163 2 20070618 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT OVERTEMP A NSVA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 EA 27 184CJ 184 785457 RIGHT ENGINE EXCEEDED ITT LIMITATION ON TAKEOFF OF 930 DEGREES LIMITATION IS 927 DEGREES FOR TAKEOFF. REMOVED AND REPLA CED RT ENG IAW CWC 71-00-01S, OPS CHK AND LEAK CHK GOOD P/N CT7- 9B, SN ON 785253 SN OFF 785457. 2 L 7 2 4T 4 T RT A52EU E8NE 2008012300014 20080123 00014 NM 2008 1 23 2007UALA05343 1 20071230 A 3350 D9239003500060 EPSU AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 816UA 871 EMERGENCY LIGHT SYSTEM FAIL TO TEST. EPSU FAILURE. REPLACED EPSU 13WL. OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007010800082 20070108 00082 NM 2007 1 8 07FDEA00001 1 20070101 A 5754 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RT WING FIXED LEADING EDGE OUTBOARD OF NR 8 SLAT FOUND WITH CHAFE MARKS. REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5720-10 5587, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007050400296 20070504 00296 EU 2007 5 4 07FDEA01655 1 20070427 A 5330 SKIN AIRBUS 310 A310203 3930313 EU FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 411FE 359 PREVIOUS REPAIR LOCATED ON L-SIDE FUSELAGE SKIN BETWEEN FR 21-22 BETWEEN STR 34-36 LT AT LAP SEAM HAS AN EXTERNAL DOUBLE R MEASURING 6.25 BY 9 IN REPAIR DETERMINED NOT TO BE IAW A310-200 SRM 53-10-12 FIG 205, REPAIR REWORKED IAW A310-200 SRM EA 6-5330-110187. 2 L 7 2 4F RT A35EU 2007092000139 20070920 00139 EU 2007 9 20 07FDEA03559 1 20070911 A 5313 A53974202 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 432FE 326 CORROSION FOUND ON STRINGER P53, 54, 55 AT C59 OUT OF LIMIT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 2007081700325 20070817 00325 2007 8 17 HALA0700336 4 20070811 A 3442 RADAR BOEING 767 7673CB 1385187 NM WX SYSTEM FAILED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 590HA 33467 ETOPS SIGNIFICANT SYSTEM, WXR FAIL DISPLAYED ON HSI WITH LEFT SYSTEM SELECTED. WXR TEST DISPLAYS WXR FAIL RT ON HSI. S TATUS PAGE INDICATES WXR SYS. VERIFED IRU'S CHK GOOD. T/S WX RADAR IAW FIM 34-43-00 BITE CHKS GOOD. WXR TRANS CHKS GO OD. RT AND LT CHKS GOOD. 2 L 7 2 4F RT A1NM 2007121400150 20071214 00150 EU 2007 12 14 F3LA200700362 1 20071204 A 5320 SILL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 901FR 5849 1488 DURING C-5 CHECK, INSPECTION REPORTED LIGHT SURFACE CORROSION ON FWD CARGO DOOR SILL WEB. REMOVED NUTPLATE AND REWORKED FOUR SMALL AREAS OF CORROSION IAW SRM 51-42-11 AND 51-74-00. EA NR A9-53R-12316 REQUIRED ACCOMPLISHMENT OF HFEC INSPEC TION OF BLENDED AREAS AND ROTOPROBE OF NUTPLATE HOLE TO VERIFY NO DAMAGE PRESENT. PERFORMED HFEC AND ROTOPROBE INSPECTI ONS IAW NTM 51-10-08 PART 6, AND 51-10-01 PART 6, PAGES 601-612. NO DEFECTS NOTED. 2 L 7 2 4F RT A28NM 2007050300382 20070503 00382 NM 2007 5 3 2007UALA01315 1 20070426 A 2560 ATTACH FITTING BOEING 737 737322 1384676 NM AFT ENTRY LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 AFT ENTRY DOOR AFT EMERGENCY SLIDE GIRT BAR FLOOR ATTACH FITTING IS LOOSE. [SUP 05-16-07] TIGHTENED GIRT BAR FLOOR FIT TING. 2 L 7 2 4F RT A16WE 2008010400007 20080104 00007 EA 2008 1 4 TRAX200701933 1 20071214 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 916EV 7757 LT OVERWING LIGHTED FLOOR LEVEL EXIT SIGN INOP. 2 L 7 2 4F RT A21EA 2007032000084 20070320 00084 NM 2007 3 20 UIEA200700131 1 20070303 A 2120 UNKNOWN BOEING 747 74747UF 1384949 NM COCKPIT SMOKE A UIEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 15 499MC 29260 CREW REPORTED SLIGHT SMOKE IN THE COCKPIT DURING PRE-FLIGHT OPS. MAINTENANCE SHUT DOWN AIRCRAFT POWER. AFTER POWER SHU T DOWN, INSPECTED COCKPIT FOR SMOKE OR DAMAGE. NONE NOTED. INSPECTED E/E BAY AND MAIN DECK NO SMOKE NOTED. TURNED POW ER BACK ON FOR AN HOUR. NO SMOKE OR SMELL NOTED. CREW PRE-FLIGHT COMPLETED WITH NO ISSUES. VERIFIED THAT NO C/B'S ARE OUT AND NO STATUS MESSAGES. 2 L 7 4 4F RT 1384945 2007101200092 20071012 00092 NM 2007 10 12 CALA0700551 1 20071002 A 5320 6916970501 SUPPORT BOEING 737 7373T0 1384582 NM BS 360 S15L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A 5 INCH CRACK IN L-1 DOOR CUTOUT AFT SIDE FORWARD SUPPORT CLIP AT STA 360, S15L. THE CLIP WAS REMOVED AND REPLACED IAW ECRA 5311-01363. 2 L 7 2 4F RT A16WE 2007030700237 20070307 00237 NM 2007 3 7 07FDEA00646 1 20070305 A 5340 654531314 STRINGER CLIP BOEING 727 727225 1384077 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 463FE 22551 FOUND MAIN DECK BODY FRAME STRINGER CLIP IS CRACKED AT BS 970, STR 9R. REMOVED CRACKED STRINGER CLIP, DRILLED UP NEW CL IP AND INSTALLED REF SRM 51-30-2. 2 L 7 3 4F A3WE 2007072400082 20070724 00082 WP 2007 7 24 AALA20071265 1 20070707 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 417AA 49328 LGA - EMERGENCY LIGHTS AT SEAT ROWS 20 TO 32 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 20 TO 32. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007041000157 20070410 00157 2007 4 10 ARWA20070308 4 20070327 A 3442 20707090101 ANTENNA DOUG DC10 DC1030 3023501 WP WX RADAR INOPERATIVE A ARWA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 19 524MD 46999 RADAR NR 2 DOES NOT PAINT AND WEATHER IN FLIGHT TEST PATTERN OK ON THE GROUND. REMOVED AND REPLACED WEATHER RADAR ANTEN NA IN ACCORDANCE WITH M/M 34-41-01. OPERATIONAL CHECK GOOD IN ACCORDANCE WITH M/M 34-41-00. 2 L 7 3 4F A22WE 2007071200042 20070712 00042 NM 2007 7 12 AALA20071158 1 20070625 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 780AN 29956 JFK - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 20C MISSING LENS. REPLACED LENS FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 20C . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007111300121 20071113 00121 WP 2007 11 13 NWAA073689853 1 20071029 A 5330 SKIN DOUG DC9 DC951 3022051 WP BS 1100 S23-25R CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 762NC 47710 DURING "H" CHECK, FOUND CRACK IN EXISTING REPAIR DOUBLER AT THE AFT EDGE OF AFT CARGO DOOR CUTOUT BS 1100 L23R-L25R. RE PAIRED PER EA 98-211036. 2 L 7 2 4F RT A6WE 2007041200039 20070412 00039 NM 2007 4 12 QXEA200700545 1 20070309 A 5700 UNKNOWN DHAV DHC8 DHC8202 2809007 NM LT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 C4 PDX - AT LEFT UNDER WING STATION YW222.4 THERE IS AN AREA OF SMALL NICKS. REPAIRED IAW RD8-57-2996 AND SRM 51-20-11. 2 H 7 2 4T RT A13NM 2007033000170 20070330 00170 EU 2007 3 30 07FDEA00931 1 20070316 A 5230 SKIN AIRBUS 310 A310304 3930339 EU ZONE 800 CHAFED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 TWO OLD NICK/CHAFING MARKS AT THE INTERNAL SKIN OF FWD CARGO DOOR C20A-25A, LONGERON 4-5. REPAIR WAS PERFORMED BY INSTA LLING A DOUBLER IAW LHT SDR. 2 L 7 2 4F RT A35EU 2007083100220 20070831 00220 NM 2007 8 31 UIEA200700311 1 20070801 A 2121 FAN BOEING 747 74747UF 1384812 NM COCKPIT FAILED A UIEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 15 498MC 29259 PRIOR TO DISPATCH BURNING SMELL IN FLIGHT DECK AND COOLING FAN AREA. ITEM TRANSFERRED TO DMI M07-066 PER 21-58-4 (E/E COOLING EXHAUST FAN FAIL MESSAGE NR 21410 DISPLAYED). 2 L 7 4 4F RT A20WE 2007060500126 20070605 00126 EU 2007 6 5 07FDEA02030 1 20070531 A 5730 A573140086 SKIN AIRBUS 300 A300B4605R 3930308 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 731FD 709 CORROSION WITH CRACK FINDINGS (A= 22MM, B= 25MM) ON HOLE 699 (DRW R571-40141 SHEET 12), LT WING BOTTOM SKIN LOWER SURFAC E. REPAIR PERFORMED BY REAM UP TO NEXT OVERSIZE IAW EA 6-5720-106453 AND RAS/BAE/1004815/2007 ISS. A 2 L 7 2 4F RT A35EU 2007022100385 20070221 00385 NM 2007 2 21 UIEA200700024 1 20070127 A 5610 65B270422 WINDOW BOEING 747 74747UF 1384949 NM COCKPIT CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 409MC 28499 30558 DURING C CHECK INSPECTION, FOUND NR 2R FLIGHT DECK WINDOW EXHIBITING SIGNS OF FAIL/SAFE INTERLAYER CRACKING IN RADIUS AR EAS. POSITIVE CONFORMATION IS NOT POSSIBLE DUE TO GENERAL IN-SERVICE WEAR AND LOCALIZED BORDER DELAMINATION. WINDOW CH ANGED PRECAUTIONARY. 2 L 7 4 4F RT 1384945 2007120700210 20071207 00210 NM 2007 12 7 F3LA200700338 1 20071117 A 2560 MOUNT AIRBUS A319 A319111 3930336 NM GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 908FR 5698 1759 DURING C4/S1 CHECK, INSPECTION REPORTED TWO CORRODED FASTENERS IN THE R2 AFT GIRT BAR MOUNT PLATE. BLENDED OUT CORROSI ON ON OTBD MIDDLE FASTENER HOLE, BOTTOM SIDE OF SILL PLATE IAW SRM 51-22-00 - WITHIN LIMITS IAW SRM 53-41-14-PG103/104. INSTALLED AFT GIRT BAR MOUNT PLATE IAW SRM 51-42-11. 2 L 7 2 4F RT A28NM 2007041300117 20070413 00117 NM 2007 4 13 2007UALA00983 1 20070401 A 3350 362624 LIGHT BOEING 777 777222 1385219 NM CABIN MISSING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 782UA 26948 SEAT 3F ARMREST EMERGENCY LIGHT MISSING. REPLACED EEL LIGHT ASSY & OPS CHECKED OK. 2 L 7 2 4F RT T0001SE 2007050800106 20070508 00106 WP 2007 5 8 DHL2007806509 1 20070328 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP BS 1675-1705 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 89284 46002 UPPER CARGO COMPT NR 4 TRACK LUG WORN (STA 1675.000 - 1705.000). CUT OUT TRACK DAMAGED SEGMENT AND FABRICATED SPLICES I AW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATED AND PRIMED AREA AND SPLICES IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGME NT AND SPLICES IAW SRM 53-2-3 PG 49-50 FIG 14, SRM 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2007012200064 20070122 00064 NM 2007 1 22 WRLA2007011 1 20070111 A 5730 SKIN DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE LT WING CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 41081 48632 DURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND LEFT WING UPPER SURFACE BULGE CORRODED UNDER FIXED PANEL NEAR XORS=1042 RE AR SPAR. REPAIR THE DAMAGE AREA PER EGAT E1 NT W2007A57B-060 REV.00 AND APPROVE DOCUMENT BOEING MESSAGE NR 1-276023171- 2. CONDITION CHECK NORMAL. (EGAT NRC NR U05011). 2 L 7 3 4F 4 F RT A22WE E24NE 2007013100119 20070131 00119 2007 1 31 DJFA2007012 4 20070124 A 2215 6226718101 SERVO BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE RUDDER BINDING E DJFA K NONE F FLT CONT AFFECTED LD LANDING 1 EA 23 798TA 7047 RK198 TRIP NR 1132520 AFTER LANDING CREW REPORTED THAT WITH THE YAW DAMPER ENGAGED RUDDER PEDDALS WERE VERY STIFF. MAINTENANC E DISCOVERED THE RUDDER SERVO CLUTCH STICKING. THE MOUNT WAS REPLACED AND THE CABLE TENSIONS ADJUSTED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007012600165 20070126 00165 NM 2007 1 26 2007UALA00182 1 20070123 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 674UA 29242 EMERGENCY ESCAPE LIGHTS FLICKER BETWEEN ROWS 10 AND 17 LEFT AISLE. CHECKED WITH CREW. THEY REPORTED LIGHTS FLICKERED ON LY ONCE. TURNED LIGHTS ON AND THEN ALSO CHECKED LIGHTS IN ARMED POSITION AND COULD NOT DUPLICATE ITEM. SUSPECT FAULTY CONNECTION. 2 L 7 2 4F 4 F RT A1NM E24NE 2007020700123 20070207 00123 2007 2 7 2007UALA00224 4 20070127 A 2565 O-RING BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE R4 DOOR SLIDE LEAKING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 217UA 30550 DOOR 4 RIGHT SLIDE BOTTLE PRESSURE OUT OF GREEN BAND. REPLACED SLIDE ASSY. A/C RETURNED TO SERVICE. SUSPECT O-RING L EAK AT BOTTLE CONNECTION. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007012500258 20070125 00258 NM 2007 1 25 2007UALA00099 1 20070113 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 669UA 30025 DOOR 1L EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED. OP CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2007020500016 20070205 00016 CE 2007 2 5 AMWA82342BC 1 20070130 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MASTER DISCHARGED A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 159YV 5002 104 UE159 BATTERY CHARGE LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED BATTERY TO CLEAR DISCREPANCY. THIS BATTERY CHARGE LIG HT ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS. 2 L 7 2 4T 3 T RT A24CE E2NE 2007021200203 20070212 00203 SO 2007 2 12 ECI10514 1 20070129 A 2750 54253021 ASYMMETRY SWITCH MOOG GULSTM G1159 GIV 3980115 SO GE CF34 CF348E5 30015 NE FLAPS MISALIGNED E E0XA K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 35 919CT 1051 FLAPS WOULD NOT RETRACT DURING TAXI. FLAP ASYMMETRY FOUND TO BE OUT OF ADJUSTMENT. REMOVED AND REPLACED RT FLAP ASYMME TRY SWITCH WITH NEWLY OVERHAULED SWITCH. REALIGNED ASYMMETRY SWITCHES. 2 L 7 2 4F 4 F RT A12EA E00063EN 2007021300082 20070213 00082 NM 2007 2 13 DXTA200701918 1 20070208 A 2120 UNKNOWN AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE CABIN ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 259QS 159 APPROX. 5 MIN AFTER DEPARTURE A STRONG ODOR, SIMILAR TO A HAIR DRYER BURNING, NOTICED IN COCKPIT. FLT ATTENDANT REPORTED SAME ODOR IN PAX CABIN AFTER NOTICED IN COCKPIT. ODOR LASTED APPROX 3 MIN. NOTICED AGAIN 4 MIN LATER, NO ODOR DETECTED AFTER LANDING. RAN ACFT, VERIFIED PUNGENT ODOR IN CABIN & COCKPIT. REMOVED ACM CONDENSOR P/N S/N E184 AND FOUND IT TO B E CLOGGED WITH DEBRIS AND SOOT. CLEANED AND VACUUMED CONDENSOR OF PARTICULATES. REINSTALLED CONDENSOR, RAN ACFT ENGINES & APU AT DIFFERENT POWER SETTINGS FOR 45 MIN. ALL CONDITIONED AIR & WARM AIR FLOW GOOD. WITH ODORS ELIMINATED. LEAK TOPS CHECK GOOD. WORK IAW F2000 AMM 20-00-00 AND 21-30-00. PHX-PHX. 2 K 7 2 4F 4 F RT A50NM E44NE 2007013100169 20070131 00169 NM 2007 1 31 2007UALA00144 1 20070120 A 3210 LANDING GEAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE INOPERATIVE A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 507UA 24743 RTFL DUE TO INABILITY TO RETRACT LANDING GEAR. ON TAKEOFF GEAR HANDLE WOULD NOT COME UP PAST OFF & GEAR WOULD NOT RETRA CT. REPLACED LEFT AND RIGHT GEAR TRUCK TILTED SENSORS. ALSO REPLACED PSEU. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022600025 20070226 00025 NE 2007 2 26 SWAA071053 2 20070221 A 7261 CFM567B24622 ENGINE BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B2US 13802 NE RIGHT LEAKING A SWAA O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 29 436WN 32456 874560 DEPARTING FROM DAL, F/A REPORTED OILY ODOR IN CABIN WHICH PERSISTED FOR 10 TO 15 MINUTES. ON SHUT DOWN AT MCI OBSERVED EXCESSIVE SMOKE FROM TAILPIPE WHICH PERSISTED FOR SEVERAL MINUTES AFTER SHUTDOWN AT GATE. REMOVED AND REPLACED NR 2 ENG INE PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2007022600033 20070226 00033 CE 2007 2 26 DXTA200701955 1 20070218 A 7500 ELBOW CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE BLEED AIR SYS LEAKING E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 328QS 5600428 AFTER TAKEOFF AND CLIMBING THRU 6000 FT RT ENGINE FIRE LIGHT CAME ON. REDUCED POWER ON RT ENGINE AND LIGHT WENT OUT. R AN THE POWER UP SLIGHTLY AND NOTICED OIL TEMP ON RT ENGINE INCREASING. FOUND ELBOW ON RT INBOARD BLEED AIR CONNECTION L EAKING. REMOVED DEFFECTIVE ELBOW AND REPLACED WITH NEW ELBOW. OPS CHECK & LEAK CHECKED GOOD. ALL WORK DONE IAW CE-560 UL TRA AMM CHAPTER 36-12-01 2 L 7 2 4F 4 F RT A22CE E25EA 2007022600062 20070226 00062 NM 2007 2 26 740006 1 20070214 A 7500 65B9453213 FLEX DUCT BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE NR 4 ENGINE BLOWN A Q2SA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 03 740SA 21380 528408 NR 4 ENGINE HAS 2 KNOB THROTTLE SPLIT. HIGH EGT, HIGH FUEL FLOW, HIGH OIL TEMPERATURE, HIGH FIRE DETECTION TEMPERATURE AND HIGH STAGE VALVE OPEN. RETURNED TO RKSI. TROUBLESHOOT IAW AMM 71-00-42. PERFORMED BLEED SYSTEM LEAK CHECK IAW AMM 71-00-00. FOUND HIGH STAGE VALVE BLEED SENSE LINE FITTING BROKEN AT 12 O'CLOCK POSITION. R & R HIGH STAGE SENSE LINE IAW AMM 36-11-05. FOUND FLEX DUCT ASSY BETWEEN PRESSURE RELIEF VALVE AND PRE-COOLER, WITH LARGE HOLE. R & R FLEX DUCT ASSY IAW AMM 36-11-03. FOUND LT AND RT LPT CASE COOLING MANIFOLDS SECURE POINTS. R & R LT AND RT LPT COOLING MANIFOLDS IAW AMM 75-24-01. R & R HIGH STAGE BLEED VALVE IAW AMM 36-11-05. R & R WEAK PRESSURE RELIEF VALVE IAW AMM 36-11-03. 2 L 7 4 4F 4 F A20WE E23EA 2007022100192 20070221 00192 NM 2007 2 21 2007UALA00279 1 20070202 A 3397 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 525UA 24978 DOOR 4R AND 4L DOOR SIDEWALL EEL LIGHTS INOP. FOUND SHORT IN WIRING BETWEEN PINS A&B. FOUND FLOOR EEL LIGHT ON GALLEY WALL SATURATED WITH WINE CAUSING CONTAMINATION OF POWER FEEDER CABLE RESULTING SYSTEM TO BE INOPERATIVE. CLEANED CONTAM INATION. DID NOT REPLACE ANY MAJOR PART/COMPONENT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022300094 20070223 00094 NM 2007 2 23 2007UALA00405 1 20070210 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY LIGHT AT ROW 17 CEILING INOPERATIVE. RELAMPED. OP CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007022300266 20070223 00266 NM 2007 2 23 2007UALA00461 1 20070214 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 518UA 24871 STOW BIN EMERGENCY EXIT LIGHT INOP AT RIGHT ROW 7. REPLACED LAMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007022700028 20070227 00028 EA 2007 2 27 VNAA0702005 1 20070206 A 3210 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE MLG UNKNOWN A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 706PS 10150 CREW REPORTED A GEAR DISAGREE MESSAGE ON CLIMBOUT. CREW ELECTED TO RETURN TO CLT AND LAND WITHOUT INCIDENT. MAINTENANC E PERFORMED OPERATIONAL TESTS IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007032100124 20070321 00124 NM 2007 3 21 WRLA2007047 1 20070314 A 5312 FRAME DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE BULKHEAD CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271WA 48518 DURING C-04 CHECK, CORROSION FOUND AT BULKHEAD TEE CHORD STA Y=2007, Z=20, X=-20. REPAIR PER MD-11 SRM 51-33-01 & 51-35- 01 REV.38 2 L 7 3 4F 4 F RT A22WE E24NE 2007032200030 20070322 00030 CE 2007 3 22 AWM070223021B 1 20070306 A 5311 1294300311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 243 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 146ZV 26382 UE146 LT FUSELAGE FRAME DAMAGED BY CHAFING. REPAIRED IAW ENGINEERING REPORT 6593-1, REV IR DATED 5 MAR 07.. 2 L 7 2 4T 4 T RT A24CE E26NE 2007031200256 20070312 00256 EU 2007 3 12 I2W2007F00000 1 20070228 A 3246 FLOAT SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE DEPLOYED E I2WA O OTHER O OTHER NR NOT REPORTED 1 WP 13 197BH 2666 9246 WHILE DOING A PHOTO CHARTER, THE PILOT PRESSED THE ARM PUSHBUTTON TO ARM THE FLOAT SYSTEM AND THE FLOATS DEPLOYED. THE PILOT RETURNED TO THE HELIPORT. THE PILOT CLAIMS THE FLOAT FIRING PUSHBUTTON WAS IN THE REST POSITION, (NOT PUSHED IN). UPON INSPECTION OF THE SYSTEM, THERE WERE NO DISCREPANCIES FOUND. THE SYSTEM TESTED NORMAL, NO POWER TO THE CONNECTOR PLUGS WHEN THE ARM BUTTON IS PRESSED, ALL (4) CIRCUITS WORKING WHEN THE FIRE BUTTON IS PUSHED. (K) 1 G 7 1 3U 3 U H9EU E19EU 2007032800214 20070328 00214 NM 2007 3 28 2007UALA00802 1 20070316 A 7603 CONTROLLER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 2 ENGINE MALFUNCTIONED A UALA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 WP 29 302UA 23643 723255 ENG 2 THROTTLE STUCK. ENG 2 N1 WILL NOT GO BELOW 75 PERCENT N1 AND 3000 FF WITH THRUST LEVER AT IDLE. [SUP 05-29-07] FAULTY MAIN ENGINE CONTROLLER. REPLACED THE MAIN ENGINE CONTROLLER. UNIT FAILED BENCH TEST. FOUND FAILED CDP. UNIT REQ UIRES OVERAHAUL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007040200209 20070402 00209 2007 4 2 A6WA200740092 4 20070305 A 3497 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE WEATHER RADAR DEFECTIVE A A6WA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 428AW 106LP 7695 CIRCUIT BREAKER PANEL 1, K3 POPPED (WEATHER RADAR RT). REMOVED AND REPLACED RADAR ANTENNA ELEC CONNECTOR AND WEATHER RA DAR ANTENNA IAW AMM 34-41-01. REMOVED AND REPLACED WEATHER RADAR CONTROL PANEL IAW 34-41-04, RAN OPS CHECK OF WEATHER R ADAR IAW AMM 34-41-00. OPS GOOD. NO NOTICE OF LIGHTNING STRIKE DAMAGE. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007040400131 20070404 00131 NM 2007 4 4 2007UALA00945 1 20070329 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 810UA 843 EMERGENCY LIGHTS EPSU POWER SUPPLY FAILS TEST. REPLACED EPSU POWER SUPPLY UNIT. 2 L 7 2 4F 4 F RT A28NM E40NE 2007040500103 20070405 00103 NM 2007 4 5 2007UALA00900 1 20070326 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 294 S7L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 CABIN FRAME BS 294 WEB ATTACH HAS OVERSIZED HOLE AT STR 7L. MAJOR REPAIR ACCOMPLISHED: INSTALLED FRAME ANGLE DOUBLER R EPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007041600013 20070416 00013 EA 2007 4 16 TRAX200700475 1 20070406 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 RT ENGINE SUPPORT BEAM LOWER WEB CRACKED AT FWD INBD NUT PLATE FOR ACCESS PANEL [SUP 4-23-07] REPAIRED IAW ALL FAA APP ROVED DATA. 2 L 7 2 4F 4 F RT A21EA E15NE 2007040600101 20070406 00101 SO 2007 4 6 N93A03042007A 1 20070403 A 2720 1159SCH2385 TORQUE TUBE GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU RUDDER WORN E N93A K NONE O OTHER IN INSP/MAINT 1 SO 13 472QS 7321 1372 RUDDER TORQUE TUBE BOLT HOLES WERE FOUND WORN (ENLARGED) DURING MAINTENANCE. 2 L 7 2 4F 4 F RT A12EA E25NE 2007040600132 20070406 00132 EA 2007 4 6 VNAA0703014 1 20070321 A 3230 895304 PSEU CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE LT MLG FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 703PS 4450 10137 CREW REPORTED A GEAR DISAGREE MESSAGE UPON RETRACTION AFTER TAKEOFF. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUA L. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007041900133 20070419 00133 NM 2007 4 19 2007UALA01112 1 20070410 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY EEL LIGHT INOPERATIVE AT SEAT 36L. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007042600277 20070426 00277 CE 2007 4 26 AMWA83918 1 20070412 A 3240 1148100559 BRAKE ASSY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A65B 52043 EA MLG WEAK A AMWA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 07 155YV N155YV AFTER LANDING THE CAPT REPORTED THAT THE BRAKES FELT SPONGY. THEY TAXIED THE PLANE TO THE HANGAR. MAINTENANCE BLED BRA KES, OPS CHECKED GOOD. 2 L 7 2 4T 4 T RT A24CE E4EA 2007043000083 20070430 00083 NM 2007 4 30 2007UALA01157 1 20070414 A 5415 FITTING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 PYLON DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 NR 2 PYLON AFT OTBD MID-SPAR FITTING UPPER TANG HAS DRILL START BESIDE FASTENER HOLE. [06-14-07] MAJOR REPAIR AC COMPLISHED. REPAIRED DAMAGED AREA. CLEANED DRILL START WITH SPOT FACE. SHOT PEENED, PASSIVATED AND INSTALLED FASTENER . 2 L 7 2 4F 4 F RT A2NM E17NE 2007050100095 20070501 00095 EU 2007 5 1 BMAC07003 1 20070423 A 2910 1379007D442 LINE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110UG 01514 WP HYD SYSTEM LEAKING A B16A O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 35 539PA 741 UPON LANDING, BRAKES AND STEERING FOUND TO BE VERY SLUGGISH AND BOTH HYD PUMPS INDICATED NEAR ZERO, APPROX. 100 PSI. TAX I TO GATE WITH NO FURTHER INCIDENT. MAINT FOUND HYD SUPPLY PIPE IN RT IB WING CHAFED. REPLACED PIPE AND ARE REPLACING B OTH HYD PUMPS DUE TO POSSIBLE CAVITATION. NOTE: JOB IS NOT COMPLETE AT THIS TIME. 2 L 7 2 4T 4 T RT A21EU E4WE 2007041700004 20070417 00004 CE 2007 4 17 4514504102007 1 20070410 A 3260 604HE162 DOWNLOCK SWITCH LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE7312 01518 WP LT MLG MALFUNCTIONED E J7SA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 05 421FX 145 LT GEAR DOWN AND LOCKED LIGHT DID NOT ILLUMINATE AFTER MULTIPLE TRIES. EVERY ATTEMPT GOT SAME INDICATION. NOSE GEAR AND RT MAIN GEAR GREEN AND LT MAIN GEAR WHITE UNSAFE AND NO GREEN LIGHT. TRIED BOTH FREE FALL AND AUX HYDRAULIC EXTENSION WI TH SAME RESULT. IN FLIGHT EMERGENCY DECLARED ENROUTE. LANDING AND TAXI UNEVENTFUL. INSTALLED NEW LT MLG ACTUATOR DOWN L OCK SWITCH. RIGGED AND OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT T00008WI E6WE 2007050700016 20070507 00016 EA 2007 5 7 A6WA200740157 1 20070327 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT/CABIN ODOR A A6WA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 31 409AW 7447 AFTER ROTATION, NOTICED ODOR LIKE (BURNED TOAST) IN COCKPIT. FLIGHT ATTENDANT REPORTED SIMILAR ODOR IN CABIN, STRONGER TOWARDS THE REAR OF THE CABIN. BOTH PACKS OPERATING ON APU. TRANSFERRED TO ENGINE BLEEDS, SMELL DISSIPATED. NO VISIBL E SMOKE SEEN. OPS CHECK PACKS WITH APU AND ENGINES IAW AMM 21-40 AND 21-50. OPERATED HOT AND COLD, NO ABNORMAL ODOR NO TED IN CABIN OR FLIGHT DECK. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007050100100 20070501 00100 CE 2007 5 1 AMWA83962BC 1 20070414 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE ZONE 600 DISCHARGED A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 159YV 18786 61 UE159 BATTERY CHARGE ANNUN CAME ON IN FLT (ILLUM FOR 2-3 MIN THEN EXTINGUISHED) CAME ON AGAIN AND EXTINGUISHED AGAIN A FEW MIN UTES LATER, ABNORMAL CKLIST ACCOMP BOTH TIMES (PROP AND W/S DEICE ON). THIS BATTERY CHARGE LIGHT ILLUM IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS. REMOVED AND REPLACED BATTERY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007050300253 20070503 00253 NM 2007 5 3 2007UALA01248 1 20070421 A 5320 SUPPORT BRACKET BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 MAIN CABIN FLOOR BEAM INTERCOSTAL SUPPORT BRACKET CRACKED STA 1503, LBL 67. MAJOR REPAIR ACCOMPLISHED: FABRICATED & IN STALLED NEW BRACKET. 2 L 7 2 4F 4 F RT A1NM E24NE 2007050300344 20070503 00344 NE 2007 5 3 042507N220CA 2 20070425 A 7200 ENGINE AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D 30010 NE NR 2 STALLED E CEDA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 05 220CA 220 304035B ON CLIMB-OUT FROM ADS AT FL250, THE NR 2 ENGINE STALLED. THE A/C RETURNED TO ADS. AFTER EXTENSIVE TROUBLESHOOTING THE CAUSE OF PROBLEM WAS NOT FOUND. THE ENGINE WAS RETURNED TO COMPANY THAT WAS LEASED FROM. 2 L 7 2 4F 4 F A7EU E7EA 2007051400202 20070514 00202 NM 2007 5 14 AMTA200700206 1 20070427 A 3620 WARNING SYSTEM BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE BLEED AIR SYS MALFUNCTIONED A AMTA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 552TZ 32586 EICAS MESSAGE L ENG BLEED, OFF LIGHT ILLUMINATED. RAN LT ENGINE, OPS CHECKED LT ENGINE BLEED REF MM 36-11-00. NO DEFEC TS NOTED, BLEED OPERATION NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007051400220 20070514 00220 EU 2007 5 14 TRBA2007018 1 20070420 A 2435 M259884113 O-RING AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE RT STARTERGEN BROKEN A TRBA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 29 408AT 408 WHILE IN CLIMB, NR 2 ENG OIL LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT, WITH MASTER WARNING. SHUTDOWN IAW CHECK LIST AND LANDED. EMERGENCY DECLARED. FOLLOW MFG FAULT ISOLATION MANUAL (PW 72-00-01). FOUND STARTER GENERATOR BROKEN O-RING. REMOVED AND INSTALLED RT ENGINE STARTER GENERATOR 0-RING IAW JIC 24-32-61, RAI 10000-006, OPS CHECK AND NO LEAKS WERE FO UND. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007051700065 20070517 00065 NE 2007 5 17 2007UALA01237 2 20070417 A 7230 BLADES BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE DAMAGED A UALA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 WP 29 663UA 60886 27160 717676 BIRD STRIKE TO NR 1 ENGINE. ACCOMPLISHED BOROSCOPE INSP OF NR 1 ENG HPC 5TH, 6TH, 10TH AND 11TH STG BLADES PER MM 72-00 -00. FOUND 1 EA 6TH STG BLADE WITH LARGE TEAR IN AREA C OF L/E BEYOND FLYBACK LIMITS, 18 EA 10TH STG BLADES WITH DAMAGE BEYOND LIMITS IN AREA B AND C, AND 2 EA 11TH STG BLADES WITH LARGE TEARS BEYOND LIMITS IN AREA C. BY- 41440: REMOVED ENG 717676 & REPLACED. COMPLETED VERIFICATION FLIGHT & ENGINE TESTED GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2007052300014 20070523 00014 NM 2007 5 23 2007UALA01546 1 20070516 A 5730 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT WING GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 LEFT WING LWR SKIN FASTENER HOLE -B- AT SIDE LINK FITTING ATTACH AREA HAS 3 EA DEEP GOUGES. [06-14-07] MAJOR REPAI R ACCOMPLISHED. REMOVED DAMAGE SKIN, REPLACED PRODUCTION SLICE AND REPAIRED HOLE PER UA ENGINEERING SPECIFICATIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007052900045 20070529 00045 NM 2007 5 29 2007UALA01626 1 20070524 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 CEILING EMERGENCY LIGHTS ARE INOPERATIVE AT THE COCKPIT, ROW 12 & ROW 13. RELAMPED EMRGENCY LIGHTS, CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007053000001 20070530 00001 2007 5 30 ASMF200705007 4 20070519 A 3442 20412170414 TRANSCEIVER DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE WX RADAR SYS FAILED W ASMF A UNSCHED LANDING O OTHER CR CRUISE 1 SW 23 754RA 3049 3049 49641 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, DUE TO THE WEATHER RADAR FAILED IN FLIGHT. MAINTENANCE PERSONNEL REPLACED THE RADAR TRANSCEIVER IAW MM 34-41-04 TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2007061400148 20070614 00148 CE 2007 6 14 HYIA052707 1 20070527 A 7620 TSIO520VB ENGINE CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO MCAULY 3AF32C 3AF32C505 GL RIGHT FAILED E HYIA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 NE 01 2611X 1825 1825 402C0072 831928R 001123 RIGHT ENGINE FAILURE ON 1/2 MILE FINAL TO RUNWAY 25 AT PVC, CREW FEATHERED ENGINE AND LANDED. LATER INSPECTION ON 5-27- 07 FOUND INTERNAL FAILURE IN THE RIGHT ENGINE. ENGINE REMOVED AND REPLACED ON 5-28-07. A/C RETURNED TO SERVICE AND ENG TO BE SENT TO MANUFACTURE FOR INVESTIGATION. 1 L 7 2 3O 3 O A7CE E8CE 5 C P22EA 2007061400226 20070614 00226 EA 2007 6 14 S9BA0907 1 20070516 A 7120 C6WM15194 ADAPTER DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA ZONE 500 CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 251SA 125 524 OB ENGINE MOUNT ADAPTOR ON LT NACELLE IS CORRODED. REPLACED MOUNT ADAPTOR PLATE IAW RD6-54-006. 1 H 7 2 3T 4 T RT A9EA E4EA 2007061800170 20070618 00170 NE 2007 6 18 DXTA200702263 2 20070614 A 7200 EEC CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE RIGHT FAILED E DXTA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 07 643QS 5605588 RT EEC FAILED DURING TAKE-OFF, ENGINE INDICATIONS WERE IN TRANSIENT LIMTS. [07-09-07] DOWNLOADED RIGHT EEC AND FOUND CODE F1-10 DISPLAYED FOR BLEED VALVE TORQUE MOTOR. CHECKED WIRING BETWEEN TORQUE MOTOR AND EED NO DEFECTS NOTED. RE MOVED AND REPLACED TORQUE MOTOR WITH OVERHAULED UNIT USING NEW PARTS. GROUND RAN ENGINE RAN ENGINE. OPS AND LEAK CHECK WAS GOOD. WORK PERFORMED PER PWA 545 MM. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007062200133 20070622 00133 NM 2007 6 22 2007UALA02006 1 20070613 A 2421 FILTER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LT ENGINE IDG CLOGGED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 786UA 26938 LEFT ENG IDG DPI POPPED. [07-13-07] REPLACED INTEGRATED DRIVE GENERATOR. OP CHECKS GOOD FOR SERVICE. SUSPECT INTERN AL DEBRIS CLOGGED FILTER & CAUSED DPI TO POP. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007062800164 20070628 00164 NM 2007 6 28 2007UALA02091 1 20070617 A 3350 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 ALL EEL STRIPS IN UPPER DECK STAIRWAY & BOTH EEL STRIPS AT TOP OF STAIRWAY ARE INOPERATIVE. *S/D* SECURED CONNECTOR AT PWR CONNECTION. 2 L 7 4 4F 4 F RT A20WE E24NE 2007061400046 20070614 00046 2007 6 14 2007UALA01890 4 20070607 A 2565 GIRT BAR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE DOOR 2R FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 402UA 439 FOUND 2R DOOR DIFFICULT TO ARM. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071300274 20070713 00274 NM 2007 7 13 2007UALA02367 1 20070630 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY EEL LIGHTS INOP AT SEATS 2J FWD, 4J AFT & 44 HJK. REPLACED LIGHT ASSYS. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071800319 20070718 00319 NM 2007 7 18 2007UALA02450 1 20070706 A 2621 FIRE BOTTLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU APU LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 301UA 23642 CREW REPORTS, THE APU FIRE EXTINGUISHER PRESSURE IS AT OR NEAR 300 PSIG (LOW). [07-27-07] REPLACED APU FIRE EXTING UISHER BOTTLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007073100061 20070731 00061 2007 7 31 2007UALA02680 4 20070716 A 2565 SLIDE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU L2 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 904UA 25004 THREADING ON DOOR 2L SLIDE IS COMING APART. [08-07-07] STOWED THREADING BACK IN SLIDE FLAP. 2 L 7 2 4F 4 F RT A16WE E21EU 2007073100126 20070731 00126 NE 2007 7 31 UPS07550215 2 20070723 A 7310 FUEL FILTER BOEING 757 75724APF 1384969 NM RROYCE RB211 RB211* 54555 NE NR 2 ENGINE UNKNOWN A IPXA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 01 468UP 25484 RECEIVED NR 2 ENGINE FUEL FILTER MESSAGE. A/C IS OOS FOR TROUBLESHOOTING. [08-01-07] REMOVED & REPLACED EPR TRANSMIT TER RT ENGINE PER MM 77-11-01-4. PERFORMED EPR HIGH POWER ENG RUN PER MM 71-00-00-5 TEST 13. ALL ENG PARAMETERS CHECK OK . ITEM CLEARED. 2 L 7 2 4F 4 F RT A2NM A12EU 2007071200123 20070712 00123 2007 7 12 ASMF200707001 4 20070701 A 3422 4056510903 DISPLAY DOUG DC9 DC987 3022087 WP CFMINT CFM567 CFM567B22 13802 NE LT SIDE DAMAGED W ASMF K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 23 754RA 6129 49641 CAPTAIN REPORTED LT NAVIGATION DISPLAY OUT OF SERVICE AND SMOKE ODOR IN CABIN. DURING MAINTENANCE CHECK, IT WAS DETECTE D THAT THE ODOR WAS ORIGINATED BY THE DISPLAY UNIT, WHICH WAS REPLACED IAW MM 34-22-06, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E00055EN 2007070300105 20070703 00105 EA 2007 7 3 A6WA200740233 1 20070430 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 452AW 7835 RT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED .5 INCH LONG IN OB RADIUS. (K) [07-17-07] MAINTENANCE REPAIRED IAW BOMBA RDIER AEROSPACE REO 601R-53-61-117. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071100188 20070711 00188 NM 2007 7 11 2007UALA02160 1 20070621 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 AFT CABIN FLOORBEAM CAP UPPER SURFACE STA 985-987 RBL 40 TO RBL 45 WL 208 HAS CORROSION. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071000482 20070710 00482 NM 2007 7 10 2007UALA02322 1 20070628 A 5754 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L/E SLAT LOOSE A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 598UA 28751 SOMETHING ON RIGHT SLAT IS LOOSE AND FLAPPING. [08-08-07] APPLIED FIBERGLASS SLAT REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071800225 20070718 00225 NM 2007 7 18 SB07051 1 20070707 A 3397 WIRE BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE EMERGENCY LIGHT BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 592US 23937 MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHT AT ROW 12, LT SIDE, INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT SEAT ROW 12, LT SIDE. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2007071800327 20070718 00327 SO 2007 7 18 N93A07072007 1 20070707 A 3250 51507 MANIFOLD GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU NLG STEERING FAILED E N93A C ABORTED TAKEOFF O OTHER TX TAXI/GRND HDL 1 SO 13 454QS 1454 WHEN TURNING ONTO RUNWAY FOR TAKEOFF, NOSE WHEEL STEERING WAS LOST FOLLOWED BY AMBER STEER BY WIRE FAIL MESSAGE. 2 L 7 2 4F 4 F RT A12EA E25NE 2007072000137 20070720 00137 NE 2007 7 20 UPS07550150 2 20070711 A 7230 COMPRESSOR BOEING 757 75724APF 1384969 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE STALLED A IPXA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 01 438UP 25469 INSPECTION TYPE:N/A ATB - SEVERAL COMPRESSOR STALLS NOTED ON CLIMBOUT LEFT ENG. *SUPPLEMENTAL SDR* REMOVED AND REPLACE D NR 1 ENGINE WITH REFERENCE TO MAINTENANCE FUNCTION TASK CARD TC 5001 (RR), ENGINE GROUND RAN NORMAL. A/C OK FOR SERVI CE. 2 L 7 2 4F 4 F RT A2NM E12EU 2007080800014 20070808 00014 2007 8 8 WNH2007F00002 4 20070722 A 3416 2871101 ALTIMETER BEECH 90 C90A 1152911 CE PWA PT6 PT6* 52043 EA COCKPIT MALFUNCTIONED E WNHA O OTHER O OTHER NR NOT REPORTED 1 WP 25 73PG 1680 LJ1607 ENCODING ALTIMETER DISPLAY FADES IN AND OUT TO THE POINT THAT THE INFORMATION DISPLAYED IS ILLEGIBLE TO THE PILOT. (K) 1 L 7 2 3T 3 T RT 3A20 E2NE 2007080900140 20070809 00140 NM 2007 8 9 2007UALA02863 1 20070727 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 23AB INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY LIGHT INOP SEAT 23 AB. 2 L 7 4 4F 4 F RT A20WE E24NE 2007080900022 20070809 00022 2007 8 9 BB07059 4 20070730 A 3442 WAVE GUIDE BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE WX RADAR SYS FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 921UW 22201 FLIGHT 1297: ENROUTE, THE WEATHER RADAR FAILED. FLIGHT RETURNED. MAINTENANCE FOUND AND REMOVED A BLOCKAGE IN THE WAVE G UIDE. NO FURTHER FAULTS. 2 L 7 2 4F 4 F RT A2NM E12EU 2007081000062 20070810 00062 NM 2007 8 10 PIDA07039 1 20070727 A 5330 SKIN BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 583CC 21069 DURING C-CHECK, NOTED CRACK IN EDGE OF SKIN AT LT AFT CORNER OF ELECTRONIC ACCESS DOOR. REPAIRED AREA IAW SRM 52-00-3 F IGURE 5. 2 L 7 2 4F 4 F A16WE E2EA 2007081000085 20070810 00085 EA 2007 8 10 A6WA200740377 1 20070707 A 5710 PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 461AW 7870 RT FUEL PANEL 640BB HAS CORROSION DAMAGED IN THE NON-CRITICAL AREA, COMPLY WITH E06/21/457 (WING PLANK CUTOUT) (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007081700146 20070817 00146 NM 2007 8 17 2007UALA03006 1 20070804 A 5320 ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSLEAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 PASSENGER CABIN STA 290 JUST ABOVE STR 11R ANGLE CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKED ANGLE. REPLACED WITH NEW ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007080800079 20070808 00079 CE 2007 8 8 AMWA06032M 1 20070725 A 5311 1294300311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 423 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007080900181 20070809 00181 NM 2007 8 9 2007UALA02905 1 20070729 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 565UA 26669 MOST FWD EEL LIGHT IN 1ST CLASS CABIN IS INOPERATIVE. REPLACED LIGHT SEGMENT. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082100038 20070821 00038 2007 8 21 2007UALA02929 4 20070731 A 2565 PIN BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EVAC SLIDE SHEARED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 669UA 30025 LEFT OVERWING SLIDE COMPARTMENT DOOR, FWD SLIDE PACK ALIGNMENT PIN SHEARED. FOUND DURING SLIDE CHANGE. REMOVED AND REP LACED LINE UP PIN. SUSPECT JOLT DURING FLIGHT TURBULENCE CAUSED ENOUGH MOVEMENT TO SHEAR PIN. 2 L 7 2 4F 4 F RT A1NM E24NE 2007082100103 20070821 00103 NM 2007 8 21 2007UALA02972 1 20070730 A 3350 767 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 210UA 30216 NR 4R DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOP. RELAMPED SLIDE LIGHT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007082900129 20070829 00129 EA 2007 8 29 VNAA0708006 1 20070810 A 2750 860D10018 ECU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE T/E FLAP FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 05 244PS 5887 7912 CREW REPORTED A FLAPS FAIL AT 20 DEGREES. CREW DIVERTED TO ILM AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE FLAP ELECTRONIC CONTROL UNIT TO BE CAUSING ERRATIC MESSAGES. MAINTENANCE REMOVED AND REPLACED THE FECU IN ACC ORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007083100149 20070831 00149 2007 8 31 2007UALA03322 4 20070822 A 2565 BOLT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE 2L SLIDE MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 478UA 1533 LEFT AFT SLIDE INDICATION INOP ON DOOR -OXY SYSTEM ECAM PAGE - DOOR-OXY CREW COMMENTS: 2L SHOWS UNARMED IN FLT ON LOWER ECAM DOOR AND GIRT BAR APPEAR NORMAL. DOOR 2L DOES NOT SHOW ARMED. FOUND BOLT FOR ARMING HAND L/E IN BACKWARDS INSTAL LED IN CORRECT MANNER. DOOR ARMS AND DISARMS NORMAL. INDICATION NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007090500242 20070905 00242 NM 2007 9 5 2007UALA03367 1 20070823 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY LIGHT STRIP INOP ON GALLEY WALL AT 4L. SECURED EMERGENCY LIGHT STRIP ON GALLEY WALL AT 4L. CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082400182 20070824 00182 EA 2007 8 24 A6WA200740408 1 20070721 A 5310 VERTICAL BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 409 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 FS 409.0+128 VERTICAL BEAM AT RBL 27 CRACKED APPROX.2 INCH LONG ON IB SIDE AT BOTTOM RIVET. (K) MAINTENANCE REMOVED DA MAGE FABRICATED AND INSTALLED REPAIR PARTS IAW BOMBARDIER REO 601R-53-41-056 REV E AND BSC EO 601R-53-12516. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007090700151 20070907 00151 NE 2007 9 7 MASA200700470 2 20070801 A 7200 CF348C5 ENGINE CNDAIR CL600 CL6002D24 1390016 EA GE CF34 CF34* NE NR 2 ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 938LR 5855 15038 194286 ASH 2711 YEG-PHX CREW RETURNED TO GATE DUE TO SMOKE ODOR AND SMOKE IN THE CABIN. MX REMOVED AND REPLACED NR 2 ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2007092500127 20070925 00127 CE 2007 9 25 DXTA200702483 1 20070916 A 3610 DUCT RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP BLEED AIR LOOSE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 821QS 258709 BAG FIRE LIGHT CAME ON IN FLIGHT DURING T/O. 09-28-07 FOUND BLEED AIR DUCT LEAKING TIGHTENED DUCT CLAMP OPS CHECKED GOOD IAW HAWKER 800XP AMM 21-10-15. 2 L 7 2 4F 4 F RT A3EU E6WE 2007100900159 20071009 00159 NM 2007 10 9 2007UALA03997 1 20070928 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RIGHT OVERWING INTERMITTENT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 677UA 30029 RIGHT OVERWING EMERGENCY EXIT LIGHTS ON INTERMITTENTLY IN FLT. ACCOMPLISHED CHECK OF OVERWING EXIT LIGHT. CYCLE SWITC H AND NO DEFECTS NOTED 2 L 7 2 4F 4 F RT A1NM E24NE 2007092500440 20070925 00440 NM 2007 9 25 2007UALA03693 1 20070912 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 643UA 25093 SHORT X AISLE EEL LIGHT IN AFT GALLEY INOP. 10-5-07 REPLACED SMALL 15 INCHER CROSS AISLE EMERGENCY LIGHT. STRIP IN A FT GALLEY SECTION. 2 L 7 2 4F 4 F RT A1NM E24NE 2007092800040 20070928 00040 NM 2007 9 28 2007UALA03735 1 20070915 A 4900 APU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SHUTDOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 APU SHUTDOWN WHILE AT GATE. 10-9-07 ACCOMPLISHED FADEC BITE TEST - LAST FIVE LEGS SHOW NO FAULTS. REPLACED OIL PRES S SWITCH. APU RUNS NORMAL WITH FULL ELECTRICAL AND AIR LOADS. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101000183 20071010 00183 2007 10 10 2007UALA03816 4 20070920 A 2565 CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE DISCONNECTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 565UA 26669 RIGHT OVERWING EVACUATION SLIDE RELEASE CABLE FOUND DISCONNECTED FROM QUICK RELEASE PIN. 2 L 7 2 4F 4 F RT A2NM E17NE 2007101100025 20071011 00025 NE 2007 10 11 AALA20071839 2 20071002 A 7261 OIL CAP BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE LOOSE A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 21 699AN 27051 31339 RNO INFLIGHT T1758/02OCT - LEFT ENGINE OIL QUANTITY LOSS INDICATION. CREW SHUT DOWN NUMBER ONE ENGINE INFLIGHT. LANDED RNO WITHOUT INCIDENT. SINGLE ENGINE TIME 25 MINUTES. FOUND LOOSE OIL CAP. RESECURED OIL CAP FOR NUMBER ONE ENGINE AN D ADDED OIL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2007101900281 20071019 00281 NM 2007 10 19 WRLA2007111 1 20071011 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 273WA 48519 DURING 4C+12A CHECK, FOUND AFT CABIN LT FLOOR CURVED SEAT TRACK HAS CORROSION AT STA Y=1964, X=107.25. 10-23-07 REPA IRED THE AFT LT FLOOR CURVED SEAT TRACK PER MD-11 SRM VOL.I 53-70-00 FIG.1 REV.40. 2 L 7 3 4F 4 F RT A22WE E24NE 2007102300167 20071023 00167 NM 2007 10 23 AMTA200700490 1 20071012 A 5412 BULKHEAD BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE NACELLE GOUGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 DURING MAINTENANCE INSPECTION AT SAA, ATA EO 757-54AD-2456D, THE MID BULKHEAD IB UPPER LUG HOLE WAS GOUGED. C/W SAA EA 757-5450-09-A1048-REV-A. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007102600176 20071026 00176 NM 2007 10 26 2007UALA04281 1 20071016 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 600 S23-24L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 FWD PIT STA 600 MAIN FRAME BETWEEN STR 23L AND 24L FRAME HAS 2 DENTS. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE AND INS TALLED ANGLE REPAIR. HIGH FREQUENCY EDDY CURRENT INSP BEFORE INSURANCE CUT, NO CRACKS FOUND. COLD WORKED 4 EA HOLES. 2 L 7 2 4F 4 F RT A2NM E17NE 2007102900005 20071029 00005 NM 2007 10 29 2007UALA04292 1 20071018 A 2612 FIRE LOOP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 2 NACELLE FAULTY A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 350UA 24301 NR 2 ENG FIRE LOOPS (ENG OVERHEAT & FIRE DET SYS DUAL LOOP). 2 L 7 2 4F 4 F RT A16WE E21EU 2007110100165 20071101 00165 SO 2007 11 1 ESPA100107 1 20071017 A 5610 159SCCE100S12 WINDSHIELD GULSTM G1159 G1159 3953505 SO RROYCE SPEY SPEY5118 54523 EU COCKPIT CRACKED E ESPA A UNSCHED LANDING O OTHER DE DESCENT 1 SO 11 183PA 4890 4890 108 DURING DECENT AT 20,000 FEET THE CO-PILOTS WINDSHIELD DEVELOPED CRACK STARTING FROM THE RT SIDE BOLT PATTERN AND EXTENDI NG DOWN AND ACROSS. CREW DECIDED TO DIVERT, AS THE CRACK HAD SPLIT INTO (2) CRACKS. ALSO, DECLARED AN EMERGENCY TO ATC PROCEEDING VISUALLY DIRECT TO RUNWAY 7R. LANDED WITHOUT ANY INCIDENT AND TAXIED TO RAMP. 2 L 7 2 4F 4 F RT A12EA E2EU 2007103100181 20071031 00181 NM 2007 10 31 2007UALA04349 1 20071023 A 3260 SENSOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NLG MALFUNCTIONED A UALA O OTHER N FALSE WARNING CR CRUISE 1 WP 29 313UA 23674 AMBER ALERT. NLG UNSAFE LIGHT ON WITH GEAR UP. ON LANDING NLG GREEN WENT INTERMITTENT THEN NO INDICATION. FOUND FAUL TY S845 SENSOR (NOSE GEAR DOWN). REPLACED S845 SENSOR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007112900056 20071129 00056 NM 2007 11 29 2007UALA04778 1 20071120 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 331UA 24192 DURING C-1 CHECK INSPECTION OF THE E&E COMPARTMENT DOOR WAY CUTOUT CORROSION WAS FOUND IN MULTIPLE LOCATIONS ALONG THE 6 5-45829-505 LOWER CHORD MATING AREA FOR THE DOOR & PRESSURE SEAL AT BS 325-345 ADJACENT TO STRINGERS 28L & 28R AT WL 150 APPROX. REPAIR ACCOMPLISHED: BLENDED OUT CORROSION. REPLACED FASTENERS IN BLENDED AREA. 2 L 7 2 4F 4 F RT A16WE E21EU 2007113000141 20071130 00141 NM 2007 11 30 AMTA200700517 1 20071017 A 5320 SILL BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE BS 1380-1426 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 550TZ 32584 AFT CARGO DOOR LOWER SILL HAS CORROSION FROM STA 1380, STA 1426 RBL 22. REPLACED Z CHANNEL IAW SRM 51-40-02-0G. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007120500011 20071205 00011 NM 2007 12 5 AMTA200700587 1 20071107 A 3030 WARNING MESSAGE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE PITOT HEAT ILLUMINATED A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 514AT 27971 EICASE MSG CAPT`S PITOT DISPLAYED. CAPTAINS PITOT PROBE HEAT LIGHT ILLUMINATED. PERFORMED FIM 30-31-00 FIG 103, IAW BL K 4, YES, BLK 26, SYS OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007120500031 20071205 00031 CE 2007 12 5 DXTA200702620 1 20071120 A 3220 ACTUATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE NLG UPLOCK MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 608QS 5605308 AFTER TAKEOFF AND GEAR RETRACTION, RED GEAR UNLOCK LIGHT REMAINED ILLUMINATED. REMOVED & REPLACED NOSE GEAR UPLOCK ACTU ATOR WITH NEW IAW MM 32-30-05. OPS CHECKS NORMAL. SERVICED HYDRAULIC RESERVOIR. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007120500023 20071205 00023 NM 2007 12 5 BKE2007F00000 1 20070914 A 3810 4AS1271081501 DRAIN LINE GULSTM 200 200 4500308 NM PWC PW306 PW306C 52169 NE POTABLE WATER CRACKED E BKEA B EMER. DESCENT K F FLUID LOSS FLT CONT AFFECTED CR CRUISE 1 WP 01 322AD 2634 22 PCECC0034 WHILE FLYING AT FLIGHT LEVEL 370, THE PILOTS WERE NOT ABLE TO MOVE THE AILERON CONTROLS. THE AIRCRAFT DESCENDED TO A LO WER ALTITUDE AND THE AILERON CONTROLS FUNCTIONED NORMALLY. THE AIRCRAFT UPON RETURN TO HOME BASE WAS INSPECTED. IT WAS DETERMINED THAT WATER HAD FROZEN ON THE AILERON ARTIFICIAL FEEL SYSTEM, INHIBITING THE CONTROL INPUTS OF THE AILERONS B Y THE PILOTS OR THE AUTOPILOT. FURTHER INSPECTION REVEALED THAT THE WATER THAT HAD FROZEN ON THE AILERON ARTIFICIAL FEE L SYSTEM HAD COME FROM A CRACKED DRAIN LINE ON THE POTABLE WATER SYSTEM DRAIN. (K) 2 L 7 2 4F 4 F RT A53NM E35NE 2007121200097 20071212 00097 NM 2007 12 12 2007UALA04830 1 20071123 A 3350 9F19948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY EXIT EEL LIGHT INOP AT ROW 51L. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007121300141 20071213 00141 EU 2007 12 13 2007UALA04875 1 20071129 A 3397 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 494UA 1840 ROW 11 EMERGENCY AISLE LIGHT INOP. FOUND CONNECTOR FOR THE EEL LIGHT AT ROW 11 HAD BEEN DAMAGED. REPAIRED CONNECTOR FOR EEL HARNESS, NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007122800077 20071228 00077 NM 2007 12 28 2007UALA05107 1 20071213 A 3350 8100133801 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 32R BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 215UA 30221 FOUND SEAT 32R, SEAT EEL BROKEN. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008010700044 20080107 00044 NM 2008 1 7 2007UALA05158 1 20071219 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 SEAT 2A AFT EEL LIGHT INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2007122800136 20071228 00136 2007 12 28 DXTA200702659 4 20071207 A 3420 102011 COMPUTER RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP FAULTY E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 895QS 531 258606 ON TAKEOFF AT APPROXIMATELY 60KTS, THE STALL IDENT 3 ANN LIGHTS ILLUMINATED. TAKEOFF ABORTED, LIGHT EXTINGUISHED. REMOV ED FAULTY THIRD CHANNEL IDENT STALL CAN P/N - 10201-1 S/N F469 INSTALLED REPAIRED STALL CAN P/N - 10201-1 S/N F415. SYST EM OPS CHECKS FUNCTIONS PROPERLY. FOR DETAILS REFERENCE FAS W/O 07-2994 & DUNCAN W/O YFY7A. DONE IAW HAWKER 800XP MM CHA P 27-33--14-501 2 L 7 2 4F 4 F RT A3EU E6WE 2008010700051 20080107 00051 NM 2008 1 7 2007UALA05163 1 20071218 A 5347 SEAT TRACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 523UA 24932 SEAT TRACK SUPPORT AT BS 365.25 AND RBL 24 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION. INSTALLED STR AP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010900250 20080109 00250 NE 2008 1 9 MASA200700690 2 20071013 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NR 1 SMOKE A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 591ML 7388 ASH FLT 7223, TUC - CREW WAS MADE AWARE OF WHITE SMOKE COMING FROM NR 1 ENGINE DURING TAXI AFTER ENGINE WAS S/D. MX TRO UBLESHOT AND FOUND OPS NORMAL. 2 L 7 2 4F 4 F RT A21EA E15NE 2008011400101 20080114 00101 NM 2008 1 14 AMTA200700724 1 20071228 A 4900 RELAY BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE APU FAILED A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 550TZ 32584 APU FAILED TO START ON THE GROUND. REMOVED AND REPLACED APU RELAY IAW FIMM 49-11-00, OPS CHECK NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008012200132 20080122 00132 EA 2008 1 22 A6WA200740696 1 20071210 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 432AW 7257 LT INTERCOSTAL CLIP AT FS 621.0 TO FS 625.0 IS CRACKED. INTERCOSTAL CLIP AT FS 621.0 TO FS 625.0 LT REPLACED IAW SRM 51 -42-20. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008011000155 20080110 00155 2008 1 10 DXTA200702702 4 20071223 A 3425 701730031444 COMPUTER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL E/E BAY INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 923QS 3238 7500023 AMBER CAS MESSAGE (TRIM SW FAIL L) ILLUMINATED IN FLIGHT. REMOVED AND REPLACED THE NR 2 INTEGRATED AVIONICS COMPUTER IA W THE CESSNA 750 MAINTENANCE MANUAL 34-25-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008011100040 20080111 00040 NM 2008 1 11 QXEA200701902 1 20071214 A 3231 ROD DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE MLG DOOR BROKEN A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 354PH 498 FLIGHT 2035. LT MAIN GEAR DOORS WERE OPEN WITH NO INDICATION FROM THE COCKPIT, ONLY THE LT SIDE OF THE DOOR IS OPEN. MAI NTENANCE REPLACED THE SPRING, CONNECT ROD WHICH WERE BROKEN. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2008011100131 20080111 00131 CE 2008 1 11 AMWA107120502 1 20071207 A 5720 DOUBLER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE WS 67 CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 135YV 24610 UE135 AFT ACM SCREEN ASSEMBLY CHAFING INTO DOUBLER P/N 114-120022-11 IN RT WING CENTER SECTION, WS 67.05. REPAIRED IAW SRM 51- 40-02 AND CLEARED DISCREPANCY. 2 L 7 2 4T 4 T RT A24CE E26NE 2008012200055 20080122 00055 EU 2008 1 22 01092008 1 20071219 A 5312 D53472193200 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A BUEA O OTHER O OTHER IN INSP/MAINT 1 GL 23 320NP 6049 6 1494 MAIN CABIN FLOOR SUPPORT FR 67-68, RBL-4765 HAS 2 EACH SPOTS OF CORROSION BY R-2 DOOR. 1 INCH X .5 REF A319 AMM 53-41-00 . 2 L 7 2 4F 4 F RT A28NM E37NE 2008050800061 20080508 00061 CE 2008 5 8 LE72008F00000 1 20070116 A 3230 6046H39A RELAY BEECH 90 E90 1152914 CE PWA PT6 PT6* 52043 EA LANDING GEAR FAILED E LE7A O OTHER O OTHER CR CRUISE 1 EA 05 10WG 9629 LW310 LANDING GEAR FAILED TO EXTEND, GEAR LOWERED MANUALLY. (K) 1 L 7 2 3T 3 T 3A20 E2NE 2007082900051 20070829 00051 NM 2007 8 29 ASAA0771958 1 20070814 A 5754 SKIN BOEING 737 737790 13844CN NM L/E SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 NR 6 SLAT LOWER SIDE T/E IS CHAFED. REPAIRED IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2007082200117 20070822 00117 NM 2007 8 22 AWXA200700986 1 20070810 A 2611 RAI2800M0706 CONTROL UNIT AIRBUS A319 A319132 3930340 NM SMOKE DETECTION FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 806AW 16085 4424 1056 PHX - OTH - LOG NR 4151512 - MX REPORTED SMOKE LAV AND CRG DET FAULT ON ECAM. MX REPLACED THE SMOKE DETECTION UNIT. OP ERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2007092500048 20070925 00048 NM 2007 9 25 SWAA074548 1 20070911 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007020200039 20070202 00039 WP 2007 2 2 UPS07849055 1 20070108 A 5312 BULKHEAD DOUG DC8 DC871F 302199D WP FS 1766 L2R-L3R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C3 - FOUND AFT PRESSURE BULKHEAD STA 1766 HAS CRACK BTWN L2R & L3R. STOP DRILLED 2 ENDS OF CRACK, FABRI CATED AND INSTALLED 2 REPAIR ANGLES IAW SRM 53-2-0 FIG 24, 51-1-20D. 2 L 7 4 4F RT 4A25 2007100900102 20071009 00102 WP 2007 10 9 07FDEA04347 1 20070927 A 5311 AGA37823 FRAME DOUG DC10 DC1010 3022110 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 DURING MD10 ACF MODIFICATION, FOUND CRACK 4" LONG ON THE FRAME STA 1821 TO NEXT STRG 11 LT SIDE REPAIRED FOR SRM 53-30-0 0 FIG 5 VOL I. 2 L 7 3 4F A22WE 2007013100252 20070131 00252 WP 2007 1 31 07FDEA00217 1 20070131 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 554FE 46708 RT WING L/E AT NR 4 CUTOUT SLAT TRACK, EXISTING DOUBLER REPAIR (LOWER AREA) XIS 286. AT NR 4 CUTOUT SLAT TRACK EXISTING DOUBLER REMOVED AND INSTALLED NEW IAW SRM 57-10-00 FIG 68 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01117 AND SRM 57-10-00 VOL1 FIG 68. 2 L 7 3 4F A22WE 2007071600089 20070716 00089 EU 2007 7 16 07FDEA02441 1 20070712 A 5313 SEE4A STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 749FD 536 FOUND CORROSION OUT OF LIMIT ON P 56 RT (A539-86212) BETWEEN C63-68 AND P55 RT (A539-86217) BETWEEN C65-66. SPLICE REPA IR PERFORMED IAW SRM 563-10-14 FIG 201 . 2 L 7 2 4F RT A35EU 2007092600012 20070926 00012 EU 2007 9 26 07FDEA04026 1 20070919 A 5313 A53970715202 STRINGER SPLICE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 807FD 492 CORROSION ON CONNECTING SEGMENT STRG 51 LT, BETWEEN FRAME 54.2-54.3. REPLACEMENT OF CONNECTING SEGMENT IAW SRM 51-72-10 . 2 L 7 2 4F RT A35EU 2007012400146 20070124 00146 EU 2007 1 24 2007UALA00103 1 20070115 A 2530 OVEN AIRBUS 320 A320232 3930326 EU GALLEY SMOKE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 463UA 1282 OVEN 105R11 WAS SMOKING IN FLT SHUT OFF POWER AND SMOKE STOPPED. REPLACED OVEN. OPS CHECKED GOOD. 2 L 7 2 4F RT A28NM 2007052500113 20070525 00113 2007 5 25 F3LA200700118 4 20070523 A 2565 GIRT BAR AIRBUS A318 A318111 3940019 EU R2 DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 802FR 4993 1991 DURING C-3 CHECK, INSPECTION REPORTED R2 FWD GIRT BAR FITTING AND HARDWARE CORRODED. REPLACED GIRT BAR BLANKING PLATE I AW AMM 52-13-31-400-007. 2 L 7 2 4F RT 2007101100154 20071011 00154 NM 2007 10 11 AALA20071863 1 20070921 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 AFW - EMERGENCY LIGHT BATTERY PACK M33424 AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK M3 3424 AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007080200108 20070802 00108 NM 2007 8 2 ZZDA2007225 1 20070605 A 5313 LONGERON BOEING 717 717200 1383700 NM BS 1037-1053 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CORROSION ON AFT CARGO COMPARTMENT (WASTE TANK AREA) AT LONGERON 23L END TIE FITTING. INSTALLED NEW END TIE FITTING LON GERON 23L AT AFT CARGO COMPARTMENT BETWEEN STA 1037 TO STA 1053 IAW B717 SRM 51-41-02 AND SRM 51-41-05. 2 L 7 2 4F TR A6WE 2007100200216 20071002 00216 NM 2007 10 2 KCSA071422 1 20070926 A 5320 FITTING BOEING 747 7472B4B 138481B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA 1242 STR 26L AFT FITTING DAMAGED. 2 L 7 4 4F RT A20WE 2007071100273 20070711 00273 2007 7 11 AWXA200700789 4 20070701 A 2565 D31516317 SLIDE AIRBUS A319 A319132 3930340 NM R1 DOOR FAILED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 808AW 28748 7567 1088 MCN - EES - BC-6 CHECK - LOG PAGE # 7739211 AND NR # 5980808, THE R1 DOOR SLIDE WAS DEPLOYED AND THE SLIDE FAILED TO INF LATE. REPLACED THE R1 DOOR SLIDE IAW AWA TASK CARD R1C25305. 2 L 7 2 4F RT A28NM 2007062600072 20070626 00072 NM 2007 6 26 AALA20071036 1 20070607 A 3350 FUSE BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 776AN 29582 JFK - EMERGENCY LIGHTS AT FORWARD GALLEY REAR BUFFET UNIT INOPERATIVE. REPLACED AT FUSE BATTERY PACK AT LEFT NUMBER ONE DOOR FOR EMERGENCY LIGHTS AT FORWARD GALLEY REAR BUFFET UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2007100100139 20071001 00139 EU 2007 10 1 07FDEA04239 1 20070924 A 5313 A53611673201 STRINGER SPLICE AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 719FD 388 FOUND CORROSION AT SPLICE C 19, P 52 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007030500022 20070305 00022 NM 2007 3 5 07FDEA00450 1 20070212 A 5313 AFA7105513 LONGERON SPLICE DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 AFT CARGO COMPARTMENT, RIGHT TUNNEL AREA LONGERON 38R SPLICE AT STA 1863 FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. THIS REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007071200104 20070712 00104 NM 2007 7 12 F3LA200700155 1 20070627 A 5321 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 934FR 5224 2287 DURING C-2 CHECK, INSPECTION REPORTED HOLES IN TOP SURFACE OF AFT CARGO COMPARTMENT FLOOR PANEL 161NF. REPAIRED HOLES I AW SRM 53-02-00, FIG 204. 2 L 7 2 4F RT A28NM 2007033000175 20070330 00175 EU 2007 3 30 07FDEA00933 1 20070316 A 5313 STRINGER AIRBUS 310 A310304 3930339 EU ZONE 100 CHAFED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 816FD 593 OLD CHAFING MARKS BETWEEN C44-45, P45 LT. REPAIR PERFORMED BY BLEND OUT IAW LHT SDR. 2 L 7 2 4F RT A35EU 2007010800269 20070108 00269 NM 2007 1 8 2007UALA00021 1 20070103 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE O OTHER DE DESCENT 1 WP 29 107UA 26900 EEL INOP AT 37L, ROWS 46-52 RIGHT, 4A AFT, AND 44HJK. RELAMPED EMERGENCY LIGHT, OP CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2007011800140 20070118 00140 NM 2007 1 18 2007UALA00046 1 20070105 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEATS 3E & 22C INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 EMERGENCY LIGHT INOP AT 3E AND 22C. *S/D* REPLACED AFT LIGHT ASSY AT SEAT 3E. OP CHECKS GOOD. REPLACED LIGHT BULB AT SEAT 22C. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007012900356 20070129 00356 CE 2007 1 29 DXTA200701877 1 20070125 A 3510 OXYGEN MASK CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LEFT BROKEN E DXTA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 964QS 7500164 LT SIDE O2 MASK BROKE WHILE DOING THE CLIMB CHECKS AND BEGAN LEAKING ALL THE 02. THE O2 WAS GONE BY THE TIME WE GOT BACK ON THE GROUND. RESERVICED OXYGEN IAW CE750 M.M. 12-10-45. REMOVED AND REPLACED LEFT SIDE OXYGEN MASK IAW CE750 MM 35-1 0-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007020600022 20070206 00022 NM 2007 2 6 UIEA200700046 1 20070202 A 5414 65B941004 SKIN BOEING 747 747341 13848AM NM GE CF6 CF650E2 30018 NE NR 1 NACELLE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 NR 1 PYLON PRECOOLER EXHAUST CUT-OUT CRACKED AT AFT CORNER STATION 248. THE SKIN ASSEMBLY AND WINDOW STRAPS WERE TRIMME D TO REMOVE CRACKS. NET FIT ALUMINUM FILLERS WERE INSTALLED AT ALL TRIMMED AREAS. REPAIR WAS NDT INSPECTED. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NAC STATION 235 TO 259. THE RIB INSTALLATION AT NAC S TATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW LOWER STEEL REPAIR ANGLE INSTALLATION ON THE MODIFIED STIFFENER. 2 L 7 4 4F 4 F RT A20WE E23EA 2007021300084 20070213 00084 NE 2007 2 13 DXTA200701920 2 20070208 A 7532 CONTROL UNIT GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE RT ENGINE BLEED MALFUNCTIONED E DXTA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 GL 07 712QS 073 RT BLEED AIR LEAK CAME ON IN FLIGHT, WARNING MESSAGE STAYED ON DURING ALL PROCEDURES ON EH-3 OF THE QRH. ENGINE WAS SHUT DOWN INFLIGHT. NO SMOKE OR FIRE REPORTED BY FIRE DEPARTMENT. REMOVED AND INSTALLED NEW RT BLEED AIR CONTROL UNIT IAW G- 200 MM / CH 21-61-00 AND REMOVED AND INSTALLED APU BLEED AIR CONTROL UNIT IAW G-200 M/M / CH 21-61-00. PERFORMED PTT OK AND ENG NR 2 HIGH POWER RUN-UP ON GND. INSPECTED DUCTS AND SENSING LOOPS AND NO DEFECT NOTED AT THE TIME. 2 L 7 2 4F 4 F RT A53NM E35NE 2007022100015 20070221 00015 2007 2 21 2007UALA00362 4 20070208 A 2565 SLIDE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE R2 DOOR LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 RIGHT NR 2 SERVICE DOOR SLIDE FOUND PARTIALLY UNLACED. REMOVED R-2 DOOR SLIDE AND REINSTALLED SLIDE RELEASE CABLES PER MM 25-66-00. THEN, REINSTALLED SLIDE. A/C OK FOR SERVICE. SLIDE PROBLEM ROOT CAUSE: SUSPECT VIBRATION AND OPEN/CLOSE C YCLE LOOSENED LACING. 2 L 7 2 4F 4 F RT A1NM E24NE 2007022100102 20070221 00102 NM 2007 2 21 2007UALA00416 1 20070209 A 2560 CIRCUIT BREAKER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TRIPPED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 558UA 26654 DOOR GIRT BAR C/B TRIPS AFTER DOORS ARMED. FOUND DOOR ARM LIGHT SOCKET MISALIGNED WITH RECEPTICAL HOLE BEHIND UPPER TRI M PANEL, FORCING LUGS TOGETHER AND SHORTING OUT CAUSING CIRCUIT BREAKER TO POP. STRAIGHTENED LUGS AND REALIGNED SOCKET, CB STAYS IN, BUT ARM LIGHT STAYS ON, SUSPECT SENSOR BAD (CAUSED BY SHORTED WIRES ON LIGHT ASSY) 2 L 7 2 4F 4 F RT A2NM E17NE 2007030100027 20070301 00027 NM 2007 3 1 2007UALA00514 1 20070217 A 2613 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FIRE-OVERHEAT NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 531UA 25042 FIRE-OVERHEAT TEST-ENG-APU-CARGO SYSTEM TEST FAIL. SYSTEM TEST LIGHT WILL NOT ILLUMINATE. [SUP 05-18-07] REPLACED LED AND SWITCH ASSY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007030600008 20070306 00008 EU 2007 3 6 2007UALA00597 1 20070226 A 5320 SUPPORT BRACKET AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 420UA 489 BELLY FAIRING SUPPORT BRACKET UPPER ANGLE -Y127 (LT SIDE) AT FRAME 46 IS CRACKED. MAJOR REPAIR ACCOMPLISHED: REPAIRED U PPER ANGLE PER SRM 53-35-11-FIG 229. 2 L 7 2 4F 4 F RT A28NM E40NE 2007030600020 20070306 00020 NM 2007 3 6 2007UALA00609 1 20070227 A 3397 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 588UA 26717 EMERGENCY EXIT LIGHT AT ROW 13 INOPERATIVE. [SUP 4-17-07] TROUBLESHOT AND FOUND CONNECTOR D07274 LOOSE, RECONNECTE D AND PERFORMED OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2007031200131 20070312 00131 NE 2007 3 12 TRAX200700312 2 20070302 A 7200 ENGINE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE LEFT MALFUNCTIONED A ASOA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 27 355CA 10067 AFTER ROTATION LEFT ENGINE HAD LOUD BANG AND SPOOLED DOWN TO AROUND 45 PERCENT N2 AUTO RELIGHT AND ENGINE RAN NORMALLY U NTIL LANDING -EMERGENCY DECLARED-. A/C RETURNED TO CVG AFTER T/O. FLTS 4484, 4485, 4492 CX AND FLTS 4472, 4478, 4519, 4484 CX ON 3/3/07 AND FLT 4212 CX ON 3/4/07. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007031500129 20070315 00129 NM 2007 3 15 2007UALA00652 1 20070302 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SEAT 3E MISSING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 795UA 26927 SEAT 3E AISLE SIDE MOVABLE ARM REST AFT EEL LIGHT IS MISSING. *S/D* REPLACED EEL LIGHT. OP CHECKS OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007031600029 20070316 00029 CE 2007 3 16 DXTA200702019 1 20070313 A 3040 CONTROLLER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL WINDSHIELD HEAT MALFUNCTIONED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 938QS 7500183 ENROUTE GOT WINDSHIELD HEAT INOP L CAS MESSAGE FOLLOWED BY STRONG SMOKE ODOR. REMOVED AND REPLACED LT WINDSHIELD TEMPER ATURE CONTROLLER. IAW 750MM 30-41-00. OPS. CHECK OK. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007031900056 20070319 00056 NE 2007 3 19 TRAX200700349 2 20070311 A 7200 ENGINE AEROSP ATR72 ATR72 EU PWA 120 PW120 NE LEFT FAILED A ASOA O OTHER J WARNING INDICATION DE DESCENT 1 SO 27 635AS 372 LEFT ENG FAILED IN FLT. EMERGENCY DECLARED. FLT 4628 CX. 2 H 7 2 4T 4 T RT E20NE 2007032200112 20070322 00112 NM 2007 3 22 2007UALA00777 1 20070315 A 3397 CONNECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 327UA 24147 LAST 20 INCHES OF EEL LIGHTING IN AFT MAIN CABIN IS INOP. CLEANED MOISTURE FROM AFT CONNECTION BETWEEN GALLEY EEL STRIP AND MAIN EEL. 2 L 7 2 4F 4 F RT A16WE E21EU 2007032000157 20070320 00157 NM 2007 3 20 2007UALA00732 1 20070310 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 772UA 26930 EEL LIGHT AT 34C INOP. REPLACED LIGHT ASSY, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007040300030 20070403 00030 SO 2007 4 3 GLBA20060930 1 20070328 A 2121 EVAC523C2 FAN EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RECIRCULATION WEAK A GLBA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 03 71GL 120071 PILOTS REPORTED AN ODOR OF SMOKE COMING FROM THE VENTS AFTER PARKING AT THE GATE. MAINTENANCE PLACED THE RECIRCULATION F AN ON MEL IAW 21-25-1 CATEGORY C. MAINTENANCE SUBSEQUENTLY REMOVED AND REPLACED THE LT RECIRCULATION FAN IAW MM 21-25. O PERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2007041200082 20070412 00082 EA 2007 4 12 A6WA200740181 1 20070403 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 457AW 7854 625 OBLIQUE ANGLE CRACKED IN RADIUS APPROX 1.0 INCH LONG, LT SIDE. (K) [SUP 05-09-07] MAINTENANCE REMOVED CRACKED ANG LE AND INSTALLED NEW ANGLE, P/N 601-35012-51, IAW CRJ SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007041900040 20070419 00040 NM 2007 4 19 2007UALA01068 1 20070408 A 5210 HANDLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 R-1 DOOR HANDLE BOX CRACKED AT CAM BASKET HOLES. [06-14-07] REPLACED HANDLE BOX 2 L 7 2 4F 4 F RT A2NM E17NE 2007041900045 20070419 00045 EA 2007 4 19 COMA0760316 1 20070413 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 916CA 7014 FLAPS FAIL CAUTION MESSAGE DURING TAXI IN. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE (FIRST EVENT) MAINTENANCE A CTION, PARAGRAPH (G) 1,2,3, (A,B,C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F 4 F RT A21EA E15NE 2007042400317 20070424 00317 NE 2007 4 24 DL76G070324 2 20070414 A 7230 FAN BLADE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 ENGINE BENT A DALA J A DUMP FUEL UNSCHED LANDING C F.O.D. CL CLIMB 1 SO 27 174DZ 30553 29693 704703 BIRD STRIKE ON TAKEOFF 700 FT RT ENG VIBS. INSPECT RT ENGINE PER FIM 71-05-00 FIG 124. 5 FAN BLADES. DAMAGED BEYOND LI MITS. BORESCOPE HPC OK. REPLACED FAN BLADES SET PER AMM 72-31-02-404-084-H00. REQUIRES VIBRATION SURVEY VIBRATION SUR VEY WITH IN LIMITS PER AMM 71-00-00-735-267-H02-2. 2 L 7 2 4F 4 F RT A1NM E13NE 2007050200010 20070502 00010 NE 2007 5 2 SIMA200712012 2 20070428 A 7200 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE NR 1 ENGINE MALFUNCTIONED A SIMA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 21 512AE 10110 NUMBER ONE ENGINE SPOOLED DOWN AND THEN BACK UP TO DIFFERENT POWER SETTING, NO EICAS MESSAGES. PERFORMED GENERAL ELECTR IC FAULT ISOLATION MANUAL LABEL BIT 350-20 AND ABD355-26. PERFORMED ENGINE STARTS ON BOTH CHANNEL A AND B WITH NO DEFEC TS. PERFORMED HIGH POWER RUNS FOR THREE MINUTES WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2007050300335 20070503 00335 NM 2007 5 3 2007UALA01293 1 20070424 A 3350 9F19948501 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 WALL EEL INOP: UPPER DECK LT WALL ACROSS FROM LAV 124. REPLACED EEL LITE ASSY. CHECKED OK 2 L 7 4 4F 4 F RT A20WE E24NE 2007050300375 20070503 00375 NM 2007 5 3 2007UALA01308 1 20070425 A 3350 20131A BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 UPPER DECK BATTERY LIGHT ON RIGHT DOOR INOPERATIVE. REPLACED BATTERY PACK, OP CHECKED GOOD . 2 L 7 4 4F 4 F RT A20WE E24NE 2007051500186 20070515 00186 GL 2007 5 15 001101 1 20070501 A 2497 16615001 WIRE CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO HARTZL HCJ3Y PHCJ3YF1 GL BATTERY BROKEN E J4PA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 13 301SR 430 2179 690129 FP5067B AT APPROXIMATELY 1420 AND DURING CLIMBOUT FROM KHXD TO KLRO, THE NR 1 ALT LIGHT CAME ON. TURNED THE MFD TO ENGINE PAGE WHEN SIGN FOR CHECK ALT 1 CAME ON. RETURNED TO KHXD AND LANDED WITH NO INCIDENT. ALTITUDE WAS APPROXIMATELY 2200 FEET WITH 1 PASSENGER ON BOARD AND NO EMERGENCY WAS DECLARED. AFTER LANDING FOUND THE NR 1 ALTERNATOR BATT WIRE TERMINAL LUG BROKEN OFF OF THE MOUNTING STUD TO ALTERNATOR. 1 L 7 1 3O 3 O NT A00009CH E3SO 5 C P36EA 2007051700115 20070517 00115 2007 5 17 2007UALA01450 4 20070508 A 2565 C179363 DISK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD DOOR SLIDE RUPTURED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 315UA 23947 LOW BOTTLE PRESSURE. LEAKING THROUGH RUPTURE DISK. REPLACED RUPTURE DISK. 2 L 7 2 4F 4 F RT A16WE E21EU 2007061900300 20070619 00300 NE 2007 6 19 DL76G070719 2 20070613 A 7320 CF680C2B6F ENGINE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 MALFUNCTIONED A DALA D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 SO 27 174DZ 31444 29693 704703 A/C RTB DUE TO RT ENGINE HAVING NO RESPONSE WITH THROTTLES MOVED FORWARD. THRUST REVERSER CDU HAD RECENTLY BEEN CHANGED . MTC ADJUSTED THE THRUST REVERSER SLEEVE TRANSDUCER. ENGINE OP CKS NML. 2 L 7 2 4F 4 F RT A1NM E13NE 2007062000040 20070620 00040 NM 2007 6 20 2007UALA01849 1 20070606 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EEL INOP ROW 38ABC. [06-22-07] REPLACED LAMP ASSY ALL OPS NORMAL 2 L 7 4 4F 4 F RT A20WE E24NE 2007062600211 20070626 00211 NM 2007 6 26 2007UALA02035 1 20070615 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1520 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 MAIN FRAME, STA 1520 AT STR 26L FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED -J- ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2007062800013 20070628 00013 EU 2007 6 28 2007UALA02062 1 20070616 A 3350 BR964422 LAMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 411UA 464 EMERGENCY EXIT LIGHTS AT BOTH OVERWING CENTER AISLE LOCATIONS AND LT OVERWING EXIT HAVE INOP LAMPS. RELAMPED, OPS NORMA L. 2 L 7 2 4F 4 F RT A28NM E40NE 2007061800185 20070618 00185 CE 2007 6 18 DJFA2007060 1 20070604 A 5511 45A21104011012 BRACKET BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 743TA 823 823 RK271 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE LT IB HORIZONTAL STA BILIZER, THE LT RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. BOTH BRACKETS WERE REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2007060700006 20070607 00006 CE 2007 6 7 M2L2007F00002 1 20070506 A 8011 DRIVE GEAR CESSNA 172 172N 2072434 CE LYC O360 O360A4M 41514 EA SNSNCH 76E 76EM8 EA STARTER BROKEN E M2LA O OTHER O OTHER NR NOT REPORTED 1 NM 11 737MY 778 17269533 L3335836A DURING AN ENGINE START, THE STARTER BENDIX DRIVE GEAR BROKE. THIS IN TURN LOCKED THE RING GEAR WHICH LOCKS PROP AND ENG INE. (K) 1 H 7 1 3O 3 O NT 3A12 E286 5 N P4EA 2007071000409 20070710 00409 NM 2007 7 10 2007UALA02239 1 20070623 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 EMERGENCY LIGHT STRIP AT 2A NEEDS REPAIR. SECURED LIGHT STRIP. 2 L 7 4 4F 4 F RT A20WE E24NE 2007071000413 20070710 00413 NM 2007 7 10 2007UALA02242 1 20070624 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY CEILING LIGHT INOP 54 RIGHT. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2007061900304 20070619 00304 NM 2007 6 19 2007UALA01834 1 20070605 A 2560 GIRT BAR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R2 DOOR LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 807UA 798 GIRT BAR ON 2R LOOSE. 2 L 7 2 4F 4 F RT A28NM E40NE 2007062000157 20070620 00157 NM 2007 6 20 2007UALA01972 1 20070612 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 RIGHT AFT CABIN CREASE BEAM IS CORRODED ON UPPER AND LOWER SURFACE FROM BS 947-1006 RBL 46 - RBL 53. MAJOR REPAIR ACCOM PLISHED: INSTALLED NEW CREASE BEAM AND SUPPORT ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007071100186 20070711 00186 NM 2007 7 11 2007UALA02159 1 20070621 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 PASSENGER CABIN BELOW FLOOR LEVEL BD 663 LBL 32, PRESSURE DECK UPPER SKIN CRACKED. MAJOR REPAIR ACCOMPLISHED: FABRICATE D & INSTALLED DOUBLER/FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007070300019 20070703 00019 EA 2007 7 3 A6WA200740255 1 20070515 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 458AW 7861 LT WING LOWER PLANK ACCESS HOLE NR 3 FOR PANEL 510BR HAS FRETTING/ CORROSION DAMAGE AT IB END 1 INCH LONG NOT IN CRITICA L AREA. S/D MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 3 PANEL 510BB IAW BOMBARDIER REO 601R-57-21-030 RE V A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007071100080 20070711 00080 NM 2007 7 11 DXTA200702294 1 20070624 A 2120 UNKNOWN AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE COCKPIT ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 222QS 122 INTERMITTENT BURNING ODOR FROM COCKPIT AIR ON GROUND AND DURING CLIMB. [07-12-07] INSPECTED COOLING SYSTEM. NO DEFECT S NOTED. INSPECTED APU INLET. FOUND NUMEROUS CUCADA INSECTS COVERING THE INLET SCREEN. CLEANED APU INLET. RAN COOLING SY STEM NO FURTHER ODORS NOTED. NO FURTHER DEFECTS NOTED. 2 K 7 2 4F 4 F RT A50NM E44NE 2007072000162 20070720 00162 2007 7 20 2007UALA02503 4 20070706 A 2565 LATCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE OVERWING SLIDE BINDING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 LEFT OVERWING SLIDE DOOR NR 2 LATCH BINDING. [08-08-07] REPLACED AND ADJUSTED LATCH PER MM25-65-98. DOOR 2 LATCH MOV ES FREELY. SLIDE & AIRCRAFT OK FOR SERVICE. SLIDE PROBLEM ROOT CAUSE: SLIDE LATCHES EXPERIENCE FRETTING CAUSED BY VIBRA TION & EXCESSIVE CLEARANCE CAUSED BY WEAR. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072300025 20070723 00025 NM 2007 7 23 2007UALA02544 1 20070711 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 673UA 29241 TROUBLESHOOTING FOR EMERGENCY LIGHTS, LIGHTS WILL NOT GO OUT IN ARMED POSITION, ALL LIGHTS ON IN ON. [07-27-07] REPA IRED WIRE WITH A NEW ONE. 2 L 7 2 4F 4 F RT A1NM E24NE 2007072300073 20070723 00073 NM 2007 7 23 2007UALA02582 1 20070711 A 5230 DOOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CARGO DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 117UA 28810 AFT CARGO DOOR SUSTAINED DAMAGE WHILE CLOSING DOOR. DOOR CAME IN CONTACT WITH CARGO LOADER. DAMAGE AT FWD LOWER CORNER , BEND APPROX 10 INCHES WIDE WITH APPROX 3 INCHES OUTBOARD DEFLECTION. A 1 INCH CRACK VISIBLE AT FWD VIEW PORT. [08-0 7-07] FWD LOWER CORNER OF AFT CARGO DOOR HAS 8"CRACK. WILL REQUIRE DOUBLER-TRIPLER REPAIR. REMOVED DAMAGE WHERE POSSIB LE, FABRICATED FILLER AND DOUBLER, PICKED UP EXISTING HOLES & USING BLIND FASTENERS, INSTALLED TEMPORARY REPAIR. INSTALL ATION PRIMED AND PAINTED, IAW SRM 52-30-01 REPAIR NR 2 AND UA-EVA-70416. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007073100059 20070731 00059 NM 2007 7 31 2007UALA02679 1 20070716 A 5210 TORQUE TUBE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FWD ENTRY DOOR EXCESS PLAY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 927UA 26649 FWD ENTRY DOOR UPPER LATCHING TORQUE TUBE HAS EXCESSIVE FWD AND AFT PLAY. [08-07-07] INSTALLED 2 SHIMS ON AFT SID E OF LATCH TORQUE TUBE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007073100065 20070731 00065 NM 2007 7 31 2007UALA02737 1 20070719 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 802UA 690 WHILE PERFORMING CABIN EMERGENCY LIGHTING CHECK RECEIVED MESSAGE -EPSU INT LOAD AFT-L- ON FWD ATTENDANT PANEL. RESET A FT GALLEY CEILING AREA POWER SUPPLY. TEST PASS. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071700055 20070717 00055 EA 2007 7 17 A6WA200740342 1 20070625 A 2930 TRANSDUCER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HYD PRESSURE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 462AW 7875 HYDRAULIC PRESSURE TRANSDUCER (PN 610R75262-157) CRACKED APPROX .2 INCH LONG INRT MLG WHEEL WELL CEILING. MAINTENANCE R EMOVED CRACKED HAT CHANNEL AND INSTALLED SERVICEABLE HAT CHANNEL PN 601R75262-157 IAW SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2007072000158 20070720 00158 NM 2007 7 20 2007UALA02499 1 20070707 A 3520 OXYGEN BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DEFECTIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 598UA 28751 BOTH O2 BOTTLES FROM ROW 34 USED. ONE APPEARS TO BE DEFECTIVE. [08-08-07] REPLACED DEFECTIVE 02 BOTTLE IN OVERHEAD BIN AT SEAT 34ABC. 2 L 7 2 4F 4 F RT A2NM E17NE 2007071100330 20070711 00330 NM 2007 7 11 2007UALA02187 1 20070623 A 3350 32145410 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 847UA 1627 DURING EMERGENCY LIGHT CHECK FOUND MGS ON CIDS PNL EPSU BATTERY EMERGENCY L FAILED. REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A28NM E40NE 2007071800336 20070718 00336 CE 2007 7 18 DXTA200702317 1 20070704 A 2170 7464513 COALESCER BAG CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL AFT SERVICE BAY DIRTY E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 07 998QS 5247 7500198 ON 5 MILE FINAL, STRONG BURNING ELECTRICAL SMELL IN COCKPIT, REMOVED BOTH COALESCER SOCKS P/N 746451-3 AND INSTALLED 2 NEW SOCKS P/N 746451-3. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007072400190 20070724 00190 2007 7 24 2007UALA02624 4 20070713 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR SLIDE OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 585UA 26709 DOOR 1R WILL NOT ARM. 2 L 7 2 4F 4 F RT A2NM E17NE 2007080700158 20070807 00158 2007 8 7 O2G2007F00002 4 20070628 A 3120 671848114 RELAY CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL START LOGIC FAILED E O2GA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 EA 63 610GR 7500163 ELECTRONIC FLIGHT DISPLAY NR1, NR2, AND NR3 DISPLAY RED (X). LEFT SIDE BEING POWERED BY BATTERY ONLY. LT BATTERY NOT C HARGING. REPLACED START LOGIC RELAY. (K) 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007080800082 20070808 00082 CE 2007 8 8 AMWA06002 1 20070724 A 5711 1181000131 SPAR CAP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LWS 124 CORRODED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV UE163 BIO CORROSION LT SPAR, ALT SPAR FLANGE ATTACHMENT OF THE RIB TO THE MAIN SPAR. REPAIRED IAW ENGINEERING REPORT 6799-3 R EV 1R. 2 L 7 2 4T 4 T RT A24CE E26NE 2007081000077 20070810 00077 EA 2007 8 10 A6WA200740368 1 20070706 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 461AW 7870 LT FS 621 FLOOR SUPPORT ANGLE CRACKED, 2 INCH LONG. (K) MAINTENANCE REPAIRED LEFT FLOOR SUPPORT ANGLE AT FS 621 IAW B OMBARDIER REO 601R-53-61-117. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2007080800035 20070808 00035 CE 2007 8 8 DXTA200702341 1 20070717 A 3150 UNKNOWN RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP WARNING SYSTEM UNKNOWN E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 833QS 258433 DURING THE TAKEOFF ROLL BEFORE 80 KNOTS BOTH RED MASTER WARNING LIGHTS CAME ON WITH NO OTHER ASSOCIATED LIGHTS. PERFORME D FUNCTIONAL TEST OF MASTER WARNING SYSYTEM IAW HAWKER 800XP MM. 31-50-00. FUNCTIONAL CHECKS NORMAL NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A3EU E6WE 2007082100080 20070821 00080 NM 2007 8 21 2007UALA02961 1 20070802 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EEL 3J AFT & 4A AFT ARE INOPERATIVE. REPLACED EEL LIGHT ASSYS IN BOTH POSITIONS. OP CHECKS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2007082300264 20070823 00264 NM 2007 8 23 2007UALA03060 1 20070806 A 2530 COFFEEMAKER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GALLEY SMOKE A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 526UA 24994 FOUND SMOKE IN CABIN. SMOKE IN CABIN CAUSED BY A BURNED COFFEE PACK. COFFEE PACKET WAS ON THE DUAL COFFEE WARMER IN FLIGHT AND WAS SMOLDERING. CLEANED AREA AND OPERATED WARMING PLATES FOR 30 MINUTES. EVERYTHING CHECKED NORMAL AND BAC K PLATE WAS COOL. 2 L 7 2 4F 4 F RT A2NM E17NE 2007083000004 20070830 00004 CE 2007 8 30 DXTA200702396 1 20070810 A 3243 FITTING CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MASTER CYLINDER LEAKING E DXTA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 GL 07 331QS 5600331 FIRST OFFICER, RT BRAKE SLOW TO DEVELOP PRESSURE. INSPECTED CO-PILOTS MASTER CYLINDERS & FOUND TOP FITTING LEAKING & LO OSE, TIGHTENED & CLEANED, BLED BRAKES SEVERAL TIMES FROM PILOTS & CO-PILOTS SEATS & ALL LEAK & OPERATIONAL CHECKS WERE G OOD IAW CESSNA 560 M/M 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2007082800034 20070828 00034 NM 2007 8 28 2007UALA03240 1 20070819 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SEAT 22 MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 555UA 26647 FOUND SEAT 22 EEL LIGHT MISSING. REPLACED LIGHT ASSY. OP CHECKS OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 2007082400206 20070824 00206 NM 2007 8 24 GAIA0710 1 20070726 A 2697 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE NR3 ENG PYLON SHORTED A GAIA O OTHER N FALSE WARNING DE DESCENT 1 SW 07 180AX 20041 DURING DESCENT, THE NR 3 ENGINE FIRE LIGHT FLICKERED ON AND OFF. AN UNEVENTFUL LANDING WAS MADE. INSPECTION REVEALED A SHORTED WIRE IN THE NR 3 ENGINE PYLON AT PLUG AT PLUG D4184P. THE WIRE WAS REPAIRED AND THE ENGINE AND FIRE WARNING O PS CHECKED GOOD ON THE GROUND. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 3 4F 4 F A3WE E2EA 2007090700022 20070907 00022 NE 2007 9 7 2007UALA03376 2 20070826 A 7261 OIL SYSTEM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 ENGINE LOW A UALA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 WP 29 771UA 26932 777100 NR 1 ENG SHUTDOWN DUE EICAS AT 10,000 FT FOR OIL PRESSURE AND QUANTITY ZERO. EMERGENCY DECLARED BY CREW. ENGINE REPLA CED. FOUND ONE HPT STAGE-2 BLADE FAILED UNDER THE PLATFORM DUE TO STRESS CORROSION CRACKING (SCC). AN ADJACENT BLADE W AS FRACTURED 0.100 INCHES ABOVE THE PLATFORM. THE LOSS OF BOTH BLADES RESULTED IN HEAVY VIBRATION AND OIL LOSS. THE FA ILED BLADE WAS FIRST RUN. THIS IS THE FIRST INDUSTRY HPT STAGE-2 SCC FAILURE ON A PW4077 ENGINE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2007090700035 20070907 00035 NM 2007 9 7 2007UALA03389 1 20070825 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 204 S26R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 303UA 23644 STR 26R SKIN LAP HAS BLEND AREA OF 60 PERCENT MATERIAL LOSS .875 INCH LENGTH AND .250 INCH WIDTH BETWEEN 2ND AND 3RD ROW RIVETS FROM UPPER ROW AND CENTER OF BLEND IS AT BS 204 OR 26 INCHES AFT OF STA 178 BULKHEAD. MAJOR REPAIR: ACCOMPLISHE D REPAIR PER SRM 53-10-01, DETAIL XIV. 2 L 7 2 4F 4 F RT A16WE E21EU 2007090700073 20070907 00073 NM 2007 9 7 2007UALA03185 1 20070815 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 35RH INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHT ROW 35 RIGHT INOP. *S/D* REPLACED EMERGENCY LIGHT. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007090700130 20070907 00130 NM 2007 9 7 2007UALA03430 1 20070825 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY CEILING LIGHT ABOVE ROW 16 INOPERATIVE. RELAMPED. OP CHECKS NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2007091100025 20070911 00025 NM 2007 9 11 AMTA200700402 1 20070823 A 2130 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN PRESSURE MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 11 401TZ 24663 DURING CLIMB PRESS DIFF INCREASED TO 7.0 AT 26000 FT (5000 FT CABIN) DIFF REMAINED AT 7.0 AS AIRCRAFT AND CABIN CONTINUE D TO CLIMB UNTIL AT 34,000 FT, DIFF WAS STILL 7.0 AND CABIN WAS 8500 FT, ABOVE 34,000 FT DIFF BEGAN TO INCREASE, PERFORM ED AMM 21-31-00 SYS TEST OK. PRESSURIZE AC TO 8.5 PSI AC MAINTAIN PRESS, NO LEAKS NOTED, INSPECTED ALL DOORS, WINDOWS N O LEAKS NOTED. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2007091100123 20070911 00123 2007 9 11 AMTA200700372 4 20070804 A 3442 RADAR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE WX SYSTEM MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 522AT 29330 WX RADAR RETURNS HEAVY NOISE AT ALL TILT SETTINGS. OPERATED WXR COULD NOT DUPE, BITE SHOWS NO FAULTS. REPLACED WXR RT IAW AMM 34-43-01-4. WXR CHECKS NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2007092000162 20070920 00162 2007 9 20 2007UALA03610 4 20070906 A 2565 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R3 DOOR SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 523UA 24932 THE 3R SLIDE ARMED LIGHT INOP. FOUND A FUSED LAMP. REPLACED LAMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2007092500095 20070925 00095 NE 2007 9 25 HEER117189 1 20070808 A 6320 7635109105068 OIL JET SKRSKY S76 S76A 8143006 NE TMECA ARRIEL ARRIEL2S2 60036 NE M/R GEARBOX MISMANUFACTURED B HEEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SW 03 764P A08100335 760276 MAIN GEARBOX REMOVED DUE TO METAL IN OIL AND DURING THE DETAIL INSPECTION FOUND THE OIL FEED HOLE OF THE LT INPUT OIL JE T MISDRILLED. THIS MAY HAVE CONTRIBUTED TO THE LT INPUT PINION AND BEVEL GEARS UNACCEPTABLE TOOTH PATTERN WHICH MADE IT NECESSARY TO REPLACE THE FOLLOWING PARTS. THIS MAY HAVE ALSO CONTRIBUTED TO IP BEVEL GEAR BEARING CUP FAILURE AND IN T URN CAUSED THE METAL IN THIS GEARBOX. INPUT PINION 76351-09132-102, SN C200-01142, TT 2,507.24 SCRAPPED DUE TO UNACCEPT ABLE TOOTH PATTERN; BEVEL GEAR 76351-09011-106, SN A017-00655, TT 2,507.24 SCRAPPED DUE TO UNACCEPTABLE TOOTH PATTERN; BEARING CUP SB3317-201, TT 2,507.24 SCRAPPED AND WAS CAUSE OF METAL IN OIL; BEARING CONE SB3317-101, TT 2,5 1 G 7 2 3U 4 U H1NE E00054EN 2007092000264 20070920 00264 2007 9 20 2007UALA03655 4 20070908 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L3 DOOR LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 590UA 28708 SLIDE PRESSURE 3L IN THE RED BAND. REPLACED CYLINDER. PRESSURE NOW READS IN THE GREEN BAND. 2 L 7 2 4F 4 F RT A2NM E17NE 2007091000111 20070910 00111 EU 2007 9 10 2007UALA03475 1 20070829 A 3397 WIRE HARNESS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS PINCHED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 460UA 1248 CABIN EMERGENCY LIGHTS INOPERATIVE UNDER SEAT 26C, DIM AT SEATS 15C, 16C, 17C. FOUND PINCHED WIRING HARNESS. REPAIRED WIRING HARNESS AND PUSH-BACK PIN AT SEAT 26C. 2 L 7 2 4F 4 F RT A28NM E40NE 2007092800181 20070928 00181 NM 2007 9 28 2007UALA03791 1 20070920 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BS 340-360 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 198UA 28716 EXTERNAL FUSELAGE SKIN DENTED, BS 340-360 STR 34R-37R. MAJOR REPAIR ACCOMPLISHED: INSTALLED EXTERNAL DOUBLER REPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 2007100200021 20071002 00021 NM 2007 10 2 AMTA200700426 1 20070907 A 2150 22064002 ACM BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE LT UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 318TZ 28247 LT PACK TRIPPED IN FLT RESET IAW TO CHECK LIST, PACK TRIPPED AGAIN. INSPECTED, REMOVED AND REPLACED DEFECTIVE ACM IAW AMM 21-51-04. GROUND OPS CHECK GOOD. LT PACK, OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A16WE E2GL 2007100500085 20071005 00085 NM 2007 10 5 2007UALA03829 1 20070922 A 3250 VALVE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU NLG STEERING FAULTY A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 919UA 25386 NOSE WHEEL STEERING PULLS TO THE RIGHT. REPLACED NOSE STEERING METERING VALVE. 2 L 7 2 4F 4 F RT A16WE E21EU 2007100500114 20071005 00114 EU 2007 10 5 2007UALA03970 1 20070928 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 463UA 1282 CABIN EMERGENCY LIGHT CHECK FAILED. 10-19-07 FOUND LT FWD POWER SUPPLY FAULTY. REPLACED LT FWD POWER SUPPLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2007102300132 20071023 00132 CE 2007 10 23 DXTA200702537 1 20071011 A 5100 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL VIBRATION E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 987QS 7500087 DURING THE TAKEOFF ROLL, PRIOR TO 80 KTS, WE HAD A SHIMMY, THE SHIMMY STARTED AT 30 KTS AND EVEN AFTER EASING THE CONTRO L YOKE BACK, THE SHIMMY CONTINUED. T/O WAS ABORTED. REMOVED AND INSTALLED RENTAL NOSE LANDING GEAR ASSEMBLY. ADJUSTED NOSE STEERING SYSTEM. OPS CHECKED GOOD. LEAK CHECKED GOOD. TRAVEL CHECKED GOOD. WORK DONE IAW 750 M.M. CHAPTER 32-20-00 . 2 L 7 2 4J 4 F RT T00007WI TE6CH 2007102900154 20071029 00154 EU 2007 10 29 2007UALA04254 1 20071016 A 3350 2LA00546900 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RIGHT OVERWING FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 480UA 1555 R AFT EMERGENCY EXIT DISPLAYED ON UPPER ECAM SCREEN. REPLACED RT OVERWING SLIDE ARMED LIGHT ASSY- NO REPEATS SINCE ORIGI NAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2007110100166 20071101 00166 EU 2007 11 1 COEA0711821 1 20070827 A 5310 S53575112200 CREASE BEAM AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE FUSELAGE DAMAGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 821FX 253 FOUND DURING HEAVY CHECK. FOUND TOOLING DAMAGE (5) PLACES ON CREASE BEAM, WEB. FABRICATED REPLACEMENT CREASE BEAM WEB. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2007101500230 20071015 00230 SW 2007 10 15 AC2A117606 1 20070927 A 2432 RG222 BATTERY BELL 206 206L3 1182108 SW ALLSN 250C 250C30 03013 GL MASTER DISCHARGED B AC2A K NONE O OTHER NR NOT REPORTED 1 SW 31 6533U 52439 BATTERY LOW VOLTAGE. REMOVED AND REPLACED BATTERY. 1 G 7 1 3U 3 U H2SW E1GL 2007101500231 20071015 00231 SW 2007 10 15 EGI2007F00001 1 20070813 A 6410 BLADES BELL 206 206L3 1182108 SW ALLSN 250C 250C30 03013 GL TAIL ROTOR DAMAGED E EGIA A UNSCHED LANDING D INFLIGHT SEPARATION NR NOT REPORTED 1 SW 09 85TC 51143 ABOUT 2 MINUTES PRIOR TO LANDING, A LARGE SUNSCREEN (3 FT X 4 FT) EXITED THE AIRCRAFT AND STRUCK THE TAIL ROTOR. CAUSIN G A PRONOUNCED VIBRATION IN THE TAIL ROTOR SYSTEM. THE PILOT SLOWED THE AIRCRAFT AND LANDED SAFETY ON THE RIG WITH OUT FURTHER INCIDENT. THE PILOT SHUTDOWN THE AIRCRAFT AND CONDUCTED A POST FLIGHT INVESTIGATION TO DETERMINE THE CAUSE. TH E PILOT FOUND THE SUNSCREEN WRAPPED AROUND BOTH SIDES OF THE TAIL ROTOR. THE PILOT NOTICED DAMAGE TO BOT TAIL ROTOR BLA DES, THE TAIL BOOM JUST FORWARD OF THE TALL ROTOR GEARBOX AND THE LOWER PART OF THE VERTICAL FIN INCLUDING THE TAIL STRI NGER. (K) 1 G 7 1 3U 3 U H2SW E1GL 2007110100153 20071101 00153 NM 2007 11 1 2007UALA04334 1 20071020 A 5512 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZONTAL STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 330UA 24191 RIGHT HORZ STAB REAR SPAR 56 INCHES FROM INBOARD END, STAB SKIN CRACKED. FABRICATED AND INSTALLED EXTERNAL SKIN DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2007102300319 20071023 00319 NM 2007 10 23 2007UALA04169 1 20071010 A 3397 CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN CUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 ZONE-C RIGHT EEL CABLE CUT. 11-01-07 REPLACED WITH NEW CABLE. OPS CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2007110800051 20071108 00051 NM 2007 11 8 2007UALA04453 1 20071027 A 2611 2156756 DETECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 180UA 25224 MSG SMOKE DR 5 REST CAME ON. SUSPECT FAULTY SMOKE DETECTOR. REPLACED SMOKE DETECTOR. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2007112100115 20071121 00115 NM 2007 11 21 2007UALA04631 1 20071111 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE 4R DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 DOOR 4R HANDLE BOX CRACKED AT CAM BASKET MOUNT HOLES. REPLACED HANDLE BOX. 2 L 7 2 4F 4 F RT A2NM E17NE 2007111300040 20071113 00040 NM 2007 11 13 2007UALA04551 1 20071102 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 616 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 CENTER CABIN LT OVERWING FRAME AT BS 616, FORWARD FRAME INNER CHORD HAS CRACK AT BOTTOM FASTENER. ACCOMPLISHED MAJOR RE PAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007113000198 20071130 00198 CE 2007 11 30 GUUA10110702 1 20071011 A 5540 10164001423 HINGE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RUDDER CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 16540 UE172 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LOWER RUDDER HINGE ASSEMBLY EXFOLIATED. REPLACED LOWER RUDDER HINGE ASS EMBLY. 2 L 7 2 4T 4 T RT A24CE E26NE 2007113000231 20071130 00231 WP 2007 11 30 AALA20072196 1 20071113 A 7810 TAILPIPE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LT ENGINE DEBONDED A AALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 21 591AA 53254 725763 STL INFLIGHT T531/13NOV - NUMBER ONE ENGINE HAD MULTIPLE COMPRESSOR STALLS DURING CLIMB. RETURNED TO STL AND LANDED WIT HOUT INCIDENT. DISCOVERED DISBONDED LINING IN TAIL PIPE. REPLACED NUMBER ONE ENGINE ON 14 NOV 2007 AT STL. REPLACED L EFT ENGINE ISOLATORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A6WE E9NE 2007120500068 20071205 00068 CE 2007 12 5 DXTA200702624 1 20071121 A 5610 WINDSHIELD CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE COCKPIT FAILED E DXTA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 699QS 5605199 CAPTAINS WINDSHIELD SHATTERED AT FL400 - OUTSIDE ONLY, NO PRESSURIZATION LOSS. REMOVED AND REPLACED CAPTAINS WINDSHIELD IAW MM 56-11-00 OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2007120400057 20071204 00057 CE 2007 12 4 DXTA200702561 1 20071022 A 2133 52771318 OUTFLOW VALVE CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE CABIN PRESSURE INOPERATIVE E DXTA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 07 804QS 4121 5600610 PRESSURIZATION WORKED NORMALLY UP TO FL 310 BETWEEN FL 310 AND FL 320 THE CABIN STARTED TO RAPIDLY CLIMB AT A RATE OF 55 00 FPM. THE CABIN BEFORE THE CLIMB WAS AROUND 4000 FT BEFORE THE RAPID CLIMB. THE 10000 FT ALTITUDE ANNUNCIATOR AND MA STER WARNING CAME ON AND AN EMERGENCY DESCENT WAS STARTED. THE CABIN CLIMBED TO 14000 FT. REPLACED PRIMARY OUTFLOW VALVE WITH NEW IAW MODEL 560 MM. 21-32-00. OPERATIONAL CHECK GOOD 2 L 7 2 4F 4 F RT A22CE E00053EN 2007121300082 20071213 00082 GL 2007 12 13 DL764071581 2 20071201 A 7210 CF680C2B8F FAN BLADE BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 1 ENGINE BIRD INGESTION A DALA A UNSCHED LANDING C E F.O.D. VIBRATION/BUFFET CL CLIMB 1 SO 27 839MH 11574 11574 706382 29712 706382 BIRD STRIKE DURING T/O OUT OF DKR, LT ENG VIBS WENT TO 5.0. ALL OTHER PARAMETER NORMAL. RETURNED TO DKR. MTC FOUND 5 FAN BLADES DAMAGE OUT LIMITS AND 1 OGV WITHIN LIMITS. SENDING PARTS ON FLT 34/02. WILL NEED UPDATE WHEN MTC COMPLETE M A KEY 5-0145. REMOVED AND REPLACED NR 1 ENG FAN BLADE ASSY PER M/M. PERFORM VIBE SURVEY, ALL CHKS GOOD PER M/M. P/N I NSTALLED C1-1 FAN S 6101. 2 L 7 2 4F 4 F RT A1NM E23EA 2007121900172 20071219 00172 NM 2007 12 19 2007UALA05011 1 20071207 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 S13L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 FUSELAGE SHEAR TIE CRACKED, BS 360 JUST BELOW STR 13L. MAJOR REPAIR ACCOMPLISHED: FABRICATED AND INSTALLED SHEAR TIE RE PAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122000080 20071220 00080 NM 2007 12 20 2007UALA05090 1 20071213 A 5340 654580734 ATTACH ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 291 S9R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 FUSELAGE INTERCOSTAL ATTACH ANGLE IS CRACKED, BS 291.5 BELOW STR 9R. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2007122700072 20071227 00072 NE 2007 12 27 HNAA0700291 2 20071212 A 7320 7982133007 EEC DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 1 ENGINE MALFUNCTIONED A HNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 07 329EN 26280 15368 290 123241 DURING CRUISE, THE NR 1 ENGINE TORQUE GAUGE DROPPED TO ZERO AND DIGITAL GAUGE READ DASHES FOR 2 OR 3 SECONDS ACCOMPANIED BY THE NR 1 ENGINE SURGING AND CAUTION LIGHTS ILLUMINATING. CREW WAS UNSURE WHICH CAUTION LIGHT. CREW WAS UNSURE IF T ORQUE OR NP CHANGED. AIRCRAFT DIVERTED TO BWI AND LANDED NORMALLY. ENGINE EEC WAS CHANGED BY MAINTENANCE AND AIRCRAFT WAS RUN UP AND ENGINE TRIMMED IAW MM PROCEDURES. ALL CHECKS WERE GOOD AT THIS TIME AND AIRCRAFT WAS RELEASED FOR SERVIC E. 2 H 7 2 4T 4 T RT A13NM E20NE 2007121400010 20071214 00010 NM 2007 12 14 2007UALA04926 1 20071201 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 554UA 26644 WALL MOUNTED EEL LIGHTS OUT BELOW GALLEY 1 AND GALLEY 3. 2 L 7 2 4F 4 F RT A2NM E17NE 2008010400236 20080104 00236 CE 2008 1 4 AMWA88898 1 20071203 A 3243 9038000133 MASTER CYLINDER BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA BRAKES WEAK A AMWA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 07 163YV 82 UE163 DURING TAXI INTO GATE, THE PILOT'S LT BRAKE PEDAL LOST PRESSURE. PRESSURE WAS REGAINED AFTER PUMPING PEDAL. MAINTENANCE BLED BRAKES AND CLEARED DISCREPANCY. 2 L 7 2 4T 3 T RT A24CE E2NE 2008010700072 20080107 00072 NM 2008 1 7 2007UALA05186 1 20071219 A 2560 SPRING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE PAX DOOR WEAK A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 LEFT FWD MAIN ENTRY DOOR DEPLOYMENT BAR GAS SPRING IS WEAK. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010900023 20080109 00023 NM 2008 1 9 2007UALA05238 1 20071223 A 5330 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 837UA 1474 FUSELAGE SKIN AT FRAME 64 AND FRAME 65 AND STRINGER 23L IS DAMAGED. MAJOR REPAIR ACCOMPLISHED AT DEN. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011800024 20080118 00024 2008 1 18 XXUA200700040 4 20071023 A 2565 D31041146 SLIDE BOEING 757 7572Q8 1384972 NM PWA PW2037 PW2037M 52117 NE L3 DOOR READS LOW A XXUA K NONE O OTHER IN INSP/MAINT 1 EA 15 926JS 24964 DURING DAILY CHECK, FOUND LEFT EMERGENCY DOOR SLIDE PRESSURE LOW. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012200054 20080122 00054 EA 2008 1 22 A6WA200740692 1 20071213 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BS 202 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 432AW 7257 CRACK ON FWD PRESSURE BULKHEAD AROUND PARKING BRAKE AT FS 202.00 LT LBL 23.00. CRACK ON FWD PRESSURE BULKHEAD AROUND PA RKING BRAKE REPAIRED IAW REO 601R53-11-563. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008011000186 20080110 00186 NM 2008 1 10 2007UALA05366 1 20071228 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 R2 DOOR UPPER HINGE ARM ASSY CUTOUT HAS DAMAGE. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012200160 20080122 00160 CE 2008 1 22 GUUA12180703 1 20071218 A 3610 CLAMP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE PRSOV LOOSE A GUUA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 29 81556 UE239 FLT 9280, IMMEDIATELY AFTER TAKEOFF, GOT LT ENVIRONMENTAL FAIL ANNUNCIATOR ILLUMINATED. CYCLED BLEED VALVE SWITCH AND LIGHT WENT OUT. TEN MINUTES LATER DETECTED SMOKE AND MELTING PLASTIC ODOR. CYCLED BLEED SWITCH OFF AND SMELL STOPPED. NOT NECESSARY TO USE OXYGEN MASK OR SMOKE GOGGLES. DETERMINED LT PRESSURE REGULATOR SHUTOFF VALVE (PRSOV) CLAMP TO BE L OOSE ALLOWING HOT BLEED AIR TO BLOW ONTO ADJACENT WIRE BUNDLE. INSPECTED WIRE BUNDLE AND DID NOT DETECT ANY DAMAGE. RE SECURED PRSOV CLAMP WITH A SATISFACTORY LEAK CHECK. 2 L 7 2 4T 4 T RT A24CE E26NE 2008022500077 20080225 00077 NM 2008 2 25 2007UALA03914 1 20070926 A 5751 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RT AILERON PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 RIGHT AILERON SN HDH 749 UPPER SKIN HAS PUNCTURE 5" FROM T/E. MAJOR REPAIR ACP'D, COMPLETED SKIN PANEL COMPOSITE REPAIR . 2 L 7 2 4F 4 F RT A16WE E21EU 2008041000230 20080410 00230 NM 2008 4 10 DXTA200701853 1 20070112 A 2810 102017301 FLOAT VALVE GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE LEAKING E DXTA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 07 737QS 912 127 INFLIGHT NOTICED FLUID TRAILING OFF OF THE RT AILERON. ON THE GROUND THE VISIBLE TRAIL DISAPPEARED BUT THERE IS RESIDUA L FUEL POCKET ON THE RT AILERON. REMOVED FUEL PANELS 640NT, 640MB. REMOVED FLOAT VALVE P/N D25W652004-507 S/N 214. IN STALLED NEW FLOAT VALVE P/N D25W652004-507 S/N 066. RECEIVED OK AND CLOSED FUEL PANELS 640NT, 640MB. FUELED AC TO 7000 LBS AND RAN BOTH ENGINES FOR OPS CHECK. OPS CHECKED GOOD AND NO LEAKS NOTED AT THIS TIME. ALL WORK DONE IAW MM 28-11- 05. 2 L 7 2 4F 4 F RT A53NM E35NE 2007031900081 20070319 00081 SO 2007 3 19 SIMA200706706 1 20070301 A 5315 14521413605 FLOORBEAM EMB 135 EMB135KL 3260302 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 807AE 13140 4800 145506 CENTER OMEGA BEAM FOUND CORRODED AT CENTER FUSELAGE III WING BOX AREA. PERFORMED CUT OUT OF CORROSION, FABRICATED REPAI R PARTS AND INSTALLED IAW EMB IC2007-145/1428, DATED 02-28-2007. RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4F RT T00011AT 2007050300261 20070503 00261 EU 2007 5 3 2007UALA01255 1 20070423 A 3397 BR963165 WIRE HARNESS AIRBUS 320 A320232 3930326 EU CABIN DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 433UA 589 SEAT 8C EEL LIGHT INOPERATIVE. FOUND WIRE HARNESS CONNECTOR UNDER SEAT ASSY TO HAVE WIRE PIN PULLED FROM CONNECTOR. TH ESE WIRE HARNESSES ARE EXPOSED AND CAN BE DAMAGED BY PASSENGER CARRY ON BAGGAGE UNDER SEATS. 2 L 7 2 4F RT A28NM 2007010900075 20070109 00075 NM 2007 1 9 07FDEA00029 1 20070105 A 5754 ARB2893502 DOUBLER DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 FOUND RIGHT WING, FIXED LEADING EDGE FINGER DOUBLER AT XOS= 584 CRACKED. REMOVED CRACKED FINGER DOUBLER SHIM AND FABRIC ATED NEW DOUBLER SHIM AS PER SRM 57-00-01 VOLUME I. INSTALLED NEW DOUBLER SHIM AT RIGHT HAND WING FIXED LEADING EDGE FIN GER DOUBLER SHIM AT XOS = 584 AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007101500053 20071015 00053 NM 2007 10 15 SWAA074989 1 20071005 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2007101900049 20071019 00049 WP 2007 10 19 07FDEA04564 1 20071010 A 5347 S492915012000 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 1351-1391 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 MAIN CABIN, STN 1358, RBL 46, "SEAT TRACK GOUGED," SCALLOPS ELONGATED CHECKED LIMITS: REMAINING MATERIAL IS .170, .260 M IN REQ OUT OF LIMITS IAW DC/MD-10 SRM 53-70-00 VOL I PG 21 FIG 5 SHT 1. REMOVED DAMAGED SECTION AND INSTALLED NEW SECTI ON IAW DC/MD-10 SRM 53-70-00 VOL I PG 3/4 AND DC/MD -10 SRM 51-31-01 VOL II PG 1. MAT' ID SECTION AND FABED SECTION AN D SPLICE HAT AND PLATE IAW DC/MD-10 SRM 53-70-00 VOL I PG 3 AND 4. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01 VOL I I PG 1 AND 21. 2 L 7 3 4F A22WE 2007071300165 20070713 00165 SO 2007 7 13 SWIA200718443 1 20070505 A 3097 WIRE EMB 120 EMB120ER 3260203 SO DEICE SYSTEM DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 216SW 120285 WIRES W110-0767-14 AND W110-1128-14 SHOW SIGNS OF HEAT DAMAGE AT SPLICE NEAR RIGHT DEICE CURRENT SENSOR CONNECTOR, DISCO VERED AT C-CHECK. REPLACED SPLICED WIRE SEGMENTS PER SB 120-30-0030. 2 L 7 2 4T RT A31SO 2007042500038 20070425 00038 NM 2007 4 25 QXEA200700629 1 20070416 A 6123 AUTOFEATHER SYS BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 418QX 4143 LAX FLIGHT NR 2307: AUTO FEATHER WILL NOT SELECT. AIRCRAFT RETURNED TO GATE. MAINTENANCE INTERROGATED CDS AND FOUND NR 1 AND NR 2 PROPELLER FAULTS 64. C/W Q400 FIM TASK 61-20-02-810-804. CLEARED FAULTS. GROUND RAN ENGINES AT DISC, AUTO FEATHER SELECTED NORMALLY. NO DEFECTS NOTED. FAULTS DID NOT RETURN. AUTO FEATHER TEST PASSED. NO PARTS REPLACED. A IRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007012400048 20070124 00048 EU 2007 1 24 AWXA200700102 1 20070117 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHT FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 628AW 36082 2733 67 PHX - EEL - AFT LT EMERGENCY LT CHARGER INOP, 3 RED FAULT. REMOVED AND REPLACED AFT LT EMERGENCY BATTERY CHARGER. OPS CK GOOD 2 L 7 2 4F RT A28NM 2007053100119 20070531 00119 EU 2007 5 31 F3LA200700120 1 20070526 A 3520 DOOR AIRBUS A318 A318111 3940019 EU LAV OXY MASK INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 802FR 4993 1991 DURING C-3 CHECK, INSPECTION REPORTED O2 MASK DOOR DID NOT OPEN IN LAV E DURING MANUAL MASK DROP TEST. REPLACED EMERGEN CY OXYGEN CONTAINER FOR AFT LAV IAW AMM 35-21-41-400-001 AND CHECKED GOOD. 2 L 7 2 4F RT 2007041900086 20070419 00086 NM 2007 4 19 F3LA200700077 1 20070411 A 5310 BUSHING AIRBUS A319 A319111 3930336 NM E/E BAY DOORWAY WORN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED FRETTING ON C-16 CROSSBEAM, DOOR ACCESS 812 (LT AVIONICS DOOR). REMOVED BOLT. FOUND WEAR ON THE BUSHING. CLEANED AREA IAW A319111 SRM 51-42-11, DRAWING D53913231. REASSEMBLED WITH NEW BUSHING IAW A319111 AMM 20-21-11-991-003. 2 L 7 2 4F RT A28NM 2007091800002 20070918 00002 EU 2007 9 18 07FDEA03615 1 20070912 A 5320 A21277885004 TUBE AIRBUS 310 A310324 3930206 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 812FD 467 DAMAGED (CRACKED) TUBE ASSY BETWEEN FRAME 24-25, STRG 52 RT. REPLACEMENT OF TUBE ASSY IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2007032200050 20070322 00050 EA 2007 3 22 COMA0760267 1 20070316 A 7500 CLAMP CNDAIR CL600 CL6002B19 1900309 EA RT NACELLE LOOSE A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 798CA 7348 FLIGHT 5677 - RIGHT 14TH DUCT WARNING ON CLIMBOUT. AIRCRAFT DIVERTED TO IND AND LANDED SAFELY. INSPECTED RIGHT PYLON 1 4TH STAGE DUCTS AND FOUND A LOOSE CLAMP. SECURED CLAMP, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2007050400018 20070504 00018 NM 2007 5 4 07FDEA01646 1 20070426 A 5712 RIB DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 574FE 48499 RIGHT WING LEADING EDGE PERFORMANCE FILLET OUTBOARD RIB FOUND CRACKED. [SUP 05-16-07] RIB REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007042500134 20070425 00134 NM 2007 4 25 SWAA071914 1 20070418 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 8 O'CLOCK POSITION. REPAIRED WEB PER S RM. 2 L 7 2 4F RT A16WE 2007060500116 20070605 00116 WP 2007 6 5 AALA20070946 1 20070525 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 575AM 53152 DFW - EMERGENCY EXIT SIGN LIGHTS AT FORWARD OVERWING DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN LI GHTS AT FORWARD OVERWING DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2007061900237 20070619 00237 EA 2007 6 19 TRAX200700822 1 20070613 A 5320 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 390CA 10106 FS 280 CROSSBEAM HAS MINOR SURFACE CORROSION. [06-26-07] REPAIRED IAW SRM 51-21-06, 51-25-06, AND 51-25-16. 2 L 7 2 4F RT A21EA 2007071000216 20070710 00216 NM 2007 7 10 07FDEA02319 1 20070628 A 5343 AEA70512 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 CTR LANDING GEAR, RT TRUNNION FITTING MATING SURFACE FOUND CORRODED. [07-10-07] REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-40-00 FIG. 16 VOL.I. FWD LUG - ORIGINAL THICKNESS: 2.505"; MATERIAL REMOVED: 0.040" REMAINING THICKNESS: 2.465"; MIN. ALLOWABLE THICKNESS: 2.430". AFT LUG - ORIGINAL THICKNESS: 2.4925"; MAT'L REMOVED: 0.040"; REMAINING THIC KNESS: 2.4525"; MIN.ALLOWABLE THICKNESS: 2.430". REWORK AREA REPROTECTED AS PER SRM 51-20- 00 VOL.II.REPAIR CLASSIF IED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2007012900377 20070129 00377 NM 2007 1 29 AWXA200700083 1 20070107 A 5340 146N518059 ATTACH ANGLE BOEING 757 7572G7 1384963 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 909AW 24522 MCN - MAJOR REPAIR - MAIN CABIN INTERCOSTAL UPPER ATTACH ANGLE CRACKED, BS 1420 - BS 1440, BL 0. REPLACED MAIN CABIN IN TERCOSTAL UPPER ATTACH ANGLE CRACKED, BS 1420 - BS 1440, BL 0 IAW B737-300SRM 51-40-02. 2 L 7 2 4F RT A2NM 2007073000020 20070730 00020 EU 2007 7 30 07FDEA02629 1 20070726 A 5347 1013420097075T SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 653FE 736 MDCC SEAT TRACK L5 FR 19-FR 24 18 SQ IN CORROSION INBOARD FLANGE IN AND AROUND FASTENER HOLES REF A300-600 AMM 53-13-11- 6 ZONE 230. CLEAN CORROSION IAW A300-600 SRM 51-74-10. CHECK LIMITS PER A300-600 SRM 53-10-16 OUT OF LIMITS. FAB REPA IR PART PER A300-600 SRM 53-10-16 FIG 202. ALODINE, PRIME, AND TOPCOAT PARTS PER A300-600 SRM 51-35-00 AND 51-21-10. I NSTALLED REPAIR IAW A300-600 SRM 53-10-16 FIG 202. 2 L 7 2 4F RT A35EU 2007062600030 20070626 00030 NM 2007 6 26 07FDEA02204 1 20070619 A 5315 BAC1518638 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 286FE 22623 ON AGING AC INSPECTION FOUND EXISTING REPAIR DID NOT CONFORM TO CURRENT FED EX SR27-53-034 AT BS STA 720D, LBL27"-43" FL OORBEAM. REMOVED OLD REPAIR, FABRICATED 2 NEW ANGLES, HEAT TREATED, CAD PLATED, PRIMED AND PAINTED. INSTALLED 2 NEW AN GLES AND FILLERS AT STA 720D, LBL 27"- 43" REF SRM 51-30-2, MM 51-20-151-7, AND FED EX DWG SR27-53-034F REPAIR NR 1. 2 L 7 3 4F RT A3WE 2007071000378 20070710 00378 NM 2007 7 10 DL764070839 1 20070630 A 2131 2711738813 CONTROLLER BOEING 767 767432ER 1385134 NM CABIN PRESSURE FAULTED A DALA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 27 845MH 29719 PRESSURIZATION AUTO INOP MASTER CAUTION AND AUTO INOP OVERHEAD LIGHT ILLUMINATED AFTER DEPARTURE. FOUND BOTH CABIN PRES S CONTROLLERS FAULTED DURING BITE CK. REMOVED AND REPLACED BOTH CONTROLLERS PER M/M. OPS CKS NML. A/C OK FOR SVC. 2 L 7 2 4F RT A1NM 2007071800400 20070718 00400 WP 2007 7 18 07FDEA02472 1 20070713 A 5730 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 LT WING L/E EXTERNAL SURFACE LWR SIDE ON SKIN FOUND CRACK 0.40" LONG. REPAIRED SKIN IAW SRM 57-10-00 VOL 1 FIG 68. 2 L 7 3 4F A22WE 2007100200130 20071002 00130 WP 2007 10 2 ABXA070300 1 20070831 A 5230 3914025501N FITTING DOUG DC9 DC941 302207N WP AFT CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 960AX 47762 AFT LOWER CARGO DOOR NR 2 AFT BEAM END FITTING CRACKED. REMOVED AND REPLACED AFT LOWER CARGO DOOR NR 2 AFT BEAM END FIT TING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2007012400067 20070124 00067 NM 2007 1 24 07FDEA00132 1 20070118 A 5315 FLOORBEAM BOEING 727 727233 138408A NM FUSELAGE DAMAGED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 284FE 22621 MAIN DECK FLOORBEAM UPPER TEE AND INTERCOSTAL ATTACHMENT HAS DOUBLE DRILLED/MISREPAIRED FASTENER HOLES AT BS 440, RBL 12 , WL 208. FABRICATED T CAP REPAIR BS 440 RBL 12, WL208 REF SRM 53-10-8 FIG 3 AND INTERCOSTAL ATTACHMENT REF SRM 53-10 -8 FIG 3. REMOVED DAMAGED UPPER CHORD AND INTERCOSTAL ATTACHMENT REF SRM 53-10-8 FIG 3. TREATED, PRIMED AND INSTALLED T CAP REPAIR AND INTERCOSTAL ATTACHMENT REF MM 51-20-21 PG 7, MM 51-20-31 PG 7 AND SRM 53-10-8 FIG 3 AND SRM 51-30-2 P G 2. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2007070200052 20070702 00052 NM 2007 7 2 AWXA200700770 1 20070425 A 5311 65465412 FRAME BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - CRACKED FRAME, BS 663, S3L TO S3R. REPAIRED FRAME, BS 663, S3L TO S3R IAW B737-300 SRM 53-00-07-2R 9, FIGURE 201. 2 L 7 2 4F RT A16WE 2007041300043 20070413 00043 NM 2007 4 13 F3LA200700053 1 20070331 A 5312 BEAM AIRBUS A319 A319111 3930336 NM BULKHEAD BENT A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 906FR 4708 1684 DURING C4/S1 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FWD BULKHEAD BEAM RT OF CENTER BENT. REPLACED BULKHEAD BE AM IAW A319 SRM 51-42-11, PARA. 5, PG 6-7 AND PARA 6, PG 22-23, AND SRM 51-44-21. 2 L 7 2 4F RT A28NM